c5 c10 c12 c14 c15 c16 c17 c18 c20 c25 c35 c40 c90 c100 c110 c120 c130 c140 c150 c152 c160 c170 c180 c190 c192 c200 c210 c220 c230 c240 c250 c260 c270 c280 c290 c300 c310a c310b c310c c310d c314a c314b c314c c314d c320a c320b c320c c324a c324b c324c c330 c332 c340 c350 c360 c370 c380 c390 c400 c410 c420 c430 c440 c450 c460 c490 c510a c510b c510c c510d c510e c510f c602 c604 c606 c608 c610 c612 c614 c616 c620 c640 c652 c654 c660 eof 2003033100081 20030331 00081 EU 2003 3 31 BMAC010001 1 20011205 A 3200 622800200 DOWNLOCK SWITCH BAG JETSTM JETSTM3101 1500215 EU MLG MALFUNCTIONED A B16A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 05 529PA 771 LANDING GEAR INTRANSIT LIGHT STAYED ON LT. COULD NOT DUPLICATE. PRECAUTIONARY REPLACEMENT OF UPLOCK AND DOWNLOCK SWITC HES PER SB32-891142, PERFORMED ON LEFT MAIN GEAR. (M) 2 L 7 2 4T RT A21EU 2003041600086 20030416 00086 WP 2003 4 16 AALA20021761 1 20010425 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 453AA 49558 TUL - FOUND CABIN FLOOR BEAM IS GOUGED STATION 389. BLENDED AREA PER SRM 51-10-3, BEYOND LIMITS. REPAIRED PER AARD 53- 20-00-21. (M) 2 L 7 2 4F A6WE 2003050500048 20030505 00048 EA 2003 5 5 A6WA200340043 1 20010622 A 2420 761341 GCU CNDAIR CL600 CL6002B19 1900309 EA ADG INOPERATIVE A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 406AW 2933 7402 COMPLY WITH ADG INFLIGHT DEPLOYMENT IAW TASK 024/24/220/701. ADG FUNCTIONAL CHECK FAILED. REMOVED AND REPLACED GCU, S/ N 0290. FLIGHT OPERATIONAL TEST OF ADG AUTO DEPLOYMENT SUCCESSFUL. GCU COMPONENT REPAIR SHOP TEAR-DOWN FINDINGS, NO FA ULT FOUND (NFF). 2 L 7 2 4F RT A21EA 2003050500228 20030505 00228 NM 2003 5 5 S01227042 1 20011222 A 5753 STRUCTURE BOEING BOEING 747 747209B NM PWA JT9 JT9D7R4G2 52054 NE TE FLAP CORRODED W SAJF O OTHER O OTHER LD LANDING 1 WP 03 87500 22299 I/B FLAPS FAILED TO EXTEND BEYOND 10 UNIT. ALT EXTENSION FAILED. GRD CK FOUND RT I/B FORE & MID FLAP DAMAGE & NR 5 MAI N CARRIAGE SPINDLE BROKEN. REPLACED RT I/B FORE/MID FLAP. REPLACED NR 5 MAIN CARRIAGE. PERFORM I/B FLAP ADJ/TEST. RE PLACED DFDR. NR 6 CARRIAGE REMOVED & FOUND CORROSION PITTING. CARRIAGES REPLACED. FRACTURED CARRIAGE SENT TO BOEING. FRACTURE INITIATED FROM CORROSION PITTING OD SURFACE & PROPAGATED. PRESENCE OF HIGH CONCENTRACTION OF CHLORINE ELEMENT FOUND ON FRACTURE SURFACE MIGHT HAVE CONTRIBUTED TO STRESS CORROSION CRACKING. ALL OVERHAUL PROCEDURES & SHOP WORKSHEE TS REVIEWED & REVISED TO COMPLY W/OHM. T/E FLAP CARRIAGE MUST BE REPEAT OVERHAULED NOT TO EXCEED 30000 FH OR 8 YRS. 2 L 7 4 4F 4 F RT A20WE E3NE 2003050700118 20030507 00118 EA 2003 5 7 CA030417008 1 20010919 A 5741 BUSHING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE WING ATTACHMENT LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) MIGRATING BUSHINGS ON WING ATTACHMENT FITTINGS. 2 L 7 2 4F 4 F RT A21EA E15NE 2003053000056 20030530 00056 NM 2003 5 30 2003F00333 1 20011227 A 5753 65413175 FLAP TRACK BOEING 727 72721 1384003 NM TE FLAPS CRACKED A XP0B O OTHER O OTHER NR NOT REPORTED 1 SO 35 727PX 19261 LEFT WING TRAILING EDGE INBOARD FLAP UPPER ROLLER BEARING TRACK ON FUSELAGE IS CRACKED IN SEVERAL PLACES AT WBL 70.5. R EMOVED AND REPLACED ROLLER BEARING TRACK. (M) 2 L 7 3 4F A3WE 2003053000058 20030530 00058 NM 2003 5 30 2003F00335 1 20011229 A 5711 65162003 SPAR BOEING 727 72721 1384003 NM LEFT WING CORRODED A XP0B O OTHER O OTHER NR NOT REPORTED 1 SO 35 727PX 34220 19261 LEFT WING FRONT SPAR UPPER CAP, LOWER LEG, HAS CORROSION AT WS 222.0 AND 224.5. CORROSION FOUND OUT OF LIMITS. REPAIRE D SPAR PER DRAWING RFB275710-122601. (M) 2 L 7 3 4F A3WE 2003053000057 20030530 00057 NM 2003 5 30 2003F00334 1 20011228 A 5753 6521630173 SKIN BOEING 727 72721 1384003 NM TE FLAP DELAMINATED A XP0B O OTHER O OTHER NR NOT REPORTED 1 SO 35 727PX 19261 LEFT INBOARD FORE FLAP DELAMINATED AT TRAILING EDGE JUST ABOVE MIDDLE TRACK. REMOVED FLAP, REPAIRED IAW B727 MM 27-51-1 1. REINSTALLED FLAP. (M) 2 L 7 3 4F A3WE 2003053000059 20030530 00059 NM 2003 5 30 2003F00336 1 20011220 A 5753 652919510 FLAP TRACK BOEING 727 72721 1384003 NM LT WING CRACKED A XP0B O OTHER O OTHER NR NOT REPORTED 1 SO 35 727PX 34220 19261 LEFT WING NR 4 FLAP TRACK FAIRING OUTBOARD TRACK, BEARING GUIDE, CRACKED. REMOVED AND REPLACED TRACK IAW B727 SRM 51-10 -01. (M) 2 L 7 3 4F A3WE 2003053000104 20030530 00104 EA 2003 5 30 CA030416004 1 20011101 A 2742 C3CF2907 ACTUATOR DHAV DHC3 DHC3 2800202 EA PWA PT6 PT6A135 52043 NE HARTZL HCB3T HCB3TN3 GL HOROZONTAL STAB FAILED W O OTHER F FLT CONT AFFECTED CL CLIMB 1 CA (CAN) FROM TSB A01A0112, FOLLOWING TAKE OFF OF A FLOAT EQUIPPED DHC 3T, THE CONTROL COLUMN PITCHED VIOLENTLY FORWARD AND BACK BEFORE RETURNING TO A NEUTRAL POSITION. THE AIRCRAFT THEN PITCHED DOWN AND CONTACTED THE WATER IN A NOSE DOWN, WIN GS LEVEL ATTITUDE. THE AIRCRAFT SUSTAINED SUBSTANTIAL DAMAGE AND SANK. THE OCCUPANTS ESCAPED WITHOUT SERIOUS INJURY. I NVESTIGATION REVEALED THE CABLE-OPERATED JACKSCREW JAMMED DUE TO INTERNAL CORROSION OF THE JACKSCREW. ONCE JAMMED, THE R IVET SECURING THE FORK END TO THE ACTUATOR SHEARED RESULTING IN A FREE FLOATING HORIZONTAL STABILIZER. 1 H 7 1 3R 4 T A815 E4EA 6 C P15EA 2003053000064 20030530 00064 NM 2003 5 30 2003F00339 1 20011229 A 5753 65413176 FLAP TRACK BOEING 727 72721 1384003 NM RT WING CRACKED A XP0B O OTHER O OTHER NR NOT REPORTED 1 SO 35 727PX 19261 RIGHT WING TRAILING EDGE INBOARD FLAP UPPER ROLLER BEARING TRACK ON FUSELGE IS CRACKED AT WBL 70.597. REMOVED AND REPLAC ED RIGHT WING TRAILING EDGE INBOARD FLAP UPPER ROLLER BEARING TRACK. (M) 2 L 7 3 4F A3WE 2001011104482 20010111 04482 WP 2001 1 11 TWAA0100101 1 20010101 A 3350 MISC0639 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 983Z 47411 THE LEFT NACELLE LIGHT WAS INOPERATIVE ON THE EMERGENCY LIGHT CHECK. REPLACED THE LEFT OVERWING EMERGENCY BATTERY PACK. CHECK-C 12-14-99. 2 L 7 2 4F A6WE 2001011102841 20010111 02841 NM 2001 1 11 DLM88010002 1 20010101 A 5200 DOOR DOUG MD88 MD88 3023688 NM LEFT FUSELAGE LOOSE A DALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 27 983DL 53247 AFTER TAKEOFF PASSING 15000. FELT AND HEARD BANG. PAX IN ROW 10 ABC FELT VIBRATION IN SEATS AND FLOOR. SLOWED A/C VIB WE NT AWAY. INCREASED SPEED VIB RETURNED - REPLACED GROUND A/C DOOR ON LEFT SIDE OF AIRCRAFT AT ROW 13 FOR WEAR 2 L 7 2 4F RT A6WE 2001011102901 20010111 02901 NM 2001 1 11 DL72W010003 1 20010101 A 3610 BACC10DU350ABE CLAMP BOEING 727 727247 138408F NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE STRETCHED A DALA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 2820W 21058 700535 AT 60 KTS ON T/O ROLL, LEFT STRUT PNEUMATIC DUCT PRESSURE WENT TO 6 O'CLOCK POSITION. ON CLIMBOUT, NR 1 ENG STRUT OVERHE AT LIGHT ILLUMINATED. NR 1 ENGINE THROTTLE BROUGHT TO IDLE. LIGHT EXTINGUISHED. FOUND WORN DUCT CLAMP ON ENG BLEED SUPP LY DUCT. REPLACED SAME. RAN ENG. STRUT OVERHEAT STAYED OUT 2 L 7 3 4F 4 F A3WE E2EA 2001011104530 20010111 04530 NM 2001 1 11 UPS01234577 1 20010101 A 3350 BULB BOEING 727 72725C 138400H NM COCKPIT MALFUNCTIONED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 931UP 19858 INSPECTION TYPE:N/A COCKPIT DOOR EMERGENCY EXIT LIGHT HAS ONE DIM BULB RELAMPED EMER. LIGHT OVER FLIGHT DECK ENTRY D OOR, OPS CHECK GOOD 2 L 7 3 4F A3WE 2001011601212 20010116 01212 NM 2001 1 16 AWXA0001165 1 20010102 A 2131 7638102 CONTROLLER BOEING 737 7373G7 1384595 NM CABIN PRESSURE FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 308AW 36234 3490 24710 *S/D* PDX - AIR TURNBACK - AUTO PRESSURIZATION PREVIOUSLY PLACED ON MEL 21-14 (12/28/2000); AFTER TAKEOFF FROM PDX, STA NDBY PRESSURIZATION FAILED AND CREW WAS UNABLE TO CONTROL CABIN PRESSURE IN NORMAL MODE; THE AIRCRAFT RETURNED TO PDX. IN PDX PRESSURIZATION INTEGRITY CHECK WAS PERFORMED PER AWA TASK CARD F1B21006 AND NO FAULTS NOTED; THE CABIN PRESSURE C ONTROLLER WAS REPLACED AND FUNCTIONAL CHECKS WERE GOOD; MEL 21-14 WAS CLEARED AND THE AIRCRAFT WAS RETURNED TO SERVICE, NO FURTHER FAULTS HAVE BEEN REPORTED AS OF 1/12/01. 2 L 7 2 4F RT A16WE 2001011102307 20010111 02307 NM 2001 1 11 AWXA0001166 1 20010102 A 5330 6545765 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 UPPER EXTERNAL FUSELAGE STA 230 LBL 7 - LBL 9 LIGHTNING STATIC DMG WENT OUT OF LIMITS. CUTOUT DMG; FABED FILLERS & DOUBL ERS; INSTALLED REPAIR PARTS IAW SRM 53-00-01 FIG 201. 2 L 7 2 4F RT A16WE 2001011100578 20010111 00578 NM 2001 1 11 AWXA0001167 1 20010102 A 3397 BMS13131122 WIRE BOEING 737 7373G7 1384595 NM SEAT 2B BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 160AW 23782 EMERGENCY ESCAPE PATH LIGHT AT SEAT 2B INOP. REPAIRED BROKEN WIRE; LIGHT OPS CHECKS GOOD 2 L 7 2 4F RT A16WE 2001011100579 20010111 00579 NM 2001 1 11 AWXA0001168 1 20010102 A 3397 BMS13131122 WIRE BOEING 737 73733A 1384673 NM SEAT 2B BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 169AW 23630 EMERGENCY ESCAPE PATH LIGHT AT SEAT 2B FAILED TO ILLUMINATE DURING TEST. FOUND BROKEN WIRE AT SEAT 2B; SPLICED THE WIRE AND LIGHT OPS CHECKED GOOD 2 L 7 2 4F RT A16WE 2001011102308 20010111 02308 NM 2001 1 11 AWXA0001169 1 20010102 A 3350 1012721 LIGHT BOEING 737 7373G7 1384595 NM SEAT 3C INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 302AW 24009 EMERGENCY ESCAPE PATH LIGHT INOP @ SEAT 3C. REPLACED LIGHT ASSY 2 L 7 2 4F RT A16WE 2001011102309 20010111 02309 EU 2001 1 11 AWXA0001170 1 20010102 A 3350 321452 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 631AW 30343 25917 077 EXIT SIGNS OVER DOOR 1L & 1R AND FIRST CLASS OVERHEAD DO NOT ILLUMINATE WHEN NO SMOKING SIGN IS OFF. REMOVED AND REPLACE D POWER SUPPLY IAW AMM 33-51-38; OPS CHECKED GOOD 2 L 7 2 4F RT A28NM 2001011102310 20010111 02310 NM 2001 1 11 AWXA0001171 1 20010102 A 3350 20121 CHARGER BOEING 737 737375 13844BN NM CABIN FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 336AW 23707 EMERGENCY LIGHTS INOP ROW 13-18. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY CHARGER ASSY; LIGHTS OPS CHECKED GOOD. 2 L 7 2 4F RT A16WE 2001011100580 20010111 00580 NM 2001 1 11 AWXA0001172 1 20010102 A 3397 BMS13131122 WIRE BOEING 737 73733A 1384673 NM SEAT 3C CHAFED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 174AW 23633 EMERGENCY LIGHTING INOP ROWS 3-7. REPAIRED WIRING AT SEAT 3C 2 L 7 2 4F RT A16WE 2001011102328 20010111 02328 NM 2001 1 11 AWXA0001173 1 20010102 A 3350 20121 CHARGER BOEING 737 737301 1384611 NM CABIN FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 326AW 23258 RIGHT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER; LIGHT CHECKS GOOD 2 L 7 2 4F RT A16WE 2001011106137 20010111 06137 NM 2001 1 11 PCAA0101001 1 20010101 A 5610 07802 WINDSHIELD DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 831EX 10554 160 LGA-ALB FLIGHT 3551. LEFT WINDSCREEN SHATTERED IN FLIGHT. AIRCRAFT LANDED IN ALB. MAINTENANCE REPLACED CAPTAINS WINDSHIE LD AND 15 NUTPLATES ALONG BOTTOM OF WINDOW SILL IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL 56-10-11, RAN A IRCRAFT, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001011100901 20010111 00901 WP 2001 1 11 01FDEA00001 1 20010103 A 7830 TRANSMITTER DOUG DC10 DC1010F 3022111 WP NR 2 ENGINE T/R FAILED A FDEA O OTHER J WARNING INDICATION LD LANDING 1 SO 25 053FE 47807 NR 2 ENGINE THRUST REVERSER FAILED TO CLOSE AFTER LANDING, REVERSER UNLOCK & REVERSER 2 VALVE OPEN CAUTION LIGHTS ILLUMI NATED. C/W RED TABS PROC. ** S/D ** R&R THRUST REVERSER. SYS CK GOOD. 2 L 7 3 4F A22WE 2001011104174 20010111 04174 NM 2001 1 11 F3LA200100001 1 20010101 A 2133 2888 GASKET BOEING 737 7373Q8 1384670 NM OUTFLOW VALVE INOPERATIVE A F3LA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 318FL 709 26301 AIR TURN BACK. FLIGHT CREW REPORTED AUTO PRESSURIZATION INOPERATIVE. RETURNED TO ATL WITHOUT INCIDENT. REPLACED OUTFL OW VALVE HEATER GASKET AND CHECKED OKAY. 2 L 7 2 4F RT A16WE 2001011104534 20010111 04534 NM 2001 1 11 UPS01234584 1 20010102 A 3350 BATTERY BOEING 727 727247 138408F NM COCKPIT FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT ABOVE ENTRY DOOR INOP R&R BATTERIES ON EMERGENCY LIGHT. SYS OP CKS GOOD 2 L 7 3 4F A3WE 2001011101433 20010111 01433 EU 2001 1 11 QXEA0100001 1 20010101 A 3350 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 491US 11156 GEG - THE FORWARD CENTER ISLE EXIT SIGN WAS FOUND INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001011105128 20010111 05128 2001 1 11 GLBA9191 4 20010102 A 3416 066030620008 ALTIMETER BEECH 1900 1900D 1154162 CE COCKPIT INOPERATIVE A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 179GL 2312 UE179 RETURN TO BLOCK - #1 ALTIMETER FLAGGED ON CLIMB OUT, R/R ALTIMETER OPS CHECKED SYSTEM GOOD 2 L 7 2 4T RT A24CE 2001011100618 20010111 00618 NM 2001 1 11 SCNA01001 1 20010101 A 3397 WIRE BOEING 727 7272J4 1384006 NM CABIN BROKEN A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 288SC 20765 THE OVERHEAD EMERGENCY LIGHT AT SEAT 24 STAYED ON AFTER THE POWERR IS WAS REMOVED AND THE SWITHC WAS TURNED OFF. REPAIR ED BROKEN DISARM WIRE ON OVERHEAD EMERGENCY LIGHT AT SEAT 24, OPERATIONAL CHECKS GOOD. 2 L 7 3 4F RT A3WE 2001011102094 20010111 02094 EU 2001 1 11 RAIA0012060 1 20010102 A 2435 8260121 STARTER GEN AEROSP ATR72 ATR72202 8680940 EU NR 1 ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER CL CLIMB 1 CE 03 721TE 1673 528 217 7158-STL-DURING CLIMB #1 DC GENERATOR FELL OF LINE AND WOULD NOT RESEST. MAINTENANCE REMOVED AND REPLACED #1 STARTER GEN ERATOR IAW J41 MAINTENANCE MANUAL. 2 H 7 2 4T RT A53EU 2001011102095 20010111 02095 EU 2001 1 11 RAIA0012061 1 20010102 A 3240 S2728117820000 SPRING AEROSP ATR42 ATR42300 8680920 EU BRAKE SYSTEM FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 421TE 102 7330-STL-LEFT HAND BRAKE GRABS FULL LOCKED WHEN PEDAL IS BARELY PUSHED IN WITH HYDRAULICS OFF. THE LEFT PEDAL GOES DOWN VERY EASILY AS IF NO SPRING TENSION. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS LEFT HAND PEDAL ARTIFITIAL FEEL SPRIN G IAW ATR42 MAINTENANCE MANUAL. 2 H 7 2 4T RT A53EU 2001011102487 20010111 02487 EU 2001 1 11 DHL2001364007 1 20010104 A 2611 WARNING SYSTEM AIRBUS 300 A300B4203 3930306 EU SMOKE DETECTION MALFUNCTIONED A DHLA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 364DH IN FLIGHT THE MAIN BAY SMOKE LIGHT ILLUMINATED WITH THE MWP SMOKE LIGHT AND CHIME. LIGHT BECAME INTERMITTENT AND EXTINGU ISHED PRIOR TO INITIATING EMERGENCY CHECKLIST. LIGHT REMAINED EXTINGUISHED AND ALL INDICATIONS WERE NORMAL. DIVERTED TO DEN FOR SAFETY REASONS. PERFORMED VISUAL INSPECTION OF MAIN BAY AND FOUND NO INDICATION OF SMOKE OR DAMAGE. PERFORMED OPERATIONAL CHECK OF ELECTRONIC SMOKE DETECTION SYSTEM PER M/M REF 26-11-00 AND SYSTEM OPS CHECKS GOOD OK TO CONTINUE. 2 L 7 2 4F RT A35EU 2001011102491 20010111 02491 NM 2001 1 11 DHL2001715001 1 20010103 A 2611 BULB BOEING 727 727155C 138404Z NM SMOKE DETECTOR BURNED OUT A DHLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 715DH 19618 UPPER MAIN CARGO SMOKE DETECTORS NOT VISIBLE. RELAMPED UPPER SMOKE DETECTOR. OPS CHECK GOOD I.A.W 26-17-01 2 L 7 3 4F A3WE 2001011102145 20010111 02145 WP 2001 1 11 DHL2001805001 1 20010103 A 2760 CURRENT LIMITER DOUG DC8 DC873F 302199F WP SPOILERS FAILED A DHLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 805DH 46125 ON TAXI OUT NOTED NO SPOILER PRESSURE. RAN ABNORMAL PROCEDURES STILL NO SPOILER PRESS. REPLACED ALL THREE CURRENT LIMIT ERS OPS CHECKS GOOD I.A.W. 27-00-00 2 L 7 4 4F RT 4A25 2001011103737 20010111 03737 WP 2001 1 11 ERKR200000010 1 20010104 A 5230 99211662 FITTING DOUG DC9 DC933F 302207A WP CARGO DOOR CRACKED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 MAIN CARGO DOOR AT STA 389 LOWER CLOSE OUT WEB ( INTERIOR DOOR ) BETWEEN LONGERON 16L AND 17L FRAME CRACKED. 2 L 7 2 4F A6WE 2001011103739 20010111 03739 WP 2001 1 11 ERKR200100011 1 20010104 A 5230 99211662 FITTING DOUG DC9 DC933F 302207A WP CARGO DOOR CRACKED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 CRACK ON MAIN CARGO DOOR LOWER FITTING AT STA.409.062 2 L 7 2 4F A6WE 2001011103738 20010111 03738 WP 2001 1 11 ERKR200100010 1 20010104 A 5230 99211662 WEB DOUG DC9 DC933F 302207A WP FITTING CRACKED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 MAIN CARGO DOOR AT STA 389 LOWER CLOSE OUT WEB ( INTERIOR DOOR ) BETWEEN LONGERON 16L AND 17L FRAME CRACKED. 2 L 7 2 4F A6WE 2001011103740 20010111 03740 WP 2001 1 11 ERKR200100012 1 20010104 A 5230 99211661 FITTING DOUG DC9 DC933F 302207A WP CARGO DOOR CRACKED B ERKR O OTHER O OTHER IN INSP/MAINT 1 WP 07 933F 47191 CRACK ON MAIN CARGO DOOR LOWER FITTING AT STATION 413.062 2 L 7 2 4F A6WE 2001011104438 20010111 04438 WP 2001 1 11 ERKR200100013 1 20010104 A 5230 NPN FITTING DOUG DC9 DC933F 302207A WP 428.062 CRACKED B ERKR O OTHER O OTHER IN INSP/MAINT 1 WP 07 933F 47191 crack on main cargo door lower fitting at station 428.062 2 L 7 2 4F A6WE 2001011102330 20010111 02330 NM 2001 1 11 AWXA0001176 1 20010103 A 5313 65528941 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 25070 23776 INTERCOSTAL UPPER FLANGE CRACKED AT SCREW HOLE BS 540 LBL 2. REMOVED AND REPLACED DAMAGED INTERCOSTAL IAW SRM 51-40-02 2 L 7 2 4F RT A16WE 2001011102331 20010111 02331 NM 2001 1 11 AWXA0001177 1 20010103 A 5347 6546815 SEAT TRACK BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 CABIN SEAT TRACK CRACKED AT RBL 45 & FS 727B. REMOVED GUSSET IAW SRM 51-40-02; FABED REPAIR PLATE AND SHIM IAW 51-70-13 FIG 1; INSTALLED REPAIR PLATE AND SHIM IAW 51-70-13; INSTALLED GUSSET IAW 51-40-02. 2 L 7 2 4F RT A16WE 2001011102332 20010111 02332 NM 2001 1 11 AWXA0001178 1 20010103 A 5347 6546815 SEAT TRACK BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER UK UNKNOWN 1 WP 28 154AW 23776 SEAT TRACK CRACKED AT RBL 25 & FS 727B. REMOVED GUSSET IAW SRM 51-40-02; FABED ABD INSTALLED REPAIR PLATE AND SHIM IAW 5 1-70-13; REINSTALLED GUSSET IAW 51-40-02 2 L 7 2 4F RT A16WE 2001011102333 20010111 02333 NM 2001 1 11 AWXA0001179 1 20010103 A 5320 6720381 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 25070 23776 FS 178 LT INTERCOSTAL CRACKED WL 195 LBL 24. REMOVED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL IAW SRM 51-40-02 2 L 7 2 4F RT A16WE 2001011102334 20010111 02334 NM 2001 1 11 AWXA0001180 1 20010103 A 5312 651630086 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 25070 23776 SIDE CHORD CRACKED FS 178 WL 207 LBL 26 (1.3L). REMOVED DAMAGED SECTION OF CHORD; INSTALLED NEW SECTION OF CHORD, SPLICE ANGLE, AND SPLICE PLATE IAW E.R. 03-5311-00342-JS2 2 L 7 2 4F RT A16WE 2001011102335 20010111 02335 NM 2001 1 11 AWXA0001181 1 20010103 A 5210 6545871 SKIN BOEING 737 7373G7 1384595 NM PAX DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 25070 23776 R1 DOOR SKIN CRACKED AT UPPER HINGE CUT OUT. CUT OUT DAMAGE AND REPAIRED IAW SB 737-52-1096 FIG 6 DETAIL 1, AWA EO 52-00 -02, AND SRM 51-40-02 2 L 7 2 4F RT A16WE 2001011103741 20010111 03741 WP 2001 1 11 ERKR200100014 1 20010104 A 5220 59101597 DOUBLER DOUG DC9 DC933F 302207A WP EMERGENCY EXIT CRACKED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 FABRICATION OF A DOUBLER TO BE INSTALLED AT THE EMERGENCY EXIT DOOR AT STATION 669.0 COMMON TO THE INNER SKIN TO REPAIR A CRACK IN THE FORWARD LOWER CORNER. REPAIRED PER ECRA 933-52-054-2 REV. B 2 L 7 2 4F A6WE 2001011102187 20010111 02187 EU 2001 1 11 RAIA0101001 1 20010102 A 2435 8260121 STARTER GEN AEROSP ATR72 ATR72202 8680940 EU NR 1 ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER CL CLIMB 1 CE 03 721TE 1673 528 217 7158-STL-DURING CLIMB #1 DC GENERATOR FELL OF LINE AND WOULD NOT RESET. MAINTENANCE REMOVED AND REPLACED #1 STARTER GENE RATOR IAW J41 MAINTENANCE MANUAL. 2 H 7 2 4T RT A53EU 2001011102188 20010111 02188 EU 2001 1 11 RAIA0101002 1 20010102 A 3240 S2728117820000 SPRING AEROSP ATR42 ATR42300 8680920 EU BRAKE SYSTEM DAMAGED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 421TE 102 7330-STL-LEFT HAND BRAKE GRABS FULL LOCKED WHEN PEDAL IS BARELY PUSHED IN WITH HYDRAULICS OFF. THE LEFT PEDAL GOES DOWN VERY EASILY AS IF NO SPRING TENSION. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS LEFT HAND PEDAL ARTIFITIAL FEEL SPRIN G IAW ATR42 MAINTENANCE MANUAL. 2 H 7 2 4T RT A53EU 2001011102337 20010111 02337 NM 2001 1 11 AWXA0001184 1 20010103 A 5512 6554821 SKIN BOEING 737 7373G7 1384595 NM HORIZONTAL STAB DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 25070 23776 LT HORIZ STABILIZER L.E. SKIN DENTED OUT OF LIMITS AT LES 24.0.: REMOVED, FABED REPLACEMENT, AND INSTALLED REPLACEMENT L E SKIN IAW BOEING DWG 65-54821 AND SRM 51-40-02 2 L 7 2 4F RT A16WE 2001011102338 20010111 02338 NM 2001 1 11 AWXA0001185 1 20010103 A 5321 65458336 WEB BOEING 737 7373G7 1384595 NM CABIN FLOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 25070 23776 FLOOR WEB CRACKED FS 180 WL 207 LBL 26. REMOVED FLOOR WEB IAW SRM 51-40-02; FABED REPLACEMENT PART IAW DWG 65-45833; INS TALLED REPLACEMENT PART IAW 51-40-02. 2 L 7 2 4F RT A16WE 2001011102341 20010111 02341 NM 2001 1 11 AWXA0001187 1 20010103 A 5312 65163006 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 25070 23776 CENTER WEB CRACKED FS 178 LBL 5.0 WL 198 (1.0L) AND WL 202 (1.0L). REMOVED DAMAGED AREA OF WEB; NDT VERIFIED NO CRACKS; FABED REPAIR PARTS AND INSTALLED IAW SRM 53-10-08 FIG 209 AT FS 178 LBL 5.0 WL 200. 2 L 7 2 4F RT A16WE 2001011102342 20010111 02342 NM 2001 1 11 AWXA0001188 1 20010103 A 5312 65163006 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 25070 23776 CENTER WEB CRACKED FS 178 RBL 5.0 WL 198 (1.0L) AND WL 202 (1.0L). REMOVED DAMAGED AREA OF WEB; NDT VERIFIED NO CRACKS; FABED REPAIR PARTS AND INSTALLED PARTS IAW SRM 53-10-08 FIG 209 AT FS 178 RBL 5.0 WL 200 2 L 7 2 4F RT A16WE 2001011102343 20010111 02343 NM 2001 1 11 AWXA0001189 1 20010103 A 5312 65163006 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 25070 23776 CENTER WEB CRACKED FS 178 LBL 0.7 WL 187. CUT OUT DAMAGE; FABED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW SRM 53-10-08 FIG 203 2 L 7 2 4F RT A16WE 2001011102344 20010111 02344 NM 2001 1 11 AWXA0001190 1 20010103 A 5312 65163006 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 25070 23776 BS 178 FWD PRESSURE BULKHEAD CENTER WEB CRACKED 2 EA 1/2 INCH LONG O/B SIDE OF LBL 5.7 AT WL 216 AND WL 214 UNDER STIFFE NER. REMOVED DAMAGED AREA OF WEB AT WL 214 LBL 7.0; FABED REPAIR PARTS; INSTALLED REPAIR PARTS IAW SRM 53-10-08 FIG 209. 2 L 7 2 4F RT A16WE 2001011102345 20010111 02345 NM 2001 1 11 AWXA0001191 1 20010103 A 5312 65163006 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 25070 23776 BS 178 FWD PRESSURE BULKHEAD CENTER WEB CRACKED 2 EA 1/2 INCH LONG O/B SIDE OF RBL 5.7 AT WL 216 AND WL 214 UNDER STIFFE NER. REMOVED DAMAGED AREA OF WEB AT WL 214 LBL 7.0; FABED REPAIR PARTS; INSTALLED REPAIR PARTS IAW SRM 53-10-08 FIG 209 2 L 7 2 4F RT A16WE 2001011102346 20010111 02346 NM 2001 1 11 AWXA0001192 1 20010103 A 5512 657378351 SKIN BOEING 737 7373G7 1384595 NM HORIZONTAL STAB DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 25070 23776 LT HORIZ STABILIZER L/E AT L/E STA 122.39 HAS DENT OUT OF LIMITS. REMOVED FASTENERS AND RIB AND CUT OUT DMG IAW SRM 55-1 0-01; HFEC INSPEC IAW B737 NTM PT.6 51-00-00 FIG 23 - NO CRACKS NOTED; FABED DOUBLER AND FILLER IAW 55-10-01; FABED REPL ACEMENT RIB IAW 55-10-01; INSTALLED PARTS IAW SRM 55-10-01 FIG 203. 2 L 7 2 4F RT A16WE 2001011102347 20010111 02347 NM 2001 1 11 AWXA0001193 1 20010103 A 5512 657378351 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 LT HORIZ STABILIZER L/E AT L/E STA 233.59 HAS DENT OUT OF LIMITS. REMOVED FASTENERS AND RIB AND CUT OUT DMG IAW SRM 55-1 0-01; HFEC INSPEC IAW B737 NTM PT.6 51-00-00 FIG 23 - NO CRACKS NOTED; FABED DOUBLER AND FILLER IAW 55-10-01; FABED REPL ACEMENT RIB IAW 55-10-01; INSTALLED PARTS IAW SRM 55-10-01 FIG 203. 2 L 7 2 4F RT A16WE 2001011102348 20010111 02348 NM 2001 1 11 AWXA0001194 1 20010103 A 5410 313A138017 ANGLE BOEING 737 7373G7 1384595 NM NACELLE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 25070 23776 LT WING O/B PYLON SKATE ANGLE HAS ELONGATED NR 3 FASTENER HOLE. REMOVED DAMAGE; FABED AND INSTALLED REPAIR AND INSTALLED SKATE ANGLE IAW SRM 51-40-02 AND 51-70-11; INSTALLED REPAIR ANGLES, 2 EA, AND 3 EA FILLERS IAW B737 SRM 51-70-11 AND 54 -50-71; FABED ANGLES, MILLED AND HEAT TREATED, 3 EA FILLERS AND 3 SHIMS IAW 51-30-01 FIG 10 2 L 7 2 4F RT A16WE 2001011102349 20010111 02349 NM 2001 1 11 AWXA0001195 1 20010103 A 5310 651758351 STIFFENER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 VERTICAL STIFFENER ANGLE CRACKED FS 178 LBL 5.7 WL 180 (1.5 INCH L). REMOVED COMPONENTS TO GAIN ACCESS; CUTOUT DMGD AREA ; NDT VERIFIED NO CRACKS; FABED AND INSTALLED REPAIR PARTS IAW SRM 53-10-08 FIG 205; REINSTALLED COMPONENTS IAW TASK CAR D 01A53006, C1A53006 2 L 7 2 4F RT A16WE 2001011102350 20010111 02350 NM 2001 1 11 AWXA0001196 1 20010103 A 5320 65176889 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 25070 23776 AT LT LAV. STR 16 FS 300, FOUND INTERCOSTAL WEB TO HAVE CRACK AT RADIUS. REMOVED DAMAGE IAW SRM 51-70-13 AND 51-70-11; N DT CONDUCTED HFEC IAW B737 NDTM PT.6, 51-00-00 FIG 23, NO CRACKS NOTED; FABED ANGLE AND FILLER REPAIR IAW SRM 53-10-15 F IG 1 AND 51-70-11; INSTALLED REPAIR IAW SRM 51-70-11 AND 51-40-02. 2 L 7 2 4F RT A16WE 2001011102366 20010111 02366 NM 2001 1 11 AWXA0001200 1 20010103 A 5320 BRACKET BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 ANGLE BRACKET CRACKED STA 616 LBL 60. REMOVED DAMAGED AREA; FABED REPAIR ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW ER 03-5310-0035-JS1A 2 L 7 2 4F RT A16WE 2001011102367 20010111 02367 NM 2001 1 11 AWXA0001201 1 20010103 A 5753 65C252752 BEAM BOEING 737 7373G7 1384595 NM WING CRACKED A AWXA K NONE O OTHER UK UNKNOWN 1 WP 28 154AW 23776 RT WING LOWER T/E METAL SEAL FWD OF AILERON IS CRACKED. REMOVED AND REPLACED BEAM ASSY IAW SRM 51-40-02, 51-40-05 AND 51 -10-02 2 L 7 2 4F RT A16WE 2001011102368 20010111 02368 EU 2001 1 11 AWXA0001202 1 20010103 A 3260 LANDING GEAR AIRBUS 320 A320231 3930325 EU MAIN MALFUNCTIONED A AWXA O OTHER J WARNING INDICATION DE DESCENT 1 WP 28 627AW 66 ON LANDING GEAR EXTENSION THE NOSE GEAR SHOWED NOT DOWN/LOCKED; THE PILOT JIGGLED THE HANDLE AND ABOUT 10 SEC LATER THE GEAR THEN SHOWED DOWN AND LOCKED; CREW MADE AN EMERGENCY LANDING. THE PROBLEM WAS TROUBLESHOT IAW TSM 32-31-00 PG.A212 & A213; NO FAULTS WERE FOUND AND NO ASSOCIATED FAULTS WERE NOTICED ON PREVIOUS FLIGHT REPORTS; THE AIRCRAFT WAS RELEASED IAW TSM 00-INTRO: PG 28 (2)(B)2 2 L 7 2 4F RT A28NM 2001011102369 20010111 02369 NM 2001 1 11 AWXA0001203 1 20010103 A 3230 65446916 MODULE BOEING 737 7373Y0 1384671 NM NLG WW MALFUNCTIONED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 330AW 38862 23499 LAS - AIR TURNBACK - UPON GEAR RETRACTION, RED TRANSIT NOSE GEAR LIGHT WOULD NOT EXTINGUISH IN GEAR UP POSITION; VIBRATI ON AND NOISE PRESENT; IN OFF POSITION GREEN AND RED NOSE GEAR LIGHT ON; ALL 3 GEAR GREEN LIGHTS WERE ON FOR LANDING. MAI NTENANCE TROUBLESHOT AND REPLACED THE NOSE GEAR HYDRAULIC MODULE; FUNCTIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2001011103970 20010111 03970 WP 2001 1 11 ERKR200100015 1 20010104 A 5230 99211583 STRAP DOUG DC9 DC933F 302207A WP FUSELAGE DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 AUTHORIZES THE REPAIR OF DOUBLE-DRILLED HOLE DAMAGE TO THE INNER CHORD OF THE STATION 354 FRAME OF THE MAIN CARGO DOOR B ELOW TRACE LL "J". THE REPAIR CONSISTS OF DRILLING OUT THE DAMAGE INSTALLING A REINFORCEMENT STRAP AND REPAIR BUSHING AN D REPLACING THE INNER SKIN. PER ECRA 933-52-059-2 REV. B. 2 L 7 2 4F A6WE 2001011102339 20010111 02339 NM 2001 1 11 AWXA0001186 1 20010103 A 5210 6545871 SKIN BOEING 737 7373G7 1384595 NM PAX DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 R1 DOOR SKIN CRACKED AT LOWER HINGE CUTOUT. CUT OUT DAMAGE AND REPAIRED IAW SB737-52-1096 FIG 6 DETAIL II AS PER AWA EO 52-00-02 AND SRM 51-40-02 2 L 7 2 4F RT A16WE 2001011101434 20010111 01434 NM 2001 1 11 QXEA0100002 1 20010102 A 3350 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 825PH 213 PDX - FOUND LEFT HAND SIDE EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001011102189 20010111 02189 NE 2001 1 11 RAIA0101004 2 20010103 A 7320 31055016 SENSOR JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE RT ENGINE FALSE INDICATION A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 560HK 9758 9758 41076 76082 7494-STL-DURING TAKE OFF RIGHT HAND IEC CAPTION ILLUMINATED. MAINTENANCE REMOVED AND REPLACED RIGHT HAND P2 SENSOR IAW G ARRETT TPE 331 MAINTANACE MANUAL. 2 L 7 2 4T 4 T RT A41NM E18NE 2001011101585 20010111 01585 EU 2001 1 11 XNA00023 1 20010103 A 2611 SMOKE AIRBUS 300 A300B4203 3930306 EU CARGO BAY DETECTED A TC8A O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 GL 23 474AS 219 ON APPROACH TO DAY A & B LIGHTS ON MID1, MID2 & AFT CARGO ILLUMINATE ACCOMPONIED WITH SMOKE AND ODER. 2 L 7 2 4F RT A35EU 2001011103971 20010111 03971 WP 2001 1 11 ERKR200100016 1 20010104 A 5230 9921583 STRAP DOUG DC9 DC933F 302207A WP CARGO DOOR DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 AUTHORIZES THE REPAIR OF THE DOUBLE-DRILLED HOLE DAMAGE TO THE INNER CHORD OF THE STATION 373 FRAME OF THE MAIN CARGO DO OR ABOVE TRACE LL "G". THE REPAIR CONSISITS OF DRILLING OUT THE DAMAGE, INSTALLING A REINFORCEMENT STRAP AND REPAIR BUSH ING AND REPLACING THE INNER SKIN. PER ECRA 933-52-060-2 REV.A 2 L 7 2 4F A6WE 2001011101388 20010111 01388 NE 2001 1 11 CALA0100001 2 20010102 A 7261 ENGINE BOEING 737 737524 1384721 NM GE CFM56 CFM563B1 13802 NE NR 2 LEAKING A CALA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 09 14604 27317 856781 SHORTLY AFTER TAKEOFF FROM EWR SMOKE ENTERED THE CABIN AND THE LAV SMOKE DETECTORS ACTIVATED. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED SAFELY. THE SMOKE DISSIPATED RAPIDLY ONCE ON THE GROUND. THE AIRCRAFT TAXIED TO THE GATE UNDER IT S OWN POWER. MAINTENANCE FOUND OIL IN THE NR 2 ENGINE BLEED DUCTS. THE NR 2 ENGINE WAS REMOVED AND REPLACED. BOTH COALES CER BAGS WERE REPLACED. THE ENGINE WAS RUN AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2001011101403 20010111 01403 WP 2001 1 11 CALA0100002 1 20010101 A 5543 TAB DOUG DC9 DC982 3022082 WP RUDDER LOOSE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16807 49261 INSPECTION FOUND RUDDER TAB T/E METAL TAB LOOSE ON RT SIDE. THE RUDDER TRIM TAB WAS REMOVED, REPAIRED, AND REINSTALLED I AW MM 27-20-02, PARAGRAPH B & C. 2 L 7 2 4F A6WE 2001011101404 20010111 01404 NM 2001 1 11 CALA0100003 1 20010102 A 7110 301A10805 COWLING BOEING 737 7373Q8 1384670 NM NR 2 ENGINE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19382 26311 INSPECTION FOUND RT ENGINE NOSE COWL DENTED. THE RT ENGINE NOSE COWL WAS REMOVED AND REPLACED IAW MM 71-11-01. 2 L 7 2 4F RT A16WE 2001011103972 20010111 03972 WP 2001 1 11 ERKR200100017 1 20010104 A 5230 99211595 STRAP DOUG DC9 DC933F 302207A WP CARGO DOOR DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 AUTHORIZES THE REPAIR OF THE DOUBLE-DRILLED HOLE TO THE INNER CHORD OF THE STATION 354 AND 373 FRAME OF THE MAIN CARGO DOOR BELOW TRACE L5L. THE REPAIR CONSISITS OF DRILLING OUT THE DAMAGE, INSTALLING A REINFORCEMENT STRAP AND REPAIR BUSHI NG AND REPLACING THE INNER SKIN. PER ECRA 933-52-062-2 REV.A 2 L 7 2 4F A6WE 2001011103973 20010111 03973 WP 2001 1 11 ERKR200100018 1 20010104 A 5230 99211585 ANGLE DOUG DC9 DC933F 302207A WP FUSELAGE DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 AUTHORIZES THE REPAIR OF DOUBLE-DRILLED HOLE DAMAGE TO THE INNER CHORD OF THE STATION 411 AND 430 FRAMES OF THE MAIN CAR GO DOOR BELOW TRACE L5L. THE REPAIR CONSISTS OF DRILLING OUT THE DAMAGE, INSTALLING A REINFORCEMENT ANGLE AND REPAIR BUS HING AND REPLACING THE INNER SKIN. PER ECRA 933-52-063-2 REV.A 2 L 7 2 4F A6WE 2001011104498 20010111 04498 EU 2001 1 11 UPS01134582 1 20010103 A 3260 BDM3003 DETECTOR AIRBUS A300 A300F4622R 3930360 EU MLG FAILED A IPXA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 124UP 0808 INSPECTION TYPE:N/A AFTER TAKEOFF, LDG GEAR WOULD NOT RETRACT ON SYS 1. SWITCHED TO SYS 2 AND GEAR RETRACTED NORMALLY. R&R POSITION DETECTOR UNIT PER MEL 32-31-71, OPS CK OK. THIS CLEARS M206586. 2 L 7 2 4F RT A35EU 2001011104535 20010111 04535 NM 2001 1 11 UPS01234586 1 20010103 A 3350 BATTERY BOEING 727 72727C 138400J NM COCKPIT FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 908UP 19114 INSPECTION TYPE:N/A EMERGENCY LIGHT AT ENTRY DOOR INOP LIGHT SWITCH LEFT ON. REPLACED BATTERIES. OPS CK OK 2 L 7 3 4F A3WE 2001011601185 20010116 01185 WP 2001 1 16 UPS01834583 1 20010103 A 2710 CONTROL VALVE DOUG DC8 DC873F 302199F WP RT AILERON BINDING A IPXA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 01 866UP 45966 INSPECTION TYPE:N/A AILERON BINDING, DURING CONTROL CHECKS AILERON WOULD NOT RETURN TO NEUTRAL ON ITS OWN AFTER BEING DI SPLACED TO THE RIGHT. RTB *S/D* REMOVED AND REPLACED RT AILERON POWER CYLINDER/CONTROL VALVE UP TO STEP B2 AGE 204 MM 27-11-06. OPS CK LEAK CK GOOD. 2 L 7 4 4F RT 4A25 2001011104561 20010111 04561 WP 2001 1 11 UPS01834585 1 20010103 A 3350 BATTERY DOUG DC8 DC871F 302199D WP CABIN FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP, SWITCH APPEARS TO BE AT FAULT R & R 'D A/C MAIN BATTERY PER MM 24-30-01 A ND 33-50-01 OPS CK GOOD 2 L 7 4 4F RT 4A25 2001011103622 20010111 03622 NM 2001 1 11 C1HA200194001 1 20010101 A 3350 SIGN BOEING 727 727290 138408W NM CABIN DISLODGED A C1HA O OTHER O OTHER TO TAKEOFF 1 GL 15 294AS 22146 AFT EMERGENCY EXIT SIGN FELL OFF ON TAKE OFF. RESECURED SIGN OPS NORMAL. 2 L 7 3 4F A3WE 2001011103794 20010111 03794 SO 2001 1 11 SWIA972241 1 20010101 A 3150 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT FALSE ACTIVATION A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 584SW 120352 WHILE APPLYING TAKEOFF POWER RAN BOTH ENGINES. COULD NOT DUPLICATE. CHECKED ENGINE CONTROL CHIME WITH EECS OFF. CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001011103795 20010111 03795 EA 2001 1 11 SWIA972242 1 20010103 A 2751 POTENTIOMETER CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT OUT OF ADJ A SWIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 423SW 7456 ON TAXI OUT FLAPS WERE SET TO 20 DEGREES AND EICAS INDICATION IS 18 DEGREES. ADJUSTED LEFT AND RIGHT FLAP INDICATION POT ENTIOMETERS PER CRJ MM 27-55-01. RAN FLAPS EICAS INDICATIONS NORMAL. FECU INDICATION OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2001011103796 20010111 03796 SO 2001 1 11 SWIA972243 1 20010103 A 3150 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 218SW 120287 ON TAKE OFF ROLL, GOT TRIM AURAL WARNING WITH TRIM SET IN GREEN RANGE. ABORTED TAKEOFF. PERFORMED AURAL WARNING RESET P ROCEDURES, CHECKS GOOD IAW MM 31-63-00 2 L 7 2 4T 4 T RT A31SO E20NE 2001011104708 20010111 04708 WP 2001 1 11 ERKR200100019 1 20010104 A 5320 99211513 ANGLE DOUG DC9 DC933F 302207A WP FUSELAGE DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 AUTHORIZES THE REPAIR OF MISS-DRILLED HOLE TO THE INNER FLANGE OF THE STATION 364 AND STATION 379.5 FRAMES OF THE MAIN C ARGO DOOR BETWEEN L5L AND L6L. THE REPAIR FOR EACH LOCATION, CONSISTS OF TRIMMING OUT THE DAMAGE AND NESTING A SET OF RE PAIR ANGLES BEHIND THE INNER FLANGE OF THE FRAME. PER ECRA 933-52-066-2. 2 L 7 2 4F A6WE 2001011104709 20010111 04709 WP 2001 1 11 ERKR200100020 1 20010104 A 5230 99211514 ANGLE DOUG DC9 DC933F 302207A WP CARGO DOOR DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 AUTHORIZES THE REPAIR OF MISS-DRILLED HOLE DAMAGE TO THE INNER FLANGE OF THE STATION 347 FRAME OF THE MAIN CARGO DOOR BE TWEEN L5L AND L6L . THE REPAIR CONSISTS OF TRIMMING OUT THE DAMAGE AND NESTING A SET OF REPAIR ANGLES BEHIND THE INNER F LANGE OF THE FRAME.PER ECRA 933-52-067-2 REV.A 2 L 7 2 4F A6WE 2001011104710 20010111 04710 WP 2001 1 11 ERKR200100021 1 20010104 A 5230 99211445 STRAP DOUG DC9 DC933F 302207A WP CARGO DOOR DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 AUTHORIZES THE REPAIR OF DOUBLE-DRILLED HOLE DAMAGE TO THE INNER CHORD OF THE STATION 392 FRAME OF THE MAIN CARGO DOOR B ELOW TRACE LL "H". THE REPAIR CONSISTS OF TRIMMING OUT THE DAMAGE, INSTALLING A FILLER, REINFORCEMENT ANGLE AND STRAP. P ER ECRA 933-52-078-2 REV.A 2 L 7 2 4F A6WE 2001011104525 20010111 04525 NE 2001 1 11 TWAA0100301 2 20010102 A 7200 ENGINE BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE NR 1 FAILED A TWAA A UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 CE 05 701TW 28160 4906 IN CRUISE A LOUD BANG WAS HEARD FROM THE LEFT ENGINE AND IT SPOOLED DOWN. MADE AN UNSCHEDULED LANDING AT MSP. THE ENGINE WAS REPLACED. CHECK-C 12-5-00 LAX. 2 L 7 2 4F 4 F RT A2NM E17NE 2001011104526 20010111 04526 WP 2001 1 11 TWAA0100302 1 20010103 A 4990 SMOKE DOUG DC9 DC982 3022082 WP CABIN DETECTED A TWAA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CE 05 919TW 49368 ON SHORT FINAL SMOKE APPEARED IN THE CABIN WHEN ANTI-ICE WAS TURNED ON. ACCOMPLISHED PACK BURN OUT AND DEACTIVATED APU P ER MEL. CHECK-C 5-12-00 MCI. 2 L 7 2 4F A6WE 2001011102870 20010111 02870 WP 2001 1 11 EFKR200100022 1 20010104 A 5230 99211445 STRAP DOUG DC9 DC933F 302207A WP CARGO DOOR DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 AUTHORIZES THE REPAIR OF DOUBLE-DRILLED HOLE DAMAGE TO THE INNER CHORD OF THE STATION 411 FRAME OF THE MAIN CARGO DOOR B ELOW LL "H". THE REPAIR CONSISTS OF TRIMMING OUT THE DAMAGE, INSTALLING A FILLER ANGLE, AND STRAP. PER ECRA 933-52-083-2 REV.A 2 L 7 2 4F A6WE 2001011104711 20010111 04711 WP 2001 1 11 ERKR200100023 1 20010104 A 5230 99211449 FRAME DOUG DC9 DC933F 302207A WP CARGO DOOR DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 AUTHORIZES THE REPAIR OF MISS-DRILLED HOLE DAMAGE, IN THE AREA OF STATION 316, LL "C" TO THE INNER WEB AND DOUBLER OF TH E MAIN CARGO DOOR. THE REPAIR CONSISTS OF PLUGGING THE DAMAGED SKIN AND LOWER WEB, BLENDING OUT THE DAMAGE TO THE FRAME. PER ECRA 933-52-085-2 REV.A 2 L 7 2 4F A6WE 2001011103869 20010111 03869 WP 2001 1 11 ERKR200100024 1 20010105 A 5230 59211653 FITTING DOUG DC9 DC933F 302207A WP CARGO DOOR DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 ADDRESSES REPAIR OF SEVERAL EXTRA HOLES AND OVERSIZE HOLES COMMON TO THE MAIN CARGO DOOR HINGES AND FITTING ASSEMBLY. PE R ECRA 933-52-086-2 2 L 7 2 4F A6WE 2001011103870 20010111 03870 WP 2001 1 11 ERKR200100025 1 20010105 A 5230 992115943 SKIN DOUG DC9 DC933F 302207A WP CARGO DOOR DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 AUTHORIZES THE REPAIR OF CHAFE DAMAGE TO THE EXTERNAL SKIN OF THE MAIN CARGO DOOR STATION 370.06 THE REPAIR CONSISTS OF TRIMMING OUT THE DAMAGE, INSTALLING A FILLER AND A EXTERNAL AREO-CHAMFERED DOUBLER. PER ECRA 933-52-088-2 REV. B 2 L 7 2 4F A6WE 2001011105192 20010111 05192 EA 2001 1 11 JBXA000233 1 20010105 A 3230 601R509675 CONTROL PANEL CNDAIR CL600 CL6002B19 EA MLG FAILED A JBXA A D UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SO 05 589ML 7376 DISCREPANCY: FLT. 371 RDU/RDU AFTER TAKEOFF WITH GEAR HANDLE SELECTED UP HAD GEAR DISAGREE MESSAGE. AIRCRAFT RETURNED TO RDU. CORRECTIVE ACTION: REMOVED AND REPLACED LANDING GEAR CONTROL PANEL IAW CL-65 MM 32-31-01. PERFORMED FUNCTIONAL CHE CK OF LANDING GEAR EXTENSION/RETRACTION SYSTEM IAW MM 32-30-00. 2 L 7 2 4F RT A21EA 2001011103871 20010111 03871 WP 2001 1 11 ERKR200100026 1 20010105 A 5330 592176469 SKIN DOUG DC9 DC933F 302207A WP FUSELAGE DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 ADDRESSES REPLACEMENT OF DAMAGED SKIN PANEL LOCATED BETWEEN STATION 229 AND 301, L11-L18, LEFT HAND SIDE. ADDITIONALLY T HE DAMAGED SINGLE SKIN PANEL WILL BE REPLACED WITH TWO (2) NEW SECTIONS DUE TO MATERIAL AVAILABILLY. PER ECRA 933-53-051 -2 REV.A 2 L 7 2 4F A6WE 2001011105815 20010111 05815 WP 2001 1 11 MWEA010001 1 20010102 A 7921 548003 COOLER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE RT ENGINE LEAKING A MWEA C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 GL 31 216ME 47740 665323 RIGHT HAND OIL PRESSURE ON TOP END OF RED LINE QUANTITY AT 2 QTS. -- REPLACED TOP AFT FUEL OIL COOLER "B" NUT PACKING, SERVICED OIL. 2 L 7 2 4F 4 F A6WE E2EA 2001011105817 20010111 05817 WP 2001 1 11 MWEA010003 1 20010104 A 5313 5911412123 LONGERON DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 LONGERON 27 LEFT AT STATION 351 HAS A DOUBLE DRILLED HOLE. -- FABRICATED AND REPAIRED SPLICE. 2 L 7 2 4F A6WE 2001011105838 20010111 05838 2001 1 11 MWEA010023 4 20010103 A 2565 113317 CLIP DOUG DC9 DC981 3022081 WP ESCAPE SLIDE MISSING A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 807ME 48033 FORWARD SERVICE DOOR SLIDE COVER RIGHT SIDE KEEPS COMING OFF. -- MAINTENANCE REATTACHED LOWER SLIDE COVER LANYARD CLIP . 2 L 7 2 4F A6WE 2001011105839 20010111 05839 WP 2001 1 11 MWEA010024 1 20010104 A 3350 60030451 BATTERY PACK DOUG DC9 DC932 3022066 WP FUSELAGE DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 401ME 47133 FORWARD BANK OF EMERGENCY LIGHTS WOULD NOT EXTINGUISH WHEN POWERING DOWN THE AIRCRAFT. -- MAINTENANCE REMOVED AND REP LACED THE FORWARD EMERGENCY LIGHT BATTERY PACK. 2 L 7 2 4F A6WE 2001011103872 20010111 03872 WP 2001 1 11 ERKR200100027 1 20010105 A 5311 5920338501 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 REPAIR OF DISCREPANT HOLE DAMAGE TO THE INNER CHORDS OF STATION 737 & 756 FRAMES, L6L & L6R. CONSISTS PLUGGING DISCREPAN T HOLES AND INSTALLING REPAIR BUSHINGS AND REINFORCEMENT STRAPS.PER ECRA 933-53-055-2 REV.A 2 L 7 2 4F A6WE 2001011104175 20010111 04175 NM 2001 1 11 F3LA200100002 1 20010102 A 7110 FAIRING BOEING 737 737228 13844AG NM NR 2 ENGINE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 234TR 3086 23004 DURING C-7 CHECK, INSPECTION REPORTED A 1/2 INCH CRACK ON INSIDE AFT CORNER OF NR 2 ENGINE INBOARD FIXED FAIRING. MAINT ENANCE REMOVED DAMAGED GUSSET AND "L" ANGLE AND FABRICATED AND INSTALLED REPLACEMENT PARTS PER SRM 54-10-2, 51-10-2 AND 51-30-2. 2 L 7 2 4F RT A16WE 2001011103873 20010111 03873 WP 2001 1 11 ERKR200100028 1 20010105 A 5343 9957975501 ANGLE DOUG DC9 DC933F 302207A WP NOSE GEAR WW DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 VISUAL INSPECTION REVEALED DAMAGE TO THE NOSE GEAR SUPPORT BEAM ON THE LEFT AND RIGHT HAND SIDES. THIS CONSISTS OF TRIMM ING OUT THE DAMAGE AREA AND INSTALLING THE REPAIR SPLICE ANGLES AND THE REPAIR CAP. PER ECRA 933-53-056-2. 2 L 7 2 4F A6WE 2001011102522 20010111 02522 NM 2001 1 11 DHL2001720001 1 20010104 A 5270 WARNING SYSTEM BOEING 727 727228 NM CARGO DOOR ACTIVATED A DHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 720DH 19544 CLIMBING THROUGH 12.0, 5.0. ANNUNCIATOR PANEL "CARGO DOOR" LIGHT ILLUM. DOOR LIGHT BY ARMING SWITCH DID NOT ILLUM. AND N O PRESSURIZATION CHANGES NOTED. CABIN DIFF. AND CABIN NET WAS ABOUT 1800". (CORRECTIVE ACTION) ADJUSTED SWITCH ON 3RD LO CK AND OPS CHECKED SYSTEM TO 6 PSI DIFF. ALL INDICATIONS OPS CHECK GOOD. 2 L 7 3 4F A3WE 2001011103899 20010111 03899 WP 2001 1 11 ERKR200100029 1 20010105 A 5311 59203381 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 REPAIR OF DISCREPANT HOLE DAMAGE TO THE INNER CHORD OF THE STATION 718 FRAME, L6L & L6R. CONSISTS OF PLUGGING DISCREPANT HOLES, INSTALLING REPAIR BUSHINGS AND REINFORCEMENT STRAPS AND REPLACING EXISTING GUESSETS AND FILLERS.PER ECRA 933-53- 058-2. 2 L 7 2 4F A6WE 2001011102523 20010111 02523 2001 1 11 DHL2001720002 4 20010104 A 3420 2588369905 ADI BOEING 727 727228 NM COCKPIT UNSERVICEABLE A DHLA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SO 01 720DH 19544 ON DEPARTURE, F.O.'S ADI TUMBLED BECAME INOP - SWITCHING F.O. TO AUX V.G. WAS OF NO HELP - STILL INOP. (CORRECTIVE ACTIO N) SWAPPED NR 2 V.G. TO AUX V.G. AND R & R NR 2 ADI OPS CHECK GOOD PER M.M. CH 34-62-11 & M.M. CH 34-22-21. 2 L 7 3 4F A3WE 2001011105119 20010111 05119 CE 2001 1 11 GLBA2001001 1 20010103 A 2120 5238001 ELEMENT BEECH 1900 1900D 1154162 CE CABIN TEMP FAILED A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 226GL UE226 RETURN TO BLOCK - DUAL ENVIROMENTAL FAILURE, REPLACED TEMP SENSOR AND PRECOOLER BYPASS VALVE SYSTEM OPS CHECKED GOOD RET URNED TO SERVICE 2 L 7 2 4T RT A24CE 2001011103902 20010111 03902 WP 2001 1 11 ERKR200100030 1 20010105 A 5320 99100789 WEB DOUG DC9 DC933F 302207A WP FUSELAGE DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 REPAIR OF CORRODED UPPER CUSP ANGLE P/N 9910078-9. CONSISTS OF CUTTING THE UPPER CUSP ANGLE AT STATION 179, REPLACING TH E CORRODED PORTION AFT OF THE CUT, AND INSTALLING A SPLICE TO JOIN THE EXISTING AND REPLACEMENTS PORTIONS, ADDITIONALLY, DAMAGE TO THE LOWER CUSP ANGLE WILL BE TRIMMED OUT AND A NESTED ANGLES INSTALLED. PER ECRA 933-53-064-02 REV. B 2 L 7 2 4F A6WE 2001011100902 20010111 00902 NM 2001 1 11 01FDEA00002 1 20010104 A 5314 65561111 KEELBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 CORROSION ON LT KEELBEAM AT BS 960 O/B FLANGE AROUND FASTENERS. ** S/D ** COMING 2 L 7 3 4F RT A3WE 2001011100903 20010111 00903 NM 2001 1 11 01FDEA00003 1 20010104 A 5313 BAC1498140 STRINGER BOEING 727 727233 138408A NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 NR 319 TEN OPEN FASTENER HOLES ON SIDE OF STRINGER 24 LT AT BS 480. ** S/D ** R&R & FAB PER FEDEX SRM 53-10-3, 53-1 0-3. 2 L 7 3 4F RT A3WE 2001011100918 20010111 00918 NM 2001 1 11 01FDEA00004 1 20010104 A 5313 65562362 STRINGER BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 CRACK AT STR 15 LT SIDE BS 720C-4 AFT OF EXT LIGHT. ** S/D ** R&R PER IAW FEDEX SRM 53-10-3 FIG 1. 2 L 7 3 4F RT A3WE 2001011101628 20010111 01628 2001 1 11 XNA01001 4 20010105 A 3418 COMPUTER AIRBUS 300 A300B4203 3930306 EU COCKPIT MALFUNCTIONED A TC8A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 370PC 134 ON CLIMB OUT SLATS RETRACTED 210 KTS. STICK SHAKER CAME ON. ICING WAS REPORTED, ALL OTHER CONDITIONS SEEMED NORMAL. ACTION TAKEN:FOUND SEVERAL PUSHED PINS BEHIND MASTER WARNING COMPUTER AT RECEPTICAL. RESUCURED PINS. MASTER WARNING SY STEM OPS CHECK GOOD. STALL WARNING SYSTEM OPS CHECK GOOD I/A/W A300 MM CH 27-36-00. 2 L 7 2 4F RT A35EU 2001011100919 20010111 00919 NM 2001 1 11 01FDEA00005 1 20010104 A 5313 655457512 STRINGER BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 NR 419 CRACK AT STR 15 LT SIDE BS 720D+4 FWD OF EXT LIGHT. ** S/D ** R&R PER IAW FEDEX SRM 53-10-3 FIG 1. 2 L 7 3 4F RT A3WE 2001011100920 20010111 00920 NM 2001 1 11 01FDEA00006 1 20010104 A 5313 65562362 STRINGER BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 NR 420 CRACK AT STR 15 RT SIDE BS 720B+4 FWD OF EXT LIGHT. ** S/D ** COMING 2 L 7 3 4F RT A3WE 2001011100921 20010111 00921 NM 2001 1 11 01FDEA00007 1 20010105 A 5320 655989634 SUPPORT BOEING 727 727232 1384082 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 NR 842 CORROSION ON WEB SUPPORT BS 572 - 580, RBL 54, WL 200. ** S/D ** R&R & FAB PER IAW FEDEX SRM 51-10-6, 51-10- 2, 51-30-2, AND 51-30-5 BAC SPEC 5300, AND FEDEX DRWG 65-59896. 2 L 7 3 4F A3WE 2001011100922 20010111 00922 NM 2001 1 11 01FDEA00008 1 20010105 A 5311 6516330 FRAME BOEING 727 727232 1384082 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 NR 397 DOUBLE HOLE IN FRAME AT BS 870 JUST O/B OF STRINGER 3R. ** S/D ** R&R PER IAW FEDEX EA 7-5310-56211. 2 L 7 3 4F A3WE 2001011103903 20010111 03903 WP 2001 1 11 ERKR200100031 1 20010105 A 5312 99579061 BULKHEAD DOUG DC9 DC933F 302207A WP FUSELAGE DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 INSPECTION REVEALED DAMAGE TO THE FORWARD CLOSE OUT WEBS. STATION 362-370 AND 427-435 THE REPAIR CONSISTS OF FABRICATE T HE REPLACEMENT WEB AND RING DOUBLERS, AND INSTALLED. PER ECRA 933-53-065-2 2 L 7 2 4F A6WE 2001011103905 20010111 03905 WP 2001 1 11 ERKR200100033 1 20010105 A 5312 99577391 BULKHEAD DOUG DC9 DC933F 302207A WP FUSELAGE DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 REPAIR OF DISCREPANT HOLE DAMAGE TO THE FRAME WEB AND SPLICE AT STATION 945 BETWEEN L9L AND L10L. CONSISTS OF INSTALLING A REPAIR BUSHING, REPLACING THE SPLICE AND INSTALLING A SPLICE DOUBLER. PER ECRA 933-53-057-2 REV. A. 2 L 7 2 4F A6WE 2001011601184 20010116 01184 NM 2001 1 16 UPS01534589 1 20010105 A 2750 18196918 FLAP BOEING 757 75724APF 1384969 NM WING MALFUNCTIONED A IPXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 412UP 23852 INSPECTION TYPE:N/A DIVERTION - FLAP DISAGREE MSG. REMOVED AND REPLACED FLAP POSITION TRANSMITTER IAW MM 27-58-03. OPS CHK FLAP TRAVEL AND BITE CHK FSEU ALL NORMAL. P/N ON/OFF 18-1969-18, S/N ON -0750B, S/N OFF 0533B. 2 L 7 2 4F RT A2NM 2001011104562 20010111 04562 WP 2001 1 11 UPS01834587 1 20010104 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:N/A CRACKS MIGRATING FROM RIVET AT STATION 1480 ON LEFT SIDE OF FUSELAGE APPROX 6 FT FWD OF OVERPRESS SA FETY VALVE CRACK LENGTH IS 3/4 INCH IN THE UPPER DIRECTION AND 1/2 INCH IN THE LOWER DIRECTION ALL.FERRY. FLIGHT.PROCED URES.HAVE.BEEN.ACCOMPLISHED.AND.ACFT. IS.IN.SAFE.OPERATING.CONDITION.FOR.FERRY.FLIGHT..UPS AUTHORIZATION.J.WRIGHT.-.MGR. AMC 2 L 7 4 4F RT 4A25 2001011104680 20010111 04680 WP 2001 1 11 UPS01834588 1 20010102 A 3350 BATTERY DOUG DC8 DC871F 302199D WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:IN EMERGENCY LIGHTS INOP. SWITCH APPEARS TO BE AT FAULT. R&R'D A/C MAIN BATTERY. 2 L 7 4 4F RT 4A25 2001030100210 20010301 00210 EU 2001 3 1 SABA010002 1 20010102 A 3260 PIN BAG JETSTM JETSTM3201 1500217 EU MLG DOWNLOCK LACK OF LUBE A SABA O OTHER P NO WARNING INDICATION DE DESCENT 1 SO 33 957AE 957 AIRCRAFT 957 ON FLIGHT 5132 FROM CLT TO OAJ. WHEN THE LANDING GEAR WAS SELECTED DOWN FOR LANDING THE NOSE SAFE INDICATI ON WOULD NOT ILLUMINATE. NO INFLIGHT EMERGENCY WAS DECLARED. AIRCRAFT LANDED AND TAXIED TO THE GATE WITH NO OTHER PROB LEMS. MAINTENANCE CLEANED AND LUBED THE DOWNLOCK PIN AND HOOK FOR FULL TRAVEL TO THE LOCK POSITION. OPS CHEC WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A56EU 2001011100664 20010111 00664 NM 2001 1 11 TWAA0100401 1 20010103 A 3397 WIRE BOEING 767 7673Y0 NM GALLEY DISCONNECTED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 639TW 26208 THE EGRESS LIGHTS WERE INOPERATIVE ON THE LT SIDE OF THE FWD GALLEY. FOUND WIRES DISCONNECTED. RECONNECTED THE WIRING. CHECK-C 2-10-00. 2 L 7 2 4F RT A1NM 2001011105841 20010111 05841 WP 2001 1 11 MWEA010026 1 20010103 A 2913 AS19593B PUMP DOUG DC9 DC932 3022066 WP HYD SYSTEM INOPERATIVE A MWEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 31 215ME 47744 RIGHT HYDRAULIC PRESSURE AND FLUID SHOWED ZERO AFTER TAKE OFF. -- REPLACED BROKEN HYDRAULIC LINE FROM AUX GEAR PUMP. R EPLACED AUXILIARY ELECTRIC PUMP AND ENGINE DRIVEN PUMP. 2 L 7 2 4F A6WE 2001011105864 20010111 05864 WP 2001 1 11 MWEA010027 1 20010103 A 5210 5910081137 SKIN DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 FOUND 3/8 INCH CRACK ON LOWER FORWARD CORNER OF PASSENGER DOOR. -- INSTALLED DOUBLER IAW MD80/DC9 SRM (STRUCTURAL REPA IR MANUAL). 2 L 7 2 4F A6WE 2001011105865 20010111 05865 WP 2001 1 11 MWEA010028 1 20010104 A 3350 60030451 BATTERY PACK DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 809ME 48071 AFT EMERGENCY LIGHT AT STATION 1308 AND 1336 REMAINED ON WITH APU POWER AND BATTERY POWER REMOVED. -- MAINTENANCE TROU BLESHOT AND VERIFIED BAD BATTERY PACK AND REPLACED B5-27. 2 L 7 2 4F A6WE 2001011105818 20010111 05818 WP 2001 1 11 MWEA010004 1 20010105 A 5313 591141217 LONGERON DOUG DC9 DC914 3022034 WP FUSELAGE TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 LONGERON 27R HAS DRILL MARKS BETWEEN STATION 427-446. -- FABRICATED AND INSTALLED LONGERON. 2 L 7 2 4F A6WE 2001011105819 20010111 05819 WP 2001 1 11 MWEA010005 1 20010105 A 5320 59114087 SPLICE DOUG DC9 DC914 3022034 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 GOUGE IN RADIUS OF LONGERON SPLICE AT LONGERON 4 RIGHT, STATION 229. -- FABRICATED AND INSTALLED LONGERON SPLICE. 2 L 7 2 4F A6WE 2001011103798 20010111 03798 SO 2001 1 11 SWIA972245 1 20010104 A 2163 SENSOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE A/C PACK FAILED A SWIA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 NM 07 288SW 120316 NOTICED HOT AIRCRAFT BEFORE TAKEOFF. AFTER TAKEOFF FA SMELLED SMOKE AND SMOKE DETECTOR IN LAV WENT OFF. RETURNED TO LA X. INSTALLED NEW LEFT PAC DUCT TEMP SENSOR. CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001011100702 20010111 00702 SO 2001 1 11 SWIA972247 1 20010104 A 2751 WIRE EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE FLAP ACTUATOR GROUNDED A SWIA K NONE F FLT CONT AFFECTED AP APPROACH 1 NM 07 200CD 120200 ON APPROACH SELECTED FLAPS 25 THE RT OUTBOARD WENT 1 LIGHT BAR PAST FLAPS 25 AND CAUSED AN ASYMETRY. WE LANDED, PERFORM ED THE QRH, THEN SELECTED FLAPS UP AND THE LT OUTBOARD DID NOT MOVE AND THE RT OUTBOARD WENT 2 LIGHT BARS UP AND CAUSED ANOTHER ASYMETRY. FOUND RT OUTBOARD FLAP ACTUATOR POTENTIOMETER WIPER WIRE GROUNDING TO AIRFRAME. ISOLATED TO SOLDER SL EEVE AT CANNON PLUG OF ACTUATOR. REPAIRED WIRING AND SOLDER SLEEVE W602-0023-22DR. OPS CHECK GOOD 2 L 7 2 4T 4 T RT A31SO E20NE 2001011103931 20010111 03931 WP 2001 1 11 ERKR200100034 1 20010105 A 5330 591970735 DOUBLER DOUG DC9 DC933F 302207A WP FUSELAGE DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 INSPECTION REVEALED AN EXISTING BLENDED SKIN LOCATED BETWEEN RT STATION 917-937 AND LONGERON 28-30. THIS PROVIDES INSTRU CTIONS TO FABRICATE AND INSTALL A REPAIR AND FINGER DOUBLER.PER ECRA 933-53-069-2. 2 L 7 2 4F A6WE 2001011102336 20010111 02336 NM 2001 1 11 AWXA0001182 1 20010104 A 5312 6552878 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 CENTER WEB BULKHEAD 178 WL 200 LBL 537 HAS CRACK 3/8 INCH. REMOVED DAMAGE AND INSTALLED REPAIR IAW 53-10-08 FIG 209 2 L 7 2 4F RT A16WE 2001011102351 20010111 02351 NM 2001 1 11 AWXA0001197 1 20010104 A 5312 6552878 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 BS 178 FWD PRESSURE BULKHEAD CENTER WEB RBL 5.7 HAS 1/2 INCH CRACK; WL 198-200 RBL 5.7 HAS 3/8 INCH CRACK UNDER STIFFENE R. REMOVED DAMAGE AND INSTALLED DOUBLER AND REPAIR FILLERS IAW SRM 53-10-08 FIG 209; NDT VERIFIES CRACKS COMPLETELY REMO VED. 2 L 7 2 4F RT A16WE 2001011102352 20010111 02352 NM 2001 1 11 AWXA0001198 1 20010104 A 5312 654583340 WEB BOEING 737 7373S3 1384711 NM CABIN FLOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 FLOOR WEB CRACKED FS 180 WL 207 LBL 26. FABED AND INSTALLED FLOOR WEB IAW SRM 51-10-02 AND BOEING DWG #65-45833 2 L 7 2 4F RT A16WE 2001011102365 20010111 02365 NM 2001 1 11 AWXA0001199 1 20010104 A 5321 654583340 WEB BOEING 737 7373S3 1384711 NM CABIN FLOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 FLOOR WEB CRACKED AT FS 180 WL 207 RBL 26. FABED AND INSTALLED FLOOR WEB IAW SRM 51-10-02 AND DWG 65-45833 2 L 7 2 4F RT A16WE 2001011102370 20010111 02370 NM 2001 1 11 AWXA0001204 1 20010104 A 5320 6720382 INTERCOSTAL BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 INTERCOSTAL CRACKED THRU FS 178 WL 195 RBL 24. CUT DAMAGED SECTION OF INTERCOSTAL IAW SRM 53-10-08; FABED REPAIR ANGLE, RADIUS BLOCK FILLER, AND FILLER IAW SRM 53-10-08 FIG 207; TREATED AND PRIMED PARTS IAW 51-20-01; INSTALLED PARTS IAW 51- 40-02. 2 L 7 2 4F RT A16WE 2001011102371 20010111 02371 NM 2001 1 11 AWXA0001205 1 20010104 A 5320 6720381 INTERCOSTAL BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER UK UNKNOWN 1 WP 28 314AW 23733 INTERCOSTAL CRACKED THRU FS 178 WL 195 LBL 24. CUT OUT DAMAGED SECTION OF INTERCOSTAL IAW SRM 53-10-08 FIG 207; HFEC - N O CRACKS NOTED; FABED REPAIR PARTS IAW 53-10-08 FIG 207; TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW 51-40-02 2 L 7 2 4F RT A16WE 2001011102372 20010111 02372 NM 2001 1 11 AWXA0001208 1 20010104 A 5312 65C380902 SPLICE BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 SIDE CHORD CRACKED FS 178 WL 207 RBL 26 AND WL 195 RBL 24. CUT OUT DAMAGED SECTION OF SIDE CHORD; DRILLED NEW CHORD; DRI LLED NEW SPLICE ANGLE; FABED UPPER REPAIR SPLICE STRAP & INSTALLED IAW BOEING SB 737-53A1173 AND ER #03-5311-00340-JS2; HFEC INSPEC IAW B737 NTM PT.6, 51-00-00 FIG 23 - NO CRACKS NOTED ABOVE OR BELOW CUTLINE. 2 L 7 2 4F RT A16WE 2001011102374 20010111 02374 NM 2001 1 11 AWXA0001210 1 20010104 A 5312 6545409245 PRESSURE PANEL BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 LT MLG WW STA 663 LBL 30 CEILING PRESSURE DECK HAS A CRACK. REMOVED DAMAGED AREA IAW ER 03-5310-99288-EY1; FABED REPAIR PARTS IAW ER 03-5310-99288-EY1; INSTALLED REPAIR PARTS IAW ER 03-5310-99288-EY1. 2 L 7 2 4F RT A16WE 2001011102375 20010111 02375 NM 2001 1 11 AWXA0001212 1 20010104 A 5330 6545765 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 EXT. FUSELAGE STA 395 BTW STR 5L & 6L SKIN HAS 2 LONG GOUGE. CUTOUT DAMAGED AREA IAW SRM 53-00-01; HFEC IAW B737 NTM PT. 6 51-00-00 FIG 23 - NO CRACKS NOTED; FABED REPAIR DOUBLER IAW SRM 53-00-01 FIG 202; INSTALLED REPAIR DOUBLER IAW 53-00-0 1 FIG 202. 2 L 7 2 4F RT A16WE 2001011102470 20010111 02470 NM 2001 1 11 AWXA0001213 1 20010104 A 5512 BACR15CE5D SKIN BOEING 737 7373S3 1384711 NM HORIZONTAL STAB GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 LT HORIZ STABILIZER L/E UPPER SURFACE AT STA 166.30 HAS A DENT WITH A GOUGE (APPROX. 2.5 X 1.5). BLENDED GOUGE OUT OF LI MITS IAW SRM 51-10-02; CUTOUT DMGD AREA IAW 55-10-01; FABED SHIMS, FILLER AND DOUBLER; TREATED AND PRIMED PARTS AND INST ALLED PARTS IAW 51-40-02. 2 L 7 2 4F RT A16WE 2001011102471 20010111 02471 NM 2001 1 11 AWXA0001214 1 20010104 A 5310 6518420 WINDOW POST BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 3/8 INCH CRACK BETWEEN FLIGHT DECK WINDOW POST 1 & 2 FS 211.8. CUT OUT CRACK; FABED FILLER; INSTALLED FILLER AND BOEING P/N 69-71947-7 DOUBLER IAW SRM 53-10-01 FIG 210. 2 L 7 2 4F RT A16WE 2001011102472 20010111 02472 NM 2001 1 11 AWXA0001215 1 20010104 A 5310 65C25229 SHEAR TIE BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 UPON OPEN UP, FOUND CRACK AT STA 727D RIGHT ON FRAME/SHEAR TIE. CUT OUT DAMAGED PORTION AT STA 727D STR 27R IAW SRM 53-0 0-07; FABED REPAIR PARTS IAW 53-00-07 FIG 203; INSTALLED REPAIR PARTS IAW 51-40-02. 2 L 7 2 4F RT A16WE 2001011102473 20010111 02473 NM 2001 1 11 AWXA0001216 1 20010104 A 5313 6942159 INTERCOSTAL BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 STA 312 BL 0 INTERCOSTAL, JUST FWD OF E&E DOOR CRACKED. REMOVED CRACKED INTERCOSTAL IAW SRM 51-40-02; FABED REPAIR PARTS IAW 51-40-02 AND ENGINEERING SUPPORT; INSTALLED PARTS IAW 51-40-02. 2 L 7 2 4F RT A16WE 2001011102474 20010111 02474 NM 2001 1 11 AWXA0001217 1 20010104 A 5312 6545614 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 CENTER WEB CRACKED FS 178 WL 187 RBL 0.7 (1.1L). CUTOUT DAMAGED SECTION OF WEB; HFEC - NO CRACKS NOTED; FABED AND INSTAL LED REPAIR DOUBLER AND FILLER IAW SRM 53-10-08 FIG 203. 2 L 7 2 4F RT A16WE 2001011102475 20010111 02475 NM 2001 1 11 AWXA0001218 1 20010104 A 5320 6545614 TIE CLIP BOEING 737 7373S3 1384711 NM FUSLEAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 STR TIE CLIP CRACKED ON LOWER END OF BOTH FLANGES FS 312 BL 0. REMOVED STR TIE CLIP IAW SRM 51-40-02; FABED SHEAR CLIP I AW 55-10-04; INSTALLED SHEAR CLIP IAW 51-40-02 2 L 7 2 4F RT A16WE 2001011102476 20010111 02476 NM 2001 1 11 AWXA0001219 1 20010104 A 5311 69878671 FRAME BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER UK UNKNOWN 1 WP 28 314AW 23733 BS 178 FWD PRESS. BULKHEAD AFT SIDE LBL 5.7 WL 185 1 CRACK IN RADIUS OF VERT. CHORD I/B SIDE. REMOVED DAMAGED AREA IAW S RM 53-10-08; INSTALLED NEW REPAIR PARTS IAW 53-10-08 FIG 205; FABED 5 EA. FILLERS AND INSTALLED SAME IAW 51-40-02. 2 L 7 2 4F RT A16WE 2001011102477 20010111 02477 NM 2001 1 11 AWXA0001220 1 20010104 A 5311 65C3760716 FRAME BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 BS 178 FWD PRESS. BLKHD AFT SIDE LBL 5.7 WL 185 1 1/2 CRACK IN RADIUS OF VERT. CHORD O/B SIDE. REMOVED DAMAGED SECTION I AW SRM 53-10-08; FABED REPAIR PARTS, FILLERS IAW 53-10-08; REMOVED AND REINSTALLED ADJACENT STRUCTURE IAW 51-40-02; REIN STALLED REPAIR PARTS. 2 L 7 2 4F RT A16WE 2001011102478 20010111 02478 NM 2001 1 11 AWXA0001221 1 20010104 A 5311 65163006301 FRAME BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 SIDE CHORD CRACKED FS 178 WL 207 LBL 26 (1.4L) & WL 195 LBL 24 (1.4L). CUTOUT DAMAGED SECTION OF SIDE CHORD; DRILLED NEW SPLICE ANGLE AND NEW CHORD; FABED UPPER FRAME SPLICE STRAP AND INSTALLED IAW BOEING SB 737-53A1173 AND ER 03-5311-00340 -JS2. 2 L 7 2 4F RT A16WE 2001011102479 20010111 02479 NM 2001 1 11 AWXA0001222 1 20010104 A 5320 6937253 BEAM BOEING 737 7373S3 1384711 NM SUB FLOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 CABIN FLOOR STA 685 LBL 46 FLOOR BEAM WEB HAS CRACK. REMOVED CRACKED STUB BEAM; FABED NEW STUB BEAM IAW DWG BAC69-37253 AND INSTALLED IAW BAC DWG 65-46543. 2 L 7 2 4F RT A16WE 2001011102518 20010111 02518 NM 2001 1 11 AWXA0001223 1 20010104 A 5330 6545765 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 UPPER EXT. FUSELAGE STA 230 LBL 7 - LBL 9 SKIN STATIC DAMAGE WENT OUT OF LIMITS. CUTOUT DAMAGE; FABED FILLER AND DOUBLER S AND INSTALLED REPAIR PARTS IAW SRM 53-00-01 FIG 201 2 L 7 2 4F RT A16WE 2001011102519 20010111 02519 EU 2001 1 11 AWXA0001224 1 20010104 A 3350 1013081 LIGHT AIRBUS 320 A320231 3930325 EU CABIN DAMAGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 643AW 315 FWD LEFT BLKHD EMERGENCY LIGHT INOP AND COVER MISSING. REMOVED AND REPLACED EMERGENCY LIGHT AT FWD LEFT BULKHEAD; LIGHT OPS CHECKS GOOD. 2 L 7 2 4F RT A28NM 2001011102520 20010111 02520 NM 2001 1 11 AWXA0001225 1 20010104 A 3350 20121 CHARGER BOEING 757 7572S7 1384962 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 903AW 23323 FWD. AIRCRAFT EMERGENCY ISLE LIGHTING INOP. REMOVED AND REPLACED FWD BATTERY PACK AND FWD BATTERY CHARGER; EMERGENCY LIG HTS OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 2001011102521 20010111 02521 NM 2001 1 11 AWXA0001226 1 20010104 A 3350 LIGHT BOEING 737 73733A 1384673 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 509DC 23636 SEAT EMERGENCY LIGHT AT SEAT 21C INOP. RESECURED LOOSE WIRE; LIGHT OPS CHECKS GOOD 2 L 7 2 4F RT A16WE 2001011100705 20010111 00705 NM 2001 1 11 AWXA0001227 1 20010104 A 3397 BMS13131122 WIRE BOEING 737 7373B7 1384580 NM ROW 18 BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 328AW 23377 AFT SECTION OF EMERGENCY TRACK LIGHTING SYSTEM DOES NOT ILLUMINATE. FOUND BROKEN WIRE AT ROW 18; REPAIRED WIRE; EMERGENC Y LIGHT OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 2001011100706 20010111 00706 NM 2001 1 11 AWXA0001228 1 20010104 A 3397 BMS13131122 WIRE BOEING 737 7373G7 1384595 NM ROW 23L BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 306AW 24633 ROW 23 EMERGENCY LIGHT INOP. REPAIRED BROKEN WIRE AT ROW 23L. 2 L 7 2 4F RT A16WE 2001011103002 20010111 03002 EU 2001 1 11 AWXA0001229 1 20010104 A 3350 CIRCUIT BREAKER AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHTS TRIPPED A AWXA O OTHER O OTHER CR CRUISE 1 WP 28 626AW 65 EMERGENCY LIGHT CIRCUIT BREAKER POPPED IN FLIGHT. PHX MAINTENANCE PER FOR RESET OF CIRCUIT BREAKER; EMERGENCY LIGHTS OPE RATIONALLY CHECKED GOOD; CIRCUIT BREAKER REMAINED ENGAGED AND NO FURTHER FAULTS NOTED. 2 L 7 2 4F RT A28NM 2001011103932 20010111 03932 WP 2001 1 11 ERKR200100035 1 20010105 A 5311 9923405501 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE GOUGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 REPAIR OF A DISCREPANT HOLE, AND A GOUGE TO THE INNER CHORD OF STATION 617 FRAME BETWEEN L15L & L16L. CONSISTS OF TRIMMI NG OUT THE DAMAGE AND INSTALLING A REINFORCEMENT STRAP.PER ECRA 933-53-070-2. 2 L 7 2 4F A6WE 2001011103703 20010111 03703 WP 2001 1 11 ERKE200100036 1 20010105 A 5311 9923408502 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 REPAIR OF DISCREPANT HOLE DAMAGE TO THE INNER CHORD OF STATION 680 FRAME, AT L6L AND BETWEEN L11R & L15R. CONSISTS OF PL UGGING HOLES AND INSTALLING REPAIR BUSHINGS AND REINFORCEMENT STRAPS.PER ECRA 933-53-071-2. 2 L 7 2 4F A6WE 2001011104176 20010111 04176 NM 2001 1 11 F3LA200100003 1 20010104 A 5610 WINDOW BOEING 737 737228 13844AG NM COCKPIT LOOSE A F3LA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 237TR 23007 AIR TURN BACK. FLIGHT CREW REPORTED PRESSURIZATION LEAK AT R-1 WINDOW, WHICH HAD BEEN REPLACED THE PREVIOUS NIGHT. RET URNED TO ELP WITHOUT INCIDENT. MAINTENANCE RETORQUED AND RESEALED R-1 WINDOW. 2 L 7 2 4F RT A16WE 2001011103933 20010111 03933 WP 2001 1 11 ERKR200100037 1 20010105 A 5311 99115411 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 REPAIR OF DISCREPANT HOLE DAMAGE TO THE INNER CHORD OF STATION 699 FRAME AT L6R & L6L. CONSISTS OF PLUGGING DISCREPANT H OLES AND INSTALLING REPAIR BUSHINGS AND REINFORCEMENT STRAPS.PER ECRA 933-53-072-2 2 L 7 2 4F A6WE 2001011105866 20010111 05866 NM 2001 1 11 MWEA010029 1 20010102 A 5320 9951888121 BRACKET DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 BULKHEAD LOWER SUPPORT BRACKET AT APPROXIMATELY LONGERON 28 LEFT CRACKED. -- REMOVED AND REPLACED SUPPORT BRACKET 2 L 7 2 4F RT A6WE 2001011105867 20010111 05867 NM 2001 1 11 MWEA010030 1 20010102 A 5312 995188889 BULKHEAD DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 BULKHEAD TEE AT FLOOR LEVEL BETWEEN LONGERON 28 LEFT AND 28 RIGHT HAS CRACK AT APPROXIMATELY LONGERON 29 LEFT. -- REMO VED AND REPLACED TEE. 2 L 7 2 4F RT A6WE 2001011105868 20010111 05868 NM 2001 1 11 MWEA010031 1 20010102 A 5312 9951888111 BULKHEAD DOUG MD88 MD88 3023688 NM FUSELAGE TORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 BULKHEAD WEB HAS A TEAR APPROXIMATELY 2 INCHES ABOVE FLOOR AT APPROXIMATELY LONGERON 29 LEFT. -- INSTALLED DOUBLER IAW DC9/MD80 STRUCTURAL REPAIR MANUAL. 2 L 7 2 4F RT A6WE 2001011105869 20010111 05869 NM 2001 1 11 MWEA010032 1 20010102 A 5312 995188835 STRUT DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 BULKHEAD VERTICLE STRUT AT LONGERON 29 LEFT CRACKED APPROXIMATELY 6 INCHES ABOVE FLOOR. -- INSTALLED DOUBLE ANGLE IAW DC9/MD80 STRUCTURAL REPAIR MANUAL. 2 L 7 2 4F RT A6WE 2001011105870 20010111 05870 NM 2001 1 11 MWEA010033 1 20010102 A 5320 9951888169 ANGLE DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 BULKHEAD LOWER FLOOR SUPPORT ANGLE BETWEEN LONGERONS 28 LEFT AND 28 RIGHT CRACKED AT APPROXIMATELY LONGERON 29 LEFT. -- REMOVED AND REPLACED SUPPORT ANGLE. 2 L 7 2 4F RT A6WE 2001011103934 20010111 03934 WP 2001 1 11 ERKR200100038 1 20010105 A 5311 9957686503 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 REPAIR OF DISCREPANT HOLE DAMAGE TO THE INNER CHORDS OF STATION 639 & 617 FRAMES, L6R, L6L,L9R & L9L. CONSISTS OF PLUGGI NG, OR TRIMMING OUT, DISCREPANT AND EXTRANEOUS HOLES AND INSTALLING REPAIR BUSHINGS, REINFORCEMENT STRAPS AND ANGLES. P ER ECRA 933-53-073-2. 2 L 7 2 4F A6WE 2001011103935 20010111 03935 WP 2001 1 11 ERKR200100039 1 20010107 A 5311 9923412502 FRAME DOUG DC9 DC933F 302207A WP 658 DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 REPAIR OF DISCREPANT HOLE DAMAGE TO THE INNER CHORDS OF STATION 658 FRAME BETWEEN L8R & L15R. CONSISTS OF PLUGGING DISCR EPANT HOLES AND INSTALLING REPAIR BUSHINGS AND REINFORCEMENT STRAPS. PER ECRA 933-075-2 REV. B 2 L 7 2 4F A6WE 2001011103936 20010111 03936 WP 2001 1 11 ERKR200100040 1 20010107 A 5730 ACCESS DOOR DOUG DC9 DC933F 302207A WP WING CORRODED B ERKR O OTHER O OTHER IN INSP/MAINT 1 WP 07 933F 47191 REPAIR OF CORROSION DAMAGE TO CENTER TANK LT S ACCESS DOOR LANDING. CONSISTS OF BLENDING OUT THE DAMAGE. PER ECRA 933-53 -081-2. 2 L 7 2 4F A6WE 2001011103937 20010111 03937 WP 2001 1 11 ERKR200100041 1 20010107 A 5311 9921594501 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 REPAIR OF DISCREPANT HOLE DAMAGE TO STATION 434 & 439 FRAMES L5L & L18L. CONSISTS OF PLUGGING AND TRIMMING OUT DISCREPAN T HOLES AND INSTALLING REPAIR BUSHINGS, REINFORCEMENT STRAPS AND GUSSETS.PER ECRA 933-53-090-2. 2 L 7 2 4F A6WE 2001011104375 20010111 04375 WP 2001 1 11 ERKR200100042 1 20010107 A 5321 592240125 FLOOR PANEL DOUG DC9 DC933F 302207A WP CABIN CRACKED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 ADDRESSES THE REPAIR OF CRACKED FLOOR PANEL LOCATED BETWEEN STATION 503-775, X=37-45 LEFT HAND SIDE.CONSISTS OF TRIMMING OUT THE DAMAGE FLOOR PLANK AND INSTALLING A SPLICE DOUBLER AND ANGLE.PER ECRA 933-53-091-2 REV.A. 2 L 7 2 4F A6WE 2001011104376 20010111 04376 WP 2001 1 11 ERKR200100043 1 20010107 A 5330 59114004 SKIN DOUG DC9 DC933F 302207A WP MGL WW IMPROPER PART B ERKR K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 07 933F 47191 REPAIR OF THE R/H 5911400-4 SKIN PANEL ABOVE NOSE WHEEL WELL FS 68 TO 79 RT PER OBSOLETE DOUGLAS DC-9 SRM 53-04, FIGURE 14,SHEET 2 WITH THE FOLLOWING DEVIATION: CLAD 2024-T3 WILL BE USED IN LIEU OF CLAD 2014-T6 FOR ALL REPAIR PARTS. PER ECR A 933-53-093-2 REV. A. 2 L 7 2 4F A6WE 2001011104377 20010111 04377 WP 2001 1 11 ERKR200100044 1 20010107 A 5311 9911504 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 REPAIR OF DAMAGED STATION 76, 89 & 95 FRAMES BETWEEN Z=-10 & Z=8 LHS. CONSISTS OF REMOVING AND REPLACING THE DAMAGED FRA ME SECTIONS AND INSTALLING SPLICES TO REJOIN THE REPLACEMENT AND EXISTING SECTIONS. PER ECRA 933-53-092-2. 2 L 7 2 4F A6WE 2001011104378 20010111 04378 WP 2001 1 11 ERKR200100045 1 20010107 A 5312 59203371 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE MISDRILLED B ERKR K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 07 933F 47191 REPAIR OF MISS-DRILLED HOLE AND DRILL START DAMAGE TO INNER CHORD AND WEB, OF STATION 598 FRAME SECTIONS, AT L18L, L11R & L6R. CONSISTS OF PLUGGING DISCREPANT HOLES AND BLENDING OUT DRILL STARTS. PER ECRA 933-53-094-2. 2 L 7 2 4F A6WE 2001011104414 20010111 04414 WP 2001 1 11 ERKR200100046 1 20010107 A 5311 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE MISDRILLED B ERKR K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 07 933F 47191 REPAIR OF MISDRILLED HOLE DAMAGE; LOCATED BETWEEN STATIONS 294 & 301, L10L TO L18L; FRAME AND CLOSEOUT WEB. CONSISTS OF REMOVING AND REPLACING THE DAMAGED LOWER PORTION OF THE FRAME AND INSTALLING A SPLICE TO JOIN THE EXISTING AND REPLACEME NT SECTIONS, INSTALLING A REPAIR BUSHING IN THE INNER CHORD OF THE FRAME ABOVE THE SPLICE AND FINALLY ADDING A DOUBLER T O THE INBD SIDE OF THE CLOSEOUT WEB. PER ECRA 933-53-095-2. 2 L 7 2 4F A6WE 2001011104484 20010111 04484 WP 2001 1 11 ERKR200100047 1 20010107 A 5347 SEAT TRACK DOUG DC9 DC933F 302207A WP FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 REPAIR OF CORROSION DAMAGE TO DOUBLE SEAT TRACK LBL 27 BETWEEN STATIONS 398.5 AND 476.5. CONSISTS OF CUTTING OUT, REMOVI NG AND REPLACING THE DAMAGED PORTION OF SEAT TRACK BETWEEN 398.5 AND 476.5 AND INSTALLING SPLICES TO JOIN THE EXISTING A ND REPLACEMENT SECTIONS. PER ECRA 933-53-097-2. 2 L 7 2 4F A6WE 2001011104485 20010111 04485 WP 2001 1 11 ERKR200100048 1 20010107 A 5320 INTERCOSTAL DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 REPAIR OF CRACKED INTERCOSTAL LOCATED AT L12R BETWEEN STATION 149 & 160. CONSISTS OF INSTALLING A NESTED REINFORCEMENT ANGLE. PER ECRA 933-53-099-2. 2 L 7 2 4F A6WE 2001011104486 20010111 04486 WP 2001 1 11 ERKR200100049 1 20010107 A 5311 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE MISDRILLED B ERKR K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 07 933F 47191 REPAIR OF MISS-DRILLED HOLE DAMAGE TO FRAME AND CLOSEOUT WEB AT STATION 207, L11L. CONSISTS OF DRILLING OUT THE MISS-DRI LLED HOLES IN THE FRAME AND THE WEB AND INSTALLING REINFORCEMENT STRAPS.PER ECRA 933-53-100-2. 2 L 7 2 4F A6WE 2001011104487 20010111 04487 WP 2001 1 11 ERKR200100050 1 20010107 A 5320 991007811 ANGLE DOUG DC9 DC933F 302207A WP FUSELAGE ELONGATED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 REPAIR OF AN ELONGATED IN THE LOWER CUSP ANGLE P/N 9910078-11 AT STATION 207, LHS. CONSISTS OF DRILLING OUT THE DAMAGE A ND INSTALLING A FILLER AND REINFORCEMENT STRAP. PER ECRA 933-53-101-2. 2 L 7 2 4F A6WE 2001011105193 20010111 05193 EA 2001 1 11 JBXA000234 1 20010106 A 3230 7179015 CONTROL PANEL CNDAIR CL600 CL6002B19 EA MLG FAILED A JBXA A UNSCHED LANDING J O WARNING INDICATION OTHER CL CLIMB 1 SO 05 572ML 7224 DISCREPANCY: UPON GEAR LEVER SELECTION UP, HAD THE FOLLOWING MESSAGES PARKING BRAKE SOV, ANTI SKID INBD, AND GEAR DISAGR EE. ALL OCCURRED WITH GEAR REMAINING DOWN AND LOCKED. CORRECTIVE ACTION: REMOVED AND REPLACED LANDING GEAR CONTROL PANEL I-A-W AMM 32-30-00 OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2001011102524 20010111 02524 NM 2001 1 11 DHL2001720003 1 20010104 A 5270 SWITCH BOEING 727 727228 NM OUT OF ADJ OUT OF ADJ A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 720DH 19544 CLIMBING THRU 12.0 S/O ANNUNCIATOR PANEL(CARGO DOOR)LIGHT ILLUM. DOOR LIGHT BY ARMING SWITCH DID NOT ILLUM, AND NO PRESS URAZATION CHANGES NOTED.CABIN DIFF AND CABIN ALT WAS ABOUT 1800. ADJUSTED SWITCH ON 3RD LOCK AND OPS CHK SYSTEM TO 6 PS I DIFF.ALL IND GOOD. 2 L 7 3 4F A3WE 2001011104488 20010111 04488 WP 2001 1 11 ERKR200100051 1 20010108 A 5315 FLOORBEAM DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 REPAIR OF CRACKED FLOOR BEAM UPPER CHORD FORWARD FLANGE AT STATION 389, RBL 54.5. CONSISTS OF TRIMMING OUT THE DAMAGE AN D INSTALLING A NET FIT FILLER AND NESTED LAYERED REPAIR ANGLES. PER ECRA 933-53-102-2. 2 L 7 2 4F A6WE 2001011104582 20010111 04582 WP 2001 1 11 ERKR200100052 1 20010108 A 5315 995821223 FLOORBEAM DOUG DC9 DC933F 302207A WP FUSELAGE ELONGATED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 REPAIR OF ELONGATED HOLE DAMAGE TO STATION 756 FLOORBEAM UPPER CAP FROM LBL 40 OUTBD. CONSISTS OF TRIMMING OFF, REMOVING AND REPLACING THE DAMAGED OUTBD MOST END OF THE FLOORBEAM UPPER CAP AND INSTALLING A SPLICE ( AT LBL 40 ) TO JOIN THE E XISTING AND REPLACEMENT SECTIONS. PER ECRA 933-53-104-2. 2 L 7 2 4F A6WE 2001011102525 20010111 02525 2001 1 11 DHL2001720004 4 20010104 A 3420 2588369905 ADI BOEING 727 727228 NM COCKPIT UNSERVICEABLE A DHLA A UNSCHED LANDING I FLT. ATTITUDE INST. CL CLIMB 1 SO 01 720DH 19544 ON DEPARTURE F/OS ADI TUMBLED AND BECAME INOP SWITHING F/O TO AUX VG WAS OF NO HELP, STILL INOP. SWAPPED NR 2 VG TO AUX VG AND R&R NR 2 ADI. OPS CHKED OK PER M/M 34-22-21 2 L 7 3 4F A3WE 2001011104583 20010111 04583 WP 2001 1 11 ERKR200100053 1 20010108 A 5330 SKIN DOUG DC9 DC933F 302207A WP FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 REPAIR OF 2 INSTANCES OF CORROSION DAMAGE TO SKIN BETWEEN L28R AND L30R AT STATIONS 427 AND 370. CONSISTS OF TRIMMING OU T THE DAMAGE AND INSTALLING AN INTERNAL AND EXTERNAL DOUBLER.PER ECRA 933-53-105-2. 2 L 7 2 4F A6WE 2001011104584 20010111 04584 WP 2001 1 11 ERKR200100054 1 20010108 A 5315 99234361 FLOORBEAM DOUG DC9 DC933F 302207A WP FUSELAGE ELONGATED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 REPAIR OF ELONGATED HOLE DAMAGE TO FLOOR BEAM / FRAME SPLICE FITTINGS AT STATION 718 CONSISTS OF DRILLING OUT THE DAMAGE AND INSTALLING REPAIR BUSHINGS. PER ECRA 933-53-106-2. 2 L 7 2 4F A6WE 2001011104585 20010111 04585 WP 2001 1 11 ERKR200100055 1 20010108 A 5310 592032339 STRUCTURE DOUG DC9 DC933F 302207A WP FUSELAGE GOUGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 ADDRESSES REPAIR OF EXISTING GOUGE IN THE WATER SERVICE DOOR CUTOUT LOCATED BETWEEN STATION 446-465, LONGERON 21-22, RIG HT HAND SIDE. PER ECRA 933-53-107-2 REV. A 2 L 7 2 4F A6WE 2001011104586 20010111 04586 WP 2001 1 11 ERKR200100056 1 20010108 A 5330 99216961 SKIN DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 REPAIR OF A CRACK IN 9921696-1 SKIN ( INNER WEB )AT STATION 306, L4L. CONSISTS OF TRIMMING OUT THE CRACK AND INSTALLING DOUBLERS. PER ECRA 933-53-110-2. 2 L 7 2 4F A6WE 2001011103904 20010111 03904 NM 2001 1 11 ERKR200100032 1 20010105 A 5311 65B01843 FRAME BOEING 747 747132 1384882 NM FUSELAGE CRACKED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 CRACKED INNER CHORD AT STA 1265. REPAIRED PER ECRA 479-53-146-2. THIS REPAIR IS A TIME LIMITED, IT PROVIDES AMOC FOR SB 747-53A2416 AND IS VALID FOR A PERIOD OF NOT MORE THAN 1000 FLIGHT CYCLES BEYOND 01-05-01. 2 L 7 4 4F A20WE 2001011102782 20010111 02782 NM 2001 1 11 SCNA01003 1 20010103 A 2910 CHECK VALVE BOEING 727 7272J4 1384006 NM HYD SYSTEM FAILED A SCNA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 15 288SC 20765 DURING TAKEOFF FROM MKE THE AIRCRAFT FILLED WITH SMOKE IN BOTH THE CABIN AND COCKPIT. THE FLIGHT CREW ABORTED THE TAKEO FF. THE AIRCRAFT WAS FERRIED TO MSP, THE ODOR RETURNED BUT NO SMOKE. THE NUMBER ONE ENGINE 13TH STAGE HYDRAULIC RESERV OIR CHECK VALVE WAS FOUND TO HAVE FAILED. REMOVED AND REPLACED BOTH NR 1 AND NR 2 CHECK VALVES AND BOTH COALESOR BAGS. RAN ALL THREE ENGINES AT DIFFERENT POWER SETTINGS SEVERAL TIMES, NO FURTHER FAULT FOUND. 2 L 7 3 4F RT A3WE 2001011101957 20010111 01957 EA 2001 1 11 COMA0160043 1 20010104 A 5320 60154103077 SPLICE CNDAIR CL600 CL6002B19 EA FUSELAGE MISMANUFACTURED A COMA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 914CA 7012 TWO SPLICE PLATES 601R31030-77 WERE FABRICATED INCORRECTLY BY MANUFACTURER. FABRICATED DOUBLER PLATE, REWORKED SPLICE P LATES AND INSTALLED I/A/W W.V.A.C. E.O. 601R-53-2076. 2 L 7 2 4F RT A21EA 2001011101958 20010111 01958 EA 2001 1 11 COMA0160044 1 20010104 A 5320 60034017595 ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 914CA 18259 7012 PERFORMED A MAJOR REPAIR AT F.S. 280.00 AFT "J" ANGLE IS CRACKED AT THE TWO CENTER NUT PLATES. REPAIRED CRACKED AFT "J" ANGLE F.S. 280 BETWEEN LBL9 AND RBL 9 IAW WVAC E.O. 601R-53-2081A. 2 L 7 2 4F RT A21EA 2001011101956 20010111 01956 NE 2001 1 11 COMA0160042 2 20010102 A 7240 NAS6303U9 BOLT CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE EXHAUST NOZZLE MISSING A COMA O OTHER K FLUID LOSS IN INSP/MAINT 1 SO 01 807539 WE WERE REMOVING THE QEC KIT FROM ENGINE 807539 THAT WAS INSTALLED ON A PORTABLE ENGINE STAND. WHEN IT CAME TIME TO REMO VE THE EXHAUST NOZZLE P/N 228-55030-11J WE FOUND 7 BOLTS (OUT OF 30) MISSING. FOUR OF THE BOLTS (P/N NAS6303U4 AND NAS 6 303U9) WERE LOCATED NEXT TO EACH OTHER WITH TWO OF THEM IN THE 6 O'CLOCK DELTA BRACKET WHICH HOLDS THE EXHAUST FAIRING.T HE OTHER 3 BOLTS WERE MISSING AT THE 7 AN 11 O'CLOCK POSITION.NO ACTION TAKEN. THE EXHAUST HARDWARE REMAINING WAS DISCA RDED AS IS STANDARD PRACTICE ON OUR QEC CHANGES. 2 L 7 2 4F 4 F RT A21EA E15NE 2001011104587 20010111 04587 WP 2001 1 11 ERKR200100057 1 20010108 A 5414 99577434 SKIN DOUG DC9 DC933F 302207A WP PYLON DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 INSPECTION REVEALED DAMAGE TO THE RIGHT HAND PYLON TRAILING EDGE UPPER SURFACE SKIN, THIS DOCUMENT PROVIDES MATERIAL SUB STITUTION INSTRUCTIONS TO USE DMS1592 IN LIEU OF DMS1536 PER ECRA 933-54-068-2 REV. A. 2 L 7 2 4F A6WE 2001011104588 20010111 04588 WP 2001 1 11 ERKR200100058 1 20010108 A 5532 59121665 SKIN DOUG DC9 DC933F 302207A WP VERTICAL STAB GOUGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 AUTHORIZES THE REPAIR OF GOUGE DAMAGE TO THE SKIN AND FINGER DOUBLER OF THE VERTICAL STABILLIZER REMOVABLE TIP FAIRING A T YV248, ZV141, R/H, L/H. THE REPAIR CONSISTS OF TRIMMING OUT THE DAMAGE AND ADDING A REPAIR DOUBLER BEHIND THE SKIN AND FINGER DOUBLER. PER ECRA 933-55-080-2 REV B. 2 L 7 2 4F A6WE 2001011105734 20010111 05734 NE 2001 1 11 NACA200100002 2 20010105 A 8530 356994 CYLINDER PWA R2800CB3 DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE NR 3 ENGINE CRACKED A NACA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 AL 03 43872 218 218 P32304 533294 P32304 DISCREPANCIES: M.I. @ 03:15Z, SHUT DOWN #3 ENGINE DUE TO RAPID BACKFIRE.CORRECTIVE ACTION: REPLACED #3 CYLINDER ON #3 ENGINE. 2 L 7 4 4R 4 R 6A3 5E8 2001011104589 20010111 04589 WP 2001 1 11 ERKR200100059 1 20010108 A 5730 9919377504 PANEL DOUG DC9 DC933F 302207A WP WING DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 ADDRESSES REPAIR OF TWO (2) EXISTING TRIM-OUTS COMMON TO THE REFUEL DOOR LAND OF THE RH WING LEADING EDGE SPAR LOCATED B ETWEEN XFS 258 AND XFS 280. PER ECRA 933-57-052-2 REV.A. 2 L 7 2 4F A6WE 2001011104590 20010111 04590 WP 2001 1 11 ERKR200100060 1 20010108 A 5730 99193711 SKIN DOUG DC9 DC933F 302207A WP WING DENTED B ERKR O OTHER O OTHER IN INSP/MAINT 1 WP 07 933F 47191 REPAIR OF DENT AND DING DAMAGE TO THE LHS L/H WING SKIN BETWEEN XIS 189 AND XOS 194. THIS CONSISTS OF TRIMMING AND DRILL ING OUT THE DAMAGE AND INSTALLING FILLERS AND AN EXTERNAL DOUBLER. PER ECRA 933-57-082-2. 2 L 7 2 4F A6WE 2001011105120 20010111 05120 CE 2001 1 11 GLBA2001002 1 20010106 A 3350 GE1864 BULB BEECH 1900 1900D 1154162 CE CABIN BURNED OUT A GLBA K NONE L NO TEST IN INSP/MAINT 1 CE 01 254GL UE254 EMERGENCY LIGHT INOP - R/R LIGHT BULB OPS CHECKED GOOD 2 L 7 2 4T RT A24CE 2001011105121 20010111 05121 CE 2001 1 11 GLBA2001003 1 20010107 A 2434 23078019 GENERATOR BEECH 1900 1900D 1154162 CE NR 2 INOPERATIVE A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 169GL 5842 1452 UE169 RETURN TO BLOCK - RIGHT GEN FELL OFF LINE WOULD NOT RESET, R/R STARTER-GEN SYSTEM OPS CHECKED GOOD 2 L 7 2 4T RT A24CE 2001011104606 20010111 04606 WP 2001 1 11 ERKR200100061 1 20010108 A 5744 99193012 FITTING DOUG DC9 DC933F 302207A WP WING MISDRILLED B ERKR K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 07 933F 47191 THIS REPAIR OF MISS-DRILLED HOLE DAMAGE TO RHS WING # 1 SLAT OUTBOARD FITTING P/N 9919301-2 AT STATION XIS 137.921. CONS ISTS OF PLUGGING THE DISCREPANT MISS-DRILLED HOLES AND INSTALLING A REINFORCEMENT FITTING. PER ECRA 933-57-096-2. 2 L 7 2 4F A6WE 2001011105122 20010111 05122 CE 2001 1 11 GLBA2001004 1 20010107 A 7700 WARNING LIGHT BEECH 1900 1900D 1154162 CE LT ENGINE ILLUMINATED A GLBA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 01 94UX UE94 RETURN TO BLOCK - LEFT ENGINE BLEEDAIR FAIL INDICATION, RESEATED PCB OPS CHECKED SYSTEM GOOD RETURNED TO SERVICE 2 L 7 2 4T RT A24CE 2001011104607 20010111 04607 WP 2001 1 11 ERKR200100062 1 20010108 A 5753 59202168 FITTING DOUG DC9 DC933F 302207A WP FLAP CARRIAGE DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 REPAIR OF RIGHT HAND SIDE WING INBD FLAP CARRIAGE FITTING WEAR MARKS. CONSISTS OF BLENDING OUT THE WEAR MARKS.PER ECRA 9 33-57-103-2. 2 L 7 2 4F A6WE 2001020700166 20010207 00166 NM 2001 2 7 UPS01634590 1 20010107 A 5720 ATTACH FITTING BOEING 767 76734AF 1385212 NM LT WING TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 302UP 27240 INSPECTION TYPE:PFLT LEFT WING, LEFT O/B FLAP, PANEL (WING) ABOVE O/B FITTING HAS AN 18 INCH CRACK THRU AND 24 INCH CRAC K THRU THE PANEL. (SEE ITEM 1, PG 534960) MARKED THE UPPER SURFACE. REMOVED PANEL AND ACCOMPLISHED INTERIM REPAIR IAW B767-5750-13691A INSPECT EA W/E CK AND PERMANENT REPAIR AT NEXT C-CK. 2 L 7 2 4F RT A1NM 2001011104537 20010111 04537 NM 2001 1 11 UPS01634591 1 20010107 A 5730 PANEL BOEING 767 76734AF 1385212 NM LT WING CRACKED A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 302UP 27240 INSPECTION TYPE:PFLT LT O/B WING PANEL CRACKED 18 INCH AND 24 INCH AT FLAP TRACK. ***MRR FILED AS OPEN*** 2 L 7 2 4F RT A1NM 2001011601186 20010116 01186 2001 1 16 UPS01834592 4 20010106 A 2565 SLIDE DOUG DC8 DC871F 302199D WP PAX DOOR LOOSE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:N/A, ESCAPE SLIDE LOOSE. *S/D* RESECURED ESCAPE SLIDE AS NEEDED PER MM 25-60. 2 L 7 4 4F RT 4A25 2001022200147 20010222 00147 WP 2001 2 22 UPS01834599 1 20010104 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:DURING PREFLIGHT, CRACKS MIGRATING FROM RIVET AT STATION 1480 ON LEFT SIDE OF FUSELAGE . APPX 6 IN. FWD OF OVERPRESS SAFETY VALVE. CRACK LENGTH IS .750 IN. THE UPPER DIRECTION & .500 IN. THE LOWER DIRECTION. REMOVED DAM AGED SKIN AT STA 1480, FABRCATED, DRILLED & FINISHED REPAIR. DFRL D206716 CLEARED ON LP 462587. 2 L 7 4 4F RT 4A25 2001011105171 20010111 05171 WP 2001 1 11 IXXA0000045 1 20010105 A 3260 CONNECTOR DOUG DC8 DC871F 302199D WP WHEEL WELL LOOSE A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 826BX 82733 621 45998 ENROUTE FROM RDU TO TOL, THE GEAR DOOR WARNING LIGHT ILLUMINATED AFTER GEAR RETRACTION. THE FLIGHT CREW CYCLED THE LANDI NG GEAR AND THE WARNING INDICATION EXTINGUISHED. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSP ECTED THE LANDING GEAR LOCATION A LOOSE CANNON PLUG ON THE LEFT MAIN GEAR DOOR SWITCH. MAINTENANCE SECURED THE CANNON PL UG AND PERFORMED PERFORMED AN OPERATIONAL CHECK. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2001011105178 20010111 05178 WP 2001 1 11 IXXA0100001 1 20010105 A 3230 CONNECTOR DOUG DC8 DC871F 302199D WP WHEEL WELL LOOSE A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 826BX 82733 621 45998 !ENROUTE FROM RDU TO TOL, THE GEAR DOOR WARNING LIGHT ILLUMINATED AFTER GEAR RETRACTION. THE FLIGHT CREW CYCLED THE LAND ING GEAR AND THE WARNING INDICATION EXTINGUISHED. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INS PECTED THE LANDING GEAR LOCATION A LOOSE CANNON PLUG ON THE LEFT MAIN GEAR DOOR SWITCH. MAINTENANCE SECURED THE CANNON P LUG AND PERFORMED PERFORMED AN OPERATIONAL CHECK. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2001011105842 20010111 05842 WP 2001 1 11 MWEA010034 1 20010104 A 3010 983810564 RELAY DOUG DC9 DC914 3022034 WP COCKPIT FAILED A MWEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 31 80ME 45795 WHILE USING AIRFOIL ANTI-ICE LEFT HAND ICE PROTECTION TEMPERATURE HI ANNUNCIATOR ILLUMINATED. AFTER SECURING SYSTEM, RH ICE PROTECTION TEMP. HI ILLUMINATED. SECURED THE SYSTEM. -- PERFORMED SYSTEM TESTS ON RIGHT HAND AND LEFT HAND SIDES . ALL TESTS WERE WITH-IN SPECIFIED LIMITS. ALL TEMPERATURES CHECK NORMAL. SYSTEM OPERATIONALLY CHECK GOOD. REMOVED A ND REPLACED RELAY R2-664. 2 L 7 2 4F A6WE 2001011101973 20010111 01973 EA 2001 1 11 COMA0160047 1 20010101 A 3244 5010598 TIRE CNDAIR CL600 CL6002B19 EA NLG FAILED A COMA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 SO 01 868CA 660 7427 NLG TIRE BLEW OUT DURING T/O. REPLACED NLG WHEEL ASSY. 2 L 7 2 4F RT A21EA 2001011101974 20010111 01974 EA 2001 1 11 COMA0160048 1 20010102 A 2750 7455001 CONTROL UNIT CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA O OTHER O OTHER AP APPROACH 1 SO 01 409CA 492 7441 FLAPS FAIL MESSAGE. REPLACED THE FLAP SELECTOR ASSY. 2 L 7 2 4F RT A21EA 2001011101975 20010111 01975 2001 1 11 COMA0160049 4 20010102 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 420CA 7451 STALL FAIL CAUTION DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001011104553 20010111 04553 WP 2001 1 11 TWAA0100501 1 20010105 A 2150 20495054 ACM DOUG DC9 DC982 3022082 WP AC BAY CONTAMINATED A TWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 911TW 49182 FUMES WERE REPORTED IN THE CABIN. OIL WAS FOUND IN THE LT ACM DUCTS. REPLACED THE ACM, CHANGED WATER SEPERATERS, AND ACC OMPLISHED PACK BURN OUT. CHECK-C 8-20-00 STL. 2 L 7 2 4F A6WE 2001011100274 20010111 00274 NM 2001 1 11 TWAA0100502 1 20010107 A 2497 WIRE BOEING 757 757231 1384950 NM RELAY PANEL DAMAGED A TWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CE 05 719TW 28487 DURING TROUBLESHOOTING RT ENGINE PROBE HEAT MALFUNCTION, ATTEMPT WAS MADE TO REPLACE RELAY K10479. AS RELAY PANEL OPENE D SPARKS CAME FROM WIRE BUNDLE. REMOVED POWER FROM THE AIRCRAFT AND FOUND WIRE 6092-20 WAS BURNED THRU, REFERENCE WIRIN G DIAGRAM MANUAL 30-24-12. SPLICED IN A NEW PIECE OF WIRE. TAPED AND SECURED WIRE BUNDLE. CHECK-C 12-19-00 LAX. 2 L 7 2 4F RT A2NM 2001011104554 20010111 04554 NM 2001 1 11 TWAA0100503 1 20010106 A 3350 0202175007 LIGHT BOEING 767 7673Q8 NM CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 635TW 28207 THE EGRESS LIGHTS WERE INOPERATIVE ON THE LEFT SIDE OF THE CABIN FROM ROW 30 AFT, AND EMERGENCY LIGHTS WERE INOPERATIVE ON THE AFT FUSELAGE AND THE RT SIDE NR 4 SLIDE LIGHT. CORRECTED EGRESS LIGHTS BY SECURING CONTACTS AT ROWS 41 LEFT AND 42 LEFT, AND REPLACED THE LIGHT ASSEMBLY, PN 0202175-007, AT THE AFT FUSELAGE AND R4 DOOR SLIDE LIGHT. CHECK-C 4-7-98. 2 L 7 2 4F RT A1NM 2001011104556 20010111 04556 NM 2001 1 11 TWAA0100504 1 20010107 A 3350 LIGHT BOEING 757 757231 1384950 NM CABIN CONTAMINATED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 714P 28482 THE EGRESS LIGHT STRIP IN FIRST CLASS WAS INOPERATIVE. DRIED MOISTURE FROM LIGHT TRACK IN FIRST CLASS. CHECK-C 8-16-00 LAX. 2 L 7 2 4F RT A2NM 2001011101976 20010111 01976 EA 2001 1 11 COMA0160050 1 20010102 A 2611 PU90421R3 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA LAVATORY FALSE INDICATION A COMA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 SO 01 812CA 7381 SMOKE TOILET CAUTION MESSAGE, F/A REPORTS SMOKE AND ELECTRIC SMELL IN CABIN.COULD NOT DUPLICATE. REPLACED LAV SMOKE DET ECTOR. 2 L 7 2 4F RT A21EA 2001011102019 20010111 02019 EA 2001 1 11 COMA0160051 1 20010102 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA PAX DOOR FALSE ACTIVATION A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 812CA 7381 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. COULD NOT DUPLICATE. DOOR LATCH MECHANISM OPERATES NORMALLY. 2 L 7 2 4F RT A21EA 2001011102031 20010111 02031 2001 1 11 COMA0160052 4 20010102 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 739CA 7273 STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001011102032 20010111 02032 EA 2001 1 11 COMA0160053 1 20010103 A 2752 853D10012 ACTUATOR CNDAIR CL600 CL6002B19 EA TE FLAPS JAMMED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 936CA 2329 7043 FLAPS FAILED WHEN SELECTED TO 45 DEGREES. REPLACED THE RT NR 3 FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2001011102033 20010111 02033 EA 2001 1 11 COMA0160054 1 20010102 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA O OTHER O OTHER AP APPROACH 1 SO 01 936CA 10327 7043 FLAPS FAIL CAUTION MESSAGE. REPLACED THE LT BPSU. 2 L 7 2 4F RT A21EA 2001011102035 20010111 02035 2001 1 11 COMA0160056 4 20010103 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 964CA 7129 STALL FAIL CAUTION MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001011102036 20010111 02036 EA 2001 1 11 COMA0160057 1 20010103 A 7810 22855030113 NOZZLE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT ENGINE DEPARTED A COMA O OTHER D E INFLIGHT SEPARATION VIBRATION/BUFFET CL CLIMB 1 SO 01 933CA 7040 807441 VIBRATION FELT DURING FLIGHT, VIBRATION STOPPED DURING DECENT. POST FLIGHT INSP FOUND LEFT ENGINE TAILPIPE AND EXHAUST FAIRING HAD DEPARTED ACFT.REPLACED LEFT ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 2001011102037 20010111 02037 2001 1 11 COMA0160058 4 20010104 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 962CA 7123 STALL FAIL CAUTION DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001011102038 20010111 02038 2001 1 11 COMA0160059 4 20010103 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 403CA 7428 STALL FAIL CAUTION MESSAGE DURINT T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001011102039 20010111 02039 EA 2001 1 11 COMA0160060 1 20010103 A 2150 601R951213 FITTING CNDAIR CL600 CL6002B19 EA ACM CLOGGED A COMA A UNSCHED LANDING O S OTHER AFFECT SYSTEMS CL CLIMB 1 SO 01 416CA 7450 WHEN AIR CONDITIONING BLEED AIR TRANSFERRED FROM APU TO ENGINES, REVERBERATIONS COULD BE HEARD AND FELT IN CABIN. UNCLO GGED WATER SEPERATOR DRAIN LINES. 2 L 7 2 4F RT A21EA 2001011102040 20010111 02040 2001 1 11 COMA0160061 4 20010103 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 975CA 7150 STALL FAIL CAUTION DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001011102062 20010111 02062 EA 2001 1 11 COMA0160062 1 20010103 A 5610 NP1393212 WINDSHIELD CNDAIR CL600 CL6002B19 EA COCKPIT FAILED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 924CA 12337 7026 COPILOTS WINDSHIELD SHATTERED. REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 2001011102063 20010111 02063 EA 2001 1 11 COMA0160063 1 20010104 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA O OTHER O OTHER NR NOT REPORTED 1 SO 01 936CA 6495 7043 FLAPS FAILED AT 41 DEGREES. REPLACED THE RT BPSU. 2 L 7 2 4F RT A21EA 2001011102064 20010111 02064 EA 2001 1 11 COMA0160064 1 20010104 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA O OTHER O OTHER AP APPROACH 1 SO 01 915CA 3700 7013 FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT BPSU. 2 L 7 2 4F RT A21EA 2001011102065 20010111 02065 2001 1 11 COMA0160065 4 20010105 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 969CA 7141 STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER 2 L 7 2 4F RT A21EA 2001011102034 20010111 02034 2001 1 11 COMA0160055 4 20010102 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 420CA 7451 STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001011101454 20010111 01454 EU 2001 1 11 QXEA0100007 1 20010104 A 4980 38075412 APU FOKKER F28 F28MK4000 4990810 EU AFT TAIL MALFUNCTIONED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 34556 163 11238 LAX- CABIN FILLED WITH SMOKE WITH APU AND CABIN PACK ON. REMOVED AND REPLACED APU. OPERATIONAL CHECKS GOOD. AIRCRAFT RET URNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001011101435 20010111 01435 EU 2001 1 11 QXEA0100003 1 20010104 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU COCKPIT MALFUNCTIONED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 11234 SEA- FORWARD EXIT LIGHT OVER COCKPIT DOOR IS DIM. REMOVED AND REPLACED FORWARD EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001011101436 20010111 01436 EU 2001 1 11 QXEA0100004 1 20010104 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN MALFUNCTIONED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 11234 SEA- EXIT LIGHT OVER ISLE MID CABIN FACING AFT IS DIM. REMOVED AND REPLACED MID CABIN AFT EMERGENCY EXIT SIGN. OPERATION AL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001011101437 20010111 01437 EU 2001 1 11 QXEA0100005 1 20010102 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU COCKPIT MALFUNCTIONED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 490US 11152 SEA- EXIT SIGN OVER COCKPIT DOOR IS DIM. REPLACED EXIT LIGHT CIRCUIT BOARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETRUNED T O SERVICE. 2 L 7 2 4F RT A20EU 2001011101453 20010111 01453 EU 2001 1 11 QXEA0100006 1 20010102 A 3350 551590004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN MALFUNCTIONED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 490US 11152 SEA- EXIT SIGN MID CABIN OVERHEAD AISLE FACING AFT IS DIM. REPLACED EXIT LIGHT CIRCUIT BOARD. OPERATIONAL CHECKS GOOD. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001011104177 20010111 04177 NM 2001 1 11 F3LA200100004 1 20010105 A 2612 FIRE DETECTOR BOEING 737 7372L9 1384497 NM APU MALFUNCTIONED A F3LA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 03 271FL 22734 FLIGHT CREW REPORTED APU FIRE WARNING ILLUMINATED IN FLIGHT FROM PHX TO DEN. THE APU FIRE BOTTLE WAS DISCHARGED AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT WAS DIVERTED TO ABQ AND LANDED WITHOUT INCIDENT.AN INSPECTION REVEALED NO SIGNS OF OVERHEATING OR FIRE. PLACARDED APU FIRE DETECTION SYSTEM PER MEL 26-8.1. SUPPLEMENTAL INFORMATION TO FOLLOW WHEN REPA IR IS ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001011103101 20010111 03101 SO 2001 1 11 SWIA972251 1 20010103 A 2751 3015001007 FCU EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FLAPS MALFUNCTIONED A SWIA K NONE N FALSE WARNING DE DESCENT 1 NM 07 195SW 120127 DURING DESCENT, FLAP CONTROL FAULT LIGHT ILLUMINATES WITHOUT SELECTING ANY FLAPS, INBOARD PAIR FLASHING PANEL. QRH PROC EDURE CLEARED FAULT. REMOVED AND REPLACED FCU DUE TO UNCOMMAND FLAPS FAULTS INBOARD. AFTER CYCLING FLAPS SEVERAL TIMES WITH OUT DUPLICATING PROBLEM IAW EMB 120 MM 27-50-06. PN ON 307500-1007 SN ON 0102 SN OFF 0169 2 L 7 2 4T 4 T RT A31SO E20NE 2001011103123 20010111 03123 SO 2001 1 11 SWIA972252 1 20010102 A 2751 CONNECTOR EMB 120 EMB120RT SO PWA 118 PW118 NE RT FLAP CONTAMINATED A SWIA K NONE J WARNING INDICATION AP APPROACH 1 NM 07 1105G 120105 FLAP ASSYMETRY INDICATION OUTBOARD SECTION ON APPROACH. AIRCRAFT REMAINED CONTROLLABLE, LANDED UNEVENTFULLY. FOUND ANTI -ICING FLUID IN RIGHT OUTBOARD FLAP ELECTRICAL CONNECTOR. CLEANED CONNECTOR. CYCLED FLAPS NUMEROUS TIMES. GROUND OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001011103124 20010111 03124 SO 2001 1 11 SWIA972253 1 20010105 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FLAP FAILED A SWIA K NONE J WARNING INDICATION DE DESCENT 1 NM 07 190SW 120050 INBOARD FLAP CONTROL FAULT INFLIGHT. NO FLAP HANDLE MOVEMENT. REMOVED AND REPLACED INBOARD FLAP ACTUATOR. CYCLED FLAPS NUMEROUS TIMES OPS CHECKS GOOD. RII 27-307PN ON 320300-1005 SN ON 0030 SN OFF 0421 2 L 7 2 4T 4 T RT A31SO E20NE 2001011103128 20010111 03128 EA 2001 1 11 SWIA972254 1 20010106 A 2760 PCU CNDAIR CL600 CL6002B19 EA SPOILER FAILED A SWIA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 NM 07 408SW 7055 SPOILERONS FAULT MESSAGE CAME ON INFLIGHT. REMOVED AND REPLACED LEFT INBOARD PCU ON LEFT SPOILERON IAW MM 27-26-01. OPS CHECK LEAK CHECK GOOD AT THIS TIME. PN ON 2700-7 SN ON MAL0581 SN OFF MAL0474 2 L 7 2 4F RT A21EA 2001011103131 20010111 03131 SO 2001 1 11 SWIA972255 1 20010106 A 2752 3203001007 ACTUATOR EMB 120 EMB120RT SO PWA 118 PW118 NE T/E FLAP FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 162CA 120150 AFTER SELECTING FLAPS 45 DEGREES DISAGREEMENT ILLUMINATED OUTBOARD PAIRS WERE AFFECTED WITH 4 LIGHT PAIRS NOT ILLUMINATE D. DID NOT FIX ITSELF. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR WITH SERVICEABLE ACTUATOR. PN ON 320300-1007 SN ON 0780 SN OFF 0954 2 L 7 2 4T 4 T RT A31SO E20NE 2001011102528 20010111 02528 NM 2001 1 11 DHL2001741001 1 20010109 A 3222 STRUT BOEING 727 7272Q9 138448M NM NLG UNDERSERVICED A DHLA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 741DH 21931 ON TAXI-OUT LOUD BANGING NOISE FROM NOSE WHEEL AREA ESPECIALLY WHEN TAXING OVER SMALL BUMPS. SERVICED NOSE STRUT WITH 5 606 AND NITROGEN PER M/M CHPT 32 2 L 7 3 4F RT A3WE 2001011102492 20010111 02492 2001 1 11 DHL2001717001 4 20010109 A 3420 25883024 GYRO BOEING 727 72723 1384004 NM COCKPIT UNSERVICEABLE A DHLA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SO 01 717DH 19389 CAPT HSI FAILED ON TAXI OUT. REMOVED AND REPLACED NR 2 DIRECTIONAL GYRO PER M/M 34-21-21,SYS OPS CHK GOOD 2 L 7 3 4F A3WE 2001011101883 20010111 01883 EU 2001 1 11 A6WA200000082 1 20010104 A 2150 A/C PACK BAG BAE146 BAE146300A 1500267 EU NR 2 ODOR A A6WA H DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 31 616AW E3145 SMOKY SMELL IN CABIN AFTER TAKEOFF, CREW SHUT OFF APU AIR AND SWITCHED TO ENGINE AIR, OPERATED ON NR 2 PACK AND SMOKY SM ELL DISSIPATED. MAINTENANCE PERFORMED DUCT CONTAMINATION CLEARING PROCEDURE COULD NOT DUPLICATE SMELL, SYSTEM OPERATES NORMALLY ON ALL ENGINES AND APU AIR. 2 H 7 4 4F RT A49EU 2001011104161 20010111 04161 WP 2001 1 11 0100019935 1 20010105 A 5330 SKIN DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1332U 47404 A fuselage crack was found on the skin at the 1 left door aft of the #4 doorstop. Repaired per EA.96-167022. Reference L ogpage 1312704. 2 L 7 2 4F A6WE 2001012500167 20010125 00167 NM 2001 1 25 01FDEA00014 1 20010109 A 5311 6515929 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 FRAME IS DENTED AT BS 520, STRINGER 22 RT. *S/D* REMOVED, REPLACED AND FAB PER FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 2001012600100 20010126 00100 NM 2001 1 26 01FDEA00011 1 20010108 A 5320 DOUBLER BOEING 727 727233 138408A NM DOOR FRAME GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 MAIN CARGO DOOR AFT FRAME BS 620 IS GOUGED AT PREVIOUS REPAIR. INGD RADIUS APPROX 21 INCHES UP FROM THE BOTTOM EDGE. * S/D* REMOVED, REPLACED AND FAB PER IAW FEDEX SRM 51-40-3. PREVIOUS REPAIR. INSTALL REPAIR DOUBLER PER IAW FEDEX SRM 5 1-30-2. 2 L 7 3 4F RT A3WE 2001011104162 20010111 04162 EU 2001 1 11 0100023212 1 20010105 A 5315 FLOORBEAM AIRBUS 320 A320211 3930320 EU FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 312US 152 DURING "L" CHECK FOUND CORROSION ON FLOORBEAMS IN AFT GALLEY AREA AT Y765 AND Y1162.5/Y1292. REPAIRED PER EA 32-181716. 2 L 7 2 4F RT A28NM 2001011105843 20010111 05843 WP 2001 1 11 MWEA010035 1 20010106 A 2150 20495055 ACM DOUG DC9 DC981 3022081 WP AFT ACCESSORY LACK OF LUBE A MWEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 31 809ME 48071 CLEANERS REPORTED SMOKE IN CABIN. UPON MAINTENANCE ARRIVAL AT AIRCRAFT, SMOKE STILL FLOATING IN CABIN WITH BURNING SMELL . NOTED RIGHT AIRCONDITIONING PACK SWITCH LEFT IN HP BLEED OFF, APU AIR SWITCH ON AND APU RUNNING WITH CORSS FEEDS OPEN. AIRCRAFT MAIN BUSSES SWITHCED OFF WITH ONLY GROUND SERVICE ON. SUSPECT RIGHT AIRCONDITIONING PACK OVERHEAT/SHUTDOWN. - - MAINTENANCE INSPECTED RIGHT ACM TURBINE, OIL SERVICED. OPERATED RIGHT ACM SYSTEM FOR APPROXIMATELY 1 HOUR. PRESSURE A ND TEMPS NORMAL. RIGHT A/C ACM SYSTEM OK FOR FURTHER SERVICE. SUSPECT RIGHT ACM OVERTEMPED AND SHUT DOWN PRIOR TO ANY DA MAGE. 2 L 7 2 4F A6WE 2001011104681 20010111 04681 WP 2001 1 11 UPS01834593 1 20010103 A 5313 37585931 LONGERON DOUG DC8 DC871F 302199D WP AFT CARGO CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C2 STA.1350 LONG. 35R IS CRACKED REMOVED AND REPLACED LONGERON ST. 1270-1350 I.A.W. DWG. 3758593,AND SRM. 51-1-20D 2 L 7 4 4F RT 4A25 2001011104693 20010111 04693 WP 2001 1 11 UPS01834595 1 20010102 A 5320 37502571N FITTING DOUG DC8 DC871F 302199D WP FWD CARGO CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C2 STA. 600 LONG. 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG.3750257,AND SR M. 51-1-20D 2 L 7 4 4F RT 4A25 2001011104695 20010111 04695 WP 2001 1 11 UPS01834597 1 20010103 A 5330 575032219 DOUBLER DOUG DC8 DC871F 302199D WP AFT CARGO CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C2 STA. 1340 LONG. 31L FINGER DOUBLER IS CRACKED AND CORRODED REMOVED,FABRICATED,AND REPLACED FINGER DOUBLER I.A.W. DWG. 5750322, AND SRM.51-1-20D,51-1-21 2 L 7 4 4F RT 4A25 2001011104696 20010111 04696 WP 2001 1 11 UPS01834598 1 20010101 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C2 STA. 325 BL.0 SEAT TRACK IS WORN BEYOND LIMITS. REPAIRED SEAT TRACK I.A.W. SRM. 53-2-3 FIG.8 2 L 7 4 4F RT 4A25 2001011102066 20010111 02066 2001 1 11 COMA0160066 4 20010105 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 946CA 7072 STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001011102067 20010111 02067 EA 2001 1 11 COMA0160067 1 20010105 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 785CA 7326 EMERGENCY LIGHTS AFT OF ROW 9 ARE INOPERABLE. AFTER AIRCRAFT WARMED, COULD NOT DUPLICATE, EMERGENCY LIGHTS OPERATE NORM AL. 2 L 7 2 4F RT A21EA 2001011102068 20010111 02068 EA 2001 1 11 COMA0160068 1 20010105 A 3010 WARNING LIGHT CNDAIR CL600 CL6002B19 EA WING DEICE ILLUMINATED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 739CA 7273 LEFT WING ANTI-ICE CAUTION DURING T/O. COULD NOT DUPLICATE. SYSTEM TEST SATISFACTORY. 2 L 7 2 4F RT A21EA 2001011101782 20010111 01782 2001 1 11 COMA010069 4 20010105 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 868CA 7427 STALL FAIL CAUTION DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001011102070 20010111 02070 EA 2001 1 11 COMA0160070 1 20010101 A 5610 601R3303310 WINDSHIELD CNDAIR CL600 CL6002B19 EA COCKPIT FAILED A COMA O OTHER O OTHER AP APPROACH 1 SO 01 430CA 19 7461 COPILOTS WINDSHIELD SHATTERED. REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 2001011102071 20010111 02071 EA 2001 1 11 COMA0160071 1 20010103 A 5610 NP1393215 WINDSHIELD CNDAIR CL600 CL6002B19 EA COCKPIT FAILED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 943CA 3999 7062 PILOTS WINDSHIELD SHATTERED. REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 2001011102072 20010111 02072 EA 2001 1 11 COMA0160072 1 20010105 A 7830 WARNING LIGHT CNDAIR CL600 CL6002B19 EA THRUST REVERSER ILLUMINATED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 916CA 7014 RT THRUST REVERSER UNLOCK MESSAGE. SECURED T/R AND DEFERRED MAINTENANCE PER M.E.L. 2 L 7 2 4F RT A21EA 2001011102086 20010111 02086 EA 2001 1 11 COMA0160073 1 20010105 A 3260 WARNING LIGHT CNDAIR CL600 CL6002B19 EA NLG ILLUMINATED A COMA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 962CA 7123 NLG DISAGREE MESSAGE. NO FAULT CODES IN PSEU, COULD NOT DUPLICATE, RETRACTION CHECKS WERE NORMAL. 2 L 7 2 4F RT A21EA 2001011102087 20010111 02087 2001 1 11 COMA0160074 4 20010105 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 956CA 7105 STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001011102088 20010111 02088 EA 2001 1 11 COMA0160075 1 20010105 A 5210 LATCH CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADJ A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 917CA 7017 CABIN DOOR CAUTION MESSAGE DURING FLIGHT. ADJUSTED DOOR LATCH MECHANISM. 2 L 7 2 4F RT A21EA 2001011102089 20010111 02089 EA 2001 1 11 COMA0160076 1 20010106 A 4990 38760016 SWITCH CNDAIR CL600 CL6002B19 EA APU MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 785CA 7326 APU OIL PRESSURE MESSAGE. REPLACED APU LOW OIL PRESSURE SWITCH. 2 L 7 2 4F RT A21EA 2001011102090 20010111 02090 EA 2001 1 11 COMA0160077 1 20010105 A 3260 WARNING LIGHT CNDAIR CL600 CL6002B19 EA MLG ILLUMINATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 960CA 7117 NLG DISAGREE MESSAGE,NLG DID NOT INDICATE UP. COULD NOT DUPLICATE. LANDING GEAR RETRACT CHECKS WERE NORMAL. 2 L 7 2 4F RT A21EA 2001011102091 20010111 02091 2001 1 11 COMA0160078 4 20010106 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 971CA 7145 STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001011102092 20010111 02092 EA 2001 1 11 COMA0160079 1 20010107 A 3230 601R751461 VALVE CNDAIR CL600 CL6002B19 EA NLG MALFUNCTIONED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 721CA 5693 7259 LANDING GEAR DISAGREE MESSAGE, NLG NOT DOWN AND LOCK.REPLACED THE NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2001011102069 20010111 02069 2001 1 11 COMA0160069 4 20010105 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 868CA 7427 STALL FAIL CAUTION DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001011105179 20010111 05179 WP 2001 1 11 IXXX0100002 1 20010108 A 3230 7000010101 SWITCH DOUG DC8 DC862 3021970 WP RT GEAR DEFECTIVE A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 799AL 68461 1178 45922 ENROUTE FROM OKO TO QPG, THE LANDING GEAR UNSAFE WARNING LIGHT ILLUMINATED DURING THE GEAR UPLATCH CHECK. THE FLIGH CREW CYCLED THE LANDING GEAR WITH THE WARNING INDICATION REMAINING THE SAME. THE FLIGHT RETURNED TO OKO FOR AN UNEVENTFUL LA NDING. MAINTEANCE INSPECTED THE LANDING GEAR LOCATING A DEFECTIVE RIGHT MAIN GEAR UPLATCH SWITCH. MAINTENANCE REPLACED T HE SWITCH AND PERFORMED A SUCCEFUL OPERATIONAL CHECK IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNE D TO SERVICE. 2 L 7 4 4F 4A25 2001011100347 20010111 00347 NM 2001 1 11 CALA0100004 1 20010106 A 3397 WIRE BOEING 737 7373T0 1384582 NM CABIN DAMAGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14325 23455 INSPECTION FOUND ROW 14-21 SEAT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND A DAMAGED WIRE UNDER SEAT 19B. THE WIRE WAS REPAIRED IAW MM 20-10-13 AND OPERATION CHECKED GOOD. 2 L 7 2 4F RT A16WE 2001011100890 20010111 00890 NM 2001 1 11 CALA0100005 1 20010107 A 3350 D71702001 POWER SUPPLY BOEING 737 737824 13844BZ NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 37255 30610 THE FIRST SIX ROWS OF COACH PATH EMERGENCY EXIT LIGHTS DID NOT ILLUMINATE DURING TEST. THE EMERGENCY LIGHT POWER SUPPLY AT BS 500C WAS REMOVED AND REPLACED. OPERATION CHECKED GOOD IAW MM 33-51-06. 2 L 7 2 4F RT A16WE 2001011100891 20010111 00891 NM 2001 1 11 CALA0100006 1 20010107 A 5330 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 312, S20R. THE DENTED AREA OF SKIN WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-00-51, FIGURE 202. 2 L 7 2 4F RT A16WE 2001011100892 20010111 00892 NM 2001 1 11 CALA0100007 1 20010108 A 3230 FUSE BOEING 737 737724 NM NLG INOPERATIVE A CALA O OTHER O OTHER AP APPROACH 1 SW 09 15710 28780 THE NOSE GEAR FAILED TO EXTEND NORMALLY ON APPROACH TO CLE. ALTERNATE EXTENSION WAS USED TO EXTEND THE GEAR AND THE AIRC RAFT LANDED SAFELY. MAINTENANCE FOUND THE NLG EXTENSION FUSE AT FAULT. THE NLG EXTENSION FUSE WAS REMOVED AND REPLACED A ND LEAK CHECK WAS GOOD. THE NLG WAS SWUNG SEVERAL TIMES AND ALL OPERATION WAS NORMAL IAW MM 32-33-71. 2 L 7 2 4F RT A16WE 2001011100944 20010111 00944 WP 2001 1 11 CALA0100008 1 20010108 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16807 49261 INSPECTION FOUND INTERCOSTAL AND AFT ATTACH ANGLE IN MID PIT CORRODED BETWEEN STA 709 AND 788, L27R TO L28R. THE INTERCO STAL AND ANGLE WERE REMOVED AND A NEW INTERCOSTAL AND ANGLE WERE INSTALLED IAW SRM 51-30-2, 51-30-3, 51-30-4, AND 51-30- 5. 2 L 7 2 4F A6WE 2001011104558 20010111 04558 WP 2001 1 11 TWAA0100601 1 20010108 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 939AS 49657 THE FWD OVERWING EMERGENCY EXIT SIGN LH AND RH HAND, THE FWD ENTRY PORTABLE EMERGENCY LIGHT, EGRESS LIGHTS ROW 5 THRU 7, AND EGRESS LIGHTS ROW 22 THRU 27 WERE INOPERATIVE. REPLACED BATTERY IN THE BATTERY PACK PN 41B030CF00101 FOR THE EXIT SIGN AND FOR THE ENTRY LIGHT, REPLACED A LIGHT MODULE PN 0105606-005 FOR FWD CABIN EGRESS LIGHTS, AND ADJUSTED BATTERY C ONTACTS FOR THE AFT CABIN EGRESS LIGHTS. CHECK-C 11-16-99 MCI. 2 L 7 2 4F RT A6WE 2001011104559 20010111 04559 2001 1 11 TWAA0100602 4 20010108 A 2565 100504205 SLIDE DOUG DC9 DC982 3022082 WP L1 DOOR UNSERVICEABLE A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 940AS 49825 ON PREFLIGHT THE LEFT SIDE FWD CABIN DOOR ESCAPE SLIDE BOTTLE PRESSURE WAS READING ZERO. REPLACED THE SLIDE ASSEMBLY. C HECK-C 7-18-00 STL. 2 L 7 2 4F A6WE 2001011104570 20010111 04570 WP 2001 1 11 TWAA0100605 1 20010102 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT CORROSION WAS FOUND ON LT FLOOR MEMBRANE AT STA 1174, AFT CARGO COMPT. FABRICATED AND INSTALLED DOU BLER . 2 L 7 2 4F RT A6WE 2001011104571 20010111 04571 WP 2001 1 11 TWAA0100606 1 20010104 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT CABIN SEAT TRACK NR 3, SEAT TRACK HAD CORROSION UNDER THE FWD LAVATORY. REMOVED CORROSION IN TRACK AREA. REPAIRED PER SRM 53-05 PAGE 10G AND 10H. REPLACED SECTION OF TRACK. 2 L 7 2 4F RT A6WE 2001011104572 20010111 04572 WP 2001 1 11 TWAA0100607 1 20010105 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT THE NR 1 SEAT TRACK, GALLEY TIE DOWN HOLE HAD CORROSION AT STA 1117. FABRICATED NEW CHAIR TRACK AN D INSTALLED PER SPM 6-70-01 PAGE 1 PARA 4, FROM STA 1030 TO 1136. 2 L 7 2 4F RT A6WE 2001011104574 20010111 04574 WP 2001 1 11 TWAA0100608 1 20010105 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT IN THE FWD CARGO BILGE, FROM STA 370 TO 427, RBL 9 INCHES, FLOOR SUPPORT AT DOOR ENTRANCE HAD CORRO SION AROUND NUT PLATE HOLES. REMOVED FLOOR SUPPORT AND INSTALLED NEW FLOOR SUPPORT PER SPM 6-70-01. 2 L 7 2 4F RT A6WE 2001011104575 20010111 04575 WP 2001 1 11 TWAA0100609 1 20010106 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT THE CABIN FLOOR SUPPORT WAS CORRODED FROM STA 157 TO 201, RBL 44 INCHES. FABRICATED NEW FROM EXTRU SION. REPLACED PER SPM 6-70-01. 2 L 7 2 4F RT A6WE 2001011104576 20010111 04576 WP 2001 1 11 TWAA0100610 1 20010106 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT CABIN FLOOR SUPPORT WAS CORRODED AT STA 177, RBL 9 TO 42. REMOVED AND REPLACED CABIN FLOOR SUPPORT PER SRM 51-30-2. 2 L 7 2 4F RT A6WE 2001011105976 20010111 05976 NE 2001 1 11 ANCF200100001 2 20010105 A 7200 BLADE BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE FAILED W ANCF A UNSCHED LANDING C J F.O.D. WARNING INDICATION TO TAKEOFF 1 SW 99 321LF 26269 31233 DURING T/O IN MIA, AFTER LIFTOFF SOME BIRDS WERE INGESTED BY RIGHT ENGINE, ENGINE FAILED. AIRCRAFT RETURNED TO MIA WITHO UT FURTHER PROBLEM.CORRECTIVE ACTIONACCOMPLISHED AS PER EWO 75-72-4226PERFORMED FIM PROCEDURE AFTER BIRD STRIKE IAW FIM 71-00-00, THEN PERFORMED AN INSPECTION TO ALL LPC BLADES IAW AMM 72-31-13, REMOVED 6 BLADES DAMAGED, ALSO APPLY DRY FILM LUBRICANT TO LPC BLADES IAW AMM 72-31-13 AND LPC ROTOR DISC IAW AMM 72-31-13, PERFORMED FAN TRIM BALANCE IAW AMM 72-31- 13, ALL TEST WERE SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2001011102489 20010111 02489 NM 2001 1 11 DHL2001702001 1 20010106 A 3150 WARNING SYSTEM BOEING 727 72730C 1384009 NM COCKPIT ACTIVATED A DHLA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 01 702DH 19793 RTO BECAUSE OF FALSE T/O WARNING HORN-RECYCLED FLAPS, WARNING DID NOT SOUND WHEN T/L ADVANCED. PREFORMED T/O WARNING TE ST,FOUND NORMAL OPS PER M/M 34-00 AND 31-00 2 L 7 3 4F A3WE 2001012600073 20010126 00073 NM 2001 1 26 01FDEA00010 1 20010109 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 FOUND CORROSION ON INNER SKIN AT LAP BS 720B + 10 INCHES, STR 26R, RBL 22. *S/D* REMOVED AND REPLACED PER IAW FEDEX SR M 53-30-3 FIG 6. 2 L 7 3 4F A3WE 2001011100923 20010111 00923 NM 2001 1 11 01FDEA00012 1 20010106 A 3233 731414 ACTUATOR BOEING 727 72722 1384002 NM RT MLG FAILED A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 186FE 18872 01-002 DURING CLIMBOUT, LANDING GEAR SELECTOR IN OFF POSITION. RED DOORS LIGHT ILLUMINATED, WITH AMBER RT MLG DOOR LIGH T. REPLACED DOOR ACTUATOR PER B727 MM 32-32-081-4. LEAK & OPS CK OK. REMOVED GEAR PINS. 2 L 7 3 4F A3WE 2001011100924 20010111 00924 NM 2001 1 11 01FDEA00013 1 20010109 A 2612 894120 FIRE DETECTOR BOEING 727 7272S2F 1384O81 NM NR 1 ENGINE FALSE ACTIVATION A FDEA F C ACTIVATE FIRE EXT. ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 25 204FE 22926 01-003 NR 1 ENGINE FIRE INDICATION ON T/O ROLL ABOUT 70 KNOTS. DISCHARGE BOTH BOTTLES, LIGHT STAYED ON. ** S/D ** R &R SENSING ELEMENT & BOTH BOTTLES PER IAW MM 26-11-012-4, 2627-071-4. ALL SYS CK GOOD. 2 L 7 3 4F A3WE 2001011105979 20010111 05979 2001 1 11 ANCF200100002 4 20010107 A 3414 INDICATOR BOEING 767 767259 1385136 NM PWA 4056 PW4056 NE AIRSPEED FAILED W ANCF C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 99 985AN 24618 DURING TAKE OFF CAPTAIN AIRSPEED INDICATOR GOT STUCK AT 100 KNTS. TAKE OFF WAS ABORTED AT 116 KNTS. DEFERRED AIRSPEED I NDICATOR INOPERATIVE PER MEL 34-13-1 ITEM 199 CAT C, ALSO CHECKED EFIS AIRSPEED INDICATOR ON CAPTAIN SIDE, IT WORKS NORM ALLY. 2 L 7 2 4F 4 F RT A1NM E24NE 2001011103615 20010111 03615 WP 2001 1 11 ABXA010001 1 20010108 A 3230 HANDLE DOUG DC8 DC863 302198A WP MLG MALFUNCTIONED A ABXA O OTHER O OTHER CL CLIMB 1 GL 23 813AX 46136 LANDING GEAR HANDLE WOULD NOT COME UP AFTER TAKEOFF. PRESSURIZATION WAS NORMAL AND THERE WAS NO WARNING HORN. CREW PUSHE D IN THE ANTI-RETRACT LATCH AND LANDING GEAR CAME UP NORMALLY. ON DESCENT INTO ILN, CREW RE-CYCLED LANDING GEAR. THE LAN DING GEAR OPERATED NORMALLY. MAINTENANCE INSPECTED AND PERFORMED LANDING GEAR EXTENSION AND RETRACTION ADJUSTMENT AND TE ST PROCEDURE, IAW DC-8 MM 32-30-00. NO DEFECTS WERE NOTED. INSPECTED NOSE GEAR AND GROUND SHIFT MECHANISM. NO DEFECTS WE RE NOTED. 2 L 7 4 4F 4A25 2001011103616 20010111 03616 WP 2001 1 11 ABXA010002 1 20010109 A 5610 59124262 WINDOW DOUG DC8 DC863 302198A WP COCKPIT STUCK A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 FIRST OFFICERS CLEARVIEW WINDOW WOULD NOT OPEN COMPLETELY. MAINTENANCE INSPECTED AND OPERATED THE FIRST OFFICERS CLEARVI EW WINDOW SEVERAL TIMES. THE WINDOW OPERATED NORMALLY IAW DC-8 MM 56-10. 2 L 7 4 4F 4A25 2001011102736 20010111 02736 NM 2001 1 11 SCNA001005 1 20010107 A 3242 26011825 BRAKE ASSY BOEING 727 727282 138408T NM MLG FAILED A SCNA O OTHER O OTHER LD LANDING 1 GL 15 281SC 888 21949 DURING LANDING THE NUMBER ONE MAIN TIRE FAILED. THE NUMBER ONE BRAKE WAS FOUND LOCKED UP AND DAMAGED THE NUMBER ONE TIR E. REMOVED AND REPLACED THE NUMBER ONE BRAKE AND THE NUMBER ONE AND TWO TIRES. OPERATIONAL CHECKS GOOD. 2 L 7 3 4F RT A3WE 2001011102821 20010111 02821 NM 2001 1 11 SCNA01006 1 20010109 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 275AF 22092 DURING A MAINTENANCE LINE CHECK THE THE FORWARD OVERHEAD EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPAIRED THE WIRING A ND REMOVED AND REPLACED SELF CONTAINED OVERHEAD EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. 2 L 7 3 4F A3WE 2001011102783 20010111 02783 NM 2001 1 11 SCNA01004 1 20010104 A 3350 1000679 LIGHT BOEING 727 7272J4 1384006 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 284SC 21438 DURING A MAINTENACE "A" CHECK THE R1 DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE EMERGENC Y EXIT LIGHT, OPERATIONAL CHECKS GOOD. 2 L 7 3 4F RT A3WE 2001011106138 20010111 06138 NM 2001 1 11 PCAA0101002 1 20010109 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 835EX 289 BGM FLIGHT 3555. ROW 1 RIGHT SIDE EMERGENCY LIGHT INOP ONE BULB. MAINTENANCE REPAIRED WIRING ON FLOOR EMERGENCY LIGHTS. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001011100925 20010111 00925 NM 2001 1 11 01FDEA00015 1 20010110 A 2613 DETECTOR BOEING 727 727232 1384082 NM NR 3 ENGINE ACTIVATED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 497FE 20866 01-004 AT 5000 FT ON CLB OUT NR 3 ENGINE STRUT OVERHEAT LIGHT CAME ON. NO IRREGULARITIES NOTED. CLEANED OVERHEAT DETE CTION ELEMENT. RAN NR 3 ENGINE IAW JET RUN HANDBOOK, NO LEAKS NOTED. OK FOR SERVICE. 2 L 7 3 4F A3WE 2001011105844 20010111 05844 2001 1 11 MWEA010036 4 20010108 A 3414 4057800901 INDICATOR DOUG MD88 MD88 3023688 NM COCKPIT INOPERATIVE A MWEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 31 701ME 49760 FIRST OFFICERS AIRSPEED INDICATOR FLAGGED. -- VERIFIED DISCREPANCY. REMOVED AND REPLACED FIRST OFFICERS AIRSPEED INDIC ATOR. 2 L 7 2 4F RT A6WE 2001011104577 20010111 04577 WP 2001 1 11 TWAA0100701 1 20010108 A 3350 58222 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN MALFUNCTIONED A TWAA K NONE O OTHER CR CRUISE 1 CE 05 9303K 49529 THE EGRESS LIGHTS CAME ON IN FLIGHT FROM ROW 15 TO 25. REPLACED THE POWER SUPPLY. CHECK-C 12-24-2000. 2 L 7 2 4F RT A6WE 2001011104536 20010111 04536 NM 2001 1 11 UPS01234600 1 20010109 A 3350 1000679 LIGHT BOEING 727 72731C 1384011 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:N/A ON SHUTDOWN, DISCOVERED COCKPIT EMERGENCY EXIT LIGHT DOES NOT WORK- BULBS CHECK GOOD-EXTREMELY DIM W HEN SWITCHED TO ON POSITION - BATTERY APPEARS BAD R/R EMERGENCY EXIT LIGHT ASSEMBLY IAW MM 33-50-00 OPS CHECK SATIS. PN/ OFF/ON 10-0067-9 SN OFF 26744 SN ON UP10498 2 L 7 3 4F A3WE 2001011104223 20010111 04223 2001 1 11 DHL2001708001 4 20010111 A 3416 A4304910004 ALTIMETER BOEING 727 72725 1384006 NM CAPT'S UNSERVICEABLE A DHLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 708DH 18275 ALTIMETER SPLIT BETWEEN CAPT AND F/O'S POSITION BY 70 FEET.INSTALLED SERVO-PNUMATIC ALTIMITER IN CAPTS POSITION PER M/M 34-11-0,OPS CHK GOOD. 2 L 7 3 4F A3WE 2001011105978 20010111 05978 2001 1 11 ANCF200100003 4 20010107 A 3140 COMPUTER BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE LOOSE W ANCF C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 23 535AW 25535 DURING TAKE OFF ROLL CAPT'S ADI AND HSI SCREENS WENT BLANK WHEN AIRCRAFT ROLLED OVER IRREGULARITIES ON RUNWAY, DURING TA XI BACK TO GATE INSTRUMENTS WENT BACK TO NORMALCORRECTIVE ACTIONTHE EICAS COMPUTER AND LH SYMBOL GENERATOR WERE ADJUSTED ON RACK, ALSO WERE ADJUSTED AND CLEANED EICAS & EFIS DISPLY'S. IAW AMM 31-41-00 AND 34-22-00 2 L 7 2 4F 4 F RT A1NM E24NE 2001011104224 20010111 04224 NM 2001 1 11 DHL2001720005 1 20010110 A 2400 MI5851622 INDICATOR BOEING 727 727228 NM ONLY BURNED A DHLA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 720DH 19544 ON CLIMB OUT, CREW NOTED AN ODER,WHEN ODER INCREASED CREW DECLEARED AN EMERGANCY AND RETURNED TO CVG.NO SMOKE OR FUEMS N OTICED.R&R RADAR INDICATOR-ODER TRACED TO RADAR INDR. REMOVED AND REPLACED INDR, OPS CHK GOOD. 2 L 7 3 4F A3WE 2001011104225 20010111 04225 NM 2001 1 11 F3LA200100005 1 20010109 A 2760 TELEFLEX CABLE BOEING 737 7372L9 1384497 NM MLG WHEEL WELL OUT OF ADJ A F3LA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 NM 03 271FL 1800 22734 AIR TURN BACK. FLIGHT CREW REPORTED GEAR HANDLE WOULD NOT MOVE TO "UP" POSITION AFTER TAKEOFF AND LANDING GEAR WARNING HORN WOULD NOT SILENCE AFTER FLAPS WERE RETRACTED. REPLACED LANDING GEAR ACCESSORY UNIT AS PRECAUTIONARY PER MM 32-07-1 00. ADJUSTED GROUND SPOILER INTERLOCK CABLE, PERFORMED OPERATIONAL TEST PER MM 27-62-51 AND CHECKED OKAY. ADJUSTED LAND ING GEAR SAFETY SENSORS, PERFORMED OPERATIONAL TEST PER MM 32-04-200 AND CHECKED OKAY. 2 L 7 2 4F RT A16WE 2001011601159 20010116 01159 WP 2001 1 16 MWEA010011 1 20010108 A 5310 99115273 SHEAR TIE DOUG DC9 DC914 3022034 WP FUSELAGE CUT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 SHEAR TIE HAS A NOTCH CUT ON EDGE, STATION 427 BETWEEN LONGERON 30 AND 29 RIGHT. FABRICATED AND INSTALLED SHEAR TIE AND REPAIR SPLICES. 2 L 7 2 4F A6WE 2001011601160 20010116 01160 WP 2001 1 16 MWEA010013 1 20010108 A 5320 99576681 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 OPEN FASTENER HOLES ON INTERCOSTAL AT LONGERON 8 RIGHT, BETWEEN STATION 642 AND 623. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001011601161 20010116 01161 WP 2001 1 16 MWEA010014 1 20010108 A 5320 99576703 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 OPEN FASTENER HOLES ON INTERCOSTAL AT LONGERON 8 RIGHT, BETWEEN STATION 566 AND 544. FABRICATED AND INSTALLED DOUBLER A ND INTERCOSTAL. 2 L 7 2 4F A6WE 2001011601162 20010116 01162 WP 2001 1 16 MWEA010015 1 20010108 A 5320 99576673 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 OPEN FASTENER HOLES ON INTERCOSTAL AT LONGERON 18 LEFT, BETWEEN STATION 566 AND 544. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001011601163 20010116 01163 WP 2001 1 16 MWEA010017 1 20010108 A 5310 991224319 SHEAR TIE DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 500ME 45711 SHEAR TIE AT STATION 786 RIGHT HAND BETWEEN LONGERONS 9 AND 13 HAS MISDRILLED HOLES. FABRICATED AND INSTALLED REPLACEM ENT SHEAR TIE. 2 L 7 2 4F A6WE 2001011601165 20010116 01165 WP 2001 1 16 MWEA010018 1 20010108 A 5412 9912243107 BULKHEAD DOUG DC9 DC914 3022034 WP LT PYLON DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 UPPER WEB ON LEFT HAND PYLON BULKHEAD AT STATION 786 HAS SEVERAL IMPROPERLY SPACED HOLES ON OUTBOARD EDGE. FABRICATED A ND INSTALLED NEW WEB. 2 L 7 2 4F A6WE 2001011601166 20010116 01166 WP 2001 1 16 MWEA010019 1 20010108 A 5321 995791917 FLOORBOARD DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 FLOORBOARD E-1 HAS SEVERAL CORROSION SPOTS THRU SKIN AND 4 HAT CHANNELS HAVE CORROSION OUT OF LIMITS. FABRICATED AND IN STALLED REPLACEMENT FLOORBOARD SKIN AND HAT CHANNELS. 2 L 7 2 4F A6WE 2001011601167 20010116 01167 WP 2001 1 16 MWEA010020 1 20010108 A 5330 591142965 SKIN DOUG DC9 DC914 3022034 WP FUSELAGE PUNCTURED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 PUNCTURE IN FUSELAGE SKIN NEAR TAIL CONE, ON BOTTOM SIDE OF FUSELAGE. FABRICATED AND INSTALLED REPAIR DOUBLER AND PLUG. 2 L 7 2 4F A6WE 2001011601168 20010116 01168 WP 2001 1 16 MWEA010021 1 20010108 A 5330 59114003 SKIN DOUG DC9 DC914 3022034 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 DENT IN EXTERNAL SKIN AT LEFT SIDE STATION 76, JUST FORWARD OF EXTERNAL POWER RECEPTACLE. FABRICATED AND DRILLED DOUBLE R. 2 L 7 2 4F A6WE 2001011601169 20010116 01169 WP 2001 1 16 MWEA010022 1 20010108 A 5313 27779224 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 CRACK INDICATED ON LONGERON 17 DIRECTLY OUTBOARD OF THE PYLON BULKHEAD OF STATION 965 ON INSIDE UPPER RADIUS. FABRICATE D AND INSTALLED LONGERON REPAIR AND SPLICES. 2 L 7 2 4F A6WE 2001011601170 20010116 01170 WP 2001 1 16 0100061152 1 20010104 A 5244 DOOR DOUG DC10 DC1040 3023508 WP ACCESSORY BAY UNSECURE A NWAA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 GL 01 152US 46761 AIRCRAFT WOULD NOT PRESSURIZE DURING CLIMBOUT OF MCO. FLIGHT RETURNED TO MCO AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND CENTER ACCESSORY DOOR UNSECURED. ACCESSORY DOOR WARNING SWITCH INOPERATIVE DUE TO BROKEN WIRE. REPAIRED BROKEN W IRE AND SECURED ACCESSORY DOOR. OPERATIONAL CHECK GOOD. 2 L 7 3 4F A22WE 2001011601172 20010116 01172 NM 2001 1 16 CALA0100012 1 20010111 A 3350 3114981 SOCKET BOEING 737 7373T0 1384582 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 70352 23590 INSPECTION FOUND THE AFT EXTERIOR OVERWING EXIT EMERGENCY LIGHT INOPERATIVE AT STA 773. THE SOCKET ASSEMBLY WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. 2 L 7 2 4F RT A16WE 2001011601180 20010116 01180 NM 2001 1 16 UPS01534601 1 20010110 A 5230 HANDLE BOEING 757 75724APF 1384969 NM CARGO DOOR OUT OF ADJ A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 465UP 28269 INSPECTION TYPE:N/A, AIR TURNBACK DUE TO: EICAS MSG FWD CARGO DOOR DISPLAYED AND CARGO DOORS OPEN LIGHT ILLUM AFTER TAKE OFF. ADJUSTED FWD DOOR HANDLE FLUSHNESS PER M/M 52-34-22. OPS NORMAL. 2 L 7 2 4F RT A2NM 2001011601193 20010116 01193 EU 2001 1 16 0100093218 1 20010104 A 5210 ROLLER AIRBUS 320 A320211 3930320 EU PAX DOOR OUT OF ADJ A NWAA K NONE O OTHER TX TAXI/GRND HDL 1 GL 01 318US 206 UPON ARRIVAL AT THE GATE, THE GATE AGENT HAD DIFFICULTY PULLING DOOR 1L OPEN WITHOUT ASSISTANCE BY A FLIGHT ATTENDANT FR OM THE AIRCRAFT INTERIOR. MAINTENANCE TROUBLESHOOTING REVEALED THE AFT UPPER DOOR ROLLER WAS NOT CLEARING THE CAM ON TH E DOOR FRAME OPENING. MAINTENANCE ADJUSTED THE DOOR ON ITS Z-AXIS. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A28NM 2001011601194 20010116 01194 NE 2001 1 16 0100109968 2 20010107 A 7510 320115 VALVE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE LEFT ENGINE INTERMITTENT A NWAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 01 9332 47264 657294 DURING TAKEOFF ROLL, THE LEFT ENGINE LEFT ANTI-ICE VALVE LIGHT ILLUMINATED ABORTED TAKEOFF AT 100 KNOTS WITHOUT INCIDENT . AIRCRAFT RETURNED TO GATE. MAINTENANCE INSPECTED AND OPERATED THE LEFT ENGINE LEFT ANTI-ICE VALVE. OPERAITONAL CHEC K NORMAL. 2 L 7 2 4F 4 F A6WE E2EA 2001011601199 20010116 01199 NM 2001 1 16 QXEA0100008 1 20010105 A 2420 DH103024600CS2B INVERTER DHAV DHC8 DHC8102 2809003 NM COCKPIT MALFUNCTIONED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 815PH 34564 17778 50 PDX- STRONG FISH SMELL EMINATING FROM LEFT SIDE BY AVIONICS RACK. REMOVED AND REPLACED PRIMARY INVERTER. OPERATIONAL C HECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001011601200 20010116 01200 EU 2001 1 16 QXEA0100010 1 20010107 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 481US 11230 BOI - THE FORWARD OVERHEAD EXIT SIGN HAS INOPERTATIVE LAMPS. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001011601201 20010116 01201 EU 2001 1 16 QXEA0100011 1 20010108 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 486US 11237 GEG - THE FORWARD EXIT SIGN FOUND TO BE INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAF T RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001011601205 20010116 01205 EU 2001 1 16 QXEA0100012 1 20010104 A 3350 6008905 POWER SUPPLY FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 488US 307 307 11240 SEA - THE LEFT UNDERWING EMERGENCY EXIT LIGHT FOUND INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001011601206 20010116 01206 NM 2001 1 16 QXEA0100014 1 20010109 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A QXEA O OTHER L NO TEST NR NOT REPORTED 1 NM 09 822PH 9872 525 106 PDX - FLIGHT COMPARTMENT OVERHEAD EMERGENCY LIGHT WILL NOT TEST. REMOVED AND REPLACED OVERHEAD EXIT LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001011601242 20010116 01242 EU 2001 1 16 0100033269 1 20010105 A 2910 NAS161212 PACKING AIRBUS 320 A320212 EU HYD MANIFOLD LEAKING A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 369NW 1011 DURING CLIMB, RECEIVED HYD Y RSVR LO LVL MESSAGE. FOLLOWED COM PROCEDURES. RETURNED TO DEPARTURE FIELD AND LANDED WITH OUT INCIDENT. MAINTENANCE REPLACED LEAKING O-RING ON PTU QUICK DISCONNECT COUPLING. LEAK CHECK OK. 2 L 7 2 4F RT A28NM 2001011601243 20010116 01243 NM 2001 1 16 0100045638 1 20010106 A 3240 SMOKE BOEING 757 757251 1384970 NM LT MLG WW DETECTED A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 01 538US 26485 AFTER LANDING, THE TOWER REPORTED A TYPE OF SMOKE COMING FROM THE LEFT MAIN GEAR AREA. ROLLED EMERGENCY EQUIPMENT WITH NO ABNORMALITIES NOTED. FLIGHT ATTENDANT REPORTED ACRID SMELL IN CABIN UPON TAXI IN. MAINTENANCE INSPECTED BRAKES. NO TROUBLE FOUND. 2 L 7 2 4F RT A2NM 2001011601244 20010116 01244 NM 2001 1 16 0100056729 1 20010102 A 2612 2156646 FIRE DETECTOR BOEING 747 747251F 1384898 NM MAIN CARGO BAY FALSE INDICATION A NWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 01 629US 5138 1038 22388 DURING CRUISE, THE MAIN DECK FIRE WARNING BELL SOUNDED AND LIGHT ILLUMINATED. AIRCRAFT DECLARED AN EMERGENCY AND DIVERT ED TO YWG AND LANDED WITHOUT INCIDENT. REPLACED THE MAIN DECK 1B FIRE DETECTOR AND TEST SWITCH. OPERATIONAL CHECK GOOD . 2 L 7 4 4F A20WE 2001011601245 20010116 01245 NE 2001 1 16 0100089863 2 20010106 A 7510 320115 VALVE DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE RT ENGINE STUCK A NWAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 01 772NC 47774 688294 DURING TAKEOFF ROLL, THE RIGHT ENGINE LEFT ANTI-ICE VALVE LIGHT ILLUMINATED. ABORTED TAKEOFF AT 110 KNOTS WITHOUT INDIC ENT. AIRCRAFT RETURNED TO GATE. MAINTENANCE REPLACED THE LEFT ANTI-ICE VALVE LOCATED ON THE RIGHT ENGINE AND PERFORMED A REJECTED TAKEOFF INSPECTION. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F 4 F RT A6WE E2EA 2001011601255 20010116 01255 WP 2001 1 16 DHL2001805003 1 20010112 A 2760 LIMIT SWITCH DOUG DC8 DC873F 302199F WP SPOILER PUMP FAILED A DHLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 805DH 46125 SPOILER PRESS 0 PERFORMED ALT PROCEDURE. REMOVED AND REPLACED SPOILER PUMP CURRENT LIMITERS. OPS OK PER M/M 27-62-0. 2 L 7 4 4F RT 4A25 2001011601262 20010116 01262 EU 2001 1 16 0100113208 1 20010110 A 5311 FRAME AIRBUS 320 A320211 3930320 EU FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 308US 107 DURING H-CHECK, FOUND CORROSION ON LT FRAME 68 SURROUNDING THE NUT PLATE HOLE AT FLOOR SILL AREA. REPAIRED PER EA 32-18 1432. 2 L 7 2 4F RT A28NM 2001011601280 20010116 01280 NM 2001 1 16 CALA0100009 1 20010109 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND FLOORBEAM CORRODED AT STA 1006, LBL 10. THE FLOORBEAM WAS REMOVED AND REPLACED IAW ECRA 5310-03851, RE V A. 2 L 7 2 4F RT A16WE 2001011601281 20010116 01281 NM 2001 1 16 CALA0100010 1 20010109 A 5210 INTERCOSTAL BOEING 737 7373T0 1384582 NM PAX DOOR GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND L-1 DOOR INTERCOSTAL GOUGED BELOW UPPER SPIGOT BUSHING. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW S RM 51-10-02 AND 51-40-2. 2 L 7 2 4F RT A16WE 2001011601282 20010116 01282 NM 2001 1 16 CALA0100011 1 20010110 A 5330 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND A GOUGE IN INTERIOR SKIN AT CENTER BAY FOR L-1 TORQUE TUBE AT STA 303, STRINGER 11L. A NEW SECTION OF SKIN PANEL WAS INSTALLED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001011601283 20010116 01283 NM 2001 1 16 CALA0100013 1 20010111 A 5315 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14381 26310 INSPECTION FOUND FLOORBEAM CAP CORRODED AT STA 344, LBL 25. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-51, FIGURE 203 . 2 L 7 2 4F RT A16WE 2001011601284 20010116 01284 NM 2001 1 16 CALA0100014 1 20010111 A 5310 FRAME BOEING 737 7373T0 1384582 NM WINDOW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND A .25 INCH CRACK AT UPPER LEFT CORNER OF THE L-1 WINDOW FRAME. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-10-01, FIGURE 210, SHEETS 1-4. 2 L 7 2 4F RT A16WE 2001011601285 20010116 01285 EA 2001 1 16 SWIA972257 1 20010108 A 3260 PROXIMITY SWITCH CNDAIR CL600 CL6002B19 EA NLG OUT OF ADJ A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 413SW 7102 ON TAKEOFF NOSE GEAR WOULD NOT RETRACT. RETURNED TO SLC. ADJUSTED NOSE GEAR PROXIMITY SWITCH IAW MM 32-61-05. SWUNG G EAR. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2001011601286 20010116 01286 NM 2001 1 16 QXEA0100015 1 20010110 A 6123 CONTROLLER DHAV DHC8 DHC8102 2809003 NM AUTOFEATHER SYS WILL NOT TEST A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 825PH 213 LWS - AUTOFEATHER WILL NOT TEST. CYCLED POWER LEVERS AND CONDITION LEVERS FULL TRAVEL NUMEROUS TIMES. TEST NORMAL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001011601287 20010116 01287 NM 2001 1 16 QXEA0100016 1 20010111 A 6123 CONTROLLER DHAV DHC8 DHC8202 2809007 NM FEATHER SYSTEM MALFUNCTIONED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 828PH 526 IDA - NR 2 PROP WILL NOT COME OUT OF FEATHER. GROUND RUN, COULD NOT DUPLICATE. NO PARTS REPLACED. AIRCRAFT RETURNED T O SERVICE. 2 H 7 2 4T RT A13NM 2001011601352 20010116 01352 WP 2001 1 16 MWEA010016 1 20010108 A 5320 99115451 FLOOR SUPPORT DOUG DC9 DC914 3022034 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 FRAME STATION 256 CENTERLINE FLOOR SUPPORT HAS .30 DIAMETER HOLE THRU UPPER LEG OF FLOORBEAM. FABRICATED AND INSTALLED REPAIR ANGLES AND FILLERS. 2 L 7 2 4F A6WE 2001011601412 20010116 01412 EU 2001 1 16 RAIA0101005 1 20010108 A 5610 NP1588013 WINDSHIELD AEROSP ATR42 ATR42300 8680920 EU COCKPIT CRACKED A RAIA O OTHER O OTHER CR CRUISE 1 CE 03 424TE 124 7541-STL- DURING CRUISE CAPTAINS FOREWARD WINDSHIELD CRACKED. MAINTENANCE REMOVED AND REPLACED THE WINDSHIELD IAW ATR42 MAINTENANCE MANUAL. 2 H 7 2 4T RT A53EU 2001011601472 20010116 01472 EA 2001 1 16 SWIA972256 1 20010107 A 2731 TRIM SWITCH CNDAIR CL600 CL6002B19 EA HORIZONTAL STAB MALFUNCTIONED A SWIA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 NM 07 416SW 7089 INFLIGHT THE STAB TRIM AND MACH TRIM DISCONNECTED AND WOULD RESET ONLY AFTER THE F/O TRIM DISCONNECT WAS CYCLED 4 OR 5 T IMES. POWER DOWN AIRCRAFT. OPERATIONAL CHECK OF HSTCU. OPS CHECKS GOOD IAW MM 27-41-01. RAN HORIZONTAL STABILIZER IA W MM 27-40-00 STAB TRIM AND MACH TRIM OPS CHECKS GOOD. UNABLE TO DUPLICATE DISCREPANCY. 2 L 7 2 4F RT A21EA 2001011601473 20010116 01473 SO 2001 1 16 SWIA972258 1 20010108 A 2752 ACTUATOR EMB 120 EMB120RT SO PWA 118 PW118 NE TE FLAPS MALFUNCTIONED A SWIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 162CA 120150 CONTROL FAULT ON FLAP DURING RETRACTION ON GROUND. PRESS RESET AS PER QRH, FAULT CLEARED BUT REOCCURS WHEN RESELECTING FLAPS TO 15 DEGREES. INSTALLED SERVICEABLE LEFT NACELLE ACTUATOR AS PER RII 27-307. OPS CHECK. P/N ON 308200-1007, S/ N ON 0195, S/N OFF 0402. 2 L 7 2 4T 4 T RT A31SO E20NE 2001011601475 20010116 01475 2001 1 16 SWIA972260 4 20010109 A 3418 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE STALL WARNING ACTIVATED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 903SW 7425 STALL FAIL MESSAGE ON TAKEOFF ROLL. ABORTED TAKEOFF. PERFORMED STALL WARNING TEST AND CHECK STALL VANES. OPS CHECK GO OD. COULD NOT DUPLICATE. 2 L 7 2 4F 4 F RT A21EA E15NE 2001011601476 20010116 01476 SO 2001 1 16 SWIA972261 1 20010109 A 2750 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS CONTAMINATED A SWIA O OTHER N FALSE WARNING DE DESCENT 1 NM 07 188SW 120039 FLAP DISAGREEMENT ON SELECTION OF FLAP 45 DEGREES (OUTBOARD FLAPS WOULD NOT EXTEND BEYOND LAST LIGHT BAR ON FLAP ANNUNCI ATOR PANEL). FOUND GLYCOL IN LEFT OUTBOARD CANNON PLUG. CLEANED PLUG. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001011601478 20010116 01478 WP 2001 1 16 MWEA010006 1 20010105 A 5313 59114129 LONGERON DOUG DC9 DC914 3022034 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 LONGERON 28 AT STATION 348 HAS A HOLE. FABRICATED AND INSTALLED NEW LONGERON. 2 L 7 2 4F A6WE 2001011601479 20010116 01479 WP 2001 1 16 MWEA010007 1 20010105 A 5313 59164411 LONGERON DOUG DC9 DC914 3022034 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 STATION 279 HAS HOLE IN LONGERON 29 LEFT JUST ABOVE FORWARD ANNTENA. FABRICATED AND INSTALLED NEW LONGERON. 2 L 7 2 4F A6WE 2001011601480 20010116 01480 WP 2001 1 16 MWEA010008 1 20010105 A 5311 59125251 FRAME DOUG DC9 DC914 3022034 WP FUSELAGE CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 FRAME AT STATION 737 IS CHAFED ON AFT SIDE BETWEEN LONGERONS 10R - 11R. FABRICATED AND INSTALLED FRAME REPAIR. 2 L 7 2 4F A6WE 2001011601481 20010116 01481 WP 2001 1 16 MWEA010009 1 20010105 A 5311 5911447505 FRAME DOUG DC9 DC914 3022034 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 GOUGE IN RADIUS OF FRAME 465, ABOVE LONGERON 10R. FABRICATED AND INSTALLED FILLER, ANGLE AND ANGLE SPLICE, AND DOUBLER REPAIR PLATE. 2 L 7 2 4F A6WE 2001011601482 20010116 01482 WP 2001 1 16 MWEA010010 1 20010105 A 5310 995821411 SHEAR TIE DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 SHEAR CLIP AT STATION 711 HAS LIGHT CORROSION ON FORWARD SIDE BETWEEN LONGERON 17 RIGHT AND 18 RIGHT. FABRICATED AND IN STALLED SHEAR CLIP. 2 L 7 2 4F A6WE 2001011601507 20010116 01507 SO 2001 1 16 SWIA972246 1 20010104 A 2930 WARNING LIGHT EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE HYD SYSTEM ILLUMINATED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 284YV 120284 AFTER TAKEOFF GREEN SYSTEM HYDRAULIC FILTER LIGHT AND HYDRAULIC MAP LIGHT ILLUMINATED AFTER GEAR RETRACTION. RETURNED T O LAX. REMOVED GREEN SYSTEM ENGINE PUMP RETURN FILTER AND INSPECTED NO PARTICLES NOTED. INSTALLED NEW FILTER AND RESET BYPASS INDICATOR PIN. RUN UP FOR OPS AND LEAK CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001011700291 20010117 00291 NM 2001 1 17 0100072286 1 20010107 A 3231 FITTING BOEING 727 727251 138408H NM DOOR ACTUATOR LOOSE A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 286US 21325 INBOUND TO MSP AND ON FINAL APPROACH, CREW RECEIVED GEAR DOOR WARNING LIGHT. CREW PERFORMED COM PROCEDURE AND CYCLED GE AR. AFTER SECOND RECYCLE, CREW RECEIVED ALL GREEN DOWN AND LOCKED INDICATION. FLIGHT MADE AN UNEVENTFUL LANDING. MSP MAINTENANCE TIGHTENED LOOSE BOLTS ON DOOR MOUNTED ACTUATOR FITTING. OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 2001011900007 20010119 00007 NM 2001 1 19 2001UALA00003 1 20010102 A 3350 TRANSFORMER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN INOPERATIVE A UALA O OTHER L NO TEST UK UNKNOWN 1 WP 29 207UA 30213 TWO ADJACENT EEL LIGHTS INOP ON SEAT 2E. REPLACED EEL TRANSFORMER AND LIGHTS CHECK GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001020500040 20010205 00040 2001 2 5 2001UALA00004 4 20010104 A 3425 25883024 GYRO BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE COCKPIT FAILED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 993UA 22383 PROBLEM WITH THE CAPTAINS HORIZONTAL SITUATION INDICATOR. *S/D* REPLACED THE NR 1 DIRECTIONAL GYRO. OPS CHECKED NORMA L. 2 L 7 2 4F 4 F A16WE E2EA 2001011900008 20010119 00008 NM 2001 1 19 2001UALA00005 1 20010103 A 3397 WIRE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 795UA 26927 TWO ADJACENT EEL LIGHTS ON SEAT 1E INOP. REPLACED SEAT CABLE. CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001011900009 20010119 00009 NM 2001 1 19 TWAA0100801 1 20010111 A 3350 85 LAMP BOEING 757 7572Q8 1384972 NM COCKPIT INOPERATIVE A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 702TW 28162 THE EGRESS SYSTEM SWITCH LIGHT WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 10-17-99 LAX. 2 L 7 2 4F RT A2NM 2001011900010 20010119 00010 2001 1 19 TWAA0100802 4 20010111 A 2330 75625688001 HARNESS BOEING 767 7673Y0 NM SEAT 3D SHORTED A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 640TW 25411 WHEN THE PASSENGER IN SEAT 3C RECLINED HIS SEAT SPARKS WERE REPORTED FROM UNDER THE SEAT. BURNING INSULATION SMELL REPO RTED. BOTH IN-SEAT VIDEO UNITS IN THIS SEAT BECAME INOPERATIVE AND THE VIDEO UNIT AT 3G BECAME INOPERATIVE. NO CIRCUIT BREAKERS IN THE COCKPIT OPENED. NO DAMAGE FOUND BY CREW. REPLACED THE CENTER CONSOLE UNIT AT SEAT 3D. CHECK-C 5-15-0 0. 2 L 7 2 4F RT A1NM 2001011900011 20010119 00011 NM 2001 1 19 SPAA0100041 1 20010109 A 3350 1000679 LIGHT BOEING 737 7372T4 1384492 NM L-2 DOOR INOPERATIVE A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 28 703S 22529 DURING ACCOMPLISHMENT OF PRE-FLIGHT CHECK FOUND EMERGENCY EXIT LIGHT AT L-2 DOOR INOPERATIVE. REMOVED AND REPLACED EMER GENCY EXIT LIGHT IAW B737 MM 33-51-101. OPERATIONAL CHECK GOOD. 2 L 7 2 4F A16WE 2001011900012 20010119 00012 NM 2001 1 19 AWXA0001242 1 20010111 A 5312 672036 WEB BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER UK UNKNOWN 1 WP 28 331AW 42277 23747 CRACKED LIGHTENING HOLE ON VERT SUPPORT WEB AT WL 195 RBL 17 FS 180. CUT OUT DAMAGE; HFEC SHOWS NO CRACKS; FABED REPAIR DOUBLER AND INSTALLED IAW SRM 51-70-13; HFEC COMPLIED WITH B737 NTM PT 6 51-00-00 FIG 23. 2 L 7 2 4F RT A16WE 2001011900013 20010119 00013 NM 2001 1 19 AWXA0001241 1 20010111 A 5312 65C37607 STRUCTURE BOEING 737 7373Y0 1384671 NM PRESSURE BLKHD CRACKED A AWXA K NONE O OTHER UK UNKNOWN 1 WP 28 331AW 23747 STA 178 WL 207 FWD PRESSURE BULKHEAD AFT SIDE CRACK .5 INCH LONG SIDE CORD LT SIDE. REMOVED DAMAGED CORD; DRILLED AND I NSTALLED REPLACEMENT CORD SECTION AND SPLICES IAW ER 03-5312-01002-DL1. 2 L 7 2 4F RT A16WE 2001011900014 20010119 00014 NM 2001 1 19 AWXA0001240 1 20010111 A 5312 651758351 STRUCTURE BOEING 737 7373Y0 1384671 NM PREESURE BLKHD CRACKED A AWXA K NONE O OTHER UK UNKNOWN 1 WP 28 331AW 23747 STA 178 WL 190 FWD PRESSURE BULKHEAD AFT SIDE CRACK 1.25 INCH VERT CORD LEFT O/B SIDE. REMOVED DAMAGED; FABED AND INSTA LLED ANGLE AND FILLERS IAW SRM 51-40-02, 53-10-08 FIG 205. 2 L 7 2 4F RT A16WE 2001011900015 20010119 00015 NM 2001 1 19 DHL2001705001 1 20010106 A 5330 SKIN BOEING 727 72722C 138400F NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 DURING SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FLA, A CRACK APROX .450 INCH LONG WAS FOUND IN THE FUSLAGE SKIN AT THE FWD RADIUS OF THE FWD ENTRY DOOR LOWER HINGE CUTOUT. CUT OUT CRACK, FABRICATED AND INSTALLED DOUBLER REPAIR PER SRM 51 -30-2. 2 L 7 3 4F A3WE 2001011900016 20010119 00016 NM 2001 1 19 AWXA0001239 1 20010111 A 5330 65C33930 SKIN BOEING 737 7373Y0 1384671 NM GRND A/C RECPT. GOUGED A AWXA K NONE O OTHER UK UNKNOWN 1 WP 28 331AW 23747 LWR FUSELAGE SKIN DOUBLER GOUGED AND TORN AT GROUND A/C RECEPTACLE. REMOVED EXISTING DOUBLER IAW SRM 51-40-02; INSTALLE D CONICAL WASHERS IAW 51-40-08; FABED REPAIR DOUBLER; TREATED AND PRIMED DOUBLER AND SKIN IAW 51-20-01; INSTALLED DOUBLE R IAW 51-40-02. 2 L 7 2 4F RT A16WE 2001011900017 20010119 00017 NM 2001 1 19 AWXA0001238 1 20010111 A 5313 69353506 TIE CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER UK UNKNOWN 1 WP 28 331AW 23747 STRINGER TIE CLIP CRACKED FS 500A STR 16R. REMOVED CRACKED TIE CLIP IAW SRM 51-40-02; FABED STRINGER TIE CLIP IAW DWG 6 9-35350; TREATED AND PRIMED IAW 51-20-01; INSTALLED IAW DWG 69-35350. 2 L 7 2 4F RT A16WE 2001011900018 20010119 00018 NM 2001 1 19 AWXA0001237 1 20010111 A 5320 651758365 WEB BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER UK UNKNOWN 1 WP 28 331AW 23747 CENTER WEB CRACKED FS 178 RBL 0.7 WL 187. REMOVED DAMAGED AREA IAW SRM 53-10-08, NDT - NO CRACKS NOTED PER B737 NTM PT 6, 51-00-00 FIG 23; FABED DOUBLER, FILLER, SHIM IAW SRM 53-10-05 FIG 203 AND INSTALLED REPAIR PARTS IAW 53-10-08 FIG 203 , 51-40-03 AND 51-40-05; TREATED AND PRIMED IAW 51-20-01. 2 L 7 2 4F RT A16WE 2001012200001 20010122 00001 NM 2001 1 22 SWAA010024 1 20010101 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD WEB CRACKS AT RBL 4.7, WL 213.25 - WL 213.75 & RBL 6.7, WL 213.25 - 2 13.75. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 2001012200002 20010122 00002 NM 2001 1 22 SWAA010013 1 20010102 A 2560 D31354 GIRT BAR BOEING 737 7373H4 1384600 NM AFT SVC DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 639SW 27712 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED EVAC SLIDE ASSY PE R MM. 2 L 7 2 4F RT A16WE 2001012200022 20010122 00022 NM 2001 1 22 AWXA0001235 1 20010111 A 5315 6545810129 FLOORBEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A AWXA K NONE O OTHER UK UNKNOWN 1 WP 28 331AW 42277 23747 CORROSION ON TOP SURFACE OF FLOORBEAM STA 312 RBL 7 - 13. REMOVED CORROSION - AREA OUT OF LIMITS IAW UT INSP PER B737 N TM PT 1, 54-04-00; MAT THICKNESS .100, MATERIAL LOSS .022. REMOVED UPPER CHORD IAW SRM 53-10-51; FABED REPLACEMENT UPPE R CHORD IAW 53-10-51; TREATED AND PRIMED REPLACEMENT CHORD IAW 51-10-02; INSTALLED REPLACEMENT UPPER CHORD IAW 53-10-51. 2 L 7 2 4F RT A16WE 2001012200033 20010122 00033 NM 2001 1 22 DL72L010009 1 20010102 A 3350 900542 BATTERY BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 501DA 21303 ON LAYOVER FOUND OVERHEAD EMERGENCY EXIT IDENTIFIER LIGHT INOP. CABIN AT FWD GALLEY IN AISLE. L1021 FWD LOWERED CEILING SIGN. FOUND ALL 6 VOLT 328 LAMPS BAD. RELAMPED, NO HELP. FOUND M1085 BATTERY CHARGER MODULE BAD. REPLACED M1085 MOD ULE AND BATTERY PACK. LIGHT NOW OPS NORMAL. 2 L 7 3 4F A3WE 2001012200034 20010122 00034 NM 2001 1 22 DL72S010015 1 20010104 A 5755 FITTING BOEING 727 727232 1384082 NM NR 4 SPOILER CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 538DA 22076 FOUND ON F1 LETTER CK, NR 4 SPOILER ACTUATOR I/B MOUNT FITTING IS CRACKED. REPAIRED PER MM 57-42-000-8. 2 L 7 3 4F A3WE 2001012200035 20010122 00035 NM 2001 1 22 DL757010020 1 20010105 A 3350 P4010021 BATTERY BOEING 757 757232 1384965 NM 2L DOOR DISCHARGED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 6707A 30395 EMERGENCY FLASHLIGHT AT 2L INOP. REPLACED BATTERY AND BULB CHECKS OK. 2 L 7 2 4F RT A2NM 2001012200036 20010122 00036 WP 2001 1 22 DLL14010026 1 20010106 A 3340 POWER SUPPLY 672320101 LKHEED 1011 1011385115 5265015 WP R1 DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 740DA 60848 193C1244 R1 EXTERIOR DOOR LIGHT DID NOT ILLUMINATE. REPLACED R1 POWER SUPPLY. 2 L 7 3 4F A23WE 2001012200037 20010122 00037 NM 2001 1 22 DL767010034 1 20010106 A 5330 143T3211 SKIN BOEING 767 767232 1385132 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 104DA 22216 THE FUSELAGE WAS STRUCK BY GROUND EQUIPMENT AT AN EXISTING REPAIR WHICH WAS INSTALLED BETWEEN FS 500 & 521 AND BETWEEN STRINGERS 33L & 39L. THE UPPER PORTION OF THE REPAIR WAS REMOVED AND THE ADDITIONAL SKIN DAMAGE REMOVED WITH AN ADDITIO NAL CUTOUT. A NEW ALUMINUM SKIN DOUBLER WAS INSTALLED AND INCORPORATED INTO THE EXISTING REPAIR PER ER/A 379697-14, REV B. 2 L 7 2 4F RT A1NM 2001012200038 20010122 00038 NM 2001 1 22 AWXA0001236 1 20010111 A 5320 6545815121 STIFFENER BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER UK UNKNOWN 1 WP 28 331AW 23747 INTERCOSTAL FWD VERTICAL STIFFENER CRACKED FS 344 LBL 10. REMOVED DAMAGED ANGLE IAW SRM 51-40-02; FABED ANGLE IAW 53-10 -51, 51-20-02 AND ENG RESPONSE DTD 01-05-01; TREATED AND PRIMED IAW 51-20-01; INSTALLED IAW 51-40-02. 2 L 7 2 4F RT A16WE 2001012200042 20010122 00042 NM 2001 1 22 AWXA0001234 1 20010111 A 5313 654576819 STRINGER BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER UK UNKNOWN 1 WP 28 331AW 42277 23747 STR CRACKED AT END FASTENER HOLE FUSE STA 500D + 15 INCHES, STR 16R. CUT OUT DAMAGED AREA OF STR; FABED REPAIR CHANNEL AND RADIUS FILLER; INSTALLED IAW AWA ER 03-5310-01003-JS2. 2 L 7 2 4F RT A16WE 2001012200043 20010122 00043 NM 2001 1 22 42458 1 20010111 A 5320 693535214 TIE CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE BENT A AWXA K NONE O OTHER UK UNKNOWN 1 WP 28 331AW 23747 AFT CARGO COMPT STA 727C STR 24L FRAME CLIP BENT. REMOVED AND REPLACED FRAME CLIP IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001012200044 20010122 00044 NM 2001 1 22 AWXA0001232 1 20010111 A 5320 672038502 INTERCOSTAL BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER UK UNKNOWN 1 WP 28 331AW 23747 STA 178 FWD PRESSURE BULKHEAD AFT SIDE CRACK 1.5 INCH LONG INTERCOSTAL RT SIDE WL 195. REMOVED AND REPLACED INTERCOSTAL RT SIDE IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001012200045 20010122 00045 NM 2001 1 22 AWXA0001231 1 20010111 A 5330 65457683 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE LIGHTNING STRIKE A AWXA K NONE O OTHER UK UNKNOWN 1 WP 28 331AW 42277 23747 LIGHTNING DISCHARGE MARK, FUSELAGE RT SIDE JUST ABOVE FWD CARGO DOOR BETWEEN FS 460 AND FS 480. REMOVED DAMAGED AREA PE R SRM 53-00-01; NDT CONDUCTED HFEC INSP PER B737 NDTM PT 6, 51-00-00 FIG 23. NO CRACKS NOTED AROUND CUTOUT; FABED FILLE R AND DOUBLER AND INSTALLED REPAIR PER 53-00-01 FIG 202. 2 L 7 2 4F RT A16WE 2001012200046 20010122 00046 NM 2001 1 22 AWXA0001233 1 20010111 A 5320 693535214 TIE CLIP BOEING 737 7373Y0 1384671 NM AFT CARGO BAY BENT A AWXA K NONE O OTHER UK UNKNOWN 1 WP 28 331AW 23747 AFT CARGO COMPT STA 727C STR 24L FRAME CLIP BENT. REMOVED AND REPLACED FRAME CLIP IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001012200047 20010122 00047 NM 2001 1 22 AWXA0001230 1 20010111 A 2730 MS2764837 BEARING BOEING BOEING 737 737277 1384570 NM ELEV.TORQUE TUBE WORN A AWXA K NONE F FLT CONT AFFECTED LD LANDING 1 WP 28 185AW 22652 ON LANDING FLARE IN SFO THE ELEVATOR CONTROL WAS STIFF. PERFORMED OPERATIONAL AND VISUAL INSPECTION OF ELEV CONTROL SYS TEM, NO DEFECTS NOTED. DUE TO PRIOR REPORT OF STIFF ELEV; BOEING WAS CONSULTED; PER THEIR RECOMMENDATION THE ELEV TORQU E TUBE BEARINGS WERE LUBRICATED AND THE AIRCRAFT MAINTENANCE FERRIED TO PHX FOR FURTHER TROUBLESHOOTING AND BEARING REPL ACEMENT. IN PHX FURTHER TROUBLESHOOTING WAS PERFORMED AND THE ELEV ACT INPUT TORQUE TUBE BEARINGS WERE REPLACED; ONE BE ARING WAS DRY AND WHEN ROTATED WAS ROUGH. AFTER REPLACEMENT A VERIFICATION FLIGHT WAS PERFORMED AND THE ELEV OPERATION WAS NORMAL. 2 L 7 2 4F RT A16WE 2001012200049 20010122 00049 NM 2001 1 22 DL757010005 1 20010101 A 3350 LIGHT 767GE BOEING 757 757232 1384965 NM RT FWD. OVERWING INOPERATIVE A DALA O OTHER L NO TEST IN INSP/MAINT 1 SO 27 669DN NONE 25142 RT OVERWING EMER SLIDE LIGHT INOP. 2 L 7 2 4F RT A2NM 2001012200051 20010122 00051 NM 2001 1 22 DL757010007 1 20010101 A 3244 B757M TIRE BOEING 757 757232 1384965 NM RT MAIN GEAR SEPARATED A DALA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SO 27 6708D DL728 30480 ON MONDAY JANUARY 1ST A/C 6708 BLEW NR 4 MAIN TIRE ON TAKEOFF FROM MIA. A/C 6708 RETURNED BACK TO MIAMI DUE TO THE INCI DENT. UPON INSPECTION AFTER LANDING THERE WAS MULTIPLE A/C DAMAGE CAUSED BY THE FAILURE OF NR 4 MAIN TIRE. REPLACED NR 3 AND NR 4 MAIN WHEEL ASSYS. REMOVED RT INBD FLAP TRACK TRUNNION FAIRING DUE TO DAMAGE. 2 L 7 2 4F RT A2NM 2001012200052 20010122 00052 NM 2001 1 22 DL738010008 1 20010102 A 2131 71211997101AC CONTROLLER BOEING 737 737832 13844CF NM E/E BAY INOPERATIVE A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 376DA 29624 ON TAKEOFF FROM CVG A/C DID NOT PRESSURIZE IN AUTO. NOT ABLE TO PRESSURIZE A/C WITH ALTERNATE MODE. FOUND NR 1 DCPC FA IL. T/S PER FIM 21-31 TASK 823-824 AND FIM21-31 TASK 825. REPLACED NR 1 DCPC, CKS GOOD PER FIM 21-31 TASK 825, PRESSURI ZED A/C, SYSTEM NORMAL. 2 L 7 2 4F RT A16WE 2001012200053 20010122 00053 NM 2001 1 22 DL72S010010 1 20010102 A 5754 ANGLE BOEING 727 727232 1384082 NM NR8 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 516DA 21432 FOUND ON MV2 CHECK, .75 INCH CRACK NR 8 SLAT COVE SKIN ANGLE BELOW THE ANTI-ICE DUCT. REPAIRED PER MM 57-54-000-8. 2 L 7 3 4F A3WE 2001012200054 20010122 00054 WP 2001 1 22 DLL14010011 1 20010102 A 3350 POWER SUPPLY 5165744 LKHEED 1011 1011385115 5265015 WP L3 DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1739D UNK 193C1237 L-3 DOOR EXT EMERGENCY LIGHT INOP. REPLACED POWER SUPPLY, CHECKS GOOD. 2 L 7 3 4F A23WE 2001012200055 20010122 00055 NM 2001 1 22 DL73K010012 1 20010102 A 5330 654580026 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 313DL 23085 A 1 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN JUST FORWARD OF THE LOWER AFT CORNER OF THE L1 DOOR. THE DAMAGE WAS REPAIRED PER BACO DWG 65C27257 AND BACO S/B 737-53-1083. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001012200056 20010122 00056 WP 2001 1 22 DLL19010014 1 20010104 A 2431 CIRCUIT BREAKER LS10159S5 LKHEED 1011 10113853 5265020 WP CABIN OVERHEAD FAILED A DALA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 27 765DA UNKNOW 193H1206 BATTERY CONDITION LIGHT ON CAT. REPLACED C/B AND REPAIRED WIRE TO C/B. 2 L 7 3 4F A23WE 2001012200057 20010122 00057 NM 2001 1 22 DL72S010016 1 20010104 A 5755 ANGLE BOEING 727 727232 1384082 NM NR 8 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 538DA 22076 A .25 INCH VISIBLE CRACK I/B OF STOP PAD NR 8 SLAT COVE SKIN ATTACH ANGLE. REPAIR PER MM 57-54-000-8. 2 L 7 3 4F A3WE 2001012200058 20010122 00058 NM 2001 1 22 DL72S010017 1 20010104 A 3350 BATTERY PACK 900542 BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 528DA 1172 21702 OVERWING EMERG EXIT LIGHT INOP. REPLACED BATTERY PACK AND TRAY, CKS GOOD. 2 L 7 3 4F A3WE 2001012200059 20010122 00059 NM 2001 1 22 DL73K010018 1 20010105 A 5311 FRAME BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 313DL 23085 A CRACK WAS FOUND AT THE LOWER FASTENER ON THE INNER CHORD OF THE LEFT AND RIGHT SIDE FS 616 FRAMES AT THE OVERWING FRA ME TO STUB JOINT. THIS IS THE TYPICAL CRACK OF S/B 737-53-1182. THE CRACK WAS CUT OUT AND THE AREA REPAIRED PER THE RE FERENCED S/B AT MV. 2 L 7 2 4F RT A16WE 2001012200060 20010122 00060 NM 2001 1 22 DL777010019 1 20010105 A 3810 COMPRESSOR BOEING 777 777232 1385232 NM CABIN OVERHEATED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 866DA 29738 A/C DIVERTED TO LGW DUE TO RUBBER SMELL IN AFT CABIN. FOUND POTABLE WATER COMPRESSOR OVERHEATED. 2 L 7 2 4F RT T00001SE 2001012200061 20010122 00061 NM 2001 1 22 DL764010021 1 20010102 A 2424 GCU 766300E BOEING 767 767432ER NM E/E BAY FAILED A DALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 27 830MH 36 29701 RIGHT BUS OFF AT LEVEL OFF WITH CORRESPONDING LOSS OF A/C COMPONENTS. BUS OFF REMAINED ILLUMINATED AFTER GEN RESET. FO UND RT GCU FAULT ON BITE CHECK. REMOVED AND REPLACED GCU. 2 L 7 2 4F RT A1NM 2001012200062 20010122 00062 NM 2001 1 22 DL767010022 1 20010104 A 5311 143T10663 FITTING BOEING 767 767232 1385132 NM FUSEAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 104DA 22216 THE CORNER SPLICE FITTING OF THE FS 500 FRAME AT STRINGER 33L WAS DAMAGED BY GROUND EQUIPMENT STRIKING THE AIRCRAFT. TH E DAMAGED FITTING WAS REMOVED AND A NEW FITTING MANUFACTURED AND INSTALLED PER ER/A 379704-14. 2 L 7 2 4F RT A1NM 2001012200063 20010122 00063 NM 2001 1 22 DL767010023 1 20010104 A 5330 143T33113 SKIN BOEING 767 767232 1385132 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 104DA 22216 THE FUSELAGE SKIN WAS STRUCK BY GROUND EQUIPMENT AT AN EXISTING REPAIR LOCATION AT FS 456 AND STRINGERS 33L-34L. THE R EPAIR WAS REMOVED AND ALL UNDERLYING DAMAGED CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALL ED PER B767 SRM 53-00-01 AND ER/A 379696-14. 2 L 7 2 4F RT A1NM 2001012200064 20010122 00064 NM 2001 1 22 DL72W010024 1 20010105 A 5520 SKIN BOEING 727 727247 138408F NM L/H ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2820W 21058 A .375 INCH CRACK IN LOWER SKIN OF LT ELEVATOR I/B AND FWD OF TAB CONTROL ROD CUTOUT. REPAIRED PER SRM 55-20-3. 2 L 7 3 4F A3WE 2001012200065 20010122 00065 NM 2001 1 22 DL76L010025 1 20010105 A 2530 COFFEEMAKER BOEING 767 767332 1382001 NM AFT GALLEY DIRTY A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 188DN 27583 AFT COFFEEMAKER SMELLS OF BURNING ODOR. COFFEEMAKER AND AREA CLEANED PULLED C/B AND FWD TO MCO. 2 L 7 2 4F RT A1NM 2001012200067 20010122 00067 NM 2001 1 22 DL767010030 1 20010106 A 2121 FAN BOEING 767 767232 1385132 NM LEFT CARGO AREA INOPERATIVE A DALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 27 109DL 22221 STRONG ODOR AND IRRITATING FUMES IN COCKPIT AT FL370. DECLARED EMERGENCY, O2 MASK ON, RETURNED TO CVG . LT RECIRCULATI ON FAN INOP, MESSAGE CAME ON DURING DESCENT. FOUND LT RECIRCULATION FAN INOP UPON ARRIVAL. PULLED AND COLLARED LT RECI RCULATION FAN C/B ON P-36 PANEL. INSPECTED LT RECIRCULATION FAN, FOUND NO FIRE DAMAGE IN DISTRIBUTION AREA. FWD TO MCO AND PLC PER MEL 21-25-01A. 2 L 7 2 4F RT A1NM 2001012200068 20010122 00068 WP 2001 1 22 DLL14010032 1 20010107 A 3350 337201956 LIGHT LKHEED 1011 1011385115 5265015 WP CABIN MISSING A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 737D 193C1228 FOUND EMERGENCY TRACK LIGHT AT SEAT 1C MISSING. REPLACED LAMP LENS AND SOCKET PER M/M, OPS CHECKS GOOD. 2 L 7 3 4F A23WE 2001012200069 20010122 00069 2001 1 22 DL73K010033 4 20010108 A 3418 STALL WARNING 693733921 BOEING 737 737232 1384475 NM COCKPIT MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 322DL D00329 23094 PASSING THROUGH FL260 STICK SHAKER WENT OFF. ALL FLT LEVELS, AIRSPEED, MACH, FUEL FLOW AND RPM READINGS WERE NORMAL. D IVERTED TO MCO. REPLACED STALL WARNING MODULE. OPN TEST GOOD. A/C DIVERTED FROM TPA. 2 L 7 2 4F RT A16WE 2001012200070 20010122 00070 NE 2001 1 22 DLM88010035 2 20010108 A 7250 JT8D219 BLADE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR1 ENGINE DAMAGED A DALA O OTHER R PARTIAL RPM/PWR LOSS AP APPROACH 1 SO 27 950DL 25792 0 49881 718170 ENCOUNTERED WINDSHEAR ON APPROACH TO TPA. HIT TOGA BUTTONS AND BEGAN CLIMB. HEARD LOUD THUMP WHEN POWER CAME UP ON LEF T ENGINE. LEFT ENGINE PRODUCED NO EPR FOR REMAINDER OF FLIGHT. FOUND BLADE DAMAGE. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A6WE E9NE 2001012200084 20010122 00084 NM 2001 1 22 SWAA010019 1 20010104 A 2560 P4010021 BATTERY BOEING 737 7375H4 138449D NM AFT CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 523SW 26565 DURING SCHEDULED RON CHECK, FOUND AFT CABIN LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PE R MM. 2 L 7 2 4F RT A16WE 2001012200085 20010122 00085 2001 1 22 SWAA010020 4 20010104 A 2565 23D22941 SLIDE BOEING 737 7372H4 138448C NM FWD ENTRY DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED A1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR LOW. REMOVED AND REPLACED EVAC SLI DE ASSY PER MM. 2 L 7 2 4F A16WE 2001012200086 20010122 00086 2001 1 22 SWAA010021 4 20010103 A 2565 22D22091 SLIDE BOEING 737 7372K6 NM AFT ENTRY DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR LOW. REMOVED AND REPLACED EVA C SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001012200087 20010122 00087 2001 1 22 SWAA010022 4 20010104 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT ENTRY LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR VIEW LENS LOOSE AND INDICATOR NOT VISIBLE. SECURED VIEW LENS PER MM. 2 L 7 2 4F RT A16WE 2001012200088 20010122 00088 NM 2001 1 22 SWAA010023 1 20010103 A 5320 BAC1503 STIFFENER BOEING 737 7373H4 1384600 NM MLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED 1/4D CHECK, FOUND BS 663 STIFFENER CRACKED AT LBL 7, WL 168. REMOVED AND REPLACED STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 2001012200089 20010122 00089 NM 2001 1 22 SWAA010025 1 20010102 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED 1/4D CHECK, FOUND LOWER FWD EMERGENCY FLASHLIGHT BROKEN. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2001012200094 20010122 00094 2001 1 22 SWAA010014 4 20010101 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM FWD ENTRY MISINSTALLED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 FWD ENTRY DOOR EMERGENCY EVAC SLIDE ASSY FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001012200095 20010122 00095 NM 2001 1 22 SWAA010015 1 20010103 A 5753 6573732 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 373SW 26581 DURING SCHEDULED RON CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2001012200096 20010122 00096 NM 2001 1 22 SWAA010016 1 20010102 A 2520 079123 COVER BOEING 737 7373H4 1384600 NM CABIN FLOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 635SW 27708 EEPLS TRACK COVER LOOSE AT ROW 15. SECURED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001012300045 20010123 00045 NM 2001 1 23 DL76L010028 1 20010105 A 2933 INDICATOR BOEING 767 767332 1382001 NM ADP PRESS MODULE LOOSE A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 177DN 25122 CTR HYD QTY EICAS MESSAGE CAME ON, QTY SHOWED 0.48 WITH MAIN ELEC PUMPS OFF QTY HELD AT 0.41. AUX PANEL ISLN LIGHT ILLU MINATED. FOUND DIFF PRESS IND ON ADP PRESS MODULE CAME LOOSE. REPLACED PACKING AND REINSTALLED DIFF PRESS IND PER MM 2 9-11-0. LEAK CHECK OK. 2 L 7 2 4F RT A1NM 2001012300046 20010123 00046 NM 2001 1 23 DLM88010029 1 20010106 A 2161 CONTROLLER 60714622 DOUG MD88 MD88 3023688 NM LT PACK MALFUNCTIONED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 916DL 073C4619 49591 FUMES IN COCKPIT AND CABIN WITH REDUCED POWER ON FINAL. SUSPECT ELECTRICAL OR AIR CONDITIONING, NO OTHER INDICATIONS. PER CAPTS VERBAL REPORT, CAPTAIN SMELLED FUMES FOR 3 FLIGHT LEGS AND THINKS IT IS GLYCOL (ANTI-ICE FLUID). SUSPECT LEFT PACK OVERTEMP. REPLACED LT PACK TEMP CONTROLLER, INSPECTED LT PACK PNEUMATIC DUCTING AND ACM. ACM OIL LEVEL FULL, RAN LT PACK SEVERAL HOURS, NO OVERTEMP OR SMELL NOTED. OK FOR FLIGHT. 2 L 7 2 4F RT A6WE 2001012300047 20010123 00047 NM 2001 1 23 DL757010037 1 20010106 A 2150 ACM 6806404 BOEING 757 757232 1384965 NM AC BAY MALFUNCTIONED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 6708D 4316 30480 CREW REPORTED BURNT RUBBER SMELL ON T/O. RAN ENGS RT PACK APPEARED TO BE SOURCE OF SMELL. REPLACED RT ACM. 2 L 7 2 4F RT A2NM 2001012300048 20010123 00048 NM 2001 1 23 DL757010038 1 20010108 A 3340 SWITCH MS25306222 BOEING 757 757232 1384965 NM COCKPIT SHORTED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 675DL NONE 25980 ON FINAL APPROACH A BURNING RUBBER ODOR ENTERED COCKPIT. ODOR INCREASED INTENSITY DURING TAXI IN AND BECAME LIKE ELECTR ICAL INSULATION. FOUND LT RUNWAY TURNOFF LIGHT SW SHORTING INTERNALLY AND OVERHEATING. FOUND SW AND WIRING BURNT. REP LACED SW AND WIRING PER MM. 2 L 7 2 4F RT A2NM 2001012300049 20010123 00049 NM 2001 1 23 DL76S010039 1 20010108 A 2933 S271T0054 INDICATOR BOEING 767 767332 1382001 NM LEFT ENG STRUT LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 128DL 24078 DURING CLIMB LEFT HYD QTY EICAS MSG ILLUMINATED. PER POM PRIMARY PUMP SELECTED OFF AND QTY CONTINUED TO DECREASE. DEMA ND PUMP SELECTED OFF WITH SAME RESULT. BOTH PUMPS OFF AND QTY STABILIZED. FOUND DPI ON LEFT HYD MODULE LEAKING. REPLA CED INDICATOR AND O-RINGS. SVCD HYD SYS. LEAK CKS GOOD. 2 L 7 2 4F RT A1NM 2001012300050 20010123 00050 NM 2001 1 23 DL72S010040 1 20010108 A 3350 S106 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 528DA 21702 OVERHEAD FWD EMERGENCY LIGHT AT ROW 13 INOP. REPLACED BATTERY PACK. CHECKS NORMAL. 2 L 7 3 4F A3WE 2001012300051 20010123 00051 NM 2001 1 23 DL73K010041 1 20010108 A 2120 65544671 DUCT BOEING 737 737232 1384475 NM FWD B/B-AFT AREA BLOWN A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 310DA 23082 SMOKE IN CABIN, RETURN TO BOSTON. REPLACED LT MIXING CHAMBER AND SUPPLY DUCT, LEAK CHECKED. NEEDS ENGINE RUN AND DUCT BURNOUT. PERFORMED SAME, CHECKS GOOD. 2 L 7 2 4F RT A16WE 2001012300052 20010123 00052 NM 2001 1 23 DL733010042 1 20010107 A 5312 651630087 FRAME BOEING 737 737347 1384647 NM BULKHEAD CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 306WA 23347 INSPECTIONS OF THE FS 178 BULKHEAD PER AD 200-05-29 REVEALED A 2 INCH CRACK IN THE RT SIDE CHORD AT WL 207. THE DAMAGED CHORD WAS REMOVED AND A NEW SECTION INSTALLED TO ELIMINATE THE CRACK CONDITION. THE REPAIR WAS ACCOMPLISHED PER ER/A 3 79675-14AD, REV A. 2 L 7 2 4F RT A16WE 2001012300092 20010123 00092 EU 2001 1 23 MALA010101 1 20010103 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 453XJ 453 FOUND DURING 4K-HEAVY CHECK, CORROSION ON SEAT TRACK BL 0 BETWEEN STA 630.112 AND 640. MAINTENANCE REPAIRED IAW EO 5307 7. 2 L 7 2 4T RT A52EU 2001012300093 20010123 00093 EU 2001 1 23 MALA010102 1 20010103 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 453XJ 453 FOUND DURING 4K-HEAVY CHECK, CORROSION ON SEAT TRACK (LT) BL18.3. MAINTENANCE REPLACED SEAT TRACK BETWEEN STA 294 - 377 IAW EO S53060. 2 L 7 2 4T RT A52EU 2001012300094 20010123 00094 EU 2001 1 23 MALA010103 1 20010103 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 453XJ 453 FOUND DURING 4K-HEAVY CHECK, CORROSION ON SEAT TRACK BL 0. MAINTENANCE REPLACED SEAT TRACK BETWEEN STA 294 TO 377 IAW E O S53060. 2 L 7 2 4T RT A52EU 2001012300095 20010123 00095 EU 2001 1 23 MALA010104 1 20010103 A 3030 SM5CXD4 RELAY SAAB SF340 SF340A 7850100 EU LT RELAY BAY MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 41XJ 041 LT PITOT, LT ALPHA, LT SIDE WINDOW LIGHT ILLUMINATED IN FLIGHT. DIVERTED DUE TO ICING CONDITIONS. MAINTENANCE REMOVED AND REPLACED 7XA RELAY IN LT RELAY BAY (P/N SM/5CXD4) OPS CHECK GOOD, LOAD TRANSFER OPS CHECK GOOD. ALSO RESET AC BUS C /B IN LT WHEEL WELL. ALL WORK DONE IAW SAAB AMM. 2 L 7 2 4T RT A52EU 2001012300096 20010123 00096 EU 2001 1 23 MALA010106 1 20010104 A 3040 7256110 WINDOW SAAB SF340 340B 7860101 EU COCKPIT MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 418XJ 418 RT SIDE WINDOW HEAT CAUTION LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE REMOVED AND REPLACED RT SIDE WINDOW, IAW SF 340 AM M 56-10-10. (P/N 7256110) (S/N OFF 1920), (S/N ON 0118), REFERENCE 409 CARD 034296. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2001012300097 20010123 00097 EA 2001 1 23 COMA0160083 1 20010110 A 2810 457370 CAP CNDAIR CL600 CL6002B19 EA LH WING LEAKING A COMA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 01 926CA 7027 FUEL LEAKING FROM LT WING FUEL CAP. REPLACED FUEL CAP. 2 L 7 2 4F RT A21EA 2001012300098 20010123 00098 EA 2001 1 23 COMA0160085 1 20010109 A 3222 STRUT CNDAIR CL600 CL6002B19 EA NLG MALFUNCTIONED A COMA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 01 960CA 7117 NLG DID NOT RETRACT, THUMPING NOISE FROM NLG AREA. SERVICED NLG SHOCK STRUT. 2 L 7 2 4F RT A21EA 2001012300099 20010123 00099 NM 2001 1 23 AWXA0001243 1 20010112 A 7931 313594 BUSHING PWA BOEING 737 737277 1384570 NM MAIN GEARBOX DAMAGED A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 179AW GZ6845 22646 P656859B NR 2 ENG LOW OIL PRESSURE LIGHT ILLUMINATED IN FLIGHT. CREW SHUT ENGINE DOWN AND COMPLETED CHECK LIST. THE ENGINE MAIN TAINED POSITIVE OIL PRESSURE THROUGHOUT THE FLIGHT; ENGINE WINDMILLED 25 - 30 MINUTES. MAINTENANCE FOUND THE HSG PLUG B USHING THREADS DAMAGED AND THE O-RING BLOWN OUT; THE PLUG WAS INSTALLED AT THE LP5 PORT ON THE MAIN GEARBOX; THE FITTING WAS REPLACED AND MAIN OIL FILTER INSPECTED, NO DEBRIS FOUND. ENGINE RUNS CHECKED GOOD. 2 L 7 2 4F RT A16WE 2001012300100 20010123 00100 SO 2001 1 23 GLBA20010002 1 20010110 A 2752 CONNECTOR EMB 120 EMB120 3260201 SO FLAP ACTUATOR CONTAMINATED A GLBA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 01 96ZK 12096 RETURN TO BLOCK - FLAP DISAGREEMENT AFTER T/O. CLEANED AND REMOVED GLYCOL FROM ACTUATOR CANNON PLUG, OPS CHECKED SYSTEM GOOD. 2 L 7 2 4T RT A31SO 2001012300101 20010123 00101 NM 2001 1 23 F3LA200100006 1 20010114 A 2610 100012701 CONTROL UNIT BOEING 737 73736Q 1384409 NM AFT CARGO MALFUNCTIONED A F3LA K NONE L NO TEST UK UNKNOWN 1 NM 03 307FL 12 28760 UPON ARRIVAL, MAINTENANCE REPORTED CARGO COMPARTMENT FIRE DETECTION/SUPPRESSION SYSTEM OK LIGHT WOULD NOT ILLUMINATE. R EPLACED CENTRAL CONTROL UNIT AND SYSTEM CHECKED OK. SYSTEM WAS ACTIVATED ON 1/12/01. 2 L 7 2 4F RT A16WE 2001012300102 20010123 00102 NM 2001 1 23 F3LA200100007 1 20010112 A 5310 SHEAR TIE BOEING 737 737228 13844AG NM FWD CARGO COMPT. CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 234TR 3086 23004 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON STRINGER TO FRAME TIE CLIP IN FORWARD CARGO COMPARTMENT STA 540, STR 25L. FABRICATED AND INSTALLED REPLACEMENT TIE CLIP PER SRM 53-10-2, 51-30-4 AND 51-30-2. 2 L 7 2 4F RT A16WE 2001012300103 20010123 00103 NM 2001 1 23 UPS01234615 1 20010113 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:N/A, LEFT AFT OVERWING SIDE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK AND EXIT ID PL ATE. OPS TEST GOOD. 2 L 7 3 4F A3WE 2001012300104 20010123 00104 NM 2001 1 23 UPS01234616 1 20010113 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:N/A, AFT CABIN ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, OPS TEST GOOD. 2 L 7 3 4F A3WE 2001012300105 20010123 00105 NM 2001 1 23 UPS01234617 1 20010112 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM LT GALLEY DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:N/A, LEFT GALLEY EMERGENCY LIGHT ON BULKHEAD INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2001012300106 20010123 00106 NM 2001 1 23 UPS01234618 1 20010112 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM GALLEY DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:N/A, EMERGENCY LIGHT LOWER GALLEY DUCT INOP. REMOVED AND REPLACED EXIT ID PLATE AND BATTERY PACK. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2001012300107 20010123 00107 NM 2001 1 23 UPS01234619 1 20010112 A 2560 BATTERY BOEING 727 72731C 1384011 NM AFT BULKHEAD DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:N/A, FLASHLIGHT ON BULKHEAD AFT OF LAV NEEDS NEW BATTERIES. REMOVED AND REPLACED BATTERIES IN FLASHLIGH T REAR BULKHEAD TOILET COMPARTMENT. OPS CHECK SATISFACTORY. 2 L 7 3 4F A3WE 2001021300402 20010213 00402 NM 2001 2 13 2001UALA00002 1 20010103 A 2751 INDICATOR BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE TE FLAP FAILED A UALA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 951UA 26696 FLAP ASYMMETRY INDICATION. *S/D* REPLACED FLAP INDICATOR. OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2001012500009 20010125 00009 NM 2001 1 25 DLM88010031 1 20010107 A 2120 UNKNOWN DOUG MD88 MD88 3023688 NM COCKPIT ODOR A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 972DL 53215 ELECTRICAL ODOR THROUGH OUT CABIN AND COCKPIT, AIRBORNE. RETURNED TO A-03. MIXED REPORTS FROM THE FLIGHT CREW ON THE EXACT ODOR. AIRCRAFT WAS INSPECTED AT THE GATE FOR ANY ELECTRICAL PROBLEMS OR POPPED CIRCUIT BREAKERS, NONE NOTED. APU AND PACKS WERE OPERATED, WITH NO ODOR NOTED. NR 2 ENGINE WAS REPLACED 01/06/01, AND FLT 356 WAS THE FIRST FLT SINCE EN G CHANGE. 2 L 7 2 4F RT A6WE 2001012500010 20010125 00010 2001 1 25 DL757010036 4 20010106 A 3440 INDICATOR BOEING 757 757232 1384965 NM NAVIGATION MALFUNCTIONED A DALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 27 620DL 22910 LOST NAV ALIGNMENT ON TAKEOFF ROLL. IN ALIGN MODE AT RETURN TO GATE. T/S PER FIM, NO PROBLEMS FOUND. REPLACED INITIAL REF MODE PANEL AS PRECAUTION. PERFORMED IRS OPERATIONAL TEST PER M/M, ALL TESTS NORMAL. 2 L 7 2 4F RT A2NM 2001012500011 20010125 00011 NM 2001 1 25 DLM11010043 1 20010105 A 5311 AFA78231 FRAME DOUG MD11 MD11 3023602 NM FUSELAGE CUT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 807DE 48478 THE FS 1681 FRAME WAS CUT AT LONG 47R AND THE FRAME SECTION FROM FS 47R TO THE FACTORY SPLICE AT 47L. THE FRAME SECTION WAS REMOVED TO ALLOW ACCESS TO UNDERLYING STRUCTURE. THE FRAME WAS REINSTALLED WITH THE FACTORY SPLICE AT L-47L AND A N IDENTICAL SPLICE AT L-47R. THE REPAIR WAS ACCOMPLISHED PER ER/A 379699-14, REV A. 2 L 7 3 4F RT A22WE 2001012500012 20010125 00012 NM 2001 1 25 DL757010044 1 20010106 A 7120 311N32613 MOUNT BOEING 757 757232 1384965 NM NR1 ENGINE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 608DA 22815 THE FWD INBD GUIDE PIN HOLE ON THE NR 1 ENGINE AFT MOUNT WAS OVERSIZED TO 1.126 INCH DIA TO CLEAN UP DAMAGE FROM A MIGR ATED BUSHING. A NEW OVERSIZE BUSHING WAS INSTALLED TO RESTORE THE AREA. THE REPAIR WAS ACCOMPLISHED PER B757 SRM 54-51 -02-2, FIG 202 AND ER/A 378101-14, REV A. 2 L 7 2 4F RT A2NM 2001012500013 20010125 00013 NM 2001 1 25 DL757010045 1 20010109 A 2910 273N21081 FITTING BOEING 757 757232 1384965 NM RT MLG BROKEN A DALA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 27 674DL 25979 LOST LEFT HYDRAULIC SYSTEM ON LANDING. FOUND PRESSURE LINE ON TOP OF RT MLG RETRACT CYL FITTING BROKEN OFF. REPLACED F ITTING AND REINSTALLED HYD LINE, LEAK CHECKS GOOD. REPLACED LT ACMP CASE DRAIN AND LT EDP CASE DRAIN FILTERS, LEAK CHEC KS GOOD. 2 L 7 2 4F RT A2NM 2001012500014 20010125 00014 NM 2001 1 25 DL757010046 1 20010109 A 2120 UNKNOWN BOEING 757 757232 1384965 NM COCKPIT ODOR A DALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 27 642DL 23996 AT CRUISE ALT FL 390 3 HRS AFTER DEPARTURE THERE WAS A FAINT SMELL OF A/C SMOKE IN THE COCKPIT AND FWD CABIN. AFTER APP ROX 10 - 15 MINS FWD LAV SMOKE ALARM SOUNDED PACKS INDICATED NORMAL. NO VISUAL SMOKE JUST ODOR. RAN PACKS WITH APU AND ENG PNEUMATICS. RAN ENGS TO 1.23 EPR, NO ODOR NOTICED. INSP CARGO COMPARTMENTS FWD/MID E/E BAYS AND E5 RACK. NO PROBLEMS FOUND. OPERATED IFE SYSTEM AND FWD GALLEY EQUIP, NO PROBLEMS FOUND. CHECKED SIDEWALL AND OVERHEAD LIGHTS FOR OPS, ALL CHECKS NORMAL. 2 L 7 2 4F RT A2NM 2001012500015 20010125 00015 NM 2001 1 25 DL72S010047 1 20010109 A 5532 SKIN BOEING 727 727232 1384082 NM VERTICAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 535DA 22048 A CRACK WAS FOUND IN THE RT SIDE SKIN OF THE VERTICAL STABILIZER EMANATING FROM UNDER THE FUSELAGE TO STABILIZER CREASE CHORD AT STA 1209. THE CRACK IS REPAIRED WITH AN EXTERNAL DOUBLER INSTALLED PER SRM 55-30-3, FIG 7 AND PER THE REQUIREM ENTS OF ER/A 379749-14. 2 L 7 3 4F A3WE 2001012500016 20010125 00016 NM 2001 1 25 DL72W010048 1 20010110 A 5330 SKIN BOEING 727 727247 138408F NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W 21057 A 2.75 INCH LONG CRACK WAS FOUND IN THE UPPER SKIN AT THE UPPER FASTENER ROW OF THE STRINGER 26L SKIN LAP JOINT AT FS 70 0. THE DAMAGED SECTION OF SKIN WAS CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOULBER PER B727 SRM 53-30-3, FIG 14 AND ER/A 379754-14. 2 L 7 3 4F A3WE 2001012500017 20010125 00017 NM 2001 1 25 DL73E010049 1 20010108 A 5753 654642833 FLAP TRACK BOEING 737 7372S3 NM LH WING CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 369DL 21776 INSPECTION OF THE INBD FLAP TRACK OF THE OUTBD FLAP ON THE LT WING REVEALED EXTENSIVE PITTING CORROSION. THE FLAP TR ACK WAS REMOVED AND DISCARDED. A NEW FLAP TRACK WAS INSTALLED PER ER/A 379729-14AD. 2 L 7 2 4F RT A16WE 2001012500018 20010125 00018 NE 2001 1 25 DL757010051 2 20010110 A 7230 BLADE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR1 ENGINE DAMAGED A DALA K NONE C F.O.D. IN INSP/MAINT 1 SO 27 657DL 19182 24419 ON WALKAROUND IN LAX FOUND NR 1 ENGINE BLADES NICKED. NR 1 ENGINE BLENDED 3 BLADES MARKED PER MM 72-31-02-06 FIGURE 605 . 2 L 7 2 4F 4 F RT A2NM E17NE 2001012500019 20010125 00019 NM 2001 1 25 DL767010052 1 20010110 A 2450 HARNESS BOEING 767 767232 1385132 NM E/E BAY BURNED A DALA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 104DA 22216 MULTIPLE EICAS WARNINGS AND ELECTRICAL BURNT SMELL IN COCKPIT AND MID CABIN. FOUND INBOARD MOST WIRE BUNDLE IN RIGHT HA ND TUNNEL AREA OF MAIN E AND E AT STATION 266.5 BURNT. WIRE BUNDLE NUMBER W451 AT CABIN FLOOR LEVEL. REPLACING WIRES, INTERNAL INVESTIGATION UNDERWAY. 2 L 7 2 4F RT A1NM 2001012500020 20010125 00020 NM 2001 1 25 DL757010053 1 20010110 A 3350 BPS73 POWER SUPPLY BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 678DL 25983 FIRST CLASS ESCAPE PATH LIGHTING INOP. REPLACED THE POWER SUPPLY AND BATTERY PACK. CHECKS GOOD. 2 L 7 2 4F RT A2NM 2001012500021 20010125 00021 NM 2001 1 25 DL72S010055 1 20010110 A 3350 BATTERY S10690083 BOEING 727 727225A 1384077 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8891Z 21860 MID CABIN OVERHEAD EMERGENCY LIGHTS AND R2 EMERGENCY LIGHTS INOP. REPLACED BATTERIES AND BATTERY PACK. 2 L 7 3 4F RT A3WE 2001012500022 20010125 00022 NM 2001 1 25 DL73K010056 1 20010111 A 2120 655447015 DUCT BOEING 737 737232 1384475 NM AIR MIX CHAMBER DETACHED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 315DL 23087 FLT ATTENDANT AND PAX NOTED SEAT RAIL AND FLOOR AROUND 7ABC IS WARM, TOO HOT TO THE TOUCH. FLT ATTENDANTS REPORTS HEAT SMELL IN AREA. FOUND LT SIDE MIX CHAMBER DISINTEGRATED AND LT HOT AIR SUPPLY DUCT SEPARATED FROM CHAMBER. REPLACED MIX CHAMBER. 2 L 7 2 4F RT A16WE 2001012500023 20010125 00023 NM 2001 1 25 DL72E010057 1 20010111 A 5350 RADOME 284A18013 BOEING 727 727247 138408F NM PWA JT8 JT8D15 52051 NE NOSE BIRD STRIKE A DALA O OTHER C F.O.D. TO TAKEOFF 1 SO 27 831WA 762 21483 BIRD STRIKE ON T/O IN BWI. AIRSPEED INDICATORS DIFFER AT FL 240. ENGINE PARAMETERS NORMAL. REPLACED RADOME PER MM. A LSO, CLEARED DEBRIS FROM CO-PILOTS PITOT TUBE. TESTED PITOT SYSTEM IAW M/M. NO SPLITS NOTED. 2 L 7 3 4F 4 F A3WE E2EA 2001012500024 20010125 00024 2001 1 25 SWAA010063 4 20010109 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT SVC DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 074SW 22674 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001012500025 20010125 00025 NM 2001 1 25 SWAA010064 1 20010109 A 3350 610478 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN OUT OF POSITION A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 344SW 24152 SEVERAL EEPLS BULBS INOP IN CABIN. RESEATED BATTERY PACK PER MM. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2001012500026 20010125 00026 NM 2001 1 25 SWAA010065 1 20010109 A 5315 6546804 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CRACKED IN HORIZONTAL FLANGE, LBL 53, WL 208. REMOVED AND REPLACED FLOOR BEAM T-CHORD PER T1-453-037 & T1-253-024. 2 L 7 2 4F A16WE 2001012500027 20010125 00027 NM 2001 1 25 SWAA010066 1 20010109 A 5314 BAC1503 STIFFENER BOEING 737 7373H4 1384600 NM MLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/4D CHECK, FOUND BS 663 STIFFENER CRACKED AT LBL 3. REPAIRED STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 2001012500028 20010125 00028 NM 2001 1 25 SWAA010067 1 20010107 A 5312 6516300 WEB BOEING 737 7373H4 1384600 NM BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED SPECIAL VISIT AT DALFORT, FOUND BS 178 BULKHEAD WEB CRACKED AT LBL 13.5, WL 234. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 2001012500029 20010125 00029 NM 2001 1 25 SWAA010068 1 20010107 A 5312 6517583 WEB BOEING 737 7373H4 1384600 NM FWD BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED SPECIAL VISIT AT DALFORT, FOUND BS 178 BULKHEAD VERTICAL BEAM WEBS CRACKED AT LBL 17.1 & RBL 17.1. REP AIRED VERTICAL BEAM WEBS PER SRM & BAC DWG. 2 L 7 2 4F RT A16WE 2001012500030 20010125 00030 NM 2001 1 25 SWAA010069 1 20010109 A 5753 6546435 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 621SW 28037 DURING SCHEDULED 1/2D CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP, INBOARD SECTION, DELAMINATED. REPAIRED AFT FLAP ASSY PER SRM. 2 L 7 2 4F RT A16WE 2001012500031 20010125 00031 NM 2001 1 25 SWAA010070 1 20010109 A 3350 20211 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 629SW 27704 DURING SCHEDULED PM CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT ASSY PER M M. 2 L 7 2 4F RT A16WE 2001012500032 20010125 00032 NM 2001 1 25 SWAA010071 1 20010108 A 5313 BAC1498 STRINGER BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED D-CHECK, FOUND 2 STRINGERS CRACKED AT BS 381, STR 4L & BS 420, STR 4L. REPAIRED STRINGERS PER SRM. 2 L 7 2 4F RT A16WE 2001012500033 20010125 00033 NM 2001 1 25 SWAA010049 1 20010107 A 3350 07912 LENS BOEING 737 7375H4 138449D NM CABIN FLOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 525SW 26567 EEPLS RED LENS MISSING AT MID CABIN. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2001012500034 20010125 00034 NM 2001 1 25 SWAA010050 1 20010107 A 5754 65C26686 SKIN BOEING 737 7373H4 1384600 NM NR2 SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/4D CHECK, FOUND NR 2 L/E SLAT LOWER SKIN CRACKED NEAR OUTBOARD END. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001012500035 20010125 00035 2001 1 25 SWAA010051 4 20010107 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 311SW 23333 DURING SCHEDULED A2 CHECK, FOUND AFT ENTRY DOOR EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001012500036 20010125 00036 NM 2001 1 25 SWAA010052 1 20010107 A 5314 BAC1506 STIFFENER BOEING 737 7373H4 1384600 NM MLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED SPECIAL VISIT, FOUND RT VERTICAL STIFFENER CRACKED, BS 663. REMOVED AND REPLACED STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 2001012500037 20010125 00037 NM 2001 1 25 SWAA010053 1 20010108 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 621SW 28037 DURING SCHEDULED 1/2D CHECK, FOUND BROKEN RECEPTACLE AT RT OVERWING EMERGENCY EXIT LIGHT. REMOVED AND REPLACED LIGHT AS SY PER MM. 2 L 7 2 4F RT A16WE 2001012500038 20010125 00038 NM 2001 1 25 SWAA010054 1 20010108 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN FLOOR DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 394SW 27380 EEPLS INOP. CONNECTED EEPLS WIRING. OPS CK GOOD PER MM. 2 L 7 2 4F RT A16WE 2001012500039 20010125 00039 NM 2001 1 25 SWAA010055 1 20010108 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN FLOOR DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 639SW 27712 EEPLS INOP AT ROWS 14 - 19. RECONNECTED WIRE TERMINALS. OPS CK GOOD PER MM. 2 L 7 2 4F RT A16WE 2001012500040 20010125 00040 NM 2001 1 25 SWAA010056 1 20010108 A 3350 BR2013 LAMP SOCKET BOEING 737 7372H4 138448C NM CABIN FLOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED C1 CHECK, FOUND EEPLS SOCKET MISSING AT MID CABIN. INSTALLED LIGHT SOCKET PER MM. 2 L 7 2 4F A16WE 2001012500041 20010125 00041 NM 2001 1 25 SWAA010057 1 20010108 A 5313 65C27314 CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED D-CHECK, FOUND 4 STRINGER CLIPS CRACKED, BS 400, STRINGERS 27L, 28L, 28R, AND BS 500B, STRINGER 24L. R EMOVED AND REPLACED CLIPS PER SRM. 2 L 7 2 4F A16WE 2001012500042 20010125 00042 NM 2001 1 25 SWAA010058 1 20010108 A 3350 101073 LIGHT BOEING 737 7373H4 1384600 NM AFT CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 363SW 26574 DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2001012500043 20010125 00043 NM 2001 1 25 SWAA010059 1 20010108 A 5511 BAC1506 SPAR BOEING 737 7373H4 1384600 NM LH HORZ STAB DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 379SW 26586 DURING SCHEDULED C4 CHECK, FOUND LT HORIZONTAL STAB REAR SPAR LOWER CHORD DAMAGED THROUGH AT SKIN ATTACH SECTION, STA 11 4 TO 116. REPAIRED PER RA 1-355-0389. 2 L 7 2 4F RT A16WE 2001012500044 20010125 00044 NM 2001 1 25 SWAA010060 1 20010108 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN FLOOR LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 389SW 26592 DURING SCHEDULED C2 CHECK, FOUND EEPLS LOOSE AND INOP FROM ROW 22 AFT. RECONNECTED LIGHT ASSY AND REMOVED AND REPLACED TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 2001012500045 20010125 00045 NM 2001 1 25 SWAA010061 1 20010108 A 5753 6546435318 FLAP BOEING 737 7373H4 1384600 NM RH WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 389SW 26592 DURING SCHEDULED C2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP AS SY PER MM. 2 L 7 2 4F RT A16WE 2001012500046 20010125 00046 NM 2001 1 25 SWAA010062 1 20010108 A 3350 20121 BATTERY PACK BOEING 737 7373A4 1384585 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2001012500047 20010125 00047 NM 2001 1 25 SWAA010027 1 20010105 A 5312 6516300 WEB BOEING 737 7372H4 138448C NM BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT WL 234, LBL 9.5. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F A16WE 2001012500048 20010125 00048 NM 2001 1 25 SWAA010028 1 20010104 A 3350 101073 LIGHT BOEING 737 7373H4 1384600 NM AFT SVC DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR SIDEWALL EMERGENCY EXIT LIGHT BULBS INOP. REMOVED AND REPLACED BULBS PER MM. 2 L 7 2 4F RT A16WE 2001012500049 20010125 00049 2001 1 25 SWAA010029 4 20010104 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM PAX DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 313SW 23335 DURING SCHEDULED C3 CHECK, FOUND FWD SVC AND ENTRY DOORS EMERGENCY EVAC SLIDE GIRT ASSY''S OUT OF ADJUST. RE-ADJUSTED E VAC SLIDE ASSY''S PER MM. 2 L 7 2 4F RT A16WE 2001012500050 20010125 00050 NM 2001 1 25 SWAA010030 1 20010104 A 5310 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED 1/4D CHECK, UPON CORROSION REMOVAL OF FUSELAGE SKIN, FOUND SHEAR TIE CORRODED AT BS 807, STR 28L TO STR 28R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2001012500051 20010125 00051 NM 2001 1 25 SWAA010031 1 20010105 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN FLOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 383SW 26589 EEPLS LOOSE AT ROW 22. SECURED EEPLS TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001012500052 20010125 00052 NM 2001 1 25 SWAA010032 1 20010105 A 3234 CIRCUIT BREAKER BOEING 737 7373Y0 1384671 NM COCKPIT TRIPPED A SWAA O OTHER O OTHER TO TAKEOFF 1 SW 07 699SW 23826 LANDING GEAR HANDLE WOULD NOT GO UP PAST OFF POSITION. FOUND LANDING GEAR LATCH PRESS WARN C/B TRIPPED. RESET C/B AND RAISED LAND GEAR AND CONTINUED. SYSTEM TEST OF LAND GEAR CONTROL LEVER LOCK GOOD AND C/B REMAINS CLOSED, NO FAULTS NOTE D PER MM. 2 L 7 2 4F RT A16WE 2001012500053 20010125 00053 2001 1 25 SWAA010033 4 20010104 A 2565 D31354 SLIDE BOEING 737 7377H4 NM AFT ENTRY OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 737JW 27869 AFT ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REPOSITIONED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001012500054 20010125 00054 NM 2001 1 25 SWAA010034 1 20010106 A 5753 6546435 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/4D CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT PREVIOUS REPAIR. REMOVED AND REPLACED A FT FLAP ASSY PER MM. 2 L 7 2 4F RT A16WE 2001012500055 20010125 00055 NM 2001 1 25 SWAA010035 1 20010106 A 5754 6573714 SLAT BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/4D CHECK, FOUND NR 1 L/E SLAT CRACKED AT TWO ADJOINING RIVET HOLES, INBOARD OF INBOARD MAIN TRACK AND OUTBOARD OF INBOARD AUX TRACK. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2001012500056 20010125 00056 NM 2001 1 25 SWAA010036 1 20010104 A 5330 6555074 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED C1 CHECK, FOUND 3.0 EXTERNAL FUSELAGE SKIN CRACK AT BS 270, STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001012500057 20010125 00057 NM 2001 1 25 SWAA010037 1 20010105 A 5330 6552880 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED C1 CHECK, FOUND 1 EXTERNAL FUSELAGE SKIN CRACK AT AFT ENTRY DOOR CUTOUT, UPPER AFT CORNER. REPAIRED SK IN PER SRM. 2 L 7 2 4F RT A16WE 2001012500058 20010125 00058 NM 2001 1 25 SWAA010038 1 20010104 A 5330 65C35775 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED C1 CHECK, FOUND 2.0 EXTERNAL FUSELAGE SKIN CRACK AT BS 727E, BELOW STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001012500059 20010125 00059 NM 2001 1 25 SWAA010039 1 20010105 A 5330 6545857 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED C1 CHECK, FOUND .75 INCH EXTERNAL FUSELAGE SKIN CRACK AT AFT SVC DOOR LOWER HINGE CUTOUT. REPAIRED SKI N PER SRM. 2 L 7 2 4F RT A16WE 2001012500060 20010125 00060 NM 2001 1 25 SWAA010040 1 20010105 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED C2 CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 940, BELOW STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001012500061 20010125 00061 NM 2001 1 25 SWAA010041 1 20010105 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 328SW 23692 DURING SCHEDULED SERVICE CHECK, FOUND 2 EXTERNAL FUSELAGE SKIN CRACK AT BS 944, STR 22L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001012500062 20010125 00062 NM 2001 1 25 SWAA010042 1 20010106 A 5320 BAC1503 STIFFENER BOEING 737 7373H4 1384600 NM MLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 328SW 23692 DURING SCHEDULED SPECIAL VISIT, FOUND BS 663 BULKHEAD VERTICAL STIFFENER CRACKED AT LWR GROUND STUD, FWD OF INBOARD END OF A SYS ELEC HYD PUMP. REMOVED AND REPLACED VERTICAL STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 2001012500063 20010125 00063 NM 2001 1 25 SWAA010043 1 20010106 A 2130 6573739 DRAIN VALVE BOEING 737 7373H4 1384600 NM LOWER FUSELAGE OPEN A SWAA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 363SW 26574 DIVERSION, LT DUAL BLEED LIGHT ILLUMINATED, RIGHT A/C WOULD NOT MAINTAIN CABIN PRESSURE. FOUND NUMEROUS BELLY DRAIN VAL VES OPENED. CLEANED AND REPOSITIONED DRAIN VALVES. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2001012500064 20010125 00064 NM 2001 1 25 SWAA010044 1 20010106 A 2130 332A235014 LINE BOEING 737 7377H4 NM NR 1 ENGINE BROKEN A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 710SW 27844 AIR TURNBACK, CABIN PRESSURE CONTROL FAILURE DURING FLIGHT. FOUND NR 1 ENG PNEU BLEED PRESS AIR SENSING LINE BROKEN. R EMOVED AND REPLACED SAME PER MM. OPS CK GOOD. 2 L 7 2 4F RT A16WE 2001012500065 20010125 00065 NM 2001 1 25 SWAA010045 1 20010107 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN FLOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 525SW 26567 EEPLS PULLED UP LOOSE. REPAIRED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001012500066 20010125 00066 2001 1 25 SWAA010046 4 20010107 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD ENTRY OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER DURING DOOR CLOSING. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001012500067 20010125 00067 2001 1 25 SWAA010047 4 20010107 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM PAX DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 FWD SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001012500068 20010125 00068 NM 2001 1 25 SWAA010048 1 20010107 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM FWD ENTRY INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 609SW 27929 FWD ENTRY EMERGENCY EXIT LIGHT LOOSE AND INOP. SECURED LENS AND RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2001012500070 20010125 00070 NE 2001 1 25 SWAA010018 2 20010103 A 7200 ENGINE BOEING 737 7373H4 1384600 NM GE CFM56 CFM56* 13802 NE NR 2 FAILED A SWAA O OTHER R Y PARTIAL RPM/PWR LOSS ENGINE STOPPAGE DE DESCENT 1 SW 07 618WN 28034 721375 INFLIGHT ENGINE SHUTDOWN, NR 2 ENGINE FAILED. BOTH ENGINES WERE STABLE HOLDING 250 KTS AT 14,000 FT. NO PRIOR WARNING INDICATIONS BEFORE FAILURE. REMOVED AND REPLACED NR 2 ENGINE ASSY PER SAM 385. PERFORMED TRIM RUN PER SAM 625 AND SAM 390, NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001012500071 20010125 00071 NE 2001 1 25 SWAA010026 2 20010103 A 7200 ENGINE BOEING 737 7373H4 1384600 NM GE CFM56 CFM56* 13802 NE NR 1 ODOR A SWAA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 07 623SW 27933 859323 AIR TURNBACK, DECLARED EMERGENCY. DURING TAKEOFF A GREY, ACRID ODOR/SMOKE STARTED FILLING THE COCKPIT. AS POWER WAS RE DUCED, SMOKE DECREASED. REMOVED AND REPLACED NR 1 ENGINE PER MM AND SAM FORMS. OPS AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2001012500072 20010125 00072 NM 2001 1 25 SWAA010010 1 20010101 A 2612 894093 FIRE LOOP BOEING 737 7372T4 1384492 NM PWA JT8 JT8* 52044 NE NR 1 ENGINE ERRATIC A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 130SW 22699 707393 IN FLIGHT ENGINE SHUT DOWN, DECLARED EMERGENCY, AIR TURNBACK. NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED. ACCOMPLISHED FIRE PROCEDURE PER QRH, FIRED BOTH EXTINGUISHER BOTTLES. INSPECTED ENGINE FOR EVIDENCE OF FIRE, NONE NOTED. VERIFIED OVERHEAT SYSTEM NORMAL. REMOVED AND REPLACED NR 1 ENG LOWER FIRE LOOP AND 4 CONNECTORS PER MM. 2 L 7 2 4F 4 F A16WE E2EA 2001012500073 20010125 00073 NM 2001 1 25 SWAA010011 1 20010102 A 3350 079123 COVER BOEING 737 7372H4 138448C NM CABIN FLOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 087SW 22903 DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVER MISSING AT ROW 16D. INSTALLED TRACK COVER PER MM. 2 L 7 2 4F A16WE 2001012500074 20010125 00074 2001 1 25 SWAA010012 4 20010102 A 2565 65C168209 RETAINER BOEING 737 7373H4 1384600 NM ESCAPE SLIDE LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 639SW 27712 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY RETAINER LOOSE. SECURED RETAINER PER MM. 2 L 7 2 4F RT A16WE 2001012500075 20010125 00075 NM 2001 1 25 SWAA010017 1 20010103 A 5320 6545819 PANEL BOEING 737 7373H4 1384600 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/4D CHECK, FOUND 2 CRACKS IN NLG W/W BELOW FWD RECESS PANEL, BS 244 & BS 245. REPAIRED NLG W/W BOX AS SY PER SRM. 2 L 7 2 4F RT A16WE 2001012500089 20010125 00089 2001 1 25 SWA010002 4 20010101 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD PAX DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001012500090 20010125 00090 NM 2001 1 25 SWA010003 1 20010102 A 3350 900545 POWER SUPPLY BOEING 737 7372K6 NM AFT GALLEY INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED SERVICE CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY PER MM. 2 L 7 2 4F RT A16WE 2001012500091 20010125 00091 NM 2001 1 25 SWA010004 1 20010102 A 5743 6937877 FITTING BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/4D CHECK, FOUND LT MLG WALKING BEAM FWD OUTBOARD ATTACH LINK CRACKED. REPAIRED FITTING PER SRM. 2 L 7 2 4F RT A16WE 2001012500092 20010125 00092 NM 2001 1 25 SWA010005 1 20010101 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT LBL 1, WL 189. REPAIRED BULKHEAD WEB PER SRM. 2 L 7 2 4F RT A16WE 2001012500093 20010125 00093 NM 2001 1 25 SWA010006 1 20010101 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM AFT CARGO BAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 772, LBL 12.5. REPAIRED FLOORBEAM PER RA 1-A53-2021. 2 L 7 2 4F RT A16WE 2001012500094 20010125 00094 NM 2001 1 25 SWA010007 1 20010102 A 5210 6545871 DOOR FRAME BOEING 737 7373H4 1384600 NM FWD ENTRY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 621SW 28037 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR AFT FRAME CRACKED AT 3RD FROM BOTTOM STOP FITTING. REPAIRED DOOR FRAM E PER SRM. 2 L 7 2 4F RT A16WE 2001012500095 20010125 00095 NM 2001 1 25 SWA010008 1 20010101 A 3350 6556633 LENS BOEING 737 737301 1384611 NM LT & RT OVERWING BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED C1 CHECK, FOUND LT & RT OVERWING EMERGENCY EXIT LIGHT LENSES BROKEN. REMOVED AND REPLACED LENS ASSY''S PER MM. 2 L 7 2 4F RT A16WE 2001012500096 20010125 00096 NM 2001 1 25 SWA010009 1 20010101 A 2560 65C168209 RETAINER BOEING 737 7373G7 1384595 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 683SW 24008 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR AFT GIRT BAR RETAINER HOOK LOOSE. SECURED RETAINER HOOK PER MM. 2 L 7 2 4F RT A16WE 2001012500102 20010125 00102 NM 2001 1 25 SWA010001 1 20010101 A 5753 6546435 SKIN BOEING 737 737317 138447P NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED C4 CHECK, FOUND LT WING T/E AFT FLAP DELAMINATED AT INBOARD AFT CORNER. REMOVED AND REPLACED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2001012500103 20010125 00103 NM 2001 1 25 SWAA010001 1 20010101 A 5753 6546435 SKIN BOEING 737 737317 138447P NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED C4 CHECK, FOUND LT WING T/E AFT FLAP DELAMINATED AT INBOARD AFT CORNER. REMOVED AND REPLACED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2001012500104 20010125 00104 2001 1 25 SWAA010002 4 20010101 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD PAX DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001012500105 20010125 00105 NM 2001 1 25 SWAA010003 1 20010102 A 3350 900545 POWER SUPPLY BOEING 737 7372K6 NM AFT GALLEY INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED SERVICE CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY PER MM. 2 L 7 2 4F RT A16WE 2001012500106 20010125 00106 NM 2001 1 25 SWAA010004 1 20010102 A 5743 6937877 FITTING BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/4D CHECK, FOUND LT MLG WALKING BEAM FWD OUTBOARD ATTACH LINK CRACKED. REPAIRED FITTING PER SRM. 2 L 7 2 4F RT A16WE 2001012500107 20010125 00107 NM 2001 1 25 SWAA010005 1 20010101 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT LBL 1, WL 189. REPAIRED BULKHEAD WEB PER SRM. 2 L 7 2 4F RT A16WE 2001012500108 20010125 00108 NM 2001 1 25 SWAA010006 1 20010101 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM AFT CARGO BAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 772, LBL 12.5. REPAIRED FLOORBEAM PER RA 1-A53-2021. 2 L 7 2 4F RT A16WE 2001012500109 20010125 00109 NM 2001 1 25 SWAA010007 1 20010102 A 5210 6545871 DOOR FRAME BOEING 737 7373H4 1384600 NM FWD PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 621SW 28037 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR AFT FRAME CRACKED AT 3RD FROM BOTTOM STOP FITTING. REPAIRED DOOR FRAM E PER SRM. 2 L 7 2 4F RT A16WE 2001012500110 20010125 00110 NM 2001 1 25 SWAA010008 1 20010101 A 3350 6556633 LENS BOEING 737 737301 1384611 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED C1 CHECK, FOUND LT & RT OVERWING EMERGENCY EXIT LIGHT LENSES BROKEN. REMOVED AND REPLACED LENS ASSYS P ER MM. 2 L 7 2 4F RT A16WE 2001012500111 20010125 00111 NM 2001 1 25 SWAA010009 1 20010101 A 2560 65C168209 RETAINER BOEING 737 7373G7 1384595 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 683SW 24008 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR AFT GIRT BAR RETAINER HOOK LOOSE. SECURED RETAINER HOOK PER MM. 2 L 7 2 4F RT A16WE 2001012500133 20010125 00133 EU 2001 1 25 MALA010105 1 20010103 A 3060 WARNING SYSTEM SAAB SF340 340B 7860101 EU PROP DEICE SYS ACTIVATED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 411XJ 411 RT PROP FAIL. WITH PROP ICE SELECTED ON CREW GOT MASTER CAUTION ON BOTH SIDES 40 SECONDS AFTER SELECTED TO NORM AND ABO UT 10 SECONDS WHEN SELECTED TO MAX. ALL DE-ICE CHECKS NORMAL ON GROUND. COMPLIED W/QRH, RESET ALL C/B, NO CHANGE ON DE SCENT INTO DTW. THE LT SIDE APPEARED TO WORK NORM WHILE RT FAILS. MAINTENANCE RAN BOTH LT AND RT PROP HEAT IN MAX FOR APPROX 6 MIN AND IN NORM FOR 6 MIN WITH NO FAIL OR MASTER CAUTION LIGHTS. BOTH BRUSH BLOCKS AND LEADS LOOK GOOD. ALL C HECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2001012500134 20010125 00134 EA 2001 1 25 COMA0160081 1 20010107 A 5730 601R10045 ACCESS PANEL CNDAIR CL600 CL6002B19 EA WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 712CA 7244 LOWER WING ACCESS HOLES CRACKED AT 550BB WS 188.040 550CB WS 209.040 AND 550EB WS 253.022. BLENDED DAMAGE AND ROTO-PEEN ED IAW REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 2001012500135 20010125 00135 2001 1 25 COMA0160084 4 20010110 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 821CA 7420 STALL FAIL CAUTION DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001012500136 20010125 00136 WP 2001 1 25 MWEA010037 1 20010110 A 5311 953609513 FRAME DOUG DC9 DC914 3022034 WP FUSELAGE NICKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 SEVERAL NICKS IN AFT RADIUS OF STATION 256 BETWEEN LONGERON 12, 13, &14 RIGHT. FABRICATED AND INSTALLED ANGLE AND SPLIC ES. 2 L 7 2 4F A6WE 2001012500137 20010125 00137 WP 2001 1 25 MWEA010039 1 20010110 A 5313 59104934 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 LEFT LAV HAD CRACKED LONGERON, UPPER FLANGE AT STATION 965, LONGERON 16 LEFT. FABRICATED AND INSTALLED NEW LONGERON SEC TION. 2 L 7 2 4F A6WE 2001012500138 20010125 00138 WP 2001 1 25 MWEA010041 1 20010110 A 5230 591014143 DOOR DOUG DC9 DC914 3022034 WP FWD CARGO BAY CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 FORWARD CARGO DOOR OUTER PAN IS CRACKED AT FORWARD LOWER STOP PAD. FABRICATED DOUBLER AND SPLICES. 2 L 7 2 4F A6WE 2001012500139 20010125 00139 WP 2001 1 25 MWEA010042 1 20010110 A 5313 591142615 LONGERON DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 500ME 45711 FASTENERS WITH IMPROPER SPACING AT LONGERONS 9 LEFT AND 10 LEFT AFT OF STATION 766. FABRICATED AND INSTALLED SPLICE DOU BLER AND STAND OFF BRACKET. 2 L 7 2 4F A6WE 2001012500140 20010125 00140 WP 2001 1 25 MWEA010038 1 20010111 A 5320 593643451 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 REMOVED AND REPLACED FORWARD BAG PIT BELLY SKIN FROM STATION 229 TO 474 AND LONGERON 26 LEFT TO LONGERON 26 RIGHT. FABR ICATED AND INSTALLED NEW SKIN. 2 L 7 2 4F A6WE 2001012500141 20010125 00141 WP 2001 1 25 MWEA010040 1 20010111 A 5240 5910084143 SKIN DOUG DC9 DC914 3022034 WP SERVICE DOOR CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 GALLEY DOOR SKIN IS CHAFED FROM THE DOOR HANDLE CONTACTING IT DURING DOOR OPERATION. FABRICATED AND INSTALLED SCUFF PLA TE. 2 L 7 2 4F A6WE 2001012500142 20010125 00142 WP 2001 1 25 MWEA010043 1 20010111 A 5311 995823870 FORMER DOUG DC9 DC914 3022034 WP FUSELAGE CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 SHEAR CLIP STATION 786 HAS DEEP CHAFE MARKS IN RADIUS ADJACENT TO LONGERON 15 RIGHT. FABRICATED AND INSTALLED NEW ANGLE . 2 L 7 2 4F A6WE 2001012500143 20010125 00143 WP 2001 1 25 MWEA010044 1 20010111 A 5311 99581992 FRAME DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 CRACK IN FRAME 503 BETWEEN LONGERON 9 AND 10 RIGHT. FABRICATED AND INSTALLED NEW ANGLE. 2 L 7 2 4F A6WE 2001012500144 20010125 00144 EA 2001 1 25 COMA0160086 1 20010109 A 5210 LATCH CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADJ A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 917CA 7017 CABIN DOOR WARNING MESSAGE. ADJUSTED DOOR LATCH MECHANISM LINKAGE. 2 L 7 2 4F RT A21EA 2001012500145 20010125 00145 2001 1 25 COMA0160087 4 20010109 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 976CA 7151 STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001012500146 20010125 00146 WP 2001 1 25 UPS01834605 1 20010103 A 5320 37558472N FITTING DOUG DC8 DC871F 302199D WP LOWER CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C2 STA 1160 LONG 32R BANANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755847, AND SRM 5 1-1-20D. 2 L 7 4 4F RT 4A25 2001012500147 20010125 00147 EA 2001 1 25 COMA0160089 1 20010109 A 2752 854D10011 ACTUATOR CNDAIR CL600 CL6002B19 EA RT WING TE FLAPS DEFECTIVE A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 786CA 4567 7333 FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT NR 4 FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2001012500148 20010125 00148 EA 2001 1 25 COMA0160090 1 20010109 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 EA CABIN FLOOR DIRTY A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 759CA 7279 EMERGENCY FLOOR LIGHTS AT ROW 1 ARE INOP. CLEANED WIRE CONNECTIONS AND SYSTEM TEST NORMAL. 2 L 7 2 4F RT A21EA 2001012500149 20010125 00149 EA 2001 1 25 COMA0160091 1 20010108 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA ROW 5 INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 819CA 7415 EMERGENCY LIGHT AT ROW 5 IS INOP. DEFERRED MAINTENANCE PER MEL. 2 L 7 2 4F RT A21EA 2001012500150 20010125 00150 EA 2001 1 25 COMA0160092 1 20010108 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA CABIN BURNED OUT A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949CA 7080 EMERGENCY LIGHT AT ROW 5 IS INOP. REPLACED LIGHT BULB. 2 L 7 2 4F RT A21EA 2001012500152 20010125 00152 EA 2001 1 25 COMA0160094 1 20010107 A 3350 20131A BATTERY CNDAIR CL600 CL6002B19 EA CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 779CA 14235 7306 EXTERIOR EMERGENCY LIGHT AT CABIN DOOR IS INOP. REPLACED EMERGENCY BATTERY. 2 L 7 2 4F RT A21EA 2001012500153 20010125 00153 EA 2001 1 25 COMA0160095 1 20010109 A 2730 276003 PCU CNDAIR CL600 CL6002B19 EA LT ELEVATOR FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 937CA 3134 7044 LEFT ELEVATOR NR 3 PCU FAILED BACKLASH CHECK TASK NR 002-27-900-106. REMOVED AND REPLACED LEFT ELEVATOR NR 3 PCU WITH S ERVICEABLE ONE. RETURNED TO SERVICEABLE CONDITION. 2 L 7 2 4F RT A21EA 2001012500154 20010125 00154 EA 2001 1 25 COMA0160096 1 20010109 A 2730 276003 PCU CNDAIR CL600 CL6002B19 EA RT ELEVATOR FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 937CA 16791 7044 RIGHT ELEVATOR NR 3 PCU (INBOARD) FAILED BACKLASH CHECK TASK NR 002-27-900-106. REMOVED AND REPLACED PCU FAILED BACKLAS H CHECK FROM STOCK (MAL0009). 2 L 7 2 4F RT A21EA 2001012500155 20010125 00155 SO 2001 1 25 COMA0110005 1 20010107 A 2133 2091G010800 OUTFLOW VALVE EMB 120 EMB120RT SO CABIN MALFUNCTIONED A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 257CA 22194 120248 AIRCRAFT WOULD NOT PRESSURIZE. REPLACED THE OUTFLOW VALVE. 2 L 7 2 4T RT A31SO 2001012500156 20010125 00156 EA 2001 1 25 COMA0160097 1 20010109 A 2730 276003 PCU CNDAIR CL600 CL6002B19 EA RT ELEVATOR FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 937CA 3134 7044 RIGHT ELEVATOR NR 2 PCU (MIDDLE) FAILED BACKLASH CHECK TASK NR002-27-900-106.REMOVED AND REPLACED RT ELEVATOR NR 2 PCU W ITH SERVICEABLE ONE. RETURNED TO SERVICEABLE CONDITION. 2 L 7 2 4F RT A21EA 2001012500157 20010125 00157 SO 2001 1 25 COMA0110006 1 20010107 A 3210 LANDING GEAR EMB 120 EMB120RT SO RIGHT LACK OF LUBE A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 258CA 120247 RT MLG INDICATED UNSAFE. CLEANED AND LUBRICATED LANDING GEAR. 2 L 7 2 4T RT A31SO 2001012500158 20010125 00158 SO 2001 1 25 COMA0110007 1 20010109 A 2131 912R0201 CONTROLLER EMB 120 EMB120RT SO COCKPIT MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 257CA 20697 120248 AIRCRAFT WILL NOT PRESSURIZE. REPLACED THE PRESSURIZATION HAND CONTROLLER. 2 L 7 2 4T RT A31SO 2001012500159 20010125 00159 EU 2001 1 25 JBXA000235 1 20010111 A 2760 WARNING LIGHT FOKKER F28 F28MK0100 4990807 EU SPOILER SYSTEM ILLUMINATED A JBXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 05 110ML 11486 LIFT DUMPER FAULT MESSAGE DISPLAYED INTERMITTENTLY. ABORTED TAKEOFF. CLEARED FAULT, AIRCRAFT DEPARTED NORMALLY, NO FUR THER FAULTS. 2 L 7 2 4F RT 2001012500160 20010125 00160 NM 2001 1 25 01FDEA00016 1 20010110 A 5720 69201124 ANGLE BOEING 727 727232 1384082 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 RT WING PIE SECTION I/B WEB SUPPORT ANGLE CRACKED AT LOWER END. *S/D* REMOVED, REPLACED AND FAB PER IAW SRM 51-30-2, 5 1-10-3, AND 51-30-5. 2 L 7 3 4F A3WE 2001012500161 20010125 00161 NM 2001 1 25 01FDEA00018 1 20010111 A 5522 65174633 SKIN BOEING 727 727233 138408A NM VERTICAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 CRACK IN SKIN, VERTICAL STAB, LEFT SIDE, STR 10, BOTTOM OF STAB. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 55-30-3 AND FEDEX EA 7-5510-56226. 2 L 7 3 4F RT A3WE 2001012500162 20010125 00162 NM 2001 1 25 01FDEA00017 1 20010110 A 5713 69728771 STRINGER BOEING 727 727232 1384082 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 RT WING 2 STRINGER NR 10, AT WS 686.5 IS CRACKED AT RIB ATTACH POINT. *S/D* REMOVED AND REPLACED PER IAW BOEING SB 727 -57A159 AND FEDEX EA 7-5710-56217. 2 L 7 3 4F A3WE 2001012500163 20010125 00163 NM 2001 1 25 01FDEA00019 1 20010112 A 2821 FILTER DOUG MD11 MD11F 3023600 NM NR 2 ENGINE FUEL MALFUNCTIONED A FDEA A UNSCHED LANDING J X WARNING INDICATION ENGINE FLAMEOUT CR CRUISE 1 SO 25 605FE 48514 RECEIVED TANK 2 FWD PMP LO ALERT. ACCOMPLISH CKLIST. NR 2 ENG FLAMED OUT AFTERWARDS. FOR PRECAUTION REMOVED AND REPLA CED NR 2 ENG FUEL FILTER AND NO LEAK PER 73-11-04-6. FUEL SHROUD DRAIN FOUND NO LEAK PER MM 28-25-00-6. 2 L 7 3 4F RT A22WE 2001012500165 20010125 00165 GL 2001 1 25 C2XA01IA022 2 20010111 A 7200 AE3007A1P ENGINE EMB 145 EMB145LR SO ALLSN AE300 AE3007A GL LEFT VIBRATION A C2XA D RETURN TO BLOCK E J VIBRATION/BUFFET WARNING INDICATION TX TAXI/GRND HDL 1 SW 27 14993 1400 145289 CAE311463 IAH - FLT 4203, CREW REPROTED THAT DURING TAXI THE NR 1 ENGINE EMMITTED A HUMMING SOUND AND VIBRATION AT LOW TO MEDIUM P OWER SETTINGS. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENIGNE IAW ROLLS ROYCE MAINTENANCE MANUAL 71-00-00. THE AIRCR AFT WAS THEN APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2001012500168 20010125 00168 EU 2001 1 25 01FDEA00020 1 20010112 A 2612 FIRE WARNING AIRBUS 310 A310203 EU NR 1 & 2 ENGINES ACTIVATED A FDEA F ACTIVATE FIRE EXT. B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION LD LANDING 1 SO 25 408FE 257 CARGO SMOKE AND FIRE ON FINAL FIRE BOTTLES ON APU ENG DISCHARGED ON LAND. REPLACED NR 1 & 2 FIRE BOTTLES IN BOTH ENG 1 & 2 AS PER MM 26-22-12-4. AC OK FOR FLIGHT. 2 L 7 2 4F RT A35EU 2001012500169 20010125 00169 NM 2001 1 25 01FDEA00021 1 20010113 A 2750 69186361 LINK BOEING 727 7272D4 138407U NM TE FLAPS CORRODED A FDEA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 SO 25 287FE 21849 AFT T/O DURING FLAP RETRACT BOTH INBOARD AND OUTBOARD TRAILING EDGE FLAP IND STOPPED. AMBER LIGHT ILLUM, BUT EDGE DEVIC E SHOW ALL GREEN ON 2ND OFF PNL. *S/D* CLEAN, LUB JACKSCREWS, GIMBALS, ROD ENDS, PULLEYS, AND CABLES PER MM 12-22-001- 2. REMOVED AND REPLACED OUTBOARD T/E FLAP CONTROL LINK ASSY PER 727-200 MM 27-51-051-4. CK GOOD PER MM 27-51-000-5. 2 L 7 3 4F A3WE 2001012500170 20010125 00170 SO 2001 1 25 C2XA01IA023 1 20010114 A 3350 3025103 LIGHT EMB 145 EMB145ER SO EXTERIOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14937 145026 IAH - DURING C-CHECK INSPECTION, THE RIGHT HAND FORWARD EXTERNAL EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAIN TENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY IN ACCORDANCE WITH EMB145 M/M 33-50-02-000-801-A, AND THE AIRCR AFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001012500171 20010125 00171 SO 2001 1 25 C2XA01IA024 1 20010114 A 3350 110049 CHARGER EMB 145 EMB145ER SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14937 145026 IAH - DURING C-CHECK INSPECTION, THE EMERGENCY LIGHT ON PANEL 243DLC WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY CHARGER IN ACCORDANCE WITH EMB145 M/M 33-50-04-000-801-A, AND THE AIRCR AFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001012500172 20010125 00172 SO 2001 1 25 C2XA01IA025 1 20010114 A 3350 1317 BULB EMB 145 EMB145ER SO CABIN BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14937 145026 IAH - DURING C-CHECK INSPECTION, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE AFFECTED LIGHT BULB IN ACCORDANCE WITH EMB145 M/M 33-26-04-400-801-A, AND THE AIRCRAFT WAS APPROVED FOR R ETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001012500173 20010125 00173 EU 2001 1 25 RAIA0101007 1 20010111 A 3210 AIR830901 LANDING GEAR JETAIR JETSTM JETSTM4101 1500501 EU L/H MLG MALFUNCTIONED A RAIA O OTHER J WARNING INDICATION CL CLIMB 1 CE 03 560HK 11535 11535 41076 7306-STL- DURING CLIMBOUT ALL LANDING GEAR WOULD NOT RETRACT. MAINTENANCE REMOVED AND REPLACED LEFT HAND MAIN LANDING G EAR IAW J41 MAINTENANCE MANUAL. 2 L 7 2 4T RT A41NM 2001012500174 20010125 00174 EU 2001 1 25 RAIA0101006 1 20010111 A 5610 NP1588621 WINDOW AEROSP ATR72 ATR72202 8680940 EU COCKPIT MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 723TE 17438 17438 283 7400-STL- DURING TAXI SIDE WINDOW HEAT FAULT LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED CAPTAINS SIDE WINDOW I AW ATR72 MAINTENANCE MANUAL. 2 H 7 2 4T RT A53EU 2001012500175 20010125 00175 SO 2001 1 25 GLBA2001005 1 20010110 A 2752 CONNECTOR EMB 120 EMB120 3260201 SO FLAP ACTUATOR CONTAMINATED A GLBA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 01 96ZK 12096 RETURN TO BLOCK - FLAP DISAGREEMENT AFTER T/O. CLEANED AND REMOVED GLYCOL FROM ACTUATOR CANNON PLUG, OPS CHECKED SYSTEM GOOD. 2 L 7 2 4T RT A31SO 2001012500176 20010125 00176 NM 2001 1 25 HNAA0100003 1 20010114 A 3350 6013211X BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 923HA 4489 20 099 FIRST TWO FLOOR LEVEL EMERGENCY EXIT LIGHTS INOP. REPLACED EMERGENCY LIGHT BATTERY PACK. 2 H 7 2 4T RT A13NM 2001012500177 20010125 00177 NE 2001 1 25 JBXA000236 2 20010114 A 7200 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE RIGHT MALFUNCTIONED A JBXA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 05 578ML 7270 872394 FLIGHT 863 RDU/EWR UPON POWER APPLICATION RIGHT ENGINE DID NOT SPOOL UP. N1, N2 AND FUEL FLOW WERE AT IDLE LEVELS TWO S ECONDS AFTER INITIAL POWER APPLICATION. TAKEOFF WAS ABORTED. PERFORMED ACCEL-DECEL CHECK OF RIGHT HAND ENGINE IAW AMM 71-00-00. ALL PERIMETERS WERE WITHIN LIMITS. ALSO PERFORMED POWER ASSURANCE CHECK OF THE RIGHT HAND ENGINE IAW AMM 71- 00-00. THIS CHECK WAS ALSO GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2001012500178 20010125 00178 EU 2001 1 25 RAIA0101008 1 20010112 A 2436 10200311 CONTROL UNIT AEROSP ATR42 ATR42300 8680920 EU NR2 GENERATOR FAILED A RAIA O OTHER J WARNING INDICATION CL CLIMB 1 CE 03 424TE 22419 22419 124 7158-STL- DURING CRUISE NR 2 DC GENERATOR FAILED. MAINTENANCE REMOVED AND REPLACED NR 2 GENERATOR CONTROL UNIT IAW ATR4 2 MAINTENANCE MANUAL. 2 H 7 2 4T RT A53EU 2001012500179 20010125 00179 EU 2001 1 25 RAIA0101009 1 20010113 A 7730 31055016 COMPUTER JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 551HK 7729 7729 41040 7443-CMI- DURING TAXI RIGHT HAND INTIGRATED ENGINE COMPUTER FAILED WITH ENGINE INLET ANTI ICE ON. MAINTENANCE REMOVED A ND REPLACED NR 2 INLET PRESSURE SENSOR IAW GARRETT MAINTENANCE MANUAL 72-10-13. 2 L 7 2 4T RT A41NM 2001012500180 20010125 00180 EU 2001 1 25 RAIA00101009 1 20010112 A 2435 8260121 STARTER GEN AEROSP ATR42 ATR42300 8680920 EU NR2 ENGINE FAILED A RAIA K NONE O OTHER CL CLIMB 1 CE 03 424TE 18387 1142 124 7176-STL- DURING CLIMB NR 2 GENERATOR FAULTED IN FLIGHT AFTER TAKEOFF. MAINTENANCE REMOVED AND REPLACED THE NR 2 STARTE R GENERATOR IAW ATR42 MAINTENANCE MANUAL. 2 H 7 2 4T RT A53EU 2001012500181 20010125 00181 EU 2001 1 25 RAIA00101010 1 20010114 A 3234 1005383400 SELECTOR VALVE AEROSP ATR42 ATR42300 8680920 EU COCKPIT FAILED A RAIA O OTHER J WARNING INDICATION DE DESCENT 1 CE 03 426TE 22424 484 228 7158-STL- DURING DESCENT LANDING GEAR WOULD NOT EXTEND NORMALLY, NO CIRCUIT BREAKERS WERE POPPED AND HAD TO EMERGENCY EX TEND THE LANDING GEAR. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR SELECTOR VALVE IAW ATR42 MAINTENANCE MANUAL. 2 H 7 2 4T RT A53EU 2001012500182 20010125 00182 EU 2001 1 25 RAIA00101011 1 20010114 A 3234 F96GAD102 SELECTOR KNOB AEROSP ATR42 ATR42300 8680920 EU COCKPIT FAILED A RAIA O OTHER O OTHER DE DESCENT 1 CE 03 426TE 11422 471 228 7158-STL- DURING DESCENT LANDING GEAR WOULD NOT EXTEND NORMALLY, NO CIRCUIT BREAKERS WERE POPPED AND HAD TO EMERGENCY EX TEND THE LANDING GEAR. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR HANDLE IAW ATR42 MAINTENANCE MANUAL. 2 H 7 2 4T RT A53EU 2001012500183 20010125 00183 WP 2001 1 25 MWEA010046 1 20010111 A 5330 4917650 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 SKIN DENTED AND SHOVEL CLIP BENT AT STATION 994, LONGERON 29 RIGHT. MAINTENANCE REMOVED AND REPLACED SHOVEL CLIP, FABRI CATED AND INSTALLED SKIN REPAIR. 2 L 7 2 4F A6WE 2001012500184 20010125 00184 SO 2001 1 25 SWIA972262 1 20010110 A 3610 WARNING LIGHT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RIGHT ENGINE ILLUMINATED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 218SW 120287 RIGHT DUCT LEAK LIGHT ILLUMINATED PRIOR TO TAKEOFF. CLOSED RIGHT BLEED VALVE AND LIGHT REMAINED ILLUMINATED FOR MORE TH AN 3 MINUTES. SHUT DOWN RIGHT ENGINE. LIGHT REMAINED ILLUMINATED FOR FOUR MINUTES, UNTIL POWER DOWN. ABORTED TAKEOFF. RAN RIGHT ENGINE AND APU BLEEDS AND INSPECTED BLEED AIR DUCT FROM ENGINE NACELLE TO CROSSBLEED VALVE. NO LEAKS NOTED. INSPECTED DUCT LEAK SENSORS ALONG SAME AREA. NO DISCREPANCIES FOUND. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001012500186 20010125 00186 2001 1 25 SWIA972264 4 20010112 A 3197 WIRE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TAIL CONE BROKEN A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 292UX 120292 TAKEOFF AURAL WARNING TRIM WITH TRIM IN GREEN ARC. ABORTED TAKEOFF. FOUND BROKEN WIRE FOR RIGHT HAND SENSOR AT TAIL CO NE. RECONNECTED PER WIRING MANUAL 20-21-00 AND CHECKED RIGGING OF RIGHT HAND SENSOR PER MM 27-32-00. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001012500187 20010125 00187 SO 2001 1 25 SWIA972265 1 20010112 A 2731 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE ELEVATOR TRIM FROZEN A SWIA H DEACTIVATE SYST/CIRCUITS F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 293SW 120320 AFTER LEVEL OFF AT FL200 IT APPEARED THAT ELEVATOR TRIM WAS NOT TURNING WHEN COMMANDED BY AUTOPILOT. AUTOPILOT WAS DISE NGAGED AND ELEVATOR TRIM WAS FROZEN. AFTER DISENGAGE BELOW FREEZING LEVEL FOR 1.5 MINUTES, TRIM MOVED FREELY. REPLACED LEFT AND RIGHT ELEVATOR TRIM ACTAUTOR IAW EMB 120 MM CH 27-32-02. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001012500188 20010125 00188 SO 2001 1 25 SWIA972266 1 20010110 A 3060 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE PROP DEICE SYS ILLUMINATED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 584SW 120352 PROP DEICE FAILURE IN BOTH CYCLES. CIRCUIT BREAKER TRIPPED. FOLLOWED QRH PROCEDURES. PROP STILL FAILED. RETURNED TO LAX. RAN DEICE SYSTEM IAW 20-10-00. ALL CHECKS OK AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 2001012500189 20010125 00189 NE 2001 1 25 SWIA972267 3 20010113 A 6140 INDICATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE HAMSTD 14RF 14RF9 NE COCKPIT FAILED A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 584SW 120352 ON TAKEOFF, PASSING THROUGH 80 KNOTS RIGHT NP GAUGE FLUCTUATED FROM 100 PERCENT DOWN TO 50 PERCENT A FEW TIMES. ABORTED TAKEOFF. REPLACED RIGHT NP INDICATOR WITH SERVICEABLE UNIT. OPS CHECK GOOD. S/N ON B939, S/N OFF 105AB. 2 L 7 2 4T 4 T RT A31SO E20NE 6 C P11NE 2001012500190 20010125 00190 SO 2001 1 25 SWIA972268 1 20010108 A 3010 SWITCH EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT DEICE BOOTS FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 268UE 120207 RIGHT INBOARD STABILIZER DEICE BOOT INOP BOTH TIMERS. RETURNED TO FIELD. INSTALLED SERVICEABLE RIGHT STABILIZER PRESSU RE SWITCH, IAW MM 30-10-00. RAN ENGINES, OPS CHECKS GOOD. S/N ON: 00497912, S/N OFF: 548048. 2 L 7 2 4T 4 T RT A31SO E20NE 2001012500191 20010125 00191 SO 2001 1 25 SWIA972269 1 20010111 A 2722 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RUDDER TRIM FROZEN A SWIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 07 268UE 120207 AFTER LEAVING FL240 RUDDER TRIM FROZEN. RUDDER FREE WITH AND WITHOUT YAW DAMPNER TRIM BEGAN WORKING OUT OF 8-7 THOUSAND FEET. REMOVED AND REPLACED RUDDER TRIM ACTUATOR IAW RII 27-301. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001012500192 20010125 00192 2001 1 25 SWIA972270 4 20010114 A 3130 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TRIM SYSTEM MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 562SW 120336 TAKEOFF TRIM AURAL WARNING ON TAKEOFF. ABORTED TAKEOFF. TRIM IN GREEN BAND. POWERED DOWN AIRCRAFT. POWERED UP AIRCRA FT. PERFORMED OPERATIONAL CHECK OF AURAL TRIM WARNING SEVERAL TIMES. TRIM AURAL WARNING OPERATES NORMAL. OPS CHECKS G OOD. COULD NOT DUPLICATE DISCREPANCY. 2 L 7 2 4T 4 T RT A31SO E20NE 2001012500193 20010125 00193 EA 2001 1 25 SWIA972271 1 20010113 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 EA COCKPIT CRACKED A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 409SW 7056 CAPTAINS WINDSHIELD CRACKED AT FL 330. DIVERTED TO RAP. REMOVED AND REPLACED CAPTAINS WINDSHIELD WITH NEW WINDSHIELD I AW CRJ MM 56-11-01. LEAK CHECKS OK. P/N ON: PPG-NP-139321-5, S/N ON: 151H8911, SN/ OFF: 94173H8253. 2 L 7 2 4F RT A21EA 2001012500194 20010125 00194 NE 2001 1 25 COMA0160098 2 20010113 A 7270 6078T62G01 SPINNER CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LEFT ENGINE VIBRATION A COMA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SO 01 954CA 7100 LEFT ENGINE FAN VIB INDICATED 2.7. REPLACED THE AFT FAN SPINNER (OUT OF BALANCE). 2 L 7 2 4F 4 F RT A21EA E15NE 2001012500195 20010125 00195 2001 1 25 COMA0160099 4 20010113 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 710CA 7241 STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001012500196 20010125 00196 EA 2001 1 25 COMA0160100 1 20010112 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA RIGHT MALFUNCTIONED A COMA O OTHER N FALSE WARNING UK UNKNOWN 1 SO 01 759CA 5094 7279 FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT BPSU. 2 L 7 2 4F RT A21EA 2001012500197 20010125 00197 EA 2001 1 25 COMA0160101 1 20010113 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 EA OVERWING BURNED OUT A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 809CA 7366 OVERWING EMERGENCY LIGHT IS INOPERABLE. REPLACED THE LIGHT BULB. 2 L 7 2 4F RT A21EA 2001012500198 20010125 00198 EA 2001 1 25 COMA0160102 1 20010112 A 2613 356024310 ELEMENT CNDAIR CL600 CL6002B19 EA RT ENGINE MALFUNCTIONED A COMA E H ENGINE SHUTDOWN DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SO 01 797CA 7344 RT 14TH STAGE BLEED AIR LEAK WARNING. REPLACED THE PYLON LEAK SENSE ELEMENT. 2 L 7 2 4F RT A21EA 2001012500199 20010125 00199 EA 2001 1 25 COMA0160103 1 20010111 A 3020 300013000002 VALVE CNDAIR CL600 CL6002B19 EA RT ENGINE MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 739CA 11880 7273 RIGHT ENGINE COWL ANTI-ICE FAILED. REPLACED THE RT ANTI-ICE VALVE. 2 L 7 2 4F RT A21EA 2001012500200 20010125 00200 EA 2001 1 25 COMA0160104 1 20010111 A 5610 NP1393216 WINDSHIELD CNDAIR CL600 CL6002B19 EA COCKPIT LEAKING A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 951CA 3773 7091 HIGH PITCH SQUEALING NOISE FROM WINDSHIELD AREA. REPLACED THE COPILOTS WINDSHIELD. 2 L 7 2 4F RT A21EA 2001012500201 20010125 00201 2001 1 25 COMA0160105 4 20010111 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 976CA 7151 STALL FAIL CAUTION DURING TAKEOFF. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001012500202 20010125 00202 EA 2001 1 25 COMA0160106 1 20010111 A 2750 CONTROLLER CNDAIR CL600 CL6002B19 EA TE FLAPS FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 408CA 7440 FLAPS FAILED WHEN SELECTED FOR LANDING APPROACH. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98 20-01. 2 L 7 2 4F RT A21EA 2001012500203 20010125 00203 EA 2001 1 25 COMA0160107 1 20010110 A 3220 TORQUE LINK CNDAIR CL600 CL6002B19 EA NLG DISCONNECTED A COMA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 01 776CA 7293 NLG DID NOT RETRACT, TREMENDOUS SHUDDER ON ROLL. FOUND NLG TORQUE LINKS DISCONNECTED. CONNECTED TORQUE LINKS, INSPECTE D FOR DAMAGE, NONE FOUND. 2 L 7 2 4F RT A21EA 2001012500204 20010125 00204 EA 2001 1 25 COMA0160108 1 20010110 A 3250 16745101 SWITCH CNDAIR CL600 CL6002B19 EA NLG MALFUNCTIONED A COMA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SO 01 966CA 7132 STEERING INOPERABLE CAUTION DURING FLIGHT. REPLACED THE NWS PRESSURE SWITCH. 2 L 7 2 4F RT A21EA 2001012500205 20010125 00205 WP 2001 1 25 TWAA0100901 1 20010113 A 3350 60030431 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 964TW 53614 THE FWD LT AND RT OVERWING EMERGENCY EXIT SIGNS WERE INOPERATIVE. REPLACED THE POWER SUPPLY. CHECK-C 5-6-00 STL. 2 L 7 2 4F RT A6WE 2001012500206 20010125 00206 WP 2001 1 25 TWAA0100902 1 20010114 A 3350 SWITCH DOUG DC9 DC982 3022082 WP EGRESS LIGHTS INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 914TW 49185 THE EGRESS LIGHTING WAS INOPERATIVE FROM CABIN ROWS 5 TO 14. RECYCLED THE EMERGENCY LIGHT SWITCH. CHECK-C 2-3-00 STL. 2 L 7 2 4F A6WE 2001012500207 20010125 00207 WP 2001 1 25 TWAA0100903 1 20010113 A 2432 BATTERY DOUG DC9 DC982 3022082 WP BATTERY BAY OVERHEATED A TWAA H DEACTIVATE SYST/CIRCUITS M B P OVER TEMP SMOKE/FUMES/ODORS/SPARKS NO WARNING INDICATION IN INSP/MAINT 1 CE 05 929TW 48014 WHILE AT THE GATE SMOKE WAS SEEN COMING FROM THE ELECTRONIC COMPARTMENT. SHIPS BATTERY WAS HOT TO TOUCH AND EVENTUALLY SPARKING. AMPS WERE CHARGING THEN DISCHARGING EVERY FEW SECONDS. TURNED BATTERY SWITCH OFF. REPLACED BOTH SHIPS BATTE RIES (P/N 30475-002), AND THE BATTERY CHARGER (P/N 26340061-06). CHECK-C 3-30-00 STL. 2 L 7 2 4F A6WE 2001012500208 20010125 00208 WP 2001 1 25 TWAA0100904 1 20010112 A 2420 9008D093 RELAY DOUG DC9 DC983 3022083 WP COCKPIT ODOR A TWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 05 9303K 49529 AFTER TAKEOFF SEVERAL CIRCUIT BREAKERS POPPED ON THE RT AC BUS, INCLUDING THE RECIRCULATION FAN AND SEVERAL FUEL BOOST P UMPS. THERE WAS ALSO AN ODOR. FLIGHT RETURNED TO STL. NOTHING WAS FOUND AFTER MANY ELECTRICAL CHECKS. REPLACED THE R T GEN POWER RELAY. CHECK-C 12-24-00 STL. 2 L 7 2 4F RT A6WE 2001012500209 20010125 00209 WP 2001 1 25 TWAA0100905 1 20010108 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP AFT CARGO BAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9403W 53139 DURING CHECK-C MAINT THE SLANTED SIDE WALL ATTACH FLANGE ON AFT CARGO BIN RT FLOOR TIE DOWN FROM STA 1111 TO 1155 WAS CO RRODED. REPLACED TIE DOWN TRACK FROM STA 1111 TO 1155 PER SRM 53-05, PAGE 10R FIG 4G. 2 L 7 2 4F RT A6WE 2001012500210 20010125 00210 WP 2001 1 25 TWAA0100906 1 20010108 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP AFT CARGO BAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9403W 53139 DURING CHECK-C MAINT IN AFT CARGO BIN, SLANT SIDE LINING ATTACH FLANGE ON THE LT CARGO BIN FLOOR TIE DOWN WAS CORRODED F ROM STA 1117 TO 1174. REPAIRED TRACK PER SRM 53-05, FIG 4G. PRIMED AND SEALED PER SRM 51-10-05. 2 L 7 2 4F RT A6WE 2001012500212 20010125 00212 WP 2001 1 25 TWAA0100908 1 20010101 A 5320 CASTING DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9403W 53139 DURING CHECK-C MAINT AT STA 845, LBL 58, CASTING WAS CRACKED BELOW FLOOR AT FUSELAGE FORMER TO FLOORBEAM TIE, LT. INSTA LLED NEW CASTING PER DOUGLAS DRAWING 3920341 AND SPM 6-70-01. INSTALLED HI-LOKS PER SRM 51-60-0 PAGE 36 FIG 4 PIN SUBST ITUTION TABLE AND PER SRM 51-3-0 PAGE 12 HI-LOK INSTALLATION. TORQUED HI-LOKS PER SRM 51-30-1 PAGE 11 TO 13. 2 L 7 2 4F RT A6WE 2001012500213 20010125 00213 WP 2001 1 25 TWAA0100910 1 20010112 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9403W 53139 DURING CHECK-C MAINT ON RT SIDE OF CABIN FLOOR, CORROSION WAS BETWEEN STA 617 TO 636 ON FLOOR MEMBRANE AT LONGERON 18R. REMOVED CORRODED SECTION OF MEMBRANE AND INSTALLED DOUBLER PER SRM 53-01, FIG 4. 2 L 7 2 4F RT A6WE 2001012500214 20010125 00214 WP 2001 1 25 TWAA0100911 1 20010112 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9403W 53139 DURING CHECK-C MAINT CORROSION WAS FOUND ON MEMBRANE AT LONGERON 18R, BETWEEN STA 636 TO 653. REMOVED CORRODED SECTION OF MEMBRANE AND INSTALLED DOUBLER PER SRM 53-01, FIG 4. 2 L 7 2 4F RT A6WE 2001012500215 20010125 00215 WP 2001 1 25 TWAA0100912 1 20010103 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9403W 53139 DURING CHECK-C MAINT CABIN MEMBRANE WAS CORRODED AT STA 503 TO 597, RT SIDE CABIN FLOOR AT STA 18R AREA. REMOVED CORROS ION PER SPM 6-80-01. REPAIRED MEMBRANE PER SRM 53-01 FIG 4 SHEET 3 FIG 7. INSTALLED RIVETS PER SRM 51-30-02. REPAIR M ATERIAL 7975-T6, 0.020 MATERIAL. 2 L 7 2 4F RT A6WE 2001012500216 20010125 00216 WP 2001 1 25 TWAA0100913 1 20010103 A 5310 DOOR FRAME DOUG DC9 DC983 3022083 WP FWD SERVICE DOOR CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9403W 53139 DURING CHECK-C MAINT THE FWD SERVICE DOOR, CORROSION WAS FOUND AT DOOR FRAME OPENING AT LOWER FWD CORNER, STA 160, APPRO X RBL 58 INCHES. REMOVED CORROSION PER SPM 6-80-01. TREATED AND PAINTED PER SRM 51-10-32. INSTALLED REMOVED FASTENERS PER SRM 51-30. 2 L 7 2 4F RT A6WE 2001012500217 20010125 00217 WP 2001 1 25 TWAA0100909 1 20010104 A 5320 BRACKET DOUG DC9 DC983 3022083 WP CARGO DOORWAY CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9403W 53139 DURING CHECK-C MAINT THE MID CARGO DOOR, FWD SIDE, THE TOP AND BOTTOM DOOR STOP BRACKETS WERE CRACKED. REPLACED BOTH BR ACKETS PER SRM 51-34-5 AND DRAWING 5910141. 2 L 7 2 4F RT A6WE 2001012500218 20010125 00218 WP 2001 1 25 TWAA0100914 1 20010113 A 5230 MOUNT BRACKET DOUG DC9 DC983 3022083 WP CARGO DOORWAY CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9403W 53139 DURING CHECK-C MAINT THE AFT CARGO DOOR, AFT SIDE, THE SECOND FROM TOP AND UPPER DOOR STOP MOUNT BRACKETS WERE CRACKED. REPLACED BOTH BRACKETS PER SPM 6-70-01. 2 L 7 2 4F RT A6WE 2001012500219 20010125 00219 WP 2001 1 25 TWAA0100915 1 20010102 A 5320 BRACKET DOUG DC9 DC983 3022083 WP CARGO DOORWAY CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9403W 53139 DURING CHECK-C MAINT ON THE AFT CARGO DOOR FWD SIDE, THE UPPER AND SECOND FROM TOP DOOR STOP BRACKETS WERE CRACKED. REP LACED BOTH BRACKETS PER SPM 6-70-01. 2 L 7 2 4F RT A6WE 2001012500220 20010125 00220 WP 2001 1 25 TWAA0100916 1 20010110 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9404V 53140 DURING CHECK-C MAINT FOUND CORROSION AND WEAR ON CHAIR TRACK NUMBER 4, RBL 22 INCHES AND STA 807 TO 1022. REPLACED CHAI R TRACK PER SPM 6-70-01. 2 L 7 2 4F RT A6WE 2001012500221 20010125 00221 WP 2001 1 25 TWAA0100917 1 20010107 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9404V 53140 DURING CHECK-C MAINT AT STA 1231, LONGERON 29R TO 28L, FORMER HAD CORROSION ON AFT SIDE. CUT OUT DAMAGED FORMER AND SPL ICED IN NEW PART PER SRM 53-03, PAGE 4C. 2 L 7 2 4F RT A6WE 2001012500222 20010125 00222 WP 2001 1 25 TWAA0100918 1 20010110 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9404V 53140 DURING CHECK-C MAINT MEMBRANE BETWEEN STA 1271 AND 1309 AT STRINGER 18R WAS CRACKED AND CORRODED. CLEANED LIGHT CORROSI ON PER SPM 6-80-01 AND SRM 51-10-03. TREATED AND INSTALLED MEMBRANE REPAIR PER SRM 53-05, FIG 96. 2 L 7 2 4F RT A6WE 2001012500223 20010125 00223 WP 2001 1 25 TWAA0100919 1 20010110 A 5320 ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9404V 53140 DURING CHECK-C MAINT FOUND CRACK AT CANT STA 1463 AND SUPPORT ANGLE AT TOP OF PYLON AND LEFT AFT FUSELAGE. ACCOMP HIGH FREQ EDDY CURRENT PER 51-00-01 PART 6 AND FOUND CRACK CONTAINED AT STOP DRILLED HOLES. REPAIRED PER SRM 54-04 FIG 10. 2 L 7 2 4F RT A6WE 2001012500224 20010125 00224 WP 2001 1 25 TWAA0100920 1 20010109 A 5310 STRUCTURE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9404V 53140 DURING CHECK-C MAINT FOUND CORROSION AT ATTACH HOLES FOR FUSELAGE FILLET AREA, BENEATH RUB STRIP AT STA 1104 TO 1136, LO WER LT SIDE. REMOVED CORROSION FROM ATTACH HOLES PER SPM 6-10-01. REPAIR MATERIAL LOSS PER PART 1-51-04-00 MARKED ON S KIN. 2 L 7 2 4F RT A6WE 2001012500225 20010125 00225 WP 2001 1 25 TWAA0100921 1 20010110 A 5310 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9404V 53140 DURING CHECK-C MAINT CORROSION WAS FOUND ON THE AFT CARGO DOOR JAMB CORNER SUPPORT AT STA 1155 LONGERON 28R, AND STA 121 2 LONGERON 28R. REPLACED DOOR JAM CORNER SUPPORTS PER SRM 51-01, PAGE 1 ITEM C. 2 L 7 2 4F RT A6WE 2001012500226 20010125 00226 WP 2001 1 25 TWAA0100922 1 20010111 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9404V 53140 DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT BETWEEN STA 160 AND 200, 53 INCHES RBL. FABRICATED NEW TRACK AND INSTALLED PER SRM 51-30-2. TREATED PART PER SRM 51-10-3. 2 L 7 2 4F RT A6WE 2001012500227 20010125 00227 WP 2001 1 25 TWAA0100923 1 20010109 A 5210 WEB DOUG DC9 DC983 3022083 WP AFT PAX DOOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9404V 53140 DURING CHECK-C MAINT IN AFT ENTRY DOOR FOUND CRACK IN WEB ON RT OUTBOARD BOTTOM PORTION OF DOOR, APPROX 12 INCHES FROM B OTTOM OF DOOR. REPAIRED WEB PER SRM 51-70-4 FIG 2. INSTALLED STACK DOUBLER PER 52-61 FIG 2. TREATED AREA PER 51-10-3. 2 L 7 2 4F RT A6WE 2001012500228 20010125 00228 WP 2001 1 25 TWAA0100924 1 20010111 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9404V 53140 DURING CHECK-C MAINT FOUND TIE DOWN TRACK CORRODED AT STA 1219 TO 1320, LT SIDE AFT CARGO BIN. REPLACED TRACK PER SRM 5 3-01 PAGE 4. 2 L 7 2 4F RT A6WE 2001012500229 20010125 00229 WP 2001 1 25 TWAA0100925 1 20010111 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9404V 53140 DURING CHECK-C MAINT FLOOR SUPPORT AT STA 153 RBL 44 INCHES, AND STA 160 RBL 45 INCHES, WAS CORRODED. FABRICATED NEW TR ACK AND INSTALLED PER SRM 51-30-2. TREATED PER SRM 51-10-3. 2 L 7 2 4F RT A6WE 2001012500230 20010125 00230 WP 2001 1 25 TWAA0100926 1 20010102 A 5320 WEB DOUG DC9 DC983 3022083 WP CABIN CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9404V 53140 DURING CHECK-C MAINT FLOOR MEMBRANE WAS CRACKED AT LT SIDEWALL, STA 1298 TO 1304. STOP DRILLED CRACK AND INSTALLED DOUB LER PER SRM 53-01, FIG 2. TREATED SURFACE PER SRM 51-10-03. INSTALLED HI-LOKS IN DOUBLER DUE TO ACCESS PER SRM 53-30-0 5. INSTALLED RIVETS PER SRM 51-30-2. 2 L 7 2 4F RT A6WE 2001012500233 20010125 00233 EU 2001 1 25 A6WA200100001 1 20010113 A 3210 LANDING GEAR BAG BAE146 BAE146200A 1500266 EU RIGHT ICED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 292UE E2087 RIGHT MAIN LANDING GEAR WOULD NOT RETRACT. MAINTENANCE FOUND THAT MLG SWITCHES HAVE EXTREME ICE BUILD-UP. DEICED GEAR, INSPECTED AND FOUND NO DAMAGE TO GEAR. 2 H 7 4 4F RT A49EU 2001012500234 20010125 00234 WP 2001 1 25 MWEA010045 1 20010115 A 3010 39271012 VALVE DOUG DC9 DC932 3022066 WP TAIL SECTION INOPERATIVE A MWEA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 GL 31 216ME 47740 LEFT ICE PROTECTION LIGHT HI TEMP ILLUMINATED 2 MINUTES AFTER TAKEOFF. REPLACED AUGMENTATION VALVE AND ANTICIPATOR ASSY . 2 L 7 2 4F A6WE 2001012500235 20010125 00235 NM 2001 1 25 MWEA010052 1 20010114 A 3260 833605 PROXIMITY SWITCH DOUG MD88 MD88 3023688 NM E/E BAY INOPERATIVE A MWEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 701ME 49760 AFTER TAKEOFF, ALL 3 RED GEAR UNSAFE LIGHTS REMAINED ILLUMINATED WITH GEAR UP. REMOVED AND REPLACED PROXIMITY ELECTRONI C BOX. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A6WE 2001012500236 20010125 00236 EA 2001 1 25 A6WA200100002 1 20010113 A 2611 WARNING LIGHT CNDAIR CL600 CL6002B19 EA LAVATORY FALSE ACTIVATION A A6WA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 GL 31 402AW 7281 INFLIGHT, RECEIVED SMOKE TOILET MESSAGE, C/W CHECKLIST, MESSAGE WENT OUT PRIOR TO COMPLETION OF CHECKLIST. MAINTENANCE INSPECTED LAV DUCTING AND FIRE EXTINGUISHER ALL FOUND TO BE GOOD. PERFORMED PACK BURNOUT PROCEDURE AS A PRECAUTION. 2 L 7 2 4F RT A21EA 2001012500246 20010125 00246 NM 2001 1 25 VNAA0101001 1 20010101 A 7332 WARNING LIGHT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FUEL PRESSURE ILLUMINATED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 460PS 3061 DURING THE TAKEOFF ROLL, THE CREW RECEIVED A RIGHT HAND FUEL PRESSURE LOW LIGHT ILLUMINATION AND THE CREW ABORTED TAKEOF F. THE CREW CLEARED THE RUNWAY AND THE LIGHT EXTINGUISHED. THE CREW PERFORMED AN ENGINE RUN WHICH CHECKED GOOD. THE C REW WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001012500249 20010125 00249 NM 2001 1 25 VNAA0101003 1 20010105 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN FAILED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 425JS 12756 3037 THE CREW REPORTED THE THE EMERGENCY LIGHTING WAS NOT ILLUMINATING AROUND THE 4LK LOCATION. MAINTENANCE INSPECTED AND RE PLACED THE EMERGENCY BATTERY AT THE 4LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CH ECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001012500291 20010125 00291 SO 2001 1 25 C2XA011A008 1 20010105 A 3260 922AA2YA6PZ722 PROXIMITY SWITCH EMB 120 EMB120RT SO RT MLG DIRTY A C2XA O OTHER J WARNING INDICATION LD LANDING 1 SW 27 27716 120128 IAH - FLT 3565 - THE CREW REPORTED A LANDING GEAR DISAGREEMENT BEFORE AND AFTER LANDING. THE RIGHT MAIN LANDING GEAR IN DICATIONS, ''A'' RED AND ''B'' GREEN, ILLUMINATED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED THE DOWN LOCK PROXIMITY SWITCH AND PERFORMED FUNCTIONAL CHECKS IAW EMB-120 MM 32-60-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE (M) 2 L 7 2 4T RT A31SO 2001012500292 20010125 00292 SO 2001 1 25 C2XA0011A009 1 20010105 A 2150 A/C PACK EMB 120 EMB120RT SO AC BAY MALFUNCTIONED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 58733 120197 LRD - FLT 3564 - THE CREW REPORTED SMOKE IN THE CABIN AND PERFORMED AN AIR RETURN. THE AIRCRAFT LANDED WITHOUT INCIDENT . MAINTENANCE DETERMINDED THE SOURCE OF THE SMOKE TO BE COMING FROM THE NR 2 AIRCONDITIONING PACK AFTER PERFORMING OPER ATIONAL CHECKS OF THE BLEED AIR SYSTEM. MAINTENANCE PLACED THE NR 2 AIRCONDITIONING PACK ON MEL REFERENCE 21-50-2, CATE GORY ''C'' CONTROL NR 003481. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001012500293 20010125 00293 SO 2001 1 25 C2XA011A010 1 20010105 A 2140 A/C PACK EMB 120 EMB120RT SO AC BAY MALFUNCTIONED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 58733 120197 IAH - FLT 3418 - THE CREW REPORTED A BURNING SMELL IN THE COCKPIT WHEN SELECTING HEAT FROM THE NR 1 AIRCONDITIONING PACK DURING FLIGHT. MAINTENANCE PERFORMED OPERATIONAL CHECK OF THE NR 1 AIRCONDITIONING PACK IAW EMB-120MM 21-40-00 AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001012500294 20010125 00294 SO 2001 1 25 C2XA011A011 1 20010104 A 2150 A/C PACK EMB 145 EMB145LR SO AC BAY MALFUNCTIONED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 16951 145063 IAH - FLT 4216 - THE CREW REPORTED RELAYS CLICKING AND A BURNING ODOR IN THE COCKPIT. MAINTENANCE DETERMINED THE SOURCE OF THE BURNING ODOR TO BE COMING FROM THE NR 1 AIRCONDITIONING PACK. THE NR 1 AIRCONDITIONING PACK WAS PLACED ON MEL R EFERENCE 21-51-00, CATEGORY ''C'' CONTROL NR 003258. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001012500331 20010125 00331 SO 2001 1 25 C2XA01CL001 1 20010108 A 3350 110049 CHARGER EMB 135 EMB135ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16501 145145 CLE - FLT 4135 - THE CREW REPORTED THAT THE 2ND AND 3RD SEAT OF AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE DURING THER E PREFLIGHT CHECK. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY IAW EMB135 MM 33- 50-04. MAINTENANCE ALSO REPLACED THE NR 2 EMERGENCY LIGHT BATTERY IAW 33-50-04. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001012500350 20010125 00350 2001 1 25 20010124SG003 4 20010103 A 2200 5223712018 COMPUTER BOEING 727 727225 1384077 NM E/E COMPT MALFUNCTIONED A MYWA O OTHER F I FLT CONT AFFECTED FLT. ATTITUDE INST. CR CRUISE 1 SO 19 806MA 22437 AUTO PILOT PORPOISES IN CRUISE MODE ''A'' CONTINUOUSLY TRIMS STAB UP AND DOWN. REMOVED AND REPLACED AUTO PILOT PITCH CO MPUTER. OPS CHECK OK IAW MM 22-11-12. (M) 2 L 7 3 4F A3WE 2001012500352 20010125 00352 NM 2001 1 25 UHLA012977 1 20010103 A 3350 307BPE LIGHT DHAV DHC8 DHC8301 NM CABIN INOPERATIVE A UHLA K NONE L NO TEST IN INSP/MAINT 1 NE 03 806SA 279 BUF-RON - DURING MAINTENANCE INSPECTION, SEVERAL EMERGENCY EXIT LIGHT BULBS WERE BURNED OUT. BULBS WERE REMOVED AND REP LACED IAW DMM 33-51-03. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 2001012500353 20010125 00353 EA 2001 1 25 UHLA002982 1 20010108 A 5210 85210240007 HAND RAIL DHAV DHC8 DHC8311 1386006 EA MAIN CABIN DOOR BROKEN A UHLA K NONE O OTHER TX TAXI/GRND HDL 1 NE 03 803SA 19092 221 FLT 268 - LGA-BED - AFTER ARRIVAL IN BED MAIN CABIN HANDRAIL SUPPORT WAS FOUND BROKEN, DOOR OPENING WAS NORMAL. MAINTEN ANCE REMOVED AND REPLACED THE HANDRAIL SUPPORT ASSY, AIRCRAFT RETURNED TO SERVICE. REF AMR/WO 4703. (M) 2 H 7 2 4T RT A13NM 2001012600001 20010126 00001 EU 2001 1 26 QXEA0100020 1 20010110 A 3350 1820 LIGHT FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 483US 11233 GEG-EXIT SIGN ABOVE COCKPIT DOOR HAS 28V LAMPS INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK GOO D. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001012600002 20010126 00002 NM 2001 1 26 CALA0100031 1 20010115 A 5320 BRACKET BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14381 26310 INSPECTION FOUND A 1 INCH CRACK IN FORWARD BAGGAGE BIN ANGLE BRACKET AT STA 380, S26R. THE ANGLE BRACKET WAS REMOVED AN D REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001012600004 20010126 00004 NM 2001 1 26 SCNA01009 1 20010116 A 5210 DOOR BOEING 727 727225 1384077 NM FWD ENTRY OUT OF ADJ A SCNA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 OPMN 21578 DURING CLIMB THE FORWARD ENTRY DOOR EXIBITED AN EXTREMELY LOUD SQUEAL IN FLIGHT, THE SOUND DID NOT ALTER DUE TO CHANGES IN AIRSPEED, ALTITUDE OR CABIN PRESSURE. THE FLIGHT CREW ELECTED TO RETURN TO MSP, THE POINT OF ORIGIN. REPOSITIONED T HE DOOR SNUBBER, AND LOWER HINGE SEAL, RECONDITIONED LOWER DOOR FRAME CORNERS. PRESSURIZED AIRCRAFT TO 7.0 PSI, OPERATI ONAL CHECK GOOD. 2 L 7 3 4F A3WE 2001012600009 20010126 00009 WP 2001 1 26 TWAA0101003 1 20010116 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 929TW 48014 THE FIRST CLASS OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE POWER SUPPLY IN NUMBER 3 POSITION (P/N 60-0304 -516B), AND REPLACED BATTERIES IN NUMBER 2 AND 3 POWER SUPPLIES (P/N 408822-101). CHECK-C 3-30-00 STL. 2 L 7 2 4F A6WE 2001012600010 20010126 00010 NM 2001 1 26 01FDEA00009 1 20010112 A 5713 0044308 STRINGER BOEING 727 727232 1384082 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 RT WING VENT STR 13 AT WS 686.50 IS CRACKED AT RIB ATTACH POINT. *S/D* REMOVED AND REPLACED PER IAW FEDEX EA 7-5710-56 217. 2 L 7 3 4F A3WE 2001012600011 20010126 00011 EA 2001 1 26 COMA0110009 1 20010112 A 5350 12031657001 FAIRING CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 267CA 21508 120259 THE AIRCRAFT LEFT AND RIGHT WING ATTACH ANGLES ARE CRACKED. THE ANGLES WERE REPAIRED IN ACCORDANCE WITH SRM CHAPTER 53- 20-13 PAGES 205 AND 206 AND AERODESIGN REPORT 1226-21. 2 L 7 2 4F RT A21EA 2001012600025 20010126 00025 NM 2001 1 26 01FDEA00022 1 20010116 A 2780 WIRE BOEING 727 727233 138408A NM SLAT CONTROL FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 283FE 22350 DURING FLAP RETRACT (FROM 5 DEG TO 2 DEG) DID NOT GET A GREEN LEAD EDGE FLAP LIGHT, 2ND OFF. POSITION IND SHOW NR 7 INT RANSIT. *S/D* REPAIRED WIRES AS PER CHAP 20 WIRING DIAGRAM PER 27-81-01, 27-82-00-1. 2 L 7 3 4F RT A3WE 2001012600029 20010126 00029 WP 2001 1 26 EIA2001006 1 20010105 A 3230 LANDING GEAR DOUG DC9 DC933F 302207A WP NLG MALFUNCTIONED A EIAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 941F 47193 FLT 823 - KSEA - NOSE GEAR FAILED TO RETRACT FULLY, LOUD NOISE IN NLG W/W AREA. NOSE GEAR UNSAFE LIGHT REMAINED ON WITH GEAR HANDLE UP. CYCLED SEVERAL TIMES, LIGHT REMAINED ON. INSPECTED NLG WHEEL WELL AREA, COMPONENTS, WIRING, GEAR HAND LE, NO DEFECTS. LUBED NLG COMPONENTS. PERFORMED RETRACT TEST. CYCLED NLG THROUGH 10 COMPLETE CYCLES. SYSTEM AND INDI CATION LIGHTS OP NORMAL. RII ACCOMPLISHED. (M) 2 L 7 2 4F A6WE 2001012600030 20010126 00030 WP 2001 1 26 EIA20001006 1 20010105 A 3230 LANDING GEAR DOUG DC9 DC933F 302207A WP NLG MALFUNCTIONED A EIAA O OTHER J WARNING INDICATION TO TAKEOFF 1 NM 09 941F 47193 KSEA - NOSE GEAR FAILED TO RETRACT FULLY. LOUD NOISE IN NLG W/W AREA. (M) 2 L 7 2 4F A6WE 2001012600038 20010126 00038 2001 1 26 GLBA2001007 4 20010114 A 6122 GOVERNOR BEECH 1900 1900D 1154162 CE HARTZL HCE4A HCE4A3I NE RT PROPELLER MALFUNCTIONED A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 01 251GL UE251 HJ395 ABORTED T/O - RIGHT PROP RPM WENT TO 1900 ON T/O ROLL. INSPECTED INDICATING, SYSTEM COULD NOT DUPLICATE FAULT. SYSTEM OPS CHECKED GOOD. RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 5 C P10NE 2001012600039 20010126 00039 NM 2001 1 26 UPS01534621 1 20010116 A 2130 13056026 CONTROL PANEL BOEING 757 75724APF 1384969 NM CABIN MALFUNCTIONED A IPXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 411UP 23851 INSPECTION TYPE:IN ATB UNABLE TO PRESS A/C. FOUND CHECK PACK 9, OPS NORMAL. BITE MHZ 21.5. REMOVED AND REPLACED PRESS CONTROL OF MM 21-31-01 AND PERFORMED CHECK OF PRESSURIZATION ON MANUAL WORKING NORMAL. PANEL REMOVED. 2 L 7 2 4F RT A2NM 2001012600048 20010126 00048 NM 2001 1 26 CALA0100020 1 20010114 A 3397 WIRE BOEING 757 757224 1384958 NM EXIT LIGHT SHORTED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14118 27560 INSPECTION FOUND EMERGENCY EXIT LIGHT AT R-4 DOOR INOPERATIVE. MAINTENANCE FOUND A SHORTED WIRE. THE WIRE WAS REPAIRED IAW WDM 33-51-15. 2 L 7 2 4F RT A2NM 2001012600049 20010126 00049 NM 2001 1 26 CALA0100026 1 20010115 A 5330 PANEL BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19623 27527 INSPECTION FOUND LT TRANSITION PANEL IN AFT CARGO PIT CORRODED AT SEVERAL FASTENER HOLES FROM STA 727 - 927. THE PANEL WAS REMOVED AND REPLACED WITH A NEW PANEL IAW SRM 51-40-2. 2 L 7 2 4F RT A16WE 2001012600050 20010126 00050 WP 2001 1 26 UPS01834632 1 20010116 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:N/A, EMERGENCY LIGHTS NOT ON IN ARMED. REMOVED AND REPLACED BATTERY PACK, OP''S CHECK NORMAL. P/N ON - OFF: 5708458-503, S/N ON: FTL243, S/N OFF: 7. 2 L 7 4 4F RT 4A25 2001012600051 20010126 00051 WP 2001 1 26 CALA0100028 1 20010115 A 5311 FRAME DOUG DC10 DC1030 3023501 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND A .5 INCH CRACK IN CENTER CARGO FRAME AT STA 1841. REPAIRED IAW SRM 53-00-01, FIGURE 4, SHEET 2. 2 L 7 3 4F A22WE 2001012600052 20010126 00052 NM 2001 1 26 CALA0100029 1 20010115 A 5320 BRACKET BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73380 26309 INSPECTION FOUND A 1 INCH CRACK IN FORWARD BAGGAGE BIN ANGLE BRACKET AT STA 380, S26L. THE ANGLE BRACKET WAS REMOVED AN D REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001012600053 20010126 00053 WP 2001 1 26 CALA0100030 1 20010116 A 3222 STRUT DOUG DC9 DC981 3022081 WP NLG DISCHARGED A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 37882 48027 THE NLG WOULD NOT RETRACT AFTER TAKEOFF FROM BOS. THE AIRCRAFT WAS RETURNED TO BOS WHERE IT LANDED WITHOUT INCIDENT. M AINTENANCE SWUNG THE NOSE GEAR SEVERAL TIMES AND WAS UNABLE TO DUPLICATE THE FAILURE. THE STRUT PRESSURE WAS FOUND LOW. THE NOSE STRUT WAS SERVICED AND THE NOSE GEAR WAS LUBRICATED IAW MM 32-21-02. 2 L 7 2 4F A6WE 2001012600054 20010126 00054 WP 2001 1 26 TWAA0101005 1 20010103 A 5210 STOP DOUG DC9 DC983 3022083 WP PAX DOOR CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9404V 53140 DURING CHECK-C MAINT, FOUND ON THE AFT PASSENGER DOOR TWO STOPS AT THE BOTTOM OF THE DOOR HAD EXFOLIATION CORROSION DELA MINATING MATERIAL. REMOVED DAMAGED STOPS AT BOTTOM AFT PASSENGER DOOR. REPLACED BOTH ANGLES PER SPM 6-70-01. 2 L 7 2 4F RT A6WE 2001012600055 20010126 00055 WP 2001 1 26 TWAA0101006 1 20010103 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9404V 53140 DURING CHECK-C MAINT, FOUND CORROSION ON MEMBRANE AT LONGERON 18R, STATION 1060 AND 1079. REPAIRED FLOOR MEMBRANE PER S RM 51-70-4. 2 L 7 2 4F RT A6WE 2001012600056 20010126 00056 EA 2001 1 26 COMA0160109 1 20010113 A 3234 7455021 HANDLE CNDAIR CL600 CL6002B19 EA INST PANEL MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 818CA 1447 7408 LANDING GEAR DOES NOT RETRACT WHEN SELECTED UP. REPLACED THE GEAR SELECTOR HANDLE. 2 L 7 2 4F RT A21EA 2001012600057 20010126 00057 WP 2001 1 26 TWAA0101007 1 20010104 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9404V 53140 DURING CHECK-C MAINT, FOUND CORROSION ON BOTTOM OF FLOOR MEMBRANE, STA 671 AND LBL 57. REPAIRED MEMBRANE PER SRM 51-70- 4. 2 L 7 2 4F RT A6WE 2001012600058 20010126 00058 WP 2001 1 26 TWAA0101008 1 20010105 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9404V 53140 DURING CHECK-C MAINT, FOUND FLOOR SUPPORT CORRODED AT STA 187 TO 194, RBL 6 TO 9. INSTALLED NEW FLOOR SUPPORT PER SRM 5 1-01. 2 L 7 2 4F RT A6WE 2001012600059 20010126 00059 WP 2001 1 26 TWAA0101009 1 20010105 A 5350 FAIRING DOUG DC9 DC983 3022083 WP RUDDER CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9404V 53140 DURING CHECK-C MAINT, FOUND 2 INCH BREAK IN RUDDER LEADING EDGE WRAP AROUND FAIRING ON RT SIDE, 60 INCHES DOWN FROM TOP. REPAIRED PER SRM 51-70-1A. 2 L 7 2 4F RT A6WE 2001012600060 20010126 00060 WP 2001 1 26 TWAA0101010 1 20010106 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9404V 53140 DURING CHECK-C MAINT, SEAT TRACK WAS CORRODED FROM STA 1032 TO 1122, LBL 44 INCHES. CUT OUT CORRODED TRACK SECTION AND SPLICED IN NEW SECTION OF TRACK PER SRM 53-05, FIG 4F. 2 L 7 2 4F RT A6WE 2001012600061 20010126 00061 WP 2001 1 26 TWAA0101011 1 20010109 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT, CABIN FLOOR PANEL ATTACH ANGLE HAD CORROSION APPROX STA 160 TO 200, RBL 52. 2 L 7 2 4F RT A6WE 2001012600062 20010126 00062 WP 2001 1 26 TWAA0101014 1 20010109 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT ON THE RT CABIN SIDEWALL, STA 275 TO 237, RBL 58, CORROSION WAS FOUND ON TOP AND BOTTOM OF WEB MEMB RANE AROUND LIGHTENING HOLES. CLEANED CORROSION PER SPM 6-80-01. ALODINED AND PAINTED PER SRM 51-10-3. INSTALLED DOUB LER PER SRM 53-01 FIG 2. 2 L 7 2 4F RT A6WE 2001012600063 20010126 00063 WP 2001 1 26 TWAA0101015 1 20010110 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP COCKPIT CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT, COCKPIT FLOOR SUPPORT ANGLE HAD CORROSION AT STA 148 TO 157, CENTER FLOOR SUPPORT APPROX LBL 12. INSTALLED NEW FLOOR SUPPORT PER SRM 51-1-0 WITH BOLTS PER SRM 51-30-0. 2 L 7 2 4F RT A6WE 2001012600064 20010126 00064 WP 2001 1 26 TWAA0101016 1 20010111 A 5313 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING CHECK-C MAINT, LONGERON 5L WAS CRACKED AT FORMER RING AT STA 737. FOUND DURING VISUAL INSPECTION FOR MD8-AD-AM. INSTALLED NEW SECTION OF LONGERON AND MANUFACTURED NEW SPLICE AND INSTALLED SPLICE ON SAID LONGERON PER SRM 53-02 PAGE 5, FIG 3. 2 L 7 2 4F A6WE 2001012600065 20010126 00065 WP 2001 1 26 TWAA0101017 1 20010111 A 5313 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING CHECK-C MAINT, LONGERON 2R WAS CRACKED AT FORMER RING AT STA 658. FOUND DURING VISUAL INSPECTION FOR MC8-AD-AM. REPLACED CRACKED SECTION OF LONGERON AND SPLICED NEW SECTION PER SRM 53-02 PAGE 48. 2 L 7 2 4F A6WE 2001012600066 20010126 00066 WP 2001 1 26 TWAA0101018 1 20010111 A 5280 DOOR DOUG DC9 DC983 3022083 WP LT MLG CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9628W 53598 DURING CHECK-C MAINT FOUND 3 INCH CRACK IN LT MAIN GEAR DOOR PAN AT OUTBOARD CORNER. INSTALLED REPAIR DOUBLER PER SRM 5 2-05, FIG 28. 2 L 7 2 4F RT A6WE 2001012600069 20010126 00069 WP 2001 1 26 TWAA0101001 1 20010116 A 3240 NAS161208 O-RING DOUG DC9 DC982 3022082 WP RT MLG WORN A TWAA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 CE 05 904TW 49156 IN DESCENT INTO SAT THE RT HYDRAULIC QUANTITY WENT TO ZERO. IT WAS NECESSARY TO MANUALLY EXTEND THE LANDING GEAR, AND T O BE TOWED OFF THE RUNWAY AFTER LANDING. REPLACED THE O-RING ON THE RT HYDRAULIC BRAKE PRESSURE MANIFOLD PLUG PORT DUE TO LEAKING HYDRAULIC FLUID. CHECK-C 3-20-00 STL. 2 L 7 2 4F A6WE 2001012600070 20010126 00070 WP 2001 1 26 TWAA0101002 1 20010116 A 3350 408822101 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 952U 49266 THE FIRST CLASS OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED TWO BATTERIES IN POWER SUPPLY. CHECK-C 3-3-00 MCI . 2 L 7 2 4F A6WE 2001012600071 20010126 00071 NM 2001 1 26 TWAA0101004 1 20010115 A 3350 767 LAMP BOEING 757 757231 1384950 NM L2 CABIN DOOR INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 725TW 30338 THE LEFT SIDE NUMBER 2 CABIN DOOR SLIDE LIGHT WAS INOPERATIVE. REPLACED THE LAMP. 2 L 7 2 4F RT A2NM 2001012600074 20010126 00074 2001 1 26 JBXA000237 4 20010118 A 3140 6229820007 PUMP CNDAIR CL600 CL6002B19 EA LT MAIN EJECTOR FAILED A JBXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 05 588ML 7368 LEFT MAIN EJECTOR PUMP FAILED. REMOVED AND REPLACED LEFT ENGINE FUEL FEED PRESSURE SWITCH IAW CRJ AMM 28-42-04. THIS W AS NOT A GOOD FIX. REMOVED AND REPLACED NR 2 DCU IAW CRJ AMM 31-41-04. PERFORMED OPERATIONAL TEST OF EJECTOR PUMP IAW CRJ AMM 28-42-04. ALL OPERATIONAL CHECKS GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2001022600110 20010226 00110 SO 2001 2 26 C2AX01IA031 1 20010117 A 2150 A/C PACK EMB 120 EMB120ER 3260203 SO NR 2 FAILED A C2XA B G A EMER. DESCENT O2 MASK DEPLOYED UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 57734 120199 CLL - FLIGHT 3463, THE CREW REPORTED SMOKE IN THE CABIN. AN EMERGENCY WAS DECLARED, THE OXYGEN MASKS DEPLOYED, AND THE AIRCRAFT RETURNED TO CLL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THAT THE NUMBER TWO PACK HAD FAILED. THE NUMBER TWO PACK WAS PLACED ON MEL 21-50-02 CONTROL NUMBER 004810, AND THE AIRCRAFT WAS APPROV ED FOR RETURN TO SERVICE, THE AIRCRAFT WENT TO SHV ON 01/18/01 WHERE MAINTENANCE PERFORMED EXTENDED OPERATIONAL CHECKS O F HTE NR 2 PACK SYSTEM WITH NO DEFECTS NOTED, REMOVED MEL 21-50-02 CONTROL 004810, AND THE AIRCRAFT WAS APPROVED FOR RET URN TO SERVICE. 2 L 7 2 4T RT A31SO 2001012600075 20010126 00075 EU 2001 1 26 01FDEA00026 1 20010118 A 2611 SMOKE WARNING AIRBUS 310 A310203 EU CARGO BAY ACTIVATED A FDEA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 408FE 257 ON APR AT 1000 FT CONFIG TO LAND GOT CARGO SMOKE ALARM/WARN LIGHTS. 2 L 7 2 4F RT A35EU 2001012600076 20010126 00076 NM 2001 1 26 0100142289 1 20010113 A 2730 680005007 PCU BOEING 727 727251 138408H NM RT ELEVATOR FAILED A NWAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 01 289US 34504 13797 21377 DURING TAKEOFF, AIRCRAFT WAS DIFFFICULT TO ROTATE. EXCESSIVE AMOUNT OF PRESSURE WAS REQUIRED TO PULL YOKE AFT. AFTER R OTATION YOKE WOULD NOT RETURN TO CENTER AND REQUIRED FORCEFUL FORWARD MOVEMENT IN CENTER CONTROL. FLIGHT RETURNED TO MC O AND MADE AN UNEVENTFUL LANDING. MAINTENANCE REPLACED THE FLIGHT ELEVATOR PCU. LEAK AND OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 2001012600077 20010126 00077 NM 2001 1 26 0100165521 1 20010110 A 2121 731376 FAN BOEING 757 757251 1384970 NM E/E BAY FAILED A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 01 521US 46937 20101 23209 DURING DESCENT, FLIGHT CREW NOTICED SMOKE ODOR IN FLIGHT DECK. DECLARED AN EMERGENCY AND MADE AN UNEVENTFUL LANDING. M AINTENANCE REPLACED THE NR 1 EQUIPMENT COOLING FAN. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A2NM 2001012600078 20010126 00078 NE 2001 1 26 0100179760 2 20010110 A 7200 ENGINE DOUG DC9 DC941 302207N WP PWA JT8 JT8D11 52044 NE RIGHT STALLED A NWAA E A ENGINE SHUTDOWN UNSCHED LANDING T J ENGINE CASE PENETRATION WARNING INDICATION CL CLIMB 1 GL 01 760NW 2583 47288 676246 ON CLIMB, JUST AFTER ROTATION, THE RIGHT ENGINE EXPERIENCED A SEVERE COMPRESSOR STALL AND AN UNCONTAINED ENGINE FAILURE . THE FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE. 2 L 7 2 4F 4 F A6WE E2EA 2001012600079 20010126 00079 NM 2001 1 26 VNAA0101005 1 20010105 A 5610 SPSDO328311 WINDOW DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT CRACKED A VNAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 432JS 2950 3045 DURING CLIMBOUT, AT 6000 FEET THE CREW NOTICED THAT THE RIGHT HAND SIDE WINDOW HAD CRACKED. THE CREW NOTIFIED ATC AND R ETURNED TO PIT FOR MAINTENANCE. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND SIDE WINDOW IN ACCORDANCE WITH DORNIE R MAINTENANCE MANUAL 56-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001012600080 20010126 00080 NM 2001 1 26 QXEA0100023 1 20010113 A 6123 CONNECTOR DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER SYS LOOSE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 347PH 480 PDX - AUTO FEATHER WILL NOT TEST. TIGHTENED NR 1 AND NR 2 ENGINE TCS CANNON PLUGS. AUTOFEATHER SYSTEM POWER SYSTEM TEST GOOD THROUGH DHC-8 ENGINE RIGGING MANUAL 3-63, TEST 6-8. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001012600083 20010126 00083 WP 2001 1 26 AT0100001 1 20010112 A 3222 STRUT DOUG DC9 DC932 3022066 WP NLG DISCHARGED A ZZDA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 15 866AT 47168 UNABLE TO RAISE GEAR ON TAKEOFF. SUSPECT SQUAT SWITCH PROBLEM. TRIED GEAR LEVER SEVERAL TIMES. SERVICED NOSE STRUT WI TH NITROGEN IAW MM 32-21. PERFORMED CHECK OF GROUND SENSING SWITCHES IAW MM 32-23-01. 2 L 7 2 4F A6WE 2001012600084 20010126 00084 WP 2001 1 26 0100189928 1 20010113 A 5320 PIN DOUG DC9 DC931 3022065 WP AFT CARGO NET DAMAGED A NWAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 01 8921E 45836 DURING TAKEOFF, THE AFT CARGO DOOR OPEN LIGHT ILLUMINATED. AIRCRAFT ABORTED TAKEOFF AT 105 KNOTS. ACCOMPLISHED COM PRO CEDURE FOR HIGH ENERGY BRAKING AND AIRCRAFT CLEARED THE RUNWAY SAFELY. MAINTENANCE REPLACED THE AFT CARGO NET RETAINING PIN, RESET CARGO DOOR LIGHT, AND COMPLETED A HIGH ENERGY STOP INSPECTION. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001012600085 20010126 00085 WP 2001 1 26 MWEA010047 1 20010113 A 3350 60030451 BATTERY PACK DOUG DC9 DC932 3022066 WP FUSELAGE DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 401ME 47133 AFT 2 FLIGHT ATTENDANT''S OVERHEAD EMERGENCY LIGHTS AT STATION 1019 ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED B 5-27 EMERGENCY BATTERY PACK. 2 L 7 2 4F A6WE 2001012600086 20010126 00086 WP 2001 1 26 ABXA0100006 1 20010116 A 5753 5912156175 VANE DOUG DC9 DC941 302207N WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 LEFT WING TRAILING EDGE INBOARD FIXED VANE WAS CRACKED AND HAD LOOSE RIVETS. MAINTENANCE INSPECTED FABRICATED AND INSTA LLED NEW TRAILING EDGE PANEL IAW DC-9 SRM 51-30-2 AND 51-30-8. 2 L 7 2 4F A6WE 2001012600087 20010126 00087 WP 2001 1 26 ABXA0100007 1 20010116 A 5320 5910141 PAN DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 OUTER BAG BIN DOOR PAN WAS CRACKED AT THE FORWARD CORNER. MAINTENANCE INSPECTED AND REPLACED THE BAG BIN DOOR IAW DC-9 MM. 2 L 7 2 4F A6WE 2001012600088 20010126 00088 WP 2001 1 26 ABXA0100008 1 20010116 A 5311 4923406502 FRAME DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 RIGHT FUSELAGE FRAME AT STATION 677 WAS CRACKED AT LOWER END BELOW CUSP IN THE RADIOUS. MAINTENANCE INSPECTED AND REPAI RED CRACK IAW DC-9 SRM 53-03 FIG 16. 2 L 7 2 4F A6WE 2001012600089 20010126 00089 WP 2001 1 26 ABXA0100009 1 20010116 A 5311 9923406503 FRAME DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 LEFT FUSELAGE FRAME 677 WAS CRACKED AT LOWER END BELOW CUSP, IN THE RADIOUS. MAINTENANCE REPAIRED CRACKED FRAME IAW DC- 9 SRM 53-03 FIG 16. 2 L 7 2 4F A6WE 2001012600090 20010126 00090 WP 2001 1 26 ABXA0100010 1 20010116 A 5330 591141563 DOUBLER DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 FORWARD UPPER ROTATING BEACON DOUBLER WAS CRACKED AT MOUNTING HOLE. MAINTENANCE REPLACED THE DOUBLER IAW DC-9 SRM 51-30 -2 AND 51-30-5. 2 L 7 2 4F A6WE 2001012600091 20010126 00091 WP 2001 1 26 ABXA0100011 1 20010116 A 5415 591326218 STRAP DOUG DC9 DC941 302207N WP RT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 UPPER RIGHT PYLON TO FUSELAGE ATTACH ANGLE AT STATION 1095 WAS REPORTED TO BE CRACKED. MAINTENANCE REMOVED SPLICE STRAP AND DYE CHECKED THE AREA. NO CRACKS WERE NOTED IAW ABX GMM CHAPTER 3 SECTION 5.01. 2 L 7 2 4F A6WE 2001012600092 20010126 00092 NM 2001 1 26 SWAA010072 1 20010109 A 3350 BR2013 BULB BOEING 737 7372H4 138448C NM CABIN FLOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED C4 CHECK, FOUND 1 EEPLS BULB INOP AND TRACK COVER CRACKED WITH WIRING EXPOSED. REMOVED AND REPLACED LA MP AND TRACK COVER PER MM. 2 L 7 2 4F A16WE 2001012600093 20010126 00093 NM 2001 1 26 SWAA010073 1 20010108 A 5315 6546804 FLOORBEAM BOEING 737 7372H4 138448C NM CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, LBL 51 TO RBL 49. REPAIRED FLOORBEAM PER T1-253-024. 2 L 7 2 4F A16WE 2001012600094 20010126 00094 NM 2001 1 26 SWAA010074 1 20010110 A 5315 6546804 FLOORBEAM BOEING 737 7372H4 138448C NM CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 344, LBL 35. REMOVED AND REPLACED FLOORBEAM UPPER CHORD PER SRM. 2 L 7 2 4F A16WE 2001012600095 20010126 00095 2001 1 26 SWAA010076 4 20010108 A 2565 INDICATOR BOEING 737 7372H4 138448C NM ESCAPE SLIDE OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001012600096 20010126 00096 NM 2001 1 26 SWAA010077 1 20010109 A 3397 5417N509 WIRE BOEING 737 7373H4 1384600 NM CABIN FLOOR EXPOSED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 638SW 27711 EEPLS WIRES EXPOSED AT OVERWING EXIT. SECURED WIRING PER MM. 2 L 7 2 4F RT A16WE 2001012600097 20010126 00097 2001 1 26 SWAA010078 4 20010110 A 2565 D31354 SLIDE BOEING 737 7373T5 NM PAX DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 667SW 23063 FWD ENTRY DOOR EMERGENCY EVAC SLIDE ASSY OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001012600098 20010126 00098 NM 2001 1 26 SWAA010079 1 20010110 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN FLOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 523SW 26565 EEPLS WIRING EXPOSED AND SEVERAL BULBS INOP IN AFT CABIN. SECURED LOOSE WIRE PIN AT SOCKET PER MM. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2001012600099 20010126 00099 NM 2001 1 26 SWAA010080 1 20010109 A 2410 761574B IDG BOEING 737 7377H4 NM NR 1 ENGINE FAILED A SWAA E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 SW 07 746SW 29798 875743 IN FLIGHT ENGINE SHUTDOWN. CREW REPORTED NR 1 ENG OIL QUANTITY STARTED DROPPING. THE ENGINE WAS SHUT DOWN. ON FURTHER INSP, IDG FAILURE WAS FOUND. REMOVED AND REPLACED NR 1 ENGINE PER MM. OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 2001012600101 20010126 00101 2001 1 26 SWAA010082 4 20010111 A 2565 1061323182 INDICATOR BOEING 737 7372H4 138448C NM ESCAPE SLIDE OUT OF TOLERANCE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED PM CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC S LIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001012600102 20010126 00102 NM 2001 1 26 SWAA010083 1 20010111 A 3350 101073 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED C3 CHECK, FOUND AFT SVC AND ENTRY DOOR EMERGENCY EXIT OVERHEAD LIGHT ASSY INOP. RELAMPED LIGHT ASSY'' ''S PER MM. 2 L 7 2 4F A16WE 2001012600103 20010126 00103 NM 2001 1 26 SWAA010084 1 20010111 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED A2 CHECK, FOUND 3.0 EXTERNAL FUSELAGE SKIN CRACK AT BS 927, STR 22L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001012600104 20010126 00104 NM 2001 1 26 SWAA010085 1 20010111 A 3350 0L3071BPL5GPL BULB BOEING 737 7373H4 1384600 NM CABIN FLOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 625SW 27701 DURING SCHEDULED C3 CHECK, FOUND EEPLS INOP AT ROW 20. RELAMPED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001012600105 20010126 00105 2001 1 26 SWAA010086 4 20010110 A 2565 INDICATOR BOEING 737 7373H4 1384600 NM ESCAPE SLIDE OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 625SW 27701 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASS Y PER MM. 2 L 7 2 4F RT A16WE 2001012600106 20010126 00106 NM 2001 1 26 SWAA010087 1 20010111 A 5310 6546529 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BL 0, WL 148. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2001012600107 20010126 00107 NM 2001 1 26 SWAA010088 1 20010110 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN FLOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 744SW 29490 DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVER CRACKED AT FWD SECTION. REMOVED AND REPLACED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001012600108 20010126 00108 NM 2001 1 26 SWAA010089 1 20010111 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN FLOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 395SW 27689 EEPLS TRACK COVER MISSING. REPLACED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001012600109 20010126 00109 NM 2001 1 26 SWAA010091 1 20010110 A 3397 5417N509 WIRE BOEING 737 7375H4 138449D NM CABIN FLOOR DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 524SW 26566 FOUR EEPLS LIGHTS INOP AT ROW 20. SECURED EEPLS WIRING PER MM. 2 L 7 2 4F RT A16WE 2001012600110 20010126 00110 2001 1 26 SWAA010092 4 20010110 A 2565 D31354 SLIDE BOEING 737 7377H4 NM AFT SERVICE DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 765SW 29805 AFT SVC DOOR EMERGENCY EVAC SLIDE ASSY FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001012600112 20010126 00112 NM 2001 1 26 SWAA010093 1 20010111 A 5610 5893543110 WINDOW BOEING 737 7372H4 138448C NM COCKPIT CRACKED A SWAA D RETURN TO BLOCK O OTHER TO TAKEOFF 1 SW 07 102SW 23108 AIR TURNBACK, R1 WINDOW CRACKED DURING T/O. REMOVED AND REPLACED WINDOW PER MM. PRESS AND LEAK CHECK GOOD PER MM. 2 L 7 2 4F A16WE 2001012600113 20010126 00113 NM 2001 1 26 SWAA010094 1 20010112 A 3610 1074925 SHUTOFF VALVE BOEING 737 7377H4 NM NR 1 ENGINE INOPERATIVE A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 759GS 30544 AIR TURNBACK, NO BLEED AIR FROM NR 1 ENGINE AFTER T/O. REMOVED AND REPLACED PRSOV, LOW PRESSURE REGULATOR (P/N 3214552- 5) AND PRSOV MUSCLE AIR LINE PER MM. OPS AND LEAK CHECK GOOD. 2 L 7 2 4F RT A16WE 2001012600114 20010126 00114 NM 2001 1 26 SWAA010095 1 20010111 A 7500 3400051030 LINE BOEING 737 7377H4 NM CFMINT CFM567 CFM567B22 13802 NE NR 2 ENGINE DISCONNECTED A SWAA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SW 07 742SW 29278 874115 IN FLIGHT ENGINE SHUTDOWN, NR 2 ENG ROLLED BACK AT FL390. DESCENDED TO FL240 & ENG RESTARTED WITH APU ASSIST. ON LANDI NG NR 2 ENG ENGINE CONTROL LIGHT ILLUMINATED. EEC BITE FAULTS PS3 LINE. FOUND PS3 LINE DISCONNECTED AT B- NUT, FAN CAS E 6 O''''CLOCK POSITION. SECURED LINE PER MM. RAN ENG, OPS CHECK NORMAL PER MM. 2 L 7 2 4F 4 F RT A16WE E00055EN 2001012600115 20010126 00115 2001 1 26 SWAA010096 4 20010112 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SERVICE DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER WHEN ARMED FOR TAXI. REINSTALLED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001012600116 20010126 00116 NM 2001 1 26 SWAA010097 1 20010113 A 3350 101073 LIGHT BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 AFT SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT ASSY LOOSE. SECURED EXIT LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 2001012600117 20010126 00117 2001 1 26 SWAA010098 4 20010113 A 2565 INDICATOR BOEING 737 7372H4 138448C NM ESCAPE SLIDE OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001012600118 20010126 00118 2001 1 26 SWAA010099 4 20010113 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT PAX DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 AFT SVC AND ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY''''S PER MM. 2 L 7 2 4F A16WE 2001012600119 20010126 00119 2001 1 26 SWAA010100 4 20010112 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT PAX DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 327SW 23691 AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001012600120 20010126 00120 2001 1 26 SWAA010102 4 20010112 A 2565 D31354 SLIDE BOEING 737 7373T5 NM FWD PAX DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 667SW 23063 FWD ENTRY DOOR EMERGENCY EVAC SLIDE ASSY FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001012600121 20010126 00121 NM 2001 1 26 SWAA010103 1 20010114 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN FLOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 394SW 27380 EEPLS TRACK COVER MISSING AT ROW 2. REPLACED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001012600122 20010126 00122 NM 2001 1 26 SWAA010104 1 20010114 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN FLOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 528SW 26570 EEPLS WIRING EXPOSED/BROKEN AND BULB INOP AT ROW 13. REPAIRED WIRING AND REPLACED BULB PER MM. 2 L 7 2 4F RT A16WE 2001012600123 20010126 00123 EA 2001 1 26 COMA0160118 1 20010112 A 5530 600210617 BUSHING CNDAIR CL600 CL6002B19 EA VERTICAL STAB WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 915CA 7013 VERTICAL STABILIZER LEFT HAND PIVOT POINT BUSHING WAS FOUND TO BE WORN. PERFORMED A MAJOR REPAIR BY REPLACING WORN VERT ICAL STABILIZER LT PIVOT POINT BUSHING. (P/N 600-2061-7) IAW WVAC EO 601R-55-7103, CRJ AMM 20-26-00-910-003 AND CRJ DRA WING 600-21029. 2 L 7 2 4F RT A21EA 2001012600124 20010126 00124 WP 2001 1 26 MWEA010050 1 20010116 A 5311 59114481 FRAME DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 CORROSION ON J SECTION OF FRAME AT STATION 256 ABOVE LONGERON 29 RIGHT. FABRICATED AND INSTALLED J-SECTION REPAIR PARTS . 2 L 7 2 4F A6WE 2001012600125 20010126 00125 WP 2001 1 26 MWEA010051 1 20010116 A 5320 591006811 SPLICE DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 500ME 45711 SKIN SPLICE STRAP AT STATION 474 AND LONGERON 29 LEFT HAS SEVERAL HOLES WITH IMPROPER SPACING. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001012600126 20010126 00126 WP 2001 1 26 MWEA010053 1 20010116 A 5310 591141911 FINGER DOUBLER DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 FINGER DOUBLER BELOW LONGERON 15 RIGHT IS CRACKED AT STATION 647. FABRICATED AND INSTALLED NEW FINGER DOUBLER AND REPAI R SPLICES. 2 L 7 2 4F A6WE 2001012600127 20010126 00127 WP 2001 1 26 MWEA010054 1 20010116 A 5310 591015849 WEB DOUG DC9 DC914 3022034 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 AFT CARGO DOOR JAMB, LOWER WEB GOUGED, FOUR PLACES, STATION 708 TO 718, BETWEEN LONGERON 29 AND 28 RIGHT. REMOVED AND R EPLACED FLOOR JAMB AND WEB. 2 L 7 2 4F A6WE 2001012600128 20010126 00128 WP 2001 1 26 MWEA010055 1 20010116 A 5310 29128921 GUSSET DOUG DC9 DC914 3022034 WP AFT BULKHEAD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 STIFFENER ON AFT RIGHT HAND SIDE OF APB IS CRACKED. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001012600129 20010126 00129 WP 2001 1 26 MWEA010056 1 20010116 A 5320 99581673 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE BUCKLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 INTERCOSTAL BELOW CENTER FLOOR IS BUCKLED FROM STATION 718 TO 737. FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 2001012600130 20010126 00130 WP 2001 1 26 MWEA010057 1 20010116 A 5310 995823869 SHEAR TIE DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 SHEAR CLIP IS CRACKED AT STATION 801 BETWEEN LONGERON 14 - 16 LEFT. FABRICATED AND INSTALLED SECTION OF SHEAR TIE. 2 L 7 2 4F A6WE 2001012600131 20010126 00131 WP 2001 1 26 MWEA010059 1 20010116 A 5320 49122611 FITTING DOUG DC9 DC914 3022034 WP FUSELAGE TOOL DAMAGE A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 500ME 45711 LONGERON 23 LEFT SPLICE HAS TOOL DAMAGE AT STATION 228 ON LOWER SIDE OF LOWER LEG. FABRICATED AND INSTALLED NEW SPLICES AND AIR DUCT SUPPORT. 2 L 7 2 4F A6WE 2001040400168 20010404 00168 WP 2001 4 4 01FDEA00025 1 20010117 A 3260 801805 SENSOR DOUG DC10 DC1030F 3023504 WP NLG WW DAMAGED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 314FE 48312 AFT T/O AND LAND GEAR UP S/O PNL IND RED UNSAFE NOSE GEAR. RECYCLED LG AND NOSE RED UNSAFE LIGHT ON EXT AND RETRACTION. *S/D* REPLACED DAMAGED NOSE GEAR LOCKED SENSOR PER A/W/D 32-61-04 PG 1 D1-79 AND S/M/P CHAP 20 MM 32-61-03-2. OPS CK NORMAL. 2 L 7 3 4F RT A22WE 2001012600144 20010126 00144 2001 1 26 SWAA010075 4 20010109 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM GIRT BAR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 606SW 27926 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY CABLE BROKEN. REPLACED CABLE PER MM. 2 L 7 2 4F RT A16WE 2001012600145 20010126 00145 2001 1 26 SWAA010081 4 20010110 A 3442 65C16130 RADAR BOEING 737 7373H4 1384600 NM E/E BAY INOPERATIVE A SWAA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 301SW 22941 DIVERSION, CREW REPORTED WEATHER RADAR INOP. DUE TO DESTINATION WEATHER, DIVERTED TO LAS. REMOVED AND REPLACED WEATHER RADAR R/T UNIT PER MM. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2001012600146 20010126 00146 NM 2001 1 26 SWAA010090 1 20010111 A 3397 079123 WIRE BOEING 737 7373H4 1384600 NM CABIN FLOOR EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 632SW 27707 EEPLS WIRING EXPOSED AT ROWS 14 & 15. SECURED FLOOR TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001012600147 20010126 00147 WP 2001 1 26 MWEA010060 1 20010116 A 5412 9912243172 BULKHEAD DOUG DC9 DC914 3022034 WP RT PYLON MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 500ME 45711 RT PYLON BULKHEAD AT STATION 786 HAS IMPROPERLY INSTALLED AND INPROPERLY SPACED HI-LOKS BETWEEN LONGERONS 9 RIGHT AND 10 RIGHT. FABRICATED AND INSTALLED REPLACEMENT WEB. 2 L 7 2 4F A6WE 2001012600148 20010126 00148 WP 2001 1 26 MWEA010062 1 20010116 A 5311 99582387 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FRAME AT STATION 980 IS CRACKED AT LONGERON 16 LEFT. REMOVED DAMAGE, FABRICATED NEW FRAME AND REPAIR SPLICES. 2 L 7 2 4F A6WE 2001012600149 20010126 00149 WP 2001 1 26 MWEA010063 1 20010116 A 5310 995823811 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 SHEAR CLIP IS CRACKED AT STATION 980 BELOW LONGERON 14 LEFT. REMOVED DAMAGED PART, FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F A6WE 2001012600150 20010126 00150 WP 2001 1 26 MWEA010064 1 20010116 A 5330 59114015 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 LIGHTNING STRIKE DAMAGE AT FUSELAGE LOWER SECTION BETWEEN STATION 216 - 229 AND LONGERON 29 LEFT AND LONGERON 30 LEFT. BLENDED AREAS AT STATION 219 OUT OF LIMITS, REMOVED DAMAGED MATERIAL AND PLUGGED WITH NEW RIVETS. 2 L 7 2 4F A6WE 2001012600151 20010126 00151 WP 2001 1 26 MWEA010065 1 20010116 A 5330 59114015 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 LIGHTNING STRIKE DAMAGE BOTTOM SIDE OF FUSELAGE BETWEEN STATION 260 - 284. BLENDED AREA, REMOVED DAMAGED RIVET, INSTALL ED NEW RIVET. REMOVED DAMAGED AREA BY DRILLING AND INSTALLED RIVET. 2 L 7 2 4F A6WE 2001012600152 20010126 00152 WP 2001 1 26 MWEA010066 1 20010116 A 5330 59114015 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 LIGHTNING STRIKE DAMAGED, BOTTOM SIDE OF FUSELAGE BETWEEN STATION 287 - 313, LONGERON 28 LEFT AND 29 LEFT. BLENDED AREA , REMOVED DAMAGE BY DRILLING, INSTALLED RIVET. 2 L 7 2 4F A6WE 2001012600153 20010126 00153 WP 2001 1 26 MWEA010067 1 20010116 A 5330 59114015 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 LIGHTNING STRIKE DAMAGE TO RIVETS AND SKIN BETWEEN STATION 416 - 427 BETWEEN LONGERON 24 LEFT AND 25 LEFT. REMOVED DAMA GED RIVETS, BLENDED DAMAGED AREA, INSTALLED NEW RIVETS. 2 L 7 2 4F A6WE 2001012600154 20010126 00154 WP 2001 1 26 MWEA010069 1 20010116 A 5313 27779224 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 AREA OF LEFT HAND LAVATORY HAD CRACKED LONGERON AT STATION 980. REMOVED DAMAGED SECTION, LOCATED, DRILLED, AND INSTALLE D NEW LONGERON. 2 L 7 2 4F A6WE 2001012600155 20010126 00155 WP 2001 1 26 MWEA010070 1 20010116 A 5410 591326237 ANGLE DOUG DC9 DC932 3022066 WP LT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 LEFT HAND LOWER PYLON ATTACH ANGLE IS CRACKED AT STATION 980. REMOVED CRACKED ANGLE, LOCATED, DRILLED, AND INSTALLED NE W ANGLE. 2 L 7 2 4F A6WE 2001012600157 20010126 00157 EA 2001 1 26 COMA0160117 1 20010115 A 5320 HOSE CNDAIR CL600 CL6002B19 EA COCKPIT DAMAGED A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 784CA 7319 DAMAGE TO HOSE UNDER PILOTS SIDE PITOT TUBE. REPAIRED PER REO 601R-53-2108. 2 L 7 2 4F RT A21EA 2001012600158 20010126 00158 2001 1 26 SWAA010101 4 20010113 A 2565 61621469 SLIDE BOEING 737 7373H4 1384600 NM AFT SERVICE DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 644SW 28329 AFT SVC DOOR EMERGENCY EVAC SLIDE ASSY FELL OUT OF CONTAINER. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001012600159 20010126 00159 2001 1 26 SWAA010105 4 20010114 A 2565 D31354 SLIDE BOEING 737 7377H4 NM FWD SERVICE DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 753SW 29848 WHEN FWD SVC DOOR OPENED, EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTANER (GIRT ASSY LEFT INSTALLED). REINSTALL ED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001012600160 20010126 00160 NM 2001 1 26 CALA0100015 1 20010112 A 5753 65C313531 FLAP TRACK BOEING 737 7373Q8 1384670 NM NR 2 TE FLAPS GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14381 26310 INSPECTION FOUND NR 1 MIDFLAP, NR 2 AFT FLAP TRACK AFT SECTION GOUGED. THE FLAP TRACK WAS REMOVED AND REPLACED IAW MM 5 7-53-18. 2 L 7 2 4F RT A16WE 2001012600161 20010126 00161 NM 2001 1 26 CALA0100016 1 20010112 A 5320 SUPPORT BRACKET BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND RT AFT LAV FORWARD WALL SUPPORT CORRODED AT STA 993. THE WALL SUPPORT WAS REMOVED AND A NEW WALL SUPPO RT WAS INSTALLED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 2001012600162 20010126 00162 NM 2001 1 26 CALA0100017 1 20010112 A 5320 ANGLE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14381 26310 INSPECTION FOUND Z-ANGLE CORRODED AT STA 1000, RBL 35. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001012600163 20010126 00163 NM 2001 1 26 CALA0100018 1 20010113 A 5320 FITTING BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND STRINGER 27L END FITTING CORRODED AT STA 727. THE CORROSION WAS REMOVED, TREATED, AND PRIMED IAW SRM 5 3-60-12. 2 L 7 2 4F RT A16WE 2001012600164 20010126 00164 NM 2001 1 26 CALA0100019 1 20010114 A 2560 BATTERY BOEING 737 737524 1384721 NM MEGAPHONE INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13624 27528 THE AFT CABIN MEGAPHONE WAS FOUND INOPERATIVE. THE MEGAPHONE BATTERIES WERE REMOVED AND REPLACED AND OPERATION CHECKED G OOD. 2 L 7 2 4F RT A16WE 2001012600165 20010126 00165 NM 2001 1 26 CALA0100021 1 20010114 A 5753 65478943 FLAP TRACK BOEING 737 7373Q8 1384670 NM NR 3 TE FLAPS GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14381 26310 INSPECTION FOUND NR 3 AFT FLAP NR 2 TRACK FROM I/B ON RIGHT WING GOUGED. THE FLAP TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW MM 57-53-18. 2 L 7 2 4F RT A16WE 2001012600166 20010126 00166 NM 2001 1 26 CALA0100022 1 20010114 A 5315 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14381 26310 INSPECTION FOUND FLOORBEAM CORRODED AROUND FASTENER HOLES FROM ENTRY DOOR TO SERVICE DOOR, STA 312, RBL 21 TO LBL 38. A REPAIR FLOORBEAM WAS INSTALLED IAW SRM 53-10-51, FIGURE 205. 2 L 7 2 4F RT A16WE 2001012600167 20010126 00167 NM 2001 1 26 CALA0100023 1 20010114 A 5311 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14381 26310 INSPECTION FOUND A .5 INCH CRACK AT RIVET HOLE IN FRAME AT STA 360, S8L. THE FRAME WAS REPAIRED IAW SRM 53-00-07, FIGUR E 201. 2 L 7 2 4F RT A16WE 2001012600168 20010126 00168 NM 2001 1 26 CALA0100024 1 20010115 A 5315 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14381 26310 INSPECTION FOUND FLOORBEAM CAP CORRODED AT STA 986, LBL 6 TO LBL 24. A REPAIR WAS INSTALLED IAW SRM 53-00-51, FIGURE 20 3. 2 L 7 2 4F RT A16WE 2001012600169 20010126 00169 NM 2001 1 26 CALA0100025 1 20010115 A 5320 WEB BOEING 737 7373Q8 1384670 NM FUSELAGE TORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14381 26310 INSPECTION FOUND WEB EDGES TORN AWAY AT AFT CARGO DOOR OPENING, FORWARD LOWER INTERNAL FACE OF JAMB, STA 809. THE DAMAG ED WEB WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 51-70-13. 2 L 7 2 4F RT A16WE 2001012600170 20010126 00170 WP 2001 1 26 CALA0100027 1 20010115 A 5720 BRACKET DOUG DC10 DC1030 3023501 WP RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND A .5 INCH CRACK IN RT WING I/B BRACKET AT I/B SIDE PANEL. A NEW BRACKET WAS INSTALLED IAW ECRA 5730-01 741. 2 L 7 3 4F A22WE 2001012600171 20010126 00171 WP 2001 1 26 MWEA010058 1 20010116 A 5522 59104102 SKIN DOUG DC9 DC914 3022034 WP RT ELEVATOR DELAMINATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 RIGHT HAND ELEVATOR OUTBOARD TRAILING EDGE DELAMINATED ALONG LOWER SURFACE. FABRICATED AND INSTALLED NEW TRAILING EDGE SECTION AND TIP END. 2 L 7 2 4F A6WE 2001012600172 20010126 00172 WP 2001 1 26 MWEA010068 1 20010116 A 5330 59114015 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 LIGHTNING STRIKE DAMAGED AT STATION 541 LONGERON 25 LEFT. REMOVED DAMAGED RIVET, BLENDED AREA, INSTALLED OVERSIZED RIVE T. 2 L 7 2 4F A6WE 2001012600173 20010126 00173 EU 2001 1 26 2001UALA00001 1 20010104 A 3350 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE J L WARNING INDICATION NO TEST IN INSP/MAINT 1 WP 29 436UA 638 BATTERY FWD L MESSAGE WHEN TESTING THE EMERGENCY LIGHT SYSTEM FROM THE FORWARD ATTENDANT PANEL. *S/D* REPLACED BATTERY AT 1L (10WLA). SYSTEM OPERATION CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2001012600174 20010126 00174 NE 2001 1 26 COMA0160110 2 20010114 A 7270 PLUG CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LEFT ENGINE CHAFED A COMA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 01 967CA 7134 LEFT ENGINE FAN VIB INDICATED 2.7. FOUND BLADES RUBBING AT ACCESS PLUG. ADJUSTED GAP AT ACCESS PLUG. 2 L 7 2 4F 4 F RT A21EA E15NE 2001012600175 20010126 00175 EA 2001 1 26 COMA0160111 1 20010114 A 4970 MS280343 SENSOR CNDAIR CL600 CL6002B19 EA APU MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 809CA 7366 APU OIL TEMP CAUTION MESSAGE. REPLACED OIL TEMP SENSOR. 2 L 7 2 4F RT A21EA 2001012600176 20010126 00176 2001 1 26 COMA0160112 4 20010114 A 2340 508812 CONTROL UNIT CNDAIR CL600 CL6002B19 EA INTERPHONE MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 969CA 15314 7141 DURING T/O AT 115 KTS, SINGLE CHIME HEARD AND T/O ABORTED. COULD NOT DUPLICATE. REPLACED THE INTERPHONE CONTROL FOR TR OUBLESHOOTING. 2 L 7 2 4F RT A21EA 2001012600177 20010126 00177 EA 2001 1 26 COMA0160113 1 20010114 A 3220 16400103 DRAG BRACE CNDAIR CL600 CL6002B19 EA NLG FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 946CA 11837 7072 GEAR DISAGREE WARNING, NLG DID NOT RETRACT. REPLACED THE NLG DRAG BRACE ASSY. 2 L 7 2 4F RT A21EA 2001012600178 20010126 00178 EA 2001 1 26 COMA0160114 1 20010114 A 5210 SENSOR CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADJ A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 806CA 7359 CABIN DOOR WARNING. ADJUSTED THE DOOR PROXIMITY SENSORS. 2 L 7 2 4F RT A21EA 2001012600179 20010126 00179 2001 1 26 COMA0160115 4 20010115 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 868CA 7427 STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001012600180 20010126 00180 EA 2001 1 26 COMA0160116 1 20010115 A 2711 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA TRIM CONFIGURE ACTIVATED A COMA C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 SO 01 951CA 7091 CONFIG TRIM WARNING DURING T/O. SET AILERON TRIM TO THE TAKEOFF RANGE SYSTEM CHECKS NORMAL. 2 L 7 2 4F RT A21EA 2001012600185 20010126 00185 2001 1 26 AWXA0001247 4 20010118 A 3431 066106048 RECEIVER BOEING 737 7373S3 1384711 NM EE BAY MALFUNCTIONED A AWXA A UNSCHED LANDING O OTHER AP APPROACH 1 WP 28 313AW 31652 179 23712 LAS - AIR TURNBACK 1/7/01 - ON APPROACH IN SLC THE CAPT''''''''S GLIDE SLOPE INDICATION WENT FULL DEFLECTION AND THE 1ST OFFICER''''''''S FULL DEFLECTION DOWN. TWO APPROACHES TRIED WITH THE SAME RESULT. THE AIRCRAFT RETURNED TO LAS AND BOT H GLIDE SLOPE INDICATORS INDICATED NORMAL. AWA DISPATCH CONTACTED SLC AND FOUND OTHER AIRCRAFT HAD SIMILAR PROBLEMS WIT H VOR/ILS. ON 1/8/01, THE NR 1 VOR/ILS RECIEVER WAS CHANGED AS A PRECAUTION. 2 L 7 2 4F RT A16WE 2001012600189 20010126 00189 SO 2001 1 26 C2XA01IA030 1 20010108 A 3234 12038594001 CONTROL UNIT EMB 120 EMB120ER 3260203 SO COCKPIT INOPERATIVE A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 27 40717 120133 IAH - FLIGHT 2950, THE CREW REPORTED THAT THE LANDING GEAR NOSEGEAR RED B-INDICATION ILLUMINATED INTERMITTANTLY IN FLIGH T. MAINTENANCE INSPECTED AND CLEANED THE PROXIMITY SWITCH ON THE NOSE LANDING GEAR, AND THE AIRCRAFT WAS APPROVED FOR R ETURN TO SERVICE. THE DISCREPANCY REPEATED ON FLIGHT 3276 ON 01/09/01, WHERE MAINTENANCE CLEANED THE UPLOCK PROXIMITY S WITCHES, AND AGAIN ON FLIGHT 2945 WHERE MAINTENANCE PLACED THE ITEM ON MEL 32-60-1 CAT B CONTROL NR 003550. THE AIRCRAF T RETURNED TO IAH ON 01/10/01 AND MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL MODULE, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001012600190 20010126 00190 SO 2001 1 26 C2XA01IA028 1 20010113 A 3397 W192867822 WIRE EMB 145 EMB145 3260210 SO CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14998 145302 IAH - FLIGHT 4027, DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD SECTION OF AISLE PATH EMERGENCY LIG HTING WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON THE AFFECTED SECTION OF LIGHT STRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001012600191 20010126 00191 SO 2001 1 26 C2XA01IA029 1 20010108 A 5411 12007882001 FRAME EMB 120 EMB120ER 3260203 SO LEFT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16729 120185 IAH - DURING MAINTENANCE INSPECTION, THE LEFT NACELLE HALF FRAME FOR THE AFT OUTBOARD GEAR DOOR HINGE POINT WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A DOUBLER REPAIR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001012600194 20010126 00194 NM 2001 1 26 DHL2001741002 1 20010117 A 2420 902F2425 GCU BOEING 727 7272Q9 138448M NM NR 1 FAILED A DHLA D RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 741DH 21931 NR 1 ENGINE GEN WOULD NOT COME ON LINE, NR 6B FAILS TO CLOSE. SWAPPED NR 1 AND APU GCU''S RAN ENG, SYS OPS GOOD PER M/M 24-20. 2 L 7 3 4F RT A3WE 2001012600196 20010126 00196 NM 2001 1 26 2001UALA00006 1 20010105 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE SEAT 20 INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 789UA 26935 SEAT 20G EMERGENCY LIGHT INOP AND DAMAGED. REPLACED LIGHT ASSY AND TESTS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001021300403 20010213 00403 EU 2001 2 13 2001UALA00007 1 20010105 A 3040 SENSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LT WINDSHIELD FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 440UA 702 LEFT WINDSHIELD ANTI-ICE ELECTRONIC CENTRALIZED AIRCRAFT MONITORING CAME ON DURING CRUISE. POST FLIGHT REPORT SHOWS LEF T WIND SHIELD SENSOR FAULT. *S/D* FOUND BAD TEMPERATURE SENSOR AT LEFT WINDSHIELD. CONNECTED SPARE SENSOR. ALL CHECK S NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2001022600101 20010226 00101 NM 2001 2 26 2001UALA00011 1 20010106 A 3350 58631 SIGN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE AIRSTAIR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7464U 21918 EMERGENCY EXIT SIGN AT THE AFT AIRSTAIR IS INOPERABLE. *S/D* REPLACED POWER CABLE TO EXIT SIGN DUE TO BEING SEVERED AT THE FLOOR. EXIT SIGN OPERATION CHECKS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001022600102 20010226 00102 NM 2001 2 26 2001UALA00013 1 20010103 A 3350 KD4A019 LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN INTERMITTENT A UALA O OTHER O OTHER TO TAKEOFF 1 WP 29 7457U 21911 DURING TAKEOFF ALL CABIN EMERGENCY LIGHTS FLICKERED. *S/D* UNABLE TO DUPLICATE PROBLEM. REPLACED R600 AND R70 RELAYS AS PRECAUTIONARY. FOUND RT HAND OVERWING SLIDE LIGHT ON AFT CARGO DOOR PULSING. REPLACED BATTERY AND ALL EMERGENCY LIG HTS OPERATIONS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001012600197 20010126 00197 NM 2001 1 26 2001UALA00016 1 20010109 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 780UA 26944 DOOR 4 RIGHT EXTERIOR EEL LIGHT IS INOP. RELAMPED AND LIGHT CHECKED GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001030500261 20010305 00261 NE 2001 3 5 2001UALA00018 2 20010110 A 7200 ENGINE BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE NR 2 MALFUNCTIONED A UALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 29 996UA 22456 688491 UNCOMMANDED POWER LOSS IN ENGINE NR 2. *S/D* REPLACED THE NR 2 ENGINE. 2 L 7 2 4F 4 F A16WE E2EA 2001022600103 20010226 00103 NM 2001 2 26 2001UALA00019 1 20010111 A 2121 SUNDSTRAND GASPER FAN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN FAILED A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 7261U 21408 AIRCRAFT RETURNED TO BLOCK FOR SMOKE ODOR IN CABIN. *S/D* GASPER FAN OVERLOADED. REPLACED GASPER FAN. 2 L 7 3 4F 4 F A3WE E2EA 2001021300405 20010213 00405 NM 2001 2 13 2001UALA00020 1 20010110 A 5270 694173030 LANYARD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOOR BROKEN A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 380UA 24655 AFT CARGO DOOR LIGHT CAME ON AFTER TAKEOFF. *S/D* FOUND AFT CARGO DOOR RELEASE HANDLE BUNGEE CORD BROKEN AND INTERFERI NG WITH DOORSWITCH. REPLACED BROKEN BUNGEE CORD. 2 L 7 2 4F 4 F RT A16WE E2GL 2001012600198 20010126 00198 WP 2001 1 26 01FDEA00024 1 20010114 A 2750 HANDLE DOUG DC10 DC1010F 3022111 WP FLAP/SLAT SEIZED A FDEA L ABORTED APPROACH F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 25 057FE 48264 UPON CONFIGURING FOR LAND FLAP/SLAT HANDLE WOULD NOT COME OUT OF THE 0/RETRACT POSITION. CYCLED FLAP/SLAT HANDLE REF MM 27-20-00-0, 27-50-00-5, NO FAULTS. NO PREV HISTORY FOUND, AC OK TO CONTINUE. 2 L 7 3 4F A22WE 2001012600199 20010126 00199 NM 2001 1 26 RAAA01B202 1 20010115 A 3350 861014 BATTERY INTVLV BOEING 727 72722C 138400F NM PAX CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED B-3 CHECK, MID CABIN DOOR EXIT IDENTIFIER INOP. REPLACED BATTERY, OPS GOOD PER ECO 86-26. 2 L 7 3 4F A3WE 2001012600200 20010126 00200 NM 2001 1 26 RAAA01B201 1 20010115 A 3350 8621014 BATTERY INTVLV BOEING 727 72722C 138400F NM PAX CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED B-3 CHECK, FOUND OVERWING EXIT IDENTIFIER BATTERY INOP. REPLACED BATTERY OPS GOOD PER ECO 86-26. 2 L 7 3 4F A3WE 2001012600224 20010126 00224 NM 2001 1 26 SCNA01007 1 20010114 A 2150 1843801 HEAT EXCHANGER BOEING 727 7272J4 1384006 NM A/C BAY OVERHEATED A SCNA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 15 284SC 21438 DURING TAKEOFF ROLL IN MKE THE ENGINE NUMBER THREE STRUT OVERHEAT LIGHT ILLUMINATED AT FULL POWER AT 70 KNOTS. THE CREW ABORTED THE TAKEOFF. REMOVED AND REPLACED THE NUMBER THREE ENGINE HEAT EXCHANGER. OPERATIONAL AND LEAK CHECK GOOD. 2 L 7 3 4F RT A3WE 2001012600225 20010126 00225 NM 2001 1 26 SCNA01008 1 20010116 A 3350 BATTERY BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 290SC 20764 DURING A LINE INSPECTION THE EMERGENCY EXIT LIGHT ABOVE THE L1 DOOR WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE EME RGENCY EXIT LIGHT BATTERIES ABOVE THE L1 DOOR. OPERATIONAL CHECKS GOOD. 2 L 7 3 4F RT A3WE 2001012600226 20010126 00226 NM 2001 1 26 AWXA0001244 1 20010118 A 5311 654653950 FRAME BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 167AW 23628 FUSELAGE FRAME ANGLE CRACKED BELOW CABIN FLOOR STA 616 RT, WL 201, RBL 60. REPAIRED AS PER AWA ER 03-5311-01010-JL2. 2 L 7 2 4F RT A16WE 2001012600227 20010126 00227 NM 2001 1 26 AWXA0001245 1 20010118 A 5320 69466111 ANGLE BOEING 737 7373Y0 1384671 NM FUSELAGE GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 O/B SUPPORT Z-ANGLE GOUGED, LT MAIN W/I CUTOUT AFT O/B SIDE. REMOVED O/B SUPPORT IAW SRM 51-40-02; LOCATED AND DRILLED 3 HOLES IAW 51-40-05; TREATED AND PRIMED IAW 51-20-01; INSTALLED REPLACEMENT O/B SUPPORT IAW 51-40-02. 2 L 7 2 4F RT A16WE 2001012600228 20010126 00228 NM 2001 1 26 AWXA0001246 1 20010118 A 5320 146N5821 STRUCTURE BOEING 757 7572G7 1384963 NM AFT CARGO CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 24233 RT LAV FLOOR VERTICAL SUPPORT CRACKED, AFT CARGO BAY STA 1320 RBL 46. REMOVED AND REPLACED RT LAV FLOOR VERT SUPPORT IA W SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A2NM 2001012600229 20010126 00229 2001 1 26 AWXA0001248 4 20010118 A 3460 B398BCM0108 COMPUTER AIRBUS 320 A320231 3930325 EU EE BAY FAILED A AWXA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 28 618AW 25297 2473 304 PHX - DIVERTED FLIGHT (1/14/01) - AFTER TAKEOFF FROM LAS, THE FLIGHT CREW EXPERIENCED A DUAL MCDU FAILURE; THEY WERE FRO ZEN ON RESPECTIVE PAGE AT THE TIME OF FAILURE AND WERE UNABLE TO INPUT DATA. CIRCUIT BREAKER B-1 & N20 WERE RESET WITH NO HELP. CREW SWITCHED TO STANDBY NAV SYSTEM AND DIVERTED TO PHX. IN PHX THE PROBLEM WAS ISOLATED TO THE NR 1 FMGC WHI CH WAS REPLACED AND FUNCTIONALLY CHECKED GOOD. CURRENT NAV DATA WAS LOADED PER AWA TASK CARD A1B34321. 2 L 7 2 4F RT A28NM 2001012600237 20010126 00237 WP 2001 1 26 AT0100006 1 20010119 A 3350 60030451 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 801AT 47275 FOUND OVERWING EMERGENCY EXIT LIGHTS WILL NOT EXTINGUISH. REPLACED BATTERY PACK IAW DC9 MM 33-50. 2 L 7 2 4F A6WE 2001012600238 20010126 00238 SO 2001 1 26 C2XA01IA027 1 20010114 A 3350 66901 LIGHT EMB 145 EMB145LR SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14993 145289 IAH- FLIGHT 3912, DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE AFT SECTION OF THE AISLE PATH EMERGENCY EXIT LIGHTS WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF LIGHT STRIP, AND THE AIRCRAFT WAS APP ROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001012600239 20010126 00239 NM 2001 1 26 AT0100002 1 20010105 A 5310 DOOR FRAME BOEING 717 717200 1383700 NM FUSELAGE DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 947AT 55010 FOUND DENT AT BS 275 AFT OF R1 DOOR. INSTALLED REPAIR DOUBLER AND FILLER IAW RES 01-004. 2 L 7 2 4F TR A6WE 2001012600240 20010126 00240 NM 2001 1 26 AT0100003 1 20010112 A 3350 6011779 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 954AT 55016 FOUND NACELLE LIGHTS FAILED TEST. REMOVED AND REPLACED BATTERY PACK IAW B717 MM 33-51. 2 L 7 2 4F TR A6WE 2001012600242 20010126 00242 WP 2001 1 26 RRXA003718 1 20010112 A 5753 SKIN DOUG DC8 DC871F 302199D WP RT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND A SMALL CRACK JUST O/B OF EXHAUST ON THE RT WING O/B FLAP T/E, DAMAGE EXCEEDED LIMITATI ONS IAW DC-8 SRM. 2 L 7 4 4F RT 4A25 2001012600243 20010126 00243 WP 2001 1 26 AT0100005 1 20010109 A 3350 60030431 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 846AT 47226 FOUND FORWARD OVERHEAD EMERGENCY LIGHT WOULD NOT ILLUMINATE. REMOVED AND REPLACED POWER SUPPLY LOCATED AT FORWARD AISLE OVERHEAD SERVICE ACCESS PANEL IAW DC9 MM 33-50. 2 L 7 2 4F A6WE 2001012600244 20010126 00244 EU 2001 1 26 QXEA0100017 1 20010113 A 2530 CA16707 CONNECTOR FOKKER F28 F28MK4000 4990810 EU GALLEY MALFUNCTIONED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 493US 11161 SEA-ELECTRICAL BURNING SMELL COMING FROM COFFEE URN LOCATION TOP AND BOTTOM. REMOVED AND REPLACED BOTH UPPER AND LOWER COFFEE JUG ELECTRICAL RECEPTICALS. OPERATIONAL WARM-UP CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001012600245 20010126 00245 EU 2001 1 26 QXEA0100018 1 20010110 A 3350 1820 LIGHT FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 477AU 11226 BOI-EMERGENCY EXIT SIGN ABOVE COCKPIT DOOR, 28V LIGHTS INOPERATIVE. REMOVED AND REPLACED EXIT SIGN LIGHT ASSEMBLY. OPE RATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001012600246 20010126 00246 EU 2001 1 26 QXEA0100019 1 20010111 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 477AU 11226 PDX-MID CABIN EXIT LIGHT FORWARD FACING IS DIM. REMOVED AND REPLACED CIRCUIT CARD ASSEMBLY. OPERATIONAL CHECK GOOD. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001012600247 20010126 00247 EU 2001 1 26 QXEA0100022 1 20010114 A 3350 6008905 BATTERY PACK FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US * 4236 11161 BOI-ALL FOUR EMERGENCY DOOR/OVERWING EXITS EVACUATION GREEN EXIT SIGNS INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001012600248 20010126 00248 EA 2001 1 26 SWIA972272 1 20010112 A 3030 PROBE CNDAIR CL600 CL6002B19 EA TAT FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 411SW 7067 TAT PROBE HEAT CAUTION IN FLIGHT. REMOVED AND REPLACED TAT PROBE IAW CRJ MM 34-11-11. OPS CHECK GOOD. P/N: 102AH2AG, S/N ON: A2058, S/N OFF: A4036. 2 L 7 2 4F RT A21EA 2001012600249 20010126 00249 SO 2001 1 26 SWIA972273 1 20010110 A 3030 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE NR 2 PITOT HEAT CONTAMINATED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 284YV 120284 NR 2 PITOT HEAT FAILED IN FLIGHT, AUTO PILOT FAILED, HIGH SPEED WARNING WENT OFF WHEN FIRST OFFICER'S AIRSPEED FLUCTUATE D. EN ROUTE FROM MRY TO LAX. DIVERTED TO SBA. FOUND CONTAMINATION OF WATER IN NUMBER TWO PITOT CANNON PLUG. DRIED WA TER AND CLEANED CONTAMINATION. OPERATED NUMBER TWO PITOT HEAT, OPS CHECK GOOD. TESTED AUTOPILOT SYSTEM. COULD NOT DUP LICATE. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001012600250 20010126 00250 2001 1 26 SWIA972274 4 20010112 A 3425 INDICATOR CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 411SW 7067 EFIS COMP MONITOR HDG FLAGS BOTH SIDES, INDICATION LASTED ONE MINUTE. ABORTED TAKEOFF. PERFORMED OPS CHECK OF THE EFIS COMP MONITOR SYSTEM. OPS CHECK GOOD IAW CRJ MM 34-20-00. 2 L 7 2 4F RT A21EA 2001012600251 20010126 00251 NE 2001 1 26 SWIA972275 2 20010116 A 7320 EEC EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 187SW 120037 LEFT EEC FAILED ON TAKEOFF ROLL. ABORTED TAKEOFF. CLEANED ALL CANNON PLUGS AND GROUND RAN LEFT ENGINE. OPS CHECK GOOD . 2 L 7 2 4T 4 T RT A31SO E20NE 2001012600252 20010126 00252 SO 2001 1 26 SWIA972276 1 20010116 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS FAILED A SWIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 291SW 120318 CONTROL FAULT ON TAXI OUT, ON BOTH THE OUTBOARD PAIRS. QRH UNSUCCESSFUL. TROUBLESHOT FLAP SYTEM SELF DIAGNOSIS INDICAT ED LEFT OUTBOARD ACTUATOR ON FCU. REMOVED AND REPLACED LEFT FLAP (OUTBOARD) ACTUATOR IAW EMB 120 MM 27-50-07. SYSTEM O PS CHECK GOOD. P/N ON 34300-1003, S/N ON 0181, S/N OFF 0518. 2 L 7 2 4T 4 T RT A31SO E20NE 2001012600253 20010126 00253 WP 2001 1 26 ABXA0100014 1 20010117 A 5610 5613217507 WINDOW DOUG DC9 DC932 3022066 WP COCKPIT SEIZED A ABXA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 939AX 47201 CREW WAS UNABLE TO OPERATE CAPTAINS CLEARVIEW WINDOW. THE AIRCRAFT RETURNED TO BLOCKS. MAINTENANCE INSPECTED AND LUBRI CATED THE CAPTAINS CLEAR VIEW WINDOW IAW DC-9 MM. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2001012600254 20010126 00254 NM 2001 1 26 01FDEA00029 1 20010117 A 2611 SMOKE WARNING BOEING 727 727227 1384078 NM CARGO BAY ILLUMINATED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 490FE 21493 AFT CARGO SMOKE LIGHT CAME ON DURING CLIMBOUT. REMOVED AND REPLACED AFT NR 1 SMOKE DETECTION UNIT PER FEDEX MM 26-17-01 1-2. SYS TEST GOOD. 2 L 7 3 4F A3WE 2001012600258 20010126 00258 NM 2001 1 26 C1HA200193001 1 20010105 A 3350 1000677 LIGHT BOEING 727 727212 138407G NM CABIN INOPERATIVE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 293AS 21348 1L EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY. 2 L 7 3 4F A3WE 2001012600259 20010126 00259 NM 2001 1 26 C1HA200193002 1 20010105 A 3350 900835A BATTERY PACK BOEING 727 727212 138407G NM CABIN DISCHARGED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 293AS 21348 2R EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 2001012600260 20010126 00260 WP 2001 1 26 ABXA0100003 1 20010109 A 3230 DOOR DOUG DC9 DC932F 3022067 WP NLG OPEN A ABXA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 23 909AX 47148 VIBRATIONS WERE NOTED FROM THE NOSE OF THE AIRCRAFT AFTER LANDING GEAR RETRACTION. CREW RECYCLED THE LANDING GEAR, VIBR ATION RETURNED UPON RETRACTION. THE AIRCRAFT RETURNED TO THE FIELD. THE RIGHT NOSE LANDING GEAR DOOR WAS NOTED TO BE O PEN DURING THE TAXI IN. MAINTENANCE INSPECTED CLEANED AND LUBRICATED THE NOSE LANDING GEAR RETRACT ASSY AND NOSE LANDIN G GEAR DOOR LATCH, IAW DC-9 MM 32-31-00. 2 L 7 2 4F A6WE 2001012600261 20010126 00261 WP 2001 1 26 ABXA010004 1 20010109 A 5610 59124262 WINDOW DOUG DC8 DC863 302198A WP COCKPIT STUCK A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 FIRST OFFICERS CLEARVIEW WINDOW DID NOT OPEN ALL THE WAY. MAINTENANCE INSPECTED AND REPLACED LOWER AFT HOOK SPRING AND ADJUSTED IAW DC-8 MM 56-10-03. PRESSURIZATION AND WINDOW OPERATION CHECKED GOOD. 2 L 7 4 4F 4A25 2001012600262 20010126 00262 NM 2001 1 26 C1HA200194002 1 20010108 A 3350 SIGN BOEING 727 727290 138408W NM CABIN DISLODGED A C1HA O OTHER O OTHER LD LANDING 1 GL 15 294AS 22146 AFT OVERHEAD EMERGENCY EXIT SIGN CAME DOWN BETWEEN ROW 30-31. RESECURED SIGN, CHECKS GOOD. 2 L 7 3 4F A3WE 2001012600264 20010126 00264 NM 2001 1 26 C1HA200194003 1 20010112 A 3350 SIGN BOEING 727 727290 138408W NM CABIN DISLODGED A C1HA O OTHER O OTHER LD LANDING 1 GL 15 294AS 22146 AFT OVERHEAD EMERGENCY EXIT SIGN KEEPS FALLING ON TAKEOFF AND LANDING. RESECURED, OPS CK GOOD. NOTE:QC NOTIFIED MAINTE NANCE CONTROL OF REPEAT PROBLEM. 2 L 7 3 4F A3WE 2001012600265 20010126 00265 2001 1 26 C1HA200184001 4 20010106 A 2211 6524917194 ACCESSORY UNIT BOEING 727 7272S7 138407Z NM AUTOPILOT FAILED A C1HA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 15 684CA 22491 ON DEPARTURE AND CLIMB THE AUTOPILOT CRUISE TRIM WOULD NOT OPERATE (NOSE UP) NORMAL OPERATION (NOSE DOWN). REMOVED AND REPLACED A/P ACCESSORY UNIT, CHECKS GOOD. 2 L 7 3 4F A3WE 2001012600266 20010126 00266 NM 2001 1 26 C1HA200185001 1 20010104 A 2720 106044143 SENSOR BOEING 727 7272S7 138407Z NM RUDDER FAILED A C1HA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 685CA 22492 DURING TAXI OUT WITH GENERATORS ON RUDDER PEDAL INDICATOR SHOWS UPPER INDICATOR INSYNC WITH RUDDER PEDALS. LOWER INDICA TION SHOWS ONE NEEDLE WIDTH LEFT. REMOVED AND REPLACED LOWER RUDDER POSITION SENSOR, CHECKS GOOD. 2 L 7 3 4F A3WE 2001012600267 20010126 00267 CE 2001 1 26 GLBA2001006 1 20010112 A 7540 WARNING LIGHT BEECH 1900 1900D 1154162 CE RT BLEED AIR ILLUMINATED A GLBA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 CE 01 202UX UE202 RETURN TO BLOCK - RIGHT BLEED AIR ANNUCIATOR ILLUMINATED ON CLIMBOUT. REPAIRED EVA TUBING. 2 L 7 2 4T RT A24CE 2001012900101 20010129 00101 EU 2001 1 29 RAIA00101015 1 20010121 A 5270 WIRE AEROSP ATR42 ATR42300 8680920 EU DOOR WARN SYS BROKEN A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 424TE 124 7434-STL- SERVICE DOOR WARNING LIGHT ILLUMINATED DURING TAXI OUT AND WOULD NOT GO OUT. MAINTENANCE REPAIRED BROKEN WIRE ON SERVICE DOOR IAW ATR42 MAINTENANCE MANUAL. 2 H 7 2 4T RT A53EU 2001012900126 20010129 00126 WP 2001 1 29 ABXA0100016 1 20010121 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 951AX 47616 EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE EMERGENCY LIGHTS POWER SUPPLY BATTERIES IAW DC-9 MM 33-53-02-4-0001. 2 L 7 2 4F A6WE 2001013000086 20010130 00086 NM 2001 1 30 20010111CW001 1 20010102 A 5270 SENSOR BOEING 737 737230 NM PWA JT8 JT8D17A 52049 NE AFT SERVICE DOOR OUT OF ADJ A U18F A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 23 271LR 22636 688429 DURING CLIMB, IN FLIGHT, TPU-012, LIM-IQT, AFT SRV ANNUNCIATION LIGHT CAME ON. PERFORMED CK ON DOOR, LISTENED FOR A PR SUR LEAK, AC RETURNED TO APRT. TECH ADJUSTED SRVC DOORPROXIMITY SENSOR, AND PRSUR TEST. AC RETURNTO NORMAL OPERATION. 2 L 7 2 4F 4 F RT A16WE E2EA 2001013000093 20010130 00093 EU 2001 1 30 QXEA0100021 1 20010112 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU ROW 8 BURNED OUT A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 481US 11230 PDX- EXIT SIGN LIGHT OUT IN CABIN LOCATED ON CEILING ADJACENT TO EXIT DOORS. REPLACED EXIT SIGN ROW 8, FACING AFT LIGHT CIRCUIT BOARD. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001013000094 20010130 00094 WP 2001 1 30 MWEA010071 1 20010116 A 5347 59101433 SEAT TRACK DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 STATION 198 TO 239 NR 4 SEAT TRACK HAS CORROSION ON IT. FABRICATED AND INSTALLED SPLICE. 2 L 7 2 4F A6WE 2001013000095 20010130 00095 EA 2001 1 30 COMA0160119 1 20010116 A 5754 601R14303 VANE CNDAIR CL600 CL6002B19 EA RIGHT AND LEFT CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 977CA 7157 THE RIGHT AND LEFT FLAP VANES, I/B LEADING EDGE SKINS WERE DAMAGED AND CHAFED WHERE THE FLAP VANE COMES IN CONTACT WITH THE RESTRAINING PADS. ALSO THE LEFT I/B FLAP VANE, MID LEADING EDGE WAS DAMAGED AND CHAFED. PERFORMED A MAJOR REPAIR B Y REPLACING CHAFED VANE CAPS ON LEFT AND RIGHT I/B FLAP VANCE CAPS IAW WVAC EO 601R-57-2125A. 2 L 7 2 4F RT A21EA 2001013000096 20010130 00096 EA 2001 1 30 COMA0160120 1 20010114 A 5330 SKIN CNDAIR CL600 CL6002B19 EA FUSELAGE DENTED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 966CA 11414 7132 LEFT FUSELAGE SKIN DENTED AT FS 310.00 BETWEEN STRINGERS 16 AND 17. REPAIRED SKIN BY INSTALLING FILLER AND EXTERNAL DOU BLERS IAW REO 601R-53-21-180. 2 L 7 2 4F RT A21EA 2001013000097 20010130 00097 EA 2001 1 30 COMA0160121 1 20010114 A 5730 601R10045 PANEL CNDAIR CL600 CL6002B19 EA WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 934CA 7042 WING PLANK CRACKED AT ACCESS HOLE 540EB. BLENDED OUT DAMAGE AND ROTO-PEENED AS REQUIRED IAW REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 2001013000098 20010130 00098 EA 2001 1 30 COMA0160122 1 20010112 A 5510 601R55110221 BUSHING CNDAIR CL600 CL6002B19 EA HORZONTAL STAB WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 915CA 7013 HORIZONTAL STABILIZER LEFT O/B PIVOT POINT BUSHING WAS FOUND TO BE WORN. PERFORMED A MAJOR REPAIR BY REPLACING HORIZONT AL STABILIZER LEFT O/B PIVOT POINT BUSHING (P/N 601R55-11-022-1) IAW CRJ REO 601R-55-11-2=022 REV A. 2 L 7 2 4F RT A21EA 2001013000099 20010130 00099 NM 2001 1 30 01FDEA00028 1 20010118 A 2613 WARNING LIGHT BOEING 727 727277 138408S NM NR 1 ENGINE ILLUMINATED A FDEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 25 242FE 21178 NR 1 ENG STRUT OVERHEAT LIGHT CAME ON SHORTLY AFT ENG ANTI-ICE OPEN. COMPLIED WITH TROUBLESHOOTING PROC ON PAGE 2-7-10 OF CFM. LIGHT WENT OUT. FOUND HEAT EXCHANGER CRACKED. *S/D* REMOVED AND REPLACED NR 1 BLEED AIR HEAT EXCHANGER PER M M 36-11-051-4 FROM STEP 2A - 2C. NO FAULTS NOTED. 2 L 7 3 4F RT A3WE 2001013000100 20010130 00100 NM 2001 1 30 UPS01234653 1 20010116 A 5312 PRESSURE PANEL BOEING 727 72762C 138402C NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 912UP 19244 INSPECTION TYPE:PFLT 2 INCH CRACK ALONG RT NLG W/W SIDE WALL FWD OF GEAR TRUNNION AT APPROX STA 228 (MARKED). VERIFIED END OF CRACK WITH HFEC. STOP DRILLED RACK IAW 51-40-02 FIG 1. REPAIRED CRACK AS PER SRM 51-40-02 FIG 1. REF LOG PAGE 589676. 2 L 7 3 4F A3WE 2001013000106 20010130 00106 WP 2001 1 30 RRXA010001 1 20010104 A 3310 TRANSFORMER DOUG DC8 DC873F 302199F WP COCKPIT LIGHT FAILED A RRXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 15 606AL 46044 ELECTRICAL SMOKE IN THE COCKPIT APPEARS TO COME OUT OF THE F/E PANEL. REMOVED AND REPLACED TRANSFORMER PER DC-8 M/M 33- 00 ON FIRST OFFICERS SIDE. ALSO DEFECTED AREA UPPER F/E''S DESK PANEL. FOUND ALL COMPONENTS AND WIRING SECURE, NO DEFE CTS. 2 L 7 4 4F RT 4A25 2001013000107 20010130 00107 WP 2001 1 30 RRXA010002 1 20010105 A 3000 9799084 COOLER DOUG DC8 DC873F 302199F WP ANTI-ICE SYSTEM FAILED A RRXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 15 870TV 46086 LEFT MANIFOLD AIR TEMP DID NOT EXCEED 170C N1 WERE AT 88 PERCENT, ENGINE ANTI-ICE ON, AIRFOIL DEICE ON, TAIL DEICE SYSTE M ON, THIS IS THE 3RD WRITTEN UP SEE PAGES 7686-24 AND 7686-23 MIN NEED IS 190C NOTE LEFT PACK ON 80 PERCENT. REMOVED AND REPLACED NR 1 ENG PRECOOLER CONTROL VALVE IAW DC8 MM 36-12-59 AND REMOVED AND REPLACED NR 1 ENG PNEU BLEED REG VALVE IAW DC8 MM 36-12-1 ENG RUN ACCOMPLISHED, SYSTEM OPS CHECK NORMAL IAW DC8 MM 36-12-58. 2 L 7 4 4F RT 4A25 2001013000108 20010130 00108 2001 1 30 RRXA010003 4 20010108 A 3421 1784775442 ADI DOUG DC8 DC871F 302199D WP COCKPIT MALFUNCTIONED A RRXA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 15 8085U 45975 CAPTAINS GYRO AND FLIGHT DIRECTOR FLAGS IN VIEW WHEN A/C PITCHES UP OR DOWN 3 DEG AND HORIZON FREEZES IN POSITION. REMO VED AND REPLACED CAPT''S ADI, OPS CKS GOOD IAW UAL MM 41-20 -22. 2 L 7 4 4F RT 4A25 2001013000109 20010130 00109 WP 2001 1 30 RRXA010004 1 20010110 A 3310 BALLAST DOUG DC8 DC871F 302199D WP COCKPIT ODOR A RRXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 15 8076U 45941 STRONG SMOKE ODOR COMING FROM FIRST OFFICERS SIDE, SUSPECT LIGHT BALLAST. TRANSFERRED TO DMI LIST AS CONTROL C-9755071 -227 CAT: C MEL 3301 ATA 3310 DUE DATE 20JAN01 PLACARD INSTALLED . REMOVED AND REPLACED LIGHTING BALLAST SIX PACK IAW DC-8 M/M 33-10-0. OPS CHECK GOOD THIS ACTION CLOSES DMI C9755071-0227 PLACARD REMOVED. 2 L 7 4 4F RT 4A25 2001013000110 20010130 00110 EA 2001 1 30 COMA0110016 1 20010112 A 5320 12022670001 FLOOR SUPPORT CNDAIR CL600 CL6002B19 EA COCKPIT CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 267CA 21508 120259 THE AIRCRAFT FLOOR PROPS IN THE COCKPIT ARE CRACKED. THE REPAIR CONSISTS OF CUTTING OUT THE DAMAGED AREA AND SPLICING I N A NEW PIECE IN ACCORDANCE WITH AERODESIGN REPORT 3647-1. 2 L 7 2 4F RT A21EA 2001013000111 20010130 00111 NM 2001 1 30 AWXA0001250 1 20010119 A 2751 BACC18Z3R CIRCUIT BREAKER BOEING 737 7373Y0 1384671 NM COCKPIT TRIPPED A AWXA O OTHER F FLT CONT AFFECTED DE DESCENT 1 WP 28 323AW 23684 SAN - 1/18/01 - ON DESCENT THE TRAILING EDGE FLAPS WOULD NOT EXTEND; THE LEADING EDGE DEVICES WERE NORMAL; THE TRAILING EDGE FLAPS WERE EXTENDED USING ALTERNATE FLAPS, HOWEVER THERE WAS NO FLAP INDICATION. MAINTENANCE ADVISED THE CREW TO R ESET THE FLAP POSITION INDICATOR CIRCUIT BREAKER AND THE INDICATOR WORKED NORMAL. MAINTENANCE REPORTED THE CIRCUIT BREA KER WAS POPPED; AFTER RESET THE FLAPS WORKED NORMAL THROUGH SEVERAL CYCLES; MAINTENANCE ALSO RERACKED THE FLAP/SLAT POSI TION MODULE; CHECKED HISTORY FOR 30 DAYS, NO PROBLEMS FOUND AND NO FURTHER PROBLEMS REPORTED. 2 L 7 2 4F RT A16WE 2001013000112 20010130 00112 NM 2001 1 30 AWXA0001249 1 20010119 A 5340 146N102115 BRACKET BOEING 757 7572G7 1384963 NM WING TO BODY CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 24233 LT FUSELAGE UNDER WING TO BODY FAIRING FWD OF EMERGENCY EXIT HAS CRACKED ATTACH BRACKET. FABBED REPAIR ANGLE; REMOVED D AMAGED ANGLE AND INSTALLED REPLACEMENT ATTACH ANGLE IAW SRM 51-40-02 AND 51-70-11. 2 L 7 2 4F RT A2NM 2001013000113 20010130 00113 SO 2001 1 30 COMA0110023 1 20010118 A 5230 12021360001 SKIN EMB 120 EMB120RT SO CARGO DOOR DENTED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 257CA 22412 120248 THE AIRCRAFT CARGO DOOR SKIN IS PULLED OUT AT FORWARD UPPER CORNER AREA. THE CARGO SKIN WAS REPAIRED BY ADDING A DOUBLE R IN ACCORDANCE WITH AERODESIGN REPORT 3872-1, REV IR DATED 1-18-01. 2 L 7 2 4T RT A31SO 2001013000114 20010130 00114 EU 2001 1 30 RAIA00101013 1 20010117 A 3250 AIR860122 SELECTOR VALVE JETAIR JETSTM JETSTM4101 1500501 EU NLG STEERING FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 568HK 10676 10676 41086 7301-DEC- DURING TAXI OUT NOSE WHEEL STEERING WOULD NOT TURN RIGHT. MAINTENANCE REMOVED AND REPLACED THE STEERING SELEC TOR VALVE IAW J41 MAINTENANCE MANUAL. 2 L 7 2 4T RT A41NM 2001013000115 20010130 00115 EU 2001 1 30 RAIA00101014 1 20010117 A 3250 190600 CONTROL CABLE JETAIR JETSTM JETSTM4101 1500501 EU NLG STEERING FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 568HK 10676 10676 41086 7301-DEC- DURING TAXI OUT NOSE WHEEL STEERING WOULD NOT TURN TO THE RIGHT. MAINTENANCE REMOVED AND REPLACED THE STEERIN G CABLE IAW J41 MAINTENANCE MANUAL. 2 L 7 2 4T RT A41NM 2001013000116 20010130 00116 EU 2001 1 30 QXEA0100025 1 20010115 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN BURNED OUT A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 481US 11230 SEA- FORWARD EMERGENCY EXIT SIGN OVER FLIGHT DECK DOOR IS UNSECURED. REPLACED FORWARD EMERGENCY LIGHT ASSEMBLY. OPERAT IONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001013000117 20010130 00117 EU 2001 1 30 QXEA0100026 1 20010115 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN BURNED OUT A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 481US 11230 SEA- MID CABIN EMERGENCY EXIT SIGN HAS LIGHT INOPERATIVE. REPLACED MID CABIN EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHE CK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001013000118 20010130 00118 EU 2001 1 30 QXEA0100024 1 20010115 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN BURNED OUT A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 493US 11161 PDX- EMERGENCY EXIT SIGN AFT LIGHTS AT MID CABIN OUT. INSTALLED NEW EXIT SIGN AT MID CABIN. OPERATIONAL CHECK GOOD. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001013000119 20010130 00119 NM 2001 1 30 QXEA0100027 1 20010115 A 2422 DH103024600CS INVERTER DHAV DHC8 DHC8202 2809007 NM COCKPIT INOPERATIVE A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 345PH 8995 476 BLI- STRONG FISHY SMELL IN COCKPIT, SMELLS LIKE AN INVERTER LEAK. REMOVED AND REPLACED PRIMARY INVERTER. OPERATIONAL T EST GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001013000120 20010130 00120 NM 2001 1 30 QXEA0100028 1 20010115 A 2422 DH103024600CS INVERTER DHAV DHC8 DHC8202 2809007 NM COCKPIT INOPERATIVE A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 354PH 7899 498 PDX-INVERTER POSSIBLY LEAKING COOLANT, STRONG FISHY SMELL IN COCKPIT. REMOVED AND REPLACED PRIMARY INVERTER. OPERATION AL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001013000121 20010130 00121 NE 2001 1 30 C2XA01IA034 2 20010114 A 7261 M832481113 O-RING VICKERS EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE NR 2 ENGINE CRACKED A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 27 15730 MX452609 120187 115383 IAH - FLIGHT 2908, THE CREW REPORTED THAT THE NUMBER TWO ENGINE LOST OIL PRESSURE IN FLIGHT WITH A LARGE VISUAL OIL LOSS ON THE RIGHT SIDE OF THE AIRCRAFT. THE CREW SHUTDOWN THE NUMBER TWO ENGINE BEFORE 40 PSID, AND RETURNED TO IAH WHERE I T LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THAT THE O-RING FOR THE ENGINE DRIVEN HYDRAULIC PUMP HAD FAILED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED O-RING, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SER VICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2001013000122 20010130 00122 NM 2001 1 30 01FDEA00030 1 20010120 A 2750 CIRCUIT BREAKER BOEING 727 727233 138408A NM FLAP INDICATOR FAILED A FDEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 25 258FE 20940 TRAILING EDGE INBOARD FLAPS FAILED TO RETRACT DURING GO-AROUND. RED TABS ACCOMPLISHED. RESET INBOARD FLAP IND CIRCUIT BREAKER. CYCLED FLAPS 4 TIMES WITH NO DISCREPANCY. TEST PER 727-200 MM 27-51-000-1. OK TO CONTINUE. 2 L 7 3 4F RT A3WE 2001013000123 20010130 00123 EU 2001 1 30 01FDEA00031 1 20010120 A 2611 SMOKE DETECTOR AIRBUS 300 A300F4605R 3930327 EU E/E BAY MALFUNCTIONED A FDEA O OTHER N FALSE WARNING LD LANDING 1 SO 25 654FE 738 ON LAND RNO AVIONICS SMOKE WARNING ON LEFT ECAM CAME ON. REMOVED SMOKE DETECTOR 13WA AVIONICS COMPT DET PER MM 26-15-12 -4. 2 L 7 2 4F RT A35EU 2001013000125 20010130 00125 EA 2001 1 30 COMA0160129 1 20010117 A 5313 STRINGER CNDAIR CL600 CL6002B19 EA FUSELAGE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 966CA 7132 STRINGER/INTERCOSTAL AT NR 16 WAS DAMAGED DURING REPAIR. REPAIRED STRINGER/INTERCOSTAL AT FS 310 IAW WVAC E/O 601R-53-2 136B. 2 L 7 2 4F RT A21EA 2001013000126 20010130 00126 EA 2001 1 30 COMA0160130 1 20010117 A 5330 DOUBLER CNDAIR CL600 CL6002B19 EA FUSELAGE LEAKING A COMA O OTHER O OTHER NR NOT REPORTED 1 SO 01 966CA 7132 FS 310.00 (LT) SKIN DOUBLER REPAIR IS LEAKING. REPAIRED FS 310 SKIN DOUBLER REPAIR IAW WVAC EO 601R-53-2136B. 2 L 7 2 4F RT A21EA 2001013000127 20010130 00127 EA 2001 1 30 COMA0160131 1 20010117 A 5320 SILL CNDAIR CL600 CL6002B19 EA CARGO DOORWAY TORN A COMA O OTHER O OTHER NR NOT REPORTED 1 SO 01 719CA 7253 THE FORWARD ATTACH FOR THE CARGO NET WAS TORN FROM THE CARGO DOORSILL. TRIMMED THE TORN SILL TO A SMOOTH RADIUS AND FAB RICATED A REPAIR DOUBLER AND INSTALLED DOUBLER IAW WVAC EO 601R-53-2142. 2 L 7 2 4F RT A21EA 2001013000128 20010130 00128 EA 2001 1 30 COMA0160132 1 20010118 A 2750 860D10018 FCU CNDAIR CL600 CL6002B19 EA E/E BAY MALFUNCTIONED A COMA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 403CA 822 7428 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2001013000129 20010130 00129 WP 2001 1 30 CALA0100047 1 20010119 A 5320 FLOOR SUPPORT DOUG DC10 DC1030 3023501 WP CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND TRANSVERSAL SUPPORT UNDER FLOOR PANEL 244AF IN MID PASSENGER CABIN CORRODED AT STA 816. REPLACED SUPPO RT IAW SRM 51-31-01. 2 L 7 3 4F A22WE 2001013000130 20010130 00130 WP 2001 1 30 CALA0100048 1 20010119 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP PAX CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND FLOORBEAM CORRODED IN PASSENGER CABIN AT STA 495, LT SIDE. A NEW FLOORBEAM WAS INSTALLED IAW SRM 51-31 -01. 2 L 7 3 4F A22WE 2001013000131 20010130 00131 NM 2001 1 30 CALA0100049 1 20010120 A 5315 FLOORBEAM BOEING 737 737524 1384721 NM PAX CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19623 27527 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, LBL 15. A REPAIR STRAP WAS INSTALLED IAW ECRA 5310-04093. 2 L 7 2 4F RT A16WE 2001013000132 20010130 00132 NM 2001 1 30 CALA0100050 1 20010121 A 2760 2732513 CONTROL CABLE BOEING 737 7373T0 1384582 NM SPOILER BROKEN A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 17317 23368 THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM DCA. CHECKLIST PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO DCA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE GROUND SPOILER INTERLOCK VALVE CABLE BROKEN. THE CABLE WAS REPLACED IAW MM 27-62-51. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2001013000133 20010130 00133 WP 2001 1 30 CALA0100051 1 20010121 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND A 1 INCH CRACK (PAST STOP DRILL) IN RT MLG DOOR SUPPORT FRAME AT STA 946, RBL 10. THE EXISTING REPAIR DOUBLERS WERE REMOVED FOR ACCESS IAW SRM 51-30-2. THE CRACK WAS STOP DRILLED IAW SRM 51-10-4. THE REPAIR DOUBLERS WERE REINSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 2001013000134 20010130 00134 WP 2001 1 30 CALA0100052 1 20010121 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 230 BETWEEN LONGERON 19L AND 20L. THE DENTED AREA WAS CUT OUT IAW SRM 53-04, FIGURE 25. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 25, 51-30-2, 51-30-4, AND 51-30-5. 2 L 7 2 4F A6WE 2001013000135 20010130 00135 EA 2001 1 30 COMA0160134 1 20010118 A 4970 MS280343 SENSOR CNDAIR CL600 CL6002B19 EA APU TEMP MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 809CA 7366 APU OIL TEMP CAUTION MESSAGE. REPLACED THE OIL TEMP BULB. 2 L 7 2 4F RT A21EA 2001013000136 20010130 00136 NM 2001 1 30 UPS01234658 1 20010105 A 5755 65982962 CASTING BOEING 727 72731C 1384011 NM NR 7 SPOILER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C, NR 7 SPOILER INBOARD HINGE CASTING CORRODED. REPLACED NR 7 SPOILER INBOARD HINGE CASTING IAW SRM 51- 30-02. 2 L 7 3 4F A3WE 2001013000137 20010130 00137 NM 2001 1 30 UPS01234659 1 20010108 A 5753 65847812 SUPPORT FITTING BOEING 727 72731C 1384011 NM NR 7 FLAP TRACK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C, NR 7 FLAP TRACK ATTACH FITTING ON REAR SPAR CRACKED. FITTING REPLACED IAW SRM 51-30-02 AND DRAWING 6 5-16201. 2 L 7 3 4F A3WE 2001013000138 20010130 00138 NM 2001 1 30 UPS01234660 1 20010108 A 5720 SUPPORT FITTING BOEING 727 72731C 1384011 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C, SUPPORT FITTING ON RT WING REAR SPAR AT WS 620 APPROX CRACKED. REPLACED SUPPORT FITTING WITH PART FA BRICATED IAW DRAWING 69-16227. 2 L 7 3 4F A3WE 2001013000139 20010130 00139 NM 2001 1 30 UPS01234661 1 20010107 A 3211 651765422 LINK BOEING 727 72731C 1384011 NM RT MLG TRUNNION CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C, RT MAIN LANDING GEAR TRUNNION LINK CORRODED EXCESSIVELY AROUND SPLINED AREA, CHROME ALSO DAMAGED DUE TO CORROSION. RT TRUNNION LINK REPLACED IAW MM 32-11-01. 2 L 7 3 4F A3WE 2001013000140 20010130 00140 NM 2001 1 30 UPS01234694 1 20010119 A 3350 LIGHT BOEING 727 72725C 138400H NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:PFLT EXIT EMERGENCY LIGHT AT FWD LWR CORNER OF FWD ENTRY DOOR IS INOP. REPLACED BATTERY, NO HELP. REMO VED AND REPLACED LAMP ASSY AT FWD LWR CORNER OF FWD ENTRY DOOR.V OPS CK GOOD AT THIS TIME. 2 L 7 3 4F A3WE 2001013000141 20010130 00141 NM 2001 1 30 UPS01234695 1 20010118 A 3350 LIGHT BOEING 727 72725C 138400H NM GALLEY INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:PFLT REAR EMERGENCY CEILING EXIT LT AT GALLEY AREA IS INOP. RELAMPED BATTERY, OPS CK GOOD. 2 L 7 3 4F A3WE 2001013000142 20010130 00142 NM 2001 1 30 UPS01234696 1 20010119 A 3350 LIGHT BOEING 727 72725C 138400H NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:PFLT EMERGENCY CEILING LT AT ROW 1, LT SIDE IS AT FWD ENTRY IS INOP. REPLACED BATTERY, NO HELP. RESEAT ED BATTERY, OPS CK GOOD AT THIS TIME. 2 L 7 3 4F A3WE 2001013000143 20010130 00143 NM 2001 1 30 UPS01234697 1 20010118 A 3350 BATTERY BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:PFLT BATTERIES IN CEILING FOR OUTSIDE EMERGENCY LIGHTS ARE WEAK. REMOVED AND REPLACED BATTERIES, OPS CK S GOOD. 2 L 7 3 4F A3WE 2001013000144 20010130 00144 NM 2001 1 30 UPS01234698 1 20010119 A 3350 BATTERY BOEING 727 72722C 138400F NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:PFLT EMERGENCY LIGHTS WILL NOT TEST. BATTERY CHARGED. 2 L 7 3 4F A3WE 2001013000145 20010130 00145 NM 2001 1 30 UPS01434686 1 20010121 A 5755 PANEL BOEING 747 747123F NM NR 6 SPOILER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, LT WING CRACK ON T/E PANEL FWD OF SPOILER NR 6 I/B HINGE. REPAIRED IAW SRM 51-40-09 MATERIAL USED BM S 8-301TY2. 2 L 7 4 4F A20WE 2001013000146 20010130 00146 NM 2001 1 30 UPS01634699 1 20010112 A 3350 BATTERY BOEING 767 76734AF 1385212 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 303UP 27241 INSPECTION TYPE:PFLT EMERGENCY LIGHTS FAILED, OPS CK. REMOVED AND REPLACED BATTERY PACK, OPS CK NORMAL AT THIS TIME. 2 L 7 2 4F RT A1NM 2001013000147 20010130 00147 WP 2001 1 30 UPS01834662 1 20010102 A 5320 4772397U1 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C2, STA 1770 LONG 17R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397 AND SRM 51-1 -20D. 2 L 7 4 4F RT 4A25 2001013000148 20010130 00148 WP 2001 1 30 UPS01834663 1 20010102 A 5320 4772397U1 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C2 STA 1770 LONG 17L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397 AND SRM 51-1- 20D. 2 L 7 4 4F RT 4A25 2001013000149 20010130 00149 WP 2001 1 30 UPS01834664 1 20010108 A 5313 5644130 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C2, STA 1770 LONG 17L IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON IAW DWG 5644130 AND SRM 53- 2-2 FIG 10. 2 L 7 4 4F RT 4A25 2001013000150 20010130 00150 WP 2001 1 30 UPS01834667 1 20010102 A 5320 37502571N FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C2, STA 440 - 460 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001013000151 20010130 00151 WP 2001 1 30 UPS01834668 1 20010104 A 5320 3754914501 FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C2, STA 1150 - 1160 ATTACHMENT FITTING IS CORRODED BEYOND LIMITS ABOVE LONG 31R. REMOVED AND REPLACED F ITTING IAW DWG 3754914 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001013000152 20010130 00152 WP 2001 1 30 UPS01834669 1 20010109 A 5313 5644130 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C2, STA 1770 LONG 17R IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON IAW DC8-53B-009-39 AND SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2001013000153 20010130 00153 WP 2001 1 30 UPS01834670 1 20010103 A 5320 3755843502 FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C2, STA 1160 BATHTUB FITTING IS CRACKED BETWEEN LONG 34R AND 35R. REMOVED AND REPLACED FITTING IAW DWG 3755843 AND SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 2001013000154 20010130 00154 WP 2001 1 30 UPS01834671 1 20010102 A 5512 5640808507N PANEL DOUG DC8 DC871F 302199D WP HORIZONTAL STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C2, LEFT HAND SIDE OF LOWER HORIZONTAL STAB FWD CONSTANT PANEL IS CRACKED BETWEEN 1ST THREE BOLT HOLES. REMOVED AND REPLACED LOWER FWD CONSTANT PANEL IAW DC8-5510-1074L. 2 L 7 4 4F RT 4A25 2001013000156 20010130 00156 WP 2001 1 30 UPS01834683 1 20010103 A 5320 37558451N FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C2, STA 1152 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG 35R - 36. REMOVED AND REPLACED FITT ING IAW DWG 3755845 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001013000157 20010130 00157 WP 2001 1 30 UPS01834684 1 20010103 A 5320 37558452N FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C2, STA 1160 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG 35R AND LONG 36. REMOVED AND REPLAC ED FITTING IAW DWG 3755845 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001013000158 20010130 00158 WP 2001 1 30 UPS01834685 1 20010103 A 5340 37558452N FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C2, STA 1230 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG 34L AND 35L. REMOVED AND REPLACED F ITTING IAW DWG 3755845 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001013000159 20010130 00159 WP 2001 1 30 UPS01834700 1 20010119 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE:N/A, DURING BITE CHECK NO EMERGENCY EXIT LIGHTS ILLUMINATED. REMOVED AND REPLACED BATTERY AND RELAY UNI T. 2 L 7 4 4F RT 4A25 2001013000160 20010130 00160 EA 2001 1 30 COMA0160135 1 20010119 A 2613 355862255 ELEMENT CNDAIR CL600 CL6002B19 EA FUSELAGE MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 786CA 7333 ANTI-ICE DUCT WARNING MESSAGE. REPLACED FUSELAGE SECTION OF LEAK DETECTION LOOP. 2 L 7 2 4F RT A21EA 2001013000161 20010130 00161 EA 2001 1 30 COMA0160136 1 20010119 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN ODOR A COMA O OTHER O OTHER LD LANDING 1 SO 01 943CA 7062 STRONG ODOR OF FUEL IN CABIN WITH APU OPERATING. COULD NOT DUPLCIATE. INSPECTED APU. NO LEAKS OR DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2001013000162 20010130 00162 2001 1 30 COMA0160137 4 20010119 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 729CA 7265 STALL FAIL CAUTION DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001013000163 20010130 00163 WP 2001 1 30 MWEA010100 1 20010119 A 5753 59359415 PANEL DOUG DC9 DC981 3022081 WP TE FLAP DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 NUMBER 2 FLAP TRAILING EDGE DAMAGED AT STATION X1FD 116. REPAIRED DAMAGED SKIN. REMOVED DAMAGED SPAR AND INSTALLED SER VICEABLE. 2 L 7 2 4F A6WE 2001013000164 20010130 00164 WP 2001 1 30 MWEA010101 1 20010122 A 5330 59114004 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FOUND DENT ON SKIN AT STATION 105 LEFT SIDE LONGERON 19. REMOVED DAMAGED AREA, FABRICATED, LOCATED, DRILLED, AND INSTAL LED DOUBLER. 2 L 7 2 4F A6WE 2001013000165 20010130 00165 WP 2001 1 30 MWEA010102 1 20010122 A 5330 5911416503 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 DRILL START IN OUTER SKIN ABOUT 3 INCHES FORWARD OF FRAME STATION 598 JUST BELOW WINDOW BELT PANEL. REMOVED DAMAGE AND FLUSH PLUGGED IAW SUBMITTAL MWX-ORD-01-00044H DATED 12 JAN 01. 2 L 7 2 4F A6WE 2001013000166 20010130 00166 WP 2001 1 30 MWEA010103 1 20010122 A 5313 27779224 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 INSIDE CABIN RIGHT LAV HAD CRACKED LONGERON STATION 965, LONGERON 17 RIGHT. REMOVED DAMAGED LONGERON, SPLICED AND INSTA LLED. 2 L 7 2 4F A6WE 2001013000167 20010130 00167 WP 2001 1 30 MWEA010104 1 20010122 A 5330 49581561 SKIN DOUG DC9 DC932 3022066 WP WINDOW BELT DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 WINDOW FRAME CORRODED AND PITTED STATION 503 - 522, ZONE 2 AND 15 LEFT WINDOW. REMOVED DAMAGED WINDOW BELT SECTION, LOC ATED, DRILLED, AND INSTALLED NEW SECTION. 2 L 7 2 4F A6WE 2001013000168 20010130 00168 WP 2001 1 30 MWEA010105 1 20010122 A 5310 995773925 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 INSIDE CABIN FORWARD OF RIGHT LAV HAD A CRACKED SHEAR CLIP AT STATION 945 BETWEEN LONGERONS 15 - 16 RIGHT. REMOVED DAMA GED AREA, FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001013000169 20010130 00169 WP 2001 1 30 MWEA010106 1 20010118 A 2720 H654 SWITCH DOUG DC9 DC932 3022066 WP TAILCONE INOPERATIVE A MWEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 31 215ME 47744 FLAP RUDDER STOP INOP LIGHT WILL NOT EXTINGUISH. REPLACED RUDDER STOP SWITCH. 2 L 7 2 4F A6WE 2001013000170 20010130 00170 NE 2001 1 30 NACA20010003 2 20010120 A 8530 356994 CYLINDER PWA DOUG DC6 DC6B 3021712 WP PWA R2800 R2800CB3 52026 NE NR 4 ENGINE CRACKED A NACA E D ENGINE SHUTDOWN RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 AL 03 867TA 576 576 45202 P31426 DUE TO NR 4 ENGINE ROUGH RUNNING, LOW POWER AT RUNUP, AIR LEAK NOISE. REPLACED NR 1 CYLINDER DUE TO CRACKED HEAD. 2 L 7 4 4R 4 R 6A4 5E8 2001013000171 20010130 00171 WP 2001 1 30 TWAA0101201 1 20010119 A 5320 WEB DOUG DC9 DC983 3022083 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT, THE RT SIDE FLOOR MEMBRANE WAS CORRODED AT CUSP LINE, STA 484 THRU 598. REMOVED AND REPLACED FLOO R MEMBRANE AS REQUIRED PER SPM 6-70-01, PAGE 2 PARA 4, AND PER DOUGLAS DRAWING 9930538. 2 L 7 2 4F RT A6WE 2001013000172 20010130 00172 WP 2001 1 30 TWAA0101202 1 20010121 A 5320 PLATE DOUG DC9 DC983 3022083 WP SERVICE DOORWAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT, THE BOTTOM SILL PLATE ON THE RT SIDE CABIN SERVICE DOOR ENTRY WAY HAD HEAVY CORROSION. REPLACED S ILL PLATE PER SPM 6-70-01. INSTALLED RIVETS PER SRM 51-30-02. 2 L 7 2 4F RT A6WE 2001013000173 20010130 00173 WP 2001 1 30 TWAA0101205 1 20010117 A 5347 GALLEY TRACK DOUG DC9 DC983 3022083 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT, FOUND NUMBER 1 CABIN TRACK, GALLEY TIE DOWN HAD CORROSION AT STA 1174. REPLACED TRACK FROM STA 11 74 TO 1308, PER SRM 51-30-1. 2 L 7 2 4F RT A6WE 2001013000174 20010130 00174 WP 2001 1 30 TWAA0101206 1 20010119 A 5315 FLOORBEAM DOUG DC9 DC983 3022083 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT, FLOOR FRAME FITTING AT STA 1174, LT AFT SIDE OF AFT SERVICE DOOR WAS CORRODED. FABRICATED NEW FIT TING PER DRAWING 3936091. INSTALLED PER DRAWING 5930490. 2 L 7 2 4F RT A6WE 2001013000175 20010130 00175 WP 2001 1 30 TWAA0101207 1 20010118 A 5320 WEB DOUG DC9 DC983 3022083 WP CARGO BAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT IN THE AFT CARGO COMPT, STA 1174 TO 1250, MEMBRANE WAS CORRODED AROUND LIGHTENING HOLES. REPLACED MEMBRANE AT STA 1174 TO 1250, PER SRM 51-30-0. 2 L 7 2 4F RT A6WE 2001013000176 20010130 00176 WP 2001 1 30 TWAA0101208 1 20010118 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT, FOUND CORROSION ON NUMBER 4 TRACK AT STA 1142 TO 1309. REPLACED TRACK WITH NEW. INSTALLED PER SR M 53-05 PAGE 106. 2 L 7 2 4F RT A6WE 2001013000177 20010130 00177 WP 2001 1 30 TWAA0101203 1 20010117 A 5320 WEB DOUG DC9 DC983 3022083 WP CARGO BAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT IN THE AFT CARGO COMPT, CORROSION WAS FOUND ON THE LT FLOOR MEMBRANE AT STA 1174. REPLACED MEMBRAN E FROM 1174 TO 1250 AT CUSP ANGLE TO CHAIR TRACK, PER SRM 51-30-02. 2 L 7 2 4F RT A6WE 2001013000178 20010130 00178 WP 2001 1 30 TWAA0101204 1 20010117 A 5315 FLOORBEAM DOUG DC9 DC983 3022083 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT FOUND IN MID CABIN ON LT SIDE, STA 940, LBL 58 INCHES, CORROSION AROUND LIGHTENING HOLE IN MEMBRANE . REMOVED CORROSION PER SRM 51-30-3, PAGE 21 PARAGRAPH 35. REPAIRED PER SRM 51-70-4, FIG 2 SHEET 2. 2 L 7 2 4F RT A6WE 2001013000179 20010130 00179 SO 2001 1 30 C2XA01IA035 1 20010122 A 3260 852701 PROXIMITY SWITCH EMB 145 EMB145LR SO NLG INOPERATIVE A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 16951 145063 IAH - FLIGHT 4160, FROM DAL TO IAH, THE CREW REPORTED AN AIR GROUND FAIL WARNING, AND THE LANDING GEAR WOULD NOT RETRACT . THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NOS E LANDING GEAR PROXIMITY SWITCH TO HAVE FAILED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PROXIMITY SWITCH, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001013000180 20010130 00180 SO 2001 1 30 C2XA01IA036 1 20010119 A 3610 CA33020 CLAMP EMB 145 EMB145ER SO CARGO BAY BROKEN A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 13929 145009 IAH - FLIGHT 4211, THE CREW REPORTED THAT ON CLIMB THE CARGO BAY FILLED WITH SMOKE AND PRESSURIZATION WAS LOST. THE AIR CRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NUMBER ONE ENG INE PNEUMATIC DUCT CLAMP IN THE CARGO BAY TO HAVE COME APART. MAINTENANCE REPLACED THE AFFECTED CLAMP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001013000181 20010130 00181 NM 2001 1 30 01FDEA00032 1 20010119 A 5347 SEAT TRACK BOEING 727 727227 1384078 NM FUSLEAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 490FE 21493 DURING ROUTINE INSP, NR 6 MAIN CABIN SEAT TRACK FOUND CORRODED FROM BS 880 - 910. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-20-1, 51-30-2. 2 L 7 3 4F A3WE 2001013000182 20010130 00182 NM 2001 1 30 01FDEA00033 1 20010119 A 5347 SEAT TRACK BOEING 727 727227 1384078 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 490FE 21493 DURING ROUTINE INSP, MAIN CABIN FLOOR TRACK AT LBL 24 FOUND CORRODED FROM BS 372 - 384. REMOVED, REPLACED AND FAB PER I AW BAC 727 SRM 53-10-1, 53-10-5. 2 L 7 3 4F A3WE 2001013000183 20010130 00183 NM 2001 1 30 01FDEA00034 1 20010119 A 5320 TIE CLIP BOEING 727 727227 1384078 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 490FE 21493 DURING ROUTINE INSP, TIE CLIP BS 660, STR 3R FOUND CRACKED. REMOVED AND REPLACED PER IAW BAC 727 SRM 51-30-2. 2 L 7 3 4F A3WE 2001013000184 20010130 00184 NM 2001 1 30 01FDEA00035 1 20010119 A 5320 TIE CLIP BOEING 727 727227 1384078 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 490FE 21493 DURING ROUTINE INSP, TIE CLIP AT BS 660, STR 3L FOUND CRACKED. REMOVED AND REPLACED PER IAW BAC 727 SRM 51-30-2. 2 L 7 3 4F A3WE 2001013000185 20010130 00185 NM 2001 1 30 01FDEA00036 1 20010119 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 490FE 21493 DURING ROUTINE INSP, BS 560 CABIN FLOORBEAM FOUND CORRODED BETWEEN NR 4 AND NR 5 SEAT TRACKS. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 53-10-8. 2 L 7 3 4F A3WE 2001013000186 20010130 00186 EU 2001 1 30 01FDEA00037 1 20010122 A 5210 DOOR AIRBUS 310 A310222 3930315 EU MAIN PAX NOT CLOSED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 420FE 339 DURING CLIMBOUT, THE ECAM WARNING ON CABIN DOOR NOT CLOSED. 2 L 7 2 4F RT A35EU 2001013000187 20010130 00187 NM 2001 1 30 HNAA0100004 1 20010123 A 4960 WIRE DHAV DHC8 DHC8201 2809001 NM APU POWER BURNED A HNAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 985HA 479 ON STARTING NR 2 ENGINE THERE WAS AN ELECTRICAL SMOKE SMELL IN THE AIRCRAFT. FOUND APU POWER CABLES AT FORWARD END OF 2 429-TB2 BURNED AWAY FROM THE TERMINAL BLOCK. INSULATED AND SECURED CABLES AND MEL APU SYSTEM. 2 H 7 2 4T RT A13NM 2001013000188 20010130 00188 SO 2001 1 30 COMA0110024 1 20010122 A 3020 12007738021 LINE EMB 120 EMB120RT SO LT ENGINE DEICE WORN A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 259CA 120252 LEFT ENGINE INTAKE DEICE IS INOPERABLE. REPLACED WORN AIR HOSE. 2 L 7 2 4T RT A31SO 2001013000189 20010130 00189 EA 2001 1 30 COMA0160143 1 20010120 A 5730 601R10045 ACCESS PANEL CNDAIR CL600 CL6002B19 EA WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 926CA 7027 FUEL ACCESS PANEL HOLE NR 65088 IS CRACKED. BLENDED OUT DAMAGE AND ROTO-PEENED IAW REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 2001013000190 20010130 00190 EA 2001 1 30 COMA0160144 1 20010121 A 5330 SKIN CNDAIR CL600 CL6002B19 EA FUSELAGE DENTED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 989CA 7636 7215 FS 310 REPAIR DOUBLER BETWEEN STR 16 AND 17 HAS TEMP REPAIR. REMOVED TEMPORARY REPAIR AND INSTALLED PERMANENT REPAIR IA W REO 601R-53-21-180 REV NC. 2 L 7 2 4F RT A21EA 2001013000191 20010130 00191 EA 2001 1 30 COMA0160147 1 20010119 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 778CA 5418 7297 FLAPS FAIL MESSAGE. REPLACED THE LT BPSU. 2 L 7 2 4F RT A21EA 2001013000192 20010130 00192 EA 2001 1 30 COMA0160148 1 20010120 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 EA CABIN BURNED OUT A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 963CA 7127 FORWARD OVERHEAD EMERGENCY LIGHT IS INOPERABLE. REPLACED LIGHT BULB. 2 L 7 2 4F RT A21EA 2001013100026 20010131 00026 NM 2001 1 31 01FDEA00023 1 20010117 A 3260 SWITCH BOEING 727 72725C 138400H NM MLG DOOR DIRTY A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 135FE 19853 AFT T/O WITH GEAR RETRACT AND DOOR LIGHT OUT, HANDLE WAS PLACED IN OFF POSTION, RMG DOOR ILLUM. RAN RED TABS. PLACED H ANDLE IN THE UP POSITION AND LIGHT WENT OUT. LT HANDLE IN UP POSITION. NO YAW OR NOISE ASSOCIATED WITH DOOR LIGHT ON. *S/D* CLEANED SWITCH ELECTRO CONTACT CLEANER RG DOOR LIGHT, OPS CK GOOD AT THIS TIME PER 32-62-011-5. 2 L 7 3 4F A3WE 2001013100028 20010131 00028 2001 1 31 USAA200101172 4 20010101 A 3423 COMPASS BOEING 737 7372B7 1384560 NM COCKPIT MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 273AU 22885 AFTER TAKEOFF, HDNG SYTM ON BOTH COMPASS SYTM BECAME UNRELIABLE. SYTM WAS APRX 30 TO 35 DEGREES OFF. CREW TRIED TO FLY D IRECT TO A VOR, COULD NOT NAVIGATE PROPERLY,SELECTED BOTH COMPASSES MULTIPLE TIMES, NO HELP. DID NOT SELECT DC IN ATTE MPT TO FIX HEADING. 20 MIN OF UNRELIABLE HEADINGS, SYSTEM STARTED TO ALIGN PROPERLY, AT TOUCHDOWN, THEY WERE CLOSE. FLI GHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. EMGCY WAS DECLARED.MAINT DID COMPASS SYTM OP CK AND FOUND BOTH HSI AND RMI READ WITHIN LMTS OF STANDBY COMPASS. SYSTM CORRECTED HEADING ERROR OF APROX 1 TO2 DEGREES PER MIN. SUSPECT ORIG PR OBLEM DUE TO MAGNETIC INTERFERENCE AT ORIG STATION, LGA, THAT CAUSED FLUX VALVES TO DISTORT HDNG. AC OK FOR SERVICE. 2 L 7 2 4F A16WE 2001013100031 20010131 00031 WP 2001 1 31 ABXA0100012 1 20010116 A 3350 CONTACTOR DOUG DC9 DC932 3022066 WP BATTERY DIRTY A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 982AX 80844 ABXM373 47317 EMERGENCY LIGHTS WOULD NOT TEST DURING PRE-DEPARTURE CHECK. MAINTENANCE INSPECTED AND CLEANED THE EMERGENCY LIGHT BATTE RY CONTACTS AND RESEATED BATTERIES IN THE CHARGER. OPS CHECKED GOOD IAW DC-9 MM. 2 L 7 2 4F A6WE 2001013100032 20010131 00032 WP 2001 1 31 ABXA0100013 1 20010116 A 3350 60030451 BATTERY DOUG DC9 DC932 3022066 WP FUSELAGE DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 982AX 80845 47317 EMERGENCY LIGHTS WOULD NOT OPERATE WHEN SWITCH WAS SELECTED ON. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERY IAW DC-9 MM 33-52-02. 2 L 7 2 4F A6WE 2001013100033 20010131 00033 WP 2001 1 31 ABXA0100005 1 20010115 A 2120 UNKNOWN DOUG DC9 DC941 302207N WP COCKPIT ODOR A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 967AX 47509 FLIGHT CREW REPORTED AN ELECTRICAL ODOR WAS NOTED IN THE AIRCRAFT DURING CLIMB. THE RIGHT CSD TEMPERATURE WAS NOTED TO BE IN THE UPPER YELLOW SCALE. ABNORMAL CSD PROCEDURES WERE PERFORMED BY THE CREW. THE CSD TEMPERATURE THEN DECREASED T O BELOW CAUTION RANGE. MAINTENANCE INSPECTED AND CLEANED THE RIGHT CSD TEMPERATURE BULBS AND TEMPERATURE INDICATION CON NECTORS. GROUND RAN THE RIGHT ENGINE, AND COULD NOT DUPLICATE THE DISCREPANCY. MAINTENANCE INSPECTED ELECTRICAL PANELS AND CIRCUIT BREAKER PANELS FOR EVIDENCE OF ARCHING OR BURNED WIRES. NO DEFECTS WERE NOTED. 2 L 7 2 4F A6WE 2001013100034 20010131 00034 NM 2001 1 31 CALA0100032 1 20010116 A 5510 STRAP BOEING 737 7373Q8 1384670 NM HORIZONTAL STAB GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14381 26310 INSPECTION FOUND BOWTIE STRAP GOUGED AT TAIL CONE ATTACH POINT AFT OF RT HORIZONTAL STABILIZER ATTACH FITTING. REPLACED WITH NEW STRAP IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 2001013100035 20010131 00035 WP 2001 1 31 CALA0100033 1 20010116 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND FLOORBEAM CORRODED AT LT MID PASSENGER CABIN, STA 857 - 899. A NEW FLOORBEAM WAS INSTALLED IAW SRM 51- 31-01. 2 L 7 3 4F A22WE 2001013100036 20010131 00036 WP 2001 1 31 CALA0100034 1 20010116 A 5320 FLOOR SUPPORT DOUG DC10 DC1030 3023501 WP CENTER LAVATORY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND AFT PASSENGER CABIN RT SUPPORT IN CENTER LAV CORRODED. THE SUPPORT WAS REPLACED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 2001013100037 20010131 00037 WP 2001 1 31 CALA0100035 1 20010116 A 5320 FLOOR SUPPORT DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND LEFT O/B GALLEY FLOOR SUPPORT CORRODED IN MID PASSENGER CABIN, STA 824 - 840. THE SUPPORT WAS REPLACED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 2001013100038 20010131 00038 WP 2001 1 31 CALA0100036 1 20010116 A 5311 FRAME DOUG DC10 DC1030 3023501 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND A 0.8 INCH CRACK IN FRAME AT STA 1841 IN CENTER CARGO AREA. REPAIRED IAW SRM 53-00-01, FIGURE 4, SHEET 2. 2 L 7 3 4F A22WE 2001013100039 20010131 00039 WP 2001 1 31 CALA0100037 1 20010116 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND E&E COMPARTMENT FRAME CRACKED PAST STOP DRILL HOLE AT FS 150, L21R. THE EXISTING REPAIR WAS REMOVED, T HE CRACK WAS STOP DRILLED, AND A REPAIR WAS INSTALLED IAW SRM 51-30-05 AND 51-10-4. 2 L 7 2 4F A6WE 2001013100040 20010131 00040 WP 2001 1 31 CALA0100038 1 20010116 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 500 - 520 BETWEEN LONGERONS 20R AND 21R AND AT FS 550 - 560 BETWEEN LONGERONS 21L AND 22L. THE DENTS WERE COLD WORKED AND DOUBLERS WERE INSTALLED AT EACH LOCATION IAW SRM 53-04-38 AND 51 -30-2. 2 L 7 2 4F A6WE 2001013100041 20010131 00041 WP 2001 1 31 CALA0100039 1 20010117 A 3350 1001191 LIGHT DOUG DC9 DC981 3022081 WP CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14871 48022 INSPECTION FOUND FORWARD ENTRY PORTABLE EMERGENCY LIGHT INOPERATIVE. THE FORWARD ENTRY EMERGENCY LIGHT ASSEMBLY WAS REM OVED AND REPLACED IAW MM 33-53-00. 2 L 7 2 4F A6WE 2001013100042 20010131 00042 WP 2001 1 31 CALA0100040 1 20010116 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A CALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 09 16894 49393 THE NLG RED UNSAFE LIGHT REMAINED ILLUMINATED ACCOMPANIED BY NOISE AND BUFFETING AFTER TAKEOFF FROM ATL. THE AIRCRAFT W AS RETURNED TO ATL WHERE IT LANDED WITHOUT INCIDENT. THE NLG STRUT WAS REPACKED IAW MM 32-21-02. LEAK CHECKS WERE GOOD . A NOSE GEAR RETRACTION WAS PERFORMED IAW MM 32-20-00, PAGE 201 AND NO FAULTS WERE NOTED. 2 L 7 2 4F A6WE 2001013100043 20010131 00043 NM 2001 1 31 CALA0100041 1 20010117 A 5320 ANGLE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14381 26310 INSPECTION FOUND A 2 INCH CRACK IN ANGLE AT STA 727, RBL 12. A REPAIR WAS INSTALLED IAW SRM 51-70-11. 2 L 7 2 4F RT A16WE 2001013100044 20010131 00044 WP 2001 1 31 IXXA0100003 1 20010109 A 3230 SWITCH DOUG DC8 DC871F 302199D WP MLG WW CONTAMINATED A IXXA O OTHER N FALSE WARNING CL CLIMB 1 SW 11 826BX 82740 629 45998 EN ROUTE FROM TOL TO JFK, THE LANDING GEAR DOOR WARNING LIGHT ILLUMINATED AFTER GEAR RETRACTION. THE FLIGHT CREW CYCLED THE GEAR WITH THE WARNING INDICATION REMAINING THE SAME. THE FLIGHT CONTINUED TO JFK FOLLOWING COMPANY PROCEDURES. MA INTENANCE INSPECTED THE LANDING GEAR AND DOORS INDICATION SYSTEM WHICH REVEALED THE LEFT MAIN GEAR DOOR SWITCH CONTAMINA TED WITH MOISTURE. MAINTENANCE CLEANED THE SWITCH CANNON PLUG AND PERFORMED A SUCCESSFUL OPERATIONAL CHECK. THE AIRCRA FT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2001013100045 20010131 00045 EU 2001 1 31 RAIA00101012 1 20010117 A 3010 E420361 PITCH HORN AEROSP ATR42 ATR42300 8680920 EU ELEVATOR FAILED A RAIA O OTHER J WARNING INDICATION CL CLIMB 1 CE 03 424TE 27193 27193 124 7136-STL- DURING CLIMBOUT, RUDDER AND ELEVATOR HORN HEAT FAULTED. MAINTENANCE REMOVED AND REPLACED THE ELEVATOR HORN IA W ATR42 MAINTENANCE MANUAL. 2 H 7 2 4T RT A53EU 2001013100047 20010131 00047 NM 2001 1 31 UPS01234635 1 20010105 A 5343 FITTING BOEING 727 72731C 1384011 NM NLG DRAG BRACE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C NLG DRAG BRACE FITTING NDT COMFIRMED 2 CRACKS LOCATED ON THE SIDE OF INTERCOSTAL ATTACH FLANGE REF B72 7-5340-0166 FOR NDT CONFIRMATION. CARRIED OUT REPAIR AS PER EO B727-5340-0167MPI RAISED NR 12786. 2 L 7 3 4F A3WE 2001013100048 20010131 00048 NM 2001 1 31 UPS01234636 1 20010103 A 5343 FITTING BOEING 727 72731C 1384011 NM RT MLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C, RT MLG UPLOCK ROLLER SUPPORT FITTING HAS EVIDENCE OF CORROSION BETWEEN SHIM AND FITTING AT UPPER ATTA CH POINT. REPLACED FITTING IAW OHM 20-50-01. 2 L 7 3 4F A3WE 2001013100049 20010131 00049 NM 2001 1 31 UPS01234638 1 20010105 A 5522 SKIN PANEL BOEING 727 72731C 1384011 NM RT ELELVATOR. CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C, CORROSION ON RT ELEVATOR UNDER STATIC DISCHARGER UPPER SKIN PANEL. SKIN PANEL REPLACED IAW BOEING DR AWING 65-25639. 2 L 7 3 4F A3WE 2001013100050 20010131 00050 WP 2001 1 31 UPS01834633 1 20010117 A 3231 5640832 ROD END DOUG DC8 DC871F 302199D WP NLG DOOR BROKEN A IPXA O OTHER E VIBRATION/BUFFET CL CLIMB 1 SO 01 715UP 45915 INSPECTION TYPE:N/A, CLIMBING THRU FL260 AT 320 KIAS A SUDDEN DEAFENING NOISE ACCOMPANIED BY CONSIDERABLE VIBRATION STAR TED. SLOWING TO 200 KTS REDUCED THE NOISE AND VIBRATION TO TOLERABLE INTENSITY. NO PRESSURIZATION PROBLEMS WERE NOTED. VISUAL INSP THRU NOSE W/W VIEW PORT SHOWED ONLY MORE LIGHT THAN NORMAL. CONCLUSION WAS AN OPEN NLG DOOR. REMOVED AND REPLACED BROKEN NLG DOOR OPERATING MECHANISM AND UPPER RETRACT ROD ASSY PER M/M 32-22-02. P/N 5640832-5, S/N ON UP1621 0, S/N OFF NSN P/N 3646504, S/N ON TAG 906792, S/N OFF NSN. CK''''D PER M/M 32-22-01. JACKED AND SWUNG NOSE GEAR, OK. 2 L 7 4 4F RT 4A25 2001013100052 20010131 00052 WP 2001 1 31 MWEA010048 1 20010118 A 5720 59112801 FITTING DOUG DC9 DC932 3022066 WP LT WING DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 LEFT HAND WING STRINGER 21 HAS MECHANICAL DAMAGE AT XRS 70. FABRICATED AND INSTALLED NEW STRINGER SECTION AND SPLICES. 2 L 7 2 4F A6WE 2001013100053 20010131 00053 WP 2001 1 31 MWEA010090 1 20010118 A 5320 49113832N FITTING DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 CORROSION AROUND FITTING AT FRAME BOTTOM, AT STATION 370 LONGERON 18 RIGHT. FABRICATED AND INSTALLED NEW FITTING. 2 L 7 2 4F A6WE 2001013100054 20010131 00054 WP 2001 1 31 MWEA010091 1 20010118 A 5320 39192561 SPLICE DOUG DC9 DC932 3022066 WP FUSELAGE TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 CENTER SPLICE NR 11 FORWARD HAS NUMEROUS DEEP TOOL MARK DAMAGE AND ELONGATED HOLES. FABRICATED NEW CENTER SPLICE. 2 L 7 2 4F A6WE 2001013100055 20010131 00055 WP 2001 1 31 MWEA010092 1 20010118 A 5347 74529527 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 NR 4 SEAT TRACK HAS CORROSION ON BOTTOM OF OUTBOARD FLANGE STATION 965. FABRICATED AND INSTALLED SPLICE ANGLES, CENTER STRAP, AND SEAT TRACK SECTION. 2 L 7 2 4F A6WE 2001013100056 20010131 00056 WP 2001 1 31 MWEA010093 1 20010118 A 5720 9919369502N CAP DOUG DC9 DC932 3022066 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 RIGHT HAND WING T-CAP REMOVED DUE TO CORROSION BEYOND SRM LIMITS. FABRICATED AND INSTALLED NEW TEE CAP. 2 L 7 2 4F A6WE 2001013100057 20010131 00057 WP 2001 1 31 MWEA010094 1 20010118 A 5720 9919369501N CAP DOUG DC9 DC932 3022066 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 LEFT HAND WING STATION XRS 58.500 T-CAP REMOVED DUE TO CORROSION BEYOND SRM LIMITS. FABRICATED AND INSTALLED NEW TEE CA P. 2 L 7 2 4F A6WE 2001013100058 20010131 00058 WP 2001 1 31 MWEA010095 1 20010118 A 5720 39192561 SPLICE DOUG DC9 DC932 3022066 WP WING DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 CENTER SPLICE 14 FORWARD HAS 9 EACH OUT OF ROUND HOLES. FABRICATED AND INSTALLED NEW CENTER SPLICE. 2 L 7 2 4F A6WE 2001013100059 20010131 00059 WP 2001 1 31 MWEA010049 1 20010118 A 5315 9911524501 FLOORBEAM DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 LOWER HALF OF FLOORBEAM AT STATION 389 RIGHT HAND SIDE ABOVE FORWARD CARGO DOOR HAS EXFOLIATION AROUND LIGHTENING HOLE. FABRICATED AND INSTALLED REPAIR ANGLES. 2 L 7 2 4F A6WE 2001013100060 20010131 00060 WP 2001 1 31 MWEA010098 1 20010115 A 2133 54447222 OUTFLOW VALVE DOUG DC9 DC932 3022066 WP FUSELAGE CONTAMINATED A MWEA O OTHER O OTHER DE DESCENT 1 GL 31 216ME 47740 AUTO AND MANUAL PRESSURIZATION INOP. CABIN PRESSURE CLIMBING AT GREATER THAN 1500 FEET PER MINUTE, MASK DROPPED. FOUND LOOSE INSULATION BAG IN OUTFLOW VALVE. REMOVED BAG, STOWED MASKS. 2 L 7 2 4F A6WE 2001013100062 20010131 00062 WP 2001 1 31 MWEA010072 1 20010118 A 5210 5910072501 PANEL DOUG DC9 DC914 3022034 WP PAX DOOR MISREPAIRED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 FORWARD PASSENGER DOOR UPPER FORWARD DOOR JAMB DOUBLER DOES NOT COMPLY WITH SRM. FABRICATED AND INSTALLED REPAIR DOUBLE R. 2 L 7 2 4F A6WE 2001013100063 20010131 00063 WP 2001 1 31 MWEA010073 1 20010118 A 5210 5910163255 DOOR FRAME DOUG DC9 DC914 3022034 WP FUSELAGE CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 AFT PRESSURE BULKHEAD DOOR JAMB HAS CHAFE DAMAGE AROUND STOP PIN HOLES. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001013100064 20010131 00064 WP 2001 1 31 MWEA010074 1 20010118 A 5230 591015833 FILLER DOUG DC9 DC914 3022034 WP CARGO DOOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 CORROSION UNDER NUT PLATED, LOCATED IN AFT CARGO DOOR WEB AT STATION 713 TO STATION 718, BETWEEN LONGERON 26 RIGHT AND 2 7 RIGHT. FABRICATED AND INSTALLED REPAIR DOUBLER AND WEB. 2 L 7 2 4F A6WE 2001013100065 20010131 00065 WP 2001 1 31 MWEA010075 1 20010118 A 5240 59100843 PAN DOUG DC9 DC914 3022034 WP SERVICE DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 GALLEY SERVICE DOOR PAN HAS A CRACK IN THE INBOARD RADIUS AREA UNDER THE AFT UPPER STOP. FABRICATED AND INSTALLED NEW P AN. 2 L 7 2 4F A6WE 2001013100066 20010131 00066 WP 2001 1 31 MWEA010076 1 20010118 A 5240 59100843 PAN DOUG DC9 DC914 3022034 WP SERVICE DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 GALLEY SERVICE DOOR PAN HAS A CRACK IN THE INBOARD RADIUS AREA UNDER THE AFT LOWER STOP WITH A REPAIR ON IT. FABRICATED AND INSTALLED NEW FRAME. 2 L 7 2 4F A6WE 2001013100067 20010131 00067 WP 2001 1 31 MWEA010077 1 20010118 A 5240 59100843 SKIN DOUG DC9 DC914 3022034 WP SERVICE DOOR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 SERVICE DOOR EXTERNAL SKIN HAS DAMAGE FROM PREVIOUS REPAIRS. FABRICATED AND INSTALLED NEW SKIN. 2 L 7 2 4F A6WE 2001013100068 20010131 00068 WP 2001 1 31 MWEA010078 1 20010118 A 5320 SR0953014111 CLIP DOUG DC9 DC914 3022034 WP FUSELAGE MISSING A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 STATION 225 LONGERON 29 LEFT AND LONGERON 30 LEFT TCAS STRUCTURE INSTALLATION IS MISSING 2 SHEAR CLIPS. FABRICATED AND INSTALLED TWO ANGLES AND TWO SHEAR CLIPS. 2 L 7 2 4F A6WE 2001013100069 20010131 00069 WP 2001 1 31 MWEA010079 1 20010118 A 5412 9912243110 BULKHEAD DOUG DC9 DC914 3022034 WP RT PYLON DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 RIGHT HAND PYLON BULKHEAD LOWER WEB AT STATION 786 HAS SEVERAL ELONGATED HOLES. FABRICATED AND INSTALLED NEW WEB. 2 L 7 2 4F A6WE 2001013100070 20010131 00070 WP 2001 1 31 MWEA010080 1 20010118 A 5315 99115931 FLOORBEAM DOUG DC9 DC914 3022034 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 GOUGE IN FLOOR WEB AT STATION 159. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001013100071 20010131 00071 WP 2001 1 31 MWEA010081 1 20010118 A 5311 39203121 FRAME DOUG DC9 DC914 3022034 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 FRAME GOUGED AT STATION 389 LONGERON 29 LEFT. FABRICATED AND INSTALLED REPAIR ANGLE, PLATE, AND FILLER. 2 L 7 2 4F A6WE 2001013100072 20010131 00072 WP 2001 1 31 MWEA010082 1 20010118 A 5315 FLOORBEAM DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 500ME 45711 TWO HOLES WITH IMPROPER SPACING ON UPPER TEE OF STATION 200. FABRICATED AND INSTALLED T-ANGLE AND OUTBOARD LEFT HAND S PLICES. 2 L 7 2 4F A6WE 2001013100073 20010131 00073 WP 2001 1 31 MWEA010083 1 20010118 A 5320 WEB DOUG DC9 DC914 3022034 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 SUBFLOOR/CUSP REMOVED FROM STATION 160 - 200. FABRICATED AND INSTALLED REPLACEMENT SUBFLOOR. 2 L 7 2 4F A6WE 2001013100074 20010131 00074 WP 2001 1 31 MWEA010084 1 20010118 A 5321 99578273 FLOORBOARD DOUG DC9 DC914 3022034 WP COCKPIT CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 FLOORBOARD BETWEEN SEAT TRACKS UNDER F/O SEAT IS CRACKED IN SEVERAL LOCATIONS OF THE SKIN. FABRICATED NEW FLOORBOARD SK IN. 2 L 7 2 4F A6WE 2001013100076 20010131 00076 WP 2001 1 31 MWEA010085 1 20010118 A 5347 5956033501 CARGO TRACK DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 LUGGAGE TRACK STATION 738 - 817 HAS CORROSION. FABRICATED AND INSTALLED NEW LUGGAGE TRACK. 2 L 7 2 4F A6WE 2001013100077 20010131 00077 WP 2001 1 31 MWEA010086 1 20010118 A 5321 995791917 FLOORBOARD DOUG DC9 DC914 3022034 WP CABIN CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 SKIN CORROSION SEVERAL PLACES OUT OF LIMITS AND 4 HAT CHANNELS HAVE CORROSION OUT OF LIMITS ON FLOORBOARD E-1. FABRICAT ED AND INSTALLED FLOORBOARD SKIN AND 4 HAT CHANNELS. 2 L 7 2 4F A6WE 2001013100078 20010131 00078 WP 2001 1 31 MWEA010087 1 20010118 A 5320 99577296 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 INTERCOSTAL BETWEEN STATION 585 - 604 AT NR 4 SEAT TRACK IS CRACKED AT LIGHTENING HOLE. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001013100079 20010131 00079 WP 2001 1 31 MWEA010088 1 20010118 A 5343 39203121 FRAME DOUG DC9 DC914 3022034 WP LT MLG WW CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 LEFT HAND MAIN LANDING GEAR MAIN FRAME FORWARD INBOARD RADIUS CRACKED. FABRICATED AND INSTALLED ANGLE AND PLATE DOUBLER S. 2 L 7 2 4F A6WE 2001013100080 20010131 00080 WP 2001 1 31 MWEA010089 1 20010118 A 5343 39203121 FRAME DOUG DC9 DC914 3022034 WP LT MLG WW CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 LEFT HAND MLG MAINFRAME AFT INBOARD RADIUS CRACKED. FABRICATED AND INSTALLED ANGLE AND PLATE DOUBLERS. 2 L 7 2 4F A6WE 2001013100081 20010131 00081 WP 2001 1 31 MWEA010096 1 20010118 A 5330 59114015 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 LIGHTNING STRIKE DAMAGE, FUSELAGE LOWER SECTION AT STATION 190 BETWEEN LONGERON 29 - 30 LEFT. BLENDED AND REMOVED DAMAG E, FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001013100082 20010131 00082 WP 2001 1 31 MWEA010097 1 20010118 A 5313 59104934 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 INSIDE CABIN, LEFT LAV HAS A CRACKED LONGERON AT STATION 965, LONGERON 16 LEFT. FABRICATED AND INSTALLED NEW LONGERON. 2 L 7 2 4F A6WE 2001013100083 20010131 00083 EA 2001 1 31 COMA0160123 1 20010115 A 5320 601R52110081 ANGLE CNDAIR CL600 CL6002B19 EA SEAL STRIKER CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 966CA 11414 7132 PAX DOOR SEAL STRIKER PREVIOUS REPAIR AT FS 349.00 IS CRACKED (FILTER ONLY). PERFORMED REPAIR TO STRIKER IAW REO 601R-5 2-11-008 REPAIR A STEP 4 ONLY. 2 L 7 2 4F RT A21EA 2001013100084 20010131 00084 EA 2001 1 31 COMA0160124 1 20010114 A 5320 601R31171 ATTACH ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 977CA 10019 7157 ATTACH ANGLE (P/N 601R31171) AT FS 484, LBL 27, WL 73.50 WAS CRACKED. REMOVED DISCREPANT ANGLE, FABRICATED AND INSTALLE D REPLACEMENT ANGLE IN ACCORDANCE WITH WVAC EO 601R-53-2124. 2 L 7 2 4F RT A21EA 2001013100085 20010131 00085 EA 2001 1 31 COMA0160125 1 20010114 A 5315 601R3111367 FLOORBEAM CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 915CA 18100 7013 FLOORBEAM (P/N 601R31113-67) AT FS 409 + 16 CRACKED .5 INCH (RBL 9 AND 409 + 16). REPAIRED FLOORBEAM AT RBL 9 AT FS 409 + 16 IAW WVAC EO 601R53-2110. 2 L 7 2 4F RT A21EA 2001013100086 20010131 00086 EA 2001 1 31 COMA0160126 1 20010116 A 3010 DUCT CNDAIR CL600 CL6002B19 EA WING ANTI-ICE LEAKING A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 917CA 7017 WING OVERHEAT AND ANTI-ICE DUCT LEAK WARNING. COULD NOT DUPLICATE. DEFERRED MAINT PER MEL. SYSTEM WORKS OK IN STANDBY MODE. 2 L 7 2 4F RT A21EA 2001013100087 20010131 00087 EA 2001 1 31 COMA0160127 1 20010117 A 2750 CONTROL UNIT CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 811CA 7380 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2001013100088 20010131 00088 NE 2001 1 31 COMA0160128 2 20010117 A 7261 5018T48P03 CARBON SEAL CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT ENGINE LEAKING A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 949CA 7080 807062 LEFT ENGINE OIL PRESSURE FLUCTUATING BETWEEN 30 AND 48 PSI. REPLACED THE ACCESSORY DRIVES CARBON SEALS. 2 L 7 2 4F 4 F RT A21EA E15NE 2001013100089 20010131 00089 WP 2001 1 31 TWAA0101101 1 20010111 A 5310 DOUBLER DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9404V 53140 DURING CHECK-C MAINT IN THE AFT CARGO COMPT, FOUND DOUBLER CORRODED AT DOOR JAMB STA 1193, LONGERON 28R TO 29R. FABRICA TED NEW DOUBLER AND INSTALLED AND PAINTED PER SPM 6-70-01 AND SRM 51-10-3. 2 L 7 2 4F RT A6WE 2001013100090 20010131 00090 WP 2001 1 31 TWAA0101102 1 20010111 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9404V 53140 DURING CHECK-C MAINT IN AFT CARGO COMPT FLOOR SUPPORT BRACE WAS CORRODED AT STA 1155 TO 1212, LONGERON 29R, AND AT STA 1 212 LONGERON 29R TO 28L TOP AND BOTTOM. REPLACED BOTH SUPPORTS REF IPC 25-52-00 FIG 3L. 2 L 7 2 4F RT A6WE 2001013100091 20010131 00091 WP 2001 1 31 TWAA0101103 1 20010113 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9404V 53140 DURING CHECK-C MAINT IN THE AFT CARGO COMPT COROSION WAS AROUND SCREW HOLES ON LT TIE DOWN TRACK FROM STA 1212 TO 1320R. INSTALLED NEW TRACK PER SRM 51-30-0. 2 L 7 2 4F RT A6WE 2001013100092 20010131 00092 WP 2001 1 31 TWAA0101104 1 20010111 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP CARGO BAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9404V 53140 DURING CHECK-C MAINT IN THE AFT CARGO COMPT FLOOR SUPPORT WAS CORRODED AT STA 1155, LONGERON 29R TO 28L. INSTALLED NEW FLOOR SUPPORT PER SRM 51-30-5. 2 L 7 2 4F RT A6WE 2001013100093 20010131 00093 WP 2001 1 31 TWAA0101105 1 20010111 A 5310 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9404V 53140 DURING CHECK-C MAINT IN THE AFT CARGO COMPT, CORROSION WAS ON LOWER DOOR JAMB AT STA 1155 TO 1212. INSTALLED NEW BEAM P ER DOUGLAS PRINT 5930483. 2 L 7 2 4F RT A6WE 2001013100094 20010131 00094 WP 2001 1 31 TWAA0101106 1 20010112 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9404V 53140 DURING CHECK-C MAINT FOUND CORROSION ON TIE DOWN TRACK LT STA 1081 TO 1219. REPLACED TRACK AT STA 1087 TO 1222 LT PER S RM 51-30-0. 2 L 7 2 4F RT A6WE 2001013100095 20010131 00095 WP 2001 1 31 TWAA0101107 1 20010110 A 5280 DOOR DOUG DC9 DC983 3022083 WP NLG TORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT ON THE NOSE LANDING GEAR, THE RT NOSE LANDING GEAR WHEEL WELL DOOR HAD CORROSION AND TORN METAL ON LEADING EDGE. REMOVED DAMAGE BY BLENDING PER SRM 52-01 FIG 1. REMOVED CORROSION PER SPM 6-80-01. 2 L 7 2 4F RT A6WE 2001013100096 20010131 00096 WP 2001 1 31 TWAA0101109 1 20010111 A 5315 FLOORBEAM DOUG DC9 DC983 3022083 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT FOUND CORROSION ON FLOORBEAM AT STA 193 AND BETWEEN LBL 16 IN TO 43 IN. MADE NEW FLOOR SUPPORT EXT RUSION AND INSTALLED FLOOR SUPPORT PER SRM 51-30-0 RIVETS. 2 L 7 2 4F RT A6WE 2001013100097 20010131 00097 WP 2001 1 31 TWAA0101110 1 20010112 A 5310 BEAM DOUG DC9 DC983 3022083 WP CARGO DOORWAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT IN THE AFT CARGO COMPT, FOUND HEAVY CORROSION ON LOWER CARGO DOOR BEAM AT STA 1155 TO 1212. REPLAC ED DOOR BEAM PER INSTALLATION PRINT 5930483 AND SPM 6-70-01, PAGE 3 ITEM B. 2 L 7 2 4F RT A6WE 2001013100098 20010131 00098 WP 2001 1 31 TWAA0101111 1 20010112 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP CARGO BAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT IN AFT CARGO COMPT, CORROSION WAS FOUND ON RT FLOOR MEMBRANE TO CARGO DOOR FRAME, STA 1155 TO 1212. REPLACED MEMBRANE PER PRINT 5936442 AND SPM 6-70-01, PAGE 3 ITEM B. 2 L 7 2 4F RT A6WE 2001013100099 20010131 00099 WP 2001 1 31 TWAA0101112 1 20010112 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT CABIN FLOOR SUPPORT WAS CORRODED AT STA 157 TO 207, RBL 7 INCHES. INSTALLED NEW PART AND INSTALLED WITH BOLTS PER SRM 6-70-01 AND SRM 51-30-1. 2 L 7 2 4F RT A6WE 2001013100100 20010131 00100 WP 2001 1 31 TWAA0101113 1 20010113 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT AT STA 597 TO 604, BOTH SIDES OF FLOOR MEMBRANE WAS CORRODED AT LBL 58. REMOVED CORROSION PER SPM 6-80-01 AND SRM 51-10-3 PAGE 21. INSTALLED REPAIR PER SRM 51-70-4 PAGE 1 TO 4. 2 L 7 2 4F RT A6WE 2001013100101 20010131 00101 WP 2001 1 31 TWAA0101114 1 20010114 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP CARGO BAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND CORROSION UNDERSIDE FLOOR MEMBRANE AT STA 1098 TO 1117, RT SIDE. INST ALLED NEW MEMBRANE PER DRAWING 993612-23 AND REINSTALLED FITTING PER SPM 6-70-01. 2 L 7 2 4F RT A6WE 2001013100102 20010131 00102 WP 2001 1 31 TWAA0101115 1 20010114 A 5320 ATTACH ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT FOUND CORROSION ON CABIN MEMBRANE ATTACH ANGLE OUTBOARD OF NUMBER 6 TRACK, STA 1155 TO 1174. INSTA LLED NEW MEMBRANE PER DRAWING 9930612-23 AND SPM 6-70-01. 2 L 7 2 4F RT A6WE 2001013100103 20010131 00103 WP 2001 1 31 TWAA0101116 1 20010114 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP CARGO BAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT IN THE AFT CARGO COMPT, CORROSION WAS FOUND UNDERSIDE RT FLOOR MEMBRANE AT STA 1117 TO 1136. INSTA LLED NEW MEMBRANE PER DRAWING 9330612-23 AND SPM 6-70-01. 2 L 7 2 4F RT A6WE 2001013100104 20010131 00104 WP 2001 1 31 TWAA0101117 1 20010114 A 5320 ATTACH ANGLE DOUG DC9 DC983 3022083 WP CARGO BAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT FOUND CORROSION ON CABIN MEMBRANE ATTACH ANGLE OUTBOARD OF NUMBER 6 TRACK, STA 1136 TO 1155. INSTA LLED NEW MEMBRANE ATTACH ANGLE PER DRAWING 9330612-23 AND SPM 6-70-01. 2 L 7 2 4F RT A6WE 2001013100105 20010131 00105 WP 2001 1 31 TWAA0101118 1 20010115 A 5320 WEB DOUG DC9 DC983 3022083 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT IN THE FWD CABIN LT, CORROSION WAS FOUND AROUND LIGHTENING HOLES ON WEB MEMBRANE AT STA 699 LBL 58 INCHES, STA 683 LBL 58 IN, STA 663 LBL 58 INCHES, AND STA 617 TO 636 LBL 58 INCHES. REPLACED MEMBRANE AT EACH LOCATION PER DRAWING 9930538. 2 L 7 2 4F RT A6WE 2001013100106 20010131 00106 WP 2001 1 31 TWAA0101119 1 20010115 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP CARGO BAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT IN THE AFT CARGO COMPT, CORROSION WAS FOUND ON UNDERSIDE OF MEMBRANE AT STA 1022 TO 1041. REPLACED MEMBRANE PER DRAWING 9930612-2. INSTALLED DOUBLERS AT STA 1022 AND 1032 PER SRM 53-01 FIG 4. 2 L 7 2 4F RT A6WE 2001013100107 20010131 00107 WP 2001 1 31 TWAA0101120 1 20010115 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP CARGO BAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT IN THE AFT CARGO COMPT, CORROSION WAS ON UNDERSIDE OF FLOOR MEMBRANE AT STA 1041 TO 1060 RT SIDE, S TA 1060 TO 1079, AND STA 1079 TO 1098. REMOVED AND REPLACED MEMBRANES PER DRAWING 9930612-25 AND SPM 6-70-14A AND B. 2 L 7 2 4F RT A6WE 2001013100108 20010131 00108 WP 2001 1 31 TWAA0101121 1 20010115 A 5310 SILL DOUG DC9 DC983 3022083 WP AFB DOOR FRAME CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT IN THE AFT CABIN, CORROSION WAS ON FWD SIDE OF SILL PLATE, AFT PRESSURE BULKHEAD DOOR JAMB. REMOVE D CORRODED SECTION OF DOOR JAMB SILL PLATE. FABRICATED NEW LOWER SECTION OF JAMB ASSY PER DRAWING 5917463. SPLICED IN FABRICATED JAMB PER SRM 53-05 FIGURE 30. 2 L 7 2 4F RT A6WE 2001013100109 20010131 00109 WP 2001 1 31 TWAA0101122 1 20010116 A 5320 WEB DOUG DC9 DC983 3022083 WP CARGO BAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT FOUND CORROSION ON MEMBRANE LT SIDE WALL AREA STA 389 TO 408. REPLACED MEMBRANE PER SPM 6-70-01. INSTALLED HI-LOK PER SPM 51-30-05. INSTALLED BOLTS PER SRM 51-30-01. INSTALLED RIVETS PER SRM 51-30-02. MEMBRANE FROM STA 389 TO 503 REPLACED. 2 L 7 2 4F RT A6WE 2001013100110 20010131 00110 WP 2001 1 31 TWAA0101123 1 20010116 A 5315 FLOORBEAM DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOORBEAM AT STA 160, LBL 8 INCHES. MADE NEW FLOOR SUPPORT PART, INSTALLE D PER SRM 51-30-02 AND SRM 51-30-05. 2 L 7 2 4F RT A6WE 2001013100111 20010131 00111 WP 2001 1 31 TWAA0101124 1 20010116 A 5320 WEB DOUG DC9 DC983 3022083 WP CARGO BAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT IN FWD CARGO COMPT CORROSION WAS ON MEMBRANE LT SIDEWALL AREA STA 503 TO 522. REMOVED CORROSION PE R SPM 6-80-01 AND SRM 51-10-3 PAGE 21. REPAIRED WITH DOUBLER PER SRM 53-01 FIG 4 SHEET 3. 2 L 7 2 4F RT A6WE 2001013100112 20010131 00112 WP 2001 1 31 TWAA0101125 1 20010117 A 5743 SUPPORT FITTING DOUG DC9 DC982 3022082 WP RT WING MLG NICKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT ON RT WING ON STRUT OF MAIN LANDING GEAR SUPPORT FITTING, THE FWD END OF HYD VALVES HAD A NICK IN T HE FITTING. BLENDED OUT NICK PER SRM 53-01 FIG 1 SHEET 1. 2 L 7 2 4F A6WE 2001013100113 20010131 00113 WP 2001 1 31 TWAA0101126 1 20010117 A 5310 PRESSURE PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9307R 49663 DURING CHECK-C MAINT FOUND DENT IN PRESSURE PANEL AT STA 37, RT SIDE, APPROX 4 INCHES INBOARD OF OUTER SKIN. DENT WAS A PPROX 2.5 INCH BY 1 INCH BY 0.250 DEEP. REMOVED DAMAGED SECTION AND SPLICED IN NEW SECTION PER SRM 53-01, FIG 2 AND 7. 2 L 7 2 4F RT A6WE 2001013100114 20010131 00114 NM 2001 1 31 TWAA0101127 1 20010115 A 5751 SKIN BOEING 767 767231 1385131 NM RT WING AILERON DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 604TW 22567 DURING CHECK-C MAINT THE RT WING OUTBOARD AILERON AT OUTBOARD END, BOTTOM 4 INCH BY 6 INCH AREA DELAMINATED. CLEANED AN D BONDED FWD EDGE OF CONDUCTIVE FRAME WITH BMS 5-95 PER MM 57-51-03. 2 L 7 2 4F RT A1NM 2001013100115 20010131 00115 WP 2001 1 31 MWEA010099 1 20010118 A 4930 36177502 FUEL CONTROL DOUG DC9 DC932 3022066 WP APU BAY OUT OF ADJ A MWEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 31 602ME 48133 WHILE IN CRUISE FLIGHT APU RPM AND GENERATOR FREQUENCY INDICATIONS WERE OUTSIDE ACCEPTABLE LIMITS. FLIGHT RETURNED TO O MAHA. MAINTENANCE ADJUSTED FUEL CONTROL UNIT. 2 L 7 2 4F A6WE 2001013100116 20010131 00116 WP 2001 1 31 ERKR200100063 1 20010118 A 5330 FINGER DOUBLER DOUG DC9 DC933F 302207A WP FUSELAGE BROKEN B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 FINGER DOUBLER REWORK AT FS 247, 320 & 326 AT L26L. REPAIRED BY TRIMMING OFF THE BROKEN DOUBLER FINGERS. PER ECRA 933- 098-2. 2 L 7 2 4F A6WE 2001013100117 20010131 00117 WP 2001 1 31 ERKR200100064 1 20010118 A 5522 9919480105 SKIN DOUG DC9 DC933F 302207A WP LT ELEVATOR DENTED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 933F 47191 REPAIR OF DENT TO ELEVATOR, LT STATION XE 193.0. THE REPAIR CONSISTS OF ADDING AN EXTERNAL DOUBLER, FILLING THE DENT WI LL FILLER AND HOT BONDING. PER ECRA 933-55-089-2 REV A. 2 L 7 2 4F A6WE 2001013100118 20010131 00118 SO 2001 1 31 C2XA01IA032 1 20010116 A 3350 D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 40717 120133 IAH - FLIGHT 2913, DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT REMAIN ILLUMINAT ED WHEN TESTED. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NUMBER ONE EMERGENCY LIGHT POWER SUPPLY TO BE INOPERAT IVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY IN ACCORDANCE WITH EMB120 M/M 33-50-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001022600111 20010226 00111 SO 2001 2 26 C2XA01IA033 1 20010116 A 2150 8021861 A/C PACK EMB 145 EMB145ER SO NR 1 FAILED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 14933 145018 DAL - FLIGHT 4061, THE CREW REPORTED THAT ON INITIAL CLIMBOUT, THE COCKPIT AND CABIN FILLED WITH SMOKE ACCOMPANIED BY AN ELECTRICAL BURNING SMELL. THE AIRCRAFT RETURNED TO DAL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIR CRAFT AND FOUND THAT THE NUMBER ONE PACK HAD FAILED. MAINTENANCE PLACED THE AFFECTED PACK ON MEL 21-51-00 CAT-C CONTROL NUMBER 004973, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH ON 01/16/01, WHERE MAIN TENANCE REMOVED AND REPLACED THE NR 1 PACK AIR CYCLE MACHINE, REMOVED MEL 21-51-00 CONTROL 004973, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001013100120 20010131 00120 WP 2001 1 31 0100139950 1 20010115 A 5320 ANGLE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9346 47376 CRACKED VERTICAL BEAM TOP END, ON BULKHEAD FS 756, SL 28 RT. STOP DRILLED CRACK, FABRICATED ANGLES FROM .050 CRES, HEAT TREATED PASSIVATED AND CLAD PLATED. INSTALLED PER EA 99-177604. 2 L 7 2 4F A6WE 2001013100121 20010131 00121 WP 2001 1 31 0100129950 1 20010114 A 5310 PRESSURE PANEL DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9346 47376 CORROSION HEAVY AROUND FLANGES FOR SLANT PRESSURE PANEL LEFT SIDE. BLENDED OUT CORROSION IN THE 5910005-49 ANGLE CAP PE R SRM. REPAIRED PER SRM AND EA 99-177600. L/P 1550091 2 L 7 2 4F A6WE 2001013100122 20010131 00122 NM 2001 1 31 UPS01234652 1 20010119 A 3350 1000679 BATTERY BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:N/A, BATTERIES IN CEILING FOR OUTSIDE EMERGENCY LIGHTS WEAK. REMOVED AND REPLACED BATTERIES, OPS CK GOO D. 2 L 7 3 4F A3WE 2001013100123 20010131 00123 NM 2001 1 31 UPS01234654 1 20010119 A 3350 LIGHT BOEING 727 72730C 1384009 NM CABIN DETACHED A IPXA O OTHER O OTHER LD LANDING 1 SO 01 906UP 19314 INSPECTION TYPE:PFLT CREW REPORTS MAIN ENTRY EMERGENCY EXIT LIGHT FELL OFF AT LANDING. REPLACED EMERGENCY EXIT LIGHT AS SY, OPS NORMAL. 2 L 7 3 4F A3WE 2001013100132 20010131 00132 NM 2001 1 31 CALA0100042 1 20010117 A 5280 DOOR BOEING 737 7373Q8 1384670 NM LT NLG GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14381 26310 INSPECTION FOUND LT NOSE GEAR DOOR GOUGED AT I/B EDGE JUST AFT OF FORWARD END. THE FILLER AND RETAINER AT NOSE GEAR DOO R WERE REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001013100133 20010131 00133 WP 2001 1 31 CALA0100043 1 20010117 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 375 BETWEEN LONGERON 29L AND 30 AND AT FS 470, BETWEEN LONGERONS 20 L AND 21L. A DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 53-04, FIGURE 38, 51-10-4, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 2001013100134 20010131 00134 WP 2001 1 31 CALA0100044 1 20010117 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 260 BETWEEN LONGERONS 24R AND 25R AND BETWEEN LONGERONS 27L AND 28L . A DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 53-04, FIGURE 38, 51-10-4, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 2001013100135 20010131 00135 NM 2001 1 31 CALA0100045 1 20010117 A 5730 SKIN BOEING 737 7373Q8 1384670 NM LT WING GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14381 26310 INSPECTION FOUND LT WING LOWER SKIN GOUGED AFT I/B T/E AT WING ROOT JUST FORWARD OF GEAR BAY. A REPAIR WAS INSTALLED IA W SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001013100136 20010131 00136 NM 2001 1 31 CALA0100046 1 20010119 A 5743 FITTING BOEING 737 7373T0 1384582 NM LT WING SPAR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND A 1 INCH CRACK IN MLG SUPPORT BEAM O/B SUPPORT FITTING AT LT WING AFT SPAR. THE FITTING WAS REPLACED I AW EA 5743-01022. 2 L 7 2 4F RT A16WE 2001013100137 20010131 00137 EA 2001 1 31 SWIA972277 1 20010115 A 3040 SENSOR CNDAIR CL600 CL6002B19 EA WINDOW HEAT FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 409SW 7056 LEFT WINDOW HEAT MESSAGE. RETURNED TO SLC. SWITCHED LEFT WINDOW HEAT SENSOR TO SPARE HEAT SENSOR IAW MM 30-40-01. LEF T WINDOW HEAT OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2001013100138 20010131 00138 EA 2001 1 31 SWIA972278 1 20010117 A 4990 PRESSURE SWITCH CNDAIR CL600 CL6002B19 EA APU FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 406SW 7030 APU LOW OIL PRESSURE IN FLIGHT. RETURNED TO SLC. REMOVED AND REPLACED APU OIL PRESSURE SWITCH IAW A/C MM 41-91-20. AL SO REMOVED AND REPLACED APU ECU. (P/N 2118800-2) (S/N ON 66-F0139) (S/N OFF 44-F0007) IAW A/C MM 49-61-01. OPS CHECKE D AND LEAK CHECKED GOOD. 2 L 7 2 4F RT A21EA 2001013100139 20010131 00139 SO 2001 1 31 SWIA972279 1 20010111 A 5246 LATCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FUEL DOOR LOOSE A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 229SW 120305 AT 90 KNOTS TAKEOFF ROLL, GOT DOOR WARNING ON MAP AND FLASHING MASTER WARNING. NO TRIPLE CHIME LIGHT WENT OFF ON DECELE RATION. FOUND INBOARD FUEL SERVICE DOOR AFT CAMLOC TO BE LOOSE AND PUSHED THROUGH. REPLACED CAMLOC AND ADJUSTED SWITCH ON OUTBOARD FUEL SERVICE DOOR. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001013100140 20010131 00140 EA 2001 1 31 SWIA972280 1 20010117 A 3260 SENSOR CNDAIR CL600 CL6002B19 EA MLG OUT OF ADJ A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 413SW 7102 AFTER TAKEOFF, UPON SELECTION OF GEAR UP, GOT A GEAR DISAGREE MESSAGE. FOLLOWED QRH BUT THE MESSAGE PERSISTED. RETURNE D TO YVR. FOUND OLEO CENTERED /EXTENDED PROXIMITY SENSOR OUT OF ADJUSTMENT. ADJUSTED PROXIMITY SENSOR IAW MM 32-81-05. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2001013100141 20010131 00141 SO 2001 1 31 SWIA972281 1 20010114 A 5270 SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CARGO DOOR OUT OF ADJ A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 233SW 120307 ABORT TAKEOFF AT 90 KNOTS FOR CARGO DOOR WARNING. RETURNED TO GATE. ADJUSTED FORWARD CARGO DOOR MICROSWITCH IAW MM 52- 30-00. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001013100142 20010131 00142 WP 2001 1 31 ABXA0100015 1 20010119 A 2510 561031519ABX1 SEAT DOUG DC8 DC863 302198A WP COCKPIT LACK OF LUBE A ABXA O OTHER O OTHER CR CRUISE 1 GL 23 824AX 46141 CAPTAINS SEAT SLIPPED OUT OF LOCKED POSITION FORWARD AND AFT. CLEANED AND LUBED PINS AND CAPTAIN''S SEAT TRACKS. OPS C HECKED GOOD IAW DC-8 MM. 2 L 7 4 4F 4A25 2001013100143 20010131 00143 2001 1 31 DHL2001803001 4 20010120 A 2397 WIRE DOUG DC8 DC873F 302199F WP HEADSET JACK BROKEN A DHLA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 803DH 46123 F/O HEADSET JACK INOP ON TAXI OUT. REPAIRED BROKEN WIRE AT F/O CONSOLE. OPS OK PER M/M 23-40-0. 2 L 7 4 4F RT 4A25 2001013100144 20010131 00144 WP 2001 1 31 MWEA010107 1 20010120 A 2913 AS66411LS666 PUMP DOUG DC9 DC981 3022081 WP RT ENGINE INOPERATIVE A MWEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 31 803ME 48029 RIGHT HYDRAULIC PRESSURE WENT TO ZERO AND RIGHT HYDRAULIC PRESSURE LOW LIGHT CAME ON WHEN AUXILLARY HYDRAULIC PUMP WAS T URNED OFF. REMOVED AND REPLACED RIGHT HAND ENGINE DRIVEN HYDRAULIC PUMP. 2 L 7 2 4F A6WE 2001013100145 20010131 00145 EA 2001 1 31 SWIA972282 1 20010109 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 EA PAX DOOR ILLUMINATED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 413SW 7102 AFTER TAKEOFF MAIN CABIN PASSENGER DOOR STOW CAUTION MESSAGE. RETURNED FOR LANDING TO SLC. INSPECTED THE PASSENGER DOO R INNER HANDLE, NO PROBLEMS NOTED. CLEANED THE INNER HANDLE SHAFT. DOOR WARNING SYSTEM CHECKS GOOD. 2 L 7 2 4F RT A21EA 2001013100146 20010131 00146 SO 2001 1 31 SWIA972283 1 20010109 A 3350 BULB EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CABIN BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 560SW 120334 CEILING EMERGENCY LIGHT OVER ROW TWO INOP. INSTALLED NEW BULB AND RESPECTIVE FUSE LAMP. CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001013100148 20010131 00148 SO 2001 1 31 SWIA972285 1 20010119 A 7712 INDICATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT FAILED A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 216SW 120285 LEFT ANALOG TORQUE GAUGE DROPPED TO ZERO ON TAKEOFF ROLL BELOW V1. ABORTED TAKEOFF. REMOVED AND REPLACED LEFT TORQUE G AUGE AS PER MM. OPS CHECKS GOOD. P/N ON: SEDL-OC2R, S/N ON: 961D, S/N OFF: 141. 2 L 7 2 4T 4 T RT A31SO E20NE 2001013100149 20010131 00149 2001 1 31 SWIA972286 4 20010118 A 3421 DISPLAY EMB 120 EMB120RT SO PWA 118 PW118 NE EADI FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 130G 120130 JUST AFTER ROTATION FIRST OFFICERS EADI FAILED. RETURNED TO SEA. INSTALLED SERVICEABLE RIGHT EADI. OPS CHECKS GOOD 34 -23-01. S/N ON: 893, S/N OFF: 2674. 2 L 7 2 4T 4 T RT A31SO E20NE 2001013100150 20010131 00150 SO 2001 1 31 SWIA972287 1 20010112 A 5350 TAIL CONE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FUSELAGE OUT OF POSITION A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 271YV 120271 ELEVATOR CONTROL BINDING IN MIDDLE OF THROW. FOUND ELEVATOR CONTACTING RIGHT SIDE OF TAIL CONE AT MID THROW. REPOSITIO NED AND SECURED TAIL CONE. CHECKS OK. 2 L 7 2 4T 4 T RT A31SO E20NE 2001013100152 20010131 00152 NM 2001 1 31 SCNA01317 1 20010116 A 5720 PLATE BOEING 727 727225 1384077 NM LT WING CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS DISCOVERED OUT OF LIMITS ON THE LEFT HAND WING FRONT SPAR LOWER FORWARD CH ORD PLATE, WS 360 TO WS 450. REMOVED CORROSION IAW B727 SRM 511006. REMOVED DAMAGED SECTION IAW B727 SRM 513002. FABR ICATED NEW CHORD FROM BAC 15201143 2024 T3511. TREATED AND PRIMED IAW B727 SRM 511002 AND MM 512002. INSTALLED IAW B72 7 SRM 513002. 2 L 7 3 4F A3WE 2001013100153 20010131 00153 NE 2001 1 31 C8GA20010001 2 20010117 A 7200 ENGINE BOEING 727 727214 138407R NM PWA JT8 JT8D15A 52051 NE NR 2 STALLED A C8GA O OTHER E R J VIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION DE DESCENT 1 SO 15 227JL 45315 35 20875 700741 ON FLT DAE232 FROM MROC TO KMIA EXPERIENCED NR 2 ENGINE STALL AT LOW ALTITUDE. ENG (S/N 700741) REPLACED WITH ENG (S/N 700748). 2 L 7 3 4F 4 F A3WE E2EA 2001013100154 20010131 00154 NM 2001 1 31 SCNA01010 1 20010119 A 2822 3823001 PUMP BOEING 727 7272J4 1384006 NM FUEL BOOST FAILED A SCNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 290SC 20764 DURING TAKEOFF ROTATION THE NUMBER TWO FUEL BOOST PUMP C/B TRIPPED, THE REMAINING C/B TRIPPED DURING CLIMB. THE NUMBER THREE FUEL PUMPS TRIPPED DURING FUEL DUMP. DUE TO INABILITY TO DUMP FUEL, A SMOOTH OVERWEIGHT LANDING OCCURRED AT MSP. (166,000 LB). CHANGED NUMBER TWO FORWARD BOOST PUMP, ALL SIX AFFECTED CIRCUIT BREAKERS, WIRING CHECK AND NUMBER THREE F ORWARD BOOST PUMP SHUTOFF VALVE CHANGE. ALSO INSPECTED AIRCRAFT DUE TO HARD LANDING, NO DAMAGE REVEALED. 2 L 7 3 4F RT A3WE 2001013100155 20010131 00155 WP 2001 1 31 MWEA010108 1 20010123 A 5310 591036749 DOOR FRAME DOUG DC9 DC914 3022034 WP FUSELAGE MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 500ME 45711 APB PLUG DOOR PAN REPAIR INTERFERES WITH DOOR OPERATION AND SEAL. REMOVED AND REPLACED DOOR FRAME. 2 L 7 2 4F A6WE 2001013100156 20010131 00156 WP 2001 1 31 MWEA010109 1 20010123 A 5320 59124921 PAN DOUG DC9 DC914 3022034 WP SERVICE DOOR MISINSTALLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 500ME 45711 GALLEY SERVICE DOOR JAMB REPAIR IMPROPERLY INSTALLED, STATION 200, NEXT TO BAYONET ROLLERS. FABRICATED AND INSTALLED DO UBLER REPAIR. 2 L 7 2 4F A6WE 2001013100157 20010131 00157 WP 2001 1 31 MWEA010110 1 20010123 A 5315 59101483 FLOORBEAM DOUG DC9 DC914 3022034 WP FUSELAGE CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 CENTER FLOOR SUPPORT IS CHAFING INTO FLOORBEAM AT STATION 484. FABRICATED AND INSTALLED FILLERS AND REPAIR ANGLES. 2 L 7 2 4F A6WE 2001013100158 20010131 00158 WP 2001 1 31 MWEA010111 1 20010123 A 5320 5912995504 PAN DOUG DC9 DC914 3022034 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 OVERWING EXIT FRAME HAS SEVERAL DEEP GOUGES ON FORWARD AND AFT LOWER CORNERS. REMOVED AND REPLACED JAMB PAN. 2 L 7 2 4F A6WE 2001013100159 20010131 00159 WP 2001 1 31 MWEA010112 1 20010123 A 5315 FASTENER DOUG DC9 DC914 3022034 WP FLOORBEAM MISSING A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 500ME 45711 CABIN FLOORBEAM UPPER ANGLE, STATION 160, AFT SIDE, HAS SIX UNFILLED FASTENER HOLES. FABRICATED AND INSTALLED SPLICE AN GLES. 2 L 7 2 4F A6WE 2001013100160 20010131 00160 WP 2001 1 31 MWEA010113 1 20010123 A 5311 39203121 FRAME DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 LEFT MAIN LANDING GEAR MAIN FRAME FORWARD OUTBOARD RADIUS CRACK NOW EXCEEDS 7 INCHES. LOCATED, DRILLED, AND INSTALLED R EPAIR ANGLE DOUBLERS. 2 L 7 2 4F A6WE 2001013100161 20010131 00161 2001 1 31 MWEA010114 4 20010123 A 2565 13621228 SLIDE DOUG DC9 DC914 3022034 WP TAIL CONE WILL NOT TEST A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 500ME 45711 THE TAIL CONE SLIDE DEPLOYMENT CHECK FAILED WHEN TAIL CONE WAS RELEASED, THE EVACUATION SLIDE COVER DID NOT RELEASE. BL ENDED CRACKED/TORN METAL FOUND AROUND GIRT BAR MOUNT HOLES AND FABRICATED AND INSTALLED REPAIR CATWALK DOUBLERS AND SHIM S. FABRICATED AND INSTALLED REPAIR DOUBLERS AND NUT PLATE DOUBLERS FOR IMPROPERLY LOCATED CLIPS. 2 L 7 2 4F A6WE 2001013100162 20010131 00162 WP 2001 1 31 CALA0100053 1 20010122 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND CABIN LT CENTER SEAT TRACK CORRODED AT FS 1032 - 1184. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F. 2 L 7 2 4F A6WE 2001013100163 20010131 00163 WP 2001 1 31 CALA0100054 1 20010122 A 5230 FITTING DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND A 3 INCH CRACK IN FORWARD CARGO DOOR FITTING I/B OF AFT HINGE. THE FITTING WAS REMOVED AND A NEW FITTI NG WAS INSTALLED IAW SRM 51-30-1, 51-30-2, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 2001013100164 20010131 00164 WP 2001 1 31 CALA0100055 1 20010123 A 5320 FLOOR SUPPORT DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13088 46850 INSPECTION FOUND I/B GALLEY NR 7 FLOORBOARD SUPPORT CORRODED AT STA Y = 1871, X = 30R. THE SUPPORT WAS REMOVED AND A NE W SUPPORT WAS INSTALLED IAW SRM 53-16-01. 2 L 7 3 4F A22WE 2001013100165 20010131 00165 WP 2001 1 31 CALA0100056 1 20010123 A 5320 FLOOR SUPPORT DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13088 46850 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA Y = 475, X = -19 TO +19. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR S UPPORT WAS INSTALLED IAW SRM 53-11-01. 2 L 7 3 4F A22WE 2001013100166 20010131 00166 WP 2001 1 31 CALA0100057 1 20010123 A 5320 FLOOR SUPPORT DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13088 46850 INSPECTION FOUND LAV D I/B FLOOR SUPPORT CORRODED AT STA Y = 840-899, X = 60R. THE SUPPORT WAS REMOVED AND A NEW ONE WA S INSTALLED IAW SRM 53-16-01. 2 L 7 3 4F A22WE 2001013100167 20010131 00167 WP 2001 1 31 CALA0100058 1 20010123 A 5320 FLOOR SUPPORT DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13088 46850 INSPECTION FOUND GALLEY NR 6 INBOARD FLOORBOARD SUPPORT CORRODED AT STA Y = 1887, X = 45L. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-11-01. 2 L 7 3 4F A22WE 2001013100168 20010131 00168 WP 2001 1 31 CALA0100059 1 20010123 A 5320 CHANNEL DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13088 46850 INSPECTION FOUNFD TOP HAT SECTION AT STA 401-459, X = 30L (GALLEY G1) CORRODED. A NEW SECTION WAS INSTALLED IAW SRM 53- 11-01. 2 L 7 3 4F A22WE 2001013100169 20010131 00169 WP 2001 1 31 CALA0100060 1 20010123 A 5320 FLOOR SUPPORT DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13088 46850 INSPECTION FOUND LAV C I/B FLOOR SUPPORT CORRODED AT STA Y = 840-899, X = 60L. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 53-13-01. 2 L 7 3 4F A22WE 2001013100170 20010131 00170 WP 2001 1 31 CALA0100061 1 20010123 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13088 46850 INSPECTION FOUND FLOORBEAM CORRODED AT STA 481. THE FLOORBEAM WAS REMOVED AND A NEW FLOORBEAM WAS INSTALLED IAW SRM 53- 11-01. 2 L 7 3 4F A22WE 2001013100171 20010131 00171 WP 2001 1 31 CALA0100062 1 20010123 A 5320 FLOOR SUPPORT DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13088 46850 INSPECTION FOUND NR 3 GALLEY LEFT O/B AND RIGHT O/B SUPPORT BEAMS CORRODED AT STA 475-535, X = +23 AND AT X = -23. THE SUPPORT BEAMS WERE REMOVED AND NEW SUPPORT BEAMS WERE INSTALLED IAW SRM 53-11-01. 2 L 7 3 4F A22WE 2001013100172 20010131 00172 WP 2001 1 31 CALA0100063 1 20010123 A 5320 FLOOR SUPPORT DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13088 46850 INSPECTION FOUND I/B CENTER FLOOR SUPPORT CORRODED AT STA 1887, X = -30L. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 53-16-01. 2 L 7 3 4F A22WE 2001013100173 20010131 00173 NM 2001 1 31 UPS01234726 1 20010102 A 5320 ANGLE BOEING 727 72722C 138400F NM FWD LAVATORY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE:C CK FWD LAV FLOOR INTERCOSTAL ANGLE HAS 2 CRACKS AT STA 320 RIGHT SIDE 20 INCHES FROM RIGHT HAND WALL. INSTALLED DOUBLER REPAIR, ACCOMPLISHED IN ACCORDANCE WITH SRM 51-40-2. REPLACED UPPER ANGLE IN ACCORDANCE WITH SRM 52- 30-2. 2 L 7 3 4F A3WE 2001013100175 20010131 00175 NM 2001 1 31 UPS01434689 1 20010106 A 5320 FITTING BOEING 747 747123F NM PAX DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, NR 3 LT DOORWAY FITTING NR 2 AND 4 CRACKED. REPLACED FITTINGS. 2 L 7 4 4F A20WE 2001013100176 20010131 00176 WP 2001 1 31 UPS01834701 1 20010102 A 5310 FITTING DOUG DC8 DC873F 302199F WP OVERWING EXIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:C1 BEAM FITTING ABOVE RT AFT O/W EXIT L14R HAS EXFOLIATION RUNNING ALONG FASTENER HOLES. REMOVED AND RE PLACED FITTING IAW DC8 SRM 51-1-20D 51-1-21 AND 51-3-0. 2 L 7 4 4F RT 4A25 2001013100177 20010131 00177 WP 2001 1 31 UPS01834702 1 20010115 A 5320 FITTING DOUG DC8 DC873F 302199F WP CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:C1 FWD CARGO PIT STA 320 L 34R - 35R FITTING IS CORRODED. REMOVED Z-FITTING, FAB SPLICE AND DRILLED NEW FITTING IAW SRM 53-2-0, ALODINED AND PRIMED IAW SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-21D. 2 L 7 4 4F RT 4A25 2001013100178 20010131 00178 WP 2001 1 31 UPS01834703 1 20010115 A 5313 LONGERON DOUG DC8 DC873F 302199F WP CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:C1 FWD PIT STA 385 LONG 31L HAS CORROSION FWD OF SPLICE. REMOVED PRODUCTION SPLICE IAW DC8 SRM 51-1-24, CLEANED AREA IAW DC8 SRM 51-1-8, LOCATED DRILLED PRODUCTION SPLICE IAW DC8 SRM 51-3-2, INSTALLED PRODUCTION SPLICE IAW DC8 SRM 21-1-20D. 2 L 7 4 4F RT 4A25 2001013100179 20010131 00179 WP 2001 1 31 UPS01834704 1 20010111 A 5320 FITTING DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:C1 STA 1265 LONGERON 35R LONGERON SPLICE CRACKED. REMOVED LONGERON SPLICE IAW DC8 SRM 51-1-20D, RECEIVE D NEW SPLICE P/N 3759258 -2N S/N TAG 0049957, LOCATED AND DRILLED NEW SPLICE IAW DC8 SRM 51-1 -24, INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001013100180 20010131 00180 WP 2001 1 31 UPS01834731 1 20010123 A 3350 5708458503 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHTS INOP ON PREFLIGHT SAFETY CK. REMOVED AND REPLACED EMERGENCY BATTERY PACK. O PS CK GOOD. 2 L 7 4 4F RT 4A25 2001013100181 20010131 00181 EA 2001 1 31 COMA0160149 1 20010120 A 3020 300013000002 VALVE CNDAIR CL600 CL6002B19 EA RT COWL MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 977CA 7157 RT COWL ANTI-ICE CAUTION MESSAGE. REPLACED THE COWL ANTI-ICE VALVE. 2 L 7 2 4F RT A21EA 2001013100182 20010131 00182 2001 1 31 COMA0160150 4 20010121 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 960CA 7117 STALL WARNING DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001013100183 20010131 00183 EA 2001 1 31 COMA0160151 1 20010121 A 2760 WARNING LIGHT CNDAIR CL600 CL6002B19 EA SPOILERS ILLUMINATED A COMA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 814CA 7387 FLIGHT SPOILERS CAUTION MESSAGE. COULD NOT DUPLICATE. NO FAULT CODES IN COMPUTER. 2 L 7 2 4F RT A21EA 2001013100184 20010131 00184 NE 2001 1 31 F3LA200100008 2 20010121 A 7200 ENGINE BOEING 737 7372L9 1384497 NM PWA JT8 JT8D17 52049 NE NR 1 VIBRATION A F3LA E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 NM 03 271FL 22734 688416 AIR TURNBACK. FLIGHT CREW REPORTED NR 1 ENGINE VIBRATION ON CLIMBOUT AT 20,000 FT. NR 1 ENGINE WAS SHUT DOWN AND AN EM ERGENCY WAS DECLARED. AIRCRAFT RETURNED TO PHX WITHOUT INCIDENT. THE NR 1 ENGINE IS IN THE PROCESS OF BEING REPLACED. AN ADDENDUM WILL BE ISSUED WHEN CAUSE OF FAILURE IS KNOWN. 2 L 7 2 4F 4 F RT A16WE E2EA 2001013100185 20010131 00185 2001 1 31 RAIA00101016 4 20010122 A 3130 7013348923 COMPUTER EMB 145 EMB145ER SO E/E BAY FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 803HK 533 145077 7603-STL- DURING TAXI OUT DATA ACQUISITIONING UNIT (DAU) 1 B FAIL EICAS MESSAGE. MAINTENANCE REMOVED AND REPLACED NR 1 DAU IAW EMB145 MAINTENANCE MANUAL. 2 L 7 2 4F RT T00011AT 2001013100186 20010131 00186 WP 2001 1 31 TWAA0101301 1 20010121 A 3350 58221 BATTERY PACK DOUG DC9 DC932 3022066 WP FWD CABIN DISCHARGED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 995Z 47027 THE CABIN EMERGENCY LIGHTS AT THE LEFT SIDE NUMBER 1 DOOR, RT SIDE NUMBER 1 DOOR, AND COCKPIT DOOR WERE ON WITH THE SWIT CH IN ARM POSITION. REPLACED THE BATTERY PACK. CHECK-C 1-2-01 STL. 2 L 7 2 4F A6WE 2001013100187 20010131 00187 WP 2001 1 31 TWAA0101302 1 20010121 A 3350 408822101 BATTERY DOUG DC9 DC983 3022083 WP FWD CABIN DISCHARGED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 9405T 53141 THE EGRESS LIGHTS AT ROWS 18 TO 22, AND THE EMERGENCY LIGHT AT THE FORWARD ENTRY DOOR, WERE INOPERATIVE. RECONNECTED WI RING AT ROW 22 FOR EGRESS LIGHTS, AND REPLACED BATTERIES FOR FWD ENTRY DOOR. CHECK-C 10-23-00 STL. 2 L 7 2 4F RT A6WE 2001013100188 20010131 00188 NM 2001 1 31 TWAA0101303 1 20010122 A 3350 LIGHT BOEING 767 76733AER 1385230 NM CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 637TW 25403 THE EGRESS LIGHTS WERE INOPERATIVE AT THE BASE OF THE RH AFT LAV WALL. REPAIRED WIRING ON SHIP SIDE OF THE RT AFT LAV E GRESS LIGHTS. CHECK-C 9-23-99. 2 L 7 2 4F RT A1NM 2001013100189 20010131 00189 NM 2001 1 31 TWAA0101304 1 20010122 A 3350 6100928 LENS BOEING 767 7673Q8 NM ROW 5 LOOSE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 635TW 28207 THE EGRESS LIGHT STRIP IN FIRST CLASS WAS REPORTED LOOSE. INSTALLED NEW BULB AND LENS COVER AT ROW 5, RT SIDE OF CABIN. CHECK-C 4-7-98. 2 L 7 2 4F RT A1NM 2001013100190 20010131 00190 WP 2001 1 31 MWEA010115 1 20010119 A 5210 995575099 INTERCOSTAL DOUG DC9 DC932 3022066 WP PAX DOOR BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 PASSENGER DOOR INTERCOSTAL BENT JUST AFT OF UPPER HINGE ATTACHMENT TO DOOR. MAINTENANCE REMOVED AND REPLACED INTERCOSTA L. 2 L 7 2 4F A6WE 2001013100191 20010131 00191 WP 2001 1 31 MWEA010116 1 20010118 A 5210 59100817 SKIN DOUG DC9 DC932 3022066 WP PAX DOOR DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 PASSENGER DOOR SKIN HAS A DENT ON MIDDLE UPPER SKIN. FABRICATED AND INSTALLED SKIN REPAIR. 2 L 7 2 4F A6WE 2001013100192 20010131 00192 WP 2001 1 31 MWEA010117 1 20010119 A 5210 591412157 PAN DOUG DC9 DC932 3022066 WP PAX DOOR GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 PASSENGER DOOR INNER PAN IS GOUGED DIRECTLY BEHIND HINGE ARM ASSEMBLY. FABRICATED AND INSTALLED DOOR PAN REPAIR DOUBLER . 2 L 7 2 4F A6WE 2001013100193 20010131 00193 WP 2001 1 31 MWEA010118 1 20010119 A 5320 995575043 STRAP DOUG DC9 DC932 3022066 WP PAX DOORWAY BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 INNER STRAP BENT UP AT STATION 170 BETWEEN NUMBER 3 AND 6 BEAM ON PASSENGER DOOR. MAINTENANCE REMOVED AND REPLACED STRA P. 2 L 7 2 4F A6WE 2001013100194 20010131 00194 EA 2001 1 31 COMA0160152 1 20010122 A 3222 16050107 STRUT CNDAIR CL600 CL6002B19 EA NLG DISCHARGED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 729CA 5530 33 7265 NLG DID NOT RETRACT. SERVICED THE NLG SHOCK STRUT. 2 L 7 2 4F RT A21EA 2001013100195 20010131 00195 GL 2001 1 31 C2XA011A012 2 20010105 A 7200 ENGINE EMB 145 EMB145LR SO ALLSN AE300 AE3007A GL NR 1 ENGINE MALFUNCTIONED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 16951 3688 145063 IAH - FLT 3997 - THE CREW REPORTED A BURNING SMELL ORIGINATING FROM THE NR 1 BLEED AIR SYSTEM. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE IAW AIRCRAFT INSPECTION PROGRAM TASK CARD 6271001, REV 49, REF EMB-145 AMM 71-00-00. THE NR 1 AIRCONDITIONING PACK WAS REMOVED FROM MEL AND THE AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2001013100196 20010131 00196 SO 2001 1 31 C2XA01CL002 1 20010110 A 3000 CS500060D4A RELAY EMB 145 EMB145 SO COCKPIT BURNED A C2XA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 27 13995 145295 CLE - FLT 3613 - THE CREW REPORTED SMOKE IN THE COCKPIT INBOUND TO CLEVELAND. A EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE TAT 2 CURRENT SENSOR (KO 494) RELAY AND RECEPTACLE BURNED . THE RELAY AND RECEPTACLE WERE REPLACED IAW EMB MM 20-21-00, 20-13-02 AND 30-33-01 AND 30-53-00. THE AIRCRAFT WAS REL EASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001013100219 20010131 00219 2001 1 31 USAABB01001 4 20010104 A 3460 FMC BOEING 767 767201 1385125 NM EE BAY FAILED A USAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 19 646US 23898 CLT - FLT 192 - FLIGHT RETURNED TO CLT DUE TO DUAL FMC FAILURE. (M) 2 L 7 2 4F RT A1NM 2001013100220 20010131 00220 WP 2001 1 31 USAAD01001 1 20010102 A 3350 MISC0639 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 967VJ 47375 IND - THE RIGHT NACELLE EMERGENCY LIGHT AND THE SERVICE DOOR EVACUATION SLIDE ACTIVATED EMERGENCY LIGHT WERE INOPERATIVE . MAINTENANCE REPLACED THE BATTERIES FOR THE RIGHT NACELLE AND SERVICE DOOR EMERGENCY LIGHTS. (M) 2 L 7 2 4F A6WE 2001013100221 20010131 00221 WP 2001 1 31 20010131SG003 1 20010102 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP SERVICE DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 967VJ 47375 IND - THE RIGHT NACELLE EMERGENCY LIGHT AND THE SERVICE DOOR EVACUATION SLIDE ACTIVATED EMERGENCY LIGHT WERE INOPERATIVE . MAINTENANCE REPLACED THE BATTERIES FOR THE RIGHT NACELLE AND SERVICE DOOR EMERGENCY LIGHTS. REF USAAD01001. (M) 2 L 7 2 4F A6WE 2001013100222 20010131 00222 WP 2001 1 31 USAAD01002 1 20010104 A 3350 MISC0639 BATTERY PACK DOUG DC9 DC931 3022065 WP CARGO BAY DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 991VJ 47310 IND - THE RIGHT NACELLE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE PROGRAMMED THE RIGHT NACELLE EMERGENCY LIGHT BATTE RY FOR REPLACEMENT DUE TO THE PART NOT IN STOCK. THE AIRCRAFT WAS RELEASED FOR FLIGHT UNDER MEL PROCEDURES. (M) 2 L 7 2 4F A6WE 2001013100223 20010131 00223 EU 2001 1 31 USAAF01001 1 20010104 A 3260 200444004 DAMPER FOKKER F28 F28MK0100 4990807 EU LT MLG MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 858US 17660 11291 BUF-PIT - FLT 356 - AFTER LANDING GEAR RETRACTION, RECEIVED LEFT MLG MESSAGE. PERFORMED QRH PROCEDURES AND RECYCLED THE LANDING GEAR. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT IN BUF. MAINTENANCE REPLACED THE LEFT MAIN GAER BU FFER DAMPER. CHECKS OK. (M) 2 L 7 2 4F RT 2001013100237 20010131 00237 WP 2001 1 31 AALA016001 1 20010104 A 2170 COALESCER BAG DOUG DC9 DC983 3022083 WP AC BAY DIRTY A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 21 879RA 53185 LAX - WHEN PACK CONTROL TEMP SELECTOR WAS MOVED TOWARD WARM, CABIN RAPIDLY FILLED WITH SMOKE. MAINTENANCE CHANGED COALE SCER BAGS, ACCOMPLISHED PACK BURN OUT, NO SMELL OR SMOKE IN CABIN. SJC- AT GATE SMELLED BURNED DUSTY SMELL WITH ONLY RI GHT PACK RUNNING, SWITCHED TO LEFT PACK AND SLOWLY CABIN FILLED WITH SMOKE AND SAME BURNT SMELL. MAINTENANCE FOUND TEMP SWITCHES IN FULL HOT. RETURNED TO NORMAL OPERATING RANGE. CHANGED COALEESCER BAGS AND CHANGED THE 130 DEGREES TEMP SE NSOR. PERFORMED OPS CHECK, NO LEAKS NOTED, NO SMOKE NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A6WE 2001013100238 20010131 00238 WP 2001 1 31 20010131SG004 1 20010104 A 2160 6712153130 SENSOR DOUG DC9 DC983 3022083 WP AC BAY MALFUNCTIONED A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 21 879RA 53185 LAX - WHEN PACK CONTROL TEMP SELECTOR WAS MOVED TOWARD WARM, CABIN RAPIDLY FILLED WITH SMOKE. MAINTENANCE CHANGED COALE SCER BAGS, ACCOMPLISHED PACK BURN OUT, NO SMELL OR SMOKE IN CABIN. SJC- AT GATE SMELLED BURNED DUSTY SMELL WITH ONLY RI GHT PACK RUNNING, SWITCHED TO LEFT PACK AND SLOWLY CABIN FILLED WITH SMOKE AND SAME BURNT SMELL. MAINTENANCE FOUND TEMP SWITCHES IN FULL HOT. RETURNED TO NORMAL OPERATING RANGE. CHANGED COALEESCER BAGS AND CHANGED THE 130 DEGREES TEMP SE NSOR. PERFORMED OPS CHECK, NO LEAKS NOTED, NO SMOKE NOTED. AIRCRAFT RETURNED TO SERVICE. REF AALA016001. 2 L 7 2 4F RT A6WE 2001020100095 20010201 00095 NE 2001 2 1 EIA2001001 2 20010101 A 7230 809402 CASE BOEING 747 747SR46 NM PWA JT9 JT9D7A 52054 NE NR 3 ENGINE WORN A EIAA O OTHER E VIBRATION/BUFFET CL CLIMB 1 NM 09 478EV 21033 AIRCRAFT VIBRATES EXCESSIVELY AFTER TAKEOFF AND DURING INTITIAL CLIMB-OUT. STOPS WHEN ABOVE 210 KCAS AND FLAPS UP. INI TIAL MAINTENANCE INSPECTION INDICATIONS OF SPOILER/AILERON CABLE SYSTEM BRACKET AND PULLEY DAMAGE. SUBSEQUENT MAINTENAN CE CHECK AND INSPECTION FOUND PRIMARY VIBRATION CAUSED BY NR 3 AND NR 4 ENGINE FAN CASE WEAR. REPLACED NR 3 AND NR 4 EN GINE FAN CASES. ALL CHECKS NORMAL ON ENGINE RUNS. REPLACED FROZEN RIGHT W/W WSIB TOP PULLEYS, RIGHT W/W AILERON CABLE AA TOP PULLEY AND LEFT W/W/ AA/AB PULLEYS (P/N''''S BACP30M3). REPAIRED AILERON PULLEY BRACKET PER ECRA 478-27-105-1 PA RT 1. AILERON RIG, OPERATIONAL CHECKS, AND RII INSPECTIONS ACCOMPLISHED. (M) 2 L 7 4 4F 4 F A20WE E20EA 2001020100096 20010201 00096 NE 2001 2 1 20010131SG006 2 20010101 A 7230 809788 CASE BOEING 747 747SR46 NM PWA JT9 JT9D7A 52054 NE NR 4 ENGINE WORN A EIAA O OTHER E VIBRATION/BUFFET CL CLIMB 1 NM 09 478EV 21033 AIRCRAFT VIBRATES EXCESSIVELY AFTER TAKEOFF AND DURING INTITIAL CLIMB-OUT. STOPS WHEN ABOVE 210 KCAS AND FLAPS UP. INI TIAL MAINTENANCE INSPECTION INDICATIONS OF SPOILER/AILERON CABLE SYSTEM BRACKET AND PULLEY DAMAGE. SUBSEQUENT MAINTENAN CE CHECK AND INSPECTION FOUND PRIMARY VIBRATION CAUSED BY NR 3 AND NR 4 ENGINE FAN CASE WEAR. REPLACED NR 3 AND NR 4 EN GINE FAN CASES. ALL CHECKS NORMAL ON ENGINE RUNS. REPLACED FROZEN RIGHT W/W WSIB TOP PULLEYS, RIGHT W/W AILERON CABLE AA TOP PULLEY AND LEFT W/W/ AA/AB PULLEYS (P/N''S BACP30M3). REPAIRED AILERON PULLEY BRACKET PER ECRA 478-27-105-1 PART 1. AILERON RIG, OPERATIONAL CHECKS, AND RII INSPECTIONS ACCOMPLISHED. REF EIA2001001. (M) 2 L 7 4 4F 4 F A20WE E20EA 2001090600320 20010906 00320 WP 2001 9 6 EIA2001003 1 20010104 A 3222 STRUT DOUG DC9 DC915F 3022037 WP NLG LEAKING A EIAA O OTHER K FLUID LOSS TO TAKEOFF 1 NM 09 915F 47061 DURING HIGH SPEED PHASE OF TAKEOFF ROLL, LOUD BANGING NOISE HEARD FROM NOSEGEAR. AFTER TAKEOFF AIRCRAFT REMAINED IN GRO UND MODE. INSPECTION AND SERVICED NOSE STRUT, NO DEFECTS/LEAKS NOTED. AT DEPARTURE, NLG SHOCK STRUT LEAKED FLUID AND D EFLATED. SERVICED NOSE STRUT PER ECRA 915-32-048-1 PART 1. (M) 2 L 7 2 4F A6WE 2001020100098 20010201 00098 NM 2001 2 1 EIA2001005 1 20010105 A 5311 FRAME BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 MZJ-EAC - DURING B-CHECK, FOUND FS 1265 L/H AROUND STRINGER 27 FRAME INBOARD CHORD CRACKED. REPAIRED CRACKED CHORD WITH ANGLE AND STRAP REPAIR PER ECRA 479-53-146-2 ON EAC W/O 70-1872-03-0028. (M) 2 L 7 4 4F A20WE 2001020200102 20010202 00102 EA 2001 2 2 COMA0160154 1 20010122 A 3350 2013A BATTERY CNDAIR CL600 CL6002B19 EA CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 779CA 4275 7306 TWO EXTERIOR EMERGENCY LIGHTS ARE INOP. REPLACED EMERGENCY BATTERY. 2 L 7 2 4F RT A21EA 2001020200103 20010202 00103 EA 2001 2 2 COMA0160142 1 20010122 A 5320 60034017595 ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 915CA 18100 7013 AFT J AT FS 280.00 IS CRACKED BETWEEN LBL 9 AND RBL 9. TRIMMED OUT DAMAGED AREA, FABED NEW SECTION OF J ANGLE. FABBED TWO SPLICE SECTIONS AND INSTALLED IAW WVAC EO 601R-53-2102. 2 L 7 2 4F RT A21EA 2001020200104 20010202 00104 EA 2001 2 2 COMA0160141 1 20010122 A 5320 60034017351 ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 915CA 18100 7013 FWD J ANGLE AT FS 280.00 BETWEEN LBL 9 AND RBL 9 IS CORRODED. REMOVED AND REPLACED FWD J ANGLE IAW WVAC EO 601R-53-2101 . 2 L 7 2 4F RT A21EA 2001020200105 20010202 00105 SO 2001 2 2 C2XA01IA037 1 20010119 A 3350 7287580501 LIGHT EMB 145 EMB145LR SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16954 145072 IAH - DURING POSTFLIGHT INSPECTION THE CREW REPORTED THAT TWO OF THE AISLE PATH EMERGENCY LIGHT STRIPS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTIONS OF LIGHT STRIP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. 2 L 7 2 4T RT T00011AT 2001020200106 20010202 00106 SO 2001 2 2 C2XA01IA038 1 20010122 A 3260 852701 PROXIMITY SWITCH EMB 145 EMB145LR SO LT MLG OUT OF ADJ A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 16951 145063 IAH - FLIGHT 3929, THE CREW REPORTED THAT ON CLIMB-OUT A LANDING GEAR AIR GROUND FAIL MESSAGE APPEARED ON THE EICAS. TH E CREW VERIFIED NORMAL OPERATION OF THE GEAR AND CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTE D THE LEFT HAND MAIN LANDING GEAR PROXIMITY SWITCH, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001020200107 20010202 00107 SO 2001 2 2 C2XA01IA039 1 20010120 A 3233 1959520006 ACTUATOR EMB 120 EMB120ER 3260203 SO RT MLG OUT OF ADJ A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 15730 120187 IAH - FLIGHT 3490, THE CREW REPORTED THAT THE RIGHT MAIN LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT CON TINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE RIGHT MAIN LANDING GEA R ACTUATOR TO BE OUT OF ADJUSTMENT. MAINTENANCE ADJUSTED THE AFFECTED ACTUATOR, AND THE AIRCRAFT WAS APPROVED FOR RETUR N TO SERVICE. 2 L 7 2 4T RT A31SO 2001022700066 20010227 00066 EU 2001 2 27 C2XA01IA040 1 20010121 A 2121 SM100D7 RELAY AEROSP ATR42 ATR42320 8680930 EU COCKPIT INOPERATIVE A C2XA D RETURN TO BLOCK J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 14834 193 IAH - FLIGHT 2990, THE CREW REPORTED A SMOKE DETECTION WARNING DURING TAXI. THE AIRCRAFT RETURNED TO THE GATE WITHOUT I NCIDENT WHERE MAINTENANCE PLACED THE NUMBER ONE PACK ON MEL 21-50-01 CONTROL NUMBER 004868, AND THE AIRCRAFT WAS APPROVE D FOR RETURN TO SERVICE. THE AIRCRAFT RETURNED TO IAH ON FLIGHT 3556 ON 01/23/01 WHERE MAINTENANCE REMOVED AND REPLACED THE AVIONICS VENT FAN RELAY, REMOVE MEL 21-50-01 CONTROL NR 004868, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE . 2 H 7 2 4T RT A53EU 2001020200108 20010202 00108 SO 2001 2 2 C2XA01IA041 1 20010121 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 13992 145284 IAH - FLIGHT 4277 FROM OMA TO IAH, THE CREW REPORTED A STRONG FUEL SMELL IN THE COCKPIT AND CABIN AFTER STARTING THE APU IN FLIGHT. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED AN OPERATION CK ON T HE APU, AND BOTH PACKS WITH NO DEFECTS NOTED. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001020200109 20010202 00109 SO 2001 2 2 C2XA01IA042 1 20010111 A 3350 7287580501 LIGHT EMB 145 EMB145LR SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13995 145295 CLE - FLIGHT 4015, DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE FIRST SECTION OF AISLE PATH EMERGENCY LIGHT S WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF LIGHT STRIP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001020200110 20010202 00110 WP 2001 2 2 ABXA0100017 1 20010119 A 2740 591096235 JACKSCREW DOUG DC9 DC941 302207N WP STABILIZER CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 34211 34211 47780 CORROSION WAS LOCATED ON THE STABILIZER JACKSCREW THREADS, RIGHT HAND SIDE. MAINTENANCE INSPECTED AND REPLACED THE JACK SCREW ASSY AND ACME NUT IAW DC-9 MM 27-40-01. 2 L 7 2 4F A6WE 2001020200111 20010202 00111 WP 2001 2 2 ABXA0100018 1 20010119 A 5530 5912175514N FAIRING DOUG DC9 DC941 302207N WP EMPENNAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 RIGHT UPPER HORSECOLLAR HORIZONTAL FAIRING FOUND WORN AND CORRODED. MAINTENANCE INSPECTED AND REPLACED THE RIGHT UPPER HORSECOLLAR FAIRING IAW DC-9 MM 55-10-00. 2 L 7 2 4F A6WE 2001020200112 20010202 00112 WP 2001 2 2 ABXA0100019 1 20010119 A 5530 591275513N FAIRING DOUG DC9 DC941 302207N WP EMPENNAGE DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 LEFT UPPER HORSECOLLAR WAS FOUND DELAMINATED. MAINTENANCE INSPECTED AND REPLACED THE HORSECOLLAR IAW DC-9 SRM 51-30-1. 2 L 7 2 4F A6WE 2001020200113 20010202 00113 WP 2001 2 2 ABXA0100020 1 20010119 A 5755 4925721502 FITTING DOUG DC9 DC941 302207N WP SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 INBOARD SPOILER TORSION BAR CENTER SUPPORT FITTING WAS FOUND CRACKED. MAINTENANCE INSPECTED AND REPLACED THE FITTING IA W DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2001020200114 20010202 00114 WP 2001 2 2 ABXA0100021 1 20010119 A 5330 5912864 SKIN DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 FUSELAGE SKIN WAS CRACKED FORWARD OF STATION 1072, BELOW LONGERON 14R. MAINTENANCE INSPECTED AND REPAIRED THE CRACKED A REA IAW ABX REA D953-39613. 2 L 7 2 4F A6WE 2001020200115 20010202 00115 WP 2001 2 2 ABXA0100022 1 20010119 A 5280 46517922 BRACKET DOUG DOUG DC8 DC863 302198A WP RT MLG DOOR BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AX 46126 RIGHT MAIN LANDING GEAR LOWER FOLLOW UP DOOR, AFT LOWER ATTACH BRACKET WAS FOUND BROKEN AT GEAR ATTACH POINT. MAINTENAN CE INSPECTED AND REPLACED THE ATTACH BRACKET IAW DC-8 MM. 2 L 7 4 4F 4A25 2001020200116 20010202 00116 NM 2001 2 2 AWXA0001251 1 20010119 A 3610 1074923 REGULATOR BOEING 737 7373G7 1384595 NM NR 2 ENGINE FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 322AW 35707 891 25400 LAS-DIVERTED FLIGHT- EN ROUTE FROM PHX TO GEG THE RT AIR CONDITIONING PACK FAILED A FL350, RT BLEED DUCT PRESSURE WENT T O 0 AND THE FLIGHT DIVERTED TO LAS. MAINTENANCE TROUBLESHOOTING FOUND THE BLEED DID NOT RESPOND TO THE SWITCH WHEN TURN ED ON. THE NR 2 ENGINE BLEED AIR REGULATOR WAS REPLACED THE THE BLEED AND RT PACK FUNCTIONED NORMALLY. 2 L 7 2 4F RT A16WE 2001020200117 20010202 00117 NM 2001 2 2 F3LA200100009 1 20010119 A 3350 6013211 CHARGER BOEING 737 7372Y5 1384554 NM ESCAPE SLIDE INOPERATIVE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 921WA 23039 L-1 DOOR SLIDE LIGHT INOPERATIVE. REPLACED L-1 DOOR SLIDE LIGHT ASSY, BATTERY AND CHARGER PER MM 33-51-71. 2 L 7 2 4U RT A16WE 2001020200118 20010202 00118 NM 2001 2 2 AWXA0001252 1 20010118 A 3230 D3231007000100 GEARBOX AIRBUS A319 A319132 NM ZONE 123 OUT OF ADJ A AWXA O OTHER J WARNING INDICATION DE DESCENT 1 WP 28 801AW 889 DURING POST MAINTENANCE FLIGHT TEST THE LANDING GEAR WAS EXTENDED USING MANUAL EXTENSION AND THE NOSE GEAR FAILED TO EXT END, LGCIU 1 & 2 FAULTS WERE PRESENT. THE GEAR WAS RESET AND GEAR WAS EXTENDED HYDRAULICALLY AND ALL GEAR EXTENDED NORM ALLY. MAINTENANCE TROUBLESHOT PER THE TSM. THE NLG VENT VALVE WAS REPLACED WHICH DID NOT HELP. THE FREE FALL CABLE RI GGING WAS CHECKED, WHICH CHECKED GOOD. THE ALTERNATE EXTENSION REDUCTION GEARBOX WAS REMOVED AND FOUND BOTH SHEAR PINS SHEARED. THE SHEAR PINS WERE REPLACED AND THE GEARBOX REINSTALLED. AFTER INSTALLATION, FOUND THE GEARBOX STOP BOLTS OU T OF ADJUSTMENT. AFTER REPLACEMENT OF THE SHEAR PINS AND ADJUSTMENT OF THE STOP BOLTS. 2 L 7 2 4F RT A28NM 2001020200119 20010202 00119 NM 2001 2 2 AWXA0001253 1 20010112 A 3350 900542 BATTERY PACK BOEING 737 737277 1384570 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 182AW 22649 DURING SCHEDULED INSPECTION FOUND EMERGENCY LIGHTS OUT IN THE FIRST CLASS CABIN. REPLACED POWER SUPPLY FOR THE FIRST CL ASS CABIN EMERGENCY LIGHTS. OPS CHECK OK. 2 L 7 2 4F RT A16WE 2001020200122 20010202 00122 NM 2001 2 2 EIA20001004 1 20010104 A 2510 SMOKE BOEING 747 747273C 1384896 NM COCKPIT CONSOLE DETECTED A EIAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 470EV 20653 AT FL340, EXPERIENCED SMOKE IN THE COCKPIT COMING FROM AFT END OF CENTER CONSOLE. ACCOMPLISHED FIRE/SMOKE PROCEDURES AN D RETURNED TO HNL. (M) 2 L 7 4 4F A20WE 2001020200126 20010202 00126 SO 2001 2 2 C2XA01IA002 1 20010102 A 5320 14525480003 SILL EMB 145 EMB145ER SO CARGO DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 IAH - DURING C-CHECK INSPECTION, THE CARGO DOOR SILL PLATE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED T HE AFFECTED SILL PLATE IAW EMB145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001020200127 20010202 00127 SO 2001 2 2 C2XAO1IA003 1 20010103 A 5553 14520736004 HINGE EMB 145 EMB145ER SO VERT STAB CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICAL STABILIZER FITTING HINGE SUPPORT FOR THE HORIZONTAL STAB WAS FOUND T O BE CORRODED IN THE PIN BORE. MAINTENANCE OVERSIZED THE BORE ON THE FITTING HINGE SUPPORT IAW CONTINENTAL EXPRESS ENGI NEERING CHANGE EC5510-01021, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001020200130 20010202 00130 NM 2001 2 2 MASA01008 1 20010110 A 3350 6519020 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SW 07 448YV 448 FLT 6284 - PHX-ASE - DURING TAXI OUT, THE CREW HAS THE FIRST TWO EMERGENCY LIGHTS INOPERATIVE. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE REPLACED THE LIGHT STRIP AND CHARGED THE BATTERIES. OPS CHECKED GOOD AND THE AIRCRAFT RETUR NED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 2001020200132 20010202 00132 NM 2001 2 2 GAIA01009OP 1 20010111 A 3242 211473 BRAKE BOEING 727 7272J0 138407E NM RT MLG FIRE A GAIA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 SW 07 281KH 21105 FLT 718 - TOL-ELP - AFTER LANDING AND COMING TO REST AT THE PARKING SPOT AT ELP, THE RIGHT GEAR BRAKES CAUGHT FIRE. GRO UND CREWS IMMEDIATELY EXTINGUISHED THE BRAKES FIRES. NR 1 BRAKE OVERTEMPED BUT DID NOT CATCH ON FIRE. APPROXIMATELY 20 MINUTES LATER, NR 1, NR 3, AND NR 4 TIRES THERMAL PROTECTION PLUGS BLEW. NO OTHER DIFFICULTIES OCCURRED. AFTER A SIGN IFICANT COOL DOWN PERIOD, THE TIRES AND BRAKES WERE REMOVED AND ASSOCIATED GEAR COMPONENTS WERE INSPECTED PER CONSIDERAT ION IN GMM CHAPTER 14, PAGE 4. NO OTHER DEFECTS WERE NOTED. REPLACED ALL WHEELS AND BRAKES. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2001020200133 20010202 00133 NM 2001 2 2 GAIA01088OP 1 20010110 A 3230 656021132 ACCESSORY UNIT BOEING 727 727251 138408H NM EE BAY MALFUNCTIONED A GAIA K NONE J WARNING INDICATION AP APPROACH 1 SW 07 279US 21158 FLT 708 - OKC-PHX - DURING APPROACH TO PHX, THE CREW NOTED ON GEAR EXTENSION THREE RED LIGHTS AND THREE GREEN LIGHTS ILL UMINATED. THE LANDING GEAR WAS RECYCLED AND ONLY THE GREEN LIGHTS ILLUMINATED. THE AIRCRAFT CONTINUED ITS APPROACH AND LANDED SAFELY AT PHX WITHOUT ANY FURTHER DIFFICULTIES. REMOVED, REPLACED AND TESTED LANDING GEAR ACCESSORY UNT IAW BOE ING MM. OPERATIONALLY CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001020200134 20010202 00134 NM 2001 2 2 GAIA01005OP 1 20010106 A 2750 SELECTOR KNOB BOEING 727 727223 1384074 NM COCKPIT BINDING A GAIA K NONE O OTHER CL CLIMB 1 SW 07 6838 20191 FLT 3864 - FWA-EWR - ON CLIMB-OUT, THE FLAP SELECTOR WAS STIFF AND INITIALLY WOULD NOT SELECT FLAPS TWO DEGREES. WORKED OK WITH SOME FORCE. THE AIRCRAFT CONTINUED TO EWR AND LANDED WITHOUT ANY FURTHER DIFFICULTIES. CHECKED FLAPS AND SLAT S FOR CONDITION AND SECURITY. NO DEFECTS WERE NOTED. LUBRICATED JACKSCREWS AND FOLLOW UP MECHANISMS. OPERATION NORMAL THROUGH SEVERAL CYCLE OPERATIONS ON THE GROUND. FOUND THE FLAP AND SLAT SYSTEM TO OPERATE NORMAL. THE AIRCRAFT WAS RE TURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001020200135 20010202 00135 NM 2001 2 2 GAIA01002OP 1 20010104 A 3350 SOCKET BOEING 727 727251 138408H NM L1 DOOR CORRODED A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 279US 21158 DURING NON-ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT THE L1 DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. CLEANED CORROS ION FROM LIGHT SOCKET PINS AND CLEANED SOCKET RECEPTACLE. OPERATIONALLY CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERV ICE. (M) 2 L 7 3 4F A3WE 2001020200136 20010202 00136 NM 2001 2 2 GAIA01001 1 20010103 A 3350 1065192 LIGHT BOEING 727 727232 1384082 NM L1 DOOR INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77780 20635 BOS - MAIN ENTRY EMERGENCY EXIT LIGHT WILL NOT TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY. OPS CHECK GOOD ON GROUND. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001020200168 20010202 00168 EU 2001 2 2 SIMA0032 1 20010103 A 3350 8GB22542405 LIGHT BOLKMS 117 BK117B1 5626012 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 214AE 7206 DFW - FLT 3868 - FLOOR PROXIMITY LIGHT AT SEAT 3BC IS INOPERATIVE. PUT ON MEL AT THIS TIME. MAINTENANCE REPLACED BULB AT SEAT 3BC. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 1 G 7 2 3U H13EU 2001020200169 20010202 00169 EU 2001 2 2 SIMA0033 1 20010103 A 3350 BE1317 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 238AE 340B238 JFK - FLT 5198 - OVERHEAD EMERGENCY LIGHT AT SEAT 3C IS INOPERATIVE. PUT ON MEL AT THIS TIME. REMOVED AND REPLACED BUL B AT SEAT 3C IAW AMM 33-50-00. OPS CHECK GOOD. RESTORED MEL. (M) 2 L 7 2 4T RT A52EU 2001020200170 20010202 00170 EU 2001 2 2 SIMA0034 1 20010103 A 3350 1317 LIGHT BOLKMS 117 BK117B1 5626012 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 214AE 7206 DFW - FLT 3868 - OVERHEAD EMERGENCY LIGHT AT SEAT 14A IS INOPERATIVE. PUT ON MEL AT THIS TIME. MAINTENANCE REPLACED BU LB AT SEAT 14A. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 1 G 7 2 3U H13EU 2001020200171 20010202 00171 EU 2001 2 2 SIMA00310 1 20010103 A 3350 66363 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST UK UNKNOWN 1 SW 21 394AE 340B394 DFW - FLT 3415 - EMERGENCY EXIT FLOOR LIGHTING AT ROW 9A IS INOPERATIVE. MAINTENANCE REPLACED FLOOR LIGHTING STRIP AT R OW 9A. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001020200172 20010202 00172 EU 2001 2 2 SIMA0071 1 20010107 A 3320 6510732 BALLAST SAAB SF340 340B 7860101 EU CABIN MALFUNCTIONED A SIMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 358RZ 340B358 BOS - FLT 5122 - FLIGHT ATTENDANT NOTICED SMOKE IN CABIN SMELLS LIKE ELECTRIAL FIRE OR BURNING PLASTIC. REMOVED AND INS TALLED BALLAST OVER 9A IAW SAAB AMM CH 33-21-00. OPS CHECK GOOD AT THIS TIME. NO DEFECTS NOTED AT THIS TIME. (M) 2 L 7 2 4T RT A52EU 2001020200173 20010202 00173 EU 2001 2 2 SIMA0073 1 20010107 A 2611 SMOKE WARNING SAAB SF340 340B 7860101 EU AVIONICS ACTIVATED A SIMA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 21 340RC 340B340 BOS - FLT 4608 - AVIONICS SMOKE WARNING ILLUMINATED DURING TAXI IN BOS. RETURNED TO GATE AND EVACUATED AIRCRAFT. MEL 2 6-3 AML PAGE 1293877. (M) 2 L 7 2 4T RT A52EU 2001020200174 20010202 00174 EU 2001 2 2 SIMA0099 1 20010109 A 3350 MS274061 SWITCH SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 394AE 340B394 SGF - FLT 3617 - FLIGHT ATTENDANT ARMED LIGHT SWITCH INTERMITTENT, SGF MAINTENANCE WENT AOG FOR BULB NO FIX. FERRIED AI RCRAFT TO DFW. REMOVED AND REPLACED SWITCH IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001020200175 20010202 00175 SO 2001 2 2 SIMA0093 1 20010109 A 2611 FD5765A2 SMOKE DETECTOR EMB 135 EMB135ER 3260203 SO LAVATORY MALFUNCTIONED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 700LE 145156 ORD - FLT 4127 - LAVATORY SMOKE INDICATION CAME ON DURING CLIMB-OUT. REMOVED AND REPLACED LAV SMOKE DETECTOR IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4F RT T00011AT 2001020200176 20010202 00176 SO 2001 2 2 SIMA0091 1 20010109 A 2611 FDS765A2 SMOKE DETECTOR EMB 135 EMB135ER 3260203 SO LAVATORY MALFUNCTIONED A SIMA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SW 21 700LE 145156 ORD - FLT 4433 - CREW REPORTED THAT AFTER TAKEOFF LAV SMOKE WARNING CAME ON EICAS. CREW FOLLOWED AOM PROCEDURE AND RETU RNED TO ORD. LAV SMOKE WARNING LIGHT WENT OUT DURING APPROACH, BUT NOTED NO BURNING SMELL IN LAV AREA. REMOVED AND REP LACED LAV SMOKE DETECTOR IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4F RT T00011AT 2001020200178 20010202 00178 SO 2001 2 2 SIMA0054 1 20010105 A 2740 3621001007 CONTROL UNIT EMB 135 EMB135LR SO HORIZ STAB FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 707EB 145195 BOS - FLT 4746 - PITCH TRIM 1 FAILED IN FLIGHT, WARNING ON EICAS. RETURNED TO BOS FOR MAINTENANCE. REMOVED AND REPLACE D HORIZONTAL STABILIZER CONTROL UNIT IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4F RT TOOO11AT 2001020500001 20010205 00001 SO 2001 2 5 COMA0110017 1 20010112 A 5310 12027289501 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 267CA 21508 120259 THE AIRCRAFT HAS CORROSION PAST THE LIMIT ON THE FLOORBEAM BUTT STRAP UNDER THE FLOOR PANEL, LOCATED AT FRAME 13A. THE FLOORBEAM BUTT STRAP WAS REPLACED IN ACCORDANCE WITH AERODESIGN REPORT NR 1671-2. 2 L 7 2 4T RT A31SO 2001020500002 20010205 00002 SO 2001 2 5 COMA0110018 1 20010112 A 5310 12027289501 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 267CA 21508 120259 THE AIRCRAFT HAS CORROSION PAST THE LIMIT ON THE FLOORBEAM BUTT STRAP UNDER THE FLOOR PANEL, LOCATED AT FRAME 13A. THE FLOORBEAM BUTT STRAP WAS REPLACED IN ACCORDANCE WITH AERODESIGN REPORT NR 1671-2. 2 L 7 2 4T RT A31SO 2001020500003 20010205 00003 SO 2001 2 5 COMA0110019 1 20010112 A 5311 12022616001 FRAME EMB 120 EMB120RT SO FUSELAGE NICKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 267CA 21508 120259 THE AIRCRAFT''S FRAME 46A HAS A NICK IN THE UPPER FRAME FLANGE AT A PREVIOUSLY INSTALLED ANGLE. THE FRAME WAS REPAIRED BY REMOVING THE OLD ANGLE, DRESSING AND BLENDING THE NICK AND INSTALLING A SERVICEABLE ANGLE IN ACCORDANCE WITH AERODESI GN REPORT NR 2400-4. 2 L 7 2 4T RT A31SO 2001020500004 20010205 00004 SO 2001 2 5 COMA0110021 1 20010112 A 5320 12035891001 SUPPORT BRACKET EMB 120 EMB120RT SO FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 267CA 21508 120259 A SKIN SUPPORT FOR FRAME 13A IS CRACKED. THE REPAIR IS TO INSTALL A DOUBLER IN ACCORDANCE WITH AERODESIGN REPORT NR 365 3-1. 2 L 7 2 4T RT A31SO 2001020500005 20010205 00005 SO 2001 2 5 COMA0110022 1 20010112 A 5330 12019737003 SKIN EMB 120 EMB120RT SO FUSELAGE GOUGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 267CA 21508 120259 THE AIRCRAFT SKIN BELOW THE LAVATORY DUMP VALVE DOUBLER IS GOUGED. THE DAMAGE WAS REPAIRED BY INSTALLING AN INTERNAL PA TCH (DOUBLER) IN ACCORDANCE WITH EMBRAER FAX SST-1403/003. 2 L 7 2 4T RT A31SO 2001022000273 20010220 00273 NE 2001 2 20 01FDEA00042 2 20010124 A 7250 TURBINE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE NR 1 ENGINE DAMAGED A FDEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 25 616FE 48747 702349 ON T/O, NR 1 ENG HAD SEVERE VIBRATION AND EVM TURBINE INDICATIONS. NO REDUCTION WITH REDUCED POWER, SECURED NR 1 ENGINE AND RETURNED TO PEK. MX FOUND METAL IN TAILPIPE AND LAST STAGE TURBINE SEVERELY DAMAGED. *S/D* REMOVED AND REPLACED NR 1 ENG PER WORK CARD MD11 71T07 C1. COWLING OPEN AND CLOSE PERF PER MM 7-13-00. 2 L 7 3 4F 4 F RT A22WE E31N3 2001020500012 20010205 00012 NM 2001 2 5 2001UALA00009 1 20010108 A 2822 91318506 CONTACTOR 3823002 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUEL BOOST FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 7460U 21914 ALL NR 2 FUEL BOOST PUMP TANK CIRCUIT BREAKERS POPPED DURING CRUISE. AIRCRAFT RETURNED TO DEN. *S/D* SPECIFIC CAUSE COULD NOT BE DETERMINED. REPLACED NR 2 RT AFT BOOST PUMP, AND NR 3 ESSENTIAL POWER CONTACTOR R110. 2 L 7 3 4F 4 F A3WE E2EA 2001020500013 20010205 00013 NM 2001 2 5 2001UALA00010 1 20010108 A 3260 189915 DOWNLOCK SENSOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT MLG FAILED A UALA O OTHER N FALSE WARNING LD LANDING 1 WP 29 7289U 21567 AIRCRAFT EXPERIENCED AN AMBER ALERT LANDING DUE TO RIGHT GEAR RED LIGHT LOCK DOWN INDICATION. *S/D* FOUND RIGHT MAIN G EAR DOWNLOCK SENSOR BAD. REPLACED SENSOR. OPS CHECK OK. 2 L 7 3 4F 4 F A3WE E2EA 2001020500015 20010205 00015 NM 2001 2 5 2001UALA00017 1 20010108 A 5315 141W8519 FLOORBEAM BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 784UA 17301 0 26951 THE STA 246 FLOORBEAM MID CHORD WAS CRACKED AT LBL 38. THE CRACK IS IN THE CENTER FLANGE. *S/D* CRACKED MID CHORD REP AIRED PER SRM 53-10-51, REPAIR 2, FIG 203. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001020500020 20010205 00020 NM 2001 2 5 2001UALA00012 1 20010103 A 2822 PUMP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 FUEL BOOST FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 7453U 21907 DURING CRUISE, THE NR 1 TANK FUEL BOOST PUMP FAILED. AIRCRAFT DIVERTED TO DSM. *S/D* RAN NR 1 AFT FUEL BOOST PUMP TO RUN APU FOR APPROXIMATELY .5 HR, RAN NR 1 ENGINE FOR 20 MINUTES. BOOST PUMP OPERATED NORMALLY. 2 L 7 3 4F 4 F A3WE E2EA 2001020500044 20010205 00044 NM 2001 2 5 UPS01234755 1 20010102 A 5312 PRESSURE PANEL BOEING 727 72722C 138400F NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C CK, NOSE LANDING GEAR WHEEL WELL SIDEWALL RIGHT BS 290 TO LWR HAS CRACK INDICATION MIGRATING FROM PREV IOUS REPAIR ABOUT 1 INCH LONG. INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH SRM 51-40-2. 2 L 7 3 4F A3WE 2001020500045 20010205 00045 NM 2001 2 5 UPS01234759 1 20010102 A 5312 PRESSURE PANEL BOEING 727 72722C 138400F NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C CK, NLG W/W RIGHT SIDEWALL BS272 LWR OF AFT ACCESS DOOR CRACK INDICATION RUNNING BETWEEN FASTENER ROW , 1.5 INCH LONG. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH SRM 51-40-2. 2 L 7 3 4F A3WE 2001020500048 20010205 00048 WP 2001 2 5 TWAA0101108 1 20010111 A 5347 GALLEY TRACK DOUG DC9 DC983 3022083 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT IN THE FWD CABIN, LIGHT CORROSION WAS ON GALLEY TIE DOWN ANGLE APPROX STA 210, RBL 10, AT NUT PLATE RIVETS. PART REMOVED AND REPLACED WITH NEW PART PER SPM 6-70-01. PAINTED WHITE PER SRM 51-10-03. INSTALLED NEW FASTE NERS PER SRM 51-30-02. SEALED AREA PER SRM 51-20-0 PAGE 2. 2 L 7 2 4F RT A6WE 2001020500049 20010205 00049 EU 2001 2 5 MALA010128 1 20010121 A 2750 7DE CONNECTOR SAAB SF340 SF340A 7850100 EU FLAP INDICATOR DAMAGED A MALA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 15 99XJ 099 IN FLIGHT NOTICED LT FLAP INDICATOR BETWEEN 7-15 DEGREE WITH FLAP HANDLE AT 0 DEGREES, RAN ORH AND DID NOT NOTICE YAW. ON APPROACH INTO DTW WHEN SELECTING FLAPS, FLAPS REMAINED AT 0 DEGREES. MAINTENANCE REPLACED CANNON PLUG 7-DE, AT FLAP IND TRASNIMTTER IAW SF 340MM, ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2001020500051 20010205 00051 WP 2001 2 5 ARWA0010101 1 20010118 A 2910 HYDRAULIC LINE DOUG DC8 DC8F54 3021926 WP NR 2 ENGINE LEAKING A ARWA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 19 57FB 45669 DURING DESCENT AT THE INITIAL PHASE OF THE APPROACH LOSS HYDRAULIC FLUID AND PRESSURE. INITIATED PHASE I AND ABNORMAL I AW PROCEDURES. AFTER CLEARING THE ACTIVE DURING TAXI, LOSS HYDRAULIC BRAKE PRESSURE. AIR BRAKE PRESSURE APPLIED. FOUN D PRESSURE LINE TO ENGINE NR 2 HYDRAULIC PUMP LEAKING. REMOVED AND REPLACED PRESSURE LINE; SYSTEM CHECK NORMAL IAW 29-1 0-12. SERVICED AIR BRAKE BOTTLE AND BLED HYDRAULIC BRAKE SYSTEM IAW MM 32-18-0 AND 29-0. SYSTEM OPERATION NORMAL, NO L EAKS NOTED. 2 L 7 4 4F 4A25 2001020500052 20010205 00052 2001 2 5 MALA010132 4 20010123 A 3420 6226342022 DISPLAY SAAB SF340 SF340A 7850100 EU ADI BROKEN A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 103XJ 340A103 F/O SIDE ADI INOP. BREAKER OUT. RETURNED TO MSP. MAINTENANCE REMOVED AND REPLACED NR 2 EADI P/N 622-6342-022, S/N ON 6 31, S/N OFF 5045. NR 2 EADI/EFIS SYSTEM OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2001020500053 20010205 00053 NE 2001 2 5 MALA010129 2 20010118 A 7510 5056T88P01 VALVE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE ANTI ICE SYSTEM MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 15 68XJ 068 LT AIR VALVE LIGHT CAME ON AFTER TAKEOFF. CYCLED ANTI-ICE ON AND AIR VALVE LIGHT ON LT SIDE ILLUMINATED. AIR TURNBACK TO DTW. MAINTENANCE REPLACED LT GARRET VALVE P/N 5056T88P01, S/N OFF AEX10253, S/N ON AEX10424, IAW CT7-MM. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2001020500054 20010205 00054 EU 2001 2 5 MALA010130 1 20010119 A 3060 666000219 BRUSH BLOCK SAAB SF340 SF340A 7850100 EU RT PROPELLER MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 68XJ 068 RT PROP HEAT CAUTION LIGHT COMES ON AFTER ABOUT 2 MINUTES INNORM MODE. BLUE ADVISORY LIGHT ALSO GOES OUT. RETURNED TO GATE. MAINTENANCE INSPECTED PROP LEADS, ALL CHECKS GOOD. REPLACED BRUSH BLOCK ASSEMBLY (FOUND BRUSHES NOT MAKING CONTA CT WITH PROP/SKIPPING) P/N 666000219, AND GROUND RAN AIRCRAFT. ALL CHECKS GOOD OF RT PROP DE-ICE. 2 L 7 2 4T RT A52EU 2001020500055 20010205 00055 EU 2001 2 5 MALA010131 1 20010122 A 2450 19GA RELAY SAAB SF340 SF340A 7850100 EU ELECTRICAL SYS DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 112XJ 340A112 FI STOP OPEN LIGHT CAME ON AFTER GEAR RETRACT ON CLIMBOUT. AIR RETURN TO MSP. MAINTENANCE CYCLED AC POWER, AMBER FI LI GHT WENT OUT. REMOVED AND REPLACED RELAYS 20GA AND 19GA. PERFORMED FI SYSTEM OPS CHECK, PER AMM 76-10-60. OPS CHECK G OOD. 2 L 7 2 4T RT A52EU 2001020500062 20010205 00062 WP 2001 2 5 TWAA0101501 1 20010123 A 4990 APU DOUG DC9 DC983 3022083 WP APU BAY CONTAMINATED A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CE 05 9302B 49528 DURING SHORT FINAL CREW NOTICED SMELL OF SMOKE. AFTER LANDING SMELL WENT AWAY. AFTER EXTENSIVE CHECKS CAUSE NOT DETERM INED. DID CLEAN SOME OIL FROM APU INLET SO APU OIL MAY HAVE BEEN OVERSERVICED. CHECK-C 10-16-00 STL. 2 L 7 2 4F RT A6WE 2001020500063 20010205 00063 NE 2001 2 5 TWAA0101502 2 20010123 A 7230 COMPRESSOR BOEING 757 757231 1384950 NM PWA 2037 PW2037 NE LT ENGINE FAILED A TWAA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 CE 05 718TW 28486 4938 ON TAKEOFF THE LEFT ENGINE SURGED AND CREW SECURED THE ENGINE. FLIGHT RETURNED TO STL. SUSPECT FAILURE WAS IN 10TH STA GE OF COMPRESSOR. REPLACED THE ENGINE. CHECK-C 11-1-00 LAX. 2 L 7 2 4F 4 F RT A2NM E17NE 2001020500064 20010205 00064 WP 2001 2 5 TWAA0101504 1 20010121 A 5313 STRINGER DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT FOUND CORROSION ON STRINGER 23L, STA 1021 TO 1041, AFT CARGO COMPT. INSTALLED NEW SECTION OF STRIN GER AND 2 SPLICES PER SRM 53-02, FIG 18 SHEET 4. 2 L 7 2 4F RT A6WE 2001020500065 20010205 00065 WP 2001 2 5 TWAA0101505 1 20010121 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT FLOOR MEMBRANE WAS CRACKED BETWEEN STA 1298 AND 1309, STRINGER 18R. REPAIRED MEMBRANE PER 53-05-96 AND SPM 6-70-01 PAGE 1, 2, AND 3. 2 L 7 2 4F RT A6WE 2001020500066 20010205 00066 WP 2001 2 5 TWAA0101506 1 20010122 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT FOUND CORROSION ON MEMBRANE AT STA 1174 TO 1212, RBL 58 INCHES. REMOVED CORROSION PER SRM 51-10-2. REPLACED MEMBRANE PER SRM 51-30-1, 51-30-02, AND 51-30-5. 2 L 7 2 4F RT A6WE 2001020500067 20010205 00067 WP 2001 2 5 TWAA0101507 1 20010125 A 5313 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 DURING CHECK-C MAINT LONGERON 3R AT STA 658 WAS CRACKED AT LOWER FLANGE .25 INCH LONG. REPAIRED PER SRM 53-02 AND DRAWI NG SRO 9530128. 2 L 7 2 4F A6WE 2001020500068 20010205 00068 NM 2001 2 5 QXEA0100009 1 20010104 A 5210 STOP DHAV DHC8 DHC8202 2809007 NM PAX DOOR LACK OF LUBE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 828PH 526 PDX - THE MAIN CABIN DOOR WAS REPORTED DIFFICULT TO OPEN. CLEANED AND LUBED MAIN CABIN DOOR STOPS AND HANDLE OPERATING MECHANISM. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2001020500069 20010205 00069 NM 2001 2 5 QXEA0100013 1 20010109 A 2120 UNKNOWN DHAV DHC8 DHC8202 2809007 NM CABIN ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 345PH 476 PSC - A STRONG FISH ODOR WAS REPORTED IN THE FLIGHT COMPARTMENT. INSPECTED INVERTERS VISUALLY AND CHECKED FOR ODOR, NON E NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2001020500070 20010205 00070 NM 2001 2 5 QXEA0100031 1 20010112 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- RIGHT HAND INBOARD SEAT TRACK HAS PITTED AREA AT STATION X519.000. REPAIRED IAW HORIZON AIR EA 9-53-588 AND DHC-8 RD8-53-1339. 2 H 7 2 4T RT A13NM 2001020500071 20010205 00071 NM 2001 2 5 QXEA0100032 1 20010114 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- RIGHT HAND INBOARD SEAT TRACK HAS MISSING MATERIAL AND GOUGED UPAT STATION X434.500. REPAIRED IAW DHC-8 RD8-53-133 9. 2 H 7 2 4T RT A13NM 2001020500072 20010205 00072 NM 2001 2 5 QXEA0100033 1 20010112 A 5340 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- RIGHT HAND INBOARD SEAT TRACK HAS PITTING ON TOP SIDE AT STATION X300.400. REPAIRED IAW DHC-8 RD8-53-1339 AND HORI ZON AIR EA 9-53-588. 2 H 7 2 4T RT A13NM 2001020500073 20010205 00073 NM 2001 2 5 QXEA0100034 1 20010110 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- RIGHT HAND INBOARD SEAT TRACK HAS PITTING ON TOP SIDE AT STATION X264.100. REPAIRED IAW DHC-8 RD8-53-1339. 2 H 7 2 4T RT A13NM 2001020500074 20010205 00074 NM 2001 2 5 QXEA0100035 1 20010113 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX-RIGHT HAND OUTBOARD SEAT TRACK HAS PITTING ON TOP SIDE AT STATION X264.100. REPAIRED IAW DHC-8 RD8-53-1342 AND SRM 51-20-16, AND HORIZON AIR EA 9-53-587. 2 H 7 2 4T RT A13NM 2001020500075 20010205 00075 NM 2001 2 5 QXEA0100036 1 20010113 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- RIGHT HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION ON TOP SIDE AT STATION X280.400. REPAIRED IAW HORIZON AIR EA 9- 53-587 AND DHC-8 RD8-53-1342 AND SRM 51-20-13. 2 H 7 2 4T RT A13NM 2001020500076 20010205 00076 NM 2001 2 5 QXEA0100037 1 20010109 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- RIGHT HAND OUTBOARD SEAT TRACK HAS PITTING AT STATION X310.350. REPAIRED IAW DHC-8 SRM 51-20-41 AND RD8-53-1342. 2 H 7 2 4T RT A13NM 2001020500077 20010205 00077 NM 2001 2 5 QXEA0100038 1 20010113 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- RIGHT HAND OUTBOARD SEAT TRACK HAS RAISED MATERIAL AT STATION X361.050. REPAIRED IAW HORIZON AIR EA 9-53-587 AND D HC-8 RD8-53-1342 AND SRM 51-20-13. 2 H 7 2 4T RT A13NM 2001020500078 20010205 00078 NM 2001 2 5 QXEA0100039 1 20010113 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- RIGHT HAND OUTBOARD SEAT TRACK HAS RAISED MATERIAL AT STATION X280.400. REPAIRED IAW HORIZON AIR EA 9-53-587 AND D HC-8 RD8-53-1342, AND SRM 51-20-16. 2 H 7 2 4T RT A13NM 2001020500079 20010205 00079 NM 2001 2 5 QXEA0100040 1 20010109 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- RIGHT HAND OUTBOARD SEAT TRACK HAS PITTING AT STATION X490.500. REPAIRED IAW DHC-8 SRM 51-20-41 AND RD8-53-1342. 2 H 7 2 4T RT A13NM 2001020500080 20010205 00080 NM 2001 2 5 QXEA0100042 1 20010117 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- LEFT HAND INBOARD SEAT TRACK HAS PAINT MISSING THROUGH OUT THE TRACK. REPAIRED IAW HORIZON AIR EA 9-53-592 AND DHC -8 SRM 51-20-16, PAGES 1-4. 2 H 7 2 4T RT A13NM 2001020500081 20010205 00081 EU 2001 2 5 MALA010134 1 20010115 A 5310 STRUCTURE SAAB SF340 340B 7860101 EU RT CABIN DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 456XJ 456 FOUND DURING C-CHECK, DENTS ON RT SIDE OF CABIN JUST AFT OF FS 339 AT SL 1616 AND SL 1617. REFER TO CELSIUS W/O 19238, TASK 2504, EO S53056 AND SAAB STATEMENT 72SDS1775. MAINTENANCE CUT OUT DAMAGE ON LOWER DENT AND STRAIGHTENED OTHERS, FA BRICATED REPAIR DOUBLER/TRIPLER PER SRM 51-20-42/43. PERFORMED CUT OUT REF SAAB SRM 53-70-10 NDT:PERFFVNDT006EC & 004UT BOND, NO DELAM AND NO CRACKS, REPAIRED RT CABIN DENTS IAW EO553056 AND SRM 53-70-10. 2 L 7 2 4T RT A52EU 2001020500082 20010205 00082 EU 2001 2 5 MALA010135 1 20010116 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 454XJ 454 FOUND DURING C-CHECK, CORROSION ON LBL18.3 SEAT TRACK AND WEB FROM STA 294 - STA 363. REFER TO CELSIUS W/O 19238, TASK 1526, AND SAAB STATEMENT 340 SDS000801. MAINTENANCE REMOVED CORROSION BETWEEEN STA 294 - 363 IAW SRM 51-70-40. ALODINE D, PRIMED IAW SRM 51-20-42/43, PAINTED SEAT TRACK AND INSTALLED AV100 ON TRACKS AND FLANGES. DAMAGE IS ACCEPTED AS IS R EF SAAB ENGINEERING STATEMENT 340SDS000801. 2 L 7 2 4T RT A52EU 2001020500090 20010205 00090 NM 2001 2 5 2001UALA00014 1 20010109 A 2150 ACTUATOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE COOLING DOOR FAILED A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 7262U 21409 DURING TAXI AIRCRAFT EXPERIENCED SMOKE IN THE CABIN. LEFT PACK WAS INOPERABLE ON THE GROUND. AIRCRAFT RETURNED TO THE GATE. *S/D* RT PACK FAN AIR COOLING DOOR DID NOT OPEN ON GROUND. REPLACED FAN COOLING DOOR ACTUATOR. 2 L 7 3 4F 4 F A3WE E2EA 2001020500092 20010205 00092 EU 2001 2 5 QXEA0100029 1 20010118 A 3240 50040702 BRAKE FOKKER F28 F28MK4000 4990810 EU LEFT MALFUNCTIONED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 477AU 6699 402 11226 SEA- LEFT BRAKE FEELS SOFT, ALSO FEELS AS IF ANTI-SKID IS RELEASING PRESSURE TO EARLY DURING LANDING ROLL-OUT. INSPECTE D AND FOUND NR 2 BRAKE INEFFECTUAL. REMOVED AND REPLACED NR 2 BRAKE. COMPLIED WITH HIGH SPEED TAXI CHECK. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001020500093 20010205 00093 EU 2001 2 5 QXEA0100030 1 20010122 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 496US 11169 GTF- EMERGENCY EXIT SIGN MID CABIN FORWARD SIDE INOPERATIVE. REMOVED AND REPLACED OVERHEAD EMERGENCY EXIT SIGN. OPERAT IONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001020500094 20010205 00094 EA 2001 2 5 COMA0160140 1 20010122 A 5315 6003401717 FLOORBEAM CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 915CA 18100 7013 FLOORBEAM (P/N 600-34017-17) AT FS 280.00 HAS A 2 INCH LONG CRACK. TRIMMED OUT CRACKED AREA, LPI, FABBED REPAIR ANGLE A ND INSTALLED IAW WVAC EO 601R-53-2100. 2 L 7 2 4F RT A21EA 2001020500095 20010205 00095 EA 2001 2 5 COMA0160139 1 20010122 A 5320 601R3103077 SPLICE CNDAIR CL600 CL6002B19 EA FUSELAGE MISMANUFACTURED A COMA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 915CA 18100 7013 TWO SPLICE PLATES (P/N 601R31030-77) WERE FABED CORRECTLY BY MANUFACTURER. FABRICATED TWO DOUBLER PLATES, REWORK SPLICE PLATES AND INSTALLED IAW WVAC EO 601R-53-2099. 2 L 7 2 4F RT A21EA 2001020500096 20010205 00096 WP 2001 2 5 UPS01834620 1 20010115 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:N/A, EMERGENCY LIGHT LEFT ON, BATTERY PACK DEAD. REMOVED AND REPLACED BATTERY PACK. TEST OK. 2 L 7 4 4F RT 4A25 2001020500098 20010205 00098 EA 2001 2 5 COMA0160138 1 20010122 A 5320 60034017373 CLIP CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 915CA 18100 7013 LT AND RT VERTICAL ANGLES AT FS 280.00 ARE CRACKED. REMOVED DAMAGED ANGLES AND INSTALLED NEW FABRICATED ANGLES IAW WVAC EO 601R-53-2098A. 2 L 7 2 4F RT A21EA 2001020500099 20010205 00099 EA 2001 2 5 COMA0160146 1 20010122 A 5320 601R3866949 DOUBLER CNDAIR CL600 CL6002B19 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 915CA 18100 7013 DOUBLER (P/N 601R-38669-49) FORWARD OF SERVICE DOOR IS CORRODED. REMOVED AND REPLACED DOUBLER IAW WVAC EO 601R-53-2104. 2 L 7 2 4F RT A21EA 2001020500100 20010205 00100 SO 2001 2 5 COMA0110025 1 20010122 A 3020 3D237606 CONTROL VALVE EMB 120 EMB120RT SO LT ENGINE DEICE MALFUNCTIONED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 259CA 7755 120252 LEFT ENGINE INTAKE DEICE IS INOP. REPLACED THE INTAKE EJECTOR VALVE. 2 L 7 2 4T RT A31SO 2001020500101 20010205 00101 NM 2001 2 5 NACA20010004 1 20010120 A 3260 SWITCH BOEING 727 72723 1384004 NM NLG DIRTY A NACA O OTHER G J MULTIPLE FAILURE WARNING INDICATION LD LANDING 1 AL 03 930FT 19387 ON LANDING AT ANCHORAGE LOSS OF BRAKE, LOSS OF LEFT PACK, LOSS OF APU, GPWS, AND STICK SHAKER CAME ON. CLEANED NOSE GEA R SAFETY WARNING SWITCH. 2 L 7 3 4F A3WE 2001020500104 20010205 00104 NM 2001 2 5 NACA20010005 1 20010123 A 3241 42527D CONTROL UNIT BOEING 727 72723 1384004 NM ANTI SKID SYSTEM MALFUNCTIONED A NACA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 AL 03 930FT 2904 2904 19387 WITH ANTI SKID ON BRAKES RELEASED ON ROLLOUT. REPLACED ANTI SKID CONTROL MODULE. 2 L 7 3 4F A3WE 2001020500105 20010205 00105 EU 2001 2 5 2001UALA00022 1 20010110 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 437UA 655 CABIN EMERGENCY LIGHT TEST FAILED. REPLACED POWER SUPPLY 13WL. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2001020500106 20010205 00106 NM 2001 2 5 2001UALA00023 1 20010112 A 3350 POWER SUPPLY BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 778UA 26940 FLOOR PROX EMERGENCY LIGHTS INOP ON ALL SEATS BETWEEN DOORS 3L AND 4L, DOORS 3R AND 4R. REPLACED POWER SUPPLY AT 3R. O PS CK GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001031200634 20010312 00634 NM 2001 3 12 2001UALA00029 1 20010112 A 3350 S106 BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7268U 21415 EMERGENCY EXIT SIGN INOPERABLE WITHIN THE CABIN. *S/D* THE BATTERY FAILED. REPLACED THE BATTERY. OPERATIONS CHECK NO RMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001031200635 20010312 00635 NM 2001 3 12 2001UALA00030 1 20010115 A 2131 CONTROLLER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN PRESSURE MALFUNCTIONED A UALA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 WP 29 7458U 21912 DURING CLIMB AIRCRAFT COULD NOT MAINTAIN CABIN PRESSURE. *S/D* MAINTENANCE REPLACED BOTH THE PRESSURE SELECTOR PANEL A ND THE CABIN PRESSURE CONTROLLER. OPERATIONS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001031200636 20010312 00636 NM 2001 3 12 2001UALA00031 1 20010116 A 2520 SEAT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE ROW 13 LOOSE A UALA O OTHER O OTHER TO TAKEOFF 1 WP 29 7256U 21403 DURING TAKEOFF ROW 13 SEATS A, B, C CAME LOOSE FROM THE FLOOR. *S/D* CAUSE UNKNOWN - AMIS ENTRY INDICATED A MISSING FO OT LOCK. FLEET ENGINEERING CONSIDERS THIS AN ISOLATED INCIDENT AND NO HISTORY EXISTS REGARDING LOOSE SEAT ASSEMBLIES AT THIS LOCATION. THE SEAT ASSEMBLY WAS REINSTALLED. 2 L 7 3 4F 4 F A3WE E2EA 2001020500107 20010205 00107 NM 2001 2 5 2001UALA00034 1 20010116 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN DETACHED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 794UA 26953 3E EEL LIGHT DETACHED AND STOWED AT SEAT. SECURED 3E EEL LIGHT. OPS CHK NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001030500263 20010305 00263 NM 2001 3 5 2001UALA00035 1 20010117 A 2121 22147504 FAN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE COCKPIT ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 797UA 9950 26924 DURING CRUISE AFTER TURNING ON RT RECIR FAN UNUSUAL ODOR FILLED THE COCKPIT AND FIRST CLASS CABIN. NOT AS BAD IN FIRST CLASS, SMELL LIKE OZONE OR ELECTRIC BURNING SMELL. ODOR COULD NOT BE DUPLICATED ON GROUND. SINCE IT WAS REPORTED THAT THE ODOR WAS LIKE OZONE, THE LT OZONE CONVERTER WAS REPLACED. THE OZONE CONVERTER WAS THEN ROUTED TO HONEYWELL FOR EFFI CIENCY TEST. THIS MRR WILL BE UPDATED WITH TEST RESULTS AS SOON AS THEY BECOME AVAILABLE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001040400172 20010404 00172 NM 2001 4 4 2001UALA00036 1 20010118 A 4920 38223643 SEAL BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE APU DAMAGED A UALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 WP 29 768UA 10570 10570 26919 CREW REPORTED ODOR AND THIN SMOKE LAYER IN CABIN. AFTER TAKE-OFF NOTED FLUX PACK FLOW AND TEMPS, ALSO HAD ASSOCIATED EC ON COOL VLV L AND TRIM AIR PRESS SOV RT, SELECTING TRIM AIR OFF CLEARED MSGS CAME BACK WITH TRIM AIR ON. *S/D* APU WAS REMOVED ON 1/21/01 DUE TO METAL SHAVINGS FOUND ON GEARBOX CHIP DETECTOR. SHOP DISASSEMBLED APU ENGINE AND CONFIRMED ME TAL. UPON FURTHER DISASSEMBLY OF LOAD COMPRESSOR, SHOP FOUND SEAL ROTOR HEAVILY SCORED AND CARBON SEAL DAMAGED. PARTS WILL BE REPLACED, ENGINE REASSEMBLED, AND TESTED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001031900074 20010319 00074 NM 2001 3 19 2001UALA00039 1 20010117 A 2133 OUTFLOW VALVE HAMLTN 7110035 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN PRESSURE FAILED A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 7458U 21912 AUTOMATIC CABIN PRESSURIZATION FAILED DURING CLIMB. *S/D* THE OUTFLOW VALVE FAILED. REPLACED OUTFLOW VALVE. 2 L 7 3 4F 4 F A3WE E2EA 2001020500108 20010205 00108 SO 2001 2 5 SWIA972288 1 20010122 A 5210 HANDLE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE PAX DOOR STUCK A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 301YV 120301 FORWARD DOOR WOULD NOT OPEN FULLY WHEN OPENED FOR PASSENGER DE-PLANNING, HANDLE IS STUCK IN HALF-TRAVEL POSITION. REMOV ED BROKEN LOCKING CAM ROD PUSH END FORWARD AND REPLACED WITH ROD END IAW EMB 120 MM 52-11-00. OPS CHECK GOOD. OPERATES NORMALLY. 2 L 7 2 4T 4 T RT A31SO E20NE 2001020500109 20010205 00109 SO 2001 2 5 SWIA972289 1 20010113 A 3010 BOOT EMB 120 EMB120RT SO PWA 118 PW118 NE STABILIZER FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 200CD 120200 INBOARD STABILIZER AND INBOARD WING DEICE BOOTS FAILED AFTER TAKEOFF. RETURNED TO SEA. REMOVED AND REPLACED INBOARD ST ABILIZER AND WING EJECTOR VALVE WITH SERVICEABLE UNIT. OPS CHECK GOOD. PANEL CLOSED. S/N ON: N3503, S/N OFF: Q7401. 2 L 7 2 4T 4 T RT A31SO E20NE 2001020500110 20010205 00110 SO 2001 2 5 SWIA972290 1 20010114 A 7111 COMPUTER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COWL FLAP FAILED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 204SW 120243 LEFT NACELLE FLAPS FAULT DISCREPANCY DURING RETRACTION. REPLACED FLAP COMPUTER. OPS CHECK BAD. REPLACED LEFT NACELLE FLAP ACTUATOR. OPS AND LEAK CHECK GOOD. WORK ACCOMPLISHED IAW EMB120 MM 27-50-00 AND RII 27-307. FLAP COMP P/N: 3472 00-1001, S/N ON: 0227, S/N OFF: 0057, FLAP ACT P/N: 343100-1001, S/N ON: 0033, S/N OFF: 0078. 2 L 7 2 4T 4 T RT A31SO E20NE 2001020500111 20010205 00111 2001 2 5 SWIA972292 4 20010124 A 3422 DETECTOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FLUX MALFUNCTIONED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 270YV 120270 RECEIVED HDG FLAG ON BOTH EHSIS AND MFD AFTER TAKEOFF. RETURNED TO SLC. ADJUSTED NUMBER TWO FLUX DETECTOR IAW MM 34-21 -00. AHRS SYSTEM OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001020500112 20010205 00112 EA 2001 2 5 SWIA972293 1 20010122 A 4990 APU CNDAIR CL600 CL6002B19 EA APU BAY FAILED A SWIA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 07 408SW 7055 LAVATORY SMOKE DETECTOR MESSAGE. FLIGHT ATTENDANT REPORTS SMOKE IN CABIN. SMOKE DISSIPATED AND SMELLS LIKE OIL OR PACK SOURCE. INSPECTED AIRCRAFT AND FOUND APU SUSPECTED TO BE INOPERATIVE. DEFERRED THE APU. 2 L 7 2 4F RT A21EA 2001020500113 20010205 00113 SO 2001 2 5 COMA0110026 1 20010124 A 5350 12031657002 ANGLE EMB 120 EMB120RT SO RT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 258CA 22700 120247 DURING 1C CHECK TASK 194-01Z, THE RIGHT OVERWING FAIRING ATTACH ANGLE ON TOP OF THE WING WAS FOUND TO BE CRACKED. THE A NGLE WAS REPLACED IN ACCORDANCE WITH AERODESIGN REPORT 1226-21, REV IR, 7/6/99. 2 L 7 2 4T RT A31SO 2001020500114 20010205 00114 SO 2001 2 5 COMA0110027 1 20010124 A 5210 12021059001 CHANNEL EMB 120 EMB120RT SO PAX DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 258CA 22700 120247 DURING 1C CHECK TASK 52-14, THE PAX DOOR STRUCTURE U-CHANNEL WAS FOUND TO BE CRACKED. THE CHANNEL WAS REPLACED PER SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001020500115 20010205 00115 SO 2001 2 5 COMA0110028 1 20010124 A 2720 12027649011 CONTROL CABLE EMB 120 EMB120RT 3260202 SO RUDDER CONTROL WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 258CA 22700 120247 DURING 1C CHECK TASK 27-62, THE RIGHT SIDE OUTBOARD RUDDER CONTROL CABLE WAS FOUND TO BE WORN WHERE IT PASSES THROUGH TH E WING BOX FAIRLEADS. THE CABLE WAS REPLACED PER THE AMM. 2 L 7 2 4T RT A31SO 2001020500116 20010205 00116 SO 2001 2 5 COMA0110030 1 20010124 A 5210 12021158001 CHANNEL EMB 120 EMB120RT SO PAX DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 258CA 22700 120247 DURING 1C CHECK TASK 52-14, THE PAX DOOR STRUCTURE CHANNEL, THIRD FROM BOTTOM, WAS FOUND TO BE CRACKED. THE CHANNEL WAS REPLACED PER SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001020500118 20010205 00118 2001 2 5 COMA0160155 4 20010123 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 810CA 7370 STALL FAIL CAUTION MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001020500119 20010205 00119 EA 2001 2 5 COMA0160157 1 20010123 A 2740 CONTROL UNIT CNDAIR CL600 CL6002B19 EA STAB TRIM MALFUNCTIONED A COMA C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 SO 01 956CA 7105 STAB TRIM AND MACH TRIM DISENGAGED DURING T/O. COULD NOT DUPLCIATE STAB TRIM OPERATION NORMAL. 2 L 7 2 4F RT A21EA 2001020500120 20010205 00120 2001 2 5 COMA0160158 4 20010123 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 975CA 7150 STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001020500121 20010205 00121 EA 2001 2 5 COMA0160159 1 20010124 A 2742 83963 ACTUATOR CNDAIR CL600 CL6002B19 EA VERTICAL STAB MALFUNCTIONED A COMA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 01 785CA 2458 7326 CONFIG STAB AND CONFIG TRIM WARNING. REPLACED THE HSTA. 2 L 7 2 4F RT A21EA 2001020500122 20010205 00122 2001 2 5 COMA0160160 4 20010124 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 783CA 7315 STALL FAIL CAUTION DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001020500123 20010205 00123 2001 2 5 COMA0160161 4 20010124 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 975CA 7150 STALL FAIL CAUTION DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001020500125 20010205 00125 EA 2001 2 5 COMA0160162 1 20010124 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA LAVATORY MALFUNCTIONED A COMA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING AP APPROACH 1 SO 01 914CA 7012 SMOKE TOILET CAUTION MESSAGE. DEFERRED MAINT ON SMOKE DETECTOR PER MEL. 2 L 7 2 4F RT A21EA 2001030600083 20010306 00083 NM 2001 3 6 2001UALA00054 1 20010114 A 2612 285N002836 CIRCUIT BOARD BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE RT ENGINE FAILED A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 610UA 21871 GOT FIRE OVERHEAT MESSAGE AND ASSOCIATED RIGHT ENGINE FIRE LOOP 1 AND 2 STATUS MESSAGE. RESET FIRE-OVERHEAT SWITCH. LI GHT STAYED OUT DIVERTED TO DEN. *S/D* CAUSE OF THE RIGHT ENGINE LOOP 1 AND LOOP 2 STATUS MESSAGE WAS RIGHT ENGINE AFOL TS CARD M10274 (MR26009). A REPLACEMENT CARD WAS INSTALLED AND OPERATION WAS NORMAL. CHECK OF THE REMOVED AFOLTS CARD MR26009-264 WAS TESTED BY SHOP 142 AND THE FAULT WAS CONFIRMED TO BE WITH THE CARD. 2 L 7 2 4F 4 F RT A1NM E3NE 2001020500127 20010205 00127 NM 2001 2 5 UPS01234756 1 20010102 A 5312 PRESSURE PANEL BOEING 727 72722C 138400F NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C CK, NLG W/W RIGHT SIDEWALL BS 251 AFT OF FWD ACCESS DOOR, CRACK INDICATION ALONG FASTENERS ROW, ABOUT 4.5 INCHES. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH SRM 51-40-2. 2 L 7 3 4F A3WE 2001020500128 20010205 00128 NM 2001 2 5 UPS01234757 1 20010102 A 5312 PRESSURE PANEL BOEING 727 72722C 138400F NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C CK, NLG W/W TOP CEILING RBL 15 AND BS 272 CRACK INDICATION ALONG FASTENER ROW ABOUT 2.5 INCHES LONG. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH SRM 51-40-2. 2 L 7 3 4F A3WE 2001020500129 20010205 00129 NM 2001 2 5 UPS01234758 1 20010102 A 5312 PRESSURE PANEL BOEING 727 72722C 138400F NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C CK, NLG W/W LT SIDEWALL BS 243 TO LWR SHOWED CRACK AROUND FASTENER, ABOU T 1 INCH LONG. INSTALLED DOU BLER REPAIR IN ACCORDANCE WITH SRM 51-40-2. 2 L 7 3 4F A3WE 2001020500131 20010205 00131 NM 2001 2 5 UPS01434751 1 20010124 A 2612 CIRCUIT BOARD BOEING 747 747123 1384873 NM FIRE DETECTION DIRTY A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:PFLT CREW PREFLT NR 2 ENG FIRE BELL WILL NOT CUT OUT. CLEANED AND RE-RACK CARD A-6, OP CK NORMAL. 2 L 7 4 4F A20WE 2001022000277 20010220 00277 NM 2001 2 20 UPS01434754 1 20010125 A 7830 12623642 THRUST REVERSER BOEING 747 747123 1384873 NM NR 4 ENGINE FAILED A IPXA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 671UP 20323 INSPECTION TYPE:IN PIREP NR 4 THRUST REVERSER FAILED TO DEPLOY. REMOVED AND REPLACED NR 4 T/R PDU PER MM 78-31-01 AND I NSTALLED NEW FLEX SHAFT PER MM 78-31-02, OPS TEST OK PER MM 78-31-00. S/N ON P-2527, SHAFT P/N ON 121652-1. CLEARED M2 08055, REMOVED PLACARD. 2 L 7 4 4F A20WE 2001020500132 20010205 00132 WP 2001 2 5 UPS01834752 1 20010124 A 2612 CIRCUIT BOARD DOUG DC8 DC873F 302199F WP FIRE DETECTION DIRTY A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:N/A, NR 4 ENGINE FIRE DETECTION, NO TEST. CLEANED AND RE-RACK CARD A-6, OP CK NORMAL, WAIT NO HELP. OPE NED NR 4 THRUST COWLING AND CLEANED ELECTRICAL CANNON PLUG AT PYLON. GROUND CHECK PERFORMED AND FOUND OK. 2 L 7 4 4F RT 4A25 2001020500133 20010205 00133 NM 2001 2 5 RAAA01B203 1 20010112 A 5310 FRAME BOEING 727 72722C 138400F NM PAX DOORWAY CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED B3 MAINTENANCE CHECK FOUND FWD ENTRY DOOR LOWER FRAME CRACKED FWD SIDE. REPAIRED CRACKED WEB REF BOEIN G SRM 51-40-2. 2 L 7 3 4F A3WE 2001020500134 20010205 00134 NM 2001 2 5 RAAAO1B204 1 20010124 A 3350 86210144 BATTERY INTVLV BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 AT END OF SCHEDULED B3 MAINTENANCE CHECK EXIT IDENTIFIER INOP AT RT FWD OVERWING EXIT. REPLACED BATTERY AND TESTED PER RAA ECO 86-26. 2 L 7 3 4F A3WE 2001020500135 20010205 00135 2001 2 5 MWEA010119 4 20010123 A 3460 258733513 COMPUTER DOUG DC9 DC932 3022066 WP FLIGHT DIRECTOR INTERMITTENT A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 204ME 47680 CAPTAINS ATTITUDE INDICATOR GYRO FLAG AND FLIGHT DIRECTOR COMPUTER FLAG CAME ON INTERMITTENTLY. REMOVED AND REPLACED NR 1 VERTICAL GYRO, REF 34-27-1. OPS CHECK GOOD. 2 L 7 2 4F A6WE 2001020500136 20010205 00136 NM 2001 2 5 RAAA01B205 1 20010124 A 3350 86210144 BATTERY INTVLV BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 AT END OF SCHEDULED B3 MAINTENANCE CHECK EXIT IDENTIFIER INOP AT MID CABIN DOOR. REPLACED BATTERY AND TESTED PER RAA EC O 86-26. 2 L 7 3 4F A3WE 2001020500137 20010205 00137 NM 2001 2 5 RAAA01B206 1 20010124 A 3350 86210144 BATTERY INTVLV BOEING 727 72722C 138400F NM PAX CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 AT END OF SCHEDULED B3 MAINTENANCE CHECK LT FWD OVERWING EXIT IDENTIFIER INOP. REPLACED BATTERY AND TESTED PER RAA ECO 86-26. 2 L 7 3 4F A3WE 2001020500138 20010205 00138 NM 2001 2 5 RAAA01B207 1 20010124 A 3350 86210144 BATTERY INTVLV BOEING 727 72722C 138400F NM PAX CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 AT END OF SCHEDULED B3 MAINTENANCE CHECK EXIT IDENTIFIER INOP AT AT SEAT ROW 11ABC OVERWING EXIT. REPLACED BATTERY AND TESTED PER RAA ECO 86-26. 2 L 7 3 4F A3WE 2001020500139 20010205 00139 CE 2001 2 5 CIEA0002 1 20010121 A 7932 310238201 DIPSTICK BEECH 90 E90 1152914 CE PWA PT6 PT6A28 EA RT ENGINE LOOSE E CIEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 03 87CH LW20 PCE51003 APPROXIMATELY 15 MINUTES AFTER TAKEOFF THE PILOT NOTICED A RIGHT ENGINE TORQUE INDICATION FLUCTUATION, FOLLOWED BY A DRO PPING OIL PRESSURE INDICATION. THE PILOT REDUCED THE POWER ON THE ENGINE. THE PILOT RETURNED TO THE AIRPORT AND LANDED WITHOUT INCIDENT, WHILE MONITORING THE OIL PRESSURE. THE OIL PRESSURE NEVER DROPPED BELOW 40 PSI. AFTER LANDING THE D IP STICK WAS FOUND TO BE LOOSE. THE ENGINE WAS INSPECTED IN ACCORDANCE WITH THE REQUIREMENTS OF THE PRATT AND WHITNEY M AINTENANCE MANUAL, SERVICED WITH ENGINE OIL, AND WAS RETURNED TO SERVICE. THE OIL DIP STICK SPRING TENSION WAS ADJUSTED . 1 L 7 2 3T 4 T 3A20 E4EA 2001020500140 20010205 00140 EU 2001 2 5 C2XA01IA043 1 20010124 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14815 104 IAH - DURING 4A INSPECTION, SEVERAL AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY BATTERY PACK IN ACCORDANCE WITH ATR42-320 JIC 33-51-21, AND THE AIRCRA FT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001020500141 20010205 00141 SO 2001 2 5 C2XA01IA044 1 20010122 A 3350 7287580505 LIGHT EMB 145 EMB145ER SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15941 145035 IAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE FIRST STRIP OF AISLE PATH EMERGENCY LIGHTS WERE INOPERAT IVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF LIGHT STRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001020500143 20010205 00143 SO 2001 2 5 C2XA01IA045 1 20010122 A 3260 852701 SENSOR EMB 145 EMB145LR SO RT MLG INOPERATIVE A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 14950 145061 IAH - FLIGHT 4095, THE CREW REPORTED THAT A LANDING GEAR AIR/GND FAIL MESSAGE APPEARED BEFORE THE GEAR WERE FULLY RETRAC TED, AND DISAPPREARED AFTER FULL RETRACTION. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENAN CE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR LOWER PROXIMITY SENSOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001020500144 20010205 00144 EU 2001 2 5 0100193220 1 20010123 A 2612 B401ACM0507 COMPUTER AIRBUS 320 A320211 3930320 EU E/E BAY FALSE INDICATION A NWAA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 GL 01 320US 1053 1053 213 DURING TAKEOFF AT ROTATION, RECEIVED A MOMENTARY NR 2 ENGINE FIRE WARNING. ALL ENGINE PARAMETERS WERE NORMAL. RETURNED TO DEPARTURE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED THE CFDIU AND NR 1 FWC NOT FUNCTI ONING PROPERLY. REPLACED CFDIU AND NR 1 FWC, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 2001020500145 20010205 00145 EU 2001 2 5 0100203220 1 20010123 A 2612 FIRE DETECTOR AIRBUS 320 A320211 3930320 EU NR 1 MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 320US 213 DURING TAKEOFF AT ROTATION, RECEIVED A MOMENTARY NR 2 ENGINE FIRE WARNING. ALL ENGINE PARAMETERS WERE NORMAL. RETURNED TO DEPARTURE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCIES BUT REPLACED NR 1 FDU, CARD 5LP, AND 18LP PRECAUTIONARY. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 2001020500146 20010205 00146 EU 2001 2 5 0100213255 1 20010116 A 2910 SEAL AIRBUS 320 A320212 EU HYD SYSTEM LEAKING A NWAA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 355NW 807 DURING CRUISE, RECEIVED HYD Y RSVR LO LVL MESSAGE. FOLLOWED COM PROCEDURES AND CONTINUED TO FINAL DESTINATION FOR A NOR MAL LANDING. MAINTENANCE REPLACED LEAKING SEAL ON YELLOW PTU MANIFOLD. LEAK CHECK OK. 2 L 7 2 4F RT A28NM 2001020500147 20010205 00147 NM 2001 2 5 0100226625 1 20010118 A 2131 CONTROLLER BOEING 747 747251B 1384892 NM CABIN PRESSURE FAILED A NWAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 625US 21707 DURING CLIMB AT 24,000 FEET, THE PRESSURIZATION AUTO FAIL LIGHT ILLUMINATED ACCOMPANIED WITH THE NR 2 PACK TRIPPING AND THE PRESSURE RELIEF LIGHT ILLUMINATING. PERFORMED AN EMERGENCY DESCENT TO 10,000 FEET AND CABIN WAS CONTROLLED MANUALLY AT 14,000 FEET. AIRCRAFT RETURNED TO NRT AND LANDED WITHOUT INCIDENT. REPLACED THE CABIN PRESSURE CONTROLLER, CONTROL PANEL, AND PRESSURE RELIEF VALVE. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2001020500149 20010205 00149 NE 2001 2 5 0100235530 2 20010122 A 7261 HOUSING BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 2 OIL FILTER LEAKING A NWAA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 530US 23845 716425 NR 2 ENGINE WAS SHUTDOWN DURING CRUISE AT 35,000 FEET DUE TO OIL QUANTITY AND PRESSURE LOSS. FLIGHT CREW DIVERTED TO SY R AND MADE AN UNEVENTFUL LANDING. MAINTENANCE FOUND OIL LEAK AT OIL FILTER HOUSING. REPLACED THE O-RINGS AND FILTER. GROUND RUN AND REQUIRED INSPECTIONS WERE COMPLETED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001020500150 20010205 00150 EU 2001 2 5 0100243263 1 20010123 A 2910 NAS161212 PACKING AIRBUS 320 A320212 EU YELLOW HYD SYS LEAKING A NWAA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 363NW 923 DURING CRUISE, RECEIVED HYD Y RSVR LO LVL MESSAGE. FOLLOWED COM PROCEDURES AND CONTINUED TO FINAL DESTINATION WITH A NO RMAL LANDING. MAINTENANCE REPLACED A LEAKING O-RING BETWEEN THE PTU QUICK DISCONNECT COUPLING AND MANIFOLD. LEAK CHECK OK. 2 L 7 2 4F RT A28NM 2001020500156 20010205 00156 NM 2001 2 5 AWXA0001254 1 20010119 A 5270 D203LB5B SWITCH BOEING 737 7373Y0 1384671 NM CARGO DOOR INTERMITTENT A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 329AW 23500 MAF-DIVERTED FLIGHT- BOTH MAIN DECK CARGO DOOR LIGHTS CAME ON DURING FLIGHT AT FL 330. THE CREW FOLLOWED QRH PROCEDURES AND LANDED AT MAF. TROUBLESHOOTING REVEALED THE PUSH TO TEST SWITCH WAS FAULTY (INTERMITTANTLY STICKING). THE AIRCRAF T WAS MAINTENANCE FERRIED TO PHX UNPRESSURIZED. IN PHX THE SWITCH WAS REPLACED AND FUNCTIONAL CHECKS GOOD. NO FURTHER PROBLEMS REPORTED. 2 L 7 2 4F RT A16WE 2001020500157 20010205 00157 NM 2001 2 5 UPS01234747 1 20010107 A 5522 PANEL BOEING 727 72731C 1384011 NM LT ELEVATOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:CCK CORROSION IN LT ELEVATOR UPPER SKIN UNDER STATIC DISCHARGER. UPPER SKIN REPLACED IAW DRAWING NR 655 640. 2 L 7 3 4F A3WE 2001020500158 20010205 00158 NM 2001 2 5 UPS01234748 1 20010109 A 5320 BRACKET BOEING 727 72731C 1384011 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C CK ATTACH BRACKET LOCATED ON LT BS 870 FITTING IS CRACKED ALONG BEND LINE. BRACKET DE-RIVETED. HEAT TREATMENT. BRACKET FABRICATED. BRACKET INSTALLED. 2 L 7 3 4F A3WE 2001020500159 20010205 00159 NM 2001 2 5 UPS01434713 1 20010105 A 5311 FRAME BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C MAIN CABIN CRACKING IN OUTER FLANGES OF FRAME AT BS 260 - 280 RT SIDE. REPAIRED IAW SRM 51-40-03. 2 L 7 4 4F A20WE 2001020500160 20010205 00160 NM 2001 2 5 UPS01434740 1 20010104 A 5720 BRACKET BOEING 747 747123F NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, RT WING LOWER T/E SUPPORT BEAM CLIP CRACKED AT FWD SIDE OF LDG BEAM AT WS 500. BRACKET REMOVED AND REPLACED IAW SRM 51-30-02. 2 L 7 4 4F A20WE 2001020500165 20010205 00165 NM 2001 2 5 TWAA0101401 1 20010122 A 3350 80741 LIGHT BOEING 767 76733AER 1385230 NM ROW 25 MISSING A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 637TW 25403 THE EGRESS LIGHT WAS MISSING AT SEAT 25. CORRECTIONS WERE DEFERRED PER MEL. THE LIGHT ASSY WAS LATER INSTALLED. CHECK- C 9-23-99. 2 L 7 2 4F RT A1NM 2001020500170 20010205 00170 NM 2001 2 5 QXEA0100041 1 20010109 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX-RIGHT HAND OUTBOARD SEAT TRACK HAS A SCRATCH AT STATION X501.000. REPAIRED IAW DHC-8 SRM 51-20-41 AND RD8-53-1342. 2 H 7 2 4T RT A13NM 2001020500172 20010205 00172 SO 2001 2 5 COMA0110029 1 20010124 A 5210 12021158001 CHANNEL EMB 120 EMB120RT SO PAX DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 258CA 22700 120247 DURING 1C CHECK TASK 52-14, THE PAX DOOR STRUCTURE LOWER CHANNEL WAS FOUND TO BE CRACKED AT BOTH ENDS. THE CHANNEL WAS REPLACED PER SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001020500173 20010205 00173 EA 2001 2 5 COMA0160156 1 20010123 A 2750 860D10018 FCU CNDAIR CL600 CL6002B19 EA TE FLAP CONTROL MALFUNCTIONED A COMA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 427CA 194 7460 FLAPS FAIL MESSAGE. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2001020500187 20010205 00187 WP 2001 2 5 ABXA0100023 1 20010122 A 3350 60030451 BATTERY PACK DOUG DC9 DC932F 3022067 WP FUSELAGE DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 85933 925 47040 CABIN EMERGENCY LIGHTS WERE INOPERATIVE DURING PREFLIGHT INSPECTION. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY L IGHT BATTERY PACK IAW DC-9 MM 33-53-02. 2 L 7 2 4F A6WE 2001020500192 20010205 00192 SO 2001 2 5 COMA0110010 1 20010112 A 5315 12046158001 FLOORBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 267CA 21508 120259 THE AIRCRAFT OMEGA BEAMS (P/N 120-46158-001) QTY 2, AND 120-46258-002 QTY 1, HAVE EXCESSIVE CORROSION. THE OMEGA BEAMS WERE REPLACED IN ACCORDANCE WITH AERODESIGN REPORT NR 2174-1. 2 L 7 2 4T RT A31SO 2001020500193 20010205 00193 SO 2001 2 5 COMA0110011 1 20010112 A 5315 12005087007 FLOORBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 267CA 21508 120259 THE AIRCRAFT SUSTAINED DAMAGE IN THE FORM OF CORROSION TO THE UPPER SURFACE OF THE CENTER OMEGA FLOORBEAM. THE OMEGA FL OORBEAM WAS REPAIRED IN ACCORDANCE WITH AERODESIGN REPORT NR 2181-11. 2 L 7 2 4T RT A31SO 2001020500194 20010205 00194 SO 2001 2 5 COMA0110012 1 20010112 A 5412 FIREWALL EMB 120 EMB120RT SO APU BAY CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 267CA 120259 THE AIRCRAFT HAS A CRACK IN THE APU FIREWALL WEB. INSTALLED A DOUBLER IN ACCORDANCE WITH AERODESIGN REPORT NR 2677-3. 2 L 7 2 4T RT A31SO 2001020500195 20010205 00195 NM 2001 2 5 MASA01001 1 20010104 A 3350 6519023 HOUSING DHAV DHC8 DHC8202 2809007 NM CABIN CRACKED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 444YV 444 DURING ROUTINE MAINTENANCE, THE CREW FOUND TWO EMERGENCY FLOOR ESCAPE PATH LIGHT FIXTURES WITH CRACKED HOUSING. MAINTEN ANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT FIXTURES AND OPS CHECKS GOOD. (M) 2 H 7 2 4T RT A13NM 2001020500196 20010205 00196 EA 2001 2 5 MASA01002 1 20010104 A 3350 487190 CONNECTOR CNDAIR CL600 CL6002B19 EA CABIN DISCONNECTED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77195 7195 FLT 5860 - CLT-BTR - DURING PREFLIGHT, THE CREW FOUND THAT THE LIGHTED ORANGE STRIP AT THE RIGHT EMERGENCY EXIT INOPERAT IVE. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE RESECURED THE CONNECTOR. OPS CHECKED GOOD AND THE AIRCRAFT RE TURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001020500197 20010205 00197 EA 2001 2 5 MASA01003 1 20010105 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27191 7191 DURING ROUTINE MAINTENANCE, THE CREW FOUND A RIGHT FORWARD EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D THE LIGHT AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2001020500198 20010205 00198 EA 2001 2 5 MASA01005 1 20010105 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27191 7191 DURING ROUTINE MAINTENANCE, THE CREW FOUND A RIGHT FORWARD EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D THE LIGHT AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2001020500203 20010205 00203 EU 2001 2 5 MALA010133 1 20010115 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 454XJ 454 FOUND DURING C-CHECK, CORROSION ON BL 0 SEAT TRACK LT FLOOR FLANGE AND WEB STA 294 - STA 363. REFER TO CELSIUS W/O 1923 8, TASK 1525. MAINTENANCE REMOVED CORROSION BETWEEN STA 294 - 363 IAW SRM 51-70-40, MATERIAL REMAINING WITHIN LIMITS, R EF SRM 51-10-10. ALODINED, PRIMED IAW 51-20-42/43. PAINTED SEAT TRACKS AND INSTALLED AV100 ON TRACKS AND FLANGES. 2 L 7 2 4T RT A52EU 2001020500208 20010205 00208 NM 2001 2 5 20010202SG009 1 20010104 A 2510 50086003 BUSS TIE BOEING 727 727227 1384078 NM NR2 GENERATOR OVERHEATED A RYNA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 07 17773 21045 FLT 421 - BED - PRIOR TO DEPARTURE FLIGHT CREW NOTED SMOKE ON FLIGHT DECK. FOUND SUSPECT EVIDENCE OF NR 2 BUS TIE BREAK ER OVERHEAT WITH SUBSEQUENT DAMAGE TO ELECTRICAL SHELF. REMOVED AND REPLACED ELECTRICAL SHELF AND NR 2 BUS TIE BREAKER. NR 2 BUS TIE BREAKER, VOLTAGE REGULATOR, AND BUS PROTECTION PANEL REPLACED AS PRECAUTION DUE TO SMOKE RESIDUE FROM FAI LED BUS TIE BREAKER. (M) 2 L 7 3 4F A3WE 2001020500210 20010205 00210 SO 2001 2 5 COMA0110013 1 20010112 A 5320 12018806002 FLOOR SUPPORT EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 267CA 21508 120259 THE AIRCRAFT''S TWO FLOOR SUPPORT ANGLES UNDER THE PAX DOOR ENTRYWAY THRESHOLD ARE CORRODED. THE PARTS WERE REPLACED IN ACCORDANCE WITH AERODESIGN REPORT NR 3711-1. 2 L 7 2 4T RT A31SO 2001020500211 20010205 00211 SO 2001 2 5 COMA0110014 1 20010112 A 5320 12006218001 SUPPORT BRACKET EMB 120 EMB120RT SO FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 267CA 21508 120259 THE AIRCRAFT''S SKIN SUPPORT FOR FRAME 40 IS CRACKED. SKIN SUPPORT WAS REPLACED WITH A SERVICEABLE UNIT IN ACCORDANCE W ITH AERODESIGN REPORT NR 3859-1. 2 L 7 2 4T RT A31SO 2001020500212 20010205 00212 SO 2001 2 5 COMA0110015 1 20010112 A 5414 12026110025 SKIN EMB 120 EMB120RT SO LEFT NACELLE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 267CA 21508 120259 THE LEFT HAND NACELLE AFT OUTBOARD SKIN IS CRACKED. A DOUBLER WAS INSTALLED IN ACCORDANCE WITH AERODESIGN REPORT NR 386 0-1. 2 L 7 2 4T RT A31SO 2001020500215 20010205 00215 WP 2001 2 5 USAAD01004 1 20010108 A 2170 V1211 COALESCER BAG DOUG DC9 DC982 3022082 WP AC BAY DIRTY A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 822US 49139 EWR - PIT, FLT 1267 - DURING INITIAL CLIMB-OUT, THE AFT FLIGHT ATTENDANT REPORTED AN UNUSUAL ODOR IN THE REAR OF THE AIR CRAFT. THE FIRST OFFICER INVESTIGATED AND FOUND NO SMELL IN CRUISE. THE FLIGHT ATTENDANT REPORTED THE SAME SMELL AT TO UCHDOWN. BOTH FLIGHT ATTENDANTS REPORTED HEADACHES AND NAUSEA. MAINTENANCE REPLACED THE LEFT AND RIGHT AIR CONDITIONIN G COALESCER BAGS. (M) 2 L 7 2 4F A6WE 2001020500218 20010205 00218 WP 2001 2 5 AALA016002 1 20010109 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 822RA 49932 LAX - FOUND SEAT MOUNTED EMERGENCY LIGHT AT 15D INOPERATIVE. RECONNECTED ELECTRICAL PLUG AT SIDE WALL TO SEAT HARNESS. (M) 2 L 7 2 4F A6WE 2001020500219 20010205 00219 WP 2001 2 5 AALA016004 1 20010112 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 871RA 49788 SJC - EMERGENCY LIGHTS ILLUMINATED FROM ROW 28 AFT DURING FLIGHT. EXTINGUISHED PRIOR TO LANDING. REPLACED BATTERY PACK /LIGHT KIT ASSY AT LEF AFT LAV LOWER SIDEWALL. OPS CHECKS OK. (M) 2 L 7 2 4F RT A6WE 2001020500220 20010205 00220 WP 2001 2 5 20010205SG002 1 20010112 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 871RA 49788 SJC - FOUND EMERGENCY LIGHTS ILLUMINATED FROM ROW 28 AFT DURING FLIGHT. EXTINGUISHED PRIOR TO LANDING. REPLACED BATTER Y PACK/LIGHT KIT ASSEMBLY AT LEFT AFT LAVATORY LOWER SIDEWALL. OPS CHECKS OK. REF AALA016004. (M) 2 L 7 2 4F RT A6WE 2001031200637 20010312 00637 NM 2001 3 12 2001UALA00032 1 20010116 A 3244 H4014519 TIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 SEPARATED A UALA C ABORTED TAKEOFF C F.O.D. TO TAKEOFF 1 WP 29 561UA 26661 NUMBER 2 REAR LT MLG TIRE TREAD SEPARATED AND WAS INGESTED INTO THE NUMBER 1 ENGINE ON TAKEOFF. *S/D* SUBSEQUENT INVES TIGATION REVEALED THAT THE NR 2 FWD TIRE ENCOUNTERED FOD ON THE RUNWAY AND THREW IT BACK TO THE NR 2 REAR TIRE. THE NR 2 REAR TIRE SUBSEQUENTLY EXPLODED. 2 L 7 2 4F 4 F RT A2NM E17NE 2001020500221 20010205 00221 EA 2001 2 5 COM0160009 1 20010112 A 5341 12031657001 ATTACH ANGLE CNDAIR CL600 CL6002B19 EA LT & RT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 267CA 21508 120259 THE AIRCRAFT LEFT AND RIGHT WING ATTACH ANGLES ARE CRACKED. THE ANGLES WERE REPAIRED IN ACCORDANCE WITH SRM CHAPTER 53- 20-13 PAGES 205 AND 206 AND AERODESIGN REPORT 1226-21. 2 L 7 2 4F RT A21EA 2001020500222 20010205 00222 SO 2001 2 5 COMA0110020 1 20010112 A 5230 12048716001 BRACKET EMB 120 EMB120RT SO CARGO DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 267CA 21508 120259 THE AIRCRAFT''S CARGO DOOR TRACK BRACKET IS CRACKED. THE CARGO DOOR AFT TRACK BRACKET WAS REPLACED USING ALTERNATE RIVE TS IN ACCORDANCE WITH AERODESING REPORT NR 1657-3. 2 L 7 2 4T RT A31SO 2001020600016 20010206 00016 WP 2001 2 6 CALA0100064 1 20010123 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND FUSELAGE EXTERNAL SKIN AT FORWARD LT SIDE OF E AND E DOOR CUTOUT STA 145, L28L DENTED. THE SKIN WAS RE PAIRED BY INSTALLING FILLER AND DOUBLERS IAW EA 9-5331-2-A0834 AND SRM 51-10-3. 2 L 7 2 4F A6WE 2001020600020 20010206 00020 WP 2001 2 6 CALA0100065 1 20010123 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND LT FORWARD FUSELAGE SKIN DENTED AT FS 133, L10L. THE DENT WAS COLD WORKED AND A DOUBLER WAS INSTALLED IAW SRM 51-30-5, 51-30-2, 53-04, FIGURE 35, 51-10-3, AND EA 9-5331-2-A0835. 2 L 7 2 4F A6WE 2001020600038 20010206 00038 WP 2001 2 6 AALA016006 1 20010113 A 3350 BR50447 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 871RA 49788 LAX-CCI - FIRST CLASS OVERHEAD EMERGENCY LIGHTS DO NOT COME ON DURING TEST. REMOVED AND REPLACED F/C CABIN BATTERY PACK PER MM. OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 2001020600039 20010206 00039 EU 2001 2 6 20010206SG001 1 20010110 A 3246 AH52786 WHEEL BRAERO DH125 HS125700A 4230170 EU LT MLG DAMAGED A KKYA K NONE O OTHER IN INSP/MAINT 1 NE 03 81KA NA0227 DURING PREFLIGHT INSPECTION OF THE AIRCRAFT AT RDU, THE LEFT OUTBOARD WHEEL, INBOARD WHEEL HALVE, WAS FOUND WITH A 10 IN CH SECTION OF THE FLANGE RIM MISSING. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND REPLACED BOTH MAIN WHEEL ASSEMBLIE S. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE AS NO OTHER DISCREPANCIES WERE FOUND. THE WHEEL ASSEMBLY HAD 92.2 H OURS AND 68 LANDINGS SINCE OVERHAUL. AT OVERHAUL THIS AREA WAS EDDY CURRENT INSPECTED. (M) 2 L 7 2 4F A3EU 2001020600040 20010206 00040 NM 2001 2 6 20010206SG002 1 20010111 A 3233 1U11986 ACTUATOR BOEING 747 747230B 1384889 NM NLG BROKEN A Q2SA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 744SA 22363 DURING CRUISE, THE RED GEAR WARNING LIGHT ILLUMINATED INTERMITTENTLY. PLACED GEAR HANDLE IN THE UP POSITION AND HEARD T HUMPING NOISE APPARENTLY FROM THE NOSE LANDING GEAR (NLG) WHEEL WELL AREA WITH SUBSEQUENT LOSS OF NR 1 SYSTEM HYDRAULIC QUANTITY. PLACED GEAR HANDLE IN THE OFF POSITION AND NR 1 SYSTEM HYDRAULIC QUANTITY CONTINUED TO DECREASE DOWN TO ZERO. FOUND NLG FORWARD LEFT DOOR ACTUATOR UPPER HOUSING BROKEN (CASE SEPARATION) AND NLG FORWARD LEFT DOOR ASSEMBLY DAMAGED . REPLACED NLG FORWARD LEFT ACTUATOR AND DOOR ASSEMBLIES. (M) 2 L 7 4 4F A20WE 2001020600041 20010206 00041 NE 2001 2 6 20010206SG003 2 20010116 A 7530 ETPU10002C PRESSURE SWITCH BOEING 757 757200 1384950 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE FAILED A N8TA K NONE X J ENGINE FLAMEOUT WARNING INDICATION TX TAXI/GRND HDL 1 WP 19 506NA 24771 30737 ON TAXI IN TO THE GATE, RIGHT ENGINE FLAMED OUT AND EICAS STATUS MESSAGE R ENG LP PUMP CAME ON. REPLACED TRANSIENT PRES SURE UNIT. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2001020600042 20010206 00042 NM 2001 2 6 TSAA0155001 1 20010108 A 5511 65913631 SPAR BOEING 737 737230 NM HORIZONTAL STAB CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 821AL 23155 IDENTIFIED CRACK AT LEFT HORIZONTAL STABILIZER CENTER SECTION REAR SPAR UPPER CHORD AFT UPPER CLEVIS LUG DURING SCHEDULE D INSPECTION PER ECO 1384R6/SB 737-55-1033R1. (M) 2 L 7 2 4F RT A16WE 2001020600044 20010206 00044 2001 2 6 USAAD01005 4 20010107 A 3418 0861FG4 SENSOR DOUG DC9 DC931 3022065 WP LT AOA FAILED A USAA K NONE J WARNING INDICATION CL CLIMB 1 EA 19 955VJ 47593 MHT-PIT - FLT 1037 - BOTH STALL WARNING SYSTEMS ACTIVATED AT ROTATION. ALL THE STALL WARNING C/B''S WERE PULLED TO STOP WARNING. THE STALL INDICATION FAILURE LIGHT WAS ON. THE ENGINES WERE FIREWALLED FOR 10 SECONDS. MAINTENANCE REPLACED THE LEFT ANGLE OF ATTACH SENSOR. THE ENGINE OPERATION WAS WITHIN LIMITS PER PW MM 72-00 PAGE 518. (M) 2 L 7 2 4F A6WE 2001020600045 20010206 00045 NM 2001 2 6 USAABB01004 1 20010111 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 617AU 27148 LAX - FOUND SEAT MOUNTED LOW LEVEL EMERGENCY LIGHT AT ROW 26 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2001020600046 20010206 00046 WP 2001 2 6 USAAD01006 1 20010106 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 922VJ 48142 DAY - THE OVERHEAD EMERGENCY LIGHTS IN THE FIRST CLASS PASSENGER CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERG ENCY LIGHT POWER SUPPLY. (M) 2 L 7 2 4F A6WE 2001020600047 20010206 00047 WP 2001 2 6 USAAD01008 1 20010111 A 3350 AD4002P BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 820US 49119 CLT - THE EMERGENCY LIGHTS DID NOT COME ON WHEN EXTERNAL POWER FELL OFF LINE. MAINTENANCE REPLACED THE BATTERIES IN THE FORWARD ENTRY EMERGENCY LIGHT PACK. (M) 2 L 7 2 4F A6WE 2001020600048 20010206 00048 WP 2001 2 6 USAAD01007 1 20010111 A 3350 9731044 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 830US 49443 CLT - THE LOW LEVEL EMERGENCY LIGHT AT SEAT ROW 11 STAYS ILLUMINATED. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY . (M) 2 L 7 2 4F A6WE 2001020600049 20010206 00049 WP 2001 2 6 USAAD01009 1 20010115 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 805US 48053 DFW - EMERGENCY LIGHTS FOUND LEFT ON FOR AN UNDETERMINED LENGTH OF TIME. MAINTENANCE REPLACED THE LOW LEVEL LIGHT BATTE RY AT PASSENGER SEAT ROW 30. (M) 2 L 7 2 4F A6WE 2001020600050 20010206 00050 NM 2001 2 6 USAABB01005 1 20010111 A 3350 8731002511REV12 SIGN BOEING 757 7572B7 1384964 NM L1 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 617AU 27148 LAX - FOUND L-1 EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE IDENTIFIER ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001020600051 20010206 00051 2001 2 6 USAAD01003 4 20010106 A 3418 STALL WARNING DOUG DC9 DC931 3022065 WP COCKPIT ACTIVATED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 955VJ 47593 PHL-YYZ - FLT 1633 - AT ROTATION THE STALL WARNING SYSTEM ACTIVATED AND THE FLIGHT CREW FIREWALLED THE ENGINES IN RESPON SE. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET THE STALL WARNING CIRCUIT BREAKE RS AND THE SYSTEM CHECKED NORMAL. ALL ENGINE PARAMETERS STAYED WITHIN LIMITS. THE ENGINES WERE INSPECTED AND CHECKED O K. (M) 2 L 7 2 4F A6WE 2001020600052 20010206 00052 NM 2001 2 6 USAASB01003 1 20010111 A 2730 654513210 COMPUTER BOEING 737 7372B7 1384560 NM EE BAY MALFUNCTIONED A USAA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 EA 19 285AU 17628 23132 BWI - FLT 2709 - EN ROUTE FROM BDL TO MCO, AT FL310, CAPTAIN REPORTED THAT THE FILGHT WAS LEVEL WITH AUTOPILOT ON WHEN T HE AIRCRAFT BEGAN A 600 FEET PER MINUTE DESCENT. CREW DISCONNECTED AUTOPILOT AND ELEVATOR AUTHORITY WAS REDUCED AND MOM ENTARILY JAMMED INPUTS. CAPTAIN THOUGHT THE ELEVATOR WAS JAMMED, SO HE STARTED A SLOW DESCENT. AT FL120, EVERYTHING WA S NORMAL. FLIGHT DIVERTED TO BWI AND LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. CAPTAIN STATED HE HA D FULL CONTROL OF THE AIRCRAFT THE ENTIRE TIME. MAINTENANCE INSPECTED AIRCRAFT ELEVATOR AND ASSOCIATED LINKAGE, TORQUE TUBES, COABLES AND POWER CONTROL UNITS. ACCOMPLISHED AUTOPILOT BITE. NO FAULTS NOTED PER MM 27-31-131. REMOVED AND RE 2 L 7 2 4F A16WE 2001020600053 20010206 00053 GL 2001 2 6 C2XA0CL003 2 20010112 A 7313 23065950 NOZZLE EMB 145 EMB145ER SO ALLSN AE300 AE3007A GL NR 2 ENGINE MALFUNCTIONED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 14945 145049 CLE - FLT 4078 - THE CREW REPORTED SMOKE IN CABIN AND COCKPIT WITH ACTIVATION OF THE DE-ICE SYSTEM DURING HIGH POWER SET TINGS. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE FUE L NOZZLES IAW MM 73-11-10. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001020600054 20010206 00054 NE 2001 2 6 C2XA0CL004 2 20010116 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NR 1 ENGINE FAILED A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING J Y WARNING INDICATION ENGINE STOPPAGE CR CRUISE 1 SW 27 69549 UE194 LEX - FLT 3108 - THE CREW REPORTED NR 1 ENGINE LOST OIL PRESSURE IN FLIGHT AND THE ENGINE SHUT DOWN. THE AIRCRAFT DIVER TED AND LANDED IN CVG WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 2001020600055 20010206 00055 SO 2001 2 6 C2XA01A015 1 20010108 A 5411 12007882001 FRAME EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16729 120185 SHV - DURING MAINTENANCE INSPECTIN, THE LEFT NACELLE HALF FRAME FOR THE LEFT MAIN LANDING GEAR AFT OUTBOARD DOOR FORWARD HINGE POINT WAS FOUND TO BE CRACKED. THE AIRCRAFT WAS FERRIED TO IAH WHERE IT LANDED WITHOUT INCIDENT, AND MAINTNANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED HALF FRAME IAW EMB120 SRM 54-20-04, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001020600059 20010206 00059 SO 2001 2 6 C2XA01IA014 1 20010107 A 5280 12004499001 BUSHING EMB 120 EMB120RT SO NLG DOOR WORN A C2XA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 27 22727 120177 IAH - FLT 2944 - THE CREW REPORTED THAT UPON RETRACTION, THE LEFT MAIN LANDING GEAR REMAINED DOWN AND LOCKED, NOSEWHEEL GEAR DOORS REMAINED OPEN, WITH AN EXTREME VIBRATION FROM THE FRONT OF THE AIRCRAFT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE HINGE BUSHINGS ON THE LEFT MAIN GEAR FORWARD OUTBOARD DOOR. THE AIR CRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001020600060 20010206 00060 SO 2001 2 6 C2XA01IA021 1 20010113 A 5280 12012347001 DOOR LATCH EMB 120 EMB120RT SO LEFT MLG BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 22727 120177 IAH - FLT 2980 - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THE LEFT MAIN LANDING GEAR, FORWARD, OUTBOARD, DOOR WO ULD NOT STAY LATCHED. FOUND HANGING DOWN. MAINTENANCE REMOVED AND REPLACED THE LEFT FORWARD OUTBOARD GEAR DOOR LATCH H ANDLE IAW EMB-120 MM 52-81-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001020600061 20010206 00061 SO 2001 2 6 C2XA01IA020 1 20010131 A 3350 BS2197 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15725 18564 120173 IAH - FLT 2926 - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE CABIN FLOOR EMERGENCY LIGHTS WOULD NOT OPERATE. MAINTENANCE REMOVED AND REPLACED THE NR 2 POSITION EMERGENCY LIGHT BATTERY PACK IAW EMB-120 MM 33-50-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001020600062 20010206 00062 SO 2001 2 6 C2XA01IA019 1 20010110 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN MALFUNCTIONED A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 40717 120133 BTR - FLT 3533 - THE CREW REPORTED THAT THE FORWARD CABIN EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE APPLIED PO WER TO THE AIRCAFT AND PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM IAW EMB-120 MM 33-50-00. NO DEFE CTS WERE NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001020600063 20010206 00063 SO 2001 2 6 C2XA01IA018 1 20010113 A 3350 AD2047 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 22727 120177 IAH - FLT 4376 - DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE RIGHT OVERWING EXTERIOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 POSITION EMERGENCY LIGHT BATTERY PACK IAW EMB-120 MM 33-52-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001020600064 20010206 00064 SO 2001 2 6 C2XA01IA017 1 20010113 A 5280 12012347002 DOOR LATCH EMB 120 EMB120RT SO RT MLG BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27716 120128 IAH - DURING A SERVICE CHECK, MAINTENANCE THE RIGHT MAIN LANDING GEAR, FORWARD, OUTBOARD, DOOR WOULD NOT STAY LATCHED. MAINTENANCE REMOVED AND REPLACED THE RIGHT FORWARD OUTBOARD GEAR DOOR LATCH-HANDLE IAW EMB-120 MM 52-81-01. THE AIRCRAF T WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001020600065 20010206 00065 SO 2001 2 6 C2XA01IA016 1 20010112 A 3260 922AA2YA6PZ722 PROXIMITY SWITCH EMB 120 EMB120RT SO RT MLG DIRTY A C2XA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SW 27 27716 120128 IAH - FLT 2934 - THE CREW REPORTED THE RIGHT MAIN LANDING GEAR, SYSTEM A RED, RED UNLOCK INDICATOR LIGHT TO ILLUMINATE I NTERMITTENTLY ON THE GROUND DURING TAXI. MAINTENANCE CLEANED THE RIGHT MAIN LANDING GEAR DOWN LOCK PROXIMITY SWITCH AND VERIFIED NORMAL OPERATION IAW EMB-120 MM 32-60-04. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001020700002 20010207 00002 NM 2001 2 7 CALA0100066 1 20010123 A 5315 FLOORBEAM BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19623 27527 INSPECTION FOUND FLOORBEAM CORRODED AT STA 947 BETWEEN LBL 27 AND RBL 5. THE FLOORBEAM WAS REPAIRED BY INSTALLING SPLIC ES IAW ECRA 5310-04095. 2 L 7 2 4F RT A16WE 2001020700003 20010207 00003 WP 2001 2 7 CALA0100067 1 20010124 A 5230 FITTING DOUG DC9 DC982 3022082 WP MID CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND A 1 INCH CRACK IN MID CARGO DOOR FITTING AND WITH UPPER INTERCOSTAL CLIP CRACKED. THE FITTING AND T-AN GLE WERE REMOVED AND A NEW FITTING AND ANGLE WERE INSTALLED IAW SRM 51-10-4, 51-30-2, AND 51-30-1. 2 L 7 2 4F A6WE 2001020700004 20010207 00004 WP 2001 2 7 CALA0100069 1 20010125 A 5312 STRUCTURE DOUG DC10 DC1030 3023501 WP BULKHEAD CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13088 46850 INSPECTION FOUND REAR PRESSURE BULKHEAD T- SECTION CORRODED AT STA 2007, X = 24. THE T-SECTION WAS REPAIRED IAW SRM 53- 40-00. 2 L 7 3 4F A22WE 2001020700005 20010207 00005 WP 2001 2 7 CALA0100070 1 20010125 A 5320 FLOOR SUPPORT DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13088 46850 INSPECTION FOUND GALLEY NR 7 I/B SUPPORT BEAM CORRODED AT STA Y = 1900-1997, X = 45R. A NEW BEAM WAS INSTALLED IAW SRM 53-16-01. 2 L 7 3 4F A22WE 2001020700006 20010207 00006 WP 2001 2 7 CALA0100071 1 20010125 A 5280 STRUCTURE DOUG DC9 DC982 3022082 WP LT MLG DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND TWO 1 INCH CRACKS IN FORWARD LOWER CORNER OF LT MLG I/B DOOR. THE CRACKS WERE STOP DRILLED AND DOUBLER S WERE INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-2, 51-30-5, AND EA 9-5331-2-A0831. 2 L 7 2 4F A6WE 2001020700007 20010207 00007 WP 2001 2 7 MWEA010122 1 20010125 A 5330 99234883 DOUBLER DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 CORROSION FOUND ON UPPER SURFACE OF INNER DOUBLER AT STATION 579 BETWEEN LONGERON 29 RIGHT AND LONGERON 30. MAINTENANCE FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 2001020700008 20010207 00008 EU 2001 2 7 C2XA01IA046 1 20010110 A 5410 S5411058620100 CHANNEL AEROSP ATR42 ATR42320 8680930 EU LEFT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14832 187 YYZ - DURING C-CHECK INSPECTION, THE LEFT HAND UPPER COWLING (425AT) WAS FOUND TO BE CRACKED AT THE LEFT HAND CHANNEL. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CHANNEL IN ACCORDANCE WITH ATR42-320 SRM 54-12-61, AND 51-25-01, AND THE A IRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001020700009 20010207 00009 NM 2001 2 7 QXEA0100043 1 20010117 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- LEFT HAND INBOARD SEAT TRACK HAS LIGHT CORROSION ON TOP AREA AT STATION X456.500. REPAIRED IAW HORIZON AIR EA 9-53 -592 AND DHC-8 RD8-53-1339, AND SRM 51-20-16, PAGE 1-4. 2 H 7 2 4T RT A13NM 2001020700010 20010207 00010 NM 2001 2 7 QXEA0100044 1 20010117 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- LEFT HAND INBOARD SEAT TRACK HAS RAISED MATERIAL AT STATION X424.124. REPAIRED IAW HORIZON AIR EA 9-53-592, AND DH C-8 RD8-53-1339, AND SRM 51-20-13, PAGES 1-4. 2 H 7 2 4T RT A13NM 2001020700011 20010207 00011 NM 2001 2 7 QXEA0100045 1 20010114 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- LEFT HAND INBOARD SEAT TRACK HAS LIGHT PITTING ON TOP AT STATION X282.400. REPAIRED IAW DHC-8 RD8-53-1339. 2 H 7 2 4T RT A13NM 2001020700012 20010207 00012 NM 2001 2 7 QXEA0100046 1 20010114 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- LEFT HAND OUTBOARD SEAT TRACK HAS SOME SMALL PITTING AT STATION X307.400. REPAIRED IAW DHC-8 SRM 51-40-00, PAGES 1 -4 AND RD8-51-102 AND RD8-53-1339. 2 H 7 2 4T RT A13NM 2001020700014 20010207 00014 EU 2001 2 7 AALA20010035 1 20010107 A 5313 LONGERON AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 40064 507 TUL - FOUND CORROSION ON LONGERON 50L AT FRAME 59. CUT OUT CORRODED SECTION AND SPLICED IN NEW SECTION PER SRM 53-10-14 FIG 203. (M) 2 L 7 2 4F RT A35EU 2001020700015 20010207 00015 EU 2001 2 7 AALA20010036 1 20010107 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 40064 507 TUL - FOUND CORROSION ALONG STRINGER 52L FRAME 57.3-58. REMOVED AND REPLACED FACTORY SPLICE PER SRM 51-72-00. (M) 2 L 7 2 4F RT A35EU 2001020700016 20010207 00016 EU 2001 2 7 AALA20010015 1 20010102 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 19059 469 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIGN AT REAR CABIN INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT CO NNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2001020700017 20010207 00017 EU 2001 2 7 AALA20010014 1 20010101 A 3350 5647141 SWITCH AIRBUS 300 A300B4605R 3930308 EU COCKPIT MALFUNCTIONED A AALA K NONE O OTHER CR CRUISE 1 SW 21 19059 469 MIA - FLT 9513 - EN ROUTE LIM-MIA, EMERGENCY EXIT LIGHT CYCLED ON AND OFF DURING FLIGHT. LANDED MIA WITHOUT FURTHER INC IDENT. REPLACED EMERGENCY EXIT ARM/DISARM SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2001020700018 20010207 00018 WP 2001 2 7 AALA20010075 1 20010113 A 3350 SPRING DOUG DC9 DC982 3022082 WP AIRSTAIR BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70404 49315 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SP RINGS AT AFT AIRSTAIRS. SYSTEM GROUND CHCKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001020700019 20010207 00019 WP 2001 2 7 AALA20010080 1 20010114 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7535A 49989 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 7D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001020700020 20010207 00020 WP 2001 2 7 AALA20010041 1 20010111 A 3397 WIRE DOUG DC9 DC982 3022082 WP TAIL LOOSE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 494AA 49732 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT TAIL COMPARTMENT INOPERATIVE. RE-SECURED EMERGENCY EXIT WIR E AT TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001020700021 20010207 00021 WP 2001 2 7 AALA20010081 1 20010113 A 2910 B-NUT DOUG DC9 DC982 3022082 WP HYDRALIC SYSTEM LOOSE A AALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 587AA 53250 ORD - FLT 864 - EN ROUTE MCI-ORD, LOST LEFT SIDE HYDRAULIC FLUID. LEFT SIDE LOW PRESSURE LIGHT ILLUMINATED. ACCOMPLISH ED EMERGENCY PROCEDURES PER THE CHECKLIST. LANDED ORD WITHOUT FURTHER INCIDENT. RE-SECURED LEFT SIDE HYDRAULIC FILTER LINE B-NUT. SERVICED LEFT SIDE HYDRAULIC SYSTEM. PERFORMED LEAK CHECK PER THE MM. NO LEAKS NOTED. SYTEM GROUND CHECK ED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001020700024 20010207 00024 NM 2001 2 7 AALA20010070 1 20010108 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 875AA 21387 TUL - FOUND BULGE IN FUSELAGE SKIN STATION 1013 BETWEEN STRINGER 9R/10R, CORROSION ON SKIN. REPAIRED PER SRM 53-30-3, P ART 1 FIG 1 SHEET 4, INSTALLED DOUBLER. (M) 2 L 7 3 4F A3WE 2001020700026 20010207 00026 NM 2001 2 7 AALA20010072 1 20010102 A 5311 FRAME BOEING 727 727223 1384074 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 875AA 21387 TUL - FOUND FS 303 FRAME CRACKED .625 INCH AT STRINGER 16L CUTOUT. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SB 727-53-153 R5. (M) 2 L 7 3 4F A3WE 2001020700027 20010207 00027 NM 2001 2 7 AALA20010073 1 20010110 A 5320 ANGLE BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 875AA 21387 TUL - FOUND CORROSION ON UPPER CHORD ANGLE AT STATION 1213. REMOVED CORROSION AND INSTALLED .032 17-7PH ANGLE REPAIR WI TH .25 INCH HI-LOCK PER ESO 11697 DATED 1/4/01. (M) 2 L 7 3 4F A3WE 2001020700028 20010207 00028 NM 2001 2 7 AALA20010018 1 20010101 A 2120 UNKNOWN BOEING 757 757223 1384957 NM CABIN ODOR A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 611AM 24487 ABQ - FLT 160 - EN ROUTE SAN-JFK, DETECTED A STRONG SMELL AT L2 AND R2 DOORS. DIVERTED ABQ AND LANDED WITHOUT FURTHER I NCIDENT. CLEANED ENTIRE PACK SYSTEM. ACCOMPLISHED ADJUSTMENT SYSTEM TEST ON RIGHT SIDE ENGINE BLEED SYSTEM. PERFORMED HIGH POWER ENGINE RUN UP. NO SMELL NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001020700029 20010207 00029 NM 2001 2 7 AALA20010022 1 20010106 A 2780 340545 VALVE BOEING 757 757223 1384957 NM LT ACM BAY LEAKING A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SW 21 643AA 24601 SNA - FLT 1409 - EN ROUTE DFW-SNA UPON LANDING, TOWER REPORTED SMOKE AT RIGHT SIDE TIRES. LANDED SNA WITHOUT FURTHER IN CIDENT. REPLACED LEFT SIDE SLAT BYPASS VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001020700031 20010207 00031 NM 2001 2 7 DLM88010062 1 20010112 A 3320 POWER SUPPLY DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 975DL 53243 PWR SUPPLY WILL NOT LIGHT LIGHTS/F1 AND F2 OPEN. REPLACED PWR SUPPLY. 2 L 7 2 4F RT A6WE 2001020700032 20010207 00032 NM 2001 2 7 DL733010066 1 20010113 A 2170 COALESCER BAG BOEING 737 737347 1384647 NM ACM BAY ODOR A DALA C ABORTED TAKEOFF C F.O.D. TO TAKEOFF 1 SO 27 304WA 23345 BIRD STRIKE NR 2 ENGINE IN CLIMBOUT. HIT BIRD AT ABOUT 500 FT AGL. ENGINE PARAMETERS NORMAL, BAD ODOR IN AIRCRAFT. PE RFORMED BIRD STRIKE INSPECTION PER MM PROCEDURES. FOUND EVIDENCE OF BIRD STRIKE NR 2 ENGINE. NO DAMAGE NOTED. REPLACE D COALESCER BAG RT PACK/RAN ENGINE. ALL PARAMETERS NORMAL PER MM BORESCOPE OF ENGINE. DELAYED 10 CYCLES OR 15 HOURS. ATL NOTIFIED. 2 L 7 2 4F RT A16WE 2001020700033 20010207 00033 NM 2001 2 7 DL73K010075 1 20010115 A 2120 DUCT BOEING 737 737232 1384475 NM LEFT A/C PACK RUPTURED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 324DL 23096 FLIGHT ATTENDANT HEARD POP IN OVERHEAD NEAR FRONT OF A/C JUST AFTER INITIATION OF T/O POWER. ANOTHER POP AT V1. AFT ER T/O SMOKE FILLED CABIN. AFTER DISCOVERY OF SMOKE IN CABIN SHUT OFF PACKS. SMOKE STARTED TO DISSIPATE. FOUND LEFT P ACK MIX CHAMBER DUCT BLOWN AND DIST DUCT DAMAGE. REPLACED BOTH DUCTS AND INSPECTED AND REPLACED BOTH COALESCER BAGS. A LL LEAK CK GOOD. 2 L 7 2 4F RT A16WE 2001020700034 20010207 00034 NE 2001 2 7 DLM88010079 2 20010114 A 7200 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 STALLED A DALA O OTHER E B J VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 27 938DL 22768 49811 726015 AT FL 290 HAD WHAT APPEARED TO BE COMPRESSOR STALL IN LT ENGINE EPR DECREASED AND RAPIDLY INCREASE BACK TO NORMAL. FELT HARD JOLT MOMENTARY OFF FLAG IN STBY ADI. SMELL OF RUBBER BURNING. FELT SLIGHT VIBRATION FOR REMAINDER OF FLT. FOUND NR 1 ENG FAN BLADE DAMAGE, 1 WITH TEAR AND 6 OTHER BLADES BENT. C/W BORO OF 6/7-5/6 COMPRESSOR AND 1/2/5/6, TURBINE BL ADES PER M/M 72-33-21-8. NO DISCREPANCIES FOUND. ITEM FOR BLADE DISCREPANCIES TRANSFERRED TO ITEM 4. REPLACED BLADES. 2 L 7 2 4F 4 F RT A6WE E9NE 2001020700046 20010207 00046 WP 2001 2 7 CALA0100068 1 20010124 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND CUSP ANGLE AT L-1 DOOR, FS 200, LBL 54 CORRODED. THE CUSP ANGLE WAS REMOVED AND REPLACED IAW EA 9-5310 -2-A0829 AND ECRA 5310-04094. 2 L 7 2 4F A6WE 2001020700047 20010207 00047 NM 2001 2 7 QXEA0100047 1 20010114 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- LEFT HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION AT STATION X434.500. REPAIRED IAW DHC-8 RD8-53-1342. 2 H 7 2 4T RT A13NM 2001020700048 20010207 00048 NM 2001 2 7 QXEA0100048 1 20010114 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- LEFT HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION AT STATION X405.737. REPAIRED IAW DHC-8 RD8-53-1342. 2 H 7 2 4T RT A13NM 2001020700049 20010207 00049 NM 2001 2 7 QXEA0100049 1 20010114 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- LEFT HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION AT STATION X376.110. REPAIRED IAW DHC-8 RD8-53-1342. 2 H 7 2 4T RT A13NM 2001020700050 20010207 00050 NM 2001 2 7 QXEA0100050 1 20010111 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- CORROSION UNDER BOLTHEAD ON STRAP ON INBOARD SIDE OF SEAT TRACK AT STATION X597.5 AND STRINGER 31L. REPAIRED IAW D HC-8 20-14-01 AND SRM 51-20-16, AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2001020700051 20010207 00051 NM 2001 2 7 QXEA0100051 1 20010115 A 3220 ARM DHAV DHC8 DHC8102 2809003 NM NLG GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- NOSE LANDING GEAR TRAILING ARM HAS A GOUGE WITH RAISED METAL. REPAIRED IAW DHC-8RD 8-32-289. 2 H 7 2 4T RT A13NM 2001020700052 20010207 00052 NM 2001 2 7 QXEA0100052 1 20010114 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- RIGHT HAND INBOARD SEAT TRACK AT STATION X257 HAS PITTING CORROSION. REPAIRED IAW HORIZON AIR EA 9-53-589 AND DHC- 8 RD8-53-1339. 2 H 7 2 4T RT A13NM 2001020700053 20010207 00053 NM 2001 2 7 C1HA200184002 1 20010119 A 2750 M59391130ZE4C MOTOR BOEING 727 7272S7 138407Z NM TE FLAPS LEAKING A C1HA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 15 684CA 22491 A-SYSTEM HYDRAULIC FAILURE FOLLOWED APPROPRIATE PROCEDURES AND CHECKLIST. REMOVED AND REPLACED NR 1 HYDRAULIC PUMP, FOU ND O/B FLAP DRIVE MOTOR LEAKING. REPLACED SAME, REPLACED CASE DRAIN AND PRESSURE FILTERS. 2 L 7 3 4F A3WE 2001020700054 20010207 00054 SO 2001 2 7 GLBA2001008 1 20010120 A 3233 20885 ACTUATOR EMB 120 EMB120ER 3260203 SO LT MLG INOPERATIVE A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 297UX 292 120297 RETURN TO BLOCK, LEFT GEAR WOULD NOT RETRACT ON T/O. REMOVED AND REPLACED UPLOCK ACTUATOR. 2 L 7 2 4T RT A31SO 2001020700055 20010207 00055 2001 2 7 GLBA2001009 4 20010121 A 3414 INDICATOR BEECH 1900 1900D 1154162 CE AIRSPEED SPLIT A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 01 219GL UE219 ABORTED T/O, AIRSPEED INDICATOR SPLIT ON ROLL-OUT. INSPECTED SYSTEM, PERFORMED HIGH SPEED TAXI, COULD NOT DUPLICATE. 2 L 7 2 4T RT A24CE 2001020700056 20010207 00056 NE 2001 2 7 GLBA2001010 2 20010123 A 7520 12938000111 BYPASS VALVE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE PRECOOLER INOPERATIVE A GLBA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 01 226GL 8701 127 UE226 RETURN TO BLOCK, RIGHT BLEEDAIR FAIL. REMOVED AND REPLACED TEMP CONTROL SENSOR AND PRECOOLER BYPASS VALVE, SYSTEM OPS C HECKED GOOD. 2 L 7 2 4T 4 T RT A24CE E26NE 2001020700057 20010207 00057 SO 2001 2 7 GLBA2001012 1 20010124 A 3260 922AA2YA6PZ722 SENSOR EMB 120 EMB120ER 3260203 SO MLG SHORTED A GLBA O OTHER O OTHER AP APPROACH 1 CE 01 297UX 120297 MLG CB POPPED, NO GREEN (DOWNLOCK) INDICATION ON B-SYSTEM. REMOVED AND REPLACED PROX SENSOR, SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT A31SO 2001020700058 20010207 00058 WP 2001 2 7 DHL2001805002 1 20010112 A 2424 CURRENT LIMITER DOUG DC8 DC873F 302199F WP SPOILER PUMP FAILED A DHLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 802DH 46076 SPOILER PRESSURE 0, PREFORMED ALT PROCEDURE. REMOVED AND REPLACED SPOILER PUMP CURRENT LIMITERS. OPS CHK OK PER M/M 27 -62-0. 2 L 7 4 4F RT 4A25 2001020700059 20010207 00059 NM 2001 2 7 DHL2001727007 1 20010125 A 5347 SEAT TRACK BOEING 727 727228 NM FUSLEAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 SEAT TRACK DAMAGED BS 1110 TO 1130 RBL 45. REPAIRED PER SRM 53-10-5. 2 L 7 3 4F A3WE 2001020700060 20010207 00060 NM 2001 2 7 DHL2001727008 1 20010125 A 5313 STRINGER BOEING 727 727228 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 STRINGER 26L DAMAGED, BETWEEN BS 720C AND 720F. REPAIRED PER SRM 53-10-3. 2 L 7 3 4F A3WE 2001020700061 20010207 00061 NM 2001 2 7 DHL2001727009 1 20010125 A 5347 SEAT TRACK BOEING 727 727228 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 SEAT TRACK DAMAGED. REPAIRED SEAT TRACK BETWEEN BS 110 AND 1130, RBL 55 PER SRM 53-10-5. 2 L 7 3 4F A3WE 2001020700062 20010207 00062 NM 2001 2 7 DHL2001727010 1 20010125 A 5311 FRAME BOEING 727 727228 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 CIRCUMFERENTIAL FRAME CRACKED. REPAIRED FRAME PER SRM 51-40-3. 2 L 7 3 4F A3WE 2001020700063 20010207 00063 WP 2001 2 7 TWAA0101601 1 20010125 A 3350 58222 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 953U 49267 THE EGRESS LIGHTS FROM ROW 30 TO AFT LAVS COME ON WHEN SWITCH IS ARMED. REPLACED POWER SUPPLY. CHECK-C 3-21-00 MCI. 2 L 7 2 4F A6WE 2001020700064 20010207 00064 WP 2001 2 7 TWAA0101602 1 20010121 A 3350 58222 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 995Z 47027 THE EMERGENCY CABIN LIGHTS AT THE LEFT NUMBER 1 CABIN DOOR, RT NUMBER 1, AND COCKPIT DOORS CAME ON WHEN THE SWITCH IS AR MED. REPLACED THE BATTERY PACK. CHECK-C 1-2-01 STL. 2 L 7 2 4F A6WE 2001020700065 20010207 00065 WP 2001 2 7 TWAA0101603 1 20010121 A 3350 408822101 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9405T 53141 THE FWD ENTRY AND COCKPIT DOOR EMERGENCY LIGHTS, AND THE EGRESS LIGHTS ROWS 18 TO 22, WERE INOPERATIVE. REPLACED THE BA TTERIES FOR THE EMERGENCY LIGHTS, AND RECONNECTED WIRING THAT WAS DISCONNECTED FOR THE EGRESS LIGHTS. CHECK-C 10-23-00 STL. 2 L 7 2 4F RT A6WE 2001020700066 20010207 00066 2001 2 7 TWAA0101604 4 20010125 A 2565 61571127 BOTTLE BOEING 757 7572Q8 1384972 NM ESCAPE SLIDE DISCHARGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 703TW 27620 THE LEFT SIDE NUMBER 4 CABIN DOOR EVACUATION SLIDE HAD LOW BOTTLE PRESSURE. REPLACED THE SLIDE ASSEMBLY. CHECK-C 9-27- 99 LAX. 2 L 7 2 4F RT A2NM 2001020700067 20010207 00067 2001 2 7 ARWA0010102 4 20010125 A 3442 BA170 BALLAST DOUG DC8 DC862 3021970 WP CABIN SMOKE A ARWA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 19 1808E 46105 DURING DESCENT, CO-PILOTS RADAR SCREEN HAD EVIDENCE OF SMOKE. TURNED OFF AND PULLED C/B. CHECKED WEATHER RADAR SYSTEM WIRING IAW W/D 34-10-0, FOUND NORMAL. GROUND OPERATIONAL CHECK IAW FDW M/M 34-41-0. NORMAL, NO TROUBLE FOUND. REF TO I TEM NR 1, FOUND EVIDENCE OF SMOKE AND BURN SMELL COMING OUT OF GLARESHIELD INST-WHITE BALLAST XFMR. REMOVED AND REPLACE D INST-WHITE LT XFMR IAW M/M 33-12-0. TESTED NORMAL. 2 L 7 4 4F 4A25 2001020700068 20010207 00068 EU 2001 2 7 MALA010136 1 20010120 A 2750 CONTROL UNIT BAC 146 AVRO146RJ85A 1500097 EU TE FLAPS DEACTIVATED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 502XJ E2307 FLAPS WOULD NOT EXTEND WHEN ELECTED TO 18 DEGREES, FLAPS WOULD NOT MOVE OUT OF 0 DEGREES. CREW GOT A FLAP INOP, FLAP FA ULT LIGHT ON. MAINTENANCE RESET A/C POWER, PERFORMED FLAP FAULT RESET. ALL CHECKS GOOD AT THIS TIME. 2 H 7 4 4F RT A49EU 2001020700069 20010207 00069 EU 2001 2 7 MALA010137 1 20010122 A 2421 31342001 GENERATOR SAAB SF340 340B 7860101 EU RIGHT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 437XJ 340B437 RIGHT AC GENERATOR CAUTION LIGHT CYCLES ON AND OFF ABOUT EVERY 6 SECONDS WITH ANIT-ICE ON. PROBLEM PERSISTED AFTER ORH RECYCLING. MAINTENANCE REPLACED RIGHT AC GEN P/N 31342-001, S/N ON 755, SN OFF 98046. ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2001020700070 20010207 00070 NE 2001 2 7 MALA010138 2 20010123 A 7530 216035039 BLEED VALVE BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 3 ENGINE BROKEN A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 515XJ E2333 DURING CLIMBOUT FROM MSP, NR 3 ENGINE WAS RUNNING EXTREMELY WARM. RECEIVED TRIM DOWN INDICATION, NOTICED N2 WAS HIGHER THAN THE OTHER 3 ENGINES, FUEL FLOW WAS NOTICEABLY LESS AND N1 WAS LESS THAN OTHER 3 ENGINES. RETURNED TO MSP, TRIED FA DEC OFF, ENGINE PARAMETERS DID NOT CHANGE WITH FADEC OFF AND ENGINE ANTI-ICE ON, THRUST WAS LESS ON N1 WHEN N2 WAS EVEN WITH THE OTHER ENGINES. COMPLETED ORH PROCEDURES FOR FADEC OFF. MAINTENANCE FOUND NR 3 ENGINE BLEED BAND BROKEN. REPL ACED BLEED BAND PN 2-161-182-16 AND ACTUATOR PN 2-160-350-39, SN ON XRC8-63, SN OFF 98E004, IAW AMM 75-30-03. ADJUSTMEN T TEST 75-30-04. OPS CHECK GOOD. POWER CHECK GOOD. 2 H 7 4 4F 4 F RT A49EU E6NE 2001020700071 20010207 00071 NM 2001 2 7 RAAA01B208 1 20010124 A 3350 8621014 BATTERY INTVLV BOEING 727 72722C 138400F NM PAX CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 AT END OF SCHEDULED B3 MAINTENANCE CHECK, AFT LT WING EXIT INDENTIFIER INOP. REPLACED BATTERY AND TESTED PER RAA ECO 86 -26. 2 L 7 3 4F A3WE 2001020700072 20010207 00072 NM 2001 2 7 RAAA01B209 1 20010124 A 3350 8621014 BATTERY INTVLV BOEING 727 72722C 138400F NM PAX CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 AT END OF SCHEDULED B3 MAINTENANCE CHECK, FWD ENTRY DOOR EXIT IDENTIFIER INOP. REPLACED BATTERY AND TESTED PER RAA ECO 86-26. 2 L 7 3 4F A3WE 2001020700073 20010207 00073 NM 2001 2 7 RAAA01B2010 1 20010104 A 3350 8621014 BATTERY INTVLV BOEING 727 72722C 138400F NM PAX CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 AT END OF SCHEDULED B3 MAINTENANCE CHECK, RT AFT OVERWING EXIT IDENTIFIER INOP. REPLACED BATTERY AND TESTED PER RAA ECO 86-26. 2 L 7 3 4F A3WE 2001020700074 20010207 00074 NM 2001 2 7 RAAA01B2012 1 20010124 A 3350 86210014 BATTERY INTVLV BOEING 727 72722C 138400F NM PAX CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 AT END OF SCHEDULED B3 MAINTENANCE CHECK, RT ROW 11 EXIT IDENTIFIER INOP. REPLACED BATTERY AND TESTED PER RAA ECO 86-26 . 2 L 7 3 4F A3WE 2001020700075 20010207 00075 NM 2001 2 7 RAAA01B2013 1 20010124 A 3350 86210066 BATTERY INTVLV BOEING 727 72722C 138400F NM PAX CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 AT END OF SCHEDULED B3 MAINTENANCE CHECK, FLOOR PROXIMITY LIGHT INOP AT SEAT ROW 13 DEF. REPLACED BATTERY AND TESTED PE R ECO 86-26. 2 L 7 3 4F A3WE 2001020700076 20010207 00076 NM 2001 2 7 RAAA01B2014 1 20010124 A 3350 86210066 BATTERY INTVLV BOEING 727 72722C 138400F NM PAX CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 AT END OF SCHEDULED B3 MAINTENANCE CHECK, FLOOR PROXIMITY LIGHT AT SEAT ROW 22 ABC. REPLACED BATTERY AND TESTED PER RAA ECO 86-26. 2 L 7 3 4F A3WE 2001020700077 20010207 00077 NM 2001 2 7 RAAA01B2015 1 20010124 A 3350 8610066 BATTERY INTVLV BOEING 727 72722C 138400F NM PAX CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 AT END OF SCHEDULED B3 MAINTENANCE CHECK, FLOOR POXIMITY LIGHT INOP AT SEAT ROW 14 DEF. REPLACED BATTERY AND TESTED PER RAA ECO 86-26. 2 L 7 3 4F A3WE 2001020700078 20010207 00078 NM 2001 2 7 UPS01234749 1 20010107 A 5522 652564053 SKIN PANEL BOEING 727 72731C 1384011 NM LT ELEVATOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C CORROSION IN LT ELEVATOR UPPER SKIN UNDER STATIC DISCHARGER AT FS 238. SKIN REPLACED IAW DRAWING NR 6 5-25640. 2 L 7 3 4F A3WE 2001020700079 20010207 00079 NM 2001 2 7 AALA20010020 1 20010103 A 2913 PV324O2F PUMP BOEING 757 757223 1384957 NM RT ENGINE LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 645AA 24603 LAX - FLT 181 - EN ROUTE BOS-LAX, DETECTED RIGHT SIDE HYDRAULIC QUANTITY LOSS. LANDED LAX WITHOUT FURTHER INCIDENT. RE PLACED RIGHT SIDE HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001020700080 20010207 00080 NM 2001 2 7 20010207SG001 1 20010111 A 2424 734284A GCU BOEING 757 75728A 1384976 NM LT ENGINE MALFUNCTIONED A AMTA A UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 521AT 24368 DURING CRUISE, EICAS MESSAGE ''LT GEN OFF'' DISPLAYED AND ''GEN OFF'' LIGHT ILLUMINATED. GENERATOR RESET, NO HELP. EIC AS MESSAGE ''L AC BUT OFF'' REMAINED DISPLAYED. CREW SMELLED BURN ODOR IN THE FLT COMPT, NO SMOKE. UNSCHEDULED LANDING PERFORMED WITHOUT FURTHER INCIDENT. REPLACED LEFT GCU PER MM 24-2-02, OPS CHECKED OK. (M) 2 L 7 2 4F RT A2NM 2001020700081 20010207 00081 NM 2001 2 7 20010207SG002 1 20010117 A 5210 NUT PLATE BOEING 727 727208 138407W NM L1 DOOR DAMAGED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 780AT 22295 DURING PREFLIGHT, FOUND THE L1 DOOR LOWER ATTACH POINT ON THE DOOR STRUCTURE SIDE HAS PULLED AWAY FROM THE DOOR STRUCTUR E. REPLACED NUT PLATES ON LOWER L1 DOOR HINGE ATTACH FITTING PER SRM 51-30-2. (M) 2 L 7 3 4F RT A3WE 2001020700082 20010207 00082 NM 2001 2 7 20010207SG003 1 20010120 A 2560 BRACKET BOEING 727 727227 1384078 NM L1 DOOR BROKEN A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 766AT 21999 DURING PREFLIGHT, FOUND THE L1 DOOR RETAINING BRACKET FOR THE GIRT BAR BROKEN. REPLACED BRACKET. (M) 2 L 7 3 4F A3WE 2001020700084 20010207 00084 EA 2001 2 7 MASA01007 1 20010109 A 2613 356024310 SENSING ELEMENT CNDAIR CL600 CL6002B19 EA RIGHT PYLON INTERMITTENT A MASA A UNSCHED LANDING M OVER TEMP CR CRUISE 1 SW 07 27314 7314 FTL - 5822 - LGA-IAD - DIVERTED TO PHL DUE TO 14TH STAGE OVERHEAT MESSAGE ON EICAS. THE CAPTAIN RETARDED THE RIGHT POWE R LEVER AND AFTER 3-5 MINUTES THE MESSAGE CLEARED AND FLICKERED ON AND OFF INTERMITTENTLY. AFTER LANDING IN PHL MAINTEN ANCE WAS CALLED. MAINTENANCE REMOVED AND REPLACED THE 14TH STAGE DUCT SENSING LOOP. OP CHECKS GOOD ON GROUND POWER TUR N UP. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001020700085 20010207 00085 EA 2001 2 7 MASA01004 1 20010108 A 2610 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT ACTIVATED A MASA E ENGINE SHUTDOWN M OVER TEMP CR CRUISE 1 SW 07 27314 7314 FLT 5780 - PHL-BHM - PILOT REPORTED A 14TH STAGE DUCT WARNING MESSAGE. UPON COMPLETION OF THE CHECK LIST AN INFLIGHT SH UT DOWN WAS INITIATED. THE AIRCRAFT MADE AN UNEVENTFUL ONE ENGINE LANDING AT BHM. MAINTENANCE INSPECTED SYSTEM, MAINTE NANCE PERFORMED A HIGH POWER ENGINE TURN ON THE AIRCRAFT. COULD NOT DUPLICATE. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001020700087 20010207 00087 NM 2001 2 7 UPS01234762 1 20010117 A 2910 HEAT EXCHANGER BOEING 727 72722C 138400F NM HYD SYSTEM LEAKING A IPXA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, RT WING HYDRAULIC HEAT EXCHANGER LEAKING HYD FLUID INTO NR 3 TANK. ACCOMPLISHED RIGHT WING HYDRAULIC COOLER ANTI-ROTATION PLATE REPLACEMENT IAW AVITAS ENGINEERING REPAIR ORDER AVHM-187RO-1. 2 L 7 3 4F A3WE 2001020700088 20010207 00088 NM 2001 2 7 UPS01234764 1 20010103 A 5230 SKIN BOEING 727 72722C 138400F NM CARGO DOOR BULGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, MAIN CARGO DOOR OUTER SKIN BULGING AT BS 610, STR 4L. INSTALLED DOUBLER REPAIR IAW 52-30-01. 2 L 7 3 4F A3WE 2001020700089 20010207 00089 NM 2001 2 7 UPS01234765 1 20010111 A 5311 FRAME BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, LEFT WHEEL WELL CASTING FRAME BS 930 SHOWS CRACK TO LOWER END STR 18L. INSTALLED REPAIR AT BS 930 CA STING FRAME IAW UPS EO B727-5310-2611B. 2 L 7 3 4F A3WE 2001020700090 20010207 00090 NM 2001 2 7 UPS01234766 1 20010102 A 5330 SKIN BOEING 727 72722C 138400F NM FUSELAGE BULGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, SKIN BULGING BETWEEN STR 5R AND STR 6R AT STA 481. INSTALLED REPAIR DOUBLER IAW UPS EO B727-5310-137 1E. 2 L 7 3 4F A3WE 2001020700091 20010207 00091 NM 2001 2 7 UPS01234767 1 20010103 A 5754 ANGLE BOEING 727 72722C 138400F NM NR 6 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, RT WING NR 6 LE SLAT, O/B TRACK RECESS CUTOUT, I/B VERT ANGLE CRACKED AT LWR END. REMOVED AND REPLAC ED I/B VERT ANGLE IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2001020700099 20010207 00099 NM 2001 2 7 BJNA010102 1 20010109 A 3350 3114981 LIGHT BOEING 737 737282 13844AT NM EXTERIOR INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 344TM 23044 FOUND L2 DOOR EMERGENCY EXTERIOR LIGHT INOPERATIVE. REPLACED REFLECTOR ASSEMBLY, OPS CHECK NORMAL IAW BMM 33-51-61. (M ) 2 L 7 2 4F RT A16WE 2001020700103 20010207 00103 2001 2 7 AALA016003 4 20010108 A 2565 D29985103 SLIDE DOUG MD90 MD9030 3023690 NM L2 DOOR DEPLOYED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 901RA 53489 AFT GALLEY DOOR EMERGENCY CHUTE WAS PARTIALLY DEPLOYED. INSTALLED NEW EMERGENCY CHUTE IAW THE MM. (M) 2 L 7 2 4F RT A6WE 2001020700108 20010207 00108 NM 2001 2 7 UPS01234770 1 20010103 A 5754 ANGLE BOEING 727 72722C 138400F NM NR 6 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, RT WING NR 6 LE SLAT, I/B TRACK RECESS CUTOUT 2 ANGLES CRACKED, I/B AND O/B AT LWR END OF ANGLE. REM OVED AND REPLACED 2 ANGLES IAW SRM 57-10-2. 2 L 7 3 4F A3WE 2001020700109 20010207 00109 NM 2001 2 7 UPS01234771 1 20010102 A 5330 SKIN BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, NOSE LANDING GEAR WHEEL WELL TOP CEILING BS 272, LBL 15 SHOWS CRACK RUNNING BETWEEN RIVETS, ABOUT 2.5 INCHES LONG. INSTALLED DOUBLER REPAIR IAW SRM 51-40-2. 2 L 7 3 4F A3WE 2001020700110 20010207 00110 NM 2001 2 7 UPS01234772 1 20010102 A 5330 SKIN BOEING 727 72722C 138400F NM FUSELAGE BULGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, SKIN BULGING AT STR 2L, STA 441. ACCOMPLISHED REPAIR IAW UPS EO B727-5310-1371E. 2 L 7 3 4F A3WE 2001020700111 20010207 00111 NM 2001 2 7 UPS01234776 1 20010126 A 3411 PITOT TUBE BOEING 727 72722C 138400F NM FIRST OFFICERS DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:IN AT FL 33.0 CAPTS ALT 33,000 FT F/OS ALT 32820 FT CAPTS A/S 296 KNOTS F/OS A/S 294.5. STANDBY ALT 33,2 00. TESTED CAPT AND FO ALT PER MM 34-12-05. TESTS GOOD. TESTED CAPT AND FO MACH A/S PER MM 34-12-06. TESTS GOOD F/OS PITOT TUBE DAMAGED BEYOND LIMIT PER MM 34-11-21 P601. REMOVED F/OS PITOT TUBE AND INSTALLED F/OS PITOT TUBE PER MM 34- 11-21. VERIFIED PITOT SYSTEM INTEGRITY (F/O) PER 34-11-02. 2 L 7 3 4F A3WE 2001020700118 20010207 00118 NM 2001 2 7 QXEA0100053 1 20010111 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- LIGHT CORROSION ON FRAME X510.000 BETWEEN STRINGER 31 AND 30. LOCATED ON FRAME FLANGE AROUND FUSELAGE RIVETS. REP AIRED IAW DHC-8 SRM 51-20-16. 2 H 7 2 4T RT A13NM 2001020700119 20010207 00119 NM 2001 2 7 QXEA0100054 1 20010115 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- LEFT HAND SIDE OF FUSELAGE THERE IS A DENT JUST FORWARD OF AFT CARGO DOOR, BELOW FLOOR LEVEL. REPAIRED IAW HORIZON AIR EA 9-53-590. 2 H 7 2 4T RT A13NM 2001020700120 20010207 00120 NM 2001 2 7 QXEA0100056 1 20010113 A 5320 CLIP DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- CLIP CRACKED BELOW LEFT HAND EMERGENCY EXIT. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001020700121 20010207 00121 NM 2001 2 7 QXEA0100057 1 20010112 A 5350 FAIRING DHAV DHC8 DHC8102 2809003 NM LT WING ROOT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- TWO AREAS OF CORROSION AT FORWARD END OF LEFT WING ROOT FAIRING BETWEEN STA X312 AND X333 AND IN LINE WITH Z168. R EPAIRED IAW DHC-8 SRM 51-10-00 AND SRM 51-20-16. 2 H 7 2 4T RT A13NM 2001020700122 20010207 00122 NM 2001 2 7 QXEA0100058 1 20010111 A 5321 FLOOR PANEL DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- MAIN CABIN DOORWAY FLOOR PANEL APERTURE FOR PANEL 131DZ HAS CORROSION ON 5 NUT PLATES AND SUROUNDING AREAS OF EACH NUT PLATE. REPAIRED IAW DHC-8 SRM 51-20-16. 2 H 7 2 4T RT A13NM 2001020700123 20010207 00123 NM 2001 2 7 QXEA0100060 1 20010112 A 5530 FLANGE DHAV DHC8 DHC8102 2809003 NM VERTICAL STAB TOOL DAMAGE A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 824PH 157 PDX- VERTICAL STAB LEADING EDGE SPAR ATTACH FLANGE FOR LEADING EDGE 321GT HAS TOOLING SCRATCH ON RIGHT HAND FLANGE. REP AIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-10-00. 2 H 7 2 4T RT A13NM 2001020700124 20010207 00124 NM 2001 2 7 QXEA0100061 1 20010112 A 5530 FLANGE DHAV DHC8 DHC8102 2809003 NM VERTICAL STAB TOOL DAMAGE A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 824PH 157 PDX- VERTICAL STAB LEADING EDGE SPAR ATTACH FLANGE FOR LEADING EDGE 321GT HAS TOOLING SCRATCH ON LEFT HAND FLANGE. REPA IRED IAW DHC-8 51-10-00 AND SRM 51-20-16. 2 H 7 2 4T RT A13NM 2001020700126 20010207 00126 NM 2001 2 7 AWXA0001255 1 20010121 A 3510 BACN10CS05JN NUT BOEING 757 757225 1384959 NM COCKPIT OXY SYS LOOSE A AWXA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 28 914AW 22208 CMH-DIVERTED FLIGHT, CREW OXYGEN WAS LOSING PRESSURE IN FLIGHT. PRESSURE AT THE START OF THE FLIGHT WAS 1620 PSI AND HA D DROPPED TO 1100 PSI. THE FLIGHT DIVERTED TO CMH. IN CMH MAINTENANCE FOUND THE CAPTAINS OXYGEN MASK BOX LEAKING AT TH E FLOOR CONNECTION. THE LINE WAS TIGHTENED AND LEAK CHECKED GOOD. THE OXYGEN BOTTLE WAS REPLACED WITH ONE FULLY SERVIC ED. NO FUTHER SERVICING HAS BEEN REQUIRED AS OF THIS DATE. 2 L 7 2 4F RT A2NM 2001020700127 20010207 00127 WP 2001 2 7 MWEA010120 1 20010124 A 7410 92743642 RELAY DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE NR 2 ENGINE INOPERATIVE A MWEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 31 212ME 47701 NR 2 ENGINE WOULD NOT START ON B-SYSTEM IGNITION. REPLACED RELAY R2-92. 2 L 7 2 4F 4 F A6WE E2EA 2001020700128 20010207 00128 NM 2001 2 7 QXEA0100063 1 20010116 A 5412 FIREWALL DHAV DHC8 DHC8102 2809003 NM NR 2 ENGINE BAY CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- NR 2 FIREWALL CRACKED AT INBOARD SIDE AT CORNER OF CUTOUT ON CLOSING MEMBER. REPAIRED IAW DHC-8 RD8-54-109, PAGE 3 . 2 H 7 2 4T RT A13NM 2001020700129 20010207 00129 NM 2001 2 7 QXEA0100064 1 20010118 A 5412 ANGLE DHAV DHC8 DHC8102 2809003 NM NR 2 ENG FIREWAL CUT A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- RIGHT HAND ENGINE FIREWALL AFT SIDE OUTBOARD ANGLE IS CUT INTO BY TGT HARNESS. REPAIRED IAW DHC-8 RD8-54-991. 2 H 7 2 4T RT A13NM 2001020700130 20010207 00130 NM 2001 2 7 QXEA0100065 1 20010119 A 5414 SKIN DHAV DHC8 DHC8102 2809003 NM RT ENG NACELLE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- ENGINE NACELLE RIGHT HAND SIDE, BOTTOM INBOARD SIDE IS A DENT IN SKIN, INBOARD OF OIL COOLER. REPAIRED IAW DHC-854 -30-21 AND HORIZON AIR EA 9-54-266. 2 H 7 2 4T RT A13NM 2001020700131 20010207 00131 NM 2001 2 7 QXEA0100066 1 20010111 A 5730 PLATE DHAV DHC8 DHC8102 2809003 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- LADDER PLATE HAS PITTING, PANEL 524BT, AFT INBOARD CORNER. REPAIRED IAW DHC-8 SRM 51-20-16 AND RD8-57-633, PAGE 3. 2 H 7 2 4T RT A13NM 2001020700132 20010207 00132 NM 2001 2 7 QXEA0100067 1 20010111 A 5730 PLATE DHAV DHC8 DHC8102 2809003 NM LADDER SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- LADDER PLATE SCRATCHED, PANEL 524BT CENTER AFT LADDER PLATE. REPAIRED IAW DHC-8 SRM 51-20-16 AND RD8-57-633. 2 H 7 2 4T RT A13NM 2001020700133 20010207 00133 NM 2001 2 7 QXEA0100069 1 20010116 A 5711 SPAR DHAV DHC8 DHC8102 2809003 NM LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- LEFT WING FRONT SPAR LOWER SURFACE HAS FRETTING CORROSION AT STATION YW210-220. REPAIRED IAW HORIZON AIR EA 9-57-5 48. 2 H 7 2 4T RT A13NM 2001020700134 20010207 00134 NM 2001 2 7 QXEA0100070 1 20010112 A 5711 SPAR DHAV DHC8 DHC8102 2809003 NM LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- LEFT WING FRONT SPAR, LOWER SURFACE HAS FRETTING CORROSION AT STATION YW 48-82. REPAIRED IAW DHC-8 RD8-57-811 AND RD8-57-1150. 2 H 7 2 4T RT A13NM 2001020700139 20010207 00139 NM 2001 2 7 QXEA0100071 1 20010118 A 5710 SEAL DHAV DHC8 DHC8102 2809003 NM LT WING TORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- SEAL IS TORN AND LEFT WING LOWER SURFACE TRAILING EDGE IS DAMAGED AT STATION YW139-00. REPAIRED IAW DHC-8 SRM 51-4 0-11 AND HORIZON AIR EA 9-57-549. 2 H 7 2 4T RT A13NM 2001020700140 20010207 00140 NM 2001 2 7 QXEA0100072 1 20010111 A 5753 SKIN DHAV DHC8 DHC8102 2809003 NM LT WING TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- LEFT WING OUTBOARD FLAP CHAFED ON UPPER SURFACE. REPAIRED IAW DHC-8 SRM 51-20-50 AND SRM 51-20-11, PAGE 6. 2 H 7 2 4T RT A13NM 2001020700141 20010207 00141 WP 2001 2 7 MWEA010121 1 20010121 A 5330 591140939 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 FUSELAGE DENT AT STATION 236 AND 237 ABOVE LONGERON LEFT 17. MAINTENANCE FABRICATED AND INSTALLED DOUBLER REPAIRS. 2 L 7 2 4F A6WE 2001020700142 20010207 00142 EU 2001 2 7 AWXA0001257 1 20010126 A 2761 31077100 ACTUATOR AIRBUS 320 A320231 3930325 EU NR 2 SPOILER LEAKING A AWXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 646AW 27636 271 PHX- EMERGENCY LANDING, FLIGHT CREW HAD ECAM MESSAGE FOR YELLOW HYDRAULIC SYSTEM LOW LEVEL. AN UNEVENTFUL LANDING WAS M ADE. IN PHX MAINTENANCE FOUND THE RT NR 2 SPOILER SERVO CONTROL LEAKING. THE SERVO CONTROL WAS REPLACED AND THE YELLOW HYDRAULIC SYSTEM SERVICED. FUNCTIONAL AND LEAK CHECKS WERE GOOD. 2 L 7 2 4F RT A28NM 2001020700143 20010207 00143 EU 2001 2 7 C2XA01IA047 1 20010110 A 5410 S5411061920300 STRUCTURE AEROSP ATR42 ATR42320 8680930 EU LEFT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14832 187 YYZ - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE LEFT HAND ENGINE LOWER COWLING WAS FOUND TO HAVE A CRACKED EDGI NG. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGING IN ACCORDANCE WITH ATR42-320 SRM 54-12-61, AND 51-25-03, AND T HE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001020700144 20010207 00144 EU 2001 2 7 C2XA01IA048 1 20010110 A 5315 S5367240820200 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14832 187 YYZ - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE FLOORBEAM AT FRAME 39 WAS FOUND TO BE CORRODED. MAINTENANCE PE RFORMED A DOUBLER REPAIR ON THE AFFECTED FLOORBEAM IN ACCORDANCE WITH ATR42-320 SRM 53-00-00, AND THE AIRCRAFT WAS APPRO VED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001020700145 20010207 00145 EU 2001 2 7 C2XA01IA049 1 20010110 A 5410 S5411058620100 CHANNEL AEROSP ATR42 ATR42320 8680930 EU RT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14832 187 YYZ - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE RIGHT HAND ENGINE COWL (425AT) WAS FOUND TO HAVE A CRACKED CHAN NEL. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CHANNEL IN ACCORDANCE WITH ATR42-320 SRM 54-12-61 AND 51-25-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001020700146 20010207 00146 EU 2001 2 7 C2XA01IA050 1 20010110 A 5410 S5411061920300 CHANNEL AEROSP ATR42 ATR42320 8680930 EU RT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14832 187 YYZ - DURING CONTINENTAL EXPRESS C-CHECK, THE RIGHT HAND ENGINE LOWER NACELLE WAS FOUND TO HAVE THE INBOARD CHANNEL CRAC KED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF CHANNEL IN ACCORDANCE WITH ATR 42-320 SRM 54-12-60 & 51-2 5-03, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001020700147 20010207 00147 EU 2001 2 7 C2XA01IA051 1 20010110 A 5311 S5357260120000 FRAME AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14832 187 YYZ - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE LEFT HAND FRAME 25 WAS FOUND TO BE CRACKED. MAINTENANCE PERFOR MED A DOUBLER REPAIR ON THE AFFECTED FRAME IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHANGE EC5310-01160, AND T HE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001020700148 20010207 00148 EU 2001 2 7 C2XA01IA052 1 20010110 A 5311 S5357260120100 FRAME AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14832 187 YYZ - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE RIGHT HAND FRAME 25 WAS FOUND TO BE CRACKED. MAINTENANCE PERFO RMED A DOUBLER REPAIR ON THE AFFECTED FRAME IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHANGE EC5310-01160, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001020700149 20010207 00149 EU 2001 2 7 C2XA01IA053 1 20010110 A 5210 S5217640420600 STRUCTURE AEROSP ATR42 ATR42320 8680930 EU PAX DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14832 187 YYZ - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE PASSENGER DOOR STAIRCASE FORWARD STRUCTURE WAS FOUND TO BE CRAC KED. MAINTENANCE PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH ATR42-320 SRM 52-11-00, AND THE AIRCRAFT WAS APPROVED FO R RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001020700150 20010207 00150 EU 2001 2 7 C2XA01IA058 1 20010110 A 5210 S5217640520400 STRUCTURE AEROSP ATR42 ATR42320 8680930 EU PAX DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14832 187 YYZ - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE PASSENGER DOOR AFT STEP STRUCTURE WAS FOUND TO BE CRACKED. MAI NTENANCE PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH ATR42-320 SRM 52-11-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001020700151 20010207 00151 EU 2001 2 7 C2XA01IA054 1 20010110 A 5347 S5367800121000 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14832 187 YYZ - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE RIGHT HAND SEAT TRACK WAS FOUND TO BE CORRODED FROM FRAME 36 TO FRAME 39. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK IN ACCORDANCE WITH ATR42-320 SRM 53-63-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001020700152 20010207 00152 EU 2001 2 7 C2XA01IA055 1 20010110 A 5315 S5367240921800 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14832 187 YYZ - DURING C-CHECK INSPECTION, THE FLOORBEAM AT FRAME 40 WAS FOUND TO BE CORRODED. MAINTENANCE PERFORMED A DOUBLER RE PAIR IN ACCORDANCE WITH ATR42-320 SRM 53-61-40, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001020700153 20010207 00153 EU 2001 2 7 C2XA01IA056 1 20010110 A 5315 S5367240720200 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14832 187 YYZ - DURING C-CHECK INSPECTION, THE FLOORBEAM AT FRAME 38 WAS FOUND TO BE CORRODED. MAINTENANCE PERFORMED A DOUBLER RE PAIR IN ACCORDANCE WITH ATR42-320 SRM 53-61-40, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001020700154 20010207 00154 EU 2001 2 7 C2XA01IA057 1 20010110 A 5315 S5367240620800 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14832 187 YYZ - DURING C-CHECK INSPECTION, THE FLOORBEAM AT FRAME 36 WAS FOUND TO BE CORRODED. MAINTENANCE PERFORMED A DOUBLER RE PAIR IN ACCORDANCE WITH ATR42-320 SRM 53-61-40, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001020700155 20010207 00155 NM 2001 2 7 HNAA0100005 1 20010126 A 3260 858601 PSU DHAV DHC8 DHC8201 2809001 NM MLG DEFECTIVE A HNAA O OTHER J WARNING INDICATION TO TAKEOFF 1 EA 07 968HA 4657 112 465 AFTER TAKEOFF AND GEAR RETRACTED, LEFT AMBER DOOR LIGHT ILLUMINATED AND GEAR INOP LIGHT ILLUMINATED. AIRCRAFT FERRIED T O NORFOLK. REPLACED PSCU, PERFORMED SEVERAL GEAR SWINGS, NO DISCREPANCIES NOTED. 2 H 7 2 4T RT A13NM 2001020700156 20010207 00156 NM 2001 2 7 DLM11010054 1 20010108 A 2121 FAN DOUG MD11 MD11 3023602 NM ROW 10 DAMAGED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 811DE 48566 LOUD VIBRATION ASSOC ELEC ODOR OCC EVERY 10 - 15MIN IN CRUISE IN O/H NEAR ROW 10. TURNED OFF ECON MODE AND PULLED RECI RC FAN C/BS, NO HELP. PULLED MID GALLEY CHILLER C/BS, NO HELP. ISOLATED FAULT BY TURNING OFF 3 GALLEY BUS. FOUND PAX OUTLET FAN OVER ROW 10GC WITH INTERNAL FAILURE REMOVED CAPPED AND STOWED FAN CONN AND PULLED CB AT DOOR 2R. RESTORED RE CIRC FAN CB. FWD TO MCO PER MEL 21-23-01 FOR FAN REPLACEMENT. REPLACED FAN. 2 L 7 3 4F RT A22WE 2001020700157 20010207 00157 NM 2001 2 7 DLM88010058 1 20010112 A 3610 CLAMP DOUG MD88 MD88 3023688 NM TAIL COMPARTMENT LOOSE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 916DL 49591 TAIL COMPARTMENT TEMP LIGHT CAME ON SHORTLY AFTER T/O. RAN CHECKLIST PER POM. LIGHT WENT OFF AFTER LEVEL OFF 3000 FT. LIGHT CAME BACK ON AFTER POWER INCREASED TO CLIMB. RETURNED TO MCO. RAN ENG AT T/O PWR. FOUND AUG VALVE LEAKING AT I /B CLAMP. REPLACED BOTH CLAMPS ON LT AUG VLV/RAN ENG TO T/O PWR, NO LEAKS. 2 L 7 2 4F RT A6WE 2001020700158 20010207 00158 NM 2001 2 7 DL72S010093 1 20010119 A 5753 SKIN BOEING 727 727232 1384082 NM NR 3 FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 521DA 21472 NR 3 MID FLAP INBOARD UPPER SKIN PANEL WAS FOUND DAMAGED. REPAIRED PER ER/A 397199-14. 2 L 7 3 4F A3WE 2001020700159 20010207 00159 NM 2001 2 7 DL76S010097 1 20010117 A 5330 146T32521 SKIN BOEING 767 767332 1382001 NM FUSELAGE PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 130DL 24080 THE FUSELAGE SKIN WAS PUNCTURED AT FS 1197+88 BETWEEN STRINGERS 35L & 36L. THE DAMAGE WAS REMOVED WITH A 12 X 12 INCH C UTOUT CENTERED OVER THE STRINGER 36L SKIN LAP JOINT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND STRU CTURAL FILLER PER B767 SRM 53-00-01-2-212 AND ER/A 379789-14, REV A. 2 L 7 2 4F RT A1NM 2001020700161 20010207 00161 NM 2001 2 7 DL72S010104 1 20010120 A 3350 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 534DA 22047 UNPON ARRIVAL AT AIRCRAFT EMERGENCY EXIT LIGHTS WOULD NOT COME ON BATTERIES OUT OF CHARGE. REPLACED BATTERY PACKS THROU GH OUT CABIN, ALL CHECKS NORMAL. 2 L 7 3 4F A3WE 2001020700162 20010207 00162 NM 2001 2 7 DL72W010116 1 20010122 A 3350 CHARGER BOEING 727 727247 138408F NM ROW 3 INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 290WA 22108 UPPER EMERGENCY EXIT SIGN AT SEAT ROW 3 INOP. REPLACED CHARGER ASSY AND BATTERY PACK. 2 L 7 3 4F A3WE 2001020700163 20010207 00163 WP 2001 2 7 DLL10010128 1 20010124 A 2120 UNKNOWN LKHEED 1011 10113851 5265010 WP CABIN ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 1734D 193C1225 ELECTRICAL ODOR REPORTED IN VICINITY OF ROW 30 SEATS ABC, NO SMOKE OBSERVED. DROPPED CEILING PANELS AND PSU PANELS FROM ROWS 27 AB TO 31 AB, NO EVIDENCE OF ANY ODOR OR ELECTRICAL DAMAGE. CHECK COCKPIT AND LOWER GALLEY C/B PANELS FOR POPPE D C/BS, ALL OK. 2 L 7 3 4F A23WE 2001020700164 20010207 00164 NM 2001 2 7 DL73K010134 1 20010125 A 5330 655298887 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 313DL 23085 A .75 INCH CRACK WAS FOUND AT THE L2 DOOR CUTOUT UPPER HINGE. THE CRACK WAS TRIMMED OUT AND DOUBLERS INSTALLED PER ERA 259485-14 AT HMV. 2 L 7 2 4F RT A16WE 2001020700165 20010207 00165 EU 2001 2 7 AALA20010012 1 20010103 A 2120 SMOKE FOKKER F28 F28MK0100 4990807 EU CABIN DETECTED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 1472B 11514 ORD - FLT 879 - EN ROUTE HPN-ORD, ON TAXI TO GATE, DETECTED SMOKE IN CABIN. TURNED OFF RECIRCULATING FANS AND TURNED TE MPERATURE CONTROL TO MANUAL FULL COLD. ARRIVED ORD GATE WITHOUT FURTHER INCIDENT. RAN BOTH PACKS WITH APU AIR AND ENGI NE BLEED. CYCLED RECIRCULATING FANS. NO SMOKE OR ODOR NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001020700167 20010207 00167 NM 2001 2 7 AALA20010069 1 20010109 A 5753 FITTING BOEING 727 727223 1384074 NM NR 6 FLAP CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 875AA 21387 TUL - FOUND NR 6 FLAP TRACK FORWARD SUPPORT FITTING CRACKED. REMOVED AND REPLACED FITTING PER 51-10-01. (M) 2 L 7 3 4F A3WE 2001020700168 20010207 00168 NM 2001 2 7 QXEA0100059 1 20010112 A 5530 FLANGE DHAV DHC8 DHC8102 2809003 NM VERTICAL STAB TOOL DAMAGE A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 824PH 157 PDX- VERTICAL STAB LEADING EDGE SPAR ATTACH FLANGE FOR LEADING EDGE 321GT HAS TOOLING GOUGES. REPAIRED IAW DHC-8 SRM 51 -10-00 AND SRM 51-20-16. 2 H 7 2 4T RT A13NM 2001020700169 20010207 00169 NM 2001 2 7 QXEA0100062 1 20010116 A 5412 ANGLE DHAV DHC8 DHC8102 2809003 NM LT ENG FIREWALL CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- LEFT HAND ENGINE FIREWALL APERTURE ANGLE IS CHAFED ON FRONT FLANGE RADIUS AND EDGE OF ANGLE NEAR TGT HARNESS AREA. REPAIRED IAW DHC-8 RD8-54-991. 2 H 7 2 4T RT A13NM 2001020700170 20010207 00170 NM 2001 2 7 QXEA0100068 1 20010116 A 5711 SPAR DHAV DHC8 DHC8102 2809003 NM LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- LEFT WING FRONT SPAR, UPPER SURFACE HAS FRETTING CORROSION AROUND ATTACH HOLES FOR PANEL 511AL. REPAIRED IAW DHC-8 RD8-57-811 AND SRM 51-2011, AND HORIZON AIR EA 9-57-546. 2 H 7 2 4T RT A13NM 2001020700171 20010207 00171 NM 2001 2 7 01FDEA00027 1 20010118 A 2610 SENSOR BOEING 727 727227 1384078 NM NR 2 ENGINE INOPERATIVE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 494FE 21532 DURING PREFLT INSP FOUND NR 2 FIRE WARN FIRE WALL INOP. FOUND 2 FIRE WALL FIRE LOOP CUT AND NR 6 BLD PLUMBING FROM FIRE WALL BLOWN OUT AND HEAT SHIELD DAMAGED AROUND DUCTING. *S/D* REMOVED AND REPLACED NR 2 ENG SENSOR / RESPONDER ON WORK RELEASE 26-10/4135. REMOVED AND REPLACED NR 2 ENG THERMAL ANTI-ICE DUCT, LWR LEFT FIREWALL PER MM 36-00-001-2, 727 SRM 54-10-3. 2 L 7 3 4F A3WE 2001020700172 20010207 00172 WP 2001 2 7 20010207SG004 1 20010116 A 3350 LIGHT LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 160AT 293A1217 DURING PREFLIGHT, FOUND EGRESS LIGHT OUT IN ONE ''C'' AND GALLEY. REPLACED WIRE STRIP, OPS CHECKED OK. (M) 2 L 7 3 4F A23WE 2001020700173 20010207 00173 NM 2001 2 7 DL764010059 1 20010110 A 5330 146T33414 SKIN BOEING 767 767432ER NM FUSELAGE PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 837MH 29710 THE FUSELAGE SKIN WAS PUNCTURED BY GROUND EQUIPMENT AT FS 1525 JUST ABOVE THE STRINGER 26L SKIN LAP JOINT. THE DA MAGE WAS REMOVED WITH A 2 INCH CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER B767-400 SRM 5 3-00-01, FIG 212 AND ER/A 379744-14. 2 L 7 2 4F RT A1NM 2001020700174 20010207 00174 NM 2001 2 7 DL757010060 1 20010111 A 5330 114N33204 SKIN BOEING 757 757232 1384965 NM FUSELAGE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 683DA 27103 THE FUSELAGE SKIN WAS FOUND GOUGED FROM FS 537 TO 563 BETWEEN STRINGERS 16L & 17L. THE GOUGE WAS REMOVED WITH A 25 X 2 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AND EXTERNAL ALUMINUM REPAIR DOUBLER INSTALLED PER ER/A 379604-14, REV A. 2 L 7 2 4F RT A2NM 2001020700175 20010207 00175 NM 2001 2 7 DL72W010061 1 20010112 A 2720 8281081 SEAL BOEING 727 727247 138408F NM RUDDER LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 291WA 22109 DURING CRUISE FLT, NR 1 ENG HYD PUMP LOW PRESS LIGHT BEGAN TO FLICKER FOLLOWED BY A RAPID DECREASE IN A HYD SYS QUANTITY TO ZERO. FOUND LOWER RUDDER PWR ACTUATOR EH VLV LEAKING. REPLACED PLATE SEALS AND O-RING. SERVICED HYD SYS AND LEAK CHECKED OK. 2 L 7 3 4F A3WE 2001020700176 20010207 00176 NM 2001 2 7 DLM88010063 1 20010112 A 3350 RPS1 POWER SUPPLY DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 910DL 49541 EGRESS LIGHTING INOP ROW 24 - 30. FOUND WIRING SHORTED BETWEEN ROWS 27 - 28. REPAIRED WIRING AND REPLACED AFT PWR SUPP LY. 2 L 7 2 4F RT A6WE 2001020700177 20010207 00177 NM 2001 2 7 UPS01534639 1 20010117 A 7712 TORQUE RING BOEING 757 75724APF 1384969 NM NR 1 ENGINE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 455UP 25476 INSPECTION TYPE:N/A, NR 1 ENG O/B SIDE TORQUE RING SCOOP CRACKED IN 2 PLACES, 2 INCHES FROM TOP AT FORWARD EDGE (2 INCHE S LONG) AND 5 INCHES FROM BOTTOM, FROM RIVET HEAD (.75 INCH LONG) AND VERIFIED WITH DYE PEN. SYS OPS CHECKS GOOD PER M/ M 23-11-00. HF TUNES PROPERLY BETWEEN FREQS. 2 L 7 2 4F RT A2NM 2001020700179 20010207 00179 NM 2001 2 7 DLM11010067 1 20010114 A 3350 BATTERY PACK DOUG MD11 MD11 3023602 NM CABIN INOPERATIVE A DALA O OTHER L NO TEST TX TAXI/GRND HDL 1 SO 27 815DE 48624 DURING PREFLT FOUND FWD B/C EMERGENCY LIGHTS INOP. REPLACED PWR SUPPLY. 2 L 7 3 4F RT A22WE 2001020700180 20010207 00180 NM 2001 2 7 DLM11010068 1 20010114 A 2420 SM600BA5N22 CIRCUIT BREAKER DOUG MD11 MD11 3023602 NM MID E/E BAY FAILED A DALA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 SO 27 803DE 48474 BUS AC AND DC GROUND OFF LEVEL ONE ALERT. WITH MTC APPR RESET POPPED C/B C-14 UPPER MAINT PANEL POPPED AGAIN IN 4 MINUT ES. DIVERTED TO PDX. REPLACED RCCB B1-1347 AGSTR CONTROL EPCU BITE THRU CFDS NO FAULTS R-T-S- NML. 2 L 7 3 4F RT A22WE 2001020700181 20010207 00181 NM 2001 2 7 DL76L010069 1 20010114 A 3830 MODULE BOEING 767 767332 1382001 NM AFT LAV TANK FAILED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 193DN 28450 AFTER T/O FIRST CLASS AND RT AFT LAV INOP. AFT WASTE SHUT DOWN. REPLACED AFT WASTE TANK LOGIC CTL MODULE, OPS NORMAL. ALSO FOUND AFT RT-R2- LAV VLV STUCK OPEN. ABLE TO CLOSE SAME MANUALLY, CONNECTED FLUSH SWITCH AND INOPED LAV. NEEDS N EW TOILET. FWD MCO AND PLACARD PER MEL 25-20-01. 2 L 7 2 4F RT A1NM 2001020700182 20010207 00182 NM 2001 2 7 DLM88010070 1 20010115 A 2150 20495062 ACM DOUG MD88 MD88 3023688 NM ACM BAY LEAKING A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 912DL 49543 ON APPROACH TO KBOS WITH ENGINE WING ANTI-ICE X BLEEDS OPEN AND APU RUNNING. PAX AND F/AS COMPLAINED OF SMOKE IN CABIN AND BOTH FORE AND AFT SMOKE DETECTORS WENT OFF. FOUND RT ACM LEAKING OIL. REPLACED SAME. PERFORMED DUCT BURNOUT. 2 L 7 2 4F RT A6WE 2001020700184 20010207 00184 NM 2001 2 7 DL72S010071 1 20010115 A 3350 1000677 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 526DA 21586 L-2 DOOR EMERGENCY EXIT SIGN INOP. REPLACED ASSY. 2 L 7 3 4F A3WE 2001020700185 20010207 00185 NM 2001 2 7 DL764010072 1 20010116 A 3350 LENS BOEING 767 767* NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 832MH 29704 EMERGENCY LIGHT LENS AT SEAT 44B BROKEN. REPLACED E-PATH LIGHT LENS LIGHT, OP CK GOOD. CAPT VERBAL REPRT ITEM FOUND BY FAA INSPTR. 2 L 7 2 4F RT A1NM 2001020700186 20010207 00186 NM 2001 2 7 DLM88010073 1 20010116 A 3240 TRANSMITTER DOUG MD88 MD88 3023688 NM RT BRAKE FAILED A DALA O OTHER J WARNING INDICATION LD LANDING 1 SO 27 990DL 53342 RIGHT BRAKE PRESSURE INDICATOR 200 PSI AT CRZ ALTITUDE. ALL OTHER PRESSURES AND QUANTITY NORMAL. ON LANDING BRAKES WORKED GOOD. IND REMAINED AT 200 PSI. REPLACED RT BRAKE PRESSURE TRANSMITTER. LEAK AND OPN CKS NORMAL. 2 L 7 2 4F RT A6WE 2001020700188 20010207 00188 NM 2001 2 7 DL72L010076 1 20010115 A 5311 FRAME BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 502DA 21304 DURING ACCOMPLISHMENT OF INSPECTIONS OF THE AFT FRAME OF THEC1 DOOR CUTOUT, AN EXISTING, UNIDENTIFIED WEB REPAIR WAS FOUND. THE REPAIR WAS REMOVED AND FOUND TO BE A SPLICE REPAIR FOR A DAMAGED SECTION OF THE WEB. THE INSPECTIONS, PER A D 99-23-13, WERE ACCOMPLISHED AT THE LOCATION AND A NEW REPAIR INSTALLED PER B727 SRM 51-40-2, FIG 1 AND ER/A 379796- 14AD. 2 L 7 3 4F A3WE 2001020700197 20010207 00197 NM 2001 2 7 DLM90010077 1 20010113 A 5312 9953015507 BULKHEAD DOUG MD90 MD9030 3023690 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 THE CANTED STATION 1520 BULKHEAD WAS FOUND WITH TWO 2 INCH CRACKS AT THE 1:00 O CLOCK POSITION (LOOKING AFT). THE CRACK S ARE NEAR THE JOGGLE LINE FOR THE FACTORY WEB SPLICE. THE DAMAGED SECTION OF WEB WAS TRIMMED OFF AND AN ALUMINUM DOUBL ER AND TRIPLER INSTALLED TO REPLACE THE REMOVED AREA AND REPLACED THE JOGGLED SPLICE. THE REPAIR WAS ACCOMPLISHED PER E R/A 379779-14, REV A. 2 L 7 2 4F RT A6WE 2001020700198 20010207 00198 NM 2001 2 7 DL72S010078 1 20010116 A 2720 591005015 CONTROL UNIT BOEING 727 727225 1384077 NM RUDDER LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 8889Z 21858 DURING CRUISE B-SYSTEM HYD QTY DECREASED. FOUND UPPER RUDDER POWER CONTROL UNIT LEAKING. REPLACED UPPER RUDDER POWER C ONTROL UNIT. 2 L 7 3 4F A3WE 2001020700199 20010207 00199 NM 2001 2 7 DL764010080 1 20010116 A 2420 GCU BOEING 767 767432ER NM LEFT FAILED A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SO 27 831MH 29702 ATB DUE TO ELECTRICAL PWR FAIL IN FLT WITH THE FOLLOWING C/B POPPED ON P-6 PANEL-DC STBY-BAT BUS DIST-L GEN CONT UNIT-RA T MANUAL AND THE ASSOCIATED ALERTS. BPCU BITE FAULTED LT GCU CODE 24-30101 PER FIM. REPLACED LT GCU, GROUND TEST OK PE R FIM USING WDM ISOLATED, VISUALLY INSP SHOOK DOWN AND MEGGED ALL RELATED WIRING TO THE FOUR POPPED C/B. NO SHORTS OR W IRING DAMAGE FOUND. INSP WIRING HARNESS IN P6 PANEL AND AB INSP CARD FILES FOR CHAFING, NONE FOUND. REPLACED STBY PWR RELAY K 109 STBY PWR CB A2 AND MAIN BATT CHGR DEPLOYED STOWED RAT SEVERAL TIMES TO VERIFY NML OPS RAN BOTH. 2 L 7 2 4F RT A1NM 2001020700200 20010207 00200 NM 2001 2 7 DL73E010081 1 20010117 A 5730 654549727 SKIN BOEING 737 737247 138448D NM WING WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 376DL 23603 THE INNER SURFACE OF THE LOWER WING SKIN WAS FOUND WORN AT THE BOOST PUMP ACCESS HOLE AT WBL 148. THE DAMAGE CLEAN UP W AS APPROXIMATELY 1.5 X 1.5 X .061 INCH. THE DAMAGE WAS REPAIRED PER ERA 396660-14 AT MV. 2 L 7 2 4F A16WE 2001020700201 20010207 00201 NM 2001 2 7 DL73E010082 1 20010117 A 5311 651630085 FRAME BOEING 737 737247 138448D NM BULKHEAD CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 376DL 23603 DURING INSPECTIONS OF THE FS 178 BLKHD CRACKS WERE FOUND IN THE LT AND RT SIDE CHORDS AND IN THE BULKHEAD WEB AT RBL 10 WL 233.5. THE CHORDS WERE REPLACED AND THE WEB REPAIRED PER ERA 396656-14AD AT MV. 2 L 7 2 4F A16WE 2001020700202 20010207 00202 NM 2001 2 7 DL72L010083 1 20010117 A 2131 CONTROLLER BOEING 727 727232 1384082 NM A/C BAY INOPERATIVE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 512DA 21314 AT 12000 FT MSL CABIN BEGAN CLIMBING AS PSID INCREASED PAST 3.5 PSID WITH SINGLE PACK. DUCT PRESSURE WAS GOOD AT 34 PSI AT 1.4 EPR. CARGO VALVE CONFIRMED CLOSED. CABIN HAD MAX CLIMB AT 5.5 PSID OF 800 FPM. MAX CABIN ALT 5,500 FT. RETUR NED TO CVG. FOUND RT A/C PACK 35 DEG TEMP CONTROLLER AT FAULT. REPLACED CONTROLLER. ALSO REPLACED LEFT PACK COCKPIT TEMP SELECTOR AND RADIO RACK COOLING VALVE. PRESSURIZATION NOW CHECKS NORMAL. 2 L 7 3 4F A3WE 2001020700203 20010207 00203 NM 2001 2 7 DLM88010084 1 20010117 A 3350 RPS1 POWER SUPPLY DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 963DL 49982 TAIL CONE EMERGENCY EXIT IDENTIFIERS INOP. REPLACED AFT CABIN POWER SUPPLY, CKS OK. 2 L 7 2 4F RT A6WE 2001020700204 20010207 00204 NM 2001 2 7 DL72L010085 1 20010117 A 3350 900835A BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 503DA 21305 EMERGENCY EXIT SIGN OVER R2 DOOR INOP WITH BATTERY POWERED LIGHTS. REPLACED M1093 BATTERY PACK, OPS OK. 2 L 7 3 4F A3WE 2001020700205 20010207 00205 NM 2001 2 7 DL73K010087 1 20010118 A 5315 FLOORBEAM BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 312DL 23084 CRACKS WERE FOUND IN THE WEB OF THE LONGITUDINAL FLOORBEAM BETWEEN FS 700 AND 717. THE WEB AND CHORDS WERE INSPECTED A ND REPAIRED PER S/B 737-57-1210 AT HMV. 2 L 7 2 4F RT A16WE 2001020700206 20010207 00206 2001 2 7 DL76L010088 4 20010117 A 3410 4040800906 COMPUTER BOEING 767 767332 1382001 NM E/E BAY FAILED A DALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 27 185DN 27961 T/O ATTEMPT ABORTED TAKEOFF DUE TO LOSS OF CAPTAINS AIRSPEED AT 117 KTS. REMOVED AND REPLACED PILOTS AIR DATA COMPUTER. OPS CHKS OK PER M/M 34-12-01-4. DURING TROUBLESHOOTING, FOUND THE CO-PILOTS ADC ALSO BAD. OFF FLAGS SHOWING AFTER AI R DATA TEST WAS PERFORMED ON THE MAINT TEST PANEL. REMOVED AND REPLACED CO-PILOTS ADC. OPS CHECK OK. 2 L 7 2 4F RT A1NM 2001020700211 20010207 00211 NM 2001 2 7 BJNA010101 1 20010103 A 3350 LIGHT BOEING 737 737214 138446R NM CABIN LOOSE A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 457TM 20156 FOUND SEAT 21B EMERGENCY EXIT AISLE LIGHT LOOSE FROM SEAT. REATTACHED EMERGENCY EXIT LIGHT. OPS CHECK GOOD IAW BMM 33- 51-11B. (M) 2 L 7 2 4F A16WE 2001020700212 20010207 00212 NM 2001 2 7 DL76L010089 1 20010118 A 2560 BATTERY BOEING 767 767332 1382001 NM FLASHLIGHT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 177DN 25122 EMERGENCY FLASHLIGHT AT MID GALLEY RT SIDE LOW BATTERY INDICATOR NOT FLASHING. REPLACED. BATTERY. OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 2001020700213 20010207 00213 NM 2001 2 7 DLM88010090 1 20010118 A 3020 VALVE DOUG MD88 MD88 3023688 NM NR 1 ENGINE INOPERATIVE A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 973DL 53241 LEFT ENGINE, RIGHT C/B OPEN IN FLIGHT. COMPLIED WITH PROCEDURE, CLOSED CB OPENED AGAIN WHEN ANTI ICE SELECTED. REPLACE D NR 1 ENGINE RIGHT ANTI ICE VALVE CHECKS OK. 2 L 7 2 4F RT A6WE 2001020700214 20010207 00214 NM 2001 2 7 DL72W010091 1 20010118 A 3310 LIGHT BOEING 727 727247 138408F NM COCKPIT SMOKE A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 297WA 22534 CAPT REPORTED ENGINEERS O/H LIGHT BULB FLASHED AND CREATED SMALL AMOUNT OF SMOKE. CONTRACT MTC WAS CALLED TO A/C NO TRO UBLE FOUND. 2 L 7 3 4F A3WE 2001020700215 20010207 00215 NM 2001 2 7 DL73K010092 1 20010119 A 5343 65569227 FITTING BOEING 737 737232 1384475 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 313DL 23085 CORROSION WAS FOUND IN THE BORES OF THE LT SIDE STRUT SUPPORT FITTING LOCATED AT FS 685. THE BORE DIAMETER WAS INCREASE D TO 2.325 INCHES AND REPAIRED PER ERA 396650-14 AT HMV. 2 L 7 2 4F RT A16WE 2001020700216 20010207 00216 NM 2001 2 7 DL757010094 1 20010119 A 5330 SKIN BOEING 757 757232 1384965 NM FUSELAGE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 683DA 27103 L-2 DOOR WAS FOUND WITH OUTER SKIN DAMAGE AT STA 701.74. REPAIRED PER ER/A 401226-14. 2 L 7 2 4F RT A2NM 2001020700217 20010207 00217 NE 2001 2 7 NACA20010006 2 20010125 A 7421 RHB32E SPARK PLUG PWA DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE NR 8 CYLINDER SHORTED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 99330 43576 P36225 FEATHERED THE NR 3 ENGINE DUE TO BACKFIRING, DOUBLE SHORTED SECONDARY, NR 8 CYLINDER. REPLACED BOTH SPARK PLUGS. 2 L 7 4 4R 4 R 6A3 5E8 2001020700218 20010207 00218 NM 2001 2 7 RAAA01B2011 1 20010124 A 3350 8621014 BATTERY BOEING 727 72722C 138400F NM PAX CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 AT END OF SCHEDULED B3 MAINTENANCE CHECK, AFT ENTRY DOOR EXIT INDENTIFIER INOP. REPLACED BATTERY AND TESTED PER RAA ECO 86-26. 2 L 7 3 4F A3WE 2001020700219 20010207 00219 NM 2001 2 7 DL733010095 1 20010118 A 5311 FRAME BOEING 737 737347 1384647 NM BULKHEAD CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 308WA 23441 THE FS 178 BULKHEAD LT SIDE CHORD WAS FOUND WITH A .5 INCH VERTICAL CRACK IN THE RADIUS OF THE CHORD. A NEW SECTION OF SIDE CHORD WAS SPLICED IN PER THE REQUIREMENTS OF BAC S/B 737-53A1173 AND DOCUMENTED PER ER/A 379791-14AD. 2 L 7 2 4F RT A16WE 2001020700220 20010207 00220 NM 2001 2 7 DL73S010096 1 20010118 A 5330 6545778 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 323DL 23095 THE LOWER FWD CORNER OF THE AFT GALLEY DOOR CUTOUT WAS FOUND WITH A 1 INCH CRACK IN THE SKIN AND BONDED DOUBLER. THE CR ACK WAS ROUTED OUT AND AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER ARE INSTALLED PER B737 SRM 53-30-3, FIG 24 AND ER/A 379 810-14, REV A. 2 L 7 2 4F RT A16WE 2001020700221 20010207 00221 NM 2001 2 7 DLM90010098 1 20010119 A 3241 TRANSDUCER DOUG MD90 MD9030 3023690 NM ANTI-SKID SYSTEM FAILED A DALA O OTHER J WARNING INDICATION LD LANDING 1 SO 27 902DA 53382 LEFT OUTBOARD MLG TIRE BLOWN OUT DURING LANDING. MAX AUTOBRAKES WERE USED. UPON BLOWING TIRE DESELECTED AND DISC ABS. LEFT OAP SHOWED LEFT OUTBOARD AND ANTISKID FAULT. TAXI CLEARED AND TOWED TO RAMP. REPLACED NR 1 ANTISKID TRANSDUCER A ND CONTROLLER. 2 L 7 2 4F RT A6WE 2001020700222 20010207 00222 NM 2001 2 7 DL72S010099 1 20010119 A 5754 STIFFENER BOEING 727 727225A 1384077 NM NR 6 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 FWD SPAR STIFFENERS CRACKED AT I/B AND O/B SIDES OF NR 6 L/E SLAT I/B TRACK. BOTH REPAIRED PER MM 57-20-021-8. 2 L 7 3 4F RT A3WE 2001020700223 20010207 00223 NM 2001 2 7 DL72S010100 1 20010119 A 5754 STIFFENER BOEING 727 727225A 1384077 NM NR 7 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 FWD SPAR STIFFENERS CRACKED AT I/B AND O/B SIDES OF NR 7 L/E SLAT I/B TRACK. BOTH REPAIRED PER MM 57-20-021-8. 2 L 7 3 4F RT A3WE 2001020700224 20010207 00224 NM 2001 2 7 DL72S010101 1 20010119 A 5754 SKIN BOEING 727 727225A 1384077 NM NR 6 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 A .5 INCH CRACK AT NR 6 SLAT I/B TRACK CUTOUT. REPAIRED PER MM 57-20-021-8. 2 L 7 3 4F RT A3WE 2001020700225 20010207 00225 NM 2001 2 7 DL738010102 1 20010120 A 2530 72077500 OVEN BOEING 737 737832 13844CF NM GALLEY OVERHEATED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 385DA 30348 GALLEY 1R OVEN OVERHEATS. LITE SMOKE OBSERVED FROM OVEN. TURNED OFF OVEN AND PULLED C/B. REPLACED OVEN. 2 L 7 2 4F RT A16WE 2001020700226 20010207 00226 NM 2001 2 7 DL76S010103 1 20010120 A 3260 SENSOR BOEING 767 767332 1382001 NM NLG FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 139DL 25984 REPEAT WRITE UP - AFTER TAKEOFF CONFIG FLAPS MSG WITH ASSOCIATED NOSE AIR/GRD DISAGREE. PSEU FAULTED TARGET 266. CLEAN ED SENSOR/TARGET, PERFORMED BIT ON PSEU, OPS CHECK WAS NORMAL PER FIM BOTH TARGETS CHECKED NORMAL 244 AND 266. ALSO SLU GGED THE TARGET TO SIMULATE NOSE GEAR EXTENSION. ALSO CHECKED NORMAL. FOUND NOSE GEAR SENSOR S266 DAMAGED. REPLACED S 266 PER M/M. 2 L 7 2 4F RT A1NM 2001020700227 20010207 00227 NE 2001 2 7 DLM11010105 2 20010121 A 7230 BLADE DOUG MD11 MD11 3023602 NM PWA 4060 PW4060 52119 NE NR 3 ENGINE FAILED A DALA E C ENGINE SHUTDOWN ABORTED TAKEOFF C J F.O.D. WARNING INDICATION TO TAKEOFF 1 SO 27 809DE 38837 0 48480 723903 NR 3 ENG COMPRESSOR STALL AND PERFORMED REJECTED T/O AT APPROX 160. ENGINE SHUT DOWN BY FLT CREW. BLADE FAILED. POSSI BLY DUE TO SOFT FOD. 2 L 7 3 4F 4 F RT A22WE E24NE 2001020700228 20010207 00228 NM 2001 2 7 DL73K010106 1 20010121 A 2560 BATTERY BOEING 737 737247 138448D NM FLASHLIGHT INOPERATIVE A DALA O OTHER O OTHER CR CRUISE 1 SO 27 238WA 23186 EN ROUTE TO TPA 1L EMERGENCY FLASHLIGHT BATTERY FAILED. REPLACED SAME. 2 L 7 2 4F A16WE 2001020700229 20010207 00229 NM 2001 2 7 DL72W010107 1 20010121 A 5610 589354313ORPR WINDSHIELD BOEING 727 727247 138408F NM COCKPIT CRACKED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 2821W 21059 R-1 OUTER WINDOW PANE IS CRACKED. REPLACED R-1 WINDOW PER M/M. 2 L 7 3 4F A3WE 2001020700230 20010207 00230 NM 2001 2 7 DL73K010108 1 20010122 A 5551 FITTING BOEING 737 737232 1384475 NM STABILIZER CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 313DL 23085 CORROSION WAS FOUND ON THE LT AND RT HORIZONTAL STABILIZER ATTACH FITTINGS. THE CORROSION WAS REMOVED AND REPAIRED PER ERA 396651-14 AT HMV. 2 L 7 2 4F RT A16WE 2001020700231 20010207 00231 NM 2001 2 7 DL73K010109 1 20010122 A 5553 6552274 FITTING BOEING 737 737232 1384475 NM STABILIZER CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 313DL 23085 CORROSION WAS FOUND ON THE VERTICAL STABILIZER ATTACHMENT LUGS AT THE FRONT SPAR. THE DAMAGE WAS REMOVED AND REPAIRED B Y ERA 396636-14 AT HMV. 2 L 7 2 4F RT A16WE 2001020700232 20010207 00232 NM 2001 2 7 DL73K010110 1 20010122 A 5342 FITTING BOEING 737 737232 1384475 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 313DL 23085 CORROSION WAS FOUND ON THE LT AND RT FUSELAGE CLEVIS LUGS THAT ATTACH THE HORIZONTAL STABILIZER. CORROSION WAS RE MOVED FROM THE LUG BORES AND FACES PER ERA 396637-14 AT HMV. 2 L 7 2 4F RT A16WE 2001020700233 20010207 00233 NM 2001 2 7 DL73K010111 1 20010122 A 2150 CONTROL VALVE BOEING 737 737232 1384475 NM A/C PACK FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 325DL 23097 AUTO PRESS MOD FAILED ABOUT 7500 FT. STANDBY ALLOWED, CABIN PRESSURE TO REACH 10,000 FT. A/C AT 25,000 FT SWITCH TO MANUAL A/C. BUT VALVE WERE ALREADY FULL CLOSED. DESCENDED TO 10,000 FT CABIN PRESSURE HELD AT 9,200 FT. EVEN TRIED US ING APU BLEED AT 10,000 FT, COULD NOT REDUCE CABIN PRESSURE. FOUND LEFT WATER SEPARATOR FROZEN. REPLACED 35 DEGREE VAL VE CONTROLLER AND MIX VALVE. 2 L 7 2 4F RT A16WE 2001020700234 20010207 00234 NM 2001 2 7 DL72E010112 1 20010122 A 5522 SKIN BOEING 727 727247 138408F NM LT ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831WA 21483 FOUND ON B2 LETTER CK 1 INCH AND .375 INCH CRACK TOGETHER AT LOWER SKIN LT ELEVATOR JUST AFT AND O/B OF ACCESS PNL 9311. REPAIRED PER SRM 55-20-3. 2 L 7 3 4F A3WE 2001020700235 20010207 00235 NM 2001 2 7 DL72E010113 1 20010122 A 5531 SKIN BOEING 727 727247 138408F NM VERTICAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831WA 21483 FOUND ON B2 LETTER CK, .25 INCH CRACK AND SHEARED RIVET AT BASE OF VERTICAL STAB AT STR 7 LT SIDE. REPLACED FASTENER AN D REPAIRED PER B727DRD 55-30-3D. 2 L 7 3 4F A3WE 2001020700236 20010207 00236 NM 2001 2 7 DL72E010114 1 20010122 A 5330 ACCESS PANEL BOEING 727 727247 138408F NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831WA 21483 FOUND ON B2 LETTER CK 1 INCH CRACK AT INNER ACCESS PANEL BEAD ON PANEL 9216. REPAIRED PER SRM 55-20-3. 2 L 7 3 4F A3WE 2001020700237 20010207 00237 NM 2001 2 7 DL72W010115 1 20010122 A 3350 BATTERY PACK BOEING 727 727247 138408F NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 290WA 22108 L-2 DOOR EMERGENCY EXIT SIGN INOP. REPLACED CHARGER AND BATTERY PACK. 2 L 7 3 4F A3WE 2001020700238 20010207 00238 NM 2001 2 7 DL76S010117 1 20010122 A 3350 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM CABIN WILL NOT TEST A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 138DL 25409 ON SERVICE CHECK FOUND C-ZONE SEAT MOUNTED EMERGENCY LIGHTS NOT WORKING. FOUND POWER SUPPLY NOT FUNCTIONING PROPERLY. REMOVED AND REPLACED AFT LEFT AND RIGHT. CHECKS GOOD. 2 L 7 2 4F RT A1NM 2001020700239 20010207 00239 NM 2001 2 7 DL757010119 1 20010122 A 5330 143N33204 SKIN BOEING 757 757232 1384965 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 683DA 27103 THE FUSELAGE SKIN WAS FOUND WITH THREE DENTED AREAS BETWEEN FS 590 & 630 AND BETWEEN STRINGERS 16L & 17L. THE SKIN WAS CUT AT FS 590 AND AT FS 630 FROM THE STRINGER 14L LAP JOINT TO THE STRINGER 19L LAP JOINT. THE DAMAGED SECTION OF SKIN WAS REMOVED AND A NEW SECTION INSERTED. THE SKIN WAS SPLICED WITH AN EXTERNAL AND INTERNAL ALUMINUM STRAP AT EACH CUT L OCATION PER ER/A 379605-14, REV A. 2 L 7 2 4F RT A2NM 2001020700240 20010207 00240 NM 2001 2 7 DL757010120 1 20010122 A 5330 143N34204 SKIN BOEING 757 757232 1384965 NM FUSELAGE LIGHTNING STRIKE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 683DA 27103 THE FUSELAGE SKIN WAS FOUND WITH SEVERAL LIGHTNING STRIKES NEAR STRINGER 25R BETWEEN FS 480 & 510. REMOVAL OF THE DAMAG E REQUIRED 4 SMALL 2 - 4 INCH CUTOUTS IN THE SKIN. THE CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL ALUMINUM DOULBER IN STALLED PER ER/A 379712-14, REV A. 2 L 7 2 4F RT A2NM 2001020700241 20010207 00241 NM 2001 2 7 DL733010121 1 20010123 A 5330 SKIN BOEING 737 737347 1384647 NM FUSELAGE DAMAGED A DALA O OTHER O OTHER LD LANDING 1 SO 27 312WA 9339 23598 DIMPLES IN FUSELAGE AT WINDOW LINE IN FRONT OF WINGS BOTH SIDES. FOUND WAVINESS 3 PLACES ON EACH SIDE OF FUSELAGE BETWE EN WINDOWS AT BS 500 - 520 WITHIN LIMITS PER SRM 51-10-01 PG 10 FIG 4 SHT 1. 2 L 7 2 4F RT A16WE 2001020700242 20010207 00242 NM 2001 2 7 DL72W010122 1 20010123 A 5754 SKIN BOEING 727 727247 138408F NM NR 2 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 296WA 22533 A 1 INCH CRACK AT NR 2 SLAT LWR COVE SKIN ANGLE O/B END. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 2001020700243 20010207 00243 NM 2001 2 7 DL757010125 1 20010123 A 5330 143N36912 SKIN BOEING 757 757232 1384965 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 606DL 22813 THE FUSELAGE SKIN WAS DENTED AND GOUGED AT FS 670 JUST BELOW THE STRINGER 19R SKIN LAP JOINT. THE DAMAGED SKIN WAS CUTO UT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND STRUCTURAL FILLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 379856-14 , REV A. 2 L 7 2 4F RT A2NM 2001020700244 20010207 00244 NE 2001 2 7 DL757010126 2 20010123 A 7220 FAN BLADE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE FOD A DALA O OTHER C F.O.D. NR NOT REPORTED 1 SO 27 649DL 37271 24389 716510 FOUND DURING L/O CHECK FOD ON RT ENG FAN BLADE AND ACOUSTICAL LINER. REPAIRED ACOUSTICAL LINER. REMOVED AND REPLACED FAN BLADES NR 15 AND 35, BLENDED BLADES 16,30 AND 31. ACCOMPLISHED ENGINE RUN PER PFHB, ALL CKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2001020700245 20010207 00245 WP 2001 2 7 DLL10010127 1 20010124 A 2120 DUCT LKHEED 1011 10113851 5265010 WP NR 2 A/C PACK WORN A DALA O OTHER G MULTIPLE FAILURE CR CRUISE 1 SO 27 735D 193C1226 UNABLE TO HOLD CABIN AT 350 DESCENDED TO 280. COULD MAINTAIN CABIN WITH OUTFLOW VALVES CLOSED AND COOL AIR OVERBOARD SW C CLOSED. LATER HAD TO DESCEND TO 260 TO HOLD CABIN AT 7500. FOUND FWD CARGO DOOR UPPER CORNERS LEAKING DURING PRESSUR E CK OF ACFT. REPLACED BOTH UPPER CORNERS OF SEAL. FOUND NR 1 PACK DUCT LEAK AT CLAMP. REPLACED CLAMP. FOUND NR 2 PA CK DUCT CRACKED IN SEVERAL AREAS INOPED NR 2 PACK PRESS ACFT WITH PACKS 1 AND 3 CKS OK PER M/M. FWD CARGO DOOR UPPER SE ALS LEAK CK OK. 2 L 7 3 4F A23WE 2001020700246 20010207 00246 NM 2001 2 7 DL72L010130 1 20010123 A 3340 LIGHT BOEING 727 727232 1384082 NM EXTERIOR INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 510DA 21312 BOTH AFT CABIN DOORS OUTSIDE LIGHTS ARE INOP. RELAMPED BOTH DOORS. OPERATION NORMAL. 2 L 7 3 4F A3WE 2001020700247 20010207 00247 NM 2001 2 7 DL73K010131 1 20010125 A 5320 69730563 CLIP BOEING 737 737232 1384475 NM FUSELAGE TOOL DAMAGE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 313DL 23085 THE STRINGER TO FRAME CLIPS AT FS 380 AND STR 5L AND 5R WERE FOUND DAMAGED AND IN NEED OF REPLACEMENT. THE EXTRUDED CLIPS COULD NOT BE PURCHASED SO THEY WERE MANUFACTURED PER ERA 396674-14 AT HMV. THIS EFFECTS SSI F-36. 2 L 7 2 4F RT A16WE 2001020700248 20010207 00248 NM 2001 2 7 DL73K010132 1 20010125 A 5551 FITTING BOEING 737 737232 1384475 NM HORIZONTAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 312DL 23084 THE LT AND RT HORIZONTAL STABILIZER ATTACH FITTINGS WERE FOUND CORRODED. CORROSION WAS REMOVED FROM SEVERAL BORES AND F ACES. THE DAMAGE WAS REPAIRED PER ERA 396666-14 AT HMV. 2 L 7 2 4F RT A16WE 2001020700249 20010207 00249 NM 2001 2 7 DL73K010133 1 20010125 A 5553 FITTING BOEING 737 737232 1384475 NM STABILIZER CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 312DL 23084 CORROSION WAS FOUND ON THE VERTICAL STABILIZER ATTACHMENT LUGS AND FUSELAGE LUGS. SOME OF THE BORES WERE OVERSIZED AN D SOME OF THE FACES WERE BLENDED PER ERA 396619-14 AT HMV. 2 L 7 2 4F RT A16WE 2001020700250 20010207 00250 NM 2001 2 7 DL757010135 1 20010124 A 5320 146N38108200 SPLICE BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 683DA 27103 THE SKIN BUTT SPLICE STRAP AT FS 1401 WAS FOUND CORRODED BETWEEN STRINGERS 27L & 28L. THE SPLICE WAS CUT BETWEEN STR INGERS 26L & 27L AND THE LOWER SECTION WITH THE CORROSION REMOVED. A NEW SECTION WAS INSTALLED AND SPLICED WITH AN AL UMINUM REPAIR STRAP PER ER/A 379695-14, REV A. 2 L 7 2 4F RT A2NM 2001020700251 20010207 00251 NM 2001 2 7 DL733010136 1 20010124 A 5312 65163007 BULKHEAD BOEING 737 737347 1384647 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 308WA 23441 WHILE ACCOMPLISHING INSPECTIONS OF THE FS 178 BULKHEAD WEB A CRACK WAS FOUND AT RBL 5.7 AND WL 211. THE CRACK WAS LOCAT ED ABOVE AND EXISTING DOUBLER REPAIR FOR CRACKS BELOW WL 205. THE NEW CRACK WAS REMOVED WITH A 1 INCH CUTOUT AND THE EX ISTING REPAIR DOUBLER REMOVED. A NEW ALUMINUM REPAIR DOUBLER WAS INSTALLED TO ENCOMPASS ALL CRACK CUTOUT REGIONS. THE REPAIR WAS ACCOMPLISHED PER ER/A 379797-14AD, REV A. 2 L 7 2 4F RT A16WE 2001020700252 20010207 00252 NM 2001 2 7 DL72S010137 1 20010124 A 5310 65561011 FRAME BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 516DA 21432 INSPECTIONS OF THE INNER CHORD, OUTER CHORD AND THE WEB OF THE C1 DOOR OPENING AFT FRAME REVEALED A 1.25 INCH CRACK IN T HE OUTER CHORD BELOW THE NR 6 DOOR STOP, AN EXISTING STEEL SPLICE REPAIR FOR THE INNER CHORD, AND AN EXISTING ALUMINUM W EB REPAIR. THE EXISTING REPAIR WERE REMOVED FOR INSPECTION OF UNDERLYING REPAIRS. AN ALUM DOUBLER WAS REINSTALLED O N THE WEB, ANGLES ON THE INNER CHORD, AND A STEEL ANGLE ON THE OUTER CHORD. REPAIRS WERE PER ER/A 379752-14AD, REV A. 2 L 7 3 4F A3WE 2001020700253 20010207 00253 NM 2001 2 7 DL72S010138 1 20010124 A 5330 65184207 SKIN BOEING 727 727232 1384082 NM FUSELAGE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 516DA 21432 THE FUSELAGE SKIN JUST FWD OF THE FWD EDGE OF THE L1 DOOR CUTOUT WAS FOUND GOUGED MIDWAY BETWEEN THE UPPER AND LOWER HIN GE CUTOUTS. BOTH HINGE CUTOUTS WERE PREVIOUSLY REPAIRED PER B727 S/B 53-0198. THE NEW DAMAGE WAS REMOVED WITH A 1 INC H CUTOUT. THE HINGE REPAIRS WERE REMOVED AND EXTENDED TO INCORPORATE THE NEW DAMAGE. THE REPAIR WAS ACCOMPLISHED P ER ER/A 379825-14. 2 L 7 3 4F A3WE 2001020700254 20010207 00254 WP 2001 2 7 DLL14010139 1 20010123 A 5320 1516389103 INTERCOSTAL LKHEED 1011 1011385115 5265015 WP FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 740DA 193C1244 A SCHEDULED REPEAT INSPECTION OF THE L4 DOOR SURROUND STRUCTURE REVEALED A CRACK IN THE NR 2 DOOR STOP BACK-UP INTE RCOSTAL AT FS 1809. THE CRACK IS ACCEPTABLE PER LOCKHEED S/B 093-53-270 FOR 2500 FLIGHT CYCLES WITH 600 CYCLE REPEAT IN SPECTIONS. ER/A 377845-14, REV A WAS ISSUED TO TRACK THE COMPLIANCE FOR THIS ITEM. 2 L 7 3 4F A23WE 2001020700255 20010207 00255 WP 2001 2 7 DLL14010140 1 20010123 A 5310 1516388102 DOOR FRAME LKHEED 1011 1011385115 5265015 WP FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 740DA 193C1244 A SCHEDULED INSPECTION OF THE R4 DOOR SURROUND STRUCTURE REVEALED A CRACK IN THE NR 2 DOOR STOP ATTACH FITTING AND THE N R 2 DOOR STOP INTERCOSTAL. A CRACK WAS ALSO FOUND IN THE NR 3 DOOR STOP INTERCOSTAL. LOCKHEED S/B ALLOWS CONTINUED SER VICE ON A TIME LIMITED BASIS WITH 2 CRACKED INTERCOSTALS. THE ATTACH FITTING WAS REPLACED AND THE TIME LIMIT AND INSPEC TION SCHEDULE OF THE INTERCOSTALS DOCUMENTED PER ER/A 377844-14, REV A. 2 L 7 3 4F A23WE 2001020700261 20010207 00261 NM 2001 2 7 UPS01234763 1 20010103 A 5230 SKIN BOEING 727 72722C 138400F NM CARGO DOOR BULGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, MAIN CARGO DOOR OUTER SKIN BULGED AT BS 490, STR 4 LEFT. INSTALLED REPAIR AT MAIN CARGO DOOR SKIN IA W SRM 52-30-01. 2 L 7 3 4F A3WE 2001020700271 20010207 00271 NM 2001 2 7 01FDEA00038 1 20010124 A 3230 ACG71705505 MANIFOLD DOUG MD11 MD11F 3023600 NM NLG INOPERATIVE A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 585FE 48481 AFTER T/O, RETRACTED GEAR, NOSE WHEEL INDICATION WENT RED. GEAR WAS NOT UP. CYCLED GEAR WITH SAME RESULTS. THEN RETUR NED TO SUBIC, GEAR SHOWED UNSAFE ON BOTH PRIMARY AND SECONDARY INDICATIONS. *S/D* REMOVED AND REPLACED NOSE LAND GEAR UNLOCK CYLINDER AND STEERING MANIFOLD PER IAW MM 32-35-06-4, 32-35-05-4. 2 L 7 3 4F RT A22WE 2001020700272 20010207 00272 2001 2 7 UPS01534769 4 20010123 A 2360 STATIC LINE BOEING 757 75724APF 1384969 NM ELEVATOR FAILED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 447UP 27736 INSPECTION TYPE:IN, ELEVATOR HEAVY FROM CAPT SIDE AND EICAS MSG ELEVATOR. SEE LOG PAGE 724839 ITEM NR 2 FOR REMOVE AND REPLACE OF ELEVATOR FEEL STATIC LINE. PERFORMED ELEVATOR CONTROL SYSTEM OPERATIONAL TEST PER MM 27-31-00. OPS CK GOOD. 2 L 7 2 4F RT A2NM 2001020700273 20010207 00273 NM 2001 2 7 QXEA0100055 1 20010113 A 5320 CLIP DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- CLIP CRACKED AT FRAME 333 OUTBOARD OF LEFT HAND OUTBOARD SEAT TRACK. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001020801024 20010208 01024 EU 2001 2 8 AALA20010083 1 20010113 A 2916 SEAL AIRBUS 300 A300B4605R 3930308 EU HYDRALIC SYSTEM WORN A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 19059 469 SJU - FLT 1218 - EN ROUTE SJU-BOS, LOST BLUE HYDRAULIC SYSTEM. RETURNED SJU AND LANDED WITHOUT FURTHER INCIDENT. REPLA CED HYDRAULIC SYSTEM MODULE PRESSURE SEALS. SERVICED HYDRAULIC SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2001020801025 20010208 01025 EU 2001 2 8 AALA20010042 1 20010104 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3075A 606 TUL - FOUND CRACK INDICATION AT FRAME 46R. REPLACED FRAME 46R, BELOW RIGHT WINDOW TO CABIN FLOOR, STRINGER 27R AND 28R PER REF EF0311D. (M) 2 L 7 2 4F RT A35EU 2001020801026 20010208 01026 WP 2001 2 8 AALA20010085 1 20010116 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A K NONE L NO TEST IN INSP/MAINT 1 SW 21 501AA 49738 ATL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEATS AND SIDE WALL INOPERATIVE. REPAIRED EMERGENCY EXIT WI RE AT SEAT 19DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001020801027 20010208 01027 WP 2001 2 8 AALA20010016 1 20010103 A 2520 SEAT DOUG DC9 DC982 3022082 WP CABIN DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 420AA 49332 DFW - FLT 1995 - EN ROUTE DFW-AUS, FLIGHT ATTENDANT REPORTED A BURNING SMELL AT MID CABIN. RETURNED DFW AND LANDED WITH OUT FURTHER INCIDENT. REMOVED DEBRIS AT SEAT 17F. RAN ENGINES AND APU WITH BOTH PACKS. NO ODOR NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001020801028 20010208 01028 WP 2001 2 8 AALA20010013 1 20010101 A 4950 SMOKE DOUG DC9 DC982 3022082 WP CABIN DETECTED A AALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 234AA 49181 LAS - FLT 1204 - EN ROUTE LAS-DFW, SHORTLY AFTER APU START, DETECTED SMOKE IN CABIN. RETURNED LAS GATE WITHOUT FURTHER INCIDENT. RAN BOTH ENGINES. ACCOMPLISHED APU AND PACK BURNOUT PER THE MM. NO SMELL OR SMOKE NOTED. SYSTEM GROUND CHE CKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001020801035 20010208 01035 2001 2 8 20010207SG018 4 20010115 A 2565 M119444 CABLE BOEING 757 757236 NM L1 DOOR BROKEN A N8TA K NONE O OTHER IN INSP/MAINT 1 WP 19 547NA 4335 29946 DURING ROUTINE C-CHECK, FOUND L1 DOOR EMERGENCY ESCAPE SLIDE DEPLOY RELEASE CABLE BREAKAWAY STRING BROKEN AT PARACHUTE P INS. REPLACED ESCAPE SLIDE. (M) 2 L 7 2 4F RT A2NM 2001020801037 20010208 01037 2001 2 8 20010207SG019 4 20010115 A 2565 M1149444 CABLE BOEING 757 757236 1384971 NM L2 DOOR BROKEN A N8TA K NONE O OTHER IN INSP/MAINT 1 WP 19 547NA 4335 29946 DURING ROUTINE C-CHECK, FOUND L2 DOOR EMERGENCY ESCAPE SLIDE DEPLOY RELEASE CABLE SAFETY STRING BROKEN AT PARACHUTE PIN. REPLACED SLIDE ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001020801038 20010208 01038 NM 2001 2 8 GAIA01012OP 1 20010117 A 3230 69353703 ROD BOEING 727 727223 1384074 NM NLG BROKEN A GAIA K NONE J WARNING INDICATION CR CRUISE 1 SW 07 6809 19484 FLT 2020 - PHX-ABQ - DURING CRUISE, THE FLIGHT CREW NOTICED THAT THE RED ''DOORS'' LIGHT ON LANDING GEAR ANNUNCIATOR PAN EL AND AMBER ''NOSE GEAR DOOR'' LIGH TON FE ANNUNCIATOR PANEL COME ON INTERMITTENTLY WITH GEAR HANDLE IN UP OR OFF POSIT ION. A UNEVENTFUL LANDING WAS MADE AT ABQ. INVESTIGATION REVEALED THAT THE NOSE GEAR PISTON ROD WAS BROKEN. THE ROD W AS REPLACED PER THE B727 MM AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001020801039 20010208 01039 NM 2001 2 8 GAIA01037ST 1 20010122 A 5311 FRAME BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6807 19482 DURING B-CHECK INSPECTION, FOUND RIGHT FUSELAGE FRAME CRACKED AT BS 760. THE FRAME WAS REPAIRED IAW THE B727 SRM 51-40- 4 FIG 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001020801040 20010208 01040 NM 2001 2 8 GAIA01013 1 20010123 A 2781 SWITCH BOEING 727 727225 1384077 NM L/E FLAP OUT OF ADJ A GAIA K NONE N FALSE WARNING CL CLIMB 1 SW 07 902RF 22549 FLT 1805 - LAX-SAN - AMBER LEADING EDGE FLAP LIGHT ILLUMINATED WHILE ACCELERATING THROUGH 290 KTS. ON LEADING EDGE PANE L NR 5 RIGHT SIDE SHOWS INTRANSIT. AIRCRAFT MADE AN UNEVENTFUL LANDING IN SAN. ADJUSTED NR 5 LEADING EDGE FLAP POSITIO N SWITCH PER B727 MM 27-82-1. OPS CHECKS GOOD ON GROUND. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001020801041 20010208 01041 NM 2001 2 8 GAIA01014 1 20010124 A 2613 LIGHT BOEING 727 727223 1384074 NM COCKPIT INTERMITTENT A GAIA K NONE L NO TEST CR CRUISE 1 SW 07 6827 20180 FLT 1777 - BOS-FWA - LOWER AFT BODY HEAT LIGHT INTERMITTENT TEST. PTT WORKS GOOD. AIRCRAFT MADE AN UNEVENTFUL LANDING IN FWA. REPLACED AFT BODY OVERHEAT LAMP. OPS CHECKS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001020801042 20010208 01042 NM 2001 2 8 GAIA01006B 1 20010122 A 5246 652166515 FUEL DOOR BOEING 727 727223 1384074 NM RT WING DAMAGED A GAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 6816 19491 FLT 202 - BIL - NR 5 TRAILING EDGE FLAP WOULD NOT RETRACT AFTER TAKEOFF. AIRCRAFT MADE AN UNEVENTFUL RETURN TO BIL. UP ON INSPECTION OF AIRCRAFT, FOUND FUEL DOOR OPEN AND DAMAGED. ALSO FOUND NR 6 LEADING EDGE SLAT DAMAGED. REMOVED AND RE PLACED NR 6 SLAT PER B727 MM 27-81-11. FUEL DOOR REPLACED PER B727 MM 57-30-2 AND CLEARED CDL. AIRCRAFT RETURNED TO SE RVICE. (M) 2 L 7 3 4F A3WE 2001020801051 20010208 01051 WP 2001 2 8 AALA20010056 1 20010102 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3507A 49801 TUL - FOUND CRACK IN CUSP SHEET UNDER NR 6 SEAT TRACK STATION 222. INSTALLED NEW CUSP SHEET PER SRM 53-01 FIG 4. (M) 2 L 7 2 4F A6WE 2001021300055 20010213 00055 CE 2001 2 13 20010122CW001 1 20010101 A 2720 501500610 TORQUE TUBE CESSNA 401 401 207590C CE RT RUDDER CBL CRACKED E MHJA K NONE O OTHER UK UNKNOWN 1 SW 05 401PW 4010269 CABLE ATTACH ARM FAILED AT WELD. MOST LIKELY CRACKED DURING TOWING OPERATION DUE TO OVERSTEERING TURN LIMITS. 1 L 7 2 3O A7CE 2001021300056 20010213 00056 WP 2001 2 13 UPS01834745 1 20010123 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:PFLT, LEFT AFT SERVICE DOOR HAS CRACK IN UPPER AFT RADIUS. CUT OUT DAMAGED SECTION OF SKIN, FABRICATED AND DRILLED UP REPAIR DOUBLER PER SRM 53 2. DAMAGE REMOVED, OK TO INSTALL. INSTALLED DOUBLER IAW SRM 53 2 1 COMPLETED TEMP REPAIR PER SRM 53 2 1 TRANSFERED TO D208115. INSTALLED LINER ON MAIN DECK AFT OF LT AFT SERVICE DOOR. CLEARED D20 8115. 2 L 7 4 4F RT 4A25 2001021300057 20010213 00057 NM 2001 2 13 01FDEA00039 1 20010124 A 5320 ANGLE DOUG MD11 MD11F 3023600 NM TORQUE BOX CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 SNRM N 67 ABOVE HORZ STAB IN UPPER TORQUE BOX AREA STA 2122 (DOG HOUSE) TOP ANGLE FROM BULKHEAD TO CROWN AREA HAS CRACKS , LT AND RT ENDS. LT CRACK APPROX .625 INCH LONG AND RT CRACK APPROX 1 INCH LONG. *S/D* REMOVED AND REPLACED PER SRM 53-30-00BB WORKED WITH EA 5530-5382. 2 L 7 3 4F RT A22WE 2001021300058 20010213 00058 NM 2001 2 13 01FDEA00040 1 20010124 A 5320 CLIP DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 SNRM N 69 ABOVE HORIZONTAL STAB UPPER TORQUE BOX AREA STA 2084 ANGLES CLIP CRACKED RT SIDE FROM FRAME TO CROWN AREA. * S/D* REMOVED AND REPLACED PER SRM 53-3-00 FIG 8. 2 L 7 3 4F RT A22WE 2001021300059 20010213 00059 NM 2001 2 13 01FDEA00041 1 20010124 A 5320 AJC70281 CLIP DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 SNRM N 75 ABOVE HORIZONTAL STAB IN UPPER TORQUE BOX STA 2047 ANGLE CLIP FROM BULKHEAD TO CROWN AREA TO BE NDT FOR SUSPE CT CRACK. *S/D* PERF HFEC OF ANGLE, NO DEFECT IND. 2 L 7 3 4F RT A22WE 2001021300060 20010213 00060 NM 2001 2 13 2001UALA00026 1 20010115 A 2450 CWC011210 TERMINAL BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COCKPIT BURNED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 195UA 26899 IN CRZ HAD ELEC BURNING ODOR AND VISIBLE SMOKE AROUND CAPTS SIDE OF THE COCKPIT. UNABLE TO DETERMINE SOURCE. SCHEDULED : MEL TO LAX, DIVERTED TO PAGO PAGO. *S/D* PERFORMED DETAILED VISUAL INSPECTION OF THE COCKPIT AND FOUND LOWER LEFT L1 WINDSHIELD HEAT LUG (SCREW) - IPC 30-41-12-051 ITEM 25. LOOSE AND INSULATION BURNT. PERFORMED INTERIM REPAIR UNTIL TH E ORDERED PART - IPC 30-41-12-051 ITEM 20 (HARNESS ASSEMBLY) CAN BE REPLACED. THE HARNESS ASSEMBLY WAS REPLACED IN NRT ON 18 JAN 2000. THE SYSTEM CHECKED GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2001021300061 20010213 00061 NM 2001 2 13 2001UALA00027 1 20010113 A 5310 STRUCTURE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE VIBRATION A UALA O OTHER E VIBRATION/BUFFET CR CRUISE 1 WP 29 7290U 21568 AIRFRAME EXPERIENCED VIBRATION WHEN AIRSPEED WAS GREATER THAN 300 KNOTS. *S/D* CHECKED AIRCRAFT PER TROUBLESHOOTING MA INTENANCE MANUAL. NO DISCREPENCIES WERE NOTED DURING GROUND CHECKS OR BY SUBSEQUENT FLIGHT CREWS SINCE THE INITIAL WRIT E-UP. NO VIBRATION OR FLUTTER NOTED. AIRCRAFT OK FOR CONTINUED SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2001021300062 20010213 00062 NM 2001 2 13 2001UALA00028 1 20010114 A 3260 189915 SENSOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE MLG FAILED A UALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 WP 29 7294U 21572 UNABLE TO RETRACT LANDING GEAR NORMALLY ON TAKEOFF. *S/D* REPLACED AIR SAFETY SENSOR AND ADJUSTED SHIM PER MAINTENANCE MANUAL. ACCOMPLISHED EXTENSION-RETRACTION AND MANUAL EXTENSION OF THE LANDING GEAR. OPERATIONS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001021300063 20010213 00063 NM 2001 2 13 2001UALA00033 1 20010116 A 5270 189915 SWITCH BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CARGO DOOR OUT OF ADJ A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 952UA 26699 AFT CARGO DOOR WARNING LIGHT ILLUMINATED IN FLIGHT. *S/D* FOUND TARGET AND SWITCH SLIGHTLY OUT OF ALIGNMENT. ADJUSTED AND SECURED SWITCH ASSEMBLY AND CHECKED GAP. OPS CHECKED OK. 2 L 7 2 4F 4 F RT A16WE E2GL 2001021300064 20010213 00064 NM 2001 2 13 2001UALA00038 1 20010116 A 2752 5708544 SHAFT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE TE FLAP ACTUATOR FAILED A UALA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 7461U 21915 AIRCRAFT RETURNED TO DEN DUE TO A SPLIT FLAP CONDITION. *S/D* FOUND LEFT INBOARD FLAP, INBOARD JACKSCREW HAD PIN ON EN D OF JACKSCREW BROKEN. INSTALLED NEW SHAFT ON AFT END OF JACKSCREW. OPERATIONS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001021300065 20010213 00065 NM 2001 2 13 01FDEA00043 1 20010125 A 5320 ANGLE DOUG MD11 MD11F 3023600 NM TORQUE BOX CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 608FE 48548 SNRM N 13, N 3, N 4, N 8 UPPER TORQUE BOX 3 EA FRAME TO CROWN ATTACH ANGLES CRACKED. YA 2046 RT END 1 INCH, LT END .25 INCH YA 2069 RT END 2 INCH, YA 2092 RT END 1 INCH. *S/D* REMOVED AND REPLACED PER MD11 SRM 53-30-00. 2 L 7 3 4F RT A22WE 2001021300066 20010213 00066 NM 2001 2 13 01FDEA00044 1 20010125 A 5320 ANGLE DOUG MD11 MD11F 3023600 NM TORQUE BOX CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 608FE 48548 SNRM N 6 - UPPER TORQUE BOX, AFT BULKHEAD YA 2122.8, UPPER ATTACH ANGLE CRACKED AT EACH END. LT 1.75 INCH, RH END 1.0 I NCH. *S/D* REMOVED AND REPLACED PER MD-11 SRM 53-30-00. INCLUDES EA 1-5530-53281. 2 L 7 3 4F RT A22WE 2001021300067 20010213 00067 CE 2001 2 13 GLBA2001011 1 20010124 A 5414 COWLING BEECH 1900 1900C 1154161 CE NACELLE SEPARATED A GLBA C ABORTED TAKEOFF D INFLIGHT SEPARATION TO TAKEOFF 1 CE 01 122GL UC122 RETURN TO BLOCK, RIGHT SIDE UPPER COWLING DERARTED FROM NACELLE ON T/O. INSPECTED COWLING FOR DAMAGE, RE-INSTALLED COWL ING. RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 2001021300068 20010213 00068 NM 2001 2 13 UPS01234774 1 20010126 A 3350 LIGHT BOEING 727 72751C 1384015 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:IN, COCKPIT EMERGENCY EXIT DOOR LIGHTS INOP. INSTALLED EMERGENCY LIGHT AND OPS CK OK IAW MM 25-60-00, P /N ON 10-60091-10, S/N ON 28518. 2 L 7 3 4F A3WE 2001021300069 20010213 00069 NM 2001 2 13 UPS01234775 1 20010126 A 3411 PITOT TUBE BOEING 727 72727C 138400J NM FEEL COMPUTER CLOGGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 910UP 19117 INSPECTION TYPE:IN, ELEVATORS REQUIRE EXCESSIVE FORCE IN FWD/AFT DIRECTION. CLEARED PITOT BLOCKAGE IN FEEL COMPUTER SYS TEM AND CHANGED FILTERS IN A-SYSTEM MODULAR PACKAGE. BREAKAWAY FORCE CHECKS NORMAL IAW MM 27-30-00. 2 L 7 3 4F A3WE 2001021300070 20010213 00070 NM 2001 2 13 UPS01534768 1 20010126 A 5610 WINDOW BOEING 757 75724APF 1384969 NM COCKPIT OUT OF RIG A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 432UP 25463 INSPECTION TYPE:IN, FIRST OFFICER''S SLIDING WINDOW OUT OF RIG. ADJUSTED RT R2 WINDOW PER MM 56 11 02 PG 501. 2 L 7 2 4F RT A2NM 2001021300071 20010213 00071 WP 2001 2 13 UPS01834773 1 20010125 A 2710 CONTROL CABLE DOUG DC8 DC873F 302199F WP AILERON CONTAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE: IN, AILERON POWER S/O LEVER FROZEN. CLEANED AND LUBED AILERON HYD S/O CABLES GOING THRU BULKHEAD IN LT W/W CABLES HAD BUILD UP OF ANTI CORROSION COMPOUND. SYS OPS CKS GOOD PER MM 27-10-00. 2 L 7 4 4F RT 4A25 2001021300072 20010213 00072 NM 2001 2 13 01FDEA00045 1 20010125 A 5320 AJC737257 ANGLE DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 SNRM N 76 LWR VERTICAL STABILIZER INTERNAL SUPPORT FRAME CRACKED AT RT END AS VIEW THRU ACCESS PNL 364FR BS 2069. *S/D * REMOVED AND REPLACED PER SRM 51-00-01. 2 L 7 3 4F RT A22WE 2001021300073 20010213 00073 NM 2001 2 13 DLM88010141 1 20010123 A 5330 9911856507 SKIN DOUG MD88 MD88 3023688 NM WINDOW BELT LIGHTNING STRIKE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 967DL 53116 THE LT WINDOW BELT SKIN WAS STRUCK BY LIGHTNING AT TWO WINDOW CUTOUTS BETWEEN FS 767 AND 807. THE STRIKES WERE AT THE E DGES OF THE CUTOUTS. EACH LOCATION WAS BLENDED TO REMOVE THE DAMAGE. THE REPAIR WAS ACCOMPLISHED PER ER/A 379840-14. 2 L 7 2 4F RT A6WE 2001021300074 20010213 00074 NM 2001 2 13 DLM88010142 1 20010123 A 5330 99115311 SKIN DOUG MD88 MD88 3023688 NM WINDOW BELT LIGHTNING STRIKE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 967DL 53116 THE WINDOW BELT SKIN SUFFERED A LIGHTNING STRIKE ON THE LWR FWD CORNER OF THE WINDOW OPENING BETWEEN FS 598 & 617. THE DAMAGED WAS BLENDED OUT AND AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER MD-88 SRM 53-05, FIG 111A AND PER ER/A 379838-14. 2 L 7 2 4F RT A6WE 2001021300075 20010213 00075 NM 2001 2 13 DL757010143 1 20010123 A 5414 311N340021 SKIN BOEING 757 757232 1384965 NM NR 1 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 683DA 27103 THE LT SIDE SKIN ON THE NR 1 PYLON WAS FOUND EMANATING FROM THE FWD UPPER CORNER OF THE FWD ACCESS HOLE. ADDITIONAL TOO LING DAMAGE WAS INCURRED ON THE SIDE SKIN AFT OF THE CUTOUT ALONG THE UPPER CHORD ATTACH AREA. THE DAMAGE WAS ROUTED OU T OF THE SIDE SKIN AND BOTH LT AND RT SIDES. REPAIRED/MODIFIED WITH STEEL DOULBERS PER B757 S/B 757-54-0037 AND ER/A 37 9648-14. 2 L 7 2 4F RT A2NM 2001021300076 20010213 00076 NM 2001 2 13 DL72S010144 1 20010125 A 2150 VALVE BOEING 727 727232 1384082 NM LT PACK ODOR A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 537DA 22073 LEFT PACK OVERHEATED WHEN TURNED OFF, SMOKE SMELL IN CABIN. REPLACED LEFT PACK SHUTOFF VALVE, CKS GOOD. 2 L 7 3 4F A3WE 2001021300077 20010213 00077 NM 2001 2 13 DL76G010145 1 20010125 A 2120 UNKNOWN BOEING 767 767332 1382001 NM AFT GALLEY ODOR A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 1610D 30594 CREW REPORTED ELEC ODOR IN AFT CABIN AROUND SEAT ROW 37. CHECKED CABIN AREA, FWD AND AFT CARGO BAYS APU BATTERY AREA AN D WATER COMPRESSOR AND SURROUNDING AREA. ALSO CHECKED E & E BAY AND COMPONENTS. ALL CHECKS WERE OK, NO UNUSUAL ODORS W ERE NOTED. PERFORMED POWER RUN-UP AND RAN PACKS, NOTHING FOUND. A/C PUT BACK IN SERVICE. 2 L 7 2 4F RT A1NM 2001021300078 20010213 00078 NM 2001 2 13 DLM90010146 1 20010124 A 5347 SR095301157003 SEAT TRACK DOUG MD90 MD9030 3023690 NM CABIN CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DA 53387 A/C 9201 IN DFW FOR E-2 CHECK FOUND CORROSION ON O/B FLOOR SEAT TRACK DIRECTLY BELOW AFT GALLEY MOUNT FOR G-2 GALLEY. R EPAIRED SAME. 2 L 7 2 4F RT A6WE 2001021300079 20010213 00079 NM 2001 2 13 DL73K010147 1 20010126 A 2121 FAN BOEING 737 737232 1384475 NM CABIN ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 309DL 23081 DURING LANDING A LINE F/A SMELLED STRONG ODOR IN FWD PORTION OF CABIN. SMELLED LIKE BURNING PLASTIC. RAN BOTH ENGS AND PACKS, NO ODORS NOTED. FWD GASPER FAN TO MCO AND PLAC MEL 21-00-24. DUE TO HISTORY OF C/B POPPING C/B PULLED AND COLL ARED E/E COMPTS AND BAGBINS, ALL NORMAL. 2 L 7 2 4F RT A16WE 2001021300080 20010213 00080 NE 2001 2 13 DL72E010148 2 20010126 A 7230 COMPRESSOR BOEING 727 727247 138408F NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE STALLED A DALA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 282WA 71616 0 21484 687425 NR 1 ENGINE COMPRESSOR STALLED AT 80 KNOTS ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO THE GATE. ENGINE CHANGED. 2 L 7 3 4F 4 F A3WE E2EA 2001021300081 20010213 00081 NM 2001 2 13 DL72S010149 1 20010126 A 3350 BATTERY PACK BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 546DA 22677 EMERGENCY EXIT LIGHTS ON FWD RAFT COMPARTMENT INOP. REPLACED BATTERY PACK, OPN NML. 2 L 7 3 4F A3WE 2001021300082 20010213 00082 NM 2001 2 13 DLM88010150 1 20010126 A 4990 38005041 APU DOUG MD88 MD88 3023688 NM APU BAY CONTAMINATED A DALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 SO 27 906DL 2508 0 49537 ENGINE ANTI-ICE ON SMELLED FUMES AFTER PLACING WING ANTI-ICE ON. SMOKE ALARMS IN REAR SOUNDED ON APPROACH WITH POWER AT IDLE. FUMES SMELLED DURING CLIMB, CRUISE, DESCENT WITH ALL AND CROSSED FEEDS OPEN. APU OFF TEMP CONTROL AT 12 O''''CL OCK, LT LAV SMOKE DECT SOUNDED SHORTLY AFTER WING ANTI-ICE PLACED TO TAIL OPERATION. FOUND APU WET WITH OIL. REPLACED APU, ALSO PERFORMED DUCT BURNOUT OPN 5088. 2 L 7 2 4F RT A6WE 2001021300083 20010213 00083 NM 2001 2 13 DLM88010151 1 20010126 A 3350 HARNESS DOUG MD88 MD88 3023688 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 942DL 49815 A 17D EMERGENCY LIGHT INOP. REPLACED WIRE ASSY, OPS CKS NORMAL. 2 L 7 2 4F RT A6WE 2001021300084 20010213 00084 NE 2001 2 13 DL76L010153 2 20010127 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 STALLED A DALA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 176DN 9160 25061 727830 RT ENG AUDIBLE STALL ON T/O AT MAD. ACFT ATB. ENG WAS NOT SHUTDOWN IN FLIGHT. ENGINE TO BE REPLACED AT MAD. 2 L 7 2 4F 4 F RT A1NM E24NE 2001021300085 20010213 00085 NM 2001 2 13 DL72S010154 1 20010126 A 3350 BATTERY PACK BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 546DA 22677 EMERGENCY EXIT SIGN ON CEILING BETWEEN AFT LAV DOORS INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 2001021300086 20010213 00086 NM 2001 2 13 DL757010155 1 20010127 A 2121 FAN BOEING 757 757232 1384965 NM CABIN OVERHEATED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 27 678DL 25983 ELECTRICAL SMELL IN COCKPIT. MTC ISOLATED PACKS AND FANS AND DETERMINED RT RECIRC FAN TO BE THE SOURCE OF ODOR. PULLED AND COLLARD C/BS FOR RT RECIRC FAN AT P37 PNL-CBS J5 AND D7. FWD MCO AND PLAC PER MEL 21-25-01A. RT RECIRC FAN SELECT ED OFF. 2 L 7 2 4F RT A2NM 2001021300087 20010213 00087 NM 2001 2 13 DL764010156 1 20010126 A 2750 FLAP BOEING 767 767432ER NM TRAILING EDGE STUCK A DALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 27 835MH 29708 AFTER TAKEOFF, EICAS MSG - TRAILING EDGE FLAP DISAGREE. FLAPS STUCK BETWEEN 1 AND 5 DEGREES. PERFORMED CHECKLIST. WEN T TO ALTN FLAPS, NO HELP. RETURNED TO HNL. LANDED OVERWEIGHT AT 390K. CREW REPORTED WORKED OK ON GROUND. MTC T/S PE R FIM BITE FSUE AND FSPM, NO FAULTS FOUND. INSPECTED AND RAN FLAP, ALL OPS NORMAL. PERFORMED OVERWEIGHT INSPECTION. 2 L 7 2 4F RT A1NM 2001021300088 20010213 00088 NM 2001 2 13 DL76G010157 1 20010127 A 2497 WIRE BOEING 767 767332 1382001 NM E/E BAY CHAFED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 1607B 30388 WHILE INVESTIGATING ITEM 001 FOUND WIRE NR W230 OFF OF GND SERVICE SELECT RELAY DAMAGED FROM AVIONICS EQUIP ACCESS DOOR. WDM24-51-52 PAGE 12 SH 1 WIRE W230-011-8. REPAIRED WIRING PER PS SECURED WIRING TO PREVENT FURTHER CHAFING. ASSOCIAT ED SYSTEM CKS OK. 2 L 7 2 4F RT A1NM 2001021300089 20010213 00089 NM 2001 2 13 DLM11010158 1 20010128 A 2530 CHILLER DOUG MD11 MD11 3023602 NM MID GALLEY MALFUNCTIONED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 802DE 48473 STRONG ELECTRICAL SMOKE SMELL REPORTED IN AREA OF BC GALLEY ODOR REPORTED BY PAX AND CREW. MID GALLEY A/C AND D/C CIRCU IT BREAKERS PULLED AND COLLARD FOUND CHILLER CYCLING ON AND OFF. CHILLER FWD TO MCO AND PLAC PER MEL 25-22-01. DUE TO CREW REPORTS OF CHILLER SMOKE SMELL INSP GALLEY COMPONENTS, NO OTHER DEFECTS NOTED. 2 L 7 3 4F RT A22WE 2001021300090 20010213 00090 NM 2001 2 13 DLM88010160 1 20010128 A 3350 BULB DOUG MD88 MD88 3023688 NM LT FUSELAGE BURNED OUT A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 918DE 49959 DURING SERVICE CHECK, FOUND LEFT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED SAME, OP CHECKS NORMAL. 2 L 7 2 4F RT A6WE 2001021300091 20010213 00091 NM 2001 2 13 HNAA0100007 1 20010128 A 5751 85711339103 HOUSING DHAV DHC8 DHC8102 2809003 NM LT WING AILERON CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 937HA 32025 148 CRACK FOUND IN AILERON QUADRANT MOUNTING BRACKET/HOUSING ON LOWER OUTBOARD CORNER RUNNING TO THE FIRST RIVET THEN .25 IN CHES INBOARD OF RIVET TOWARDS THE NEXT RIVET. CRACK IS TO BE EDDY CURRENT INSPECTED EVERY 70 HOURS AND REPAIRED WITH IN 500 HOURS PER PIEDMONT EO8-57-01-620. 2 H 7 2 4T RT A13NM 2001021300092 20010213 00092 WP 2001 2 13 ABXA0100024 1 20010126 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC932F 3022067 WP FUSELAGE DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 904AX 47040 THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE DURING THE PREFLIGHT INSPECTION. MAINTENANCE INSPECTED AND REPLACED T HE EMERGENCY LIGHT BATTERIES IAW DC-9 MM 33-53-00. 2 L 7 2 4F A6WE 2001021300093 20010213 00093 NM 2001 2 13 HNAA0100008 1 20010124 A 7921 28E997 OIL COOLER DHAV DHC8 DHC8102 2809003 NM NR 2 NACELLE DIRTY A HNAA O OTHER O OTHER UK UNKNOWN 1 EA 07 979HA 5331 877 373 NR 2 ENGINE OIL GAUGE FLUCTUATING BETWEEN 55 PSI TO 45 PSI, NEVER BELOW 40. COMPLIED WITH ABNORMAL OIL PRESSURE CHECKLI ST. REMOVED AND REPLACED OIL COOLER. 2 H 7 2 4T RT A13NM 2001021300094 20010213 00094 NM 2001 2 13 F3LA200100010 1 20010125 A 4950 170101106B APU BOEING 737 73736E NM APU BAY ODOR A F3LA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 03 316FL 6103 25264 PRIOR TO DEPARTURE, FLIGHT CREW REPORTED APU PRODUCED ODOR AND SMOKE IN CABIN DURING BLEED AIR OPERATION. MAINTENANCE A DDED OIL TO APU, OPERATED BOTH PACKS AND NO ODOR OR SMOKE WAS NOTED. 2 L 7 2 4F RT A16WE 2001021300095 20010213 00095 2001 2 13 GLBA2001013 4 20010128 A 3418 VANE BEECH 1900 1900D 1154162 CE STALL WARNING ICED A GLBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 01 220GL UE220 ABORTED T/O, STALL WARNING HORN STUCK ON. INSPECTED FOUND STALL VANE ICED OVER. CLEANED, OPS CHECKED SYSTEM GOOD. 2 L 7 2 4T RT A24CE 2001021300096 20010213 00096 2001 2 13 GLBA2001014 4 20010128 A 3418 VANE BEECH 1900 1900D 1154162 CE STALL WARNING ICED A GLBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 01 240GL UE240 ABORTED T/O, STALL WARNING HORN STUCK ON. INSPECTED FOUND STALL VANE ICED OVER. CLEANED, OPS CHECKED SYSTEM GOOD. 2 L 7 2 4T RT A24CE 2001021300097 20010213 00097 CE 2001 2 13 GLBA2001015 1 20010128 A 2130 CONNECTOR BEECH 1900 1900D 1154162 CE SQUAT SWITCH LOOSE A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 153GL UE153 RETURN TO BLOCK, WILL NOT PRESSURIZE. INSPECTED FOUND LOOSE CONNECTION ON SQUAT SWITCH. TIGHTENED, OPS CHECKED SYSTEM GOOD. 2 L 7 2 4T RT A24CE 2001021300098 20010213 00098 NM 2001 2 13 QXEA0100073 1 20010120 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM FUSELAGE TORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 PDX- RIGHT HAND NACELLE SKIN TORN LEFT HAND SIDE AT STATION XN137.35, ADJACENT TO MAIN LANDING GEAR FORWARD DOOR CUTOUT. REPAIRED IAW DHC-8 RD8-54-729. 2 H 7 2 4T RT A13NM 2001021300099 20010213 00099 NM 2001 2 13 QXEA0100074 1 20010120 A 5753 SKIN DHAV DHC8 DHC8102 2809003 NM TE FLAP MISREPAIRED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 824PH 157 PDX- LEFT HAND OUTBOARD FLAP FAILED CLEARANCE CHECK AT REPAIR DOUBLER ON TOP OF SKIN. REPAIRED IAW DHC-8 MRD8-57-1908. 2 H 7 2 4T RT A13NM 2001021300100 20010213 00100 NM 2001 2 13 QXEA0100075 1 20010124 A 5753 SKIN DHAV DHC8 DHC8102 2809003 NM TE FLAP MISREPAIRED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 824PH 157 PDX- LEFT HAND OUTBOARD FLAP FAILED CLEARANCE CHECK AT REPAIR DOUBLER ON TOP SKIN AT STATION YW 391.5 TO 405. REPAIRED IAW HORIZON AIR EA 9-57-551. 2 H 7 2 4T RT A13NM 2001021300101 20010213 00101 EU 2001 2 13 QXEA0100076 1 20010124 A 3350 5515800106 LIGHT FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA O OTHER O OTHER UK UNKNOWN 1 NM 09 494US 11167 SEA- EMERGENCY EXIT LIGHT, FORWARD AND FORWARD FACING CENTER IS INOP. REMOVED AND REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001021300102 20010213 00102 WP 2001 2 13 MWEA010131 1 20010129 A 5720 59192372 FITTING DOUG DC9 DC932 3022066 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 RIGHT WING STRINGER 12 HAS .5 INCH BY .5 INCH AREA OF LIGHT CORROSION STATION 101. FABRICATED AND INSTALLED BUSHINGS AN D REPAIR STRINGER. 2 L 7 2 4F A6WE 2001021300103 20010213 00103 WP 2001 2 13 MWEA010132 1 20010129 A 5720 4911484513 FITTING DOUG DC9 DC932 3022066 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 LEFT WING AT STATION 69 HAS LIGHT CORROSION ON A FITTING AT STRINGER 13. REMOVED AND REPLACED NEW CLIP FITTING. 2 L 7 2 4F A6WE 2001021300104 20010213 00104 WP 2001 2 13 MWEA010133 1 20010129 A 5720 5911279504 FITTING DOUG DC9 DC932 3022066 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 RIGHT WING STRINGER 20 HAS .5 INCH BY .5 INCH OF LITE CORROSION ON FORWARD BOTTOM FLANGE, STATION 79. FABRICATED AND IN STALLED BUSHINGS AND REPAIR STRAPS. 2 L 7 2 4F A6WE 2001021300105 20010213 00105 WP 2001 2 13 MWEA010134 1 20010129 A 5753 5912168503 STRUCTURE DOUG DC9 DC932 3022066 WP LT WING TE FLAP CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 LEFT FLAP FORWARD MOVEABLE VANE LEADING EDGE IS CHAFED. FORMED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001021300106 20010213 00106 WP 2001 2 13 MWEA010135 1 20010129 A 5230 591014119 SKIN DOUG DC9 DC932 3022066 WP FWD CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FORWARD CARGO DOOR, LOWER FORWARD CORNER DOOR SKIN HAS A CRACK. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001021300107 20010213 00107 WP 2001 2 13 MWEA010136 1 20010129 A 5320 5910130309 ANGLE DOUG DC9 DC932 3022066 WP BULKHEAD GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 AFT SIDE OF AFT PRESSURE BULKHEAD HAS AN ANGLE WITH A GOUGE IN RADIUS 36 INCHES UP FROM FLOORLINE AND 12 INCHES OUTBOARD OF LEFT SIDE OF DOOR JAMB. REMOVED, FABRICATED AND INSTALLED NEW ANGLE. 2 L 7 2 4F A6WE 2001021300108 20010213 00108 WP 2001 2 13 MWEA010123 1 20010129 A 5720 59192382 FITTING DOUG DC9 DC932 3022066 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 RIGHT WING STATION 13 HAS 2 AREAS OF LITE CORROSION AT STATION 91 AND 94. FABRICATED AND INSTALLED ANGLE DOUBLER AND FI LLER. 2 L 7 2 4F A6WE 2001021300109 20010213 00109 WP 2001 2 13 MWEA010124 1 20010129 A 5751 5910045504 SKIN DOUG DC9 DC932 3022066 WP RT WING AILERON CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 RIGHT AILERON UPPER OUTBOARD SKIN JUST FORWARD OF STATIC WICK HAS A SPOT OF CORROSION. FABRICATED AND INSTALLED DOUBLER . 2 L 7 2 4F A6WE 2001021300110 20010213 00110 WP 2001 2 13 MWEA010125 1 20010129 A 5330 99581561 PANEL DOUG DC9 DC932 3022066 WP WINDOW BELT CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 WINDOW NR 19 LEFT BELT PANEL HAS CORROSION IN ZONE 1 (INTERNAL) ON RIGHT SIDE. REMOVED AND REPLACED WINDOW BELT. 2 L 7 2 4F A6WE 2001021300111 20010213 00111 WP 2001 2 13 MWEA010127 1 20010129 A 5313 27779224 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 LONGERON 17 LEFT IS CRACKED AT STATION 965. FABRICATED AND INSTALLED LONGERON AND SPLICES. 2 L 7 2 4F A6WE 2001021300112 20010213 00112 WP 2001 2 13 MWEA010128 1 20010129 A 5321 995792926 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 HOLE IN SUBFLOOR, RIGHT SIDE JUST AFT OF STATION 945, OUTBOARD OF NR 4 SEAT TRACK. FABRICATED AND INSTALLED DOUBLERS. 2 L 7 2 4F A6WE 2001021300113 20010213 00113 WP 2001 2 13 MWEA010129 1 20010129 A 5312 9912243109 BULKHEAD DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 LEFT FORWARD WEB ON BULKHEAD AT STATION 965 CRACKED NEAR SUBFLOOR, OUTBOARD OF NR 1 SEAT TRACK. FABRICATED AND INSTALLE D WEB. 2 L 7 2 4F A6WE 2001021300114 20010213 00114 WP 2001 2 13 MWEA010130 1 20010129 A 5712 99193498 RIB DOUG DC9 DC932 3022066 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 RIGHT WING RIB STATION 69 WEB AND LOWER T-EXTRUSION HAS AREAS OF MODERATE CORROSION FROM AFT SPAR TO STRINGER 17. REMOV ED AND REPLACED T-CORD. 2 L 7 2 4F A6WE 2001021300115 20010213 00115 EU 2001 2 13 DHL2001364008 1 20010127 A 2760 23778347 SWITCH AIRBUS 300 A300B4203 3930306 EU SPEED BRAKE FAILED A DHLA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 364DH SHORTLY AFTER TAKEOFF LEVELING AT FL 330 / 280 KIAS, SPEED BRAKE LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURE PER AO M. FLIGHT RETURNED TO KMIA. REMOVED AND REPLACED 4 SPEED BRAKE SWITCHES, POSITION 1, 2, 3, & 4 IAW MAINTENANCE MANUAL 27-61-00, OPERATION CHECK GOOD. 2 L 7 2 4F RT A35EU 2001021300116 20010213 00116 NM 2001 2 13 SWAA010151 1 20010116 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 383SW 26589 DURING SCHEDULED C3 CHECK, FOUND FWD EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2001021300117 20010213 00117 NM 2001 2 13 SWAA010152 1 20010116 A 5330 6546881 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 620SW 28036 DURING SCHEDULED 1/2D CHECK, FOUND 2 EXTERNAL FUSELAGE SKIN CRACKS AT BS 1064, STR 26R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001021300118 20010213 00118 NM 2001 2 13 SWAA010153 1 20010117 A 5754 6546431279 SKIN BOEING 737 7373G7 1384595 NM LT WING LE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED 1/4D CHECK, FOUND LEFT WING L/E OUTBOARD FORE FLAP T/E DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM. 2 L 7 2 4F RT A16WE 2001021300119 20010213 00119 NM 2001 2 13 SWAA010154 1 20010117 A 5310 6545871 DOOR FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR AFT FRAME CRACKED AT 3RD FROM TOP DOOR PIN FITTING. REPAIRED DOOR FRAME PER T1-152-003 & SRM. 2 L 7 2 4F RT A16WE 2001021300120 20010213 00120 NM 2001 2 13 SWAA010155 1 20010117 A 2560 P2070021 BATTERY BOEING 737 7372H4 138448C NM FLASHLIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 086SW 22827 AFT CABIN LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY MM. 2 L 7 2 4F A16WE 2001021300121 20010213 00121 NM 2001 2 13 SWAA010156 1 20010117 A 2560 P4010021 BATTERY BOEING 737 7377H4 NM FLASHLIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 732SW 27864 FWD SECTION LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001021300122 20010213 00122 NM 2001 2 13 SWAA010136 1 20010115 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN FLOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 636WN 27709 EEPLS TRACK COVER MISSING AT ROWS 4 & 9. INSTALLED TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 2001021300123 20010213 00123 2001 2 13 SWAA010137 4 20010115 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM PAX DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 FWD ENTRY DOOR EMERGENCY EVAC SLIDE ASSY FELL OUT OF CONTAINER INADVERTENTLY. REINSTALLED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001021300124 20010213 00124 NM 2001 2 13 SWAA010138 1 20010116 A 5310 6546546 SHEAR TIE BOEING 737 7372H4 138448C NM CARGO BAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED AT BS 727A, STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F A16WE 2001021300125 20010213 00125 NM 2001 2 13 SWAA010139 1 20010115 A 5330 6546881 SKIN BOEING 737 7372H4 138448C NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED D-CHECK, FOUND EXTERNAL FUSELAGE SKIN CREASED AT BS 1138, RT SIDE, UNDER VORTEX GENERATORS. REPAIRED S KIN PER SRM. 2 L 7 2 4F A16WE 2001021300126 20010213 00126 NM 2001 2 13 SWAA010140 1 20010116 A 5310 6546546 SPLICE BOEING 737 7372H4 138448C NM FUSELAGE FRAME CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED D-CHECK, FOUND FRAME SPLICE ANGLE CRACKED AT BS 727, BETWEEN STR 11L & STR 13L. REMOVED AND REPLACED F RAME SPLICE ANGLE PER BAC DWG 65-46547 & SRM. 2 L 7 2 4F A16WE 2001021300127 20010213 00127 2001 2 13 SWAA010141 4 20010115 A 2565 INDICATOR BOEING 737 7372K6 NM ESCAPE SLIDE OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASS Y PER MM. 2 L 7 2 4F RT A16WE 2001021300128 20010213 00128 NM 2001 2 13 SWAA010142 1 20010116 A 5754 6573714 SKIN BOEING 737 7373H4 1384600 NM LT WING SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED C2 CHECK, FOUND NR 2 L/E SLAT AFT OUTBOARD EDGE DELAMINATED. REPAIRED SLAT PER RA 1-357-0946. 2 L 7 2 4F RT A16WE 2001021300129 20010213 00129 2001 2 13 SWAA010143 4 20010115 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM PAX DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 633SW 27936 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001021300130 20010213 00130 NM 2001 2 13 SWAA010144 1 20010116 A 5320 6545409 WEB BOEING 737 7373G7 1384595 NM CENTER SECTION CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED 1/4D CHECK, FOUND PRESSURE BEADED WEB CRACKED AT BS 665, LBL 33. REPAIRED BEADED WEB PER TI-353-046. 2 L 7 2 4F RT A16WE 2001021300131 20010213 00131 NM 2001 2 13 SWAA010145 1 20010115 A 5320 BAC1503 STIFFENER BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 684WN 23941 DURING SCHEDULED SPECIAL VISIT, FOUND BS 663 BULKHEAD STIFFENER CRACKED AT LBL 6.5. REMOVED AND REPLACED STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 2001021300132 20010213 00132 NM 2001 2 13 SWAA010146 1 20010115 A 5312 6516300 BULKHEAD BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 684WN 23941 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED AT RBL 1.0, WL 206. REPAIRED BULKHEAD WEB PER SRM. 2 L 7 2 4F RT A16WE 2001021300133 20010213 00133 NM 2001 2 13 SWAA010147 1 20010115 A 5753 6573732 SKIN BOEING 737 7373T0 1384582 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 684WN 23941 DURING SCHEDULED SPECIAL VISIT, FOUND RT WING OUTBOARD AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED AFT FL AP PER MM. 2 L 7 2 4F RT A16WE 2001021300134 20010213 00134 NM 2001 2 13 SWAA010148 1 20010116 A 5313 BAC1498 STRINGER BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED D-CHECK, FOUND STR 14L CRACKED AT BS 360, WL 230. REPAIRED STR PER SRM. 2 L 7 2 4F RT A16WE 2001021300135 20010213 00135 NM 2001 2 13 SWAA010149 1 20010115 A 5310 6551698 SPLICE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED D-CHECK, FOUND STR SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2001021300136 20010213 00136 NM 2001 2 13 SWAA010150 1 20010116 A 3620 129642 SENSOR BOEING 737 7373A4 1384585 NM RT WING PYLON MALFUNCTIONED A SWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 673AA 23251 DIVERSION, AT FL370, LOST PNEU BLEED PRESS DURING DESCENT, BLEED TRIP OFF LIGHT ILLUMINATED. BOTH DUCT PRESS INDICATOR S SHOWED APPROX 65 - 75 PSI. COULD NOT DUPLICATE PROBLEM. PERFORMED PRESS DECAY CHECK, PRESS CONTROL CHECK AND BLEED A IR OPS CHECK OK PER MM. FOR MX CONVENIENCE, REMOVED AND REPLACED NR 2 POS 390 SENSOR (P/N 12966-2) & 450 SENSOR. 2 L 7 2 4F RT A16WE 2001021300137 20010213 00137 NM 2001 2 13 SWAA010106 1 20010114 A 2751 1817389 TRANSMITTER BOEING 737 7373H4 1384600 NM RT WING TE FLAP ERRATIC A SWAA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 372SW 26599 DECLARED EMERGENCY, T/E FLAP INDICATORS ERRATIC. REMOVED AND REPLACED FLAP INDICATOR (P/N 2061-14-1) & FLAP POS TRANSMI TTER PER MM. OPS CHECK GOOD PER MM. 2 L 7 2 4F RT A16WE 2001021300138 20010213 00138 2001 2 13 SWAA010107 4 20010113 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 AFT SVC DOOR EMERGENCY EVAC SLIDE ASSY FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001021300139 20010213 00139 NM 2001 2 13 SWAA010108 1 20010112 A 5320 6517583 BEAM BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 684WN 23941 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT RBL 17.1, WL 228. REPAIRED VERTICAL BEAM WEB PER RA 1-353-2435. 2 L 7 2 4F RT A16WE 2001021300140 20010213 00140 NM 2001 2 13 SWAA010109 1 20010112 A 3350 PL2230LH00 LIGHT BOEING 737 7375H4 138449D NM CABIN FLOOR DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 511SW 24188 DURING SCHEDULED C3 CHECK, FOUND EEPLS STRIP (PHOTO-LUMINESCENT) DISBONDED AT ROW 7. SECURED LIGHTING STRIP PER MM. 2 L 7 2 4F RT A16WE 2001021300141 20010213 00141 2001 2 13 SWAA010110 4 20010112 A 2565 BOTTLE BOEING 737 7375H4 138449D NM ESCAPE SLIDE DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 0834 26568 DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND LOW. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001021300142 20010213 00142 NM 2001 2 13 SWAA010111 1 20010112 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 604SW 27955 DURING SCHEDULED C3 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT OUT OF RETAINER AT ROW 16. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001021300143 20010213 00143 NM 2001 2 13 SWAA010112 1 20010113 A 5753 6546434 SKIN BOEING 737 7373H4 1384600 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 604SW 27955 DURING SCHEDULED C3 CHECK, FOUND LT WING T/E INBOARD AFT FLAP DELAMINATED ON OUTBOARD LOWER SURFACE. REPAIRED AFT FLAP PER SRM & RA 1-A57-0608. 2 L 7 2 4F RT A16WE 2001021300144 20010213 00144 NM 2001 2 13 SWAA010113 1 20010113 A 5753 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 604SW 2524 27955 DURING SCHEDULED C3 CHECK, FOUND RT WING T/E INBOARD AFT FLAP DELAMINATED AT OUTBOARD LOWER CORNER. REMOVED AND REPLACE D AFT FLAP ASSY PER MM. 2 L 7 2 4F RT A16WE 2001021300145 20010213 00145 NM 2001 2 13 SWAA010114 1 20010113 A 3350 101073 LIGHT BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 607SW 27927 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2001021300146 20010213 00146 2001 2 13 SWAA010115 4 20010113 A 2565 6557463 BRACKET BOEING 737 7373A4 1384585 NM ESCAPE SLIDE LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 680AA 23505 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY BRACKET RIVETS LOOSE. SECURED GIRT BRACK ET PER MM. 2 L 7 2 4F RT A16WE 2001021300147 20010213 00147 NM 2001 2 13 SWAA010116 1 20010114 A 5753 BOLT BOEING 737 7372H4 138448C NM LT WING TE FLAP BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 074SW 127 22674 DURING SCHEDULED SERVICE CHECK, FOUND LT WING T/E OUTBOARD AFT MID FLAP INBOARD SPIGOT BOLT BROKEN. REMOVED AND REPLACE D OUTBOARD MID FLAP PER MM. 2 L 7 2 4F A16WE 2001021300148 20010213 00148 NM 2001 2 13 SWAA010117 1 20010114 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 324SW 23414 DURING SCHEDULED SERVICE CHECK, FOUND 2 EXTERNAL FUSELAGE SKIN CRACK AT BS 500D, WL 246 LT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001021300149 20010213 00149 NM 2001 2 13 SWAA010118 1 20010113 A 3350 101073 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 609SW 27929 DURING SCHEDULED C2 CHECK, FOUND FWD AND AFT ENTRY DOOR EMERGENCY EXIT LIGHT LENS ASSYS LOOSE. SECURED LENS ASSY''''S P ER MM. 2 L 7 2 4F RT A16WE 2001021300150 20010213 00150 2001 2 13 SWAA010119 4 20010114 A 2565 6557463 BRACKET BOEING 737 7373H4 1384600 NM ESCAPE SLIDE LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 620SW 28036 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR GIRT ASSY FWD FLOOR BRACKET LOOSE. SECURED BRACKET PER MM. 2 L 7 2 4F RT A16WE 2001021300151 20010213 00151 NM 2001 2 13 SWAA010120 1 20010113 A 5743 6582770 FITTING BOEING 737 737317 138447P NM RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED SERVICE CHECK, FOUND RT MLG ACTUATOR BEAM SUPPORT FWD FITTING, AT AFT SPAR, CORRODED. REMOVED AND REPL ACED FITTING PER MM. 2 L 7 2 4F RT A16WE 2001021300152 20010213 00152 NM 2001 2 13 SWAA010121 1 20010115 A 5312 6516300 BULKHEAD BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED 1/4D CHECK, FOUND 4 BS 178 BULKHEAD WEB CRACKS BETWEEN RBL 26 TO LBL 12.5, WL 207 TO WL 232. REPAIRED BULKHEAD WEB PER SRM. 2 L 7 2 4F RT A16WE 2001021300153 20010213 00153 NM 2001 2 13 SWAA010122 1 20010114 A 5330 6555074 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED 1/4D CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACKED AT BS 178, WL 240 RT. REPAIRED SKIN PER ER 01-0045. 2 L 7 2 4F RT A16WE 2001021300154 20010213 00154 NM 2001 2 13 SWAA010123 1 20010113 A 5311 AND10133 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 684WN 23941 DURING SCHEDULED SPECIAL VISIT, FOUND T-CHORDS CRACKED AT BS 178, WL 207, LBL 28.0 & RBL 28.0. REPAIRED T-CHORDS PER RA ''S. 2 L 7 2 4F RT A16WE 2001021300155 20010213 00155 NM 2001 2 13 SWAA010124 1 20010114 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN FLOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 624SW 27934 EEPLS LOOSE IN CABIN. SECURED EEPLS FLOOR TRACK PER MM. 2 L 7 2 4F RT A16WE 2001021300156 20010213 00156 NM 2001 2 13 SWAA010125 1 20010115 A 5310 6545818 SHEAR TIE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F A16WE 2001021300157 20010213 00157 NM 2001 2 13 SWAA010126 1 20010115 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED D-CHECK, FOUND STR 10L CRACKED AT BS 540. REPAIRED STR PER SRM. 2 L 7 2 4F A16WE 2001021300158 20010213 00158 NM 2001 2 13 SWAA010127 1 20010115 A 5310 6551698 SPLICE BOEING 737 7372H4 138448C NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED D-CHECK, FOUND STR SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F A16WE 2001021300159 20010213 00159 NM 2001 2 13 SWAA010128 1 20010115 A 5315 6545812 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 328, RBL 28 TO RBL 29. REPAIRED FLOORBEAM UPPER CH ORD PER SRM. 2 L 7 2 4F A16WE 2001021300160 20010213 00160 2001 2 13 SWAA010129 4 20010115 A 2565 6557463 BRACKET BOEING 737 7372H4 138448C NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR GIRT BAR ATTACH FLOOR BRACKETS CORRODED. REMOVED AND REPLACED GIRT BAR B RACKETS PER SRM. 2 L 7 2 4F A16WE 2001021300161 20010213 00161 2001 2 13 SWAA010130 4 20010115 A 2565 D31354 SLIDE BOEING 737 7372K6 NM AFT PAX DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED PM CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE ASSY OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PE R MM. 2 L 7 2 4F RT A16WE 2001021300162 20010213 00162 NM 2001 2 13 SWAA010131 1 20010115 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 500C, ABOVE STR 15R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001021300163 20010213 00163 NM 2001 2 13 SWAA010132 1 20010115 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 500B, STR 9R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001021300164 20010213 00164 NM 2001 2 13 SWAA010133 1 20010115 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN FLOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED SPECIAL VISIT AT DALFORT, FOUND EEPLS TRACK COVER BROKEN AT ROW 15. REPLACED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001021300165 20010213 00165 NM 2001 2 13 SWAA010134 1 20010115 A 5310 6545871 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 620SW 28036 DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR AFT LOWER FRAME CRACKED AT LOWER STOP OUTBOARD FASTENER. REPAIRED DOOR FRAME PER BAC DWG 69-69854. 2 L 7 2 4F RT A16WE 2001021300166 20010213 00166 NM 2001 2 13 SWAA010135 1 20010115 A 5311 BAC1505 FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD VERTICAL CHORD CRACKED AT LBL 5.7, AFT SIDE, INBOARD RADIUS, WL 182.5 TO WL 184. REPAIRED VERTICAL CHORD PER SRM. 2 L 7 2 4F RT A16WE 2001021300167 20010213 00167 NM 2001 2 13 SWAA010157 1 20010118 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 636WN 27709 EEPLS LOOSE AT ROW 16. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001021300168 20010213 00168 NM 2001 2 13 SWAA010158 1 20010117 A 2560 P4010021 BATTERY BOEING 737 737317 138447P NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 686SW 23175 FWD SECTION OUTBOARD EMERGENCY FLASHLIGHT HAS LOW BATTERY INDICATION. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001021300169 20010213 00169 NM 2001 2 13 SWAA010159 1 20010117 A 5315 6546804 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 1016, LBL 10 TO LBL 20. REPAIRED FLOORBEAM UPPE R CHORD PER SRM. 2 L 7 2 4F A16WE 2001021300170 20010213 00170 NM 2001 2 13 SWAA010160 1 20010118 A 5311 6546574 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED D-CHECK, FOUND BS 1115 TO BS 1127 APU INLET UPPER AND LOWER CHORDS CORRODED. REMOVED AND REPLACED CHOR DS PER SRM. 2 L 7 2 4F A16WE 2001021300171 20010213 00171 NM 2001 2 13 SWAA010161 1 20010118 A 5311 6546575 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED D-CHECK, FOUND BS 1138 FRAME CRACKED AT STR CLIP, STR 13L. REMOVED AND REPLACED STR CLIP (P/N 65C27314 ) AND REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2001021300172 20010213 00172 2001 2 13 SWAA010162 4 20010117 A 2565 INDICATOR BOEING 737 7372T4 1384492 NM SLIDE OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED C2 CHECK, FOUND AFT SVC AND ENTRY DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY''S PER MM. 2 L 7 2 4F A16WE 2001021300173 20010213 00173 2001 2 13 SWAA010163 4 20010118 A 2565 65C168209 RETAINER BOEING 737 7373H4 1384600 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED C1 CHECK, FOUND FWD SVC AND ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY RETAINER CLIPS LOOSE. SECURED GI RT ASSY RETAINERS PER MM. 2 L 7 2 4F RT A16WE 2001021300174 20010213 00174 NM 2001 2 13 SWAA010164 1 20010118 A 5311 963820 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 620SW 28036 DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD LT SIDE CHORD CRACKED AT LBL 28.5, WL 207. REMOVED AND REPLACED SIDE CHORD PER ACO. 2 L 7 2 4F RT A16WE 2001021300175 20010213 00175 NM 2001 2 13 SWAA010165 1 20010118 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM CARGO BAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 620SW 28036 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 860, LBL 3 & RBL 3. REPAIRED FLOORBEAM PER RA. 2 L 7 2 4F RT A16WE 2001021300176 20010213 00176 NM 2001 2 13 SWAA010166 1 20010117 A 5315 6546804 FLOORBEAM BOEING 737 7373G7 1384595 NM CARGO BAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 773, LBL 13 TO RBL 8. REPAIRED FLOORBEAM PER RA. 2 L 7 2 4F RT A16WE 2001021300177 20010213 00177 NM 2001 2 13 SWAA010167 1 20010117 A 5315 6546804 FLOORBEAM BOEING 737 7373G7 1384595 NM CARGO BAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 814, RBL 3 & RBL 8. REPAIRED FLOORBEAM PER SRM & RA. 2 L 7 2 4F RT A16WE 2001021300178 20010213 00178 NM 2001 2 13 SWAA010168 1 20010117 A 5753 SKIN BOEING 737 7373H4 1384600 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 388SW 2307 26591 DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM. 2 L 7 2 4F RT A16WE 2001021300179 20010213 00179 NM 2001 2 13 SWAA010169 1 20010119 A 5311 6546573 FRAME BOEING 737 7372H4 138448C NM AFT FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 1104, STR 14L. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2001021300180 20010213 00180 NM 2001 2 13 SWAA010170 1 20010118 A 3350 65C34691 LENS BOEING 737 7373Q8 1384670 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 317WN 24068 DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT LIGHT LENS MISSING AT BULLNOSE, ROW 13 DEF. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2001021300181 20010213 00181 NM 2001 2 13 SWAA010171 1 20010119 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM CARGO BAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 620SW 28036 DURING SCHEDULED 1/2D CHECK, FOUND BS 747 FLOORBEAM CRACKED AT RBL 14. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2001021300182 20010213 00182 NM 2001 2 13 SWAA010172 1 20010119 A 5320 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED D-CHECK, FOUND STR CLIP CRACKED AT BS 400, STR 4L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001021300183 20010213 00183 NM 2001 2 13 SWAA010173 1 20010118 A 2560 P2070004 CHARGER BOEING 737 7373G7 1384595 NM FLASHLIGHT MALFUNCTIONED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED A1 CHECK, FOUND AFT CABIN LOWER EMERGENCY FLASHLIGHT WOULD NOT TURN OFF. REMOVED AND REPLACED FLASHLIG HT HOLDER PER MM. 2 L 7 2 4F RT A16WE 2001021300184 20010213 00184 2001 2 13 SWAA010174 4 20010119 A 2565 BOTTLE BOEING 737 7373H4 1384600 NM ESCAPE SLIDE DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 365SW 0638 26576 FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001021300185 20010213 00185 NM 2001 2 13 SWAA010175 1 20010120 A 5330 65C35770 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED SERVICE CHECK, FOUND 3 EXTERNAL FUSELAGE SKIN CRACK AT BS 580, ABOVE STR 10L. REPAIRED SKIN PER RA. 2 L 7 2 4F A16WE 2001021300186 20010213 00186 NM 2001 2 13 SWAA010176 1 20010119 A 5330 65C35772 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 314SW 23336 DURING SCHEDULED SERVICE CHECK, FOUND 4 EXTERNAL FUSELAGE SKIN CRACK AT BS 727A-B, STR 10R. REPAIRED SKIN PER RA. 2 L 7 2 4F RT A16WE 2001021300187 20010213 00187 NM 2001 2 13 SWAA010177 1 20010120 A 5315 6546804 FLOORBEAM BOEING 737 7373G7 1384595 NM CARGO BAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 727A, RBL 3. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2001021300188 20010213 00188 NM 2001 2 13 SWAA010178 1 20010120 A 3350 65C34691 LIGHT BOEING 737 7373G7 1384595 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY LIGHT LOOSE AT BULLNOSE ROW 10 ABC. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001021300189 20010213 00189 NM 2001 2 13 SWAA010179 1 20010120 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN FLOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 714CB 27848 DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACKS COVERS CRACK AT ROW 2, ROW 6 & FWD SECTION. REMOVED AND REPLACED TRACK CO VERS PER MM. 2 L 7 2 4F RT A16WE 2001021300190 20010213 00190 2001 2 13 SWAA010180 4 20010120 A 2565 INDICATOR BOEING 737 7372K6 NM SLIDE OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001021300191 20010213 00191 NM 2001 2 13 SWAA010181 1 20010120 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN FLOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 637SW 27710 EEPLS TRACK COVER BROKEN AT ROW 11. INSTALLED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001021300192 20010213 00192 NM 2001 2 13 SWAA010183 1 20010121 A 5754 SKIN BOEING 737 7373G7 1384595 NM LT WING LE FLAP DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 1893 23785 DURING SCHEDULED 1/4D CHECK, FOUND LT WING L/E INBOARD FORE FLAP HAS 10 INCH CREASE ON UPPER SURFACE. REMOVED AND REPLA CED INBOARD FORE FLAP PER MM. 2 L 7 2 4F RT A16WE 2001021300193 20010213 00193 2001 2 13 SWAA010184 4 20010121 A 2565 SCREW BOEING 737 7373H4 1384600 NM ESCAPE SLIDE MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 FWD ENTRY DOOR EMERGENCY EVAC SLIDE ASSY MISSING SCREW. INSTALLED SCREW INBOARD SIDE PER MM. 2 L 7 2 4F RT A16WE 2001021300194 20010213 00194 NM 2001 2 13 SWAA010185 1 20010122 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING WALK-AROUND INSPECTION, FOUND 1.5 INCH EXTERNAL FUSELAGE SKIN CRACK BETWEEN BS 500C & BS 520, STR 10L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001021300195 20010213 00195 NM 2001 2 13 SWAA010186 1 20010122 A 3397 WIRE BOEING 737 7373H4 1384600 NM CABIN FLOOR EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 362SW 26573 EEPLS WIRING EXPOSED AT MID CABIN. REINSTALLED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001021300196 20010213 00196 NM 2001 2 13 SWAA010187 1 20010121 A 2560 P4010021 BATTERY BOEING 737 7373G7 1384595 NM FLASHLIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 690SW 23783 AFT CABIN LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001021300197 20010213 00197 NM 2001 2 13 SWAA010188 1 20010121 A 5311 6546546 FRAME BOEING 737 7372H4 138448C NM CARGO BAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED D-CHECK, FOUND BS 794 FRAME CORRODED AT RBL 7 TO RBL 12. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2001021300198 20010213 00198 NM 2001 2 13 SWAA010189 1 20010122 A 5311 BAC1503 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD VERTICAL CHORD CRACKED AT RBL 5.7, WL 184. REPAIRED CHORD PER SRM. 2 L 7 2 4F A16WE 2001021300199 20010213 00199 NM 2001 2 13 SWAA010190 1 20010122 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED D-CHECK, FOUND STR 7L CRACKED AT BS 1010. REMOVED AND REPLACED STR SECTION PER SRM. 2 L 7 2 4F A16WE 2001021300200 20010213 00200 NM 2001 2 13 SWAA010191 1 20010122 A 5740 6563961 ANGLE BOEING 737 7372H4 138448C NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED D-CHECK, FOUND LT WING, RSS 541, INBOARD CENTER AILERON HINGE RIB OUTBOARD UPPER ANGLE CRACKED. REMOVE D AND REPLACED ANGLE PER SRM & BAC DWG. 2 L 7 2 4F A16WE 2001021300201 20010213 00201 NM 2001 2 13 SWAA010192 1 20010121 A 3350 0L3071BPL5GPL BULB BOEING 737 7372H4 138448C NM CABIN FLOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED C3 CHECK, FOUND 1 EEPLS BULB INOP NEAR AFT GALLEY. REMOVED AND REPLACED BULB PER MM. 2 L 7 2 4F A16WE 2001021300202 20010213 00202 NM 2001 2 13 SWAA010193 1 20010121 A 3350 079123 COVER BOEING 737 7372H4 138448C NM CABIN FLOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVER MISSING AT MID CABIN. REPLACED TRACK COVER PER MM. 2 L 7 2 4F A16WE 2001021300203 20010213 00203 NM 2001 2 13 SWAA010194 1 20010122 A 5754 SKIN BOEING 737 7373H4 1384600 NM LT WING LE FLAP DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 329SW 23693 DURING SCHEDULED C1 CHECK, FOUND LT WING OUTBOARD FORE FLAP DISBONDED AT T/E, INBOARD SECTION. REMOVED AND REPLACED FOR E FLAP PER MM. 2 L 7 2 4F RT A16WE 2001021300204 20010213 00204 NM 2001 2 13 SWAA010195 1 20010122 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 355SW 25250 DURING SCHEDULED SPECIAL VISIT AT DALFORT, FOUND EMERGENCY EXIT LIGHT INOP AT BULLNOSE, ROW 7 ABC. REMOVED AND REPLACED LAMP PER MM. 2 L 7 2 4F RT A16WE 2001021300205 20010213 00205 2001 2 13 SWAA010196 4 20010122 A 2565 6557463 BRACKET BOEING 737 7373Q8 1384670 NM ESCAPE SLIDE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BRACKET CORRODED. REMOVED AND REPLACED GIRT BR ACKET PER SRM. 2 L 7 2 4F RT A16WE 2001021300206 20010213 00206 NM 2001 2 13 SWAA010197 1 20010122 A 5313 BAC1498 STRINGER BOEING 737 7373Q8 1384670 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED D-CHECK, FOUND STR CRACKED AT BS 400, STR 4L. REPAIRED STR PER SRM. 2 L 7 2 4F RT A16WE 2001021300207 20010213 00207 NM 2001 2 13 SWAA010198 1 20010122 A 5320 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED D-CHECK, FOUND STR CLIPS CRACKED AT BS 500A, STR 16L, BS 380, STR 1, BS 277 STR 15R & BS 616, STR 8L. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001021300208 20010213 00208 NM 2001 2 13 SWAA010199 1 20010122 A 5320 6547978 CREASE BEAM BOEING 737 7373Q8 1384670 NM CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CORRODED FROM BS 950 TO BS 996, RBL 48 TO RBL 52. REPAIRED CREASE BEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2001021300209 20010213 00209 NM 2001 2 13 SWAA010200 1 20010122 A 5320 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED D-CHECK, FOUND STR CLIPS CRACKED AT BS 727, STR 6R, BS 727A STR 3R, 727C STR 5R & STR 6R, BS 727D, STR 1, STR 2L, STR 5L/R, STR 6L, STR 7L, STR 8L & STR 9L. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001021300210 20010213 00210 NM 2001 2 13 SWAA010201 1 20010122 A 5310 6551698 SPLICE BOEING 737 7375H4 138449D NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 512SW 24189 DURING SCHEDULED D-CHECK AT DALFORT, FOUND STR SPLICE CRACKED AT BS 907 & BS 908, STR 4L. REMOVED AND REPLACED STR SPLI CE PER SRM. 2 L 7 2 4F RT A16WE 2001021300211 20010213 00211 NM 2001 2 13 SWAA010202 1 20010122 A 5310 6546569 SHEAR TIE BOEING 737 7375H4 138449D NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 512SW 24189 DURING SCHEDULED D-CHECK AT DALFORT, FOUND SHEAR TIE CRACKED AT BS 967, BETWEEN STR 6L & STR 7L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2001021300212 20010213 00212 NM 2001 2 13 SWAA010203 1 20010121 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN FLOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 716SW 27850 DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVERS CRACKED AT ROWS 1 & 8. REMOVED AND REPLACED TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 2001021300213 20010213 00213 2001 2 13 SWAA010204 4 20010121 A 2565 65C168209 RETAINER BOEING 737 7377H4 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 716SW 27850 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT RETAINER HOOKS HAVE LOOSE RIVETS. SECURED GIR T RETAINER PER MM. 2 L 7 2 4F RT A16WE 2001021300214 20010213 00214 NM 2001 2 13 SWAA010205 1 20010122 A 3230 R276 RELAY BOEING 737 7373Y0 1384671 NM MLG HANDLE ERRATIC A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 665WN 23497 AIR TURNBACK, ON T/O GEAR HANDLE WOULD NOT COME UP. PULLED OVERRIDE TRIGGER AND GEAR RETRACTED. RESEATED R276 RELAY, R ESET C/B. HANDLE OPS CHECKED GOOD PER MM. 2 L 7 2 4F RT A16WE 2001021300215 20010213 00215 NM 2001 2 13 SWAA010206 1 20010122 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 EMERGENCY EXIT LIGHT LENS LOOSE/CRACKED AT BULLNOSE, ROW 20 DEF. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2001021300216 20010213 00216 2001 2 13 SWAA010207 4 20010122 A 2565 BOTTLE BOEING 737 7373A4 1384585 NM ESCAPE SLIDE DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 2589 23253 DURING SCHEDULED RON CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED AFT SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001021300217 20010213 00217 NM 2001 2 13 SWAA010208 1 20010123 A 5315 6546804 FLOORBEAM BOEING 737 7372H4 138448C NM CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAMS CORRODED AT BS 967, RBL 51, RBL 41, RBL 27, RBL 4 & BS 329, RBL 65. REPAI RED FLOORBEAMS PER SRM. 2 L 7 2 4F A16WE 2001021300218 20010213 00218 NM 2001 2 13 SWAA010209 1 20010123 A 5315 6546804 FLOORBEAM BOEING 737 7372H4 138448C NM CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAMS CORRODED AT BS 294, LBL 13 TO RBL 51, BS 312, LBL 8 TO RBL 8 & BS 328, LBL 30. REPAIRED FLOORBEAMS PER SRM. 2 L 7 2 4F A16WE 2001021300219 20010213 00219 NM 2001 2 13 SWAA010210 1 20010123 A 5311 6558280 FRAME BOEING 737 7372H4 138448C NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, BETWEEN STR 13R & STR 14R. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2001021300220 20010213 00220 NM 2001 2 13 SWAA010211 1 20010123 A 3350 612825 CHARGER BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS SECTION INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F A16WE 2001021300221 20010213 00221 NM 2001 2 13 SWAA010212 1 20010122 A 3350 BR2013 LIGHT BOEING 737 7372T4 1384492 NM CABIN FLOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED C2 CHECK, FOUND EEPLS LOOSE IN CABIN. REINSTALLED EEPLS PER MM. 2 L 7 2 4F A16WE 2001021300222 20010213 00222 NM 2001 2 13 SWAA010213 1 20010123 A 3350 0L3071BPL5GPL BULB BOEING 737 7373H4 1384600 NM CABIN FLOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED C1 CHECK, FOUND EEPLS BULB INOP IN AFT SECTION. REMOVED AND REPLACED BULB PER MM. 2 L 7 2 4F RT A16WE 2001021300223 20010213 00223 2001 2 13 SWAA010214 4 20010123 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM PAX DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. REPOSITIONED EVAC SLIDE ASS Y PER MM. 2 L 7 2 4F RT A16WE 2001021300224 20010213 00224 2001 2 13 SWAA010215 4 20010122 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 382SW 26588 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. REPOSITIONED EVAC SLIDE ASS Y PER MM. 2 L 7 2 4F RT A16WE 2001021300225 20010213 00225 NM 2001 2 13 SWAA010216 1 20010123 A 3350 101073 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 382SW 26588 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT HAS SEVERAL BULBS INOP AND LENS BROKEN. REMOVED AN D REPLACED LENS AND REPLACED BULBS PER MM. 2 L 7 2 4F RT A16WE 2001021300226 20010213 00226 NM 2001 2 13 SWAA010217 1 20010122 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN FLOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 385SW 26600 DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVERS CRACKED AT ROWS 9, 16, 18, 19 & 21. REMOVED AND REPLACED TRACK COVE RS PER MM. 2 L 7 2 4F RT A16WE 2001021300227 20010213 00227 NM 2001 2 13 SWAA010218 1 20010123 A 5320 6545409 WEB BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED 1/4D CHECK, FOUND PRESSURE BEADED WEB CRACKED AT BS 665, RBL 40. REPAIRED BEADED WEB PER SRM & T1-353- 032. 2 L 7 2 4F RT A16WE 2001021300228 20010213 00228 NM 2001 2 13 SWAA010219 1 20010123 A 5310 BAC1520 WINDOW POST BOEING 737 7373G7 1384595 NM COCKPIT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED 1/4D CHECK, FOUND CAPTS WINDOW POST CRACKED ON UPPER SECTION, BETWEEN NR 1 & NR 2 WINDOWS. REPAIRED WI NDOW POST PER SRM. 2 L 7 2 4F RT A16WE 2001021300229 20010213 00229 NM 2001 2 13 SWAA010220 1 20010123 A 5740 65C25922 FITTING BOEING 737 7372H4 138448C NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/2D CHECK, FOUND RT WING AILERON FITTING CRACKED, 2ND FROM INBOARD. REMOVED AND REPLACED FITTING PER SRM. 2 L 7 2 4F A16WE 2001021300230 20010213 00230 2001 2 13 SWAA010221 4 20010124 A 2565 INDICATOR BOEING 737 7372H4 138448C NM ESCAPE SLIDE OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 087SW 22903 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. RE-ADJUSTED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001021300231 20010213 00231 2001 2 13 SWAA010222 4 20010124 A 2565 BOTTLE BOEING 737 7377H4 NM ESCAPE SLIDE DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 700GS 27835 DURING SCHEDULED RON CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001021300232 20010213 00232 2001 2 13 SWAA010223 4 20010124 A 2565 416A2302 RETAINER BOEING 737 7377H4 NM ESCAPE SLIDE OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 782SA 29808 FWD ENTRY DOOR EMERGENCY EVAC SLIDE RETENTION BAR HITTING FUSELAGE DURING DOOR CLOSING/OPENING. REMOVED AND REPLACED EV AC SLIDE COVER PER MM. 2 L 7 2 4F RT A16WE 2001021300233 20010213 00233 NM 2001 2 13 SWAA010224 1 20010124 A 3350 0L3071BPL5GPL BULB BOEING 737 7372H4 138448C NM CABIN FLOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED C4 CHECK, FOUND 1 RED EEPLS BULB INOP. RELAMPED EEPLS BULB PER MM. 2 L 7 2 4F A16WE 2001021300234 20010213 00234 NM 2001 2 13 SWAA010225 1 20010124 A 5310 6551698 SPLICE BOEING 737 7372H4 138448C NM CARGO BAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED D-CHECK, FOUND STR SPLICE ANGLE CORRODED AT BS 907, STR 25L. REPAIRED STR SPLICE ANGLE PER SRM. 2 L 7 2 4F A16WE 2001021300235 20010213 00235 NM 2001 2 13 SWAA010226 1 20010123 A 5311 6546529 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED D-CHECK, FOUND 2 FUSELAGE FRAME CRACKS BS 440, RBL 37, WL 158 & WL 160. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2001021300236 20010213 00236 NM 2001 2 13 SWAA010227 1 20010124 A 5311 6554892 FRAME BOEING 737 7372H4 138448C NM E/E BAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED D-CHECK, FOUND 2 FUSELAGE FRAME CRACKS AT BS 344, LBL 38, 4 ABOVE STR 24L & LBL 44, ABOVE STR 23L. REP AIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2001021300237 20010213 00237 NM 2001 2 13 SWAA010228 1 20010123 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN FLOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVERS CRACKED AT ROW 1 & AT AFT GALLEY. REMOVED AND REPLACED TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 2001021300238 20010213 00238 2001 2 13 SWAA010229 4 20010123 A 2565 6557463 BRACKET BOEING 737 7373H4 1384600 NM ESCAPE SLIDE LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BRACKET LOOSE. SECURED GIRT BRACKET PER MM. 2 L 7 2 4F RT A16WE 2001021300239 20010213 00239 NM 2001 2 13 SWAA010230 1 20010122 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 355SW 25250 DURING SCHEDULED SPECIAL VISIT AT DALFORT, FOUND 8 BS 178 BULKHEAD WEB CRACKS AT LBL 17.1 TO RBL 17.1, WL 198 TO WL 232. REPAIRED BULKHEAD WEB PER SRM. 2 L 7 2 4F RT A16WE 2001021300240 20010213 00240 NM 2001 2 13 SWAA010231 1 20010124 A 5320 6517583 BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 355SW 25250 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT RBL 17.1, WL 227. REPAIRED VERTICAL BEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2001021300241 20010213 00241 NM 2001 2 13 SWAA010232 1 20010124 A 5311 963820 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 620SW 28036 DURING SCHEDULED 1/2D CHECK, FOUND BS 178 RT SIDE CRACKED AT RBL 28.5. REMOVED AND REPLACED SIDE CHORD PER ACO. 2 L 7 2 4F RT A16WE 2001021300242 20010213 00242 NM 2001 2 13 SWAA010233 1 20010124 A 5730 65C27043 SKIN BOEING 737 7372H4 138448C NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED C4 CHECK, FOUND RT WING UPPER WING SKIN CRACKED AT STA 160, AFT SPAR. REPAIRED SKIN PER T1-257-014. 2 L 7 2 4F A16WE 2001021300243 20010213 00243 NM 2001 2 13 SWAA010234 1 20010124 A 3030 0851HT PROBE BOEING 737 7377H4 NM EMPENNAGE INOPERATIVE A SWAA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 729SW 27861 DIVERSION, LEFT ELEVATOR PITOT HEAT INOP. DIVERTED DUE TO DESTINATION WEATHER. REMOVED AND REPLACED PITOT HEAT PROBE P ER MM. LEAK & OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2001021300244 20010213 00244 NM 2001 2 13 SWAA010235 1 20010124 A 5743 6567172 FITTING BOEING 737 7373Q8 1384670 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED D-CHECK, FOUND RT MLG STABILIZER BEAM FITTING CORRODED. REMOVED AND REPLACED STABILIZER FITTING PER MM . 2 L 7 2 4F RT A16WE 2001021300245 20010213 00245 2001 2 13 SWAA010236 4 20010124 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM PAX DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001021300246 20010213 00246 NM 2001 2 13 SWAA010237 1 20010125 A 3350 101073 LIGHT BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 AFT ENTRY DOOR EMERGENCY EXIT LIGHT COVER LOOSE. SECURED LIGHT COVER PER MM. 2 L 7 2 4F A16WE 2001021300247 20010213 00247 NM 2001 2 13 SWAA010238 1 20010124 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN FLOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 312SW 23334 EEPLS TRACK COVER LOOSE AT ROW 9. SECURED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001021300248 20010213 00248 NM 2001 2 13 SWAA010239 1 20010124 A 5753 SKIN BOEING 737 7373Y0 1384671 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 308SA 1678 23498 DURING SCHEDULED C2 CHECK, FOUND RT WING T/E OUTBOARD AFT FLAP DELAMINATED AT PREVIOUS REPAIR, INBOARD END. REMOVED AND REPLACED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2001021300249 20010213 00249 2001 2 13 SWAA010240 4 20010124 A 2565 65C168209 RETAINER BOEING 737 7373H4 1384600 NM ESCAPE SLIDE LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 630WN 27705 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT RETAINER HOOK LOOSE. SECURED RETAINER HOOK PE R MM. 2 L 7 2 4F RT A16WE 2001021300250 20010213 00250 2001 2 13 SWAA010241 4 20010125 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 630WN 27705 DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001021300251 20010213 00251 NM 2001 2 13 SWAA010242 1 20010125 A 5314 6545866 KEELBEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 665WN 23497 DURING SCHEDULED SPECIAL VISIT, FOUND RT LOWER KEEL BEAM CORRODED AT BS 525. REPAIRED KEEL BEAM PER RA. 2 L 7 2 4F RT A16WE 2001021300252 20010213 00252 NM 2001 2 13 SWAA010243 1 20010125 A 5320 6517583 BEAM BOEING 737 7373Q8 1384670 NM BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAMS CRACKED AT LBL 17.1, WL 184 & RBL 5.7, WL 184. REPAIRED VERTICAL BEAMS PER ER. 2 L 7 2 4F RT A16WE 2001021300253 20010213 00253 NM 2001 2 13 SWAA010244 1 20010125 A 5314 6545866 KEELBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED D-CHECK, FOUND KEEL BEAM CORRODED AT BS 723, LBL 7. REPAIRED KEEL BEAM PER ER. 2 L 7 2 4F RT A16WE 2001021300254 20010213 00254 NM 2001 2 13 SWAA010245 1 20010124 A 3350 079123 COVER BOEING 737 7375H4 138449D NM CABIN FLOOR DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 523SW 26565 DURING SCHEDULED C4 CHECK, FOUND EEPLS TRACK COVER DAMAGED AT ROW 12. REPLACED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001021300255 20010213 00255 NM 2001 2 13 SWAA010246 1 20010124 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN FLOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 742SW 29278 DURING SCHEDULED C4 CHECK, FOUND EEPLS TRACK COVER CRACKED AT ROWS 1, 11, 14 & 19. REMOVED AND REPLACED TRACK COVERS PE R MM. 2 L 7 2 4F RT A16WE 2001021300256 20010213 00256 NM 2001 2 13 SWAA010247 1 20010125 A 5743 6567172 FITTING BOEING 737 7375H4 138449D NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 512SW 24189 DURING SCHEDULED D-CHECK AT DALFORT, FOUND LT MLG SUPPORT BEAM FITTING CRACKED. REMOVED AND REPLACED BEAM FITTING PER A CO. 2 L 7 2 4F RT A16WE 2001021300257 20010213 00257 NM 2001 2 13 SWAA010248 1 20010124 A 5712 6545445 RIB BOEING 737 7373Q8 1384670 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED D-CHECK, FOUND LT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN S-2 & S-3. REPAIRED RIB LOWER CHO RD PER ER. 2 L 7 2 4F RT A16WE 2001021300258 20010213 00258 NM 2001 2 13 SWAA010249 1 20010125 A 5313 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED D-CHECK, FOUND STR CLIPS CRACKED AT BS 400, STR 4R, BS 440, STR 16L, BS 616, STR 5L & BS 727C, STR 3L. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001021300259 20010213 00259 NM 2001 2 13 SWAA010250 1 20010125 A 5313 BAC1498 STRINGER BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED D-CHECK, FOUND STRINGERS CRACKED AT BS 400, STR 4R, BS 440, STR 16L. REPAIRED STRINGERS PER SRM. 2 L 7 2 4F RT A16WE 2001021300260 20010213 00260 NM 2001 2 13 SWAA010251 1 20010125 A 5310 6551698 SPLICE BOEING 737 7373Q8 1384670 NM STRINGER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED D-CHECK, FOUND STR SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM & T1-A51- 002. 2 L 7 2 4F RT A16WE 2001021300261 20010213 00261 NM 2001 2 13 SWAA010252 1 20010125 A 5311 6546546 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 787 & 727C, BETWEEN STR 8R & 9R, BS 767& 827 BETWEEN STR 8 L & 9L, & BS 887, BETWEEN STR 8L & 9L. REPAIRED FRAMES PER ER & SRM. 2 L 7 2 4F RT A16WE 2001021300262 20010213 00262 NM 2001 2 13 SWAA010253 1 20010125 A 5311 6546525 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, RBL 68, WL 268. REPAIRED FRAME PER ER & SRM. 2 L 7 2 4F RT A16WE 2001021300263 20010213 00263 NM 2001 2 13 SWAA010254 1 20010125 A 5311 6546546 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, BETWEEN STR 8R & 9R. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2001021300264 20010213 00264 NM 2001 2 13 SWAA010255 1 20010125 A 5311 6546558 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, BETWEEN STR 1L & 2L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001021300265 20010213 00265 NM 2001 2 13 SWAA010256 1 20010125 A 2751 10619264 INDICATOR BOEING 737 7372H4 138448C NM COCKPIT ERRATIC A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 081SW 22730 AIR TURNBACK, FLAPS WOULD NOT RETRACT FROM POSITION 5. NO C/B TRIPPED AND NO ASYMETRIC CONDITION. ALT FLAPS USED TO LA ND. REMOVED AND REPLACED FLAP POSITION IND. OPS CHECK GOOD PER MM. 2 L 7 2 4F A16WE 2001021300266 20010213 00266 NM 2001 2 13 VNAA0101007 1 20010110 A 3350 501122803 POWER SUPPLY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN FAILED A VNAA O OTHER O OTHER UK UNKNOWN 1 GL 07 442JS 11742 3060 THE CREW REPORTED THAT THE EMERGENCY POWER SUPPLY WILL NOT TEST. THE AIRCRAFT WAS FERRIED TO PIT WHERE MAINTENANCE INSP ECT AND REPLACED THE EMERGENCY POWER SUPPLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001021300267 20010213 00267 NM 2001 2 13 VNAA0101009 1 20010112 A 2530 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COFFEE MAKER SHORTED A VNAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 328JS 3030 THIRTY MINUTES INTO THE FLIGHT, THE FLIGHT ATTENDANT INFORMED THE CAPTAIN THAT THERE WAS A ELECTRICAL SMELL IN THE GALLE Y. THE FIRST OFFICER WENT BACK AND CONFIRMED THIS. THE CREW INFORMED DISPATCH THAT THEY WERE RETURNING TO PIT. THE CR EW WAS ADVISED TO GO TO CAK BECAUSE OF THE AVAILABILITY OF MAINTENANCE BUT THE CREW WANTED TO GET ON THE GROUND. THE CR EW STATED THIS WAS ONLY A PRECAUTIONARY LANDING, NO FIRE OR EMERGENCY WAS DECLARED. FLIGHT 4191 LANDED WITH NO FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 HOT JUG AND CONNECTOR PINS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 25-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001021300268 20010213 00268 NM 2001 2 13 VNAA0101011 1 20010115 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN FAILED A VNAA O OTHER O OTHER UK UNKNOWN 1 GL 07 440JS 12576 3058 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 4, 5, AND 6 WERE NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001021300269 20010213 00269 NM 2001 2 13 VNAA0101010 1 20010115 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN FAILED A VNAA O OTHER O OTHER UK UNKNOWN 1 GL 07 442JS 13367 3060 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 4 AND 7 WERE NOT WORKING. THE AIRCRAFT WAS FERRIED TO PIT WERE MA INTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIO NAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001021300270 20010213 00270 NM 2001 2 13 VNAA0101012 1 20010116 A 2420 2438 CONTROL UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ALTERNATOR FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 433JS 10464 3047 THE CREW RECEIVED A RIGHT HAND ALTERNATOR FAIL CAS MESSAGE AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE ALTERNATOR CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND T HE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001021300271 20010213 00271 2001 2 13 VNAA0101020 4 20010122 A 3130 RECORDER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FLIGHT DATA MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 424JS 3033 DURING THE TAKEOFF ROLL, THE CREW RECEIVED A FLIGHT DATA RECORDER FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE CREW CLEARE D THE RUNWAY AND RESET THE FLIGHT DATA RECORDER. FLIGHT 4011 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITHO UT ANY FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001021300272 20010213 00272 NE 2001 2 13 VNAA0101019 2 20010121 A 7321 EEC DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ENGINE MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 424JS 3033 DURING THE TAKEOFF ROLL, THE CREW RECEIVED A CAS MESSAGE FOR LEFT HAND ELECTRONIC CONTROL UNIT FAIL. FLIGHT 4135 ABORTE D TAKEOFF. AFTER THE AIRCRAFT CLEARED THE RUNWAY, THE CREW RESET THE ELECTRONIC CONTROL UNIT AND WAS CLEARED FOR ANOTHE R TAKEOFF ATTEMPT. FLIGHT 4135 DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001021300273 20010213 00273 NM 2001 2 13 VNAA0101018 1 20010120 A 3060 BRUSH BLOCK DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT PROP HEAT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 425JS 3037 DURING THE TAKEOFF ROLL, THE CREW RECEIVED AN AMBER CAS MESSAGE FOR LEFT PROP HEAT FAIL AND A CHIME. FLIGHT 4001 ABORTE D TAKE OFF. MAINTENANCE INSPECTED AND CLEANED THE BRUSH BLOCK AND SLIP RING IN ACCORDANCE WITH DORNIER MAINTENANCE MANU AL 30-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001021300274 20010213 00274 NM 2001 2 13 VNAA0101017 1 20010120 A 7331 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FUEL FEED SENSOR LOOSE A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 431JS 3028 WHILE ATTEMPTING TO TAKEOFF, THE CREW RECEIVED A FUEL FEED TEMPERATURE CAS MESSAGE AND ABORTED TAKEOFF. MAINTENANCE INS PECTED AND TIGHTENED THE CANNON PLUG FOR THE FUEL FEED SENSOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 28-00-00. O PERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001021300275 20010213 00275 NM 2001 2 13 VNAA0101015 1 20010117 A 3397 WIRE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ROW 9 FAILED A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 07 423JS 3032 THE CREW REPORTED THAT THE EMERGENCY LIGHT AND BOARDING LIGHT BY ROW 9A WAS NOT WORKING. MAINTENANCE INSPECT AND REPAIR ED A BROKEN WIRE IN ACCORDANCE WITH STANDARD MAINTENANCE PRACTICES. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001021300276 20010213 00276 NM 2001 2 13 VNAA0101014 1 20010117 A 3350 501122803 POWER SUPPLY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN FAILED A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 07 440JS 13028 3058 THE CREW REPORTED THAT THE EMERGENCY POWER SUPPLY UNITS WOULD NOT TEST. THE AIRCRAFT WAS FERRIED TO PIT. MAINTENANCE I NSPECTED AND REPLACED BOTH EMERGENCY POWER SUPPLY UNITS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATI ONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001021300277 20010213 00277 NM 2001 2 13 VNAA0101013 1 20010116 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ROW 9 FAILED A VNAA O OTHER O OTHER UK UNKNOWN 1 GL 07 423JS 12511 3032 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROW 9A WAS NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE EMERGEN CY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT W AS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001021300278 20010213 00278 EA 2001 2 13 SWIA972295 1 20010119 A 2751 COMPUTER CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 07 406SW 7030 FLAP FAIL CAUTION MESSAGE AFTER LANDING. RESET THE FLAP CONTROL COMPUTERS. RAN FLAPS SEVERAL TIMES ALL WITHIN LIMITS. OPS CHECKS GOOD 27-00-00. C/W AD 98-20-01. 2 L 7 2 4F RT A21EA 2001021300279 20010213 00279 EA 2001 2 13 SWIA972296 1 20010117 A 4990 OIL COOLER CNDAIR CL600 CL6002B19 EA APU CLOGGED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 406SW 7030 APU OIL PRESSURE CAUTION MSG COMES ON AFTER TAKEOFF AND REMAINS ON. RETURNED TO SLC. TROUBLESHOT SYSTEM. FAULT CODES IN ECU INDICATED HOT INDICATION DUE TO HIGH OIL TEMP. REPLACED PLUGGED OIL COOLER IAW MM 49-91-07 AND HIGH OIL TEMP SEN SOR IAW MM 49-91-25. CHECKED FOR CONTAMINENTS IN OIL FILTER, NONE NOTED. OPS AND LEAK CHECKS GOOD. CLEARED FAULT CODE S IN ECU. P/N ON 160382-1, S/N ON 1514, P/N OFF 160346-2, S/N OFF 76-974. 2 L 7 2 4F RT A21EA 2001021300280 20010213 00280 SO 2001 2 13 SWIA972297 1 20010127 A 2750 CONTROL UNIT EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE TE FLAPS FAILED A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 293SW 120320 WHEN SELECTING FLAPS UP AFTER TAKEOFF HAD A CONTROL FAULT FOR THE OUTBOARD FLAPS. FOLLOWED QRH PROCEDURE BUT WOULD NOT RESET. RETURNED TO SFO. REPLACED FLAPS CONTROL UNIT. FLAP SYSTEM OPS CHECKS OK. P/N ON: 347-200-1001, S/N ON: 0034 . 2 L 7 2 4T 4 T RT A31SO E20NE 2001021300281 20010213 00281 SO 2001 2 13 SWIA972298 1 20010128 A 3150 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE PITOT STATIC FALSE INDICATION A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 214SW 120280 HIGH SPEED AURAL WARNING UPON APPLICATION OF TAKEOFF POWER. PRESSURIZED PITOT STATIC SYSTEM USING TEST BOX THROUGH ENTI RE AIRSPEED RANGE IAW MM 34-17-01. AURAL WARNING OPS CHECKS GOOD. RAN BOTH ENGINES AT TAKEOFF POWER IN TAKEOFF CONFIGU RATION WITH NO HIGH SPEED WARNINGS. AURAL WARNING SYSTEM OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001021300282 20010213 00282 SO 2001 2 13 SWIA972299 1 20010126 A 7712 PROBE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE TORQUE FAILED A SWIA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 NM 07 237SW 120314 DURING TAKEOFF ROLL JUST AFTER TORQUE REACHED 80 PERCENT AND 100 PERCENT , FIRST OFFICER SAW TORQUE ON NR 1 (LEFT) ENGIN E DROP. DIGITAL DROPPED TO 4 PERCENT AND ANALOG DROPPED TO 10 PERCENT BUT WAS FLUCTUATING. JUST AS TAKEOFF WAS ABORTED THE LEFT ENGINE LOST THRUST AND YAWED LEFT AS POWER WAS BROUGHT TO FLIGHT IDLE. ENGINE PARAMETERS APPEARED NORMAL ON T AXI BACK TO RAMP. INSTALLED SERVICEABLE TORQUE SIGNAL CONDITIONER. ALSO INSTALLED SERVICEABLE TORQUE PROBE. PERFORMED FULL POWER RUN. OPS CHECKS GOOD. S/N ON: 1730. 2 L 7 2 4T 4 T RT A31SO E20NE 2001021300283 20010213 00283 2001 2 13 SWIA972300 4 20010126 A 3414 INDICATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE AIRSPEED MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 203SW 120240 JUST AFTER GEAR RETRACT ON TAKEOFF, ERRONEOUS HIGH SPEED WARNING SOUNDED TWO TIMES THEN EXTINGUISH. TEN MINUTES LATER J UST BEFORE LEVEL OFF AT 26000 WARNINGS START AGAIN AND PERSIST. PULLED POWER BACK IN CRUISE AND WARNING CEASED. RETUNE D TO SLC. REMOVED AND REPLACED RIGHT AIR SPEED INDICATOR. PERFORMED PITOT STATIC CHECK ON RIGHT ASI ALL CHECKS GOOD. P/N ON: 39948-E2908, S/N ON: 2048, P/N OFF 320 ASI S/N ON: AH485. 2 L 7 2 4T 4 T RT A31SO E20NE 2001021300285 20010213 00285 SO 2001 2 13 SWIA972302 1 20010126 A 3260 SENSOR EMB 120 EMB120RT SO PWA 118 PW118 NE RT MLG PROX FAILED A SWIA O OTHER O OTHER DE DESCENT 1 NM 07 162CA 120150 LANDING GEAR WOULD NOT EXTEND NORMALLY. CYCLED TWICE, NO EFFECT. PERFORMED QRH GEAR EXTENSION BY ELECTRICAL OVERRIDE T O EXTEND GEAR. REPLACED RIGHT MAIN A DOWNLOCK PROXIMITY SENSOR AND HARNESS PER MM 32-61-01. PERFORMED MULTIPLE GEAR SW INGS. OPS CHECK GOOD. P/N: 120-41127-001 2 L 7 2 4T 4 T RT A31SO E20NE 2001021300286 20010213 00286 EU 2001 2 13 MALA010107 1 20010109 A 3350 330151 SWITCH SAAB SF340 340B 7860101 EU LIGHT PANEL FAILED A MALA O OTHER N FALSE WARNING CR CRUISE 1 GL 15 447XJ 447 EMERGENCY LIGHTS UNARMED LIGHT ILLUMINATED WITH EMERGENCY LIGHT SWITCH IN ARMED POSITION. MAINTENANCE REPLACED EMERGENC Y LIGHT SWITCH AT FA''''S PANEL. ALL CHECKS GOOD. P/N 3301-51, S/N ON 2196. 2 L 7 2 4T RT A52EU 2001021300297 20010213 00297 EU 2001 2 13 MALA010120 1 20010104 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 456XJ 456 FOUND DURING C-CHECK, FLOORBOARD FLANGE BL0.0 FROM STA 294 TO 345.0 HAS CORROSION. REFER TO CELSIUS TASK CARD 1521, W0 19193. MAINTENANCE REMOVED CORROSION, CHECK LIMIT, BLENDED OUT CORROSION, REMAINING MATERIALS WITHIN LIMITS REF SRM 51 -10-10. PREPED, ALODINED AND PRIMED BLENDED AREAS, PAINTED SET TRACK FLANGES IAW SRM 51-20-10. 2 L 7 2 4T RT A52EU 2001021300298 20010213 00298 EU 2001 2 13 MALA010121 1 20010114 A 3060 666000219 BRUSH BLOCK SAAB SF340 340B 7860101 EU LT & RT PROP FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 417XJ 340B417 LT AND RT PROP LIGHTS ILLUMINATE WHEN PRO DEICE SELECTED TO ORM (AFTER 30 SECONDS) AND MAX (IMMEDIATELY) WHILE AIRBORNE. ORH COMPLETED, DOES NOT RECTIFY THE PROBLEM. TESTS NORMAL ON GROUND, AIR TURNBACK TO MSP. MAINTENANCE REPLACED LT AN D RT PROP BRUSH BLOCKS P/N 666000219. 2 L 7 2 4T RT A52EU 2001021300299 20010213 00299 EU 2001 2 13 MALA010122 1 20010116 A 3230 DOWNLOCK BAC 146 AVRO146RJ85A 1500097 EU NLG LACK OF LUBE A MALA O OTHER O OTHER LD LANDING 1 GL 15 508XJ E2317 NOSE GEAR DID NOT COME DOWN UPON INITIAL EXTENSION. PILOT WAS GOING TO CYCLE GEAR THEN NOSE RELEASED AND CAME DOWN. MAI NTENANCE INSPECTED NOSE GEAR NO OBVIOUS DEFECTS NOTED, INSPECTED A/C AND FOUND SAFE FOR ONE FERRY FLIGHT FROM XNA TO MSP . NOSE GEAR PINNED IN DOWN POSITION. MAINTENANCE FOUND UPLOCK/DOWNLOCK PLUNGER PIN STICKY LUBRICATED ITEM 20 PER AMM 1 2-20-21 UNIT TOOK ONE TUBE OF GREASE, CYCLED GEAR NUMBEROUS TIMES. OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 2001021300300 20010213 00300 EU 2001 2 13 MALA010123 1 20010116 A 3610 5056T88P01 VALVE SAAB SF340 SF340A 7850100 EU START BLEED FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 115XJ 340A115 AIR RETURN TO DTW WITH LT AIR VALVE LIGHT ON. MAINTENANCE REPLACED LT START BLEED VALVE P/N 5056T88P01, S/NB ON AEX1053 7, S/N OFF AEX10630. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2001021300301 20010213 00301 EU 2001 2 13 MALA010124 1 20010117 A 5347 SEAT TRACK SAAB SF340 SF340A 7850100 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 27XJ 027 FOUND DURING 4K HEAVY CHECK, DURING INSPECTION FOUND CORROSION ON LT CENTER AISLE SEAT TRACK INBOARD UPPER FLOORBOARD FL ANGE FROM STA 650.88 TO 686.8. COMPLETED REPAIR IAW EO S53078. 2 L 7 2 4T RT A52EU 2001021300302 20010213 00302 EU 2001 2 13 MALA010125 1 20010117 A 5347 SEAT TRACK SAAB SF340 SF340A 7850100 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 27XJ 027 FOUND DURING 4K HEAVY CHECK, DURING INSPECTION FOUND CORROSION ON RT CENTER AISLE SEAT TRACK UPPER FLOORBOARD FLANGE FRO M STA 657 TO 686.8. COMPLETED REPAIR IAW EO S53078. 2 L 7 2 4T RT A52EU 2001021300303 20010213 00303 NE 2001 2 13 MALA010126 2 20010114 A 7320 6055T19P14 HMU SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE NR 1 ENGINE FAILED A MALA E C ENGINE SHUTDOWN ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 15 106XJ 106 WHILE ADVANCING THE PL FOR TAKEOFF NR 1 ENGINE TORQUE RAN AWAY, OVER TORQUED RETARDED PL- NO TORQUE REDUCTION, SHUT DOWN ENGINE WITH CL. DID NOT NOTE TEMP BUT DID NOT SEE OVER TEMP LIGHT ILLUMINATED. ABORTED TAKEOFF. MAINTENANCE REMOVED FDAU SENT IN FOR DOWN LOADING. DUE TO OVER TORQUE, MAINTENANCE REPLACED LT HMU PER GE MM 72-00-00. LT HMU P/N 6055T19P 14, S/N ON UDAJ3337, S/N OFF UDAJ1468. ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE6 2001021300304 20010213 00304 EU 2001 2 13 MALA010127 1 20010114 A 2750 8519M3 CONTROL UNIT SAAB SF340 SF340A 7850100 EU TE FLAPS FAILED A MALA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 GL 15 99XJ 099 DURING APPROACH INTO PIA, AFTER SELECTING FLAPS 20 DEGREES, CREW RECEIVED AN AURAL WARNING OF TOO LOW FLAPS AT APPROXIMA TELY 500 FEET AGL. CREW EXECUTED A MISSED APPROACH AND TRIED TO COMPLETE ANOTHER APP AND LANDING AFTER SELECTING FLAPS 20 DEGREES NOTICED THAT THE FLAP INDICATOR WAS POINTED TO 17 DEGREES, EXECUTED ANOTHER MISSED APP AND RETURNED TO DTW. MAINTENANCE REPLACED FLAP COMPUTER, SEE MM 409 CARD 091674 FOR DETAILS, RESECURE FLAP STOP, REINSTALLED FLOOR PANEL, REM OVED AND REPLACED FLAP CONTROL BOX P/N 8519M3, S/N ON 051, S/N OFF 145, CHECK FLAP RIGGING IAW ASSB MM 27-51-00. ALL CH ECK GOOD. 2 L 7 2 4T RT A52EU 2001021300305 20010213 00305 EU 2001 2 13 MALA010139 1 20010124 A 2822 5034T91P06 PUMP SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE FUEL BOOST FAILED A MALA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 15 402XJ 340B402 LT ENGINE EXPERIENCED UNCOMMANDED ROLLBACK CLIMBING THROUGH 6000 FT. CREW SHUT THE ENGINE DOWN AND RETURNED TO DTW. AT 5000 FT NR 1 ENGINE QUICKLY LOST 40 PERCENT TORQUE. ENGINE SEEMED TO RECOVER SLIGHTLY THEN CONTINUED ON TO LOSE POWER. ENGINE WAS SHUTDOWN AND ORH COMPLETED. MAINTENANCE REPLACED RT ENGINE FUEL BOOST PUMP AND FILTER P/N 5034T91P06, S/N ON LJA41237, S/N OFF LJA20693 IAW SF340 AMM CHAP 28. OPS CHECK GOOD. REFER TO MM 409 091503 FOR DETAILS. 2 L 7 2 4T 4 T RT A52EU E8NE 2001021300306 20010213 00306 NM 2001 2 13 UPS01234744 1 20010124 A 3210 NUT BOEING 727 72727C 138400J NM MLG LOOSE A IPXA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 939UP 19532 INSPECTION TYPE:N/A AFTER GEAR RETRACTION RIGHT MAIN GEAR DOOR WARNING AND RED GEAR DOOR LIGHTS REMAINED ILLUMINATED. S ELECTED GEAR UP 2 TIMES BEFORE LIGHTS EXTINGUISHED. FOUND RT GEAR DOOR WARNING SWITCH, JAM NUTS LOOSE, TIGHTENED JAM NU TS AND RE-SAFTIED NUTS, PERFORMED ADJ AND TEST PER MM 32-62-11. RT GEAR DOOR WARNING OPS CKS OK THIS CLEARS M 207973. 2 L 7 3 4F A3WE 2001021300307 20010213 00307 NM 2001 2 13 UPS01234750 1 20010109 A 5320 BRACKET BOEING 727 72731C 1384011 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C, ATTACH BRACKET LOCATED ON LT 870 FITTING IS CRACKED ALONG BEND LINE. BRACKET DERIVETED IAW SRM 51-30 -02, BRACKET FABRICATED IAW SRM 51-20- 01, BRACKET INSTALLED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 2001021300308 20010213 00308 NM 2001 2 13 UPS01234786 1 20010121 A 3350 LIGHT BOEING 727 72722C 138400F NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE:IN, NEITHER EMERGENCY ENT LIGHT WORKING. RESET SWITCH, OPS CHECK IAW MM 33-50-01. OPS CHECK NORMAL. 2 L 7 3 4F A3WE 2001021300309 20010213 00309 NM 2001 2 13 UPS01234787 1 20010122 A 3350 BATTERY PACK BOEING 727 727172C 1384058 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 916UP 19808 INSPECTION TYPE:IN, EMERGENCY EXIT LIGHT DOES NOT COME ON WHEN ARMED BY A/C. BATTERY CHECK GOOD. REMOVED AND REPLACED, RE-INSTALLED LIGHT ASSY. CHECKS GOOD. 2 L 7 3 4F A3WE 2001021300310 20010213 00310 NM 2001 2 13 UPS01234788 1 20010127 A 3260 SWITCH BOEING 727 72725C 138400H NM LANDING GEAR MALFUNCTIONED A IPXA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 948UP 19357 INSPECTION TYPE:IN, RIGHT LDG GEAR LIGHT NOT ILLUMINATED WHILE TAXIING IN RIGHT LDG GEAR LIGHT EXTINGUISHED STOPPED AIRC RAFT WHILE MAINTENANCE PINNED GEAR. LIGHT ILLUMINATED AGAIN BRIEFLY THEN WENT OUT AGAIN. REMOVED AND REPLACED RIGHT LA NDING GEAR DOWN AND LOCKED SWITCH AND CANNON PLUG, OPS CKS REQUIRED SEE LOG PAGE 226825 ITEM 3. 2 L 7 3 4F A3WE 2001021300311 20010213 00311 SO 2001 2 13 COMA0110031 1 20010126 A 2916 RESERVOIR EMB 120 EMB120RT SO HYD SYSTEM LOW A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 264CA 120256 HYDRAULIC RESERVOIR LOW LEVEL CAUTION. SERVICED HYD RESERVOIR, NO DEFECTS FOUND WITH HYDRAULIC SYSTEM. 2 L 7 2 4T RT A31SO 2001021300312 20010213 00312 2001 2 13 COMA0160171 4 20010126 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 973CA 7146 STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001021300313 20010213 00313 2001 2 13 COMA0160170 4 20010126 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 948CA 7079 STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001021300314 20010213 00314 2001 2 13 COMA0160169 4 20010126 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 964CA 7129 STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001021300315 20010213 00315 2001 2 13 COMA0160168 4 20010126 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 964CA 7129 STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001021300316 20010213 00316 WP 2001 2 13 CALA0100072 1 20010126 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND A 1 INCH CRACK IN LT FUSELAGE SKIN ABOVE NR 1 ENGINE PYLON AT STA 1401. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, SHEET 3, 53-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 2001021300317 20010213 00317 WP 2001 2 13 CALA0100073 1 20010126 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 237 BETWEEN LONGERONS 17L AND 18L. THE SKIN WAS REMOVED AND REPLAC ED IAW SRM 53-34-0, FIGURE 2, PAGE 7, 51-30-2, 51-30-5, AND 51-10-3. 2 L 7 2 4F A6WE 2001021300318 20010213 00318 WP 2001 2 13 CALA0100074 1 20010126 A 5230 FITTING DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND A 2 INCH CRACK IN AFT CARGO DOOR LOWER FITTING. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLE D IAW SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-1. 2 L 7 2 4F A6WE 2001021300319 20010213 00319 WP 2001 2 13 CALA0100075 1 20010127 A 5230 WEB DOUG DC9 DC982 3022082 WP CARGO DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND AFT CARGO DOOR WEB CORRODED AROUND ATTACH RIVNUT HOLES. THE CORROSION WAS REMOVED IAW SRM 51-10-3. TH E CORRODED AREAS WERE REPAIRED IAW SRM 52-01, FIGURE 2 AND 51-10-3. 2 L 7 2 4F A6WE 2001021300320 20010213 00320 WP 2001 2 13 CALA0100076 1 20010127 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 275 BETWEEN LONGERONS 21L AND 22L. THE DENT WAS COLD WORKED IAW SR M 53-04-38. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04-38, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 2001021300321 20010213 00321 NM 2001 2 13 CALA0100077 1 20010127 A 5740 FITTING BOEING 737 7373T0 1384582 NM LT WING CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND LT WING REAR SPAR ATTACH FITTING CORRODED IN O/B LOWER FASTENERS AT WS 200. THE ATTACH FITTING WAS REP AIRED IAW SRM 51-20-05. 2 L 7 2 4F RT A16WE 2001021300322 20010213 00322 NM 2001 2 13 CALA0100078 1 20010127 A 5743 BEAM BOEING 737 7373T0 1384582 NM LT WING CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND LT WING REAR SPAR LT MLG TRUNNION BEAM STABILIZER FWD LINK CORRODED AT RSS 179.56. REPAIR WAS PERFORME D IAW SRM 51-20-05. 2 L 7 2 4F RT A16WE 2001021300323 20010213 00323 WP 2001 2 13 CALA0100079 1 20010129 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND AFT LT LAV FLOORBEAM CORRODED AT STA 1322, LBL 41. THE CORROSION WAS TRIMMED OUT AND A DOUBLER, REPAIR STRIP, AND SHIM WERE INSTALLED IAW SRM 53-05, FIGURE 20A, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 2001021300324 20010213 00324 WP 2001 2 13 CALA0100080 1 20010129 A 5230 PAN DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND A 1 INCH CRACK IN MID CARGO DOOR PAN. THE CRACK WAS STOP DRILLED IAW SRM 52-03, FIGURE 8. A REPAIR DO UBLER WAS INSTALLED IAW SRM 52-03, FIGURE 8, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 2001021300325 20010213 00325 2001 2 13 COMA0160167 4 20010126 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 963CA 7127 STALL FAIL CAUTION DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001021300326 20010213 00326 2001 2 13 COMA0160166 4 20010125 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 810CA 7370 STALL FAIL CAUTION DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001021300327 20010213 00327 EA 2001 2 13 COMA0160165 1 20010125 A 5755 600106021002 SPOILER CNDAIR CL600 CL6002B19 EA RIGHT BROKEN A COMA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 01 785CA 3987 7326 WHEN FLAP SELECTED TO 45 DEGGREES, THE AIRCRAFT ROLLED RIGHT. POST FLIGHT INSP FOUND RT FLIGHT SPOILER BROKEN. REPLACE D FLIGHT SPOILER. 2 L 7 2 4F RT A21EA 2001021300328 20010213 00328 WP 2001 2 13 PNSA010101 2 20010101 A 7200 ENGINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP LEFT STALLED A PNSA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 AL 03 41NE AC741B P44744 DURING CRUISE, JUST BEFORE DESCENT TO DESTINATION, LT ENGINE SHUTDOWN WITHOUT WARNING. ENGINE WAS SECURED AND LANDING W AS UNEVENTFUL. INVESTIGATION REVEALED METAL PARTICALS IN THE OIL FILTER AND ABNORMAL NOISE FROM THE GEARBOX. 2 L 7 2 4T 4 T RT A8SW E4WE 2001021300329 20010213 00329 EA 2001 2 13 COMA0160164 1 20010125 A 5610 NP1393212 WINDSHIELD CNDAIR CL600 CL6002B19 EA COCKPIT FAILED A COMA O OTHER O OTHER CR CRUISE 1 SO 01 931CA 9159 7037 CO-PILOTS WINDSHIELD SHATTERED. REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 2001021300330 20010213 00330 2001 2 13 COMA0160163 4 20010126 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 719CA 7253 STALL FAIL CAUTION DURING T/O.RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001021300331 20010213 00331 WP 2001 2 13 MWEA010137 1 20010129 A 2510 580748001 CABLE DOUG DC9 DC932 3022066 WP COCKPIT SEAT STUCK A MWEA O OTHER O OTHER LD LANDING 1 GL 31 205ME 47601 CAPTAINS CHAIR UNLATCHED AND MOVED FORWARD ON THE LANDING ROLL IN MILWAUKEE. LUBED FORWARD AND AFT CONTROL HANDLE TO FL EX LINKAGE, OPERATION CHECK GOOD. 2 L 7 2 4F A6WE 2001021300332 20010213 00332 WP 2001 2 13 TWAA0101701 1 20010128 A 3350 MISC0639 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 950U 49230 THE LT AND RT REAR OVERWING EMERGENCY EXIT LIGHTS WERE INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY. CHECK-C 11-11- 00 STL. 2 L 7 2 4F A6WE 2001021300334 20010213 00334 WP 2001 2 13 TWAA0101703 1 20010126 A 5313 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 DURING CHECK-C MAINT LONGERON 6L AT STA 718 WAS FOUND CRACKED AT LOWER FLANGE, .25 INCH CRACK. REMOVED AND REPLACED SEC TION OF LONGERON 6L AT STA 699 TO 718 PER SRM 53-02. INSTALLED DOUBLER ON FACE OF INTERCOSTAL AT LONGERON LEG, FABRICAT ED FROM 0.032 2024-T3. REINSTALLED INTERCOSTAL BETWEEN STA 718 AND 699. 2 L 7 2 4F A6WE 2001021300335 20010213 00335 NM 2001 2 13 HNAA0100009 1 20010122 A 7120 8DK1763001 MOUNT DHAV DHC8 DHC8102 2809003 NM NR 1 ENGINE BROKEN A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 909HA 018 DURING ENGINE CHANGE, THE AFT OUTBOARD VERTICAL MOUNT STRUT WAS FOUND BROKEN. THE STRUT WAS REPLACED. 2 H 7 2 4T RT A13NM 2001021300336 20010213 00336 NM 2001 2 13 F3LA200100011 1 20010126 A 5320 WEB BOEING 737 737228 13844AG NM CARGO DOORWAY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 234TR 3086 23004 DURING C-7 CHECK, INSPECTION REPORTED AFT CARGO DOOR SCUFFPLATE WEB CORRODED. REPLACED STRAP PER SRM 51-30-2 AND DRAWIN G NR 65-47957. 2 L 7 2 4F RT A16WE 2001021300337 20010213 00337 SO 2001 2 13 C2XA01IA059 1 20010125 A 3350 3025103 LIGHT EMB 145 EMB145 SO RT EXTERIOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13964 145123 BNA - DURING MAINTENANCE INSPECTION, THE TOP RT EXTERNAL OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAI NTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001021300338 20010213 00338 SO 2001 2 13 C2XA01IA060 1 20010127 A 5280 12036136001 BRACKET EMB 120 EMB120ER 3260203 SO LT MLG DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16731 120190 IAH - DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT MAIN LANDING GEAR OUTBOARD AFT GEAR DOOR HAD A BROK EN AFT HINGE BRACKET. MAINTENANCE REMOVED AND REPLACED THE AFFECTED HINGE BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RE TURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001021300339 20010213 00339 SO 2001 2 13 C2XAO1IA061 1 20010127 A 5280 12036136002 BRACKET EMB 120 EMB120ER 3260203 SO RT MLG DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16731 120190 IAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE RIGHT MAIN LANDING GEAR INBOARD AFT GEAR DOOR HAD A BROK EN FORWARD HINGE BRACKET. MAINTENANCE REMOVED AND REPLACED THE AFFECTED HINGE BRACKET, AND THE AIRCRAFT WAS APPROVED FO R RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001021300340 20010213 00340 SO 2001 2 13 C2XA01IA062 1 20010122 A 5320 14522459003 FLOOR SUPPORT EMB 145 EMB145ER SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14938 145029 IAH - DURING C-CHECK INSPECTION, THE CENTER FLOOR SUPPORT AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOOR SUPPORT IN ACCORDANCE WITH EMB145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001021300341 20010213 00341 NM 2001 2 13 01FDEA00046 1 20010126 A 2120 UNKNOWN BOEING 727 72722 1384002 NM COCKPIT ODOR A FDEA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 25 148FE 19086 AN ODOR OF ELECTRICAL OR BURNT MATCH NOTED IN COCKPIT. NO CIRCUIT BREAKERS POPPED AND NO EQUIPMENT FAILURE NOTED. INSP CARGO AND HAZARDOUS CONTAINER NO ODOR NOTED. INSP WIRES AND E&E COMP FOR ODOR NONE NOTED PER MM 20-30-000-6. 2 L 7 3 4F A3WE 2001021300346 20010213 00346 NM 2001 2 13 AT0100011 1 20010108 A 5347 SEAT TRACK BOEING 737 7372L9 1384497 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 FOUND LEFT IN BOARD SEAT TRACK HAS CORROSION BEYOND LIMITS BS 727. REMOVED AND REPLACED SECTION OF SEAT TRACK IAW B737 SRM 51-30-2, 53-10-5. 2 L 7 2 4F RT A16WE 2001021300347 20010213 00347 NM 2001 2 13 AT0100012 1 20010109 A 5321 FLOOR PANEL BOEING 737 7372L9 1384497 NM FUSELAGE DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 FOUND CABIN CENTER FLOOR PANEL SPONGY IN SEVERAL PLACES. REMOVED, FABRICATED AND INSTALLED NEW FLOOR PANEL IAW B737 SRM 53-20-1, 51-10-1 AND CMM 25-00-66. 2 L 7 2 4F RT A16WE 2001021300348 20010213 00348 NM 2001 2 13 AT0100013 1 20010109 A 5321 FLOOR PANEL BOEING 737 7372L9 1384497 NM CABIN TORN A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 FOUND CABIN FLOOR PANEL METAL SKIN TORN, GOUGED, CRACKED, AND PUNCTURED AT SEVERAL PLACES. REMOVED, FABRICATED, AND INS TALLED NEW FLOORBOARD IAW B737 SRM 53-20-1, 53-20-2, 51-10-1, CMM 25-00-66. 2 L 7 2 4F RT A16WE 2001021300349 20010213 00349 NM 2001 2 13 AT0100014 1 20010109 A 5315 FLOOR SUPPORT BOEING 737 7372L9 1384497 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 FOUND CORRODED FLOOR SUPPORT AT RBL 12 BS 344 - 360. REMOVED, FABRICATED, AND INSTALLED REPAIR IAW B737 SRM 51-40-4. 2 L 7 2 4F RT A16WE 2001021300350 20010213 00350 NM 2001 2 13 DHL2001717002 1 20010130 A 3150 WARNING SYSTEM BOEING 727 72723 1384004 NM TE FLAPS WILL NOT TEST A DHLA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SO 01 717DH 19389 FLIGHT CONTROL WARNING TEST SYSTEM WILL NOT TEST. NOTE-FLAPS AT 15 DEGREE AND SPEEDBRAKE DEPLOYED. RECYCLED FLAPS AND SPOILERS AS WELL AS NR 3 THROTTLE, RETESTED SYSTEM USING OVERHEAD TEST SWITCH, SYSTEM OP''S CHECKS NORMAL PER 31-26-0 AN D IS OK FOR SERVICE. 2 L 7 3 4F A3WE 2001021300351 20010213 00351 2001 2 13 DHL2001717003 4 20010130 A 3418 WARNING SYSTEM BOEING 727 72723 1384004 NM STALL WARNING FALSE ACTIVATION A DHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 717DH 19389 AT APPOX 95 KTS IAS STICK SHAKER ACTIVATED T/O ABORTED. UPON CREW DEBRIEF, FOUND 3 SECONDS OF FLIGHT TIME ON CAPTS CLOC K. THAT IN COMBINATION WITH STICK SHAKER INDICATE THAT THE NOSE STRUT FULLY EXTENDED ON T/O ROLL. CHECKED STALL VANE O PERATION PER 34-18-0. STALL VANE CALIBRATION TEST WELL WITHIN LIMITS AND STICK SHAKER SYSTEM OPS NORMAL PER 34-18-0. A /C IS OK FOR SERVICE. 2 L 7 3 4F A3WE 2001021300352 20010213 00352 NM 2001 2 13 QXEA0100077 1 20010127 A 2120 UNKNOWN DHAV DHC8 DHC8202 2809007 NM CABIN ODOR A QXEA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 358PH 506 SEA- AFTER PUSHBACK, FLIGHT ATTENDANT REPORTED BURNING SMELL IN FRONT OF CABIN, FIRST OFFICER WENT TO CABIN AND CONFIRME D. CONDITION OCCURRED AT IDLE POWER WITH BLEEDS ON. GROUND RAN AIRCRAFT AT IDLE POWER WITH BLEEDS ON NR 1 & NR 2 ENGINE . CYCLED BLEEDS AND HEAT CABIN AND FLIGHT COMPARTMENT. COULD NOT DUPLICATE SMELL. CONSULT WITH CAPTAIN NO BURN SMELL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001021300353 20010213 00353 WP 2001 2 13 IXXA0100004 1 20010125 A 7830 FR02B COWLING DOUG DC8 DC871F 302199D WP ENGINE T/R DAMAGED A IXXA O OTHER D INFLIGHT SEPARATION DE DESCENT 1 SW 11 829BX 83464 1955 45994 DURING DESCENT FROM RDU TO ATL, THE FLIGHT CREW NOTICED THE NUMBER THREE ENGINE THRUST REVERSER WAS VERY SLOW TO STOW AF TER DEPLOYMENT. THE FLIGHT CONTINUED TO ATL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE ENGINE WHICH REVEALED A PORTION OF THE NUMBER THREE ENGING INBOARD THRUST REVERSER TRANSLATING COWLING HAD DEPARTED FROM THE ENGINE. MAINTEN ANCE REPLACED THE INBOARD THRUST REVERSER HALF IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2001021300354 20010213 00354 NE 2001 2 13 ARWA0010103 2 20010128 A 7532 BLEED VALVE PWA DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE NR 2 ENGINE DIRTY A ARWA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 19 1808E 46105 671318 AT THE BEGINNING OF TAKEOFF ROLL NR 2 ENGINE HAD COMPRESSOR STALL. ENGINE PARAMETER WERE TAKEOFF, EPR WAS 1.88; DROPPED TO 1.75 N2 AND RECOVERED, FUEL FLOW DMI AND EGT WAS NORMAL. PERFORMED VISUAL CHECK AIR BLEED VALVE, CLEANED AND LUBRI CATED IAW M/M 75-30-3; CHECKED DURING ENGINE RUN IAW M/M 71-00, WORKS NORMAL. 2 L 7 4 4F 4 F 4A25 1E8 2001041000022 20010410 00022 NM 2001 4 10 01FDEA00050 1 20010130 A 5311 6515938 FRAME BOEING 727 727227 1384078 NM FUSELAGE MISDRILLED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 491FE 21529 FIGURE EIGHT HOLE IN FRAME BS 700 AT STR 7R. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 53-10-4. 2 L 7 3 4F A3WE 2001021300355 20010213 00355 EA 2001 2 13 COMA0160172 1 20010129 A 5553 600210617 BUSHING CNDAIR CL600 CL6002B19 EA VERTICAL STAB WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 937CA 7044 LEFT VERTICAL STABILIZER STAB BUSHING WORN. REMOVED AND REPLACED BUSHING (P/N 600-21061-7). MACHINED BUSHING FLANGE TH ICKNESS TO .077 INCH AND REMOVED INSIDE DIAMETER TO 1.5002 IAW CRJ AMM 20-26-00-910-803, DRAWING 600-21061 AND WWVAC EO 601R-55-2175. 2 L 7 2 4F RT A21EA 2001021300356 20010213 00356 NM 2001 2 13 UPS01234805 1 20010130 A 5310 STRUCTURE BOEING 727 7272A1 138407F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 213UP 21341 INSPECTION TYPE:IN, CRACK FOUND IN LIGHTENING HOLE, AFT AIRSTAIRS AREA AT APPROX STATION 1283 AT WL 175, LT SIDE. STOPP ED DRILLED CRACK PER SRM 51-10-1/11, ITEM 9A. 2 L 7 3 4F A3WE 2001030700634 20010307 00634 NM 2001 3 7 UPS01434803 1 20010130 A 5711 SPAR CAP BOEING 747 747200B NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 524UP INSPECTION TYPE:IN PER EO-13738A REPAIR RT WING LWR SKIN FWD ANGLE ATTACH CHORD. *S/D* REPAIR ACCOMPLISHED PER EO -137 38A. 1 L 7 4 4F RT A20WE 2001021300357 20010213 00357 WP 2001 2 13 UPS01834777 1 20010123 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1,3 RIGHT WING L/E UPPER RIBS ARE CRACKED AT FASTENER END AT XS442.185, XS448.581, XS467.323, XS478.897 . REPAIRED RIBS IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001021300358 20010213 00358 WP 2001 2 13 UPS01834778 1 20010125 A 5711 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, LEFT WING CENTER L/E UPPER RIBS ARE CRACKED AT XFS 347.75, XFS 354, XFS 372.75, XFS 379. REPAIRED RIBS IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001021300359 20010213 00359 WP 2001 2 13 UPS01834779 1 20010122 A 5320 37552222 FITTING DOUG DC8 DC871F 302199D WP CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, STA 781.5 FLOORBEAM ATTACH FITTING IS CRACKED AT RBL 24. REMOVED AND REPLACED FITTING IAW DWG 375 5222 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001021300360 20010213 00360 WP 2001 2 13 UPS01834780 1 20010124 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, RIGHT WING L/E UPPER RIBS ARE CRACKED AT XFS 616.25, XFS 622.250. REPAIRED RIBS IAW SRM 57-2-0 FI G 2. 2 L 7 4 4F RT 4A25 2001021300361 20010213 00361 WP 2001 2 13 UPS01834781 1 20010123 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, RIGHT WING L/E UPPER RIBS ARE CRACKED AT FASTENER END AT XFS 297.5, XFS 354. REPAIRED RIBS IAW SR M 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001021300362 20010213 00362 WP 2001 2 13 UPS01834782 1 20010124 A 5730 576960040 DOUBLER DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, RIGHT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 572.5. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769600, AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001021300364 20010213 00364 WP 2001 2 13 UPS01834784 1 20010124 A 5730 576960036 DOUBLER DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, RIGHT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 597.5. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769600, AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001021300365 20010213 00365 WP 2001 2 13 UPS01834785 1 20010121 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, STA 1670 - 1705 SEAT TRACK IS CORRODED BEYOND LIMITS AT RBL 24. REPAIRED SEAT TRACK SECTION IAW S RM 53-2-3 FIG 14. 2 L 7 4 4F RT 4A25 2001021300366 20010213 00366 WP 2001 2 13 UPS01834804 1 20010129 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:IN, EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK ASSEMBLY. CHECKED GOOD. 2 L 7 4 4F RT 4A25 2001021300367 20010213 00367 EA 2001 2 13 COMA0160173 1 20010129 A 5530 600210617 BUSHING CNDAIR CL600 CL6002B19 EA VERTICAL STAB WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 937CA 7044 RIGHT VERTICAL STABILIZER STAB BUSHING WORN. REMOVED AND REPLACED BUSHING (P/N 600-21061-7), MACHINED BUSHING FLANGE TH ICKNESS TO .077 INCH AND REAMED INSIDE DIAMETER TO 1.5002 IAW CRJ AMM 20-26-00-910-803, DRAWING 600-21061 AND WVAC EO 60 1R-55-21-2175. 2 L 7 2 4F RT A21EA 2001021300368 20010213 00368 EA 2001 2 13 COMA0160174 1 20010127 A 5320 60034017373 ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 17939 7026 VERTICAL J-ANGLE INSIDE CBP1 W/L 73 IS CRACKED NEAR LBL 9. REMOVED CRACKED J-ANGLE (P/N 600-34017-373), FABRICATED NEW ANGLE FROM 7075-0 PO 24325-1 AND INSTALLED ANGLE IAW WVAC EO 601R-53-2160. 2 L 7 2 4F RT A21EA 2001021300369 20010213 00369 EU 2001 2 13 RAIA00101017 1 20010128 A 5220 S52277301200 SKIN AEROSP ATR72 ATR72202 8680940 EU EMERGENCY EXIT CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 217 MX-STL- DURING MAINTENANCE CHECK FOUND CORROSION ON RIGHT HAND EMERGENCY EXIT INTERNAL LOWER SKIN. MAINTENANCE REMOVED CORROSION, TREATED AND PRIMED THE AREA IAW ATR72 SRM. 2 H 7 2 4T RT A53EU 2001021300370 20010213 00370 EU 2001 2 13 RAIA00101018 1 20010128 A 5220 NAS6028 RETAINER AEROSP ATR72 ATR72202 8680940 EU DOOR SEAL CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 217 MX-STL-DURING MAINTENANCE CHECK FOUND CORROSION ON RIGHT HAND EMERGENCY EXIT LOWER SEAL RETAINING HARDWARE. MAINTENANCE REMOVED AND REPLACED THE HARDWARE IAW ATR72 MAINTENANCE MANUAL. 2 H 7 2 4T RT A53EU 2001021300371 20010213 00371 EU 2001 2 13 RAIA00101019 1 20010128 A 5220 S52277301200 SKIN AEROSP ATR72 ATR72202 8680940 EU EMER EXIT CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 217 MX-STL- DURING MAINTENANCE CHECK FOUND CORROSION ON LEFT HAND EMERGENCY EXIT LOWER INTERNAL SKIN. MAINTENANCE REMOVED C ORROSION, TREATED AND PRIMED THE AREA IAW ATR72 SRM. 2 H 7 2 4T RT A53EU 2001021300372 20010213 00372 EU 2001 2 13 RAIA00101020 1 20010128 A 5320 S53371502213 SILL AEROSP ATR72 ATR72202 8680940 EU CARGO DOORWAY CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 217 MX-STL- DURING MAINTENANCE CHECK FOUND FORWARD CARGO DOOR SILL PLATE HAS CORROSION. MAINTENANCE REMOVED CORROSION, PRIM ED AND TREATED THE AREA IAW ATR72 SRM. 2 H 7 2 4T RT A53EU 2001021300373 20010213 00373 EU 2001 2 13 RAIA00101021 1 20010128 A 5347 13S53375001209 SEAT TRACK AEROSP ATR72 ATR72202 8680940 EU FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 217 MX-STL- DURING MAINTENANCE CHECK FOUND CORROSION ON LEFT HAND INBOARD SEAT TRACK AT FUSELAGE FRAME 33. MAINTENANCE REPL ACED THE SEAT TRACK IAW ATR72 SRM. 2 H 7 2 4T RT A53EU 2001021300374 20010213 00374 EU 2001 2 13 RAIA00101022 1 20010128 A 5313 S53371311226 STRINGER AEROSP ATR72 ATR72202 8680940 EU FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 217 MX-STL- DURING MAINTENANCE CHECK FOUND CORROSION ON STRINGER 16R AT FUSELAGE FRAMES 29 AND 30. MAINTENANCE REMOVED CORR OSION FROM STRINGER, PRIMED AND TREATED THE AREA IAW ATR72 SRM. 2 H 7 2 4T RT A53EU 2001021300375 20010213 00375 EU 2001 2 13 RAIA00101023 1 20010128 A 5311 15S53570203200 FRAME AEROSP ATR72 ATR72202 8680940 EU FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 217 MX-STL- DURING MAINTENANCE CHECK FOUND CORROSION ON FUSELAGE FRAME 27 JUST I/B OF OUTER SEAT TRACK. MAINTENANCE REMOVED CORROSION, PRIMED AND TREATED AREA IAW ATR72 SRM. 2 H 7 2 4T RT A53EU 2001021300376 20010213 00376 EU 2001 2 13 RAIA00101024 1 20010128 A 5313 S53572500208 STRINGER AEROSP ATR72 ATR72202 8680940 EU FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 217 MX-STL- DURING MAINTENANCE CHECK FOUND CORROSION ON STRINGERS 21R AND 20R AT FUSELAGE FRAME 28D. MAINTENANCE REMOVED CO RROSION, TREATED AND PRIMED THE AREA IAW ATR72 SRM. 2 H 7 2 4T RT A53EU 2001021300377 20010213 00377 EU 2001 2 13 RAIA00101025 1 20010128 A 5313 S53372410226 STRINGER AEROSP ATR72 ATR72202 8680940 EU FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 217 MX-STL- DURING MAINTENANCE CHECK FOUND CORROSION ON STRINGER 17L AT FUSELAGE FRAME 23A. MAINTENANCE REMOVED CORROSION, TREATED AND PRIMED AREA IAW ATR72 SRM. 2 H 7 2 4T RT A53EU 2001021300378 20010213 00378 EU 2001 2 13 RAIA00101026 1 20010128 A 5230 S53070205209 CHANNEL AEROSP ATR72 ATR72202 8680940 EU CARGO DOOR CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 217 MX-STL- DURING MAINTENANCE CHECK FOUND CORROSION ON FLOOR LEVEL Z-CHANNEL AT FORWARD CARGO DOOR, RIGHT HAND SIDE. MAINT ENANCE REMOVED CORROSION, TREATED AND PRIMED THE AREA IAW ATR72 SRM. 2 H 7 2 4T RT A53EU 2001021300379 20010213 00379 EA 2001 2 13 COMA0160175 1 20010129 A 5320 ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 17939 7026 ANGLES ON INTERCOSTAL FS 484.00 CRACKED OUTBOARD OF LBL 27 AND RBL 27. REPLACED CRACKED ANGLE ON LBL 27 AND REPAIRED CR ACKED INTERCOSTAL ON LBL 36 AT FS 484 IAW WVAC EO NR 601R-53-2171. REPLACED CRACKED ANGLE ON RBL 27 IAW WVAC EO NR 601R -53-2171. 2 L 7 2 4F RT A21EA 2001021300380 20010213 00380 EA 2001 2 13 COMA0160176 1 20010129 A 5542 SKIN CNDAIR CL600 CL6002B19 EA RUDDER DENTED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 937CA 7044 RUDDER SKIN IS DENTED ON THE LEFT SIDE SKIN PANEL AT RS 99.43. PERFORMED A MAJOR REPAIR TO THE LEFT SIDE OF THE RUDDER RS 99.43 BY CUTTING OUT THE DAMAGE, FABRICATING A EXTERNAL DOUBLER MADE FROM 2024-T3 .040 PO 12676/1 AND INSTALLED IAW W VAC EO 601R-55-2174A. 2 L 7 2 4F RT A21EA 2001021300381 20010213 00381 EA 2001 2 13 COMA0160177 1 20010129 A 5310 STRUCTURE CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 17939 7026 RIGHT OUTBOARD POST AT RBL 9 AND FS 599 IS CRACKED. REPAIRED VERTICAL WEB O/B SIDE OF RBL 9 IAW WVAC EO 601R-53-2173. 2 L 7 2 4F RT A21EA 2001021300382 20010213 00382 EA 2001 2 13 COMA0160178 1 20010129 A 5320 6003106819 FLOOR SUPPORT CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 17939 7026 FLOOR SUPPORT FITTING OUTBOARD SIDE OF RBL 9 FS 460 AND STA 513 CRACKED. REMOVED FLOOR SUPPORT FITTING AT RBL 9 FS 460 AND INSTALLED NEW FITTING (P/N 600-31068-19) IAW WVAC EO 601R-53-2172. 2 L 7 2 4F RT A21EA 2001021300383 20010213 00383 EA 2001 2 13 COMA0160179 1 20010129 A 5510 600230681 BUSHING CNDAIR CL600 CL6002B19 EA HORIZONTAL STAB WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 937CA 7044 HORIZONTAL STABILIZER RIGHT OUTBOARD BUSHING IS WORN. REMOVED AND REPLACED BUSHING (P/N 600-23068-1) AND REAMED BUSHING TO 1.5004 IAW CRJ AMM 20-26-00-910-803 AND DRAWING 600-23068. 2 L 7 2 4F RT A21EA 2001021300384 20010213 00384 EU 2001 2 13 RAIA00101027 1 20010129 A 3060 HEATER MCAULY JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE MCAULY 5JFR36 B5JFR36C1103 GL LT PROPELLER FAILED A RAIA O OTHER J WARNING INDICATION CL CLIMB 1 CE 03 571HK 9915 277 950961 41090 76091 950961 7490-STL- DURING CLIMBOUT LEFT HAND PROP HEAT FAILED. MAINTENANCE REMOVED AND REPLACED THE PROPELLER IAW J41 MAINTENANC E MANUAL. 2 L 7 2 4T 4 T RT A41NM E18NE 6 C P15NE 2001021300385 20010213 00385 EU 2001 2 13 RAIA00101028 1 20010129 A 3060 BOOT MCAULY JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE MCAULY 5JFR C5JFR36C1104 GL RT PROP DEICE FAILED A RAIA O OTHER J WARNING INDICATION CL CLIMB 1 CE 03 565HK 9519 1030 960663 41082 76105 960663 7440-CMI- DURING CLIMBOUT RIGHT HAND PROP HEAT FAILED. MAINTENANCE REMOVED AND REPLACED NR 2 DEICE BOOT IAW J41 MAINTEN ANCE MANUAL. 2 L 7 2 4T 4 T RT A41NM E18NE 5 C P15NE 2001021300386 20010213 00386 EA 2001 2 13 COMA0160180 1 20010129 A 5320 WEB CNDAIR CL600 CL6002B19 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 17939 7026 WEB BETWEEN LB 9 AND RB 9 AT FS 280 IS CORRODED. FABRICATED FILLER AND DOUBLER FROM 7075-T6 X .040 INCH PO 33741/1. RE MOVED CORROSION AND TREATED. INSTALLED FILLERS AND DOUBLERS IAW WVAC EO 601R-53-2165. 2 L 7 2 4F RT A21EA 2001021300387 20010213 00387 EA 2001 2 13 COMA0160181 1 20010126 A 5320 601R3114863 SILL CNDAIR CL600 CL6002B19 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 7026 FWD END OF SILL AFT OF PAX DOOR ENTRANCE IS CORRODED. CUT OUT CORRODED SECTION OF SILL AND SPLICED IN A NEW SECTION OF SILL IAW WVAC EO 601R-53-2162B. 2 L 7 2 4F RT A21EA 2001021300388 20010213 00388 EA 2001 2 13 COMA0160182 1 20010124 A 5320 60034017595 ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 17939 7026 AFT J-ANGLE AT FS 280.00 BETWEEN LBL 18 AND RBL 22 IS CORRODED. TRIMMED OUT DAMAGE J-ANGLE, FABED NEW SECTION OF J-ANGL E, FABED TWO SPLICE SECTIONS AND INSTALLED IAW WVAC EO 601R-53-2163. 2 L 7 2 4F RT A21EA 2001021300389 20010213 00389 EA 2001 2 13 COMA0160183 1 20010124 A 5320 60034017351 ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 17939 7026 FORWARD J-ANGLE AT FS 280.00 BETWEEN LBL 9 AND RBL 9 IS CORRODED. REMOVED AND REPLACED FORWARD J-ANGLE AT FS 280.00 BET WEEN LBL 9 AND RBL 9 IAW WVAC EO 601R-53-2159. 2 L 7 2 4F RT A21EA 2001021300390 20010213 00390 EA 2001 2 13 COMA0160184 1 20010127 A 5320 60034017374 ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 17939 7026 VERTICAL J-ANGLE INSIDE CBP2 W/L 73 IS CRACKED NEAR RBL 9. REMOVED J-ANGLE (P/N 600-34017-374), FABRICATED NEW ANGLE FR OM 7075-0 PO 24325 AND INSTALLED ANGLE IAW WVAC EO 601R-53-2160. 2 L 7 2 4F RT A21EA 2001021300391 20010213 00391 NM 2001 2 13 TWAA0101801 1 20010129 A 3350 362624 LAMP BOEING 757 757231 1384950 NM CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 719TW 28487 AN EGRESS LIGHT WAS INOPERATIVE IN THE AFT CABIN. REPLACED THE FLEX LAMP. CHECK-C 1-5-01 LAX. 2 L 7 2 4F RT A2NM 2001021300392 20010213 00392 NM 2001 2 13 SCNA01011 1 20010128 A 2781 H1010261 POSITION SWITCH BOEING 727 727225 1384077 NM LE FLAPS FAILED A SCNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 OPMN 21578 THE NUMBER FOUR KRUEGER FLAP DID NOT RETRACT ON DEPARTURE, CREW FOLLOWED COM PROCEDURES AND RETURNED TO POINT OF ORIGIN. REMOVED AND REPLACED NUMBER FOUR KRUEGER FLAP POSITION SWITCH WITH A SERVICEABLE ONE. OPERATIONAL CHECKS GOOD. 2 L 7 3 4F A3WE 2001021300393 20010213 00393 NM 2001 2 13 QXEA0100078 1 20010129 A 5330 PANEL DHAV DHC8 DHC8202 2809007 NM FUSELAGE SEPARATED A QXEA O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 NM 09 363PH 520 YKM- PRELIMINARY REPORT. AFTER DEPARTURE FROM YKM NOISE HEARD AT ROTATION. NOTIFIED EN ROUTE BY YKM TOWER. PANEL(S) S EPARATED FROM AIRCRAFT. ON DESCENT IN SEA A SECOND NOISE HEARD. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT DOWN FOR R EPAIR. 2 H 7 2 4T RT A13NM 2001021300394 20010213 00394 WP 2001 2 13 MWEA010126 1 20010129 A 5713 5911259502 STRINGER DOUG DC9 DC932 3022066 WP RT WING DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 STRINGER 22 RIGHT DAMAGED IN RADIUS BEYOND LIMITS/BETWEEN XCW 20 RIGHT AND XCW 42 RIGHT. REMOVED AND REPLACED STRINGER REPAIR ANGLE. 2 L 7 2 4F A6WE 2001021300397 20010213 00397 2001 2 13 DHL2001807005 4 20010130 A 3422 258733511 GYRO DOUG DC8 DC873 302199C WP COCKPIT MALFUNCTIONED A DHLA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 807DH 45990 AFTER T/O, F/O GYRO FROZE IN NOSE UP TURN WITH GYRO FLAG. SWITCHING TO AUX CAUSED GYRO TO UNSTICK, BUT STILL CAUSED INT ERMITTENT GYRO FLAG. INTERMITTENT HDG COMPARATOR LT CAPT HSI 328, RMI 320 DEGREE SWITCHING TO NR 1 COMPASS. CAUSED CAP T RMI TO SWING TO 090 DEGREE WITH OFF FLAG. SWITCHING TO NR 2 COMPASS CAUSED CAPT HSI TO READ 330 DEGREE AND RMI TO REA D 320 DEGREE. F/O INSTURMENTS FOLLOWED CAPTS RMI NORMALLY. REPLACED F/O''S VERTICAL GYRO. OPS CHECKS GOOD IAW DC-8 MM 34-25-01. REMOVED AND REPLACED F/O''S FLUX VALVE. PERFORMED COMPASS SWING. OPS CHECKS GOOD IAW DACO M/M 34-21-2. CO MPONENTS REPLACED:VERTICAL GYRO P/N 2587335-11, S/N 5028118 AND FLUX VALVE P/N 620359, S/N 91058155. 2 L 7 4 4F RT 4A25 2001041000021 20010410 00021 NM 2001 4 10 01FDEA00051 1 20010130 A 5311 6516344 FRAME BOEING 727 727227 1384078 NM FUSELAGE PUNCTURED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 FRAME PUNCTURED AT BS 1070, RBL 20, UNDER FLOOR TO SIDEWALL SUPPORT. *S/D* DRILLED UP PUNCTURES IN FRAME TO .1875 INCH DIA AND PLUGGED WITH RIVETS PER FEDEX SRM 53-10-1 DETAIL 4. 2 L 7 3 4F A3WE 2001021300398 20010213 00398 NE 2001 2 13 QXEA01000079 2 20010128 A 7200 310450001 ENGINE DHAV DHC8 DHC8201 2809001 NM PWA 120 PW120A NE NR 1 MALFUNCTIONED A QXEA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 828PH 26090 1369 287 PCE120730 PDX- ENGINE OIL PRESSURE LIGHT CAME ON. ACCOMPLISHED ENGINE SHUT-DOWN CHECK LIST. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ENGINE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2001030500264 20010305 00264 NM 2001 3 5 2001UALA00040 1 20010120 A 5610 141N00121 WINDOW BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 LEFT LEAKING A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 583UA 26705 LOUD SQUEAL FROM WINDOW 2 LEFT. *S/D* PRESSURE SEAL WAS REPLACED PER MM 56-11-53 AND WINDOW ADJUSTED PER MM 56-11-0 2 WHEREIN, VERTICAL UP AND FORWARD CLEARANCES WERE FOUND WITHIN LIMITS. SUBSEQUENT PRESSURIZATION TO A DIFFERENTIAL PRE SSURE OF 8.0 PSI, REVEALED NO DEFECTS. 2 L 7 2 4F 4 F RT A2NM E17NE 2001030500265 20010305 00265 NM 2001 3 5 2001UALA00042 1 20010121 A 3350 5822 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 653UA 25391 EMERGENCY LIGHTING INOP FIRST CLASS, LEFT RIGHT AND CROSS AISLE. *S/D* BATTERY PACK REPLACED FOR LT EEL LIGHTS. REPLA CED POWER SUPPLY STRIP FOR RT F/C EEL AND ACCOMPLISHED PERMANENT REPAIR OF EEL STRIP. 2 L 7 2 4F 4 F RT A1NM E24NE 2001030600081 20010306 00081 NM 2001 3 6 2001UALA00043 1 20010119 A 4900 38621442 PIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE GEARBOX FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 768UA 10570 0 26919 P1008 DURING CLIMBOUT BUT MORE NOTICEABLE ON DESCENT A SMELL LIKE METAL ON METAL WAS SMELLED THROUGHOUT THE AIRPLANE. *S/D* APU REPLACED 21 JAN DUE TO METAL FOUND ON CHIP DETECTORS. APU ALSO TOOK 2 QTS OIL. METAL CONFINED TO GEARBOX. APU DI SASSEMBLED TO REPLACE GEARBOX. GEARBOX DISASSEMBLED. SOURCE OF METAL PROVED TO HIGH SPEED PINION GEAR BEARING SPINNING IN IT''S BEARING LINER. THE SPINNING WAS CAUSED BY FAILURE OF THE LINER ANTI-ROATION DEVICE IN THE LINER. THE SPINNIN G BEARING WORE THE ANTI-ROTATION DEVICE WHICH GENERATED THE METAL FOUND ON THE CHIP DETECTOR. ADDITIONAL SHOP FINDINGS: C-1 IMPELLER ALSO WITH ONE BENT BLADE DUE TO SOFT FOD. IMPELLER TO BE REPLACED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001030600082 20010306 00082 NM 2001 3 6 2001UALA00044 1 20010119 A 3350 BPS7 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE OVERWING EXIT DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 661UA 27158 RIGHT OVERWING EXIT LOWER EEL EXIT SIGN COMES ON AND OFF BY ITSELF. *S/D* REPLACED BATTERY PACK, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2001021300406 20010213 00406 NM 2001 2 13 2001UALA00045 1 20010121 A 3260 WARNING LIGHT BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE MLG ILLUMINATED A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 612UA 21873 GEAR DISAGREE AND GEAR DOORS CAUTION MESSAGE AND LIGHTS ILLUMINATED AFTER GEAR UP AND HANDLE MOVED TO OFF. 2 L 7 2 4F 4 F RT A1NM E3NE 2001021300407 20010213 00407 2001 2 13 2001UALA00046 4 20010122 A 3432 6223257008 RECEIVER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE GLIDE SLOPE INOPERATIVE A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 334UA 24229 NR 1 NAVIGATION RECEIVER IS INOPERATIVE. *S/D* REPLACED NR 1 NAVIGATION RECEIVER. OPS CHECKED OK. 2 L 7 2 4F 4 F RT A16WE E2GL 2001031200638 20010312 00638 NM 2001 3 12 2001UALA00047 1 20010123 A 2780 65C267661 BELLCRANK BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT LE FLAP BROKEN A UALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 WP 29 308UA 23669 LEFT SIDE INBOARD LEADING EDGE FLAP STUCK IN DOWN POSITION AFTER TAKEOFF. *S/D* FOUND BROKEN BELLCRANK. REPLACED THE BELLCRANK. 2 L 7 2 4F 4 F RT A16WE E2GL 2001031200639 20010312 00639 NM 2001 3 12 2001UALA00048 1 20010122 A 2120 DUCT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RIGHT A/C PACK FAILED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 549UA 25397 AT 12,00FT IN CRUISE RIGHT PACK STOPPED OPERATING. *S/D* REMOVED AND INSTALLED RT EXTRACTOR DUCT AND LEAK CHECKED. FA ILED WELD JOINT ON DEFECTIVE DUCT. 2 L 7 2 4F 4 F RT A2NM E17NE 2001032600210 20010326 00210 NM 2001 3 26 2001UALA00051 1 20010124 A 2120 UNKNOWN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE COCKPIT ODOR A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 206UA 30212 FLT RETURNED TO DEN DUE TO HEAVY SMOKE ODOR IN THE COCKPIT & FIRST CLASS. NO SMOKE WAS SEEN. AT FL250, THERE WAS A SHI FT OFF THE ENGINE, AT FL270 THERE WAS AN ACRID SMELL AND AT FL310-320 THE SMELL WAS VERY HEAVY IN 2A/2B. CAPT DECLARED AN EMERGENCY. F/O WORE THE 02 MASK FOR SAFETY. *S/D* BOTH PACKS WERE RUN AT HIGH POWER, BUT THE SMOKE ODOR COULD NOT BE DUPLICATED. AS A PRECAUTION, LT AND RT OZONE CONVERTERS WERE REPLACED. AIRCRAFT WAS RETURNED TO REVENUE SERVICE WIT H NO FURTHER REPORTS OF SMOKE OR SMELL. THE 2 OZONE CONVERTERS WERE SENT TO VENDOR FOR EFFICIENCY TEST. EACH OF THEM P ASSED WITH AN AVERAGE EFFICIENCY HIGHER THAN 90 PERCENT (COMPLIED WITH FAR 121.578). 2 L 7 2 4F 4 F RT T0001SE E46NE 2001021300408 20010213 00408 NM 2001 2 13 2001UALA00053 1 20010124 A 2530 OVEN BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE GALLEY CONTAMINATED A UALA H F DEACTIVATE SYST/CIRCUITS ACTIVATE FIRE EXT. A B FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 603UA 21864 SMALL FLAME AND SMOKE IN FORWARD CABIN OVEN FROM PAPER WRAPPER. CIRCUIT BREAKER PULLED AND FIRE EXTINGUISHER USED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001021300409 20010213 00409 EU 2001 2 13 2001UALA00055 1 20010122 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SEAT 9 INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 412UA 465 EMERGENCY ESCAPE PATH LIGHT AT SEAT 9C IS INOPERABLE. REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2001031200641 20010312 00641 NM 2001 3 12 2001UALA00056 1 20010125 A 3233 273N10051 ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NLG FAILED A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 567UA 26673 NOSE GEAR FAILED TO EXTEND ON APPROACH. GEAR EXTENDED WITH ALTERNATE SYSTEM. *S/D* REPLACED NOSE GEAR UPLOCK ACTUATOR . 2 L 7 2 4F 4 F RT A2NM E17NE 2001021300410 20010213 00410 WP 2001 2 13 ABXA0100025 1 20010130 A 3350 60030451 POWER SUPPLY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 978AX 82902 525 47628 EMERGENCY LIGHTS WOULD NOT ILLUMINATE ON PREFLIGHT INSPECTION. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT P OWER SUPPLY IAW DC-9 MM 33-53-02. 2 L 7 2 4F A6WE 2001021300411 20010213 00411 CE 2001 2 13 GLBA2001016 1 20010130 A 3030 1013840841011 ANNUNCIATOR BEECH 1900 1900D 1154162 CE COCKPIT DETACHED A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 226GL UE226 RETURN TO BLOCK - PITOT HEAT ANNUNCIATOR POPPED OUT. REMOVED AND REPLACED ANNUNCIATOR, OPS CHECKED SYSTEM GOOD. 2 L 7 2 4T RT A24CE 2001021300412 20010213 00412 EU 2001 2 13 01FDEA00057 1 20010131 A 2421 IDG AIRBUS 310 A310222 3930315 EU NR 2 INOPERATIVE A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 449FE 217 DURING CLIMBOUT, NR 2 IDG TEMP CONT TO CLIMB. VERIFIED NR 2 IDG DEFERRED CORRECTLY. VERIFIED PROPER SERVICE ACCOMPLISH . NO FAULTS NOTED. IDG TEMP WITHIN LIMITS REF MM 24-11-00-001. AC OK FOR SERVICE. NR 2 IDG REMAINS DEFERRED. 2 L 7 2 4F RT A35EU 2001021300413 20010213 00413 EU 2001 2 13 01FDEA00058 1 20010131 A 2133 OUTFLOW VALVE AIRBUS 310 A310222 3930315 EU CABIN PRESSURE FAILED A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 419FE 345 ON CLIMBOUT OF BOM AC WOULD NOT PRESSURIZE. COCKPIT IND SHOW NR 1 FWD OUTFLOW VLV OPEN. AC RELEASED PER MEL 21-47 OUTF LOW VLV FWD NR 1 DE-ACTIVATED IN THE CLOSE POS PER MXP 21-47B. 2 L 7 2 4F RT A35EU 2001021300414 20010213 00414 EU 2001 2 13 QXEA0100081 1 20010128 A 2120 UNKNOWN FOKKER F28 F28MK4000 4990810 EU CABIN & COCKPIT ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 498US 11181 PDX- CABIN AND COCKPIT BOTH HAVE STRONG ODOR OF FUEL. ACCOMPLISHED BLEED AIR SYSTEM BLOWOUT OF BOTH AIR CONDITIONING PA CK SYSTEMS DURING ENGINE RUN-UP. NO FURTHER FUEL ODOR NOTICED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001021300415 20010213 00415 WP 2001 2 13 01FDEA00062 1 20010128 A 2750 ANB7253501 ATTACH FITTING DOUG DC10 DC1010 3022110 WP TE FLAP HYD SYS BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 LEFT INBOARD FLAP INBOARD HYD CYLINDER LWR ATTACH FITTING BROKEN AND HYD LINES BENT. CHANGE FITTING, CYLINDER LINES 2 E ACH AND CHECK FLAP RIGGING. 2 L 7 3 4F A22WE 2001021300416 20010213 00416 EU 2001 2 13 QXEA01000080 1 20010128 A 4990 OIL TANK FOKKER F28 F28MK4000 4990810 EU APU ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 498US 11181 BOI- STRONG FUEL SMELL IN FORWARD CABIN AND GALLEY AREA. REMOVED AND REPLACED APU OIL TANK. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001021300417 20010213 00417 EA 2001 2 13 COMA0160185 1 20010129 A 3010 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA WING OVERHEAT FALSE ACTIVATION A COMA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SO 01 776CA 7293 WING OVERHEAT WARNING. COULD NOT DUPLICATE. FUNCTION CHECK OF SYSTEM WAS NORMAL. 2 L 7 2 4F RT A21EA 2001021300418 20010213 00418 EA 2001 2 13 COMA0160186 1 20010128 A 3020 12681 SWITCH CNDAIR CL600 CL6002B19 EA RT ENG ANTI ICE MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 956CA 3077 7105 RT ENGINE COWL ANTI-ICE CAUTION MESSAGE. REPLACED THE COWL ANTI-ICE PRESSURE SWITCH. 2 L 7 2 4F RT A21EA 2001021300419 20010213 00419 EA 2001 2 13 COMA0160187 1 20010127 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA CABIN BURNED OUT A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 967CA 7134 ONE CABIN OVERHEAD EMERGENCY LIGHT IS INOPERABLE. REPLACED LIGHT BULB. 2 L 7 2 4F RT A21EA 2001021300420 20010213 00420 SO 2001 2 13 SWIA972303 1 20010129 A 2750 FCU EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 07 293SW 120320 AFTER TAKEOFF OUTBOARD FLAPS WOULD NOT RETRACT ABOVE 5 DEGREES INDICATED AND CONTROL FAULT WARNING OCCURRED. CONTROL FA ULT WOULD NOT RESET. CONTINUED AT 180 KNOTS. FLAPS EXTENDED NORMALLY FOR LANDING. AFTER LANDING OUTBOARD FLAPS WOULD NOT RETRACT ABOVE 15 DEGREES. INSPECTED OUTBOARD FLAP ROLLERS. REPLACED FCU. P/N 347200-101. CLEARED ALL FAULTS. RA N FLAPS. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001021300421 20010213 00421 SO 2001 2 13 SWIA972304 1 20010121 A 2730 SPRING EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE ELEVATOR LACK OF LUBE A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 207SW 120266 ELEVATOR MOVEMENT PRODUCES ABNORMAL SOUNDS, SOUNDS LIKE CABLES PRANGING. LUBED ELEVATOR RETURN SPRING FWD ATTACH POINT. SYSTEM CHECK OK. 2 L 7 2 4T 4 T RT A31SO E20NE 2001021300422 20010213 00422 SO 2001 2 13 SWIA972305 1 20010121 A 2752 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS CONTAMINATED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 194SW 120120 OUTBOARD FLAPS WOULD NOT RAISE OR LOWER FROM FLAPS 15 DEGREES AFTER DEICE. FOUND DEICE FLUID ON OUTBOARD FLAP CANNON PL UGS (LEFT AND RIGHT). CLEANED CANNON PLUGS WITH CONTACT CLEANER. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001021300423 20010213 00423 SO 2001 2 13 SWIA972306 1 20010124 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE TE FLAPS FAILED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 293SW 120320 FLAP CONTROL FAULT ON FLAP RETRACT, WOULD NOT RESET. OUTBOARD FLAP PAIR STUCK AT 15 DEGREES. RETURNED TO SFO. (3RD REP EAT). READ FAULT CODES AND TROUBLESHOOTING CODES SOL SHORT TO GROUND IAW INSTRUCTION PROVIDED. CLEANED OUT LEFT OUTBOAR D FLAP ACTUATOR EXTENSION AND RETRACTION SOLENOID. OHM IS WITHIN LIMITS PER MM 27-50-00. ALSO PERFORMED FLAP ACTUATOR VELOCITY TEST AND DRIFT TESTS, BOTH TEST NORMAL. REPLACED LEFT OUTBOARD FLAP ACTUATOR DUE TO FAULT CODES. PER MM 27-5 0-00 RII CARD 27-307 TASK CARD. CYCLED FLAPS AND CLEARED ALL FLAP FAULTS. OPS CHECK OF FLAPS GOOD ON GROUND. 2 L 7 2 4T 4 T RT A31SO E20NE 2001021300425 20010213 00425 SO 2001 2 13 SWIA972308 1 20010127 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS FAILED A SWIA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 289YV 120289 WHEN CYCLING FLAPS FROM 45 DEGREES TO 0 DEGREES, FLAPS GET A DISAGREEMENT ON THE NACELLE FLAPS AT ABOUT 25 DEG - 15 DEG . REPLACED LEFT NACELLE FLAP ACTUATOR WITH SERVICEABLE UNIT. CYCLED FLAPS SEVERAL TIMES. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001021300426 20010213 00426 2001 2 13 COMA0160188 4 20010127 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 976CA 7151 STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001021300427 20010213 00427 EA 2001 2 13 COMA0160189 1 20010127 A 5240 DOOR CNDAIR CL600 CL6002B19 EA SERVICE OPEN A COMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 01 960CA 7117 EXIT/SERVICE DOOR POPPED OPEN INFLIGHT. INSPECTED FOR DAMAGE, AND CLOSED DOOR. 2 L 7 2 4F RT A21EA 2001021300428 20010213 00428 NM 2001 2 13 DHL2001727003 1 20010127 A 5210 DOOR BOEING 727 727228 NM MAIN PAX NOT CLOSED A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 727DH 20204 AFTER TAKEOFF AIRCRAFT WOULD NOT PRESSURIZE, AUTOFAIL LIGHT ILLUMINATED AND FAILURE TO PRESSURIZE. AFTER TAKEOFF ABNORM AL PROCEDURES WERE COMPLETED. THIS DID NOT RESTORE NORMAL CABIN PRESSURIZATION. A LOUD NOISE WAS COMING FROM THE FORWA RD ENTRY DOOR AIRCRAFT AT 1200 FEET HAD 1.2 DIF. WITH CABIN AT 9000 FEET DURING INSPECTION A GAP WAS AT REAR OF DOOR BUT THE S/O DOOR ANNUNICIATOR DID NOT ILLUMINATE AT ANY TIME. FOUND FWD ENTRY DOOR NOT SHUT PROPERLY. CLOSED ENTRY DOOR, PRESSURIZED AIRCRAF. OPS GOOD IAW 52-11-01 AND 21-31-0. 2 L 7 3 4F A3WE 2001021300429 20010213 00429 2001 2 13 COMA0160190 4 20010127 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 969CA 7141 STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001021300430 20010213 00430 NM 2001 2 13 DHL2001702002 1 20010130 A 3150 WARNING SYSTEM BOEING 727 72730C 1384009 NM COCKPIT FALSE ACTIVATION A DHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 702DH 19793 DISCONTINUED TAKEOFF DUE TO TAKEOFF WARNING HORN. FLAPS, SPEEDBRAKE AND TRIM ALL PROPERLY SET. PERFORMED T/O WARN TEST PER MM 31-26-0 PARA 6, TEST OK. 2 L 7 3 4F A3WE 2001021300431 20010213 00431 NM 2001 2 13 CALA0100081 1 20010129 A 5320 FLOOR SUPPORT BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17620 27333 INSPECTION FOUND A .5 INCH CRACK IN FLOOR SUPPORT WEB AT STA 344 - 360, BL 0. THE WEB WAS REMOVED AND A NEW WEB WAS INS TALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001021300432 20010213 00432 NM 2001 2 13 CALA0100082 1 20010130 A 5315 FLOORBEAM BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17620 27333 INSPECTION FOUND CABIN FLOORBEAM CORRODED AROUND NUT PLATE HOLES AT STA 986.5, LBL 18 - 31. A DOUBLER WAS INSTALLED IAW SRM 53-60-51, FIGURE 203. 2 L 7 2 4F RT A16WE 2001021300433 20010213 00433 WP 2001 2 13 CALA0100083 1 20010131 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND INNER SKIN DOUBLER CORRODED AT FS 1286 BETWEEN LONGERONS 21L AND 22L. THE INNER DOUBLER WAS REMOVED AN D REPLACED IAW SRM 51-30-2, 51-30-5, AND ECRA 5332-01009. 2 L 7 2 4F A6WE 2001021300434 20010213 00434 WP 2001 2 13 CALA0100084 1 20010130 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND A 4 INCH CRACK IN AFT ACCESSORY COMPARTMENT FRAME UNDER RADIUS BLOCK AT LONGERON ATTACH POINT, FS 1446, LONGERON 5L. THE FRAME WAS REMOVED AND A NEW FRAME WAS INSTALLED IAW SRM 51-10-4, 53-03, FIGURE 30, AND 51-30-5. 2 L 7 2 4F A6WE 2001021300435 20010213 00435 WP 2001 2 13 CALA0100085 1 20010131 A 3350 RPS1B CHARGER DOUG DC10 DC1030 3023501 WP CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 13066 46591 INSPECTION FOUND EMERGENCY SEAT LIGHTS INOPERATIVE AT ROWS 29 - 45 A, B. THE BATTERY CHARGER WAS REMOVED AND REPLACED A ND OPERATION CHECKED GOOD IAW MM 33-55-00. 2 L 7 3 4F A22WE 2001021300436 20010213 00436 WP 2001 2 13 TWAA0101901 1 20010126 A 3397 WIRE DOUG DC9 DC983 3022083 WP EGRESS LIGHT BROKEN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9618A 53565 THE EGRESS LIGHTING WAS INOPERATIVE FROM THE FORWARD GALLEY TO ROW 3. SPLICED BROKEN WIRES AT SEAT ROW 3. CHECK-C 12-1 2-00 STL. 2 L 7 2 4F RT A6WE 2001021300437 20010213 00437 WP 2001 2 13 TWAA0101902 1 20010130 A 3260 MS250081 SWITCH DOUG DC9 DC931 3022065 WP GEAR HANDLE SHORTED A TWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CE 05 989Z 47135 WHEN CREW WAS ACCOMPLISHING THE LANDING GEAR HANDLE CHECK, SMOKE APPEARED FROM THE LANDING GEAR HANDLE SWITCH. FOUND SW ITCH SHORTED. REPLACED THE SWITCH. CHECK-C 4-16-00 MCI. 2 L 7 2 4F A6WE 2001021300438 20010213 00438 WP 2001 2 13 TWAA0101903 1 20010124 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT, FOUND CRACKED FLOOR SUPPORT AT STA 948, LBL 6. FABRICATED NEW SUPPORT PER DRAWING 5930560-61. IN STALLED PER SPM 6-70-01 AND SRM 51-01. TYPE FASTENERS PER SRM 51-30-2. PRIMED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001021300439 20010213 00439 WP 2001 2 13 TWAA0101904 1 20010124 A 5730 DOUBLER DOUG DC9 DC982 3022082 WP LT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT, FOUND DOUBLER AND TIE ANGLE CRACK AT PREVIOUS REPAIR BETWEEN NUMBER 5 AND 6 LE TRACK AT LT WING LE ADING EDGE SKIN, AT PRODUCTION BREAK. FABRICATED DOUBLER PER SRM 57-32-1 ITEM 4. FABRICATED NEW ANGLE PER DRAWING 9937 517. REF SRM 51-30-2 FOR RIVET INSTALLATION. SRM 51-30-5 FOR HI-LOK INSTALLATION. 2 L 7 2 4F A6WE 2001021300440 20010213 00440 WP 2001 2 13 TWAA0101905 1 20010124 A 5280 DOOR DOUG DC9 DC982 3022082 WP LT MLG CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT, THE LT WHEEL WELL GEAR DOOR HAD APPROX .75 INCH CRACK IN INNER PAN RADIUS, IN AFT, OUTBOARD CORNER . CONFIRMED BY EDDY CURRENT. REPLACED CORNER ON GEAR DOOR USING FASTENERS PER SRM 51-30-5 AND SRM 51-30-2. 2 L 7 2 4F A6WE 2001021300456 20010213 00456 WP 2001 2 13 AALA20010058 1 20010103 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3507A 49801 TUL - FOUND CORROSION ON CUSP SHEET UNDER AFT GALLEY AREA AT STATION 1307 LEFT. INSTALLED NEW CUSP SHEET UNDER AFT GALL EY STATION 1307 TO STATION 1183 LEFT IAW SRM 53-01 FIG 4 SHEET 3. (M) 2 L 7 2 4F A6WE 2001021300457 20010213 00457 WP 2001 2 13 AALA20010059 1 20010103 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3507A 49801 TUL - FOUND NR 3 TRACK LUGS GOUGED. GOUGE BLENDED OUT, AND SEAT TRACK REPAIR PLUG INSTALLED PER SRM 53-05 FIG 4 SHT 2. (M) 2 L 7 2 4F A6WE 2001021300458 20010213 00458 WP 2001 2 13 AALA20010060 1 20010104 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3507A 49801 TUL - FOUND CABIN FLOOR FS 1302-1306 NR 3 SEAT TRACK CORRODED. REMOVED CORRODED SECTION OF SEAT TRACK AND SPLICED IN NE W SECTION PER 53-05 AND 51-01 SRM. (M) 2 L 7 2 4F A6WE 2001021300459 20010213 00459 WP 2001 2 13 AALA20010061 1 20010105 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE SCRATCHED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3507A 49801 TUL - FOUND 3 SCRATCHES AT STATION 320 AT L22L. INSTALLED DOUBLER PER ESO 80559 DATED 1/4/01. (M) 2 L 7 2 4F A6WE 2001021300461 20010213 00461 WP 2001 2 13 AALA20010063 1 20010115 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3507A 49801 TUL - FOUND CORROSION BEYOND LIMITS ON SEAT TRACK NR 1 AT STATION 671. INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10. (M) 2 L 7 2 4F A6WE 2001021300463 20010213 00463 WP 2001 2 13 AALA20010065 1 20010106 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3507A 49801 TUL - FOUND CRACK IN LEFT CANTED FRAME WEB STATION 1485 TOP HOLE. INSTALLED DOUBLER PER AARD 53-10-00-32. (M) 2 L 7 2 4F A6WE 2001021300464 20010213 00464 WP 2001 2 13 AALA20010066 1 20010110 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3507A 49801 TUL - FOUND TWO DENTS IN FUSELAGE AT FS 218 BETWEEN STRINGERS 18 AND 19 LEFT. INSTALLED DOUBLER REPAIR PER ESO 80559 DA TED 1/4/2001. (M) 2 L 7 2 4F A6WE 2001021300465 20010213 00465 WP 2001 2 13 AALA20010084 1 20010110 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3507A 49801 TUL - FOUND FLOOREAM GOUGED AT LBL 0 STATION 389. BLENDED GOUGE PER SRM AND INSTALLED DOUBLER PER ESO 80559 DATED 9/29/ 97. (M) 2 L 7 2 4F A6WE 2001021300482 20010213 00482 GL 2001 2 13 AALA20010088 2 20010116 A 7321 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU GE CF6 CF680C GL NR 1 ENGINE DIRTY A AALA K NONE J WARNING INDICATION CR CRUISE 1 SW 21 33069 512 LHR - NR 1 ENGINE FUEL FLOW FLUCTUATES WITH CORRESPONDING FLUCTUATION IN N1 EGT AND N2. ACCOMP TS PER TSM 72-00-20-1 CL EANED CONN ON MEC. ALL CHECKS OK DURING ENGINE GROUND RUN. CLEANED MEC CONNECTOR, GROUND RUN UP OK. (M) 2 L 7 2 4F 4 F RT A35EU E23EA 2001021300487 20010213 00487 WP 2001 2 13 GTIA000351 1 20010104 A 3350 LIGHT DOUG DC9 DC932 3022066 WP CABIN LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 133NK 48111 ACY - FLT 284 - EMERGENCY FLOOR TRACK LIGHTING STRIP NOT SECURED TO FLOOR BETWEEN ROWS 14-16. AS PER SPIRIT GMM 5.39 PL ACED ON CARRY-OVER ITEM NR 1024204. (M) 2 L 7 2 4F A6WE 2001021300498 20010213 00498 NM 2001 2 13 ASAA0110003 1 20010103 A 3350 883200312 RECEIVER BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROW 18 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY RECEIVER AND BATTERY. LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2001021300499 20010213 00499 NM 2001 2 13 20010212SG002 1 20010103 A 3350 86210144 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROW 18 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY RECEIVER AND BATTERY. LIGHTS OPERATED NORMALLY. REF ASAA0110003. (M) 2 L 7 2 4F A16WE 2001021300502 20010213 00502 NM 2001 2 13 ASAA0110001 1 20010101 A 3350 883200312 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING MAINTENANCE CHECK, EMERGENCY LIGHT TRANSMITTER INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT TRANSMITT ER BATTERY. LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2001021300503 20010213 00503 NM 2001 2 13 ASAA0110009 1 20010105 A 3350 6013211 BATTERY PACK BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 ANC - DURING MAINTENANCE CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE AT L2 AND R2 DOORS. REMOVED AND REPLAC ED BATTERY PACK. LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2001021300504 20010213 00504 NM 2001 2 13 ASAA0110002 1 20010102 A 3350 86210144 BATTERY BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS ON SMOKE BATTERY WOULD NOT TEST. REMOVED AND REPLACED REMOT E ASSEMBLY BATTERY. LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2001021300505 20010213 00505 WP 2001 2 13 ASAA0180008 1 20010109 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 933AS 49234 LAX - DURING PRE-FLIGHT, EMERGENCY LIGHTS IN BOTH THE PASSENGER CABIN AND COCKPIT WERE DETERMINE TO BE INOPERATIVE. REP LACED ASSOCIATED BATTERY PACKS. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001021300506 20010213 00506 WP 2001 2 13 ASAA0180006 1 20010106 A 3350 1315 LIGHT DOUG DC9 DC983 3022083 WP TAILCONE INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 948AS 53021 PHX - DURING LINE CHECK, TAILCONE EMERGENCY LIGHT WAS DETERMINED TO BE INOPERATIVE. BURNISHED CONNECTION TO RESTORE ELE CTRICAL GROUND. LIGHT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001021300507 20010213 00507 WP 2001 2 13 ASAA01800010 1 20010112 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 OAK - DURING LINE CHECK, OVERWING EMERGENCY EXIT IDENTIFIER LIGHTS WERE DETERMINED TO BE INOPERATIVE. REPLACED LIGHT BU LBS AND ASSOCIATED BATTERY PACKS. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001021300508 20010213 00508 WP 2001 2 13 ASAA0180007 1 20010109 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 967AS 49103 SEA - DURNG A1 LINE CHECK, OVERHEAD EMERGENCY LIGHTS AT ROW 19-23 WERE DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATE D BATTERY PACKS. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001021300509 20010213 00509 WP 2001 2 13 ASAA0180011 1 20010112 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 934AS 49235 SEA - DURNG LINE CHECK, OVERHEAD EMERGENCY LIGHTS AT ROWS 13-17 WERE DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BATTERY PACKS. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 2001021300510 20010213 00510 WP 2001 2 13 ASAA0180009 1 20010111 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 974AS 53450 SEA - DURING PRE-FLIGHT, OVERHEAD EMERGENCY LIGHTS AT ROWS 28-30 FLASHED ON WHEN AUX HYD PUMP WAS TURNED ON. REPLACED A SSOCIATED BATTERY PACKS. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001021300511 20010213 00511 WP 2001 2 13 ASAA0180005 1 20010105 A 3350 0105606 LIGHT DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 958AS 53024 SEA - DURING PREFLIGHT CHECK, 1ST CLASS CABIN EMERGENCY FLOOR TRACK LIGHTS AT ROW 3 WERE DETERMINED TO BE INOPERATIVE. TIGHTENED LOOSE ELECTRICAL CONNECTIONS. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001021300512 20010213 00512 WP 2001 2 13 ASAA0180004 1 20010106 A 3350 0105606 LIGHT DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 SEA - DURING PREFLIGHT CHECK, 1ST CLASS CABIN EMERGENCY FLOOR TRACK LIGHTS AT ROW 3 WERE DETERMINED TO BE INOPERATIVE. REATTACHED TRACK ELECTRICAL CONNECTIONS. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001021300513 20010213 00513 WP 2001 2 13 ASAA0180003 1 20010104 A 3350 01056061 LIGHT DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 LAX - DURING PREFLIGHT CHECK, SOME OF THE 1ST CLASS CABIN EMERGENCY FLOOR TRACK LIGHTS WERE DETERMINED TO BE INOPERATIVE . REATTACHED TRACK ELECTRICAL CONNECTIONS. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001021300521 20010213 00521 NM 2001 2 13 TSAA0136007 1 20010121 A 3610 39271611 VALVE BOEING 737 73725A 1384481 NM NR 2 ENGINE DEFECTIVE A TSAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 21 819AL 23791 FLT 210 - HNL-OGG - DURING TAKEOFF, NR 2 ENGINE BLEED LIGHT CAME ON. ABORTED TAKEOFF AND RETURNED TO GATE. REMOVED AND REPLACED THE NR 2 ENGINE PNEUMATIC SHUTOFF VALVE IAW MM 21-11-011-6. OPS AND LEAK CHECK OK. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F RT A16WE 2001021300522 20010213 00522 NM 2001 2 13 TSAA0157009 1 20010124 A 5711 69578331 SPAR BOEING 737 7372T4 1384492 NM RT WING CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 807AL 23443 IDENTIFIED CORROSION AT RT WING FRONT SPAR LOWER CHORD FSS 475. REPAIRED CONSISTS OF REMOVING DAMAGED AREA AT HORIZONTA L FLANGE AND INSTALLING A TAPERED FILLER, HFEC COMPLETED ON ALL FASTENER HOLES AND REWORKED AREA. NO DEFECTS NOTED. CL EAN AND TREATED ALL EXPOSED AREAS AND INSTALLED DOUBLER NESTED ANGLES TO COMPLETE REPAIR. (M) 2 L 7 2 4F A16WE 2001021300523 20010213 00523 WP 2001 2 13 USAAD01013 1 20010120 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP SERVICE DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 959VJ 47352 IND - THE GALLEY SERVICE DOOR EVACUATION SLIDE ACTIVATED EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMER GENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 2001021300524 20010213 00524 WP 2001 2 13 USAAD01012 1 20010119 A 3350 1001191 LIGHT DOUG DC9 DC931 3022065 WP L1 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 958VJ 47351 IND - THE PORTABLE EMERGENCY LIGHT AT THE MAIN ENTRANCE DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT. (M) 2 L 7 2 4F A6WE 2001021300531 20010213 00531 NM 2001 2 13 ASAA0140001 1 20010104 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 774AS 25107 SEA - DURING LINE CHECK INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE AT ROWS 17-20, BROKEN WIRE. REPAIR ED WIRE, OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2001021300540 20010213 00540 WP 2001 2 13 AALA20010044 1 20010102 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3507A 49801 TUL - FOUND STATION 1210-1213, NR 2 TRACK CORRODED. INSTALLED SEAT TRACK SPLICE REPAIR AND NEW SECTION OF TRACK FROM ST ATION 1183-1309 PER SRM 53-05. (M) 2 L 7 2 4F A6WE 2001021300541 20010213 00541 WP 2001 2 13 ASAA20010045 1 20010102 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3507A 49801 TUL - FOUND STATION 1251, NR 2 TRACK CORRODED. INSTALLED SEAT TRACK SPLICE AT STATION 1183 NR 2 SEAT TRACK TO STATION 1 309 PER SRM 53-05 PART 1. (M) 2 L 7 2 4F A6WE 2001021300545 20010213 00545 SW 2001 2 13 20010212SG006 1 20010104 A 2613 WARNING LIGHT SWRNGN SA227 SA227AC 8780603 SW COCKPIT ILLUMINATED A BSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 05 27465 AC755B FLT 1325 - BWD - DURING CLIMB-OUT, THE RIGHT WING OVERHEAT LIGHT CAME ON. THE LIGHT WENT OUT WHEN LANDING GEAR WAS EXTE NDED FOLLOWING THE EMERGENCY CHECKLIST. CREW RETURNED TO STATION. NO APPARENT MECHANICAL CAUSE. THIS TEMP SENSOR IS L OCATED IN THE WHEEL WELL FORWARD OF THE MASS FLOW VALVE, APPROXIMATELY THE LEADING EDGE OF THE TIRES. IF THE BRAKES WER E HOT, AND FULL HEAT IS SELECTED, IT IS POSSIBLE THAT THE COMBINATION OF HEAT SOAKED BRAKES AND THE HOT BLEED AIR IN THE BLEED AIR LINE GOING TO THE MASS FLOW VALVE REACHED THE TRIP POINT FOR THE WING OVERHEAT SENSOR. MAINTENANCE WAS DISPA TCHED, INSPECTED WINGS FOR SIGNS OF OVERHEAT, BLEED AIR LEAKS, AND DAMAGED WIRING. NONE WAS FOUND. NO FURTHER DISCREPA 2 L 7 2 4T RT A8SW 2001021300546 20010213 00546 SW 2001 2 13 20010212SG007 1 20010119 A 2910 27810032135 HYDRAULIC LINE SWRNGN SA227 SA227AC 8780603 SW LT MLG WW LEAKING A BSAA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 NM 05 702M AC702 BIL - FLT 2573 - CREW WS ON DOWNWIND LEG WHEN THE HYDRAULIC PRESSURE LIGHTS STARTED COMING ON INTERMITTENTLY. AFTR FLAP S WERE SELECTED TO 1/2 AND WENT TO THAT SETTING, THE GEAR WOULD NOT INDICATE DOWN AND LOCKED WHEN GEAR DOWN WAS SELECTED . CREW FOLLOWED GEAR EMERGENCY EXTENSION PROCEDURES AND GEAR LOCKED DOWN, WITH ''THREE GREEN'' INDICATED. FULL FLAPS D OWN WAS SELECTED ON FINAL AND FLAPS WENT TO FULL POSITION. CREW LANDED WITH NO FURTHER INCIDENT. HYDRAULIC LEAK CAUSED LOSS OF HYDRAULIC FLUID. REMOVED DAMAGED PORTION OF FLAP UPLINE IN LEFT WHEEL WELL AND SPLICED IN NEW LINE. GEAR SWIN G AND FLAP OPERATION OPS CHECK GOOD. HYD SYSTEM RESERVICED. (M) 2 L 7 2 4T RT A8SW 2001021300552 20010213 00552 EU 2001 2 13 YENA0101 1 20010123 A 3260 848401 SENSOR AIRBUS 320 A320232 3930326 EU RT MLG MALFUNCTIONED A YENA O OTHER J WARNING INDICATION DE DESCENT 1 EA 15 509JB 1270 FLT 14 - JFK-FLL - EN ROUTE, THE LGCIU NR 1 FAULTED. AT GEAR EXTENSION CREW OBSERVED XX''S ON GEAR IND WITH TRIANGLE GR EEN ON SECONDARY IND. MX CONTROL WAS PATCH TO THE CREW VIA ARINC, MX CONTROL RELAYED THIS WAS PROPER IND. FOR THE LGCIU NR 1 FAULT. THE CREW REQUESTED A ''FLYBY'' AND TOWER CONFIRMED ALL THREE LANDING GEAR WERE EXTENDED. A/C LANDED WITHO UT INCIDENT. DURNIG T/S OF THE LGCIU NR 1 THE INTERROGATION CHECK INDICATED THE RIGHT GEAR UPLOCK SENSOR 8GA WAS FAULTE D. THE LGCIU''S WERE SWAPPED AND PROBLEM DID NOT FOLLOW. A/C MX DISCONNECTED, CLEANED AND REPOSITIONED CANNON PLUG FOR THE RT GEAR UPLOCK SENSOR 8GA. FAULT CONDITION CORRECTED. 2 L 7 2 4F RT A28NM 2001021300557 20010213 00557 EU 2001 2 13 SIMA0012 1 20010101 A 2131 21179662 CONTROLLER SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE J WARNING INDICATION DE DESCENT 1 SW 21 326AE 340B326 YQB - FLT 4610 - AIRCRAFT LOST PRESSURIZATION DURING DESCENT AT 6000 FT, REMOVED AND REPLACED CABIN PRESSURIZATION CONTR OLLER WITH A SERVICEABLE UNIT IAW SAAB AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001021300558 20010213 00558 EU 2001 2 13 SIMA0021 1 20010102 A 3222 STRUT SAAB SF340 340B 7860101 EU NLG LEAKING A SIMA O OTHER J WARNING INDICATION CL CLIMB 1 SW 21 177AE 340B177 AMA - FLT 3652 - DURING TAKEOFF LANDING, GEAR INTRANSIT LIGHT STAYED ILLUMINATED. CREW SELECTED GEAR HANDLE DOWN AND CO NTINUED TO DFW. INTRANSIT LIGHT EXTINGUISHED WITH LANDING GEAR EXTENDED. MAINTENANCE REPACKED THE NLG STRUT ASSEMBLY I AW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURND TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001021400082 20010214 00082 WP 2001 2 14 USAAD01010 1 20010116 A 3260 833604 CONTROL UNIT DOUG DC9 DC982 3022082 WP E/E COMPT MALFUNCTIONED A USAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 19 816US 48096 FLL-CLT - FLT 806 - THE NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE WHEN THE LANDING GEAR WAS EXTENDED. THE CREW EXCERCISE D A GO AROUND, THE LANDING GEAR WAS CYCLED AND THE NOSE GEAR GREEN LIGHT ILLUMINATED. THE AIRCRAFT LANDED WITHOUT INCID ENT. MAINTENANCE REPLACED THE PROXIMITY SWITCH ELECTRONIC UNIT. (M) 2 L 7 2 4F A6WE 2001021400083 20010214 00083 NM 2001 2 14 USAABB01002 1 20010109 A 3350 20121 CHARGER BOEING 767 767201 1385125 NM CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 645US 23897 SFO - THE RIGHT EXTERIOR EMERGENCY LIGHTS ILLUMINATED WHEN THE SWITCH WAS PLACED IN THE ARMED POSITION. MAINTENANCE REP LACED THE BATTERY CHARGER. (M) 2 L 7 2 4F RT A1NM 2001021400084 20010214 00084 NM 2001 2 14 USAABB01003 1 20010109 A 3350 S417N5091 LIGHT BOEING 767 7672B7 1385107 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 656US 26847 LAX - FOUND THE FIRST TWO EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE WIRING BETWEEN THE LIGHTS AND THE TWO LIGHT ASSEMBLIES. (M) 2 L 7 2 4F RT A1NM 2001021400086 20010214 00086 NM 2001 2 14 20010214SG002 1 20010107 A 3510 10003018 TRANSDUCER BOEING 757 757236 NM OXYGEN SYSTEM INOPERATIVE A N8TA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 19 526NA 24794 AIR RETURN DUE TO AFTER TAKEOFF CREW O2 DROPPED TO 10 PSI. RETURNED TO NORMAL AFTER LANDING. PLACARDED CREW 02 PRESS I NDICATION ON EICAS PER MEL 35-11-02 SIT 1. PRESSURE TRANSDUCER INOPERATIVE. REPLACED TRANSDUCER AND RETURN TO SERVICE. (M) 2 L 7 2 4F RT A2NM 2001021400087 20010214 00087 NE 2001 2 14 WRLA01001 2 20010122 A 7261 57T39701 B-NUT DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE NR 3 ENGINE LOOSE A WRLA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 27 278WA 48746 LOST ELEVEN QUARTS OF ENGINE OIL ON NR 3 ENGINE IN THE MATTER OF TWO MINUTES OF FL370, FROM THAT POINT, WE LOST ONE QUAR T EVERY FIFTEEN MINUTES. AT TWO QUARTS REMAINING A PRECAUTIONARY SHUTDOWN OF THE NR 3 ENGINE WAS MADE. AFTER SHUTDOWN NINE QUARTS DECREASED TO 6 QUARTS TO LANDING. TEMP PRESSURE BEFORE SID. TEMP 106, PRESS 195. AFTER SHUTDOWN, TEMP 103 , PRESS 18. FOUND PRESSURE OIL LINE FITTING TO NR 3 BEARING LEAKING. RETORQUED AND SAFETY WIRED FITTING PER MM 79-21-0 0, WIND MILLED ENGINE. LEAK CHECK GOOD PER MM 71-00-05. OK TO PROCEED. SERVICED NR 3 ENGINE OIL EIGHTEEN QUARTS. (M) 2 L 7 3 4F 4 F RT A22WE E24NE 2001021400088 20010214 00088 SO 2001 2 14 C2XA01CL006 1 20010116 A 3230 355022002MOD2 CONTROL UNIT EMB 135 EMB135ER 3260203 SO COCKPIT FAILED A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 12519 26 145366 CLE - FLT 3798 - THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM CLEVELAND. THE AIRCRAFT RETURN ED AND LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT IAW EMB MM 32-32-01. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001021400089 20010214 00089 SO 2001 2 14 C2XA01CL008 1 20010120 A 5610 163500110 WINDSHIELD EMB 135 EMB135ER 3260203 SO FLT COMPARTMENT BROKEN A C2XA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 27 14505 2460 145192 DCA-CLE - FLT 3657 - THE CREW REPORTED THE FIRST OFFICERS WINDSHIELD SHATTERED IN FLIGHT AT 31,000 FT. THE AIRRAFT DIVE RTED INTO PITTSBURGH AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIEL D IAW EMB MM 56-10-01. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001021400090 20010214 00090 SO 2001 2 14 C2XA01CL009 1 20010117 A 3610 14530722411 DUCT EMB 145 EMB145LR SO BLEED AIR CRACKED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 15980 145202 CLE - FLT 3641 - THE CREW REPORTED ON CLIMB-OUT, RECEIVED A NR 2 BLEED LEAK INDICATION. THE REPORTED A STRONG BURNING S MELL UNTIL THE BLEED WAS SHUT OFF. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 BLEED AIR DUCT ASSEMBLY IAW EMB MM 21-60-01. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001021400091 20010214 00091 EU 2001 2 14 C2XA01BT004 1 20010119 A 3350 3011180A POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11835 194 BTV - FLT 2930 - MAINTENANCE FUOND OUTSIDE EMERGENCY LIGHT FORWARD SIDE INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY AT 10WL, OPS CHECKED GOOD IAW AMM 33-51-21. (M) 2 H 7 2 4T RT A53EU 2001021400092 20010214 00092 EU 2001 2 14 C2XA01BT003 1 20010116 A 3350 EO38802 LIGHT AEROSP ATR42 ATR42320 8680930 EU AIRSTAIR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 19812 99 EWR - FLT 3325 - CREW REPORTED STAIRS EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED STAIRS EMERGENCY LI GHT IAW 33-50-00. OPS CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 2001021400093 20010214 00093 NM 2001 2 14 20010214SG003 1 20010112 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 803MA 22434 ON PREFLIGHT TRANSIT, FOUND LEFT MID EXTERNAL OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LEFT MID OVERWING EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-22-101. OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 2001021400094 20010214 00094 NM 2001 2 14 20010214SG004 1 20010120 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 803MA 22434 ON PREFLIGHT TRANSIT, FOUND RIGHT MID EXTERNAL OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT MI D OVERWING EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-50-22. OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 2001021400095 20010214 00095 NM 2001 2 14 20010214SG005 1 20010110 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 803MA 22434 ON PREFLIGHT TRANSIT, FOUND FORWARD EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT FORW ARD OVERWING EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-50-22. OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 2001021400096 20010214 00096 NM 2001 2 14 20010214SG006 1 20010108 A 3350 100677 LIGHT DHAV DHC8 DHC8102 2809003 NM L1 DOOR INOPERATIVE A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 802MA 245 DURING A-CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLAED L1 EMERGENCY LIGHT IAW MM 33-50-22. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 2001021400097 20010214 00097 EA 2001 2 14 REXA01001 1 20010106 A 2612 47259701 CONTROL UNIT CNDAIR CL600 CL6002B19 EA COCKPIT SHORTED A REXA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SO 25 8416B 1116 7416 DURING APPROACH TO MEMPHIS, THE L FIRE FAIL, L JETOVHT FAIL, APU FAIL, R FIRE FAIL, AND R JETOVHT FAIL CAUTION MESSAGES ILLUMINATED. APPROXIMATELY 20 SECONDS LATER, THE L JETOVHT WARNIGN MESSAGE ILLUMINATED INTERMITTENTLY, FOLLOWED BY THE L ENG FIRE AND APU FIRE WARNING MESSAGES. THE APU WAS NOT RUNNING AT THE TIME. EMERGENCY PROCEDURES WERE CARRIED OUT, LEFT ENGINE WAS SHUT DOWN AND FIRE BOTTLE DISCHARGED. APU FIRE BOTTLE WAS ALSO DISCHARGED. LANDING WAS OTHERWISE UNEVE NTFUL. DURING T/S, MX FOUND THE FIRE DETECTECTION CONTROL UNIT LOCATED UNDER LEFT CONSOLE SHORTED AND CONTAMINATED WITH A LIQUID (COFFEE). A NEW CONTROLLER, ENGINE FIRE BOTTLE AND APU FIRE BOTTLE WERE INSTALLED. 2 L 7 2 4F RT A21EA 2001021400098 20010214 00098 NE 2001 2 14 REXA01002 2 20010107 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE LEAKING A REXA E A ENGINE SHUTDOWN UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SO 25 935MA 340A073 GEE367215 DURING CRUISE FLIGHT FROM MEM TO TRI, AT FL 190, THE L ENG OIL PRESSURE AND MASTER WARNING LIGHTS ILLUMINATED. LEFT ENG INE OIL PRESSURE GAUGE WAS IN THE LOWER YELLOW AREA. COMPLIED WITH EMERGENCY PROCEDURES AND SHUTDOWN ENGINE. DECLARED AN EMERGENCY WITH ATLANTA CENTER AND WAS DIVERTED TO TYS. LANDING WAS OTHERWISE UNEVENTFUL. MAINTENANCE FOUND A LOSS O F OIL FROM THE ENGINE. CHIP DETECTOR WAS REMOVED AND IT REVEALED CHIPS. ENGINE WAS REMOVED AND REPLACED. (M) 2 L 7 2 4T 4 T RT A52EU E8NE6 2001021500169 20010215 00169 EA 2001 2 15 20010215SG002 1 20010123 A 2450 A701D RELAY DHAV DHC6 DHC6300 2802606 EA CABIN SHORTED A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 19 533SW 533 FLT 9658 - VIJ/SJU - SPARKS NOTICED AT ROW 2EF OVERHEAD PANEL. REMOVED AND REPLACED NR 1 STARTER GENERATOR RELAY. (M) 1 H 7 2 3T RT A9EA 2001021500170 20010215 00170 NM 2001 2 15 20010215SG003 1 20010101 A 2611 LIGHT BOEING 727 72721 1384003 NM COCKPIT INOPERATIVE A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 329QS 19038 FLT 649 - IND - NR 1 SMOKE DETECTOR SYSTEM WOULD NOT TEST. RELAMPED NR 1 SMOKE DETECTOR BEACON AND TEST LAMPS. SYSTEM OPERATES NORMAL. (M) 2 L 7 3 4F A3WE 2001021500171 20010215 00171 NM 2001 2 15 20010215SG004 1 20010123 A 2916 RESERVOIR BOEING 727 72751C 1384015 NM HYDRAULIC SYS OVERSERVICED A RYNA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 07 435EX 19288 FLT 715 - DEPARTING PHL EXPERIENCED NAUSEATING FUMES IN COCKPIT. TURNED OFF BOTH PACKS, WENT ON TO OXYGEN. CREW PERFOR MED AN AIR TURN BACK TO PHL AND LANDED SAFELY WITHOUT FURTHER INCIDENT. FOUND A-SYSTEM AND STANDBY HYDRAULIC RESERVOIRS OVERSERVICED. DRAINED EXCESS FLUID TO FULL MARK. SYSTEM OPERATES NORMAL. (M) 2 L 7 3 4F A3WE 2001021500172 20010215 00172 EA 2001 2 15 MASA01013 1 20010126 A 2740 3094334 SWITCH CNDAIR CL600 CL6002B19 EA YOLK MALFUNCTIONED A MASA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 07 7264V 7264 FLT 6022 - FAT-PHX - RETURNED TO FIELD DUE TO AIRCRAFT TRIMMED NOSE DOWN THREE TIMES DURING CLIMB-OUT. MAINTENANCE DISC OVERED A CHAFFED WIRE IN THE CAPTAINS YOLK. MAINTENANCE REPLACED THE WIRE AND THE SWITCH. OPS CHECKED GOOD. THE AIRCR AFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001021500173 20010215 00173 NM 2001 2 15 USAA010051 1 20010122 A 5511 FITTING BOEING 737 737201 1384454 NM REAR SPAR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 245US 49326 22751 CLT - FOUND REAR SPAR FITTING CORRODED 4 INCHES, RT HINGE ATTACH CLEVIS. CORROSION LEVEL 1 C53-701-02. SPOT FACED INBO ARD/OUTBOARD CLEVIS PER EA 68752. (M) 2 L 7 2 4F A16WE 2001021500174 20010215 00174 NM 2001 2 15 USAA010052 1 20010122 A 5511 FITTING BOEING 737 737201 1384454 NM REAR SPAR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 245US 49326 22751 CLT - FOUND FITTINGS SPAR CORRODED 4 INCHES, REAR SPAR HINGE FITTING LT CLEVIS AND LUG. CORROSION LEVEL 1 C53-701-02. SPOT FACED LUG PER EA 68689. (M) 2 L 7 2 4F A16WE 2001021500175 20010215 00175 NM 2001 2 15 USAASB01016 1 20010122 A 2781 189929 PROXIMITY SWITCH BOEING 737 737201 1384454 NM LE SLATS OUT OF ADJ A USAA O OTHER E VIBRATION/BUFFET AP APPROACH 1 EA 19 259AU 22806 BWI - FLT 2679 - ON APPROACH TO BWI, THE LEADING EDGE TRANSIT LIGHT ILLUMINATED, ALONG WITH A BAD VIBRATION, DURING FLAP EXTENSION. THE NR 3 AND NR 4 LEADING EDGE SLATS WOULD NOT EXTEND. CREW DECLARED AN EMERGENCY, ACCOMPLISHED QUICK REFE RENCE HANDBOOK PROCEDUES AND ON THIRD ATTEMPT TO EXTEND SLATS, SLATS FINALLY EXTENDED AND THE FLIGHT LANDED WITHOUT FURT HER INCIDENT. MAINTENANCE ADJUSTED MID PROXIMITY SWITCHES ON NR 3 AND NR 4 SLATS. CHECKED ANDLUBED ALL ROLLERS AND CHE CKED DETENT SPRING TENSION. OPERATIONAL CHECK NORMAL. NO EVIDENCE OF BYPASSING ACTUATORS. (M) 2 L 7 2 4F A16WE 2001021500176 20010215 00176 NM 2001 2 15 USAASB01019 1 20010123 A 4930 36177501 FUEL CONTROL BOEING 737 7372B7 1384560 NM APU MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 283AU 33114 23116 MCO - FLT 2993 - EN ROUTE FROM BOS-FLL, AT FL330, THE APU SHUTDOWN IN FLIGHT. WITH THE NR 1 CSD/GENERATOR ALREADY ON ME L, FLIGHT DIVERTED TO MCO. CAPTAIN WAS ABLE TO RESTART THE APU DESCENDING THROUGH FL240. FLIGHT LANDED WITHOUT FURTHER INCIDENT AT MCO AND TAXIED TO THE GATE. AN EMERGENCY WAS DECLARED. MX REPLACED THE APU FUEL CONTROL UNIT AND THE COMB USTOR ASSY (P/N 3604524-54). APU STARTED AND OPERATED NORMALLY. OPERATIONAL CHECK AND LEAK CHECK GOOD. MAINTENANCE AL SO REPLACED BROKEN TERMINAL LEADS ON NR 1 GENERATOR FEEDER WIRES, BUT WERE UNABLE TO RECONNECT CSD. THE NR 1 CSD/GENERA TOR REMAINED ON MEL. (M) 2 L 7 2 4F A16WE 2001021500177 20010215 00177 NM 2001 2 15 USAA010053 1 20010122 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND FRAME CRACKED .75 INCH, BS 597 LEFT JUST ABOVE CENTER WING. INSTALLED NEW FRAME PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2001021500178 20010215 00178 NM 2001 2 15 USAA010054 1 20010122 A 5312 ANGLE BOEING 737 737201 1384454 NM BULKHEAD CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND UPPER CHORD ANGLE CRACKED 2 INCHES, 727 BULKHEAD AT RBL 25. INSTALLED REPAIR ANGLE PER TR 53-10-03A. (M) 2 L 7 2 4F A16WE 2001021500179 20010215 00179 NM 2001 2 15 USAA010005 1 20010115 A 5313 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND TIE CLIP CRACKED .75 INCH, BS 520, STRINGER 19L. INSTALLED NEW STRINGER TIE CLIP PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2001021500180 20010215 00180 NM 2001 2 15 USAA010006 1 20010115 A 5320 WEB BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND WEB CRACKED 1 INCH, LT CREASE BEAM WEB STATION 616-639, STRINGER 18L. INSTALLED NEW WEB PER SRM 51-10-1 AND 51-30-3. (M) 2 L 7 2 4F A16WE 2001021500181 20010215 00181 NM 2001 2 15 USAA010007 1 20010115 A 5313 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND TIE CLIP CRACKED .25 INCH STATION 643, STRINGER 4R. REPAIRED PER EO 5393G227. (M) 2 L 7 2 4F A16WE 2001021500182 20010215 00182 NM 2001 2 15 USAA010008 1 20010115 A 5313 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 663-675, STRINGER 10L. REPAIRED PER EO 5393G227. (M) 2 L 7 2 4F A16WE 2001021500183 20010215 00183 NM 2001 2 15 USAA010009 1 20010115 A 5313 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 685, STRINGER 2L. REPAIRED PER EO 5393G227. (M) 2 L 7 2 4F A16WE 2001021500184 20010215 00184 NM 2001 2 15 USAA010010 1 20010115 A 5313 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND TIE CLIP CRACKED .25 INCH, STATIN 727A, STRINGER 1. REPAIRED PER EO 5393G227. (M) 2 L 7 2 4F A16WE 2001021500185 20010215 00185 NM 2001 2 15 USAA010011 1 20010115 A 5313 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 727B, STRINGER 2L, 6L AND 7L. REPAIRED PER EO 5393G227. (M) 2 L 7 2 4F A16WE 2001021500186 20010215 00186 NM 2001 2 15 USAA010012 1 20010115 A 5313 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 727A, STRINGER 4R, 6R, 8L AND 9L. INSTALLED MODIFIED TIE CLIP PER EO 539 3G227. (M) 2 L 7 2 4F A16WE 2001021500187 20010215 00187 NM 2001 2 15 USAA010013 1 20010115 A 5313 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 747, STRINGER 5L. REPAIRED PER EO 5393G227. (M) 2 L 7 2 4F A16WE 2001021500188 20010215 00188 NM 2001 2 15 USAA010014 1 20010115 A 5313 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 767, STRINGER 4R. REPAIRED PER EO 5393G227. (M) 2 L 7 2 4F A16WE 2001021500189 20010215 00189 NM 2001 2 15 USAA010015 1 20010115 A 5313 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 767, STRINGER 5L, 6L. INSTALLED MODIFIED TIE CLIP PER EO 5393G227. (M) 2 L 7 2 4F A16WE 2001021500190 20010215 00190 NM 2001 2 15 USAA010016 1 20010115 A 5313 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 787, STRINGER 5R. REPAIRED PER EO 5393G227. (M) 2 L 7 2 4F A16WE 2001021500191 20010215 00191 NM 2001 2 15 USAA010017 1 20010115 A 5313 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 787, STRINGER 10R. REPAIRED PER EO 5393G227. (M) 2 L 7 2 4F A16WE 2001021500192 20010215 00192 NM 2001 2 15 USAA010018 1 20010115 A 5313 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 807, STRINGER 2R AND STRINGER 4L. REPAIRED PER EO 5393G227. (M) 2 L 7 2 4F A16WE 2001021500193 20010215 00193 NM 2001 2 15 USAA010019 1 20010115 A 5313 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 827 STRINGER 2L, 6L AND 10L. REPAIRED PER EO 5393G227. (M) 2 L 7 2 4F A16WE 2001021500194 20010215 00194 NM 2001 2 15 USAA010020 1 20010115 A 5320 INTERCOSTAL BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 288AU 46103 23135 CLT - FOUND INTERCOSTAL CRACKED .5 INCH, 178 BULKHEAD, WL 195, RBL 24 AND LBL 24. INSTALLED NEW PART PER SRM 53-10-11 F IG 7. (M) 2 L 7 2 4F A16WE 2001021500195 20010215 00195 NM 2001 2 15 USAA010021 1 20010115 A 5312 WEB BOEING 737 7372B7 1384560 NM BULKHEAD CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 288AU 46103 23135 CLT - FOUND WEB CRACKED .5 INCH, BS 178, WL 211, BL 23 RT AND BL 23 LT. REPLACED WEB PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2001102500158 20011025 00158 EU 2001 10 25 USAAF01003 1 20010121 A 3350 9EL00621200 SIGN FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 866US 11310 PHL - FOUND THE EMERGENCY EXIT LIGHT OVER SEAT 12F TO BE INOPERATIVE. MAINTENANCE REPLACED THE EXIT SIGN. (M) 2 L 7 2 4F RT 2001021500196 20010215 00196 NE 2001 2 15 USAASB01011 2 20010119 A 7200 ENGINE BOEING 737 737201 1384454 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE FAILED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 247US 22754 709116 LGA - FLT 2990 - ON CLIMB-OUT FROM LGA, AFTER FL120, CREW REPORTED LOSS OF NR 1 ENGINE OIL AND THE LOW OIL PRESSURE LIGH T ILLUMINATING. OIL PRESSURE DROPPED BELOW THE RED LINE AND HELD AT ABOUT 20 PSI. CREW SHUT DOWN THE NR 1 ENGINE, DECL ARED AN EMERGENCY AND RETURNED TO FIELD AT LGA. FLIGHT LANDED WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS 8 MINUTES. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE ASSEMBLY. OPS CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F 4 F A16WE E2EA 2001021500197 20010215 00197 NE 2001 2 15 USAASB01015 2 20010121 A 7200 ENGINE BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE FAILED A USAA O OTHER R E X PARTIAL RPM/PWR LOSS VIBRATION/BUFFET ENGINE FLAMEOUT DE DESCENT 1 EA 19 371US 22950 725108 CLT - FLT 862 - DURING DESCENT INTO CLT, AT APPROX FL100, THE NR 2 ENGINE STALLED AND VIBRATED MULTIPLE TIMES AT LOW POW ER SETTINGS. CREW DISCONNECTED AUTOTHROTTLE AND PLACED POWER TO IDLE. EGT WAS NOTED AS HIGHER BUT SMOOTH. APPROX 10 M INUTES OUT ON APPROACH, THE NR 2 ENGINE FAILED/FLAMED OUT. CREW SHUTDOWN THE NR 2 ENGINE AT FL080, DECLARED AN EMERGENC Y AND CONTINUED THE APPROACH. FLIGHT LANDED WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS 5 MINUTES. MAINTEN ANCE REMOVED AND REPLACED THE NR 2 ENGINE ASSEMBLY PER JOB CARD. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F 4 F RT A16WE E2GL 2001021500198 20010215 00198 NM 2001 2 15 USAASB1017 1 20010122 A 7603 580291025 THROTTLE CABLE BOEING 737 7373B7 1384580 NM NR 2 ENGINE FAILED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 373US 22952 EWR - FLT 1024 - EN ROUTE FROM DCA TO ALB, THE NR 2 THRUST LEVER STUCK AT CLIMB POWER. CREW DISENGAGED AUTO THROTTLES B UT WAS STILL UNABLE TO RETARD THRUST LEVER. CREW DECLARED AN EMERGENCY, ACCOMPLISHED ENGINE SHUTDOWN CHECKLIST AND SHUT DOWN THE NR 2 ENGINE. FLIGHT DIVERTED TO EWR AND LANDED WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS 25 MINU TES. MAINTENANCE REMOVED, REPLACED AND RIGGED THE NR 2 ENGINE TELEFLEX THROTTLE CABLE. THROTTLE OPERATES SMOOTHLY THRO UGHTOUT ALL TRAVEL. PERFORMED POWER ASSURANCE ENGINE RUM. ENGINE PERFORMED WITHIN LIMITS PER MM 71-00-00, TEST NR 5. (M) 2 L 7 2 4F RT A16WE 2001021500199 20010215 00199 NM 2001 2 15 USAASB01008 1 20010117 A 2420 941D3391 TRANSFORMER BOEING 737 7372B7 1384560 NM NR 1 ENGINE FAILED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 EA 19 277AU 22889 CLT - FLT 9265 - A/C PREPARING FOR FERRY FLT WHEN ELECT PROBLEMS OCCURED. ACARS WENT INTO BITE TEST BEFORE TAKING RUNWA Y. AUTO THROTTLE WENT INOP. AT FL180, NR 1 GEN DROPPED OFF LINE, WOULD NOT RESET. CAPT COULDN''T COMMUNICATE W/DISPAT CH DUE TO ACARS PROBLEM. RETURNED TO FIELD. MX REPAIRED ACARS, R/R ACARS IDU (P/N 2229346-121). SYS OPS CHECK GOOD. RELEASED AUTO THROTTLES ON MEL DUE INOP NR 2 LVDT. REPLACED NR 2 LVDT (P/N 65-51534-12). OPS TEST GOOD, CLEARED MEL. NR 1 GEN FEEDER WIRE INSULATION CHAFED AND SHORTED TO WIRE BUNDLE CLAMP 18 INCHES FROM FIREWALL CONNECTOR. ACCOMP TEMP REPAIR PER BOEING WPM 20-10-13 AND PROGRAMMED NEW HARNESS REPLACEMENT NEXT MX CHECK. 2 L 7 2 4F A16WE 2001021500200 20010215 00200 NM 2001 2 15 USAASB01022 1 20010126 A 3260 6552811109 ACCESSORY UNIT BOEING 737 737201 1384454 NM E/E BAY FAILED A USAA O OTHER J WARNING INDICATION DE DESCENT 1 EA 19 245US 40057 22751 BWI - FLT 2735 - UPON GEAR EXTENSION INTO BWI, CREW RECEIVED THREE GREEN AND THREE RED GEAR LIGHTS. CREW ENSURED GEAR H ANDLE WAS IN DOWN DETENT. AFTER RECYCLING GEAR, CREW RECEIVED NORMAL THREE GREEN GEAR LIGHTS AND NO RED LIGHTS. FLIGHT LANDED AT BWI WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR LEVER SWITCH (P/N MS25383-1) AND THE LANDING GEAR ACCESSORY UNIT. PERFORMED GEAR SWING. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 2001021500201 20010215 00201 NM 2001 2 15 USAASB01021 1 20010123 A 4990 6984302 PRESSURE SWITCH BOEING 737 7372B7 1384560 NM APU FAULTY A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 283AU 23116 CHS - FLT 2622 - EN ROUTE FROM MCO TO BWI, THE APU SHUTDOWN. THE NR 1 CSD/GENERATOR WAS ALREADY ON MEL, SO THE FLIGHT D IVERTED TO CHS AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE APU SEQUENCING OIL PRESSURE SWITCH. ALSO, REMOVED AND REPLACED THE APU TACHOMETER GENERATOR (P/N 2CM9ABHY) AND REPINNED TE TACHOMETER GENERATOR CONNECTOR. OPERATIONAL CHECK OF APU GOOD. CLEARED MEL ON NR 1 CSD/GENERATOR BY REMOVING AND REPL ACING THE CSD (P/N 731753), GENERATOR (P/N 976J498-1) AND OIL COOLER (P/N 6A47-000) PER MM 24-11-11 AND MM 24-21-11. RA N ENGINE. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F A16WE 2001021500202 20010215 00202 2001 2 15 USAAD01015 4 20010125 A 2565 11331780 SLIDE DOUG DC9 DC931 3022065 WP SERVICE DOOR DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 955VJ 26710 47593 PHL - THE GALLEY SERVICE DOOR EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS BELOW THE GREEN ARC. MAINTENANCE REPLACED THE EVACUATION SLIDE. (M) 2 L 7 2 4F A6WE 2001021500203 20010215 00203 2001 2 15 GTIA010015 4 20010116 A 2565 SLIDE DOUG DC9 DC982 3022082 WP SERVICE DOOR OUT OF POSITION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 DTW - FORWARD SERVICE DOOR EVACUATION SLIDE CAME OFF. INSTALLED SLIDE PACK IAW MD-80 MM 25-62-00. NO DEFECTS NOTED AT THIS TIME. (M) 2 L 7 2 4F A6WE 2001021500204 20010215 00204 2001 2 15 GTIA010011 4 20010109 A 2565 SLIDE DOUG DC9 DC983 3022083 WP FWD DOOR OUT OF POSITION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 DALLR 53015 DTW - FLT 709 - FORWARD SLIDE PACK FELL OFF. REINSTALLED FORWARD SLIDE PACK IAW MD-80 MM 25-62-00. (M) 2 L 7 2 4F RT A6WE 2001021500205 20010215 00205 WP 2001 2 15 GTIA010008 1 20010106 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INTERMITTENT A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 809NK 49503 DTW - TRACK LIGHTING (RED) AT ROW 22 FLICKERS WHEN YOU STEP IN THE AISLE. REPLACED PIGTAIL WIRING ASSEMBLY. OPS CHECKE D GOOD IAW MD-80 MM 33-43-01. (M) 2 L 7 2 4F RT A6WE 2001021500206 20010215 00206 2001 2 15 GTIA010002 4 20010108 A 2565 SLIDE DOUG DC9 DC932 3022066 WP L1 DOOR OUT OF POSITION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 133NK 48111 ACY - FLT 953 - L1 DOOR EMERGENCY SLIDE PACK CAME OFF. REINSTALLED SLIDE, OPS CHECK GOOD IAW MM 25-62-0. (M) 2 L 7 2 4F A6WE 2001021500207 20010215 00207 WP 2001 2 15 GTIA010001 1 20010101 A 3397 WIRE DOUG DC9 DC931 3022065 WP COCKPIT LOOSE A K NONE O OTHER IN INSP/MAINT 1 GL 23 934ML 47526 DTW - FLT 58 - WHEN TURNING ON THE NOSE LIGHT TO BRIGHT POSITION, SPARKS WERE VISIBLE COMING FROM THE SWITCH AREA FOLLOW ED BY LIGHT SMOKE. TIGHTENED LOOSE WIRE IAW DC-9 MM 33-41. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2001021500208 20010215 00208 NM 2001 2 15 GAIA01007B 1 20010129 A 2830 AV16B1659C DUMP VALVE BOEING 727 727223 1384074 NM RT DUMP VALVE INOPERATIVE A GAIA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 6816 19491 FLT 202 - BIL - RIGHT FUEL DUMP NOZZLE VALVE WOULD NOT OPEN TO DUMP. AIRCRAFT MADE AN UNEVENTFUL RETURN TO BIL. REMOVE D AND REPLACED NR 4 FUEL DUMP VALVE IAW B727 MM 28-31-1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001021500209 20010215 00209 NM 2001 2 15 GAIA01015 1 20010129 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69739 20667 THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. DENT IN FRAME BETWEEN STRINGER 4R AND 5R AT FS 380. REMOVED DAMAGED AT STATION 380 AND FABRICATED NEW REPAIR ANGLES IAW B727 53-10-4 FIG 2. TREATED AND PRIMED IAW B727 SRM 51-10-2 AND 51-20-151. INSTALLED NEW ANGLES AT STATION 380 BETWEEN STRINGER 4R AND 5R, IAW B727 SR M 51-30-2. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001021500210 20010215 00210 NM 2001 2 15 GAIA01017 1 20010129 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM CABIN DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69739 20667 THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY, CENTER SEAT TRACK IS REQUIRED TO B E SPLICED AT BS 450 AND BS 550. REMOVED AND REPLACED SEAT TRACK AT CENTER LINE FROM BS 450 TO BS 550 IAW B727 SRM 53-30 -5, 51-10-2 AND 51-30-2. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001021500211 20010215 00211 NM 2001 2 15 GAIA01018 1 20010129 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM CABIN CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69739 20667 THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. SEAT TRACK HAS CORROSION ON INBOA RD FLANGE AT BS 686 AND BS 700. REMOVED DAMAGED SECTION OF SEAT TRACK AND FABRICATED REPAIR PARTS AND INSTALLED IAW B72 7 SRM 53-10-5. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001021500212 20010215 00212 NM 2001 2 15 GAIA01019 1 20010129 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM CABIN CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69739 20667 THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. CORROSION AROUND FASTENERS IN SEA T TRACK AT LBL 25, STATION 760 TO 870. REMOVED SEAT TRACK FROM 760 TO 870. FABRICATED NEW SEAT TRACKS IAW B727 SRM 53- 10-2. TREATED AND PRIMED IAW B727 SRM 51-10-2 AND B727 MM 51-20-151. INSTALLED TRACKS IAW B727 SRM 51-30-2. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001021500213 20010215 00213 NM 2001 2 15 GAIA01020 1 20010129 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69739 20667 THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY, BS 1090 CABIN FLOORBEAM IS CORRODE D AT THE LOWER CHORD AS SEEN FROM THE AFT CARGO COMPARTMENT, RBL 10 TO RBL 23. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED NEW REPAIR ANGLES. ALODINED AND PRIMED REPAIR AREA. REINSTALLED REPAIR IAW B727 SRM 51-10-6, 51-1 0-2, 53-10-8 FIG 8 AND B727 MM 51-20-151. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001021500214 20010215 00214 NM 2001 2 15 GAIA01021 1 20010129 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69739 20667 THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. STATION 720E FORWARD SIDE OF CIRC UMFERENTIAL FRAME HAS CORROSION BETWEEN STRINGERS 27R AND 28R ACROSS 4 FASTENERS GOING THROUGH SKIN AND UP APPROX 3 INCH ES. REMOVED DAMAGED AREA IAW B727 SRM 51-30-2. FABRICATED SHEAR TIE IAW B727 SRM 53-10-4. INSTALLED SHEAR TIE IAW B72 7 SRM 51-30-5 AND 51-30-2. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001021500215 20010215 00215 NM 2001 2 15 GAIA01022 1 20010129 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM CABIN CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69739 20667 THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. CORROSION FOUND AROUND FASTENERS IN SEAT TRACK AT LBL 45 FROM STATION 760 TO 870. REMOVED CORROSION AND FOUND OUT OF LIMITS. FABRICATED NEW SEAT TRACK, ALODINED AND PRIMED AND REINSTALLED SEAT TRACKS IAW B727 SRM 51-30-2, 51-10-6, 53-10-1, 51-10-2, 51-10-1. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001021500216 20010215 00216 NM 2001 2 15 GAIA01023 1 20010129 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69739 20667 THIS ITME WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. CABIN FLOORBEAM FOUND CORRODED ON UPPER SURFACE OF UPPER CHORD AT BS 400, RBL 45. REMOVED CORROSION FROM UPPER BEAM IAW B727 SRM 51-10-6, FOUND TO BE OU T OF LIMITS. FABRICATED NEW REPAIR PART IAW B727 SRM 53-10-8. TREATED AND PRIMED IAW B727 SRM 51-10-2 AND MM 51-20-151 . INSTALL NEW REPAIR ANGLE IAW B727 SRM 53-10-8. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001021500217 20010215 00217 NM 2001 2 15 GAIA01024 1 20010129 A 5310 SHEAR TIE BOEING 727 727224 1384076 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69739 20667 THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. CORROSION FOUND ON SHEAR TIE, FOR WARD SIDE AT BS 700 BETWEEN STRINGER 27L AND 28L, FORWARD PIT. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. INSTAL LED DOUBLER REPAIR IAW B727 SRM 53-10-4 FIGURE 15. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001021500218 20010215 00218 NM 2001 2 15 GAIA01025 1 20010129 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM CABIN CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69739 20667 THIS ITEM WAS FOUND DURING ROUTINE NAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. CORROSION FOUND ON SEAT TRACK INB OARD FLANGE AT BS 634, OUTBOARD FLANGE AT BS 697 TO BS 715. REMOVED AND REPLACED SEAT TRACK FROM BS 690 TO BS 720B PER B727 PER B727 SRM 51-10-2, 53-10-2, 53-10-05 AND MM 51-20-151. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001021500219 20010215 00219 NM 2001 2 15 GAIA01026 1 20010129 A 5330 SKIN BOEING 727 727224 1384076 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69739 20667 THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. CORROSION FOUND ON BILGE SKIN FRO M BS 720D TO 720E, STRINGER 29L TO 29R. CORRODED FASTENERS RUNNING THROUGH FLANGE ON DUCT IN SAME AREA. REPAIRED CORRO DED SKIN AND REMOVED AND REPLACED CORRODED FASTENERS IAW B727 SRM 53-30-3 FIG 13 AT BS 720D TO 702E STRINGERS 29L TO 29R . AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001021500220 20010215 00220 NM 2001 2 15 GAIA01027 1 20010129 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM CABIN CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69739 20667 THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY, COROSION FOUND ON SEAT TRACK AT BS 760 TO 870 RBL 45. REMOVED CORROSION IAW B727 SRM 51-10-6. FOUND TO BE OUT OF LIMITS. FABRICATED NEW SEAT TRACK IAW B727 SRM 53-10-1. TREATED AND PRIMED IAW B727 SRM 51-10-2 AND MM 55-20-151. INSTALLED NEW SEAT TRACK IAW B727 SRM 51-3 0-2. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001021500221 20010215 00221 NM 2001 2 15 GAIA01028 1 20010129 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM FUSELAGE MISDRILLED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 69739 20667 THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. FLOORBEAM UPPER CAP AT BS 344 HAS SEVERAL HOLES WITH NO EDGE DISTANCE. REMOVED AND REPLACED FLOORBEAM UPPER CAP AT BS 344 FROM RBL 67 TO LBL 67 IAW B727 SRM 53-10-2 AND 51-30-2. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001021500222 20010215 00222 NM 2001 2 15 GAIA01029 1 20010129 A 5347 SPLICE BOEING 727 727224 1384076 NM SEAT TRACK CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 27 69739 20667 THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. SEAT TRACK SPLICE FOUND CORRODED AT BS 690 RBL 24. REMOVED SEAT TRACK SPLICE STRAP FROM BS 690 RBL 24, IAW B727 SRM 51-30-2. FABRICATED SPLICE STRAP IA W B727 SRM 53-10-5. INSTALLED SPLICE STRAP AT BS 690 RBL IAW B727 SRM 51-30-2. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001021500223 20010215 00223 NM 2001 2 15 GAIA01030 1 20010129 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM CABIN CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69739 20667 THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. SEAT TRACK AND FASTENERS AT BS 76 0 TO 870 RBL 25 CORRODED. REMOVED AND REPLACED SEAT TRACK FROM BS 760 TO 870 RBL 25, IAW B727 SRM 51-30-2. AIRCRAFT WA S RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001021500224 20010215 00224 NM 2001 2 15 GAIA01031 1 20010129 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69739 20667 THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE ACILITY. CABIN FRAME DENTED AT BS 600, STRI NGER 9R. FABRICATED REPAIR DOUBLER IAW B727 SRM 53-10-2, FIG 4. INSTALLED FRAME REPAIR DOUBLER AT BS 600 STRINGER 9R I AW B727 SRM 53-10-4. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001021500225 20010215 00225 NM 2001 2 15 GAIA01032 1 20010129 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM FUSELAGE MISDRILLED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 69739 20667 THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. FLOORBEAM UPPER CAP AT BS 360, RB L 63 HAS DOUBLER DRILLED HOLES. REMOVED DAMAGES SECTION OF FLOORBEAM. FABRICATED REPAIR ANGLE IAW B727 SRM 53-10-8. I NSTALLED REPAIR IAW B727 SRM 53-10-8 FIG 8. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001021500226 20010215 00226 NM 2001 2 15 GAIA01033 1 20010129 A 5310 SHEAR TIE BOEING 727 727224 1384076 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69739 20667 THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. CORROSION FOUND ON BELLY FRAME TO SKIN ATTACH ANGLE AT BS 600, LBL 3 TO RBL 3. REMOVED DAMAGES SECTION IAW B727 SRM 53-10-4. FABRICATED SHEAR TIE ANGLE IAW B727 SRM 53-10-4 SHEET 3 INSTALLED SHEAR TIE ANGLE IAW B727 SRM 53-10-4 SHEET 3. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001021500227 20010215 00227 NM 2001 2 15 GAIA01034 1 20010129 A 5314 KEELBEAM BOEING 727 727224 1384076 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69739 20667 THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. KEELBEAM LOWER CHORD AT BS 873, C RACKED THROUGH FASTENER. REMOVED FASTENERS AND DAMAGE, FABRICATED REPAIR DOUBLER IAW B727 SRM B727 51-30-2, 51-10-2, MM 51-20-151 AND SB 727 53-0280. (M) 2 L 7 3 4F A3WE 2001021500228 20010215 00228 NM 2001 2 15 GAIA01035 1 20010129 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69739 20667 THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. FLOORBEAM UPPER SURFACE OF UPPER CHORD AT BS 420, RBL 45 IS CORRODED. REPAIRED FLOORBEAM AT BS 420 RBL 45 IAW B727 SRM 53-10-8 AND 51-30-2. FABRICATED REPAIR ANGLES IAW B727 SRM 53-10-8 AND INSTALLED REPAIR ANGLES IAW B727 SRM 53-10-8 AND 51-30-2. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001021500229 20010215 00229 NM 2001 2 15 GAIA01036 1 20010129 A 5310 DOOR FRAME BOEING 727 727224 1384076 NM FWD CARGO BAY CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69739 20667 THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. THRESHOLD FRAME BOTTOM FLANGE AT THE C-1 DOOR, BS 593, RBL 20, FORWARD PIT. FABRICATED REPAIR DOUBLER AND REPAIRED THRESHOLD. INSTALLED REPAIR IAW B727 SRM 53-10-1, SRM 51-10-6, 53-10-1, 51-10-2 AND 51-20-151. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001021500230 20010215 00230 NM 2001 2 15 GAIA01041 1 20010131 A 8012 VALVE BOEING 727 727259 138408J NM NR 3 ENGINE MALFUNCTIONED A GAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 901RF 22476 FLT - 1863 - EWR-FWA - ON CLIMB-OUT, NR 3 STARTER VALVE LIGHT CAME ON. RIGHT PACK WENT TO 62 PSI. PERFORMED ENGINE SHU TDOWN. AIRCRAFT MADE AN UNEVENTFUL RETURN TO EWR. INSPECTED INLET AND EXHAUST AND MAIN OIL SCREEN AND FOUND NO DEFECTS . CHECKED PNEUMATIC DUCT AND ENGINE CASE. FOUND NO DEFECTS. OPERATED ENGINE AT MCT. OPERATION WAS NORMAL. CHECKED N ORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001021500231 20010215 00231 NM 2001 2 15 GAIA01040 1 20010130 A 3297 WIRE BOEING 727 727223 1384074 NM NOSE GEAR BROKEN A O OTHER N FALSE WARNING AP APPROACH 1 SW 07 854AA 20995 FLT 1807 - DEN-PHX - RED NOSE GEAR LIGHT ILLUMINATED, GREEN NOSE GEAR LIGHT NOT ILLUMINATED ON PRIOR TO LANDING. AIRCRA FT MADE AN UNEVENTFUL LANDING IN PHX. FOUND WIRE TO NOSE GEAR DOWN SWITCH BROKEN AT SPLICE. RE-SPLICED WITH ENVIROMENT AL SPLICE AND TIED BUNDLE PER CHAPTER 20 STD WIRING PRACTICES AS REQUIRED. OPS CHECK GOOD ON GROUND. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001021500232 20010215 00232 NM 2001 2 15 GAIA01039 1 20010127 A 7830 LIGHT BOEING 727 727223 1384074 NM COCKPIT ILLUMINATED A GAIA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SW 07 6807 19482 FLT 2023 - ABQ-PHX - AFTER TAKEOFF, THE FLIGHT CREW NOTICED THAT THE NR 2 ENGINE THRUST REVERSER LIGHT ILLUMINATED. THE CREW DECLARED AN EMERGENCY AND RETURNED TO ABQ. AN UNEVENTFUL LANDING WAS MADE. INSPECTION DID NOT REVEAL ANY PROBLEM S AND THE THRUST REVERSER INDICATION PROBLEM COULD NOT BE DUPLICATED. THE AIRCRAFT WAS RETURND TO SERVICE. (M) 2 L 7 3 4F A3WE 2001021600069 20010216 00069 NM 2001 2 16 AWXA0001258 1 20010127 A 3020 ZZLRC12123S CONNECTOR BOEING 757 757225 1384959 NM RROYCE RB211 RB211535E4 54555 NE NR 2 ENGINE MISMANUFACTURED A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 907AW 22691 30576 LAX-DIVERTED FLIGHT- EN ROUTE FROM FLL TO LAS, EICAS MESSAGE RT ENG ANTI-ICE DISPLAYED AND ANTI-ICE VALVE LIGHT REMAINED ILLUMINATED WITH THE SWITCH ON. DUE TO ICING CONDITIONS IN LAS THE AIRCRAFT DIVERTED TO LAX. IN LAX THE RT ENG ANTI-I CE VALVE WAS PLACED ON MEL 30-21-1 COND 2 AND THE VALVE LOCKED IN THE OPEN POSITION. IN LAS THE RT ENG ANTI-ICE VALVE W AS REPLACED WITH NO HELP AND THE ANTI-ICE VALVE WAS LOCKED IN THE OPEN POSITION. THE RT ENGINE ANTI-ICE VALVE REMAINS O N MEL 30-21-1 COND 2 AT THIS TIME. 28 JAN 01 - LAS - FURTHER TROUBLESHOOTING FOUND AN ADDITIONAL INSERT IN THE CONNECTO R FOR THE ANTI-ICE VALVE NOT ALLOWING FULL CONTACT OF THE PINS IN THE CONNECTOR. 2 L 7 2 4F 4 F RT A2NM E12EU 2001021600070 20010216 00070 NM 2001 2 16 UPS01234802 1 20010130 A 5751 SKIN BOEING 727 72727C 138400J NM AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 908UP 19114 INSPECTION TYPE:N/A, LT OUTBOARD AILERON HAS DELAMINATION AND .25 INCH CRACK AILERON REMOVED WD 66470 INSTALLED LT O UTBOARD AILERON TO STEP D (4) MM 27-10-31. OK FOR SERVICE. 2 L 7 3 4F A3WE 2001021600071 20010216 00071 WP 2001 2 16 TWAA0101906 1 20010123 A 5230 STRUCTURE DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT, THE FWD CARGO DOOR T/E WAS CRACKED AT AFT SIDE BETWEEN STRINGER 24R AND 25R. ACCOMP HIGH FREQ EDD Y CURRENT PER 51-00-03 PART 6 AND NO CRACKS FOUND. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 52-05. INSTALLED FASTENERS PER SRM 51-30-02. 2 L 7 2 4F A6WE 2001021600072 20010216 00072 WP 2001 2 16 TWAA0101907 1 20010125 A 5320 CLIP DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT AT STA 236, BETWEEN STRINGER 28 AND 27, A CLIP FOR FLOOR SUPPORT WAS CRACKED UNDER RT FLOOR TRACK. MADE AND INSTALLED NEW PART PER DRAWING 9915554 AND SRM 51-30-5. 2 L 7 2 4F A6WE 2001021600073 20010216 00073 WP 2001 2 16 TWAA0101908 1 20010126 A 5320 CLIP DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT, FOUND CLIP CRACKED AT STA 236, LT SIDE BETWEEN STRINGER 28 AND 27 UNDER LT TRACK. REMOVED CRACKED ANGLE AND FABRICATED NEW ANGLE PER SPM 6-70-01, AND DOUGLAS DRAWING 9915554, ANGLE ITEM -7, AND REINSTALLED. 2 L 7 2 4F A6WE 2001021600074 20010216 00074 WP 2001 2 16 TWAA0101909 1 20010128 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT, FOUND CORROSION ON FLOOR MEMBRANE AT STA 1250, LBL 49. CUT OUT CORRODED AREA AND INSTALLED WEB RE PAIR PER SRM 51-70-4. 2 L 7 2 4F A6WE 2001021600075 20010216 00075 WP 2001 2 16 TWAA0101910 1 20010129 A 5320 PAN DOUG DC9 DC982 3022082 WP CABIN FLOOR CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT, FOUND CORROSION ON FLOOR PAN AT STA 150, LBL 8 INCHES AND RBL 8 INCHES. REPAIRED PER SRM 53-01 PA GE 18. TREATED AND PAINTED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001021600076 20010216 00076 WP 2001 2 16 TWAA0101911 1 20010129 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT, FOUND MEMBRANE WITH 3 INCH CRACK AT LBL 50, STA 1022, BETWEEN NUMBER 1 AND 2 FLOOR TRACKS. REPAIR ED CRACK AT LBL 50 INCHES, STA 1022 MEMBRANE PER SRM 53-01, FIG 2, SHEET 3 AND PAGE 9. TREATED AND PRIMED AREA PER SRM 51-10-2. 2 L 7 2 4F A6WE 2001021600077 20010216 00077 WP 2001 2 16 TWAA0101912 1 20010129 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT, FOUND INTERCOSTAL CORRODED, ATOP FLOORBEAM AT STA 1250, LBL 23 TO 46. REPLACED CORRODED FLOORBEAM SUPPORT AND INSTALLED FASTENERS PER SRM 51-30-05. 2 L 7 2 4F A6WE 2001021600078 20010216 00078 WP 2001 2 16 TWAA0101913 1 20010123 A 5312 BULKHEAD DOUG DC9 DC982 3022082 WP FUSELAGE BIRD STRIKE A TWAA C ABORTED TAKEOFF C F.O.D. TO TAKEOFF 1 CE 05 922TW 48013 ON TAKEOFF SUFFERED BIRD STRIKE AT THE RADOME AREA. THE RADOME BULKHEAD WEB AT STA 37 WAS DAMAGED. INSTALLED NEW BULKH EAD WEB WITH RIVETS AND HI-LOK''S PER SRM 51-30-2 AND SRM 51-30-5. CHECK-C 6-10-00 JFK. 2 L 7 2 4F A6WE 2001021600079 20010216 00079 WP 2001 2 16 TWAA0101917 1 20010102 A 5320 WEB DOUG DC9 DC983 3022083 WP CABIN FLOOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9404V 53140 DURING CHECK-C MAINT, FOUND AFT CABIN FLOOR MEMBRANE CRACKED AT LT SIDEWELL, STA 1298 TO 1304. STOP DRILLED CRACK AND I NSTALLED DOUBLER PER SRM 53-01, FIG 2. TREATED SURFACE PER SRM 51-10-3. INSTALLED HI-LOK''S IN DOUBLER DUE TO ACCESS P ER SRM 53-30-05. INSTALLED RIVETS PER SRM 51-30-2. 2 L 7 2 4F RT A6WE 2001021600080 20010216 00080 WP 2001 2 16 TWAA0101918 1 20010126 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT, FOUND CORROSION ON FLOOR SUPPORT BETWEEN NUMBER 3 AND 4 TRACKS, STA 1308. REPLACED FLOOR SUPPORT PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-5. 2 L 7 2 4F RT A6WE 2001021600081 20010216 00081 WP 2001 2 16 TWAA0101919 1 20010127 A 5320 WEB DOUG DC9 DC983 3022083 WP CABIN FLOOR CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT, FOUND FLOOR MEMBRANE CRACKED AND CORRODED FROM STA 1287 TO 1309, BETWEEN LBL 54 TO LBL 60. CRACKS AND CORROSION RAN UNDER TRACK AND LAV FWD BULKHEAD. REMOVED CORROSION PER SRM 51-10-3, PAGE 21 PARAGRAPH 35. REPLACED MEMBRANE PER SRM 53-05, FIG 97. 2 L 7 2 4F RT A6WE 2001021600082 20010216 00082 WP 2001 2 16 TWAA0101920 1 20010129 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT, MEMBRANE AT STA 617, LONGERON 18R, WAS CORRODED ON LOWER SURFACE. INSTALLED NEW MEMBRANE PER SPM 6-70-01 PAGES 2 AND 3. INSTALLED FASTENERS PER SRM 51-30 AND 51-10-4. PAINTED PER SPM 1-20-02. 2 L 7 2 4F RT A6WE 2001021600083 20010216 00083 WP 2001 2 16 TWAA0101921 1 20010129 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT, FOUND RT FLOOR MEMBRANE CORRODED AT CUSP LINE, STA 598 THRU 712. INSTALLED NEW MEMBRANE PER SPM 6 -70-01. INSTALLED FASTENERS PER SRM 51-30 AND 51-10-4. PAINTED PER SPM 1-20-02. 2 L 7 2 4F RT A6WE 2001021600084 20010216 00084 WP 2001 2 16 TWAA0101922 1 20010129 A 5313 LONGERON DOUG DC9 DC983 3022083 WP CARGO BAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT, IN THE AFT CARGO COMPT, FOUND CORROSION ON LONGERON 19L, BETWEEN STA 1287 AND 1209. REMOVED SECTI ON OF LONGERON AND CORROSION PER SRM 51-10-3. REPLACED PORTION OF LONGERON PER SRM 53-02, FIG 18. 2 L 7 2 4F RT A6WE 2001021600085 20010216 00085 WP 2001 2 16 TWAA0101923 1 20010129 A 5315 FLOORBEAM DOUG DC9 DC983 3022083 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT, IN THE AFT CABIN, FLOORBEAM CORROSION WAS REMOVED BEYOND LIMITS AT STA 1338, LBL 19 AND LBL 26. I NSTALLED REPAIR PER SRM 53-05, FIG 20A, PAGE 31. 2 L 7 2 4F RT A6WE 2001021600086 20010216 00086 WP 2001 2 16 TWAA0101924 1 20010129 A 5320 INTERCOSTAL DOUG DC9 DC983 3022083 WP CABIN CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT, IN THE AFT CABIN, INTERCOSTAL LOWER LEG WAS CRACKED AT STA 1322, ZERO BL, JUST FWD OF FLOORBEAM. REMOVED LOWER LEG. REPLACED WITH NEW LEG USING MS20470AD5 RIVETS PER 53-01, FIG 2. 2 L 7 2 4F RT A6WE 2001021600087 20010216 00087 NM 2001 2 16 UPS01234820 1 20010130 A 3350 LIGHT BOEING 727 72722C 138400F NM COCKPIT MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE:IN, COCKPIT DOOR EMERGENCY LIGHT VERY DIM. OPS CHECK COCKPIT EMERGENCY LIGHTS WITH BOTH THE SWITCH AT T HE ASSY AND THE EMERGENCY LIGHT ARM/DISARM ON THE P4. NO DEFECTS NOTED. 2 L 7 3 4F A3WE 2001021600088 20010216 00088 NM 2001 2 16 UPS01234822 1 20010131 A 3350 BATTERY PACK BOEING 727 727247 138408F NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 210UP 21697 INSPECTION TYPE:PFLT, EMERGENCY EXIT LIGHTS FAILED TO TEST. REMOVED AND REPLACED BATTERY PACK, OPS CHECK OK. 2 L 7 3 4F A3WE 2001021600089 20010216 00089 NM 2001 2 16 UPS01434806 1 20010103 A 5754 65B024004 MOUNT BOEING 747 747123F NM LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, R WING L/E KRUEGER FLAP NR 15 INBOARD HINGE MOUNT CRACKED. NEW FLAP ASSY FITTED IAW MM 27-81-01. 2 L 7 4 4F A20WE 2001021600090 20010216 00090 NM 2001 2 16 UPS01434807 1 20010104 A 5754 20240071 CHANNEL BOEING 747 747123F NM LT WING LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, LT WING L/E LEADING EDGE FLAP DRIVE UNIT SUPPORT CHANNEL CRACKED AT POSITION NR 2 LEFDU. SUPPORT CHA NNEL REPAIRED IAW SRM 51-40-03. 2 L 7 4 4F A20WE 2001021600091 20010216 00091 NM 2001 2 16 UPS01434808 1 20010109 A 5320 BAC1522203 GUARD BOEING 747 747123F NM THROTTLE CABLE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, FWD CARGO COMPARTMENT SEVERAL CRACKS ON THROTTLE CABLE CIVER GUARDS BS 980 LT AND RT. CABLE COVER GU ARDS REPLACED IAW MM 76-11-00. 2 L 7 4 4F A20WE 2001021600092 20010216 00092 NM 2001 2 16 UPS01434809 1 20010103 A 5755 65B022501 PANEL BOEING 747 747123F NM NR 12 SPOILER DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, NR 12 SPOILER PANEL IS DELAMINATED. SPOILER PANEL REPLACED AT NR 12 POSITION. 2 L 7 4 4F A20WE 2001021600093 20010216 00093 WP 2001 2 16 UPS01834789 1 20010122 A 5320 4753360501 FITTING DOUG DC8 DC871F 302199D WP CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, STA 822 RBL 63 INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 4753360, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001021600094 20010216 00094 WP 2001 2 16 UPS01834790 1 20010125 A 5730 576958929 DOUBLER DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, LEFT WING CENTER L/E INTERNAL DOUBLER IS CRACKED AT XFS 297.5. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769589, AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001021600095 20010216 00095 WP 2001 2 16 UPS01834791 1 20010127 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, LEFT WING L/E UPPER RIB IS CRACKED AT XFS 728.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001021600096 20010216 00096 WP 2001 2 16 UPS01834792 1 20010127 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, LEFT WING L/E UPPER RIB IS CRACKED AT XFS 741.250. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001021600097 20010216 00097 WP 2001 2 16 UPS01834793 1 20010127 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, LEFT WING L/E UPPER RIB IS CRACKED AT XFS 760. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001021600098 20010216 00098 WP 2001 2 16 UPS01834794 1 20010125 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, LEFT WING L/E LOWER RIB IS CRACKED AT XFS 828.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001021600099 20010216 00099 WP 2001 2 16 UPS01834795 1 20010125 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, LEFT WING L/E LOWER RIBS ARE CRACKED AT XFS 616.25, XFS 641.25, XFS 653.75. REPAIRED RIBS IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001021600100 20010216 00100 WP 2001 2 16 UPS01834796 1 20010125 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 835, XFS 828.75, XFS 822.5, XFS 816.25, XFS 803.75, XF S 797.5, XFS 785, XFS 766.25. REPAIRED RIBS IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001021600101 20010216 00101 WP 2001 2 16 UPS01834797 1 20010125 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, LEFT WING L/E UPPER RIBS ARE CRACKED AT XOLDI 6.225, XS 435.78, XS 442.185, XS 448.581, XS 466.651 . REPAIRED RIBS IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001021600102 20010216 00102 WP 2001 2 16 UPS01834798 1 20010124 A 5720 97532977 ANGLE DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, RIGHT WING CENTER L/E VERTICAL ATTACH ANGLE AT XS 520 IS CRACKED. REMOVED, FABRICATED, AND REPLAC ED ANGLE IAW DWG 9753297, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001021600103 20010216 00103 WP 2001 2 16 UPS01834799 1 20010121 A 5320 47516402 FITTING DOUG DC8 DC871F 302199D WP CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, STA 717 LONG 18L INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACE D FITTING IAW DWG 4751640, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001021600104 20010216 00104 WP 2001 2 16 UPS01834800 1 20010125 A 5730 576960039 DOUBLER DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, LEFT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 572.5. REMOVED, FABRICATED, AND REPLACED D OUBLER IAW DWG 5769600, AND SRM 51-1-20D, 51-1-21, AND REPAIRED CRACKED SKIN IAW EO DC8-5720-7767A. 2 L 7 4 4F RT 4A25 2001021600105 20010216 00105 WP 2001 2 16 UPS01834819 1 20010130 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:IN, EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK PER MM 33. OPS CK GOO D. 2 L 7 4 4F RT 4A25 2001021600106 20010216 00106 EU 2001 2 16 MALA010140 1 20010109 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 501XJ E2208 FOUND DURING C-CHECK, NR 3 SEAT RAIL HAS CORROSION BEYOND LIMITS, BETWEEN FRAMES 19 - 21A IAW EO A53026. MAINTENANCE RE PLACED NR 3 SEAT RAIL BETWEEN FRAMES 19 - 21A IAW EOA53026, SEE CONTINUATION CARDS 075432 AND 075450 FOR DETAIL. 2 H 7 4 4F RT A49EU 2001021600107 20010216 00107 EU 2001 2 16 MALA010141 1 20010109 A 5260 TRACK BAC 146 AVRO146RJ85A 1500097 EU AIRSTAIR CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 501XJ E2208 FOUND DURING C-CHECK, OUTBOARD AIRSTAIR RAIL HAS SURFACE CORROSION BEYOND LIMITS. REMOVED AND REPLACED OUTBOARD AIRSTA IR RAIL IAW SRM 51-43-00. MAINTENANCE REPLACED AIRSTAIR RAIL IAW SRM 51-43-00 AND IPC 52-60-02-20. 2 H 7 4 4F RT A49EU 2001021600108 20010216 00108 EU 2001 2 16 MALA010142 1 20010109 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 501XJ E2208 FOUND DURING C-CHECK, NR 4 SEAT RAIL HAS CORROSION BEYOND LIMITS. MAINTENANCE REPLACED NR 4 SEAT RAIL BETWEEN FRAMES 19 -21A IAW EO A53026. SEE CONTINUATION CARDS NR 075426 AND 075448 FOR DETAILS. 2 H 7 4 4F RT A49EU 2001021600109 20010216 00109 EU 2001 2 16 MALA010143 1 20010118 A 5753 SKIN BAC 146 AVRO146RJ85A 1500097 EU TE FLAP TAB SCRATCHED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 501XJ E2208 FOUND DURING C-CHECK, RT INBOARD FLAP TAB TOP SKIN HAS ABRASIONS. THE INBOARD FLAP TAB TOP SKIN WAS DAMAGED FROM CHAFIN G ON THE SPOILER TRAILING EDGE, MAINTENANCE RESKINNED RT I/B FLAP TAB IAW MESABA EO A57026. MAINTENANCE REPAIRED THE I/ B FLAP TAB TOP O/B SKIN IN ACCORDANCE WITH BAE REPAIR DRAWING HC579H9029. 2 H 7 4 4F RT A49EU 2001021600110 20010216 00110 EU 2001 2 16 MALA010144 1 20010118 A 5753 SKIN BAC 146 AVRO146RJ85A 1500097 EU TE FLAP TAB SCRATCHED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 501XJ E2208 FOUND DURING C-CHECK, LT I/B FLAP TAB TOP SKIN HAS ABRASIONS. RESKINNED LT I/B FLAP TAB IAW MESABA EO A57025. THE I/B FLAP TAB TOP SKIN WAS DAMAGED FROM CHAFING ON THE SPOILER TRAILING EDGE. MAINTENANCE REPAIRED THE I/B FLAP TAB TOP INBO ARD SKIN IN ACCORDANCE WITH BAE REPAIR DRAWING HC579H9006. 2 H 7 4 4F RT A49EU 2001021600111 20010216 00111 EU 2001 2 16 MALA010145 1 20010126 A 7933 4053T73P01 BULB SAAB SF340 SF340A 7850100 EU PROP OIL TEMP BURNED OUT A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 119XJ 119 RT PROPELLER OIL TEMPERATURE FLUCTUATES IN FLIGHT. FLUCTUATES FROM APPROXIMATELY 100 DEGREESTO 150 DEGREES CELSIUS. NO RMAL INDICATION ON GROUND. AIR TURNBACK TO DTW. MAINTENANCE REPLACED PGB TEMP BULB WITH SERVICEABLE IAW AMM PN ON/OFF 4053T73P01. OPS AND SECURITY CHECK GOOD AT THE TIME. 2 L 7 2 4T RT A52EU 2001021600112 20010216 00112 EU 2001 2 16 MALA010146 1 20010126 A 3010 6068T56P01 WARNING LIGHT SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ANTI ICE SYSTEM ILLUMINATED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 415XJ 340B415 RT AIR VALVE LIGHT ILLUMINATED IN FLIGHT. AIR TURNBACK TO DTW. MAINTENANCE REPLACED ANTI-ICEVALVE P/N 6068T56P01, S/N OFF GRTB7662, S/N ON GRTG1442, PER SF340AMM. PERFORMED OPS CHECK, ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T 4 T RT A52EU E8NE 2001021600113 20010216 00113 EU 2001 2 16 MALA010147 1 20010128 A 3020 CONNECTOR SAAB SF340 340B 7860101 EU LT ENGINE DIRTY A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 404XJ 340B404 LT INTAKE LIGHT ILLUMINATED AND CYCLED ON/OFF EVERY 10 SECONDS. ORH COMPLETED, NO HELP. PROBLEM CLEARED AFTER EXITING PRECIPITATION. MAINTENANCE CHECKED AND CLEANED CANNON PLUG CONNECTIONS ONON LT SHOEBOX. OPS CHECK GOOD IAW SF3 AMM 30- 20-00. 2 L 7 2 4T RT A52EU 2001021600114 20010216 00114 2001 2 16 RAIA00101029 4 20010130 A 3420 7003110901 INDICATOR JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 563HK 12709 2037 41079 5412-EWR- DURING TAXI OUT THE FIRST OFFICERS ELECTRONIC HORIZON SITUATION INDICATOR (EHSI) WENT BLANK. MAINTENANCE REMO VED AND REPLACED THE EHSI IAW J41 MAINTENANCE MANUAL. 2 L 7 2 4T RT A41NM 2001021600115 20010216 00115 NM 2001 2 16 F3LA200100012 1 20010126 A 3340 3002134 HOUSING BOEING 737 737228 13844AG NM EXTERIOR LIGHT CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 234TR 3086 23004 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON RT WING INSPECTION LIGHT HOUSING MATING SURFACE BETWEEN HOUSING AND F USELAGE SKIN. REPLACED RT WING INSPECTION LIGHT HOUSING PER SRM 51-30-02. 2 L 7 2 4F RT A16WE 2001021600116 20010216 00116 NM 2001 2 16 DHL2001740C07 1 20010116 A 5320 ANGLE BOEING 727 7272Q9 138448M NM FUSELAGE CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 HYD COMP B-SYS SUPPORT FRAME AT FWD SIDE OF ENTRY ACCESS HAS 2 CHAFE HOLES. INSTALLED ANGLE PER B727 SRM 51-40-3 PG 3 S IZE OF MATERIAL 6 X 3 INCHES. 2 L 7 3 4F RT A3WE 2001021600117 20010216 00117 NM 2001 2 16 DHL2001740C08 1 20010116 A 5315 FLOORBEAM BOEING 727 7272Q9 138448M NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AFT CARGO CROSS SECTION FLOOR ANGLE AT STA 950 HAS CORROSION AND TOO MANY DOUBLE HOLES. INSTALLED NEW ANGLE 50 X 4.75 I NCHES PER B727 SRM53-10-2 AND 51-30-2. 2 L 7 3 4F RT A3WE 2001021600118 20010216 00118 NM 2001 2 16 DHL2001740C09 1 20010109 A 5321 FLOORBOARD BOEING 727 7272Q9 138448M NM CABIN CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 CORROSION ON LOWER SURFACE OF CABIN FLOOR AT FS 1166 LBL 52. FABRICATED AND INSTALLED NEW FLOOR BOARD PER B727 SRM 51-3 0-2. MATERIAL USED 18 X 68 INCHES. 2 L 7 3 4F RT A3WE 2001021600119 20010216 00119 NM 2001 2 16 DHL2001740C10 1 20010109 A 5320 FLOOR SUPPORT BOEING 727 7272Q9 138448M NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 FLOOR SUPPORT ANGLE IS CORRODED BETWEEN STA 312 AND 328 RBL-4. INSTALLED NEW T-ANGLE FLOOR SUPPORT. MATERIAL USED 20 I NCHES. 2 L 7 3 4F RT A3WE 2001021600120 20010216 00120 NM 2001 2 16 DHL2001740C11 1 20010111 A 5320 FLOOR SUPPORT BOEING 727 7272Q9 138448M NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 CORROSION UNDER SEALING TAPE AT LAVATORY AREA FWD FROM BS 304 TO 343. REPLACED ANGLE. 2 L 7 3 4F RT A3WE 2001021600121 20010216 00121 NM 2001 2 16 DHL2001740C12 1 20010114 A 5730 SKIN BOEING 727 7272Q9 138448M NM RT WING TIP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 RIGHT WING TIP ASSY FWD INBOARD TOP CORNER HAS CRACKS. FABRICATE REPAIR PER B727 SRM 57-20-5, MATERIAL LOSS 4 X 2.5 INC HES. 2 L 7 3 4F RT A3WE 2001021600122 20010216 00122 NM 2001 2 16 DHL2001740C13 1 20010110 A 5246 BRACKET BOEING 727 7272Q9 138448M NM ACCESS DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 REFUELING BAY ACCESS DOOR HOLD OPEN LINKAGE ATTACH BRACKET IS CRACKED. REPLACED BRACKET PER B727 SRM 51-10-2, MATERIAL USED 9 X 2 X 1 INCHES. 2 L 7 3 4F RT A3WE 2001021600123 20010216 00123 NM 2001 2 16 DHL2001740C14 1 20010125 A 5754 ATTACH ANGLE BOEING 727 7272Q9 138448M NM NR 5 SLAT CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 NR 5 L/E SLAT I/B TRACK ROLLER SUPPORT O/B VERTICAL ATTACH ANGLE HAS CORROSION AT LOWER SPAR. INSTALLED NEW VERTICAL AT TACH ANGLE PER B727 SRM 57-10-2 AND 51-30-2. 2 L 7 3 4F RT A3WE 2001021600124 20010216 00124 NM 2001 2 16 DHL2001740C15 1 20010111 A 5753 FAIRING BOEING 727 7272Q9 138448M NM NR 5 FLAP TRACK CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 NR 5 FLAP TRACK FWD FAIRING CRACKED AND CHAFING AT SEVERAL SPOTS ALONG THE EDGE. REPAIRED PER B727 SRM 51-30-2. SIZE O F MATERIAL 13 X 1.5 INCHES. 2 L 7 3 4F RT A3WE 2001021600125 20010216 00125 NM 2001 2 16 DHL2001740C16 1 20010111 A 5753 FAIRING BOEING 727 7272Q9 138448M NM NR 5 FLAP TRACK TORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 NR 5 FLAP TRACK MID FAIRING SKIN TORN AT FWD END. REPLACED SKIN AT NR 5 FLAP TRACK MIN FAIRING PER B727 SRM 51-30-2 AND 51-10-2. SIZE OF MATERIAL 13 X 6 INCHES. 2 L 7 3 4F RT A3WE 2001021600126 20010216 00126 NM 2001 2 16 DHL2001740C17 1 20010115 A 5753 SKIN BOEING 727 7272Q9 138448M NM RT WING TE FLAP SPLIT A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 RIGHT WING OUTBOARD FLAP AFT FLAP T/E SPLITTING. INSTALLED BOND REPAIR PER B727 SRM 51-40-6. SIZE OF REPAIR 10 X 4 INC HES. 2 L 7 3 4F RT A3WE 2001021600127 20010216 00127 NM 2001 2 16 DHL2001740C18 1 20010109 A 5753 FAIRING BOEING 727 7272Q9 138448M NM NR 4 FLAP TRACK CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 NR 4 FLAP TRACK CENTER FAIRING CRACKED AT PREVIOUS REPAIR. REPAIRED TRACK FAIRING PER B727 SRM 51-30-2. SIZE OF REPAIR 7 X 3 INCHES. 2 L 7 3 4F RT A3WE 2001021600128 20010216 00128 NM 2001 2 16 DHL2001740C19 1 20010111 A 5753 FAIRING BOEING 727 7272Q9 138448M NM NR 4 FLAP TRACK CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 NR 4 FLAP TRACK FWD FAIRING CRACKED IN 2 PLACES. REPAIRED TRACK FAIRING PER B727 SRM 51-30-2. SIZE OF MATERIAL 19 X 2 INCHES. 2 L 7 3 4F RT A3WE 2001021600129 20010216 00129 NM 2001 2 16 DHL2001740C20 1 20010124 A 5711 ANGLE BOEING 727 7272Q9 138448M NM LT WING SPAR CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 LEFT WING FRONT SPAR LOWER CHORD ANGLE LOWER SECTION WHERE L/E PANELS ATTACH, CORROSION ON TWO SECTIONS APPROX BETWEEN W S 383.0 AND 477.0. FABRICATED AND INSTALLED REPAIR PLATE 18.375 X 2.875 INCHES. INSTALLED PER AVITAS EO AVHM-0186 RO-1 FORM 337 FILED BY AVBORNE. 2 L 7 3 4F RT A3WE 2001021600130 20010216 00130 NM 2001 2 16 DHL2001740C21 1 20010115 A 5754 SKIN BOEING 727 7272Q9 138448M NM LT WING LE FLAP DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 LEFT WING INBOARD FORE FLAP HAS DENT AT CENTER ACCESS PANEL 8442 MAKING CONTACT WITH NR 6 SPOILER ACTUATOR ROD END. INS TALLED NEW ACCESS PANEL PER B727 SRM 51-30-2. SIZE OF REPAIR 8 X 8 INCHES. 2 L 7 3 4F RT A3WE 2001021600131 20010216 00131 NM 2001 2 16 DHL2001740C22 1 20010118 A 5754 STRUCTURE BOEING 727 7272Q9 138448M NM LT WING LE FLAP GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 LEFT WING INBOARD FORE FLAP OUTBOARD END HAS DEEP GOUGE IN PREVIOUS REPAIR DOUBLER. INSTALLED DOUBLER PER B727 SRM 51-3 0-2. SIZE OF MATERIAL USED 5 X 6 INCHES. 2 L 7 3 4F RT A3WE 2001021600132 20010216 00132 NM 2001 2 16 DHL2001740C23 1 20010118 A 5330 PANEL BOEING 727 7272Q9 138448M NM FUSELAGE BULGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 EXTERIOR LOWER FUSELAGE, PANEL 3420 BULGE. INSTALLED NEW SKIN FUSELAGE PANEL NR 3420 PER B727 SRM 53-50-1 AND 51-30-2. SIZE OF MATERIAL USED 19.25 X 20.25 INCHES. 2 L 7 3 4F RT A3WE 2001021600133 20010216 00133 NM 2001 2 16 DHL2001740C24 1 20010117 A 5320 ANGLE BOEING 727 7272Q9 138448M NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 FOUND SMALL CRACK LOCATED AT A/C BAY AREA RAM AIR DOORS UPPER OUTBOARD CORNER AT BS 720B. REMOVED AND REPLACED UPPER AN GLE AT BS 720B PER B727 SRM 51-10-1, 5110-2 AND 51-30-2. SIZE OF ANGLE 1.5 X 29 INCHES. 2 L 7 3 4F RT A3WE 2001021600134 20010216 00134 EA 2001 2 16 JBXA000238 1 20010131 A 3234 601R50967 HANDLE CNDAIR CL600 CL6002B19 EA MLG DETACHED A JBXA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SO 05 591ML 7388 LANDING GEAR HANDLE FELL OFF IN HAND ON CLIMBOUT. REMOVED AND REPLACED IAW AMM 32-31-01. 2 L 7 2 4F RT A21EA 2001021600135 20010216 00135 2001 2 16 01FDEA00069 4 20010129 A 3441 WIRE BOEING 727 727233 138408A NM VERTICAL GYRO BROKEN A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 218FE 21101 RADAR STILL INOP. FOUND BROKEN WIRE BETWEEN F11 AT RT TO R68 U ON VERTICAL GYRO CONNECTOR D669. REMOVED AND REPLACED W IRE ACCORDANCE WITH BOEING WIRE STANDARD CHAPTER 20. OPS CK OK. 2 L 7 3 4F RT A3WE 2001021600136 20010216 00136 NM 2001 2 16 01FDEA00070 1 20010201 A 3220 656021123 ACCESSORY UNIT BOEING 727 727233 138408A NM E/E BAY MALFUNCTIONED A FDEA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 222FE 20933 NOSE GEAR UNSAFE. RECYCLE TWICE TO GET ALL DOWN. *S/D* REMOVED AND REPLACED PER MM 32-09-122-5, 32-33-000-5. JACKED AND LWR A/C PER MM 07-11-000-2. 2 L 7 3 4F RT A3WE 2001021600137 20010216 00137 EU 2001 2 16 QXEA0100083 1 20010130 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN BURNED OUT A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486US 11237 GEG- EMERGENCY EXIT SIGN FORWARD SIDE OF ROW 8 IS INOPERATIVE. REPLACED SIGN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNE D TO SERVICE. 2 L 7 2 4F RT A20EU 2001021600138 20010216 00138 NM 2001 2 16 ANCF200100006 1 20010130 A 3411 HOSE BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE ALTIMETER PITOT LEAKING W ANCF A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 23 535AW 25535 DURING CLIMB, PASSING 25,000 FT, THE STANDBY ALTIMETER SHOWED 17,000 FT AND THE AIRSPEED INDICATORS SHOWED 320 KNTS WHIL E THE STANDBY AIRSPEED INDICATOR SHOWED 220 KNTS. WITH 28,000 FT IN THE CAPTAIN AND F/O ALTIMETER THE STANDBY ALTIMETER SHOWED 18,000 FT. DURING THE T/O ROLL AT 80 KNTS CROSS CHECK ALL THREE-AIRSPEED INDICATIONS SHOWED THE SAME. CREW DEC IDED TO RETURN TO SKBO. PERFORMED LEAK TEST IAW AMM 34-11-00 PAGE 525, WITH PITOT STATIC TEST EQUIPMENT, FOUND LEAK AT STANDBY ALTIMETER STATIC HOSE. ADJUSTED IAW AMM 20-10-10 PAGE 401, PERFORMED LEAK TEST IAW AMM 34-13-00 PAGE 501/502 TA BLE 501, TESTS PASSED OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2001021600139 20010216 00139 NM 2001 2 16 QXEA0100082 1 20010131 A 3350 6104789 BATTERY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 355PH 5005 281 500 SEA- EMERGENCY FLOOR PATH LIGHTS, FORWARD RED SECTION INOPERATIVE. REPLACED FORWARD RED SECTION OF FLOOR PATH LIGHTS (8 2520999-001), POWER SUPPLY (60-3844-1) AND BATTERY PACK. EMERGENCY LIGHTS TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001021600141 20010216 00141 NM 2001 2 16 UPS01234824 1 20010201 A 2710 CONTROL CABLE BOEING 727 72725C 138400H NM AILERON LACK OF LUBE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE: IN, AILERON BINDING (REPEAT W/U). TROUBLESHOT PER MM 27-10-00 PAGE 111 INSP CABLE AA & AB NO DEFECT NO TED LUB CABLE, OPS CHECK GOOD. 2 L 7 3 4F A3WE 2001021600142 20010216 00142 WP 2001 2 16 UPS01834810 1 20010121 A 5320 47516251N FITTING DOUG DC8 DC871F 302199D WP CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, STA 680 LONG 11L INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 47 51625, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001021600143 20010216 00143 WP 2001 2 16 UPS01834811 1 20010128 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, LEFT WING L/E LOWER RIB IS CRACKED AT XFS 360. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001021600144 20010216 00144 WP 2001 2 16 UPS01834812 1 20010122 A 5340 37739061 FITTING DOUG DC8 DC871F 302199D WP CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, STA 717 LBL 24 FLOORBEAM ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3773906, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001021600145 20010216 00145 WP 2001 2 16 UPS01834813 1 20010122 A 5340 37552222 FITTING DOUG DC8 DC871F 302199D WP CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, STA 822 LBL 24 FLOORBEAM ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755222 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001021600146 20010216 00146 WP 2001 2 16 UPS01834814 1 20010122 A 5340 37739061 FITTING DOUG DC8 DC871F 302199D WP CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, STA 781 LBL 24 FLOORBEAM ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3773906, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001021600147 20010216 00147 WP 2001 2 16 UPS01834815 1 20010125 A 5730 576960035 DOUBLER DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, LEFT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 597.5. REMOVED, FABRICATED AND REPLACED DO UBLER IAW DWG 5769600, AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001021600148 20010216 00148 WP 2001 2 16 UPS01834816 1 20010121 A 5320 577384443 CLIP DOUG DC8 DC871F 302199D WP CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, STA 1766 LONG 6L INTERCOSTAL TO BULKHEAD ATTACH CLIP IS CORRODED BEYOND LIMITS. REMOVED, FABRICAT ED AND REPLACED CLIP IAW DWG 5773844, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001021600149 20010216 00149 WP 2001 2 16 UPS01834817 1 20010123 A 5753 RIB DOUG DC8 DC871F 302199D WP TE FLAPS CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, RIGHT INBOARD FLAP RIB IS CRACKED AT AFT SPAR MOST I/B RIB AT XCW 64. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001021600150 20010216 00150 WP 2001 2 16 UPS01834818 1 20010121 A 5320 575503281 FLOOR SUPPORT DOUG DC8 DC871F 302199D WP CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, STA 1717 TO 1725 LBL 10 FLOOR SUPPORT IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED SUPPORT IAW DWG 5755032 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001021600151 20010216 00151 WP 2001 2 16 DHL2001803002 1 20010119 A 3250 CONTROL BOX DOUG DC8 DC873F 302199F WP NLG STEERING MALFUNCTIONED A DHLA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 803DH 46123 NOSE WHEEL STEERING UNRESPONSIVE DURING START OF TAKEOFF ROLL. REJECTED T/O. INSPECTED NOSE AND MAIN GEAR, NO DISCREPA NCIES FOUND. OPERATED NOSE WHEEL STEERING, OPS CHECKS OK IAW 32-50-0. SUSPECT RUNWAY CONDITIONS. A/C OK FOR SERVICE. 2 L 7 4 4F RT 4A25 2001021600152 20010216 00152 WP 2001 2 16 DHL2001807006 1 20010119 A 3250 GUARD DOUG DC8 DC873 302199C WP NLG STEERING SYS LOOSE A DHLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 807DH 45990 TAKEOFF ABORTED DURING INITIAL T/O ROLL DUE TO LOSS OF CONTROL. NO RESPONSE WITH NOSE WHEEL. INSPECTED NOSE WHEEL STEE RING SYSTEM, FOUND CABLE PULLEY GUARD LOOSE AND RUBBING CABLE. RESECURED CABLE PULLEY GUARD, SYSTEM OPS CHECKS GOOD IAW 32-51-0. 2 L 7 4 4F RT 4A25 2001021600153 20010216 00153 NM 2001 2 16 TWAA0102001 1 20010131 A 3350 417N5206 SIGN BOEING 757 757231 1384950 NM CABIN MISSING A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 709TW 28168 THE EMERGENCY EXIT SIGN WAS MISSING FROM THE CEILING BY THE OVERWING EXITS. RE-INSTALLED LIGHT ASSEMBLY. CHECK-C 5-3-0 0 LAX. 2 L 7 2 4F RT A2NM 2001021600154 20010216 00154 WP 2001 2 16 TWAA0102002 1 20010201 A 3350 58531 LEAD DOUG DC9 DC983 3022083 WP CABIN WORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 931TW 49527 THE EGRESS LIGHTS WERE INOPERATIVE AT STATION 895 TO 1125. REPLACED THE POWER SUPPLY LEAD. CHECK-C 12-28-2000 STL. 2 L 7 2 4F RT A6WE 2001021600155 20010216 00155 NM 2001 2 16 TWAA0102003 1 20010131 A 5210 80330035 BOTTLE BOEING 757 757231 1384950 NM DOOR ASSIST DISCHARGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 718TW 28486 THE LEFT SIDE FWD CABIN DOOR ASSIST BOTTLE PRESSURE WAS ZERO. REPLACED THE ASSIST BOTTLE. CHECK-C 11-1-00 LAX. 2 L 7 2 4F RT A2NM 2001021600156 20010216 00156 WP 2001 2 16 TWAA0102004 1 20010131 A 2612 H05A003510 WARNING SYSTEM DOUG DC9 DC983 3022083 WP CAWS FALSE ACTIVATION A TWAA F E ACTIVATE FIRE EXT. ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 CE 05 9617R 53564 3261 IN FLIGHT THE RT ENGINE FIRE WARNING GIVE VISUAL AND AURAL SIGNAL. REDUCED THROTTLE TO IDLE, NO HELP. SHUT DOWN ENGINE AND FIRED BOTH BOTTLES, STILL NO HELP. LANDED AT SCHEDULED STATION, SJU. FOUND THE CENTRAL AURAL WARNING SYSTEM (CAWS ) AT FAULT FOR ERRONEOUS INDICATION, AND REPLACED SAME. ALSO REPLACED BOTH ENGINE FIRE WARNING LOOPS PRECAUTIONARY, AND THE UNITS NECESSARY TO RESTORE THE FIRE EXTINGUISHING SYSTEM. CHECK-C 10-8-00 JFK. 2 L 7 2 4F RT A6WE 2001021600157 20010216 00157 WP 2001 2 16 TWAA0102005 1 20010131 A 2420 976J2528 GENERATOR DOUG DC9 DC982 3022082 WP LEFT MALFUNCTIONED A TWAA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 CE 05 919TW 49368 AT FL 330 CAPT INSTRUMENTS WENT DEAD AND FLT GUIDANCE CONTROL PANEL FROZE. LT AND RT GEN VOLTS AND FREQS NORMAL. MADE UNSCHEDULED LANDING AT TPA. AFTER LANDING NOTICED LT CSD TEMP WAS LOW. TURNED OFF LT GEN AND INDICATIONS RETURNED TO N ORMAL. REPLACED THE LT GEN. ALSO REPLACED PRECAUTIONARY THE RT DC BUS SENSING RELAY P/N 9227-10127, THE LT GENERATOR C ONTROL UNIT P/N 947F945-3, AND THE DC EMERGENCY POWER TRANSFER RELAY P/N EP-410. CHECK-C 5-12-00 MCI. 2 L 7 2 4F A6WE 2001021600158 20010216 00158 NM 2001 2 16 DHL2001712002 1 20010121 A 3510 FITTING BOEING 727 72729 1384007 NM OXYGEN BOTTLE LEAKING A DHLA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 712DH 19401 O2 PSI DROPPED FROM 1450 TO 200 DURING CRUISE FLIGHT. SERVICED CREW O2 FROM 200 PSI TO 1750 PSI. PERFORMED LEAK CHECK AND FOUND A LEAKING FITTING IN E&E BAY. TIGHTENED AND LEAK CHECKED GOOD IAW MM 12-15-11. OK TO CONTINUE. 2 L 7 3 4F A3WE 2001021600159 20010216 00159 EU 2001 2 16 DHL2001366006 1 20010125 A 2751 615500014 INDICATOR AIRBUS 300 A300B4203 3930306 EU TE FLAPS UNSERVICEABLE A DHLA O OTHER O OTHER AP APPROACH 1 SO 01 366DH 249 DURING APPROACH TRAILING EDGE FLAP POSITION INDICATOR FAILED TO DISPLAY FLAP POSITION. REPLACED FLAP/SLAT POSITION INDI CATOR IAW 27-55-11, OPS CHECK NORMAL. 2 L 7 2 4F RT A35EU 2001021600160 20010216 00160 EU 2001 2 16 DHL2001362003 1 20010130 A 5270 WARNING LIGHT AIRBUS 300 A300B4103 3930104 EU E/E BAY DOOR ILLUMINATED A DHLA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 362DH 84 DOORS LIGHT ILLUMINATED ON MWP DURING TAXI OUT. NO INDICATION ON S/O PANEL. E&E COMPARTMENT LT DOOR HANDLE RESET, OPS CHECK GOOD PER MM 52-11-14. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2001021600161 20010216 00161 NM 2001 2 16 F3LA200100015 1 20010121 A 5310 SHEAR TIE BOEING 737 737228 13844AG NM CARGO BAY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 234TR 3086 23004 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON SHEAR TIE AT STA 500A BETWEEN STR 27L AND 26L. FABRICATED AND INSTAL LED REPLACEMENT SHEAR TIE PER SRM 53-10-2, SRM 53-10-4, SRM 51-30-2 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2001021600162 20010216 00162 EU 2001 2 16 DHL2001364009 1 20010201 A 3241 DSF002011 SENSOR AIRBUS 300 A300B4203 3930306 EU NLG UNSERVICEABLE A DHLA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 364DH ANTI-SKID OFF LIGHT ILLUMINATED, ALL RELEASE LIGHTS OUT. PROXIMITY DETECTOR 55GB ON NLG. ANTI-SKID CHECKS NORMAL IAW M M 32-42-00. 2 L 7 2 4F RT A35EU 2001021600163 20010216 00163 CE 2001 2 16 GLBA2001017 1 20010127 A 3010 TUBE BEECH 1900 1900D 1154162 CE LT WING DAMAGED A GLBA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 CE 01 210UX UE210 RETURN TO BLOCK - LEFT BLEED AIR FAIL, REPAIRED EVA TUBING LEFT I/B WING OPS CHECKED SYSTEM GOOD. 2 L 7 2 4T RT A24CE 2001021600164 20010216 00164 WP 2001 2 16 AT01000019 1 20010106 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSLEAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FOUND FLOOR SUPPORT CORRODED BEYOND LIMITS AT BS 198 LBL 0 - LBL 51. REPLACED FLOOR SUPPORT IAW DC9 SRM 51-30-03, 51-30 -05, 51-10-04, AND 53-11-01 FIG 13. 2 L 7 2 4F A6WE 2001021600167 20010216 00167 WP 2001 2 16 AT0100020 1 20010106 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FOUND CABIN FLOOR PANEL SUPPORT AT BS 200 RBL 0 - RBL 51 CORRODED BEYOND LIMITS. REPLACED FLOOR SUPPORT IAW DC9 SRM 51- 20-05, 51-10-04, 51-10-02, AND 53-11-01 FIG 12. 2 L 7 2 4F A6WE 2001021600168 20010216 00168 WP 2001 2 16 AT0100021 1 20010106 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP CABIN CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FOUND CORROSION ON FLOOR PANEL BS 180 RBL 0 - RBL 44 BEYOND LIMITS. FABRICATED AND INSTALLED DOUBLERS IAW DC9 SRM 51-30 -08 AND 53-01 FIG 4. 2 L 7 2 4F A6WE 2001021600190 20010216 00190 WP 2001 2 16 AT0100044 1 20010112 A 5713 STRINGER DOUG DC9 DC932 3022066 WP RT WING CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FOUND RIGHT WING TANK XCW 58.6 CORRODED BEYOND LIMITS. INSTALLED REPAIR STRAP ON STRINGER 22 IAW DC9 SRM 57-08 FIG 2. 2 L 7 2 4F A6WE 2001021600191 20010216 00191 WP 2001 2 16 AT0100046 1 20010106 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FOUND FLOOR SUPPORT ANGLE AT BS 180 RBL 0-44 CORRODED BEYOND LIMITS. FABRICATED AND REPLACED ANGLE IAW DC9 SRM 51-10-03 , 51-30-05, AND 53-01 FIG 1. 2 L 7 2 4F A6WE 2001021600192 20010216 00192 WP 2001 2 16 AT0100047 1 20010114 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP CABIN CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FOUND FLOOR PANEL 97 CORRODED BEYOND LIMITS. REPAIRED FLOOR PANEL IAW DC9 SRM 53-05, 53-21, 51-10-03, AND MM 53-20-01. 2 L 7 2 4F A6WE 2001021600193 20010216 00193 WP 2001 2 16 AT0100040 1 20010129 A 2530 COFFEEMAKER DOUG DC9 DC932 3022066 WP GALLEY ODOR A ZZDA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 15 801AT 47275 FOUND ACRID BURNING SMELL IN COCKPIT AND FORWARD FLIGHT ATTENDANT STATION. FOUND BURNT COFFEE GROUNDS ON FORWARD COFFEE MAKER. CLEANED BURNT GROUNDS, NO SMELL NOTED. ALSO CHECKED E&E COMPARTMENT, FORWARD CARGO COMPARTMENT AND FORWARD FLI GHT ATTENDANT STATION. NO BURNT ODOR DETECTED IAW DC9 MM 25-30. 2 L 7 2 4F A6WE 2001021600194 20010216 00194 NM 2001 2 16 F3LA200100016 1 20010121 A 5320 STRAP BOEING 737 737228 13844AG NM CARGO BAY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 234TR 3086 23004 DURING C-7 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR NUT PLATE STRAP AT STA 770 CORRODED. REPLACED STRAP P ER SRM 51-10-2. 2 L 7 2 4F RT A16WE 2001021600195 20010216 00195 NM 2001 2 16 F3LA200100013 1 20010130 A 7711 LG80A6 TRANSMITTER BOEING 737 7372Y5 1384554 NM NR 1 ENGINE READS LOW A F3LA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 118RW 1170 23040 AIR TURNBACK. FLIGHT CREW REPORTED NR 1 ENGINE ANTI-ICE VALVES INDICATED OPEN ON OVERHEAD PANEL. AT CLIMB POWER, NR 1 ENGINE EPR AT APPROXIMATELY 87 PERCENT AND NR 2 ENGINE EPR AT 90 PERCENT. REPLACED NR 1 ENGINE EPR TRANSMITTER PE R MM 77-11-21. PERFORMED ENGINE RUN PER MM 71-09-236, PAGE 206, AND FOUND TO BE WITHIN LIMITS. 2 L 7 2 4U RT A16WE 2001021600196 20010216 00196 NM 2001 2 16 AWXA0001259 1 20010129 A 5311 65163008687 FRAME BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 167AW 23628 STA 178 BULKHEAD SKIN CRACKED IN 2 PLACES, INTERCOSTALS (2) CRACKED AT SIDE CHORDS, AND SIDE CHORDS CRACKED AT 3 PLACES STA 178 WL 184 TO 207 LBL 45.50 TO RBL 45.50. REPAIRED PER EO 53-12-07. 2 L 7 2 4F RT A16WE 2001021600197 20010216 00197 NM 2001 2 16 F3LA200100014 1 20010130 A 7711 6546858172 LINE BOEING 737 7372Y5 1384554 NM NR 1 ENGINE DAMAGED A F3LA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 118RW 1170 23040 AIR TURNBACK. FLIGHT CREW REPORTED ON CLIMBOUT WITH EPR SET AT 2.20, THE NR 1 ENGINE N1 WAS APPROXIMATELY .7 LOW. NR 1 EGT WAS APPROXIMATELY 40 LOW, N2 APPROXIMATELY .5 LOW AND FUEL FLOW 800LB LOW. WHEN THROTTLES WERE MATCHED AND ALL OTH ER ENGINE GAUGES MATCHED, THE NR 1 EPR WAS HIGH. PERFORMED EPR SYSTEM TEST PER MM 77-11-00 AND FOUND DAMAGED PT2 SENSE LINE. REPLACED PT2 SENSE LINE PER MM 20-10-51. PERFORMED ANOTHER EPR SYSTEM TEST PER MM 77-11-00 AND SYSTEM CHECKED GO OD. PERFORMED RIG CHECK OF THRUST REVERSERS AND THROTTLES PER MM 76-11-00 AND CHECKED OK. PERFORMED ENGINE RUN TRIM CH ECK PER MM 71-00-00 AND CHECKED TO STATED VALUES. ALSO REPAIRED DAMAGED WIRING TO NR 1 ENGINE FWD BOOST PUMP PER. 2 L 7 2 4U RT A16WE 2001021600198 20010216 00198 SO 2001 2 16 SWIA972309 1 20010124 A 3010 PRESSURE SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE DEICE SYSTEM FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 560SW 120334 MIDDLE LEFT DEICE INOP INFLIGHT. DIVERTED TO FAT FROM VIS. REPLACED LEFT MIDDLE DEICE BOOT PRESSURE SWITCH AND PATCHED SMALL HOLE IN BOOT. OPS CHECKS GOOD. P/N ON: 211C117-183, S/N ON: N735, S/N OFF: 088D10021A. 2 L 7 2 4T 4 T RT A31SO E20NE 2001021600200 20010216 00200 SO 2001 2 16 SWIA972311 1 20010125 A 3260 DOWNLOCK SENSOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NLG FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 251YV 120251 SELECTING GEAR UP NOSE INDICATION WAS A GREEN, B RED. WHEN CYCLING TO GEAR DOWN INDICATION - LEFT: A & B RED, NOSE: B R ED, A GREEN, RIGHT; A&B RED. AFTER 5 MINUTES GEAR DROPPED BY ITSELF AND 6 GREEN LIGHTS. REPLACED DOWNLOCK PROX SENSOR FOR A-SYSTEM ON THE NOSE GEAR. PERFORMED GEAR SWING. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001021600201 20010216 00201 NM 2001 2 16 DHL2001740C25 1 20010109 A 5330 SKIN BOEING 727 7272Q9 138448M NM AFT FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AFT AIRSTAIRS CUTOUT EXTERNAL SKIN HAS A CRACK AT FWD CORNER. STOP DRILL CRACK AT AFT AIRSTAIRS CUTOUT EXTERNAL SKIN AS PER SRM 51-10-1. REMOVED FASTENERS FOR INSTALL DOUBLER AS PER SRM 51-30-2. INSP IAW B727NDT MANUAL PART 6-51-00-00 FI G 4, FOUND NO CRACKS BEYOND STOP HOLE. INSTALLED DOUBLER MATERIAL 2024T3, .063 7 X 3 INCH LOT N 507B71966, PO 8315343 A T AFT AIRSTAIRS CUTOUT EXTERNAL SKIN AS PER SRM 51-10-2. APPLIED ALODINE AND PRIME 51-10-2. 2 L 7 3 4F RT A3WE 2001021600202 20010216 00202 NM 2001 2 16 DHL2001740C26 1 20010117 A 5330 SKIN BOEING 727 7272Q9 138448M NM FUSELAGE TORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 MAIN CARGO DOOR CUTOUT FWD LOWER CORNER IS TORN BY DOOR SILL. REMOVED DOOR CUTOUT FWD LOWER CORNER SILL IAW B727SRM-51- 30-2. FABRICATE AND INSTALLED NEW WEB AT MAIN CARGO DOOR FWD LOWER CUTOUT AS PER B727 SRM 53-10-2 FIG 5 AND 51-30-2. M AT USED 7075T6 .063 16 X 6 INCH, LOT 57301724, PO 93774772. ALODINED AND PRIMED AS PER B727 SRM 51-10-2. INSTALLED NEW SCUFF PLATE AT MAIN CARGO DOOR FWD LOWER CUTOUT AS PER B727 SRM 53-10-2, FIG 5 AND 51-30-2. P/N AE2361-13. SEALED WIT H PRC AS PER SRM 51-20-4. 2 L 7 3 4F RT A3WE 2001021600203 20010216 00203 NM 2001 2 16 DHL2001740C28 1 20010116 A 3240 BRACKET BOEING 727 7272Q9 138448M NM LT MLG VALVE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 LEFT MLG W/W PARKING BRAKE SHUTTLE VALVE MOUNT BRACKET CRACKED AT STATION 930 AT KEEL BEAM. REMOVED VALVE FOR S/M REPAI R BRAKE IAW B727 M/M 32-40-0 LT TO W/W. REMOVED DAMAGED MOUNT BRACKET FOR LT MLG PARKING BRAKE SHUT OFF VALVE AND FABRI CATED REPLACEMENT IAW B727 SRM 51-10-2, MAT USED 2024T3 .040 13 X 6 INCH, LOT 1012582, PO 8319615 PER B727 SRM 53-10-2 F IG 5. INSTALLED MOUNT BRACKET FOR PARKING BRAKE SHUT OFF VALVE AT LT MLG WHEEL WELL PER B727 SRM 51-30-2. INSTALLED BR AKE VALVE LT WHEEL WELL AS PER B727 MM 32-40-0. OPS AND LEAK CHECKS GEAR SWING IN LT MLG GOOD AS PER B727 MM 32032-0 AN D BRAKE SYSTEM PARKING. 2 L 7 3 4F RT A3WE 2001021600204 20010216 00204 NM 2001 2 16 DHL2001740C27 1 20010116 A 5320 FLOOR SUPPORT BOEING 727 7272Q9 138448M NM CARGO BAY CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AFT CARGO STA 950A RBL 4 FLOOR SUPPORT ANGLE HAS CORROSION AND DOUBLE HOLES. ROUTED OUT CORROSION AND DOUBLE HOLES AT S TA 950A FLOOR SUPPORT B727 SRM 51-40-4. INSTALLED ANGLE REPAIR AT FS 950A RBL 4 FLOOR SUPPORT AS PER B727 SRM 51-40-21, PO 8318692, LOT 74758/01. ALODINE AND PRIME AREA AS PER B727 SRM 51-10-2. MAT LOSS .035 FOUND OUT OF LIMITS. REPAIR SIZE 1 X 1 X 14 INCH. 2 L 7 3 4F RT A3WE 2001021600205 20010216 00205 NM 2001 2 16 ABXA0100027 1 20010131 A 3260 WARNING LIGHT BOEING 767 767231 1385131 NM MLG FALSE INDICATION A ABXA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 707AX 22570 A DISAGREE MESSAGE WAS DISPLAYED AND A GEAR AMBER LIGHT ILLUMINATED WITH A GEAR GREEN DOWN INDICATION LIGHT. RECYCLED L ANDING GEAR AND INDICATIONS WERE NORMAL. MAINTENANCE INSPECTED AND PERFORMED A BITE CHECK. THE CHECK SHOWED NR 1 AND 2 GEAR LEVER SWITCH ON PSEU. MAINTENANCE CHECKED THE LANDING GEAR CONTROL MODULE IAW B767 MAINTENANCE MANUAL 32-31-01. NO DEFECTS WERE FOUND. 2 L 7 2 4F RT A1NM 2001021600206 20010216 00206 2001 2 16 0100255513 4 20010127 A 3417 4040800906 ADC BOEING 757 757251 1384970 NM LEFT INOPERATIVE A NWAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 01 513US 23201 ABORTED TAKEOFF AT 110 KNOTS DUE TO NO INDICATION ON CAPTAINS AIRSPEED INDICATOR. MAINTENANCE REPLACED THE LEFT AIR DAT A COMPUTER. AIRSPEED INDICATION CHECKED OK. 2 L 7 2 4F RT A2NM 2001021600207 20010216 00207 NM 2001 2 16 0100265503 1 20010126 A 3350 6012113RF POWER SUPPLY BOEING 757 757251 1384970 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 503US 23192 WHILE POWERING DOWN AIRCRAFT FOR OTHER MAINTENANCE, FOUND FLOOR ROWS 23 TO 33 FLOOR EMERGENCY LIGHTS INOPERATIVE. MAINT ENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A2NM 2001021600208 20010216 00208 NM 2001 2 16 0100275521 1 20010124 A 3350 6012113RF POWER SUPPLY BOEING 757 757251 1384970 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 521US 23209 DURING LINE CHECK, FOUND EMERGENCY LIGHTS AT DOORS 2L, 2R, AND FLOOR TRACK INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY M9002. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A2NM 2001021600209 20010216 00209 NM 2001 2 16 0100286311 1 20010129 A 2530 OVEN BOEING 747 747451 1384940 NM NR 2 CONTAMINATED A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 671US 26477 DURING CRUISE, NOTICED A STRONG ELECTRICAL SMELL IN UPPER DECK GALLEY AND DIMINISHED WHEN LIGHTS WERE TURNED OFF. MAINT ENANCE INSPECTED AREA AND FOUND PLASTIC MELTED ON NR 2 OVEN. CLEANED AND REMOVED RESIDUE. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001021600210 20010216 00210 2001 2 16 DHL2001807007 4 20010201 A 3422 GYRO DOUG DC8 DC873 302199C WP COCKPIT STUCK A DHLA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 807DH 45990 F/O ON AUX GYRO WAS STICKING DURING TURN WITH NUMEROUS FLAGS SEEMED TO WORK OK AFTER BEING ON FOR 20 MINUTES. REMOVED A ND REPLACED SWITCHING UNIT AND OPS CHECK GOOD THE HORIZON SYSTEM PER DC-8 MM 34-25-0. 2 L 7 4 4F RT 4A25 2001021600211 20010216 00211 WP 2001 2 16 SABA010004 2 20010130 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE331* 01514 WP LEFT MALFUNCTIONED A SABA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 33 964AE 964 11426 ON TAKEOFF ROLL AT CLT, THE LEFT ENGINE TORQUE WAS ONLY 92 PERCENT. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GA TE WITH NO OTHER PROBLEMS. MAINTENANCE PERFORMED A GROUND RUN OF THE LEFT ENGINE. ALL INDICATIONS WERE NORMAL PER THE MAINTENANCE MANUAL. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 3 T RT A56EU E2WE 2001021600212 20010216 00212 NM 2001 2 16 AWXA0001256 1 20010124 A 2133 6774E010000 OUTFLOW VALVE AIRBUS A319 A319132 NM IAE V2524 V2524A5 NE CABIN PRESSURE MALFUNCTIONED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 822AW 57 1410 V10884 CMH-DIVERTED FLIGHT- ON CLIMBOUT THE CABIN PRESSURE RATE FLUCTUATED FROM -600 FPM TO +1400 FPM. PRESSURIZATION SYSTEM 1 FAILED. AUTO SWITCH TO SYSTEM 2 AND CABIN PRESSURE FLUCTUATIONS CONTINUED. THE OUTFLOW VALVE CYCLED CONTINOUSLY, EVEN IN LEVEL FLIGHT AT FL 280. THE BLEED PAGE SHOWED N1 PACK PRESSURE PULSING BETWEEN 8 PSI AND 26 PSI. WITH NR 1 PACK OF F THE CABIN STABILIZED AND THE AIRCRAFT DIVERTED TO CMH. IN CMH MX REPLACED THE CABIN OUTFLOW VALVE AND OPERATIONAL CHE CKS WERE GOOD. ON A SUBSEQUENT FLIGHT THE SAME DISCREPANCY WAS REPORTED AND THE CREW OPENED THE CROSSBLEED AND TURNED T HE NR 1 BLEED OFF AND THE SYSTEM OPERATED NORMAL. IN PHX MAINTENANCE TROUBLESHOT THE PROBLEM. 2 L 7 2 4F 4 F RT A28NM E40NE 2001021600213 20010216 00213 EU 2001 2 16 QXEA0100084 1 20010131 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN BURNED OUT A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US 11161 PDX- THE FORWARD, MIDDLE AND AFT EMERGENCY EXIT SIGNS HAVE SEVERAL BURNED OUT BULBS. REMOVED AND REPLACED SIGNS. OPERA TIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001021600214 20010216 00214 NM 2001 2 16 QXEA0100085 1 20010201 A 3350 6104781 BATTERY PACK DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 369PH * 340 513 SEA- MOST FORWARD RED FLOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED 3352 PS2 BATTERY PACK. OPERATIONAL CHECK GOOD. AIR CRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001021600215 20010216 00215 NM 2001 2 16 QXEA0100086 1 20010131 A 3350 6104781 BATTERY GRIMES DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 824PH 4449 54 636 157 SEA- FORWARD 2 EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY AND POWER SUPPLY AT PS-2. OPERAT IONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001021600216 20010216 00216 NM 2001 2 16 CALA0100086 1 20010131 A 5320 FLOOR SUPPORT BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14383 26312 INSPECTION FOUND A .5 INCH CRACK IN FLOOR SUPPORT AT STA 540, RBL 1. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001021600217 20010216 00217 NM 2001 2 16 CALA0100087 1 20010131 A 5320 FLOOR SUPPORT BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14383 26312 INSPECTION FOUND A .5 INCH CRACK IN FLOOR SUPPORT AT STA 540, LBL 1. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001021600218 20010216 00218 WP 2001 2 16 CALA0100088 1 20010201 A 5320 FITTING DOUG DC9 DC982 3022082 WP LT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND A 1 INCH CRACK IN LEFT W/W FORWARD I/B (FWD OF MLG ATTACH) ANGLE T-FITTING. THE FITTING WAS REMOVED AN D A NEW FITTING WAS INSTALLED IAW SRM 51-30-05 AND 51-30-3. 2 L 7 2 4F A6WE 2001021600219 20010216 00219 NM 2001 2 16 CALA0100089 1 20010201 A 3397 WIRE BOEING 737 737524 1384721 NM EMER LIGHTS LOOSE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 18622 27526 THE L-1 DOOR OVERHEAD EMERGENCY LIGHT FAILED TO ILLUMINATE DURING EMERGENCY LIGHT CHECK. MAINTENANCE FOUND NUT ON GROUN D LUG AT GROUND 622 BACKED OFF AND GROUND WIRE LOOSE. REPLACED NUT AND TIGHTENED. ALSO REPLACED DAMAGED PIN ON LIGHT A SSEMBLY. 2 L 7 2 4F RT A16WE 2001021600220 20010216 00220 WP 2001 2 16 CALA0100090 1 20010201 A 5320 FLOOR SUPPORT DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13088 46850 INSPECTION FOUND LT AND RT FLOOR SUPPORT BEAMS CORRODED IN GALLEY G5 AREA AT STA 775-899, X = 40R AND AT X = 40L. THE F LOOR SUPPORT BEAMS WERE REMOVED AND NEW FLOOR SUPPORT BEAMS WERE INSTALLED IAW SRM 53-13-01 AND GMM 10-900-01. 2 L 7 3 4F A22WE 2001021600221 20010216 00221 NM 2001 2 16 CALA0100091 1 20010201 A 5330 PANEL BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17620 27333 INSPECTION FOUND ABB LT TRANSITION PANEL CORRODED AT STA 727 - 947.5. THE CORRODED SECTION WAS REMOVED AND A NEW SECTIO N WAS INSTALLED IAW SRM 53-60-53, FIGURE 204. 2 L 7 2 4F RT A16WE 2001021600222 20010216 00222 NM 2001 2 16 CALA0100092 1 20010201 A 5320 FLOOR SUPPORT BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13624 27528 INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 907 - 927, RBL 17, STA 927 - 947.5, RBL 17, STA 947 - 967, LBL 17, AND A T STA 967 - 986,5, LBL 17. THE FLOOR SUPPORTS WERE REPLACED IAW SRM 51-10-2 AND ECRA 5310-03585. 2 L 7 2 4F RT A16WE 2001021600223 20010216 00223 2001 2 16 CALA0100093 4 20010201 A 2565 GIRT BAR BOEING 737 737524 1384721 NM ESCAPE SLIDE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13624 27528 INSPECTION FOUND L-1 DOOR ESCAPE SLIDE FORWARD AND AFT GIRT BAR SUPPORTS CORRODED AT STA 312 AND STA 344. THE GIRT BAR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 2001021600224 20010216 00224 NM 2001 2 16 CALA0100094 1 20010202 A 5311 BELTFRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17620 27333 INSPECTION FOUND A 2.5 INCH CRACK IN BELT FRAME AT STA 787, RBL 27. THE BELT FRAME WAS REPAIRED IAW SRM 51-70-11. 2 L 7 2 4F RT A16WE 2001021600225 20010216 00225 WP 2001 2 16 CALA0100095 1 20010202 A 5320 FLOOR SUPPORT DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13088 46850 INSPECTION FOUND FLOOR SUPPORT ON RT SIDE OF FORWARD CARGO COMPARTMENT CORRODED AT STA 879. THE FLOOR SUPPORT WAS REMOV ED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 53-12-01. 2 L 7 3 4F A22WE 2001021600226 20010216 00226 NM 2001 2 16 RAAA01B216 1 20010126 A 5330 SKIN BOEING 727 72722C 138400F NM FUSLAGE DAMAGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED B3 MAINTENANCE CHECK INSPECTED EXISTING REPAIR PER REPAIR ASSESSMENT PROCESS. REMOVED ORIGINAL REPAIR AND INSTALLED NEW REPAIR PER ENGINEERING REPAIR PLAN AND RAA ECO ECO 2001-001 AND PLAN NR TASS - ERP -01-0021 M54 87. 2 L 7 3 4F A3WE 2001021600227 20010216 00227 EU 2001 2 16 MALA010148 1 20010128 A 3610 LINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE AIR VALVE LOOSE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 106XJ 106 DURING CLIMBOUT OF DTW, LT AIR VALVE LIGHT ILLUMINATED. AIR TURNBACK TO DTW. MAINTENANCE FOUND LINE LOOSE ON LT AIR VA LVE AND LOOSE C-CLAMP, TIGHTENED LINE AND CLAMPS AND OPS CHECK IAW SF340 MM CHAP 76. ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2001021600228 20010216 00228 EU 2001 2 16 MALA010149 1 20010129 A 7720 CONNECTOR SAAB SF340 340B 7860101 EU NR 2 ENGINE LOOSE A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 410XJ 410 NR 2 ITT FLUCTUATING BOTH READOUTS. RT ENGINE ITT NEEDLE AND NUMBERS ARE BOUNCING 75-100 DEGREES. ALL OTHER ENGINE PAR AMETERS ARE NORMAL. AIR TURNBACK TO DTW. MAINTENANCE FOUND YELLOW HARNESS (ITT INDICATION) CANNON PLUG LOOSE AT ECU. TIGHTENED AS NEEDED, ALL CHECKS GOOD WITH ENGINE RUN. 2 L 7 2 4T RT A52EU 2001021600229 20010216 00229 EU 2001 2 16 MALA010150 1 20010130 A 2612 SMOKE DETECTOR SAAB SF340 SF340A 7850100 EU E/E BAY FALSE INDICATION A MALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 15 89XJ 089 AVIONICS SMOKE MASTER WARNING LIGHT CAME ON AT APPROXIMATELY 80 KTS, FOR 2-3 SECONDS AND WENT BACK OUT. ABORTED TO. MA INTENANCE DEFERRED AVIONIC RACK SMOKE DETECTING SYSTEM IAW MEL 26-13-2 (B). 2 L 7 2 4T RT A52EU 2001021600230 20010216 00230 EU 2001 2 16 MALA010151 1 20010130 A 3260 UPLOCK SENSOR BAC 146 AVRO146RJ85A 1500097 EU MLG BINDING A MALA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 526XJ E2351 GEAR INTRANSIT LIGHT ILUMINATED AFTER GEAR UP. RECYCLED C/B AND LANDING GEAR, NO IMPROVEMENT. LIGHT WENT OUT ON IT OWN AFTER 50 MINUTES OF FLIGHT. MAINTENANCE FOUND LT GEAR DOOR UPLOCK SENSOR TARGET BINDING IN ACTUATOR AREA. CLEANED AND LUBRICATED SENSOR TARGET MECHANISM. REQ TEST FLIGHT FOR OPS CHECK DUE TO INADEQUATE FACILITIES IN DTW. 2 H 7 4 4F RT A49EU 2001021600231 20010216 00231 EU 2001 2 16 MALA010152 1 20010131 A 3260 GJ21 WARNING LIGHT BAC 146 AVRO146RJ85A 1500097 EU RT MLG ILLUMINATED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 513XJ E2329 RT GEAR NOT RETRACTING LIGHT ILLUMINATED AFTER TAKEOFF. AFTER TO, ON GEAR RETRACTION THE RT MAIN RED (UNSAFE) GEAR INDI CATION REMAINED ILLUMINATED AND THE RED GEAR HANDLE LIGHTS REMAINED ILLUMINATED. UNDER THE DIRECTION OF MAINTENANCE CON TROL CYCLED GEAR 2 TIMES WITH THE SAME RESULTS DOWN 3 GREEN, NO RED, UP, RED ON RT MAIN GEAR. GEAR CONTINUED NO DRAG WA S NOTED WITH THE GEAR SELECTED UP. THE A/C FLEW STRAIGHT AND COORDINATED. RETURNED TO MSP. MAINTENANCE COULD NOT FIND FAULT, CLEANED AND LUBED RT GEAR UPLOCK AND RT DOOR UPLOCK. REPLACED PCB GJ21 FOR PRECAUTION MEASURES CYCLED GEAR MULT IPLE TIMES NO DEFECTS NOTED. 2 H 7 4 4F RT A49EU 2001021600232 20010216 00232 EU 2001 2 16 MALA010153 1 20010201 A 7603 POWER LEVER SAAB SF340 340B 7860101 EU COCKPIT UNDERTORQUED A MALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 GL 15 416XJ 416 LT AND RT ENGINE WILL ONLY MAKE 72 PERCENT TORQUE WITH POWER LEVERS FIREWALLED. AT FL210 WHILE SETTING POWER FOR TREND TRIED TO SET TORQUE TO 74 PERCENT, PL''S MAXED OUT AT 73 - 74 PERCENT AFTER RAM RISE. MAINTENANCE COMPLETED GPA RUNS WI TH BOTH ENGINES, FOUND TO BE MAKING POWER, MARGIN CHECKS GOOD. ENGINES NOT FUEL LIMITED. COMPLETED CHECK OF LT AND RT POWER LEVERS, NO DISCREPANCIES NOTED. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2001021600233 20010216 00233 WP 2001 2 16 ABXA0100026 1 20010131 A 3260 H1410051 PROXIMITY SWITCH DOUG DOUG DC9 DC941 302207N WP LT MLG FAILED A ABXA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 23 976AX N7625 47596 DURING APPROACH WHEN LANDING GEAR WAS SELECTED DOWN, THE NOSE LANDING GEAR DOWN (GREEN) LIGHT FAILED TO ILLUMINATE. MIS SED APPROACH PROCEDURES WERE COMPLIED WITH. THE CREW REPLACED THE NOSE LANDING GEAR DOWN INDICATOR LIGHT BULBS AND RECY CLED THE LANDING GEAR. THE LANDING GEAR FUNCTIONED PROPERLY. DURING THE SECOND APPROACH, THE LEFT LANDING GEAR UNSAFE LIGHT FAILED TO ILLUMINATE. ANOTHER MISSED APPROACH WAS CONDUCTED. MAINTENANCE INSPECTED AND FOUND THE LEFT MAIN LANDI NG GEAR GROUND PROX SWITCH TO BE DEFECTIVE. THE SWITCH WAS REPLACED IAW DC-9 MM 32-60-01. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2001021600234 20010216 00234 NM 2001 2 16 HNAA0100010 1 20010130 A 2450 51608003 CONTROL UNIT DHAV DHC8 DHC8102 2809003 NM MLG WW CONTAMINATED A HNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 07 911HA 15423 2240 034 DURING TAKEOFF ROLL, THE LEFT AC BUS CAUTION LIGHT ILLUMINATED. CREW ABORTED TAKEOFF. FOUND DEICE FLUID CONTAMINATION IN NR 1 AC GENERATOR CONNECTOR. CLEANED CONNECTOR. ALSO REPLACED NR 1 AC GEN CONTROL UNIT. 2 H 7 2 4T RT A13NM 2001021600235 20010216 00235 NM 2001 2 16 UPS01234826 1 20010201 A 3350 BATTERY PACK BOEING 727 727247 138408F NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 210UP 21697 INSPECTION TYPE:IN, COCKPIT EMER EXIT LIGHT WILL NOT COME ON DURING TEST. REMOVED AND REPLACED BATTER PACK, OPS CHECK G OOD. 2 L 7 3 4F A3WE 2001021600236 20010216 00236 NM 2001 2 16 UPS01234827 1 20010131 A 3350 LIGHT BOEING 727 72727C 138400J NM COCKPIT MALFUNCTIONED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 907UP 19118 INSPECTION TYPE:IN, COCKPIT EMERGENCY EXIT LIGHT COMES ON WHEN SWITCH PLACED IN AUTO BUT GOES OUT WHEN LIGHT MOVED BY HA ND WORKS FINE WITH SWITCH IN ON FWD ENTRY LIGHT WORKS NORMALLY. RESEATED COCKPIT EMER LIGHT ASSY, CHECKS GOOD. 2 L 7 3 4F A3WE 2001021600237 20010216 00237 NM 2001 2 16 UPS01234828 1 20010131 A 3350 LIGHT BOEING 727 727247 138408F NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 210UP 21697 INSPECTION TYPE:IN, BATTERIES REMOVED FROM EMERGENCY EXIT LIGHT. REPLACED COCKPIT DOOR EMERGENCY EXIT LIGHT ASSY, OPS C HECK GOOD. 2 L 7 3 4F A3WE 2001021600238 20010216 00238 NM 2001 2 16 UPS01234829 1 20010201 A 3350 LIGHT BOEING 727 727247 138408F NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 207UP 21699 INSPECTION TYPE:IN, ON TAKEOFF EMERGENCY UNIT LIGHT ABOVE COCKPIT DOOR CAME ON. LIGHT WAS LOOSE AND WILL NOT STAY IN SO CKET. RE-INSTALLED ASSEMBLY, OPS CHECK NORMAL. 2 L 7 3 4F A3WE 2001021600239 20010216 00239 WP 2001 2 16 UPS01834830 1 20010201 A 5314 STRUCTURE DOUG DC8 DC873F 302199F WP KEELBEAM LOOSE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:IN, KEEL BEAM STRUCTURE BETWEEN MAIN GEAR DOORS LOOSE. 2 L 7 4 4F RT 4A25 2001021600240 20010216 00240 WP 2001 2 16 MWEA010142 1 20010201 A 5510 993612585 WEB DOUG DC9 DC981 3022081 WP HORIZONTAL STAB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 805ME 48031 LEFT HORIZONTAL STABILIZER LEADING EDGE SIDE ROLLER SUPPORT WEB IS CRACKED. REMOVED CRACKED SUPPORT WEB AND INSTALLED N EW SUPPORT WEB. 2 L 7 2 4F A6WE 2001021600241 20010216 00241 WP 2001 2 16 MWEA010138 1 20010122 A 5320 99576593 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 TOOL DAMAGE IN RADIUS AND NEXT TO FASTENER, STATION 522, LONGERON 10 LEFT. REMOVED AND REPLACED INTERCOSTAL. 2 L 7 2 4F A6WE 2001021600242 20010216 00242 WP 2001 2 16 MWEA010139 1 20010122 A 5320 99576673 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 THREE FASTENER HOLES NOT FILLED, STATION 558, INTERCOSTAL AT LONGERON 8 LEFT. INSTALLED FASTENERS. WHILE REPAIRING FOU ND INTERCOSTAL CRACKED. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001021600243 20010216 00243 WP 2001 2 16 MWEA010140 1 20010122 A 5311 59114471 FRAME DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 CRACK ON FRAME AT STATION 256, LONGERON 8 LEFT. REMOVED FASTENERS AND DAMAGED AREA, FABRICATED AND INSTALLED FRAME SPLI CE AND ANGLE. 2 L 7 2 4F A6WE 2001021600244 20010216 00244 WP 2001 2 16 TWAA0102101 1 20010130 A 3350 8039001 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 979TW 53629 AT THE FWD OVERWING EMERGENCY EXITS, THE LT AND RT EMERGENCY EXIT LIGHTS WERE INOPERATIVE. REPLACED THE B5-103 POWER SU PPLY. CHECK-C 11-8-00 STL. 2 L 7 2 4F RT A6WE 2001021600245 20010216 00245 WP 2001 2 16 TWAA0102102 1 20010124 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 906TW 49160 THE FUSELAGE SKIN WAS GOUGED BELOW THE FWD LAV SERVICE PANEL, APPROX .5 BY .5 INCH. REPAIRED DAMAGE WITH CLASS III REPA IR PER 53-04 12B. CHECK-C 1-9-00 STL. 2 L 7 2 4F A6WE 2001021600246 20010216 00246 EU 2001 2 16 QXEA01000087 1 20010130 A 4990 38075412 APU FOKKER F28 F28MK4000 4990810 EU APU BAY ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 498US * 276 11181 PDX- OIL SMELL IN CABIN. REMOVED AND REPLACED APU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001021600247 20010216 00247 SO 2001 2 16 SWIA972312 1 20010131 A 2750 SELECTOR KNOB EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 585SW 120353 FLAP CONTROL FAULT ON TAXI OUT ALL SEGEMENTS. INSTALLED SERVICEABLE FLAP SELECTOR S/N 120031R. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001021600248 20010216 00248 SO 2001 2 16 SWIA972313 1 20010201 A 2460 RELAY EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT DC RELAY BOX BURNED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 07 568SW 120343 BURNING SMELL IN COCKPIT INFLIGHT REPORTED BY FLIGHT CREW. ISOLATED SMELL AND EVIDENCE OF SMOKE TO K0543 FEEDER PROTECT ION RELAY IN LEFT DC RELAY BOX. REMOVED AND REPLACED K0543 IAW MM 54-52-00 AND MM 24-52-00. RAN ENGINES, SYSTEMS OPS C HECKS GOOD. NO FURTHER ODORS NOTED. 2 L 7 2 4T 4 T RT A31SO E20NE 2001021600249 20010216 00249 NE 2001 2 16 SWIA972314 2 20010131 A 7320 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE EEC FAILED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 187SW 120037 LEFT EEC FAILED ON TAKEOFF ROLL. ABORTED TAKEOFF. FOUND CANNON PLUG P5 ON LEFT EEC WITH FAULT. REMOVED AND REPLACED L EFT EEC HARNESS IAW EMB 120 MM 73-21-00, OPS CHECK GOOD. P/N ON 3115911-01, S/N ON AA4313, S/N OFF AA3712. 2 L 7 2 4T 4 T RT A31SO E20NE 2001021600250 20010216 00250 SO 2001 2 16 SWIA972315 1 20010201 A 2752 WIRE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS CHAFED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 195SW 120127 DURING FLAP RETRACTION ON GROUND, GOT FLAP CONTROL FAULT AND ADVANCED SWS WITH INBOARD PAIR NOT MOVING. CLEARED ONLY AF TER RESET. REPLACED CHAFED WIRE AT LEFT INBOARD FLAP ACTUATOR CANNON PLUG. REPLACED RIGHT INBOARD FLAP ACTUATOR CANNO N PLUG AND REPLACED SHIELDED WIRE FROM RIGHT INBOARD FLAP ACTUATOR TO OVERWING FUSELAGE CONNECTOR. GROUND CHECK NORMAL FLAP OPERATION. 2 L 7 2 4T 4 T RT A31SO E20NE 2001021600251 20010216 00251 2001 2 16 SWIA972316 4 20010128 A 3130 WARNING LIGHT EMB 120 EMB120RT SO PWA 118 PW118 NE TRIM WARNING ILLUMINATED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 130G 120130 TRIM AURAL WARNING WITH TRIM IN GREEN BAND AT TAKEOFF. ABORTED TAKEOFF. RESET AURAL WARNING COMPUTER. RAN AIRCRAFT WI TH TRIM SET TO TAKEOFF. COULD NOT DUPLICATE. CYCLED TRIM OUT OF GREEN BAND FORWARD AND AFT. TRIM AURAL WARNING CHECKS GOOD. RAN TRIM THROUGH GREEN BAND SLOWLY AND STOPPED AT EACH POSITION WHILE RUNNING. ALL CHECKS FOUND GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001021600252 20010216 00252 SO 2001 2 16 SWIA972317 1 20010131 A 5246 DOOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FUEL DOOR DAMAGED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 299SW 120329 DURING TAKEOFF ROLL PRIOR TO V1 RECEIVED RED DOOR LIGHT ON MAP AND RED FLASHING WARNS LIGHT. ABORTED TAKEOFF. FOUND OU TBOARD REFUEL DOOR FWD FASTENER BAD AND POPPED OUT. REPLACED FASTENER AND RESECURED FORWARD DOOR. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001021600253 20010216 00253 SO 2001 2 16 SWIA972318 1 20010123 A 2910 ACTUATOR CABLE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE HYD SYSTEM ACT OUT OF ADJ A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 204SW 120243 AT V1 AIRCRAFT BRAKES SEEMED TO LOCK UP. ABORTED TAKEOFF. INSPECTED AND ADJUSTED BLUE HYDRAULIC SYSTEM ACTUATION CABLE S. OPS CHECK AND PRESSURE CHECK GOOD. TAXI CHECK GOOD IAW EMB120 MM 32-41-00. 2 L 7 2 4T 4 T RT A31SO E20NE 2001021600254 20010216 00254 2001 2 16 SWIA972319 4 20010128 A 2215 SERVO EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE AUTOPILOT MALFUNCTIONED A SWIA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 190SW 120050 WHILE PERFORMING FLIGHT CONTROL TEST ON TAXI CHECK, THE ELEVATOR CONTROL SEEMED TO SNAG OR CATCH ON SOMETHING MIDWAY OF TRAVEL. RETURNED TO GATE. REMOVED AND REPLACED ELEVATOR AUTO PILOT SERVO IAW MM 27-00-03. OPS CHECKS GOOD. P/N ON: 622-5734-002, S/N ON: 5371, S/N OFF: 3893. 2 L 7 2 4T 4 T RT A31SO E20NE 2001021600255 20010216 00255 SO 2001 2 16 SWIA972320 1 20010126 A 3260 UPLOCK EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT & RT MLG OUT OF ADJ A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 299SW 120329 UPON ATTEMPTING TO RAISE LANDING GEAR, RECEIVED A RED-A LIGHT AND A RED-B LIGHT. VISUALLY NOTICED THAT GEAR DOORS FOR L EFT AND RIGHT GEAR DO NOT CLOSE. DIVERTED TO FAT. ADJUSTED LEFT AND RIGHT UPLOCK HOOK PLUNGERS IAW 32-11-01. SWUNG GE AR SEVERAL TIMES IAW 32-00-00. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001021600256 20010216 00256 EU 2001 2 16 DHL2001367500 1 20010131 A 5753 NSA51775 BOLT AIRBUS 300 A300B4203 3930306 EU FLAP TRACK CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH MSN265 BOLTS AND NUTS AT RT WING FLAP TRACK NR 3 & 6 FOUND CORRODED BOLT AND NUT FOR SCREWJACK. REF IPC 57-25-13 PG 1, FIG 1 I TEMS 20 & 40A FOR TRACK 3 AND IPC 57-25-16 PG 1, FIG 1 ITEM 20 & 40 FOR TRACK 6. REPLACED BOLTS AND NUT. (NUT P/N IS M S21250-05034) NO S/N. 2 L 7 2 4F RT A35EU 2001021600257 20010216 00257 NM 2001 2 16 DHL2001740C29 1 20010115 A 5310 STRUCTURE BOEING 727 7272Q9 138448M NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 FUS LOWER AREA, UPPER WALL OF AIR CONDITIONING RAM AIR PLENUM AT LT PRIMARY HEAT EXCHANGER AREA WITH SIGNS OF CORROSION (RED MARKS). REMOVED FASTENERS FOR S/M ACCESS AS PER B727 SRM 51-30-2. REMOVED CORROSION AT RAM AIR PLENUM LT LOWER EX TERNAL SKIN AS PER B727 SRM 51-10-6. MATERIAL LOSS LOWER WING SKIN AREA STRINGER 5 ONE AREA 2 X 2 INCH .065 AND ONE ARE A 1.5 X 2 INCH .06 FRD PER B727 SRM 57-30-1 AREA WITHIN 1.5 INCH OF SPANWISE SKIN SPLICES OUT OF SRM LIMIT. ACCOMPLISHE D PENETRANT INSPECTION AND HFEC INSP LOWER WING SKIN NO CRACKS NOTED PER B727 NDT PART 6 51-00-00 MIL STD 6866B. REMOVE D FASTENERS AT PANEL 3218 AND REMOVED ATTACH FITTING AT KEEL BEAM TO LOWER SKIN STA 5 LB 12 PLENUM AREA AS PER B72. 2 L 7 3 4F RT A3WE 2001021600258 20010216 00258 SO 2001 2 16 GLBA2001018 1 20010201 A 5270 LATCH EMB 120 EMB120ER 3260203 SO SERVICE DOOR DAMAGED A GLBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 01 297UX 120297 ABORTED T/O, SERVICE DOOR ANNUNCIATOR ILLUMINATED. REPLACED LATCH, OPS CHECKED SYSYEM GOOD. 2 L 7 2 4T RT A31SO 2001021600259 20010216 00259 CE 2001 2 16 GLBA2001019 1 20010201 A 2130 CONTROL UNIT BEECH 1900 1900D 1154162 CE CABIN PRESSURE FAILED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 261GL UE261 RETURN TO BLOCK, WOULD NOT PRESSURIZE. CND ON GROUND, OPS CHECKED SYSTEM GOOD. 2 L 7 2 4T RT A24CE 2001021600260 20010216 00260 WP 2001 2 16 DHL2001802001 1 20010202 A 2612 FIRE LOOP DOUG DC8 DC873F 302199F WP NR 2 ENGINE MALFUNCTIONED A DHLA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 802DH 46076 CLIMBING THROUGH 12,000, NR 2 ENG FIRE WARNING ILLUMINATED, PERFORMED CHECKLIST AND RETURNED TO CVG. OIL PRESS= 30 PSI, WINDMILL TIME= 17 MINUTES, A LOOP WOULD NOT TEST, B LOOP DID TEST OK. INSPECTED ENGINE AND COWLING FOR EVIDENCE OF FIR E, OVERTEMP, INSPECTED ENG AIR DUCTS, NO DEFECTS NOTED. CHANGED ENG FIRE LOOPS (ITEM 8M LOG 216512) FIRE DETECT SYSTEM OPS GOOD IAW MM 26-10-0. PERFORMED ENG RUN PER JRH. UNABLE TO DUPLICATE DISCREPENCY. SUSPECT FAULTY A LOOP. A/C OK F OR CONTINUED SERVICE. 2 L 7 4 4F RT 4A25 2001021600261 20010216 00261 NM 2001 2 16 AWXA0001260 1 20010128 A 2780 31EN1016 SWITCH BOEING 757 7572G7 1384963 NM LE FLAPS DEFECTIVE A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 909AW 24522 LAS-AIR TURNBACK- DURING FLAP RETRACTION AFTER TAKEOFF, EICAS DISPLAYED LEADING EDGE SLAT DISAGREE MESSAGE AS FLAP HANDL E WAS MOVED TO THE FLAP UP POSITION. THE AIRCRAFT RETURNED TO LAS AND MADE AN UNEVENTFUL LANDING. IN LAS MAINTENANCE T ROUBLESHOT AND REPLACED THE LT AND RT INBOARD LEADING EDGE SLAT LOSS SENSING SWITCHES. SYSTEM TESTED GOOD. SWITCH P/N' 'S (LT) 31EN101-6, (RT) 31EN102-6. 2 L 7 2 4F RT A2NM 2001021600262 20010216 00262 EU 2001 2 16 01FDEA00071 1 20010131 A 2120 UNKNOWN AIRBUS 310 A310222 3930315 EU COCKPIT ODOR A FDEA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 25 421FE 342 JUST PRIOR TO DESCENT, A STRONG BURNING ODOR SMELL IN COCKPIT. AC RELEASED PER MEL 34-32A 1WX RADAR SYS INOP. 2 L 7 2 4F RT A35EU 2001021600263 20010216 00263 NM 2001 2 16 C8GA20010002 1 20010130 A 7933 56B17D PROBE PWA BOEING 727 727223 1384074 NM NR 2 ENGINE DEFECTIVE A C8GA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 15 899AA 700789 22015 FLIGHT 739 FROM KDEN TO KMCI, NUMBER 2 ENGINE OIL TEMP WENT INTO THE YELLOW BAND DURING CLIMBOUT FROM DEN. AIR TURNBACK TO DEN. REPLACED NR 2 ENGINE OIL TEMP BULB, OPS CHECK NORMAL ON ENG RUN. 2 L 7 3 4F A3WE 2001021600264 20010216 00264 NM 2001 2 16 DHL200171201C 1 20010130 A 5320 FLOOR SUPPORT BOEING 727 72729 1384007 NM CARGO BAY DEFORMED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 MAIN CARGO FLOOR D SUPPORT ANGLE DEFORMED AT STA 848.95. REMOVED FLOOR SUPPORT ANGLE PER SRM 51-30-2. FABRICATED NEW S UPPORT ANGLE PER SRM 53-10-5. TREATED AND PRIMED PER SRM 51-10-2. INSTALLED SUPPORT ANGLE PER SRM 51-30-2. 2 L 7 3 4F A3WE 2001021600265 20010216 00265 NM 2001 2 16 DHL200171202C 1 20010130 A 5320 FLOOR SUPPORT BOEING 727 72729 1384007 NM CARGO BAY DEFORMED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 MAIN CARGO FLOOR SUPPORT ANGLE DEFORMED AT TRACK 2 AND 3. REMOVED FLOOR SUPPORT ANGLE PER SRM 51-30-2. FABRICATED NEW SUPPORT ANGLE PER SRM 53-10-5. CLEANED, TREATED AND PRIMED PER SRM 51-10-2. INSTALLED NEW ANGLE PER SRM 51-30-2. 2 L 7 3 4F A3WE 2001021600266 20010216 00266 NM 2001 2 16 DHL200171203C 1 20010130 A 5320 FLOOR SUPPORT BOEING 727 72729 1384007 NM CARGO BAY BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 MAIN CARGO FLOOR SUPPORT ANGLE BROKEN .25 INCH AND CRACKED .25 INCH AT STA 760.95. STOP DRILLED CRACK PER SRM 51-10-1. FABRICATED DOUBLER PER SRM 51-40 PG 1. CLEANED, TREATED AND PRIMED PER SRM 51-10-2, INSTALLED DOUBLER PER SRM 51-40 PG 1. 2 L 7 3 4F A3WE 2001021600267 20010216 00267 NM 2001 2 16 DHL200171204C 1 20010130 A 5320 FLOOR SUPPORT BOEING 727 72729 1384007 NM CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 FWD BAGGAGE FLOOR SUPPORT ANGLE CRACKED BETWEEN STRINGER 26 TO 27 RT STA 670.000 RT SIDE. STOP DRILLED PER SRM 51-10-1. FABRICATED DOUBLER PER SRM 51-40 PG 1. CLEANED, TREATED AND PRIMED PER SRM 51-10-2, INSTALLED DOUBLER PER SRM 51-40 P G 1. 2 L 7 3 4F A3WE 2001021600268 20010216 00268 NM 2001 2 16 DHL200171205C 1 20010130 A 5320 FRAME BOEING 727 72729 1384007 NM CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 FWD CARGO COMPT FRAME CRACKED 1.5 INCH BETWEEN S25 AND S26 LT STA 680.000. STOP DRILLED PER SRM 51-10-1, FABRICATED DOU BLER PER SRM 53-10-4, CLEANED, TREATED AND PRIMED PER SRM 51-10-2, INSTALLED DOUBLER PER SRM 53-10-4. 2 L 7 3 4F A3WE 2001021600269 20010216 00269 NM 2001 2 16 DHL200171206C 1 20010130 A 5320 INTERCOSTAL BOEING 727 72729 1384007 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 FWD BAGGAGE BIN INTERCOSTAL CRACKED 1 INCH STA 640.000 UPPER PART LT BETWEEN STR 18 AND 19 LT. STOP DRILLED PER SRM 51- 10-1, FABRICATED DOUBLER PER SRM 51-40 PG 1, CLEANED, TREATED AND PRIMED PER SRM 51-10-2. INSTALLED DOUBLER PER SRM 51- 40 PG 1. 2 L 7 3 4F A3WE 2001021600270 20010216 00270 WP 2001 2 16 MWEA010141 1 20010201 A 5330 5910228209 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 805ME 48031 DENT IN FUSELAGE SKIN JUST FORWARD OF TAIL CONE AND JUST BELOW AFT COMPARTMENT VENT AT STATION 1497. REPAIRED DENT BY F ABRICATING REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001021600271 20010216 00271 NE 2001 2 16 MWEA010143 2 20010131 A 7321 7436024 FUEL CONTROL DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE LT ENGINE INOPERATIVE A MWEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 31 207ME 47794 667125 LEFT ENGINE WS SLOW TO SPOOL UP. REPLACED FUEL CONTROL UNIT ON LEFT ENGINE. 2 L 7 2 4F 4 F A6WE E2EA 2001021600272 20010216 00272 2001 2 16 COMA0160191 4 20010131 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 729CA 7265 STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001021600273 20010216 00273 EA 2001 2 16 COMA0160192 1 20010131 A 2612 47259701 CONTROLLER CNDAIR CL600 CL6002B19 EA APU FIRE DETECT MALFUNCTIONED A COMA F D ACTIVATE FIRE EXT. RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 403CA 930 7428 APU FIRE WARNING DURING TAXI. REPLACED THE FIRE DETECTION CONTROLLER. 2 L 7 2 4F RT A21EA 2001021600274 20010216 00274 2001 2 16 COMA0160193 4 20010130 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 969CA 7141 STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001021600275 20010216 00275 2001 2 16 COMA0160194 4 20010130 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 959CA 7116 STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001021600276 20010216 00276 EA 2001 2 16 COMA0160195 1 20010202 A 5730 SKIN PANEL CNDAIR CL600 CL6002B19 EA RT WING CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 937CA 15711 7044 CORROSION DAMAGE ON LOWER WING PLANK RT SIDE JUST AFT OF FUEL ACCESS PANEL 610AB BETWEEN WS 0.00 AND 22.50. TRIMMED OUT DAMAGED AREA AND INSTALLED SEAL RETAINER IAW CANADAIR REO 601R-57-21-128. 2 L 7 2 4F RT A21EA 2001021600277 20010216 00277 EA 2001 2 16 COMA0160196 1 20010201 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA LAVATORY MALFUNCTIONED A COMA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING AP APPROACH 1 SO 01 721CA 7259 SMOKE TOILET WARNING. COULD NOT DUPLICATE. FOUND NO DISCREPANCIES. 2 L 7 2 4F RT A21EA 2001021600281 20010216 00281 NM 2001 2 16 AT0100051 1 20010103 A 5520 SKIN PANEL BOEING 737 7372L9 1384497 NM RT ELEVATOR GOUGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 FOUND RIGHT ELEVATOR LEADING EDGE GOUGED AT OUTBOARD END FROM OUTBOARD SEAL HARDWARE. REMOVED AND REPLACED LEADING EDGE SECTION, REPLACED SEAL ATTACH FASTENERS IAW TIMCO SERVICE ORDER 151151-23696. 2 L 7 2 4F RT A16WE 2001021600282 20010216 00282 NM 2001 2 16 AT0100052 1 20010120 A 5321 FLOORBOARD BOEING 737 7372L9 1384497 NM FUSELAGE DELAMINATED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 FOUND CABIN FLOOR PANEL RBL 45 BS 430 DELAMINATED. REMOVED, FABRICATED, AND INSTALLED REPLACMENT IAW REO L-00363 AND SR M 53-20-1. 2 L 7 2 4F RT A16WE 2001021600283 20010216 00283 NM 2001 2 16 AT0100053 1 20010118 A 5347 SEAT TRACK BOEING 737 7372L9 1384497 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 FOUND SEAT TRACK WAS CORRODED BEYOND LIMITS. INSTALLED NEW SECTION OF SEAT TRACK IAW B737 SRM 73-10-5 FIGURE 2, 53-20-1 . 2 L 7 2 4F RT A16WE 2001021600285 20010216 00285 WP 2001 2 16 AT0100017R1 1 20010111 A 5311 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 807AT 47444 FOUND 1 INCH CRACK IN FRAME AT BS 718L. REMOVED AND REPLACED FRAME AT BS 718L IAW EO 12-5311-29-B1044 1R. 2 L 7 2 4F A6WE 2001021600286 20010216 00286 WP 2001 2 16 AT0100032R1 1 20010111 A 5711 SPAR DOUG DC9 DC932 3022066 WP RT WING CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 FOUND RIGHT WING REAR SPAR TO HAVE INTERGRANULAR EXFOLIATED CORROSION INBOARD OF CENTER FLAP SUPPORT FITTING. REMOVED C ORROSION AND FABRICATED AND INSTALLED SPLICES IAW REO-L00303. 2 L 7 2 4F A6WE 2001021600287 20010216 00287 WP 2001 2 16 AT0100033R1 1 20010101 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 FOUND FORWARD ENTRY FLOORBOARD 4693 CORRODED BEYOND LIMITS. REPLACED FLOORBOARD IAW DC9 SRM 53-01 FIG 1, 51-10-02, 51-1 0-04, 51-30-03, 51-10-03, AND 51-30-01. 2 L 7 2 4F A6WE 2001021600288 20010216 00288 WP 2001 2 16 AT0100041R1 1 20010102 A 5330 SKIN PANEL DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FOUND SKIN UNDER C2 LOWER THRESHHOLD AT BS 917 CORRODED. INSTALLED REPAIR IAW DC9 REO-L00364. 2 L 7 2 4F A6WE 2001021600289 20010216 00289 WP 2001 2 16 AT0100042R1 1 20010119 A 5310 PAN DOUG DC9 DC932 3022066 WP CARGO DOORWAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 FOUND C2 DOOR LOWER PAN CORRODED BEYOND LIMITS. REPLACED LOWER PAN IAW DC9 SRM 53-04 FIG 44, 51-10-03, 51-10-04, 51-30- 02, AND 51-30-05. 2 L 7 2 4F A6WE 2001021600290 20010216 00290 WP 2001 2 16 AT0100043R1 1 20010105 A 5347 CARGO TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FOUND AFT PIT CARGO TRACK BS 937 - 966 CORRODED BEYOND LIMITS. REPAIRED CARGO TRACK IAW DC9 SRM 51-10-03, 51-10-04, AND 53-21. 2 L 7 2 4F A6WE 2001021600291 20010216 00291 EU 2001 2 16 MALA010166 1 20010122 A 5320 INTERCOSTAL SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 420XJ 420 FOUND DURING C-CHECK, CORROSION ON UPPER ANGLES AT INTERCOASTAL BETWEEN FRAMES AT STA 236 AND STA 238, BENEATH FLOOR AT LBL 10. REFER TO CELSIUS W/O 19279, TASK 1541. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40. MATERIAL IS OUT OF LIM ITS REF: 51-10-10, FABRICATED REPAIR ANGLE IAW SRM 51-20-20/51-40-60, ALODINED, PRIMED AND PAINTED IAW SRM 51-20-42/43. INSTALLED REPAIR ANGLES IAW SRM 51-40-21. 2 L 7 2 4T RT A52EU 2001021600292 20010216 00292 NM 2001 2 16 CALA0100099 1 20010202 A 5230 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND A .5 INCH CRACK AT LIGHTENING HOLE IN FORWARD CARGO DOOR INNER SKIN ABOVE INTERIOR HANDLE. THE CRACK W AS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 52-30-01 AND 51-70-13. 2 L 7 2 4F RT A16WE 2001021600293 20010216 00293 NM 2001 2 16 CALA0100100 1 20010203 A 5330 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14383 26312 INSPECTION FOUND FUSELAGE SKIN DENTED AFT OF L-1 DOOR AT STA 380. THE DENTED AREA WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 208. 2 L 7 2 4F RT A16WE 2001021600294 20010216 00294 NM 2001 2 16 CALA0100103 1 20010204 A 5342 ANGLE BOEING 737 7373Q8 1384670 NM FUSELAGE GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14383 26312 INSPECTION FOUND RT SIDE VERTICAL STABILIZER TO FUSELAGE ANGLE GOUGED AT STA 1088 - 1156. THE LT ANGLE AT STA 1121 - 11 38 WAS ALSO GOUGED. THE GOUGED SECTIONS WERE REMOVED AND REPLACED IAW ECRA 5380-01013. 2 L 7 2 4F RT A16WE 2001021600295 20010216 00295 2001 2 16 UPS01234852 4 20010202 A 2565 BOTTLE BOEING 727 72725C 138400H NM ESCAPE SLIDE DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:IN, GALLEY SLIDE PRESS AT LOWER LIMIT. REMOVED AND REPLACED GALLEY SLIDE ASSY, PRESS GOOD. 2 L 7 3 4F A3WE 2001021600296 20010216 00296 NM 2001 2 16 UPS01234853 1 20010202 A 3350 BATTERY BOEING 727 72725C 138400H NM OVERWING DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:IN REF M208478 RT OVERWING DOOR EMERGENCY LIGHT OUT. REMOVED AND REPLACED BATTERY, OPS GOOD. 2 L 7 3 4F A3WE 2001021600298 20010216 00298 CE 2001 2 16 GLBA2001020 1 20010202 A 3233 SWITCH BEECH 1900 1900D 1154162 CE NLG ACTUATOR INOPERATIVE A GLBA A UNSCHED LANDING P NO WARNING INDICATION AP APPROACH 1 CE 01 195GL 6344 5270 UE195 NOSE GEAR ANNUNCIATOR DID NOT ILLUMINATE WITH GEAR SELECT DOWN. INSPECTED FOUND FAULTY ACTUATOR SWITCH. REMOVED AND RE PLACED ACTUATOR, OPS CHECKED SYSTEM GOOD. 2 L 7 2 4T RT A24CE 2001021600299 20010216 00299 2001 2 16 GLBA2001021 4 20010202 A 3421 6224565001 GYRO BEECH 1900 1900D 1154162 CE COCKPIT INOPERATIVE A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 228GL 9158 8 UE228 RETURN TO BLOCK. PILOT EADI SHOWED EXTREME PITCH VARIATIONS. REMOVED AND REPLACED NR 1 VERTICAL GYRO, OPS CHECKED SYST EM GOOD. 2 L 7 2 4T RT A24CE 2001021600300 20010216 00300 CE 2001 2 16 GLBA2001022 1 20010202 A 3260 INDICATOR BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A GLBA A UNSCHED LANDING P NO WARNING INDICATION AP APPROACH 1 CE 01 251GL UE251 NO INTRANSIT GEAR INDICATION WHEN GEAR SELECTED DOWN. INSPECTED RESEATED PCB AND RESET CIRCUIT BREAKER, SYSTEM OPS CHEC KED GOOD WITH TEST FLIGHT. 2 L 7 2 4T RT A24CE 2001021600301 20010216 00301 EU 2001 2 16 DHL2001366007 1 20010206 A 3600 6272481 CONTROLLER AIRBUS 300 A300B4203 3930306 EU PNEUMATIC SYS MALFUNCTIONED A DHLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 366DH 249 RETURNED TO BLOCK ON TAXI OUT. PNEUMATIC LIGHT ON MWP AND CHIME SOUNDED. ALL SYSTEMS APPEAR NORMAL. LIGHT WOULD NOT E XTINGUISH. SWAPPED PNEUMATIC CONTROLLERS FOR TROUBLESHOOTING. PERFORMED BITE CHECK. BOTH CHECK NORMAL IAW 36-10-01. 2 L 7 2 4F RT A35EU 2001021600302 20010216 00302 EU 2001 2 16 DHL2001366008 1 20010206 A 3600 354971008 CONTROL BOX AIRBUS 300 A300B4203 3930306 EU PNEUMATIC SYS FAILED A DHLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 366DH 249 DURING BEFORE T/O CHECKLIST, PRESSED MWP RECALL BUTTON. PNEU LIGHT ILLUMINATED WITH NO CHIME, ALL SYS NORMAL. REMOVED AND REPLACED PRESS SEQ BOX IAW 21-31-00, OPS NORMAL. 2 L 7 2 4F RT A35EU 2001021600303 20010216 00303 CE 2001 2 16 GLBA2001 1 20010204 A 5270 WARNING LIGHT BEECH 1900 1900D 1154162 CE PAX DOOR ILLUMINATED A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 01 122UX UE122 ABORTED T/O, CABIN DOOR ANNUNCIATOR ILLUMINATED ON ROLL-OUT. INSPECTED SYSTEM CND. 2 L 7 2 4T RT A24CE 2001021600304 20010216 00304 CE 2001 2 16 GLBA2001025 1 20010205 A 7500 TUBE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT WING BLEEDAIR FAILED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 220GL UE220 RETURN TO BLOCK, RIGHT BLEED AIR FAILURE. REPAIRED EVA TUBING RIGHT WING, OPS CHECKED SYSTEM GOOD. 2 L 7 2 4T 4 T RT A24CE E26NE 2001021600305 20010216 00305 NE 2001 2 16 GLBA2001030 3 20010206 A 6140 INDICATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3A NE RT PROPELLER FAILED A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 01 249GL UE249 ABORTED T/O, RIGHT PROP RMP INDICATOR DROPPED OFF. INSPECTED, SWAPPED INDICATORS CND OPS CHECKED GOOD. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2001021600306 20010216 00306 NM 2001 2 16 UIEA01001 1 20010125 A 3213 65B0146643 CYLINDER BOEING 747 747230B 1384889 NM LANDING GEAR CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 507MC 90204 21380 DURING THE RECENT C-CHECK, THE LEFT OUTER CYLINDER SPUD BOSS WAS FOUND CORRODED IN THE AREA OF CHROME LOSS. AREA CLEANE D OF CORROSION, TREATED, CHECKED FOR HEAT RELATED DAMAGE. REWORK AREA IS 5MM IN DIAMETER WITH MISSING CHROME AND MATERI AL LOSS OF .4 MM AFTER CORROSION CLEAN UP. ATLAS AIR EO 4732A014 ISSUED FOR REWORK AND FOLLOW UP INSPECTION. (M) 2 L 7 4 4F A20WE 2001021600307 20010216 00307 NM 2001 2 16 UIEA01004 1 20010125 A 5711 65B665015 SPAR BOEING 747 747230B 1384889 NM WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 507MC 90204 21380 DURING THE RECENT C-CHECK, THE REAR SPAR (OUTSIDE SURFACE) WAS FOUND CORRODED IN THE VICINITY OF THE NR 2 INBOARD FUELIN G VALVE MOUNT BOLT HOLES AT WS 562.50. FUELING EQUIPMENT AND MOUNT BOLT REMOVED. AREA REWORKED BY SPOT FACING CORRODED AREA, BLENDED, TREATED AND FINISHED PER BOEING TELEX. FUELING EQUIPMENT AND MOUNT HARDWARE REINSTALLED. (M) 2 L 7 4 4F A20WE 2001021600308 20010216 00308 NM 2001 2 16 UIEA01002 1 20010125 A 5730 65B1441918 SKIN BOEING 747 747230B 1384889 NM RT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 507MC 90204 21380 DURING THE RECENT C-CHECK, THE R/W EXTERNAL SKIN WAS CORRODED AT WS 320 COMMON TO STRINGER 15 AND WBL 179. CORROSION RE MOVED, AREA BLENDED, TREATED AND REFINISHED IAW 57-30-01 FIG 2. (M) 2 L 7 4 4F A20WE 2001021600309 20010216 00309 NM 2001 2 16 UIEA01003 1 20010125 A 5320 65B17767113 STRUCTURE BOEING 747 747230B 1384889 NM FUSELAGE CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 SW 07 507MC 90204 21380 DURING THE RECENT C-CHECK, THE UPPER CHORD AT BS 1840 WAS FOUND CORRODED BETWEEN LBL 75 AND 98 ON THE HORIZONTAL SURFACE AND EXTENDED DOWN ONTO THE VERTICAL SIDE. CORRODED SECTION WAS REMOVED, REPLACED AND REPAIR ANGLES WERE INSTALLED. RE WORKED AREA EXTENDS FROM LBL 65 AND 105. REPAIR APPROVED PER BOEING TELEX. (M) 2 L 7 4 4F A20WE 2001021600310 20010216 00310 EU 2001 2 16 USAASA01003 1 20010131 A 2530 OVEN AIRBUS A319 A319112 EU FWD GALLEY FIRE A USAA F A ACTIVATE FIRE EXT. UNSCHED LANDING A FLAME/FIRE CL CLIMB 1 EA 19 709UW 0997 CLT-LGA- FLT 1886 - AFTER DEPARTING CLT, AND CLIMBING THROUGH FL170,FIRE WAS REPORTED TO BE COMING FROM THE FORWARD GALL EY OVEN. THE FIRE WAS EXTINGUISHED USING A PORTABLE FIRE EXTINGUISHER. THE FLIGHT RETURNED TO CLT AND LANDED WITHOUT I NCIDENT. MAINTENANCE INSPECTED THE OVEN AND FOUND NO FIRE DAMAGE. THE OVEN WAS REPLACED AS A PRECAUTION. OPS CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2001021600311 20010216 00311 EU 2001 2 16 USAASA01001 1 20010126 A 2120 SMOKE AIRBUS A319 A319112 EU CABIN DETECTED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 714US 1046 PVD-DCA - FLT 716 - SMOKE WAS DETECTED IN THE CABIN SHORTLY AFTER TAKEOFF. THE FLIGHT RETURNED TO PVD AND LANDED WITHOU T INCIDENT. (M) 2 L 7 2 4F RT A28NM 2001021600312 20010216 00312 NM 2001 2 16 USAASB01026 1 20010128 A 3020 655812310 DUCT BOEING 737 737201 1384454 NM NR 2 ENGINE LEAKING A USAA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 EA 19 263AU 22869 FLL - FLT 2626 - ON CLIMB-OUT FROM FLL, AT 6,000 FEET, THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW ACCOMPLISHED PR OCEDURES, REDUCED POWER TO IDLE AND LIGHT EXTINGUISHED. FLIGHT RETURNED TO FIELD AT FLL AND LANDED WITHOUT FURTHER INCI DENT. NO EMERGENCY WAS DECLARED AND NO ENGINE SHUTDOWN OCCURRED. MAINTENANCE FOUND THE NR 2 ENGINE COWL ANTI-ICE DUCT ASSEMBLY, BETWEEN THE 13TH STAGE SADDLE DUCT AND TEMPERATURE ANTI-ICE NOSE COWL VALVE, BLOWN AT THE EXPANSION COUPLING. REMOVED AND REPLACED DUCT ASSEMBLY, EXPANSION COUPLING (P/N 808153) AND 13TH STAGE SADDLE DUCT TO FAN CASE SEAL (P/N RD 3022), RIGHT SIDE. ACCOMPLISHED ENGINE RUN. NO LEAKS NOTED. (M) 2 L 7 2 4F A16WE 2001021600313 20010216 00313 NM 2001 2 16 USAABB01007 1 20010126 A 7330 21SN04333 PRESSURE SWITCH BOEING 767 767201 1385125 NM GE CF6 CF680C2B2 30025 NE RT ENGINE FAULTY A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 650US 23902 695422 CLT - FLT 192 - SHORTLY AFTER TAKEOFF, CREW RECEIVED THE EICAS MESSAGE ''R ENG FUEL FILTER.'' FLIGHT RETURNED TO CLT AN D LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FUEL FILTER AN FUEL FILTER DIFFERENTIAL PRESSURE SWITCH. ( M) 2 L 7 2 4F 4 F RT A1NM E13NE 2001021600314 20010216 00314 NM 2001 2 16 20010216SG001 1 20010128 A 3350 10005511 LIGHT DHAV DHC8 DHC8103 1386005 NM COCKPIT INOPERATIVE A IQJA K NONE L NO TEST IN INSP/MAINT 1 NM 01 807WP 209 023 HNL - COCKPIT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED (PORTABLE EMERGENCY) LIGHT ASSY. OPS CHECK GOOD IAW PS M 1-8-2 CHAPTER 33-51-00 PAGE 201-202. (M) 2 H 7 2 4T RT A13NM 2001021600315 20010216 00315 GL 2001 2 16 HALA0100014 2 20010121 A 7200 ENGINE DOUG DC10 DC1010 3022110 WP GE CF6 CF6* 30020 GL NR 3 ENGINE FAILED A HALA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 WP 13 129AA 46996 PDX - FLT 25 - RIGHT AFTER AIRCRAFT ROTATION, LOUD BANG WAS NOTED COMING FROM RIGHT SIDE OF AIRCRAFT. SHORTLY AFTER NOT ICED HIGH TEMP LIGHT NR 3 ENGINE. FOLLOWED CHECKLIST AND SHUT DOWN NR 3 ENGINE. DUMPED FUEL AND LANDED. SUSPECT COMPR ESSOR STALL NR 3 ENGINE. REMOVED AND REPLACED NR 3 ENGINE PER CARD DR719401. LEAK AND OPS CHECK PER CARD AR719518 POWE R CHECK OK. (M) 2 L 7 3 4F 4 F A22WE E23EA 2001021600316 20010216 00316 WP 2001 2 16 HALA0100013 1 20010121 A 2611 47597404 SMOKE DETECTOR DOUG DC9 DC951 3022051 WP FWD CARGO BAY MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 699HA 47763 HNL - FOUND CARGO SMOKE SYSTEM FORWARD FAULT LIGHT ''A'' ON WHEN TESTED. REMOVED AND REPLACED NR 003 SMOKE DETECTOR FOR FORWARD CARGO SMOKE. OPS CHECKED OK. (M) 2 L 7 2 4F RT A6WE 2001021600317 20010216 00317 EA 2001 2 16 20010216SG002 2 20010109 A 7200 ENGINE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA ENGINE CONTAMINATED A GUUA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 19 147GA UC86 FLT 9311 - MCO-FLL - DURING DESCENT, WHEN BRINGING TORQUE BELOW 1000 LB, FUEL SMELL ON FLIGHT DECK. CLEANED ENGINES. R AN AIRCRAFT ON GROUND WITH BLEEDS ON AND OFF. NO FUEL SMELL NOTED AT THIS TIME. (M) 2 L 7 2 4T 4 T RT A24CE E4EA 2001021600318 20010216 00318 CE 2001 2 16 20010216SG004 1 20010105 A 2120 UNKNOWN BEECH 1900 1900C 1154161 CE COCKPIT ODOR A GUUA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 19 147GA UC86 FLT 9311 - MCO-FLL - DURING DESCENT, STRONG ODOR OF FUEL WHEN POWER REDUCED APPROXIMATELY 1000 LBS. INSPECTED AIRCRAFT AND PERFORMED GROUND RUN. NO DEFECTS NOTED. (M) 2 L 7 2 4T RT A24CE 2001021600319 20010216 00319 CE 2001 2 16 20010216SG003 1 20010109 A 2810 10138901165 CHECK VALVE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA LT/RT ENGINE MALFUNCTIONED A GUUA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 19 147GA UC86 FLT - 9195 - FPO-FLL, DURING DESCENT WITH POWER REDUCED BELOW APPROX 1000 LB TORQUE, STRONG FUEL SMELL ON FLIGHT DECK AN D AT SEATS 1 AND 2. REMOVED AND REPLACED FUEL PURGE VALVES ON LEFT AND RIGHT ENGINES. (M) 2 L 7 2 4T 4 T RT A24CE E4EA 2001021600320 20010216 00320 CE 2001 2 16 20010216SG005 1 20010120 A 7810 BOLT BEECH 1900 1900C 1154161 CE EXHST FLEX HOSE LOOSE A GUUA O OTHER J WARNING INDICATION TO TAKEOFF 1 SO 19 197GA UB16 FLT 9391 - EYW - DURING TAKEOFF, RIGHT FIREWALL FUEL VALVE T-HANDLE ILLUMINATED. ALL ENGINE INSTRUMENTS INDICATED NORMA L. TIGHTENED BOLT ON RIGHT EXHAUST FLEX HOSE FLANGE. ENGINE RUN CHECK NORMAL. (M) 2 L 7 2 4T RT A24CE 2001021600321 20010216 00321 CE 2001 2 16 20010216SG006 1 20010124 A 3260 444EN496 SQUAT SWITCH BEECH 1900 1900C 1154161 CE LEFT L/G OUT OF ADJ A GUUA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 19 137GA UC105 FLT 9195 - FLL - ABORTED DEPARTURE DUE TO STALL AURAL WARNING SOUNDED CONTINUOUSLY DURING TAKEOFF ROLL ABOUT 90 KIAS. A DJUSTED LEFT SQUAT SWITCH. AIRCRAFT TEST FLIGHT SATISFACTORY. (M) 2 L 7 2 4T RT A24CE 2001021600322 20010216 00322 EA 2001 2 16 ASOA01011 1 20010127 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 EA COCKPIT CRACKED A ASOA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 11 833AS 6558 7246 FLT 4451 - DURING FLIGHT FROM DFW-AUS, FIRST OFFICERS WINDSHIELD CRACKED. AIRCRAFT RETURNED TO DFW AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD. OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURN ED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001021600323 20010216 00323 SO 2001 2 16 ASOA01012 1 20010127 A 3260 12022623001 HARNESS EMB 120 EMB120RT SO RT MLG INOPERATIVE A ASOA K NONE N FALSE WARNING AP APPROACH 1 SO 11 239AS 120057 FLT 4861 - DURING APPROACH INTO ICT FROM DFW, CREW RECEIVED AN ''A'' AND ''B'' RED LIGHT INDICATION. CAPTAIN CYCLED GEA RS, BUT STILL HAD THE INDICATION. CAPTAIN FLEW PAST TOWER TO CONFIRM GEAR WAS DOWN. ICT TOWER DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RIGHT MLG SENSOR HARNESS. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001021600324 20010216 00324 NE 2001 2 16 ASOA01010 2 20010127 A 7320 5009984C HMU EMB 120 EMB120RT SO PWA 118 PW118 NE ENGINE INOPERATIVE A ASOA O OTHER R X PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT CR CRUISE 1 SO 11 236AS 18202 120049 115146 FLT 4960 - DURING FLIGHT FROM HOU TO DFW AFTER 2 MINUTES IN CRUISE, THE LEFT ENGINE WENT TO 20 PERCENT TORQUE, NP WENT T O 85 PERCENT, NH WENT TO 80 PERCENT, AND ENGINE OIL PRESSURE DROPPED TO ZERO. TEN TO TWELVE SECONDS AFTER FLAMEOUT, ENG INE STARTED BACK UP AND EVERYTHING WAS NORMAL. AIRCRAFT CONTINUED TO DFW AND LANDED SAFELY. MAINTENANCE REPLACED THE H MU AND FUEL PUMP. MAINTENANCE RAN ENGINES AND TESTED SYSTEM. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 2001021600325 20010216 00325 EA 2001 2 16 20010216SG007 1 20010112 A 5330 SKIN CNDAIR CL600 CL6002B16 1900305 EA FUSELAGE CORRODED A AJCA K NONE O OTHER IN INSP/MAINT 1 EA 25 224F 25509 5163 DURING COMPLIANCE OF BOMBARDIER SB 601-0528 DATED 10/17/00, INSPECTION OF FUSELAGE SKIN, FOUND BURNED SKIN STRIPPED PAIN T AND DISCOVERED CORROSION, IN AREA ADJACENT TO CUTOUT FOR APU EXHAUST. (M) 2 L 7 2 4F RT A21EA 2001021600326 20010216 00326 EA 2001 2 16 20010216SG008 1 20010116 A 2913 601R751133 PUMP CNDAIR CL600 CL6002B16 1900305 EA NR 2 ENGINE LEAKING A UWUA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NE 03 708SC 5391 WHILE AT CRUISE, THE CREW OBSERVED NR 2 HYD SYSTEM QTY WAS LOW. CREW MONITORED NR 2 HYD SYSTEM QUANTITY AND TEMPERATURE , HYD TEMP ROSE ABOVE 135 DEGREES CELSIUS AND QUANTITY DEPLETED TO ZERO. CREW SHUT DOWN NR 2 ENGINE PER CNDAIR ''QUICK REF HANDBOOK'' ABNORMAL PROCEDURES SECT 10. CREW DIVERTED A/C TO IRELAND AND LANDED WITHOUT INCIDENT. UPON INSPECTION OF NR 2 HYD SYSTEM, FOUND RT ENGINE DRIVEN HYD PUMP LEAKING HYD FLUID FROM ENGIEN GANG DRAIN. REPLACED NR 2 ENGINE DRIV EN HYD PUMP AND CASE DRAIN FILTER IAW A/C MM. A/C RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001021600327 20010216 00327 SO 2001 2 16 SIMA6270041S 1 20010104 A 2910 14531063419 HYDRAULIC LINE EMB 145 EMB145LR SO HYDRAULIC SYSTEM FAILED A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 627 145121 DFW - FLT 3653 - NR 1 HYDRAULIC SYSTEM FAILURE AIRCRAFT RETURNED TO DFW WITHOUT INCIDENT. RAI PRESSURE LINE AND SERVICE D HYDRAULIC FLUID IAW 29-10-00. (M) 2 L 7 2 4T RT T00011AT 2001022000001 20010220 00001 EU 2001 2 20 KBMA97422 1 20010107 A 6410 355A09103601 BEARING SNIAS 350 AS350BA 8680817 EU TAIL ROTOR WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 350SH 4396 2957 BEARING WORN BEYOND LIMITS. 1 G 7 1 3U NC H9EU 2001022000002 20010220 00002 2001 2 20 KBMA99412 4 20010110 A 3422 103002201 GYRO SNIAS 350 AS350BA 8680817 EU COCKPIT PRECESSES E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 270SH 7399 1864 DIRECTIONAL GYRO PRESSING AND FLAG STAYS UP. 1 G 7 1 3U NC H9EU 2001022000003 20010220 00003 2001 2 20 KBMA99417 4 20010116 A 3422 103002201 GYRO SNIAS 350 AS350BA 8680817 EU COCKPIT PRECESSES E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 270SH 7406 1864 DIREDTIONAL GYRO PRECESSING, INOPERATIVE. 1 G 7 1 3U NC H9EU 2001022000005 20010220 00005 2001 2 20 KBMA99406 4 20010105 A 3422 RCA15BK1 GYRO SNIAS 350 AS350B 8680801 EU COCKPIT PRECESSES E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 37SH 9137 1288 DIRECTIONAL GYRO PRESSES 20-3- DEGREES. SEAT FOR REPAIR. 1 G 7 1 3U H9EU 2001022000006 20010220 00006 2001 2 20 KBMA99402 4 20010105 A 3452 06601062000 TRANSPONDER SNIAS 350 AS350BA 8680817 EU COCKPIT ATC INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 1188P 9662 2347 TRANSPONDER NON-OPERATIONAL. 1 G 7 1 3U NC H9EU 2001022000008 20010220 00008 2001 2 20 COMA0160205 4 20010205 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 409CA 7441 STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001022000009 20010220 00009 WP 2001 2 20 ABXA0100031 1 20010202 A 5753 5910042503 VANE DOUG DC9 DC941 302207N WP LT FLAP CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 FIXED VANE ON LEFT WING WAS CORRODED INTERNALLY. MAINTENANCE INSPECTED AND REPLACED THE LEFT FIXED VANE IAW DC-9 MM. 2 L 7 2 4F A6WE 2001022000010 20010220 00010 NM 2001 2 20 UPS01234821 1 20010130 A 2612 INDICATOR BOEING 727 72722C 138400F NM NR 1 ENG FIRE INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:PFLT, NR 1 ENG A FIRE LIGHT WILL NOT TEST. ACCOMPLISH WAN 558661/REF DMI M 208397, NR 1 ENGINE B LOOP F IRE TEST INOP, TECH RECOMMENDS CHECK RESISTANCE BETWEEN PINS E AND G RESISTANCE CHECKED BETWEEN PINS E AND G, FOUND TO B E WITHIN LIMITS IAW MM 26-11-02. SYSTEM OPS CHECK, PERFORMED FOUND SATIS. THIS CLOSES DMI 208397. 2 L 7 3 4F A3WE 2001022000011 20010220 00011 NM 2001 2 20 UPS01234823 1 20010204 A 3510 OXYGEN MASK BOEING 727 72725C 138400H NM COCKPIT BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:PFLT, 2ND OBSERVERS 02 MASK HANGER IS BROKEN. *S/D* REMOVED AND REPLACED MASK HOLDER. 2 L 7 3 4F A3WE 2001022000012 20010220 00012 2001 2 20 SWIA972330 4 20010201 A 3130 WARNING LIGHT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT ILLUMINATED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 295SW 120322 TRIM FAIL ILLUMINATED ON MAP. NO AURAL WARNING WHILE ON TAKEOFF ROLL. ABORTED TAKEOFF. MEL 22-10-1B, ELECT TRIM, MC 1 22. RE-RACKED NUMBER ONE AND NUMBER TWO APC-65S. OPERATED AND TESTED TRIM SYSTEM. NO DEFECTS NOTED, COULD NOT DUPLICA TE. 2 L 7 2 4T 4 T RT A31SO E20NE 2001022000013 20010220 00013 EA 2001 2 20 SWIA972331 1 20010204 A 3610 SHUTOFF VALVE CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE LEFT FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 905SW 7437 LEFT 10TH SOV FAILED TO OPEN. RECEIVED STATUS MESSAGE L 10TH ARMED OPEN. RETURNED TO DEN. POWERED DOWN AIRCRAFT AND R E-POWERED. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2001022000014 20010220 00014 2001 2 20 SWIA972332 4 20010205 A 2215 SERVO EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE AILERON FAILED A SWIA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 199SW 120237 WHEN CONTROL YOKE MOVED SIDE TO SIDE A NOISE IS HEARD IN THE FLOOR PANEL AREA. REPLACED AILERON SERVO WITH SERVICEABLE UNIT. OPS CHECK GOOD. S/N ON: 9961, S/N OFF: 5507. 2 L 7 2 4T 4 T RT A31SO E20NE 2001050300216 20010503 00216 SO 2001 5 3 SWIA972333 1 20010204 A 3040 WINDSHIELD EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 07 271YV 120271 EN ROUTE AT 22,000 FT NOTED SMOKE COMING FROM FORWARD PORTION OF GLARESHIELD. DIVERTED TO LAX. AFTER A DETAILED INSPEC TION OF WIRING AND COMPONENTS LOCATED UNDER GLARESHIELD FOUND GROUND WIRE ON LT WINDSHIELD HEATING BLOCK TO HAVE BEEN AR CING AT THE TERMINAL TO LUG ATTACH POINT. REPLACED LUG ON GROUND WIRE (G1). UPON REINSTALLATION ON HEATING BLOCK DISCO VERED HEATING BLOCK TO HAVE BEEN DAMAGED. SECURED GROUND WIRE (G-1) IN HEATING BLOCK AND DEFERRED LT WINDSHIELD HEAT PE R MEL 30-40-1. SECURED CB TO PREVENT INADVERTANT OPERATION DEFERRED. 02/05/01 R&R LT WINDSHIELD IAW EMB 120 MM 56-10-01 . OPS CHECKS GOOD. 02/12/01 R&R LT WINDSHIELD HEAT RCCB. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001022000016 20010220 00016 SO 2001 2 20 SWIA972321 1 20010130 A 3150 WARN PANEL EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 214SW 120280 ON TAKEOFF ROLL RECEIVED HIGH SPEED AURAL WARNING THROUGH 80 KNOTS. ABORTED TAKEOFF. PERFORMED INSULATION TEST ON ALL WIRES IN HIGH SPEED WARNING SYSTEM. WIRES CHECK GOOD. REMOVED AND REPLACED AURAL WARNING UNIT WITH SERVICEABLE UNIT IA W 31-53-02. HIGH SPEED WARNING ONLY SOUNDS AT PROPER SPEED. OPS CHECK GOOD. P/N: 80-0557-11, S/N ON: 0472, S/N OFF: 0405. 2 L 7 2 4T 4 T RT A31SO E20NE 2001022000017 20010220 00017 SO 2001 2 20 SWIA972322 1 20010202 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT TE FLAPS FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 195SW 120127 AFTER TAKEOFF, WHEN FLAPS WERE RETRACTED, CONTROL FAULT AND INBOARD FLAP LIGHT BAR (2ND DIGIT) ILLUMINATED. WHEN RESET PRESSED, LIGHT EXTINGUISHED APPROXIMATELY 10 SECONDS, THEN RE-ILLUMINATED. RETURNED TO FAT. MEGGER TESTED RIGHT INBOAR D FLAP ACTUATOR WIRE BUNDLE. CHECKS GOOD. REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATOR IAW MM 27-50-00. OPS CHECK AND LEAK CHECK GOOD. P/N: 320300-1005, S/N ON: 0109, S/N OFF: 0103. 2 L 7 2 4T 4 T RT A31SO E20NE 2001022000018 20010220 00018 SO 2001 2 20 SWIA972323 1 20010201 A 2711 TAB EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE ELEVATOR TRIM BINDING A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 190SW 120050 INFLIGHT WITH F/O AUTOPILOT ENGAGED THE AIRCRAFT LEVELED OFF TO CATCH THE COURSE AND FELT A VIBRATION LIKE TENSION BEING RELEASED ON THE CABLES TO THE AILERON. THE YOKE VIBRATED LEFT AND RIGHT, THEN EVERYTHING RETURNED TO NORMAL. DISENGAG ED AUTOPILOT, TESTED AILERON/ELEVATOR TRAVEL, SEEMED OK. FOUND LEFT AILERON TRIM TAB BINDING AND POPPING. INSTALLED NE W TRIM TAB, BEARINGS AND REINSTALLED TRIM TAB IAW EMB MM 22-12-02. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001022000019 20010220 00019 EU 2001 2 20 MALA010157 1 20010121 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 420XJ 420 FOUND DURING C-CHECK, THE INBOARD FLANGE ON LBL 18.3 SEAT TRACK FROM STA 294 THRU STA 412 IS CORRODED. REFER TO CELSIUS W/O 19279, TASK 1534 AND SAAB STATEMENT 340 SDS000867. MAINTENANCEREMOVED CORROSION, CHECK LIMIT. REMOVED NEG MAT IAW SRM 51-10-30. REMOVED CORROSION, REF: SAAB SRM 51-70-40. MATERIAL BETWEEN STA 294 - 339 AREAS OUT OF LIMITS, AREAS FR OM 339 TO 412 WITHIN LIMITS REF: SRM 51-10-10, ALODINED, PRIMED, AND PAINTED SEAT TRACK FLANGE IAW SRM 51-20-10. MATERI AL REMOVED IS ACCEPTABLE IAW SAAB DOCUMENT 340 SDS000867. 2 L 7 2 4T RT A52EU 2001022000020 20010220 00020 WP 2001 2 20 CALA0100096 1 20010202 A 5230 SKIN DOUG DC9 DC982 3022082 WP CARGO DOOR GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND SKIN GOUGED AT AFT CARGO DOOR LOWER EDGE OF PAN. THE RIVETS WERE REMOVED AND A DOUBLER WAS INSTALLED I AW SRM 51-30-2 AND EA 9-5230-2-A0832. 2 L 7 2 4F A6WE 2001022000021 20010220 00021 WP 2001 2 20 CALA0100101 1 20010204 A 5511 SPAR CAP DOUG DC10 DC1030 3023501 WP HORIZONTAL STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13088 46850 INSPECTION FOUND A .75 INCH CRACK AT AFT BARREL NUT HOLE OF UPPER AFT RT REAR SPAR CAP ON HORIZONTAL STABILIZER. THE SP AR CAP WAS REPAIRED IAW ECRA 5511-01041. 2 L 7 3 4F A22WE 2001022000022 20010220 00022 WP 2001 2 20 CALA0100102 1 20010204 A 3350 60030451 BATTERY PACK DOUG DC9 DC981 3022081 WP CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 13881 48045 INSPECTION FOUND EIGHT OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. THE BATTERY PACKS AT STA 427R AND 570R WERE REMOVED AND REPLACED IAW SRM 33-53-00. 2 L 7 2 4F A6WE 2001022000023 20010220 00023 SO 2001 2 20 SWIA972324 1 20010202 A 2751 ANNUNCIATOR EMB 120 EMB120RT SO PWA 118 PW118 NE TE FLAP SYSTEM MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 07 137H 120137 FLAP DISAGREEMENT AFTER FLAP RETRACTION AFTER TAKEOFF. DIVERTED TO FAT FROM MOD. REPLACED FLAP ANNUNCIATOR UNIT. OPS CHECK GOOD IAW EMB 120 MM 27-50-05. P/N ON 306900-1005, S/N ON 0212, P/N OFF 306900-1017, S/N OFF 0155. 2 L 7 2 4T 4 T RT A31SO E20NE 2001022000024 20010220 00024 EA 2001 2 20 SWIA972325 1 20010131 A 3030 CONTROLLER CNDAIR CL600 CL6002B19 EA AD SENSOR HEAT FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 416SW 7089 L AOA HEAT CAUTION MESSAGE ILLUMINATED SHORTLY AFTER TAKEOFF. RETURNED TO SLC. REPLACED NUMBER ONE AIR DATA SENSOR HEA T CONTROLLER IAW MM 30-31-15. LEFT AOA OPS CHECK GOOD. P/N 785-806-2, S/N ON 218, S/N OFF 169. 2 L 7 2 4F RT A21EA 2001022000025 20010220 00025 EA 2001 2 20 SWIA972326 1 20010203 A 2131 CONTROLLER CNDAIR CL600 CL6002B19 EA CABIN PRESSURE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 407SW 7034 AIRCRAFT FAILED TO PRESSURIZED. QRH NO EFFECT. RETURNED TO SLC. PRESSURIZED AIRCRAFT ON GROUND USING BOTH AUTO CONTRO LLER NUMBER ONE AND NUMBER TWO. ALSO PRESSURIZED AIRCRAFT IN MANUAL MODE. SYSTEM OPERATES NORMAL IAW CRJ MM 21-31-00. 2 L 7 2 4F RT A21EA 2001022000026 20010220 00026 EA 2001 2 20 SWIA972327 1 20010202 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 EA EVAC LIGHTS FAILED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 411SW 7067 LOWER EXIT LIGHT AT SERVICE DOOR WILL NOT ILLUMINATE. FORWARD FLOOR ORANGE EMERGENCY STRIP LIGHTS WILL NOT ILLUMINATE A ND FLOOR LEVEL EXIT SIGN AT PAX DOOR INOP. REMOVED AND REPLACED CONNECTOR AT LOWER EXIT LIGHT AT SERVICE DOOR ON WIRE N UMBER P10LY. OPS CHECKS GOOD. EMERGENCY LIGHTING OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2001022000027 20010220 00027 SO 2001 2 20 SWIA972328 1 20010202 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 194SW 120120 FLAP CONTROL FAULT ON INBOARD FLAP PAIR, WHEN SELECTING FLAPS FROM 15 DEGREES TO 25 DEGREES ON LANDING. REMOVED AND REP LACED LEFT INBOARD FLAP ACTUATOR. OPS CHECKS AND LEAK CHECKS GOOD. P/N ON 320300-1005, S/N ON 0067, S/N OFF 0067. 2 L 7 2 4T 4 T RT A31SO E20NE 2001022000028 20010220 00028 SO 2001 2 20 SWIA972329 1 20010201 A 5270 LOCK EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE FUEL DOOR FAILED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 226SW 120296 DURING TAKEOFF ROLL, RED DOORS LIGHT ON MAP ILLUMINATED FOR ABOUT 2 SECONDS WITH POSSIBLE DOOR SPECIFIC LIGHT ILLUMINATI NG ON OVERHEAD PANEL. LIGHTS DID NOT REMAIN ON LONG ENOUGH TO DETERMINE WHICH OVERHEAD DOOR LIGHT ILLUMINATED. TAKEOFF ABORTED. RETURNED TO BOX CONTACTED MAINT. RESECURED FORWARD CAMLOCK AT OUTER FUEL DOOR. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001022000029 20010220 00029 EA 2001 2 20 COMA0160198 1 20010202 A 2810 45737012 FUEL CAP CNDAIR CL600 CL6002B19 EA RT WING LEAKING A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 951CA 7091 RT WING LEAKING FUEL AT FILLER CAP. REPLACED THE FUEL CAP. 2 L 7 2 4F RT A21EA 2001022000030 20010220 00030 EU 2001 2 20 MALA010167 1 20010122 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 420XJ 420 FOUND DURING C-CHECK, CARGO AREA SEAT TRACK RBL18.0 HAS CORROSION AT STA 630 THRU STA 668 ON THE OUTBOARD FLOOR PANEL FL ANGE. REFER TO CELSIUS W/O 19279, TASK 1529 AND SAAB STATEMENT 340SDS000867. MAINTENANCE REMOVED CORROSION IAW SRM 51- 10-10/51-70-40 REMAINING MATERIAL IS OUT OF LIMIT, REF: SRM 51-10-10, ALODINED, PRIMED AND PAINTED SEAT TRACK IAW SRM 51 -20-10. MATERIAL REMOVED IS ACCEPTABLE IAW SAAB DOCUMENT 340SDS000867. 2 L 7 2 4T RT A52EU 2001022000031 20010220 00031 EU 2001 2 20 MALA010168 1 20010122 A 7500 DUCT SAAB SF340 340B 7860101 EU RT ENGINE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 420XJ 420 FOUND DURING C-CHECK, RT ENGINE OUTBOARD COWL 463BR NACA DUCT IS CRACKED. REFER TO CELSIUS W/O 19279, TASK 4548, AND SA AB STATEMENT 340SDS000867. MAINTENANCE ROUTED OUT CRACK REF: SAAB DOCUMENT 340SDS000867, NDT: NO CRACKS NOTED IAW FFVN DT006. 2 L 7 2 4T RT A52EU 2001022000032 20010220 00032 EU 2001 2 20 MALA010154 1 20010119 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 420XJ 420 FOUND DURING C-CHECK, SEVERAL DENTS IN A PREVIOUS REPAIR ON THE RT FUSELAGE AT STA 310.0. REFER TO CELSIUS W/O 19279, T ASK 2530 AND SAAB STATEMENT 72SDS1745. MAINTENANCE REMOVED, REPAIR, AND REWORKED. NO CRACKS NOTED IAW FFVNDT006, REFER TO IPM 12 FOR WORK ACCOMPLISHED AND REPAIR DONE ON RT SIDE IAW SAAB STATEMENT 72SDS1745. 2 L 7 2 4T RT A52EU 2001022000033 20010220 00033 EU 2001 2 20 MALA010155 1 20010120 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 420XJ 420 FOUND DURING C-CHECK, GROUP OF DENTS ON LT FUSELAGE AT STA 355.0, REFER TO CELSIUS W/O 19279, TASK 2529, AND SAAB STATEM ENT 340 SDS000867. MAINTENANCE CHECKED LIMIT, GROUP OF DENTS STA 355.0 SL1515 WITHIN ALLOWABLE LIMIT REF SRM 51-10-10. DENT STA 355 SL1518 IS OUT OF ALLOWABLE LIMIT REF: SRM 51-10-10 AREA 2. PERFORMED NDT NO CRACKS NOTED IAW FFVNDT006. DENTS ARE ACCEPTABLE AS IAW SAAB DOCUMENT 340SDS000867. 2 L 7 2 4T RT A52EU 2001022000034 20010220 00034 EU 2001 2 20 MALA010156 1 20010121 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 420XJ 420 FOUND DURING C-CHECK, THE OUTBOARD FLANGE ON BL 0 SEAT TRACK FROM STA 294 THRU STA 412 IS CORRODED. REFER TO CELSIUS W/ O 19279, TASK 1535, AND SAAB STATEMENT 340SDS000867. MAINTENANCEREMOVED CORROSION, AND CHECK LIMIT, REMOVED MATERIAL IA W 51-10-30. REMOVED CORROSION REF: SAAB SRM 51-70-40. SEVERAL AREAS OUT OF LIMITS BETWEEN 294 & 339 REF: SRM 51-10-10, AREA BETWEEN 339 AND 412 WITHIN LIMITS REF: 51-10-10, ALODINE, PRIME AND PAINTED SEAT TRACK IAW SRM 51-20-10. 2 L 7 2 4T RT A52EU 2001022000035 20010220 00035 EU 2001 2 20 MALA010158 1 20010122 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 420XJ 420 FOUND DURING C-CHECK, THE INBOARD FLANGE ON LBL 18.3 SEAT TRACK IS CORRODED FROM STA 464 THRU STA 594. REFER TO CELSIUS W/O 19279, TASK 1536. MAINTENANCE REMOVED CORROSION AND CHECK LIMIT. REMOVED CORROSION IAW SRM 51-10-30. RESTORE FIN ISH ALODINE, PRIME AND PAINTED SEAT TRACKS IAW SRM 51-20-10. 2 L 7 2 4T RT A52EU 2001022000036 20010220 00036 EU 2001 2 20 MALA010159 1 20010121 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 420XJ 420 FOUND DURING C-CHECK, GALLEY SEAT TRACK CORRODED. REFER TO CELSIUS W/O 19279, TASK 1537. MAINTENANCE REMOVED CORROSION , CHECK LIMIT. REMOVED SEAT TRACK IAW SRM 51-40-27. REMOVED NEG MAT IAW SRM 51-10-30, REMOVED CORROSION REF: SRM 51-70 -40. REMAINING MATERIAL WITHIN LIMITS REF:SRM 51-10-10. ALODINED, PRIMED, AND PAINTED IAW SRM 51-20-42/43. FAY SEALED AND INSTALLED IAW SRM 51-40-00. 2 L 7 2 4T RT A52EU 2001022000037 20010220 00037 EU 2001 2 20 MALA010160 1 20010122 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 420XJ 420 FOUND DURING C-CHECK, SUPPORT ANGLE FOR GALLEY SEAT TRACK IS CORRODED. REFER TO CELSIUS W/O 19279, TASK 1538. MAINTENA NCE REMOVED CORROSION CHECK LIMIT. REMOVED CORROSION IAW SRM 51-70-40. MATERIAL IS WITHIN LIMITS REF: SRM 51-10-10. A LODINED, PRIMED AND PAINTED IAW SRM 51-20-42/43. 2 L 7 2 4T RT A52EU 2001022000038 20010220 00038 EU 2001 2 20 MALA010161 1 20010122 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 420XJ 420 FOUND DURING C-CHECK, CORROSION ON UPPER ANGLE FRAME AT STA 236 BELOW FLOOR AREA. REFER TO CELSIUS W/O 19279, TASK 1539 . MAINTENANCE REMOVED SEVERAL CORRODED RIVETS AND REMOVED CORROSION IAW SRM 51-70-40. MATERIAL IS WITHIN LIMITS REF: S RM 51-10-10, ALODINED PRIMED AND PAINTED REF: SRM 51-20-42/43. INSTALL RIVETS IAW SRM 51-40-21. 2 L 7 2 4T RT A52EU 2001022000039 20010220 00039 EU 2001 2 20 MALA010162 1 20010122 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 420XJ 420 FOUND DURING C-CHECK, CORROSION ON FLOOR SUPPORT ANGLE AT STA 225. REFER TO CELSOIS W/O 19279, TASK 1540. MAINTENANCE REMOVED CORROSION IAW SRM 51--70-40. MATERIAL IS OUT OF LIMITS REF: SRM 51-10-10. FABRICATED NEW ANGLE IAW SRM 51-20-2 0/51-40-60, ALODINED, PRIMED AND PAINTED IAW SRM 51-20-42/43. INSTALLED IAW SRM 51-40-21. 2 L 7 2 4T RT A52EU 2001022000040 20010220 00040 EU 2001 2 20 MALA010163 1 20010122 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 420XJ 420 FOUND DURING C-CHECK, CORROSION ON UPPER ANGLE OF FRAME AT STA 258 BENEATH FLOOR. REFER TO CELSIUS W/O 19279, TASK 1542 . MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40. MATERIAL IS OUT OF LIMITS REF: SRM 51-10-10. FABRICATED NEW ANGLE I AW SRM 51-20-20/30, 51-40-60, ALODINED, PRIMED AND PAINTED IAW SRM 51-20-42/43. INSTALLED IAW SRM 51-40-21. 2 L 7 2 4T RT A52EU 2001022000041 20010220 00041 EU 2001 2 20 MALA010164 1 20010122 A 5320 7253721439 WEB SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 420XJ 420 FOUND DURING C-CHECK, CORROSION ON WEB AT STA 294 BENEATH FLOOR. REFER TO CELSIUS W/O 19279, TASK 1544. MAINTENANCE RE MOVED CORROSION AND SEVERAL CORRODED RIVETS IAW SRM 51-70-40 AND SRM 51-40-21. REMAINING MATERIAL IS OUT OF LIMITS 51-1 0-10. REMOVED DAMAGED WEB IAW SRM 51-40-21, CLEANED AREA IAW SRM 51-20-41; LOCATED, DRILLED AND COUNTERSUNK NEW WEB IAW SRM 51-40-40, INSTALLED NEW WEB SRM 51-40-21 AND FAY SEALED IAW SRM 51-20-51. 2 L 7 2 4T RT A52EU 2001022000042 20010220 00042 EU 2001 2 20 MALA010165 1 20010122 A 5320 CHANNEL SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 420XJ 420 FOUND DURING C-CHECK, CORROSION ON CHANNEL PIECE ATTACHED TO FLOOR PANEL 122BZ. REFER TO CELSIUS W/O 19279, TASK 1545. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40. REMOVED AND REPLACED 3 NUT PLATES WITH NEW RIVETS IAW SRM 51-40-21. R EMAINING MATERIAL IS WITHIN LIMITS REF: SRM 51-10-10. ALODINED, PRIMED, AND PAINTED IAW SRM 51-20-42/43. 2 L 7 2 4T RT A52EU 2001022000043 20010220 00043 WP 2001 2 20 NACA2001007 1 20010202 A 7922 1893013 REGULATOR DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE NR 3 ENGINE OIL LEAKING A NACA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION LD LANDING 1 AL 03 2907F 2269 967 44636 34767 SHUT DOWN NR 3 ENGINE DUE TO OIL LOSS. REMOVED AND REPLACED OIL TEMP REGULATOR. 2 L 7 4 4R 4 R 6A3 5E8 2001022000044 20010220 00044 2001 2 20 MWEA010144 4 20010203 A 3410 4058254902 PANEL DOUG MD88 MD88 3023688 NM COCKPIT INOPERATIVE A MWEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 31 601ME 49762 DURING TAXI, NO MODE LIGHT ILLUMINATED. REMOVED AND REPLACED THRUST RATING PANEL. 2 L 7 2 4F RT A6WE 2001022000045 20010220 00045 WP 2001 2 20 CALA0100097 1 20010202 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND CABIN LEFT O/B SEAT TRACK CORRODED AT FS 1117 - 1136. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED A ND A NEW SECTION OF TRACK WAS INSTALLED IAW SRM 53-05, FIGURE 4F. 2 L 7 2 4F A6WE 2001022000046 20010220 00046 WP 2001 2 20 CALA0100098 1 20010202 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND MID CARGO LT TIE DOWN TRACK CORRODED AT FS 522 - 788. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTAL LED IAW SRM 51-30-2 AND 53-05, FIGURE 6. 2 L 7 2 4F A6WE 2001022000048 20010220 00048 EA 2001 2 20 COMA0160197 1 20010202 A 5610 NP1393222 WINDOW CNDAIR CL600 CL6002B19 EA COCKPIT CRACKED A COMA B EMER. DESCENT O OTHER CR CRUISE 1 SO 01 962CA 12153 7123 COPILOTS SIDE WINDOW CRACKED. REPLACED WINDOW. 2 L 7 2 4F RT A21EA 2001022000049 20010220 00049 2001 2 20 COMA0160199 4 20010202 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 971CA 7145 STALL FAIL WARNING DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001022000050 20010220 00050 2001 2 20 COMA0160201 4 20010202 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 963CA 7127 STALL FAIL WARNING DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001022000052 20010220 00052 2001 2 20 COMA0160200 4 20010202 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 966CA 7132 STALL FAIL WARNING DURING T/O. RESET THE STLAL COMPUTER. 2 L 7 2 4F RT A21EA 2001022000053 20010220 00053 NM 2001 2 20 UPS01434847 1 20010112 A 5242 BRACKET BOEING 747 747123F NM E/E BAY DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, E&E COMPARTMENT DOOR CRACK ON OUTER FRAME AT RT SUPPORT BRACKET MOUNT BOLT HOLE AND SUSPECT CRACK ON OUTER CHORD OF FRAME 3 LHS. REPAIRS CARRIED OUT IAW SRM 51-40-03. HFEC INSP CARRIED TO DETERMINE CRACKING PER D67170 PART 6 CH 51-00-00 FIG 4. 2 L 7 4 4F A20WE 2001022000054 20010220 00054 WP 2001 2 20 UPS01834833 1 20010125 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, LEFT WING CENTER L/E UPPER RIB IS CRACKED AT XOLDI 6.225. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001022000055 20010220 00055 WP 2001 2 20 UPS01834834 1 20010123 A 5320 3750330505N FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, STA 440 - 460 LONG 34R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750330, A ND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001022000056 20010220 00056 WP 2001 2 20 UPS01834835 1 20010122 A 5313 564932749 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, STA 1740 LONG 15R IS CRACKED. REMOVED, FABRICATED, AND REPLACED LONGERON SECTION IAW DWG 5649327, AND SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2001022000057 20010220 00057 WP 2001 2 20 UPS01834836 1 20010123 A 5320 37502571N FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, STA 600 - 620 LONG 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257, A ND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001022000058 20010220 00058 WP 2001 2 20 UPS01834837 1 20010121 A 5320 47516401 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, STA 759 LONG 18L INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4751640, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001022000059 20010220 00059 WP 2001 2 20 UPS01834838 1 20010125 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, LEFT NR 2 STUBWING HAS UPPER RIB CRACKED AT XILD .7095. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001022000060 20010220 00060 WP 2001 2 20 UPS01834839 1 20010122 A 5315 5773275177 FLOORBEAM DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, STA 680 LBL 48 VERTICAL FLOORBEAM SUPPORT ANGLE IS CRACKED. REMOVED, FABRICATED AND REPLACED ANGL E IAW DWG 5773275, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001022000061 20010220 00061 WP 2001 2 20 UPS01834840 1 20010122 A 5320 36169481N FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, STA 720 LBL 63 FLOORBEAM VERTICAL SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DW G 3616948, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001022000062 20010220 00062 WP 2001 2 20 UPS01834841 1 20010123 A 5320 37502571N FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, STA 440 - 460 LONG 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257, A ND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001022000063 20010220 00063 WP 2001 2 20 UPS01834842 1 20010122 A 5320 37552222 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, STA 742 LBL 24 FLOORBEAM ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755222, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001022000064 20010220 00064 NM 2001 2 20 USAA010092 1 20010129 A 5320 ANGLE BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND CHORD ANGLE CRACKED .75 INCH, STATION 663, LBL 23, WL 201.5. INSTALLED DOUBLER PER EA 68798. (M) 2 L 7 2 4F A16WE 2001022000065 20010220 00065 NM 2001 2 20 USAA010093 1 20010129 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND FRAME CRACKED .25 INCH, STATION 747 FRAME PLUS STRINGER 13L. INSTALLED DOUBLER PER SRM 53-10-4. (M) 2 L 7 2 4F A16WE 2001022000066 20010220 00066 NM 2001 2 20 USAA010094 1 20010129 A 5210 SKIN BOEING 737 737201 1384454 NM AFT ENTRY DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND SKIN CRACKED 2.5 INCHES, LEFT AFT ENTRY DOOR OUTER SKIN STRINGER 17L PLUS 960. INSTALLED DOUBLER PER SRM 53 -30-3. (M) 2 L 7 2 4F A16WE 2001022000067 20010220 00067 NM 2001 2 20 USAA010095 1 20010129 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND SKIN CRACKED 14 INCHES BY 8 INCHES, STRINGER 17R TO 19R, STATION 727A. INSTALLED DOUBLER PER SRM 53-30-3 FI G 1. (M) 2 L 7 2 4F A16WE 2001022000068 20010220 00068 NM 2001 2 20 USAA010096 1 20010130 A 5320 STIFFENER BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND STIFFENER CRACKED 2 INCHES, STRINGER 10L 294. INSTALLED STIFFENER PER EA 68991. (M) 2 L 7 2 4F A16WE 2001022000069 20010220 00069 WP 2001 2 20 UPS01834843 1 20010122 A 5320 577327558 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, STA 680 BL 0 FLOORBEAM VERTICAL SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 5773275, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001022000070 20010220 00070 WP 2001 2 20 UPS01834844 1 20010125 A 5754 97532977 ATTACH ANGLE DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, LEFT WING CENTER L/E VERTICAL ATTACH ANGLE IS CRACKED AT XS 520. REMOVED, FABRICATED, AND REPLACE D ANGLE IAW DWG 9753297, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001022000071 20010220 00071 WP 2001 2 20 UPS01834845 1 20010125 A 5754 5769759501 DOUBLER DOUG DC8 DC871F 302199D WP LT WING BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, LEFT WING L/E LOWER INTERNAL DOUBLER HAS A CORNER BROKEN OFF AT XS 520. REMOVED AND REPLACED DOUB LER AND SKIN IAW DWG 5769759, AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001022000072 20010220 00072 WP 2001 2 20 UPS01834846 1 20010121 A 5320 3779762501 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, STA 675 LONG 4L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779762, AND SRM 51- 1-20D, 51-1-21, 51-1-23. 2 L 7 4 4F RT 4A25 2001022000073 20010220 00073 WP 2001 2 20 UPS01834855 1 20010203 A 2610 SOCKET DOUG DC8 DC873F 302199F WP INDICATOR LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:IN, LOADING CARGO SMOKE DET SYSTEM WOULD NOT TEST. BAD LIGHT SOCKET. REMOVED AND REPLACED TEST LAMP AS SY BASE, OPS CHECKS NORMAL. 2 L 7 4 4F RT 4A25 2001022000074 20010220 00074 EU 2001 2 20 QXEA01000090 1 20010203 A 2612 473054 FIRE LOOP FOKKER F28 F28MK4000 4990810 EU NR 2 ENGINE MALFUNCTIONED A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 486US 3738 1524 11237 SEA- CLIMBING OUT OF FAT, THE NR 2 FIRE WARNING ALARM GAVE FOUR SHORT WARNINGS OF A SECOND OR LESS. ABNORMAL INDICATION S 470/480 TGT 410, WARNING BETWEEN 10,000 AND 25,000 FEET. REMOVED AND REPLACED NR 2 ENGINE FIRE CONTROL UNIT AND NR 2 SENSING LOOP CABLE. AIRCRAFT RETURNED TO SERVICE. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 2001022000075 20010220 00075 SO 2001 2 20 C2XA01IA063 1 20010205 A 3260 2050500101 PROXIMITY SWITCH EMB 120 EMB120ER 3260203 SO RT MLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 47722 120166 IAH - FLIGHT 3580, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LAN DED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR WEIGHT ON WHEELS PROXIMITY SWITCH, A ND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001022000076 20010220 00076 NM 2001 2 20 01FDEA00075 1 20010203 A 3350 1000679 LIGHT BOEING 727 72722 1384002 NM CABIN INOPERATIVE A FDEA K NONE L NO TEST IN INSP/MAINT 1 SO 25 193FE 19142 DURING MAINT TEST FLT FWD ENTRY DOOR EMERGENCY EXIT LIGHT FAILED TO EXTINGUISH IN EITHER DISARM OR OFF POS. REMOVED AND REPLACED LIGHT ASSY PER IAW FEDEX MM 33-50-00. OPS CK GOOD. 2 L 7 3 4F A3WE 2001022000077 20010220 00077 WP 2001 2 20 TWAA0102201 1 20010131 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT, FOUND CORROSION AT LBL 36 INCHES, STA 1138 TO 1110. REPLACED TRACK. FABRICATED NEW TRACK FROM ST OCK AND INSTALLED PER SRM 51-30-01. PRIMED PER SRM 51-10-3. PAINTED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001022000078 20010220 00078 WP 2001 2 20 TWAA0102202 1 20010131 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT, FOUND LONGERON 12L CRACKED AT ATTACH POINT TO 1287 FORMER RING. REMOVED CRACKED LONGERON FOR REPA IR PER SRM 53-02 FIG 18. 2 L 7 2 4F A6WE 2001022000079 20010220 00079 WP 2001 2 20 TWAA0102203 1 20010130 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT, FOUND CORROSION ON MEMBRANE ON LT SIDE WALL AREA OF MID-CARGO COMPT, STA 522 TO 541 (O/B TO SIDEWA LL). REMOVED CORROSION PER SPM 6-80-01 AND SRM 51-10-3 PAGE 21. INSTALLED WEB REPAIR PER SRM 53-01, FIG 2 PAGE 9. 2 L 7 2 4F RT A6WE 2001022000080 20010220 00080 WP 2001 2 20 TWAA0102204 1 20010131 A 5315 FLOORBEAM DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT IN AFT CABIN FOUND FLOORBEAM CORROSION REMOVAL WAS BEYOND LIMITS AT STA 1322, LBL 41, UNDER LT AFT LAV. REPAIRED PER SRM 53-05, PAGE 31. 2 L 7 2 4F RT A6WE 2001022000081 20010220 00081 NM 2001 2 20 PCAA0102003 1 20010202 A 3350 82410162001 CONTROL BOX DHAV DHC8 DHC8102 2809003 NM CABIN FALSE ACTIVATION A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 830EX 155 LGA FLIGHT 3704. FLIGHT ATTENDANT REPORTED EMERGENCY LIGHTS FLASHING ON AND OFF. MAINTENANCE INSPECTED CONTROL SWITCH A ND WIRING, NO DEFECTS NOTED. EMERGENCY LIGHTS CONTROL BOX REPLACED. OPERATED LIGHTS, COULD NOT DUPLICATE PROBLEM. AIR CRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001022000082 20010220 00082 NM 2001 2 20 C1HA200194004 1 20010202 A 3350 900835A CHARGER BOEING 727 727290 138408W NM CABIN FAILED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 294AS 22146 FWD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY AND CHARGER. CHECKS GOOD. 2 L 7 3 4F A3WE 2001022000083 20010220 00083 NM 2001 2 20 C1HA200194005 1 20010204 A 3150 WARNING SYSTEM BOEING 727 727290 138408W NM COCKPIT FALSE ACTIVATION A C1HA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 15 294AS 22146 TAKEOFF WARNING SOUNDED AT START OF TAKEOFF ROLL. TAKEOFF ABORTED AT LESS THAN 30 KTS. PERFORMED TAKEOFF WARNING CHECK IAW 31-26-00, ALL OPS CHECKS NORMAL. SUSPECT DEICE FLUID CAUSING HORN. 2 L 7 3 4F A3WE 2001022000084 20010220 00084 NM 2001 2 20 C1HA200194006 1 20010204 A 3150 WARNING SYSTEM BOEING 727 727290 138408W NM COCKPIT FALSE ACTIVATION A C1HA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 15 294AS 22146 TAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL. ABORTED TAKEOFF AT LESS THAN 30 KTS. ADJUSTED FLAP TAKEOFF WARNING SWITC H IAW 31-26-0, CHECKS GOOD. 2 L 7 3 4F A3WE 2001022000085 20010220 00085 NM 2001 2 20 C1HA200195001 1 20010126 A 3010 32146451 ANTI-ICE VALVE BOEING 727 727290 138408W NM LEFT FAILED A C1HA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 295AS 22147 ON CLIMBOUT WITH WING A/I ON THE ENG NR 1 WING ANTI ICE VALVE FAILED CLOSED. DIVERTED TO DFW FOR REPAIR. REMOVED AND R EPLACED LEFT WING ANTI ICE VALVE IN VENTRAL AREA. 2 L 7 3 4F A3WE 2001022000086 20010220 00086 2001 2 20 KBMA97429 4 20010118 A 3422 RCA15BK1 GYRO SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT MALFUNCTIONED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 180EH 3425 2337 WILL NOT SET PRECESSES AND NO FLAG. 1 G 7 1 3U 3 U H9EU E19EU 2001022000087 20010220 00087 2001 2 20 KBMA97428 4 20010116 A 3422 103002201 GYRO SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT MALFUNCTIONED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 180EH 3416 2337 DIRECTIONAL GYRO IS TUMBLING. 1 G 7 1 3U 3 U H9EU E19EU 2001022000088 20010220 00088 NM 2001 2 20 AALA20010105 1 20010111 A 5310 SHEAR TIE BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 863AA 21090 TUL - FOUND SHEAR TIE CORRODED BETWEEN STRINGER 26L AND 27L STATION 520. REMOVED CORRODED SHEAR TIE STATION 520 STRINGE R 26L. REPLACED SHEAR TIE PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 2001022000089 20010220 00089 NM 2001 2 20 AALA20010109 1 20010112 A 5310 SHEAR TIE BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 863AA 21090 TUL - FOUND STATION 700 AFT SIDE OF FRAME, FRAME SHEAR TIE CORRODED, BETWEEN STRINGER 27R AND 28R. REMOVED CORRODED SHE AR TIE, REMOVED CORROSION FROM SURROUNDING AREA. INSTALLED NEW SHEAR TIE IAW SRM 51-10-6. (M) 2 L 7 3 4F A3WE 2001022000090 20010220 00090 NM 2001 2 20 AALA20010114 1 20010112 A 5310 SHEAR TIE BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 863AA 21090 TUL - FOUND FORWARD SIDE OF FRAME BETWEEN STRINGER 28L AND 27L FS 680, SHEAR TIE, FLANGE CORRODED. REMOVED CORRODED SEC TION OF SHEAR TIE, REPAIRED IAW SRM 53-10-4. (M) 2 L 7 3 4F A3WE 2001022000091 20010220 00091 NM 2001 2 20 C1HA200183001 1 20010130 A 3350 900835A BATTERY PACK BOEING 727 7272S7 138407Z NM CABIN FAILED A C1HA O OTHER O OTHER CR CRUISE 1 GL 15 683CA 22490 THE EMERGENCY EXIT LIGHT IN THE AFT FOR 2L & 2R DOORS FLASHES ON AND OFF DURING FLIGHT. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK CKS GOOD. 2 L 7 3 4F A3WE 2001022000092 20010220 00092 NM 2001 2 20 C1HA200186001 1 20010127 A 2121 10608551 GASPER FAN BOEING 727 7272S7 138407Z NM AIR DISTRIBUTION FAILED A C1HA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 15 686CA 22021 IN CRUISE FLIGHT F/A NOTICED BURNING SMELL IN AFT CABIN NEAR FORWARD GALLEY. TURNED GASPER FAN OFF, SMELL DISAPPEARED. CONTINUES FLIGHT WITH GASPER FAN OFF. REMOVED AND REPLACED GASPER FAN, CHECKS NORMAL. 2 L 7 3 4F A3WE 2001022000093 20010220 00093 NE 2001 2 20 MALA010169 3 20010201 A 6140 PRESSURE SWITCH SAAB SF340 SF340A 7850100 EU ROTOL R390 R3904123F27 NE RT & LT PROP FAILED A MALA O OTHER P NO WARNING INDICATION TO TAKEOFF 1 GL 15 99XJ 099 AUTO COARSEN DID NOT ARM ON TAKEOFF. MAINTENANCE RAN ENGINE WITH CREW, AUTO COARSEN WOULD NOT ARM, INSPECTED AIRCRAFT A ND SAFE FOR ONE TIME FERRY FLIGHT FROM ATW TO MSP. MAINTENANCE REPLACED THE LT AND RT P3 PRESSURE SWITCHES. OPS CHECK GOOD ON THE AUTO COARSENING SYSTEM IAW 61-22-00 OF THE AMM. 2 L 7 2 4T RT A52EU 6 C P31NE 2001022000094 20010220 00094 SO 2001 2 20 GLBA2001023 1 20010203 A 3260 2050500101 PROXIMITY SWITCH EMB 120 EMB120RT SO MLG FAILED A GLBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 01 85GL 12085 ABORTED T/O, FLIGHT IDLE UNLOCK ANNUNCIATOR ILLUMINATED AT POWER-UP. INSPECTED FOUND FAULTY PRX SWITCH. REMOVED AND RE PLACED SWITCH, OPS CHECKED SYSTEM GOOD. 2 L 7 2 4T RT A31SO 2001022000096 20010220 00096 EU 2001 2 20 RAIA00102001 1 20010205 A 3020 3970202 ANTI-ICE VALVE JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 559HK 9503 9503 41075 ROC- LEFT ENGINE ANTI-ICE FAILED. MAINTENANCE INSPECTED AND REPLACED LEFT ENGINE ANTI-ICE VALVE. 2 L 7 2 4T RT A41NM 2001022000097 20010220 00097 WP 2001 2 20 TWAA0102301 1 20010205 A 3350 1864 LIGHT DOUG DC9 DC983 3022083 WP ROW 19 INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 962TW 53612 THE EMERGENCY EGRESS LIGHT AT CABIN ROW 19 WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 4-11-00 STL. 2 L 7 2 4F RT A6WE 2001022000098 20010220 00098 WP 2001 2 20 TWAA0102302 1 20010130 A 5730 SKIN DOUG DC9 DC982 3022082 WP RT WING MISREPAIRED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT, A RT WING L/E BLIND RIVET REPAIR WAS FOUND INSTALLED ON L/E LOWER SURFACE AT INBOARD END OF FUEL S ERVICE PANEL, STA X05250. REMOVED OLD REPAIR AND MADE NEW REPAIR DOUBLER AND INSTALLED WITH HI-LOKS PER SRM 57-06B, PAG E 9 FIG 3. 2 L 7 2 4F A6WE 2001022000099 20010220 00099 WP 2001 2 20 TWAA0102304 1 20010130 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT IN THE AFT ACCY COMPT, FORMER RING WAS DAMAGED AT STA 1418, LONGERON 13R. REPAIRED FORMER PER SRM 53-03, FIG 4. INSTALLED FASTENERS PER SRM 51-10-03. 2 L 7 2 4F A6WE 2001022000100 20010220 00100 WP 2001 2 20 TWAA0102305 1 20010130 A 5315 BRACKET DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT IN THE FWD CARGO COMPT BILGE, STA 237, BETWEEN LONGERON 29R AND 28R, ANGLE BRACKET WAS CRACKED IN R ADIUS IN INTERCOSTAL AFT END UNDER TIE DOWN TRACK. INSTALLED NEW BRACKET PER DRAWING 9915554. 2 L 7 2 4F A6WE 2001022000101 20010220 00101 WP 2001 2 20 TWAA0102306 1 20010130 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9401W 53137 DURING CHECK-C MAINT FOUND CORROSION IN MEMBRANE BETWEEN STA 845 AND 964 AT LONGERON 18L. CUT OUT CORRODED PIECE FROM M EMBRANE STA 845 TO 855 APROXIMATELY. TREATED REPAIR PARTS AND AREA PER SRM 51-10-3 PAGE 54. REPAIRED DAMAGED AREA PER SRM 51-70-4. 2 L 7 2 4F RT A6WE 2001022000102 20010220 00102 NM 2001 2 20 01FDEA00047 1 20010130 A 5310 6516339 FRAME BOEING 727 727227 1384078 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 FRAME DENTED AT BS 970, STR 25L. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-10-1, 51-40-3. 2 L 7 3 4F A3WE 2001022000103 20010220 00103 WP 2001 2 20 TWAA0102307 1 20010130 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9401W 53137 DURING CHECK-C MAINT FOUND CORROSION IN MEMBRANE BETWEEN STA 826 AND 845, AT LONGERON 18L. REMOVED CORROSION PER SPM 6- 80-01. TREATED AREA PER SRM 51-10-3 PAGE 54. REINSTALLED FASTENERS PER SRM 51-30-2. 2 L 7 2 4F RT A6WE 2001022000104 20010220 00104 WP 2001 2 20 TWAA0102308 1 20010131 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9401W 53137 DURING CHECK-C MAINT FOUND LONGERON 18R, STA 560 TO 579, THE FLOOR WEB HAD CORROSION. CUT OUT CORROSION. INSTALLED DOU BLER PER SRM 53-01, PAGE 9. 2 L 7 2 4F RT A6WE 2001022000105 20010220 00105 WP 2001 2 20 TWAA0102310 1 20010201 A 2500 ANGLE DOUG DC9 DC983 3022083 WP F/A SEAT DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9401W 53137 DURING CHECK-C MAINT THE AFT BULKHEAD DOOR, RT UPPER HINGE ARM FOR THE FLT ATTENDANT SEAT, HAD DAMAGED ANGLE BELOW THE P IVOT POINT. CUT OUT DAMAGED AREA AND INSTALLED STACKED DOUBLERS PER SRM 52-01, PAGE 9. 2 L 7 2 4F RT A6WE 2001022000106 20010220 00106 2001 2 20 COMA0110032 4 20010205 A 3420 6226190204 DISPLAY EMB 120 EMB120RT SO AHRS MALFUNCTIONED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 264CA 21291 120256 ATTITUDE DISPLAY AND FLIGHT DIRECTOR FAILURE WARNINGS. REPLACED THE NR 2 AHRS. 2 L 7 2 4T RT A31SO 2001022000107 20010220 00107 2001 2 20 COMA0160202 4 20010205 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 409CA 7441 STALL FAIL CAUTION MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001022000108 20010220 00108 EA 2001 2 20 COMA0160204 1 20010203 A 4990 APU CNDAIR CL600 CL6002B19 EA APU BAY OVERSERVICED A COMA O OTHER W B J INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 SO 01 721CA 7259 SMOKE TOILET WARNING, VISIBLE SMOKE IN CABIN AND COCKPIT. APU WAS OVER SERVICED WITH OIL. REMOVED OIL FROM APU TO PROP ER LEVEL. 2 L 7 2 4F RT A21EA 2001022000109 20010220 00109 WP 2001 2 20 ABXA0100034 1 20010202 A 5313 39248091 LONGERON DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 CORROSION WAS FOUND ON LONGERON 29L, FUSELAGE STATION 617 - 642. MAINTENANCE REPLACED THE LONGERON IAW DC-9 SRM 51-30-5 AND 51-30-2. 2 L 7 2 4F A6WE 2001022000110 20010220 00110 WP 2001 2 20 ABXA0100028 1 20010202 A 5330 DOUBLER DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 INTERNAL FUSELAGE DOUBLER AT STA 642 L30 WAS CORRODED FORWARD OF THE KIDNEY PANEL. MAINTENANCE INSPECTED AND REPLACED T HE DOUBLER IAW DC-9 SRM 51-30-1 AND DRAWING 9923434. 2 L 7 2 4F A6WE 2001022000111 20010220 00111 WP 2001 2 20 ABXA0100029 1 20010202 A 5230 591015707 LATCH DOUG DC9 DC941 302207N WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 REPAIR NEAR THE AFT BAG BIN AFT LATCH WAS CRACKED. MAINTENANCE INSPECTED AND REPLACED THE BAG BIN DOOR IAW DC-9 SRM AN D ABX NEA52300001-005. 2 L 7 2 4F A6WE 2001022000112 20010220 00112 WP 2001 2 20 ABXA0100030 1 20010202 A 5313 3924050501 LONGERON DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 FUSELAGE LONGERON 28L WAS CRACKED. MAINTENANCE INSPECTED AND REPLACED THE LONGERON AT 28L IAW DC-9 SRM 51-30-2 AND 51-3 0-5. 2 L 7 2 4F A6WE 2001022000113 20010220 00113 WP 2001 2 20 ABXA0100032 1 20010202 A 5313 592481659 LONGERON DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 LONGERON AT STRINGER 29L WAS EXFOLIATED ON THE HORIZONTAL FLANGE AT APPROX FUSELAGE STATION 675. MAINTENANCE INSPECTED AND REPLACED THE LONGERON IAW DC-9 SRM 51-30. 2 L 7 2 4F A6WE 2001022000114 20010220 00114 WP 2001 2 20 ABXA0100033 1 20010202 A 5313 39248091 LONGERON DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 LONGERON 30 AT FUSELAGE STATION 617 - 642 WAS CRACKED. MAINTENANCE INSPECTED AND REPLACED THE LONGERON IAW DC-9 SRM 51- 30-5 AND 51-30-2. 2 L 7 2 4F A6WE 2001022000115 20010220 00115 NM 2001 2 20 UPS01434850 1 20010101 A 5753 STRUCTURE BOEING 747 747123F NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, NR 1, 5 & 8 FLAP BALLSCREWS CORRODED AND NR 7 POSITION HAS WORN MOUNT BOLT HOLES. REPLACED 1, 5, 7, AND 8 BALLSCREWS. 2 L 7 4 4F A20WE 2001022000116 20010220 00116 NM 2001 2 20 UPS01434857 1 20010111 A 5340 ANGLE BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, MAIN DECK CORROSION ON AFT CARGO HOLD CEILING SUPPORT ANGLES BS 1840 - 1860 LBL 7 AND RBL 7. NEW SUP PORT ANGLES FABRICATED AND FITTED IAW SRM 51-20-01 AND SRM 51-30-02. 2 L 7 4 4F A20WE 2001022000117 20010220 00117 NM 2001 2 20 UPS01434858 1 20010112 A 5340 69B620501 FITTING BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, MAIN DECK CORROSION ON SUPPORT PLATE UNDER PALLET LOCK TIE DOWN FITTING AT BS 1980 RBL 58. FITTING R EPLACED IAW SRM 51-30-02. 2 L 7 4 4F A20WE 2001022000118 20010220 00118 NM 2001 2 20 UPS01434859 1 20010108 A 5310 BACC30M6 SHEAR TIE BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, MAIN DECK SHEAR TIE IS CRACKED AT BS 1295 BETWEEN STRS 14 &15 LT SIDE. SHEAR TIE FABRICATED IAW SRM 51-30-02. 2 L 7 4 4F A20WE 2001022000119 20010220 00119 NM 2001 2 20 UPS01434860 1 20010106 A 5280 BAC1505100778 ANGLE BOEING 747 747123F NM RT MLG DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, RT WING GEAR STRUT DOOR I/B FAIRING SUPPORT ANGLE IS CRACKED. SUPPORT ANGLE REPLACED IAW SRM 51-30-0 2. 2 L 7 4 4F A20WE 2001022000120 20010220 00120 NM 2001 2 20 UPS01434861 1 20010105 A 5311 FRAME BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, MAIN DECK FUSELAGE FRAME WEB IS CRACKED AT CUTOUT FOR STR AT BS 929 STR 24 LT. REPAIRED IAW SRM 53-1 0-04. 2 L 7 4 4F A20WE 2001022000121 20010220 00121 EU 2001 2 20 KBMA99422 1 20010115 A 2110 5AS35034 COMPRESSOR SNIAS 350 AS350B2 8680813 EU AIR DISTRIBUTION FAILED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 53SH 4856 2009 COIL INOPERATIVE AND HOSE FITTING IS CROSS THREADED. SPRING IN PULLEY ASSEMBLY FAILED AND CAUSED A DEEP GROVE IN RT AFT M/A/BOX STRUT LEG, IT WAS REPLACED ALSO AT THIS TIME. 1 G 7 1 3U H9EU 2001022000122 20010220 00122 EU 2001 2 20 KBMA99427 1 20010120 A 6710 704A44831124 SERVO SNIAS 350 AS350BA 8680817 EU MAIN ROTOR LEAKING E KBMA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 19 180EH 3431 2337 SERVO FORE-AFT, M/R SERVO LEAKING 1 G 7 1 3U NC H9EU 2001022000125 20010220 00125 WP 2001 2 20 TWAA0102309 1 20010131 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9401W 53137 DURING CHECK-C MAINT FOUND FLOOR WEB AT LONGERON 18R, STA 484 TO 503, WAS CORRODED. REMOVED CORROSION PER SRM 53-10-3. INSTALLED REPAIR PER SRM 53-01, PAGE 9, WITH 5/32 AD RIVETS. 2 L 7 2 4F RT A6WE 2001022000126 20010220 00126 EA 2001 2 20 COMA0160203 1 20010203 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 408CA 735 7440 FLAPS FAIL MESSAGE. REPLACED THE LT BPSU. 2 L 7 2 4F RT A21EA 2001022000127 20010220 00127 EU 2001 2 20 KBMA9743410 1 20010117 A 6320 FTD14194 STRUT SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE M/R GEARBOX DAMAGED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 53SH 4856 2009 STRUT DAMAGED DUE TO COMPRESSOR CLUTCH. 1 G 7 1 3U 3 U H9EU E19EU 2001022000129 20010220 00129 EU 2001 2 20 KBMA99428 1 20010120 A 6710 123668P ROD END SNIAS 350 AS350BA 8680817 EU MAIN ROTOR WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 180EH 3431 2337 REPLACED TOP AND BOTTOM PLUS LEFT LATERAL SERVO ROD ENDS. ALL WORN EXCESSIVELY. 1 G 7 1 3U NC H9EU 2001022000130 20010220 00130 WP 2001 2 20 ABXA0100035 1 20010202 A 5311 5911448503 FRAME DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 FUSELAGE FRAME AT STATION 560 LONGERON 29R WAS CORRODED. MAINTENANCE INSPECTED AND REPAIRED THE FRAME IAW DC-9 SRM 53-0 3 PAGE 4E FIG 2A. 2 L 7 2 4F A6WE 2001022000131 20010220 00131 WP 2001 2 20 ABXA0100036 1 20010202 A 5310 99577403 SHEAR TIE DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 FUSELAGE SHEAR TIE AT FRAME 675 WAS CORRODED ON LEFT SIDE AT KEEL AREA. MAINTENANCE REPLACED THE SHEAR TIE IAW DC-9 SRM . 2 L 7 2 4F A6WE 2001022000132 20010220 00132 WP 2001 2 20 ABXA0100037 1 20010202 A 5313 3924810 LONGERON DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 LONGERON 26R WAS CRACKED FROM FUSELAGE STATION 617 TO 642. MAINTENANCE INSPECTED AND REPLACED THE LONGERON IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 2001022000133 20010220 00133 WP 2001 2 20 ABXA0100038 1 20010206 A 3260 0351881008 SOCKET DOUG DOUG DC9 DC932 3022066 WP COCKPIT INTERMITTENT A ABXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 988AX 47084 THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED INTERMITTANTLY AFTER GEAR WAS FULLY RETRACTED, AND CONTINUED TO INT ERMITTANTLY ILLUMINATE FOR THE REMAINDER OF THE FLIGHT. FLIGHT CREW RECYCLED THE LANDING GEAR. MAINTENANCE INSPECTED A ND REPLACED THE RIGHT MAIN LANDING GEAR UNSAFE INDICATION LIGHT SOCKET IAW DC-9 MM 32-61-00. LANDING GEAR INDICATION OP S CHECKED GOOD ON GEAR SWING CHECKS. 2 L 7 2 4F A6WE 2001022000134 20010220 00134 WP 2001 2 20 AT0100054 1 20010206 A 3350 6011779 BATTERY PACK DOUG DC9 DC932 3022066 WP LT NACELLE DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 867AT 47170 FOUND LEFT NACELLE EMERGENCY LIGHT WOULD NOT COME ON. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW DC9 MM 33-50. 2 L 7 2 4F A6WE 2001022000135 20010220 00135 WP 2001 2 20 AT0100055 1 20010206 A 3350 LIGHT DOUG DC9 DC932 3022066 WP CABIN CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 FOUND EMERGENCY LIGHTS JUST INSIDE CABIN INOPERATIVE. CLEANED SLIGHT OXIDATION FROM BATTERIES AND HOLDER, REINSTALLED I AW DC9 MM 33-50. 2 L 7 2 4F A6WE 2001022000137 20010220 00137 NM 2001 2 20 AT0100057 1 20010108 A 5321 FLOOR PANEL BOEING 737 7372L9 1384497 NM FUSELAGE DELAMINATED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 FOUND CABIN FLOOR PANEL AT BS 430 DELAMINATED AND METAL SKIN CRACKED. REMOVED, FABRICATED AND INSTALLED PANEL IAW B737 SRM 53-21-0, 51-40-8, 51-10-1, 53-20-1, 51-10-1, AND REO-L00363. 2 L 7 2 4F RT A16WE 2001022000138 20010220 00138 NM 2001 2 20 AT0100058 1 20010103 A 5321 FLOORBOARD BOEING 737 7372L9 1384497 NM FUSELAGE TORN A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 FOUND CABIN FLOORBOARD AT BS 295 - 360 AFT SIDE WALL METAL SKIN TORN. REMOVED AND REPLACED FLOORBOARD IAW B737 SRM 53-2 0-2, 51-10-1, CMM25-00-66 AND RE0-L00363IR. 2 L 7 2 4F RT A16WE 2001022000139 20010220 00139 NM 2001 2 20 USAA010079 1 20010129 A 5312 BULKHEAD BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND BULKHEAD CRACKED .250 INCH, STATION 178, BULKHEAD, WL 214, RBL 5. INSTALLED DOUBLER PER EO 5300V153. (M) 2 L 7 2 4F A16WE 2001022000140 20010220 00140 NM 2001 2 20 USAA010090 1 20010129 A 5310 BEAM BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND BEAM CRACKED 1.8 INCH, STATION 520, RBL 45.5. REPAIRED DOUBLER PER SB 737-53-1120. (M) 2 L 7 2 4F A16WE 2001022000141 20010220 00141 NM 2001 2 20 USAA010097 1 20010130 A 5320 CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND CLIP CRACKED .75 INCH, INTERCOSTAL FUSELAGE FRAME ATTACHED CLIP. INSTALLED DOUBLER PER SRM 51-40-3. (M) 2 L 7 2 4F A16WE 2001022000144 20010220 00144 NM 2001 2 20 AT0100061 1 20010105 A 5321 FLOOR PANEL BOEING 737 7372L9 1384497 NM FUSELAGE DELAMINATED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 FOUND CABIN FLOOR PANEL IN COCKPIT ENTRY AT BS 295, MUSHY. REMOVED, FABRICATED AND INSTALLED FLOOR PANEL IAW B737 SRM 5 3-20-2, 53-20-1, 51-10-1 AND CMM 25-00-66 AND REO-L000363IR. 2 L 7 2 4F RT A16WE 2001022000145 20010220 00145 NM 2001 2 20 AT0100062 1 20010103 A 5320 PANEL BOEING 737 7372L9 1384497 NM CARGO BAY CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 FOUND FORWARD PIT CEILING PANEL AT BS 380 - 420 HAS SEVERAL TORN AND CRACKED AREAS. REMOVED, FABRICATED, AND INSTALLED PANEL IAW REO-L00361 REV A. 2 L 7 2 4F RT A16WE 2001022000146 20010220 00146 WP 2001 2 20 ABXA0100039 1 20010201 A 5250 AR25291GR41 LATCH DOUG DC9 DC941 302207N WP COCKPIT DEFECTIVE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 COCKPIT DOOR WOULD NOT OPEN FROM THE OUTSIDE. MAINTENANCE INSPECTED AND REPLACED THE COCKPIT DOOR LATCH IAW DC-9 MM. 2 L 7 2 4F A6WE 2001022000147 20010220 00147 NE 2001 2 20 ARWA0010201 2 20010203 A 7311 715447 OIL COOLER DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE NR 1 ENGINE DAMAGED A ARWA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 19 8968U 46069 671150 RETURNED TO MKJP SHORTLY AFTER THE TAKEOFF DUE TO HIGH OIL TEMP NR 1 ENGINE. PRECAUTIONARY ENGINE SHUTDOWN AT 22:28Z TE MP 142 DEGREES, FOLLOW BY ABNORMAL CHECK LIST OIL PRESSURE WAS 47 PSL. WINDMILLING OIL PRESSURE 8 PSI. REMOVED AND REP LACED NR 1 ENGINE FUEL/OIL COOLER IAW DC8 MM 79-20-2. REMOVED AND REPLACED NR 1 ENGINE OIL TEMP SENSOR IAW DC8 MM 79-34 -1. PERFORMED ENGINE RUN UP, FOUND NORMAL IAW MM 71-00. 2 L 7 4 4F 4 F 4A25 1E8 2001022000148 20010220 00148 WP 2001 2 20 ARWA0010202 1 20010204 A 2910 23722884 O-RING DOUG DC8 DC863F 302198F WP RT WING AILERON DAMAGED A ARWA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 19 661AV 45969 CLIMBOUT A LOSS OF HYDRAULIC FLUID DOWN TO STAND PIPE. AFTER LANDING MIA, FOUND HEAVY HYDRAULIC LEAK COMING FROM RT WIN G AILERON SWIVEL. INSPECTED SWIVEL AND FOUND BOTH O-RINGS DAMAGED. REMOVED AND REPLACED O-RINGS AS REQUIRED. FOUND NO RMAL, NO LEAKS IAW DC-8 MM 27-11-0. 2 L 7 4 4F 4A25 2001022000149 20010220 00149 NM 2001 2 20 UPS01434856 1 20010102 A 5754 65B0247110 HINGE BOEING 747 747123F NM LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, RT WING L/E NR 15 KRUEGER FLAP O/B FOLDING FAIRING ATTACH HINGE FITTING IS CRACKED. P/N 65B02471- 10. DUE TO ADDITIONAL DAMAGE ON FLAP, FLAP REPLACED. 2 L 7 4 4F A20WE 2001022000150 20010220 00150 NM 2001 2 20 UPS01634862 1 20010205 A 2612 FIRE LOOP BOEING 767 76734AF 1385212 NM LT ENGINE FALSE INDICATION A IPXA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 305UP 27243 INSPECTION TYPE:N/A, FIRE/OVHT SYS EICAS MSG ON DESCENT. RESET W/EICAS MSG OUT-TWO OCCURRANCES. PERFORMED ENG FIRE DET ECTION SYS BITE PROCEDURE IAW 26 11 00 FIG 104. RESEATED AFOLTS CARDS M10224 & M10274 PER FIM MANUAL SYS TESTS GOOD. O K FOR CONTINUED SERVICE. 2 L 7 2 4F RT A1NM 2001022000151 20010220 00151 WP 2001 2 20 UPS01834831 1 20010201 A 5340 FITTING DOUG DC8 DC873F 302199F WP BULKHEAD CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:IN, LT W/W OUTBOARD FWD BULKHEAD HAS 4 CRACKS AROUND HYD LINE BULKHEAD FTG (MARKED). *S/D* REMOVED DAM AGED MATERIAL. INSTALLED DOUBLER PER SRM 53-2-0 FIG 23. 2 L 7 4 4F RT 4A25 2001022000152 20010220 00152 SO 2001 2 20 SWIA972335 1 20010131 A 3150 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CENTRAL WARNING DAMAGED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 215SW 120281 ON TAKEOFF ROLL RECEIVED A TRIPLE CHIME WITH AURAL TRIM WARNING. AIRCRAFT TRIM WAS SELECTED IN GREEN ARC TO 34 PERCENT. ABORTED TAKEOFF. FOUND PIN-L AT PO349 SEVERED. INSTALLED NEW PINS AT JO349 AND PO349 IAW 20-00-00. GROUND OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001022000166 20010220 00166 NM 2001 2 20 AALA20010161 1 20010119 A 5730 SKIN BOEING 727 727227 1384078 NM WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 722AA 20730 TUL - FOUND CORROSION ON BOTTOM OF CENTER WING SKIN ABOVE LEFT AND RIGHT HEAT EC4. REMOVED CORROSION AND INSTALLED TWO 2024T3-.080 TRIPLERS, ONE SET BETWEEN STRINGER 5/6 AND ONE SET AT STRINGER 3 ENGINE DISPOSITION DATED 1-13-2001. (M) 2 L 7 3 4F A3WE 2001022000167 20010220 00167 NM 2001 2 20 AALA20010162 1 20010119 A 5320 ANGLE BOEING 727 727227 1384078 NM CARGO BAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 722AA 20730 TUL - FOUND AIRCRAFT CARGO DOOR AFT CUTOUT THRESHOLD LOWER CHORD ANGLE CORRODED FORWARD CORNER BETWEEN STATION 950D AND 950E. REPAIRED PER ESO11697 DATED 1/19/2001. (M) 2 L 7 3 4F A3WE 2001022000168 20010220 00168 NM 2001 2 20 AALA20010164 1 20010118 A 5330 SKIN BOEING 727 727227 1384078 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 722AA 20730 TUL - FOUND CORROSION ON TOP SKIN SURFACE. REMOVED CORROSION AND INSTALLED REPAIR STRAP PER ESO 11697 DATED 1-15-2001. (M) 2 L 7 3 4F A3WE 2001022000169 20010220 00169 NM 2001 2 20 AALA20010165 1 20010118 A 5330 SKIN BOEING 727 727227 1384078 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 722AA 20730 TUL - FOUND CORROSION ON SKIN SURFACE. REMOVED CORROSION AND INSTALLED HI-LOK WITH WASHER PER ESO 11697 DATED 1-16-01. (M) 2 L 7 3 4F A3WE 2001022000170 20010220 00170 NM 2001 2 20 AALA20010158 1 20010123 A 5730 SKIN BOEING 727 727227 1384078 NM WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 722AA 20730 TUL - FOUND LOWER WING SKIN ABOVE RIGHT PRIMARY HEAT EXCHANGER IS INFECTED WITH MODERATE TO HEAVY CORROSION LBL 32-RBL 3 2 STRINGER 3-5, STATION 805-820. REMOVED CORROSION AND INSTALLED DOUBLER AND TRIPLER .080, 2024-T3 (TWO EACH) PER SRM 5 7-30-3. (M) 2 L 7 3 4F A3WE 2001022000171 20010220 00171 NM 2001 2 20 BJNA010103 1 20010129 A 3350 362624 LIGHT BOEING 737 737282 13844AT NM CABIN INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 SW 21 233TM 23043 FLOOR EMERGENCY LIGHT LAMP INOPERATIVE AT ROW 4 D/E/F. AIRCRAFT RELEASED PER MEL 33-19, ITEM TRANSFERRED TO DMI LOG NR 0127, ITEM PLACARDED. REF MEL 33-19, DMI 0127, REMOVED AND REPLACED LAMP ON FLOOR TRACK PER LUMINESCENT CCM2-5-1. (M) 2 L 7 2 4F RT A16WE 2001022000172 20010220 00172 SO 2001 2 20 C2XA01TY003 1 20010201 A 5320 14522459001 ANGLE EMB 145 EMB145 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 TYS - DURING A SCHEDULED 1C INSPECTION, RAMP ANGLE HAS CORROSION AT CARBON FIBER CROSS BEAM ABOVE FRAMES 19 AND 20, BETW EEN STRINGERS 21L AND 21R. MAINTENANCE REMOVED AND REPLACED CARBON FIBER BEAM AND RAMP ANGLE IAW EMB 145 SRM 51-40-02. REPAIRS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001022000174 20010220 00174 WP 2001 2 20 AALA20010130 1 20010109 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 TUL - FOUND CUSP CORRODED RIGHT STATION 1080. CUT OUT CORROSION, CUSP DOUBLER INSTALLED AS PER SRM 53-01 FIG 4 SHT 3. (M) 2 L 7 2 4F RT A6WE 2001022000175 20010220 00175 NM 2001 2 20 AALA20010115 1 20010119 A 5313 STRINGER BOEING 727 727223 1384074 NM FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 891AA 22007 TUL - FOUND STRINGER 2L CUT INTO AT STATION 466. REPAIRED STRINGER 26L AT STATION 466 PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 2001022000176 20010220 00176 NM 2001 2 20 AALA20010103 1 20010119 A 5313 STRINGER BOEING 727 727223 1384074 NM FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 891AA 22007 TUL - FOUND STRINGER CUT AND DAMAGED, FS 457, 12 INCHES BY 1 INCH. REMOVED AND REPLACED STRINGER PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 2001022000177 20010220 00177 NM 2001 2 20 AALA20010104 1 20010119 A 5311 FRAME BOEING 727 727223 1384074 NM FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 891AA 22007 TUL - FOUND BELL FRAME CUT INTO, STATION 460, 12 INCHES BY 1 INCH. REMOVED AND REPLACED BELL FRAME PER SRM 51-10-01. ( M) 2 L 7 3 4F A3WE 2001022000178 20010220 00178 NM 2001 2 20 AALA20010102 1 20010119 A 5313 STRINGER BOEING 727 727223 1384074 NM FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 891AA 22007 TUL - FOUND STRINGER DAMAGED, FS 463, 12 INCHES BY 2 INCHES. REPAIRED STRINGER 27 LEFT STATION PER SRM 53-10-03. (M) 2 L 7 3 4F A3WE 2001022000179 20010220 00179 NM 2001 2 20 AALA20010091 1 20010115 A 5313 STRINGER BOEING 727 727223 1384074 NM FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 891AA 22007 TUL - FOUND STRINGER 25 LEFT CUT INTO STATION 471. AIRCRAFT DAMAGED BY GROUND EQUIPMENT. SPLICED IN NEW SECTION OF STR INGER 25 LEFT AT STATION 471 PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 2001022000180 20010220 00180 NM 2001 2 20 AALA20010092 1 20010115 A 5311 FRAME BOEING 727 727223 1384074 NM FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 891AA 22007 TUL - FOUND FRAME CUT IN AFT AND OF E/E DOOR OPENING STATION 450 STATION 27 LEFT TO 27 RIGHT. REMOVED AND REPLACED FRAM E PER SRM 51-10-1. AIRCRAFT DAMAGED BY GROUND EQUIPMENT. (M) 2 L 7 3 4F A3WE 2001022000181 20010220 00181 NM 2001 2 20 AALA20010093 1 20010115 A 5320 CHANNEL BOEING 727 727223 1384074 NM FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 891AA 22007 TUL - FOUND CHANNEL DAMAGED STRINGER 28 LEFT TO BELLFRAME STATION 460. AIRCRAFT DAMAGED BY GROUND EQUIPMENT. REMOVED A ND REPLACED CHANNEL PER SRM 51-10-4. (M) 2 L 7 3 4F A3WE 2001022000182 20010220 00182 NM 2001 2 20 AALA20010094 1 20010105 A 5320 ANGLE BOEING 727 727223 1384074 NM FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 891AA 22007 TUL - FOUND VERTICAL ANGLE DAMAGED ON WEB LEFT SIDE OF E/E DOOR OPENING STATION 460 BETWEEN STRINGER 27/28 LEFT. AIRCRA FT DAMAGED BY GROUND EQUIPMENT. REMOVED AND REPLACED VERTICAL ANGLE PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 2001022000183 20010220 00183 NM 2001 2 20 AALA20010095 1 20010116 A 5311 FRAME BOEING 727 727223 1384074 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 891AA 22007 TUL - FOUND STATION 720E STRINGER 286 FRAME CRACKED. AIRCRAFT DAMAGED BY GROUND EQUIPMENT. REMOVED DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 2001022000197 20010220 00197 NM 2001 2 20 AWXA0001261 1 20010206 A 2761 MS219024 O-RING BOEING BOEING 737 737301 1384611 NM NR 5 SPOILER ACT CRACKED A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 28 324AW 3923 23261 PHX - AIR TURNBACK - 1/31/01 - AFTER DEPARTURE FROM PHX THE AIRCRAFT LOST A-SYSTEM HYDRAULIC QUANTITY AND THE AIRCRAFT R ETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. MAINTENANCE FOUND A UNION ON THE NR 5 INBOARD GROUND SPOILER ACTUATOR LE AKING, CRACKED. THE UNION AND O-RING WERE REPLACED. THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP SHOWED SIGNS OF LEAKAGE AND WAS CHANGED AS WELL BUT THE CAUSE OF THE QUANTITY LOSS WAS THE SPOILER ACTUATOR UNION. 2 L 7 2 4F RT A16WE 2001022000198 20010220 00198 EU 2001 2 20 01FDEA00077 1 20010206 A 2131 CONTROLLER AIRBUS 310 A310222 3930315 EU CABIN PRESSURE FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 416FE 288 A/C WOULD NOT PRESSURIZE AFTER T/O. 2 L 7 2 4F RT A35EU 2001022000201 20010220 00201 GL 2001 2 20 01FDEA00078 2 20010206 A 7200 ENGINE DOUG DC10 DC1010F 3022111 WP GE CF6 CF66D 30020 GL NR 3 OVERHEATED A FDEA C ABORTED TAKEOFF R M J PARTIAL RPM/PWR LOSS OVER TEMP WARNING INDICATION TO TAKEOFF 1 SO 25 051FE 47805 ON T/O NR 3 ENGINE N1 ONLY REACHED 90.5 PERCENT WITH FULL THROTTLE. NR 3 EGT READ 80 - 100 DEG HOTTER THAN 1 & 2. 2 L 7 3 4F 4 F A22WE E23EA 2001022000202 20010220 00202 EU 2001 2 20 01FDEA00076 1 20010206 A 7830 WARNING LIGHT AIRBUS 300 A300F4605R 3930327 EU NR 2 ENGINE T/R ILLUMINATED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 686FE 804 DURING T/O ROLL, RECEIVED ECAM WARNING NR 2 ENG REVERSER PRESSURIZED. AC RELEASED FOR SERVICE PER MEL 78-1. 2 L 7 2 4F RT A35EU 2001022000203 20010220 00203 EU 2001 2 20 01FDEA00079 1 20010206 A 3230 DAMPER AIRBUS 310 A310203 EU RT MLG PITCH FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 428FE 248 LANDING GEAR FAILED TO RETRACT WITH POSITION DETECTOR ON BOTH NR 1 AND 2 POS. REMOVED AND REPLACED RT MLG PITCH DAMPER PER MM REF 32-11-15. PERF GEAR SWING IN BOTH POS PER MM REF 7-11. OPS CK GOOD. 2 L 7 2 4F RT A35EU 2001022000204 20010220 00204 NM 2001 2 20 PCAA0102004 1 20010206 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 811AW 201 LGA FLIGHT 3909. CREW REPORTED ROW ONE FLOOR EMERGENCY LIGHT STRIP IS INOPERATIVE, FOUR RED LIGHTS OUT. MAINTENANCE IN SPECTED AND REPAIRED FIVE BROKEN WIRES. EMERGENCY LIGHTS CHECKED GOOD AT THIS TIME. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001032900170 20010329 00170 NM 2001 3 29 01FDEA00080 1 20010206 A 5314 65564413 KEELBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION ON STRAP ON LT KEEL BEAM BS 950E - 950E+16 IN AFT CARGO BAY. *S/D* REMOVED AND REPLACED OUT OF LIMIT CORROSI ON PER IAW FEDEX SRM 53-10-1, EA 7-5310-56529. 2 L 7 3 4F RT A3WE 2001022000205 20010220 00205 NM 2001 2 20 UPS01234888 1 20010125 A 5330 SKIN BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C, CRACK IN FUSELAGE SKIN AT BS 243.7 LT. REPAIR CARRIED OUT IAW SRM 51-30-03. 2 L 7 3 4F A3WE 2001022000206 20010220 00206 NM 2001 2 20 UPS01234894 1 20010124 A 5714 FRAME BOEING 727 72722C 138400F NM CENTER WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C, RIVET POPPED AND EVIDENCE OF CORROSION ON WING CENTER SECTION REAR SPAR LWR CHORD BS 870. REPAIR CAR RIED OUT IAW SRM 51-30-02 & SRM 51-20-4 AND DRAWING 65C215 66. 2 L 7 3 4F A3WE 2001022000207 20010220 00207 EA 2001 2 20 A6WA200100003 1 20010117 A 7110 COWL DOOR CNDAIR CL600 CL6002B19 EA RT ENGINE SEPARATED A A6WA O OTHER D INFLIGHT SEPARATION LD LANDING 1 GL 31 409AW 7447 LOWER ENGINE COWL DOOR (RT) FELL OFF ON LANDING. MAINTENANCE REPLACED THE RT ENGINE LOWER COWL DOOR. 2 L 7 2 4F RT A21EA 2001022000208 20010220 00208 NM 2001 2 20 A6WA200100004 1 20010131 A 2435 8160121 STARTER GEN DORNER DO32 DO328100 2996000 NM LT ENGINE FAILED A A6WA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION NR NOT REPORTED 1 GL 31 338PH 1713 621 3029 LEFT GENERATOR FAILED IN FLIGHT, STRANGE VIBRATION IN LEFT POWER LEVER AFTER FAILURE. MAINTENANCE REMOVED AND REPLACED STARTER GENERATOR. 2 H 7 2 4T RT A45NM 2001022000209 20010220 00209 NM 2001 2 20 A6WA200100005 1 20010128 A 3020 001A716E1000010 INTAKE DUCT DORNER DO32 DO328100 2996000 NM LT ENGINE DELAMINATED A A6WA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 GL 31 334PH 1594 1594 3012 LEFT ENGINE LOST POWER TORQUE WENT FROM 85 PERCENT TO 45 PERCENT FOLLOWED BY LEFT ENGINE DEICE FAIL. POWER NORMAL WITH LEFT ENGINE DEICE OFF. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE INTAKE BOOT ASSEMBLY, OPERATIONAL CHECK OK. 2 H 7 2 4T RT A45NM 2001022000210 20010220 00210 SO 2001 2 20 COMA0110033 1 20010204 A 5310 12034416002 SHEAR TIE EMB 120 EMB120RT SO FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 268CA 21366 120262 DURING 400 FLIGHT CYCLE CHECK, A CRACKED RIVET HEAD WAS DISCOVERED ON THE RIGHT SIDE OF AIRCRAFT FUSELAGE ALONG FRAME 9. UPON FURTHER INVESTIGATION, THE SKIN SUPPORT BRACKET IN WHICH SAID RIVET PASSES THROUGH WAS CRACKED. THE SUPPORT BRAC KET WAS REMOVED AND A SERVICEABLE BRACKET WAS INSTALLED. WORK WAS DONE IN ACCORDANCE WITH AERODESIGN REPORT 660-1, IR D ATED 2-16-93. 2 L 7 2 4T RT A31SO 2001022000211 20010220 00211 EA 2001 2 20 COMA0160206 1 20010205 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 EA LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 713CA 7245 LT LOWER WING PLANK CRACKED AT ACCESS HOLES, 540 CB WS 76.161, 550 AB WS 163.00 AND 550 FB WS 274.319. BLENDED OUT DAMA GE AND ROTO-PEENED AS REQUIRED IAW REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 2001022000212 20010220 00212 EA 2001 2 20 COMA0160207 1 20010203 A 5320 601R31171 ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 17981 7022 ANGLES AT RBL 27 AND LBL 27 AND INTERCOSTALS AT RBL/LBL 36 AT FS 484 ARE CRACKED. REMOVED AND REPLACED ANGLES IAW WVAC EO 601R-53-2197. 2 L 7 2 4F RT A21EA 2001022000213 20010220 00213 EA 2001 2 20 COMA0160208 1 20010204 A 5320 6003106819 SUPPORT FITTING CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 7022 FLOOR SUPPORT FITTING OUTBOARD SIDE OF RBL 9 AT FS 460 AND FS 513 CRACKED. REMOVED AND REPLACED SUPPORT FITING IAW WVAC EO 601R-53-2196. 2 L 7 2 4F RT A21EA 2001022000214 20010220 00214 EA 2001 2 20 COMA0160209 1 20010123 A 5320 SPLICE CNDAIR CL600 CL6002B19 EA FUSELAGE MISMANUFACTURED A COMA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 924CA 7026 TWO SPLICE PLATES 601R31030-77 WERE FABRICATED INCORRECTLY BY THE MANUFACTURER. FABRICATED TWO DOUBLER PLATES FROM 7075 -16-032 IAW WVAC EO 601R-53-2158. INSTALLED DOUBLER PLATES IAW WVAC EO 601R-53-2158. 2 L 7 2 4F RT A21EA 2001022000217 20010220 00217 WP 2001 2 20 MWEA010145 1 20010205 A 7710 7958994ABX3 SENSE LINE DOUG DC9 DC932 3022066 WP RT ENGINE CHAFED A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 401ME 47133 FLIGHT CREW REPORTED RIGHT ENGINE EXHAUST PRESSURE RATIO INDICATION READS HIGH. ALL OTHER INDICATIONS READ NORMAL. MAI NTENANCE FOUND PRESSURE RATIO SENSE LINE CHAFED AND REPLACED THE LINE. 2 L 7 2 4F A6WE 2001022000218 20010220 00218 EU 2001 2 20 A6WA200100008 1 20010130 A 5320 WEB BAG BAE146 BAE146200A 1500266 EU FUSELAGE DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 DAMAGE TO WEBS ABOVE AND BELOW FORWARD PASSENGER DOOR DAMPER CAN. MAINTENANCE REMOVED AND REPLACED DAMPER CAN LOWER AND UPPER WED ASSEMBLIES IAW BAE 146 SRM. 2 H 7 4 4F RT A49EU 2001022000219 20010220 00219 NM 2001 2 20 UPS01234884 1 20010124 A 5310 STRUCTURE BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C, SUSPECT CRACK IN UPPER LIGHTENING HOLE 6 O CLOCK POSITION BS 1300 LT. CRACK STOPPED DRILLED IAW SRM 51-10-1, CRACK FOUND TO BE WITHIN LIMITS. 2 L 7 3 4F A3WE 2001022000220 20010220 00220 NM 2001 2 20 UPS01234885 1 20010129 A 5310 DOOR FRAME BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C, CRACK ON FWD LT CORNER OF FWD LWR NOSE ACCESS DOOR ON INNER LIP OF DOOR FRAME. REPAIR CARRIED OUT IA W SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2001022000221 20010220 00221 NM 2001 2 20 UPS01234886 1 20010125 A 5350 FLANGE BOEING 727 72722C 138400F NM FAIRING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C, FAIRING 3608 AFT SUPPORT FRAME AFT FLANGE CORRODED. REPAIR CARRIED OUT IAW SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2001022000222 20010220 00222 NM 2001 2 20 UPS01234887 1 20010125 A 5320 STIFFENER BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C, ON INSP HORIZ STIFFENER ON LWR BODY 740 FRAME FOUND CORRODED AT BBL 0. STIFFENER REMOVED IAW SRM 51- 30-02, STIFFENER REPLACED IAW SRM 51-10-02. 2 L 7 3 4F A3WE 2001022000223 20010220 00223 NM 2001 2 20 UPS01234890 1 20010124 A 5313 STRINGER BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C, CORROSION ON STR 18L AT BS 360. REPAIR CARRIED OUT IAW SRM 51-10-54 AND SRM 51-30-2. 2 L 7 3 4F A3WE 2001022000224 20010220 00224 NM 2001 2 20 UPS01234893 1 20010122 A 5320 STRUCTURE BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C, SUSPECT CRACK IN UPPER LIGHTENING HOLE 70 C POS BS 1243 LT AFT AIRSTAIRS AREA. REPAIR CARRIED OUT IA W SRM 51-10-1. 2 L 7 3 4F A3WE 2001022000225 20010220 00225 NM 2001 2 20 UPS01634905 1 20010206 A 7722 SHUNT BOEING 767 76734AF 1385212 NM RT ENGINE EGT FAILED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 319UP 27758 INSPECTION TYPE:IN PILOT REPORT - RT ENG EGT FLUCTUATES. INSPECTED CONNECTIONS ON THERMOCOUPLES AND CONNECTIONS ON JUNC TION BOX. RAN RT ENG ALL INDICATIONS NORMAL AT THIS TIME. REMOVED AND REPLACED EGT SHUNT. 2 L 7 2 4F RT A1NM 2001022000226 20010220 00226 NM 2001 2 20 01FDEA00049 1 20010130 A 5311 651592533 FRAME BOEING 727 727227 1384078 NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 MECHANICAL DAMAGE ON FRAME, BS 440 AT STR 6R. *S/D* REMOVED, REPLACED AND FAB PER IAW FEDEX SRM 51-20-1, 51-10-2, 53-1 0-4, 51-30-2. 2 L 7 3 4F A3WE 2001022000227 20010220 00227 EU 2001 2 20 01FDEA00072 1 20010203 A 5210 ROLLER AIRBUS 310 A310203 EU PAX DOOR DIRTY A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 407FE 254 AFT T/O RIGHT FWD ENTRY DOOR LIGHT CAME ON. CLEANED ICE FROM UPR FWD ROLLER HOOK BRACKET. INSP MECHANICAL LINKS AND RO LLERS, NO DEFECTS NOTED. DOOR OPS NORMAL. 2 L 7 2 4F RT A35EU 2001022000228 20010220 00228 NM 2001 2 20 AALA20010032 1 20010108 A 5313 STRINGER BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 871AA 21383 TUL - FOUND STATION 720D STRINGER 28R CORRODED AROUND FASTENER HOLES ON STRINGER. INSTALLED REPAIR STRAP AT STRINGER 28 RT STATION 720D PER ESO 11697 DATED 1/4/2001. (M) 2 L 7 3 4F A3WE 2001022000229 20010220 00229 NM 2001 2 20 AALA20010033 1 20010106 A 5330 PANEL BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 871AA 21383 TUL - FOUND PANEL BULGING IN RIGHT RAM AIR INLET AFT OF DOOR ACT, BS 720B-720L. INSTALLED REPAIR DOUBLER AT RAM AIR SCO OP BETWEEN STRINGER 28L AND 28R PER ESO 11697 DATED 01/03/2001. (M) 2 L 7 3 4F A3WE 2001022000230 20010220 00230 NM 2001 2 20 AALA20010034 1 20010104 A 5310 DOOR FRAME BOEING 727 727223 1384074 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 871AA 21383 TUL - FOUND CRACK INDICATION WITH HFEC UNDER STOP FITTING AT TOP OF FITTING, FS 950. STOP DRILLED CRACKS FABRICATED AND INSTALLED REPAIR DOUBLER IAW SB 727-53-AO199. (M) 2 L 7 3 4F A3WE 2001022000231 20010220 00231 NM 2001 2 20 AALA20010174 1 20010130 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 865AA 21370 TUL - FOUND CRACK INDICATED IN OUTERSKIN BETWEEN RIVET AND DOOR RADIUS LOWER AFT CORNER, 420. INSTALLED REPAIR DOUBLER AT FORWARD GALLEY DOOR CUTOUT LOWER AFT CORNER IAW SERVICE BULLETIN 727-53-018 FIG 2. (M) 2 L 7 3 4F A3WE 2001022000232 20010220 00232 NM 2001 2 20 AALA20010175 1 20010127 A 5313 STRINGER BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 865AA 21370 TUL - FOUND CORROSION IN CENTER OF STRINGER 27R STATION 738-739. CUT OUT DAMAGED AND INSTALLED STRINGER SPLICE PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 2001022000233 20010220 00233 NM 2001 2 20 AALA20010176 1 20010130 A 5313 STRINGER BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 865AA 21370 TUL - FOUND CORROSION IN STRINGER 28R STATION 965-973. INSTALED NEW STRINGER SECTION AND REPAIR SPLICE PER ESO 11697 DA TED 1-25-01. (M) 2 L 7 3 4F A3WE 2001022000234 20010220 00234 NM 2001 2 20 AALA20010177 1 20010126 A 5313 STRINGER BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 865AA 21370 TUL - FOUND CORROSION IN CENTER OF STRINGER 27R STATION 704-705. REMOVED STRINGER AND SPLICE. INSTALLED NEW STRINGER A ND SPLICE PER SRM 53-10-03. (M) 2 L 7 3 4F A3WE 2001022000235 20010220 00235 NM 2001 2 20 AALA20010106 1 20010111 A 5310 SHEAR TIE BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 863AA 21090 TUL - FOUND FRAME SHEAR TIE CORRODED OUTBOARD OF STRINGER 26R STATION 720F. REPLACED CORRODED SHEAR TIE SRM 51-10-1. ( M) 2 L 7 3 4F A3WE 2001022000236 20010220 00236 NM 2001 2 20 AALA20010107 1 20010112 A 5320 TORQUE BOX BOEING 727 727223 1384074 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 863AA 21090 TUL - FOUND UPPER LIGHTENING HOLE IN RIGHT TORQUE BOX AT STATION 1248 IS CRACKED. STOP DRILLED, FABRICATED AND INSTALLE D DOUBLER PER SRM 51-40-2. (M) 2 L 7 3 4F A3WE 2001022000237 20010220 00237 NM 2001 2 20 AALA20010108 1 20010112 A 5320 TORQUE BOX BOEING 727 727223 1384074 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 863AA 21090 TUL - FOUND LOWER LIGHTENING HOLE IN RIGHT TORQUE BOX AT STATION 1240 IS CRACKED. STOP DRILLED, FABRICATED AND INSTALLE D DOUBLER, PER SRM 51-40-2. (M) 2 L 7 3 4F A3WE 2001022000238 20010220 00238 NM 2001 2 20 AALA20010110 1 20010115 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE BULGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 863AA 21090 TUL - FOUND 1 INCH SKIN BULGE, STATION 1071-1022. INSTALLED SKIN DOUBLER PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 2001022000239 20010220 00239 NM 2001 2 20 AALA20010111 1 20010114 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 863AA 21090 TUL - FOUND CORROSION ON SKIN OUTBOARD SIDE OF STRINGER 27L, STATION 1010-1012. INSTALLED DOUBLER ON SKIN AS PER SRM 53 -30-3 FIG 1. (M) 2 L 7 3 4F A3WE 2001022000240 20010220 00240 NM 2001 2 20 AALA20010112 1 20010115 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 863AA 21090 TUL - FOUND STATION 1130 FLOORBEAM HAS CORROSION ON TOP FLANGE AT APPROX LBL 25-LBL 10. FABRICATED STRAP TREATED AND PR IMED AND INSTALLED PER SRM 53-10-07. (M) 2 L 7 3 4F A3WE 2001022000241 20010220 00241 NM 2001 2 20 AALA20010113 1 20010115 A 5313 STRINGER BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 863AA 21090 TUL - FOUND CORROSION ON STRINGER 27L OUTBOARD EDGE STATION 1011-1121. INSTALLED NEW STRINGER SECTION AND SPLICE AS PE SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 2001022000242 20010220 00242 NM 2001 2 20 AALA20010121 1 20010109 A 5730 SKIN BOEING 727 727223 1384074 NM WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 875AA 21387 TUL - FOUND BOTTOM CENTER WING SKIN HAS CORROSION AROUND HI-LOCK IN PLEUM CHAMBER ABOVE RIGHT PRIMARY HEAT EXCHANGER STR INGER 5 RBL 27. REMOVED CORROSION AND INSTALLED DOUBLER PER ESO 11697 DATED 1108101. (M) 2 L 7 3 4F A3WE 2001022000243 20010220 00243 NE 2001 2 20 AALA20010097 2 20010118 A 7230 BLADE BOEING 727 727227 1384078 NM PWA JT8 JT8D9 52048 NE NR 1 ENGINE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 722AA 20730 TUL - FOUND NR 1 ENGINE FAN BLADE CRACKED AT FIR TREE AS VIEWED FROM AFT SIDE OF DISH. REMOVED AND REPLACED FAN ASSY PE R WORK CARD 11-17. (M) 2 L 7 3 4F 4 F A3WE E2EA 2001022000244 20010220 00244 NM 2001 2 20 AALA20010159 1 20010117 A 5330 LAP JOINT BOEING 727 727227 1384078 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 722AA 20730 TUL - FOUND STRINGER 26L SKIN LAP 4 INCH LONG AREA BULGING AT RIVETS STATION 661-665. FOUND CORROSION IN SKIN LAP. CUT OUT CORRODED AREA AND INSTALLED DOUBLER AND FILLER PER SRM 53-30-3 FIG 5 SHEET 5. (M) 2 L 7 3 4F A3WE 2001022000262 20010220 00262 NE 2001 2 20 20010208CW004 2 20010109 A 7261 CHIP DETECTOR SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE ENGINE CONTAMINATED E HCMA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 13 194BH 2903 9402 JAN 9, 2001 WHILE ON A SIGHTSEEING FLIGHT, THE PILOT EXPERIENCED AN ENGINE CHIP WARNING. HE MADE A PRECAUTIONARY LANDIN G. A MECHANIC WAS FLOWN TO THE SCENE AND A SMALL HAIRLIKE SLIVER WAS FOUND ON THE MAGNETIC PLUG. THE CHIP PLUG WAS CLE ANED AND THE AIRCRAFT WAS GROUND RUN. LEAK CHECKED WITH NO FURTHER INCIDENT. 1 G 7 1 3U 3 U H9EU E19EU 2001022000275 20010220 00275 2001 2 20 DHL2001741003 4 20010206 A 3415 INDICATOR BOEING 727 7272Q9 138448M NM COCKPIT MALFUNCTIONED A DHLA D RETURN TO BLOCK L N NO TEST FALSE WARNING TX TAXI/GRND HDL 1 SO 01 741DH 21931 F/O AIRSPEED INDICATOR GOT MACH AND UMO FLAGS IN VIEW DURING TAXI-OUT. UMO FLAG IN VIEW ON F/O MACH A/S INDICATOR NR 2 MACH A/S AURAL WARNING WOULD NOT TEST. UMO FLAG MOVED TO ITEM 2M, MACH FLAG DEF PER MEL 34-3-2 CTRL NR 4287 CAT C PLA I NSTALLED. SEE RESTRICTIONS. 2) DEF PER MEL 34-4-1 CTRL NR 4288 CAT B PLA INSTALLED SEE RESTRICTIONS. 2 L 7 3 4F RT A3WE 2001022000276 20010220 00276 WP 2001 2 20 TWAA0102303 1 20010130 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT AT THE AFT ACCY COMPT, STA 1418, BETWEEN LONGERON 13R AND 14R, THE FORMER FOOT WAS CRACKED. REPLAC ED FORMER FOOT PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-10. 2 L 7 2 4F A6WE 2001022000278 20010220 00278 NM 2001 2 20 AALA20010160 1 20010122 A 5320 PAN BOEING 727 727227 1384078 NM LAVATORY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 722AA 20730 TUL - FOUND LAVATORY PAN CORRODED AROUND LAV TANK WEB FORWARD MOUNTS AND SURROUNDING WEB LBL 36, BS 1146. BLENDED OUT C ORROSION AND INSTALLED DOUBLER PER SRM 51-40-2 PAGE 1. (M) 2 L 7 3 4F A3WE 2001022000279 20010220 00279 NM 2001 2 20 AALA20010163 1 20010119 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 722AA 20730 TUL - FOUND CORROSION ON TOP OF FORWARD UPPER CHORD OF FS 1130 FLOORBEAM LBL 26-60. BLENDED OUT CORROSION AND INSTALLED REPAIR STRAP PER AARD 53-10-07-1. (M) 2 L 7 3 4F A3WE 2001022000280 20010220 00280 NM 2001 2 20 AALA20010090 1 20010115 A 5311 FRAME BOEING 727 727223 1384074 NM FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 891AA 22007 TUL - FOUND FRAME DAMAGED 1 INCH BY 3 INCHES, RIGHT SIDE OF E/E DOOR OPENING STATION 443, STRINGER 27 RT. DAMAGE CAUSED BY GROUND EQUIPMENT. REMOVED AND REPLACED DAMAGED FRAME PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 2001022000282 20010220 00282 NM 2001 2 20 20010220SG001 1 20010201 A 2781 SLAT BOEING 757 757200 1384950 NM WING L/E LACK OF LUBE A N8TA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 19 506NA 24771 AFTER TAKEOFF UPON RETRACTION, ''LE SLAT DISAGREE'' EICAS MESSAGE ILLUMINATED. AIRCRAFT RETURNED TO DEPARTURE STATION. LUBRICATED SLAT SYSTEM IAW FAULT ISOLATION MANUAL 27-81 AND AMM 12-21-08. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2001022000283 20010220 00283 NM 2001 2 20 GAIA01044OP 1 20010207 A 2612 FIRE DETECTOR BOEING 727 727223 1384074 NM APU MALFUNCTIONED A GAIA F D ACTIVATE FIRE EXT. RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 07 856AA 20997 FLT 2025 - OAK-DEN - AFTER BLOCKING OUT FROM PARKING, THE APU FIRE WARNING SOUNDED. THE CREW PERFORMED EMERGENCY APU FI RE CHECKLIST AND ACTUATED THE APU FIRE HRD BOTTLE. THE AIRCRAFT RETURNED PARKING WITHOUT ANY FURTHER DIFFICULTIES. MAI NTENANCE INSPECTED THE APU AND FOUND NO EVIDENCE OF FIRE. MAINTENANCE DEFERRED THE APU AND APU FIRE WARNING SYSTEM AND THE AIRCRAFT WAS RETURNED TO SERVICE. ON 2/7/2001 THE APU FIRE HRD BOTTLE WAS REPLACED IN MHR. TROUBLESHOT THE FIRE WA RNING SYSTEM. NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001022000284 20010220 00284 EU 2001 2 20 USAASA01002 1 20010129 A 3397 E0053R8B3ASNE WIRE AIRBUS A319 A319112 3930323 EU CONNECTOR BACKED OUT A K NONE L NO TEST IN INSP/MAINT 1 EA 19 716UW 1055 DCA - MAINTENANCE FOUND THE 3351-1820 WIRE PULLED FROM CONNECTOR 7260VC5 AT THE ROW 11 EMERGENCY LIGHTING WIRING HARNESS . MAINTENANCE REPAIRED THE WIRING AND PROGRAMMED THE REPLACEMENT OF THE CONNECTOR. (M) 2 L 7 2 4F RT A28NM 2001022000285 20010220 00285 NM 2001 2 20 USAA010059 1 20010122 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND FLOORBEAM CORRODED 24 INCHES, STATION 312, LBL 12 TO RBL 12. CORROSION LEVEL 2 C53-107-01. SPLICED IN NEW T-CAP SECTION PER TR 53-10-13. (M) 2 L 7 2 4F A16WE 2001022000286 20010220 00286 NM 2001 2 20 USAA010076 1 20010129 A 5313 STRINGER BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND STRINGER CORRODED 2 INCHES, STRINGER 28R OUTBOARD SIDE OF STRINGER 8 AFT OF FRAME 312. CORROSION LEVEL 1. REMOVED AND REPLACED AND INSTALLED DOUBLER PER SRM 51-40-2. (M) 2 L 7 2 4F A16WE 2001022000287 20010220 00287 NM 2001 2 20 USAA010075 1 20010129 A 5320 ANGLE BOEING 737 737201 1384454 NM FWD ENTRY DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND Z-ANGLE CORRODED, 8 PLACES 1 INCH BY 1 INCH, FORWARD ENTRY DOOR Z-ANGLE. CORROSION LEVEL 1 C53-107-01. REP LACED Z-ANGLE PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2001022000288 20010220 00288 NM 2001 2 20 USAA010077 1 20010129 A 5312 BULKHEAD BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND BULKHEAD CRACKED .250 INCH, STATION 178, BULKHEAD WL 207, RBL 1.5. INSTALLED DOUBLER PER EO 5300V153. (M) 2 L 7 2 4F A16WE 2001022000289 20010220 00289 NM 2001 2 20 USAA010078 1 20010129 A 5312 BULKHEAD BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND BULKHEAD .250 INCH CRACKED, STATION 178, WL 214, LBL 5. INSTALLED DOUBLER PER EO 5300V153. (M) 2 L 7 2 4F A16WE 2001022000290 20010220 00290 NM 2001 2 20 USAA010080 1 20010129 A 5312 BULKHEAD BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND BULKHEAD .250 INCH CRACK, STATION 178, BULKHEAD, WL 214, LBL 6.5. INSTALLED DOUBLER PER EO 5300V153. (M) 2 L 7 2 4F A16WE 2001022000291 20010220 00291 NM 2001 2 20 USAA010081 1 20010129 A 5312 BULKHEAD BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND BULKHEAD CRACKED .250 INCH, STATION 178 BULKHEAD WL 210.5, RBL 6.75. INSTALLED DOUBLER PEREO 5300V153. (M) 2 L 7 2 4F A16WE 2001022000292 20010220 00292 NM 2001 2 20 USAA010082 1 20010129 A 5312 BULKHEAD BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND BULKHEAD CRACKED .250, STATION 178, BULKHEAD WL 218, RBL 10.0. INSTALLED DOUBLER PER EO 5300V153. (M) 2 L 7 2 4F A16WE 2001022000293 20010220 00293 NM 2001 2 20 USAA010083 1 20010129 A 5312 BULKHEAD BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND BULKHEAD CRACKED .250 INCH, STATION 178, BULKHEAD, WL 218, LBL 12.5. INSTALLED DOUBLER PER EO 5300V153. (M ) 2 L 7 2 4F A16WE 2001022000294 20010220 00294 NM 2001 2 20 USAA010084 1 20010129 A 5312 BULKHEAD BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND BULKHEAD CRACKED .250 INCH, STATION 178, BULKHEAD WL 218, RBL 13. INSTALLED DOUBLER PER EO 5300V153. (M) 2 L 7 2 4F A16WE 2001022000295 20010220 00295 NM 2001 2 20 USAA010085 1 20010129 A 5312 BULKHEAD BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND BULKHEAD CRACKED .5 INCH, WL 234, RBL 10. INSTALLED DOUBLER PER SRM 53-10-08. (M) 2 L 7 2 4F A16WE 2001022000296 20010220 00296 NM 2001 2 20 USAA010086 1 20010129 A 5320 STRUCTURE BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND INNER CHORD CRACKED 3 INCHES, STATION 294, WL 208. REPLACED CHORD PER SRM 51-10-01. (M) 2 L 7 2 4F A16WE 2001022000297 20010220 00297 NM 2001 2 20 USAA010087 1 20010129 A 5320 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND TIE CLIP CRACKED 1 INCH, BS 520, STRINGER 19R. INSTALLED REPAIR PER SRM 51-40-3. (M) 2 L 7 2 4F A16WE 2001022000298 20010220 00298 NM 2001 2 20 USAA010088 1 20010129 A 5310 BEAM BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND BEAM CRACKED 1.5 INCH, STATION 520, LBL 24. REPAIRED DOUBLER PER SB 737-53-1120. (M) 2 L 7 2 4F A16WE 2001022000299 20010220 00299 NM 2001 2 20 USAA010089 1 20010129 A 5310 BEAM BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND BEAM CRACKED 1.3 INCH, STATION 520-540, LBL 45.5. REPAIRED DOUBLER PER SB 737-53-1120. (M) 2 L 7 2 4F A16WE 2001022000300 20010220 00300 NM 2001 2 20 USAA010091 1 20010129 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND FLOORBEAM CRACKED 1 INCH, STATION 663, LBL 0.0. INSTALLED DOUBLER AND ANGLES PER SRM 53-10-9. (M) 2 L 7 2 4F A16WE 2001022000301 20010220 00301 NM 2001 2 20 QXEA01000088 1 20010128 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM LAVATORY MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 348PH 484 PUW- LAVATORY SMOKE DETECTOR ACTIVATED IN FLIGHT. REMOVED AND REPLACED LAVATORY SMOKE DETECTOR. OPERATIONAL CHECKS GOO D. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001022000303 20010220 00303 2001 2 20 KBMA974369 4 20010115 A 3421 5040017901 GYRO SNIAS 350 AS350B2 8680813 EU COCKPIT MALFUNCTIONED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 53SH 4856 2009 NOT PRECESSING FLAG STITCHING. 1 G 7 1 3U H9EU 2001022000304 20010220 00304 CE 2001 2 20 GLBA2001024 1 20010204 A 5270 ANNUNCIATOR BEECH 1900 1900D 1154162 CE PAX DOOR FALSE INDICATION A GLBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 01 122UX UE122 ABORTED T/O, CABIN DOOR ANNUNCIATOR ILLUMINATED. INSPECTED SYSTEM CND OPS CHECKED GOOD. 2 L 7 2 4T RT A24CE 2001022000305 20010220 00305 NM 2001 2 20 01FDEA00053 1 20010130 A 5311 6516342 FRAME BOEING 727 727227 1384078 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 FRAME DENTED AT BS 1030 BETWEEN STR 25 & 26 RT SIDE. *S/D* REMOVED AND REPLACED PER FEDEX SRM 51-40-3. 2 L 7 3 4F A3WE 2001022000306 20010220 00306 NM 2001 2 20 01FDEA00054 1 20010130 A 5311 6516341 FRAME BOEING 727 727227 1384078 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 FRAME DENTED AT BS 1010, STR 26 RT SIDE. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 53-10-1, 51-40-3. 2 L 7 3 4F A3WE 2001022000307 20010220 00307 NM 2001 2 20 01FDEA00055 1 20010130 A 5311 6556124 FRAME BOEING 727 727227 1384078 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 FRAME DENTED AT BS 950R, STR 25L. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-10-1, 51-40-3. 2 L 7 3 4F A3WE 2001022000308 20010220 00308 NM 2001 2 20 01FDEA00059 1 20010131 A 5330 6572702 SKIN BOEING 727 727227 1384078 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 AFT LWR CORNER OF MAIN CARGO DOOR WAS DAMAGED BY LOADER DENT IN FUSELAGE JUST AFT AND BELOW MAIN CARGO DOOR. *S/D* REM OVED AND REPLACED PER IAW FEDEX SRM 53-30-1, EA 7-5330-55769A AND SRM 53-30-3 FIG 3. 2 L 7 3 4F A3WE 2001022000309 20010220 00309 NM 2001 2 20 01FDEA00060 1 20010131 A 5315 6520838 FLOORBEAM BOEING 727 727227 1384078 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 CORROSION (C53-113-01, 2) ON 1130 FLOORBEAM LOWER FLANGE, ON AND AROUND THE NUT CLIPS / FASTENER HOLES FROM LBL 40 TO RB L 50, WL 201. *S/D* REMOVED AND REPLACED FAB PER 51-20-1, 51-10-2, 51-30-2. 2 L 7 3 4F A3WE 2001022000311 20010220 00311 2001 2 20 20010131CW001 4 20010109 A 3421 5040017901 GYRO SNIAS 350 AS350B2 8680813 EU COCKPIT PRECESSES E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 53SH 4844 2009 PRECESSING 30 DEGREES. 1 G 7 1 3U H9EU 2001022000312 20010220 00312 2001 2 20 KMBA99408 4 20010109 A 3421 5040017901 GYRO SNIAS 350 AS350B2 8680813 EU COCKPIT PRECESSES E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 53SH 4516 2009 PRECESSING 30 DEGREES. 1 G 7 1 3U H9EU 2001022000313 20010220 00313 NE 2001 2 20 KBMA99415 2 20010112 A 7321 0164248850 FUEL CONTROL SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE LEAKING E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 53SH 4846 2009 FUEL CONTROL UNIT LEAKING. 1 G 7 1 3U 3 U H9EU E19EU 2001022000314 20010220 00314 2001 2 20 KBMA99409 4 20010109 A 3421 5070209180516 INDICATOR SNIAS 350 AS350B2 8680813 EU COCKPIT PRECESSES E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 53SH 4844 2009 PRECESSING AT 30 DEGREES. 1 G 7 1 3U H9EU 2001022000315 20010220 00315 EU 2001 2 20 KBMA97421 1 20010107 A 6720 350A33214501 LINK SNIAS 350 AS350BA 8680817 EU PITCH CONTROL DAMAGED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 350SH 4396 2957 PITCH CONTROL LINK EXCEEDS INSPECTION CRITERIA. 1 G 7 1 3U NC H9EU 2001022100019 20010221 00019 NM 2001 2 21 USAA010098 1 20010130 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND T-CAP CRACKED 4 INCHES, STATION 663, BL 0. INSTALLED REPAIR ANGLES PER TR 57-10-04 AND EA 69046. (M) 2 L 7 2 4F A16WE 2001022100020 20010221 00020 NM 2001 2 21 USAA010099 1 20010130 A 5320 WEB BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND WEB CRACKED 3 INCHES, STATION 663.7, BL 0. INSTALLED DOUBLER PER TR 57-10-04. (M) 2 L 7 2 4F A16WE 2001022100022 20010221 00022 WP 2001 2 21 AALA016007 1 20010111 A 3397 WIRE DOUG DC9 DC983 3022083 WP AFT EMERG EXIT BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 21 880RA 53186 RNO-CCI - AFT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BROKEN WIRE, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 2001022100023 20010221 00023 WP 2001 2 21 AALA016008 1 20010115 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 880RA 53186 LAX-CCI - EMERGENCY LIGHT AT SEAT 17D BROKEN AND INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY AT SEAT 17D, OPS CHEC K OK. (M) 2 L 7 2 4F RT A6WE 2001022100024 20010221 00024 WP 2001 2 21 AALA016009 1 20010119 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 821RA 49931 CCI-LAX - EMERGENCY LIGHT IN CEILING OVER SEATS 28D AND 29D INOPERATIVE. CLEANED AND ADJUSTED BATTERY TERMINALS IN BATT ERY PACK. (M) 2 L 7 2 4F A6WE 2001022100025 20010221 00025 SO 2001 2 21 ASOA01002 1 20010105 A 3010 3D237606 EJECTOR VALVE EMB 120 EMB120RT SO TAIL INOPERATIVE A ASOA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 11 240AS 3376 120060 FLT 4331 - DURING FLIGHT FROM ATL-ROA AIRCRAFT ENTERED ICING CONDITIONS AND STARTED ACCUMULATING ICE. CREW HAD A FAILUR E OF THE LEFT AND RIGHT O/B STABILIZER AND VERTICAL FIN DE-ICE BOOTS. CREW DECLARED AN EMERGENCY AND DESCENDED TO 7,000 FEET. CREW FOLLOWED DE-ICE FAILURE CHECKLIST, BUT BOOTS DID NOT START OPERATING. CREW LANDED SAFELY IN ROA. MAINTENA NCE REMOVED AND REPLCED THE EJECTOR VALVE. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001022100026 20010221 00026 EA 2001 2 21 ASOA01013 1 20010128 A 5610 NP1393219 WINDSHIELD CNDAIR CL600 CL6002B19 EA COCKPIT CRACKED A ASOA K NONE O OTHER CR CRUISE 1 SO 11 835AS 6037 7258 FLT 4738 - DURING FLIGHT FROM ATL-ICT, CAPTAIN''S WINDSHIELD CRACKED. MAINTENANCE REMOVED AND REPLACED CAPTAIN''S WINDS HIELD. OPS AND LEAK CHECK WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001022100027 20010221 00027 SO 2001 2 21 ASOA01014 1 20010129 A 3350 D36604001 BATTERY EMB 120 EMB120 3260201 SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 262AS 25064 120146 DURING INSPECTION, CREW FOUND ROW 5 EMERGENCY FLOOR TRACKING LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERG ENCY BATTERY. OPS CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001022100028 20010221 00028 EA 2001 2 21 ASOA01015 1 20010131 A 2740 70608 CONTROL UNIT CNDAIR CL600 CL6002B19 EA FUSELAGE INOPERATIVE A ASOA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SO 11 839AS 5548 7284 FLT 4469 - DURING FLIGHT FROM YYZ TO ATL, CREW RECEIVED STAB TRIM AND MACH TRIM CAUTION MESSAGE ON RANDOM INTERVALS. CR EW RESET SYSTEM, BUT MESSAGE WOULD START AGAIN. STAB AND MACH TRIM FAILED AGAIN UPON APPROACH. CREW DECLARED AN EMERGE NCY AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED HSTCU. OPERTIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F RT A21EA 2001022100029 20010221 00029 EU 2001 2 21 REXA01005 1 20010130 A 3230 HP848430621 CONTROL VALVE SAAB SF340 340B 7860101 EU LANDING GEAR FAILED A REXA K NONE O OTHER AP APPROACH 1 SO 25 364PX 340B262 ON APPROACH WHEN LANDING GEAR WAS SELECTED DOWN, THE CIRCUIT BREAKER FOR THE LANDING GEAR CONTROL VALVE ''POPPED'' AND T HE GEAR DID NOT EXTEND. THE CREW ATTEMPTED ONE RESET OF THE CIRCUIT BREAKER BUT IT WOULD NOT STAY SET. ABNORMAL AND EM ERGENCY CHECKLISTS WRE COMPLETED AND THE GEAR WAS EXTENDED UTILIZING THE EMERGENCY EXTENSION SYSTEM. THE GEAR EXTENDED AND INDICATED DOWN AND LOCKED AND THE CREW DECLARED AN EMERGENCY AS A PRECAUTION AND A SUCCESSFUL LANDING WAS MADE. LAN DING GEAR CONTROL VALVE WAS REMOVED AND REPLACED AND A GEAR SWING PERFORMED AFTER REPLACEMENT WITH NO DEFECTS NOTED. (M ) 2 L 7 2 4T RT A52EU 2001022100030 20010221 00030 EU 2001 2 21 SIMA0325 1 20010201 A 3350 LIGHT AEROSP ATR72 ATR72212 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 536AT 536 DFW - FLT 3656 - CREW REPORTED NUMEROUS EMERGENCY LIGHTS ARE INOPERATIVE WHEN AIRCRAFT IS POWERED DOWN. (M) 2 H 7 2 4T RT A53EU 2001022100031 20010221 00031 EU 2001 2 21 SIMA0304 1 20010130 A 3350 5001309111 LIGHT AEROSP ATR72 ATR72212 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 499AT 499 DFW - EMERGENCY STRIP LIGHTING SECOND FROM GALLEY HAS BROKEN PIECES. RAI EMERGENCY LIGHT FLOOR STRIP SECTION IAW ATR 20 -25-00 STD PRACTICES. OPERATIONAL CHECK OF SYSTEM WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001022100032 20010221 00032 EU 2001 2 21 SIMA0264 1 20010126 A 3350 CONNECTOR AEROSP ATR72 ATR72212 EU PAX DOOR MISWIRED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 434AT 434 DFW - FLT 3350 - DURING PHASE 1 INSPECTION, MAINTNANCE REPORTED THE PASSENGER DOOR EMERGENCY LIGHT WAS INOPERATIVE. MAI NTENANCE FOUND CANNON PLUG 253VC WIRED INCORRECTLY CAUSING A FUSE TO BLOW IN POWER SUPPLY 62WL. CANNON PLUG WAS REWIRED IAW ATR MM 52-71-01. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001022100033 20010221 00033 EU 2001 2 21 SIMA0234 1 20010123 A 3350 AQS1000 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN MISSING A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 540AM 540 DFW - DURING PRE-FLIGHT, PILOT REPORTED EMERGENCY LIGHTS DID NOT WORK WITHOUT GROUND POWER. MAINTENANCE FOUND ALL FOUR EMERGENCY LIGHT POWER SUPPLY UNITS DID NOT HAVE BATTERY PACKS INSTALLED. BATTERY PACKS WERE INSTALLED INTO THE POWER SU PPLY UNITS 61WL, 43WL, 73WL, AND 62WL. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001022100034 20010221 00034 EU 2001 2 21 SIMA0343 1 20010203 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN LOOSE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 261AE 340B261 JFK - FLT 5072 - EMERGENCY LIGHT AT SEAT POSITION 10BC IS INOPERATIVE. PUT ON MEL AT THIS TIME. MAINTENANCE RESECURED BULB IN SOCKET. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001022100035 20010221 00035 EU 2001 2 21 SIMA0311 1 20010131 A 3350 72252751065 LIGHT SAAB SF340 340B 7860101 EU GALLEY INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 313AE 340B313 BOS - FLT 4894 - CREW REPORTED THE FLIGHT ATTENDANTS EMERGENCY LIGHT ARM BUTTON DOES NOT ILLUMINATE. MAINTENANCE REPLAC ED ARM LIGHT BUTTON. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001022100097 20010221 00097 SO 2001 2 21 ASOA01016 1 20010131 A 2613 DETECTOR EMB 120 EMB120 3260201 SO ENGINE MALFUNCTIONED A ASOA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 11 262AS 120146 FLT 4240 - DURING FLIGHT FROM ILM-ATL, LEFT DUCT LEAK LIGHT ILLUMINATED. CAPTAIN FOLLOWED POH AND SHUTDOWN ENGINE. AIR CRAFT DIVERTED TO MYR AND LANDED SAFELY. MAINTENANCE OPERATED AIRCRAFT AT 60 PERCENT TORQUE FOR 10 MINUTES AND THEN WEN T UP TO 95 PERCENT TORQUE FOR 7 MINUTES. MAINTENANCE RECEIVED A BLEED OVERHEAT CAUTION, BUT WHEN POWER WAS REDUCED THE SYSTEM RESET CORRECTLY. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001022100138 20010221 00138 CE 2001 2 21 20010208CW005 1 20010110 A 3230 50450101 TORQUE TUBE CESSNA 401 401 207590C CE LT MLG CRACKED E MHJA K NONE O OTHER IN INSP/MAINT 1 SW 05 4021Q 10368 4010121 WELD AT FORK BOLT THRU HOLE, HAD CRACK IN IT FOR SOME TIME , THAT WENT UNDETECTED. IT FINALLY PROGRESSED IN A SPIRAL PA TTERN AND THE TUBE COMPLETELY FAILED. 1 L 7 2 3O A7CE 2001022100142 20010221 00142 EU 2001 2 21 20010122CW015 1 20010103 A 7931 646600251 CONNECTOR SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE OIL TEMP PROBE LOOSE E HCMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 13 972BH 2804 9587 DURING A TOUR FLIGHT WITH 4 PASSENGERS ON BOARD, PILOT NOTICED A HIGH ENGINE OIL TEMPERATURE READING. HE ELECTED TO PER FORM A PRECAUTIONARY LANDING. UPON INSPECTION, THE MECHANIC FOUND THE SPADE CONNECTION LOOSE AND IT HAD MOISTURE ON IT . CONNECTION WAS TIGHTENED ADN MOISTURE REMOVED. 1 G 7 1 3U 3 U H9EU E19EU 2001022100147 20010221 00147 EU 2001 2 21 20010122CW016 1 20010109 A 6710 11745020 MODULE BOLKMS 117 BK117B1 5626012 EU M/R HYDRAULICS BINDING E BAQA K NONE O OTHER IN INSP/MAINT 1 EA 03 136AE 5284 5284 7234 AIRCRAFT HAD COLLECTIVE BINDING DURING PITCH MOVEMENT. 1 G 7 2 3U H13EU 2001022100163 20010221 00163 NE 2001 2 21 A1UR135H 2 20010102 A 7323 430121204 GOVERNOR BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE NR 2 ENGINE FAILED E A1UA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 CE 03 211SL 7201 LE45666 PILOT REPORTED ENROUTE TORQUE SPLITS BETWEEN ENGINE. AC MADE SCHEDULED LANDING AT HOSPITAL. PILOT ATTEMPTED TO START N R 2 ENGINE, ENG WOULD NOT ACCELERATE BEYOND 42% NG SPEED. UPON INSP OF ENGINE AND COMPONENTS, TECH DISCOVERED NP GOVERN OR SHAFT SEIZED, REPLACED GOVERNOR WITH SERVICEABLE UNIT. AC CHECK RUN AND FLIGHT COMPLETED AND RETURNED TO SERVICE. GO VERNOR DISASSEMBLED, BRG BETWEEN FLYWEIGHTS AND INTERNAL GOV LEVER FAILED, WHICH BENT THE SHAFT PROHIBITING ANY ROTATION WITHIN THE GOVENOR, SUSPECTED WHEN SHAFT BENT IT ALSO WEDGED GOV LEVER WHICH MODULATES PR BLEED PORT OPEN IN THE MIDRAN GE. 1 G 7 2 3U 3 U H13EU E5NE10 2001022200007 20010222 00007 SO 2001 2 22 WVBA2001005 1 20010125 A 2140 A23D04 REGULATOR PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HARTZL HCE3Y HCE3YR2A GL HEATER LEAKING E WVBA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 01 3582P 318052103 DURING ROUTINE INSPECTION OBSERVED FUEL LEAK FROM PRESSURE REGULATOR CONTAINMENT VESSEL. REMOVED CONTAINMENT VESSEL AND FOUND FUEL LEAKING FROM PARTING SURFACE AT THE TOP OF THE REGULATOR. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 2001022200008 20010222 00008 EA 2001 2 22 WVBA2001006 2 20010125 A 8520 LW19340 CAMSHAFT PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HARTZL HCE3Y HCE3YR2A GL ENGINE DAMAGED E WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 3582P 1128 318052103 RL604561A DURING VALVE CLEARANCE CHECK, INTAKE VALVE 3 AND 4 EXHIBITED EXCESSIVE LIFT. NR 4 CYLINDER WAS REMOVED AND DAMAGE OBSER VED ON 3 AND 4 INTAKE LOBES OF CAMSHAFT AND TAPET BODIES. ENGINE WAS REMOVED FROM SERVICE. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 2001022200009 20010222 00009 SO 2001 2 22 WVBA2001007 1 20010129 A 2140 FR65D793EL COMBUSTION LINER ELECTROSYS PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA MCAULY 3DF36C B3DF36C526 GL HEATER FAILED E WVBA O OTHER O OTHER NR NOT REPORTED 1 AL 01 59829 2804 A98020014 317652081 PILOT REPORTED FRONT COMBUSTION HEATER INOPERATIVE. IT WAS DISCOVERED THAT THE HEATER CONBUSTION CAN HAD A HOLE IN THE REAR OF THE CAN, AFT OF THE EXHAUST. UNIT WAS REMOVED FROM SERVICE. IT IS SUSPECT THAT IMPROPER COOL DOWN PROCEDURES L ED TO PREMATURE CAN FAILURE. 1 L 7 2 3O 3 O A20SO E14EA 5 C 2001022200010 20010222 00010 SO 2001 2 22 WVBA2001008 1 20010130 A 2140 A233D04 REGULATOR PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA MCAULY 3DF36C B3DF36C526 GL HEATER LEAKING E WVBA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 01 3527U 301 317952141 DURING ROUTINE INSPECTION REGULATOR WAS FOUND TO BE LEAKING FROM THE PARTING SURFACE. THE UNIT WAS REMOVED AND REPLACED . 1 L 7 2 3O 3 O A20SO E14EA 5 C 2001022200012 20010222 00012 CE 2001 2 22 20010214CW003 1 20010214 A 3230 08411066 BELLCRANK CESSNA 340 340A 2076405 CE MLG BROKEN E VVRA O OTHER J WARNING INDICATION LD LANDING 1 NM 13 2741R 5273 340A0922 ON LANDING, GEAR EXTENTION, RIGHT MAIN LANDING GEAR BELLCRANK BROKE CAUSING INBOARD GEARDOOR TO HANG OPEN AT END OF GEAR EXTENTION CYCLE. AIRCRAFT LANDED WITH NO INCIDENT.PILOT REPORTED THAT AIRSPEED MAY HAVE BEEN SOMEWHAT HIGHER THAN GEAR OPERATING SPEED WHEN GEAR WAS EXTENDED. 1 L 7 2 3O 3A25 2001022200013 20010222 00013 CE 2001 2 22 20010214CW004 1 20010115 A 3230 S232113 ROD END CESSNA 210 T210N 2073456 CE NLG BROKEN E VVRA K NONE O OTHER IN INSP/MAINT 1 NM 13 5495A 3230 21063470 BEARING OF NOSE LANDING GEAR ACTUATING ROD ROD END SEPARTED FROM BODY OF ROD END, CAUSING RT NLG DOOR TO CLOSE UNDER AI R LOAD PRIOR TO NLG RETRACTION, DAMAGING DOOR. DOOR AND ROD END WERE REPLACED. GEAR EXTENSION/RETRACTION IS NORMAL. 1 H 7 1 3O 3A21 2001022200020 20010222 00020 EU 2001 2 22 SIMA0171 1 20010117 A 5315 S5367240420601 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AT 431 SAW - DURING MBV-1 INSPECTION, MAINTENANCE REPORTED FLOORBEAM 34 HAD OVAL SHAPED HI-LOCK HOLES AT SEAT TRACK ATTACH POIN T. MAINTENANCE REPAIRED THE FLOORBEAM IAW SRM 53-00-00 FIGURE 435. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001022200021 20010222 00021 EU 2001 2 22 SIMA0223 1 20010110 A 5347 S53375001222 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AT 431 DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE OUTBOARD, LE FT MIDDLE INBOARD, LEFT AFT INBOARD, RIGHT AFT INBOARD, RIGHT MIDDLE OUTBOARD, RIGHT MIDDLE INBOARD, AND RIGHT FORWARD I NBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNE D TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001022200022 20010222 00022 EU 2001 2 22 20010222SG008 1 20010110 A 5347 S53375001214 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AT 431 DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE OUTBOARD, LE FT MIDDLE INBOARD, LEFT AFT INBOARD, RIGHT AFT INBOARD, RIGHT MIDDLE OUTBOARD, RIGHT MIDDLE INBOARD, AND RIGHT FORWARD I NBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNE D TO SERVICE. REF SIMA0223. (M) 2 H 7 2 4T RT A53EU 2001022200023 20010222 00023 EU 2001 2 22 20010222SG009 1 20010110 A 5347 S53570203202 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AT 431 DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE OUTBOARD, LE FT MIDDLE INBOARD, LEFT AFT INBOARD, RIGHT AFT INBOARD, RIGHT MIDDLE OUTBOARD, RIGHT MIDDLE INBOARD, AND RIGHT FORWARD I NBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNE D TO SERVICE. REF SIMA0223. (M) 2 H 7 2 4T RT A53EU 2001022200024 20010222 00024 EU 2001 2 22 20010222SG011 1 20010110 A 5347 S53678001246 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AT 431 DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE OUTBOARD, LE FT MIDDLE INBOARD, LEFT AFT INBOARD, RIGHT AFT INBOARD, RIGHT MIDDLE OUTBOARD, RIGHT MIDDLE INBOARD, AND RIGHT FORWARD I NBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNE D TO SERVICE. REF SIMA0223. (M) 2 H 7 2 4T RT A53EU 2001022200025 20010222 00025 EU 2001 2 22 20010222SG012 1 20010110 A 5347 S53570203202 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AT 431 DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE OUTBOARD, LE FT MIDDLE INBOARD, LEFT AFT INBOARD, RIGHT AFT INBOARD, RIGHT MIDDLE OUTBOARD, RIGHT MIDDLE INBOARD, AND RIGHT FORWARD I NBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNE D TO SERVICE. REF SIMA0223. (M) 2 H 7 2 4T RT A53EU 2001022200026 20010222 00026 CE 2001 2 22 20010222AP001 1 20010209 A 3340 C6220100101 LIGHT CESSNA 208 208B 2073701 CE LT WING MISINSTALLED G BQTA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 01 28AN 208B0751 LEFT WING POSITION LIGHT/STROBE ASSY INSTALLED INCORRECTLY(BACKWARDS). RED LIGHT FACING AFT AND STROBE FACING FOWARD. ASSY CAN BE INSTALLED INCORRECTLY AT FACTORY OR BY MECHANIC IN THE FIELD. 1 H 7 1 3T A37CE 2001022200027 20010222 00027 CE 2001 2 22 20010222AP002 1 20010209 A 3340 C6220100102 LIGHT CESSNA 208 208B 2073701 CE RT WING MISINSTALLED G BQTA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 01 29AN 208B0753 RIGHT WING POSITION/STROBE LIGHT INSTALLED INCORRECTLY(BACKWARDS). GREEN LIGHT FACING AFT AND STROBE FACING FOWARD. LI GHT ASSY CAN BE INSTALLED INCORRECTLY AT FACTORY OR BY MECHANIC IN THE FIELD. 1 H 7 1 3T A37CE 2001022200028 20010222 00028 CE 2001 2 22 20010222AP003 1 20010209 A 3340 C6220100101 LIGHT CESSNA 208 208B 2073701 CE LT WING MISINSTALLED G BQTA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 01 28AN 208B0751 LEFT WING POSITION/STROBE LIGHT ASSY INSTALLED INCORRECTLY(BACKWARDS). RED LIGHT FACING AFT AND STROBE FACING FOWARD. LIGHT ASSY CAN BE INSTALLED INCORRECTLY AT FACTORY OR BY MECHANIC IN THE FIELD. 1 H 7 1 3T A37CE 2001022200029 20010222 00029 EU 2001 2 22 SIMA0303 1 20010130 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 323AE 340B323 LAX - FLT 3241 - CREW REPORTED ALL FORWARD EMERGENCY LIGHTS WOULD NOT OPERATE. MAINTENANCE REMOVED AND REPLACED BATTERI ES IN EMERGENCY LIGHT POWER SUPPLY UNITS 20LN, AND 21LN. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVIC E. (M) 2 L 7 2 4T RT A52EU 2001022200030 20010222 00030 EU 2001 2 22 SIMA0276 1 20010127 A 3350 FUSE SAAB SF340 340B 7860101 EU CABIN BLOWN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 266AE 340B266 SBP - MAINTENANCE REPORTED EMERGENCY LIGHT ABOVE SEAT 11A IS INOPERATIVE. MAINTENANCE FOUND FUSE 76LN AND REPLACED BULB . OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001022200031 20010222 00031 EU 2001 2 22 20010222SG001 1 20010127 A 3350 GE4713 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 266AE 340B266 SBP - MAINTENANCE REPORTED EMERGENCY LIGHT ABOVE SEAT 11A IS INOPERATIVE. MAINTENANCE FOUND FUSE 76LN AND REPLACED BULB . OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0276. (M) 2 L 7 2 4T RT A52EU 2001022200032 20010222 00032 EU 2001 2 22 SIMA0253 1 20010125 A 2530 1095A COFFEEMAKER SAAB SF340 340B 7860101 EU GALLEY INOPERATIVE A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 371AE 340B371 HOU - FLT 3401 - CREW REPORTED A BURNING ORDER IN FLIGHT WITH NO SMOKE REPORTED. CREW ALSO REPORTED CIRCUIT BREAKER M25 POPPED. FORWARD HOT JUG WAS PUT ON MEL. FORWARD HOT JUG WAS REPLACED, OPERATIONAL CHECK WAS GOOD MEL WAS CLEARED. (M) 2 L 7 2 4T RT A52EU 2001022200033 20010222 00033 NM 2001 2 22 EIA2001009 1 20010203 A 3230 65B406768 FITTING BOEING 747 747132 1384882 NM RT MLG MALFUNCTIONED A EIAA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 09 481EV 19896 KJFK - FLT RCF7 - GEAR WOULD NOT RETRACT. LANDING GEAR LEVER LATCH DID NOT RELEASE. RT BODY GEAR WAS NOT TILTED PRIMAR Y AND ALT. REPLACED COBRA FITTING, PRIM TILT SWITCH, AND ALT TILT SWITCH ADJUSTED RIGHT BODY GEAR PRI AND ALT TILT SWIT CHES PER MM 32-61-04. RETRACTION TEST OK. (M) 2 L 7 4 4F A20WE 2001022200034 20010222 00034 SO 2001 2 22 C2XA0TY004 1 20010201 A 5320 14533997001 SUPPORT BRACKET EMB 145 EMB145 SO AFT FUSELAGE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 TYS - DURING A SCHEDULED 1C INSPECTION, THE APU BLEED AIR SUPPORT BRACKET WAS FOUND GOUGING INTO THE FIREWALL HEAT SHIEL D. MAINTENANCE BLENDED APU BLEED AIR SUPPORT BRACKET IAW EMB REF GST 0247/01 AND REPLACED APU HEAT BLANKET. REPAIRS WE RE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001022200035 20010222 00035 SO 2001 2 22 C2XA01TY005 1 20010201 A 4980 14533997001 BLANKET EMB 145 EMB145 SO AFT FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 TYS - DURING A SCHEDULED 1C INSPECTION, THE HEAT BLANKET ON THE APU FIREWALL HAS SEVERAL GOUGES. MAINTENANCE REMOVED AP U HEAT BLANKET, CLEANED AND INSPECTED, AND FOUND 2 GOUGED OUT OF LIMITS. REPAIRED DAMAGE IAW EMB REF GST 024/01, THEN R EINSTALLED BLANKET. REPAIRS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001022200036 20010222 00036 SO 2001 2 22 C2XA01TY006 1 20010202 A 5240 14524000001 STOP EMB 145 EMB145 SO SERVICE DOOR WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 TYS - DURING A SCHEDULED 1C INSPECTION, SERVICE DOOR FRAME STOP NR 8 WAS FOUND TO BE WORN BEYOND LIMITS. MAINTENANCE RE MOVED AND REPLACD NR 8 DOORSTOP IAW EMB-145 MM 52-43-06. (M) 2 L 7 2 4F RT T00011AT 2001022200037 20010222 00037 SO 2001 2 22 C2XA01TY007 1 20010202 A 2612 3601135470 FIRE DETECTOR EMB 145 EMB145 SO APU GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 3952 145161 TYS - DURING A SCHEDULED 1C INSPECTION, THE APU FIRE LOOP WAS GOUGED. MAINTENANCE REMOVED AND REPLACED THE APU FIRE LOO P IAW EMB 145 MM 26-10-00. OPS CHECKED GOOD. REPAIRS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001022200038 20010222 00038 SO 2001 2 22 C2XA01TY002 1 20010201 A 5320 14522460009 STRAP EMB 145 EMB145 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 TYS - DURING A SCHEDULED 1C INSPECTION, CORROSION WAS FOUND ON TOP CAP ABOVE OMEGA BEAM BETWEEN FRAMES 19 AND 23, STRING ERS 21L AND 21R. MAINTENANCE REMOVED AND REPLACED TOP CAP IAW EMB 145 SRM 51-40-02. REPAIRS WERE SATISFACTORY, AIRCRAF T RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001022200039 20010222 00039 SO 2001 2 22 C2XA01CL010 1 20010129 A 3230 23092900001 UPLOCK EMB 145 EMB145 SO NLG FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 15926 8808 145005 CLE - FLT 3670 - THE CREW REPORTED THAT AFTER TAKEOFF FROM CLEVELAND, THE NOSE GEAR FAILED TO RETRACT. THE AIRCRAFT RET URNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NOSE GEAR UPLOCK BOX ASSY IAW EMB MM 32-33-07. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001022200040 20010222 00040 NM 2001 2 22 GAIA01042 1 20010201 A 3350 LIGHT BOEING 727 727224 1384076 NM CABIN INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 69739 20667 FLT 739 - OSC - AFTER COMPLETION OF C-CHECK MAINTENANCE, EMERGENCY EXIT LIGHTS UNABLE TO SWITCH OFF. RE-SEATED COCKPIT ENTRY ''EMERGENCY EXIT'' LIGHT. OPS CHECK GOOD ON GROUND. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001022200041 20010222 00041 NM 2001 2 22 GAIA01043 1 20010202 A 3350 LIGHT BOEING 727 727225 1384077 NM COCKPIT MALFUNCTIONED A GAIA K NONE O OTHER CL CLIMB 1 SW 07 902RF 22549 FLT 1850 - SEA-FWA - ON ROTATION, EMERGENCY EXIT LIGHT ILLUMINATED WITH SWITCH IN ARMED POSITION. AIRCRAFT MADE AN UNEV ENTFUL LANDING IN FWA. CLEANED AND RESEATED CONTACTS ON COCKPIT EMERGENCY EXIT LIGHT. LIGHT OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001022200042 20010222 00042 NM 2001 2 22 GAIA01039OP 1 20010127 A 7830 33100021 THRUST REVERSER BOEING 727 727223 1384074 NM NR 2 ENGINE MALFUNCTIONED A GAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 6807 19482 FLT 2023 - ABQ-PHX - AFTER TAKEOFF, THE FLIGHT CREW NOTICED THAT THE NR 2 ENGINE THRUST REVERSER LIGHT ILLUMINATED. THE CREW DECLARED AN EMERGENCY AND RETURNED TO ABQ. AN UNEVENTFUL LANDING WAS MADE. INSPECTION DID NOT REVEAL ANY PROBLEM S AND THE THRUST REVERSER INDICATION PROBLEM COULD NOT BE DUPLICATED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001022200043 20010222 00043 SO 2001 2 22 SIMA0213 1 20010121 A 2740 14530477401 TRIM SWITCH EMB 145 EMB145LR SO COCKPIT DIRTY A SIMA K NONE F FLT CONT AFFECTED CL CLIMB 1 SW 21 701MH 145162 DAY - FLT 4196 - DURING CLIMB-OUT FROM DAY, FIRST OFFICERS PITCH TRIM SWITCH WOULD NOT WORK. ALL OTHER TRIM SWITCHES FU NCTIONED NORMALLY IN NORMAL AND STANDBY POSITIONS. MAINTENANCE FOUND FIRST OFFICERS TRIM SWITCH TO BE STICKING DUE TO D IRT/GRIME CONTAMINATION. CLEANED SWITCH AND PERFORMED SYSTEM OPERATIONS TEST PER AMM 27-40-00. AIRCRAFT WAS RETURNED T O SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001022200044 20010222 00044 SO 2001 2 22 SIMA0204 1 20010120 A 2740 3621001007 CONTROL UNIT EMB 145 EMB145LR SO HORIZONTAL STAB FAILED A SIMA K NONE F FLT CONT AFFECTED DE DESCENT 1 SW 21 632AE 145143 MAF - FLT 3555 - DURING DESCENT, CAPTAINS YOKE PITCH TRIM SWITCH FAILED. AIRCRAFT WAS FERRIED TO ABI FOR REPAIR. HSCU WAS REMOVED AND REPLACED. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001022200045 20010222 00045 SO 2001 2 22 SIMA0185 1 20010118 A 2740 3621001007 CONTROL UNIT EMB 145 EMB145LR SO HORIZONTAL STAB FAILED A SIMA K NONE F FLT CONT AFFECTED AP APPROACH 1 SW 21 612AE 145079 MSN - FLT 3431 - CREW REPORTED PITCH TRIM NR 1 FAIL DURING APPROACH. MAINTENANCE REMOVED AND REPLACED HSCU IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001022200046 20010222 00046 SO 2001 2 22 SIMA0206 1 20010120 A 2740 3621001007 CONTROL UNIT EMB 145 EMB145LR SO HORIZONTAL STAB FAILED A SIMA K NONE F FLT CONT AFFECTED CL CLIMB 1 SW 21 622AE 145108 CID - FLT 3954 - AFTER TAKEOFF, THE CAPTAIN AND FIRST OFFICERS YOKE TRIM SWITCHES FAILED. MAINTENANCE REMOVED AND REPLA CED HORIZONTAL STABILIZER ELECTRONIC CONTROL UNIT. AIRCRAFT PASSED A FUNCTIONAL CHECK FLIGHT AND WAS RETURNED TO SERVIC E. (M) 2 L 7 2 4T RT T00011AT 2001022200047 20010222 00047 SO 2001 2 22 SIMA0173 1 20010117 A 2760 14533022401 CONTROL UNIT EMB 145 EMB145LR SO COCKPIT FAILED A SIMA K NONE J WARNING INDICATION CR CRUISE 1 SW 21 706RG 145194 BOS - FLT 4975 - SPOILER FAIL MESSAGE IN FLIGHT AND ON GROUND. FAIL MESSAGE IN AIR WHEN LEVER IS OPEN. AFTER LEVER IS CLOSED, ALERT MESSAGE GOES AWAY. ALSO DAU WARNING ''MISCOMP'' MSG COMES ON WITH SPOILER FAIL MESSAGE IN AIR OR ON GROUN D. AIRCRAFT FERRIED TO CMH WITH SPOILER SYSTEM DEACTIVATED FOR REPAIR. REPLACED SPOILER CONTROL UNIT IAW AMM 27-63-02- 000-801A AND PERFORMED SYSTEM CHECKS. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001022200048 20010222 00048 EU 2001 2 22 SIMA0092 1 20010109 A 2430 103003 SENSOR AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 277AT 277 EYW - FLT 5263 - AFTER TAKEOFF FROM EYW CREW HAD A NR 1 DC GEN FAULT. DIVERTED TO MIA. REMOVED AND REPLACED HAIL EFFEC T SENSOR IAW AMM. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 2001022200049 20010222 00049 EU 2001 2 22 SIMA0022 1 20010102 A 3230 UPLOCK AEROSP ATR42 ATR42300 8680920 EU MLG OUT OF POSITION A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 255AE 254 MIA - FLT 5371 - AFTER TAKEOFF, CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT WHEN GEAR HANDLE WAS SELECTED UP. MAIN TENANCE FOUND ONE OF THE LANDING GEAR UPLOCK HOOKS IN THE UP POSITION AND A PROXIMITY SWITCH TARGET BRACKET LOOSE. MAIN TENANCE RESET ALL LANDING GEAR UPLOCK TO THE CORRECT POSITIONS AND TIGHTENED TARGET BRACKET. AIRCRAFT WAS RETURNED TO S ERVICE. NO PARTS WERE CHANGED. (M) 2 H 7 2 4T RT A53EU 2001022200051 20010222 00051 EU 2001 2 22 SIMA0152 1 20010115 A 3350 3012701 LIGHT AEROSP ATR72 ATR72212 EU PAX DOOR INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 545AT 545 DFW - DURING SCHEDULED PERIODIC SERVICE 2 CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHT IN THE PASSENGER DOOR TO BE INOPE RATIVE. LIGHT ASSEMBLY WAS REMOVED AND REPLACED IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SE RVICE. (M) 2 H 7 2 4T RT A53EU 2001022200052 20010222 00052 EU 2001 2 22 SIMA0117 1 20010111 A 5320 S53678008222 FLOOR SUPPORT AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 322AC 320 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT FLOOR SUPPORT BETWEEN FRAMES 39 AND 40 CORRODED. MAINTENA NCE REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-25-01. AIRCRAFT WAS RETUREND TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001022200053 20010222 00053 EU 2001 2 22 SIMA0116 1 20010111 A 5320 S536780008216 STRUCTURE AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 322AC 320 SAW - DURNG CPCP-2 INSPECTION, MAINTENANCE REPORTED THE RIGHT AFT ZEE MEMBER BETWEEN FRAMES 39 AND 42 CORRODED. MAINTEN ANCE REMOVED AND REPLACED THE ZEE MEMBER IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001022200054 20010222 00054 EU 2001 2 22 SIMA0115 1 20010111 A 5320 S5367121729800 TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 322AC 320 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE SERVICE DOOR AND PAX DOOR DRAIN TRACKS CORRODED BETWEEN FRAMES 36 AND 39. MAINTENANCE REMOVED AND REPLACED THE DRAIN TRACKS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001022200055 20010222 00055 EU 2001 2 22 20010222SG002 1 20010111 A 5320 S5367121729801 TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 322AC 320 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE SERVICE DOOR AND PAX DOOR DRAIN TRACKS CORRODED BETWEEN FRAMES 36 AND 39. MAINTENANCE REMOVED AND REPLACED THE DRAIN TRACKS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001022200059 20010222 00059 EU 2001 2 22 SIMA0113 1 20010111 A 5315 S5367240420601 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 322AC 320 SAW - DURING CPCP-8 INSPECTION, MAINTENANCE REPORTED THE LEFT SIDE OF FLOORBEAM 34 HAD A CRACK IN A HI-LOCK HOLE. MAINT ENANCE REPAIRED FLOORBEAM 34 IAW SRM 53-00-00 FIGURE 435. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001022200060 20010222 00060 EU 2001 2 22 SIMA0112 1 20010111 A 5320 S5367121729402 SILL AEROSP ATR72 ATR72212 EU PAX DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 322AC 320 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE PAX DOOR SILL PLATE CORRODED BETWEEN FRAMES 36 AND 39. MAINTEN ANCE REMOVED AND REPLACED THE SILL PLATE IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001022200061 20010222 00061 EU 2001 2 22 SIMA0111 1 20010111 A 2731 38S27381971004 CONTROL ROD AEROSP ATR72 ATR72212 EU ELEVATOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 322AC 320 SAW - DURING HMBV-1 INSPECTION REPORTED, THE LEFT AND RIGHT ELEVATOR TRIM TAB CONTROL RODS CORRODED INTERNALLY. MAINTEN ANCE REMOVED AND REPLACED THE CONTROL RODS IAW JIC 27-31-41 RAI-1000. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001022200062 20010222 00062 EU 2001 2 22 20010222SG003 1 20010111 A 2731 38S27381971004 CONTROL ROD AEROSP ATR72 ATR72212 EU ELEVATOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 322AC 320 SAW - DURING HMBV-1 INSPECTION REPORTED, THE LEFT AND RIGHT ELEVATOR TRIM TAB CONTROL RODS CORRODED INTERNALLY. MAINTEN ANCE REMOVED AND REPLACED THE CONTROL RODS IAW JIC 27-31-41 RAI-1000. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0111. (M) 2 H 7 2 4T RT A53EU 2001022200063 20010222 00063 EU 2001 2 22 SIMA0098 1 20010109 A 5753 S5751204920500 GUIDE AEROSP ATR72 ATR72212 EU RT FLAP CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 322AC 320 SAW - DURING MBV-2 INSPECTION MAINTENANCE REPORTED, THE NR 1, 2, 3, AND NR 4 CAM GUIDES CORRODED ON THE RIGHT INBOARD FL AP. MAINTENANCE REMOVED AND REPLACED THE CAM GUIDES IAW CMM 57-52-11. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001022200067 20010222 00067 EU 2001 2 22 SIMA0097 1 20010109 A 5753 S5751204920400 GUIDE AEROSP ATR72 ATR72212 EU LT FLAP CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 322AC 320 SAW - DURING MBV-2 INSPECTION, MAINTENANCE REPORTED THE NR 1, NR 2 AND NR 3 CAM GUIDES CORRODED ON THE LEFT INBOARD FLAP . MAINTENANCE REMOVED AND REPLACED THE CAM GUIDES IAW CMM 57-53-11. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001022200069 20010222 00069 EU 2001 2 22 SIMA0095 1 20010109 A 5753 S57512085008500 FLAP AEROSP ATR72 ATR72212 EU LT WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 322AC 320 SAW - DURNIG MBV-2 INSPECTION, MAINTENANCE REPORTED ALL SIX CAM GUIDES, NR 2 AND NR 6 CAM GUIDE ATTACH BRACKETS, OUTBOAR D BEAM ATTACH BRACKETS, AND THE MIDDLE BEAM ATTACH BRACKET CORRODED ON THE LEFT OUTBOARD FLAP. MAINTENANCE REMOVED AND REPLACED THE FLAP ASSEMBLY IAW JIC 57-53-00-RAI-10000-004. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001022200074 20010222 00074 SO 2001 2 22 SIMA0275 1 20010127 A 2740 3621001007 CONTROL UNIT EMB 145 EMB145LR SO HORIZONTAL STAB FAILED A SIMA K NONE F FLT CONT AFFECTED TO TAKEOFF 1 SW 21 616AE 145092 ORD - FLT 4329 - DURING TAKEOFF AT APPROXIMATELY 150-155 KNOTS CREW REPORTED PITCH TRIM FAIL ON EICAS FOLLOWED BY BOTH B ACK UP SWITCHES FAILING. AT APPROXIMATELY 220 KNOTS CAPTAIN WAS ABLE TO USE BACK UP SWITCHES, WHICH OPERATED THROUGH TH E REMAINDER OF THE FLIGHT. PITCH TRIM 1 FAIL LIGHT REMAINED ON AFTER LANDING. MAINTENANCE REMOVED AND REPLACED HORIZON TAL STAB CONTROL UNIT AND SPOILER CONTROL UNIT IAW EMB MM. FUNCTIONAL CHECK FLIGHT OF AIRCRAFT WAS SATISFACTORY AND AIR CRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001022200075 20010222 00075 SO 2001 2 22 20010222SG005 1 20010127 A 2760 14533022405 CONTROL UNIT EMB 145 EMB145LR SO SPOILER FAILED A SIMA K NONE F FLT CONT AFFECTED TO TAKEOFF 1 SW 21 616AE 145092 ORD - FLT 4329 - DURING TAKEOFF AT APPROXIMATELY 150-155 KNOTS CREW REPORTED PITCH TRIM FAIL ON EICAS FOLLOWED BY BOTH B ACK UP SWITCHES FAILING. AT APPROXIMATELY 220 KNOTS CAPTAIN WAS ABLE TO USE BACK UP SWITCHES, WHICH OPERATED THROUGH TH E REMAINDER OF THE FLIGHT. PITCH TRIM 1 FAIL LIGHT REMAINED ON AFTER LANDING. MAINTENANCE REMOVED AND REPLACED HORIZON TAL STAB CONTROL UNIT AND SPOILER CONTROL UNIT IAW EMB MM. FUNCTIONAL CHECK FLIGHT OF AIRCRAFT WAS SATISFACTORY AND AIR CRAFT WAS RETURNED TO SERVICE. REF SIMA0275. (M) 2 L 7 2 4T RT T00011AT 2001022200076 20010222 00076 EU 2001 2 22 SIMA0214 1 20010121 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU AVIONICS RACK ACTIVATED A SIMA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 21 297AE 340B297 PSM - FLT 4611 - AVIONICS RACK SMOKE DETECTION LIGHT CAME ONE IN FLIGHT ALONG WITH A SMOKE SMELL FROM THE FLIGHT ATTENDA NT. DECLARED EMERGENCY AND LANDED AT PSM. ISSUED MEL 26-3. MAINTENANCE CLEANED CANNON PLUG. REINSTALLED AVIONICS DOO R. OPERATIONAL CHECK WAS GOOD. NO DEFECTS WERE FOUND. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001022200077 20010222 00077 EU 2001 2 22 SIMA0229 1 20010102 A 5320 7253721427 INTERCOSTAL SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 400BR 340B400 SBP - FOUND CORROSION ON INTERCOSTAL AND SUPPORT ANGLE BETWEEN STATIONS 258 AND 236.5 AT BL 12 LEFT SIDE. REPLACED INTE RCOSTAL AND SUPPORT ANGLE. (M) 2 L 7 2 4T RT A52EU 2001022200078 20010222 00078 EU 2001 2 22 20010222SG006 1 20010102 A 5320 7253721447 ANGLE SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 400BR 340B400 SBP - FOUND CORROSION ON INTERCOSTAL AND SUPPORT ANGLE BETWEEN STATIONS 258 AND 236.5 AT BL 12 LEFT SIDE. REPLACED INTE RCOSTAL AND SUPPORT ANGLE. REF SIMA0229. (M) 2 L 7 2 4T RT A52EU 2001022200079 20010222 00079 EU 2001 2 22 SIMA02210 1 20010102 A 5320 7253721439 WEB SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 400BR 340B400 SBP - FOUND CORROSION ON WEB REINFORCEMENT AT STATION 294. REPLACED WEB. (M) 2 L 7 2 4T RT A52EU 2001022200080 20010222 00080 EU 2001 2 22 SIMA02211 1 20010102 A 5320 7253721413 WEB SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 400BR 340B400 SBP - FOUND CORROSION ON WEB PLATE FORWARD OF FRAME 258 AT BL 18.3 TO BL 12. REPLACED WEB. (M) 2 L 7 2 4T RT A52EU 2001022200081 20010222 00081 EU 2001 2 22 SIMA02212 1 20010103 A 5320 MS2047AD45 RIVET SAAB SF340 340B 7860101 EU WEB CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 400BR 340B400 SBP - FOUND CORROSION ON RIVETS THROUGH THE FORWARD END OF WEB AT FUSELAGE STATION 236.5 AT BL 18.3 LEFT SIDE ARE CORROD ED. REPLACED RIVETS. (M) 2 L 7 2 4T RT A52EU 2001022200082 20010222 00082 EU 2001 2 22 SIMA02213 1 20010112 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 400BR 340B400 SBP - FOUND CORROSION ON FUSELAGE FRAME AT STATION 272. REMOVED CORRODED AREA. APPLIED SURFACE TREATMENT AND INSTALLED REINFORCEMENT ANGLE, FILLERS AND TRIPLER IAW SAAB STRUCTURAL REPAIR STATEMENT 340SDS000775. (M) 2 L 7 2 4T RT A52EU 2001022200083 20010222 00083 EU 2001 2 22 SIMA02215 1 20010112 A 5320 7253720337 INTERCOSTAL SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 400BR 340B400 SBP - FOUND CORROSION ON FUSELAGE INTERCOSTAL BETWEEN FUSELAGE STATION 272 AND 288 RIGHT SIDE. REPLACED INTERCOSTAL ANG LE. (M) 2 L 7 2 4T RT A52EU 2001022200084 20010222 00084 EU 2001 2 22 SIMA02216 1 20010112 A 5320 7253711245 PLATE SAAB SF340 340B 7860101 EU LT ENTRY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 400BR 340B400 SBP - FOUND CORROSION ON LEFT ENTRY KICKPLATE. REPLACED KICKPLATE. (M) 2 L 7 2 4T RT A52EU 2001022200085 20010222 00085 EU 2001 2 22 SIMA02217 1 20010101 A 5312 MS20470AD54 RIVET SAAB SF340 340B 7860101 EU AFT BULKHEAD CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 400BR 340B400 SBP - FOUND CORROSION ON RIVETS BELOW FLOOR AT THE AFT CABIN BULKHEAD AT FUSELAGE STATION 630. REPLACED RIVETS. (M) 2 L 7 2 4T RT A52EU 2001022200086 20010222 00086 EU 2001 2 22 20010222SG007 1 20010101 A 5312 MS2047AD55 RIVET SAAB SF340 340B 7860101 EU AFT BULKHEAD CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 400BR 340B400 SBP - FOUND CORROSION ON RIVETS BELOW FLOOR AT THE AFT CABIN BULKHEAD AT FUSELAGE STATION 630. REPLACED RIVETS. REF SI MA02217. (M) 2 L 7 2 4T RT A52EU 2001022200087 20010222 00087 EU 2001 2 22 SIMA0252 1 20010125 A 6121 WARNING LIGHT SAAB SF340 340B 7860101 EU COCKPIT MALFUNCTIONED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 250AE 340B250 LAX - FLT 3057 - CREW ABORTED TAKEOFF DUE TO RIGHT AUTOMATIC POWER RESERVE LIGHT DID NOT ILLUMINATE. CREW ALSO REPORTED LEFT PROPELLER RPM LAGS BEHIND THE RIGHT. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL CHECK OF APR SYSTE M WAS COMPLIED WITH IAW WORK CARD 2813, NO LAG OF PROPELLER RPM WAS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001022200088 20010222 00088 EU 2001 2 22 SIMA0172 1 20010117 A 2120 UNKNOWN AEROSP ATR42 ATR42300 8680920 EU COCKPIT ODOR A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 424MQ 045 MIA - FLT 5439 - DURING CLIMB-OUT, CREW REPORTED A SUDDEN STRONG SMELL IN THE COCKPIT. NO SMOKE WAS PRESENT IN COCKPIT NOR WERE ANY WARNING NOTED DURING THE EVENT. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. MAINTENANCE INSPECTED ELECTR ICAL RACKS AND FOUND NO PROBLEMS. AIRCRAFT WAS RAN ON GROUND WITH NO DEFECTS. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001022200092 20010222 00092 EU 2001 2 22 SIMA0231 1 20010123 A 3350 LIGHT AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 971NA 017 MIA - FLT 5421 - CREW REPORTED FLOOR PROXIMITY LIGHTS IN THE FORWARD SECTION ARE INOPERATIVE. PUT ON MEL AT THIS TIME. MAINTENANCE FOUND CANNON PLUG FOR THE POWER SUPPLY UNIT DIRTY. CANNON PLUG WAS CLEANED, OPS CHECK WAS GOOD AND AIRCRAF T WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001022200095 20010222 00095 SW 2001 2 22 20010208CW007 1 20010112 A 6210 206015001105 BLADE BELL 206 206L 1181522 SW MAIN ROTOR CRACKED E JJWA O OTHER E F VIBRATION/BUFFET FLT CONT AFFECTED AG AGRICULTURE 1 SO 17 522BM 1398 512121 AIRCRAFT WAS FLYING LOW SPEED OVER A CORN FIELD AT NIGHT FOR FROST PREVENTION. ON RETURN LEG TO AIRPORT FOR REFUELING. AT 11:30 PM AIRCRAFT DEVELOPED SEVERE MAIN ROTOR VIBRATION. UPON SHUTDOWN, FOUND CRACK IN BLADE AREA. 1 G 7 1 3U H2SW 2001022200099 20010222 00099 CE 2001 2 22 20010208CW011 1 20010106 A 5520 1016100198 TORQUE TUBE BEECH 1900 1900D 1154162 CE RT ELEVATOR LOOSE A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 838CA 832 UE396 DURING SCHEDULED INSPECTION, RIGHT ELEVATOR WAS FOUND WITH EXCESSIVE, FREE PLAY,. LOOSENESS WAS THE RESULT OF LOOSE RI VETS ON TORQUE TUBE. 2 L 7 2 4T RT A24CE 2001022200100 20010222 00100 NM 2001 2 22 20010222AP005 1 20010220 A 2150 7858943 VALVE AMD FALC50 FALCON2000 2730170 NM AIR CONDITIONING FAILED E I5EA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 07 220EJ 639 6105 FALCON 2000 COCKPIT PAX AND CREW LIGHTS ILLUMINATED ON THE GROUND. FOLLOWING COMPUTER DOWNLOAD FAULT ANALYSIS RECOMMEND ATION, REPLACED CONDITIONING CONTROL VALVE. THIRD FAILURE OF SAME P/N VALVE IN EIGHT MONTHS OF OPERATION - EACH TIME IN A DIFFERENT POSITION IN THE SYSTEM. (FOUR VALVES SAME P/N IN SYS.) NEW AIRCRAFT F2000-0128 SAME FAULT AND ACTION TAKEN AT APPROX. 30 HRS. OF OPERATION. 2 K 7 3 4F RT A50NM 2001022200101 20010222 00101 CE 2001 2 22 20010208CW012 1 20010116 A 3230 LANDING GEAR CESSNA 500 550 2076604 CE NOSE MALFUNCTIONED E UG8A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 225J 5500283 DURING CLIMB, NOSE LANDING GEAR WOULD NOT RETRACT. WE WOULD BRING GEAR UP, RED LIGHT WOULD REMAIN ON AND THEN NOSE GEAR GREEN LIGHT WOULD COME BACK ON. RECYCLED FIVE TIME BEFORE FULL RETRACTION. UNSCHEDULED LANDING 1 L 7 2 4F A22CE 2001022200102 20010222 00102 WP 2001 2 22 AALA20010169 1 20010131 A 2170 1808492 COALESCER BAG DOUG DC9 DC982 3022082 WP ACM BAY DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 553AA 53083 JFK - EN ROUTE LGA-ORD, DETECTED SMOKE AND HAZE IN CABIN AND COCKPIT. DIVERTED JFK AND LANDED WITHOUT FURTHER INCIDENT. REPLACED LEFT AND RIGHT SIDE COALESCER BAGS. ACCOMPLISHED HIGH POWER RUN UP. NO SMOKE OR HAZE NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001022200103 20010222 00103 WP 2001 2 22 AALA20010171 1 20010130 A 2910 5544822 HYDRAULIC LINE DOUG DC9 DC983 3022083 WP ACM BAY LEAKING A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 21 596AA 53286 ORD - FLT 862 - EN ROUTE ORD-EWR, SHORTLY AFTER TAKEOFF DETECTED ELECTRICAL SMELL IN CABIN. FLIGHT ATTENDANT REPORTED S EEING SMOKE AT AFT CABIN. RETURNED ORD AND LANDED WITHOUT FURTHER INCIDENT. REPLACED HYDRAULIC LINE. REPLACED COALESC ER BAGS. PERFORMED PACK BURNOUT PER THE MM. NO SMELL OR SMOKE NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001022200104 20010222 00104 NE 2001 2 22 AALA20010179 2 20010128 A 7261 515107 PUMP DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 1 ENGINE LEAKING A AALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SW 21 594AA 53284 SAT - FLT 1156 - EN ROUTE MEX-DFW, DETECTED LEFT ENGINE OIL LOSS TO THREE QUARTS. DIVERTED SAT AND LANDED WITHOUT FURTH ER INCIDENT. REPLACED OIL PUMP ASSEMBLY. ACCOMPLISHED HIGH POWER ENGINE RUN UP. NO LEAKS NOTED SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2001022200105 20010222 00105 WP 2001 2 22 AALA20010180 1 20010124 A 2613 DETECTOR DOUG DC9 DC982 3022082 WP TAIL MALFUNCTIONED A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 428AA 49340 IND - FLT 1849 - EN ROUTE IND-DFW - SHORTLY AFTER TAKEOFF TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. RETURNED IND AND LANDED WITHOUT INCIDENT. RAN APU AND BOTH PACKS. NO DEFECTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001022200106 20010222 00106 CE 2001 2 22 20010208CW013 1 20010116 A 3233 99144522 ACTUATOR CESSNA 750 750 2076810 CE NLG MALFUNCTIONED E UG8A O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 5113 486 7500013 AFTER LANDING AT PDU THE RED GEAR UNLOCK LIGHT IN THE GEAR SELECTOR HANDLE ASSEMBLY ILLUMINATED AND THE GEAR WARNING HOR N SOUNDED. WHILE TAXING TO PARKING THE GEAR WARNING INDICATIONS CEASED AND ALL INDICATIONS RETURNED TO NORMAL. AFTER P ARKING THE AIRCRAFT, THE WARNING INDICATIONS RETURNED. CESSNA SERVICE CENTER AT GREENSBORO WAS CONTACTED AND TECHNICIAN S WERE DISPATCHED TO REPAIR AIRCRAFT. FAULTY DOWN AND LOCKED SWITCH IN NOSE GEAR RETRACT ACTUATOR. REPLACED THE NOSE GEAR RETRACT ACTUATOR ADN PERFORMED REQUIRED GEAR SWINGS. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4J RT T00007WI 2001022200112 20010222 00112 WP 2001 2 22 AALA20010149 1 20010126 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A K NONE L NO TEST IN INSP/MAINT 1 SW 21 479AA 49654 RDU - DURING OVERNIGHT MAINTENANCE, AFT EMERGENCY EXIT PATH LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SI DE WALL HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001022200113 20010222 00113 WP 2001 2 22 AALA20010100 1 20010122 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP AFT AIRSTAIR DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 578AA 53155 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIR STAIRS INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIG HT CONNECTOR AT AFT AIRSTAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001022200115 20010222 00115 EU 2001 2 22 20010222SG014 1 20010110 A 5347 S53375001223 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AT 431 DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE OUTBOARD, LE FT MIDDLE INBOARD, LEFT AFT INBOARD, RIGHT AFT INBOARD, RIGHT MIDDLE OUTBOARD, RIGHT MIDDLE INBOARD, AND RIGHT FORWARD I NBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNE D TO SERVICE. REF SIMA0223. (M) 2 H 7 2 4T RT A53EU 2001022200116 20010222 00116 EU 2001 2 22 SIMA0232 1 20010123 A 3350 3013000 POWER SUPPLY AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 533AT 533 DFW - MAINTENANCE REPORTED SEVERAL EMERGENCY LIGHTS TO BE INOPERATIVE. ALL FOUR EMERGENCY LIGHT POWER SUPPLY UNITS WERE REMOVED AND REPLACED IAW ATR M. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001022200117 20010222 00117 EU 2001 2 22 20010222SG015 1 20010123 A 3350 3013000 POWER SUPPLY AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 533AT 533 DFW - MAINTENANCE REPORTED SEVERAL EMERGENCY LIGHTS TO BE INOPERATIVE. ALL FOUR EMERGENCY LIGHT POWER SUPPLY UNITS WERE REMOVED AND REPLACED IAW ATR M. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0232. (M) 2 H 7 2 4T RT A53EU 2001022200118 20010222 00118 EU 2001 2 22 20010222SG016 1 20010123 A 3350 3013000 POWER SUPPLY AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 533AT 533 DFW - MAINTENANCE REPORTED SEVERAL EMERGENCY LIGHTS TO BE INOPERATIVE. ALL FOUR EMERGENCY LIGHT POWER SUPPLY UNITS WERE REMOVED AND REPLACED IAW ATR M. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0232. (M) 2 H 7 2 4T RT A53EU 2001022200119 20010222 00119 EU 2001 2 22 20010222SG017 1 20010123 A 3350 3013000 POWER SUPPLY AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 533AT 533 DFW - MAINTENANCE REPORTED SEVERAL EMERGENCY LIGHTS TO BE INOPERATIVE. ALL FOUR EMERGENCY LIGHT POWER SUPPLY UNITS WERE REMOVED AND REPLACED IAW ATR M. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0232. (M) 2 H 7 2 4T RT A53EU 2001022200120 20010222 00120 EU 2001 2 22 SIMA0233 1 20010123 A 3350 FST5X201A FUSE AEROSP ATR72 ATR72212 EU POWER SUPPLY BLOWN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 434AT 434 DFW - MAINTENANCE REPORTED THE PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED FUSE IN POWER SUP PLY 62WL. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001022200121 20010222 00121 EU 2001 2 22 SIMA0241 1 20010113 A 5210 S5217620421002 PAN AEROSP ATR72 ATR72212 EU PAX DOOR DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AT 431 SAW - DURING MBV-1 INSPECTION, MAINTENANCE REPORTED THE PAX DOOR FORWARD UPPER PAN DENTED. MAINTENANCE REPAIRED THE PAN IAW SRM 52-11-10. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001022200122 20010222 00122 EU 2001 2 22 SIMA0262 1 20010126 A 2913 4019501 PUMP AEROSP ATR72 ATR72212 EU HYD BAY FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 322AC 320 MIA - FLT 5339 - CREW REPORTED AFTER TAKEOFF, THE LANDING GEAR WOULD NOT FULLY RETRACT. CREW ALSO REPORTED A THUMPING N OISE AND RECEIVED A LEFT MLG UNLOCK LIGHT. CREW RETURNED TO MIA AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED TH E GREEN SYSTEM HYDRAULIC PUMP IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001022200123 20010222 00123 SO 2001 2 22 SI8MA0215 1 20010121 A 7830 INDICATOR EMB 145 EMB145LR SO ENGINE ILLUMINATED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 649PP 145234 ABI - FLT 9735 - THE FLIGHT CREW ABORTED TAKEOFF DUE TO BOTH THRUST REVERSER DISAGREE INDICATION. (M) 2 L 7 2 4T RT T00011AT 2001022200125 20010222 00125 SO 2001 2 22 20010213CW007 1 20010123 A 2140 94E423 SWITCH PIPER PA31 PA31325 7103105 SO COMBUST HEATER MALFUNCTIONED E P8LA K NONE O OTHER IN INSP/MAINT 1 GL 25 62992 317712013 TROUBLE SHOOTING A MINOR HEATER PROBLEM, COMBUSTION AIR PRESSURE SWITCH WAS FOUND TO BE FAILED IN THE ON POSITION. CONS ULTING WITH A HEATER OVERHAUL SHOP, BEING INFORMED THAT THIS SWITCH SHOULD FAIL ONLY IN THE OFF POSITION, THUS SHUTTING THE HEATER OFF. UNKNOWN HOW LONG THIS SWITCH HAS BEEN DEFECTIVE, AS HEATER WORKS NORMALLY BUT HAS NO SAFETY FACTOR. 1 L 7 2 3O A20SO 2001022200126 20010222 00126 CE 2001 2 22 20010213CW008 1 20010105 A 7931 S2085 INDICATOR LEAR 24 24 5170302 CE GE CJ610 CJ6101 30006 NE COCKPIT INOPERATIVE E IJDA O OTHER O OTHER NR NOT REPORTED 1 WP 01 241JA 131 LEFT ENGINE OIL PRESSURE GAGE NOTED TO HAVE DROPPED AND STUCK AT 12 PSI, OIL PRESSURE ON TAXI FOR TAKEOFF. AC WAS RETURN ED TO MAINTENANCE AND A SERVICEABLE OIL PRESSURE INDICATOR WAS INSTALLED. OIL PRESSURE INDICATED NORMAL ON RUNUP/FUNCTI ONAL CHECK. 2 L 7 2 4J 4 J A10CE 1E16 2001022200127 20010222 00127 CE 2001 2 22 20010213CW009 1 20010110 A 2130 CONTROL UNIT LEAR 24 24 5170302 CE GE CJ610 CJ6101 30006 NE CABIN PRESSURE MALFUNCTIONED E CJPA K NONE O OTHER IN INSP/MAINT 1 NM 03 241JA 131 AC COULD NOT MAINTAIN PRESSURIZATION AND INCREASE IN CABIN ALTITUDE RESULTED IN OXYGEN MASK DROP AND AURAL WARNINGS, AS APPROPRIATE. AC DESCENDED TO FL220 AND CREW WAS ABLE TO MANUALLY RESTORE CABIN ALTITUDE TO NORMAL. AC CONTINUED FLT TO HOME BASE, NORMALLY. AT SUBMISSION OF M&D REPORT, MALFUNCTION HAS NOT BEEN DETERMINED. 8010-4 WILL BE SUBMITTED ON DI SCOVERY CAUSE OF PROBLEM. 2 L 7 2 4J 4 J A10CE 1E16 2001022200132 20010222 00132 EU 2001 2 22 SIMA0114 1 20010111 A 5320 S53375000204 FLOOR SUPPORT AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 322AC 320 SAW - DURNIG CPCP-8 INSPECTION, MAINTENANCE REPORTED THE FLOOR BOARD SUPPORT PLATE AT FRAME 13 RIGHT CORRODED. MAINTENA NCE REMOVED AND REPLACED THE SUPPORT PLATE IAW SRM 51-25-02. AIRCRAFT WAS RETURNED SERVICE. (M) 2 H 7 2 4T RT A53EU 2001022200134 20010222 00134 EU 2001 2 22 SIMA0228 1 20010102 A 5260 7253710871 TRACK SAAB SF340 340B 7860101 EU PAX DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 400BR 340B400 SBP - FOUND CORROSION ON AIR STAIR TRACK AND SUPPORTS. REPLAED AIR STAIRS TRACK. (M) 2 L 7 2 4T RT A52EU 2001022200135 20010222 00135 EU 2001 2 22 SIMA02214 1 20010112 A 5320 7253722001 ANGLE SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 400BR 340B400 SBP - FOUND CORROSION ON PREVIOUS REPAIR FILLER AND SUPPORT ANGLE AT FUSELAGE STATION 258. REPLACED REPAIR FILLER AND S UPPORT ANGLE. (M) 2 L 7 2 4T RT A52EU 2001022200136 20010222 00136 2001 2 22 20010213CW011 4 20010109 A 3457 CONTROL UNIT LEAR 25 25D 5170514 CE GPS FAILED E CJPA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 03 727CS 3410500 25D313 PRIOR TO START, PILOT NOTED SMOKE AND BURNT ODOR IN AREA OF THROTTLE QUADRANT WITH SHIPS BATTERIES ON.MAINTENANCE DID T ROUBLESHOOT AND DISCOVERED ODOR TO BE FROM GPS CONTROL UNIT IN PEDESTAL (GPS WAS INOPERATIVE) GPS UNIT WAS REMOVED FOR R EPAIR AND AIRCRAFT DEFERRED FOR REMOVED GPS. AC RETURNED TO SERVICE. 2 L 7 2 4J A10CE 2001022200146 20010222 00146 EU 2001 2 22 20010222SG010 1 20010110 A 5347 S53570203200 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AT 431 DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE OUTBOARD, LE FT MIDDLE INBOARD, LEFT AFT INBOARD, RIGHT AFT INBOARD, RIGHT MIDDLE OUTBOARD, RIGHT MIDDLE INBOARD, AND RIGHT FORWARD I NBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNE D TO SERVICE. REF SIMA0223. (M) 2 H 7 2 4T RT A53EU 2001022200148 20010222 00148 EU 2001 2 22 20010222SG013 1 20010110 A 5347 S53570203200 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AT 431 DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE OUTBOARD, LE FT MIDDLE INBOARD, LEFT AFT INBOARD, RIGHT AFT INBOARD, RIGHT MIDDLE OUTBOARD, RIGHT MIDDLE INBOARD, AND RIGHT FORWARD I NBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNE D TO SERVICE. REF SIMA0223. (M) 2 H 7 2 4T RT A53EU 2001022200160 20010222 00160 CE 2001 2 22 20010212CW005 1 20010119 A 5310 STRUCTURE CESSNA 500 550 2076604 CE PWA JT15 JT15D1 52060 NE NLG WW CRACKED E UG8A K NONE O OTHER IN INSP/MAINT 1 GL 23 225J 5500283 DURING A HARD OR OVERWEIGHT LANDING, CHECK FOUND THE NOSE WHEEL WELL UPPER STRUCTURE CRACKED JUST FORWARD AND LEFT OF TH E NLG UPLOCK MOUNT. ALSO, NUMEROUS UPLOCK FORWARD MOUNT STRUCTURE RIVETS ARE PULLED THROUGH THE WHEEL WELL SKIN. 1 L 7 2 4F 4 F A22CE E1NE 2001022200161 20010222 00161 CE 2001 2 22 20010212CW006 1 20010119 A 5310 ATTACH FITTING CESSNA 500 550 2076604 CE PWA JT15 JT15D1 52060 NE NLG ACTUATOR BUCKLED E UG8A K NONE O OTHER IN INSP/MAINT 1 GL 23 225J 5500283 AFTER THE NOSE LANDING GEAR ACTUATOR WAS REMOVED, THE NOSE LANDING GEAR ACTUATOR AFT ATTACH STRUCTURE WAS FOUND BUCKLED AND 4 FASTENERS WERE FOUND SHEARED OFF AROUND THE ATTACH FITTING ON THE TOP AND RIGHT HAND SIDE. 1 L 7 2 4F 4 F A22CE E1NE 2001022200162 20010222 00162 EU 2001 2 22 20010213CW012 1 20010203 A 3240 BRAKE AIRBUS 320 A320233 EU IAE V2527 V2527A5 NE MLG MALFUNCTIONED W RJEF O OTHER O OTHER TX TAXI/GRND HDL 1 SO 23 465TA 1374 V1089287 DURING LANDING OF FLIGHTAT HONDURAS AIRPORT, CREW REPORTED AT SPEED OF 80 KNOTS, THE BRAKING BECAME VERY POOR, DUE TO TH IS SITUATION, HIGH SPEED EXIT OF RUNWAY WAS PERFORMED, BUT LEFT MAIN LANDING GEAR GOT STUCK OUTSIDE OF TAXIWAY. NOTE: F IRST REVENUE FLIGHT AFTER DELIVERY FROM AIRBUS INDUSTRY. AC WAS TOWED OUTSIDE OF THE INCIDENT SITE, AT THIS TIME IT REM AINS ON GROUND TO COMPLETE INSPECTIONS ACCORDING TO AMM. 2 L 7 2 4F 4 F RT A28NM E40NE 2001022200165 20010222 00165 CE 2001 2 22 20010213CW014 1 20010109 A 7810 1099500003 STACK BEECH 90 C90A 1152911 CE PWA PT6 PT6A21 52043 EA LT ENGINE CRACKED G BQVR K NONE O OTHER IN INSP/MAINT 1 EA 01 600FL 1296 LJ1540 DURING INSPECTION THE LEFT ENGINE INBOARD EXHAUST STACK WAS FOUND TO BE CRACKED. THE EXHAUST STACK HAS A 1.5 INCH DIAME TER TUBE WELDED TO IT FOR NACELLE INLET DE-ICE. THIS TUBE WAS FOUND CRACKED AROUND THE CIRCUMFERENCE AT ITS WELD ATTACH POINT, AND EXTENDS ALONG THE STACK FLANGE WELD. TOTAL LENGTH IS APPROX 1 INCH. THIS TS THE EIGHTH EXHAUST STACK FOUN D CRACKED ON THIS AIRCRAFT. THE OPERATOR HAS REPORTED PREVIOUS CRACKS FOUND ON LEFT AND RIGHT ENGINE, INBOARD AND OUTBO ARD SIDES. MANUFACTURING PROCESS IS CURRENTLY BEING EVALUATED AND AN IMPROVED EXHAUST STACK IS BEING DEVELOPED. 1 L 7 2 3T 4 T RT 3A20 E4EA 2001022200170 20010222 00170 CE 2001 2 22 DBCR122D0213 1 20010123 A 7400 CONTROL UNIT LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP NR 1 ENGINE FAILED E DBCA O OTHER O OTHER NR NOT REPORTED 1 GL 13 505EE 4016 35505 89374 NR1 ENGINE WOULD NOT START.1-DID TROUBLESHOOT TO FAILED IGNITION CONTROL UNIT. 2-REPLACED UNIT PN 3070378-2 SN452505 OF F, SN0002180160783-OPS CHECK OK 2 L 7 2 4F 4 F A10CE E6WE 2001022300086 20010223 00086 WP 2001 2 23 UPS01834865 1 20010122 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP CABIN BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1,3 STA 250 BL 0 MAIN CABIN SEAT TRACK HAS A BROKEN TANG. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 6D. 2 L 7 4 4F RT 4A25 2001022300087 20010223 00087 WP 2001 2 23 UPS01834866 1 20010121 A 5320 3779659501 FITTING DOUG DC8 DC871F 302199D WP CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1,3 STA 857 LONG 7R END FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 3779659, AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001022300088 20010223 00088 WP 2001 2 23 UPS01834869 1 20010120 A 5320 4611067N FITTING DOUG DC8 DC871F 302199D WP A/C BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1,3 STA 67 LONG 24R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4611067, AND SRM 51-1 -20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001022300089 20010223 00089 WP 2001 2 23 UPS01834870 1 20010122 A 5340 37558471N FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1,3 STA 340 LONG 33R O/B BANANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755847, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001022300090 20010223 00090 WP 2001 2 23 UPS01834871 1 20010121 A 5320 4750521U1 FITTING DOUG DC8 DC871F 302199D WP MAIN CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1,3 STA 834 - 857 LONG 1 SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750521, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001022300091 20010223 00091 WP 2001 2 23 UPS01834872 1 20010131 A 5320 WEB DOUG DC8 DC871F 302199D WP CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1,3 STA 1300 AND 1350 LT CUSP MEMBRANE IS CRACKED. REPAIRED CUSP MEMBRANE IAW EO DC8-5330-2159. 2 L 7 4 4F RT 4A25 2001022300092 20010223 00092 WP 2001 2 23 UPS01834873 1 20010123 A 5313 3750330529 LONGERON DOUG DC8 DC871F 302199D WP CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1,3 STA 600 - 620 LONG 36 SPLICE AND LONGERON ARE CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING AND REPAIRED LONGERON IAW DWG 3750330, AND SRM 53-2-2 FIG 10, 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001022300093 20010223 00093 WP 2001 2 23 UPS01834875 1 20010122 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1, 3 STA 590 RBL 24 SEAT TRACK CORRODED BEYOND LIMITS. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A. 2 L 7 4 4F RT 4A25 2001022300094 20010223 00094 WP 2001 2 23 UPS01834877 1 20010202 A 5320 47516401N FITTING DOUG DC8 DC871F 302199D WP CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1, 3 STA 742 LONG 18L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4751640, AND SRM 51 -1-20D. 2 L 7 4 4F RT 4A25 2001022300095 20010223 00095 WP 2001 2 23 UPS01834878 1 20010123 A 5320 37540231N FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1, 3 STA 290 LONG 33R FWD LOWER LATCH BACKUP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754023, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001022300096 20010223 00096 WP 2001 2 23 UPS01834879 1 20010121 A 5320 575352225 FLOOR SUPPORT DOUG DC8 DC871F 302199D WP CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1, 3 STA 1766 RBL 10 - 18 FLOOR SUPPORT IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED S UPPORT IAW DWG 5753522, AND SRM 51-1-20D, 51-1-21A. 2 L 7 4 4F RT 4A25 2001022300097 20010223 00097 WP 2001 2 23 UPS01834880 1 20010122 A 5320 5751966504 FITTING DOUG DC8 DC871F 302199D WP CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1, 3 STA 940 FRAME FITTING AT RBL 60 IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED FRAM E FITTING IAW 8110-3 APPROVED 8110-3 DH SK 701-332, AND SRM 51-1-20D, 51-1-21, 53-1-0. 2 L 7 4 4F RT 4A25 2001022300098 20010223 00098 WP 2001 2 23 UPS01834882 1 20010123 A 5330 577991321 DOUBLER DOUG DC8 DC871F 302199D WP CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1, 3 STA 600 - 620 FINGER DOUBLER IS CORRODED BEYOND LIMITS BETWEEN LONG 31L-31R. REMOVED, FABRICATED, AND REPLACED FINGER DOUBLER IAW DWG 5779913, AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001022300099 20010223 00099 WP 2001 2 23 UPS01834883 1 20010126 A 5320 588871432 FITTING DOUG DC8 DC871F 302199D WP CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1, 3 STA 1325 LONG 21L T-1 DOOR FITTING IS CRACKED AT CUSP. REMOVED AND REPLACED FITTING IAW DWG 58887 14, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001022300100 20010223 00100 WP 2001 2 23 UPS01834906 1 20010207 A 2710 AILERON DOUG DC8 DC873F 302199F WP WINGS BINDING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:IN AILERONS BINDING CYCLED AILERONS, POWER AND FLIGHT SPOILER HYDRAULIC PUMP AND CYCLED FLAPS, AILER ONS, AND SPEEDBRAKES. OPS CK OK. NO BINDING FOUND. A/C OK FOR SERVICE. IAW MM 27-10-00 2 L 7 4 4F RT 4A25 2001022300103 20010223 00103 WP 2001 2 23 TWAA0102404 1 20010201 A 5315 FLOORBEAM DOUG DC9 DC983 3022083 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT FLOORBEAM CORROSION REMOVED WAS BEYOND LIMITS AT STA 1322, LBL 19 INCHES. INSTALLED FLOORBEAM REPA IR PER SRM 53-05, PAGE 31. TREATED, PRIMED AND PAINTED WHITE AND REPAIR PARTS INSTALLED PER SRM 51-10-3. 2 L 7 2 4F RT A6WE 2001022300104 20010223 00104 WP 2001 2 23 TWAA0102405 1 20010101 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT IN THE AFT CARGO COMPT, THE AFT CARGO TIE DOWN TRACK HAD CORROSION FROM STA 1212 TO 1322, RT SIDE. INSTALLED NEW TRACK PER SRM 51-30-1. 2 L 7 2 4F RT A6WE 2001022300105 20010223 00105 WP 2001 2 23 TWAA0102406 1 20010201 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT FOUND CORRODED FLOOR SUPPORT AT RBL 44 INCHES, STA 160 TO 200. REMOVED CORRODED SUPPORT AND FABRIC ATED NEW SUPPORT. INSTALLED PER SRM 51-30-2. TREATED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001022300106 20010223 00106 WP 2001 2 23 TWAA0102407 1 20010201 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT FOUND CORRODED FLOOR PANEL SUPPORT AT STA 200, RBL 4 INCHES TO LBL 4 INCHES. REMOVED CORRODED SUPP ORT. FABRICATED NEW SUPPORT FROM STOCK AND TREATED PER SRM 51-10-3. INSTALLED PER SRM 51-30-2 AND 51-20-0. 2 L 7 2 4F A6WE 2001022300107 20010223 00107 WP 2001 2 23 TWAA0102408 1 20010201 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 992Z 47095 DURING OP 15 MAINT CHECK FOUND NLG RT STRUT DOOR AFT HINGE CUTOUT HAD A 1 INCH CRACK. STOP DRILLED CRACK. MANUFACTURED REPAIR PER SRM 53-05, PAGE 169 TO 171. TREATED REPAIR AND FUSELAGE SKIN PER SRM 51-10-3. INSTALLED REPAIR REF SRM 53- 05 PAGE 169 TO 171. 2 L 7 2 4F A6WE 2001022300108 20010223 00108 WP 2001 2 23 TWAA0102409 1 20010205 A 5522 SKIN DOUG DC9 DC931 3022065 WP LT ELEVATOR DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 992Z 47095 DURING OP 15 MAINT CHECK THE LT ELEVATOR WAS DAMAGED AT THE T/E AT OUTBOARD END FROM IMPACT. DAMAGE APPROX 1.5 IN BY 4 IN HOLE IN T/E WEDGE. REPLACED SHROUD REF DRAWING 9918453 AND DRAWING 5910412. 2 L 7 2 4F A6WE 2001022300110 20010223 00110 WP 2001 2 23 TWAA0102411 1 20010202 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT FOUND 2 CABIN FLOOR SUPPORTS BETWEEN STA 1182 AND 1250, AND BETWEEN CHAIR TRACKS 2 AND 3, WERE CORR ODED. INSTALLED NEW FLOOR SUPPORTS PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-05. 2 L 7 2 4F A6WE 2001022300111 20010223 00111 WP 2001 2 23 TWAA0102412 1 20010206 A 5230 STOP DOUG DC9 DC982 3022082 WP CARGO DOORWAY CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT FWD CARGO DOOR, TOP AFT EXTERNAL STOP AND LOWER FWD EXTERNAL STOP, HAD CRACKED ATTACH BRACKETS. IN STALLED NEW BRACKETS AND FASTENERS PER SRM 51-30-0. 2 L 7 2 4F A6WE 2001022300112 20010223 00112 WP 2001 2 23 TWAA0102413 1 20010204 A 5720 BRACKET DOUG DC9 DC982 3022082 WP RT WING CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT ON RT WING THE AFT RT END OF KEEL BEAM BOX HAD CORROSION ON DUCT BRACKET. REMOVED AND REPLACED ANG LE PER SPM 6-70-01 USING DRAWING 5936395 CALLING FOR USE OF PART NUMBER 5936395-7 ANGLE. INSTALLED ANGLE USING HI-LOKS. INSTALLED HI-LOKS PER SRM 51-3-5 PAGE 12. INSTALLED ALL FASTENERS USING TORQUE REQUIREMENTS PER SRM 51-30-1, PAGES 11 , 12, AND 13. 2 L 7 2 4F A6WE 2001022300113 20010223 00113 WP 2001 2 23 TWAA0102414 1 20010204 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT FOUND HEAVY CORROSION ON NUMBER 3 CHAIR TRACK, LBL 22 INCHES, STA 1088 TO 1308. REMOVED AND REPLAC ED CHAIR TRACK WITH STOCK PART AT STA 1088 TO 1308. SPLICED NEW TRACK AT STA 1088 PER SRM 53-05, FIG 4F. 2 L 7 2 4F A6WE 2001022300114 20010223 00114 WP 2001 2 23 TWAA0102415 1 20010206 A 5230 FLANGE DOUG DC9 DC982 3022082 WP CARGO DOOR DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT THE FORWARD CARGO DOOR FLANGE AREA UNDER THE CAM LOCK HAD A FIELD REPAIR, ON AFT SIDE. REMOVED OLD REPAIR AND INSTALLED REPAIR PER SRM 52-05, PAGE 110. 2 L 7 2 4F A6WE 2001022300115 20010223 00115 WP 2001 2 23 TWAA0102416 1 20010205 A 5230 FLANGE DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT ON THE AFT CARGO DOOR, THE FLANGE AREA UNDER THE AFT CAMLOCK WAS CRACKED. STOP DRILLED AND INSTAL LED REPAIR DOUBLER PER SRM 52-05, FIG 26A. INSTALLED FASTENERS PER SRM 52-05, FIG 26A. 2 L 7 2 4F A6WE 2001022300116 20010223 00116 WP 2001 2 23 TWAA0102417 1 20010203 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9401W 53137 DURING CHECK-C MAINT LONGERON 18R, STA 636 TO 644, FLOOR WEB HAD CORROSION. REMOVED CORROSION BY CUTTING DAMAGE OUT PER SRM 53-01 PAGE 18. INSTALLED REPAIR PER SRM 53-01 PAGE 18. 2 L 7 2 4F RT A6WE 2001022300117 20010223 00117 WP 2001 2 23 TWAA0102401 1 20010204 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9401W 53137 DURING CHECK-C MAINT RT SIDE OF CABIN FLOOR, MEMBRANE WAS CRACKED OUT NEXT TO SIDE WALL AT STA 1297, JUST FWD OF LAV WAL L. INSTALLED DOUBLER PER SRM 53-01 FIG 2, SHEET 3. 2 L 7 2 4F RT A6WE 2001022300118 20010223 00118 EU 2001 2 23 A6WA200100009 1 20010121 A 5270 WARNING LIGHT BAG BAE146 BAE146200A 1500266 EU LT MLG ILLUMINATED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 292UE E2087 ON DEPARTURE FROM ORD LT GEAR INTRANSIT LIGHT REMAINS ILLUMINATED. MAINTENANCE SECURED LT MLG DOOR IN INFLIGHT POSITION . 2 H 7 4 4F RT A49EU 2001022300120 20010223 00120 EU 2001 2 23 MALA010171 1 20010103 A 3240 50105893 BRAKE ASSY SAAB SF340 340B 7860101 EU LT MLG MISSING A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 439XJ 439 NOTED ON POSTFLIGHT INSPECTION LT INBOARD MAIN GEAR TIRE AND RIM WAS MISSING. MAINTENANCE REPLACED THE LT INBOARD BRAKE (P/N 5010488-2) (S/N OFF AUG91-0751), (S/N ON DEC89-0336), REPLACED RT INBOARD (P/N 5010488-2), (S/N ON JUL98-2709) MAI N TIRE. REPLACED THE LT OUTBOARD BRAKE ASSEMBLY (P/N 5010589-3), (S/N OFF MAR98-0501), (S/N ON JUN90-0436). ALL CHECKS GOOD IAW SF3403240-301/302. 2 L 7 2 4T RT A52EU 2001022300121 20010223 00121 EU 2001 2 23 MALA010172 1 20010201 A 3240 50104882 BRAKE ASSY SAAB SF340 SF340A 7850100 EU RT MLG MISSING A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 106XJ 106 RT INBOARD TIRE MISSING. MAINTENANCE REMOVED AND REPLACED RT WHEEL ASSEMBLY (P/N 5010488-2), (S/N OFF FEB98-2480), (S/N ON OCT00-3322). REMOVED AND REPLACED RT AXLE IAW SMM CHAP 32, ALL SECURITY CHECKS GOOD. MAINTENANCE REPLACED RT INBOA RD BRAKE ASSY IAW SMM CHAP 32, ALL SECURITY CHECKS GOOD. 2 L 7 2 4T RT A52EU 2001022300122 20010223 00122 NE 2001 2 23 MALA010173 3 20010205 A 6140 INDICATOR SAAB SF340 SF340A 7850100 EU ROTOL R389 R3894123F25 NE RT PROP OIL PRES MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 119XJ 119 RT PROP OIL TEMP GAUGE INDICATING IN THE RED ZONE AND SOMETIMES OVER RED LINE PROP OIL PRESSURE INDICATING NORMAL. MAIN TENANCE REPLACED RT PGB OIL COOLER PRESS/TEMP CONTROL REGULATING VALVE AT COOLER, AND REPLACED RT PROP OIL PSI GAUGE. R EFERENCE MM 409 CARD 05351 DBL 1-5 FOR DETAILS. OPS CHECKS GOOD ON GROUND RUN. 2 L 7 2 4T RT A52EU 6 C P30NE 2001022300123 20010223 00123 EU 2001 2 23 MALA010174 1 20010205 A 3060 660714263 LEAD SAAB SF340 SF340A 7850100 EU DEICE SYSTEM DAMAGED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 76XJ 076 FLIGHT 2769, EN ROUTE DEICE MALFUNCTION IN BOTH LOW AND HIGH MODE ON LT PROP. AIR TURNBACK TO MSP. MAINTENANCE REPLACE D DEICE LEAD TO NR 3 PROP BLADE AS REQUIRED (P/N 660714263). OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2001022300124 20010223 00124 EU 2001 2 23 A6WA200100010 1 20010121 A 3350 CONNECTOR BAG BAE146 BAE146300A 1500267 EU CABIN DISCONNECTED A A6WA K NONE L NO TEST IN INSP/MAINT 1 GL 31 611AW E3120 THREE LIGHTS IN FRONT OF PASSENGER CABIN NOT ILLUMINATING. MAINTENANCE CLEANED AND RESECURED CONNECTOR PLUG TO EMERGENC Y POWER SUPPLY ABOVE ROW 7, OPS CHECKED GOOD. 2 H 7 4 4F RT A49EU 2001022300125 20010223 00125 EU 2001 2 23 A6WA200100011 1 20010203 A 2780 COMPUTER BAG BAE146 BAE146300A 1500267 EU LE FLAPS MALFUNCTIONED A A6WA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 31 611AW E3120 AFTER TAKEOFF, FLAPS RETRACTED TO BETWEEN 0-18 DEGREES AND THEN STOPPED. AFTER CHECKLIST, RETRACTED TO 18 DEGREES RET URNED TO LANDING FLAP FAULT ILLUMINATED. MAINTENANCE RESET C/B L9, D24, E12, RERACKED FLAP COMPUTER, CLEARED FLAP FAULT . OP CHECKED GOOD. 2 H 7 4 4F RT A49EU 2001022300126 20010223 00126 EU 2001 2 23 A6WA200100012 1 20010204 A 2620 HC262H0061004 COUPLING BAG BAE146 BAE146300A 1500267 EU NR 3 ENGINE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 614AW E3132 PIPE ASSEMBLY COUPLING, BOTTLE RT, TO COUPLING FLOW VALVE WAS CRACKED ON NR 3 ENGINE. MAINTENANCE REMOVED AND REPLACED NR 3 ENGINE PIPE ASSEMBLY FROM FIRE EXTINGUISHER BOTTLE RT TO FLOW VALVE. 2 H 7 4 4F RT A49EU 2001022300127 20010223 00127 WP 2001 2 23 ABXA0100040 1 20010204 A 2720 CONTROL UNIT DOUG DC8 DC863F 302198F WP RUDDER FAILED A ABXA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 GL 23 811AX 46113 DURING TAXI WHILE PERFORMING THE FLIGHT CONTROL CHECK, THE RUDDER WAS REPORTED TO BE BINDING NEAR THE LAST 1/3 OF RIGHT INPUT TRAVEL. MAINTENANCE INSPECTED AND CYCLED THE RUDDER NUMEROUS TIMES. THE RUDDER POWER CONTROL UNIT AND PRESSURE R EDUCER VALVE WAS INSPECTED IAW DC-8 MM 27-21-07. NO DEFECTS OR BINDING WAS FOUND. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 2001022300128 20010223 00128 2001 2 23 A6WA200100013 4 20010126 A 2565 D31050105 SLIDE BAG BAE146 BAE146200A 1500266 EU PAX DOOR WILL NOT TEST A A6WA K NONE L NO TEST IN INSP/MAINT 1 GL 31 607AW 6336 6336 E2052 LIGHTS ON EMERGENCY ESCAPE SLIDE NOT ILLUMINATE DUE TO PIN IN BATTERY NOT BEING PULLED OUT UPON DEPLOYMENT. SNAP THAT H OLDS PIN LANYARD BECAME DETACHED INSTEAD. MAINTENANCE REMOVED AND REPLACED EMERGENCY SLIDE ASSEMBLY. 2 H 7 4 4F RT A49EU 2001022300129 20010223 00129 WP 2001 2 23 ABXA010025 1 20010130 A 3350 60030451 POWER SUPPLY DOUG DC9 DC941 302207N WP FUSELAGE DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 978AX 82902 525 47628 EMERGENCY LIGHTS WOULD NOT ILLUMINATE ON PREFLIGHT INSPECTION. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT P OWER SUPPLY IAW DC-9 MM 33-53-02. 2 L 7 2 4F A6WE 2001022600098 20010226 00098 2001 2 26 2001UALA00049 4 20010118 A 3160 285W01293 DISPLAY BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE INSTRUMENT PANEL FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 785UA 26954 SMOKE REPORTED AT 4R CACP ON TAXI OUT. AIRCRAFT RETURNED TO GATE. *S/D* BOTH BACKLIGHTS ON THE SCREEN FAILED CAUSING AN OVERHEAT CONDITION AT THE INSULATION OF THE BACKLIGHTS. THE TOUCHSCREEN WAS REPLACED. NO EVIDENCE OF ACFT ELECTRICA L PROBLEMS WERE NOTED. BOEING IS SCHEDULED TO RELEASE, IN EARLY APRIL, SERVICE BULLETINS TO CORRECT THIS ISSUE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001022600099 20010226 00099 NM 2001 2 26 2001UALA00052 1 20010122 A 5320 141W8519 STIFFENER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RADIUS CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 210UA 3002 30216 CRACKED STA 246 FLOORBEAM VERTICAL STIFFENERS AT THE FOLLOWING LOCATIONS: LBL - 7.88, 26.06 RBL - 7.88, 26.06. *S/D* REPLACED STIFFENERS PER SRM 53-10-51, REPAIR 3. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001022600100 20010226 00100 SO 2001 2 26 LR7A01001 1 20010202 A 6120 7383381 BRACKET LKHEED 382 382G 526414U SO HAMSTD 54H 54H60117 NE NR 2 ENGINE OUT OF ADJ A LR7A E ENGINE SHUTDOWN O OTHER LD LANDING 1 AL 03 404LC 4763 230456 NR 2 PROP FLUCUATING OUT OF LIMITS. ENGINE SHUTDOWN ON SHORT FINAL. RPM FLUCTUATING +/- 1 PERCENT. DATE: 2FEB01 TIME: 1047Z. ADJUSTED NR 2 NTS BRACKET IAW HAM STD MM P5059 PARA 4-1, PG I-405 AND I-406. 2 H 7 4 4T A1SO 6 C P906 2001022600104 20010226 00104 NM 2001 2 26 2001UALA00037 1 20010118 A 3240 CONTROL UNIT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE BRAKE SYSTEM MALFUNCTIONED A UALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 29 208UA 30214 ON LANDING ROLLOUT PHASE AT FRA, APPROX 20 KTS, SPEEDBRAKES DOWN, REVERSERS STOWED, BRAKES APPLIED, UNCOMMANDED SWERVE TO RIGHT. NOSE GEAR OFF RUNWAY AND MAINS ON RUNWAY. NO EICAS MSG TOWED TO GATE. NO APPARENT DAMAGE TO AIRCRAFT AND N O INJURIES. *S/D* A CHECK OF THE BRAKES, ANTI-SKID, AUTOBRAKE, AND STEERING SYSTEMS FOUND NO FAULTS OR DISCREPANCIES. AIRCRAFT WAS RETURNED TO SERVICE WITHOUT FURTHER REPORTS OF PROBLEM. THE BRAKE SYSTEM CONTROL UNIT WHICH CONTROLS OPER ATION OF AUTOBRAKE AND ANTI-SKID SYSTEMS WAS REPLACED AS A PRECAUTION. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001022600105 20010226 00105 NM 2001 2 26 2001UALA00057 1 20010125 A 2750 91318506 RELAY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE TE FLAPS FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 590UA 28708 VARIOUS EICAS MESSAGES, FLAP ISOLATION STATUS, RUDDER RATIO, MACH SPEED TRIM, STAB TRIM, ANTISKID AUTOBRAKE. *S/D* FAI LURE OF TWO RELAYS, (LISTED BELOW), CAUSED THE EICAS MESSAGES TO APPEAR. VERIFICATION FLIGHT CONFIRMED ALL SYSTEMS NORM AL AFTER REPLACEMENT OF RELAYS. REPLACED K10104 RELAY PART NUMBER KD4A017 AND K106 RELAY PART NUMBER 9131-8506. 2 L 7 2 4F 4 F RT A2NM E17NE 2001032600211 20010326 00211 NM 2001 3 26 2001UALA00060 1 20010127 A 2410 106106611 CSD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 FAILED A UALA A UNSCHED LANDING G H MULTIPLE FAILURE ELECT. POWER LOSS-50 PC CL CLIMB 1 WP 29 360UA 24453 NR 2 GENERATOR FAILED DURING CLIMBOUT. *S/D* ISOLATED SOURCE OF FAILURE TO NR 2 ENGINE GENERATOR CONSTANT SPEED DRIVE UNIT. THE CSD WAS REPLACED. THE NR 2 AC GENERATOR UNIT AND NR 2 GENERATOR CONTROL UNIT WERE REPLACED AS PRECAUTIONARY. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2001032600212 20010326 00212 NM 2001 3 26 2001UALA00062 1 20010126 A 2780 CONNECTOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LE FLAPS DIRTY A UALA O OTHER J WARNING INDICATION TO TAKEOFF 1 WP 29 7463U 21917 DURING TAKOFF THE LEADING EDGE FLAP INDICATION LIGHT ILLUMINATED. THE AIRCRAFT CONTINUED TO DFW. *S/D* CLEANED AND RE SEATED CONNECTOR ON UPPER SWITCH GROUND. SYSTEM OPERATION CHECKS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001022600106 20010226 00106 NM 2001 2 26 2001UALA00065 1 20010130 A 2613 355604310 LOOP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BODY OVERHEAT DAMAGED A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 385UA 24660 WING-BODY OVERHEAT LIGHT ILLUMINATED. *S/D* FOUND LOOP M487 LOCATED IN LEFT ENGINE STRUT CAVITY SHORTED TO GROUND. RE PLACED LOOP M487. 2 L 7 2 4F 4 F RT A16WE E2GL 2001022600107 20010226 00107 NM 2001 2 26 2001UALA00066 1 20010129 A 5610 WINDOW BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COCKPIT FAILED A UALA O OTHER O OTHER CR CRUISE 1 WP 29 181UA 25278 NUMBER THREE COCKPIT LEFT WINDOW INNER PANE SHATTERED INFLIGHT. CREW NOTED PRIOR TO WINDSHIELD FAILURE WINDOW WAS FROST ED OVER AND NOT DEFOGGING. REMOVED WINDOW AND FOUND CORROSION ON UPPER AND AFT LOWER SIDES. 2 L 7 4 4F 4 F RT A20WE E24NE 2001032700248 20010327 00248 NM 2001 3 27 2001UALA00067 1 20010131 A 2910 AC11504K0232 HOSE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT MLG LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 534UA 25129 LEFT HYDRAULIC SYSTEM QUANTITY WENT TO ZERO. GEAR EXTENDED PRIOR TO SYSTEM DEPLETION. FLAPS EXTENDED WITH ALTERNATE SY STEM. *S/D* REPLACED LEFT GEAR DOWNLOCK PRESSURE LINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001022600109 20010226 00109 NM 2001 2 26 2001UALA00069 1 20010130 A 2410 IDG BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LEFT AND RIGHT CONTAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 LEFT AND RIGHT IDG AND STARTER OIL FOUND CONTAMINATED. 2 L 7 2 4F 4 F RT A1NM E24NE 2001032700249 20010327 00249 EU 2001 3 27 2001UALA00071 1 20010201 A 2131 90221570210 CONTROLLER NORD AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN PRESSURE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 407UA 456 CABIN PRESSURE SYSTEMS 1 AND 2 FAILED IN FLIGHT. *S/D* CABIN PRESSURE CONTROLLERS NR 1 AND NR 2 WERE BOTH REPLACED. T HERE HAVE BEEN NO CABIN PRESSURE ANOMALIES SINCE THE REPAIR WAS ACCOMPLISHED. 2 L 7 2 4F 4 F RT A28NM E40NE 2001022600112 20010226 00112 EU 2001 2 26 QXEA01000091 1 20010205 A 3350 900542 BATTERY PACK FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 482US 11231 PDX- ROWS 10 - 17 SEAT EMERGENCY LIGHTING INOPERATIVE. REMOVED AND REPLACED ROW 14 BATTERY PACK. OPERATIONAL CHECKS GO OD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001022600113 20010226 00113 WP 2001 2 26 TWAA0102501 1 20010207 A 3350 0105606003 HARNESS DOUG DC9 DC983 3022083 WP GALLEY FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9405T 53141 THE EGRESS LIGHT SYSTEM HAD TWO RED LIGHTS INOPERATIVE FOR THE REAR GALLEY. REPLACED CABLE ASSEMBLY. CHECK-C 10-23-00 STL. 2 L 7 2 4F RT A6WE 2001022600114 20010226 00114 NM 2001 2 26 TWAA0102502 1 20010207 A 3397 WIRE BOEING 757 757231 1384950 NM CABIN BROKEN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 705TW 28479 THE EGRESS LIGHTS FORWARD OF THE LAV DOOR WERE INOPERATIVE. REPAIRED CABLE BY SPLICING IN A CONNECTOR. CHECK-C 12-31- 99 LAX. 2 L 7 2 4F RT A2NM 2001022600115 20010226 00115 NM 2001 2 26 TWAA0102503 1 20010207 A 3397 WIRE BOEING 767 7673Y0 NM CABIN BROKEN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 640TW 25411 THE EGRESS LIGHTS AT ROWS 37 AND 38, LT SIDE OF THE AIRCRAFT, WERE INOPERATIVE. FOUND FEEDER WIRE BROKEN AT SEAT 37. R EPAIRED BROKEN WIRE PER MM 20-51-01 PAGE 201. CHECK-C 5-15-00. 2 L 7 2 4F RT A1NM 2001022600116 20010226 00116 WP 2001 2 26 TWAA0102504 1 20010207 A 3350 105606002 SOCKET DOUG DC9 DC983 3022083 WP ROW 33 FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 939AS 49657 THE EGRESS LIGHTS WERE INOPERATIVE AT ROW 33. SPLICED IN NEW LIGHT SOCKET. CHECK-C 1-20-01 STL. 2 L 7 2 4F RT A6WE 2001022600117 20010226 00117 WP 2001 2 26 TWAA0102506 1 20010204 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT FOUND CABIN FLOOR TRACK AT LBL 54, THE NUMBER 1 TRACK WAS GROUND BEYOND LIMITS AT STA 1237 AND 1303 . REMOVED DAMAGED TRACK STA 1174 TO 1303. MADE NEW PER DRAWING 5930966. INSTALLED PER SPM 6-70-01 AND SRM 51-30-1. 2 L 7 2 4F A6WE 2001022600118 20010226 00118 WP 2001 2 26 TWAA0102507 1 20010204 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT AT LBL 54, STA 1309, FOUND CORROSION ON CABIN CHAIR TRACK FLANGE. REMOVED CORROSION PER SPM 6-80-0 1. REMOVED DAMAGED TRACK PER DRAWING 5930966. INSTALLED PER SPM 6-70-01 AND SRM 51-30-1. 2 L 7 2 4F A6WE 2001022600119 20010226 00119 WP 2001 2 26 TWAA0102508 1 20010204 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT AT STA 1106 TO 1221, AND 1168 TO 1222, THE AFT CARGO COMPT LT TIE DOWN TRACK WAS CORRODED IN SEVERA L LOCATIONS. FABRICATED NEW TRACK AND SPLICED AND INSTALLED PER SRM 53-05, FIG 46. 2 L 7 2 4F RT A6WE 2001022600120 20010226 00120 WP 2001 2 26 TWAA0102509 1 20010204 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 DURING CHECK-C MAINT THE AFT CARGO COMPT TIE DOWN TRACK WAS CORRODED IN SEVERAL LOCATIONS FROM STA 1222 TO 1322, 16L BL. REMOVED AND REPLACED WITH NEW TRACK PER SRM 53-01, PAGE 1 ITEM C. 2 L 7 2 4F RT A6WE 2001022600121 20010226 00121 NM 2001 2 26 01FDEA00083 1 20010208 A 2430 0802032501 TRANSFORMER BOEING 727 727233 138408A NM NR 1 FAILED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 267FE 21673 OUTPUT DIFFERENCE BETWEEN TR 1 & 2 VS ESSENTIAL TR. REMOVED AND REPLACED NR 1 T/R PER IAW MM 24-53-000 & SYS OPS CK NOR MAL. 2 L 7 3 4F RT A3WE 2001022600122 20010226 00122 NM 2001 2 26 01FDEA00084 1 20010207 A 5320 FITTING BOEING 727 72725C 138400H NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DURING ROUTINE INSP, RIGHT BS 870 TERMINAL FITTING FOUND CRACKED AT FASTENER HOLE AT ROW 4 HOLE 3 & ROW 4 HOLE 3. 2 L 7 3 4F A3WE 2001022600123 20010226 00123 NM 2001 2 26 0100326633 1 20010202 A 2120 UNKNOWN BOEING 747 747227B 1384888 NM AFT CABIN ODOR A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 633US 21991 DURING CRUISE, THERE WAS AN ELECTRICAL WIRE BURNING SMELL IN AFT LAVATORIES. MAINTENANCE THOROUGHLY EXAMINED LAV EQUIPM ENT. NO EVIDENCE OF ODOR WAS FOUND. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F A20WE 2001022600124 20010226 00124 NM 2001 2 26 0100336307 1 20010206 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 667US 24222 DURING LINE CHECK, MAINTENANCE FOUND NUMEROUS FLOOR MOUNTED EMERGENCY LIGHTS INOPERATIVE. RECONNECTED WIRING. OPERATIO NAL TEST NORMAL. 2 L 7 4 4F RT A20WE 2001022600125 20010226 00125 NE 2001 2 26 0100346636 2 20010130 A 7200 ENGINE BOEING 747 747251B 1384892 NM PWA JT9 JT9D7R4G2 52054 NE NR 3 MALFUNCTIONED A NWAA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 01 636US 23547 725345 DURING TAKEOFF ROLL, THE NR 3 ENGINE WAS SLOW TO ACCELERATE AND THEN SUFFERED A COMPRESSOR STALL. THE TAKEOFF WAS ABORT ED AT APPROXIMATELY 100 KTS AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE ENGINE WITH NO DEFECTS NOT ED. THE EVBC WAS REPLACED AND AN ENGINE TRIM RUN WAS PERFOMRED WITH ALL INDICATIONS NORMAL. 2 L 7 4 4F 4 F A20WE E3NE 2001022600126 20010226 00126 WP 2001 2 26 0100359619 1 20010201 A 3350 BATTERY DOUG DC9 DC932 3022066 WP TAIL SECTION INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 619NW 47518 DURING LINE CHECK, FOUND ALL CATWALK EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES FOR CATWALK EMERGENCY EXIT LIGHTING. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 2001022600127 20010226 00127 NM 2001 2 26 0100366613 1 20010203 A 3230 PIN BOEING 747 747251B 1384892 NM NLG INSTALLED A NWAA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 GL 01 613US 20358 DURING CLIMB, THE NOSE LANDING GEAR DID NOT RETRACT. AIRCRAFT DUMPED 120,000 LBS OF FUEL AND RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REMOVED THE NOSE LANDING GEAR GROUND LOCK SAFETY PIN. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F A20WE 2001022600128 20010226 00128 EU 2001 2 26 0100373240 1 20010131 A 2120 SMOKE AIRBUS 320 A320212 EU CABN DETECTED A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 01 340NW 372 DURING APPROACH, PASSENGERS AND CREW SMELLED SMOKE AND SAW SLIGHT HAZE IN CABIN. FLIGHT MADE NORMAL LANDING AND PROCEED ED TO THE GATE WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCIES. 2 L 7 2 4F RT A28NM 2001022600129 20010226 00129 EU 2001 2 26 0100383226 1 20010203 A 2900 HYDRAULIC SYSTEM AIRBUS 320 A320211 3930320 EU YELLOW SYSTEM LOW A NWAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 01 326US 282 FOLLOWING APPLICATION OF TAKEOFF POWER, RECEIVED HYD Y RSVR LO LVL MESSAGE. ABORTED TAKEOFF AT 60 KNOTS AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE SERVICED THE YELLOW HYDRAULIC SYSTEM BUT NO LEAKS WERE FOUND. OPERATIONAL CHEC K OK. 2 L 7 2 4F RT A28NM 2001022600130 20010226 00130 EU 2001 2 26 0100393207 1 20010201 A 2910 D3247002308800 B-NUT AIRBUS 320 A320211 3930320 EU RT MLG WW LOOSE A NWAA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 307US 106 DURING CRUISE, RECEIVED HYD Y RSVR LO LVL MESSAGE. FOLLOWED ECAM AND COM PROCEDURES. CONTINUED TO FINAL DESTINATION AN D LANDED WITHOUT INCIDENT. MAINTENANCE SECURED A LOOSE B-NUT AT THE YELLOW SYSTEM BRAKE ACCUMULATOR. SERVICED SYSTEM W ITH NO OTHER LEAKS NOTED. 2 L 7 2 4F RT A28NM 2001022600131 20010226 00131 NM 2001 2 26 0100403118 1 20010205 A 2120 SMOKE AIRBUS A319 A319114 NM CABIN DETECTED A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 01 318NB 1325 DURING TAXI TO THE GATE, SMOKE WITH A STRONG BURNING ODOR WAS REPORTED IN THE CABIN AFT OF THE WINGS. MAINTENANCE TROUB LESHOOTING REVEALED NO DISCREPANCIES. 2 L 7 2 4F RT A28NM 2001032900191 20010329 00191 NM 2001 3 29 01FDEA00085 1 20010207 A 5280 FITTING BOEING 727 72725C 138400H NM LT MLG DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DURING ROUTINE INSP, LT MLG DOOR ACTUATOR RIB FITTING FOUND CRACKED BY HFEC. *S/D* REMOVED AND REPLACED LT MLG DOOR PE R IAW BAC 727 MM 32-12-001. 2 L 7 3 4F A3WE 2001032900190 20010329 00190 NM 2001 3 29 01FDEA00086 1 20010207 A 5230 FITTING BOEING 727 72725C 138400H NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DURING ROUTINE INSP, MAIN CARGO DOOR LATCH CAM SUPPORT FITTING AT FS 487.1 FOUND CRACKED. *S/D* REMOVED AND REPLACED F ITTING PER IAW FEDEX EO 7-5230-7-2323F PART 2. 2 L 7 3 4F A3WE 2001032900189 20010329 00189 NM 2001 3 29 01FDEA00087 1 20010207 A 5230 FITTING BOEING 727 72725C 138400H NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DURING ROUTINE INSP, MAIN CARGO DOOR LATCH CAM SUPPORT FITTING AT FS 500 FOUND CRACKED. *S/D* REMOVED AND REPLACED FIT TING PER IAW FEDEX EO 7-5230-7-2323F PART 2. 2 L 7 3 4F A3WE 2001032900188 20010329 00188 NM 2001 3 29 01FDEA00088 1 20010207 A 5320 FITTING BOEING 727 72725C 138400H NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DURING ROUTINE INSP, BS 870 TERMINAL FITTING WEB FOUND CRACKED NEAR STR 10R. *S/D* REMOVED AND REPLACED FITTING PER IA W SR DRW 27-53-026 AND EA 7-5310-56279. 2 L 7 3 4F A3WE 2001022600132 20010226 00132 NM 2001 2 26 DHL2001707001 1 20010207 A 3040 XW20548MIA MOTOR BOEING 727 72722 1384002 NM WINDSHIELD WIPER INOPERATIVE A DHLA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 707DH 18321 CAPTS WINDSHIELD WIPERS INOP IN ALL SPEEDS. REMOVED AND REPLACED CAPTS WIPER MOTOR IAW MM 30-42-11. 2 L 7 3 4F A3WE 2001032600036 20010326 00036 NM 2001 3 26 01FDEA00090 1 20010207 A 3350 LIGHT BOEING 727 72725C 138400H NM CABIN INOPERATIVE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DURING ROUTINE INSP, FWD ENTRY DOOR EMERGENCY EVACUATION SLIDE LIGHT FOUND INOP. *S/D* REMOVED AND REPLACED BULB. OPS CK GOOD PER IAW BAC 727 MM 33-50-121-2. 2 L 7 3 4F A3WE 2001022600133 20010226 00133 NM 2001 2 26 HNAA0100011 1 20010206 A 5410 85420006001 DOOR DHAV DHC8 DHC8102 2809003 NM NR 2 NACELLE SEPARATED A HNAA O OTHER D INFLIGHT SEPARATION CR CRUISE 1 EA 07 906HA 6919 009 NR 2 MLG FWD DOOR CAME OFF IN FLIGHT, DAMAGING SURROUNDING NACELLE STRUCTURE. REPLACED GEAR DOOR AND REPAIRED NACELLE S TRUCTURE PER EO8-54-01-061. 2 H 7 2 4T RT A13NM 2001032600037 20010326 00037 2001 3 26 01FDEA00093 4 20010207 A 2565 CLIP BOEING 727 72725C 138400H NM ESCAPE SLIDE BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DURING ROUTINE INSP, FWD ENTRY DOOR EMERGENCY EVACUATION SLIDE CONTAINER RELEASE SPRING CLIPS BENT. *S/D* REMOVED AND REPLACED PER IAW BAC 727 MM 25-60-013-4. 2 L 7 3 4F A3WE 2001022600134 20010226 00134 EU 2001 2 26 DHL2001367507 1 20010130 A 5532 ATTACH ANGLE AIRBUS 300 A300B4203 3930306 EU VERTICAL STAB CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH MSN265 C-CHECK--VERT STAB RIB 1 ATTACH ANGLE TO FRONT SPAR HAS CORROSION ON SURFACE. N/R 78826. CORROSION REMOVED IAW SRM 51-4 0-11, METAL REMOVED= .006-.008, WITHIN LIMITS REF SRM 55-30-00, PG 602 LIMITS, REPROTECTED AREA. 2 L 7 2 4F RT A35EU 2001022600135 20010226 00135 EU 2001 2 26 DHL2001367510 1 20010129 A 5710 DOUBLER AIRBUS 300 A300B4203 3930306 EU WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH MSN265 C-CHECK--CORROSION AT DOUBLER FITTED TO REAR SPAR AFT OF NR 5 RT DOWN DRIVE GEARBOX. REMOVED CORROSION IAW SRM 51-40-11 , REMOVED METAL =0.001, WITHIN LIMITS. RETREATED AREA. 2 L 7 2 4F RT A35EU 2001022600136 20010226 00136 WP 2001 2 26 01FDEA00094 1 20010102 A 5320 AEA05012 WEB DOUG DC10 DC1010F 3022111 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 399FE 48262 DURING D-CK, 1 INCH CRACK FOUND AT Y=1386 ON AEA0501-2 KEEL WEB UPPER SPLICE ONLY. REMOVED AND REPLACED TITANIUM REPAIR DOUBLER PER IAW FEDEX EA 8-5314-56044. 2 L 7 3 4F A22WE 2001032900187 20010329 00187 NM 2001 3 29 01FDEA00096 1 20010208 A 5330 SKIN BOEING 727 72725C 138400H NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DURING ROUTINE INSP, FUSELAGE SKIN FOUND CRACKED AT BS 1313 LEFT AND AFT OR THE AIRSTAIR FRAME CUTOUT. *S/D* REAM UP H OLE PER IAW BAC 727 SRM 53-30-1. REMOVED AND REPLACED FASTENER PER IAW BAC 727 SRM 51-30-2. 2 L 7 3 4F A3WE 2001022700027 20010227 00027 NM 2001 2 27 01FDEA00067 1 20010131 A 5320 AJC702119 CLIP DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 582FE 48420 AFT FUSELAGE COMPARTMENT ZONE 312 BS Y 2046 CANT, CROWN AREA, CLIP FOUND CRACKED. *S/D* REMOVED AND REPLACED CLIP PER SRM 51-35-01 & 51-33-01 VOL II AND DWG AJC 7021. 2 L 7 3 4F RT A22WE 2001022700028 20010227 00028 NM 2001 2 27 01FDEA00068 1 20010131 A 5340 AJC737239 ATTACH ANGLE DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 582FE 48420 AFT FUSELAGE COMPARTMENT ZONE 312 BS 2014 CROWN AREA, ANGLE FOUND CRACKED. *S/D* REMOVED AND REPLACED PER SRM 51-35-01 & 51-33-01 VOL II AND DWG AJC 7372. 2 L 7 3 4F RT A22WE 2001022700029 20010227 00029 NM 2001 2 27 UPS01234902 1 20010203 A 2611 SMOKE DETECTOR BOEING 727 72727C 138400J NM CARGO BAY FAILED A IPXA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 910UP 19117 INSPECTION TYPE:IN LOWER CARGO SMOKE M208340, ALERT H19221. REMOVED AND REPLACED SMOKE DETECTION SYSTEM CONFIGURATION M ODULE PER MM 26-18-01 AND OPS CHECKED SYSTEM PER MM 26-18-00 SYSTEM OPS CHECKS GOOD THIS CLEARS M208340 PLACARD REMOVED. 2 L 7 3 4F A3WE 2001022700030 20010227 00030 NM 2001 2 27 UPS01534898 1 20010207 A 2612 WARN HORN BOEING 757 75724APF 1384969 NM APU FIRE WARNING INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 435UP 25466 INSPECTION TYPE:IN APU FIRE WARNING GROUND HORN INOP. *S/D* PERFORMED APU FIRE WARNING TEST PER MM 26-15-00. NO DEFEC TS NOTED. OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2001022700031 20010227 00031 WP 2001 2 27 UPS01834899 1 20010208 A 5240 SKIN DOUG DC8 DC871F 302199D WP SERVICE DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:N/A R1 SERVICE DOOR HAS 1 .125 INCH CRACK IN LOWER AFT RADIUS D208801. *S/D* TRANSFERRED TO UPS NON RO UTINE 936452 TO CLEAR D208801. ONE TIME FERRY PERMIT ORD/GSO FOR REPAIR OF R1 DOOR. 2 L 7 4 4F RT 4A25 2001040900322 20010409 00322 NM 2001 4 9 01FDEA00098 1 20010207 A 5540 RIB BOEING 727 72725C 138400H NM RUDDER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DURING ROUTINE INSP, UPPER RUDDER, UPPER THRUST HINGE RIB FOUND CRACKED BY HFEC IN LEFT FWD LWR RADIUS. *S/D* REMOVED AND REPLACED RIB PER IAW BAC 727 51-30-2 AND BAC SB 727-55-68. 2 L 7 3 4F A3WE 2001022700032 20010227 00032 NM 2001 2 27 XNA01003 1 20010208 A 2781 INDICATOR BOEING 727 727* NM COCKPIT MALFUNCTIONED A TC8A D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 23 793A 20774 DURING TAXI FLAPS POS TO 150 LEADING EDGE FLAP INDICATOR REMAINED AMBER. 2 L 7 3 4F RT A3WE 2001040900321 20010409 00321 NM 2001 4 9 01FDEA00099 1 20010207 A 5540 RIB BOEING 727 72725C 138400H NM RUDDER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DURING ROUTINE INSP, LWR RUDDER, LWR THRUST HINGE RIB FLANGE FOUND CRACKED BY HFEC AT RIGHT AFT END. *S/D* REMOVED AND REPLACED RIB PER IAW BAC 727 SRM 51-30-2 AND BAC SB 727 DD-68. 2 L 7 3 4F A3WE 2001022700033 20010227 00033 EU 2001 2 27 XNA01002 1 20010120 A 3240 BRAKE ASSY AIRBUS 300 A300B4203 3930306 EU MLG MALFUNCTIONED A TC8A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 474AS 219 DURING TAXI WITH SLIGHT BRAKE APPLICATION, BRAKES APPEARED TO GRAB SUDDENLY. ANTI-SKID SWITCH IN NORM. 2 L 7 2 4F RT A35EU 2001032600035 20010326 00035 NM 2001 3 26 01FDEA00100 1 20010207 A 5311 FRAME BOEING 727 72725C 138400H NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DURING ROUTINE INSP, BS 1070 FRAME FOUND CRACKED AT STR 28R. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-40 -3, 51-30-2. 2 L 7 3 4F A3WE 2001022700035 20010227 00035 NM 2001 2 27 AT0100064 1 20010101 A 5320 FLOOR SUPPORT BOEING 737 7372L9 1384497 NM CARGO BAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 FOUND AFT CARGO PIT AREA WAS CORRODED AT SUPPORT BEAMS AT BS 947 - 987. REMOVED CORROSION, TREATED, PRIMED, FABRICATED AND INSTALLED REPAIR SUPPORT BEAMS IAW B737 SRM 51-21-31, 53-10-9 AND TIMCO SERVICE ORDER 151151-23634. 2 L 7 2 4F RT A16WE 2001022700037 20010227 00037 NM 2001 2 27 AT0100066 1 20010103 A 5330 SKIN BOEING 737 7372L9 1384497 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 FOUND AT LEFT WHEEL WELL, CORROSION ON CUT OUT SKIN AROUND FASTENERS. FABRICATED DOUBLERS AND INSTALLED IAW B737 SRM 51 -10-6, 51-10-2, 51-30-2. 2 L 7 2 4F RT A16WE 2001022700038 20010227 00038 NM 2001 2 27 AT0100067 1 20010103 A 5310 PANEL BOEING 737 7372L9 1384497 NM GALLEY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 FOUND SIDE WALL PANEL BEHIND G1 GALLEY IS CORRODED. REMOVED CORROSION, FABRICATED REPLACEMENT PANEL IAW B737 SRM 53-00, 51-40-3, 51-10-2, 51-30-2. 2 L 7 2 4F RT A16WE 2001022700039 20010227 00039 NM 2001 2 27 AT0100068 1 20010107 A 5310 STRUCTURE BOEING 737 7372L9 1384497 NM LAVATORY WALL CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 FOUND LAVATORY WALL SUPPORT AT BS 308 CORRODED AT FLANGE. REMOVED CORRODED LAVATORY WALL, FABRICATED AND INSTALLED REPA IR IAW B737 SRM 51-40-4. 2 L 7 2 4F RT A16WE 2001022700040 20010227 00040 NM 2001 2 27 AT0100069 1 20010108 A 5347 SEAT TRACK BOEING 737 7372L9 1384497 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 FOUND LEFT OUTBOARD SEAT TRACK HAS CORROSION BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK IAW B737 SRM 53-10-5 FIGURE 1. 2 L 7 2 4F RT A16WE 2001022700041 20010227 00041 NM 2001 2 27 AT0100070 1 20010109 A 5321 FLOOR PANEL BOEING 737 7372L9 1384497 NM CABIN DELAMINATED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 FOUND CABIN FLOOR DELAMINATED AT BS 767 - 727. REMOVED, FABRICATED AND INSTALLED REPAIR PANEL IAW B737 SRM 53-20-1, 53- 20-2, 51-10-1, BCMM 25-00-66. 2 L 7 2 4F RT A16WE 2001022700042 20010227 00042 NM 2001 2 27 AT0100071 1 20010111 A 5321 FLOOR PANEL BOEING 737 7372L9 1384497 NM CABIN TORN A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 FOUND CABIN FLOOR SKIN TORN AT BS 767 - 827. REMOVED, FABRICATED AND INSTALLED REPAIR PANEL IAW B737 SRM 53-20-1, 53-20 -2, 51-10-1 AND BCMM 25-00-66. 2 L 7 2 4F RT A16WE 2001022700043 20010227 00043 NM 2001 2 27 AT0100072 1 20010101 A 5320 FLOOR SUPPORT BOEING 737 7372L9 1384497 NM CARGO BAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 FOUND CORROSION IN AFT CARGO PIT AREA ON SUPPORT BEAM AT BS 857. REMOVED CORROSION, FORMED L ANGLE REPAIR, TREATED, PRI MED AND INSTALLED IAW B737 SRM 51-30-2, 53-10-1, 51-20-11, 51-40-3. 2 L 7 2 4F RT A16WE 2001022700044 20010227 00044 NM 2001 2 27 CALA0100104 1 20010205 A 5311 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13624 27528 INSPECTION FOUND A 7 INCH CRACK IN AFT CARGO COMPARTMENT CENTER BELT FRAME TO SKIN ATTACH AREA AT STA 807, S27L TO S27R. THE CRACKED FRAME WAS REMOVED AND A NEW BOTTOM FRAME WAS INSTALLED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001022700045 20010227 00045 NM 2001 2 27 CALA0100105 1 20010205 A 5320 ANGLE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14383 26312 INSPECTION FOUND A .5 INCH CRACK IN ANGLE AT STA 380, L26L. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001022700046 20010227 00046 NM 2001 2 27 CALA0100106 1 20010205 A 5315 FLOORBEAM BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13624 27528 INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, RBL 42. A STRAP REPAIR WAS INSTALLED IAW SRM 53-00-51. 2 L 7 2 4F RT A16WE 2001022700047 20010227 00047 NM 2001 2 27 CALA0100107 1 20010206 A 5320 PANEL BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14383 26312 INSPECTION FOUND AFT CARGO PIT RT TRANSITION PANEL CORRODED AT STA 727 - 767 AND LT TRANSITION PANEL CORRODED AT STA 727 - 847. THE RT TRANSITION PANEL WAS REMOVED AND REPLACED IAW SRM 51-10-02. THE CORRODED SECTION OF LT TRANSITION PANEL WAS REMOVED AND REPLACED IAW SRM 53-60-53. 2 L 7 2 4F RT A16WE 2001022700048 20010227 00048 NM 2001 2 27 CALA0100108 1 20010206 A 5330 SKIN BOEING 737 737824 13844BZ NM FUSELAGE GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27246 28956 THE FUSELAGE SKIN WAS GOUGED FORWARD OF THE AFT LAV SERVICE PANEL AT STA 827. THE GOUGED SECTION OF SKIN WAS REMOVED AN D THE AREA WAS REPAIRED IAW SRM 53-00-01. 2 L 7 2 4F RT A16WE 2001022700049 20010227 00049 EA 2001 2 27 COMA0160210 1 20010206 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 EA TE FLAPS SYSTEM ILLUMINATED A COMA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 949CA 7080 FLAP FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE IAW AD 98-20-01. 2 L 7 2 4F RT A21EA 2001022700050 20010227 00050 WP 2001 2 27 MWEA010146 1 20010208 A 5320 5935024 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 INTERCOSTAL CRACKED (2 PLACES), LONGERON 5 RIGHT, STATION 766 - 786. REMOVED CRACKED INTERCOSTAL, FABRICATED AND INSTAL LED NEW INTERCOSTAL. 2 L 7 2 4F A6WE 2001022700051 20010227 00051 WP 2001 2 27 MWEA010147 1 20010208 A 5320 59101609 CLIP DOUG DC9 DC914 3022034 WP FUSELAGE TOOL DAMAGE A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 TOOLING MARKS ON ANGLE BRACKET ATTACHED TO AFT LOWER SIDE OF INTERCOSTAL ON LONGERON 9 LEFT BETWEEN STATION 503 AND 484. REMOVED AND REPLACED CLIP. 2 L 7 2 4F A6WE 2001022700052 20010227 00052 NM 2001 2 27 UPS01234895 1 20010131 A 5313 STRINGER BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C, CORROSION ON STR 19 L AT BS 360 IN E & E BAY. STR 19L REPLACED IAW DRAWING 65-18420. 2 L 7 3 4F A3WE 2001022700053 20010227 00053 NM 2001 2 27 UPS01234896 1 20010129 A 5311 FRAME BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C, RT MLG WHEEL WELL SUSPECT CRACK TO VERT CHORD AT BS 870 TO KEEL BEAM JOINT, 16.5 INCHES FROM BOTTOM O F CHORD. REPAIR CARRIED OUT IAW B727-5330-1995-B. 2 L 7 3 4F A3WE 2001022700054 20010227 00054 NM 2001 2 27 UPS01234897 1 20010131 A 5320 WEB BOEING 727 72722C 138400F NM LT MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C, LT MLG WHEEL WELL, SUSPECT CRACKS IN KEEL BEAM WEB, AREA FWD OF APU CUTOUT COVERED BY REPAIR PLATE. REPAIR CARRIED OUT IAW EO B727-5330-1995-B. 2 L 7 3 4F A3WE 2001022700055 20010227 00055 NM 2001 2 27 UPS01234903 1 20010125 A 2750 JACKSCREW BOEING 727 72722C 138400F NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C, NR 5 TRANSMISSION YOKE ASSY & JACKSCREW ARE BADLY CORRODED. JACKSCREW REPLACED IAW MM 27-51-41. 2 L 7 3 4F A3WE 2001022700056 20010227 00056 NM 2001 2 27 UPS01234910 1 20010207 A 3350 BATTERY BOEING 727 72722C 138400F NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHTS FOUND INOP, PRE-FLT. FOUND BATTERIES WEAK, INSTALLED NEW BATTERIES. OPS CKS NORMAL. 2 L 7 3 4F A3WE 2001022700057 20010227 00057 WP 2001 2 27 UPS01834907 1 20010207 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:PFLT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK. CKS OK. 2 L 7 4 4F RT 4A25 2001022700058 20010227 00058 WP 2001 2 27 UPS01834911 1 20010209 A 3260 WARNING LIGHT DOUG DC8 DC871F 302199D WP NLG MALFUNCTIONED A IPXA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 750UP 45950 INSPECTION TYPE:N/A, NOSE GEAR DOWN GREEN LT EXTINGUISHES. DOOR NOT LATCHED LIGHTS COME ON WHEN NOSE WHEEL STEERING IS ACTIVATED AND RELEASED TO NEUTRAL POS D208866. TRANSFERRED TO UPS NR 215073. ONE TIME FERRY FLT FROM ATL TO SAT (DHC) FOR REPAIR ON NOSE & MAIN GEAR FAULTS. 2 L 7 4 4F RT 4A25 2001022700059 20010227 00059 NM 2001 2 27 QXEA0100093 1 20010206 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT MALFUNCTIONED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 816PH 54 SEA- COCKPIT EMERGENCY LIGHT INOPERATIVE WHEN CONTROL SWITCH IS ON POSITION. INTERMITTENTLY ILLUMINATED ON WHEN SWITCH IN ARM OR OFF POSITION. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT ASSEMBLY. OPERATIONAL TEST NORMAL. AIRCRAFT RETU RNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001022700060 20010227 00060 EU 2001 2 27 QXEA0100094 1 20010206 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486US 11237 GEG- AFT OVERHEAD EXIT SIGN HAS LAMP INOPERATIVE. REMOVED AND REPLACED SIGN ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAF T RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001022700061 20010227 00061 EU 2001 2 27 QXEA0100095 1 20010204 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 491US 11156 SEA- NR 1 AND NR 2 OVERHEAD EMERGENCY EXIT SIGNS HAVE INOPERATIVE BULBS. REPLACED NR 1 AND NR 2 EXIT SIGN CIRCUIT BOARD S. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001022700062 20010227 00062 NM 2001 2 27 QXEA0100092 1 20010204 A 2121 83428002001 COOLING FAN DHAV DHC8 DHC8202 2809007 NM COCKPIT OVERHEATED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 09 348PH 484 SEA- NOTICED A HOT SMELL IN THE COCKPIT DURING DESCENT AFTER SHUTDOWN, HEARD LOUD NOISE, FOLLOWED BY A BURNING SMELL. AVIONICS FAN CIRCUIT BREAKER POPPED. REPLACED INDICATOR COOLING FAN NR 1. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED T O SERVICE. 2 H 7 2 4T RT A13NM 2001022700063 20010227 00063 NM 2001 2 27 DHL200171207C 1 20010130 A 5320 INTERCOSTAL BOEING 727 72729 1384007 NM CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CK; FWD CARGO COMPT BEAM LOWER PART INTERCOSTAL CRACKED 2 INCHES (CEILING) AT STA 720.000 LBL 46. PERFORMED STOP D RILL IAW SRM 51-10-1 PG 6B, CLEANED TREATED AND PRIMED IAW SRM 51-10-2 PG 1-2, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-40 PG 1. 2 L 7 3 4F A3WE 2001022700064 20010227 00064 NM 2001 2 27 DHL200171208C 1 20010130 A 5350 ANGLE BOEING 727 72729 1384007 NM RT WING FAIRING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CK; RT WING FAIRING SUPPORT ANGLE CRACKED .5 INCH AT STA 330.000. PERFORMED STOP DRILL IAW SRM 51-10-1, PG 6B, CLE ANED,TREATED AND PRIMED AREA IAW SRM 51-10-2, PG 1-2, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-40, PG 1-2. 2 L 7 3 4F A3WE 2001022700065 20010227 00065 SO 2001 2 27 C2XA01IA066 1 20010207 A 3230 MS33205 CIRCUIT BREAKER EMB 145 EMB145ER SO LANDING GEAR TRIPPED A C2XA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 27 15941 145035 HSV-FLIGHT3951, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT ON TAKEOFF. THE AIRCRAFT RETURNED TO HSV WHER E IT LANDED WITHOUT INCIDENT. MAINTENANCE RESET THE AIR/GROUND CIRCUIT BREAKER, OPERATIONALLY CHECKED RETRACTION SYSTEM WITH NO DEFECTS FOUND. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001022700073 20010227 00073 SO 2001 2 27 C2XA01IA073 1 20010207 A 3350 MS33205 CIRCUIT BREAKER EMB 145 EMB145ER SO COCKPIT POPPED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15941 145035 IAH - FLIGHT 3951, DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE MID-CABIN EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE RESET THE AFFECTED CIRCUIT BREAKER, AND PERFORMED AN OPERATIONAL TEST WITH NO DEFECTS NOTED. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001022700074 20010227 00074 SO 2001 2 27 C2XA01IA074 1 20010130 A 3350 836604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16724 120171 IAH - DURING MAINTENANCE INSPECTION, THE MIDDLE EMERGENCY AISLE PATH LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENAN CE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001022700075 20010227 00075 NM 2001 2 27 AT0100073 1 20010128 A 5315 FLOORBEAM BOEING 737 7372L9 1384497 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 FOUND FLOORBEAM AT BS 1016 UPPER FORWARD FLANGE CORRODED. REMOVED, FABRICATED AND INSTALLED REPAIR BEAM IAW REO-L00367 REV D. 2 L 7 2 4F RT A16WE 2001022700076 20010227 00076 NM 2001 2 27 AT0100074 1 20010107 A 5321 FLOORBOARD BOEING 737 7372L9 1384497 NM CABIN PUNCTURED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 FOUND FLOORBOARD AT BS 540 - 616 HAS TWO PUNCTURES AND IS MISSING HARDWARE. REMOVED, FABRICATED, AND INSTALLED REPAIR F LOORBOARD IAW REO-00363. 2 L 7 2 4F RT A16WE 2001022700077 20010227 00077 NM 2001 2 27 AT0100075 1 20010107 A 5321 FLOORBOARD BOEING 737 7372L9 1384497 NM CABIN PUNCTURED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 FOUND FLOORBOARD AT BS 520 - 540 HAS PUNCTURES AND CRACKS ON METAL SKIN. REMOVED, FABRICATED AND INSTALLED REPAIR FLOOR BOARD IAW REO-L00363. 2 L 7 2 4F RT A16WE 2001022700078 20010227 00078 EU 2001 2 27 MALA010175 1 20010203 A 2611 CGAB120101 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY MALFUNCTIONED A MALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 429XJ 429 WHEN DEPRESSING RT START SWITCH, CARGO SMOKE LIGHT ILLUMINATES, GOES OUT WHEN SWITCH IS RELEASED. MAINTENANCE REPLACED FWD CARGO SMOKE DETECTOR P/N CGAB1201-01 S/N OFF 97, S/N ON 115, BOTH LT P/N 4078-7, S/N OFF P2128, S/N ON G01911& RT BA TTERIES P/N 4078-7, S/N OFF 076322, S/N ON N2379 AND THE WEU. 2 L 7 2 4T RT A52EU 2001022700079 20010227 00079 EU 2001 2 27 MALA010176 1 20010205 A 3610 460200 PERISEAL BAC 146 AVRO146RJ85A 1500097 EU ENGINE BLEED LEAKING A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 532XJ E2366 NR 2 LT ZONE HI TEMP LIGHT ILLUMINATED EN ROUTE. AIR TURNBACK TO DTW. UPON INSPECTION MAINTENANCE FOUND PERI-SEALS LEA KING AT LEADING EDGE ON NR 1 PYLON, REMOVED AND REPLACED PERI-SEALS IAW AVRO MM CHAP 30. P/N 460-200. PERFORMED GROUND RUNS AND ANTI-ICE SYSTEM AND LEAK CHECK GOOD, ALL CHECK GOOD AT THIS TIME. 2 H 7 4 4F RT A49EU 2001022700080 20010227 00080 NE 2001 2 27 MALA010177 2 20010207 A 7200 200304015 ENGINE BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 2 FAILED A MALA A UNSCHED LANDING R E Y PARTIAL RPM/PWR LOSS VIBRATION/BUFFET ENGINE STOPPAGE CL CLIMB 1 GL 15 512XJ E2328 NR 2 ENGINE FAILED AT 500 - 1000 FT ABOVE GROUND DURING TAKE-OFF. CREW HEARD A BANG AND AIRCRAFT VIBRATED. ENGINE SHUT DOWN, AIR TURNBACK TO MSP. MAINTENANCE REPLACED ENGINE, REF TASK CARD 7100-502 P/N 2-003-040-15, S/N OFF LF07616, S/N O N P07654, ALL RUNS AND LEAK CHECK GOOD. 2 H 7 4 4F 4 F RT A49EU E6NE 2001022700081 20010227 00081 CE 2001 2 27 GLBA2001027 1 20010205 A 2750 BZ7RW82255518T SWITCH BEECH 1900 1900D 1154162 CE TE FLAPS FAILED A GLBA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 CE 01 226GL UE226 RETURN TO BLOCK - FLAPS WOULD NOT RETRACT. REPLACED SAFETY SWITCH. 2 L 7 2 4T RT A24CE 2001022700082 20010227 00082 CE 2001 2 27 GLBA2001026 1 20010205 A 3260 10136459813 CONTROL UNIT BEECH 1900 1900D 1154162 CE MLG ANNUNCIATOR FAILED A GLBA O OTHER P NO WARNING INDICATION AP APPROACH 1 CE 01 251GL UE251 NO TRANSIT OR GEAR INDICATION LIGHTS WHEN GEAR SELECTED DOWN. REMOVED AND REPLACED ANNUNCIATOR CONTROL PCB AND POWER SO URCE BOARD. 2 L 7 2 4T RT A24CE 2001022700083 20010227 00083 SO 2001 2 27 GLBA2001029 1 20010206 A 5270 PLATE EMB 120 EMB120ER 3260203 SO CARGO DOOR OUT OF ADJ A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 01 71GL 120071 RETURN TO BLOCK - CARGO DOOR ANNUNCIATOR ILLUMINATED. ADJUSTED TARGET PLATE, OPS CHECKED SYSTEM GOOD. 2 L 7 2 4T RT A31SO 2001022700084 20010227 00084 2001 2 27 GLBA2001031 4 20010206 A 3421 6224565001 GYRO BEECH 1900 1900D 1154162 CE COCKPIT INOPERATIVE A GLBA D RETURN TO BLOCK O OTHER CL CLIMB 1 CE 01 247GL 7499 4356 UE247 RETURN TO BLOCK - NR 1 VG FAILED. REMOVED AND REPLACED VERTICAL GYRO. 2 L 7 2 4T RT A24CE 2001032900126 20010329 00126 NM 2001 3 29 01FDEA00101 1 20010207 A 5311 FRAME BOEING 727 72725C 138400H NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DURING ROUTINE INSP, BS 1070 FRAME CRACKED AT STR 29R. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-40-3, 51 -30-2. 2 L 7 3 4F A3WE 2001022700085 20010227 00085 WP 2001 2 27 ABXA010039 1 20010201 A 5250 AR25291GR41 LATCH DOUG DC9 DC941 302207N WP COCKPIT DOOR DEFECTIVE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 COCKPIT DOOR WOULD NOT OPEN FROM THE OUTSIDE. MAINTENANCE INSPECTED AND REPLACED THE COCKPIT DOOR LATCH IAW DC-9 MM. 2 L 7 2 4F A6WE 2001022700086 20010227 00086 WP 2001 2 27 ABXA010024 1 20010126 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC932F 3022067 WP FUSELAGE DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 904AX 47040 THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE DURING THE PREFLIGHT INSPECTION. MAINTENANCE INSPECTED AND REPLACED T HE EMERGENCY LIGHT BATTERIES IAW DC-9 MM 33-53-00. 2 L 7 2 4F A6WE 2001022700087 20010227 00087 WP 2001 2 27 ABXA010040 1 20010204 A 5540 RUDDER DOUG DC8 DC863F 302198F WP TAIL BINDING A ABXA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 811AX 46113 DURING TAXI WHILE PERFORMING THE FLIGHT CONTROL CHECK, THE RUDDER WAS REPORTED TO BE BINDING NEAR THE LAST 1/3 OF RIGHT INPUT TRAVEL. MAINTENANCE INSPECTED AND CYCLED THE RUDDER NUMEROUS TIMES. THE RUDDER POWER CONTROL UNIT AND PRESSURE R EDUCER VALVE WAS INSPECTED IAW DC-8 MM 27-21-07. NO DEFECTS OR BINDING WAS FOUND. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 2001022700088 20010227 00088 WP 2001 2 27 ABXA010034 1 20010202 A 5313 39248091 LONGERON DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 CORROSION WAS FOUND ON LONGERON 29L, FUSELAGE STATION 617 - 642. MAINTENANCE REPLACED THE LONGERON IAW DC-9 SRM 51-30-5 AND 51-30-2. 2 L 7 2 4F A6WE 2001022700089 20010227 00089 WP 2001 2 27 ABXA010035 1 20010202 A 5311 5911448503 FRAME DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 FUSELAGE FRAME AT STATION 560 LONGERON 29R WAS CORRODED. MAINTENANCE INSPECTED AND REPAIRED THE FRAME IAW DC-9 SRM 53-0 3 PAGE 4E FIG 2A. 2 L 7 2 4F A6WE 2001022700090 20010227 00090 WP 2001 2 27 ABXA010036 1 20010202 A 5310 99577403 SHEAR TIE DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 FUSELAGE SHEAR TIE AT FRAME 675 WAS CORRODED ON LEFT SIDE AT KEEL AREA. MAINTENANCE REPLACED THE SHEAR TIE IAW DC-9 SRM . 2 L 7 2 4F A6WE 2001022700091 20010227 00091 WP 2001 2 27 ABXA010037 1 20010202 A 5313 3924810 LONGERON DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 LONGERON 26R WAS CRACKED FROM FUSELAGE STATION 617 TO 642. MAINTENANCE INSPECTED AND REPLACED THE LONGERON IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 2001022700092 20010227 00092 WP 2001 2 27 ABXA010038 1 20010206 A 3260 0351881008 SOCKET DOUG DOUG DC9 DC932 3022066 WP COCKPIT INTERMITTENT A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 988AX 47084 THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED INTERMITTANTLY AFTER GEAR WAS FULLY RETRACTED, AND CONTINUED TO INT ERMITTANTLY ILLUMINATE FOR THE REMAINDER OF THE FLIGHT. FLIGHT CREW RECYCLED THE LANDING GEAR. MAINTENANCE INSPECTED A ND REPLACED THE RIGHT MAIN LANDING GEAR UNSAFE INDICATION LIGHT SOCKET IAW DC-9 MM 32-61-00. LANDING GEAR INDICATION OP S CHECKED GOOD ON GEAR SWING CHECKS. 2 L 7 2 4F A6WE 2001022700093 20010227 00093 EA 2001 2 27 COMA0160212 1 20010207 A 4920 APU CNDAIR CL600 CL6002B19 EA APU BAY FIRE A COMA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 SO 01 981CA 7163 WHEN APU WAS SHUTDOWN, FIRE IN TAIL PIPE WAS VISIBLE FOR 5 TO 10 MINUTES. DEFERRED MAINT ON APU IAW MEL. 2 L 7 2 4F RT A21EA 2001022700094 20010227 00094 NM 2001 2 27 ABXA010027 1 20010131 A 3260 WARNING LIGHT BOEING 767 767231 1385131 NM MLG ILLUMINATED A ABXA O OTHER J WARNING INDICATION AP APPROACH 1 GL 23 707AX 22570 A DISAGREE MESSAGE WAS DISPLAYED AND A GEAR AMBER LIGHT ILLUMINATED WITH A GEAR GREEN DOWN INDICATION LIGHT. RECYCLED L ANDING GEAR AND INDICATIONS WERE NORMAL. MAINTENANCE INSPECTED AND PERFORMED A BITE CHECK. THE CHECK SHOWED NR 1 AND N R 2 GEAR LEVER SWITCH ON PSEU. MAINTENANCE CHECKED THE LANDING GEAR CONTROL MODULE IAW B767 MAINTENANCE MANUAL 32-31-01 . NO DEFECTS WERE FOUND. 2 L 7 2 4F RT A1NM 2001022700095 20010227 00095 WP 2001 2 27 ABXA010042 1 20010209 A 5311 99196132 FRAME DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 FUSELAGE FRAME AT STATION 617 WAS FOUND TO HAVE TWO CRACKS (1.25 AND .5 INCH LENGTHS). MAINTENANCE INSPECTED AND REPAIR ED THE FRAME IAW ABX REA D953-39920-MR. 2 L 7 2 4F A6WE 2001022700096 20010227 00096 WP 2001 2 27 ABXA010043 1 20010209 A 5313 591143271 LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 LONGERON 2L WAS CRACKED. MAINTENANCE INSPECTED AND REPAIRED THE LONGERON IAW DC-9 SRM 53-01, 51-30. 2 L 7 2 4F A6WE 2001022700097 20010227 00097 WP 2001 2 27 ABXA010044 1 20010209 A 5313 591143271 LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 LONGERON 2R WAS CRACKED. MAINTENANCE INSPECTED AND REPAIRED THE LONGERON IAW DC-9 SRM 53-01, 53-30. 2 L 7 2 4F A6WE 2001022700098 20010227 00098 WP 2001 2 27 ABXA010045 1 20010209 A 5311 9911840166 SHEAR TIE DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 SHEAR TIE AT FUSELAGE STATION 1087, LONGERON 2R WAS CRACKED. MAINTENANCE INSPECTED AND REPLACED THE SHEAR TIE IAW DC-9 SRM 51-30. 2 L 7 2 4F A6WE 2001022700099 20010227 00099 WP 2001 2 27 ABXA010028 1 20010202 A 5330 DOUBLER DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 INTERNAL FUSELAGE DOUBLER AT STA 642 L30 WAS CORRODED FORWARD OF THE KIDNEY PANEL. MAINTENANCE INSPECTED AND REPLACED TH E DOUBLER IAW DC-9 SRM 51-30-1 AND DRAWING 9923434. 2 L 7 2 4F A6WE 2001022700100 20010227 00100 WP 2001 2 27 ABXA010029 1 20010202 A 5230 591015707 LATCH DOUG DC9 DC941 302207N WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 REPAIR NEAR THE AFT BAG BIN AFT LATCH WAS CRACKED. MAINTENANCE INSPECTED AND REPLACED THE BAG BIN DOOR IAW DC-9 SRM AND ABX NEA52300001-005. 2 L 7 2 4F A6WE 2001022700101 20010227 00101 WP 2001 2 27 ABXA010030 1 20010202 A 5313 3924050501 LONGERON DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 FUSELAGE LONGERON 28L WAS CRACKED. MAINTENANCE INSPECTED AND REPLACED THE LONGERON AT 28L IAW DC-9 SRM 51-30-2 AND 51-3 0-5. 2 L 7 2 4F A6WE 2001022700102 20010227 00102 WP 2001 2 27 ABXA010031 1 20010202 A 5753 5910042503 VANE DOUG DC9 DC941 302207N WP LT FLAP CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 FIXED VANE ON LEFT WING WAS CORRODED INTERNALLY. MAINTENANCE INSPECTED AND REPLACED THE LEFT FIXED VANE IAW DC-9 MM. 2 L 7 2 4F A6WE 2001022700103 20010227 00103 WP 2001 2 27 ABXA010032 1 20010202 A 5313 592481659 LONGERON DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 LONGERON AT STRINGER 29L WAS EXFOLIATED ON THE HORIZONTAL FLANGE AT APPROX FUSELAGE STATION 675. MAINTENANCE INSPECTED AND REPLACED THE LONGERON IAW DC-9 SRM 51-30. 2 L 7 2 4F A6WE 2001022700104 20010227 00104 WP 2001 2 27 ABXA010033 1 20010202 A 5313 39248091 LONGERON DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 LONGERON 30 AT FUSELAGE STATION 617 - 642 WAS CRACKED. MAINTENANCE INSPECTED AND REPLACED THE LONGERON IAW DC-9 SRM 51- 30-5 AND 51-30-2. 2 L 7 2 4F A6WE 2001022700105 20010227 00105 WP 2001 2 27 ABXA010041 1 20010209 A 5230 5910141 PAN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 FORWARD LOWER CARGO DOOR LOWER PAN WAS CRACKED IN THE RADIOUS. MAINTENANCE INSPECTED AND REPAIRED THE CRACKED AREA IAW DC-9 SRM 52-03 FIG 8. 2 L 7 2 4F A6WE 2001022700106 20010227 00106 WP 2001 2 27 ABXA010026 1 20010131 A 3260 H1410051 SWITCH DOUG DOUG DC9 DC941 302207N WP LT MLG FAILED A ABXA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 23 976AX N7625 47596 DURING APPROACH WHEN LANDING GEAR WAS SELECTED DOWN, THE NOSE LANDING GEAR DOWN (GREEN) LIGHT FAILED TO ILLUMINATE. MIS SED APPROACH, PROCEDURES WERE COMPLIED. THE CREW REPLACED THE NOSE LANDING GEAR DOWN INDICATOR LIGHT BULBS AND RECYCLED THE LANDING GEAR. THE LANDING GEAR FUNCTIONED PROPERLY. DURING THE SECOND APPROACH, THE LEFT LANDING GEAR UNSAFE LIGH T FAILED TO ILLUMINATE. ANOTHER MISSED APPROACH WAS CONDUCTED. MAINTENANCE INSPECTED AND FOUND THE LEFT MAIN LANDING G EAR GROUND PROX SWITCH TO BE DEFECTIVE. THE SWITCH WAS REPLACED IAW DC-9 MM 32-60-01. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2001022700107 20010227 00107 2001 2 27 COMA0160213 4 20010207 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 924CA 7026 STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001022700108 20010227 00108 2001 2 27 COMA0160215 4 20010208 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 971CA 7145 STALL FAIL CAUTION MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001022700109 20010227 00109 EA 2001 2 27 COMA0160214 1 20010208 A 2750 FLAP CNDAIR CL600 CL6002B19 EA TRAIL EDGE STUCK A COMA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 805CA 7354 FLAPS FAIL MESSAGE. FLAPS STUCK AT 24 DEGREES. RESET THE FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2001022700110 20010227 00110 EA 2001 2 27 COMA0160216 1 20010206 A 5210 601R317231 COLLAR CNDAIR CL600 CL6002B19 EA DOOR WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 917CA 7017 DURING PASSENGER DOOR RIGGING FOUND LOWER LATCH CAM (P/N 601R31723-1) WOULD NOT LOCK TO PREVENT DOOR PINS FROM COMING OU T WITH HANDLE IN OPEN POSITION. MACHINED LATCH AREA OF CAM (P/N 601R31723-1) IAW WVAC EO 601R-52-2209. 2 L 7 2 4F RT A21EA 2001022700111 20010227 00111 EA 2001 2 27 COMA0160217 1 20010207 A 5240 601R31148127 PLATE CNDAIR CL600 CL6002B19 EA SERVICE DOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 7022 THRESHOLD PLATE AFT OF SERVICE DOOR FS 349.00 TO 364.00 AT WL 73 RBL 42 IS CORRODED (P/N 601R31148-127) FORMED REPAIR DO UBLER USING 7075-T6 .063 INCH. REMOVED AREA AND SPLICED NEW SECTION OF THRESHOLD IN IAW WVAC EO 601R-53-2201B. 2 L 7 2 4F RT A21EA 2001022700112 20010227 00112 EA 2001 2 27 COMA0160218 1 20010208 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 EA CABIN CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 7022 FLOORBEAM CRACKED AT FS 409 + 16, RBL 9.0. REPAIRED FLOORBEAM AT FS 409 + 16 RBL 9.0 IAW WVAC EO 601R-53-2207. 2 L 7 2 4F RT A21EA 2001022700113 20010227 00113 EA 2001 2 27 COMA0160219 1 20010209 A 5320 601R310377 SPLICE CNDAIR CL600 CL6002B19 EA FUSELAGE MISMANUFACTURED A COMA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 920CA 7022 TWOSPLICE PLATES( P/N 601R31030-77) WERE FABRICATED INCORRECTLY BY THE MANUFACTURER. REMOVED, FABED AND REPLACED SPLICE PLATES IAW WVAC EO 601R-53-2194. 2 L 7 2 4F RT A21EA 2001022700114 20010227 00114 NM 2001 2 27 SCNA01012 1 20010204 A 2613 DETECTOR BOEING 727 727227 1384078 NM NR 3 OVERHEAT MALFUNCTIONED A SCNA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 275AF 22092 DURING DEPARTURE FROM MSP THE NUMBER THREE ENGINE OVERHEAT LIGHT ILLUMINATED. PERFORMED COM PROCEDURES THE LIGHT EXTING UISHED. CLIMB TO 25,000 WAS RESUMED, THE CABIN PRESSURE CONTINUED TO CLIMB AT 400 FPM IN BOTH MANUAL AND AUTO MODE. RE TURNED TO MSP, REMOVED AND REPLACED THE NUMBER THREE STRUT OVERHEAT DETECTOR. OPERATIONAL CHECKS GOOD. 2 L 7 3 4F A3WE 2001022700115 20010227 00115 NM 2001 2 27 SCNA01013 1 20010208 A 3350 1102833 LIGHT BOEING 727 727227 1384078 NM AIRSTAIR INOPERATIVE A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 275AF 22092 DURING A MAINTENANCE LINE CHECK THE AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED T HE EMERGENCY LIGHT IN THE AFT STAIRWAY OVERHEAD. OPERATIONAL CHECKS GOOD. 2 L 7 3 4F A3WE 2001022700116 20010227 00116 NM 2001 2 27 AT0100076 1 20010209 A 3350 6013211 POWER SUPPLY BOEING 737 7372L9 1384497 NM CARGO BAY DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 464AT 21278 FOUND FORWARD ESCAPE SLIDE LIGHT AT L1 AND R1 FAILED TO ILLUMINATE. REMOVED AND REPLACED BATTERY PACK POWER SUPPLY ASSE MBLY IAW B737 MM33-51-71. 2 L 7 2 4F RT A16WE 2001022700117 20010227 00117 NM 2001 2 27 C1HA200192001 1 20010125 A 3230 656021132 ACCESSORY UNIT BOEING 727 727121C 1384044 NM LT MLG FAILED A C1HA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 292AS 21458 AFTER GEAR RETRACTION LEFT MAIN GEAR DOOR INDICATED DOWN. CYCLED GEAR A 2ND TIME AND LEFT AND RIGHT GEAR DOORS INDICATE D DOWN. ALSO, LEFT AND RIGHT GEAR INDICATED DOWN AND LOCKED WITH GEAR HANDLE IN THE UP POSITION AND IN THE OFF POSITION . REMOVED AND REPLACED LANDING GEAR MODULE, ALL CKS NORMAL. 2 L 7 3 4F A3WE 2001022700118 20010227 00118 NM 2001 2 27 C1HA200192002 1 20010208 A 3350 900542 CHARGER BOEING 727 727121C 1384044 NM RT WING FAILED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 292AS 21458 RT FWD EMERGENCY OVERWING WALKWAY LIGHT INOP. REMOVED AND REPLACED BATTERY AND CHARGER. 2 L 7 3 4F A3WE 2001022700119 20010227 00119 NM 2001 2 27 C1HA200194007 1 20010208 A 5297 WIRE BOEING 727 727290 138408W NM E/E DOOR BROKEN A C1HA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 GL 15 294AS 22146 A/C DID NOT PRESSURIZE DOOR ANNUNCIATOR LIGHTS ALL OUT. (AIR RETURN). FOUND E&E COMPARTMENT DOOR UNSECURED AND BROKEN W IRE TO DOOR SWITCH. REPAIED WIRE, SECURED DOOR AND CHECKS NORMAL. 2 L 7 3 4F A3WE 2001022700120 20010227 00120 NM 2001 2 27 C1HA200194008 1 20010205 A 2751 BEARING BOEING 727 727290 138408W NM FLAP SWITCH DISPLACED A C1HA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 15 294AS 22146 ON TAKEOFF ROLL THE TAKEOFF WARNING HORN SOUNDED. ABORTED T/O WITH NO BRAKING REQUIRED. (REPEAT WRITE UP). REPOSITION ED BEARING ON MICROSWITCH IAW 27-26-0. ADJUSTED AND TEST OF T/O WARNING SYSTEM NORMAL. 2 L 7 3 4F A3WE 2001022700121 20010227 00121 NM 2001 2 27 C1HA200196001 1 20010204 A 3260 656021132 ACCESSORY UNIT BOEING 727 7272J4 1384006 NM LT MLG FAULTY A C1HA O OTHER N FALSE WARNING CR CRUISE 1 GL 15 696CA 22574 LEFT MAIN GEAR UNSAFE LIGHT COMES ON INTERMITTANTLY. REMOVED AND REPLACED LDG ACCY UNI,T ALL CKS NORMAL. 2 L 7 3 4F RT A3WE 2001022700122 20010227 00122 WP 2001 2 27 TWAA0107101 1 20010207 A 3350 105606002 BATTERY DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A TWAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 05 939AS 49657 DURING PREFLIGHT, FOUND EGRESS PATH MARKING SYSTEM LIGHTS INOP. REPLACED BATTERIES. OP 00-05 01-31-01 STL. 2 L 7 2 4F RT A6WE 2001022700123 20010227 00123 NM 2001 2 27 TWAA0107103 1 20010208 A 3350 767 LAMP BOEING 767 7673Q8 NM CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 634TW 28132 DURING MAINTENANCE FOUND L4 DOOR EMERGENCY SLIDE LIGHT INOP. RELAMPED LIGHT. OP 00 11 12-25-00 JFK. 2 L 7 2 4F RT A1NM 2001022700124 20010227 00124 NM 2001 2 27 UPS01234900 1 20010126 A 5530 SUPPORT BRACKET BOEING 727 72722C 138400F NM VERTICAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C, VERT STAB, FAIRING SUPPORT AT JUNCTION OF TENSION TIE RIB AND VERT STAB FRONT SPAR IS WORN DUE TO FRE TTING CORROSION LT. REPLACED FAIRING SUPPORT STRUCTURE IAW BOEING INST DRG 65-17485 & SRM 51-30-02. 2 L 7 3 4F A3WE 2001022700125 20010227 00125 NM 2001 2 27 UPS01234918 1 20010126 A 5330 ACCESS PANEL BOEING 727 727180C 138406G NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE:IN FUSELAGE - RT ACCESS PANEL 3420 - BS 630 AFT FRAME OF ACCESS PANEL CUTOUT HAS CORROSION BEYOND LIMITS PER B727 SRM 53-01-1. REMOVED CENTER SECTION OF AFT FRAME OF PANEL CUTOUT ON FUSELAGE BODY PANEL 3420 AT BS 630, FABRI CATED A NEW SECTION OF AFT FRAME AND INSTALLED PER B727 SRM 51040-3 AND 51-30-2. 2 L 7 3 4F A3WE 2001022700126 20010227 00126 NM 2001 2 27 UPS01234919 1 20010125 A 5720 ANGLE BOEING 727 727180C 138406G NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE:IN RT WING LEADING EDGE STA 349.6 WEB O/B UPPER SUPPORT ANGLE CRACKED. STOPPED DRILLED CRACK PER B727 S RM 51-10-1, NDT STOPPED DRILLED INSTALLED ANGLE REPAIR PER B727 SRM 51-40-3. 2 L 7 3 4F A3WE 2001022700127 20010227 00127 EU 2001 2 27 QXEA0100098 1 20010207 A 3350 XB864041 LIGHT FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 481US 11230 GEG- ESCAPE PATH LIGHTING ON SEAT 1 A/B INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY ON SEAT 1 A/B. OPERATIONAL CH ECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001022700128 20010227 00128 EU 2001 2 27 QXEA0100099 1 20010207 A 3350 MGG1055 LIGHT FOKKER F28 F28MK4000 4990810 EU ROW 9 INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 483US 11233 BOI- EMERGENCY EXIT SIGN ON ROW 9 HAS BROKEN LENS. REMOVED AND REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001022700129 20010227 00129 NM 2001 2 27 QXEA0100097 1 20010206 A 5210 85210127051 CABLE DHAV DHC8 DHC8202 2809007 NM PAX DOOR MALFUNCTIONED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 374PH 528 MFR- MAIN CABIN DOOR OPENS ABOUT 1 FOOT AND THEN STOPS. WILL NOT OPEN FURTHER. REMOVED AND REPLACED MAIN CABIN DOOR CO UNTER BALANCE CABLE ON DOOR AND AFT DRUM. ADJUSTED BALANCE SYSTEM IAW DHC MM 52-10-00. AIRCRAFT RETURNED TO SERVICE. OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2001022700130 20010227 00130 SO 2001 2 27 SWIA972336 1 20010202 A 5610 ROLLER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT WINDOW DAMAGED A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 560SW 120334 RIGHT DIRECT VISION WINDOW AFT ROLLER ASSEMBLY (ON BOTTOM) FELL APART. REPLACED SNAP RING ON AFT LOWER RIGHT DIRECT VIS ION WINDOW ROLLER. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001022700131 20010227 00131 SO 2001 2 27 SWIA972337 1 20010207 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS FAILED A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 189SW 120048 OUTBOARD FLAPS WILL NOT RETRACT FULLY AFTER TAKEOFF. RETURNED TO EKO. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATO R. OPS CHECKS, LEAK CHECKS GOOD. P/N ON 320300-1007, S/N ON 0516, S/N OFF 1093. 2 L 7 2 4T 4 T RT A31SO E20NE 2001022700132 20010227 00132 SO 2001 2 27 SWIA972338 1 20010205 A 3260 UPLOCK SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT MLG OUT OF ADJ A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 296SW 120325 WHEN LANDING GEAR WAS SELECTED UP THE RIGHT GEAR INDICATOR TWO RED LIGHTS, NO GREEN, AND WE COULD HEAR THAT A GEAR DOOR WAS OPEN. NORMAL INDICATIONS WHEN GEAR SELECTED DOWN. RETURNED TO MRY. ADJUSTED RIGHT MLG UPLOCK SWITCH IAW MM 32-61- 01. SWUNG GEAR SEVERAL TIMES. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 2001022700133 20010227 00133 SO 2001 2 27 SWIA972339 1 20010208 A 3260 UPLOCK SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT MLG MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 195SW 120127 LEFT GEAR DOOR INTERMITTENTLY WILL NOT RETRACT. (RED DISAGREEMENT LIGHT ON COLUMN A ON). ADJUSTED LEFT GEAR ACTUATOR IAW 32-30-00 AND UPLOCK PROX SWITCH ADJUSTED IAW 32-61-01. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001022700134 20010227 00134 SO 2001 2 27 SWIA972340 1 20010208 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS MALFUNCTIONED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 189SW 120048 FLAP DISAGREEMENT ON DEPARTURE, OUTBOARD FLAPS. RETURNED TO SLC. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR IAW EMB 120 MM 27-50-00. OPS CHECK AND LEAK CHECKED OK. P/N ON 320300-1007, S/N ON 0522, S/N OFF 0316. 2 L 7 2 4T 4 T RT A31SO E20NE 2001022700135 20010227 00135 EU 2001 2 27 C2XA01IA075 1 20010209 A 3350 AD3127 BATTERY AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 21837 202 IAH- DURING MAINTENANCE INSPECTION SEVERAL EMERGENCY AISLE PATH LIGHTS WERE FOUND TO BE INOPERATIVE. THE NUMBER THREE E MERGENCY BATTERY WAS REMOVED AND REPLACED AND THE OPERATIONAL CHECK OF THE EMERGENCY AISLE PATH LIGHTING WAS SATISFACTOR Y. REFERENCE ATR-42JIC 33-50-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001022700136 20010227 00136 SO 2001 2 27 C2XA01IA076 1 20010206 A 2121 MS3320712 CIRCUIT BREAKER EMB 120 EMB120ER 3260203 SO COCKPIT TRIPPED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 15730 120187 SHV - FLIGHT 3525, THE CREW REPORTED A SMOKE SMELL IN THE CABIN AREA. THE AIRCRAFT LANDED AT SHV WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE AVIONICS COOLING FAN CIRCUIT BREAKER TO BE POPPED. MAINTENANCE RESET THE CIRCUIT BREAKER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001032700374 20010327 00374 SO 2001 3 27 C2XA01IA077 1 20010208 A 2150 8152403 A/C PACK EMB 145 EMB145LR SO NR 1 FAILED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 17928 145007 IAH - FLIGHT 3761, THE CREW REPORTED A STRONG ODOR IN THE CABIN WITH THE NUMBER ONE PACK RUNNING. THE AIRCRAFT LANDED A T OAH WITHOUT INCIDENT WHERE MAINTENANCE PLACED THE NUMBER ON PACK ON MEL 21-51-00 CAT-C CONTROL NUMBER 00962, AND THE A IRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RETURNED TO IAH ON 02/13/01 WHERE MAINTENANCE REMOVED AND REPL ACED THE NUMBER TWO AIR CYCLE MACHINE. REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001022700137 20010227 00137 EU 2001 2 27 C2XA01IA078 1 20010208 A 3260 141FL01D3 PROXIMITY SWITCH AEROSP ATR42 ATR42320 8680930 EU RT MLG INOPERATIVE A C2XA O OTHER N FALSE WARNING CL CLIMB 1 SW 27 99838 259 IAH - FLIGHT 3209, THE CREW REPORTED A RIGHT MAIN LANDING GEAR UNLOCK LIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDEN T. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR UPLOCK BOX PROXIMITY SWITCH, AND THE AIRCRAFT WAS APPRO VED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001022700138 20010227 00138 EU 2001 2 27 DHL2001362005 1 20010210 A 7331 911519 CONTROL UNIT AIRBUS 300 A300B4103 3930104 EU FUEL FLOW MALFUNCTIONED A DHLA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 SO 01 362DH 84 NR 1 FUEL FLOW VARIES BETWEEN 6000 TO 20000 LBS. NR 2 FUEL FLOW VARIES BETWEEN 6000 TO 22000. ALL OTHER ENG INDICATION S INDICATED STEADY AND NORMAL INDICATIONS. REMOVED AND REPLACED FUEL FLOW ELECTRONIC UNIT WITH A SERV UNIT. GROUND RUN OPS CK IS GOOD IAW MM 73-31-00. 2 L 7 2 4F RT A35EU 2001022700139 20010227 00139 WP 2001 2 27 ABXA010046 1 20010210 A 3297 G357E20 WIRE DOUG DC8 DC861 3021952 WP WING BROKEN A ABXA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 23 850AX 45894 WHEN THE LANDING GEAR WAS SELECTED DOWN, THE LEFT MAIN LANDING GEAR DOWN AND LOCKED INDICATION FAILED TO ILLUMINATE. CR EW ABORTED APPROACH AND COMPLIED WITH THE ABNORMAL CHECKLIST. THE CREW DECLARED AN EMERGENCY AND COMPLETED A TOWER FLY BY. THE TOWER STATED THAT THE GEAR APPEARED TO BE DOWN AND LOCKED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAIN TENANCE INSPECTED AND REPAIRED A BROKEN WIRE ON THE LEFT LANDING GEAR DOWN INDICATION CIRCUIT. 2 L 7 4 4F 4A25 2001022700140 20010227 00140 WP 2001 2 27 MWEA010149 1 20010209 A 5754 9955845501 RIB DOUG DC9 DC932 3022066 WP LT NR 4 SLAT WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LEFT NR 4 SLAT OUTBOARD BUSHINGS AT THE COMMON LINK WORN. REMOVED AND REPLACED RIB. 2 L 7 2 4F A6WE 2001022700141 20010227 00141 WP 2001 2 27 MWEA010148 1 20010209 A 5415 49198641 FITTING DOUG DC9 DC932 3022066 WP LT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 FITTING CRACKED AT VERTICAL WEB AT LEFT ENGINE PYLON STRUCTURE, VIEWED THROUGH PANEL 8105A. REMOVED AND REPLACED FITTIN G. 2 L 7 2 4F A6WE 2001022700142 20010227 00142 WP 2001 2 27 ARWA0010203 1 20010207 A 2751 57511521 LINK DOUG DC8 DC862 3021970 WP LT TE FLAP BROKEN A ARWA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 19 802BN 1781 45909 FLAP IND HAS SPLIT NEEDLES. FOUND LEFTI/B FLAP LINK BROKEN ON THE O/B HINGE. REMOVED AND REPLACED WITH NEW P/N 5751152 -501. REFERENCE MM 27-51-4. OPS CHECK SATISFACTORY. 2 L 7 4 4F 4A25 2001022700144 20010227 00144 WP 2001 2 27 0100319950 1 20010114 A 5320 ANGLE DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9346 47376 HEAVY CORROSION AROUND FLANGES FOR SLANT PRESSURE PANEL LEFT SIDE. BLENDED OUT CORROSION IN THE 5910005-49 ANGLE CAP PE R SRM 57-01 FIGURE 1 SHEET 3. FABRICATED REPAIR STRAP .063 TITANIUM AND PASSIVATED EA 99-177600 AND L/P 1550091. 2 L 7 2 4F A6WE 2001022700145 20010227 00145 WP 2001 2 27 0100299974 1 20010207 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9338 47347 CRACKED FUSELAGE SKIN AT FWD CARGO DOOR JAMB UPPER FWD CORNER AT FASTENER AREA MARKED. .0937 INCH LONGREPAIRED PER EA 9 9-180917 L/P 1561171. 2 L 7 2 4F A6WE 2001022700146 20010227 00146 EA 2001 2 27 JBXA000241 1 20010210 A 3411 PITOT LINE CNDAIR CL600 CL6002B19 EA PITOT STATIC CONTAMINATED A JBXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 05 573ML 7227 INDICATED AIR SPEED ON FIRST OFFICERS SIDE SHOWS 65 KNOTS ABOVE CAPTAINS. STALL FAIL MESSAGE ON TAKEOFF. INSPECTED AIR CRAFT FOR MAINTENANCE FERRY FLIGHT FROM BUF TO RDU. REMOVED WATER FROM PITOT STATIC SYSTEM. PERFORMED LEAKS AND OPS CH ECKS OF SYSTEM IN ACCORDANCE WITH CRJ AMM 27-35-25, 34-11-00, AND 27-41-20. REFERENCED AOM 452 AND 470 AND CRJ SERVICE LETTER RJ-SL-32-029 FOR CRJ WITH EICAS 2000 EQUIPPED AIRCRAFT. 2 L 7 2 4F RT A21EA 2001022700147 20010227 00147 NE 2001 2 27 AT0100077 2 20010208 A 7200 ENGINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE NR 2 FAILED A ZZDA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 15 816AT 47445 665816 ON CLIMBOUT CAPTAIN REPORTED NR 2 ENGINE PARAMETERS ACCELERATED WITH N1/N2 CLIMBING THRU 99 PERCENT AND EGT AT 750C FOR 30 SECONDS. SHUT DOWN ENGINE AND SECURED AIRCRAFT FOR ENGINE OUT APPROACH. REMOVED AND REPLACED NR 2 ENGINE DUE TO EGT LIMITS EXCEEDING TEMPERATURE AND TIME LIMIT PER P&W 72-00-00. 2 L 7 2 4F 4 F A6WE E2EA 2001022700148 20010227 00148 NM 2001 2 27 0100152289 1 20010112 A 2730 ELEVATOR BOEING 727 727251 138408H NM TAIL OUT OF RIG A NWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 01 289US 21377 DURING CLIMBOUT, FLIGHT CONTROLS WERE STIFF IN NOSE DOWN MODE. FLIGHT CONTROLS IN NOSE UP MODE AND AILERONS AND RUDDER WERE OK. CREW RETURNED TO DTW AND MADE AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED STABILIZER CONTROLS. CHECKED OK. ALSO RIGGED AND OPERATIONALLY CHECKED ELEVATOR. ALL TESTS WERE SUCCESSFUL PER MM 27-30-00, PG 101. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2001022700150 20010227 00150 NM 2001 2 27 01FDEA00107 1 20010210 A 2780 CONTROL UNIT DOUG MD11 MD11F 3023600 NM FLAPS/SLATS FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 609FE 48549 UPON FLAP/SLAT RETRACT GOT 2 ALERT DEF AIL DISAGREE. REMOVED AND REPLACED NR 2 FCC PER IAW MM 27-01-03-4. 2 L 7 3 4F RT A22WE 2001022700151 20010227 00151 WP 2001 2 27 CALA0100109 1 20010209 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND CABIN LEFT I/B SEAT TRACK CORRODED AT FS 1031 - 1169. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS I NSTALLED IAW SRM 51-30-1 AND 53-05, FIGURE 4. 2 L 7 2 4F A6WE 2001022700152 20010227 00152 NM 2001 2 27 CALA0100110 1 20010129 A 5312 BULKHEAD BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 61304 23355 INSPECTION FOUND TWO 1 INCH CRACKS IN BULKHEAD WITH A STIFFENER BROKEN IN HALF AT STA 178. THE BULKHEAD WAS REMOVED AND REPLACED IAW EA 5310-03040. 2 L 7 2 4F RT A16WE 2001022700153 20010227 00153 NM 2001 2 27 CALA0100111 1 20010209 A 5320 ANGLE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14383 26312 INSPECTION FOUND AFT FLOOR ATTACH ANGLE IN FORWARD CARGO AREA CORRODED AT STA 500D ABOVE S26L-S26R. THE ANGLE WAS REMOV ED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001022700154 20010227 00154 WP 2001 2 27 CALA0100112 1 20010210 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 275 BETWEEN LONGERON 22L AND 23L. THE DENT WAS COLD WORKED AND A D OUBLER WAS INSTALLED IAW SRM 53-04-38 AND 51-10-3. 2 L 7 2 4F A6WE 2001022700155 20010227 00155 NM 2001 2 27 CALA0100113 1 20010210 A 2560 ACREM1A MEGAPHONE ACR BOEING 737 7373T0 1384582 NM AFT CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14325 23455 THE AFT CABIN MEGAPHONE WAS FOUND INOPERATIVE. THE MEGAPHONE WAS REMOVED AND REPLACED. 2 L 7 2 4F RT A16WE 2001022700156 20010227 00156 NM 2001 2 27 CALA0100114 1 20010210 A 5330 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70330 23460 INSPECTION FOUND A 1 INCH CRACK IN AFT SKIN CUTOUT FOR THE E&E COMPARTMENT COOLING EXHAUST. A REPAIR DOUBLER WAS INSTAL LED IAW ECRA 5330-02894. 2 L 7 2 4F RT A16WE 2001022700157 20010227 00157 NM 2001 2 27 JBXA000242 1 20010211 A 3260 CONNECTOR BOEING 737 7377CG 13844FA NM RT MLG DAMAGED A JBXA O OTHER N FALSE WARNING LD LANDING 1 SO 05 364ML 30739 RIGHT MAIN LANDING GEAR DOWN INDICATION ON MAIN AND OVERHEAD PANEL WITH GEAR HANDLE IN THE UP POSITION. PSEU LIGHT ILLU MINATED UPON TOUCHDOWN. PERFORMED TASK 32-61-801. FOUND PUSHED BACK PIN ON RIGHT LOCK PROX SWITCH AT CONNECTOR PLUG ON PSEU. RESECURED PIN. PERFORMED GEAR RETRACTION AND EXTENSION IAW B-737 AMM 32-32-00, ALL INDICATION NORMAL. 2 L 7 2 4F RT A16WE 2001022700158 20010227 00158 NM 2001 2 27 AWXA0001262 1 20010207 A 5315 654681138 FLOORBEAM BOEING 737 7373G7 1384595 NM CABIN CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 FLOORBEAM UPPER CAP CORRODED AT BS 986.5 FROM BL 0 TO RBL 45. FLOORBEAM CAP REPLACED IAW SRM 53-00-31 FIG 202. 2 L 7 2 4F RT A16WE 2001022700159 20010227 00159 NM 2001 2 27 AWXA0001263 1 20010207 A 5312 651758240 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 STA 178 FWD BULKHEAD RT UPPER WEB RBL 17 WL 225 IS CRACKED. REPLACED WEB IAW SRM 51-10-02 PG 12. 2 L 7 2 4F RT A16WE 2001022700160 20010227 00160 NM 2001 2 27 AWXA0001264 1 20010207 A 5320 6547973 WEB BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 RT WEB CRACKED STA 578 RBL 70. REPAIRED IAW SRM 51-70-13 FIG 1. 2 L 7 2 4F RT A16WE 2001022700161 20010227 00161 NM 2001 2 27 AWXA0001265 1 20010207 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 FLOORBEAM INTERCOSTAL CRACKED AT BL 0 STA 540; INTERCOSTAL HOLED AND SKIN PEELED OFF AT STA 540 RBL 65. REPLACED INTERC OSTAL AND DAMAGED SKIN IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001022700162 20010227 00162 NM 2001 2 27 AWXA0001266 1 20010207 A 5311 654653931 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 FUSELAGE FRAME INNER CHORD CRACKED STA 616 LBL 65. REPAIRED IAW SERVICE BULLETIN 737-53-1182. 2 L 7 2 4F RT A16WE 2001022700163 20010227 00163 NM 2001 2 27 AWXA0001267 1 20010207 A 5311 654653932 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 FUSELAGE FRAME INNER CHORD CRACKED STA 616 RBL 65. REPAIRED IAW SERVICE BULLETIN 737-53-1182. 2 L 7 2 4F RT A16WE 2001022700164 20010227 00164 NM 2001 2 27 AWXA0001268 1 20010207 A 5320 65528942 CHANNEL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 STA 540 RBL 0 TO RBL 25 HAS CRACK INDICATION IN THE FWD O/B END RADIUS OF THE HOT SECTION. REPLACED INTERCOSTAL IAW SRM 51-10-02 FIG 12. 2 L 7 2 4F RT A16WE 2001022700165 20010227 00165 NM 2001 2 27 AWXA0001269 1 20010207 A 5311 651630086 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 FWD PRESSURE BULKHEAD LT SIDE CHORD CRACKED AT WL 207 STA 178. RECTIFIED IAW NR5382636 AND EO 53-12-07 (REV C). 2 L 7 2 4F RT A16WE 2001022700166 20010227 00166 NM 2001 2 27 AWXA0001270 1 20010207 A 5311 651630087 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 FWD PRESSURE BULKHEAD SIDE CHORD CRACKED RT STA 178 WL 207. RECTIFIED IAW NR 5382636 AND EO 53-12-7 (REV C). 2 L 7 2 4F RT A16WE 2001022700167 20010227 00167 NM 2001 2 27 AWXA0001271 1 20010207 A 5312 6516300 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 TWO CRACKS ON PRESSURE BULKHEAD STA 178 RT SIDE I/B OF RBL 5.7 BELOW WL 207. SERVICE BULLETIN 737-53A1173 FUSELAGE - BO DY STATION 178 BULKHEAD - INSPECTION, REPAIR AND PREVENTATIVE MODIFICATION INCORPORATED. 2 L 7 2 4F RT A16WE 2001022700168 20010227 00168 NM 2001 2 27 AWXA0001272 1 20010207 A 5312 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 3 CRACKS ON PRESSURE BULKHEAD 178 WEB, LT SIDE JUST INBOARD OF LBL 57 BELOW. 2 L 7 2 4F RT A16WE 2001022700169 20010227 00169 NM 2001 2 27 AWXA0001273 1 20010207 A 5311 6517583U51 FRAME BOEING 737 7373G7 1384595 NM BULKHEAD CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 ONE CRACK AT AFT SIDE OF FWD PRESSURE BULKHEAD 178 AT LBL 5.7 VERTICAL CHORD INNER RADIUS JUST BEHIND L/G SWITCH PACK. RECTIFIED IAW NR 5382636 AND EO 53-12-07 (REV C). 2 L 7 2 4F RT A16WE 2001022700170 20010227 00170 NM 2001 2 27 AWXA0001274 1 20010207 A 5340 6545834 ATTACH ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 STA 328 LBL 47 FORE AND AFT INTERCOSTAL ATTACH ANGLES ARE CRACKED. ATTACH ANGLES REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001022700171 20010227 00171 NM 2001 2 27 AWXA0001275 1 20010207 A 5320 6545834 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 CRACKED FLOORBEAM INTERCOSTAL BS 328 AND LBL 45. REPAIRED IAW SRM 51-70-11 FIG 1. 2 L 7 2 4F RT A16WE 2001022700172 20010227 00172 NM 2001 2 27 AWXA0001276 1 20010207 A 5320 6545834 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 CRACKED FLOORBEAM INTERCOSTAL STA 328 LBL 45 IN RADIUS FWD END. REPAIRED IAW SRM 51-70-11 FIG 1. 2 L 7 2 4F RT A16WE 2001022700173 20010227 00173 NM 2001 2 27 AWXA0001277 1 20010207 A 5330 65C33753 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 FWD SERVICE DOOR CUTOUT RT LOWER AFT CORNER HAS A CRACK APPROX 3.25 INCH IN LENGTH. REPAIRED IAW SRM 53-10-01 FIG 202 ( TRIPLER INSTALLED). 2 L 7 2 4F RT A16WE 2001022700174 20010227 00174 NM 2001 2 27 AWXA0001278 1 20010207 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 FLOORBEAM CRACKED AT STA 664 AND BL 0 TWO LOCATIONS. HFEC CONFIRMS CRACK, LOWER SURFACE OF UPPER FLOORBEAM, ANGLE AT FA STENER HOLE. REPAIRED IAW DWG 65C34537 AND ER 03-5710-00357-J51. 2 L 7 2 4F RT A16WE 2001022700175 20010227 00175 NM 2001 2 27 AWXA0001279 1 20010207 A 5311 65163019 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 STA 188 LT FRAME BL 208 CRACKED. REPLACED OUTBOARD CHORD IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 2001022700176 20010227 00176 NM 2001 2 27 AWXA0001280 1 20010207 A 5310 65C251805 DOOR FRAME BOEING BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 1258 23779 AFT CARGO DOOR FRAME CRACKED AT FWD LOWER CORNER. REPLACED FRAME IAW DWG 65C25180. 2 L 7 2 4F RT A16WE 2001022700177 20010227 00177 NE 2001 2 27 AWXA0001281 2 20010208 A 7321 FMU500MK4 FMU AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NR 1 ENGINE MALFUNCTIONED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 645AW 1234 1075 238 V0103 PHX - AIR TURNBACK - 2/3/01 - DURING INITIAL CLIMB, LEFT ENG UNCOMMANDED THRUST INCREASE ABOVE CLIMB EPR LIMIT WITH DEFI NITE YAW TO THE RIGHT; EVENT WAS MOMENTARY AND LEFT EPR WAS NOTICED DECREASING THRU 1.5 BACK TO CLIMB EPR OF 1.3, OTHER PARAMETERS NORMAL. AIRCRAFT RETURNED TO PHX WITH NO FURTHER EVENTS. CONTINUED ON SUP SDR AWXA0001282. 2 L 7 2 4F 4 F RT A28NM E311NE 2001022700178 20010227 00178 NM 2001 2 27 AWXA0001283 1 20010208 A 5313 BAC1498108 STRINGER BOEING 737 73733A 1384673 NM FUSELAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 167AW 23628 STR 28L STA 1016 HAS AN ELONGATED BOLT HOLE. REPAIRED IAW SRM 53-00-03 FIG 201 DETAIL V. 2 L 7 2 4F RT A16WE 2001022700179 20010227 00179 NM 2001 2 27 AWXA0001284 1 20010208 A 5313 6546568519 STRINGER BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 167AW 23628 AFT BULKHEAD STA 1016 CTR STRINGER FOUND CORRODED AT BOTTOM. REPAIRED IAW SRM 51-70-11 FIG 1. 2 L 7 2 4F RT A16WE 2001022700180 20010227 00180 NM 2001 2 27 AWXA0001285 1 20010208 A 5320 65468045 STRAP BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 167AW 23628 FLOOR TRACK SUPPORT CRACKED AT STA 717B RBL 45.5. FABED, REPAIRED, AND INSTALLED IAW ER 5310-01010-SSI. 2 L 7 2 4F RT A16WE 2001022700181 20010227 00181 NM 2001 2 27 AWXA0001286 1 20010208 A 5310 146N102115 SHEAR TIE BOEING 757 7572G7 1384963 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 24233 AFT CARGO COMPARTMENTS STA 1300 LEFT SIDE BETWEEN STR 20L AND 21L SHEAR TIE ANGLE CRACKED. REMOVED CRACKED ANGLE; FABED ANGLE; INSTALLED ANGLE IAW SRM 51-40-02, 51-30-02, AND 51-30-01. 2 L 7 2 4F RT A2NM 2001022700182 20010227 00182 NM 2001 2 27 AWXA0001287 1 20010208 A 5312 65163007 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 509DC 23636 ULTRASONIC INSPECTION REVEALED CRACK INDICATION BS 178 BULKHEAD WEB AT RBL 1.3 TO UNDETERMINED POINT BENEATH STRAP AT WL 205.7; CONFIRMED HFEC. REMOVED LOWER L-ANGLE BS 178 WL 184 RBL 18 TO LBL 18; CUTOUT DAMAGED AREA WHERE HFEC CONFIRMED CRACK; LOCATED, DRILLED, TRIMMED, AND INSTALLED REPAIR DOUBLER AND FILLER IAW BOEING TR 737-300 SRM 53-10-08; INSTALLED LOWER L-ANGLE IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001022700183 20010227 00183 NM 2001 2 27 AWXA0001288 1 20010208 A 5312 65163007 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 509DC 23636 HFEC AND VISUAL (10X) CONFIRMS CRACK OF UNDETERMINED LENGTH UNDER STRAP AT BS 178 RBL 4 7/8 WL 199.5 TO 201.5. REMOVED STIFFENERS, RADOME ATTACH BRACKETS AND BACKUP STRIPS BS 178 WL 188 TO 218 RBL 10 TO LBL 4; LOCATED, DRILLED AND INSTALLE D DOUBLER AND FILLER IAW B737 SRM 53-10-08; REINSTALLED STIFFENERS AND BACKUP STRIPS IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001022700184 20010227 00184 NM 2001 2 27 AWXA0001289 1 20010208 A 5315 BAC1505100246 FLOORBEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 509DC 23636 CORROSION ON UPPER SURFACE OF TRANSVERSE FLOORBEAM AT BS 312 RBL 3 - 9. REMOVED UPPER T-ANGLE OF TRANSVERSE FLOORBEAM; REMOVED LT SPLICE ANGLES; FABED SPLICE PLATES, FABED T-ANGLE; TREATED, PRIMED, AND INSTALLED REPAIR IAW B737-300 SRM 51- 20-01, 53-10-51. 2 L 7 2 4F RT A16WE 2001022700185 20010227 00185 NM 2001 2 27 AWXA0001290 1 20010208 A 5512 SKIN BOEING 737 73733A 1384673 NM HORIZONTAL STAB DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 509DC 23636 HORIZONTAL STABILIZER LEADING EDGE SKIN DENTED STA 258.28. REPAIRED DENT IN LEADING EDGE SKIN OF LEFT HORIZONTAL STABIL IZER IAW B737-300 SRM 55-10-01 FIG 203 WITH -1 PLATE, -2 FILLER. 2 L 7 2 4F RT A16WE 2001022700186 20010227 00186 NM 2001 2 27 AWXA0001291 1 20010208 A 5320 654581283 FLOOR SUPPORT BOEING 737 73733A 1384673 NM FUSELAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 509DC 23636 FLOOR SUPPORT END FITTING AT BS 328 HAS A HOLE DRILLED IN THE RADIUS. DRILLED HOLE TO .159 THROUGH INTERNAL DOUBLER AND EXTERNAL SKIN; COUNTERSUNK SKIN; INSTALLED RIVET IAW AWA ER 03-5310-01024-SS2. 2 L 7 2 4F RT A16WE 2001022700187 20010227 00187 NM 2001 2 27 AWXA0001292 1 20010208 A 5330 65C27755 SKIN BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 509DC 23636 L-2 DOOR UPPER HINGE CUTOUT SKIN IS CRACKED.CUTOUT DAMAGED FUSELAGE SKIN; FABED REPAIR DOUBLER AND FILLER; DRILLED ATTAC HMENT LOCATIONS; TREATED AND PRIMED REPAIR PARTS; INSTALLED REPAIR IAW B737 SRM 53-60-01 FIG 205. 2 L 7 2 4F RT A16WE 2001022700188 20010227 00188 NM 2001 2 27 AWXA0001293 1 20010208 A 5320 654581283 FLOOR SUPPORT BOEING 737 73733A 1384673 NM FUSELAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 509DC 23636 SUSPECT CRACK IN LEFT W/W AT STA 664.75 BL 33 UPPER PRESSURE PANEL. HFEC PERFORMED; CUTOUT DAMAGED AREA; FABED REPAIR D OUBLER, FILLER AND STIFFENER; INSTALLED IAW AWA ER 03-5710-01025-JS1 AND B737-300 SRM 51-00-00 FIG 23, 51-10-02, 51-20-0 1. 2 L 7 2 4F RT A16WE 2001022700189 20010227 00189 NM 2001 2 27 AWXA0001294 1 20010208 A 5730 177PH003011 DOUBLER BOEING 737 73733A 1384673 NM RT WING CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 509DC 23636 CRACK IN RT WING INBOARD L/E SKIN JUST ABOVE INBOARD END OF L/E FLAP SEAL DOOR. CUT OUT CRACKED AREA; HFEC PERFORMED; F ABED FILLER AND INTERNAL DOUBLER; INSTALLED IAW AWA ER 03-5741-01027-SS1 AND B737-300 SRM 57-41-01. 2 L 7 2 4F RT A16WE 2001022700190 20010227 00190 NM 2001 2 27 AWXA0001295 1 20010208 A 5753 6547929 SKIN BOEING 737 73733A 1384673 NM LT WING TE FLAP CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 509DC 23636 LT WING O/B MID FLAP HAS A CHAFED AREA AT I/B FLAP TRACK ON LOWER SKIN. REPAIRED IAW AWA ER 03-5754-01027. 2 L 7 2 4F RT A16WE 2001022700191 20010227 00191 NM 2001 2 27 AWXA0001296 1 20010208 A 5753 6547929 SKIN BOEING 737 73733A 1384673 NM RT WING TE FLAP CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 509DC 23636 RT WING O/B MID FLAP HAS A CHAFED AREA AT I/B FLAP TRACK ON LOWER SKIN. REPAIRED IAW AWA ER 03-5754-01027. 2 L 7 2 4F RT A16WE 2001022700192 20010227 00192 NM 2001 2 27 AWXA0001297 1 20010208 A 5330 65C33756 SKIN BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 509DC 23636 R-1 DOOR FRAME LOWER AFT CORNER SKIN IS CRACKED; EMINATING FROM FASTENER TRAVELING TOWARD RADIUS. STOP DRILLED CRACK; F ABED REPAIR DOUBLERS; DRILLED, TREATED, PRIMED, AND INSTALLED IAW B737-300 SRM 53-10-01 PG 204. 2 L 7 2 4F RT A16WE 2001022700193 20010227 00193 NM 2001 2 27 AWXA0001298 1 20010208 A 5315 BAC30M06A FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 UPPER CHORD, FWD FACE OF FLOORBEAM AT BS 520 HAS A CRACK EXTENDING THROUGH PREVIOUS STOP DRILL. REMOVED PREVIOUS REPAIR ; CUT OUT PREVIOUS REPAIR; FABED DOUBLERS, T-CAP AND STRAPS; DRILLED, DEBURRED, TREATED AND INSTALLED IAW B737-200 SRM 5 3-10-09 FIG 2; INSTALLED KIT 65C34688-2 IAW S/B 737-53-1120. 2 L 7 2 4F RT A16WE 2001022700194 20010227 00194 NM 2001 2 27 AWXA0001299 1 20010208 A 5313 BAC1498156 STRINGER BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 STR 27L IS CORRODED OUT OF LIMITS IAW B737-200 SRM 53-20-2, FROM FS 1016 TO FS 986. REMOVED CORRODED SECTION; FABED AND TREATED REPAIR PARTS; INSTALLED NEW SECTION OF STRINGER AND REPAIR PARTS IAW B737-200 SRM 53-10-2 AND 51-20-2. 2 L 7 2 4F RT A16WE 2001022700195 20010227 00195 NM 2001 2 27 AWXA0001300 1 20010208 A 5315 65458101 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 CORROSION ON UPPER SURFACE OF FLOORBEAM AT FS 312 RBL 8 TO RBL 10; OUT OF LIMITS IAW B737-200 SRM 53-16-1 PG 7. REPAIRE D FLOORBEAM IAW B737-200 SRM 53-10-9. 2 L 7 2 4F RT A16WE 2001022700196 20010227 00196 NM 2001 2 27 AWXA0001301 1 20010208 A 5312 65163007 BULKHEAD BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 ULTRASONIC INSPECTION REVEALED CRACK INDICATION AT FS 178 BLKHEAD WEB BENEATH STRAP AT LBL 6 WL 230 TO 233. REMOVED STI FFENERS, BRACKETS AND ANGLES; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER, FILLERS AND SHIMS IAW B737-200 SRM 53-10-11 ; INSTALLED STIFFENERS, BRACKETS AND ANGLES IAW B737-200 SRM 53-10-11 AND 51-30-2. 2 L 7 2 4F RT A16WE 2001022700197 20010227 00197 NM 2001 2 27 AWXA0001302 1 20010208 A 5753 657093049 ANGLE BOEING 737 737277 1384570 NM LT WING FLAP CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 LEFT WING O/B HINGED FLAP TRACK ATTACH ANGLE CRACKED. REMOVED ANGLE; FABED, TREATED AND PRIMED IAW SRM 51-20-1 AND 51-1 0-2; INSTALLED ANGLE IAW SRM 51-30-2. 2 L 7 2 4F RT A16WE 2001022700198 20010227 00198 NM 2001 2 27 AWXA0001303 1 20010208 A 5312 65163007 BULKHEAD BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 ULTRASONIC INSPECTION REVEALED CRACK INDICATION AT FS 178 BLKHEAD BENEATH STRAP FROM LBL 5 TO LBL 8 WL 217 IN WEB. REMO VED STIFFENERS, BRACKETS AND ANGLES AT FS 178 WL 207 TO WL 241 FROM RBL 18 TO LBL 18; LOCATED, DRILLED, TREATED AND INST ALLED REPAIR DOUBLER, FILLERS AND SHIMS IAW SRM 53-10-11; INSTALLED STIFFENERS, BRACKETS AND ANGLES IAW SRM 53-10-11 AND 51-30-2. 2 L 7 2 4F RT A16WE 2001022700199 20010227 00199 NM 2001 2 27 AWXA0001304 1 20010208 A 5315 ANO101362401 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 FLOORBEAM TOP CAP AT BS 294.5 RBL 41 FOUND TO BE OUT OF LIMITS AFTER CORROSION CLEAN UP IAW SRM 53-10-01. REPAIRED FLOO RBEAM UPPER CHORD IAW SRM 53-10-02 FIG 7 AND 53-40-04. 2 L 7 2 4F RT A16WE 2001022700200 20010227 00200 NM 2001 2 27 AWXA0001305 1 20010208 A 5531 65529139 RIB BOEING 737 737277 1384570 NM VERTICAL STAB CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 AREA OF DEEP CHAFING ON VERT STAB FWD LWR END CAP RIB. REMOVED FWD LWR END CAP AND REPLACED WITH A NEW PART IAW SRM 53- 10-11 AND 51-30-2. 2 L 7 2 4F RT A16WE 2001022700201 20010227 00201 NM 2001 2 27 AWXA0001306 1 20010209 A 5315 6546811 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 CORROSION ON FLOOR SUPPORT FWD OF LT LAV WASTE EXIT AND FLOORBEAM AT FS 1006 FOUND TO BE OUT OF LIMITS IAW B737-200 SRM 53-10-6. REMOVED CORROSION ON SUPPORT AND FLOORBEAM IAW SRM 52-10-2; CUT OUT DAMAGED AREA ON BEAM; FABED, DRILLED, TREA TED AND INSTALLED REPAIR PARTS AND WEB IAW SRM 51-10-1, 51-10-9, 51-20-2 AND 51-30-2. 2 L 7 2 4F RT A16WE 2001022700202 20010227 00202 NM 2001 2 27 AWXA0001307 1 20010209 A 5312 65163007 BULKHEAD BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 HFEC INDICATES A .200 INCH LONG CRACK EMINATING FROM FASTENER HOLE AT BLKHD FS 178 RBL 12.75 WL 234. REMOVED STIFFENERS , BRACKETS AND ANGLES; FABED, DRILLED, TREATED AND INSTALLED DOUBLER, FILLERS AND SHIMS IAW SRM 53-10-11; REINSTALLED ST IFFENERS, BRACKETS AND ANGLES IAW SRM 51-30-2. 2 L 7 2 4F RT A16WE 2001022700203 20010227 00203 NM 2001 2 27 AWXA0001308 1 20010209 A 5312 65163007 BULKHEAD BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 ULTRASONIC INSPECTION REVEALED CRACK INDICATION AT FS 178 BULKHEAD WEB BENEATH STRAP AT RBL 7 TO RBL 15 WL 218. REMOVED STIFFENERS, BRACKETS AND ANGLES; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER, FILLERS AND SHIMS IAW SRM 53-10-11; INS TALLED STIFFENERS BRACKETS AND ANGLES IAW SRM 53-10-11 AND 51-30-2. 2 L 7 2 4F RT A16WE 2001022700204 20010227 00204 NM 2001 2 27 AWXA0001309 1 20010209 A 5330 BAC15171470 SKIN BOEING 737 737277 1384570 NM FUSELAGE GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 GOUGED AREA ON RT AFT UPPER FUSELAGE SKIN BETWEEN STA 807 AND 827 APPROX 50 INCHES ABOVE WINDOW. REMOVED DAMAGED SKIN; FABED, TREATED FILLER AND DOUBLER; DRILLED AND INSTALLED IAW SRM 53-30-03. 2 L 7 2 4F RT A16WE 2001022700205 20010227 00205 NM 2001 2 27 AWXA0001310 1 20010209 A 5315 65468032 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 CABIN FLOORBEAM UPPER CHORD FWD FACE HAS A CRACK IN RADIUS EXTENDING BEYOND STOP DRILL FS 526 RBL 24.75. REPAIRED FLOOR BEAM UPPER CHORD IAW BOEING MESSAGE CPZ-MCN-01-0010N AND ER 15-5310-01023-JS1. 2 L 7 2 4F RT A16WE 2001022700206 20010227 00206 NE 2001 2 27 AALA20010021 2 20010104 A 7314 3782015 PUMP BOEING 727 727223 1384074 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE LEAKING A AALA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SW 21 893AA 22009 MIA - FLT 9212 - EN ROUTE MIA-ABQ - DETECTED NR 1 ENGINE SHUT DOWN. RETURNED MIA AND LANDED WITHOUT FURTHER INCIDENT. REPLACED NR 1 SIDE FUEL PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F 4 F A3WE E2EA 2001022700207 20010227 00207 NM 2001 2 27 AALA20010011 1 20010101 A 2720 DAMPENER BOEING 727 727227 1384078 NM RUDDER MALFUNCTIONED A AALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 21 729AA 20736 MIA - FLT 1587 - EN ROUTE MIA-DFW, SHORTLY AFTER TAKEOFF DETECTED AIRCRAFT DRIFTING TO THE RIGHT. FULL LEFT RUDDER EID NOT CORRECT THE DRIFT. RETURNED MIA AND LANDED WITHOUT FURTHER INCIDENT. ACCOMPLISHED YAW DAMP RUDDER CHECK PER THE MM . NO DEFECT NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001022700208 20010227 00208 2001 2 27 AALA20010151 4 20010126 A 3460 CDU BOEING 777 777223 1385213 NM COCKPIT FAILED A AALA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 SW 21 796AN 30796 DFW - FLT 78 - LOST LEFT FMC, DIVERTED TO JFK FOR MAINTENANCE. REPLACED LEFT CDU. ACCOMPLISHED CHECKS AS PER MM. ALL CHECKS NORMAL. (M) 2 L 7 2 4F RT T00001SE 2001022700209 20010227 00209 NM 2001 2 27 AALA20010087 1 20010114 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 21 370AA 25197 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 37H INOPERATIVE. REPAIRED EMERGENCY EXIT WIRE AT SEAT 37H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001022700210 20010227 00210 WP 2001 2 27 AALA20010132 1 20010120 A 3231 DOOR DOUG DC9 DC982 3022082 WP NLG OUT OF ADJ A AALA A UNSCHED LANDING E VIBRATION/BUFFET TO TAKEOFF 1 SW 21 275AA 49272 DFW - FLT 1707 - EN ROUTE DFW-SMF, SHORTLY AFTER TAKEOFF, UPON RAISING NOSE GEAR DETECTED A STRONG VIBRATION. LOWERED G EAR, DECLARED EMERGENCY AND RETURNED DFW WITHOUT FURTHER INCIDENT. RESET NOSE LANDING DOOR SEQUENCE. PERFORMED VISUAL INSPECTION. NO DEFECTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001022700217 20010227 00217 NM 2001 2 27 AALA20010037 1 20010105 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 632AA 24590 ATL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 15DEF THROUGH 22DEF INOPERATIVE. RE-CONNECTED EMERGENC Y EXIT LIGHT PIN CONNECTORS AT SEAT 15DEF AND 22DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001022700218 20010227 00218 NM 2001 2 27 AALA20010031 1 20010107 A 3350 SWITCH BOEING 757 757223 1384957 NM COCKPIT MALFUNCTIONED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 649AA 24607 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT WHEN UNARMED AT COCKPIT REMAIN ILLUMINATED. REPLACED EMERGENCY EXIT LIGHT SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001022700219 20010227 00219 NM 2001 2 27 AALA20010028 1 20010106 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN DISCONNECTED A K NONE L NO TEST IN INSP/MAINT 1 SW 21 372AA 25199 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT LAVATORY WALL INOPERATIVE. RE-CONNECTED EMERGENCY EXIT WIRE AT LAVATORY WALL. SYSTM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001022700220 20010227 00220 NM 2001 2 27 AALA20010029 1 20010106 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 386AA 27060 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 22B INOPERATIVE. RE-CONNECTED EMEREGNCY EXIT LIGHT CON NECTOR AT SEAT 22B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001022700221 20010227 00221 NM 2001 2 27 AALA20010026 1 20010106 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 674AN 29424 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT FLOOR PA TH STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001022700222 20010227 00222 NM 2001 2 27 AALA20010027 1 20010106 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 332AA 22331 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 25J INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT CONNE CTOR AT SEAT 25J. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001022700223 20010227 00223 NM 2001 2 27 AALA20010025 1 20010105 A 3350 LIGHT BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 304AA 22310 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 11B BROKEN. REPLACED EMERGENCY EXIT AFT AISLE LIGHT ST RIP AT SEAT 11B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001022700224 20010227 00224 NM 2001 2 27 AALA20010024 1 20010105 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 359AA 24040 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 38H INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT CONNE CTOR AT SEAT 38H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001022700225 20010227 00225 NM 2001 2 27 AALA20010019 1 20010102 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN DAMAGED A K NONE L NO TEST IN INSP/MAINT 1 SW 21 376AN 25445 MIA - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT AT 21H INOPERATIVE. REPAIRED EMERGENCY EXIT WIRE AT CON NECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001022700226 20010227 00226 NM 2001 2 27 AALA20010001 1 20010101 A 3350 4008751 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 601AN 27052 LAX - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY LIGHT AT 18D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSE MBLY AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001022700227 20010227 00227 NM 2001 2 27 AALA20010074 1 20010111 A 3350 LIGHT BOEING 767 767223 1385123 NM GALLEY INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 301AA 22307 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT MID GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEM BLY AT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001022700228 20010227 00228 NM 2001 2 27 AALA20010079 1 20010114 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 632AA 24590 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 22D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECT OR AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001022700229 20010227 00229 NM 2001 2 27 AALA20010078 1 20010114 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 184AN 29594 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT CABIN INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001022700230 20010227 00230 NM 2001 2 27 AALA20010077 1 20010112 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 329AA 22329 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 28H INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT CONNE CTOR AT SEAT 28H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001022700231 20010227 00231 NM 2001 2 27 AALA20010076 1 20010112 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN DAMAGED A K NONE L NO TEST IN INSP/MAINT 1 SW 21 369AA 25196 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT AT SEAT 36H INOPERATIVE. REPAIRED EMERGENCY EXIT WIRE AT SEAT 36H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001022700232 20010227 00232 NM 2001 2 27 AALA20010086 1 20010116 A 3350 PIN BOEING 767 767323 1385205 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 385AM 27059 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 8A AND 8B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT C ONNECTOR PINS AT SEAT 8A AND 8B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001022700233 20010227 00233 NM 2001 2 27 AALA20010082 1 20010113 A 2530 46700017 COFFEEMAKER BOEING 757 757223 1384957 NM GALLEY DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 699AN 27051 SJU - FLT 1574 - EN ROUTE SJU-BOS - DETECTED SMELL AND SMOKE IN CABIN. RETURNED SJU AND LANDED WITHOUT FURTHER INCIDENT . REPLACED NR 3 COFFEEMAKER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001022700245 20010227 00245 NM 2001 2 27 AALA20010131 1 20010123 A 2421 GEN0002 IDG BOEING 777 777223 1385213 NM NR 1 ENGINE FAILED A AALA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 SW 21 788AN 30011 ORD - FLT 38 - ELEC GEN DRIVE L MESSAGE APPEARED FOLLOWED BY ELEC BACK UP GEN L. ONE RESET ATTEMPT, UNSUCCESSFUL. GENE RATOR DISCONNECTED PER CHECKLIST PROCEDURE. REMOVED AND REPLACED NR 1 ENGINE IDG, BACKUP GEN AND GENERATOR CONVERTER PE R MM LEAK AND OPS CHECK OK. (M) 2 L 7 2 4F RT T00001SE 2001022700246 20010227 00246 NM 2001 2 27 AALA20010099 1 20010121 A 3350 LIGHT BOEING 777 777223 1385213 NM GALLEY INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 770AN 29578 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT LEFT CORNER GALLEY BROKEN. REPLACED EMERGENCY EXIT LIGHT AT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001022700247 20010227 00247 WP 2001 2 27 AALA20010152 1 20010129 A 2613 S1309 SENSOR DOUG DC9 DC982 3022082 WP A/C BAY MALFUNCTIONED A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 553AA 53083 MIA - FLT 1304 - EN ROUTE MIA-CLE, DETECTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. AIR INTERRUPTED, RETUR NED MIA AND LANDED WITHOUT FURTHER INCIDENT. REPLACED LEFT SIDE AFT TAIL COMPARTMENT OVERHEAT SENSOR. SYSTEM GROUND CH ECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001022700248 20010227 00248 WP 2001 2 27 AALA20010142 1 20010124 A 2913 31495 PUMP DOUG DC9 DC982 3022082 WP NR 1 ENGINE FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 474 49649 DFW - FLT 1431 - EN ROUTE DFW-ONT, DETECTED NR 1 ENGINE HYDRAULIC PUMP FAILURE. AIR INTERRUPTED, RETURNED DFW AND LANDE D WITHOUT FURTHER INCIDENT. REPLACED NR 1 SIDE ENGINE HYDRAULIC PUMP. ACCOMPLISHED LEAK CHECK. NO LEAKS NOTED. SYSTE M GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001022700249 20010227 00249 WP 2001 2 27 AALA20010141 1 20010122 A 4990 TUBE DOUG DC9 DC982 3022082 WP APU LEAKING A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 441AA 49460 DFW - FLT 2437 - EN ROUTE DFW-LAX, SHORTLY AFTER TAKEOFF DETECTED LIGHT SMOKE AND FUMES AT COCKPIT. RETURNED DFW AND LA NDED WITHOUT FURTHER INCIDENT. REPLACED OIL FILL SCUPPER ASSEMBLY AT APU. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001022700250 20010227 00250 WP 2001 2 27 AALA20010117 1 20010108 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 TUL - FOUND CUSP CORRODED RIGHT STATION 635. INSTALLED DOUBLER PER SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2001022700251 20010227 00251 WP 2001 2 27 AALA20010118 1 20010108 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 TUL - FOUND CUSP PANEL CORRODED JUST ABOVE MID CX DOOR AFT HINGE BRACKETS AT STATION 674 AND 686 RIGHT SIDE. REPAIRED P ER SRM 53-01, INSTALLED DOUBLER. (M) 2 L 7 2 4F RT A6WE 2001022700252 20010227 00252 WP 2001 2 27 AALA20010119 1 20010108 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP AFT CARGO BAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 TUL - FOUND LIGHT CORROSION ON RIGHT CARGO TIE DOWN TRACK STATION 1250-1287, AROUND ALL FASTENERS LENGTH OF TRACK. INST ALLED NEW TIE DOWN TRACK PER SRM 51-01. (M) 2 L 7 2 4F RT A6WE 2001022700253 20010227 00253 WP 2001 2 27 AALA20010120 1 20010112 A 5320 SUPPORT BRACKET DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 TUL - FOUND CRACK IN SEAT TRACK SUPPORT AFT NR 4 TRACK FS 927. REMOVED CRACKED SEAT TRACK SUPPORT AND INSTALLED NEW SUP PORT SRM 51-01 PAGE 1. (M) 2 L 7 2 4F RT A6WE 2001022700254 20010227 00254 WP 2001 2 27 AALA20010122 1 20010108 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 TUL - FOUND LONGERON 29R AT STATION 320 IS DAMAGED, INBOARD SIDE OF LONGERON CHANNEL IS BENT DOWNWARD. REPAIRED AREA PE R SRM 53-02, PAGES 48-53, FIG 18, SHT V. (M) 2 L 7 2 4F RT A6WE 2001030100080 20010301 00080 WP 2001 3 1 TWAA0102505 1 20010204 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT FOUND CORROSION IN CABIN ON SEAT TRACK, AT LBL 54 INCHES, STA 1252 AND STA 1283 TO 1280. REMOVED D AMAGED TRACK AT BOTH LOCATIONS. INSTALLED NEW PER DRAWING 5930566, SPM 6-70-01 AND SRM 51-30-1. 2 L 7 2 4F A6WE 2001030100081 20010301 00081 EU 2001 3 1 QXEA0100096 1 20010207 A 3350 1820 LIGHT FOKKER F28 F28MK4000 4990810 EU GALLEY INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 499US 11182 SEA- EXIT LIGHT GALLEY OVERHEAD INOPERATIVE. INSTALLED NEW LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001030100082 20010301 00082 NM 2001 3 1 TWAA0107102 1 20010208 A 3350 LIGHT BOEING 767 7673Q8 NM ROWS 16 - 18 INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 634TW 28132 DURING MAINTENANCE, FOUND EGRESS LIGHTING LT SIDE ROW 16-18, AND RT SIDE 24-27 INOP. RESECURED LOOSE CONNECTION, OPS CH ECK. OP 00 11 12-25-00 JFT. 2 L 7 2 4F RT A1NM 2001030100083 20010301 00083 NE 2001 3 1 AWXA0001282 2 20010208 A 7321 RESOLVER AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUEL FLOW MALFUNCTIONED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 645AW 238 V0103 MAINTENANCE TROUBLESHOT IAW TSR 73-22-00-810-851 AND IAE TELEX; CELL CODE FAULT OF 59 ON FMU/HC/EEC 1 MESSAGE; (WFXCF) F UEL FLOW RESOLVER FAULT; CH B ON CONNECTOR J8 HAD HIGH RESISTANCE OF 104 OHMS BETWEEN PINS I & J (NORM: 15-78 OHMS); WIR ING CHECKED GOOD; RANG OUT FMU RESOLVER ON CHANNEL B; (CONNECTOR 4000KC-C) AND RESOLVER WAS READING 82 OHMS; FOUND TCA V LV/HC/EECI MESSAGE IN GROUND SCANNING FADEC TEST; BLEED SYSTEM TESTS WERE PERFORMED - CHECKED GOOD. THE FOLLOWING COMPO NENTS WERE REPLACED DUE TO TROUBLESHOOTING PROCEDURES IN ADDITION TO THE FMU: NR 1 ENG EEC P/N 798300-15-052 S/N 250001 56 - HAMILTON STANDARD - TT 23201, TC 10818, TSR 2807 NR 1 ENG TCA. 2 L 7 2 4F 4 F RT A28NM E311NE 2001030100084 20010301 00084 NM 2001 3 1 AWXA0001311 1 20010209 A 5320 6516300 BEAM BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 HFEC INDICATES A 2 INCH CRACK AT I/B SIDE OF VERTICAL CHORD ON AFT SIDE OF FS 178 BLKHEAD BETWEEN WL 183 AND 185 LBL 5.7 . REPAIRED I/B SIDE OF VERTICAL CHORD ON AFT SIDE OF FS 178 BLKHEAD BETWEEN WL 183 AND 185 LBL 5.7 IAW SRM 53-10-11 FIG 8 PG 46-65. 2 L 7 2 4F RT A16WE 2001030100085 20010301 00085 NM 2001 3 1 AWXA0001314 1 20010209 A 5551 65505782 FITTING BOEING 737 737277 1384570 NM HORIZONTAL STAB GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 RT HORIZ STAB AFT SPAR UPPER ATTACH LUG AFT FACE GOUGED. BLENDED GOUGE IAW ER 15-5510-01027-ES1. 2 L 7 2 4F RT A16WE 2001030100086 20010301 00086 NM 2001 3 1 AWXA0001316 1 20010209 A 5551 65505794 FITTING BOEING 737 737277 1384570 NM HORIZONTAL STAB GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 RT HORIZ STAB AFT SPAR MID ATTACH AFT FACE GOUGED. BLENDED GOUGE IAW ER 15-5510-01027-ES1. 2 L 7 2 4F RT A16WE 2001030100087 20010301 00087 NM 2001 3 1 AWXA0001317 1 20010209 A 5551 65505827 FITTING BOEING 737 737277 1384570 NM HORIZONTAL STAB GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 LT HORIZ STAB FWD LWR LUG HAS A GOUGE ON THE FWD SIDE OF SPOT FACE. BLENDED GOUGE IAW ER 15-5510-01027-ES2. 2 L 7 2 4F RT A16WE 2001030100088 20010301 00088 NM 2001 3 1 AWXA0001318 1 20010209 A 5551 65505817 FITTING BOEING 737 737277 1384570 NM HORIZONTAL STAB GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 LT HORIZ STAB FWD SPAR UPPER ATTACH LUG FWD FACE GOUGED. BLENDED GOUGE IAW ER 15-5510-01027-ES2. 2 L 7 2 4F RT A16WE 2001030100089 20010301 00089 NM 2001 3 1 AWXA0001320 1 20010209 A 5551 6547595 FITTING BOEING 737 737277 1384570 NM HORIZONTAL STAB GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 LT HORIZ STAB CENTER SECTION LUGS, LT REAR, AFT SIDE OF MID LUG HAS GOUGES AND NICKS ON AFT SIDE OF LUG. BLENDED NICKS AND GOUGES IAW ER 15-5510-01027-SS4. 2 L 7 2 4F RT A16WE 2001030100090 20010301 00090 NM 2001 3 1 AWXA0001321 1 20010209 A 5551 65505781 FITTING BOEING 737 737277 1384570 NM HORIZONTAL STAB GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 LT HORIZ STAB REAR SPAR UPPER ATTACH LUG AFT SIDE FACE GOUGED. BLENDED GOUGE IAW ER 15-5510-01027-ES2. 2 L 7 2 4F RT A16WE 2001030100091 20010301 00091 NM 2001 3 1 AWXA0001322 1 20010209 A 5551 6548874504 FITTING BOEING 737 737277 1384570 NM HORIZONTAL STAB CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 VERT STAB REAR LUGS, RT AFT O/B LUG HAS CORROSION ON ID OF BORE. REAMED LUG IAW BAC DWG 65C22124-10 AND EO 55-50-01; HF EC INDICATES NO DEFECTS NOTED. 2 L 7 2 4F RT A16WE 2001030100092 20010301 00092 NM 2001 3 1 AWXA0001323 1 20010209 A 5412 6579414V92 BULKHEAD BOEING 737 737277 1384570 NM NR 2 PYLON CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 NR 2 PYLON O/B STRUCTURE CHAFED AT FWD END ABOVE ENGINE. REMOVED BLKHEAD; LOCATED, DRILLED AND INSTALLED NEW BLKHEAD (P /N 65-79415-92) IAW SRM 51-30-02. 2 L 7 2 4F RT A16WE 2001030100093 20010301 00093 NM 2001 3 1 AWXA0001324 1 20010209 A 5321 654583340 WEB BOEING 737 7373Y0 1384671 NM CABIN FLOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 FLOOR WEB CRACKED FS 180 WL 207 RBL 26. REMOVED FLOOR WEB IAW SRM 51-40-02; FABED REPLACEMENT WEB IAW DWG 65-45833; INS TALLED REPLACEMENT WEB IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001030100094 20010301 00094 NM 2001 3 1 AWXA0001325 1 20010209 A 5320 69259663 INTERCOSTAL BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 INTERCOSTAL CRACKED TOP FWD EDGE FS 329 LBL 48. REMOVED INTERCOSTAL; CUT OUT DAMAGED AREA - NDT NO CRACKS NOTED; FABED AND INSTALLED REPAIR PARTS IAW SRM 51-70-11, 53-10-51, 51-30-02; INSTALLED INTERCOSTAL IAW 51-40-02. 2 L 7 2 4F RT A16WE 2001030100095 20010301 00095 NM 2001 3 1 AWXA0001326 1 20010209 A 5321 654583340 WEB BOEING 737 7373Y0 1384671 NM CABIN FLOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 FLOOR WEB CRACKED FS 180 WL 207 LBL 26. REMOVED FLOOR WEB IAW SRM 51-40-02; FABED REPLACEMENT WEB IAW DWG 65-45833; INS TALLED REPLACEMENT WEB IAW 51-40-02. 2 L 7 2 4F RT A16WE 2001030100096 20010301 00096 NM 2001 3 1 AWXA0001327 1 20010209 A 5312 6516300 BULKHEAD BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 CENTER WEB CRACKED RBL 5.0 WL 202 FS 178. REMOVED DAMAGED AREA OF WEB IAW SRM 53-10-08 FIG 209; FABED 3 FILLERS AND 1 D OUBLER; INSTALLED DOUBLER AND FILLERS IAW SRM 53-10-08 FIG 209. 2 L 7 2 4F RT A16WE 2001030100097 20010301 00097 NM 2001 3 1 AWXA0001328 1 20010209 A 5312 651630 BULKHEAD BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 CENTER WEB CRACKED FS 178 WL 202 LBL 5.0. REMOVED DAMAGED AREA OF WEB IAW SRM 53-10-08 FIG 209; FABED AND INSTALLED 3 F ILLERS AND 1 DOUBLER IAW SRM 53-10-08 FIG 209. 2 L 7 2 4F RT A16WE 2001030100098 20010301 00098 NM 2001 3 1 AWXA0001329 1 20010209 A 5320 67203859 INTERCOSTAL BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 STA 178 FWD PRESSURE BLKHEAD AFT SIDE CRACK 1.5 INCH LONG INTERCOSTAL LT SIDE WL 195. REMOVED AND REPLACED INTERCOSTAL IAW SRM 53-10-08 FIG 207. 2 L 7 2 4F RT A16WE 2001030100099 20010301 00099 NM 2001 3 1 AWXA0001330 1 20010209 A 5320 6546812 INTERCOSTAL BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 CORROSION ON TOP SURFACE INTERCOSTAL BETWEEN FS 294.5 TO FS 312.0 RBL 10. BLENDED DISCREPANT AREA AND FOUND TO BE OUT O F LIMITS IAW SRM 53-00-04; REMOVED FLOOR SUPPORT IAW 51-40-02; FABED FLOOR SUPPORT IAW ENGINEERING SUPPORT; ALODINED AND PRIMED SUPPORT IAW SRM 51-20-02; INSTALLED SUPPORT IAW 51-40-02. 2 L 7 2 4F RT A16WE 2001030100100 20010301 00100 NM 2001 3 1 AWXA0001331 1 20010209 A 5320 65366564 FLOOR SUPPORT BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 AFT CABIN FLOOR BOARD SUPPORT AT STA 927 TO 947 BL 0 IS CRACKED AT FASTENERS HOLES. REMOVED CRACKED SUPPORT IAW SRM 51- 40-02; FABED NEW BRACKET IAW 51-30-01; TREATED AND PRIMED IAW 51-20-01; INSTALLED IAW 51-40-01. 2 L 7 2 4F RT A16WE 2001030100101 20010301 00101 NM 2001 3 1 AWXA0001332 1 20010209 A 5311 65458071 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 FS 294 FRAME AT FWD SIDE OF R-1 DOOR IS CRACKED AT LOWER I/B FASTENER HOLE AT FLOOR LEVEL. REMOVED DAMAGED AREA; HFEC N O CRACKS NOTED AFTER CUT OUT; FABED AND INSTALLED FILLER AND ANGLE; TREATED AND PRIMED; ALL WORK ACCOMPLISHED IAW SRM 51 -70-11 FIG 1, 51-20-07 AND 51-40-02 AND NDTM PT 51-00-00 FIG 23. 2 L 7 2 4F RT A16WE 2001030100102 20010301 00102 2001 3 1 HNAA0100013 4 20010211 A 3460 10161110 DISPLAY DHAV DHC8 DHC8201 2809001 NM COCKPIT SMOKE A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 07 990HA 11492 9305 428 ELECTRICAL FUMES NOTED ON FINAL APPROACH. SOURCE OF FUMES WAS DETERMINED TO BE THE FMS. THE FMS WAS MEL''D ON FEBRUARY 10, 2001 FOR THE SAME PROBLEM. THE UNIT WAS DEACTIVATED PER EO8-34-01-629, UNIT CONTINUED MEL''D. 2 H 7 2 4T RT A13NM 2001030100103 20010301 00103 NM 2001 3 1 AWXA0001333 1 20010209 A 5320 69466111 FITTING BOEING 737 7373Y0 1384671 NM FUSELAGE GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 O/B SUPPORT Z-ANGLE GOUGED, LT MAIN W/W CUTOUT AFT O/B SIDE. REMOVED O/B SUPPORT IAW SRM 51-40-02; LOCATED AND DRILLED 3 HOLES IAW SRM 51-40-05; TREATED & PRIMED IAW SRM 51-20-01; INSTALLED REPLACEMENT O/B SUPPORT IAW 51-40-02. 2 L 7 2 4F RT A16WE 2001030100104 20010301 00104 NM 2001 3 1 HNAA0100014 1 20010209 A 2710 CONTROL CABLE DHAV DHC8 DHC8102 2809003 NM AILERON CONTROL OUT OF TOLERANCE A HNAA O OTHER F FLT CONT AFFECTED CR CRUISE 1 EA 07 915HA 069 UPON RELEASE OF AUTO PILOT, NOTED ROLL CONTROL VERY STIFF, SEEMS TO REDUCE WITH REDUCTION IN AIR SPEED. INSPECTED AILER ONS AND ROLL SPOILERS, FOUND AILERON CONTROL CABLE TENSIONS OUT OF LIMITS. RE-TENSIONED CABLES. EVALUATION FLIGHT SATI SFACTORY. 2 H 7 2 4T RT A13NM 2001030100105 20010301 00105 WP 2001 3 1 IXXA01000052 1 20010212 A 5280 56489332 DOOR DOUG DC8 DC862 3021970 WP RT MLG MISSING A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 45918 AFTER AN UNEVENTFUL LANDING AND DURING POST FLIGHT INSPECTION AT WRI. MAINTENANCE FOUND THE RIGHT MAIN LANDING GEAR LOW ER FLYING DOOR MISSING FROM THE GEAR. NO OTHER DAMAGE TO THE AIRCRAFT WAS NOTED. 2 L 7 4 4F 4A25 2001030100106 20010301 00106 WP 2001 3 1 TWAA0102701 1 20010211 A 3350 MISC0639 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 964TW 53614 THE LIGHTS OVER LT FWD AND RT FWD OVERWING EMERGENCY EXITS WERE INOPERATIVE. REPLACED THE BATTERIES. CHECK-C 5-6-00 ST L. 2 L 7 2 4F RT A6WE 2001030100107 20010301 00107 NM 2001 3 1 TWAA0102702 1 20010211 A 3350 582243 BATTERY PACK BOEING 767 767231 1385131 NM CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 605TW 22568 THE CABIN FLOOR EGRESS LIGHTS WERE INOPERATIVE ON THE RT SIDE FROM ROW 11 TO THE MID-CABIN LAVATORIES. REPLACED THE BAT TERY PACK. CHECK-C 12-23-00 MCI. 2 L 7 2 4F RT A1NM 2001030100108 20010301 00108 WP 2001 3 1 TWAA0102703 1 20010210 A 3350 0105606004 MODULE DOUG DC9 DC983 3022083 WP ROW 14 INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9412W 53187 THE EGRESS FLOOR LIGHT WAS INOPERATIVE AT ROW 14. REPLACED THE LIGHT MODULE AT ROW 14. CHECK-C 9-7-00 STL. 2 L 7 2 4F RT A6WE 2001030100109 20010301 00109 WP 2001 3 1 TWAA0102704 1 20010210 A 3350 58222 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 920TW 49369 THE PORTABLE EMERGENCY LIGHT AND THE FIRST CLASS CABIN EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE PORTABLE LIGHT ASSE MBLY, (P/N 10-0119-1), AND CLEANED MOISTURE FROM THE FIRST CLASS EGRESS LIGHT STRIP AND REPLACED THE POWER SUPPLY. CHEC K-C 9-20-00 MCI. 2 L 7 2 4F A6WE 2001030100110 20010301 00110 WP 2001 3 1 TWAA0102705 1 20010204 A 7830 LINE DOUG DC9 DC983 3022083 WP T/R ACCUMULATOR LEAKING A TWAA H DEACTIVATE SYST/CIRCUITS K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CE 05 9307R 49663 WITH AIRFOIL ANTI-ICE ON FOR FINAL 5 MINUTES OF FLIGHT SOME VISIBLE SMOKE APPEARED IN CABIN WITH SLIGHT SMOKY SMELL IN C OCKPIT. SMELL AND SMOKE DISAPPEARED WHEN AIRFOIL ANTI-ICE AND ENG ANTI-ICE TURNED OFF AND PNEUMATIC CROSS-FEED VALVES W ERE CLOSED. FOUND LT REVERSER CONTROL VLV TO ACCUMULATOR LINE LEAKING ALLOWING FLUID TO ENTER APU INLET WHEN RUNNING. REPLACED FITTING AND O-RING. CHECK-C 12-3-00 MCI. 2 L 7 2 4F RT A6WE 2001030100111 20010301 00111 WP 2001 3 1 TWAA0102706 1 20010210 A 3350 0105607001 LENS DOUG DC9 DC983 3022083 WP ROW 10 OUT OF POSITION A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 969TW 53619 THE EGRESS LIGHTING FROM ROW 12 TO 16 WERE INOPERATIVE, AND A RED EGRESS LENS WAS LOCATED WHERE A WHITE LENS WAS REQUIRE D. RE-ATTACHED THE EGRESS LIGHT CONNECTOR AT ROW 16, AND INSTALLED A WHITE LENS. CHECK-C 7-28-00 JFK. 2 L 7 2 4F RT A6WE 2001030100112 20010301 00112 WP 2001 3 1 TWAA0102707 1 20010207 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C IN THE FWD CARGO COMPT, THE LT TIE DOWN TRACK AT STA 541 WAS CORRODED. SPLICED IN NEW CARGO TRACK PER SR M 53-05, FIG 4G, PAGE 10R. PAINTED PER SRM 51-10-03. 2 L 7 2 4F A6WE 2001030100113 20010301 00113 WP 2001 3 1 TWAA0102708 1 20010206 A 5210 LATCH DOUG DC9 DC983 3022083 WP PAX DOOR DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9401W 53137 DURING CHECK-C MAINT A TIME LIMITED REPAIR AT THE FWD CABIN DOOR ON THE LT SIDE, THE GUST LOCK LATCH, REPAIR HAD BLIND F ASTENERS. REMOVED REPAIR PATCH AND INSTALLED NEW PERMANENT REPAIR PER SRM 53-04, FIG 24. 2 L 7 2 4F RT A6WE 2001030100114 20010301 00114 WP 2001 3 1 TWAA0102709 1 20010206 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9401W 53137 DURING CHECK-C MAINT IN THE AFT CARGO COMPT THE LT FLOOR TRACK WAS CORRODED AT STA 1222 TO 1322. REPLACED WITH NEW FLOO R TRACK PER SRM 51-01, PAGE 1 ITEM C. 2 L 7 2 4F RT A6WE 2001030100115 20010301 00115 WP 2001 3 1 TWAA0102710 1 20010208 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9401W 53137 DURING CHECK-C MAINT CABIN FLOOR TRACK AT LBL 22, STA 807 TO 1308, HAD CORROSION REMOVED BEYOND LIMITS. REPLACED FLOOR TRACK FROM STA 807 TO 1308, PER SRM 53-05 PAGE 109. 2 L 7 2 4F RT A6WE 2001030100116 20010301 00116 WP 2001 3 1 TWAA0102711 1 20010206 A 5320 ANGLE DOUG DC9 DC931 3022065 WP PAX DOORWAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 992Z 47095 DURING OP 15 MAINT CHECK THE FWD PASSENGER DOOR ENTRY THRESHOLD PLATE SUPPORT ANGLE AT LBL 55, STA 160 TO 200, WAS CORRO DED. REPLACED SUPPORT ANGLE PER SPM 6-70-01. MADE PART FROM MATERIAL PER DRAWING 9936534. INSTALLED PER SRM 51-30-02 AND SRM 51-30-03. 2 L 7 2 4F A6WE 2001030100117 20010301 00117 WP 2001 3 1 TWAA0102712 1 20010207 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT FOUND HEAVY CORROSION ON MEMBRANE AT LBL 54 INCHES, BETWEEN STA 160 AND 190. REMOVED CORRODED AREA . FABRICATED DOUBLER AND INSTALLED PER SRM 53-01 FIG 4 SHEET 3. TREATED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001030100118 20010301 00118 WP 2001 3 1 TWAA0102713 1 20010207 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT FOUND FLOOR MEMBRANE CORRODED AT STA 163, LBL 16 INCHES. REMOVED CORROSION PER SPM 6-80-01. TREAT ED AREA PER SRM 51-10-3. FABRICATED DOUBLERS AND INSTALLED PER SRM 53-01, FIG 4 SHEET 3. 2 L 7 2 4F A6WE 2001030100119 20010301 00119 EA 2001 3 1 COMA0160220 1 20010211 A 5210 ANGLE CNDAIR CL600 CL6002B19 EA PAX DOOR DAMAGED A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 938CA 7046 DAMAGE TO PASSENGER DOOR SEAL STRIKER AT FUSELAGE STA 310.00 AND 349.00. REPAIRED PASSENGER DOOR SEAL STRIKER AT FS 310 .00 AND 349.00 IAW REO 601R-52-11-008 REPAIR A, SHEETS 2-3. 2 L 7 2 4F RT A21EA 2001030100120 20010301 00120 EU 2001 3 1 MALA010178 1 20010208 A 3260 LIGHT SAAB SF340 340B 7860101 EU LT MLG DIRTY A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 439XJ 439 RT PROP ANN ON OVERHEAD PANEL ILLUMINATED, RESET TWICE ON THIRD ATTEMPT THE LIGHT NO LONGER ILLUMINATED. LT CAME ON AFT ER 2 MINUTES IN FIRST TWO ATTEMPTS. MAINTENANCE REPLACED TERMINAL END ON BRUSH BLOCK. LANDING GEAR AMBER INTRANSIT LIG HT REMAINED ILLUMINATED WITH HANDLE UP, COMPLIED WITH ORH AND RECYCLED THE GEAR BUT LIGHT REMAINED ILLUMINATED. CHECKED CIRCUIT BREAKERS AND ALL WERE IN. DID NOT NOTICE PUMP RUNNING WHILE GEAR WAS UP. MAINTENANCE INSPECTED, SUSPECT ICE A ND GRIME BUILDUP IN GEAR WELL, REASON FOR INTRANSIT LIGHT. CLEANED NOSE AND LT & RT GEAR AND GEAR WELLS. LUBED GEAR, O PS CHECK GOOD. 2 L 7 2 4T RT A52EU 2001030100121 20010301 00121 EU 2001 3 1 MALA010179 1 20010208 A 2420 51634002 GENERATOR SAAB SF340 340B 7860101 EU LEFT DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 450XJ 450 LT AC GENERATOR AND INTAKE LIGHT ON IN FLIGHT, EVERYTHING BUT INTAKE TRANSFERED. MAINTENANCE FOUND LT AC GEN CONTROL UN IT CONNECTOR CONTAMINATED, CLEANED CONNECTOR, REPLACED LT AC GEN CONTROL UNIT (P/N 51634-002), SN/OFF 98029, SN/ON 97059 . IAW SF340 AMM 24-21-10-2. FAILED OPS CHECK. MAINTENANCE REPLACED LT AC GCU (P/N 51634-002) (S/N OFF 97059) (S/N ON 98028), FOR TROUBLESHOOTING, FAILED OPS CHECK. SWAPPED AC GEN FOR T-SHOOTING, FAILED OPS CHECK. RETURNED AC GEN TO ORI GINAL POSITION, LT & RT LEAK CHECK GOOD. REPLACED IAW SF340-AMM. LEFT AC GEN HARNESS-GCU CONNECTOR AT FAULT, DEFERRED LT AC GEN IAW MEL 24-21-18. 2 L 7 2 4T RT A52EU 2001030100122 20010301 00122 EU 2001 3 1 MALA010180 1 20010208 A 3020 NH24668169 HEATER SAAB SF340 340B 7860101 EU LT INTAKE DUCT MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 453XJ 453 LT INTAKE HEAT FAILED EN ROUTE TO MLI. FLIGHT RETURNED TO DTW. MAINTENANCE REPLACED LOWER DUCT ON LEFT ENGINE. RAN AC 1/2 HR. OPS CHECK GOOD, IAW SAAB MM 30-00-00, P/N NH24668-169, S/N OFF L283723, S/N ON L198033. 2 L 7 2 4T RT A52EU 2001030100123 20010301 00123 EU 2001 3 1 MALA010181 1 20010208 A 3260 WARNING LIGHT BAC 146 AVRO146RJ85A 1500097 EU LT MLG ILLUMINATED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 526XJ E2351 LT MAIN INTRANSIT LIGHT AND GEAR HANDLE UNSAFE LIGHT REMAINS ILLUMINATED IN FLIGHT, CYCLED GEAR-NO EFFECT. MAINTENANCE REPLACED PCB P/N 8-060-02, S/N OFF A184704, S/N ON A185321, PERFORMED OPS AND GEAR CYCLES. OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 2001030100125 20010301 00125 NM 2001 3 1 MWEA010150 1 20010209 A 2121 6054577 FAN DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A MWEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 31 701ME 49760 PILOTS AND FLIGHT ATTENDANTS NOTICED A STRONG RUBBER ODOR THROUGHOUT AIRCRAFT. REMOVED AND REPLACED CABIN AIR RECIRCULA TION FAN. 2 L 7 2 4F RT A6WE 2001030100126 20010301 00126 NM 2001 3 1 UPS01434921 1 20010103 A 5730 DOUBLER BOEING 747 747123F NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, RT WING LOOSE FASTENERS ON JOINT IN L/E BULL NOSE SECTION O/B AT WS 320. REPAIRED IAW SRM 57-30-04 F IG 1 AND Q/NOTE 5/01. 2 L 7 4 4F A20WE 2001030100127 20010301 00127 NM 2001 3 1 UPS01434922 1 20010103 A 5730 DOUBLER BOEING 747 747123F NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, RT WING L/E CRACK ON INNER STRUCTURE OF WING BULLNOSE JUST I/B OF NR 4 ENGINE. REPAIRED IAW SRM 51-4 0-03. 2 L 7 4 4F A20WE 2001030100128 20010301 00128 NM 2001 3 1 UPS01434923 1 20010106 A 5720 ANGLE BOEING 747 747123F NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, RT WING FEAR STRUT DOOR I/B FAIRING SUPPORT ANGLE IS CRACKED. SUPPORT ANGLE REPLACED IAW SRM 51-30- 02. 2 L 7 4 4F A20WE 2001030100129 20010301 00129 NM 2001 3 1 UPS01434924 1 20010101 A 5414 DOUBLER BOEING 747 747123F NM NR 3 PYLON DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, NR 3 ENGINE INBOARD LOWER PYLON SKIRT AREA DAMAGED ON THE INSIDE AFT OF REAR ENGINE MOUNT. REPAIRED SKIRT IAW SRM 51-40-02. 2 L 7 4 4F A20WE 2001030100130 20010301 00130 NM 2001 3 1 UPS01434925 1 20010104 A 5753 CHANNEL BOEING 747 747123F NM NR 5 FLAP TRACK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, RT WING DIAPHRAM SUPPORT CHANNEL CRACKED IN TWO PLACES LOCATED ABOVE FLAP TRACK NR 5 AND AFT OF MOUNT . SUPPORT CHANNEL REPLACED IAW SRM 51-30-02. ANGLE FABRICATED PER BAC 5300 AND SOLUTION HEAT TREATED AND INSTALLED. 2 L 7 4 4F A20WE 2001030100131 20010301 00131 NM 2001 3 1 UPS01434928 1 20010102 A 5730 SKIN BOEING 747 747123F NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, RT WING L/E CORROSION ON L/E LWR IN SPAR SKIN AT OLES 833 RT. NDT INSPECTION OF AREA ACCOMPLISHED, D AMAGED REMOVED AND REPROTECTED IAW QUERY NOTE 2/01, BLEND OUTS PER INSTRUCTIONS. 2 L 7 4 4F A20WE 2001030100132 20010301 00132 NM 2001 3 1 UPS01434930 1 20010111 A 5320 SPLICE BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, LOWER BILGE AREA AFT CORROSION ON STR AT CLIP FRAME BS 2320 STR 50 RHS. STRINGER REPAIRED IAW SRM 5 3-10-03 FIG 9. 2 L 7 4 4F A20WE 2001030100133 20010301 00133 NM 2001 3 1 UPS01434931 1 20010111 A 5320 ANGLE BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, MAIN DECK ON AFT CARGO HOLD CEILING ANGLES AT BS 1840 - 1860 LBL 7 AND RBL 7 CORRODED. NEW SUPPORT A NGLES FABRICATED AND FITTED IAW SRM 51-20-01 AND SRM 51-30-02. 2 L 7 4 4F A20WE 2001030100134 20010301 00134 NM 2001 3 1 UPS01434932 1 20010112 A 5330 DOUBLER BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C AFT CARGO HOLD FUSELAGE FRAMES AT BS 1520 - AND 1560 ARE CRACKED BETWEEN STRS 39 AND 40 LT. FRAMES A T BS 1520 & 1560 REPAIRED IAW QUERY NOTE 10/01 BOEING APPROVED REPAIRS. 2 L 7 4 4F A20WE 2001030100135 20010301 00135 NM 2001 3 1 UPS01434933 1 20010109 A 5347 SEAT TRACK BOEING 747 747123F NM CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, MAIN DECK LIGHT CORROSION ON INNER FLANGE OF SEAT TRACK AT BS 485 - 495 RBL 66. SEAT TRACK REPLACED IAW SRM 51-80-02. 2 L 7 4 4F A20WE 2001030100136 20010301 00136 NM 2001 3 1 UPS01434934 1 20010101 A 5330 DOUBLER BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, MAIN DECK FRAME WEB IS CRACKED AT CUTOUT FOR STR AT BS 920 STR 24 RT. FRAME WEB REPAIRED IAW SRM 53- 10-04. 2 L 7 4 4F A20WE 2001030100137 20010301 00137 NM 2001 3 1 UPS01434936 1 20010111 A 5340 69B620491 FITTING BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, MAIN DECK CORROSION ON PALLET LOCK TIE DOWN FITTING AT BS 2040 RBL 80. FITTING REPLACED IAW SRM 51-3 0-02. 2 L 7 4 4F A20WE 2001030100138 20010301 00138 NM 2001 3 1 UPS01434937 1 20010129 A 5340 69B620501 FITTING BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, CORROSION ON PALLET LOCK TIE DOWN FITTING AT BS 2080 LBL 60. FITTING REPLACED IAW SRM 51-30-02. 2 L 7 4 4F A20WE 2001030100139 20010301 00139 NM 2001 3 1 QXEA0100103 1 20010211 A 3350 CONNECTOR DHAV DHC8 DHC8202 2809007 NM CABIN DISCONNECTED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 358PH 506 SEA - FLOOR EMERGENCY LIGHT, ROW 5-7 INOP. RE-CONNECTED ELECTRIC PLUG AT FLOOR LT STRIP. OPS CHECKED GOOD. NO PARTS R EPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001030100140 20010301 00140 EA 2001 3 1 SWIA972342 1 20010203 A 3030 HEATER CNDAIR CL600 CL6002B19 EA PITOT STATIC INOPERATIVE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 416SW 7089 AT 1500 FEET AFTER TAKEOFF PITOT BASE HEAT, LAOA HEAT, L STATIC HEAT, AND L PITOT HEAT MESSAGES ON EICAS WOULDN''T EXTIN GUISH. RETURNED TO SLC. CYCLED POWER TO AC LEFT PITOT HEAT. MESSAGES OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2001030100142 20010301 00142 SO 2001 3 1 20010226CW006 1 20010130 A 2740 62701113 CONTROL CABLE PIPER PA28 PA28161 7102803 SO STABILATOR WORN E K NONE O OTHER IN INSP/MAINT 1 EA 05 9182X 5000 2841130 LEFT FORWARD STABILATOR CONTROL CABLE WORN PAST LIMITS IN 43.13 DVC TO EXCESSIVE PRESSURE ON FAIRLEAD WHERE CABLE TRAVER SES SPAR. 1 L 7 1 3O 2A13 2001030100143 20010301 00143 WP 2001 3 1 AALA20010123 1 20010108 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 TUL - FOUND LONGERON 28R AT STATION 320 IS DAMAGED INBOARD SIDE OF LONGERON CHANNEL IS BENT DOWNWARD. REPAIRED AREA PER SRM 53-02 PAGE 48-53, FIG 18 SHEET 1. (M) 2 L 7 2 4F RT A6WE 2001030100144 20010301 00144 WP 2001 3 1 AALA20010124 1 20010108 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 TUL - FOUND LONGERON ABOVE FORWARD ENTRY DOOR STATION 168 CRACKED. REPAIRED LONGERON PER SRM 53-02, PAGE 48, FIG 18 SHE ET 1. (M) 2 L 7 2 4F RT A6WE 2001030100145 20010301 00145 WP 2001 3 1 AALA20010125 1 20010108 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 TUL - FOUND RIGHT CUSP CORRODED TOP SIDE, STATION 522-528. REPAIRED CORROSION AREA PER AARD 53-00-00-02. (M) 2 L 7 2 4F RT A6WE 2001030100146 20010301 00146 WP 2001 3 1 AALA20010126 1 20010108 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 TUL - FOUND SEAT TRACK NR 5 CORRODED AT STATION 237. REMOVED SECTION AND INSTALLED NEW SECTION WITH SPLICE PER SRM 53-0 5 PART 1 FIG 4F. (M) 2 L 7 2 4F RT A6WE 2001030100153 20010301 00153 SO 2001 3 1 SIMA0364 1 20010205 A 7500 BAS1016762MMZ78M DUCT EMB 145 EMB145LR SO RT NACELLE DAMAGED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING LD LANDING 1 SW 21 631AE 145139 XNA - FLT 3721 - ON TOUCHDOWN, THE CREW REPORTED THE NR 2 ENGINE FIRE WARNING INDICATION. THE CREW PULLED THE FIRE BOTT LE HANDLES AND RELEASED THE AGENT. AFTER THE AIRCRAFT WAS PARKED, THE CREW AND CRASH FIRE AND RESCUE WALKED AROUND AND FOUND NO VISIBLE EVIDENCE OF ACTUAL FIRE. NO PASSENGER INCIDENTS REPORTED. MAINTENANCE FOUND BLEED DUCT BLOWN OUT IN N R 2 ENGINE NACELLE AREA AND BLOWING DIRECTLY ON FIRE SENSING LOOP. MAINTENANCE REMOVED AND REPLACED BLEED DUCT ASSEMBLY . BOTH ENGINE FIRE BOTTLES WERE REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001030100154 20010301 00154 SO 2001 3 1 SIMA0342 1 20010203 A 2130 2014ABREVC MODULE EMB 145 EMB145LR SO CABIN PRESSURE MALFUNCTIONED A SIMA B EMER. DESCENT O OTHER CL CLIMB 1 SW 21 643AE 145200 SGF - FLT 3560 - DURING CLIMB, WITH AUTO PRESSURIZATION SELECTED CABIN WENT TO 15,000 CAUSING ALL OXYGEN MASKS TO DEPLOY . AIRCRAFT DESCENDED TO 10,000 AND USED MANUAL PRESSURIZATION. MAINTENANCE REMOVED AND REPLACED CABIN PRESSURE AQUISTI ON MODULE IAW EMB 145 AMM 21-32-01. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001030100155 20010301 00155 SO 2001 3 1 SIMA00311 1 20010103 A 2530 XK0438 COFFEEMAKER EMB 145 EMB145 SO GALLEY MALFUNCTIONED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 609AE 145069 CMH - FLT 4039 - CREW REPORTED THREE BREAKERS IN THE GALLEY POPPED IN FLIGHT FOLLOWED BY A SMOKE ODOR IN THE COFFEE HOT JUG AREA. SEVERAL MINUTES LATER THE EMERGENCY LIGHTS CAME ON AND THE CABIN LIGHTS FLICKERED. AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS REPORTED. REMOVED AND REPLACED HOT JUGS IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4F RT T00011AT 2001030100156 20010301 00156 SO 2001 3 1 SIMA0215 1 20010121 A 7830 WARNING SYSTEM EMB 145 EMB145LR SO COCKPIT ACTIVATED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 649PP 145234 ABI - FLT 9735 - THE FLIGHT CREW ABORTED TAKEOFF DUE TO BOTH THRUST REVERSER DISAGREE INDICATION. SERVICED NOSE STRUT I AW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT T00011AT 2001030100157 20010301 00157 SO 2001 3 1 SIMA0265 1 20010126 A 5610 8103731 WINDSHIELD EMB 145 EMB145LR SO COCKPIT FAILED A SIMA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 630AE 145132 IND - FLT 4048 - IN CRUISE CAPTAINS WINDSHIELD SHATTERED. MAINTENANCE REMOVED AND REPLACED CAPTAINS WINDSHIELD IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001030100160 20010301 00160 NE 2001 3 1 SIMA0392 3 20010208 A 6111 730305OLN8173873 SEAL SAAB SF340 340B 7860101 EU ROTOL R354 R3544123F13 NE RT ENGINE PROP FAILED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 304AE 340B304 BOS - FLT 4579 - RIGHT ENGINE INTAKE SATURATED WITH OIL. CABIN AIR HAS CONTINUOUS FAINT OIL SMELL INFLIGHT. REMOVED AN D REPLACED NR 1 PROP BLADE SEAL. (M) 2 L 7 2 4T RT A52EU 6 C P61GL 2001030100161 20010301 00161 NE 2001 3 1 SIMA0382 2 20010207 A 7200 WARNING SYSTEM SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE COCKPIT MALFUNCTIONED A SIMA C ABORTED TAKEOFF J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 21 901AE 340B401 DFW - FLT 3307 - LEFT ENGINE HAD POPPING NOISE, ENGINE OVERTEMP AND IGNITION LIGHTS ILLUMINATED ON TAKEOFF ROLL. PAX RE PORTED SEEING SPARKS FROM EXHAUST. PERFORMED ENGINE WASH AND BORESCOPE NO DEFECTS NOTE. PERFORMED OPERATIONAL CHECK OF APR SYSTEM AND ANTI-ICE START BLEED VALVE. NO DEFECTS NOTED. ENGINE RUNS AND OPS CHECKS WERE GOOD. ALL CHECKS PERFOR MED IAW MM. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 2001030100162 20010301 00162 NM 2001 3 1 USAASB01028 1 20010126 A 3350 6104789 BATTERY PACK BOEING 737 7372B7 1384560 NM AFT CARGO BAY DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 277AU 22889 IAD - MAINTENANCE FOUND THE EXTERIOR AFT SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE AFT CARGO BAY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 2001030100163 20010301 00163 WP 2001 3 1 USAAD01020 1 20010203 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 813US 48093 PIT - THE EMERGENCY LIGHTS FOUND ON. AFTER TESTING THE EMERGENCY LIGHT SYSTEM MAINTENANCE REPLACED TWO LOW LEVEL EMERGE NCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001030100164 20010301 00164 WP 2001 3 1 USAAD01021 1 20010205 A 3350 873100272 LIGHT DOUG DC9 DC981 3022081 WP CABIN SHORTED A USAA K NONE O OTHER CR CRUISE 1 EA 19 807US 48039 MHT-PIT - FLT 395 - DURING CRUISE, THE EMERGENCY LIGHTS ILLUMINATED WITH THE EMERGENCY LIGHT SWITCH IN THE ARM POSITION. WITH THE EMERGENCY LIGHT SWITCH IN THE OFF POSITION ALL LIGHTS EXTINGUISHED EXCEPT THE EMERGENCY LIGHTS AT THE EMERGEN CY EXIT ROWS. THE EMERGENCY LIGHTS ARM AND CHARGE CIRCUIT BREAKER WAS FOUND POPPED. MAINTENANCE REPLACED THE FORWARD L EFT OVERWING EXIT IDENTIFIER LIGHT. (M) 2 L 7 2 4F A6WE 2001030100165 20010301 00165 WP 2001 3 1 USAAD01022 1 20010207 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 805US 48053 IND - THE LOW LEVEL EMERGENCY LIGHTS WERE DIM. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001030100166 20010301 00166 WP 2001 3 1 USAAD01018 1 20010204 A 3350 9721055 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 829US 49429 TPA - THE LOW LEVEL EMERGENCY LIGHT AS SEAT ROW 25 WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 2001030100167 20010301 00167 WP 2001 3 1 USAAD01017 1 20010123 A 2560 1001191 FLASHLIGHT DOUG DC9 DC982 3022082 WP PAX DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 830US 49443 BOS - THE EMERGENCY FLASHLIGHT MOUNTED AT THE MAIN ENTRY DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY FLASH LIGHT. (M) 2 L 7 2 4F A6WE 2001030100168 20010301 00168 WP 2001 3 1 USAAD01019 1 20010202 A 3350 AD4002P BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 924VJ 48144 IND - THE CEILING EMERGENCY LIGHTS ABOVE SEAT ROWS 1 THROUGH 4 WERE DIM. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTE RY. (M) 2 L 7 2 4F A6WE 2001030100169 20010301 00169 WP 2001 3 1 USAAD01014 1 20010124 A 3350 AD4002P BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 955VJ 47593 IND - THE EMERGENCY LIGHTS IN THE AFT FUSELAGE WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 2001030100170 20010301 00170 WP 2001 3 1 USAAD01016 1 20010126 A 3350 AD4002P BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 955VJ 47593 IND - THE FORWARD OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 2001030100171 20010301 00171 NM 2001 3 1 USAASB01031 1 20010131 A 2410 CSD BOEING 737 7372B7 1384560 NM NR 1 ENGINE MALFUNCTIONED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 277AU 22889 ORD - FLT 2800 - EN ROUTE FROM BWI-MDW, CAPTAIN REPORTED THAT THE NR 1 TRANSFER BUS TRIPPED OFF LINE. MOST OF THE CAPTA INS FLIGHT INSTRUMENTS WERE LOST ALONG WITH PARTIAL ANTI-SKID AND RADIO. CIRCUIT BREAKER WAS FOUND POPPED OUT BUT COULD NOT BE RESET. FLIGHT DIVERTED TO ORD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE DIS CONNECTED NR 1 CSD, RESET BREAKER AND RAN ENGINES/APU. POWER TRANSFERS OK. (M) 2 L 7 2 4F A16WE 2001030100172 20010301 00172 EU 2001 3 1 SIMA0251 1 20010125 A 2530 1095A COFFEEMAKER SAAB SF340 340B 7860101 EU GALLEY MALFUNCTIONED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 324AE 340B324 LAX - FLT 3113 - CREW REPORTED AN ELECTRICAL SMELL AFTER TAKEOFF. NO SMOKE WAS OBSERVED AND SMELL APPEARED TO BE COMING FROM THE GALLEY AREA. REMOVED AND REPLACED HOT JUG CONTAINERS IAW SAAB AMM 25-32. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001030100173 20010301 00173 EU 2001 3 1 SIMA0263 1 20010126 A 3240 AIR130904 HARNESS SAAB SF340 340B 7860101 EU LT MAIN GEAR FAILED A SIMA K NONE J WARNING INDICATION AP APPROACH 1 SW 21 273AE 340B273 DFW - FLT 3789 - CREW REPORTED AN ANTI-SKID FAULT WHEN GEAR WAS SELECTED DOWN. REMOVED AND REPLACED LEFT MAIN ANTI-SKID HARNESS IAW SAAB 340 AMM 32-31-00. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001030100174 20010301 00174 EA 2001 3 1 MASA02015 1 20010207 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77195 7195 FLT 5776 - LIT-CLT, PILOT REPORTED FLOOR EMERGENCY ESCAPE LIGHTING INOPERATIVE. MAINTENANCE RESET THE CANNON PLUG TO TH E NR 3 INVERTER. OPS CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2001030100175 20010301 00175 EA 2001 3 1 MASA02016 1 20010208 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 EA PAX DOOR INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17217 7217 DURING OVERNIGHT MAINTENANCE, IT WAS DISCOVERED THAT THE PAX DOOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMVOED AND REPLACED THE LIGHT BULB. OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001030100176 20010301 00176 EA 2001 3 1 MASA02017 1 20010208 A 3350 BATTERY CNDAIR CL600 CL6002B19 EA CABIN DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27191 7191 FLT 6591 - DCA-CMH - PILOT REPORTED ALL EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE FOUND THE FA''S SWITCH TURNED ON . MAINTENANCE CHARGED THE BATTERIES. OPS CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001030100177 20010301 00177 NM 2001 3 1 GAIA01003OP 1 20010104 A 2700 CONTROL UNIT BOEING 727 727287 1384020 NM COCKPIT MALFUNCTIONED A GAIA K NONE E F VIBRATION/BUFFET FLT CONT AFFECTED CR CRUISE 1 SW 07 916PG 21690 FLT 1735 - BNA-FWA - THE CREW REPORTED THAT THE AIRPLANE VIBRATES AND TE CONTROL WHEEL HARD TO TURN AS IF MAYBE A FLIGHT CONTROL IS OUT OF ADJUSTMENT. IT TAKES TWO UNITS OF RUDDER TRIM TO STRAIGHTEN THE PLANE IN LEVEL FLIGHT. THE AIRCRAFT MADE A SAFE LANDING IN FWA. MAINTENANCE INSPECTED AND OPERATED ALL FLIGHT CONTROLS. NO DEFECTS NOTED. THE AIRCRAFT W AS THEN RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2001030100178 20010301 00178 NM 2001 3 1 GAIA01004OP 1 20010104 A 3350 1104441 PLATE BOEING 727 727214 138407R NM COCKPIT BROKEN A GAIA K NONE O OTHER CR CRUISE 1 SW 07 751US 21513 FLT 710 - MKE-MSP - DURING CRUISE, THE EMERGENCY EXIT LIGHT ILLUMINATED AND REMAINED ILLUMINATED. THE AIRCRAFT CONTINUE D ON TO MSP AND LANDED WITH NO FURTHER PROBLEMS. MAINTENANCE FOUND THE BASE PLATE BROKEN. REMOVED AND REPLACED BASE PL ATE. OPERATIONAL CHECK PERFORMED OK. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001030100179 20010301 00179 NM 2001 3 1 GAIA01010OP 1 20010112 A 2761 1060779108 ROD END BOEING 727 727223 1384074 NM NR 10 SPOILER BROKEN A GAIA K NONE O OTHER DE DESCENT 1 SW 07 6809 19484 FLT 2018 - MHR-SEA - ON DESCENT, THE FLIGHT CREW OBSERVED THAT ON SPEED BRAKE DEPLOYMENT THE AIRCRAFT ROLLED TO THE LEFT . A UNEVENTFUL LANDING WAS MADE AT SEA. INVESTIGATION REVEALED THAT THE NR 10 SPOILER ACTUATOR ROD END WAS BROKEN. TH E NR 10 SPOILER ROD END WAS REMOVED AND REPLACED IAW THE B727 MM. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001030100180 20010301 00180 NM 2001 3 1 GAIA01011OP 1 20010119 A 3350 1864 LIGHT BOEING 727 727223 1384074 NM COCKPIT INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6831 20184 EMERGENCY EXIT UNARMED LIGHT WAS FOUND TO BE INOPERATIVE DURING ROUTINE MAINTENANCE AT FWA. RELAMPED AS REQUIRED OPS CH ECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001030100181 20010301 00181 NM 2001 3 1 USAA010049 1 20010116 A 5310 ANGLE BOEING 737 7374B7 1384702 NM AFT SERVICE DR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 32038 24556 CLT - FOUND Z-ANGLE CORRODED 2.25 INCH BY 27 INCHES, RT AFT SERVICE DOOR Z-ANGLE STATION 956-996, RBL 53. INSTALLED NEW Z-ANGLE PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001030100182 20010301 00182 NM 2001 3 1 USAA010025 1 20010115 A 5310 ANGLE BOEING 737 7374B7 1384702 NM AFT SEVICE DR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 32038 24556 CLT - FOUND Z-ANGLE CORRODED 2.25 INCH BY 40 INCH, LEFT AFT ENTRY DOOR Z-ANGLE STATION 953-994, LBL 53. REPLACED Z-ANGL E PER 51-10-1. (M) 2 L 7 2 4F RT A16WE 2001030100183 20010301 00183 NM 2001 3 1 USAA010024 1 20010115 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 32038 24556 CLT - FOUND FLOORBEAM CORRODED 2 INCHES BY .5 INCHES, BS 967, LBL 14-18. CORROSION LEVEL 1 C53-107-02. INSTALLED LEG R EPAIR AND DOUBLER PER SRM 53-60-51 FIG 203. (M) 2 L 7 2 4F RT A16WE 2001030100187 20010301 00187 NM 2001 3 1 USAA0106 1 20010130 A 5320 STRUCTURE BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 520AU 40660 23706 CLT - FOUND CHORD CRACKED .6 INCH, AFT SIDE OF BS 178 BULKHEAD, LBL 5-7, WL 184. INSTALLED DOUBLER PER 53-10-08 BOEING 65-22732. (M) 2 L 7 2 4F RT A16WE 2001030100188 20010301 00188 NM 2001 3 1 USAA010105 1 20010130 A 5312 STRAP BOEING 737 7373B7 1384580 NM BULKHEAD CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 520AU 40660 23706 CLT - FOUND STRAP .75 INCH, BS 178 BULKHEAD LBL 5-7, WL 205. INSTALLED DOUBLER PER EA 68728. (M) 2 L 7 2 4F RT A16WE 2001030100189 20010301 00189 NM 2001 3 1 USAA010104 1 20010130 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 32258 24554 CLT - FOUND FRAME CRACKED .5 INCH, STATION 727B BETWEEN STRINGER 9R AND 8R. FABRICATED DOUBLER AND INSTALLED PER TR 53- 10-14. (M) 2 L 7 2 4F RT A16WE 2001030100190 20010301 00190 CE 2001 3 1 20010228CW006 1 20010118 A 5610 10138402521 WINDSHIELD BEECH B300 B300 1159232 CE PWA PT6 PT6* 52043 EA COCKPIT CRACKED B O OTHER O OTHER NR NOT REPORTED 1 SW 99 2298B 4 FL198 PILOT SIDE WINDSHIELD WAS INSTALLED . AC COMPLETED 1 FLIGHT APPROX 4.2 HRS WHEN OUTER PLY OF WINDSHIELD CRACKED. AC LA NDED AT MAIN FACILITY FOR REPLACEMENT OF THE WINDSHIELD. PER PROCEDURES, INSTALLATION IS ACCOMPLISHED USING STRESS FREE KITS AND PROCEDURES MAKING INSTALLATION INDUCED STRESS OF THE WINDSHIELD UNLIKELY. QUESTION CONCERNING INTEGRITY OF WI NDSHIELD ASSEMBLY. 2 L 7 2 4T 3 T RT A24CE E2NE 2001030100192 20010301 00192 NM 2001 3 1 USAA010102 1 20010130 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 32258 24554 CLT - FOUND FRAME CRACKED .25 INCH, STATION 727D BETWEEN STRINGER 9R AND 8R. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001030100193 20010301 00193 NM 2001 3 1 USAA010101 1 20010130 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 32258 24554 CLT - FOUND FRAME CRACKED .25 INCH, STATION 747 BETWEEN STRINGER 9L AND 8L. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001030100194 20010301 00194 NM 2001 3 1 USAA010100 1 20010130 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 395US 43156 23317 CLT - FOUND SKIN CRACKED 3 INCHES, STATION 727D PLUS 3, STRINGER 23R. INSTALLED DOUBLER PER EA 69060. (M) 2 L 7 2 4F RT A16WE 2001030100195 20010301 00195 NM 2001 3 1 USAA010073 1 20010129 A 5320 TIE CLIP BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT - FOUND TIE CLIP CRACKED .5 INCH, STRINGER 10R, STATION 663. REPLACED WITH NEW TIE CLIP PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001030100196 20010301 00196 NM 2001 3 1 USAA010072 1 20010129 A 5730 SKIN BOEING 737 7374B7 1384702 NM LT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 32258 24554 CLT - FOUND SKIN CRACKED .75 INCH, LOWER LEFT WING SURFACE PYLON AFT ENGINE MOUNT OUTBOARD WBL 198. REPAIRED PER EA 690 37. (M) 2 L 7 2 4F RT A16WE 2001030100197 20010301 00197 NM 2001 3 1 USAA010064 1 20010123 A 5320 GUSSET BOEING 737 7373B7 1384580 NM NLG WW CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 520AU 40659 23706 CLT - FOUND GUSSETT CRACKED 2 INCHES, BL 0, BS 259.5 NOSE LANDING GEAR W/W CEILING. REMOVED AND REPLACED GUSSETT PER SR M 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001030100198 20010301 00198 NM 2001 3 1 USAA010061 1 20010122 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 520AU 40660 23706 CLT - FOUND WEB BULKHEAD CRACKED .7 INCH, BS 178 BULKHEAD WEB LBL 5.7, WL 213. INSTALLED DOUBLER PER EA 68728 AND SRM 5 3-10-08. (M) 2 L 7 2 4F RT A16WE 2001030100199 20010301 00199 NM 2001 3 1 USAA010060 1 20010122 A 5414 SKIN BOEING 737 7374B7 1384702 NM NR 1 PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 448US 29402 24892 CLT - FOUND PYLON SKIN CRACKED .5 INCH, TOP OF NR 1 PYLON LOWER AFT CORNER PYLON PANEL 5727L. INSTALLED DOUBLER PER TR 54-30-07. (M) 2 L 7 2 4F RT A16WE 2001030100200 20010301 00200 NM 2001 3 1 USAA010056 1 20010122 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 32038 24556 CLT - FOUND FLOORBEAM CRACKED .5 INCH, STATIN 520, RBL 45 IN RADIUS UPPER CHORD/WEB. INSTALLED REPAIR PER SRM 53-00-51 FIG 201. (M) 2 L 7 2 4F RT A16WE 2001030100201 20010301 00201 NM 2001 3 1 USAA010055 1 20010122 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 32038 24556 CLT - FOUND CRACKS IN WEB, .5 INCH, .25 INCH AND 1 INCH, STATION 178 BETWEEN LBL 7 AND RBL 7, WL 188 AND WL 201. INSTAL LED DOUBLER PER SRM 53-10-08 FIG 211. (M) 2 L 7 2 4F RT A16WE 2001030100202 20010301 00202 NM 2001 3 1 USAA010042 1 20010115 A 5320 ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 520AU 40659 23706 CLT - FOUND ANGLE/WEB CRACKED .750 INCH, STRINGER 11R BS 294.5. FABRICATED AND INSTALLED WEB ANGLE PER SRM 51-0-02. (M ) 2 L 7 2 4F RT A16WE 2001030100203 20010301 00203 NM 2001 3 1 USAA010041 1 20010115 A 5313 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 520AU 40659 23706 CLT - FOUND STRINGER CRACKED .5 INCH, STRINGER 10L AT STATION 295.5. INSTALLED REPAIR DOUBLER PER SRM 51-70-11. (M) 2 L 7 2 4F RT A16WE 2001030100204 20010301 00204 NM 2001 3 1 USAA010040 1 20010115 A 5210 SKIN BOEING 737 7373B7 1384580 NM PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 520AU 40659 23706 CLT - FOUND DOOR SKIN CRACKED .250 INCH, INNER SKIN FORWARD ENTRY DOOR AFT LOWER EDGE. INSTALLED REPAIR DOUBLER PER EA 68819. (M) 2 L 7 2 4F RT A16WE 2001030100205 20010301 00205 NM 2001 3 1 USAA010039 1 20010115 A 5320 ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 520AU 40659 23706 CLT - FOUND ANGLE AT STRINGER CRACKED .25 INCH, STRINGER 13L FORWARD DOOR SPIGOT. REPAIRED PER 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001030100206 20010301 00206 NM 2001 3 1 USAA010038 1 20010115 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 32038 24556 CLT - FOUND FRAME CRACKED .500 INCH, BS 727B BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLE RPER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001030100207 20010301 00207 NM 2001 3 1 USAA010037 1 20010115 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 32038 24556 CLT - FOUND FRAME CRACKED .125 INCH, BS 500A BETWEEN STRINGER 8L AND 9L. REMOVED DAMAGE AND INSTALLED OVERSIZED HI-LOCK PER SRM 51-40-03. (M) 2 L 7 2 4F RT A16WE 2001030100208 20010301 00208 NM 2001 3 1 USAA010036 1 20010115 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 32038 24556 CLT - FOUND FRAME CRACKED .5 INCH, BS 480 BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001030100209 20010301 00209 NM 2001 3 1 USAA010035 1 20010115 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 32038 24556 CLT - FOUND FRAME CRACKED .250 INCH, BS 440, BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER PER TR 53-10-04. (M) 2 L 7 2 4F RT A16WE 2001030200085 20010302 00085 WP 2001 3 2 01FDEA00063 1 20010126 A 5320 BRACKET DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 309FE 48298 FUSELAGE COMPARTMENT ZONE 312 BS Y2092.880 CANT UPPER ANGLE BRACKET FOUND CRACKED. *S/D* ANGLE FAB AND REPLACED PER DR AWING AJC 7028. 2 L 7 3 4F RT A22WE 2001030200086 20010302 00086 WP 2001 3 2 01FDEA00064 1 20010126 A 5320 BRACKET DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 309FE 48298 AFT FUSELAGE COMPARTMENT ZONE 312 BS Y2122.881 CANT UPPER ANGLE BRACKET FOUND CRACKED. *S/D* ANGLE FAB AND REPLACED PE R DRAWING AJC 7372. 2 L 7 3 4F RT A22WE 2001030200087 20010302 00087 NM 2001 3 2 01FDEA00065 1 20010131 A 5320 AJC702817 CLIP DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 582FE 48420 AFT FUSELAGE COMPARTMENT ZONE 312 BS Y 2092 CANT, CROWN AREA, CLIP CRACKED. *S/D* REMOVED AND REPLACED CLIP PER SRM 51 -35-01 & 51-33-01 VOL II AND DWG AJC 7028. 2 L 7 3 4F RT A22WE 2001030200088 20010302 00088 NM 2001 3 2 01FDEA00066 1 20010131 A 5320 AJC702933 CLIP DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 582FE 48420 AFT FUSELAGE COMPARTMENT ZONE 312 BS Y 2060 CANT, CROWN AREA, TOP SIDE CHANNEL AND LWR SIDE CLIP FOUND CRACKED. *S/D* REMOVED AND REPLACED CHANNEL AND CLIP PER SRM 51-35-01 & 51-33-01 VOL II AND DWG AJC 7372 & AJC 7029. NEW CHANNEL HEAT TREAT CARRIED OUT PER DPS 7.00-01 AND HARDNESS RESULT HRB 83 AS PER DPS 1.05-3. 2 L 7 3 4F RT A22WE 2001030200089 20010302 00089 NM 2001 3 2 01FDEA00073 1 20010203 A 3220 CYLINDER BOEING 727 727233 138408A NM HYD TRANSFER FAILED A FDEA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 222FE 20933 NOSE GEAR FAILED TO EXTEND NORMALLY ON FIRST ATTEMPT. OK WHEN CYCLED UP TO DOWN- REPEAT WRITE-UP. *S/D* REMOVED AND R EPLACED NOSE GEAR HYDRAULIC TRANSFER CYLINDER AS PER MM 32-35-011-4. JACK AND LWR NOSE PER MM 07-11-000-2. ACCOMP EXT AND RETRACT PER 32-33-000-5, 32-61-001-5. CHECK OK. 2 L 7 3 4F RT A3WE 2001030200090 20010302 00090 NM 2001 3 2 01FDEA00074 1 20010202 A 5310 651634659 SHEAR TIE BOEING 727 727227 1384078 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 CORROSION C53-111-01-03 ON SHEAR TIE BS 1110, LBL 1, WL 145. *S/D* REMOVED AND REPLACED PER FEDEX SRM 51-10-6, 53-10-4 , 53-30-3 AND EA 7-5310-56295. 2 L 7 3 4F A3WE 2001030200091 20010302 00091 NM 2001 3 2 01FDEA00092 1 20010207 A 5311 FRAME BOEING 727 72725C 138400H NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DURING ROUTINE INSP, FWD LWR CARGO COMP, DOOR CUTOUT, FRAME CRACKED AT BS 580 AT RBL 60 NEAR FWD STOP FITTING. *S/D* R EMOVED PAIN, TREATED AND PRIMED AREA PER IAW BAC 727 SRM 51-10-2. HFEC IND NO CRACKS FOUND IAW B727 NDT MANUAL PART 6. 2 L 7 3 4F A3WE 2001030200092 20010302 00092 NM 2001 3 2 01FDEA00095 1 20010208 A 5754 SKIN BOEING 727 72725C 138400H NM NR 5 SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DURING ROUTINE INSP, RIGHT WING NR 5 SLAT OUTBOARD UP STOP PAD CUTOUT FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB P ER IAW BAC 727 SRM 51-40-2. 2 L 7 3 4F A3WE 2001030200093 20010302 00093 NM 2001 3 2 01FDEA00097 1 20010208 A 5320 BRACKET BOEING 727 72725C 138400H NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DURING ROUTINE INSP, ATTACH BRACKET BS 359, STR 8R FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-20-1 AND BAC 5602, 51-30-2. 2 L 7 3 4F A3WE 2001030200094 20010302 00094 SO 2001 3 2 SWIA972343 1 20010207 A 3260 PROXIMITY SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE MLG OUT OF ADJ A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 190SW 120050 ON CLIMBOUT AFTER TAKEOFF RED B-RIGHT GEAR LIGHT CAME ON. CYCLED GEAR PER QRH ON GEAR RETRACTION RT MAIN DID NOT FULLY COME UP. EXTENDED GEAR AND GOT GOOD 3 GREEN INDICATION. RETURNED TO SLC. REPLACED TIGHT GEAR UPLOCK B-SYSTEM PROXIMIT Y SWITCH IAW 32-61-01. ADJUSTED RIGHT MAIN LANDING GEAR ACTUATOR IAW 32-30-00. CYCLED GEAR SEVERAL TIMES, FOUND TO OPE RATE NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 2001030200095 20010302 00095 2001 3 2 SWIA972344 4 20010209 A 2220 DAMPER CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE NR 2 YAW FAILED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 905SW 7437 UNABLE TO ENGAGE YAW DAMPER NUMBER TWO PRIOR TO FLIGHT. POWERED AIRCRAFT DOWN AND BACK UP. CYCLED YAW DAMPER SEVERAL T IMES. BOTH YAW DAMPER ONE AND TWO OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2001030200096 20010302 00096 2001 3 2 SWIA972345 4 20010209 A 3425 FLIGHT DIR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 221SW 120290 CAPTAINS COURSE SELECTOR NEEDLE TURNS ON ITS OWN INFLIGHT. UNABLE TO SELECT AND RETAIN A COURSE. RETURNED TO FAT. REP LACED CAPTAINS HCP AND CAPTAINS COURSE SELECTOR. OPS CHECKS GOOD IAW MM 34-21-00. 2 L 7 2 4T 4 T RT A31SO E20NE 2001030200097 20010302 00097 EA 2001 3 2 SWIA972346 1 20010209 A 3260 VALVE CNDAIR CL600 CL6002B19 EA NLG SELECTOR FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 406SW 7030 LANDING GEAR (NOSE) WILL NOT RETRACT. RETURNED TO ABQ. REMOVED AND REPLACED NLG SELECTOR VALVE IAW CRJ MM 32-33-10. G EAR RETRACTION NORMAL, LEAK CHECKED GOOD. P/N ON: 750006000, S/N ON: 1551, S/N OFF: 1204. 2 L 7 2 4F RT A21EA 2001030200098 20010302 00098 SO 2001 3 2 SWIA972347 1 20010209 A 2750 HANDLE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS FAILED A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 189SW 120048 FLAP DISAGREEMENT AFTER TAKEOFF, WOULD NOT GO UP ABOVE 5 DEGREES TOTAL. OUTBOARD FLAP PAIR WOULD NOT GO ABOVE TWO LIGHT BARS ON FLAP PANEL. RETURNED TO SLC. REMOVED AND REPLACED FLAP SELECTOR HANDLE IAW MM 27-00-00. FAILED TEST FLIGHT. REMOVED AND REPLACED ALL FOUR ROLLERS ON BOTH OUTBOARD FLAPS. REMOVED AND REPLACED LEFT OUTBOARD FLAP ACTUATOR WITH SE RVICEABLE UNIT. OPS CHECKS GOOD. ACTUATOR P/N ON: 320300-1007, S/N ON: 0516, S/N OFF: 1093. 2 L 7 2 4T 4 T RT A31SO E20NE 2001030200099 20010302 00099 EA 2001 3 2 SWIA972348 1 20010209 A 7830 ACTUATOR CNDAIR CL600 CL6002B19 EA THRUST REVERSER MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 408SW 7055 ON TAKEOFF ROLL RIGHT REVERSER UNLOCKED AND EICAS MESSAGE DISPLAYED. ABORTED TAKEOFF. UNABLE TO DEPLOY OR STOW RIGHT R EVERSER. RIGHT THRUST REVERSER IS DEACTIVATED AND DEFERRED. CLEANED AND LUBRICATED THE 4 BALL SCREW ACTUATORS ON THE T HRUST REVERSER ASSEMBLY. OPERATED THE REVERSER SEVERAL TIMES WITH NO PROBLEMS NOTED. RIGHT REVERSER OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2001030200100 20010302 00100 SO 2001 3 2 SWIA972349 1 20010209 A 2750 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAP CONTAMINATED A SWIA O OTHER N FALSE WARNING CL CLIMB 1 NM 07 195SW 120127 FLAPS GET DISAGREEMENT WHEN RETRACTING FROM 15 DEGREES TO 0 DEGREES. CLEANED DEICE FLUID FROM BOTH OUTBOARD FLAP CONNEC TOR PLUGS. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001030200101 20010302 00101 SO 2001 3 2 SWIA972350 1 20010205 A 2612 FIRE LOOP EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE DAMAGED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 196CA 120196 RIGHT DET INOP ENGINE/WW LIGHT ILLUMINATED INFLIGHT. RETURNED TO LAX. INSTALLED SERVICEABLE ENGINE FIRE DETECTION LOOP ON RIGHT ENGINE IAW MM 26-11-00. OPS CHECKS GOOD. S/N ON: 92233, S/N OFF: 80052. 2 L 7 2 4T 4 T RT A31SO E20NE 2001030200102 20010302 00102 SO 2001 3 2 SWIA972351 1 20010206 A 3350 BATTERY EMB 120 EMB120RT SO PWA 118 PW118 NE CABIN DISCHARGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 196CA 120196 EMERGENCY LIGHTS WILL NOT STAY ON WHEN TURNED ON. REPLACED FORWARD EMERGENCY LIGHT BATTERY. OPS CHECKS GOOD. P/N ON: D366-04-00, S/N ON: 1213, S/N OFF: 349. 2 L 7 2 4T 4 T RT A31SO E20NE 2001030200103 20010302 00103 SO 2001 3 2 SWIA972352 1 20010210 A 7931 PRESSURE SWITCH EMB 120 EMB120RT SO PWA 118 PW118 NE ENGINE OIL MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 156CA 120156 OIL PRESSURE RED LIGHT ILLUMINATES AND ORAL WARNING OIL PRESSURE GAUGE FLUCTUATED BETWEEN 45-55. RETURNED TO LAX. REMO VED AND REPLACED LEFT ENGINE OIL PRESSURE SWITCH WITH SERVICEABLE SWITCH. PERFORMED ENGINE RUN OIL PRESSURE INDICATION WAS NORMAL WITH NO FLUCTUATION. OPS CHECKS GOOD. S/N ON: 535, S/N OFF: 0669. 2 L 7 2 4T 4 T RT A31SO E20NE 2001030200104 20010302 00104 WP 2001 3 2 TWAA0102601 1 20010207 A 3350 105606002 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 939AS 49657 DURING PREFLIGHT, FOUND EGRESS PATH MARKING SYSTEM LIGHTS INOP. REPLACED BATTERYS. OP 00-05 01-31-01 STL. 2 L 7 2 4F RT A6WE 2001030200105 20010302 00105 NM 2001 3 2 TWAA0102602 1 20010208 A 3350 CONNECTOR BOEING 767 7673Q8 NM CABIN LOOSE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 634TW 28132 DURING MAINTENANCE, FOUND EGRESS LIGHTING LT SIDE ROW 16-18, AND RT SIDE 24-27 INOP. RESECURED LOOSE CONECTION, OPS CHE CK. OP 00 11 12-25-00 JFT. 2 L 7 2 4F RT A1NM 2001030200106 20010302 00106 NM 2001 3 2 TWAA0102603 1 20010208 A 3350 LIGHT BOEING 767 7673Q8 NM ESCAPE SLIDE INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 634TW 28132 DURING MAINTENANCE FOUND L4 DOOR EMERGENCY SLIDE LIGHT INOP. RELAMPED LIGHT. OP 00 11 12-25-00 JFK. 2 L 7 2 4F RT A1NM 2001030200107 20010302 00107 NM 2001 3 2 QXEA0100100 1 20010204 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE MISDRILLED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 814PH 43 PDX- LEFT HAND INBOARD NR 4 SEAT TRACK SUPPORT ANGLE AT STATION 355.950 AND 354.250 HAS A 10:32 FASTENER HOLE THAT HAS B EEN MISDRILLED. REPAIRED IAW HORIZON AIR EA 9-53-596. 2 H 7 2 4T RT A13NM 2001030200108 20010302 00108 NM 2001 3 2 QXEA0100101 1 20010131 A 5753 FLAP TRACK DHAV DHC8 DHC8102 2809003 NM NR 1 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 814PH 43 PDX- RIGHT HAND INBOARD FLAP, NR 1 INBOARD UPPER TRACK HAS DIVETS IN TOP AND BOTTOM 10 INCHES AFT OF FORWARD END. REPAI RED IAW DHC-8 RD 8-57-985. 2 H 7 2 4T RT A13NM 2001030200109 20010302 00109 NM 2001 3 2 QXEA0100102 1 20010131 A 5753 FLAP TRACK DHAV DHC8 DHC8102 2809003 NM NR 2 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 814PH 43 PDX- RIGHT HAND INBOARD FLAP, NR 2 OUTBOARD FLAP TRACK UPPER TRACK HAS A DIVET 10 INCHES AFT OF FORWARD END. REPAIRED I AW DHC-8 RD 8-57-986. 2 H 7 2 4T RT A13NM 2001030200110 20010302 00110 NM 2001 3 2 HNAA0100012 1 20010211 A 3350 6013211 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 938HA 9291 216 152 FIRST TWO RED EMERGENCY FLOOR LIGHTS INOP. REPLACED EMERGENCY LIGHT BATTERY PACK 3352-P2. 2 H 7 2 4T RT A13NM 2001030200111 20010302 00111 NM 2001 3 2 DHL2001712500 1 20010201 A 5311 FRAME BOEING 727 72729 1384007 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 C-CHECK - COMPARTMENT FRAME SHOWS CORROSION AT STA 110.000, STR 26 LT. CUT OUT DAMAGED AREA AT STA 110.000 STR 26L, AND FABRICATED FILLER AND CHANNEL (ALCLAD 707S.T6.0.063 INCH) IAW SRM 53-10-4 PAGE 3. CLEANED, TREATED AND PRIMED IAW SRM 51-10-2 PAGE 1 & 2. INSTALLED FILLER AND CHANNEL IAW SRM 53-10-4 PAGE 3. 2 L 7 3 4F A3WE 2001030200112 20010302 00112 NM 2001 3 2 01FDEA00048 1 20010130 A 5313 BAC1498141 STRINGER BOEING 727 727227 1384078 NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 STRINGER 6R IS DAMAGED IN RADIUS, BS 420 - 440. *S/D* REMOVED AND REPLACED STR 6R AND BEAR STRAP PER IAW FEDEX SRM 53- 10-3, 53-30-3 AND EA 7-5310-56263. 2 L 7 3 4F A3WE 2001030500020 20010305 00020 EU 2001 3 5 CA010111002 1 20010103 A 2133 9599091151 CHECK VALVE PILATS 521311200 PILATS PC12 PC1245 EU VACUUM LINE FROZEN W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) WHEN AIRCRAFT WAS STARTED THE CABIN STARTED TO PRESSURIZE. ICE HAD FROZEN AND NOT ALLOWED THE SAFETY OR OUTFLOW VA LVE TO COME OFF IT SEAT, THUS THE AIRCRAFT PRESSURIZED ON THE GROUND. LINE AND CHECK VALVE CLEARED OF ICE AND WATER AND AIRCRAFT RETURNED TO SERVICE. THIS IS THE SECOND OCCURRENCE OF THIS SORT ON THIS TYPE OF AIRCRAFT THIS WINTER. 1 L 7 1 3T RT A78EU 2001030500025 20010305 00025 EU 2001 3 5 CA010111007 1 20010103 A 5530 5553012211 PLATE PILATS 5535212049 PILATS PC12 PC1245 EU STABILIZER WORN W K NONE O OTHER IN INSP/MAINT 1 CA 1205 (CAN) ON ANNUAL INSPECTION EXCESSIVE WEAR WAS NOTICED BETWEEN THE STAP PART NR 555.30.12.211 AND PLATE PART NR 553.52.12 .074. THESE PARTS ENGAGE AND PREVENT FLUTTER OF THE FAIRING. THE STRAP IS RIVETED TO THE TOP OF REAR SPAR ON THE VERTICA L STABILIZER. THE PLATE IS ATTACHED TO FAIRING PART NR 553.52.12.049. THE STRAP AND PLATE WERE REPLACED WITH NEW PARTS. ALIGNMENT WAS CHECKED AS THIS IS A NOTED PROBLEM THAT HAS CAUSED SKIN CRACKING IN THE VERTICAL STABILIZER. DUE TO POOR D ESIGN THESE PARTS WILL HAVE TO BE REPLACED ANNUALLY. 1 L 7 1 3T RT A78EU 2001030500095 20010305 00095 2001 3 5 CA010105009 4 20010105 A 2210 102EH2BF PROBE AIRBUS 310 A310304 EU GE CF6 CF680C2* GL TAT READS HIGH W A UNSCHED LANDING E R J VIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 CA 1853 1853 (CAN) ON CLIMB, AIRCRAFT BEGAN TO GIVE ERRONEOUS COMMANDS TO PILOTS FLIGHT DIRECTOR, FLIGHT DIRECTOR THEN FAILED, AUTO T HROTTLE MOVED TO IDLE WITHOUT COMMAND. AIRCRAFT RETURNED TO BASE. ON LANDING ALL INDICATIONS RETURNED TO NORMAL. FAULT C ODE INDICATED NR 1 FLIGHT AUGMENTATION COMPUTER HAD FAILED DURING PREVIOUS FLIGHT. NR 1 FAC REPLACED AS PER AMM 22-26-34 . DURING COCKPIT CHECK, NR 1 TOTAL AIR TEMP WAS INDICATING PLUS 50 DEGREES, NR 1 TAT PROBE REPLACED AS PER AMM 34-11-18. AIRCRAFT HAS FLOWN WITHOUT FURTHER PROBLEMS. 2 L 7 2 4F 4 F RT A35EU E23EA 2001030500102 20010305 00102 NM 2001 3 5 CA010108013 1 20010104 A 3320 BR63031023 LIGHT DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE CABIN OVERHEATED W K NONE M OVER TEMP IN INSP/MAINT 1 CA (CAN) DURING ROUTINE MAINTENANCE TO REPLACE AN INOPERATIVE SIDEWALL LIGHT, THE FORWARD RECEPTACLE SHOWED SIGNS OF OVERHE ATING. THE COMPLETE LIGHT FIXTURE WAS REPLACED. FURTHER INSPECTION OF THE FIXTURE REVEALED THAT BRUCE INDUSTRIES SL-BC5- 0618-901-33-01 HAD BEEN COMPLIED WITH, AND THE SPRINGS INTRODUCED BY THE SL WERE FOUND TO HAVE MIGRATED OUT OF POSITION AND BECOME INEFFECTIVE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001030500103 20010305 00103 NM 2001 3 5 CA010108014 1 20010105 A 2910 DSC252B40124 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM LEAKING W O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 CA (CAN) THE FLIGHT CREW REPORTED LOW FLUID LEVEL IN NR 2 HYDRAULIC SYSTEM DURING DESCENT. THEY LANDED UNEVENTFULLY. MAINTE NANCE INVESTIGATION RESULTED IN REPLACEMENT OF THE NOSE LANDING GEAR DRAG STRUT ACTUATOR FLEX LINE WHICH WAS LEAKING AT THE BASE OF THE STRAIGHT END SWAGE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001030500116 20010305 00116 WP 2001 3 5 01FDEA00056 1 20010126 A 5320 BRACKET DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 309FE 48298 AFT FUSELAGE COMPARTMENT ZONE 312 BS Y2046.000 CANT UPPER ANGLE BRACKET FOUND CRACKED. *S/D* ANGLE FAB AND REPLACED PE R DRAWING AJC 7021. 2 L 7 3 4F RT A22WE 2001030500117 20010305 00117 WP 2001 3 5 DHL2001802002 1 20010205 A 2612 CONNECTOR DOUG DC8 DC873F 302199F WP NR 2 ENGINE SHORTED A DHLA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 01 802DH 46076 DURING CRUISE, NR 2 ENGINE FIRE WARNING ACTIVATED. PERFORMED ENG FIRE CHECKLIST, FIRE LEVER LIGHT REMAINED ILLUMINATED AND FIRE BELL SOUNDED INTERMITTENTLY ON A LOOP. SWITCHED TO B-LOOP AND EXPERIENCED NO FURTHER FIRE WARNINGS. B-LOOP SH ORT TESTED OK. ENGINE WINDMILLED 57 MINUTES AT 5 PSI. FOUND NR 2 ENG A-LOOP CORE CONNECTOR SHORTED. REPLACED CONNECTO R P1-7036, CHECKS GOOD PER MM 26-10-0. 2 L 7 4 4F RT 4A25 2001030500118 20010305 00118 NM 2001 3 5 UPS01634863 1 20010206 A 2612 FIRE LOOP BOEING 767 76734AF 1385212 NM LT ENGINE INTERMITTENT A IPXA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 305UP 27243 INSPECTION TYPE:N/A, ON TAXI OUT RECEIVED EICAS STATUS MSG OF L ENG FIRE LP 2 INTERMITTENTLY WITH THROTTLE LEVER MOVEMEN T. *S/D* CLEARED M208730. NR 2 FIRE WARNING TESTS OK. NO MSGS, 2 FLTS. 2 L 7 2 4F RT A1NM 2001030500119 20010305 00119 NM 2001 3 5 UPS01234832 1 20010131 A 3350 9621033 LIGHT BOEING 727 72725C 138400H NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:N/A, EMERGENCY INTERIOR OVERWING LIGHT INOP ACFT IN CARGO MODE. *S.D* REMOVED AND REPLACED BATTERY, OP S GOOD. THIS CLEARS M208478. 2 L 7 3 4F A3WE 2001030500120 20010305 00120 EU 2001 3 5 DHL2001366010 1 20010208 A 2760 ROD AIRBUS 300 A300B4203 3930306 EU SPOILER PICKOFF FAILED A DHLA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 366DH 249 ON FLT CONTROL CHECK, ASYMMETRIC SPOILER INDICATION. DEFERRED SPOILER INDICATION, REPLACED RT SPOILER PICKOFF ROD. OPS CHECK GOOD PER MM 27-65-00. 2 L 7 2 4F RT A35EU 2001030500121 20010305 00121 NM 2001 3 5 UPS01234909 1 20010207 A 5730 SKIN BOEING 727 72725C 138400H NM LT WING DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:W/E LT WING UPPER T/E FIXED WING PANEL FWD OF GROUND SPOILERS, UPPER SKIN DELAMINATED (P/N 65-21655-475) REF IPC 57-30-00 FIG 10 ITEM 735 FOR LOCATION. REMOVED ICE AND WATER, PERFORMED A DETAILED INSPECTION (SRM 51-00-6) US ING NDT TAP TEST. PANEL WAS DETERMINED TO BE NOT DELAMINATED. 2 L 7 3 4F A3WE 2001030500122 20010305 00122 CE 2001 3 5 GLBA2001028 1 20010205 A 2822 1143890425 PUMP BEECH 1900 1900D 1154162 CE NR 2 ENGINE LEAKING A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 192GL 8491 276 UE192 RETURN TO BLOCK - LEFT LP FUEL PUMP FAILED. REMOVED AND REPLACED FUEL PUMP, OPS CHECKED GOOD. 2 L 7 2 4T RT A24CE 2001030500123 20010305 00123 EU 2001 3 5 DHL2001362004 1 20010209 A 2710 SERVO AIRBUS 300 A300B4103 3930104 EU AILERON CONTROL FAILED A DHLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 362DH 84 UPON NR 2 ENGINE START, YELLOW SYSTEM JAM SERVO LIGHT ILLUMINATED. T/S TO LT LOW SPEED AILERON DISCONNECT SAME AND DEFE RRED PEN. 2 L 7 2 4F RT A35EU 2001030500124 20010305 00124 NM 2001 3 5 UPS01434947 1 20010210 A 2612 DETECTOR BOEING 747 747121 1384871 NM FIRE WARNING FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:IN PRE DEPARTURE - FIRE WARNING TEST D/N RESET. REMOVED AND REPLACED FIRE WARNING CARD A-4. ALL OP CKS NORMAL. OK FOR SERVICE. 2 L 7 4 4F A20WE 2001030500125 20010305 00125 WP 2001 3 5 UPS01834948 1 20010209 A 5230 FRAME DOUG DC8 DC873F 302199F WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:IN P32 DOOR UPPER AFT RADIUS FRAME CRACK. *S/D* REMOVED AND REPLACED NR 32 PIT DOOR ASSY PER DC8-MM 52 -32-01, OPS CHK AND LEAK CK GOOD. 2 L 7 4 4F RT 4A25 2001030500126 20010305 00126 NM 2001 3 5 01FDEA00110 1 20010211 A 2610 PRESSURE SWITCH BOEING 727 7272D4 138407U NM ENGINE FALSE INDICATION A FDEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 25 287FE 21849 ON T/O, GLARESHIELD ENG FAIL AND MASTER WARNING LIGHT WITH BELL ILLUM. REMOVED AND REPLACED ALL 3 AUTO PACK TRIP SYS PR ESSURE SWITCHES PER B727-200 MM 21-11-011-4. REPLACED F/O''S FIRE BELL RESET LIGHT ASSY PER SMP. 2 L 7 3 4F A3WE 2001030500127 20010305 00127 NM 2001 3 5 DHL2001712501 1 20010207 A 5330 SKIN BOEING 727 72729 1384007 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 SKIN EXTERIOR HAS 0.250 INCH CRACK AT STA 1102, STR 4L. CUT AFFECTED AREA IAW SRM 53-30-3, PAGE 24. FABRICATED FILLER WITH ALCLAD 2024 T3 0.040 INCH, SRM 53-30-3, PAGE 24. FABRICATED DOUBLER WITH ALCLAD 2024 T3 0.063 INCH IAW SRM 53-30-3 PAGE 24. TREATED AND PRIMED IAW SRM 51-10-2, PAGE 1 AND 2. INSTALLED FILLER AND DOUBLER IAW SRM 53-30-3, PAGE 24. 2 L 7 3 4F A3WE 2001030500129 20010305 00129 EU 2001 3 5 01FDEA00111 1 20010210 A 3210 LANDING GEAR AIRBUS 300 A300F4605R 3930327 EU MAINS FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 667FE 771 LANDING GEAR WOULD NOT RETRACT AFT T/O FROM MCI EITHER IN POS DET SYS 1 OR 2. 2 L 7 2 4F RT A35EU 2001030500130 20010305 00130 NM 2001 3 5 MJYA200102001 1 20010210 A 2781 189915 PROXIMITY SWITCH BOEING 737 737230C 1384472 NM NR 3 LE FLAP OUT OF ADJ A MJYA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 767TW 1 1 20258 WITH FLAPS SELECTED TO FLAP 1, L/E FLAP LIGHT REMAINED INTRANSIT ON FWD INSTRUMENT PANEL. 2 L 7 2 4F A16WE 2001030500131 20010305 00131 EA 2001 3 5 JBXA000243 1 20010211 A 2910 AE2460010H0264 HYDRAULIC LINE CNDAIR CL600 CL6002B19 EA TAIL BAY CRACKED A JBXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 05 575ML 5675 7256 NR 1 HYDRAULIC SYSTEM INDICATED ZERO PERCENT AT FL290 EN ROUTE TO BUF. RAN QRH AND DIVERTED TO PHL. FOUND PRESSURE LIN E FROM EDP NR 1 TO PRESSURE FILTER CRACKED AT PRESSURE FILTER CONNECTION. REMOVED AND REPLACED PRESSURE LINE, REMOVED A ND REPLACED EDP NR 1, REMOVED AND REPLACED PRESSURE CASE DRAIN, RETURN FILTERS, SERVICED HYRAULIC SYSTEM NR 1. LEAK CHE CK AND OPERATIONAL CHECK OF SYSTEM NR 1 IAW CRJ AMM 29-11-01. LEAK CHECK AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2001030500132 20010305 00132 EA 2001 3 5 COMA0160222 1 20010210 A 5551 600230681 BUSHING CNDAIR CL600 CL6002B19 EA HORIZONTAL STAB WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 17981 7022 LEFT OUTBOARD HORIZONTAL STAB PIVOT BUSHING IS SCORED. REMOVED SCORED BUSHING. VERIFIED LUG BORE OUT OF LIMITS AT 1.70 18. REAMED LUG TO 1ST OVERSIZE 1.7160 AND PERFORMED DYE PENETRANT INSPECTION IAW REO 601R-55-11-022 REV A. INSTALLED 1 ST OVERSIZED BUSHING 601R-55-11-022-1 IAW CRJ AMM 20-26-00-910-803. REAMED BUSHING TO 1.5000 IAW DWG 600-23050. 2 L 7 2 4F RT A21EA 2001030500133 20010305 00133 EA 2001 3 5 COMA0160223 1 20010209 A 5320 601R52110081 ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 978CA 7158 PASSENGER DOOR SEAL STRIKER REPAIR AT FS 310 IS DAMAGED. REPAIRED PREVIOUS REPAIR TO PASSENGER DOOR SEAL STRIKER AT FS 310 IAW CRJ REO 601R-52-11-008 REV B REPAIR A ITEM 4. 2 L 7 2 4F RT A21EA 2001030500134 20010305 00134 2001 3 5 COMA0160224 4 20010209 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 966CA 7132 STALL FAIL CAUTION MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001030500135 20010305 00135 WP 2001 3 5 MWEA010151 1 20010213 A 5320 9911839244 ANGLE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 CRACK AT STATION 1121 AT LONGERON 17 RIGHT. DRILLED AND INSTALLED REPAIR ANGLES. 2 L 7 2 4F A6WE 2001030500136 20010305 00136 WP 2001 3 5 MWEA010152 1 20010213 A 5321 995791819 FLOOR PANEL DOUG DC9 DC932 3022066 WP CABIN CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 FLOOR PANEL E-6 IS CRACKED ON AFT OUTBOARD CORNER. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001030500137 20010305 00137 WP 2001 3 5 MWEA010153 1 20010213 A 5313 591022839 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 CORROSION ON LONGERON 12 LEFT AT STATION 1104. FABRICATED AND INSTALLED LONGERON AND ANGLE. 2 L 7 2 4F A6WE 2001030500138 20010305 00138 WP 2001 3 5 MWEA010154 1 20010213 A 5410 995819310 WEB DOUG DC9 DC932 3022066 WP RT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 VERTICAL WEB CRACKED IN RIGHT PYLON OUTBOARD OF 13TH STRINGER. BLEED NUT ACCESSIBLE THROUGH PANEL 8204A. FABRICATED AN D INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F A6WE 2001030500139 20010305 00139 NM 2001 3 5 01FDEA00116 1 20010213 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DURING ROUTINE INSP THE AFT CARGO FLOORBEAM AT BS 1130, STR 17R FOUND CORRODED. *S/D* REMOVED, REPLACED AND FAB DAMAGE D AREA PER IAW FEDEX EA 7-5310-56274. 2 L 7 3 4F A3WE 2001030500140 20010305 00140 NM 2001 3 5 01FDEA00119 1 20010210 A 2550 BLOCK DOUG MD11 MD11 3023602 NM CARGO BAY CRUSHED A FDEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 25 596FE 48554 AFT P-F CONV DURING T/O CREW NOTED A LEVEL ONE AC TIE 1 OFF ALERT. FOUND A BLOCK OF THE CONCRETE BALLAST HAD BROKEN FRE E OF AN LD3 CONTAINER IN POS 1 LEFT IN THE FWD LWR CARGO COMP. THE BLOCK ROLLED THRU THE FWD CARGO COMP AND PASS THRU B ULKHEAD AND LODGED IN THE NR 1 EPC BAY. 2 L 7 3 4F RT A22WE 2001030500141 20010305 00141 EU 2001 3 5 DHL2001367512 1 20010203 A 5230 A5397822420000 SEAL AIRBUS 300 A300B4203 3930306 EU CARGO DOOR DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH MSN265 C-CHECK, AFT CARGO BAY DOOR FRAME 63 UPPER SEALING STRIP BADLY DAMAGED. SEALING STRIP REPLACED IAW AMM 20-00-00. NO FU RTHER DAMAGE. 2 L 7 2 4F RT A35EU 2001030500142 20010305 00142 EU 2001 3 5 DHL2001367513 1 20010207 A 3213 A2551305600151 GUIDE AIRBUS 300 A300B4203 3930306 EU LT MLG CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH MSN265 C CHECK, LT FWD MLG GUIDE STRUT CRACKED IN 2 PLACES, BOTH 3 INCHES NR 80866. CRACKED BEYOND MM LIMITS. REPLACED GUIDE STRUT IAW SRM 51-30-10. 2 L 7 2 4F RT A35EU 2001030500143 20010305 00143 EU 2001 3 5 DHL2001367514 1 20010207 A 5720 STIFFENER AIRBUS 300 A300B4203 3930306 EU ACCESS DOOR DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH MSN265 C-CHECK- CENTER TANK: IMPACT DAMAGE ON UPPER LATERAL STIFFENER AT FR 46 FWD OF LT ACCESS NR 80972. BLENDED OUT DAMAGE I AW SRM 51-40-01, DAMAGED ASSESSED AT 0.006 INCH AREA REPROTECTED IAW SRM 51-40-12. 2 L 7 2 4F RT A35EU 2001030500144 20010305 00144 EU 2001 3 5 DHL2001367515 1 20010207 A 5720 STIFFENER AIRBUS 300 A300B4203 3930306 EU CENTER TANK DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH MSN265 C-CHECK- CENTER TANK IMPACT DAMAGE ON TOP FLANGE OF LATERAL STIFFENER FWD OF TANK OVERFLOW VALVE FR 45R. DAMAGE BLENDED OUT, 0.006 INCH ALL AREAS REPROTECTED IAW SRM 51-40-12. 2 L 7 2 4F RT A35EU 2001030500145 20010305 00145 EU 2001 3 5 DHL2001367516 1 20010206 A 5210 FS218135620000 SEAL AIRBUS 300 A300B4203 3930306 EU PAX DOOR SPLIT A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH MSN265 C-CHECK- L1 DOOR SEAL SPLIT NR 78791. REPLACED DOOR SEAL IAW AMM 52-10-18. 2 L 7 2 4F RT A35EU 2001030500146 20010305 00146 EU 2001 3 5 DHL2001367517 1 20010207 A 5230 A2557328800000 BRACKET AIRBUS 300 A300B4203 3930306 EU DOOR ACTUATOR SHEARED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH MSN265 C-CHECK- AFT CARGO DOOR ACTUATOR TO PANEL BRACKET (OUTBOARD) SHEARED. REPLACED AFT CARGO DOOR O/B ACT TO PANEL BRACKET IAQ AMM 25-52-11. 2 L 7 2 4F RT A35EU 2001030500147 20010305 00147 GL 2001 3 5 DHL2001367518 2 20010208 A 8510 BLADE AIRBUS 300 A300B4203 3930306 EU GE CF6 CF6* 30020 GL NR 2 ENGINE FAN NICKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH MSN265 528369 C CHECK, NR 2 ENGINE FAN ROTOR BLADES FOUND TO BE NICKED AND BURRED. ALL BLADES BLENDED PER GE STANDARD PRACTICES MANUA L 70-42-00 AND AMM 72-21-00. 2 L 7 2 4F 4 F RT A35EU E23EA 2001030500148 20010305 00148 EU 2001 3 5 DHL2001367519 1 20010212 A 5610 SPSA340141A WINDSHIELD AIRBUS 300 A300B4203 3930306 EU COCKPIT SCRATCHED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH MSN265 C CHECK, COPILOT WINDSCREEN SCRATCHED INNER PLY. REPLACED COPILOTS WINDSCREEN IAW AMM 56-11-11, OPS CHECK GOOD. 2 L 7 2 4F RT A35EU 2001030500149 20010305 00149 NM 2001 3 5 DHL2001712502 1 20010202 A 5754 SKIN BOEING 727 72729 1384007 NM LE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 C-CHECK, FORE FLAP CRACKED 2.0 INCH AT WBL 440. PERFORMED STOP DRILL IAW SRM 57-50-4, FIG 1. FABRICATED DOUBLER (ALCLA D 2024, T3, 0.050 INCH) IAW 57-50-4, FIG 1. CLEANED, TREATED AND PRIMED IAW 51-10-2, PAGE 1 AND 2. INSTALLED DOUBLER I AW SRM 57-50-4, FIG 4. 2 L 7 3 4F A3WE 2001030500150 20010305 00150 EA 2001 3 5 COMA0160226 1 20010212 A 5320 ANGLE CNDAIR CL600 CL6002B19 EA DOOR SEAL DAMAGED A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 977CA 7157 DAMAGE TO PASSENGER DOOR SEAL STRIKER AT FS 310.00 (AT PREVIOUS REPAIR). PREVIOUS REPAIR WAS REMOVED AND NEW REPAIR WA S CARRIED OUT IAW BOMBARDIER REO 601R-52-11-008. REPAIR A, SHEETS 2-3. 2 L 7 2 4F RT A21EA 2001030500151 20010305 00151 WP 2001 3 5 AT0100078 1 20010202 A 5330 TRIPLER DOUG DC9 DC932 3022066 WP AIRSTAIR CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FOUND FORWARD AIRSTAIR CUT OUT DOUBLER CRACKED IN AFT LOWER CORNER. INSTALLED TRIPLER, FILLER, INTERCOSTAL, AND CHANNEL IAW REO L00360. 2 L 7 2 4F A6WE 2001030500157 20010305 00157 NM 2001 3 5 UPS01234964 1 20010206 A 3350 LIGHT BOEING 727 72762C 138402C NM COCKPIT FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 912UP 19244 INSPECTION TYPE:IN COCKPIT EMERGENCY EXIT LIGHT INOP W/OP CHECKED IN FLIGHT. RELAMPED, OPS CHECKS GOOD. 2 L 7 3 4F A3WE 2001030500158 20010305 00158 NM 2001 3 5 UPS01234968 1 20010213 A 2612 FIRE LOOP BOEING 727 72725C 138400H NM NR 3 ENGINE INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 933UP 19857 INSPECTION TYPE:IN ENG NR 3 A-LOOP WILL NOT TEST. *S/D* FOUND CONNECTOR D354J CONTAMINATED WITH DIRT AND MOISTURE. CL EANED SAME THOROUGHLY. TESTED NORMAL. M209166 CLEARED. 2 L 7 3 4F A3WE 2001030500159 20010305 00159 NM 2001 3 5 UPS01434939 1 20010105 A 5210 66138736 STOP BOEING 747 747123F NM PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C MAIN ENTRY DOOR NR 2 LT SIDE LOWER FWD STOP CRACKED. DOOR 2 LT CRACK IN FWD LOWER CORNER REPAIRED I AW SRM 52-10-02 STOP FITTING REPLACED. 2 L 7 4 4F A20WE 2001030500160 20010305 00160 NM 2001 3 5 UPS01434940 1 20010105 A 5210 DOUBLER BOEING 747 747123F NM PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, DOOR 1 RT BOTTOM FWD L/E CORNER FOUND CRACKED. BOTTOM FWD CORNER CRACK REPAIRED IAW SRM 52-10-02, R EPAIR PARTS FABRICATED IAW BAC 5300 AND VERTICAL FRAME REPAIRED IAW 52-10-02 FIG 10. CRACK NDT INSPECTED TO MARK CRACK E NDS. ALSO, BLIND FASTNERS ON PREVIOUS REPAIR REPLACED WITH SOLIDS. 2 L 7 4 4F A20WE 2001030500161 20010305 00161 NM 2001 3 5 UPS01434941 1 20010105 A 5210 DOUBLER BOEING 747 747123F NM PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C DOOR 1 LT BOTTOM FWD L/E CORNER OF DOOR CRACKED. DOOR 1 LT FWD LWR CORNER CRACK REPAIRED IAW SRM 52- 10-02. NDT ACCOMPLISHED TO CONFIRM CRACK ENDS IAW SRM 52-10-02 FIG 10. CRACK REPAIRS IN VERTICAL FRAME. 2 L 7 4 4F A20WE 2001030500162 20010305 00162 NM 2001 3 5 UPS01434942 1 20010105 A 5210 DOUBLER BOEING 747 747123F NM PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C DOOR 4 RT BOTTOM FWD CORNER OF DOOR FOUND CRACKED. BOTTOM FWD CORNER OF DOOR CRACK REPAIRED IAW SRM 5 2-10-02 FIG 10. DOOR SKIN REPAIRED AT HINGE CUTOUTS PREVIOUS REPAIRS HAD BLIND FASTENERS. BLIND FASTENERS REMOVED AND SOLIDS INSTALLED IAW SRM 51-30 -02. FASTENERS MS 2024D6. REPAIR PARTS FABRICATED IAW BAC 53 00. 2 L 7 4 4F A20WE 2001030500163 20010305 00163 NM 2001 3 5 UPS01434943 1 20010105 A 5210 DOUBLER BOEING 747 747123F NM PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C DOOR 4 LT BOTTOM AFT L/E CORNER FOUND CRACKED. DOOR 4 FWD AND AFT LOWER CORNERS CRACK REPAIRED IAW SR M 52-10-02. TWO REPAIR PIECES CAD PLATED AND INSTALLED, CRACK ENDS CONFIRMED WITH NDT HFEC D6-7170 PT 6 CH 51-00-00 FIG 4. 2 L 7 4 4F A20WE 2001030500164 20010305 00164 NM 2001 3 5 UPS01434944 1 20010105 A 5210 DOUBLER BOEING 747 747123F NM PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, DOOR 4 LT BOTTOM L/E CORNER OF DOOR FOUND CRACKED. DOOR 4 LT FWD AND AFT LOWER CORNERS CRACKED, REPA IRED IAW SRM 52-10-02. ENDS OF CRACKS MARKED USING NDT ON HORZ BEAMS IAW SRM 52-10-02 FIG 10. CRACKS FOUND IN VERTICA L ANGLES. 2 L 7 4 4F A20WE 2001030500165 20010305 00165 NM 2001 3 5 UPS01434945 1 20010105 A 5210 DOUBLER BOEING 747 747123F NM PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, DOOR 5 RT BOTTOM FWD CORNER OF DOOR FOUND CRACKED. REPAIR PLATE FABRICATED AND CAD PLATED. REPAIRED IAW SRM 52-10-00. ENDS OF CRACKS MARKED USING NDT HFEC NDTM PT 6 51-00-00 FIG 23. 2 L 7 4 4F A20WE 2001030500166 20010305 00166 NM 2001 3 5 UPS01434950 1 20010105 A 5210 DOUBLER BOEING 747 747123F NM PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, MAIN CABIN DOOR 2 RT BOTTOM FWD CORNER CRACKED. BOTTOM FWD CORNER REPAIRED VERTICAL FRAME IAW SRM 5 2-10-02, USING AI SI301X0.050 2024T3. ALSO, REPLACED PULLED RIVETS. NDT CARRIED OUT ON CRACKS TO DETERMINE ENDS IAW B7 47 NDTM D6-7170 PART 6 51-00-00 FIG 23. 2 L 7 4 4F A20WE 2001030500167 20010305 00167 NM 2001 3 5 UPS01434951 1 20010107 A 5210 65B0834410 FITTING BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, NR 3 ENTRY DOOR BS 1265 RT SIDE HINGE FITTING CRACKED. HINGE FITTING REPLACED IAW SRM 51-30-02. 2 L 7 4 4F A20WE 2001030500168 20010305 00168 NM 2001 3 5 UPS01434952 1 20010110 A 5350 65B0271255 STRAP BOEING 747 747123F NM FUSELAGE WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, WEAR AT FUSE STA 2568 WHERE FRONT END OF APU DOORS CONTACT FUSELAGE STRAP WORN. REPLACED STRAP WITH NEW PART IAW SRM & QUERY NOTE 12/01. 2 L 7 4 4F A20WE 2001030500169 20010305 00169 NM 2001 3 5 UPS01434953 1 20010108 A 5320 155PHX071 FLOOR SUPPORT BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, MAIN DECK CORROSION ON UPPER CHORD OF BS 400 BULKHEAD RBL 15 TO 46. UPPER CHORD AT BS 400 RBL 15-46 REPAIRED IAW QUERY NOTE 6/01, ANGLES FABRICATED. HEAT TREATED 15-5 PH X.071 AND INSTALLED. 2 L 7 4 4F A20WE 2001030500170 20010305 00170 NM 2001 3 5 UPS01434955 1 20010115 A 5753 65B020482 CASTING BOEING 747 747123F NM RT TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, RIGHT I/B MIDFLAP O/B DEFLECTOR ROLLER SUPPORT CASTING CRACKED. CRACKED CASTING REPLACED IAW SRM 51- 30-02. 2 L 7 4 4F A20WE 2001030500171 20010305 00171 NM 2001 3 5 UPS01434959 1 20010111 A 5310 BAC1505100849 CREASE BEAM BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, MAIN DECK T-CHORD OF LOWER CREASE BEAM WEB IS CRACKED STR 26 AT BS 1241 LT. DAMAGED T-CHORD REMOVED AND NEW SECTION FITTED IAW SRM 51-30-02 NDT USED TO MARK CRACK ENDS. 2 L 7 4 4F A20WE 2001030500172 20010305 00172 WP 2001 3 5 UPS01834946 1 20010208 A 5330 SKIN DOUG DC8 DC871F 302199D WP PAX DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:L/S R-1 SERVICE DOOR HAS A 1/8 INCH CRACK IN THE LOWER AFT RADIUS OF THE FUSELAGE SKIN. ROUTED OUT CRAC KED SKIN, VERIFIED NO CRACK REMAINING IAW DC8 SRM NDT SRM 06-10-11-001. FABBED DOUBLERS AND FILLERS, ALODINED, PRIMED A ND INSTALLED IAW DC8 SRM 53-2-0 AND DC8 SRM 51-1-8. PERFORM A NDT INSPECTION PROCEDURE S/N 08550001-7001 AT RECOMMENDED INSP INTERVALS PSE NO 53.08.039 FWD OF STA 9-680.50, APPLIES TO THIS FIGURE. 2 L 7 4 4F RT 4A25 2001030500173 20010305 00173 NM 2001 3 5 TWAA0102801 1 20010212 A 3350 7024092007 LENS BOEING 767 767330 NM CABIN MISSING A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 961LF 25137 THE LEFT SIDE NUMBER 1 CABIN DOOR EMERGENCY LIGHT LENS WAS MISSING, AND THE EGRESS LIGHTS WERE INOPERATIVE FROM ROWS 35 THRU 40 ON LT SIDE. INSTALLED L1 DOOR LIGHT LENS, AND RECONNECTED SEVERAL LOOSE CONNECTORS FOR EGRESS LIGHTS. CHECK-C 2-2-01 JFK. 2 L 7 2 4F RT A1NM 2001030500174 20010305 00174 WP 2001 3 5 TWAA0102802 1 20010207 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT FOUND CRACK AT FORMER FOOT (SHEAR TIE) STA 1429, BETWEEN LONGERON 1 AND 2R. REPLACED FORMER FOOR P ER DRAWING 9911840-112. INSTALLED PER 51-30-02/05. 2 L 7 2 4F A6WE 2001030500175 20010305 00175 WP 2001 3 5 TWAA0102803 1 20010209 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT IN THE AFT CARGO COMPT, CORROSION WAS FOUND ON FORMER AT STA 1271, LONGERON 28R TO 28L. REMOVED CO RROSION. INSTALLED NEW J-ANGLE. PAINTED REMOVED PARTS WHITE AND INSTALLED REPAIR PER SRM 53-03, FIG 2. 2 L 7 2 4F A6WE 2001030500176 20010305 00176 WP 2001 3 5 TWAA0102804 1 20010210 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT FOUND 4 INCH J-ANGLE FLOOR SUPPORT CORRODED AT STA 1155, RBL 13 INCHES. REPLACED ANGLE WITH NEW. INSTALLED HI-LOKS PER SRM 51-30-5. 2 L 7 2 4F A6WE 2001030500177 20010305 00177 WP 2001 3 5 TWAA0102805 1 20010210 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT FOUND DENT 2.7 BY 3.6 BY 0.093 DEEP IN SKIN OF AFT CARGO DOOR. CUT OUT 2 .6875 ROUND PLUG FROM SKI N 0.050. INSTALLED 2024-T3 PLUG WITH A BACK UP PLATE 301 .25 H, 0.032 PER SRM 52-05, PAGE 4 FIG 3. 2 L 7 2 4F A6WE 2001030500178 20010305 00178 WP 2001 3 5 TWAA0102806 1 20010212 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT FOUND FORMER FOOT CRACKED AT STA 1309, BETWEEN LONGERON 13 AND 14. REPLACED CRACKED FORMER FOOT. SPLICED PER SRM 53-03 FIG 3. INSTALLED PER SRM 51-30-02/05. PRIMED AND TREATED PER SRM 51-10-03. 2 L 7 2 4F A6WE 2001030500179 20010305 00179 WP 2001 3 5 TWAA0102807 1 20010208 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT FOUND CORROSION IN THE NUMBER 1 CABIN CHAIR TRACK, STA 1118. REPLACED NUMBER 1 CHAIR TRACK FROM ST A 1030 TO 1136 PER SPM 6-70-01. REPLACED FASTENERS PER SRM 51-30-0. 2 L 7 2 4F A6WE 2001030500180 20010305 00180 WP 2001 3 5 TWAA0102808 1 20010211 A 5347 GALLEY TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT FOUND CORROSION AT FWD GALLEY HOLD DOWN SUPPORT AT STA 160, BLR 38 IN. REPLACED GALLEY TIE DOWN PE R SRM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-5. 2 L 7 2 4F A6WE 2001030500181 20010305 00181 WP 2001 3 5 TWAA0102809 1 20010211 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR SUPPORT AT STA 200 FROM BLR AND ON TO APPROX 37 INCHES. REPLACED FL OOR SUPPORT PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-5. 2 L 7 2 4F A6WE 2001030500182 20010305 00182 WP 2001 3 5 TWAA0102810 1 20010211 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 160 TO 200, RBL 44 INCHES. REPLACED FLOOR SUPPORT PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-02 AND 51-30-5. 2 L 7 2 4F A6WE 2001030500183 20010305 00183 WP 2001 3 5 TWAA0102811 1 20010212 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT FOUND CORROSION INSIDE LONGERON 24L, BETWEEN STA 1193 AND 1212. REPLACED LONGERON SPLICE WITH NEW SPLICE. SEALED PART FOR INSTALLING PER SRM 51-20-0. REPLACED RIVETS IN FLANGE WITH HI-LOKS PER SRM 51-60-0. 2 L 7 2 4F A6WE 2001030500184 20010305 00184 WP 2001 3 5 TWAA0102812 1 20010212 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR SUPPORT AT STA 148 TO 200, RBL 5 INCHES. REPLACED FLOOR SUPPORT PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-1, STA 148 TO 200. 2 L 7 2 4F A6WE 2001030500185 20010305 00185 WP 2001 3 5 TWAA0102813 1 20010212 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT IN THE RT SIDE NUMBER 1 CABIN DOOR AREA, FOUND FLOOR SUPPORT AT STA 200 WITH CORROSION, RBL 44 TO 5 4. REPLACED FLOOR SUPPORT PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2001030500186 20010305 00186 WP 2001 3 5 TWAA0102814 1 20010112 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT FOUND THE RT SIDE NUMBER 1 CABIN DOOR AREA, WITH CORROSION ON MEMBRANE AT STA 180 TO 200, BL 0 TO R BL 35 INCHES. SEVERAL PLACES. CORROSION REMOVED PER SPM 6-80-01. TREATED AREA PER SRM 51-10-3. INSTALLED DOUBLER PER SRM 53-01 FIG 2. INSTALLED FASTENERS PER SRM 51-30-02. 2 L 7 2 4F A6WE 2001030500187 20010305 00187 WP 2001 3 5 TWAA0102815 1 20010206 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9401W 53137 DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT OUTBOARD OF NUMBER 4 FLOOR PANEL, UNDER A-GALLEY DRAIN PAN. REMOV ED DRAIN PAN AND FLOOR SUPPORT. FABRICATED FLOOR SUPPORT FROM STOCK PER SPM 6-70-01. INSTALLED SUPPORT AND DRAIN PAN P ER SPM 6-70-01. 2 L 7 2 4F RT A6WE 2001030500188 20010305 00188 CE 2001 3 5 ERYA682D3 1 20010205 A 7603 45AS42010033 THROTTLE CABLE BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE RT ENGINE FROZEN E ERYA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 CE 07 710T 131 RK183 PCEJA0133 DURING FLIGHT FROM KLGA TO CYYZ AT FLIGHT LEVEL 310, THE RIGHT ENGINE THROTTLE FROZE IN POSITION. THE AIRCRAFT DECENDED TO 14000 FT. DURING THE APPROACH, THE THROTTLE WAS STILL FROZEN SO THE RIGHT ENGINE WAS SHUT DOWN AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED AT TORONTO WITHOUT FURTHER INCIDENT. 2 H 7 2 4F 4 F RT A16SW E25EA 2001030500189 20010305 00189 2001 3 5 GLBA2001032 4 20010209 A 3418 WARN HORN BEECH 1900 1900D 1154162 CE STALL WARNING ACTIVATED A GLBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 01 219GL UE219 RETURN TO BLOCK - STALL WARNING HORN SOUNDS AT LIFT OFF, CND TEST FLIGHT OPS CHECKED GOOD. 2 L 7 2 4T RT A24CE 2001030500190 20010305 00190 CE 2001 3 5 GLBA2001033 1 20010210 A 3210 LANDING GEAR BEECH 1900 1900D 1154162 CE FUSELAGE FAILED A GLBA O OTHER J WARNING INDICATION LD LANDING 1 CE 01 97UX UE97 LANDING GEAR NOT EXTENDED UPON LANDING, WAITING RESULTS FROM NTSB. 2 L 7 2 4T RT A24CE 2001030500191 20010305 00191 CE 2001 3 5 GLBA2001035 1 20010212 A 7931 REGULATOR BEECH 1900 1900D 1154162 CE OIL SYSTEM OUT OF ADJ A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 01 255GL UE255 ABORTED T/O - LEFT OIL PRESSURE FLUX ON T/O ROLL. ADJUSTED PRESSURE REGULATOR, OPS CHECKED SYSTEM GOOD. 2 L 7 2 4T RT A24CE 2001030500192 20010305 00192 SO 2001 3 5 C2XA01IA079 1 20010210 A 3350 LP010 BULB EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12715 120125 IAH - FLIGHT 3534, DURING PRE-FLIGHT INSPECTION, ONE AISLE PATH EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANC E PLACED THE LIGHT ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RETURNED TO IAH WHERE MAIN TENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURNN TO SERV ICE. 2 L 7 2 4T RT A31SO 2001030500193 20010305 00193 SO 2001 3 5 C2XA01IA080 1 20010211 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 13992 145284 IAH - FLIGHT 3938, THE CREW REPORTED AN ELECTRIC ODOR IN THE CABIN AND COCKPIT DURING TAXI. THE AIRCRAFT RETURNED TO TH E GATE WHERE MAINTENANCE INSPECTED THE AIRCRAFT, FOUND NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001030500194 20010305 00194 EU 2001 3 5 C2XA01IA081 1 20010211 A 3240 BRAKE ASSY AEROSP ATR42 ATR42320 8680930 EU MLG FAILED A C2XA O OTHER J WARNING INDICATION LD LANDING 1 SW 27 86842 286 CRP - FLIGHT 3352, THE CREW REPORTED THAT BRAKES WERE LOST ON LANDING WITH ALL PRESSURE READINGS BEING NORMAL. MAINTENA NCE INSPECTED THE AIRCRAFT AND FOUND NO DEFECTS. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001030500195 20010305 00195 SO 2001 3 5 C2XA01IA082 1 20010211 A 3230 852701 PROXIMITY SWITCH EMB 145 EMB145 SO LT MAIN GEAR INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 14925 145004 IAH - FLIGHT 4211, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE IN CRUISE. THE AIRCRAFT RETURNED TO IAH WHE RE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND MAIN LANDING GEAR WEIGHT ON WHEELS PROX S WITCH, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001030500196 20010305 00196 SO 2001 3 5 C2XA01IA083 1 20010213 A 3350 3025101 LIGHT EMB 145 EMB145ER SO FUSELAGE INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13929 145009 IAH - DURING A-CHECK INSPECTION, THE LEFT AND RIGHT HAND AFT OVERWING EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE R EMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLIES IN ACCORDANCE WITH EMB145 M/M 33-50-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001030500197 20010305 00197 WP 2001 3 5 DHL2001803003 1 20010214 A 2720 POWERPACK DOUG DC8 DC873F 302199F WP RUDDER LACK OF LUBE A DHLA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SO 01 803DH 46123 DURING CONTROL CHECK, NO DROP IN PRESSURE WHEN RUDDER WAS CHECKED. INSPECTED AND LUBED RUDDER POWER PACK. SYSTEM OPS C HECKS NORMAL PER MM 27-21-6. 2 L 7 4 4F RT 4A25 2001030500200 20010305 00200 EU 2001 3 5 2570481 1 20010210 A 5310 STRUCTURE HAWKER BAE125 BAE125700B 7450007 EU LT MLG WW CRACKED E ERYA K NONE O OTHER IN INSP/MAINT 1 CE 07 731DL 8385 NA0234 CRACK IN LEFT HAND WHEEL WELL TUB EXTENDING BEYOND PREVIOUS STOP DRILL REPAIR. 2 L 7 2 4F RT A3EU 2001030500201 20010305 00201 NM 2001 3 5 PCAA0102006 1 20010209 A 3350 28VS200Y4DH TRANSFORMER DHAV DHC8 DHC8102 2809003 NM RT TRU FLUCTUATES A PCAA O OTHER O OTHER CL CLIMB 1 EA 13 830EX 26428 155 ALB FLIGHT 3539. FLIGHT ATTENDANT REPORTED EMERGENCY LIGHTS WERE FLASHING ON AND OFF DURING CLIMBOUT. MEL 24-01 ISSUED FOR TRANSFORMER RECTIFIER UNIT (TRU) AND AIRCRAFT RETURNED TO SERVICE. DURING NEXT SCHEDULED MAINTENANCE VISIT RIGHT T RU REPLACED. SYSTEM OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001030500202 20010305 00202 NM 2001 3 5 PCAA0102007 1 20010213 A 5260 GUARD DHAV DHC8 DHC8102 2809003 NM AIRSTAIR DOOR JAMMED A PCAA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 13 832EX 280 RDG FLIGHT 3555. CREW REPORTED AIRSTAIR DOOR WILL NOT OPEN. MAINTENANCE UNJAMMED DIRT GUARD FROM BOTTOM OF DOOR. OPER ATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001030500203 20010305 00203 NM 2001 3 5 DHL2001724001 1 20010213 A 7900 GARLOCK SEAL BOEING 727 727228 NM NR 3 ENGINE LEAKING A DHLA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 724DH 19862 NR 3 ENG OIL QTY SLOWLY DECREASED TO ZERO IN FLIGHT. OIL PRESSURE DECREASED TO 37 PSI AND THEN BECAME ERRATIC. NR 3 EN G WAS THEN SHUT DOWN ACCORDING TO AOM. TIME WAS 0553. AFTER SHUT DOWN, ENGINE WAS SHOWING OIL PRESSURE. REMOVED AND R EPLACED FUEL PUMP GARLOCK AND SHAFT O-RING IAW JT8D MM 72-61-0 AND 73-11-1. NO LEAKS NOTED ON ENGINE RUN PER DHL JRH CHA PTER 5. 2 L 7 3 4F A3WE 2001030500204 20010305 00204 NM 2001 3 5 JBXA000244 1 20010214 A 3020 32156182 VALVE BOEING 737 73776N NM NR 1 ENGINE FAILED A JBXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 05 311ML 30051 FLT 488 RDU/DEN ABORTED TAKEOFF FOR LEFT ENGINE ANTI-ICE OVER PRESSURE LIGHT CAME ON AFTER REACHING FULL POWER. RETURNE D TO GATE. REMOVED AND REPLACED NR 1 ENGINE ANTI-ICE VALVE. OPERATIONAL CHECK AND LEAK CHECK GOOD IAW B-737 MM 30-21-1 1. 2 L 7 2 4F RT A16WE 2001030500205 20010305 00205 NM 2001 3 5 DHL2001712504 1 20010201 A 5310 DOOR FRAME BOEING 727 72729 1384007 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 C-CHECK - MAIN CARGO DOOR CORNER JAMB, LWR PART DENTED AND BROKEN 1.0 INCH AT STA 480. READIED LWR CORNER COVER IAW SRD 51-30-2 PAGE 1 AND 2. FABRICATED COVER SUPPORT ANGLE WITH ALCAD 2024, T3, 0.063 INCH IAW SRM 52-20-2, FIG 1. FABRICAT ED COVER CORNER WITH ALCAD 2024, T3, 0.050 INCH IAW SRM 52-20-2 FIG 1. TREATED AND PRIMED IAW SRM 51-10-2, PAGE 1 AND 2 . INSTALLED SUPPORT ANGLE AND COVER CORNER IAW SRM 51-30-2, PAGE 1 AND 2. (NON-ROUTINE CARD 1477). 2 L 7 3 4F A3WE 2001030500206 20010305 00206 NM 2001 3 5 DHL2001712505 1 20010207 A 5210 SEAL BOEING 727 72729 1384007 NM PAX DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 C-CHECK - BASE OF LWR HINGE SEAL FROM FWD ENTRY DOOR CRACKED 1.0 INCH. REMOVED HINGE SEAL BASE IAW SRM 51-30-2, PAGE 13 . PERFORMED STOP DRILL IAW SRM 51-40, PAGE 1. FABRICATED DOUBLER (ALCAD 2024, T3, 0.032 INCH IAW SRM 51-40, PAGE 1. C LEANED, TREATED, AND PRIMED IAW SRM 51-10-2, PAGE 1 AND 2. INSTALLED DOUBLER IAW SRM 51-40, PAGE 1. REINSTALLED HINGE SEAL BASE IAW SRM 51-30-2, PAGE 13. (NON-ROUTINE CARD 0526). 2 L 7 3 4F A3WE 2001030500207 20010305 00207 NM 2001 3 5 DHL2001712506 1 20010206 A 5310 DOOR FRAME BOEING 727 72729 1384007 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 C-CHECK - MAIN CARGO DOOR JAMB CORNER DENTED AND BROKEN 1 INCH LWR PART STA 620.000. REMOVED CORNER IAW SRM 51-30-2, PA GE 1 AND 2. FABRICATED SUPPORT ANGLE WITH ALCLAD 2024, T3, 0.063 INCH IAW SRM 52-30-00, PAGE 4. FABRICATED CORNER COVE R WITH ALCLAD 2024, T3, 0.050 INCH IAW SRM 52-30-00, PAGE 4. TREATED AND PRIMED IAW SRM 51-10-2, PAGE 1 AND 2. INSTALL ED SUPPORT ANGLE AND CORNER COVER IAW SRM 52-30-00, PAGE 4. (NON-ROUTINE CARD 1478). 2 L 7 3 4F A3WE 2001030500208 20010305 00208 NM 2001 3 5 DHL2001712507 1 20010202 A 5414 SKIN BOEING 727 72729 1384007 NM NR 3 NACELLE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 C-CHECK - NR 3 ENG UPPER COWLING SKIN, 0.125 INCH CRACKS. PERFORMED STOP DRILL IAW SRM 51-10-1, PAGE 6B. FABRICATED DO UBLER WITH ALCLAD 2024, T3, 0.050 INCH IAW SRM 54-10-3, FIG 5. INSTALLED DOUBLER IAW SRM 54-10-3, FIG 5. (NON-ROUTINE CARD 1177). 2 L 7 3 4F A3WE 2001030500209 20010305 00209 NM 2001 3 5 DHL2001712508 1 20010206 A 5720 ANGLE BOEING 727 72729 1384007 NM RT WING FAIRING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 C-CHECK - RT WING WINGLET FAIRING LWR PART SUPPORT ANGLES CRACKED 1.0 INCH. REMOVED SUPPORT ANGLES IAW SRM 51-30-2, PAG E 13. FABRICATED ANGLES (SUPPORT ANGLE) NEW WITH ALCLAD 2024, T3, 0.05 INCH IAW SRM 57-20-3, PAGE 1-3. TREATED AND PRI MED IAW SRM 51-10-2, PAGE 1 AND 2. INSTALLED ANGLES IAW SRM 51-30-2, PAGE 13. (NON-ROUTINE CARD 0930). 2 L 7 3 4F A3WE 2001030500210 20010305 00210 NM 2001 3 5 DHL2001712511 1 20010202 A 5312 BULKHEAD BOEING 727 72729 1384007 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 C-CHECK- AFT BAGGAGE RT AFT BULKHEAD PANEL CRACKED 2.0 INCHES AT STA 1166.0. CLEANED AND REPAIRED AFT BAGGAGE RT AFT BU LKHEAD PANEL AT STA 1166.0 WITH FIBER GLASS CLOTH AND RESIN POLYSTER IAW SRM 51-20-03, FIG 2. (NON-ROUTINE CARD 0995). 2 L 7 3 4F A3WE 2001030500211 20010305 00211 NM 2001 3 5 DHL2001712513 1 20010203 A 7830 FAIRING BOEING 727 72729 1384007 NM THRUST REVERSER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 C-CHECK - NR 3 ENGINE THRUST REVERSER FWD FAIRING 1.0 INCH CRACK AT 3 O CLOCK. PERFORMED STOP DRILL IAW SRM 51-10-1, PA GE 6B. INSPECTED DOUBLER WITH ALCLAD 2024, T3, 0.032 INCH IAW SRM 51-40, PAGE 1. TREATED AND PRIMED IAW SRM 51-10-2, P AGE 1 AND 2. INSTALLED DOUBLER WITH ALCLAD IAW SRM 51-40, PAGE 1. (NON-ROUTINE CARD 1476). 2 L 7 3 4F A3WE 2001030500212 20010305 00212 NM 2001 3 5 DHL2001712514 1 20010202 A 7830 FAIRING BOEING 727 72729 1384007 NM THRUST REVERSER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 C-CHECK - NR 3 ENGINE RT REVERSE CASE FAIRING CRACKED 0.50 INCH AT STA 210, 9 O CLOCK POSITION. WELDED NR 3 ENGINE RT R EVERSE CASE FAIRING WITH ALUMINIUM AGS WELDING .0625 INCH WITH TIG IAW OVERHAUL MANUAL 72-21-1, PAGE 402. (NON-ROUTINE CARD NR 1519). 2 L 7 3 4F A3WE 2001030500213 20010305 00213 NM 2001 3 5 DHL2001712515 1 20010205 A 5343 FITTING BOEING 727 72729 1384007 NM RT MLG CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 C-CHECK - RT MLG FITTING TO ANGLE SPLICE CRACKED 1.0 INCH BS 945.000 TO BS 950.000, 5-18 RT. REMOVED CRACKED ANGLE IAW SRM 51-30-2, PAGE 66. FABRICATED TWO ANGLES WITH ALCLAD 2024, T3, 0.090 AND ALCLAD 2024, T3, 0.040 IAW SRM 53-40-1, PAG E 1-2. TREATED AND PRIMED IAW SRM 51-10-2, PAGE 1-5. INSTALLED ANGLES IAW SRM 51-30-2, PAGE 66. (NON-ROUTINE CARD 021 7). 2 L 7 3 4F A3WE 2001030500214 20010305 00214 SO 2001 3 5 SWIA972353 1 20010212 A 3060 RCCB EMB 120 EMB120RT SO PWA 118 PW118 NE RT PROPELLER FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 162CA 120150 RIGHT PROPELLER HEAT CONTINUES TO FAIL IN FLIGHT. EN ROUTE LAX DIVERTED TO PSP. INSPECTED LEFT AND RIGHT PROPELLER DEI CE LEADS, LOOKED OK. CHECKED RIGHT PROPELLER HEAT RCCB. INSPECTED WIRING AT SWITCH AND RELAYS. FOUND POWER AT A2 OF R CCB 226 DROPS TO BELOW 1 VOLT. WHEN PROPELLER DEICE ACTIVATED POWER AT A1 REMAINS 28 VOLTS. REMOVED AND REPLACED RCCB 226. OPS CHECK GOOD OF RIGHT PROPELLER DEICE SYSTEM. 2 L 7 2 4T 4 T RT A31SO E20NE 2001030500215 20010305 00215 SO 2001 3 5 SWIA972354 1 20010212 A 2731 SENSOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ELEVATOR FAILED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 568SW 120343 TRIM AURAL WARNING ACTIVATED ON TAKEOFF ROLL WHEN TRIM WAS SET CORRECTLY. ABORTED TAKEOFF. FOUND RIGHT ELEVATOR TRIM P ROXIMITY SENSOR BAD. REMOVED AND REPLACED SENOR, OPS CHECKED GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001030500216 20010305 00216 SO 2001 3 5 SWIA972355 1 20010212 A 2720 RUDDER PEDAL EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT OUT OF ADJ A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 187SW 120037 FOS RUDDER PEDALS WILL NOT EXTEND FULL FORWARD. ADJUSTED RIGHT RUDDER PEDAL ADJUSTEMENT CRANK AS NECESSARY. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001030500217 20010305 00217 SO 2001 3 5 SWIA972356 1 20010212 A 3040 HEATER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE WINDSHIELD MALFUNCTIONED A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 291SW 120318 WINDSHIELD HEAT INOP LIGHT (RIGHT) CAME ON DURING TAKEOFF. TAKEOFF ABORTED. OPERATED RIGHT WINDSHIELD HEAT THROUGH SEV ERAL CYCLES, DID NOT FAIL. OPS CHECK GOOD. COULD NOT DUPLICATE. 2 L 7 2 4T 4 T RT A31SO E20NE 2001030500218 20010305 00218 EA 2001 3 5 SWIA972357 1 20010213 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 905SW 7437 ON PREFLIGHT INSPECTION, NOTICED CAPTAINS SIDE WINDSHIELD CRACKED REPLACED CAPTAINS WINDSCREEN IAW 56-11-04. P/N ON NP- 139321-5, S/N ON 9927H9235, S/N OFF 00133H7393. 2 L 7 2 4F 4 F RT A21EA E15NE 2001030500219 20010305 00219 2001 3 5 SWIA972358 4 20010212 A 3418 SENSOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE STICK SHAKER CORRODED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 293SW 120320 AT TAKEOFF BEGINNING OF ROLL, THREE CHIME TRIM FAIL. ABORTED TAKEOFF. TRIM WAS IN GREEN AT 35 PERCENT. TESTED AND ADJ USTED TRIM. ATTEMPTED STATIC TAKEOFF AND RECEIVED TRIM FAIL TRIPLE CHIME. WENT BACK TO BOX. FOUND CORROSION ON HAND S HAKES AT RIGHT PROXIMITY SENSOR. INSTALLED NEW WRIST LOCKS AND OPERATED TRIM WARNING IAW 31-00-00. OPS CHECK GOOD AT T HIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 2001030500220 20010305 00220 WP 2001 3 5 TWAA0102901 1 20010208 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9401W 53137 DURING CHECK-C MAINT FLOOR TRACK AT LBL 44 WAS CORRODED FROM STA 1136 TO 1211. REPLACED TRACK PER SRM 53-05, FIG 4F SHE ET 1. 2 L 7 2 4F RT A6WE 2001030500221 20010305 00221 WP 2001 3 5 TWAA0102902 1 20010209 A 5531 RIB DOUG DC9 DC983 3022083 WP DORSAL FIN CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9401W 53137 DURING CHECK-C MAINT NUMBER 3 AND 4 DORSAL FIN RIBS, FROM UPPER EDGE ON LT SIDE, WERE CRACKED. ROUTED AND RADIUSED END OF RIB. INSTALLED REPLACEMENT FILLER ON NUMBER 3 AND 4. INSTALLED 2024-T3 0.050 DOUBLER PICKING UP MINIMUM 3 ROWS OF FA STENERS BEYOND CRACK PER 55-30-102. 2 L 7 2 4F RT A6WE 2001030500222 20010305 00222 WP 2001 3 5 TWAA0102903 1 20010209 A 5320 CASTING DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9401W 53137 DURING CHECK-C MAINT CABIN LONGERON 18R, STA 732, FORMER ATTACH CASTING INBD LEG HAD CORROSION. REMOVED CORRODED ATTACH CASTING AND REPLACED WITH NEW PER SRM 51-30-1 AND 53-03. 2 L 7 2 4F RT A6WE 2001030500223 20010305 00223 WP 2001 3 5 TWAA0102904 1 20010209 A 5320 CASTING DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9401W 53137 DURING CHECK-C MAINT FORMER ATTACH CASTING AFT INBOARD LEG WAS CORRODED AT STA 1079, LONGERON 18R. REPLACED CASTING PER SPM 6-70-01. 2 L 7 2 4F RT A6WE 2001030500224 20010305 00224 WP 2001 3 5 TWAA0102905 1 20010212 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9401W 53137 DURING CHECK-C MAINT IN THE AFT CARGO COMPT, FORMER 1250 WAS CORRODED TOP AND BOTTOM AT LONGERON 29L TO 29R. REMOVED CO RROSION AND INSTALLED DOUBLER REPAIR PER SRM 53-03, FIG 2A SHEET 4. 2 L 7 2 4F RT A6WE 2001030500225 20010305 00225 WP 2001 3 5 TWAA0102906 1 20010212 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9401W 53137 DURING CHECK-C MAINT FOUND FLOOR WEB CORRODED AT STA 1098 TO 1117, AT LONGERON 18R. CUT OUT CORROSION AND INSTALLED REP AIR PER SRM 53-01, FIG 4 SHEET 3. 2 L 7 2 4F RT A6WE 2001030500226 20010305 00226 NM 2001 3 5 UPS01434961 1 20010110 A 5320 69B620501 FITTING BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, CORROSION ON PALLET LOCK TIE DOWN FITTING. FITTING REPLACED REF SRM 51-30-02. 2 L 7 4 4F A20WE 2001030500227 20010305 00227 NM 2001 3 5 UPS01434963 1 20010115 A 5320 65B0799224 FITTING BOEING 747 747123F NM PAX DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, NR 1 RT MAIN ENTRY DOORWAY FWD EDGE JUST ABOVE LOWER HINGE IS CRACKED. ALSO, CLOSURE PANEL CRACKED FITTING REPLACED IAW SRM 51-30-02. CLOSURE PANEL REPLACED IAW SRM 51-30-02. 2 L 7 4 4F A20WE 2001030500228 20010305 00228 WP 2001 3 5 UPS01834967 1 20010213 A 3510 OXYGEN BOTTLE DOUG DC8 DC873F 302199F WP COCKPIT LEAKING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE:IN BOTH 02 SYS LEAKING. *S/D* REMOVED AND REPLACED BOTH CREW AND COURIER 02, LEAK CHECKED GOOD. 2 L 7 4 4F RT 4A25 2001030500229 20010305 00229 WP 2001 3 5 UPS01834979 1 20010205 A 3350 6012235 BATTERY PACK DOUG DC8 DC873F 302199F WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:IN ON PDC FOUND EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW MM 33-50-01 . OPS CHECKS GOOD. 2 L 7 4 4F RT 4A25 2001030500230 20010305 00230 EU 2001 3 5 QXEA0100104 1 20010211 A 3350 5515800106 LIGHT FOKKER F28 F28MK4000 4990810 EU GALLEY INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 498US 11181 SEA - EXIT LIGHT GALLEY OVERHEAD INOP. INSTALLED NEW LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SER VICE. 2 L 7 2 4F RT A20EU 2001030500232 20010305 00232 EA 2001 3 5 JBXA000245 1 20010214 A 3260 UPLOCK SENSOR CNDAIR CL600 CL6002B19 EA RT MLG OUT OF ADJ A JBXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 05 574ML 7242 RIGHT MAIN LANDING GEAR DISAGREE ON TAKEOFF. ADJUSTED RIGHT MLG UPLOCK SENSOR AND TARGET ARM I-A-W AMM 32-61-05, OPS CH ECK GOOD. 2 L 7 2 4F RT A21EA 2001030500233 20010305 00233 2001 3 5 01FDEA00120 4 20010214 A 3442 6625136001 ANTENNA DOUG MD11 MD11F 3023600 NM WX RADAR FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 608FE 48548 WX RADAR FAILURE BOTH SYS WX FAIL ON VAV DISPLAY AND ALL INFO DISAPPEARED. REMOVED AND REPLACED RADAR ANTENNA, OPS CK O K PER MD11 MM 34-41-07-4. 2 L 7 3 4F RT A22WE 2001030500235 20010305 00235 NM 2001 3 5 DHL2001712516 1 20010215 A 5755 STRUCTURE BOEING 727 72729 1384007 NM RT WING SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 C-CHECK - RT WING NR 14 SPOILER LWR PART CRACKED 2.0 INCHES. CLEANED AND REPAIRED RT WING NR 14 SPOILER LOWER PART WITH POLYESTER RESIN AND CATALYST IAW SRM 51-20-3, FIG 2. (NON-ROUTINE CARD NR 1412). 2 L 7 3 4F A3WE 2001030500236 20010305 00236 NM 2001 3 5 DHL2001712512 1 20010203 A 7110 STRUCTURE BOEING 727 72729 1384007 NM NR 1 ENG COWL DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 C-CHECK - NR 1 ENGINE LWR COWLING 2/B DOUBLER BROKEN 2.0 INCHES (INTERIOR) AT STA 136.0. REMOVED DOUBLER IAW SRM 51-30- 2, PAGE 1 AND 2. FABRICATED DOUBLER WITH ALCLAD 2024, T3, 0.050 INCHES IAW SRM 54-10-3, FIG 2. CLEANED, TREATED, AND P RIMED IAW SRM 51-10-2 PAGE 6A. INSTALLED DOUBLER IAW SRM 51-30-2, PAGE 1 AND 2. (NON-ROUTINE CARD 0925). 2 L 7 3 4F A3WE 2001030500237 20010305 00237 EU 2001 3 5 MALA010182 1 20010208 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 425XJ 425 SEVERAL DENTS ON RT FUSELAGE JUST AFT OF ICE SHIELD LOCATED BELOW SL1618. CWA MAINTENANCE COMPLETED REPAIR IAW EO S5303 5. 2 L 7 2 4T RT A52EU 2001030500238 20010305 00238 EU 2001 3 5 MALA010187 1 20010208 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 425XJ 425 SEVERAL DENTS IN FUSELAGE ON LT SIDE JUST AFT ON ICE SHIELD. CWA MAINTENANCE COMPLETED REPAIR IAW EO S53009. 2 L 7 2 4T RT A52EU 2001030500239 20010305 00239 2001 3 5 COMA0160227 4 20010209 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 915CA 7013 STALL FAIL CAUTION MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001030500240 20010305 00240 EA 2001 3 5 COMA0160228 1 20010209 A 3040 NP1393221 HEATER CNDAIR CL600 CL6002B19 EA COCKPIT WINDOW MALFUNCTIONED A COMA O OTHER O OTHER CR CRUISE 1 SO 01 783CA 4314 7315 LEFT WINDOW HEAT CAUTION MESSAGE. REPLACED THE LEFT SIDE WINDOW. 2 L 7 2 4F RT A21EA 2001030500241 20010305 00241 2001 3 5 COMA0160229 4 20010209 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 816CA 7398 STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001030500242 20010305 00242 EA 2001 3 5 COMA0160230 1 20010209 A 3150 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 420CA 7451 SPOILERON CAUTION MESSAGE DURING T/O. COULD NOT DUPLICATE. SYSTEM OPERATION NORMAL. 2 L 7 2 4F RT A21EA 2001030500243 20010305 00243 EA 2001 3 5 COMA0160231 1 20010205 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA CABIN DOOR MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 917CA 7017 CABIN DOOR LATCH CAUTION MESSAGE. COULD NOT DUPLICATE. DOOR OPERATION CHECKS NORMAL. 2 L 7 2 4F RT A21EA 2001030500244 20010305 00244 EA 2001 3 5 COMA0160232 1 20010209 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA PAX DOOR ACTIVATED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 778CA 7297 CABIN DOOR OUTER HANDLE MESSAGE. COULD NOT DUPLICATE. DOOR OPERATES NORMAL. 2 L 7 2 4F RT A21EA 2001030500245 20010305 00245 EA 2001 3 5 COMA0160233 1 20010209 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 821CA 1223 7420 FLAPS FAIL CAUTION MESSAGE. REPLACED THE LEFT BPSU. 2 L 7 2 4F RT A21EA 2001030500246 20010305 00246 EA 2001 3 5 COMA0160235 1 20010210 A 2752 853D10018 ACTUATOR CNDAIR CL600 CL6002B19 EA RT WING TE FLAPS JAMMED A COMA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 420CA 517 7451 FLAPS FAILED. REPLACED THE NR 3 FLAP ACTUATOR ON RT WING. 2 L 7 2 4F RT A21EA 2001030500247 20010305 00247 EA 2001 3 5 COMA0160236 1 20010211 A 5270 SENSOR CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADJ A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 719CA 7253 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. ADJUSTED DOOR HANDLE PROXIMITY SENSOR. 2 L 7 2 4F RT A21EA 2001030500248 20010305 00248 EA 2001 3 5 COMA0160237 1 20010211 A 5270 840534 PROXIMITY SWITCH CNDAIR CL600 CL6002B19 EA PAX DOOR MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 778CA 7297 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. REPLACED THE HANDLE PROXIMITY SENSORS. 2 L 7 2 4F RT A21EA 2001030500249 20010305 00249 EA 2001 3 5 COMA0160238 1 20010211 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 EA CABIN DIRTY A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 979CA 7159 FORWARD FLOOR EMERGENCY LIGHT IS INOP. CLEANED CONNECTION, LIGHT OPERATION IS NORMAL. 2 L 7 2 4F RT A21EA 2001030500250 20010305 00250 EA 2001 3 5 COMA0160239 1 20010211 A 2750 601R930507 FCU CNDAIR CL600 CL6002B19 EA E/E BAY MALFUNCTIONED A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 815CA 1825 7397 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2001030500251 20010305 00251 EU 2001 3 5 MALA010188 1 20010214 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 425XJ 425 CWA MAINTENANCE PERFORMED EO S53086 ON FRAME AT STA 258, ANGLE FLANGE CORROSION. 2 L 7 2 4T RT A52EU 2001030500252 20010305 00252 EU 2001 3 5 MALA010189 1 20010209 A 2610 CONNECTOR SAAB SF340 SF340A 7850100 EU NACELLE DIRTY A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 46XJ 046 ON DEPARTURE FROM MKG DOWNWIND, HAD A RT TAILPIPE HOT INDICATION. COMPLETED ORH AND RETURNED TO MKG. MAINTENANCE CLEAN ED CANNON PLUG ON NACELLE, PERFORMED HIGH POWER RUN-UP. ALL CHECKS GOOD. OK FOR CONTINUED SERVICE REF: SAAB 340 MM 54- 20-00-0. 2 L 7 2 4T RT A52EU 2001030500253 20010305 00253 EU 2001 3 5 MALA010190 1 20010209 A 3260 PLUNGER BAC 146 AVRO146RJ85A 1500097 EU UP/DOWN LOCK OUT OF ADJ A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 516XJ E2334 NOSE LANDING GEAR WOULD NOT MOVE WHEN SELECTED GEAR DOWN, USED EMERGENCY GEAR DOWN LEVER, ALL OTHER INDICATIONS WERE THE N NORMAL. MAINTENANCE ADJUSTED TURNBUCKLE FOR UPLOCK/DOWNLOCK PLUNGER ON NOSE GEAR IAW CMM 32-20-53. GEAR SWINGS CHECK GOOD. SEE CONTINUATION CARD 007077 FOR MORE DETAIL. 2 H 7 4 4F RT A49EU 2001030500254 20010305 00254 EU 2001 3 5 MALA010191 1 20010209 A 3020 WARNING LIGHT BAC 146 AVRO146RJ85A 1500097 EU NR 1 ENGINE ILLUMINATED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 532XJ E2366 NR 1 INTAKE LOW PRESSURE LIGHT ON DEPARTURE FROM DTW, COMPLETED ORH, CYCLED SEVERAL TIMES, NO HELP. GETTING MULTI-WARNI NGS ON AND OFF THOUGH WARNING REMAINS ON. MAINTENANCE DEFERRED NR 1 ENGINE LO-PRESSURE LIGHT PER MEL 30-20-2 (1) ALL MA INTENANCE PROCEDURES COMPLIED. 2 H 7 4 4F RT A49EU 2001030500255 20010305 00255 2001 3 5 MALA010192 4 20010208 A 3442 20412170414 R/T UNIT BAC 146 AVRO146RJ85A 1500097 EU WX RADAR DEFECTIVE A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 510XJ E2325 SHORTLY AFTER TAKEOFF, THE WEATHER RADAR FAILED, CYCLED RADAR OFF SEVERAL TIMES, UNABLE TO FIX PROBLEM. MAINTENANCE REP LACED 2 WEATHER RIGHT P/N 204-1217-0414, S/N OFF 4253, S/N ON 7404. ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 2001030500256 20010305 00256 EA 2001 3 5 COMA0160145 1 20010122 A 5311 FRAME CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 989CA 7636 7215 LEFT SIDE FS 718.0 FRAME AND AFT DOUBLER AND RT SIDE AFT DOUBLER AT FS 718.0 BETWEEN STR 11 AND 12 CRACKED. DOUBLER P/N 600-3603-31/32. REPAIRED LT FRAME AND AFT DOUBLER AT FS 718.0 AND RT SIDE AFT DOUBLER AT FS 718.0 BETWEEN STR 11 AND 1 2 IAW REO 601R-53-61-193 REV A. 2 L 7 2 4F RT A21EA 2001030500257 20010305 00257 EA 2001 3 5 COMA0160221 1 20010210 A 5530 BUSHING CNDAIR CL600 CL6002B19 EA RT/LT VERTICAL WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 17981 7022 LT AND RT VERTICAL STAB BUSHINGS ARE WORN/SCORED AT HORIZONTAL STAB PIVOT POINT. REMOVED WORN/SCORED BUSHINGS. VERIFIE D LT LUG BORE 1.7005 AND RT LUG BORE 1.7002 TO BE WITHIN LIMITS. MACHINED FLANGE OF NEW BUSHING (P/N 600-21061-7) TO .0 86 IAW WVAC EO 601R-55-2224. INSTALLED MACHINED BUSHING IAW CRJ AMM 20-26-00-910-803 AND REAMED TO 1.5001 IAW DWG 600-2 1029. 2 L 7 2 4F RT A21EA 2001030500258 20010305 00258 EA 2001 3 5 COMA0160225 1 20010210 A 5530 BUSHING CNDAIR CL600 CL6002B19 EA VERTICAL STAB WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 17981 7022 LT AND RT VERTICAL STAB BUSHINGS ARE WORN/SCORED AT HORIZONTAL STAB PIVOT POINT. REMOVED WORN/SCORED BUSHINGS. VERIFIE D LT LUG BORE 1.7005 AND RT LUG BORE 1.7002 TO BE WITHIN LIMITS. MACHINED FLANGE OF NEW BUSHING (P/N 600-21061-7) TO .0 86 IAW WVAC 601R-55-2224. INSTALLED MACHINED BUSHING IAW CRJ AMM 20-26-00-910-803 AND REAMED TO 1.5001 IAW DWG 600-2102 9. 2 L 7 2 4F RT A21EA 2001030500259 20010305 00259 NE 2001 3 5 COMA0160234 2 20010210 A 7270 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE RT ENGINE ILLUMINATED A COMA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SO 01 958CA 7111 807088 RT ENGINE FAN VIB ICON ON EICAS. INSPECTED ENGINE AND FOUND NO DEFECTS. COULD NOT DUPLICATE. 2 L 7 2 4F 4 F RT A21EA E15NE 2001030500262 20010305 00262 NM 2001 3 5 2001UALA00021 1 20010110 A 2170 8102101 CONDENSER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE AIR DISTRIBUTION CLOGGED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 772UA 22937 0 26930 POOR AIR QUALITY IN THE AIRCRAFT. *S/D* PROBLEM COULD NOT BE DUPLICATED ON GROUND. HOWEVER, WHEN CHECKING LT CONDENSE R/REHEATER, IT WAS FOUND CLOGGED. A CLOGGED CONDENSER/REHEATER CAN CAUSE PACK LOW FLOW PROBLEM WHICH MAY CONTRIBUTE TO POOR AIR QUALITY. THE LT CONDENSER/REHEATER WAS REPLACED. AIRCRAFT WENT BACK TO REVENUE SERVICE WITHOUT FURTHER POOR A IR QUALITY PROBLEM. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001030500266 20010305 00266 CE 2001 3 5 20010222CW007 1 20010126 A 3320 SO10488308 RECEPTACLE A519 BEECH B300 B300 1159232 CE PWA PT6 PT6* 52043 EA LIGHTING PANEL DAMAGED C S1AM K NONE L NO TEST IN INSP/MAINT 1 SW 99 2SC 3444 FL9 CABIN FLUORESCENT LIGHTS WOULD BLINK ON AND OFF IN FLIGHT. FOUND BAD SOCKET AND PINS AT K1 RELAY OF CABIN LIGHTING PANE L ASSEMBLY. SOCKET PINS OF RECEPTACLE WERE CRIMPED AND INSTALLED BACKWARDS. 2 L 7 2 4T 3 T RT A24CE E2NE 2001030500267 20010305 00267 NM 2001 3 5 USAA010034 1 20010115 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 32038 24556 CLT - FOUND FRAME CRACKED .250 INCH, BS 380, BETWEEN STRINGER 8R AND 9R. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001030500268 20010305 00268 NM 2001 3 5 USAA010032 1 20010115 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 32038 24556 CLT - FOUND FRAME CRACKED .500 INCH, BS 907 BETWEEN STRINGER 8R AND 9R AND 8L AND 9L. INSTALLED DOUBLER PER TR 53-10-14 AND SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 2001030500269 20010305 00269 NM 2001 3 5 USAA010031 1 20010115 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 32038 24556 CLT - FOUND FRAME CRACKED .125 INCH, BS 727D BETWEEN STRINGER 8R AND 9R. REINSTALLED OVERSIZED FASTENER PER SRM 51-40-0 3. (M) 2 L 7 2 4F RT A16WE 2001030500270 20010305 00270 NM 2001 3 5 USAA010030 1 20010115 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 32038 24556 CLT - FOUND FRAME CRACKED, BS 727D BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001030500271 20010305 00271 NM 2001 3 5 USAA010029 1 20010115 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 32038 24556 CLT - FOUND FRAME CRACKED .50 INCH, BS 827 BETWEEN STRINGER 8 AND 9L. INSTALLED DOUBLER PER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001030500272 20010305 00272 NM 2001 3 5 USAA010028 1 20010115 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 32038 24556 CLT - FOUND FRAME CRACKED .125 INCH, BS 827 BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001030500273 20010305 00273 NM 2001 3 5 USAA010027 1 20010115 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 32038 24556 CLT - FOUND FRAME CRACKED .500 INCH, BS 867 BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001030500274 20010305 00274 NM 2001 3 5 USAA010026 1 20010115 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 32038 24556 CLT - FOUND FRAME CRACKED .250 INCH, BS 867 BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001030500275 20010305 00275 NM 2001 3 5 USAA010023 1 20010115 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 32038 24556 CLT - FOUND FLOORBEAM CORRODED 3 INCHES, AT 967, RBL 17 AND 31. CORROSION LEVEL 1. REPAIRED DOUBLER, TRIPLER AND FILLE R PER SRM 53-30-51. (M) 2 L 7 2 4F RT A16WE 2001030500276 20010305 00276 NM 2001 3 5 USAA010022 1 20010115 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 355US 38054 23558 CLT - FOUND SKIN CRACKED, STATION 200, LBL 5. INSTALLED EXTERIOR DOUBLER PER EA 68798. (M) 2 L 7 2 4F RT A16WE 2001030500290 20010305 00290 SO 2001 3 5 C2XA01TY011 1 20010204 A 5310 14522102001 DOOR FRAME EMB 145 EMB145 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 TYS - DURING A SCHEDULED 1C INSPECTION, SERVICE DOOR INNER REINFORCEMENT FRAME HAS GOUGES IN UPPER FORWARD INNER REINFOR CEMENT PLATE AND BELOW PLATE IN FRAME. MAINTENANCE BLENDED GOUGES AND INSTALLED A REINFORCEMENT PLATE ON SERVICE DOOR R EINFORCEMENT FRAME IAW EMB 145 SRM 51-40-02 AND EMB REF GST 0203/2001. REPAIRS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001030500291 20010305 00291 SO 2001 3 5 C2XA01TY012 1 20010204 A 5210 14524000001 STOP EMB 145 EMB145 SO CABIN DOOR GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 TYS - DURING A SCHEDULED 1C INSPECTION, THE TOP AFT RADIAL STOP ON MAIN CABIN DOOR WAS GOUGED AT CORNER. MAINTENANCE BL ENDED STOP IAW EMB REF GST-0244/01. REPAIRS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001030500292 20010305 00292 SO 2001 3 5 C2XA0TY013 1 20010204 A 5310 14524000001 STOP EMB 145 EMB145 SO DOOR FRAME GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 TYS - DURING A SCHEDULED 1C INSPECTION, MAIN DOOR FRAME STOPS NR 1 AND 7 ARE WORN AND GOUGED, STOPS NR 4, 6, 9, 11 AND 1 2 ARE WORN. MAINTENANCE BLENDED STOPS IAW EMB 145MM 53-21-03 AND BLENDED UPPER FORWARD STOP IAW EMB REF GST 0244/01. R EPAIRS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001030500293 20010305 00293 SO 2001 3 5 C2XA01TY014 1 20010204 A 5610 12003060001 FRAME EMB 145 EMB145 SO COCKPIT NICKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 TYS - DURING A SCHEDULED 1C INSPECTION, SCRAPES AND NICKS WERE FOUND ON LEFT COCKPIT WINDSHIELD FRAME. MAINTENANCE BLEN DED, DYE PENETRANT INSPECTED, ALODINED, PRIMED AND PAINTED THE AFFECTED AREA IAW EMB REF GST 0255/01. REPAIRS WERE SATI SFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001030500294 20010305 00294 SO 2001 3 5 C2XA01TY009 1 20010203 A 5310 14521700007 BEAM EMB 145 EMB145 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 TYS - DURING A SCHEDULED 1C INSPECTION, CORROSION WAS FOUND ON OMEGA BEAM AT CARBON FIBER CROSS BEAM ABOVE FRAMES 20 BET WEEN STRINGERS 18L AND 19L. MAINTENANCE REMOVED AND REPLACE OMEGA BEAM AND FABRICATED Z PROFILES IAW EMB 145 SRM 51-40- 01 AND EMB REF GST-0272/01. REPAIRS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001030500295 20010305 00295 SO 2001 3 5 C2XA01TY008 1 20010203 A 5310 1452171803 BEAM EMB 145 EMB145 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 TYS - DURING A SCHEDULED 1C INSPECTION, THE LEFT OMEGA BEAM AFT RAMP ANGLE BETWEEN FRAME 19 AND 20 HAS CORROSION. REMOV ED RAMP ANGLE, FABRICATED NEW RAMP ANGLE IAW EMB 145 SRM 51-30-01), ALODINED AND PRIMED IAW EMB 145 CPM 51-21-04 AND 05. REINSTALLED RAMP ANGLE IAW EMB 145 SRM 51-40-02. REPAIRS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001030500296 20010305 00296 EU 2001 3 5 C2XA01BT009 1 20010207 A 2560 011798 FIRST AID KIT AEROSP ATR42 ATR42320 8680930 EU CABIN MISSING A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14832 187 EWR - FLT 3575 - MAINTENANCE REPORTED THAT THE FIRST AID KIT NEEDED REPLACEMENT, ITEMS MISSING. REMOVED AND REPLACED FI RST AID KIT. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001030500297 20010305 00297 SO 2001 3 5 C2XA01BT008 1 20010206 A 2560 017093 SEAL EMB 145 EMB145 SO EMER MEDICAL KIT BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 CLE - FLT 3862 - CREW REPORTED MEDICAL KIT SEAL BROKEN. MAINTENANCE REMOVED AND REPLACED EMERGENCY MEDICAL KIT AND RETU RNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001030500298 20010305 00298 SO 2001 3 5 C2XA01BT007 1 20010206 A 2612 3601134480 FIRE LOOP EMB 145 EMB145LR SO RT ENG PYLON FAULTY A C2XA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 27 13975 145163 YHZ - CREW REPORTED E2 FIRE DETECTOR FAILED. DISPATCHED MAINTENANCE TO HALIFAX. TROUBLESHOT PROBLEM AND FOUND A BAD NR 2 ENGINE FIRE LOOP. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE PYLON FIRE LOOP. OPS CHECKED GOOD IAW EMB 145 AMM, J IC 26-11-02. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001030500301 20010305 00301 SO 2001 3 5 C2XA01CL016 1 20010202 A 2120 SMOKE EMB 145 EMB145 SO CABIN DETECTED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 15932 145015 YUL - FLT 4005 - THE CREW REPORTED SMOKE IN CABIN AND COCKPIT. THE AIRCRAFT RETURNED TO YUL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE AIR CONDITION SYSTEM IAW 21-00-00. NO DEFECTS WERE NOTED. T HE AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001030500302 20010305 00302 SO 2001 3 5 C2XA01BT016 1 20010210 A 3520 OXYGEN MASK EMB 145 EMB145 SO CABIN DEPLOYED A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 16927 145006 BTV - FLT 4218 - CREW REPORTED SEAT 17A OXYGEN MASK DEPLOYED INFLIGHT. MAINTENANCE ADJUSTED LATCHING MECHANISM AND RESE CURED THE OXYGEN MASK IAW EMB145 AMM 35-20-01. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001030500303 20010305 00303 SO 2001 3 5 MASA02018 1 20010210 A 2611 FDS765A2 SMOKE DETECTOR EMB 145 EMB145LR SO LAVATORY MALFUNCTIONED A MASA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 827MJ 145217 FLT 5808 - RETURNED TO THE FIELD AFTER THE LAV SMOKE DETECTOR WENT OFF INFLIGHT. THE F/A INSPECTED THE LAVATORY AND FOU ND NO SMOKE OR EVIDENCE OF FIRE. MAINTENANCE PERFORMED AN INSPECTION IAW WITH THE MAINTENANCE PROCEDURES. MAINTENANCE MEL''D THE DISCREPANCY. THE AIRCRAFT WAS RETURNED TO SERVICE. MEL CLEARED BHM 2/14/2001. REMOVED LAV SMOKE DETECTOR, CLEANED CONTACTS. REINSTALLED LAV SMOKE DETECTOR. OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001030500304 20010305 00304 NM 2001 3 5 GAIA01046OP 1 20010209 A 3222 651636410 STRUT BOEING 727 727223 1384074 NM NLG LOW A GAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 6807 19482 FLT 718 - TOL-STL - AFTER TAKEOFF, THE FLIGHT CREW NOTICED THAT THE AMBER NOSE GEAR DOOR LIGHT AND THE RED NOSE GEAR LIG HT REMAINED ILLUMINATED WITH THE GEAR RETRACTED. THE CREW FOLLOWED ABNORMAL PROCEDURES AND RETURNED TO TOL. AN UNEVENT FUL LANDING WAS MADE. INSPECTION REVEALED THAT THE NOSE STRUT SERVICE WAS LOW AND THE FORWARD INBOARD CORNER OF THE RIG HT NOSE GEAR STRUT DOOR WAS BROKEN. THE NOSE STRUT WAS SERVICED AND THE AIRCRAFT WAS FERRIED TO JAX. THE NOSE GEAR DOO R WAS REPLACED AND THE NOSE GEAR DOOR LIGHT OPS CHECK WAS NORMAL PER THE B727 MM. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001030500305 20010305 00305 NM 2001 3 5 GAIA01047ST 1 20010210 A 5755 65173522 ANGLE BOEING 727 727251 138408H NM SPOILER ACTUATOR CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A B CHECK LEVEL INSPECTION AT FLIGHTSTAR AIRCRAFT SERVICES AT JAX, IT WAS DISCOVERED THAT THE NR 12 SPOILER ACTUA TOR OUTBOARD SUPPORT ANGLE WAS FOUND CRACKED AT THE LOWER MOUNTING HOLE. REMOVED AND REPLACED THE SUPPORT ANGLE. THE A IRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001030500306 20010305 00306 NM 2001 3 5 USAASB1035 1 20010203 A 2110 WARNING SYSTEM BOEING 737 7373B7 1384580 NM COCKPIT ACTIVATED A USAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 514AU 23700 YUL - FLT 442 - EN ROUTE FROM PIT, AT FL330, THE CABIN ALTITUDE WARNING HORN SOUNDED. CREW PERFORMED EMERGENCY PROCEDUR ES AND WHEN CABIN ALTITUDE CLIMBED TO MORE THAN 10,000 FEET, THE DECLARED AN EMERGENCY. CREW DESCENDED THE FIGHT TO FL1 00 AND WERE ABLE TO CONTROL CABIN ALTITUDE IN MANUAL AND STANDBY MODE. FLIGHT CONTINUED ONTO YUL AT FL100 AND LANDED WI THOUT FURTHER INCIDENT. (M) 2 L 7 2 4F RT A16WE 2001030500307 20010305 00307 NM 2001 3 5 USAASB01025 1 20010128 A 5240 SEAL BOEING 737 7373B7 1384580 NM SERVICE DOOR LEAKING A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 522AU 23857 BOS - FLT 783 - DURING CLIMB-OUT FROM BOS, CREW NOTICED A LEAKING AFT SERVICE DOOR SEAL. NO DOOR INDICATION WAS PRESENT IN COCKPIT. ONCE CREW WAS UNABLE TO PRESSURIZE AIRCRAFT, CAPTAIN ELECTED TO RETURN TO FIELD AT BOS. FLIGHT LANDED WIT HOUT INCIDENT WITH NO EMERGENCY BEING DECLARED. MAINTENANCE REMOVED DEBRIS FROM AFT SERVICE DOOR JAM, LEFT SIDE. LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001030500308 20010305 00308 NM 2001 3 5 USAASB01014 1 20010121 A 3610 1074922 REGULATOR BOEING 737 737301 1384611 NM NR 2 ENGINE FAILED A USAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 339US 41624 23236 BWI - FLT 1801 - EN ROUTE FROM BOS-ATL, THE CREW HAD TROUBLE MAINTAINING CABIN PRESSURIZATION. AT FL230, THE RIGHT BLEE D PRESSURE WENT TO 30 PSI WHILE THE LEFT STAYED AT 0. CABIN ALTITUDE CLIMBED TO OVER 10,000 FEET AND SET OFF THE CABIN ALTITUDE WARNING HORN. CREW DESCENDED FLIGHT TO FL100 AND THEN DIVERTED TO BWI WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE INSPECTED AIRCRAFT AND RAN BOTH ENGINES. REMOVED AND REPLACED THE RI GHT ENGINE BLEED AIR REGULATOR. RAN ENGINES AGAIN. BLEED PRESSURE OPS CHECKS NORMAL. PRESSURIZATION OPS CHECKS NORMAL . (M) 2 L 7 2 4F RT A16WE 2001030500309 20010305 00309 NM 2001 3 5 USAASB01020 1 20010123 A 2131 106120913 CONTROLLER BOEING 737 7373B7 1384580 NM EE BAY FAILED A USAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 506AU 58302 23381 CLT - FLT 1187 - EN ROUTE FROM IAH TO CLT, CRUISING AT FL330, THE CABIN ALTITUDE CLIMBED TO 10 WITH WARNING HORN SOUNDIN G. CREW DESCENDED THE FLIGHT TO FL110, WHEREAS UPON DESCENDING THROUGH FL160, THE WARNING HORN SILENCED. FLIGHT CONTIN UED ON TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER. TEST ED GOOD PER MM 21-31-00. ALSO, FOUND THE AFT CARGO DOOR SEAL TORN AND HANGING OUT. REMOVED AND REPLACED THE AFT CARGO DOOR SEAL (P/N 10-60821-4) PER MM 52-09-12. PRESSURIZED AIRCRAFT. LEAK CHECKED GOOD. (M) 2 L 7 2 4F RT A16WE 2001030500310 20010305 00310 NM 2001 3 5 USAASB01007 1 20010115 A 2913 PMP2V7D10 PUMP BOEING 737 737301 1384611 NM MLG W/W FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 592US 15217 23937 PIT - FLT 9228 - DURING CRUISE, EN ROUTE FROM YUL-YYZ, THE NR 2 ELECTRIC HYDRAULIC PUMP OVERHEAT LIGHT ILLUMINATED. DEC ISION WAS MADE FOR FLIGHT TO DIVERT TO PIT. FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DELCARED. MAINTENANCE RE MOVED AND REPLACED THE NR 2 ELECTRIC HYDRAULIC PUMP PER MM 29-15-21. REPLACED PRESSURE AND CASE DRAIN FILTERS AND FLUSH ED METAL FROM CASE DRAIN LINE. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001030500311 20010305 00311 NM 2001 3 5 USAASB01010 1 20010118 A 3297 WIRE BOEING 737 737301 1384611 NM SELECTOR LEVER DISCONNECTED A K NONE O OTHER CL CLIMB 1 EA 19 337US 23235 PIT - FLT 276 - AFTER TAKEOFF FROM AVP, EN ROUTE TO PIT, THE LANDING GEAR HANDLE WOULD NOT MOVE BEYOND THE OFF POSITION. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES. LANDING GEAR HANDLE WAS MOVED TO THE DOWN POSITION, FLAPS WERE RET RACTED AND THE GEAR OVERRIDE TRIGGER WAS PULLED. LANDING GEAR HANDLE WAS MOVED TO THE UP AND OFF POSITION AND THE GEAR RETRACTED. FLIGHT CONTINUED ONTO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR LEVER LATCH SOLENOID (P/N A420-060283-05) PER MM 32-31-31 WITH NO HELP. FOUND GROUND WIRE FOR LANDING GEAR LEVER LATCH SOLENOID AT AIR SENSING SWITCH S-1 OFF OF PIN. RECONNECTED SOCKET. CHECKED OPERATION OF LATCH SOLENOID PER MM 32 2 L 7 2 4F RT A16WE 2001030500312 20010305 00312 NM 2001 3 5 USAASB01012 1 20010119 A 3260 WARNING SYSTEM BOEING 737 737301 1384611 NM COCKPIT MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 346US 23515 ORF - FLT 12 - AFTER TAKEOFF FROM MCO, CREW RECEIVED A RIGHT MLG RED LIGHT WHEN PLACING THE GEAR HANDLE TO THE UP POSITI ON AS WELL AS THE OFF POSITION. AFTER RECYCLING GEAR TO THE DOWN POSITION, INDICATIONS WERE NORMAL AS THREE GEAR GREEN LIGHTS ILLUMINATED. WHEN GEAR HANDLE WAS MOVED UP, THE RIGHT MLG RED LIGHT RE-ILLUMINATED AS WELL AS WHEN MOVED TO THE OFF POSITION. CREW DETERMINED RT MLG GEAR WAS DOWN AFTER QUICK REFERENCE HANDBOOK PROCEDURES WERE COMPLIED WITH. FLIGH T DIVERTED TO ORF DUE TO HIGH FUEL BURN AND CONCERN FOR ICING CONDITIONS IN PHL. FLIGHT LANDED WITHOUT FURTHER INCIDENT . NO EMERGENCY WAS DECLARED. MX JACKED AIRCRAFT PER MM 07-11-11 CHECKED OPERATION OF MLG EXTENSION AND RETRACTION SYST 2 L 7 2 4F RT A16WE 2001030600026 20010306 00026 EU 2001 3 6 CA010111016 1 20010104 A 3010 9598901031 BOOT PILATS PC12 PC1245 EU DEICE SYSTEM DELAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA 1205 (CAN) ON ANNUAL INSPECTION DE-ICE BOOTS WERE INFLATED FOR FUNCTIONAL TEST. THE INFLATION RIBS ON THE INBOARD BOOTS AT TR AILING EDGE BOTTOM WERE, FOUND TO BE DELAMINATING TOWARD THE TRAILING EDGE. NEW BOOTS WERE ORDERED AND BOTH SIDES REPLAC ED. 1 L 7 1 3T RT A78EU 2001030600034 20010306 00034 2001 3 6 CA010112005 4 20010102 A 3425 CIRCUIT BREAKER COLLINS 332E4 SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE HSI SYSTEM POPPED W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA (CAN) NR1 HSI SYSTEM CIRCUIT BREAKER POPPED AND COULD NOT BE RESET. AIRCRAFT RETURNED TO THE GATE AND MAINTENANCE FOUND NR1 SLAVING ACCESSORY CAUSING THE FAULT. SLAVING ACCESSORY REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 2001030600069 20010306 00069 2001 3 6 DL78K010064 4 20010113 A 3418 285A10104 COMPUTER BOEING 737 737832 13844CF NM STALL YAW FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 3731T 30775 DURING CLIMB YAW DAMP LIGHT ILLUMINATED AND YAW DAMP SWITCHED OFF. CREW FELT AIRCRAFT WAS UNSAFE AND DECLARED AN EMERG ENCY. REPLACED NR 1 STALL WX/YAW COMPUTER. 2 L 7 2 4F RT A16WE 2001030600070 20010306 00070 NE 2001 3 6 SWAA010182 2 20010119 A 7300 8063208 EEC BOEING 737 7373Q8 1384670 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE ERRATIC A SWAA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SW 07 663SW 23256 721392 DIVERSION, DECLARED EMERGENCY. NR 1 ENGINE ROLLED BACK. EGT DROPPED RAPIDLY AND OTHER INDICATIONS FLUCTUATED FOR APPRO X 10 SECONDS. NOTED A STRONG ODOR IN THE COCKPIT. ENGINE RECOVERED ON ITS OWN AND ODOR DISSAPATED AFTER ABOUT 10 MINUT ES. NR 1 ENG FUEL SHUT OFF VALVE C/B TRIPPED WHEN FUEL CUT OFF. REMOVED AND REPLACED FUEL PUMP (P/N 301-779-005) AND M EC OPS, LEAK CHECK AND TRIM GOOD PER MM. REPAIRED FUEL SHUT OFF VALVE WIRING AT DISCONNECT BRACKET, STA 720L, PER MM. OPS CHECK NORMAL PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2001030600072 20010306 00072 EU 2001 3 6 DHL2001367501 1 20010131 A 3213 A2551305600151 STRUT AIRBUS 300 A300B4203 3930306 EU LT MLG CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH MSN265 C CHECK, LT FWD MLG GUIDE STRUT CRACKED IN TWO PLACES BOTH 3 INCHES. REPLACED GUIDE STRUT IAW SRM 51-30-10. (NON ROUTI NE 80866) 2 L 7 2 4F RT A35EU 2001030600073 20010306 00073 EU 2001 3 6 DHL2001367502 1 20010130 A 5230 A2557328800000 BRACKET AIRBUS 300 A300B4203 3930306 EU CARGO DOOR SHEARED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH MSN265 C-CHECK, AFT CARGO DOOR ACTUATOR PANEL BRACKET (OUTBOARD) SHEARED. REPLACED CARGO DOOR ACT-PANEL BRACKET IAW STD PRACTI CE AND IPC 25-52-11 FIG 5 PG 5 NR 78882. 2 L 7 2 4F RT A35EU 2001030600074 20010306 00074 EU 2001 3 6 DHL2001367503 1 20010131 A 5540 STRUCTURE AIRBUS 300 A300B4203 3930306 EU RUDDER DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH MSN265 C CHECK, SLIGHT DAMAGE TO TRAILING EDGE OF RUDDER BETWEEN RIBS 25 AND 26. REPAIRED TRAILING EDGE IAW SRM 55-40-00 PG 74 0 PAINTED AREA. NR 80921 2 L 7 2 4F RT A35EU 2001030600075 20010306 00075 EU 2001 3 6 DHL2001367504 1 20010126 A 5523 STRUCTURE AIRBUS 300 A300B4203 3930306 EU LT ELEVATOR TAB DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH MSN265 C-CHECK, LT ELEVATOR TIP OUTBOARD DAMAGE TO AFT 3 FASTENERS DUE TO POSSIBLE LIGHTNING STRIKE. DAMAGE TO ELEVATOR TIP RE PAIRED IAW SRM 51-42-20. NR 78820 2 L 7 2 4F RT A35EU 2001030600076 20010306 00076 EU 2001 3 6 DHL2001367505 1 20010130 A 5512 STRUCTURE AIRBUS 300 A300B4203 3930306 EU HORIZONTAL STAB DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH MSN265 C-CHECK, THS 341AB RT SIDE HAS SLIGHT SURFACE DAMAGE AROUND O/B EDGE. (NON-ROUTINE 78827) SCRATCHES REMOVED FROM L/E I AW SRM 51-40-10, MATERIAL REMOVED 0.001 TO 0.002 INCH WITHIN LIMITS OF SRM 55-10-00, REPROTECTED AREA. 2 L 7 2 4F RT A35EU 2001030600077 20010306 00077 EU 2001 3 6 DHL2001367009 1 20010128 A 5753 MS2125005034 BOLT AIRBUS 300 A300B4203 3930306 EU FLAP TRACK CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH MSN265 C-CHECK--BOLTS AND NUTS CORRODED AT RT FLAP BEAM NR 3 & 6, AT BRACKETS FOR SCREWJACK, NR 79748. REPLACED NUT AND BOLT O N NR 3 & 6 FLAP BEAMS. NUT (P/N NSA5177-5). 2 L 7 2 4F RT A35EU 2001030600079 20010306 00079 WP 2001 3 6 UPS01834965 1 20010213 A 3510 15830N REGULATOR DOUG DC8 DC873F 302199F WP COCKPIT OXYGEN FAILED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:IN CAPTS OXYGEN REGULATOR INOP. *S/D* REMOVED AND REPLACED CAPTS REGULATOR P/N 15830N, S/N OFF 01065/0 1377. REPLACED HOSE CLAMP ON FLEX LINE AT MASK BOX. SYSTEM CK''D GOOD. 2 L 7 4 4F RT 4A25 2001030600080 20010306 00080 WP 2001 3 6 DHL2001803004 1 20010214 A 2720 CONTROL UNIT DOUG DC8 DC873F 302199F WP RUDDER MALFUNCTIONED A DHLA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SO 01 803DH 46123 RUDDER CONTROL CHECK DID NOT HAVE INDICATION ON HYD SYS GAUGE. INSPECTED AND OPS CHECK RUDDER HYD SYS PER MM 27-21-6. NO DEFECTS NOTED. INSPECTED FLAP PRESS REDUCER VALVE AND LINKAGE PER MM 27-21-7. NO DEFECTS NOTED. PERFORMED RUDDER C ONTROL CHECK AND OBSERVED DEFLECTION ON HYD SYS PRESSURE INDICATOR. 2 L 7 4 4F RT 4A25 2001040400173 20010404 00173 2001 4 4 2001UALA00075 4 20010202 A 2565 SLIDE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE PAX DOOR FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1856U 46975 DOOR 4 LEFT SLIDE PRESSURE LIGHT ON. CHECK OF SLIDE PRESSURE WITH OHM METER SHOWS 0 WHICH IS A BAD SLIDE. *S/D* THE S LIDE FROM AC 3056 WAS ROBBED AND INSTALLED ON AC 3058. WHEN 3058 LATER RETURNED TO ORD, THE SLIDE WAS REMOVED, A SERVIC EABLE SLIDE WAS INSTALLED AND THE SLIDE OFF, WAS REINSTALLED ON AC 3056 (WHICH WAS BEING PREPPED FOR RETIREMENT). THE O RIGINAL SLIDE WHICH FAILED FROM 3058 WAS DUE TO A LOW BOTTLE READING. EG IS UNABLE TO PERFORM A FAILURE ANALYSIS, BECAUS E THE SLIDE AND THE AC ARE RETIRED IN THE DESERT. THE FAILED SLIDE WAS CHECKED A SECOND TIME WITH A SIMPSON 260 METER, AND THE SLIDE CHECKED OK. 2 L 7 3 4F 4 F A22WE E23EA 2001041600047 20010416 00047 NM 2001 4 16 2001UALA00079 1 20010204 A 2421 50086003MOD CIRCUIT BREAKER HARTMAN 50086003MOD BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE E&E BAY FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7284U 21562 AIRCRAFT RETURNED TO DEN DUE TO A DIFFERENTIAL FAULT ON NR 1 GENERATOR. *S/D* MAINTENANCE REPLACED NR 1 GENERATOR BREA KER. NO FURTHER PROBLEMS REPORTED. 2 L 7 3 4F 4 F A3WE E2EA 2001041100032 20010411 00032 NM 2001 4 11 2001UALA00086 1 20010206 A 2780 FSEU 285T0049 BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE L/E FLAP MALFUNCTIONED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 29 609UA 21870 L/E SLAT ASSYM EICAS MSG AND ASSOC LIGHT ILLUM WHEN FLAP HANDLE PLACED TO ZERO. SLAT INDICATION STICKS BETWEEN 1 AND ZE RO. PER FLT MANUAL IRREG 7-40 CYCLE FLAPS TO EXTEND, NO HELP. L/E ASSYM RETURNED UPON RETRACT SELECTION. PER FLT MANU AL DID NOT SELECT ALT L/E SYSTEM. AIRCRAFT RETURNED TO SFO. *S/D* NUISANCE MESSAGE GENERATED BY FLAP/SLAT ELECTRONICS UNIT (FSEU). REPLACED FSEU PER MM 27-51-01. RAN FLAPS AND SLATS TO FULL EXTEND AND RETRACT TWICE AND THEN ACCOMPLISHE D BITE CHECK OF FSEU. ALL OPERATIONS WERE NORMAL AND NO FAULTS FOUND. 2 L 7 2 4F 4 F RT A1NM E3NE 2001030600084 20010306 00084 NM 2001 3 6 2001UALA00087 1 20010206 A 3350 LIGHT BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN INTERMITTENT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 615UA 21876 RIGHT HAND FORWARD CABIN EEL LIGHTS COMES ON INTERMITTENTLY WITH SWITCH IN ARM POSITION. 2 L 7 2 4F 4 F RT A1NM E3NE 2001040400175 20010404 00175 NM 2001 4 4 2001UALA00088 1 20010205 A 2760 GM69375 TRANSFORMER GM69375600U BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SPOILER SYS FAILED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 547UA 25368 SPOILER EICAS AND OVERHEAD LIGHTS ILLUMINATED. FLIGHT LEVEL 380. *S/D* FAULTY RVDT ON SPOILER PCA CAUSING EICAS MESSA GE. REPLACED ROTARY VARIABLE DIFFERENTIAL TRANSFORMER ON SPOILER PCA NR 6 AND NR 7. 2 L 7 2 4F 4 F RT A2NM E17NE 2001040400177 20010404 00177 NM 2001 4 4 2001UALA00091 1 20010207 A 3350 582213 BATTERY PACK BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN DISCHARGED A UALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 29 615UA 21876 RIGHT SIDE EEL LIGHTS ON WITH OVERHEAD SWITCH IN THE ARM POSITION. *S/D* ADJUSTED EMERGENCY LIGHT MICROSWITCH ON OVERH EAD PANEL. CHECKED 28VDC CHARGING VOLTAGE AND GROUNDS, ALL OK. REPLACED EMERGENCY LIGHT POWER SUPPLY. (NOTE - EEL LIG HT PROBLEMS IN 2 PREVIOUS FLIGHTS ON 02/06/01) 2 L 7 2 4F 4 F RT A1NM E3NE 2001030600085 20010306 00085 NM 2001 3 6 2001UALA00094 1 20010208 A 3234 HANDLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE MLG STUCK A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 646UA 25283 UNABLE TO RAISE GEAR HANDLE WITHOUT USING OVERRIDE. 2 L 7 2 4F 4 F RT A1NM E24NE 2001040400178 20010404 00178 NM 2001 4 4 2001UALA00097 1 20010208 A 5754 651622189 RIB BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7461U 21915 NR 4 SLAT OUTBOARD SIDE OF ACTUATOR ROD END ATTACH POINT INTERNAL WEB CRACKED. *S/D* REPAIRED RIB IN ACCORDANCE WITH O VERHAUL MANUAL. 2 L 7 3 4F 4 F A3WE E2EA 2001030600086 20010306 00086 WP 2001 3 6 ABXA010047 1 20010213 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC931 3022065 WP FUSELAGE DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 924AX 3547 47403 COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERIES IAW DC-9 MM 33-53-00. LATER ON 02/13/01 THE EMERGENCY LIGHT POWER SUPPLY WAS ALSO REPLACED FOR RELIABILITY CONCERNS. 2 L 7 2 4F A6WE 2001030600087 20010306 00087 WP 2001 3 6 ABXA010048 1 20010207 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC931 3022065 WP FUSELAGE DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 943AX 8746 47528 EMERGENCY LIGHTS WOULD NOT ILLUMINATE WHEN SELECTED ON. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERIE S IAW DC-9 MM 33-53-00. LATER ON 02/07/01 MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY FOR RELIABILITY CONCERN S, IAW DC-9 MM 33-53-02. 2 L 7 2 4F A6WE 2001030600088 20010306 00088 WP 2001 3 6 ABXA010049 1 20010207 A 3310 ELECTRICAL BOX DOUG DC9 DC941 302207N WP COCKPIT LIGHTS ODOR A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 23 953AX 47608 A HOT ELECTRICAL ODOR WAS NOTED COMING FROM THE FORWARD CENTER CONSOLE AREA. WHEN THE FORWARD CONSOLE CIRCUIT BREAKER W AS PULLED, THE ODOR SUBSIDED. MAINTENANCE INSPECTED THE PEDESTAL LIGHTS SWITCH BOX AND CONSOLE AREA WIRING. NO DEFECTS WERE NOTED. MAINTENANCE OPERATED LIGHTS FOR 20 MINUTES. NO ODORS OR DEFECTS WERE NOTED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001030600089 20010306 00089 WP 2001 3 6 ABXA010050 1 20010213 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP FUSELAGE DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 979AX ABX8145 47492 THE COCKPIT EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE INSPECTED AND REPLACED THE COCKPIT EMERGENCY LIGHT BATTERIES I AW DC-9 MM 33-53-00. LATER ON 02/13/01 MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY AS A RELIABILITY PRECAUTIO N IAW DC-9 MM 33-53-02. 2 L 7 2 4F A6WE 2001030600091 20010306 00091 EU 2001 3 6 DHL2001367509 1 20010213 A 5330 SKIN AIRBUS 300 A300B4203 3930306 EU FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH MSN265 C-CHECK, SKIN DAMAGE AT FR 59A & FR 63A AFT CARGO DOOR CUTOUT. SKIN BLENDED IAW SRM 51-40-11, BLENDED DEPTH MAX 0.015 I NCH REMOVED WITHIN LIMIT OF SRM 53-10-00 FIG 605A, REPROTECTED. NON ROUTINE 80927. 2 L 7 2 4F RT A35EU 2001030600092 20010306 00092 WP 2001 3 6 ABXA010051 1 20010214 A 2130 7760417 DUCT DOUG DC8 DC863 302198A WP NR 1 DISCHARGE FAILED A ABXA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 23 821AX 46116 A LOUD BANG WAS HEARD PASSING THROUGH FL22 FOLLOWED BY RAPID CABIN DECOMPRESSION. THE FLIGHT CREW DONNED OXYGEN MASKS A ND RETURNED TO EWR WHERE THE AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE INSPECTED AND REPLACED THE NR 1 CABIN DISCHARGE DUCT ASSEMBLY, COUPLING AND O-RINGS. PRESSURIZATION CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2001030600093 20010306 00093 WP 2001 3 6 ABXA010052 1 20010213 A 3297 WIRE DOUG DC9 DC932 3022066 WP LT MLG DAMAGED A ABXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 939AX 47201 THE LEFT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED INTERMITTANTLY. THE FLIGHT RETURNED TO ILN TO COMPLETE REPAIRS. MA INTENANCE INSPECTED AND REPAIRED A WIRE FOR CONNECTOR P1-130 PIN NR 4. LANDING GEAR OPERATIONAL CHECKS WERE COMPLETED A ND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001030600094 20010306 00094 NM 2001 3 6 F3LA200100017 1 20010213 A 5315 BAC1505100617 FLOORBEAM BOEING 737 7373S1 138447S NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 24856 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ACROSS TOP OF AFT FUSELAGE FLOORBEAM AT STA 967. REPLACED FLOORBEAM CAP AT STA 967 FROM LBL 37.5 TO RBL 36 PER SRM 53-00-51. 2 L 7 2 4F RT A16WE 2001030600095 20010306 00095 NM 2001 3 6 DHL2001712503 1 20010201 A 5320 INTERCOSTAL BOEING 727 72729 1384007 NM FUSELAGE BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 C-CHECK, FWD CARGO COMPARTMENT BEAM LOWER PART INTERCOSTAL BROKEN 1.0 INCH (CEILING) AT STA 540.000 LBL 43.0 INCH. PERF ORMED STOP DRILL HOLE IAW SRM 51-10-1, PAGE 6. FABRICATED DOUBLER WITH ALCLAD 2024, T3, 0.032 INCH, 5 X 3 INCH IAW SRM 51-40, PAGE 1. TREATED AND PRIMED IAW SRM 51-10-2 PAGE 1 AND 2. INSTALLED DOUBLER IAW SRM 51-32-0, PAGE 1 AND 2. (NON -ROUTINE CARD 0915). 2 L 7 3 4F A3WE 2001030600096 20010306 00096 EU 2001 3 6 DHL2001367520 1 20010213 A 5330 SKIN AIRBUS 300 A300B4203 3930306 EU FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH MSN265 C-CHECK, SKIN DAMAGE AT FR 20A & FR 25A FWD CARGO DOOR CUTOUT. SKIN BLENDED IAW SRM 51-40-11, BLEND DEPTH 0.10 WITHIN L IMITS OF SRM 53-13-00 FIG 603. RETREATED AREA. 2 L 7 2 4F RT A35EU 2001030600097 20010306 00097 NM 2001 3 6 DHL2001701001 1 20010212 A 5753 SKIN BOEING 727 72730C 1384009 NM TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 REFERENCE DMI 4025 RT O/B MID FLAP INSP OF REPAIR NEXT 30 DAYS AT 5 DAY INTERVALS TILL REPAIR COMPLETED. REMOVED TEMP R EPAIR, INSTALLED PERM REPAIR RT O/B MID FLAP THAT WAS DELAMINATED, IAW BOEING 727 SRM 51-40-20. 2 L 7 3 4F A3WE 2001030600098 20010306 00098 NM 2001 3 6 DHL2001712509 1 20010205 A 5320 ANGLE BOEING 727 72729 1384007 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 C-CHECK, MAIN CARGO COMPART CABLES PLACARD PROTECTIVE ANGLE CRACKED 0.50 INCH AT RBL 20 INCH BETWEEN STA 930.000 AND STA 940.000. PERFORMED STOP DRILL IAW SRM 51-10-1, PAGE 6B. FABRICATED DOUBLER (2024, T3, 0.032 INCH) IAW SRM 51-40, PAGE 1. CLEANED, TREATED, AND PRIMED IAW SRM 51-10-2, PAGE 1-2. INSTALLED DOUBLER IAW SRM 51-40, PAGE 1. (NON-ROUTINE CAR D 0583). 2 L 7 3 4F A3WE 2001030600099 20010306 00099 NM 2001 3 6 DHL2001712510 1 20010201 A 5720 SUPPORT BRACKET BOEING 727 72729 1384007 NM HYDRAULIC LINE BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 C-CHECK, NR 4 GROUND SPOILER AFT ACTUATOR HYDRAULIC TUBING ATTACH SUPPORT BROKEN. REMOVED BROKEN SUPPORT IAW SRM 51-30- 2, PAGE 1-2. FABRICATED SUPPORT T-ANGLE (EXTRUDED 7075, T6) IAW SRM 51-20-2, FIG 6. CLEANED, TREATED, AND PRIMED IAW S RM 51-10-2, PAGE 1-2. INSTALLED NEW SUPPORT IAW SRM 51-30-2, PAGE 1-2. (NON-ROUTINE CARD 0612). 2 L 7 3 4F A3WE 2001030600100 20010306 00100 EU 2001 3 6 RAIA00102002 1 20010214 A 3230 1469 RELAY AEROSP ATR42 ATR42300 8680920 EU MLG FAILED A RAIA O OTHER J WARNING INDICATION CL CLIMB 1 CE 03 426TE 228 7136-STL-DURING CLIMBOUT LANDING GEAR WOULD NOT RETRACK. MAINTENANCE REMOVED AND REPLACED RELAY 1469 IAW ATR42 MAINTENA NCE MANUAL. 2 H 7 2 4T RT A53EU 2001030600101 20010306 00101 EU 2001 3 6 DHL2001366009 1 20010207 A 2760 TRANSMITTER AIRBUS 300 A300B4203 3930306 EU SPOILER LACK OF LUBE A DHLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 366DH 249 DURING TAXI AND FLIGHT CONTROL CHECKS, FLIGHT SPOILER INDICATION ON RIGHT SIDE ONLY CAME UP TO 10 DEGREES. LEFT SIDE WA S SLUGGISH AND SLOW TO COME UP TO Y DEGREES. CLEANED, LUBED AND EXERCISED SPOILER XMTR ARM LINKAGE. OPERATIONAL CHECK PER MM 27-65-00 GOOD ON GROUND. THIS CLEARS DMI 4311 PLACARD REMOVED. 2 L 7 2 4F RT A35EU 2001030600102 20010306 00102 NM 2001 3 6 DHL2001707002 1 20010212 A 5310 FASTENER BOEING 727 72722 1384002 NM FUSELAGE LOOSE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 DURING A/C RECEIVING INSPECTION FOUND LOOSE BLIND FASTENERS ON EXTERNAL SKIN REPAIR BS 218, STRINGER 25R. REMOVED EXTER NAL SKIN REPAIR AND BLIND FASTENERS. INSTALLED EXTERNAL REPAIR WITH SOLID FASTENERS AT BS 218, STRINGER 25R IAW B727 SR M 53-30-3. 2 L 7 3 4F A3WE 2001030600103 20010306 00103 WP 2001 3 6 TWAA0103001 1 20010212 A 5315 WEB DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 992Z 47095 DURING OP 15 MAINT CHECK THE CABIN SUB FLOOR MEMBRANE WAS CORRODED AT STA 160 TO 200, LBL 21 AND LBL 42 INCHES. REMOVED CORRODED MEMBRANE AND INSTALLED NEW SECTION AT STA 160 TO 200, LBL 21 IN AND LBL 42 IN, PER SRM 53-01, FIG 2 AND SRM 51 -30-02. 2 L 7 2 4F A6WE 2001030600104 20010306 00104 WP 2001 3 6 TWAA0103002 1 20010213 A 5320 FLOOR SUPPORT DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 992Z 47095 DURING OP 15 MAINT CHECK, THE CABIN FLOOR SUPPORT WAS CORRODED AT BL ZERO, STA 160 TO 200 AND 218 TO 229. INSTALLED NEW FLOOR SUPPORTS AT BOTH LOCATIONS PER SPM 6-70-01 AND SRM 51-30-2. 2 L 7 2 4F A6WE 2001030600105 20010306 00105 WP 2001 3 6 TWAA0103003 1 20010213 A 5313 STRINGER DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 992Z 47095 DURING CHECK-C MAINT FOUND HEAVY CORROSION ON STRINGER 19R AT STA 180. REMOVED CORROSION ON STRINGER 18L, STA 150 TO 22 9, AND REPLACED WITH NEW LONGERON PER SRM 53-11-1, FIG 3, AND SRM 51-30-02 AND 51-30-5. 2 L 7 2 4F A6WE 2001030600106 20010306 00106 WP 2001 3 6 TWAA0103004 1 20010213 A 5320 PAN DOUG DC9 DC982 3022082 WP GALLEY DRAIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT AT THE RT SIDE FWD CABIN DOOR AREA, THE MEMBRANE AROUND AND UNDER THE FWD GALLEY DRAIN PAN HAD CORR OSION. REMOVED CORROSION PER SPM 6-80-01. INSTALLED DOUBLER PER SRM 53-01 FIG 2. INSTALLED FASTENERS PER SRM 51-30-02 . 2 L 7 2 4F A6WE 2001030600107 20010306 00107 WP 2001 3 6 TWAA0103005 1 20010213 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT THE RT SIDE FWD DOOR AREA, FWD GALLEY DRAIN PAN FLOOR SUPPORT HAD CORROSION. REPLACED OUTBOARD FLO OR SUPPORT PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-02. 2 L 7 2 4F A6WE 2001030600108 20010306 00108 WP 2001 3 6 TWAA0103006 1 20010213 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT CORRODED AT STA 160 TO 200, RBL 52 INCHES. REPLACED FLOOR SUPPORT AT STA 160 TO 200 PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-02 AND 51-30-5. 2 L 7 2 4F A6WE 2001030600109 20010306 00109 WP 2001 3 6 TWAA0103007 1 20010213 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT IN THE AFT CARGO COMPT, STA 1309, LONGERON 28R, THE FORMER REPAIR WAS CORRODED. FABRICATED NEW SPL ICE PER SPM 6-70-01. INSTALLED REPAIR AND FASTENERS PER SRM 51-10-05. 2 L 7 2 4F A6WE 2001030600110 20010306 00110 WP 2001 3 6 TWAA0103008 1 20010213 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9401W 53137 DURING CHECK-C MAINT THE NUMBER 4 CABIN FLOOR TRACK WAS CORRODED AT STA 200 TO 229. SPLICED SECTION OF TRACK PER SRM 53 -05, FIG 4F. 2 L 7 2 4F RT A6WE 2001030600111 20010306 00111 WP 2001 3 6 TWAA0103009 1 20010213 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT FOUND FORMER CORRODED AT STA 1212, LONGERON 26 TO 27L. REMOVED CORROSION BY REPLACEMENT OF PART. INSTALLED NEW FRAME PER PRINT 9936073. 2 L 7 2 4F A6WE 2001030600112 20010306 00112 WP 2001 3 6 TWAA0103010 1 20010214 A 5313 LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING CHECK-C MAINT FOUND LONGERON REPAIR AT STA 1079, LONGERON 2R, WAS CRACKED 1.5 INCHES. REPAIRED PER SRM 53-02. 2 L 7 2 4F A6WE 2001030600113 20010306 00113 WP 2001 3 6 TWAA0103011 1 20010214 A 5530 ATTACH ANGLE DOUG DC9 DC931 3022065 WP VERTICAL STAB CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING CHECK-C MAINT IN THE VERT STAB FOUND CRACK IN RT AFT VERTICAL ATTACH ANGLE. CUT OUT CRACKED AREA AND FABRICATED FILLER AND REPAIR ANGLE AND INSTALLED PER SRM 53-05, FIG 23. 2 L 7 2 4F A6WE 2001030600114 20010306 00114 NM 2001 3 6 UPS01234996 1 20010215 A 3350 1000679 LIGHT BOEING 727 72730C 1384009 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:IN ON PREFLIGHT CHECK EMERGENCY EXIT LIGHT OVER COCKPIT DOOR WOULD NOT TEST WITH EMERGENCY EXIT LIGHT SW ITCH ON O/H. LIGHTS WORK OK AT LIGHT ASSY W/SWITCH ON. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY AT COCKPIT DOOR. OPS CHECK OK PER MM 33-50-101. 2 L 7 3 4F A3WE 2001030600115 20010306 00115 NM 2001 3 6 UPS01434969 1 20010107 A 5230 65B083449 FITTING BOEING 747 747123F NM PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, NR 3 ENTRY DOOR BS 1265 LT SIDE HINGE FITTING CRACKED. FITTING REPLACED IAW SRM 51-30-02. 2 L 7 4 4F A20WE 2001030600116 20010306 00116 NM 2001 3 6 UPS01434970 1 20010106 A 5320 015U057971 STOP BOEING 747 747123F NM PAX DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, NR 3 DOORWAY LT STOP FITTINGS NR 2 & 4 FWD STOP FITTINGS CRACKED. FITTINGS REPLACED IAW SRM 51-30-02 . 2 L 7 4 4F A20WE 2001030600117 20010306 00117 NM 2001 3 6 UPS01434971 1 20010106 A 5320 015U057972 FITTING BOEING 747 747123F NM PAX DOORWAY CRACKED A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, DOOR 3 RT STOP FITTINGS FWD NR 2 & 5 CRACKED. NOTE DOORWAY STOP FITTINGS NOT DOOR. FITTINGS REPLACE D IAW SRM 51-30-02. 2 L 7 4 4F A20WE 2001030600118 20010306 00118 NM 2001 3 6 UPS01434972 1 20010103 A 2780 65B107803 FITTING BOEING 747 747123F NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, RT WING L/E INBOARD UPSTOP FITTING IS CRACKED ON INBOARD LINKAGE OF VCF 20. UP STOP FITTING REPLACE D IAW SRM 51-30-02. 2 L 7 4 4F A20WE 2001030600119 20010306 00119 NM 2001 3 6 UPS01434974 1 20010119 A 3510 275501 SHUTOFF VALVE BOEING 747 747123F NM CREW OXYGEN LEAKING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, DURING CREW OXY SYS LEAK CHECK. FOUND CREW OXY SYS SHUT OFF VALVE LEAKING. REPLACED CREW OXYGEN SHU TOFF VALVE. 2 L 7 4 4F A20WE 2001030600120 20010306 00120 NM 2001 3 6 UPS01434976 1 20010124 A 5310 SHEAR TIE BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, FWD CARGO RT SIDE SHEAR TIE CRACKED AT BS 940 STR 38 & 39 RT. REPAIR CARRIED OUT IAW SRM 53-10-04. 2 L 7 4 4F A20WE 2001030600121 20010306 00121 NM 2001 3 6 UPS01434977 1 20010129 A 5310 SHEAR TIE BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, FWD CARGO CRACK FOUND IN SHEAR TIE AT BS 960- STR 37 & 38 LT. SHEAR TIE REPLACED IAW SRM 53-10-04. 2 L 7 4 4F A20WE 2001030600122 20010306 00122 NM 2001 3 6 UPS01434978 1 20010119 A 5320 BRACKET BOEING 747 747123F NM APU BAY DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, APU AREA DAMAGED BRACKET ON UPPER DETECTOR U-BRACKET. NEW BRACKET FABRICATED IAW SRM 51-20-01. 2 L 7 4 4F A20WE 2001030600123 20010306 00123 NM 2001 3 6 UPS01434981 1 20010116 A 5410 STIFFENER BOEING 747 747123F NM NR 2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, NR 2 PYLON CRACK OTBD PYLON STIFFENER NAC 286. REPAIRED STIFFENER IAW SRM 54-14-03. 2 L 7 4 4F A20WE 2001030600124 20010306 00124 NM 2001 3 6 UPS01434987 1 20010106 A 5753 65B15650111312 SHAFT BOEING 747 747123F NM FLAP TRACK CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, NR 4, 2, 5, 6 AND 8 FLAP TRACK GENEVA SHAFTS CORRODED AND CHROME CHIPPED ON BRGS. FLAP TRACK ROLLER SHAFTS REPLACED, ALSO BEARINGS IAW MM 27-51-40. 2 L 7 4 4F A20WE 2001030600125 20010306 00125 NM 2001 3 6 UPS01434988 1 20010110 A 2750 554265 BALLSCREW BOEING 747 747123F NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, NR 1, 5, & 8 FLAP BALLSCREWS CORRODED AND NR 7 HAS WORN BOLT HOLE. BALLSCREWS 1, 5, 7 & 8 REPLACED I AW MM. 2 L 7 4 4F A20WE 2001030600126 20010306 00126 NM 2001 3 6 UPS01434989 1 20010107 A 5753 BACB30UU12K37 BOLT BOEING 747 747123F NM NR 4 FLAP TRACK CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, NR 4 FLAP TRACK AFT LOCATING MOUNT BOLTS AND SHIMS CORRODED. NR 4 FLAP TRACK AFT MOUNT BOLTS AND SHI MS REPLACED IAW MM 27-51-22. 2 L 7 4 4F A20WE 2001030600127 20010306 00127 WP 2001 3 6 UPS01834984 1 20010123 A 5320 3754047501 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1, 3, STA 350 RT LOWER CUSP FITTING IS CRACKED AT LONG 21R. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 3754047 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001030600128 20010306 00128 WP 2001 3 6 UPS01834986 1 20010124 A 5730 DOUBLER DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1,3, RIGHT WING NR 4 STUB WING L/E LOWER DOUBLER IS CRACKED AT XW485. REMOVED, FABRICATED AND REPLACE D DOUBLER IAW SRM 57-2-1A. 2 L 7 4 4F RT 4A25 2001030600129 20010306 00129 WP 2001 3 6 UPS01834997 1 20010215 A 5610 WINDOW DOUG DC8 DC873F 302199F WP COCKPIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:IN CAPTAINS CLEARVIEW WINDOW RIGHT LOWER CORNER APPEARS TO BE CRACKED. REMOVED AND REPLACED CAPTS CLEAR VIEW WINDOW PER MM 56-10-03 WINDOW CHECK NORMAL. 2 L 7 4 4F RT 4A25 2001030600130 20010306 00130 WP 2001 3 6 MWEA010156 1 20010213 A 5542 9957485511 SKIN DOUG DC9 DC981 3022081 WP RUDDER DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 LEFT LOWER SIDE OF RUDDER HAS FOUR DENTS ON SKIN. MAINTENANCE INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001030600131 20010306 00131 WP 2001 3 6 MWEA010155 1 20010209 A 5520 9918480501 SKIN DOUG DC9 DC932 3022066 WP LT ELEVATOR LIGHTNING STRIKE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 FOUND LIGHTNING STRIKE DAMAGE TO LEFT ELEVATOR OUTBOARD TRAILING EDGE. MAINTENANCE FABRICATED AND INSTALLED ELEVATOR SK IN REPAIR. 2 L 7 2 4F A6WE 2001030600132 20010306 00132 NM 2001 3 6 DL767010161 1 20010110 A 3150 HARNESS BOEING 767 767232 1385132 NM COCKPIT OVERHEATED A DALA O OTHER J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 104DA 22216 MULTIPLE EICAS WARNINGS AND AN ELECTRICAL BURNT SMELL IN COCKPIT AND MID CABIN. FOUND WIRE BUNDLE BURNED ABOVE P50 PANE L DUE TO CHAFING ON STRUCTURE. REPAIRED WIRE AND TESTED ON NR 1 THROUGH 120, EXCEPT 6, 7 AND 106. 2 L 7 2 4F RT A1NM 2001030600133 20010306 00133 NM 2001 3 6 DL72S010163 1 20010129 A 3350 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 544DA 22493 DURING STBY PWR CK LT SIDE OVERWING EXIT LIGHTS FAILED TO ILLUMINATE. REPLACED BATTERY PACK. ALL CHECKS NORMAL. 2 L 7 3 4F A3WE 2001030600134 20010306 00134 NM 2001 3 6 DLM88010165 1 20010129 A 2150 A/C PACK DOUG MD88 MD88 3023688 NM LEFT SMOKE A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 918DL 49583 SMOKE IN CABIN WHEN LEFT PACK A/C SWITCH TURNED ON. LEFT COCKPIT TEMP WENT FULL HOT, TURNED SWITCH OFF, SMOKE SUBSIDED. PERFORMED DUCT BURNOUT. 2 L 7 2 4F RT A6WE 2001030600135 20010306 00135 NM 2001 3 6 DL733010166 1 20010129 A 2120 UNKNOWN BOEING 737 737300 1384610 NM CABIN ODOR A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 242DL 23834 AFTER PUSHBACK BOTH ENGINES RUNNING, TWO F/A NOTICED ELECTRICAL ODOR AFT OF EMERGENCY EXITS, FWD OF AFT GALLEY. F/O CON FIRMS ELECTRICAL ODOR AROUND ROW 24 THE STRONGEST ODOR SEEMS TO DISSIPATE AFTER 3 - 4 MINUTES. RAN BOTH ENGINES, NTF. 2 L 7 2 4F RT A16WE 2001030600136 20010306 00136 NM 2001 3 6 DL72S010167 1 20010129 A 5754 ANGLE BOEING 727 727225A 1384077 NM NR 6 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 805EA 22436 FOUND ON C1 LETTER CK, TWO .25 INCH CRACKS IN THE NUMBER 6 SLAT LOWER COVE SKIN ATTACH ANGLE. REPAIRED PER MM 57-54-000 -8. 2 L 7 3 4F RT A3WE 2001030600137 20010306 00137 NM 2001 3 6 DL72S010168 1 20010129 A 3350 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 544DA 22493 ON L/O FOUND C-2 DOOR EMERGENCY FLOOD LIGHT INOP. REPLACED SAME. 2 L 7 3 4F A3WE 2001030600138 20010306 00138 2001 3 6 DL72L010169 4 20010130 A 3410 694859311 PANEL BOEING 727 727232 1384082 NM COCKPIT FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 512DA 21314 AT FL 330 CREW NOTICED ELECTRICAL FUMES/SMOKE EMINATING FROM OVERHEAD PANEL THROUGH CONTROL STAND LIGHT OPENING. STALL WARNING FAIL BATTERY C/B WAS POPPED, STALL WARNING PANEL WAS WARM TO TOUCH, WIND SHEAR FAIL LIGHT ALSO ILLUMINATED. FOU ND PRINTED CIRCUIT BOARD IN STALL WARNING PANEL BURNED PANEL ORDERED AGP FROM LAX. REPLACED SAME. 2 L 7 3 4F A3WE 2001030600139 20010306 00139 NM 2001 3 6 DL76S010170 1 20010126 A 5311 141T138033 FRAME BOEING 767 767332 1382001 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 124DE 23438 CORROSION WAS FOUND ON THE FWD FRAME AT THE CUTOUT FOR THE FWD LT PASSENGER DOOR. THE CORROSION WAS LOCATED ON THE AF T SURFACE OF THE FRAME WEB SURROUNDING THE GIRT BAR HOLE (JUST ABOVE CABIN FLOOR LEVEL). REPAIRED DAMAGE PER ER/A 39669 9-14. 2 L 7 2 4F RT A1NM 2001030600140 20010306 00140 NM 2001 3 6 DL76S010171 1 20010125 A 5330 141T32214 SKIN BOEING 767 767332 1382001 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 124DE 23438 FUSELAGE SKIN WAS DENTED DUE TO NOSE TIRE BLOWOUT. THE DENTS WERE APPROVED FOR INTERIM SERVICE PER ER/A 269377-14. THE DAMAGE WAS PERMANENTLY REPAIRED PER ER/A 269377-14 AT OVERHAUL MTC VISIT. REPAIRED DAMAGE PER ER/A 269377-14. 2 L 7 2 4F RT A1NM 2001030600141 20010306 00141 NM 2001 3 6 DL76S010172 1 20010130 A 2400 HARNESS BOEING 767 767332 1382001 NM CARGO BAY BURNED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 130DL 24080 ON L/O FOUND SEVERAL CIRCUIT BRAKERS POPPED. T/S AND FOUND WIRE BUNDLE SHORTED AND BURNT ABOVE C-1 CARGO DOOR CEILING. REPLACED/REPAIRED APPROX 80 WIRES. INCIDENT UNDER INVESTIGATION. 2 L 7 2 4F RT A1NM 2001030600142 20010306 00142 NM 2001 3 6 DL72L010173 1 20010130 A 2782 ACTUATOR BOEING 727 727232 1384082 NM NBR 4 SLAT LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 514DA 21430 SYSTEM A HYDRAULIC FLUID DECREASED BELOW 1 GALLON. TURNED OFF A-SYSTEM PUMPS AND COMPLIED WITH POM PROCEDURES FOR HYDRAULIC SYSTEM EMERGENCY. CRANKED GEAR AND FLAPS DOWN AND PERFORMED UNEVENTFUL LANDING AT 160000 LBS, RATE OF DESCEN T AT TOUCHDOWN WAS 400 FEET PER SECOND AT 150 KNOTS. REPLACED SLAT ACTUATOR, SERVICED HYDRAULIC SYS, LEAK CKS GOOD. 2 L 7 3 4F A3WE 2001030600143 20010306 00143 NM 2001 3 6 DL72S010174 1 20010131 A 3610 HARNESS BOEING 727 727225A 1384077 NM NR 2 ENGINE BURNED A DALA O OTHER O OTHER CR CRUISE 1 SO 27 8889Z 21858 NR 2 ENGINE RT ISOLATION VALVE WIRING HARNESS BURNT IN TWO. REPAIRED WIRING. SYS OP CKS GOOD. 2 L 7 3 4F RT A3WE 2001030600144 20010306 00144 NM 2001 3 6 DL757010175 1 20010122 A 5754 SKIN BOEING 757 757232 1384965 NM NR 1 SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 695DA 29727 SLAT DELAMINATED. NUMBER ONE SLAT SEALER CRACKED AND T/E WEDGE DELAMINATED AT UPPER OUTBD T/E. REF SUPPLEMENTAL CARD A TTACHMENT A. 2 L 7 2 4F RT A2NM 2001030600145 20010306 00145 NM 2001 3 6 DLM88010176 1 20010130 A 2121 TD19045001 RELAY DOUG MD88 MD88 3023688 NM RECIRC FAN INOPERATIVE A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 913DL 49544 AIRCRAFT OUT AND OFF AND RETURNED TO PHX DUE TO AN ODOR COMING FROM AIR CONDITIONING VENTS IN THE BACK CABIN. FOUND AIR CONDITIONING RECIRCULATING FAN INOP. FOUND FAN RELAY R2-278 BAD. REPLACED RELAY, FAN NOW OPERATES NORMALLY. ALSO NOT ED FLUID ACCUMULATION NEAR APU INLET. PERFORMED DUCT BURNOUT PROCEDURE PER OP 5088. CLEANED INLET SCREEN. 2 L 7 2 4F RT A6WE 2001030600146 20010306 00146 NE 2001 3 6 DL72S010177 2 20010131 A 7200 ENGINE BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 3 MISSING A DALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SO 27 543DA 75762 22392 687367 NR 3 OIL QTY DECREASE TO ZERO. DURING CRUISE FOLLOWED BY FLUCUATING OIL PRESS, SHUT DOWN NR 3 ENGINE PER POM. COMPLETE D ENGINE FLAME OUT / LOSS OF THRUST SHUTDOWN FORM. ENGINE SHUTDOWN TIME 30 MIN / OIL PRESS WINDMILL 25 PSI / OIL QTY 0. FOUND 3 STUDS ON GEARBOX BAD. REPAIRED SAME PER JT8D MANUAL, LEAK CKS GOOD. 2 L 7 3 4F 4 F A3WE E2EA 2001030600147 20010306 00147 NM 2001 3 6 DL72W010178 1 20010131 A 5754 SLAT TRACK BOEING 727 727247 138408F NM LE FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W 21057 DURING OVERHAUL THE INBD TRACK, CORROSION AND WEAR WAS FOUND, WHICH WERE BEYOND ALLOWABLE LIMITS, AT MLG BEAM ATTACH BOL T HOLE AND SPOTFACES, SPOILER BEAM ATTACH HOLES, THE MLG DOOR AFT HINGE FITTING HOLES, THE TOGGLE DETENT HOLE AND THE CL IP ASSEMBLY ATTACH BOLT HOLES. REPAIR PER ER/A 387604-14AD AND BF GOODRICH ENGINEERING REPAIR 23-0708. 2 L 7 3 4F A3WE 2001030600148 20010306 00148 NM 2001 3 6 DL72W010179 1 20010131 A 5753 FLAP TRACK BOEING 727 727247 138408F NM TE FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W 21057 DURING OVERHAUL, THE NR 4 INBD FLAP TRACK WAS FOUND WITH WEAR AND CORROSION, WHICH WAS BEYOND ALLOWABLE LIMITS, AT THE M LG BEAM ATTACH BOLT HOLES AND SPOTFACES, SPOILER BEAM ATTACH HOLES, HINGE SUPPORT FITTING ATTACH BOLT HOLES, AND THE C LIP ASSY ATTACH BOLT HOLES. REPAIR PER ER/A 401306-14AD AND BF GOODRICH ENGINEERING REPORT 23-0776. 2 L 7 3 4F A3WE 2001030600149 20010306 00149 NM 2001 3 6 DL72S010180 1 20010131 A 2780 SWITCH BOEING 727 727232 1384082 NM NR 6 LE FLAP SHORTED A DALA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 535DA 22048 AIR TURNBACK ACCOUNT LEADING EDGE AMBER LIGHT ON F/OS PANEL AT FLAPS 2 WITH S/OS PANEL LIGHTS INDICATING NORMAL. FLAPS NOT RETRACTED PAST 2 DEGREES INFLIGHT. FOUND NR 5 L/E FLAP SW S206 SHORTED. REPLACED SAME. 2 L 7 3 4F A3WE 2001030600150 20010306 00150 NM 2001 3 6 DL73K010181 1 20010131 A 5330 SKIN BOEING 737 737247 138448D NM WINDSHIELD POST CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 374DL 23521 FOUND AT N-1 LTR CK, CAPTS WINDSHIELD POST OUTER SKIN CRACKED AT UPPER FWD CORNER. REPAIRED PER SRM 53-30-3. 2 L 7 2 4F A16WE 2001030600151 20010306 00151 NM 2001 3 6 DL733010182 1 20010201 A 5312 65163007 BULKHEAD BOEING 737 737300 1384610 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 241DL 23833 THE CENTER WEB OF THE FS 178 BULKHEAD WAS FOUND CRACKED AT WL 195 AT BOTH LBL 5 AND RBL 5. THE CRACKS WERE REPAIRED PER S/B 737-53A1173, REV 3. 2 L 7 2 4F RT A16WE 2001030600152 20010306 00152 NM 2001 3 6 DL757010183 1 20010121 A 5414 SKIN BOEING 757 757232 1384965 NM NR 2 NACELLE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 686DA 27589 716596 PYLON SKIN CRACKED AT TORQUE BOX FWD I/B ACCESS CUTOUT FWD UPPER CORNER. REPAIRED PER SRM 54-51-01-2-2. 2 L 7 2 4F RT A2NM 2001030600153 20010306 00153 NM 2001 3 6 DL757010184 1 20010122 A 5414 SKIN BOEING 757 757232 1384965 NM LT WING PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 686DA 27589 NR 1 PYLON CRACKED O/B FWD AT 433AL CUTOUT AFT UPPER CORNER. REPAIRED PER SRM 54-51-01-2-2. 2 L 7 2 4F RT A2NM 2001030600154 20010306 00154 NE 2001 3 6 DL76L010185 2 20010201 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 FAILED A DALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 199DN 42913 0 28456 724144 AT 400 FT RIGHT ENGINE COMPRESSOR STALL. BOTH TOWER AND PASSENGERS REPORTED SMOKE FROM RIGHT ENGINE. THROTTLE RETARDED TO IDLE AND RETURNED FOR LANDING IN SFO. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 2001030600155 20010306 00155 NE 2001 3 6 DL73E010186 2 20010201 A 7200 ENGINE BOEING 737 737247 138448D NM PWA JT8 JT8D15A 52051 NE NR 1 FOD A DALA C ABORTED TAKEOFF C F.O.D. TO TAKEOFF 1 SO 27 245WA 34175 0 23519 709225 ON T/O ROLL, LOUD BANG W/ FULL PWR FELT VIBRATIONS. ABORTED T/O AT 10 KTS. PASSENGER REPORTED FLASH FROM AFT OF NR 1 E NG. PASSENGERS REPORTED BURNING SMELL IN CABIN AFTER BANG. FOUND NR 1 ENGINE INGESTED PLASTIC BAG. PERFORMED BORESCOP E OF NR 1 ENGINE PER PFHB, CHECKS GOOD. 2 L 7 2 4F 4 F A16WE E2EA 2001030600156 20010306 00156 NM 2001 3 6 DL72W010187 1 20010201 A 2750 TRANSMITTER BOEING 727 727247 138408F NM TE FLAP FAILED A DALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 27 2820W 21058 OUTBOARD FLAPS WOULD NOT RETRACT. AIR TURNBACK. INSPECTED FLAP, NO DAMAGE NOTED. RETRACTED FLAPS, NORMAL OPERATED FLA PS AND NO DEFECTS NOTED. FOUND RT O/B FLAP TRANSMITTER CANNON PLUG EXCESSIVELY LOOSE. CLEANED AND RESECURED PLUG. REP LACED RT O/B TRANSMITTER, FLAP PER MM OPS CKS NORMAL. 2 L 7 3 4F A3WE 2001030600157 20010306 00157 NM 2001 3 6 DL72S010189 1 20010201 A 5320 WEB BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 517DA 21433 A .375 INCH CRACK AT UPPER LIGHTENING HOLE RT LOWER TORQUE BOX, VERTICAL WEB AFT OF STA 1223 IN 48 SECTION. REPAIR PER MM 53-11-000-8. 2 L 7 3 4F A3WE 2001030600158 20010306 00158 NM 2001 3 6 DL72L010190 1 20010201 A 3350 1000677 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 502DA 21304 AFT DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERY, NO HELP. REPLACED LIGHT, OPS NOW OK. 2 L 7 3 4F A3WE 2001030600159 20010306 00159 NM 2001 3 6 DL73K010191 1 20010202 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 315DL 23087 THE KEEL BEAM LOWER SKIN FROM FS 661 TO FS 727 HAS BEEN REPLACED AS A PREVENTATIVE MODIFICATION PER S/B 737-53-1104, REV 4. THIS MODIFICATION WAS DONE AT HMV. 2 L 7 2 4F RT A16WE 2001030600160 20010306 00160 NM 2001 3 6 DL72S010192 1 20010201 A 3350 900542 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 546DA 22677 EMERGENCY LIGHT AT STA 360 FORWARD CENTER AISLE INOP. REPLACED BATTERY PACK AND RACK, OPS OK. 2 L 7 3 4F A3WE 2001030600161 20010306 00161 NM 2001 3 6 DL73K010193 1 20010202 A 3350 POWER SUPPLY BOEING 737 737232 1384475 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 321DL 23093 EMERGENCY ESCAPE PATH LIGHTS SEAT ROW 1 TO 4 AND CLOSET LIGHTS INOP. REPLACED BATTERY AND POWER SUPPLY. 2 L 7 2 4F RT A16WE 2001030600162 20010306 00162 NM 2001 3 6 DLM88010194 1 20010202 A 2910 AS15308K0254 LINE DOUG MD88 MD88 3023688 NM HYD SYSTEM LEAKING A DALA L ABORTED APPROACH K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 27 962DL 49981 ACFT LOST HYD PRESS AND QTY ON RT SYS, MADE EMERGENCY LANDING GEAR DOORS WERE UP AND RT SYS HYD QTY DID NOT GO TO ZERO. FOUND RT ENG HYD RETURN LINE IN 48 SECTION TO HAVE A HOLE IN IT. REPLACED LINE. SERVICED SYS, LK CKS GOOD. 2 L 7 2 4F RT A6WE 2001030600163 20010306 00163 NM 2001 3 6 DL757010195 1 20010203 A 5320 BOLT BOEING 757 757232 1384965 NM COCKPIT WRONG PART A DALA K NONE W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 628DL 22918 OVERHEAD WIRE BUNDLE CHAFED BY MOUNTING BOLT HOLDING LIGHT ASSY M10549 CAUSING DAMAGE TO ABOUT 8 WIRES. SEVEN CIRCUIT BREAKERS WERE POPPED ON OVERHEAD. 2 L 7 2 4F RT A2NM 2001030600164 20010306 00164 NM 2001 3 6 DL767010196 1 20010204 A 3350 BATTERY PACK BOEING 767 767232 1385132 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 101DA 22213 COACH CLASS SEAT MOUNTED EMERGENCY EXIT LIGHTS INOP ON BOTH LEFT AND RIGHT SIDE. REPLACED BOTH LEFT AND RIGHT BATTERY P ACKS. 2 L 7 2 4F RT A1NM 2001030600165 20010306 00165 NM 2001 3 6 DLM88010197 1 20010204 A 3260 HANDLE DOUG MD88 MD88 3023688 NM COCKPIT FAILED A DALA O OTHER J WARNING INDICATION DE DESCENT 1 SO 27 935DL 49722 UNSAFE GEAR LIGHT IND ON ALL 3 GEARS. FOUND GEAR HANDLE NOT FULLY DOWN. PERFORMED GEAR EXT, RET TEST PER M/M. CHECKS GOOD. 2 L 7 2 4F RT A6WE 2001030600166 20010306 00166 NM 2001 3 6 DL73K010198 1 20010202 A 5312 654583340 BULKHEAD BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 238WA 23186 DURING ACCOMPLISHMENT OF THE FS 178 BULKHEAD INSPECTIONS PER AD 2000-05-29, CRACKS WERE FOUND IN THE ADJACENT FLOOR WEB AT WL 207 & LBL 25. THE CRACKS ARE TYPICAL OF BAC S/B 737-53A1173. THE CRACKED WEB WAS REMOVED AND A NEW WEB INSTA LLED PER THE BAC S/B AND PER ER/A 379940-14AD. 2 L 7 2 4F A16WE 2001030600167 20010306 00167 NM 2001 3 6 DL757010199 1 20010204 A 2130 ACM BOEING 757 757232 1384965 NM LT PACK WORN A DALA O OTHER J WARNING INDICATION CR CRUISE 1 SO 27 603DL 22810 A/C WILL NOT MAINTAIN HIGHER THAN 7.2 PSID UNTIL RT RECIRC FAN TURNED OFF. WITH RT RECIRC FAN OFF PRESSURIZATION AND TE MP CONTROL WERE NORMAL. AT FL 390 RT PACK OFF LIGHT CAME ON, LATER RT ENG BLEED OFF LIGHT ON. COULD NOT RECOVER RT PK UNTIL ON GROUND AT LAX. THE LEFT PACK OPERATING ALONE WOULD NOT HOLD CABIN PRESSURE UNTIL DESCENDED BELOW FL 220. LEFT PACK WOULD NOT HOLD CABIN PRESSURE AT IDLE THRUST UNTIL BELOW FL 180. REPLACED AIR CYCLE MACHINE. 2 L 7 2 4F RT A2NM 2001030600168 20010306 00168 NM 2001 3 6 DL73K010200 1 20010205 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 326DL 23098 FOUND ON T1 LETTER CK, COCKPIT WINDOW POST IS CRACKED AT THE UPPER OUTBD CORNER OF THE CAPTS WINDSHIELD. REPAIRED PER S RM 53-30-3. 2 L 7 2 4F RT A16WE 2001030600169 20010306 00169 NM 2001 3 6 DL76L010201 1 20010206 A 2432 BA0601 BATTERY BOEING 767 767332 1382001 NM FUSELAGE FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 189DN 25990 MAIN BATTERY CHARGER MESSAGE APPEARED ON EICAS. A/C RETURNED TO JFK. REPLACED MAIN BATTERY AND CHARGER. ETO PS CATEGORY ''B'': DIVERSION OR TURNBACK 2 L 7 2 4F RT A1NM 2001030600170 20010306 00170 NM 2001 3 6 DL76L010202 1 20010205 A 2121 FAN BOEING 767 767332 1382001 NM E/E BAY FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 182DN 25987 ACRID ODOR SMELLED, FAN NOISE HEARD. FORWARD EXHAUST EQ COOLING FAN CB POPPED AND FWD EQ EXH FAN EICAS MESSAGE. DISPAT CHED PER MEL CB PULLED AND COLLARED. 2 L 7 2 4F RT A1NM 2001030600171 20010306 00171 NM 2001 3 6 DL733010203 1 20010206 A 5312 654583340 BULKHEAD BOEING 737 737347 1384647 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 307WA 23440 WEB CRACKS WERE FOUND IN THE FS 178 BULKHEAD AT WL 207, RBL AND LBL 25. THE WEBS WERE REPLACED PER S/B 737-53A1173 AT CV. 2 L 7 2 4F RT A16WE 2001030600172 20010306 00172 NM 2001 3 6 DL76G010204 1 20010205 A 2420 IDG BOEING 767 7673P6 1385105 NM GE CF6 CF680C2B6 30025 NE NR 2 ENGINE FAILED A DALA O OTHER J WARNING INDICATION CR CRUISE 1 SO 27 156DL 25354 695690 RIGHT GEN DRIVE LIGHT FLICKERED TWICE, 30 MIN LATER LIGHT ON STEADY. IAW POM, DISCONNECTED RT GEN DRIVE. APU STARTED A T FL310. REMOVED AND REPLACED RT IDG. RUNUP AND OPS CHECK OK. 2 L 7 2 4F 4 F RT A1NM E13NE 2001030600173 20010306 00173 NM 2001 3 6 DL767010205 1 20010205 A 5315 141T511077 FLOORBEAM BOEING 767 767232 1385132 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 104DA 22216 THE LOWER CHORD AREA OF THE FS 266.5 FLOORBEAM SUFFERED HEAT DAMAGE FROM AN ELECTRICAL WIRE ARCING BETWEEN RBL 23 & 30. THE LOWER CHORD AND LOWER PORTION OF THE FLOORBEAM WEB WERE CUT OUT OVER A 6.5 INCH LONG X 2.7 INCH HIGH AREA TO REMOVE ALL AREAS OF HEAT DAMAGE. THE CUTOUT WAS REPAIRED WITH AN ALUMINUM DOUBLER AND TWO ALUMINUM REPAIR CHANNELS PER ER/A 379869-14, REV A. 2 L 7 2 4F RT A1NM 2001030600174 20010306 00174 NM 2001 3 6 DL72L010206 1 20010206 A 3320 106075211 BALLAST BOEING 727 727232 1384082 NM CABIN BURNED A DALA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 509DA 21311 P/R SMOKE IN COCKPIT, FWD LAV SMOKE ALARM WENT OFF. SMOKE NOT ICED FROM BEHIND P-18 PNL. VERY ACRID SMELL IN THE COCKP IT, DID NOT NOTICE SMOKE FROM EYEBALL VENTS. SMELL VERY STRONG IN FWD LAV SMOKE, CLEARED AFTER APPROX 2 MIN. NO SMELL NOTED FROM AFT OF FIRST CLASS. EMERG EQUIP CALLED OUT. FOUND FWD ENTRY LIGHT BALLAST M217 BURNED. REPLACED BALLAST. 2 L 7 3 4F A3WE 2001030600175 20010306 00175 NM 2001 3 6 DL777010208 1 20010206 A 5310 STRUCTURE BOEING 777 777232 1385232 NM FUSELAGE VIBRATION A DALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 27 865DA 29737 MODERATE VIBRATION REPORTED BY F/A ON T/O LOUD NOISE AT 2L/2R DOORS F/O CONFIRMED AT APPROX 10K FEET. STAB WAS 4.5 FOR T/O BUT REQUIRED SUBSTANTIAL FORCE FOR ROTATION. VIB DOES DECREASE AS DID NOISE WITH A/S INCREASE. INSPECTED ALL A/C C OMPONENTS IN MID FUS AND RAM AIR DOOR HINGES, RAN ENGS TO T/O PWR AND PRESSURISED A/C. NO NOISE NOTED. A/C REQUIRES TE ST FLT. NOTE: TEST FLT NTF. 2 L 7 2 4F RT T00001SE 2001030600176 20010306 00176 NM 2001 3 6 DL72W010209 1 20010206 A 5330 SKIN BOEING 727 727247 138408F NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2813W 20869 FROM E-2 LTR CK, FUSELAGE SKIN IS CRACKED AT R-4 COCKPIT WINDOW CUTOUT. REPAIR PER SRM 53-30-3. 2 L 7 3 4F A3WE 2001030600177 20010306 00177 NM 2001 3 6 DL72S010210 1 20010206 A 3350 S106 BATTERY BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 543DA 22392 L2 OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERIES, CHECKS GOOD. 2 L 7 3 4F A3WE 2001030600178 20010306 00178 NM 2001 3 6 DL72W010211 1 20010206 A 5330 SKIN BOEING 727 727247 138408F NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2813W 20869 FROM E-2 LTR CK N/R 55, SHEARED RIVET AND CRACKS EXTENDING FROM A FASTENER WITH VISIBLE CORROSION AT STG 26L LAP JOINT 8 INCHES AFT OF STA 680. REPAIR PER SRM 53-30-3. 2 L 7 3 4F A3WE 2001030600179 20010306 00179 NM 2001 3 6 DL72S010212 1 20010207 A 3350 S106 BATTERY BOEING 727 727232 1384082 NM COCKPIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 516DA 21432 EMERGENCY EXIT LIGHT OVER COCKPIT DOOR INOP. REPLACED EMERGENCY EXIT LIGHT BATTERIES, OPS CKS OK. 2 L 7 3 4F A3WE 2001030600180 20010306 00180 NM 2001 3 6 DL72S010213 1 20010121 A 5313 STRINGER BOEING 727 727232 1384082 NM CARGO BAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 521DA 21472 CRACKED STRINGER 28R O/B FLANGE JUST FWD OF STA 990. INSTALLED REPAIR AS PER DRD 53-10-11D. 2 L 7 3 4F A3WE 2001030600181 20010306 00181 NM 2001 3 6 DL764010214 1 20010207 A 2150 ACM BOEING 767 767432ER NM LT & RT MALFUNCTIONED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 833MH 29706 ON TAXIOUT- F/A REPORTS BURNING SMELL IN AREA OF 3L DOOR. INSP AFT B/B AND IFE EQUIP. INSP LT/RT WHEEL WELL AREAS. IN SP LT/RT ACM AREAS, ALSO INSP APU PNEU DUCT FROM AFT B/B TO FWD OF LT ACM. INSP CN AREA FROM SEATS 27AB-33AB. INSP CEI LING AND FLOOR AREAS. RAN BOTH ENGS AND APU UNDER VARYING PNEUMATIC LOADS. NO ABNORMAL ODORS/SMELLS NOTED. NO ABNORMA L CONDITIONS NOTED IN INSP AREAS. 2 L 7 2 4F RT A1NM 2001030600182 20010306 00182 NM 2001 3 6 DL73K010215 1 20010207 A 5610 5893543130RPR WINDOW BOEING 737 737247 138448D NM COCKPIT CRACKED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 244WA 23518 FIRST OFFICERS FRONT WINDOW CRACKED AT FL 310. REMOVED AND REPLACED F/OS R-1 WINDOW AND WINDOW HEAT CONTROLLER. 2 L 7 2 4F A16WE 2001030600183 20010306 00183 NM 2001 3 6 DL73K010216 1 20010206 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 326DL 23098 A 3 INCH LONG CRACK WAS FOUND IN THE SKIN JUST BELOW STRINGER 18R AT FS 749. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN ALUMINUM EXTERNAL DOUBLER PER B737 SRM 53-30-3, FIG 1 AND ER/A 379971-14, REV A. 2 L 7 2 4F RT A16WE 2001030600184 20010306 00184 NM 2001 3 6 DL73K010217 1 20010206 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 326DL 23098 THE SKIN AND UNDERLYING BEARSTRAP OF THE L2 DOOR CUTOUT WERE FOUND CRACK AT THE LOWER HINGE CUTOUT. CRACK REMOVAL RESU LTED IN A 2 INCH X 2 INCH CUTOUT IN SKIN AND BONDED DOUBLER AND A .5 INCH CUTOUT IN THE BEARSTRAP. THE DAMAGE WAS REPAI RED WITH THREE EXTERNAL ALUMINUM DOUBLERS INSTALLED PER ER/A 379973-14, REV B. 2 L 7 2 4F RT A16WE 2001030600185 20010306 00185 NM 2001 3 6 DL76L010218 1 20010207 A 5320 CLAMP BOEING 767 767332 1382001 NM GIRTBAR BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 186DN 27962 WHILE COMPLYING WITH EO 01-073595-12 LATCH INSPECTION FOR OFF-WING ESCAPE SYSTEM IT WAS DISCOVERED THAT A BAR THAT RETAI NS THE SLIDE IN THE TRAY AND LAYS ACROSS THE LACES HAD COME LOOSE WHEN ALL THE PLASTIC CLAMPS THAT FIX THIS BAR TO THE T RAY HAD BROKEN. THIS BAR WAS JAMMED BETWEEN THE FUSELAGE AND THE SLIDE PACK, PREVENTING THE SLIDE DOOR FROM OPENING AND POSSIBLY PREVENTING THE SLIDE FROM DEPLOYING IN THE EVENT OF AN EMERGENCY. 2 L 7 2 4F RT A1NM 2001030600186 20010306 00186 NM 2001 3 6 DL757010219 1 20010205 A 2420 WIRE BOEING 757 757232 1384965 NM CENTER IRU BURNED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 6711M 30483 IMMEDIATELY AT LIFTOFF THE CENTER IRU FAILED, ALSO THE LT AFT RT FWD AND LT OVRD PUMP C/BS POPPED. THE FWD EQUIP COOLIN G FAN AND SUPPLY FAN 1 C/BS ALSO POPPED. MAINTENANCE REPLACED THE LT IDG AND GCU. ADDITIONAL INVESTIGATION FOUND BURNT WIRING AT THE P31 POWER BREAKER. ALL DAMAGED PARTS WERE REPLACED. 2 L 7 2 4F RT A2NM 2001030600187 20010306 00187 NM 2001 3 6 DL73K010220 1 20010207 A 3040 2312 CONTROLLER BOEING 737 737247 138448D NM AVIONICS BAY FAILED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 244WA 23518 DUE TO F/OS WINDSHIELD CRACKED IN FLT. REPLACED WINDSHIELD HEAT CONTROLLER, OPS CK OK. 2 L 7 2 4F A16WE 2001030600188 20010306 00188 NM 2001 3 6 DL72L010221 1 20010207 A 3350 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 501DA 21303 LT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK, ALL OPS OK. 2 L 7 3 4F A3WE 2001030600189 20010306 00189 NM 2001 3 6 DL72S010224 1 20010208 A 5730 69162413 PANEL BOEING 727 727225A 1384077 NM LT WING MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 ON WALK-AROUND FOUND PANEL AFT OF LT WING FENCE MISSING. REPLACED PANEL. 2 L 7 3 4F RT A3WE 2001030600190 20010306 00190 NM 2001 3 6 DL72W010225 1 20010208 A 2751 INDICATOR BOEING 727 727247 138408F NM TE FLAPS INACCURATE A DALA A UNSCHED LANDING F FLT CONT AFFECTED LD LANDING 1 SO 27 2820W 21058 A/C DIVERSION DUE OUTBOARD FLAPS LOCKED OUT. INSPECTED T/E FLAPS. NO DEFECTS NOTED. OPERATED FLAPS. OP CK NML. SWAP PED INDICATORS AS PRECAUTION. FLAP IND AND OPN NML. 2 L 7 3 4F A3WE 2001030600191 20010306 00191 NM 2001 3 6 DL72L010226 1 20010208 A 2780 SWIVEL BOEING 727 727232 1384082 NM NR 3 LE SLAT LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 514DA 21430 AT PUSH BACK HYD A QTY WAS 4.1 GAL, DURNING CRUISE HYD A QTY DROPPED TO 1.2 GAL. ACCOMPLISHED A SYS HYD LEAK/LOSS CK LI ST AND RETURNED TO SALT LAKE. LEAK STOPPED WHEN BOTH A PUMP SHUT OFF. FOUND B-NUT AT SWIVEL JOINT LEAKING FOR NR 3 LEA DING EDGE SLAT, INBD SIDE. REMOVED B-NUT, INSP,TIGHTENED AND REINSTALL SERVICED HYD TO FULL, OPERATED FLAP/SLATS, NO LE AKS FOUND. 2 L 7 3 4F A3WE 2001030600192 20010306 00192 NM 2001 3 6 DLM90010228 1 20010208 A 5248 3913359557 CABLE DOUG MD90 MD9030 3023690 NM TAILCONE OUT OF ADJ A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 914DN 53394 FOUND DURING ROUTINE TAIL CONE JETTISON CHECK AT DFW, D-2 LETTER CHECK. FROM NON ROUTINE CARD 50: HANDLE INOP DURING T AIL CONE JETTISON TEST, OUTSIDE DEPLOY HANDLE WOULD NOT OPERATE. HANDLE APPEARS TO BE CAUGHT BEHIND AIRCRAFT SKIN. STR AIGHTENED AND ADJUSTED HANDLE RETAINING CLIPS. OPS CHECK GOOD. 2 L 7 2 4F RT A6WE 2001030600193 20010306 00193 NM 2001 3 6 DL733010229 1 20010209 A 5312 65163007 BULKHEAD BOEING 737 737347 1384647 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 307WA 23440 DURING INSPECTIONS PER S/B 737-53A1173 CRACKS WERE FOUND IN THE CENTER WEB OF THE FS 178 BULKHEAD AT WL 234 AND LBL 6. THE CRACKS WERE REPAIRED PER S/B AND SRM 53-10-8, FIGURE 209THE DAMAGE WAS FOUND AT CV. 2 L 7 2 4F RT A16WE 2001030600194 20010306 00194 NM 2001 3 6 DL73K010230 1 20010209 A 5311 FRAME BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 315DL 23087 A CRACK WAS FOUND AT THE LOWER FASTENER ON THE LEFT SIDE OF THE FS 616 FRAME AT THE OVERWING FRAME TO STUB BEAM. THE C RACK IS TYPICAL TO THAT SHOWN ON S/B 737-53-1182. THE DAMAGE WAS REPAIRED PER S/B 737-53-1182 AT HMV. 2 L 7 2 4F RT A16WE 2001030600195 20010306 00195 NM 2001 3 6 DL72W010231 1 20010208 A 5311 651766436 FRAME BOEING 727 727247 138408F NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 THE FS 720D FUSELAGE FRAME WEB WAS DAMAGED BY TOOLING JUST BELOW STRINGER 25R AND THE EXISTING FRAME SPLICE. THE D AMAGE WAS REMOVED WITH A 2 INCH CUTOUT IN THE WEB. THE DAMAGE WAS REPAIRED BY REMOVING THE EXISTING FRAME SPLICE AND FABRIACTING A LARGER SPLICE TO ENCOMPASS THE DAMAGE. THE REPAIR WAS ACCOMPLISHED PER ER/A 379941-14, REV A. 2 L 7 3 4F A3WE 2001030600196 20010306 00196 NM 2001 3 6 DL72W010232 1 20010208 A 5330 655456716 SKIN BOEING 727 727247 138408F NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 296WA 22533 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP JOINT INDICATED CRACKS BETWEEN FS 680 & 740. INTERNAL MFEC INSPECTION CONFI RMED 5 CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. THE ENTIRE SKIN LAP SPLICE WAS CUT AWAY TO REMOVE ALL DAMAGE . THE LAP WAS RESTORED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 379959-14AD. 2 L 7 3 4F A3WE 2001030600197 20010306 00197 NM 2001 3 6 DL72W010233 1 20010207 A 5330 SKIN BOEING 727 727247 138408F NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2813W 20869 AN AREA OF CORROSION WAS FOUND IN THE FUSELAGE SKIN AT FS 660 NEAR STRINGER 30. THE CORROSION WAS JUST FWD OF AN EXISTI NG SKIN REPAIR. THE EXISTING REPAIR WAS REMOVED, THE UNDERLYING SKIN INSPECTED, AND THE NEW CORROSION REMOVED WITH A 2. 5 INCH CUTOUT. THE EXISTING REPAIR CUTOUT AND THE NEW CUTOUT WERE INCORPORATED INTO A SINGLE REPAIR WITH AN EXTERNAL AL UMINUM DOUBLER INSTALLED PER ER/A 379984-14. 2 L 7 3 4F A3WE 2001030600198 20010306 00198 NM 2001 3 6 DL72S010234 1 20010207 A 5311 65561001 FRAME BOEING 727 727225A 1384077 NM FUSELAGE TOOL DAMAGE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 MISDRILLED HOLE REPAIR WHILE ACCOMPLISHING INSPECTIONS AND MTC. TO THE FWD FRAME OF THE C1 DOOR OPENING, THREE HOLES COM MON TO THE OUTER FRAME CHORD AND FRAME SPLICE NEAR S-18R WERE BADLY MISDRILLED. THE DAMAGED SECTION OF CHORD W AS REMOVED AND A NEW SECTION SPLICED IN WITH A STEEL SPLICE ANGLE. THE WEB WAS CUT AND A NEW SECTION SPLICED IN WITH AN ALUMINUM DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 379930-14AD, REV A. 2 L 7 3 4F RT A3WE 2001030600199 20010306 00199 NM 2001 3 6 DL757010235 1 20010209 A 2560 BATTERY BOEING 757 757232 1384965 NM FLASHLIGHT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 641DL 23995 FWD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT HAS WEAK BATTERY. REPLACED BATTERY, OPS NORMAL. 2 L 7 2 4F RT A2NM 2001030600200 20010306 00200 NE 2001 3 6 DL757010236 2 20010209 A 7200 ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 MALFUNCTIONED A DALA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 602DL 18267 22809 727156 AT 41000 FT LEFT OIL QTY DROPPED TO 0 WITH INCREASING OIL TEMP. OIL TEMP REACH YELLOW BAND, MAX TEMP 171.ENG WAS OPERAT ED AT IDLE AND DESCENDED TO 29000. OIL QTY AND TEMP RETURNED TO NORMAL AT 41000 FT. SCAVANGE PUMP PRES WAS 2 PSI. REP LACED GEARBOX SCAVANGE PUMP AND MAIN ENG LUBE/SCAVANGE PUMP. LEAK CKS GOOD. ALSO REPLACED SCAVANGE OIL PRES XMITTER A ND NR 4 BEARING SCAVANGE VLV. RAN ENG PER M/M ALL INDICATIONS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2001030600201 20010306 00201 NM 2001 3 6 DL767010237 1 20010210 A 2121 FAN BOEING 767 767232 1385132 NM E/E BAY ODOR A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 101DA 22213 AFTER ENG START ELECTRICAL ODOR IN COCKPIT AND BY L1 DOOR. FOUND EICAS MSG, FWD SUP FAN 1. SECURED C/B H18. RAN ENGS, PACKS, CKD E/E COMPARTMENT, FWD GALLEY. UNABLE TO DUPLICATE WITH FAN DEACTIVATED. FWD FAN TO MCO/PLAC 21-58-03A. 2 L 7 2 4F RT A1NM 2001030600202 20010306 00202 NE 2001 3 6 DL72L010239 2 20010210 A 7314 SHAFT BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 3 ENG PUMP SHEARED A DALA C ABORTED TAKEOFF X J ENGINE FLAMEOUT WARNING INDICATION TO TAKEOFF 1 SO 27 504DA 74060 21306 687420 NR 3 ENG FAILED ON T/O ROLL. ABORTED AT 130 KIAS. REPLACED NR 3 ENG FUEL PUMP PER M/M. OPS CK AND LEAK CK ON IDLE RUN . ALSO TRIM ENG PER PFHB 4077 TEST Y. CK NML. RETORQUED FUEL PUMP QUAD RING PER M/M. 2 L 7 3 4F 4 F A3WE E2EA 2001030600203 20010306 00203 2001 3 6 DL72S010240 4 20010211 A 3413 GYRO BOEING 727 727225A 1384077 NM COCKCPIT INOPERATIVE A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 8891Z 21860 RADAR STABILIZATION INOP, PANTS GROUND EITHER ONE SIDE OR OTHER. REPLACED NR 2 VERTICAL GYRO. 2 L 7 3 4F RT A3WE 2001030600204 20010306 00204 NM 2001 3 6 DLM88010241 1 20010211 A 3222 STRUT DOUG MD88 MD88 3023688 NM NLG LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 971DL 53214 AFTER TAKEOFF GEAR UNSAFE LIGHT ILLUMINATED (RED NOSE GEAR LIGHT). FOUND NOSE STRUT HAD LEAKED DOWN. REPACKED AND SERV ICED STRUT. 2 L 7 2 4F RT A6WE 2001030600205 20010306 00205 NM 2001 3 6 DL72S010243 1 20010211 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM RT OVERWING INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 526DA 21586 FWD RT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, LIGHT OPN NORMAL. 2 L 7 3 4F A3WE 2001030600206 20010306 00206 NM 2001 3 6 DL73K010244 1 20010209 A 5312 6516300 BULKHEAD BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 238WA 23186 THE FS 178 BULKHEAD WEB WAS FOUND WITH TWO 1 INCH CRACKS AT RBL 5.7 AND WL 213. THE WEB HAD A PREVIOUS REPAIR DOUBLER F OR CRACKS AT RBL 5.7, WL 200 & BL 0, WL 190. THE EXISTING REPAIR WAS REMOVED AND A NEW ALUMINUM DOUBLER FABRICATED AND INSTALLED TO ENCOMPASS ALL DAMAGE CUTOUTS. THE REPAIR WAS ACCOMPLISHED PER ER/A 379924-14AD, REV A. 2 L 7 2 4F A16WE 2001030600207 20010306 00207 NM 2001 3 6 DL757010245 1 20010212 A 5410 STRUCTURE BOEING 757 757232 1384965 NM NR 1 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 686DA 27589 NR 1 PYLON CRACKED AT FWD INBOARD TORQUE BOX CUTOUT 443AR AT UPPER FWD EXT CORNER. REPAIRED PER SRM 54-51-01. 2 L 7 2 4F RT A2NM 2001030600209 20010306 00209 NM 2001 3 6 DLM88010247 1 20010212 A 2432 CHARGER DOUG MD88 MD88 3023688 NM FWD E/E BAY OVERHEATED A DALA H D DEACTIVATE SYST/CIRCUITS RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 968DL 53161 PRIOR TO DEPARTURE RAMP REPORTED SMOKE COMING FROM FUSELAGE AFT OF NOSE GEAR. FOUND BATTERIES OVERHEATED AND VERY HOT. A/C HAD A SUNDSTRAND CHARGER INSTALLED (P/N 249001276) (S/N 5030008). REPLACED BATTERIES AND CHARGER. 2 L 7 2 4F RT A6WE 2001030600210 20010306 00210 NM 2001 3 6 DL72W010248 1 20010212 A 5753 SKIN BOEING 727 727247 138408F NM NR 2 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 A 1 INCH CRACK NR 2 L/E FLAP OUTER SKIN AT LOWER LIP INBD HINGE CUTOUT. REPAIR PER M/M 57-53-000-8. 2 L 7 3 4F A3WE 2001030600211 20010306 00211 NM 2001 3 6 DL72W010249 1 20010212 A 5754 STIFFENER BOEING 727 727247 138408F NM NR 3 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 WING L/E SPAR STIFFENER CRACKED I/B SIDE NR 3 SLAT O/B TRACK. REPAIR PER M/M 57-20-021-8. 2 L 7 3 4F A3WE 2001030600212 20010306 00212 NM 2001 3 6 DL72W010250 1 20010212 A 5754 STIFFENER BOEING 727 727247 138408F NM NR 3 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 WING L/E SPAR STIFFENER CRACKED O/B SIDE NR 3 SLAT O/B TRACK. REPAIR PER M/M 57-20-21-8. 2 L 7 3 4F A3WE 2001030600213 20010306 00213 NM 2001 3 6 DLM88010251 1 20010212 A 2170 COALESCER BAG DOUG MD88 MD88 3023688 NM AIR DISTRIBUTION CONTAMINATED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 912DE 49997 F/A REPORTED SMOKE AND FUMES AFT CABIN ON CLIMBOUT. RETURNED ENOUGH TO NOTICE IN COCKPIT. FOUND NO HYD LEAKS, FOUND AP U INLET CLEAN. RAN ENGINES TO TAKEOFF, NO SMOKE NOTED. REPLACED WATER SEP BAGS, PERFORMED DUCT BURNOUT. (PERFORMED OP N 5088 SMOKE/SMELL TROUBLESHOOTING). 2 L 7 2 4F RT A6WE 2001030600214 20010306 00214 NM 2001 3 6 DL757010253 1 20010211 A 2420 IDG BOEING 757 757232 1384965 NM NR 2 ENGINE MAKING METAL A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 640DL 23994 RIGHT GEN DRIVE LIGHT CAME ON DURING CLIMB. DISCONNECTED RIGHT DRIVE PER POM. FOUND METAL ON CHIP DETECTOR REPLACED ID G PER MM. 2 L 7 2 4F RT A2NM 2001030600215 20010306 00215 NM 2001 3 6 DL72W010254 1 20010212 A 5330 65545664 SKIN BOEING 727 727247 138408F NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 296WA 22533 LFEC INSPECTION OF THE STRINGER 26L SKIN LAP JOINT BETWEEN FS 480 & 680 INDICATED CRACKS. INTERNAL MFEC INSPECTION CO NFIRMED MULTIPLE CRACKS IN THE LOWER SKIN AT THE LOWER FASTENER ROW. THE ENTIRE LAP JOINT WAS CUTOUT TO REMOVE ALL CRAC KS. THE JOINT WAS RESTORED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 379961-14AD, REV A. 2 L 7 3 4F A3WE 2001030600216 20010306 00216 NM 2001 3 6 DLM88010255 1 20010213 A 2133 REGULATOR DOUG MD88 MD88 3023688 NM CABIN PRESSURE FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 913DL 49544 BURNING SMELL THROUGHOUT A/C AFTER T/O. AFT LAV SMOKE DETECTOR SOUNDED. ENGS AT T/O ENG A/I ON, AIRFOIL A/I OFF CROSS FEEDS CLOSED APU OFF. REPLACED LT PRESS REG, C/W DUCT BURNOUT PROCEDURE PER OPN 5088 AND M/M 21-20-02-2 ITEM 7C. 2 L 7 2 4F RT A6WE 2001030600218 20010306 00218 NM 2001 3 6 DL72W010257 1 20010212 A 5330 655457416 SKIN BOEING 727 727247 138408F NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 296WA 22533 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 480 & 681 INDICATED CRACKS. INTERNAL MFEC INSPECTION CONF IRMED 11 CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN ALONG THE LENGTH OF THE LAP JOINT. THE ENTIRE SKIN LAP WAS CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOULBER INSTALLED PER ER/A 379957-14AD. 2 L 7 3 4F A3WE 2001030600219 20010306 00219 2001 3 6 DL76G010258 4 20010214 A 2330 CONTROLLER BOEING 767 767332 1382001 NM ENTERTAIN SYS FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 169DZ 29689 DURING T/O ROLL, FAINT ODOR OF BURNING PLASTIC. NEVER BECAME A STRONG ODOR BUT WAS NOTICEABLE FOR 1 HR. BEGAN TO DISSI PATE SOON AFTER T/O. FLT ATTENDANT NOTICED THE IN-FLIGHT ENTERTAINMENT SYSTEM HAD FAILED IN SEVERAL MODES AFTER T/O AND WOULD NOT RECOVER. ODOR WAS NOTICEABLE IN COCKPIT AND BACK TO ROW 3 OF BUSINESS CLASS. FOUND CABIN FILE SERVER WITH N O POWER. REMOVED CFS AND FOUND INTERNAL HARDWARE WITH SLIGHT ELECTRICAL ODOR. REPLACED CFS. INSPECTED ALL LRU IN VIDE O CONTROL CABINET AND E&E BAY. ALL CHECK NORMAL. 2 L 7 2 4F RT A1NM 2001030600220 20010306 00220 NE 2001 3 6 DL72S010260 2 20010214 A 7200 ENGINE BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 1 INTERMITTENT A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 536DA 80399 22049 657254 NR 1 ENG FILTER BY PASS LIGHT ILLUMINATED ON TAKEOFF ROLL AT 100 KTS. RETURNED TO BLOCKS. INSP AND REPLACED NR 1 ENG MAIN OIL SCREEN. FWD FILTER BY PASS LIGHT TO MCO AND PLACARD PER MEL 79-00-02. 2 L 7 3 4F 4 F A3WE E2EA 2001030600221 20010306 00221 NM 2001 3 6 RAAA01B101 1 20010209 A 2612 1825280037525 FIRE LOOP BOEING 727 72722C 138400F NM NR 1 ENGINE GROUNDED A RAAA O OTHER N FALSE WARNING NR NOT REPORTED 1 AL 03 831RV 19093 NR 1 ENG FIRE DETECTOR CIRCUIT GROUND LIGHT ON. REPOSITIONED LOWER ENG FIRE LOOP FROM COWLING. 2 L 7 3 4F A3WE 2001030600222 20010306 00222 EU 2001 3 6 DHL2001367511 1 20010213 A 5730 SKIN PANEL AIRBUS 300 A300B4203 3930306 EU LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH MSN265 C-CHECK, LT WING LOWER SKIN PANEL NR 2 I/B OF RIB 9 CRACKED. NDT OF AREA SHOWED 2 CRACKS, (16MM & 26MM). CARRIED OUT R EPAIR TO LOWER SKIN PANEL IAW DRAWING R57340199 NON ROUTINE 78863. 2 L 7 2 4F RT A35EU 2001030600223 20010306 00223 EU 2001 3 6 DHL2001367521 1 20010215 A 5730 SKIN PANEL AIRBUS 300 A300B4203 3930306 EU RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH MSN265 C-CHECK, LOWER SKIN PANEL CRACKED I/B OF RIB 9 REAR SPAR RT WING. NDT SHOWED 2 CRACKS 3 & 7 MM. REPAIR ACCOMPLISHED PE R DRAWING R573-40199. 2 L 7 2 4F RT A35EU 2001030600233 20010306 00233 NM 2001 3 6 DHL2001712517 1 20010215 A 5755 FITTING BOEING 727 72729 1384007 NM LT WING SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 C-CHECK, LEFT WING T/E NR 4 SPOILER HOUSING FITTING WS 436.5 CRACKED 1.0 INCH. REMOVED FITTING CRACK IAW SRM 51-30-2, P AGE 1-2. PERFORMED ANTI-CORROSION TREATMENT AND PRIMED IAW SRM 51-10-2, PAGE 1 AND 2. INSTALLED NEW FITTING IAW SRM 51 -30-2, PAGE 1 AND 2. (NON-ROUTINE CARD 0157) 2 L 7 3 4F A3WE 2001030600234 20010306 00234 NM 2001 3 6 DHL2001712518 1 20010203 A 5320 655343316 FITTING BOEING 727 72729 1384007 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 51673 19401 C-CHECK, AFT CARGO COMPARTMENT NR 2 DOOR STOP CRACKED 1.0 INCH AT STA 1058.000 STR 23 RT. REMOVED SKIN TO GAIN ACCESS I AW SRM 51-30-2 PAGE 1 AND 2. REMOVED FITTING (STOP) CRACKED IAW SRM 51-30-2 PAGE 1 AND 2. REINSTALLED SKIN IAW SRM 51- 30-2 PAGE 1 AND 2. (NON-ROUTINE CARD 0302) 2 L 7 3 4F A3WE 2001030600235 20010306 00235 NM 2001 3 6 DHL2001712519 1 20010203 A 5751 STRUCTURE BOEING 727 72729 1384007 NM LT WING AILERON CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 C-CHECK, LT WING TRIM TAB L/E PART FROM EXTERNAL AILERON SHOWS CRACK .25 INCH. REMOVED LEADING EDGE FROM TRIM TAB IAW S RM 51-10-2, PAGE 1 AND 2. FABRICATED NEW LEADING EDGE WITH ALCLAD 2024, T3, 0.020 INCH IAW SRM 57-20-03, FIG 2. TREATE D AND PRIMED IAW SRM 51-10-2, PAGE 1 AND 2. INSTALLED LEADING EDGE NEW IAW SRM 51-30-2 PAGE 1 AND 2. (NON-ROUTINE CARD 1166) 2 L 7 3 4F A3WE 2001030600236 20010306 00236 NM 2001 3 6 DHL2001712520 1 20010209 A 5312 PRESSURE PANEL BOEING 727 72729 1384007 NM MLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 C-CHECK, MLG WHEEL WELL TOP SURFACE SHOWS 6 CRACKS OF .75 INCH BETWEEN LBL 25 AND LBL 40, STA 900.000 AND STA 910.000. REMOVED FLOOR PANELS, BRACKETS, CLIPS, STRAPS IAW DWG 65-89360-3. PERFORMED STOP DRILL IAW DWG 65-89360. FABRICATED DO UBLER (ALCLAD 2024, T3, 0.80 INCH; 53 INCH X 15 INCH) IAW SRM 51-10-2, PAGE 1 AND 2. REINSTALLED FLOOR PANELS, BRACKETS , CLIPS, STRAPS IAW DWG 65-89360-3. REFER TO J/C 7107.1 FOR OPS CHECK. (NON-ROUTINE CARD 0413) 2 L 7 3 4F A3WE 2001030600237 20010306 00237 NM 2001 3 6 USAASB01005 1 20010113 A 5240 DOOR BOEING 737 737301 1384611 NM SERVICE DOOR NOT CLOSED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 351US 23554 PHL - FLT 1228 - ON CLIMB-OUT FROM PHL, EN ROUTE TO CLT, CAPTAIN REPORTED THAT THE AIRCRAFT CABIN PRESSURE CONTINUED TO CLIMB ALONG WITH OUTSIDE PRESSURE. MIX VALVE APPEARS TO BE WORKING FINE. HOWEVER, FLIGHT ATTENDANT REPORTED THAT THE S EAL FOR THE AFT RIGHT SERVICE DOOR APPEARED TO BE MISSING. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER I NCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE AFT RIGHT SERVICE DOOR NOT CLOSED PROPERLY. CYCLED DOOR TO CLOSED POSITION. DOOR CHECKS OK. INSPECTED DOOR AND DOOR SEAL. PRESSURIZED AIRCRAFT. NO LEAKS OR DEFECTS NOTED. (M) 2 L 7 2 4F RT A16WE 2001030600238 20010306 00238 NM 2001 3 6 USAASB01002 1 20010102 A 2781 2061141 INDICATOR BOEING 737 737301 1384611 NM COCKPIT FAILED A USAA K NONE O OTHER DE DESCENT 1 EA 19 351US 37117 23554 PIT - FLT 1950 - ON DESCENT TO PIT, THE TRAILING EDGE FLAPS WOULD NOT EXTEND. AS CREW POSITIONED FLAPS TO ONE DEGREE FL APS, THE LEFT FLAP INDICATOR STOPPED AT ONE QUARTER DEGREE WHILE THE RIGHT FLAP INDICTOR STOPED AT JUST LESS THAN ONE DE GREE. CREW ACCOMPLISHED QUICK REF HANDBOOK PROCEDURES. FLIGHT LANDED WITHOUT FURTHER INCIDENT AT PIT. NO EMERGENCY WA S DECLARED. MAINTENANCE OPERATED FLAPS SEVERAL TIMES AND INSPECTED FLAPS. NO PROBLEMS NTOED. REMOVED AND REPLACED FLA P POSITION INDICATOR AS PRECAUTIONARY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001030600239 20010306 00239 NM 2001 3 6 USAASB01004 1 20010112 A 3230 806002 CIRCUIT BOARD BOEING 737 7373B7 1384580 NM EE BAY FAULTY A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 533AU 24515 CLE - FLT 1515 - CREW REPORTED THAT DURING CLIMB-OUT FROM CLE, THE LANDING GEAR LEVER WOULD NOT MOVE TO THE UP POSITION. GEAR INDICATION SHOWED THREE RED AND THREE GREEN GEAR LIGHTS. FLIGHT REQUESTED WITH CEL TOWER TO STAY AT 3,000 FEET D UE TO GEAR INDICATION PROBLEM. CLE TOWER REPORTED THAT IT APPEARED THE LEFT MAIN GEAR DID NOT RETRACT. CREW PLACED GEA R HANDLE TO THE DOWN POSITION AND RECEIVED THREE GREEN GEAR LIGHTS. CREW DECLARED AN EMERGENCY AS A PRECAUTION AND RETU RNED TO FIELD AT CLE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE M991 PRINTED CIRCUI T CARD PER MM. CYCLED GEAR NUMEROUS TIMES. ALSO, CHECKED ALL GEAR SENSORS AND CABLE RUNS. ALL CHECKED NORMAL. (M) 2 L 7 2 4F RT A16WE 2001030600240 20010306 00240 WP 2001 3 6 USAAD01029 1 20010211 A 3350 LIGHT DOUG DC9 DC981 3022081 WP CABIN MISINSTALLED A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 810US 48042 MCO - WHILE COMPLETING AND ''A'' CHECK INSPECTION, THE LOWER LEVEL EMERGENCY LIGHTS WERE FOUND TO BE INSTALLED AT SEAT R OWS OTHER THEN THOSE INDICATED BY THE PAPERWORK. THE LOW LEVEL EMERGENCY LIGHTS WERE INSTALLED IN THE PROPER POSITIONS. (M) 2 L 7 2 4F A6WE 2001030600241 20010306 00241 WP 2001 3 6 USAAD01028 1 20010212 A 3350 9731044 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 830US 49443 IND - THE LOW LEVEL EMERGENCY LIGHT AST SEAT ROW 11, AFT EMERGENCY CEILING LIGHTS, AND THE EXTERIOR EMERGENCY LIGHTS WER E INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL LIGHT ASSEMBLY, AND THE BATTERIES FOR THE AFT CEILING EMERGENCY LIGHT S AND THE EXTERIOR EMERGENCY LIGHTS. (M) 2 L 7 2 4F A6WE 2001030600243 20010306 00243 WP 2001 3 6 20010305SG002 1 20010212 A 3350 MISC0639 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 830US 49443 IND - THE LOW LEVEL EMERGENCY LIGHT AST SEAT ROW 11, AFT EMERGENCY CEILING LIGHTS, AND THE EXTERIOR EMERGENCY LIGHTS WER E INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL LIGHT ASSEMBLY, AND THE BATTERIES FOR THE AFT CEILING EMERGENCY LIGHT S AND THE EXTERIOR EMERGENCY LIGHTS. REF USAAD01028. REF USAAD01028. (M) 2 L 7 2 4F A6WE 2001030600245 20010306 00245 NM 2001 3 6 USAA010033 1 20010115 A 5310 PRESSURE PANEL BOEING 737 7374B7 1384702 NM LT MLG CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 32038 24556 CLT - FOUND SKIN CRACKED, LEFT MLG UPPER PRESS DECK BS 664, LBL 32, WL 203. INSTALLED DOUBLER PER TR 53-60-04. (M) 2 L 7 2 4F RT A16WE 2001030600246 20010306 00246 NM 2001 3 6 USAA010069 1 20010129 A 5743 SUPPORT FITTING BOEING 737 7373B7 1384580 NM WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 520AU 40659 23706 CLT - FOUND FITTING CRACKED .5 INCH, MLG BEAM OUTBOARD SUPPORT FITTING AFT WING SPAR. DEFERRED PER TR 57-40-13. (M) 2 L 7 2 4F RT A16WE 2001030600247 20010306 00247 NM 2001 3 6 USAA010071 1 20010129 A 5730 SKIN BOEING 737 7374B7 1384702 NM WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 32258 24554 CLT - FOUND SKIN CRACKED .875 INCH, FS 215, 2 INCHES FORWARD FRONT SPAR OUTBOARD MID SPAR ATTACH FITTING. REPAIRED PER EA 69037. (M) 2 L 7 2 4F RT A16WE 2001030600248 20010306 00248 NM 2001 3 6 USAASB01042 1 20010208 A 2611 100064904 SMOKE DETECTOR BOEING 737 7374B7 1384702 NM FWD CARGO BAY MALFUNCTIONED A USAA K NONE N FALSE WARNING CR CRUISE 1 EA 19 448US 190 24892 TPA - FLT 589 - EN ROUTE FROM PHL-TPA, THE FORWARD CARGO COMPARTMENT FIRE LIGHT AND CAUTION ILGHTS ILLUMINATED FOR 60 SE CONDS, THEN EXTINGUISHED. CREW DID NOT FIRE THE BOTTLES AS THE LIGHTS REMAINED EXTINGUISH. SYSTEM WAS ALREADY ON MEL F OR A CARGO FIRE PROTECTION MAINTENANCE LIGHT ON THE OVERHEAD ILLUMINATING. FLIGHT CONTINUED ONTO TPA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED FORWARD CARGO COMPARTMENT UPON AIRCRAFT ARRIVAL. NO DEFECTS, ODORS OR WARM SP OTS NOTED. INSPECTED LUGGAGE UPON UNLOADING. ALL CHECKED OK. REMOVED AND REPLACED THE FORWARD CARGO COMPARTMENT NR 4 SMOKE DETECTOR UNIT. OPERATIONAL CHECK GOOD. CLEARED AND REMOVED MEL. (M) 2 L 7 2 4F RT A16WE 2001030600249 20010306 00249 NM 2001 3 6 USAASB01046 1 20010210 A 2781 2061141 INDICATOR BOEING 737 737301 1384611 NM COCKPIT FAILED A USAA O OTHER J WARNING INDICATION DE DESCENT 1 EA 19 585US 27618 23930 BUF - FLT 638 - DURING DESCENT INTO BUF, CREW EXTENDED FLAPS TO 5 DEGREES AND THEN TO 10 DEGREES BUT RECEIVED A FLAP LIG HT. FLAPS WOULD NOT EXTEND BEYOND 5 DEGREES. CAPTAIN DECLARED AN EMERGENCY AND THE FLIGHT LANDED AT BUF WITHOUT FURTHE R INCIDENT. MAINTENANCE REMOVED AND RELACED THE FLAP POSITION INDICATOR. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001030600250 20010306 00250 NM 2001 3 6 USAASB01045 1 20010209 A 3610 106200823 REGULATOR BOEING 737 7373B7 1384580 NM NR 1 ENG FAILED A USAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 518AU 41721 23704 PHL - FLT 1598 - EN ROUTE FROM IND TO PHL, AT FL370, THE LEFT ENGINE BLEED TRIP OFF LIGHT ILLUMINATED. CABIN RAPIDLY CL IMBED, SO THE CREW EXECUTED AN EMERGENCY DESCENT TO FL100. CREW WAS ABLE TO RESET THE PACK TO THE LOWER ALTITUDE AND IT OPERATED NORMALLY. FLIGHT CONTINUED ONTO PHL AND LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED DURING EM ERGENCY DESCENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE BLEED AIR REGULATOR. OPERATIONAL CHECK AND LEAK CHEC K GOOD. (M) 2 L 7 2 4F RT A16WE 2001030600251 20010306 00251 NM 2001 3 6 USAASB01041 1 20010208 A 5210 DOOR BOEING 737 7373B7 1384580 NM AFT ENTRY DOOR NOT CLOSED A USAA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 EA 19 522AU 23857 PIT - FLT 474 - ON CLIMB-OUT FROM PIT, AT 8,000 FEET, THE AIRCRAFT WOULD NOT PRESSURIZE. FLIGHT RETURNED TO FIELD AT PI T AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE DETERMINED THAT CATERING DID NOT PROPERL Y CLOSE THE AFT LEFT ENTRY DOOR. CHECKED OPERATION AND LATHCES OF DOOR. FOUND OK. CHECKED LIGHT OPERATION OF DOOR. F OUND NORMAL. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2001030600252 20010306 00252 NM 2001 3 6 USAASB01036 1 20010204 A 2810 FUEL TANK BOEING 737 7373B7 1384580 NM RT WING OVERSERVICED A USAA A UNSCHED LANDING K FLUID LOSS TO TAKEOFF 1 EA 19 523AU 23858 CLT - FLT 1712 - ON TAKEOFF FROM CLT, THE CLT TOWER REPORTED FUEL STREAMING FROM THE RIGHT WING AT 600 FEET. TOWER NOTI FIED CREW AND THEY INITIATED A RETURN TO FIELD TO CLT WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WA S DECLARED. MAINTENANCE SUSPECTS AIRCRAFT WAS OVERSERVICED WITH FUEL AS FUEL WAS FOUND COMING FROM THE RIGHT WING FUEL VENT SCOOP. WHEN AIRCRAFT ARRIVED AT THE GATE, FUELER WAS ASKED TO PUT FUEL IN THE TANKS. AIRCRAFT WOULD NOT ACCEPT AN YMORE FUEL. AIRCRAFT WAS RELEASED ON MEL. ON 2/10/01, MAINTENANCE MEASURED FUEL IN LEFT AND RIGHT WING TANKS WITH FUEL DRIP STICKS. DRIP STICKS AND FUEL QUANTITY INDICATORS AGREED WITH EACH OTHER. PERFORMED AUTO FUEL SHUTOFF CHECK BY RE 2 L 7 2 4F RT A16WE 2001030600253 20010306 00253 NM 2001 3 6 USAA010107 1 20010130 A 5320 ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 520AU 40660 23706 CLT - FOUND Z-ANGLE CORRODED 1 INCH BY 2 INCHES, FORWARD ENTRANCE DOOR Z-ANGLE. REPLACED Z-ANGLE PER TR 53-20-08. (M) 2 L 7 2 4F RT A16WE 2001030600254 20010306 00254 NM 2001 3 6 USAA010103 1 20010130 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 32258 24554 CLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH, STATION 328, RBL 24-60. CORROSION LEVEL 1. REMOVED T-CAP AND INSTALLE D NEW ONE PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2001030600255 20010306 00255 NM 2001 3 6 USAA010074 1 20010129 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 32258 24554 CLT - FOUND FLOORBEAM TOP CAP CORRODED .75 INCH BY .75 INCH, BS 967, RBL 29.5 AND RBL 30. INSTALLED REPAIR PARTS PER SR M 53-00-51 FIG 201 AND 202. (M) 2 L 7 2 4F RT A16WE 2001030600256 20010306 00256 NM 2001 3 6 USAA010070 1 20010129 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 32038 24556 CLT - FOUND FLOORBEAM T-CAP CORRODED .5 INCH, STATION 947, LBL 4 TOP OF FLOORBEAM. INSTALLED NEW T-CAP SECTION PER SRM 53-00-51. (M) 2 L 7 2 4F RT A16WE 2001030600257 20010306 00257 NM 2001 3 6 USAA010067 1 20010123 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 32038 24556 CLT - FOUND BEAM CHORD CORRODED 3 INCHES, FLOORBEAM 328 UPPER CHORD LBL 33 - RBL 65. INSTALLED REPAIR DOUBLER AND T-CAP PER SRM 53-10-54 FIG 205. (M) 2 L 7 2 4F RT A16WE 2001030600258 20010306 00258 NM 2001 3 6 USAA010066 1 20010123 A 5320 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 32038 24556 CLT - FOUND Z-ANGLE CORRODED 48 INCHES, CREASEBEAM STATION 312 TO 360 INNER CHORD. CORROSION LEVEL 1. INSTALLED NEW Z- ANGLE PER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 2001030600259 20010306 00259 NM 2001 3 6 USAA010065 1 20010123 A 5320 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 32038 24556 CLT - FOUND CHORD Z-ANGLE CORRODED 52 INCHES, RIGHT CREASE BEAM STATION 294.5 AFT OF 344 INNER CHORD. INSTALLED NEW SEC TION PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001030600260 20010306 00260 NM 2001 3 6 USAA010062 1 20010122 A 5313 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 520AU 40660 23706 CLT - FOUND STRINGER CORRODED 1 INCH BY 4 INCHES, STATION 520 TO 526 JUST ABOVE STRINGER 28L. INSTALLED STEEL REPAIR AN GLE PER EA 68919. (M) 2 L 7 2 4F RT A16WE 2001030600261 20010306 00261 NM 2001 3 6 USAA010058 1 20010122 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 32038 24556 CLT - FOUND CORROSION ON FLOORBEAM 1 INCH BY 1 INCH, STATION 344, LBL 12 - RBL 12 UPPER CHORD SURFACE. INSTALLED REPAIR PART AND ANGLES PER SRM 53-10-51 FIG 205. (M) 2 L 7 2 4F RT A16WE 2001030600262 20010306 00262 NM 2001 3 6 USAA010057 1 20010122 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 32038 24556 CLT - FOUND BEAM CHORD CORRODED 56 INCHES, FLOORBEAM 312, LBL 17.5 INCH TO RBL 11 INCH. NEW T-CAP SECTION INSTALLED PER SRM 53-10-51 AND 51-20-01. (M) 2 L 7 2 4F RT A16WE 2001030600263 20010306 00263 NM 2001 3 6 USAA010050 1 20010116 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 32038 24556 CLT - FOUND FLOORBEAM CORRODED 2 INCH BY 4 INCH, TOP OF FLOORBEAM STATION 986.5, LBL 6-43. REPLACED FLOORBEAM PER TR 53 -60-01. (M) 2 L 7 2 4F RT A16WE 2001030600278 20010306 00278 NM 2001 3 6 USAABB01006 1 20010122 A 2100 20224324 DOOR ACTUATOR BOEING 767 767201 1385125 NM RAM AIR EXHUAST FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 646US 56052 23898 PHL - FLT 196 - EN ROUTE PHL-MAN, THE CREW RECEIVED THE EICAS MESSAGE ''R PACK TEMP'' AND THE PACK ''INOP'' LIGHT ILLUMI NATED. CREW TRIED MANUAL CONTROL AND WAS UNSUCCESSFUL. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MA INTENANCE REPLACE THE RAM AIR EXHAUST DOOR ACTUATOR. (M) 2 L 7 2 4F RT A1NM 2001030600279 20010306 00279 NM 2001 3 6 USAA010044 1 20010115 A 5347 SEAT TRACK BOEING 757 7572B7 1384964 NM CABIN CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 630AU 21104 27808 CLT - FOUND FORWARD COAT CLOSET TRACK CORRODED 3 INCHES BY 2 INCHES, STATION 377.7, LB 24.75. INSTALLED NEW SEAT TRACK PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 2001030600280 20010306 00280 NM 2001 3 6 USAA010045 1 20010115 A 5347 SEAT TRACK BOEING 757 7572B7 1384964 NM CABIN CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 630AU 21104 27808 CLT - FOUND FORWARD COAT CLOSET TRACK CORRODED 3 INCHES BY 2 INCH, STATION 377.7, LBL 45.75. INSTALLED NEW SEAT TRACK P ER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 2001030600281 20010306 00281 NM 2001 3 6 USAA010046 1 20010115 A 5347 SEAT TRACK BOEING 757 7572B7 1384964 NM CABIN CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 630AU 21104 27808 CLT - FOUND SEAT TRACK CORRODED 3 INCHES, STATION 1640 R OUTBOARD SEAT TRACK UPPER SURFACE. REMOVED AND REPLACED PER SR M 51-40-02. (M) 2 L 7 2 4F RT A2NM 2001030600282 20010306 00282 NM 2001 3 6 USAA010047 1 20010115 A 5347 SEAT TRACK BOEING 757 7572B7 1384964 NM CABIN CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 630AU 21104 27808 CLT - FOUND SEAT TRACK CORRODED 3 INCHES, STATION 1640 RT INBOARD SEAT TRACK UPPER SURFACE. REMOVED AND REPLACED PER SR M 51-40-02. (M) 2 L 7 2 4F RT A2NM 2001030600283 20010306 00283 NM 2001 3 6 USAA010063 1 20010122 A 5320 PAN BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 630AU 21104 27808 CLT - FOUND FLOORPAN CORRODED 35 INCHES, BETWEEN STATION 1681.8 TO 1720. CORROSION LEVEL 1C 53-251-03. INSTALLED DOUBL ER PER SRM 53-60-51. (M) 2 L 7 2 4F RT A2NM 2001030600284 20010306 00284 NM 2001 3 6 USAA010043 1 20010115 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 630AU 21104 27808 CLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 5.5 INCHES, STATION 377.7, LBL 24.5. INSTALLED FABRICATED T-CAP PER TR 53-15 -01 AND SRM 53-00-01. (M) 2 L 7 2 4F RT A2NM 2001030600285 20010306 00285 NM 2001 3 6 USAA010068 1 20010123 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 630AU 21104 27808 CLT - FOUND T-CAP CORRODED 20 INCHES, LBL 55 TO RBL 55 STATION 1640 ENTIRE LENGTH OF T-CAP. FABRICATED FILLER AND REPAI R DOUBLER PER EA 68897. (M) 2 L 7 2 4F RT A2NM 2001030600286 20010306 00286 NM 2001 3 6 USAA010048 1 20010116 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 630AU 21104 27808 CLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH, STATION 377.7, LBL 22 - LBL 48. INSTALLED FABRICATED T-CAP PER TR 53-1 5-01 AND SRM 53-00-01. (M) 2 L 7 2 4F RT A2NM 2001030600299 20010306 00299 NM 2001 3 6 USAASB01040 1 20010207 A 2150 204050101 ACM BOEING 737 7373B7 1384580 NM AC BAY FAILED A USAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 391US 16462 23313 SAV - FLT 357 - EN ROUTE FROM MCO-DCA, AT FL330, FLIGHT LOST PRESSURIZATION CONTROL. CABIN ALTITUDE WARNING HORN SOUNDE D AS THE CABIN INDICATOR SHOWED THE CABIN CLIMBING TO 11,000 FT. SEVERAL ATTEMPTS WERE MADE TO CONTROL THE CABIN BUT WER E UNSUCCESSFUL. CREW DESCENDED THE FLIGHT TO 10,000 FEET AND THEN DIVERTED TO SAV. FLIGHT LANDED WITHOUT FURTHER INCID ENT. NO EMERGENCY WAS DECLARED AND THE OXYGEN MASKS WERE NOT DEPLOYED. MX ACCOMPLISHED PRESSURIZATION CONTROL SYSTEM O PS CHECK. OPS TEST GOOD. PRESSURIZED FUSELAGE TO OVER 6 PSI. NO LEAKS FOUND AT DOORS IN FUSELAGE. ACCOMPLISHED PRESS URIZATION CONTROL FUNCTIONAL CHECK PER JOB CARD J321-30-10. FUNCTIONAL CHECK GOOD WITH ALL PIN VOLTAGES NORMAL. REPLAC 2 L 7 2 4F RT A16WE 2001030600300 20010306 00300 NM 2001 3 6 USAASB01029 1 20010130 A 2913 6507506 PUMP BOEING 737 7373B7 1384580 NM NR 1 ENGINE FAILED A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 517AU 18106 23703 CLT - FLT 1633 - EN ROUTE FROM IAH-PHL, THE ''A'' HYDRAULIC SYSTEM LOW PERSSURE LIGHT ILLUMINATED ALONG WITH ''A'' HYDRA ULIC QUANTITY READING BELOW QUARTER. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECL ARED. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP PER MM 29-15-12. OPS CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001030700584 20010307 00584 EU 2001 3 7 20010227CW006 1 20010223 A 7120 BOLT AMD FALC20 FALCON200 2730150 EU GARRTT ATF3 ATF3* 29002 WP THRUST BEARING MISSING E K NONE O OTHER IN INSP/MAINT 1 SW 99 500RR 3990 491 P20173 DURING BOTH OB SLAT REMOVALS FOR RESKINS WERE NOISES INSIDE LE, S. UPON INVESTIGATION, FOUND 3 EA BOLTS IN THE RT OB AND 1 EA IN LT OB LE,S. DETERMINED TO BE FROM NR 1 ENG THRUST BRG SUPPT PLATE, WHICH IS SUPPOSED TO HAVE 8 EA BOLTS. ENG MFG REQUESTED ENG TO BE REMOVED AND SENT TO MFG FOR TEARDOWN AND INVESTIGATION. OUT OF 8 BOLTS INSTALLED, ONLY 2 EA REMAINED INTACT ON THE ENG, THEREFORE 6 EA BOLTS WERE IN THE AIRCRAFT SYSTEM TO BE LOCATED. AT SENDING OF SDR, HAVE LO CATED 4 EA BOLTS, 2EA STILL MISSING. THIS AREA OF ENG CAN NOT BE SEEN COMPLETELY. VIA BOROSCOPE ONLY, CAN 5 OR 6 BOLT S BE VISUAL CKD. 2 L 7 2 4F 4 F RT A7EU E7WE 2001030700586 20010307 00586 CE 2001 3 7 20010227CW008 1 20010201 A 3710 242CW PUMP BEECH 36 36BEECH 1151602 CE VACUUM SYSTEM MALFUNCTIONED B EBTR O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 09 6222V E3 LOST VACUUM IN FLIGHT. FOUND DRIVE SHAFT SHEARED. INSTALLED REPLAACEMENT PUMP SYSTEM. CK SATISFACTORY. NO LOG ENTRY FOUND FOR S/N OF VACUUM PUMP REMOVED 1 L 7 1 3O 3A15 2001030700588 20010307 00588 CE 2001 3 7 20010227CW010 1 20010212 A 3110 LIGHT CESSNA 182 182S 2072701 CE LYC O540 IO540* 41532 EA INSTRUMENT PANEL INOPERATIVE B ESMR K NONE O OTHER IN INSP/MAINT 1 SO 11 72689 18280820 PILOT/OWNER REPORTED THAT RADIO INDICATOR BACKLIGHTING AND RADIO CONTROL BACKLIGHTING HAD NOT WORKED SINCE AIRCRAFT DELI VERY. TROUBLESHOT SYSTEM, FOUND THAT PIN 1 OF JC005 WAS AT GROUND POTENTIAL, PREVENTING DIMMER POTENTIOMETER FROM FUNCT IONING AS IT IS SUPPOSED TO. REMOVED WIRE 6JC015-1JC005 FROM CIRCUIT AND FOUND THAT RADIO LIGHTING WORKED AS IT WAS SUP POSED TO. WIRE 6JC015-1JC005 HOOKS INTO THE WARNING/CAUTION ANNUNCIATOR. THIS ANNUNCIATOR HAS ITS OWN SWITCH/ LOCATED A T THE TOP OF THE RADIO STACK/ FOR BRIGHT/DIM/TEST. 1 H 7 1 3O 3 O NT 3A13 1E4 2001030700599 20010307 00599 NE 2001 3 7 20010226CW001 2 20010128 A 8530 153084 CYLINDER DOUG DC4 C54BDC 3021516 WP PWA R2000 R20007M2 52023 NE HAMSTD 23E 23E50 NE NR 4 ENGINE DAMAGED I B2OB K NONE O OTHER IN INSP/MAINT 1 AL 01 44911 856 10461 104147 8388 VALVE CHECK SHOWS EXCESS WOBLE IN EX GUIDE. 2 L 7 4 4R 4 R A762 5E5 6 C P603 2001030700600 20010307 00600 WP 2001 3 7 20010226CW002 1 20010129 A 8011 JH6FR3 STARTER DOUG DC4 C54BDC 3021516 WP PWA R2000 R20007M2 52023 NE HAMSTD 23E 23E50 NE NR4 ENGINE INOPERATIVE I B2OB K NONE O OTHER IN INSP/MAINT 1 AL 01 44911 860 10461 104147 8388 WOULD NOT TURN ENGINE OVER, INOPERATIVE. 2 L 7 4 4R 4 R A762 5E5 6 C P603 2001030700602 20010307 00602 WP 2001 3 7 20010226CW003 1 20010123 A 5753 SKIN DOUG DC4 C54BDC 3021516 WP PWA R2000 R20007M2 52023 NE HAMSTD 23E 23E50 NE TE FLAPS DAMAGED I B2OB K NONE O OTHER IN INSP/MAINT 1 AL 01 44911 10461 WEAR AND TEAR FROM GRAVEL STRIPS, NEED NEW SKINS. BEARING IN PORK CHOPS WERE CHANGED EVEN IF NOT NEEDED. 2 L 7 4 4R 4 R A762 5E5 6 C P603 2001030700603 20010307 00603 WP 2001 3 7 20010226CW004 1 20010123 A 5542 FABRIC DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE HAMSTD 23E 23E50 NE RUDDER DAMAGED I B2OB K NONE O OTHER IN INSP/MAINT 1 AL 01 44911 10461 RUDDER WAS BEYOND PATCHING. NEEDS RECOVER. 2 L 7 4 4R 4 R A762 5E5 6 C P603 2001030700615 20010307 00615 NM 2001 3 7 DHL2001712521 1 20010208 A 5312 PRESSURE PANEL BOEING 727 72729 1384007 NM MLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 C-CHECK, MAIN CARGO MLG WHEEL WELL TOP SURFACE SHOWS 4 CRACKS OF .5 INCH BETWEEN RBL 17 AND RBL 25, STA 910 AND STA 920. REMOVED FLOOR PANELS, BRACKETS, CLIPS, STRAPS DWG 65-89360-3. PERFORMED STOP DRILL IAW DWG 65-89360-3. FABRICATED DO UBLER (ALCLAD 2024, T3, 0.080 INCH; 14 INCH X 32 INCH) IAW DWG 65-89360-3. CLEANED, TREATED AND PRIMED IAW SEM 51-10-2, PAGE 1 AND 2. REINSTALLED FLOOR PANELS, BRACKETS, CLIPS, STRAPS IAW DWG 65-89360-3. REFER TO J/C 7107 FOR OPS CHECK. (NON-ROUTINE CARD 0412) 2 L 7 3 4F A3WE 2001030700628 20010307 00628 CE 2001 3 7 20010222CW012 1 20010117 A 5320 1455078528 BRACKET CESSNA 500 550 2076604 CE CARGO BAY CRACKED C U1CM K NONE O OTHER IN INSP/MAINT 1 SW 17 26496 5215 5500607 DURING SCHEDULED INSPECTION, IT WAS FOUND THAT THE RIGHT HAND BATTERY SUPPORT BRACKET HAD A CRACK 3/4 OF THE WAY THROUGH THE SUPPORT CHANNEL. THIS BRACKET SUPPORTS HALF OF THE WEIGHT OF YOU NICAD OR LEAD ACID BATTERY. IT SHOULD BE CAREFUL LY LOOKED AT DURING ALL INSPECTIONS. 1 L 7 2 4F A22CE 2001030700638 20010307 00638 CE 2001 3 7 20010208CW009 1 20010106 A 3230 LANDING GEAR BEECH 1900 1900D 1154162 CE MLG/NLG MALFUNCTIONED A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 27 87555 UE234 CLE FLIGHT 3231 THE CREW REPORTED THE LANDING GEAR FAILED TO EXTEND WHEN THE HANDLE WAS PLACED IN THE DOWN POSITION. T HE GEAR WAS EXTENDED MANUALLY AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SERVICED THE LANDING GEAR, HYDRAULIC ACCUMULATOR. OPERATIONAL CHECKS WERE GOOD. AC WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT A24CE 2001030700679 20010307 00679 EA 2001 3 7 20010213CW013 2 20010123 A 7200 ENGINE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA RIGHT FAILED A NSVA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 15031 * 68397 UC103 32344 DURING TAKE OFF FROM ISP, PILOTS REPORTED HEARING A BANG AND OBSERVED SPARKS COMING FROM THE RIGHT ENGINE EXHAUST DUCT. ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO GATE WITH NO FURTHER EVENT. PILOTS PERFORMED WALK AROUND INSPECTION AND DISCOVERED DENTS AND HOLES IN THE RIGHT ENGINE EXHAUST STACK. MAINTENANCE WAS DISPATCHED AND DISCOVERED DAMAGE TO THE POWER TURBINE DISC. ENGINE WAS CHANGED AND AIRCRAFT WAS RETURNED TO SERIVCE. 2 L 7 2 4T 4 T RT A24CE E4EA 2001030900132 20010309 00132 EU 2001 3 9 DHL2001367506 1 20010130 A 5315 FLOORBEAM AIRBUS 300 A300B4203 3930306 EU FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH MSN265 C CHECK, HINGED FLOORBEAMS AT FR 54 HAVE EXCESSIVE PLAY N/R 78796. REPAIRED HINGED FLOORBEAM IAW SRM 53-15-00-1 & FSI S B94FS494-53-12. REFITTED FLOORBEAM. 2 L 7 2 4F RT A35EU 2001030900133 20010309 00133 NM 2001 3 9 UPS01434908 1 20010207 A 2760 SPOILER BOEING 747 747121 1384871 NM WING INOPERATIVE A IPXA O OTHER O OTHER LD LANDING 1 SO 01 683UP 20353 INSPECTION TYPE:N/A, NR 6 SPOILER INOP. PIREP - ROLLS RIGHT ON LANDING. *S/D* REMOVED NR 6 SPOILER PANEL AND ACT. IN STALLED NR 6 SPOILER PER MM 27-61-01. OPS CKS GOOD. 2 L 7 4 4F A20WE 2001030900134 20010309 00134 NM 2001 3 9 01FDEA00102 1 20010208 A 2611 SMOKE DETECTOR BOEING 727 727227 1384078 NM CARGO BAY MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 487FE 21490 CARGO SMOKE LIGHT CAME ON AFT APPROX 1 MIN NO BOTTLES FIRED. LIGHT WENT OUT. SYS CK OK. *S/D* TROUBLESHOT SYS PER MM 26-17-001-1. PERF BITE TEST ON CEU''S NR 1 AND 2, NO FAULTS. NO FAULTS ON FIRE PROTECTION CONTROL PNL. ALL SQUIB LIG HTS ILLUM. SYS TEST NORMAL. 2 L 7 3 4F A3WE 2001030900135 20010309 00135 NM 2001 3 9 01FDEA00103 1 20010208 A 2613 WARNING LIGHT BOEING 727 727227 1384078 NM COCKPIT ILLUMINATED A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 492FE 21530 NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUM AFT T/O. *S/D* TIGHTENED LOOSE CLAMPS IN STUB WING. REF 36-00-001-2. RAN ENG PER JET RUN HDBK CHPT 5, NO LEAKS NOTED. OK FOR SERVICE. 2 L 7 3 4F A3WE 2001030900136 20010309 00136 CE 2001 3 9 GLBA2001034 1 20010212 A 3610 CLAMP BEECH 1900 1900D 1154162 CE BLEED AIR OUT OF POSITION A GLBA D RETURN TO BLOCK J WARNING INDICATION NR NOT REPORTED 1 CE 01 226GL UE226 RETURN TO BLOCK - RIGHT BLEED AIR FAIL. REPOSITIONED CLAMP AND REPAIRED EVA TUBING, OPS CHECKED SYSTEM GOOD. RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 2001030900137 20010309 00137 CE 2001 3 9 GLBA2001037 1 20010212 A 3230 LANDING GEAR BEECH 1900 1900D 1154162 CE NLG & MLG MALFUNCTIONED A GLBA O OTHER O OTHER AP APPROACH 1 CE 01 251GL UE251 GEAR WOULD NOT EXTEND, RECYCLED FOUND C/B POPPED RESET AND GEAR EXTENDED. INSPECTED WIRING, PERFORMED GEAR SWING. SYST EM OPS CHECKED GOOD. RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 2001030900138 20010309 00138 NM 2001 3 9 UPS01234998 1 20010215 A 3510 FITTING BOEING 727 727180C 138406G NM O2 BOTTLE BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE:IN OXYGEN BOTTLE ATTACHING HARDWARE BROKEN. *S/D* REMOVED AND REPLACED MS FITTING ON BLOWOUT LINE AND UPPER 02 BOTTLE CLAMP. REMOVED AND REPLACED 02 BOTTLE. LK CHECK GOOD. 2 L 7 3 4F A3WE 2001030900139 20010309 00139 WP 2001 3 9 RRXA010005 1 20010201 A 2731 TAB DOUG DC8 DC873F 302199F WP ELEVATOR VIBRATION A RRXA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 15 602AL 45991 ELEVATOR CONTROL HAS VIBRATION WHICH INCREASES WITH AIRSPEED ABOVE 250 KTS ANY DOWNWARD PRESSURE ON THE YOKE WILL CAUSE THE YOKE TO KICK BACK (AUTOPILOT OFF) (PTC ON/OFF MADE NO DIFFERENCE). REMOVED AND REPLACED ELEV LOUD FEEL CENTERING ME CHANISM IAW DC-8 M/M 27-30-4, OPS CK GOOD ON GROUND. REMOVED AND REPLACED LT ELEVATOR CONTROL TAB IAW DC-8 M/M 27-30-2. 2 L 7 4 4F RT 4A25 2001030900140 20010309 00140 NE 2001 3 9 RRXA010006 2 20010201 A 7220 ENGINE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE NR 3 ENGINE FOD A RRXA K NONE C F.O.D. IN INSP/MAINT 1 WP 15 795FT 46103 ON WALK-AROUND FOUND FOD ON NR 3 ENGINE. 2 L 7 4 4F 4 F RT 4A25 E2GL 2001030900141 20010309 00141 WP 2001 3 9 RRXA010007 1 20010206 A 7120 MOUNT DOUG DC10 DC1010F 3022111 WP NR 1 ENGINE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 68042 46901 NR 1 ENG AFT PYLON AFT MOUNT SUPPORT CORRODED AND DOWL PINS ARE LOOSE. REMOVED AND REPLACED NR 1 ENGINE AFT MOUNT AS RE QUIRED IAW DC-10 M/M 71-20-00, TORQUED ENGINE MOUNT IAW DC-10 M/M 20-50-02. OPS CHECK GOOD. 2 L 7 3 4F A22WE 2001030900142 20010309 00142 WP 2001 3 9 RRXA010008 1 20010206 A 3244 TIRE DOUG DC8 DC871 302199A WP MLG FAILED A RRXA K NONE O OTHER LD LANDING 1 WP 15 811AL 46099 RIGHT MAIN GEAR TIRES BLEW ON LANDING. REMOVED AND REPLACED RT MLG WHEEL AND TIRE ASSYS IAW M/M 32-40-1 (TIRE POSITIONS 4, 5, 7, 8). 2 L 7 4 4F 4A25 2001030900143 20010309 00143 WP 2001 3 9 RRXA010009 1 20010211 A 7931 LIGHT DOUG DC8 DC873F 302199F WP INSTRUMENT PNL MALFUNCTIONED A RRXA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 WP 15 961R 46133 NR 3 ENGINE OIL PRESSURE LIGHT ILLUMINATED IN FLIGHT 3900 FEET, M.8 249 KIAS OIL PRESS 42, PSI IDLE 32 PSI. LIGHT REMAI NED ILLUMINATED AS POWER REDUCED FROM CRUISE TO IDLE POWER. INFLIGHT SHUTDOWN PERFORMED IAW QRH. AFTER SHUTDOWN OIL PR ESSURE LIGHT REMAINED ILLUMINATED CONTINUOUSLY THROUGH LANDING, WINDMILLING PSI 4. TROUBLESHOOTING FOUND THE LIGHT BULB IN NR 3 LOW OIL PRESSURE LIGHT CONNECTION BAD DUE TO SOLDER ON LIGHT SOCKET. CLEANED SOCKET, RELAMPED, OPS CHK NORMAL IAW M/M 79-31-05. 2 L 7 4 4F RT 4A25 2001030900144 20010309 00144 2001 3 9 RRXA010010 4 20010212 A 2215 61574317 SERVO DOUG DC8 DC871F 302199D WP AUTOPILOT SYS MALFUNCTIONED A RRXA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 WP 15 8177U 3530 45983 AUTOPILOT PORPOISING IN VERTICAL SPEED AND PITCH DUMP MODES (ROUGH PORPOISING). PROBLEM DUPLICATED, REPLACED A/P ELEVAT OR SERVO IAW DC-8 M/M 22-12-02 AND A/P PITCH CHANNEL COMPUTER IAW DC-8 M/M 22-10-39, SYS OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2001030900145 20010309 00145 NM 2001 3 9 CALA0100115 1 20010214 A 5311 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32626 27530 INSPECTION FOUND A 1 INCH CRACK IN FWD STUB FRAME AT STA 295, FLOOR LEVEL. THE CRACKED SECTION OF FORWARD FRAME WAS TRI MMED OFF AND REPAIR WAS ACCOMPLISHED IAW ECRA 5310-03895. 2 L 7 2 4F RT A16WE 2001030900146 20010309 00146 NM 2001 3 9 CALA0100116 1 20010214 A 5347 SEAT TRACK BOEING 737 737524 1384721 NM CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32626 27530 INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT STA 344-360. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INST ALLED IAW SRM 53-00-52. 2 L 7 2 4F RT A16WE 2001030900147 20010309 00147 NM 2001 3 9 CALA0100117 1 20010214 A 5754 SKIN BOEING 737 7373T0 1384582 NM LT SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND LT WING NR 3 SLAT COVER SKIN CRACKED AROUND FASTENER HOLE AT WBL 254.0. THE CRACKED SKIN WAS CUT OUT. DOUBLER AND FILLER WERE INSTALLED IAW SRM 57-43-01, PAGE 216. 2 L 7 2 4F RT A16WE 2001030900148 20010309 00148 NM 2001 3 9 CALA0100118 1 20010214 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND TWO FLOOR SUPPORTS CORRODED AT STA 967-986, RBL 16. THE FLOOR SUPPORTS WERE REMOVED AND NEW FLOOR SUPP ORTS WERE INSTALLED IAW SRM 51-40-2. 2 L 7 2 4F RT A16WE 2001030900149 20010309 00149 NM 2001 3 9 CALA0100119 1 20010214 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND SEAT TRACK CORRODED AT STA 927-967, RBL 13. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SR M 51-10-2 AND 53-00-52. 2 L 7 2 4F RT A16WE 2001030900150 20010309 00150 NM 2001 3 9 CALA0100120 1 20010214 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 950, LBL 25 - LBL 40. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPP ORT WAS INSTALLED IAW SRM 51-40-2. 2 L 7 2 4F RT A16WE 2001030900151 20010309 00151 NM 2001 3 9 CALA0100121 1 20010215 A 5312 BULKHEAD BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70330 23460 INSPECTION FOUND TWO CRACKS ON FLOOR STRUCTURE WEB AT LT AND RT W/L 195, ONE CRACK ON CENTER WEB AT W/L 200, LBL 5.7 AND ONE CRACK ON CENTER WEB AT W/L 201, RBL 5.7 DURING 737 FUS-BS 178 BULKHEAD INSPECTION. THE CRACKS WERE .5 INCH IN LE NGTH. REPAIRS WERE ACCOMPLISHED IAW EA 5310-1-0037. 2 L 7 2 4F RT A16WE 2001030900152 20010309 00152 NM 2001 3 9 CALA0100122 1 20010215 A 5330 SKIN BOEING 737 737524 1384721 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13624 27528 INSPECTION FOUND A DENT IN FUSELAGE SKIN AT STA 396, JUST ABOVE STRINGER 18L. A REPAIR WAS INSTALLED IAW ECRA 5330-0303 1. 2 L 7 2 4F RT A16WE 2001030900153 20010309 00153 NM 2001 3 9 CALA0100123 1 20010216 A 5330 SKIN BOEING 737 737524 1384721 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32626 27530 INSPECTION FOUND EXTERIOR FUSELAGE SKIN DENTED BETWEEN STA 320 AND 335, STRINGER 24-25R. INSTALLED REPAIR PER SRM 53-00 -01, FIGURE 210. 2 L 7 2 4F RT A16WE 2001030900154 20010309 00154 EA 2001 3 9 COMA0160240 1 20010213 A 3250 16900107 ECU CNDAIR CL600 CL6002B19 EA EE BAY FAILED A COMA K NONE J WARNING INDICATION CR CRUISE 1 SO 01 979CA 9875 7159 STEERING INOP CAUTION MESSAGE. REPLACED THE STEERING ECU. 2 L 7 2 4F RT A21EA 2001030900155 20010309 00155 EA 2001 3 9 COMA0160241 1 20010213 A 2750 7455001 LEVER CNDAIR CL600 CL6002B19 EA INST PANEL MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 936CA 235 7043 FLAPS FAIL MESSAGE. REPLACED THE FLAP SELECTOR LEVER ASSY. 2 L 7 2 4F RT A21EA 2001030900156 20010309 00156 EA 2001 3 9 COMA0160242 1 20010212 A 3230 46193 VALVE CNDAIR CL600 CL6002B19 EA NLG MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 986CA 9205 7174 LANDING GEAR DISAGREE MESSAGE. NLG DID NOT RETRACT. REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2001030900157 20010309 00157 NM 2001 3 9 PCAA0102005 1 20010215 A 3350 40005130003 SWITCH DHAV DHC8 DHC8102 2809003 NM FA PANEL DEFECTIVE A PCAA K NONE O OTHER CL CLIMB 1 EA 13 830EX 155 MDT FLIGHT 3800. CREW REPORTED CABIN EMERGENCY LIGHTS FLICKERED ON INTERMITTANTLY DURING CLIMBOUT, AFTER POWER REDUCTIO N, AFTER CRUISE. MAINTENANCE REPLACED SWITCH AT FLIGHT ATTENDANTS LIGHTING PANEL. OPERATIONAL CHECK GOOD. AIRCRAFT RE TURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001030900158 20010309 00158 NM 2001 3 9 UPS01235000 1 20010213 A 2910 65178218 MODULE BOEING 727 72731C 1384011 NM HYDRAULIC SYS FAILED A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 922UP 19231 INSPECTION TYPE:N/A ON CLIMBOUT OF WAW A-SYS HYD PRESS DROPPED TO ZERO. NO FLUID LOSS. INADVERTANT DEPLOYMENT OF NR 1 THRUST REVERSER ON TOUCH DOWN. REPLACED A-HYD SYS PRESSURE MODULE DEACTIVATED NR1 T-R PER MEL. SUSPECT OUT OF RIG. 2 L 7 3 4F A3WE 2001030900159 20010309 00159 NM 2001 3 9 UPS01434993 1 20010110 A 5330 69B0279041 SKIN BOEING 747 747123F NM FUSELAGE WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, TAIL AT STA 2742 ON LT SIDE OF FUSE WHERE APU DOOR SITS ON FUSE SKIN REPLACE ANGLE SKIN ANGLE WORN AWAY. NEW FRAME FITTED IAW SRM 51-30-02. 2 L 7 4 4F A20WE 2001030900160 20010309 00160 NM 2001 3 9 UPS01434995 1 20010103 A 2780 65B0113519 FITTING BOEING 747 747123F NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, RT WING L/E INBOARD SWAN NECK HINGE FITTING ON BULL NOSE OF VCF 20 IS CRACKED. REPLACED SWAN NECK HI NGE FITTING INBOARD NR 20 VCF IAW MM 27-81-02. 2 L 7 4 4F A20WE 2001030900161 20010309 00161 WP 2001 3 9 UPS01834999 1 20010124 A 5310 5772785103 SHEAR TIE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1,3, STA 134 AND 140 HAS CRACKED SHEAR TIES BETWEEN LONG 5L AND 6L. REMOVED, FABRICATED, AND REPLACED SHEAR TIES IAW DWG 5772785, AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001030900162 20010309 00162 NM 2001 3 9 0100306310 1 20010212 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 670US 24225 DURING OVERNIGHT LINE CHECK, MAINTENANCE FOUND EMERGENCY PATH LIGHTS ROWS 1AB-12AB INOPERATIVE. MAINTENANCE SECURED WIR ING AT ROW 12AB. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001030900163 20010309 00163 NM 2001 3 9 0100426303 1 20010215 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 663US 23818 DURING OVERNIGHT LINE CHECK, MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE IN ZONE-B LEFT SIDE AND D-ZONE RIGHT SIDE. MAINTENANCE REPAIRED LOOSE WIRES. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001030900164 20010309 00164 WP 2001 3 9 0100439610 1 20010212 A 4990 APU DOUG DC9 DC932 3022066 WP FUSELAGE OVERSERVICED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 610NW 47432 DURING CLIMB, FLIGHT ATTENDANTS REPORTED SMOKE IN CABIN. FORWARD LAV DETECTOR SOUNDED. FLIGHT CREW RETURNED TO DEPARTU RE AIRPORT. SMOKE BEGAN TO DISSIPATE DURING RETURN TO DEPARTURE AIRPORT. AN UNEVENTFUL LANDING WAS PERFORMED. MAINTEN ANCE FOUND APU OIL OVERSERVICED AND OIL IN THE PNEUMATIC DUCTS. PACK BURNOUT PROCEDURES WERE PERFORMED AND WATER SEPARA TORS WERE REPLACED. 2 L 7 2 4F A6WE 2001030900165 20010309 00165 WP 2001 3 9 0100449880 1 20010209 A 2611 SMOKE DOUG DC9 DC951 3022051 WP LAVATORY DETECTED A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 675MC 47651 BOTH AFT LAVATORY SMOKE DETECTORS ACTIVATED WHILE EN ROUTE. FLIGHT ATTENDANTS REPORTED BLUE SMOKE IN LAVS. APU WAS NOT OPERATING AND NO INDICATION OF PACK MALFUNCTIONS. ELECTRICAL SMELL WAS REPORTED. IDLE DESCENT BEGAN AT 10,000 FEET. NO POWER TO SMOKE RELATED ISSUES. FLIGHT LANDED SAFELY AT DTW. MAINTENANCE INSPECTED AFT LAVS AND CABIN OVERHEAD WITH ALL FOUND NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2001030900166 20010309 00166 NE 2001 3 9 0100459984 2 20010205 A 7321 7436024 FUEL CONTROL DOUG DC9 DC932 3022066 WP PWA JT8 JT8D15 52051 NE RT ENGINE MALFUNCTIONED A NWAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 01 984US 1032 47383 696472 DURING TAKEOFF, THE FLIGHT CREW REPORTED A COMPRESSOR STALL BELIEVED TO BE FROM THE RIGHT ENGINE. A HIGH SPEED ABORTED TAKEOFF WAS ACCOMPLISHED AND THE FLIGHT RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REPLACED THE FUEL CONTROL UN ITS LOCATED ON BOTH LEFT AND RIGHT ENGINES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F 4 F A6WE E2EA 2001030900167 20010309 00167 NM 2001 3 9 0100462289 1 20010204 A 2730 FEEL UNIT BOEING 727 727251 138408H NM ELEVATOR MALFUNCTIONED A NWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 01 289US 21377 AFTER TAKEOFF, CREW REPORTED ELEVATORS FELT STIFF. MOST STIFF IN UP MOVEMENTS. FLIGHT RETURNED TO MSP AND LANDED WITHO UT INCIDENT. MAINTENANCE REPLACED ELEVATOR FEEL COMPUTER. CABLE TENSIONS AND CABLE RUNS ALL CHECKED OK. OPERATIONAL C HECKS AND TEST FLIGHT FOUND ELEVATORS OK. 2 L 7 3 4F A3WE 2001030900168 20010309 00168 2001 3 9 MWEA010157 4 20010215 A 2565 100503117 SLIDE DOUG DC9 DC981 3022081 WP AFT SERV DOOR DISLODGED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 806ME 48032 AFT GALLEY SERVICE DOOR FELL OUT. MAINTENANCE REINSTALLED AFT GALLEY DOOR SLIDE. 2 L 7 2 4F A6WE 2001030900169 20010309 00169 WP 2001 3 9 MWEA010158 1 20010210 A 5520 591041235 ELEVATOR DOUG DC9 DC932 3022066 WP LT ELEVATOR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 LEFT ELEVATOR HAD LIGHTNING STRIKE EXIT DAMAGE OUTBOARD OF LAST STATIC WICK MOUNT ON TRAILING EDGE. REMOVED DAMAGED PAR TS, FABRICATED, LOCATED AND INSTALLED NEW PARTS. 2 L 7 2 4F A6WE 2001030900170 20010309 00170 NM 2001 3 9 TWAA0103101 1 20010216 A 3350 582243 POWER SUPPLY BOEING 767 767231 1385131 NM CABIN DISCHARGED A TWAA K NONE O OTHER CR CRUISE 1 CE 05 602TW 22565 THE EGRESS LIGHTS ON RT SIDE OF CABIN ROWS 11 THRU 16 ILLUMINATED INTERMITTENTLY. REPLACED THE POWER SUPPLY. CHECK-C 1 1-29-00 LAX. 2 L 7 2 4F RT A1NM 2001030900171 20010309 00171 WP 2001 3 9 TWAA0103102 1 20010215 A 3350 408822101 BATTERY DOUG DC9 DC983 3022083 WP FWD ENTRY DISCHARGED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 931TW 49527 THE OVERHEAD EMERGENCY LIGHTS IN THE COCKPIT AND FWD ENTRY WERE INOPERATIVE. REPLACED THE BATTERIES. CHECK-C 12-28-00. 2 L 7 2 4F RT A6WE 2001030900172 20010309 00172 WP 2001 3 9 TWAA0103103 1 20010214 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT, THE RT SIDE FWD CABIN DOOR AREA, FLOOR SUPPORT AT STA 172, 18 INCHES TO RT OF BL 0, WAS CORRODED. REPLACED FLOOR SUPPORT PER SPM 6-70-01. INSTALLED FASTENERS PER 51-30-5. 2 L 7 2 4F A6WE 2001030900173 20010309 00173 WP 2001 3 9 TWAA0103104 1 20010213 A 5320 BRACKET DOUG DC9 DC982 3022082 WP AFT CARGO BAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT FOUND BRACKETS CORRODED AT FWD CARGO DOOR STA 1155 LOWER AFT CORNER OF ENTRY SILL AREA, AND STA 121 2 LOWER FWD CORNER OF ENTRY SILL AREA. INSTALLED NEW BRACKETS PER SRM 51-30-5. PART MANUFACTURED PER DRAWING 5936070. 2 L 7 2 4F A6WE 2001030900175 20010309 00175 SO 2001 3 9 SWIA972360 1 20010213 A 2731 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE ELEVATOR TRIM JAMMED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 298SW 120328 AT FL250 WITH AUTOPILOT ENGAGED THE YELLOW TRIM LIGHT ON AUTOPILOT PANEL ILLUMINATED. DISCONNECTED THE AUTOPILOT AND MA NUALLY MOVED THE TRIM WHEEL AND FOUND IT TO BE JAMMED. TRANSFERRED AUTOPILOT TO CAPTAIN SIDE AND THE SAME OCCURRED. DI SCONNECTED AUTOPILOT AND FOUND TRIM STILL JAMMED. DECLARED AN EMERGENCY AND CONTINUED TO YUM. UPON DESCENT DID NOT TOU CH TRIM PER QRH. REPLACED BOTH ELEVATOR TRIM TABS ACTUATORS. RIGGING AND OPS CHECKS GOOD. SWAPPED OUT FDR. LEFT ACT P/N: 5299, S/N ON: 824, S/N OFF: 738, RIGHT ACT P/N: 5299, S/N ON: FA339, S/N OFF: 743. 2 L 7 2 4T 4 T RT A31SO E20NE 2001030900176 20010309 00176 SO 2001 3 9 SWIA972361 1 20010214 A 3260 SQUAT SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NLG FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 564SW 120339 DURING CLIMBOUT 2000 FEET AURAL WARNING TAKEOFF CONTINOUSLY SOUNDED. ONCE POWER LEVERS PULLED BACK WARNING WENT AWAY. RETURNED TO AIRPORT. REPLACED LANDING GEAR RELAY BOX. P/N ON: 1201110-001, S/N ON: 125399-305, OFF: 120-339. REPLACED RELAY K0122 FOR OPERATIONAL CHECK. FAILED TEST FLIGHT. FOUND NOSE GEAR SQUAT SWITCH BAD. REMOVED AND REPLACED NOSE G EAR SQUAT SWITCH IAW EMB 120 MM 32-01-01. FUNCTIONAL CHECK OF AURAL WARNING SYSTEM WORKS NORMALLY. OPS CHECK GOODP/N O N: 25-00417-02. FOUND BAD FEMALE PIN AT RELAY K0194 RECEPTACLE. REPLACED FEMALE PIN. GROUND OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001030900177 20010309 00177 NE 2001 3 9 SWIA972362 2 20010211 A 7200 ENGINE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE WING FLUCTUATES A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 234SW 120308 CLIMBING THROUGH 15,000 FT EXPERIENCED LARGE ENGINE FLUCTUATIONS (TORQUE DROPS OF 25 TO 45 PERCENT) POWER WAS REDUCED, R ETURNED TO THE MFR APT. EECS DEF. CLEANED EEC CANNON PLUGS. OHMED EEC SYSTEM AND RAN EXTENSIVE GROUND CHECKS OF ALL PARAMETERS AND COULD NOT DUPLICATE. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001030900178 20010309 00178 SO 2001 3 9 SWIA972363 1 20010214 A 2933 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT ACTIVATED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 221SW 120290 HYDRAULIC MASTER CAUTION AND GREEN HYDRAULIC SYSTEM LOW LEVEL LIGHT ON TAKEOFF ROLL. FLUID QUANTITY GAUGE SHOWED IN GRE EN. ABORTED TAKEOFF. DEFERRED PER MEL 29-31-4. 2 L 7 2 4T 4 T RT A31SO E20NE 2001030900179 20010309 00179 CE 2001 3 9 GLBA2001038 1 20010215 A 2730 ELEVATOR BEECH 1900 1900C 1154161 CE TAIL FLUTTER A GLBA O OTHER F FLT CONT AFFECTED DE DESCENT 1 CE 01 122GL UC122 PILOT REPORTED ELEVATOR FLUTTER ON DESCENT AND CLIMB. INSPECTED FLIGHT CONTROLS, PERFORMED TEST FLIGHT. COULD NOT DUPL ICATE, OPS CHECKED GOOD. RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 2001030900180 20010309 00180 EA 2001 3 9 JBXA000246 1 20010216 A 2913 O-RING CNDAIR CL600 CL6002B19 EA HYD PUMP WORN A JBXA A D UNSCHED LANDING RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 05 585ML 7334 SYSTEM NR 1 HYDRAULIC QUANTITY INDICATED 25 PERCENT. REMOVED AND REPLACED O-RINGS ON ENGINE DRIVEN PUMP IAW SERVICE BUL LETIN NR 887055-29-04. SERVICED HYDRAULICS, OPS CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2001030900181 20010309 00181 EA 2001 3 9 JBXA000247 1 20010217 A 2613 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT ACTIVATED A JBXA K NONE J WARNING INDICATION DE DESCENT 1 SO 05 583ML 7327 WING OVERHEAT MASTER CAUTION RT WING AFTER COMPLETEING QRH EMERGENCY 12-2 WING OVERHEAT WARNING CONTINUED TO PERSIST AND WOULD NOT CLEAR. IN LAST 8 MINUTES OF FLIGHT WARNING CLEARED. MAINTENENCE FERRIED TO RDU. PERFORMED OPS CHECK TEST O F WING ANTI-ICE CONTROL AND INDICATION SYSTEM PER AMM 30-12-00-710801. NO DEFECTS FOUND, NO FAIL OR FAULT INDICATIONS. REMOVED AND REPLACED SUSPECTED BAD ANTI-ICE TEMP CONTROLLER (HOLDING ORIGINAL CONTROLLER FOR TROUBLESHOOTING). SYSTEM OPS CHECKED GOOD IAW AMM 30-12-00. NO DEFECTS. 2 L 7 2 4F RT A21EA 2001030900182 20010309 00182 SO 2001 3 9 C2XA01IA087 1 20010214 A 3350 1317 LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12715 120125 IAH - FLIGHT 3408, DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD OVERHEAD EMERGENCY LIGHT WAS INOPER ATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001030900183 20010309 00183 SO 2001 3 9 C2XA01IA088 1 20010210 A 3350 03092022 CONNECTOR EMB 120 EMB120ER 3260203 SO CABIN LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12715 120125 IAH- DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE AISLE PATH EMERGENCY EXIT LIGHT AT SEAT 2A WAS FOUND TO BE INOPERATIVE. MAINTENANCE PLACED THE LIGHT ON MEL 33-51-01 CONTROL NUMBER 009385, AND THE AIRCRAFT WAS APPROVED FOR RET URN TO SERVICE. THE AIRCRAFT LANDED AT SHV ON FLIGHT 3340 ON 02/11/01 WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND RECO NNECTED A LOOSE CONNECTOR FOR THE AFFECTED LIGHT. REMOVED MEL 33-51-01 CONTROL NUMBER 009385, AND THE AIRCRAFT WAS APPR OVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001030900184 20010309 00184 SO 2001 3 9 C2XA01IA089 1 20010214 A 3350 7287114501 SWITCH EMB 145 EMB145LR SO FA PANEL MALFUNCTIONED A C2XA K NONE O OTHER CR CRUISE 1 SW 27 17984 145246 IAH - FLIGHT 4027, THE CREW REPORTED THAT THE EMERGENCY LIGHTS FLASHED INTERMITTENTLY DURING FLIGHT. MAINTENANCE RESET THE FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH, OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED. AIRCRAF T WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001030900185 20010309 00185 NM 2001 3 9 DHL2001720006 1 20010217 A 5630 WINDOW BOEING 727 727228 NM R1 DOOR UNDERTORQUED A DHLA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 720DH 19544 LOUD SQUEAL FROM R1 WINDOW, VARIED WITH AIRSPEED. LANDED AT MCI. RETORQUED R1 WINDOW PER B-727 REF 56-11-11, PRESSURED A/C NO SQUEAL NOTED. 2 L 7 3 4F A3WE 2001030900186 20010309 00186 WP 2001 3 9 ABXA010053 1 20010216 A 3260 H1410051 DOWNLOCK SWITCH DOUG DOUG DC9 DC941 302207N WP NLG DEFECTIVE A ABXA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 968AX N6356 47499 A NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED WHEN LOWERING THE LANDING GEAR. THE CREW PERFORMED A MANUAL GEAR EXTENSION . MAINTENANCE INSPECTED AND REPLACED THE NOSE LANDING GEAR DOWNLOCK SWITCH IAW DC-9 MM 32-60-01. THE AIRCRAFT WAS INSP ECTED FOR STRUCTURAL DAMAGE, NONE WAS NOTED. OPERATION CHECKS WERE PERFORMED IAW DC-9 MM 32-60-01, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001030900187 20010309 00187 2001 3 9 01FDEA00132 4 20010216 A 3442 6225132101 RADAR BOEING 727 72722 1384002 NM NOSE BAY WEAK A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 149FE 19087 WEATHER RADAR WEAK. REPLACED WEATHER RADAR R/T PER MM 34-41-041-4. OPS CK GOOD PER MM 34-41-00-5. 2 L 7 3 4F A3WE 2001030900188 20010309 00188 NM 2001 3 9 01FDEA00135 1 20010216 A 2781 INDICATOR BOEING 727 7272S2F 1384O81 NM COCKPIT MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 215FE 22936 NR 6 SLAT SHOW INTRANSIT AFT FLAPS WERE RAISED TO 0 RED TAB PROC FOLLOW WITH NO IMPROVEMENT. AC ARRIVED WITH FLAPS SEL TO 5 DEGREES, PERF VISUAL INSP, NO DISCREP. OPERATED FLAPS OVER 15 MIN, NO DISCREP. L/E FLAP AND SLAT POS IND SYS CK O K PER MM 27-82-000-0. AS PER MOCC AC OK FOR SERVICE. NO HISTORY IN LAST 90 DAYS. 2 L 7 3 4F A3WE 2001030900189 20010309 00189 EU 2001 3 9 01FDEA00137 1 20010216 A 2611 CG7G011 DETECTOR AIRBUS 300 A300F4605R 3930327 EU EE BAY MALFUNCTIONED A FDEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 25 663FE 766 ON T/O ROLL, ABORTED FOR AVIONICS SMOKE ECAM. RAN CK LIST AND NO SMOKE DETECTED ON SNIFFER. REMOVED AND REPLACED SMOKE DET PER IAW A300-600 MM 26-15-12-4. SYS OPS CK GOOD. 2 L 7 2 4F RT A35EU 2001030900190 20010309 00190 WP 2001 3 9 01FDEA00139 1 20010218 A 2810 TRANSFER TUBE DOUG DC10 DC1010F 3022111 WP NR 2 TANK FAULTY A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 058FE 46705 APPROX 45 MIN AFT T/O FUEL QUANTITY IN NR 2 TANK STARTED TO INCREASE. UNABLE TO STOP TRANSFER FROM OUTBOARD INTO NR 2 T ANK, AND UNABLE TO FEED FUEL FROM NR 2 TANK TO OUTBOARD ENG USING EITHER TRANSFER OR CROSSFEED. REMOVED AND REPLACED NR 2 TANK FUEL LT TRANSFER LINE ASSY PER MM 28-10-00. FUEL SYS OPS CK NORMAL. 2 L 7 3 4F A22WE 2001030900191 20010309 00191 WP 2001 3 9 01FDEA00140 1 20010208 A 3230 CYLINDER DOUG DC10 DC1010 3022110 WP MLG FAULTY A FDEA O OTHER O OTHER TO TAKEOFF 1 SO 25 550FE 46521 ON T/O, GEAR HANDLE WOULD NOT RAISE NORMALLY. RECYCLED GEAR HANDLE, ALL GEAR RETRACTED. REMOVED AND REPLACED THE MAIN LANDING GEAR INTERLOCK FUSE AND THE MLG TRIM INTERLOCK CYLINDER, LAND GEAR OPS CK NORMAL. 2 L 7 3 4F A22WE 2001030900192 20010309 00192 EU 2001 3 9 01FDEA00141 1 20010217 A 7830 PRESSURE SWITCH AIRBUS 300 A300F4605R 3930327 EU NR1 T/R CONTAMINATED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 675FE 789 705261 REJECT T/O, NR 1 ENGINE REVERSER PRESSURIZED LIGHT ON AT ABOUT 69 KTS. FOUND MOISTURE IN PRESSURE SWITCH. PUT HEAT ON THE SWITCH AND DRIED OUT THE SWITCH. RAN ENGINE PER A300 JRH TO T/O POWER AND NO FAULTS NOTED. 2 L 7 2 4F RT A35EU 2001030900193 20010309 00193 EU 2001 3 9 01FDEA00143 1 20010217 A 3230 D221270005 DAMPENER AIRBUS 310 A310203 EU RT MLG FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 403FE 230 AFT T/O GEAR WOULD NOT RETRACT USING EITHER POSITION 1 OR 2, SEL GEAR HANDLE WOULD NOT RETRACT BEYOND NEUTRAL. FOUND SE RVICE IND ON RT GEAR POPPED. REMOVED AND REPLACED RT MLG PITCH DAMPNER PER IAW FX A310 MM 32-11-15-4-01 AND SERVICED IA W FX A310 MM 12-12-32-0. LUBED ALL PIVOT POINTS ON LWR PART OF GEAR. 2 L 7 2 4F RT A35EU 2001030900194 20010309 00194 NM 2001 3 9 DHL2001743001 1 20010217 A 3411 0851CM2 PITOT TUBE BOEING 727 727225 1384077 NM LT FUSELAGE FAILED A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 743DH ON CLIMBOUT MCO LEFT PITOT HEAT LIGHT ILLUMINATED. PERFORMED ABNORMAL PROC. FOUND LEFT PITOT CB TRIPPED. REMOVED AND REPLACED CAPT PITOT PROBE IAW B727 M/M 34-11-21. OP CK NORMAL IAW B727 MM 30-31-0 L/C CHECK GOOD IAW B727 MM 34-11-0. 2 L 7 3 4F A3WE 2001030900195 20010309 00195 NM 2001 3 9 01FDEA00081 1 20010206 A 5347 BAC75061108 SEAT TRACK BOEING 727 727227 1384078 NM CABIN CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 CORROSION ON SEAT TRACK FLANGE AT LBL 24, WL 208 AT BS 774.5 - 779. *S/D* REMOVED AND REPLACED FLANGE ON LONGITUDINAL BEAM PER FEDEX EA 7-5310-56251. 2 L 7 3 4F A3WE 2001030900196 20010309 00196 NM 2001 3 9 01FDEA00082 1 20010206 A 5315 7075T6511 FLOORBEAM BOEING 727 727227 1384078 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 CORROSION ON PREVIOUS REPAIR TO FLOORBEAM UPPER FLANGE BS 360, RBL 8 - LBL 8, WL 208. *S/D* REMOVED AND REPLACED PER F EDEX EA 7-5310-5620. 2 L 7 3 4F A3WE 2001030900197 20010309 00197 EU 2001 3 9 ERYA682D2101 1 20010210 A 5320 STRUCTURE HAWKER BAE125 BAE125700B 7450007 EU LT MLG WW CRACKED E ERYA K NONE O OTHER IN INSP/MAINT 1 CE 07 731DL 8385 NA0234 CRACK IN LEFT HAND WHEEL WELL TUB, EXTENDING BEYOND PREVIOUS STOP DRILL REPAIR. 2 L 7 2 4F RT A3EU 2001031200482 20010312 00482 NM 2001 3 12 01FDEA00106 1 20010210 A 7830 41011003 LIGHT BOEING 727 72725 1384006 NM COCKPIT INOPERATIVE A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 509FE 18280 NR 3 ENG REVERSER LIGHT ILLUM. REMOVED AND REPLACED REVERSER ACTUATOR COVERS. NEED SOCKET MPN 04-1011-003. ALL CKS GO OD. ALL PNLS REINSTALLED. AC OK FOR SERVICE. 2 L 7 3 4F A3WE 2001031200483 20010312 00483 EU 2001 3 12 ERYA682D2 1 20010210 A 5320 STRUCTURE HAWKER BAE125 BAE125700B 7450007 EU LT MLG WW CRACKED E ERYA K NONE O OTHER IN INSP/MAINT 1 CE 07 731DL 8385 NA0234 CRACK IN LEFT HAND WHEEL WELL TUB, EXTENDING BEYOND PERVIOUS STOP DRILL REPAIR. 2 L 7 2 4F RT A3EU 2001031200484 20010312 00484 NM 2001 3 12 AWXA0001312 1 20010209 A 5553 6546874503 FITTING BOEING 737 737277 1384570 NM VERTICAL STAB CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 LT AFT VERT STAB I/B (FAILSAFE) LUG GOUGED IN ID AND CORRODED ON FWD FACE. LOCALLY BLENDED GOUGED AREAS OF LUG FWD SPOT FACE AREA IAW ER 15-5510-0123-JS3. 2 L 7 2 4F RT A16WE 2001031200485 20010312 00485 NM 2001 3 12 AWXA0001313 1 20010209 A 5553 6546874504 FITTING BOEING 737 737277 1384570 NM VERTICAL STAB CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 RT AFT VERT STAB I/B (FAILSAFE) LUG CORRODED/GOUGED ON ID AND CORRODED/GOUGED ON FWD FACE. LOCALLY BLENDED GOUGE AREAS IAW ER 15-5510-01023-JS3. 2 L 7 2 4F RT A16WE 2001031200486 20010312 00486 NM 2001 3 12 AWXA0001319 1 20010209 A 5551 65505717 FITTING BOEING 737 737277 1384570 NM HORIZ STAB CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 RT HORIZ STAB REAR SPAR UPPER ATTACH FITTING CORRODED. BLENDED CORROSION IAW ER 15-5510-01027-ES2. 2 L 7 2 4F RT A16WE 2001031200487 20010312 00487 EU 2001 3 12 AWXA0001340 1 20010214 A 2910 HYDRAULIC SYSTEM AIRBUS 320 A320231 3930325 EU FUSELAGE LOW A AWXA O OTHER J WARNING INDICATION DE DESCENT 1 WP 28 627AW 66 SEA - EMERGENCY LANDING - 2/10/01 - ON DESCENT INTO SEA THE GREEN HYDRAULIC SYSTEM WENT TO LOW LEVEL. IN SEA THE AIRCRA FT WAS INSPECTED AND NO LEAKS FOUND. THE GREEN SYSTEM HYDRAULIC SYSTEM WAS SERVICED TO FULL AND NO FURTHER PROBLEMS REP ORTED. THIS WAS THE FIRST FLIGHT AFTER NR 1 ENGINE CHANGE AND PROBABLY HAD AIR TRAPPED IN THE SYSTEM AFTER THE ENGINE C HANGE. 2 L 7 2 4F RT A28NM 2001031200488 20010312 00488 EU 2001 3 12 AWXA0001339 2 20010214 A 7200 ENGINE BOEING 737 7373G7 1384595 NM CFMINT CFM56 CFM563B2 13802 EU NR 1 ENGINE BIRD STRIKE A AWXA A UNSCHED LANDING C F.O.D. TO TAKEOFF 1 WP 28 308AW 24710 860173 AUS - AIR TURNBACK - 2/9/01 - ON TAKEOFF A BIRD WAS INGESTED INTO NR 1 ENGINE; THE AIRCRAFT RETURNED TO AUS MAKING AN UN EVENTFUL LANDING; TECHNICHIANS WERE SENT FROM PHX. THREE FAN BLADES WERE REPLACED; THE 1ST THRU 4TH STAGE OF BOOSTER WE RE BORESCOPE INSPECTED WITH NO EVIDENCE OF INGESTION NOTED. AN OVERWEIGHT LANDING INSPECTION WAS PERFORMED WITH NO DISC REPANCIES NOTED. A VIBRATION SURVEY WAS PERFORMED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2001031200489 20010312 00489 NM 2001 3 12 AWXA0001336 1 20010214 A 3260 666000077 SENSOR AIRBUS A319 A319132 NM NLG WW DEFECTIVE A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 810AW 1116 PHX - AIR TURNBACK - 2/6/01 - AFTER TAKEOFF THE NOSEGEAR FAILED TO FULLY RETRACT, NOSE AND MAIN LANDING GEAR DOORS DID N OT FULLY RETRACT; THE CREW CYCLED THE GEAR DOWN AND MADE AN UNEVENTFUL LANDING IN PHX. MAINTENANCE TROUBLESHOT AND FOUN D NOSE GEAR UPLOCK SENSORS GA12 & GA13 BAD; THE SENSORS WERE REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A28NM 2001031200490 20010312 00490 NM 2001 3 12 AWXA0001334 1 20010214 A 2130 28410 VALVE BOEING 737 7373Y0 1384671 NM EE BAY FAILED A AWXA G B A O2 MASK DEPLOYED EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 334AW 35926 7669 23748 DIVERTED FLIGHT - 2/4/01 - EN ROUTE SJC TO PHX, FL 290 ACFT EXPERIENCED A RAPID DEPRESSURIZATION; ALT ALERT HORN SOUNDED 10000 FT, CLIMBING 2000-3000 FPM; OXYGEN MASKS DEPLOYED, RAPID DESCENT MADE; UNEVENTFUL LANDING AT FAT. TECHS SENT FRO M PHX TO TROUBLESHOOT. DURING PRESS TEST, EQUIP COOLING EXHAUST VALVE FAILED; ALL OTHER CHECKS GOOD. REPLACED EQUIP CO OLING VALVE, FERRIED TO PHX FOR REPLACEMENT OF USED OXYGEN GENERATORS, REPACKING OF OXYGEN MASKS. DURING THE FLIGHT TO PHX THE PRESSURIZATION SYSTEM OPERATED NORMALLY. CABIN PRESSURE REPLACED, PRECAUTION. TWO MASK FAILED TO DROP (FWD F/A & ROW 23 RT). REPLACEMENT OF PASSENGER OXYGEN GENERATOR AND ALL FUNCTIONED NORMALLY. 2 L 7 2 4F RT A16WE 2001031200491 20010312 00491 NM 2001 3 12 AWXA0001341 1 20010216 A 5230 SKIN BOEING BOEING 737 7373G7 1384595 NM FWD CARGO DR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 1583 24009 FWD CARGO DOOR LOWER LIGHTENING HOLE ON INNER SKIN, 2ND HOLE FROM AFS FRAME HAS 0.5 INCH CRACK. CRACK IDENTIFIED DURING C-CHECK INITIAL INSPECTION. REPAIRED IAW SRM 51-70-13. 2 L 7 2 4F RT A16WE 2001031200492 20010312 00492 NM 2001 3 12 AWXA0001342 1 20010216 A 5310 6517684638 SUPPORT FITTING BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 42381 24009 DOOR STOP FITTING SUPPORT IS CRACKED AT STA 294 STR 12L LT FITTING SUPPORT IS CRACKED 0.5 INCH. SUPPORT WEB REPLACED IA W SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001031200493 20010312 00493 NM 2001 3 12 AWXA0001343 1 20010216 A 5312 6516300 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 42381 24009 BS 178 WEB CRACKED AT WL 199 RBL 5.5 (CRACK IDENTIFIED DURING C-12 INITIAL INSPECTION). REPAIRED WEB IAW BSB 737-53A117 3 AND SRM 53-10-08 FIG 209. 2 L 7 2 4F RT A16WE 2001031200494 20010312 00494 NM 2001 3 12 AWXA0001344 1 20010216 A 5311 65163019 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 42381 24009 STA 188 LT SIDE CHORD CRACKED AT WL 207 (IDENTIFIED DURING INITIAL INSPECTION C-12 CHECK). REPLACED LT OUTBOARD CHORD I AW SRM 51-10-02 AND DWG 65-16301. 2 L 7 2 4F RT A16WE 2001031200495 20010312 00495 NM 2001 3 12 AWXA0001345 1 20010216 A 5312 654583391 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 42381 24009 BS 178 BULKHEAD LT INTERCOSTAL AT LT SIDE CHORD WL 207 IS CRACKED (IDENTIFIED DURING INITIAL INSP ON C-12 CHECK). REPAI RED CRACKS IN WEB, CLIP AND INTERCOSTAL AT STA 178 LT IAW BSB 737-53A1173 PARTS I, D, 2, A, 2 & 3, FIG 68, PAGE 73 AND S RM 51-70-12. PARTS REPAIRED: WEB - P/N 65-45833-40, CLIP - P/N 65-45833-467. 2 L 7 2 4F RT A16WE 2001031200496 20010312 00496 NM 2001 3 12 AWXA0001346 1 20010216 A 5311 651630086 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 42381 24009 BS 178 LT SIDE CHORD CRACKED AT WL 207 ABOVE FLOOR (IDENTIFIED DURING INITIAL INSPECTION ON C-12 CHECK). REPLACED IAW S RM 51-10-02 AND DWG 65-16300. 2 L 7 2 4F RT A16WE 2001031200497 20010312 00497 SO 2001 3 12 RAIA00102003 1 20010216 A 3246 31551 WHEEL EMB 145 EMB145LR SO NLG VIBRATES A RAIA D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 CE 03 811HK 145256 BOS-5272- DURING TAXI NOSE WHEEL VIBRATES AND GRINDS. WHILE STEERING, NOSE GEAR MAKES A GRINDING METAL TO METAL NOISE A ND COULD BE FELT THROUGH RUDDER PEDALS AND TILLER. MAINTENANCE REMOVED AND REPLACED BOTH NOSE LANDING GEAR WHEEL/TIRE A SSEMBLIES IAW EMB145 MAINTENANCE MANUAL. 2 L 7 2 4T RT T00011AT 2001031200498 20010312 00498 EU 2001 3 12 RAIA00102004 1 20010216 A 2422 PC125123B INVERTER JETAIR JETSTM JETSTM4101 1500501 EU RT INVERTER FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 556HK 8464 1426 41073 EWR-5402- DURING TAXI OUT RIGHT HAND INVERTER FAILED. MAINTENANCE REMOVED AND REPLACED THE INVERTER IAW J41 MAINTENANCE MANUAL. 2 L 7 2 4T RT A41NM 2001031200499 20010312 00499 NM 2001 3 12 AWXA0001347 1 20010216 A 5312 654583340 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 42381 24009 STA 178 BULKHEAD RT SIDE INTERCOSTAL CRACKED AT WL 207 AS MARKED (VIEW FROM ABOVE FLOOR). REPAIRED CRACK IN INTERCOSTAL , CLIP AND WEB IAW BSB 737-53A, PART 1 WORK PLAN D, 2, A, 2&3, AND FIG 68 (PAGE 73). CLIP - P/N 65-45833-468. 2 L 7 2 4F RT A16WE 2001031200500 20010312 00500 NM 2001 3 12 AWXA0001348 1 20010216 A 5312 6516300 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 BS 178 BLKHD WEB CRACKED AT LBL 5.5 WL 199. REPAIRED WEB IAW BSB 737-53A1173 AND SRM 53-10-08 FIG 209. 2 L 7 2 4F RT A16WE 2001031200501 20010312 00501 NM 2001 3 12 AWXA0001349 1 20010216 A 5311 651630087 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 STA 178 BLKHD RT SIDE CHORD IS CRACKED AT WL 207. REPLACED IAW SRM 51-10-02 AND DWG 65-16300. 2 L 7 2 4F RT A16WE 2001031200502 20010312 00502 NM 2001 3 12 AWXA0001350 1 20010216 A 5312 6516300 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 BS 178 BLKHD WEB CRACKED AT WL 202 RBL 5.5. REPAIRED IAW BSB 737-53A1173 AND SRM 53-10-08 FIG 209. 2 L 7 2 4F RT A16WE 2001031200503 20010312 00503 EU 2001 3 12 JBXA000248 1 20010218 A 3240 BRAKE ASSY FOKKER F28 F28MK0100 4990807 EU LT&RT MLG FAILED A JBXA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 05 110ML 11486 GATE RETURN. BRAKES RELEASED WITH BRAKE APPLICATION SEVERAL TIMES. SET PARKING BRAKE, PUSHED ANTI-SKID TEST, BRAKES RE LEASED WITH AIRCRAFT MOVEMENT. TOWED AIRCRAFT TO GATE. BLEED BRAKE SYSTEM IAW F100 AMM 32-44-00, SERVICED HYDRAULIC SY TEM 1 AND 2 IAW F100 AMM 12-12-01. SERVICED BRAKE ACCUMULATORS IAW F100 AMM 12-14-01 PERFROMED ANTI-SKID OPERATIONAL CH ECK IAW F100 AMM 32-45-00, SYSTEM OPS CK GOOD. 2 L 7 2 4F RT 2001031200504 20010312 00504 NM 2001 3 12 AWXA0001351 1 20010216 A 5312 6516300 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 BS 178 BKLHD WEB CRACKED AT WL 202 LBL 5.5. REPAIRED IAW BSB 737-53A1173 AND SRM 53-10-08 FIG 209. 2 L 7 2 4F RT A16WE 2001031200505 20010312 00505 NM 2001 3 12 AWXA0001352 1 20010216 A 5312 6516300 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 BS 178 BKLHD WEB CRACKED AT WL 201 LBL 6. REPAIRED IAW BSB 737-53A1173 AND SRM 53-10-08 FIG 209. 2 L 7 2 4F RT A16WE 2001031200506 20010312 00506 NM 2001 3 12 AWXA0001353 1 20010216 A 5553 65495598 FITTING BOEING 737 7373G7 1384595 NM VERTICAL STAB CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 RIGHT O/B AFT FUSELAGE LUG OF AFT VERT STAB ATTACHMENT CORRODED INBOARD (AFT FACE). AFT LUG REWORKED IAW ER 03-5384-010 33-BA1. 2 L 7 2 4F RT A16WE 2001031200507 20010312 00507 NM 2001 3 12 AWXA0001354 1 20010216 A 5553 FITTING BOEING 737 7373G7 1384595 NM VERTICAL STAB CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 RIGHT O/B FWD LUG OF AFT VERT STAB ATTACHMENT CORRODED IN BORE. VERT STAB REMOVED AND INSTALLED IAW W/C R6B55001 & F6B2 7001, MAIN CHORD FITTING REWORKED IAW ER 03-5384-01033-BA1 & WIP 0192290. 2 L 7 2 4F RT A16WE 2001031200508 20010312 00508 NM 2001 3 12 AWXA0001355 1 20010216 A 5313 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 FUSELAGE STRINGER 10L CRACKED AT STA 296. REPAIRED IAW SRM 51-70-11 FIG 201. REPAIR, PRIME, PAINTED ON WIP 0192447. 2 L 7 2 4F RT A16WE 2001031200509 20010312 00509 NM 2001 3 12 AWXA0001356 1 20010216 A 5330 143N3320 SKIN BOEING 757 7572G7 1384963 NM FUSELAGE DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 24233 THERE IS A DENT IN THE FUSELAGE AT STA 634 AT STR 16L. CUT OUT DAMAGE; FABBED, TREATED, PRIMED AND INSTALLED REPAIR IAW SRM 53-00-01 FIG 205. 2 L 7 2 4F RT A2NM 2001031200510 20010312 00510 NM 2001 3 12 AWXA0001357 1 20010216 A 5311 65163004301 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 SIDE CHORD CRACKED AT FS 178 WL 207 LBL 26. REMOVED, FABED AND INSTALLED SPLICE PLATE IAW ER 03-5312-01036DC1. 2 L 7 2 4F RT A16WE 2001031200511 20010312 00511 NM 2001 3 12 AWXA0001358 1 20010216 A 5312 65163007 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 ULTRASONIC INSPECTION DETECTED 2 CRACKS BEHIND STRAP AT LBL 5.7 APPROX 3 INCHES ABOVE WL 207 AT FS 178. STOP DRILLED CR ACK IAW SRM 53-10-08 FIG 209; NDT FOUND OUT CRACK TERMINATED; FABED DOUBLER AND 2 FILLERS AND DOUBLER; TREAT AND PRIMED IAW SRM 53-10-08 FIG 209 AND 51-20-01; INSTALLED DOUBLER AND 2 FILLERS IAW SRM 51-40-02 AND 53-10-08. 2 L 7 2 4F RT A16WE 2001031200512 20010312 00512 NM 2001 3 12 AWXA0001359 1 20010216 A 5312 65163007 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 ULTRASONIC INSPEC DETECTED 2 CRACKS AT LBL 5.7 BEHIND STIFFENER BETWEEN WL 195 & WL 207 STA 178. CUT OUT DAMAGED AREA, FABED FILLERS & DOUBLER, INSTALLED FILLERS AND DOUBLER IAW SRM 53-10-08 & 51-40-02. 2 L 7 2 4F RT A16WE 2001031200513 20010312 00513 NM 2001 3 12 AWXA0001360 1 20010216 A 5312 65163007 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 CENTER WEB CRACKED FS 178 LBL 5.0 WL 198 & 202. CUT OUT DAMAGED AREA, FABED FILLERS AND DOUBLER; INSTALLED FILLERS AND DOUBLER IAW SRM 53-10-08, 51-40-02. 2 L 7 2 4F RT A16WE 2001031200514 20010312 00514 EA 2001 3 12 COMA0160243 1 20010213 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA RT FLAP MALFUNCTIONED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 729CA 15771 7265 FLAPS FAILED. REPLACED THE RT BPSU. 2 L 7 2 4F RT A21EA 2001031200515 20010312 00515 NM 2001 3 12 AWXA0001361 1 20010216 A 5312 65163007 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 ULTRASONIC INSP DETECTED ONE CRACK AT RBL 5.7 BEHIND STIFFENER AT WL 195-207 FS 178. CUT OUT DAMAGED AREA, FABED FILLER S AND DOUBLER; INSTALLED FILLERS AND DOUBLER IAW SRM 53-10-08 AND 51-40-02. 2 L 7 2 4F RT A16WE 2001031200516 20010312 00516 EA 2001 3 12 COMA0160244 1 20010214 A 2750 865D1007 POWER UNIT CNDAIR CL600 CL6002B19 EA WING MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 936CA 3784 1152 7043 FLAPS FAILED. REPLACED THE FLAP POWER DRIVE. 2 L 7 2 4F RT A21EA 2001031200517 20010312 00517 EA 2001 3 12 COMA0160245 1 20010215 A 2742 83963 ACTUATOR CNDAIR CL600 CL6002B19 EA HORIZONTAL STAB MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 918CA 15053 7018 STAB TRIM, MACH TRIM DISENGAGED. REPLACED THE HSTA. 2 L 7 2 4F RT A21EA 2001031200518 20010312 00518 NM 2001 3 12 AWXA0001362 1 20010216 A 5320 654583340 WEB BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 FLOOR WEB CRACKED FS 180 WL 207 RBL 26. REMOVED DAMAGED FLOOR WEB IAW SRM 51-40-02; FABED REPLACEMENT WEB IAW DWG 65-45 833; INSTALLED REPLACEMENT WEB IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001031200519 20010312 00519 NM 2001 3 12 AWXA0001363 1 20010216 A 5320 693727111 TIE CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 FUSELAGE BS 294.5 AND STR 25L INTERCOSTAL AND CLIP IS CRACKED. REMOVE STRINGER AND CRACKED CLIP IAW SRM 51-40-02; FABED REPLACEMENT CLIP IAW 51-30-01; INSTALLED CLIP IAW B737 SRM 51-40-02 AND STRINGER; DAMAGED CONTAINED BY THE REMOVAL OF T HE CLIP, ALODINE AND PRIMER CLIP IAW B737 M/M 51-21-00. 2 L 7 2 4F RT A16WE 2001031200520 20010312 00520 NM 2001 3 12 AWXA0001364 1 20010216 A 5312 65163007 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 CENTER WEB CRACKED AT FS 178 RBL 5.0 WL 198, WL 202. CUT OUT 2 CRACKS IAW SRM 53-10-08, NDT NO CRACKS; FABED AND INSTAL LED REPAIR PARTS IAW SRM 53-10-08, TOP COAT APPLIED. 2 L 7 2 4F RT A16WE 2001031200521 20010312 00521 EA 2001 3 12 COMA0160246 1 20010215 A 3010 14466103 COUPLING CNDAIR CL600 CL6002B19 EA RT MLG WW LEAKING A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 917CA 7017 WING ANTI ICE DUCT WARNING. REPLACED BLEED AIR COUPLING IN RT WHEEL WELL. 2 L 7 2 4F RT A21EA 2001031200522 20010312 00522 NM 2001 3 12 AWXA0001365 1 20010216 A 5312 65163007 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 CENTER WEB CRACKED FROM STA 178 LBL 5.0 WL 198 AND 202. CUT OUT 2 CRACKS IAW SRM 53-10-08, NDT NO CRACKS NOTED; FABED A ND INSTALLED 1 DOUBLER AND 3 FILLERS IAW SRM 53-10-08. 2 L 7 2 4F RT A16WE 2001031200523 20010312 00523 EA 2001 3 12 COMA0160247 1 20010215 A 3010 32144424 VALVE CNDAIR CL600 CL6002B19 EA ANTI-ICE SYS MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 811CA 2356 7380 RT WING ANTI ICE CAUTION MESSAGE. REPLACED THE LT MODULATING VALVE. 2 L 7 2 4F RT A21EA 2001031200524 20010312 00524 NM 2001 3 12 AWXA0001366 1 20010216 A 5320 69353501 TIE CLIP BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 AFT CARGO COMP STA 773 LONG 26R HAS CRACKED TIE CLIP. REMOVED AND REPLACED TIE CLIP IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001031200525 20010312 00525 NM 2001 3 12 AWXA0001367 1 20010216 A 5230 WEB BOEING 737 7373S3 1384711 NM AFT CARGO DR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 AFT CARGO DOOR WEB CUTOUT FOR THE ROD END IS CRACKED. STOP DRILLED CRACK IAW B737-300 SRM 51-70-13; HFEC INSP IAW IAW B 737 NTM PT.6 51-00-00 FIG 23. CRACK TERMINATED AT STOP DRILL; FABED AND INSTALLED REPAIR DOUBLER ON AFT CARGO DOOR INNE R WEB CUTOUT FOR LATCH ROD END IAW B737-300 SRM 51-70-13 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001031200526 20010312 00526 EA 2001 3 12 COMA0160248 1 20010215 A 3250 16900107 ECU CNDAIR CL600 CL6002B19 EA STEERING SYS MALFUNCTIONED A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 408CA 822 7440 FULL LEFT RUDDER REQUIRED DURING T/O ROLL. REPLACED THE STEERING ELECTRONIC CONTROL UNIT. 2 L 7 2 4F RT A21EA 2001031200527 20010312 00527 NM 2001 3 12 AWXA0001368 1 20010216 A 5320 WEB BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 FLOOR WEB CRACKED AT FS 180 RBL 26 WL 207. REMOVED DAMAGED WEB IAW SRM 51-40-02; FABED NEW WEB IAW DWG 65-45833; INSTAL LED NEW WEB IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001031200528 20010312 00528 NM 2001 3 12 AWXA0001369 1 20010216 A 5320 WEB BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 FLOOR WEB CRACKED FS 180 LBL 26 WL 207. REMOVED DAMAGED WEB IAW SRM 51-40-02; FABED NEW WEB IAW DWG 65-45833; INSTALLED NEW WEB IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001031200529 20010312 00529 NM 2001 3 12 AWXA0001370 1 20010216 A 5312 65163007 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 CENTER WEB CRACKED FS 178 WL 202 RBL 6.0. STOP DRILLED CRACK IAW SRM 53-10-08 FIG 209; NDT IAW NTMP 51-00-00 CRACK TERM INATED. 2 L 7 2 4F RT A16WE 2001031200530 20010312 00530 NM 2001 3 12 AWXA0001371 1 20010216 A 5312 65163007 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 CENTER WEB CRACKED FS 178 WL 202 LBL 6.0. STOP DRILLED CRACK IAW SRM 53-10-08 FIG 209; NDT IAW NTM PT 6 51-00-00; STOP DRILL TERMINATED CRACK. 2 L 7 2 4F RT A16WE 2001031200531 20010312 00531 WP 2001 3 12 MWEA010159 1 20010219 A 5330 5911422503 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 FUSELAGE SKIN DENTED STATION 980, 2 INCHES BELOW LONGERON 2 RIGHT. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001031200532 20010312 00532 WP 2001 3 12 MWEA010160 1 20010219 A 5620 912285515 RING DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LEFT WINDOW RING CRACKED, STATION 639 - 658. REMOVED AND REPLACED WINDOW RING. 2 L 7 2 4F A6WE 2001031200533 20010312 00533 WP 2001 3 12 MWEA010162 1 20010219 A 5730 59127373 PANEL DOUG DC9 DC932 3022066 WP LT WING DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LEFT WING UPPER TRAILING EDGE PANEL IS DENTED, STATION 419, 4 INCHES AFT OF REAR SPAR. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER. 2 L 7 2 4F A6WE 2001031200534 20010312 00534 WP 2001 3 12 MWEA010163 1 20010214 A 7603 5910327 THROTTLE CABLE DOUG DC9 DC932 3022066 WP LT ENGINE STUCK A MWEA K NONE O OTHER DE DESCENT 1 GL 31 401ME 47133 STARTED DESCENT FROM FLIGHT LEVEL 350 AND LEFT THROTTLE STUCK AT 80 PERCENT N2. THROTTLE FREED UP PRIOR TO LANDING. MA INTENANCE DISASSEMBLED LEFT THROTTLE CABLE, CLEANED AND LUBRICATED INNER ELEMENT. ALSO FOUND CABLE CLAMPED IN A WAY CAU SING MISALIGNMENT. REPOSITIONED CLAMPS. 2 L 7 2 4F A6WE 2001031200535 20010312 00535 NM 2001 3 12 UPS01235015 1 20010217 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:N/A, EMERGENCY LIGHT NEED BATTERY PACK ROW 2 L AISLE LIGHT. INSTALLED NEW BATTERY ROW L AISLE. 2 L 7 3 4F A3WE 2001031200536 20010312 00536 NM 2001 3 12 UPS01235016 1 20010217 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:N/A, EMERGENCY LIGHT IN LT GALLEY NEEDS BATTERY. INSTALLED NEW BATTERY PACK FOR LT GALLEY, OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2001031200537 20010312 00537 NM 2001 3 12 UPS01435009 1 20010215 A 5330 SKIN BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, CORROSION AND PULLED RIVETS AT BS 1000 STR 41R. REPAIRS ACCOMPLISHED TO SKIN AND CHORD IAW Q/NOTE 4/ 01 AND SRM 53-30 -03. REFERENCE ALSO NRCS 44374471, 44370677 AND 44374732. 2 L 7 4 4F A20WE 2001031200538 20010312 00538 NM 2001 3 12 UPS01435011 1 20010217 A 2612 CONNECTOR BOEING 747 747123 1384873 NM NR1 ENGINE FAULTY A IPXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 674UP 20100 INSPECTION TYPE:N/A BTB- REJECTED T/O, NR 1 ENGINE FIRE WARNING. T/S FOUND UPPER AFT LOOP CONNECTORS BAD DEFERRED OK FO R SERVICE REF WIRING DIA 26-11-51. 2 L 7 4 4F A20WE 2001031200539 20010312 00539 NM 2001 3 12 UPS01435014 1 20010216 A 2131 CONTROLLER BOEING 747 747283B 1384867 NM PRESSURE SYS INOPERATIVE A IPXA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 523UP 22381 INSPECTION TYPE:N/A, ON CLIMBOUT LOST PRESSURIZATION AND WAS UNABLE TO CONTROL PRESSURIZATION. IN AUTO PRESS WAS UNCONT ROLABLE AT 8.4PSI WENT TO MANUAL AND COULD NOT GAIN CONTROL OF PRESS. PRESS LIGHT CAME ON. DUMPED FUEL AND RTB. INSPE CTED FUSELAGE EXTERIOR, NO DEFECT NOTED. SUSPECT AUTO CABIN PRESS CONTROLLER WAS INOP, MANUAL CONTROL IS NORMAL. ITEM TRANSFERRED TO MEL 21-22-1. SECURED PRESS RELIEF VALVE PER MM 21-32-01. OK FOR SERVICE. 2 L 7 4 4F A20WE 2001031200540 20010312 00540 WP 2001 3 12 UPS01835017 1 20010216 A 3350 BATTERY DOUG DC8 DC873F 302199F WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT PER M33-50-0 1. 2 L 7 4 4F RT 4A25 2001031200541 20010312 00541 NM 2001 3 12 F3LA200100018 1 20010218 A 5320 FLOOR SUPPORT BOEING 737 7373S1 138447S NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 24856 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT FUSELAGE FLOOR SUPPORT, 14 INCHES LT OF CENTER LINE 0, BETWEEN ST A 967 AND 986.5. MAINTENANCE INSTALLED INTERCOSTAL PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001031200542 20010312 00542 NE 2001 3 12 COMA0110034 3 20010219 A 6111 8175972 SPRING EMB 120 EMB120RT SO HAMSTD 14RF 14RF9 NE LT PROP BROKEN A COMA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 269CA 32 120263 910519 ON POST-FLIGHT INSPECTION CREW NOTICED OIL LEAKING FROM LEFT PROPELLER. MAINTENANCE DETERMINED SOURCE TO BE THE NR 1 PR OP BLADE. THE BLADE WAS REMOVED, AND THE BLADE SEAL COIL SPRING WAS FOUND TO BE BROKEN. THE BLADE SEAL ASSEMBLY WAS RE PLACED, THE BLADE REINSTALLED, AND THE PROPELLER RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 6 C P11NE 2001031200543 20010312 00543 EA 2001 3 12 COMA0160250 1 20010216 A 3000 20035008067 CONTROLLER CNDAIR CL600 CL6002B19 EA ANTI-ICE SYS MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 986CA 9226 7174 ANTI ICE DUCT WARNING. REPLACED THE BLEED LEAK CONTROL UNIT. 2 L 7 2 4F RT A21EA 2001031200544 20010312 00544 EA 2001 3 12 COMA0160252 1 20010215 A 3250 16900107 ECU CNDAIR CL600 CL6002B19 EA NLG FAILED A COMA K NONE O OTHER NR NOT REPORTED 1 SO 01 957CA 12709 7109 NWS IS INOPERABLE. REPLACED THE STEERING ECU. 2 L 7 2 4F RT A21EA 2001031200545 20010312 00545 EA 2001 3 12 COMA0160253 1 20010215 A 2760 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT ACTIVATED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 779CA 7306 CONFIG SPOILERS WARNING DURING T/O. COULD NOT DUPLICATE. RESET SPOILER SYSTEM. NO FAULTS LOGGED IN COMPUTER. 2 L 7 2 4F RT A21EA 2001031200546 20010312 00546 NM 2001 3 12 CALA0100124 1 20010217 A 5320 BRACKET BOEING 737 7373T0 1384582 NM FWD CARGO BAY CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND A 2 INCH CRACK IN FWD CARGO COMPARTMENT BRACKET FOR VHF NR 2 ON AFT SIDE OF FRAME AT STA 500 BETWEEN ST RINGERS 28L AND 28R. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A16WE 2001031200547 20010312 00547 NM 2001 3 12 CALA0100125 1 20010217 A 5330 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND EXTERNAL FUSELAGE SKIN CREASED WITH A GOUGE AT STA 285 JUST BELOW STRINGER 4L. A REPAIR DOUBLER WAS IN STALLED IAW SRM 53-00-01, FIGURE 202, 51-20-01, AND 51-40-00. 2 L 7 2 4F RT A16WE 2001031200548 20010312 00548 NM 2001 3 12 CALA0100126 1 20010217 A 5330 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND TWO DENTS IN FUSELAGE EXTERNAL SKIN AT STA 727A, STRINGER 8L. THE DENTED AREA WAS REPAIRED IAW SRM 53- 00-01, FIGURE 213. 2 L 7 2 4F RT A16WE 2001031200549 20010312 00549 NM 2001 3 12 CALA0100127 1 20010217 A 5320 WEB BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND LT AND RT FLOOR WEBS CORRODED AROUND FASTENERS AT STA 1006-1016, BL 0 TO LEFT SIDE AND BL 0 TO RIGHT SI DE. THE CORRODED SECTIONS OF WEB WERE ROUTED OUT AND REPAIR DOUBLERS WERE INSTALLED IAW SRM 51-70-13, FIGURE 1. 2 L 7 2 4F RT A16WE 2001031200550 20010312 00550 NM 2001 3 12 CALA0100128 1 20010217 A 5320 CREASE BEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND CORROSION ON CREASE BEAM AT R-1 DOOR, STA 315, RBL 50.5. THE CREASE BEAM WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001031200551 20010312 00551 NM 2001 3 12 CALA0100129 1 20010218 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND FLOORBEAM CAP UPPER AND LOWER FLANGE CORRODED AT STA 312, RBL 12. THE UPPER CAP WAS REMOVED AND A REPA IR WAS INSTALLED IAW SRM 53-10-51, FIGURE 205. 2 L 7 2 4F RT A16WE 2001031200552 20010312 00552 NM 2001 3 12 CALA0100130 1 20010217 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 328, RBL 26.75. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INST ALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001031200553 20010312 00553 NM 2001 3 12 CALA0100131 1 20010217 A 5330 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND FUSELAGE SKIN DENTED AND CREASED AT STA 350, STRINGER 22R. A REPAIR WAS INSTALLED IAW SRM 51-20-01 AND 53-00-01, FIGURE 202, SHEET 3. 2 L 7 2 4F RT A16WE 2001031200554 20010312 00554 NM 2001 3 12 CALA0100132 1 20010217 A 5320 STRAP BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND FLOORBOARD SUPPORT STRAP CORRODED AT STA 1006-1016, RBL 2. THE STRAP WAS REMOVED AND A NEW STRAP WAS I NSTALLED IAW SRM 51-10-2 AND DRAWING 65C32677. 2 L 7 2 4F RT A16WE 2001031200555 20010312 00555 WP 2001 3 12 CALA0100133 1 20010217 A 5320 WEB DOUG DC9 DC982 3022082 WP FWD CARGO BAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10801 49127 INSPECTION FOUND FORWARD CARGO DOOR JAMB OPENING AFT TORQUE BOX WEB CORRODED AT FS 430. THE CORRODED AREA WAS CUT OUT, A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW EA 9-5310-2-A0851. 2 L 7 2 4F A6WE 2001031200556 20010312 00556 NM 2001 3 12 CALA0100134 1 20010217 A 5320 FLOOR SUPPORT BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73385 26314 INSPECTION FOUND FLOOR SUPPORTS CRACKED AT STA 540, LBL 1 AND RBL 1. THE CRACKS WERE 1 INCH LONG. THE FLOOR SUPPORTS W ERE REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001031200557 20010312 00557 NM 2001 3 12 CALA0100135 1 20010218 A 5330 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND FOUR DENTS WITHIN A FOUR INCH AREA IN FUSELAGE EXTERNAL SKIN AT STA 460, STRINGER 7R. REPAIRED SKIN IA W SRM 53-00-01, FIGURE 201. 2 L 7 2 4F RT A16WE 2001031200558 20010312 00558 NM 2001 3 12 CALA0100136 1 20010218 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 947-967, LBL 12. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT W AS INSTALLED IAW SRM 51-40-2. 2 L 7 2 4F RT A16WE 2001031200559 20010312 00559 NM 2001 3 12 CALA0100137 1 20010218 A 5320 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND L-1 DOOR LOWER SILL OUTER ANGLE CORRODED AT STA 315-340. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INS TALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001031200560 20010312 00560 NM 2001 3 12 CALA0100138 1 20010218 A 5330 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND A 0.3 INCH CRACK IN FUSELAGE SKIN AT R-2 DOOR LOWER HINGE CUTOUT, STA 951, S15R-16R. THE SKIN WAS REPA IRED IAW SRM 53-60-01, FIGURE 7, SHEET 207. 2 L 7 2 4F RT A16WE 2001031200561 20010312 00561 EA 2001 3 12 COMA0160254 1 20010217 A 3350 363782 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 779CA 7306 FLOOR EMERGENCY LIGHTS ARE INOP ROW 2 TO 5. REPLACED THE FLEXIBLE LAMP ASSY. 2 L 7 2 4F RT A21EA 2001031200562 20010312 00562 EU 2001 3 12 QXEA0100121 1 20010216 A 3350 5515800106 LIGHT FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 482US 11231 BOI- CENTER AND AFT AISLE EXIT PLACARDS HAVE BULBS INOPERATIVE. REPLACED BOTH LIGHT ASSEMBLIES. OPERATIONAL CHECKS GOO D. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001031200563 20010312 00563 NM 2001 3 12 QXEA0100119 1 20010216 A 5210 DOOR DHAV DHC8 DHC8202 2809007 NM PAX DOOR LACK OF LUBE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 SEA- MAIN CABIN DOOR VERY STIFF TO OPEN. CLEANED AND LUBED DOOR LINKAGE AND STOPS. NO PARTS REPLACED. OPERATIONAL CHE CKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001031200564 20010312 00564 NM 2001 3 12 QXEA0100120 1 20010215 A 5210 SCREW DHAV DHC8 DHC8201 2809001 NM HANDRAIL LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 828PH 287 SEA- PASSENGER DOOR DIFFICULT TO OPEN. SCREW ON HANDRAIL COMING LOOSE. RESECURED BOLT ON DOOR SUPPORT. NO PARTS REPLA CED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001031200565 20010312 00565 NM 2001 3 12 F3LA200100019 1 20010217 A 5320 FLOOR SUPPORT BOEING 737 7373S1 138447S NM AFT FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 3095 24856 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT FUSELAGE FLOOR SUPPORT, 2 INCHES FROM LT CENTER LINE 0, BETWEEN S TA 986.5 AND 967. MAINTENANCE INSTALLED WEB BETWEEN STA 986.5 AND 967 PER SRM 51-10-2 AND REPLACED FLOORBEAM CAP AT STA 967 PER SRM 53-00-51. 2 L 7 2 4F RT A16WE 2001031200566 20010312 00566 NM 2001 3 12 QXEA0100106 1 20010206 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 814PH 43 PDX- FRETTING CORROSION ON INBOARD FLANGE OF LEFT INBOARD SEAT TRACK AT STATION X252.700 IN LINE WITH AFT EDGE OF MAIN C ABIN DOOR. REPAIRED IAW PSM 1-GEN-5 CHAPTER 4 PAGE 4-16. 2 H 7 2 4T RT A13NM 2001031200567 20010312 00567 NM 2001 3 12 QXEA0100107 1 20010128 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 814PH 43 PDX- CORROSION ON LEFT INBOARD SEAT TRACK FLANGE LOCATED IN CARGO AREA AT STATION 580.50. REPAIRED IAW DHC-8 SRM 51-20- 16. 2 H 7 2 4T RT A13NM 2001031200568 20010312 00568 NM 2001 3 12 QXEA0100108 1 20010205 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 814PH 43 PDX- FRETTING CORROSION ON INBOARD FLANGE OF LEFT HAND INBOARD SEAT TRACK AT STATION X252.700 IN LINE WITH AFT EDGE OF M AIN CABIN DOOR. REPAIRED IAW DHC-8 SRM 51-40-00 AND RD 8-53-1102. 2 H 7 2 4T RT A13NM 2001031200569 20010312 00569 NM 2001 3 12 QXEA0100109 1 20010205 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 814PH 43 PDX- DENT IN AFT FUSELAGE SKIN 6 INCHES LONG, .020 INCH DEEP AFT OF FRAME X600.0 BETWEEN STRINGERS 22R AND 23R. REPAIRE D IAW DHC-8 RD 8-53-436. 2 H 7 2 4T RT A13NM 2001031200570 20010312 00570 NM 2001 3 12 QXEA0100110 1 20010131 A 5320 SPLICE DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 814PH 43 PDX- FRAME JOINT SPLICE ANGLE AT STATION X136.80 AT STRINGER 15A RIGHT HAND IS CRACKED. REPAIRED IAW DHC-8 RD 8-53-576. 2 H 7 2 4T RT A13NM 2001031200571 20010312 00571 NM 2001 3 12 QXEA0100111 1 20010130 A 5320 SPLICE DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 814PH 43 PDX- CRACK FOUND IN LEFT HAND JOINT SPLICE FRAME AT STATION X136.80 AND STRINGER 15A. REPAIRED IAW DHC-8 RD 8-53-576. 2 H 7 2 4T RT A13NM 2001031200572 20010312 00572 NM 2001 3 12 QXEA0100112 1 20010130 A 5542 SKIN DHAV DHC8 DHC8102 2809003 NM RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 814PH 43 PDX- TOP RIGHT HAND SIDE OF TRAILING RUDDER SKIN HAS A CRACK PROGRESSING OUT FROM RIVET HOLE AT PREVIOUS REPAIR SKIN PAT CH. REPAIRED IAW DHC-8 SRM 55-40-28 AND 51-40-00. 2 H 7 2 4T RT A13NM 2001031200573 20010312 00573 NM 2001 3 12 QXEA0100114 1 20010201 A 3233 ATTACH FITTING DHAV DHC8 DHC8102 2809003 NM LT MLG CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 814PH 43 PDX- LEFT HAND MAIN LANDING GEAR RETRACTION ACTUATOR ATTACH FITTING ATTACH POINT ON H-MEMBER HAS FRETTING CORROSION AT L EFT HAND SIDE OF UPPER MOUNT HOLES. REPAIRED IAW HORIZON AIR EA 9-54-267. 2 H 7 2 4T RT A13NM 2001031200574 20010312 00574 NM 2001 3 12 QXEA0100115 1 20010131 A 5400 STIFFENER DHAV DHC8 DHC8102 2809003 NM NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 814PH 43 PDX- FINGERNAIL DECK STIFFENER CHAFED THIN AT XN232.0 TOP SIDE. REPAIRED IAW DHC-8 SRM 51-40-11 AND 51-20-16. 2 H 7 2 4T RT A13NM 2001031200575 20010312 00575 NM 2001 3 12 QXEA0100116 1 20010131 A 5400 STIFFENER DHAV DHC8 DHC8102 2809003 NM NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 814PH 43 PDX- LOWER FINGERNAIL DECK OUTBOARD FORE/AFT STIFFENER IS CRACKED AT GEARWELL WALL VERTICAL STIFFENER OF LEFT HAND NACEL LE. REPAIRED IAW DHC-8 SRM 51-40-11 AND 51-20-16. 2 H 7 2 4T RT A13NM 2001031200576 20010312 00576 NM 2001 3 12 QXEA0100117 1 20010129 A 5310 DOOR FRAME DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 814PH 43 PDX- MAIN CABIN DOOR SURROUND FORWARD FRAME CORRODED AROUND NUTPLATE THAT IS BETWEEN 2ND AND 3RD STOPS FROM BOTTOM. REP AIRED IAW DHC-8 SRM 51-20-11 AND 53-00-16. 2 H 7 2 4T RT A13NM 2001031200577 20010312 00577 NM 2001 3 12 F3LA200100020 1 20010218 A 5320 FLOOR SUPPORT BOEING 737 7373S1 138447S NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 3095 24856 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT FUSELAGE FLOOR SUPPORT, 14 INCHES RBL, BETWEEN STA 967 AND 986.5. MAINTENANCE FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT PER SRM 51-10-02, 51-40-02 AND EA 53-737-113. 2 L 7 2 4F RT A16WE 2001031200578 20010312 00578 SO 2001 3 12 SWIA972364 1 20010209 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CABIN INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 292UX 120292 ONE EMERGENCY LIGHT INOP AT ROW 7 FLOOR. REPLACED ONE EMERGENCY AISLE MONITOR UNIT AT ROW 7 FLOOR (P/N 10-1307-3). GRO UND CHECK NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 2001031200579 20010312 00579 SO 2001 3 12 SWIA972365 1 20010215 A 2751 INDICATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT MALFUNCTIONED A SWIA O OTHER N FALSE WARNING DE DESCENT 1 NM 07 217SW 120286 WHEN SELECTING FLAPS 45 DEGREES, GET DISAGREEMENT. OUTBOARD INDICATING LIGHTS FLASHING. CLEANED FLAP TRACKS AND OPERAT ED FLAPS. COULD NOT DUPLICATE. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001031200580 20010312 00580 SO 2001 3 12 SWIA972366 1 20010212 A 3230 CONTROL BOX EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LANDING GEAR MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 229SW 120305 UPON RETRACTION AFTER TAKEOFF ALL OF THE LANDING GEAR RED AND GREEN LIGHTS ILLUMINATE WITHOUT COMPLETING GEAR RETRACTION . WHEN RECYCLED, LANDING GEAR ONLY RETRACTS AFTER ABOUT A 5 SECOND DELAY AND EXTENDS NORMALLY. PERFORMED MULTIPLE GEAR SWINGS, COULD NOT DUPLICATE. REPLACED LANDING GEAR CONTROL BOX FOR TROUBLESHOOTING. OPS CHECK GOOD. P/N 120-38594-50 1, S/N ON: 120060, OFF: 148922-305. 2 L 7 2 4T 4 T RT A31SO E20NE 2001031200581 20010312 00581 2001 3 12 SWIA972367 4 20010217 A 2210 TRACK EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE ELEV TRIM DIRTY A SWIA O OTHER C F.O.D. CR CRUISE 1 NM 07 268UE 120207 WHEN AUTOPILOT ON, GRINDING NOISE FROM UNDER COCKPIT FLOOR. DEFERRED ELEVATOR TRIM SYSTEM. CLEANED DEBRIS FROM TRIM WH EEL STOP TRACKS AND INSPECTED SERVOS BENEATH FLOORBOARDS. NO DEFECTS NOTED. TRIM SYSTEM OPERATIONAL CHECKS GOOD IAW MM 22-10-00. 2 L 7 2 4T 4 T RT A31SO E20NE 2001031200582 20010312 00582 SO 2001 3 12 SWIA972368 1 20010217 A 2722 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RUDDER FAILED A SWIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 07 229SW 120305 DURING DESCENT, RUDDER REQUIRED FULL NOSE LEFT RUDDER TRIM TRAVEL TO STOP. RUDDER TRIM INEFFECTIVE. PERFORMED RUDDER A CT HEALTH CHECK, AND PCU CHECK IAW EMB 120 MM 27-22-00. FOUND GREEN RUDDER ACTUATOR TO FAIL. REMOVED AND REPLACED GREE N RUDDER ACTUATOR WITH A SERVICEABLE PART. CHECKED OPERATION OF RUDDER AND RUDDER TRIM SATISFACTORY REF EMB MM 27-22-02 . P/N ON: 308140-1003, S/N ON: 00026, S/N OFF 0650. PERFORMED OPS CHECK ON RUDDER AND RUDDER TRIM. WITH AUTOPILOT Y AW ENGAGED SEEMS TO OPERATE A LITTLE SLOW USING RUDDER TRIM WHEEL. ALL OTHER FUNCTIONS OPERATE NORMAL. REPLACED RUDDER SERVO IAW MM 22-10-00, OPS CHECK GOOD. P/N ON: 622-5734-002, S/N ON: 1604, S/N OFF: 7835. 2 L 7 2 4T 4 T RT A31SO E20NE 2001031200583 20010312 00583 NM 2001 3 12 SWAA010319 1 20010131 A 3350 100031 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 610WN 27696 DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2001031200584 20010312 00584 NM 2001 3 12 SWAA010320 1 20010131 A 5330 65C35786 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED RON CHECK, FOUND 2 EXTERNAL FUSELAGE SKIN CRACKS AT BS 500C, BETWEEN STR 9R & STR 10R, BS 525, BETWEEN STR 9R & STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001031200585 20010312 00585 2001 3 12 SWAA010321 4 20010131 A 2565 6567380 MOUNT BOEING 737 7372H4 138448C NM SERVICE DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE CONTAINER FWD MOUNT LOOSE. SECURED EVAC SLIDE MOUNT PER MM. 2 L 7 2 4F A16WE 2001031200586 20010312 00586 2001 3 12 SWAA010322 4 20010131 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASS Y PER MM. 2 L 7 2 4F A16WE 2001031200587 20010312 00587 NM 2001 3 12 SWAA010323 1 20010131 A 2752 113A3920 CONTROL ROD BOEING 737 7373A4 1384585 NM RT WING BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 NR 8 OUTBOARD T/E FLAP FAIRING CONTROL ROD BROKEN. REMOVED AND REPLACED ROD ASSY PER MM. 2 L 7 2 4F RT A16WE 2001031200588 20010312 00588 NM 2001 3 12 SWAA010324 1 20010201 A 5312 6517582 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/2D CHECK, FOUND 2 BS 178 BULKHEAD VERTICAL BEAM WEB CRACKS AT RBL 17, WL 230. REPAIRED VERTICAL BEAM WEB PER ER. 2 L 7 2 4F A16WE 2001031200589 20010312 00589 NM 2001 3 12 SWAA010325 1 20010201 A 5310 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 374SW 26582 DURING SCHEDULED 1/4D CHECK, FOUND BS 747 SHEAR TIE CORRODED AT STR 27R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2001031200590 20010312 00590 NM 2001 3 12 SWAA010326 1 20010201 A 5753 6573732 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 630WN 27705 DURING SCHEDULED SERVICE CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT RT INBOARD LOWER CORNER. REPAIRED AF T FLAP PER SRM. 2 L 7 2 4F RT A16WE 2001031200591 20010312 00591 NM 2001 3 12 SWAA010327 1 20010201 A 5312 6516300 BULKHEAD BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED 1/2D CHECK, FOUND 3 BS 178 BULKHEAD WEB CRACKS AT WL 234, LBL 12, LBL 10 & RBL 10. REPAIRED BULKHEAD W EB PER SRM. 2 L 7 2 4F RT A16WE 2001031200592 20010312 00592 NM 2001 3 12 SWAA010307 1 20010130 A 2131 8907119 CONTROLLER BOEING 737 7373H4 1384600 NM COCKPIT FAILED A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 347SW 24374 AIR TURNBACK, UNABLE TO CONTROL CABIN PRESSURE. REMOVED AND REPLACED CABIN PRESS CONTROLLER. PERFOMED TEST AND LEAK TE ST, OPS CHECK GOOD PER MM. 2 L 7 2 4F RT A16WE 2001031200593 20010312 00593 NM 2001 3 12 SWAA010308 1 20010131 A 3397 5417N509 WIRE BOEING 737 7373H4 1384600 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 380SW 26587 EEPLS WIRING EXPOSED. RESECURED EEPLS WIRING PER MM. 2 L 7 2 4F RT A16WE 2001031200594 20010312 00594 NM 2001 3 12 SWAA010309 1 20010131 A 3350 90083 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 389SW 26592 DURING PREFLIGHT, SELECTED EMERGENCY EXIT LIGHT SWITCH TO ARM AND THE NOT-ARMED LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED FWD EMERGENCY LIGHT BATTERY PACK. 2 L 7 2 4F RT A16WE 2001031200595 20010312 00595 2001 3 12 SWAA010310 4 20010130 A 2565 D31354 SLIDE BOEING 737 7373G7 1384595 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF HOLDER. REINSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001031200596 20010312 00596 NM 2001 3 12 SWAA010311 1 20010131 A 3350 BR2013 LIGHT BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED C1 CHECK, FOUND EEPLS LOOSE & END CAP MISSING AT AFT END. SECURED EEPLS AND REPLACED END CAP PER MM. 2 L 7 2 4F A16WE 2001031200597 20010312 00597 NM 2001 3 12 SWAA010312 1 20010131 A 5312 6517583 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT LBL 5.7, WL 205. REPAIRED VERTICAL BEAM WEB PER ER. 2 L 7 2 4F A16WE 2001031200598 20010312 00598 NM 2001 3 12 SWAA010313 1 20010130 A 5754 65C26601 SLAT BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED C1 CHECK, FOUND 2 INCH CRACKAT NR 6 L/E SLAT EXTENDING FROM AFT ROW OF RIVETS, NEAR CENTER AUX TRACK, O TBD OF PREVIOUS REPAIR. REMOVED AND REPLACED SLAT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001031200599 20010312 00599 NM 2001 3 12 SWAA010314 1 20010130 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED C1 CHECK, FOUND 2 INCH CRACK ON KEEL BEAM, LOWER RT CHORD, BS 681. REPAIRED KEEL BEAM PER SRM. 2 L 7 2 4F RT A16WE 2001031200600 20010312 00600 NM 2001 3 12 SWAA010315 1 20010130 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 374SW 26582 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CRACKED AT BS 787, RBL 13. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2001031200601 20010312 00601 NM 2001 3 12 SWAA010316 1 20010131 A 5330 65C35775 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED C4 CHECK, FOUND 2 EXTERNAL FUSELAGE SKIN CRACK AT BS 727D, BETWEEN STR 19R & STR 20R. REPAIRED SKIN PE R SRM. 2 L 7 2 4F RT A16WE 2001031200602 20010312 00602 NM 2001 3 12 SWAA010317 1 20010131 A 5330 65C35786 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING WALK-AROUND INSPECTION, FOUND 4 EXTERNAL FUSELAGE SKIN CRACK AT BS 516.5, STR 10R & .75 INCH CRACK AT BS 500B STR 10R. REPAIRED SKIN PER RA. 2 L 7 2 4F RT A16WE 2001031200603 20010312 00603 NM 2001 3 12 SWAA010318 1 20010131 A 5312 6517582 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 374SW 26582 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT RBL 17.1, UPPER SECTION. REPAIRED VERTI CAL BEAM WEB PER RA. 2 L 7 2 4F RT A16WE 2001031200604 20010312 00604 2001 3 12 SWAA010293 4 20010130 A 2565 D31354 SLIDE BOEING 737 7372T4 1384492 NM SEVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 AFT ENTRY AND SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF VIEW. RE-ADJUSTED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001031200605 20010312 00605 NM 2001 3 12 SWAA010294 1 20010129 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 347SW 24374 AFT LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2001031200606 20010312 00606 2001 3 12 SWAA010295 4 20010129 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 607SW 27927 FWD SVC DOOR EMERGENCY EVAC SLIDE ASSY FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001031200607 20010312 00607 NM 2001 3 12 SWAA010297 1 20010130 A 3350 079123 LENS BOEING 737 7377H4 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 749SW 29801 EEPLS WHITE LENS MISSING NEAR FWD SECTION. REPLACED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001031200608 20010312 00608 NM 2001 3 12 SWAA010298 1 20010129 A 3350 0L3071BPL5GPL LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED PM CHECK, FOUND 2 EEPLS BULBS INOP AT ROW 3. RELAMPED EEPLS PER MM. 2 L 7 2 4F A16WE 2001031200609 20010312 00609 NM 2001 3 12 SWAA010299 1 20010130 A 5315 6546804 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 277, LBL 17 & LBL 24. REPAIRED FLOORBEAM UPPER CHORD PER SRM. 2 L 7 2 4F A16WE 2001031200610 20010312 00610 NM 2001 3 12 SWAA010300 1 20010129 A 5754 6546422 SLAT BOEING 737 7372H4 138448C NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 073SW 22673 DURING SCHEDULED C2 CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED. REMOVED AND REPLACED L/E SLAT PER MM. 2 L 7 2 4F A16WE 2001031200611 20010312 00611 NM 2001 3 12 SWAA010301 1 20010129 A 5754 6546422 SLAT BOEING 737 7372H4 138448C NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 073SW 22673 DURING SCHEDULED C2 CHECK, FOUND RT WING NR 6 L/E SLAT DELAMINATED. REPAIRED L/E SLAT PER SRM. 2 L 7 2 4F A16WE 2001031200612 20010312 00612 NM 2001 3 12 SWAA010302 1 20010129 A 5755 6546451 SPOILER BOEING 737 7372H4 138448C NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 073SW 22673 DURING SCHEDULED C2 CHECK, FOUND NR 7 SPOILER OTBD AREA DELAMINATED. REMOVED AND REPLACED NR 7 SPOILER PER MM. 2 L 7 2 4F A16WE 2001031200613 20010312 00613 NM 2001 3 12 SWAA010303 1 20010129 A 5755 6546451 SPOILER BOEING 737 7372H4 138448C NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 073SW 22673 DURING SCHEDULED C2 CHECK, FOUND NR 6 SPOILER DELAMINATED. REMOVED AND REPLACED NR 6 SPOILER PER MM. 2 L 7 2 4F A16WE 2001031200614 20010312 00614 NM 2001 3 12 SWAA010304 1 20010130 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED C1 CHECK, FOUND EEPLS LOOSE AT FWD SECTION. SECURED EPPLS PER MM. 2 L 7 2 4F RT A16WE 2001031200615 20010312 00615 NM 2001 3 12 SWAA010305 1 20010130 A 5312 6517583 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 374SW 26582 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT RBL 17, WL 277. REPAIRED VERTICAL BEAM WEB PER RA. 2 L 7 2 4F RT A16WE 2001031200616 20010312 00616 NM 2001 3 12 SWAA010306 1 20010129 A 3350 100031 LIGHT BOEING 737 737317 138447P NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED C4 CHECK, FOUND MID CABIN OVERHEAD EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001031200617 20010312 00617 NM 2001 3 12 SWAA010277 1 20010127 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 515SW 25154 EEPLS BULBS INOP AT ROW 9, ROW 11 AND TRACK COVER BROKEN AT ROW 7. RELAMPED EEPLS AND REPLACED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001031200618 20010312 00618 NM 2001 3 12 SWAA010278 1 20010127 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 EEPLS TRACK COVER MISSING AND WIRES EXPOSED AT EMERGENCY EXIT ROW. SECURED WIRING AND REPLACED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001031200619 20010312 00619 2001 3 12 SWAA010279 4 20010127 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 514SW 25153 FWD ENTRY DOOR EMERGENCY EVAC SLIDE ASSY FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001031200620 20010312 00620 2001 3 12 SWAA010280 4 20010128 A 2565 D31354 SLIDE BOEING 737 7372K6 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001031200621 20010312 00621 2001 3 12 SWAA010281 4 20010128 A 2210 4051601 CONTROL PANEL BOEING 737 7373H4 1384600 NM COCKPIT FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 332SW 23696 AIR TURNBACK, MCP FAILED. RESET ALL FMC C/B AND RESEATED ALL DIGITAL FLIGHT COMPUTERS. RESEATED CONNECTORS AT MCP. PE RFORMED DFCS BITE TEST. ALL INDICATIONS AND BITE TEST GOOD. AT PHX, REPLACED A FCC FOR MX CONVENIENCE. 2 L 7 2 4F RT A16WE 2001031200622 20010312 00622 NM 2001 3 12 SWAA010282 1 20010129 A 3397 5417N509 WIRE BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 388SW 26591 EEPLS WIRING BROKEN NEAR EMERGENCY EXIT ROW. REPAIRED WIRING PER MM. 2 L 7 2 4F RT A16WE 2001031200623 20010312 00623 NM 2001 3 12 SWAA010283 1 20010129 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 388SW 26591 EEPLS TRACK COVER MISSING AT ROW 12. REPLACED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001031200624 20010312 00624 2001 3 12 SWAA010284 4 20010128 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 616SW 27699 AFT SVC DOOR EMERGENCY EVAC SLIDE ASSY INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001031200625 20010312 00625 NM 2001 3 12 SWAA010285 1 20010127 A 3350 079123 COVER BOEING 737 737317 138447P NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 EEPLS TRACK COVER LOOSE BETWEEN ROW 18 & 20. SECURED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001031200627 20010312 00627 NM 2001 3 12 VNAA0101026 1 20010128 A 3234 7178011 CONTROL HANDLE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FAILED A VNAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 07 438JS 13848 3056 WHILE ON FINAL, THE CREW RECEIVED NO INDICATION WHETHER THE LANDING GEAR WAS DOWN OR NOT. THE CREW EXECUTED A GO AROUND AND REVIEWED THE QUICK REFERENCE HANDBOOK AND MANUALLY EXTENDED THE GEAR. THE CREW THEN RECEIVED THREE GREEN LIGHTS AN D LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR CONTROL LEVER IN ACCORDANCE WIT H DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001031200629 20010312 00629 NM 2001 3 12 VNAA0101023 1 20010125 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 434JS 12501 3051 THE CREW REPORTED THAT THE EMERGENCY LIGHTS WERE NOT ILLUMINATING AT ROWS 4 THROUGH 6. MAINTENANCE INSPECTED AND REPLAC ED THE EMERGENCY BATTERY AT THE 5LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONALS CHECK S WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001031200630 20010312 00630 NM 2001 3 12 VNAA0101022 1 20010124 A 3520 OXYGEN MASK DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DEPLOYED A VNAA K NONE O OTHER CL CLIMB 1 GL 07 436JS 3052 WHILE CLIMBING THROUGH 10,000 FEET THE OXYGEN MASKS DEPLOYED INADVERTENTLY. THE FLIGHT LANDED IN PIT WITH NO FURTHER IN CIDENTS. MAINTENANCE TROUBLESHOT THE WIRING, REPLACED THE SOLENOID AND OXYGEN PANEL, AND HAD A TEST FLIGHT. THE TEST F LIGHT WAS GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001031200631 20010312 00631 NM 2001 3 12 VNAA0102002 1 20010206 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 457PS 7592 3048 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROW FOUR WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 5LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WERE P ERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001031200632 20010312 00632 NM 2001 3 12 VNAA0102001 1 20010204 A 3060 TERMINAL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE PROPELLER BROKEN A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 437JS 3055 ON CLIMBOUT, THE CREW RECEIVED A PROPELLER ICE FAIL CAS MESSAGE. FLIGHT 4042 RETURNED TO THE FIELD WHERE MAINTENANCE IN SPECTED AND REPLACED A BROKEN TERMINAL END ON A PROPELLER DE-ICE LEAD WIRE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001031300113 20010313 00113 WP 2001 3 13 ABXA010054 1 20010215 A 3241 422551 CONTROL UNIT DOUG DC9 DC941 302207N WP ANTI-SKID SYS CONTAMINATED A ABXA O OTHER O OTHER LD LANDING 1 GL 23 976AX 27019 96 47596 THE WHEEL BRAKES FAILED TO OPERATE ON LANDING AT JAN. WHEN ANTI-SKID WAS SELECTED OFF, BRAKES WORKED NORMALLY. MAINTEN ANCE INSPECTED AND REPLACED THE ANTI-SKID CONTROL UNIT DUE TO WATER INTRUSION IAW DC-9 MM. MAINTENANCE DEFERRED THE ANT I-SKID SYSTEM IAW DC-9 MEL. *S/D* REMOVED WHEEL SPEED TRANSDUCERS AND INSPECTED WIRING AND TRANSDUCERS FOR DEFECTS. N ONE WHERE NOTED. PERFORMED ANTI-SKID ADJ/TEST IAW DC-9 MM 32-43-02 AND 32-43-00, AND RETURNED A/C TO SERVICE. 2 L 7 2 4F A6WE 2001031300114 20010313 00114 NM 2001 3 13 UPS01235012 1 20010218 A 4990 APU BOEING 727 727185C 138406N NM FUSELAGE OVERSERVICED A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:N/A, AFTER RUNNING PACK ON COCKPIT FILLED WITH SMOKE. SHUTDOWN PACK, SMOKE STARTED TO DISSIPATE. SMELL ED LIKE BURNING OIL. *S/D* FOUND APU OVER SERVICED OPERATED PACK COOL AND HOT. NO PROBLEM NOTED. 2 L 7 3 4F A3WE 2001031300115 20010313 00115 NM 2001 3 13 QXEA0100118 1 20010215 A 2120 ODOR DHAV DHC8 DHC8102 2809003 NM CABIN DETECTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX- STRONG FUEL ODOR AFTER ENGINE START. GROUND RAN ENGINES. NO FUEL SMELL NOTED IN BLEED SYSTEM. SUSPECT SLIGHT TAI L WIND CAUSED FUEL VAPOR TO ENTER BLEED SYSTEM OF NR 2 ENGINE DURING NR 1 ENGINE START. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001031300116 20010313 00116 NM 2001 3 13 SWAA010286 1 20010128 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED C3 CHECK, FOUND EEPLS LOOSE NEAR AFT GALLEY. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001031300117 20010313 00117 NM 2001 3 13 SWAA010287 1 20010128 A 3350 6556633 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED C3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2001031300118 20010313 00118 NM 2001 3 13 SWAA010288 1 20010129 A 5330 6552988 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED SERVICE CHECK, FOUND 3 EXTERNAL FUSELAGE SKIN CRACK AT BS 971, BETWEEN STR 21L & STR 22L. REPAIRED SKI N PER SRM. 2 L 7 2 4F RT A16WE 2001031300119 20010313 00119 NM 2001 3 13 SWAA010289 1 20010127 A 5314 6545866 KEELBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED D-CHECK, FOUND KEEL BEAM CORRODED AT BS 721, RBL 7 & BS 500D, LT SIDE. REPAIRED KEEL BEAM PER ER''S & SRM. 2 L 7 2 4F RT A16WE 2001031300120 20010313 00120 NM 2001 3 13 SWAA010290 1 20010129 A 5313 BAC1498 STRINGER BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED D-CHECK, FOUND STR 27L CORRODED FROM BS 500B TO BS 500D. REPAIRED STR PER SRM & ER. 2 L 7 2 4F RT A16WE 2001031300121 20010313 00121 NM 2001 3 13 SWAA010291 1 20010128 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 762SW 27876 DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVER CRACKED AT ROW 1. REMOVED AND REPLACED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001031300122 20010313 00122 NM 2001 3 13 SWAA010292 1 20010129 A 2750 113A3920 ROD BOEING 737 7377H4 NM RT WING BROKEN A SWAA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SW 07 794SW 30605 AIR TURNBACK, AFTER FLAP RETRACTION, A/C REQUIRED 3 UNITS OF RT RUDDER AND 2 UNITS OF AILERON TRIM TO REMAIN STRAIGHT AN D LEVEL. REMOVED AND REPLACED INBOARD AFT FLAP DRIVE ROD AND NR 6 FLAP TRACK FAIRING (P/N 113A9350) PER MM. 2 L 7 2 4F RT A16WE 2001031300123 20010313 00123 NM 2001 3 13 SWAA010257 1 20010126 A 5310 6546529 DOOR FRAME BOEING 737 7372H4 138448C NM FWD CARGO BAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/2D CHECK, FOUND FWD CARGO DOOR AFT FUSELAGE FRAME CRACKED AT BS 492.4, LOWER DOOR STOP. REPAIRED FRA ME PER SRM. 2 L 7 2 4F A16WE 2001031300124 20010313 00124 NM 2001 3 13 SWAA010258 1 20010126 A 5320 65C27314 CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/2D CHECK, FOUND STR CLIP CRACKED AT STR 24R, BS 493 TO BS 500. REMOVED AND REPLACED STR CLIP PER SRM . 2 L 7 2 4F A16WE 2001031300125 20010313 00125 NM 2001 3 13 SWAA010259 1 20010126 A 2560 6557463 BRACKET BOEING 737 7372H4 138448C NM FWD ENTRY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR AFT GIRT ASSY BRACKET CORRODED. REMOVED AND REPLACED GIRT BRACKET ASS Y PER SRM. 2 L 7 2 4F A16WE 2001031300126 20010313 00126 NM 2001 3 13 SWAA010260 1 20010126 A 5315 6546804 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 1016, LBL 15. REPAIRED FLOORBEAM UPPER CHORD PE R SRM. 2 L 7 2 4F A16WE 2001031300127 20010313 00127 NM 2001 3 13 SWAA010261 1 20010126 A 5330 65C35773 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/2D CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK BETWEEN BS 727 & BS 747, STR 13R. REPAIRED SKIN PER SRM & SWA SI. 2 L 7 2 4F A16WE 2001031300128 20010313 00128 2001 3 13 SWAA010262 4 20010126 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM CABIN OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 643SW 27716 DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001031300129 20010313 00129 NM 2001 3 13 SWAA010263 1 20010126 A 5320 AND10137 STIFFENER BOEING 737 7373Y0 1384671 NM RT MLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 665WN 23497 DURING SCHEDULED SPECIAL VISIT, FOUND BS 663 VERTICAL STIFFENER CRACKED AT RBL 6.25. REMOVED AND REPLACED VERTICAL STIF FENER PER SRM. 2 L 7 2 4F RT A16WE 2001031300130 20010313 00130 NM 2001 3 13 SWAA010264 1 20010126 A 5312 6517583 BULKHEAD BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM CRACKED AT RBL 17.1, WL 191. REPAIRED VERTICAL BEAM PER E R. 2 L 7 2 4F RT A16WE 2001031300131 20010313 00131 NM 2001 3 13 SWAA010265 1 20010126 A 3350 65C34691 LENS BOEING 737 7373Q8 1384670 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 317WN 24068 EMERGENCY EXIT LIGHT LENS COVER MISSING AT BULLNOSE, ROW 12 DEF. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2001031300132 20010313 00132 NM 2001 3 13 SWAA010266 1 20010126 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 LEFT OVERWING EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001031300133 20010313 00133 NM 2001 3 13 SWAA010267 1 20010127 A 5311 6546574 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/2D CHECK, FOUND BS 1142 UPPER FUSELAGE FRAME CHORD CRACKED AT STR 12R. REPAIRED FRAME CHORD PER SRM. 2 L 7 2 4F A16WE 2001031300134 20010313 00134 NM 2001 3 13 SWAA010268 1 20010127 A 3350 610478 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 089SW 22904 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK AND BASE (P/N 61-0779) PER MM. 2 L 7 2 4F A16WE 2001031300135 20010313 00135 NM 2001 3 13 SWAA010269 1 20010127 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 651SW 27721 DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT BULLNOSE, ROW 20 DEF. RELAMPED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001031300136 20010313 00136 NM 2001 3 13 SWAA010270 1 20010128 A 3221 6546206 GUSSET BOEING 737 7373H4 1384600 NM NLG CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED SERVICE CHECK, FOUND NOSE LANDING GEAR MAIN ACTUATOR UPPER ATTACH POINT GUSSET CRACKED. REMOVED AND RE PLACED GUSSET BRACKET PER SRM. 2 L 7 2 4F RT A16WE 2001031300137 20010313 00137 NM 2001 3 13 SWAA010271 1 20010128 A 5753 6546435 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 355SW 25250 DURING SCHEDULED C2 CHECK, FOUND RT WING T/E INBOARD AFT FLAP OUTBOARD LWR SURFACE DISBONDED. REPAIRED AFT FLAP ASSY PE R SRM. 2 L 7 2 4F RT A16WE 2001031300138 20010313 00138 NM 2001 3 13 SWAA010272 1 20010126 A 4960 38762594 SWITCH BOEING 737 7373H4 1384600 NM APU INOPERATIVE A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 346SW 24153 AIR TURNBACK, APU WENT TO OVERSPEED CONDITION DURING CLIMBOUT. REMOVED AND REPLACED 280 MODULE (P/N 65-52801) AND ELECT RONIC 3 SPEED SWITCH. OPS CHECK GOOD PER MM. 2 L 7 2 4F RT A16WE 2001031300139 20010313 00139 NM 2001 3 13 SWAA010273 1 20010127 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 386SW 26601 EEPLS LOOSE FROM OVERWING EXIT TO ROW 16. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001031300140 20010313 00140 NM 2001 3 13 SWAA010274 1 20010127 A 3350 079123 COVER BOEING 737 737317 138447P NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 EEPLS TRACK COVER LOOSE AT ROW 18 TO ROW 20. SECURED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001031300141 20010313 00141 NM 2001 3 13 SWAA010275 1 20010126 A 5610 5893543130 WINDOW BOEING 737 7373H4 1384600 NM COCKPIT CRACKED A SWAA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 614SW 28033 DECLARED EMERGENCY, FL 330, R1 WINDOW OUTER PANE CRACKED AND ARCED. PRESSURIZATION REMAINED NORMAL. REMOVED AND REPLA CED R1 WINDOW AND RT FRONT WINDOW HEAT CONTROLLER (P/N 531-2) PER MM. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2001031300142 20010313 00142 2001 3 13 SWAA010276 4 20010128 A 2210 4051601938 CONTROL PANEL BOEING 737 7373H4 1384600 NM COCKPIT INOPERATIVE A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 639SW 27712 AIR TURNBACK, PASSING FL 270, AUTO PILOT C/B TRIPPED OFF AND WOULD NOT RE-ENGAGE IN A OR B-MODE. MCP PANEL WOULD NOT RE SPOND TO ANY CHANGES. REMOVED AND REPLACED MCP PER MM. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2001031300143 20010313 00143 2001 3 13 SWAA010328 4 20010202 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 068SW 22357 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001031300144 20010313 00144 NM 2001 3 13 SWAA010329 1 20010202 A 2560 P2070001 FLASHLIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 082SW 22731 FWD OTBD FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT AND BATTERIES PER MM. 2 L 7 2 4F A16WE 2001031300145 20010313 00145 NM 2001 3 13 SWAA010330 1 20010202 A 3350 6104789 BATTERY PACK BOEING 737 7373Y0 1384671 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 682SW 23496 DURING SCHEDULED RON CHECK, FOUND EEPLS INOP AT FWD HALF OF CABIN. REMOVED AND REPLACED FWD EEPLS BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2001031300146 20010313 00146 NM 2001 3 13 SWAA010331 1 20010202 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 EEPLS BROKEN. INSTALLED FLOOR TRACKING, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2001031300147 20010313 00147 NM 2001 3 13 SWAA010332 1 20010202 A 5315 6546804 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 270, LBL 10 TO RBL 11. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F A16WE 2001031300148 20010313 00148 NM 2001 3 13 SWAA010333 1 20010204 A 5711 6545324 SPAR BOEING 737 7372H4 138448C NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED D-CHECK, FOUND 3 RT WING REAR SPAR UPPER CHORD CRACKS AT HOLE B24, RSS 222.14, HOLE C27, RSS 223.14 & H OLE D27, RSS 225.15. REPAIRED SPAR CHORD PER ER. 2 L 7 2 4F A16WE 2001031300149 20010313 00149 NM 2001 3 13 SWAA010334 1 20010202 A 5330 6545857 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 374SW 26582 DURING SCHEDULED 1/4D CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT AFT SVC DOOR LOWER FWD CORNER CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001031300150 20010313 00150 NM 2001 3 13 SWAA010335 1 20010202 A 5310 6545871 DOOR FRAME BOEING 737 7373H4 1384600 NM FWD CARGO BAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 374SW 26582 DURING SCHEDULED 1/4D CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT LOWER STOP, BS 493. REPAIRED DOOR FRAME PER T1-653-0 44. 2 L 7 2 4F RT A16WE 2001031300151 20010313 00151 NM 2001 3 13 SWAA010336 1 20010202 A 3350 101073 SIGN BOEING 737 7373H4 1384600 NM FWD/AFT ENTRY INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 398SW 27692 DURING SCHEDULED SERVICE CHECK, FOUND FWD AND AFT ENTRY EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED 4 BULBS PER MM. 2 L 7 2 4F RT A16WE 2001031300152 20010313 00152 NM 2001 3 13 SWAA010337 1 20010202 A 5312 6516300 BULKHEAD BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT RBL 4.75, WL 202. REPAIRED BULKHEAD WEB PER SRM. 2 L 7 2 4F RT A16WE 2001031300153 20010313 00153 NM 2001 3 13 SWAA010338 1 20010202 A 5330 6545774 SKIN BOEING 737 7373T5 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 667SW 23063 DURING SCHEDULED SERVICE CHECK, FOUND 3 EXTERNAL LT FUSELAGE SKIN CRACK BETWEEN BS 727C & BS 747, WL 208.1. REPAIRED SK IN PER SRM. 2 L 7 2 4F RT A16WE 2001031300154 20010313 00154 NM 2001 3 13 SWAA010339 1 20010203 A 5330 6552988 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 089SW 22904 DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACKED, APPROX BS 975, ABOVE STR 21L, EXTENDING FROM PREVI OUS REPAIR. REPAIRED SKIN PER RA. 2 L 7 2 4F A16WE 2001031300155 20010313 00155 NM 2001 3 13 SWAA010340 1 20010203 A 3350 300432 LIGHT BOEING 737 7373A4 1384585 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 345SA 23786 DURING SCHEDULED SERVICE CHECK, FOUND RT FUSELAGE EXTERNAL EMERGENCY LIGHT INOP AT BS 773. REMOVED AND REPLACED LIGHT A SSY PER MM. 2 L 7 2 4F RT A16WE 2001031300156 20010313 00156 NM 2001 3 13 SWAA010341 1 20010202 A 5320 65C27314 STRINGER CLIP BOEING 737 737301 1384611 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED 1/2D CHECK, FOUND 2 STRINGER CLIPS CRACKED AT BS 663, STRS 10R & 10L. REMOVED AND REPLACED STRINGER CL IPS PER SRM. 2 L 7 2 4F RT A16WE 2001031300157 20010313 00157 NM 2001 3 13 SWAA010342 1 20010203 A 3350 AD20131A BATTERY PACK BOEING 737 7373Q8 1384670 NM SERVICE DOOR DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 663SW 23256 DURING SCHEDULED PM CHECK, FOUND FWD SVC DOOR OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2001031300158 20010313 00158 NM 2001 3 13 SWAA010343 1 20010203 A 5320 6551698 SPLICE BOEING 737 7375H4 138449D NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 512SW 24189 DURING SCHEDULED D-CHECK AT DALFORT, FOUND STR 4R SPLICE CRACKED AT BS 907. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2001031300159 20010313 00159 NM 2001 3 13 SWAA010344 1 20010203 A 5340 144A2604 CASTING BOEING 737 7377H4 NM RT MLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 705SW 27839 DURING SCHEDULED C3 CHECK, FOUND RT MLG WHEEL WELL AFT SUPPORT WEB & SUPPORT CASTING CRACKED. REMOVED AND REPLACED WEB AND CASTING PER SRM. 2 L 7 2 4F RT A16WE 2001031300160 20010313 00160 2001 3 13 SWAA010361 4 20010205 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 068SW 22357 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASS Y PER MM. 2 L 7 2 4F A16WE 2001031300161 20010313 00161 2001 3 13 SWAA010362 4 20010205 A 2565 6567380 COVER BOEING 737 7372H4 138448C NM ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 068SW 22357 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CONTAINER LOOSE. SECURED CONTAINER PER MM. 2 L 7 2 4F A16WE 2001031300162 20010313 00162 NM 2001 3 13 SWAA010363 1 20010206 A 3350 610479 POWER SUPPLY BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 089SW 22904 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EXIT LIGHT INOP. REMOVED AND REPLACED POWER SUPPLY PER MM. 2 L 7 2 4F A16WE 2001031300163 20010313 00163 NM 2001 3 13 SWAA010364 1 20010206 A 2560 65C168209 RETAINER BOEING 737 7373H4 1384600 NM ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER LOOSE. REMOVED AND REPLACED RETA INER RIVETS PER SRM. 2 L 7 2 4F RT A16WE 2001031300164 20010313 00164 NM 2001 3 13 SWAA010365 1 20010206 A 5330 6545857 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED C3 CHECK, FOUND .1875 INCH EXTERNAL FUSELAGE SKIN CRACK AT AFT SVC DOOR UPPER CUTOUT. REPAIRED SKIN PE R RA. 2 L 7 2 4F RT A16WE 2001031300165 20010313 00165 NM 2001 3 13 SWAA010366 1 20010206 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 711HK 27845 DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVER CRACKED AT FWD SECTION. REMOVED AND REPLACED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001031300166 20010313 00166 NM 2001 3 13 SWAA010367 1 20010206 A 3397 079123 WIRE BOEING 737 7377H4 1384404 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 701GS 27836 EEPLS WIRING EXPOSED. INSTALLED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001031300167 20010313 00167 NM 2001 3 13 SWAA010368 1 20010206 A 2560 P4010021 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 OUTBOARD FWD EMERGENCY FLASHLIGHT RED LIGHT INDICATOR INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2001031300168 20010313 00168 NM 2001 3 13 SWAA010369 1 20010206 A 2782 65445519 ACTUATOR BOEING 737 7373H4 1384600 NM LT WING FAILED A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 379SW 26586 AIR TURNBACK, 3 L/E FLAP FAILED TO RETRACT AFTER TAKEOFF. REMOVED AND REPLACED NR 3 L/E FLAP ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2001031300169 20010313 00169 NM 2001 3 13 SWAA010345 1 20010203 A 5210 507945 DOOR BOEING 737 7373H4 1384600 NM FWD ENTRY OUT OF ADJ A SWAA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SW 07 604SW 27955 AIR TURNBACK, AIRCRAFT FAILED TO PRESSURIZE DURING CLIMB. NO DOOR WARNING INDICATIONS. ADJUSTED FWD ENTRY DOOR PER MM. PRESSURIZED A/C & FOUND NO LEAKS PER MM. 2 L 7 2 4F RT A16WE 2001031300170 20010313 00170 NM 2001 3 13 SWAA010346 1 20010204 A 3350 20121 CHARGER BOEING 737 7373Q8 1384670 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 663SW 23256 FWD SVC DOOR EMERGENCY EXIT LIGHT ILLUMINATED AFTER PUSHBACK. REMOVED AND REPLACED HOUSING CHARGER ASSY PER MM. 2 L 7 2 4F RT A16WE 2001031300171 20010313 00171 NM 2001 3 13 SWAA010347 1 20010204 A 3350 20121 CHARGER BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 361SW 26572 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED HOUSING CHARGER ASSY PER MM. 2 L 7 2 4F RT A16WE 2001031300172 20010313 00172 NM 2001 3 13 SWAA010348 1 20010204 A 2560 P2070004 RETAINER BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 610WN 27696 DURING SCHEDULED SERVICE CHECK, FOUND FWD RT FLASHLIGHT HOLDER BROKEN. REMOVED AND REPLACED FLASHLIGHT HOLDER PER MM. 2 L 7 2 4F RT A16WE 2001031300173 20010313 00173 2001 3 13 SWAA010349 4 20010205 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 AFT SVC AND ENTRY DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF VIEW. REPOSITIONED SLIDE ASSY''S PER MM. 2 L 7 2 4F A16WE 2001031300174 20010313 00174 NM 2001 3 13 SWAA010350 1 20010205 A 3350 207377 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 362SW 26573 EEPLS LENS MISSING AT OVERWING EXIT. REMOVED AND REPLACED TRACK COVER ASSY PER MM. 2 L 7 2 4F RT A16WE 2001031300175 20010313 00175 NM 2001 3 13 SWAA010351 1 20010205 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 636WN 27709 EEPLS TRACK COVERS MISSING AT ROWS 19 & 20. INSTALLED TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 2001031300176 20010313 00176 2001 3 13 SWAA010352 4 20010205 A 2565 D31354 SLIDE BOEING 737 7377H4 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 743SW 29279 FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001031300177 20010313 00177 NM 2001 3 13 SWAA010353 1 20010205 A 5551 6551524 FITTING BOEING 737 7372H4 138448C NM HORIZ STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED D-CHECK, FOUND LT AND RT HORIZ STAB CENTER SECTION, FWD SPAR LOWER CLEVIS, FWD AND AFT LUG OUT OF LIMIT S. REPAIRED LUGS PER ACO & ER. 2 L 7 2 4F A16WE 2001031300178 20010313 00178 NM 2001 3 13 SWAA010354 1 20010205 A 3350 300432 LIGHT BOEING 737 7372H4 138448C NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 2001031300179 20010313 00179 2001 3 13 SWAA010355 4 20010204 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001031300180 20010313 00180 NM 2001 3 13 SWAA010356 1 20010204 A 3350 207377 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 635SW 27708 DURING SCHEDULED C2 CHECK, FOUND EEPLS MISSING RED LENS AT REAR SECTION OF CABIN. INSTALLED TRACK COVER ASSY PER MM. 2 L 7 2 4F RT A16WE 2001031300181 20010313 00181 NM 2001 3 13 SWAA010357 1 20010204 A 5310 6517978 CREASE BEAM BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM WEB CRACKED AT LT SIDE, BS 616 TO BS 639. REPAIRED CREASE BEAM WEB PER S RM. 2 L 7 2 4F RT A16WE 2001031300182 20010313 00182 NM 2001 3 13 SWAA010358 1 20010205 A 5311 6545808 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT SVC DOOR CUTOUT, BS 294, WL 208. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001031300183 20010313 00183 NM 2001 3 13 SWAA010359 1 20010203 A 5754 6573714 SLAT BOEING 737 7373T0 1384582 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 684WN 23941 DURING SCHEDULED SERVICE CHECK, FOUND NR 2 L/E SLAT INBD EDGE OF T/E WEDGE DELAMINATED. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2001031300184 20010313 00184 NM 2001 3 13 SWAA010360 1 20010204 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 775SW 30590 DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVER BROKEN AT FWD SECTION. REMOVED AND REPLACED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001031300185 20010313 00185 NM 2001 3 13 VNAA0102004 1 20010208 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 440JS 11413 3058 THE CREW REPORTED THAT THE LAST STRIP OF EMERGENCY FLOOR LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLA CED THE EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001031300187 20010313 00187 NM 2001 3 13 VNAA0102006 1 20010211 A 3350 501122803 POWER SUPPLY 501122803 DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN FAILED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 432JS 14644 7465 3045 THE CREW REPORTED THAT THE EMERGENCY POWER SUPPLY UNITS WOULD NOT TEST. THE AIRCRAFT WAS FERRIED TO PIT WHERE MAINTENAN CE INSPECTED AND REPLACED BOTH EMERGENCY POWER SUPPLY UNITS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPE RATIONAL TESTS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001031300188 20010313 00188 EU 2001 3 13 DHL2001365001 1 20010220 A 5610 WINDOW AIRBUS 300 A300B4203 3930306 EU COCKPIT MALFUNCTIONED A DHLA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 365DH 149 ON PRE TAKEOFF CHECKLIST DISCOVERED THE CAPTAINS SLIDING WINDOW WOULD NOT LATCH PROPERLY. LUBED LOCKING MECHANISM. PER FORMED OPERATIONAL CHECK IAW MM 56-10-0. OPS CHECK NORMAL. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2001031300189 20010313 00189 NM 2001 3 13 SWAA010479 1 20010216 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 379SW 26586 FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001031300190 20010313 00190 NM 2001 3 13 SWAA010480 1 20010216 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 388SW 26591 EEPLS LOOSE AT MID CABIN. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001031300191 20010313 00191 NM 2001 3 13 SWAA010481 1 20010216 A 3350 079123 COVER BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 525SW 26567 EEPLS TRACK COVER BROKEN. REMOVED AND REPLACED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001031300192 20010313 00192 2001 3 13 SWAA010482 4 20010216 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 396SW 27690 DURING SCHEDULED C1 CHECK, FOUND AFT SVC AND ENTRY DOOR EMERGENCY EVAC SLIDE ASSYS OUT OF ADJUST. RE-ADJUSTED EVAC SLID E ASSYS PER MM. 2 L 7 2 4F RT A16WE 2001031300193 20010313 00193 NM 2001 3 13 SWAA010483 1 20010216 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM ENTRY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 396SW 27690 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2001031300194 20010313 00194 NM 2001 3 13 SWAA010484 1 20010216 A 5240 6969854 GUSSET BOEING 737 737301 1384611 NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR CRACKED AT AFT LOWER CORNER GUSSET. REPAIRED GUSSET PER BAC DWG. 2 L 7 2 4F RT A16WE 2001031300195 20010313 00195 NM 2001 3 13 SWAA010485 1 20010216 A 5310 6545409 PRESSURE PANEL BOEING 737 737301 1384611 NM LT MLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED 1/2D CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 665, LBL 32. REPAIRED BEADED WEB PER TR T1-353-046 . 2 L 7 2 4F RT A16WE 2001031300196 20010313 00196 NM 2001 3 13 SWAA010486 1 20010216 A 5311 6546546 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 21R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001031300197 20010313 00197 NM 2001 3 13 SWAA010487 1 20010216 A 5320 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED, BS 500B, STR 9L, BS 500D, STR 5L, BS 520, STRS 5R, 6L & 8L, BS 1 121, STR 21L. REMOVED AND REPLACED CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001031300198 20010313 00198 NM 2001 3 13 SWAA010488 1 20010216 A 5320 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED D-CHECK, FOUND 12 STRINGER CLIPS CRACKED, BS 559-BS 727A, STRINGERS 10L, 5R, 8L, 5L, 4L, 1, 2L, 6R, 7R , 3L & 6L. REMOVED AND REPLACED CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001031300199 20010313 00199 NM 2001 3 13 SWAA010489 1 20010217 A 3350 07912 TRACK BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 067SW 22356 EEPLS TRACK SECTION LOOSE. SECURED TRACK SECTION PER MM. 2 L 7 2 4F A16WE 2001031300200 20010313 00200 2001 3 13 SWAA010490 4 20010217 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 AFT ENTRY DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001031300201 20010313 00201 NM 2001 3 13 SWAA010491 1 20010217 A 2781 2061141 INDICATOR BOEING 737 7373H4 1384600 NM COCKPIT MALFUNCTIONED A SWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 07 336SW 23940 AIR TURNBACK, L/E FLAPS WOULD NOT RETRACT DURING CLIMB. REMOVED AND REPLACED FLAP/SLAT POSITION INDICATOR. OPS CK GOOD PER MM. 2 L 7 2 4F RT A16WE 2001031300202 20010313 00202 2001 3 13 SWAA010492 4 20010217 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 384SW 26590 FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER DURING DOOR OPENING. LATER AT BHM, CONTAINER CAME LOOSE FROM DOOR . REINSTALLED SLIDE ASSY AND SECURED CONTAINER TO DOOR PER MM. 2 L 7 2 4F RT A16WE 2001031300203 20010313 00203 NM 2001 3 13 SWAA010493 1 20010217 A 3350 07912 COVER BOEING 737 7377H4 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 714CB 27848 EEPLS TRACK COVER BROKEN AT ROW 1. REPAIRED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001031300204 20010313 00204 2001 3 13 SWAA010494 4 20010217 A 2565 D31354 SLIDE BOEING 737 7373Y0 1384671 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED BC4 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE OUT OF ADJUST. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001031300205 20010313 00205 NM 2001 3 13 SWAA010495 1 20010217 A 3350 07912 COVER BOEING 737 7377H4 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 778SW 27883 DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK CRACKED AT ROW 1. REMOVED AND REPLACED TRACK COVER. 2 L 7 2 4F RT A16WE 2001031300206 20010313 00206 2001 3 13 SWAA010469 4 20010215 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 AFT SERVICE DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001031300207 20010313 00207 2001 3 13 SWAA010470 4 20010215 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING CLOSING OF FWD ENTRY DOOR, EVACUATION SLIDE FELL OUT OF BRACKET. SECURED SLIDE ASSY AND COVER PER MM. 2 L 7 2 4F RT A16WE 2001031300208 20010313 00208 2001 3 13 SWAA010471 4 20010214 A 3442 65C26143 FILTER BOEING 737 7373H4 1384600 NM EE BAY CLOGGED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 07 615SW 27698 AT APPROX 4000 FEET, ELECTRICAL FUMES PRESENT IN COCKPIT. NO SMOKE OBSERVED. C/W BOTH ENGS BORESCOPE INSP, REMOVED AND REPLACED A/C COALESCER BAGS, INSP ACM''S, INSP FWD E&E COMPT AND E&E EQUIPMENT IN COCKPIT. NO DEFECT NOTED. FOUND RAD AR FILTER CLOGGED, SUSPECT RADAR R/T OVERHEAT. CLEANED FILTER. OPS CK GOOD PER MM. 2 L 7 2 4F RT A16WE 2001031300209 20010313 00209 NM 2001 3 13 SWAA010472 1 20010215 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 636WN 27709 EEPLS TRACK COVER LOOSE. REMOVED AND REPLACED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001031300210 20010313 00210 NM 2001 3 13 SWAA010473 1 20010215 A 5240 6969854 FRAME BOEING 737 7373H4 1384600 NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR FRAME CRACKED AT AFT LOWER CORNER. REPAIRED FRAME PER BAC DRAWING. 2 L 7 2 4F RT A16WE 2001031300211 20010313 00211 NM 2001 3 13 SWAA010474 1 20010215 A 5753 6546434 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED 1/4D CHECK, FOUND LT INBD T/E AFT FLAP DELAMINATED AT OUTBD T/E. REMOVED AND REPLACED FLAP ASSY PER MM . 2 L 7 2 4F RT A16WE 2001031300212 20010313 00212 2001 3 13 SWAA010475 4 20010215 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF TOLERANCE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 608SW 27928 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF LIMITS. REMOVED AND REPLAC ED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001031300213 20010313 00213 NM 2001 3 13 SWAA010476 1 20010215 A 5312 6516300 BULKHEAD BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 4.7, WL 212-213. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 2001031300214 20010313 00214 NM 2001 3 13 SWAA010477 1 20010215 A 2782 65445519 ACTUATOR BOEING 737 7373H4 1384600 NM RT WING INOPERATIVE A SWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 07 616SW 27699 AIR TURNBACK, RT KRUEGER FLAP WOULD NOT RETRACT. REMOVED AND REPLACED RT KRUEGER FLAP ACTUATOR. OPS CK GOOD PER MM. 2 L 7 2 4F RT A16WE 2001031300215 20010313 00215 NM 2001 3 13 SWAA010478 1 20010214 A 2612 896767 SENSOR BOEING 737 7373H4 1384600 NM APU FAULTY A SWAA F ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 SW 07 331SW 23695 DECLARED EMERGENCY. DURING APU START, APU FIRE WARNING LIGHT ILLUMINATED. APU FIRE HANDLE PULLED. NO OTHER IND OF AP U FIRE. INSPECTED APU AREA FOR EVIDENCE OF FIRE. NO DEFECT NOTED. DEFERRED APU SYS. DURING RON IN HOU, FOUND APU TAI LPIPE HARNESS AND SENSOR DEFECTIVE. REMOVED AND REPLACED BOTH PER MM. OPS CK GOOD. APU FIRE BOTTLE REPLACED. 2 L 7 2 4F RT A16WE 2001031300216 20010313 00216 NM 2001 3 13 SWAA010455 1 20010213 A 3350 90083 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT FWD SECTION. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2001031300217 20010313 00217 2001 3 13 SWAA010456 4 20010213 A 2565 1061323161 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF TOLERANCE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF LIMITS. REMOVED AND REPLACE D EVAC SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001031300218 20010313 00218 NM 2001 3 13 SWAA010457 1 20010214 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 932, STR 22L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001031300219 20010313 00219 NM 2001 3 13 SWAA010458 1 20010214 A 5754 6573714 SLAT BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED 1/4D CHECK, FOUND NR 5 L/E SLAT CRACKED AT LOWER SKIN, 7 INBD OF ACTUATOR. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2001031300220 20010313 00220 NM 2001 3 13 SWAA010459 1 20010213 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED 1/4D CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHTS LOOSE AT ROWS 18 ABC & 21 ABC. SECURED LIGHTS PER MM. 2 L 7 2 4F RT A16WE 2001031300221 20010313 00221 NM 2001 3 13 SWAA010460 1 20010214 A 5330 6552880 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED C4 CHECK, FOUND EXTERNAL FUSELAGE SKIN DOUBLER CRACKED AT AFT SVC DOOR UPPER HINGE CUTOUT. REPAIRED SK IN PER SWA RA. 2 L 7 2 4F RT A16WE 2001031300222 20010313 00222 NM 2001 3 13 SWAA010461 1 20010214 A 3350 57771 CAP BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED C4 CHECK, FOUND EEPLS END CAP MISSING AT AFT SECTION. INSTALLED END CAP PER MM. 2 L 7 2 4F RT A16WE 2001031300223 20010313 00223 NM 2001 3 13 SWAA010462 1 20010213 A 5310 6546569 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 1040, BETWEEN STR 2L & 3L. REMOVED AND REPLACED SHEAR TIE PER S RM. 2 L 7 2 4F RT A16WE 2001031300224 20010313 00224 NM 2001 3 13 SWAA010463 1 20010213 A 5320 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED D-CHECK, FOUND STR CLIPS CRACKED AT BS 380, STR 8L, BS 520, STR 16L, BS 500D, STR 3L, 6L, 7L, 8L, 5R, & 8R, BS 500C, STR 7R, BS 360, STR 5L, BS 360, STR 2L, BS 344, STR 11R, BS 639, STR 8L, BS 597, STR 8R, & BS 663.75, STR 10R. REMOVED AND REPLACED STR CLIPS PER SRM & TRM. 2 L 7 2 4F RT A16WE 2001031300225 20010313 00225 NM 2001 3 13 SWAA010464 1 20010213 A 5310 6546529 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 520, BETWEEN STR 15L & 16L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2001031300226 20010313 00226 NM 2001 3 13 SWAA010465 1 20010212 A 2560 6557463 BRACKET BOEING 737 7373Q8 1384670 NM ENTRY DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED D-CHECK, FOUND BOTH FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR BRACKETS CORRODED. REMOVED AND REPLACED BRACKETS PER SRM. 2 L 7 2 4F RT A16WE 2001031300227 20010313 00227 NM 2001 3 13 SWAA010466 1 20010214 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 527SW 26569 EEPLS WIRING EXPOSED AND INOP AT OVERWING EXIT. RECONNECTED WIRING AND SECURED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001031300228 20010313 00228 NM 2001 3 13 SWAA010467 1 20010214 A 3260 6546141 UPLOCK SENSOR BOEING 737 7373H4 1384600 NM LT MLG OUT OF ADJ A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 327SW 23691 AIR TURNBACK, DECLARED EMERGENCY. LEFT MLG RED LIGHT REMAINED ILLUMINATED UPON GEAR RETRACTION. CYCLED GEAR, LIGHT REM AINED ILLUMINATED. REPOSITIONED UPLOCK TARGET SENSOR & OPS CHECK GOOD PER MM. 2 L 7 2 4F RT A16WE 2001031300229 20010313 00229 2001 3 13 SWAA010468 4 20010214 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 520SW 25319 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001031300230 20010313 00230 NM 2001 3 13 SWAA010437 1 20010212 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 EEPLS LOOSE IN FWD SECTION. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001031300231 20010313 00231 NM 2001 3 13 SWAA010438 1 20010212 A 3350 BR2013 CONNECTOR BOEING 737 7373H4 1384600 NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 362SW 26573 EEPLS DAMAGED. REPAIRED DAMAGED EEPLS CONNECTIONS PER MM. 2 L 7 2 4F RT A16WE 2001031300232 20010313 00232 2001 3 13 SWAA010439 4 20010212 A 2565 D31354 SLIDE BOEING 737 7377H4 NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 753SW 29848 FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001031300233 20010313 00233 NM 2001 3 13 SWAA010440 1 20010213 A 5551 6551524 FITTING BOEING 737 7372H4 138448C NM HORIZONTAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/2D CHECK, FOUND LT HORIZ STAB CENTER SECTION REAR SPAR UPPER AND LOWER AFT CLEVIS LUGS CORRODED. REP AIRED LUGS PER BFG ER. 2 L 7 2 4F A16WE 2001031300234 20010313 00234 2001 3 13 SWAA010441 4 20010212 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SVC/ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED C3 CHECK, FOUND AFT SVC & ENTRY DOOR EMERGENCY EVAC SLIDE ASSY''S OUT OF ADJUST. RE-ADJUSTED EVAC SLID E ASSY''S PER MM. 2 L 7 2 4F A16WE 2001031300235 20010313 00235 2001 3 13 SWAA010442 4 20010212 A 2565 65C19901 CABLE BOEING 737 7372H4 138448C NM ESCAPE SLIDE MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT CABLE MISROUTED. REPOSITIONED CABLE PER MM. 2 L 7 2 4F A16WE 2001031300236 20010313 00236 NM 2001 3 13 SWAA010443 1 20010212 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED C2 CHECK, FOUND 2.36 EXTERNAL FUSELAGE SKIN CRACK AT AFT SVC DOOR LOWER FWD CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001031300237 20010313 00237 NM 2001 3 13 SWAA010444 1 20010211 A 5755 65C2525121A SPOILER BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED C2 CHECK, FOUND NR 3 SPOILER UPPER SKIN DELAMINATED ABOVE THE ACTUATOR RECESS. REMOVED AND REPLACED SP OILER PER MM. 2 L 7 2 4F RT A16WE 2001031300238 20010313 00238 NM 2001 3 13 SWAA010445 1 20010213 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED 1/4D CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LOOSE AT ROW 2 DEF. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001031300239 20010313 00239 NM 2001 3 13 SWAA010446 1 20010213 A 3350 610478 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 344SW 24152 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS SECTION INOP AT AFT CABIN. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2001031300240 20010313 00240 NM 2001 3 13 SWAA010447 1 20010212 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 391SW 27378 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS TRACK COVER MISSING AT ROW 19. INSTALLED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001031300241 20010313 00241 NM 2001 3 13 SWAA010448 1 20010213 A 5753 6546435278A FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 636WN 27709 DURING SCHEDULED C2 CHECK, FOUND RT WING OTBD T/E AFT FLAP DISBONDED AT LOWER INBD SIDE. REMOVED AND REPLACED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2001031300242 20010313 00242 NM 2001 3 13 SWAA010449 1 20010212 A 5753 6546434369 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 636WN 27709 DURING SCHEDULED C2 CHECK, FOUND LT WING T/E INBD AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2001031300243 20010313 00243 NM 2001 3 13 SWAA010450 1 20010213 A 3350 65C34691 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 636WN 27709 DURING SCHEDULED C2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 16 DEF. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2001031300244 20010313 00244 NM 2001 3 13 SWAA010451 1 20010213 A 3350 6556633 LENS BOEING 737 737301 1384611 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED 1/2D CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2001031300245 20010313 00245 NM 2001 3 13 SWAA010452 1 20010213 A 5311 963820 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD VERTICAL CHORD CRACKED AT LBL 5.7, WL 184. REPAIRED VERTICAL CHORD P ER SRM. 2 L 7 2 4F RT A16WE 2001031300246 20010313 00246 NM 2001 3 13 SWAA010453 1 20010213 A 5312 6516300 BULKHEAD BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD WEB CRACKS AT LBL 12 TO LBL 13, WL 218 & RBL 6.7, WL 200 TO WL 201. RE PAIRED BULKHEAD WEB PER SRM. 2 L 7 2 4F RT A16WE 2001031300247 20010313 00247 NM 2001 3 13 SWAA010454 1 20010212 A 5320 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED D-CHECK, FOUND STR CLIPS CRACKED AT BS 616, STR 3R, BS 639, STR 4R & BS 706, STR 2L. REMOVED AND REPLA CED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001031300248 20010313 00248 2001 3 13 SWAA010416 4 20010211 A 2565 22D22900131 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF TOLERANCE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001031300249 20010313 00249 NM 2001 3 13 SWAA010417 1 20010211 A 3350 6040681 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED RON CHECK, FOUND EEPLS INOP ROWS 1 TO 5. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2001031300250 20010313 00250 NM 2001 3 13 SWAA010418 1 20010211 A 2560 P2070001 FLASHLIGHT BOEING 737 7373A4 1384585 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 680AA 23505 AFT UPPER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT, BATTERY AND HOLDER PER MM. 2 L 7 2 4F RT A16WE 2001031300251 20010313 00251 NM 2001 3 13 SWAA010419 1 20010210 A 5754 6573714 SLAT BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED 1/4D CHECK, FOUND NR 2 L/E SLAT T/E SKIN CRACKED AT RIVETS HEADS, 3 INBD OF T-DUCT. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2001031300252 20010313 00252 NM 2001 3 13 SWAA010420 1 20010211 A 5330 6545877 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED 1/2D CHECK, FOUND 1.5 EXTERNAL FUSELAGE SKIN CRACK AT FWD SVC DOOR CUTOUT, AFT LOWER CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001031300253 20010313 00253 NM 2001 3 13 SWAA010421 1 20010211 A 3350 610478 CHARGER BOEING 737 7377H4 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 700GS 27835 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER M M. 2 L 7 2 4F RT A16WE 2001031300254 20010313 00254 NM 2001 3 13 SWAA010422 1 20010212 A 2560 6557463 BRACKET BOEING 737 7372H4 138448C NM SERVICE DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BRACKET LOOSE. SECURED GIRT BRACKET PER MM. 2 L 7 2 4F A16WE 2001031300255 20010313 00255 NM 2001 3 13 SWAA010423 1 20010212 A 3350 BR2013 TRACK BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 EEPLS FLOOR TRACK LOOSE AT EMERGENCY EXIT ROW. SECURED EEPLS TRACK PER MM. 2 L 7 2 4F RT A16WE 2001031300256 20010313 00256 NM 2001 3 13 SWAA010424 1 20010211 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 362SW 26573 EEPLS WIRING EXPOSED AND BULBS INOP AT ROW 11 &12. SECURED EEPLS TRACK AND RELAMPED 2 BULBS PER MM. 2 L 7 2 4F RT A16WE 2001031300257 20010313 00257 NM 2001 3 13 SWAA010425 1 20010212 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 502SW 24179 EEPLS BROKEN AT OVERWING EXIT. REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001031300258 20010313 00258 NM 2001 3 13 SWAA010426 1 20010211 A 3350 079123 COVER BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 519SW 25318 EEPLS TRACK COVER BROKEN. REMOVED AND REPLACED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001031300259 20010313 00259 2001 3 13 SWAA010427 4 20010211 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 091SW 22963 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE ASSY OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PE R MM. 2 L 7 2 4F A16WE 2001031300260 20010313 00260 NM 2001 3 13 SWAA010428 1 20010212 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 313SW 23335 DURING SCHEDULED SERVICE CHECK, FOUND 2 EXTERNAL FUSELAGE SKIN CRACK AT BS 500C, STR 15L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001031300261 20010313 00261 NM 2001 3 13 SWAA010429 1 20010212 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED A1 CHECK, FOUND AFT LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2001031300262 20010313 00262 NM 2001 3 13 SWAA010430 1 20010212 A 2560 65C16820 RETAINER BOEING 737 7373H4 1384600 NM SERVICE DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED 1/4D CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER CORRODED. REMOVED AND REPLACED G IRT RETAINER PER MM. 2 L 7 2 4F RT A16WE 2001031300263 20010313 00263 NM 2001 3 13 SWAA010431 1 20010211 A 3350 0L3071BPL5GPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 653SW 28398 DURING SCHEDULED C2 CHECK, FOUND EEPLS INOP AT ROW 20. RELAMPED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001031300264 20010313 00264 NM 2001 3 13 SWAA010432 1 20010211 A 3350 207377 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 653SW 28398 DURING SCHEDULED C2 CHECK, FOUND EEPLS RED LENS MISSING AT AFT END. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2001031300265 20010313 00265 NM 2001 3 13 SWAA010433 1 20010212 A 5320 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED D-CHECK, FOUND STR CLIPS CRACKED AT STR 8R, BS 578 & 637, STR 7R, BS 557, STR 8L, BS 616, STR 4R, BS 61 6, & STR 6L BS 597 & 616. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001031300266 20010313 00266 NM 2001 3 13 SWAA010434 1 20010211 A 3350 65C27095 BATTERY PACK BOEING 737 7372H4 138448C NM COCKPIT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 091SW 22963 DURING SCHEDULED C1 CHECK, FOUND COCKPIT EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2001031300267 20010313 00267 NM 2001 3 13 SWAA010435 1 20010212 A 5315 6545410 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED 1/4D CHECK, FOUND TRANSVERSE BEAM WEB CRACKED AT BS 663, BL 0. REPAIRED BEAM WEB PER SWA RA & SB. 2 L 7 2 4F RT A16WE 2001031300268 20010313 00268 2001 3 13 SWAA010436 4 20010212 A 3425 H321AKM1 INDICATOR BOEING 737 7373L9 1384470 NM COCKPIT FAILED A SWAA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 657SW 23331 DIVERSION, STANDBY ADI FAILED DURING CRUISE. RESET C/B, NO HELP. ALL OTHER SYSTEMS NORMAL. REMOVED AND REPLACED STAND BY HORIZON PER MM, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2001031300269 20010313 00269 NM 2001 3 13 SWAA010397 1 20010209 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 EEPLS LOOSE IN FWD SECTION. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001031300270 20010313 00270 NM 2001 3 13 SWAA010398 1 20010209 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 344SW 24152 FWD INBOARD EMERGENCY FLASHLIGHT WOULD NOT TEST. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2001031300271 20010313 00271 NM 2001 3 13 SWAA010399 1 20010209 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 706SW 27840 EEPLS TRACK COVER MISSING AT ROW 9. REMOVED AND REPLACED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001031300272 20010313 00272 NM 2001 3 13 SWAA010400 1 20010211 A 5551 6551524 FITTING BOEING 737 7372H4 138448C NM HORIZONTAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED D-CHECK, FOUND LT AND RT HORIZ STAB CENTER SECTION HINGE HOUSING UPPER AND LOWER ATTACH LUGS CORRODED. REPAIRED LUGS PER BFG ER''S. 2 L 7 2 4F A16WE 2001031300273 20010313 00273 2001 3 13 SWAA010401 4 20010219 A 2565 106123167 SLIDE BOEING 737 7372K6 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REMOVED AND REPLACED E VAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001031300274 20010313 00274 NM 2001 3 13 SWAA010402 1 20010209 A 3350 0L3071BPL5GPL LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED A2 CHECK, FOUND EEPLS BULB INOP AT OVERWING EXIT. RELAMPED EEPLS PER MM. 2 L 7 2 4F A16WE 2001031300275 20010313 00275 NM 2001 3 13 SWAA010403 1 20010209 A 5330 6545778 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 927, BELOW STR 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001031300276 20010313 00276 NM 2001 3 13 SWAA010404 1 20010209 A 5310 BAC1517 DOOR FRAME BOEING 737 7373H4 1384600 NM ENTRY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR FRAME UPPER HINGE CUTOUT CRACKED AT FWD CORNER. REPAIRED FRAME PER SW A RA. 2 L 7 2 4F RT A16WE 2001031300277 20010313 00277 NM 2001 3 13 SWAA010405 1 20010209 A 5320 BAC1503 STIFFENER BOEING 737 7373Q8 1384670 NM MLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED SPECIAL VISIT, FOUND BS 663 VERTICAL STIFFENERS CRACKED AT LBL 6.5 & RBL 6.5. REMOVED AND REPLACED VER TICAL STIFFENERS PER SRM. 2 L 7 2 4F RT A16WE 2001031300278 20010313 00278 NM 2001 3 13 SWAA010406 1 20010210 A 3397 5417N509 WIRE BOEING 737 7373H4 1384600 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 387SW 26602 EEPLS INOP IN THREE PLACES. SECURED EEPLS WIRING PER MM. 2 L 7 2 4F RT A16WE 2001031300279 20010313 00279 NM 2001 3 13 SWAA010407 1 20010210 A 5315 6546804 FLOORBEAM BOEING 737 7372H4 138448C NM CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 987, LBL 22 TO RBL 55. REPAIRED FLOORBEAM UPPER CHORD PER BFG ER. 2 L 7 2 4F A16WE 2001031300280 20010313 00280 NM 2001 3 13 SWAA010408 1 20010210 A 5330 6545765 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACKED AT BS 595, STR 4R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001031300281 20010313 00281 NM 2001 3 13 SWAA010409 1 20010210 A 5753 6546435278 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED 1/4D CHECK, FOUND RIGHT T/E OUTBOARD AFT FLAP INBOARD EDGE DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2001031300282 20010313 00282 NM 2001 3 13 SWAA010410 1 20010210 A 2560 6557463 BRACKET BOEING 737 7373H4 1384600 NM SERVICE DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 364SW 26575 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BRACKET LOOSE. SECURED BRACKET PER MM. 2 L 7 2 4F RT A16WE 2001031300283 20010313 00283 2001 3 13 SWAA010411 4 20010209 A 2565 6567380 COVER BOEING 737 7373Q8 1384670 NM ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY RETAINER HOOKS LOOSE. REMOVED AND REPLAC ED EVAC SLIDE COVER ASSY PER MM. 2 L 7 2 4F RT A16WE 2001031300284 20010313 00284 2001 3 13 SWAA010412 4 20010209 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMEGRENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE AS SY PER MM. 2 L 7 2 4F RT A16WE 2001031300285 20010313 00285 NM 2001 3 13 SWAA010413 1 20010209 A 5230 6547952358 STRUCTURE BOEING 737 7375H4 138449D NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 504SW 24181 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR CRACKED INSIDE AT LOWER FWD CORNER ANGLE BRACKET, WEB SKIN AND FWD SIDE OF DOOR, INSIDE, LOWER SIDE STOP FITTING FASTENER. REMOVED AND REPLACED AFT CARGO DOOR PER MM. 2 L 7 2 4F RT A16WE 2001031300286 20010313 00286 NM 2001 3 13 SWAA010414 1 20010210 A 5330 65C33930 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED 1/2D CHECK, FOUND .75 INCH EXTERNAL FUSELAGE SKIN CRACK AT AFT SIDE OF EQUIPMENT EXHUAST CUTOUT. REPAI RED SKIN DOUBLER PER SWA ACO. 2 L 7 2 4F RT A16WE 2001031300287 20010313 00287 NM 2001 3 13 SWAA010415 1 20010211 A 3260 65C28034 UPLOCK SENSOR BOEING 737 7372H4 138448C NM NLG WW FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 063SW 22061 AIR TURNBACK, NLG GEAR INDICATED DOWN WITH HANDLE SELECTED IN UP POS. CYCLED GEAR, NO HELP. RETURNED TO DAL WITH NORMA L GEAR DOWN INDICATIONS. REMOVED AND REPLACED UP/DOWN LOCK SENSOR PER MM. OPS CHECK NORMAL PER MM. 2 L 7 2 4F A16WE 2001031300288 20010313 00288 2001 3 13 SWAA010389 4 20010208 A 2565 22D22901151 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF TOLERANCE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 090SW 22905 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001031300289 20010313 00289 NM 2001 3 13 VNAA0102009 1 20010217 A 3230 LANDING GEAR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NLG & MLG MALFUNCTIONED A VNAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 07 425JS 3037 FLIGHT 4189 WAS NOT GETTING THE LANDING GEAR LOCK DOWN INDICATION. THE CREW PERFORMED A MISS APPROACH AND RAN THROUGH T HE QUICK REFERENCE HANDBOOK. THE CREW USED THE EMERGENCY HYDRAULIC SYSTEM TO PUMP THE GEAR DOWN AND GOT A GEAR DOWN AND LOCKED INDICATION. NO EMERGENCY WAS DECLARED BUT THE CREW ASKED THAT THE TRUCKS BE ROLLED OUT. THE FLIGHT ATTENDENT D ID PREPARE THE CABIN FOR AN EMERGENCY LANDING. THE LANDING WAS UNEVENTFUL AND THERE WAS NO FLUCUATION IN HYDRAULIC PRES SURE. MAINTENANCE INSPECTED AND CLEANED THE NOSE WHEEL STEERING CANNON PLUG AND PERFORMED SEVERAL OPERATIONAL CHECKS WH ICH ALL CHECKED GOOD IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. THE ACFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001031300290 20010313 00290 NM 2001 3 13 VNAA0102007 1 20010213 A 3350 SIGN DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DETACHED A VNAA K NONE O OTHER TX TAXI/GRND HDL 1 GL 07 437JS 3055 THE CREW REPORTED THAT THE EMERGENCY EXIT SIGN AT ROW 9A FELL DOWN. MAINTENANCE INSPECTED AND SECURED THE EMERGENCY SIG N IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL TESTS WERE PERFORMED AND THE AIRCRAFT WAS RELEASE D FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001031300291 20010313 00291 NE 2001 3 13 RAIA00102005 2 20010216 A 7200 TPE33114 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE RT ENGINE FAILED A RAIA A UNSCHED LANDING J Y WARNING INDICATION ENGINE STOPPAGE TO TAKEOFF 1 CE 03 554HK 6916 2317 41067 75097R 5353-ALB- DURING TAKEOFF NR 2 ENGINE SHUTDOWN IN FLIGHT. OIL CONTAMINATION LIGHT, ENGINE SURGE, OIL PRESSURE FLUX, TORQ UE DROP, EGT 790-800. MAINTENANCE REMOVED AND REPLACED THE ENGINE IAW J41 MAINTENANCE MANUAL. 2 L 7 2 4T 4 T RT A41NM E18NE 2001031300292 20010313 00292 NE 2001 3 13 NACA2001008 2 20010215 A 7421 RHB32E SPARK PLUG DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE NR 4 ENGINE UNSERVICEABLE A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 AL 03 43872 533294 33325 FEATHERED NR 4 ENGINE DUE TO 200 RPM, 2 MANIFOLD, AND 30 BMEP LOSSES. COMPRESSION CHECK OK, BORESCOPED NR 16 NO DEFECTS , CHECKED OIL SCREENS, NOMETAL FOUND. REPLACED ALL SPARK PLUGS, GROUND RUNUP SATISFACTORY. 2 L 7 4 4R 4 R 6A3 5E8 2001031300293 20010313 00293 SO 2001 3 13 C2XA01CL027 1 20010215 A 3222 STRUT EMB 145 EMB145LR SO NLG LOW A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 13994 145291 EWR FLIGHT 4036 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE ALONG WITH A THRUST REVERSER 1/2 DISAGREE. TH E AIRCRAFT RETURNED TO EWR AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND SERVICED THE NOSE LANDING GEA R SHOCK ABSORBER. OPERTIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001031300294 20010313 00294 SO 2001 3 13 C2XA01CL028 1 20010218 A 3230 355022002MOD2 CONTROL UNIT EMB 135 EMB135LR SO COCKPIT FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 17521 152 152 145378 CLE FLIGHT 4135 THE CREW REPORTED THE LANDING GEAR DID NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLEVELAND A ND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT AND THE LANDING G EAR CONTROL LEVER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT TOOO11AT 2001031300295 20010313 00295 SO 2001 3 13 C2XA01CL029 1 20010218 A 3350 1317 LIGHT EMB 145 EMB145ER SO EXTERIOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15948 145056 DURING A MAINTENANCE SERVICE CHECK THE EMERGENCY LIGHT OVER THE RIGHT WING WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULB FOR THE EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001031300296 20010313 00296 EU 2001 3 13 C2XA01CL030 1 20010217 A 6123 SWITCH AEROSP ATR42 ATR42320 8680930 EU COCKPIT CONTAMINATED A C2XA K NONE O OTHER CR CRUISE 1 SW 27 14828 179 CLE FLIGHT 3232 THE CREW REPORTED DURING CRUISE THAT THE NR 2 PROPELLER WENT INTO FEATHER MOMENTARILY. THE AIRCRAFT LA NDED IN DAY WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND THE MICROSWITCHES IN THE CONTROL PEDSTAL TO BE ST ICKING. CLEANED THE SWITCHES AND CHANGED THE TORQUE SIGNAL CONDITIONER UNIT FOR PERCAUTIONARY PURPOSES. THE CREW REPOR TED THAT SOME APPLE JUICE WAS SPILLED IN THE COCKPIT. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED F OR SERVICE. 2 H 7 2 4T RT A53EU 2001031300297 20010313 00297 NM 2001 3 13 F3LA200100021 1 20010218 A 5320 WEB BOEING 737 7373S1 138447S NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 3095 24856 DURING C-4 CHECK, INSPECTION REPORTED WEB CORRODED AT LT SIDE OF FUSELAGE, AFT OF STA 986.5, FWD OF PRESSURE WEB. MAINT ENANCE FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 53-60-15, 51-40-02 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2001031300298 20010313 00298 NM 2001 3 13 F3LA200100022 1 20010218 A 5320 FLOOR SUPPORT BOEING 737 7373S1 138447S NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 3095 24856 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FUSELAGE STRUCTURE AT AFT GALLEY LOWER DOOR FRAME, STA 990 - 1006. M AINTENANCE REPLACED MOP SILL AND WEB PER SRM 51-40-02, 51-10-02 AND 51-20-05. 2 L 7 2 4F RT A16WE 2001031300299 20010313 00299 NM 2001 3 13 F3LA200100023 1 20010218 A 5310 CREASE BEAM BOEING 737 7373S1 138447S NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 3095 24856 DURING C-4 CHECK, INSPECTION REPORTED CORROSION AT AFT ENTRY DOOR THRESHOLD, STA 986. MAINTENANCE REMOVED CREASE BEAM, CLEANED UPPER AND LOWER SURFACE BELOW CREASE BEAM, BURNISHED LIGHT SURFACE CORROSION AND FOUND TO BE WITHIN LIMITS. REM OVED DAMAGED DOUBLER, FABRICATED AND INSTALLED REPLACEMENT DOUBLER. FABRICATED AND INSTALLED REPLACEMENT CREASE BEAM. WORK WAS PERFORMED PER SRM 51-40-06 AND 53-60-15. 2 L 7 2 4F RT A16WE 2001031300300 20010313 00300 WP 2001 3 13 TWAA0103301 1 20010220 A 3350 408822101 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 THE OVERWING INTERIOR EMERGENCY LIGHT WAS ON ALL THE TIME. REPLACED THE BATTERIES FOR BOTH INTERIOR OVERWING EMERGENCY LIGHTS. CHECK-C 2-18-01 MCI. 2 L 7 2 4F RT A6WE 2001031300301 20010313 00301 WP 2001 3 13 TWAA0103302 1 20010220 A 3350 7732 LIGHT DOUG DC9 DC983 3022083 WP CABIN BURNED OUT A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 974TW 53624 THE EGRESS LIGHT AT CABIN ROW 1 WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 9-20-00 STL. 2 L 7 2 4F RT A6WE 2001031300302 20010313 00302 WP 2001 3 13 TWAA0103303 1 20010220 A 3350 58222 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 908TW 49169 THE EGRESS LIGHTS WERE INOPERATIVE FROM ROW 1 THRU 5, THE FWD GALLEY EXIT SIGN, AND ROW 19 AND 20 EGRESS LIGHTS. REMOVE D MOISTURE FROM CONNECTORS FOR FWD CABIN EGRESS LIGHTS, REPLACED BATTERY PACK FOR EXIT LIGHT, AND CLEANED AND RESEATED F LOOR LIGHTS IN MID CABIN. CHECK-C 2-12-00 STL. 2 L 7 2 4F A6WE 2001031300303 20010313 00303 WP 2001 3 13 TWAA0103304 1 20010216 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9401W 53137 DURING CHECK-C MAINT THE NUMBER 5 CABIN SEAT TRACK, O/B FLANGE, STA 229, HAD CORROSION. REMOVED AND REPLACED FWD SECTIO N OF TRACK, APPROX 5 INCHES, TO EXISTING SPLICE PER SPM 6-70-01, PARA 4, ITEM A AND B. INSTALLED FASTENERS PER 51-30-2. 2 L 7 2 4F RT A6WE 2001031300304 20010313 00304 WP 2001 3 13 TWAA0103305 1 20010213 A 5320 STIFFENER DOUG DC9 DC983 3022083 WP AUX TANK BROKEN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9401W 53137 DURING CHECK-C MAINT THE FWD FUEL AUX TANK TOP LT SIDE STIFFENER WAS BROKEN APPROX 12 INCHES. INSTALLED 2 CHANNELS AND 1 FILLER PER ARA 17624. 2 L 7 2 4F RT A6WE 2001031300305 20010313 00305 WP 2001 3 13 TWAA0103306 1 20010214 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT A CABIN FLOOR PANEL MOUNT HAD CORROSION ON AFT EDGE OF FLOOR PANEL MOUNT, STA 1174, FLOOR PANEL NUM BER 85. FABRICATED NEW FLOOR SUPPORT PER SPM 6-70-01. PRIMED AND PAINTED NEW SUPPORT PER SRM 51-10-03. INSTALLED NEW SUPPORT AND FASTENERS PER SRM 51-10-05. 2 L 7 2 4F A6WE 2001031300306 20010313 00306 WP 2001 3 13 TWAA0103307 1 20010215 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT IN FWD CABIN FOUND CORROSION AT STA 180, LBL 13 INCHES TO 38 IN, ON FLOOR SUPPORT TOP AND UNDERSIDE . REPLACED FLOOR SUPPORT. REMOVED RIVETS AND INSTALLED RIVETS PER SRM 51-30-2. TREATED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001031300307 20010313 00307 WP 2001 3 13 TWAA0103308 1 20010212 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT IN CABIN FWD END OF TRACK AT RBL 24 INCHES HAD CORROSION GROUND BEYOND LIMITS AT STA 200. REMOVED CORROSION PER SPM 6-80-01. REPAIRED TRACK PER SRM 53-05, PAGE 10G. 2 L 7 2 4F A6WE 2001031300308 20010313 00308 WP 2001 3 13 TWAA0103309 1 20010216 A 5320 SUPPORT BRACKET DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT IN MID CARGO COMPT, FOUND CORROSION ON TRACK SUPPORT RT SIDE STA 598 TO 642. REMOVED TRACK SUPPORT AND FABRICATED NEW PER SRM 53-24-0, PAGE 19 AND 20. HEAT TREATED PER SRM 51-10-2A. ALODINE PER SRM 51-10-3. PRIMED A ND TOP COATED PER SRM 51-10-3. INSTALLED WITH ORIGINAL TYPE OF FASTENERS AND TORQUED PER SRM 51-30-1, DRAWING 5936660. 2 L 7 2 4F A6WE 2001031300309 20010313 00309 WP 2001 3 13 TWAA0103310 1 20010216 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT IN THE AFT CARGO COMPT THE RT FLOOR TIE DOWN TRACK HAD CORROSION INSIDE OF TRACK FROM STA 1008 TO 1 155. REMOVED TRACK AND REPLACED WITH NEW AND INSTALLED PER SPM 6-70-01, SRM 51-30-1, 51-30-2, AND DRAWING 5936660. 2 L 7 2 4F A6WE 2001031400137 20010314 00137 NM 2001 3 14 UPS01435013 1 20010218 A 5230 DOOR BOEING 747 747123F NM AFT CARGO DOOR UNSECURE A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 672UP 20324 INSPECTION TYPE:N/A, ATB- UNABLE TO PRESSURIZE IN AUTO OR MANUAL MODE AFTER TAKEOFF. A/C PRESURRIZED ON LANDIND. *S/D* SECURED AFT LOWER CARGO DOOR LATCH LOCK HANDLE AND VENT DOORS PERFORMED CARGO DOOR TEST, NO FAULTS NOTED. 2 L 7 4 4F A20WE 2001031400138 20010314 00138 SO 2001 3 14 C2XA01IA091 1 20010215 A 3231 DOOR EMB 145 EMB145LR SO NLG MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 13958 145085 IAH - FLIGHT 4240, THE CREW REPORTED THAT THE NOSE LANDING GEAR DOORS OPENED IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WH ERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE LANDING GEAR WITH NO DEFECTS NOTED, A ND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE DISCREPANCY REOCCURRED ON 02/16/01 FLIGHT 4121, THE AIRCRAFT RE TURNED TO IAH WITHOUT INCIDENT AND MAINTENANCE AGAIN PERFORMED AN OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM WITH NO D EFECTS NOTED. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001031400139 20010314 00139 SO 2001 3 14 C2XA01CL026 1 20010216 A 3610 S2U2226 O-RING EMB 145 EMB145ER SO BLEED AIR SYS LEAKING A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 15932 145015 CLE FLIGHT 4293, THE CREW REPORTED A BLEED 1 LEAK MESSAGE AFTER TAKEOFF. THE NR 1 ENGINE WAS SHUTDOWN AND THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED AN O-RING ON THE NR 1 BLE ED LINE IN THE CARGO BAY. OPERTIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001031400140 20010314 00140 NM 2001 3 14 SWAA010390 1 20010208 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 389SW 26592 EEPLS TRACK COVERS OUT OF POSITION AT MID CABIN. SECURED TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 2001031400141 20010314 00141 NM 2001 3 14 SWAA010391 1 20010208 A 5320 65C27314 STRINGER CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/2D CHECK, FOUND STR CLIP CRACKED AT BS 500, STR 11R. REMOVED AND REPLACED STR CLIP PER BAC DWG. 2 L 7 2 4F A16WE 2001031400142 20010314 00142 2001 3 14 SWAA010392 4 20010207 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SVC/ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 090SW 22905 DURING SCHEDULED C3 CHECK, FOUND AFT SVC AND ENTRY DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY''S PER MM. 2 L 7 2 4F A16WE 2001031400143 20010314 00143 NM 2001 3 14 SWAA010393 1 20010208 A 5752 65C25925 HINGE BOEING 737 7373H4 1384600 NM LT AILERON LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED 1/4D CHECK, FOUND LT AILERON OUTBOARD CENTER TAB HINGE SHAFT LOOSE IN SUPPORT HOUSING. REMOVED AND REP LACED HINGE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001031400144 20010314 00144 NM 2001 3 14 SWAA010394 1 20010208 A 2761 654485113 ACTUATOR BOEING 737 7373H4 1384600 NM RT WING BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED 1/4D CHECK, FOUND NR 5 GROUND SPOILER OUTBOARD ACTUATOR ATTACH LUG BROKEN. REMOVED AND REPLACED SPOILE R ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2001031400145 20010314 00145 NM 2001 3 14 SWAA010395 1 20010207 A 3350 65C27093 LENS BOEING 737 7373H4 1384600 NM SERVICE DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 620SW 28036 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2001031400146 20010314 00146 NM 2001 3 14 SWAA010396 1 20010208 A 2612 90163504 FIRE DETECTOR BOEING 737 7373T5 NM AFT CARGO BAY MALFUNCTIONED A SWAA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 07 667SW 23063 DECLARED EMERGENCY, AFT CARGO FIRE WARNING INDICATION DURING CRUISE. BOTH BOTTLES DISCHARGED. VERIFIED NO SIGN OF FIRE IN AFT CARGO COMPARTMENT. FIRE DETECTION/SUPPRESSION SYSTEM DEACTIVATED PER ACO. 2 L 7 2 4F RT A16WE 2001031400147 20010314 00147 NM 2001 3 14 SWAA010370 1 20010207 A 3350 65C27093 COVER BOEING 737 7372H4 138448C NM SERVICA DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 AFT SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT COVER LOOSE. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 2001031400148 20010314 00148 NM 2001 3 14 SWAA010371 1 20010206 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 389SW 26592 EEPLS INOP AT ROW 14. REPAIRED WIRING CONNECTION PER MM. 2 L 7 2 4F RT A16WE 2001031400149 20010314 00149 NM 2001 3 14 SWAA010372 1 20010205 A 3397 079123 WIRE BOEING 737 7373H4 1384600 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 656SW 28401 EEPLS WIRING EXPOSED AT ROW 2. SECURED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001031400150 20010314 00150 NM 2001 3 14 SWAA010373 1 20010206 A 5310 6547978 CREASE BEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM INBOARD CHORD CORRODED AT BS 915 TO BS 1006, RBL 44 TO RBL 60. REPAIRED CREASE BEAM PER SRM. 2 L 7 2 4F A16WE 2001031400151 20010314 00151 NM 2001 3 14 SWAA010374 1 20010206 A 5315 6546804 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 947, RBL 43 TO RBL 47. REPAIRED FLOORBEAM PER BFG ER. 2 L 7 2 4F A16WE 2001031400152 20010314 00152 2001 3 14 SWAA010375 4 20010206 A 2565 22D22901151 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR TORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY TORN AT FWD END. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001031400153 20010314 00153 NM 2001 3 14 SWAA010376 1 20010206 A 3350 BR2013 LIGHT BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED C3 CHECK, FOUND EEPLS LOOSE AT FWD SECTION. SECURED EEPLS PER MM. 2 L 7 2 4F A16WE 2001031400154 20010314 00154 NM 2001 3 14 SWAA010377 1 20010206 A 5330 6545778 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED C3 CHECK, FOUND 2.75 EXTERNAL FUSELAGE SKIN CRACK BETWEEN BS 930 & BS 936, STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001031400155 20010314 00155 2001 3 14 SWAA010378 4 20010206 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001031400156 20010314 00156 NM 2001 3 14 SWAA010379 1 20010207 A 5312 6517582 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT LBL 17.1, WL 229. REPAIRED VERTICAL BEA M WEB PER BFG ER. 2 L 7 2 4F RT A16WE 2001031400157 20010314 00157 NM 2001 3 14 SWAA010380 1 20010206 A 5753 6546435 FLAP BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED 1/4D CHECK, FOUND RT WING T/E INBOARD AFT FLAP CRACKED AND DELAMINATED ON OUTBOARD END. REPAIRED AFT F LAP PER BAC DWG & SRM. 2 L 7 2 4F RT A16WE 2001031400158 20010314 00158 NM 2001 3 14 SWAA010381 1 20010206 A 5310 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIES CORRODED BETWEEN STR 26R & STR 27R, BS 727C, RBL 10, BS 727D, RBL 8 & BS 7 47 RBL 12. REPAIRED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 2001031400159 20010314 00159 2001 3 14 SWAA010382 4 20010207 A 2565 61620468 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF TOLERANCE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 618WN 28034 DURING SCHEDULED A1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS OUT OF LIMITS. REMOVED AND REPLACED EVAC SLI DE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001031400160 20010314 00160 NM 2001 3 14 SWAA010383 1 20010206 A 5330 6545775 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED 1/2D CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 870, STR 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001031400161 20010314 00161 2001 3 14 SWAA010384 4 20010207 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASS Y PER MM. 2 L 7 2 4F RT A16WE 2001031400162 20010314 00162 NM 2001 3 14 SWAA010385 1 20010206 A 5311 6546529 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500, RBL 1. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001031400163 20010314 00163 NM 2001 3 14 SWAA010386 1 20010206 A 5312 6516300 BULKHEAD BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED 1/2D CHECK, FOUND 2 BS 178 BULKHEAD WEB CRACKS AT WL 187.5, LBL 1 & RBL 1. REPAIRED BULKHEAD WEB PER S RM. 2 L 7 2 4F RT A16WE 2001031400164 20010314 00164 NM 2001 3 14 SWAA010387 1 20010207 A 5320 6545819 BEAM BOEING 737 737301 1384611 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED 1/2D CHECK, FOUND 2.5 CRACK AT NLG ACTUATOR SUPPORT WEB, BS 232, BL 0, WL 184. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001031400165 20010314 00165 NM 2001 3 14 SWAA010388 1 20010207 A 5310 6546529 SHEAR TIE BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CORRODED AT BS 360. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2001031400167 20010314 00167 NM 2001 3 14 UPS01434690 1 20010107 A 5340 65B0834410 FITTING BOEING 747 747123F NM NR 3 ENTRY DR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, NR 3 ENTRY DOOR RT SIDE HINGE FITTING FOUND CRACKED AT BS 1265. FITTING REPLACED IAW SRM 51-30-02. 2 L 7 4 4F A20WE 2001031400168 20010314 00168 NM 2001 3 14 UPS01434706 1 20010101 A 5315 AC1505101050 FLOORBEAM BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, MAIN DECK CABIN CORROSION ON UPPER CHORD OF FLOORBEAM AT BS 1720 LBL 85-98. UPPER CHORD AT BS 1720 LBL 85-98 REPAIRED IAW QUERY NOTE 9/01 SPLICED IN A NEW SECTION OF UPPER CHORD FLOORBEAM PER SRM 51-40-04. 2 L 7 4 4F A20WE 2001031400169 20010314 00169 NM 2001 3 14 UPS01434707 1 20010112 A 5320 65B1009886 SUPPORT BRACKET BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, FRAME SUPPORT STA 987 LT LOWER WING TO BODY SUPPORT FRAME HAS CORROSION. WING TO BODY FRAME REPAIRED IAW QUERY NOTE 15/91 AND SRM 51-40-04 FIG 1. INSTALLED REPAIR SECTION. 2 L 7 4 4F A20WE 2001031400170 20010314 00170 NM 2001 3 14 UPS01434708 1 20010112 A 5347 BAC15201566 SEAT TRACK BOEING 747 747123F NM CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, MAIN DECK CORROSION ON SEAT TRACK INNER FLANGE BS 1765, 1785 AND 1820 LBL 76 REPAIR REQUIRED. REPAIR ED IAW SRM 53-10-05. 2 L 7 4 4F A20WE 2001031400171 20010314 00171 NM 2001 3 14 UPS01434710 1 20010105 A 5311 FRAME BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, MAIN DECK CABIN FRAME WEB IS CRACKED AT CUTOUT FOR STR AT BS 920 STR 24 LT FOR REPAIR. FRAME WEB R EPAIR CARRIED OUT IAW SRM 53-10-04. 2 L 7 4 4F A20WE 2001031400172 20010314 00172 NM 2001 3 14 UPS01434714 1 20010112 A 5312 BULKHEAD BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, MAIN DECK CANTED PRESSURE BULKHEAD WEB IS CRACKED UNDER LWR CREASE BEAM WEB STR 26 LT BS 260 (CPCP T ASK C53-210-07-1B ). CANTED PRESSURE BULKHEAD REPAIRED, WEB REPAIR IAW QUERY NOTE 19/01. 2 L 7 4 4F A20WE 2001031400173 20010314 00173 NM 2001 3 14 UPS01434715 1 20010109 A 5312 BAC15062032 BULKHEAD BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, CABIN MAIN DECK CORROSION ON UPPER CHORD OF CANTED PRESS BULKHEAD AT BS 260 RBL 35-48. UPPER CHORD REPAIRED IAW QUERY NOTE 17/01 AND SRM 53-10-04. 2 L 7 4 4F A20WE 2001031400174 20010314 00174 NM 2001 3 14 UPS01434716 1 20010111 A 5347 BAC15201567 SEAT TRACK BOEING 747 747123F NM CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, MAIN CABIN UPPER DECK FLOOR SEAT TRACK AT BS 540 - 670 LBL 66 CORRODED. CORRODED SECTION OF SEAT TRA CK REMOVED AND NEW SECTION FITTED IAW SRM 51-40-02. 2 L 7 4 4F A20WE 2001031400175 20010314 00175 NM 2001 3 14 UPS01434717 1 20010111 A 5347 SEAT TRACK BOEING 747 747123F NM CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, UPPER DECK SEAT TRACK BS 600 - 630 LBL 47 CORRODED. CORRODED SECTION REMOVED AND NEW SECTION FITTED IAW SRM 51-40-02. 2 L 7 4 4F A20WE 2001031400176 20010314 00176 NM 2001 3 14 UPS01434718 1 20010109 A 5320 WEB BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, MAIN DECK FLOOR INTERCOSTAL WEB IS CRACKED AND UPPER CHORD DAMAGED AT BS 500 - 520 LBL 60. NEW WEB A ND UPPER CHORD FABRICATED IAW SRM 51-30-02. 2 L 7 4 4F A20WE 2001031400177 20010314 00177 NM 2001 3 14 UPS01434719 1 20010108 A 5310 SHEAR TIE BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, MAIN DECK SHEAR TIE CRACKED AT BS 1295 BETWEEN STRS 14 AND 15 LT. SHEAR TIE FABRICATED IAW EO 206671 AND INSTALLED IAW SRM 51-30-02. 2 L 7 4 4F A20WE 2001031400178 20010314 00178 NM 2001 3 14 UPS01434720 1 20010111 A 5310 BAC1505100849 CREASE BEAM BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, CABIN MAIN DECK INNER T-CHORD OF LOWER CREASE BEAM WEB IS CRACKED STR 26 AT BS 1241 LT SIDE. DAMAGED T-CHORD REMOVED AND NEW SECTION FITTED IAW SRM 51-30-02. 2 L 7 4 4F A20WE 2001031400179 20010314 00179 NM 2001 3 14 UPS01434721 1 20010110 A 5347 BAC15201566 SEAT TRACK BOEING 747 747123F NM CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, MAIN DECK CORROSION ON SEAT TRACK AT BS 1660 - 1680 RBL 34. SEAT TRACK REPLACED AT BS 1660 - 1680 RB L 34 REPLACED IAW SRM 53-10-05. 2 L 7 4 4F A20WE 2001031400180 20010314 00180 NM 2001 3 14 UPS01434724 1 20010108 A 5312 BULKHEAD BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, MAIN DECK CORROSION ON UPPER CHORD BS 400 BULKHEAD RBL 15 TO 46. UPPER CHORD AT BS 400 RBL 15 - 4 6 REPAIRED IAW QUERY NOTE 6/01. 2 L 7 4 4F A20WE 2001031400181 20010314 00181 NM 2001 3 14 UPS01434725 1 20010110 A 5320 BRACKET BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, MAIN DECK FLOOR INTERCOSTAL IS CRACKED AT BS 440 - 460 RBL 60 AND ATTACH BRACKET TO FLOOR WEB IS CRA CKED AT BS 440. INTERCOSTAL RE-WORKED AND NEW BRACKETS FITTED IAW SRM 51-30-02. 2 L 7 4 4F A20WE 2001031400182 20010314 00182 NM 2001 3 14 UPS01434742 1 20010102 A 5314 BRACKET BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, KEEL BEAM CORROSION ON FAIRING SUPPORT BEAM AT BS 1000 BBL .0. BRACKET REPAIRED IAW SRM 51-20-01 AND SRM 51-30-02. 2 L 7 4 4F A20WE 2001031400183 20010314 00183 WP 2001 3 14 UPS01835018 1 20010220 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP ON PRE-DEPARTURE CHECK. REPLACED BATTERY PACK. 2 L 7 4 4F RT 4A25 2001031400185 20010314 00185 WP 2001 3 14 0100471223 1 20010104 A 5311 FRAME DOUG DC10 DC1030 3023501 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 223NW 46580 DURING H-CHECK, FOUND CRACK IN LOWER NOSE FUSELAGE FRAME AT BS 459 X58L AND X61L, CRACKS BEGIN AT EDGE OF FRAME AND TERM INATE AT LIGHTENING HOLES. REPAIRED PER EA 12-181414. 2 L 7 3 4F A22WE 2001031400186 20010314 00186 WP 2001 3 14 0100481149 1 20010118 A 5320 STIFFENER DOUG DC10 DC1040 3023508 WP BULKHEAD CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 149US 46758 DURING L-CHECK, FOUND CORROSION ON THE LOWER END OF VERTICAL STIFFENER UNDER WING FUEL TANK FORWARD PRESSURE BULKHEAD AT BS 1156 L45L-L45R. REPAIRED PER EA 11-180793. 2 L 7 3 4F A22WE 2001031400187 20010314 00187 WP 2001 3 14 0100491223 1 20010109 A 5310 DOOR FRAME DOUG DC10 DC1030 3023501 WP MID CARGO BAY CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 223NW 46580 DURING H-CHECK, FOUND CORROSION ON THE CENTER CARGO DOOR JAMB FRAME AT BS 1781 L41R AND 42R. REPAIRED PER EA 12-178406. 2 L 7 3 4F A22WE 2001031400188 20010314 00188 WP 2001 3 14 0100501223 1 20010104 A 5730 SKIN DOUG DC10 DC1030 3023501 WP RT WING CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 223NW 46580 DURING H-CHECK, FOUND CORROSION ON THE RIGHT UPPER WING SKIN AT REAR SPAR BETWEEN XORS 770-775. REPAIRED PER EA 12-1816 26. 2 L 7 3 4F A22WE 2001031400189 20010314 00189 WP 2001 3 14 0100511223 1 20010103 A 5311 FRAME DOUG DC10 DC1030 3023501 WP RT MLG WW CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 223NW 46580 DURING H-CHECK, FOUND CRACK IN THE RT MAIN LANDING GEAR WHEEL WELL FRAME AT BS 1505. REPAIRED PER EA 12-181629. 2 L 7 3 4F A22WE 2001031400190 20010314 00190 WP 2001 3 14 MWEA010164 1 20010219 A 5310 99155871 BELT DOUG DC9 DC932 3022066 WP WINDOW CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 NR 20 LEFT WINDOW FRAME CORRODED IN BOTH LOWER, INNER CORNERS. REMOVED AND REPLACED WINDOW BELT. 2 L 7 2 4F A6WE 2001031400191 20010314 00191 WP 2001 3 14 MWEA010165 1 20010219 A 5330 591142379 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 AFT CARGO BAG FUSELAGE SKIN HAS MECHANICAL DAMAGE FROM STATION 876 - STATION 890 BETWEEN LONGERON 23 THRU LONGERON 22 LE FT. FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLERS. 2 L 7 2 4F A6WE 2001031400192 20010314 00192 WP 2001 3 14 MWEA010166 1 20010219 A 5542 99574853 SKIN DOUG DC9 DC932 3022066 WP RUDDER DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 RUDDER LEFT SKIN HAS .75 INCH BY .75 INCH DENT .010 INCH DEEP AT ZR 28.936. REMOVED AND REPLACED DOUBLER. 2 L 7 2 4F A6WE 2001031400193 20010314 00193 WP 2001 3 14 MWEA010167 1 20010216 A 3010 39271411 REGULATOR VALVE DOUG DC9 DC932 3022066 WP AC BAY STUCK A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 302ME 47102 DURING CLIMBOUT FROM MILWAUKEE, AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT CAME ON. AIRCRAFT RETURNED TO MILWAUKEE. MAINTENANCE REMOVED AND REPLACED THE RIGHT PRESSURE REGULATOR VALVE FOR STICKING OPEN. 2 L 7 2 4F A6WE 2001031400194 20010314 00194 WP 2001 3 14 MWEA010168 1 20010218 A 5320 3913575501 INTERCOSTAL DOUG DC9 DC914 3022034 WP AFT CARGO BAY CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 AFT CARGO COMPARTMENT, UPPER CENTER LINE INTERCOSTAL CRACKED AT FORWARD LIGHTENING HOLE. STOP DRILLED CRACK. FABRICATE D AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001031400195 20010314 00195 EU 2001 3 14 C2XA01IA092 1 20010217 A 6123 30005000025 TSCU AEROSP ATR42 ATR42320 8680930 EU HAMSTD 14RF 14RF9 NE NR2 ENGINE INOPERATIVE A C2XA K NONE O OTHER CR CRUISE 1 SW 27 14828 179 DAY - FLIGHT 3229, THE CREW REPORTED THAT THE NUMBER TWO PROPELLER WENT INTO FEATHER UNCOMMANDED. THE AIRCRAFT LANDED A T DAY WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO TORQUE SIGNAL CONDITIONER UNIT (TSCU), AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 6 C P11NE 2001031400196 20010314 00196 GL 2001 3 14 C2XA01IA093 2 20010214 A 7200 23065323 BLADE ALLSN EMB 145 EMB145ER SO ALLSN AE300 AE3007A GL NR2 ENGINE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14943 CAE311561 145040 CAE311561 IAH - DURING C-CHECK INSPECTION, THE NUMBER TWO ENGINE WAS FOUND TO HAVE A CRACKED FAN BLADE. MAINTENANCE REMOVED AND R EPLACED THE AFFECTED BLADE IN ACCORDANCE WITH ROLLS ROYCE AE3007A-M/M 72-21-15-300-801, AND THE AIRCRAFT WAS APPROVED FO R RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001031400197 20010314 00197 NM 2001 3 14 CALA0100139 1 20010218 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND SEAT TRACK CORRODED AT STA 900 - 947, LBL 45, LBL 25, AND RBL 25. THE CORRODED SECTIONS OF SEAT TRACK WERE REMOVED AND REPAIR SECTIONS WERE INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001031400198 20010314 00198 2001 3 14 AWXA0001373 4 20010219 A 3460 B398BCM0108 FMC AIRBUS 320 A320231 3930325 EU COCKPIT FAILED A AWXA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 28 646AW 2505 34 271 PHX - DIVERTED FLIGHT - 2/14/01 - AFTER TAKEOFF FROM LAS TO BOS THE MCDU FROZE IN THE FLIGHT PLAN MODE; RNAV UNAVAILABLE ; THE FLIGHT WAS DIVERTED TO PHX. IN PHX MAINTENANCE REPLACED THE LEFT AND RIGHT FMGC; AFTER REPLACEMENT, CURRENT NAV D ATA WAS UPLOADED AND BITE CHECKS WERE GOOD. FMGC - SEXTANT, (P/N B398BCM0108), (S/N 1798), POS RIGHT, CONDITION UNRELIA BLE, TT 16964, TC 8177, TSR 1244. 2 L 7 2 4F RT A28NM 2001031400199 20010314 00199 EU 2001 3 14 AWXA0001374 1 20010219 A 2782 830A000002 ACTUATOR AIRBUS 320 A320231 3930325 EU LT & RT WING CONTAMINATED A AWXA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 WP 28 645AW 28440 238 PHX - EMERGENCY LANDING - 2/12/01 - ON APPROACH, THE CREW GOT AN ECAM WARNING, F/CTL SLATS FAULT AND THE CREW DECLARED A N EMERGENCY; AN UNEVENTFUL LANDING WAS MADE IN PHX. MAINTENANCE TROUBLESHOT AND FOUND 1 LT AND 2 RT LEADING EDGE SLAT R OTARY ACTUATORS WITH WATER CONTAMINATION IN THEM. ALSO FOUND THE LEFT APPU/FPPU DATA READING OUT OF LIMITS AT 0 DEGREE FLAPS. REPLACED THE 3 CONTAMINATED LEADING EDGE SLAT ROTARY ACTUATORS AND REMOVED THE LT AND RT APPU''S AND ADJUSTED IA W AMM TASK 27-81-18-991-001. ALL FUNCTIONAL CHECKS GOOD WITH NO FURTHER PROBLEMS REPORTED. SLAT ROTARY ACT - LIEBHERR, (P/N 830A0000-02), (S/N 4062/4386), LOC 6083/6091 CM, CONTAMINATED, TT 28440, TC 13019. 2 L 7 2 4F RT A28NM 2001031400200 20010314 00200 NE 2001 3 14 AWXA0001375 2 20010219 A 7532 10746012 VALVE BOEING 757 7572G7 1384963 NM RROYCE RB211 RB211535* NE NR1 ENGINE FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 909AW 2742 22 24522 30570 BWI - AIR TURNBACK - 2/10/01 - ON TAKEOFF THE NR 1 ENGINE HIGH STAGE LIGHT ILLUMINATED. DURING CLIMB THE AIRCRAFT WAS U NABLE TO MAINTAIN CABIN PRESSURIZATION IN AUTO AND THE CREW SWITCHED TO MANUAL AND CONTROL OF PRESSURIZATION WAS ESTABLI SHED AT 10000 FT CABIN ALTITUDE. THE AIRCRAFT RETURNED TO BWI MAKING AN UNEVENTFUL OVERWEIGHT LANDING. MAINTENANCE REP LACED THE HIGH STAGE VALVE AND FOUND A FOREWARD CARGO COMPARTMENT NET STRAP CAUGHT IN THE DOOR. AN ENGINE RUN AND PRESS URIZATION TEST WAS PERFORMED; ALL CHECKS WERE GOOD. AN OVERWEIGHT LANDING INSPECTION WAS PERFORMED AND NO DISCREPANCIES NOTED. 2 L 7 2 4F 4 F RT A2NM E12EU 2001031400201 20010314 00201 NM 2001 3 14 AWXA0001396 1 20010220 A 5512 6547532539 CAP BOEING 737 7373G7 1384595 NM HORIZONTAL STAB CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 LT HORIZ L/E SKIN FOUND CRACKED RIB END CAP AT APPROX STA 58. REMOVED CRACKED END CAP IAW SRM 51-40-02; DRILLED AND INS TALLED REPLACEMENT END CAP IAW SRM 51-40-02; OG DMG MEASURED 0.5 INCH LONG. 2 L 7 2 4F RT A16WE 2001031400202 20010314 00202 EU 2001 3 14 AWXA0001395 1 20010220 A 5347 D53112092 SEAT TRACK AIRBUS 320 A320231 3930325 EU CABIN CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 NR 3 SEAT TRACK AT FR 20 CORRODED, -Y765-Z500. FABED SEAT TRACK IAW DWG D53112092; INSTALLED IAW SRM 53-11-14. 2 L 7 2 4F RT A28NM 2001031400203 20010314 00203 EU 2001 3 14 AWXA0001394 1 20010220 A 5347 D53112092 SEAT TRACK AIRBUS 320 A320231 3930325 EU CABIN CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 NR 4 SEAT TRACK AT FR 20 CORRODED, -0Y1292 -Z500. FABED SEAT TRACK IAW DWG D53112092; INSTALLED IAW SRM 53-11-14. 2 L 7 2 4F RT A28NM 2001031400204 20010314 00204 NM 2001 3 14 AWXA0001393 1 20010220 A 5342 69702514 BOLT BOEING 737 7373G7 1384595 NM VERTICAL STAB CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 RIGHT O/B AFT VERT STAB ATTACH BOLT CORRODED AND REQUIRED REPLACEMENT STA 1088 WL 301.11. BOLT REPLACED ON C-12 CHECK I AW AWA W/C 1GB55002. 2 L 7 2 4F RT A16WE 2001031400205 20010314 00205 NM 2001 3 14 AWXA0001392 1 20010220 A 5320 69366564 ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 SUPPORT ANGLE ATTACHED TO INTERCOSTAL WEB CRACKED AT BL 0 FROM BS 927-947 IN AFT CABIN FLOOR AREA. REPLACED SUPPORT ANG LE IAW DWG 69-36656-4 AND SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001031400206 20010314 00206 NM 2001 3 14 AWXA0001391 1 20010220 A 5753 113N26053 ATTACH ANGLE BOEING 757 7572G7 1384963 NM LT FLAP CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 24233 ATTACH ANGLE CRACKED ON LT WING I/B MID FLAP O/B END. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2001031400207 20010314 00207 NM 2001 3 14 AWXA0001390 1 20010220 A 5412 BULKHEAD BOEING 757 7572G7 1384963 NM NR1 PYLON CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 24233 NR 1 PYLON NSA 290 AFT ELECTRICAL SUPPORT BULKHEAD CRACKED. REMOVED, FABED, AND INSTALLED REPAIR ANGLE IAW SRM 51-40-02 AND 51-30-01 FIG 7. 2 L 7 2 4F RT A2NM 2001031400208 20010314 00208 NM 2001 3 14 AWXA0001389 1 20010220 A 5320 141N5115 FLOOR SUPPORT BOEING 757 7572G7 1384963 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 24233 CABIN FLOOR SUPPORT AT STA 365 BL 0 HAS CORROSION. REMOVED CORROSION; OG MAT .071, MAT LOSS .040 - OUT OF LIMITS. REMO VED AND REPLACED FLOOR SUPPORT IAW 51-40-05, 51-10-02, 51-40-02. 2 L 7 2 4F RT A2NM 2001031400209 20010314 00209 NM 2001 3 14 AWXA0001388 1 20010220 A 2540 2A114004121 FITTING BOEING 757 7572G7 1384963 NM LT AFT LAV CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 24233 LT AFT LAV AFT RETAINER BRACKET HAS CORROSION AND BLUE WATER STAIN. REPLACED LAV AFT RETAINER BRACKET IAW MM 25-41-03. 2 L 7 2 4F RT A2NM 2001031400210 20010314 00210 NM 2001 3 14 AWXA0001387 1 20010220 A 5320 143N5140 INTERCOSTAL BOEING 757 7572G7 1384963 NM FWD CARGO BAY CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 24233 FWD CARGO PIT FLOOR STRUCTURE AT STA 690 LBL 3 INTERCOSTAL CRACKED. REMOVED, FABED AND INSTALLED FLOOR SUPPORT INTERCOS TAL IAW SRM 53-30-53 FIG 1 AND SRM 51-40-02. 2 L 7 2 4F RT A2NM 2001031400211 20010314 00211 NM 2001 3 14 AWXA0001386 1 20010220 A 5320 143N514010 ATTACH ANGLE BOEING 757 7572G7 1384963 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 24233 INTERCOSTAL ATTACH ANGLE FOUND CRACKED AT FS 660 AFT SIDE OF FLOORBEAM AT RBL 45.5. REMOVED CRACKED ANGLE; FABED NEW AN GLE IAW SRM 51-30-01 FIG 7 AND INSTALLED NEW ANGLE IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2001031400212 20010314 00212 NM 2001 3 14 AWXA0001385 1 20010220 A 5315 143N51974 FLOORBEAM BOEING 757 7572G7 1384963 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 24233 FWD CARGO PIT STA 680 RBL 20 INTERCOSTAL IS CRACKED AT ITS UPPER CHORD (UPPER FLOORBEAM). REMOVED, FABED AND INSTALLED INTERCOSTAL REPAIR ANGLE IAW SRM 51-30-01 AND ENGINEERING SUPPORT; TREATED AND PRIMED IAW SRM 51-20-01. 2 L 7 2 4F RT A2NM 2001031400213 20010314 00213 NM 2001 3 14 AWXA0001384 1 20010220 A 5320 146N5821 FLOOR SUPPORT BOEING 757 7572G7 1384963 NM AFT CARGO BAY CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 24233 RT LAV FLOOR VERT SUPPORT CRACKED, AFT CARGO BAY STA 1320 RBL 46. REMOVED AND REPLACED RT LAV FLOOR VERT SUPPORT IN AFT CARGO BAY IAW SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A2NM 2001031400214 20010314 00214 NM 2001 3 14 AWXA0001383 1 20010220 A 5320 146N5416 FLOOR SUPPORT BOEING 757 7572G7 1384963 NM AFT CARGO BAY BENT A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 24233 AFT CARGO STA 1320 RBL 20 FLOORBOARD SUPPORT IS BENT. REMOVED DAMAGED SECTION OF FLOORBOARD SUPPORT; FABED SPLICE AND F LOOR SUPPORTS INSTALLED IAW SRM 51-70-12. 2 L 7 2 4F RT A2NM 2001031400215 20010314 00215 NM 2001 3 14 AWXA0001382 1 20010220 A 5340 146N102115 BRACKET BOEING 757 7572G7 1384963 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 24233 LT FUSELAGE UNDER WING TO BODY FAIRING FWD OF EMERGENCY EXIT HAS CRACKED ATTACH BRACKET. FABED REPAIR ANGLE, REMOVED DA MAGED ANGLE AND INSTALLED REPAIR ANGLE IAW SRM 51-40-02 AND 51-70-11. 2 L 7 2 4F RT A2NM 2001031400216 20010314 00216 NM 2001 3 14 AWXA0001381 1 20010220 A 5310 146N102115 SHEAR TIE BOEING 757 7572G7 1384963 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 24233 AFT CARGO COMPARTMENT STA 1300 LEFT SIDE BETWEEN STR 20L AND 21L SHEAR TIE ANGLE CRACKED. REMOVED CRACKED ANGLE, FABED REPAIR ANGLE AND INSTALLED REPAIR ANGLE IAW SRM 51-40-02, 51-30-02 AND 51-30-01. 2 L 7 2 4F RT A2NM 2001031400217 20010314 00217 NM 2001 3 14 AWXA0001380 1 20010220 A 5315 143N5140 FLOORBEAM BOEING 757 7572G7 1384963 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 24233 FWD CARGO PIT UPPER FLOORBEAM INTERCOSTAL IS CRACKED AT STA 780-800 BL 0. REMOVED, FABED AND REPLACED UPPER INTERCOSTAL ANGLE IAW SRM 53-30-51, 51-40-02, 51-20-05. 2 L 7 2 4F RT A2NM 2001031400218 20010314 00218 NM 2001 3 14 AWXA0001379 1 20010220 A 5315 143N5140 FLOORBEAM BOEING 757 7572G7 1384963 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 24233 FWD CARGO PIT STA 660 BL 0, UPPER FLOORBEAM INTERCOSTAL IS CRACKED. REMOVED, FABED AND REPLACED ANGLE IAW SRM 53-30-51, 51-30-01 FIG 7, 51-40-02. 2 L 7 2 4F RT A2NM 2001031400219 20010314 00219 NM 2001 3 14 AWXA0001378 1 20010220 A 5247 148N66014 SKIN BOEING 757 7572G7 1384963 NM APU DOOR PUNCTURED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 24233 APU ACCESS DOOR HAS .5 INCH PUNCTURE IN SKIN. STOP DRILLED CRACK, FABED AND INSTALLED REPAIR DOUBLER IAW SRM 52-40-01. 2 L 7 2 4F RT A2NM 2001031400220 20010314 00220 NM 2001 3 14 AWXA0001377 1 20010220 A 5320 146N5821 BRACKET BOEING 757 7572G7 1384963 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 24233 LT LAV FLOOR SUPPORT INTERCOSTAL, AFT SUPPORT BRACKET CRACKED, AFT CARGO BAY STA 1300 LBL 46. REMOVED INTERCOSTAL IAW S RM 51-40-02, FABED INTERCOSTAL SUPPORT BRACKET AND INSTALLED SUPPORT BRACKET IAW SRM 51-40-02 AND SRM 51-30-01. 2 L 7 2 4F RT A2NM 2001031400221 20010314 00221 NM 2001 3 14 AWXA0001376 1 20010220 A 5315 146N5821 FLOORBEAM BOEING 757 7572G7 1384963 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 24233 FWD CARGO PIT UPPER FLOORBEAM STA 560 RBL 0 INTERCOSTAL CRACKED. REMOVED, FABED AND INSTALLED ANGLE IAW SRM 53-30-51, 5 1-30-02, AND 51-40-02. 2 L 7 2 4F RT A2NM 2001031400222 20010314 00222 SO 2001 3 14 C2XA01IA097 1 20010112 A 5320 12019264001 BEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12715 120125 MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED FROM FRAME 38 TO FRAME 40. MAINTENANCE PERFORMED A SPLICE REPAIR TO THE AFFECTED SECTION OF OMEGA BEAM IN ACCORDANCE WITH CONTINENTAL EX PRESS ENGINEERING CHANGE EC5310-01163 REV-B, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001031400223 20010314 00223 SO 2001 3 14 C2XA01IA098 1 20010112 A 5320 12046162001 BEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12715 120125 MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE RIGHT HAND OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 3 8 AND 40. MAINTENANCE PERFORMED A SPLICE REPAIR IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHANGE EC5310-01163 REV-B, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001031400224 20010314 00224 SO 2001 3 14 C2XA01IA099 1 20010119 A 5315 12046162001 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12715 120125 MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE RIGHT HAND FLOORBEAM WAS FOUND TO BE CRACKED AT FRAME 38. MAIN TENANCE PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH EMB120 SRM 51-70-05, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO S ERVICE. 2 L 7 2 4T RT A31SO 2001031400225 20010314 00225 SO 2001 3 14 C2XA01IA101 1 20010108 A 7130 12027129501 RETAINER EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12715 120125 MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION THE LEFT HAND NACELLE FIRE SEAL RETAINER WAS FOUND TO BE CRACKED. M AINTENANCE REMOVED AND REPLACED THE AFFECTED RETAINER IN ACCORDANCE WITH EMB120 SRM 51-25-00, AND THE AIRCRAFT WAS APPRO VED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001031400226 20010314 00226 SO 2001 3 14 C2XA01IA102 1 20010108 A 7130 12027129501 RETAINER EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12715 120125 MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE RIGHT HAND NACELL FIRE SEAL RETAINER WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RETAINER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001031400227 20010314 00227 SO 2001 3 14 C2XA01IA094 1 20010109 A 5320 12019264001 BEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12715 120125 MYR - DURING CONTINENTAL EXPRESS C-CHECK, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND LIMITS BETWEEN FRAMES 37 AND 39. MAINTENANCE REMOVED AND REPLACED THE AFFECTED OMEGA BEAM IN ACCORDANCE WITH EMB120 SRM 51-40-02, AND THE AIRCR AFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001031400228 20010314 00228 SO 2001 3 14 C2XA01IA1095 1 20010109 A 5320 12005779001 INTERCOSTAL EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12715 120125 MYR - DURING CONTINENTAL EXPRESS C-CHECK, THE RIGHT HAND T-SECTION AT FRAME 40 WAS FOUND TO BE CORRODED. MAINTENANCE RE MOVED AND REPLACED THE AFFECTED T-SECTION IN ACCORDANCE WITH EMB120 SRM 51-20-10, AND THE AIRCRAFT WAS APPROVED FOR RETU RN TO SERVICE. 2 L 7 2 4T RT A31SO 2001031400229 20010314 00229 SO 2001 3 14 C2XA01IA096 1 20010109 A 5320 12027929001 STRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12715 120125 MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE CENTER BUTT STRAP WAS FOUND TO BE CORRODED FROM STATION 11430 T O 13255. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IN ACCORDANCE WITH EMB120 SRM 51-40-02, AN D THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001031400230 20010314 00230 WP 2001 3 14 ABXA010055 1 20010220 A 5753 992344529 MOUNT DOUG DC9 DC941 302207N WP RT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 RIGHT FLAP CARRIAGE MOUNT ANGLE WAS CORRODED. MAINTENANCE INSPECTED AND MANUFACTURED NEW FLAP MOUNT ANGLE PER DOUGLAS D RAWING 9923445 AND INSTALLED IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2001031400231 20010314 00231 WP 2001 3 14 ANCF0329351 1 20010220 A 7714 LINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE LT ENGINE DISCONNECTED W ANCF A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 SO 23 190AN 53190 P726811D DURING CRUISE LT ENGINE N2 STARTED TO DECREASE UNTIL REACHING 36 PERCENT (OSCILLATING BETWEEN 32 AND 40 PERCENT), THERE IS MORE THAN ONE KNOB SPLIT BETWEEN ENGINES TO KEEP SAME EPR. FLIGHT DIVERTED TO PTY. MOISTURE TRAP WAS CHECK FOR COND ITION AND BURNER PRESSURE. LT ENGINE INLET/OUTLET AND PT2 LINE WERE CHECK. EPR TRANSMITTER WAS SWAPPED. LT ENGINE TAC HOMETER B-ELECTRICAL LINE WAS FOUND DISCONNECTED. REPAIRED IAW AMM 77-12-00 P 201. RUN UP TEST OK. 2 L 7 2 4F 4 F RT A6WE E9NE 2001031400232 20010314 00232 NE 2001 3 14 AWXA0001409 2 20010222 A 7230 15720090009 BLADE BOEING 737 7372U9 1384498 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE DAMAGED A AWXA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 28 149AW 22575 P708371B SAT - ABORTED TAKEOFF - 2/16/01 - ON TAKEOFF ROLL THE AIRCRAFT EXPERIENCED A COMPRESSOR STALL; THE TAKEOFF WAS ABORTED U NDER 60 KTS, THE CREW WAS NOT ABLE TO DETERMINE WHICH ENGINE STALLED, SO BOTH ENGINES WERE INSPECTED. NO DEFECTS WERE F OUND ON NR 2 ENGINE; NR 1 ENGINE HAD 6TH STAGE COMPRESSOR BLADE DMG BEYOND LIMITS AND WAS REPLACED. 2 L 7 2 4F 4 F RT A16WE E2EA 2001031400233 20010314 00233 EU 2001 3 14 A6WA200100015 1 20010210 A 2120 UNKNOWN BAG BAE146 BAE146200A 1500266 EU CABIN ODOR A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 31 290UE E2080 FLIGHT ATTENDANT REPORTED LIGHT SMOKE ODOR COMING FROM SEAT 18 D&F AREA INFLIGHT. MAINTENANCE INSPECTED SEAT AREA, NO O DOR NOTED. NO ODOR NOTED FROM AIR CONDITIONING PACKS AS WELL. 2 H 7 4 4F RT A49EU 2001031400234 20010314 00234 WP 2001 3 14 ABXA010056 1 20010220 A 5330 SKIN DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 FUSELAGE SKIN LOCATED AT STA 61 LONGERON 19R WAS CRACKED. MAINTENANCE INSPECTED AND REPAIRED THE CRACK IAW DC-9 SRM 53- 01 FIG 2. 2 L 7 2 4F A6WE 2001031400235 20010314 00235 WP 2001 3 14 ABXA010057 1 20010220 A 5751 5910045501 AILERON DOUG DC9 DC941 302207N WP LT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 LEFT AILERON WAS CORRODED. MAINTENANCE INSPECTED AND REPLACED THE AILERON IAW DC-9 MAINTENANCE MANUAL. 2 L 7 2 4F A6WE 2001031400236 20010314 00236 WP 2001 3 14 ABXA010058 1 20010220 A 5711 991707341 RIB DOUG DC9 DC941 302207N WP LT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 LEFT WING TRAILING EDGE RIB AT STATION 140 WAS CORRODED. MAINTENANCE INSPECTED AND REPAIRED THE RIB IAW ABX REA D957-40 000. 2 L 7 2 4F A6WE 2001031400237 20010314 00237 WP 2001 3 14 ABXA010059 1 20010220 A 5320 49125402N FITTING DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 FLOORBEAM TO PYLON BULKHEAD ATTACH FITTING AT APPROX RBL 44.0 WAS CRACKED. MAINTENANCE INSPECTED AND REPLACED THE ATTAC H FITTING IAW DC-9 SRM 51-30-5 AND 51-30-1. 2 L 7 2 4F A6WE 2001031400238 20010314 00238 WP 2001 3 14 ABXA010060 1 20010220 A 5320 9923406502 FITTING DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 LOWER FRAME ATTACH FITTING AT FUSELAGE STATION 677R WAS CRACKED APPROX 3 INCHES. VERIFIED WITH DYE PEN AND EDDY CURRENT INSPECTION. 2 L 7 2 4F A6WE 2001031400239 20010314 00239 WP 2001 3 14 ABXA010061 1 20010220 A 5310 591013095 DOOR FRAME DOUG DC9 DC941 302207N WP VENTRAL DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 UPPER LEFT CORNER VENTRAL DOOR JAMB WAS CRACKED AND WAS PROPAGATING FROM STOP DRILL. MAINTENANCE INSPECTED AND REPAIRED THE CRACKED AREA IAW ABX REA D953-39998-MR. 2 L 7 2 4F A6WE 2001031400240 20010314 00240 NM 2001 3 14 AWXA0001397 1 20010221 A 5320 6535362 INTERCOSTAL BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 INTERCOSTAL BENT AND CRACKED AT STA 747 - 764 STR 25R. REMOVED INTERCOSTAL IAW SRM 51-40-02; FABED INTERCOSTAL IAW SRM 53-60-15; INSTALLED INTERCOSTAL IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001031400241 20010314 00241 NM 2001 3 14 AWXA0001398 1 20010221 A 5414 311A1450 DOUBLER BOEING 737 7373S3 1384711 NM NR 2 PYLON CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 NR 2 ENGINE PYLON SKIN DOUBLER CRACKED .4 AT OUTBOARD SIDE OF PANEL 5828R ACCESS OPENING. REPAIRED IAW BOEING SERVICE B ULLETIN 737-54-1035; INSTALLED ACCESS DOOR MODIFICATION IAW ER 03-5433-01037-04. 2 L 7 2 4F RT A16WE 2001031400242 20010314 00242 NM 2001 3 14 AWXA0001399 1 20010221 A 5754 65C26600 SKIN BOEING 737 7373S3 1384711 NM NR 3 SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 LT WING NR 3 SLAT CRACKED 2.4 INCHES LONG O/B EDGE LOWER T/E SKIN. REMOVED NR 3 SLAT O/B PANEL IAW SRM 51-40-02; REMOVE D DAMAGE, INSP BY HFEC - NO CRACKS NOTED. FABED AND INSTALLED DOUBLER AND FILLER IAW SRM 51-20-05, 51-40-02 AND REINSTA LLED PANEL. 2 L 7 2 4F RT A16WE 2001031400243 20010314 00243 NM 2001 3 14 AWXA0001400 1 20010221 A 5312 65163007 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 CENTER WEB CRACKED FS 178 WL 187 LBL 0.7 AND RBL 0.7. REMOVED DAMAGE; NDT - NO CRACKS NOTED. FABED DOUBLER AND FILLER; INSTALLED DOUBLER AND FILLER IAW SRM 53-10-08. 2 L 7 2 4F RT A16WE 2001031400244 20010314 00244 NM 2001 3 14 AWXA0001401 1 20010221 A 5312 65163007 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 CENTER WEB CRACKED AT FS 178 RBL 6 WL 210. STOP DRILLED CRACK IAW SRM 53-10-08; NDT NO CRACKS NOTED. FABED AND INSTALL ED DOUBLER AND FILLER IAW SRM 53-10-08. 2 L 7 2 4F RT A16WE 2001031400245 20010314 00245 NM 2001 3 14 AWXA0001402 1 20010221 A 5312 65463007 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 CENTER WEB CRACKED AT FS 178 LBL 6 WL 212. STOP DRILLED CRACK; NDT CRACK TERMINATED. FABED AND INSTALLED DOUBLER AND 2 FILLERS IAW SRM 53-10-08. 2 L 7 2 4F RT A16WE 2001031400246 20010314 00246 NM 2001 3 14 AWXA0001403 1 20010221 A 5230 65C36231 SKIN BOEING 737 7373S3 1384711 NM AFT CARGO DOOR BENT A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 AFT CARGO DOOR FWD EDGE IS BENT FOR APPROX 18 INCHES. REMOVED, FABED AND INSTALLED FABED SKIN IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001031400247 20010314 00247 NM 2001 3 14 AWXA0001404 1 20010221 A 5414 354331038 DOUBLER BOEING 737 7373S3 1384711 NM NR1 PYLON CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 NR 1 ENGINE PYLON SKIN DOUBLER CRACKED .5 INCH AT O/B SIDE OF PANEL 5727L ACCESS OPENING. REPAIRED IAW ER 03-5433-01037 -DC1. 2 L 7 2 4F RT A16WE 2001031400248 20010314 00248 NM 2001 3 14 AWXA0001405 1 20010221 A 5330 6545775 SKIN BOEING 737 7373S3 1384711 NM AFT CARGO DOOR DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 AFT CARGO DOOR CUTOUT UPPER FWD CORNER HAS DENT (APPROX 1 X 5 INCH AND .0937 INCH DEEP). REMOVED DAMAGE; FABED AND INST ALLED 3 DOUBLER PLATES AND 1 FILLER; NDT NO CRACKS NOTED IAW B737 NTM PT 6 FIG 51-00-00, SRM 53-30-3 FIG 46. 2 L 7 2 4F RT A16WE 2001031400249 20010314 00249 NM 2001 3 14 AWXA0001406 1 20010221 A 5753 65C2630933 FORMER BOEING 737 7373S3 1384711 NM LT FLAP WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 LT WING NR3 FLAP TRACK FAIRING AFT I/B FORMER AND FORMER ANGLE WORN AT AFT END. REMOVED FORMER AND FORMER ANGLE IAW SRM 51-40-02; FABED ANGLE AND INSTALLED NEW FORMER AND ANGLE IAW DWG 65C28309-33. 2 L 7 2 4F RT A16WE 2001031400250 20010314 00250 NM 2001 3 14 AWXA0001407 1 20010221 A 5230 65C36231 SKIN BOEING 737 7373G7 1384595 NM AFT CARGO DOOR DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 AFT CARGO DOOR OUTER DOOR SKIN SURFACE HAS DENT 2.8 X 1.0 X .039 INCH LOCATED BS 826 BETWEEN STR 19R AND 20R. REMOVED, FABED AND REINSTALLED DAMAGED OUTER SKIN ON AFT CARGO DOOR IAW 52-30-01, 51-20-01, 51-40-02, 52-31-00. 2 L 7 2 4F RT A16WE 2001031400251 20010314 00251 NM 2001 3 14 AWXA0001408 1 20010221 A 5512 655482133 SKIN BOEING 737 7373G7 1384595 NM HORIZONTAL STAB DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 DENT ON HORIZ STAB, LT SIDE BETWEEN STA 56.01 AND 86.66. REMOVED DAMAGED SKIN IAW SRM 51-40-02; REMOVED O/B LEADING EDG E RIB SKIN TO GAIN ACCESS TO INSTALL FIXED LEADING DOOR SKIN IAW SRM 51-40-02; INSTALLED NEW SKIN ON FIXED LEADING EDGE IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001031400253 20010314 00253 WP 2001 3 14 ABXA010063 1 20010224 A 3350 60030451 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DIRTY A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 951AX 82163 171 47616 EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE INSPECTED AND CLEANED EMERGENCY LIGHT BATTERY PACK AT FSD AND RETURNED THE A/C TO SERVICE. UPON ARRIVAL AT ILN, MAINTENANCE REPLACED EMERGENCY LIGHT PACK AS A RELIABILITY PRECAUTION IAW DC9 MM 33-02-4. 2 L 7 2 4F A6WE 2001031400254 20010314 00254 WP 2001 3 14 ARWA1000204 1 20010225 A 2910 NAS16126 O-RING DOUG DC8 DC862 3021970 WP RT AILERON TORN A ARWA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 802BN 45909 HYDRAULIC SYSTEM LOSS DOWN TO STADPIPE, EMERGENCY CHECK, LIST C/W. RETURNED TO STATION. FOUND O-RING FROM RT AILERON A CTUATOR TUBING FITTING LEAKING. REPLACED O-RING IAW MM 20-60-0, OPS CHECK NORMAL. NO LEAKS NOTED, SYSTEM CHECK SATISFA CTORY. 2 L 7 4 4F 4A25 2001031400255 20010314 00255 NM 2001 3 14 AWXA0001410 1 20010226 A 2150 20405010 ACM BOEING 737 737277 1384570 NM AC BAY OVERSERVICED A AWXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 183AW 56122 3363 22650 PHX - AIR TURNBACK - 2/25/01 - AFTER LEVELING OFF AT FL 310, FLIGHT ATTENDANTS REPORTED A BURNING SMELL IN THE CABIN; TH E CREW STARTED A DESCENT AND TURNED OFF THE GRASPER FAN AND THE SMELL SEEMED TO GO AWAY; THE FLIGHT RETURNED TO PHX. IN PHX, MAINTENANCE FOUND OIL DRIPPINGS ON THE RT AIR CYCLE MACHINE (ACM); BOTH THE LT AND RT ACM''''S APPEARED TO BE OVER SERVICED; BOTH ACM''''S WERE DRAINED AND REFILLED; THE AIR CONDITIONING PACKS WERE RUN FOR 30 MIN AT MAX TEMPERATURE AND NO ODORS NOTED. 2 L 7 2 4F RT A16WE 2001031400256 20010314 00256 NM 2001 3 14 AWXA0001411 1 20010226 A 2741 INDICATOR BOEING 737 7373Y0 1384671 NM COCKPIT OUT OF ADJ A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 323AW 23684 D: PHX - ABORTED TAKEOFF - 2/22/01 - AT THE BEGINNING OF THE TAKEOFF ROLL THE CREW GOT A CONFIGURATION AURAL WARNING AND ABORTED THE TAKEOFF (UNDER 60 KTS); THE FLAPS WERE AT 1, SPEED BRAKE STOWED AND THE CAPT HAD SET THE STAB TRIM AT 5.2 U NITS; THE FIRST OFFICERS STAB TRIM INDICATOR WAS SHOWING 5.9 TO 6.0 UNITS. MAINTENANCE TROUBLESHOT AND ADJUSTED THE STA B TRIM INDICATORS IAW AMM 27-41-00 PG 509(7); TAKEOFF WARNING SYSTEM TESTED GOOD. 2 L 7 2 4F RT A16WE 2001031400257 20010314 00257 2001 3 14 AWXA0001412 4 20010226 A 3170 350E5500201 COMPUTER AIRBUS A319 A319132 NM COCKPIT FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 813AW 3089 1223 LAS - DIVERTED FLIGHT - 2/19/01 - WHILE IN CRUISE FLIGHT FROM PDX TO PHX THE CREW STARTED GETTING VARIOUS AND CONTINUOUS ECAM FAILURE MESSAGES TOO RAPID TO READ; NO FAULT LIGHTS ILLUMINATED ON OVERHEAD PANEL. PER MAINTENANCE CONTROL INSTRU CTIONS, THE CREW CYCLED CIRCUIT BREAKERS F1 & Q7 WITH NO HELP. THE FLIGHT WAS DIVERTED TO LAS. IN LAS MAINTENANCE REPL ACED THE NR 1 SDAC WHICH WAS BAD, (FAULTED) AND THE NR 2 SDAC TO MATCH PART NUMBER INSTALLED IN THE NR 1 POSITION; AFTER REPLACEMENTS SYSTEM OPERATION WAS NORMAL. 2 L 7 2 4F RT A28NM 2001031400258 20010314 00258 NM 2001 3 14 AWXA0001413 1 20010226 A 5230 DOOR BOEING 737 73733A 1384673 NM FWD CARGO BAY NOT CLOSED A AWXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 28 166AW 23627 PHX - ABORTED TAKEOFF - 2/19/01 - AT START OF POWER UP FOR TAKEOFF ROLL THE FWD CARGO DOOR ANNUNCIATOR LIGHT ILLUMINATED . THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO GATE. AT THE GATE A LARGE PIECE OF BAGGAGE WAS FOUND ON TOP OF THE INSIDE DOOR HANDLE NOT ALLOWING THE DOOR TO CLOSE PROPERLY. THE BAG WAS SECURED BEHIND THE BAGGAGE NET, THE DOOR CL OSED AND ALL INDICATIONS WERE NORMAL. 2 L 7 2 4F RT A16WE 2001031400259 20010314 00259 NM 2001 3 14 AWXA0001414 1 20010226 A 5320 6938929 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 STR CLIP CRACKED FUSELAGE STATION 344 STR 11R. REMOVED CLIP IAW SRM 51-40-02; FABED STR CLIP IAW DWG 69-38939; INSTALLE D CLIP IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001031400260 20010314 00260 NM 2001 3 14 AWXA0001415 1 20010226 A 5320 65528941 FLOOR SUPPORT BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 CABIN FS 540 BL 0 FLOOR SUPPORT CHANNEL IS CRACKED AT EXPANSION JOINT I/B FASTENER. REMOVED AND REPLACED FLOOR SUPPORT CHANNEL IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001031400261 20010314 00261 NM 2001 3 14 AWXA0001416 1 20010226 A 5320 6561777 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 INTERCOSTAL CRACKED AT STR 16L STA 357. STOP DRILLED, FABED AND INSTALLED DOUBLER IAW SRM 53-10-15. 2 L 7 2 4F RT A16WE 2001031400262 20010314 00262 NM 2001 3 14 AWXA0001417 1 20010226 A 5312 65163007 BULKHEAD BOEING 737 7373G7 1384595 NM FUSLEAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 CENTER WEB CRACKED FS 178 RBL 5.0 WL 198 AND WL 202. CUT OUT DAMAGED AREA, NDT - NO CRACKS NOTED. FABED DOUBLER AND 3 FILLERS IAW SRM 53-10-08; INSTALLED IAW 51-40-02; TREAT AND PRIMED IAW SRM 51-20-01. 2 L 7 2 4F RT A16WE 2001031400263 20010314 00263 NM 2001 3 14 AWXA0001418 1 20010226 A 5312 65163007 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 CENTER WEB CRACKED FS 178 WL 187 RBL 0.7 (1.0L). REMOVED DAMAGE, NDT VERIFIED CRACK TERMINATED. FABED FILLERS AND DOUB LER; TREATED AND PRIMED AND INSTALLED REPAIR PARTS IAW SRM 53-10-03, NTM PT 6 51-00-00, SRM 53-10-08 AND SRM 51-40-02 AN D SRM 51-20-01. 2 L 7 2 4F RT A16WE 2001031400264 20010314 00264 NM 2001 3 14 AWXA0001419 1 20010226 A 5320 654583340 WEB BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 FLOOR WEB CRACKED AT FS 180 WL 207 LBL 26. REMOVED DAMAGED WEB IAW SRM 51-40-02. FABED REPLACEMENT WEB IAW DWG 65-4583 3; INSTALLED REPLACEMENT WEB IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001031500185 20010315 00185 NM 2001 3 15 CALA0100140 1 20010218 A 5320 INTERCOSTAL BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73385 26314 INSPECTION FOUND A 1 INCH CRACK AT NUTPLATE HOLE IN INTERCOSTAL AT STA 927 - 947, BL 0. THE INTERCOSTAL WAS REPLACED IA W SRM 53-60-51, FIGURE 1, SHEET 7. 2 L 7 2 4F RT A16WE 2001031500186 20010315 00186 NM 2001 3 15 CALA0100141 1 20010218 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND FLOOR SUPPORT CORRODED IN AFT CARGO COMPARTMENT AT STA 727E-807 ABOVE STRINGER 26R. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED USING TWO SPLICES IAW SRM 53-60-53. 2 L 7 2 4F RT A16WE 2001031500187 20010315 00187 NM 2001 3 15 CALA0100142 1 20010219 A 5320 INTERCOSTAL BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73385 26314 INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL AT STA 380 - 400, BL 0. A NEW INTERCOSTAL WAS INSTALLED IAW SRM 53-30-51 AND 51-10-02. 2 L 7 2 4F RT A16WE 2001031500188 20010315 00188 WP 2001 3 15 CALA0100143 1 20010219 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP CABIN TORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10801 49127 INSPECTION FOUND MAIN CABIN O/B FLOORBOARD TORN AT FS 140 - 200. THE FLOORBOARD WAS REMOVED AND A NEW FLOORBOARD WAS IN STALLED IAW ECRA 5100-01844. 2 L 7 2 4F A6WE 2001031500189 20010315 00189 NM 2001 3 15 CALA0100144 1 20010219 A 5311 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32626 27530 INSPECTION FOUND A 5.5 INCH CRACK IN AFT CARGO COMPARTMENT FRAME AT STA 807 BETWEEN S28L AND S28R. A REPAIR WAS INSTALL ED IAW SRM 53-00-07. 2 L 7 2 4F RT A16WE 2001031500190 20010315 00190 NM 2001 3 15 CALA0100145 1 20010220 A 5330 SKIN BOEING 737 737524 1384721 NM FUSELAGE GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32626 27530 INSPECTION FOUND GOUGES ON RT FUSELAGE SKIN PLATE CLOSE TO HORIZONTAL ATTACH FITTING BETWEEN STA 1140 AND 1150. THE SKI N PLATE WAS REMOVED AND A NEW SKIN PLATE WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001031500191 20010315 00191 SO 2001 3 15 C2XA01IA103 1 20010108 A 5320 12006962001 CROSSBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12715 120125 MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE CROSSBEAM AT STATION 5118.0 WAS FOUND TO BE CORRODED. MAINTENA NCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IN ACCORDANCE WITH EMB-120 SRM 51-22-00, 51-25-00, 51-40-06, AND 51-40-0 2. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001031500192 20010315 00192 SO 2001 3 15 C2XA01IA104 1 20010108 A 5347 12026864007 SEAT TRACK EMB 120 EMB120ER 3260203 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12715 120125 MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE LEFT HAND INBOARD SEAT TRACK WAS FOUND TO BE CORRODED FROM STAT ION 11715.0 TO 13509.0. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF SEAT TRACK IN ACCORDANCE WITH EMB-120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001031500193 20010315 00193 SO 2001 3 15 C2XA01IA105 1 20010108 A 5320 12004166005 STRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12715 120125 MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE RIGHT HAND AFT BUTT STRAP WAS FOUND TO BE CORRODED FROM STATION 11715.0 TO STATION 13509.0. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IN ACCORDANCE WITH EMB -120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001031500194 20010315 00194 SO 2001 3 15 C2XA01IA106 1 20010108 A 5320 12006158002 STRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12715 120125 MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE RIGHT HAND AFT BUTT STRAP WAS FOUND TO BE CORRODED FROM STATION 12130.0 TO 13509.0. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IN ACCORDANCE WITH EMB-120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001031500195 20010315 00195 SO 2001 3 15 C2XA01IA107 1 20010108 A 5320 12027929001 STRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12715 120125 MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE LEFT HAND AFT BUTT STRAP WAS FOUND TO BE CORRODED FROM STATION 12130.0 TO STATION 13255.0. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IN ACCORDANCE WITH EMB- 120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001031500196 20010315 00196 SO 2001 3 15 C2XA01IA108 1 20010108 A 5320 12004449001 CROSSBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12715 120125 MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE AFT CROSSBEAM AT STATION 12445.0 WAS FOUND TO BE CORRODED. MAI NTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IN ACCORDANCE WITH EMB-120 SRM 51-40-02, AND THE AIRCRAFT WAS APPRO VED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001031500197 20010315 00197 SO 2001 3 15 C2XA01IA109 1 20010108 A 5320 12004449001 CROSSBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12715 120125 MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE AFT CROSSBEAM AT STATION 13509.0 WAS FOUND TO BE CORRODED. MAI NTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IN ACCORDANCE WITH EMB-120 SRM 51-40-02, AND THE AIRCRAFT WAS APPRO VED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001031500198 20010315 00198 SO 2001 3 15 C2XA01IA110 1 20010108 A 7810 12033750004 DUCT EMB 120 EMB120ER 3260203 SO RT EXHAUST CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12715 120125 MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, RIGHT HAND EXHAUST DUCT WAS FOUND TO BE CRACKED ON THE OUTBOARD SID E. MAINTENANCE PERFORMED A WELD REPAIR IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHANGE EC7810-01002, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001031500199 20010315 00199 SO 2001 3 15 C2XA01IA111 1 20010109 A 5320 12008972001 STRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12715 120125 MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE CENTER BUTT STRAP WAS FOUND TO BE CORRODED FROM STATION 13255 T O STATION 15050. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IN ACCORDANCE WITH EMB-120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001031500200 20010315 00200 SO 2001 3 15 C2XA01IA112 1 20010107 A 5230 12035109613 STOP EMB 120 EMB120ER 3260203 SO CARGO DOOR WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12715 120125 MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION ,THE CARGO DOOR LATERAL STOPS WERE FOUND TO BE WORN OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STOPS IN ACCORDANCE WITH EMB-120 SRM 52-30-02, AND THE AIRCRAFT WAS APPROV ED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001031500201 20010315 00201 SO 2001 3 15 C2XA01IA114 1 20010107 A 5230 12036702603 STOP EMB 120 EMB120ER 3260203 SO CARGO DOOR WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12715 120125 MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE CARGO DOOR LATERAL STOPS WERE FOUND TO BE WORN OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STOPS IN ACCORDANCE WITH EMB-120 M/M 52-30-02, AND THE AIRCRAFT WAS APPROV ED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001031500202 20010315 00202 SO 2001 3 15 C2XA01IA113 1 20010109 A 5320 12006158001 STRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12715 120125 MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE LEFT HAND BUTT STRAP WAS FOUND TO BE CORRODED AT STATION 13255. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IN ACCORDANCE WITH EMB-120 SRM 51-22-00 AND 51-40- 02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001031500203 20010315 00203 SO 2001 3 15 C2XA01IA115 1 20010218 A 4920 4501968A APU EMB 145 EMB145LR SO TAIL MALFUNCTIONED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 14972 6210 6210 145151 IAH - FLIGHT 3781, THE CREW REPORTED A VERY STRONG FUEL SMELL IMMEDIATELY AFTER STARTING THE APU IN FLIGHT. THE AIRCRAF T LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE OPERATIONALLY CHECKED THE APU WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE FUEL SMELL WAS AGAIN REPORTED, THE APU WAS STARTED ON THE GROUND AND MAINTENAN CE PLACED THE APU ON MEL 49-00-00 CONTROL NUMBER 009774, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCR AFT RETURNED TO IAH ON 02/21/01 WHERE MAINTENANCE REMOVED AND REPLACED THE APU. CLEARED MEL 49-00-00 CONTROL NUMBER 009 774, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001031500204 20010315 00204 SO 2001 3 15 C2XA01IA095 1 20010109 A 5320 12005779001 INTERCOSTAL EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12715 120125 MYR - DURING CONTINENTAL EXPRESS C-CHECK, THE RIGHT HAND T-SECTION AT FRAME 40 WAS FOUND TO BE CORRODED. MAINTENANCE RE MOVED AND REPLACED THE AFFECTED T-SECTION IN ACCORDANCE WITH EMB120 SRM 51-20-10, AND THE AIRCRAFT WAS APPROVED FOR RETU RN TO SERVICE. 2 L 7 2 4T RT A31SO 2001031500205 20010315 00205 GL 2001 3 15 C2XA01TY027 2 20010221 A 7200 23070401 ENGINE EMB 145 EMB145 SO ALLSN AE300 AE3007A GL LT ENGINE VIBRATION A C2XA C ABORTED TAKEOFF E J VIBRATION/BUFFET WARNING INDICATION TO TAKEOFF 1 SW 27 13989 1870 1870 145271 CAE311431 IAH FLIGHT 3977. CREW ABORTED TAKEOFF DUE TO THE LEFT HAND ENGINE VIBRATION REACHING THE AMBER RANGE. THE AIRCRAFT WA S FERRIED TO TYS AFTER EXTENSIVE TROUBLESHOOTING BY MAINTENANCE. THE LEFT HAND ENGINE WAS REMOVED AND REPLACED IAW CONT INENTAL EXPRESS TASK CARD 6271001. THE OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001031500206 20010315 00206 SO 2001 3 15 C2XA01IA116 1 20010221 A 2460 12039804001 MOUNT EMB 120 EMB120ER 3260203 SO COCKPIT BURNED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 15730 120187 IAH - FLIGHT 3551, THE CREW REPORTED THAT WHILE CLIMBING THROUGHT 6000 FEET THE COCKPIT BEGAN TO SMELL LIKE SMOKE FOLLOW ED BY A RIGHT PACK FAIL MESSAGE AND A COMPLETE LOSS OF PRESSURIZATION CONTROL. THE AIRCRAFT RETURNED TO IAH WHERE IT LA NDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE SEAT ASSEMBLY FOR THE OVER CURRENT RELAY TO HAV E LOOSE NUTS AND TO BE BURNT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT ASSEMBLY, AND OPERATIONALLY CHECKED AL L AFFECTED SYSTEMS WITH NO DEFECTS NOTED. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001031500207 20010315 00207 SO 2001 3 15 C2XA01IA117 1 20010222 A 3350 78241 POWER SUPPLY EMB 145 EMB145ER SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13936 145025 IAH - DURING C-CHECK INSPECTION, THE AFT EXIT ROW CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND RE PLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY IN ACCORDANCE WITH EMB145 M/M 33-50-11-400-801-A, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001031500208 20010315 00208 SO 2001 3 15 C2XA01IA118 1 20010221 A 3350 110049 POWER SUPPLY EMB 145 EMB145ER SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13936 145025 IAH - DURING C-CHECK INSPECTION, THE SERVICE DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED POWER SUPPLY IN ACCORDANCE WITH EMB-145 M/M 33-50-04-000-801-A, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001031500209 20010315 00209 SO 2001 3 15 C2XA01IA119 1 20010209 A 3350 66901 LIGHT EMB 145 EMB145ER SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13936 145025 IAH - DURING C-CHECK INSPECTION, THE AISLE PATH LIGHTING STRIP AT THE EMERGENCY EXIT WAS FOUND TO HAVE BROKEN WIRES. MA INTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP IN ACCORDANCE WITH EMB-145 M/M 33-50-12-000-801-A, AND THE AIRCR AFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001031500210 20010315 00210 SO 2001 3 15 C2XA01IA120 1 20010206 A 5520 PE64042K502802 BUSHING EMB 145 EMB145ER SO ELEVATOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13936 145025 IAH - DURING C-CHECK INSPECTION, THE CENTER BUSHING ON THE RIGHT HAND SERVO TAB WAS FOUND TO HAVE PITTING CORROSION. MA INTENANCE REMOVED AND REPLACED THE AFFECTED BUSHING IN ACCORDANCE WITH EMB-145 M/M 20-10-08, AND THE AIRCRAFT WAS APPROV ED FOR RETURN TO SERVICE. (P/N PE64042K5-028-022S). 2 L 7 2 4F RT T00011AT 2001031500211 20010315 00211 SO 2001 3 15 C2XA01IA121 1 20010214 A 3211 14571035409 CAP EMB 145 EMB145ER SO LT MLG CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14943 145040 IAH - DURING C-CHECK INSPECTION, THE LEFT MAIN LANDING GEAR LOWER FORWARD BEARING CAP WAS FOUND TO HAVE PITTING CORROSIO N. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEARING CAP IN ACCORDANCE WITH EMB-145 M/M 57-26-00-220-803-A00, AND T HE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001031500212 20010315 00212 SO 2001 3 15 C2XA01IA122 1 20010213 A 3211 14571035409 CAP EMB 145 EMB145ER SO LT MLG CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14943 145040 IAH - DURING C-CHECK INSPECTION, THE LEFT MAIN LANDING GEAR AFT LOWER BEARING CAP WAS FOUND TO HAVE PITTING CORROSION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEARING CAP IN ACCORDANCE WITH EMB-145 M/M 57-26-00-220-803-A00, AND THE A IRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001031500213 20010315 00213 SO 2001 3 15 C2XA01CL031 1 20010220 A 5210 14531554001 ROLLER EMB 145 EMB145LR SO FWD DOOR LACK OF LUBE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15980 145202 EWR FLIGHT 4258 THE CREW REPORTED THE FORWARD DOOR IS VERY DIFFICULT TO OPEN. MAINTENANCE INSPECTED AND LUBED THE DOOR ROLLERS. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001031500214 20010315 00214 WP 2001 3 15 CALA0100146 1 20010221 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FWD CARGO BAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10801 49127 INSPECTION FOUND FORWARD CARGO DOOR JAMB PAN CORRODED AROUND RIVET NUTS. THE LOWER DOOR JAMB PAN WAS REMOVED AND A NEW SECTION WAS INSTALLED USING SPLICES IAW SRM 53-05, FIGURE 44 AND 51-30-01. 2 L 7 2 4F A6WE 2001031500215 20010315 00215 NM 2001 3 15 CALA0100147 1 20010221 A 5315 FLOORBEAM BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32626 27530 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, LBL 48 TO RBL 48. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-04093. 2 L 7 2 4F RT A16WE 2001031500216 20010315 00216 WP 2001 3 15 CALA0100148 1 20010221 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10801 49127 INSPECTION FOUND FORWARD CARGO AREA CUSP WEB CORRODED AT FS 237, L18R, FORWARD AND AFT OF FLOORBEAM JOIST FITTING. THE CORRODED SECTION OF CUSP WEB WAS REMOVED AND A NEW CUSP WEB REPAIR DOUBLER WAS INSTALLED IAW 53-01, FIGURE 2, 51-30-2, 5 1-30-5, AND 51-30-1. 2 L 7 2 4F A6WE 2001031500217 20010315 00217 WP 2001 3 15 CALA0100149 1 20010221 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10801 49127 INSPECTION FOUND A 5 INCH CRACK IN AFT FACE OF FRAME AT LT SIDE, STA 1380, AT ANTI-ICING VALVE. THE CRACKED AREA WAS RO UTED OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 1 & FIGURE 2, 51-10-3, 51-10-8, AND 51-30-2. 2 L 7 2 4F A6WE 2001031500218 20010315 00218 WP 2001 3 15 CALA0100150 1 20010221 A 5310 TORQUE BOX DOUG DC9 DC982 3022082 WP AFT CARGO BAY PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10801 49127 INSPECTION FOUND TORQUE BOX WEB PUNCTURED AROUND NUT PLATES UPON REMOVAL OF AFT CARGO TIEDOWN TRACK. THE WEB SECTION WA S REMOVED AND REPLACED IAW ECRA 5310-04106 AND EA 9-5310-2-A0853. 2 L 7 2 4F A6WE 2001031500219 20010315 00219 WP 2001 3 15 CALA0100151 1 20010221 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10801 49127 INSPECTION FOUND SKIN CRACKED AT AFT SIDE OF CANTED FRAME STA 1485, LT SIDE. THE CRACK WAS STOP DRILLED AND A DOUBLER W AS INSTALLED IAW SRM 51-10-4, 53-01, FIGURE 3, 51-30-2, AND MM 20-10-17. 2 L 7 2 4F A6WE 2001031500220 20010315 00220 WP 2001 3 15 CALA0100152 1 20010222 A 3350 1001193 LIGHT GRIMES DOUG DC9 DC982 3022082 WP ENTRY DOOR INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14840 49580 THE FORWARD ENTRY PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE PORTABLE EMERGENCY LIGHT WAS REMOVED AND REPLACED IAW MM 33-53-01. 2 L 7 2 4F A6WE 2001031500221 20010315 00221 NM 2001 3 15 CALA0100153 1 20010222 A 5730 SKIN BOEING 757 757224 1384958 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19117 27559 INSPECTION FOUND A 9 INCH CRACK IN RT WING FIXED LEADING EDGE UPPER SURFACE BETWEEN SLAT NR 7 AND NR 8. THE CRACK WAS R EPAIRED IAW ECRA 5721-01009 AND A DIP WAS ISSUED TO REINSPECT EVERY 1000 HOURS AND TO ACCOMPLISH A PERMANENT REPAIR WITH IN 1800 HOURS OR NEXT C4 CHECK. 2 L 7 2 4F RT A2NM 2001031500222 20010315 00222 NM 2001 3 15 CALA0100154 1 20010222 A 5730 SKIN BOEING 757 757224 1384958 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19117 27559 INSPECTION FOUND A 9 INCH CRACK IN LT WING LEADING EDGE BETWEEN SLAT NR 3 & 4, WS 459.5. THE CRACK WAS REPAIRED IAW ECR A 5721-01009 AND A DIP WAS ISSUED TO REINSPECT EVERY 1000 HOURS AND TO ACCOMPLISH A PERMANENT REPAIR WITHIN 1800 HOURS O R NEXT C4 CHECK. 2 L 7 2 4F RT A2NM 2001031500223 20010315 00223 WP 2001 3 15 CALA0100155 1 20010223 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10801 49127 INSPECTION FOUND SKIN CRACKED IN TWO PLACES AT STA 1485 JUST FORWARD OF RUDDER TRIM ACTUATOR, RT SIDE. THE CRACKS WERE 1 INCH LONG. THE CRACKED AREAS WERE ROUTED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 1, 52-01, FIGURE 1, AND 51-30-2. 2 L 7 2 4F A6WE 2001031500224 20010315 00224 NM 2001 3 15 CALA0100156 1 20010223 A 5320 BRACKET BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73385 26314 INSPECTION FOUND A 1 INCH CRACK IN PANEL SUPPORT BRACKET AT PRESSURE BULKHEAD STA 727, JUST ABOVE STRINGER 27R. A FORME D SECTION REPAIR WAS INSTALLED IAW SRM 51-70-11. 2 L 7 2 4F RT A16WE 2001031500225 20010315 00225 WP 2001 3 15 CALA0100157 1 20010223 A 5320 ANGLE DOUG DC10 DC1030 3023501 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND A 1 INCH CRACK IN CENTER CARGO LT ANGLE AT STA 1721. THE ANGLE WAS REPLACED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 2001031500226 20010315 00226 NM 2001 3 15 CALA0100158 1 20010223 A 5320 FLOOR SUPPORT BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73385 26314 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 500D BETWEEN S26L AND S26R. THE FLOOR SUPPORT WAS REMOVED AND REPLACED I AW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001031500227 20010315 00227 WP 2001 3 15 CALA0100159 1 20010224 A 5755 SPOILER DOUG DC10 DC1030 3023501 WP RT WING DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND RT WING NR 1 AND 2 SPOILER PANELS DELAMINATED ON UPPER SURFACE. THE NR 1 AND 2 SPOILERS WERE REMOVED A ND REPLACED IAW MM 27-60-01. 2 L 7 3 4F A22WE 2001031500228 20010315 00228 WP 2001 3 15 CALA0100160 1 20010224 A 5755 SPOILER DOUG DC10 DC1030 3023501 WP RT WING DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND RT WING SPOILER PANELS NR 3, 4, & 5 DELAMINATED ON UPPER SURFACE. THE SPOILERS WERE REMOVED AND REPLAC ED IAW MM 27-60-01. 2 L 7 3 4F A22WE 2001031500229 20010315 00229 WP 2001 3 15 CALA0100161 1 20010224 A 5247 SKIN DOUG DC10 DC1030 3023501 WP APU DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND A 1.2 INCH CRACK IN APU DOOR SKIN. A NEW DOOR WAS INSTALLED IAW DRAWING AHL7008 AND SRM 51-31-01. 2 L 7 3 4F A22WE 2001031500230 20010315 00230 WP 2001 3 15 CALA0100162 1 20010224 A 5755 SPOILER DOUG DC10 DC1030 3023501 WP LT WING DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND LT WING SPOILER NR 2 DELAMINATED WITH LOWER SKIN CORRODED. THE NR 2 LT SPOILER WAS REMOVED AND REPLACE D IAW MM 27-60-01. 2 L 7 3 4F A22WE 2001031500231 20010315 00231 NM 2001 3 15 CALA0100163 1 20010224 A 2560 61020 BATTERY BOEING 737 737524 1384721 NM FLASHLIGHT DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16646 28907 INSPECTION FOUND FORWARD FLIGHT ATTENDANT RT EMERGENCY FLASHLIGHT INOPERATIVE. THE FLASHLIGHT BATTERY WAS REPLACED IAW MM 25-60-00. 2 L 7 2 4F RT A16WE 2001031500232 20010315 00232 NM 2001 3 15 CALA0100164 1 20010225 A 5520 FITTING BOEING 737 7373Q8 1384670 NM LT ELEVATOR SEPARATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73385 26314 INSPECTION FOUND LT ELEVATOR HORN BEARING FITTING SEPARATED. THE LT ELEVATOR WAS REMOVED AND REPLACED IAW MM 27-31-11. 2 L 7 2 4F RT A16WE 2001031500233 20010315 00233 NM 2001 3 15 CALA0100165 1 20010225 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17329 23459 INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 967-986, LBL 18.32. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001031500263 20010315 00263 EU 2001 3 15 USAASB01038 2 20010205 A 7230 BLADE BOEING 737 737401 1384701 NM CFMINT CFM56 CFM563B2 13802 EU LT & RT ENGINE DAMAGED A USAA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 EA 19 413US 23882 BWI - FLT 1882 - EN ROUTE FROM CLT TO PHL, BOTH ENGINE VIBRATION INDICATORS APPROACHED NR 5. FLIGHT DIVERTED TO BWI AND LANDED WITHOUT FURTHER INCIDENT. UPON ARRIVAL, MAINTENANCE FOUND ACOUSTICAL PANELS BEHIND BOTH N1 FANS TORN. APPEARS ENGINES ENCOUNTERED MODERATE MIXED ICING. DURING INSPECTION OF THE ENGINES, MAINTENANCE FOUND THE LEFT ENGINE FAN BLADE S NR 24 AND N 25 AND THE RIGHT ENGINE FAN BLADES NR 26 AND NR 28 OUT OF SERVICEABLE LIMITS PER MM 72-31-02. ALSO, FOUND 10 MID ACOUSTICAL PANELS, ON EACH ENGINE, DAMAGED BEYOND SERVICEABLE LIMITS. REMOVED AND REPLACED ENGINE FAN BLADES (P /N 1590M21P01) PER MM 72-31-02 AND MID ACOUSTICAL PANELS (P/N 335-011-904-0) PER MM 72-33-02. ALL ENGINE PARAMETERS NOR 2 L 7 2 4F 4 F RT A16WE E21EU 2001031500269 20010315 00269 NM 2001 3 15 USAASB01037 1 20010204 A 4900 APU BOEING 737 737201 1384454 NM TAIL MALFUNCTIONED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 259AU 22806 BWI- FLT 2993 - EN ROUTE FROM BOS TO FLL, AT FL350, THE APU SHUTDOWN. THE NR 2 CSD/GENERATOR WAS ALREADY ON MEL SO THE CREW DECLARED AN EMERGENCY AND BEGAN TO DIVERT TO BWI. AT FL240, THE APU WAS RESTARTED AND THE EMERGENCY WAS CANCELED. FLIGHT CONTINUED TO DIVERT TO BWI AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RAN THE APU AND COULD FIND NO FAULTS . REMOVED AND REPLACED, AS PRECAUTIONARY, THE APU CONTROL MODULE UNIT M280, AND THE APU FUEL SHUTOFF SOLENOID (P/N 6925 45-1), THE APU TACHOMETER GENERATOR (P/N 2CM9ABH7) AND THE APU THREE SPEED SWITCH (P/N 3876259-4). APU OPERATIONAL CHEC K NORMAL. CLEARED THE MEL ON THE NR 2 CSD/GENERATOR BY REMOVING AND REPLACING THE NR 2 CSD (P/N 731753), GENERATOR (P/N 2 L 7 2 4F A16WE 2001031500270 20010315 00270 NM 2001 3 15 USAASB01034 1 20010203 A 4990 6984301 PRESSURE SWITCH BOEING 737 737201 1384454 NM APU MALFUNCTIONED A USAA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 EA 19 259AU 22806 CLT - FLT 2826 - EN ROUTE FROM MCO TO BOS, THE NR 2 ENGINE CSD HIGH OIL TEMPERATURE LIGHT ILLUMINATED ALONG WITH HIGH OI L TEMPERATURE INDICATION ON THE CSD TEMPERATURE GAUGE. CREW DISCONNECTED THE NR 2 ENGINE CSD AND STARTED THE APU. CREW THEN RECEIVED AN APU LOW OIL PRESSURE LIGHT WITH AN APU AUTO SHUTDOWN. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTH ER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE APU LOW OIL PRESSURE SWITCH. OPS CHECK O F APU GOOD. ALSO, FOUND THE NR 2 CSD OIL LEVEL LOW AND A MISSING PLUG. REFILLED OIL AND REPLUGGED CASE ON NR 2 CSD. RE SET CSD AND OPS CHECKED. OPS CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F A16WE 2001031500271 20010315 00271 NM 2001 3 15 USAASB01027 1 20010128 A 4920 360452454 COMBUSTION LINER BOEING 737 7372B7 1384560 NM APU FAILED A USAA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 EA 19 266AU 1561 22878 MCO - FLT 2703 - EN ROUTE FROM LGA TO FLL, AT APPROXIMATELY FL310, THE APU SHUTDOWN DUE TO AN OVERSPEED CONDITION. THE NR 1 GENERATOR WAS ALREADY ON MEL, SO THE CAPTAIN ADVISED HE WOULD BE DIVERTING TO MCO. FLIGHT LANDED WITHOUT FURTHER I NCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE APU COMBUSTOR ASSEMBLY. OPERATIONAL CHECK GO OD. CLEARED MEL ON THE NR 1 GENERATOR BY REMOVING AND REPLACING THE CSD (P/N 731753) AND GENERATOR (P/N 976J498-1). OP S CHECK GOOD. (M) 2 L 7 2 4F A16WE 2001031500329 20010315 00329 NM 2001 3 15 USAA010144 1 20010212 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND SKIN CRACKED .5 INCH, FUSELAGE SKIN STATION 727A PLUS 8 JUST ABOVE STRINGER 18L. INSTALLED DOUBLER PER SRM 53-30-03. (M) 2 L 7 2 4F A16WE 2001031500330 20010315 00330 NM 2001 3 15 USAA010145 1 20010212 A 5320 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND TIE CLIP CRACKED, STATION 747, STRINGER 4R. INSTALLED NEW CLIP PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2001031500331 20010315 00331 NM 2001 3 15 USAA010146 1 20010212 A 5320 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 747, STRINGER 7R. INSTALLED NEW CLIP PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2001031500332 20010315 00332 NM 2001 3 15 USAA010147 1 20010212 A 5320 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND TIE CLIP CRACKED .125 INCH, BS 807, STRINGER 10L. INSTALLED NEW CLIP PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2001031500333 20010315 00333 NM 2001 3 15 USAA010148 1 20010212 A 5320 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 807, STRINGER 11L. REPLACED TIE CLIP PER SRM 51-10-01 AND DWG 69-45156. (M) 2 L 7 2 4F A16WE 2001031500334 20010315 00334 NM 2001 3 15 USAA010149 1 20010212 A 5320 WEB BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND WEB CRACKED .25 INCH, STATION 767 WEB CRACKED STRINGER 13R. INSTALLED RADIUS BLOCK PER EA 69053. (M) 2 L 7 2 4F A16WE 2001031500335 20010315 00335 NM 2001 3 15 USAA010150 1 20010212 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND FRAME CRACKED .5 INCH, STATION 767, STRINGER 13L. INSTALLED DOUBLER PER SRM 53-10-4 FIG 1. (M) 2 L 7 2 4F A16WE 2001031500336 20010315 00336 NM 2001 3 15 USAA010151 1 20010212 A 5240 SKIN BOEING 737 737201 1384454 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND SKIN CRACKED 1.60 INCH, RIGHT AFT SERVICE DOOR BEAR STRAP. INSTALLED TRIPLER PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 2001031500338 20010315 00338 SO 2001 3 15 C2XA01TY021 1 20010212 A 3222 1170B000001 STRUT EMB 145 EMB145LR SO NLG GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16976 145171 TYS - DURING A SCHEDULED 1C INSPECTION, SEVERAL GOUGES WERE FOUND IN THE NOSE LANDING GEAR STRUT ASSY, MAINTENANCE BLEND ED GOUGES, DYE-PENNED IAW EMB 145 REF GST 0401/01, RESTORED THE REWORKED AREA IAW EMB 145 CPM 51-21-03,-04 AND -06. NO FURTHER ACTION REQUIRED. PROCEDURES WERE SATISFACTORY, AIRCRAFT WILL BE RELEASED FOR SERVICE UPON COMPLETION OF C-CHECK . (M) 2 L 7 2 4T RT T00011AT 2001031500339 20010315 00339 EU 2001 3 15 SIMA0205 1 20010120 A 3300 SMOKE SAAB SF340 340B 7860101 EU CABIN DETECTED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 21 234AE 340B234 PWM - FLT 4495 - FLIGHT ATTENDANT REPORTED SMOKE SMELL FROM ROW 9. MAINTENANCE INSPECTED SOCKETS WHILE AIRCRAFT HAD POW ER APPLIED. NO SMOKE SMELL OR ARCING OR BURNING OF SOCKETS WAS OBSERVED. WINDOW LIGHT FOR SEAT 10A WAS PUT ON MEL AT T HIS TIME. AIRCRAFT WAS PREVIOUSLY WAS INSPECTED WITH NO DEECTS NOTED. MEL WAS CLEARED AND AIRCRAFT HAS BEEN RETURNED T O SERVICE. (M) 2 L 7 2 4T RT A52EU 2001031500340 20010315 00340 SO 2001 3 15 C2XA01CL019 1 20010212 A 3260 23092900001 UPLOCK EMB 145 EMB145 SO NLG FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14925 8853 145004 CLE - FLT 4041 - THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER TAKEOFF FROM CLEVELAND. THE AIRCRAFT RE TURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR UPLOCK BOX. THE O PERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001031500341 20010315 00341 SO 2001 3 15 C2XA01CL018 1 20010212 A 3234 355022022 CONTROL UNIT EMB 145 EMB145 SO COCKPIT FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14925 1202 145004 EWR-CVG - FLT 4226 - THE CREW REPORTED AFTER TAKEOFF RECEIVED A LANDING GEAR AIR GROUND FAIL MESSAGE. THE LANDING GEAR COULD NOT BE RETRACTED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED INTO CLEVELAND AND LANDED WITHOUT FURTHER I NCIDENT. MAINTNANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT AND CHECKED THE LANDING GEAR PROXIMITY SWITCH ES IAW EMB MM 32-32-01 AND 32-60-00. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001031500342 20010315 00342 NM 2001 3 15 TSAA0132011 1 20010210 A 3230 LANDING GEAR BOEING 737 7372X6C 1384552 NM NLG MALFUNCTIONED A TSAA O OTHER J WARNING INDICATION CL CLIMB 1 WP 13 816AL 23122 FLT 275 - OGG-HNL - AFTER TAKEOFF AND RAISING THE LANDING GEAR, NOSE WHEEL RED WARNING LIGHT REMAINED ON. CYCLED THE LA NDING GEAR, LIGHT WENT OUT. ETOPS AIRCRAFT ON A NON-ETOPS FLIGHT. INSPECTED NOSE LANDING GEAR DOWN AND UPLOCK SENSORS. ADJUSTED LEFT AND RIGHT DOOR ROD ENDS AND DOOR STOPS. THE NOSE LANDING GEAR OPERATIONAL CHECKED OK PER BOEING MM 32-6 1-41. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001082800085 20010828 00085 NM 2001 8 28 TSAA0132010 1 20010814 A 3260 6552811109 ACCESSORY UNIT BOEING 737 7372S5C 1384499 NM E/E BAY FAULTY A TSAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 WP 13 802AL 22148 ON APPROACH, WITH GEAR DOWN THREE GREEN AND FLAPS AT 40 GREEN LIGHT, AURAL WARNING 'TOO LOW GEAR' SOUNDED AT APPROX 900 FT. THREE RED GEAR LIGHTS ILLUMINATED, THREE GREEN LIGHTS REMAINED ILLUMINATED. CREW EXECUTED GO AROUND APPROX 700 FT AN D DELAYED GEAR RETRACTION TO HAVE TOWER CONFIRM GEAR CONFIGURATION. TOWER CONFIRMED GEAR WAS DOWN. GEAR WAS RETRACTED A ND QRH PROCEDURES REVIEWED. DOWNWIND, THE LANDING GEAR EXTENDED AND FLAPS SELECTED TO 40, THE PROBLEM DID NOT RETURN. LA NDING WAS ACCOMPLISHED WITH NO PROBLEMS. THE AIRCRAFT WAS INSPECTED AND FERRIED FOR MAINTENANCE. MAINTENANCE REPLACED TH E LANDING GEAR ACCESSORY UNIT AS PRECAUTIONARY. (M) 2 L 7 2 4F RT A16WE 2001031500343 20010315 00343 NM 2001 3 15 20010315SG001 1 20010213 A 2752 793T1005 MOTOR BOEING 727 72751C 1384015 NM FLAP FAILED A RYNA J A DUMP FUEL UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 CE 07 436EX 19289 FLT 733 - EN ROUTE TO ORD HAD A SPLIT FLAP INDICATION. AIR CREW CONDUCTED AN AIR TURN BACK TO SEA. AIR CREW DUMPED FUE L AND DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY AND WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED OUTBOARD FLAP A LTERNATE DRIVE ELECTRIC MOTOR, FLAP ALTERNATE DRIVE MOTOR ELECTRICAL CONNECTOR PLUG AND FLAP INDICATOR. REMOVED AND REP LACED LEADING EDGE DEVICE BYPASS VALVE. SYSTEM OPERATES NORMAL. (M) 2 L 7 3 4F A3WE 2001031500344 20010315 00344 NM 2001 3 15 20010315SG002 1 20010131 A 2611 100102403 SMOKE DETECTOR BOEING 727 72776 1384016 NM CARGO BAY MALFUNCTIONED A RYNA K NONE N FALSE WARNING IN INSP/MAINT 1 CE 07 721JE 18843 FLT 612 - IND - LOWER CARGO SMOKE DETECTION MAINTENANCE LIGHT CAME ON. REMOVED AND REPLACED LOWER SMOKE CARGO DETECTOR MODULE SYSTEM. SYSTEMS OPERATES NORMAL. (M) 2 L 7 3 4F A3WE 2001031500345 20010315 00345 EU 2001 3 15 REXA01003 1 20010118 A 3234 D49408001 HANDLE SAAB SF340 SF340A 7850100 EU COCKPIT FAILED A REXA K NONE J WARNING INDICATION AP APPROACH 1 SO 25 922MA 340A077 ON APPROACH TO MEMPHIS, WHEN LANDING GEAR WAS SELECTED DOWN, GEAR EXTENDED NORMALLY BUT FAILED TO GIVE A DOWN AND LOCKED GREEN LIGHT FOR THE NOSE GEAR. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. LANDING GEAR CONTROL HANDLE P/ N D494-08-001 WAS REPLACED WITH A GEAR SWING PERFORMED AFTER REPLACEMENT WITH NO DEFECTS BEING FOUND. (M) 2 L 7 2 4T RT A52EU 2001031500346 20010315 00346 NM 2001 3 15 USAA010137 1 20010212 A 5312 BULKHEAD BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND BULKHEAD CRACKED .125 INCH, TWO PLACES, BS 1016 AT APPROX STRINGER 3L. INSTALLED DOUBLER PER EA 69021. (M) 2 L 7 2 4F A16WE 2001031500347 20010315 00347 NM 2001 3 15 USAA010138 1 20010212 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND FLOORBEAM CORRODED 1 INCH, STATION 328, LBL 54. CORROSION LEVEL 1. INSTALLED UPPER SECTION PER TR 53-10-13 AND SRM 51-10-6. (M) 2 L 7 2 4F A16WE 2001031500348 20010315 00348 NM 2001 3 15 USAA010139 1 20010212 A 5320 CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND CLIP CRACKED .125 INCH, STATION 597, STRINGER 4R. INSTALLED NEW TIE CLIP PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2001031500349 20010315 00349 NM 2001 3 15 USAA010140 1 20010212 A 5320 CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND CLIP CRACKED .125 INCH, STATION 616, STRINGER 2R. INSTALLED NEW CLIP PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2001031500350 20010315 00350 NM 2001 3 15 USAA010141 1 20010212 A 5320 CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND CLIP CRACKED .125 INCH, STATION 639, STRINGER 3L. INSTALLED NEW CLIP PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2001031500351 20010315 00351 NM 2001 3 15 USAA010142 1 20010212 A 5320 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND TIE CLIP CRACKED .125 INCH, BS 706, STRINGER 6L. INSTALLED NEW TIE CLIP PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2001031500352 20010315 00352 NM 2001 3 15 USAA01043 1 20010212 A 5320 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 707, STRINGER 10R. INSTALLED NEW TIE CLIP PER SRM 51-10-1 AND 51-30-2. (M) 2 L 7 2 4F A16WE 2001031500353 20010315 00353 SO 2001 3 15 C2XA01TY020 1 20010212 A 5744 14569009408 ATTACH FITTING EMB 145 EMB145LR SO RT AILERON GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16976 145171 TYS - DURING A SCHEDULED 1C INSPECTION, THE RIGHT AILERON INBOARD ATTACH BRACKET WAS FOUND TO BE GOUGED. MAINTENANCE BL ENDED AND DYE PENETRANT THE ATTACH BRACKET IAW EMB REF GST 0421/01, ALODINED AND PRIMED AREA IAW EMB 145 CMP 51-21-03, 5 1-21-04 AND 51-21-06. PROCEDURES WERE SATISFACTORY, AIRCRAFT WILL BE RELEASED FOR SERVICE UPON COMPLETION OF C-CHECK. (M) 2 L 7 2 4T RT T00011AT 2001031900001 20010319 00001 NM 2001 3 19 UPS01235040 1 20010223 A 2560 SLIDE BOEING 727 72731C 1384011 NM CABIN OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:N/A, SLIDE FELL OUT OF CONTAINER. ITEM DEFFERRED IAW MEL 52-15, NOT REQUIRED FOR FLIGHT. 2 L 7 3 4F A3WE 2001031900002 20010319 00002 NE 2001 3 19 01FDEA00125 2 20010215 A 7261 RELIEF VALVE BOEING 727 72724C 1384005 NM PWA JT8 JT8D7B 52053 NE NR 2 ENGINE FAILED A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 114FE 19527 649245 WHILE IN FLT NR 2 ENG OIL PRESSURE ABOVE RED LINE (60 PSI) COMPLIED WITH RED TABS TO SHUT DOWN ENG. NOTE: ABOVE RED LIN E FOR LESS THAN 5 MIN WHILE ADDRESSING PROB. OIL TEMP CONT TO RISE AND WAS EVENTUALLY 120 DEG C. *S/D* REMOVED AND RE PLACED NR 2 ENG OIL PRESSURE RELIEF VALVE PER IAW PWA MM 72-61-0. LEAK CK OK. REMOVED AND REPLACED MAIN OIL STRAINER P ER PWA JT8D MM 72-61-8. A/C OK FOR SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2001031900003 20010319 00003 EU 2001 3 19 01FDEA00126 1 20010214 A 3220 A5361058020300 BUSHING AIRBUS 310 A310222 3930315 EU NLG CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 417FE 333 NOSE LANDING GEAR - AFT REMOVAL OF RT NLG SWIVEL BEARING FOUND BUSHING AT FITTING WITH CORROSION. *S/D* REMOVED AND RE PLACED BUSHING PER SRM 51-72-20. 2 L 7 2 4F RT A35EU 2001031900004 20010319 00004 WP 2001 3 19 UPS01835035 1 20010124 A 5320 SPLICE PLATE DOUG DC8 DC873F 302199F WP AFT CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3 AFT PIT LONGERON 31L SPLICE PLATE CRACKED AT FS 1270. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D , LOCATED AND DRILLED FITTING IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001031900005 20010319 00005 WP 2001 3 19 UPS01835036 1 20010124 A 5320 SPLICE PLATE DOUG DC8 DC873F 302199F WP AFT CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3 AFT PIT LONGERON 31L SPLICE PLATE CRACKED AT FS 1270. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D . LOCATED AND DRILLED FITTING IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001031900006 20010319 00006 WP 2001 3 19 UPS01835037 1 20010124 A 5320 NA SPLICE PLATE DOUG DC8 DC873F 302199F WP AFT PIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3 AFT PIT, LONGERON 34L SPLICE PLATE CRACKED AT FS 1270. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20 D, LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001031900007 20010319 00007 WP 2001 3 19 UPS01835038 1 20010124 A 5310 TORQUE BOX DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3 MAIN CABIN FS 390 L12RT TORQUE BOX WEB CRACKED. FABBED REPAIR DOUBLER IAW DC8 SRM 53-2-0 FIG 1D, A LODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED WITH HI-LOKS IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001031900008 20010319 00008 WP 2001 3 19 UPS01835039 1 20010123 A 5312 BULKHEAD DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3 LT AFT PRESSURE BULKHEAD STA 1766 APPROX L11L IS CRACKED. REPAIRED AREA IAW DAC DWG SRO 8530007. 2 L 7 4 4F RT 4A25 2001031900009 20010319 00009 WP 2001 3 19 UPS01835043 1 20010222 A 3350 BATTERY DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:PFLT EMERGENCY EXIT BATTERY LOW. REMOVED AND REPLACED EMERGENCY EXIT BATTERY. PACK OK FOR SERVICE. 2 L 7 4 4F RT 4A25 2001031900010 20010319 00010 2001 3 19 01FDEA00133 4 20010216 A 3442 ANTENNA BOEING 727 72722 1384002 NM WEATHER RADAR FAILED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 149FE 19087 DURING TAXI OUT RADAR GROUND TEST OK. ONCE IN AIR RADAR WOULD NOT CONTOUR ANY WEATHER, IT ONLY PAINT GREEN OR LOWEST IN T. ATC WAS POINTING OUT VARIOUS WEATHER CELL WHICH THE RADAR DID NOT PAINT. GROUND TEST OK. *S/D* REMOVED AND REPLAC ED RADAR ANTENNA, RADAR R/T UNIT, IND PER 727-100 MM 34-41-022-4, 34-41-041-4, 34-031-4. SYS OPS CK NORMAL. 2 L 7 3 4F A3WE 2001031900011 20010319 00011 NM 2001 3 19 01FDEA00134 1 20010216 A 5610 WINDOW BOEING 727 727233 138408A NM COCKPIT CRACKED A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 281FE 22348 CAPT L1 FRONT WINDOW IS CRACKED. WINDOW HEAT CAUSES ARCHING AND FURTHER CRACKING. OUTER PANE APPEARS TO BE MOST AFFECT ED. WINDOW HEAT IS INOP. *S/D* REMOVED AND REPLACED L1 WINDOW AND HEAT CONTROLLER REF MM 30-41-013-5, 56-11-011-4. S EALED AND INSTALL WIPER ON L1 WINDOW MM 56-11-011-4. 2 L 7 3 4F RT A3WE 2001031900012 20010319 00012 NM 2001 3 19 01FDEA00136 1 20010216 A 2782 651781822 ACTUATOR BOEING 727 7272S2F 1384O81 NM NR 6 SLAT FAILED A FDEA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 SO 25 215FE 22936 REPEAT WRITE-UP NR 6 SLAT SHOW INTRANSIT AFT FLAPS WERE RAISED TO 0. RED TAB PROC FOLLOW WITH NO IMPROVEMENTS. CREW RE PORTS A/C ROLLS TO THE LEFT WITH THE FLAPS SEL UP AND THE NR 6 L/E INTRANSIT LIGHT ON. REMOVED AND REPLACED SLAT ACTUAT OR PER MM 27-81-03-4. 2 L 7 3 4F A3WE 2001031900013 20010319 00013 NM 2001 3 19 01FDEA00109 1 20010210 A 5310 SHEAR TIE BOEING 727 72725C 138400H NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DURING ROUTINE INSP FUSELAGE SHEAR TIE AT BS 1030, STR 5R & 6R FOUND CRACKED. *S/D* REMOVED, REPLACED, FAB, TREATED AN D PRIMED PER IAW BAC 727 SRM 51-20-1, 51-10-2, 51-30-2. 2 L 7 3 4F A3WE 2001031900014 20010319 00014 SO 2001 3 19 C2XA01BT014 1 20010210 A 5240 WARNING SYSTEM EMB 145 EMB145ER SO COCKPIT ACTIVATED A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 14945 145049 MHT - FLT 3978 - CREW REPORTED AIR RETURN FOR GALLEY DOOR INDICATOR AFTER TAKEOFF, LANDING WAS 400 LBS OVERWEIGHT. AIRC RAFT RELEASED IAW MEL NR 52-70-00/1 CONTROL NR 009233. AIRCRAFT FEW TO EWR WHERE MAINTENANCE OPERATIONALLY CHECKED THE GALLEY DOOR, OPS CHECKED AT THIS TIME WAS GOOD IAW EMB145 MM 52-43-00. MAINTENANCE CLEARED THE MEL AND RETURNED THE AIR CRAFT TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001031900015 20010319 00015 SO 2001 3 19 C2XA01BT012 1 20010211 A 2530 CONNECTOR EMB 145 EMB145ER SO GALLEY FAULTY A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 14942 145037 EWR - FLT 4088 - CREW REPORTED BURNING SMELL FROM COFFEE CONNECTOR NR 2 POSITION. MAINTENANCE REMOVED AND REPLACED NR 2 COFFEE POT CONNECTOR IAW EMB145AMM NR 25-16-02, OPS CHECKED GOOD. (M) 2 L 7 2 4F RT T00011AT 2001031900016 20010319 00016 SO 2001 3 19 C2XA01BT011 1 20010210 A 3350 3011210 LIGHT EMB 145 EMB145 SO CABIN DOOR INOPERATIVE A C2XA K NONE L NO TEST NR NOT REPORTED 1 SW 27 15926 145005 EWR - FLT 3572 - CREW REPORTED EMERGENCY LIGHT AT PAX DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LIGHT ASSEMBLY . OPS CHECKED SATISFACTORY. (M) 2 L 7 2 4F RT T00011AT 2001031900017 20010319 00017 SO 2001 3 19 C2XA01BT013 1 20010208 A 2612 36011335002300C FIRE LOOP EMB 145 EMB145LR SO NR 1 ENGINE FAILED A C2XA K NONE N FALSE WARNING NR NOT REPORTED 1 SW 27 14952 145067 LGA - FLT 4161 - CREW REPORTED ''E1 FIRE DETECTOR FAIL'', LGA MAINTENANCE REMVOED AND REPLACED NR 1 ENGINE FIRE LOOP IAW EMB145 MM 26-11-01, OPS CHECKED GOOD. (M) 2 L 7 2 4T RT T00011AT 2001031900018 20010319 00018 SO 2001 3 19 C2XA01CL007 1 20010117 A 3350 7287580505 LIGHT EMB 135 EMB135ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12519 145366 CLE - FLT 3670 - THE CREW REPORTED THE FRONT EMERGENCY AISLE PATH LIGHT STRIP INOPERATIVE. MAINTENANCE REPLACED THE FRO NT EMERGENCY AISLE PATH LIGHT STRIP. OPS CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001031900019 20010319 00019 SO 2001 3 19 C2XA01CL020 1 20010213 A 3260 852701 PROXIMITY SWITCH EMB 145 EMB145 SO LT/RT MLG OUT OF ADJ A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14925 145004 CLE - FLT 4058 - THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER TAKEOFF ALONG WITH THE LANDING GEAR FAIL ED TO RETRACT. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE GAP ON THE LEFT AND RIGHT MAIN GEAR WEIGHT ON WHEELS 2 PROXIMITY SWITCHES. OPS CHECKS WERE GOOD. THE AIRCRAFT WAS TEST FLOWN AND NO DEFECTS WERE NOTED. (M) 2 L 7 2 4F RT T00011AT 2001031900020 20010319 00020 SO 2001 3 19 C2XA01TY025 1 20010214 A 5311 14531937004 FRAME EMB 145 EMB145LR SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16976 145171 TYS - DURING A SCHEDULED 1C INSPECTION, A GOUGE WAS FOUND ON FRAME 63 IN CARGO BAY, RIGHT PYLON ATTACHMENT POINT. MAINT ENANCE BLENDED GOUGE AND PERFORMED NDT INSPECTION IAW EMB REF GST 0467/01. ALODINE AND PRIMED AREA IAW EMB CPM 51-21-31 AND 04. REPAIR PROCEDURES WERE SATISFACTORY. AIRCRAFT WILL BE RELEASED FOR SERVICE UPON COMPLETION OF C CHECK. (M) 2 L 7 2 4T RT T00011AT 2001031900021 20010319 00021 NM 2001 3 19 01FDEA00112 1 20010212 A 5311 651593810 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 FRAME DENTED AT BS 700 BETWEEN STR 22 LT AND 23 LT. *S/D* REMOVED, REPLACED AND FAB PER FEDEX SRM 51-40-3 AND EA 7-531 0-56528. 2 L 7 3 4F RT A3WE 2001031900022 20010319 00022 NM 2001 3 19 01FDEA00113 1 20010212 A 5311 FRAME BOEING 727 72725C 138400H NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DURING ROUTINE INSP, MAIN CABIN FRAME AT BS 1130 FOUND CRACKED AT STR 11L. *S/D* HFEC IND NO CRACKS PER IAW BAC 727 ND T MANUAL PART 6. TREATED, PRIMED AND REINSTALL CLIP PER SRM 51-10-2, 51-30-2. 2 L 7 3 4F A3WE 2001031900023 20010319 00023 SO 2001 3 19 C2XA01TY024 1 20010214 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A K NONE O OTHER IN INSP/MAINT 1 SW 27 16976 145171 TYS - DURING A SCHEDULED 1C INSPECTIN, THE OMEGA BEAM TOP CAP BETWEEN FRAMES 19 AND 23, STRINGERS 21E AND 20R WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED OMEGA BEAM TOP CAP IAW EMB-145-SRM 51-40-02. REPAIR PROCEDURES WERE SAT ISFACTORY, AIRCRAFT WILL BE RELEASED FOR SERVICE UPON COMPLETION OF C-CHECK. (M) 2 L 7 2 4T RT T00011AT 2001031900024 20010319 00024 SO 2001 3 19 C2XA01BT021 1 20010212 A 4930 FUEL LINE EMB 145 EMB145LR SO APU LOOSE A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 14972 145151 STL/EWR - FLT 4271 - CREW REPORTED ''STRONG SMELL OF FUEL AFTER STARTING THE APU IN FLIGHT''. MAINTENANCE CONTROL MEL'' D AIRCRAFT PER MEL 49-00-00 PLACARD PLACARD NR 009259. AIRCRAFT RETURNED TO EWR. MAINTENANCE SECURED FUEL LINE AT FUEL FILTER, AND GROUND RUN CHECKED GOOD IAW EMB 145 MM 49-00-00. MEL CLEARED, AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001031900025 20010319 00025 SO 2001 3 19 C2XAO1BT019 1 20010213 A 2560 892480 PLATE EMB 145 EMB145 SO FIRE EXTINGUISH MISSING A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14939 145030 EWR - FLT 4142 - DURING RON CHECK, MAINTENANCE FOUND WATER BOTTLE FIRE EXTINGUISHER MISSING DATA PLAT ON BOTTLE. REMOVE D AND REPLACED BOTTLE WITH SERVICEABLE UNIT. (M) 2 L 7 2 4F RT T00011AT 2001031900026 20010319 00026 SO 2001 3 19 C2XA01TY026 1 20010218 A 7110 14576518003 SUPPORT BRACKET EMB 145 EMB145LR SO LT COWLING CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16976 145171 TYS - DURING A SCHEDULED 1C INSPECTION, THE LEFT ENGINE LOWER COWLING CHAFFED AT EDGE SUPPORT AFT OF REAR HINGE. MAINTE NANCE BLENDED AREA AND INSTALLED AN L SHAPED SUPPORT OVER THE AFFECTED AREA IAW EMB RED GST 0519/01. PROCEDURES WERE SA TISFACTORY. AIRCRAFT WILL BE RELEASED FOR SERVICE UPON COMPLETION OF C-CHECK. (M) 2 L 7 2 4T RT T00011AT 2001031900027 20010319 00027 NM 2001 3 19 TSAA0133016 1 20010216 A 3350 86210066 BATTERY PACK BOEING 737 7372M6C 1384708 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 REPLAED NR 2 FLOOR EMERGENCY LIGHT BATTERY PACK FOR BEING LOW. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001031900028 20010319 00028 NM 2001 3 19 TSAA0133015 1 20010216 A 3350 8610066 BATTERY PACK BOEING 737 737297 1384480 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 REPLACED BATTERY FOR THE NR 3 AND NR 4 POSITION FOR THE EMERGENCY FLOOR PROX LIGHT. OPS CHECK OK. AIRCRAFT RETURNED SE RVICE. (M) 2 L 7 2 4F A16WE 2001031900029 20010319 00029 NM 2001 3 19 TSAA0133017 1 20010216 A 3350 86210066 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 809AL 21720 REPLACED FORWARD SERVICE EMERGENCY EXIT IDENT AND RIGHT CENTER EXIT IDENT BATTERY PACKS. OPS CHECK OK. AIRCRAFT RETURN ED TO SERVICE. (M) 2 L 7 2 4F A16WE 2001031900030 20010319 00030 NM 2001 3 19 TSAA0153006 1 20010215 A 5311 6549906511 FRAME BOEING 737 737230 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 821AL 23155 IDENTIFIED CRACK AT FASTENER HOLE CAUSED BY A SHORT EDGE DISTANCE AT BS 1112 FRAME. TRIM OUT THE DAMAGED AREA OF FRAME, FABRICATED AND INSTALLED FILLER OF 056 INCH 7075-T6, FABRICATED AND INSTALLED 063 INCH REPAIR STRAP, CLEANED AND TREATE D ALL EXPOSED AREAS IAW ECO 3202, 8110-3 APPROVAL RECEIVED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001031900038 20010319 00038 NM 2001 3 19 01FDEA00114 1 20010212 A 5310 SHEAR TIE BOEING 727 72725C 138400H NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DURING ROUTINE INSP, FUSELAGE SHEAR TIE AT BS 1070, STR 6L FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB CLIP PER IAW BAC 727 SRM 51-20-1, 51-10-2, 51-30-2. 2 L 7 3 4F A3WE 2001031900039 20010319 00039 NM 2001 3 19 UPS01235092 1 20010227 A 2622 FIRE BOTTLE BOEING 727 727185C 138406N NM CARGO BAY LOW A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:N/A, PORTABLE CARGO COMP FIRE EXTINGUISHER BELOW LIMITS. REMOVED AND REPLACED FIRE BOTTLE. 2 L 7 3 4F A3WE 2001031900041 20010319 00041 SO 2001 3 19 C2XA01TY015 1 20010211 A 5320 14521713003 BEAM EMB 145 EMB145LR SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16976 145171 TYS - DURING A SCHEDULED 1C INSPECTION, RIGHT OMEGA BEAM AT FRAME 20 BETWEEN STRINGERS 21R AND 20R WAS FOUND TO HAVE COR ROSION. MAINTENANCE BLENDED OMEGA BEAM, PERFORMED DYE PENETRANT INSPECTION. ALODINED AND PRIMED IAW EMB REF GST 0409/0 1, EMB 145 NDI MM 53-00-00 AND CMP 51-21-03 AND 51-21-04. BLENDING PROCEDURES WERE SATISFACTORY, AIRCRAFT WILL BE RELEA SED FOR SERVICE UPON COMPLETION OF C-CHECK. (M) 2 L 7 2 4T RT T00011AT 2001031900042 20010319 00042 NM 2001 3 19 USAA010164 1 20010116 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 246US 50479 22753 BOS - FOUND SKIN CRACKED 2 INCHES, BS 727A STRINGER 15L. INSTALLED DOUBLER PER SRM 53-30-3 PP 2E, FIG 1. (M) 2 L 7 2 4F A16WE 2001031900043 20010319 00043 NM 2001 3 19 USAA010116 1 20010205 A 5320 FLOOR SUPPORT BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND FLOOR SUPPORT CRACKED 1 INCH, STATION 540. REPLACED FLOOR SUPPORT PER SRM 51-10-01. (M) 2 L 7 2 4F A16WE 2001031900044 20010319 00044 NM 2001 3 19 USAA010136 1 20010212 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND SKIN CRACKED 1 INCH, FS 785 AT STRINGER 19L. INSTALLED DOUBLER PER EA 69066. (M) 2 L 7 2 4F A16WE 2001031900045 20010319 00045 NM 2001 3 19 UPS01235091 1 20010227 A 3510 REGULATOR BOEING 727 727247 138408F NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 210UP 21697 INSPECTION TYPE:N/A, O2 REGULATOR AT F/O POSITION WILL NOT INDICATE FLOW DURING MASK TEST. *S/D* REMOVED AND REPLACED F/O''S REGULATOR O2, OPS CHECKED AND LEAK CHECKED GOOD. 2 L 7 3 4F A3WE 2001031900046 20010319 00046 NM 2001 3 19 UPS01235099 1 20010213 A 2760 LINK BOEING 727 72722C 138400F NM NR6 SPOILER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, SURFACE CORROSION ON NR 6 SPOILER ACTUATING LINKAGE. REPLACED ACTUATOR LINKAGE IAW MM 27-61-01. 2 L 7 3 4F A3WE 2001031900047 20010319 00047 EA 2001 3 19 COMA0160256 1 20010217 A 2750 FLAP CNDAIR CL600 CL6002B19 EA WING FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 821CA 7420 FLAPS FAILED AT ZERO DURING APPROACH. RESET THE FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2001031900048 20010319 00048 NM 2001 3 19 TWAA0103206 1 20010219 A 3350 LIGHT BOEING 767 7673Q8 NM CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 634TW 28132 THE EGRESS LIGHT STRIP WAS INOPERATIVE AT ROWS 10 TO 14, RT SIDE OF CABIN. RECONNECTED WIRING THAT HAD BECOME DISCONNEC TED. CHECK-C 10-25-00 LAX. 2 L 7 2 4F RT A1NM 2001031900049 20010319 00049 NM 2001 3 19 UPS01435084 1 20010121 A 5315 FLOORBEAM BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, CORROSION ON UPPER SURFACE OF HORIZ FLANGE MAIN CABIN FLOORBEAM AT BS 260 BETWEEN RBL 35 AND RBL 48. REPAIRS ACCOMPLISHED PER FLS QUERY NOTE 17 / 01 REFERENCE ALSO QUERY NOTE 19 / 01. 2 L 7 4 4F A20WE 2001031900050 20010319 00050 NM 2001 3 19 UPS01435086 1 20010201 A 5312 BULKHEAD BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, 2 INCH CRACK FOUND BS 260 CANTED BULKHEAD AT UPPER EDGE LT SIDE. REPAIR ACCOMPLISHED IN ACCORDANCE W ITH QUERY NOTE 17 / 01. 2 L 7 4 4F A20WE 2001031900051 20010319 00051 NM 2001 3 19 UPS01435089 1 20010112 A 5315 FLOORBEAM BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, CORROSION BEYOND LIMITS AT FLOORBEAM BS 1720 BETWEEN LBL 85 AND LBL 98. NEW SECTION SPLICED IN PER Q / NOTE 9/01. 2 L 7 4 4F A20WE 2001031900052 20010319 00052 WP 2001 3 19 UPS01835076 1 20010221 A 5330 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP STA 1668 SKIN IS BULGED RT SIDE OF A/C, STA 1655 BETWEEN LONG 29R AND 30R INTERNAL DOUBLER IS CORRODE D BEYOND LIMITS. REPAIRED DOUBLER IAW 8110-3 APPROVED DH SK 803-121. 2 L 7 4 4F RT 4A25 2001031900053 20010319 00053 WP 2001 3 19 UPS01835093 1 20010227 A 3150 RELAY DOUG DC8 DC871F 302199D WP COCKPIT FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:N/A, CREW PREFLT-MASTER WARNING LIGHT FAILS TO RESET. REMOVED AND REPLACED R2-94 RELAY R2-100. 2 L 7 4 4F RT 4A25 2001031900054 20010319 00054 EU 2001 3 19 2001UALA00109 1 20010112 A 2934 C60AA0062 SWITCH AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYDRAULIC SYS MALFUNCTIONED A UALA O OTHER J WARNING INDICATION LD LANDING 1 WP 29 443UA 10411 820 LANDED UNDER AMBER DUE TO LOSS OF THE GREEN HYDRAULIC SYSTEM. *S/D* SERVICED GREEN SYSTEM TO FULL LEVEL AND RAN SYSTEM FOR 4 CONTINUOUS HOURS. DUE TO NO POSITIVE DISCREPANCIES FOUND WITH GREEN HYDRAULIC SYSTEM QUANTITY INDICATION, REPLAC ED THE RESERVOIR LOW LEVEL SWITCH AS PRECAUTIONARY. 2 L 7 2 4F 4 F RT A28NM E40NE 2001031900057 20010319 00057 NM 2001 3 19 UPS01235096 1 20010227 A 3350 LIGHT BOEING 727 72727C 138400J NM COCKPIT MALFUNCTIONED A IPXA K NONE O OTHER UK UNKNOWN 1 SO 01 908UP 19114 INSPECTION TYPE:AS-E INFLIGHT, EMERGENCY EXIT LIGHTS ILLUMINATED FOR APPROX 2 MINUTES, THEN EXTINGUISHED. SWITCH WAS C HECKED TO BE IN ARMED THE ENTIRE TIME. UNABLE TO DUPLICATE PROBLEM. TESTED NORMAL PER MM 33-50-101. 2 L 7 3 4F A3WE 2001031900058 20010319 00058 NM 2001 3 19 UPS01235097 1 20010212 A 5310 BEAM BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, APB 1183 VERT BEAM AT LBL 26.83 HAS A CRACK RUNNING FROM FLANGE LIGHTENING HOLE AT WL 258. REPAIR ED PER APPENDIX D OF EO B727-5311-0651 & BOEING DRWG 65C34406. 2 L 7 3 4F A3WE 2001031900059 20010319 00059 NM 2001 3 19 UPS01235098 1 20010213 A 2760 BOLT BOEING 727 72722C 138400F NM NR7 SPOILER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, NR 7 SPOILER ACTUATING LINKAGE BOLT CORRODED. REPLACED BOLT AND LINKAGE IAW MM 27-61-01. 2 L 7 3 4F A3WE 2001031900060 20010319 00060 NM 2001 3 19 UPS01235100 1 20010213 A 2760 LINK BOEING 727 72722C 138400F NM NR7 SPOILER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, SURFACE CORROSION ON NR 7 SPOILER ACTUATING LINKAGE. LINKAGE REPLACED IAW MM 27-61-01. 2 L 7 3 4F A3WE 2001031900061 20010319 00061 NM 2001 3 19 UPS01235101 1 20010214 A 2780 LINK BOEING 727 72722C 138400F NM NR4 KRUEGER FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, NR 4 KRUEGER FLAP O/B LINK CORRODED AT O/B SIDE. REPLACED LINK IAW OHM 20-50-01. 2 L 7 3 4F A3WE 2001031900062 20010319 00062 NM 2001 3 19 UPS01235102 1 20010215 A 5310 WEB BOEING 727 72722C 138400F NM AFT CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, CRACK IN AFT CARGO HOLD CLOSURE WEB FWD OF DOOR CUTOUT. WEB REPAIRED IAW SRM 51-40-02 PRIMER APPL IED TO WEB IAW SRM 51-20-15. 2 L 7 3 4F A3WE 2001031900063 20010319 00063 NM 2001 3 19 UPS01235103 1 20010219 A 5320 INTERCOSTAL BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, INTERCOSTAL T-PROFILE HAS CRACK AT ATTACH POINT BS 1183 VERT BEAM LBL 17.8 WL 283. T-PIECE REPLAC ED IAW SRM 51-30-2, FABRICATED IAW BOEING DWG 65C34406. 2 L 7 3 4F A3WE 2001031900065 20010319 00065 NM 2001 3 19 UPS01235104 1 20010216 A 5552 BRACKET BOEING 727 72722C 138400F NM LT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, LT ELEV POSITION SENSOR BRACKET ON FRONT SPAR CRACKED. REPLACED IAW MM 20-80-01. 2 L 7 3 4F A3WE 2001031900066 20010319 00066 NM 2001 3 19 UPS01235110 1 20010228 A 3350 BATTERY BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:IN, EMERGENCY EXIT LIGHTS INOP ON LT OVERWING LIGHTS AND LT REAR EMERGENCY EXIT LIGHT NEXT TO LAV DOOR. REMOVED AND REPLACED BATTERIES, OPS CHECK GOOD. 2 L 7 3 4F A3WE 2001031900071 20010319 00071 NM 2001 3 19 USAA010162 1 20010110 A 7120 CROSSBEAM BOEING 737 7373B7 1384580 NM ENG MOUNT CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 5646 23315 PIT - FOUND ENGINE MOUNT CROSSBEAM CORRODED, BEARING BORE OF CROSS BEAM. CORROSION LEVEL 1. ENLARGED BORE .010 CHANFER ED BORE, MPI ROTO PEEN. INSTALLED OVERSIZED BEARING PER TYP REP 54-50-09. (M) 2 L 7 2 4F RT A16WE 2001031900072 20010319 00072 NM 2001 3 19 VNAA0101024 1 20010127 A 2750 CONTROLLER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 461PS 3075 AFTER TAKING THE RUNWAY, THE CREW RECEIVED A FLAP CONTROL FAIL CAS MESSAGE AND ABORTED TAKEOFF. MAINTENANCE INSPECTED A ND RESET THE FLAP CONTROL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001031900073 20010319 00073 NM 2001 3 19 AWXA0001421 1 20010227 A 5320 6936677 INTERCOSTAL BOEING 737 7373S3 1384711 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 AT STA 927 STR 26R INTERCOSTAL HAS EXFOLIATION ON LOWER LEG. REMOVED DAMAGED INTERCOSTAL IAW SRM 51-40-02; FABED INTERC OSTAL IAW SRM 51-20-01; INSTALLED INTERCOSTAL IAW 51-40-02. 2 L 7 2 4F RT A16WE 2001031900083 20010319 00083 EU 2001 3 19 AWXA0001420 1 20010227 A 5520 D5528000100159 ELEVATOR AIRBUS 320 A320231 3930325 EU RT ELEVATOR DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 ON REMOVAL OF RT ELEVATOR ABNORMAL SHEAR LOAD NOTED ON ELEVATOR ATTACH BOLTS AND ELEVATOR HINGE BEARINGS FOUND TO BE MIS ALIGNED. COMPLIED WITH AWA ER 26-5552-01054-DL2; ELEVATOR REPLACED IAW AMM 27-34-41-401. 2 L 7 2 4F RT A28NM 2001031900086 20010319 00086 NM 2001 3 19 UPS01434743 1 20010102 A 2550 GUARD BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, MAIN DECK CARGO PROFILE INDICATORS ARE CRACKED AT BS 1720 LT AND RT SIDES, LT MAX CARGO PROFILE INDI CATOR CENTER ATTACH BRACKET TO FUSELAGE FRAME IS CRACKED. NEW PROFILE GUARDS FABRICATED IAW SRM 51-20-01 AND SRM 51-30 -02. 2 L 7 4 4F A20WE 2001031900100 20010319 00100 NM 2001 3 19 TSAA0153012 1 20010209 A 5311 65C3372247 FRAME BOEING 737 7372M6C 1384708 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 FOUND IDENTIFIED CRACK AT BS 727, STRINGER 18L UPPER CHORD BY UTILIZING HFEC METHOD. (M) 2 L 7 2 4F RT A16WE 2001031900101 20010319 00101 NM 2001 3 19 USAA010171 1 20010202 A 5542 SKIN BOEING 737 7373B7 1384580 NM RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 519AU 40839 23705 PIT - FOUND SKIN WORN .25 INCH BY .5 INCH THROUGH 4 PLIES, RUDDER STATION 0.0 RT SIDE LEADING EDGE. STEP SAND INSTALLED 6 LAY OF CLOTH CURED 200-230 FINISHED PER APPEAR MN PER EA 70006 AND SRM 51-70-17. (M) 2 L 7 2 4F RT A16WE 2001031900102 20010319 00102 NM 2001 3 19 USAA010108 1 20010205 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46235 22950 TPA - FOUND SKIN CRACKED .5 INCH, FUSELAGE SKIN AT EQUIP COOLING OUTLET STATION 380. INSTALLED DOUBLER PER EA 69090A. (M) 2 L 7 2 4F RT A16WE 2001031900103 20010319 00103 NM 2001 3 19 USAA010126 1 20010206 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 32258 24554 CLT - FOUND FRAME .5 INCH, STATION 867 BETWEEN STRINGER 9L AND 8L. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001031900104 20010319 00104 NM 2001 3 19 USAA010127 1 20010206 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 32258 24554 CLT - FOUND FRAME CRACKED .5 INCH, STATION 727F BETWEEN STRINGER 9L AND 8L. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001031900105 20010319 00105 NM 2001 3 19 USAA010165 1 20010123 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 23555 PIT - FOUND BEAM CORRODED 1 INCH BY 4 INCHES BY .017 INCH, DECK STRUCTURE 810 LBBL AFT STATION 727D. CORROSION LEVEL 1, TASK NR C53-202-01. INSTALLED DOUBLER PER TYP REPAIR 53-10-20. (M) 2 L 7 2 4F RT A16WE 2001031900106 20010319 00106 WP 2001 3 19 01FDEA00144 1 20010219 A 5230 HANDLE DOUG DC10 DC1030F 3023504 WP MID CARGO BAY MISSING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 310FE 48299 ON WALK-AROUND FOUND CTR LWR CARGO VENT PANEL HANDLE ACCESS MISSING. INSTALLED VENT PANEL HANDLE ACCESS DOOR PER STANDA RD PRACTICE, OPS CK GOOD. 2 L 7 3 4F RT A22WE 2001031900107 20010319 00107 EU 2001 3 19 01FDEA00145 1 20010219 A 2780 SLAT AIRBUS 310 A310222 3930315 EU WING MALFUNCTIONED A FDEA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 25 416FE 288 ON APPROACH RECD SLAT FAULT AS HANDLE WAS MOVED TO EXTEND SLATS. RECYCLED, NO HELP. BOTH SFCC 1 & 2 SHOW JAM ON SLATS. SFCC''S RESET FLAPS AND SLAT CYCLED. NO FURTHER FAULTS. JACK SCREWS SERVICED PER IAW AMM 12-13-27-0 PG 30. NO EVIDE NCE OF WATER CONTAMINATION. 2 L 7 2 4F RT A35EU 2001031900108 20010319 00108 NM 2001 3 19 01FDEA00147 1 20010220 A 2781 SWITCH BOEING 727 727233 138408A NM NR 3 SLAT FAILED A FDEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 25 281FE 22348 ON APPROACH WHEN SEL FLAPS 5 AMBER LIGHT ON FRONT PNL REMAIN ILLUM. NR 3 LEAD EDGE FLAP ON POS IND SHOW NOT DEPLOYED. REMOVED AND REPLACED NR 3 LEAD EDGE FLAP SWITCH PER MM 27-82-011-4, GOOD PER MM 27-81-000-5. 2 L 7 3 4F RT A3WE 2001031900110 20010319 00110 NM 2001 3 19 USAA010166 1 20010123 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 38667 23555 PIT - FOUND BEAM CORRODED 1 INCH BY 5 INCHES BY .011 INCH, FLOOR DECK SUPPORT 810 LBBL AFT OF STATION 767. CORROSION LE VEL 1, TASK NR C53-202-01. INSTALLED DOUBLER PER TYP REPAIR 53-10-068. (M) 2 L 7 2 4F RT A16WE 2001031900111 20010319 00111 NM 2001 3 19 USAA010167 1 20010123 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 38667 23555 PIT - FOUND BEAM CORRODED 1 INCH BY 4 INCHES BY .016 INCH, FLOOR DECK SUPPORT 810 RBBL AFT OF STATION 767. CORROSION LE VEL 1, TASK NR C53-202-01. INSTALLED DOUBLER PER TYP REPAIR 53-10-068. (M) 2 L 7 2 4F RT A16WE 2001031900112 20010319 00112 NM 2001 3 19 USAA010168 1 20010123 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 38667 23555 PIT - FOUND SUPPORT BEAM CORRODED 1 INCH BY 4 INCHES BY .011 INCH, FLOOR DECK SUPPORT 300 LBBL AFT STATION 767. CORROSI ON LEVEL 1, TASK NR C53-202-01. INSTALLED DOUBLER PER TYP REP 53-10-06B. (M) 2 L 7 2 4F RT A16WE 2001031900113 20010319 00113 NM 2001 3 19 USAA010169 1 20010123 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 38667 23555 PIT - FOUND BEAM CORRODED 1 INCH BY 4 INCHES BY .014 INCH, FLOOR DECK SUPPORT 1250 LBBL AFT STATION 767. CORROSION LEVE L 1, TASK C53-202-01. INSTALLED DOUBLER PER TYP REPAIR 53-10-06B. (M) 2 L 7 2 4F RT A16WE 2001031900114 20010319 00114 NM 2001 3 19 USAA010109 1 20010205 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 32258 24554 CLT - FOUND FLOORBEAM CORRODED 1 INCH BY 6 INCHES, STATION 344, BL 0 TO RBL 6. INSTALLED T-CAP PER 53-10-51 FIG 205. C ORROSION LEVEL 1. (M) 2 L 7 2 4F RT A16WE 2001031900115 20010319 00115 NM 2001 3 19 USAA010110 1 20010205 A 5313 STRINGER BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 32258 24554 CLT - FOUND STRINGER CORRODED .5 INCH BY 4 INCHES, BS 500F PLUS 13 INCHES TO 17 INCHES, STRINGER 26L OUTBOARD UPPER FLAN GE. REPAIRED PER SRM 53-00-03. CORROSION LEVEL 1 C53-208-01. (M) 2 L 7 2 4F RT A16WE 2001031900116 20010319 00116 NM 2001 3 19 USAA010111 1 20010205 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 520AU 40659 23706 CLT - FOUND T-CAP CORRODED 70 INCHES, RBL 46 TO LBL 48. REPLACED T-CAP PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2001031900117 20010319 00117 NM 2001 3 19 USAA010130 1 20010206 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 32258 24554 CLT - FOUND T-CAP CORRODED 1 INCH, STATION 312, 7 INCHES LEFT CENTER. CORROSION LEVEL 2 C53-107-02. INSTALLED NEW T-CA P PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2001031900118 20010319 00118 NM 2001 3 19 USAA010129 1 20010206 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 32258 24554 CLT - FOUND T-CAP CORRODED 1 INCH, STATION 312, 15 INCHES LEFT OF CENTER. CORROSION LEVEL 2 C53-107-02. INSTALLED NEW T-CAP PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2001031900119 20010319 00119 NM 2001 3 19 USAA010128 1 20010206 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 32258 24554 CLT - FOUND FLOORBEAM CORRODED 20 INCHES, FLOORBEAM 986.5 UPPER CHORD FROM LBL 51 TO RBL 51. REMOVED AND REPLACED UPPER CHORD PER TR 53-60-01 A. (M) 2 L 7 2 4F RT A16WE 2001031900120 20010319 00120 NE 2001 3 19 USAASB01032 2 20010201 A 7200 COMPRESSOR BOEING 737 737201 1384454 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE STALLED A USAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 EA 19 254AU 39971 968 22796 709061 CLT - FLT 2676 - EN ROUTE FROM TPA TO LGA, AT FL330, CAPTAIN REPORTED THAT THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STAL L. NO ENGINE PARAMETERS WERE EXCEEDED. THROTTLE WAS REDUCED AND THE ENGINE RAN NORMALLY AFTER THE INITIAL STALL. FLIG HT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED TH E NR 2 ENGIEN ASSEMBLY PER JOB CARD. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F 4 F A16WE E2EA 2001031900121 20010319 00121 EU 2001 3 19 SIMA0242 1 20010124 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 272AE 340B272 BOS - OVERHEAD EMERGENCY LIGHTS AT SEATS 7A, 8A, AND 10A ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY UNIT 22LN. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001031900122 20010319 00122 EU 2001 3 19 SIMA0224 1 20010122 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN LOOSE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 905AE 340B319 HOU - FLT 3613 - FLOOR PROXIMITY LIGHT AT 5BC IS INOPERATIVE. PUT ON MEL AT THIS TIME. MAINTENANCE FOUND BULB LOOSE IN SOCKET. BULB WAS RESECURED INTO ASSEMBLY. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001031900123 20010319 00123 NM 2001 3 19 20010316SG002 1 20010114 A 2750 285N001132 FSEU BOEING 757 75723A 1384967 NM FLAPS FAILED A N8TA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 WP 19 757NA 24567 ON APPROACH WHEN FLAPS 30 WAS SELECTED FLAPS WOULD NOT EXTEND BEYOND 25, LEADING EDGE LIGHT CAME ON. NORMAL FLAPS 25 LA NDING ACCOMPLISHED. ADJUSTED SLAT 5 LOSS SENSING SENSOR AND REPLACED FSEU. (M) 2 L 7 2 4F RT A2NM 2001031900124 20010319 00124 NM 2001 3 19 01FDEA00149 1 20010216 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM CABIN CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DURING ROUTINE INSP, NR 2 MAIN CABIN SEAT TRACK FOUND CORRODED AT BS 825. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 53-10-5. 2 L 7 3 4F A3WE 2001031900126 20010319 00126 NM 2001 3 19 01FDEA00151 1 20010216 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM CABIN CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DUR ROUTINE INSP NR 3 MAIN CABIN SEAT TRACK FOUND CORRODED FROM BS 420 - 440. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 53-10-5. 2 L 7 3 4F A3WE 2001031900127 20010319 00127 NM 2001 3 19 01FDEA00154 1 20010216 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM CABIN CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DURING ROUTINE INSP NR 3 MAIN CABIN SEAT TRACK FOUND CORRODED AT BS 837. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 7 27 SRM 53-10-5. 2 L 7 3 4F A3WE 2001031900129 20010319 00129 NM 2001 3 19 20010316SG003 1 20010205 A 3150 WARNING SYSTEM BOEING 757 75728A 1384976 NM COCKPIT ACTIVATED A N8TA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 19 517NA 24260 UPON CLIMBING THROUGH 9,000 FEET, LOWER EICAS MESSAGE, FLT DATA ACC ILLUMINATED. AIRCRAFT ACCOMPLISHED UNSCHEDULED LAND ING AT ORGINATION STATION. REASON FOR RETURN IS THAT JUST PRIOR TO DEPARTURE THE CVR HAD BEEN PLACED ON MEL STATUS. AC COMPLISHED TEST PROCEDURE ON FDAU, NO FAULTS FOUND. CLEARED MESSAGE, PERFORMED OPS CHECK. SYSTEM OPS CHECKED GOOD. AI RCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A2NM 2001031900130 20010319 00130 NM 2001 3 19 20010316SG004 1 20010214 A 3350 10005511 LIGHT DHAV DHC8 DHC8103 1386005 NM COCKPIT INOPERATIVE A KPVA K NONE L NO TEST IN INSP/MAINT 1 WP 13 807WP 77 023 DURING MAINTENANCE, COCKPIT EMERGENCY LIGHT DID NOT TEST. REMOVED AND REPLACED (PORTABLE EMERGENCY) LIGHT ASSY. OPS CH ECK GOOD IAW PSM 1-8-2 CHAPTER 33-51-00 PAGE 201-202. (M) 2 H 7 2 4T RT A13NM 2001031900131 20010319 00131 NM 2001 3 19 20010316SG005 1 20010208 A 7170 2525150 DRAIN VALVE BOEING 757 757236 NM RT ENGINE INOPERATIVE A N8TA O OTHER O OTHER NR NOT REPORTED 1 WP 19 547NA 29946 RIGHT ENGINE DID NOT SHUTDOWN WITH FUEL CONTROL SWITCH (2 ATTEMPTS), PULLED FIRE HANDLE. ENGINE STILL DID NOT SHUTDOWN. RECYCLED FUEL SWITCHES AGAIN, ENGINE SHUTDOWN. REPLACED PRESSURIZING AND DRAIN VALVE, OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A2NM 2001031900136 20010319 00136 NM 2001 3 19 F3LA200100024 1 20010219 A 5315 FLOORBEAM BOEING 737 7373S1 138447S NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 3095 24856 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT FUSELAGE FLOORBEAM AT STA 947.5. MAINTENANCE REMOVED FLOORBEAM, FABRICATED, TREATED, PRIMED AND INSTALLED REPLACEMENT FLOORBEAM PER SRM 53-00-51. 2 L 7 2 4F RT A16WE 2001031900137 20010319 00137 EA 2001 3 19 COMA0160255 1 20010214 A 3222 35333601364A SEAL CNDAIR CL600 CL6002B19 EA NLG DEFECTIVE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 977CA 7157 WHEN AIRCRAFT DEPARTED CKB A GEAR DISAGREE WARNING, NOSE DOOR OPEN WARNING AND A NOSE WHEEL STEERING INOP CAUTION FOLLOW ED BY A WOW INPUT CAUTION. INVESTIGATED AND FOUND NLG STRUT WOULD NOT FULLY EXTEND DUE TO DEFECTIVE O-RING SEAL ON LOWE R BEARING AND FLOATING PISTON. INSTALLED SERVICEABLE SEALS ON LOWER BEARING AND PISTON IAW CRJ AMM 32-21-20-400-801 AND 32-21-25-400-801. 2 L 7 2 4F RT A21EA 2001031900138 20010319 00138 NM 2001 3 19 F3LA200100025 1 20010219 A 5320 FLOOR SUPPORT BOEING 737 7373S1 138447S NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 3095 24856 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT FUSELAGE FLOOR SUPPORT AT LBL 24, STA 947.5 TO 967. MAINTENANCE REMOVED AFT FUSELAGE FLOOR SUPPORT, TREATED, PRIMED AND INSTALLED NEW FLOOR SUPPORT PER SRM 53-60-51. 2 L 7 2 4F RT A16WE 2001031900139 20010319 00139 WP 2001 3 19 TWAA0103201 1 20010219 A 3350 58222 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9405T 53141 THE EGRESS LIGHTS WERE INOPERATIVE FROM CABIN ROW 7 TO 20. REPLACED THE BATTERY PACK. CHECK-C 10-23-00 STL. 2 L 7 2 4F RT A6WE 2001031900140 20010319 00140 NM 2001 3 19 TWAA0103202 1 20010216 A 3350 LIGHT BOEING 767 7673Q8 NM CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 634TW 28132 THE LOWER AFT RT SIDE EMERGENCY LIGHT, THE L2 CABIN DOOR EXTERIOR EMERGENCY LIGHT, THE EGRESS LIGHTS ROWS 24 TO 27 RT SI DE, AND MID GALLEY AFT BULKHEAD EGRESS LIGHTS WERE INOPERATIVE. RESET THE LAMP BASE FOR BOTH OF THE INOPERATIVE EMERGEN CY LIGHTS, RECONNECTED THE EGRESS WIRING FOR ROW 24 TO 27, AND RECONECTED WIRING FOR THE MID GALLEY EGRESS LIGHTS. CHEC K-C 10-25-00 LAX. 2 L 7 2 4F RT A1NM 2001031900148 20010319 00148 NM 2001 3 19 TWAA0103203 1 20010216 A 3350 0201720001 LIGHT BOEING 717 717200 1383700 NM CABIN MISSING A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 408TW 55075 THE EGRESS LIGHT WAS MISSING FROM THE SEAT AT ROW 3D AND 9D. REPLACED THE LIGHT, P/N 0201720-001, AND THE LENS, P/N 020 1804-001, AT BOTH LOCATIONS. NO CHECK-C AS YET. 2 L 7 2 4F TR A6WE 2001031900149 20010319 00149 WP 2001 3 19 TWAA0103204 1 20010217 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 920TW 49369 THE EGRESS LIGHTS ROW 1 TO 5, AFT OVERWING EMERGENCY EXIT SIGNS, AND THE EGRESS LIGHTS ROWS 30 TO 33, WERE INOPERATIVE. DRIED WATER IN TRACKS FOR FWD CABIN EGRESS LIGHTS, REPLACED THE BATTERIES FOR THE OVERWING SIGN P/N 408822-101, AND (AF TER MAINTENANCE FERRY TO STL). REPAIRED FEEDER STRIP AT ROW 33 AND 2W WIRES AT 3-901 IN OVERHEAD FOR THE LIGHTS AT ROWS 30 TO 33. CHECK-C 9-20-00 MCI. 2 L 7 2 4F A6WE 2001031900150 20010319 00150 NM 2001 3 19 TWAA0103205 1 20010219 A 3350 80741 LIGHT BOEING 767 7673Q8 NM CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 634TW 28132 THE EGRESS LIGHTS WERE INOPERATIVE FROM CABIN ROW 16 TO 20, RT SIDE OF CABIN. REPLACED LAMP AT SEAT 16, AND REATTACHED WIRES AT SEATS 17 AND 19. CHECK-C 10-25-00 LAX. 2 L 7 2 4F RT A1NM 2001031900151 20010319 00151 NM 2001 3 19 TWAA0103207 1 20010218 A 3350 807331 LIGHT BOEING 767 7673Y0 NM CABIN MISSING A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 638TW 26205 THE EGRESS LIGHT STRIP OPPOSITE THE LT CENTER LAV WAS MISSING, AND THE STRIP OPPOSITE THE CENTER RT LAV WAS INOPERATIVE. REPLACED BOTH LIGHT STRIPS. CHECK-C 2-23-00. 2 L 7 2 4F RT A1NM 2001031900152 20010319 00152 NM 2001 3 19 F3LA200100026 1 20010219 A 5320 FLOOR SUPPORT BOEING 737 7373S1 138447S NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 3095 24856 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT FUSELAGE FLOOR SUPPORT AT LBL 3, STA 947.5 TO 967. MAINTENANCE R EMOVED AFT FUSELAGE FLOOR SUPPORT, TREATED, PRIMED AND INSTALLED NEW FLOOR SUPPORT PER EA 53-737-113. 2 L 7 2 4F RT A16WE 2001031900153 20010319 00153 NM 2001 3 19 F3LA200100037 1 20010225 A 2810 2800003103 RELIEF VALVE BOEING 737 737228 13844AG NM LT WING FAILED A F3LA A UNSCHED LANDING K FLUID LOSS TO TAKEOFF 1 NM 03 234TR 23004 AIR TURNBACK. FLIGHT CREW REPORTED FUEL LEAK FROM LT WING ON TAKEOFF AND CLIMB. FOUND LT WING SURGE TANK RELIEF VALVE FAILED OPEN AND REPLACED SAME PER MM 28-13-41. 2 L 7 2 4F RT A16WE 2001031900168 20010319 00168 EU 2001 3 19 MALA010203 1 20010215 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 425XJ 425 FOUND DURING 4K HEAVY INSPECTION, FOUND HEAVY CORROSION ON LT CENTER AISLE SEAT TRACK LBL 18.3 FROM STA 297 TO STA 378. COMPLETED REAIR IAW EO53060. 2 L 7 2 4T RT A52EU 2001031900175 20010319 00175 EA 2001 3 19 COMA0160258 1 20010214 A 3222 16100105 STRUT CNDAIR CL600 CL6002B19 EA NLG LEAKING A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 977CA 10149 7157 GEAR DISAGREE WARNING, WOW INPUT WARNING. RESEALED NLG SHOCK STRUT AND SERVICED TO M/M SPECIFICATIONS. 2 L 7 2 4F RT A21EA 2001031900176 20010319 00176 EA 2001 3 19 COMA0160265 1 20010218 A 5530 600210615 BUSHING CNDAIR CNDAIR CL600 CL6002B19 EA LT&RT VERT STAB SCORED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 912CA 7011 LT AND RT BUSHINGS (P/N 600-21061-5) IN VERTICAL STABILIZER WAS FOUND TO BE SCORED DURING INCORPORATION OF COMAIR EO 55- 007. REPLACED LT AND RT BUSHING IN VERTICAL STABILIZER WITH (P/N 600-21061-7) IAW CRJ AMM 20-26-00-910-803, CRJ DRWG 60 0-23068 AND WVAC EO 601R-55-2236. 2 L 7 2 4F RT A21EA 2001031900181 20010319 00181 2001 3 19 DHL2001362006 4 20010220 A 3416 2594620915 ALTIMETER AIRBUS 300 A300B4103 3930104 EU COCKPIT FAILED A DHLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 362DH 84 DURING TAXI-OUT, FLAG INST ON MWP WITH CAPTAINS OFF FLAG ON ALTIMETER. REMOVED AND REPLACED CAPT ALTIMETER INDICATOR. OPS CHECK OK PER MM 34-11-30. 2 L 7 2 4F RT A35EU 2001031900182 20010319 00182 NM 2001 3 19 2001UALA00059 1 20010127 A 3610 REGULATOR ALIDSG 1074923 BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE BLEED AIR FAILED A UALA A UNSCHED LANDING O OTHER TO TAKEOFF 1 WP 29 915UA 25382 856126 RETURNED TO DEN DUE TO A PROBLEM WITH THE NR 1 BLEED AIR SYSTEM. *S/D* BLEED AIR VALVE WOULD NOT OPEN AFTER BLEEDS OFF TAKEOFF. REPLACED THE BLEED AIR REGULATOR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001031900183 20010319 00183 NM 2001 3 19 2001UALA00070 1 20010201 A 2751 INDICATOR 1812996 BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE COCKPIT FAILED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 WP 29 904UA 20888 25004 FLAP EXTENSION PROBLEM. *S/D* REPLACED FLAP POSITION INDICATOR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001031900184 20010319 00184 EU 2001 3 19 2001UALA00114 1 20010214 A 2913 693335 PUMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYDRAULIC SYS OVERHEATED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 426UA 510 BLUE SYSTEM HYDRAULICS ELECTRIC PUMP OVERHEATED. *S/D* REPLACED BLUE SYSTEM ELECTRIC HYDRAULIC PUMP. SYSTEM CHECKS N ORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2001031900185 20010319 00185 WP 2001 3 19 IXXA0100005 1 20010212 A 5280 56489332 DOOR DOUG DC8 DC862 3021970 WP RT MLG MISSING A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 79428 187 45918 AFTER AN UNEVENTFUL LANDING AND DURING POST FLIGHT INSPECTION AT WRI. MAINTENANCE FOUND THE RIGHT MAIN LANDING GEAR LOW ER FLYING DOOR MISSING FROM THE GEAR. NO OTHER DAMAGE TO THE AIRCRAFT WAS NOTED. THE AIRCRAFT WAS FERRIED TO A MAINTEN ANCE FACILITY FOR REPAIRS. THE MAINTENANCE FACILITY REPLACED THE LOWER FLYING DOOR AND PERFORMED A SUCCESSFUL OPERATION AL CHECK IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2001031900186 20010319 00186 EU 2001 3 19 MALA010193 1 20010204 A 5320 INTERCOSTAL SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 423XJ 423 FOUND DURING C-CHECK, CORROSION ON TOP FLANGE OF INTERCOSTAL AT LBL10.0 BETWEEN FRAMES AT STATIONS 236.5 AND 258.0 BELOW FLOOR AREA. REFER TO CELSIUS W/0 193,TASK 1509. MAINTENANCE REMOVED CORROSION OUT OF LIMIT FROM TOP FLANGE OF INTERCO STAL. FABRICATED NEW FLANGE IAW SRM 51-20-42/43. APPLIED TOPCOAT AND INSTALLED WET SEALED IAW SRM 51-20-41. 2 L 7 2 4T RT A52EU 2001031900187 20010319 00187 EU 2001 3 19 MALA010194 1 20010204 A 5320 ANGLE SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 423XJ 423 FOUND DURING C-CHECK, CORROSION ON UPPER ANGLE OF FRAME STA 236.5. REFER TO CELSIUS W/O 19317, TASK 1510. MAINTENANCE REMOVED CORROSION, OUT OF LIMITS ON UPPER ANGLE FRAME 236.5. FABRICATED NEW ANGLE IAW SRM 51-40-21, 51-20-30. ALODINE AND PRIMED PARTS IAW SRM 51-20-42/43. APPLIED TOPCOAT AND INSTALLED WET SEAL IAW SRM 51-20-41. 2 L 7 2 4T RT A52EU 2001031900188 20010319 00188 EU 2001 3 19 MALA010197 1 20010205 A 5320 ANGLE SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 423XJ 423 FOUND DURING C-CHECK, CARGO FLOOR TRIM ANGLE IS CORRODED. REFER TO CELSIUS W/O 19317, TASK 2585. MAINTENANCE REMOVED C ORROSION IAW SRM 51-10-10. ALODINED IAW SRM 51-20-42. MATERIALS REMAINING OUT OF LIMITS REF SRM 51-10-10. FABRICATED NEW ANGLE SAME AS ORIGINAL PER SAMPLE 2024T3.050, TREATED AND PRIMED IAW SRM 51-20-42/43, INSTALLED SRM 51-20-42. 2 L 7 2 4T RT A52EU 2001031900189 20010319 00189 EU 2001 3 19 MALA010199 1 20010206 A 5753 FLAP SAAB SF340 340B 7860101 EU LT WING CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 423XJ 423 FOUND DURING C-CHECK, LT FLAP PANEL 541 AT CHAFED AT THE AFT EDGE. REFER TO CELSIUS W/O 19317, TASK 5523 AND SAAB STATE MENT 72SAS1691, AND SB34-57-012. MAINTENANCE SMOOTHED, CHECKED LIMIT. CHAFE DAMAGE IS OUT OF ALLOWABLE LIMIT REF: SAAB SRM51-10-10. FOUND TO BE WITHIN LIMITS AS GIVEN IN SAAB STATEMENT 72SAS1691 AND SB34-57-012. NDTPERFFVNDT006EDDY CURR ENT NO CRACKS NOTED. FABRICATED NEW CHAFE STRIP FROM .004 SHIM STOCK AND INSTALLED CHAFE STRIP IAW SAAB STATEMENT 72SAS 1691. 2 L 7 2 4T RT A52EU 2001031900190 20010319 00190 EU 2001 3 19 MALA010200 1 20010207 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 423XJ 423 FOUND DURING C-CHECK, SERIES OF 34 DENTS IN RT FUSELAGE SKIN AT STA 351.0 WL 90.5. REFER TO CELSIUS W/O 19317, TASK 253 6, AND SAAB STATEMENT 340SDS000925. MAINTENANCE CHECK LIMITS, FOUND DENTS OUT OF ALLOWABLE LIMIT REF SAAB SRM 51-10-10/ DENT TYPE 1 AND 2, LESS THAN 4L APART. NO CRACKS NOTED IAW FFVNDT006. FABRICATED, LOCATED, DRILLED AND TRIMMED 1 REPA IR DOUBLER AND TRIPLER IAW SRM 53-70-10. TREATED, PRIMED AND TOPCOATED IAW SRM 51-20-42/43. INSTALLED DOUBLER IAW SRM 51-40-21 AND SAAB STATEMENT 340SDS000925. FOR PAINT TOUCH UP SEE W/O 19317 TASK 2514, IPM 12 FORM 25. 2 L 7 2 4T RT A52EU 2001031900191 20010319 00191 EU 2001 3 19 MALA010201 1 20010207 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 423XJ 423 FOUND DURING C-CHECK, SERIES OF EIGHT DENTS ON RT FUSELAGE SKIN AT STA 345, WL 67.0. REFER TO CELSIUS W/O 19317, TASK 1 521 AND SAAB STATEMENT 340SDS000925. MAINTENANCE CHECKED LIMI, FOUND DENTS OUT OF ALLOWABLE LIMIT REF SRM 51-10-10 LESS THAN 4L APART. NO CRACKS NOTED IAW FFVNDT006. DENTS ARE ACCEPTED AS IS REF SAAB STATEMENT 340SDS000925. 2 L 7 2 4T RT A52EU 2001031900192 20010319 00192 EU 2001 3 19 MALA010202 1 20010215 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 425XJ 425 DURING 4K INSPECTION FOUND HEAVY CORROSION ON RT CENTER AISLE SEAT TRACK BL 0 FROM STA 297 TO STA 379. COMPLETED REPAIR IAW EO 53060. 2 L 7 2 4T RT A52EU 2001031900193 20010319 00193 EU 2001 3 19 MALA010204 1 20010221 A 3230 UPLOCK SAAB SF340 340B 7860101 EU NOSE & MLG ICED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 445XJ 445 AIR RETURN TO ESC FOR GEAR HANDLE INTRANSIT LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. MAINTENANCE INSPECTED AIR CRAFT AND FOUND ICE ON UPLOCK LATCHES. APPLIED HEAT TO LANDING GEAR, INSPECTED AIRCRAFT AND FOUND SAFE FOR A ONE TIME F ERRY FLIGHT FROM ESC TO DTW WITH LANDING GEAR DOWN AND NOT PINNED. MAINTENANCE INSPECTED LANDING GEAR, CLEANED LANDING GEAR UPLOCK SWITCHES, PERFORMED SEVERAL LANDING GEAR OPS CHECK. ALL GOOD AT THIS TIME PER SAAB 340 MM CHAP 32. 2 L 7 2 4T RT A52EU 2001031900194 20010319 00194 EU 2001 3 19 MALA010205 1 20010217 A 3230 CONNECTOR SAAB SF340 340B 7860101 EU LT MLG CONTAMINATED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 454XJ 454 AIR RETURN TO MSP. CREW REPORTED THE GEAR INTRANSIT LIGHT STAYED ON AND PUMP CONTINUED TO RUN WHEN GEAR WAS SELECTED UP . MAINTENANCE DUPLICATED FAULT, FOUND CONTAMINATION IN LT UPLOCK SWITCH CANNON PLUG. CLEANED PLUG AND FAULT IS GONE. SWUNG GEAR 10 TIMES, FAULT GONE, OPS CHECK GOOD. UNFASTENED AND REFASTENED LT O/B GEAR BAY DOOR FOR TOUBLESHOOTING. 2 L 7 2 4T RT A52EU 2001031900195 20010319 00195 EU 2001 3 19 MALA010198 1 20010206 A 5753 FLAP SAAB SF340 340B 7860101 EU RT WING CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 423XJ 423 FOUND DURING C-CHECK, RT FLAP PANEL 641AT IS CHAFED AT THE AFT END. REFER TO CELSIUS W/O 19317, TASK 6519 AND SAAB STAT EMENT 72SAS1691 AND SB 340-57-012. MAINTENANCE CHECKED LIMIT, CHAFE DAMAGE IS OUT OF ALLOWABLE LIMIT, REF SAAB SRM 51-1 0-10. FOUND TO BE WITHIN LIMITS AS GIVEN IN SAAB STATEMENT 72SAS1691 AND SB340-57-012. NDTPERFFVNDT006 EDDY CURRENT NO CRACKS NOTED. FABRICATED NEW CHAFE STRIP FROM .004 SHIM STOCK AND INSTALLED IAW SAAB STATEMENT 72SAS1691. 2 L 7 2 4T RT A52EU 2001031900196 20010319 00196 SW 2001 3 19 PNSA010102 1 20010117 A 5270 SWITCH SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR FAULTY A PNSA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 AL 03 650PA AC775B DURING CLIMB, CARGO DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO BASE. REPLACED FAULTY DOOR WARNING SWITCH. 2 L 7 2 4T RT A8SW 2001031900197 20010319 00197 SW 2001 3 19 PNSA010103 1 20010108 A 5610 WINDSHIELD PPG SWRNGN SA227 SA227AC 8780603 SW COCKPIT CRACKED A PNSA I A CABIN DEPRESSURIZATION UNSCHED LANDING O OTHER CL CLIMB 1 AL 03 640PA 268 AC759B RT WINDSHIELD CRACKED DURING CLIMB. DE-PRESSURIZED CABIN, RETURNED TO AIRPORT. REPLACED WINDSHIELD. 2 L 7 2 4T RT A8SW 2001031900198 20010319 00198 SW 2001 3 19 PNSA010104 1 20010105 A 5230 2729050155 CABLE SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR BROKEN A PNSA K NONE O OTHER IN INSP/MAINT 1 AL 03 640PA AC759B PASSENGERS WERE ALREADY LOADED, WHILE CLOSING CARGO DOOR, CABLE FOR CLOSING DOOR BROKE. FLT DELAYED WHILE NEW CABLE INS TALLED. 2 L 7 2 4T RT A8SW 2001031900199 20010319 00199 EA 2001 3 19 COMA0160257 1 20010220 A 5320 601R3103077 SPLICE PLATE CNDAIR CL600 CL6002B19 EA FUSELAGE MISMANUFACTURED A COMA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 912CA 7011 SPLICE PLATES (P/N 601R31030-77) WERE FABRICATED INCORRECTLY BY THE MANUFACTURER. REMOVED, FABED AND REPLACED SPLICE PL ATES IAW WVAC EO 601R-53-2239. 2 L 7 2 4F RT A21EA 2001031900200 20010319 00200 EA 2001 3 19 COMA0160259 1 20010216 A 2752 852D100MD01 ACTUATOR CNDAIR CL600 CL6002B19 EA RT FLAP FAILED A COMA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 01 936CA 17404 7043 FLAPS FAILED DURING APPROACH. REPLACED RT FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2001031900201 20010319 00201 EA 2001 3 19 COMA0160260 1 20010217 A 3222 161201 PISTON CNDAIR CL600 CL6002B19 EA NLG LEAKING A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 918CA 7018 NLG DISAGREE MESSAGE AFTER T/O. REPLACED THE NLG PISTON ASSY. 2 L 7 2 4F RT A21EA 2001031900202 20010319 00202 EA 2001 3 19 COMA0160261 1 20010217 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA RT FLAP FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 812CA 2249 7381 FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT BPSU. 2 L 7 2 4F RT A21EA 2001031900203 20010319 00203 EA 2001 3 19 COMA0160262 1 20010218 A 2750 865D1007 POWER UNIT CNDAIR CL600 CL6002B19 EA WING FAILED A COMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 01 964CA 11785 7129 FLAPS FAILED AT 20 DEGREES. REPLACED THE FLAP PDU. 2 L 7 2 4F RT A21EA 2001031900204 20010319 00204 EA 2001 3 19 COMA0160263 1 20010218 A 2613 356024310 SENSING ELEMENT CNDAIR CL600 CL6002B19 EA LT PYLON FALSE INDICATION A COMA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 779CA 7306 LEFT 14TH STAGE BLEED AIR LEAK WARNING. REPLACED THE LT PYLON LEAK SENSING ELEMENT. 2 L 7 2 4F RT A21EA 2001031900205 20010319 00205 EA 2001 3 19 COMA0160264 1 20010218 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA RT FLAP FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 936CA 6342 7043 FLAPS FAIL MESSAGE. REPLACED THE RT BPSU. 2 L 7 2 4F RT A21EA 2001031900206 20010319 00206 NM 2001 3 19 AWXA0001372 1 20010219 A 2810 L95F50603 RELIEF VALVE AIRBUS A319 A319132 NM CENTER TANK RUPTURED A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 820AW 566 1397 CMH - DIVERTED FLIGHT - 2/14/01 - EN ROUTE FROM PHL TO PHX THE CREW GOT AN ECAM AUTO FUEL FAULT. SELECTED MANUAL AND NO TICED FLASHING QUANTITY NR 2 MAIN AND OUTBOARD RESERVE AND DECREASING FUEL QUANTITY IN NR 1 MAIN; TRIED NR 1 FUEL PUMPS OFF, DECREASE CONTINUED; FLIGHT WAS DIVERTED TO CMH. IN CMH, MAINTENANCE FOUND THE CENTER TANK OVERPRESSURE PROTECTOR R UPTURED; IT WAS REPLACED AND CHECKS WERE GOOD. 2 L 7 2 4F RT A28NM 2001031900207 20010319 00207 NM 2001 3 19 F3LA200100034 1 20010223 A 5350 6548674160 FAIRING BOEING 737 7372L9 1384497 NM RT WING DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 22733 AIRCRAFT DIVERTED TO GRAND JUNCTION, COLORADO DUE TO WEATHER. UPON WALKAROUND, FLIGHT CREW REPORTED DAMAGE TO RT INBD W ING-TO-BODY FAIRING ELEPHANT EAR SCUFF PLATES DAMAGED. AIRCRAFT WAS FERRIED TO DEN FOR REPAIR. MAINTENANCE REPLACED RT INBD WING-TO-BODY FAIRING AND RT INBD MID FLAP FAIRING ATTACHMENT NUT PLATES. 2 L 7 2 4F RT A16WE 2001031900208 20010319 00208 EU 2001 3 19 UPS01135073 1 20010223 A 2612 273902 CONTROL UNIT AIRBUS A300 A300F4622R 3930360 EU NR1 ENGINE INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 124UP 0808 INSPECTION TYPE:N/A REF M209397 ENG 1 LOOP B-INOP. *S/D* REPLACED NR 1 FIRE DETECTION CONTROL UNIT AND NR 1 B-SENSE CK ELEMENT (RIGHT SIDE). OPS CKS OK AS PER AMM 26-12-12. THIS CLEARS M-209397 CONTROL UNIT P/N OFF/ON 2739-02, S/N ON 74 4, S/N OFF 6001. SENSE LOOP OFF/ON 3601-92-1250/650-5, S/N. ON 96094, S/N 94439. 2 L 7 2 4F RT A35EU 2001031900209 20010319 00209 NM 2001 3 19 QXEA0100122 1 20010219 A 3260 SENSOR DHAV DHC8 DHC8202 2809007 NM LT MLG OUT OF ADJ A QXEA K NONE O OTHER CR CRUISE 1 NM 09 379PH 530 PDX - LEFT SIDE MAIN LANDING GEAR DOORS OPENED IN FLIGHT. ADJUSTED LEFT MAIN LANDING GEAR UPLOCK PROXIMITY SENSOR TARGE T DISTANCE. PERFORMED MANDITORY GEAR SWINGS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001031900210 20010319 00210 EU 2001 3 19 QXEA0100123 1 20010219 A 3350 551590004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN FAULTY A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 SEA - FORWARD CABIN EXIT SIGN FOUND INOPERATIVE. REMOVED AND REPLACED EXIT SIGN CIRCUIT BOARD. OPERATIONAL CHECKS GOOD . AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001031900211 20010319 00211 NM 2001 3 19 01FDEA00105 1 20010210 A 5310 SHEAR TIE BOEING 727 72725C 138400H NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DURING ROUTINE INSP FUSELAGE SHEAR TIE AT BS 1070, STR 5R FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 7 27 SRM 51-20-1, 51-10-2, 51-30-2. 2 L 7 3 4F A3WE 2001031900212 20010319 00212 NM 2001 3 19 01FDEA00108 1 20010210 A 5310 SHEAR TIE BOEING 727 72725C 138400H NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DURING ROUTINE INSP THE FUSELAGE SHEAR TIE AT BS 1050, STR 5R & 6R FOUND CRACKED. *S/D* REMOVED, REPLACED, FAB, TREATE D AND PRIMED PER IAW 727 SRM 51-20-1, 51-10-2, 51-30-2. 2 L 7 3 4F A3WE 2001031900213 20010319 00213 NM 2001 3 19 UPS01235033 1 20010222 A 3260 WARNING LIGHT BOEING 727 727108C 1384039 NM COCKPIT ILLUMINATED A IPXA K NONE J WARNING INDICATION UK UNKNOWN 1 SO 01 936UP 19503 INSPECTION TYPE:N/A, RT MLG DOOR WARNING ILLUM. OK TO FLY ON REVENUE TO CAE FROM PHL AS PER EO B727-1245B-DISSUED. A/C MUST FLY WITH GEAR HANDLE IN UP POSITION AT ALL TIMES NO FURTHER ACTION IS REQUIRED. 2 L 7 3 4F A3WE 2001031900214 20010319 00214 NM 2001 3 19 F3LA200100027 1 20010221 A 5315 FLOORBEAM BOEING 737 7373S1 138447S NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 3095 24856 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ACROSS TOP OF AFT FUSELAGE FLOORBEAM INTERCOSTAL CAP, STA 951.5, BETWEEN 26 LBL AND 50 LBL. MAINTENANCE REMOVED FLOORBEAM INTERCOSTAL, AND FABRICATED, PRIMED AND INSTALLED REPLACEMENT FLOORBE AM INTERCOSTAL PER EA 53-737-113. 2 L 7 2 4F RT A16WE 2001031900215 20010319 00215 NE 2001 3 19 2001UALA00058 2 20010127 A 7321 FPK121407PT06D CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EEC DAMAGED A UALA K NONE J WARNING INDICATION CR CRUISE 1 WP 29 545UA 25323 726724 LEFT ENGINE CONTROL MESSAGE DISPLAYED 3 HOURS INTO FLIGHT. *S/D* REPLACED EEC ALTERNATOR AND CONNECTOR D4858 ON EEC. EEC ALTERNATOR STATOR WAS REPLACED PRIOR TO DEPARTURE FOR MESSAGES. THREE HOURS INTO OUTBOUND FLT MESSAGE REOCCURRED. FOUND TWO PINS PUSHED BACK AND LOCKS DAMAGED ON EEC ALTERNATOR CONNECTOR D4858. REPLACED CONNECTOR D4858 AND AS A PRECA UTIONARY MEASURE THE EEC ALTERNATOR WAS REPLACED AGAIN. 2 L 7 2 4F 4 F RT A2NM E17NE 2001031900216 20010319 00216 NM 2001 3 19 2001UALA00061 1 20010128 A 2910 651782119 MODULE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE HYDRAULIC SYS LEAKING A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7283U 21561 AIRCRAFT LOST SYSTEM A HYDRAULIC PRESSURE AFTER TAKEOFF. AIRCRAFT RETURNED TO ORD. *S/D* FOUND HYDRAULIC LEAK IN AIRS TAIR AREA AT SYSTEM A HYDRAULIC MODULE. REPLACED SYSTEM A HYDRAULIC MODULE. NO LEAKS INDICATED AFTER REPLACEMENT. 2 L 7 3 4F 4 F A3WE E2EA 2001031900217 20010319 00217 2001 3 19 2001UALA00064 4 20010130 A 3414 2083111 INDICATOR BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE COCKPIT FAILED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 953UA 26700 CAPTAIN''S AIRSPEED INDICATOR HAD AN OFF FLAG COME INTO VIEW ON TAKEOFF. *S/D* MACH AIRSPEED INDICATOR FAILED. SHOP F INDINGS CONFIRMED FAILURE, DUE TO AN INTERMITTENT POTENTIOMETER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001031900218 20010319 00218 NM 2001 3 19 2001UALA00072 1 20010129 A 2130 CONTROL VALVE AIRESRCH 39608831MOD BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN PRESSURE INOPERATIVE A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 7458U 21912 AIRCRAFT RETURNED TO ORD DUE TO A CABIN PRESSURE PROBLEM. *S/D* THE AIRFLOW CONTROL VALVES WERE INOPERATIVE. REPLACED LEFT AND RIGHT VALVES. 2 L 7 3 4F 4 F A3WE E2EA 2001031900219 20010319 00219 NM 2001 3 19 F3LA200100028 1 20010221 A 5320 FLOOR SUPPORT BOEING 737 7373S1 138447S NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 3095 24856 DURING C-4 CHECK, INSPECTION REPORTED AFT FUSELAGE FLOOR SUPPORT CORRODED AT LBL 12, BETWEEN STA 947.5 AND STA 967. MAI NTENANCE FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT PER EA 53-737-113. 2 L 7 2 4F RT A16WE 2001031900220 20010319 00220 NM 2001 3 19 F3LA200100029 1 20010221 A 5320 FLOOR SUPPORT BOEING 737 7373S1 138447S NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 3095 24856 DURING C-4 CHECK, INSPECTION REPORTED AFT FUSELAGE FLOOR SUPPORT CORRODED AT LBL 16, STA 950. MAINTENANCE FABRICATED AN D INSTALLED REPLACEMENT FLOOR SUPPORT PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001031900221 20010319 00221 SO 2001 3 19 C2XA01TY022 1 20010212 A 5210 14533678401 HINGE EMB 145 EMB145LR SO PAX DOOR GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16976 145171 TYS - DURING A SCHEDULED 1C INSPECTION, A GOUGE WAS FOUND IN THE PASSENGER ENTRY DOOR FRAME UPPER HINGE. MAINTENANCE BL ENDED GOUGE, DYE-PENNED IAW EMB 145 REF GS 0422/01, RESTORED THE REWORKED AREA IAW EMB 145 CPM 51-21-03, -04 AND -06. N O FURTHER ACTION REQUIRED. PROCEDURES WERE SATISFACTORY. AIRCRAFT WILL BE RELEASED FOR SERVICE UPON COMPLETION OF C-CH ECK. (M) 2 L 7 2 4T RT T00011AT 2001031900222 20010319 00222 NM 2001 3 19 UPS01635074 1 20010226 A 2612 FIRE LOOP BOEING 767 76734AF 1385212 NM LT ENGINE INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 308UP 27761 INSPECTION TYPE:N/A, LT ENG FIRE DET LOOP 1 INOP REF M209352. *S/D* COMPLETED EXTENDED CORRECTIVE ACTION 05044 WIRE NU MBER W5324-002R-16 REPLACED ON LEFT ENGINE SYSTEM OPS CHECKS GOOD PER MM 26-11-00. 2 L 7 2 4F RT A1NM 2001031900223 20010319 00223 SO 2001 3 19 C2XA01TY023 1 20010212 A 5210 14533677401 HINGE EMB 145 EMB145LR SO PAX DOOR GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16976 145171 TYS - DURING A SCHEDUELD 1C INSPECTION, A GOUGE WAS FOUND IN THE PASSENGER DOOR FRAME LOWER HINGE. MAINTENANCE BLENDED GOUGE, DYE-PENNED IAW EMB 145 REF GST 0422/01, RESTORED THE REWORKED AREA IAW EMB 145-CPM-51-21-03, -04 AND -06. NO FUR THER ACTION REQUIRED. PROCEDURES WERE SATISFACTORY. AIRCRAFT WILL BE RELEASED FOR SERVICE UPON COMPLETION OF C-CHECK. (M) 2 L 7 2 4T RT T00011AT 2001031900224 20010319 00224 NM 2001 3 19 F3LA200100030 1 20010222 A 5315 FLOORBEAM BOEING 737 7373S1 138447S NM AFT CARGO BAY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 3095 24856 DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOORBEAM CORRODED AT STA 847, STR 26R. MAINTENANCE REPLACE D FLOORBEAM SUPPORT STRAP AND WEB PER SDR 51-10-02. 2 L 7 2 4F RT A16WE 2001031900225 20010319 00225 NM 2001 3 19 F3LA200100031 1 20010222 A 5315 FLOORBEAM BOEING 737 7373S1 138447S NM AFT CARGO BAY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 3095 24856 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT BEAM AT STA 867, RBL 15. MAINTEN ANCE REPLACED FLOOR SUPPORT BEAM PER SRM 51-30-02 AND 51-10-02. 2 L 7 2 4F RT A16WE 2001031900226 20010319 00226 NM 2001 3 19 F3LA200100032 1 20010222 A 5315 FLOORBEAM BOEING 737 7373S1 138447S NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 3095 24856 DURING C-4 CHECK, INSPECTION REPORTED AFT FUSELAGE FLOORBEAM AT STA 986.5 CORRODED ACROSS TOP. MAINTENANCE FABRICATED A ND INSTALLED REPLACEMENT FLOOR BEAM PER SRM 53-00-51. 2 L 7 2 4F RT A16WE 2001031900227 20010319 00227 NM 2001 3 19 01FDEA00089 1 20010207 A 5754 RIB BOEING 727 72725C 138400H NM NR 5 SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DURING ROUTINE INSP, NR 5 SLAT INBOARD ACTUATOR ATTACH RIB FOUND CRACKED. *S/D* BLENDED, TREATED AND PRIMED PER IAW BA C 727 SRM 57-50-1, 51-10-2. 2 L 7 3 4F A3WE 2001031900228 20010319 00228 SO 2001 3 19 C2XA01TY019 1 20010212 A 7110 14576679001 STRAP EMB 145 EMB145LR SO LT COWLING DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16976 145171 TYS - DURING A SCHEDULED 1C INSPECTION, THE LEFT LOWER COWLING AFT FASTENER STRUCTURE HAS A TEAR IN THE METAL. MAINTENA NCE REMOVED AND REPLACED STRAP IAW EMB 145 MM 51-40-02. FABRICATED NEW STRAP IAW EMB REF GST 0438/01. PROCEDURES WERE SATISFACTORY. AIRCRAFT WILL BE RELEASED FOR SERVICE UPON COMPLETION OF C-CHECK. (M) 2 L 7 2 4T RT T00011AT 2001031900229 20010319 00229 SO 2001 3 19 C2XA01TY018 1 20010211 A 2612 3601135470200C FIRE LOOP EMB 145 EMB145LR SO FUSELAGE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16976 6330 145171 TYS - DURING A SCHEDULED 1C INSPECTION, THE APU FIRE LOOP WAS FOUND CHAFED. MAINTENANCE REMVOED AND REPLACED THE FIRE L OOP IAW EMB 145 MM 26-12-01. PROCEDURES WERE SATISFACTORY, AIRCRAFT WILL BE RELEASED FOR SERVICE UPON COMPLETION OF C-C HECK. (M) 2 L 7 2 4T RT T00011AT 2001031900231 20010319 00231 NM 2001 3 19 F3LA200100035 1 20010219 A 2751 10619264 INDICATOR BOEING 737 7372L9 1384497 NM COCKPIT INOPERATIVE A F3LA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 NM 03 270FL 22733 FLIGHT CREW REPORTED STICK SHAKER ACTIVATED ON TAKEOFF FOR APPROXIMATELY 3 SECONDS. REPLACED RT TRAILING EDGE FLAP POSI TION INDICATOR PER MM 27-58-01. 2 L 7 2 4F RT A16WE 2001031900232 20010319 00232 NM 2001 3 19 01FDEA00091 1 20010207 A 5310 FITTING BOEING 727 72725C 138400H NM FWD CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DURING ROUTINE INSP, FWD LWR CARGO COMPT DOOR CUTOUT, UPPER FWD DOOR STOP FITTING FOUND CRACKED. *S/D* REMOVED PAINT. HFEC IND NO CRACKS PER IAW BAC 727 NDT MANUAL PART 6. TREATED AND PRIMED PER IAW BAC 727 SRM 51-10-2. 2 L 7 3 4F A3WE 2001031900239 20010319 00239 NE 2001 3 19 EIAA2001010 2 20010207 A 7230 BLADE DOUG DC9 DC933F 302207A WP PWA JT8 JT8D9A 52048 NE NR 1 ENGINE DAMAGED A EIAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 09 944F 47194 678072 AFTER TAKEOFF, TOWER REPORTED SPARKS FROM REAR OF AIRCRAFT. NO ABNORMAL INDICATIONS. RETURNED TO FAR. SUBSEQUENT INSP ECTION FOUND DAMAGE TO NR 1 ENGINE 1ST STAGE BLADES. (M) 2 L 7 2 4F 4 F A6WE E2EA 2001031900240 20010319 00240 NM 2001 3 19 AALA016010 1 20010125 A 2424 976J2544 GCU DOUG MD90 MD9030 3023690 NM EE BAY FAILED A AALA K NONE J WARNING INDICATION AP APPROACH 1 SW 21 903RA 53551 SJC - ON SHORT FINAL WHEN DISCONNECTED THE AUTOPILOT, LOST THE GENERATOR AND GOT A L AC POWER FAULT LIGHT. DID NOT ATTE MPT TO RESET. CHECKED EPCU AND FOUND THE LEFT ENGINE GENERATOR CEU FAILED. DEFERRED LEFT ENGINE GENERATOR INOPERATIVE PER ML 24-21-01 DMI NR 24215. ENTERED IN MCI. VERIFIED APU OIL AND ENGINE OIL FULL PRIOR TO DEPARTURE. REPLACED LEFT CHANNEL CEU PER MM 24-21-26. OPS CHECK OK PER MM 24-21-01. REMOVED PLACARD 24-21-01 AUTH 24215, CLEARED MIC. (M) 2 L 7 2 4F RT A6WE 2001031900241 20010319 00241 NM 2001 3 19 AALA016011 1 20010129 A 3222 5940497501 STRUT DOUG MD90 MD9030 3023690 NM NLG LOW A AALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 21 904RA 53570 SNA - UNSAFE GEAR DOOR (NOSE GEAR) INDICATION AFTER RETRACTION AIRCRAFT NOT ACCELERATED ABOVE 200 KTS. LANDING GEAR LOW ERED WITH NORMAL INDICATION FOLLOWED BY A NORMAL LANDING AUTO SPOILER FAIL MESSAGE ON IN CONJUNCTION WITH UNSAFE GEAR IN DICATION MESSAGE WENT OUT WITH GEAR DOWN. SERVICED NOSE GEAR STRUT WITH OIL AND AIR GEAR SWING OPERATION CHECKS GOOD IN D CHECKS GOOD AUTO SPOILER OPERATION CHECKS GOOD. (M) 2 L 7 2 4F RT A6WE 2001031900242 20010319 00242 NM 2001 3 19 AALA016012 1 20010126 A 2421 28B5276 GENERATOR DOUG MD90 MD9030 3023690 NM LT ENGINE MALFUNCTIONED A AALA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 21 905RA 53573 LAX - ON FCF, DURING TAKEOFF ROLL, LEFT GENERATOR DROPPED OFF LINE AND AC POWER FAULT LIGHT ILLUMINATED AT ABOUT 70 KNOT S AIRBORNE PERFORMED RESET PER THE CHECKLIST GENERATOR CAME BACK ON LINE AND REMAINED ON FOR REMAINING FOUR MINUTES OF F LT. REMOVED AND REPLACED LEFT GENERAT0R, OPS CHECK. REPLACED GENERATOR HARNESS ON LEFT ENGINE TAXIED AC NO FAULTS NOTE D. (M) 2 L 7 2 4F RT A6WE 2001031900243 20010319 00243 WP 2001 3 19 AALA016013 1 20010130 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A K NONE O OTHER IN INSP/MAINT 1 SW 21 832RA 53044 EMERGENCY SEAT LIGHTING WIRE FOUND BROKEN AT SEAT 3EF. REPAIRED WIRE PER MM, OPS NORMAL. (M) 2 L 7 2 4F RT A6WE 2001031900244 20010319 00244 WP 2001 3 19 AALA016014 1 20010130 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 754RA 49641 CCI-LAX - RED EMERGENCY SEAT LIGHTS INOPERATIVE. REPLACED BATTERIES, OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 2001031900245 20010319 00245 WP 2001 3 19 AALA016015 1 20010130 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A K NONE O OTHER IN INSP/MAINT 1 SW 21 832RA 53044 CCI-LAX - FOUND BROKEN WIRE AT SEATS 3EF FOR SEAT MOUNTED EMERGENCY LIGHT. REPAIRED BROKEN WIRE PER MM. OPS NORMAL. ( M) 2 L 7 2 4F RT A6WE 2001031900246 20010319 00246 WP 2001 3 19 AALA016016 1 20010204 A 2170 21D101 COALESCER BAG DOUG DC9 DC983 3022083 WP AC BAY DIRTY A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 882RA 49949 LAX - WITH PACKS ON, WET SMELL FILLED CABIN WITH SMOKE. MAINTENANCE SUGGESTS COALESCERS REQUIRE REPLACEMENT. ACCOMPLIS HED PACK BURN. REPLACED COALESCER BAGS. COULD NOT DUPLICATE SMOKE IN CABIN. (M) 2 L 7 2 4F RT A6WE 2001031900247 20010319 00247 NE 2001 3 19 UPS01535010 2 20010217 A 7260 GEARBOX BOEING 757 75724APF 1384969 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE FAILED A IPXA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 01 436UP 25467 31261 INSPECTION TYPE:N/A, ON TAKEOFF OUT OF 2000 FEET, THE LEFT ENGINE LOST OIL PRESSURE. MAINTENANCE VERIFIED THAT HIGH SPE ED GEARBOX DRIVE FOR OIL PUMP FAILED. SUSPECT INTERNAL GEARBOX MALFUNCTION. REMOVED AND REPLACED ENGINE. 2 L 7 2 4F 4 F RT A2NM E12EU 2001031900248 20010319 00248 NM 2001 3 19 QXEA0100113 1 20010202 A 5520 ELEVATOR DHAV DHC8 DHC8102 2809003 NM TAIL INCORRECT A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 814PH 43 PDX- RIGHT HAND ELEVATOR INBOARD TRAILING EDGE DOES NOT FARE WITH ELEVATOR SKIN. REPAIRED IAW DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2001031900249 20010319 00249 NM 2001 3 19 F3LA200100036 1 20010225 A 5523 BACB28AK04XXX BUSHING BOEING BOEING 737 7373L9 1384470 NM LT ELEVATOR TAB WORN A F3LA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 NM 03 310FL 26440 AIR TURNBACK. FLIGHT CREW REPORTED VIBRATION TO FLIGHT CONTROLS DURING CLIMB. NO VIBRATION INDICATION, ALL ENGINE INDI CATIONS NORMAL. CYCLED GEAR AT LOWER SPEED AND ALTITUDE AND VIBRATION STOPPED. VIBRATION PRESENT WITH AUTOPILOT BOTH O N AND OFF. FOUND NR 1 INBOARD LT ELEVATOR TRIM TAB ATTACH HARDWARE WORN. REPLACED HARDWARE, PERFORMED FLIGHT CONTROL T EST/INSPECTION, PERFORMED TEST FLIGHT AND SYSTEM CHECKED OK. 2 L 7 2 4F RT A16WE 2001031900250 20010319 00250 SO 2001 3 19 C2XA01TY016 1 20010211 A 5311 14523509401 FRAME EMB 145 EMB145LR SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16976 145171 TYS - DURING A SCHEDULED 1C INSPECTION, A GOUGE WAS FOUND IN FRAME 70 BETWEEN BLEED LINE AND CARGO FLOOR. MAINTENANCE B LENDED GOUGE, DYE PENETRANT INSPECTED, ALODINED AND PRIMED AREA IAW EMB REF GST 0427/01, 145-NDI MANUAL 53-31-00, CMP 51 -21-03 AND 51-21-05. PROCEDURES WERE SATISFACTORY. AIRCRAFT WILL BE RELEASED FOR SERVICE UPON COMPLETION OF C-CHECK. (M) 2 L 7 2 4T RT T00011AT 2001031900251 20010319 00251 SO 2001 3 19 C2XA01TY017 1 20010211 A 4910 14533997001 FIREWALL EMB 145 EMB145LR SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16976 145171 TYS - DURING A SCHEDULED 1C INSPECTION, A GOUGE IN THE APU FIREWALL BELOW UPPER APU MOUNT. MAINTENANCE BLENDED AND DYE- PENNED, AND NO DEFECTS NOTED IAW EMB 145 REF GST 0433/01. PROCEDURES WERE SATISFACTORY. AIRCRAFT WILL BE RELEASED FOR SERVICE UPON COMPLETION OF C-CHECK. (M) 2 L 7 2 4T RT T00011AT 2001031900252 20010319 00252 NM 2001 3 19 USAA010172 1 20010207 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 281AU 48267 23114 BOS - FOUND SKIN CRACKED 1 INCH, STATION 747 STRINGER 18R. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6. (M) 2 L 7 2 4F A16WE 2001031900253 20010319 00253 NM 2001 3 19 USAASB01024 1 20010127 A 3350 AD20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 397US 23319 TPA - MAINTENANCE FOUND THE AFT AISLE EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT BATTE RY PACK IN OVERHEAD PANEL AT STATION 736. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001031900254 20010319 00254 EU 2001 3 19 USAASA01004 1 20010213 A 2120 UNKNOWN AIRBUS A319 A319112 3930323 EU COCKPIT ODOR A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 705UW 0929 PIT-SAN - FLT 89 - AFTER DEPARTING PIT, AND CLIMBING THROUGH FL160, AND ELECTRICAL ODOR WAS REPORTED IN THE COCKPIT. TH E FLIGHT RETURNED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE RAN THE AIR CONDITIONING PACKS WITH BOTH THE APU AND ENGINES. CHECKS OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2001031900255 20010319 00255 NM 2001 3 19 USAASB01043 1 20010209 A 3350 6104789 BATTERY PACK BOEING 737 7372B7 1384560 NM CARGO BAY DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 283AU 23116 BWI - MAINTENANCE FOUND THE RIGHT OVERWING EXTERIOR EMERGENCY LIGHT, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A16WE 2001031900256 20010319 00256 NM 2001 3 19 USAASB01006 1 20010114 A 3350 900835A BATTERY PACK BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 245US 22751 TPA - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTS ON SEAT ROWS 1 THROUGH 8 INOPERATIVE. MAINTENANCE REPAIRED A BROKEN W IRE AT SEAT 8A AND REMOVED AND REPLACED THE BATTERY PACK AT SEAT 17A. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 2001031900257 20010319 00257 NM 2001 3 19 USAASB01047 1 20010209 A 3350 1000679 LIGHT BOEING 737 7372B7 1384560 NM GALLEY INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 279AU 22891 LGA - MAINTENANCE FOUND THE EMERGENCY LIGHT ABOVE THE FORWARD GALLEY SERVICE DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERIES (P/N S106) AND LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 2001031900259 20010319 00259 NM 2001 3 19 USAA010152 1 20010212 A 5310 TORQUE BOX BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND TORQUE BOX WEB CRACKED .5 INCH, BS 947 JUST BELOW STRINGER 11L. REMOVED AND REPLACED DOUBLER AND FILLER PER TR 53-30-07 REV A. (M) 2 L 7 2 4F A16WE 2001031900260 20010319 00260 NM 2001 3 19 USAA010154 1 20010212 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND SIDE CHORD CRACKED 1 INCH, TWO PLACES, STATION 178, WL 207, AND WL 195, LEFT SIDE. SPLICED IN NEW SIDE CHOR D PER EO 5300V157. (M) 2 L 7 2 4F A16WE 2001031900261 20010319 00261 NM 2001 3 19 USAA010155 1 20010212 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND SIDE CHORD CRACKED 1 INCH, STATION 178, WL 207 AND 195 RIGHT SIDE. SPLICED IN NEW SIDE CORD PER EO 5300V157 . (M) 2 L 7 2 4F A16WE 2001031900262 20010319 00262 NM 2001 3 19 USAA010156 1 20010213 A 5310 CREASE BEAM BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND CREASEBEAM WEB CRACKED 1 INCH, AFT OUTBOARD CORNER AT STATION 638. SPLICED IN NEW SECTION PER SRM 51-10-1 A ND 51-40-4. (M) 2 L 7 2 4F A16WE 2001031900263 20010319 00263 NM 2001 3 19 USAA010157 1 20010213 A 5320 ANGLE BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND CREASEBEAM ANGLE .5 INCH, BS 630, RBL 45. FABRICATED NEW ANGLE PER SRM 51-10-1 AND DWG 65 47973. (M) 2 L 7 2 4F A16WE 2001031900264 20010319 00264 WP 2001 3 19 USAA010160 1 20010108 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 918VJ 46661 48138 PIT - FOUND SKIN CRACKED .75 INCH, STATION 101.50 RIGHT AFT NOSE GEAR DOOR HINGE CUTOUT. REPLACED DOUBLER PER SRM 53-05 , FIG 62. (M) 2 L 7 2 4F A6WE 2001031900265 20010319 00265 WP 2001 3 19 USAA010161 1 20010112 A 5330 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 814US 51567 48094 PIT - FOUND SKIN CRACKED 1 INCH BY .5 INCH, STATION 1437 AT LONGERON 3L. CUT OUT DAMAGE, INSTALLED FILLERS AND DOUBLER PER SRM 53-04 FIG 27. (M) 2 L 7 2 4F A6WE 2001031900266 20010319 00266 WP 2001 3 19 USAA010163 1 20010117 A 5755 59328321 FITTING DOUG DC9 DC981 3022081 WP LT SPOILER CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 807US 52914 48039 PIT - FOUND FITTING CRACKED .75 INCH, LEFT SPOILER ACTUATOR FITTING AT BOLT BOSS. REPLACED PART PER EO 5788M381. (M) 2 L 7 2 4F A6WE 2001031900267 20010319 00267 2001 3 19 USAASB01023 4 20010126 A 3441 HG1050AF04 IRU BOEING 737 7374B7 1384702 NM EE BAY FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 785AU 36199 25024 PHL - FLT 99 - EN ROUTE FROM PHL-SJU, THE NR 1 INERTIAL REFERENCE SYSTEM FAULT LIGHT ILLUMINATED. FLIGHT RETURNED TO FI ELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 1 I NERTIAL REF UNIT. BITE CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001031900268 20010319 00268 NM 2001 3 19 USAASB01033 1 20010202 A 3350 6104789 BATTERY PACK BOEING 737 7372B7 1384560 NM CARGO BAY DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 277AU 22889 PIT - DURING THE OVERNIGHT CHECK, MAINTENANCE FOUND THE AFT CABIN AND AFT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. MAINTE NANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A16WE 2001031900269 20010319 00269 NM 2001 3 19 USAASB01030 1 20010131 A 3350 500000043 CHARGER BOEING 737 7372B7 1384560 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 275AU 22887 BWI - MAINTENANCE FOUND THE CENTER OVERHEAD CEILING EMERGENCY LIGHT AT OVERWING EMERGENCY EXIT ROW INOPERATIVE. MAINTEN ANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY AND THE BATTERY SUPPLY (P/N 9008-3-5A). OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 2001031900270 20010319 00270 EU 2001 3 19 USAAF01004 1 20010125 A 3230 200444004 DAMPER FOKKER F28 F28MK0100 4990807 EU RT MLG MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 854US 10474 11282 PIT-ERI - FLT 257 - AFTER TAKEOFF, THE LANDING GEAR DID NOT RETRACT WHEN SELECTED UP. THE LANDING GEAR WAS RECYCLED, BU T STILL DID NOT RETRACT. THE FLIGHT THEN RETURNED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE UPSTOP DAMPER. OPS CHECK OK. (M) 2 L 7 2 4F RT 2001031900271 20010319 00271 EU 2001 3 19 USAA010170 1 20010131 A 5330 SKIN FOKKER F28 F28MK0100 4990807 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 852US 26432 11280 PIT - FOUND SKIN CRACKED 2 INCHES BY 10 INCHES, STATION 27026 STRINGER 46 LEFT TO 48 RIGHT. CUT OUT SKIN, INSTALLED FIL LER AND INSTALLED EXT DOUBLER PER EA 54392 AND TYP REPAIR 53-40-01 FIG 1B. (M) 2 L 7 2 4F RT 2001031900272 20010319 00272 NM 2001 3 19 USAA010113 1 20010205 A 5312 BULKHEAD BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND BULKHEAD CRACKED .250 INCH, STATION 178 BULKHEAD, WL 224, RBL 2. INSTALLED TRIPLER PER EA 68961 AND EO 5300 V153. (M) 2 L 7 2 4F A16WE 2001031900273 20010319 00273 NM 2001 3 19 USAA010114 1 20010205 A 5330 DOUBLER BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND PRODUCTION DOUBLER CRACKED 1 INCH, 4 PLACES, BL 0, STATION 370 TO 380. INSTALLED DOUBLER PER EA 69056. (M) 2 L 7 2 4F A16WE 2001031900274 20010319 00274 NM 2001 3 19 USAA010115 1 20010205 A 5320 WEB BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND WEB CRACKED 6 INCHES, STATION 520, RBL 24.5. REPAIRED PER SRM 51-10-10. (M) 2 L 7 2 4F A16WE 2001031900275 20010319 00275 NM 2001 3 19 USAA010117 1 20010205 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND FLOORBEAM CRACKED 1 INCH, STATION 695 LBL 45.5. INSTALLED DOUBLER PER SRM 51-40-4. (M) 2 L 7 2 4F A16WE 2001031900276 20010319 00276 NM 2001 3 19 USAA010118 1 20010205 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND FLOORBEAM WEB CRACKED 1 INCH, STATION 706, LBL 24.5. FABRICATED REPAIR AND INSTALLED PER EA 69008 AND 69031 . (M) 2 L 7 2 4F A16WE 2001031900277 20010319 00277 NM 2001 3 19 USAA010119 1 20010205 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND FLOORBEAM WEB CRACKED 1 INCH, STATION 727, RBL 24.5. FABRICATED REPAIR AND INSTALLED PER EA 68992A. (M) 2 L 7 2 4F A16WE 2001031900278 20010319 00278 NM 2001 3 19 USAA010120 1 20010205 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND SKIN CRACKED 2.5 INCH, STATION 727B PLUS 2 AND 727A PLUS 8 STRINGER 18L. INSTALLED REPAIR DOUBLER PER SRM 5 3-30-3. (M) 2 L 7 2 4F A16WE 2001031900279 20010319 00279 NM 2001 3 19 USAA010121 1 20010205 A 5310 SHEAR TIE BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND SHEAR TIE CRACKED 1 INCH, STATION 1040 STRINGER 2L AND 3L. INSTALLED REPAIR PER DWG 65 46569. (M) 2 L 7 2 4F A16WE 2001031900280 20010319 00280 NM 2001 3 19 USAA010122 1 20010205 A 5310 SHEAR TIE BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND SHEAR TIE CRACKED .75 INCH, FS 1040 BETWEEN STRINGER 2/3 RT. INSTALLED SHEAR TIE PER DWG 65-46569. (M) 2 L 7 2 4F A16WE 2001031900281 20010319 00281 NM 2001 3 19 USAA010123 1 20010206 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND CHORD FRAME CRACKED .75 INCH, STATION 639, WL 210. REMOVED AND REPLACED PER REPAIR DOCUMENT 51-30-2. (M) 2 L 7 2 4F A16WE 2001031900282 20010319 00282 NM 2001 3 19 USAA01024 1 20010206 A 5320 ANGLE BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND UPPER CHORD ANGLE CRACKED .5 INCH, STATION 663, RBL 24, WL 201.5. INSTALLED REPAIR ANGLES PER EA 68973. (M ) 2 L 7 2 4F A16WE 2001031900283 20010319 00283 NM 2001 3 19 USAA010125 1 20010206 A 5312 BULKHEAD BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND BULKHEAD CRACKED .125 INCH, BS 1016, STRINGER 6L. INSTALLED DOUBLER AND TRIPLER PER SRM 53-10-4 FIG 15. (M ) 2 L 7 2 4F A16WE 2001031900284 20010319 00284 NM 2001 3 19 USAA010131 1 20010206 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51082 22754 CLT - FOUND OVERNIGHT FUSELAGE SKIN CRACKED 5 INCHES, LOWER FORWARD CORNER OF AFT ENTRY DOOR CUTOUT. INSTALLED REPAIR P LATES PER SRM 53-30-3 FIG 24. (M) 2 L 7 2 4F A16WE 2001031900285 20010319 00285 NM 2001 3 19 USAA010132 1 20010212 A 5320 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND TIE CLIP CRACKED .125 INCH, STATION 616, STRINGER 6L. INSTALLED NEW TIE CLIP PER EO 5393G227. (M) 2 L 7 2 4F A16WE 2001031900286 20010319 00286 NM 2001 3 19 USAA010133 1 20010212 A 5320 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND TIE CLIP CRACKED .125 INCH, STATION 616, STRINGER 2L. INSTALLED NEW TIE CLIP PE EO 5393G227. (M) 2 L 7 2 4F A16WE 2001031900287 20010319 00287 NM 2001 3 19 USAA010134 1 20010212 A 5320 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 727G, STRINGER 8R. REPLACED TIE CLIP PER EO 5393G227. (M) 2 L 7 2 4F A16WE 2001031900288 20010319 00288 NM 2001 3 19 USAA010135 1 20010212 A 5320 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND TIE CLIP CRACKED .125 INCH, STATION 685 STRINGER 4L. REPLACED TIE CLIP PER EO 5393G227. (M) 2 L 7 2 4F A16WE 2001031900289 20010319 00289 NM 2001 3 19 USAASB01050 1 20010218 A 5200 652999413 ARM BOEING 737 7374B7 1384702 NM PAX DOOR OUT OF RIG A USAA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 EA 19 436US 24558 PHL - FLT 1484 - ON CLIMB-OUT FROM PHL, EN ROUTE TO BTV, THE AIRCRAFT WOULD NOT PRESSURIZE. THE FORWARD MAIN ENTRY DOOR DID NOT SEAL PROPERLY. CREW NOTED THAT NO DOOR INDICATION WAS GIVEN BEFORE TAKEOFF. FLIGHT RETURNED TO FIELD AT PHL A ND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE FORWARD MAIN ENTRY DOOR SEAL FULL OF GUMMY DIRT. CLEANED DOOR SEAL. ALSO, FOUND GUIDE ARM OUT OF RIG. RE-RIGGED GUIDE ARM. OPS CHECK AND LEAK CHECK G OOD PER MM 52-11-00. (M) 2 L 7 2 4F RT A16WE 2001031900290 20010319 00290 NM 2001 3 19 USAASB01049 1 20010216 A 2810 FLOAT VALVE BOEING 737 7373B7 1384580 NM RT WING FAULTY A USAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 EA 19 523AU 23858 CLT - FLT 429 - AFTER TAKEOFF, THE TOWER REPORTED TO THE CAPTAIN THAT WAS LOSING FUEL FROM THE RIGHT WING. CREW SAW NO ABNORMAL FUEL CONSUMPTION BUT ELECTED TO RETURN TO FIELD AT CLT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE RIGHT CENTER VENT VALVE OK. REMOVED AND REPLACED THE RIGHT WING FLOAT VALVE. FUEL ED AIRCRAFT. NO LEAKS NOTED. (M) 2 L 7 2 4F RT A16WE 2001031900291 20010319 00291 NE 2001 3 19 USAASB01048 2 20010215 A 7200 ENGINE BOEING 737 7372B7 1384560 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 269AU 44893 22881 709112 MCO - FLT 2727 - ON CLIMB-OUT FROM FLL, EN ROUTE TO LGA, CAPTAIN REPORTED THAT THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL. FLIGHT DIVERTED TO MCO AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND METAL IN THE TAILPIPE OF THE NR 1 ENGINE. REMOVED AND REPLACED THE NR 1 ENGINE ASSEMBLY. OPS CHECK AND LEAK CHECK GOOD. (M ) 2 L 7 2 4F 4 F A16WE E2EA 2001031900292 20010319 00292 NM 2001 3 19 USAASB01044 1 20010209 A 2130 7207375 RELIEF VALVE BOEING 737 7372B7 1384560 NM PRESSURE SYS OBSTRUCTED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 286AU 40122 12382 23133 TPA - FLT 2850 - ON CLIMB-OUT FROM PBI, EN ROUTE TO BOS, THE AIRCRAFT WOULD NOT PRESSURIZE. DECISION WAS MADE TO DIVERT TO TPA. WHEN AIRCRAFT HIT THE GROUND AND LANDED AT TPA, AIRCRAFT PRESSURIZED NORMALLY. NO EMERGENCY WAS DECLARED. MA INTENANCE FOUND INSULATION IN THE RIGHT UPPER SAFETY RELIEF VALVE. REMOVED AND REPLACED VALVE AS PRECAUTIONARY PER MM 2 1-32-22. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 2001031900293 20010319 00293 NE 2001 3 19 2001UALA00073 2 20010202 A 7230 3350889510 BLADE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE DAMAGED A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 377UA 0 24642 727142 NR 2 ENGINE VIBRATION. *S/D* FOUND TWO FAN BLADES SHINGLED. REPLACED THE TWO FAN BLADES. A SUBSEQUENT TRIM RUN REVEA LED NO VIBRATION. 2 L 7 2 4F 4 F RT A16WE E2GL 2001031900294 20010319 00294 EU 2001 3 19 USAASA01005 1 20010210 A 3350 3211430 BATTERY AIRBUS A319 A319112 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 700UW 0885 MCO - THE AIRCRAFT DISPLAYED AN EPSU L AFT FAULT DURING THE CIDS EMERGENCY LIGHTS CHECK. MAINTENANCE REPLACED THE BATTE RIES IN AN EMERGENCY POWER SUPPLY UNIT. CHECKS OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2001031900295 20010319 00295 NM 2001 3 19 USAASB01039 1 20010207 A 3350 110049 CHARGER BOEING 737 7372B7 1384560 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 285AU 23132 TPA - MAINTENANCE FOUND THE AFT SERVICE DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BA TTERY PACK (P/N 61-0478-9) IN THE AFT CARGO COMPARTMENT, RIGHT SIDE, WITH NO HELP. FOUND CHARGER ASSEMBLY INOPERATIVE A T AFT OVERHEAD LAVATORY AREA. REMOVED AND REPLACED CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 2001031900296 20010319 00296 EA 2001 3 19 MASA01011 1 20010121 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN ODOR A MASA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 27172 7172 FLT 6003 - FAT-PHX - RETURNED TO FIELD DUE TO A RUBBERY SMOKE SMELL IN THE AIRCRAFT. MAINTENANCE PERFORMED AN INSPECTIO N OF THE AIRCRAFT. RAN BOTH ENGINES TO DISSIPATE THE SOLUTION FROM THE PREVIOUS NIGHTS COMP WASH. OPS CHECKS GOOD. TH E AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001031900297 20010319 00297 EA 2001 3 19 MASA01014 1 20010128 A 2824 PUMP CNDAIR CL600 CL6002B19 EA FUEL CROSSFEED MALFUNCTIONED A MASA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 17217 7217 FLT 6070- PHX-EUG - HAD A FUEL IMBALANCE THAT REACHED 1000 LBS. EICAS DISPLAYED AN APU FUEL CROSS FEED PUMP INOPERATIVE . THE CAPTAIN DECLARED AN EMERGENCY. AFTER SECURING THE ENGINE THE AIRCRAFT MADE AN UNEVENTFUL LANDING AT RNO. MAINTEN ANCE COULD NOT DUPLICATE THE DISCREPANCY. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001031900298 20010319 00298 EA 2001 3 19 MASA01021 1 20010218 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17337 7337 DURING AN OVERNIGHT INSPECTION IT WAS DISCOVERED THAT THE UPPER FORWARD EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINT ENANCE REMOVED AND REPLACED THE LIGHT BULB. OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001031900299 20010319 00299 EA 2001 3 19 MASA01020 1 20010218 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 EA EXTERIOR INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77302 7302 DURING SERVICE MAINTENANCE IT WAS DISCOVERED THAT THE NR 5 EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE AT FUSELAGE STATION 416.50. REMOVED AND REPLACED THE BULB IAW AMM 33-51-21. OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001031900300 20010319 00300 NM 2001 3 19 2001UALA00082 1 20010205 A 3600 SMOKE BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE COCKPIT DETECTED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 991UA 21981 SMOKE IN THE COCKPIT. *S/D* THREE WIRE SOCKETS IN CONNECTOR D96 BROKE OFF AND SHORTED TOGETHER. REPLACED THE SOCKETS. 2 L 7 2 4F 4 F A16WE E2EA 2001031900301 20010319 00301 NM 2001 3 19 2001UALA00083 1 20010206 A 5210 SEAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE PAX DOOR TORN A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 357UA 24378 CABIN PRESSURIZATION PROBLEM. *S/D* FOUND FORWARD ENTRY SEAL TORN, AFT CARGO DOOR REN MISSING, AND FORWARD DRAIN VALVE S LEAKING. REPLACED FORWARD ENTRY DOOR SEAL, AFT CARGO DOOR REN, AND 12 DRAIN PLUGS. 2 L 7 2 4F 4 F RT A16WE E2GL 2001031900302 20010319 00302 NE 2001 3 19 GAIA01045BOP 2 20010214 A 7310 AV16815AD SHUTOFF VALVE BOEING 727 727224 1384076 NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE SHORTED A GAIA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SW 07 69739 20667 FLT 2724 - ROC-BOS - NR 2 ENGINE FAILED ON CLIMB-OUT. ATTEMPTED RESTART FAILED. DID HAVE OIL PRESSURE AND ROTATION. AI RCAFT MADE AN UNEVENTFUL RETURN TO ROC. FOUND NR 2 FUEL SHUTOFF VALVE WIRES SHORTED IN AIRCONDITIONING BAY, CAUSING NR 2 FUEL SHUTOFF VALVE TO OPEN AND CLOSE ERRATICALLY AND SHORT OUT VALVE MOTOR. REPLACED WIRING IAW B727 MM 20-10-13. RE MOVED AND REPLACED NR 2 FUEL SHUTOFF VALVE IAW B727 MM 28-22-1. VALVE OPS AND LEAK CHECKS GOOD. NR 2 ENGINE PERFORMS N ORMALLY ON GROUND RUNS. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F 4 F A3WE E2EA 2001031900303 20010319 00303 SO 2001 3 19 ASOA01020 1 20010214 A 5311 FRAME EMB 120 EMB120RT SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 283AS 120236 FLT 4815 - DURING INSPECTION, MAINTENANCE FOUND CORROSION AT FRAME 21. MAINTENANCE REPAIRED CORROSION FOLLOWING EO 120- 53-0149 WHICH OUTLINES PROCEDURES FOR FRAME 21 CORROSION REPAIR. (M) 2 L 7 2 4T RT A31SO 2001031900304 20010319 00304 SO 2001 3 19 ASOA01021 1 20010215 A 5311 FRAME EMB 120 EMB120RT SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 504AS 120278 DURING INSPECTION, MAINTENANCE FOUND CORROSION AT FRAME 21. MAINTENANCE REPAIRED CORROSION FOLLOWING EO 120-53-0150 WHI CH OUTLINES PROCEDURES FOR FRAME 21 CORROSION REPAIR. (M) 2 L 7 2 4T RT A31SO 2001031900305 20010319 00305 EA 2001 3 19 ASOA01018 1 20010206 A 5610 NP1393221 WINDSHIELD CNDAIR CL600 CL6002B19 EA COCKPIT CRACKED A ASOA K NONE O OTHER TX TAXI/GRND HDL 1 SO 11 835AS 6110 7258 FLT 4696 - DURING TAXI IN ON FLIGHT FROM ATL TO SWF, CAPTAIN''S SIDE WINDSHIELD CRACKED. MAINTENANCE REMOVED AND REPLAC ED CAPTAIN''S SIDE WINDSHIELD. OPERATIONAL AND CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001031900306 20010319 00306 EA 2001 3 19 ASOA01019 1 20010207 A 2170 601R960503 DUCT CNDAIR CL600 CL6002B19 EA WATER SEARATOR DISCONNECTED A ASOA B A EMER. DESCENT UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 820AS 7188 FLT 4545 - DURING FLIGHT FROM ISP TO ATL, CREW EXPERIENCED A LOSS OF CABIN PRESSURIZATION IN AUTO MODE. CABIN WAS CLIMB ING AT 4000 FEET PER MINUTE. CREW MADE AN EMERGENCY DESCENT TO 10,000 FEET. CREW USED THE QRH TO REGAIN PRESSURIZATION IN MANUAL MODE, BUT THAT WAS UNSTABLE. CREW DECLARED AN EMERGENCY AND RETURNED TO ISP. AIRCAFT LANDED SAFELY. MAINTE NANCE INSPECTED AIRCRAFT AND FOUND LEFT AIRCRAFT DUCT DISCONNECTED AT THE FORWARD CLAMP OF THE WATER SEPARATOR. MAINTEN ANCE RECONNECTED DUCT AND CLAMP IAW CRJ MM 21-51-00. OPS CHECK WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001031900309 20010319 00309 EU 2001 3 19 20010316SG001 1 20010213 A 2751 354411002 INDICATOR AIRBUS 300 A300B4203 3930306 EU COCKPIT FAILED A WRNA J A DUMP FUEL UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 05 820SC 154 KRUGER FLAPS WOULD NOT RETRACT AFTER TAKEOFF OUT OF LOCK. AIRCRAFT DUMPED APPROXIMATELY 1750 GALLONS OF FUEL AND RETURN ED TO LCK. LANDING NORMAL. PROBLEM WAS TROUBLESHOT AND KRUGER INDICATOR UNIT WAS FOUND TO BE UNSERVICEABLE. PART ORDE RED AND KRUGER AND NOTCH FLAPS PUT ON MEL AND DEACTIVATED IAW 27-84-02. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A35EU 2001031900310 20010319 00310 NM 2001 3 19 BJNA010201 1 20010211 A 2611 LS14500 BATTERY BOEING 737 737282 13844AT NM SMOKE DETECTOR DISCHARGED A BJNA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 11 233TM 23043 OVERHEAD MAINTENANCE LIGHT ILLUMINATED FOR LOWER CARGO COMPARTMENT FIRE DETECTION AND SUPPRESSION SYSTEM. AIRCRAFT RELE ASED PER MEL 26-19-5-6, ITEM TRANSFERRED TO DMI LOG DMI NR 207, ITEM PLACARDED. REF MEL 26-19-56, DMI 0207, REMOVED AND REPLACED BATTERIES ON FORWARD SMOKE DETECTOR, S/N F12671. OPS CHECKS PER STC 3000 COMPONENT INSTALLATIONS MANUAL. (M) 2 L 7 2 4F RT A16WE 2001031900311 20010319 00311 NM 2001 3 19 BJNA010202 1 20010211 A 2611 100064901 SMOKE DETECTOR BOEING 737 737282 13844AT NM CARGO BAY MALFUNCTIONED A BJNA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 11 233TM 23043 CARGO COMPARTMENT FIRE DETECTION AND SUPPRESSION SYSTEM MESSAFE 1 F12671 ON OVERHEAD CONTROL DISPLAY UNIT. REMOVED AND REPLACED FORWARD SMOKE DETECTOR PER ST 3000 COMPONENT INSTALLATION MANUAL, OPS TESTED SYSTEM NORMAL. (M) 2 L 7 2 4F RT A16WE 2001031900312 20010319 00312 NM 2001 3 19 BJNA010203 1 20010217 A 2612 MODULE BOEING 737 737282 13844AT NM EE BAY NOT SEATED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 789TM 23046 WHEEL WELL FIRE WARNING WON''T TEST. AIRCRAFT RELEASED PER MEL 26-4, DMI0214. REF MEL 26-4, DMI 0214, RESEATED OVERHEA T MODULE M237 IN ELECTRONIC COMP. OPS CHECK NORMAL. PLACARD REMOVED. (M) 2 L 7 2 4F RT A16WE 2001031900313 20010319 00313 NM 2001 3 19 BJNA010204 1 20010220 A 3350 LIGHT BOEING 737 737282 13844AT NM CABIN INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 344TM 23044 FORWARD EMERGENCY FLOOR LIGHTING INOPERATIVE. FOUND WATER IN EMERGENCY FLOOR LIGHT PLUGS, REMOVED PER CMM 33-50-01, OPS CHECK GOOD AT THIS TIME. (M) 2 L 7 2 4F RT A16WE 2001031900314 20010319 00314 SO 2001 3 19 C2XA01CL011 1 20010202 A 3350 7287580505 LIGHT EMB 145 EMB145ER SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15941 145035 CLE - FLT 4019 - THE CREW REPORTED THE FORWARD EMERGENCY AISLE PATH LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE FORWARD EMERGENCY LIGHT STRIP IAW EMBRAER MM 33-50-12. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001031900315 20010319 00315 SO 2001 3 19 C2XA01BT015 1 20010206 A 2740 WARNING SYSTEM EMB 145 EMB145LR SO COCKPIT ACTIVATED A C2XA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 27 14952 145067 RIC - FLT 3669 - CREW REPORTED ''RIGHT AFTER V1 ON GROUND ON TAKEOFF, RECEIVED MASTER WARNING (NO EICAS MESSAGES) PITCH TRIM HAD RUN FROM 7 UNITS UP TO 2 UNITS UP WITHIN 2 SECONDS. AIRCRAFT COULD NOT BE TRIMMED AGAIN UNTIL APPROXIMATELY 50 0 FEET, 160 KNOTS. NO OTHER IRREGULARITIES NOTED. MAINTENANCE IN RIC, REPORTED OPS CHECKED GOOD IAW EMB145 MM 27-40-00. (M) 2 L 7 2 4T RT T00011AT 2001031900316 20010319 00316 SO 2001 3 19 C2XA01CL005 1 20010114 A 3030 CS500060D4A SENSOR EMB 135 EMB135ER 3260203 SO PITOT SYS BURNED A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 15509 145238 EWR - FLT 3619 - THE CREW REPORTED SMOKE IN THE COCKPIT WHILE TAXI. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER I NCIDENT. MAINTENANCE REMOVED AND REPLACED THE PITOT 2 CURRENT SENSOR AND RELAY. OPS CHECK WERE GOOD IAW 30-53-00 AND 3 0-31-00. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001031900317 20010319 00317 SO 2001 3 19 C2XA01CL025 1 20010215 A 3350 727580503 LIGHT EMB 135 EMB135ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16501 145145 CLE - FLT 3949 - THE CREW REPORTED THE CABIN EMERGENCY LIGHTS WILL NOT ILLUMINATE AT ROWS 3 THROUGH 6. MAINTENANCE REPL ACED THE LIGHT STRIP ASSEMBLY NR 3. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001031900318 20010319 00318 SO 2001 3 19 C2XA01BT022 1 20010215 A 3350 1317 LIGHT EMB 145 EMB145 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15932 145015 BTV - FLT 3944 - DURING 4A INSPECTION, MAINTENANCE FOUND TWO INOPERATIVE EMERGENCY LIGHTS AT PSU SEAT 12A AND SEAT 12BC LOCATIONS. REMOVED AND REPLACED BULB WITH SERVICEABLE UNITS. OPS CHECKED GOOD. (M) 2 L 7 2 4F RT T00011AT 2001031900320 20010319 00320 NM 2001 3 19 2001UALA00085 1 20010206 A 2100 SWITCH ALIDSG 5486206U1 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE AC BAY FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 390UA 24665 NR 2 PACK TRIPPED AFTER TAKEOFF AND WOULD NOT RESET. *S/D* FOUND THE COMPRESSOR DISCHARGE SWITCH FAILED. REPLACED THE COMPRESSOR DISCHARGE SWITCH. 2 L 7 2 4F 4 F RT A16WE E2GL 2001031900328 20010319 00328 EA 2001 3 19 COMA0160251 1 20010215 A 3010 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT ACTIVATED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 435CA 7473 ANTI ICE DUCT WARNING. INSTALLED RUBBER BOOTS ON THERMAL SWITCHES WIRE CONNECTION LT OUTBOARD WING LEADING EDGE. 2 L 7 2 4F RT A21EA 2001032000105 20010320 00105 NM 2001 3 20 VNAA0102003 1 20010207 A 2731 ELEVATOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE TAIL MALFUNCTIONED A VNAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 436JS 3052 DURING CLIMB, THE CREW NOTICED THAT THE ELEVATOR TRIM WOULD NOT WORK WHEN SELECTED UP. FLIGHT 4061 RETURNED TO GSP. MA INTENANCE INSPECTED AND RECYCLED AIRCRAFT POWER AND PERFORMED OPERATIONAL CHECKS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-00-00. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001032000106 20010320 00106 NM 2001 3 20 2001UALA00112 1 20010211 A 4990 APU BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE APU BAY LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 617UA 21877 AIRCRAFT DISPATCHED WITH NR 1 GENERATOR INOPERATIVE. CREW REPORTED THAT THE APU OIL QUANTITY WAS DROPPING. AIRCRAFT DI VERTED TO DEN. 2 L 7 2 4F 4 F RT A1NM E3NE 2001032000107 20010320 00107 EA 2001 3 20 COMA0160266 1 20010218 A 5320 6003106819 FITTING CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 912CA 18910 7011 FLOOR SUPPORT FITTING AT LBL 9, FS 460 IS CRACKED. REMOVED AND REPLACED FITTING IAW WVAC EO 601R-53-2229. 2 L 7 2 4F RT A21EA 2001032000108 20010320 00108 EA 2001 3 20 COMA0160267 1 20010218 A 5330 SKIN CNDAIR CL600 CL6002B19 EA FUSELAGE DENTED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 868CA 7427 DENTS BEHIND RT NOSE DOOR ON FUSELAGE. INSTALLED REPAIR IAW REO 601R-53-2230 REV A DATED 2-17-01. 2 L 7 2 4F RT A21EA 2001032000109 20010320 00109 EA 2001 3 20 COMA0160268 1 20010218 A 5510 600230681 BUSHING CNDAIR CNDAIR CL600 CL6002B19 EA HORZ STAB SCORED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 912CA 7011 HORIZONTAL STABILIZER LEFT O/B BUSHING (P/N 600-23068-1) WAS FOUND SCORED DURING INCORPORATION OF COMAIR EO 55-007. REP LACED BUSHING IN LT ORIZ STAB WITH 1ST OVERSIZE BUSHING (P/N 601R-55-11-022-1) IAW CRJ REO 601R-55-11-022A CRJ DRWG 600- 23068 AND CRJ AMM 20-26-00-910-803. 2 L 7 2 4F RT A21EA 2001032000110 20010320 00110 EA 2001 3 20 COMA0160269 1 20010219 A 5311 FRAME CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 991CA 7216 FS 718 RT FRAME IS CRACKED. ROUTED OUT DAMAGE. INSTALLED DOUBLER AND RADIUS BLOCKS AND FWD DOUBLER IAW CANADAIR REO 60 1R-53-61-193 REV A. 2 L 7 2 4F RT A21EA 2001032000111 20010320 00111 EA 2001 3 20 COMA0160270 1 20010220 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 991CA 7216 FLOOR SUPPORT ANGLE AT FS 621.0 WL 72 RBL 27 RBL 42 CRACKED. PERFORMED A MAJOR REPAIR TO CRACKED FLOOR SUPPORT ANGLE AT FS 621.0 RBL 27 - RBL 42 IAW CRJ REO 601R-53-61-117 REV A. 2 L 7 2 4F RT A21EA 2001032000112 20010320 00112 WP 2001 3 20 IXXA0100006 1 20010221 A 3260 6F83407 PLATE DOUG DC8 DC871F 302199D WP LT MLG DAMAGED A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 825BX 81091 989 45978 EN ROUTE FROM SJC TO TOL, AFTER THE LANDING GEAR WAS RETRACTED THE GEAR DOOR WARNING LIGHT REMAINED ILLUMINATED. THE FL IGHT CREW CYCLED THE LANDING GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO TOL FOLLOWING C OMPANY PROCEDURES. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED A DAMAGED GEAR DOOR SWITCH STRIKER ON THE LEFT MAI N GEAR DOOR. MAINTENANCE REPLACED THE STRIKER AND PERFORMED A SUCCESFUL OPERATIONAL CHECK. THE AIRCRAFT WAS RETURNED T O SERVICE. 2 L 7 4 4F RT 4A25 2001032000113 20010320 00113 WP 2001 3 20 IXXA0100007 1 20010221 A 3260 WARNING LIGHT DOUG DC8 DC871F 302199D WP COCKPIT ILLUMINATED A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 826BX 45998 EN ROUTE FROM TOL TO JFK, THE LANDING GEAR DOOR WARNING LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE FLIGHT CR EW CYCLED THE LANDING GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO JFK FOR AN UNEVENTFUL LANDING. THE LANDING GEAR DOOR UPLATCH SYSTEM WAS PLACED ON DEFERRAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2001032000114 20010320 00114 NM 2001 3 20 UPS01235022 1 20010107 A 5310 SHEAR TIE BOEING 727 7272A1 138407F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE:C CORROSION (C53-113-01.00-01) ON FRAME SHEAR TIE, BS 600 BETWEEN STR 28R AND STR 28L. FABRICATED REPAI R PARTS AND INSTALLED PER SRM 53-10-4, 51-10-2, 51-30-2 AND MM 51-20-151. 2 L 7 3 4F A3WE 2001032000115 20010320 00115 NM 2001 3 20 UPS01235023 1 20010110 A 5313 BAC1498147 STRINGER BOEING 727 7272A1 138407F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE:C CORROSION (C53-100-01.00-04) UNDER STRINGER 29L BETWEEN BS 1166- BS 1183 AND T-CLIP AT 1183. REMOVED CORROSION ON STRINGER 29L IN AN AREA OF 1.0 X.5 X.020 INCH FROM ORIG THICKNESS OF .090 INCH OUT OF LIMITS PER SRM 53-10- 1, SRM 53-10-2 SRM 51-10-7. REMOVED STRINGER, FABRICATED REPAIR PARTS. FOUND CORROSION ON SKIN. REMOVED CORROSION, FO UND ALL TO BE WITHIN LIMITS. REINSTALLED ALL NEW REPAIRS PARTS PER SRM 51-30-2. 2 L 7 3 4F A3WE 2001032000116 20010320 00116 NM 2001 3 20 UPS01435026 1 20010208 A 5512 SKIN BOEING 747 747259B NM LT HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 527UP 21730 INSPECTION TYPE:C, LEFT HORIZONTAL STAB L/E IS CRACKED AT STA 400 ON UPPER SKIN OF L/E. REPAIRED SKIN IAW SRM 55-10-03. 2 L 7 4 4F RT A20WE 2001032000117 20010320 00117 NM 2001 3 20 UPS01435027 1 20010207 A 5754 SKIN BOEING 747 747259B NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 527UP 21730 INSPECTION TYPE:C, RIGHT WING NR 12 K-FLAP BULLNOSE INNER SKIN IS CRACKED AT INBOARD END. REPAIRED SKIN IAW SRM 57-50-0 3 FIG 8. 2 L 7 4 4F RT A20WE 2001032000118 20010320 00118 NM 2001 3 20 UPS01535021 1 20010208 A 5315 FLOORBEAM BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 420UP 23907 INSPECTION TYPE:MOD 879 LT FLOORBEAM UPPER FLANGE IS CORRODED WL 208 LBL 45-65 APPROX. REPAIRED PER ER 01-154. 2 L 7 2 4F RT A2NM 2001032000119 20010320 00119 WP 2001 3 20 UPS01835025 1 20010220 A 2450 50137002 RELAY DOUG DC8 DC873F 302199F WP NR 2 BUSS TIE FAILED A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SO 01 852UP 46052 INSPECTION TYPE:N/A, BEFORE BLOCK OUT NR 2 BUS WENT OFF LINE AND LIGHT SMOKE WAS OBSERVED IN THE COCKPIT. REMOVED AND R EPLACED NR 2 BUS TIE RELAY W/REF TO M/M 24-20-03. RAN ALL ENGINES, NR 2 BUS TIE OPERATES NORMALLY, W/REF TO M/M 24-20-0 0. NO SMOKE OBSERVED IN COCKPIT. 2 L 7 4 4F RT 4A25 2001032000120 20010320 00120 WP 2001 3 20 TWAA0103311 1 20010216 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT IN THE FWD CABIN, FOUND CORROSION ON FLOOR PAN AT STA 160 TO 169, LBL 9 INCHES. INSTALLED REPAIR P ER SRM 51-70-4. INSTALLED FASTENERS PER SRM 51-30-2. TREATED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001032000121 20010320 00121 WP 2001 3 20 TWAA0103312 1 20010216 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT FOUND 4 INTERCOSTALS UNDER THE MEMBRANE AT STA 160 TO 200, LBL 55 INCHES, WERE CORRODED. REMOVED L IGHT CORROSION FROM INTERCOSTAL AT STA 175.688 AND 193.688. REPLACED INTERCOSTALS AT STA 167.688 AND STA 185.688 PER DR AWING 9936534. 2 L 7 2 4F A6WE 2001032000122 20010320 00122 WP 2001 3 20 TWAA0103313 1 20010216 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FWD CARGO BAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT FOUND HEAVY CORROSION IN FWD CARGO COMPT ON RT TIE DOWN TRACK, STA 332 TO 370. REMOVED CORROSION P ER SRM 51-10-3 PAGE 21 PARA 35. FABRICATED NEW TRACK PER SAMPLE AND SPM 6-70-01. PRIMED AND PAINTED PER SRM 51-10-3. INSTALLED WITH FASTENERS PER SRM 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 2001032000123 20010320 00123 WP 2001 3 20 TWAA0103314 1 20010216 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT IN THE FWD CABIN FOUND CORROSION ON FLOOR SUPPORT AT STA 200, LBL 8 INCHES. INSTALLED NEW FLOOR SU PPORT PER DRAWING 9936534. INSTALLED FASTENERS PER SRM 51-30-1. 2 L 7 2 4F A6WE 2001032000124 20010320 00124 WP 2001 3 20 TWAA0103315 1 20010217 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP AFT CARGO BAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND CORROSION ON RT TIE DOWN TRACK FROM STA 1212 THRU 1320. REPLACED TRAC K PER SPM 6-70-01, PAGE 2 AND 3 AND DRAWING 5936663. FABRICATED FROM STOCK AND INSTALLED PER 5936663-505 FOR ASSEMBLY A ND SRM 51-30-1 PARAGRAPH 6 AND PAGE 13. 2 L 7 2 4F A6WE 2001032000125 20010320 00125 WP 2001 3 20 TWAA0103316 1 20010218 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP AFT CARGO BAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT IN AFT CARGO COMPT FOUND CORROSION ON UNDERSIDE OF RT TIE DOWN TRACK, BETWEEN STA 1309 AND 1320. R EPLACED TRACK PER SPM 6-70-01 PAGE 2 AND 3 AND DAC DRAWING 5936663. FABRICATED FROM STOCK AND INSTALLED PER 5936663-505 ASSEMBLY AND SRM 51-30-1 PARA 6 AND PAGE 13. 2 L 7 2 4F A6WE 2001032000126 20010320 00126 WP 2001 3 20 TWAA0103317 1 20010218 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT FOUND CORROSION ON TOP OF INTERCOSTAL BETWEEN STA 1322 AND 1338, BELOW LONGERON 21L, AND ON 2 ADJAC ENT INTERCOSTALS BETWEEN STA 1322 AND 1338 AND LONGERON 21L AND 22L. REMOVED INTERCOSTALS FOR REPLACEMENT. REMOVED COR ROSION ON SKIN PER SPM 6-80-01. INSTALLED NEW INTERCOSTALS AND FASTENERS WITH RIVETS PER SRM 51-30-02. 2 L 7 2 4F A6WE 2001032000127 20010320 00127 WP 2001 3 20 TWAA0103318 1 20010215 A 5320 SPLICE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT FOUND CORROSION ON LONGERON SPLICE AT STA 1193, LONGERON 29L. REMOVED CORROSION BY REPLACEMENT OF PART. INSTALLED FABRICATED PART MANUFACTURED PER DRAWING 3914677 AND INTERSHOP TAG 892670. INSTALLED FASTENERS PER SRM 51-30-5. 2 L 7 2 4F A6WE 2001032000128 20010320 00128 WP 2001 3 20 TWAA0103319 1 20010215 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT FOUND FLOOR SUPPORT CORRODED AT SEVERAL PLACES STA 1136 TO 1212, RBL 8 INCHES. INSTALLED NEW SUPPO RT PER DRAWING 5936660. INSTALLED BOLTS, WASHERS AND NUTS PER SRM 51-30-1. 2 L 7 2 4F A6WE 2001032000129 20010320 00129 WP 2001 3 20 TWAA0103320 1 20010215 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT FOUND TOP OF FLOOR SUPPORT CORRODED IN SEVERAL PLACES AT STA 1155, BETWEEN LBL 15 AND RBL 07. INST ALLED NEW SUPPORT REF IPC 25-52-00 FIG 3L. SRM 51-30-2 RIVET INSTALLATION. 2 L 7 2 4F A6WE 2001032000130 20010320 00130 WP 2001 3 20 TWAA0103321 1 20010210 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT IN FWD CARGO COMPT FOUND CORROSION ON BOTTOM OF FLOOR SUPPORT AT STA 138, AT INTERSECTION WITH LONG ERON 18R, CORROSION ON REAR OF BULKHEAD AT STA 1338 APPROX 18 INCHES INBD OF LONGERON 18R, AND CORROSION AT STA 1338 EXT REME UPPER RT FWD CORNER OF BULKHEAD JUST BELOW LONGERON 18R. ABOVE 3 WRITE-UPS ARE ON THE SAME FLOORBEAM. REPAIRED PE R SRM 53-05 FIG 108. ALL PARTS PRE-PAINTED. 2 L 7 2 4F A6WE 2001032000131 20010320 00131 WP 2001 3 20 TWAA0103322 1 20010215 A 5311 FORMER DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT FOUND FORMER WITH CORROSION AT STA 1338, 5 INCHES ABOVE LONGERON 18R AT ATTACH POINT FOR LAV TANK H OLD DOWN CABLE. REPAIRED FORMER PER SRM 53-03 FIG 14 PAGE 37. TREATED BARE METAL PER 51-10-3. ALL REPAIR PARTS PRE PA INTED. 2 L 7 2 4F A6WE 2001032000132 20010320 00132 WP 2001 3 20 TWAA0103323 1 20010216 A 5311 FORMER DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT FOUND CORROSION ON FORMER 1338, 4 INCHES ABOVE LONGERON 18L, AFT OF LAV TANK HOLD DOWN CLIP, BETWEE N CLIP AND FORMER. REPAIRED PER SRM 53-03 FIG 14. TREATED METAL PER SRM 51-10-03. 2 L 7 2 4F A6WE 2001032000133 20010320 00133 WP 2001 3 20 TWAA0103324 1 20010219 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT FOUND CORROSION ON LONGERON 29L, STA 1287 TO 1308. REMOVED CORROSION BY REPLACING PART. INSTALLED NEW LONGERON PER SRM 53-14-3, PAGE 21. INSTALLED FASTENERS PER SRM 51-30-02 AND 51-30-5. 2 L 7 2 4F A6WE 2001032000134 20010320 00134 WP 2001 3 20 TWAA0103325 1 20010216 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT FOUND CORROSION ON BOTTOM OF LONGERON 20R AT INTERSECTION WITH STA 1338 AND TIE CLIP AT END OF LONG ERON. REMOVED CORRODED EXTRUSION SECTION AND INSTALLED EXTRUSION AND REPAIR SPLICE FROM STA 1314 TO 1338 PER SRM 53-02 FIG 18. 2 L 7 2 4F A6WE 2001032000135 20010320 00135 NM 2001 3 20 PCAA0102009 1 20010218 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN MALFUNCTIONED A PCAA K NONE O OTHER CR CRUISE 1 EA 13 830EX 155 LGA-FLIGHT 3635. CREW REPORTED FLOOR LEVEL EMERGENCY LIGHTS AND GALLEY LIGHT SWITCH CAME ON AND FLICKERED FOR 30 MINUTE S AFTER TAKEOFF. MAINTENANCE CLEANED CANNON PLUG ON FLIGHT ATTENDANTS PANEL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNE D TO SERVICE. 2 H 7 2 4T RT A13NM 2001032000136 20010320 00136 2001 3 20 SWIA972369 4 20010211 A 3414 INDICATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT FAILED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 576SW 120345 ON TAKEOFF AT 80 KTS, HIGH SPEED AURAL SOUNDED. ABORTED TAKEOFF. REMOVED AND REPLACED FIRST OFFICERS HIGH SPEED INDICA TOR WITH SERVICEABLE. PERFORMED OPS CHECK WITH PITOT STATIC BOX. OPS CHECK GOOD. LEAK CHECK GOOD IAW MM 34-12-01. (S /N ON: 1795) (S/N OFF: AH732). 2 L 7 2 4T 4 T RT A31SO E20NE 2001032000137 20010320 00137 SO 2001 3 20 SWIA972370 1 20010212 A 2910 HYDRAULIC LINE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE HYD SYSTEM CHAFED A SWIA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 NM 07 583SW 120351 ON APPROACH RECIEVED A GREEN (LEFT) SYTEM LOW LEVEL LIGHT GAUGE SHOWED TOP OF YELLOW ARC. A FEW MINUTES LATER RECEIVED A LOW PRESSURE LIGHT. THEN A FEW MINUTES LATER RECEIVED A MAIN PUMP LOW PRESSURE LIGHT WITH THE ELEC HYDRAULIC PUMP ON LIGHT. THE HYDRAULIC FLUID LEVEL GAUGE DID SHOW A SLOW DECREASE IN FLUID LEVEL THE ENTIRE TIME. LANDED NORMALLY WITH G AUGE SHOWING IN MIDDLE OF YELLOW ARC. ELEC PUMP RAN EMTPY APPROXIMATELY 5 MINUTES AFTER LANDING. TROUBLESHOT SYSTEM FO R LEAKS. FOUND CHAFED LINE AT GREEN HYD SYTEM MAIN ENGINE DRIVEN PUMP PRESSURE LINE. REMOVED AND REPAIRED LINE TO SERV ICEABLE CONDITION. OPS CHECK GOOD. NO LEAKS NOTED. ALL HYDRAULIC SYSTEMS AND EQUIPMENT OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032000138 20010320 00138 2001 3 20 SWIA972371 4 20010217 A 3425 COMPUTER EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 284YV 120284 ON BEGINNING OF TAKEOFF ROLL, A SINGLE CHIME SOUNDED AND THE ATTITUDE DISPLAY MAP LIGHT ILLUMINATED WITH ASSOCIATED PIT AND ROLL FLAGS ON THE CAPTS EHSI. ABORTED TAKEOFF. REORIENTED NR 1 AHRS COMPUTER. GROUND CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032000139 20010320 00139 EA 2001 3 20 SWIA972372 1 20010204 A 3240 SHUTOFF VALVE CNDAIR CL600 CL6002B19 EA BRAKE SYSTEM FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 412SW 7101 AFTER TAKEOFF, PARK BRAKE SOV CAUTION MESSAGE ILLUMINATED. RETURNED TO SLC. REMOVED AND REPLACED PARKING BRAKE SHUTOFF VALVE IAW 32-45-11. OPS AND LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2001032000140 20010320 00140 SO 2001 3 20 SWIA972374 1 20010218 A 2750 FCU EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FLAPS FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 195SW 120127 RECEIVED FLAP CONTROL FAULT ON GROUND. FLAPS WOULD NOT RESET. REMOVED AND REPLACED FCU IAW EMB MM 27-50-06. OPS CHECK GOOD. (P/N: 3077500-1007) (S/N ON: 0093) (S/N OFF: 0033). 2 L 7 2 4T 4 T RT A31SO E20NE 2001032000141 20010320 00141 SO 2001 3 20 SWIA972375 1 20010218 A 2720 RUDDER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TAIL VIBRATION A SWIA O OTHER E F VIBRATION/BUFFET FLT CONT AFFECTED CR CRUISE 1 NM 07 583SW 120351 RUDDER HAS A VIBRATION WITH YAW AND/OR RUDDER ON AND OFF. SEEMS TO LESSEN AS RUDDER TRIM APPROACHED ZERO. INSPECTED RU DDER AND RUDDER TRIM IAW EMB 120 MM 27-21-00 PG 601. NO DEFECTS NOTED. AIRCRAFT IS OK FOR RETURN TO SERVICE. ALL PANE LS ARE CLOSED. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032000142 20010320 00142 SO 2001 3 20 SWIA972376 1 20010219 A 3150 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE COCKPIT ACTIVATED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 293SW 120320 ABORTED TAKEOFF DUE TO AURAL WARNING FOR TRIM. AURAL WARNING SOUNDS AT INDEX OF 32-31, OK AT INDEX OF 30. ADJUSTED BOT H AURAL WARNING PROXIMITY SENSORS. OPS CHECK GOOD IAW EMB120 MM. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032000143 20010320 00143 EA 2001 3 20 SWIA972377 1 20010219 A 5210 DOOR CNDAIR CL600 CL6002B19 EA PAX DOOR LACK OF LUBE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 409SW 7056 DURING CLIMBOUT, PAX DOOR HANDLE OUT (CAUTION) MESSAGE CAME ON EICAS. QRH PROCEDURE CALLS FOR RE-STOWING THE DOOR HANDL E. WHEN THIS WAS DONE MASTER WARNING CAUTION DOOR MESSAGE CAME ON (RED). AS PER QRH AIRCRAFT WAS LANDED AT NEAREST SUI TABLE AIRPORT. PAX DOOR AMBIENT NOISE WAS HIGH. INSPECTED DOOR, FOUND TO NEED LUBRICATION. LUBRICATED DOOR AND FUNCTI ONAL CHECK THROUGH 20 CYCLES. CHECKS OK AT THIS TIME. 2 L 7 2 4F RT A21EA 2001032000144 20010320 00144 EU 2001 3 20 XNA01004 1 20010213 A 3230 LANDING GEAR AIRBUS 300 A300B4203 3930306 EU MLG FAILED A TC8A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 474AS 219 MLG WILL NOT RETRACT. USED ALTERNATE SYSTEM. NO HELP. 2 L 7 2 4F RT A35EU 2001032000145 20010320 00145 NM 2001 3 20 01FDEA00156 1 20010222 A 3231 SEAL BOEING 727 727227 1384078 NM NLG DOOR BINDING A FDEA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 25 496FE 21670 NOSE GEAR DOOR LIGHT CAME ON WHEN GEAR DOWN. RECYCLE AND DOOR LIGHT CAME ON AGAIN. HYD PRESS NORMAL. FOUND SEAL BINDI NG THE LNG DOOR. REMOVED SEAL FROM AC 124 AND INSTALL ON THIS AC. AC OK TO CONTINUE. 2 L 7 3 4F A3WE 2001032000146 20010320 00146 2001 3 20 DHL2001801001 4 20010222 A 3425 177836623 INDICATOR DOUG DC8 DC873F 302199F WP COCKPIT FAILED A DHLA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 801DH 46033 F/O''S HSI IS FROZEN, OFF FLAG INTERMITTENT. REPLACED AND TESTED F/O HSI PER M/M 34-21-0. ALL TESTED GOOD. 2 L 7 4 4F RT 4A25 2001032000147 20010320 00147 EU 2001 3 20 RAIA00102006 1 20010221 A 5751 1415762412 FAIRING JETAIR JETSTM JETSTM4101 1500501 EU RT AILERON DAMAGED A RAIA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 CE 03 556HK 12939 41073 5391-EWR- DURING TAXI OUT CREW REPORTED RIGHT AILERON TIP FAIRING DAMAGED. CREW RETURNED TO GATE. MAINTENANCE INSPECTE D, PERFORMED HIDDEN DAMAGE INSPECTION, AILERON TRAVEL/DEFLECTION CHECK. MAINTENANCE REPLACED RIGHT AILERON TIP FAIRING. 2 L 7 2 4T RT A41NM 2001032000148 20010320 00148 2001 3 20 MWEA010169 4 20010219 A 3418 80098717 STALL WARNING DOUG DC9 DC932 3022066 WP LT FUSELAGE MALFUNCTIONED A MWEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 602ME 48133 AFTER GEAR UP, AIRCRAFT FAILED TO PRESSURIZE AND STALL INDICATION FAILURE LIGHT CAME ON AT FLAPS 5 DEGREES. MAINTENANCE FOUND OUTFLOW VALVE WAS INLOCKED OPEN/MANUAL POSITION ON PEDESTAL. RETURNED TO OPEN/AUTO POSITION. ALSO REMOVED AND R EPLACED LEFT ANGLE OF ATTACK SENSOR. 2 L 7 2 4F A6WE 2001032000149 20010320 00149 NE 2001 3 20 COMA0110035 3 20010219 A 6111 8175972 SPRING HAMLTN EMB 120 EMB120RT SO HAMSTD 14RF 14RF9 NE PROP BLADE BROKEN A COMA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 269CA 32 120263 910519 ON POST-FLIGHT INSPECTION, CREW NOTICED OIL LEAKING FROM LEFT PROPELLER. MAINTENANCE DETERMINED SOURCE TO BE THE NR 1 P ROP BLADE. THE BLADE WAS REMOVED, AND THE BLADE SEAL COIL SPRING WAS FOUND TO BE BROKEN. THE BLADE SEAL ASSEMBLY WAS R EPLACED, THE BLADE REINSTALLED, AND THE PROPELLER RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 6 C P11NE 2001032000150 20010320 00150 EA 2001 3 20 COMA0160271 1 20010220 A 3230 46193 PRIORITY VALVE CNDAIR CL600 CL6002B19 EA MLG MALFUNCTIONED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 951CA 13203 7091 GEAR DISAGREE WARNING, NLG SLOW TO EXTEND. REPLACED THE MLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2001032000151 20010320 00151 EA 2001 3 20 COMA0160272 1 20010220 A 3230 SENSOR CNDAIR CL600 CL6002B19 EA NLG OUT OF ADJ A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 798CA 7348 NLG DID NOT RETRACT. ADJUSTED THE NLG CENTERED PROXIMITY SENSOR, TO M/M SPECIFICATIONS. 2 L 7 2 4F RT A21EA 2001032000152 20010320 00152 EA 2001 3 20 COMA0160273 1 20010220 A 4900 APU CNDAIR CL600 CL6002B19 EA FUSELAGE MALFUNCTIONED A COMA K NONE O OTHER CR CRUISE 1 SO 01 959CA 7116 APU SHUT DOWN IN FLIGHT. SECURED APU AND DEFERRED MAINTENANCE PER MEL. 2 L 7 2 4F RT A21EA 2001032000154 20010320 00154 EU 2001 3 20 0100523207 1 20010216 A 2910 D3247002302300 HYDRAULIC LINE AIRBUS 320 A320211 3930320 EU RT MLG WW LEAKING A NWAA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 307US 106 DURING CRUISE, RECEIVED HYD Y RSVR LO LVL MESSAGE. FOLLOWED COM PROCEDURES, CONTINUED TO FINAL DESTINATION, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED HYDRAULIC LINE BETWEEN THE AUTO BRAKE SELECTOR AND PARK BRAKE VALVE. NO OTHER L EAK NOTED. 2 L 7 2 4F RT A28NM 2001032000155 20010320 00155 NM 2001 3 20 0100536642 1 20010221 A 3350 BATTERY BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 642NW 21942 DURING OVERNIGHT LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE BETWEEN PASSENGER ENTRANCE DOORS 2 AND 3. MAINTENANCE REPLACED POWER SUPPLY AND BATTERY LIGHT. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F A20WE 2001032000156 20010320 00156 NM 2001 3 20 0100546308 1 20010216 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 668US 24223 DURING OVERNIGHT LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE BETWEEN SOWS 51HJK-65HJK. MAINTENANCE REC ONNECTED LIGHT ASSEMBLY AT 51K. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001032000157 20010320 00157 NM 2001 3 20 0100556307 1 20010217 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 667US 24222 DURING OVERNIGHT LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE BETWEEN ROWS 31-43. MAINTENANCE RECONNECT ED LOOSE WIRE. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001032000158 20010320 00158 NM 2001 3 20 0100566729 1 20010214 A 3610 CLAMP BOEING 747 747251F 1384898 NM PWA JT9 JT9D7J 52054 NE NR 1 ENGINE FAILED A NWAA E F J A ENGINE SHUTDOWN ACTIVATE FIRE EXT. DUMP FUEL UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 GL 01 629US 22388 689562 DURING INITIAL CLIMB AT 300 FEET, THE NR 1 ENGINE FIRE WARNING ACTIVATED. THE NACELLE TEMPERATURE INDICATION WAS PEGGED IN THE WARNING RANGE AND THE POWER LEVER WAS STUCK IN MID RANGE. THE ENGINE WAS SHUT DOWN PER COM AND ONE FIRE BOTTLE WAS DISCHARGED. AFTER DUMPING 60K LBS OF FUEL, THE AIRCRAFT RETURNED TO KIX AND LANDED WITHOUT INCIDENT. MAINTENANCE I NSPECTED THE ENGINE AND FOUND A FAILED PNEUMATIC DUCT CLAMP. THE ENGINE WAS REPLACED. 2 L 7 4 4F 4 F A20WE E20EA 2001032000159 20010320 00159 NE 2001 3 20 0100571158 2 20010216 A 7261 ENGINE DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 1 ENGINE LEAKING A NWAA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 158US 46767 686132 DURING CLIMB AFTER TAKEOFF, THE CREW REPORTED SMOKE ENTERING THE CABIN FROM A PNEUMATIC SOURCE. THE FLIGHT RETURNED TO LAX AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED THE NR 1 ENGINE TO BE LEAKING OIL AN D CONTAMINATING THE NR 1 PNEUMATIC SYSTEM. THE AIRCRAFT WAS FERRIED TO MSP TO REPLACE THE NR 1 ENGINE. 2 L 7 3 4F 4 F A22WE E20EA 2001032000160 20010320 00160 2001 3 20 0100585532 4 20010213 A 2565 031042190 SLIDE BOEING 757 757251 1384970 NM CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 532US 17972 12493 24263 DURING SLIDE SHOP TEST, INFLATABLE SUB ASSEMBLY RUPTURED DURING FLAT FIRE PROCEDURE AT NORMAL OPERATING PRESSURE. INFLA TABLE SEAMS FAILED AT UPPER TUBE LEFT AND RIGHT. NEW INFLATABLE SUB ASSEMBLY WAS INSTALLED. 2 L 7 2 4F RT A2NM 2001032000161 20010320 00161 WP 2001 3 20 0100609874 1 20010217 A 2781 DUCT DOUG DC9 DC951 3022051 WP LT & RT WINGS BINDING A NWAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 01 783NC 48108 DURING APPROACH, THE SLAT DISAGREEMENT LIGHT ILLUMINATED AND AIRCRAFT HAD A NOTICEABLE ROLL THE THE RIGHT WHEN SLATS EXT ENDED. FOLLOWED COM PROCEDURES. FLAP/SLAT HANDLE WAS SPLIT. FLIGHT MADE AN UNEVENTFUL LANDING AT MSP. MAINTENANCE IN SPECTION OF SLATS DETERMINED THE LEFT T-DUCT WAS BINDING. REPLACED T-DUCT. LUBED ALL SLAT TRACKS AND ROLLERS AND INSPE CTED CABLES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 2001032000162 20010320 00162 NE 2001 3 20 0100619933 2 20010215 A 7314 378200 PUMP DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE RT ENGINE FAILED A NWAA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 GL 01 1334U 16604 2079 47280 666961 DURING FLIGHT AT FL350, THE RIGHT ENGINE CEASED OPERATING. THE FLIGHT CREW FOLLOWED COM PROCEDURES, DIVERTED TO CLE, AN D LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE ENGINE DRIVEN FUEL PUMP LOCATED ON THE RIGHT ENGINE. OPERATIONAL C HECK NORMAL. 2 L 7 2 4F 4 F A6WE E2EA 2001032000163 20010320 00163 NM 2001 3 20 0100626308 1 20010222 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 668US 24223 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE ON LEFT SIDE OF AIRCRAFT BETWEEN ROWS 21-31. MAINTE NANCE RECONNECTED LOOSE WIRE AT ROW 23L. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001032000164 20010320 00164 CE 2001 3 20 GLBA2001039 1 20010217 A 5260 12951405929 CABLE BEECH 1900 1900D 1154162 CE PAX DOOR BROKEN A GLBA K NONE O OTHER IN INSP/MAINT 1 CE 01 122UX UE122 AIRSTAIR DOOR WOULD NOT OPEN. INSPECTED DOOR, FOUND INNER DOOR CABLE BROKEN. REPLACED DOOR CABLE. 2 L 7 2 4T RT A24CE 2001032000165 20010320 00165 WP 2001 3 20 UPS01835029 1 20010222 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:IN EMERGENCY EXIT BATTERY LOW. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK. OK FOR SERVICE. 2 L 7 4 4F RT 4A25 2001032000166 20010320 00166 2001 3 20 UPS01835030 4 20010221 A 2565 BRACKET DOUG DC8 DC873F 302199F WP COCKPIT BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:IN EVAC SLIDE BRACKET BROKEN (REFER TO M209762). REMOVED AND REPLACED BROKEN BRACKET ON SLIDE COVER. R EINSTALLED SLIDE CHECKS OK. THIS CLEARS M209762. 2 L 7 4 4F RT 4A25 2001032000167 20010320 00167 WP 2001 3 20 UPS01835031 1 20010220 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:IN EMERGENCY LIGHT BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK. TESTS OK. 2 L 7 4 4F RT 4A25 2001032000168 20010320 00168 WP 2001 3 20 AT0100084 1 20010214 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 REPLACE TEMPORARY REPAIR WITH PERMANENT REPAIR AT BS 976. REPLACED REPAIR IAW DC SRM 53-04 FIG 12B, 51-10-03, AND 51-20 . 2 L 7 2 4F A6WE 2001032000169 20010320 00169 WP 2001 3 20 AT0100085 1 20010216 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP CABIN CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 FOUND LEFT INBOARD SEAT TRACK AT BS 918 - 965 CORRODED BEYOND LIMITS. REPLACED CORRODED SECTION OF SEAT TRACK IAW DC9 S RM 53-05 FIG 4B & 4F. 2 L 7 2 4F A6WE 2001032000170 20010320 00170 WP 2001 3 20 AT0100087 1 20010207 A 5310 591015899N DOOR FRAME DOUG DC9 DC932 3022066 WP AFT CARGO BAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 FOUND AFT CARGO DOOR JAMB CORRODED BEYOND LIMITS. INSTALLED NEW DOOR JAMB IAW DC9 SRM 53-05 FIG 44, 51-30-01, 51-30-02, 51-30-04, 51-10-03, 51-30-05, AND RES 01-220. 2 L 7 2 4F A6WE 2001032000171 20010320 00171 WP 2001 3 20 AT0100088 1 20010209 A 5310 DOOR FRAME DOUG DC9 DC932 3022066 WP GALLEY DOOR GOUGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 FOUND FORWARD GALLEY DOOR JAMB GOUGED BEYOND LIMITS. REMOVED GOUGED SECTION AND INSTALLED REPAIR IAW DC9 SRM 53-05 FIG 55, 51-10-02, 51-10-03, 51-10-04, 51-30-01, 51-30-02, 51-30-05, AND 53-01 FIG 1. 2 L 7 2 4F A6WE 2001032000172 20010320 00172 WP 2001 3 20 AT0100089 1 20010209 A 5320 PAN DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 FOUND G4 GALLEY FLOOR PAN CORRODED BEYOND LIMITS. FORMED AND INSTALLED FLOOR PAN AND HAT CHANNELS IAW DC9 SRM 51-10-03, 51-30-02, 53-01 FIG 1, AND 53-20 FIG 5C. 2 L 7 2 4F A6WE 2001032000173 20010320 00173 WP 2001 3 20 AT0100090 1 20010206 A 5347 CARGO TRACK DOUG DC9 DC932 3022066 WP FWD CARGO BAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 FOUND FORWARD PIT CARGO TRACK BS 239 - 340 CORRODED BEYOND LIMITS. INSTALLED NEW SECTION OF CARGO TRACK IAW DC9 SRM 51- 10-03, 51-10-04, 53-05 FIG 4C, AND 53-21. 2 L 7 2 4F A6WE 2001032000174 20010320 00174 WP 2001 3 20 AT0100091 1 20010213 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP CABIN CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 FOUND FLOOR PANEL 47 CORRODED BEYOND LIMITS. REPLACED FLOOR PANEL IAW DC9 SRM 53-21 AND 51-20-02. 2 L 7 2 4F A6WE 2001032000175 20010320 00175 WP 2001 3 20 AT0100092 1 20010214 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP CABIN CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 FOUND FORWARD CABIN FLOOR PANEL BS 155 CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW DC9 SRM 51- 10-02, 51-10-03, 51-10-04, 53-21 FIG 20 AND DC9 MM 53-20-01. 2 L 7 2 4F A6WE 2001032000176 20010320 00176 WP 2001 3 20 AT0100093 1 20010208 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 FOUND FORWARD CABIN FLOOR SUPPORT AT BS 200 CORRODED. REPLACED FLOOR SUPPORT IAW DC9 SRM 53-21, 53-11-01, AND 53-30-05. 2 L 7 2 4F A6WE 2001032000177 20010320 00177 SO 2001 3 20 GLBA2001040 1 20010217 A 3232 ACTUATOR EMB 120 EMB120ER 3260203 SO RT MLG OUT OF ADJ A GLBA O OTHER O OTHER TO TAKEOFF 1 CE 01 71GL 120071 AFTER T/O GEAR FAILED TO RETRACT. CYCLED CONTROL SEVERAL TIMES BEFORE GEAR RETRACTED. ADJUSTED RIGHT MAIN LANDING GEAR ACTUATOR AND UPLOCK SENSOR OPS CHECKED LANDING GEAR SYSTEM GOOD. 2 L 7 2 4T RT A31SO 2001032000178 20010320 00178 2001 3 20 TWAA0103401 4 20010221 A 3460 FMC BOEING 757 7572Q8 1384972 NM COCKPIT FAILED A TWAA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 CE 05 704X 28163 AIRCRAFT RETURNED FROM FLIGHT AT LAX TWICE WITH A DUAL FMC FAILURE. THE FIRST TIME THE RT FMC COMPUTER WAS REPLACED, (P /N 4052506-941-945). THE SECOND TIME THE AIRCRAFT WAS REMOVED FROM SERVICE. CHECK-C 11-20-99 LAX. 2 L 7 2 4F RT A2NM 2001032000179 20010320 00179 NM 2001 3 20 TWAA0103402 1 20010221 A 3350 LIGHT BOEING 767 767231 1385131 NM CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 610TW 22573 THE EGRESS LIGHTING WAS INOPERATIVE IN MID GALLEY AND RT SIDE OF CABIN ROWS 18 TO 23. REPLACED FLEX CABLE 5854-3 AT MID GALLEY AND FLEX CABLE 5854-5 FOR ROWS 18 TO 23. CHECK-C 12-27-00 LAX. 2 L 7 2 4F RT A1NM 2001032000180 20010320 00180 WP 2001 3 20 TWAA00103403 1 20010221 A 5312 DOUBLER DOUG DC9 DC931 3022065 WP LT MLG WW CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 992Z 47095 DURING OP 15 MAINT CHECK FOUND PRESSURE DECK BULKHEAD DOUBLER WAS CRACKED AT 718 CASTING, LT MLG WHEEL WELL. REPLACED D OUBLER AND SEALED PER SRM 51-20-0 AND 51-60-0. FASTENER SUBSTITUTION PER SRM 51-30-5 FASTENER INSTALLATION. 2 L 7 2 4F A6WE 2001032000181 20010320 00181 WP 2001 3 20 TWAA0103404 1 20010220 A 5311 FORMER DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT FOUND AIR SUPPLY VALVE HAD WORN HOLE INTO FORMER RING AT STA 1380, BELOW LONGERON 5L AND 6L. INSTA LLED DOUBLER PER SRM 53-01 FIG 4. REINSTALLED LT TEMP CONTROL VALVE PER MM 20-10-11. LEAK CHECKED. 2 L 7 2 4F A6WE 2001032000182 20010320 00182 WP 2001 3 20 TWAA0103405 1 20010221 A 5320 SUPPORT BRACKET DOUG DC9 DC982 3022082 WP AFT CARGO BAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 957U 49702 DURING CHECK-C MAINT FOUND CORROSION ON AFT CARGO COMPT TRACK SUPPORT, RT SIDE, FROM STA 1117 TO 1155, RBL 16. MADE NEW 2 ANGLE PER DRAWING 5936660 ITEM 167 FROM 7-75-0 24 HOUR HEAT TREAT OF 0.090 X 4 X 40. 2 L 7 2 4F A6WE 2001032000184 20010320 00184 NM 2001 3 20 UPS01235113 1 20010228 A 3350 1000679 LIGHT BOEING 727 72730C 1384009 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:PFLT, ON PREDEPT CK FOUND COCKPIT EMERGENCY EXIT ASSY INOP IN ARM OR ON. REMOVED AND REPLACED COCKPIT E MERGENCY EXIT LIGHT ASSY, OPS CHECK OK. 2 L 7 3 4F A3WE 2001032000185 20010320 00185 WP 2001 3 20 UPS01835108 1 20010223 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C2/3, LEFT WING CENTER L/E LOWER RIB IS CRACKED AT XW 461.372. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001032000188 20010320 00188 SO 2001 3 20 C2XA01BT018 1 20010212 A 4930 LINE EMB 145 EMB145ER 3260211 SO APU LEAKING A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 14945 145049 EWR - FLT 3605 - CREW REPORTED STRONG ODOR OF FUEL IN COCKPIT AND CABIN DURING APU START IN FIGHT. MAINTENANCE INVESTIG ATED AND PLACED APU ON NEL NR 49-00-00-C PLACARD NR 009254, AND RELEASED AIRCRAFT TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001032000189 20010320 00189 SO 2001 3 20 C2XA01BT017 1 20010211 A 4930 4501968 LINE EMB 145 EMB145ER 3260211 SO COCKPIT LEAKING A C2XA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 14945 145049 EWR - FLT 4254 - CREW REPORTED STRONG ODOR OF GAS IN COCKPIT WHEN APU STARTED IN AIR. NO ODOR WHEN STARTED ON GROUND. MAINTENANCE PERFORMED OPERATIONAL CHECK OF APU REFERENCE TO EMB145 MM 49-00-00. OPS CHECKED GOOD. LEAK CHECKED GOOD. (M) 2 L 7 2 4F RT T00011AT 2001032000190 20010320 00190 NE 2001 3 20 WRLA200102 2 20010205 A 7261 AS3209010216 PACKING DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 3 ENGINE LEAKING A WRLA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION DE DESCENT 1 EA 27 271WA 48518 NR 3 OIL QTY INDICATION 1 QT IN FLIGHT TEMP AND PRESS. OK IN CRUISE. PRESSURE LOW ON DESCENT SHUTDOWN NR 3 ENGINE. PE RFORMED VISUAL INSPECTION OF THE OIL TANK, LINES/CHIP DETECTORS. PRATT WHITNEY REP ALSO LOOKED OVER ENGINE DELTA ENGINE SHOP PERFORM GEAR BOX BOROSCOPE NO DEFECTS NOTED. OIL TANK SERVICED TO PROPER LEVEL (28 QTS ADDED). STARTS AND GROUND IDEL RUN AND LEAK CHECK AND OPS CHECKED GOOD. PRIOR TO ENGINE RUN DMI M29 FE 05-09 WAS WORKED, THE BLOCKING KIT FOR TH E NR 3 ENGINE RIGHT/HYD PUMP WAS REMOVED, THE NR 3 HYDRAULIC SYSTEM WAS FLUSHED AND A OVERHAULED HYDRAULIC PUMP WAS INST ALLED. SUBMITTER STATES, THAT THE PREFORED PACKING ON THE BEVEL GEARSHAFT PLUG WAS THE SOURCE OF THE LEAK. DURING THE 2 L 7 3 4F 4 F RT A22WE E24NE 2001032000191 20010320 00191 NM 2001 3 20 20010320SG001 1 20010211 A 7711 INDICATOR BOEING 727 727224 1384076 NM COCKPIT MALFUNCTIONED A FX7A C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 19 79750 22452 ABORTED TAKEOFF DUE TO A LOW EPR INDICATION AT REDUCED POWER ON ENGINE NR 2. INSPECTED AND CREW RAN ENGINE UP TO MAX PO WER. NR 2 ENGINE OPS PROPERLY ON GROUND ENGINE RUN AND ALL ENGINE INDICATIONS READ NORMAL AS PER TRIM CHART 71-00-87. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001032000192 20010320 00192 NM 2001 3 20 20010320SG002 1 20010114 A 2750 285N001132 FSEU BOEING 757 75723A 1384967 NM FLAPS FAILED A N8TA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 WP 19 757NA 24567 ON APPROACH, WHEN FLAPS 30 WAS SELECTED FLAPS WOULD NOT EXTEND BEYOND 25, LEADING EDGE LIGHT CAME ON. NORMAL FLAPS 25 L ANDING ACCOMPLISHED. ADJUSTED SLAT 5 LOSS SENSING SENSOR AND REPLACED FSEU. (M) 2 L 7 2 4F RT A2NM 2001032000200 20010320 00200 WP 2001 3 20 USAAD01027 1 20010210 A 3510 15830AB REGULATOR DOUG DC9 DC982 3022082 WP COCKPIT FAILED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 818US 48098 RSW-PIT - FLT 1032 - DURING CRUISE, THE CREW OXYGEN SUPPLY PRESSURE DROPPED TO ZERO. THE AIRCRAFT DIVERTED TO CLT AND L ANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE CAPTAINS OXYGEN REGULATOR PANEL. (M) 2 L 7 2 4F A6WE 2001032000201 20010320 00201 WP 2001 3 20 USAAD01026 1 20010209 A 3220 1D322404REVC PISTON DOUG DC9 DC931 3022065 WP NLG FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 922VJ 40766 2003 48142 STL-PIT - FLT 742 - AFTER TAKEOFF, THE LANDING GEAR WAS RETRACTED THE NOSE GEAR UNSAFE LIGHT STAYED ILLUMINATED. THE AI RCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE GEAR PISTON AXLE ASSEMBLY. (M) 2 L 7 2 4F A6WE 2001032000202 20010320 00202 WP 2001 3 20 USAAD01025 1 20010209 A 2120 700569400112 FLEX DUCT DOUG DC9 DC981 3022081 WP FUSELAGE RUPTURED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 814US 48094 MCO-PIT - FLT 1120, DURING CRUISE, SMOKE AND FUMES STARTED EMITTING FROM THE RIGHT REAR LAVATORY. THE AIRCRAFT DIVERTED TO JAX AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AIR CONDITIONING DUCTING OVERHEATING DUE TO A RUPTURED FLEXI BLE DUCT AT THE RIGHT AIR CONDITIONING ACM. THE DUCT WAS REPLACED AND ALL CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 2001032000203 20010320 00203 WP 2001 3 20 USAAD01024 1 20010208 A 3260 1D32140201 HARNESS DOUG DC9 DC931 3022065 WP LT MLG SHORTED A USAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 19 922VJ 48142 AVP-PHL - FLT 1819 - AFTER TAKEOFF, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON. THE FLIGHT CREW ACCOMPLISHED Q RH PROCEDURES AND RECYCLED THE GEAR. THE FLIGHT LANDED AT PHL WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT MLG PROX IMITY HARNESS. THE GEAR WAS SWUNG SEVERAL TIMES AND OPS CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 2001032000204 20010320 00204 WP 2001 3 20 USAAD01023 1 20010207 A 3260 1D32140201 HARNESS DOUG DC9 DC931 3022065 WP LT MLG SHORTED A USAA O OTHER J WARNING INDICATION CR CRUISE 1 EA 19 955VJ 47593 PHL-SYR - FLT 562 - THE LEFT MAIN LANDING GEAR UNSAFE LIGHT CAME ON DURING FLIGHT. THE FLIGHT CREW ACCOMPLISHED QRH PRO CEDURES AND RECYCLED THE GEAR. THE LIGHT REMAINED ON, THEN WENT OFF OCCASIONALLY. THE FLIGHT LANDED AT SYR WITHOUT INC IDENT. MAINTENANCE REPLACED THE LEFT MLG PROXIMITY HARNESS. SENSORS TESTED GOOD. (M) 2 L 7 2 4F A6WE 2001032000248 20010320 00248 NM 2001 3 20 2001UALA00099 1 20010211 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 538UA 25222 EXTERNAL FUSELAGE DENTED-CREASED AT FUSELAGE STATION 560 BETWEEN STRINGER 26LT AND STRINGER 26. SUPPLEMENTAL DATA UPDATE DAMAGE WAS CUTOUT IN THE LOWER SKIN MEASURING 5.5 LONGITUDINALLY BY 14.25 CIRCUMFRENTIALLY, SPANNING FROM THE S-26L LAP SEAM TO ONE FASTENER ROW INBOARD OF S-28L. DAMAGE REMOVAL TO THE UPPER SKIN RESULTED IN A CUTOUT MEASURING 2.75 LONGIT UDINALLY BY 1.75 CIRCUMFRENTIALLY. THE REPAIR INCLUDED A STRUCTURAL FILLER/DOUBLER BUTT AGAINST THE LOWER SKIN, AND A TRIPLER OVER THE UPPER AND LOWER SKIN. THE TRIPLER EXTENDS THREE ROWS BEYOND CUTOUT IN THE LOWER SKIN. THE DOUBLER EXT ENDS ONE ROW BEYOND THE TRIPLER ON THE FORWARD, AFT, AND LOWER EDGE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001032100096 20010321 00096 NM 2001 3 21 01FDEA00127 1 20010215 A 5311 FRAME BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 WHILE WORKING NR-329 FOUND CRACK IN FRAME AT BS 540, RBL 3, WL 156. *S/D* REMOVED, REPLACED, FAB, ALODINED AND PRIMED PER FEDEX SRM 51-40-3 FIG 1 AND 51-20-1 FIG 3 & 7, 51-30-2, 51-10-2. 2 L 7 3 4F RT A3WE 2001032100097 20010321 00097 NM 2001 3 21 01FDEA00128 1 20010215 A 5315 BAC149027347075 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION (C53-224-01,1) ON BS 328 FLOORBEAM UPPER CHORD, LBL 4, WL 208. *S/D* OUT OF LIMITS PER FEDEX SRM 53-10-1. R EMOVED AND REPLACED PER FEDEX DWG SR 27-53-017. 2 L 7 3 4F RT A3WE 2001032100098 20010321 00098 NM 2001 3 21 01FDEA00129 1 20010215 A 5315 BAC1505100240 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION (C53-224-01) ON BS 312 FLOORBEAM UPPER CHORD LBL 4, WL 208. *S/D* OUT OF LIMITS PER IAW FEDEX SRM 53-10-1. FAB ANGLE AND FILLER PER IAW FEDEX SRM DWG 27-53-017. INSTALLED ALL FASTENERS PER IAW FEDEX SRM 51-30-5, 51-30-2 AND MM 51-20-151. 2 L 7 3 4F RT A3WE 2001032100099 20010321 00099 NM 2001 3 21 01FDEA00130 1 20010215 A 5313 65562392 STRINGER BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION (C53-111-01,2) ON I/B SIDE OF STR 27 RT, BS 680. *S/D* REMOVED AND REPLACED STR CAP PER FEDEX SRM 51-30-2. CAP FOUND OUT OF LIMITS PER FEDEX SRM 53-10-1. 2 L 7 3 4F RT A3WE 2001032100100 20010321 00100 NM 2001 3 21 01FDEA00131 1 20010216 A 5313 BAC1498158 STRINGER BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CRACKED STR BS 720B+4, STR 15L. *S/D* REMOVED, REPLACED, FAB, ALODINED, AND PRIMED PER FEDEX SRM 51-10-2 AND 53-10-3. 2 L 7 3 4F RT A3WE 2001032100101 20010321 00101 NM 2001 3 21 01FDEA00146 1 20010220 A 3260 SWITCH BOEING 727 727227 1384078 NM COCKPIT DIRTY A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 483FE 21465 WHEN PUTTING GEAR HANDLE IN OFF AFT T/O RED DOOR LIGHT AND RG DOOR LIGHT ILLUM. REPOSITIONED HANDLE TO UP AND LIGHTS WE NT OUT. *S/D* FOUND SWITCH AND CANNON PLUG DIRTY. CLEANED, OPS CK OK. 2 L 7 3 4F A3WE 2001032100102 20010321 00102 NM 2001 3 21 01FDEA00155 1 20010221 A 2612 4205840000 HARNESS DOUG MD11 MD11F 3023600 NM FIRE DETECTION FAULTY A FDEA J A DUMP FUEL UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 619FE 48770 IN CRUISE GEAR UP RECD INTERMITTENT FIRE DET 3 FAIL ALERT. CLEARANCE AND PERM TO DUMP FUEL ON RADAR VECTORS. FOUND TER MINAL LUG LOOSE AT DH22C FOR LOOP-B TIGHTENED. FOUND OPEN WIRE BETWEEN DH23C & DH4C OF LOOP-A. REMOVED AND REPLACED WI RE HARNESS PER MM. NO PNEU LEAKS FOUND. RAN RTS PASSED. PERF A HIGH PWR ENG RUN, OPS CK GOOD. AC OK FOR SERVICE. 2 L 7 3 4F RT A22WE 2001032100103 20010321 00103 WP 2001 3 21 AT0100086 1 20010207 A 5310 WEB DOUG DC9 DC932 3022066 WP R1 DOOR JAMB CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 FOUND R-1 DOOR JAMB LOWER CORNER SKIN CRACKED. CUT OUT CRACK AND INSTALLED REPAIR IAW EO 09-5310-29-E1472. 2 L 7 2 4F A6WE 2001032100104 20010321 00104 WP 2001 3 21 TWAA0103406 1 20010221 A 5542 SKIN DOUG DC9 DC982 3022082 WP RUDDER DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 957U 49702 DURING CHECK-C MAINT FOUND RUDDER WITH DAMAGE SPOT ON RT SIDE, FWD OF RUDDER TAB UPPER HINGE AREA, GROUND THRU FLAME SPR AY. REPAIRED DAMAGE PER SRM 51-70-1A, FIG 58. RUDDER PAINTED AND BALANCED. 2 L 7 2 4F A6WE 2001032100105 20010321 00105 WP 2001 3 21 TWAA0103407 1 20010129 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT FOUND CHAIR TRACK WITH HEAVY CORROSION AT STA 1130 TO 1322, LBL 22 INCHES. REMOVED AND REPLACED TR ACK PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-01, STA 1307 TO 1028. TRACK PREPAINTED. 2 L 7 2 4F A6WE 2001032100106 20010321 00106 CE 2001 3 21 GLBA2001043 1 20010221 A 3260 SENSOR BEECH 1900 1900D 1154162 CE RT MLG OUT OF ADJ A GLBA A D UNSCHED LANDING RETURN TO BLOCK O OTHER CL CLIMB 1 CE 01 211UX UE211 RETURN TO BLOCK, MAIN LANDING GEAR WOULD NOT RETRACT. INSPECTED FOUND RIGHT PROX SENSOR OUT OF ADJUSTMENT. ADJUSTED PR OX SENSOR, OPS CHECKED LANDING GEAR SATISFACTORY. 2 L 7 2 4T RT A24CE 2001032100107 20010321 00107 EA 2001 3 21 A6WA200100014 2 20010211 A 7310 1WN05799 FLOW DIVIDER LYC BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502* 41580 EA NR2 ENGINE LEAKING A A6WA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 GL 31 291UE 4223 1628 LF05771A E2084 LF05771A DURING START OF NR 2 ENGINE, A FLIGHT ATTENDANT AND SEVERAL PASSENGERS VERBALLY REPORTED FIRE. NO INDICATION IN COCKPIT . THE NR 2 ENGINE WAS SHUTDOWN AND BOTH FIRE BOTTLES WERE RELEASED. ACFT WAS EVACUATED VIA RT SIDE EVACUATION SLIDES. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE. 2 H 7 4 4F 4 F RT A49EU E6NE 2001032100108 20010321 00108 NM 2001 3 21 DHL2001705002 1 20010223 A 3260 CONNECTOR BOEING 727 72722C 138400F NM NLG DIRTY A DHLA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 705DH 19191 ON GEAR EXTENSION, RECEIVED NO GREEN-LIGHT ON NOSE GEAR INDICATION ON FWD CENTER PANEL. AFTER LANDING AND DURING ROLLOU T LIGHT INDICATION ILLUMINATED AS NORMAL. CLEANED CONNECTOR ON NOSE DOWNLOCK SWITCH. COMPLIED WITH NOSE GEAR LOCK TEST PER B727 MM CH 32-61-2. OPS CHECK GOOD. NO DEFECTS NOTED. 2 L 7 3 4F A3WE 2001032100109 20010321 00109 WP 2001 3 21 MWEA010170 1 20010223 A 5210 9929480519 BEAM DOUG DC9 DC932 3022066 WP VENTRAL DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 VENTRAL STAIR DOOR, LOWER LEFT HAND SIDE BEAM IS CRACKED IN 2 AREAS. REMOVED, FABRICATED AND INSTALLED BEAM. 2 L 7 2 4F A6WE 2001032100110 20010321 00110 WP 2001 3 21 MWEA010171 1 20010223 A 5320 5956034557 BRACKET DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 BRACKET AT STATION 484 BETWEEN LONGERON 27 RIGHT AND LONGERON 28 RIGHT AT FORWARD END OF INTERCOSTAL IS CORRODED AND CRA CKED. REMOVED, FABRICATED AND INSTALLED BRACKET. 2 L 7 2 4F A6WE 2001032100111 20010321 00111 WP 2001 3 21 MWEA010172 1 20010223 A 5330 59114023 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 CRACK ON FUSELAGE OUTER SKIN AT STATION 130, LONGERON 14 LEFT ABOVE PAX DOOR HOLD OPEN CUP. REMOVED, FABRICATED AND INS TALLED PLATE AND DOUBLER. 2 L 7 2 4F A6WE 2001032100112 20010321 00112 WP 2001 3 21 MWEA010173 1 20010223 A 5320 9958167401 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 CENTER CEILING INTERCOSTAL STATION 895-917 IS BENT. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001032100113 20010321 00113 WP 2001 3 21 MWEA010174 1 20010223 A 5320 99581703 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 CENTER CEILING INTERCOSTAL AND STRAP DENTED AT STATION 917. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001032100114 20010321 00114 WP 2001 3 21 MWEA010175 1 20010223 A 5412 991224381 WEB DOUG DC9 DC932 3022066 WP LT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 LEFT FUSELAGE BULKHEAD SKIN WEB AT PYLON FRONT SPAR BELOW LONGERON 17 IS CRACKED, APPROXIMATELY 6 INCHES OF FUSELAGE SKI N AND JUST ABOVE FLOOR LINE. REMOVED WEB, FABRICATED AND INSTALLED WEB AND STIFFENER. 2 L 7 2 4F A6WE 2001032100115 20010321 00115 WP 2001 3 21 AT0100094 1 20010215 A 2610 TFC120055101 WARN PANEL DOUG DC9 DC932 3022066 WP COCKPIT MALFUNCTIONED A ZZDA K NONE N FALSE WARNING CR CRUISE 1 SO 15 830AT 47723 FOUND SMOKE DETECTOR LOOP LIGHT ON IN FLIGHT, FORWARD CARGO COMPARTMENT LOOP-B. CREW REPORTED LOWER CARGO COMPARTMENT S MOKE DETECTION SYSTEM DID NOT TEST AFTER B-LOOP LIGHT ILLUMINATED. INSPECTED FORWARD AND AFT CARGO COMPARTMENT, NO DEFE CTES NOTED. CHECKED CONTROL PANEL, ALL NORMAL ON GROUND. ASSIGNED TO MEL. FURTHER TROUBLESHOOTING REQUIRED. REMOVED AND REPLACED FAULT PANEL ASSEMBLY IAW DC9 MM 26-10. 2 L 7 2 4F A6WE 2001032100116 20010321 00116 SO 2001 3 21 C2XA01CL032 1 20010222 A 3260 852701 PROXIMITY SWITCH EMB 145 EMB145ER SO LT MLG MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 15948 145056 CLE FLIGHT 3750 THE CREW REPORTED THE LANDING GEAR DISAGREE MESSAGE DURING RETRACTION. THE AIRCRAFT RETURNED TO CLEVELA ND AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BOTH LEFT MAIN GEAR UPLOCK PROXIMITY SENSORS. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001032100117 20010321 00117 SO 2001 3 21 C2XA01CL033 1 20010223 A 3350 20131A BATTERY PACK EMB 145 EMB145LR SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16981 2601 351 145208 CLE FLIGHT 3901 THE CREW REPORTED THE AFT EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001032100118 20010321 00118 NM 2001 3 21 AT0100065R1 1 20010108 A 5347 SEAT TRACK BOEING 737 7372L9 1384497 NM CABIN CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 FOUND LEFT INBOARD SEAT TRACK CORRODED AT BS 500B-52D. REMOVED AND REPLACED SEAT TRACK IAW B737 SRM 53-10-5 FIGURE 1. 2 L 7 2 4F RT A16WE 2001032100119 20010321 00119 CE 2001 3 21 GLBA2001044 1 20010223 A 3260 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE MLG DIRTY A GLBA K NONE O OTHER AP APPROACH 1 CE 01 96UX UE96 LANDING GEAR C/B POPPED WITH GEAR FULL UP ON APPROACH. INSPECTED LAND GEAR SYSTEM, CLEANED ALL UP-LOCK AND DOWN-LOCK SW ITCHES, OPS CHECKED SYSTEM GOOD. RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 2001032100120 20010321 00120 SO 2001 3 21 SWIA972378 1 20010210 A 3010 BOOT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT WING TORN A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 578SW 120346 ENTIRE LEADING EDGE DEICE SYSTEM FAILED AT CRUISE. UPON INSPECTION FOUND A LARGE TEAR IN THE UPPER PORTION OF THE LEFT OUTBOARD BOOT. DIVERTED FROM RDM TO RDD. COMPLIED WITH REPLACEMENT OF LEFT OUTBOARD DEICE BOOT. OPS CHECK AND FUNCTIO NAL CHECK GOOD OF LEFT OUTBOARD BOOT. (P/N ON: P29S-705135-29) (S/N ON: MM07380). 2 L 7 2 4T 4 T RT A31SO E20NE 2001032100121 20010321 00121 NE 2001 3 21 SWIA972379 2 20010219 A 7261 REGULATOR VALVE EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE LEAKING A SWIA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 269UE 120194 RIGHT ENGINE INFLIGHT SHUTDOWN DUE TO LOW OIL PRESSURE LIGHT ON MAP AND OIL PRESSURE GAUGE BELOW 40 PSI. REMOVED AND RE PLACED RIGHT ENGINE OIL PRESSURE REGULATING VALVE ASSEMBLY IAW P&W MM 72-01-50, PAGE 418. PERFORMED ENGINE RUNS AS REQU IRED. OPS CHECK GOOD. NO LEAKS NOTED. VALVE (P/N ON: 3105732-01) (P/N OFF: 3108007) (HOUSING P/N: 3105735). 2 L 7 2 4T 4 T RT A31SO E20NE 2001032100123 20010321 00123 SO 2001 3 21 SWIA972381 1 20010221 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT WING FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION IN INSP/MAINT 1 NM 07 195SW 120127 ON GROUND RECEIVED FLAP CONTROL FAULT. REMOVED AND REPLACED LEFT OUTBOARD FLAP ACTUATOR REF MM 27-50-09 AND RII 27-307. RAN FLAPS, OPS CHECKS GOOD WITH NO LEAKS NOTED. ALL REMOVED PANELS SECURED. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032100124 20010321 00124 NE 2001 3 21 SWIA972382 2 20010220 A 7200 ENGINE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE MALFUNCTIONED A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 209SW 120269 ON INITIAL POWER APPLICATION LEFT TORQUE ONLY CAME UP TO APPROXIMATELY 25 PERCENT, RIGHT CAME UP NORMALLY. ABORTED TAKE OFF. RAN AIRCRAFT, ADVANCED BOTH ENGINES TO TAKEOFF POWER 6 TIMES. CHECKS NORMAL. VERIFIED EEC MANUAL REVERSION FOR OP ERATION AND ADJUSTMENT. BOTH ENGINES CHECK OK. REMOVED RIGGING DOOR, OPEN LEFT COWL (OUTBOARD), INSPECTED LEFT ENGINE POWER LEVER LINKAGES AND ATTACHMENTS FOR CONDITION AND SECURITY. CHECKS GOOD. RIG DOOR REINSTALLED. COWL SECURED. UN ABLE TO DUPLICATE SQUAWK. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032100125 20010321 00125 EA 2001 3 21 SWIA972383 1 20010221 A 2752 ACTUATOR CNDAIR CL600 CL6002B19 EA LT WING FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 407SW 7034 FLAP FAIL MESSAGE ON APPROACH TO SLC. FLAPS STUCK AT 22 DEGREES. REPLACED LEFT FLAPS NUMBER THREE ACTUATOR IAW 27-53-0 5. OPS CHECK GOOD. (P/N ON 853P100-17) (S/N ON 0964) (S/N OFF 1272). 2 L 7 2 4F RT A21EA 2001032100126 20010321 00126 SO 2001 3 21 SWIA972384 1 20010221 A 2710 CONNECTING ROD EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT AILERON BROKEN A SWIA O OTHER F FLT CONT AFFECTED IN INSP/MAINT 1 NM 07 580SW 120348 AFTER SHUTDOWN, AILERON CONTROL WHEEL WOULD NOT MOVE LEFT OR RIGHT WITHOUT EXCESSIVE FORCE. INSPECTED LEFT AND RIGHT AI LERON CABLE ROUTING. NO DEFECTS NOTED. AILERONS HAVE FREE MOVEMENT. PSP MX REQUEST CHECK LEFT AND RIGHT RVIT (AILERON ) FOR CONDITION. CHECK OF LEFT RVIT, FOUND TO BE OK. CHECK OF RIGHT RVIT FOUND SUPPORT (P/N 120-63140-001) BENT. FOUN D CONNECTING ROD (P/N 120-63143) BROKEN. FOUND BELLCRANK (P/N 123-82549-007) FOR RUDDER INSTALLED. REMOVED AND REPLACE D BELLCRANK. OPS CHECK GOOD. BELLCRANK (P/N: 123-82549-009). 2 L 7 2 4T 4 T RT A31SO E20NE 2001032100127 20010321 00127 SO 2001 3 21 SWIA972385 1 20010219 A 3620 WARNING LIGHT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT ILLUMINATED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 190SW 120050 APU DUCT LEAK ILLUMINATED INFLIGHT WITH APU NOT OPERATING AND BLEEDS CLOSED. RETURNED TO SLC. CHECKED ALL DUCT LEAK SE NSORS FOR APU BLEEDS IAW MM 36-20-00. RAN APU BLEEDS TO CHECK FOR LEAKS, NO LEAKS NOTED. DUCT LEAK SENSORS ALL OPS CH ECK GOOD. NO FAULTS DETECTED. UNABLE TO DUPLICATE SQUAWK. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032100128 20010321 00128 SO 2001 3 21 SWIA972386 1 20010222 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT WING FAULTY A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 195SW 120127 DEPARTURE FROM RNO FLAPS WOULD NOT RETRACT PAST APPROXIMATELY 6 DEGREES FOR OUTBOARD PAIRS, WITH A CORRESPONDING FLAP FA ULT. RESET WOULD NOT CLEAR THE FAULT. LEFT OUTBOARD FLAP ACTUATOR FOUND TO HAVE FLUCUATING OHMS. REPLACED LEFT OUTBOA RD ACTUATOR. FOUND MOISTURE IN CANNON PLUG. REMOVED OLD PLUG, INSTALLED MATRIX CANNON PLUG. LEAK CHECKED AND GROUND O PS CHECK GOOD IAW 27-50-09. (P/N ON 320300-1007) (S/N ON 0210A) (S/N OFF 0736). 2 L 7 2 4T 4 T RT A31SO E20NE 2001032100129 20010321 00129 EA 2001 3 21 SWIA972387 1 20010221 A 2742 ACTUATOR CNDAIR CL600 CL6002B19 EA HORIZ STAB INOPERATIVE A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 411SW 7067 STAB TRIM WILL NOT OPERATE (PILOT OR COPILOTS) USING STAB TRIM CH-2. REMOVED AND REPLACED MOTOR CONTROL UNIT. REMOVED AND REPLACED HORIZONTAL STABILIZER ACTUATOR, REF MM 27-42-61, 27-42-05. OPS CHECK GOOD ON BOTH CHANNELS. MEETS CAT II STANDARDS. CONTROL UNIT (P/N: 7062-3) (S/N ON: 329) (S/N OFF: 215). ACTUATOR (P/N: 8396-3) (S/N ON: 177) (S/N OFF : 281). 2 L 7 2 4F RT A21EA 2001032100133 20010321 00133 EU 2001 3 21 QXEA0100223 1 20010226 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 477AU 11226 PDX - FORWARD EMERGENCY EXIT SIGN HAS INOPERATIVE LAMPS. REMOVED AND REPLACED LAMP CIRCUIT BOARD. OPERATIONAL CHECKS G OOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001032100139 20010321 00139 EU 2001 3 21 AALA20010157 1 20010130 A 5754 STRUCTURE AIRBUS 300 A300B4605R 3930308 EU LT KRUEGER FLAP CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 8067A 510 TUL - FOUND LEFT KRUEGER FLAP HAS CORROSION IN NUMEROUS AREAS INTERNALLY THROUGHOUT VANE. INSTALLED KRUEGER FLAP DOOR. OPS CHECK AND RIGGED OK IAW MM 27-87-11-4. (M) 2 L 7 2 4F RT A35EU 2001032100140 20010321 00140 NM 2001 3 21 AALA20010178 1 20010122 A 3610 212T31091 DUCT BOEING 767 767223 1385123 NM LT WING LEAKING A AALA K NONE J WARNING INDICATION AP APPROACH 1 SW 21 316AA 22318 ORD - FLT 682 - EN ROUTE SFO-ORD, ON FINAL APPROACH DETECTED A LOUD BANG AND LEFT SIDE PACK TURNED OFF. LEFT SIDE DUCT LIGHT ILLUMINATED. LANDED ORD WITHOUT FURTHER INCIDENT. REPLACED PNEUMATIC DUCTS AT WING AREA. ACCOMPLISHED LEAK CHEC KS IAW THE MM. NO LEAKS NOTED. SYTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001032100141 20010321 00141 NM 2001 3 21 AALA20010170 1 20010130 A 2910 LJ38085 DRAIN LINE BOEING 757 757223 1384957 NM HYDRAULIC SYS LEAKING A AALA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 631AA 24589 DEN - FLT 2329 - EN ROUTE DFW-DEN, LOST LEFT SIDE HYDRAULIC PRESSURE. LANDED DEN WITHOUT FURTHER INCIDENT. REPLACED HY DRAULIC DRAIN TUBE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001032100142 20010321 00142 2001 3 21 AALA20010181 4 20010122 A 2565 D31038201 SLIDE BOEING 757 757223 1384957 NM R1 DOOR DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 609AA 27447 SJC - WHILE ON GROUND, R1 DOOR INADVERTENTLY DEPLOYED. SLIDE PARTIALLY DEPLOYED. REPLACED R1 DOOR SLIDE. SYSTEM GROUN D CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001032100145 20010321 00145 2001 3 21 AALA20010156 4 20010129 A 2565 D31038201 SLIDE BOEING 757 757223 1384957 NM L1 DOOR DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 622AA 24580 LGA- WHILE ON GROUND L1 DOOR INADVERTENTLY DEPLOYED. SLIDE PARTIALLY DEPLOYED. REPLACED L1 DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001032100146 20010321 00146 EU 2001 3 21 AALA20010138 1 20010124 A 3350 4002243 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 25071 514 JFK - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT 7D BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEM BLY AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2002081900010 20020819 00010 EU 2002 8 19 AALA20010153 1 20010128 A 4990 38843103 COOLING FAN FOKKER F28 F28MK0100 4990807 EU APU LEAKING A AALA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 1435D 11425 ICT - FLT 487 - AT GATE SHORTLY BEFORE TAKEOFF, FLIGHT ATTENDANT REPORTED HEAVY SMOKE AT COCKPIT. GROUND PERSONNEL REPO RTED FLAMES AT APU AREA. CREW IMMEDIATELY SHUT DOWN APU AND REMOVED ALL POWER FROM AIRCRAFT. REPLACED APU. INVESTIGAT ION DETERMINED OIL COOLING FAN WAS LEAKING OIL WHERE IT MOUNTS TO THE APU. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001032100147 20010321 00147 NM 2001 3 21 AALA20010196 1 20010130 A 5310 DOOR FRAME BOEING 727 727227 1384078 NM GALLEY DOOR CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 727AA 20734 TUL - FOUND LOWER AFT CORNER OF FORWARD GALLEY DOOR HAS TWO SKIN CRACKS DOOR CUTOUT. STRIPED PAINT INSTALLED DOUBLER PE R SERVICE BULLETIN 727-53-0188. (M) 2 L 7 3 4F A3WE 2001032100148 20010321 00148 NM 2001 3 21 AALA20010197 1 20010130 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 727AA 20734 TUL - FOUND CABIN FLOOR BEAM CORRODED BOTTOM FLANGE PLATE HOLES, STATION 1130. REPAIRED PER ESO11697 DATED 1/30/01. (M ) 2 L 7 3 4F A3WE 2001032100149 20010321 00149 NM 2001 3 21 AALA20010198 1 20010201 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 727AA 20734 TUL - FOUND FS 825.95 FLOOR FRAME WEB IS CRACKED THROUGH BOTH SIDES OF LIGHTENING HOLE NEXT TO BL 48 RT SEAT TRACK. STO P DRILLED CRACKS. INSTALLED DOUBLER PER SRM 51-402. (M) 2 L 7 3 4F A3WE 2001032100150 20010321 00150 NM 2001 3 21 AALA20010199 1 20010131 A 5713 STRINGER BOEING 727 727227 1384078 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 727AA 20734 TUL - FOUND LIGHT TO MODERATE CORROSION ON BOTTOM OF STRINGER, ABOVE LEFT PRIMARY HEAT EXCHANGER AFT INBOARD SECTION. I NSTALLED REPAIR PER SRM 57-30-3 FIG 9. (M) 2 L 7 3 4F A3WE 2001032100151 20010321 00151 NM 2001 3 21 AALA20010200 1 20010201 A 5320 STRAP BOEING 727 727227 1384078 NM BULKHEAD CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 727AA 20734 TUL - FOUND THE STRAP ON VERTICAL STIFFENER RBL 26.83 WL 273 AT 1183 BULKHEAD WAS GOUGED UPON REMOVAL OF STRAP FASTENER HOLE AND FOUND CRACKED FROM HOLE. STRAP WAS REMOVED AND NEW STRAP INSTALLED SRM 51-10-1 DOUBLERS ON BOTH SIDE OF VERTIC AL STIFFENER WERE INSTALLED WITH STEEL FASTENERS SRM 51-42-4. (M) 2 L 7 3 4F A3WE 2001032100152 20010321 00152 WP 2001 3 21 AALA20010231 1 20010208 A 3397 WIRE DOUG DC9 DC982 3022082 WP TAIL CONE BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 21 7546A 53028 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT AT TAIL CONE INOPERATIVE. RE-SPLICED OVERHEAD EMERGEN CY EXIT LIGHT WIRE AT TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001032100153 20010321 00153 WP 2001 3 21 AALA20010234 1 20010129 A 3350 HARNESS DOUG DC9 DC982 3022082 WP CABIN INCORRECT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7541A 49995 DEN - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH SEAT LIGHTS DIM. ONE WIRE HARNESS OF DUAL BATTERY POWERE D SYSTEM NOT CONNECTED DUE TO INCORRECT HARNESS LENGTH. SPLICED ADDITIONAL WIRE INTO HARNESS BETWEEN SEATS 19 AND 20. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001032100154 20010321 00154 WP 2001 3 21 AALA20010237 1 20010209 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 218AA 49168 SAT - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT FORWARD SECTION INOPERATIVE. REINSTALLED EMERGENCY EXIT LIG HT CONNECTOR AT FORWARD BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002121600095 20021216 00095 NM 2002 12 16 AALA20010233 1 20010208 A 7797 WIRE BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4 54555 NE VIBRATE MONITOR NOT SEATED A AALA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 612AA 24488 ORD - FLT 259 - EN ROUTE BOS-SJC, DETECTED NR 2 ENGINE VIBRATION. RIGHT SIDE VIBRATION MONITOR RANGE OUT OF LIMITS. DI VERTED ORD, SHUT DOWN NR 2 ENGINE AND LANDED WITHOUT FURTHER INCIDENT. INSPECTED AND FOUND VIBRATION MONITOR WIRING CAU SING INDICATION PROBLEMS. RESEATED WIRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2001032100156 20010321 00156 NM 2001 3 21 AALA20010244 1 20010210 A 2611 SMOKE DETECTOR BOEING 757 757223 1384957 NM AFT LAVATORY ACTIVATED A AALA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 641AA 24599 LAX - FLT 207 - EN ROUTE MIA-LAX - DETECTED SMOKE/FIRE AT AFT LAVATORY. LANDED LAX WITHOUT FURTHER INCIDENT. REPLACED FIRE EXTINGUISHER. PERFORMED OPERATIONS CHECK OF SMOKE DETECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001032100157 20010321 00157 NM 2001 3 21 AALA20010245 1 20010213 A 3250 3800014106 VALVE BOEING 757 757223 1384957 NM NLG DEFECTIVE A AALA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 183AN 29593 CCS - FLT 2155 - EN ROUTE DFW-CCS, SHORTLY AFTER LANDING CAPTAIN REPORTED PROBLEMS WITH NOSE LANDING GEAR STEERING SYSTE M. ARRIVED CCS GATE WITHOUT FURTHER INCIDENT. REPLACED NOSE LANDING WHEEL STEERING VALVE. SYSTEM GROUND CHECKED NORMA L OPERATION. (M) 2 L 7 2 4F RT A2NM 2001032100158 20010321 00158 NM 2001 3 21 AALA20010246 1 20010209 A 2435 35057002 STARTER BOEING 757 757223 1384957 NM NR 1 ENGINE DEFECTIVE A AALA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 612AA 24488 ORD - FLT 453 - EN ROUTE ORD-LAX, SHORTLY BEFORE TAKEOFF PASSENGERS AND GROUND CREW REPORTED SPARKS AT LEFT ENGINE DURIN G START. SHUTOFF ENGINE. REPLACED LEFT ENGINE STARTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001032100159 20010321 00159 NM 2001 3 21 AALA20010236 1 20010205 A 5310 SHEAR TIE BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 860AA 21087 TUL - FOUND SHEAR TIE CORRODED AT STATION 720A BETWEEN STRINGER 28R AND 27R. INSTALLED REPAIR DOUBLER PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 2001032100160 20010321 00160 NM 2001 3 21 AALA20010333 1 20010222 A 2913 PV32402F PUMP BOEING 757 757223 1384957 NM NR 1 ENGINE LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 619AA 24577 ORD - FLT 2353 - EN ROUTE ORD-JAC, SHORTLY AFTER TAKEOFF DETECTED HYDRAULIC QUANTITY QUICKLY DROP TO ZERO. RETURNED ORD AND LANDED WITHOUT FURTHER INCIDENT. REPLACED NR 1 ENGINE HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001032100161 20010321 00161 WP 2001 3 21 AALA20010201 1 20010121 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 TUL - FOUND CORROSION AROUND ANTENNA ATTACHMENT HOLE STATION 402, BELLY. CUT OUT CORROSION AND INSTALLED REPAIR DOUBLER PER SRM 53-04 FIG 12B SHEET 2 AT STATION 402. (M) 2 L 7 2 4F A6WE 2001032200127 20010322 00127 SO 2001 3 22 SWIA972373 1 20010213 A 3250 POTENTIOMETER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NLG INOPERATIVE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 233SW 120307 AIRCRAFT WANTED TO VEER RIGHT DURING TAXI. AFTER ROTATION THE PEDAL STEER INOP LIGHT ILLUMINATED. RETURNED TO SEA. AF TER LANDING THE AIRCRAFT WANTED TO VEER RIGHT WHEN NOSE WHEEL TILLER WAS APPLIED. REPLACED NOSE WHEEL FEEDBACK POT WIDT H A SERVICEABLE UNIT IAW MM 32-50-05. OPS CHECKS GOOD AT THIS TIME. (S/N ON: 191) (S/N OFF: 257) (P/N ON/OFF: 20500 -000-02). 2 L 7 2 4T 4 T RT A31SO E20NE 2001032200128 20010322 00128 SO 2001 3 22 C2XA01IA100 1 20010107 A 5320 12004549001 PAD EMB 120 EMB120ER 3260203 SO FUSELAGE WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12715 120125 MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE EMERGENCY EXIT CUTOUT CHAFE PADS ON THE FUSELAGE WERE FOUND TO BE WORN BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PADS IN ACCORDANCE WITH EMB120 SRM 51-40-02, AND T HE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001032200132 20010322 00132 WP 2001 3 22 0100599909 1 20010216 A 2700 CONTROL CABLE DOUG DC9 DC931 3022065 WP WING RESTRICTED A NWAA O OTHER F FLT CONT AFFECTED DE DESCENT 1 GL 01 959N 47255 DURING DESCENT, THE AILERON TRIM LOCKED UP COMPLETELY. AILERONS WERE FUNCTIONAL BUT FELT HEAVY IN FLIGHT. AIRCRAFT ROL LED TO THE RIGHT WHEN SPEED BRAKES APPLIED. SPOILERS DEPLOYED ASYMMETRICALLY WITH SPEED BRAKE HANDLE OUT OF STOWED POSI TION. FOLLOWED COM PROCEDURES AND LANDED SAFELY AT MSP WITHOUT SPOILERS. MAINTENANCE FOUND LEFT SLAT PANEL DRAIN VALVE CLOGGED AND SUSPECT ICE BUILD-UP RESTRICTING CONTROL CABLE MOVEMENT. REPLACED SLANT PANEL DRAIN VALVES AND DRAINED TRA PPED WATER. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 2001032200135 20010322 00135 2001 3 22 SWIA972388 4 20010219 A 2215 SERVO EMB 120 EMB120RT SO PWA 118 PW118 NE ELEVATOR WORN A SWIA O OTHER F FLT CONT AFFECTED IN INSP/MAINT 1 NM 07 137H 120137 E002 INSPECTION - RIGHT YOKE MAKES GRINDING NOISE WHEN PULLED BACK (ELEVATOR SERVO CLUTCH) CONTROLS DISCONNECTED. FOUN D ELEVATOR SERVO TO BE WORN TO LIMITS. REMOVED AND REPLACED ELEVATOR SERVO IAW MM 22-10-05 PG 6. PERFORMED INSPECTION IAW MM 22-10-05 PAGE 601. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032200136 20010322 00136 WP 2001 3 22 MWEA010176 1 20010223 A 5320 991559616 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 INTERCOSTAL CRACKED AT FS 1040 ABOVE LONGERON 16 RIGHT. STOP DRILLED CRACK, FABRICATED REPAIR DOUBLERS, LOCATED AND INS TALLED. 2 L 7 2 4F A6WE 2001032200139 20010322 00139 NM 2001 3 22 XNA01005 1 20010223 A 8012 LIGHT BOEING 727 727100 1384036 NM COCKPIT ILLUMINATED A TC8A C ABORTED TAKEOFF N FALSE WARNING TX TAXI/GRND HDL 1 GL 23 792A 19195 NR 3 START VALVE OPEN LIGHT CAME ON START OF T/O RUN, MADE LOW SPEED ABORT (80 KTS). ON TAXI BACK - INDICATION WAS DETE RMINED TO BE FALSE. MADE NORMAL DEPARTURE. LIGHT WENT OUT IN CRUISE (310) CAME BACK ON IN DESCENT (2000 FT). TRANSFER RED TO DMI LOG 1125 IAW MEL 80-1-1 CAT C. 2 L 7 3 4F RT A3WE 2001032200140 20010322 00140 SO 2001 3 22 COMA0110036 1 20010223 A 5310 12034416002 SHEAR TIE EMB 120 EMB120RT SO FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 269CA 21978 120263 DURING A 400 FLIGHT CYCLE CHECK, A CRACKED RIVET HEAD WAS DISCOVERED ON THE RIGHT SIDE OF AIRCRAFT FUSELAGE ALONG FRAME 9. UPON FURTHER INVESTIGATION, THE SKIN SUPPORT BRACKET IN WHICH SAID RIVET PASSES THROUGH WAS FOUND TO BE CRACKED. TH E SUPPORT BRACKET WAS REMOVED AND A SERVICEABLE BRACKET WAS INSTALLED. WORK WAS COMPLETED IN ACCORDANCE WITH AERODESIGN REPORT 660-I, IR DATED 2-16-93. 2 L 7 2 4T RT A31SO 2001032200141 20010322 00141 EA 2001 3 22 COMA0160275 1 20010222 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 918CA 7018 THE SECOND CEILING EMERGENCY CEILING LIGHT IS INOPERATIVE. TRANSFERRED CEILING LIGHT TO THE DEFERRED DISCREPANCY LIST. 2 L 7 2 4F RT A21EA 2001032200142 20010322 00142 EA 2001 3 22 COMA0160276 1 20010222 A 3350 747SP100200 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 934CA 7042 THE EMERGENCY FLOOR LIGHTING AFT OF ROW 8 IS INOPERATIVE. REPLACED DEFECTIVE FLOOR LIGHTING STRIP. 2 L 7 2 4F RT A21EA 2001032200144 20010322 00144 2001 3 22 COMA0160282 4 20010221 A 3418 STALL WARNING CNDAIR CL600 CL6002B19 EA COCKPIT ACTIVATED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 946CA 7072 STALL FAIL CAUTION DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001032200145 20010322 00145 EA 2001 3 22 COMA0160277 1 20010222 A 2750 860D10018ABC ECU CNDAIR CL600 CL6002B19 EA EE BAY FAILED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 956CA 2998 7105 DURING APPROACH INTO CVG, RECEIVED FLAP FAIL CAUTION WHEN FLAPS WERE SELECTED TO 3 DEGREES. REPLACED THE FLAP ELECTRONI C CONTROL UNIT. 2 L 7 2 4F RT A21EA 2001032200146 20010322 00146 NM 2001 3 22 DHL2001703001 1 20010220 A 5330 SKIN BOEING 727 72730C 1384009 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 STRINGER 19 RIGHT AT FS 369 TO FS 400 LAP SEAM HAS BULGING SKIN AROUND SEVERAL FASTENERS. CUT OUT DAMAGED AREA, INSTALL ED DOUBLER AND FILLER 12.55 X 7.05 INCH DOUBLER. REWORKED LAP AT STA 360 TO 390 WORK DONE IAW SRM 53-30-3. 2 L 7 3 4F A3WE 2001032200147 20010322 00147 WP 2001 3 22 MWEA010161 1 20010219 A 5350 S2274640 CLIP DOUG DC9 DC932 3022066 WP TAIL CONE BROKEN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 TAIL CONE AFT INTERIOR HANDLE HAS A BROKEN CLIP AND FAILS PULL CHECK (25 - 35 LBS). REMOVED AND REPLACED CLIP. 2 L 7 2 4F A6WE 2001032200148 20010322 00148 WP 2001 3 22 MWEA010177 1 20010222 A 7710 2047011 INDICATOR DOUG DC9 DC981 3022081 WP COCKPIT FAILED A MWEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 31 810ME 48072 DURING TAKEOFF ROLL, RIGHT ENGINE EPR INDICATOR FLAGGED OFF. REJECTED TAKEOFF AT APPROXIMATELY 20 KTS. REMOVED AND REP LACED RIGHT ENGINE EPR INDICATOR. 2 L 7 2 4F A6WE 2001032200150 20010322 00150 NE 2001 3 22 DL72S010262 2 20010215 A 7200 JT8D15AHK ENGINE BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE STALLED A DALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 27 540DA 66999 0 22386 687335 ON TAKEOFF IN ATL NR 1 ENGINE COMPRESSOR STALLED AT APPROXIMATELY 400 - 500 FT AGL- EPR DROPPED TO 1.7 WITH AUTO PACK TR IP. INSPECTED ENGINE PER M/M, RAN ENGINE PER PFHB AND TESTS OK. 2 L 7 3 4F 4 F A3WE E2EA 2001032200151 20010322 00151 NM 2001 3 22 DL72S010263 1 20010214 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 515DA 21431 RT AFT EXTERIOR EMERGENCY OVERWING EXIT LIGHT INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 2001032200152 20010322 00152 NM 2001 3 22 DL72S010264 1 20010215 A 5330 65184203 SKIN BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 525DA 21585 INSPECTIONS OF THE FUSELAGE SKIN AROUND THE L1 DOOR CUTOUT REVEALED A CRACK IN THE UPPER FWD CORNER. THE CRACK WAS ROUT ED OUT OF THE SKIN ASSY. THE FWD AND AFT UPPER CORNERS WERE MODIFIED WITH AN EXTERNAL DOUBLER TO REPAIR THE DAMAGE AND INCORPORATE AND EXISTING SMALL HOLE REPAIR ABOVE THE DOOR CUTOUT. THE REPAIR WAS ACCOMPLISHED PER BAC S/B 727- 53-0186 AND ER/A 380046-14AD. 2 L 7 3 4F A3WE 2001032200153 20010322 00153 NM 2001 3 22 DL72W010267 1 20010214 A 5320 6516350313 BEAM BOEING 727 7272Q8 138407W NM BULKHEAD CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831L 21826 A TYPICAL CRACK WAS FOUND AT THE LOWER END OF THE LBL 8 VERTICAL BEAM ON THE FS 1183 BULKHEAD AT WL 182. THE CRACK WAS REPAIRED WITH AN ANGLE REPAIR PER BAC S/B 727-53-0175 AND ER/A 380021-14. 2 L 7 3 4F A3WE 2001032200154 20010322 00154 NM 2001 3 22 DL72S010268 1 20010214 A 5311 65175061 FRAME BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 525DA 21585 THE FS 1303 FRAME INNER CHORD WAS FOUND WITH A FLANGE CRACK AT AN EXISTING HYDRAULIC CLAMP ATTACH POINT. THE CRACK IS J UST ABOVE THE AFT ENTRY STAIR TORQUE BOX. THE CRACK WAS ROUTED OUT OF THE FLANGE AND REPAIRED WITH AN ALUMINUM REP AIR ANGLE. THE REPAIR WAS ACCOMPLISHED PER ER/A 380047- 14, REV A. 2 L 7 3 4F A3WE 2001032200155 20010322 00155 NM 2001 3 22 DL72E010269 1 20010213 A 5330 6518420404 SKIN BOEING 727 727247 138408F NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 283WA 21485 THE FUSELAGE SKIN AROUND THE L1 DOOR CUTOUT WAS FOUND WITH A CRACK IN THE LOWER HINGE CUTOUT. THE CRACK WAS ROUTED OUT OF THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER INSTALLED PER ER/A 380012-14, REV A. 2 L 7 3 4F A3WE 2001032200156 20010322 00156 NM 2001 3 22 DL72S010270 1 20010214 A 5312 BULKHEAD BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 525DA 21585 THE FS 1183 BULKHEAD WEB WAS FOUND WITH A .5 INCH CRACK AT RBL 8 AND WL 182. THE CRACK WAS ROUTED OUT OF THE WEB AND RE PAIRED WITH A TITANIUM DOUBLER PER ER/A 380049-14. 2 L 7 3 4F A3WE 2001032200157 20010322 00157 NM 2001 3 22 DL72W010271 1 20010213 A 5330 SKIN BOEING 727 727247 138408F NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 THE UPPER AFT CORNER OF THE R5 COCKPIT WINDOW WAS FOUND WITHA .25 INCH LONG CRACK IN THE SKIN. THE CRACK WAS STOP DRILL ED AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 380034-14, REV A. 2 L 7 3 4F A3WE 2001032200158 20010322 00158 NM 2001 3 22 DL73K010272 1 20010213 A 5330 SKIN BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 A CRACK WAS FOUND IN THE SKIN AND UNDERLYING BEARSTRAP AT THE LOWER FWD CORNER OF THE L2 DOOR CUTOUT. THE CRACK WAS RE MOVED WITH A 1.25 INCH DEEP CUTOUT. THE CUTOUT WAS REPAIRED WITH THREE EXTERNAL ALUMINUM DOUBLERS PER ER/A 380029-14. 2 L 7 2 4F A16WE 2001032200159 20010322 00159 NM 2001 3 22 DL72W010273 1 20010213 A 5311 65175061 FRAME BOEING 727 727247 138408F NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 THE INNER CHORD OF THE FS 1303 RT FRAME WAS FOUND WITH A CRACKED FLANGE AT A HYDRAULIC BRACKET ATTACH POINT JUST ABO VE THE AFT VENTRAL STAIRWAY TORQUE BOX. THE CRACKED PORTION OF FLANGE WAS TRIMMED OUT AND REPAIRED WITH AN ALUMINU M REPAIR ANGLE PER ER/A 380030-14, REV A. 2 L 7 3 4F A3WE 2001032200160 20010322 00160 2001 3 22 DL764010275 4 20010216 A 3160 COMPUTER 8221381101 BOEING 767 767432ER NM COCKPIT MALFUNCTIONED A DALA A UNSCHED LANDING O OTHER DE DESCENT 1 SO 27 839MH 29712 BOTH INBOARD NAV DISPLAYS AND BOTH EICAS DISPLAYS BLANKED ON ATL APPROACH. REPLACED DISPLAY COMPUTER. 2 L 7 2 4F RT A1NM 2001032200161 20010322 00161 NM 2001 3 22 DL757010276 1 20010216 A 2530 COFFEEMAKER 811150417 BOEING 757 757232 1384965 NM AFT GALLEY DIRTY A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 684DA 27104 BURNING ODOR COMING FROM R AFT GALLEY COFFEEMAKER. FOUND HEAVY COFFEE DEPOSITS ON HEATING PAN. CLEANED PAN AND ODOR WA S NO LONGER DETECTED DEACTIVATED UNIT AS A PRECAUTIONARY ACTION C/B COLLARDED. UNIT WAS NOT REPLACED, NOT IN STOCK AT T HIS TIME. 2 L 7 2 4F RT A2NM 2001032200162 20010322 00162 NM 2001 3 22 DLM11010277 1 20010216 A 2530 2676 CHILLER DOUG MD11 MD11 3023602 NM G4 GALLEY OVERHEATED A DALA K NONE M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 815DE 48624 MCO MID GALLEY G-4 CHILLER INOP. DUE REPORTS OF ELECTRICAL SMELL INSPECT CHILLER WIRING INSTALLATION FOR SIGNS OF OVERH EATING / CHAFING / ETC. INSPECTED WIRING INSTALLATION, NO TROUBLE FOUND. CHILLER ITSELF HAS A STRONG ELECTRICAL SMELL. SHOP INSPECTION REVEALED BURNED COMPONENTS INSIDE. 2 L 7 3 4F RT A22WE 2001032200163 20010322 00163 NM 2001 3 22 DL72W010278 1 20010216 A 5610 5893543130 WINDOW BOEING 727 727247 138408F NM COCKPIT CRACKED A DALA K NONE O OTHER LD LANDING 1 SO 27 294WA 22112 UPON LANDING, NOTICED R-1 WINDOW CRACKED. REPLACED R-1 WINDOW AND WINDOW HEAT CONTROLLER. 2 L 7 3 4F A3WE 2001032200164 20010322 00164 NE 2001 3 22 DL72S010280 2 20010217 A 7200 JT8D15AHK ENGINE BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR1 ENGINE STALLED A DALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 27 540DA 66999 0 22386 687335 NR 1 ENGINE COMPRESSOR STALLED AT APPROXIMATELY 200 - 300 FT. AFTER TAKEOFF REPLACED PRBC. PERFORMED POWER RUN, CKS OK . 2 L 7 3 4F 4 F A3WE E2EA 2001032200165 20010322 00165 NM 2001 3 22 DLM88010281 1 20010217 A 2530 ODOR DOUG MD88 MD88 3023688 NM CABIN DETECTED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 992DL 53344 DURING DESCENT AT 2500 FT SMELLED STRONG ELECTRICAL BURNING ODOR. CONFIRMED BY F/A IN AFT OF A/C. TURNED OFF GALLEY PW R AS PRECAUTION AND SMELL DISSIPATED. MTC INSPD TAIL COMPRT-BAG BINS-CBN-POWERED ALL GALLEY EQUIP AND INSPD CB PNL BEHI ND CAPT SEAT AND E/E COMPT AND ALL WAS NORMAL, NO ELECTRICAL ODOR DETECTED. RAN ENGS AND APU PNEUS FOR AIR COND OPRN NO ODOR DETECTED. 2 L 7 2 4F RT A6WE 2001032200166 20010322 00166 NM 2001 3 22 DL72S010282 1 20010217 A 3350 BATTERY PACK 900835A BOEING 727 727225A 1384077 NM CABIN DISCHARGED A DALA O OTHER L NO TEST IN INSP/MAINT 1 SO 27 8882Z T3989 21579 ON L/O CHECK, FOUND R-2 OVERHEAD EMERGENCY EXIT DOOR LIGHT INOP. REPLACED R-2 OVERHEAD EMERGENCY EXIT DOOR BATTERY PACK , OPS NOW NORMAL. 2 L 7 3 4F RT A3WE 2001032200167 20010322 00167 NM 2001 3 22 DL72W010283 1 20010218 A 3350 PIN BOEING 727 727247 138408F NM CONNECTOR BACKED OUT A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 293WA 22111 AFT CARGO EMERGENCY LIGHT INOP ON CARGO DOOR. PIN PUSHED BACK IN D5024P. RESEATED PIN, CKS GOOD. 2 L 7 3 4F A3WE 2001032200168 20010322 00168 NM 2001 3 22 DLM88010285 1 20010217 A 3222 PISTON 5920629519 DOUG MD88 MD88 3023688 NM NLG FLAKING A DALA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SO 27 962DL 49981 NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF DESPITE NUMEROUS ATTEMPTS. WHILE SERVICING NOSE STRUT FOUND CHROME FLAKING FR OM STRUT CYL. REPLACED NOSE PISTON PER M/M, SWUNG GEAR AND OPS CKS OK. 2 L 7 2 4F RT A6WE 2001032200169 20010322 00169 NM 2001 3 22 DLM88010286 1 20010217 A 2421 GENERATOR 976J2528 DOUG MD88 MD88 3023688 NM NR 2 ENGINE FAILED A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SO 27 973DL 53241 ON 3 OCCASIONS INDICATION OF RT AC FAILURE. AC CROSSTIE REMAINED ON THROUGHOUT. REPLACED RT CSD AND GEN PER M/M, LK CK S, OPS CKS OK. CROSSTIE FUNCTIONS OP NML. 2 L 7 2 4F RT A6WE 2001032200170 20010322 00170 NM 2001 3 22 DL73K010287 1 20010217 A 2612 WARNING LIGHT BOEING 737 737232 1384475 NM COCKPIT INTERMITTENT A DALA K NONE N FALSE WARNING CR CRUISE 1 SO 27 306DL 23078 CARGO FIRE DET AFT LIGHT ILLUMINATED ERRATICALLY/INTERMITENT. DEFERRED TO MCO AND PLAC PER MEL 26-00-19A. 2 L 7 2 4F RT A16WE 2001032200171 20010322 00171 NM 2001 3 22 DLM88010288 1 20010218 A 2420 GENERATOR 947F9453 DOUG MD88 MD88 3023688 NM RT ENGINE FAILED A DALA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SO 27 973DL RL3014B 53241 AT CRUISE ALT RT GEN FAILED WITH AN AC CROSSTIE LOCKOUT. RT GEN WAS RESTORED AND FLT CONTINUED WITH GENS ISOL. NO FURT HER EVENTS. APU INOP ON PREV MCO/PLAC. CKD CSD SVC, CKS GOOD. FOUND GEN FAULT ON GCU. REPLACED SAME AND RAN ENGS. G ENS AND AC CROSSTIE OPS NML PER PFHB. MCO ON APU GEN CLEARED. 2 L 7 2 4F RT A6WE 2001032200172 20010322 00172 NM 2001 3 22 DLM88010289 1 20010217 A 2550 HARNESS DOUG MD88 MD88 3023688 NM AFT CARGO BAY CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 917DE 49958 AFT CARGO LOADING SYSTEM WILL NOT WORK. FOUND WIRE BUNDLE BURNED 6 INCHES AFT FROM DISCONNECT PLUG P1-9035 OF THE AFT C ARGO LOADING SYSTEM DUE TO CHAFING ON SCREW SHANK ON THE FORWARD SIDE OF THE MOVING WALL. RE-TERMINATED CONNECTOR P1-90 35. 2 L 7 2 4F RT A6WE 2001032200173 20010322 00173 NM 2001 3 22 DLM88010290 1 20010218 A 3340 8906K1268 SWITCH DOUG MD88 MD88 3023688 NM COCKPIT ARCED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 933DL 49720 ON FINAL APP NOTICED SMOKE COMING FROM CAPT EXT LIGHT CONTROL PANEL. FLOOD AND WING LIGHTS ON, NOSE LIGHTS OFF. TURNED OFF ALL LIGHTS AND SMOKE CEASED. LANDED UNEVENTFUL AND TAXIED IN. REMOVED LT WING/NOSE LIGHT SW FOR ACCESS. FOUND LT WING LANDING LIGHT SW ARCED AT CASE. REPLACED SAME. 2 L 7 2 4F RT A6WE 2001032200174 20010322 00174 NM 2001 3 22 DL73K010292 1 20010218 A 2121 6068502 FAN 6068502 BOEING 737 737232 1384475 NM COCKPIT FAULTY A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 314DA 35925 23086 SMOKE AND FUMES IN COCKPIT DURING PREFLIGHT. FOUND CONTROL CABIN AUGMENTATION FAN PUTTING FUMES INTO COCKPIT. FWD TO M CO AND PLACARD. 2 L 7 2 4F RT A16WE 2001032200175 20010322 00175 NM 2001 3 22 DL76L010293 1 20010218 A 3350 BATTERY PACK 61020 BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 176DN 25061 AT DEPARTURE AFT LEFT HAND EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY PACK. 2 L 7 2 4F RT A1NM 2001032200176 20010322 00176 NM 2001 3 22 DL757010294 1 20010219 A 3350 LIGHT 0201720001 BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 610DL 22817 ON INSPECTION FOUND ALL IN SEAT EMERGENCY PATH LIGHTS INOP IN FIRST CLASS. FOUND LIGHT SOCKET AT SEAT 2CD SHORTED. RE PLACED LIGHT SOCKET AND POWER SUPPLY. OPN OF EMERGENCY LIGHT NORMAL PER MM. 2 L 7 2 4F RT A2NM 2001032200177 20010322 00177 NM 2001 3 22 DL72S010295 1 20010219 A 3350 BATTERY S106 BOEING 727 727225A 1384077 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8889Z 21858 AFT EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY, OPS NOW OK. 2 L 7 3 4F RT A3WE 2001032200178 20010322 00178 NM 2001 3 22 DLM88010296 1 20010218 A 2720 ROD 5912801503 DOUG MD88 MD88 3023688 NM RUDDER CORRODED A DALA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 SO 27 977DL 53258 DURING T/S OF AUTOPILOT INOP. FOUND RUDDER INPUT CRANK LOOSE, .065 UP AND DOWN MOTION AND CORROSION COMING OUT ENDS OF CRANK. REPLACING RUDDER CRANK, RUDDER INPUT TORQUE TUBE, RUDDER INPUT SECTOR BELLCRANK, RUDDER TRIM ACTUATOR, YAW DAMP ACTUATOR, RUDDER POWERPACK. 2 L 7 2 4F RT A6WE 2001032200179 20010322 00179 NM 2001 3 22 DL733010297 1 20010120 A 5311 FRAME BOEING 737 737347 1384647 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 307WA 23440 WHILE ACCOMPLISHING INSPECTIONS PER S/B 737-53A1173 A .25 INCH CRACK WAS FOUND IN THE RADIUS OF THE RT SIDE CHORD JUST A BOVE WL 207. THE PART WAS REPAIRED PER S/B AT CV. 2 L 7 2 4F RT A16WE 2001032200180 20010322 00180 WP 2001 3 22 DLL14010298 1 20010220 A 2550 HARNESS LKHEED 1011 1011385115 5265015 WP MID CARGO BAY CHAFED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 1739D 193C1237 DURING LOADING OF C2 BIN, SPARKS WERE SEEN COMING FROM UNDER LEFT SIDE BALLMAT IN DOORWAY OF BIN, WHEN CIRCUIT BREAKER TRIPPED, SPARKING STOPPED. DISCONNECTED ELECTRICAL POWER CONNECTIONS TO LOADING PANEL CONTAINING CIRCUIT BREAKERS R ENDERING LOADING SYSTEM INOP AND DISPATCHED A/C PER MEL 25-52-00. 2 L 7 3 4F A23WE 2001032200181 20010322 00181 NM 2001 3 22 DL72L010299 1 20010217 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 511DA 21313 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 480 & 680 INDICATED CRACKS. INTERNAL MFEC INSPECTIONS C ONFIRMED 7 CRACKS ALONG THE LOWER FASTENER ROW OF THE LOWER SKIN. THE SKIN LAP WAS CUTOUT TO REMOVE ALL HOLES. THE JOI NT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 380057-14AD. 2 L 7 3 4F A3WE 2001032200182 20010322 00182 NM 2001 3 22 DL72L010300 1 20010219 A 5330 655456716 SKIN BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 511DA 21313 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 & 740 INDICATED CRACKS. INTERNAL MFEC INSPECTION C ONFIRMED SEVERAL CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. THE ENTIRE SKIN LAP WAS CUTOUT TO REMOVE ALL CRA CKED HOLES. THE JOINT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 380056-14AD. 2 L 7 3 4F A3WE 2001032200183 20010322 00183 NM 2001 3 22 DL72E010301 1 20010220 A 5754 ATTACH ANGLE BOEING 727 727247 138408F NM SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA BN165 21482 A .5 INCH VISIBLE CRACK AT I/B STOP ATTACH ANGLE ON NR 7 L/E SLAT. REPAIRED PER MM 57-54-000-8. 2 L 7 3 4F A3WE 2001032200184 20010322 00184 NM 2001 3 22 DL72W010302 1 20010220 A 3350 1000677 BATTERY BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 296WA 22533 L1 DOOR OVERHEAD EMERGENCY LIGHT BATTERY DEAD. REPLACED LIGHT ASSY. 2 L 7 3 4F A3WE 2001032200185 20010322 00185 NM 2001 3 22 DL73K010303 1 20010221 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 313DL 23085 THE FUSELAGE SKIN WAS FOUND WITH A 3 INCH CRACK AT FS 520 NEAR STRINGER 16L. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B737 SRM 53-30-3 AND ER/A 380104-14. 2 L 7 2 4F RT A16WE 2001032200186 20010322 00186 NM 2001 3 22 DLM11010304 1 20010220 A 5210 HANDLE DOUG MD11 MD11 3023602 NM ENTRY DOOR MISLOCATED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 801DE 48472 L1 DOOR OPEN HANDLE FOUND TO HAVE INSUFFICIENT CLEARANCE TO CREW REST MODULE. MODIFIED MODULE PER ERA. 2 L 7 3 4F RT A22WE 2001032200187 20010322 00187 NM 2001 3 22 DLM11010305 1 20010221 A 5210 HANDLE DOUG MD11 MD11 3023602 NM L-1 DOOR MISLOCATED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 805DE 48476 L1 DOOR OPEN HANDLE FOUND TO HAVE INSUFFICIENT CLEARANCE TO CREW REST MODULE. MODIFIED MODULE PER ERA 388450/14. 2 L 7 3 4F RT A22WE 2001032200188 20010322 00188 NM 2001 3 22 DL76K010306 1 20010221 A 2750 FSEU 285T0049053 BOEING 767 767332 1382001 NM EE BAY FAILED A DALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 SO 27 175DZ D00710 29696 T/E FLAP DISAGREE AND L/E SLAT DISAGREE, T/E INDICATED 20. EMERGENCY DECLARED BY CREW. REPLACED FLAP/SLAT ELECTRONICS UNIT. 2 L 7 2 4F RT A1NM 2001032200189 20010322 00189 NM 2001 3 22 DLM11010307 1 20010221 A 5210 HANDLE DOUG MD11 MD11 3023602 NM L-1 DOOR MISLOCATED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 807DE 48478 L1 DOOR OPEN CONTROL HANDLE FOUND WITH INSUFFUCIENT CLEARANCE TO CREW REST MODULE. MODIFIED STRUCTURE PER ERA 388450-14 . 2 L 7 3 4F RT A22WE 2001032200190 20010322 00190 NM 2001 3 22 DL72W010308 1 20010130 A 5753 RIB BOEING 727 727247 138408F NM FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W BN15 21057 DURING SHOP VISIT THE I/B AFT CLOSEOUT RIB WAS FOUND CRACKED. THE RIB WAS REPAIRED PER 727 MM 57-52-0, FIG 808 BY REMOV ING THE DAMAGE AND INSTALLING A FILLER AND DOUBLER. 2 L 7 3 4F A3WE 2001032200191 20010322 00191 NM 2001 3 22 DL72L010309 1 20010221 A 5310 WEB BOEING 727 727232 1384082 NM TORQUE BOX CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 A 1 INCH CRACK IN LT TORQUE BOX VERT WEB AT UPPER RIVET ROW STA 1210 AND TWO CRACKS IN LT TORQUE BOX VERT WEB AT UPPER RIVET ROW STA 1235. REPAIR PER M/M 53-11-000-8. 2 L 7 3 4F A3WE 2001032200192 20010322 00192 NM 2001 3 22 DLM88010310 1 20010221 A 5270 UPLOCK SWITCH DOUG MD88 MD88 3023688 NM AFT AIRSTAIR DR FAILED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 918DL 49583 AIR TURNBACK, AFT AIRSTAIR DOOR ILLUMINATED DURING CLIMBOUT. VERIFIED DOOR CLOSED AND FWD TO MCO. REPLACED UPLOCK SWIT CHES S1-276 AND S1-277, LIGHT CHKS GOOD. 2 L 7 2 4F RT A6WE 2001032200193 20010322 00193 NM 2001 3 22 DL73K010311 1 20010221 A 3260 LIGHT 3186301001 BOEING 737 737232 1384475 NM COCKPIT INTERMITTENT A DALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 27 314DA 23086 ON LANDING GEAR EXTENSION, RT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE. BULB CK WAS GOOD. CYCLED GEAR WITH SAM E INDICATION. PUSHED LIGHT ASSY SEVERAL TIMES. THEN RT GEAR LIGHT CAME ON. ALL INDICATIONS GOOD. CONFIRMED GEAR DOW N WITH CONFIG HORN AND TOWER FLY BY. CKED RT GEAR DOWNLOCK SENSOR AND TARGET. CKS OK. FOUND RT GEAR GREEN LIGHT ASSY B AD. REPLACED LIGHT ASSY. ALL IND NOW NORMAL. OK FOR SVC. 2 L 7 2 4F RT A16WE 2001032200194 20010322 00194 NM 2001 3 22 DL72W010313 1 20010222 A 5310 651635024 DOOR FRAME BOEING 727 727247 138408F NM FUSELAGE MISDRILLED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 2819W 21057 THE RT AFT ENTRY DOOR FRAME SPLICE INSTALLED PER S/B 727-53-0210 WAS FOUND TO HAVE SHORT EDGE DISTANCE. THE AREA WAS MODIFIED PER S/B AT HMV. 2 L 7 3 4F A3WE 2001032200195 20010322 00195 NE 2001 3 22 DL78K010314 2 20010221 A 7200 CFM567 ENGINE BOEING 737 737832 13844CF NM CFMINT CFM567 CFM567B2US 13802 NE NR 1 ENGINE FAILED A DALA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION TO TAKEOFF 1 SO 27 398DA 768 768 30774 876561 ON INITIAL ENGINE SPOOL UP LEFT ENGINE MADE A LOUD BANG, A/C PULLED TO LEFT AND ENGINE FAIL WAS INDICATED. N1 WAS AT AB OUT 50 PERCENT AND ROLL WAS NOT STARTED YET. REPLACED ENGINE FOR INTERNAL FAILURE. 2 L 7 2 4F 4 F RT A16WE E2GL 2001032200196 20010322 00196 WP 2001 3 22 TWAA0103501 1 20010222 A 2170 17946081 SEPARATOR DOUG DC9 DC983 3022083 WP AC BAY CONTAMINATED A TWAA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 CE 05 9302B 49528 CABIN ATTENDANTS REPORTED SMOKE IN CABIN ON LANDING. BOTH PACKS AND ENGINE AND AIRFOIL ANTI-ICE ON. PERFORMED PACK BUR N OUT, RESET PINS ON LT HOT AIR VALVE, AND REPLACED THE WATER SEPARATORS. CHECK-C 10-16-00 STL. 2 L 7 2 4F RT A6WE 2001032200198 20010322 00198 SO 2001 3 22 C2XA01IA126 1 20010223 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 16987 145261 IAH - FLIGHT 4175, THE CREW REPORTED THAT WITH DEICING SYSTEM ON THERE WAS A STRONG ODOR LIKE BURNING PAPER IN THE COCKP IT AND CABIN THAT SUBSIDED DURING FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE PERFORMED OPERA TIONAL TESTS OF THE ANTI-ICING SYSTEM WITH NO DEFECTS NOTED. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001032200199 20010322 00199 CE 2001 3 22 20010227CW001 1 20010123 A 3230 504501019 TORQUE TUBE CESSNA 401 401 207590C CE CONT O520 TSIO520C 17040 SO LT WHEELWELL MLG CRACKED E MHJA K NONE O OTHER NR NOT REPORTED 1 SW 05 3208Q 9586 4010008 TORQUE TUBE CRACKED AT FORK BOLT TUBE BOSS. THIS IS 2ND 5/8 BOSS WE HAVE HAD FAIL AND RECOMMEND INSPECTION IMMEDIATELY ON UNITS OVER 5000 HOURS. THE 1/2 BOSS TORQUE TUBES DONT SEEM AS VUNERABLE. WE HAVE HAD 4 XRAYED THAT SHOW UNDERCUTTIN G AT WELDS AROUND BOSS. 1 L 7 2 3O 3 O A7CE E8CE 2001032200204 20010322 00204 EU 2001 3 22 A6WA200100016 1 20010222 A 2150 A/C PACK BAG BAE146 BAE146300A 1500267 EU AC BAY FAILED A A6WA O OTHER J WARNING INDICATION CR CRUISE 1 GL 31 612AW E3122 AT 20,000 FEET NR 1 PACK VALVE LIGHT CAME ON, FLIGHT CREW TRIED TO RESET COULD NOT. THE RECIRCULATION VALVE WENT FREST COULD NOT RESET. NR 2 PACK VALVE LIGHT CAME ON, LOST PRESSURE. RESTORED CABIN PRESSURE AT 10,000 FEET PACK WORKED. MA INTENANCE PRESSURIZED A/C TO MAX DIFF, ON APU AIR AND ENGINE AIR LEAK CHECKED AT PACKS AT MAX DIFF GOOD, NO LEAKS NOTED. BOTH PACKS OPERATE NORMAL ON GROUND CHECKS, TEST FLIGHT SATISFACTORY. 2 H 7 4 4F RT A49EU 2001032200206 20010322 00206 SO 2001 3 22 C2XA01IA128 1 20010225 A 2120 SMOKE EMB 145 EMB145LR SO CABIN DETECTED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 13964 145123 CAE - FLIGHT 4205, THE CREW REPORTED SMOKE IN THE CABIN, THE AIRCRAFT DIVERTED TO CAE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND OPERATIONALLY CHECKED THE AIR CONDITIONING SYSTEM WITH NO DEFECTS NOTED. THE A IRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001032200207 20010322 00207 SO 2001 3 22 C2XA01IA131 1 20010225 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 13964 145123 IAH - FLIGHT 4205, THE CREW REPORTED A STRONG ODOR IN THE COCKPIT AND CABIN. MAINTENANCE PERFORMED OPERATIONAL CHECKS O N THE AIR CONDITIONING SYSTEM WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001032200208 20010322 00208 GL 2001 3 22 C2XA01IA130 2 20010222 A 7200 COMPRESSOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL ENGINE CONTAMINATED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 22971 145149 IAH - FLIGHT 375, THE CREW REPORTED A STRONG ODOR COMING FROM THE NR 1 PACK WHEN SUPPLIED BY ENGINE BLEED AIR. MAINTENA NCE INSPECTED THE AIRCRAFT AND DETERMINED THAT THE ODOR WAS CAUSED BY RESIDUAL FLUID FROM THE PREVIOUS NIGHT COMPRESSOR WASH, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2001032200211 20010322 00211 SO 2001 3 22 C2XA01IA134 1 20010228 A 2121 EVAC2322C2AMDT4 COOLING FAN EMB 120 EMB120ER 3260203 SO FUSELAGE INOPERATIVE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 22727 120177 IAH - FLIGHT 2964, THE CREW REPORTED SMOKE IN THE AIRCRAFT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LEFT HAND GROUND COOLING FAN TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FAN IN ACCORDANCE WITH EMB-120 M/M 21-51-03, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001032200212 20010322 00212 SO 2001 3 22 20010301CW007 1 20010123 A 2410 635796 COUPLER CONT PIPER PA34 PA34200T 7103406 SO CONT O360 TSIO360EB 17025 SO LEFT ENGINE FAILED E HEBA O OTHER O OTHER CR CRUISE 1 SW 03 304CW 307572 347870153 307572H LT ALTERNATOR FAILED IN FLIGHT AT NIGHT. ALTERNATOR FAILURE CAUSE: DRIVE COUPLER FAILURE. 1 L 7 2 3O 3 O A7SO E9CE 2001032200213 20010322 00213 2001 3 22 VNAA0102019 4 20010207 A 3140 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT ACTIVATED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 434JS 3051 AS THE AIRCRAFT WAS TAXIING ON TO THE RUNWAY RECEIVED A PACK FAIL CAS MESSAGE. THE CREW ADVISED TOWER OF NEED TO EXIT T HE RUNWAY. THE CREW WENT THRU THE QRH AND THE CAS MESSAGE CLEARED. RE-ENTERED THE RUNWAY AND DEPARTED WITHOUT FURTHER INCIDENT. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001032200214 20010322 00214 NM 2001 3 22 VNAA0103001 1 20010303 A 5242 DOOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE EE BAY NOT SEATED A VNAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 434JS 3051 DURING CLIMBOUT THE AIRCRAFT WOULD NOT PRESSURIZE. THE FLIGHT CREW RETURNED TO THE FIELD. MAINTENANCE INSPECTED AND RE SEATED THE AVIONICS BAY MAINTENANCE HATCH IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 06-04-02. GROUND PRESSURIZATION CHECKS WERE COMPLETED AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001032200217 20010322 00217 NM 2001 3 22 AALA20010150 1 20010128 A 5414 PANEL BOEING 757 757223 1384957 NM NACELLE SEPARATED A AALA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SW 21 660AM 25294 BOS - FLT 1183 - EN ROUTE BOS-STT SHORTLY BEFORE TAKEOFF DETECTED NR 2 ENGINE SHUTDOWN DUE TO INGESTION FROM ACOUSTICAL PANEL AT NACELLE. RETURNED BOS GATE WITHOUT FURTHER INCIDENT. REPLCED NR 2 ENGINE DUE TO FOD FROM DETACHED PANEL. SYS TEM IS CURRENTLY UNDER INVESTIGATION. (M) 2 L 7 2 4F RT A2NM 2001032200218 20010322 00218 CE 2001 3 22 20010319CW001 1 20010208 A 3240 5300116 BRAKE CESSNA 340 340A 2076405 CE CONT O520 TSIO520* 17040 SO RT BRAKE LINE LEAKING B R2JR K NONE K FLUID LOSS IN INSP/MAINT 1 EA 21 55RB 3792 340A0015 WHILE INVESTIGATING HYDRAULIC LEAK EVIDENCE ON BELLY OF AIRCRAFT, FOUND RIGHT PILOTS BREAK LINE UNDER THE FLOOR, WET. P RESSURE TEST OF LINE SHOWED PIN HOLE DUE TO CORROSION. ROUTING OF LINE PUTS IT AGAINST HEAT DUCT HOSE, WHICH APPREARS T O REACT WITH THE 5052-0 LINE CAUSING CORROSION. NEW LINE INSTALLED AND WRAPPED WITH ANTI-CHAFFE MATERIAL. SUGGEST INSP ECTION OF THIS AREA CLOSELY NEXT INSPECTION. LINE PROVIDES PARAK PRESSURE TO RIGHT BRAKE AND COULD CAUSE FAILURE OF ONE BRAKE TO WORK PROPERLY. 1 L 7 2 3O 3 O 3A25 E8CE 2001032200219 20010322 00219 CE 2001 3 22 20010319CW002 1 20010208 A 2820 530010841 FUEL LINE CESSNA 340 340A 2076405 CE CONT O360 TSIO360* 17025 SO CROSSFEED LEAKING B R2JR K NONE K FLUID LOSS IN INSP/MAINT 1 EA 21 55RB 3792 340A0015 WHILE INVESTIGATING FUEL SMELL INSIDE AIRCRAFT, FOUND FUEL CROSSFEED LINE BELOW FLOOR LEAKING. LINE ATTACHES DIRECTLY T O MAIN FUEL TANK AND RUNS UNDER FLOOR TO OTHER FUEL SOV. LINE FAILED DUE TO CORROSION DUE TO WATER NOT BEING SUMPED FRO M FUEL DRAIN POINTS. A LEAKY LINE INSIDE AIRCRAFT IS A FLIGHT HAZARD. FUEL FROM THE MAIN TANK CAN KEEP DRAINING UNTIL MAIN TANK EMPTYS. THERE IS NO WAY TO SHUT IT OFF. LINES REPLACED WITH NEW. MORE SUMPING ADVISED. 1 L 7 2 3O 3 O 3A25 E9CE 2001032200220 20010322 00220 SO 2001 3 22 20010319CW004 1 20010202 A 2450 293712 PANEL PIPER PA31T PA31T 7103124 SO PWA PT6 PT6* 52043 EA LT MAIN BRKR PAN DAMAGED E PAZA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 03 88QM 3675 31T8104025 SHORTLY AFTER TAKEOFF, PILOT SAW SMOKE COMING FROM LEFT MAIN CIRCUIT BREAKER PANEL AND RETURNED TO AIRPORT. UPON REMOVI NG LEFT MAIN BREAKER PANEL, FOUND SEVERE HEAT DAMAGE ON ATTACH CLIP FOR RIGHT WINDSHIELD HEAT CIRCUIT BREAKER. THESE AR E PLUG IN STYLE BREAKERS. THE SMALL BRASS RIVET THAT ATTACHES CLIP TO BREAKER PANEL WAS NOT MAKING SUFFICIENT CONTACT T O HANDLE MAKING SUFFICIENT CONTACT TO HANDLE 35 AMP LOAD OF SYSTEM. RECOMMEND INSPECTING LIKE AIRCRAFT BREAKER PANELS F OR HEAT DAMAGE. 1 L 7 2 3T 3 T A8EA E2NE 2001032200233 20010322 00233 NM 2001 3 22 ASAA0140022 1 20010209 A 3397 WIRE BOEING 737 7374Q8 NM CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 NM 01 785AS 27628 SEA - WHILE PERFORMING A LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 1 INOPERATIVE, WIRE BROKEN. REMOVED AND REPLACED EMERGENCY FLOOR ASSEMBLY. OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A16WE 2001032200234 20010322 00234 NM 2001 3 22 ASAA0140020 1 20010203 A 3350 CONNECTOR BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 765AS 25102 PDX - BEFORE FLIGHT FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 14/15, DISCONNECTED. RECONNECTED FLOOR TRACK LIGHTS. OPERATIONAL CHECKS GOOD. (M) 2 L 7 2 4F RT A16WE 2001032200235 20010322 00235 NM 2001 3 22 ASAA0140019 1 20010203 A 3350 CONNECTOR BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 774AS 25107 TUS - BEFORE FLIGHT, FOUND EMERGENCY FLOOR ESCAPE EXIT MARKERS INOPERATIVE. FOUND LOOSE CONNECTION, RESECURED CONNECTIO N. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001032200236 20010322 00236 NM 2001 3 22 ASAA0140018 1 20010202 A 3350 8100022605 LIGHT BOEING 737 737490 1384715 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 796AS 28891 ONT - BEFORE FLIGHT FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROWS 14 INOPERATIVE. REPLACED EMERGENCY FLOOR TRACK LIGHTS AT ROW 14. OPERATIONAL CHECKS NORMAL. (M) 2 L 7 2 4F RT A16WE 2001032200237 20010322 00237 SO 2001 3 22 SIMA0324 1 20010201 A 2613 132FU SENSOR EMB 145 EMB145LR SO LT MLG FAILED A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 638AE 145172 SAV - FLT 3478 - LEFT INBOARD BRAKE INDICATOR IS ON MEL AND THE CREW GOT A LEFT INBOARD BRAKE TEMP WARNING ON TAKEOFF. CREW ABORTED AND RETURNED TO GATE. REMOVED AND REPLACED NR 4 BRAKE TEMP SENSOR IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT T00011AT 2001032200238 20010322 00238 NM 2001 3 22 AALA20010325 1 20010225 A 2121 13116011 FAN BOEING 727 727223 1384074 NM FUSELAGE FAULTY A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 869AA 21374 IAH - FLT 1791 - EN ROUTE IAH-MIA - DETECTED LIGHT SMOKE AT FLOOR VENT NEAR ROW 27 DEF. LANDED MIA WITHOUT FURTHER INCI DENT. REPLACED GROUND VENTURI FAN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001032200239 20010322 00239 NM 2001 3 22 AALA20010274 1 20010206 A 5730 SKIN BOEING 727 727223 1384074 NM WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 879AA 21391 TUL - FOUND CORROSION ON LOWER WING SKIN IN PLENUM AREA STATION 826 RBL 30. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-30-3 PAGE 19. (M) 2 L 7 3 4F A3WE 2001032200240 20010322 00240 NM 2001 3 22 AALA20010327 1 20010220 A 5320 STRAP BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 843AA 20984 TUL - FOUND HEAVY FRAME SPLICE STRAP ON UNDERSIDE OF FRAME CORRODED AT TWO NUT PLATE ATTACH POINTS STATION 616, LOWER AF T CORNER OF DOOR OPENING. REPLAED TAPERED STRAP AS PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 2001032200241 20010322 00241 NM 2001 3 22 AALA20010326 1 20010220 A 5310 SHEAR TIE BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 843AA 20984 TUL - FOUND CORROSION BETWEEN BELL FRAME AND SHEART TIE STATION 720A STRINGER 28L-27R. CUT OFF SHEAR TIE FLANGE INSTALL ED SHEAR TIE FLANGE PER SRM 53-10-04. (M) 2 L 7 3 4F A3WE 2001032200242 20010322 00242 NM 2001 3 22 AALA20010183 1 20010201 A 3350 0201806021 LIGHT BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 601AN 27052 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT 15D . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001032200243 20010322 00243 NM 2001 3 22 AALA20010184 1 20010203 A 3350 SOCKET BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 366AA 25193 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 2H THROUGH 8H INOPERATIVE. REPLACED EMERGENCY EXIT LIG HT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001032200244 20010322 00244 EU 2001 3 22 AALA20010185 1 20010204 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU CABIN DAMAGED A K NONE L NO TEST IN INSP/MAINT 1 SW 21 7076A 610 JFK - DURING OVERNIGHT MAINTENANCE, LEFT SIDE EMERGENCY EXIT LIGHT AT FIRST CLASS CLOSET INOPERATIVE. REPAIRED EMERGENC Y EXIT FLOOR PATH LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2001032200245 20010322 00245 WP 2001 3 22 AALA20010186 1 20010204 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 441AA 49460 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 9D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001032200246 20010322 00246 WP 2001 3 22 AALA20010255 1 20010131 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 411AA 49322 TUL - FOUND TWO DEEP GOUGES ON BELLFRAME AT STATION 370 BETWEEN LONGERON 16R AND 17R. BLENDED OUT GOUGES TO 20 PERCENT TO 50 PERCENT THICKNESS REMOVAL AND INSTALLED DOUBLER PER AARD 53-10-00-14. (M) 2 L 7 2 4F A6WE 2001032200247 20010322 00247 WP 2001 3 22 AALA20010256 1 20010131 A 5610 WINDOW FRAME DOUG DC9 DC982 3022082 WP COCKPIT CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 411AA 49322 TUL - FOUND CRACK IN F/O AFT WINDOW RETAINER BETWEEN SKIN AND WINDOW POST, UPPER FORWARD CORNER OF WINDOW. REMOVED DAMA GE AND INSTALLED DOUBLER PER ESO 80559, DATED 1/30/2001. (M) 2 L 7 2 4F A6WE 2001032200248 20010322 00248 WP 2001 3 22 AALA20010257 1 20010206 A 5310 BEAM DOUG DC9 DC982 3022082 WP AFT CARGO BAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 411AA 49322 TUL - FOUND STATION 1155-1212 CARGO DOOR CUTOUT LOWER CHORD SUPPORT ANGLE CORRODED MULTIPLE AREA. REMOVED AND REPLACED LOWER DOOR CUTOUT BEAM STATION 1117-1250 PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2001032200249 20010322 00249 WP 2001 3 22 AALA20010258 1 20010205 A 5320 FITTING DOUG DC9 DC982 3022082 WP AFT CARGO BAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 411AA 49322 TUL - FOUND STATION 1210 TO STATION 1212 DOOR CUTOUT FRAME CORNER FITTING CORRODED, OUTBOARD LONGERON 28R. INSTALLED NE W FITTING PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2001032200250 20010322 00250 WP 2001 3 22 AALA20010259 1 20010205 A 5310 WEB DOUG DC9 DC982 3022082 WP AFT CARGO BAY DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 411AA 49322 TUL - FOUND STATION 1215-1216, WEB DOOR FRAME BELOW NUTPLATE HAS HOLE, STATION 1216. INSTALLED NEW WEB SPLICE PER AARD 53-10-00-24 AND SRM 53-01. (M) 2 L 7 2 4F A6WE 2002040500053 20020405 00053 NM 2002 4 5 AALA20010260 1 20011203 A 5753 STRUCTURE BOEING 767 767323 1385205 NM TE FLAPS CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 39367 25194 AFW - FOUND RIGHT INBOARD FLAP SUPPORT BEAM (9-10 BEAM ASSY) HAD THE MOST OUTBOARD FLAP ATTACH HOLE REAMED TO .503 TO RE MOVE CORROSION. OVERSIZE HOLE TO REMOVE CORROSION AND VISUALLY INSPECT THE BORE TO ENSURE COMPLETE CORROSION REMOVAL. FABRICATED AND REPAIR BUSHING TRIM AL-N1-BR WITH DIMENSION TO ACHIEVE A .001 INCH INTERFERENCE FIT. ALODINE THE REWORKE D HOLE. INSTALLED BUSHING WET WITH BMS5-95 SEALANT. REAM THE BUSHING BORE TO THE ORIGINAL HOLE DIAMETER. VISUALLY INS PECT THE BUSHING BORE FOR DAMAGE. FABRICATE A REPAIR WASHER FROM .125 INCH THICK CRES WITH AN OUTER DIA OF .75 INCH. R EFINISH REPAIR WASHER PER AARD 51-20-01-1. INSTALL REPAIR WASHER AGAINST THE SUPPORT BEAM IN PLACE OF THE ORIGINAL WASH 2 L 7 2 4F RT A1NM 2001032200251 20010322 00251 WP 2001 3 22 AALA20010155 1 20010127 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 133AA 47828 TUL - FOUND CORROSION BEYOND LIMITS, BS 1902 LONGERON 48 LEFT. REPAIR PER SRM 53-20-00. INSTALLED DOUBLER AND STRINGER TIES. (M) 2 L 7 3 4F A22WE 2001032200252 20010322 00252 WP 2001 3 22 AALA20010144 1 20010123 A 5330 SKIN DOUG DC10 DC1010 3022110 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 133AA 47828 TUL - FOUND LEFT FUSELAGE FROM STATION 1099 TO 1129 BETWEEN LONGERON 43L AND 45L HAS CLASS AND C REPAIR. INSTALLED A PE RMANENT REPAIR FROM STATION 1099 TO 1129 BETWEEN LONGER 43L AND 45L PER SRM 53-20-00 VOL I AND ESO 7349 DATED 08-18-98. (M) 2 L 7 3 4F A22WE 2001032200253 20010322 00253 WP 2001 3 22 AALA20010145 1 20010123 A 5315 FLOORBEAM DOUG DC10 DC1010 3022110 WP MID CARGO BAY CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 133AA 47828 TUL - FOUND FLOORBEAM IN CENTER CARGO AT STATION 1701 CRACKED ABOVE LONGERON 45R. REPLACED 40 INCHES OF FLOORBEAM AT ST ATION 1701 ON RIGHT SIDE PER SRM 53-60-01 VOL I. (M) 2 L 7 3 4F A22WE 2001032200254 20010322 00254 WP 2001 3 22 AALA20010116 1 20010116 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 133AA 47828 TUL - FOUND LONGERON 52 CORRODED FROM STATION 815 TO 825. SPLICED IN NEW SECTION OF LONGERON 52 PER AARD 51-01-00-05. (M) 2 L 7 3 4F A22WE 2001032200255 20010322 00255 WP 2001 3 22 AALA20010128 1 20010123 A 5330 SKIN DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 133AA 47828 TUL - FOUND SKIN CORRODED UNDER TEAR STRAP. INSTALLED DOUBLER PER SRM 53-20-00. (M) 2 L 7 3 4F A22WE 2001032200256 20010322 00256 WP 2001 3 22 AALA20010129 1 20010123 A 5330 SKIN DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 133AA 47828 TUL - FOUND STRINGER 41L HAS TWO FASTENERS MISSING, SKIN HAS CORROSION UNDER TEAR STRAP, STATION 1950. REPAIRED PER SRM 53-20-00. (M) 2 L 7 3 4F A22WE 2001032200257 20010322 00257 WP 2001 3 22 AALA20010193 1 20010205 A 3231 39567851 LINK DOUG DC9 DC983 3022083 WP NLG DEFECTIVE A AALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SW 21 562AA 49344 LAX - FLT 1232 - EN ROUTE LAX-ORD, DETECTED LOUD VIBRATION AT NOSE LANDING GEAR. RETURNED LAX AND LANDED WITHOUT FURTHE R INCIDENT. REPLACED NOSE LANDING GEAR DOOR LINK ASSEMBLY. ACCOMPLISHED LANDING GEAR SWING RETRACTION TEST. SYSTEM GR OUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001032200258 20010322 00258 NM 2001 3 22 ASAA0140016 1 20010128 A 3350 20131 POWER SUPPLY BOEING 737 7374Q8 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 775AS 25108 SEA - DURING LINE CHECK, FOUND OVERHEAD BIN EMERGENCY LIGHT AT ROW 16 RIGHT INOPERATIVE. REMOVED AND REPLACED POWER SUP PLY, OPERATIONAL CHECKS NORMAL. (M) 2 L 7 2 4F RT A16WE 2001032200259 20010322 00259 NM 2001 3 22 ASAA0140015 1 20010127 A 3350 LIGHT BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 778AS 25110 PDX - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE IN AFT CABIN AFT 3 LIGHTS. RECONNECTED EMERGENCY FLOOR LIGHTS IN AFT CABIN. OPERATIONAL CHECKS NORMAL. (M) 2 L 7 2 4F RT A16WE 2001032200260 20010322 00260 NM 2001 3 22 ASAA0140014 1 20010127 A 3350 LIGHT BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 776AS 25109 PDX - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE AT ROWS 13-15. RECONNECTED EMERGENCY FLOOR LIGHTS AT R OWS 13-15. OPERATIONAL CHECKS NORMAL. (M) 2 L 7 2 4F RT A16WE 2001032200261 20010322 00261 NM 2001 3 22 ASAA0140013 1 20010123 A 3350 8100022607 LIGHT BOEING 737 7374Q8 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 765AS 25102 PDX - DURING LINE CHECK, FOUND 2 FORWARD RED EMERGENCY TRACK LIGHTS INOPERATIVE. REPLACED EMERGENCY FLOOR TRACK LIGHT A SSEMBLY. OPERATIONAL CHECKS GOOD. (M) 2 L 7 2 4F RT A16WE 2001032200262 20010322 00262 NM 2001 3 22 ASAA0140012 1 20010121 A 3350 LIGHT BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 765AS 25102 SAN - BEFORE FLIGHT, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 12-15. RECONNECTED LIGHTS OPS NORMAL. (M) 2 L 7 2 4F RT A16WE 2001032200263 20010322 00263 NM 2001 3 22 ASAA0140011 1 20010120 A 3350 LIGHT BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 784AS 28199 SEA - WHEN PERFORMING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 15-18. RECONNECTED LIGHTS OPS N ORMAL. (M) 2 L 7 2 4F RT A16WE 2001032200264 20010322 00264 NM 2001 3 22 ASAA0140010 1 20010121 A 3350 LIGHT BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 778AS 25110 PDX - WHEN PERFORMING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 17-19. RECONNECTED LIGHTS OPS N ORMAL. (M) 2 L 7 2 4F RT A16WE 2001032200265 20010322 00265 NM 2001 3 22 ASAA0140009 1 20010121 A 3350 LIGHT BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 778AS 25110 PDX - WHEN PERFORMING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN AFT CABIN. RECONNECTED LIGHTS, OPS NORMAL. (M) 2 L 7 2 4F RT A16WE 2001032200266 20010322 00266 EA 2001 3 22 WVBA2001015 2 20010226 A 8520 LW19340 CAMSHAFT PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA NR5/NR6 IN LOBES DAMAGED E WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 59764 913 913 317652037 L540261A DURING INSPECTION METAL CONTAMINATION WAS DISCOVERED IN THE OIL FILTER. A CHECK OF VALVELIFT WAS DONE AND IT WAS DISCOV ERED THAT NR5 AND NR6 INTAKE LOBES WERE EXCESSIVE. NR6 CYLINDER WAS REMOVED AND DAMAGE OBSERVED ON THE CAM LOBES AND TA PPET FOLLOWERS. NOTE: THIS IS THE 17TH ENGINE IN THREE YEARS. 1 L 7 2 3O 3 O A20SO E14EA 2001032200267 20010322 00267 EA 2001 3 22 WVBA2001014 2 20010226 A 8520 LW19340 CAMSHAFT PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA NR1/NR2 IN LOBE DAMAGED E WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 42WP 970 970 318252038 L508661A DURING INSPECTION METAL CONTAMINATION WAS DISCOVERED IN THE OIL FILTER. A CHECK OF VALVELIFT WAS DONE AND IT WAS DISCOV ERED THAT NR1 AND NR2 INTAKE LOBES WERE EXCESSIVE. NR1 CYLINDER WAS REMOVED AND DAMAGE OBSERVED ON THE CAM LOBES AND TA PPET FOLLOWERS. NOTE: THIS IS THE 18TH ENGINE IN THREE YEARS. 1 L 7 2 3O 3 O A20SO E14EA 2001032200268 20010322 00268 EA 2001 3 22 WVBA2001016 2 20010228 A 8520 LW19340 CAMSHAFT PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA NR1/NR2 IN LOBE DAMAGED E WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 3527U 516 516 317952141 L602061A DURING INSPECTION METAL CONTAMINATION WAS DISCOVERED IN THE OIL FILTER. A CHECK OF VALVELIFT WAS DONE AND IT WAS DISCOV ERED THAT NR1 AND NR2 INTAKE LOBES WERE EXCESSIVE. NR1 CYLINDER WAS REMOVED AND DAMAGE OBSERVED ON THE CAM LOBES AND TA PPET FOLLOWERS. NOTE: THIS IS THE 19TH ENGINE IN THREE YEARS. 1 L 7 2 3O 3 O A20SO E14EA 2001032600001 20010326 00001 NM 2001 3 26 UPS01235041 1 20010223 A 3510 LINE BOEING 727 7272A1 138407F NM O2 SYSTEM LEAKING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 213UP 21341 INSPECTION TYPE:PFLT 1ST OBS 02 PRESS LINE LEAKING. *S/D* REMOVED CAP AND INSTALLED NEW O2 FLEX LINE (P/N 10-60174-36) (SP0707172) PER M/M 35-00-00/201-204. INSTALLED DEMAND DILUTER REGULATOR AND TESTED PER M/M 35-11-31, LEAKED CK''ED B OTH LINE AND REGULATOR, CK''S OK. 2 L 7 3 4F A3WE 2001032600002 20010326 00002 NM 2001 3 26 DHL2001709001 1 20010217 A 8012 HARNESS BOEING 727 72782C 1384026 NM COCKPIT CHAFED A DHLA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 709DH 19968 DURING TAXI-OUT, ENGINE NR 3 START VALVE OPEN LIGHT ILLUMINATED. TROUBLESHOT SYSTEM AND FOUND START VALVE LIGHT SWITCH CANNON PLUG WIRES CHAFING (BARE) AND WITHOUT STRAIN RELIEF. INSTALLED NEW PINS AND STRAIN-RELIEF BACKSHELL REFERENCE M/ M 20-11-0. PERFORMED ENGINE START SYSTEM. OPS CHECK GOOD IAW M/M 80-11-0. 2 L 7 3 4F A3WE 2001032600003 20010326 00003 NM 2001 3 26 UPS01535042 1 20010222 A 3230 LANDING GEAR BOEING 757 75724APF 1384969 NM NLG & MLG MALFUNCTIONED A IPXA K NONE O OTHER CL CLIMB 1 SO 01 424UP 25369 INSPECTION TYPE:N/A, AFTER TAKEOFF (SDF) LANDING GEAR LEVER COULD NOT BE RAISED USED LOCK OVRD BUTTON. *S/D* REMOVED A ND REPLACED LT MLG EM DEFERRED TRUCK TILT POSTIONER SHUTTLE VALVE. OPS AND LEAK CHECK GOOD. SEVERAL GEAR SWINGS C/W. NO DEFECTS NOTED. 2 L 7 2 4F RT A2NM 2001032600006 20010326 00006 EA 2001 3 26 COMA0160278 1 20010222 A 2750 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA TE FLAPS ACTIVATED A COMA K NONE J WARNING INDICATION DE DESCENT 1 SO 01 976CA 7151 DURING DESCENT INTO NAS RECEIVED FLAP FAIL CAUTION WHEN FLAPS WERE SELECTED TO 8 DEGREES. COMPLIED WITH AD 98-20-01 PAR AGRAPH (B) 1, 2, 3 (A, B, C AND E) AND DEFERRED FLAP FAIL MESSAGE. 2 L 7 2 4F RT A21EA 2001032600007 20010326 00007 EA 2001 3 26 COMA0160279 1 20010222 A 2750 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA TE FLAPS ACTIVATED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 735CA 7267 ON APPROACH TO YYZ RECEIVED A FLAP FAIL CAUTION WHEN FLAPS WERE SELECTED FROM 30-45 DEGREES. COMPLIED WITH AD 98-20-01 PARAGRAPH (B) 1, 2, 3, (A, B, C, AND E) AND DEFERRED FLAP FAIL MESSAGE. 2 L 7 2 4F RT A21EA 2001032600008 20010326 00008 EA 2001 3 26 COMA0160280 1 20010221 A 2750 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA TE FLAPS ACTIVATED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 408CA 7440 FLAPS FAIL MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2001032600021 20010326 00021 WP 2001 3 26 AT0100103 1 20010208 A 5310 DOOR FRAME DOUG DC9 DC932 3022066 WP AFT CARGO BAY CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 FOUND AFT CARGO DOOR FRAME CRACKED. STOP DRILLED CRACK AND FABRICATED AND INSTALLED DOUBLER IAW DC9 SRM 51-10-02, 51-10 -03, 51-10-04, 51-30-02, 51-30-01, AND 52-03. 2 L 7 2 4F A6WE 2001032600022 20010326 00022 NM 2001 3 26 DL73E010315 1 20010222 A 2613 LOOP BOEING 737 737247 138448D NM FUSELAGE INTERMITTENT A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 376DL 23603 AFTER T/O LEFT BODY OVERHEAT LIGHT ILLUMINATED AND REMAINED ON THEN FLICKERD AFTER POM. DROPPED ECS BAY LEADING EDGE FL APS, SHOOK DOWN WIRES TO THERMOCOUPLES (FOUND NO INTERMITTENT LIGHT) REP COMPONENT OVERHEAT UNIT AND TESTED GOOD. 2 L 7 2 4F A16WE 2001032600023 20010326 00023 2001 3 26 DL777010316 4 20010222 A 2330 AUDIO VIDEO UNIT BOEING 777 777232 1385232 NM ENTERTAIN SYS ODOR A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 862DA 29734 IN FLIGHT AN ELECTRICAL ODOR WAS EVIDENT AROUND SEAT 37 A/B AND SEAT 38 A/B. NO SMOKE WAS VISIBLE NO CAUSTIC BURNING EY ES OR NOSE. ENTERTAINMENT SYS/CABIN LIGHTS/GALLEYS WERE DEPOWERED. ODOR WAS NO LONGER EVIDENT. VISUAL INSP OF ALL AUD IO/VIDEO POWER BOXES FROM SEAT 30 A/B--40 A/B GOOD FUNCTIONAL OPERATION 30 A/B-40 A/B NORMAL. REMOVED AND REPLACED AVU POWER BOX AT SEAT 37 A/B AND 38 A/B AS A PRECAUTIONARY MEASURE ONLY. RAN SYS FOR 5 HOURS WITH NO EVIDANCE OF SMOKE OR F UMES. 2 L 7 2 4F RT T00001SE 2001032600024 20010326 00024 NM 2001 3 26 DL72E010318 1 20010222 A 5754 STIFFENER BOEING 727 727247 138408F NM SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 283WA 21485 FWD SPAR VERTICAL STIFFENER CRACKED AT I/B SIDE OF NR 6 SLAT I/B TRACK. REPLACED STIFFENER PER MM 57-20-021-8. 2 L 7 3 4F A3WE 2001032600027 20010326 00027 WP 2001 3 26 01FDEA00122 1 20010212 A 5320 BRACKET DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 308FE 48297 AFT FUSELAGE COMP ZONE 312 STA Y2092.880 CAN''T TOP ANGLE BRACKET FOUND CRACKED AT BOTH ENDS. *S/D* REMOVED, REPLACED AND FAB PER IAW DRW AJC 7028, SRM 51-31-01 VOL 11. 2 L 7 3 4F RT A22WE 2001032600028 20010326 00028 WP 2001 3 26 01FDEA00123 1 20010212 A 5320 BRACKET DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 308FE 48297 AFT FUSELAGE COMP ZONE 312 STA Y2069.440 CAN''T TOP ANGLE BRACKET LT CORNER CRACKED. *S/D* REMOVED, REPLACED AND FAB P ER IAW DRW AJC 7029, SRM 51-31-01 VOL 11. 2 L 7 3 4F RT A22WE 2001032600029 20010326 00029 WP 2001 3 26 01FDEA00124 1 20010212 A 5320 BRACKET DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 308FE 48297 AFT FUSELAGE COMPARTMENT ZONE 312 STA Y2046.000 CAN''T TOP ANGLE BRACKET FOUND CRACKED AT BOTH ENDS. *S/D* REMOVED, RE PLACED AND FAB PER DRW AJC 7021, SRM 51-31-01 VOL 11. 2 L 7 3 4F RT A22WE 2001032600030 20010326 00030 NM 2001 3 26 DL72E010319 1 20010222 A 5754 STIFFENER BOEING 727 727247 138408F NM SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 283WA 21485 FWD SPAR STIFFENER CRACKED AT I/B SIDE OF NR 6 SLAT O/B TRACK. REPLACED STIFFENER PER MM 57-20-021-8. 2 L 7 3 4F A3WE 2001032600031 20010326 00031 NM 2001 3 26 DL72E010320 1 20010222 A 5754 ANGLE BOEING 727 727247 138408F NM L/E FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 283WA 21485 A .25 INCH CRACK AT FWD SIDE OF NR 6 L/E FLAP ACTUATOR MOUNT BOX O/B TRUNNION UPPER ATTACH ANGLE. REPAIRED PER MM. 2 L 7 3 4F A3WE 2001032600032 20010326 00032 WP 2001 3 26 TWAA0103502 1 20010222 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT FOUND RIVET HOLES ALONG INSIDE EDGE OF MEMBRANE DAMAGED FROM STA 1238 TO 1250, LT SIDE. INSTALLED DOUBLER PER SRM 53-01, PAGE 9 FIG 2 AND SHEET 3. PRIMED AND PAINTED DOUBLER PER SRM 51-10-3. INSTALLED FASTENERS PER S RM 51-10-05. 2 L 7 2 4F A6WE 2001032600033 20010326 00033 EU 2001 3 26 MALA010207 1 20010209 A 3020 NH24668169 DUCT SAAB SF340 340B 7860101 EU LT INTAKE BURNED A MALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 15 453XJ 453 LT ENGINE INTAKE HEAT MAT BEGAN TO SHOOT SPARKS, BURN INFLIGHT. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED LOWER D UCT ON LT ENGINE. RAN A/C HALF HR, OPS CHECK GOOD IAW SAAB MM 30-00-0. (P/N NH24668-169) (S/N OFF L283723) (S/N ON L19 8033). 2 L 7 2 4T RT A52EU 2001032600038 20010326 00038 EU 2001 3 26 MALA010208 1 20010216 A 3222 STRUT SAAB SF340 SF340A 7850100 EU NLG LOW A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 76XJ 076 LANDING GEAR INTRANSIT LIGHT REMAINED ON AFTER RETRACTING GEAR. AIR RETURN TO RHI. MAINTENANCE SERVICED NOSE LANDING G EAR IAW 12-30-32-3. COMPLETED SEVERAL RETRACTION AND EXTENSION CHECKS. ALL OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2001032600039 20010326 00039 EU 2001 3 26 MALA010209 1 20010217 A 2436 51530007B GCU SAAB SF340 340B 7860101 EU RT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 430XJ 430 DC GENERATOR CAUTION LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. COULD NOT RESET. AIR RETURN TO DTW. MAINTENANCE REPLACE D RT DC GCU (P/N 51539-007B) (S/N ON 99572). RT AIRCRAFT IN SEVERAL CONFIGUATIONS. ALL CHECKS GOOD AT THIS TIME. ALL IAW SF340 AMM. 2 L 7 2 4T RT A52EU 2001032600040 20010326 00040 EU 2001 3 26 MALA010210 1 20010221 A 2430 501171202 POWER SUPPLY SAAB SF340 SF340A 7850100 EU COCKPIT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 102XJ 340A102 AIR RETURN DUE TO EMERGENCY POWER PROBLEM. LOST EMERGENCY POWER AFTER TAKEOFF. VOLTAGE WAS NORMAL. LOST STANDBY HORIZ ON AND COM 1. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY (P/N 501-1712-02) (S/N ON 1679) (S/N OFF 4585) PE R SAAB AMM 24-35-10-4. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2001032600041 20010326 00041 EU 2001 3 26 MALA010206 1 20010218 A 5755 STRAP BAC 146 AVRO146RJ85A 1500097 EU SPOILER BENT A MALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 15 514XJ E2330 AIRFRAME VIBRATION CLIMBING THROUGH 18,000 FT. FLIGHT RETURNED TO DTW. MAINTENANCE FOUND RT SECOND AND THIRD FROM FUSE LAGE SPOILERS TITANIUM STRIP BENT UP. RE-ADJUSTED TITANIUM STRIP IAW RJ85 MM 27-61-00, GAPPED CHECKED SPOILERS TO FLAPS , ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 2001032600042 20010326 00042 NM 2001 3 26 NACA2001009 1 20010120 A 5315 FLOORBEAM BOEING 727 72746 1384013 NM FUSELAGE CORRODED A NACA K NONE O OTHER IN INSP/MAINT 1 AL 03 190AJ 18878 FLOORBEAM AT BS 1090, LBL 62.5 CORRODED. REMOVED CORRODED AREA, FABBED AND INSTALLED REPAIR PARTS PER SRM 53-10-8 FIG 8 . 2 L 7 3 4F A3WE 2001032600043 20010326 00043 NM 2001 3 26 NACA2001010 1 20010120 A 5320 STRINGER CLIP BOEING 727 72746 1384013 NM FUSELAGE CRACKED A NACA K NONE O OTHER IN INSP/MAINT 1 AL 03 190AJ 18878 BS 680 STRINGER 17L CRACK AT FUSELAGE TO FRAME CLIPS FORWARD AND AFT. REPLACED (2) SHEAR TIES, MADE FROM 7075-T6, .040. PER SRM 53-10-4 FIG 11, 12 AND 13. 2 L 7 3 4F A3WE 2001032600044 20010326 00044 NE 2001 3 26 SCNA01015 2 20010211 A 7230 COMPRESSOR BOEING 727 727282 138408T NM PWA JT8 JT8D17 52049 NE NR 3 ENGINE STALLED A SCNA K NONE O OTHER LD LANDING 1 GL 15 281SC 21949 688213 DURING LANDING ROLL AT MSP SOFT COMPRESSOR STALL ON ENGINE NUMBER THREE. INSPECTED INLETS AND EXAUST ON NUMBER THREE EN GINE. NO DEFECTS NOTED. 2 L 7 3 4F 4 F RT A3WE E2EA 2001032600046 20010326 00046 EU 2001 3 26 JBXA000249 1 20010225 A 3241 60042752 TRANSDUCER FOKKER F28 F28MK0100 4990807 EU MLG FAILED A JBXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 05 110ML 11486 LIFT DUMPER FAULTED ON TAKEOFF ROLL 80-90 KNOTS. FOUND RIGHT OUTBOARD WHEEL SPEED TRANSDUCER FAULTING. REMOVED AND REP LACED NR 4 WHEEL SPEED TRANSDUCER IAW AMM 32-45-02, OPS CHECK GOOD. 2 L 7 2 4F RT 2001032600047 20010326 00047 SO 2001 3 26 C2XA01IA123 1 20010226 A 3350 110049 POWER SUPPLY EMB 145 EMB145ER SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14938 145029 IAH - DURING A-CHECK INSPECTION, THE PASSENGER DOOR OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENA NCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY IN ACCORDANCE WITH EMB-145 M/M 33-50-04, AND THE AIRC RAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001032600048 20010326 00048 SO 2001 3 26 C2XA01IA124 1 20010225 A 2613 W510007522A WIRE EMB 120 EMB120ER 3260203 SO LT WING BROKEN A C2XA E A D ENGINE SHUTDOWN UNSCHED LANDING RETURN TO BLOCK N FALSE WARNING CR CRUISE 1 SW 27 58733 120197 IAH - FLIGHT 3035, THE CREW REPORTED A LEFT ENGINE DUCT LEAK LIGHT ILLUMINATED IN FLIGHT, THE LEFT ENGINE SHUT DOWN AS A PRECAUTION, AND THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND RESECURED A LOOSE WIRE ON A DUCT TEMP SENSOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE DISCREPANCY REPE ATED ON FLIGHT 3442, THE ENGINE WAS PRECAUTIONARILY SHUTDOWN, THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCID ENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPAIRED A BROKEN WIRE ON THE LEFT WING INBOARD DUCT LEAK SENSOR, AND THE A IRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001032600049 20010326 00049 SO 2001 3 26 C2XA01IA125 1 20010220 A 3260 WARNING LIGHT EMB 120 EMB120ER 3260203 SO COCKPIT ILLUMINATED A C2XA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 27 22727 120177 IAH - FLIGHT 3243, THE CREW REPORTED THAT THE LEFT MAIN LANDING GEAR INDICATION WAS RED. THE AIRCRAFT RETURNED TO IAH W HERE IT LANDED WITHOUT INCIDENT. MAINTENANCE OPERATIONALLY CHECKED THE LANDING GEAR WITH NO DEFECTS NOTED, AND THE AIRC RAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001032600050 20010326 00050 WP 2001 3 26 0100721148 1 20010217 A 2170 COALESCER BAG DOUG DC10 DC1040 3023508 WP AC BAY DIRTY A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 148US 46757 AFTER TAKEOFF, AIR CONDITIONING PACKS PRODUCED A BLUE CLOUD OF BILLOWING SMOKE. FLIGHT RETURNED TO DTW AND LANDED WITHO UT INCIDENT. FOUND NR 2 AND NR 3 COALESCER BAGS DIRTY. REPLACED COALESCER BAGS AND PERFORMED PACK BURNOUT PROCEDURE. REPLACED AIR CYCLE MACHINE. OPERATIONAL CHECK NORMAL. 2 L 7 3 4F A22WE 2001032600051 20010326 00051 WP 2001 3 26 ABXA010079 1 20010106 A 5320 97549495 INTERCOSTAL DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 820AX 46155 CORROSION WAS FOUND AT FUSELAGE STATION 1200 - 1180 L34R INSIDE THE TORQUE BOX. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW ABX REA D853-39259 AND DC-8 SRM 51-1-20. 2 L 7 4 4F 4A25 2001032600052 20010326 00052 2001 3 26 DHL2001801002 4 20010226 A 3425 2587909903 ADI DOUG DC8 DC873F 302199F WP COCKPIT MALFUNCTIONED A DHLA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 801DH 46033 F/O ADI BANKS 1/4 OF CAPTAINS AND DURING TURNS HORIZON FLAG ILLUMINATED. F/O HSI HAS OFF FLAG AND DRIFTS FROM CAPTAIN'' S HSI. REMOVED AND REPLACED F/O''S ADI. OPS CHECKED OK IAW M/M 34-20-0 AND LITTON LTR-97 SUP M/M 34-20-25. RERACKED H SI INDICATOR AND COULD NOT DUPLICATE PROBLEM. SWAPPED NR 1 AND NR 2 HSI FOR FURTHER TROUBLESHOOTING. OPS CHECK OK IAW M/M 34-21-0 AND LITTON LTR-97. 2 L 7 4 4F RT 4A25 2001032600053 20010326 00053 WP 2001 3 26 0100759853 1 20010222 A 2160 CONTROL VALVE DOUG DC9 DC951 3022051 WP RT A/C PACK CONTAMINATED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 762NC 47710 FLIGHT ATTENDANT NOTIFIED CREW OF THE RIGHT AFT LAV SMOKE DETECTOR IN ALARM ALONG WITH A SMELL OF SMOKE IN THE AFT CABIN . AN EMERGENCY WAS DECLARED AND A SAFE LANDING WAS MADE IN JAX. NO EVIDENCE OF FIRE OR SMOKE WAS FOUND AFTER LANDING. SOME OIL RESIDUE WAS FOUND IN THE RIGHT WATER SEPARATOR TEMPERATURE CONTROL VALVE. REPLACED THE RIGHT WATER SEPARATOR TEMPERATURE CONTROL VALVE. REPLACED THE RIGHT WATER SEPARATOR BAG PRECAUTIONARY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2001032600054 20010326 00054 NM 2001 3 26 DHL2001743002 1 20010227 A 2701 CONTROL COLUMN BOEING 727 727225 1384077 NM COCKPIT BINDING A DHLA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 743DH 22438 DURING ELEVATOR CHECK, CONTROL COLUMN PRESSURE FORE AND AFT IS VERY HIGH. UNUSUALLY STIFF CONTROL FORCES IN BOTH DIRECT IONS. PER BMM 27-30-0, PERFORMED HORIZONTAL STABILIZER T/E TO ELEVATOR. INSPECT AND SPRING SCALE PULL TEST AT 45 LBS F ULL AFT. SYSTEM HAS NO BINDS. A/C OK FOR SERVICE. 2 L 7 3 4F A3WE 2001032600055 20010326 00055 NM 2001 3 26 AWXA0001424 1 20010301 A 5312 651630084 BULKHEAD BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 FS 178 BLKHD HAS A CRACK IN WEB EMINATING FROM FASTENER HOLE. CUT OUT DAMAGED AREA; HFEC CONFIRMS NO CRACKS ON EDGE OF CUTOUT. FABED, DRILLED AND INSTALLED FILLER AND DOUBLER IAW B737-200 SRM 53-30-02. 2 L 7 2 4F RT A16WE 2001032600056 20010326 00056 NM 2001 3 26 AWXA0001425 1 20010301 A 5210 50079454 SKIN BOEING 737 737277 1384570 NM ENTRY DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 FWD ENTRY DOOR INNER SKIN CRACKED AT UPPER FWD ACCESS OPENING. FABED REPAIR DOUBLER AND INSTALLED IAW B737-200 SRM 51-4 0-02. 2 L 7 2 4F RT A16WE 2001032600057 20010326 00057 NM 2001 3 26 AWXA0001426 1 20010301 A 5312 651630084 BULKHEAD BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 FS 178 BLKHD HAS 3 CRACKS IN WEB MEASURING 1.3, 0.2, AND 0.3 INCH. REPAIRED WEB IAW SRM 53-10-02 PG 3, 5, 8-10, 53-10-1 1 PG 1-8, 53-30-02 PG 2, 3, 5, 32, 51-20-04 PG 1-7 AND B737-200 MM 51-21-40 PG 702-706. 2 L 7 2 4F RT A16WE 2001032600058 20010326 00058 NM 2001 3 26 AWXA0001427 1 20010301 A 5320 654583340 WEB BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 FLOOR WEB ON AFT SIDE OF BS 178 BLKHD SIDE CHORD AREA AT WL 207 CRACKED. REPLACED FLOOR WEB IAW SRM 51-20-4 PG 1-7, SRM 51-30-5 PG 32, 2, 3, 5, SRM 51-40-03 PG 1-10, SRM 51-10-01 PG 20-24 AND MM 51-21-41 PG 702-706. 2 L 7 2 4F RT A16WE 2001032600060 20010326 00060 NM 2001 3 26 AWXA0001430 1 20010301 A 5310 65528747 DOOR FRAME BOEING 737 737277 1384570 NM L2 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 CRACK IN L2 DOOR JAMB FWD UPPER WEB AT BS 947. REMOVED DAMAGED AREA AND INSTALLED A REPAIR DOUBLER AND FILLER IAW SRM 5 1-40-03. 2 L 7 2 4F RT A16WE 2001032600061 20010326 00061 NM 2001 3 26 AWXA0001433 1 20010301 A 5230 521065R5 WEB BOEING 737 737277 1384570 NM AFT CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 AFT CARGO DOOR INTERNAL WEB IS CRACKED AT ATTACH POINT TO LWR CROSS BEAM, LOCATED IN CENTER OF DOOR BELOW HANDLE MECHANI SM. INSTALLED FILLER AND DOUBLER IAW SRM 51-10-03, 52-30-01, 51-10-01, 51-30-02 AND 51-40-03. 2 L 7 2 4F RT A16WE 2001032600062 20010326 00062 NM 2001 3 26 AWXA0001434 1 20010301 A 5320 65C278151 ANGLE BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 NR 2 VHF ANTENNA SUPPORT ANGLE IS CRACKED OUT OF FASTENER HOLE ON RT SIDE AT FS 500 TO 500A BETWEEN STR 28L AND 28R. RE MOVED CRACKED ANGLE AND SUPPORTING STRUCTURE; INSTALLED NEW SUPPORTS, CLIPS, ANGLE, FITTING AND DOUBLER IAW AWA EO 53-33 -02 AND DWG 65C27810. 2 L 7 2 4F RT A16WE 2001032600063 20010326 00063 NM 2001 3 26 AWXA0001436 1 20010301 A 5320 693535214 STRINGER CLIP BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 CABIN STR CLIP AT FS 787 STR 5R IS CRACKED. REMOVED AND REPLACED STR CLIP IAW SRM 51-30-02 PG 5. 2 L 7 2 4F RT A16WE 2001032600064 20010326 00064 NM 2001 3 26 AWXA0001437 1 20010301 A 5320 694545214 STRINGER CLIP BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 CABIN STR CLIP AT FS 787 STR 2R IS CRACKED. REMOVED AND REPLACED STR CLIP IAW SRM 51-30-02 PG 5. 2 L 7 2 4F RT A16WE 2001032600065 20010326 00065 NM 2001 3 26 AWXA0001438 1 20010301 A 5320 693535214 STRINGER CLIP BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 CABIN STR CLIP AT FS 727B STR 4R IS CRACKED. REMOVED AND REPLACED STR CLIP IAW SRM 51-30-02 PG 5. 2 L 7 2 4F RT A16WE 2001032600066 20010326 00066 NM 2001 3 26 AWXA0001439 1 20010301 A 5320 693535214 STRINGER CLIP BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 CABIN STR CLIP AT FS 727A 3L IS CRACKED. REMOVED AND REPLACED CLIP IAW SRM 51-30-02 PG 5. 2 L 7 2 4F RT A16WE 2001032600067 20010326 00067 NM 2001 3 26 AWXA0001440 1 20010301 A 5320 693535214 STRINGER CLIP BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 CABIN STR CLIP AT FS 727A STR 6L IS CRACKED. REMOVED AND REPLACED STR CLIP IAW SRM 51-30-02 PG 5. 2 L 7 2 4F RT A16WE 2001032600068 20010326 00068 NE 2001 3 26 DLM88010312 2 20010222 A 7320 THROTTLE CABLE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE OBSTRUCTED A DALA E ENGINE SHUTDOWN O OTHER AP APPROACH 1 SO 27 911DL 36511 49542 716782 RIGHT THROTTLE STUCK AT 79 PERCENT COULD NOT RETARD BELOW THAT SETTING. SHUT DOWN THE ENGINE. REMOVED OBSTRUCTION FROM TAIL COMPARTMENT QUADRANT, CHECKS OK. 2 L 7 2 4F 4 F RT A6WE E9NE 2001032600069 20010326 00069 NM 2001 3 26 DL76L010321 1 20010223 A 3240 BRAKE BOEING 767 767332 1382001 NM LT MLG SMOKE A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 180DN 25985 REPORT ON LANDING SNN OF SMOKE FROM LEFT MAIN LANDING GEAR AREA. INSPECTED LEFT L/G AND SMOKE CAUSED BY HEATING OF RESI DUAL DEICING FLUID ON MLG BRAKES. BRAKE TEMP WAS NORMAL. A/C OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2001032600070 20010326 00070 NE 2001 3 26 DL72S010322 2 20010223 A 7314 O-RING BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE FUEL PUMP LEAKING A DALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 542DA 63696 22391 696519 AT FL 310, NR 2 ENGINE OIL PRESSURE WAS BELOW GREEN BAND. OIL QTY WAS ZERO. ENGINE SHUT DOWN PER POM. FOUND O-RING LEA KING AT FUEL PUMP TO GEARBOX INTERFACE. REPLACED SAME. 2 L 7 3 4F 4 F A3WE E2EA 2001032600071 20010326 00071 NM 2001 3 26 DL72L010324 1 20010223 A 5753 651626920 FLAP TRACK BOEING 727 727232 1384082 NM WING CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 510DA 21312 DURING OVERHAUL AT BF GOODRICH THE INBOARD FLAP, NR 4 INBOARD TRACK WAS FOUND WITH WEAR AND CORROSION AT THE MLG AND SPO ILER BEAM ATTACH PADS, THE MLG DOOR FWD HINGE FITTING AND FWD BRACKET LOWER ATTACH HOLES, FWD LUG BORES, AND IN THE TOGGLE DETENT HOLE. REPAIR PER ER/A 401433-14AD AND BF GOODRICH ENGINEERING REPAIR DOCUMENT 23-0683. 2 L 7 3 4F A3WE 2001032600072 20010326 00072 NE 2001 3 26 DLM11010326 2 20010223 A 7261 PW4460 ENGINE DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 2 ENGINE OVERSERVICED A DALA A UNSCHED LANDING M OVER TEMP CR CRUISE 1 SO 27 805DE 11935 11935 48476 723870 THE NUMBER TWO ENGINE WAS RUNNING AT 149 DEG CELSIUS TO 152 DEG CELSIUS IN CRUISE. THIS WAS APPROX 40 DEG CELSIUS ABOVE NR 1 AND NR 3. THE FLIGHT (79) DIVERTED TO PDX. FOUND ENGINE OIL OVERSERVICED. REMOVED OIL TO PROPER LEVEL. 2 L 7 3 4F 4 F RT A22WE E24NE 2001032600073 20010326 00073 NM 2001 3 26 DL767010327 1 20010223 A 3350 1000677 LIGHT BOEING 767 767232 1385132 NM COCKPIT INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 109DL 22221 FLIGHT DECK EMERGENGY EXIT LIGHT FAILED TO ILLUM WITH OVHD EMERGENCY LIGHT SW ON ALL CABIN EMERGENCY LIGHTS WORK NORMAL. REPLACED EMERGENCY LIGHT ASSY OPS CKS GOOD. 2 L 7 2 4F RT A1NM 2001032600074 20010326 00074 WP 2001 3 26 ABXA010067 1 20010228 A 5711 SPAR DOUG DC9 DC941 302207N WP WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 972AX 47631 THE FORWARD WING SPAR HAD A THREE INCH CRACK AT BL 0 DIRECTLY ABOVE THE PRESSURE WEB. MAINTENANCE INSPECTED AND REPAIRE D THE CRACK IAW ABX REA D953-38815-MR. 2 L 7 2 4F A6WE 2001032600075 20010326 00075 NM 2001 3 26 DL733010328 1 20010224 A 2530 8606010000 OVEN BOEING 737 737301 1384611 NM FWD GALLEY MALFUNCTIONED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 948WP 23259 FWD OVEN HAD AN ELECTRICAL /BURNT SMELL. GALLEY PWR WAS REMOVED, CONDITION IMPROVED. REPLACED FWD GALLEY OVEN AND BOTH CONTROLLERS. OVEN DPN 255701023, S/N 98-12-0066, CONTROL DPN 255701024, S/N OFF 8601-0701 & 8612-1728. 2 L 7 2 4F RT A16WE 2001032600076 20010326 00076 NM 2001 3 26 DL73K010330 1 20010226 A 5311 6546541504 FRAME BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 315DL 23087 THE FS 663 FRAME WAS FOUND CRACKED AT STR 1R AND 3R. REPAIRED SIMILIARLY TO SRM 53-10-4, FIG 14. THE SKIN WAS CUT AT EACH LOCATION TO FACILITATE THE REPAIR AT HMV. 2 L 7 2 4F RT A16WE 2001032600077 20010326 00077 NM 2001 3 26 DL72W010331 1 20010226 A 5313 65564414 STRINGER BOEING 727 727247 138408F NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W 21057 STRINGER 29R WAS FOUND CRACKED AT FS 950E AND 975. THE STRINGER WAS CUT AT FS 950D +10 AND REPLACED AFT TO THE MFG SPLI CE LOCATION. THE DAMAGE WAS FOUND AT MV. 2 L 7 3 4F A3WE 2001032600078 20010326 00078 NM 2001 3 26 DL733010332 1 20010227 A 5330 65458774 DOUBLER BOEING 737 737330 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242DL 23834 THE BEAR STRAP AT THE LOWER AFT CORNER OF THE R1 DOOR WAS FOUND WITH A 1 INCH CRACK. THE DAMAGE WAS TRIMMED OUT AND A R EPAIR WAS INSTALLED PER SRM 53-10-01, FIGURE 202. THE REPAIR WAS ACCOMPLISHED AT MV. 2 L 7 2 4F RT A16WE 2001032600079 20010326 00079 2001 3 26 COMA0160290 4 20010225 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 988CA 7204 STALL FAIL CAUTION MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001032600080 20010326 00080 WP 2001 3 26 ABXA010075 1 20010228 A 5311 99115055 FRAME DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 972AX 47631 FRAME (P/N 9911505-5) FUSELAGE STATION 83.5 WAS CRACKED. MAINTENANCE INSPECTED AND REPAIRED THE FRAME IAW DC-9 SRM 53-0 3 FIG 34. 2 L 7 2 4F A6WE 2001032600084 20010326 00084 NE 2001 3 26 RAIA00102010 2 20010226 A 7200 TPE33114HR ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RT ENGINE FLAMED OUT A RAIA K NONE X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 CE 03 553HK 10059 1324 41066 76101 5372-BWI- AFTER LANDING IN EWR RIGHT ENGINE LOST POWER ON TAXI IN. MAINTENANCE INSPECTED, PERFORMED ENGINE PERFORMANCE RUN. ALL PARAMETERS NORMAL. 2 L 7 2 4T 4 T RT A41NM E18NE 2001032600085 20010326 00085 SO 2001 3 26 LR7A01002 1 20010227 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 536 4763 DURING SCHEDULED B3 CHECK PER JOB CARD HB0505, FOUND FS 902 RT WEB CRACKED AT RBL 62, WL 220. REPAIRED IAW SRM SMP 583- 51-140-17. 2 H 7 4 4T A1SO 2001032600086 20010326 00086 SO 2001 3 26 LR7A01003 1 20010227 A 5320 RETAINER LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 536 4763 DURING SCHEDULED B3 CHECK PER JOB CARD HB0505, FOUND FS 838 SEAL RETAINER BENT AND CRACKED AT RLB 62, WL 160. REPAIRED IAW SRM SMP 583-51-140-19. 2 H 7 4 4T A1SO 2001032600087 20010326 00087 SO 2001 3 26 LR7A01004 1 20010227 A 5312 BULKHEAD LKHEED 382 382G 526414U SO LT MLG WW CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 536 4763 DURING SCHEDULED B3 CHECK PER JOB CARD HB0506, FOUND FS 608 LT WW BULKHEAD CRACKED AT RBL 62, WL 192 INSULATION MOUNT ST UD. REPAIRED IAW SRM SMP 583-53-40-10. 2 H 7 4 4T A1SO 2001032600088 20010326 00088 WP 2001 3 26 TWAA0103701 1 20010223 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT FOUND FLOORBEAM/CEILING SUPPORT CORRODED ALONG STA 1308, 20 INCHES INBD OF LONGERON 19L. REPAIRED FLOORBEAM AT STA 1308 PER SRM 53-05 FIG 79 SHEET 8-9-10, ARA 17629 PAGE 1-2-3, SRM 51-60-0, SRM 51-20-0, AND SRM 51-10-3 . 2 L 7 2 4F A6WE 2001032600089 20010326 00089 WP 2001 3 26 TWAA0103702 1 20010224 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT FOUND CORROSION ON NUMBER 2 CABIN TRACK AT LBL 44 INCHES, STA 1155 TO 1308. REMOVED AND REPLACED T RACK STA 1145 TO 1309. INSTALLED WITH HARDWARE PER SRM 51-30-5. INSTALLED TRACK WITH NAS 6203 BOLTS, MS 2104L3 NUTS, M S 250 WASHERS, AND TORQUED PER SRM 51-30-1. ATTACHED MEMBRANE TO TRACK WITH AD RIVETS PER SRM 51-30-2, AND SRM 53-05 FI G 4F. 2 L 7 2 4F A6WE 2001032600090 20010326 00090 WP 2001 3 26 TWAA0103703 1 20010223 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE MISDRILLED A TWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT FOUND IN FWD CABIN MEMBRANE MISDRILLED AT FASTENER HOLE LBL 56 INCHES OTBD SIDE, STA 200 TO 215. R EMOVED MISDRILLED MEMBRANE. INSTALLED REPAIR AND BRACKET THAT WAS REMOVED FOR REPAIR PER SRM 51-70-4. PAINTED AND TREA TED PER SRM 51-10-3. INSTALLED FASTENERS PER SRM 51-30-8. 2 L 7 2 4F A6WE 2001032600091 20010326 00091 WP 2001 3 26 TWAA0103704 1 20010224 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING CHECK-C MAINT FOUND CORROSION ON CHAIR TRACK AT STA 1098 TO 1139, SHORT TRACK UNDER FORWARD AFT GALLEY. INSTALLE D NEW SECTION OF FLOOR TRACK AT STA 1098 TO 1139 PER SPM 6-70-01, PAGE 3 AND DOUGLAS INSTALLATION DRAWING 5930566. 2 L 7 2 4F A6WE 2001032600092 20010326 00092 WP 2001 3 26 TWAA0103705 1 20010224 A 5313 LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 986Z 47589 THE BOTTOM AFT SIDE OF LONGERON 17L WAS CRACKED .125 INCH AT STA 965 AND FOUND EXISTING REPAIR HAD HI-LOKS TOO LONG. RE MOVED AND REPLACED LONGERON 17L FROM STA 965 TO 996 PER SRM 51 AND STANDARD PRACTICES FROM ORIGINAL SPLICE TO END FITTIN G, AND ADDED WASHER TO HI-LOK. CHECK-C 1-13-0 STL. 2 L 7 2 4F A6WE 2001032600093 20010326 00093 NM 2001 3 26 C1HA200193003 1 20010217 A 2530 WIRE BOEING 727 727212 138407G NM GALLEY DETACHED A C1HA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 15 293AS 21348 FLIGHT ATTENDENT SMELLED SMOKE IN AFT GALLEY ON APPROACH INTO PUJ. UPON LANDING FOUND A WIRE HANGING IN AFT GALLEY COMP ARTMENT BELOW COFFEEMAKER. FOUND WIRE PULLED OFF HOT PLATE TERMINAL REPAIRED WIRE, OPS CHECKED NORMAL. 2 L 7 3 4F A3WE 2001032600094 20010326 00094 NM 2001 3 26 C1HA200181001 1 20010211 A 3260 SWITCH BOEING 727 7272S7 138407Z NM RT MLG OUT OF ADJ A C1HA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 681CA 22020 RIGHT MAIN GEAR DOOR LIGHT CAME ON WHEN GEAR HANDLE MOVED TO OFF POSITION. INSPECTED AND ADJUSTED DOOR UPLOCK SWITCH PE R 32-62, OK FOR SERVICE. 2 L 7 3 4F A3WE 2001032600095 20010326 00095 NM 2001 3 26 C1HA200182001 1 20010216 A 3222 STRUT BOEING 727 7272S7 138407Z NM NLG LOW A C1HA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 682CA 22019 UPON GEAR RETRACTION NOSE GEAR LIGHT STAYED ON. CYCLED GEAR TWO TIMES, LIGHT STAYED ON. RETURNED TO LAS, OVERWEIGHT LA NDING VERY SOFT LANDING. INSP AND FOUND NOSE STRUT FLAT. RESERVICED LUBED GEAR SWIVELS AND ALL ROD ENDS CLEANED AND CH ECKED NOSE GEAR SWITCHES AND NO DEFECTS NOTED. PERFORMED NOSE GEAR EXTENSION AND RETRACT PER 32-21, CKS NORMAL. OK FOR SERVICE. OVERWEIGHT LANDING INSPECTION ACCOMPLISHED. 2 L 7 3 4F A3WE 2001032600096 20010326 00096 NM 2001 3 26 C1HA200186002 1 20010209 A 3350 1001141 LIGHT BOEING 727 7272S7 138407Z NM AFT AIRSTAIR INOPERATIVE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 686CA 22021 AFT AIRSTAIR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED AFT AIRSTAIR EXIT LIGHT. 2 L 7 3 4F A3WE 2001032600097 20010326 00097 NM 2001 3 26 C1HA200197001 1 20010211 A 2751 106079112 INDICATOR BOEING 727 727270 138408P NM COCKPIT FAILED A C1HA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 15 697CA 23052 ON TAXI OUT FLAPS SET TO 15 DEGREES OUTBOARD FLAPS EXTENDED TO 15 DEGREES, INBOARD FLAPS ONLY EXTEND 2 DEGREES. RETURNE D TO GATE. REMOVED AND REPLACED INBOARD FLAP POSITION INDICATOR, OPS CHECK OK PER 27-52-2. 2 L 7 3 4F RT A3WE 2001032600098 20010326 00098 WP 2001 3 26 ABXA010069 1 20010228 A 5312 5910130387 TEE FITTING DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 972AX 47631 THE NR 5 T-CAP ABOVE LONGERON 18L WAS CRACKED AS INDICATED BY LOW FREQUENCY EDDY CURRENT INSPECTION. MAINTENANCE INSPEC TED AND REPLACED THE NR 5 T-CAP IAW ABX EA 53120036-006. 2 L 7 2 4F A6WE 2001032600099 20010326 00099 WP 2001 3 26 ABXA010070 1 20010228 A 5412 991224618 BULKHEAD DOUG DC9 DC941 302207N WP PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 972AX 47631 A WEB WAS CRACKED AT FUSELAGE STATION 1114 LONGERON 12R. MAINTENANCE INSPECTED AND REPLACED THE WEB IAW DC-9 SRM. 2 L 7 2 4F A6WE 2001032600100 20010326 00100 WP 2001 3 26 ABXA010072 1 20010228 A 5311 99115057 FRAME DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 972AX 47631 FRAME (P/N 9911505-7) HAD ONE INCH CRACKS AT STATION 83.5. MAINTENANCE INSPECTED AND REPAIRED THE CRACKED AREA IAW DC-9 SRM 53-03 FIG 4. 2 L 7 2 4F A6WE 2001032600101 20010326 00101 WP 2001 3 26 AT0100096 1 20010209 A 5320 WEB DOUG DC9 DC932 3022066 WP FWD CARGO BAY DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 FOUND HOLE AT NUT PLATE IN FORWARD PIT WEB BS 370 LONG 24R. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-10-0 3, 51-10-04, 53-01 FIG 2, 53-30-02, AND REO-L00408. 2 L 7 2 4F A6WE 2001032600102 20010326 00102 WP 2001 3 26 AT0100097 1 20010208 A 5320 ANGLE DOUG DC9 DC932 3022066 WP NLG WW CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 FOUND RIGHT NOSE LANDING GEAR WHEEL WELL LOWER ANGLE CORRODED BEYOND LIMITS AT BS 109 RBL 27. INSTALLED REPAIR IAW REO- L00405. 2 L 7 2 4F A6WE 2001032600103 20010326 00103 WP 2001 3 26 AT0100098 1 20010222 A 5320 ANGLE DOUG DC9 DC932 3022066 WP FWD CARGO BAY CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 FOUND FLOOR SUPPORT ANGLE CRACKED IN FORWARD PIT AT BS 218 LONGERON 28 RIGHT. FABRICATED AND INSTALLED ANGLE SUPPORT IA W DC9 SRM 51-30, 51-10-04, 51-10-03, AND 53-21 FIG 7. 2 L 7 2 4F A6WE 2001032600104 20010326 00104 WP 2001 3 26 AT0100099 1 20010214 A 5313 LONGERON DOUG DC9 DC932 3022066 WP EE BAY CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 FOUND LONGERON IN E&E COMPARTMENT CRACKED AT BS 200 LONGERON 29 RIGHT. INSTALLED LONGERON SPLICES IAW DC9 SRM 53-02 FIG 18. 2 L 7 2 4F A6WE 2001032600105 20010326 00105 WP 2001 3 26 AT0100100 1 20010208 A 5230 SKIN DOUG DC9 DC932 3022066 WP AFT CARGO DOOR GOUGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 FOUND AFT PIT CARGO DOOR SKIN GOUGED BEYOND LIMITS. INSTALLED REPAIR DOUBLER IAW DC9 SRM 52-05 FIG 3, 52-01 FIG 1, 51-1 0-04, 51-10-02, AND 51-10-03. 2 L 7 2 4F A6WE 2001032600106 20010326 00106 WP 2001 3 26 DLL14010317 1 20010222 A 2421 IDG LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524* NE NR 2 ENGINE FAILED A DALA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 737D 193C1228 014771 DURING CLIMB NR 2 IDG LOW PRESSURE LIGHT FLICKERING. GEN DISCONNECTED, POM C/W. FOUND METAL IN NR 2 IDG CASE DRAIN AND PRESS FILTERS NR 2 IDG AND COOLER REPLACEMENT. 2 L 7 3 4F 4 F A23WE E12EU 2001032600107 20010326 00107 WP 2001 3 26 TWAA0103802 1 20010226 A 5240 SKIN DOUG DC9 DC931 3022065 WP SERVICE DOOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 992Z 47095 DURING OP 15 MAINT CHECK FOUND .1875 INCH LONG CRACK AT STA 193, UPPER AFT CORNER OF FWD SERVICE DOOR OUTER SKIN. CRACK CONFIRMED BY HIGH FREQ EDDY CURRENT PER 51-00-03, PART 6. REPAIRED PER SRM 53-05 FIG 112, DOUGLAS REWORK DRAWING SRO 9 530172, AND SRM 51-10-04. RIVETS PER SRM 51-30-02. HI-LOK PER SRM 51-30-5, AND SEALING REPAIR PER SRM 51-20-0. 2 L 7 2 4F A6WE 2001032600108 20010326 00108 NM 2001 3 26 AWXA0001463 1 20010302 A 5210 50079454 TAB BOEING 737 7373S3 1384711 NM L1 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 FWD ENTRY DOOR TORQUE TUBE COVER TAB IS CRACKED AT EACH END AT BS 328. INSTALLED REPAIR DOUBLERS IAW SRM 51-30-01 & 51- 40-02. 2 L 7 2 4F RT A16WE 2001032600109 20010326 00109 NM 2001 3 26 VNAA0102010 1 20010217 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 440JS 12133 3058 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 4 THROUGH 6 WERE NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE 5LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001032600110 20010326 00110 NM 2001 3 26 VNAA0102011 1 20010218 A 3610 4067B000002 BLEED VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE BLEED SYSTEM FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 436JS 12421 3052 AFTER CLIMB OUT, THE CREW RECEIVED A RIGHT HAND PACK OVERHEAT MESSAGE. THE CREW REFERENCED THE QUICK REFERENCE HANDBOOK THEN CONTACTED MAINTENANCE CONTROL WHO DIRECTED THEN TO RETURN TO PIT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HA ND HIGH PRESSURE BLEED VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 36-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001032600111 20010326 00111 NE 2001 3 26 VNAA0102012 2 20010220 A 7532 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE BLEED VALVE DIRTY A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 425JS 3037 AFTER TAKING THE RUNWAY THE CREW RECEIVED A RIGHT ENGINE ELECTRONIC CONTROL UNIT FAIL CAS MESSAGE. FLIGHT CREW ABORTED THE TAKEOFF. AFTER THE AIRCRAFT CLEARED THE RUNWAY THE FLIGHT CREW RESET THE ELECTRONIC CONTROL UNIT AND ANOTHER TAKEOF F ATTEMPT WAS MADE AND THE FAIL MESSAGE RETURNED. MAINTENANCE INSPECTED AND CLEANED THE INLET BLEED VALVE CONNECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 75-35-01 AND OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001032600112 20010326 00112 NM 2001 3 26 VNAA0102013 1 20010222 A 7603 250205004 LEVER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT BINDING A VNAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 07 437JS 3055 AT CRUISE ALTITUDE OF FL220 THE RIGHT CONDITION LEVER BECAME STIFF AND WOULD NOT MOVE IN EITHER DIRECTION. THE CREW RET URNED TO PIT AND MAINTENANCE REPLACED THE RIGHT CONDITIONER LEVER TELEFLEX IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 76-11-00 THE RIGHT CONDITION LEVER CHECKED GOOD. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001032600113 20010326 00113 NM 2001 3 26 VNAA0102015 1 20010222 A 6120 A5656 PUMP DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT PROPELLER FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 442JS 13407 3060 ON LANDING IN EVV THE FLIGHT CREW REPORTED A LEFT ENGINE ELECTRONIC CONTROL UNIT FAILED. MAINTENANCE INSPECTED AND CLEA NED THE CONNECTOR FOR THE ELECTRONIC CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-21-01 AND OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RETURNED TO SERVICE. UPON TAKEOFF THE LEFT HAND ELECTRONIC CONTROL UNIT FAILED AND THE TAKEOFF WAS ABORTED. MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND PROPELLOR HIGH PRESSURE PUMP IN ACCORDANC E WITH DORNIER MAINTENANCE MANUAL 61-21-01. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001032600128 20010326 00128 WP 2001 3 26 ABXA010065 1 20010227 A 3243 305323001 VALVE DOUG DC8 DC863 302198A WP BRAKE SYS DEFECTIVE A ABXA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 825AX 6467 46115 THE LEFT MAIN LANDING GEAR WHEEL BRAKES WOULD NOT OPERATE. MAINTENANCE INSPECTED AND FOUND THE BRAKE HYDRAULIC POWER VA LVE ASSY TO HAVE A BROKEN FORK. THE POWER VALVE WAS REPLACED IAW DC-8 MM 32-42-02. 2 L 7 4 4F 4A25 2001032600129 20010326 00129 WP 2001 3 26 ABXA010077 1 20010227 A 5744 4919290503 STUD DOUG DC9 DC941 302207N WP LT TE FLAP BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 LEFT FLAP OUTBOARD FLAP HINGE FITTING, OUTBOARD LOWER SPAR ATTACH STUD WAS BROKEN. MAINTENANCE INSPECTED AND REPLACD 4 OUTBD FLAP HINGE STUDS IAW DC-9 MM 57-118, 57-40-01 AND SERVICE SKETCH 2673. 2 L 7 2 4F A6WE 2001032600135 20010326 00135 WP 2001 3 26 ABXA010076 1 20010228 A 5312 591746313 BULKHEAD DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 972AX 47631 UPPER CORNER OF AFT PRESSURE BULKHEAD DOOR JAMB WAS CRACKED ON LEFT SIDE. MAINTENANCE INSPECTED AND REPAIRED THE CRACKE D AREA IAW DC-9 SRM 53-05 FIG 30. 2 L 7 2 4F A6WE 2001032600136 20010326 00136 WP 2001 3 26 ABXA010074 1 20010228 A 5311 99115056 FRAME DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 972AX 47631 FUSELAGE FRAME (P/N 9911505-6) AT FUSELAGE STATION 83.5 WAS CRACKED. MAINTENANCE INSPECTED AND REPAIRED FRAME IAW DC-9 SRM 53-03 FIG 34. 2 L 7 2 4F A6WE 2001032600137 20010326 00137 WP 2001 3 26 ABXA010073 1 20010228 A 5320 99578608 ANGLE DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 972AX 47631 ANGLE (P/N 9957860-8) AT FUSELAGE STATION 83.5 WAS CRACKED. MAINTENANCE INSPECTED AND REPAIRED THE ANGLE IAW DC-9 SRM 5 1-03 FIG 34. 2 L 7 2 4F A6WE 2001032600138 20010326 00138 WP 2001 3 26 ABXA010068 1 20010228 A 5330 5924872 SKIN DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 972AX 47631 FUSELAGE SKIN AT STATION 851 BELOW LONGERON 20L WAS CORRODED. MAINTENANCE INSPECTED AND REPLACED THE CORRODED SKIN IAW DC-9 SRM. 2 L 7 2 4F A6WE 2001032600145 20010326 00145 NM 2001 3 26 AWXA0001422 1 20010227 A 5320 65C31240 SUPPORT FITTING BOEING 737 7373S3 1384711 NM AFT CARGO BAY CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 AFT CARGO COMPARTMENT RT SIDEWALL PANEL FWD OF CARGO DOOR CRACKED AT STA 787 STR 25R. CUT OUT DAMAGED SECTION OF DOUBLE R IAW SRM 51-70-13; FABED REPAIR PARTS IAW SRM 51-70-13 (PLATE AND FILLER); TREATED AND PRIMED PARTS IAW 51-20-01; INSTA LLED PARTS IAW 51-40-02; HFEC B737 NTM PT 6 ON FIG 23. NO CRACKS NOTED. 2 L 7 2 4F RT A16WE 2001032600148 20010326 00148 SO 2001 3 26 C2XA01IA127 1 20010222 A 3260 922AA2YA6PZ722 SENSOR EMB 120 EMB120ER 3260203 SO RT MLG OUT OF ADJ A C2XA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 27 15725 120173 SHV - FLIGHT 3443, THE CREW REPORTED THAT THE RIGHT MAIN LANDING GEAR WOULD NOT LOCK IN THE UP POSITION. THE AIRCRAFT D IVERTED TO SHV WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE RIGHT MAIN GEAR UPLOCK PROXIMITY SENSOR IN AC CORDANCE WITH EMB-120 M/M 32-61-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001032600153 20010326 00153 NM 2001 3 26 VNAA0103002 1 20010303 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST NR NOT REPORTED 1 GL 07 442JS 1377 3060 THE FLIGHT CREW REPORTED THAT A SECTION OF THE EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE INSPECTED AND REPLACED THE 5LK BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-00. OPERATION CHECKS WERE COMPLETED AND THE AIRCRAFT RE TURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001032600156 20010326 00156 WP 2001 3 26 MWEA010192 1 20010226 A 5320 991557110 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 MISDRILLED HOLES WITH NO PITCH DISTANCE AT INTERCOSTAL LOWER FORWARD SIDE ON LONGERON 10 LEFT, AFT OF STATION 218. REMO VED, FABRICATED AND INSTALLED INTERCOSTAL, LONGERON AND SPLICE. 2 L 7 2 4F A6WE 2001032600157 20010326 00157 WP 2001 3 26 MWEA010193 1 20010226 A 5320 9958212 CHANNEL DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 AFT CARGO BAY FORWARD PRESSURE BULKHEAD STATION 637 HORIZONTAL HAT CHANNEL UPPER AND LOWER FLANGES CRACKED, 30 INCHES AB OVE LONGERON 29 RIGHT. REMOVED, FABRICATED AND INSTALLED HAT CHANNEL. 2 L 7 2 4F A6WE 2001032600158 20010326 00158 SO 2001 3 26 C2XA01CL035 1 20010225 A 3232 14571121403 ROD EMB 135 EMB135LR SO MLG DOOR WORN A C2XA K NONE E F VIBRATION/BUFFET FLT CONT AFFECTED CL CLIMB 1 SW 27 14516 145323 LGA FLIGHT 4244 THE CREW REPORTED A VIBRATION IN FLIGHT IN THE ELEVATOR CONTROL, NOTICABLE ABOVE 250 KNOTS. THE VIBRATI ON INCREASED AS THE SPEED INCREASED. A HUMMING SOUND WAS ALSO HEARD ON THE FLIGHT DECK. MAINTENANCE INSPECTED AND FOUN D THE LEFT AND RIGHT MAIN GEAR DOORS TO HAVE EXCESS PLAY ON THE ATTACH RODS. THE DOORS APPEARED TO BE SLIGHTLY HANGING DOWN IN THE AIRSTREAM. BOTH ATTACH RODS WERE REPLACED AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS TEST FLOWN SA TISFACTORY AND RELEASED FOR SERVICE. 2 L 7 2 4F RT TOOO11AT 2001032600164 20010326 00164 NM 2001 3 26 DHL2001709002 1 20010220 A 8012 97925411 START VALVE BOEING 727 72782C 1384026 NM NR 3 ENGINE MALFUNCTIONED A DHLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 709DH 19968 NR 3 ENGINE START VALVE OPEN LIGHT ILLUMINATED ON TAXI-OUT. SHUT DOWN ENGINE AND CLOSED NR 3 BLEED. REMOVED AND REPLAC ED NR 3 ENGINE START VALVE (P/N 979254-1-1) (S/N 13835) OFF WITH (P/N 979254-1-1) (S/N P-1541) ON, PER M/M 80-11-11. OP S CHECK GOOD. 2 L 7 3 4F A3WE 2001032600168 20010326 00168 EA 2001 3 26 COMA0160283 1 20010224 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 EA CABIN DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 912CA 7011 PERFORMED A MAJOR REPAIR TO RBL 9.0 AND LBL 9.0 BY FABRICATING NEW SEAT TRACK AND INSTALLED IAW WVAC EO 601R-53-2253. 2 L 7 2 4F RT A21EA 2001032600169 20010326 00169 EA 2001 3 26 COMA0160284 1 20010223 A 5320 601R31527217 CHANNEL CNDAIR CL600 CL6002B19 EA PAX DOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 912CA 7011 AFT U-CHANNEL AT ENTRANCE OF PAX DOOR HAS MAJOR CORROSION. REMOVED, FABED, AND REPLACED U-CHANNEL IAW WVAC EO 601R-53-2 234A. 2 L 7 2 4F RT A21EA 2001032600174 20010326 00174 NM 2001 3 26 DHL2001701002 1 20010223 A 5415 SUPPORT FITTING BOEING 727 72730C 1384009 NM NR 3 ENGINE CRACKED A DHLA O OTHER O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 DURING A POST-MOD INSPECTION OF PYLON, CRACKS WERE FOUND IN FWD ENGINE SUPPORT FITTING UPPER FLANGE BOLT HOLES E AND F. REPAIRED NR 3 ENGINE PYLON AT BOLT HOLES E AND F, IAW BOEING MESSAGE CPZ-OSC-01-00017H APPROVED AS ALTERNATE MEANS OF C OMPLIANCE TO AD 97-05-08 ON 8110-3, DATED FEBRUARY 23, 2001, AND TIMCO REO S00553, REV, ORIG 02/23/01. (REFERENCE TIMCO OPS 24490). 2 L 7 3 4F A3WE 2001032600175 20010326 00175 SO 2001 3 26 C2XA01CL034 1 20010225 A 3260 852701 SENSOR EMB 135 EMB135ER 3260203 SO RT MLG FAILED A C2XA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 27 15509 145238 YYZ FLIGHT 3991 THE CREW REPORTED A AIR/GROUND MESSAGE WHILE POWERING UP THE AIRCRAFT AT THE GATE. REPORTED THE SENSORS APPEAR TO INDICATE THE AIRCRAFT WAS IN FLIGHT. MAINTENANCE REPLACED THE RIGHT MAIN GEAR AFT WOW PROXIMITY SENSOR. OPE RATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2001032600176 20010326 00176 SO 2001 3 26 C2XA01IA129 1 20010223 A 3350 1317 LIGHT EMB 145 EMB145ER SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14939 145030 IAH - FLIGHT 4230, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT SEVERAL EMERGENCY LIGHTS WERE INOPERATIVE. MAIN TENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BULBS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001032600177 20010326 00177 NM 2001 3 26 01FDEA00168 1 20010227 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM CABIN CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DURING ROUTINE INSP, NR 6 MAIN CABIN SEAT TRACK FOUND CORRODED FROM BS 850 - 870. REMOVED AND REPLACED SEAT TRACK PER I AW BAC 727 SRM 51-30-2. 2 L 7 3 4F A3WE 2001032600178 20010326 00178 NM 2001 3 26 01FDEA00117 1 20010213 A 5310 CROSSBEAM BOEING 727 72725C 138400H NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DURING ROUTINE INSP, UPPER CTR SECTION LWR CARGO COMPT LWR CHORD OF CTR CROSSBEAM BL 0 FROM BS 500 - 640 FOUND CORRODED. *S/D* REPLACED, REMOVED & FAB PER IAW BAC DRW SR 27-53-009, 727 SRM 51-30-2. 2 L 7 3 4F A3WE 2001032600179 20010326 00179 NM 2001 3 26 01FDEA00118 1 20010213 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DURING ROUTINE INSP, MAIN CABIN FLOORBEAM AT BS 950, RBL 6 FOUND CORRODED. *S/D* REMOVED, REPLACED, AND FAB PER IAW BA C 727 SRM 53-10-8. 2 L 7 3 4F A3WE 2001032600180 20010326 00180 2001 3 26 JBXA000250 4 20010227 A 3418 45150340 SENSOR CNDAIR CL600 CL6002B19 EA RT AOA MALFUNCTIONED A JBXA D RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 05 570ML 7206 STALL WARNING MESSAGE ON T/O WOULD NOT CLEAR. RETURNED TO RDU. (RT SIDE AFFECTED) ON GROUND CK MCD SPC 350 FOUND BIT 12 FAULTED. REMOVED AND REPLACED RT ANGLE OF ATTACK SENSOR IAW CRJ MM 27-35-05, OPS CK GOOD. 2 L 7 2 4F RT A21EA 2001032600181 20010326 00181 WP 2001 3 26 ARWA0010204 1 20010227 A 5312 1549334 BULKHEAD LKHEED 1011 1011385114 WP FUSELAGE CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 260FA 193A1158 DURING ROUTINE MAINTENANCE, A CRACK IN THE BULKHEAD CAP AT STATION 449.0 BETWEEN STRINGERS 40 & 41 WAS DISCOVERED. PERM ANENT REPAIR COMPLETED IAW SRM 53-11-00. 2 L 7 3 4F A23WE 2001032600182 20010326 00182 NM 2001 3 26 SABA010003 1 20010112 A 2916 RESERVOIR DHAV DHC8 DHC8103 1386005 NM HYD SYSTEM LOW A SABA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 33 801WP 086 AIRCRAFT 801 ON FLIGHT 5024 FROM CLT TO PGV. DURING THE TAKEOFF ROLL THE NUMBER 1 HYDRAULIC ISOLATION VALVE WARNING LIG HT, INBOARD SPOILER WARNING LIGHT, AND FLAP POWER WARNING LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT W AS TOWED TO THE GATE DUE THE COCKPIT PARKING BRAKE PRESSURE INDICATOR WAS DEFERRED. MAINTENANCE FOUND THE NUMBER 1 HYDR AULIC RESERVOIR LOW. THE RESERVOIR WAS SERVICED AND A LEAK CHECK PERFORMED. NO LEAKS FOUND. OPS CHECK WAS GOOD. AIRC RARFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001032600183 20010326 00183 SO 2001 3 26 C2XA01CL037 1 20010227 A 3350 1317 LIGHT EMB 145 EMB145ER SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16944 145045 DURING A ROUTINE INSPECTION MAINTENANCE FOUND THE EMERGENCY LIGHT ON THE CEILING AFT OF THE EMERGENCY EXIT WAS INOPERATI VE. MAINTENANCE REPLACED THE LIGHT BULB AND PERFORMED THE OPERATIONAL CHECKS. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001032600184 20010326 00184 NM 2001 3 26 AWXA0001423 1 20010227 A 5330 0353321054 DOUBLER BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 SMALL CRACK ON EXTERNAL SKIN DOUBLER TOP FUSELAGE SKIN AFT OF RADOME. BLENDED OUT CRACK FROM EXTERNAL DOUBLER; ALODINED , PRIMED AND GAP SEALED IAW ER 03-5332-01054. 2 L 7 2 4F RT A16WE 2001032600185 20010326 00185 2001 3 26 UPS01835114 4 20010301 A 2300 MICROPHONE DOUG DC8 DC873F 302199F WP COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:N/A PREFLIGHT- FE O2 MIC INOP. *S/D* FOUND WIRE AT CONNECTOR R50-299 BROKEN. REPAIRED, OPS CHECK OK. 2 L 7 4 4F RT 4A25 2001032600186 20010326 00186 WP 2001 3 26 UPS01835116 1 20010301 A 3230 LANDING GEAR DOUG DC8 DC871F 302199D WP MLG FAILED A IPXA K NONE J WARNING INDICATION CL CLIMB 1 SO 01 701UP 45938 INSPECTION TYPE:N/A, AFTER TAKEOFF MLG FAILED TO RETRACT. MAINTAINED AIRSPEED BELOW 230 KTS AND CLIMBED TO 15000 FT. P ERFORMED GEAR HANDLE JAMMED CHECKLIST ON DESCENT TO PHL BELOW 10000 FT NOSE GEAR POSITION APPEARED. AIRCRAFT FERRY PERM IT DMI CONTROL NR D210467 COMPLIED WITH AIRCRAFT IN SAFE CONDITION FOR FERRY A/C ARRIVED SAFELY 8:30 PM THIS CLEARS D-2 10467 ITEM. 2 L 7 4 4F RT 4A25 2001032600198 20010326 00198 EU 2001 3 26 AWXA0001451 1 20010301 A 2612 782702 FIRE LOOP AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NR 2 ENGINE CHAFED A AWXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 631AW 077 V0035 PHX - AIR TURNBACK - 2/22/01 - DURING CLIMB THE CREW GOT A CLASS I ECAM MESSAGE, ENG 2 FIRE DET FAULT AND RETURNED TO PH X. IN PHX MAINTENANCE FOUND THE NR 2 ENG LOWER CORE FIRE LOOP CHAFED; THE LOWER CORE FIRE DETECTOR ASSY WAS REPLACED AN D FUNCTIONALLY CHECKED GOOD. 2 L 7 2 4F 4 F RT A28NM E311NE 2001032600199 20010326 00199 EU 2001 3 26 AWXA0001452 1 20010301 A 3830 LINE AIRBUS 320 A320231 3930325 EU LAVATORY CLOGGED A AWXA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 28 640AW 448 LAS - AIR TURNBACK - 2/22/01 - ALL LAVS WOULD NOT FLUSH (CIDS PANEL RED LIGHT WAS ON, WASTE AT 0 PERCENT FULL, WATER AT 40 PERCENT FULL); AIRCRAFT DESTINATION WAS JFK SO THE FLIGHT RETURNED TO LAS. THE LAV SYSTEM HAD PREVIOUSLY BEEN PLACED ON MEL 38-30-01 FOR THE VAC GENERATOR INOP. HOWEVER THE SYSTEM FAILED TO FLUSH USING DIFFERENT DIFFERENTIAL PRESSURE A T ALTITUDE. IN LAS MAINTENANCE FOUND THE WASTE LINE CLOGGED AT THE LAV WASTE TANK; THE LINE WAS DISCONNECTED AND CLEANE D OUT; AFTER CLEANING THE SYSTEM FUNCTIONALLY CHECKED GOOD. 2 L 7 2 4F RT A28NM 2001032600208 20010326 00208 NM 2001 3 26 UPS01235061 1 20010223 A 3350 PLATE BOEING 727 72725C 138400H NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:N/A, FWD L1 EMERGENCY EXIT ID AND PLATE IS INOPERATIVE DUE TO EMERGENCY LIGHT TEST INOP ON FWD L1 DOOR. REMOVED AND REPLACED BASE EXIT ID AND PLATE ON L1 DOOR. 2 L 7 3 4F A3WE 2001032600209 20010326 00209 NM 2001 3 26 2001UALA00117 1 20010214 A 3350 LIGHT BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN MALFUNCTIONED A UALA K NONE O OTHER CR CRUISE 1 WP 29 617UA 21877 EMERGENCY EXIT LIGHTS ON DURING CRUISE WITH COCKPIT SWITCH IN ARMED POSITION. RECYCLED SWITCH PER LHRLM.SUPPLEMENTAL DA TA UPDATE ACCOMPLISHED EMERGENCY LIGHTS OP CHECK, OPS CHECK GOOD. OBSERVED LIGHTS FOR SEVERAL HOURS WITH NO PROBLEMS NO TED 2 L 7 2 4F 4 F RT A1NM E3NE 2001032600213 20010326 00213 WP 2001 3 26 ABXA010080 1 20010131 A 5330 577992549 SKIN DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AX 46126 EXTERNAL FUSELAGE AT STATION 110 L36 WAS FOUND TO HAVE BULGING SKIN NEAR FLAPPER VALVE. MAINTENANCE INSPECTED AND REPAI RED THE AREA IAW ABX REA D853-39745-MR AND DC-8 SRM 51-1-21. 2 L 7 4 4F 4A25 2001032600215 20010326 00215 NM 2001 3 26 UPS01235068 1 20010223 A 3350 BATTERY BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:N/A, REAR EXIT CEILING EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED REAR EXIT CEILING EMERGENCY LI GHT BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD. 2 L 7 3 4F A3WE 2001032600216 20010326 00216 NM 2001 3 26 UPS01235077 1 20010223 A 3350 BATTERY BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:IN, FWD PAY DOOR LOWER FLOOR EMERGENCY LIGHT IS OUT. REMOVED AND REPLACED BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD. 2 L 7 3 4F A3WE 2001032600217 20010326 00217 WP 2001 3 26 IXXA0100008 1 20010227 A 3232 ROD DOUG DC8 DC871F 302199D WP NLG MALFUNCTIONED A IXXA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 11 828BX 77934 778 45993 EN ROUTE FORM LRD TO TOL, WHEN THE LANDING GEAR WAS RETRACTED THE FLIGHT CREW NOTICE A VIBRATION IN THE NOSE OF THE AIRC RAFT. THE FLIGHT CREW CYCLED THE LANDING GEAR BUT THE VIBRATION REMAINED PRESENT. THE AIRCRAFT RETURN TO LRD FOR AN UN EVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED THE LEFT NOSE LANDING GEAR DOOR OPEN. MAINTENANCE CLEANED, LUBRICATED AND SECURED THE TELESCOPING DOOR ROD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2001032600218 20010326 00218 WP 2001 3 26 IXXA0100009 1 20010302 A 3297 WIRE DOUG DC8 DC871F 302199D WP COCKPIT BROKEN A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 826BX 82852 740 45998 EN ROUTE FOR JFK TO TOL, THE GEAR DOOR WARNING LIGHT REMAINED ON DIM AFTER GEAR RETRACTION. THE FLIGHT CREW CYCLED THE LANDING GEAR AND THE WARNING LIGHT EXTINGUISHED. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE IN SPECTED THE AIRCRAFT LOCATING A BROKEN WIRE LOCATED AT THE INSTRUMENT DIMMING CONTROL BOX. MAINTENANCE REPAIRED THE WIR E A PERFORMED A SUCCESSFUL OPERATION CHECK IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERV ICE. 2 L 7 4 4F RT 4A25 2001032600219 20010326 00219 WP 2001 3 26 ABXA010071 1 20010302 A 2161 60714622 CONTROLLER DOUG DC9 DC931 3022065 WP COCKPIT DEFECTIVE A ABXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 946AX 80000 47003 A HOT DUCT ODOR WAS NOTED FROM THE RIGHT AIR CONDITIONING SYSTEM. THE TEMPERATURE OF THE RIGHT AIR CONDITIONING PACK WA S NOTED TO BE 150 DEGREES. BY REDUCING THE TEMPERATURE SETTING, THE TEMPERATURE DECREASED. THE AIRCRAFT RETURNED TO TH E FIELD. MAINTENANCE INSPECTED AND DEFERRED THE RIGHT AIR CONDITIONING SYSTEM AND RETURNED THE AIRCRAFT TO SERVICE. ON 02/03/01 MAINTENANCE INSPECTED AND REPLACED THE RIGHT AUTO TEMP CONTROLLER IAW DC9 MM 21-60-00. 2 L 7 2 4F A6WE 2001032600220 20010326 00220 WP 2001 3 26 MWEA010184 1 20010226 A 5311 SR095300953 FRAME DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 OPEN HOLES AND FASTENERS IMPROPERLY INSTALLED ON FRAME STATION 218 BETWEEN LONGERON 5 RIGHT AND 6 RIGHT. REMOVED DAMAGE , FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F A6WE 2001032600228 20010326 00228 SO 2001 3 26 SWIA972390 1 20010222 A 7712 INDICATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 234SW 120308 AFTER TAKEOFF LEFT ANALOG REACHED ONLY 80 PERCENT TORQUE WHILE DIGITAL 100 PERCENT, T6 650, LEFT YAW AND POWER LEVER SPL IT 1 - .5 INCH. RETURNED TO ONT. PERFORMED EEC RUNS IAW 73-21-00. RE-TRIMMED ENGINE AS NEEDED. OK FOR RETURN TO SERV ICE. ALL OTHER INDICATION/FUNCTION OK. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032600233 20010326 00233 WP 2001 3 26 TWAA0103607 1 20010221 A 5311 FORMER DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT FOUND CORROSION ON FORMER AT STA 1308 AT LONGERON 28L TO 28R. CUT OUT CORROSION. INSTALLED NEW FO RMER SECTION LONGERON 28L TO 28R AND REPAIRS PER SRM 53-03, PAGE 4A. PAINTED AND TREATED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001032600234 20010326 00234 NM 2001 3 26 SWAA010591 1 20010226 A 2121 215201 GASPER FAN BOEING 737 7373H4 1384600 NM CABIN DEFECTIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 394SW 27380 SMOKE ODOR IN CABIN. GASPER AND RECIRCULATION FAN TURNED OFF AND ODOR WENT AWAY. ODOR STRONGEST AT MID CABIN. REMOVED AND REPLACED GASPER FAN MOTOR ASSY PER MM. 2 L 7 2 4F RT A16WE 2001032600246 20010326 00246 NM 2001 3 26 DL76L010329 1 20010225 A 3350 012206548 FUSE BOEING 767 767332 1382001 NM CABIN BLOWN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 188DN 27583 SEAT ROW 22 TO 28 BOTH SIDES EMERGENCY SEAT LIGHTS OUT. REPLACE FUSE IN BATT PACK M9009. NOW CKS GOOD. 2 L 7 2 4F RT A1NM 2001032600247 20010326 00247 NM 2001 3 26 AWXA0001429 1 20010301 A 5230 AND101361604 SKIN BOEING 737 737277 1384570 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 AFT CARGO DOOR INNER SKIN HAS A 1 INCH CRACK AT LIGHTENING HOLE BELOW HANDLE MECHANISM. STOP DRILLED CRACK; FABED, DRIL LED, TREATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-02, 51-10-01, 51-30-01. 2 L 7 2 4F RT A16WE 2001032600248 20010326 00248 NM 2001 3 26 AWXA0001432 1 20010301 A 5320 653535214 STRINGER CLIP BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 STRINGER CLIP AT FS 807, STRINGER 3L IS CRACKED. REMOVED AND REPLACED CLIP IAW SRM 51-30-01 PG 5. 2 L 7 2 4F RT A16WE 2001032600259 20010326 00259 NM 2001 3 26 PCAA0102010 1 20010225 A 3320 BV0330012150 SOCKET DHAV DHC8 DHC8102 2809003 NM CABIN BURNED A PCAA K NONE A FLAME/FIRE UK UNKNOWN 1 EA 13 839EX 226 DTW FLIGHT 3529. CREW REPORTED SMOKE AND FLAME COMING FROM OVERHEAD LIGHT 8 AC. CONTRACTED MAINTENANCE INSPECTED AND C ONFIRMED LIGHT SOCKET AT ROW 8AC OVERHEAD AT FAULT, LIGHT SOCKET ISOLATED. MAINTENANCE CONTROL ISSUED MEL 33-02. AIRCR AFT SCHEDULED TO BGM MAINTENANCE THAT NIGHT, LIGHT SOCKET AND BULB REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001032600260 20010326 00260 EU 2001 3 26 RAIA00102007 1 20010224 A 2913 NTA152506 O-RING AEROSP ATR42 ATR42300 8680920 EU HYD PUMP LEAKING A RAIA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 CE 03 426TE 228 7145-MEM- CREW REPORTS LOSS OF BLUE SYSTEM HYDRAULIC PRESSURE ON DESCENT. MAINTENANCE INSPECTED AND REPLACED O-RING SEA L AT BLUE SYSTEM HYDRAULIC PUMP. 2 H 7 2 4T RT A53EU 2001032600261 20010326 00261 2001 3 26 RAIA00102008 4 20010225 A 3425 7003110901 TUBE JETAIR JETSTM JETSTM4101 1500501 EU INSTRUMENT PNL INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 553HK 11018 2735 41066 5367-EWR- RIGHT INSTRUMENT PANEL LOWER EFIS TUBE IS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED RIGHT INSTRUMENT PA NEL LOWER EFIS TUBE. 2 L 7 2 4T RT A41NM 2001032600262 20010326 00262 NM 2001 3 26 UPS01235059 1 20010223 A 3350 BATTERY BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:N/A, ON EMERGENCY EXIT LIGHT TEST THE FOLLOWING LIGHTS FAILED MED EXIT MARKERS, RT GALLEY EXIT MARKER AN D 2 GALLEY EXIT LOCATORS. REPLACED EMERGENCY EXIT BATTERIES PACKS, TESTED OK. 2 L 7 3 4F A3WE 2001032600263 20010326 00263 NM 2001 3 26 UPS01235060 1 20010223 A 3350 TRANSMITTER BOEING 727 72725C 138400H NM L1 DOOR INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:N/A, FWD L1 DOOR EMERGENCY BATTERY LIGHT DOES NOT TEST ON GROUND. REMOVED AND REPLACED TRANSMITTER, OPS CK GOOD. 2 L 7 3 4F A3WE 2001032600264 20010326 00264 NM 2001 3 26 UPS01235064 1 20010223 A 3350 BATTERY BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:IN ROW 4 SEAT 4 EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED ROW 4 EMERGENCY LIGHT BATTERY ASSY PE R MM 33-50-22. OPS CHECKS GOOD. 2 L 7 3 4F A3WE 2001032600265 20010326 00265 NM 2001 3 26 UPS01235065 1 20010223 A 3350 BATTERY BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:IN ROW 9 LEFT SEAT EMERGENCY LIGHT TEST. REMOVED AND REPLACED ROW 9 SEAT EMERGENCY LIGHT BATTERY ASSY P ER MM 33-50-22. OPS CHECKS GOOD. 2 L 7 3 4F A3WE 2001032600266 20010326 00266 NM 2001 3 26 UPS01235066 1 20010223 A 3350 BATTERY BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:N/A, ROW 19 LEFT SEAT EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED ROW 19 EMERGENCY LIGHT BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD. 2 L 7 3 4F A3WE 2001032600267 20010326 00267 NM 2001 3 26 UPS01235067 1 20010223 A 3350 BATTERY BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:N/A, FORWARD ENTRY WAY CEILING EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED FWD ENTRY WAY CEILING EMERGENCY EXIT LIGHT BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD. 2 L 7 3 4F A3WE 2001032600276 20010326 00276 WP 2001 3 26 UPS01835034 1 20010222 A 5350 FAIRING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:N/A, LEFT (CENTER FUESLAGE) PANEL CRACKED AND DELAMINATED JUST FWD OF LEFT MAIN GEAR DOOR. REMOVED PANE L. *S/D* REINSTALLED SERVICEABLE ADF PANEL PER 34-51-01. 2 L 7 4 4F RT 4A25 2001032600294 20010326 00294 NM 2001 3 26 UPS01235184 1 20010303 A 2510 SEAT BOEING 727 72722C 138400F NM COCKPIT DEFECTIVE A IPXA K NONE O OTHER UK UNKNOWN 1 SO 01 942UP 19101 INSPECTION TYPE:N/A, CAPT''S SEAT W/N LOCK INTO POSITION. CLEANED AND LUBED HORIZONTAL MECHANISM ON CAPT''S SEAT O/C IA W M/M 25-10-42. SEAT CHECKS OK. 2 L 7 3 4F A3WE 2001032600295 20010326 00295 WP 2001 3 26 ABXA010078 1 20010301 A 5250 AR25291GR41 LATCH DOUG DC8 DC861 3021952 WP FUSELAGE INOPERATIVE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 842AX 46015 AT EWR THE COCKPIT ENTRY DOOR LATCH WAS FOUND TO BE INOPERATIVE DURING PREFLIGHT INSPECTION. MAINTENANCE COMPLIED WITH ABX REA D852-40152 AND RETURNED THE AIRCRAFT TO SERVICE. AT ILN MAINTENANCE INSPECTED AND REPLACED THE COCKPIT ENTRY DO OR LATCH ASSY. 2 L 7 4 4F 4A25 2001032600296 20010326 00296 NM 2001 3 26 UPS01235069 1 20010223 A 3350 BATTERY BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:N/A, AFT LEFT LAV LOWER EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD. 2 L 7 3 4F A3WE 2001032600297 20010326 00297 NM 2001 3 26 UPS01235070 1 20010223 A 3350 BATTERY BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:IN, LEFT LOWER FLOOR EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED BATTERY ASSY PER MM 33-50-22. O PS CHECKS GOOD. 2 L 7 3 4F A3WE 2001032600298 20010326 00298 NM 2001 3 26 UPS01235071 1 20010223 A 3350 BATTERY BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:IN RT FWD OVERWING EXIT LIGHT FAILED TEST. REMOVED AND REPLACED BATTERY ASSY PER MM 33-50-22. OPS CHEC KS GOOD. 2 L 7 3 4F A3WE 2001032600299 20010326 00299 NM 2001 3 26 UPS01235072 1 20010223 A 3350 BATTERY BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:N/A, RT CEILING OVERWING EMERGENCY LIGHT FAILED. REMOVED AND REPLACED BATTERY ASSY PER MM 33-50-22. OP S CHECKS GOOD. 2 L 7 3 4F A3WE 2001032600300 20010326 00300 NM 2001 3 26 UPS01235075 1 20010223 A 3350 BATTERY BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:N/A, RIGHT FWD OVERWING FLOOR EMERGENCY LIGHT FAILED TO TEST. REMOVED AND REPLACED BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD. 2 L 7 3 4F A3WE 2001032600301 20010326 00301 NM 2001 3 26 UPS01235079 1 20010223 A 3350 BATTERY BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:IN, FWD BULKHEAD EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED BATTERY ASSY PER MM 33-50-22. OPS C HECKS GOOD. 2 L 7 3 4F A3WE 2001032600302 20010326 00302 NM 2001 3 26 UPS01235080 1 20010222 A 3231 DOOR BOEING 727 727108C 1384039 NM MLG INOPERATIVE A IPXA K NONE J WARNING INDICATION CL CLIMB 1 SO 01 936UP 19503 INSPECTION TYPE:N/A, UPON PLACING GEAR HANDLE IN OFF POSITION AFTER T/O RED DOOR LIGHT ON FROM PANEL AND RIGHT MAIN GEAR DOOR LIGHT ON S/O PANEL ILLUMINATED. GEAR WAS CYCLED, SAME INDICATIONS AGAIN OCURRED WHEN GEAR HANDLE WAS PLACED IN OF F POSITION. *S/D* OK TO FLY ON REVENUE TO CAE FROM PHL AS PER EO B727-1245B-DISSUED D. A/C MUST FLY WITH GEAR HANDLE IN UP POSITION AT ALL TIMES. NO FURTHER ACTION IS REQUIRED. 2 L 7 3 4F A3WE 2001032600303 20010326 00303 WP 2001 3 26 UPS01835044 1 20010124 A 5320 SPLICE PLATE DOUG DC8 DC873F 302199F WP AFT CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, AFT PIT LONGERON 36 SPLICE PLATE CORRODED AT FS 1270. REMOVED CORROSION IAW DC8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. LOCATED AND DRILLED IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001032600304 20010326 00304 WP 2001 3 26 UPS01835045 1 20010124 A 5320 FITTING DOUG DC8 DC873F 302199F WP AFT CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, AFT LWR CARGO PIT AT FS 1150 - 1160 AT LONG 33R Z-FITTING IS CRACKED. REMOVED CRACKED Z-FITTING, BACK UP FITTING DOOR JAMB FITTING AND ANGLE SPLICE. LOCATED AND DRILLED, DEBURRED NEW Z-FITTING INSTALLED NEW Z-FITTING BACK UP FITTING DOOR JAMB FITTING AND ANGLE SPLICE. 2 L 7 4 4F RT 4A25 2001032600305 20010326 00305 WP 2001 3 26 UPS01835047 1 20010126 A 5320 FITTING DOUG DC8 DC873F 302199F WP FWD CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, FWD LWR CARGO PIT AT FS 340 - 350 INSIDE X-SLIDE DOOR AFT TORQUE BOX AT LONG 34R - 35R FITTING IS CORRODED. REMOVED CORROSION OUT OF LIMITS IAW DC8 SRM 51-1-8. REMOVED AND REPLACED FITTING IAW 51-1-20D DC8 SRM. 2 L 7 4 4F RT 4A25 2001032600306 20010326 00306 WP 2001 3 26 UPS01835049 1 20010124 A 5320 FITTING DOUG DC8 DC873F 302199F WP AFT CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, AFT LWR CARGO PIT AT FS 1200 BETWEEN LONG 27L-28L Z-FITTING IS CRACKED. REMOVED AND REPLACED FITT ING. ALODINED AND PRIMED SPLICE IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-20. 2 L 7 4 4F RT 4A25 2001032600307 20010326 00307 WP 2001 3 26 UPS01835050 1 20010125 A 5320 SPLICE DOUG DC8 DC873F 302199F WP AFT CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, AFT LWR CARGO PIT AT FS 1040 - 1060 LONG 35L IS CRACKED AT SPLICE FITTING. REMOVED AND REPLACED S PLICE FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001032600308 20010326 00308 WP 2001 3 26 UPS01835051 1 20010130 A 5320 GUSSET DOUG DC8 DC873F 302199F WP AFT CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, AFT PIT FS 1240 GUSSET AT L35R CRACKED. REMOVED DAMAGED GUSSET, FABRICATED NEW GUSSET IAW DAC DWG 9754949. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. GUSSET TO BE INSTALLED ON UPS NR 304036 TIMCO NR 21036. 2 L 7 4 4F RT 4A25 2001032600309 20010326 00309 WP 2001 3 26 UPS01835052 1 20010125 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, MAIN CABIN L21RT SHORT FRAME TO CUSP FITTING CRACKED AT FS 1170. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 2001032600310 20010326 00310 WP 2001 3 26 UPS01835053 1 20010131 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, FS 1800 L28R LONG DOUBLER CORRODED. DRILLED NEW DOUBLER PER DC8 SRM 53-5-3. ALODINED AND PRIMED PER DC8 SRM 51-1-8. INSTALLED PER DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001032600312 20010326 00312 WP 2001 3 26 UPS01835054 1 20010126 A 5320 FITTING DOUG DC8 DC873F 302199F WP AFT CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, AFT PTI Z-FITTING CRACK AT STA 1220 BETWEEN L30L AND L29L IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 S RM 51-1-20. REMOVED AND REPLACED FITTING. ALODINED AND PRIMED SPLICE IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-2 0. 2 L 7 4 4F RT 4A25 2001032600313 20010326 00313 WP 2001 3 26 UPS01835056 1 20010201 A 5343 SUPPORT FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, TAIL SKID SUPPORT FITTING CRACKED AT FS 1753 LONG 36. REMOVED AND REPLACED FITTING IAW DC8 SRM 51 -1-20D AND DAC DWG 375086 5. 2 L 7 4 4F RT 4A25 2001032600314 20010326 00314 WP 2001 3 26 UPS01835057 1 20010129 A 5320 GUSSET DOUG DC8 DC873F 302199F WP AFTCARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, AFT PIT FS 1050 GUSSET L31L CRACKED. REMOVED AND REPLACED GUSSET IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001032600315 20010326 00315 2001 3 26 UPS01835062 4 20010224 A 2565 BOTTLE DOUG DC8 DC871F 302199D WP ESCAPE SLIDE DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE:IN, CABIN DOOR EMERGENCY SLIDE BOTTLE PRESS LOW. REMOVED AND REPLACED CABIN DOOR EMERGENCY SLIDE AS PER MM 25-60-00. 2 L 7 4 4F RT 4A25 2001032600316 20010326 00316 2001 3 26 UPS01835081 4 20010225 A 2561 LIFE VEST DOUG DC8 DC873F 302199F WP CABIN TORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:PFLT, 2ND COURIER SEAT LIFE VEST BAG TORN. INSTALLED NEW LIFE VEST. 2 L 7 4 4F RT 4A25 2001032600317 20010326 00317 WP 2001 3 26 UPS01835082 1 20010224 A 2560 SEAL DOUG DC8 DC873F 302199F WP FIRST AID KIT MISSING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:PLFT, FIRST AID KIT MISSING SEAL. REMOVED AND REPLACED FIRST AID KIT. 2 L 7 4 4F RT 4A25 2001032600318 20010326 00318 SO 2001 3 26 COMA0110037 1 20010223 A 5310 12034416002 SHEAR TIE EMB 120 EMB120RT SO FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 269CA 2197 120263 DURING A 400 FLIGHT CYCLE CHECK, A CRACKED RIVET HEAD WAS DISCOVERED ON THE RIGHT SIDE OF AIRCRAFT FUSELAGE ALONG FRAME 9. UPON FURTHER INVESTIGATION, THE SKIN SUPPORT BRACKET IN WHICH SAID RIVET PASSES THROUGH WAS FOUND TO BE CRACKED. TH E SUPPORT BRACKET WAS REMOVED AND A SERVICEABLE BRACKET WAS INSTALLED. WORK WAS COMPLETED IN ACCORDANCE WITH AERODESIGN REPORT 660-1, IR DATED 2-16-93. 2 L 7 2 4T RT A31SO 2001032600319 20010326 00319 WP 2001 3 26 MWEA010178 1 20010226 A 5320 2913044505 GUSSET DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 OPEN HOLE AND RIVET WITH NO ED ON GUSSET AT STATION 218, LONGERON 9 LEFT. REMOVED, FABRICATED AND INSTALLED GUSSET. 2 L 7 2 4F A6WE 2001032600320 20010326 00320 WP 2001 3 26 MWEA010179 1 20010226 A 5320 49146812 FITTING DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 STATION 566 LEFT SIDE AT LONGERON 15 HAS A CRACKED FITTING COMMON TO 566 FRAME AND SKIN. REMOVED AND REPLACED FITTING. 2 L 7 2 4F A6WE 2001032600321 20010326 00321 WP 2001 3 26 MWEA010180 1 20010226 A 5313 27779223 LONGERON DOUG DC9 DC914 3022034 WP FUSELAGE BULGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 SMALL BULGE IN THE BOTTOM OF LONGERON 30 IN THE E&E COMPARTMENT. IMMEDIATELY FORWARD OF THE E&E DOOR. REMOVED AND REPLA CED LONGERON. 2 L 7 2 4F A6WE 2001032600322 20010326 00322 WP 2001 3 26 MWEA010181 1 20010226 A 5311 9919619501 FRAME DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 DURING COMPLIANCE OF CARD 9035 PCI 9151 AND WATCH ITEMS -03796 AND 02616 FOUND ON AIRCRAFT LEFT SIDE FRAME FS 623 HAS AN EXISTING CRACK 2.75 INCH AT LOWER INBOARD FLANGE AT PTH CRACK HAS NOW GROWN INTO PTE AREA IN LOWER POCKET APPROXIMATELY 3.3125 INCH (2.25 INCH HORIZONTAL, 1.0625 INCH VERTICAL) VERIFIED BY HEC. REMOVED AND REPLACED FRAME. 2 L 7 2 4F A6WE 2001032600323 20010326 00323 WP 2001 3 26 MWEA010185 1 20010226 A 5311 SR095300953 FRAME DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 HOLES WITH NO EDGE DISTANCE AT FRAME STATION 218, BETWEEN LONGERON 9 LEFT AND LONGERON 10 LEFT. FABRICATED AND INSTALLE D REPAIR ANGLE. 2 L 7 2 4F A6WE 2001032600324 20010326 00324 WP 2001 3 26 MWEA010186 1 20010226 A 5311 59125261 FRAME DOUG DC9 DC914 3022034 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 ELONGATED FASTENER HOLE, STATION 718, LONGERON 9 LEFT. DAMAGE FOUND ON FRAME. FABRICATED AND INSTALLED REPAIR ANGLE. 2 L 7 2 4F A6WE 2001032600325 20010326 00325 WP 2001 3 26 MWEA010188 1 20010226 A 5320 99576774 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FASTENER HOLES OPEN, STATION 406, LONGERON 8 LEFT. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001032600326 20010326 00326 WP 2001 3 26 MWEA010189 1 20010226 A 5311 99577393 FRAME DOUG DC9 DC914 3022034 WP FUSELAGE TOOL DAMAGE A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 STATION 766, FROM LONGERON 13 RIGHT TO LONGERON 17 RIGHT, DRILL DAMAGE. TWENTY-ONE LOCATIONS, OUTBOARD FACE OF FRAME. REMOVED, FABRICATED AND INSTALLED FRAME, FORMER AND BRACKET. 2 L 7 2 4F A6WE 2001032600330 20010326 00330 WP 2001 3 26 MWEA010182 1 20010226 A 5313 5911421421 LONGERON DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 LONGERON 5 RIGHT CRACKED AT FASTENER HOLES APPROXIMATELY STATION 776. REMOVED, FABRICATED AND INSTALLED LONGERON. 2 L 7 2 4F A6WE 2001032600331 20010326 00331 WP 2001 3 26 MWEA010183 1 20010226 A 5313 5911415459 LONGERON DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 CRACK IN LONGERON 2 RIGHT AT STATION 566. REMOVED, FABRICATED AND INSTALLED LONGERON SPLICE REPAIR. 2 L 7 2 4F A6WE 2001032600332 20010326 00332 WP 2001 3 26 MWEA010187 1 20010226 A 5313 5911415413 LONGERON DOUG DC9 DC914 3022034 WP FUSELAGE TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 TOOL DAMAGE IN RADIUS ON LONGERON 8 RIGHT, STATION 556. REMOVED, FABRICATED AND INSTALLED LONGERON SPLICE REPAIR. 2 L 7 2 4F A6WE 2001032600333 20010326 00333 WP 2001 3 26 MWEA010190 1 20010226 A 5330 99581561 SKIN DOUG DC9 DC914 3022034 WP FUSELAGE TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FUSELAGE SKIN AT STATION 480 BELOW LONGERON 11 LEFT HAS A TOOLING MARK. REMOVED, REPLACED AND INSTALLED PANEL. 2 L 7 2 4F A6WE 2001032600334 20010326 00334 WP 2001 3 26 UPS01835182 1 20010224 A 5310 SHEAR TIE DOUG DC8 DC873F 302199F WP FWD CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C2,3, STA 360 SHEAR TIE IS CRACKED BETWEEN LONG 31L TO 32L. REPAIRED SHEAR TIE IAW SRM 53-2-0 FIG 2A. 2 L 7 4 4F RT 4A25 2001032600335 20010326 00335 WP 2001 3 26 UPS01835187 1 20010301 A 2170 SEPARATOR DOUG DC8 DC871F 302199D WP AC BAY MALFUNCTIONED A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 730UP 46030 INSPECTION TYPE:IN FUMES IN C/P DURING ENTIRE FLIGHT, SEEM TO BE COMING FROM EITHER PACK. ON GROUND FOUND R PACK EMITTI NG ODOR. DER R PACK PER MEL 21-38-1. PERF MAINTENANCE PROCEDURES. M 210419 ASSIGNED PLACARDS INSTALLED. REMOVED AND R EPLACED RT WATER SEPARATOR IAW 21-55-03. PERFORMED ADJUSTMENT AND TEST IAW 21-55-00. ALL CHECK GOOD. 2 L 7 4 4F RT 4A25 2001032600342 20010326 00342 WP 2001 3 26 MWEA010191 1 20010226 A 5313 39132142 LONGERON DOUG DC9 DC914 3022034 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 LEG OF LONGERON BLENDED BEYOND LIMITS, LONGERON 15 RIGHT, STATION 758. REMOVED, FABRICATED AND INSTALLED SPLICE AND NEW LONGERON. 2 L 7 2 4F A6WE 2001032600343 20010326 00343 2001 3 26 RAIA00102009 4 20010223 A 3140 350A52005009 COMPUTER AEROSP ATR72 ATR72202 8680940 EU EE BAY FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 721TE 10259 1700 217 7006-SGF- DURING TAXI CREW REPORTED NO TRIM INDICATION, NO FLAP INDICATION, AIRSPEED INDICATOR FLAGGED, FLIGHT CONTROL F AULT, NO TRIM WOOLER, ELECTRIC SMOKE CAPTION ILLUMINATED WITH ASSOCIATED SMELL. MAINTENANCE INSPECTED AND REPLACED MFC COMPUTER. 2 H 7 2 4T RT A53EU 2001032600344 20010326 00344 WP 2001 3 26 TWAA0103601 1 20010223 A 2730 ELEVATOR DOUG DC9 DC983 3022083 WP TAIL JAMMED A TWAA D RETURN TO BLOCK F FLT CONT AFFECTED IN INSP/MAINT 1 CE 05 9406W 53126 DURING FLIGHT CONTROL CHECK FOLLOWING FWD MOVEMENT OF ELEVATOR, SUBSEQUENT REARWARD MOVEMENT JAMMED CONTROL COLUMN IN NE UTRAL POSITION ONLY ALLOWING THE CONTROL COLUMN TO BE MOVED FORWARD AGAIN. ACCOMPLISHED EXTENSIVE CHECKS OF CABLES, LIN KAGE, PULLEYS, CONTROL COLUMN, ETC. LUBED ALL APPLICABLE AREAS AND PERFORMED NUMEROUS CONTROL CHECKS. CHECK-C 1-22-01 JFK. 2 L 7 2 4F RT A6WE 2001032600345 20010326 00345 NM 2001 3 26 PCAA0103014 1 20010302 A 3350 MS274081A SWITCH DHAV DHC8 DHC8102 2809003 NM FA PANEL MALFUNCTIONED A PCAA K NONE O OTHER NR NOT REPORTED 1 EA 13 830EX 155 PHL FLIGHT 3800. CREW REPORTED CABIN EMERGENCY LIGHTS FLASHING ON AND OFF. PHL MAINTENANCE REPLACED RELAY 2431-K14 AND 15. ALSO REPLACED EMERGENCY LIGHTS SWITCH. OPERATIONAL CHECK GOOD.AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001032600349 20010326 00349 NM 2001 3 26 TWAA0103602 1 20010225 A 3350 20121 CHARGER BOEING 767 7673Q8 NM CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 634TW 28132 THE EXIT LIGHT AT THE LT SIDE NUMBER 3 CABIN DOOR WAS INOPERATIVE. REPLACED THE BATTERY CHARGER. CHECK-C 10-25-00 LAX. 2 L 7 2 4F RT A1NM 2001032600350 20010326 00350 WP 2001 3 26 TWAA0103603 1 20010225 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN MISSING A TWAA K NONE O OTHER NR NOT REPORTED 1 CE 05 9619V 53566 THE EGRESS LIGHTING SYSTEM WAS MISSING A PIECE AT ROW 23. INSTALLED LIGHT, (P/N 81000-22701ATS), AND REPLACED BATTERY C ELL, (P/N 408822-101). CHECK-C 1-8-01 JFK. 2 L 7 2 4F RT A6WE 2001032600351 20010326 00351 WP 2001 3 26 TWAA0103604 1 20010225 A 5242 65B0467916 LATCH DOUG DC9 DC982 3022082 WP GROUND PWR DR UNLATCHED A TWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CE 05 913TW 49184 STRONG VIBRATION FELT AND HEARD IN FWD PART OF THE AIRCRAFT DURING CLIMB. FLIGHT RETURNED TO STL. THE EXTERNAL POWER D OOR UPPER LATCH WAS NOT SECURED. RESECURED THE LATCH. CHECK-C 12-18-01 LAX. 2 L 7 2 4F A6WE 2001032600352 20010326 00352 NM 2001 3 26 TWAA0103605 1 20010222 A 3350 80731 LIGHT BOEING 767 76733AER 1385230 NM AFT GALLEY DETACHED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 637TW 25403 THE EGRESS LIGHTS AT THE AFT GALLEY HAD LAMP DETACHED. REPLACED THE LIGHTING STRIP. CHECK-C 1-27-01 LAX. 2 L 7 2 4F RT A1NM 2001032600353 20010326 00353 NM 2001 3 26 TWAA0103606 1 20010226 A 3350 CONNECTOR BOEING 767 7673Q8 NM CABIN LOOSE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 636TW 30301 THE EGRESS LIGHTS WERE INOPERATIVE FROM ROW 30 THRU AFT CABIN ON LT SIDE, AND ROW 45 AFT ON RT SIDE. RESEATED CONNECTOR S ON THE BATTERY PACKS ACCOUNT LOOSE. 2 L 7 2 4F RT A1NM 2001032600354 20010326 00354 WP 2001 3 26 TWAA0103608 1 20010222 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP AFT CARGO BAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 957U 49702 DURING CHECK-C MAINT IN AFT CARGO COMPT FOUND CORROSION ON LOWER SIDE OF FLOOR SUPPORT AT STA 1212, LONGERON 28L TO 29R. REPLACED FLOOR SUPPORT. INSTALLED WET PER SRM 51-10-3 FASTENERS PER SRM 51-30-0. 2 L 7 2 4F A6WE 2001032600355 20010326 00355 WP 2001 3 26 MWEA010226 1 20010306 A 5210 99557633 INTERCOSTAL DOUG DC9 DC914 3022034 WP PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FORWARD PAX DOOR HAS A CRACKED INTERCOSTAL OVER RECESS HANDLE PAN. (INTERCOSTAL AND REPAIR DOUBLER ARE CRACKED) REMOVE D, FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001032600360 20010326 00360 2001 3 26 SWIA972389 4 20010221 A 3160 DISPLAY EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 284YV 120284 AT APPROXIMATELY 60 KNOTS ON TAKEOFF FIRST OFFICERS EADI AND EHSI BOTH WENT BLANK FOR APPROXIMATELY 3 - 5 SECONDS. RED DPU FAIL ON EADI. AFTER CALLING ABORT (30 KNOTS) SCREENS RELIT. REMOVED AND REPLACED FIRST OFFICERS DPU. P/N 622-7711 -003, S/N OFF 7032, S/N ON 2774. OPS CHECK NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032600361 20010326 00361 SO 2001 3 26 SWIA972391 1 20010225 A 3340 LIGHT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE EXTERIOR INOPERATIVE A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 234SW 120308 RIGHT WING INSPECTION LIGHT INOP. KNOWN ICING CONDITIONS AT DESTINATION. RETURNED TO LAX. REPLACED LIGHT BULB FOR RIG HT WING INSPECTION. CHECKED GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032600362 20010326 00362 NM 2001 3 26 PCAA0102011 1 20010221 A 3320 BV0330012150 SOCKET DHAV DHC8 DHC8102 2809003 NM CABIN BURNED A PCAA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 EA 13 804EX 227 PVD FLIGHT 3555. CREW REPORTED AN ELECTRICAL SMELL IN CABIN NEAR OVERHEAD BINS BY ROW 1 AND 2 AC. CONTRACT MAINTENANCE REMOVED LIGHT BULB, NO ODOR NOTED. MAINTENANCE CONTROL ISSUED MEL 33-02. THE FOLLOWING DAY SYR MAINTENANCE REPLACED A FFECTED LIGHT SOCKET AND BULB. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001032600363 20010326 00363 NM 2001 3 26 PCAA0102012 1 20010220 A 5220 DOOR DHAV DHC8 DHC8102 2809003 NM FWD EMERG EXIT OBSTRUCTED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 838EX 220 MDT- DURING MAINTENANCE TASK FOR INSPECTION OF EMERGENCY EXIT DOOR AREA, RIGHT FORWARD EMERGENCY EXIT DOOR WAS FOUND TO BE HARD TO OPEN. INTERIOR TRIM PANEL INTERFERRING WITH DOOR OPERATION. PANEL REINSTALLED TO ALLOW FREE MOVEMENT. OPER ATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2001032600364 20010326 00364 NM 2001 3 26 PCAA0102013 1 20010221 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INTERMITTENT A PCAA K NONE O OTHER CL CLIMB 1 EA 13 830EX 155 SYR FLIGHT 3800. CREW REPORTED THAT SOON AFTER TAKEOFF ALL EMERGENCY LIGHTS IN THE CABIN ILLUMINATED DIMLY, AND FLICKER ED FOR 5 MINUTES. SYR MAINTENANCE CYCLED EMERGENCY LIGHT SWITCH AND COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT WAS THEN RETURNED TO SERVICE. SUBSEQUENT MAINTENANCE FOUND AND REPAIRED INTERMITTANT WIRE SPLICE. AIRCRAFT RETURNED TO SERVICE . NO REOCCURANCE OF PROBLEM EXISTS TO THIS DATE. 2 H 7 2 4T RT A13NM 2001032600365 20010326 00365 WP 2001 3 26 MWEA010237 1 20010306 A 5210 99557519 INTERCOSTAL DOUG DC9 DC914 3022034 WP PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FORWARD PAX DOOR INTERCOSTAL IS CRACKED ABOVE BAYONET AB9. REMOVED, LOCATED, DRILLED AND INSTALLED NEW INTERCOSTAL. 2 L 7 2 4F A6WE 2001032600373 20010326 00373 WP 2001 3 26 01FDEA00162 1 20010225 A 2822 PUMP DOUG DC10 DC1030F 3023504 WP FUEL SYSTEM FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 310FE 48299 LOST NR 2 LT AND NR 2 RT AND NR 3 AFT TANK PUMPS. REMOVED AND REPLACED LT AFT FUEL BOOST PUMP. OPS CK NORM PER MM. CK WIRING TO ALL 3 PUMPS NO FAULT FOUND. ALL PUMPS OPS NORMAL. 2 L 7 3 4F RT A22WE 2001032600374 20010326 00374 EU 2001 3 26 01FDEA00163 1 20010224 A 2612 PANEL AIRBUS 310 A310 EU COCKPIT FAULTY A FDEA O OTHER J WARNING INDICATION CR CRUISE 1 SO 25 680FE 794 NR 1 ENG AGENT NR 2 DISCHARGE LIGHT CAME ON IN FLT. REMOVED AND REPLACED NR 1 ENG OVERHEAD FIRE SHUTOFF PNL. RECHECK G OOD. OPS CK PER A300 AMM 26-12-20-4. 2 L 7 2 4F RT A35EU 2001032600375 20010326 00375 WP 2001 3 26 MWEA010248 1 20010306 A 5210 9955758 BEAM DOUG DC9 DC914 3022034 WP PAX DOOR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 PAX DOOR BEAM NR 7 HAS NON-REPAIRABLE DAMAGE. REMOVED, LOCATED, DRILLED AND INSTALLED NR 7 BEAM. 2 L 7 2 4F A6WE 2001032600379 20010326 00379 WP 2001 3 26 0100639867 1 20010124 A 3246 WHEEL DOUG DC9 DC951 3022051 WP RT MLG CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 776NC 02880 47786 DURING PUSHBACK FROM THE GATE AREA AT YUL, THE PUSHBACK CREW REPORTED THAT THE RIGHT INNER WHEEL WAS CRACKED. THE AIRCR AFT WAS RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT INNER AND RIGHT OUTER MAIN WHEEL AND TIRE ASSEMBLIES. NOTE: IT WAS REPORTED THAT A 22 INCH SECTION OF THE RIGHT INNER WHEEL HAD SEPARATED WHEN THE AIRCRAFT DEPA RTED DTW TO YUL. THE 22 INCH PIECE OF WHEEL MATERIAL WAS RECOVERED IN DTW. 2 L 7 2 4F RT A6WE 2001032600387 20010326 00387 NM 2001 3 26 UPS01435192 1 20010305 A 2420 CONNECTOR BOEING 747 747123 1384873 NM NR1 ENG FIREWALL DISCONNECTED A IPXA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 674UP 20100 INSPECTION TYPE:N/A DURING CLIMB TO FL300 NR 1 GEN TRIPPED NR 1 FIELD TRIPPED.CSD NR 1 ENG ABOVE REDLINE/180C IND. RAN CKLIST & DISCONNECTED CSD ATTEMPTED. CSD DISCONNECT NOT EFFECTIVE. CSD RPM0 & CSD PMG BETWEEN 75 AND 100. NR 1 ENG PR ECAUTIONARY SHUTDOWN. CHECKED AND FOUND ELECTRICAL CONNECTOR D11P WAS DISCONECTED AT NR1 ENG HORIZONTAL FIREWALL. CLEA NED AND INSTALLED CONNECTOR, PERFORMED OPS CK''D CSD DISCONNECT FUNCTION NORMAL. RECONNECTED CSD & NR 1 GEN OP''S NORMA L. OK FOR SERVICE. PERFORMED NR 1 ENG WINDMILLING INSPECTION NO CONTAMINATION NOTED AT FILTER & MAG TIP. OK TO OPERAT E NR 1 ENG. 2 L 7 4 4F A20WE 2001032600389 20010326 00389 EU 2001 3 26 MALA010211 1 20010222 A 2910 RESERVOIR SAAB SF340 340B 7860101 EU HYDRAULIC SYS LOW A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 414XJ 340B414 ON TAKEOFF FLIGHT 2822 GEAR WAS RETRACTED, THE 3 GREEN LIGHTS WENT OUT BUT THE INTRANSIT LIGHT REMAINED ILLUMINATED AND THE HYDRAULIC PUMP KEPT RUNNING. AIR RETURN TO DTW. MAINTENANCE SERVICED HYDRAULIC SYSTEM UP TO LIMIT, CYCLED THE GEAR SEVERAL TIMES, ALL CHECK GOOD ON THE GROUND IAW SAAB MM 32. 2 L 7 2 4T RT A52EU 2001032600390 20010326 00390 EU 2001 3 26 MALA010212 1 20010222 A 3297 WIRE SAAB SF340 340B 7860101 EU EXHAUST NOZZLE CHAFED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 452XJ 452 FLIGHT 2907 RT INTAKE HEAT INTERMITTANT. WORKED WELL ON THE GROUND, CAME ON ABOUT 10 MINUTES INTO THE FLIGHT. AIR RETU RN TO DTW. MAINTENANCE TROUBLESHOT FOUND CHAFED WIRE ON EXHAUST NOZZLE, REPAIRED WIRE, REPLACED DEICE CONTROL MODULE AS A PRECAUTIONARY MEASURE. P/N 44730-501, S/N OFF L248371, S/N ON A00021, RAN AIRCRAFT 1 HOUR. NO DEFECTS NOTED. 2 L 7 2 4T RT A52EU 2001032600391 20010326 00391 EU 2001 3 26 MALA010213 1 20010222 A 3020 THERMISTER SAAB SF340 340B 7860101 EU ANTI-ICE SYS OUT OF POSITION A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 452XJ 452 FLIGHT 2800, RT INTAKE HEAT CYCLED ON DEPARTURE. FLIGHT RETURNED TO DTW. MAINTENANCE SWAPPED THERMISTORS 1 & 3, TO 4 & 5 POSITIONS. RAN AIRCRAFT ALL CHECK GOOD. 2 L 7 2 4T RT A52EU 2001032600392 20010326 00392 EU 2001 3 26 MALA010214 1 20010225 A 3213 STRUT SAAB SF340 340B 7860101 EU LT MLG LOW A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 443XJ 443 ON FLIGHT 3205 LANDING GEAR WOULD NOT RETRACT. ATTEMPTED 3 TIMES ON DEPARTURE. AIR RETURN TO MSP. MAINTENANCE FOUND L T MAIN GEAR STRUT UNDERSERVICED. STRUT WAS HANGING UP AND NOT MAKING WOW SWITCHES, SERVICED LT STRUT PER MM 12-30-32, P ERFORMED GEAR SWINGS, ALL OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2001032600393 20010326 00393 EU 2001 3 26 MALA010215 1 20010212 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 424XJ 424 FOUND DURING C-CHECK, RT FUSELAGE HAS SEVERAL DENTS BETWEEN STA 339 THRU STA 363, AND SL1618 THRU SL1622. REFER TO CELS IUS W/O 19347, TASK 2518, AND SAAB EO STATEMENT 340SDS001021. MAINTENANCE CHECK LIMITS, FOUND TO BE OUT OF ALLOWABLE LI MIT REF SAAB SRM 51-10-10. PERFORM NDT: EC AND BOND TEST. NDT PER FFV. NDT006 & 004 EC & UT NO CRACKS, NO DISBONDS, DE NTS ARE ACCEPTED AS IS REF SAAB ENGINEERING STATEMENT 340SDS001021. 2 L 7 2 4T RT A52EU 2001032600394 20010326 00394 WP 2001 3 26 AT0100095 1 20010302 A 3340 8906K1665 SWITCH DOUG DC9 DC932 3022066 WP INSTRUMENT PANEL SHORTED A ZZDA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 15 818AT 47320 FOUND LEFT LANDING LIGHT SWITCH SHORTED INTERNALLY AND SMOKING. REPLACED LEFT LIGHT SWITCH IAW DC9 MM 33-41-01. 2 L 7 2 4F A6WE 2001032600395 20010326 00395 EU 2001 3 26 MALA010219 1 20010219 A 5320 7253721439 WEB SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 424XJ 424 FOUND DURING C-CHECK, CORROSION ON WEB AT STA 294.0 REFER TO CELSIUS W/O 19347, TASK 2566. MAINTENANCE REMOVED CORROSIO N AND CHECK LIMIT. REMOVED WEB AT STA 294 IAW SRM 51-40-21. MATERIAL IS OUT OF LIMITS REF SRM 51-10-10, LOCATED AND DRI LLED COUNTERSANK NEW WEB IAW SRM 51-40-40. INSTALLED NEW WEB IAW SRM 51-40-21/23, P/N 7253721-439. 2 L 7 2 4T RT A52EU 2001032600397 20010326 00397 EU 2001 3 26 MALA010221 1 20010221 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 424XJ 424 FOUND DURING C-CHECK, CARGO AREA SEAT TRACK LBL18.3 FLOOR PANEL FLANGES HAVE CORROSION AT STA 622.0 THRU STA 686.0 REFER TO CELSIUS W/O 19347, TASK 1510, AND SAAB STATEMENT 340SDS001037. MAINTANENCE REMOVED CORROSION AND CHECK LIMIT. REMO VED CORROSION IN CARGO AREA LBL18.3 STA 622 - 686 IAW SRM 51-70-40. SEVERAL AREAS OF MATERIAL OUT OF LIMITS REF SRM 51- 10-10. ALODINED, PRIMED AND TOPCOATED IAW SRM51-20-42/43. MATERIAL REMOVED ARE ACCEPTED AS IS REF SAAB EO 340SDS001037 . 2 L 7 2 4T RT A52EU 2001032600398 20010326 00398 EU 2001 3 26 MALA010223 1 20010219 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 424XJ 424 FOUND DURING C-CHECK, FLOORBOARD FLANGE AT STA 258.0 FOR FLOOR PANEL 121AZ HAS CORROSION. REFER TO CELSIUS W/O 19347, T ASK 2572. MAINTENANCE REMOVED CORROSION, CHECK LIMIT. REMOVED FWD FLANGE AT STA 258 IAW SRM 51-40-21, BLENDED OUT CORR OSION IAW SRM 51-10-10/MATERIALS REMOVED IS OUT OF LIMITS IAW SRM 51-10-10. FABRICATED NEW FWD ANGLE IAW SRM 51-20-20/3 0. ALODINED, AND PRIMED PAINTED, IAW SRM 51-20-42/43. INSTALLED IAW SRM 51-40-21. 2 L 7 2 4T RT A52EU 2001032600399 20010326 00399 WP 2001 3 26 AT0100101 1 20010209 A 5313 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 FOUND LONGERON 27R CRACKED AT BS 258. FABRICATED AND INSTALLED REPAIR SPLICES IAW DC9 SRM 51-10-05, 51-10-04, AND 53-02 FIG 18. 2 L 7 2 4F A6WE 2001032600400 20010326 00400 WP 2001 3 26 AT0100102 1 20010213 A 5230 SKIN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 FOUND AFT PIT CARGO DOOR INNER SKIN TORN AT AFT HINGE. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 52-05, 51-30 -01, 51-30-02, AND 51-30-05. 2 L 7 2 4F A6WE 2001032600401 20010326 00401 WP 2001 3 26 AT0100104 1 20010208 A 5532 PANEL DOUG DC9 DC932 3022066 WP VERT STABILIZER CHAFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 FOUND VERTICAL STABILIZER UPPER FAIRING CHAFED OUT OF LIMITS. REPLACED SKIN PANEL IAW DC9 SRM 55-01 FIG 1, 55-31, 51-10 -02, 51-10-03, 51-10-04, AND 51-30-02. 2 L 7 2 4F A6WE 2001032600402 20010326 00402 EU 2001 3 26 MALA010225 1 20010219 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 424XJ 424 FOUND DURING C-CHECK, FLOORBOARD FLANGE FOR PANEL 122 DZ HAS CORROSION. REFER TO CELSIUS W/O 19347, TASK 2574. MAINTEN ANCE FABRICATED NEW FLANGE PER SAMPLE SAME AS ORIGINAL MATERIAL. ALODINED, AND PRIMED IAW SRM 51-20-42 & 51-20-43. TOP COATED IAW SRM 51-20-43. 2 L 7 2 4T RT A52EU 2001032600403 20010326 00403 EU 2001 3 26 MALA010226 1 20010221 A 5313 STRINGER SAAB SF340 340B 7860101 EU FUSELAGE DAMAGED A MALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 15 424XJ 424 FOUND DURING C-CHECK, LOWER ROW OF RIVETS ON PREVIOUS REPAIR LOCATED ON RT SKIN AT STA 39 IS INSTALLED IN THE EDGE OF ST RINGER-IMPROPER EDGE DISTANCE. REFER TO CELSIUS W/O 19347, TASK 2631 AND SAAB STATEMENT 340SDS001021. MAINTENANCE REMO VE REPAIR PATCH FOR FURTHER EVALUATION REQ 337 FORM. REMOVED REPAIR FOR FURTHER INSPECTION OF AREA IAW SRM 51-10-00 PER FORM NDT: EC AND BOND TEST NDT PER FFVNDT006EC &004UT BOND NO CRACKS, NO DISBONDS. FABRICATED STRINGER REPAIR AND FILLE R FROM 2024T3 .050, ALODINED/PRIMED IAW SRM 51-20-42/43 AND INSTALLED REF SAAB EO 340SDS001021, EXTERNAL DAMAGE IS REPAI RED UNDER W/O 19347 TASK 2517-DOUBLER REPAIR. 2 L 7 2 4T RT A52EU 2001032600404 20010326 00404 EU 2001 3 26 MALA010227 1 20010221 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 424XJ 424 FOUND DURING C-CHECK, LOWER TAIL IS DENTED AT 4 PLACES BETWEEN STA 827 THRU STA 853. REFER TO CELSIUS W/O 19347, TASK 3 503 AND SAAB STATEMENT 340SDS001037. MAINTENANCE CHECKED LIMIT. FOUND 1 EACH DENT WITHIN LIMIT, FOUND 3 EACH DENT OUT OF ALLOWABLE LIMIT REF SRM 51-10-10, PERFORM NDT: NDT PER FFVNDT006EC NO CRACKS NOTED. FABRICATE REPAIR DOUBLER, LAY O UT RIVET PATTERN AND DRILLED IAW SRM 53-90-10. TREAT AND PRIME IAW SRM 51-10-30 AND SAAB EO 340SDS001037. INSTALLED DO UBLER IAW SRM 51-40-21 FOR PAINT SEE W/O 19347, TASK 2515 IPM12 ITEM 31, REMAINING DENTS ACCEPTED AS IS REF SAAB EO 340S DS001037. 2 L 7 2 4T RT A52EU 2001032600405 20010326 00405 EU 2001 3 26 MALA010228 1 20010221 A 5347 CARGO TRACK SAAB SF340 340B 7860101 EU CARGO BAY CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 424XJ 424 FOUND DURING C-CHECK, CARGO AREA SEAT TRACK BL-0 FLOOR PANEL FLANGES AND IB SIDE AT FLOOR PANEL 171DZ STA 622.0 THRU STA 686.0 HAVE CORROSION. REFER TO CELSIUS W/O 19347, TASL 1511 AND SAAB STATEMENT 340SDS001037. MAINTENANCE REMOVE CORRO SION, CHECK LIMIT. REMOVED CORROSION IN CARGO AREA AT BL-0 FROM STA 622 TO 686 IAW SRM 51-70-40. SEVERAL AREAS OF MATE RIAL IS OUT OF ALLOWABLE LIMITS. FABRICATED L-ANGLE PER PRINCIPLES OF SRM 53-70-60, ALODINED, PRIMED AND TOPCOATED PER SRM 51-20-42/43. INSTALLED REPAIR ANGLE IAW SAAB SRM 53-70-60. REMAINING AREAS, ARE ACCEPTED AS IS REF EO 340SDS001037 , APPLIED AVIVO TO SEAT TRACK FLANGES IAW EO340SDS001037. 2 L 7 2 4T RT A52EU 2001032600406 20010326 00406 EU 2001 3 26 MALA010230 1 20010221 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 424XJ 424 FOUND DURING C-CHECK, RT SIDE OF FUSELAGE HAS A CLUSTER OF DENTS IN CLOSE PROXIMITY BETWEEN STA 339, AND STA 363 AND BET WEEN STRINGERS SL1615, AND SL1617. REFER TO CELSIUS W/O 19347, TASK 2517, AND SAAB STATEMENT 340SDS001021. MAINTENANCE CHECK LIMIT, FOUND DENTS OUT OF ALLOWABLE LIMIT REF SAAB SRM 51-10-10. PERFORM NDT: EC AND BOND TEST NDT PER FFVNDT006 EC AND 004UT BOND, NO CRACKS, NO DISBONDS. REMOVED EXISTING REPAIR IAW SAAB STATEMENT 340SDS001021. INSTALLED REPAIR, SEALED AND TOPCOATED REMAINING DENTS ARE ACCEPTED AS IS REF SAAB EO 340SDS001021. 2 L 7 2 4T RT A52EU 2001032600407 20010326 00407 EU 2001 3 26 MALA010229 1 20010221 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 424XJ 424 FOUND DURING C-CHECK, CORROSION ON IB FLOOR SUPPORT FLANGE ON SEAT TRACK AT LBL 18.3 THRU STA 630. REFER TO CELSIUS, W/ O 19347, TASK 1525 AND SAAB STATEMENT 340SDS0010137. MAINTENANCE REMOVED CORROSION, CHECK LIMIT. CLEANED AREA IAW SRM 51-20-41, BLENDED OUT CORROSION IAW SRM 51-10-10. MATERIAL REMOVED IS OUT OF LIMITS IN SEVERAL AREAS AS MARKED IAW SRM 53-70-60. REMOVED FWD CLIP, IAW SRM 51-40-21, FABRICATED NEW CLIP, ALODINED, PRIMED AND PAINTED IAW SRM 51-20-42/43, IN STALLED IAW SRM 51-40-21/23. 2 L 7 2 4T RT A52EU 2001032600408 20010326 00408 WP 2001 3 26 ABXA010064 1 20010224 A 3231 4932017501 LINK DOUG DC9 DC931 3022065 WP LT MLG WORN A ABXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 947AX 47004 THE MAIN LANDING GEAR FAILED GEAR UPLATCH CHECKS AFTER TAKEOFF. THE FLIGHT CREW COMPLIED WITH ABNORMAL CHECKLIST. MAIN TENANCE INSPECTED AND REPLACED THE LEFT MAIN LANDING GEAR DOOR, LATCH TO DOOR JAMB LINK ASSY IAW DC-9 MM 32-31-04. MAIN TENANCE INSPECTED AND REPLACED THE LEFT MAIN LANDING GEAR OVER CENTER LINK SWITCH (P/N 7000010101ABX, S/N 11504) AS A PR ECAUTION. THE LEFT MAIN LANDING GEAR INDICATION WIRING WAS ALSO INSPECTED FOR DEFECTS. THE LANDING GEAR INDICATION LIG HT BULBS WERE REPLACED AND OPERATION CHECKS WERE COMPLETED. 2 L 7 2 4F A6WE 2001032600409 20010326 00409 WP 2001 3 26 ABXA010066 1 20010227 A 3241 422551 CONTROL UNIT DOUG DC9 DC941 302207N WP ANTI-SKID SYS FAILED A ABXA O OTHER O OTHER LD LANDING 1 GL 23 963AX 84774 0 47780 UPON LANDING WHEN BRAKES WERE APPLIED, THE BRAKES DID NOT OPERATE. WITH THE ANTI-SKID SYSTEM SELECTED OFF, BRAKING ACTI ON RETURNED. MAINTENANCE INSPECTED AND REPLACED THE ANTI-SKID CONTROL UNIT IAW DC-9 MAINTENANCE MANUAL 32-43-04. 2 L 7 2 4F A6WE 2001032600410 20010326 00410 EA 2001 3 26 COMA0160285 1 20010226 A 5330 SKIN CNDAIR CL600 CL6002B19 EA FUSELAGE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 973CA 7146 V-SHAPED TEAR IN THE FUSELAGE BELOW DC EXT POWER RECEPTACLE. REPAIRED DAMAGED IAW EO 601R-53-2269. 2 L 7 2 4F RT A21EA 2001032600411 20010326 00411 EA 2001 3 26 COMA0160286 1 20010226 A 2741 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT FALSE ACTIVATION A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 958CA 7111 MACH TRIM AND STAB TRIM CAUTION MESSAGE. COULD NOT DUPLICATE. SYSTEM TEST NORMAL. NO FAULTS CODES IN COMPUTER. 2 L 7 2 4F RT A21EA 2001032600412 20010326 00412 EA 2001 3 26 COMA0160287 1 20010226 A 4900 SMOKE CNDAIR CL600 CL6002B19 EA APU DETECTED A COMA F H ACTIVATE FIRE EXT. DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 995CA 7229 SMOKE COMING FROM APU INLET WHEN APU WAS SHUT DOWN. INSPECTED APU AND FOUND NO DEFECTS. 2 L 7 2 4F RT A21EA 2001032600413 20010326 00413 EA 2001 3 26 COMA0160288 1 20010223 A 2752 853D10014 ACTUATOR CNDAIR CL600 CL6002B19 EA RT FLAP FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 976CA 2798 7151 FLAPS FAIL CAUTION MESSAGE. REPLACED RT OUTBD FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2001032600414 20010326 00414 2001 3 26 COMA0160289 4 20010225 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 721CA 7259 STALL FAIL CAUTION MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001032600415 20010326 00415 NM 2001 3 26 DHL2001701003 1 20010228 A 7931 SRL0C4N INDICATOR BOEING 727 72730C 1384009 NM COCKPIT DEFECTIVE A DHLA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 701DH 19011 NR 2 OIL PRESURE GAUGE BEGAN READING 20 PSI AT POSITION AND HOLD. PULLED-OFF RUNWAY AND SHUTDOWN ENGINE NR 2. TROUBLES HOT SYSTEM AND FOUND NR 2 ENGINE OIL PRESSURE INDICATOR DEFECTIVE. REMOVED AND REPLACED NR 2 OIL PRESSURE INDICATOR. R AN ENGINE, SYSTEM OPS CHECKED GOOD IAW M/M 79-32-0. 2 L 7 3 4F A3WE 2001032600419 20010326 00419 NM 2001 3 26 UPS01235063 1 20010223 A 3350 BATTERY BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:N/A, ROW 2 LEFT SEAT EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED ROW 2 EMERGENCY LIGHT BATTERY AS SY PER MM 33-50-22. OPS CHECKS GOOD. 2 L 7 3 4F A3WE 2001032600490 20010326 00490 NM 2001 3 26 2001UALA00090 1 20010205 A 5210 140N264026 GUIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 DOOR 2 LEFT IS HARD TO OPEN. *S/D* GUIDE ARM PIN WAS FOUND LOOSE DURING TROUBLESHOOTING. NEW GUIDE ARM WAS INSTALLED AND ADJUSTED. 2 L 7 2 4F 4 F RT A2NM E17NE 2001032600493 20010326 00493 NM 2001 3 26 01FDEA00148 1 20010217 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM CABIN CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DURING ROUTINE INSP, NR 6 MAIN CABIN SEAT TRACK FOUND CORRODED AT BS 475. *S/D* REMOVED, REPLACED AND FAB SEAT TRACK P ER IAW BAC 727 SRM 53-10-5. 2 L 7 3 4F A3WE 2001032600494 20010326 00494 EU 2001 3 26 MALA010218 1 20010219 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 424XJ 424 FOUND DURING C-CHECK, CORROSION ON FLOOR SUPPORT FLANGE LBL 33 STA 376. REFER TO CELSIUS W/O 19347, TASK 1518. MAINTEN ANCE REMOVED CORROSION, CHECK LIMIT. REMOVED CORROSION IAW SRM 51-70-40 MATERIAL REMOVED IS OUT OF LIMITS IAW SRM 51-10 -10. FABRICATED REPAIR ANGLE IAW SRM 51-40-40, TREATED AND PRIMED REPAIR ANGLE IAW SRM 51-20-42/43, INSTALLED REPAIR AN GLE WET IAW SRM 51-40-21, PRIMED AND TOPCOATED IAW SRM 51-21-42/43. 2 L 7 2 4T RT A52EU 2001032700198 20010327 00198 NM 2001 3 27 2001UALA00074 1 20010203 A 3350 9003 SIGN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN MISSING A UALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 29 7444U 21898 CENTER AISLE EXIT SIGN IS MISSING. *S/D* AIRCRAFT RETURNED TO GATE BECAUSE FLIGHT ATTENDANT NOTICED CENTER EXIT SIGN W AS MISSING FROM CEILING. REINSTALLED LIGHT ASSEMBLY ABOVE CEILING PANEL. OPERATIONS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001032700199 20010327 00199 NM 2001 3 27 2001UALA00076 1 20010202 A 5310 STRUCTURE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUSELAGE VIBRATES A UALA O OTHER E VIBRATION/BUFFET UK UNKNOWN 1 WP 29 772UA 26930 CREW REPORTS LOUD NOISE AND VIBRATION ON RIGHT SIDE OF AIRCRAFT BY ROW 15. *S/D* DUCTS IN AFT OF FORWARD CARGO COMPART MENT (MIX MANIFOLD AREA) WERE CHECKED, BUT NO DISCREPANCIES WERE FOUND. AIR ON TEST WAS PERFORMED ON RIGHT HAND PACK, A ND THERE WAS NO EICAS MESSAGE INDICTING THE RIGHT PACK. AIRCRAFT WENT BACK TO REVENUE SERVICE WITH NO FURTHER INCIDENT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001032700200 20010327 00200 NE 2001 3 27 AWXA0001337 2 20010214 A 7261 MS9388151 PACKING BOEING 737 737277 1384570 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE BROKEN A AWXA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CL CLIMB 1 WP 28 181AW 3710 22648 P700272B INFLIGHT NR 2 ENGINE OIL PRESSURE DROPPED BELOW THE RED RADIAL; THE CREW ACCOMPLISHED ENGINE SHUTDOWN PER THE ORH, RETUR NED TO OAK. THE ENGINE WAS SHUTDOWN FOR 25 MIN WITH WINDMILLING OIL PRESSURE OF 20 PS. IN OAK THE OIL PRESSURE TRANSMI TTER AND OIL PRESSURE INDICATOR WERE REPLACED AND TESTED GOOD; THE ENGINE WINDMILLING INSPECTION WAS PERFORMED AND THE M AIN OIL FILTER WAS REPLACED (NO DEBRIS IN FILTER); ON THE NEXT FLIGHT THE OIL QUANTITY WAS FOUND TO FOLLOW THE POWER LEV ER AT ALL SETTINGS; TAKEOFF 2.0-2.5 GALS, IDLE 3.0-3.5 GALS AND AFTER SHUTDOWN IN PHX 4.0 GALS. IN PHX OIL PUMP WAS REPL ACED. UPON REMOVAL TE CENTER O-RING WAS FOUND TO BE BROKEN, THE OTHER 2 WERE OK. PUMP WAS REPLACED THOUGH NORMAL. 2 L 7 2 4F 4 F RT A16WE E2EA 2001032700201 20010327 00201 NM 2001 3 27 C8GA20010003 1 20010218 A 5610 57176244 SLIDING WINDOW BOEING 727 727227 1384078 NM COCKPIT CRACKED A C8GA B I A EMER. DESCENT CABIN DEPRESSURIZATION UNSCHED LANDING O OTHER CR CRUISE 1 SO 15 308AS 2596 22002 FLIGHT 399 FROM KBWI TO KDAY AT FL 330 CO-PILOTS SLIDING WINDOW OUTER PANE EXPERIENCED MULTIPLE CRACKS EMANATING FROM FW D LWR CORNER. AIRCRAFT DESCENDED TO FL 010 AND DEPRESSURIZED CABIN. AIR TURNBACK TO KBWI WITH NO FURTHER INCIDENTS. 2 L 7 3 4F A3WE 2001032700202 20010327 00202 NE 2001 3 27 PCAA0102008 3 20010218 A 6114 7827015 HUB DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE LT PROPELLER GALLED A PCAA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 13 816EX 9085 329 120701 1894 BGM - DURING ROUTINE MAINTENANCE VISIT LEFT PROPELLER ASSEMBLY HAD EVIDENCE OF OIL LEAK. UPON FURTHER INVESTIGATION LEAK WAS FOUND TO BE COMING FROM NR4 BLADE. AFTER REMOVING THE LEFT NR4 BLADE THE OUTER BEARING RACE WITHIN THE PROPELLER HU B WAS FOUND TO BE CRACKED AND GALLED. LEFT PROPELLER HUB, PROPELLER ACTUATOR, AND 3 BLADES WERE REPLACED DUE TO OIL CONT AMINATION AND AN ADDITIONAL BEARING RACE FOUND GALLED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001032700203 20010327 00203 2001 3 27 UPS01435032 4 20010221 A 2210 COMPUTER BOEING 747 747123 1384873 NM COCKPIT MALFUNCTIONED A IPXA O OTHER O OTHER CL CLIMB 1 SO 01 671UP 20323 INSPECTION TYPE:N/A, WHILE CLIMBING THRU FL 345 TO FL 350 (500 FT TO GO), AT 500 FT PER MINUTE THE A-AUTOPILOT PITCHED U P TO CAPTURE THE ALTITUDE WITH A 1500 TO 2000 FPM CLIMB. CREW HAD TO INTERCEDE TO PREVENT OVERSHOOT IN RVSM AIRSPACE. RESEATED A A/P PITCH CHANNEL AND TESTED PER MM 22-12-01. NO FAULTS FOUND. 2 L 7 4 4F A20WE 2001032700218 20010327 00218 SO 2001 3 27 SWIA972394 1 20010221 A 5246 FASTENER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FUEL DOOR UNSECURE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 216SW 120285 SERVICE DOOR LIGHT COMES ON IN FLIGHT. RETURNED TO SLC. FOUND FASTENER OPEN ON FUEL DOOR. LATCHED FASTENER. OPS CHEC K GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032700219 20010327 00219 SO 2001 3 27 SWIA972395 1 20010225 A 2170 SEPARATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT & RT FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 585SW 120353 DURING FLIGHT RIGHT OUTBOARD STABILIZER PROTECTION FAILED. RETURNED TO FAT. REMOVED AND REPLACED BOTH LEFT AND RIGHT D EICE WATER SEPERATORS WITH SERVICEABLE UNIT. OPS CHECK GOOD. NO SYSTEM FAILURE NOTED. P/N ON LT 443221A, S/N ON RF261 4, S/N OFF B-3161, P/N ON RT 44E22-1A, S/N ON RF-2607, S/N OFF 13-3163. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032700220 20010327 00220 SO 2001 3 27 SWIA972397 1 20010226 A 5610 WINDOW FRAME EMB 120 EMB120RT SO PWA 118 PW118 NE COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 593SW 120191 WINDOW FRAME CRACKED ON PILOTS SIDE. DISCOVERED DURING LINE INSPECTION. INSTALLED WINDOW FRAME REPAIR ON PILOTS SIDE P ER SB 120-053-0010. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032700221 20010327 00221 SO 2001 3 27 SWIA972398 1 20010227 A 3340 LIGHT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE EXTERIOR INOPERATIVE A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 565SW 120340 LIGHT INSPECTION LEFT SIDE DOES NOT ILLUMINATE. ICING CONDITIONS EXIST AT DESTINATION. RETURNED TO LAX. REPLACED LEFT DEICE INSPECTION LIGHT BULB. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032700222 20010327 00222 SO 2001 3 27 SWIA972399 1 20010225 A 2731 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE ELEVATOR TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 288SW 120316 ELEVATOR TRIM FROZE IN FLIGHT AND BROKE LOOSE SUDDENLY, CAUSING VIOLENT PITCH DOWN. REMOVED AND REPLACED RIGHT AND LEFT ELEVATOR TRIM TAB LINEAR ACTUATORS IAW EMB 120 MM 27-32-02 AND 27-00-01. LEFT TRIM ACTUATOR S/N OFF: 735, S/N ON: UNKN OWN. RIGHT TRIM ACTUATOR S/N OFF: 736, S/N ON: 426. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032700223 20010327 00223 NM 2001 3 27 C8GA20010004 1 20010221 A 3150 FIRE WARNING PWA BOEING 727 727223 1384074 NM NR 2 ENGINE ACTIVATED A C8GA E F B A ENGINE SHUTDOWN ACTIVATE FIRE EXT. EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 15 899AA 700789 22015 ON FLIGHT 1721 FROM KFLL TO KTOL AT FL 190 NR 2 ENGINE EXPERIENCED A FIRE WARNING. ENGINE WAS SHUT DOWN AND FIRE BOTTLE DISCHARGED. FIRE WARNING LIGHT WENT OUT AND AIRCRAFT RETURNED TO KFLL. 2 L 7 3 4F A3WE 2001032700224 20010327 00224 NM 2001 3 27 UPS01235112 1 20010227 A 3350 CONTROL UNIT BOEING 727 72725C 138400H NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:IN DD 3/7 FUNCTIONAL CHECK EMERGENCY LIGHT CONTROL MODULES. (TRANSMITTERS) FUNCTIONAL CK COMPLETED. 2 L 7 3 4F A3WE 2001032700225 20010327 00225 NM 2001 3 27 QXEA0100234 1 20010216 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 PDX- LEFT HAND INBOARD SEAT TRACK CORROSION AT X330.00. REPAIRED IAW DHC-8 RD8-53-1339. 2 H 7 2 4T RT A13NM 2001032700226 20010327 00226 SO 2001 3 27 SWIA972400 1 20010224 A 2731 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE ELEVATOR TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 07 189SW 120048 ELEVATOR TRIM BINDING ON DESCENT TO SLC. INSTALLED SERVICEABLE TRIM TAB ACTUATOR FOR LEFT ELEVATOR TRIM IAW MM 27-32-02 . P/N ON 5299-1, S/N ON 842, S/N OFF 174. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032700227 20010327 00227 2001 3 27 SWIA972401 4 20010223 A 2216 SERVO EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE AUTOPILOT OBSTRUCTED A SWIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 07 586SW 120354 TRIM (ELECTRIC) LATCHES ON THE DESCENT WHEN AUTOPILOT IS ENGAGED. INSPECTED TRIM CABLES AND MECHANISMS. FOUND LINT IN ACTUATOR CHAIN NEAR SERVO FOR AUTO PILOT. REMOVED LINT, OPS CHECKS GOOD IAW MM 27-00-00. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032700228 20010327 00228 2001 3 27 SWIA972402 4 20010228 A 3417 ADC CNDAIR CL600 CL6002B19 EA COCKPIT FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 416SW 7089 CLIMBING THROUGH FL250 OFF BZN STAB TRIM CH2 AND MACH TRIM FAILED. RAN THE QRH AND DID NOT FIX THE PROBLEM. TROUBLESHO T SYSTEM. REPLACED ADC IAW 34-13-01. SYSTEM OPS CHECK AND STATIC LEAK CHECK OK. P/N ON 822-0371-140, S/N ON 5VYN, S/ N OFF 2145. 2 L 7 2 4F RT A21EA 2001032700229 20010327 00229 SO 2001 3 27 SWIA972403 1 20010226 A 3010 EJECTOR VALVE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE DEICE SYSTEM MALFUNCTIONED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 561SW 120335 AFTER TAKEOFF INBOARD LEFT AND RIGHT STAB AND INBOARD LEFT AND RIGHT WING DEICE LIGHT CAME ON BOTH TIMERS IN HEAVY AND L IGHT CYCLE. RETURNED TO LAX. INSTALLED SERVICEABLE RIGHT FOWARD EJECTOR VALVE FOR BOOTS IAW 30-10-00. RAN ENGINE AND OPS CHECK GOOD. REINSTALLED PANEL AND ALL CHECKS OK AT THIS TIME. S/N ON P1263, S/N OFF N1671. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032700230 20010327 00230 SO 2001 3 27 SWIA972404 1 20010228 A 2750 CONTROL UNIT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FLAPS FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 195SW 120127 FLAP CONTROL FAULT AT FL260 DURING CRUISE. RESET ONCE BUT REOCCURRED AGAIN AFTER ABOUT 10 MINUTES AND WOULD NOT RESET. COULD NOT RESET ON GROUND. REMOVED AND REPLACED FLAP CONTROL UNIT WITH SERVICEABLE UNIT IAW 27-50-06. FLAPS OPS CHECK GOOD. CYCLED MORE THAN 20 TIMES. P/N: 307500-1017, S/N ON: 0169, S/N OFF: 0093. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032700234 20010327 00234 NM 2001 3 27 AWXA0001431 1 20010301 A 5330 659187912 SKIN BOEING 737 737277 1384570 NM LT & RT WW BUCKLED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 KEEL BEAM SKIN PANEL BETWEEN GEAR WELLS BUCKLED AND HAS LOOSE RIVETS. REMOVED AND REPLACED KEEL BEAM SKIN PANEL IAW ER 15-5331-01040-JS2. 2 L 7 2 4F RT A16WE 2001032700235 20010327 00235 NM 2001 3 27 AWXA0001435 1 20010301 A 5330 6573748 SKIN BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 CRACK IN FUSELAGE SKIN AT FS 1153 RIGHT SIDE 12 INCHES ABOVE THE HORIZONTAL STABILIZER. REMOVED DAMAGED AREA AND INSTAL LED A REPAIR DOUBLER AND FILLER IAW SRM 53-30-03 FIG 2. 2 L 7 2 4F RT A16WE 2001032700236 20010327 00236 NM 2001 3 27 AWXA0001441 1 20010301 A 5320 693535214 TIE CLIP BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 CABIN STR CLIP AT FS 727B STR 8L IS CRACKED. REMOVED AND REPLACED STR CLIP IAW SRM 51-30-02 PG 5. 2 L 7 2 4F RT A16WE 2001032700237 20010327 00237 NM 2001 3 27 AWXA0001442 1 20010301 A 5320 693535214 TIE CLIP BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 CABIN STR CLIP AT FS 597 STR 8L IS CRACKED. REMOVED AND REPLACED STR CLIP IAW SRM 51-30-02 PG 5. 2 L 7 2 4F RT A16WE 2001032700238 20010327 00238 NM 2001 3 27 AWXA0001443 1 20010301 A 5330 655056323 SKIN BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 EXTERNAL SKIN CRACKED IN RADIUS AT L2 DOOR UPPER HINGE CUTOUT. INSTALLED SKIN REPAIR IAW SRM 53-30-03 AND 51-10-02. 2 L 7 2 4F RT A16WE 2001032700239 20010327 00239 NM 2001 3 27 AWXA0001444 1 20010301 A 5315 6546803 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 FLOORBEAM AT FS 520 LBL 24 HAS A 3 INCH CRACK IN UPPER RADIUS THAT HAS BEEN PREVIOUSLY STOP DRILLED. REMOVED EXISTING D OUBLERS AND INSTALLED REPAIR IAW AWA ER 15-5346-00354-JL1A AND SRM 51-30-02 PG 2 & 5. 2 L 7 2 4F RT A16WE 2001032700240 20010327 00240 NM 2001 3 27 AWXA0001445 1 20010301 A 5315 6546803 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 FLOORBEAM AT FS 520 LBL 44 HAS A 3 INCH CRACK IN UPPER RADIUS AND HAS BEEN PREVIOUSLY STOP DRILLED. REMOVED EXISTING DO UBLERS AND REPAIRED IAW AWA ER 15-5346-00354-JL1A AND SRM 51-30-02 PG 5. 2 L 7 2 4F RT A16WE 2001032700241 20010327 00241 NM 2001 3 27 AWXA0001446 1 20010301 A 5330 65458492 SKIN BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 R2 SERVICE DOOR UPPER HINGE LWR AFT CORNER OF CUTOUT HAS A .125 INCH CRACK. REMOVED FASTENERS, ROUTED OUT CRACK AND INS TALLED REPAIR DOUBLER IAW SRM 51-10-02 AND 51-30-02. 2 L 7 2 4F RT A16WE 2001032700242 20010327 00242 NM 2001 3 27 AWXA0001447 1 20010301 A 5313 BAC1498157 STRINGER BOEING 737 737277 1384570 NM FUSELAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 ELONGATED HOLES THRU SKIN AND STRINGER AT FS 760 STR 20R. REPAIRED MISDRILLED HOLES IAW AWA ER 15-5330-01049 DL2 AND SR M 53-10-03 FIG 1 AND 53-30-03 FIG 10. 2 L 7 2 4F RT A16WE 2001032700243 20010327 00243 NM 2001 3 27 AWXA0001448 1 20010301 A 5313 BAC1498157 STRINGER BOEING 737 737277 1384570 NM FUSELAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 ELONGATED HOLES THRU SKIN AND STRINGER AT FS 790 STR 20R. REPAIRED MISDRILLED HOLES IAW AWA ER 15-5330-01049-DL1 AND SR M 53-10-03 FIG 1 AND 53-30-03 FIG 10. 2 L 7 2 4F RT A16WE 2001032700244 20010327 00244 NM 2001 3 27 AWXA0001449 1 20010301 A 5330 6545775 SKIN BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 CRACK IN FUSELAGE SKIN RT BS 747 STR 17R. REPLACED FUSELAGE SKIN RT SIDE BS 727-817 STR 14R - 20R IAW AWA ER 15-5330-01 045-JS1 AND SRM 51-30-02 PG 2 AND 51-30-01 PG 2&3. 2 L 7 2 4F RT A16WE 2001032700245 20010327 00245 EU 2001 3 27 AWXA0001453 1 20010302 A 5270 DOOR AIRBUS 320 A320231 3930325 EU AFT CARGO BAY ICED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 629AW 076 DTW - ABORTED TAKEOFF - 2/26/01 - DURING TAKEOFF ROLL THE CREW GOT AN ECAM MESSAGE FOR THE AFT CARGO DOOR. THE TAKEOFF WAS ABORTED BELOW 60 KTS. THE AFT CARGO DOOR WAS INSPECTED AND AN ICE BUILDUP AROUND THE DOOR WAS FOUND. THE ICE WAS R EMOVED AND THE CARGO DOOR INDICATION CHECKED GOOD; NO FURTHER REPORTS HAVE BEEN NOTED. 2 L 7 2 4F RT A28NM 2001032700246 20010327 00246 NM 2001 3 27 AWXA0001454 1 20010302 A 3020 1726257 ANTI-ICE VALVE BOEING 737 73733A 1384673 NM NR 1 ENGINE FAILED A AWXA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 28 172AW 39438 1943 23631 PHX - AIR TURNBACK - 2/26/01 - EN ROUTE FROM PHX TO DEN WHEN THE LEFT ENGINE ANTI-ICE WAS SELECTED ON THE BLUE LIGHT REM AINED BRIGHT WITH NO INCREASE IN N2; THE AIRCRAFT RETURNED TO PHX. IN PHX MAINTENANCE TROUBLESHOT AND FOUND THE ANTI-IC E VALVE HAD FAILED IN THE CLOSED POSITION; THE LEFT ENGINE ANTI-ICE VALVE WAS REPLACED AND FUNCTIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2001032700247 20010327 00247 NM 2001 3 27 AWXA0001455 1 20010302 A 2612 899321 FIRE DETECTOR BOEING 737 7373G7 1384595 NM NR 1 ENGINE WILL NOT TEST A AWXA A UNSCHED LANDING L NO TEST CL CLIMB 1 WP 28 157AW 23779 PHX - AIR TURNBACK - 2/25/01 - DURING CLIMB AT 18,000 FT THE CREW PERFORMED AN ENGINE FIRE WARNING TEST; NEITHER ENGINE WOULD TEST PLUS THE FAULT LIGHT WAS ON. THE AIRCRAFT RETURNED TO PHX. ON GROUND THE ENGINE FIRE TEST WAS NORMAL; THE N R 1 ENG FIRE LOOP B HAD BEEN PLACED ON MEL 26-2 ON THE PREVIOUS FLIGHT. IN PHX MAINTENANCE RANG OUT THE WIRING FROM THE FIRE CONTROL MODULE TO THE FIRE PROTECTION BOX AND ALL CHECKS WERE GOOD. REMOVED AND TESTED NR 1 ENG STRUT DETECTOR AS SY AND FIRE DETECTOR ASSY, TESTED GOOD. BOTH WERE REPLACED AS PRECAUTION AND FUNCTIONAL TESTS WERE GOOD. DETECTOR ASSY P/N 472094 - LOCATION: NR 1 ENGINE. 2 L 7 2 4F RT A16WE 2001032700250 20010327 00250 NM 2001 3 27 F3LA200100038 1 20010227 A 5310 DOOR FRAME BOEING 737 7373S1 138447S NM AFT CARGO BAY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 3095 24856 DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT DOOR FRAME CORRODED AT STA 867. MAINTENANCE REMOVED SUPPORT ANGLE, INTERCOSTAL AND TRANSITION WEB AT STR 25R, STA 847 TO 867, AND CUT OUT DAMAGED PORTION OF FRAME. FABRICATED AND INSTALLED FRAME DOUBLER PER SRM 51-70-11 AND EA 53-737-114, FIG 2. INSTALLED NEW INTERCOSTAL AND SUPPORT ANGLE AND REI NSTALLED TRANSITION WEB PER EA 53-737-114. 2 L 7 2 4F RT A16WE 2001032700251 20010327 00251 NM 2001 3 27 F3LA200100039 1 20010227 A 5330 SKIN BOEING 737 7373S1 138447S NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 3095 24856 DURING C-4 CHECK, INSPECTION REPORTED INTERGRANULAR CORROSION ON INSIDE SKIN OF C2 DOOR CUTOUT, AFT LOWER CORNER. REMOV ED CORROSION ON BEAR STRAP PER SRM 51-10-02. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER AND TRIPLER P ER SRM 53-30-3, FIG 46, DETAIL 6. FABRICATED AND INSTALLED NEW SCUFF PLATE PER EA 53-737-114. 2 L 7 2 4F RT A16WE 2001032700252 20010327 00252 NM 2001 3 27 AWXA0001456 1 20010302 A 5312 65163007 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 PRESSURE WEB AT FS 178 RBL 5 HAS A 1 INCH CRACK. REMOVED FASTENERS; CUTOUT DAMAGED AREA; FABBED, LOCATED, DRILLED, INST ALLED FILLER AND DOUBLER IAW SRM 53-10-08. 2 L 7 2 4F RT A16WE 2001032700253 20010327 00253 NM 2001 3 27 AWXA0001457 1 20010302 A 5320 672038U1 INTERCOSTAL BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 FOUND INTERCOSTAL CRACKED AT FS 179 LBL 26 WL 195; CONFIRMED W/ HFEC. REMOVED INTERCOSTAL; LOCATED, DRILLED AND INSTALL ED NEW INTERCOSTAL IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001032700254 20010327 00254 NM 2001 3 27 AWXA0001458 1 20010302 A 5320 6720382 INTERCOSTAL BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 VISUAL INSPEC FOUND INTERCOSTAL CRACKED AT FS 179 RBL 26 WL 195. REMOVED ATTACH ANGLE AND DAMAGED INTERCOSTAL; FORMED, HEAT TREATED, DRILLED AND INSTALLED REPLACEMENT INTERCOSTAL IAW BOEING DWG 6-72038 AND SRM 51-40-02 PG 10; INSTALLED ATT ACH ANGLE IAW SRM 51-40-02 PG 10. 2 L 7 2 4F RT A16WE 2001032700256 20010327 00256 NM 2001 3 27 AWXA0001460 1 20010302 A 5320 6545833440 WEB BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 VISUAL INSPEC FOUND CRACK IN COCKPIT FLOOR WEB EMANATING FROM O/B EDGE TO LIGHTENING HOLE AT FS 178 - 181 RBL 29 WL 207; HFEC CONFIRMED. REMOVED CRACKED WEB; DRILLED AND INSTALLED NEW WEB IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001032700257 20010327 00257 NM 2001 3 27 AWXA0001461 1 20010302 A 5320 651758347 STIFFENER BOEING 737 7373S3 1384711 NM BULKHEAD CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 VISUAL INSPEC FOUND 1.25 INCH CRACK IN FS 178 BLKHD VERTICAL TEE AT LBL 5.7 WL 185; CONFIRMED HFEC. CUT OUT CRACKED ARE A OF FLANGE, HFEC VERIFIED CRACK CONTAINED W/I CUTOUT; FABBED REPAIR ANGLES, STRAP AND FILLER; TREATED, DRILLED AND INST ALLED IAW SRM 51-20-01, 51-20-05 AND 53-10-08 FIG 205. 2 L 7 2 4F RT A16WE 2001032700258 20010327 00258 NM 2001 3 27 AWXA0001462 1 20010302 A 5414 311A10001SP SKIN BOEING 737 7373S3 1384711 NM NR 1 PYLON CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 NR 1 PYLON SKIN CRACKED AT AFT LWR CORNER OF PNL 5724L OPENING. STOP DRILLED CRACK, HFEC CONFIRMED CRACK CONTAINED W/I STOP DRILL; INSTALLED DOUBLER IAW AWA EO 54-33-01. 2 L 7 2 4F RT A16WE 2001032700259 20010327 00259 NM 2001 3 27 AWXA0001464 1 20010302 A 5230 65C8073527 FRAME BOEING 737 7373S3 1384711 NM FWD CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 FWD CARGO DOOR INNER PAN CRACKED 4 INCHES IN LENGTH IN RADIUS AT FWD END OF DOOR AT LATCH ROLLER AREA. REMOVED AND REPL ACED FWD LWR FRAME OF CARGO COMPARTMENT DOOR IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001032700260 20010327 00260 NM 2001 3 27 AWXA0001465 1 20010302 A 5330 6552988 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 FUSELAGE SKIN GOUGED AT L2 DOOR CUTOUT AFT LWR CORNER. BLENDED AND TREATED AREA; FABBED, DRILLED, TREATED AND INSTALLED REPAIR DOUBLERS IAW SRM 53-60-01 FIG 203. 2 L 7 2 4F RT A16WE 2001032700261 20010327 00261 NM 2001 3 27 AWXA0001466 1 20010302 A 5330 6552988 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 FUSELAGE SKIN CRACKED AT L2 DOOR CUT OUT AT FWD LWR CORNER EMANATING FROM FASTENER AND RUNNING TO EDGE OF RADIUS. STOP DRILLED CRACK; CUT OUT ADJACENT DENTED AREA; FABBED REPAIR DOUBLERS AND FILLER; TREATED AND INSTALLED IAW AWA ER 03-5330 -0-1052-SS1 AND SRM 53-60-01, 51-20-01 AND 51-40-02. 2 L 7 2 4F RT A16WE 2001032700262 20010327 00262 NM 2001 3 27 SWAA010496 1 20010218 A 5330 6545773 DOUBLER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/2D CHECK, FOUND WINDOW BELT DOUBLER UPPER FWD CORNER OF WINDOW CUTOUTS CRACKED AT RT POSITIONS NR 1, 2, 6, 9, 10 & LT POSITIONS 1, 2, 4, 7, 8 & 10. REPAIRED WINDOWS CUTOUTS PER BFG ER, SRM & SWA SI. 2 L 7 2 4F A16WE 2001032700263 20010327 00263 NM 2001 3 27 SWAA010497 1 20010218 A 5330 6545773 DOUBLER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/2D CHECK, FOUND WINDOW BELT DOUBLER LOWER AFT CORNER OF WINDOW CUTOUTS CRACKED AT RT POSITIONS NR 3, 5, 8, & LT POSITIONS 2, 8 & 9. REPAIRED WINDOW CUTOUTS PER BFG ER, SRM & SWA SI. 2 L 7 2 4F A16WE 2001032700264 20010327 00264 NM 2001 3 27 SWAA010498 1 20010218 A 5330 6545773 DOUBLER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/2D CHECK, FOUND WINDOW BELT DOUBLER UPPER AFT CORNER OF WINDOW CUTOUTS CRACKED AT LT POSITIONS NR 26 & 28. REPAIRED WINDOW CUTOUTS PER BFG ER, SRM & SWA SI. 2 L 7 2 4F A16WE 2001032700265 20010327 00265 NM 2001 3 27 SWAA010499 1 20010218 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/2D CHECK, FOUND STRINGERS CRACKED, STR 13R, BS 417 & 477 & STR 13L, BS 514. REPAIRED STRINGERS PER B FG ER, SRM & SWA SI. 2 L 7 2 4F A16WE 2001032700266 20010327 00266 NM 2001 3 27 SWAA010500 1 20010219 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 379SW 26586 EEPLS TRACK COVER MISSING AT EXIT ROW. INSTALLED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001032700267 20010327 00267 NM 2001 3 27 SWAA010501 1 20010219 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 627SW 27935 EEPLS WIRING EXPOSED. REPLACED MISSING TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001032700268 20010327 00268 NM 2001 3 27 SWAA010502 1 20010219 A 2560 P4010021 BATTERY BOEING 737 737317 138447P NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 693SW 23174 LEFT AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001032700269 20010327 00269 NM 2001 3 27 SWAA010503 1 20010219 A 5311 6546529 FRAME BOEING 737 7373Q8 1384670 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 500D, 2 ABOVE STR 13R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001032700270 20010327 00270 NM 2001 3 27 SWAA010504 1 20010219 A 5310 6558280 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 13L & 14L. 2 L 7 2 4F RT A16WE 2001032700271 20010327 00271 NM 2001 3 27 SWAA010505 1 20010219 A 5311 BAC1514 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED D-CHECK, FOUND FWD SVC DOOR CUTOUT FWD UPPER FRAME CRACKED AT UPPER INBD RADIUS, BS 296.5, WL 274. REP AIRED UPPER FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001032700272 20010327 00272 NM 2001 3 27 SWAA010506 1 20010219 A 3350 BR2013 TRACK BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 EEPLS TRACK LOOSE AT ROW 12. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001032700273 20010327 00273 2001 3 27 SWAA010507 4 20010219 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 520SW 25319 FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001032700274 20010327 00274 NM 2001 3 27 SWAA010508 1 20010219 A 5330 6545857 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACKED AT AFT SVC DOOR LOWER FWD CUTOUT. REPAIRED SKIN PE R SRM. 2 L 7 2 4F RT A16WE 2001032700275 20010327 00275 2001 3 27 SWAA010509 4 20010219 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SVC DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 357SW 26594 FWD SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001032700276 20010327 00276 NM 2001 3 27 SWAA010510 1 20010220 A 5753 6546434 SKIN BOEING 737 7372T4 1384492 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED SERVICE CHECK, FOUND LT INBD T/E AFT FLAP OTBD EDGE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2 L 7 2 4F A16WE 2001032700277 20010327 00277 2001 3 27 SWAA010511 4 20010220 A 2565 1061323459 INDICATOR BOEING 737 7373H4 1384600 NM EVAC SLIDE OUT OF TOLERANCE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 327SW 23691 DURING SCHEDULED SERVICE CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF LIMITS. REMOVED AND REPL ACED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001032700278 20010327 00278 2001 3 27 SWAA010512 4 20010220 A 2565 1061323 INDICATOR BOEING 737 7373H4 1384600 NM EVAC SLIDE OUT OF TOLERANCE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 621SW 28037 DURING SCHEDULED A2 CHECK, FOUND AFT ENTRY & SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF LIMITS. REMOVED AND R EPLACED EVAC SLIDE ASSY''''S PER MM. 2 L 7 2 4F RT A16WE 2001032700279 20010327 00279 NM 2001 3 27 SWAA010513 1 20010220 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 638SW 27711 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS TRACK COVERS MISSING AT ROWS 16 & 18. INSTALLED TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 2001032700280 20010327 00280 NM 2001 3 27 SWAA010514 1 20010220 A 5712 BAC1520 RIB BOEING 737 7373Y0 1384671 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664WN 23495 DURING SCHEDULED SERVICE CHECK, FOUND 1.5 INCH CRACK IN LT WING LOWER RIB CHORD, WBL 135.5, AFT END, STRINGER 3. REPAIR ED LOWER CHORD PER SWA RA. 2 L 7 2 4F RT A16WE 2001032700281 20010327 00281 NM 2001 3 27 SWAA010515 1 20010220 A 5753 6546435 SKIN BOEING 737 7373Y0 1384671 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664WN 23495 DURING SCHEDULED SERVICE CHECK, FOUND LT WING OTBD T/E AFT FLAP DELAMINATED AT INBD END. REMOVED AND REPLACED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2001032700282 20010327 00282 2001 3 27 SWAA010516 4 20010220 A 2565 61621469 INDICATOR BOEING 737 7373A4 1384585 NM EVAC SLIDE OUT OF TOLERANCE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF LIMITS. REMOVED AND REPL ACED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001032700283 20010327 00283 NM 2001 3 27 SWAA010543 1 20010223 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 387SW 26602 EEPLS TRACK COVER DAMAGED AND WIRES EXPOSED AT ROW 20. REMOVED AND REPLACED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001032700284 20010327 00284 2001 3 27 SWAA010544 4 20010223 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SVC DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 643SW 27716 FWD SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001032700285 20010327 00285 NM 2001 3 27 SWAA010545 1 20010223 A 5610 571762322 WINDOW BOEING 737 7375H4 138449D NM COCKPIT CRACKED A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 511SW 24188 AIR TURNBACK - DURING CLIMB, R2 COCKPIT WINDOW CRACKED. REMOVED AND REPLACED R2 WINDOW & WINDOW HEAT CONTROLLER PER MM. OPS CHECK GOOD PER MM. 2 L 7 2 4F RT A16WE 2001032700286 20010327 00286 NM 2001 3 27 SWAA010546 1 20010223 A 5315 6546529 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CRACKED AT BS 400, RBL 14. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2001032700287 20010327 00287 NM 2001 3 27 SWAA010547 1 20010223 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 622SW 27932 DURING SCHEDULED 1/2D CHECK, FOUND STR CLIP CRACKED AT BS 580, STR 11R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001032700288 20010327 00288 NM 2001 3 27 SWAA010548 1 20010223 A 3350 65C34691 LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 513SW 24190 DURING SCHEDULED D-CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHTS LOOSE AT ROWS 9 & 11 DEF. SECURED LIGHT ASSY''S PER MM. 2 L 7 2 4F RT A16WE 2001032700289 20010327 00289 NM 2001 3 27 SWAA010549 1 20010223 A 5754 114A110 RIB BOEING 737 7377H4 NM LT KRUEGER FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 707SA 27841 DURING SCHEDULED C1 CHECK, FOUND LT WING L/E OUTBD KRUEGER FLAP RIB CRACKED AT THIRD RIB FROM OUTBD END. REMOVED AND RE PLACED KRUEGER FLAP PER MM. 2 L 7 2 4F RT A16WE 2001032700290 20010327 00290 NM 2001 3 27 SWAA010550 1 20010223 A 3397 WIRE BOEING 737 7377H4 1384404 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 710SW 27844 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT MID CABIN. RECONNECTED WIRING PER MM. 2 L 7 2 4F RT A16WE 2001032700291 20010327 00291 NM 2001 3 27 SWAA010551 1 20010223 A 3350 300432 LIGHT BOEING 737 7377H4 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 794SW 30605 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EXTERNAL EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001032700292 20010327 00292 NM 2001 3 27 SWAA010552 1 20010223 A 3350 6104781 BATTERY PACK BOEING 737 7377H4 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 794SW 30605 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EXTERNAL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2001032700293 20010327 00293 NM 2001 3 27 SWAA010553 1 20010224 A 3350 65C34691 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 3 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2001032700294 20010327 00294 NM 2001 3 27 SWAA010554 1 20010224 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED C1 CHECK, FOUND 1.75 EXTERNAL FUSELAGE SKIN CRACK AT BS 494, STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001032700295 20010327 00295 2001 3 27 SWAA010555 4 20010223 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001032700296 20010327 00296 2001 3 27 SWAA010556 4 20010223 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT SVC DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001032700297 20010327 00297 NM 2001 3 27 SWAA010557 1 20010224 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 706SW 27840 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS TRACK COVER MISSING AT ROW 8. INSTALLED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001032700298 20010327 00298 NM 2001 3 27 SWAA010558 1 20010225 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME ANGLE CORRODED AT BS 500D, STR 27R. REMOVED AND REPLACED FRAME ANGLE PER SRM. 2 L 7 2 4F RT A16WE 2001032700299 20010327 00299 2001 3 27 SWAA010559 4 20010224 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 651SW 27721 AFT ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001032700300 20010327 00300 NM 2001 3 27 SWAA010560 1 20010223 A 3097 07622 WIRE BOEING 737 7373A4 1384585 NM COCKPIT LOOSE A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 678AA 23290 AIR TURNBACK - DURING CRUISE, R1 COCKPIT WINDOW OVERHEAT LIGHT ILLUMINATED AND C/B TRIPPED. RETURNED TO PHX DUE TO DEST INATION WEATHER. FOUND R1 WINDOW OVERHEAT SENSOR WIRE LOOSE. SECURED WIRE PER MM. 2 L 7 2 4F RT A16WE 2001032700301 20010327 00301 NM 2001 3 27 SWAA010561 1 20010223 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 362SW 26573 DURING SCHEDULED C2 CHECK, FOUND 2 EXTERNAL FUSELAGE SKIN CREASES, 5 TO 6 INCHES LENGTH, AT BS 440 & 470, BETWEEN STR 25 R & 26R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001032700302 20010327 00302 NM 2001 3 27 SWAA010534 1 20010221 A 5753 6546435 SKIN BOEING 737 7372H4 138448C NM LT T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 063SW 22061 DURING SCHEDULED SERVICE CHECK, FOUND LT WING T/E OUTBD AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2 L 7 2 4F A16WE 2001032700303 20010327 00303 NM 2001 3 27 SWAA010535 1 20010222 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND STR 27R CORRODED AT BS 500D. REPAIRED STR PER SRM. 2 L 7 2 4F RT A16WE 2001032700304 20010327 00304 NM 2001 3 27 SWAA010536 1 20010221 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM LOWER LT CHORD CORRODED AT BS 500D + 4. REPAIRED KEEL BEAM PER SRM. 2 L 7 2 4F RT A16WE 2001032700305 20010327 00305 NM 2001 3 27 SWAA010537 1 20010222 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND 2 BS 178 BULKHEAD WEB CRACK, BEHIND DOUBLER, AT RBL 5.9, WL 201. REPAIRED BULKHEAD W EB PER SRM. 2 L 7 2 4F RT A16WE 2001032700306 20010327 00306 NM 2001 3 27 SWAA010538 1 20010221 A 3350 65C34691 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED C4 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2001032700307 20010327 00307 2001 3 27 SWAA010539 4 20010221 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM AFT SVC DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 501SW 24178 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001032700308 20010327 00308 NM 2001 3 27 SWAA010540 1 20010221 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 391SW 27378 DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVERS BROKEN AT ROWS 2 & 13. REMOVED AND REPLACED TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 2001032700309 20010327 00309 NM 2001 3 27 SWAA010541 1 20010222 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 362SW 26573 DURING SCHEDULED PM CHECK, FOUND EEPLS LOOSE THROUGHOUT CABIN. INSTALLED EEPLS SPACERS PER MM. 2 L 7 2 4F RT A16WE 2001032700310 20010327 00310 NM 2001 3 27 SWAA010542 1 20010222 A 5320 6517583 BEAM BOEING 737 7373H4 1384600 NM BULKHEAD DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM LOWER WEB DAMAGED AT RBL 5.7, WL 187. REPAIRED VERTICA L BEAM WEB PER SWA RA. 2 L 7 2 4F RT A16WE 2001032700311 20010327 00311 NM 2001 3 27 SWAA010517 1 20010221 A 3350 BR2013 RECEPTACLE BOEING 737 7373H4 1384600 NM CABIN DEFECTIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 379SW 26586 EEPLS INOP BETWEEN ROWS 10 & 13. REMOVED AND REPLACED EEPLS RECEPTICAL PER MM. 2 L 7 2 4F RT A16WE 2001032700312 20010327 00312 NM 2001 3 27 SWAA010518 1 20010221 A 2560 P2070001 FLASHLIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 671SW 23785 FWD OUTBD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2001032700313 20010327 00313 SO 2001 3 27 SWIA972405 1 20010301 A 2752 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FLAP ACTUATOR DIRTY A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 194SW 120120 ON APPROACH INBOARD FLAP PAIRS STUCK AT 25 DEGREES. UABLE TO RAISE OR LOWER INBOARD FLAPS WITH FLAP HANDLE. CLEANED IN BOARD FLAP ACTUATOR CANNON PLUGS AND RERACKED FCU. OPS CHECK NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032700314 20010327 00314 SO 2001 3 27 SWIA972406 1 20010304 A 2731 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE ELEVATOR TRIM FROZEN A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 226SW 120296 ELEVATOR TRIM FROZE INFLIGHT. FREE MOVEMENT AFTER DESCENT TO 17,000. -09 DEG C. INSTALLED SERVICEABLE ELEVATOR TRIM LINEAR ACTUATORS. RIGHT S/N ON: 860, S/N OFF: 682. LEFT S/N ON: 800, S/N OFF: 681. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032700315 20010327 00315 SO 2001 3 27 SWIA972407 1 20010303 A 2752 WIRE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FLAP ACTUATOR BROKEN A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 291SW 120318 CONTROL FAULT OUTBOARD PAIR WILL NOT RESET. FAULT OCCURS WHEN SELECTING 15 DEGREES. FOUND TWO BROKEN WIRES AT LEFT OUT BOARD FLAP ACTUATOR. REPAIRED AS NEEDED. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032700317 20010327 00317 NE 2001 3 27 SWIA972409 2 20010302 A 7321 ENGINE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE OUT OF ADJ A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 209SW 120269 LEFT ENGINE SPOOLED UP TO 30 PERCENT ON TAKEOFF THEN HUNG AT 30 PERCENT. ABORTED TAKEOFF. DEFERRED EEC. FOUND LEFT EN GINE OUT OF TRIM. TRIMMED ENGINE IAW MM 71-00-00. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032700318 20010327 00318 SO 2001 3 27 SWIA972410 1 20010227 A 5270 SWITCH EMB 120 EMB120RT SO PWA 118 PW118 NE FUEL DOOR OUT OF ADJ A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 269UE 120194 SERVICE DOOR LIGHT ILLUMINATED AGAIN ON TAKEOFF ROLL. REMOVED AND REPLACED SERVICE DOOR LIGHT INDICATOR. INSPECTED SER VICE DOOR MICROSWITCH WIRING FOUND TO BE NORMAL. ADJUSTED OUTBOARD FUEL DOOR MICROSWITCH. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032700319 20010327 00319 SO 2001 3 27 SWIA972411 1 20010228 A 5310 STRUCTURE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FUSELAGE VIBRATES A SWIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 NM 07 189SW 120048 HIGH FREQUENCY VIBRATION AND A LOWER FREQUENCY RUMBLING NOISE INFLIGHT. CHECKED PROP SYNC, FLAPS AND GEAR INFLIGHT. AL L INDICATIONS NORMAL. PHENOMENON WENT AWAY WITH GEAR DOWN. INSPECTED AIRCRAFT FOR ABNORMALITIES IN AIRSTREAM GEAR AND GEAR DOOR OPERATIONS. FOUND NORMAL. NO DISCREPANCIES FOUND. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032700320 20010327 00320 SO 2001 3 27 C2XA01IA143 1 20010227 A 2121 4611028900 FAN EMB 145 EMB145LR SO CABIN INOPERATIVE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 13964 145123 EWR - FLIGHT 4148, THE CREW REPORTED THAT DURING THE IN-FLIGHT PORTION OF THE ICE TEST THE CABIN BEGAN TO FILL WITH SMOK E AND A STRONG ODOR. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT WHERE MAINTENANCE PLACED THE NUMBER TWO RECIRCULATION FAN ON MEL 21-24-01 CONTROL NR 007600, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH ON 03/03/01 WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO RECIRCULATION FAN, REMOVED THE MEL, AND THE AIRCRAFT W AS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001032700322 20010327 00322 EU 2001 3 27 QXEA0100225 1 20010304 A 3350 55159000004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 483US 11233 PDX- EMERGENCY EXIT DSIGN OVER GALLEY HAS BULBS INOPERATIVE. REPLACED CIRCUIT CARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001032700323 20010327 00323 EU 2001 3 27 QXEA0100226 1 20010225 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487US 11238 PDX- CENTER EMERGENCY SIGN LIGHT BULBS INOPERATIVE. REMOVED AND REPLACED TWO LIGHT PANELS. OPERATIONAL CHECKS GOOD. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001032700324 20010327 00324 NM 2001 3 27 AWXA0001479 1 20010306 A 2120 654957117 DUCT BOEING 737 737277 1384570 NM A/C BAY DETERIORATED A AWXA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 28 187AW 22654 LAS - DIVERTED FLIGHT - 2/27/01 - EN ROUTE FROM RNO TO PHX THE AIRCRAFT EXPERIENCED AIRFRAME VIBRATIONS THAT WERE NOTICE D IN THE COCKPIT AND AFT GALLEY; THE CREW FELT IT IN THE CONTROL WHEEL AND RUDDER PEDALS. IT INCREASED IN FREQUENCY FRO M 230 KTS TO .77 MACH. THE FLIGHT WAS DIVERTED TO LAS. IN LAS A VISUAL INSPECTION WAS PERFORMED ON THE RUDDER, ELEVATO RS, TABS, RUDDER PCU ATTACH POINTS, INPUT RODS, STANDBY ACTUATOR AND ATTACH POINTS, AFT FUSELAGE AREA, DOORS, PANELS AND VORTEX GENERATORS; ALL WERE GOOD. REPLACED YAW DAMPER COUPLER AS A PRECAUTION. THE AIRCRAFT WAS REPOSITIONED TO PHX. 2 L 7 2 4F RT A16WE 2001032700325 20010327 00325 NM 2001 3 27 AWXA0001480 1 20010306 A 2120 654957117 DUCT BOEING 737 737277 1384570 NM A/C BAY DETERIORATED A AWXA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 28 187AW 22654 EN ROUTE TO PHX, ONCE AGAIN EXPERIENCED A VIBRATION. IN PHX ADDITIONAL CHECKS WERE PERFORMED TO THE RUDDER SYSTEM; THE STANDBY RUDDER FAIL AMM TEST 27-21-141 STEP 2B; THE STANDBY RUDDER DEAD BAND WAS ADJUSTED IN LIMITS PER AMM 27-21-14-1. THE PROBLEM CAUSING THE VIBRATION WAS ISOLATED TO THE LT AIR CONDITIONING HEAT EXCHANGER EXHAUST DUCT WHICH WAS BADLY D ETERIORATED. REPLACED DUCT AND NO FURTHER PROBLEMS HAVE BEEN REPORTED. 2 L 7 2 4F RT A16WE 2001032700326 20010327 00326 WP 2001 3 27 UPS01835197 1 20010306 A 2900 HYDRAULIC SYSTEM DOUG DC8 DC873F 302199F WP FUSELAGE LEAKING A IPXA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 874UP 46074 INSPECTION TYPE:N/A, HYD QTY LOSS IN FLT. 2 L 7 4 4F RT 4A25 2001032700327 20010327 00327 NM 2001 3 27 AWXA0001467 1 20010305 A 5312 65163007 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 CENTER WEB CRACKED AT FS 178 RBL 5.0 WL 198 WL 202. CUT OUT (2) CRACKS IAW SRM 53-10-08, NDT NO CRACKS. FABBED AND INS TALLED REPAIR PARTS IAW SRM 53-10-08; TOP COAT APPLIED. 2 L 7 2 4F RT A16WE 2001032700328 20010327 00328 NM 2001 3 27 AWXA0001468 1 20010305 A 5312 65163007 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 CENTER WEB CRACKED STA 178 LBL 5.0 WL 198 AND 202. CUT OUT (2) CRACKS IAW SRM 53-10-08, NDT NO CRACKS. FABBED AND INST ALLED (1) DOUBLER AND (3) FILLERS IAW SRM 53-10-08. 2 L 7 2 4F RT A16WE 2001032700329 20010327 00329 NM 2001 3 27 AWXA0001469 1 20010305 A 5320 69353501 TIE CLIP BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 AFT CARGO COMPT STA 773 LONG 26R HAS CRACKED TIE CLIP. REMOVED AND REPLACED TIE CLIP IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001032700330 20010327 00330 NM 2001 3 27 AWXA0001470 1 20010305 A 5230 WEB BOEING 737 7373S3 1384711 NM AFT CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 AFT CARGO DOOR WEB CUTOUT FOR THE ROD END IS CRACKED. STOP DRILLED CRACK IAW SRM 51-40-13; HFEC INSP IAW NTM PT.6 51-00 -00 FIG 23. CRACK TERMINATED AT STOP DRILL; FABBED AND INSTALLED REPAIR DOUBLER ON AFT CARGO DOOR INNER WEB CUTOUT FOR LATCH ROD END IAW SRM 51-70-13 AND 51-40-02. 2 L 7 2 4F RT A16WE 2001032700331 20010327 00331 NM 2001 3 27 AWXA0001471 1 20010305 A 5320 654583340 WEB BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 FLOOR WEB CRACKED AT FS 180 RBL 26 WL 207. REMOVED DAMAGED WEB IAW SRM 51-40-02; FABBED NEW WEB IAW DWG 65-45833; INSTA LLED NEW WEB IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001032700332 20010327 00332 NM 2001 3 27 AWXA0001472 1 20010305 A 5320 654583340 WEB BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 FLOOR WEB CRACKED FS 180 LBL 26 WL 207. REMOVED DAMAGED WEB IAW SRM 51-40-02; FABBED NEW WEB IAW DWG 65-45833; INSTALLE D NEW WEB IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001032700333 20010327 00333 NM 2001 3 27 AWXA0001473 1 20010305 A 5312 65163007 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 CENTER WEB CRACKED FS 178 WL 202 RBL 6.0. STOP DRILLED CRACK IAW SRM 53-10-08 FIG 209; NDT IAW NTM PT 6 51-00-00. CRAC K TERMINATED; REPAIR PARTS FABBED AND INSTALLED IAW SRM 53-10-08. 2 L 7 2 4F RT A16WE 2001032700334 20010327 00334 NM 2001 3 27 AWXA0001474 1 20010305 A 5312 65163007 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 CENTER WEB CRACKED FS 178 WL 202 LBL 6.0. STOP DRILLED CRACK IAW SRM 53-10-08 FIG 209; NDT IAW NTM PT 6 51-00-00. STOP DRILL TERMINATED CRACK; REPAIR PARTS FABBED AND INSTALLED IAW SRM 53-10-08. 2 L 7 2 4F RT A16WE 2001032700335 20010327 00335 NM 2001 3 27 AWXA0001475 1 20010305 A 5330 65293816 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 FUSELAGE SKIN AT L1 DOOR CUTOUT HAS CRACK EMANATING FROM FASTENER HOLE INTO RADIUS OF JAMB. REPAIRED CRACK IAW AWA ER 0 3-5310-01059-JS1 AND DWG 65C27257-5. 2 L 7 2 4F RT A16WE 2001032700336 20010327 00336 NM 2001 3 27 AWXA0001476 1 20010305 A 5330 65293816 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 FUSELAGE SKIN AT L1 DOOR CUTOUT HAS NUMEROUS GOUGES AT FWD LWR CORNER. REPAIRED AREA IAW AWA ER 03-5310-01059-JS1 AND D WG 65C27257-5. 2 L 7 2 4F RT A16WE 2001032700337 20010327 00337 NM 2001 3 27 AWXA0001477 1 20010305 A 5210 143N61004 SKIN BOEING 757 7572S7 1384962 NM L2 DOOR DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 905AW 23567 L2 DOOR FWD LWR CORNER EDGE SKIN HAS 2 DENTS. CUT OUT DAMAGED SKIN; NDT - NO CRACKS. FABBED DOUBLER AND FILLER IAW SRM 52-10-01; INSTALLED REPAIR PARTS IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2001032700338 20010327 00338 NM 2001 3 27 AWXA0001478 1 20010305 A 5313 143N3110 STRINGER BOEING 757 7572S7 1384962 NM FUSELAGE DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 905AW 23567 AFTER REMOVING DOUBLER AT STA 626 STR 16L FOUND STR 16L DENTED AND CREASED. CUT OUT DAMAGE; FABBED AND INSTALLED REPAIR SPLICE IAW SRM 53-00-03 FIG 201. 2 L 7 2 4F RT A2NM 2001050300225 20010503 00225 NE 2001 5 3 QXEA0100227 2 20010306 A 7200 312103101 BEARING PRATT PW120A DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 2 ENGINE FAILED A QXEA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. E B J VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 NM 09 822PH 9466 PCE120412 106 PCE120412 851116 PDX - ON APPROACH TO PDX AN INCREASING ITT ON NR 2 ENGINE NOTED ALONG WITH VIBRATION. AFTER GEAR AND FLAP EXTENSION SMO KE SMELL NOTED. DECLARED AN EMERGENCY. AFTER LANDING TOWER ADVISED SMOKE ON NR 2 ENGINE. THE FIRE/SHUTDOWN ON GROUND CHECKLIST WAS CONDUCTED. REMOVED AND REPLACED PROP AND ENGINE. ENGINE TORN DOWN AT PWC. DISTRESS DAMAGE OBSERVED ON N R 5 BEARING. THE LIKELIHOOD OF BEARING DISTRESS WAS FROM WEAR DAMAGE ON THE BEARING FROM LOSS OF OIL PRESSURE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001032700339 20010327 00339 NM 2001 3 27 SWAA010665 1 20010305 A 2170 1808494 COALESCER BAG BOEING 737 7373H4 1384600 NM A/C BAY DIRTY A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 07 335SW 23939 AIR TURNBACK. SMOKE AND FUMES IN CABIN. FOUND WATER SEPARATOR BAGS DIRTY. REMOVED AND REPLACED BAGS AND RAN BOTH ENGI NES AT 75 PERCENT N1 FOR 10 MINS. NO SMOKE OR FUMES NOTED. REPLACED WATER SEPARATOR BAGS AGAIN FOR MX CONVENIENCE OP'' S CHECK GOOD PER MM. 2 L 7 2 4F RT A16WE 2001032700340 20010327 00340 EU 2001 3 27 C2XA01CL049 1 20010306 A 2120 SMOKE AEROSP ATR42 ATR42320 8680930 EU COCKPIT DETECTED A C2XA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 14834 193 CLE FLIGHT 3147 THE CREW REPORTED A BURNING SMELL AND SMOKE IN COCKPIT AFTER STARTING NR 1 ENGINE AND GOING TO MAX RPM. THE ENGINE WAS SHUT DOWN. MAINTENANCE INSPECTED AND STARTED THE NR 1 ENGINE AND RAN NR 1 PACK BOTH FULL HOT AND COLD W ITH ENGINE AT MAX RPM. NO SMOKE OR BURNING SMELL WAS NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A53EU 2001032700341 20010327 00341 SO 2001 3 27 C2XA01TY028 1 20010305 A 3350 GE1317 LIGHT EMB 145 EMB145LR SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18982 145223 TYS DURING A SCHEDULED INSPECTION THE LEFT HAND OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANC E REMOVED AND REPLACED THE LEFT HAND OVERWING EMERGENCY EXIT LIGHT BULB IAW EMB-145 MM 33-50-10. OPERATIONAL CHECKS WER E SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001032700342 20010327 00342 SO 2001 3 27 C2XA01TY029 1 20010306 A 3350 3025101 LIGHT EMB 145 EMB145LR SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14950 145061 TYS DURING A SCHEDULED INSPECTION THE FORWARD RIGHT HAND EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD RIGHT HAND EMERGENCY EXIT LIGHT ASSEMBLY IAW EMB-145 MM 33-50-10. OPERATIONAL CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001041600285 20010416 00285 NM 2001 4 16 2001UALA00163 1 20010227 A 2910 7321161002 MODULE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE HYD SYSTEM LEAKING A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 797UA 26924 STRONG ODOR DETECTED IN COCKPIT DURING CRUISE WHEN UPPER RECIRCULATING FAN IS TURNED OFF. ODOR GOES AWAY QUICKLY WHEN FAN IS TURNED BACK ON. LOWER FAN OK. SUPPLEMENTAL DATA UPDATE THE PROBLEM WAS DUE TO FAULTY RT HYDRAULIC PNEUMATIC PRES SURIZATION MODULE. THE PNEUMATIC DUCTING WAS CONTAMINATED BECAUSE THIS UNIT WAS ALLOWING A SMALL AMOUNT OF HYDRAULIC FL UID PASS THROUGH THE CHECK VALVE. THE MODULE WAS REPLACED, AND A VERY THOROUGH PNEUMATIC DUCTING AND PACK BURNOUT WAS A CCOMPLISHED. AIRCRAFT WAS RETURNED TO SERVICE WITHOUT FURTHER ODOR COMPLAINTS. THE ABOVE IS ALSO THE RESPONSE TO MRR NU MBER 2001UALA00216. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001032700343 20010327 00343 NE 2001 3 27 ARWA0010301 2 20010303 A 7200 ENGINE LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B02 54555 NE NR 1 ENGINE VIBRATION A ARWA E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 19 308GB 193U1133 NR 1 ENGINE SHUTDOWN IN FLIGHT AND RETURNED TO MIAMI DUE TO 2.5 SPIKE ON VIBRATION, BOTH CHANNELS IN THE LOW RANGE. REM OVED AND INSPECTED MASTER INTERNAL GEARBOX CHIP DETECTORS IAW 72-01-00, NO EVIDENCE OF INTERNAL FAILURE FOUND. VISUALLY INSPECTED AIR INLET LOW PRESS COMPRESSOR AND EXHAUST, NO EVIDENCE OF FOD. CLEANED AND LUBRICATE CLAPPERS IAW MM 72-31- 05. PERFORMED VIBRATION SURVEY TEST NR 11 IAW 71-00-00 VIBRATION WITHIN LIMITS CHECK OK. 2 L 7 3 4F 4 F A23WE E12EU 2001032700344 20010327 00344 WP 2001 3 27 ARWA0010302 1 20010303 A 3260 008004006 CONTROL BOX DOUG DC8 DC861 3021952 WP MLG FAILED A ARWA O OTHER J WARNING INDICATION AP APPROACH 1 SO 19 29UA 46159 ON GEAR DOWN HAD NO RIGHT MAIN GEAR GREEN LIGHT AND HAD GEAR NOT LATCHED AND DOOR NOT LATCHED RED LIGHTS ON. EMERGENCY CHECK LIST ACCOMPLISHED PLUS SEVERAL CYCLES. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED PROXIMITY SWITCH CONTROL BOX . INDICATION SYSTEM WORK NORMAL IAW 32-60-0. PERFORMED LANDING GEAR EXTENSION AND RETRACTION IAW 32-30-1, FOUND ALL IN DICATION NORMAL. 2 L 7 4 4F 4A25 2001032700345 20010327 00345 NM 2001 3 27 QXEA0100228 1 20010225 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 PDX- A 2 INCH LONG CRACK IN VERTICAL, RIGHT HAND SIDE OF AIRCRAFT, 3.5 AFT OF X 97.3 BELOW 2112. REPAIRED IAW DHC-8 SRM 51-40-00, AND 51-40-11, 2 H 7 2 4T RT A13NM 2001032700346 20010327 00346 NM 2001 3 27 QXEA0100229 1 20010216 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 PDX- LEFT HAND INBOARD SEAT TRACK CORROSION AT FRAME 545.000. REPAIRED IAW DHC-8 RD8-53-1339. 2 H 7 2 4T RT A13NM 2001032700347 20010327 00347 NM 2001 3 27 QXEA0100230 1 20010216 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 PDX- LEFT HAND INBOARD SEAT TRACK CORROSION AT X515.00. REPAIRED IAW DHC-8 RD8-83-1339. 2 H 7 2 4T RT A13NM 2001032700348 20010327 00348 NM 2001 3 27 QXEA0100231 1 20010216 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 PDX- LEFT HAND SEAT TRACK CORROSION AT X542.00. REPAIRED IAW DHC-8 RD8-53-1342. 2 H 7 2 4T RT A13NM 2001032700349 20010327 00349 NM 2001 3 27 QXEA0100232 1 20010216 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 PDX- LEFT HAND INBOARD SEAT TRACK CORROSION AT X390.00. REPAIRED IAW DHC-8 RD8-53-1339. 2 H 7 2 4T RT A13NM 2001032700350 20010327 00350 NM 2001 3 27 QXEA0100233 1 20010216 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 PDX- LEFT HAND INBOARD SEAT TRACK CORROSION AT X361.00. REPAIRED IAW DHC-8 RD8-53-1339. 2 H 7 2 4T RT A13NM 2001032700351 20010327 00351 NM 2001 3 27 QXEA0100235 1 20010216 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 PDX- RIGHT HAND OUTBOARD SEAT TRACK CORROSION AT X456.00. REPAIRED IAW DHC-8 RD8-53-1342. 2 H 7 2 4T RT A13NM 2001032700352 20010327 00352 NM 2001 3 27 QXEA0100236 1 20010216 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 PDX- RIGHT HAND INBOARD SEAT TRACK CORROSION AT X520.00. REPAIRED IAW DHC-8 RD8-53-1339. 2 H 7 2 4T RT A13NM 2001032700353 20010327 00353 NM 2001 3 27 QXEA0100237 1 20010216 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 PDX- RIGHT HAND INBOARD SEAT TRACK CORROSION AT X485.00. REPAIRED IAW DHC-8 RD8-53-1339. 2 H 7 2 4T RT A13NM 2001032700354 20010327 00354 NM 2001 3 27 QXEA0100238 1 20010216 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 PDX- RIGHT HAND INBOARD SEAT TRACK CORROSION AT X500.00. REPAIRED IAW DHC-8 RD8-53-1339. 2 H 7 2 4T RT A13NM 2001032700355 20010327 00355 NM 2001 3 27 QXEA0100239 1 20010225 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 PDX- FRAME 545.00 CHAFED BY FLOORBOARD Y40.00 RIGHT HAND. REPAIRED IAW HORIZON AIR EA 9-53-604. 2 H 7 2 4T RT A13NM 2001032700356 20010327 00356 NM 2001 3 27 QXEA0100240 1 20010216 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 PDX- LEFT HAND OUTBOARD SEAT TRACK CORROSION AT X518.00. REPAIRED IAW DHC-8 RD8-53-1342. 2 H 7 2 4T RT A13NM 2001032700357 20010327 00357 NM 2001 3 27 QXEA0100241 1 20010217 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 PDX- RIGHT HAND FORWARD OUTBOARD SEAT TRACK STA 262-429 WORN BEYOND LIMITS. REPAIRED IAW DHC-8 SRM 51-40-11 AND SRM 51- 40-00. 2 H 7 2 4T RT A13NM 2001032700358 20010327 00358 NM 2001 3 27 QXEA0100242 1 20010220 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 PDX- RIGHT HAND INBOARD SEAT TRACK STATION 182-424 WORN BEYOND LIMITS. REPAIRED IAW DHC-8 SRM 51-40-11 AND HORIZON AIR EA 9-53-599. 2 H 7 2 4T RT A13NM 2001032700359 20010327 00359 NM 2001 3 27 QXEA0100243 1 20010217 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 PDX- LEFT HAND OUTBOARD SEAT TRACK STATION 262-429 WORN BEYOND LIMITS. REPAIRED IAW DHC-8 51-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001032700360 20010327 00360 NM 2001 3 27 QXEA0100244 1 20010218 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 PDX- LEFT HAND OUTBOARD SEAT TRACK STATION 429-504 WORN BEYOND LIMITS. REPAIRED IAW DHC-8 SRM 51-40-00 AND SRM 51-40-11 . 2 H 7 2 4T RT A13NM 2001032700361 20010327 00361 NM 2001 3 27 QXEA0100245 1 20010219 A 2701 YOKE DHAV DHC8 DHC8102 2809003 NM COCKPIT CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 PDX- RIGHT HAND YOKE, RIGHT HAND AFT EDGE IS BEING CHAFED BY THE HYDRAULIC STANDBY PUMP BLUE FLEX LINE. 2 H 7 2 4T RT A13NM 2001032700362 20010327 00362 NM 2001 3 27 QXEA0100246 1 20010305 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY MALFUNCTIONED A QXEA K NONE N FALSE WARNING UK UNKNOWN 1 NM 09 369PH 3682 2746 513 PDX- FLIGHT ATTENDANT SMELLS FUEL. SMOKE WARNING LIGHT ILLUMINATED OCCASIONALLY FOR A FEW SECONDS AT A TIME. REMOVED A ND REPLACED FORWARD AND AFT BAGGAGE SMOKE DETECTORS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001032700363 20010327 00363 EU 2001 3 27 QXEA0100247 1 20010305 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 BOI- EVACUATION EXIT LIGHT SIGN IS BROKEN ABOVE SEAT 9. REMOVED AND REPLACED SIGN ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001032700364 20010327 00364 EU 2001 3 27 QXEA0100248 1 20010301 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 492US 11159 SEA- EMERGENCY EXIT SIGN ABOVE COCKPIT DOOR HAS SEVERAL INOPERATIVE BULBS. REPLACED LAMP CARD. OPERATIONAL CHECKS GOOD . AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001032700365 20010327 00365 SO 2001 3 27 SWIA972412 1 20010205 A 7931 WARNING LIGHT EMB 120 EMB120RT SO PWA 118 PW118 NE COCKPIT ILLUMINATED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 156CA 120156 LEFT OIL PRESSURE LIGHT ILLUMINATED CLIMBING THROUGH 16,500 FEET. FOLLOWED QRH PROCEDURES RETURNED BACK TO SBA. LIGHT EXTINGUISH THEREAFTER. INSPECTED LEFT ENGINE, SERVICED ENGINE OIL, CLEANED CANNON PLUG ON OIL PRESS SWITCH AND RAN ENGI NE AT 100 PERCENT TORQUE FOR 15 MINUTES. ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032700366 20010327 00366 SO 2001 3 27 SWIA972413 1 20010225 A 3010 EJECTOR VALVE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE DEICE SYSTEM FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 196SW 120151 VERTICAL FIN LEADING EDGE DEICE INOP. FAILED AIRBORNE. REMOVED AND REPLACED DEICE EJECTOR VALVE IAW 30-20-04. OPS CHE CK GOOD. P/N 3D2376-06, S/N ON PM878, OFF PM805. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032700367 20010327 00367 SO 2001 3 27 SWIA972414 1 20010225 A 2750 WARNING LIGHT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT ILLUMINATED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 195SW 120127 CONTROL FAULT LIGHT ILLUMINATED IN FLIGHT. WOULD RESET MOMENTARILY BUT ALWAYS CAME BACK. SECOND LIGHT BAR ON FLAP ANNU NCIATOR OUTBOARD PAIR ILLUMINATED. DIVERTED TO TWF FROM SUN. REWIRED RIGHT FLAP SYSTEM FROM WING TO FUSELAGE - INBOARD FLAP ACTUATORS, OUTBOARD FLAP ACTUATOR AND NACELLE FLAP ACTUATOR IAW STANDARD PRACTICES WMM 20-00-00 AND WMM 27-51-00. RAN FLAPS, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032700369 20010327 00369 SO 2001 3 27 SWIA972416 1 20010216 A 5270 PLATE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CARGO DOOR OUT OF ADJ A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 290SW 120317 CARGO DOOR WARNING LIGHT ILLUMINATED JUST AFTER TAKEOFF. RETURNED TO FRESNO. ADJUSTED MICROSWITCH STRIKE PLATE AND RES ET CIRCUIT BREAKER IN RIGGING BAY. OPS TEST DOOR LIGHT AND WARNING GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032700370 20010327 00370 SO 2001 3 27 SWIA972417 1 20010301 A 3150 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT FALSE ACTIVATION A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 579SW 120347 TAKEOFF TRIM FAIL AURAL WARNING WITH APPLICATION OF TAKEOFF POWER. ALL SWITCHES AND TRIM SETTINGS VERIFIED IN LIMITS. ABORTED TAKEOFF. RAN AIRCRAFT AT TAKEOFF POWER IN TAKEOFF CONFIGURATION. CYCLED TRIM THROUGHOUT GREEN BAND WITH NO DEF ECTS NOTED. OPS CHECK GOOD. COULD NOT DUPLICATE DISCREPANCY. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032700371 20010327 00371 2001 3 27 SWIA972418 4 20010302 A 2215 SERVO EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE AUTOPILOT SYS MALFUNCTIONED A SWIA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 NM 07 234SW 120308 PILOT REPORTS ELEVATOR SEEMS TO CATCH WITH AUTO PILOT ENGAGED. WITH AUTO PILOT NOT ENGAGED ALL IS NORMAL. PERFORMED EL EVATOR FLIGHT CONTROL FREEDOM OF MOVEMENT CHECKS WITHOUT AUTOPILOT ENGAGED, NO DISCREPANCIES NOTED. OBSERVED ERRATIC SM ALL MOVEMENT TO BE CAUSED BY THE ELEVATOR SERVO WHEN AUTOPILOT IS ENGAGED. REPLACED ELEVATOR SERVO PER MM 22-20-05. P/ N 622-5734-002, S/N OFF 5983, S/N ON 5760, ALL PANELS SECURED. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032700372 20010327 00372 SO 2001 3 27 SWIA972419 1 20010304 A 3030 SENSOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT AOA FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 579SW 120347 LEFT AOA FAILED AND STAYED FAILED AFTER RESETTING. RETURNED TO LAX. REPLACED CURRENT SENSOR. ALL CHECK GOOD. P/N ON 120-41406-501, S/N OFF 120-347. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032700373 20010327 00373 SO 2001 3 27 C2XA01IA146 1 20010303 A 2120 UNKNOWN EMB 120 EMB120ER 3260203 SO COCKPIT ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 58733 120197 IAH - FLIGHT 2933, THE CREW REPORTED A FUEL ODOR IN THE COCKPIT. MAINTENANCE DRAINED THE APU EPA TANK AND OPERATIONALLY CHECKED THE AIR CONDITIONING SYSTEM WITH NO FUEL SMELL NOTED. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001032700375 20010327 00375 WP 2001 3 27 ABXA010086 1 20010307 A 5330 59114103 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 CORROSION WAS FOUND BENEATH LEFT SIDE OF FUSELAGE STATIC PORT FS 446 AND 465. MAINTENANCE INSPECTED AND REPAIRED THE AR EA IAW DC-9 SRM 53-04. 2 L 7 2 4F A6WE 2001032700376 20010327 00376 WP 2001 3 27 ABXA010085 1 20010307 A 5315 991556171 FLOORBEAM DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 FLOORBEAM UPPER ANGLE AT FUSELAGE STATION 996 HAD A 4 INCH CRACK. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW ABX R EA D953-40085. 2 L 7 2 4F A6WE 2001032700377 20010327 00377 WP 2001 3 27 ABXA010084 1 20010307 A 5320 5956879501 WEB DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 WEB AT FS 200 STRINGER 8L WAS CRACKED AND MISSING A SECTION OF MATERIAL. MAINTENANCE INSPECTED AND REPLACED THE WEB. 2 L 7 2 4F A6WE 2001032700378 20010327 00378 WP 2001 3 27 ABXA010083 1 20010307 A 5320 991834117 WEB DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 CORROSION WAS FOUND AT FUSELAGE STATION 1121 ON FWD SIDE OF WEB, JUST OUTBOARD AND BELOW PULLY BRACKET. MAINTENANCE INS PECTED AND REPAIRED THE CORRODED AREA IAW ABX REA D953-400600. 2 L 7 2 4F A6WE 2001032700379 20010327 00379 WP 2001 3 27 ABXA010082 1 20010307 A 5230 5910141067 PAN DOUG DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 56263 47352 47419 FORWARD LOWER CARGO DOOR PAN WAS CRACKED AT THE NR 3, 4 AND 10 DOOR STOPS. MAINTENANCE INSPECTED AND REPLACED THE FORWA RD CARGO DOOR IAW DC-9 MM 52-31-00. 2 L 7 2 4F A6WE 2001032700380 20010327 00380 WP 2001 3 27 ABXA010081 1 20010307 A 5755 5910055514 SPOILER DOUG DC9 DC931 3022065 WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 THE RIGHT WING OUTBOARD SPOILER HAD A LARGE AREA THAT WAS CORRODED. THE SPOILER WAS ALSO FOUND TO BE CRACKED. MAINTENA NCE INSPECTED AND REPLACED THE SPOILER IAW DC-9 MM. 2 L 7 2 4F A6WE 2001032700381 20010327 00381 NM 2001 3 27 F3LA200100040 1 20010307 A 3520 2250407 CONTROL UNIT BOEING 737 7372L9 1384497 NM OXYGEN SYS FAILED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 1936 22733 PRIOR TO DEPARTURE, FLIGHT CREW REPORTED ALL PASSENGER OXYGEN MASKS DEPLOYED AFTER OXYGEN SYSTEM WAS SERVICED. REPLACED PASSENGER OXYGEN CONTINUOUS FLOW CONTROL UNIT PER MM 35-21-21, RESTOWED OXYGEN MASKS, PERFORMED OPERATIONAL TEST AND LE AK CHECK, AND SYSTEM CHECKED OK. 2 L 7 2 4F RT A16WE 2001032700382 20010327 00382 SO 2001 3 27 C2XA01TY030 1 20010304 A 5412 14533997001 HEAT SHIELD EMB 145 EMB145LR SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13975 145163 TYS DURING A SCHEDULED INSPECTION THE APU FIREWALL HEAT BLANKET WAS FOUND GOUGED AT THE BLEED VALVE MOUNT BRACKET. MAI NTENANCE REMOVED AND REPLACED THE APU FIREWALL HEAT BLANKET IAW EMB-145 SB 145-53-0004. REPAIR WAS SATISFACTORY, AIRCRA FT WILL BE RELEASED FOR SERVICE UPON COMPLETION OF SCHEDULED INSPECTION. 2 L 7 2 4T RT T00011AT 2001032700383 20010327 00383 2001 3 27 C2XA01TY031 4 20010305 A 3130 980470019 FLIGHT RECORDER EMB 145 EMB145LR SO EMPENAGE FAILED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13975 3835 3835 145163 TYS DURING A SCHEDULE INSPECTION THE FLIGHT DATA RECORDER FAILED FUNCTIONAL CHECKS, REFER TO CONTINENTAL EXPRESS TASK C ARD 31-31-00-720-001-A00. MAINTENANCE REMOVED AND REPLACED THE FLIGHT DATA RECORDER IAW EMB-145 MM 31-31-01, OPERATIONA L CHECKS WERE SATISFACTORY. AIRCRAFT WILL BE RELEASED FOR SERVICE UPON COMPLETION OF SCHEDULED INSPECTION. 2 L 7 2 4T RT T00011AT 2001032700384 20010327 00384 SO 2001 3 27 C2XA01TY032 1 20010306 A 5315 14522459001 FLOORBEAM EMB 145 EMB145LR SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13975 145163 TYS DURING A SCHEDULED INSPECTION THE SUPPORT STRUCTURE FOR THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED. MAINTEN ANCE REPAIRED SUPPORT STRUCTURE BY INSTALLING DOUBLER IAW EMB-145 SRM 53-21-10 AND 53-40-02. REPAIR WAS SATISFACTORY, A IRCRAFT WILL BE RELEASED UPON COMPLETION OF SCHEDULED INSPECTION. 2 L 7 2 4T RT T00011AT 2001032700385 20010327 00385 SO 2001 3 27 C2XA01TY033 1 20010306 A 5220 14525738401 SKIN EMB 145 EMB145LR SO EXIT DOOR DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13975 145163 TYS DURING A SCHEDULE INSPECTION THE LEFT HAND OVERWING EMERGENCY EXIT DOOR, INNER SKIN BY WINDOW WAS FOUND TO BE DAMAG ED. MAINTENANCE REPAIRED SKIN BY BLENDING IAW EMB GST-0720/01 AND EMB-145 CPM 51-21-03,04,06. REPAIR WAS SATISFACTORY, AIRCRAFT WILL BE RELEASED FOR SERVICE UPON COMPLETION OF SCHEDULED INSPECTION. 2 L 7 2 4T RT T00011AT 2001032700386 20010327 00386 SO 2001 3 27 C2XA01TY034 1 20010306 A 5220 14525738401 SKIN EMB 145 EMB145LR SO EXIT DOOR DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13975 145163 TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND OVERWING EMERGENCY EXIT DOOR, INNER SKIN BY WINDOW WAS FOUND TO BE DAM AGED. MAINTENANCE REPAIRED SKIN BY BLENDING IAW EMB GST-0720/01 AND EMB-145 CPM 51-21-03,04,06. REPAIR WAS SATISFACTOR Y, AIRCRAFT WILL BE RELEASED UPON COMPLETION OF SCHEDULED INSPECTION. 2 L 7 2 4T RT T00011AT 2001032700387 20010327 00387 NM 2001 3 27 UPS01235209 1 20010212 A 5210 FRAME BOEING 727 72722C 138400F NM ENTRY DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, CRACK IN TOP FRAME (AFT) OF FWD ENTRY DOOR TOP FRAME. REPLACED IAW SRM 51-30-2 WITH REFERENCE TO BOEING DWG 50 -7954. 2 L 7 3 4F A3WE 2001032700388 20010327 00388 NM 2001 3 27 UPS01235210 1 20010213 A 5753 CARRIAGE BOEING 727 72722C 138400F NM FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, NR 6 FLAP CARRIAGE HAS CORROSION INSIDE SPINDLE BORE. NR 6 FLAP CARRIAGE REPLACED IAW MM 27-51-13 . 2 L 7 3 4F A3WE 2001032700389 20010327 00389 NM 2001 3 27 UPS01235213 1 20010215 A 5320 FLANGE BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, DURING INSP 2 DISCREPANT HOLES WERE FOUND ON AFT O/B FLANGE OF BS 950 LT SIDE FITTING (1 CRACK) (1 HOLE CORRODED). REPAIR CARRIED OUT IAW SMRO EO 2001-006-003 UPS ENGINEERING FILE NR 727-57-20006. 2 L 7 3 4F A3WE 2001032700390 20010327 00390 NM 2001 3 27 UPS01235214 1 20010223 A 5320 SPLICE BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, SPLICE FITTING AT BS 1040 (REAR CARGO COMPT) CORRODED AND CRACKED. REPLACED FITTING IAW SRM 51-30 -2. 2 L 7 3 4F A3WE 2001032700391 20010327 00391 NM 2001 3 27 UPS01235215 1 20010218 A 5510 PIN BOEING 727 72722C 138400F NM LT HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, LT OUTER HORIZ STAB HINGE PIN CRACKED. REPLACED PIN IAW MM 55-10-01. 2 L 7 3 4F A3WE 2001032700392 20010327 00392 NM 2001 3 27 UPS01235216 1 20010215 A 5320 INTERCOSTAL BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, UPPER CHORD OF INTERCOSTAL BETWEEN BS 1148 & BS 1156 CRACKED. REPLACED UPPER CHORD OF INTERCOSTAL IAW SRM 51-20-2. 2 L 7 3 4F A3WE 2001032700393 20010327 00393 NM 2001 3 27 UPS01235217 1 20010213 A 5753 CARRIAGE BOEING 727 72722C 138400F NM NR 3 FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, NR 3 FLAP CARRIAGE HAS CORROSION IN SPINDLE BORE. NR 3 FLAP CARRIAGE REPLACED IAW MM 27-51-03. 2 L 7 3 4F A3WE 2001032700394 20010327 00394 NM 2001 3 27 UPS01235218 1 20010215 A 5700 STRUCTURE BOEING 727 72722C 138400F NM WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, X-RAY REPORT - SUSPECT CORROSION ON WING CENTER SECTION AT WBL 70.5 UPPER LT AREA AT BS 870. REPA IR CARRIED OUT IAW SRM 51-30-2 BOEING DWG 69-13965 & SMRO EO 200 1-006-015, UPS ENGINEERING FILE NR 727-57-20009. 2 L 7 3 4F A3WE 2001032700395 20010327 00395 NM 2001 3 27 ASAA0140008 1 20010120 A 3397 WIRE BOEING 737 7374Q8 NM CABIN DISCONNECTED A K NONE L NO TEST IN INSP/MAINT 1 NM 01 774AS 25107 PDX - WHEN PERFORMING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 13-16. RECONNECTED LIGHTS, OPS NORMAL. (M) 2 L 7 2 4F RT A16WE 2001032700396 20010327 00396 NM 2001 3 27 ASAA0140005 1 20010113 A 3397 WIRE BOEING 737 737490 1384715 NM CABIN DISCONNECTED A K NONE L NO TEST IN INSP/MAINT 1 NM 01 767AS 27081 SEA - BEFORE FLIGHT, FOUND EMERGENCY FLOOR TRACK LIGHTING IN AFT CABIN INOPERATIVE. RECONNECTED WIRES OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2001032700397 20010327 00397 NM 2001 3 27 ASAA0140004 1 20010111 A 3397 WIRE BOEING 737 7374Q8 NM CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 NM 01 760AS 25098 SEA - DURING PREFLIGHT, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE. REPLACED BROKEN WIRES OPERATIONAL CHECKED NORMAL. (M ) 2 L 7 2 4F RT A16WE 2001032700398 20010327 00398 NM 2001 3 27 ASAA0140003 1 20010111 A 3397 WIRE BOEING 737 7374Q8 NM CABIN DISCONNECTED A K NONE L NO TEST IN INSP/MAINT 1 NM 01 775AS 25108 SEA - BEFORE FLIGHT, FOUND FLOOR TRACK LIGHTING IN MID CABIN INOPERATIVE. RECONNECTED WIRING, OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2001032700399 20010327 00399 NM 2001 3 27 AALA20014021 1 20010125 A 5315 FLOORBEAM BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 NM 01 688AA 25730 AFW - FOUND CORROSION ON 1640 LBL 25 FLOORBEAM 2 INCHES WL RT. CORROSION ON 1640 AT WL FLOORBEAM 8 INCHES RIGHT. INSTA LLED REPAIR STRAP FROM 301.5 H STAINLESS STEEL .50 THICKNESS. PER ATTACH ALODINE ALL BARE METAL SURFACE. FINISH BLEND AND REPAIRS PARTS WITH TWO COATS BMS 10-11 PRIMER UNTIL BLENDS WITH BMS 5-92. INSTALLED STRAPS WET WITH BMS 5-95 SEALAN T PROSEAL 870. (M) 2 L 7 2 4F RT A2NM 2001032700400 20010327 00400 NM 2001 3 27 AALA20010365 1 20010222 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 861AA 21088 TUL - FOUND FLOORBEAM WEB CRACKED STATION 875 LBL 61. INSTALLED FAB WEB AT FLOORBEAM AT STATION 825 LBL 61 SRM 51-40-2. (M) 2 L 7 3 4F A3WE 2001032700401 20010327 00401 NM 2001 3 27 AALA20010301 1 20010218 A 2422 100201021000 INVERTER BOEING 767 767323 1385205 NM EE BAY DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 359AA 24040 CUR - FLT 950 - EN ROUTE GRU-JFK - DETECTED SMOKE IN CABIN. AIR INTERRUPTED, DIVERTED CRU AND LANDED WITHOUT FURTHER IN CIDENT. REPLACED STANDBY INVERTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001032700402 20010327 00402 NM 2001 3 27 AALA20010275 1 20010216 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 661AA 25295 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 20DEF LOOSE. RE-SECURED EMERGENCY EXIT LIGHT AT SEAT 2 0DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001032700403 20010327 00403 NM 2001 3 27 AALA20010241 1 20010214 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 691AA 25697 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 1E THROUGH SEAT 16D INOPERATIVE. REPLACED EMERGENCY EX IT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001032700404 20010327 00404 NM 2001 3 27 AALA20010239 1 20010214 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 622AA 24580 BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 28 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001032700405 20010327 00405 NM 2001 3 27 AALA20010242 1 20010213 A 3350 4000873 LIGHT BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 620AA 24578 TUL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT SEAT 3E DIM. REPLACED EMERGENCY EXIT LAMP AT SEAT 3E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001032700406 20010327 00406 NM 2001 3 27 AALA20010243 1 20010213 A 3350 5862553 LIGHT BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39364 24045 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT STRIP BROKEN. REPLACED EMERGENCY EXIT LIGHT STRIP. SYSTEM GRO UND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001032700407 20010327 00407 NM 2001 3 27 AALA20010298 1 20010214 A 3350 CONNECTOR BOEING 757 757223 1384957 NM COCKPIT DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 691AA 25697 SNA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT DID NOT ILUMINATE IN ARMED POSITION. RE-CONNECTED EMERGENCY EX IT LIGHT AT CIRCUIT BREAKER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001032700408 20010327 00408 NM 2001 3 27 AALA20010294 1 20010220 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN DAMAGED A K NONE L NO TEST IN INSP/MAINT 1 SW 21 397AN 29604 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 31B AND 32B INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001032700409 20010327 00409 NM 2001 3 27 AALA20010290 1 20010220 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN DAMAGED A K NONE L NO TEST IN INSP/MAINT 1 SW 21 397AN 29604 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT FROM SEAT 31 THROUGH 38 INOPERATIVE. REPAIRED EMERGENCY EXIT L IGHT WIRE AT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001032700410 20010327 00410 NM 2001 3 27 AALA20010288 1 20010221 A 3350 LIGHT BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 317AA 22319 LAX - DURING OVERNIGHT MAINTENANE, EMERGENCY EXIT LIGHT AT SEAT 9H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001032700411 20010327 00411 NM 2001 3 27 AALA20010287 1 20010220 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 650AA 24608 TUL - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT 19D INOPERATIVE. RE-SEATED EMERGENCY EXIT LIGHT PIN AT SIDE WALL CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001032700412 20010327 00412 NM 2001 3 27 AALA20010286 1 20010219 A 3350 LIGHT BOEING 757 757223 1384957 NM OVERWING BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 661AA 25295 DFW - DURING OVERNIGHT MAINTENANCE, OVERWING EMERGENCY EXIT LIGHT BROKEN. REPLACED OVERWING EMERGENCY EXIT LIGHT ASSEMB LY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001032700413 20010327 00413 NM 2001 3 27 AALA20010284 1 20010217 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 390AA 27450 MIA - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT AT SEAT 20C BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SY STEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001032700414 20010327 00414 NM 2001 3 27 AALA20010281 1 20010216 A 3350 LIGHT BOEING 767 767223 1385123 NM MID GALLEY MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 316AA 22318 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT MID GALLEY MISSING. REPLACED WALL MOUNTED EMERGENCY EXIT LI GHT ASSEMBLY AT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001032700415 20010327 00415 NM 2001 3 27 AALA20010332 1 20010223 A 3350 0201922001 LIGHT BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 643AA 24601 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 17D BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001032700416 20010327 00416 EU 2001 3 27 AALA20010280 1 20010224 A 2913 5548385 O-RING FOKKER F28 F28MK0100 4990807 EU HYD PUMP LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 1469D 11502 STL - FLT 1618 - EN ROUTE STL-LGA - DETECTED NR 1 HYDRAULIC SYSTEM SLOWLY DECREASE TO TWELVE PERCENT. ON FINAL APPROACH NR 1 HYDRAULIC SYSTEM LOW LIGHT ILLUMINATED. LANDED JFK WITHOUT FURTHER INCIDENT. REPLACED NR 1 SYSTEM ENGINE HYDRAUL IC PUMP O-RING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001032700423 20010327 00423 SO 2001 3 27 C2XA01TY045 1 20010318 A 5230 14522493003 SKIN EMB 145 EMB145LR SO CARDO DOOR GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 99 13978 145180 TYS DURING A SCHEDULED INSPECTION THE CARGO DOOR SKIN WAS FOUND GOUGED AT THE CUTOUT FOR THE ACTUATING HANDLE. MAINTEN ANCE REPAIRED THE SKIN IAW EMB GST-0815/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION O F INSPECTION. 2 L 7 2 4T RT T00011AT 2001032700424 20010327 00424 EU 2001 3 27 MALA010282 1 20010319 A 2710 CONTROL UNIT SAAB SF340 SF340A 7850100 EU AILERONS MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 99 114XJ 340A114 DURING FLIGHT 2790 AFTER LT TURN, INFLIGHT, BANK ANGLE 30 DEGREES: AILERONS STUCK FOR ABOUT 1 SECOND AT 25 DEGREES: AS T HE WINGS ROLLED LEVEL. MAINTENANCE PERFORMED AILERON RANGE OF MOVEMENT CHECK AND VISUAL CHECK OF AILERON SYSTEM. NO DE FECTS NOTED. CREW REPOLRTED THAT AILERONS OPERATED NORMALLY FOR REMAINDER OF FLIGHT, BUT FELT THAT THE INCIDENT SHOULD B E DOCUM ENTED ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2001032700426 20010327 00426 WP 2001 3 27 MWEA010370 1 20010323 A 5242 59127561 PAN DOUG DC9 DC932 3022066 WP E/E BAY DOOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 SW 99 205ME 47601 E&E BAY DOOR JAMB PAN WAS CORRODED BEYOND LIMITS. REMOVED PAN, LOCATED, DRILLED AND INSTALLED NEW PAN. 2 L 7 2 4F A6WE 2001032800001 20010328 00001 EU 2001 3 28 QXEA0100128 1 20010125 A 5320 STIFFENER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED STIFFENER BETWEEN WHEEL BAYS AT BL245L, BETWEEN STATIONS 13853 AND 14333. REPAIRED IAW FOKKER SRM 53-22-14 PAGE 2 AND 51-31-01 PAGE 13 AND 14. 2 L 7 2 4F RT A20EU 2001032800002 20010328 00002 EU 2001 3 28 QXEA0100129 1 20010125 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CASTELLATION ON REAR CARGO PIT AT STRINGER 2 AND FRAME 13815B. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 AND 51-31-01 PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001032800003 20010328 00003 EU 2001 3 28 QXEA0100130 1 20010125 A 5280 FITTING FOKKER F28 F28MK4000 4990810 EU RT MLG DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- RIGHT HAND AFT MAIN LANDING GEAR DOOR ACTUATOR UPPER ATTACHMENT HAS A CRACKED BACKUP FORGED FITTING. REPAIRED IAW FOKKER SRM 51-31-01 PAGES 13 AND 14 AND 51-30-02 PAGES 9 AND 10. 2 L 7 2 4F RT A20EU 2001032800004 20010328 00004 EU 2001 3 28 QXEA0100131 1 20010127 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CASTELLATION IN FORWARD CARGO PIT AT FRAME 7305 AND STRINGER 7. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800005 20010328 00005 EU 2001 3 28 QXEA0100132 1 20010127 A 5315 FLOORBEAM FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CORROSION ON SURFACE OF FLOORBEAM STRUCTURE, INBOARD OF SERVICE EMERGENCY DOOR SURROUND. REPAIRED IAW FOKKER SRM 5 1-10-4 PAGE 9. 2 L 7 2 4F RT A20EU 2001032800006 20010328 00006 EU 2001 3 28 QXEA0100134 1 20010204 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CASTELLATION AT FRAME 5805 AND STRINGER 18. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2. 2 L 7 2 4F RT A20EU 2001032800007 20010328 00007 EU 2001 3 28 QXEA0100135 1 20010209 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CASTELLATION AT FRAME 14285 BETWEEN STRINGERS 73 AND 74. REPAIRED IAW FOKKER SRM 53-02-13 AND 51-31-01 PAG ES 13 AND 14. 2 L 7 2 4F RT A20EU 2001032800008 20010328 00008 EU 2001 3 28 QXEA0100124 1 20010123 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX- FORWARD FUSELAGE LEFT HAND SIDE HAS SCRATCHES IN SKIN. REPARIED IAW FOKKER SRM 53-01-01 AND 53-12-01. 2 L 7 2 4F RT A20EU 2001032800009 20010328 00009 EU 2001 3 28 QXEA0100125 1 20010125 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACK ON VERTICAL ANGLE BRACKET BETWEEN HORIZONTAL BEAMS 3 AND 4, LEFT HAND SIDE OF FRONT PRESSURE BULKHEAD. REPAI RED IAW FOKKER SRM 51-31-01 PAGE 13 AND 14. 2 L 7 2 4F RT A20EU 2001032800010 20010328 00010 EU 2001 3 28 QXEA0100126 1 20010125 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACK ON ANGLE BRACKET INBOARD OF BL325L VERTICAL BEAM, LOWER SECTION. REPARIED IAW FOKKER SRM 51-30-02 PAGE 9 AND 10 AND 51-31-01 PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001032800011 20010328 00011 EU 2001 3 28 QXEA0100127 1 20010123 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- FORWARD CARGO PIT AFT OF DOOR HAS DEEP SCRATCHES IN SKIN. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 3. 2 L 7 2 4F RT A20EU 2001032800012 20010328 00012 EU 2001 3 28 QXEA0100136 1 20010124 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- SKIN UNDER NAV/COMM ANTENNA IS GOUGED AND SCRATCHED. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 3. 2 L 7 2 4F RT A20EU 2001032800013 20010328 00013 EU 2001 3 28 QXEA0100137 1 20010127 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 13815 AND STRINGER 57. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 AND 51-31-01 PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001032800014 20010328 00014 EU 2001 3 28 QXEA0100138 1 20010127 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- MAIN CABIN DOOR SURROUND HAS A GOUGE IN LOWER BOTTOM AFT CORNER. REPAIRED IAW FOKKER SRM 53-01-01 AND 53-14-08. 2 L 7 2 4F RT A20EU 2001032800015 20010328 00015 EU 2001 3 28 QXEA0100140 1 20010124 A 5755 SKIN FOKKER F28 F28MK4000 4990810 EU SPEED BRAKE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- RIGHT HAND SPEED BRAKE PADDLE OUTER SKIN HAS A HOLE. REPAIRED IAW FOKKER SRM 53-02-17. 2 L 7 2 4F RT A20EU 2001032800016 20010328 00016 EU 2001 3 28 QXEA0100141 1 20010123 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE MISDRILLED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 475AU 11222 YYC- THERE IS A HOLE DRILLED THROUGH FUSELAGE SKIN AT FRAME 32-2 BETWEEN STRINGERS 11 AND 9. REPAIRED IAW FOKKER SRM 53 -02-13, 51-31-01 PAGE 13 AND 14 AND 51-30-02 PAGES 9 AND 10. 2 L 7 2 4F RT A20EU 2001032800017 20010328 00017 EU 2001 3 28 QXEA0100142 1 20010124 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- A CRACK ON A CASTELLATION HAS GONE BEYOND STOP DRILL AT FRAME 32-2 AND STRINGER 22. REPAIRED IAW FOKKER SRM 53-26- 04 PAGE 14 AND 51-31-01. 2 L 7 2 4F RT A20EU 2001032800018 20010328 00018 EU 2001 3 28 QXEA0100143 1 20010208 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AFT OF VERTICAL BEAM AT RIGHT HAND SIDE OF PANEL 41A OPENING. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 5 , 53-10-05 PAGE 601, AND 51-31-01 PAGE 13 AND 14. 2 L 7 2 4F RT A20EU 2001032800019 20010328 00019 EU 2001 3 28 QXEA0100144 1 20010125 A 5541 RIB FOKKER F28 F28MK4000 4990810 EU RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- RIB 5 IN RUDDER IS CRACKED. REPAIRED IAW FOKKER SRM 51-31-01 PAGE 13 AND 14, 51-30-02 PAGES 9 AND 10 AND 51-31-05 PAGES 8, 9 AND 10. 2 L 7 2 4F RT A20EU 2001032800020 20010328 00020 EU 2001 3 28 QXEA0100145 1 20010125 A 5541 RIB FOKKER F28 F28MK4000 4990810 EU RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- RIB 6 IN RUDDER IS CRACKED. REPAIRED IAW FOKKER SRM 51-31-01 PAGES 13 AND 14, 51-30-02 PAGES 9 AND 10, AND 55-40-0 4. 2 L 7 2 4F RT A20EU 2001032800021 20010328 00021 EU 2001 3 28 QXEA0100146 1 20010125 A 5541 RIB FOKKER F28 F28MK4000 4990810 EU RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACK FOUND ON RIB WEB STRUCTURE AT RUDDER BASE. REPAIRED IAW FOKKER SRM 51-31-01 PAGE 13 AND 14. 2 L 7 2 4F RT A20EU 2001032800022 20010328 00022 EU 2001 3 28 QXEA0100147 1 20010227 A 5711 SPAR FOKKER F28 F28MK4000 4990810 EU RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- RIGHT HAND WING REAR SPAR WEB PLATE IS CRACKED AT STATION 5010. REPAIRED IAW HORIZON AIR EA 4-57-533 AND FOKKER SR M 51-31-01 PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001032800023 20010328 00023 EU 2001 3 28 QXEA0100148 1 20010204 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- SKIN DAMAGE BETWEEN FRAMES 6305 AND 5805 AT STRINGER 17. REPAIRED IAW FOKKER SRM 53-02-06 PAGE 8. 2 L 7 2 4F RT A20EU 2001032800024 20010328 00024 EU 2001 3 28 QXEA0100150 1 20010208 A 3350 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 475AU 11222 YYC- 3V AND 28V EMERGENCY EXIT SIGNS ARE ALL BURNT OUT. 2 L 7 2 4F RT A20EU 2001032800025 20010328 00025 EU 2001 3 28 QXEA0100151 1 20010125 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACK ON STRINGER, RIGHT HAND BL270R AT FRAME 1550 THROUGH ACCESS PANEL 21A. REPAIRED IAW HORIZON AIR EA 4-53-1438 . 2 L 7 2 4F RT A20EU 2001032800026 20010328 00026 EU 2001 3 28 QXEA0100152 1 20010207 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CASTELLATION AT FRAME 6305 AND STRINGER 17 AND 16. REPAIRED IAW HORIZON AIR EA 4-53-1443. 2 L 7 2 4F RT A20EU 2001032800027 20010328 00027 EU 2001 3 28 QXEA0100153 1 20010124 A 5753 BRACKET FOKKER F28 F28MK4000 4990810 EU LT FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- FORWARD LEFT HAND FLAP BEAM SUPPORT BRACKET WORN. REPAIRED IAW HORIZON AIR EA 4-57-534. 2 L 7 2 4F RT A20EU 2001032800028 20010328 00028 EU 2001 3 28 QXEA0100154 1 20010131 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CASTELLATION AT LEFT HAND FRAME 5805 AND STRINGERS 15 AND 16. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 AND HORIZON AIR EA 4-53-1439. 2 L 7 2 4F RT A20EU 2001032800029 20010328 00029 EU 2001 3 28 QXEA0100155 1 20010129 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- LEFT HAND FUEL PANEL 73A IS CRACKED. REPAIRED IAW HORIZON AIR EA 4-57-537. 2 L 7 2 4F RT A20EU 2001032800030 20010328 00030 EU 2001 3 28 QXEA0100157 1 20010125 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACK ON STRINGER 3 BL 270L AT FRAME 1550 THROUGH ACCESS PANEL 21A. REPAIRED IAW HORIZON AIR EA 4-53-1438. 2 L 7 2 4F RT A20EU 2001032800031 20010328 00031 EU 2001 3 28 QXEA0100158 1 20010126 A 3110 PANEL FOKKER F28 F28MK4000 4990810 EU COCKPIT CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CHAFE DAMAGE FOUND ON INSTRUMENT PANEL CENTER SUPPORT. REPAIRED IAW HORIZON AIR EA 4-53-1437. 2 L 7 2 4F RT A20EU 2001032800032 20010328 00032 EU 2001 3 28 QXEA0100159 1 20010125 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACK ON STRINGER 3 BL270L AT FRAME 1550 THROUGH ACCESS PANEL 21A. REPAIRED IAW HORIZON AIR EA 4-53-1438. 2 L 7 2 4F RT A20EU 2001032800033 20010328 00033 EA 2001 3 28 COMA0160281 1 20010221 A 2760 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT FALSE INDICATION A COMA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 769CA 7292 GROUND SPOILER UNSAFE CAUTION DURING TAXI. COULD NOT DUPLICATE. RESET SYSTEM, OPERATION CHECK NORMAL. 2 L 7 2 4F RT A21EA 2001032800034 20010328 00034 EU 2001 3 28 QXEA0100160 1 20010124 A 5320 STRUCTURE FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- HOLE IN AUXILLARY STRUCTURE AT BL1735L ABOVE LEFT HAND 1700 COVE DOOR. REPAIRED IAW FOKKER SRM 53-53-01 PAGE 2 AND HORIZON AIR EA 4-53-1436. 2 L 7 2 4F RT A20EU 2001032800035 20010328 00035 EU 2001 3 28 QXEA0100161 1 20010202 A 5330 STRAP FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- FUSELAGE SKIN AT STATION 16495, AFT REINFORCING STRAP CUT AT STRINGER 1 AND 72. REPAIRED IAW HORIZON AIR EA 4-53-1 435. 2 L 7 2 4F RT A20EU 2001032800036 20010328 00036 EU 2001 3 28 QXEA0100162 1 20010123 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- LOWER FUSELAGE SKIN IS BADLY CHAFED BELOW FAIRING PANELS 91BC AND 91BD. REPAIRED IAW HORIZON AIR EA 4-53-1435. 2 L 7 2 4F RT A20EU 2001032800037 20010328 00037 EU 2001 3 28 QXEA0100163 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 10346 AND STRINGER 44. REPAIRED IAW FOKKER SRM 53-020-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800038 20010328 00038 EU 2001 3 28 QXEA0100165 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 10346 AND STRINGER 41. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800039 20010328 00039 EU 2001 3 28 QXEA0100166 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 10346 AND STRINGER 34. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800040 20010328 00040 EU 2001 3 28 QXEA0100167 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 10346 AND STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800043 20010328 00043 NM 2001 3 28 UPS01235111 1 20010227 A 3350 LIGHT BOEING 727 72725C 138400H NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:IN, CEILING EXIT FWD/RT PORTION OF POS 3 INOP DURING TEST. OK TO CONTINUE IN SERVICE IAW MEL 33-15-1. TRANSFERRED TO MEL LOG UNDER M210243. REMOVED AND REPLACED LIGHT ASSY AND BATTERY. OPS CK''S GOOD AT SDF. THIS CLEARS M210243-PLACARD REMOVED S/N ON 1022, S/N OFF 1016-LIGHT ASSY. 2 L 7 3 4F A3WE 2001032800044 20010328 00044 NM 2001 3 28 UPS01435115 1 20010301 A 2131 CONTROLLER BOEING 747 747121 1384871 NM COCKPIT FAILED A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 682UP 20349 INSPECTION TYPE:N/A, ATB-DURING CLIMB, UNABLE TO CONTROL PRESSURIZATION. FIRST IND- AUTO FAIL LT ILLUM, RAN CK LIST. U NABLE TO GAIN CONTROL, PRESS RELIEF LT ILLUM, DESCENDED TO 16,000 FT. GAINED PARTIAL CONTROL MOMENTARILY, RETURN TO NRT , DIFF PRESS STABILIZED AT APPRX 9.2 PSI UNTIL FURTHER DESCENT CABIN ALT IND 10,100 FT AT ON POINT. NEVER GOT WARNING H ORN. CABIN DEPRESS CONDITION CK PERFORMED. NO DAMAGE FOUND. T/S FOUND AUTO PRESS CONTROL FAIL. MANUAL DEPRESS CNTRL WORKS NORMAL. M210343 CHECKED PRESS RELIEF VLVS. REMOVED AND REPLACED CABIN PRESS CONTROLLER IAW MM 21-31-02 ACC TEST ALL TESTS OK. THIS CLEARS MEL M210343 LOG PAGE 676680. 2 L 7 4 4F A20WE 2001032800045 20010328 00045 NM 2001 3 28 UPS01535154 1 20010302 A 2730 ACTUATOR BOEING 757 75724APF 1384969 NM ELEVATOR FAILED A IPXA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SO 01 409UP 23731 INSPECTION TYPE:N/A, ELEV ASYM DISPLAYED. A/C DIVERTED TO MIA. REMOVED AND REPLACED ELEV CNTRL LINEAR ACT ASSY PER M/M 27-31-03. OPS CKS GOOD. 2 L 7 2 4F RT A2NM 2001032800046 20010328 00046 WP 2001 3 28 UPS01835118 1 20010124 A 5320 FITTING DOUG DC8 DC873F 302199F WP CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, AFT LWR CARGO PIT AT FS 1160 BETWEEN LONG 29L-30L Z-FITTING IS CORRODED. Z-FITTING OUT OF LIMITS IAW DC8 SRM 53-2-0. RCVD FITTING P/N 375584-2- 2N PO 699381 MAT ID FOR REPAIR ANGLES BAC 1505-101167 EXTRUSION .12 5 70 75-T6571 IAW DC8 SRM 53-2-0. FABD REPAIR ANGLES IAW DC8 SRM 53-2- 0. ALODINED AND PRIMED IAW 51-1-8. INSTALLED FITTIN G AND REPAIR ANGLES IAW 51-1-20D. 2 L 7 4 4F RT 4A25 2001032800047 20010328 00047 WP 2001 3 28 UPS01835120 1 20010124 A 5320 FITTING DOUG DC8 DC873F 302199F WP CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, AFT LWR CARGO PIT AT FS 1160 BETWEEN L33R-L34R Z-FITTING IS CORRODED. REMOVED AND REPLACED FITTIN G IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001032800048 20010328 00048 WP 2001 3 28 UPS01835121 1 20010201 A 5312 BULKHEAD DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, LEFT NWW TUNNEL, BOTTOM OF PRESSURE WEB AT FS -67 FROM CUSP TO INBD STIFFENER CORRODED. WEB REPAI RED IAW REO-G07874. 2 L 7 4 4F RT 4A25 2001032800049 20010328 00049 WP 2001 3 28 UPS01835123 1 20010124 A 5320 WEB DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, AFT LWR CARGO PIT AT FS 1160 - 1220 AT LONG 26L WEB SKIN IS PUNCTURED AND CRACKED. REMOVED DAMAGE D WEB, FABBED NEW WEB IAW DAC DWG 9753776. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED WEB IAW DC8 SRM 51-1-21 . 2 L 7 4 4F RT 4A25 2001032800050 20010328 00050 WP 2001 3 28 UPS01835126 1 20010124 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, AFT LWR CARGO PIT AT FS 1220 - 1230 INSIDE X-SLIDE DOOR AFT TORQUE BOX AT LONG 33R Z-FITTING IS CO RRODED. REMOVED Z-FITTING FOR ACCESS IAW DC8 SRM 51-1-20D. REMOVED CORROSION LONGERON AND PRIMED IAW DC8 SRM 51-1-8. Z-FITTING. REMOVED FOR ACCESS WAS NOTED CRACKED RECD LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24, FAB REPAIR DO UBLERS IAW 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001032800051 20010328 00051 WP 2001 3 28 UPS01835128 1 20010125 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, FWD LWR CARGO PIT AT FS 280 AT LONG 33R Z-FITTING IS CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1 -8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. FABBED REPAIR DOUBLER IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC 8 SRM 51-1-8. INSTALLED IAW DC8 SRM 53-2-0 FIG 2D & 51-1-20D. 2 L 7 4 4F RT 4A25 2001032800052 20010328 00052 WP 2001 3 28 UPS01835131 1 20010126 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, FWD LWR CARGO AT FS 440 - 460 LONG 34R IS CRACKED AT SPLICE FITTING. REMOVED AND REPLACED LONGERO N 34R IAW DC8 SRM 51-1-20 DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001032800054 20010328 00054 EU 2001 3 28 QXEA0100176 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 12405 AND STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800055 20010328 00055 EU 2001 3 28 QXEA0100177 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 12405 AND STRINGER 34. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800056 20010328 00056 EU 2001 3 28 QXEA0100178 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 12405 AND STRINGER 33. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800057 20010328 00057 EU 2001 3 28 QXEA0100179 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 12405 AND STRINGER 31. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800058 20010328 00058 EU 2001 3 28 QXEA0100181 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 12405 AND STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800059 20010328 00059 EU 2001 3 28 QXEA0100182 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 12405 AND STRINGER 21. REPAIRED IAW FOKKER SRM 53-20-04 FIGURE 3 AND 51-31-01 PAGES 13 AND 1 4. 2 L 7 2 4F RT A20EU 2001032800060 20010328 00060 EU 2001 3 28 QXEA0100183 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 12875 AND STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800061 20010328 00061 EU 2001 3 28 QXEA0100184 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 12875 AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800062 20010328 00062 EU 2001 3 28 QXEA0100185 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 12875 AND STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800063 20010328 00063 EU 2001 3 28 QXEA0100186 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 13815 AND STRINGER 58. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 AND 51-31-01 PAGE 13 AND 14. 2 L 7 2 4F RT A20EU 2001032800064 20010328 00064 EU 2001 3 28 QXEA0100187 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 13815 AND STRINGER 33. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800065 20010328 00065 EU 2001 3 28 QXEA0100189 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 13815 AND STRINGER 28. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800066 20010328 00066 EU 2001 3 28 QXEA0100190 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 13815A AND STRINGER 47. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800067 20010328 00067 EU 2001 3 28 QXEA0100191 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 13815A AND STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800068 20010328 00068 EU 2001 3 28 QXEA0100192 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 13815A AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800069 20010328 00069 EU 2001 3 28 QXEA0100193 1 20010204 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 13815A AND STRINGER 37. REPAIRED IAW FOKKER SRM 51-31-01 PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001032800070 20010328 00070 EU 2001 3 28 QXEA0100194 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 13815A AND STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 AND 51-31-01 PAGES 13 AND 14 . 2 L 7 2 4F RT A20EU 2001032800071 20010328 00071 EU 2001 3 28 QXEA0100195 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 13815A AND STRINGER 28. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 AND 51-31-01 PAGE 13 AND 14. 2 L 7 2 4F RT A20EU 2001032800072 20010328 00072 EU 2001 3 28 QXEA0100197 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 13815A AND STRINGER 26. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800073 20010328 00073 EU 2001 3 28 QXEA0100198 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 13815A AND STRINGER 17. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800074 20010328 00074 EU 2001 3 28 QXEA0100199 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 13815B AND STRINGER 42. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 AND 51-31-01 PAGES 13 AND 14 . 2 L 7 2 4F RT A20EU 2001032800075 20010328 00075 EU 2001 3 28 QXEA0100200 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 13815B AND STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 AND 51-31-01 PAGE 13 AND 14. 2 L 7 2 4F RT A20EU 2001032800076 20010328 00076 EU 2001 3 28 QXEA0100201 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 13815B AND STRINGER 28. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 AND 51-31-01 PAGES 13 AND 14 . 2 L 7 2 4F RT A20EU 2001032800077 20010328 00077 EU 2001 3 28 QXEA0100202 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 14755 AND STRINGER 47. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 AND 53-31-01 PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001032800078 20010328 00078 EU 2001 3 28 QXEA0100203 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 14755 AND STRINGER 57. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 AND 51-31-01 PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001032800079 20010328 00079 EU 2001 3 28 QXEA0100205 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 15205 AND STRINGER 18. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800080 20010328 00080 EU 2001 3 28 QXEA0100206 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 15205 AND STRINGER 26. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800081 20010328 00081 EU 2001 3 28 QXEA0100207 1 20010127 A 5315 BRACKET FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- FLOORBEAM BRACKET IS CRACKED AT FRAME 4175, INBOARD OF MAIN CABIN DOOR. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001032800082 20010328 00082 NM 2001 3 28 SWAA010617 1 20010302 A 3350 100031 LIGHT BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 EMERGENCY EXIT LIGHT ASSY LOOSE AT MID CABIN. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 2001032800083 20010328 00083 NM 2001 3 28 SWAA010619 1 20010302 A 5315 6546804 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 344, LBL 4.5 TO RBL 8. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F A16WE 2001032800084 20010328 00084 NM 2001 3 28 SWAA010620 1 20010302 A 3350 65C27095 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 087SW 22903 DURING SCHEDULED A2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXIT LIGHT DIM. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2001032800085 20010328 00085 NM 2001 3 28 SWAA010621 1 20010302 A 5330 6545778 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 087SW 22903 DURING SCHEDULED A2 CHECK, FOUND 2 EXTERNAL FUSELAGE SKIN CRACK AT APPROX BS 925, STR 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001032800086 20010328 00086 NM 2001 3 28 SWAA010622 1 20010302 A 5755 6573735 SKIN BOEING 737 7373H4 1384600 NM RT SPOILER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND NR 5 SPOILER DELAMINATED ON BOTTOM CORNER. REMOVED AND REPLACED NR 5 SPOILER PER MM. 2 L 7 2 4F RT A16WE 2001032800087 20010328 00087 EU 2001 3 28 QXEA0100208 1 20010127 A 5315 FLOORBEAM FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CORROSION ON SURFACE OF FLOORBEAM STRUCTURE INBOARD OF SERVICE EMERGENCY DOOR SURROUND. REPAIRED IAW FOKKER SRM 51 -10-4 PAGE 9AND 53-01-01 PAGE 6. 2 L 7 2 4F RT A20EU 2001032800088 20010328 00088 EU 2001 3 28 QXEA0100209 1 20010214 A 5315 FLOORBEAM FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CORROSION FOUND ON FLOORBEAM FRAME 6805 BETWEEN BL600RH AND BL1390RH. REPAIRED IAW HORIZON AIR EA 4-53-1445. 2 L 7 2 4F RT A20EU 2001032800089 20010328 00089 EU 2001 3 28 QXEA0100210 1 20010214 A 5315 FLOORBEAM FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CORROSION FOUND ON FLOORBEAM FRAME 6805 BETWEEN BL600RH AND BL1390RH. REPAIRED IAW HORIZON AIR EA 4-53-1445. 2 L 7 2 4F RT A20EU 2001032800090 20010328 00090 NM 2001 3 28 SWAA010624 1 20010302 A 5330 6545775 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 313SW 23335 DURING SCHEDULED SERVICE CHECK, FOUND 3 EXTERNAL FUSELAGE SKIN CRACK AT BS 940, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001032800091 20010328 00091 NM 2001 3 28 PCAA0103016 1 20010306 A 3350 GROUND WIRE DHAV DHC8 DHC8102 2809003 NM EMERGENCY LGHT DAMAGED A PCAA K NONE O OTHER CR CRUISE 1 EA 13 830EX 155 AVP-FLIGHT 3558 CREW REPORTED EMERGENCY LIGHTS FLICKER IN TURBULANCE. ACFT FERRIED TO MDT. MX CHECKED ALL CONNECTIONS AT FLT ATTENDANTS EMERGENCY LIGHT SWITCH, AND CANNON PLUG BEHIND SWITCH PANEL. NO DEFECTS NOTED. RELAY 3315-K2 REPLACE D. COULD NOT DUPLICATE. AIRCRAFT RETURNED TO SERVICE. PROBLEM REOCCURED ON 08 MAR 01 SCE FLT 3831. EMERGENCY LIGHTS FLICKERED DURING TAKEOFF AND CLIMB. MX REPLACED CIRCUIT BREAKER C3 ON RT. SECONDARY BUSS AND REPLACED 8 WIRES IN EMERG ENCY LIGHT SYSTEM. COULD NOT DUPLICATE DURING TEST FLIGHT. ACFT RETURNED TO SERVICE. PROBLEM REOCCURED FLIGHT 3743-MD T EMERGENCY LIGHTS FLICKERED ON SHORT FINAL. MX FOUND AND REPAIRED A BAD GROUNG WIRE. 2 H 7 2 4T RT A13NM 2001032800092 20010328 00092 WP 2001 3 28 ARWA0010303 1 20010306 A 3244 TIRE ALIDSG DOUG DC8 DC862 3021970 WP RT MLG SEPARATED A ARWA K NONE O OTHER TO TAKEOFF 1 SO 19 1808E 59 B1651 46105 AFTER TAKEOFF FROM KATL ATC ADVISED FLIGHT 509 THAT A TIRE WAS LEFT ON THE RUNWAY, FLIGHT CREW REPORTED THE INCIDENT TO MIAMI MX AND CONTINUE TO TJSJ. EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT AT TJSJ. ON POST FLIGHT INSPECTION IT WAS CONFIRMED THAT NR 7 TIRE WAS MISSING FROM THE RIM. REMOVED AND REPLACED NR 7 MAIN WHEEL ASSY DUE TO TIRE MISSING. REMOVED AND REPLACED NR 8 MAIN WHEEL ASSY DUE TO WHEEL OVERLOAD. REMOVED AND REPLACED NR 6 MAIN WHEEL AS SY DUE TO RIM DAMAGE BY DEBRIS. 2 L 7 4 4F 4A25 2001032800093 20010328 00093 EU 2001 3 28 PNSA010204 1 20010209 A 3150 WARNING LIGHT SAAB SF340 340B 7860101 EU COCKPIT FALSE INDICATION A PNSA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 AL 03 685PA 212 DURING TAKEOFF ROLL MASTER WARNING LIGHT ILLUMINATED. ABORTED TAKEOFF RETURNED FOR MAINTENANCE. RE-RACKED WARNING ELEC TRONIC UNIT. NO FAULTS FOUND. SUBSEQUENT FLIGHTS WERE MADE WITH NO OTHER FAULTS. 2 L 7 2 4T RT A52EU 2001032800094 20010328 00094 SW 2001 3 28 PNSA010202 1 20010219 A 7931 PT506C584S CONNECTOR SWRNGN SA227 SA227AC 8780603 SW RT ENGINE WORN A PNSA A UNSCHED LANDING O OTHER CL CLIMB 1 AL 03 2719H AC713B DURING CLIMB RT ENGINE OIL PRESSURE BEGAN TO FLUCUATE. HOWEVER, OIL PRESSURE LIGHT DID NOT ILLUMINATE. RETURNED TO BAS E. REPLACED CANNON PLUG AT OIL PRESSURE TRANSDUCER. OPS CHECKED OK. 2 L 7 2 4T RT A8SW 2001032800095 20010328 00095 SW 2001 3 28 PNSA010206 1 20010206 A 5270 2720038001 SWITCH SWRNGN SA227 SA227AC 8780603 SW CABIN DOOR FAILED A PNSA I A CABIN DEPRESSURIZATION UNSCHED LANDING N FALSE WARNING CL CLIMB 1 AL 03 2708D AC713B CLIMBING THROUGH 15,000 FT CABIN DOOR WARNING LIGHT ILLUMINATED. DEPRESSURIZED CABIN AND RETURNED TO BASE. REPLACED UP PER FORWARD DOOR SWITCH. 2 L 7 2 4T RT A8SW 2001032800096 20010328 00096 NM 2001 3 28 UPS01235238 1 20010307 A 3350 COVER BOEING 727 727180C 138406G NM COCKPIT LOOSE A IPXA K NONE O OTHER LD LANDING 1 SO 01 920UP 19873 INSPECTION TYPE:N/A, COCKPIT EMERGENCY EXIT LIGHT COVER FALLS OFF ON LANDING. REPLACED EXIT LIGHT COVER. 2 L 7 3 4F A3WE 2001032800097 20010328 00097 SO 2001 3 28 C2XA01TY035 1 20010306 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13975 145163 TYS DURING A SCHEDULED INSPECTION THE FORWARD OMEGA BEAM TOP CAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REP LACED THE TOP CAP IAW EMB-145 SRM 51-40-02, REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF S CHEDULED INSPECTION. 2 L 7 2 4T RT T00011AT 2001032800098 20010328 00098 NM 2001 3 28 PCAA0103015 1 20010308 A 5210 85210240055 STRUT DHAV DHC8 DHC8102 2809003 NM AIRSTAIR DOOR BROKEN A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 841EX 249 ROC FLIGHT 3512. CREW REPORTED, UNABLE TO OPEN THE AIRSTAIR DOOR. AIRCRAFT FERRIED TO MDT. MDT MAINTENANCE REPLACED F ORWARD UPPER DOOR STRUT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001032800099 20010328 00099 WP 2001 3 28 UPS01835109 1 20010223 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C2/3, LEFT WING L/E LOWER RIBS ARE CRACKED AT XFS 310.25 AND XFS 335.25. REPAIRED RIBS IAW SRM 57-2-0 F IG 2. 2 L 7 4 4F RT 4A25 2001032800100 20010328 00100 NM 2001 3 28 UPS01235221 1 20010219 A 5410 DUCT BOEING 727 72730C 1384009 NM NR 2 ENG CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:C-CK, NR 2 ENG INLET S-DUCT INNER SKIN HAS APPROX 3 INCH CIRCUMFERENTIAL CRACK APPROX 104 INCHES FROM AF T EDGE AT 3 O''CLOCK. CUT OUT DAMAGE AREA. INSTALLED REPAIR. 2 L 7 3 4F A3WE 2001032800101 20010328 00101 NM 2001 3 28 UPS01235224 1 20010213 A 5753 CARRIAGE BOEING 727 72722C 138400F NM LT FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, NR 2 CARRIAGE ON LEFT O/B FLAP HAS CORROSION IN SPINDLE BORE. REPLACED CARRIAGE IAW MM 27-51-13. 2 L 7 3 4F A3WE 2001032800102 20010328 00102 NM 2001 3 28 UPS01235225 1 20010219 A 5753 BOLT BOEING 727 72722C 138400F NM NR 6 ROLLER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, DURING MAG PARTICLE INSP DEAD WEIGHT ROLLER BOLT NR 6 FOUND CRACKED. BOLT REPLACED IAW MM 27-51-0 3. 2 L 7 3 4F A3WE 2001032800103 20010328 00103 NM 2001 3 28 UPS01235227 1 20010215 A 5741 PIN BOEING 727 72722C 138400F NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, RIGHT BS 740 BOTTLE PIN CORRODED. BOTTLE PIN REPLACED IAW MM 57-41-01. 2 L 7 3 4F A3WE 2001032800120 20010328 00120 NM 2001 3 28 SWAA010519 1 20010221 A 3350 082081 DIODE BOEING 737 7372H4 138448C NM EMERGENCY LIGHT WEAK A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 060SW 21812 DURING SCHEDULED C4 CHECK, FOUND EEPLS LIGHTS DIM BETWEEN ROWS 5 & 10. REMOVED AND REPLACED BLOCKING DIODE AT MID CABIN PER MM. 2 L 7 2 4F A16WE 2001032800121 20010328 00121 NM 2001 3 28 PCAA0103017 1 20010309 A 3350 PIN DHAV DHC8 DHC8102 2809003 NM CANNON PLUG LOOSE A PCAA K NONE O OTHER CR CRUISE 1 EA 13 830EX 155 SCE-FLIGHT 3814. CREW REPORTED EMERGENCY LIGHTS FLICKER IN FLIGHT. AIRCRAFT FERRIED TO MDT. MAINTENANCE MEGGED CONTRO L BOX WIRING TO COCKPIT SWITCH. LOOSE PIN FOUND AT CANNON PLUG 3351PI. PIN REPLACED. OPERATIONAL CHECK GOOD. AIRCRAF T RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001032800134 20010328 00134 EU 2001 3 28 MALA010232 1 20010129 A 5330 SKIN BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 503XJ E2310 FOUND DURING C-CHECK, DAMAGE TO RT FUSELAGE SKIN 77 INCHES AFT CARGO DOOR. MAINTENANCE COMPLETED PERMANENT REPAIR IAW E OA53028. 2 H 7 4 4F RT A49EU 2001032800135 20010328 00135 EU 2001 3 28 MALA010233 1 20010129 A 5330 SKIN BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 503XJ E2310 FOUND DURING C-CHECK, TWO DENTS FWD OF FRAME 20. MAINTENANCE REPAIRED TWO DENTS FWD OF FRAME 20 IAW EO A53029. 2 H 7 4 4F RT A49EU 2001032800136 20010328 00136 EU 2001 3 28 MALA010234 1 20010129 A 5330 SKIN BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 503XJ E2310 FOUND DURING C-CHECK, THREE DENTS ON LT SIDE OF FUSELAGE AT FRAMES 9, 10, 11. MAINTENANCE COMPLETED PERMANENT REPAIR IA W EO A53032. 2 H 7 4 4F RT A49EU 2001032800137 20010328 00137 EU 2001 3 28 MALA010235 1 20010129 A 5330 SKIN BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 503XJ E2310 FOUND DURING C-CHECK, TWO DENTS IN LT SIDE OF FUSELAGE BETWEEN FRAMES 19 AND 20 UNDER WINDOW. MAINTENANCE COMPLETED REP AIR IAW EO A53030. 2 H 7 4 4F RT A49EU 2001032800138 20010328 00138 EU 2001 3 28 MALA010237 1 20010201 A 5260 HAND RAIL BAC 146 AVRO146RJ85A 1500097 EU AIRSTAIRS CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 503XJ E2310 FOUND DURING C-CHECK INBOARD AIRSTAIR RAIL HAS CORROSION BEYOND LIMITS. REPLACED IAW BAE SRM 51-44-00. 2 H 7 4 4F RT A49EU 2001032800139 20010328 00139 EU 2001 3 28 MALA010238 1 20010201 A 5311 FRAME BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 503XJ E2310 FOUND DURING C-CHECK, CORROSION ON FLOOR FRAME BEYOND REPAIR. PERFORMED PERMANENT REPAIR IAW EO A53031. 2 H 7 4 4F RT A49EU 2001032800140 20010328 00140 EU 2001 3 28 MALA010239 1 20010201 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU CABIN CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 503XJ E2310 FOUND DURING C-CHECK, NR 3 SEAT RAIL HAS CORROSION BEYOND LIMITS. MAINTENANCE REPAIRED IAW EO A53026. 2 H 7 4 4F RT A49EU 2001032800141 20010328 00141 EU 2001 3 28 MALA010240 1 20010201 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU CABIN CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 503XJ E2310 FOUND DURING C-CHECK, NR 2 SEAT RAIL HAS CORROSION BEYOND LIMITS. MAINTENANCE REPAIRED IAW EO A53026. 2 H 7 4 4F RT A49EU 2001032800142 20010328 00142 EU 2001 3 28 MALA010241 1 20010201 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU CABIN CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 503XJ E2310 FOUND DURING C-CHECK, NR 4 SEAT RAIL HAS CORROSION BEYOND LIMITS. MAINTENANCE REPAIRED IAW EO A53026. 2 H 7 4 4F RT A49EU 2001032800143 20010328 00143 EU 2001 3 28 MALA010242 1 20010201 A 7160 DOUBLER BAC 146 AVRO146RJ85A 1500097 EU NR 1 INTAKE DELAMINATED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 503XJ E2310 FOUND DURING C-CHECK, NR 1 INTAKE LIPSKIN DOUBLER FOUND DISBONDED. MAINTENANCE REPAIRED IAW RILS HC510H9015, HCS10H9016 , AND HC716H9073. THIS REPAIR REQUIRES INSPECTION REPEATED EVERY 500 HOURS. 2 H 7 4 4F RT A49EU 2001032800144 20010328 00144 EU 2001 3 28 MALA010243 1 20010201 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU CABIN CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 503XJ E2310 FOUND DURING C-CHECK, NR 1 SEAT RAIL HAS CORROSION BEYOND LIMITS. REPAIRED IAW EO A53026. 2 H 7 4 4F RT A49EU 2001032800159 20010328 00159 NM 2001 3 28 SWAA010520 1 20010221 A 3350 079123 COVER BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 060SW 21812 DURING SCHEDULED C4 CHECK, FOUND EEPLS FLOOR TRACK COVERS MISSING AT FWD SECTION. INSTALLED TRACK COVERS PER MM. 2 L 7 2 4F A16WE 2001032800160 20010328 00160 NM 2001 3 28 SWAA010521 1 20010220 A 3350 65C27095 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 060SW 21812 DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2001032800161 20010328 00161 NM 2001 3 28 SWAA010522 1 20010220 A 2560 6557463 BRACKET BOEING 737 7372H4 138448C NM FWD SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 060SW 21812 DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE FWD GIRT BRACKET LOOSE. SECURED BRACKET PER MM. 2 L 7 2 4F A16WE 2001032800162 20010328 00162 NM 2001 3 28 SWAA010523 1 20010221 A 5311 963820 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD AFT SIDE VERTICAL CHORD CRACKED AT LBL 5.7, WL 184 TO WL 188. REMOVE D AND REPLACED VERTICAL CHORD PER SRM. 2 L 7 2 4F RT A16WE 2001032800163 20010328 00163 NM 2001 3 28 SWAA010525 1 20010221 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 399WN 27693 DURING SCHEDULED C4 CHECK, FOUND LT EMERGENCY EXIT LIGHT SIDEWALL LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2001032800164 20010328 00164 NM 2001 3 28 01FDEA00159 1 20010223 A 5730 SKIN BOEING 727 727247 138408F NM WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 233FE 21327 DURING ROUTINE INSP, NR3 LEAD EDGE FLAP, OTBD GUIDE, WING LEAD EDGE CUTOUT WAS FOUND CRACKED. ** S/D ** STOP DRILL C RACK. FAB & INSTALL PER IAW BAC 727 SRM 57-30-4. 2 L 7 3 4F A3WE 2001032800165 20010328 00165 NM 2001 3 28 SWAA010526 1 20010221 A 5312 6516300 BULKHEAD BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD WEB CRACKS AT RBL 17.1, WL 163 & LBL 17.1, WL 229. REPAIRED BULKHEAD WE B PER BFG ER. 2 L 7 2 4F RT A16WE 2001032800166 20010328 00166 NM 2001 3 28 SWAA010528 1 20010221 A 5320 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED D-CHECK, FOUND STR CLIPS CRACKED AT STR 6R, BS 500D & BS 520. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001032800167 20010328 00167 NM 2001 3 28 SWAA010529 1 20010221 A 5311 BAC1514 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED D-CHECK, FOUND FWD SVC DOOR CUTOUT FWD LOWER FRAME CRACKED AT INBD LOWER CORNER. REPAIRED FRAME PER SR M. 2 L 7 2 4F RT A16WE 2001032800168 20010328 00168 NM 2001 3 28 SWAA010530 1 20010221 A 5313 BAC1498 STRINGER BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED D-CHECK, FOUND STR 6R CRACKED AT BS 520. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2001032800169 20010328 00169 NM 2001 3 28 SWAA010531 1 20010220 A 5754 6546430 PLATE BOEING 737 737317 138447P NM L/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED C1 CHECK, FOUND LT WING L/E INBD FORE FLAP REPAIR PLATE DISBONDED. REMOVED AND REPLACED FORE FLAP PER MM. 2 L 7 2 4F RT A16WE 2001032800170 20010328 00170 2001 3 28 SWAA010532 4 20010220 A 2565 6567380 COVER BOEING 737 7372T4 1384492 NM AFT SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 AFT SVC DOOR EMERGENCY EVAC SLIDE COVER LOOSE. SECURED COVER ASSY PER MM. 2 L 7 2 4F A16WE 2001032800171 20010328 00171 NM 2001 3 28 SWAA010533 1 20010221 A 5743 6567172 FITTING BOEING 737 7373Q8 1384670 NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED D-CHECK, FOUND LT MLG STABILIZER BEAM FITTING CORRODED AT SUPPORT BEAM. REMOVED AND REPLACED FITTING P ER MM. 2 L 7 2 4F RT A16WE 2001032800172 20010328 00172 NM 2001 3 28 SWAA010602 1 20010228 A 3350 57771 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED C3 CHECK, FOUND EEPLS END CAP MISSING AT FWD SECTION. INSTALLED END CAP PER MM. 2 L 7 2 4F A16WE 2001032800173 20010328 00173 NM 2001 3 28 SWAA010603 1 20010228 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 331SW 23695 DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK COVER DAMAGED BETWEEN ROWS 1 & 2. REMOVED AND REPLACED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001032800174 20010328 00174 NM 2001 3 28 SWAA010604 1 20010228 A 5754 6573714 SKIN BOEING 737 7373H4 1384600 NM LT SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND 2 SKIN CRACKS AT NR 1 L/E SLAT FASTENER HOLES. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2001032800175 20010328 00175 NM 2001 3 28 SWAA010606 1 20010228 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND STR SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2001032800176 20010328 00176 NM 2001 3 28 SWAA010607 1 20010301 A 5311 AND10133 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD VERTICAL T-CHORD CRACKED AT LBL 5.7, WL 184. REPAIRED T-CHORD PER SR M. 2 L 7 2 4F RT A16WE 2001032800177 20010328 00177 NM 2001 3 28 SWAA010608 1 20010301 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 642WN 27715 EEPLS WIRING EXPOSED AT ROW 14. SECURED WIRING PER MM. 2 L 7 2 4F RT A16WE 2001032800178 20010328 00178 NM 2001 3 28 SWAA010609 1 20010301 A 3350 207377 LENS BOEING 737 7377H4 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 709SW 27843 EEPLS RED LENS LOOSE AT FWD SECTION. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2001032800179 20010328 00179 NM 2001 3 28 SWAA010610 1 20010301 A 5753 6546435 SKIN BOEING 737 7373H4 1384600 NM FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND RT WING OUTBD AFT FLAP INBD CORNER DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM . 2 L 7 2 4F RT A16WE 2001032800180 20010328 00180 NM 2001 3 28 SWAA010611 1 20010301 A 2560 65C168209 RETAINER BOEING 737 7377H4 NM FWD ENTRY LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 700GS 27835 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER LOOSE. SECURED GIRT RETAINER PER MM. 2 L 7 2 4F RT A16WE 2001032800181 20010328 00181 NM 2001 3 28 SWAA010613 1 20010301 A 3350 BR2013 LIGHT BOEING 737 7377H4 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 700GS 27835 DURING SCHEDULED C4 CHECK, FOUND EEPLS INOP AT ROW 21. RELAMPED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001032800182 20010328 00182 NM 2001 3 28 SWAA010614 1 20010301 A 3350 65C27093 LENS BOEING 737 7377H4 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 700GS 27835 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001032800183 20010328 00183 NM 2001 3 28 SWAA010615 1 20010301 A 5315 BAC1509 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAMS CORRODED AT BS 727D+4, RBL 2.5, BS 867, LBL 7.5, BS 858 TO 86 1, LBL 7.5 TO LBL 12. REPAIRED BEAMS PER SWA RA. 2 L 7 2 4F RT A16WE 2001032800184 20010328 00184 NM 2001 3 28 SWAA010587 1 20010227 A 5330 6545857 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/4D CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT AFT SVC DOOR CUTOUT, BS 960, RBL 70, WL 210. REPAIRE D SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001032800185 20010328 00185 NM 2001 3 28 SWAA010588 1 20010227 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR EMERGENCY LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2001032800186 20010328 00186 2001 3 28 SWAA010589 4 20010227 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY AND SVC DOOR EMERGENCY EVAC SLIDE ASSY''S OUT OF ADJUST. RE-ADJUSTED EVAC SL IDE ASSY''S PER MM. 2 L 7 2 4F RT A16WE 2001032800187 20010328 00187 NM 2001 3 28 SWAA010590 1 20010227 A 5312 6516300 SPLICE PLATE BOEING 737 7373H4 1384600 NM BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD SKIN SPLICE PLATE CRACKED AT LBL 4, WL 242. REPAIRED SKIN SPLICE PER BFG ER. 2 L 7 2 4F RT A16WE 2001032800188 20010328 00188 NM 2001 3 28 SWAA010593 1 20010227 A 4960 38763264 SWITCH BOEING 737 7373H4 1384600 NM APU FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 371SW 26598 DIVERSION - APU OVERSPEED LIGHT ILLUMINATED. LEFT BUS OFF LIGHT ILLUMINATED. (NR 1 GENERATOR ALREADY ON MEL). REMOVED AND REPLACED APU 3-SPEED SWITCH PER MM. 2 L 7 2 4F RT A16WE 2001032800190 20010328 00190 NM 2001 3 28 SWAA010524 1 20010221 A 5320 6517583 BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND 1.5 BS 178 BULKHEAD VERTICAL BEAM CRACK AT RBL 17.1, WL 227. REMOVED AND REPLACED VE RTICAL BEAM PER SRM. 2 L 7 2 4F RT A16WE 2001032800191 20010328 00191 NM 2001 3 28 SWAA010527 1 20010219 A 5311 BAC1517 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED D-CHECK, FOUND BS 727 CHORD CORRODED AT BL 0, WL 148. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2001032800192 20010328 00192 NM 2001 3 28 SWAA010605 1 20010228 A 5330 65C32362 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND 3 EXTERNAL FUSELAGE SKIN CRACK AT BS 907, STR 4L. REPAIRED SKIN PER SWA RA. 2 L 7 2 4F RT A16WE 2001032800193 20010328 00193 NM 2001 3 28 SWAA010612 1 20010301 A 3350 20131A BATTERY PACK BOEING 737 7377H4 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 700GS 27835 DURING SCHEDULED C4 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2001032800194 20010328 00194 NM 2001 3 28 SWAA010586 1 20010226 A 3350 6556633 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 074SW 22674 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 2001032800197 20010328 00197 NM 2001 3 28 SWAA010592 1 20010227 A 5320 BAC1518 FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/4D CHECK, FOUND FITTING CRACKED AT BS 727, LBL 19, WL 201. REMOVED AND REPLACED FITTING PER SRM. 2 L 7 2 4F RT A16WE 2001032800198 20010328 00198 NM 2001 3 28 SWAA010595 1 20010228 A 5330 6547955 SKIN BOEING 737 7372K6 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED SERVICE CHECK, FOUND 3 EXTERNAL FUSELAGE SKIN CRACK AT AT BS 890, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001032800199 20010328 00199 NM 2001 3 28 SWAA010600 1 20010227 A 3350 207377 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 652SW 27722 DURING SCHEDULED C2 CHECK, FOUND EEPLS RED LENS MISSING AT AFT SECTION. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2001032800200 20010328 00200 NM 2001 3 28 SWAA010563 1 20010224 A 5311 6546529 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED SERVICE CHECK, FOUND BELT FRAME CRACKED AT BS 344, STR 20R. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2001032800202 20010328 00202 NM 2001 3 28 SWAA010567 1 20010225 A 5522 65C25753 SKIN BOEING 737 7373H4 1384600 NM LT ELEVATOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 392SW 27379 DURING SCHEDULED C2 CHECK, FOUND LT ELEVATOR UPPER SKIN CRACKED 1.5 INCH AT APPROX 12 INCHES FWD OF TAB, 46 INCHES OUTBD OF INBD SIDE OF ELEVATOR. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001032800203 20010328 00203 2001 3 28 SWAA010572 4 20010225 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 521SW 25320 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001032800204 20010328 00204 NM 2001 3 28 SWAA010575 1 20010226 A 3350 20121 CHARGER BOEING 737 737301 1384611 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED RON CHECK, FOUND 2 BULLNOSE EMERGENCY EXIT LIGHTS INOP AT LEFT AFT CABIN. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2001032800208 20010328 00208 NM 2001 3 28 SWAA010581 1 20010226 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND STR 26R CORRODED BETWEEN BS 827 TO BS 870. REPAIRED STR PER SRM. 2 L 7 2 4F RT A16WE 2001032800215 20010328 00215 NM 2001 3 28 UPS01235228 1 20010216 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, CORROSION ON FLOORBEAM TOP CAP BS 344 BETWEEN LBL 10 & RBL 14. FLOORBEAM REPAIRED IAW SRM 53-10-8 . 2 L 7 3 4F A3WE 2001032800231 20010328 00231 NM 2001 3 28 SWAA010594 1 20010228 A 3350 57771 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED C3 CHECK, FOUND EEPLS END CAP MISSING AT FWD SECTION. INSTALLED END CAP PER MM. 2 L 7 2 4F A16WE 2001032800232 20010328 00232 NM 2001 3 28 SWAA010596 1 20010227 A 5330 6545857 DOUBLER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR SKIN CUTOUT 2 INCH CRACK AT LOWER FWD CORNER. REPAIRED SKIN DOUBLER PER S RM. 2 L 7 2 4F RT A16WE 2001032800233 20010328 00233 NM 2001 3 28 SWAA010597 1 20010227 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND STR 26L CORRODED AT BS 827, 847 & 867. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2001032800234 20010328 00234 NM 2001 3 28 SWAA010598 1 20010228 A 5330 65C32362 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND 5 FUSELAGE SKIN CRACKS AT FASTENER HOLES, BS 907, STR 4L (AT DOUBLER). REPAIRED SKIN PER SWA RA. 2 L 7 2 4F RT A16WE 2001032800235 20010328 00235 2001 3 28 SWAA010599 4 20010228 A 2565 1061323 INDICATOR BOEING 737 7373H4 1384600 NM EVAC SLIDE OUT OF TOLERANCE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 380SW 26587 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001032800236 20010328 00236 NM 2001 3 28 SWAA010601 1 20010227 A 3397 BR2013 WIRE BOEING 737 7377H4 1384404 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 754SW 29849 DURING SCHEDULED C1 CHECK, FOUND EEPLS INOP AT ROW 10. RECONNECTED WIRING PER MM. 2 L 7 2 4F RT A16WE 2001032800237 20010328 00237 2001 3 28 SWAA010562 4 20010225 A 3421 H341BWM INDICATOR BOEING 737 7377H4 NM INST PANEL FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 740SW 29276 DIVERSION - STANDBY ATTITUDE GYRO BEGAN MAKING NOISE AND STARTED TILTING. CYCLED C/B AND GYRO TUMBLED AND WOULD NOT ERE CT. GYRO FLAG IN VIEW. REMOVED AND REPLACED STANDBY HORIZON PER MM. 2 L 7 2 4F RT A16WE 2001032800238 20010328 00238 NM 2001 3 28 SWAA010564 1 20010226 A 5320 6517583 BEAM BOEING 737 7373H4 1384600 NM BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT LBL 17.1, WL 227. REPAIRED VERTICAL BEA M WEB PER SWA ACO. 2 L 7 2 4F RT A16WE 2001032800239 20010328 00239 NM 2001 3 28 SWAA010565 1 20010225 A 5754 65C30461 FLAP BOEING 737 7373Q8 1384670 NM LT WING BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 317WN 24068 DURING SCHEDULED SERVICE CHECK, FOUND LT WING L/E NR 1 KRUEGER FLAP OUTBD END BROKEN AT SPRING LOADED FLAP DOOR. REMOVE D AND REPLACED KRUEGER FLAP PER MM. 2 L 7 2 4F RT A16WE 2001032800240 20010328 00240 NM 2001 3 28 SWAA010566 1 20010225 A 5754 6546431 SKIN BOEING 737 7373H4 1384600 NM LT FORE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED PM CHECK, FOUND LT WING L/E OUTBD FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM. 2 L 7 2 4F RT A16WE 2001032800241 20010328 00241 NM 2001 3 28 SWAA010568 1 20010226 A 5320 6551698 SPLICE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED D-CHECK, FOUND STR SPLICE CHANNEL CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STR SPLICE CHANNEL P ER SRM. 2 L 7 2 4F RT A16WE 2001032800242 20010328 00242 NM 2001 3 28 SWAA010569 1 20010226 A 5311 6546529 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294.5, BETWEEN STR 1R & 2R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001032800243 20010328 00243 NM 2001 3 28 SWAA010570 1 20010225 A 5240 6545871 FRAME BOEING 737 7373H4 1384600 NM SVC DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 622SW 27932 DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR AFT LOWER FRAME CRACKED, OUTBD OF 3RD FASTENER HOLE. REPAIRED FRAME PER BAC DWG. 2 L 7 2 4F RT A16WE 2001032800244 20010328 00244 NM 2001 3 28 SWAA010571 1 20010226 A 5240 6969854 GUSSET BOEING 737 7373H4 1384600 NM SVC DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 622SW 27932 DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR AFT LOWER GUSSET CRACKED AT OUTBD FASTENER HOLE. REPAIRED GUSSET PER BA C DWG. 2 L 7 2 4F RT A16WE 2001032800245 20010328 00245 2001 3 28 SWAA010573 4 20010226 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 601WN 27695 AFT ENTRY EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001032800246 20010328 00246 NM 2001 3 28 SWAA010574 1 20010226 A 3350 BR2013 COVER BOEING 737 7373H4 1384600 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 642WN 27715 EEPLS WIRING EXPOSED. REPOSITIONED TRACK COVERS AND INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2001032800247 20010328 00247 NM 2001 3 28 SWAA010576 1 20010226 A 3397 BR2013 WIRE BOEING 737 7375H4 138449D NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 EEPLS WIRING EXPOSED AT MID CABIN. SECURED FLOOR TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001032800248 20010328 00248 2001 3 28 SWAA010577 4 20010226 A 2565 D31354 SLIDE BOEING 737 7377H4 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 787SA 29812 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001032800249 20010328 00249 NM 2001 3 28 SWAA010578 1 20010226 A 3350 1000679 BATTERY PACK BOEING 737 7372H4 138448C NM COCKPIT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED SERVICE CHECK, FOUND COCKPIT OVERHEAD EMERGENCY EXIT LIGHT BATTERY CHARGE LOW. REMOVED AND REPLACED BA TTERY PACK PER MM. 2 L 7 2 4F A16WE 2001032800250 20010328 00250 NM 2001 3 28 SWAA010579 1 20010226 A 5240 6545871 FRAME BOEING 737 7373H4 1384600 NM SVC DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR AFT FRAME CRACKED AT NR 3 & 4 STOP FITTINGS. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001032800251 20010328 00251 NM 2001 3 28 SWAA010580 1 20010226 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 907, STR 27L TO STR 27R, FWD SIDE. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001032800252 20010328 00252 NM 2001 3 28 SWAA010582 1 20010226 A 5753 6573731 SKIN BOEING 737 7373H4 1384600 NM LT T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND LT WING INBD T/E AFT FLAP DELAMINATED AT OUTBD AFT EDGE. REPAIRED AFT FLAP PER SRM. 2 L 7 2 4F RT A16WE 2001032800253 20010328 00253 NM 2001 3 28 SWAA010583 1 20010225 A 5330 65C35775 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED C3 CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 771, STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001032800254 20010328 00254 NM 2001 3 28 SWAA010584 1 20010225 A 3350 079123 COVER BOEING 737 7373T5 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 667SW 23063 DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVER LOOSE AT MID CABIN. REMOVED AND REPLACED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001032800255 20010328 00255 NM 2001 3 28 SWAA010585 1 20010225 A 2997 W16800620 WIRE BOEING 737 7373H4 1384600 NM A/C BAY CHAFED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 626SW 27702 AIR TURNBACK - ELECTRIC HYDRAULIC A PUMP LOW PRESS LIGHT ILLUMINATED. CYCLED C/B, NO EFFECT. SHUT OFF ELECTRIC HYDRAUL IC SWITCH PER QRH. FOUND A SYSTEM WIRE CHAFING ON DUCT IN RT A/C BAY. REPAIRED WIRE PER MM. 2 L 7 2 4F RT A16WE 2001032800333 20010328 00333 NE 2001 3 28 UPS01635181 2 20010304 A 7230 COMPRESSOR BOEING 767 76734AF 1385212 NM GE CF6 CF680C2B7 NE NR 1 ENG STALLED A IPXA O OTHER R PARTIAL RPM/PWR LOSS UK UNKNOWN 1 SO 01 329UP 27755 INSPECTION TYPE:ETOP PILOT REPORT - NR 1 ENG FLUX/COMP STALLS. LEFT ENGINE STALLED. STALL STOPPED AFTER THRUST REDUCED TO IDLE AS THRUST LEVER WAS ADVANCED, FLUCTUATIONS AGAIN OCCURRED. ENGINE LEFT AT IDLE. ENGINE BORESCOPE INSPECTION C /O IAW MM 72-00-00 PAGE 601, ALL LOOKS NORMAL AS PER MM. ENGINE GROUND RUNS C/O IAW MM 71-00-00, ALL CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E13NE 2001032800338 20010328 00338 WP 2001 3 28 UPS01835185 1 20010305 A 5320 ANGLE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:PFLT, CRACKED T-ANGLE ATTACHED TO KEEL BEAM. *S/D* REMOVED AND REPLACED TEE. 2 L 7 4 4F RT 4A25 2001032800349 20010328 00349 NE 2001 3 28 SCNA01017 2 20010305 A 7200 ENGINE BOEING 727 7272J4 1384006 NM PWA JT8 JT8D17 52049 NE NR 2 ENGINE FAILED A SCNA C ABORTED TAKEOFF Y ENGINE STOPPAGE TO TAKEOFF 1 GL 15 284SC 21438 702640 THE NUMBER TWO ENGINE FAILED ON TAKEOFF FROM PVR AT LOW SPEED. 2 L 7 3 4F 4 F RT A3WE E2EA 2001032800350 20010328 00350 EU 2001 3 28 QXEA0100168 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 10346 AND STRINGER 31. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800351 20010328 00351 EU 2001 3 28 QXEA0100169 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 10966 AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800352 20010328 00352 EU 2001 3 28 QXEA0100170 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 10966 AND STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800353 20010328 00353 EU 2001 3 28 QXEA0100171 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 10966 AND STRINGER 31. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800354 20010328 00354 EU 2001 3 28 QXEA0100173 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 12405 AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800355 20010328 00355 EU 2001 3 28 QXEA0100175 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 12405 AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800356 20010328 00356 SO 2001 3 28 C2XA01TY036 1 20010306 A 5320 14524095003 FITTING EMB 145 EMB145LR SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13975 145163 TYS DURING A SCHEDULED INSPECTION, THE FITTING FOR STRINGER 36 WAS FOUND TO BE GOUGED AT THE UPPER AFT EDGE OF THE PASS ENGER DOOR CUTOUT. MAINTENANCE REPAIRED THE FITTING IAW EMB GST-0723/01, AND EMB-145 CPM 51-21-03, 04, 06. THE REPAIR WAS SATISFACTORY, AIRCRAFT WILL BE RELEASED UPON COMPLETION OF SCHEDULED INSPECTION. 2 L 7 2 4T RT T00011AT 2001032800357 20010328 00357 SO 2001 3 28 C2XA01TY037 1 20010307 A 5523 14532751001 TAB EMB 145 EMB145LR SO RT ELEVATOR CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13975 145163 TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND ELEVATOR SPRING TAB ACTUATOR INBOARD FAIL SAFE TAB, WAS FOUND TO BE CH AFED. MAINTENANCE REPAIRED THE FAIL SAFE TAB IAW EMB GST-0705/01 AND EMB-145 CPM 51-21-06, REPAIR WAS SATISFACTORY. TH E AIRCRAFT WILL BE RELEASED UPON COMPLETION OF SCHEDULED INSPECTION. 2 L 7 2 4T RT T00011AT 2001032800358 20010328 00358 SO 2001 3 28 C2XA01TY038 1 20010307 A 5330 14523056001 SKIN EMB 145 EMB145LR SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13975 145163 TYS DURING A SCHEDULED INSPECTION THE CARGO DOOR CUTOUT WAS FOUND TO BE GOUGED FROM STATION 20793 THROUGH 25581. MAINT ENANCE REPAIRED CARGO DOOR CUTOUT IAW EMB GST-0707/01 AND EMB-145 CPM 51-21-04, 05, 06. THE REPAIR WAS SATISFACTORY, AI RCRAFT WILL BE RELEASED UPON COMPLETION OF SCHEDULED INSPECTION. 2 L 7 2 4T RT T00011AT 2001032800359 20010328 00359 SO 2001 3 28 C2XA01TY039 1 20010308 A 3350 66366 LIGHT EMB 135 EMB135ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12519 145366 TYS DURING A SCHEDULED INSPECTION THE MIDDLE EMERGENCY FLOOR TRACK LIGHTING STRIP WAS FOUND TO BE INOPERATIVE. MAINTEN ANCE INSPECTED THE STRIP AND FOUND THE WIRES HAD PULLED OUT OF THE ASSEMBLY. THE STRIP WAS REMOVED AND REPLACED IAW EMB -135 MM 33-50-12, OPERATIONAL CHECKS WERE SATISFACTORY IAW EMB-135 MM 33-50-10. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001032800360 20010328 00360 EU 2001 3 28 QXEA0100249 1 20010306 A 2530 JA010001 COFFEEMAKER FOKKER F28 F28MK4000 4990810 EU GALLEY MALFUNCTIONED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 498US 11181 PDX- NR 1 COFFEE POT CIRCUIT BREAKER POPPED. F/A REPORTED SLIGHT ELECTRICAL SMELL. REMOVED AND REPLACED NR 1 COFFEE PO T. RESET CIRCUIT BREAKER. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001032800361 20010328 00361 EU 2001 3 28 QXEA0100250 1 20010306 A 2530 CA16707 RECEPTACLE FOKKER F28 F28MK4000 4990810 EU GALLEY DEFECTIVE A QXEA K NONE O OTHER CR CRUISE 1 NM 09 498US 11181 SMF- ELECTRICAL SMELL IN GALLEY. NR 1 COFFEE CIRCUIT BREAKER POPPED. REMOVED AND REPLACED NR 1 HOT JUG RECEPTICAL. IN SPECTED, CLEANED AND LUBED NR 2 RECEPTICAL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001032800362 20010328 00362 NE 2001 3 28 UPS01535195 2 20010306 A 7200 HOUSING BOEING 757 75724APF 1384969 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE LEAKING A IPXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 439UP 25470 INSPECTION TYPE:N/A DIVERSION - RT ENG OIL QTY LOSS. FOUND OIL LEAKING FROM HIGH SPEED RADIAL DRIVE SHAFT HOUSING. REP LACED DRIVE SHAFT SEALS PER TC5013(RR). IDLE RUN LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E12EU 2001032800363 20010328 00363 SO 2001 3 28 SWIA972396 1 20010225 A 3233 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT MLG OUT OF ADJ A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 224SW 120294 LEFT MAIN LANDING GEAR WOULD NOT FULLY RETRACT AFTER TAKEOFF, (BOTH A AND B RED DISAGREEMENT LIGHTS ILLUMINATED). RETUR NED TO RDM. TROUBLESHOT SYSTEM. FOUND LEFT MAIN GEAR ACTUATOR OUT OF ADJUSTMENT. ADJUSTED AS PER EMB MM 32-32-11. O PS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032800364 20010328 00364 EU 2001 3 28 QXEA0100196 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 13815A AND STRINGER 27. REPAIRED IAW FOKKER SRM 53-02-13 PAGE4 AND 53-31-01 PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001032800365 20010328 00365 EU 2001 3 28 QXEA0100204 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 15205 AND STRINGER 19. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800366 20010328 00366 NM 2001 3 28 SWAA010618 1 20010302 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/4D CHECK, FOUND 2 BS 178 BULKHEAD WEB CRACKS AT RBL 5.0 TO RBL 6.0, WL 212 TO WL 213. REPAIRED BULKH EAD PER SRM. 2 L 7 2 4F RT A16WE 2001032800367 20010328 00367 EU 2001 3 28 MALA010236 1 20010201 A 5260 HAND RAIL BAC 146 AVRO146RJ85A 1500097 EU AIRSTAIRS CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 503XJ E2310 FOUND DURING C-CHECK, OUTBOARD AIRSTAIR RAIL HAS CORROSION BEYOND LIMITS. MAINTENANCE REPLACED AIRSTAIR RAIL IAW BAE SR M 51-44-00. 2 H 7 4 4F RT A49EU 2001032800368 20010328 00368 NM 2001 3 28 SWAA010623 1 20010302 A 5320 BAC1503 STIFFENER BOEING 737 7373H4 1384600 NM MLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 313SW 23335 DURING SCHEDULED SERVICE CHECK, FOUND BS 663 BULKHEAD STIFFENER CRACKED AT LBL 6.5. REPAIRED STIFFENER PER SWA RA. 2 L 7 2 4F RT A16WE 2001032800369 20010328 00369 NM 2001 3 28 ABXA010088 1 20010309 A 3260 MS25237387 LIGHT BOEING 767 767281 1385109 NM COCKPIT INOPERATIVE A ABXA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 786AX 23019 THE RIGHT MAIN LANDING GEAR DOWN INDICATOR WAS NOTED TO BE INOPERATIVE DURING APPROACH. THE FLIGHT CREW COMPLIED WITH A BNORMAL PROCEDURES AND REPLACED THE INDICATOR BULB AS REQUIRED. THE LANDING GEAR WAS RECYCLED AND THE AIRCRAFT LANDED W ITHOUT ANY FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REPLACED THE INDICATOR LAMPS AND COMPLETED OPERATIONAL CHECKS. 2 L 7 2 4F RT A1NM 2001032800370 20010328 00370 WP 2001 3 28 ABXA010087 1 20010308 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 53194 47552 A FIVE INCH CREASE WAS NOTED ON THE FUSELAGE OUTER SKIN, APPROX 24 INCHES AFT AND 24 INCHES BELOW MAIN ENTRY DOOR. MAIN TENANCE REPAIRED AREA IAW DC-9 SRM 53-04 FIG 12B. 2 L 7 2 4F A6WE 2001032800371 20010328 00371 EU 2001 3 28 QXEA0100133 1 20010131 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- RIGHT HAND SIDE OF FUSELAGE HAS SCRATCHES IN SKIN ABOVE LAV SUMP VALVE PANEL. REPAIRED IAW FOKKER SRM 53-02-02 PAG E 2. 2 L 7 2 4F RT A20EU 2001032800373 20010328 00373 EU 2001 3 28 QXEA0100139 1 20010124 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CASTELLATION AT FRAME 200.75 AND STRINGER 41. REPAIRED IAW FOKKER SRM 53-10-05 PAGE 601. 2 L 7 2 4F RT A20EU 2001032800374 20010328 00374 EU 2001 3 28 QXEA0100149 1 20010213 A 7110 COWLING FOKKER F28 F28MK4000 4990810 EU LT ENGINE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- LEFT HAND ENGINE INBOARD COWL IS CHAFED ON FRAME 1200. REPAIRED IAW FOKKER SRM 51-31-01 PAGE 13 AND 14 AND HORIZON AIR EA 4-71-219. 2 L 7 2 4F RT A20EU 2001032800375 20010328 00375 EU 2001 3 28 QXEA0100156 1 20010126 A 5520 FITTING FOKKER F28 F28MK4000 4990810 EU ELEVATOR WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- LOWER LEFT HAND AND RIGHT HAND FITTING ON ELEVATOR BOOST UNIT HAS PLAY. REPAIRED IAW FOKKER SRM 20-20-03 AND HOR IZON AIR EA 4-55-280. 2 L 7 2 4F RT A20EU 2001032800376 20010328 00376 EU 2001 3 28 QXEA0100164 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 10346 AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800377 20010328 00377 EU 2001 3 28 QXEA0100172 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 12405 AND STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800378 20010328 00378 EU 2001 3 28 QXEA0100180 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 12405 AND STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032800379 20010328 00379 EU 2001 3 28 QXEA0100188 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 13815 AND STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032900122 20010329 00122 NM 2001 3 29 01FDEA00152 1 20010219 A 5311 65136481 FRAME BOEING 727 727233 138408A NM FUSELAGE MISDRILLED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 TWO DRILL STARTS IN I/B FLANGE OF FRAME BS 1010 ABOVE STR 16L. *S/D* REMOVED, REPLACED AND FAB OUT OF LIMITS DRILL STA RTS PER FEDEX SRM 53-10-1. REPAIR PARTS AND STR CLIP PER FEDEX SRM 51-40-3 & 51-30-2. 2 L 7 3 4F RT A3WE 2001032900123 20010329 00123 NM 2001 3 29 01FDEA00153 1 20010219 A 5313 BAC1493412 STRINGER BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CRACK IN STRINGER, BS 720B+4 INCH, STR 15R. *S/D* REMOVED, REPLACED AND FAB PER FEDEX 727 SRM 51-10-2 & 53-10-3 FIG 5. 2 L 7 3 4F RT A3WE 2001032900124 20010329 00124 NM 2001 3 29 01FDEA00157 1 20010216 A 5311 65163481 FRAME BOEING 727 727233 138408A NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 GOUGE IN O/B FLANGE OF FRAME BS 1148 ADJACENT TO STR 8L. *S/D* REMOVED, REPLACED AND FAB PER FEDEX SRM 51-40-3 FIG 1. 2 L 7 3 4F RT A3WE 2001032900125 20010329 00125 NM 2001 3 29 01FDEA00158 1 20010222 A 5531 65168113 RIB BOEING 727 727233 138408A NM VERTICAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 VERTICAL STAB, RT RIB CHORD IS CRACKED IN 3 PLACES AT FIN STA 133.8, STR 7 - 10R. *S/D* REMOVED, REPLACED AND FAB PER FEDEX SRM 55-30-5. 2 L 7 3 4F RT A3WE 2001032900127 20010329 00127 SO 2001 3 29 C2XA01CL036 1 20010227 A 3350 7287580503 LIGHT EMB 135 EMB135ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 25504 145186 CKE FLIGHT 3846 THE CREW REPORTED THE EMERGENCY LIGHT STRIP IN CABIN CENTER AISLE AT SEAT 5/6 IS INOPERATIVE. MAINTENAN CE RELEASED AIRCRAFT IAW MEL.33-50-00. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001032900128 20010329 00128 WP 2001 3 29 TWAA0103801 1 20010227 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DIRTY A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 922TW 48013 THE EGRESS LIGHTS FROM CABIN ROWS 29 THRU 33, AND THE EMERGENCY LIGHTS IN THE TAIL COMPARTMENT, WERE INOPERATIVE. FOUND RIBBON LIGHTS WITH MOISTURE AND DIRT AT CONTACTS. CLEANED RIBBON LIGHT CONNECTOR AND FEED CONNECTOR. CHECK-C 6-10-00 JFK. 2 L 7 2 4F A6WE 2001032900129 20010329 00129 WP 2001 3 29 TWAA0103803 1 20010227 A 5400 STRUCTURE DOUG DC9 DC931 3022065 WP PYLON CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 992Z 47095 DURING OP 15 MAINT CHECK NUMBER 2 ENGINE PYLON FAIRING STRUCTURE ON LOWER SIDE, FWD END HAD A CRACK BETWEEN TWO RIVETS. INSTALLED REPAIR PER SRM 54-01, PAGE 6. 2 L 7 2 4F A6WE 2001032900130 20010329 00130 WP 2001 3 29 MWEA010194 1 20010222 A 5310 99122439 ANGLE DOUG DC9 DC932 3022066 WP PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 FOUND CRACK ON LEFT FRONT SPAR PYLON BULKHEAD ANGLE AT FS 965, 2.75 LONG BETWEEN LONGERON 15-16 LEFT. REMOVED, FABRICAT ED, LOCATED AND INSTALLED NEW ANGLE. 2 L 7 2 4F A6WE 2001032900131 20010329 00131 WP 2001 3 29 MWEA010195 1 20010228 A 5310 9912451 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FORWARD BAG PIT, SHEAR TIE BETWEEN LONGERON 29 LEFT AND 29 RIGHT, STATION 362 HAS AREAS OF LIGHT CORROSION. REMOVED, FA BRICATED AND INSTALLED SHEAR CLIP. 2 L 7 2 4F A6WE 2001032900132 20010329 00132 EU 2001 3 29 C2XA01CL038 1 20010225 A 6123 WIRE AEROSP ATR42 ATR42320 8680930 EU RT WING CHAFED A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CR CRUISE 1 SW 27 14828 179 CLE FLIGHT 3175 THE CREW REPORTED THE NR 2 PROPELLER HAD A UNCOMMANDED FEATHER IN FLIGHT. THE CREW SHUTDOWN THE NR 2 EN GINE AND DECLARED A EMERGENCY. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE EVA LUATING THE PROBLEM. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND 2 WIRES CHAFED. THE WIRES ARE LOCATED BEHIND THE NR 2 EN GINE NACELLE AND THE WING SPAR IN THE FLAP WELL. THE WIRES CHAFED WERE 61-22-CF22 AND 61-22-473. ONE OF THE WIRES CARR IES 28VDC WHILE THE OTHER WIRE WENT TO THE FEATHER SOLENOID ON THE PCU. INTERMITTENTLY THE WIRES WOULD TOUCH AND SEND V OLTAGE TO THE FEATHER SOLENOID. THE WIRES WERE REPAIRED AND OPERATIONAL CHECKS WERE GOOD. 2 H 7 2 4T RT A53EU 2001032900133 20010329 00133 SO 2001 3 29 C2XA01IA132 1 20010225 A 3246 13889 BEARING EMB 145 EMB145ER SO NLG WHEEL FAILED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13936 0172 145025 IAH - FLIGHT 4137, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT THE LEFT HAND NOSE WHEEL INBOARD BEARING HAD FAIL ED. MAINTENANCE REMOVED AND REPLACED THE NOSE STRUT, AND BOTH WHEEL ASSEMBLIES, AND THE AIRCRAFT WAS APPROVED FOR RETUR N TO SERVICE. 2 L 7 2 4F RT T00011AT 2001032900134 20010329 00134 EU 2001 3 29 C2XA01IA133 1 20010228 A 3350 44 LIGHT AEROSP ATR42 ATR42320 8680930 EU PAX DOOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 86842 286 IAH - DURING A-CHECK INSPECTION, THE PASSENGER DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001032900135 20010329 00135 NM 2001 3 29 0100416304 1 20010208 A 2550 LOCK BOEING 747 747451 1384940 NM CARGO BAY LOOSE A NWAA K NONE O OTHER UK UNKNOWN 1 GL 01 664US 23819 UPON ARRIVAL, FLIGHT CREW ADVISED, A LOUD BANGING NOISE COMING FROM FORWARD CARGO COMPARTMENT. MAINTENANCE FOUND LOOSE PALLET LOCK AT STA 600, LEFT SIDE. MAINTENANCE REMOVED AND REPLACED LOCK. ALL CARGO EQUIPMENT CHECKED OK. 2 L 7 4 4F RT A20WE 2001032900136 20010329 00136 EU 2001 3 29 RAIA00103001 1 20010228 A 3297 WIRE AEROSP ATR42 ATR42300 8680920 EU NLG WW DAMAGED A RAIA K NONE O OTHER TO TAKEOFF 1 CE 03 426TE 228 7136-STL- DURING TAKEOFF ALL THREE LANDING GEAR TOOK TWO MINUTES TO RETRACT. MAINTENANCE REPLACED THE NOSE LANDING GEAR WEIGHT ON WHEELS WIRE IAW ATR42 WIRING MANUAL. 2 H 7 2 4T RT A53EU 2001032900147 20010329 00147 NM 2001 3 29 01FDEA00169 1 20010301 A 3231 DOOR BOEING 727 727233 138408A NM NLG OUT OF ADJ A FDEA O OTHER J WARNING INDICATION CR CRUISE 1 SO 25 282FE 22349 AT FL 250 340 KTS/84 GOT INTERMITTENT RED GEAR DOOR LIGHTS AND LOUD THUMP FROM NOSE GEAR. FOLLOW RED TAB AND RAISE GEAR HANDLE. LIGHT WENT OUT. ADJUSTED AND RETRACTED NOSE GEAR WHEEL WELL DOORS AS PER MM 32-22-001. 2 L 7 3 4F RT A3WE 2001032900148 20010329 00148 NM 2001 3 29 01FDEA00170 1 20010301 A 2752 MS9391130ZE4C MOTOR BOEING 727 727233 138408A NM MLG WW LEAKING A FDEA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 280FE 22347 DURING CRUISE SYS HYD QUANTITY READ ZERO, PRESS ZERO TOO. RED TAB PROC PUMPS TURN OFF 20 MIN. FOUND FLAP PWR UNIT HYD MOTOR LEAKING FROM TOP OF MOUNTING FLANGE AT FLAP PWR UNIT GEARBOX. REMOVED AND REPLACED FLAP HYD MOTOR IN REF TO 727-2 00 MM 27-51-062-4. OPS AND LEAK CK GOOD. REMOVED AND REPLACED BOTH 1 & 2 HYD CASE DRAIN FILTER PER MM 29-11-062-. OPS GOOD. 2 L 7 3 4F RT A3WE 2001042700043 20010427 00043 NM 2001 4 27 01FDEA00172 1 20010227 A 5343 MOUNT DOUG MD11 MD11F 3023600 NM CTR LAND GEAR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 CTR LAND GEAR - RT PILLOW BLOCK MOUNT HAS CORROSION IN BOLT HOLES, GUIDE PIN HOLE AND MATING SURFACE. *S/D* REMOVED AN D REPLACED BUSHING PER SRM 53-40-00 PG 69, CMM 20-20-07. 2 L 7 3 4F RT A22WE 2001042700044 20010427 00044 NM 2001 4 27 01FDEA00173 1 20010227 A 5343 MOUNT DOUG MD11 MD11F 3023600 NM CTR LAND GEAR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 CTR LAND GEAR - LT PILLOW BLOCK MOUNT HAS CORROSION IN BOLT HOLES, GUIDE PIN HOLE AND MATING SURFACE. REMOVED AND REPLA CED BUSHINGS PER SRM 53-40-00 PG 69, CMM 20-20-07. 2 L 7 3 4F RT A22WE 2001032900149 20010329 00149 WP 2001 3 29 MWEA010196 1 20010301 A 5320 2912412 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 INTERCOSTAL AT LONGERON 9 LEFT BETWEEN STATION 465 AND 484 HAS 3 MISDRILLED HOLES AND 2 IMPROPERLY PLUGGED HOLES. REMOV ED, FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001032900150 20010329 00150 WP 2001 3 29 MWEA010197 1 20010301 A 5320 277793 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FORWARD CARGO COMPARTMENT INTERCOSTAL BETWEEN STATION 465 AND 484 AND JUST OUTBOARD OF LONGERON 28 RIGHT HAS LIGHT CORRO SION AROUND NUT PLATES. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001032900151 20010329 00151 WP 2001 3 29 MWEA010198 1 20010301 A 5321 995780917 FLOOR PANEL DOUG DC9 DC914 3022034 WP CABIN DELAMINATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FROM E&E COMPARTMENT, FLOOR ABOVE SNAPS SHARPLY WHEN FLOOR ABOVE IS WALKED ON, AT AIRCRAFT AND APPROXIMATELY FS 200. LO CATED AND INSTALLED NEW PANEL. 2 L 7 2 4F A6WE 2001032900152 20010329 00152 WP 2001 3 29 MWEA010199 1 20010301 A 5330 5911424 SKIN DOUG DC9 DC914 3022034 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 DENT IN FUSELAGE SKIN AT STATION 791, 1.5 INCH ABOVE LONGERON 25 RIGHT. FABRICATED AND INSTALLED PATCH REPAIR. 2 L 7 2 4F A6WE 2001032900153 20010329 00153 WP 2001 3 29 MWEA010200 1 20010301 A 5320 99576703 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FASTENER HOLE NOT FILLED, INTERCOSTAL AT LONGERON 9 RIGHT, STATION 568. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001032900154 20010329 00154 WP 2001 3 29 MWEA010201 1 20010301 A 5320 2912901 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 TOOL MARKS ON INTERCOSTAL, CONTINUING UNDER FITTING, INTERCOSTAL AT LONGERON 10 RIGHT, STATION 556. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001032900155 20010329 00155 WP 2001 3 29 MWEA010202 1 20010301 A 5320 2912901 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 THREE FASTENER HOLES NOT FILLED, STATION 634, INTERCOSTAL AT LONGERON 10 RIGHT. REMOVED, FABRICATED AND INSTALLED REPAI R DOUBLER. 2 L 7 2 4F A6WE 2001032900156 20010329 00156 WP 2001 3 29 MWEA010203 1 20010301 A 5320 9957669 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 THREE FASTENER HOLES NOT FILLED, STATION 709, INTERCOSTAL AT LONGERON 8 LEFT. REMOVED, FABRICATED AND INSTALLED INTERCO STAL. 2 L 7 2 4F A6WE 2001032900157 20010329 00157 WP 2001 3 29 MWEA010204 1 20010301 A 5313 27779221 LONGERON DOUG DC9 DC914 3022034 WP FUSELAGE TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 TOOLING MARKS AT LONGERON 8 LEFT UPPER INNER SIDE BETWEEN STATION 218 AND 237. REMOVED, FABRICATED AND INSTALLED LONGER ON. 2 L 7 2 4F A6WE 2001032900158 20010329 00158 WP 2001 3 29 MWEA010205 1 20010301 A 5313 2777922 LONGERON DOUG DC9 DC914 3022034 WP FUSELAGE TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 TOOLING MARKS AT LONGERON 9 LEFT UPPER INNER SIDE BETWEEN STATION 218 AND 237. REMOVED, FABRICATED AND INSTALLED NEW LO NGERON SECTION. 2 L 7 2 4F A6WE 2001032900159 20010329 00159 WP 2001 3 29 MWEA010206 1 20010301 A 5313 2777922 LONGERON DOUG DC9 DC914 3022034 WP FUSELAGE TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 TOOLING MARKS AT LONGERON 7 LEFT UPPER INNER SIDE BETWEEN STATION 218 AND 237. REMOVED, FABRICATED AND INSTALLED NEW LO NGERON SECTION. 2 L 7 2 4F A6WE 2001032900160 20010329 00160 WP 2001 3 29 MWEA010207 1 20010301 A 5313 9915549 LONGERON DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 OPEN HOLES WITH IMPROPER SPACING ON LONGERON 5 RIGHT FORWARD OF FRAME STATION 218. REMOVED LONGERON SECTION, FABRICATED AND INSTALLED LONGERON SECTION AND SPLICE. 2 L 7 2 4F A6WE 2001032900161 20010329 00161 WP 2001 3 29 MWEA010208 1 20010301 A 5320 9915571 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 OPEN HOLES WITH NO SPACING AT INTERCOSTAL LOCATED AT LONGERON 9 RIGHT BETWEEN STATION 218 AND 237. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001032900162 20010329 00162 WP 2001 3 29 MWEA010209 1 20010301 A 5313 2912412 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 MISDRILLED HOLES WITH NO SPACING AT INTERCOSTAL LOCATED AT LONGERON 10 RIGHT, FORWARD SIDE OF INTERCOSTAL LOOKING FROM I NBOARD, STATION 218 - 237. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL AND BRACKETS. 2 L 7 2 4F A6WE 2001032900163 20010329 00163 NM 2001 3 29 UPS01235105 1 20010226 A 3260 SWITCH BOEING 727 72751C 1384015 NM MLG OUT OF ADJ A IPXA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 01 904UP 18946 INSPECTION TYPE:N/A ATB-AIR/GROUND SAFETY SENSOR FAILED IN GROUND ILLEG BUT LANDING GEAR RETRACTED NORMALLY. REPOSITION MAIN GEAR SAFETY SWITCH ILLEG AND PERFORMED SWITCH OPS CHECK AS PER B727 M/M 32-0211. NO DEFECTS NOTED. 2 L 7 3 4F A3WE 2001032900164 20010329 00164 WP 2001 3 29 TWAA0103901 1 20010223 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 EIBWD 49575 DURING CHECK-C MAINT FOUND INTERIM REPAIR AT STA 237, LONGERON 18L AND 19L. INSTALLED AND SECURED EXTERNAL DOUBLER PER SRM 53-04, PAGE 51 FIG 12B, SHEET 10. 2 L 7 2 4F RT A6WE 2001032900165 20010329 00165 WP 2001 3 29 TWAA0103902 1 20010227 A 5313 LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 992Z 47095 DURING OP 15 MAINT CHECK FOUND STRAP REPAIR AT LONGERON 20L, AT STA 223. FABRICATED LONGERON SECTION FOR L20 FROM STA 2 00 TO 229 PER SPM 6-70-01, AND SRM 53-11-1 PAGE 25 AND 26. ORDERED NEW LONGERON CLIP AT STA 200 PER SRM 53-11-1 PAGE 25 AND 26. TREATED SURFACES PER SRM 51-10-3. INSTALLED PER SRM 51-30-5, SRM 51-60-0, AND SRM 51-20-2. SEALED PER SRM 51 -20-0. 2 L 7 2 4F A6WE 2001032900166 20010329 00166 EU 2001 3 29 C2XA01IA135 1 20010228 A 2421 800326 COVER AEROSP ATR42 ATR42300 8680920 EU NR 2 ENGINE OUT OF POSITION A C2XA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 SW 27 16824 166 GPT - FLIGHT 4110, THE CREW REPORTED THAT THE NR 2 ENGINE POWER LEVER WOULD NOT RETARD. THE CREW SHUTDOWN THE NUMBER 2 ENGINE AS A PRECAUTION, AND THE AIRCRAFT LANDED AT GPT WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND T HE A/C GENERATOR LUG COVER TO BE BLOCKING THE POWER LEVER CONTROL AT THE HMU. MAINTENANCE REMOVED THE COVER FROM THE HM U AREA, REINSTALLED THE COVER IN ITS APPROPRIATE LOCATION, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001032900167 20010329 00167 SO 2001 3 29 C2XA01IA136 1 20010228 A 3350 3071BPE LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 58733 120197 IAH - FLIGHT 3353, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT SEVERAL EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED SEVERAL INOPERATIVE EMERGENCY EXIT LIGHT BULBS, AND THE AIRCRAFT WAS APPROVED FOR RETUR N TO SERVICE. 2 L 7 2 4T RT A31SO 2001032900168 20010329 00168 EU 2001 3 29 C2XA01IA137 1 20010228 A 3260 OL3112 LIGHT AEROSP ATR42 ATR42320 8680930 EU COCKPIT SHORTED A C2XA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SW 27 15816 105 IAH - FLIGHT 2990, THE CREW REPORTED THAT WHEN THE LANDING GEAR SELECTOR WAS PLACED IN THE UP POSITION THE LANDING GEAR CONTROL CIRCUIT BREAKER POPPED. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED T HE AIRCRAFT AND FOUND A BULB SHORTING OUT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, PERFORMED OPERATIO NAL CHECKS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001032900169 20010329 00169 GL 2001 3 29 C2XA01IA139 2 20010214 A 7230 23065323 BLADE ALLSN EMB 145 EMB145ER SO ALLSN AE300 AE3007A GL NR 2 ENGINE NICKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14943 CAE311561 145040 CAE311561 IAH - DURING C-CHECK INSPECTION, THE NUMBER TWO ENGINE WAS FOUND TO HAVE A NICKED FAN BLADE. MAINTENANCE REMOVED AND RE PLACED THE AFFECTED BLADE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001032900171 20010329 00171 NM 2001 3 29 HNAA0100015 1 20010228 A 3230 82245 TUBE DHAV DHC8 DHC8102 2809003 NM NLG BENT A HNAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 07 911HA 13565 034 NOSE LANDING GEAR DID NOT INDICATE LOCKED DOWN WITH NORMAL AND ALTERNATE INDICATION. CREW RETRACTED GEAR AND PERFORMED ALTERNATE EXTENSION. NORMAL INDICATION STILL SHOWED UNSAFE, BUT ALTERNATE INDICATION SHOWED GEAR AS LOCKED DOWN. AIRCR AFT LANDED WITHOUT INCIDENT. FOUND NLG DRAG STRUT PIVOT TUBE BENT. REPLACED PIVOT TUBE. 2 H 7 2 4T RT A13NM 2001032900172 20010329 00172 NM 2001 3 29 0100646302 1 20010228 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 622US 23720 DURING OVERNIGHT LINE CHECK, MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT ROW 51ABC-62ABC. REPLACED THE LIGHT ASSEMBLY AT ROW 61ABC. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001032900173 20010329 00173 NM 2001 3 29 0100656303 1 20010226 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 663US 23818 DURING LINE CHECK, MAINTENANCE FOUND PATH ESCAPE PATH LIGHTING INOPERATIVE ROW 21 - 31R AND ROW 51 - 65L. SECURED LOOSE WIRE. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001032900174 20010329 00174 NM 2001 3 29 0100666302 1 20010221 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 662US 23720 DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE ROWS 51 - 62L. RECONNECTED LOOSE WIRING AT ROW 62ABC - 51ABC. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001032900175 20010329 00175 NM 2001 3 29 0100676634 1 20010227 A 3350 BATTERY PACK BOEING 747 747227B 1384888 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 634US 22234 DURING LINE CHECK, MAINTENANCE FOUND C-ZONE EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATION AL CHECK NORMAL. 2 L 7 4 4F A20WE 2001032900176 20010329 00176 NM 2001 3 29 0100682289 1 20010226 A 3233 65178322 CYLINDER BOEING 727 727251 138408H NM NLG LEAKING A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 289US 50982 22207 21377 DURING CLIMB, THE HYDRAULIC SYSTEM A-QUANTITY WENT TO ZERO. CREW FOLLOWED COM PROCEDURES AND RETURNED TO MSP AND MADE A N UNEVENTFUL LANDING. MAINTENANCE REPLACED NOSE GEAR TRANSFER CYLINDER. LEAK AND OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 2001032900177 20010329 00177 NM 2001 3 29 0100692287 1 20010226 A 2761 ROD END BOEING 727 727251 138408H NM SPOILER BROKEN A NWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 01 287US 21375 DURING CLIMBOUT, CREW NOTICED RIGHT ROLL REQUIRING 30'' YOKE INPUT TO MAINTAIN LEVEL FLIGHT. UPON VISUAL INSPECTION OF WINGS, CREW NOTED RIGHT WING NR 13 AND NR 14 SPOILERS WERE ABOUT 10 TO 15 INCHES IN UP POSITION. MAINTENANCE REPLACED B ROKEN SPOILER CONTROL ROD END. OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 2001032900178 20010329 00178 NE 2001 3 29 0100709986 2 20010223 A 7321 7436024 FUEL CONTROL DOUG DC9 DC932 3022066 WP PWA JT8 JT8D15 52051 NE RT ENGINE FAILED A NWAA C ABORTED TAKEOFF X ENGINE FLAMEOUT TO TAKEOFF 1 GL 01 986US 48939 3936 47480 700519 DURING TAKEOFF, THE RIGHT ENGINE EXPERIENCED A COMPRESSOR STALL AND THEN CEASED TO OPERATE. TAKEOFF WAS ABORTED AT 60 K TS WITHOUT INCIDENT. MAINTENANCE INSPECTED THE RIGHT ENGINE WITH NO DISCREPANCIES REPORTED AND REPLACED THE RIGHT ENGIN E FUEL CONTROL UNIT. OPERATIONAL CHECK NORMAL. ALSO, THERE WAS HEAVY SNOWFALL REPORTED AT LGA AT THE TIME OF THE INCID ENT AND DEICING PROCEDURES WERE ACCOMPLISHED PRIOR TO DEPARTURE. 2 L 7 2 4F 4 F A6WE E2EA 2001032900179 20010329 00179 WP 2001 3 29 0100719855 1 20010223 A 7830 SWITCH DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE LT ENG T/R DIRTY A NWAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 01 764NC 47717 696701 DURING TAKEOFF, THE LEFT ENGINE REVERSER UNLOCK INDICATION LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AT 120 KTS WITHOUT IN CIDENT. MAINTENANCE CLEANED THE UPPER AND LOWER REVERSER INDICATING SWITCHES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F 4 F RT A6WE E2EA 2001032900180 20010329 00180 2001 3 29 0100733206 4 20010223 A 3140 COMPUTER AIRBUS 320 A320211 3930320 EU COCKPIT MALFUNCTIONED A NWAA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 306US 60 SHORTLY AFTER LIFT-OFF, RECEIVED SMOKE AFT CARGO SMOKE MESSAGE. FOLLOWED ECAM AND COM PROCEDURES AND RETURNED TO DEPART URE FIELD FOR NORMAL LANDING. MAINTENANCE REPLACED THE SPENT FIRE EXTINGUISHER BOTTLE AND THE FLIGHT WARNING COMPUTER. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 2001032900181 20010329 00181 WP 2001 3 29 0100749868 1 20010221 A 5754 59267456 STOP DOUG DC9 DC951 3022051 WP RT SLAT DOOR BROKEN A NWAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 01 777NC 47787 DURING APPROACH WHEN SLATS EXTENDED, AIRCRAFT EXPERIENCED A ROLL TO THE LEFT AND THE SLAT DISAGREEMENT LIGHT ILLUMINATED . FOLLOWED COM PROCEDURES AND ACCOMPLISHED A SAFE NO SLAT LANDING AT JAX. MAINTENANCE FOUND THE MECHANICAL STOP ON NR 9R SLAT DOOR BROKEN AND LEFT AND RIGHT NR 9 SLAT TRACK DOOR JAMMED. NR 9L AND NR 9R LEADING EDGE SLAT TRACK CUTOUT DOOR S WERE MISSING. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2001032900182 20010329 00182 CE 2001 3 29 C2XA01CL039 1 20010226 A 7120 12991004713 TRUSS BEECH 1900 1900D 1154162 CE NR 1 ENGINE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 81556 5758 5758 UE239 DURING A 2ND 200 HR INSPECTION MAINTENANCE DISCOVERED A CRACK ON THE NR 1 ENGINE TRUSS ASSEMBLY AT THE WELD OF THE TOP A TTACHMENT POINT OF THE OUTBOARD COWLING MOUNT BRACKET. MAINTENANCE REPLACED THE TRUSS ASSEMBLY AND THE AIRCRAFT WAS REL EASED FOR SERVICE. 2 L 7 2 4T RT A24CE 2001032900183 20010329 00183 EA 2001 3 29 COMA0160291 1 20010228 A 3234 7179015 CONTROL HANDLE CNDAIR CL600 CL6002B19 EA INST PANEL MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 917CA 4698 7017 LANDING GEAR DID NOT RETRACT. REPLACED THE LANDING GEAR SELECTOR LEVER. 2 L 7 2 4F RT A21EA 2001032900184 20010329 00184 EA 2001 3 29 COMA0160292 1 20010228 A 2760 COMPUTER CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTIONED A COMA K NONE N FALSE WARNING TO TAKEOFF 1 SO 01 814CA 7387 GLD UNSAFE, SPOILER FAULT, INBD GROUND SPOILER FAULT. COULD NOT DUPLICATE. RESET THE SPOILER COMPUTER. 2 L 7 2 4F RT A21EA 2001032900185 20010329 00185 EA 2001 3 29 COMA0160293 1 20010228 A 3040 16591 CONTROLLER CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 776CA 5010 7293 RIGHT WINDSHIELD HEAT CAUTION MESSAGE. REPLACED THE RT WINDSHIELD HEAT CONTROLLER. 2 L 7 2 4F RT A21EA 2001032900186 20010329 00186 EA 2001 3 29 COMA0160294 1 20010228 A 3040 16591 CONTROLLER CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 785CA 11768 7326 LEFT WINDOW HEAT CAUTION MESSAGE. REPLACED THE LT WINDOW HEAT CONTROLLER. 2 L 7 2 4F RT A21EA 2001032900192 20010329 00192 WP 2001 3 29 MWEA010210 1 20010302 A 5230 591015793 DOOR DOUG DC9 DC932 3022066 WP CARGO DOOR CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 AFT PIT DOOR SKIN HAS 10 CHAFED AREAS ON THE UPPER AREA OF THE SKIN. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001032900193 20010329 00193 WP 2001 3 29 MWEA010211 1 20010302 A 5320 991050131 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 CUSP MEMBRANE IS CRACKED UNDER NR 4 SEAT BETWEEN FS 218 - 237. REMOVED WEB, FABRICATED, LOCATED, DRILLED AND INSTALLED NEW WEB. 2 L 7 2 4F A6WE 2001032900194 20010329 00194 WP 2001 3 29 MWEA010212 1 20010302 A 5313 591141581 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 LONGERON 5 LEFT IS CRACKED WHERE IT ATTACHES TO FRAME AT FS 639. REMOVED DAMAGE SECTION, DRILLED AND INSTALLED NEW SECT IONS. 2 L 7 2 4F A6WE 2001032900195 20010329 00195 NM 2001 3 29 CALA0100173 1 20010228 A 5330 DOUBLER BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73385 26314 INSPECTION FOUND LOWER STRAP DOUBLER CORRODED AT LOWER DOOR JAMB, STA 787 - 796. THE STRAP DOUBLER WAS REMOVED AND REPL ACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001032900196 20010329 00196 NM 2001 3 29 CALA0100174 1 20010301 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND FLOORBEAM CORRODED AROUND FASTENER HOLES ON TOP SURFACE AT STA 967, LBL 20 - LBL 45. THE CORRODED SECT ION OF FLOORBEAM WAS CUT OUT AND A REPAIR WAS INSTALLED IAW ECRA 5310-04101 AND EA 04-5310-0678. 2 L 7 2 4F RT A16WE 2001032900197 20010329 00197 NM 2001 3 29 CALA0100175 1 20010301 A 5320 ANGLE BOEING 737 7373T0 1384582 NM L1 DOOR SILL CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND L-1 LOWER DOOR SILL INNER ANGLE SUPPORT CORRODED FROM STA 315 - 340. THE ANGLE SUPPORT WAS REMOVED AND A NEW ANGLE SUPPORT WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001032900198 20010329 00198 NM 2001 3 29 CALA0100176 1 20010301 A 5320 WEB BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND CREASE BEAM SHEAR WEB CORRODED AT STA 797, LT SIDE. A NEW WEB WAS INSTALLED IAW SRM 51-40-2. 2 L 7 2 4F RT A16WE 2001032900199 20010329 00199 NM 2001 3 29 CALA0100177 1 20010301 A 5230 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND INNER SKIN TORN ON INSIDE OF FWD CARGO DOOR AT LIGHTENING HOLE. THE TORN AREA WAS REMOVED AND A DOUBLE R WAS INSTALLED IAW SRM 51-70-13, 52-30-01, AND 51-40-02. 2 L 7 2 4F RT A16WE 2001032900200 20010329 00200 NM 2001 3 29 CALA0100178 1 20010301 A 5320 STRAP BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND FLOORBOARD SUPPORT STRAP CORRODED AT STA 1006 - 1016, LBL 2. THE STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW DRAWING 65C32677 AND SRM 51-10-2. 2 L 7 2 4F RT A16WE 2001032900201 20010329 00201 NM 2001 3 29 CALA0100179 1 20010301 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND AFT CABIN FLOORBEAM T-CAP CORRODED FROM LEFT TO RIGHT SIDE AT STA 986.5. THE FLOORBEAM T-CAP WAS REMOV ED AND REPLACED IAW SRM 51-70-13 AND ECRA 5310-03851. 2 L 7 2 4F RT A16WE 2001032900202 20010329 00202 NM 2001 3 29 CALA0100180 1 20010301 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND FLOOR SUPPORT ATTACH ANGLE CORRODED AROUND FASTENER AT STA 259, RBL 2.0. THE CORROSION WAS REMOVED IAW SRM 51-10-2 AND A REPAIR WAS INSTALLED IAW SRM 51-70-11. 2 L 7 2 4F RT A16WE 2001032900203 20010329 00203 NM 2001 3 29 CALA0100181 1 20010301 A 5311 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND A 1 INCH CRACK IN R-1 DOOR FORWARD STUB FRAME JUST ABOVE THE INNER FLANGE OF THE LOWER SILL AT STA 294. 5. THE INNER FLANGE OF THE FWD FRAME WAS REPAIRED IAW EA 5310-03895 AND SRM 51-20-01. 2 L 7 2 4F RT A16WE 2001032900204 20010329 00204 NM 2001 3 29 CALA0100182 1 20010301 A 5320 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND FLOOR SUPPORT CUSP ANGLE CORRODED AT STA 927 - 1000, LBL 50. THE FLOOR SUPPORT CUSP ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-2. 2 L 7 2 4F RT A16WE 2001032900205 20010329 00205 NM 2001 3 29 CALA0100183 1 20010301 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND SEAT TRACK CORRODED AT STA 900 - 927, RBL 45. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A REP AIR SECTION OF SEAT TRACK WAS INSTALLED IAW SRM 51-10-02 AND 53-00-52. 2 L 7 2 4F RT A16WE 2001032900206 20010329 00206 NM 2001 3 29 CALA0100184 1 20010301 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 967 - 986, LBL 16. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51 -40-2. 2 L 7 2 4F RT A16WE 2001032900207 20010329 00207 NM 2001 3 29 CALA0100185 1 20010301 A 5320 WEB BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND A 1.25 INCH CRACK IN WEB AT FRAME OF AFT PIT CUTOUT AREA, FORWARD SIDE, BS 787, S25R. THE WEB WAS REMO VED AND A NEW WEB WAS INSTALLED IAW SRM 53-60-15, FIGURE 1, 51-20-01, AND 51-40-01. 2 L 7 2 4F RT A16WE 2001032900208 20010329 00208 NM 2001 3 29 CALA0100186 1 20010301 A 5743 FITTING BOEING 737 7373T0 1384582 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17329 23459 INSPECTION FOUND A 1 INCH CRACK IN LT WING MLG SUPPORT BEAM O/B ATTACH FITTING AT AFT SPAR. A NEW FITTING WAS INSTALLED IAW WORK CARD 03-5743-1-0003. 2 L 7 2 4F RT A16WE 2001032900209 20010329 00209 SO 2001 3 29 C2XA01CL040 1 20010227 A 3350 7287580503 LIGHT EMB 145 EMB145ER SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13935 145022 CLE FLIGHT3989 THE CREW REPORTED CABIN EMERGENCY LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT STRIP AND PERFORMED OPERATIONAL CHECKS. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001032900210 20010329 00210 SO 2001 3 29 C2XA01CL041 1 20010228 A 3350 7287580503 LIGHT EMB 135 EMB135ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 25504 145186 CLE FLIGHT 4118 THE CREW REPORTED CABIN EMERGENCY LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT STRIP AND PERFORMED OPERATIONAL CHECKS. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001032900211 20010329 00211 WP 2001 3 29 MWEA010213 1 20010302 A 5313 S27779223 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 LONGERON 4 LEFT CRACKED AT STATION 699, RIGHT ABOVE THE FRAME. REMOVED SPLICES AND LONGERON SECTION, FABRICATED AND INS TALLED SPLICES AND LONGERON SECTION. 2 L 7 2 4F A6WE 2001032900212 20010329 00212 WP 2001 3 29 MWEA010214 1 20010302 A 5320 991556163 ANGLE DOUG DC9 DC932 3022066 WP STATION 996 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 CORROSION ON ANGLE BRACKET ON AFT SIDE OF LEFT LAV FLOORBEAM AT STATION 996 UNDER U-CHANNEL SUPPORT, 19 INCHES RIGHT OF CUSP. REMOVED, FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F A6WE 2001032900213 20010329 00213 WP 2001 3 29 MWEA010215 1 20010302 A 5320 2913044513 CLIP DOUG DC9 DC932 3022066 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DEEP GOUGE ON CLIP AND INTERCOSTAL, BETWEEN FLOORBEAMS STATION 699 & 718, JUST RIGHT OF CENTER SUPPORT. REMOVED, FABRIC ATED AND INSTALLED CLIP. 2 L 7 2 4F A6WE 2001032900214 20010329 00214 WP 2001 3 29 MWEA010216 1 20010302 A 5320 99577247 CLIP DOUG DC9 DC932 3022066 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DEEP GOUGE ON CLIP AND INTERCOSTAL BETWEEN FLOORBEAMS, STATION 699 AND STATION 718, BETWEEN CENTER SUPPORT AND NR 2 SEAT TRACK. REMOVED, FABRICATED AND INSTALLED CLIP. 2 L 7 2 4F A6WE 2001032900215 20010329 00215 WP 2001 3 29 MWEA010217 1 20010302 A 5311 5911448507 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FORWARD BAG PIT, FUSELAGE FRAME AT STATION 351, AFT SIDE, HAS A LARGE AREA OF LIGHT CORROSION FROM LONGERON 28 LEFT TO L ONGERON 28 RIGHT. FORMED, LOCATED, DRILLED AND INSTALLED RIGHT AND LEFT HAND REPAIR PARTS. 2 L 7 2 4F A6WE 2001032900216 20010329 00216 WP 2001 3 29 UPS01835132 1 20010125 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, FWD BAG PIT CRACK UNDER UPPER FLANGE OF FRAME 420 AT LONG 29L. REMOVED SUPPORT, FABBED SUPPORT, A LODINED, PRIMED AND INSTALLED CHANNEL SUPPORT IAW DAC DWG 3773159 DC8 SRM 51-1-21 & 51-1-8. 2 L 7 4 4F RT 4A25 2001032900217 20010329 00217 WP 2001 3 29 UPS01835135 1 20010126 A 5510 BULKHEAD DOUG DC8 DC873F 302199F WP RT HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, RT HORIZ STAB JACKSCREW FWD MOUNTING BULKHEAD HAS CRACKS THAT HAVE GONE THROUGH STOP DRILLS 2 EACH . REPAIRED IAW DC8 SRM 53-2-0 FIG 23. 2 L 7 4 4F RT 4A25 2001032900218 20010329 00218 WP 2001 3 29 UPS01835136 1 20010126 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, EXTERIOR FUSELAGE SKIN HAS LG CORROSION BULGE AT LAP SEAM STA 1875.0 S-32-R. REPLACED SKIN PER DA C DWG 5649329. 2 L 7 4 4F RT 4A25 2001032900219 20010329 00219 WP 2001 3 29 UPS01835138 1 20010127 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, AFT PIT FS 1240 FRAME CORRODED BETWEEN L36 AND L34R. MAT ID FOR REPAIR ANGLES .080 7075-0 IAW REO -G07850 CORROSION ON FRAME FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. LOCATED AND DRILLED IAW DC8 SRM 51-1-24. ALOD INED AND PRIMED REPAIR ANGLES IAW DC8 SRM 51-1-8. INSTALLED REPAIR ANGLES INTERCOSTALS AND FITTING/CLIPS IAW DC8 SRM 51 -1-20D. 2 L 7 4 4F RT 4A25 2001032900220 20010329 00220 WP 2001 3 29 UPS01835140 1 20010130 A 5320 WEB DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, COCKPIT SUBFLOOR RT O/B SIDE BETWEEN FS -50.6 & FS -38.6 CORROSION ON FINGER WEB O/B AND BELOW F/E CONTROL PANEL LOWER PULLEY BRACKET ASSY. FABBED FINGER DOUBLERS -21 -27 -25 DOUBLERS FILLER AND -23 SPLICE IAW DAC DWG SRO 8530026. INSTALLED FINGER DOUBLERS DUCTS, PULLEY COVERS AND GROUNDING PANELS IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001032900221 20010329 00221 WP 2001 3 29 UPS01835143 1 20010223 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C2,3 RIGHT WING L/E RIB IS CRACKED AT XFS 597.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001032900222 20010329 00222 WP 2001 3 29 UPS01835144 1 20010223 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C2,3 RIGHT WING L/E RIB IS CRACKED AT XFS 585. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001032900223 20010329 00223 WP 2001 3 29 UPS01835145 1 20010223 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C2,3 RIGHT WING L/E RIBS ARE CRACKED AT XFS 647.5, 672.5, 685, AND 697.5. REPAIRED RIBS IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001032900224 20010329 00224 WP 2001 3 29 UPS01835146 1 20010223 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C2,3 LEFT WING L/E UPPER RIBS ARE CRACKED AT XS 491.193, XS 503.789. REPAIRED RIBS IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001032900225 20010329 00225 WP 2001 3 29 UPS01835147 1 20010223 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C2,3 RIGHT WING L/E RIB IS CRACKED AT XFS 778.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001032900226 20010329 00226 WP 2001 3 29 UPS01835148 1 20010223 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C2,3 RIGHT WING L/E RIB IS CRACKED AT XFS 816.25. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001032900227 20010329 00227 WP 2001 3 29 UPS01835149 1 20010223 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C2,3 RIGHT WING L/E RIB IS CRACKED AT XFS 785. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001032900228 20010329 00228 WP 2001 3 29 UPS01835150 1 20010223 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C2,3 RIGHT WING L/E RIB IS CRACKED AT XFS 747.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001032900229 20010329 00229 WP 2001 3 29 UPS01835151 1 20010222 A 5320 4645535503 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C2,3 STA 950 LOWER KEEL BETWEEN GEAR DOORS DOOR SUPPORT ANGLE IS CRACKED. REMOVED, FABRICATED, AND REP LACED ANGLE IAW DWG 4645535, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001032900230 20010329 00230 NM 2001 3 29 SWAA010625 1 20010302 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 387SW 26602 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED AT LBL 5, WL 198 & RBL 5, WL 201. REPAIRED BULKHEAD W EB PER SRM. 2 L 7 2 4F RT A16WE 2001032900231 20010329 00231 NM 2001 3 29 SWAA010626 1 20010302 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 387SW 26602 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD VERTICAL WEB CRACKED AT LBL 17, WL 190. REPAIRED BULKHEAD VERTICA L WEB PER SRM. 2 L 7 2 4F RT A16WE 2001032900232 20010329 00232 NM 2001 3 29 SWAA010627 1 20010302 A 5753 6546434 SKIN BOEING 737 7373H4 1384600 NM LT T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 622SW 27932 DURING SCHEDULED 1/2D CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD SIDE. REMOVED AND REPLACED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2001032900233 20010329 00233 NM 2001 3 29 SWAA010628 1 20010302 A 5753 6546435 SKIN BOEING 737 7373H4 1384600 NM LT T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 622SW 27932 DURING SCHEDULED 1/2D CHECK, FOUND LT WING T/E OUTBOARD AFT FLAP DELAMINATED AT INBOARD SIDE. REMOVED AND REPLACED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2001032900234 20010329 00234 NM 2001 3 29 SWAA010629 1 20010302 A 5753 6546435 SKIN BOEING 737 7373H4 1384600 NM LT T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 623SW 27933 DURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD LOWER SURFACE. REMOVED AND REPLAC ED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2001032900235 20010329 00235 NM 2001 3 29 SWAA010630 1 20010302 A 3350 6556633 LENS BOEING 737 7373A4 1384585 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT LIGHT LENS MISSING AT BOTH OVERWING EXITS. REPLACED LENSES PER MM. 2 L 7 2 4F RT A16WE 2001032900236 20010329 00236 NM 2001 3 29 SWAA010631 1 20010302 A 5312 6546547 BULKHEAD BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED D-CHECK, FOUND BS 727 BULKHEAD WEB CRACKED AT WL 148, LBL 6.5 & RBL 6.5. REPAIRED BULKHEAD WEB PER BFG ER. 2 L 7 2 4F RT A16WE 2001032900237 20010329 00237 NM 2001 3 29 SWAA010632 1 20010302 A 5330 6545775 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED D-CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 727E+5, BELOW STR 26R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001032900238 20010329 00238 NM 2001 3 29 SWAA010633 1 20010302 A 5313 6551698 SPLICE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 513SW 24190 DURING SCHEDULED D-CHECK AT DALFORT, FOUND STR SPLICE 4L CRACKED AT BS 907. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2001032900239 20010329 00239 NM 2001 3 29 SWAA010634 1 20010302 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 723SW 27855 DURING SCHEDULED C4 CHECK, FOUND NUMEROUS EEPLS TRACK COVERS CRACKED THROUGHOUT CABIN. REMOVED AND REPLACED TRACK COVER S PER MM. 2 L 7 2 4F RT A16WE 2001032900240 20010329 00240 NM 2001 3 29 SWAA010635 1 20010303 A 2752 M59391130ZE4C MOTOR BOEING 737 7373Q8 1384670 NM MLG W/W INOPERATIVE A SWAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 07 687SW 23388 DECLARED EMERGENCY. DURING APPROACH, FLAPS WOULD NOT EXTEND BEYOND POSITION 1. REMOVED AND REPLACED FLAP DRIVE HYDRAUL IC MOTOR PER MM. 2 L 7 2 4F RT A16WE 2001032900241 20010329 00241 NM 2001 3 29 SWAA010636 1 20010302 A 5754 65C26601 SKIN BOEING 737 7373H4 1384600 NM RT SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND NR 6 L/E SLAT SKIN CRACKED AT OUTBOARD TRACK CUTOUT, AFT ROW OF RIVETS. REMOVED AND REPLACED NR 6 SLAT PER PER MM. 2 L 7 2 4F RT A16WE 2001032900242 20010329 00242 NM 2001 3 29 SWAA010637 1 20010303 A 5210 6545871 DOOR FRAME BOEING 737 7373H4 1384600 NM ENTRY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR FRAME CRACKED AT UPPER FWD LATCH ATTACHMENT POINT. REMOVED AND REPLAC ED FWD ENTRY DOOR PER MM. 2 L 7 2 4F RT A16WE 2001032900243 20010329 00243 NM 2001 3 29 SWAA010638 1 20010303 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT LBL 17 TO LBL 29. REPAIRED BULKHEAD PER SWA ACO. 2 L 7 2 4F RT A16WE 2001032900244 20010329 00244 NM 2001 3 29 SWAA010639 1 20010303 A 5230 6545871 DOOR FRAME BOEING 737 7373H4 1384600 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO DOOR FWD FRAME CRACKED AT ASSIST CABLE PULLEY LOWER ATTACH BOLT. REMOVED A ND REPLACED CARGO DOOR PER MM. 2 L 7 2 4F RT A16WE 2001032900245 20010329 00245 NM 2001 3 29 SWAA010640 1 20010303 A 5330 6545857 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT AFT SVC DOOR, FWD LOWER CORNER CUTOUT. REPAIRED SKIN PER SWA RA. 2 L 7 2 4F RT A16WE 2001032900246 20010329 00246 NM 2001 3 29 SWAA010641 1 20010303 A 5754 6573714 SKIN BOEING 737 7373A4 1384585 NM RT SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED C2 CHECK, FOUND NR 5 L/E SLAT HAS 5 SKIN CRACKS AT AFT ROW OF FASTENERS, INBOARD OF ACTUATOR. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2001032900247 20010329 00247 NM 2001 3 29 SWAA010642 1 20010302 A 5310 6547978 CREASE BEAM BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED C3 CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 639, STR 17L. REPAIRED CREASE BEAM WEB PER SRM. 2 L 7 2 4F A16WE 2001032900248 20010329 00248 NM 2001 3 29 SWAA010643 1 20010302 A 5311 6546540 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 17L. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2001032900249 20010329 00249 NM 2001 3 29 SWAA010644 1 20010303 A 3260 65C28034 SENSOR BOEING 737 7373Y0 1384671 NM NLG MALFUNCTIONED A SWAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 308SA 23498 AIR TURNBACK. DURING DEPARTURE, NLG HAD RED AND GREEN LIGHTS ILLUMINATED UPON RETRACTION. ACCOMPLISHED CHECKLIST AND R ECEIVED THREE GREEN LIGHT INDICATION. REMOVED AND REPLACED BOTH NLG UPLOCK AND DOWNLOCK SENSORS PER MM. 2 L 7 2 4F RT A16WE 2001032900250 20010329 00250 NM 2001 3 29 AWXA0001481 1 20010307 A 7711 005RL03 RELAY AIRBUS A319 A319132 NM IAE V2524 V2524A5 NE NR 2 ENG FAULTY A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 807AW 15521 1323 1064 V10587 PHX - AIR TURNBACK - 3/1/01 - THE CREW GOT A ENG NR 2 EPR MODE FAULT, N1 MODE XX AND RETURNED TO PHX. IN PHX DURING TRO UBLESHOOTING OF NR 2 FADEC, HAD P2T2 SENSE/RELAY BOX/HC2 MESSAGE. INSPECTED THE FADEC WIRE HARNESS AND CONNECTOR FOR SE CURITY AND NO DISCREPANCIES FOUND. REPLACED THE RELAY BOX IAW AMM 71-51-49-000-010 AND 71-51-49-400-010 AND OPERATIONAL LY TESTED GOOD IAW AMM 71-51-49-710-050. NO FAULTS WERE RECORDED ON FADEC2A AND FADEC2B; ENGINE RUNS WERE GOOD AND ALL INDICATIONS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2001032900251 20010329 00251 EU 2001 3 29 QXEA0100174 1 20010124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CRACKED CLIP AT FRAME 12405 AND STRINGER 42. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 2001032900252 20010329 00252 EU 2001 3 29 QXEA0100211 1 20010127 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CORROSION ON LEFT HAND INBOARD SEAT TRACK BL600LH AT FRAME 11905. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 AND 53-40 -01 PAGE 206. 2 L 7 2 4F RT A20EU 2001032900253 20010329 00253 EU 2001 3 29 QXEA0100212 1 20010127 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CORROSION ON LEFT HAND INBOARD SEAT TRACK BL600LH AT FRAME 11905. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 AND 53-40 -01 PAGE 206. 2 L 7 2 4F RT A20EU 2001032900254 20010329 00254 EU 2001 3 29 QXEA0100213 1 20010127 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CORROSION ON RIGHT HAND SEAT TRACK BL600RH BETWEEN STATIONS 6805 AND 7305. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 AND 53-40-01 PAGE 206. 2 L 7 2 4F RT A20EU 2001032900255 20010329 00255 EU 2001 3 29 QXEA0100214 1 20010127 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CORROSION ON RIGHT HAND INBOARD SEAT TRACK BL600RH BETWEEN STATIONS 6805 AND 7305. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 AND 53-40-01 PAGE 206. 2 L 7 2 4F RT A20EU 2001032900256 20010329 00256 EU 2001 3 29 QXEA0100215 1 20010127 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CORROSION ON RIGHT HAND INBOARD SEAT TRACK BL600RH BETWEEN STATIONS 7305 AND 7805. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 AND 53-40-01 PAGE 206. 2 L 7 2 4F RT A20EU 2001032900257 20010329 00257 EU 2001 3 29 QXEA0100216 1 20010127 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CORROSION FOUND ON RIGHT HAND INBOARD SEAT TRACK BL600RH BETWEEN STATION 7305 AND 7805. REPAIRED IAW FOKKER SRM 51 -10-4 PAGE 9 AND 53-40-01 PAGE 206. 2 L 7 2 4F RT A20EU 2001032900258 20010329 00258 EU 2001 3 29 QXEA0100217 1 20010126 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CORROSION ON STRINGER 60 BETWEEN FRAMES 3820 AND 4175, BELOW STATIC INVERTER. REPAIRED IAW FOKKER SRM 53-02-05. 2 L 7 2 4F RT A20EU 2001032900259 20010329 00259 EU 2001 3 29 QXEA0100218 1 20010126 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CORROSION ON STRINGER 68 BETWEEN FRAMES 3820 AND 4175 BELOW STATIC INVERTER. REPAIRED IAW FOKKER SRM 51-31-01 AND 53-02-05. 2 L 7 2 4F RT A20EU 2001032900260 20010329 00260 EU 2001 3 29 QXEA0100219 1 20010126 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CORROSION ON AFT SIDE OF FRAME 9305A BETWEEN STRINGER 1 AND 2. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 AND 53-01-01 PAGE 5. 2 L 7 2 4F RT A20EU 2001032900261 20010329 00261 EU 2001 3 29 QXEA0100220 1 20010126 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CORROSION ON AFT SIDE OF FRAME 9305A ABOVE STRINGER 73. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, 53-01-01 PAGE 5 AN D 51-31-01 PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001032900262 20010329 00262 EU 2001 3 29 QXEA0100221 1 20010126 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CORROSION ON AFT SIDE OF FRAME 9305A ABOVE STRINGER 73. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 AND 53-01-01 PAGES 5 AND 6. 2 L 7 2 4F RT A20EU 2001032900263 20010329 00263 EU 2001 3 29 QXEA0100222 1 20010126 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 YYC- CORROSION ON AFT SIDE OF FRAME 9305A BETWEEN STRINGERS 1 AND 2. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 AND 53-01-0 1 PAGE 5. 2 L 7 2 4F RT A20EU 2001032900264 20010329 00264 NM 2001 3 29 F3LA200100041 1 20010308 A 5753 69378151 TUBE BOEING 737 73736E NM LT FOREFLAP CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 317FL 2959 25263 DURING C-1 CHECK, INSPECTION REPORTED INTERIOR OF LT INBD FOREFLAP SUPPORT TUBE CORRODED. REPLACED LT INBD FOREFLAP SUP PORT TUBE PER BAC OHM 57-53-26. 2 L 7 2 4F RT A16WE 2001032900265 20010329 00265 EU 2001 3 29 QXEA0100252 1 20010307 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478US 11227 GEG-EXIT SIGN ABOVE COCKPIT DOOR INOPERATIVE IN 28V POSITION. REPLACED LIGHT CIRCUIT BOARD. LIGHTS CHECK GOOD IN 3V AN D 28V POSITION. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001032900267 20010329 00267 NM 2001 3 29 F3LA200100042 1 20010310 A 2130 CONTROL UNIT BOEING 737 7372L9 1384497 NM PRESSURIZE SYS MALFUNCTIONED A F3LA G A O2 MASK DEPLOYED UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 270FL 22733 AIR TURNBACK. FLIGHT CREW REPORTED PRESSURIZATION SYSTEM WARNING HORN SOUNDED AT 14000 FT AND OXYGEN MASKS DROPPED. AI RCRAFT RETURNED TO DEN WITHOUT INCIDENT. PERFORMED OPERATIONAL TEST OF PRESSURIZATION CONTROL SYSTEM PER MM 21-31-0 AND FOUND NO DISCREPANCIES. SERVICED CREW OXYGEN PER MM 12-15-21. REPLACED PASSENGER OXYGEN BOTTLE PER MM 12-15-21. CLEA NED AND STOWED CABIN OXYGEN MASKS PER MM 35-21-59 AND 35-21-52. SERVICED THREE PORTABLE CABIN OXYGEN BOTTLES PER MM 12- 15-21. AS A PRECAUTIONARY PROCEDURE, PRESSURIZED AIRCRAFT TO 4 PSI DIFFERENTIAL PRESSURE WITH NO PROBLEMS NOTED. 2 L 7 2 4F RT A16WE 2001032900268 20010329 00268 WP 2001 3 29 RRXA010011 1 20010213 A 8097 WIRE DOUG DC10 DC1010F 3022111 WP STARTER VALVE DAMAGED A RRXA C E ABORTED TAKEOFF ENGINE SHUTDOWN J WARNING INDICATION TO TAKEOFF 1 WP 15 68043 46902 DURING TAKEOFF ROLL, NR 3 ENGINE START LIGHT CAME ON AND STAYED ON AFTER ENGINE SHUT DOWN. REPAIRED WIRING AT PRESSURE FEED THROUGH ON NR 3 ENGINE STARTER VALVE SYSTEM OP CHECKS GOOD IAW DC-10 M/M CHAPTER 74-00-01. 2 L 7 3 4F A22WE 2001032900269 20010329 00269 WP 2001 3 29 RRXA010012 1 20010216 A 3250 CONTROL CABLE DOUG DC8 DC873F 302199F WP NLG DEFECTIVE A RRXA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 15 795FT 46103 ON TAXI OUT LOST NOSE STEERING AIRCRAFT WAS TOWED BACK TO EMERGENCY RAMP BY AIRPORT DELTA SUPER TUG. GEAR PIN INSTALLED . REMOVED AND REPLACED RIGHT SIDE NOSE STEERING CABLE IAW DC-8 M/M 22-51-0. OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2001032900270 20010329 00270 WP 2001 3 29 RRXA010013 1 20010227 A 7931 12583 PRESSURE SWITCH DOUG DC8 DC871F 302199D WP NR 4 ENG INOPERATIVE A RRXA K NONE O OTHER CR CRUISE 1 WP 15 8076U 45941 NR 4 ENGINE LOW OIL PSI LIGHT INOP. TRANSFERRED TO DMI LIST AS CONTROL B-9616122-0962 CAT: B MEL 7906 ATA 7910 DUE DATE 02MAR01 PLACARD INSTALLED. REMOVED AND REPLACED NR 4 ENG LOW OIL PRESS SW, OPS AND LEAK CHECK GOOD IAW DC-8 M/M 79-32- 2. (LOW OIL PRESS SWITCH) NO DEFECTS NOTED ON ENG RUN THIS CLEARS DMI B9616122-0962. PLACARD REMOVED. 2 L 7 4 4F RT 4A25 2001032900271 20010329 00271 WP 2001 3 29 RRXA010014 1 20010228 A 3250 ACCUMULATOR DOUG DC8 DC873F 302199F WP NLG STEERING LOW A RRXA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 15 604AL 46047 ON TAKEOFF ROLL AIRPLANE YAWED TO THE LEFT UNCONTROLLABLE, ALL ENGINE PARAMETERS WERE EQUAL AND THROTTLES ALIGNED MAX SP EED WAS 70 KNOTS F/O HAD FULL RIGHT RUDDER APPLIED. INSPECTED NOSE GEAR FOUND FWD ACCUMALTOR LOW NOSE STEERING SERVICE D FWD NOSE STEERING ACCUMALTOR TO 500 PSI IAW M/M CH 32-52-0. NO OTHER DEFECTS NOTED. 2 L 7 4 4F RT 4A25 2001032900272 20010329 00272 WP 2001 3 29 RRXA010015 1 20010302 A 2910 AE24600002E0270 HYDRAULIC LINE DOUG DC8 DC862F 3021972 WP HYD SYSTEM RUPTURED A RRXA K NONE K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 15 997CF 46154 ON TAXI IN A/C LOST ALL HYD FLUID. FOUND FLEX LINE ON STOW PUMP RUPTURED. REMOVED AND REPLACED FLEX LINE. LEAK AND OP CK''S GOOD. A/C RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2001032900273 20010329 00273 WP 2001 3 29 RRXA010016 1 20010308 A 2612 FIRE DETECTOR DOUG DC8 DC871F 302199D WP NR 2 ENGINE ACTIVATED A RRXA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 15 500MH 45812 NR 2 ENG FIRE WARN SYS ACTIVATED INFLIGHT. ENG SHUTDOWN. OUTBOARD FIRE AGENT DISCHARGED. REMOVED AND REPLACED 3 FIRE DETECTOR ELEMENTS AND FIRE DETECTOR CNT''L UNIT. OP''S CHECKS GOOD IAW UAL MM 26-11-07. 2 L 7 4 4F RT 4A25 2001032900274 20010329 00274 NM 2001 3 29 AWXA0001483 1 20010312 A 2612 654956928 FIRE LOOP BOEING 737 73733A 1384673 NM NR 2 PYLON OUT OF POSITION A AWXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 165AW 23626 PHX - AIR TURNBACK - 3/5/01 - ON CLIMBOUT AT FL270 W/ FULL POWER, THE RT WING BODY OVERHEAT LIGHT ILLUMINATED; W/ THE IS OLATION VALVE CLOSED AND RIGHT BLEED OFF THE LIGHT EXTINGUISHED. MAINTENANCE TROUBLESHOT AND FOUND FIRE LOOP IN NR 2 PY LON TO CLOSE TO THE DUCT AND REPOSITIONED; FOUND A LEAK AT THE CLAMP ON THE NR 2 ENGINE STRUT TO WING DUCT AND THE RT PA CK PRIMARY HEAT EXCHANGER DUCT PULLED AWAY FROM THE HEAT EXCHANGER DUE TO 3 SCREW HOLES BROKEN OUT OF THE DUCT; THE RAM AIR DUCT ASSY WAS REPLACED; FUNCTIONAL AND LEAK CHECKS WERE GOOD. ELEMENT - KIDDIE - P/N 899319 - LOC: RT PYLON - COND: TO CLOSE CLAMP - VOSS IND. - P/N VC1139-350 - LOC: RT L/E - COND: DISTORTED. 2 L 7 2 4F RT A16WE 2001032900275 20010329 00275 EU 2001 3 29 AWXA0001484 2 20010312 A 7200 ENGINE BOEING 737 73733A 1384673 NM CFMINT CFM56 CFM563B2 13802 EU NR 2 ENGINE MALFUNCTIONED A AWXA O OTHER J WARNING INDICATION DE DESCENT 1 WP 28 175AW 23634 721533 PHX - EMERGENCY LANDING - 3/5/01 - INBOUND TO PHX THE AIRCRAFT WAS DESCENDING AT 210 KTS AS DIRECTED BY THE FMC, THE CRE W SELECTED 250 KTS MANUALLY AND THE AIRCRAFT YAWED TO THE RIGHT; THE FIRST OFFICER REPORTED NR 2 ENGINE FAILURE. THE CR EW THEN STARTED TO GO THROUGH THE ENGINE SHUTDOWN CHECKLIST AND NOTICED ALL ENGINE INDICATIONS WERE NORMAL. AN UNEVENTF UL LANDING IN PHX WAS MADE. PHX MAINTENANCE RAN BOTH ENGINES; PERFORMED TEST NR 8 PER AMM 71-00-00 W/ NO FAULTS NOTED. PERFOMED A POWER ASSURANCE RUN PER AMM 71-00-01 W/ NO DISCREPANCIES. NO FURTHER PROBLEMS REPORTED TO DATE. 2 L 7 2 4F 4 F RT A16WE E21EU 2001032900276 20010329 00276 NM 2001 3 29 01FDEA00161 1 20010223 A 5730 SKIN BOEING 727 727247 138408F NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 233FE 21327 DURING ROUTINE INSP, LT WING LEAD EDGE SKIN FOUND CRACKED NEAR NR 3 LEAD EDGE SLAT. ** S/D ** R&R & FAB PER IAW BAC 727 SRM 57-30-4. 2 L 7 3 4F A3WE 2001033000049 20010330 00049 NM 2001 3 30 CA010125008 1 20010104 A 7603 77620049001 CABLE DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE CONTROL CABLE WORN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING SCHEDULED ENGINE INSPECTION, THE NR 1 ENGINE LOWER CONDITION LEVER CABLE WAS FOUND TO BE WORN TO LIMITS IN THE USUAL PLACE, FORWARD OF THE FIREWALL. THE CABLE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2001033000050 20010330 00050 NM 2001 3 30 CA010125009 1 20010106 A 2910 82910010197 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) INVESTIGATION OF A HYDRAULIC LEAK IN THE NOSE OF THE AIRCRAFT REVEALED A LARGE PINHOLE IN THE LINE FROM THE TEE AT STN X37.00 TO THE STEERING CONTROL GEAR UP. THE LINE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001033000051 20010330 00051 EA 2001 3 30 CA010125010 1 20010104 A 7110 7892132002 EEC DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NR 2 ENGINE FAILED W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA 16351 1646 (CAN) THE FLIGHT CREW REORTED THAT THE NR 2 ENGINE TORQUE GAUGE WENT BLANK ON ROTATION. DURING THE UNSCHEDULED LANDING, THE NR 2 ENGINE WOULD NOT CONTROL PROPERLY. THE FDR WAS PULLED AND THE READOUT SHOWED NO EVIDENCE OF OVERTORQUE OR ANY O THER ABNORMALITIES. ENGINE OVERTORQUE OR AN ELECTRICAL SIGNAL INTERRUPTION TO THE TORQUE INDICATOR ARE THE ONLY CARITERI A WHICH CAUSE THE TORQUE INDICATOR TO GO BLANK. THE SIGNAL FOR THE GAUGE COMES THROUGH THE EECU THE EECU WAS REPLACED AN D THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2001033000052 20010330 00052 EA 2001 3 30 CA010125011 1 20010108 A 2910 82950010175 LINE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE LT NR 2 SPOILER LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) DURING ROUTINE INSPECTOIN A HYDRAULIC LEAK WAS DISCOVERED IN THE LT NR 2 SPOILER UNLOADING LINE. THE SOURCE WAS A PINHOLE IN THE LINE. A REPLACEMENT LINE WAS INSTALLED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2001033000053 20010330 00053 EA 2001 3 30 CA010126002 1 20010104 A 3231 83232036001 ROD END DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE LT MLG DOOR BROKEN W O OTHER D INFLIGHT SEPARATION CR CRUISE 1 CA (CAN) THE FLIGHT CREW REPORTED A HARMONIC NOISE FROM THE FORWARD COCKPIT FLOOR AREA WHICH VARIED WITH AIRSPEED. INVESTIG ATION AREVEALED A BROKEN ACTUATING ROD ON THE LT AFT DOOR OF THE NOSE LANDING GEAR. THE ROD ASSY WAS REPLACED AND THE AI RCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2001033000054 20010330 00054 EA 2001 3 30 CA010126003 1 20010104 A 2710 82700568S00 CONTROL CABLE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE AILERON WORN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING SCHEDULED INSPECTION, THE RT LOWER AILERON CABLE WAS FOUND TO BE WORN AND SPIKED IN AN AREA IMMEDIATELY OUT BOARD OF THE RT NACELLE. THE CABLE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. TTAF 22,210 HRS.TCAF 32,196 CY C. 2 H 7 2 4T 4 T RT A13NM E20NE 2001033000055 20010330 00055 NM 2001 3 30 CA010126004 1 20010105 A 3260 PIN DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE CONNECTOR PLUG DAMAGED W O OTHER R PARTIAL RPM/PWR LOSS AP APPROACH 1 CA (CAN) THE FLIGHT CREW REPORTED AND UNSAFE GEAR LIGHT WITH NO NOSE GEAR GREEN INDICATION AFTER LANDING GEAR DOWN SELECTIO N. AN ALTERNATE EXTENSION WAS PERFORMED AND THE AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE INVESTIGATION REVEALED THAT A CONNECTOR PLUG FROM THE NOSEO GEAR HARNESS TO THE AIRFRAME RECEPTACLE HAD A WIRING PIN THAT HAD BEEN PUSHED BACK AND WAS NOT MAKING A POSITIVE CONNECTION IN THE RECEPTACLE. THE PIN WAS REINSTALLED AND GEAR SWINGS PERFORMED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001033000056 20010330 00056 NM 2001 3 30 CA010126005 1 20010105 A 3060 KCD4N RELAY DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE PROP HEAT STUCK W H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 CA (CAN) THE FLIGHT CREW REPORTED THAT THE RT PROPELLER HEAT B PHASE WAS STUCK IN THE ON POSITION. THIS WAS CONFIRMED WITH THE LOADMETER. THEY PULLED THE CB TO DEACTIVATE THE SYSTEM. MAINTENANCE INVESTIGATION RESULTED IN REPLACEMENT OF PROP HE AT RELAY 3061-K4 WHICH HAD COANTACTS A1 AND A2 STUCK CLOSED. THE RELAY WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SER VICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001033000057 20010330 00057 WP 2001 3 30 CA010126011 1 20010126 A 2730 CON1316D27210345 CONTROL CABLE GRUMAN TS2 TS2ACALFORST 3951102 WP WRIGHT R1820 982C9HE2 67020 EA HAMSTD 43D 43D51 NE ELEVATOR WORN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING WINTER MAINTENANCE, INSPECTION OF THE ELEVATOR DOWN CABLE REVEALED EXCESSIVE WEAR ON THE CABLE. THE CABLE I S BEING REPLACED WITH A NEW CABLE. ALL OTHER ELEVATOR AND RUDDER CABLES INSPECTED AND WERE SERVICEABLE. NOTE: THIS AIRCR AFT WAS MODIFIED IAW CONAIR SL 1288-001 CONTROL CABLE GROMMET REPLACEMENT. ALL OTHER CONAIR FLEET AIRCRAFT WILL BE INSPE CTED FOR SERVICEABILITY OF THE ELEVATOR AND RUDDER CABLES. 2 H 7 2 4R 4 R A25WE E259 6 C P8879 2001033000060 20010330 00060 NM 2001 3 30 CA010129003 1 20010102 A 7921 28E997 FITTING PWA PW120A DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE OIL COOLER LEAKING W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 12748 120320 (CAN) ON JAN 02/2001 CREW OF A/C C-GTAF, S/N 087 ABORTED ITS TAKEOFF OUT OF GRAND PRAIRE (YQU) DUE TO ILLUMINATED OF NR 2 OIL PRESSURE LIGHT DURING TAKEOFF ROLL. A/C RETURNED TO GATE WITH NO FURTHER INCID. TO RPT. CRA CONTRA CTED ENGINEER F ROM SWAN AERO 2000 TO INSPECT A/C. INIT INSP REVEALED LOW OIL QUANTITY. OIL LEVEL TOPPED UP & GROUND RUNS WERE COMPLETED . POST RUN UP INSP FOUND LEAK AT INBOARD OIL COOLER CONNECTION. CARA ENG INEER SENT TO YQU WITH PARTS & FURTHER INSP. MA INT FOUND CAUSE OF LEAK TO BE O-RING IN OIL COOLER BYPASS VALVE. PARTS WERE REPL&A/C GROUND CHECKED FOR LEAKS.A/C RT-SRV WITH NO FURTHER I NCIDENTS TO RPT. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001033000063 20010330 00063 NE 2001 3 30 CA010129011 2 20010103 A 7321 0164248800 FUEL CONTROL SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1A2 60030 NE ENGINE MALFUNCTIONED W E ENGINE SHUTDOWN O OTHER TX TAXI/GRND HDL 1 CA 766 (CAN) ENGINE FAILED TO ACCELERATE BEYOND 32 PERCENT NG DURING FIRST START OF DAY. FCU REPLACED AND SENT FOR INSPECTION/R EPAIR. RENTAL FCU INSTALLED. 2001-01-30TC: AWAIT SUPPLIMENTAL SDR WHEN MORE INFORMATION BECOMES AVAILABLE. 1 G 7 1 3U 3 U H9EU E19EU 2001033000077 20010330 00077 EU 2001 3 30 CA010201002 1 20010106 A 5610 NP1653114 WINDSHIELD AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE COCKPIT FAILED W O OTHER O OTHER AP APPROACH 1 CA (CAN) ON APPROACH, FIRST OFFICER WINDSHIELD SHATTERED.WINDSHIELD CHANGED. 2 L 7 2 4F 4 F RT A28NM E29NE 2001033000095 20010330 00095 SO 2001 3 30 CA010205024 1 20010115 A 5712 78500002 RIB PIPER PA34 PA34200 7103405 SO LYC O360 IO360C1E6 41514 EA WING CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 8014 (CAN) DURING THE 50 HOURS INSPECTION, THE RIB MEMBRANE LOCATED OUTSIDE THE MAIN LANDING GEAR (LT SIDE) WAS FOUND CRACKED AND DEFORMED. 1 L 7 2 3O 3 O A7SO 1E10 2001033000096 20010330 00096 EA 2001 3 30 CA010205025 1 20010118 A 3260 6008500185 INDICATOR MESSIER 6008500185 CNDAIR CL601 CL6012A12 1900303 EA GE CF34 CF341A NE LT MLG LOCK STUCK W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 15667 1380 DCL2198699R (CAN) ON JAN 16, IT RPTED IN LOG BOOK THAT THE LEFT MLG GREEN LIGHT REMAINS ON WHILE RETRACTING. LEFT LOCK IND THEN CLEA RED BY MAINT PERS & RETRACTION TESTS WERE PERFORMED BEFORE A/C RETURNED TO SERVIC E.ON JAN 17, LOWERED LDG GEAR LIGHT ON WITH GREEN LDG GEAR UP TWICE ON LT SIDE&ONCE ON RT SIDE.IN EACH CASE, IT RPTED THAT GREEN LDG GEAR LIGHT WENT OFF ON I TS OWN 5 TO 10 MIN AFTER RETRACTION. THESE PROBLEMS WERE LINKED TO MLG STRUT RETRACTION ACTUATOR LOCK IND. 2 ACTUATOR ML G SIDE STAY WERE REPL BEFORE RETURNING A/C TO SERVICE. 2 L 7 2 4F 4 F RT A21AE E15NE 2001033000097 20010330 00097 NM 2001 3 30 2001UALA00077 1 20010205 A 5270 S283W2023 SENSOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CARGO DOOR MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 773UA 23004 0 26929 FWD CARGO DOOR WARNING LIGHT CAME ON AT FL310 ON CLIMBOUT. DIVERTED TO LHR. *S/D* MAINTENANCE AT LHR CLEANED SENSOR, CONFIRMED LATCHED AND LOCKED DOOR, AND APPLIED MEL CARD TO REQUIRE VERBAL CONFIRMATION THAT DOOR IS LOCKED AND LATCHED P RIOR TO EACH TAKEOFF. DISPLAY MESSAGE 52-12330 WAS CONFIRMED FOR THIS PROBLEM. BASED ON INFORMATION, OAKEG 777 FLEET UPDATED DEFERRED ITEM DF657 TO ACCOMPLISH TROUBLESHOOTING PROCEDURE AND PROVIDE UPDATED PART INFORMATION. RECOMMENDATIO N TO REPLACE NOTED SENSOR HAS YET TO BE ACCOMPLISHED (AIRCRAFT PRESENTLY IN PME FOR MAINTENANCE). 2 L 7 2 4F 4 F RT T0001SE E46NE 2001033000098 20010330 00098 NM 2001 3 30 2001UALA00078 1 20010204 A 3260 656021132 ACCESSORY UNIT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE EE BAY FAILED A UALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 WP 29 7258U 21405 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO LGA. *S/D* REPLACED LANDING GEAR ACCESSORY UNIT PE R MAINTENANCE MANUAL. JACKED AIRCRAFT AND CYCLED GEAR HANDLE 30 TIMES. OPERATIONAL CHECK NORMAL ON GROUND. 2 L 7 3 4F 4 F A3WE E2EA 2001033000099 20010330 00099 NM 2001 3 30 2001UALA00092 1 20010207 A 5330 SKIN PANEL BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 618UA 21878 EXTERIOR FUSELAGE VHF RIGHT ANTENNA SKIN CUTOUT CORRODED STATION 510 BL 0. *S/D* SKIN REPAIRED PER SRM 53-30-01 AT OSV TIMCO. 2 L 7 2 4F 4 F RT A1NM E3NE 2001033000100 20010330 00100 NM 2001 3 30 2001UALA00093 1 20010208 A 5311 FRAME BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 618UA 21878 AFT CARGO PIT AT BS 1197 FROM RBL 13-19, FRAME CAP IS CORRODED. *S/D* FRAME T-CAP WAS REPLACED BY OSV TIMCO, REFRENCE 51-40-02 FOR FASTENER INSTALLATION PROCEDURES. 2 L 7 2 4F 4 F RT A1NM E3NE 2001033000101 20010330 00101 NM 2001 3 30 2001UALA00095 1 20010208 A 5270 CIRCUIT BOARD BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EE BAY FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 643UA 25093 ON DEPARTURE FROM SFO AT APPROX 1500 FT FORWARD CARGO DOOR EICAS MESSAGE ILLUMINATED. WENT OFF AFTER APPROX FIVE MINUTE S. DID NOT CHECK CARGO LIGHTS. *S/D* REPEAT NUISANCE MESSAGE WAS CORRECTED BY VERIFYING ADJUSTMENT OF FORWARD CARGO D OOR LOCK SENSOR, CLOSE SWITCH AND INDICATION LIGHT PER MM 52-71-02, WHICH WERE FOUND WITHIN LIMITS DESCRIBED. PROBLEM W AS ISOLATED TO NR 3 LOGIC CARD WHICH WAS REPLACED AND SUBSEQUENT OPERATIONAL CHECK SATISFACTORY WITH ALL OPERTIONS NORMA L. 2 L 7 2 4F 4 F RT A1NM E24NE 2001033000102 20010330 00102 NM 2001 3 30 2001UALA00096 1 20010209 A 2751 10619263 INDICATOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE TE FLAPS MALFUNCTIONED A UALA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 7445U 21899 CREW REPORTED THAT TRAILING EDGE FLAPS WERE IN ASYMMETRIC LOCKOUT. INBOARD FLAPS WERE AT 5 DEGREES AND OUTBOARD FLAPS D ID NOT REACH 5 DEGREES AND LOCKED UP. DIVERTED TO COS FOR BETTER BRAKING ACTION. EMERGENCY DECLARED. *S/D* REPLACED INBOARD AND OUTBOARD FLAP INDICATORS. SYSTEM OPERATION CHECKS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001033000103 20010330 00103 NM 2001 3 30 2001UALA00101 1 20010210 A 5320 141W8518 STIFFENER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 204UA 9369 0 28713 CRACKED STA 246 FLOORBEAM FORWARD VERTICAL STIFFENERS AT: LBL - 7.88, 38.5RBL - 7.88, 38.0, 44.95, 50.0. *S/D* REPLAC ED STIFFENERS PER SRM 53-10-51, REPAIR 3. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001033000104 20010330 00104 NM 2001 3 30 2001UALA00102 1 20010209 A 2910 B-NUT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE ELEV FEEL COMP LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 7461U 21915 THE AIRCRAFT EXPERIENCED A SYSTEM A-HYDRAULIC FLUID LOSS DURING CRUISE. AIRCRAFT DIVERTED TO CLE. *S/D* FOUND LOOSE B -NUT ON ELEVATOR FEEL COMPUTER FILTER HOUSING LINE. TIGHTENED APPROX 1 FULL TURN. STATIC LEAK STOPPED. SERVICED A-HYD SYSTEM TO FULL. RAN ENGINES, CYCLED FLIGHT CONTROLS. NO LEAKS NOTED. 2 L 7 3 4F 4 F A3WE E2EA 2001033000105 20010330 00105 NM 2001 3 30 2001UALA00107 1 20010209 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 618UA 21878 AFT CARGO PIT AT BS 1307 BETWEEN STRINGERS 36L AND 36R SHEAR TIE IS CORRODED. *S/D* SHEAR TIE WAS REPLACED BY OSV TIMC O, REFERENCE SRM 51-40-02 FOR FASTENER INSTALLATION PROCEDURES. 2 L 7 2 4F 4 F RT A1NM E3NE 2001033000106 20010330 00106 NM 2001 3 30 2001UALA00108 1 20010209 A 2782 ACTUATOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LE SLAT BROKEN A UALA K NONE K J FLUID LOSS WARNING INDICATION LD LANDING 1 WP 29 7442U 21896 HYDRAULIC SYSTEM-A FAILURE OCCURRED DURING FINAL APPROACH. LOST FLUID THEN PRESSURE. *S/D* FOUND NR 6 L/E SLAT ACT RE TAINER CAP SEVERED FROM END OF THE ACTUATOR, WITH THE ACTUATOR IN THE FULLY EXTENDED AND LOCKED POSITION. REMOVED FAILE D ACTUATOR, INSTALLED AND SAFETIED REPLACEMENT ACTUATOR. OPERATED SYSTEM SEVERAL TIMES WITH NORMAL FLIGHT DECK INDICATI ONS AND NO LEAKAGE. 2 L 7 3 4F 4 F A3WE E2EA 2001033000107 20010330 00107 NM 2001 3 30 2001UALA00111 1 20010212 A 5320 ATTACH ANGLE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 618UA 21878 AFT CARGO PIT BS 1087 STRINGER 39R FRAME TO STRINGER ATTACH ANGLE CORRODED. *S/D* STRINGER ATTACH ANGLE WAS REPLACED B Y OSV TIMCO, REFERENCE SRM 51-40-02 FOR FASTENER INSTALLATION PROCEDURES. 2 L 7 2 4F 4 F RT A1NM E3NE 2001033000108 20010330 00108 NM 2001 3 30 2001UALA00115 1 20010213 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 645UA 25280 EXTERIOR FUSELAGE SKIN DENT STATION 445, BETWEEN STRINGERS 24L AND 26L. *S/D* SKIN REPAIR PER SRM 53-00-01 FIGURE 206 WAS ACCOMPLISHED AT OSV TIMCO. 2 L 7 2 4F 4 F RT A1NM E24NE 2001033000109 20010330 00109 NM 2001 3 30 2001UALA00118 1 20010215 A 5311 FRAME BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 618UA 21878 AFT PIT BS 1153 BETWEEN STRINGER 39L AND 39R FRAME WEB HAS ELONGATED HOLE. *S/D* WEB REPAIR INSTALLED BY OSV TIMCO, RE FERENCE SRM 51-40-02 FOR FASTENER INSTALLATION PROCEDURES. 2 L 7 2 4F 4 F RT A1NM E3NE 2001033000110 20010330 00110 EU 2001 3 30 MALA010231 1 20010221 A 5330 DOUBLER SAAB SF340 340B 7860101 EU FUSELAGE SEPARATED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 424XJ 424 FOUND DURING C-CHECK, RT ICESHIELD IS LIFTING AT SL 1615. REFER TO CELSIUS W/O 19347, TASK 2544, AND SAAB EO 340SDS0010 21. MAINTENANCE REMOVED AND REPLACED, CHECKED FOR HIDDEN DAMAGE. REMOVED ICESHIELD AND CLEANED AREA IAW SRM 53-70-10. FABRICATED NEW ICESHEILD REF: SRM 53-70-10, PREPED, INSTALLED IPM12 030 AND SEALED REF: SRM 53-70-10. FOR PAINT SEE W /O 19347, TASK 2515. DENTS WITHIN LIMIT REF SRM 51-10-10 AND ACCEPTED AS IS REF SAAB EO 340SDS001021 NDT PERFORMED. 2 L 7 2 4T RT A52EU 2001033000111 20010330 00111 EU 2001 3 30 C2XA01CL042 1 20010227 A 3150 NSA93412101C MOUNT AEROSP ATR42 ATR42320 8680930 EU COCKPIT BURNED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 14819 156 RDU FLIGHT 3003 THE CREW REPORTED THE ANNUNCIATOR LIGHT TEST CIRCUIT BREAKER POPPED AND SMOKE SMELL WAS NOTICED BUT DISS IPATED QUICKLY. MAINTENANCE REPLACED DIODE MOUNT VD35. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SE RVICE. 2 H 7 2 4T RT A53EU 2001033000112 20010330 00112 EU 2001 3 30 MALA010252 1 20010222 A 3260 UPLOCK SWITCH SAAB SF340 340B 7860101 EU LANDING GEAR ICED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 427XJ 427 FLIGHT 2969 LANDING GEAR WOULD NOT RETRACT (INTRANSIT LIGHT STAYS ON). AIR TURNBACK TO CLE. MAINTENANCE UPON INSPECTIO N FOUND ICE BUILD UP ON UPLOCK SWITCHES. CLEANED AND MELTED ICE, PERFORMED NUMEROUS GEAR SWINGS AND CHECKS IAW SAAB AMM CH 32. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2001033000113 20010330 00113 NM 2001 3 30 DHL2001720007 1 20010302 A 5230 LATCH BOEING 727 727228 NM CARGO DOOR OUT OF ADJ A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 720DH 19544 MAIN CARGO DOOR ANN LIGHT ON S/O''S DOOR ANN PANEL ILLUMINATED IN FLIGHT AT 6.0 PSI DIFF. ABNORMAL PROCEDURES COMPLETED . ADJUSTED LATCH OVER CENTER SWITCH, S12. OPS CHECK GOOD. PERFORMED VISUAL INSPECTION OF MECHANISM, NO FAULTS NOTED. PRESSURIZED A/C TO 7.0 PSI. NO DEFECTS NOTED IAW PEMCO MM SUP 52-32-0. 2 L 7 3 4F A3WE 2001033000114 20010330 00114 2001 3 30 DHL2001717005 4 20010302 A 3431 5222450115 RECEIVER BOEING 727 72723 1384004 NM COCKPIT MALFUNCTIONED A DHLA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 717DH 19389 CAPTAIN AND F/O''S VOR''S SCALLOPS AND WILL NOT TRACK PROPERLY. DIVERTED TO CVG. REMOVED AND REPLACED NR 1 VOR/ILS REC EIVER IAW B727 MM 34-31-21. OPS CHECK OK. P/N OFF 522450-115, S/N 5889, P/N ON 522-4280-107, S/N ON B9818. 2 L 7 3 4F A3WE 2001033000115 20010330 00115 EU 2001 3 30 C2XA01CL043 1 20010301 A 3260 D22924010 SENSOR AEROSP ATR42 ATR42320 8680930 EU LT MLG DIRTY A C2XA K NONE N FALSE WARNING CL CLIMB 1 SW 27 14819 156 CLE FLIGHT 3024 THE CREW REPORTED THE LEFT MAIN GEAR HAD UNLOCK LIGHT WHEN THE GEAR WAS RETRACTED. THE SYSTEM INDICATED NORMAL WHEN THE GEAR IS DOWN. MAINTENANCE INSPECTED AND CLEANED THE PROXIMITY SENSORS AND PERFORMED OPERATIONAL CHECKS . THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A53EU 2001033000118 20010330 00118 NM 2001 3 30 2001UALA00124 1 20010215 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 618UA 21878 AFT CARGO PIT BS 1197 BETWEEN STR 37L AND 38L SHEAR TIE CORRODED. REPLACED SHEAR TIE BY OSV TIMCO, REFERENCE SRM 51-40 -02 FOR FASTENER INSTALLATION PROCEDURES. 2 L 7 2 4F 4 F RT A1NM E3NE 2001033000119 20010330 00119 NM 2001 3 30 2001UALA00125 1 20010217 A 5322 ANGLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 645UA 25280 MAIN CABIN BS 860 - 870 LBL 89 FLOORBEAM L-ANGLE BETWEEN UPPER CHORD TO SEAT TRACK CRACKED. C-CHECK. REPLACED L-ANGLE, REF SRM 51-40-02 FOR FASTENER INSTALLATION PROCEDURES. 2 L 7 2 4F 4 F RT A1NM E24NE 2001033000120 20010330 00120 NM 2001 3 30 2001UALA00134 1 20010214 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 618UA 21878 AFT CARGO PIT AT BS 1395, STRINGER 39L END FITTING IS CORRODED BOTH SIDES OF STRINGER. REMOVED CORROSION FROM STRINGER PER GN-MM 5-0-6-1. REPLACED STRINGER SPLICE CLIPS PER BAC DWG 146T3006 STRINGER SPLICE CLIPS PER BAC DWG 146T3006 AND I NSTALLED PER SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001033000121 20010330 00121 NM 2001 3 30 2001UALA00136 1 20010206 A 5311 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 645UA 25280 AFT CARGO PIT AT BS 1197 AT LBL 5 - 26 FRAME T-CAP HAS AREAS OF CORROSION. REPLACED T-CAP PER SRM. 2 L 7 2 4F 4 F RT A1NM E24NE 2001033000122 20010330 00122 WP 2001 3 30 TWAA0104001 1 20010302 A 3350 20131 BATTERY DOUG DC9 DC983 3022083 WP TAIL CONE DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 931TW 49527 THE TAIL CONE EMERGENCY EXIT LIGHTS WERE INOPERATIVE. REPLACED THE TAIL CONE EMERGENCY EXIT LIGHT BATTERIES. CHECK-C 1 2-28-00 STL. 2 L 7 2 4F RT A6WE 2001033000123 20010330 00123 WP 2001 3 30 MWEA010218 1 20010302 A 5320 99236894 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FORWARD BAG PIT, INTERCOSTAL BETWEEN LONGERON 27 AND 28 RIGHT, STATION 484 - 503 HAD AREAS OF LIGHT CORROSION ON UPPER F LANGE AND UNDER THE NUT PLATES. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001033000124 20010330 00124 WP 2001 3 30 MWEA010219 1 20010302 A 5320 99579111 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FORWARD BAG PIT, INTERCOSTAL AT LONGERON 29 LEFT, STATION 351 - 370 IS EXFOLIATED ON LOWER FLANGE AND HAS OTHER AREAS OF LIGHT CORROSION. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001033000125 20010330 00125 WP 2001 3 30 MWEA010220 1 20010302 A 5311 99115127 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 MODERATE TO HEAVY CORROSION ON LEG AND IN RADIUS OF FRAME AT STATION 130, LONGERON 28 RIGHT TO 30. LOCATED, DRILLED AND INSTALLED FRAME. 2 L 7 2 4F A6WE 2001033000127 20010330 00127 WP 2001 3 30 MWEA010222 1 20010302 A 5321 995792611 FLOOR PANEL DOUG DC9 DC932 3022066 WP CABIN CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 CABIN FLOOR PANEL E5, SKIN IS CRACKED BY FASTENER FOR CHANNEL AT ONE END. REMOVED, FABRICATED AND INSTALLED PANEL SKIN. 2 L 7 2 4F A6WE 2001033000128 20010330 00128 WP 2001 3 30 MWEA010223 1 20010302 A 5321 99577169 FLOOR PANEL DOUG DC9 DC932 3022066 WP CABIN MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 209ME 47730 CABIN FLOOR PANEL F3 HAS SIX MISDRILLED FASTENER HOLES. REMOVED, FABRICATED AND INSTALLED FLOOR PANEL SKIN. 2 L 7 2 4F A6WE 2001033000129 20010330 00129 WP 2001 3 30 MWEA010224 1 20010302 A 5320 99155853 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 THREE AREAS OF GOUGES ON RIGHT SIDE OF CENTER INTERCOSTAL AT STATION 979. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL . 2 L 7 2 4F A6WE 2001033000130 20010330 00130 WP 2001 3 30 MWEA010225 1 20010302 A 5320 59197415 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 CABIN INTERCOSTAL BETWEEN FLOORBEAMS STATION 522 TO 503 HAS TWO CRACKS, LOCATED BELOW RIGHT SUBFLOOR. REMOVED, FABRICAT ED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001033000131 20010330 00131 CE 2001 3 30 GLBA2001048 1 20010227 A 7722 1303800415 INDICATOR BEECH 1900 1900D 1154162 CE COCKPIT INOPERATIVE A GLBA E D ENGINE SHUTDOWN RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 01 219GL 43 43 UE219 RETURN TO BLOCK. RIGHT ENGINE ITT WENT TO 1200. REPAIRED T5 HARNESS AND REMOVED AND REPLACED INDICATOR. 2 L 7 2 4T RT A24CE 2001033000132 20010330 00132 CE 2001 3 30 GLBA2001046 1 20010224 A 3234 1013841377 CONTROL HANDLE BEECH 1900 1900D 1154162 CE COCKPIT FAILED A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 260GL 9980 UE260 LANDING GEAR FAILED TO RETRACT WHEN SELECTED. REPLACED CONTROL HANDLE, PERFORMED TEST FLIGHT AND OPS CHECKED GOOD. 2 L 7 2 4T RT A24CE 2001033000133 20010330 00133 EA 2001 3 30 JBXA000251 1 20010304 A 3150 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT ACTIVATED A JBXA A D UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SO 05 592ML 7410 ON TAKEOFF MASTER CAUTION MESSAGE. INBOARD ANTI-SKID INOP FOLLOWED BY PARKING BRAKE SOV CAUTION MESSAGE. GEAR STAYED D OWN THRU 2000 FT. MAIN GEAR CAME UP SLOW FOLLOWED BY NOSE GEAR TOOK 30-SECONDS TO COME UP. PERFORMED OPS CHECK OF ANTI -SKID SYSTEM IAW AMM 32-44-00, OPS CHECK GOOD. PERFORMED GEAR SWINGS IAW AMM 07-11-01, NO PROBLEMS NOTED WITH GEAR. PE RFORMED OPS CHECK OF PSEU IAW AMM 32-61-00, OPS CHECK GOOD. PERFORMED OPS CHECK OF NR 3 HYD ELEC PUMPS IAW AMM 29-12-03 , OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2001033000134 20010330 00134 SO 2001 3 30 C2XA01IA140 1 20010303 A 3350 LIGHT EMB 145 EMB145ER SO CABIN INTERMITTENT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14943 145040 IAH - DURING C-CHECK INSPECTION, THE EMERGENCY EXIT LIGHT ABOVE SEAT 12CB WAS FOUND TO BE INOPERATIVE. MAINTENANCE REIN SPECTED THE AIRCRAFT AND FOUND THE AFFECTED LIGHT ASSY TO BE FUNCTIONING PROPERLY, AND THE AIRCRAFT WAS APPROVED FOR RET URN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001033000135 20010330 00135 SO 2001 3 30 C2XA01IA141 1 20010215 A 5320 14521725013 SILL EMB 145 EMB145ER SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14943 145040 IAH - DURING C-CHECK INSPECTION, THE SILL PLATE FROM FRAME 18 TO FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL PLATE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001033000136 20010330 00136 SO 2001 3 30 C2XA01IA142 1 20010215 A 5320 14522459001 FLOOR SUPPORT EMB 145 EMB145ER SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14943 145040 IAH - DURING C-CHECK INSPECTION, THE LEFT HAND AND CENTER FLOOR SUPPORTS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CENTER FLOOR SUPPORT, AND PERFORMED A DOUBLER REPAIR ON THE LEFT HAND SUPPORT IN ACCORDANCE WITH EMB14 5 SRM 53-21-10, AND 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001033000137 20010330 00137 2001 3 30 XNA01006 4 20010302 A 3414 O-RING AIRBUS 300 A300B4203 3930306 EU AIRSPEED IND LEAKING A TC8A A UNSCHED LANDING O OTHER CL CLIMB 1 GL 23 372PC 196 AFTER TAKEOFF, F/O''S AIRSPEED BECAME UNRELIABLE. REPLACED BAD O-RING AT QD AT AOC. OP''S CHECK GOOD ON PITOT STATIC T EST IAW A300 MM 34-11. 2 L 7 2 4F RT A35EU 2001033000138 20010330 00138 NE 2001 3 30 DHL2001702003 2 20010302 A 7314 378200 PUMP BOEING 727 72730C 1384009 NM PWA JT8 JT8D7B 52053 NE NR 2 ENGINE FAILED A DHLA C ABORTED TAKEOFF X ENGINE FLAMEOUT TO TAKEOFF 1 SO 01 702DH 19793 NR 2 ENGINE FAILURE ON TAKEOFF ROLL AT 90 KTS. REMOVED AND REPLACED FUEL PUMP. FUEL CONTROL UNIT CHECKS GOOD PER M/M 7 3-11-1 & 72-00. 2 L 7 3 4F 4 F A3WE E2EA 2001033000139 20010330 00139 NM 2001 3 30 DL72S010333 1 20010227 A 2782 BRACKET BOEING 727 727232 1384082 NM SLAT ACTUATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 540DA 22386 NR 7 SLAT ACTUATOR INBD ATTACH BRACKET CRACKED. REPAIRED PER 57-42-000-8. 2 L 7 3 4F A3WE 2001033000140 20010330 00140 NM 2001 3 30 DL72S010334 1 20010227 A 5754 RIB BOEING 727 727232 1384082 NM SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 540DA 22386 FOUND ON F1 LETTER CK, NR 6 SLAT ACTUATOR ATTACH RIBS CRACKED INBD AND OUTBD SIDES OF SLAT ACT ROD END. REPAIRED PER MM 57-54-000-8. 2 L 7 3 4F A3WE 2001033000141 20010330 00141 NM 2001 3 30 DL72L010335 1 20010227 A 3350 S106 BATTERY BOEING 727 727232 1384082 NM ENTRY DOOR DISCHARGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 ON L/O, FOUND 1L OVERHEAD EMERGENCY EXIT SIGN DIM. REPLACED EXIT SIGN BATTERIES, CKS OK. 2 L 7 3 4F A3WE 2001033000142 20010330 00142 NM 2001 3 30 DL76S010337 1 20010227 A 3350 BACR13CE2 RELAY 20131A BOEING 767 767332 1382001 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 126DL 6411 24076 SQUIB TEST N1 RT OVERWING LIGHT WILL NOT TEST. T/S PER FIRM AND M/M REPLACED K 839 AND BATTERY PACK ON RIGHT SIDE OVERW ING SLIDE, OPS NORMALLY OK FOR SERVICE PER MM. 2 L 7 2 4F RT A1NM 2001033000143 20010330 00143 NM 2001 3 30 DL757010339 1 20010228 A 2910 HYDRAULIC LINE 000AE906D05 BOEING 757 757232 1384965 NM RT MLG LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 660DL 24422 AIRCRAFT DIVERTED TO MCO WITH GEAR DOOR LIGHT AND EICAS MSG WITH GEAR RETRACTED OR EXTENDED. FOUND HYD LINE LEAKING RT GEAR TRUCK POSITION LINE AT TOP OF RT GEAR FLEX LINE. PER MM 20-10-09 INSTALLED TEMP HYD LINE LEAK AND OPN CKS NORMAL. FWD TEMP LINE TO MCO. RESTRICTED FOR 350 FLT HRS. 2 L 7 2 4F RT A2NM 2001033000144 20010330 00144 NM 2001 3 30 DL72W010340 1 20010228 A 5754 ATTACH ANGLE BOEING 727 727247 138408F NM SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 295WA 22532 A .5 INCH VISABLE CRACK O/B END NR 2 SLAT IN COVE SKIN ATTACH ANGLE. REPAIR PER M/M 57-54-000-8. 2 L 7 3 4F A3WE 2001033000145 20010330 00145 NM 2001 3 30 DL757010341 1 20010226 A 3260 434093003 MODULE BOEING 757 757232 1384965 NM COCKPIT INTERMITTENT A DALA K NONE N FALSE WARNING AP APPROACH 1 SO 27 6705Y 30397 RT MAIN GEAR GREEN LIGHT BULBS INTERMITTENTLY INOP. PRESS TO TEST OK, BUT HAD TO TAP ON LIGHT REPEATEDLY TO SEE A GOOD GEAR DOWN IND. REPLACED RT GEAR LIGHT TRAY ASSY, OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 2001033000146 20010330 00146 NM 2001 3 30 DLM88010342 1 20010228 A 3350 SOCKET 02011875003 DOUG MD88 MD88 3023688 NM CABIN DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 953DL 49884 ON INSPECTION FOUND EMERGENCY PATH LIGHT AT SEAT 2C INOP. FOUND LAMP SOCKET AND SEAT WIRING DAMAGED. REPLACED LAMP SOCKET AND SEAT ELECTRICAL HARNESS. OPN OF LIGHT NORMAL. 2 L 7 2 4F RT A6WE 2001033000147 20010330 00147 NM 2001 3 30 DL73K010343 1 20010301 A 5342 FITTING BOEING 737 737232 1384475 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 315DL 23087 CORROSION WAS FOUND ON THE LT AND RT FUSELAGE CLEVIS ATTACH LUGS FOR THE HORIZONTAL STABILIZER. THE CORROSION WAS FOUND ON SEVERAL LUG BORES AND FACES. THE CORROSION WAS REMOVED AND NEW BUSHINGS WERE INSTALLED. THE DAMAGE WAS FOUND AT HM V. 2 L 7 2 4F RT A16WE 2001033000148 20010330 00148 NM 2001 3 30 DLM88010345 1 20010228 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 944DL 49817 THE FUSELAGE SKIN WAS FOUND WITH AN AREA OF CORROSION, ADJACENT TO AN EXISTING ANTENNA CUTOUT AT FS 610 BETWEEN STRIN GERS 29R AND 30. THE CORROSION WAS REMOVED WITH A 5.2X 4.6 CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINU M DOUBLER PER ER/A 380167-14, REV B. 2 L 7 2 4F RT A6WE 2001033000149 20010330 00149 NM 2001 3 30 DL73K010346 1 20010301 A 5342 FITTING BOEING 737 737232 1384475 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 315DL 23087 CORROSION WAS FOUND ON THE VERTICAL STABILIZER ATTACH LUGS AND FUSELAGE CLEVIS LUGS. CORROSION WAS FOUND ON VARIOUS L UG BORES AND FACES. THE CORROSION WAS REMOVED AND THE BUSHINGS AND SLEEVES REMANUFACTURED PER ERA 397239-14 AT HMV. 2 L 7 2 4F RT A16WE 2001033000150 20010330 00150 NM 2001 3 30 DL73K010347 1 20010301 A 5711 SPAR BOEING 737 737232 1384475 NM WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 315DL 23087 WHILE ACCOMPLISHING INSPECTIONS PER S/B 737-57-1216 SEVERAL CRACKS WERE FOUND IN 9 FASTENER HOLES COMMON TO THE LT MLG BEAM AFT FITTING AND THE REAR SPAR. THE AFT FITTING WAS REPLACED AND THE FASTENER HOLES WERE OVERSIZED PER ERA 397280-1 4 AT HMV. 2 L 7 2 4F RT A16WE 2001033000151 20010330 00151 NM 2001 3 30 DL73K010348 1 20010301 A 5311 654654049 FRAME BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 315DL 23087 A 2.5 INCH CRACK WAS FOUND IN THE FS 639 FRAME AT STR 16L IN THE INBOARD CHORD AND WEB. A NEW SECTION OF WEB WAS SPLICE D IN AND TWO REPAIR ANGLES WERE ADDED TO THE INBOARD CHORD PER ERA 397256-14 AT HMV. 2 L 7 2 4F RT A16WE 2001033000152 20010330 00152 NM 2001 3 30 DL72W010349 1 20010301 A 5210 SKIN 507945103 BOEING 727 727247 138408F NM ENTRY DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W BN1148 21057 DURING MAINTENANCE VISIT, THE FWD ENTRY DOOR WAS FOUND CRACKED AROUND THE UPPER LATCH CUTOUT. REPAIR PER ER/A 401383-14 . 2 L 7 3 4F A3WE 2001033000153 20010330 00153 NM 2001 3 30 DLM11010350 1 20010228 A 7120 AVB7554503 MOUNT DOUG MD11 MD11 3023602 NM NR 2 PYLON DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 801DE 48472 AFT ENGINE MOUNT DAMAGED FROM WEAR RESULTING FROM CONTACT WITH BLIND RIVET TAILS ON BOTH THE LT AND RT SIDES. ER/A 3967 04-14. 2 L 7 3 4F RT A22WE 2001033000154 20010330 00154 NM 2001 3 30 DL76S010351 1 20010226 A 5720 111T20055 WEB BOEING 767 767332 1382001 NM CENTER WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 125DL 24075 DAMAGE FOUND IN WEB OF THE LBL VERTICAL STIFFENER ON THE CENTER SECTION FRONT SPAR AT THE OVERWING FLOORBEAM TO VERTICAL STIFFENER JOINT. CRACKED PORTION OF WEB WILL BE REMOVED AND REPAIRED BY SPLICING IN NEW SECTION OF STIFFENER. ER/A 39 7281-14. 2 L 7 2 4F RT A1NM 2001033000155 20010330 00155 NM 2001 3 30 DL733010352 1 20010301 A 2450 B451 CIRCUIT BREAKER BOEING 737 737347 1384647 NM COCKPIT MALFUNCTIONED A DALA K NONE H ELECT. POWER LOSS-50 PC DE DESCENT 1 SO 27 304WA 23345 AT TOP OF DESCENT ALL COCKPIT INSTRUMENTS AND INDICATORS EXPERIENCED A MOMENTARY LOSS OF POWER - ON ENGINE GENERATORS, V ISUAL CONDITIONS. POWER WAS RESTORED IMMEDIATELY WITH NO CREW ACTION. REMAINDER OF FLIGHT NORMAL. REPLACED NR 2 GENER ATOR BREAKER. 2 L 7 2 4F RT A16WE 2001033000156 20010330 00156 NM 2001 3 30 DL72W010354 1 20010228 A 5320 651751737 GUSSET BOEING 727 727247 138408F NM RT TORQUE BOX CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 295WA 22532 INSPECTION OF THE RT TORQUE BOX OF THE VENTRAL STAIRWAY REVEALED A 2 INCH CRACK IN A GUSSET AT FS 1263. THE CRACK IS TY PICAL OF BAC S/B 727-53-0129. THE CRACKED GUSSET WAS REPLACED PER THE REQUIREMENTS OF THE S/B AND PER ER/A 380187-14AD. 2 L 7 3 4F A3WE 2001033000157 20010330 00157 NM 2001 3 30 DL76S010355 1 20010228 A 5330 141T32316 SKIN BOEING 767 767332 1382001 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 125DL 24075 AN EXISTING TIME LIMITED REPAIR WAS REMOVED AT STA 325 AND S-34R. THE TIME LIMITED REPAIR IS REPLACED AT THIS TIME WITH A PERMANENT REPAIR. ER/A 397247-14. 2 L 7 2 4F RT A1NM 2001033000158 20010330 00158 NM 2001 3 30 DLM11010356 1 20010302 A 5511 ALC81311 SPAR DOUG MD11 MD11 3023602 NM HORIZ STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 801DE 48472 PITTING CORROSION WAS DISCOVERED IN THE LT AND RT SIDES OF THE HORIZ STAB REAR SPAR UPPER CAPS. THE CORROSION WAS CONTA INED IN THE BARREL NUT HOLES NEAR THE ROOT OF THE STAB. DAMAGE WAS REWORKED PER ERA 397231-14. 2 L 7 3 4F RT A22WE 2001033000159 20010330 00159 NM 2001 3 30 DL76L010357 1 20010302 A 2800 HG1057LR02 COMPUTER BOEING 767 767332 1382001 NM E/E BAY MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 178DN 90010138 25143 A 1200 LB FUEL IMBALANCE RT SIDE LOW WHILE BURNING OUT OF CTR TANK. CORRECTED, 10 MIN LATER SAME IMBALANCE. FMC INITIA LLY 1000 MORE THAN TOTALIZER. TOTALIZER INDICATED 700 LBS OVERBURN FROM FLT PLAN, BY 35 MIN LATER TOTAL WAS 4000 LB LES S THAN FMC. FUEL NOW 2500 LB OVERBURN FROM FLT PLAN. REBAL FUEL 600 LB SPLIT TILL LANDING. THEN 2000 LB SPLIT AT GATE . COCKPIT NOW READS 3500 LB HIGHER ON RT SIDE. REPLACED FQIS COMP AND COCKPIT IND SUMPED ALL TANKS. ALL OPS CHECK NOR MAL. 2 L 7 2 4F RT A1NM 2001033000160 20010330 00160 NM 2001 3 30 DL757010358 1 20010302 A 3610 S312N5096 CLAMP BOEING 757 757232 1384965 NM PNEUMATIC SYS FAILED A DALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 SO 27 657DL 24419 SHORTLY AFTER TURNING ON WING A/I DUCT LEAK ILLUMINATED ALONG WITH RT ENG ANTI ICE. A/C DIVERTED INTO PHX. FOUND CLAMP DPN 366201022 HAD FAILED IN THE RT ENG/PYLON FWD SECTION, 16 SMALL RIVITS HAD FAILED ON THE CLAMP ALLOWING THE DUCT TO S EPARATE. 2 L 7 2 4F RT A2NM 2001033000161 20010330 00161 NM 2001 3 30 DLM11010359 1 20010302 A 2530 OVEN 831610405 DOUG MD11 MD11 3023602 NM GALLEY OVERHEATED A DALA K NONE M OVER TEMP CR CRUISE 1 SO 27 804DE 48475 BULKHEAD NEXT TO G-7 GALLEY IS CHARRED, OTHER AREAS SHOW BURN DAMAGE. VISUAL INSPECTED AFT GALLEY AREA FOUND OVEN 327 A ND 328 DUAL OVEN SHOWED BURN. OTHER AREA NO ABNORMALITY OBSERVED. SUSPECT OVEN PROBLEM. OVEN 327 AND 328 REPLACED. 2 L 7 3 4F RT A22WE 2001033000162 20010330 00162 NM 2001 3 30 DLM88010360 1 20010303 A 2170 COALESCER BAG DOUG MD88 MD88 3023688 NM AC BAY CONTAMINATED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 949DL 49880 IMMEDIATELY AFTER T/O, F/A CALLED TO REPORT FUMES IN CABIN, NO VISUAL INDICATIONS. RETURNED TO AIRPORT AFTER DECLARING EMERGENCY. FOUND OIL IN APU INLET. PERFORMED DUCT BURNOUT. 2 L 7 2 4F RT A6WE 2001033000163 20010330 00163 NM 2001 3 30 DL73K010361 1 20010303 A 2611 72130001008 SMOKE DETECTOR BOEING 737 737247 138448D NM LAVATORY MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 374DL 23521 LAV SMOKE LIGHT ILLUMINATED ON CLIMBOUT OF FLL. LAV SMOKE ALARM, POM PROCEDURE COMPLETED. DIVERTED TO MCO. LAV SMOKE LIGHT WENT OUT AFTER 13 MIN. CHECKED BOTH LAV TEMP PLATE INDICATORS. NO OVERHEAT INDICATED BOTH LAV EXT BOTTLES SEALED . FOUND 2 WIRES ON FWD LAV DET TEST SWITCH OFF AND 2 LOOSE. REINSTALLED WIRES REPLACED BOTH LAV SMOKE DETECTORS AS A P RECAUTION BOTH TEST OK. 2 L 7 2 4F A16WE 2001033000164 20010330 00164 NE 2001 3 30 DL757010362 2 20010304 A 7230 PW2037RTC ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE FAILED A DALA O OTHER Y ENGINE STOPPAGE CR CRUISE 1 SO 27 678DL 35331 716552 25983 716552 AT CRUISE FLT LVL 390 NUMBER 2 ENGINE COMPRESSOR STALLED AND SHUT DOWN. REPLACED NUMBER 2 ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001033000165 20010330 00165 NM 2001 3 30 DL73K010364 1 20010305 A 5551 FITTING BOEING 737 737232 1384475 NM HORIZ STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 315DL 23087 THE LT AND RT HORIZONTAL STABILIZER FITTING ATTACH LUGS WERE FOUND CORRODED. CORROSION WAS REMOVED FROM SEVERAL LUG BOR E AND FACES. NEW BUSHINGS WERE INSTALLED. REPAIR WAS ACCOMPLISHED PER ERA 397265-14 AT HMV. 2 L 7 2 4F RT A16WE 2001033000166 20010330 00166 NM 2001 3 30 01FDEA00175 1 20010305 A 2612 FIRE WARNING DOUG MD11 MD11 3023602 NM NR 3 ENGINE ACTIVATED A FDEA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. R J PARTIAL RPM/PWR LOSS WARNING INDICATION LD LANDING 1 SO 25 584FE 48436 ON LANDING, AC WAS NOT DECELERATING WITH AUTO BRAKES, USED MAX REV THRUST ON ALL 3 ENG. NR 3 COMPRESSOR STALL AND A FIR E ALERT ENSUED. STOP SHUT DOWN NR 3 ENG AND RAN FIRE CK, ONE BOTTLE FIRED. 2 L 7 3 4F RT A22WE 2001033000167 20010330 00167 EU 2001 3 30 AALA20010295 2 20010219 A 7200 22058205 ENGINE FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAYMK65015 EU NR 2 ENGINE MALFUNCTIONED A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 1425A 11408 DFW - FLT 592 - EN ROUTE DFW-OKC, SHORTLY AFTER TAKEOFF, DETECTED GRINDING NOISE AT CABIN. RETURNED DFW AND LANDED WITH OUT FURTHER INCIDENT. REPLACED LEFT SIDE TURBINE PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F RT 2001033000168 20010330 00168 EU 2001 3 30 AALA20010299 1 20010216 A 3610 CLAMP FOKKER F28 F28MK0100 4990807 EU TAIL LOOSE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 1405J 11356 ORD - FLT 430 - EN ROUTE ORD-DCA, DETECTED NR 1 BLEED FAULT LIGHT ILLUMINATE. RETURNED ORD AND LANDED WITHOUT FURTHER I NCIDENT. RE-SECURED NR 1 TAIL DUCT CLAMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001033000169 20010330 00169 EU 2001 3 30 AALA20010312 1 20010225 A 2121 6451101 FAN FOKKER F28 F28MK0100 4990807 EU AC BAY DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 1401G 11352 DCA - FLT 559 - EN ROUTE DCA-ORD, AFTER STARTING ENGINES COCKPIT FILLED WITH SMOKE. SHUT DOWN ENGINES, RETURNED DCA GAT E WITHOUT FURTHER INCIDENT. REPLACED RECIRCULATION FAN. PERFORMED PACK BURNOUT. NO SMOKE NOTED. SYSTEM GROUND CHECKE D NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001033000170 20010330 00170 WP 2001 3 30 AALA20010330 1 20010223 A 3610 5875867 CLAMP DOUG DC9 DC982 3022082 WP TAIL BROKEN A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 241AA 49254 RDU - FLT 1389 - EN ROUTE RDU-ORD, DETECTED TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATE. AIR INTERRUPTED, RETURN ED RDU AND LANDED WITHOUT INCIDENT. REPLACED CLAMP AT RIGHT SIDE ACM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001033000171 20010330 00171 WP 2001 3 30 AALA20010331 1 20010224 A 2170 1808492 COALESCER BAG DOUG DC9 DC983 3022083 WP AC BAY DIRTY A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 76200 53290 ORD - FLT 1224 - EN ROUTE SAN-ORD, DURING CLIMB-OUT, DETECTED SMOKE AT COCKPIT. TURNED OFF LEFT SIDE PACK, SMOKE DISSIP ATED. LANDED ORD WITHOUT FURTHER INCIDENT. REPLACED LEFT AND RIGHT SIDE COALESCER BAGS. PER PACK BURNOUT PER MM. NO SMOKE NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001033000172 20010330 00172 WP 2001 3 30 AALA20010296 1 20010221 A 2121 60544578 FAN DOUG DC9 DC983 3022083 WP AC BAY DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 589AA 53252 ICT - FLT 1802 - EN ROUTE LAX-ORD, CREW REPORTS SMOKE IN CABIN. ACCOMPLISHED SMOKE/FIRE CHECKLIST. DIVERTED ICT AND LA NDED WITHOUT FURTHER INCIDENT. REPLACED RECIRCULATION FAN. PERFORMED PACK BURNOUT PER THE MM. NO SMOKE OR ODOR NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001033000173 20010330 00173 WP 2001 3 30 AALA20010279 1 20010217 A 3350 LIGHT DOUG DC9 DC982 3022082 WP COCKPIT DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 484AA 49677 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD COCKPIT EMERGENCY EXIT LIGHT DIM. RELAMPED OVERHEAD COCKPIT EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001033000174 20010330 00174 WP 2001 3 30 AALA20010283 1 20010216 A 3397 WIRE DOUG DC9 DC982 3022082 WP VENTRAL STAIRS BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 21 450AA 49476 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT STAIRWAY INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIR E AT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001033000175 20010330 00175 WP 2001 3 30 AALA20010285 1 20010218 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 210AA 49161 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM G ROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001033000176 20010330 00176 WP 2001 3 30 AALA20010289 1 20010221 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7509 49803 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT AT SEAT ROW 27 DIM. RELAMPED EMERGENCY EXIT LIGHT AT SEAT 27. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001033000177 20010330 00177 WP 2001 3 30 AALA20010291 1 20010220 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 590AA 53253 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 7D INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT CONN ECTOR AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001033000178 20010330 00178 WP 2001 3 30 AALA20010293 1 20010222 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 590AA 53253 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 7D INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT CONN ECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001033000179 20010330 00179 WP 2001 3 30 AALA20010272 1 20010126 A 3350 AB51 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 RDU - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT FORWARD HALF DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001033000180 20010330 00180 WP 2001 3 30 AALA20010270 1 20010201 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 234AA 49181 LGA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT CONNECTOR PIN AT CA BIN SIDE WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001033000181 20010330 00181 NM 2001 3 30 ASAA0110098 1 20010214 A 3350 86210144 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, FOUND EXIT LIGHTS ON SEAT PALLET 5-7 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY AND RECEIVER AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 2001033000182 20010330 00182 NM 2001 3 30 20010329SG001 1 20010214 A 3350 883200312 RECEIVER BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, FOUND EXIT LIGHTS ON SEAT PALLET 5-7 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY AND RECEIVER AND LIGHTS OPERATED NORMALLY. REF ASAA0110098. (M) 2 L 7 2 4F RT A16WE 2001033000183 20010330 00183 NM 2001 3 30 ASAA0110078 1 20010209 A 3350 883200312 RECEIVER BOEING 737 737298C 1384490 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROWS 11 AND 16 WILL NOT TEST. REMOVED AND REPLACED REMOV E BATTERY AND RECEIVER ASSEMBLIES, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 2001033000184 20010330 00184 NM 2001 3 30 20010329SG002 1 20010209 A 3350 86210144 BATTERY BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROWS 11 AND 16 WILL NOT TEST. REMOVED AND REPLACED REMOV E BATTERY AND RECEIVER ASSEMBLIES, LIGHTS OPERATED NORMALLY. REF ASAA0110078. (M) 2 L 7 2 4F RT A16WE 2001033000185 20010330 00185 NM 2001 3 30 ASAA0110066 1 20010208 A 3350 86210144 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS ON SMOKE BARRIER AND ROW 9 FAILED OPERATIONS TEST. REPLACED REMOTE ASSEMBLY BATTERY FOR SMOKE BARRIER AND ROW 9, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 2001033000186 20010330 00186 NM 2001 3 30 ASAA0110049 1 20010207 A 3350 86210144 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT ON SMOKE BARRIER WILL NOT TEST. REPLACED BATTERY, LIGHT OPER ATED NORMAL. (M) 2 L 7 2 4F A16WE 2001033000187 20010330 00187 NM 2001 3 30 ASAA0110048 1 20010206 A 3350 883200312 RECEIVER BOEING 737 7372Q8C 138448S NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT ON SMOKE BARRIER WILL NOT TEST. REPLACED BATTERY AND RECEIVE R, LIGHT OPERATED NORMAL. (M) 2 L 7 2 4F A16WE 2001033000188 20010330 00188 NM 2001 3 30 20010329SG003 1 20010206 A 3350 86210144 BATTERY BOEING 737 7372Q8C 138448S NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT ON SMOKE BARRIER WILL NOT TEST. REPLACED BATTERY AND RECEIVE R, LIGHT OPERATED NORMAL. (M) 2 L 7 2 4F A16WE 2001033000189 20010330 00189 NM 2001 3 30 ASAA0110034 1 20010202 A 3350 8821004 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROW 8 WILL NOT EXTINGUISH. REMOVED AND REPLACED BATTERY PACK, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 2001033000190 20010330 00190 NM 2001 3 30 GAIA01048ST 1 20010228 A 5532 SKIN BOEING 727 7272J0 138407E NM VERTICAL STAB CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 281KH 21105 DURING A LTC INSPECTION AT FLIGHTSTAR JAX, THE RIGHT VERTICAL STAB ROOT AT BS 1342 SKIN CRACKED AT STRINGER 10R. ACCOMP LISHED DOUBLER REPAIR IAW B727 SERVICE BULLETIN 727-55-82 FIG 2 AND FIG 3 MATERIAL 2024 T3 .063 PO NR 9812 DIM''S 10 INC H BY 5.5 INCH. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2001033000191 20010330 00191 NM 2001 3 30 GAIA01049ST 1 20010228 A 5320 WEB BOEING 727 7272J0 138407E NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 281KH 21105 DURING A LTC INSPECTION AT FLIGHTSTAR JAX, IT WAS DISCOVERED THAT THE WEB AT BS 1283R WAS CRACKED AT A LIGHTING HOLE, RI GHT AFT AIRSTAIR. ACCOMPLISHED TYPICAL WEB REPAIR IAW B727 SRM 51-40-0. MATERIALS 2024-T3 .032 PO NR 9812 DIM''S 2 INC H BY 4 INCH. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2001033000192 20010330 00192 NM 2001 3 30 GAIA01050ST 1 20010228 A 5320 69455963 GUSSET BOEING 727 7272J0 138407E NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 281KH 21105 DURING AT LTC INSPECTION AT FLIGHTSTAR JAX, IT WAS DISCOVERED THAT THE GUSSET AT BS 825.95 LEFT FRAME WAS CRACKED AT WL 198. ACCOMPLISHED BS 825.95 LEFT GUSSETT REMOVAL AND REPLACEMENT IAW B727 SERVICE BULLETIN 727-53-0197. PART 2 FIG 2, P/N 69-45596-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2001033000193 20010330 00193 NM 2001 3 30 GAIA01051ST 1 20010228 A 5320 69455964 GUSSET BOEING 727 7272J0 138407E NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 281KH 21105 DURING A TLC INSPECTION AT FLIGHT STAR JAX, IT WAS DISCOVERED HAT THE GUSSET AT BS 825.95 RIGHT FRAME WAS CRACKED AT WL 198. ACCOMPLISHED BS 825.95 GUSSET REMOVAL AND REPLACEMENT IAW B727 SERVICE BULLETIN 727-53-0197 PART 2 FIG P/N 69-4559 6-4. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2001033000194 20010330 00194 NM 2001 3 30 GAIA01052ST 1 20010228 A 5320 69191222 FITTING BOEING 727 7272J0 138407E NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 281KH 21105 DURING A LTC INSPECTION AT FLIGHTSTAR JAX, IT WAS DISCOVERED THAT THE NOSE LANDING GEAR DOWNLOCK ACTUATOR MOUNT FITTING CRACKED BS 351. ACCOMPLISHED REMOVAL AND REPLACEMENT OF NOSE LANDING GEAR DOWN LOCK ACTUATOR FITTING P/N 69-191122-2 IA W B727 SRM 51-30-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2001033000195 20010330 00195 NM 2001 3 30 GAIA01053ST 1 20010228 A 5330 SKIN BOEING 727 7272J0 138407E NM FUSELAGE DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 281KH 21105 DURING A LTC INSPECTION AT FLIGHTSTAR JAX, MECHANICAL/TOOLING MARKS ON FUSELAGE SKIN BS 440-460 ABOVE STRINGER 7L. ACCO MPLISHED FUSELAGE SKIN REPAIR BS 440-460 ABOVE STRINGER 7L IAW B727 SRM 53-30-3 FIG 1. MATERIAL DOUBLER 2024-T3 .050 PO NR 991378. DIM''S 20.500 BY 7.5 INCH CLASS B REPAIR. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2001033000196 20010330 00196 NM 2001 3 30 GAIA01054ST 1 20010228 A 5330 SKIN BOEING 727 7272J0 138407E NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 281KH 21105 DURING A LTC INSPECTION AT FLIGHTSTAR JAX, DENT IN FUSELAGE SKIN AT BS 675 1 INCH ABOVE STRINGER 26R. ACCOMPLISHED FUSE LAGE SKIN REPAIR BS 675 1 INCH ABOVE STRINGER 26R IAW B727 SRM 53-30-3 FIG 1. MATERIAL DOUBLER 2024-T3 .063 PO NR 99142 0. DIM''S 13.750 INCH BY 7.5 INCH. CLASS B REPAIR. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2001033000197 20010330 00197 NM 2001 3 30 GAIA01055ST 1 20010201 A 5330 SKIN BOEING 727 7272J0 138407E NM FUSELAGE GOUGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 281KH 21105 DURING TLC INSPECTION AT FLIGHTSTAR, GOUGE IN FUSELAGE SKIN AT BS 1150-1160 BETWEEN STRINGER 22L AND 23L. ACCOMPLISHED FUSELAGE SKIN REPAIR BS 1150-1160 BETWEEN STRINGER 22L AND 23L IAW B727 SRM 53-30-3 FIG 1. MATERIAL DOUBLER 2024-T3 .08 0 PO NR 9818. DIM''S 23.125 INCH BY 8 INCH. CLASS B REPAIR. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2001033000198 20010330 00198 NM 2001 3 30 GAIA01056ST 1 20010228 A 5330 SKIN BOEING 727 7272J0 138407E NM FUSELAGE GOUGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 281KH 21105 DURING A LTC INSPECTION AT FLIGHTSTAR JAX, DENT IN FUSELAGE SKIN AT BS 1090 BETWEEN STRINGER 17L AND 18L. ACCOMPLISHED FUSELAGE SKIN REPAIR BS 1090 BETWEEN STRINGER 17L AND 18L IAW B727 SRM 53-30-3 FIG 1. MATERIAL DOUBLER 2024-T3 .063 PO NR 991578. DIM''S 16 INCH BY 17 INCH, CLASS B REPAIR. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2001033000199 20010330 00199 NM 2001 3 30 GAIA01057ST 1 20010228 A 5330 SKIN BOEING 727 7272J0 138407E NM FUSELAGE BULGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 281KH 21105 DURING A LTC INSPECTION AT FLIGHTSTAR JAX, BULGING SKIN ALONG STRINGER 4L SKIN LAP BS 1130-1166. ACCOMPLISHED FUSELAGE SKIN LAP REPAIR BS 1130-1166 AT STRINGER 4L IAW B727 SRM 53-30-3 FIG 5. MATERIAL DOUBLER 2024-T3 .071 PO NR 20029. DIM ''S 30 INCH 32.75 INCH BY 8.25 INCH. CLASS B REPAIR. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2001033000200 20010330 00200 NM 2001 3 30 GAIA01058ST 1 20010222 A 5347 SEAT TRACK BOEING 727 7272J0 138407E NM CABIN CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 281KH 21105 DURING A LTC INSPECTION OF FLIGHTSTAR JAX, CABIN SEAT TRACK AT LBL 45.50 FROM BS 690-480 EXFOLIATED ON ATTACH FLANGE AT BS 577. ACCOMPLISHED SEAT TRACK REMOVAL AND REPLACEMENT BS 550-630 LBL 45.50 IAW B727 SRM 53-10-5 FIG 1 AND VAI DWG NR 2902. MATERIALS TRACK BAC 1520-792 PO NR 214244. DIM''S 8 FT ANGLE BAC 1503-1100122 PO NR 220287. DIM''S 5 FT STRAP 2 EA 7075-T6 .250 PO NR 220287. DIM''S 7 INCH BY 2 INCH. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2001033000201 20010330 00201 NM 2001 3 30 GAIA01059ST 1 20010228 A 5311 FRAME BOEING 727 7272J0 138407E NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 281KH 21105 DURING A LTC INSPECTION AT FLIGHTSTAR JAX, IT WAS DISCOVERED THAT THE AFT CARGO FRAME BS 1070 HAS A DENT BELOW STRINGER 26L. ACCOMPLISHED FUSELAGE FRAME REPAIR BS 1070 AT STRINGER 26L IAW B727 SRM 51-40-3 FIG 1. MATERIALS FILLER 7075-T6 . 100 PO NR 9991-1117. DIM''S 1.187 INCH BY 5.812 INCH. ANGLE 7075-T6 .090 PO NR 999-117. DIM''S .750 INCH BY 2.187 INC H BY 5.812 INCH. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2001033000202 20010330 00202 NM 2001 3 30 GAIA01060ST 1 20010228 A 5330 SKIN BOEING 727 7272J0 138407E NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 281KH 21105 DURING A LTC INSPECTION AT FLIGHTSTAR JAX, FOUND OUTWARD FACING DENT AT BS 720A PLUS 10 INCHES ABOVE STRINGER 18 RT. AC COMPLISHED FUSELAGE SKIN REPAIR BS 720A PLUS 10 INCHES ABOVE STRINGER 18RT IAW B727 SRM 53-30-3 FIG 1. MATERIAL 2024-T3 .063 PO NR 991420. DIM''S 9.500 INCH BY 9.750 INCH. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2001033000203 20010330 00203 NM 2001 3 30 GAIA01061ST 1 20010228 A 5330 SKIN BOEING 727 7272J0 138407E NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 281KH 21105 DURING A LTC INSPECTION AT FLIGHTSTAR JAX, FOUND DENT IN FUSELAGE SKIN AT BS 1153 BETWEEN STRINGER 21-22 RIGHT. ACCOMPL ISHED FUSELAGE SKIN REPAIR BS 1153 BETWEEN STRINGER 21R AND 22R IAW B727 SRM 53-30-3 FIG 1. MATERIALS 2024-T3 .100 PO N R 2006763. DIM''S 10 INCH BY 11.875 INCH. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2001033000205 20010330 00205 NM 2001 3 30 ASAA0110033 1 20010201 A 3350 883200312 RECEIVER BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS SLOW TO ILLUMINATE. REPLACED EMERGENCY EXIT LIGHTS REMOTE A SSEMBLY RECEIVER AND BATTERY, LIGHTS THEN TESTED NORMAL. (M) 2 L 7 2 4F A16WE 2001033000206 20010330 00206 NM 2001 3 30 20010329SG004 1 20010201 A 3350 86210144 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS SLOW TO ILLUMINATE. REPLACED EMERGENCY EXIT LIGHTS REMOTE A SSEMBLY RECEIVER AND BATTERY, LIGHTS THEN TESTED NORMAL. (M) 2 L 7 2 4F A16WE 2001033000207 20010330 00207 NM 2001 3 30 ASAA0110032 1 20010201 A 3350 8821004 BATTERY PACK BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 JNU - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROWS 11 AND 16 INTERMITTENT. REPLACED EMERGENCY EXIT BAT TERY PACKS AT ROWS 11 AND 16, LIGHTS THEN TESTED NORMAL. (M) 2 L 7 2 4F A16WE 2001033000208 20010330 00208 NM 2001 3 30 ASAA0110031 1 20010131 A 3350 6013211 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT OVER L2 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT BATTERY PACK, LI GHTS THEN TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2001033000209 20010330 00209 NM 2001 3 30 ASAA0110030 1 20010130 A 3350 86210144 BATTERY BOEING 737 7372Q8C 138448S NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 SEA - DURING MAINTENANCE CHECK, FOUND SMOKE BARRIER EMERGENCY EXIT LIGHT FAILS TEST. REPLACED SMOKE BARRIER EMERGENCY E XIT BATTERY, LIGHTS THEN TESTED NORMAL. (M) 2 L 7 2 4F A16WE 2001033000210 20010330 00210 NM 2001 3 30 ASAA0110019 1 20010123 A 3350 655663311 LIGHT BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT AT THE R1 DOOR INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEM BLY AND LIGHT FUNCTIONED PROPERLY. (M) 2 L 7 2 4F A16WE 2001033000211 20010330 00211 NM 2001 3 30 ASAA0110018 1 20010122 A 3350 86210144 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING MAINTENANCE CHECK, FOUND SMOKE BARRIER EMERGENCY EXIT LIGHT BATTERY WOULD NOT TEST. REMOVED AND REPLACED R EMOTE ASSEMBLY BATTERY AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2001033000212 20010330 00212 NM 2001 3 30 ASAA0110016 1 20010114 A 3350 883200312 RECEIVER BOEING 737 737210C 1384459 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROW 14 WERE INOPERATIVE. REMOVED AND REPLACED REMOTE ASS EMBLY RECEIVER AND BATTERY. LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2001033000213 20010330 00213 NM 2001 3 30 20010329SG005 1 20010114 A 3350 BATTERY BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROW 14 WERE INOPERATIVE. REMOVED AND REPLACED REMOTE ASS EMBLY RECEIVER AND BATTERY. LIGHTS OPERATED NORMALLY. REF ASAA0110016. (M) 2 L 7 2 4F A16WE 2001033000214 20010330 00214 WP 2001 3 30 ASAA0180065 1 20010213 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS IN PAX CABIN AFT OF OVERWING EXITS INOPERATIVE. REMOVED AND REPLACED ASSOCIATED BATTERY PACK ASSEMBLY. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001033000215 20010330 00215 WP 2001 3 30 ASAA0180063 1 20010208 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP TAILCONE DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 OAK - DURNG C09 C-CHECK, EMERGENCY LIGHT L2-694 ON TAILCONE SLIDE WAS DETERMINED TO BE INOPERATIVE. REMOVED AND REPLACE D ASSOCIATED BATTERY PACK ASSEMBLY. LIGHT THEN TESTED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001033000216 20010330 00216 2001 3 30 ASAA0180062 4 20010209 A 2565 D29982107 HARNESS DOUG DC9 DC983 3022083 WP SLIDE FAILED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 22326 53022 OAK - DURING C09 C-CHECK, R1 DOOR EMERGENCY SLIDE HARNESS FAILED THE AMPERAGE CHECK. REMOVED AND REPLACED SLIDE ASSEMBL Y. AMPERAGE CHECKED OK. (M) 2 L 7 2 4F RT A6WE 2001033000217 20010330 00217 WP 2001 3 30 ASAA0180059 1 20010211 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 973AS 53449 SEA - DURING PREFLIGHT CHECK, FOUND SEVERAL EMERGENCY FLOOR TRACK LIGHTS DISCONNECTED. RECONNECTED MODULES AND REPLACED LAMP ASSEMBLIES AT ROWS 7 AND 10. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001033000218 20010330 00218 WP 2001 3 30 ASAA0180058 1 20010211 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 PDX - DURING PRE-FLIGHT CHECK, EIGHT EMERGENCY FLOOR TRACK LIGHTING MODULES WERE DETERMINED TO BE INOPERATIVE IN THE FIR ST CLASS CABIN. REPLACED DEFECTIVE EMERGENCY FLOOR TRACK LIGHTING MODULES. LIGHT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001033000219 20010330 00219 WP 2001 3 30 ASAA0180057 1 20010211 A 3350 0105611001 LIGHT DOUG DC9 DC983 3022083 WP TAILCONE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 981AS 53472 SEA - DURING LINE CHECK, TWO OF SIX EXIT IDENTIFIER LIGHT ASSEMBLIES IN THE TAILCONE WERE DETERMINED TO BE DAMAGED. REP LACED THE L2-849 AND L2-850 EXIT IDENTIFIER LIGHT ASSEMBLIES. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001033000220 20010330 00220 WP 2001 3 30 ASAA0180055 1 20010208 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP GALLEY DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 977AS 53453 SEA - DURING LINE CHECK, OVERHEAD EMERGENCY LIGHTS AT AFT GALLEY WERE DETERMINED TO BE INOPERATIVE. REMOVED AND REPLACE D ASSOCIATED BATTERY PACK ASSEMBLIES. LIGHTS THEN OPERATED PROPELY. (M) 2 L 7 2 4F RT A6WE 2001033000221 20010330 00221 WP 2001 3 30 ASAA0180054 1 20010207 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 951AS 49111 PDX - DURING LINE CHECK, OVERHEAD EMERGENCY LIGHTS AT OVERWING EXIT LOCATION WERE DETERMINED TO BE INOPERATIVE. REMOVED AND REPLACED ASSOCIATED BATTERY PACK ASSEMBLIES. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001033000222 20010330 00222 WP 2001 3 30 ASAA0180053 1 20010207 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 SEA - DURING LINE CHECK, EMERGENCY FLOOR TRACK LIGHTING MODULE WAS DETERMINED TO BE INOPERATIVE, WIRES WERE BROKEN. REP LACED EMERGENCY FLOOR TRACK LIGHTING MODULE. LIGHT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001033000223 20010330 00223 WP 2001 3 30 ASAA0180052 1 20010206 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 935AS 28786 49236 SEA - DURING LINE CHECK, PORTABLE EMERGENCY LIGHT WAS DETERMINED TO BROKEN. REPLACED LIGHT ASSEMBLY. LIGHT THEN OPERAT ED PROPERLY. (M) 2 L 7 2 4F A6WE 2001033000224 20010330 00224 WP 2001 3 30 ASAA0180050 1 20010206 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP TAILCONE INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SEA - DURING LINE CHECK, EMERGENCY FLOOR TRACK LIGHTING MODULE WAS DETERMINED TO BE BROKEN IN TAILCONE AREA. REPLACED B ROKEN EMERGENCY FLOOR TRACK LIGHTING MODULE. LIGHT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001033000225 20010330 00225 WP 2001 3 30 ASAA0180049 1 20010206 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP CABIN MISSING A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 960AS 53074 SEA - DURING LINE CHECK, EMERGENCY FLOOR TRACK LIGHTING MODULE WAS DETERMINED TO BE MISSING. REPLACED MISSING EMERGENCY FLOOR TRACK LIGHTING MODULE. LIGHT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001033000226 20010330 00226 WP 2001 3 30 ASAA0180048 1 20010206 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 934AS 22812 49235 PDX - DURING LINE CHECK, PORTABLE EMERGENCY LIGHT WAS DETERMINED TO INOPERATIVE. REPLACED LIGHT ASSEMBLY. LIGHT THEN O PERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001033000227 20010330 00227 WP 2001 3 30 ASAA0180047 1 20010206 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 934AS 49235 PDX - DURING SERVICE CHECK, OVERHEAD EMERGENCY LIGHTS AT AFT CABIN DOOR WERE DETERMINED TO BE INOPERATIVE. REMOVED AND REPLACED ASSOCIATED BATTERY PACK ASSEMBLIES. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001033000228 20010330 00228 WP 2001 3 30 ASAA0180046 1 20010206 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 934AS 49235 PDX - DURING SERVICE CHECK, OVERHEAD EMERGENCY LIGHTS AT ROWS 14-17 WERE DETERMINED TO BE INOPERATIVE. REMOVED AND REPL ACED ASSOCIATED BATTERY PACK ASSEMBLIES. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001033000229 20010330 00229 WP 2001 3 30 ASAA0180045 1 20010205 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 979AS 39206 53471 SEA - DURING LINE CHECK, PORTABLE EMERGENCY LIGHT WAS DETERMINED TO INOPERATIVE. REPLACED LIGHT ASSEMBLY. LIGHT THEN O PERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001033000230 20010330 00230 WP 2001 3 30 ASAA0180044 1 20010203 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 SEA - DURING PREFLIGHT CHECK, EMERGENCY FLOOR TRACK LIGHTING MODULE WAS DETERMINED TO BE UNPLUGGED AND INOPERATIVE. REC ONNECTED EMERGENCY FLOOR TRACK LIGHING MODULE. LIGHT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001033000231 20010330 00231 WP 2001 3 30 ASAA01800034 1 20010127 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 32. REMOVED AND REPLACED FLOOR TR ACK MODULE. OPERATIONAL CHECKS NORMAL. (M) 2 L 7 2 4F RT A6WE 2001033000232 20010330 00232 WP 2001 3 30 ASAA0180033 1 20010127 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 948AS 53021 SEA - DURING SERVICE CHECK, OVERHEAD EMERGENCY LIGHTS AT ROWS 21-31 WERE DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIA TED BATTERY PACKS. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001033000233 20010330 00233 WP 2001 3 30 ASAA018000032 1 20010127 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 934AS 49235 PDX - DURING SERVICE CHECK, FIVE OVERHEAD EMERGENCY LIGHTS AT ROWS 14-17 WERE DETERMINED TO BE INOPERATIVE. REPLACED AS SOCIATED BATTERY PACKS. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001033000234 20010330 00234 WP 2001 3 30 ASAA0180031 1 20010127 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP COCKPIT DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 977AS 53453 SEA - DURING PREFLIGHT, COCKPIT EMERGENCY EXIT LIGHTS FOUND INOPERATIVE. REPLACED BATTERY PACK. EXIT LIGHTS OPERATED P ROPERLY. (M) 2 L 7 2 4F RT A6WE 2001033000235 20010330 00235 2001 3 30 ASAA0180029 4 20010123 A 2565 D29985107 BATTERY DOUG DC9 DC983 3022083 WP EVAC SLIDE DISCHARGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 981AS 37520 53472 PHX - DURING K-CHECK, AFT SERVICE DOOR EMERGENCY SLIDE LIGHTING HARNESS BATTERY WAS DETERMINED TO HAVE LOW VOLTAGE. REP LACED COMPLETE SLIDE ASSEMBLY. VOLTS/AMPS CHECKED OK. (M) 2 L 7 2 4F RT A6WE 2001033000236 20010330 00236 WP 2001 3 30 ASAA0180026 1 20010123 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 934AS 49235 PDX - DURING SERVICE CHECK, FIVE OVERHEAD EMERGENCY LIGHTS AT ROWS 14-17 WERE DETERMINED TO BE INOPERATIVE. REPLACED AS SOCIATED BATTERY PACKS. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001033000237 20010330 00237 WP 2001 3 30 ASAA0180025 1 20010123 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 948AS 53021 SEA - DURING PREFLIGHT CHECK, FIRST FOUR EMERGENCY TRACK LIGHTS IN 1ST CLASS WERE DETERMINED TO BE INOPERATIVE. RECONNE CTED TRACK LIGHT WIRING. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001033000238 20010330 00238 WP 2001 3 30 ASAA0180017 1 20010120 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 982AS 53473 SJC - DURING PREFLIGHT CHECK, OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 19 AND 22 REMAINED ILLUMINATED WITH ALL POWER AND S WITCHES OFF. REPLACED ASSOCIATED BATTERY PACKS. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001033000239 20010330 00239 WP 2001 3 30 ASAA0180016 1 20010122 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 32313 53451 SEA - DURING LINE CHECK, PORTABLE EMERGENCY LIGHT WAS DETERMINED TO BE INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT. LIGHT OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001040200001 20010402 00001 WP 2001 4 2 UPS01835133 1 20010126 A 5320 3610130501N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, FWD ACC COMPT AT FS 56 - 70 RT CUSP AT LONG 21R IS CORRODED AND CRACKED. *S/D* REMOVED AND REPLA CED FITTING P/N 3610130501N IAW DC8 SRM 51-1-21 & 51-3-0. 2 L 7 4 4F RT 4A25 2001040200002 20010402 00002 WP 2001 4 2 UPS01835137 1 20010127 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, AFT PIT FS 1240 FRAME CORRODED BETWEEN L36 AND L34R. *S/D* MAT ID FOR REPAIR ANGLES .080 7075-0 IAW REO G07850 CORROSION ON FRAME FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. LOCATED AND DRILLED REPAIR ANGLES IAW D C8 SRM 51-1-24. ALODINED AND PRIMED REPAIR ANGLES IAW DC8 SRM 51-1-8. INSTALLED REPAIR ANGLES INTERCOSTALS AND FITTING /CLIPS IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001040200003 20010402 00003 WP 2001 4 2 UPS01835142 1 20010302 A 2420 51508000 PANEL DOUG DC8 DC871F 302199D WP CABIN FAILED A IPXA D RETURN TO BLOCK B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 798UP 45898 INSPECTION TYPE:N/A, RTR-NR 4 GEN PWR FAIL ILLUM, LWR CGO FIRE LIGHT ILLUM ALL PANEL LIGHTS WENT OUT, SMOKE OF UNKNOWN O RIGIN FILLED COCKPIT AND CABIN. SHUTDOWN 1, 2 AND 4 ENGINES. *S/D* T/S AND FOUND NR 4 VRG FAILED PREVENTING NR 1 BTR CLOSURE. REMOVED AND REPLACED NR 4 VRG PANEL. RAN ALL ENGINES. AC GEN SYST PREF CK AND OP CK NORMAL MM 24-20- 00. P/ N ON/OFF 51508-000, S/N ON: 937ABC, OFF: 265ABC. 2 L 7 4 4F RT 4A25 2001042700093 20010427 00093 WP 2001 4 27 RRXA010020 1 20010315 A 2612 FIRE LOOP DOUG DC8 DC873F 302199F WP NR4 ENGINE MALFUNCTIONED A RRXA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 796FT 46104 SHORTLY AFTER DEPARTURE FROM IAH, EB127/796FT AIR RETURNED TO IAH DUE TO NR 4 FIRE WARNING. REPLACED O/B LOOP ASSY ON L OWER FAN CASE, ADJUSTED WIRE BUNDLES NEXT TO START VALVE DUCT. RAN ENGINE NO MALFUNCTION FOUND. DID BLEED AIR LEAK CHE CK. NO LEAK NOTED. RAN FIRE WARNING AND LOOP SHORT CHECK, ALL NORMAL. OK FOR SERVICE. 2 L 7 4 4F RT 4A25 2001040200004 20010402 00004 WP 2001 4 2 RRXA010021 1 20010314 A 7722 WIRE DOUG DC8 DC862F 3021972 WP NR 1 ENGINE DAMAGED A RRXA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 WP 15 996CF 46162 NR 1 EGT INDICATOR WENT TO ZERO ON GAUGE. PERFORMED INFLIGHT SHUTDOWN OF NR 1 ENGINE PER QRH PROCEDURES. WINDMILLING O IL PRESSURE 30 PSI AT 0633Z. REPAIRED WIRING AT NR 1 ENGINE DISCONNECT. PERFORMED ENGINE RUN-UP, NR 1 ENGINE EGT INDIC ATES NORMAL IAW 27-20-0. AT THIS TIME ENGINE RUN IAW JRH. 2 L 7 4 4F 4A25 2001040200005 20010402 00005 WP 2001 4 2 RRXA010023 1 20010216 A 2612 899096 FIRE LOOP DOUG DC8 DC873F 302199F WP NR 4 ENGINE INTERMITTENT A RRXA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 WP 15 796FT 46104 INTERMITTENT SHORT AND FIRE INDICATION ON NR 4 ENGINE, SHUTDOWN NR 4 ENG PER QRH 1 BOTTLE DISCHARGED. REMOVED AND REPLA CED ALL 5 FIRE LOOPS. OPS CKS NORMAL IAW 26-10-1. 2 L 7 4 4F RT 4A25 2001040200006 20010402 00006 2001 4 2 RRXA010024 4 20010216 A 2214 SCREW DOUG DC8 DC871F 302199D WP AUTOPILOT UNSECURE A RRXA A UNSCHED LANDING F FLT CONT AFFECTED TO TAKEOFF 1 WP 15 996GE 45996 ON TAKEOFF A/C FELT UNCOORDINATED. APPLIED SOME RT TRIM, ON CLIMBOUT ON AUTOPILOT A/C STILL UNCOORDINATED. TURNED OFF CHANGE DAMPER. A/C ROLLED SHARPLY RIGHT, CHECKED RUDDER TRIM, INDICATED 5 UNITS RIGHT-WITH 2 1/2 UNITS AILERON. A/C ST ILL ROLLED LEFT. FOUND SCREW FOR A/P TRIM INDICATOR SHORTING ACROSS LIGHT PLATE AND CASE. REPOSITIONED AND SECURED SCR EW PROPERLY. YAW DAMP SYSTEM CHECKS GOOD M/M 22-10-37. 2 L 7 4 4F RT 4A25 2001040200007 20010402 00007 NM 2001 4 2 UPS01235286 1 20010315 A 2611 SMOKE DETECTOR BOEING 727 72725C 138400H NM CARGO BAY INOPERATIVE A IPXA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:PFLT REF TO M-211066, LWR CARGO SMOKE DET SYS INOP (MX LIGHT ILLUM). REMOVED AND REPLACED CONFIGURATION MODULE, OPS CK NORMAL. THIS CLEARS M-211066. 2 L 7 3 4F A3WE 2001040200008 20010402 00008 2001 4 2 UPS01835287 4 20010314 A 2565 SLIDE DOUG DC8 DC871F 302199D WP DOOR UNSECURE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:PFLT, DOOR SLIDE NEEDS TO BE RESECURED. REINSTALLED SLIDE. 2 L 7 4 4F RT 4A25 2001040200009 20010402 00009 EU 2001 4 2 QXEA0100263 1 20010305 A 5330 WINDOW POST FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 PDX-TYPE 3 CRACK ON RIGHT HAND NR 2 WINDOW POST. PERFORMED STOP DRILL REPAIR. PERFORMED EDDIE CURRENT NDT. NO FURTHER DEFECTS NOTED. RII COMPLIED WITH. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A20EU 2001040200010 20010402 00010 NE 2001 4 2 RRXA010017 2 20010310 A 7200 CFM562C1 ENGINE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C1 13802 NE NR 1 ENGINE FAILED A RRXA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 WP 15 870TV 817 46086 692132 AFTER 1 HR INFLT NOTICED N2 DROPPED +0 2 PERCENT N1 EGT FUEL FLOW NORMAL QTS CKD OTHER GAUGES OIL QTY AT 6 QTS AND DROPP ING OIL PRESS 40 PSI, RETARDED THE THROTTLE AND PERFORMED A PRECAUTIONARY SHUTDOWN AS PER QRH. WHEN OIL QTY DROP TO 20 PRESS BETWEEN 20-25 ABOUT 10 MIN AFTER SHUTDOWN OIL QTY AND PRESS 0. REPLACED NR 1 ENG IAW EWA M/M CH 12 SEC V 3 P 53 T HRU 87. 2 L 7 4 4F 4 F RT 4A25 E2GL 2001040200011 20010402 00011 WP 2001 4 2 RRXA010018 1 20010311 A 3244 TIRE DOUG DC8 DC873F 302199F WP RT MLG BLOWN A RRXA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 WP 15 831AL 46146 ON LANDING, TOWER REPORTED SMOKE OF RIGHT MLG NR 8 TIRE BLEW, NR 3 TIRE DAMAGED UPON LANDING. NO SECONDARY CAUTION LIGH T OR ANTI SKID LIGHT ILLUMINATED. TRANSFERRED TO DMI LIST AS CONTROL C-9272181-1171 CAT: C MEL 3101 ATA 3245 DUE DATE 2 3MAR01 PLACARD INSTALLED. REMOVED AND REPLACED NR 6 ANTI SKID SYSTEM TRANSDUCER PERFORMED BITE CHECK ON ANTISKID CONTR OL BOX, OPS CHECK GOOD. REF ABOVE ITEM NR 2, PERFORMED BITE CHECK ON ANTI-SKID CONTROL BOX. SYSTEM OPS CHECKS NORMAL I AW DC-8 MM 32-43-0. THIS CLEARS DMI 3C9272181-1171. PLACARD REMOVED. 2 L 7 4 4F RT 4A25 2001040200012 20010402 00012 2001 4 2 RRXA010019 4 20010313 A 3441 7890860011 INU DOUG DC8 DC873F 302199F WP COCKPIT FAILED A RRXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 15 831AL 1375 699 46146 NR 1 INS FAILED WENT ATT MODE. TRANSFERRED TO DMI LIST AS CONTROL D-9272201-1175 CAT: D MEL 3420 ATA 3410 DUE DATE 1 1JUL01 PLACARD INSTALLED. REMOVED AND REPLACED NR 1 INU PERFORMED OPERATIONAL CHECK IAW SUPPLEMENTAL MANUAL CHECK GOOD. THIS CLEARS DMI D9272201- 1175, PLACARD REMOVED. 2 L 7 4 4F RT 4A25 2001040200053 20010402 00053 NM 2001 4 2 AWXA0001486 1 20010312 A 5320 654583340 WEB BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 FLOOR WEB CRACKED FS 180 WL 207 LBL 26. REMOVED CRACKED WEB IAW SRM 51-40-02; FABBED NEW WEB IAW DWG 65-45833; TREATED AND PRIMED IAW SRM 51-20-01; INSTALLED WEB IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001040200054 20010402 00054 NM 2001 4 2 AWXA0001487 1 20010312 A 5320 6546812 FLOOR SUPPORT BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 MAIN CABIN FLOOR SUPPORT AT STA 940-960 BL 10R HAS CORROSION IN 3 PLACES ON TOP OF SUPPORT. REMOVED FLOOR SUPPORT; FABB ED REPLACEMENT; INSTALLED REPLACEMENT - ALL IAW SRM 53-60-51 AND 51-30-01. 2 L 7 2 4F RT A16WE 2001040200055 20010402 00055 NM 2001 4 2 AWXA001488 1 20010312 A 5312 53A1173 BULKHEAD BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 CENTER WEB CRACKED 1.1 INCH FS 178 WL 202 LBL 5.0. STOP DRILLED CRACK AND INSTALLED REPAIR PARTS IAW SRM 53-10-08 FIG 2 09. 2 L 7 2 4F RT A16WE 2001040200056 20010402 00056 NM 2001 4 2 AWXA0001489 1 20010312 A 5312 53A11173 BULKHEAD BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 CENTER WEB CRACKED FS 178 WL 202 RBL 3.0. CUT OUT DAMAGED AREA AND INSTALLED REPAIR IAW SRM 53-10-08 FIG 209. 2 L 7 2 4F RT A16WE 2001040200057 20010402 00057 NM 2001 4 2 AWXA0001490 1 20010312 A 5312 53A1117 BULKHEAD BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 CENTER WEB CRACKED FS 178 WL 187 RBL 0.5. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PARTS IAW SRM 53-10-08 FIG 203. 2 L 7 2 4F RT A16WE 2001040200058 20010402 00058 NM 2001 4 2 AWXA0001485 1 20010312 A 5330 65457758 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 LOWER FUSE SKIN HAS 3 DEEP CREASES FROM AROUND FS 847 - 907 STR 19R AND 20R. CUT OUT DAMAGED AREAS IAW SRM 53-00-01 FIG 202; AFTER REWORK, NDT INSP. HFEC IAW NTM PG 6 51-00-00 FIG 23. NO CRACKS DETECTED. INSTALLED CONICAL WASHERS IAW SRM 53-00-01 FIG 202; FABBED REPAIR DOUBLER; TREATED, PRIMED AND INSTALLED DOUBLER IAW SRM 53-00-01 FIG 202. 2 L 7 2 4F RT A16WE 2001040200059 20010402 00059 NM 2001 4 2 AWXA0001491 1 20010312 A 5320 672038 INTERCOSTAL BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 INTERCOSTAL CRACKED FS 180 WL 195 LBL 24. REMOVED CRACKED INTERCOSTAL IAW SRM 51-40-02; FABBED NEW PART IAW DWG 65-1630 0; TREATED AND PRIMED NEW PART IAW SRM 51-20-01; INSTALLED INTERCOSTAL IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001040200060 20010402 00060 NM 2001 4 2 AWXA0001492 1 20010312 A 5230 42509J00141 WEB BOEING 737 7373Y0 1384671 NM CARGO DOOR GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 AFT CARGO DOOR AT LWR CENTER EDGE INTERIOR WEB GOUGED. CUT OUT DAMAGED AREA IAW SRM 51-70-13; FABBED, TREATED AND PRIME D IAW SRM 51-20-01; INSTALLED DOUBLER AND FILLER IAW SRM 51-20-01, 51-40-02, 51-70-13. 2 L 7 2 4F RT A16WE 2001040200061 20010402 00061 NM 2001 4 2 AWXA0001493 1 20010312 A 5330 6545775 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 FUSELAGE STA 780 STR 22R FOUND CREASE IN SKIN ABOUT 4 INCHES LONG. REMOVED DAMAGE; HFEC INSP; FABBED DOUBLER; INSTALLED CONICAL WASHERS AND DOUBLER IAW SRM 53-00-01 FIG 202; TREATED AND PRIMED IAW 53-00-01. 2 L 7 2 4F RT A16WE 2001040200062 20010402 00062 EU 2001 4 2 QXEA0100260 1 20010311 A 3350 XB864041 LIGHT FOKKER F28 F28MK4000 4990810 EU CABIN DETACHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 SEA-12B CHAIR PROXIMITY LIGHT FELL OFF. REMOVED AND REPLACED SEAT 12B EMERGENCY EXIT ARROW LIGHT, OPERATIONAL CHECK GOO D. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001040200063 20010402 00063 EU 2001 4 2 QXEA0100261 1 20010310 A 3350 6008905 BATTERY FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 499US 7840 11182 PDX-DURING OVERNIGHT CHECK FOUND CEILING AND RIGHT HAND FORWARD AND AFT EVACUATION LIGHTS INOPERATIVE. REMOVED AND REPL ACED BATTERY POWER SUPPLY UNIT RIGHT HAND AFT, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001040200064 20010402 00064 EU 2001 4 2 QXEA0100262 1 20010309 A 5312 BULKHEAD FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX-CRACK IN AFT PRESSURE BULKHEAD TO THE RIGHT OF APU. COMPLIED WITH PROVISIONS FOR FERRY FLIGHT TO MTX FACILITY. 2 L 7 2 4F RT A20EU 2001040200065 20010402 00065 EU 2001 4 2 QXEA0100224 1 20010224 A 3350 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 494US 11167 BOI - EXIT SIGN IN PASSENGER COMPARTMENT HAS NUMEROUS BURNT OUT LAMPS. REMOVED AND REPLACED EXIT SIGN ASSEMBLY. OPERAT IONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001040200079 20010402 00079 NM 2001 4 2 GAIA01066ST 1 20010228 A 5720 651720927 STIFFENER BOEING 727 7272J0 138407E NM LT WING CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 281KH 21105 DURING A LTC INSPECTION AT FLIGHTSTAR JAX, FOUND LEFT WING FRONT SPAR HYDRAULIC LINE SUPPORT ANGLE (VERTICAL STIFFENER) AT FSS 386 IS CORRODED. ACCOMPLISHED VERTICAL STIFFENER REMOVAL AND REPLACEMENT FSS LEFT 386 IAW B727 SRM 51-30-2 AND 5 1-30-5. P/N 65-17209-27. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2001040200096 20010402 00096 WP 2001 4 2 RRXA010022 1 20010313 A 2910 O-RING DOUG DC8 DC862F 3021972 WP SLOT VALVE LEAKING A RRXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 15 996CF 46162 LOST HYDRAULICS DOWN TO THE STAND-PIPE. PERFORMED PROCEDURES PER QRH ABNORMAL CHECKLIST. REPLACED O-RINGS ON SLOT VAL VE PER DC8 MM 29-10-20, LK AND OPS CK GOOD AT THIS TIME. 2 L 7 4 4F 4A25 2001040200115 20010402 00115 NM 2001 4 2 UPS01235107 1 20010228 A 5542 FAIRING BOEING 727 72725C 138400H NM RUDDER DAMAGED A IPXA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 01 951UP 19850 INSPECTION TYPE:N/A BTB-DURING T/O ROLL SOMETHING RESTRICTED THE RUDDER WHEN LT RUDDER PEDAL APPLIED. *S/D* FOUND WEAR STRIP ON TOP/LT CORNER OF LOWER RUDDER AND THE FAIRING JUST FORWARD OF STRIP DAMAGED. REMOVED FAIRING SECTION, RUDDER OPS WAS NORMAL. OK TO CONTINUE WITH FAIRING REMOVED XFR TO CDL LOG C210328. 2 L 7 3 4F A3WE 2001040200116 20010402 00116 NM 2001 4 2 UPS01535276 1 20010313 A 3350 LIGHT BOEING 757 75724APF 1384969 NM CABIN MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 443UP 27388 INSPECTION TYPE:IN PRIOR TO ENG START EMERGENCY EXIT LT REMAINED ILLUMINATED IN ARMED POSITION WITH NORMAL ELECTRICAL PO WER ON A/C. *S/D* REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY, NO HELP. ALL POWER REMOVED FROM A/C AND CONNECTO RS CLEANED AND CHECKED AT EMERGENCY LIGHT POWER SUPPY AND PILOTS CONTROL PANEL CB N35. CYCLED, POWER RESTORED TO AIRCRA FT, SYSTEM TESTED SERVICABLE. 2 L 7 2 4F RT A2NM 2001040200117 20010402 00117 NM 2001 4 2 QXEA01000259 1 20010220 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 PDX-NICK LOCATED INBOARD SEAT TRACK FORWARD OF X197.00. REPAIRED IAW DHC-8 RD8-53-833. 2 H 7 2 4T RT A13NM 2001040200142 20010402 00142 EU 2001 4 2 QXEA0100265 1 20010313 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU COCKPIT INOPERATIVE A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 476US 11224 BOI- EXIT SIGN ABOVE COCKPIT DOOR INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETU REND TO SERVICE. 2 L 7 2 4F RT A20EU 2001040200143 20010402 00143 EU 2001 4 2 QXEA0100266 1 20010312 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 499US 11182 GEG- ROW 8 AFT EXIT SIGN HAS INOPERATIVE BULBS. REMOVED AND REPLACED CIRCUIT BOARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001040200144 20010402 00144 EU 2001 4 2 QXEA0100264 1 20010307 A 3350 A43350 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN LOOSE A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 476US 11224 SEA- EXIT LIGHTING FIXTURE BELOW OVERWING EXIT AT 8E IS LOOSE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD . AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001040200147 20010402 00147 WP 2001 4 2 2001FAT010 1 20010305 A 3213 5935347517 STRUT DOUG DC9 DC983 3022083 WP RT MLG LEAKING W FE5F K NONE O OTHER IN INSP/MAINT 1 WP 03 49807 B-28007 EXPERIENCED RT STRUT LEAKAGE DURING TRANSIT CHECK. AFTER SUBSEQUENT TEAR DOWN, THE PISTON CHROME PLATING FLAKED- OFF WAS FOUND AND FURTHER DISCOVERING GALLING OF THE BASE METER PIN, BEARING LOWER SLEEVE, AND THE STOP.THIS BRAND NEW P ISTON WAS INSTALLED, ON JUL 13, 2000 FOR INCORPORATING SB MD80-32-309. IT DID NOT HAPPEN ANY DEFECT ON THE MLG, EXCEPT R EPLACING WORN SEAL ON FEB.5,2001 FOR STRUT LEAKAGE.THIS PISTON WILL BE SHIPPED TO BOEING, ON 28 MAR 2001, FOR INVESTIGAT ION 2 L 7 2 4F RT A6WE 2001040200148 20010402 00148 WP 2001 4 2 2001FAT007 1 20010228 A 5310 STRUCTURE DOUG DC9 DC982 3022082 WP ACCESSORY BAY CORRODED W FE5F K NONE O OTHER IN INSP/MAINT 1 WP 03 53118 DURING THE 7C CHECK, A VISUAL INSPECTION WAS PERFORMED AT AFT ACCESSORY COMPARTMENT. CORROSION AND WATER ENTRAPMENT WAS DISCOVERED SCATTERED IN THIS AREA.FAT (FAR EASTERN AIR TRANSPORT CORP.) PERFORMED ONE TIME INSPECTION ON THIS AREA FOR C URRENT MD FLEET, 9 MD-80. 3 OTHER A/C ARE DISCOVERED CORROSION SLIGHTLY AND CORRECTED. 2 L 7 2 4F A6WE 2001040200149 20010402 00149 NM 2001 4 2 UPS01235206 1 20010211 A 5310 PRESSURE PANEL BOEING 727 72751C 1384015 NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE:C-CK, NOSE W/W LT SIDEWALL, CRACK INDICATION ALONG VERTICAL ROW OF RIVETS HEADS. CUT OUT DAMAGE AREA AN D INSTALLED DOUBLER. 2 L 7 3 4F A3WE 2001040200150 20010402 00150 WP 2001 4 2 ASAA0180060 1 20010209 A 5610 5613217520 WINDOW DOUG DC9 DC983 3022083 WP COCKPIT BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 948AS 53021 LAX - DURING PREFLIGHT CHECK, FIRST OFFICERS SLIDING CLEARVIEW WINDOW LEAKAGE WAS DETERMINED TO BE BROKEN. REINSTALLED HINGE PIN. WINDOW THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001040200151 20010402 00151 2001 4 2 ASAA0180056 4 20010211 A 2565 3961899501 LANYARD DOUG DC9 DC983 3022083 WP EVAC SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 969AS 53063 ANC - DURING PREFLIGHT CHECK, L2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD BETWEEN GIRT BAR AND SLIDE COVER. (M) 2 L 7 2 4F RT A6WE 2001040200152 20010402 00152 WP 2001 4 2 ASAA01800067 1 20010215 A 5210 5910081167 DOOR DOUG DC9 DC983 3022083 WP ENTRY DOOR OUT OF RIG A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 30058 1945 53075 SEA - DURING PREFLIGHT CHECK, L1 DOOR FORWARD LEFT CREW/PAX DOOR WAS DETERMINED TO BE HARD TO OPEN. RE-RIGGED DOOR. DO OR THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001040200153 20010402 00153 2001 4 2 ASAA0180072 4 20010216 A 2565 3961899501 LANYARD DOUG DC9 DC983 3022083 WP EVAC SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 948AS 53021 LAX - DURING PRE-FLIGHT CHECK, L1 DOOR EMERGNECY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD BETWEEN GIR T BAR AND SLIDE COVER. (M) 2 L 7 2 4F RT A6WE 2001040200154 20010402 00154 WP 2001 4 2 ASAA0180073 1 20010216 A 5347 59366691 CARGO TRACK DOUG DC9 DC983 3022083 WP CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 982AS 53473 PHX - DURING K-CHECK, FOUND AFT CARGO BAY CARGO TRACK AND SPLICES CORRODED AT LBL 15, FS 1221-1322. REMOVED AND REPLACE D CARGO TRACK AND SPLICES, REF SRM 51-30-0. (M) 2 L 7 2 4F RT A6WE 2001040200155 20010402 00155 WP 2001 4 2 ASAA0180071 1 20010216 A 3350 HPD54053858 LIGHT DOUG DC9 DC983 3022083 WP TAILCONE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 981AS 53472 SEA - DURING LINE CHECK, SEVERAL EMERGENCY LIGHT ASSEMBLIES IN THE TAILCONE AREA WERE FOUND TO BE DAMAGED. REMOVED AND REPLACED DAMAGED LIGHT ASSEMBLIES. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001040200156 20010402 00156 WP 2001 4 2 ASAA0180069 1 20010215 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 SEA - DURING LINE CHECK, FOUND BOTH LEFT AND RIGHT EMERGENCY OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND RE PLACED ASSOCIATED BATTERY PACKS. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001040200157 20010402 00157 WP 2001 4 2 ASAA0180068 1 20010215 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 973AS 53449 PDX - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS IN AFT PAX CABIN DISCONNECTED. RECONNECTED LIGHTS. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001040200158 20010402 00158 WP 2001 4 2 ASAA0180040 1 20010131 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 29729 1828 53075 PDX - DURING SERVICE CHECK, OVERWING EMERGENCY SPOTLIGHTS CAME ON WHEN SWITCHING FROM EXTERNAL POWER TO APU POWER. EMER GENCY LIGHTS SWITCH IN COCKPIT WAS IN OFF POSITION. REMOVED AND REPLACED BATTERY PACK ASSEMBLY. LIGHTS THEN OPERATED N ORMALLY. (M) 2 L 7 2 4F RT A6WE 2001040200159 20010402 00159 WP 2001 4 2 ASAA0180039 1 20010131 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 948AS 53021 PDX - DURING SERVICE CHECK, OVERHEAD EMERGENCY LIGHTS AT THE AFT GALLEY AND CENTER AISLE WERE DETERMINED TO BE INOPERATI VE. REMOVED AND REPLACED ASSOCIATED BATTERY PACK ASSEMBLIES. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001040200160 20010402 00160 NM 2001 4 2 ASAA0110095 1 20010213 A 3350 86210144 BATTERY BOEING 737 7372Q8C 138448S NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 SEA - DURING MAINTENANCE CHECK, FOUND AFT EMERGENCY EXIT IDENTIFIER INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY B ATTERY AND SIGN WORKED NORMALLY. (M) 2 L 7 2 4F A16WE 2001040200161 20010402 00161 NM 2001 4 2 ASAA0110096 1 20010214 A 3350 08163009120 LIGHT BOEING 737 737210C 1384459 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING MAINTENANCE CHECK, FOUND TWO EMERGENCY EXIT LIGHTS AT ROW 8, SEAT PALLET 5-10 INOPERATIVE. REPAIRED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2001040200162 20010402 00162 NM 2001 4 2 QXEA01000254 1 20010303 A 3211 FITTING DHAV DHC8 DHC8102 2809003 NM LT MLG CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 PDX-LEFT HAND MAIN LANDING GEAR H MEMBER HAS CORROSION ON MOUNTING PAD FOR RETRACTION ACTUATOR ATTACH FITTING. REPAIRED IAW DHC-8 SRM 32-30-00, PAGE 200-207 AND RD8-54-921. 2 H 7 2 4T RT A13NM 2001040200163 20010402 00163 NM 2001 4 2 QXEA01000255 1 20010222 A 3211 FITTING DHAV DHC8 DHC8102 2809003 NM RT MLG CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 PDX-RIGHT HAND H MEMBER HAS CORROSION AT MOUNTING PAD FOR RETRACTION ACTUATOR ATTACH FITTING. REPAIRED IAW HORIZON AIR EA 9-54-271. 2 H 7 2 4T RT A13NM 2001040200164 20010402 00164 NM 2001 4 2 QXEA01000256 1 20010303 A 5414 SKIN DHAV DHC8 DHC8102 2809003 NM NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 PDX-CRACK PROPAGATING FROM 3RD RIVET HOLE FROM OUTBOARD SIDE OF RIGHT NACELLE AT STATION XN239. REPAIRED IAW HORIZON AI R EA 9-54-276. 2 H 7 2 4T RT A13NM 2001040200165 20010402 00165 NM 2001 4 2 QXEA01000257 1 20010219 A 5751 SKIN DHAV DHC8 DHC8102 2809003 NM AILERON TORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 PDX-LEFT HAND AILERON HAS LOWER SKIN TEAR AT TRAILING EDGE OF INBOARD TRIM TAB ATTACH POINT. REPAIRED IAW DHC-8 RD8-27- 005. 2 H 7 2 4T RT A13NM 2001040200166 20010402 00166 NM 2001 4 2 QXEA01000258 1 20010224 A 5512 SKIN DHAV DHC8 DHC8102 2809003 NM HORIZ STAB TORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 PDX-SHEET METAL TORN AT PANEL 333XB APERTURE. REPAIRED IAW HORIZON AIR EA 9-55-141. 2 H 7 2 4T RT A13NM 2001040200167 20010402 00167 NM 2001 4 2 ASAA0110097 1 20010214 A 3350 08163009120 LIGHT BOEING 737 737210C 1384459 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING MAINTENANCE CHECK, FOUND EXIT LIGHTS IN FORWARD ROW INOPERATIVE. REPAIRED WIRING AND LIGHTS OPERATED NORMA LLY. (M) 2 L 7 2 4F A16WE 2001040200168 20010402 00168 NM 2001 4 2 USAA010228 1 20010221 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 32258 24554 CLT - FOUND FRAME CRACKED .5 INCH, STATION 747 BETWEEN STATION 9R AND 8R. INSTALLED DOUBLER PER T/R 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001040200169 20010402 00169 NM 2001 4 2 USAA010229 1 20010221 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 NM 01 432US 32258 24554 CLT - FOUND FRAME CRACKED .5 INCH, STATION 827 BETWEEN STATION 9R AND 8R. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001040200170 20010402 00170 NM 2001 4 2 GAIA01062ST 1 20010228 A 5330 SKIN BOEING 727 7272J0 138407E NM FUSELAGE CANNING A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 281KH 21105 DURING LTC INSPECTION AT FLIGHTSTAR JAX, FOUND SKIN OIL CANNED AT BS 196R AREA IS MARKED. ACCOMPLISHED FUSELAGE SKIN RE PAIR BS 196 R IAW B727 SRM 53-30-3 FIG 1 MATERIAL 2024-T3 .050 PO NR 991266. DIM''S 10.400 INCH BY 8.5 INCH. THE AIRCR AFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2001040200171 20010402 00171 NM 2001 4 2 GAIA01063ST 1 20010228 A 5330 SKIN BOEING 727 7272J0 138407E NM FUSELAGE GOUGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 281KH 21105 DURING A TLC INSPECTION AT FLIGHTSTAR JAX, FOUND SEVERAL DENT''S AND GOUGES ON FUSELAGE SKIN BS 1050-1055 AT STRINGER 23 -25R. ACCOMPLISHED FUSELAGE SKIN REPAIR BS 1050-1055 BETWEEN STRINGER 23R AND 25R IAW B727 SRM 53-30-3 FIG 3. MATERIAL S FILLER 2024-T3 .063 PO NR 9812. DIM''S .750 INCH BY 1.75O. DOUBLER 2024-T3 .071 PO NR 991508. DIM''S 9.250 INCH BY 10 INCH. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2001040200172 20010402 00172 NM 2001 4 2 GAIA01064ST 1 20010228 A 5720 STIFFENER BOEING 727 7272J0 138407E NM LT WING CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 281KH 21105 DURING A LTC INSPECTION AT FLIGHTSTAR JAX, FOUND LEFT WING L/E WS 390 HAS CORROSION ON FORWARD SPAR STIFFENER. ACCOMPLI SHED VERTICAL STIFFENER REMOVAL AND REPLACEMENT FSS LEFT 390 LEFT 390 IAW B727 SRM 57-10-2 FIG 3 AND 51-30-2. MATERIAL STIFFENER BAC 1517-1473 PO NR 270893. DIM''S 11.5 INCH BY 1 INCH SHIM 2024-T3 .250 PO NR 20093117. DIM''S 7.750 INCH B Y 1 INCH. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2001040200173 20010402 00173 NM 2001 4 2 GAIA01065ST 1 20010228 A 5720 651721027 STIFFENER BOEING 727 7272J0 138407E NM LT WING CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 281KH 21105 DURING A LTC INSPECTION AT FLIGHTSTAR JAX, FOUND LEFT WING FRONT SPAR HYD LINE SUPPORT ANGLE (VERTICAL STIFFENER) AT FSS 396 IS CORRODED. ACCOMPLISHED VERTICAL STIFFENER REMOVAL AND REPLACEMENT FSS LEFT 396 YAW B727 SRM 51-30-2 AND 51-30-5 P/N 65-17210-27. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2001040200174 20010402 00174 NM 2001 4 2 QXEA01000252 1 20010222 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 PDX- LEFT HAND OUTBOARD SEAT TRACK GOUGED AT X270.500. REPAIRED IAW HORIZON AIR EA 9-53-600 AND DHC-8 RD8-53-1342. 2 H 7 2 4T RT A13NM 2001040200175 20010402 00175 NM 2001 4 2 QXEA01000253 1 20010227 A 5347 FASTENER DHAV DHC8 DHC8102 2809003 NM SEAT TRACK MISINSTALLED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 815PH 50 PDX- RIGHT HAND INBOARD CABIN SEAT TRACK HAS 1 HI-LOK ON THE INBOARD FLANGE THAT HAS THE HEAD UNDERFLUSH. REPAIRED IAW HORIZON AIR EA 9-53-605. 2 H 7 2 4T RT A13NM 2001040200176 20010402 00176 NM 2001 4 2 GAIA01067ST 1 20010228 A 5711 SPAR BOEING 727 7272J0 138407E NM LT WING CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 281KH 21105 DURING A LTC INSPECTION AT FLIGHTSTAR JAX, FOUND LEFT WING STATION 431.5 CORROSION ON FRONT SPAR WEB AT LOWER CHORD. AC COMPLISHED LEFT WING FRONT SPAR WEB REPAIR WS 431.5 IAW B727 SRM 57-10-6 FIG 1 MATERIAL 2024-T3 .250 PO NR 20093117. DI M''S 12 INCH BY 14 INCH. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2001040200177 20010402 00177 NM 2001 4 2 GAIA01068ST 1 20010228 A 5730 SKIN BOEING 727 7272J0 138407E NM RT WING CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 281KH 21105 DURNG A LTC INSPECTION OF FLIGHTSTAR JAX, FOUND RIGHT WING L/E HAS A CRACK AT WS 464. ACCOMPLISHED RIGHT WING FIXED L/E SKIN REPAIR WS 464 IAW B727 SRM 57-30-4 FIG 4. MATERIAL FILLER 2024-T3 .040 PO NR 9812. DIM''S 2.330 INCH BY 3 INCH. DOUBLER 2024-T3 .050 PO NR 9815. DIM''S 6.5 INCH BY 7.33 INCH. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2001040200179 20010402 00179 EU 2001 4 2 AWXA0001498 1 20010313 A 3350 321430 BATTERY PACK AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 619AW 527 OVERWING EMERGENCY EXITS FAIL TEST NR 4 ON CARD FIC52301; WHITE INDICATOR LIGHT SLIDE ARMED DOES NOT COME ON. BATTERY P ACKS CHANGED IAW JC RIC33301; RETESTED ON JC FIB52301; NO FAULT FOUND. 2 L 7 2 4F RT A28NM 2001040200180 20010402 00180 NM 2001 4 2 QXEA0100267 1 20010310 A 3310 MS3320712 CIRCUIT BREAKER DHAV DHC8 DHC8202 2809007 NM COCKPIT MALFUNCTIONED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 358PH 506 PDX - FLIGHT CREW NOTICED ACRID SMELL IN FLIGHT COMPARTMENT. REMOVED AND REPLACED APPROACH LIGHT CIRCUIT BREAKER. OPER ATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001040200181 20010402 00181 NM 2001 4 2 AWXA0001494 1 20010313 A 5712 654953555 RIB BOEING 737 737277 1384570 NM LT WING CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 LT WING L/E RIB CRACKED IN RADIUS, I/B OF NR 1 PYLON WBL 183.4. STOP DRILLED CRACK; FORMED, DRILLED AND INSTALLED REPAI R ANGLES IAW SRM 51-40-3 FIG 1. 2 L 7 2 4F RT A16WE 2001040200182 20010402 00182 EU 2001 4 2 AWXA0001495 1 20010313 A 5320 D53112091200 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 620AW 052 FLOOR SUPPORT AT RT FR 16 Y-1292 CORRODED. FLOOR SUPPORT FABBED AND INSTALLED IAW AIRBUS DWG 53112091200. 2 L 7 2 4F RT A28NM 2001040200183 20010402 00183 EU 2001 4 2 AWXA0001496 1 20010313 A 5347 D53112092206 SEAT TRACK AIRBUS 320 A320231 3930325 EU CABIN CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 620AW 052 NR 4 SEAT TRACK FRAME 20 CORRODED FR 220 Y-1292 TO FR 16 Y-1252. FABBED AND INSTALLED NEW SEAT TRACK IAW AIRBUS DWG 531 12092206 AND SRM 51-42-00. 2 L 7 2 4F RT A28NM 2001040200184 20010402 00184 EU 2001 4 2 AWXA0001497 1 20010313 A 5320 B2D53112091 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 620AW 052 FLOOR SUPPORT AT FR 16-20 Y-765 RT CORRODED. FLOOR SUPPORT FABBED IAW A320 DWG 53112091203 AND INSTALLED IAW SRM 51-42- 00. 2 L 7 2 4F RT A28NM 2001040200185 20010402 00185 NM 2001 4 2 UPS01435153 1 20010212 A 5320 65B07942339 WEB BOEING 747 747259B NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 527UP 21730 INSPECTION TYPE:C2,3, HFEC INSP REVEALED TWO CRACKS EXTENDING FROM 3RD INSULATION BLANKET STANDOFF HOLE FROM TOP AT LT S IDE STA 320 ON VERTICAL WEB OF NOSE WHEEL WELL IN CABIN. REMOVED AND REPLACED WEB IAW DWG 65B07942, AND SRM 51-30-02. 2 L 7 4 4F RT A20WE 2001040200186 20010402 00186 NM 2001 4 2 UPS01435162 1 20010211 A 5320 SUPPORT FITTING BOEING 747 747259B NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 527UP 21730 INSPECTION TYPE:C, LEFT LOWER BODY FAIRING SUPPORT IS CORRODED BEYOND LIMITS AT STA 1000 LBL 43. REPAIRED SUPPORT IAW S RM 53-50-04. 2 L 7 4 4F RT A20WE 2001040200187 20010402 00187 NM 2001 4 2 UPS01435163 1 20010211 A 5320 SUPPORT FITTING BOEING 747 747259B NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 527UP 21730 INSPECTION TYPE:C, LEFT LOWER BODY FAIRING SUPPORT AT STA 940 LBL 14 TO LBL 20 IS CORRODED BEYOND LIMITS. REPAIRED SUPP ORT IAW SRM 53-50-04 FIG 1. 2 L 7 4 4F RT A20WE 2001040200189 20010402 00189 NM 2001 4 2 UPS01235176 1 20010217 A 5320 INTERCOSTAL BOEING 727 72722C 138400F NM RT MLG CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+S, RT MLG FWD CUTOUT INTERCOSTAL CRACKED AT MLG DOOR MANUAL RELEASE HANDLE. REPAIR CARRIED OUT IAW SR M 51-40-03. 2 L 7 3 4F A3WE 2001040200190 20010402 00190 NM 2001 4 2 UPS01235177 1 20010216 A 5755 SUPPORT FITTING BOEING 727 72722C 138400F NM SPOILER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, EVIDENCE OF SURFACE CORROSION ON NR 13 SPOILER ACTUATOR SUPPORT CASTING AND LIGHT SURFACE CORROSIO N ON O/B RIB ATTACHED TO SUPPORT CASTING. REPAIR CARRIED OUT IAW MM 27-61-81 & MM 27-61-81. 2 L 7 3 4F A3WE 2001040200191 20010402 00191 NM 2001 4 2 UPS01235178 1 20010215 A 5755 CASTING BOEING 727 72722C 138400F NM SPOILER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, LT WING T/E, NR 1 SPOILER, O/B END SUPPORT CASTING IS CORRODED. REPAIR CARRIED OUT IAW SRM 51-30- 2. 2 L 7 3 4F A3WE 2001040200192 20010402 00192 NM 2001 4 2 UPS01235179 1 20010213 A 5753 CARRIAGE BOEING 727 72722C 138400F NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, NR 5 FLAP CARRIAGE HAS CORROSION IN SPINDLE BORE. REPLACED CARRIAGE IAW MM 27-51-03. 2 L 7 3 4F A3WE 2001040200193 20010402 00193 NM 2001 4 2 UPS01435152 1 20010212 A 5320 65B07942338 WEB BOEING 747 747259B NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 527UP 21730 INSPECTION TYPE:C HFEC INSP REVEALED TWO CRACKS AT 3RD INSULATION BLANKET STANDOFF HOLE FROM TOP AT STA 300 ON VERTICAL WEB OF NOSE WHEEL WELL INSIDE CABIN RT SIDE. REMOVED AND REPLACED WEB IAW DWG 65B07942 AND SRM 51-30-02. 2 L 7 4 4F RT A20WE 2001040200194 20010402 00194 NM 2001 4 2 UPS01435157 1 20010205 A 5280 SKIN BOEING 747 747259B NM RT STRUT DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 527UP 21730 INSPECTION TYPE:C, RT BODY GEAR I/B STRUT DOOR INNER SKIN IS CORRODED BEYOND LIMITS. REPAIRED SKIN IAW SRM 51-40-2 FIG 1. 2 L 7 4 4F RT A20WE 2001040200195 20010402 00195 NM 2001 4 2 UPS01435159 1 20010211 A 5320 SUPPORT FITTING BOEING 747 747259B NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 527UP 21730 INSPECTION TYPE:C, LEFT WING LOWER BODY FAIRING SUPPORT IS CORRODED BEYOND LIMITS AT STA 1170 BETWEEN BL 0 AND LBL 60. REPAIRED SUPPORT IAW SRM 53-50-04. 2 L 7 4 4F RT A20WE 2001040200196 20010402 00196 NM 2001 4 2 UPS01435160 1 20010211 A 5320 SUPPORT FITTING BOEING 747 747259B NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 527UP 21730 INSPECTION TYPE:C, LEFT BODY FAIRING SUPPORT IS CORRODED BEYOND LIMITS AT STA 1112 BETWEEN LBL 25 TO LBL 40. REPAIRED S UPPORT IAW SRM 53-50-04. 2 L 7 4 4F RT A20WE 2001040200197 20010402 00197 NM 2001 4 2 UPS01435161 1 20010211 A 5320 SUPPORT FITTING BOEING 747 747259B NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 527UP 21730 INSPECTION TYPE:C, LEFT BODY FAIRING SUPPORT IS CORRODED BEYOND LIMITS AT STA 1064 LBL 23 TO LBL 50. REPAIRED SUPPORT I AW SRM 53-50-04 FIG 2. 2 L 7 4 4F RT A20WE 2001040200198 20010402 00198 NM 2001 4 2 UPS01435164 1 20010211 A 5320 65B018341 CLIP BOEING 747 747259B NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 527UP 21730 INSPECTION TYPE:C, LEFT LOWER BODY FAIRING SUPPORT HANGER CLIPS ARE CORRODED BEYOND LIMITS AT STA 860 LBL 31 FWD AND AFT CLIP. REMOVED, FABRICATED, AND REPLACED CLIPS IAW DWG 65B01834, AND SRM 51-30-02. 2 L 7 4 4F RT A20WE 2001040200199 20010402 00199 WP 2001 4 2 UPS01835165 1 20010206 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, RIGHT O/B FIXED L/E HAS CRACK ON L/E OF MATING SURFACE AT FASTENER ATTACH HOLES. FABBED NEW -8 AN GLE AND -11 DOUBLER IAW DAC DWG 9753297, LOCATED AND DRILLED NEW -4 RIB IAW DC-8 SRM 51-1-24. INSTALLED -8 ANGLE, -11 D OUBLER & -4 RIB IAW DC8 SRM 51-1-20D, 51-3-0, 51-1-21, 51-1-21A, 51-1-2 0B, 51-1-20A. INSTALLED FIXED L/E SECTION IAW D C-8 SRM 51-1-3. 2 L 7 4 4F RT 4A25 2001040200200 20010402 00200 WP 2001 4 2 UPS01835167 1 20010201 A 5310 SHEAR TIE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, SHEAR TIE AT FS 1746, BETWEEN L28R AND L26R CORRODED. REMOVED SHEAR TIE, FABBED NEW SHEAR TIE PER DAC DWG 5612148. ALODINED, PRIMED PER DC8 SRM 51-1-8. INSTALLED PER DC8 SRM 51-1-21D. 2 L 7 4 4F RT 4A25 2001040200201 20010402 00201 WP 2001 4 2 UPS01835168 1 20010202 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, FITTING CRACKED STA 1690 LONG 30R. REPLACED FITTING IAW DC8 SRM 51-1-20D. RETORQUED BOLT DC8 SRM 51-3-1 TABLE 3. 2 L 7 4 4F RT 4A25 2001040200202 20010402 00202 WP 2001 4 2 UPS01835169 1 20010207 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, FLOORBEAM HAS CORROSION UNDER PREVIOUS REPAIR. REPAIRED IAW REO-G07863. 2 L 7 4 4F RT 4A25 2001040200203 20010402 00203 WP 2001 4 2 UPS01835170 1 20010219 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, APPROX STA 1690 LONG 30 RT HAS CRACK AT VERY AFT END GEN RFTS N810UP-16-21382, REC REO G07872. FABBED AND INSTALLED REPAIR STRAP IAW REO G07872. 2 L 7 4 4F RT 4A25 2001040200204 20010402 00204 NM 2001 4 2 UPS01635281 1 20010314 A 5610 141T00132 WINDOW BOEING 767 76734AF 1385212 NM COCKPIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 326UP 27752 INSPECTION TYPE:PFLT ON PREFLIGHT WHEN TURNING ON WINDOW HEAT RIGHT SIDE WINDOW CRACKED AND RIGHT SIDE WINDOW HEAT INOP EICAS MESSAGE DISPLAYED. *S/D* REMOVED AND REPLACED THE RT NR 2 WINDOW. 2 L 7 2 4F RT A1NM 2001040200251 20010402 00251 CE 2001 4 2 CA010206003 1 20010108 A 5741 130909B175 ATTACH FITTING BEECH B300 B300 1159232 CE PWA PT6 PT6A60A 52043 NE RT WING WORN W K NONE O OTHER IN INSP/MAINT 1 CA 3827 (CAN) DURING ROUTINE MAINTENANCE TECHNICIAN NOTICED MOVEMENT IN RIGHT WING FRONT SPAR ATTACHMENT. FURTHER INVESTIGATION REVEALED THAT THE LOOSENNESS WAS CAUSED BY WORN BUSHINGS AND BOLT P/N 130909B175. BEECH CRAFT WAS NOTIFIED AND FIELD CRE W ARE ON THEIR WAY TO REPAIR WING ATTACHMENT. FURTHER INFORMATION WILL BE PROVIDED WHEN WORK IS COMPLETED. 2 L 7 2 4T 4 T RT A24CE E4EA 2001040200255 20010402 00255 NE 2001 4 2 CA010206008 2 20010106 A 7310 216062036 MANIFOLD LYC ALF502R5 BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NR 2 ENGINE CRACKED W E F A ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING A J FLAME/FIRE WARNING INDICATION CL CLIMB 1 CA LFO5485A (CAN) DURING CLIMB A NR 2 ENGINE FIRE WAS EXPERIENCED AND THE ENGINE WAS SHUT DOWN. INSPECTION REVEALED SIGNS OF A FIRE IN ZONE 2. ITS LEFT FUEL MANIFOLD WAS CRACKED. THIS CRACK WAS IN SUCH A POSITION THAT THE TASK GENERATED BY AD 97-11-05 WOULD NOT LIKELY HAVE DISCOVERED IT. FURTHER INFORMATION TO FOLLOW. 2001-02-06 TC: FOLLOW-UP INFORMATION EXPECTED FROM O PERATOR WHEN AVAILABLE. 2 H 7 4 4F 4 F RT A49EU E6NE 2001040200256 20010402 00256 CE 2001 4 2 CA010208006 1 20010129 A 2780 6046H39A RELAY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE TE FLAPS INTERMITTENT W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 7138 7138 (CAN) AIRCRAFT DEPARTED PRINCE GEORGE AIRPORT ENROUTE TO DAWSON CREEK. AFTER TAKEOFF THE FLAPS FAILED TO RETRACT FROM TH E 17 DEGREE POSITION. THEY RETURNED TO PRINCE GEORGE AND LANDED UNEVENTFULLY. DURING TAXI TO GATE THE FLAPS RETRACTED. A FTER INSPECTION BY MAINTENANCE THE FLAP RELAY WAS FOUND TO BE INTERMITTENT. THE FLAP SYSTEM WAS DEFERRED AS PER THE APPR OVED GMEL AND A NEW RELAY WAS ORDERED. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2001040200257 20010402 00257 NM 2001 4 2 UPS01235198 1 20010212 A 5320 ATTACH ANGLE BOEING 727 72751C 1384015 NM RT MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE:C-CK RT MLG W/W UPPER O/B SIDE, FS 910, MLG UPLOCK SUPPORT FRAME FWD O/B ATTACH ANGLE CRACKED IN THE O/B RADIUS APPROX 6 INCHES BELOW PRESSURE DECK. REPAIRED RIGHT MLG W/W UPPER O/B SIDE FS 910 MLG UPLOCK SUPPORT FRAME. 2 L 7 3 4F A3WE 2001040200258 20010402 00258 NM 2001 4 2 UPS01235199 1 20010219 A 5310 PRESSURE PANEL BOEING 727 72751C 1384015 NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE:C, NOSE WHEEL WELL RT SIDE WALL BS 259.5 FWD OF AFT ACCESS DOOR CRACK INDICATION ALONG ROW OF RIVET HEAD S. CUT OUT DAMAGE AREA AS PER B727 SRM 51-40-2, INSTALLED DOUBLER. REPAIR PER SRM 51-40-20. 2 L 7 3 4F A3WE 2001040200259 20010402 00259 NM 2001 4 2 UPS01235200 1 20010214 A 5320 65263073 ANGLE BOEING 727 72751C 1384015 NM AFT AIRSTAIR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE:C-CK, AFT AIRSTAIR SUPPORT ANGLE CORROSION UNDER 4TH STEP FROM TOP. REMOVED AND REPLACED CHORD SUPPORT ANGLE ON AFT AIRSTAIRS. 2 L 7 3 4F A3WE 2001040200260 20010402 00260 NM 2001 4 2 UPS01235201 1 20010219 A 5310 PRESSURE PANEL BOEING 727 72751C 1384015 NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE:C, NOSE WHEEL WELL RT SIDEWALL BS 264.3 WL 154 LWR OF AFT ACCESS DOOR CRACK INDICATION ALONG ROW OF RIVE T HEADS. CUT OUT DAMAGE AREA AS PER B727 SRM 51-40-2 & 51-10-1. INSTALLED DOUBLER REPAIR AS PER B727 SRM 51-40-2 MAT U SED 2024-T3.050 30, .5 X 27.5. 2 L 7 3 4F A3WE 2001040200261 20010402 00261 NM 2001 4 2 UPS01235202 1 20010219 A 5310 PRESSURE PANEL BOEING 727 72751C 1384015 NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE:C, NOSE WHEEL WELL RT SIDEWALL BS 248 LWR OF FWD ACCESS DOOR CRACK INDICATION AROUND FASTENER HEAD. CUT OUT DAMAGE AREA AS PER B727 SRM 51-40-2 & 51-10-1. INSTALLED DOUBLER REPAIR AS PER B727 SRM 51-40-2. 2 L 7 3 4F A3WE 2001040200262 20010402 00262 NM 2001 4 2 UPS01235203 1 20010219 A 5310 PRESSURE PANEL BOEING 727 72751C 1384015 NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE:C, NOSE WHEEL WELL BS 227.8 FWD WALL BL 0 CRACK INDICATION AROUND ROW OF FASTENER HEADS. CUT OUT DAMAGE AREA AS PER B727 SRM 51-40-2 & 51-10-1, INSTALLED DOUBLER REPAIR AS PER B727 51-40-2. 2 L 7 3 4F A3WE 2001040200263 20010402 00263 NM 2001 4 2 UPS01235204 1 20010210 A 5730 PANEL BOEING 727 72751C 1384015 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE:C-CK, RT WING T/E TOP PANEL HAS 2 CRACKS BY NR 10 SPOILER O/B HINGE. STOP DRILLED CRACKS AT RT WING T/E PANEL, ACCOMPLISHED HFEC INSP. NO CRACKS EXTENDED BEYOND STOP DRILLED HOLES. REMOVED NR 10 SPOILER O/B SUPPORT BRACKE T. REMOVED AND REPLACED CRACKED ANGLE AND RT WING, INSTALLED, REPAIRED,TREATED AND PRIMED. INSTALLED NR 10 SPOILER O/B SUPPORT BRACKET AT RT WING T/E. 2 L 7 3 4F A3WE 2001040200264 20010402 00264 NM 2001 4 2 UPS01235205 1 20010219 A 5320 PANEL BOEING 727 72751C 1384015 NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE:C, NOSE WHEEL WELL LT SIDEWALL LOWER CHORD COVER PANEL SHOWS CRACK INDICATION 2 AROUND RIVET HEADS. REM OVED PANEL AND MADE NEW PER SAMPLE AND INSTALLED AS PER B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2001040200265 20010402 00265 NM 2001 4 2 UPS01235207 1 20010211 A 5310 PRESSURE PANEL BOEING 727 72751C 1384015 NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE:C-CK, NOSE W/W LT SIDEWALL CRACK INDICATION ALONG ROW OF RIVETS HEADS. CUT OUT DAMAGE AREA AND INSTALLE D DOUBLER. 2 L 7 3 4F A3WE 2001040200266 20010402 00266 NM 2001 4 2 UPS01235208 1 20010213 A 5340 65852081 BRACKET BOEING 727 72751C 1384015 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE:C-CK, TAIL SKID COMPT, 2 UPPER SUPPORT RODS AFT ATTACH BRACKETS, LT AND RT CRACKED. REMOVED AND REPLACE D BOTH LT AND RT ATTACH BRACKETS FOR TAIL SKID UPPER SUPPORT RODS. 2 L 7 3 4F A3WE 2001040200297 20010402 00297 WP 2001 4 2 ASAA0180015 1 20010119 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 32408 53016 PDX - DURING LINE CHECK, PORTABLE EMERGENCY LIGHT WAS DETERMINED TO BE INOPERATIVE. RESEATED LIGHT ASSEMBLY CONNECTOR. LIGHT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001040200298 20010402 00298 WP 2001 4 2 ASAA0180014 1 20010116 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 948AS 53021 PDX - DURING PREFLIGHT CHECK, SECTION OF EMERGENCY FLOOR TRACK LIGHTING IN 1ST CLASS WAS DETERMINED TO BE INOPERATIVE. RECONNECTED LIGHTING SECTION. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001040200299 20010402 00299 NM 2001 4 2 GAIA01077OP 1 20010228 A 2612 FIRE LOOP BOEING 727 727259 138408J NM NR 3 ENGINE MALFUNCTIONED A GAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 901RF 22476 FLT 1806 - DEN-FWA - NR 3 FIRE WARNING BELL AND LIGHT SOUNDED AND ILLUMINATED INTERMITTENTLY DURING CLIMB-OUT. AS THROT LE WAS RETARDED AND WARNINGS CEASED. AIRCRAFT MADE AN UNEVENTFUL RETURN TO DEN. AFTER LANDING DURING TAXI TO RAMP, NR 3 FIRE WARNING CAME ON STEADY. CREW ACCOMPLISHED THE ENGINE FIRE FAILURE CHECKLIST. DEFERRED ''B'' SYSTEM NR 3 ENGINE FIRE LOOP DETECTION SYSTEM PER KHA MEL 26-6. DMI 8475. PLACARD INSTALLED. AIRCRAFT RETURNED TO SERVICE. THIS AIRCRAF T WAS TAKEN OFF THE KHA OPERATING CERTIFICATE MARCH 01, 2001. (M) 2 L 7 3 4F A3WE 2001040200300 20010402 00300 WP 2001 4 2 ASAA0180013 1 20010115 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 933AS 49234 SEA - DURING PRE-FLIGHT CHECK, OVERHEAD EMERGENCY LIGHTS AT VARIOUS LOCATIONS WERE DETERMINED TO BE INOPERATIVE. REPLAC ED ASSOCIATED BATTERY PACKS. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001040300005 20010403 00005 WP 2001 4 3 UPS01835285 1 20010315 A 2611 SMOKE DETECTOR DOUG DC8 DC873F 302199F WP CARGO BAY FAILED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:PFLT PIT 31 SMOKE DETECTOR FAILED AT DEPARTURE. REPLACED BATTERIES IN PIT 31 SMOKE DETECTOR FA3450 IAW MM 26-18-02. THIS CLEARS M211233, PLACARD REMOVED. 2 L 7 4 4F RT 4A25 2001040300006 20010403 00006 NM 2001 4 3 QXEA0100268 1 20010312 A 3030 ELEMENT DHAV DHAV DHC8 DHC8202 2809007 NM STATIC SYS CONTAMINATED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 355PH 500 SEA - FLIGHT CREW REPORTED AN UNIDENTIFIED FUME (SMELL) IN THE FLIGHT COMPARTMENT. MAINTENANCE FOUND SEALANT ON STATIC HEATER ELEMENT. REMOVED AND REPLACED STATIC PORT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001040300007 20010403 00007 NM 2001 4 3 QXEA0100269 1 20010313 A 2560 INDICATOR DHAV DHAV DHC8 DHC8202 2809007 NM FLASHLIGHT INOPERATIVE A QXEA K NONE O OTHER NR NOT REPORTED 1 NM 09 346PH 477 SEA - FLIGHT ATTENDENTS EMERGENCY FLASH LIGHT CHARGING INDICATOR INOPERATIVE. REMOVED AND REPLACED FLASH LIGHT. OPERAT IONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001040300008 20010403 00008 NM 2001 4 3 QXEA0100270 1 20010312 A 3350 6038441 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 355PH 500 SEA - A PORTION OF THE FLOOR ESCAPE PATH LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL C HECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001040300009 20010403 00009 EU 2001 4 3 QXEA0100271 1 20010313 A 3350 BRACKET GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN BROKEN A QXEA K NONE O OTHER NR NOT REPORTED 1 NM 09 484US 11234 PDX - EMERGENCY LIGHT BRACKET AT ROW 8B WAS FOUND BROKEN. REMOVED AND REPLACED EMERGENCY LIGHT. OPERATIONAL CHECKS GOO D. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001040300010 20010403 00010 NM 2001 4 3 QXEA0100273 1 20010310 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-FRETTING CORROSION ON LEFT HAND INBOARD SEAT TRACK STATION 545. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36, A ND RD-8-53-3644. 2 H 7 2 4T RT A13NM 2001040300012 20010403 00012 NM 2001 4 3 QXEA0100274 1 20010310 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN GROOVED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-12 INCH GROOVE ON RIGHT HAND INBOARD SEAT TRACK STATION 510. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36, AND RD-8-53-1339. 2 H 7 2 4T RT A13NM 2001040300013 20010403 00013 NM 2001 4 3 QXEA0100276 1 20010310 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN GROOVED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-12 INCH GROOVE WORN ON RIGHT HAND INBOARD SEAT TRACK STATION 450. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36, AND RD-8-53-1339. 2 H 7 2 4T RT A13NM 2001040300014 20010403 00014 NM 2001 4 3 QXEA0100277 1 20010309 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN GROOVED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-LIGHT CORROSION ON LEFT HAND OUTBOARD SEAT TRACK STATION 436. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36, AND RD-8-53-1342. 2 H 7 2 4T RT A13NM 2001040300015 20010403 00015 NM 2001 4 3 QXEA0100278 1 20010309 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-LIGHT CORROSION ON LEFT HAND SEAT TRACK STATION 456. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36, AND RD-8-53- 1342. 2 H 7 2 4T RT A13NM 2001040300016 20010403 00016 NM 2001 4 3 QXEA0100279 1 20010309 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-LIGHT CORROSION ON LEFT HAND OUTBOARD SEAT TRACK STATION 465. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36, AND RD-8-53-1342. 2 H 7 2 4T RT A13NM 2001040300017 20010403 00017 NM 2001 4 3 QXEA0100280 1 20010309 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-LIGHT CORROSION ON LEFT HAND OUTBOARD SEAT TRACK STATION 501. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36, AND RD-8-53-1342. 2 H 7 2 4T RT A13NM 2001040300018 20010403 00018 NM 2001 4 3 F3LA200100043 1 20010301 A 2722 65C370539 PCU BOEING 737 73736E NM RUDDER LEAKING A F3LA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 03 317FL 2938 25263 DURING C-1 CHECK, INSPECTION REPORTED RUDDER PCU FAILED INTERNAL LEAK TEST. REPLACED RUDDER PCU. PERFORMED RIG CHECK P ER MM 27-21-00 AND CHECKED GOOD. PERFORMED LEAK CHECK, NO LEAKAGE NOTED. 2 L 7 2 4F RT A16WE 2001040300019 20010403 00019 EU 2001 4 3 ERYA257011 1 20010217 A 2432 018465 BATTERY HAWKER BAE125 BAE125700B 7450007 EU EE BAY OVERHEATED E ERYA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING M OVER TEMP CR CRUISE 1 CE 07 70X 257011 NR 1 MAIN BATTERY HAD MOMENTARY BATTERY OVERHEAT RED LIGHT INDICATION. CREW EXECUTED EMERGENCY CHECKLIST; ISOLATED BATT ERIES FROM CIRCUIT, DECLARED AN EMERGENCY WITH ATC AND LANDED AT NEAREST AIRPORT (KLGC), LAGRANGE, GA. AIRCRAFT WAS SHU T DOWN WITHOUT INCIDENT. BATTERY WAS REPLACED. 2 L 7 2 4F RT A3EU 2001040300020 20010403 00020 NM 2001 4 3 UPS01435237 1 20010309 A 2621 EXTINGUISHER BOEING 747 747123F NM APU INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:PFLT, APU FIRE EXTINGUISHER INOP. *S/D* REMOVED AND REPLACED APU FIRE EXTINGUISHER BOTTLE. OPS CK NOR MAL. 2 L 7 4 4F A20WE 2001040300021 20010403 00021 NM 2001 4 3 UPS01535236 1 20010309 A 2730 1846T1003 ACTUATOR BOEING 757 75724APF 1384969 NM ELEVATOR DEFECTIVE A IPXA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 01 407UP 23729 INSPECTION TYPE:N/A DIVERSION - ELEV ASMY MSG DISPLAYED. *S/D* REMOVED AND REPLACED ELEV ASYM LIMITER ACT, OPS AND BIT E CK OK. MSG CLEARED. 2 L 7 2 4F RT A2NM 2001040300022 20010403 00022 NM 2001 4 3 UPS01235292 1 20010316 A 3350 CONTACTOR BOEING 727 72725C 138400H NM BATTERY PACK CORRODED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 931UP 19858 INSPECTION TYPE:PFLT PRE FLT - EMER EXIT LIGHT FWD ENTRY W/N STAY ILLUM. REMOVED LIGHT ASSY AFTER INSPECTION FOUND BATT ERY CONTACTS TO HAVE LIGHT CORROSION. CLEANED CONTACTS, AND RE-LAMPED LIGHT ASSY, RE-INSTALLED OPS GOOD REF M/M 33-50-1 01. 2 L 7 3 4F A3WE 2001040300023 20010403 00023 2001 4 3 UPS01835289 4 20010315 A 2564 LIFE RAFT DOUG DC8 DC871F 302199D WP CABIN MISSING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:IN A/C NEEDS TWO SIX MAN LIFE RAFTS FOR OVERWATER FLIGHT. INSTALLED TWO SIX MAN LIFE RAFTS PART 600- 107RU SER D112M & F41M. 2 L 7 4 4F RT 4A25 2001040300024 20010403 00024 WP 2001 4 3 UPS01835290 1 20010315 A 2560 SEAL DOUG DC8 DC871F 302199D WP FIRST AID KIT BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:IN, FIRST AID KIT SEAL BROKEN. REMOVED AND REPLACED FIRST AID KIT. 2 L 7 4 4F RT 4A25 2001040300025 20010403 00025 2001 4 3 UPS01835291 4 20010316 A 2565 SLIDE DOUG DC8 DC871F 302199D WP CABIN LOOSE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:IN, ESCAPE SLIDE NEEDS REPACKING. RESECURED SLIDE TO DOOR. 2 L 7 4 4F RT 4A25 2001040300026 20010403 00026 SO 2001 4 3 LR7A01005 1 20010301 A 5522 3538931 SKIN LKHEED 382 382G 526414U SO ELEVATOR DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 DURING LIGHTNING STRIKE INSPECTION PER HN51147 FOUND HSS 311 RT ELEVATOR TIP HOLED APPROX 1.5 INCH X 1.75 INCH. ACCOMPL ISHED TEMPORARY REPAIR IAW LAC MEA 382-55-01-017. PERMANENT REPAIR ACCOMPLISHED AT WSAP DURING SCHEDULED C CHECK BY TIP FABRICATION AND INSTALLATION IAW SRM SMP 583-55-30-01. NR 2005. 2 H 7 4 4T A1SO 2001040300027 20010403 00027 CE 2001 4 3 ERYAFL288 1 20010222 A 2752 100384040 MOTOR BEECH B300 B300 1159232 CE FLAP FAILED E ERYA K NONE F FLT CONT AFFECTED AP APPROACH 1 CE 07 168ET 129 FL288 ON APPROACH INTO HAYWARD, UNABLE TO EXTEND FLAPS. REPLACED FLAP MOTOR (P/N 100-384040), (S/N 3070) WITH (S/N 2536) NEW COMPONENT. PERFORMED RIGGING AND OPERATIONAL CHECKS. NO MALFUNCTIONS OR DEFECTS NOTED. 2 L 7 2 4T RT A24CE 2001040300028 20010403 00028 NM 2001 4 3 F3LA200100045 1 20010315 A 5242 DOOR BOEING 737 7372P6 NM E&E BAY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 272 3512 21613 DURING C-1 CHECK, INSPECTION REPORTED RT UPPER FWD CORNER OF E&E DOOR CORRODED. MAINTENANCE REMOVED CORROSION AND PERFO RMED A WEB REPAIR PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001040300029 20010403 00029 NE 2001 4 3 RK180 2 20010125 A 7532 7664004 BLEED VALVE BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE RT ENGINE FAILED E ERYA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 CE 07 709TA RK180 PCEJA0128 WHILE IN CRUISE FLIGHT FROM KBCT TO KBVT AT FL410 THE FLIGHT HEARD A LOUD BANG FOLLOWED BY OSCILLATIONS ON THE ROLL AXIS . AN EMERGENCY WAS DECLARED AND THE AIRCRAFT WAS LANDED AT KLACY WITH NO FURTHER PROBLEMS. REPLACED RT ENGINE BLEED AC TUATOR VALVE PER PWC JT15D-5 MM 72-30-00. OPS CHECK GOOD. TEST FLIGHT WAS SATISFACTORY. 2 H 7 2 4F 4 F RT A16SW E25EA 2001040300030 20010403 00030 NE 2001 4 3 DHL2001712003 2 20010316 A 7421 103558754 IGNITER BOX BOEING 727 72729 1384007 NM PWA JT8 JT8D7B 52053 NE NR 1 ENGINE FAILED A DHLA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 712DH 19401 655249 DURING START ATTEMPT NR 1 ENGINE DID NOT OBTAIN LIGHT-OFF. RESET IGNITION C/B''S PER THE ABNORMAL PROCEDURE. ATTEMPTED A SECOND START AND STILL DID NOT OBTAIN LIGHT-OFF. REMOVED AND REPLACED IGNITOR BOX, OPS CHECKS GOOD IAW B727 MM 74-31 -00 ENGINE RUN (CREW). 2 L 7 3 4F 4 F A3WE E2EA 2001040300031 20010403 00031 NM 2001 4 3 UPS01435294 1 20010317 A 3350 S135610A BATTERY BOEING 747 747123 1384873 NM L1 DOOR DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:W/E AFT EMERG LIGHT AT L1 DOOR INOP. COMES ON THEN FADES OUT. REMOVED AND REPLACED BATTERY, OPS CK GOO D. 2 L 7 4 4F A20WE 2001040300032 20010403 00032 NM 2001 4 3 UPS01435296 1 20010318 A 3350 GE1317 LIGHT BOEING 747 747283B 1384867 NM VERT STAIRS INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 524UP INSPECTION TYPE:W/E EMERGENCY LIGHT MCD - IN LINE VERTICAL WITH STAIRS HAD 2 BULBS BURNED. REMOVED AND REPLACED BULBS, OPS CK GOOD. 2 L 7 4 4F A20WE 2001040300033 20010403 00033 NM 2001 4 3 UPS01635293 1 20010316 A 3510 MC1025104 OXYGEN MASK BOEING 767 76734AF 1385212 NM COCKPIT DEFECTIVE A IPXA K NONE O OTHER UK UNKNOWN 1 SO 01 317UP 27745 INSPECTION TYPE:N/A, CAPTAIN''S O2 MASK HEAD STRAPS FAILED TO INFLATE. CAPT''S WRITE-UP: OXYGEN MASK HOSE DEFECTIVE. A PPEARS TO BE A HOLE IN HARNESS. HARNESS WILL NOT INFLATE PROPERLY. REPLACED CAPTAIN''S O2 MASK ASSY PER B767 MM 35-11- 51. CAPTAIN''S MASK OPS CHECKS NORMAL. 2 L 7 2 4F RT A1NM 2001040300034 20010403 00034 NM 2001 4 3 VNAA0102018 1 20010227 A 3020 3D355601 EJECTOR VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 439JS 8155 3057 DURING CLIMBOUT THE LEFT ENGINE INLET DEICE FAILED. THE FLIGHT CREW FOLLOWED THE PROCEDURES OF THE QUICK REFERENCE HAND BOOK BUT THE FAIL MESSAGE WOULD NOT CLEAR. DUE TO ICING CONDITIONS THE FLIGHT CREW RETURNED TO THE FIELD. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LEFT ENGINE INLET DEICE EJECTOR FLOW CONTROL VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-22-00. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RETURNED TO SER VICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001040300036 20010403 00036 NM 2001 4 3 01FDEA00171 1 20010301 A 5210 507945155 DOOR BOEING 727 727233 138408A NM L1 DOOR DAMAGED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 222FE 20933 FWD ENTRY DOOR LIGHT ILLUM AT 18,000. LOUD BANG AT 3000 ON DEP I FRONT AREA OF A/C. *S/D* REMOVED AND REPLACED FWD EN TRY DOOR PER 727-200 MM 52-11-00-4. PERF RIG ADJUSTMENT TEST PER B727-200 MM 52-11-001-5. INSTALL DOOR LINER PER MM 52 -11-001-5. REINSTALL ESCAPE SLIDE PER MM 25-60-015-2 AND PERF DOOR WARNING CHECK. 2 L 7 3 4F RT A3WE 2001040300038 20010403 00038 WP 2001 4 3 ASAA0180061 1 20010212 A 5248 HANDLE DOUG DC9 DC982 3022082 WP TAILCONE NOT CLOSED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 951AS 49111 SEA - DURING LINE CHECK, EXTERNAL DOOR OVER TAILCONE RELEASE HANDLE WAS FOUND TO NOT CLOSE COMPLETELY. LUBRICATED FLAPP ER DOOR HINGE. DOOR THEN CLOSED PROPERLY. (M) 2 L 7 2 4F A6WE 2001040300039 20010403 00039 WP 2001 4 3 ASAA0180042 1 20010131 A 5610 5613217520 WINDOW DOUG DC9 DC983 3022083 WP COCKPIT LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 SEA - DURING PREFLIGHT CHECK, FIRST OFFICERS SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. CLEANED AND LUBRICATED F/O WINDOW SLIDING MECHANISM. WINDOW THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001040300040 20010403 00040 NM 2001 4 3 USAA010182 1 20010226 A 5312 PRESSURE PANEL BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND PRESSURE DECK CRACKED 1 INCH, BS 664, LBL 32. INSTALLED DOUBLER AND STIFFENER PER TR 53-60-04 FIG 1. (M) 2 L 7 2 4F RT A16WE 2001040300041 20010403 00041 NM 2001 4 3 2001FAT008 1 20010310 A 7920 TUBE BOEING 757 757* NM PWA 2037 PW2037 NE SCAV PUMP COKED W FE5F E ENGINE SHUTDOWN O OTHER CR CRUISE 1 WP 03 29607 727292 DURING CRUISE AT 41,000 FEET, PILOT NOTICED THE RT ENG LOW OIL PRESSURE LIGHT COME ON FOLLOWED BY OIL QUANTITY DROPPING NEAR ZERO AND OIL PRESSURE DROPPING ALSO. IAW QRH, PILOT SHUT DOWN THE RT ENG AND DIVERTED. AFTER LANDING, THE MECHANICS FOUND OIL IN THE TAILPIPE AND THE 6QT OIL LEFT IN TANK . THE TAIL PLUG WAS REMOVED FOR CHECKING THE NR 5 BEARING COMPAR TMENT. THE OIL SCAVENGE TUBE FOUND SLIGHT COKE. IT DID NOT DETECT ANY ABNORMAL DURING THE THEREAFTER GROUND RUNNING AND FERRIED BACK TAIWAN. THE P&W PRELIMINARILY SUGGESTED REMOVE LUBE SCAVENGE PUMP FOR INVESTIGATION.THIS ENG INSTALL ON THI S A/C, SINCE NEW AT BOEING, DID NOT REMOVE BEFORE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001040300042 20010403 00042 NM 2001 4 3 UPS01235235 1 20010220 A 5522 652791715 PANEL BOEING 727 72722C 138400F NM LT ELEVATOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, NR 5 BALANCE BAY HINGE LT ELEVATOR HAS SLIGHT SURFACE CORROSION. BALANCE PANEL REPLACED IAW MM 27 -30-21. 2 L 7 3 4F A3WE 2001040300043 20010403 00043 NM 2001 4 3 UPS01235239 1 20010215 A 5753 SKIN BOEING 727 7272A1 138407F NM LT FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE:C, LEFT WING I/B AFT FLAP LOWER SURFACE L/E CRACKED AT O/B CENTER ECCENTRIC ROLLER FITTING CUTOUT. R EPAIRED PER SRM 57-50-4. 2 L 7 3 4F A3WE 2001040300044 20010403 00044 NM 2001 4 3 UPS01235242 1 20010212 A 5310 PRESSURE PANEL BOEING 727 72722C 138400F NM RT MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, CRACK IN RT MLG WHEEL WELL PRESSURE WEB AT BS 930 FWD REINFORCING BEAM AT RBL 44. CRACK STOP DRIL LED IAW SRM 51-10-1 AND EO APPENDIX C, REPAIRED IAW EO B727-5310-0460. 2 L 7 3 4F A3WE 2001040300045 20010403 00045 NM 2001 4 3 UPS01235243 1 20010218 A 5711 SPAR BOEING 727 72722C 138400F NM WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, CORROSION FOUND ON REAR SPAR UPPER CHORD OUT OF LIMITS. CHORD REPLACED IAW BOEING DRG 65C21531 AN D SMRO EO 2001-006-004 UPS ENGINEERING FILE NR B727-5710-4094-A. 2 L 7 3 4F A3WE 2001040300046 20010403 00046 NM 2001 4 3 UPS01235244 1 20010221 A 5313 STRINGER BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, CORROSION ON STRINGER 25R BS 463. REPLACED STRINGER IAW SRM 53-10-3. 2 L 7 3 4F A3WE 2001040300047 20010403 00047 NM 2001 4 3 UPS01235247 1 20010214 A 5753 FLAP TRACK BOEING 727 72722C 138400F NM LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, NR 7 FLAP TRACK, FWD ATTACH LUGS HAS HEAVY SURFACE CORROSION FOUND ON BOTH LUGS ON BOTH INBD AND O TBD THRUST FACES BORE HAS ALSO GOT SIGNS OF CORROSION. CORROSION REMOVED BY MACHINING AND BUSHINGS INSTALLED AS REQUIRE D. 2 L 7 3 4F A3WE 2001040300048 20010403 00048 NM 2001 4 3 UPS01235279 1 20010305 A 5311 FRAME BOEING 727 72730C 1384009 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:C-CK, CRACK AT FUSELAGE FRAME BS 930 ABOVE STR 13L. CUT OUT DAMAGE SECTION OF FRAME BETWEEN STR 12L & 1 3L. INSTALLED FORMED ANGLE REPAIR, HEAT TREATED. 2 L 7 3 4F A3WE 2001040300050 20010403 00050 WP 2001 4 3 ASAA0180051 1 20010207 A 5610 5613217519 WINDOW DOUG DC9 DC982 3022082 WP COCKPIT JAMMED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 954AS 49387 SFO - DURING PREFLIGHT CHECK, CAPTAINS SLIDING CLEARVIEW WINDOW JAMMED ON ATTEMPT TO OPEN. REINSTALLED LOOSE LOCK BAR P IN ON HINGE. LUBRICATED HINGE. WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001040300051 20010403 00051 WP 2001 4 3 ASAA0180041 1 20010128 A 2910 HYDRAULIC LINE DOUG DC9 DC983 3022083 WP HYD SYSTEM LEAKING A ASAA K NONE K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 01 981AS 53472 PVR - DURING GEAR RETRACTION, RIGHT HYDRAULIC SYSTEM PRESSURE AND QUANTITY WENT TO ZERO. USED ALTERNATE GER EXTENSION T O LOWER GEAR FOR LANDING. RUDDER PCU HYDRAULIC COIL ASSY LINE HAD A CRACKED SLEEVE. REPLACED HYDRAULIC LINE. SYSTEM O PERATES NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001040300053 20010403 00053 NM 2001 4 3 QXEA0100272 1 20010309 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-LIGHT CORROSION ON RIGHT HAND OUTBOARD SEAT TRACK STATION 440. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36, AN D RD-8-53-1242. 2 H 7 2 4T RT A13NM 2001040300054 20010403 00054 NM 2001 4 3 QXEA0100275 1 20010310 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN GROOVED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-15 INCH GROOVE ON RIGHT HAND INBOARD SEAT TRACK BETWEEN STATION 467 - 488. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36, AND RD-8-53-1339. 2 H 7 2 4T RT A13NM 2001040300055 20010403 00055 EU 2001 4 3 CA010212012 1 20010202 A 2434 9789601090 BRUSHES PILATS 5243212158 PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL GENERATOR WORN W O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION LD LANDING 1 CA 399 399 100272 (CAN) GEN BRUSHES WERE WORN AND COMMUTATOR DAMAGED. GEN 2 REPLACED. THE DRIVE HAD ALSO SHEARED. THE P/N OF THE DRIVE IS 524.32.12.137. THESE 2 ITEMS ARE TROUBE ITEMS AND NEED LOOKING INTO FOR THE CAUSE AND CURE. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001040300056 20010403 00056 CE 2001 4 3 CA010212013 1 20010119 A 3297 WIRE BEECH 9982000065 BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA TERMINAL BLOCK BROKEN W A UNSCHED LANDING J WARNING INDICATION LD LANDING 1 CA ALS3358 (CAN) AIRCRAFT WAS ON DESCENT AND SELECTED GEAR DOWN. MAIN GREEN LIGHTS WERE ON BUT NOT THE NOSE GEAR GREEN LIGHT. IN TR ANSIT LIGHT IN THE GEAR LIGHT WAS NOT ON. AIRCRAFT DID A FLY BY TO CONFIRM GEAR DOWN AND THEN LANDED WITHOUT INCIDENT. B ROKEN WIRE FOUND IN NOSE COMPARTMENT FOR THE GEAR DOWN GREEN FOR THE NOSE LIGHT AT THE TERMINAL BLOCK. THIS COMPARTMENT IS IN A HARSH ENVIRONMENT AND IT IS COMMON FOR THIS TO HAPPEN ON A IRREGULAR BASIS. VERY DIFFICULT TO ISOLATE WIRING AS THE MOVEMENT OF THE GEAR DICTATES THE SECURING OF THE WIRING AND ROUTING. 1 L 7 2 3T 4 T A14CE E4EA 2001040300057 20010403 00057 CE 2001 4 3 CA010212014 1 20010202 A 7312 3032710 HEATER BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA FUEL/OIL LEAKING W D RETURN TO BLOCK K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA 2646 (CAN) AIRCRAFT SMOKING ON START AND SHUTDOWN. OIL TO FUEL HEATER SUSPECTED OF INTERNAL LEAK. OIL TO FUEL HEATER REPLACED AND AIRCRAFT RETURNED TO SERCICE AFTER GROUND RUN. 1 L 7 2 3T 4 T A14CE E4EA 2001040300058 20010403 00058 EU 2001 4 3 CA010212017 1 20010116 A 2750 C125B24 WIRE PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL LT WING TE FLAPS CHAFED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 1746 (CAN) FLAPS SELECTED UUP FROM 15 DEGS. FLAPS WARNING ON CAWS, FLAPS SHUTDOWN AGAIN.PROBELM COULD NOT BE DUPLICATED IN HA NGAR.FLAP COMPUTER ON ORDER FOR TROUBLESHOOTING. FLAP CNTL WARNING UNIT WOULD CAUSE FLAP FAILURE IN AIR WHEN FLAP SELECT ION MADE. INVEST. REVEALED CODE E203 INDICATING DIFFERENCE OF 20 REVOLUTIONS BETWEEN LT & RT ROTATION SENSORS. FURTHER I NVEST. REVEALED ROTATIION SENSE WIRES ALONG WITH A.O.A. SENSE WIRES CHAFED THROUGH IN LT WING AT WING RIB 2A. CAUSE OF CHAFING IMPROPER ROUTING OF WIRES. THESE WIRES WERE ROUTED OUTSIDE OF WIRING BUNDLE SADDLE AT RIB 2A & WERE ALLOWED TO C HAFE ON AIRFRAME. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001040300059 20010403 00059 WP 2001 4 3 ASAA0180027 1 20010123 A 5610 5913217519 WINDOW DOUG DC9 DC982 3022082 WP COCKPIT INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 951AS 49111 SEA - DURING PREFLIGHT CHECK, CAPTAINS SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. RESEATED LOOSE HINGE PIN AND LUBRICATED WINDOW. WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001040300060 20010403 00060 WP 2001 4 3 ASAA0180028 1 20010122 A 4930 FUEL LINE DOUG DC9 DC983 3022083 WP APU BAY LEAKING A ASAA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 01 944AS 53019 PDX - FLT 719, DURING CLIMB, STRONG FUEL ODOR WAS NOTED IN COCKPIT. DISCOVERED FUEL LEAK AT APU ATOMIZER-TO-FUEL LINE E LBOW. TIGHTENED ELBOW FITTINGS. SYSTEM WAS THEN OPS CHECKED, WITH NO ODOR OR LEAKS BEING NOTED. (M) 2 L 7 2 4F RT A6WE 2001040300062 20010403 00062 WP 2001 4 3 ASAA0180001 1 20010103 A 5210 5910081167 DOOR DOUG DC9 DC983 3022083 WP L1 DOOR LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 29640 1526 53075 LAX - AFTER ARRIVAL AT GATE, L1 DOOR (FORWARD LEFT CREW/PAX DOOR) WAS DETERMINED TO BE HARD TO OPEN. LUBRICATED DOOR HI NGE. DOOR THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001040300065 20010403 00065 2001 4 3 ASAA0180030 4 20010126 A 2565 3961899501 LANYARD DOUG DC9 DC983 3022083 WP L1 DOOR DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PDX - DURING PRE-FLIGHT CHECK, L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DISCONNECTED FROM SLIDE COVER AND FROM GI RT BAR. RECONNECTED GIRT BAR TO BOTH THE SLIDE COVER AND GIRT BAR. (M) 2 L 7 2 4F RT A6WE 2001040300066 20010403 00066 EU 2001 4 3 DHL2001367522 1 20010118 A 5400 PYLON AIRBUS 300 A300B4203 3930306 EU FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH T02130 0265 C-CHECK, DAMAGED PYLON INSPECTED AND REMOVED FOR REPAIR. PYLON ROUTED FOR REPAIR. REPAIRED PYLON FITTED AND RE-INSTALL ED ON AIRCRAFT PER AIRBUS A300 MM. 2 L 7 2 4F RT A35EU 2001040300067 20010403 00067 NM 2001 4 3 UPS01235278 1 20010228 A 5313 BAC14935088 STRINGER BOEING 727 72730C 1384009 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:C-CK, STRINGER 18 LEFT CORRODED BETWEEN BS 440 TO BS 460. REMOVED CORROSION ON STRINGER FLANGE. FOUND OUT OF UNIT. INSTALLED STRINGER REPAIR. 2 L 7 3 4F A3WE 2001040300068 20010403 00068 NM 2001 4 3 UPS01235282 1 20010219 A 5330 SKIN BOEING 727 72730C 1384009 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:C-CK, LOW FREQ EDDY CURRENT INSP OF SKIN AT BS 441 BETWEEN STRG 18R & 19R HAS INDICATION OF CORROSION LO SS GREATER THAN 10 PERCENT. REMOVED EQUIPMENT TO ACCESS REPAIR, CUT DAMAGED AREA AND INSTALLED REPAIR PER EO -1371. 2 L 7 3 4F A3WE 2001040300069 20010403 00069 NM 2001 4 3 UPS01235283 1 20010219 A 5330 SKIN BOEING 727 72730C 1384009 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:C-CK, FUSELAGE SKIN HAS CORROSION BULGE AND APPROX 3 INCH LATERAL CRACK. REMOVED FASTENERS, REMOVED COR ROSION. NDT INSP C/W CUT DAMAGE AREA AND INSTALL DOUBLER REPAIR AT FUSE SKIN. 2 L 7 3 4F A3WE 2001040300070 20010403 00070 NM 2001 4 3 UPS01235284 1 20010219 A 7160 INTAKE DUCT BOEING 727 72730C 1384009 NM NR 2 ENGINE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:C-CK, NR 2 ENG INLET S-DUCT INNER SKIN HAS APPROX 6 INCH CIRCUMFERENTIAL CRACK AT 4 O''CLK APPROX 30 INC HES AFT OF WHERE S-DUCT ATTACHES TO INLET. CUT OUT DAMAGED AREA APPROX 7 X 1 INCHES. PERFORMED NDT AND NO CRACK INDICA TIONS. INSTALLED SKIN DOUBLER AND RIB REPAIR. 2 L 7 3 4F A3WE 2001040300071 20010403 00071 NM 2001 4 3 UPS01435275 1 20010312 A 3510 INDICATOR BOEING 747 747212B 1384886 NM OXYGEN SYSTEM INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:IN TARGET ALERT 19396 PAX O2 REQUIRES FREQUENT SERVICE M210827 - DUAL PRESS O2 IND ON S/O STATION INOP. *S/D* CLEARED AND RESEATED C/P''S ON BOTH CREW O2 BOTTLES INDICATION NORMAL. THIS CLEARS MEL M210827. 2 L 7 4 4F A20WE 2001040300072 20010403 00072 2001 4 3 UPS01835280 4 20010313 A 2565 SLIDE DOUG DC8 DC871F 302199D WP CABIN OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:IN, ESCAPE SLIDE NEEDS TO BE PUT BACK IN SLIDE CASE. RE-SECURED ESCAPE SLIDE IN CASE. 2 L 7 4 4F RT 4A25 2001040300073 20010403 00073 NE 2001 4 3 DHL2001724002 2 20010308 A 7532 VALVE BOEING 727 727228 NM PWA JT8 JT8D7 52053 NE NR 2 ENGINE SATURATED A DHLA D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 SO 01 724DH 19862 NR 2 ENGINE COMPRESSOR STALLING AT THRUST LEVELS ANYWHERE ABOVE IDLE. N1 FLUCTUATING 3 TO 4 PERCENT (UNSTABLE) N1 INDIC ATING 28 TO 33 PERCENT, N2 52 PERCENT AFTER COMPRESSOR STALL. EXIT TEMP AT 390 FUEL HEAT AND ENGINE ANTI-ICE TRIED. TR OUBLESHOT SYSTEM, FOUND PRBC SOAKED WITH WATER. CLEANED (AIR), PERFORMED ENGINE RUN IAW JRH, CH 7.9, PAGE 13, NO DEFECT S NOTED. 2 L 7 3 4F 4 F A3WE E2EA 2001040300074 20010403 00074 EU 2001 4 3 CA010212026 1 20010115 A 3010 9738114312 PRESSURE SWITCH PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL VERTICAL STAB FAILED W A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CA 1231 (CAN) PILOT REPORTED WHEN AIR FRAME DE-ICE ACTIVATED YELLOW CAUTION LIGHT STAYED ON. THE HORIZONTAL STABILIZER BOOT PRES SURE SWITCH WAS REPLACED AND SYSTEM CHECKED SERVICEABLE. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001040300075 20010403 00075 NE 2001 4 3 CA010212028 2 20010125 A 7320 3246854 DRAIN MAST AIRBUS 320 A320212 EU CFMINT CFM56 CFM565A3 NE NR 2 ENGINE LEAKING W D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 CA 18010 (CAN) THE AIRCRAFT WAS ON TAXI IN, FROM FLT 812, TO THE PARKING STAND IN VRA. THE GROUD HANDLING CREW ALERTED THE FLIGHT CREW THAT FUEL WAS LEAKING FROM THE BOTTOM OF THE NR 2 ENGINE PRIOR TO SHUTDOWN AND A PUDDLE OF FUEL HAD FORMED UNDER T HE ENGINE. INVESTIGATION OF THE LEAK, DETERMINED THE LEAK WAS FROM THE DRAIN MAST ASSEMBLY, HPT ACC DRAIN PORT. THE HPTA CC DRAIN LINE WAS REMOVED AT THE HPTACC AND CONFIRMED THE FUEL WAS LEAKING FROM THE ACTUATOR ASSEMBLY. THE HPT ACC ACTUA TOR WAS REPLACED AND LEAK CHECK AND ENGINE RUN CARRIED OUT, SERVICEABLE. 2 L 7 2 4F 4 F RT A28NM E29NE 2001040300076 20010403 00076 SO 2001 4 3 CA010212030 1 20010130 A 3242 RA16403906 DISK PIPER PA31T PA31T 7103124 SO PWA PT6 PT6A28 EA LEFT BRAKE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 120 (CAN) CRACKS WERE FOUND ON THE LT BRAKE DISC, DURING INSPECTION. THE CRACKS WERE ON THE FLANGE, BETWEEN THE WEARING SURF ACE AND THE MOUNTING SURFACE, AND CIRCUMFERENTIAL IN DIRECTION. THIS PART WAS ON 120 HOURS SINCE NEW. 1 L 7 2 3T 4 T A8EA E4EA 2001040300079 20010403 00079 CE 2001 4 3 CA010212034 1 20010123 A 3240 124K0016CL0150 HOSE CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE BRAKE ASSY LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 3104 (CAN) MAIN HYDRAULIC BRAKE HOSE ASSEMBLY LEAKING EXCESSIVELY WHENEVER GEAR IS RETRACTED OR EXTENDED. AIRCRAFT HAD NO BRA KE PRESSURE AND HAD TO RETURN TO BASE, AND DECLARED EMERGENCY. THIS IS THE SECOND INCIDENT IN TWO DAYS INVOLVING THE SAM E HOSE ASSEMBLY (DIFFERENT AIRCRAFT). HOSE RELACED, GEAR SWINGS CARRIED OUT AND SYSTEM CHECKED SERVICEABLE. 1 L 7 2 4F 4 F A22CE E1NE 2001040300082 20010403 00082 2001 4 3 CA010213007 4 20010124 A 3451 097011610039 CAPACITOR BENDIX KNR634066107 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NAV RECEIVER EXPLODED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA 24415 4577 (CAN) CAPACITOR C104 IN POWER SUPPLY EXPLODED RELEASING A STRONG BURNING SMELL WHICH WAS NOTICED BY PILOTS. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001040300083 20010403 00083 SO 2001 4 3 CA010213016 1 20010124 A 5280 12036136601 HINGE EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE HAMSTD 14RF 14RF9 NE MLG DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 4953 (CAN) LEFT MLG OUTBOARD AFT DOOR AFT HINGE ASSY FOUND BROKEN DURING LINE CHECK. HINGE FITTING IS ALUMINIUM ALLOY CASTING WHICH ALSO CONNECT TO MLG BY PUSH PULL ROD FOR DOOR CLOSURE AFTER RETRACTION. EVIDENCE OF EXISTING C RACK ABOUT 0.75 IN CH LONG FOUND ON BROKEN FITTING. CRACK COULD NOT BE SEEN DURING NORMAL VISUAL INSP OF FITTING. SINCE SECTION OF FITTING IS BETWEEN 2 ATTACHMENT ANGLES, FATIGUE CRACKING & SUBSEQUENT FAILURE OF THIS FITTING IS PROBABLY CAUSED BY STRESS DUE T O IMPROPER RIGGING OF DOOR. IS KNOWN PROBLEM ON TYPE OF A/C,&2ND OCCURRENCE ON A/C. 1ST ONE AT 9394.4 HRS&8073 CYCLES. S CHED REPETITIVE INSP OF FITTING SHOULD BE CONSIDERED FOR EARLY DETEC 2 L 7 2 4T 4 T RT A31SO E20NE 6 C P11NE 2001040300088 20010403 00088 SO 2001 4 3 CA010214009 2 20010131 A 8550 12509221 ADAPTER CESSNA 210 210L 2073448 CE CONT O520 IO520L 17032 SO MCAULY D3A34 D3A34C404 GL OIL FILTER BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 909 (CAN) OIL FILTER ADAPTER WAS FOUND LOOSE DURING OIL FILTER REMOVAL. THIS PART IS SUBJECT TO INSPECTION IN ACCORDANCE WIT H AD 96-12-22. ADAPTER WAS REMOVED AND SOME THREADS WERE BROKEN OR MISSING. NEW ADAPTER WILL BE INSTALLED. 1 H 7 1 3O 3 O 3A21 E5CE 5 C P47GL 2001040300090 20010403 00090 CE 2001 4 3 CA010214012 1 20010117 A 5210 SEAL CESSNA 650 650 2076802 CE GARRTT TFE731 TFE7313 01518 WP PAX DOOR FROZEN W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) AFTER OR DURING CLIMB TO CRUISE ALTITUDE, DOOR SEAL ANNUNCIATOR LIGHT CAME ON AND PASSENGER DOOR SEAL STARTED WHIS TLING.PILOT RETURNED TO YUL WITH NO PROBLEM.AFTER INVESTIGATION, SUSPECT THAT DOOR SEAL WAS FROZEN, FOUND LOT OF SNOW AN D ICE AROUND DOOR FRAME. 2 L 7 2 4F 4 F A9NM E6WE 2001040300092 20010403 00092 CE 2001 4 3 CA010215010 1 20010115 A 2435 23078019 BEARING BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE STARTER GEN FAILED W A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 CA 1012 (CAN) DURING CRUISE LT GENERATOR WARNING ANNUNCIATOR ILLUMINATED. CREW ATTEMPTED TO RESET BUT NO SUCCESS. INSPECTION OF THE STARTER GENERATOR REVEALED THE DRIVESHAFT END BEARING FAILED CAUSING EXCESSIVE ENDPLAY. GENERATOR OVERHAUL INTERVAL IS 1500 HOURS. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2001040300093 20010403 00093 EA 2001 4 3 CA010215011 2 20010120 A 7230 310240101 BLADE BEECH 99 B99 1154004 CE PWA PT6 PT6A28 EA COMPRESSOR FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING Y A ENGINE STOPPAGE FLAME/FIRE CL CLIMB 1 CA 522 (CAN) ENGINE FAILURE DURING CLIMB EMERGENCY DECLARED ENGINE FUEL SHUT OFF AND ENGINE SECURED. RETURNED TO AIRPORT. ENGIN E SPLIT A C FLANGE, PRELIMINARY INSPECTION FOUND CT DISC BLADE FAILURE ACCOUNTING FOR DAMAGE TO DOWNSTREAM HOT SECTION A ND POWER SECTION COMPONENTS. ENGINE SHIPPED TO SHOP FOR FURTHER EXAMINATION, UPON RECEIVING DATA CLOSING. REPORT TO FOLL OW. 1 L 7 2 3T 4 T A14CE E4EA 2001040300096 20010403 00096 EU 2001 4 3 CA010212019 1 20010124 A 2751 9787320015EX WARNING SYSTEM PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL TE FLAP CONTROL FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) UPON INSTALLATION OF FLAP CONTROL WARNING UNIT, FLAP FAILURE WAS EXPERIENCED ON INITIAL FUNCTION TESTS. ERRONEOUS ERROR CODE E212 DISPLAYED CAUSING FLAP FAILURE. F.C.W.U. REPLACED AND SYSTEM FUNCTION CHECKS WERE OK. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001040300097 20010403 00097 EU 2001 4 3 CA010212020 1 20010124 A 5610 9598110121 SEAL PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL WINDOW LEAKING W O OTHER D INFLIGHT SEPARATION DE DESCENT 1 CA 765 (CAN) DURING DESCENT, A WHISTLING NOISE WAS HEARD FROM THE WINDOW. INSPECTION REVEALED THAT THE WINDOW SEAL HAD SEPARATE D FROM THE WINDOW CAUSING AN AIR LOSS DURING DEPRESSURIZATION. THE WINDOW WAS REPLACED WITH NEW. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001040300099 20010403 00099 EU 2001 4 3 CA010212023 1 20010129 A 3246 9595601627 COVER BFGOODRICH 31543 PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL WHEEL CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 865 (CAN) WHEEL COVER FOUND TO HAVE A CRACK AROUND THE SCREW MOUNTING HOLE, DURING NORMAL DAILY INSPECTION. COVER REPLACED W ITH NEW UNIT. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001040300100 20010403 00100 EA 2001 4 3 CA010212025 2 20010115 A 7261 3008623 TUBE DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA LT ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING A SCHEDULED EMMA INSPECTION WHAT APPEARED TO BE A LONGITUDINAL CRACK APPROXIMATELY 6.5 INCHES WAS NOTICED I N THE FORWARD UPPER SCAVENGE OIL TUBE ON THE LEFT ENGINE. FURTHER VISUAL INSPECTION WAS CARRIED OUT USING A 10X MAGNIFYI NG GLASS. SUBSEQUENT TO THIS A DYE PENETRANT INSPECTION WAS PERFORMED. UPON DEVELOPMENT OF THE DYE PENETRANT IT BLED OUT CONSISTENT WITH A CRACK IDENTIFICATION.THE TUBE WAS REPLACED WITH AN OVERHAULED TUBE. 1 H 7 2 3T 4 T RT A9EA E4EA 2001040300101 20010403 00101 NM 2001 4 3 USAA010183 1 20010226 A 5312 PRESSURE PANEL BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND PRESSURE DECK CRACKED .25 INCH, BS 727B BETWEEN STRINGER 8 AND 9L. REPAIRED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001040300102 20010403 00102 NM 2001 4 3 USAA010184 1 20010226 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FRAME CRACKED .5 INCH, STATION 727F RT SIDE BETWEEN STRINGER 8/9R. REPAIRED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001040300103 20010403 00103 NM 2001 4 3 USAA010185 1 20010226 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FRAME CRACKED .25 INCH, BS 907, BETWEEN STRINGER 8/9L. DOUBLER REPAIR PER SRM 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001040300104 20010403 00104 WP 2001 4 3 UPS01835196 1 20010306 A 3231 DOOR DOUG DC8 DC873F 302199F WP RT MLG MALFUNCTIONED A IPXA K NONE J WARNING INDICATION CR CRUISE 1 SO 01 874UP 46074 INSPECTION TYPE:N/A, RT MLG DOOR OPENING IN FLT. ACCOMPLISHED GEAR SWING AND UPLATCH CHECK PER M/M 32-31-04. ALL LIGHT S AND INDICATIONS NORMAL. 2 L 7 4 4F RT 4A25 2001040300105 20010403 00105 NM 2001 4 3 USAA010189 1 20010228 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 506AU 46088 23381 CLT - FOUND FUSELAGE SKIN CRACKED 1 INCH, AFT END OF E/E COOLING DUCT OUTLET. INSTALLED EXTERNAL DOUBLER PER TR 53-30-0 7. (M) 2 L 7 2 4F RT A16WE 2001040300106 20010403 00106 NM 2001 4 3 USAA010191 1 20010228 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FRAME CRACKED .5 INCH, STATION 907 RIGHT SIDE BETWEEN STRINGER 8R/9R. TRIMMED OUT DAMAGE PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001040300107 20010403 00107 NM 2001 4 3 USAA010197 1 20010228 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FORWARD PRESSURE BULKHEAD CRACKED .5 INCH, STATION 178 WL 188, RLB .5. INSTALLED DOUBLER PER EA 69140. (M) 2 L 7 2 4F RT A16WE 2001040300109 20010403 00109 NM 2001 4 3 TSAA0133023 1 20010301 A 3350 86210066 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 807AL 23443 REPLACED NR 2 POSITION FLOOR EMERGENCY LIGHT ASSEMBLY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2001040300110 20010403 00110 NM 2001 4 3 TSAA0133024 1 20010302 A 3350 1000679 LIGHT BOEING 737 737230 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED CENTER AISLE EMERGENCY EXIT LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001040300111 20010403 00111 SO 2001 4 3 MASA01006 1 20010108 A 2740 CONTROL UNIT EMB 145 EMB145LR SO AFT EQUIP BAY FAILED A MASA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 07 828MJ 145218 FLT 5833 - CLT-MGM - PILOT REPORTED SHORTLY AFTER TAKEOFF FROM CLT, UNCOMMANDED PITCH TRIM ACTUATION. MAINTAINED CONTRO L OF THE PLANE USING HIS STANDBY TRIM SYSTEM. MX TROUBLESHOT TO A BAD HSTCU. MAINTENANCE REMOVED AND REPLACED THE HSTC U. OPS CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001040300112 20010403 00112 NM 2001 4 3 MASA01022 1 20010223 A 3350 6519024 LIGHT DHAV DHC8 DHC8* NM CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 435YV 436 DURING ROUTINE MAINTENANCE, FOUND NR 4, NR 5 AND NR 6 PAX FLOOR ESCAPE LIGHTING FIXTURES BROKEN. REMOVED AND REPLACED N R 4 AND NR 5, NR 6 LIGHT FIXTURES. OPS CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 2001040300113 20010403 00113 EA 2001 4 3 MASA01023 1 20010225 A 3320 BC10059001 LIGHT CNDAIR CL600 CL6002B19 EA GALLEY SHORTED A MASA K NONE B A SMOKE/FUMES/ODORS/SPARKS FLAME/FIRE NR NOT REPORTED 1 SW 07 97325 7325 FLT 6339 - PHX-BFL, A GALLEY LIGHT FIXTURE SHORTED WITH SPARKS AND FLAMES. THE SOCKET MELTED AND THE FLAMES WENT OUT IM MEDIATELY. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001040300114 20010403 00114 NM 2001 4 3 20010402SG001 1 20010303 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 804MA 22435 DURING P/T, FOUND EMERGENCY EXIT LIGHT ABOVE EMERGENCY EXIT 19 AND 21 DEF INOPERATIVE. REMOVED AND REPLACED BATTERY PAC K IAW MM 33-50-22. OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 2001040300115 20010403 00115 NM 2001 4 3 USAA010230 1 20010221 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 32258 24554 CLT - FOUND FRAME CRACKED .25 INCH, STATION 867 BETWEEN STATION 9R AND 8R. INSTALLED DOUBLER PER T/R 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001040300116 20010403 00116 NM 2001 4 3 USAA010231 1 20010221 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 32258 24554 CLT - FOUND FRAME CRACKED .25 INCH, STATION 907 BETWEEN STATION 9L AND 8L. INSTALLED DOUBLER PER T/R 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001040300117 20010403 00117 NM 2001 4 3 USAA010240 1 20010218 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FRAME CRACKED .5 INCH, STATION 867 RIGHT SIDE BETWEEN STRINGER 8R-9R. INSTALLED DOUBLER PER TYP REP 53-10-1 4. (M) 2 L 7 2 4F RT A16WE 2001040300118 20010403 00118 NM 2001 4 3 USAA010242 1 20010218 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32126 24557 CLT - FOUND FRAME CRACKED .5 INCH, STATION 827 FRAME RT SIDE BETWEEN STRINGER 8R-9R. INSTALLED DOUBLER PER TYP REP 53-1 0-14. (M) 2 L 7 2 4F RT A16WE 2001040300119 20010403 00119 NM 2001 4 3 USAA010243 1 20010218 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FRAME CRACKED .5 INCH, FRAME 747 RIGHT BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER TYP REPAIR 53-10-1 4. (M) 2 L 7 2 4F RT A16WE 2001040300120 20010403 00120 NM 2001 4 3 USAA010244 1 20010218 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FRAME CRACKED .25 INCH, STATION 787 FRAME RT SIDE BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER TYP REP 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001040300121 20010403 00121 NM 2001 4 3 USAA010245 1 20010218 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FRAME CRACKED .25 INCH, BS 827 BETWEEN STATION 8/9 LEFT. INSTALLED DOUBLER PER TYP REP 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001040300123 20010403 00123 CE 2001 4 3 CA010208012 1 20010117 A 3230 70000140 CIRCUIT BREAKER BEECH 76 76 1153005 CE LYC O360 O360A1G6D EA MLG INTERMITTENT W O OTHER R PARTIAL RPM/PWR LOSS AP APPROACH 1 CA 3642 (CAN) LANDING GEAR FAILED TO EXTEND WHEN GEAR SELECTED DOWN. GEAR WAS EXTENDED USING EMERGENCY PROCEDURES. AIRCRAFT WAS PUT ON JACKS HYDRAULIC POWER WOULD NOT RUN UNTIL CIRCUIT BREAKER WAS CYCLED. 1 L 7 2 3O 3 O A29CE E286 2001040300140 20010403 00140 EU 2001 4 3 UPS01135268 1 20010308 A 3150 321490 POWER SUPPLY AIRBUS A300 A300F4622R 3930360 EU CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 126UP 0810 INSPECTION TYPE:IN EVACUATION SLIDE WARNING SYSTEM LIGHTS INOP WARNING BUZZER OPERATES NORMALLY. DEFERRED M210809. REP LACED AUTONOMOUS STANDBY POWER SUPPLY UNIT PER AMM 527318. 2 L 7 2 4F RT A35EU 2001040300141 20010403 00141 NM 2001 4 3 UPS01235229 1 20010305 A 5313 STRINGER BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, DURING REPAIR TO CORRODED STRINGER 24R AT BS 463 FASTENER HOLE SIZES AT ENDS OF FRAME TO SKIN WERE FOUND TO BE EXCESSIVE BS 460 BETWEEN S2 4R AND S25R. CARRIED OUT REPAIR IAW SRM 53-10-4. 2 L 7 3 4F A3WE 2001040300142 20010403 00142 NM 2001 4 3 UPS01235231 1 20010212 A 5310 PRESSURE PANEL BOEING 727 72722C 138400F NM LT MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, CRACK IN LT WHEEL WELL PRESSURE FLOOR AT BS 940 AFT REINFORCING BEAM AT LBL 30. REPAIRED IAW EOB7 27-5310-0460 APPENDIX C. 2 L 7 3 4F A3WE 2001040300143 20010403 00143 NM 2001 4 3 UPS01235232 1 20010217 A 5320 ANGLE BOEING 727 72722C 138400F NM RT MLG CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, RT MLG DOOR ACTUATOR REACTION SUPPORT STRUCTURE 2 ANGLES CRACKED. REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2001040300144 20010403 00144 NM 2001 4 3 UPS01235233 1 20010219 A 5720 65413016 STIFFENER BOEING 727 72722C 138400F NM WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, WHILE REMOVING CORROSION FROM NR 3 FLAP TRACK TO AUX SPAR MOUNT HOLES THE STIFFENER ABOVE MOUNT RI VETED TO THE AUX SPAR WAS FOUND TO HAVE EXCESSIVE CORROSION IN BARREL NUT HOLE. STIFFENER REPLACED IAW SRM 51-30-00 AND DRAWING 65-16216. 2 L 7 3 4F A3WE 2001040300145 20010403 00145 NM 2001 4 3 UPS01235234 1 20010219 A 5755 654130115 BRACKET BOEING 727 72722C 138400F NM SPOILER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, LT WING NR 5 SPOILER INBD BRACKET SUPPORT RIVETED TO AUX SPAR HAS A NUMBER OF POPPED RIVET HEADS. BRACKET FOUND CORRODED THEREFORE BRACKET REPLACED. 2 L 7 3 4F A3WE 2001040300146 20010403 00146 NM 2001 4 3 UPS01235220 1 20010306 A 5210 STRAP BOEING 727 72751C 1384015 NM ENTRY DOOR UNSERVICEABLE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE:IN FWD ENTRY DOOR HANDLE STRAP IS NOT LONG ENOUGH TO ENGAGE VELCRO PAD WHEN LOOPED AROUND THE DOOR HANDL E. REMOVED FWD ENTRY DOOR HANDLE STRAP AS PER EO B727-2560-12064. OK FOR SERVICE. 2 L 7 3 4F A3WE 2001040300147 20010403 00147 WP 2001 4 3 UPS01835190 1 20010215 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, FITTING CRACKED STA 1690 LONG 34R. REPLACED FITTING IAW DC8 SRM 51-1-20D RETORQUED BOLT IAW DC8 S RM 51-3-1 TABLE 3. 2 L 7 4 4F RT 4A25 2001040300148 20010403 00148 WP 2001 4 3 UPS01835191 1 20010215 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, FITTING CRACKED STA 1690 LONG 34L. REPLACED FITTING IAW DC8 SRM 51-1-20D RETORQUED BOLT IAW DC8 S RM 51-3-1 TABLE 3. 2 L 7 4 4F RT 4A25 2001040300149 20010403 00149 WP 2001 4 3 UPS01835194 1 20010201 A 5310 PRESSURE PANEL DOUG DC8 DC873F 302199F WP NLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C1/3, LEFT NWW TUNNEL BOTTOM OF PRESSURE WEB AT FS -67 FROM CUSP TO I/B STIFFENER CORRODED. WEB REPAIRE D IAW REO G07874. 2 L 7 4 4F RT 4A25 2001040300150 20010403 00150 NM 2001 4 3 AWXA0001482 1 20010307 A 5350 141N782012 RADOME BOEING 757 757225 1384959 NM NOSE PUNCTURED A AWXA K NONE E VIBRATION/BUFFET DE DESCENT 1 WP 28 907AW 11207 4993 22691 LAS - 3/5/01 - ON DESCENT INTO LAS PASSING THROUGH 18,000 FT THE CREW HEARD A LOUD BANG AND AIR RUSHING SOUND FROM THE N OSE AREA AND FELT VIBRATION IN THE FLOOR. AN UNEVENTFUL LANDING WAS MADE IN LAS. UPON INSPECTION THE RADOME WAS FOUND TO HAVE A LARGE DENT AND PUNCTURE; NO EVIDENCE OF BIRD STRIKE OR OTHER MATERIAL FOUND. CREW ALSO REPORTED THE RADAR FAI LED THE ANTENNA; INSPECTION OF AIRCRAFT SHOWED NO OTHER EVIDENCE OF DAMAGE. WEATHER RADAR TESTED IAW AMM AND ALL TESTS GOOD. THE RADOME WAS REPLACED. CAUSE OF DAMAGE UNDETERMINED. 2 L 7 2 4F RT A2NM 2001040300160 20010403 00160 NM 2001 4 3 UPS01235248 1 20010216 A 5311 FRAME BOEING 727 72722C 138400F NM LT MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, LT 910 FRAME CRACKED IN MAIN LANDING GEAR WELL. REPAIRED IAW EO B727-5319-1896-B. 2 L 7 3 4F A3WE 2001040300161 20010403 00161 NM 2001 4 3 UPS01235249 1 20010216 A 5311 FRAME BOEING 727 72722C 138400F NM RT MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, RT BS 910 CRACKED IN MAIN LANDING GEAR WHEEL WELL. REPAIRED IAW DRAWING NR 65C27194. 2 L 7 3 4F A3WE 2001040300162 20010403 00162 NM 2001 4 3 UPS01435241 1 20010311 A 3350 1317 LIGHT BOEING 747 747121 1384871 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:N/A, EMERGENCY LIGHT L1854 INOP. CLEANED CONTACT AND RELAMPED. OPS CHECK OK. 2 L 7 4 4F A20WE 2001040300191 20010403 00191 NM 2001 4 3 UPS01235230 1 20010222 A 5310 PRESSURE PANEL BOEING 727 72722C 138400F NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, NOSE WHEEL WALKWAY AREA PRESSURE PANEL CRACKED AT UPPER SIDE BS 309 LBL 4. CARRIED OUT REPAIR IAW SRM 51-20-1. 2 L 7 3 4F A3WE 2001040300192 20010403 00192 NM 2001 4 3 UPS01235240 1 20010222 A 5347 SEAT TRACK BOEING 727 727247 138408F NM CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE:C, SEAT TRACK FLANGE CORRODED AT LBL 45, STA 520-529, WL 208. FOUND SEAT TRACK CORROSION TO BE OUT OF L IMITS. REPLACED SEAT TRACK FROM BS 480--BS 530 PER SRM 53-10-05 FIG 1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 2001040300199 20010403 00199 NM 2001 4 3 UPS01235267 1 20010210 A 2611 SMOKE DETECTOR BOEING 727 72725C 138400H NM CARGO BAY INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:IN REF: M210868 LOWER CARGO SMOKE DETECTOR INOP. REMOVED AND REPLACED CCU AND CONFIGURATION MODULE AS P ER MM 26-18-00. OPS CHECK GOOD, PLACARD REMOVED. DEFERRAL CLEARED. 2 L 7 3 4F A3WE 2001040400002 20010404 00002 NM 2001 4 4 TWAA0103208 1 20010219 A 7830 THRUST REVERSER BOEING 717 717200 1383700 NM RT ENGINE UNLOCKED A TWAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 05 2410W 55077 2223 AFTER TAKEOFF AT 1400 FEET THE RT ENGINE THRUST REVERSER DEPLOYED. THE ENGINE WAS SHUT DOWN AND FLIGHT RETURNED TO MKE. NO CHECK-C. *S/D* INVESTIGATION FOUND THE REVERSER UNLOCK LIGHT WAS ON AT INITIAL DEPARTURE AND CREW RETURNED TO THE GATE. MAINTENANCE DEACTIVATED THE REVERSER ELECTRICALLY AND HYDRAULICALLY BUT MISUNDERSTOOD THE INSTRUCTIONS CONCERNING INSTALLATION OF LOCKOUT PINS, AND DID NOT INSTALL THEM. THAT ENABLED THE REVERSER TO DEPLOY IN FLIGHT. THE INSTRUCTIO NS HAVE SINCE BEEN CLARIFIED, AND DISPATCH WITH THE UNLOCK LIGHT ILLUMINATED IS NOW PROHIBITED. 2 L 7 2 4F TR A6WE 2001040400003 20010404 00003 NM 2001 4 4 2001UALA00103 1 20010209 A 2150 A/C PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE AC BAY ICED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 7280U 21558 DURING CLIMB AIRCRAFT EXPERIENCED SMOKE IN THE COCKPIT. THE AIRCRAFT RETURNED TO DSM. *S/D* THE PACK TEMPERATURE BECA ME VERY HIGH. FOUND RAM AIR INLETS PACKED WITH ICE. CLEANED ICE FROM INLETS AND ACCOMPLISHED A HIGH POWER RUN. OPERAT ION CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001040400004 20010404 00004 NM 2001 4 4 2001UALA00105 1 20010212 A 2133 CONTROL VALVE AIRESRCH 39608831MOD BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN PRESSURE FAILED A UALA K NONE O OTHER DE DESCENT 1 WP 29 7274U 21421 CABIN PRESSURE COULD NOT BE MAINTAINED DURING DESCENT. *S/D* FLOW CONTROL VALVES FAILED. REPLACED LEFT AND RIGHT AIR FLOW CONTROL VALVES. 2 L 7 3 4F 4 F A3WE E2EA 2001040400005 20010404 00005 NM 2001 4 4 2001UALA00106 1 20010212 A 2130 VALVE 6577MOD BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN PRESSURE FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 7295U 21573 CABIN PRESSURIZATION COULD NOT BE MAINTAINED DURING CLIMB. AIRCRAFT DIVERTED TO RNO. *S/D* FOUND EQUIPMENT COOLING VA LVE NOT CLOSING. REPLACED EQUIPMENT COOLING VALVE. 2 L 7 3 4F 4 F A3WE E2EA 2001040400006 20010404 00006 NM 2001 4 4 2001UALA00110 1 20010213 A 2120 UNKNOWN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 766UA 26917 PUNGENT ELECTRICAL ODOR ROWS 12 - 20 REPORTED BY FLIGHT ATTENDANTS AT GEAR EXTENSION. DISSIPATED TO MUCH LESS BY TAXI-I N. THERE WAS NO INDICATION OF ANY ELECTRICAL RELATED PROBLEM(S) IN THE CABIN. ACCOMPLISHED HIGH POWER ENGINE RUN ON BO TH ENGINES, OPERATED AC PACKS AND INSPECTED CABIN LIGHTING FOR ANY POSSIBLE SHORTS. THE SYSTEMS OPERATIONAL CHECKED SAT ISFACTORY AND NO PROBLEMS FOUND. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001040400007 20010404 00007 NM 2001 4 4 2001UALA00113 1 20010213 A 2130 VALVE 6577MOD BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN PRESSURE FAILED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 7295U 21573 AIRCRAFT RETURNED TO DEN DUE TO A CABIN PRESSURIZATION PROBLEM. *S/D* FOUND AIR TASK VALVE NOT CLOSING. REPLACED AIR TASK VALVE. 2 L 7 3 4F 4 F A3WE E2EA 2001040400008 20010404 00008 NM 2001 4 4 2001UALA00116 1 20010215 A 3260 CIRCUIT BREAKER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT POPPED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 330UA 24191 LANDING GEAR WARNING INDICATION. *S/D* ACCOMPLISHED CHECK OF LEVER LOCK SOLENOID. FOUND LANDING GEAR LATCH AND PRESS WARNING CIRCUIT BREAKER OPEN. RESET CIRCUIT BREAKER. SYSTEM CHECKED NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2001040400009 20010404 00009 SO 2001 4 4 GLBA2001041 1 20010218 A 3260 922FS2A6NZ735A SENSOR EMB 120 EMB120ER 3260203 SO LT MLG CONTAMINATED A GLBA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 CE 01 297UX 120297 LEFT LANDING GEAR AIR/GROUND C/B POPPED. INSPECTED FOUND MOISTURE IN LEFT AIR/GROUND PROX SWITCH. REPLACED, OPS CHECK ED GOOD. 2 L 7 2 4T RT A31SO 2001040400010 20010404 00010 CE 2001 4 4 GLBA2001042 1 20010220 A 7722 3053995011 PROBE BEECH 1900 1900D 1154162 CE LT ENGINE DEFECTIVE A GLBA A D UNSCHED LANDING RETURN TO BLOCK O OTHER CR CRUISE 1 CE 01 219GL UE219 RETURN TO BLOCK, LEFT ENGINE ITT INDICATOR FAILED. REMOVED AND REPLACED LEFT T5 HARNESS AND TRIM PROBE. 2 L 7 2 4T RT A24CE 2001040400015 20010404 00015 CE 2001 4 4 CA010219010 1 20010201 A 2720 03101965 SPRING CESSNA 172 172L 2072432 CE LYC O320 O320E2D 41508 EA RUDDER PEDAL BROKEN W A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CA 8858 (CAN) HOOK BROKEN OFF SPRING (FOR LT RUDDER BAR) AND ALLOWED R/H SPRING TO PULL RUDDER TO RIGHT. PILOT HAD TO MAINTAIN P RESSURE ON LEFT PEDAL TO MAINTAIN CONTROL OF AIRCRAFT. UNEVENTFUL LANDING CARRIED OUT AFTER COMPLETE CIRCUIT AND APPROAC H. SPRING DID NOT BREAK AT AREA OF NORMAL WEAR AS RUDDER BAR LEVER HOLE CONTACT AREA. IT BROKE ABOUT 3/8 INCH FURTHER DO WN THE HOOK TOWARD THE MAIN PART OF THE SPRING. FATIGUE SUSPECTED. 1 H 7 1 3O 3 O NT 3A12 E274 2001040400016 20010404 00016 EU 2001 4 4 CA010219011 1 20010205 A 2750 9742001214 RELAY PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL TE FLAPS FAILED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 427 (CAN) WHEN FLAPS WERE SELECTED FOR APPROACH THEY DID NOT RESPOND, PILOT PROCEEDED TO DO A 0-DEGREE FLAP LADNING. DURING MAINTENANCE CHECKS, A FLAP RESET WAS CARRIED OUT. THE FLAPS RESPONDED TO 15 DEGREE SELECTION BUT WOULD NOT RETRACT BACK TO 0-DEGREES WITHOUT GOING ALL THE WAY TO 40 DEGREES AND HITTING THE DOWN LIMIT SWITCH, THEN FLAP WOULD RETRACT. RELAY K 32 UP/DOWN WAS REPLACED.NOTE: SB 27-011R1 REFERS TO SIMILAR FLAP CONTROL PROBLEM AND WAS INCORPORATED SUBSEQUENTLY. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001040400018 20010404 00018 SO 2001 4 4 CA010219019 2 20010201 A 7314 705272 DIAPHRAGM G714769 CESSNA 414 414 2075908 CE CONT O520 TSIO520J 17040 SO MCAULY 3AF32C 3AF32C93 GL FUEL PUMP CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) DURING AN INSPECTION, A FUEL STAIN WAS NOTICED ON AN ADF ANTENNA. IT WAS TRACED TO THE HEATER FUEL PUMP. THE PUMP WAS DISASSEMBLED AND A CRACKED DIAPHRAGM WAS FOUND. WHEN THE HEATER WAS RUNNING, FUEL POURED OUT AT THE FUEL PUMP HOUSIN G. THE DIAPHRAGM LOOKED VERY OLD. THE FUEL PUMP WAS REPLACED. 1 L 7 2 3O 3 O RT A7CE E8CE 5 C P22EA 2001040400020 20010404 00020 CE 2001 4 4 CA010222002 1 20010205 A 3246 1143880241 BEARING BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE NR 3 WHEEL DEFORMED W K NONE O OTHER IN INSP/MAINT 1 CA 340 (CAN) MAINTENANCE NOTED MOVEMENT OF MAIN WHEEL NR 3 DURING ROUTINE MAINTENANCE AND INVESTIGATED. OUTER BEARING SHOWED SI GNS OF FAILURE AND DAMAGE TO BOTH WHEEL AND BRAKE ASSEMBLY REQUIRED REPLACEMENT. LIKELY CAUSE DUE TO BEARING REINSTALLED THAT SHOULD HAVE BEEN REPLACED ON PREVIOUS BUILD. WHEEL AND BRAKE WAS REPLACED AND AIRCRAFT RELEASED. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2001040400021 20010404 00021 NM 2001 4 4 CA010222005 1 20010206 A 2781 40173 SWITCH BOEING 727 727223 1384074 NM PWA JT8 JT8* 52044 NE LE FLAPS FAILED W D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CA (CAN) DURING TAXI TO RUNWAY, NR 2 KRUEGER FLAP GREEN LIGHT FAILED TO ILLUMINATE. AMBER LEADING EDGE WARNING LIGHT ON FOR WARD PANEL REMAINED ILLUMINATED. NR 2 KRUEGER LEADING EDGE EXTEND SWITCH REPLACED IN ACCORDANCE WITH MM 27-82-1, OPERATI ON CHECKS SERVICEABLE. NO FURTHER DEFECT NOTED. 2 L 7 3 4F 4 F A3WE E2EA 2001040400022 20010404 00022 EU 2001 4 4 CA010222008 1 20010119 A 3222 5322012200 RING PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL NLG STRUT BINDING W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 2483 2483 (CAN) AFTER TAKEOFF, THE CREW HAD A RED NOSE GEAR INIDCTION. THE GEAR WAS CYCLED DOWN & THREE GREEN WAS INDICATED. THE A IRCRAFT RETURNED & LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS PUT ON JACKS & IT WAS NOTED THAT THE NOSE GEAR SHOCK STRUT DID NOT EXTEND. WHEN THE GEAR WAS RETRACTED INTO THE WHEEL WELL, THE NOSE GEAR FORKS HAD COME INTO CONTACT WITH THE L/H NOSE GEAR DOOR ROD WHICH WAS FOUND BROKEN. DISASSEMBLY OF THE NOSE GEAR REVEALED THAT THE GUIDE RING CAN BIND WITH REDUC ED TEMPERATURES AND RESTRICTS THE MOTION OF THE SHOCK STRUT. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001040400027 20010404 00027 EU 2001 4 4 CA010222017 1 20010208 A 3010 9738114311 PRESSURE SWITCH PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL DEICE SYSTEM INTERMITTENT W O OTHER N FALSE WARNING DE DESCENT 1 CA 1163 1163 (CAN) DURING FLTS WHEN DE-ICE SYS IS DEPLOYED & OAT IS IN -30 & BELOW RANGE, & EITHER 1 OR 3 MIN CYCLE DURATION IS SELEC TED, SYS INDICATES PROPER OP THROUGHOUT CYCLE. UPON COMPLETION OF CYCLE AMBER DE-ICE CAWS CAUTION WOULD ILLUMINATE IN CO NJUNCTION WITH FLASHING GREEN DEICE CAWS, THUS INDICATING FAILURE: WHEN SYS IS TURNED OFF & THEN BACK ON ENTIRE PROCESS WOULD REPEAT.THIS PROBLEM DOESNT APPEAR TO ARISE WHEN OP AT WARMER TEMPS.WHEN TROUBLESHOOTING TO IDENTIFY FAILED PART O F SYS IT DETERMINED (ON SEPARATE OCCASIONS) THAT OUTBOARD UPPER & OUTBOARD LOWER L/H & R/H PRESSURE SWITCHES WOULD APPEA R TO BE STUCK OPEN INDICATING FAILURE THAT SIMULATED INFLIG HT SYMPTOMS. BY REMOVING SWITCHES & APPLYI 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001040400029 20010404 00029 CE 2001 4 4 CA010223004 1 20010108 A 2701 126014017 YOKE CESSNA 182 182Q 2072732 CE CONT O470 O470U 17026 SO MCAULY 2A34C C2A34C204 GL CONTROL COLUMN LOOSE W A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 CA 8323 (CAN) CENTRAL/AILERON CONTROL: SLIGHT TWITCH OR LOOSE IN YOKE POSITION TO THE RIGHT. SLIGHT LAG IN CONTROL RESPONSE ON I NITIAL ROLL INPUT. PILOT CONTROL YOKE FASTENERS AT THE CONTROL COLUMN TUBE FOUND LOOSE. BOLTS SECURED WITH LOCKTITE. AIL ERON CABLE TENSIONS WERE FOUND WITHIN LIMITS. 1 H 7 1 3O 3 O NT 3A13 E273 5 C P3EA 2001040400036 20010404 00036 CE 2001 4 4 CA010223014 1 20010214 A 5311 05120118 BULKHEAD CESSNA 172 172P 2072436 CE LYC O320 O320D2J 41508 EA FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 12955 (CAN) DURING CESSNA PHASED INSP, BULKHEAD, STATION 108, FOUND CRACKED IN 3 PLACES AT RADIUS OF EACH CORNER EXCEPT FOR TO P LEFT. BULKHEAD FORMS BACK OF BAGAGE COMPT AREA. CRACKS RADIATE FROMTHE FLANGE OF BULKHEAD & EXTEND INTO WEB OF BULKHE AD. CHECK OF REST OF FLEET OF SIMILAR AGED AIRCRAFT DISCLOSED 2 OTHER A/C WITH SIMILAR CRACKS & 2 ADDITIONAL A/C WITH CR ACKS IN BOTTOM RIGHT RADIUS ONLY. CESSNA HAS BEEN NOTIFIED OF PROBLEM AREA. ALL A/C AFFECTED HAVE BEEN GROUNDED UNTIL EF FECTIVE REPAIRS CAN BE DEVELOPED. 1 H 7 1 3O 3 O NT 3A12 E274 2001040400037 20010404 00037 EU 2001 4 4 CA010223015 1 20010216 A 2434 5005012235 BRUSHES BOSCH 5243212158 PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL GENERATOR WORN W A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 CA 156 100271 (CAN) NR 2 GENERATOR SYSTEM TRIPPED OFF LINE IN FLIGHT. WOULD NOT COME BACK ON LINE. INVESTIGATION SHOWED THAT THE BRUS HES WERE WORN OUT AND THE COMMUTATOR SHOWED SIGNS OF PITTING AND ARCING. THE GENERATOR ASSEMBLY WAS REPLACED AND THE AIR CRAFT WAS RETURNED TO SERVICE. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001040400045 20010404 00045 EU 2001 4 4 CA010226013 1 20010127 A 7500 200645001 DUCT AIRBUS 310 A310304 EU GE CF6 CF680C2A5 NE NR 2 ENGINE DAMAGED W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA (CAN) DURING CLIMB, NR 2 ENGINE FIRE INDICATION OBSERVED. ENGINE RETARDED TO IDLE. FIRE WARNING DISAPPEARED. AIRCRAFT LA NDED WITHOUT INCIDENT. 14TH STAGE DUCT FOUND DAMAGED. REPLACED I.A.W. MM 36-00-00. SUSPECT CLAMP CAUSED PROBLEM. RELATED PARTS REPLACED INCLUDED THROTTLE CABLE, HP VALVE, HARNESS ASSEMBLY AND FAN REVERSER COWL. AIRCRAFT GROUND RUN SERVICEAB LE. NO FURTHER PROBLEMS DURING SUBSEQUENT FLIGHT. 2 L 7 2 4F 4 F RT A35EU E13NE 2001040400053 20010404 00053 GL 2001 4 4 C2XA01IA138 2 20010228 A 7313 2306590A NOZZLE ALLSN EMB 145 EMB145 SO ALLSN AE300 AE3007A GL NR 2 ENGINE ODOR A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 13964 CAE311209 145123 CAE311209 AMA - FLIGHT 4022, THE CREW REPORTED A FUEL SMELL IN THE COCKPIT AND CABIN, THE AIRCRAFT RETURNED TO AMA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 4 THROUGH NR 13 FUEL NOZZLES ON THE NUMBER TWO ENGINE IN ACC ORDANCE WITH R/R MM 73-11-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE PROBLEM REOCCURED ON 03/02/01 ON FLIGHT 3997 FROM LBB TO IAH. THE AIRCRAFT RETURNED TO LBB WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND R EPLACED THE NR 1, 2, 3, 14, 15 AND 16 FUEL NOZZLES ON THE NUMBER TWO ENGINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE WITH NO FURTHER INCIDENTS TO DATE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001040400054 20010404 00054 NM 2001 4 4 VNAA0103003 1 20010303 A 2150 A/C PACK DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE AC BAY FAILED A VNAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 07 460PS 3061 WHILE PARKED AT THE GATE THE FLIGHT CREW REPORTED THE RIGHT ENVIROMENTAL UNIT FAILED AND SMOKE ENTERED THE CABIN. MAINT ENANCE INSPECTED AND FERRIED THE AIRCRAFT TO DAY. UPON ARRIVAL IN DAY MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL C HECKS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 21-50-00 AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001040400055 20010404 00055 NM 2001 4 4 VNAA0103004 1 20010304 A 3010 001B574A2000005 ANTI-ICE SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT WING FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 436JS 1856 3052 DURING CLIMBOUT THE FLIGHT CREW RECEIVED A RIGHT WING MIDDLE AIRFOIL DEICE FAIL MESSAGE. THE FLIGHT CREW RETURNED TO T HE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT MIDDLE LEADING EDGE ASSEMBLY IN ACCO RDANCE WITH DORNIER MAINTENANCE MANUAL 30-10-00. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RETURNED TO SERVIC E. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001040400056 20010404 00056 NM 2001 4 4 SWAA010616 1 20010228 A 3397 WIRE BOEING 737 7372H4 138448C NM LAVATORY CHAFED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 092SW 22964 DIVERSION - SMOKE/FUMES IN COCKPIT. COCKPIT CHECKLIST C/W AND SMOKE DISSIPATED. FOUND EVIDENCE THAT FWD LAV MIRROR LIG HT BALLAST OVERHEATED. COLLARED C/B AND PLACED ON MEL. BALLAST TO BE REPLACED IN DAL ON 03/03/01. REPLACED BALLAST IN DAL ON 03/03/01. DID NOT REMEDY PROBLEM. COLLARED C/B AND ACFT REMAINS ON MEL. ON 03/04/01 AT DAL, FOUND CHAFED WIRE S AT CONNECTOR D466. REPAIRED WIRING AND REMOVED AND REPLACED BALLAST PER MM, OPS CHECK GOOD. 2 L 7 2 4F A16WE 2001040400057 20010404 00057 EU 2001 4 4 RAIA00103002 1 20010104 A 7600 31055016 SENSOR JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE NR 2 ENGINE FAILED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 566HK 4650 4650 41084 75089 MEM- DURING TAKEOFF ROLL NR 2 IEC FAULTED. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE P2 SENSOR IAW TPE331-14 MAINTEN ANCE MANUAL. 2 L 7 2 4T 4 T RT A41NM E18NE 2001040400058 20010404 00058 NM 2001 4 4 CALA0100187 1 20010302 A 5330 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73385 26314 INSPECTION FOUND FUSELAGE SKIN GOUGED JUST AFT OF RIGHT LOWER HORIZONTAL LUG AT STA 1150. THE DAMAGED SKIN WAS REMOVED AND REPLACED IAW SRM 51-40-01. 2 L 7 2 4F RT A16WE 2001040400059 20010404 00059 NM 2001 4 4 CALA0100188 1 20010302 A 5320 WEB BOEING 737 7373T0 1384582 NM CARGO BAY CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND A 1 INCH CRACK BETWEEN RIVETS ON FORWARD EDGE OF WEB ON AFT CARGO DOOR CUTOUT AFT SIDE, BS 847 BETWEEN S24R AND S25R. THE CRACKED AREA OF WEB WAS REMOVED AND A REPAIR WEB WAS INSTALLED IAW SRM 53-60-15, 51-20-01, AND 51-40 -02. 2 L 7 2 4F RT A16WE 2001040400060 20010404 00060 NM 2001 4 4 CALA0100189 1 20010302 A 5310 DOOR FRAME BOEING 737 7373T0 1384582 NM CARGO BAY DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND FORWARD CARGO DOOR JAMB DENTED AT STA 440 AT FLOOR LINE. THE DENTED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW DRAWING 69-15224 AND SRM 51-70-13. 2 L 7 2 4F RT A16WE 2001040400061 20010404 00061 NM 2001 4 4 CALA0100190 1 20010302 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND INTERCOSTAL CRACKED BETWEEN STA 500D AND 520, RBL 45, WL 208.1. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-40-2. 2 L 7 2 4F RT A16WE 2001040400062 20010404 00062 NM 2001 4 4 CALA0100191 1 20010302 A 5330 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 344 AND TWO INCHES BELOW S19R. THE DENTED AREA WAS REMOVED AND A REPAIR WA S INSTALLED IAW ECRA 5330-03035 AND EA 04-5310-0679. 2 L 7 2 4F RT A16WE 2001040400063 20010404 00063 NM 2001 4 4 CALA0100192 1 20010302 A 5730 SKIN BOEING 737 7373T0 1384582 NM RT WING DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND RT WING L/E DELAMINATED AT WBL 254.0. THE LEADING EDGE WAS REPAIRED IAW SRM 57-41-01, FIGURE 2, 51-70- 16, PARAGRAPH 3A, ECRA 5720-01838, AND EA 04-5741-0672. 2 L 7 2 4F RT A16WE 2001040400064 20010404 00064 NM 2001 4 4 CALA0100193 1 20010302 A 5531 RIB BOEING 737 7373T0 1384582 NM VERTICAL STAB GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17329 23459 INSPECTION FOUND L/E RIB OF VERTICAL STABILIZER GOUGED AT STA 10-40. THE DORSAL FIN RIB WAS REMOVED AND REPLACED IAW SR M 51-10-02. 2 L 7 2 4F RT A16WE 2001040400065 20010404 00065 NM 2001 4 4 CALA0100194 1 20010302 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND FLOORBEAM CORRODED AROUND FASTENER HOLES ON TOP SURFACE AT STA 947, RBL 12 TO LBL 25. THE CORROSION WA S REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5310-03851. 2 L 7 2 4F RT A16WE 2001040400066 20010404 00066 NM 2001 4 4 CALA0100195 1 20010303 A 5522 SKIN BOEING 737 7373Q8 1384670 NM LT ELEVATOR DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73385 26314 INSPECTION FOUND A HOLE IN LT ELEVATOR UPPER SKIN AT STA 39.02 (APPROXIMATELY 21 INCHES I/B AND 4 INCHES FROM AFT SPAR). THE LT ELEVATOR SKIN WAS REPAIRED IAW ECRA 5520-01250. 2 L 7 2 4F RT A16WE 2001040400067 20010404 00067 NM 2001 4 4 CALA0100196 1 20010303 A 5313 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND A CRACK APPROXIMATELY .25 INCH LONG AT HOLE IN STRINGER 21L BETWEEN STA 460 - 480. THE HOLE WAS REAMED TO 0.312 INCH. AN ANGLE REPAIR WAS INSTALLED IAW SRM 53-00-03. 2 L 7 2 4F RT A16WE 2001040400068 20010404 00068 NM 2001 4 4 CALA0100197 1 20010303 A 5310 DOOR FRAME BOEING 737 7373T0 1384582 NM CARGO BAY DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND FORWARD CARGO DOOR JAMB DENTED AT STA 492, FLOOR LINE. THE DENTED AREA WAS REMOVED AND A REPAIR WAS IN STALLED IAW SRM 51-70-13. 2 L 7 2 4F RT A16WE 2001040400069 20010404 00069 WP 2001 4 4 CALA0100198 1 20010303 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14889 49118 INSPECTION FOUND FORWARD CARGO DOOR JAMB PAN CORRODED AROUND RIVNUTS. THE CORRODED AREA OF DOOR PAN WAS CUT OUT AND A R EPAIR ANGLE AND SPLICE ANGLES WERE INSTALLED IAW SRM 53-05, FIGURE 44, 51-10-3, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 2001040400070 20010404 00070 NM 2001 4 4 CALA0100199 1 20010303 A 5330 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73385 26314 INSPECTION FOUND FUSELAGE SKIN GOUGED BELOW LT AFT HORIZONTAL LUG FITTING AT STA 1142. NEW SKIN WAS INSTALLED IAW SRM 5 1-10-02 AND MM 20-10-34. 2 L 7 2 4F RT A16WE 2001040400071 20010404 00071 NM 2001 4 4 CALA0100200 1 20010303 A 5311 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73385 26314 INSPECTION FOUND A 2 INCH CRACK IN BELTFRAME IN AFT CARGO BIN AT STA 807, RBL 2. THE LOWER FRAME SECTION WAS REMOVED AN D REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001040400072 20010404 00072 NM 2001 4 4 CALA0100201 1 20010303 A 5330 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND A VERTICAL GOUGE IN FUSELAGE EXTERNAL SKIN FROM WINDOW EDGE TO LAP SEAM AT STA 877, STRINGER 14L. THE SKIN WAS REPAIRED IAW ECRA 5330-03037. 2 L 7 2 4F RT A16WE 2001040400073 20010404 00073 NM 2001 4 4 CALA0100202 1 20010303 A 5320 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 47332 23570 INSPECTION FOUND LT SIDE Z-ANGLE CORRODED AT STA 312 - 360. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 2 4F RT A16WE 2001040400074 20010404 00074 NM 2001 4 4 CALA0100203 1 20010304 A 5330 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE EXTERNAL SKIN AT R-1 DOOR LOWER HINGE CUTOUT. THE SKIN WAS REPAIRED IAW ECR A 5330-03036 AND EA 04-5311-0688. 2 L 7 2 4F RT A16WE 2001040400075 20010404 00075 NM 2001 4 4 CALA0100204 1 20010304 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND FLOORBEAM UPPER FLANGE CORRODED AT STA 294.5, BL 0. THE FLOORBEAM UPPER FLANGE WAS REPAIRED IAW ECRA 5 310-04110 AND EA 04-5310-0697. 2 L 7 2 4F RT A16WE 2001040400076 20010404 00076 NM 2001 4 4 CALA0100205 1 20010305 A 3397 WIRE BOEING 737 7373T0 1384582 NM CABIN DAMAGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14334 23572 THE FLOOR TRACK LIGHTS IN FIRST CLASS SECTION OF CABIN WERE FOUND INOPERATIVE. MAINTENANCE FOUND WIRES DAMAGED NEAR ROW 1 LEFT. THE WIRES WERE REPAIRED AND THE BLOWN FUSE IN POWER SUPPLY WAS REPLACED IAW MM 20-10-13. 2 L 7 2 4F RT A16WE 2001040400077 20010404 00077 SO 2001 4 4 COMA0110038 1 20010301 A 3230 LANDING GEAR EMB 120 EMB120RT SO NLG & MLG MALFUNCTIONED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 269CA 120263 LANDING GEAR SLOW TO EXTEND, AND INDICATED UNSAFE. RECYCLED GEAR WITH SAME RESULTS. COULD NOT DUPLICATE. LANDING GEAR RETRACTION CHECKS WERE NORMAL. 2 L 7 2 4T RT A31SO 2001040400078 20010404 00078 EA 2001 4 4 COMA0160295 1 20010301 A 2750 FLAP CNDAIR CL600 CL6002B19 EA WING FAILED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 818CA 7408 FLAPS FAILED AT 26 DEGREES WHEN SELECTED UP. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2001040400079 20010404 00079 WP 2001 4 4 TWAA0104101 1 20010303 A 3350 58222 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A TWAA K NONE O OTHER CR CRUISE 1 CE 05 925TW 49357 THE EGRESS LIGHTS AT ROWS 16 TO 23 CAME ON IN FLIGHT. REPLACED THE POWER SUPPLY. CHECK-C 11-2-00 MCI. 2 L 7 2 4F A6WE 2001040400080 20010404 00080 WP 2001 4 4 TWAA0104102 1 20010304 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 969TW 53619 THE EGRESS LIGHT STRIP AT ROW 15 TO 20, AND ROW 24 TO 28 WERE INOPERATIVE. RECONNECTED EGRESS LIGHT POWER FEEDER TO THE STRIP. CHECK-C 7-28-00 JFK. 2 L 7 2 4F RT A6WE 2001040400081 20010404 00081 NM 2001 4 4 TWAA0104103 1 20010303 A 3350 58222 POWER SUPPLY BOEING 767 767231 1385131 NM CABIN INTERMITTENT A TWAA K NONE O OTHER CR CRUISE 1 CE 05 605TW 22568 THE EGRESS LIGHTS FLICKERED ON AND OFF IN THE B-ZONE, RT SIDE OF THE CABIN. REPLACED THE POWER SUPPLY. CHECK-C 12-23-0 0. 2 L 7 2 4F RT A1NM 2001040400082 20010404 00082 WP 2001 4 4 TWAA0104104 1 20010305 A 5313 LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 985Z 47491 DURING CHECK-C MAINT FOUND .25 INCH CRACK AT LONGERON 5L LOWER LEFT LEG, STA 699. REPAIRED PER SRM 53-11-3. INSTALLED LAST TWO BOLTS PER SRM 51-30-1. 2 L 7 2 4F A6WE 2001040400084 20010404 00084 SO 2001 4 4 C2XA01CL044 1 20010302 A 3234 7455501REVF CONTROL HANDLE EMB 135 EMB135LR SO COCKPIT FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14522 144 144 145383 LGA FLIGHT 4100 THE CREW REPORTED AFTER TAKEOFF THE LANDING GEAR LEVER DISAGREE MESSAGE CAME ON THE ECIAS ALONG WITH 3 U P RED INDICATIONS. THE GEAR WAS RECYCLED UNSUCESSFULLY. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MA INTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER MODULE AND PERFORMED OPERATIONAL CHECKS. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT TOOO11AT 2001040400085 20010404 00085 CE 2001 4 4 GLBA2001049 1 20010302 A 3520 OXYGEN MASK BEECH 1900 1900D 1154162 CE CABIN DEPLOYED A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 01 195GL UE195 PASSENGER O2 MASK DEPLOYED INFLIGHT. RESECURED MASK, OPS CHECKED SYSTEM GOOD. 2 L 7 2 4T RT A24CE 2001040400086 20010404 00086 2001 4 4 C2XA01CL045 4 20010228 A 2330 SPEAKER AEROSP ATR42 ATR42320 8680930 EU CABIN SPARKS A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 42836 200 CLE FLIGHT 3813 THE CREW REPORTED THE F/A SAW SPARKS COMING FROM THE SPEAKER GRILL WHILE TAXIING. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED BY REMOVING THE GRILL OF THE SPEAKER AND LOOKING AT ASSOCI ATED COMPONENTS. THERE WAS NO EVIDENCE OF SPARKS OR BURNING NOTED. THE COVER WAS REINSTALLED AND THE AIRCRAFT WAS RELE ASED FOR SERVICE. 2 H 7 2 4T RT A53EU 2001040400087 20010404 00087 EU 2001 4 4 C2XA01CL046 1 20010304 A 3230 C245890002 UPLOCK AEROSP ATR42 ATR42320 8680930 EU RT MLG FAILED A C2XA K NONE J WARNING INDICATION CL CLIMB 1 SW 27 34817 13208 152 CLE FLIGHT 3191 THE CREW REPORTED AFTER TAKEOFF HAD TO CYCLE THE GEAR NUMEROUS TIMES BEFORE THE RIGHT MAIN GEAR WOULD UP LOCK. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN GEAR UPLOCK BOX. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A53EU 2001040400088 20010404 00088 WP 2001 4 4 MWEA020228 1 20010306 A 5347 5910143 SEAT TRACK DOUG DC9 DC914 3022034 WP CABIN GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 NR 2 SEAT TRACK IS SCRATCHED AT STATION 620, ALSO A DEEP GOUGE IN OUTBOARD FLANGE. BLENDED SCRATCHES, TRIMMED OUT NR 2 SEAT TRACK, LOCATED HOLE AND INSTALLED PLUG AND CHANNEL. 2 L 7 2 4F A6WE 2001040400089 20010404 00089 WP 2001 4 4 MWEA010229 1 20010306 A 5310 2912538 SHEAR TIE DOUG DC9 DC914 3022034 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 SHEAR TIE AT STATION 256 LONGERON 8 LEFT WAS CUT TO ACCOMADATE LONGERON AND FRAME REPAIRS. REMOVED SHEAR TIE, FABRICATE D AND INSTALLED REPAIR SPLICE. 2 L 7 2 4F A6WE 2001040400090 20010404 00090 WP 2001 4 4 MWEA010230 1 20010306 A 5330 5911412 SKIN DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FUSELAGE SKIN UNDER FAIRING RIB HAS LIGHT CORROSION STATION 465 BETWEEN LONGERON 23-24 LEFT. REMOVED CORROSION, FABRICA TED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001040400091 20010404 00091 WP 2001 4 4 MWEA010231 1 20010306 A 5313 2777922 LONGERON DOUG DC9 DC914 3022034 WP FUSELAGE TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 LONGERON 10 RIGHT HAS TOOL DAMAGE AT STATION 222. REMOVED, FABRICATED AND INSTALLED LONGERON. 2 L 7 2 4F A6WE 2001040400092 20010404 00092 WP 2001 4 4 MWEA010232 1 20010306 A 5313 2777922 LONGERON DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 LONGERON 10 RIGHT HAS A CRACK AT STATION 236. REMOVED LONGERON SECTION, FABRICATED AND DRILLED UP LONGERON AND SPLICE, INSTALLED LONGERON. 2 L 7 2 4F A6WE 2001040400093 20010404 00093 WP 2001 4 4 MWEA010233 1 20010306 A 5313 2912727 LONGERON DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FORWARD CARGO COMPARMENT LONGERON 28 LEFT HAS ONE RIVET TAIL NOT FILLING HOLE AND CORROSION AROUND THREE OTHERS BETWEEN STATION 275 AND 294. REMOVED DAMAGED AREA, FABRICATED, LOCATED AND INSTALLED LONGERON AND SPLICES. 2 L 7 2 4F A6WE 2001040400094 20010404 00094 WP 2001 4 4 MWEA010234 1 20010306 A 5310 995791718 SHEAR TIE DOUG DC9 DC914 3022034 WP FUSELAGE TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 TOOL DAMAGE IN RADIUS OF SHEAR TIE STATION 758, LONGERON 14 RIGHT. FABRICATED AND INSTALLED T-FORMER. 2 L 7 2 4F A6WE 2001040400095 20010404 00095 WP 2001 4 4 MWEA010235 1 20010306 A 5311 99579177 FRAME DOUG DC9 DC914 3022034 WP FUSELAGE TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 TOOL MARKS AROUND FASTENER, STATION 756, LONGERON 10 RIGHT. FABRICATED AND INSTALLED FRAME, LOCATED, DRILLED AND INSTAL LED STRAP. 2 L 7 2 4F A6WE 2001040400096 20010404 00096 WP 2001 4 4 MWEA010236 1 20010306 A 5242 9911547 DOOR DOUG DC9 DC914 3022034 WP E&E BAY CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 E&E DOOR HAS MODERATE CORROSION AROUND A BN FASTENER (ON INSIDE) AFT OF THE AFT LATCH PIN. REMOVED BN FASTENER, CLEANED CORROSION. FOUND CRACK RADIATING FROM FASTENER HOLES. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001040400097 20010404 00097 WP 2001 4 4 MWEA010238 1 20010306 A 5313 2777922 LONGERON DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 AFT CARGO BAY LONGERON 28 LEFT HAS AREAS OF LIGHT CORROSION STATION 748-800. REMOVED LONGERON SECTION, FABRICATED AND I NSTALLED LONGERON AND REPAIR SPLICE. 2 L 7 2 4F A6WE 2001040400098 20010404 00098 WP 2001 4 4 MWEA010239 1 20010306 A 5347 5910143 SEAT TRACK DOUG DC9 DC914 3022034 WP CABIN CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 CORROSION ON TOP OF NR 3 SEAT TRACK, ALSO AROUND FASTENER HOLES ON BOTTOM OF SEAT TRACK SEEN WITH MIRROR TAGGED FROM STA TION 200 TO 237. REMOVED SEAT TRACK SECTION, FABRICATED AND INSTALLED REPAIR PARTS AND SEAT TRACK. 2 L 7 2 4F A6WE 2001040400099 20010404 00099 WP 2001 4 4 MWEA010240 1 20010306 A 5311 99581961 FRAME DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 FRAME AT STATION 484 BELOW LONGERON 11 LEFT HAS ONE MISDRILLED HOLE. DRILLED HOLE IN FRAME FOR BUSHING AND INSTALLED BU SHING. 2 L 7 2 4F A6WE 2001040400100 20010404 00100 WP 2001 4 4 MWEA010241 1 20010306 A 5320 9915571 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 MISDRILLED HOLES ON INTERCOSTAL, LONGERON 9 LEFT BETWEEN STATION 218 AND 237, FORWARD AND AFT SIDE OF INTERCOSTAL. REMO VED, FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001040400101 20010404 00101 WP 2001 4 4 MWEA010242 1 20010306 A 5311 2777930 FRAME DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 FASTENERS WITH NO SPACING AND TWO MISDRILLED HOLES AT FRAME STATION 237 BETWEEN LONGERON 9 LEFT AND 10 LEFT. CUT OUT DA MAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLE, SPLICE PLATE AND FILLER. 2 L 7 2 4F A6WE 2001040400102 20010404 00102 WP 2001 4 4 MWEA010243 1 20010306 A 5330 5911416 SKIN DOUG DC9 DC914 3022034 WP FUSELAGE CANNING A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 OIL CANNING DENT AT STATION 446 - 465 BETWEEN LONGERON 16 AND 17 RIGHT. REMOVED AREA, FABRICATED AND INSTALLED DOUBLER AND FINGER DOUBLER. 2 L 7 2 4F A6WE 2001040400103 20010404 00103 WP 2001 4 4 MWEA010244 1 20010306 A 5240 5910084 WEB DOUG DC9 DC914 3022034 WP SERVICE DOOR MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 GALLEY SERVICE DOOR WEB STATION 176 TO 194, 21.5 HAS RIVET HOLES WITH INCORRECT PITCH DISTANCE IN SEVERAL PLACES. FABRI CATED, LOCATED AND DRILLED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001040400104 20010404 00104 WP 2001 4 4 MWEA010254 1 20010306 A 5520 59107412 STRUCTURE DOUG DC9 DC914 3022034 WP LT ELEVATOR TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 LEFT ELEVATOR AT STATION XE 14.5 HAS A SMALL AREA OF TOOL MARKS. VIEWED THROUGH PANEL ACCESS 3503. FABRICATED AND INST ALLED DOUBLERS. 2 L 7 2 4F A6WE 2001040400105 20010404 00105 WP 2001 4 4 MWEA010249 1 20010306 A 5210 591412115 ATTACH ANGLE DOUG DC9 DC914 3022034 WP PAX DOOR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 LOWER FORWARD PAN ATTACH ANGLE ON PAX DOOR HAS AREAS OF DAMAGE. REMOVED, FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F A6WE 2001040400106 20010404 00106 WP 2001 4 4 MWEA010250 1 20010306 A 5330 5911408 SKIN DOUG DC9 DC914 3022034 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FUSELAGE LEFT SIDE HAS A DENT AT STATION 470 AND LONGERON 16 LEFT. REMOVED DENT, FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001040400107 20010404 00107 WP 2001 4 4 MWEA010251 1 20010306 A 5313 27779225 LONGERON DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 AFT CARGO BAY LONGERON 28 UNDER SPLICE AFT SIDE IS CORRODED. REMOVED LONGERON SECTION, LOCATED, DRILLED AND INSTALLED L ONGERON AND SPLICE. 2 L 7 2 4F A6WE 2001040400108 20010404 00108 WP 2001 4 4 MWEA010252 1 20010306 A 5710 99116073 FRAME DOUG DC9 DC914 3022034 WP LT WING TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 LEFT WING FRAME AT STATION 137 INBOARD SIDE HAS TOOL MARKS BY THE FASTENER HOLES FOR THE HOURGLASS STIFFENER. FABRICATE D AND INSTALLED FILLER AND DOUBLER. 2 L 7 2 4F A6WE 2001040400109 20010404 00109 WP 2001 4 4 MWEA010253 1 20010306 A 5320 2912901 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE MISALIGNED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 INTERCOSTAL AT LONGERON 8 RIGHT, FROM STATION 556 - 544 DOES NOT LINE-UP CORRECTLY DUE TO LONGERON REPAIR. REMOVED, FAB RICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001040400110 20010404 00110 WP 2001 4 4 MWEA010255 1 20010306 A 5347 B060151 SEAT TRACK DOUG DC9 DC914 3022034 WP CABIN CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 STATION 642 TO 661, NR 3 FLOOR TRACK HAS CORROSION IN SEAT TRACK. REMOVED CORROSION, FABRICATED, LOCATED AND INSTALLED SEAT TRACK AND SPLICE. 2 L 7 2 4F A6WE 2001040400111 20010404 00111 WP 2001 4 4 MWEA010256 1 20010306 A 5347 5910143 SEAT TRACK DOUG DC9 DC914 3022034 WP CABIN CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 NR 4 SEAT TRACK BETWEEN STATION 237 - 251 HAS LIGHT CORROSION PRESENT UNDER CLIP NUTS TOP OR BOTTOM SIDE. BLENDED CORRO SION, REMOVED DAMAGED SEAT TRACK, LOCATED, DRILLED AND INSTALLED SEAT TRACK. 2 L 7 2 4F A6WE 2001040400112 20010404 00112 WP 2001 4 4 MWEA010257 1 20010306 A 5311 95300953 FRAME DOUG DC9 DC914 3022034 WP FUSELAGE TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 TOOL DAMAGE IN RADIUS OF FRAME, STATION 737, LONGERON 15 RIGHT. FABRICATED, LOCATED, DRILLED AND INSTALLED REPAIR DOUBL ER. 2 L 7 2 4F A6WE 2001040400113 20010404 00113 WP 2001 4 4 MWEA010258 1 20010306 A 5310 J06011930 SHEAR TIE DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 SHEAR TIE CRACKED, STATION 786, BELOW LONGERON 14 RIGHT. REMOVED DAMAGED SHEAR TIE, POSITIONED, DRILLED AND INSTALLED N EW ANGLE AND SHEAR TIE. 2 L 7 2 4F A6WE 2001040400114 20010404 00114 WP 2001 4 4 MWEA010259 1 20010306 A 5210 591412161 PAN DOUG DC9 DC914 3022034 WP PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FORWARD PAX DOOR PAN IS CRACKED AT BN FASTENER AT FORWARD LOWER CORNER AB2. LOCATED, DRILLED AND INSTALLED NEW DOOR PAN SEGMENT. 2 L 7 2 4F A6WE 2001040400115 20010404 00115 WP 2001 4 4 MWEA010261 1 20010306 A 5330 5910228209 SKIN DOUG DC9 DC914 3022034 WP FUSELAGE CANNING A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FUSELAGE SKIN STATION 942 - 989 DIRECTLY AFT OF LEFT PYLON TRAILING EDGE DOWN TO FACTORY SPLICE HAS SEVERAL REPAIRS CAUS ING OIL CANNING. REMOVED, FABRICATED AND INSTALLED SKIN AND STIFFENERS. 2 L 7 2 4F A6WE 2001040400116 20010404 00116 WP 2001 4 4 MWEA010262 1 20010306 A 5320 2912901 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 TOOLING MARKS ON RADIUS OF INTERCOSTAL LOCATED AT LONGERON 15 LEFT BETWEEN STATION 585 AND 566. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001040400117 20010404 00117 WP 2001 4 4 MWEA010263 1 20010306 A 5330 591022817 SKIN DOUG DC9 DC914 3022034 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 DENT IN UNPRESSUIRZED FUSELAGE SKIN BETWEEN CANTED FRAMES 953.604 AND 964.019 AT APPROXIMATELY LONGERON 22 RIGHT AREA (2 1 INCH BELOW PYLON) D=2 INCHES, X=.060, D/X=33.34. FABRICATED AND INSTALLED REPAIR SKIN. 2 L 7 2 4F A6WE 2001040400118 20010404 00118 WP 2001 4 4 MWEA010264 1 20010306 A 5330 591022817 SKIN DOUG DC9 DC914 3022034 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 DENT IN UNPRESSURIZED FUSELAGE SKIN BETWEEN CANTED FRAMES 953.604 AND 964.019 AT APPROXIMATELY LONGERON 22 RIGHT AREA. ( 26 INCHES BELOW PYLON) D=1 INCH, X=.055, D/X=18.19. FABRICATED AND INSTALLED REPAIR SKIN. 2 L 7 2 4F A6WE 2001040400119 20010404 00119 WP 2001 4 4 MWEA010265 1 20010306 A 5330 591022817 SKIN DOUG DC9 DC914 3022034 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FUSELAGE SKIN LEFT SIDE HAS A DENT AT STATION 964 CANTED FRAME AREA AND 8 INCHES FORWARD OF LEFT LOUVER VENT DRAIN. FAB RICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001040400120 20010404 00120 WP 2001 4 4 MWEA010266 1 20010306 A 5310 5910132 SHEAR TIE DOUG DC9 DC914 3022034 WP FUSELAGE BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 SHEAR TIE BENT AT STATION 351 LONGERON 29-30 RIGHT. REMOVED FRAME REPAIR AND SHEAR TIE, FABRICATED SHEAR TIE, INSTALLED SHEAR TIE AND FRAME REPAIR. 2 L 7 2 4F A6WE 2001040400121 20010404 00121 WP 2001 4 4 MWEA010267 1 20010306 A 5330 5911409 SKIN DOUG DC9 DC914 3022034 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FUSELAGE LEFT SIDE HAS A DENT AT STATION 246 AND 2 INCHES ABOVE LONGERON 19 LEFT. FABRICATED, DRILLED AND INSTALLED REP AIR DOUBLER. 2 L 7 2 4F A6WE 2001040400122 20010404 00122 WP 2001 4 4 MWEA010268 1 20010306 A 5330 5911412 SKIN DOUG DC9 DC914 3022034 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 DENT IN FUSELAGE SKIN AT STATION 351 - 355 BETWEEN LONGERON 30 AND 29 RIGHT, SHEAR CLIP SUPPORTING THIS AREA IS BENT. F ABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001040400123 20010404 00123 WP 2001 4 4 MWEA010260 1 20010306 A 5313 27779235 LONGERON DOUG DC9 DC914 3022034 WP FUSELAGE TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 TOOLING MARKS ON LONGERON 11 LEFT, FORWARD OF STATION 503. FABRICATED LONGERON AND INSTALLED LONGERON AND SPLICE. 2 L 7 2 4F A6WE 2001040400124 20010404 00124 WP 2001 4 4 MWEA010269 1 20010306 A 5330 5911411 SKIN DOUG DC9 DC914 3022034 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 CREASE IN FUSELAGE SKIN AT STATION 369-388 ON LONGERON 24 RIGHT. TOTAL LENGTH 19 INCHES D=1.4, A=.041, B=.002, X=.0438, D/X=31.92. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001040400125 20010404 00125 WP 2001 4 4 MWEA010270 1 20010306 A 5330 5911409 SKIN DOUG DC9 DC914 3022034 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FUSELAGE LEFT SIDE HAS A DENT AT STATION 239 AND 3 INCHES BELOW LONGERON 17 LEFT. FABRICATED, DRILLED AND INSTALLED REP AIR DOUBLER. 2 L 7 2 4F A6WE 2001040400126 20010404 00126 WP 2001 4 4 MWEA010271 1 20010306 A 5330 5911432 SKIN DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FUSELAGE OUTER SKIN IS CRACKED IN 3 PLACES AT CANTED STATION 895. ONE CRACK IS BETWEEN LONGERON 3 & 4 LEFT AND 2 CRACKS ARE BETWEEN LONGERON 4 & 5 LEFT. FABRICATED, DRILLED, LOCATED AND INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001040400127 20010404 00127 WP 2001 4 4 MWEA010272 1 20010306 A 5330 5911432 SKIN DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FUSELAGE OUTER SKIN IS CRACKED AT CANTED STATION 895. ONE CRACK IS BETWEEN LONGERON 3 & 4 RIGHT AND ONE CRACK IS BETWEE N LONGERON 4 & 5 RIGHT. FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 2001040400128 20010404 00128 WP 2001 4 4 MWEA010273 1 20010306 A 5330 59114015 SKIN DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 HEAVY CORROSION IN E&E COMPARTMENT FLOOR MARKER BEACON ANTENNA, BETWEEN FUSELAGE SKIN AND INTERNAL DOUBLER, FORWARD END, APPROXIMATELY STATION 180 LONGERON 29 LEFT TO 30. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED DOUBLERS AND FILLER. 2 L 7 2 4F A6WE 2001040400129 20010404 00129 WP 2001 4 4 TWAA0104201 1 20010301 A 5320 CLIP DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 928TW 48012 DURING CHECK-C MAINT ON RT INTERCOSTAL CLIP AT LONGERON 15R, STA 1003, FOUND CORROSION. REMOVED CORROSION PER SPM 6-80- 01. TREATED AND PRIMED AREA PER SRM 51-10-3. INSTALLED AND SEALED NEW T-CLIP WITH HI-LOKS PER SRM 51-30-5. 2 L 7 2 4F A6WE 2001040400130 20010404 00130 WP 2001 4 4 TWAA0104202 1 20010301 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 928TW 48012 DURING CHECK-C MAINT FOUND CORROSION ON FORMER FRAME AT STA 1212, LONGERON 18R. REMOVED CORROSION PER SPM 6-80-01. REP LACED FASTENERS PER SRM 51-01. 2 L 7 2 4F A6WE 2001040400131 20010404 00131 GL 2001 4 4 RAIA00103003 2 20010303 A 7200 AE3007A ENGINE EMB 145 EMB145 SO ALLSN AE300 AE3007A GL NR 1 ENGINE FAILED A RAIA O OTHER Y ENGINE STOPPAGE CR CRUISE 1 CE 03 807HK 3742 3742 145119 310165 5285-IAD- DURING CRUISE NR 1 ENGINE SHUT DOWN IN FLIGHT. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE IAW EMB145 MAINTE NANCE MANUAL. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001040400132 20010404 00132 EA 2001 4 4 JBXA000252 1 20010304 A 3010 601R5120333 CONTROL PANEL CNDAIR CL600 CL6002B19 EA COCKPIT DEFECTIVE A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 583ML 7327 WING OVERHEAT IN FLT RIGHT WING. REMOVED AND REPLACED ANTI ICE CONTROL PANEL IAW CL-65 AMM 30-12-21. TEST FLEW A/C, CH ECKED GOOD IN FLT. 2 L 7 2 4F RT A21EA 2001040400133 20010404 00133 2001 4 4 DHL2001720008 4 20010307 A 3425 2588369905 ADI BOEING 727 727228 NM COCKPIT FAILED A DHLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 720DH 19544 FIRST OFFICER VERT GYRO FAILED DURING TAXI OUT FOR TAKEOFF ATT FLAG ALSO NOTED. REMOVED AND REPLACED NR 2 INST AMP AND ADI INSTRUMENT, OPS CK GOOD MM 34-62-21, 34-62-61. 2 L 7 3 4F A3WE 2001040400134 20010404 00134 NM 2001 4 4 SWAA010645 1 20010303 A 3610 107484 REGULATOR BOEING 737 7377H4 NM NR 1 ENGINE INOPERATIVE A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 716SW 27850 AIR TURNBACK. AFTER TAKEOFF, NR 1 ENG PNEUMATIC BLEED C/B TRIPPED. WOULD NOT RESET ON FIRST ATTEMPT AND BLEED AIR PRES S NOT STABLE. REMOVED AND REPLACED NR 1 PNEUMATIC HIGH STAGE REGULATOR PER MM. 2 L 7 2 4F RT A16WE 2001040400135 20010404 00135 2001 4 4 SWAA010646 4 20010304 A 2565 6557463 BRACKET BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 AFT ENTRY DOOR EMERGENCY EVAC SLIDE ASSY WOULD NOT ARM. ADJUSTED GIRT BRACKET ASSY PER MM. 2 L 7 2 4F RT A16WE 2001040400136 20010404 00136 NM 2001 4 4 SWAA010647 1 20010304 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 386SW 26601 TWO EEPLS TRACK COVERS MISSING. INSTALLED TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 2001040400137 20010404 00137 NM 2001 4 4 SWAA010649 1 20010304 A 5310 6546569 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED AT BS 967, LBL 3. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2001040400138 20010404 00138 NM 2001 4 4 SWAA010650 1 20010305 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 396SW 27690 EEPLS TRACK COVER MISSING. INSTALLED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001040400139 20010404 00139 NM 2001 4 4 SWAA010651 1 20010305 A 3350 BR2013 LENS BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 639SW 27712 EEPLS RED TRACK COVER LENS BROKEN. REMOVED AND REPLACED TRACK COVER LENS PER MM. 2 L 7 2 4F RT A16WE 2001040400140 20010404 00140 2001 4 4 SWAA010652 4 20010303 A 2565 D31354 SLIDE BOEING 737 737317 138447P NM SERVICE DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 AFT SVC DOOR EMERGENCY EVAC SLIDE ASSY LOOSE. SECURED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001040400141 20010404 00141 NM 2001 4 4 SWAA010653 1 20010305 A 5754 6546423 SKIN BOEING 737 7372H4 138448C NM SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED SERVICE CHECK, FOUND NR 4 L/E SLAT DELAMINATED AT INBOARD UPPER T/E. REMOVED AND REPLACED NR 4 SLAT P ER MM. 2 L 7 2 4F A16WE 2001040400142 20010404 00142 NM 2001 4 4 SWAA010654 1 20010305 A 5315 6545808 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 294, RBL 52. REPAIRED FLOORBEAM WEB PER SRM. 2 L 7 2 4F A16WE 2001040400143 20010404 00143 NM 2001 4 4 SWAA010655 1 20010305 A 5320 6551698 SPLICE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND STR 4R SPLICE CRACKED AT BS 908. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F A16WE 2001040400144 20010404 00144 2001 4 4 SWAA010656 4 20010305 A 2565 D31354 INDICATOR BOEING 737 7372T4 1384492 NM EVAC SLIDE OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLID E ASSY PER MM. 2 L 7 2 4F A16WE 2001040400145 20010404 00145 NM 2001 4 4 SWAA010657 1 20010305 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM MLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 608SW 27928 DURING SCHEDULED C3 CHECK, FOUND 4 KEEL BEAM SKIN CRACK AT BS 700, WL 148.5, ADJACENT TO PREVIOUS REPAIR. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 2001040400146 20010404 00146 2001 4 4 SWAA010658 4 20010305 A 2565 D31354 INDICATOR BOEING 737 7373H4 1384600 NM EVAC SLIDE OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 608SW 27928 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001040400147 20010404 00147 NM 2001 4 4 SWAA010659 1 20010305 A 5712 BAC1520 RIB BOEING 737 7373Q8 1384670 NM LT&RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED D-CHECK, FOUND LT AND RT WING RIB LOWER CHORDS CRACKED AT WBL 135.5, BETWEEN STR 2 AND 3. REPAIRED LOW ER CHORDS PER BFG ER''S. 2 L 7 2 4F RT A16WE 2001040400148 20010404 00148 NM 2001 4 4 SWAA010660 1 20010304 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 524SW 26566 DURING SCHEDULED C4 CHECK, FOUND EEPLS INOP FROM ROW 19 AFT. SECURED CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 2001040400149 20010404 00149 NM 2001 4 4 SWAA010661 1 20010304 A 5512 65C25727 SKIN BOEING 737 7375H4 138449D NM LT HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 524SW 26566 DURING SCHEDULED C4 CHECK, FOUND LT HORIZ STAB SKIN CRACK 3 LONG, 37 OUTBOARD OF FUSELAGE AT AFT SPAR FASTENER ROW. REP AIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001040400150 20010404 00150 NM 2001 4 4 SWAA010662 1 20010305 A 5720 6552235 FITTING BOEING 737 7373Q8 1384670 NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED D-CHECK, FOUND LT WING STABILIZER BEAM FITTING CORRODED ON REAR SPAR CHORD. REMOVED AND REPLACED BEAM FITTING PER MM. 2 L 7 2 4F RT A16WE 2001040400151 20010404 00151 NM 2001 4 4 SWAA010663 1 20010305 A 7120 310A102014 MOUNT BOEING 737 7373H4 1384600 NM NR 1 ENGINE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 646SW 28331 DURING SCHEDULED SERVICE CHECK, FOUND NR 1 ENGINE AFT MOUNT CORRODED. REMOVED AND REPLACED AFT ENGINE MOUNT PER MM. 2 L 7 2 4F RT A16WE 2001040400152 20010404 00152 NM 2001 4 4 SWAA010664 1 20010304 A 5754 65C26686 WEDGE BOEING 737 7373A4 1384585 NM SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 345SA 23786 DURING SCHEDULED C4 CHECK, FOUND NR 4 L/E SLAT INBOARD AND NR 5 L/E SLAT OUTBOARD T/E WEDGES DELAMINATED. REPAIRED WEDG ES PER SRM. 2 L 7 2 4F RT A16WE 2001040400153 20010404 00153 NM 2001 4 4 VNAA0103007 1 20010303 A 2897 191311000 COAX DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FUEL SYSTEM IND DEFECTIVE A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 440JS 3058 DURING REPOSITION FLIGHT 9405 GSP-ELM THE FLIGHT CREW RECEIVED A RIGHT FUEL QUANTITY FAIL AND LEFT FUEL LOW FAIL WARNING MESSAGES. THE FLIGHT CREW DIVERTED TO PIT WHERE A NORMAL LANDING WAS MADE. MAINTENANCE INSPECTED AND REPLACED THE COA XIAL CABLE REDUCER IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 28-23-10. OPERATIONAL CHECKS WERE COMPLETED AND THE AI RCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001040400154 20010404 00154 NM 2001 4 4 VNAA0103006 1 20010305 A 2931 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT ACTIVATED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 430JS 3044 DURING CLIMBOUT THE FLIGHT CREW RECEIVED A EMERGENCY PARKING BRAKE ACCUMULATOR PRESSURE WARNING MESSAGE. THE FLIGHT CRE W FOLLOWED THE QUICK REFERENCE HANDBOOK PROCEDURES TO EXTINGUISH THE MESSAGE BUT IT REAPPEARED. THE FLIGHT CREW RETURNE D TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND OPERATIONALLY CHECKED THE EMERGENCY PARKING BRAKE IN ACCORDANCE WITH DORNIER MAINTENANCE 29-21-05, OPERATIONAL CHECK WAS COMPLETED AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001040400155 20010404 00155 NM 2001 4 4 VNAA0103005 1 20010303 A 3397 WIRE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DAMAGED A VNAA O OTHER L NO TEST NR NOT REPORTED 1 GL 07 457PS 3048 THE FLIGHT CREW FOUND THE SERVICE DOOR EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. THE AIRCRAFT WAS FERRIED TO PIT WHERE MAINTENANCE REPAIRED THE EXIT LIGHT WIRES IN ACCORDANCE WITH DORNIER WIRING MANUAL 33-51-00. OPERATIONAL CHECKS WERE C OMPLETED AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001040400156 20010404 00156 WP 2001 4 4 MWEA010275 1 20010307 A 5313 2777922 LONGERON DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 LONGERON 8 LEFT, STATION 256 HAS DOUBLE HOLES IN FLANGE. REMOVED, FABRICATED AND INSTALLED LONGERON SECTION AND SPLICE REPAIR. 2 L 7 2 4F A6WE 2001040400157 20010404 00157 WP 2001 4 4 MWEA010276 1 20010307 A 5320 99579103 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 FORWARD CARGO COMPARTMENT, INTERCOSTAL AT LONGERON 29 RIGHT HAS TWO MISDRILLED HOLES UNDER GUSSET JUST FORWARD OF FRAME, STATION 389. LOCATED, DRILLED AND INSTALLED NEW INTERCOSTAL. 2 L 7 2 4F A6WE 2001040400158 20010404 00158 WP 2001 4 4 MWEA010277 1 20010307 A 5320 99576814 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 INTERCOSTAL AT LONGERON 9 RIGHT BETWEEN STATION 465 AND 484 HAS 3 MISDRILLED HOLES AND 2 IMPROPERLY PLUGGED HOLES. REMO VED, FABRICATED, LOCATED, DRILLED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001040400159 20010404 00159 WP 2001 4 4 MWEA010278 1 20010307 A 5320 99576783 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 INTERCOSTAL AT LONGERON 10 LEFT BETWEEN STATION 465 AND 484 HAS AN IMPROPER REPAIR. FABRICATED, LOCATED, DRILLED AND IN STALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001040400160 20010404 00160 WP 2001 4 4 MWEA010279 1 20010307 A 5330 5911416 SKIN DOUG DC9 DC914 3022034 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FUSELAGE LEFT SIDE HAS A DENT AT STATION 553 AND 5 INCHES ABOVE CUSP LINE. CUT OUT DAMAGE, LOCATED, FABRICATED, DRILLED AND INSTALLED DOUBLERS AND FILLERS. 2 L 7 2 4F A6WE 2001040400161 20010404 00161 2001 4 4 MWEA010280 4 20010307 A 2565 13621229 COVER DOUG DC9 DC914 3022034 WP TAILCONE DEFECTIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 800ME 45842 TAIL CONE SLIDE COVER DID NOT COME OFF PER WORK CARD FOR TAIL CONE DROP. REMOVED AND REPLACED TAIL CONE SLIDE COVER AND TAIL CONE SLIDE. 2 L 7 2 4F A6WE 2001040400162 20010404 00162 EU 2001 4 4 MALA010253 1 20010224 A 7933 4053T73P01 DETECTOR SAAB SF340 SF340A 7850100 EU RT ENGINE DEFECTIVE A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 48XJ 048 RT ENGINE OIL TEMPERATURE GAUGE READING HIGH END OF YELLOW ARC ALL OTHER INDICATIONS NORMAL. AIR TURNBACK TO DTW. MAIN TENANCE REMOVED AND REPLACED RT OIL TEMP DETECTOR IAW GE MM CHAP 79. PERFORMED GROUND RUNS AT VARIOUS POWER SETTINGS. ALL INDICATIONS GOOD. P/N 4053T73PO1, S/N ON EGNAB470. LEAK CHECK GOOD. 2 L 7 2 4T RT A52EU 2001040400163 20010404 00163 EU 2001 4 4 MALA010254 1 20010228 A 7722 523402 INDICATOR SAAB SF340 340B 7860101 EU COCKPIT DEFECTIVE A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 430XJ 430 DURING FLIGHT 3372 NOTED 46 DEGREE DELTA T SHIFT DURING TREND. CREW FOLLOWED ORH AND AVOIDED BOTH 80 - 84 PERCENT NG AN D 95 - 98 PERCENT NG FOR REMAINDER OF FLIGHT. AIR RETURN TO MSP. MAINTENANCE FOUND T4.5 TRIMMER AND ITT GAUGE READING INCORRECTLY. REPLACED TRIMMER P/N 4078T09P02, S/N ON GDB02 TIE AND ITT GAUGE P/N 523402, S/N ON 02890005, OPS CHECK GOO D. NEW TREND DATA NEEDS TAPE ACCOMPLISHED USING NEW GPA REF NR 409, 088498 FOR FURTHER DETAILS. 2 L 7 2 4T RT A52EU 2001040400164 20010404 00164 EU 2001 4 4 MALA010255 1 20010226 A 2840 INDICATOR BAC 146 AVRO146RJ85A 1500097 EU COCKPIT INOPERATIVE A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 512XJ E2328 CENTER FUEL TANK OTY IND INOP. CREW THOUGHT THEY WERE USING MORE FUEL THAN THEY WERE. THE FUEL GAUGE CENTER TANK GAVE ERRONEOUS INFORMATION 4600165 ERROR. DEFER CENTER TANK FUEL GAUGE PER MEL 28-40 (C) ENTERED INTO DMR. MAINTENANCE NOTI FIED NR 3822. MAINTENANCE REPLACED EDP, OPS CHECKED GOOD. EDP P/N 322EDP2-1, S/N ON HV2149, S/N OFF HV27681. 2 H 7 4 4F RT A49EU 2001040400165 20010404 00165 EU 2001 4 4 MALA010256 1 20010227 A 3260 UPLOCK SWITCH SAAB SF340 SF340A 7850100 EU LT MLG OUT OF ADJ A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 327XJ 059 ON FLIGHT 2926 ON GEAR RETRACTION INTRANSIT LIGHT STAYS ILLUMINATED AND HYDRAULIC PUMP RUNS. AIR RETURN TO MSP. MAINTE NANCE FOUND LT GEAR UPLOCK SWITCH NOT MAKING CONTACT. FOUND LEFT GEAR DOORS OUT OF ADJUSTMENT. ADJUSTED LT GEAR DOORS IAW 32-12-15. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2001040400166 20010404 00166 GL 2001 4 4 01FDEA00176 2 20010306 A 7200 ENGINE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 2 ENGINE FIRE A FDEA F D ACTIVATE FIRE EXT. RETURN TO BLOCK A J FLAME/FIRE WARNING INDICATION TO TAKEOFF 1 SO 25 375FE 46613 451336 NR 2 ENGINE FIRE ON T/O. FIRED FIRE BOTTLES. 2 L 7 3 4F 4 F A22WE E23EA 2001040400169 20010404 00169 SO 2001 4 4 C2XA01CL047 1 20010305 A 4900 APU EMB 135 EMB135LR SO APU BAY FAILED A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 27 14514 145303 CLE FLIGHT 3683 THE CREW REPORTED THE APU FAILED IN FLIGHT. ATTEMPTED RESTART BUT IT WOULD NOT CONTINUE TO RUN. MAINTE NANCE PERFORMED OPERATIONAL CHECKS ON APU AND NO DEFECTS WERE NOTED. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RE LEASED FOR SERVICE. 2 L 7 2 4F RT TOOO11AT 2001040400170 20010404 00170 2001 4 4 RAIA00103004 4 20010306 A 3425 HG2010AC02 COMPUTER EMB 145 EMB145ER SO EE BAY FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 803HK 5443 5443 145077 7628-STL- DURING TAXI OUT PILOTS RECEIVED EFIS COMPUTER WARNING, HEADINGS FLAGGED AND HEADINGS WERE OF BY 5 TO 12 DEGREE S. MAINTENANCE REMOVED AND REPLACED NR 1 AHRS COMPUTER IAW EMB145 MAINTENANCE MANUAL. 2 L 7 2 4F RT T00011AT 2001040400171 20010404 00171 SO 2001 4 4 RAIA00103005 1 20010306 A 3250 12302328403 CONTROL HANDLE EMB 145 EMB145LR SO COCKPIT FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 802HK 5275 5275 145066 7626-XNA- DURING TAXI OUT NOSE WHEEL STEERING FAILED. MAINTENANCE REMOVED AND REPLACED THE NOSE WHEEL STEERING CONTROL KNOB IAW EMB145 MAINTENANCE MANUAL. 2 L 7 2 4T RT T00011AT 2001040400174 20010404 00174 NM 2001 4 4 2001UALA00081 1 20010203 A 2530 CA709 CART BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE GALLEY SHORTED A UALA H DEACTIVATE SYST/CIRCUITS A FLAME/FIRE CR CRUISE 1 WP 29 614UA 0 0 21875 ENTRY CART 300 IN MID-GALLEY SPARKED WHEN PLUGGED IN AND THE 60 AMP AC CB POPPED. OK AT FIRST SERVICE OF FLIGHT. LEFT U NPLUGGED AND DID NOT RESET. *S/D* CART CONTROL PANEL HAD SHORT TO GROUND. TAGGED CART AND NOTIFIED DOBBS FOOD SERVICE . RESET 15 AMP CIRCUIT BREAKER NUMBER 60. OPS CHECK NORMAL ON NEW CART. 2 L 7 2 4F 4 F RT A1NM E3NE 2001040400179 20010404 00179 NM 2001 4 4 2001UALA00120 1 20010217 A 2910 840002074 FILTER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HYD SYSTEM LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 384UA 24659 LOSS OF THE B-SYSTEM HYDRAULICS. *S/D* REPLACED B-SYSTEM ACOUSTIC FILTER AND ASSOCIATED O-RING, AND SERVICED B-SYSTEM HYDRAULICS. NO FURTHER LEAKS EVIDENT. 2 L 7 2 4F 4 F RT A16WE E2GL 2001040400180 20010404 00180 NM 2001 4 4 2001UALA00123 1 20010215 A 4920 6957531 BEARING BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE APU CRACKED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7275U 8577 8577 21422 APU SMOKE IN CABIN. *S/D* APU WAS REMOVED ON 2/17/01 DUE TO SMOKE IN CABIN. SHOP DISASSEMBLED ENGINE. DURING DISASSE MBLY OF THE NUCLEUS MODULE, FOUND BEARING CARRIER CRACKED RESULTING TO LEAKAGE PAST THE COMPRESSOR SEAL AREA CAUSING A S MELL OR SMOKE IN CABIN. 2 L 7 3 4F 4 F A3WE E2EA 2001040400181 20010404 00181 NM 2001 4 4 2001UALA00131 1 20010220 A 2916 3111794 CHECK VALVE BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE RESERVOIR RESTRICTED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 996UA 22456 RETURNED TO FIELD DUE TO LOSS OF THE B-SYSTEM HYDRAULICS. *S/D* FOUND B-SYSTEM RESERVOIR CHECK VALVE FAILED AND RESTRI CTING FLOW. REPLACED BOTH RESERVOIR CHECK VALVES. SERVICED HYDRAULICS TO FULL AND LEAKED CHECKED GOOD. 2 L 7 2 4F 4 F A16WE E2EA 2001040400182 20010404 00182 NM 2001 4 4 2001UALA00140 1 20010222 A 5270 PROXIMITY SWITCH BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE L1 DOOR FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 909UA 25009 DIVERTED DUE TO THE DOOR 1L WARNING LIGHT ILLUMINATING. *S/D* ADJUSTED GUIDE ARM, DOOR STOP PINS, AND DOOR INDICATION SWITCH. ALSO FOUND A BAD DOOR PROXIMITY SWITCH. REPLACED THE SWITCH. OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2001040400184 20010404 00184 NM 2001 4 4 2001UALA00145 1 20010216 A 5522 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT ELEVATOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7443U 21897 LEFT ELEVATOR LOWER SKIN CRACKED FROM PANEL 9312 AFT. REPAIRED PER SRM 55-20-03. 2 L 7 3 4F 4 F A3WE E2EA 2001040400185 20010404 00185 NM 2001 4 4 2001UALA00149 1 20010226 A 3397 WIRE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 821UA 944 EMERGENCY EXIT LIGHTS NOT WORKING IN ROWS 1, 2, 5, AND 6. REPLACED THE POWER SUPPLY AND REPAIRED EMERGENCY LIGHT WIRES IN ROW 1. OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2001040400186 20010404 00186 NM 2001 4 4 2001UALA00080 1 20010207 A 3610 BACC10DU350Y CLAMP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7253U 21400 NR 3 ENGINE OVERHEAT LIGHT CAME ON DURING CLIMB. RETURNED TO MIA. DECLARED AN AMBER ALERT AND LANDED OVERWEIGHT. *S/D * FOUND 2 CLAMPS LEAKING PNEUMATIC AIR FROM 6TH STAGE DUCTS. REPLACED BOTH CLAMPS. NO LEAKS FOUND. 2 L 7 3 4F 4 F A3WE E2EA 2001040400187 20010404 00187 EA 2001 4 4 CA010301006 1 20010218 A 5210 CLAMP DHAV DHC8311 DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE AIRSTAIR DOOR SLIPPED W O OTHER O OTHER TX TAXI/GRND HDL 1 CA 262 (CAN) THE FLIGHT AND GROUND CREW REPORTED THAT THE AIRSTAIR DOOR WOULD NOT CLOSE. IT WOULD NOT ENGAGE ON TO THE DOOR STO PS. MAINTENANCE INVESTIGATION REVEALED THAT THE CLAMP INSTALLED WHEN INCORPORATING MODSUM 8Q101086, SB (8052-56 REV C), HAD SLIPPED OFF THE RAIL TO WHICH IT WAS SECURED. THIS MOD IS PART OF THE REQUIREMENT FOR AIRWORTHINESS DIRECTIVE CF-200 0-19R1. THE CLAMP HAD FALLEN TO THE BOTTOM OF THE GAS STRUTS AND INTERFERED WITH THE OPERATION OF THE DOOR CLOSING MECHA NISM. THE BRACKET WAS REMOVED AND THE AIRCRAFT DEMODED. PLANNED ACTION IS TO INCORPORATE MODSUM 8Q101074, (SB 8-52-59, R EPLACEMENT OF GAS SPRINGS), WHEN THE NEW STYLE SPRINGS BECOME AVAILABLE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001040400188 20010404 00188 EA 2001 4 4 CA010301007 1 20010131 A 7603 87600516003 CABLE PW123 DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE NR 2 ENGINE DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING SCHEDULED INSPECTION OF THE NR 2 ENGINE, THE LOWER POWER CONTROL CABLE WAS FOUND TO BE BLENDED TO MAX ALLOW ABLE LIMITS IN THE AREA OF CONTACT WITH THE STEEL PULLEY JUST FORWARD OF THE FIREWALL. THE CABLE WAS REPLACED AND THE AI RCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001040400189 20010404 00189 EU 2001 4 4 CA010301008 1 20010120 A 3040 NF20216525 CONTROL PANEL BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE WINDSHIELD HEAT FAILED W O OTHER O OTHER NR NOT REPORTED 1 CA 3045 L298465 (CAN) THE FLIGHT CREW REPORTED THAT THE CAPTAINS A PANEL WINDSHIELD HEAT WAS U/S. THE WINDSHIELD WAS REPLACED AND THE AI RCRAFT WAS RETURNED TO SERVICE. 2 H 7 4 4F 4 F RT A49EU E6NE 2001040400190 20010404 00190 NM 2001 4 4 CA010301009 1 20010122 A 3232 83232036001 ROD END DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NLG BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) THE FLIGHT CREW REPORTED A LOUD NOISE FROM THE FLOOR AREA DURING FLIGHT. MAINTENANCE INVESTIGATION REVEALED A BROK EN LT NOSE LANDING GEAR AFT DOOR ACTUATING ROD. THE ROD END WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001040400191 20010404 00191 NM 2001 4 4 CA010301010 1 20010118 A 3010 3D147211 TIMER DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE DEICE SYSTEM FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) THE FLIGHT CREW REPORTED THAT THE AIRFRAME DEICE SYSTEM WAS OPERATING ERRATICALLY IN THE AUTO SLOW MODE. THE DEICE TIMER WAS REPLACED AND THE AIRCRAFT WAS ARETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001040400192 20010404 00192 NM 2001 4 4 CA010301011 1 20010217 A 2910 82950010115 TUBE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYDRAULIC SYS LEAKING W K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 CA (CAN) THE FLIGHT CREW OBSERVED HYDRAULIC FLUID LEAKING FROM THE L/H NACELLE DURING WALKAROUND. MAINTENANCE INVESTIGATION RESULTED IN REPLACEMENT OF THE NR 2 FLIGHT SPOILER UNLOADING LINE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001040400193 20010404 00193 NM 2001 4 4 CA010301012 1 20010120 A 3230 54C546349 SOLENOID VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE MLG FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA 20465 (CAN) THE FLIGHT CREW REPORTED A RED GEAR UNSAFE LIGHT ASSOCIATED WITH THE NOSE LANDING GEAR WHEN GEAR WAS SELECTED DOWN DURING APPROACH. THE CREW INITIATED AN OVERSHOOT, AND PRFORMED AN ALTERNATE EXTENSION. THE AIRCRAFT LANDED UNEVENTFULY. MAINTENANCE REPLACED A FAULTY NLG SOLENOID SEQUENCE VALVE AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001040400194 20010404 00194 2001 4 4 CA010301013 4 20010225 A 3422 HARNESS DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE RT WING CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA 30472 (CAN) WHILE INSPECTING RT OUTER WING SPAR AS PER TASK 5710/08A, CHAFING DAMAGE WAS NOTED ON THE R/H WING FLUX VALVE WIRI NG HARNESS WHERE IT PASSES THROUGH THE ORCON TAPE COVERING THE FORWARD SPAR LIGHTENING HOLES. DAMAGE LOCATION AT YW 502. 50. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001040400195 20010404 00195 EU 2001 4 4 CA010301014 1 20010225 A 2131 2783A000 CONTROLLER BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE CABIN PRESSURE FAILED W O OTHER J W WARNING INDICATION INADEQUATE Q C CR CRUISE 1 CA 12133 (CAN) DURING CRUISE FLIGHT AT FL270, THE CREW EXPERIENCED A CABIN HI ALT LIGHT. BLEED FLOW WAS INCREASED AND THE CABIN A LT DESCENDED, EXTINGUISHING THE LIGHT. MAINTENANCE INVESTIGATION REVEALED THAT THE AFT OUTFLOW VALVE WAS NOT CLOSING COM PLETELY. THE CABIN PRESSURIZATION CONTROLLER WAS REPLACED AND THE OUTFLOW VALVE OPERATED NORMALLY. THE CONTROLLER HAD BE EN REPAIRED 1059 HOURS AND 677 CYCLES PREVIOUS. 2 H 7 4 4F 4 F RT A49EU E6NE 2001040400197 20010404 00197 NE 2001 4 4 CA010301020 2 20010206 A 7200 ENGINE BOEING 737 737275C NM PWA JT8 JT8D9A 52048 NE NR 2 DAMAGED W A UNSCHED LANDING B P SMOKE/FUMES/ODORS/SPARKS NO WARNING INDICATION CL CLIMB 1 CA 49066 22136 (CAN) AT END OF TAKEOFF ROLL AND DURING INITIAL CLIMB, A CABIN ATTENDANT CALL ANNUNCIATOR COULD BE HEARD RINGING REPEATE DLY. WHEN AIRCRAFT LEVELLED OUT AT 5000 FEET, FLIGHT ATTENDANT SPOKE TO PASSENGER WHO REPORTED THAT SPARKS WERE COMING F ROM RIGHT ENGINE. CAPT WAS ADVISED BY TOWER OF REPORTS OF CINDERS FALLING FROM AN AIRCRAFT. THERE WERE NO ABNORMAL READI NGS, NR 2 ENGINE WAS KEPT ON REDUCED POWER AND RETURNED TO YOW. NR 2 ENGINE WAS REPLACED. 2001-03-06 TC: 2 L 7 2 4F 4 F A16WE E2EA 2001040400198 20010404 00198 NM 2001 4 4 CA010301028 1 20010216 A 3244 DR24321T TIRE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE MLG FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) SEPARATION OF TIRE SIDEWALL CORDS. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001040400206 20010404 00206 NM 2001 4 4 CA010302005 1 20010228 A 3232 82970018009 ACTUATOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE MLG DOOR MALFUNCTIONED W O OTHER J WARNING INDICATION AP APPROACH 1 CA (CAN) THE LT MLG FWD DOOR WOULD NOT CLOSE WHEN GEAR SELECTED UP. (NO LT AMBER - NO LT GREEN) RT & NLG PERFORMED NORMALLY .VISUAL CONFIRMATION CONDUCTED THAT DOOR OPEN. GEAR CYCLED&DOOR REMAINED OPEN AGAIN. DECISION MADE TO RETURN.AN ALT EXTE NSION CARRIED OUT & A/C LANDED W/O INCID. (NO CFR). MAINT CHANGED SEVERAL COMPONENTS FOR TROUBLESHOOTING PURPOSES BUT PR OBLEM REMAINED. LT FWD MLG DO OR ACTUATOR FOUND TO BE CAUSE OF PROBLEM. COMPONENT CHANGED, WITH SEVERAL GEAR SWINGS CARR IED OUT&ALT EXTENSIONS COMPLETED. FUNCTION & LEAK CHECKED AS SERVICEABLE. A/C RETURNED TO SERVICE WITH NO FURTHER INCID. S TO RPT. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001040400214 20010404 00214 SW 2001 4 4 CA010305005 1 20010215 A 2913 PV304426 PUMP SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE HYD SYSTEM WORN W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA 2020 1619 (CAN) AFTER START HYDRAULIC PRESSURE WAS AT 0. PUMP REPLACED AND IT WAS FOUND THAT THE DRIVE SPLINES WERE WORN OUT ON TH E HYDRAULIC PUMP. PUMP SPLINES ARE SOFTER THAN THE ENGINE DRIVE. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 2001040400215 20010404 00215 SW 2001 4 4 CA010305006 1 20010226 A 3231 2751041153 MECHANISM SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE MLG DOOR OUT OF RIG W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) UPON SELECTION OF GEAR UP, THE RIGHT HAND MAIN GREAR WOULD NOT LOCK IN THE UP POSITION. THE GEAR WAS CYCLED UP AND DOWN. AIRCRAFT WAS FERRIED BACK TO BASE AND GEAR SWINGS WERE CARRIED OUT. THE RIGHT HAND INBOARD GEAR DOOR WAS FOUND OU T OF RIG. GEAR DOOR WAS RIGGED TO MANUFACTURERS SPECIFICATION AND AIRCRAFT WAS RELEASED TO SERVICE. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 2001040400217 20010404 00217 EU 2001 4 4 CA010305009 1 20010215 A 2750 9742001212 RELAY PILATS PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL FLAP PDU INOPERATIVE W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) FLAPS STICKING AT 15 PERCENT. FLAPS WOULD GO DOWN BUT WOULD NOT GO UP UNLESS ALL POWER WAS TURNED OFF AND THEN BAC K ON. RELAY K667 WAS AT FAULT. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001040400218 20010404 00218 EU 2001 4 4 CA010305010 1 20010215 A 7810 5781012041 EXHAUST STACK PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) CRACK WAS FOUND IN THE TIP OF STACK. STACK WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001040400219 20010404 00219 EU 2001 4 4 CA010305014 1 20010209 A 3242 9595601511 BRAKE ASSY PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL MLG FROZEN W O OTHER O OTHER LD LANDING 1 CA 14 (CAN) WHEN LANDING IN FOR CHIPEWYAN, AB, THE PILOT FOUND BOTH BRAKES FROZEN SOLID AND AFTER SLIDING DOWN THE RUNWAY BOTH TIRES BLEW.CHANGED BOTH TIRES AND HAD TO USE HEAT TO THAW THE BRAKES OUT. WE TRIED POURING GAS LINE DE-ICE OVER THE BRA KES, THIS DID NOT WORK. AFTER WARMING THE BRAKES WE THEN POURED ALCOHOL OVER THE BRAKES. THIS SEEMED TO WORK. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001040400220 20010404 00220 NE 2001 4 4 CA010305022 2 20010221 A 7200 ENGINE BOEING 727 727227 1384078 NM PWA JT8 JT8D7A 52053 NE NR 3 FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA (CAN) CREW NOTICED THAT NR 3 ENGINE OIL PRESSURE AND QUANTITY WERE DECREASING. ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNE D TO YHM. UPON MAINTENANCE TROUBLESHOOTING IT WAS FOUND THAT ENGINE WOULD NOT CONTAIN ENGINE OIL. TAIL PIPE WAS WET AND UPON INVESTIGATION BY PERFORMANCE OF A BORESCOPE INSPECTION IT WAS FOUND THAT JUST AFT OF BURNER CAN SECTION, ENGINE INT ERNALLY WAS WET.AT THIS TIME THE ENGINE WIL BE REMOVED AND SENT TO REPAIR FACILITY FOR REPAIR. NO FURTHER INFORMATION AT THIS TIME. 2 L 7 3 4F 4 F A3WE E2EA 2001040400222 20010404 00222 NM 2001 4 4 CA010301015 1 20010207 A 2750 285T0049053A FSEU BOEING 767 767375 NM GE CF6 CF680C2B6 30025 NE TE FLAPS FAILED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 43270 43270 (CAN) ON TAKEOFF, WITH FLAPS SELECTED 5, FLAPS WOULD NOT MOVE. MOMENTARY TRAILING EDGE FLAP DISAGREE LIGHT. STATUS MESSA GE TE FLAP SHUTDOWN. WHEN AUTOPILOT DISENGAGED AIRCRAFT ROLLED TO THE RIGHT. AIRCRAFT RETURNED TO YYZ. MAINTENANCE ON AR RIVAL FOUND FLAPS/SLATS RETRACTED. FLAP SLAT ELECTRONICS UNIT BITE COMPLETED AS PER FIM 27-51-00 PAGE 148, NO FAULT INDI CATED. FSEU REPLACED AS PER W/C 27310. TRAILING EGE FLAP ROTARY ACTUATORS CHECKED SERVICEABLE. FLAPS OPERATED IN ALTERNA TE AND NORMAL MODES CHECKED SERVICEABLE. 2 L 7 2 4F 4 F RT A1NM E13NE 2001040400223 20010404 00223 NM 2001 4 4 CA010301018 1 20010125 A 3260 43467410033 WARNING LIGHT BOEING 767 767375 NM GE CF6 CF680C2B6F 30025 NE MLG MALFUNCTIONED W O OTHER N FALSE WARNING LD LANDING 1 CA (CAN) ON LANDING, WHEN GEAR SELECTED DOWN, MAIN GEAR YELLOW WARNING LIGHT EMAINED ON. GEAR WAS RE-CYCLED ON FINAL APPROA CH, WITHOUT SUCCESS. A GO-AROUND WAS INITIATED AND GEAR WAS RE-CYCLES 2 MORE TIMES WITHOUT SUCCESS. A FLY-BY THE TOWER W AS ACCOMPLISHED AND TOWER ADVISED GEAR APPEARED DOWN. ON THE DOWNWARD LEG THE GEAR INDICATION CHANGED TO GREEN WHEN LIGH T ASSEMBLY WAS TAPPED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE LEFT AND RIGHT MAIN GEAR GREEN LIGHT ASSEMBLIES REPLA CED. AIRCRAFT JACKED AND GEAR SWING COMPLETED AS PER WORK CARD 96123. ALL FUNCTIONS CHECKED OK. 2 L 7 2 4F 4 F RT A1NM E13NE 2001040400224 20010404 00224 NM 2001 4 4 CA010301019 1 20010128 A 5610 WINDOW BOEING 767 7673Y0 NM PWA 4060 PW4060 52119 NE COCKPIT FAILED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA (CAN) ON CLIMBOUT A VERY LOUD SQUEAL FROM VICINITY OF CAPTS SLIDING WINDOW. FLIGHT RETURNED. INVESTIGATION FOUND A LOOSE DUCT IN LEFT TUNNEL OF THE AVIONICS COMPARTMENT. DUCTING REPOSITIONED AND SECURED. FLIGHT DEPARTED. ON CLIMBOUT AGAIN E XCESSIVE NOISE FROM AREA OF CAPTS WINDOW. FLIGHT CREW SUSPECTED PRESSURIZATION PROBLEMS AND RETURNED. MAINTENANCE REPLAC ED CAPTAINS NR 2 SLIDING WINDOW. 2 L 7 2 4F 4 F RT A1NM E24NE 2001040400225 20010404 00225 NM 2001 4 4 CA010301022 1 20010216 A 3097 WIRE BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE PITOT HEAT FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) IN CRUISE, LT ELEVATOR PITOT HEAT SYSTEM INDICATED HEATER SYSTEM UNSERVICEABLE. DUE TO WEATHER CONCERNS DIVERTED. REPAIRED WIRING TO LT PITOT TUBE. 2 L 7 2 4F 4 F A16WE E2EA 2001040400226 20010404 00226 NM 2001 4 4 CA010301025 1 20010219 A 2710 654476117 CONTROL UNIT BOEING 737 7372L9 1384497 NM PWA JT8 JT8D17A 52049 NE AILERON LEAKING W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 60587 46587 (CAN) AT FL350 IN CRUISE, NR 2 B HYDRAULIC PUMP OVERHEAT LIGHT CAME ON. PUMP WAS SELECTED OFF. 30 SECONDS LATER THE NR 1 B HYDRAULIC PUMP LOW PRESSURE LIGHT CAME ON. PUMP WAS SELECTED OFF, B HYDRAULIC SYSTEM QUANTITY DROPPED TO 1.2 GALLONS. AIRCRAFT RETURNED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A STEADY DRIP FROM THE B SYSTEM AILERON POWER CONTROL UNI T. B PUMP CASE DRAIN FILTERS INSPECTED, NO CONTAMINATION FOUND. NEW FILTERS INSTALLED. AILERON SYSTEM B POWER CONTROL UN IT REPLACED AS PER WORK CARD 51148. 2 L 7 2 4F 4 F RT A16WE E2EA 2001040400227 20010404 00227 EU 2001 4 4 CA010301026 1 20010130 A 3020 3241951 VALVE AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE ANTI ICE SYSTEM FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 25990 25990 (CAN) ON CLIMBOUT, NR 1 ENGINE ANTI-ICE FAULT INDICATED ON ECAM. VALVE REMAINED CLOSED. DUE TO ICING CONDITIONS FORECAST AT DESTINATION, ELECTED TO RETURN. REPLACED NR 1 ENGINE ANTI-ICE VALVE AS PER MM 30-21-51 PAGE 401. 2 L 7 2 4F 4 F RT A28NM E29NE 2001040400230 20010404 00230 EU 2001 4 4 CA010305007 1 20010215 A 2420 P111B20 WIRE PILATS 524321215 PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL GENERATOR BURNED W K NONE O OTHER IN INSP/MAINT 1 CA 100320 (CAN) WIRE FOUND BURNED ON ROUTINE INSPECTION. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001040400231 20010404 00231 EU 2001 4 4 CA010305015 1 20010216 A 2910 9603001261 SELECTOR VALVE PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL HYD SYSTEM FAILED W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA 952 (CAN) THE PILOT REPORTED THE HYDRAULIC LIGHT WAS ILLUMINATED ON THE CAWS PANEL. THE ACCUMULATOR PRESSURE WAS VERIFIED, A ND FOUND CORRECT. THE SERVICE SLECTOR WAS REPLACED. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001040400232 20010404 00232 EU 2001 4 4 CA010305016 1 20010220 A 5610 9598110108 WINDSHIELD PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL COCKPIT FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 970 (CAN) WHEN THE AIRCRAFT WAS BROUGHT IN FROM OUTSIDE (-36C) INTO THE HANGAR (+11C) THE CO-PILOTS WINDSHIELD SHATTERED. TH E WINDOW HAS BEEN REPLACED. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001040400233 20010404 00233 EU 2001 4 4 CA010305017 1 20010219 A 3150 9802811201 POTENTIOMETER PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL CENTRAL WARNING BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 1802 (CAN) THE GONG GENERATED BY THE CAWS WAS VERY LOW IN VOLUME OVER THE SPEAKER, THE VOLUME WAS NORMAL IN THE HEADSETS. THE PILOT POTENTIOMETER/SWITCH WAS FOUND WITH AN ELECTRICAL PIN BROKEN OFF INTERNALLY IN THE SWITCH. PART WAS REPLACED WITH NEW. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001040400234 20010404 00234 GL 2001 4 4 CA010305019 3 20010219 A 6140 9731011101 SWITCH MICRO PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL PROPELLER LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 1802 (CAN) EXCESSIVE PLAY FOUND AT SHAFT AREA OF SWITCH, ADJUSTMENT ERRACTIC.SWITCH REPLACED WITH NEW. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001040400235 20010404 00235 EU 2001 4 4 CA010305021 1 20010221 A 3260 5321112111 TARGET 5321112081 PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL MLG DOOR DEBONDED W K NONE O OTHER IN INSP/MAINT 1 CA 1802 (CAN) THE LT METAL TARGET PLATE FOR THE UP ROXIMITY SWITCH WAS FOUND DEBONDED FROM THE COMPOSITE GEAR DOOR.IT IS ALSO HE LD IN PLACE BY A BRACKET ATTACHED WITH SCREWS. THE PROPER EPOXY AS SPECIFIED BY A PILATUS FSE IS ON ORDER. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001040400236 20010404 00236 NM 2001 4 4 CA010305024 1 20010214 A 2751 1812994 INDICATOR BOEING 727 727221 1384071 NM PWA JT8 JT8D17 52049 NE TE FLAP FAILED W O OTHER N FALSE WARNING CL CLIMB 1 CA (CAN) DURING FLAP RETRACTION FROM FLAPS 2 TO FULL UP, OUTBOARD FLAPS FAILED TO RETRACT. OUTBOARD FLAP NEEDLES INDICATE A SYMMETRIC FLAPS, SPLIT 2 NEEDLE WIDTHS. REPLACED OUTBOARD FLAP INDICATOR PER MM 27-52-00, SYSTEM TESTED SERVICEABLE, 2 L 7 3 4F 4 F A3WE E2EA 2001040400237 20010404 00237 EU 2001 4 4 CA010307003 2 20010216 A 7230 COMPRESSOR GULSTM G1159 G1159A 3970109 SO RROYCE SPEY SPEY5118 54523 EU LT & RT ENGINE DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING ROUTINE POST FLIGHT INSPECTION FOD IMPACT DAMAGE WAS FOUND ON INBOARD LEADING EDGE/WING ROOT AREAS IN ADDIT ION TO DAMAGE ON BOTH ENGINE INLETS AND 1ST STAGE COMPRESSOR BLADES. DAMAGE IS SUSPECTED TO HAVE BEEN CAUSED FROM NOSE W HEEL SPRAY DURING TAKEOFF ON CONTAMINATED RUNWAY SURFACE AT CYYZ. NOTE: THE SUBMITTER HAS DISCOVERED THAT THE DAMAGE WAS MOST PROBABLY THE RESULT OF THE USE OF OVERSIZE SAND/ GRAVEL ON THE RUNWAY BY THE AIRPORT AUTHORITY 2 L 7 2 4F 4 F A12EA E2EU 2001040500001 20010405 00001 NM 2001 4 5 DHL2001712522 1 20010213 A 3270 65429724 FITTING BOEING 727 72729 1384007 NM DRAG LINK CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 C-CHECK - AFT FUSELAGE LUG OF LOWER FITTING FROM TAIL SKID DRAG LINK DOOR CRACKED 3 INCHES. REMOVED DAMAGED FITTING, CL EANED, TREATED, AND PRIMED AREA AND INSTALLED NEW FITTING IAW SRM 51-30-2, PAGE 13; SRM 51-10-2 PAGE 1, 2. (NON-ROUTIN E CARD 1498) 2 L 7 3 4F A3WE 2001040500002 20010405 00002 SO 2001 4 5 CA010222007 1 20010207 A 3310 110780108010 LIGHT EMB 110 EMB110P1 3260122 SO PWA PT6 PT6A34 52043 EA CABIN FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) IN FLT AFTER LEVELING OFF AT 9000 ODOUR STARTED COMING FROM HEATING VENTS. CREW OPTED TO SHUT AIR-COND SYS OFF TO FIND OUT WHERE SMELL COMING FROM. AT SAME TIME CREW CHECKED OP OF SMOKE ALARMS. THEY FUNCTIONED NORMALLY. CREW HAD THOUG HT THAT GLYCOL COULD OF MADE THAT ODOUR SO THEY ELECTED TO TURN SYS BACK ON. EVERYTHING WORKED NORMALLY FOR WHILE, BUT O DOUR CAME BACK SO THEY IMMEDIATELY TURNED AIR-COND OFF. AFTER THE SYS BEING OFF FOR FEW MINS, SMELL GETTING PROGRESSIVE LY STRONGER. CREW SUSPECTED ELECT. FIRE IN SYS. CREW ELECTED TO DECLARE EMEREGENCY & FOLLOWED EMERG CHECK LIST FOR ELECT . FIRE: CCT BREAKERS FOR TH E A/C SYS WERE PULLED. BAGGAGE AREA INS 1 L 7 2 4T 4 T A21SO E4EA 2001040500003 20010405 00003 2001 4 5 2001UALA00152 4 20010226 A 2565 62424407 SLIDE AIRCRUISERS 62774413 BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE DOOR CUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 778UA 864 0050 26940 DOOR 4 L/R SLIDE-RAFT (P/N 62774-413) HAS TWO CUTS IN THE INFLATABLE FOUND BY SHOP MECHANIC DURING UNPACKING FOR SHOP OV ERHAUL VISIT. UNIT WAS LAST OVERHAULED BY THE VENDOR. UNIT WAS SENT TO VENDOR FOR WARRANTY REPAIR. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001040500004 20010405 00004 NM 2001 4 5 2001UALA00153 1 20010223 A 5230 RIB BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CARGO DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 618UA 21878 AFT CARGO DOOR BS 1270-1350 RIB NR 3 CORRODED. REPAIRED DOOR BEAM PER TIMCO REO-GO7862 REF: SRM 52-30-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001040500005 20010405 00005 NM 2001 4 5 2001UALA00154 1 20010224 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 618UA 21878 AFT PIT BS 1153 BETWEEN STRINGERS 38R - 39R SHEAR TIE CORRODED. REPLACED SHEAR TIE REF: BAC DWG 140T2102, SRM 53-00-07, 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001040500006 20010405 00006 NM 2001 4 5 2001UALA00155 1 20010223 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 618UA 21878 AFT PIT BS 1263 BETWEEN STRINGERS 37L - 38L SHEAR TIE CORRODED. REPLACED SHEAR TIE REF: BAC DWG 140T2101, SRM 51-10-00 , AND 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001040500007 20010405 00007 NM 2001 4 5 2001UALA00156 1 20010224 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 618UA 21878 AFT PIT BS 1307 - 1329 STRINGER 35L CORRODED. INSTALLED STRINGER REPAIR REF: SRM 53-00-03 FIG 202. 2 L 7 2 4F 4 F RT A1NM E3NE 2001040500008 20010405 00008 NM 2001 4 5 2001UALA00162 1 20010224 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 790UA 26943 THE 3F EMERGENCY LIGHT STRIP BROKEN. REPLACED LIGHT STRIP. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001040500009 20010405 00009 NM 2001 4 5 2001UALA00165 1 20010221 A 5522 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT ELEVATOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7288U 21566 STATIC DISCHARGE FOUND AT RT ELEVATOR TRAILING EDGE JUST OUTBOARD OF TAB. INSTALLED SKIN REPAIR PER CMM SM-70-55-20-03- JD FIG 19. 2 L 7 3 4F 4 F A3WE E2EA 2001040500010 20010405 00010 2001 4 5 JBXA000253 4 20010307 A 3418 STALL WARNING CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTIONED A JBXA D RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 05 570ML 7206 STALL FAIL MESSAGE DURING TAKEOFF ROLL. PERFORMED OPS CHECK OF STALL PROTECTION SYSTEM IAW CL-65 AMM 27-35-01. MDC STA TUS PAGE SHOWS ALL GOOD CODES. MDC DIAGNOSTICS PAGE ALSO SHOWS NORMAL. 2 L 7 2 4F RT A21EA 2001040500011 20010405 00011 NE 2001 4 5 NACA2001011 2 20010301 A 7421 RHB32E SPARK PLUG PWA CB3 DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE NR 12 CYLINDER DEFECTIVE A NACA E D ENGINE SHUTDOWN RETURN TO BLOCK E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 AL 03 2907F 34767 44636 34767 ON RUNUP NR 3 ENGINE RUNNING ROUGH, 12 BMEP MAG DROP, (LEFT MAG). REPLACED NR 12L SPARK PLUG AND SHORT LEAD. 2 L 7 4 4R 4 R 6A3 5E8 2001040500012 20010405 00012 NM 2001 4 5 DHL2001702005 1 20010217 A 5347 SEAT TRACK BOEING 727 72730C 1384009 NM CABIN DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 SIDE BASH BAR NR 3 AND 4 MUSHROOM OUT OF FLOOR TRACK. REMOVED AND REPLACED FLOOR TRACK FROM STA 480 TO 560 PER SRM 53-1 0-2 AND 53-10-5. 2 L 7 3 4F A3WE 2001040500013 20010405 00013 NM 2001 4 5 DHL2001702004 1 20010217 A 5315 FLOORBEAM BOEING 727 72730C 1384009 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 AT FS 1050 LBL 3 ON BOTTOM OF FLOORBEAM WL 200 CORROSION ON FLOORBEAM AND GILLINER ATTACH ANGLE. REMOVED AND REPLACED L OWER SUPPORT TEE. 2 L 7 3 4F A3WE 2001040500014 20010405 00014 EU 2001 4 5 DHL2001362008 1 20010306 A 2760 SPOILER AIRBUS 300 A300B4103 3930104 EU WING MALFUNCTIONED A DHLA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 01 362DH 84 DURING FLIGHT CONTL CHK, RT SPOILER ONLY INDICATES 7 DEG DEFLECTION. TRANSFERRED TO DMI 4626 PER MEL 27-15-01-1 CAT B, SPECIAL PROCEDURE COMPLIED WITH. 2 L 7 2 4F RT A35EU 2001040500016 20010405 00016 SO 2001 4 5 COMA0110040 1 20010306 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 266CA 16378 120258 AFT CABIN EMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERY. 2 L 7 2 4T RT A31SO 2001040500017 20010405 00017 EA 2001 4 5 CA010307006 2 20010124 A 7200 ENGINE PWA DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A34 52043 EA RIGHT FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 CA 7368 755 (CAN) WHILE IN LEVEL CRUISE AT 500 AGL THE RT ENGINE FAILED. FIRST OBSERVATION WAS DROPPING OIL PRESSURE, PROPELLER AUTO -FEATHERING AND AIRCRAFT YAWING TO RIGHT. RT ENGINE WAS SECURED AND AIRCRAFT RETURNED TO BASE. UPON EXAMINATION AT BASE, THE POWER TURBINE WHEEL HAD DISINTEGRATED (CONTAINED) AND A LARGE QUANTITY OF METAL WAS RECOVERED FROM THE REDUCTION GE ARBOX (NOSE) SUMP AND SCREEN AREA.2001-03-12 TC: EXPECT OPERATOR FOLLOW-UP AFTER TEARDOWN INVESTIGATION. 1 H 7 2 3T 4 T RT A9EA E4EA 2001040500018 20010405 00018 EA 2001 4 5 COMA0160296 1 20010306 A 3350 6464 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 408CA 7440 EMERGENCY FLOOR LIGHTING ROWS 1 THRU 5 ARE INOPERABLE. REPLACED THE CABLE ASSY. 2 L 7 2 4F RT A21EA 2001040500019 20010405 00019 EA 2001 4 5 COMA0160297 1 20010306 A 2750 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT ACTIVATED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 964CA 7129 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2001040500020 20010405 00020 2001 4 5 COMA0160299 4 20010305 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 812CA 7381 STALL FAIL CAUTION MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2001040500021 20010405 00021 EA 2001 4 5 COMA0160300 1 20010304 A 2750 601R931001 POWER UNIT CNDAIR CL600 CL6002B19 EA WING MALFUNCTIONED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 785CA 4289 7326 FLAPS FAIL CAUTION MESSAGE. REPLACED THE PDU. 2 L 7 2 4F RT A21EA 2001040500022 20010405 00022 EA 2001 4 5 COMA0160301 1 20010305 A 2710 6229820008 COMPUTER CNDAIR CL600 CL6002B19 EA EE BAY MALFUNCTIONED A COMA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 01 416CA 13977 116 7450 AILERON TRIM INOP, C/B TRIPPED. PREVIOUS HISTORY OF RUNAWAY AILERON TRIM REPORTED BY FLIGHT CREW. REPLACED THE NR 2 DC U PREVIOUS REPORTS OF RUNAWAY TRIM WERE ERRONEOUS INDICATIONS. 2 L 7 2 4F RT A21EA 2001040500023 20010405 00023 EA 2001 4 5 COMA0160302 1 20010304 A 4990 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT FALSE INDICATION A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 914CA 7012 APU OIL PRESSURE CAUTION MESSAGE. COULD NOT DUPLICATE. APU OIL LEVEL AND PRESSURE NORMAL. 2 L 7 2 4F RT A21EA 2001040500024 20010405 00024 NE 2001 4 5 COMA0110039 2 20010305 A 7321 7898415008 EEC EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE MALFUNCTIONED A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 463CA 23315 120267 RT ENGINE IS SLOW TO ACCELERATE. POWER LEVER SPLIT. REPLACED THE EEC. 2 L 7 2 4T 4 T RT A31SO E20NE 2001040500025 20010405 00025 EA 2001 4 5 COMA0160298 1 20010306 A 2613 434419898 SENSOR CNDAIR CL600 CL6002B19 EA WING MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 420CA 7451 WING OVERHEAT WARNING MESSAGE. REPLACED THE LT WING OVERHEAT SENSOR. 2 L 7 2 4F RT A21EA 2001040500026 20010405 00026 WP 2001 4 5 TWAA0104301 1 20010201 A 5347 SEAT TRACK DOUG DC9 DC931 3022065 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 992Z 47095 DURING OP 15 MAINT CHECK FOUND CORROSION ON SEAT TRACK NUMBER 3, BETWEEN STA 200 AND 237. CUT TRACK AT STA 257 AND INST ALLED 7 FT AND 1 INCH OF TRACK PER SRM 53-05, FIG 4F. --CLOSED--- 2 L 7 2 4F A6WE 2001040500027 20010405 00027 WP 2001 4 5 TWAA0104302 1 20010306 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 992Z 47095 DURING OP 15 MAINT CHECK, FOUND FWD CARGO FUSELAGE SKIN UPPER FWD CORNER AT STA 316 WITH FASTENER HAVING CRACK INDICATIO N CONFIRMED WITH HIGH FREQ EDDY CURRENT PER 51-00-03, PART 6. CRACK .125 INCH LONG. REPAIRED CRACK IN FUSELAGE SKIN PE R DRAWING SRO9530117, AND ARA 17541 (WASHER SUBSTITUTED). 2 L 7 2 4F A6WE 2001040500028 20010405 00028 EU 2001 4 5 C2XA01IA147 1 20010306 A 2424 243211 GCU AEROSP ATR42 ATR42320 8680930 EU NR 2 FAILED A C2XA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 27 14815 104 LFT - FLIGHT 3431, THE CREW REPORTED SMOKE IN THE COCKPIT FOLLOWED BY THE NUMBER 2 A/C WILD GENERATOR FAULTING. THE AIR CRAFT LANDED AT LFT WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE NUMBER 2 A/C WILD GENERATOR ON MEL 24-22-04 CONTORL NUMBER 009893, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH ON FLIGHT 2914, WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO A/C WILD GENERATOR CONTORL UNIT, AND THE A/C WILD GENERATOR AS A PRECAUTION, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001040500029 20010405 00029 GL 2001 4 5 C2XA01IA148 2 20010306 A 7313 2306590A NOZZLE ALLSN EMB 145 EMB145LR SO ALLSN AE300 AE3007A GL NR 1 ENGINE DEFECTIVE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 16987 CAE3117411 145261 CAE311411 IAH - FLIGHT 3937, THE CREW REPORTED A FUEL SMELL IN THE COCKPIT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAI NTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE FUEL NOZZLES, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2001040500030 20010405 00030 WP 2001 4 5 MWEA010281 1 20010307 A 5320 991557713 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FORWARD BAG PIT, INTERCOSTAL STATION 362 TO 370, BETWEEN LONGERON 29 RIGHT AND LONGERON 30 IS CRACKED AT LOWER FLANGE AN D UPPER FLANGE IS BENT. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001040500031 20010405 00031 WP 2001 4 5 MWEA010282 1 20010307 A 5310 99124512 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FORWARD CARGO DOOR JAMB STATION 370 LONGERON 25 RIGHT TO 29 RIGHT, 8 NUT PLATES HAVE CORROSION BETWEEN NUT PLATES AND FR AME. REMOVED CORROSION, INTERCOSTAL AND CLIP. FABRICATED, DRILLED AND INSTALLED ANGLE REPAIR. LOCATED, DRILLED AND IN STALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001040500032 20010405 00032 WP 2001 4 5 MWEA010283 1 20010307 A 5320 99577003 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FORWARD BAG PIT, INTERCOSTAL AT LONGERON 29 RIGHT BETWEEN STATION 332 AND 351 HAS AREAS OF LIGHT CORROSION ON LOWER FLAN GE RIVET CHANNEL AND OUTBOARD SIDE. REMOVED CORROSION. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001040500033 20010405 00033 WP 2001 4 5 MWEA010284 1 20010307 A 5347 593054765 SEAT TRACK DOUG DC9 DC981 3022081 WP CABIN DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 ONE AREA OF NR 4 SEAT TRACK IS BLENDED BEYOND LIMITS STATION 673. REMOVED DAMAGED AREA, LOCATED, DRILLED AND INSTALLED PLUG AND CHANNEL. 2 L 7 2 4F A6WE 2001040500034 20010405 00034 WP 2001 4 5 MWEA010285 1 20010307 A 5320 5936097IN CLIP DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 SHOVEL CLIP ON LONGERON 27 RIGHT HAS CORROSION AND TOOL MARKS AROUND FASTENER HOLES 700 - 712. REMOVED CORROSION, DRILL ED AND INSTALLED SHOVEL CLIP. 2 L 7 2 4F A6WE 2001040500035 20010405 00035 WP 2001 4 5 MWEA010286 1 20010308 A 5320 49113832 ATTACH FITTING DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 STATION 1238 LEFT SIDE FRAME ATTACH FITTING AT THE FLOOR LINE HAS HEAVY CORROSION. REMOVED, LOCATED AND DRILLED AND INS TALLED FRAME FLOOR FITTING. 2 L 7 2 4F A6WE 2001040500036 20010405 00036 WP 2001 4 5 MWEA010287 1 20010308 A 5315 59560805 FLOORBEAM DOUG DC9 DC981 3022081 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 CABIN FLOORBEAM IN E&E STATION 200 GOUGED ON LOWER SIDE JUST RIGHT OF CENTER. CUT OUT DAMAGED AREA, FABRICATED AND INST ALLED REPAIR PIECES. 2 L 7 2 4F A6WE 2001040500037 20010405 00037 WP 2001 4 5 MWEA0110288 1 20010308 A 5313 592480219 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 LONGERON 17 RIGHT IS CRACKED AROUND FASTENER HOLES AT FRAME STATION 313. CUT, REMOVED, FABRICATED AND INSTALLED LONGERO N. 2 L 7 2 4F A6WE 2001040500038 20010405 00038 WP 2001 4 5 MWEA010289 1 20010308 A 5320 99364545 CLIP DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 SHEAR CLIP AT FRAME 750 FROM LONGERON 26 LEFT TO LONGERON 26 RIGHT HAS CORROSION AND TOOL MARKS. REMOVED CORROSION, BLE NDED TOOL MARKS, DRILLED, LOCATED AND INSTALLED SHEAR CLIP. 2 L 7 2 4F A6WE 2001040500039 20010405 00039 WP 2001 4 5 MWEA010290 1 20010308 A 5310 99360747 SHEAR TIE DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 SHEAR TIE AT FRAME STATION 703 BETWEEN LONGERONS 29 LEFT - 29 RIGHT IS CORRODED. REMOVED SHEAR TIE FRAME AND CORROSION. DRILLED, LOCATED AND INSTALLED NEW FRAME. 2 L 7 2 4F A6WE 2001040500040 20010405 00040 WP 2001 4 5 MWEA010291 1 20010308 A 5330 59360153 DOUBLER DOUG DC9 DC981 3022081 WP FUSELAGE MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 LEFT AFT FILLET PANEL 2108 HAS ONE MISSING DOME NUT WITHIN DOUBLE DRILLED HOLE AT STATION 1106, JUST ABOVE LONGERON 19. CUT OUT DAMAGED SECTION, FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER. 2 L 7 2 4F A6WE 2001040500041 20010405 00041 NM 2001 4 5 CALA0100206 1 20010305 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 47332 23570 INSPECTION FOUND LAV WALL LOWER FLOOR SUPPORT CORRODED AT STA 990, RBL 16-45. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001040500042 20010405 00042 NM 2001 4 5 CALA0100207 1 20010305 A 5531 RIB BOEING 737 737824 13844BZ NM VERTICAL STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14235 28947 INSPECTION FOUND RIG PIN HOLE BOSS CRACKED ON RIB WEB AT STA 56.48. THE CRACK WAS 2 INCHES LONG. AN INTERIM REPAIR WAS PERFORMED IAW ECRA 5530-01092. A PERMANENT REPAIR IS TO BE ACCOMPLISHED AT THE EARLIER OF 500 HOURS OR THE NEXT MX CHE CK WHERE USE OF RIG PIN IS REQUIRED NOT TO EXCEED 12 MONTHS. 2 L 7 2 4F RT A16WE 2001040500043 20010405 00043 WP 2001 4 5 CALA0100208 1 20010306 A 5320 FLOOR SUPPORT DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14062 47863 INSPECTION FOUND GALLEY G7 O/B FLOOR SUPPORT BEAM CORRODED AT STA Y = 1902-2007, X = 48L. THE FLOOR SUPPORT BEAM WAS RE MOVED AND A NEW SECTION WAS INSTALLED IAW GMM 10-900-01, SRM 53-16-01, AND ECRA 5100-01844. 2 L 7 3 4F A22WE 2001040500044 20010405 00044 WP 2001 4 5 CALA0100209 1 20010306 A 5320 FLOOR SUPPORT DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14062 47863 INSPECTION FOUND GALLEY G7 I/B FLOOR SUPPORT BEAM CORRODED AT STA Y = 1887-2007, X = 24L. THE FLOOR SUPPORT BEAM WAS RE MOVED AND A NEW SECTION WAS INSTALLED IAW GMM 10-900-01, SRM 53-16-01, AND ECRA 5100-01844. 2 L 7 3 4F A22WE 2001040500045 20010405 00045 EU 2001 4 5 MALA010257 1 20010228 A 7720 CLAMP SAAB SF340 340B 7860101 EU RT ENGINE MISALIGNED A MALA K NONE J WARNING INDICATION CR CRUISE 1 GL 15 430XJ 430 DURING FLIGHT 3322, THE RT ENGINE RUNNING EXCESSIVELY HOT 80-84 PERCENT RPM RANGE. AVOIDED ALL ENGINE INDICATIONS NORMA L BESIDES ITT. MAINTENANCE INSPECTED RT ENGINE. FOUND HIGH PRESS BLEED CLAMP MISALIGNED, INSTALLED NEW CLAMP. INSPECT ED INLET, NO DEFECTS NOTED. VERIFIED DDT ONLY 26 DEGREES WITHIN LIMITS, NO FURTHER ACTION REQUIRED. 2 L 7 2 4T RT A52EU 2001040500046 20010405 00046 EU 2001 4 5 MALA010258 1 20010302 A 3020 SPLICE SAAB SF340 340B 7860101 EU EXHAUST NOZZLE DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 414XJ 340B414 ON DEPARTURE OUT OF DTW ON FLIGHT 2942, LT ENGINE INTAKE LIGHT ILLUMINATED. CYCLING ON AFTER 1 MINUTE. AIR RETURN TO D TW. MAINTENANCE FOUND BAD SPLICE ON EXHAUST NOZZLE. REPLACED SPLICE, PERFORMED GROUND RUN FOR 20 MIN. NO FAULTS NOTED . IAW SAAB AMM 30-20-00. 2 L 7 2 4T RT A52EU 2001040500047 20010405 00047 EU 2001 4 5 MALA010259 1 20010302 A 7711 HTE690041 PRESSURE SWITCH BAC 146 AVRO146RJ85A 1500097 EU NR 2 ENGINE MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 514XJ E2330 INFLIGHT ON FLIGHT 3685, NR 2 ENGINE LOW PRESSURE LIGHT ILLUMINATED. AIR RETURN TO MEM. MAINTENANCE REPLACED NR 2 LOW PRESSURE SWITCH IAW AMM 30-21-14-201. P/N HTE690041, S/N ON FRO59BA, S/N OFF 20259. RAN BOTH ENGINES, ALL CHECK GOOD. 2 H 7 4 4F RT A49EU 2001040500048 20010405 00048 EU 2001 4 5 MALA010260 1 20010304 A 3020 44730501 MODULE SAAB SF340 SF340A 7850100 EU LT ENGINE DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 102XJ 340A102 DURING CLIMBOUT ON FLIGHT 2849, LEFT INTAKE LIGHT CAME ON DURING CLIMBOUT OF MSP. CREW FOLLOWED ORH AND RECYCLED THE SW ITCH. ALSO, RESET C/B''S H25, 26 & 27. LIGHT STAYS ON STEADY. MAINTENANCE REMOVED AND REPLACED SHOE BOX P/N 44730-501 , S/N ON A00232, S/N OFF 098, IAW SAAB AMM. 2 L 7 2 4T RT A52EU 2001040500049 20010405 00049 EU 2001 4 5 MALA010261 1 20010304 A 3620 SWITCH SAAB SF340 340B 7860101 EU BLEED AIR DEFECTIVE A MALA A UNSCHED LANDING M P OVER TEMP NO WARNING INDICATION CR CRUISE 1 GL 15 412XJ 340B412 DURING FLIGHT 2919 LEFT LP BLEED VALVE WOULD NOT STAY OPEN MORE THAN 2 MINUTES IN EITHER MANUAL OR AIR TURNBACK TO MSP. MAINTENANCE TROUBLESHOT, FOUND RIGHT DUCT OVERTEMP IN AUTO AND DUCT OVERTEMP LIGHT NOT ILLUMINATING. REPLACED DUCT TE MP SWITCHES M2035-501. OVERTEMP AND MCP LIGHT NOT ILLUMINATED. 2 L 7 2 4T RT A52EU 2001040500051 20010405 00051 NM 2001 4 5 UPS01235250 1 20010215 A 5753 FITTING BOEING 727 72722C 138400F NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, NR 7 FLAP TRACK ATTACH FITTING ON LWR SURFACE OF RT WING HAS LIGHT SURFACE CORROSION ON INBD FACE OF FITTING. CORROSION REMOVED IAW OHM REF EO SMRO 2001-006-008 FOR DETAILS. 2 L 7 3 4F A3WE 2001040500052 20010405 00052 NM 2001 4 5 UPS01235251 1 20010219 A 5711 SPAR BOEING 727 72722C 138400F NM LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, AFTER REMOVING A STIFFENER LOCATED AT FWD SIDE OF LT AUX SPAR, THE UPPER CHORD OF THE AUX SPAR WA S FOUND TO HAVE CORROSION IN A 2 INCH SECTION AROUND WS 277. UPPER CHORD REPAIRED IAW SRM 51-10-01. 2 L 7 3 4F A3WE 2001040500053 20010405 00053 NM 2001 4 5 UPS01235253 1 20010223 A 5312 BULKHEAD BOEING 727 72722C 138400F NM FUSELAGE CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, OPERATING HANDLE FOR AIRSTAIRS PUMP HAS CHAFED AFT PRESSURE BULKHEAD. REPAIRED IAW SMRO EO 2001-0 06-019. 2 L 7 3 4F A3WE 2001040500054 20010405 00054 NM 2001 4 5 UPS01235254 1 20010219 A 5714 STIFFENER BOEING 727 72722C 138400F NM CENTER WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, ON REMOVAL OF CENTER SECTION REAR SPAR UPPER CHORD SEVERAL STIFFENERS FOUND DAMAGED AND CORRODED. REPLACED STIFFENERS IAW 51-30-02 AND DWG 65C21531. 2 L 7 3 4F A3WE 2001040500055 20010405 00055 NM 2001 4 5 UPS01235255 1 20010222 A 5311 FASTENER BOEING 727 72722C 138400F NM FRAME CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, BOLTS FOUND CORRODED AT BS 360 BETWEEN STR 24-26L AND 24-26R. HOLES REWORKED IAW SMRO EO 2001-006 -020. 2 L 7 3 4F A3WE 2001040500056 20010405 00056 NM 2001 4 5 UPS01235256 1 20010215 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, CORROSION FOUND ON FLOORBEAM TOP CAP BS 950 RBL 55. REPAIRED IAW SMRO EO 2001-006-017. 2 L 7 3 4F A3WE 2001040500057 20010405 00057 NM 2001 4 5 UPS01235257 1 20010214 A 5753 ATTACH FITTING BOEING 727 72722C 138400F NM FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, NR 1 FLAP TRACK EVIDENCE OF HEAVY CORROSION FOUND ON FWD ATTACH LUGS, ON BOTH INBD AND OUTBD THRUS T FACES. ALSO, BORE HAS SIGNS OF LITE SURFACE CORROSION. REWORKED IAW SMRO EO 2001-006-006. 2 L 7 3 4F A3WE 2001040500058 20010405 00058 NM 2001 4 5 UPS01235258 1 20010214 A 5753 FLAP TRACK BOEING 727 72722C 138400F NM WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, NR 7 FLAP TRACK, AFT MOUNT OTBD HOLE DAMAGED DUE TO CORROSION. REWORKED IAW OHM 57-40-01. 2 L 7 3 4F A3WE 2001040500059 20010405 00059 NM 2001 4 5 UPS01235259 1 20010215 A 5753 FLAP TRACK BOEING 727 72722C 138400F NM WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, NR 5 FLAP TRACK HAS EVIDENCE OF CORROSION TO INBD LUG AT FWD ATTACH POINT. CORROSION REMOVED AND REWORKED IAW OHM 57-40-01. 2 L 7 3 4F A3WE 2001040500060 20010405 00060 NM 2001 4 5 UPS01235260 1 20010215 A 5753 ATTACH FITTING BOEING 727 72722C 138400F NM LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, NR 1 FLAP TRACK ATTACH FITTING ON LWR SURFACE OF WING HAS LIGHT SURFACE CORROSION ON INBOARD SIDE AND OUTBOARD SIDE. REWORKED IAW SMRO EO 2001-006-006. 2 L 7 3 4F A3WE 2001040500061 20010405 00061 NM 2001 4 5 UPS01235261 1 20010216 A 5755 SUPPORT FITTING BOEING 727 72722C 138400F NM SPOILER WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, INBOARD SUPPORT ARM FOR NR 7 SPOILER IS LOOSE AND HAS WEAR, WHERE SUPPORT ARM CONNECTS TO MAIN LAN DING GEAR BEAM. BUSHING INSTALLED IAW SMRO EO 2001-006-018. 2 L 7 3 4F A3WE 2001040500062 20010405 00062 NM 2001 4 5 UPS01235262 1 20010216 A 5311 FRAME BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, SUSPECT CRACK ON UPPER CHORD AT BS 740 AT LBL 60 APP. REPAIRED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 2001040500063 20010405 00063 NM 2001 4 5 UPS01235263 1 20010215 A 5714 STRUCTURE BOEING 727 72722C 138400F NM WING CNTR BOX CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, X-RAY REPORTS SUSPECT CRACKS AND CORROSION IN WING CENTER SECTION AT WBL 70.5 UPPER RT AREA AT BS 870. REPAIRED IAW SMRO EO 2001-006-016. 2 L 7 3 4F A3WE 2001040500064 20010405 00064 NM 2001 4 5 UPS01235264 1 20010216 A 5311 FRAME BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, FWD CARGO BAY, EVIDENCE OF CORROSION ON BS 520 AFT FACE AT LOWER FORWARD AREA ADJACENT TO DOOR OPE N CLOSE SWITCH. REPAIRED IAW SRM 51-10-06. 2 L 7 3 4F A3WE 2001040500065 20010405 00065 NM 2001 4 5 UPS01235265 1 20010212 A 5310 PRESSURE PANEL BOEING 727 72722C 138400F NM MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, CRACK IN LT MLG WHEEL WELL PRESSURE FLOOR AT 930 AFT REINFORCING BEAM AT LBL 54. REPAIRED IAW B72 7-5310-0460 APPENDIX C. 2 L 7 3 4F A3WE 2001040500068 20010405 00068 EU 2001 4 5 CA010307008 1 20010214 A 2131 13300114 CONTROLLER AMD FALC10 FALCON10 2730101 EU GARRTT TFE731 TFE7312 01518 WP CABIN PRESSURE FAILED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA (CAN) NR 1 CONTROLLER INSTALLED PROBLEM IN DESCENT LOST PRESSURE ON/AT 4,000 FEET. NR 2 CONTROLLER INSTALLED UNIT WOULD NOT PRESSURIZE IN AIR. NR 3 OUR CONTROLLER REPAIRED. INSTALLED AND FLIGHT TESTED OK. 2 L 7 2 4F 4 F A33EU E6WE 2001040500069 20010405 00069 EU 2001 4 5 CA010307010 1 20010122 A 2721 D25W582050003 ACTUATOR ISRAEL 1125 ASTRASPX 4500205 EU GARRTT TFE731 TFE73140 29001 NE RUDDER FAILED W O OTHER J WARNING INDICATION CR CRUISE 1 CA 1056 (CAN) RUDDER TRIM FREEZING AT ALTITUDE. FOUND UPPER RUDDER TRIM MOTOR TO BE THE PROBLEM.THE TRIM MOTOR WAS REPLACED AND NO FURTHER PROBLEMS HAVE BEEN EXPERIENCED. 2 L 7 2 4F 4 F RT A16NM E1NM 2001040500070 20010405 00070 NM 2001 4 5 CA010307011 1 20010219 A 3231 65224787 BRACKET BOEING 727 727217 NM PWA JT8 JT8D17 52049 NE NLG DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 68223 (CAN) NOSE LANDING GEAR FORWARD DOORS ACTUATING BRACKET WHICH ATTACHES TO THE NOSE GEAR. THE ACTUATING ROD END ATTACH PO INT WAS FOUND CRACKED DURING AIRCRAFT SERVICING. THE BRACKET WAS REMOVED AND REPLACED WITH SERVICEABLE PART I.A.W. BOEIN G 727 MM 32-22-1. 2 L 7 3 4F 4 F RT A3WE E2EA 2001040500071 20010405 00071 NM 2001 4 5 CA010307012 1 20010221 A 3222 65207441 TUBE BOEING 727 72722C 138400F NM PWA JT8 JT8D7B 52053 NE ALLSN A6441 A6441FN606 GL NLG STRUT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 7342 (CAN) AIRCRAFT ARRIVED WITH NOSE LANDING GEAR FLAT. ATTEMPTS TO RESERVICE OLEO FAILED DUE TO RAPID LEAKING. UPON INVESTI GATION IT WAS FOUND THAT THE INNER PISTON TUBE ASSEMBLY WAS CRACKED AT ITS LOWER FLANGE ALLOWING FLUID AND NITROGEN TO E SCAPE. TUBE ASSEMBLY REPLACED, AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 6 C P898 2001040500073 20010405 00073 NE 2001 4 5 CA010307014 2 20010222 A 7520 BACB30LE8U19 BOLT 311N51481 BOEING 757 757236 NM RROYCE RB211 RB211535E437 54555 NE NR 1 ENGINE SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING ROUTINE CHECK FOUND NR 1 ENGINE RT C DUCT AFT FORWARD BOLT SHEARED. AIRCRAFT WAS FERRIED ON A FERRY FLIGHT PERMIT WITH BOEING SUPPORT AND BOLT REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2001040500075 20010405 00075 WP 2001 4 5 CA010307016 1 20010216 A 2913 3508807 PUMP LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21122B02 54555 NE HYD SYSTEM CRACKED W H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 CA MX455905 (CAN) IN CRUISE AT FL300, HYDRAULIC SYSTEM C, LOST OF PRESSURE, EDP SHUT-OFF ACTIVATED BY FLIGHT CREW AND GEARS EXTENDED USING MANUAL SYSTEM. MAINTENANCE FOUND A 7.5 INCH CRACK IN EDP CASING, EDP REPLACED AND AIRCRAFT RETURNED TO SERVICE. P ART IS AVAILABLE. 2 L 7 3 4F 4 F A23WE E12EU 2001040500085 20010405 00085 WP 2001 4 5 CA010308002 1 20010131 A 3310 39564823 LIGHT DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE COCKPIT ARCED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) PRIOR TO TAKEOFF ELECTRICAL ARCHING AND ASSOCIATED SMOKE OBSERVED COMING FROM CAPTAINS FORWARD OVERHEAD PANEL LIGH TS FOLLOWED BY CIRCUIT BREAKER FOR MAP LIGHT TRIPPING. ELECTRICAL INSULATION (PART OF CRIMPED WIRE CONNECTOR (LUG) FOR C APTAINS MAP LIGHT FOUND DETERIORATED, ALLOWING ARCHING TO ROUND. CONNECTOR (AMP CONNECTOR (LUG)) BURNT WIRING REPLACED. NOTE: FLEET MANAGMENT REQUEST ALSO ISSUED, TO CHECK THE REMAINDER OF DC9 FLEET FOR CONDITION OF WIRING AND LUGS IN THE S AME AREA. 2 L 7 2 4F 4 F A6WE E2EA 2001040500086 20010405 00086 NM 2001 4 5 CA010308003 1 20010228 A 7920 B-NUT BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE ENGINE OIL LOOSE W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA (CAN) ENROUTE LEFT ENGINE STARTED TO LOOSE OIL RAPIDLY. ENGINE THROTTLED BACK TO IDLE AND CREW DIVERTED. ENGINE WAS NOT SHUTDOWN. ENGINE RUN CARRIED OUT. ENGINE OIL LINE SUPPLY B NUT FOR 3/4 BEARING FOUND LOOSE, NOT LOCKWIRED PROPERLY AND L EAKING. B NUT TIGHTENED AND LOCKWIRED. ENGINE RERUN AND NO LEAKS, CHECKED SERVICEABLE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001040500087 20010405 00087 NM 2001 4 5 CA010308004 1 20010119 A 3246 2601483 BOLT BOEING 767 767333 NM PWA 4060 PW4060 52119 NE WHEEL SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ONE BOLT FOUND SHEARED ATTACHING WHEEL HUN HALVES OF NR 3 MAIN WHEEL TIRE ASSEMBLE. MAIN WHEEL TIRE ASSEMBLE REPLA CED AS PER MAINTENANCE MANUAL TASK 32-45-08-400. 2 L 7 2 4F 4 F RT A1NM E24NE 2001040500088 20010405 00088 2001 4 5 CA010308005 4 20010214 A 2300 8990850003 CONTROL PANEL AIRBUS A319 A319114 NM GE CFM56 CFM565A 13802 NE RADIO MANAGEMENT FAULTY W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA (CAN) AFTER TAKEOFF, SMELL OF ELECTRICAL SMOKE PRESENT. NR 2 RADIO MANAGEMENT PANEL WENT BLANK, SWITCHED OFF AND PULLED CIRCUIT BREAKER FOR NR 2 RADIO MANAGEMENT PANEL.ODOR TOOK A LONG TIME TO DISSIPATE. UNABLE TO CLEAR SMOKE FOR DURATION O F FLIGHT. FOUND NR 2 RDIO MANAGEMENT PANEL AT FAULT.CHANGED NR 2 RADIO MANAGEMENT PANEL. 2 L 7 2 4F 4 F RT A28NM E29NE 2001040500089 20010405 00089 NM 2001 4 5 CA010308006 1 20010121 A 5753 D5757065000200 STRUCTURE AIRBUS A319 A319114 NM GE CFM56 CFM565A 13802 NE TE FLAPS DAMAGED W O OTHER F FLT CONT AFFECTED CL CLIMB 1 CA (CAN) FLAP DAMAGE DUE TO A BLOWN TIRE ON TAKEOFF.ATC REPORTED TIRE FRAGMENTS ON THE RUNWAY AFTER THE AIRCRAFT DEPARTURE. MAIN WHEEL ASSEMBLIES (P/N 32-2001-1 )LT AND RT CHANGED AND PRODUCTION PERMIT ISSUED TO REPAIR THE LEFT HAND INBOARD FLA P. 2 L 7 2 4F 4 F RT A28NM E29NE 2001040500101 20010405 00101 EU 2001 4 5 MALA010262 1 20010208 A 3060 TERMINAL SAAB SF340 340B 7860101 EU RT PROP DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 439XJ 439 ON FLIGHT 2978 RT PROP ANN ON OVERHEAD PANEL ILLUMINATED. RESET TWICE ON THIRD ATTEMPT THE LIGHT NO LONGER ILLUMINATED. LIGHT CAME ON AFTER 2 MINUTES IN FIRST TWO ATTEMPTS. AIR RETURN TO MSP. MAINTENANCE REPLACED TERMINAL END ON BRUSH B LOCK. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2001040500102 20010405 00102 EU 2001 4 5 MALA010263 1 20010208 A 2424 CONNECTOR SAAB SF340 340B 7860101 EU GCU FAULTY A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 450XJ 97059 450 DURING FLIGHT 3047 LEFT AC GENERATOR FELL OFF LINE. LEFT AC GEN AND INTAKE LIGHT ON IN FLIGHT, EVERYTHING BUT INTAKE TR ANSFER OK. AIR RETURN TO INL. MAINTENANCE FOUND LEFT AC GEN. CONTROL UNIT CONNECTOR CONTAMINATED. CLEANED CONNECTOR, REPLACED LEFT AC GEN CONTROL UNIT P/N 51634-002, S/N OFF 97059, S/N ON 98028, FAILED OPS CHECK. SWAPPED AC GENERATORS F OR TROUBLESHOOTING, FAILED OPS CHECK. RETURNED AC GENERATOR TO ORIGINAL POSITION LT AND RT LEAK CHECK GOOD. RT OPS CHE CK GOOD. REPLACED LT AC GEN HARNESS-GCU CONNECTOR AT FAULT. REPAIRED CHAFED WIRES IN FLAP COVE. OPS CHECK GOOD IAW 24 -20-00-2. MXC NOTIFIED, REMOVED FROM DMR REF: 409 0878 FOR MORE INFORMATION. 2 L 7 2 4T RT A52EU 2001040500103 20010405 00103 EU 2001 4 5 MALA010264 1 20010309 A 3040 SYL2509201 CONTROLLER SAAB SF340 SF340A 7850100 EU COCKPIT DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 98XJ 098 ON CLIMBOUT OF FLIGHT 3387 FROM DTW, THE LEFT SIDE HEAT LIGHT ILLUMINATED. CREW PERFORMED THE ORH AND LIGHT REMAINED ON . AIR RETURN TO DTW. MAINTENANCE REPLACED RT WINDSHIELD TEMP CONTROLLER P/N SYL250920-1, S/N ON 1860, S/N OFF 1786, RA N A/C FOR 20 MINUTES WITH CABIN PRESSURE, NO FAULTS NOTED. SYSTEM OPERATES NORMALLY. ALL IAW SF340 MM CHAP 30. 2 L 7 2 4T RT A52EU 2001040500104 20010405 00104 EU 2001 4 5 MALA010265 1 20010209 A 3260 806002 CIRCUIT BOARD BAC 146 AVRO146RJ85A 1500097 EU EE BAY MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 526XJ E2351 AFTER TAKEOFF ON FLIGHT 3563 OUT OF MSP, LEFT MAIN GEAR INTRANSIT LIGHT AND GEAR HANDLE UNSAFE LIGHT REMAINED ILLUMINATE D IN FLIGHT. CYCLE GEAR, NO EFFECT. AIR RETURN TO MSP. MAINTENANCE REPLACED LEFT MLG DOOR UPLOCK, REF: 409 CARD 087496 FOR DETAILS. REPLACED PCB P/N 8-060-02, S/N ON A158321, S/N OFF A184904S, PERFORMED OPS AND GEAR CYCLES. OPS CHECK GO OD. 2 H 7 4 4F RT A49EU 2001040500126 20010405 00126 EU 2001 4 5 MALA010266 1 20010312 A 2720 MS21251B5L TURNBUCKLE SAAB SF340 SF340A 7850100 EU RUDDER SYS BROKEN A MALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 15 98XJ 098 FLIGHT 2742 DURING APPROACH TO CRW NO RUDDER AUTHORITY ON FO SIDE. UPON LANDING NO RUDDER AUTHORITY ON CAPT. SIDE. (NO TENSION IN FOOT PEDALS). CREW HEARD A SMALL POP SOUND. MAINTENANCE REMOVED AFT CARGO PANEL TO ACCESS RUDDER CABLES, REMOVED ROUND FLOORBOARD PANEL IN CARGO AREA NR 2, REMOVED FLOORBOARD PANEL IN WHERE FDR IS, FOUND RT TURNBUCKLE BARREL TO BE BROKEN. REMOVED BARREL ASSEMBLY. AS PRECAUTIONARY MEASURE, REMOVED AND REPLACED NR 2 RT TURNBUCKLE P/N MS21251- B5L, IAW SF340 AMM 27-21. PERFORM NECESSARY RIGGING CHECKS FOR REPLACEMENT OF RUDDER CABLE TURNBUCKLES. 2 L 7 2 4T RT A52EU 2001040500127 20010405 00127 EU 2001 4 5 MALA010267 1 20010312 A 3020 44730501 MODULE SAAB SF340 SF340A 7850100 EU LT ENGINE DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 31XJ 031 FLIGHT 2903 AFTER TAKEOFF THE LEFT INTAKE HEAT CAUTION LIGHT KEPT CYCLING. AIR TURNBACK TO MSP. MAINTENANCE REMOVED AN D REPLACED DEICE MODULE P/N 44730-501, S/N OFF 400592, S/N ON A00112. 2 L 7 2 4T RT A52EU 2001040500128 20010405 00128 NM 2001 4 5 UPS01235299 1 20010316 A 5320 SUPPORT FITTING BOEING 727 727108C 1384039 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE:HFEC REFERENCE D211423 VERTICAL SUPPORT FITTINGS AT BS 930 BETWEEN STRINGERS 14 AND 18A HAS APPROX 5 INC HES CRACK (LEFT HAND SIDE). CLEANED AREA PERFORMED HFEC INSP PER B727 NDT MANUAL PART 6-51-00-00 FIG 4 ON BS 930 FITTIN G LT SIDE CRACK DOES NOT EXTEND ABOVE W/L 201.4. PREVIOUS REPAIR INSTALLED PER EO B727-5310-2611 APPLIED CORROSION INHI BITING COMPOUND THIS CLEARS DMI D211423. 2 L 7 3 4F A3WE 2001040500129 20010405 00129 WP 2001 4 5 UPS01835300 1 20010222 A 5313 564932742 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C2, 3, STA 1766 LONG 17R IS CRACKED. REPAIRED LONGERON IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2001040500130 20010405 00130 WP 2001 4 5 UPS01835302 1 20010228 A 5320 477239U1 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C2, 3, STA 1766 LONG 17R LONG FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001040500131 20010405 00131 WP 2001 4 5 UPS01835303 1 20010228 A 5320 37585702N1 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C2, 3, STA 1227 LONG 35R INTERCOSTAL FITTING AFT SIDE OF FRAME IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758570, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001040500132 20010405 00132 WP 2001 4 5 UPS01835306 1 20010228 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C2, 3, STA 1308 LONG 33L IS CORRODED BEYOND LIMITS ON OUTBOARD UPPER FLANGE. REPAIRED LONGERON IAW 8110 -3 APPROVED DH SK 811-942. 2 L 7 4 4F RT 4A25 2001040500133 20010405 00133 WP 2001 4 5 UPS01835307 1 20010228 A 5320 3755841501N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C2, 3, STA 1180 BATHTUB FITTING IS CRACKED BETWEEN LONG 33R-34R. REMOVED AND REPLACED FITTING IAW DWG 3 755841, AND SRM 53-2-0 FIG 2G. 2 L 7 4 4F RT 4A25 2001040500134 20010405 00134 WP 2001 4 5 UPS01835308 1 20010305 A 5320 4758514U521 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C2, 3, STA 1140 RT FWD SIDE LONG 34R INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTIN G IAW DWG 4758514, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001040500135 20010405 00135 WP 2001 4 5 UPS01835309 1 20010302 A 5512 SKIN DOUG DC8 DC873F 302199F WP HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C2, 3, LT HORIZONTAL STAB L/E UPPER SKIN IS CORRODED BEYOND LIMITS AT XFS 178. REPAIRED SKIN IAW SRM 55 -2-1 FIG 4. 2 L 7 4 4F RT 4A25 2001040500136 20010405 00136 WP 2001 4 5 UPS01835310 1 20010228 A 5320 37584951N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C2, 3, STA 1240 LONG 35L INTERCOSTAL FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758495, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001040500138 20010405 00138 EU 2001 4 5 20010319CW007 1 20010319 A 6720 704A34130184 CONTROL CABLE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE TAIL ROTOR BINDING E A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 13 971H 7417 2955 4548 WHILE PILOT WAS FLYING ON TOUR FLIGHT, NOTICED THAT TAIL ROTOR CONTROL PEDAL STUCK. PILOT MADE A PRECAUTIONARY LANDING. INSPECTED AIRCRAFT, FOUND THAT TAIL ROTOR CABLE WAS BINDING . REMOVED AND REPLACED TAIL ROTOR CABLE. COMPLIED WITH OPERATIONAL CHECK AND FUNCTIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 1 G 7 1 3U 3 U NC H9EU E19EU 2001040500139 20010405 00139 WP 2001 4 5 UPS01835311 1 20010228 A 5320 975494955 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C2, 3, STA 1240 - 1260 LONG 33R INTERCOSTAL IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACE D INTERCOSTAL IAW DWG 9754949, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001040500140 20010405 00140 WP 2001 4 5 UPS01835312 1 20010228 A 5320 37558471N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C2, 3 STA 1220 BANANA FITTING IS CORRODED BEYOND LIMITS AT LONG 33R. REMOVED AND REPLACED FITTING IAW D WG 3755847, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001040500141 20010405 00141 WP 2001 4 5 UPS01835313 1 20010222 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C2, 3, LEFT WING L/E UPPER SKIN HAS INTERGRANULAR CORROSION BETWEEN XFS 591.25 AND XFS 597.5. REPAIRED SKIN IAW 8110-3 APPROVED DH SK 811-336. 2 L 7 4 4F RT 4A25 2001040500142 20010405 00142 WP 2001 4 5 UPS01835315 1 20010222 A 5530 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C2, 3 VERTICAL STAB LT SKATE ANGLE IS CORRODED BEYOND LIMITS AT STA 1766. REPAIRED ANGLE IAW SRM 53-2-5 FIG 16A. 2 L 7 4 4F RT 4A25 2001040500143 20010405 00143 WP 2001 4 5 UPS01835316 1 20010222 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C2, 3, LEFT WING L/E UPPER SKIN HAS INTERGRANULAR CORROSION AT XFS 728.75 AND XFS 747.5. REPAIRED SKIN IAW 8110-3 APPROVED DH SK 811-335. 2 L 7 4 4F RT 4A25 2001040500144 20010405 00144 WP 2001 4 5 UPS01835317 1 20010307 A 5320 4645516501 ANGLE DOUG DC8 DC871F 302199D WP MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:B STA 958 CRACKED T-ANGLE ATTACHED TO KEEL BEAM. REMOVED AND REPLACED TEE IAW DRAWING 5616306. 2 L 7 4 4F RT 4A25 2001040500145 20010405 00145 WP 2001 4 5 UPS01835318 1 20010227 A 5347 9753289 SEAT TRACK DOUG DC8 DC873F 302199F WP CABIN GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C2, 3, STA 257 AND 230 AT LBL 60 SEAT TRACK IS GOUGED BEYOND LIMITS. REMOVED, FABRICATED, REPLACED SEAT TRACK IAW DWG 9753289 AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001040500146 20010405 00146 WP 2001 4 5 UPS01835319 1 20010302 A 5320 3750545502N SPLICE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C2, 3, STA 1040 - 1060 LONG 35R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750545 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001040500147 20010405 00147 WP 2001 4 5 UPS01835320 1 20010222 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C2, 3, STA 1766 AFT OF BULKHEAD LONG 17R IS CRACKED. REPAIRED LONGERON IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2001040500148 20010405 00148 CE 2001 4 5 CA010313018 1 20010211 A 3230 HYH5001 PUMP BEECH 76 76 1153005 CE MLG FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA 504 (CAN) GEAR WOULD NOT EXTEND WHEN SELECTED DURING APPROACH. MANUAL GEAR EXT REQUIRED. PROBLEM FOUND WITH PUMP ASSEMBLY, M OTOR WOULD NOT RUN UNLESS TAPPED WITH LIGHT BLUNT OBJECT. SUSPECT BRUSHES WORN. 1 L 7 2 3O A29CE 2001040500150 20010405 00150 EU 2001 4 5 CA010313020 1 20010307 A 5210 5521012339 STRUT PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL PAX DOOR JAMMED W K NONE O OTHER IN INSP/MAINT 1 CA 6015 (CAN) WHEN DOOR WAS OPENED TO DEPLANE PASSENGERS, SHOCK STRUT JAMMED AND POPPED RIVETS ON BRACKET (P/N 552.10.12.176) WH EN BRACKET FAILED DOOR FREE FELL UNTIL CHECK CABLES ATTEMPTED TO STOP TRAVEL, BUT THE MOMENTUM SNAPPED THE CABLE ATTACH BRACKETS (P/N 552.10.12.179 & 552.10.12.175). NEW BRACKETS HAD TO BE INSTALLED ALONG WITH A NEW DOOR SHOCK STRUT. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001040500151 20010405 00151 2001 4 5 CA010313021 4 20010301 A 8300 717000 GEARBOX BOEING 737 7372M8 1384483 NM PWA JT8 JT8D15 52051 NE ACCESSORY WORN W E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 CA (CAN) AIRCRAFT WAS ENROUTE FROM CALGARY TO WINNIPEG WHEN THE RIGHT HAND ENGINE EXPERIENCED A LOSS OF ENGINE OIL. THE CRE W SHUT DOWN THE ENGINE WHEN THE OIL PRESSURE STARTED TO DROP AND THE ENGINE OIL TEMPERATURE BEGAN TO CLIMB. THE OIL APPE ARED TO HAVE LEAKED FROM THE OIL FITTING ATTACH HOUSING IN THE GEAR CASE JUST ABOVE THE MAIN ENGINE OIL FILTER. THE MAIN ENGINE GEARBOX WAS REPLACED SO IT COULD BE SENT OUT FOR REPAIRS. 2 L 7 2 4F 4 F A16WE E2EA 2001040500152 20010405 00152 NM 2001 4 5 CA010313022 1 20010305 A 2752 5701802 JACKSCREW 2751281 BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE TE FLAP ACTUATOR SEPARATED W D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 CA 0292 (CAN) AFTER LANDING CREW WAS NOT ABLE TO RETRACT THE WING FLAPS ABOVE 1 UNIT. UPON INVESTIGATION THE NR 3 FLAP TRANSMISS ION SCREWJACK WAS FOUND SEPARATED FROM THE TRANSMISSION AT THE UNIVERSAL JOINT. THE FLAP TRANSMISSION AND SCREWJACK ASSE MBLY WAS BOTH REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F A16WE E2EA 2001040500153 20010405 00153 NM 2001 4 5 CA010313023 1 20010307 A 3231 65800511B STRUT BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE NLG DOOR BENT W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 12191 4031 (CAN) ON TAKEOFF WHEN THE GEAR WAS SELECTED UP THE CREW HEARD A BANG FOLLOWED BY A LOUD NOISE AND ACCOMPANIED BY A VIBR ATION IN THE AIRFRAME. THE CREW ELECTED TO RETURN. UPON LANDING, MAINTENANCE INSPECTED THE AIRCRAFT AND DISCOVERED THAT THE NOSE GEAR ATTACH LUG ON THE UPPER DRAG STRUT HAD BENT AND THE GEAR DOOR ROD HAD BROKEN WHICH ALLOWED THE GEAR DOOR T O FALL OPEN IN FLIGHT. THE AIRCRAFT WAS FERRIED WITH THE GEAR DOWN. IN CALGARY, THE UPPER DRAG STRUT AND THE DOOR ACTUAT ING ROD ON THE NOSE GEAR WERE REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 2001040500156 20010405 00156 CE 2001 4 5 CA010313027 1 20010309 A 5751 991300009 SKIN BEECH 100 100BEECH 1152916 CE PWA PT6 PT6A28 EA LT AILERON CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 13292 (CAN) ON INSPECTION IT WAS NOTICED THAT THE UPPER SKIN INBOARD WAS CRACKED UNDER THE LAP 1.50 INCH LONG. THE SKIN WAS RE MOVED AND NEW BEECH SKIN INSTALLED. LT AILERON. 1 L 7 2 3T 4 T A14CE E4EA 2001040500157 20010405 00157 CE 2001 4 5 CA010313028 1 20010309 A 5751 991300003 SKIN BEECH BEECH 100 100BEECH 1152916 CE PWA PT6 PT6A28 EA RT AILERON CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 13292 70898 (CAN) WHEN CHECKING SB 57-3148 IT WAS NOTICED THAT THIS AILERON WAS ALSO CRACKED AS PER SB 57-3148. KIT 109-4011-1 INSTA LLED. 1 L 7 2 3T 4 T A14CE E4EA 2001040500158 20010405 00158 CE 2001 4 5 CA010314002 1 20010228 A 3260 1CH25 DOWNLOCK SWITCH BEECH 100 100BEECH 1152916 CE PWA PT6 PT6A28 EA RT MLG FAILED W A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 CA (CAN) PILOT SELECTED GEAR DOWN & NOTICED NO GEAR SAFETY LIGHT FOR THE R/H MAIN GEAR. AFTER A FEW RETRACTIONS & EXTENSION S A GREEN LIGHT WAS OBTAINED. AIRCRAFT FLEW BY TOWER FOR A GEAR DOWN CONFIRMATION. A NORMAL LANDING TOOK PLACE. A JACK W AS POSITIONED UNDER RT WING & THE GEAR WAS CHECKED FOR POSITIVE LOCKING. AIRCRAFT PUT IN HANGAR ON JACKS & GEAR RETRACTE D & EXTENDED, IT WAS NOTED THE RT INDICATION LIGHT LAGGED 3-5 SECONDS AFTER FULL EXTENSION. THE SWITCH TESTED INTERMITTE NT & WAS REPLACED. SEVERAL GEAR SWINGS WERE PERFORMED & THE AIRCRAFT RELEASED.OCCURRENCE FEB 27 AT ABOUT 3:15 PMTTAF: 12 698.4 1 L 7 2 3T 4 T A14CE E4EA 2001040500160 20010405 00160 NM 2001 4 5 CA010314006 1 20010307 A 3310 69482725 CIRCUIT BOARD BOEING 727 727243 138408D NM PWA JT8 JT8D15 52051 NE CENTRAL DISPLAY SHORTED W A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 CA (CAN) ON TAKEOFF ROTATION MASTER WARNING LIGHT ILLUMINATED WITH NO LOSS OF ESSENTIAL POWER, ELEVATOR LOW PRESSURE LIGHT, GPWS WARNING LIGHTS, FLIGHT CONTROL PCU LIGHTS, ALL OIL PRESSURE/FILTER BYPASS LIGHTS, FLIGHT INSTRUMENT TRANSFER LIGHT S TRANSPONDER FAIL LIGHT, ALTITUDE ALERTER LIGHTS ILLUMINATED. FOUND STRAY TERMINAL SCREW SHORTING OUT RUDDER B, LOW PRE SSURE LIGHT CONTACTS. SCREW REMOVED. UPON FURTHER INVESTIGATION MASTER DIM CIRCUIT CARD FOUND UNSERVICEABLE. CARD REPLAC ED. MASTER DIM WARNING SYSTEM CHECKS SERVICEABLE. 2 L 7 3 4F 4 F RT A3WE E2EA 2001040500164 20010405 00164 EU 2001 4 5 CA010314013 1 20010216 A 2750 9742001212 RELAY PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL TE FLAPS FAILED W A UNSCHED LANDING F FLT CONT AFFECTED AP APPROACH 1 CA 17 (CAN) THE PILOT TRIED TO EXTEND FLAPS ON APPROACH INTO CORAL HARBOR, NU, AND WAS NOT ABLE. THE A/C DIVERTED TO RANKIN IN LET AND MADE A ZERO DEGREE FLAP LANDING. THE FLAP SYSTEM WAS RESET IN RANKIN SUCCESSFULLY, AND THE A/C DEPARTED FOR BAKE R LAKE. THE PILOT TRIED TO EXTEND THE FLAPS FOR DEPARTURE FROM BAKER, AND WAS UNABLE, HE HAD TO WAIT APPROXIMATELY THIRT Y MINUTES BEFORE THE FLAPS WOULD EXTEND. THE PILOT TRIED AN APPROACH INTO CORAL HARBOR, AND AGAIN WAS UNSUCCESSFUL IN EX TENDING THE FLAPS. THE AIRCRAFT DIVERTED TO IQALUIT, AND MADE A ZERO DEGREE FLAP LANDING. THE RELAY WAS REPLACED, AND TH E SYSTEM TESTED SERVICEABLE IN THE HANGAR. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001040500165 20010405 00165 2001 4 5 CA010314014 4 20010226 A 3420 1242102000 GYRO PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL COCKPIT FAILED W O OTHER P NO WARNING INDICATION CR CRUISE 1 CA 6 (CAN) WHEN TRYING TO SWITCH THE NUMBER ONE ATTITUDE HEADING REFERENCE UNIT (AHRU) FROM MAGNETIC TO FREE GYRO THE UNIT W OULD NOT SWITCH. THE NR 1 AHRU WAS REPLACED. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001040500166 20010405 00166 CE 2001 4 5 CA010314016 1 20010227 A 3230 66710 SOLENOID VALVE CESSNA 500 500CESSNA 2076602 CE PWA JD15 JT15D1A NE HYD SYSTEM FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 211 1014 (CAN) GEAR FAILED TO RETRACT AFTER TAKEOFF. REPLACED 4 WAY SOLENOID HYDRAULIC VALVE GEAR CYCLED TESTED OK. IAW C500 MM C H.32. 1 L 7 2 4F 4 F A22CE E25EA 2001040500171 20010405 00171 NE 2001 4 5 DHL2001708002 2 20010316 A 7260 717000 GEARBOX BOEING 727 72725 1384006 NM PWA JT8 JT8D7B 52053 NE NR 1 ENGINE LEAKING A DHLA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 708DH 18275 655459 NR 1 ENGINE LOST OIL QUANTITY AND PRESSURE IN FLIGHT. COMMENCED ENGINE SHUTDOWN AT INDICATION OF LOW OIL PRESSURE. T/S SYSTEM. REMOVED AND REPLACED N2 GEARBOX IAW P&W MM 72-60. NO LEAKS NOTED ON ENGINE RUN. TESTED OK IAW P&W MM72-00 AN D DHL JRH. 2 L 7 3 4F 4 F A3WE E2EA 2001040500172 20010405 00172 NE 2001 4 5 AWXA0001499 2 20010319 A 7321 8080504042 EEC AIRBUS A319 A319132 NM IAE V2524 V2524A5 NE NR 2 ENGINE MALFUNCTIONED A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 807AW 4906 2439 1064 V10587 OMA - DIVERTED FLIGHT - 3/15/01 - EN ROUTE FROM MKE TO PHX AT CRUISE FL 350 CREW GOT ECAM MSG, ENG 2 SENSOR FAULT; CREW ADVD MAINTENANCE AND DISPATCH AND FOLLOWED ECAM PROCEDURES; MADE PRECAUTIONARY LANDING IN OMA. OMA MAINTENANCE BLEW OUT THE NR2 ENG PB LINE WITH NITROGEN AND PERFORMED GROUND RUN USING FLIGHT CREW; ENG CHECKED NORMAL IAW TSM 73-22-00-810-8 68 & 73-22-00-710-40; NO FURTHER PROBLEMS ENCOUNTERED; AWA TECH SUPPORT ADVD THIS WAS 2ND OCCURENCE OF THIS MSG IN 2 DAY S AND REQ NR 2 ENG EEC TO BE REPLACED; AFTER 1ST OCCURENCE A BITE CHECK OF NR 1 AND NR 2 EIU WAS PERFORMED; NO FAULTS AN D NO ASSOCIATED SENSOR FAILURE NOTED ON POST FLIGHT REPORT. 2 L 7 2 4F 4 F RT A28NM E40NE 2001040500173 20010405 00173 NM 2001 4 5 AWXA0001500 1 20010319 A 5310 654587418 DOOR FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 CABIN R1 DOOR FWD DOOR FRAME FS 303 STR 17R CREASE BEAM FRAME CRACKED. REMOVED AND REINSTALLED R1 DOOR SURROUND PARTS, CASTING AND ANGLE IAW SRM 51-40-02. REMOVED DAMAGE, NDT - NO CRACKS IAW NTM PT 6 51-00-00. FABED REPAIR PARTS AND INST ALLED IAW SRM 51-40-02 AND 51-70-11. 2 L 7 2 4F RT A16WE 2001040500174 20010405 00174 NM 2001 4 5 AWXA0001501 1 20010319 A 5313 6546579595 STRINGER BOEING 737 7373Y0 1384671 NM APU BAY CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 APU COMPT RT SIDEWALL AIR INLET UPPER FWD CUTOUT HAS CORROSION. REMOVED CORRODED STRINGER; FABBED AND INSTALLED IAW BAC DWG 65-46579-595 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001040500175 20010405 00175 EU 2001 4 5 AWXA0001502 1 20010319 A 5320 D53112821200 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 620AW 052 FLOOR SUPPORT AT FR 16 TO FR 20 TO FR 20 Y-254 RT CORRODED. REPAIRED FLOOR SUPPORT IAW SRM 53-11-14 3A FIG 202. 2 L 7 2 4F RT A28NM 2001040500176 20010405 00176 EU 2001 4 5 AWXA0001503 1 20010319 A 5320 D53112818200 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 620AW 052 FLOOR SUPPORT AT FR 16-20 Y-254 LT CORRODED. REPAIRED FLOOR SUPPORT IAW SRM 53-11-14 3A FIG 202. 2 L 7 2 4F RT A28NM 2001040500177 20010405 00177 EU 2001 4 5 AWXA0001504 1 20010319 A 5320 D53112600200 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 620AW 052 FLOOR SUPPORT AT FR 16 Y-503.2 LT CORRODED. FABBED AND REPLACED FLOOR SUPPORT IAW AIRBUS DWG D533112600200 AND ASSY DWG D53112005 AND D53117005 AND SRM 53-11-14 PAGE 41. 2 L 7 2 4F RT A28NM 2001040500178 20010405 00178 EU 2001 4 5 AWXA0001505 1 20010319 A 5330 SKIN AIRBUS 320 A320231 3930325 EU FUSELAGE SCRATCHED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 620AW 052 LT FUSELAGE BETWEEN FR 60 AND 61 STR 26 SKIN HAS SEVERAL SCRATCHES AND NICKS. REPAIRED DAMAGE IAW SRM 53-00-11. 2 L 7 2 4F RT A28NM 2001040500179 20010405 00179 EU 2001 4 5 AWXA0001506 1 20010319 A 5754 D57460156201 FITTING AIRBUS 320 A320231 3930325 EU NR 1 SLAT GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 620AW 052 RT WING NR 1 SLAT OUTBOARD T/E LOWER SURFACE GOUGED. REPAIRED IAW AWA ER 26-5711-01072-JS2. 2 L 7 2 4F RT A28NM 2001040500180 20010405 00180 EU 2001 4 5 AWXA0001507 1 20010319 A 5720 D57130215200 FITTING AIRBUS 320 A320231 3930325 EU LT WING DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 620AW 052 LEFT FR 40 INNER FITTING FOUND DAMAGED. REPAIRED IAW AWA ER 26-5711-01072-JS5. 2 L 7 2 4F RT A28NM 2001040500181 20010405 00181 EU 2001 4 5 AWXA0001508 1 20010319 A 3350 321430 BATTERY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 620AW 052 D: EMERGENCY LIGHT TEST FAILS FOWARD LEFT BATTERYC: 10 WL BATTERY REPLACED IAW AMM 33-51-48-401 AND CHECKED SERV. IAW T/ C R1C33301 2 L 7 2 4F RT A28NM 2001040500182 20010405 00182 NM 2001 4 5 QXEA0100282 1 20010316 A 3350 5515800106 LIGHT DHAV DHC8 DHC8202 2809007 NM COCKPIT INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 359PH 514 PDX-OVERHEAD EMERGENCY COCKPIT LIGHT WILL NOT TEST. REMOVED AND REPLACED WITH NEW LIGHT ASSEMBLY. OPERATIONAL CHECK GO OD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001040500183 20010405 00183 EU 2001 4 5 QXEA0100283 1 20010316 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 BOI-EXIT SIGN ABOVE COCKPIT DOOR 28V LIGHTS INOPERATIVE. REPLACED EXIT SIGN ABOVE COCKPIT DOOR. OPERATIONAL CHECK GOOD . AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001040500184 20010405 00184 EU 2001 4 5 QXEA0100284 1 20010317 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481US 11230 SEA-MID CABIN OVERHEAD EXIT SIGNS HAVE INOPERATIVE BULBS. REPLACED BOTH OVERHEAD EXIT SIGN CIRCUIT BOARDS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001040500185 20010405 00185 EU 2001 4 5 QXEA0100285 1 20010316 A 3350 900542 BATTERY PACK FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 482US 32191 7876 11231 PDX-LAST 4 ROWS OF ESCAPE PATH LIGHTING INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT SEAT 14A FOR REAR 4 ESCAPE PA TH LIGHTS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001040500186 20010405 00186 EU 2001 4 5 QXEA0100286 1 20010317 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 496US 11169 BOI-OVERHEAD EMERGENCY EXIT SIGN ROW 8 HAS SEVERAL 28V LIGHTS INOPERATIVE. REMOVED AND REPLACED OVERHEAD EMERGENCY EXIT SIGN AT ROW 8. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001040500187 20010405 00187 2001 4 5 DHL2001805004 4 20010321 A 3420 CONNECTOR DOUG DC8 DC873F 302199F WP COCKPIT DIRTY A DHLA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 805DH 7020112 46125 COMPASS SYSTEM NR 1 AND NR 2 ARE NOT SLAVING TO MAGNETIC HEADING, DG FUNCTION APPEARS NORMAL. CLEANED CONNECTOR AT COMP ASS COMPARATOR SYSTEM SLAVING NORMAL, SWUNG TO KNOWN HEADING, SYSTEM CHECKED OK IAW MM 34-24-0. 2 L 7 4 4F RT 4A25 2001040500188 20010405 00188 EU 2001 4 5 DHL2001364010 1 20010321 A 3610 REGULATOR VALVE AIRBUS 300 A300B4203 3930306 EU BLEED AIR MALFUNCTIONED A DHLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 364DH 0141 AFTER NR 2 START, APU BLEED IN CLOSE RESET, X-BLEED OPEN, NR 2 BLEED PRESS INDICATED 0 PSI, WITH NR 2 REGU FAULT LIGHT ILLUMINATED. RAN ABNORMAL PROCEDURE. STILL NO PRESSURE AND FAULT LIGHT RE-ILLUMINATED. EXERCISED AND RESET NR 2 ENG B LEED PRESSURE REGULATOR VALVE. OPS CHECKED OK PER MM 36-11-00. 2 L 7 2 4F RT A35EU 2001040500189 20010405 00189 WP 2001 4 5 ASAA0180012 1 20010113 A 5210 5910081167 DOOR DOUG DC9 DC982 3022082 WP L1 DOOR OBSTRUCTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 954AS 44817 2034 49387 SEA - FOLLOWING FLIGHT, FORWARD CABIN (L1) DOOR WAS HARD TO OPEN. CLEARED ICE IN AND AROUND DOOR DRAIN HOLE. DOOR THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001040500190 20010405 00190 NE 2001 4 5 MASA01019 2 20010216 A 7200 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE NR 2 ENGINE FAILED A MASA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SW 07 37178 7178 FLT 6197 - PHX-SBA - THE PILOT NOTICED ZERO OIL PRESSURE INDICATION ON NR 2 ENGINE. THE ENGINE WAS SECURED IAW THE CFM. THE PILOT DECLARED AN EMERGENCY. THE AIRCRAFT LANDED UNEVENTFUL AT SBA. MAINTENANCE WAS INVESTIGATING IF INDEED THE NR 2 ENGINE WENT WITHOUT OIL FOR MORE THAN 30 SECONDS. AFTER INVESTIGATING, MAINTENANCE DECIDED TO REPLACE THE NR 2 ENG INE. THE ENGINE CHANGE IS IN PROGRESS. THE NR 2 ENGINE WAS REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2001040500191 20010405 00191 NM 2001 4 5 USAASB01072 1 20010302 A 3620 1296662 SENSOR BOEING 737 737401 1384701 NM NR 1 ENGINE MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 409US 17432 23879 TPA - FLT 1648 - CLIMBING THROUGH 8,000 FEET OUT TPA, EN ROUTE TO PIT, CREW ADVISED THAT THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. POWER WAS REDUCED ON THE NR 1 ENGINE AND THE LIGHT EXTINGUISHED. FLIGHT RETURNED TO FIELD AT TPA AND LAND ED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE NR 1 ENGINE PRECOOLER CONTROL VALVE SENS OR AND 450 DEGREE THERMOSTAT O-RING BLOWN OUT. REMOVED AND REPLACED THE SENSOR AND THE THERMOSTAT. RAN NR 1 ENGINE TO POWER. OPS CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001040500192 20010405 00192 NM 2001 4 5 20010404SG001 1 20010302 A 3620 1296942 THERMOSTAT BOEING 737 737401 1384701 NM NR 1 ENGINE LEAKING A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 409US 23879 TPA - FLT 1648 - CLIMBING THROUGH 8,000 FEET OUT TPA, EN ROUTE TO PIT, CREW ADVISED THAT THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. POWER WAS REDUCED ON THE NR 1 ENGINE AND THE LIGHT EXTINGUISHED. FLIGHT RETURNED TO FIELD AT TPA AND LAND ED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE NR 1 ENGINE PRECOOLER CONTROL VALVE SENS OR AND 450 DEGREE THERMOSTAT O-RING BLOWN OUT. REMOVED AND REPLACED THE SENSOR AND THE THERMOSTAT. RAN NR 1 ENGINE TO POWER. OPS CHECK AND LEAK CHECK GOOD. REF USAASB01072. (M) 2 L 7 2 4F RT A16WE 2001040500193 20010405 00193 WP 2001 4 5 USAA010204 1 20010225 A 5730 SKIN DOUG DC9 DC931 3022065 WP LT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 926VJ 46777 48146 PIT - FOUND SKIN CRACKED 2.5 INCHES, LEADING EDGE LT WING BOTTOM SIDE STATION XFS 126.438. CUT OUT DAMAGE, INSTALLED FL USH REPAIR WITH INNER DOUBLER PER SRM 57-06A FIG 3. (M) 2 L 7 2 4F A6WE 2001040500194 20010405 00194 WP 2001 4 5 USAAD01041 1 20010228 A 3350 AD4002P BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 919VJ 48139 PIT - FOUND THE COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001040500195 20010405 00195 EU 2001 4 5 USAASB01064 2 20010227 A 7200 ENGINE BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU LT WING OVERHEATED A USAA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 EA 19 446US 37233 24873 721822 CLT - FLT 1883 - ON CLIMB-OUT FROM CLT, EN ROUTE TO GCM, THE NR 1 ENGINE EGT REACHED 931 DEGREES WITH N1 CLIMB LIMIT. P OWER WAS REDUCED TO MAINTAIN WITHIN LIMITS, BUT NR 1 ENGINE RAN APPROX 100 DEGREES GREATER THAN NR 2 ENGINE. FLIGHT RET URNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE ASSEMBLY PER JOB CARD JK71-00-01. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F 4 F RT A16WE E21EU 2001040500196 20010405 00196 NE 2001 4 5 USAASB01051 2 20010220 A 7510 577957 DUCT BOEING 737 737201 1384454 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 248US 22755 BWI - FLT 2639 - ON CLIMB-OUT FROM BWI, AT FL120, THE NR 2 ENG OVERHEAT LIGHT ILLUMINATED. CREW REDUCED POWER ON NR 2 E NG TO IDLE AND LIGHT EXTINGUISHED. CREW DECLARED AN EMERG AND RETURNED TO FIELD AT BWI. FLT LANDED W/O FURTHER INCIDEN T. PRIOR TO LANDING. CAPT BROUGHT BACK SOME POWER ON THE NR 2 ENG TO CONFIRM IT WAS USABLE AND THEN RETURNED THE ENG T O IDLE. MX FOUND NR 2 ENG UPPER FUEL HEAT MANIFOLD DUCT BLOWN. LOWERED ENG AND REMOVED AND REPLACED UPPER FUEL HEAT MA NIFOLD DUCT. REINSTALLED ENG. ALSO, DUE TO HEAT DAMAGE, REMOVED AND REPLACED BOTH THROTTLE (P/N 20825-5) AND FUEL SHUT OFF (P/N 20800-5) TELEFLEX CABLES PER MM 76-11-81A AND THE ANTI-ICE (P/N 320115)AND FUEL HEAT (P/N 320115) VALVES. RAN 2 L 7 2 4F 4 F A16WE E2EA 2001040500197 20010405 00197 NM 2001 4 5 USAASB01058 1 20010224 A 2121 6454051 FAN BOEING 737 7374B7 1384702 NM CABIN FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 783AU 28747 25022 ORF - FLT 888 - EN ROUTE FROM PBI TO PHL, CRUISING AT FL290, FUMES WERE NOTICED FOLLOWED BY SMOKE ORIGINATING AT ROW 23 NEAR THE OVERHEAD. CREW DECLARED AN EMERGENCY AND DIVERTED TO ORF. FLIGHT LANDED WITHOUT FURTHER INCIDENT AS SMOKE AND HAZE CLEARED. AIRCRAFT TAXIED TO THE GATE AND DEPLANED NORMALLY. MAINTENANCE FOUND THE RIGHT RECIRCULATION FAN NOISY AND THE BEARING BAD. REMOVED AND REPLACED THE RIGHT RECIRCULATION FAN PER MM. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001040500198 20010405 00198 NM 2001 4 5 USAA010192 1 20010228 A 5320 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND Z-ANGLE CORRODED 1 INCH BY 5 INCHES, BETWEEN STATION 294 AND 344, LBL 60. REPLACED Z-ANGLE PER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 2001040500199 20010405 00199 NM 2001 4 5 USAA010193 1 20010228 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FLOORBEAM FLANGE CORRODED 1 INCH BY 2 INCHES, 6 PLACES, BS 344, BL 0, RBL 12, 18, 33, 40, 54, LBL 12, 28. I NSTALLED REPAIR ANGLE AND T-CAP PER SRM 53-10-51 FIG 205. (M) 2 L 7 2 4F RT A16WE 2001040500200 20010405 00200 NM 2001 4 5 USAA010194 1 20010228 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH, BS 380, LBL 12, 28 RBL 12, 18 33. CORROSION LEVEL 1. REPLACED T-CAP, FILLER, SHIMS, ANGLES PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2001040500201 20010405 00201 NM 2001 4 5 USAA010195 1 20010228 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FLOORBEAM CORRODED 2 INCHES BY 2 INCHES, STATION 967, LBL 16. CORROSION LEVEL 1. REPLACED T-CAP PER TR 53-10-05A . (M) 2 L 7 2 4F RT A16WE 2001040500202 20010405 00202 NM 2001 4 5 USAA010202 1 20010228 A 5310 CREASE BEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 519AU 40839 23705 PIT - FOUND WEB CORRODED 4 INCHES BY 6 INCHES, LEFT SIDE STRINGER 17 CREASE BEAM STATION 727D-727E. REPLACED CREASE BEA M WEB, FABRICATED NEW PER SRM 53-60-13 AND 51-40-02 AND 51-70-13. (M) 2 L 7 2 4F RT A16WE 2001040500203 20010405 00203 NM 2001 4 5 USAA010203 1 20010216 A 5310 CREASE BEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 519AU 40839 23705 PIT - FOUND WEB CORRODED 2 INCHES BY 3 INCHES, LEFT SIDE STRINGER 17, CREASE BEAM STATION 747-767. CORROSION LEVEL 2, T ASK NR C53-107-01. REPLACED CREASE BEAM WEB PER SRM 51-40-02, 51-40-03 AND DWG 65C26402. (M) 2 L 7 2 4F RT A16WE 2001040500204 20010405 00204 NM 2001 4 5 USAA010205 1 20010215 A 5510 FITTING BOEING 737 737301 1384611 NM RT HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 38667 23555 PIT - FOUND FITTING BUSHING DAMAGE, RIGHT HORIZONTAL STAB FORWARD CENTER SECTION, TOP AFT CLEVIS FITTING. CORROSION LEV EL 1. MACHINED FORWARD FACE OF LUG REMOVED .014 INCH PER SRM 55-10-10, MFG NEW BUSHING PER SRM 55-10-10. (M) 2 L 7 2 4F RT A16WE 2001040500205 20010405 00205 NM 2001 4 5 USAA010232 1 20010221 A 5320 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 32258 24554 CLT - FOUND CHORD CORRODED 13 INCHES, LEFT Z-ANGLE. REPLACED ANGLE CHORD PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001040500206 20010405 00206 NM 2001 4 5 USAA010233 1 20010221 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 32258 24554 CLT - FOUND FLOORBEAM CORRODED 1.5 INCH, STATION 294.5, 12 INCHES LEFT OF CENTER. FILLED VOID WITH SEALANT PER EA 69083 . (M) 2 L 7 2 4F RT A16WE 2001040500207 20010405 00207 NM 2001 4 5 USAA010239 1 20010221 A 5320 6552878497 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND Z-ANGLE CORRODED 4 INCHES BY 27 INCHES, STATION 967-944 FLOOR LEVEL AFT ENTRY DOORWAY. DEFECTIVE PART REPLA CED WITH IDENT PART NR PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001040500208 20010405 00208 NM 2001 4 5 USAA010241 1 20010218 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND CORROSION 3 INCHES BY 108 INCHES, STATION 986.5 LBL 54 TO RBL 54. SPLICED IN NEW T-CAP PER TYP REP 53-50-01 . CORROSION LEVEL 1. (M) 2 L 7 2 4F RT A16WE 2001040500209 20010405 00209 NM 2001 4 5 USAA010251 1 20010215 A 5320 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 32258 24554 CLT - FOUND Z-ANGLE CORRODED 36 INCHES, STATION 950-986 RBL 4, RT Z-ANGLE. BURNISH OUT CORROSION PRIME AND ALODINE PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001040500210 20010405 00210 NM 2001 4 5 USAASB01065 1 20010227 A 2781 654476028 SWITCH BOEING 737 737301 1384611 NM SLAT FAULTY A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 575US 23740 CLT - FLT 1625 - EN ROUTE FROM CLT-JAX, AS CREW RETRACTED THE FLAPS/SLATS, THE NR 6 LEADING EDGE SLAT INTRANSIT LIGHT IL LUMINATED ON THE FORWARD AND OVERHEAD PANELS AND WOULD NOT EXTINGUISH. THE CREW VISUALLY LOOKED AT THE SLATS ON THE WIN GS AND APPEARED TO BE STOWED. HOWEVER, AIRCRAFT DID ENCOUNTER SOME ROLL TO THE RIGHT. DECISION WAS MADE TO RETURN TO F IELD AT CLT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. SUBSEQUENT DISCUSSION WITH THE CREW V ERIFIED PROBLEM AS INDICATION ONLY. PERFORMED SLAT OPERATION EXTEND/RETRACTION CHECKS. OPERATION NORMAL. MAINTENANCE REMOVED AND REPLACED THE NR 6 SLAT ACTUATOR ROD END SWITCH ASSY PER MM 27-81-44. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001040500211 20010405 00211 NM 2001 4 5 USAA010173 1 20010226 A 5310 PRESSURE PANEL BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 32258 24554 CLT - FOUND PRESSURE DECK 1 INCH, BS 664, LBL 32, WL 202. INSTALLED DOUBLER PER TR 53-60-04. (M) 2 L 7 2 4F RT A16WE 2001040500212 20010405 00212 NM 2001 4 5 USAA010177 1 20010226 A 5320 INTERCOSTAL BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND WEB INTERCOSTAL CRACKED .25 INCH, STATION 277.5 AT FORWARD SERVICE DOOR. REPLACED INTERCOSTAL PER SRM 51-10 -02. (M) 2 L 7 2 4F RT A16WE 2001040500213 20010405 00213 NM 2001 4 5 USAA010178 1 20010226 A 5320 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND ANGLE CRACKED .25 INCH, APPROX STATION 289 FORWARD SERVICE DOOR STRUCTURE. REPLACED ANGLE PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001040500214 20010405 00214 NM 2001 4 5 USAA010179 1 20010226 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FRAME CRACKED .250 INCH, BS 380 BETWEEN STRINGER 8-9L. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001040500215 20010405 00215 NM 2001 4 5 USAA010180 1 20010226 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND SKIN CRACKED .5 INCH, STATION 328 LOWER AFT DOOR CUTOUT RADIUS. INSTALLED REPAIR DOUBLER PER SRM 53-10-01. (M) 2 L 7 2 4F RT A16WE 2001040500216 20010405 00216 NM 2001 4 5 USAA010181 1 20010226 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND INNER CHORD OF FRAME CRACKED .5 INCH, BS 601 BELOW STRINGER 17L CREASEBEAM BOTTOM RIVET. REPLACED REPAIR AN GLE AND FILLER PER TR 53-62-01 AND EA 69176. (M) 2 L 7 2 4F RT A16WE 2001040500217 20010405 00217 SO 2001 4 5 SIMA0533 1 20010222 A 7830 ACTUATOR EMB 145 EMB145 SO NR 1 T/R OUT OF ADJ A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 613AE 145081 DFW - FLT 3437 - DURING TAKEOFF ROLL, CREW NOTED ENGINE NR 1 THRUST REVERSER DISAGREE MESSAGE ON EICAS. TAKEOFF WAS ABO RTED AND AIRCRAFT WAS RETURNED TO THE GATE. MAINTENANCE ADJUSTED LOWER T/R ACTUATOR IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001040500218 20010405 00218 EU 2001 4 5 SIMA0502 1 20010219 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 322AC 320 MIA - FLT 5236 - PASSENGER DOOR EMERGENCY EXIT LIGHT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY. OP ERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001040500219 20010405 00219 EU 2001 4 5 SIMA0421 1 20010211 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 335AE 340B335 SAN - FLT 9731 - CREW REPORTED SEVERAL CABIN EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TWO EME RGENCY LIGHT POWER SUPPLY UNITS (S/N 17164 AND 19879) IAW SAAB MM. OPS HECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVI CE. (M) 2 L 7 2 4T RT A52EU 2001040500220 20010405 00220 EU 2001 4 5 SIMA0422 1 20010211 A 5270 WARNING LIGHT SAAB SF340 340B 7860101 EU COCKPIT ILLUMINATED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 313AE 340B313 BOS - MAIN DOOR HANDLE LIGHT CAME ON IN FLIGHT. CREW RETURNED TO BOS. (M) 2 L 7 2 4T RT A52EU 2001040500225 20010405 00225 NM 2001 4 5 CA010320019 1 20010206 A 7920 7515128 FILTER BOEING 737 737242C 1384478 NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE CLOGGED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA (CAN) DURING TAKEOFF NR 2 ENGINE FILTER BYPASS LIGHT ILLUMINATED. REJECTED TAKEOFF CARRIED AND AIRCRAFT RETURNED TO GATE . NR 2 ENGINE BYPASS REMOVED AND FOUND CLOGGED. NEW FILTER INSTALLED AND LEAK CHECK CARRIED OUT. SERVICEABLE. NO FURTHER INCIDENT DURING SUBSEQUENT FLIGHT. 2 L 7 2 4F 4 F A16WE E2EA 2001040500226 20010405 00226 NE 2001 4 5 CA010320020 2 20010202 A 7314 243600 PUMP BOEING 737 737242C 1384478 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE FAILED W C ABORTED TAKEOFF Y J ENGINE STOPPAGE WARNING INDICATION TO TAKEOFF 1 CA (CAN) DURING TAKEOFF, NR 1 ENGINE FAILED. REJECTED TAKEOFF ACCOMPLISHED. A/CSECURED AND AIRCRAFT RETURNED TO GATE. H.P. PUMP AND FCU CHANGED I.A.W. 73-11-1, TRIM RUNS AND LEAK CHECK CARRIED OUT I.A.W. 71-09-00. NO FURTHER INCIDENT DURING SU BSEQUENT FLIGHT. 2 L 7 2 4F 4 F A16WE E2EA 2001040500229 20010405 00229 2001 4 5 CA010321008 4 20010207 A 2310 8221047003 TRANSCEIVER BOEING 767 767209 NM PWA JT9 JT9D7R4D 52054 NE HF RADIO ODOR W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) LEFT HIGH FREQUENCY (HF) RADIO FAILED WHILE TRANSMITTING DURING CRUISE. SHORTLY AFTER BURNING ACRID ELECTRICAL SME LL FILLED COCKPIT. QUICK REFERENCE HANDBOOK ELECTRICAL SMOEK DRILL CARRIED OUT. LEFT HF TURNED OFF, CIRCUIT BREAKERS PUL LED, AND UTILITY BUSSES SELECTED OFF. SMELL EVENTUALLY DISSIPATED. BURNING SMELL TRACED TO LEFT HF TRANSCEIVER. HF TRANS CEIVER REPLACED AND OPERATION CHECKED SERVICEABLE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001040500230 20010405 00230 WP 2001 4 5 CA010321009 1 20010213 A 2120 CA67072 RECEPTACLE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE GALLEY BURNED W O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CA (CAN) ON TAKEOFF, BURN SMELL REPORTED IN THE GALLEY AREA. CIRCUIT BREAKER PULLED NO APPARENT SMOKE. FOUND NR 16 OVEN REC EPTACLE BURNT. REPLACED NR 16 RECEPTABLE. 2 L 7 2 4F 4 F A6WE E2EA 2001040500232 20010405 00232 SW 2001 4 5 CA010321014 1 20010228 A 2436 VR15284 GCU GULSTM 690TP 690D 3970405 SW GARRTT TPE331 TPE3315 01514 WP ROTOL R306 R306382F7 GL RT GENERATOR SHORTED W O OTHER H B J ELECT. POWER LOSS-50 PC SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) RT GENERATOR WOULD NOT COME ON LINE. SWITCHED R/H GENERATOR TO LT GENERATOR CONTROL UNIT (GCU) WORKED FINE. REPLAC ED RT GCU AND IT SHORTED OUT AND SMOKED. UNIT HAD OTSO. 1 H 7 2 3T 4 T 2A4 E4WE 6 C P8EU 2001040500234 20010405 00234 CE 2001 4 5 CA010322004 1 20010311 A 3244 301392641 TIRE BEECH 200 B200 1152922 CE PWA PT6 PT6A42 52043 NE HARTZL HCD4N3 HCD4N3A GL MLG IMBALANCED W A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CA 327 (CAN) SEVERE VIBRATION WAS FELT ON TAKEOFF. AIRCRAFT RETURNED TO BASE. NOSE WHEEL REMOVED AND UNABLE TO BALANCE. UPON TI RE REMOVAL AN INTERNAL BALANCE PATCH WAS FOUND UNATTACHED. THIS TIRE WAS PURCHASED NEW IS A GOODYEAR P/N 301-392-641, S/ N 91851436 WAS INSTALLED ON OCT 06/2000 AND HAD ACCUMULATED A TOTAL OF 460 LANDINGS. A NEW TIRE WAS MOUNTED BALANCED AND INSTALLED WITH NO VIBRATION NOTED ON THE NEXT FLIGHT. 1 L 7 2 4T 4 T A24CE E4EA 5 C STC 2001040500235 20010405 00235 NM 2001 4 5 CA010322005 1 20010314 A 2910 69547672 LINE BOEING 737 7372L9 1384497 NM PWA JT8 JT8D17A 52049 NE HYD SYSTEM LEAKING W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA (CAN) AIRCRAFT WAS CLIMBING THROUGH 8000 FEET WHEN NR 1 A SYSTEM HYDRAULIC PUMP FAILED, FOLLOWED SHORTLY BY THE NR 2 PUM P FAILURE. QUANTITY WAS DECREASING RAPIDLY. AIRCRAFT RETURNED. INSPECTION FOUND A SYSTEM FLEX LINE, LOCATED FORWARD OF L /H GEAR LEAKING. REPLACED LINE, TOPPED UP HYDRAULIC FLUID, RUN UP ENGINES SYSTEMS CHECKED SERVICEABLE. 2 L 7 2 4F 4 F RT A16WE E2EA 2001040500236 20010405 00236 CE 2001 4 5 CA010322007 1 20010314 A 2110 11455505511 COMPRESSOR BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA AIR CONDITIONING FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING ROUTINE 5TH DETAILED CHECK THE FOLLOWING ITEMS WERE FOUND DEFECTIVE ON THE VAPOR CYCLE COMPRESSOR. QUILL SH AFT, TEETH STRIPPED P/N 115-555025-9PULLEY DRIVE, TEETH STRIPPEDP/N 114-555065-1OUTER PULLEY DRIVE BEARING P/N 206SZZC STIFF & ROUGH TO TURNDRIVE BELT, SEVERAL CRACKSP/N 8147-0175 PARTS REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A24CE E4EA 2001040500238 20010405 00238 EU 2001 4 5 CA010322011 1 20010317 A 5210 5521012176 BRACKET PILATS PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL PAX DOOR LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 2934 (CAN) WHEN PASSENGER DOOR WAS INSPECTED, SEVERAL OF THE CHERRY MAX RIVETS THAT HOLD THE BRACKET WERE FOUND TO BE SHEARE D. BRACKET WAS REMOVED INSPECTED FOR DAMAGE AND RE-ATTACHED USING NEW HARDWARE. THIS IS THE SECOND BRACKET THAT WE HAVE FOUND LOOSE. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001040500242 20010405 00242 CE 2001 4 5 CA010323004 1 20010309 A 3233 99121114 ACTUATOR CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE RT MLG FAILED W O OTHER R PARTIAL RPM/PWR LOSS AP APPROACH 1 CA 2620 (CAN) ON APPROACH TO YC, GEAR WAS SELECTED DOWN, R/H GREEN DOWN AND LOCKED LIGHT FAILED TO ILLUMINATE. GEAR WAS CYCLED S EVERAL TIMES, SAME RESULT. PILOTS WERE ABLE TO VISUALLY CONFIRM R/H GEAR WAS DOWN AND BLEW THE EMERGENCY GEAR BOTTLE. AI RCRAFT WAS LANDED WITHOUT INCIDNET, AND UPON REACHING TAH WAY, SHUT DOWN, R/H GREEN STILL FAILED TO ILLUMINATE AND VISUA L INSPECTION OF ACTUATOR INDICATED THAT GEAR WAS NOT LOCKED (INDICATOR ON ACTUATOR WAS FLUSH). GEAR WAS BRACED AND AIRCR AFT WAS TOWED TO A HANGAR. 2 L 7 2 4F 4 F RT A22CE E25EA 2001040500245 20010405 00245 SO 2001 4 5 CA010323007 1 20010201 A 2912 MS2877516 O-RING PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HYD FILTER NICKED W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA (CAN) GEAR HANDLE DID NOT RETURN TO NEUTRAL WHEN GEAR SELECTED UP & GEAR UNSAFE LIGHT ON. WHEN GEAR SELECTED DOWN DID NO T GET 3 GREEN LIGHTS ON FIRST ATTEMPT, ON SECOND ATTEMPT GOT 3 GREEN LIGHTS & HANDLE DID NOT RETURN TO NEUTRAL. LANDING WAS UNEVENTFUL. MAINTENANCE INSPECTION REVEALED HOW HYDRAULIC FLUID LEVEL CAUSED BY LEAKING O-RING ON R/H HYDRAULIC FILT ER CANISTER, O-RING FOUND NICKED WHEN REMOVED AND INSPECTED. 1 L 7 2 3O 3 O A20SO E14EA 2001040500247 20010405 00247 EU 2001 4 5 CA010323009 1 20010222 A 2770 MS253481 SWITCH SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ROTOL R390 R3904123F27 NE RUDDER GUSTLOCK BURNED OUT W D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CA (CAN) ON PREPARATION FOR TAKEOFF WARNING LIGHT ILUMINATED WHEN GUSTLOCK RELEASED. A/C RETURNED TO RAMP. INVEST. REVEALED THAT SWITCH CNTLLING LIGHT BURNED, GIVING UNSAFE WARNING, ALTHOUGH GUSTLOCK SYS WAS IN NORMAL OP CONDITION. DEFECT DEFE RRED IAW A/C MEL 27-11,&IN COMPLIANCE WITH NOTE 4(A) ACTUATOR REMVD & ELECT. CONNECTIONS SECURED TO STRUCTURE: A/C DEPAR TED BUT AGAIN HAD WARNING LIGHT ON RELEASE OF GUSTLOCK. A/C RETURNED TO RAMP & WITHDRAWN FROM SERVICE, PENDING REPL SWIT CH. IT HAD NOT BEEN REALIZED THAT REMOVING ACTUATOR DID NOT DEACTIVATE WARNING LIGHT CCT, HENCE REPEAT WARNING WITH DEAC TIVATED SYS. 2 L 7 2 4T 4 T RT A52EU E8NE 6 C P31NE 2001040500248 20010405 00248 CE 2001 4 5 CA010323010 1 20010301 A 2140 721526 PUMP CESSNA 401 401 207590C CE CONT O520 TSIO520E 17040 SO HEATER SEIZED W O OTHER O OTHER CR CRUISE 1 CA (CAN) WHILE IN CRUISE, THE CABIN HEATER QUIT. THE HEATER FUEL PUMP DRIVE SHAFT WAS FOUND BROKEN OFF. THERE WA NO SIGN OF LUBRICATION ON THE DRIVE SHAFT BEARINGS. THE BEARINGS WERE VERY WORN AND DRY. THE PUMP WAS REPLACED. 1 L 7 2 3O 3 O A7CE E8CE 2001040500251 20010405 00251 CE 2001 4 5 CA010323019 1 20010315 A 3246 16218000 WHEEL BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1832 334 (CAN) RT INBOARD WHEEL WAS REMOVED FOR A ROUTINE TIRE CHANGE. UPON DISASSEMBLY IT WAS NOTICED THAT THERE WAS A 4 - 5 INC H CRACK IN THE BEAD AREA. THE RIM WAS BENT AND DEFORMED IN THIS AREA. THERE ARE NO INDICATIONS OF A STRIKE WITH A GROUND OBJECT YET THE CRACK / DEFORMATION IS QUITE OUT OF THE NORMAL. THE ADJACENT TIRE ASSEMBLY WAS REMOVED AND INSPECTED WIT H NO FINDINGS. 1 L 7 2 3T 4 T A14CE E4EA 2001040500252 20010405 00252 EU 2001 4 5 CA010323020 1 20010315 A 3242 9595601511 ROTOR PILATS 5321012050 PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL BRAKE ASSY FROZEN W O OTHER O OTHER LD LANDING 1 CA 97 IL165 (CAN) RT BRAKE FROZE ON LANDING. ICE REMOVED AND AIRCRAFT CONTINUED ON. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001040500253 20010405 00253 NM 2001 4 5 2001UALA00168 1 20010228 A 5310 PLATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 AFT DECK PLATE STA. 1681 BLENDED EXCESSIVELY RBL 39, 40, 46.5-47.5, 50-52. CORROSION STILL EXISTS AROUND REVET HOLES AT RBL 47. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REPAIRED DECK PLATE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001040500358 20010405 00358 NM 2001 4 5 2001UALA00170 1 20010228 A 2510 SEAT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE COCKPIT DEFECTIVE A UALA K NONE O OTHER LD LANDING 1 WP 29 7443U 21897 CAPTAIN REPORTS THAT HIS SEAT WILL NOT LOCK INTO POSITION. REQUESTED SPECIAL HANDLING FROM ATC. SUPPLEMENTAL DATA UPDATE SHOP HISTORY ON SEATS WITH THIS DISCREPANCY TEND TO INDICATE A CONTROL CABLE ADJUSTMENT PROBLEM. NO SHOP REPAIR RECOR DS CAN BE FOUND FOR THIS PARTICULAR SEAT. THIS 20 YEARS OLD PLUS TECHNOLOGY AVERAGES ONLY 2 WRITE-UPS PER MONTH FOR TH IS TYPE OF GRIPE. FLEET ENGINEERING CONSIDERS THIS AN ISOLATED INCIDENT. SEAT WAS REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 2001040900001 20010409 00001 WP 2001 4 9 MWEA010296 1 20010305 A 5311 991245110 FORMER DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 500ME 45711 FORMER AT STATION 305 HAS MISDRILLED HOLES. INSTALLED DOUBLERS. 2 L 7 2 4F A6WE 2001040900002 20010409 00002 WP 2001 4 9 MWEA010297 1 20010305 A 5320 591014211 WEB DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 500ME 45711 WEB AT STATION 305 HAS MISDRILLED HOLES. INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001040900003 20010409 00003 WP 2001 4 9 MWEA010298 1 20010305 A 5320 99579111 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 INTERCOSTAL AT STATION 305 HAS DAMAGED UPPER HORIZONTAL LEG. INSTALLED DOUBLERS. 2 L 7 2 4F A6WE 2001040900004 20010409 00004 WP 2001 4 9 TWAA0104502 1 20010308 A 5512 SKIN DOUG DC9 DC931 3022065 WP HORIZ STAB DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 992Z 47095 DURING 0P 15 MAINT CHECK, THE LT HORIZONTAL STABILIZER L/E HAD TWO AREAS THAT WERE BELOW MM LIMITS IN 55-10-108 PAGE 201 ITEM 1C AND 2B, XFS 175.5 AND XFS 216, 0.052 AND 0.050. INSTALLED INBD (XFS 175.5) AND OTBD (XFS 216) DOUBLER PER SRM 55-03, FIG 3 PAGE 5 TO 7. INSTALLED FASTENERS PER SRM 51-60-0 PAGE 19. 2 L 7 2 4F A6WE 2001040900005 20010409 00005 SO 2001 4 9 COMA0110044 1 20010312 A 5210 1202115801 CHANNEL EMB 120 EMB120RT SO PAX DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 21213 120264 DURING 2C CHECK TASK 811-02Z, THE PAX DOOR 1ST U-CHANNEL WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EM B-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001040900008 20010409 00008 SO 2001 4 9 C2XA01TY049 1 20010318 A 3222 1171402 AXLE EMB 145 EMB145LR SO NLG GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13978 3772 3772 145180 TYS DURING A SCHEDULED INSPECTION THE NOSE LANDING GEAR AXLE WAS FOUND TO BE GOUGED. MAINTENANCE REPAIRED THE AXLE IAW EMB GST-0866/01 AND EMB-CPM-51-21-05, THE REPAIR WAS FOUND TO BE SATISFCATORY. THE AIRCRAFT WILL BE RELEASED UPON COMP LETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2001040900011 20010409 00011 EU 2001 4 9 MALA010274 1 20010315 A 2612 899253 FIRE LOOP SAAB SF340 SF340A 7850100 EU LT ENGINE CHAFED A MALA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 68XJ 068 LT ENGINE FIRE INDICATION WARNING, ON DEPARTURE FROM DTW RECEIVED LT ENGINE FIRE WARNING INTERMITTENTLY. SHUTDOWN LT EN GINE, ORH COMPLETED. FIRE WARNING DID NOT RECUR AFTER SHUTDOWN, LANDING WEIGHT WAS 26,700 LBS. AIR RETURN TO DTW. MAI NTENANCE FOUND LT FIRE LOOP P/N 899253. CHAFING, SEE 409 NR 13289 FOR DETAILS. ALL RUNS GOOD. 2 L 7 2 4T RT A52EU 2001040900012 20010409 00012 NE 2001 4 9 MALA010275 2 20010315 A 7200 CT79B ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE NR 1 ENGINE MALFUNCTIONED A MALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 15 422XJ 422 GEE78572676 ON TAKEOFF ROLL ON FLIGHT 2755 DURING INITIAL POWER-UP FOR TO, NR 1 ENGINE TORQUE GAUGE SHOWED 0 PERCENT, ENGINE DROPPED TO 15 PERCENT PROP RPM READ 0, AND LIGHT DID NOT ILLUMINATE AFTER ENGINE SHUTDOWN. ABORTED TO. MAINTENANCE REPLACED L T ENGINE SN/OFF GE-E785726, S/N ON GE-E785676 IAW TASK CARD 7100-301. ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2001040900013 20010409 00013 EU 2001 4 9 MALA010276 1 20010317 A 3260 UPLOCK SWITCH SAAB SF340 SF340A 7850100 EU LANDING GEAR DIRTY A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 98XJ 098 GEAR INTRANSIT LIGHT REMAINS ON DURING GEAR RETRACTION, RAN QRH, PROBLEM CONTINUED. AIR RETURN TO DTW. MAINTENANCE CLE ANED UPLOCK SWITCHES AND PERFORMED SEVERAL GEAR SYSTEM CHECKS IAW SF340MM, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2001040900014 20010409 00014 EU 2001 4 9 MALA010277 1 20010317 A 3260 UPLOCK SWITCH SAAB SF340 SF340A 7850100 EU RT MLG OUT OF ADJ A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 98XJ 098 GEAR INTRANSIT LIGHT REMAINS ILLUMINATED AFTER SELECTING GEAR UP. AIR RETURN TO DTW. MAINTENANCE PERFORMED TROUBLESHOO TING OF LANDING GEAR EXTENSION AND RETRACTION SYSTEMS. FOUND RT MLG UPLOCK SWITCH OUT OF ADJUSTMENT. ADJUSTED RT UPLOC K SWITCH SF340MM 32-61-15-2. PERFORMED FUNCTIONAL TEST OF EXTENSION AND RETRACTION SYSTEM. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2001040900017 20010409 00017 NM 2001 4 9 EISA20010014 1 20010202 A 5230 656023411 FRAME BOEING BOEING 727 727223 1384074 NM CARGO DOOR PUNCTURED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ROUTINE C-CHECK INSPECTION FOUND AFT UPPER CORNER AFT CARGO DOOR HAS HOLE IN FRAME. REMOVED AND REPLACED CORNER BRACE IAW SRM 51-20-4, 51-30-2. 2 L 7 3 4F A3WE 2001040900018 20010409 00018 NM 2001 4 9 EISA20010016 1 20010202 A 5230 SKIN BOEING 727 727223 1384074 NM CARGO DOOR CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ROUTINE C-CHECK FOUND SEVERAL CRACK INDICATIONS ON EXTERNAL SKIN AND DOUBLER AT MAIN CARGO DOOR. STEP REAMED HOL ES, FABRICATED FREEZE PLUG BUSHINGS, AND RADIUS FILLER, ALODINED, PRIMED, AND INSTALLED IAW FVC DRAWING 53-0066-1, ATLAN TA ACO APPROVAL LETTER, B727-200 SRM 51-30-2, 51-10-2, 51-10-7. 2 L 7 3 4F A3WE 2001040900022 20010409 00022 WP 2001 4 9 ABXA010098 1 20010312 A 5320 39135771 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 52416 47364 INTERCOSTAL BETWEEN FUSELAGE STATION 541-560 HAD LEVEL 1 CORROSION AND WAS CRACKED. MAINTENANCE INSPECTED AND REPAIRED THE INTERCOSTAL IAW DC-9 SRM 51-10-3. 2 L 7 2 4F A6WE 2001040900026 20010409 00026 SO 2001 4 9 COMA0110045 1 20010312 A 5210 12021059001 CHANNEL EMB 120 EMB120RT SO PAX DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 21213 120264 DURING 2C CHECK TASK 811-02Z, THE PAX DOOR AFT U-CHANNEL WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EM B-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001040900027 20010409 00027 SO 2001 4 9 COMA0110046 1 20010312 A 5210 12021158001 CHANNEL EMB 120 EMB120RT SO PAX DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 21213 120264 DURING 2C CHECK TASK 811-02Z, THE PAX DOOR 3RD U-CHANNEL WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EM B-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001040900028 20010409 00028 CE 2001 4 9 20010315CW001 1 20010131 A 5520 1016200113 HINGE BRACKET BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE ELEVATOR CORRODED A TIMR K NONE O OTHER IN INSP/MAINT 1 NM 07 154GA UB25 UPON INSPECTION OF RIGHT HAND OUTBOARD HORIZONTAL STABILATOR ELEVATOR HINGE BRACKET A BADLY EXFOLIATED BRACKET WAS FOUND . A FLEET INSPECTION REVEALED 4 OUT OF 5 AIRCRAFT HAD THE CORRODED BRACKET THAT NEEDED REPLACED. 2 L 7 2 4T 4 T RT A24CE E4EA 2001040900036 20010409 00036 CE 2001 4 9 20010320CW009 1 20010122 A 7120 50910279 MOUNT BEECH 99 B99 1154004 CE PWA PT6 PT6A27 52043 EA HARTZL HCB3T HCB3TN2 GL RT ENGINE CHAFED E TIMA K NONE O OTHER IN INSP/MAINT 1 SW 99 899CA 34768 U104 IT WAS DISCOVERED DURING AN ENGINE CHANGE, THAT THE TUBE MOUNT HAD CHAFE MARKS BEYOND LIMITS. THE TUBE MOUNT WAS REPLAC ED WITH A SERVICABLE TUBE MOUNT. THE CAUSE OF THE CHAFING WAS DUE TO INDEQUATE CLEARANCE BETWEEN MOUNT AND BAFFLING AND FUEL LINES. 1 L 7 2 3T 4 T A14CE E4EA 6 C P15EA 2001040900037 20010409 00037 EA 2001 4 9 20010320CW010 2 20010205 A 7320 RSATA0125765362 SERVO CESSNA 172 172S 2072439 CE LYC IO360 IO360L2A EA INJECTOR MALFUNCTIONED D K NONE O OTHER IN INSP/MAINT 1 NM 11 74GW 665 665 172S8143 L2813751A FUEL INJECTOR SERVO CAUSING ERATIC IDLE. BACK FIRING AND EXTREMELY RICH MIXTURE WHEN THROTTLE IS RETARDED. DISCUSSION WITH TECH REP SUGGESTED TO SEND UNIT TO REPAIR STATION FOR CLEANING. DUE TO SERVO MOUNTED VERTICALLY, NOT ALLOWING FU EL TO BE PROPERLY EXPELLED, TENDS TO PLUG DIAPHRAM PARTS AND IMPACT TUBES. 1 H 7 1 3O 3 O NT 3A12 1E10 2001040900040 20010409 00040 CE 2001 4 9 20010320CW008 1 20010209 A 3260 BEP62GBP BULB LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE731* 01518 WP MLG INDICATOR BURNED OUT E DELA O OTHER N FALSE WARNING AP APPROACH 1 CE 03 550HC 083 ON FINAL APPROACH, CREW NOTICED 1 LANDING LIGHT DOWNLOCK INOPERATIVE. PROCEEDED WITH CHECK LIST TO VERIFY GEAR DOWN AND LOCK. AFTER A FLY-BY THE TOWER, THEY CONDUCTED A VISUAL WITH NO CONSENSUS. REMOVED AND REPLACED LIGHT BULB. SYSTEM C HECKED OK. 2 L 7 2 4F 4 F A10CE E6WE 2001040900041 20010409 00041 EU 2001 4 9 MALA010271 1 20010311 A 3340 LIGHT SAAB SF340 340B 7860101 EU EXTERIOR INOPERATIVE A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 406XJ 406 DURING FLIGHT 3345 AT 11,000 FT MSL CREW ATTEMPTED TO USE OUR LANDING LIGHTS TO SEE THE UPCOMING CLOUD, AND NOTED BOTH L T AND RT LANDING LIGHTS INOP. AIR RETURN TO MSP. MAINTENANCE REPLACED LT AND RT LANDING LIGHTS. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2001040900042 20010409 00042 EU 2001 4 9 MALA010272 1 20010315 A 3020 447301 MODULE SAAB SF340 SF340A 7850100 EU LT INTAKE DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 46XJ 046 FLIGHT 3391, LT INTAKE LIGHT CYCLING. LIGHT ON FOR 6 SECONDS, OUT OF 1:30 THEN REPEATS CYCLE. AIR RETURN TO DTW. MAIN TENANCE REPLACED LT DE-ICE MODULE IAW SF340, MM CHAP 30 P/N 44730-1, S/N OFF A00022, S/N ON A00461. RAN A/C FOR 30 MINU TES. NO FAULTS NOTED. SYSTEM OPERATES NORMAL. 2 L 7 2 4T RT A52EU 2001040900043 20010409 00043 EU 2001 4 9 R7MR32681 1 20010104 A 5210 350A25109521 JETTISON ROD SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE DOOR WEAK B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 392LG 353 3252 DOOR JETTISON ROD WEAK. REPLACED WITH NEW UNIT, CORRECTED PROBLELM. 1 G 7 1 3U 3 U H9EU E19EU 2001040900044 20010409 00044 CE 2001 4 9 20010320CW011 1 20010209 A 3230 CONNECTOR LEAR 35 35LEAR 5170600 CE GARRTT TFE731 TFE73122B 01518 WP MLG DIRTY E BSYA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 37WR 313 P74328 GEAR WOULD NOT RETRACT AFTER TAKE OFF. HAD MAINTENANCE JACK AIRCRAFT, CLEAN CONNECTOR PLUGS IN BOTH WHEEL WELLS, CLEAN ED ALL SWITCHES. OPS CHECKED GOOD, OK FOR SERVICE. 2 L 7 2 4F 4 F A10CE E6WE 2001040900045 20010409 00045 CE 2001 4 9 20010320CW012 1 20010209 A 2910 2307003235 LINE LEAR 35 35LEAR 5170600 CE GARRTT TFE731 TFE73122B 01518 WP HYD SYSTEM FAILED E BSYA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 GL 07 64CP 264 P74642 LOST ALL HYDRAULIC PRESSURE GOING INTO AIRPORT. BLEW GEAR DOWN, LANDED, NO PROBLEMS. FOUND NOSE GEAR RETRACT LINE BURS T, CAUSING LOSS OF ALL HYDRAULIC FLUID. REMOVED AND REPLACED HYDRAULIC LINE AND BOTH HYDRAULIC PUMPS. 2 L 7 2 4F 4 F A10CE E6WE 2001040900049 20010409 00049 CE 2001 4 9 20010406CW007 1 20010215 A 5730 0820009 SKIN CESSNA 402 402B 207590P CE CONT O520 TSIO520* 17040 SO LT & RT WING CRACKED A OEZA K NONE O OTHER IN INSP/MAINT 1 WP 19 767EA 9522 402B1244 DURING SCHEDULED INSPECTION OF AIRCRAFT, FOUND CRACKS IN LEFT AND RIGHT UPPER WING SKINS APPROXIMATELY 5 IN TO 6 INCHES IN LENGTH FORWARD OF WING BAGGAGE LOCKER AND AFT OF FIREWALL OVER CENTER RIBS AT WING STATIONS 57.50. THIS AREA IS NOR MALLY COVERED BY NACELLE PANEL AND CRACKS WERE SEEN FROM UNDERSIDE IN WHEEL WELLS. LANDING GEAR SIDE BRACES ATTACH TO R IB IN THIS AREA AND CRACKS MAY BE CAUSED BY FATIGUE AND HARD LANDINGS. 1 L 7 2 3O 3 O A7CE E8CE 2001040900051 20010409 00051 NM 2001 4 9 EISA20010026 1 20010216 A 5297 AE2933 WIRE BOEING 727 727225 1384077 NM CARGO DOOR GROUNDED A EISA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 353PA 20622 REJECTED TAKEOFF DUE TO MAIN CARGO DOOR LIGHT ILLUMINATING. INSPECTED DOOR, WARNING SWITCHES OK, FOUND WIRES TO INDICAT OR SWITCH CONTACTING GROUND IN DOOR. REPAIRED WIRES AND SECURED PER M/M AERONUTICAL ENGINEERS M/M. 2 L 7 3 4F A3WE 2001040900054 20010409 00054 CE 2001 4 9 20010406CW010 1 20010312 A 2140 94E423 PRESSURE SWITCH CESSNA 340 340A 2076405 CE CONT O520 TSIO520* 17040 SO HEATER INOPERATIVE E DUFA K NONE L NO TEST IN INSP/MAINT 1 GL 27 177VM 400 340A0964 FOUND COMBUSTION AIR PRESSURE SWITCH IN THE CLOSED POSITION WHEN HOOKED UP BETWEEN THE COMMON AND NORMAL OPEN TERMINALS WHEN NO PRESSURE WAS PRESENT. THIS IS THE NEW STYLE PRESSURE SWITCH, WHICH DOES NOT REQUIRE TESTING. 1 L 7 2 3O 3 O 3A25 E8CE 2001040900056 20010409 00056 SW 2001 4 9 20010406CW011 1 20010208 A 3246 2751000960 BEARING SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE331* 01514 WP WHEEL MISSING B MEJR K NONE O OTHER IN INSP/MAINT 1 SW 17 378PH 1132 AC575 LEFT INBOARD MAIN WHEEL WAS MISSING AFTER A NORMAL LANDING. WHEEL NUT, WITH COTTER KEY AND BOTH INNER BEARING RACES WE RE STILL ON THE AXLE. A BEARING FAILURE SEEMS MOST LIKELY CAUSE BECAUSE THE OUTER RACES AND ROLLERS WERE MISSING. 2 L 7 2 4T 3 T RT A8SW E2WE 2001040900057 20010409 00057 NM 2001 4 9 USAA010153 1 20010212 A 5313 STRINGER BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 618AU 47860 22210 CLT - FOUND STRINGER CORRODED 2 INCHES BY 6 INCHES, AFT CARGO STATION 1380-1400, RBL 8. INSTALLED NEW STRINGER SECTION PER SRM 51-10-01. CORROSION LEVEL 1. (M) 2 L 7 2 4F RT A2NM 2001040900058 20010409 00058 WP 2001 4 9 GTIA010035 1 20010211 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP BATTERY PACK DISCONNECTED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 603CA 49508 ACY - FOUND COCKPIT EMERGENCY LIGHTS WILL NOT ILLUMINATE. RESECURED LEAD TO BATTERY PACK IAW 33-50-00. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2001040900063 20010409 00063 EA 2001 4 9 ASOA01024 1 20010225 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA CARGO BAY MALFUNCTIONED A ASOA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 11 832AS 3553 7243 FLT 4545 - DURING FLIGHT FROM ISP TO ATL, CREW RECEIVED A CARGO SMOKE WARNING. CREW BLEW EMERGENCY FIRE BOTTLES AND DIV ERTED TO BWI. AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED SMOKE DETECTORS AND REPLACED FIRE BOTTLES AND S QUIBBS. OPERATIONAL TESTS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001040900065 20010409 00065 EU 2001 4 9 G1FR100Y 1 20010122 A 3010 FAL1005 HOSE AMD FALC10 FALCON10 2730101 EU GARRTT TFE731 TFE731* 01518 WP RT SLAT FAILED B G1FR K NONE L NO TEST IN INSP/MAINT 1 GL 13 147G 214 AFTER COMPLETING A MFG 1200 HR B INSPECTION, A MAINTENANCE GROUND RUN OPERATIONAL CK OF THE WING ANTI-ICE SYSTEM WAS REQ UIRED AND ACCOMPLISHED. NO HEAT WAS NOTICED AT RT OUTBOARD SLAT WITH ANTI-ICE WINGS SELECTED AND GREEN OPERATIONAL LIGH T ILLUMINATED. FURTHER INSPECTION REVEALED OUTBOARD SLAT AIR SUPPLY FLEX HOSE INSIDE WALL MATERIAL SEPARTED AND COLLAPS ED, RESTRICTING AIR FLOW. EXTERIOR CONDITION OF HOSE FOUND TO BE GOOD. THIS HOSE WAS RECENTLY REPLACED WHILE AIRCRAFT WAS IN SERVICE. ACTUAL TOTAL TIME IS UNKNOWN AT THIS TIME. HOSE MFG DATE:2000 THIS HOSE IS LIFE LIMITED TO 3000 HOURS AC TIME LIMITS. COCKPIT INDICATION SHOWED SYSTEM TO BE OPERATING NORMALLY IN THIS CONFIGURATION. 2 L 7 2 4F 4 F A33EU E6WE 2001040900066 20010409 00066 NM 2001 4 9 20010315CW002 1 20010213 A 2761 656952211 HOUSING BOEING 737 737200 1384453 NM SPOILER ACTUATOR CRACKED A IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 67059 HOUSING ASSEMBLY IS CRACKED AROUND THE NUT FLANGE AREA. FATIGUED, OVERSTRESSED. 2 L 7 2 4F A16WE 2001040900067 20010409 00067 WP 2001 4 9 TWAA0104503 1 20010307 A 5320 CASTING DOUG DC9 DC982 3022082 WP NLG WW CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 928TW 48012 DURING CHECK-C MAINT, CASTINGS WERE CRACKED APPROXIMATELY STA 69, 16 INCHES TO RT OF BL AND 16 INCHES TO LT OF BL, IN CE ILING AREA OF NOSE GEAR WELL. REPLACED CASTINGS PER SRM 51-30-1, SRM 51-30-5, SPM 6-70-01, AND DRAWING 9910088. 2 L 7 2 4F A6WE 2001040900068 20010409 00068 NM 2001 4 9 TWAA0104504 1 20010309 A 5754 SKIN BOEING 767 767205 1385121 NM SLAT DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 650TW 23057 DURING CHECK-C MAINT ON THE RT WING THE NUMBER 8 L/E SLAT, 61 IN FROM OTBD END AND 7 IN FROM THE WEDGE T/E, HAD 3.5 BY 5 .75 INCH DELAMINATION. INSTALLED 8 IN BY 8 IN METAL TO METAL HOT BOND REPAIR PER SRM 51-70-09. 2 L 7 2 4F RT A1NM 2001040900069 20010409 00069 EA 2001 4 9 JBXA000256 1 20010309 A 3610 SHUTOFF VALVE CNDAIR CL600 CL6002B19 EA ENGINE MALFUNCTIONED A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 593ML 7465 AFTER TAKEOFF LT TENTH ARM OPEN MESSAGE APPEARED ON EICAS. THE LEFT TENTH SOV SWITCH WAS IN THE OPEN POSITION BUT VALVE WOULD NOT OPEN. PERFORMED SATISFACTORY OPERATIONAL TEST OF TENTH STAGE BLEED SYSTEM IAW CRJ AMM 36-11-00. NO FAULTS N OTED. 2 L 7 2 4F RT A21EA 2001040900070 20010409 00070 SO 2001 4 9 COMA0110051 1 20010312 A 5320 12005803001 SILL EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 7922 120264 DURING 2C CHECK TASK 132-01Z, THE FUSELAGE RT FORWARD FLOORBEAM SILL WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCOR DANCE WITH EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001040900072 20010409 00072 SO 2001 4 9 COMA0110055 1 20010312 A 5210 12036410001 BEAM EMB 120 EMB120RT SO PAX DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 21213 120264 DURING 2C CHECK TASK 811-02Z, THE PAX DOOR AFT LATERAL BEAM WAS FOUND CRACKED. THE PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 SRM 52-10-02, FIGURE 201. 2 L 7 2 4T RT A31SO 2001040900073 20010409 00073 EU 2001 4 9 20010305CW001 1 20010128 A 2440 LDG150Y4 CONTACTOR BRAERO DH125 BAE125800A 1500285 EU GARRTT TFE731 TFE731* 01518 WP GROUND POWER OPEN D UG8A O OTHER O OTHER NR NOT REPORTED 1 GL 23 941HC 3258 NA0458 WITH BATTERY SWITCH ON, NO START POWER. APPARENT CAUSE: NO DC POWER TO START POWER BUSS. CORRECTIVE ACTION: REPLACED GROUND POWER CONTRACTOR, OPERATIONAL CHECKED GOOD. AC RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A3EU E6WE 2001040900074 20010409 00074 SW 2001 4 9 02210176 1 20010221 A 7603 SCREW SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP LT ENGINE LOOSE B HKGR A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 SW 17 255AM TC331E P54131 PILOT REPORTED THAT LT ENGINE RPM CONTINUED TO DECREASE IN FLIGHT. ON APPROACH, ELECTED TO SHUT THE LT ENGINE DOWN. U PON INSPECTION, IT WAS DETERMINED THAT THE LT ENGINE RPM ADJUSTING SCREW SELF LOCKING INSERT WAS LOOSE, ALLOWING SCREW TO BACK OFF DUE TO ENGINE VIBRATION. UPDATE:THE LOWER OUTER SHAFT LEVER WAS REPAIRED BY REPLACING THE SELF LOCKING THR EADED INSERT, AND INSTALLING A NEW SCREW. 2 L 7 2 4T 4 T RT A8SW E4WE 2001040900076 20010409 00076 NE 2001 4 9 20010305CW003 2 20010122 A 8520 BEARING CVAC 440 C131D 2422750 WP PWA R2800 R2800CB16 52026 NE NR 8 CYLINDER DETERIORATED I X3FB K NONE O OTHER IN INSP/MAINT 1 SO 15 145GT 1200 537804 NK510299 AFTER TAKEOFF, CLIMBING THROUGH 2,200 FT CREW NOTICED OIL TEMPERATURE RISING AND OIL PRESSURE DECREASING. ENGINE SHUTDO WN/FEATHERED, RETURNED TO AIRPORT. INSPECTION REVEALED BEARING MATERIAL IN OIL SCREENS. ENGINE REMOVED FROM SERVICE FO R REPAIRS. 2 L 7 2 4R 4 R 6A6 5E8 2001040900079 20010409 00079 EA 2001 4 9 COMA0160309 1 20010308 A 2750 7805013 SELECTOR VALVE CNDAIR CL600 CL6002B19 EA COCKPIT FAILED A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 796CA 3973 7338 FLAPS FAIL MESSAGE. REPLACED THE FLAP SELECTOR LEVER. 2 L 7 2 4F RT A21EA 2001040900080 20010409 00080 EA 2001 4 9 COMA0160310 1 20010304 A 5320 6003603032 DOUBLER CNDAIR CL600 CL6002B19 EA FRAME CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 796CA 3949 7338 FS 718.00 RT AFT DOUBLER CRACKED. REMOVED AND REPLACED RT AFT DOUBLER P/N 600-36030-32 IAW CANADAIR REO 601R-53-61-193 REV A. 2 L 7 2 4F RT A21EA 2001040900083 20010409 00083 SO 2001 4 9 COMA0110042 1 20010309 A 3010 BOOT EMB 120 EMB120RT SO WING DAMAGED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 264CA 120256 WING DE-ICE FAIL WARNING. REPAIRED HOLES IN WING LEADING EDGE DE-ICE BOOTS, USING PATCH KIT. 2 L 7 2 4T RT A31SO 2001040900084 20010409 00084 SO 2001 4 9 COMA0110043 1 20010310 A 2121 EVAC2322C2AMDT FAN EMB 120 EMB120RT SO CABIN FAILED A COMA D RETURN TO BLOCK B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 269CA 22894 120263 LAVATORY SMOKE DETECTOR ACTIVATED, SMOKE SMELL IN COCKPIT. REPLACED THE LEFT HAND GROUND COOLING FAN. 2 L 7 2 4T RT A31SO 2001040900085 20010409 00085 NE 2001 4 9 20010313CW002 2 20010204 A 7321 32447556 FUEL CONTROL BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A60A 52043 NE RT ENGINE FAILED E CTUA K NONE O OTHER IN INSP/MAINT 1 GL 21 553R 2832 BB589 PCE80439 PILOT CALLED IN AND REPORTED FLUCTUATION OF FUEL AND TORQUE INDICATION ON RIGHT ENGINE. RETURNED TO BASE AND MONITORED ENGINE PARAMETERS, SHUT DOWN RIGHT ENGINE WHEN UNABLE TO CONTROL TORQUE SETTINGS. ON INSPECTION FOUND BEARING FAILED ON FUEL CONTROL UNIT, WAS THE FRONT BEARING ON DRIVESHAFT,PN 2525501. TEARDOWN REPORTED BEARING WASHED OUT/ LUBRICANT WAS LOST THROUGH SEAL. 1 L 7 2 4T 4 T A24CE E4EA 2001040900086 20010409 00086 CE 2001 4 9 20010215CW001 1 20010111 A 3000 1013810125 VALVE BEECH B300 B300 1159232 CE PWA PT6 PT6* 52043 EA BRAKE DEICE SYST INOPERATIVE B LX5R O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 GL 19 991LL 348 223 FL142 LT BRAKE DE-ICE LIGHT NOT ILLUMINATING. LIGHT SYSTEM / SWITCH IS INOPERATIVE. 2 L 7 2 4T 3 T RT A24CE E2NE 2001040900087 20010409 00087 EA 2001 4 9 COMA0160308 1 20010310 A 5553 600210615 BUSHING CNDAIR CL600 CL6002B19 EA VERTICAL STAB OUT OF POSITION A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 719CA 6311 7253 RT VERT STAB BUSHING IS MIGRATED AT HORIZONTAL STAB ATTACH POINT. REMOVED MIGRATED BUSHING. INSTALLED BUSHING P/N 600- 21061-7 (THAT WAS MACHINED IAW WVAC EO 601R-55-2291) IAW CRJ AMM 20-26-00-910-803. REAMED BUSHING IAW DWG 600-21029. 2 L 7 2 4F RT A21EA 2001040900088 20010409 00088 EA 2001 4 9 WVBA2001011 2 20010220 A 8520 CAMSHAFT PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA ENGINE DAMAGED E WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 792FC 382 382 317552108 RL159361A DURING INSPECTION, METAL CONTAMINATION WAS DISCOVERED IN OIL FILTER. A CHECK OF VALVELIFT WAS DONE AND IT WAS DISCOVERE D THAT NR5 AND NR6 INTAKE LOBES WERE EXCESSIVE. NR 6 CYLINDER WAS REMOVED AND DAMAGE OBSERVED ON THE CAM LOBES AND TAPP ET FOLLOWERS. NOTE: THIS IS THE 15TH ENGINE IN 3 YEARS. 1 L 7 2 3O 3 O A20SO E14EA 2001040900090 20010409 00090 EU 2001 4 9 GXPA0102 1 20010206 A 7921 15441062 COOLER AMD FALC20 FALCON20C5 2730107 EU GE CF700 CF7002D2 30010 NE NR 1 ENGINE LEAKING E GXPA K NONE O OTHER IN INSP/MAINT 1 GL 25 179GA 62 100 299103 DUE TO LOW OIL PRESSURE NR 1 ENGINE SHUT DOWN IN FLIGHT AND DIVERTED. FOUND NR 1 ENGINE FUEL / OIL COOLER LEAKING. RE MOVED AND REPLACED NR1 ENGINE FUEL / OIL COOLER. LEAK AND OPS CHECK . NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4F 4 F RT A7EU E7EA 2001040900091 20010409 00091 SO 2001 4 9 WVBA2001009 1 20010216 A 2140 93C31 COIL ELECTROSYS 17E243 PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HEATER INOPERATIVE E WVBA K NONE L NO TEST IN INSP/MAINT 1 AL 01 792FC 317552108 PILOT REPORTED FRONT HEATER INOPERATIVE. IT WAS FOUND THAT THE COIL WAS INOPERATIVE ON THE IGNITION UNIT. THE IGNITION UNIT WAS REPLACED, OPS CHECKED GOOD. 1 L 7 2 3O 3 O A20SO E14EA 2001040900093 20010409 00093 NM 2001 4 9 0100816637 1 20010126 A 5313 STRINGER BOEING 747 747251B 1384892 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 637US 23548 DURING M-CHECK, FOUND CORROSION ON INBOARD VERTICAL SURFACE OF STRINGER AT STATION 2203, STR 51 L. REPAIRED PER EA 66-1 80581. 2 L 7 4 4F A20WE 2001040900094 20010409 00094 NM 2001 4 9 0100826637 1 20010104 A 5314 KEELBEAM BOEING 747 747251B 1384892 NM FUSELAGE DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 637US 23548 DURING M-CHECK FOUND DAMAGE TO LOWER KEEL BEAM AT STATION 1325, RBL 5. REPAIRED PER EA 66-180576. 2 L 7 4 4F A20WE 2001040900095 20010409 00095 NM 2001 4 9 0100836716 1 20010209 A 5311 FRAME BOEING 747 747251F 1384898 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 616US 21120 DURING M-CHECK, FOUND CRACK AT LEFT SIDE INNER FRAME, AFT HOLE, STATION 2231, STR 25L. REPAIRED PER EA 67-165008. 2 L 7 4 4F A20WE 2001040900096 20010409 00096 NM 2001 4 9 0100846716 1 20010209 A 5330 SKIN BOEING 747 747251F 1384898 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 616US 21120 DURING M-CHECK, FOUND CORROSION UNDER FORWARD LOWER SKIN AT LT OUTFLOW VALVE, STATION 2184, STR 45L. REPAIRED PER EA 67 -165012. 2 L 7 4 4F A20WE 2001040900097 20010409 00097 NM 2001 4 9 0100856716 1 20010209 A 5314 KEELBEAM BOEING 747 747251F 1384898 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 616US 21120 DURING M-CHECK, FOUND CORROSION ON UPPER SURFACE OF KEEL BEAM LOWER STRUCTURE, STATION 1310 TO 1329. REPAIRED PER EA 67 -165004. 2 L 7 4 4F A20WE 2001040900098 20010409 00098 SW 2001 4 9 I7WAB1536 1 20010103 A 2910 2781032167 LINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE331* 01514 WP HYD SYSTEM CRACKED E I7WA K NONE O OTHER IN INSP/MAINT 1 NM 05 445MA AC687 LOSS OF HYDRULIC FLUID. CAUSE:HARD LINE CRACKED, GEAR UP PRESSURE LINE. PART CRACKED AT 90 DEGREE BEND. REPLACED LINE . 2 L 7 2 4T 3 T RT A8SW E2WE 2001040900100 20010409 00100 2001 4 9 WVBA2001012 4 20010220 A 2211 011033T COMPUTER PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA PITCH CONTROL UNSERVICEABLE E WVBA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 AL 01 4434D 317552020 AFTER INITIAL INSTALL AIRCRAFT WAS ON CHECK FLIGHT, IN ALTITUDE HOLD, AIRCRAFT PORPOISES. IT WAS DETERMINED THAT THE PI TCH COMPUTER WAS THE CAUSE. UNIT WAS REMOVED FOR ANALYSIS. 1 L 7 2 3O 3 O A20SO E14EA 2001040900101 20010409 00101 EA 2001 4 9 WVBA2001010 2 20010219 A 8520 LW19430 CAMSHAFT PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA ENGINE DAMAGED E WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 4082T 318152089 L424861A DURING INSPECTION, METAL CONTAMINATION WAS DISCOVERED IN OIL FILTER. A CHECK OF VALVELIFT WAS DONE AND IT WAS DISCOVERE D THAT NR5 AND NR6 INTAKE LOBES WERE EXCESSIVE. NR6 CYLINDER WAS REMOVED AND DAMAGE OBSERVED ON THE CAM LOBES AND TAPPE T FOLLOWERS. NOTE: THIS IS THE 14TH ENGINE IN 3 YEARS. LUBRICATION PRACTICES HAVE BEEN MONITORED/ POOR QUALITY CONTRO L ON NITRIDING. 1 L 7 2 3O 3 O A20SO E14EA 2001040900103 20010409 00103 NM 2001 4 9 CALA0100214 1 20010308 A 2611 2156604 SMOKE DETECTOR BOEING 757 757224 1384958 NM CARGO BAY FALSE INDICATION A CALA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 09 17133 9650 29282 BOTH CARGO FIRE BOTTLES WERE DISCHARGED AND AIRCRAFT WAS RETURNED TO GLA DUE TO A FIRE WARNING IN THE AFT CARGO COMPARTM ENT. THE AIRCRAFT LANDED SAFELY AND THE L-1 AND L-2 DOOR SLIDES WERE DEPLOYED TO EVACUATE THE PASSENGERS AS A PRECAUTION ARY MEASURE. THE EMERGENCY EVACUATION SLIDES OPERATED PROPERLY AND PASSENGERS EXITED THE AIRCRAFT WITHOUT INJURY. SUBSEQ UENT INVESTIGATION REVEALED NO EVIDENCE OF FIRE OR SMOKE. THE AIRCRAFT WILL BE FERRIED TO EWR FOR MAINTENANCE AND TROUBL ESHOOTING. *S/D* MAINTENANCE PERFORMED A SYSTEM TEST OF CARGO COMPARTMENT SMOKE DETECTION IAW MM 26-16-00 AND MM 26-01 -01 AND NO DEFECTS WERE NOTED. 2 L 7 2 4F RT A2NM 2001040900104 20010409 00104 NM 2001 4 9 CALA0100215 1 20010308 A 5311 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17329 23459 INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 807 BETWEEN STRINGER 27L AND 27R. A REPAIR WAS INSTALLED IAW SRM 53-00- 07. 2 L 7 2 4F RT A16WE 2001040900105 20010409 00105 NM 2001 4 9 CALA0100216 1 20010311 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 47332 23570 INSPECTION FOUND INTERCOSTAL CORRODED IN AFT BAGGAGE BIN AT STA 847 - 867, S25R. THE INTERCOSTAL WAS REMOVED AND REPLAC ED IAW SRM 51-10-1 AND 51-40-02. 2 L 7 2 4F RT A16WE 2001040900106 20010409 00106 NM 2001 4 9 20010312CW008 1 20010212 A 8011 35046194 CLUTCH BOEING 777 777* UTILUSE NM GE GE90 GE9090B NE ENGINE STARTER DESTROYED B LP3R O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 07 5035 2245 H2AKI 900187 IMPROPER INSTALLATION OF CLUTCH PAWL SPRING RETAINING RIVETS DURING LAST MAINT., RESULTED IN CLUTCH FAILURE AND DAMAGE T O ENGINE STARTER. NEW TOOLING, ASSEMBLY AND INSPECTION PRACTICES WILL BE IMPLEMENTED TO PREVENT RECURRENCE, FIELD EVALU ATION OF OTHER POSSIBLE UNIT AFFECTED. 2 L 7 2 4F 4 F RT T00001SE E00049EN 2001040900107 20010409 00107 WP 2001 4 9 CALA0100217 1 20010311 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14062 47863 INSPECTION FOUND A 2 INCH CRACK IN FLOORBEAM AT STA 1298, RT, APPROXIMATELY TEN INCHES FROM EXTERNAL SKIN JOINT. A REPA IR WAS INSTALLED IAW SRM 53-00-01, FIGURE 7. 2 L 7 3 4F A22WE 2001040900108 20010409 00108 NM 2001 4 9 CALA0100218 1 20010311 A 2910 AS154A04EE0500B HYDRAULIC LINE BOEING 757 757224 1384958 NM LT MLG LEAKING A CALA A UNSCHED LANDING K FLUID LOSS TO TAKEOFF 1 SW 09 17126 27566 THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM EWR. OVERRIDE WAS USED AND THE GEAR RETRACTED. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT MAIN GEAR TRUCK PRESSURE LINE LEAKING. THE LINE WAS REPLACED USING A FLEX HOSE. A DIP WAS ISSUED TO REPLACE WITH A RIGID LINE AT 1200 HOURS OR 500 FLIGHTS, WHICHE VER COMES FIRST. A GEAR SWING WAS PERFORMED, HYDRAULIC FUSE WAS RESET, AND SYSTEM TESTED GOOD IAW MM 32-31-00. 2 L 7 2 4F RT A2NM 2001040900109 20010409 00109 WP 2001 4 9 CALA0100219 1 20010309 A 3230 59516395001 CYLINDER DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A CALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SW 09 34838 42221 49634 THE NLG DID NOT EXTEND ON APPROACH TO IAH. THE NOSE LIGHT INDICATED UNSAFE AND THE NLG INDICATION PIN WAS RETRACTED. R AN UNSAFE GEAR, GEAR HANDLE DOWN CHECKLIST DURING A GO AROUND AND THE GEAR EXTENDED WITH SAFE INDICATION. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NLG BUNGEE CYLINDER AT FAULT. THE NLG BUNGEE CYLINDER WAS REMOVED AND R EPLACED IAW MM 32-32-07 AND THE NOSE GEAR FORWARD DOORS WERE RIGGED IAW MM 32-22-01. NLG EXTENSION AND RETRACTION CHECK S WERE GOOD. 2 L 7 2 4F A6WE 2001040900110 20010409 00110 NM 2001 4 9 CALA0100220 1 20010312 A 5320 STRAP BOEING 737 7373T0 1384582 NM CARGO BAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 47332 23570 INSPECTION FOUND AFT BAGGAGE BIN CARGO DOOR JAMB METAL STRAP CORRODED ALONG SCREW HOLES AT LOWER JAMB AREA BETWEEN BS 78 7-867, S25R. THE STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001040900112 20010409 00112 EU 2001 4 9 RAIA00103009 1 20010314 A 2434 1030032 SENSOR AEROSP ATR72 ATR72202 8680940 EU RT ENGINE FAILED A RAIA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 CE 03 723TE 7397 283 7170-STL- RIGHT DC GENERATOR FAULTED IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED RIGHT HALL EFFECT SENSOR. 2 H 7 2 4T RT A53EU 2001040900113 20010409 00113 SO 2001 4 9 RAIA00103010 1 20010314 A 3610 BLEED VALVE EMB 145 EMB145 SO BLEED SYSTEM FAILED A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 03 804HK 145082 5256-GSP- AFTER TAKEOFF, LAV SMOKE EICAS MESSAGE APPEARED WITH VISIBLE SMOKE IN THE CABIN. FLIGHT RETURNED TO GSP. MAI NTENANCE INSPECTED AND PERFORMED GROUND RUN, MAINTENANCE DETERMINED CAUSE AS ENGINE BLEED AIR FOULED. MAINTENANCE CLEAR ED BLEED AIR SYSTEM, NO DEFECTS NOTED ON ENGINE RUNS. 2 L 7 2 4F RT T00011AT 2001040900114 20010409 00114 NM 2001 4 9 20010315CW003 1 20010213 A 2761 654494715 HOUSING BOEING 737 737* NM SPOILER ACTUATOR CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 HOUSING IS CRACKED NEXT TO THE EXTEND PORT. 2 L 7 2 4F RT A16WE 2001040900115 20010409 00115 NM 2001 4 9 AWXA0001335 1 20010214 A 3520 OXYGEN MASK BOEING 737 7373Y0 1384671 NM CABIN FAILED A AWXA K NONE O OTHER CR CRUISE 1 WP 28 334AW 35926 7669 23748 IN PHX A FURTHER PRESSURIZATION CHECK WAS PERFORMED WITH NO DISCREPANCIES NOTED; THE CABIN PRESSURE WAS REPLACED AS A PR ECAUTION. TWO OXYGEN MASK PANELS FAILED TO DROP DURING EVENT. OXYGEN MASKS DEPLOYED DUE TO RAPID DEPRESSURIZATION; A R EPORT WAS GIVEN THAT THE FWD FLIGHT ATTENDANTS AND ROW 23 RT OXYGEN MASKS MAY HAVE FAILED TO DEPLOY. AFTER PASSENGER OX YGEN GENERATORS WERE REPLACED AND ALL OXYGEN MASKS WERE REPLACKED A TEST OF THE OXYGEN MASK MANUAL DEPLOYMENT SYSTEM WAS MADE AND ALL POSITIONS FUNCTIONED NORMALLY IAW AMM 35-22-00. NOTE: NOBODY WAS AT THE FWD FLIGHT ATTENDANTS POSITION WH EN THE EVENT OCCURRED; UNABLE AT THIS TIME TO CONFIRM IF ANYONE WAS SEATED AT ROW 23 RT. 2 L 7 2 4F RT A16WE 2001040900116 20010409 00116 EU 2001 4 9 C2XA01CL053 1 20010308 A 3231 S5397131700200 LINK AEROSP ATR42 ATR42320 8680930 EU RT MLG BROKEN A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 15816 105 CLE FLIGHT 3042 THE CREW REPORTED THE RIGHT MAIN GEAR DOOR HINGES BROKE AFTER TAKEOFF. THE AIRCRAFT DID AN AIR RETURN W ITH EMERGENCY DECLARED. MAINTENANCE INSPECTED AND FOUND THE RIGHT MAIN LANDING GEAR DOOR LINK ASSEMBLY BROKEN. THE LIN K ASSEMBLY WAS REPLACED ALONG WITH THE GEAR DOORS. THE DOORS WERE DAMAGED DUE TO THE LINK FAILURE. OPERATIONAL CHECKS WERE GOOD OF THE LANDING GEAR SYSTEM AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A53EU 2001040900117 20010409 00117 EU 2001 4 9 C2XA01CL054 1 20010308 A 3260 E0276ANOPO16 ANNUNCIATOR AEROSP ATR42 ATR42320 8680930 EU COCKPIT LOOSE A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 14825 170 CLE FLIGHT 3121 THE CREW REPORTED THE NOSE GEAR UNLOCK LIGHT FLICKERS ON SYSTEM 1 IN FLIGHT WITH GEAR RETRACTED. MAINTE NANCE FOUND NOSE GEAR SYSTEM 1 LIGHT SOCKET LOOSE. TIGHTENED THE SOCKET AND CLEANED THE NOSE GEAR PROXIMITY SENSORS. O PERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A53EU 2001040900118 20010409 00118 WP 2001 4 9 N879980 1 20010205 A 3240 95607887 BRAKE DOUG DC9 DC9* WP MLG DAMAGED B A3LD K NONE O OTHER IN INSP/MAINT 1 EA 25 AXLE NUT LOOSE DAMAGED BRAKE ASSEMBLY. NR 1 AND 2 STATORS DAMAGED. NR 1 AND 2 ROTORS DAMAGED. 5 OUT OF 7 SPRING CAPSU LES DAMAGED. CUSTOMER CLAIM OF: AXLE NUT LOOSE DAMAGED BRAKE ASSEMBLY. 2 L 7 2 4F A6WE 2001040900119 20010409 00119 WP 2001 4 9 ARWA0010305 1 20010314 A 5753 47544201 BOLT DOUG DC8 DC863F 302198F WP LT FLAP BROKEN A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING PREFLIGHT INSPECTION FOUND LT INBOARD FLAP TRACK BROKEN HANGER BOLT. REMOVED AND REPLACED LT INBOARD FLAP STA 97 TRACK HANGER BOLT IAW MM 27-51-3. OPERATIONAL CHECK OF THE FLAP SYSTEM FOUND NORMAL IAW MM 27-53-1. 2 L 7 4 4F 4A25 2001040900120 20010409 00120 NM 2001 4 9 CALA0100228 1 20010314 A 5230 PAN BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 47332 23570 INSPECTION FOUND A 3 INCH CRACK IN FORWARD CARGO DOOR PAN AT LOWER FORWARD STOP AND AFT LOWER PAN WAS GOUGED. THE FORWA RD LOWER AND AFT LOWER DOOR PANS WERE REPLACED IAW SRM 51-30-2. 2 L 7 2 4F RT A16WE 2001040900121 20010409 00121 NM 2001 4 9 CALA0100231 1 20010314 A 5230 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17329 23459 INSPECTION FOUND A 2 INCH CRACK IN FORWARD CARGO DOOR INNER SKIN. A REPAIR WAS INSTALLED IAW ECRA 5230-01604. 2 L 7 2 4F RT A16WE 2001040900122 20010409 00122 NM 2001 4 9 SCNA01018 1 20010225 A 3260 SWITCH BOEING 727 727259 138408J NM TAIL SKID LOOSE A SCNA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 289SC 20765 AFTER GEAR RETRACTION, TAIL SKID LIGHT REMAINED ILLUMINATED, FOLLOWED COM AND RETURNED TO POINT OF ORIGIN, MSP. THE TAI L SKID UP SWITCH S663 WAS FOUND LOOSE. TIGHTENED, CLEANED, AND TESTED, OPERATIONAL CHECKS GOOD. 2 L 7 3 4F A3WE 2001040900123 20010409 00123 NM 2001 4 9 SCNA01019 1 20010215 A 3350 6104789 BATTERY PACK BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 285SC 21676 DURING A MAINTENANCE LINE CHECK THE EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REMOVED AND REPLACED BATTERY POWER PA CK FOR THE AFT EXIT EMERGENCY LIGHTS, OPERATIONAL CHECKS GOOD. 2 L 7 3 4F RT A3WE 2001040900124 20010409 00124 NM 2001 4 9 SCNA01020 1 20010228 A 3350 10126215 LIGHT BOEING 727 727227 1384078 NM CABIN BROKEN A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 275AF 22092 DURING A MAINTENANCE INSPECTION THE EMERGENCY PATH LIGHTING WAS FOUND BROKEN AT THE L2 DOOR. REMOVED AND REPLACED THE L 2 DOOR EMERGENCY EXIT LIGHING ASSY. 2 L 7 3 4F A3WE 2001040900125 20010409 00125 NM 2001 4 9 SCNA01021 1 20010301 A 3350 10126215 LIGHT BOEING 727 727227 1384078 NM CABIN BROKEN A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 275AF 22092 EMERGENCY EXIT LIGHT ON LEFT REAR OVERWING DOOR CASE WAS FOUND BROKEN. REMOVED AND REPLACED EMERGENCY EXIT ASSEMBLY. 2 L 7 3 4F A3WE 2001040900126 20010409 00126 CE 2001 4 9 GLBA2001057 1 20010307 A 2430 WIRE BEECH 1900 1900D 1154162 CE COCKPIT LOOSE A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 195GL UE195 RETURN TO BLOCK - LEFT GENERATOR FELL OFF LINE. INSPECTED FOUND LOOSE WIRES ON DC PWR PANEL. OPS CHECKED GOOD. 2 L 7 2 4T RT A24CE 2001040900127 20010409 00127 EA 2001 4 9 COMA0160304 1 20010308 A 2742 83963 ACTUATOR CNDAIR CL600 CL6002B19 EA HORZ STAB MALFUNCTIONED A COMA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SO 01 967CA 1656 7134 STABILIZER TRIM WILL NOT REMAIN ENGAGED. REPLACED THE HSTA. 2 L 7 2 4F RT A21EA 2001040900128 20010409 00128 EA 2001 4 9 COMA0160306 1 20010308 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA T/E FLAP MALFUNCTIONED A COMA D RETURN TO BLOCK J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 01 964CA 6181 7129 FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT BPSU. 2 L 7 2 4F RT A21EA 2001040900129 20010409 00129 EA 2001 4 9 COMA0160307 1 20010308 A 2740 9960013 SWITCH CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTIONED A COMA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 01 958CA 7111 STABILIZER TRIM CAUTION MESSSAGE. REPLACED THE PILOTS PITCH TRIM DISCONNECT SWITCH. 2 L 7 2 4F RT A21EA 2001040900130 20010409 00130 WP 2001 4 9 MWEA010349 1 20010316 A 5220 5912995503 PAN DOUG DC9 DC914 3022034 WP EMERGENCY EXIT DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 HOLE IN EMERGENCY EXIT PAN AT STATION 525 APPROXIMATELY 4 INCHES BELOW LONGERON 11 LEFT. REMOVED SEAL DEPRESSOR AND PAN , LOCATED, DRILLED AND INSTALLED NEW PAN. 2 L 7 2 4F A6WE 2001040900131 20010409 00131 EU 2001 4 9 MALA010268 1 20010313 A 3020 CONNECTOR SAAB SF340 340B 7860101 EU LT ENGINE DIRTY A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 420XJ 420 ON FLIGHT 2962, LEFT INTAKE HEAT INOP. CREW DID ORH-RESET SWITCH STILL INOP. ON RETURN APPROACH TO DTW STARTED WORKING AGAIN. AIR RETURN TO DTW. MAINTENANCE REMOVED AND CLEANED AND RESECURED LT LOWER DUCT CANNON PLUG. RAN A/C FOR 30 MI NUTES ON THE GROUND. ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2001040900132 20010409 00132 EU 2001 4 9 MALA010269 1 20010314 A 8012 START VALVE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE RT ENGINE DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 31XJ 031 ON FLIGHT 2871, RT AIR VALVE LIGHT ILLUMINATED IN FLIGHT. CYCLED ON AND OFF CONTINUOUSLY-NO TORQUE OR ITT CHANGES OBSER VED. AIR RETURN TO DTW. MAINTENANCE REPLACED RT START BLEED VALVE S/N OFF AEX10047, S/N ON AEX10322. 2 L 7 2 4T 4 T RT A52EU E8NE 2001040900133 20010409 00133 EU 2001 4 9 MALA010270 1 20010314 A 3020 THERMISTER SAAB SF340 SF340A 7850100 EU RT INTAKE FAILED A MALA O OTHER N FALSE WARNING DE DESCENT 1 GL 15 98XJ 098 DURING DESCENT ON FLIGHT 3356 AFTER PLACING RT ENGINE ANTI-ICE SWITCH ON RT INTAKE LIGHT ILLUMINATED. RECYCLED AS PER O RH AND LIGHT ILLUMINATED AGAIN. RT INTAKE LIGHT REMAINED ON FOR APPROXIMATELY 5 MINUTES THEN WENT OUT. MAINTENANCE SWA PPED THERMISTORS IN DE-ICE CONTROL AND RESECURED GROUND WIRE. GROUND RAN A/C 45 MINUTES IAW SF340 AMM. OPS CHECK GOOD ON RT ENGINE ANTI-ICE SYSTEM. 2 L 7 2 4T RT A52EU 2001040900134 20010409 00134 SO 2001 4 9 GLBA2001054 1 20010306 A 5240 SWITCH EMB 120 EMB120RT SO SERVICE DOOR OUT OF ADJ A GLBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 01 108UX 120108 ABORTED T/O - SERVICE DOOR ANNUNICATOR ILLUMINATED. INSTALLED NEW SCREW/JAM-NUT ON DOOR SWITCH, OPS CHECKED GOOD. 2 L 7 2 4T RT A31SO 2001040900136 20010409 00136 CE 2001 4 9 20010320CW014 1 20010209 A 3241 40911 GENERATOR LEAR 35 35LEAR 5170600 CE GARRTT TFE731 TFE73122B 01518 WP NR 2 BRAKE MALFUNCTIONED E BSYA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 07 4358N 065 P74214 RT INBOARD ANTI-SKID FAILED. ABORTED TAKE OFF BECAUSE OF OVER SENSITIVE STEERING. FOUND NR 2 ANTI-SKID GENERATOR DEFEC TIVE. REMOVED AND REPLACED. OPS CHECKED GOOD. 2 L 7 2 4F 4 F A10CE E6WE 2001040900137 20010409 00137 2001 4 9 20010320CW015 4 20010209 A 2330 KMA20066102403 AUDIO PANEL BEECH 58 58 1152740 CE CONT O520 IO520C 17032 SO COCKPIT SMOKE E BSYA K NONE O OTHER IN INSP/MAINT 1 GL 07 2892W TH389 02221E AFTER LANDING , HAD SMOKE COMING OUT FROM AUDIO PANEL. HAD AVIONIC SHOP REMOVE AND REPLACED. AUDIO PANEL OPS CHECKS GO OD. 1 L 7 2 3O 3 O 3A16 E5CE 2001040900139 20010409 00139 EA 2001 4 9 SWIA972438 1 20010318 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT ACTIVATED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 412SW 7101 PASSENGER OUTER DOOR LATCH MESSAGE IN FLIGHT OVER DILLON. LANDED IDA. MESSAGE WENT OUT ON ROLLOUT. GROUND CREW IN IDA CLOSE DOOR AND VISUALLY CONFIRM LATCHED AND CONTINUED TO SLC. FLIGHT ATTENDANT CAN''T COMPLETELY CLOSE DOOR. OPERATED PASSENGER DOOR HANDLE. INDICATION AND OPERATION GOOD. UNABLE TO DUPLICATE SQUAWK. 2 L 7 2 4F RT A21EA 2001040900140 20010409 00140 EA 2001 4 9 20010320CW016 2 20010226 A 7414 6350 ROTOR SHAFT PIPER PA32 PA32R300 7103213 SO LYC O540 IO540K1A5 41532 EA MAGNETO CRACKED E GSBA K NONE O OTHER IN INSP/MAINT 1 AL 01 8540F 292 32R7780108 DURING ENGINE RUNUP THE PILOT NOTICED A 250 RPM DROP DURING MAG CHECK AT 2000 RPM. THE ENGINE WAS ALSO RUNNING VERY ROU GH ON THIS ONE MAG. MAG INSPECTION REVEALED THAT THE ROTOR SHAFT WAS CRACKED IN TWO AT THE BASE OF THE SLOT IN THE SHA FT. 1 L 7 1 3O 3 O A3SO 1E4 2001040900141 20010409 00141 EA 2001 4 9 20010320CW017 2 20010226 A 7414 6351 ROTOR SHAFT PIPER PA32 PA32R300 7103213 SO LYC O540 IO540K1A5 41532 EA MAGNETO CRACKED E GSBA K NONE O OTHER IN INSP/MAINT 1 AL 01 8540F 457 32R7780108 DURING ENGINE RUNUP, PILOT NOTICED 250 RPM DROP DURING MAG CHECK AT 2000 RPM. THE ENGINE WAS ALSO RUNNING VERY ROUGH ON ONE MAG. MAG INSPECTION REVEALED THAT THE ROTOR SHAFT WAS CRACKED IN TWO AT THE BASE OF THE SLOT IN THE SHAFT. 1 L 7 1 3O 3 O A3SO 1E4 2001040900142 20010409 00142 2001 4 9 GLBA2001050 4 20010303 A 2210 DAMPENER BEECH 1900 1900D 1154162 CE AUTOPILOT SYS MALFUNCTIONED A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 01 247GL UE247 YAW DAMP ENGAGED ON T/O ROLL. COULD NOT DUPLICATE FAILURE. RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 2001040900143 20010409 00143 CE 2001 4 9 GLBA2001051 1 20010303 A 2434 23078019 STARTER GEN BEECH 1900 1900D 1154162 CE LT ENGINE FAILED A GLBA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 CE 01 195GL 5900 5 UE195 LEFT DC GENERATOR ANNUCIATOR ILLUMINATED INFLIGHT WOULD NOT RESET. REPLACED STARTER-GEN, OPS CHECKED GOOD. 2 L 7 2 4T RT A24CE 2001040900144 20010409 00144 CE 2001 4 9 GLBA2001052 1 20010304 A 7712 1143800653 INDICATOR BEECH 1900 1900D 1154162 CE COCKPIT INOPERATIVE A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 01 122UX 10 UE122 RIGHT TORQUE INDICATOR FROZE ON T/O ROLL. REPLACED TORQUE INDICATOR. 2 L 7 2 4T RT A24CE 2001040900145 20010409 00145 NM 2001 4 9 20010306CW002 1 20010130 A 2760 656952211 HOUSING BOEING 737 737 UTILSYS NM SPOILER ACTUATOR CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 38400 38400 HOUSING IS CRACKED AROUND NUT FLANGE AREA. FATIGUE, STRESS AND / OR HIGH TSO HOURS ON HOUSING WAS PROBABLE CAUSE. 2 L 7 2 4F RT A16WE 2001040900146 20010409 00146 WP 2001 4 9 CALA0100210 1 20010306 A 5320 FLOOR SUPPORT DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14062 47863 INSPECTION FOUND GALLEY G6 O/B FLOOR SUPPORT BEAM CORRODED AT STA Y = 1902-2007, X = 48R. THE FLOOR SUPPORT BEAM WAS RE MOVED AND A NEW SECTION WAS INSTALLED IAW GMM 10-900-01, SRM 53-16-01, AND ECRA 5100-01844. 2 L 7 3 4F A22WE 2001040900147 20010409 00147 NM 2001 4 9 CALA0100211 1 20010306 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND A .25 INCH CRACK IN FLOORBEAM AT STA 520, RBL 45.5. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-04105 AND EA 04-5310-0669. 2 L 7 2 4F RT A16WE 2001040900148 20010409 00148 CE 2001 4 9 20010321CW001 1 20010209 A 3244 JUN86650 TIRE LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE7313D WP MLG FLAT B DELR K NONE O OTHER IN INSP/MAINT 1 CE 03 550HG 10 10 083 UPON LANDING, CREW NOTICED ON POST FLIGHT NR 2 TIRE, FLAT SPOTED. DISPATCHED MAINTENANCE TECH. WITH THE APPROPRIATE PA RTS, REMOVED AND REPLACED NR2 MAIN WHEEL ASSEMBLY. RETURNED AC TO SERVICE. 2 L 7 2 4F 4 F A10CE E6WE 2001040900149 20010409 00149 SO 2001 4 9 C2XA01TY046 1 20010318 A 5751 14569009407 BRACKET EMB 145 EMB145LR 3260212 SO AILERON GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13978 145180 TYS DURING A SCHEDULED INSPECTION THE LEFT HAND AILERON ATTACHMENT BRACKET WAS FOUND TO BE GOUGED. MAINTENANCE REPAIRE D THE BRACKET IAW EMB GST-085/01, THE REPAIR WAS FOUND SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF I NSPECTION. 2 L 7 2 4T RT T00011AT 2001040900150 20010409 00150 SO 2001 4 9 C2XA01TY047 1 20010318 A 7110 14576608047 SKIN EMB 145 EMB145LR SO COWLING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13978 145180 TYS DURING A SCHEDULED INSPECTION THE LEFT HAND UPPER COWLING SKIN WAS FOUND CRACKED JUST FORWARD OF THE CENTER HINGE P OINT. MAINTENANCE REPAIRED THE SKIN IAW EMB GST-0821/01, THE REPAIR WAS FOUND TO BE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2001040900151 20010409 00151 WP 2001 4 9 CALA0100213 1 20010308 A 5320 WEB DOUG DC9 DC982 3022082 WP TORQUE BOX CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14889 49118 INSPECTION FOUND FORWARD SIDE OF AFT CARGO TORQUE BOX WEB CORRODED. THE TORQUE BOX WEB AND ATTACHMENTS WERE REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-5, 51-10-4, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 2001040900152 20010409 00152 NM 2001 4 9 01FDEA00179 1 20010308 A 2612 WARNING LIGHT BOEING 727 7272S2F 1384O81 NM COCKPIT FALSE ACTIVATION A FDEA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SO 25 211FE 22933 NR 2 ENG FIRE WARN LIGHT/BELL. INSP ENG FIRE WARN ELEMENTS, FUEL HEATER, PLUMBING, AND BLD AIR DUCTS. NO DEFECTS NOTED . RAN NR 2 ENG PER JET RUN HDBK. COULD NOT DUPLICATE DISCREPANCY. 2 L 7 3 4F A3WE 2001040900155 20010409 00155 EA 2001 4 9 WVBA2001013 2 20010221 A 8520 LW19340 CAMSHAFT PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA ENGINE DAMAGED E WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 300ED 703 703 317852008 L521861A DURING INSPECTION METAL CONTAMINATION WAS DISCOVERED IN OIL FILTER. A CHECK OF VALVE LIFT WAS DONE AND IT WAS DISCOVERE D THAT NR5 AND NR6 INTAKE LOBES WERE EXCESSIVE. NR6 CYLINDER WAS REMOVED AND DAMAGE OBSERVED ON THE CAM LOBES AND TAPPE T FOLLOWERS. NOTE: THIS IS THE 16TH ENGINE IN 3 YEARS. 1 L 7 2 3O 3 O A20SO E14EA 2001040900156 20010409 00156 SO 2001 4 9 C2XA01TY048 1 20010318 A 5311 14524792003 FRAME EMB 145 EMB145LR SO FUSELAGE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13978 145180 TYS DURING A SCHEDULED INSPECTION, FRAME 64 LOCATED INSIDE OF CARGO BAY WAS FOUND CHAFED. MAINTENANCE REPAIRED THE DAM AGED AREA IAW EMB GST-0812/01, THE REPAIR WAS FOUND TO BE SATISFCATORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION O F INSPECTION. 2 L 7 2 4T RT T00011AT 2001040900165 20010409 00165 NM 2001 4 9 COOSDR00032 1 20010215 A 3211 652165127 FITTING BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE LT WING CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 EA 25 8887Z 21856 INSPECTION REPORTED A CORRODED FORWARD SUPPORT TRUNNION BEARING FITTING ON THE LEFT SIDE OF THE AIRCRAFT. 2 L 7 3 4F 4 F A3WE E2EA 2001040900166 20010409 00166 WP 2001 4 9 MWEA010354 1 20010316 A 5210 39570871 PAN DOUG DC9 DC914 3022034 WP PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FORWARD PAX DOOR EXTERIOR HANDLE RECESS PAN IS CRACKED AB5. REMOVED RECESS PAN, LOCATED DRILLED AND INSTALLED NEW RECES S PAN. 2 L 7 2 4F A6WE 2001040900167 20010409 00167 EU 2001 4 9 DHL2001362007 1 20010306 A 2760 SPOILER AIRBUS 300 A300B4103 3930104 EU RT WING MALFUNCTIONED A DHLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 362DH 84 DURING FLIGHT CONTL CHK, RT SPOILER ONLY INDICATES 7 DEG DEFLECTION. TRANSFERRED TO DMI 4626 PER MEL 27-15-01-1 CAT B, SPECIAL PROCEDURE COMPLIED WITH. 2 L 7 2 4F RT A35EU 2001040900172 20010409 00172 NM 2001 4 9 MWEA010315 1 20010312 A 5270 TARGET DOUG MD88 MD88 3023688 NM CARGO BAY OUT OF ADJ A MWEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 31 701ME 49760 AFT CARGO DOOR LIGHT ILLUMINATED AFTER NUMBER 2 ENGINE START. ADJUSTED AFT CARGO DOOR PROXIMITY SWITCH TARGET. 2 L 7 2 4F RT A6WE 2001040900173 20010409 00173 2001 4 9 UPS01235272 4 20010313 A 3421 25873351112 GYRO BOEING 727 727173C 1384059 NM COCKPIT FAILED A IPXA D RETURN TO BLOCK I FLT. ATTITUDE INST. TX TAXI/GRND HDL 1 SO 01 938UP 19506 INSPECTION TYPE:N/A (BTB) DURING TAKEOFF INITIAL ACCELERATION F/O''S EADI BLANKED. REPLACED NR 2 VERT GYRO PER BMM 34-2 2-21. NOTE: THIS SAME NR 2 VG WAS REPLACED ON INB FLT FOR A 5 DEGREE ROLL. THE S/N REMOVED FROM BTB IS 81144914, THE P IREP DEBRIEF, INDICATED THE EADI BLANKED WHEN A/C WAS TURNED OR BRAKED DURING OUTBOARD TAXI. A/C DEPARTED WITHOUT FURTH ER PROBLEMS. 2 L 7 3 4F A3WE 2001040900175 20010409 00175 NM 2001 4 9 UPS01535270 1 20010312 A 2120 DUCT BOEING 757 75724APF 1384969 NM RT AC PACK LOOSE A IPXA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 402UP 23724 INSPECTION TYPE:N/A, DURING CRUISE (33K) ALT WARNING HORN SOUNDED. CABIN ALTITUDE WAS CLIMBING AT 300 FT PER MINUTE. M AN CONTROL DID NOT STOP CABIN FROM CLIMBING. REGAINED CONTROL TURNING ON LEFT PACK. WITH BOTH PACKS OPERATING LT PACK READS 44 PSI, RIGHT PACK READS 37 PSI. FOUND RIGHT PACK OUTLET DUCT LOOSE. RECONNECTED DUCT, PERFORMED WORK WITH REFER ENCE TO M/M 21-51-00. OPS AND LEAK CHECKS GOOD. OK FOR CONTINUED SERVICE. 2 L 7 2 4F RT A2NM 2001040900176 20010409 00176 WP 2001 4 9 MWEA010314 1 20010307 A 5240 591142341 SERVICE DOOR DOUG DC9 DC914 3022034 WP LAV DOOR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 LAV SERVICE DOOR WILL NOT CLOSE. REPAIRED LAV SERVICE AREA AND REINSTALLED SERVICE DOOR. 2 L 7 2 4F A6WE 2001040900177 20010409 00177 WP 2001 4 9 ARWA0010304 1 20010313 A 2920 HYDRAULIC LINE DOUG DC8 DC863 302198A WP HYDRAULIL SYS LEAKING A ARWA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 19 345JW 46042 IN TOP OF CLIMB LOSS OF HYDRAULIC FLUID AND PRESSURE DOWN TO THE STAND-PIPE SLOWLY. FOLLOWED EMERGENCY CHECK LIST. AIR CRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED PRESSURE LINE TO AUXILIARY PUMP OPERATIONAL CHECK IAW MM 29-0-3 OPS NORMAL, NO LEAKS NOTED. 2 L 7 4 4F 4A25 2001040900178 20010409 00178 EU 2001 4 9 01FDEA00208 1 20010317 A 5270 WARNING LIGHT AIRBUS 310 A310222 3930315 EU COCKPIT ILLUMINATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 422FE 346 LWR ACCESS DOOR OPEN LIGHT LIGHT CAME ON DURING FLT. RELEASE PER MEL 52-9. 2 L 7 2 4F RT A35EU 2001040900184 20010409 00184 SO 2001 4 9 C2XA01TY042 1 20010318 A 4910 14535770401 COWLING EMB 145 EMB145LR SO APU GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13978 145180 TYS DURING A SCHEDULED INSPECTION THE APU COWLING UPPER PROFILE WAS FOUND TO BE BENT AND GOUGED. MAINTENANCE REMOVED A ND REPLACED THE PROFILE IAW EMB-GST-0801/01, REPAIR WAS SATISFACTORY. AIRCRAFT WILL BE RELEASED FOR SERVICE UPON COMPLE TION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2001040900185 20010409 00185 EU 2001 4 9 010093232 1 20010227 A 3230 FITTING AIRBUS 320 A320211 3930320 EU RT MLG CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 332NW 319 DURING L-CHECK FOUND CRACK ON RIGHT HAND MAIN LANDING GEAR DOOR ACTUATOR FITTING. REPAIRED PER EA 32-181770. 2 L 7 2 4F RT A28NM 2001040900186 20010409 00186 NM 2001 4 9 0100946637 1 20010126 A 5320 STRAP BOEING 747 747251B 1384892 NM BULKHEAD CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 637US 23548 DURING M-CHECK FOUND CORROSION ON BULKHEAD SPLICE STRAP AT BS 400. REPAIRED PER EA 66-181942. 2 L 7 4 4F A20WE 2001040900187 20010409 00187 SO 2001 4 9 C2XA01TY043 1 20010318 A 5320 14522460011 GUSSET EMB 145 EMB145LR SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13978 145180 TYS DURING A SCHEDULED INSPECTION THE FLOOR STRUCTURE DIGITAL GUSSET LOCATED JUST AFT OF THE COCKPIT DOORWAY, WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE DIGITAL GUSSET IAW EMB-145 SRM 51-40-03 AND EM B-145 CMP 51-21-06, REPAIR WAS SATISFACTORY. AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2001040900188 20010409 00188 WP 2001 4 9 ARWA0010306 1 20010318 A 2910 NAS1611112 SWIVEL DOUG DC8 DC863F 302198F WP RT AILERON LEAKING A ARWA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 19 661AV 45969 AT 1245Z ON CLIMBOUT HYD SYS QTY LOSS FLUID DOWN TO 5 GALLONS. HYD EMERGENCY CK LIST COMPLETED, ABNORMAL LANDING CK LIS T COMPLIED WITH AND COMPLETED. FOUND RT AILERON SWIVEL GLAND PORT LEAKING, REPACKED IAW MM 20-60-0 SERVICED FLUIDS IAW MM 12-00-1, OPERATIONAL AND LEAK CHECK IAW 27-11-6. NO DEFECTS NOTED. 2 L 7 4 4F 4A25 2001040900189 20010409 00189 SO 2001 4 9 C2XA01TY044 1 20010318 A 5320 14522459003 ANGLE EMB 145 EMB145LR SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13978 145180 TYS DURING A SCHEDULED INSPECTION THE RIGHT OMEGA BEAM RAMP ANGLE BETWEEN FRAMES 19 AND 20 WAS FOUND BENT AND CORRODED. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW EMB-145 SRM 51-40-02, REPAIR WAS SATISFACTORY. AIRCRAFT WILL BE R ELEASED FOR SERVICE UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2001040900193 20010409 00193 EA 2001 4 9 JBXA000254 1 20010307 A 2750 FLAP CNDAIR CL600 CL6002B19 EA WINGS FAILED A JBXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 05 582ML 7322 FLAPS FAIL MESSAGE WHEN FLAPS SELECTED TO 45 DEGREES LEFT AND RIGHT FLAPS REMAIN AT 30 DEGREES. CYCLED FLAP C/B''S AND PERFORMED OPS CHECK IAW CRJ AMM 27-51-05. ALL OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2001040900194 20010409 00194 WP 2001 4 9 TWAA0104401 1 20010307 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INTERMITTENT A TWAA K NONE O OTHER CR CRUISE 1 CE 05 929TW 48014 THE EMERGENCY EXIT LIGHTS AT THE REAR OF THE AIRCRAFT WERE REPORTED TO FLICKER IN FLIGHT. MAINTENANCE FOUND THE EMERGEN CY LIGHTS OPERATED NORMALLY PER MAINT MANUAL 33-51-0. CHECK-C 3-30-00 STL. 2 L 7 2 4F A6WE 2001040900195 20010409 00195 WP 2001 4 9 TWAA0104402 1 20010307 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INTERMITTENT A TWAA K NONE O OTHER CR CRUISE 1 CE 05 914TW 49185 THE FIRST SECTION OF CABIN EGRESS LIGHTS REPORTED TO INTERMITTENTLY STAY ILLUMINATED. RESET THE EMERGENCY LIGHT ARM AND CHARGE CIRCUIT BREAKER AND LIGHTS OPERATED NORMALLY. CHECK-C 2-13-01 STL. 2 L 7 2 4F A6WE 2001040900196 20010409 00196 WP 2001 4 9 TWAA0104403 1 20010307 A 3350 58222 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A TWAA K NONE O OTHER CR CRUISE 1 CE 05 914TW 49185 THE EGRESS LIGHTS ON CABIN FLOOR AND AT THE LEFT SIDE NUMBER 2 CABIN DOOR OCCASIONALLY ILLUMINATED IN FLIGHT. REPLACED THE BATTERY PACK. CHECK-C 2-13-01 STL. 2 L 7 2 4F A6WE 2001040900197 20010409 00197 NM 2001 4 9 TWAA0104404 1 20010306 A 5210 DOOR BOEING 757 7572Q8 1384972 NM L4 DOOR DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 703TW 27620 ENGINEERING REQUESTED A PERMANENT REPAIR TO A DENT JUST FWD AND BELOW THE LEFT SIDE NUMBER 4 CABIN DOOR, STA 1610 AND ST RINGER 18L. INSTALLED AN EXTERNAL DOUBLER 8 IN BY 10 INCHES USING BLIND FASTENERS PER SRM 53-00-01. CHECK-C 9-27-99 LA X. 2 L 7 2 4F RT A2NM 2001040900198 20010409 00198 NM 2001 4 9 PCAA0103019 1 20010316 A 2433 TRANSFORMER DHAV DHC8 DHC8102 2809003 NM EE BAY DEFECTIVE A PCAA K NONE O OTHER CL CLIMB 1 EA 13 830EX 155 PHL-FLIGHT 3722 EMERGENCY LIGHTS FLASH ON AND OFF DURING CLIMB (ALL LIGHTS FLASH DIMLY). MAINTENANCE TROUBLESHOT AND FO UND NR 2 TRANSFORMER RECTIFIER UNIT LOAD VALUE LOW. NR 2 TRU, NR 2 PROPELLER BRUSH BLOCK AND 1 RT PROP HEATER LEAD REPL ACED DUE TO VOLTAGE DROP ON RIGHT SECONDARY BUS CAUSING EMERGENCY LIGHTS AND OTHER INDICATIONS TO FLICKER. OPERATIONAL CHECK OF NR 2 PROP HEAT AND EMERGENCY LIGHTS NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001040900199 20010409 00199 SO 2001 4 9 20010319CW003 1 20010219 A 3233 89075005 ACTUATOR PIPER PA46 PA46350P SO LYC O540 IO540* 41532 EA MLG STUCK D K NONE O OTHER IN INSP/MAINT 1 EA 07 49PK 1305 32 4622050 AFTER OVERHAUL OF RIGHT MAIN LANDING GEAR ACTUATOR AND DURING NORMAL GEAR EXTENSION THE RIGHT MLG DID NOT INDICATE LOCKE D. AFTER CYCLING GEAR 3 TIME IT INDICATED LOCKED AND A NORMAL LANDING WAS MADE. THE ACTUATOR WAS REMOVED AND SENT BACK TO THE OVERHAUL FACILITY FOR INSPECTION AND REPAIR.THIS IS A RECURRING PROBLEM , IT IS RECOMMENDED THAT 500 HOUR I.R.A. N. BE MADE A SERVICE ITEM. FOR CONTINUED AIRWORTHINESS. THIS MALFUNCTION IS BELIEVED TO BE RELATED TO HYDRAULIC FLUID LINK INTERNALLY COMPOUNDED WITH COLD TEMPERATURES AND ALTITUDED. 1 L 7 1 3O 3 O RT A25SO 1E4 2001040900201 20010409 00201 CE 2001 4 9 20010323CW006 1 20010209 A 2810 FUEL CELL BEECH 58 58 1152740 CE CONT O520 IO520CB 17032 SO WING CONTAMINATED E BSYA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 GL 07 456WW TH444 L298743R LT ENGINE NOT MAKING FULL TO POWER. FOUND CONTAMINATED FUEL(WATER). DEFUELED AIRCRAFT, OPENED FUEL CELL COMPLETELY DRI ED OUT TANK, REPLACED ORING AND FUEL CAP. AIRCRAFT RETURNED TO SERVICE, OPS OK 1 L 7 2 3O 3 O 3A16 E5CE 2001040900202 20010409 00202 SO 2001 4 9 20010323CW007 1 20010209 A 3244 TIRE PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA RT MLG FAILED E BSYA O OTHER E VIBRATION/BUFFET LD LANDING 1 GL 07 35871 318052123 BLEW RIGHT MAIN TIRE ON TOUCHDOWN AND RAN OFF RUNWAY. REMOVED AND REPLACED RIGHT MAIN TIRE AND WHEEL ASSEMBLY. OK FOR SERVICE. 1 L 7 2 3O 3 O A20SO E14EA 2001040900204 20010409 00204 2001 4 9 RAIA00103011 4 20010315 A 3140 350A52005009 COMPUTER AEROSP ATR72 ATR72202 8680940 EU COCKPIT MALFUNCTIONED A RAIA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 CE 03 723TE 12923 2860 283 7182-STL-DURING LANDING ELECTRICAL SMOKE SMELL ENTERED THE FLIGHT DECK. MAINTENANCE REMOVED AND REPLACED THE NR 2 MULTI FUNCTIONAL COMPUTER IAW ATR72 MAINTENANCE MANUAL. 2 H 7 2 4T RT A53EU 2001040900205 20010409 00205 WP 2001 4 9 TWAA0104708 1 20010312 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 928TW 48012 DURING CHECK-C MAINT FOUND IN THE FWD CARGO BIN FUSELAGE SKIN METAL WAS REMOVED BEYOND LIMITS ON CORROSION REMOVAL, LONG ERON 28L, STA 285 THRU 298. SEALED FILLET AREA AND SHAVED NACA RIVETS. COMPLETED REPAIR PER SRM 53-04, PAGE 41 FIG 12B , SHEET 5. 2 L 7 2 4F A6WE 2001040900206 20010409 00206 WP 2001 4 9 TWAA0104709 1 20010312 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE TOOL DAMAGE A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 928TW 48012 DURING CHECK-C MAINT FOUND HI-SPEED CUT IN FUSELAGE SKIN IN FWD CARGO BIN SIDE OF SKIN, STA 285, LONGERON 28L. WIDENED CUTOUT FROM 2.625 INCHES TO 4.25 INCHES. REPAIRED PER SRM 53-04, PAGE 41 FIGURE 12B SHEET 5. 2 L 7 2 4F A6WE 2001040900207 20010409 00207 WP 2001 4 9 TWAA0104701 1 20010313 A 3350 0105606004 MODULE DOUG DC9 DC983 3022083 WP CABIN MISSING A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9621A 53592 AT CABIN ROW 22 TWO RED EGRESS LIGHT LENSES AND A LIGHT MODULE WERE MISSING. REPLACED THE LENSES P/N 0105607-310, AND T HE LIGHT MODULE. CHECK-C 6-3-00 STL. 2 L 7 2 4F RT A6WE 2001040900208 20010409 00208 EA 2001 4 9 20010323CW008 2 20010130 A 8520 CRANKCASE GULSTM 500 500B 0141106 SW LYC O540 TIO540* 41532 EA ENGINE LEAKING H CGKG E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 CE 07 516DT 570 1574 L65448 NR 2 CYLINDER BASE DEVELOPED OIL LEAK AND ENGINE WAS SHUT DOWN. ONE CYLINDER BASE STUD WAS BROKEN AND 5 OTHERS, THE NUT S BACKED OFF DUE TOTHE STUDS LOOSENING IN THE CASE. THE STUDES WOULD NOT TIGHTEN INTO CASE DUE TO WHAT SEEMS SOFT CRANK CASE MATERIAL. 1 H 7 2 3O 3 O 6A1 E14EA 2001040900209 20010409 00209 NM 2001 4 9 20010323CW009 1 20010216 A 2761 65C268636 HOUSING BOEING 737 737* NM SPOILER ACTUATOR CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 07 THE THREADED AREA OF THE HOUSING ASSEMBLY IS CRACKED. OVERSTRESSING OF THE HOUSING IN THE LOCKED POSITION. 2 L 7 2 4F RT A16WE 2001040900210 20010409 00210 EA 2001 4 9 20010323CW010 1 20010220 A 3230 601R102371 SHAFT CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF34* NE MLG SHEARED B LN4R K NONE O OTHER IN INSP/MAINT 1 SO 17 811BP 611 5405 AT RT MAIN LANDING GEAR SIDE BRACE ACTUATOR THE INBOARD TRUNION PIN WAS FOUND TO BE SHEARED OFF AT THE FORWARD ATTACH NU T WHICH HOLDS THE PIN INTO THE WING ATTACH FITTING. UNABLE TO DETERMNE THE TIME AT WHICH THE PART FAILED. 2 L 7 2 4F 4 F RT A21EA E15NE 2001040900212 20010409 00212 CE 2001 4 9 20010319CW008 1 20010201 A 7602 991043510 CONTROL CABLE CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO MIXTURE CONTROL SEPARATED E D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 01 747WS 402C0080 START UP, PILOT PUSHED MIXTURE FORWARD, COULD NOT START LEFT MOTOR OR GET FUEL FLOW. INVESTIGATION REVEALLED MIXTURE KN OB WOULD MOVE, ROD END AT MIXTURE CONTROL DID NOT. FOUND CABLE HOUSING SEPARATED FROM FACTORY CRIMP INSIDE FUSELAGE AT CONTROL COLUM AREA. 1 L 7 2 3O 3 O A7CE E8CE 2001040900213 20010409 00213 SO 2001 4 9 GLBA2001060 1 20010316 A 5610 NP1573112 WINDSHIELD EMB 120 EMB120RT SO COCKPIT CRACKED A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 85GL 12085 CO-PILOTS WINDSHIELD CRACKED IN FLIGHT. REPLACED WINDSHIELD. 2 L 7 2 4T RT A31SO 2001040900214 20010409 00214 NM 2001 4 9 01FDEA00174 1 20010227 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11F 3023600 NM CABIN CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 A 12.75 CRACK FOUND ON NR 4 SEAT TRACK BETWEEN BS 781-800 AT MAIN CARGO COMPT. *S/D* REMOVED AND REPLACED BETWEEN STA 745-816+27 PER IAW SRM 53-70-00 VOL 1. 2 L 7 3 4F RT A22WE 2001040900217 20010409 00217 CE 2001 4 9 JDMA648B 1 20010214 A 2910 2607003459 LINE LEAR 28 28 5170528 CE GE CJ610 CJ6108 30006 NE HYD SYSTEM CRACKED E JDMA K NONE O OTHER IN INSP/MAINT 1 WP 23 28AY 4460 004 HYDRAULIC TRANSFER LINE IN AUXILARY SYSTEM, LINE WAS FOUND BROKEN AT FLAIR CAUSING LOSS OF HYDRAULIC FLUID AND HYDRAULIC SYSTEM FAILURE. AIRCRAFT WAS REPAIRED AND RETURNED TO SERVICE. 2 L 7 2 4J 4 J A10CE 1E16 2001040900218 20010409 00218 NM 2001 4 9 0100776304 1 20010309 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN DAMAGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 664US 23819 DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY PATH LIGHTING INOPERATIVE BETWEEN ROWS 72-74L AND 51-60L. REPAIRED WIRIN G AT 74B AND 60C. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001040900219 20010409 00219 WP 2001 4 9 0100789139 1 20010308 A 3350 BATTERY DOUG DC9 DC914 3022034 WP TAIL DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 948L 47049 DURING LINE CHECK, FOUND CATWALK AREA EMERGENCY EXIT LIGHTING INOPERATIVE. MAINTENANCE REPLACED BATTERIES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 2001040900220 20010409 00220 WP 2001 4 9 0100799956 1 20010217 A 2710 110370 DRAIN VALVE DOUG DC9 DC931 3022065 WP LT MLG WW CLOGGED A NWAA K NONE F FLT CONT AFFECTED CR CRUISE 1 GL 01 923RW 47183 WHILE AIRBORNE BETWEEN RDU AND MSP, THE AILERON TRIM CONTROL JAMMED. FLIGHT CONTINUED UNDER FULL CONTROL AND LANDED WIT HOUT INCIDENT. MAINTENANCE FOUND CONTROL CABLE PULLEYS IN THE RIGHT WHEEL WELL LOCKED UP WITH ICE. FOUND TORN SEAL AT AFT BOTTOM OF FORWARD EXIT WINDOW AND SLANT PANEL DRAIN VALVES WERE CLOGGED. CLEARED DRAIN VALVES, REMOVED ICE, AND REP LACED SEAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001040900221 20010409 00221 WP 2001 4 9 0100809915 1 20010202 A 2424 VOLT REGULATOR DOUG DC9 DC931 3022065 WP RT GENERATOR FAILED A NWAA C ABORTED TAKEOFF H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 GL 01 965N 47417 DURING TAKEOFF ROLL, THE RIGHT GENERATOR FAILED. NUMEROUS ELECTRICAL SYSTEM ANNUNCIATORS LIT UP INDICATING LEFT GENERAT OR DID NOT CROSSTIE SUCCESSFULLY. CREW ABORTED TAKEOFF AT 120 KTS. AIRCRAFT STOPPED SAFELY AND TAXIED TO GATE. CROSST IE ACCOMPLISHED DURING TAXI. MAINTENANCE REPLACED THE RIGHT VOLTAGE REGULATOR, GENERATOR POWER RELAY, AND GENERATOR CON TROL PANEL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001040900223 20010409 00223 NM 2001 4 9 0100766309 1 20010307 A 3397 WIRE BOEING 747 747451 1384940 NM GALLEY DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 669US 24224 DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT THE NR 1 GALLEY RIGHT WALL AND INOPER ATIVE BETWEEN 51-60R. RECONNECTED WIRING. OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 2001040900230 20010409 00230 NE 2001 4 9 DHL2001742001 2 20010316 A 7261 JT8D17 ENGINE BOEING 727 727225 1384077 NM PWA JT8 JT8D17 52049 NE NR 2 ENGINE LEAKING A DHLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 742DH 21290 685530 ON GROUND PRIOR TO TAKEOFF ROLL, LOW OIL PRESSURE LIGHT ILLUMINATED, OIL QUANTITY WENT TO ZERO, AND OIL PRESSURE INDICAT ED-20 PSI ON NR 2 ENG. PERFORMED ENG FAILURE EMERGENCY CHECK LIST. SHUTTING DOWN NR 2 ENG IMMEDIATELY AFTER BLOCK IN V ISUAL INSPECTION SHOWED LARGE AMOUNT OF FLUID DRIPPING FROM ENG NR 2. REMOVED AND REPLACED NR 2 ENGINE PER DHL MTM ENGI NE CHANGE WORK SHEET. PERFORMED ENG RUNUP, OPS AND LEAK CHECKS PER JRH 7.0 SYSTEMS OPS AND LEAK CHECK GOOD. 2 L 7 3 4F 4 F A3WE E2EA 2001040900231 20010409 00231 SO 2001 4 9 20010320CW001 1 20010215 A 3233 89075005 ACTUATOR PIPER PA46 PA46350P SO LYC O540 IO540* 41532 EA RT MLG STUCK D O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 07 49PK 1269 4622050 DURING NORMAL GEAR EXTENSION THE RIGHT MAIN LANDING GEAR DID NOT INDICATE LOCKED. AFTER CYCLING THE GEAR AND FISH TAILI NG IT INDICATED LOCKED AND A NORMAL LANDING OCCURRED. THE ACTUATOR WAS CHECKED AND AN ADJUSTMENT OF THE SWITCH WAS MADE . THE ACTUATOR OPS CHECKED OK AND THE AIRCRAFT WAS RETURNED TO SERVICE ON THE NEXT FLIGHT THE SAME MALFUNCTION OCCURRED . 1 L 7 1 3O 3 O RT A25SO 1E4 2001040900235 20010409 00235 EU 2001 4 9 R7MR32711 1 20010119 A 2140 JBS8803 VALVE UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE HEATER INOPERATIVE B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 135N 27 EC1350086 UNIT INOPERATIVE. BLEED AIR HEAT ON AT ALL TIMES. BLEED AIR ADVISORY ON WITH HEAT TURNED TO OFF POSITION. REPLACED WI TH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2001040900236 20010409 00236 NM 2001 4 9 01FDEA00217 1 20010319 A 5311 6515929 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 FRAME 520 DENTED AT RBL 67, WL 212. REMOVED AND REPLACED PER FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 2001040900237 20010409 00237 NE 2001 4 9 RAIA00103008 2 20010312 A 7421 CH34687 IGNITER AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW124B NE LT ENGINE FAILED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 722TE 220 7400-STL- LEFT ENGINE WOULD NOT START. MAINTENANCE INSPECTED AND REPLACED LEFT ENGINE IGNITERS. 2 H 7 2 4T 4 T RT A53EU E2ONE 2001040900239 20010409 00239 NE 2001 4 9 R7MR32715 2 20010112 A 7261 350A54113800 TUBE SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE AIR OIL VENT CRACKED B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 392LG 374 3252 CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2001040900244 20010409 00244 NE 2001 4 9 20010321CW004 2 20010221 A 7230 50L485A SEAL BOEING 747 747400 NM PWA 4056 PW4056 NE HP TURBINE DEFECTIVE B WA2D C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NE 03 9VSML 23147 16733 P727358CM DURING TO, ENGINE SURGED AND DECREASING NR 2 ROTOR SPEED AND INCREASING EGT TAKEOFF CONTINUED, ENGINE SHUT DOWN AND AIR TURNBACK ACCOMPLISHED. DISASSEMBLY INSPECTION REVEALED HTP 1ST STAGE OUTER AIRSEAL (ROTATING) FAILED MATERIAL HAS BEEN SENT FOR REVIEW AND ANALYSIS. 2 L 7 4 4F 4 F RT A20WE E24NE 2001040900246 20010409 00246 CE 2001 4 9 20010326CW006 1 20010204 A 3230 169380104 VALVE BEECH 23 C24R 1151254 CE LYC O360 IO360A1B 41514 EA HARTZL HCM2Y HCM2YR GL LANDING GEAR WORN D O OTHER O OTHER TX TAXI/GRND HDL 1 WP 25 67079 1966 1966 MC707 L2111851A EN628 EMERGENCY GEAR EXTENSION VALVE WAS OPENED DURING EMERGENCY GEAR EXTENSION TRAINING. THE NOSE GEAR FAILED TO FULLY EXTEN D. THE VALVE WAS CLOSED AND NORMAL GEAR EXTENSION WAS ATTEMPTED. THE NOSE GEAR FAILED TO EXTEND. AFTER LANDING WITH T HE NOSE GEAR TRAILING, THE AIRCRAFT WAS JACKED UP AND NORMAL GEAR EXTENSION WAS TESTED. THE NOSE GEAR FAILED TO EXTEND. THE EMERGENCY GEAR EXTENSION VALVE WAS FOUND TO BE UNSEATED AND WAS CAUSING LOSS OF HYDRAULIC PRESSURE. THE EMERGENC Y GEAR EXTENSION VALVE WAS FOUND TO BE WORN AND THE VALVE HAD NO STOP POSITION FOR FULLY OPEN AND FULLY CLOSED. 1 L 7 1 3O 3 O A1CE 1E10 5 C P43GL 2001040900247 20010409 00247 GL 2001 4 9 20010326CW007 3 20010129 A 6114 HUB BEECH 58 58 1152740 CE CONT O520 IO520* 17032 SO HARTZL HCJ3Y PHCJ3YF2 GL PROPELLER UNDERSIZE B M71R K NONE O OTHER IN INSP/MAINT 1 SW 15 263AC 1810 TH382 ED226 HUB GREASE FITTING HOLE NOT CHAMFERED PROPERLY. THREE BLADE SHANKS UNDER MINIMUM AND HAVE NOT BEEN COMPRESSIVELY ROLLED . HUBS HAVE WRONG GREASE FITTING AND WRONG NUT. 1 L 7 2 3O 3 O 3A16 E5CE 5 C P36EA 2001040900256 20010409 00256 CE 2001 4 9 20010402CW005 1 20010301 A 2612 875135 FIRE LOOP LEAR 25 25B 5170511 CE GE CJ610 CJ610* 30006 NE RT ENGINE MALFUNCTIONED E DQIA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 NM 07 252BK 107 RIGHT ENGINE FIRE LIGHT ILLUMINATED. CREW SHUT ENGINE DOWN, LIGHT STAYED ON. BLEW ONE FIRE BOTTLE, LIGHT STAYED ON. B LEW SECOND FIRE BOTTLE, LIGHT STAYED ON. LANDED WITHOUT INCIDENT. FALSE FIRE INDICATION. FOUND FORWARD FIRELOOP SENSO R MOUNTED ON UPPER COWLING HAD CHAFED WITH WIRE ASSEMBLY BUNDLE MOUNTED TO ENGINE. ADJUSTED BUNDLE TO REMOVE INTERFEREN CE. 2 L 7 2 4J 4 J A10CE 1E16 2001040900258 20010409 00258 2001 4 9 SIMA0423 4 20010211 A 3425 62277130021 COMPUTER SAAB SF340 340B 7860101 EU COCKPIT INOPERATIVE A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 317AE 340B317 JFK - DURING CLIMB-OUT FROM JFK, CAPTAINS EADI WENT BLANK NUMEROUS TIMES WITH RED HEADING FLAG NOTED. PROBLEM CLEARED O N FINAL APPROACH. MAINTENANCE REMOVED AND REPLACED DISPLAY PROCESSER UNIT IAW SAAB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001040900259 20010409 00259 EU 2001 4 9 SIMA0441 1 20010213 A 3350 7239410802 LIGHT SAAB SF340 340B 7860101 EU CABIN MISSING A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 297AE 340B297 DFW - FOUND EMERGENCY LIGHT AT LEFT OVERWING ESCAPE HATCH MISSING. FOUND DURING FLOORBOARD REPLACEMENT. MAINTENANCE IN STALLED NEW LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001040900260 20010409 00260 EU 2001 4 9 SIMA0462 1 20010215 A 3350 192414A FUSE SAAB SF340 340B 7860101 EU POWER SUPPLY BLOWN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 232AE 340B232 BGR - FLT 4929 - EMERGENCY EXIT LIGHT OVER 3BC INOPERATIVE. REMOVED AND REPLACED FUSE BY 20LN EPS PACK IAW SAAB AMM CH 20-10. OPS CHECK GOOD AT THIS TIME. (M) 2 L 7 2 4T RT A52EU 2001040900261 20010409 00261 CE 2001 4 9 20010321CW007 1 20010129 A 2730 666000115 CONTROL CABLE CESSNA 560 560XL CE PWA 545 PW545A NE ELEVATOR BINDING B R2JR K NONE O OTHER IN INSP/MAINT 1 EA 21 565AB 224 5605072 FORWARD ELEVATOR CONTROL CABLE UP. CABLE WAS FOUND WRAPPED AROUND RUDDER PULLEY RETAINER. WAS RIDING RUDDER PULLEY, CA BLE GUARD PIN. AT APPROX FUSELAGE STA. 426.5 SUSPECT CABLE BLOCKS NOT USED DURING PRIOR MAINTENANCE OF ELEVATOR CONTROL CABLES. 2 L 7 2 4F 4 F RT A22CE E00059EN 2001040900262 20010409 00262 EU 2001 4 9 SIMA0501 1 20010219 A 3350 3071BPEGPL LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE O OTHER NR NOT REPORTED 1 SW 21 345SB 340B345 YUL - FLT 4748 - CREW REPORTED FLOOR PROXIMITY EMERGENCY LIGHT STRIP BY SEAT 7B HAS ONE BULB INOPERATIVE. MAINTENANCE R EPLACED BULB IN FLOOR PROXIMITY EMERGENCY LIGHT AT SEAT 7B. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SER VICE. (M) 2 L 7 2 4T RT A52EU 2001040900263 20010409 00263 EU 2001 4 9 SIMA0503 1 20010219 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 301AE 340B301 JFK - FLT 5013 - CREW REPORTED THE EMERGENCY LIGHT OVER CABIN DOOR IS DIM AND FLICKERS. MAINTENANCE REMOVED AND REPLACE D POWER SUPPLY UNIT 21LN. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001040900264 20010409 00264 EU 2001 4 9 SIMA0504 1 20010219 A 2611 721112111000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY MALFUNCTIONED A SIMA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 392AE 340B392 BTR - FLT 3280 - DURING CLIMB, CREW REPORTED THE CARGO SMOKE LIGHT CAME ON. CREW FIRED CARGO FIRE BOTTLE AND RETURNED T O BTR. CARGO FIRE EXTINGUISHER SYSTEM WAS PUT ON MEL. INSPECTION OF CARGO BAY SHOWED NO EVIDENCE OF FIRE. AIRCRAFT WA S REPOSITIONED TO DFW WITH NO PASSENGERS. MAINTENANCE REMOVED AND REPLACED FORWARD AND AFT CARGO SMOKE DETECTORS (S/N A 3096 & A3387) IAW SAAB MM. OPERATIONAL CHECK WAS GOOD. CARGO FIRE BOTTLE WAS REPLACED AND AIRCRAFT WAS RETURNED TO SER VICE. (M) 2 L 7 2 4T RT A52EU 2001040900265 20010409 00265 EU 2001 4 9 SIMA0519 1 20010220 A 3350 66362 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 397AE 340B397 SBP - EMERGENCY FLOOR LIGHTS AT SEATS 4 AND 5 DO NOT ILLUMINATE. MAINTENANCE REPLACED LIGHT UNDER SEATS 4A AND 5A. OPE RATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001040900266 20010409 00266 EU 2001 4 9 SIMA0505 1 20010219 A 3330 3716 BALLAST AEROSP ATR42 ATR42300 8680920 EU CARGO BAY BURNED A SIMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 282AT 282 SRQ - FLT 5284 - CREW DETECTED AN ELECTRICAL SMELL BEFORE TAXI OUT FROM GATE. MAINTENANCE FOUND CARGO LIGHT BALLAST BUR NED. BALLAST WAS REMVOED AND REPLACED. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001040900267 20010409 00267 SO 2001 4 9 SIMA0432 1 20010212 A 5330 14520554001 SKIN EMB 145 EMB145LR SO FUSELAGE GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 706RG 145194 SAW - DURING PS-2 INSPECTION MAINTENANCE REPAIRED TDMI 706530052. GOUGE IN LEFT CENTER FUSELAGE BETWEEN FRAMES 16 AND 2 0 STRINGERS 15 AND 16. MAINTENANCE REPAIRED THE GOUGE IAW EO EB-53MR-012. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001040900268 20010409 00268 SO 2001 4 9 SIMA0553 1 20010224 A 3610 S21226 O-RING EMB 145 EMB145 SO BLEED AIR SYS WORN A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 609AE 145069 ORD - FLT 4137 - DURING CLIMB, CREW NOTED NR 1 BLEED LEAK, NO OTHER PROBLEMS WERE REPORTED. AIRCRAFT WAS RETURNED TO OR D. MAINTENANCE REPLACED O-RINGS AT THE UPPER BLEED DUCT LINE. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001040900269 20010409 00269 SO 2001 4 9 C2XA01TY040 1 20010310 A 3350 72875513 LIGHT EMB 145 EMB145LR SO CABIN DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13975 145163 TYS DURING A SCHEDULED INSPECTION THE AFT SECTION OF THE FLOOR TRACK EMERGENCY LIGHTING STRIP WAS FOUND DAMAGED. MAINT ENANCE REMOVED AND REPLACED THE AFT SECTION OF THE FLOOR TRACK EMERGENCY LIGHTING STRIP IAW EMB-145 MM 33-50-12, OPERATI ONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001040900270 20010409 00270 EU 2001 4 9 SIMA0326 1 20010201 A 3350 3013017 POWER SUPPLY AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 536AT 536 DFW - FLT 3656 - CREW REPORTED NUMEROUS EMERGENCY LIGHTS ARE INOPERATIVE WHEN AIRCRAFT IS POWERED DOWN. MAINTENANCE REM OVED AND REPLACED THREE EMERGENCY LIGHT POWER SUPPLY UNITS (S/N 1611, 1148, 1721) IAW ATR MM. OPS CHECK WAS GOOD AND AIR CRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001040900271 20010409 00271 EU 2001 4 9 SIMA0391 1 20010208 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 541AT 541 SGF - NUMEROUS FLOOR AND OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACKS AT 43WL AND 61WL AMM . OPS CHECK GOOD IAW MM 33-50-00. (M) 2 H 7 2 4T RT A53EU 2001040900272 20010409 00272 EU 2001 4 9 SIMA05310 1 20010211 A 5320 S5317320600301 PAN AEROSP ATR72 ATR72212 EU COCKPIT CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 348AE 349 SAW - DURING MBV-1 INSPECTION, MAINTENANCE REPORTED THE FIRST OFFICERS SEAT FLOOR PAN CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR PAN IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001040900273 20010409 00273 EU 2001 4 9 SIMA0542 1 20010223 A 3350 3013000 POWER SUPPLY AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 498AT 498 DFW - FLT 3833 - CREW REPORTED FORWARD EMERGENCY LIGHTS INOPERATIVE WITHOUT POWER ON AIRCRAFT. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY UNIT 62WL IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SER VICE. (M) 2 H 7 2 4T RT A53EU 2001040900274 20010409 00274 SO 2001 4 9 C2XA01TY041 1 20010310 A 4980 14528571401 SHROUD EMB 145 EMB145LR SO EMPENAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13975 145163 TYS DURING A SCHEDULED INSPECTION THE APU COWLING EXHAUST SHROUD WAS FOUND CRACK. MAINTENANCE REPAIRED THE APU COWLING IAW EMB-145 GST-0771/01. THE REPAIR WAS SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001040900275 20010409 00275 EU 2001 4 9 SIMA0534 1 20010222 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 424MQ 045 MIA - FLT 5224 - CREW REPORTED EMERGENCY LIGHTS ON FLOOR BELOW FORWARD CABIN EMERGENCY EXITS TO BE INOPERATIVE. MAINTEN ANCE REMOVED AND REPLACED BATTERIES IN POWER SUPPLY UNITS 29 WL AND 3WL. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RE TURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001040900278 20010409 00278 EU 2001 4 9 SIMA0013 1 20010101 A 3350 1317 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 334AE 340B334 JFK - FLT 5160 - FOUND OVERHEAD 11A EMERGENCY LIGHT INOPERATIVE MEL 33-13. OVERHEAD EMERGENCY LIGHT AT SEAT 11A IS INOP ERATIVE. MAINTENANCE REPLACED BUBL AT 11A OVERHEAD. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001040900279 20010409 00279 SO 2001 4 9 SIMA0312 1 20010131 A 5330 14523053003 SKIN EMB 145 EMB145LR SO FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 626AE 145117 SAW - AIRCRAFT FERRIED TO SAW FROM ORD FOR A HOLE IN THE LEFT SIDE OF FUSELAGE BETWEEN FRAMES 65 AND 66 STRINGERS 19L AN D 20L. MAINTENANCE REPAIRED THE SKIN IAW SRM 53-31-01 TYPE A REPAIR FIGURE 201. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001040900280 20010409 00280 NM 2001 4 9 AALA20010356 1 20010227 A 3397 WIRE BOEING 727 727223 1384074 NM AFT DOOR DAMAGED A K NONE L NO TEST IN INSP/MAINT 1 SW 21 861AA 21088 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT RIGHT AFT DOOR INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT W IRES AT RIGHT AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001040900281 20010409 00281 NM 2001 4 9 AALA20010357 1 20010227 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 848AA 20989 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 3 EXIT SIGN INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STRIP AT ROW 3 EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001040900284 20010409 00284 NM 2001 4 9 ANCF200100005 1 20010115 A 2913 PUMP BOEING 767 767284 1385184 NM PWA 4056 PW4056 NE RT ENGINE FAILED W ANCF A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 23 988AN 24742 DURING FLIGHT FROM FRA TO SJU RH EDP HYD LOW PRESSURE CAME ON, FLIGHT PROCEDED TO BAQ. RT EDP WAS REPLACED IAW AMM 29-11 -05, TEST WAS SATISFACTORY 2 L 7 2 4F 4 F RT A1NM E24NE 2001040900285 20010409 00285 WP 2001 4 9 01FDEA00184 1 20010310 A 2780 SLAT DOUG DC10 DC1030F 3023504 WP WING MALFUNCTIONED A FDEA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 SO 25 303FE 46802 SLATS WOULD NOT EXTEND WHEN SEL FOR LAND. LAND WITH FLAPS BUT NO SLATS. TROUBLESHOT SYS PER DC-10-30 TAFT 27-80-00 PG 119. OPS CK NORMAL, NO DEFECTS NOTED. 2 L 7 3 4F RT A22WE 2001040900286 20010409 00286 WP 2001 4 9 AALA20010358 1 20010227 A 3397 WIRE DOUG DC9 DC982 3022082 WP TAILCONE LOOSE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 423AA 49335 DFW - DURING OVERNIGHT MAINTENANCE, TAILCONE EMERGENCY LIGHT INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001040900287 20010409 00287 EU 2001 4 9 AALA20010355 1 20010228 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 21 1413A 11376 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT HAS BROKEN WIRES. REPAIRED EMERGENCY EXIT LIGHT WIRES AT MID C ABIN CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001040900288 20010409 00288 NM 2001 4 9 AALA20010354 1 20010228 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 693AA 26973 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 4E INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT CONN ECTOR AT SEAT 4E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001040900289 20010409 00289 NM 2001 4 9 AALA20010353 1 20010228 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 693AA 26973 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 23D MISSING. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 23D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001040900290 20010409 00290 NM 2001 4 9 AALA20010351 1 20010228 A 3350 1001141 LIGHT BOEING 727 727223 1384074 NM AFT AIRSTAIR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 885AA 21524 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASS EMBLY AT AFT AIRSTAIR. SYTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001040900291 20010409 00291 NM 2001 4 9 AALA20010352 1 20010228 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM ENTRY DOOR DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 885AA 21524 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT MAIN ENTRY DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT LEFT SIDE MAIN ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001040900292 20010409 00292 WP 2001 4 9 AALA016017 1 20010217 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST NR NOT REPORTED 1 SW 21 832RA 53044 CCI-LAX - EMERGENCY LIGHTS L1 DOOR, SEATS 3EF AND 4EF INOPERATIVE. REMOVED AND REPLACED FORWARD BATTERY PACK AND FUSE O N L1 DOOR LIGHT. OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 2001040900294 20010409 00294 NM 2001 4 9 EIA2001011 1 20010217 A 7933 56B17S2 BULB BOEING 747 747212B 1384886 NM NR 4 ENGINE DEFECTIVE A EIAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 NM 09 485EV 20712 NR 4 ENGINE OIL TEMP INCREASED TO RED BAND. INFLIGHT SHUTDOWN CHECKLIST ACCOMPLISHED. REPLACED NR 4 ENGINE OIL TEMP BU LB PER MM 79-34-01. OPS CHECK NORMAL. PERFORMED WINDMILL INSPECTION. NO DEFECTS NOTED. (M) 2 L 7 4 4F A20WE 2001040900295 20010409 00295 EU 2001 4 9 ASOA01025 1 20010227 A 3350 3012000 BATTERY PACK AEROSP ATR72 ATR72 EU CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 533AS 11214 460 DURING INSPECTION, CREW REPORTED EMERGENCY LIGHTS CAME ON WHEN IN ''ARM'' POSITION EVEN IF THE GENERATOR IS ONLINE AND E XTERNAL POWER IS REMOVED. MAINTENANCE REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. AIRC RAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT 2001040900296 20010409 00296 NM 2001 4 9 GAIA01110OP 1 20010309 A 2424 905D9774 GCU BOEING 727 727223 1384074 NM GEN SYSTEM FAULTY A GAIA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SW 07 6827 20180 FLT 2019 - ABQ-PHX, NO CLIMB-OUT, SHORTLY AFTER FLAP RETRACTION, EXPERIENCED DIFFERENTIAL FAULT IN NR 2 SYSTEM IN COMBIN ATION WITH ESSENTIAL POWER LOSS AND OVER EXCITATION IN SYSTEMS 1 AND 3, WHICH RESULTED IN THE LOSS OF THE SYNCHRONIZING BUS. AIRCRAFT MADE AN UNEVENTFUL LANDING IN ABQ. INSTALLED VOLTAGE REGULATOR AND GCU AND APU ELECTRICAL SYSTEM INTO NR 2 VOLTAGE REG AND GCU. OPS CHECKS NR 1 AND NR 2 AND NR 3 SYSTEMS AND COULD NOT FIND ANY FAULTS WITH ESSENTIAL POWER SY NCRO OR DIFFERENTIAL FAULT ELECTRICAL SYSTEM. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001040900297 20010409 00297 NE 2001 4 9 SIMA0684 2 20010309 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE MALFUNCTIONED A SIMA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 263AE 340B263 ALB - FLT 5064 - CREW REPORTED THE RIGHT ENGINE ROLLED BACK THREE TIMES, TWICE DURING CLIMB-OUT AND ONCE ENROUTE. ON TH E FIRST ROLL BACK TORQUE WENT TO YELLOW ARC AND POWER WAS REDUCED, ITT ROSE APPROXIMATELY 15-20 DEGREES. AFTER THIS ALL INSTRUMENTS WERE NORMAL. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 2001040900298 20010409 00298 EU 2001 4 9 SIMA0683 1 20010309 A 6100 PROPELLER SAAB SF340 340B 7860101 EU ENGINE VIBRATION A SIMA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SW 21 283AE 340B283 BGR - FLT 9753 - CREW REPORTED VIBRATION IN FLIGHT AT 1396, 1270, AND 1230 PROPELLER RPM. CREW COULD NOT TELL IF VIBRAT ION WAS FROM LEFT OR RIGHT ENGINE. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. MAINTENANCE PERFORMED AN INTENSIVE INS PECTION OF FUSELAGE AND PROPELLERS WITH NO DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR AN FUNCTIONAL CHECK FLIGHT. AIRCRA FT PASSED FUNCTIONAL CHECK FLIGHT AND WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001040900299 20010409 00299 NE 2001 4 9 SIMA0322 2 20010201 A 7200 S95404002V805 HARNESS AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE NR 2 ENGINE SHORTED A SIMA A UNSCHED LANDING J R WARNING INDICATION PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 21 135MQ 135 120978 TPA - FLT 5244 - AFTER TAKEOFF, THE NR 2 ENGINE FAILED. OIL PRESSURE WENT TO ZERO PSI, TORQUE GAUGE INDICATED 20 PERCEN T. NO INDICATION OF SEVERE DAMAGE TO THE ENGINE OR AIRFRAME. RETURNED AIRCRAFT TO TPA WITH NO FURTHER INCIDENTS REPORT ED. MAINTENANCE FOUND WIRING HARNESS AT 410VC SHORTED. WIRING HARNESS WAS REMOVED AND REPLACED IAW ATR MM. OPERATIONAL CHECK WAS GOOD. DURING TROUBLE SHOOTING THE FDAU READOUT SHOWED AN OVERTORQUE WAS RECORDED ON NR 2 ENGINE. PROPELLER WAS REPLACED IAW HS MM. OVERTORQUED PROCEDURES FOR THE ENGINE WERE FOLLOWED IAW THE PWC MM. AIRCRAFT WAS RETURNED TO S ERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 2001040900300 20010409 00300 EU 2001 4 9 SIMA0603 1 20010301 A 3320 SOCKET AEROSP ATR72 ATR72212A 8680902 EU CABIN BURNED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 541AT 541 DFW - FLT 3401 - FLIGHT CREW SMELLED AN ELECTRIC WIRE BURNING FOR ABOUT 2 MINUTES IN THE COCKPIT. A CHECK OF THE CARGO AND CABIN REVEALED NO ELECTRIC BURNING SMELL. MAINTENANCE FOUND THE OVERHEAD CABIN LATERAL LIGHT AT ROW 5 C/D END SOCKE T BURNED/MELTED. MEL PER 33-2. (M) 2 H 7 2 4T RT A53EU 2001040900301 20010409 00301 WP 2001 4 9 MWEA010299 1 20010309 A 2910 FITTING DOUG DC9 DC982 3022082 WP HYDRAULIC SYS LEAKING A MWEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 31 810ME 48072 GATE CREW REPORTED HAZE/SMOKE WITH ODOR IN CABIN. MAINTENANCE FOUND HYDRAULIC LEAK AT PRESSURE TRANSMITTER FITTING LOOS E CAUSING FLUID TO BE SUCKED INTO APU INLET. TIGHTENED LOOSE FITTING, PRESSURIZED SYSTEM AND NO LEAKS NOTED. 2 L 7 2 4F A6WE 2001040900303 20010409 00303 SW 2001 4 9 KBMA88680 1 20010301 A 2822 7G547 PRESSURE SWITCH BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL BOOST PUMP INOPERATIVE E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 73DP 11187 2513 FORWARD BOOST PUMP PRESSURE SWITCH INOPERATIVE. 1 G 7 1 3U 3 U H2SW E4CE 2001040900304 20010409 00304 CE 2001 4 9 AWKR19889 1 20010220 A 2421 649304 ALTERNATOR BEECH 58 58 1152740 CE CONT O550 IO550* SO ENGINE INOPERATIVE B AWKR K NONE O OTHER IN INSP/MAINT 1 WP 25 214KP 191 191 TH1894 ALTERNATOR INOPERATIVE. 1 L 7 2 3O 3 O 3A16 E3SO 2001040900305 20010409 00305 2001 4 9 20010323CW018 4 20010214 A 3417 HG2010AC03 COMPUTER CESSNA 750 750 2076810 CE ALLSN AE300 AE3007A GL E/E BAY AHRS INOPERATIVE E UG8A K NONE L NO TEST IN INSP/MAINT 1 GL 23 5113 1857 7500013 AFTER INITIAL POWER UP OF THE AIRCRAFT THE CREW NOTED A FAILED NR 2 AHRS INDICATION ON THE COPILOTS PRIMARY FLIGHT DISPL AY. FAILED NR 2 AHRS COMPUTER. REPLACED NR 2 AHRS COMPUTER WITH SERVICEABLE UNIT AND COMPLETED OPERATIONAL CHECKS. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2001040900307 20010409 00307 WP 2001 4 9 U2RB030101 1 20010307 A 5711 580271231 SPAR CAP DOUG DC8 DC863F 302198F WP LT WING CRACKED I U2RB K NONE O OTHER IN INSP/MAINT 1 GL 23 865F 76152 18931 46088 DURING COMPLIANCE OF MCDONNELL DOUGLAS DC-8 S/B 57-90 R5 (NPRM 99-NM-60-AD) DETECTED CRACK ATLOWER FORWARD SPAR AT ATTAC H FASTENERS STA XFS 524. CRACK BEYOND S/B 57-90 R5 REPAIR LIMITS. 2 L 7 4 4F 4A25 2001040900308 20010409 00308 EU 2001 4 9 20010327CW003 1 20010213 A 3213 136638 BEARING JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE331* 01514 WP NLG STRUT BROKEN B FW1R K NONE O OTHER IN INSP/MAINT 1 NE 03 316UE 13664 100 OZ9460054 41055 THIS BEARING TYPE WAS USED FOR OVERHAULS STARTING SOMETIME AFTER 3/99. SINCE DEC/2000 THER HAVE BEEN 3 FAILURES OF THI S BEARING. THS PLASTIC BEARING IS BORKEN IN THE AREA OF THE RETAINING PIN HOLE AND DRAGED OUT OF THE CYLINDER. THIS CO ULD BE RELATED TO THE SHRINKAGE OF THE BEARING DUE TO LOW TEMPERATURE. THE BEARING IS SUPPOSED TO BE HELD IN PLACE BY L OCKTITE 415 AND A SMALL PIN WHERE WE HAVE SEEN THE BREAKAGE. 2 L 7 2 4T 3 T RT A41NM E2WE 2001040900309 20010409 00309 2001 4 9 20010409CW004 4 20010409 A 2210 CONNECTOR TEIJINSEIKI BOEING 757 757* NM YAW DAMNPER DAMAGED B J4IR K NONE O OTHER IN INSP/MAINT 1 NM 13 DURING DISASSEMBLY OF 11 YAW DAMPNER ASSEMBLIES. FOUND ELECTRICAL CONNECTOR PINS FOR THE HYDRAULIC SOLENOID VALVE BURNE D AND IN SOME CASES COMPLETELY DETACHED FROM THE WIRE WITH THE CONNECTOR DAMAGED IN 5 OF THE 11 UNITS REPAIRED. 2 L 7 2 4F RT A2NM 2001040900310 20010409 00310 2001 4 9 20010409CW005 4 20010409 A 2210 CONNECTOR TEIJINSEIKI BOEING 757 757* NM YAW DAMPNER DAMAGED B J4IR K NONE O OTHER IN INSP/MAINT 1 NM 13 DURING DISASSEMBLY OF 11 YAW DAMPNER ASSEMBLIES, FOUND ELECTRICAL CONNECTOR PINS FOR THE HYDRAULIC SOLENOID VALVE BURNE D AND N SOME CASES COMPLETELY DETACHED FROM THE WIRE WITH THE CONNECTOR DAMAGED IN 5 OF THE 11 UNITS REPAIRED. 2 L 7 2 4F RT A2NM 2001040900311 20010409 00311 EU 2001 4 9 20010327CW004 1 20010215 A 3250 135650 UNIVERSAL JOINT JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE331* 01514 WP NLG STEERING DAMAGED B FW1R K NONE O OTHER IN INSP/MAINT 1 NE 03 568HK 11222 APB951395 41086 UNIT RECEIVED WITH FAILURE REASON OF WHEEL WONT TURN. UNIT HAD EXCESSIVE FREE PLAY BEFORE DISASSEMBLY. INTERNAL STEEL PARTS WERE FOUND TO BE CORRODED. THE DIFFERENTIAL WAS PITTED OVER ALL SURFACES. IT LOOKED LIKE IT WAS DISINTIGRATING. THE OTHER INTERNAL PARTS HAD LARGE PITS ON SMALLER AREAS. CORROSION OF THE STEEL PARTS IN THIS UNIT, TO THIS EXTENT HA S NOT BEEN SEEN AT THIS FACILITY. NOTE: UNIT ALSO HAD AN OUTPUT SHAFT SPLIT PIN WHICH WAS CRACKED AS PREVIOUSLY REPORT ED. THE SAFETY WIREAS REQUIRED, WAS NOT PRESENT TO PREVENT THE LOSS OF STEERING WHEN THE BROKEN PIN FALLS OUT OF THE OU TPUT SHAFT. 2 L 7 2 4T 3 T RT A41NM E2WE 2001040900312 20010409 00312 NE 2001 4 9 NAFA2001001 2 20010222 A 8530 358994 CYLINDER DOUG DC8 DC8* WP PWA R2800 R2800* 52026 NE NR 2 ENGINE CRACKED G NAFA K NONE O OTHER IN INSP/MAINT 1 AL 01 77808 2182 2182 45372 34219 FEATHERED NR 2 ENGINE DUE TO CYLINDER FAILURE. REMOVED AND REPLACED THE NR1 CYLINDER ON THE NR 2 ENGINE. 2 L 7 4 4J 4 R F 4A25 5E8 2001040900313 20010409 00313 CE 2001 4 9 20010322CW001 1 20010206 A 2731 31324375 PIN CESSNA CESSNA 182 R182 2072734 CE LYC O540 O540J3C5 41532 EA MCAULY 2D34C B2D34C218 GL TRIM ACTUATOR SHEARED E OI9A K NONE O OTHER IN INSP/MAINT 1 GL 25 2557S 5535 922 R18201349 L2217240A 796618 WHILE ATTEMPTING TO TRIM THE AIRCRAFT FOR STRAIGHT AND LEVEL FLIGHT, THE PILOT RAN OUT OF NOSE DOWN TRIM. AFTER A SUCCE SSFUL LANDING AND MAINTENANCE INVESTIGATION IT WAS FOUND THAT THE ELEVATOR TRIM TAB WAS NOT MAKING IT ALL THE WAY TO THE NOSEDOWN/ TABUP LIMIT. FURTHER INVESTIGATION REVEALED THAT THE ELEVATOR TAB ACTUATOR SPROCKET WAS SPINNING ON THE SHAF T DUE TO ONE OF THE GROOVE PINS THAT TIE THE TWO PIECES TOGETHER WAS MISSING AND THE OTHER WAS SHEARED IN HALF. THE TWO PINS WERE REPLACED WITH NEW, USING LOCTITE TO INSTALL, AND THE SYSTEM WAS RERIGGED AND OPERATIONALLY CHECKED OK. RECOM MEND CAREFUL INSPECTION OF THESE PINS EVERY 100 HOURS OF OPERATION. 1 H 7 1 3O 3 O RT 3A13 E295 5 C P7EA 2001040900314 20010409 00314 2001 4 9 20010409CW006 4 20010409 A 2210 CONNECTOR TEIJINSEIKI BOEING 757 757* NM YAW DAMPNER DAMAGED B J4IR K NONE O OTHER IN INSP/MAINT 1 NM 13 DURING DISASSEMBLY OF 11 YAW DAMPNER ASSEMBLIES, FOUND ELECTRICAL CONNECTOR PINS FOR THE HYDRAULIC SOLENOID VALVE BURNED AND IN SOME CASES COMPLETELY DETACHED FROM THE WIRE WITH THE CONNECTOR DAMAGED IN 5 OF THE 11 UNITS REPAIRED. 2 L 7 2 4F RT A2NM 2001040900315 20010409 00315 2001 4 9 20010409CW007 4 20010409 A 2210 CONNECTOR TEIJINSEIKI BOEING 767 767* NM YAW DAMPNER DAMAGED B J4IR K NONE O OTHER IN INSP/MAINT 1 NM 13 DURING DISASSEMBLIES OF 11 YAW DAMPNER ASSEMBLIES, FOUND ELECTRICAL CONNECTOR PINS FOR THE HYDRAULIC SOLENOID VALVE BURN ED AND IN SOME CASES COMPLETELY DETACHED FROMTHE WIRE WITH THE CONNECTOR DAMAGED IN 5 OF THE 11 UNITS REPAIRED. 2 L 7 2 4F RT A1NM 2001040900316 20010409 00316 NM 2001 4 9 CALA0100212 1 20010307 A 5320 WEB BOEING 737 7373T0 1384582 NM CARGO BAY CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17329 23459 INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR JAMB LOWER FORWARD INSIDE CORNER WEB AT STA 440, S25. REPAIRED WE B IAW SRM 51-70-13, FIGURE 1. 2 L 7 2 4F RT A16WE 2001040900317 20010409 00317 2001 4 9 20010409CW008 4 20010409 A 2210 CONNECTOR TEIJINSEIKI BOEING 767 767* NM YAW DAMPNER DAMAGED B J4IR K NONE O OTHER IN INSP/MAINT 1 NM 13 DURING DISASSEMBLY OF 11 YAW DAMPNER ASSEMBLIES, FOUND ELECTRICAL CONNECTOR PINS FOR THE HYDRAULIC SOLENOID VALVE BURNE D AND IN SOME CASES COMPLETELY DETACHED FROM THE WIRE WITH THE CONNECTOR DAMAGED IN 5 OF THE 11 UNITS REPAIRED. 2 L 7 2 4F RT A1NM 2001040900318 20010409 00318 EA 2001 4 9 20010327CW008 2 20010129 A 8530 LS74644 ROD BOLT GULSTM 500 500B 0141106 SW LYC O540 TIO540* 41532 EA ENGINE BROKEN D K NONE O OTHER IN INSP/MAINT 1 SW 15 690RR 1196 1196 500B116988 L1921048 NR 4 CYLINDER BOTH ROD BOLTS BROKEN. CYLINDER WAS BROKEN FREE OF CRANKCASE ALL THE CYLINDER HOLD DOWN STUDS BROKEN. 1 H 7 2 3O 3 O 6A1 E14EA 2001040900319 20010409 00319 CE 2001 4 9 20010322CW002 1 20010214 A 2400 63283733 BUSS TIE CESSNA 172 172S 2072439 CE LYC O360 IO360A1C 41514 EA COMM / NAV ARCED D K NONE O OTHER IN INSP/MAINT 1 NM 03 789EP 967 967 172S8135 PILOT REPORTED TRANSPONDER INOP, NR1 COMM/NAV INTERMIT. MAINT REPLCD NR1 COMM/NAV AND REMOVED TRANSPONDER FOR REPAIR S. NEXT FLIGHT, PILOT REPORTED NR2 COMM/NAV INTERMIT LOSS OF POWER & THE INTERCOMM INOP. MAINT TROUBLESHOOTING FOUND AUDIO PANEL COMM SELECTOR FUNCTION INOP NR2 COMM/NAV INTERMIT, INTERCOMM INOP & AUTO PILOT AUDIO WARN INOP. CAUSE WAS FOUND TO BE AVIONICS BUS BAR HAD FOUR LOOSE SCREWS WITH SEVERE ARCING. THE LOOSE SCREWS WERE ON THE FOLLOWING C/B, AU TO PILOW, GPS, NAV COMM 1 AND NAV COMM 2. NO MAINT PERFORMED ON ANY ELECTRICAL C/BS SINCE PURCHASE OF AC AND THE BUS I S HIDDEN BEHIND THE MAIN WIRE HARNESS W/LMTD VISUAL OF CB. RECMD AC BE INSP ASAP FOR LOOSE SCREWS ON ALL CIRCUIT BRKRS 1 H 7 1 3O 3 O NT 3A12 1E10 2001040900320 20010409 00320 NE 2001 4 9 S13R01001 2 20010222 A 7210 792207 DAMPER RING SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE IDLER GEAR DAMAGED G K NONE O OTHER IN INSP/MAINT 1 NE 03 19493 UPON DISASSEMBLY OF GEARCASE, FOUND LEFT IDLER GEAR DAMPER RING BROKEN RT IDLER GEAR HAS 2 TEETH DAMAGED / BROKEN. LT I DLER GEAR HAS ONE TOOTH BROKEN. 2 L 7 2 4T 4 T RT A52EU E8NE 2001040900323 20010409 00323 WP 2001 4 9 20010409CW009 2 20010409 A 7320 30710491 TUBE HWKSLY DH125 HS125600A 4230158 EU GARRTT TFE731 TFE7313R1H 29001 WP P3 PLENNUM CRACKED B K NONE O OTHER IN INSP/MAINT 1 WP 19 700XJ 5972 256015 P83416 RIGHT ENGINE ROLLED BACK TO IDLE ON ITS OWN AFTER TAKEOFF. MAINTENANCE FOUND THE P3 TUBE ASSEMBLY BETWEEN THE FUEL CON TROL UNIT AND THE ENGINE PLENNUM CRACKED IN HALF. FATIGUE FAILURE IS SUSPECTED. 2 L 7 2 4J 4 F A3EU E6WE 2001040900325 20010409 00325 CE 2001 4 9 20010328CW005 1 20010130 A 2750 D160003 MOTOR BEECH 55 D55 1152730 CE TE FLAP DEFECTIVE B DPOR K NONE L NO TEST IN INSP/MAINT 1 NM 07 13RJ TC2247 SQUAKED FLAP C/B TRIPS WHEN FLAPS ACTUATED. ISOLATED FLAP MOTOR WITH REMOTE C/B & EXT POWER. FOUND BAD FLAP MOTOR. LO CATED NEW MOTOR. INST MOTOR WORKED ON GROUND, TRIPPED C/B IN FLIGHT. ISOLATED MOTOR, DETERMINED BAD MOTOR. LOCATED ANO THER MTR, WHEN REC''D , NOTICED DATA PLATES WERE IDENTICAL EXCEPT ONE WAS LABELED 11.5 AMPS THE OTHER WAS 5.0. CLOSER AT TENTION TO DETAIL ON DATA PLATES COULD HAVE PREVENTED THIS OCCURANCE. 1 L 7 2 3O 3A16 2001040900327 20010409 00327 WP 2001 4 9 20010403CW001 1 20010110 A 3397 3386L2253 WIRE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D* 52039 NE GALLEY BROKEN B A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 09 959R 46143 AFTER TAKEOFF, PILOT NOTICED ODD SMELL, FOLLOWED BY SMOKE. HE DECLARED AN EMERGENCY AND RETURNED TO AIRPORT WITHOUT INC IDENT. TROUBLE SHOT SYSTEM, FOUND OLD DEAD END GALLEY WIRE LAYING ON RES R4-35. REMOVED OLD WIRE. CHECKED WIRING TO S WITCHES 51-403, 51-332 AND 51-331 AND CHECKED OK. CHECKED LIGHT ASSEMBLY L2-253, FOUND POWER WIRE BROKEN OFF AND SHORTI NG TO GROUND. ALSO FOUND SWITCH 51-403 IN DIM POSITION. REMOVED AND REPLACED LIGHT ASSEMBLY AND OPS CHECKED LIGHT ASSE MBLY. NO FURTHER PROBLEM NOTED. 2 L 7 4 4F 4 F 4A25 1E8 2001040900331 20010409 00331 NM 2001 4 9 PCAA0103018 1 20010310 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 819EX 016 MDT- DURING ROUTINE MAINTENANCE, SECTION OF EMERGENCY LIGHTING FOUND INOPERATIVE APROXIMATELY 8 FEET ON RIGHT FLOOR PATH . LOOSE CONNECTORS FOUND AND RESECURED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001040900332 20010409 00332 EA 2001 4 9 20010403CW002 2 20010403 A 7414 1068291018 MAGNETO PIPER PA31 PA31P350 7103111 SO LYC O540 LTIO540* 41533 EA RT ENGINE BROKEN D K NONE O OTHER IN INSP/MAINT 1 CE 07 9225Y 160 31P8414015 RIGHT ENGINE FAILED DURING CRUISE FLIGHT IN IMC. MAG HOUSING FLANGES BROKE AND MAG FELL OUT OF ACCESSORY MOUNT. ENGINE FACTORY OVERHAUL WITH THIS NEW MAG 3/27/00. NO SIGNS OF OIL LEAKAGE BEFORE FAILURE. ENGINE FEATHERED AND AIRCRAFT RET URNED WITHOUT INCIDENT. 1 L 7 2 3O 3 O RT A8EA E14EA 2001040900339 20010409 00339 EA 2001 4 9 20010320CW002 3 20010223 A 6110 A251392 BOLT MCAULY A251392 CESSNA 172 172R 2072401 CE LYC IO360 IO360L2A EA MCAULY IC235 IC235LFA7570 EA PROPELLLER MISMANUFACTURED D K NONE O OTHER IN INSP/MAINT 1 NM 10 172N 217 QF003 17280004 L2688251A QF003 THE SIX A2513-92 PROPELLER MOUNTING BOLTS ARE APPROX .250 INCHES TOO SHORT. THEY ARE THREE THREADS TOO SHORT FROM BEING FLUSH WITH THE BACK SIDE OF THE PRESSED IN NUT ON CRANKSHAFT FLANGE. A LONGER BOLT (APPROX .250 IN) WOULD CORRECT THI S PROBLEM. THIS AIRCRAFT AND ANOTHER NEW (172S MODEL) HAVE THIS DEFECT. THE NUT IS THIN AT THE POINT WERER IT GOES THR OUGH THE CRANKSHAFT FLANGE AND ONLY A FEW THREADS CATCH THE BACKSIDE(FAT PART) OF THE NUT. 1 H 7 1 3O 3 O NT 3A12 1E10 5 N P12EA 2001040900340 20010409 00340 CE 2001 4 9 20010403CW009 1 20010219 A 2720 14603201 RUDDER PEDAL CESSNA 150 150G 2071816 CE CONT O200 O200* 17020 SO COCKPIT WORN H K NONE O OTHER IN INSP/MAINT 1 SO 13 3057S 5790 15066957 DURING ANNUAL INSPECTION PILOTS SIDE RUDDER PEDALS AND SHAFTS WERE FOUND TO BE BADLY WORN WHERE SHAFT PINS PASS THROUGH THE HOLES. IT IS EVIDENT THAT THIS ITEM IS OVERLOOKED. 1 H 7 1 3O 3 O 3A19 E252 2001040900341 20010409 00341 CE 2001 4 9 20010403CW010 1 20010302 A 7500 TUBE BEECH B300 B300 1159232 CE PWA PT6 PT6* 52043 EA BLEED AIR MELTED G O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 21 701FC FL291 PILOT REPORTED BLEED AIR WARNING INDICATION ON LEFT SIDE. TROUBLE SHOT AND FOUND EVA TUBING MELTED BELOW HEAT DUCT. DI SCOVERED EARLIER REPAIR (WITHIN 1O HOURS) OF RIGHT SIDE TUBING 2 INCHES FROM LATEST FAILURE. TUBING IS COMING IN CONTAC T WITH DUCT AND MELTING. ANOTHER STANDOFF IS REQUIRED TO MAINTAIN TUBING CLEARANCE NOTED IN MM. 1683 HOURS TOTAL TIME 2 L 7 2 4T 3 T RT A24CE E2NE 2001040900342 20010409 00342 CE 2001 4 9 20010403CW011 1 20010222 A 3222 5842000231 STRUT CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO NOSE GEAR DISCHARGED D A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 01 514NC 10764 402C0514 UPON GEAR RETRACT, HYDR PRES LIGHT REMAINED ILLUMINATED. GEAR EXTENSION WAS ATTEMPTED, NOSE GEAR FAILED TO EXTEND. GEA R WAS EXTENDED USING EMERGENCY BLOW DOWN PROCEDURE, ALL GEAR DOWN INDICATORS SHOWED GREEN AND AIRCRAFT LANDED WITHOUT IN CIDENT. MECH FOUND NOSE GEAR STRUT FLAT AND ALL FOUR NOSE GEAR DOOR ATTACH BRACKETS BROKEN. WHEN THE GEAR WAS RETRACTE D, COMPRESSED NOSE STRUT FAILED TO ENTER WHEEL WELL PROPERLY, DAMAGING THE GEAR DOOR BRACKETS AND CAUSED THE GEAR TO STI CK IN THE WELL. THE STRUT WAS SERVICED, BRACKETS REPLACED. EXTENSION AND RETRACTION TEST WAS PERFORMED, ALL INDICATION S NORMAL. AC RETURNED TO SERVICE. 1 L 7 2 3O 3 O A7CE E8CE 2001040900347 20010409 00347 CE 2001 4 9 20010403CW015 1 20010219 A 5330 10704 SKIN RKWELL NA265 NA26565 7630107 CE GARRTT TFE731 TFE731* 01518 WP FUSELAGE CORRODED B UVVR K NONE O OTHER IN INSP/MAINT 1 CE 03 700JC 46574 UPON REMOVAL OF GPS ANTENNA FROM AIRCRAFT, THE MATING SURFACE OF THE ANTENNA TO THE AIRCRAFT WAS RUSTING, CAUSING THE AI RCRAFT SKIN TO CORRODE. SUSPECT A VOID IN THE SEALANT AROUND BASE CAUSED MOISTURE TO GET UNDER ANTENNA AND CAUSE CORRO SION. RECOMMEND CLOSE ATTENTION TO SEALANT BEAD TO ENSURE NO MOISTURE ENTRAPMENT. ANTENNA WAS REPLACED DUE TO SEVERITY OF RUST ON BOTTOM SURFACE. 2 L 7 2 4J 4 F A2WE E6WE 2001040900351 20010409 00351 CE 2001 4 9 20010406CW008 1 20010227 A 2810 991202010 FUEL CAP CESSNA 500 550 2076604 CE PWA JT8 JT8D* NE RT WING MISSING E DELA A UNSCHED LANDING D J INFLIGHT SEPARATION WARNING INDICATION NR NOT REPORTED 1 CE 03 900PB 5500566 AIRCAFT DEPARTED AIRPORT, ENROUTE. UPON ROTATION THE CREW NOTICED RIGHT FUEL CAP HAD COME OFF. ADVISED CENTER AND RETU RNED FOR PRECAUTIONARY LANDING. REPLACED FUEL CAP AND RETURNED AIRCRAFT TO SERVICE. 1 L 7 2 4F 4 F A22CE E2EA 2001040900352 20010409 00352 CE 2001 4 9 20010322CW003 1 20010205 A 5312 12121331 BULKHEAD CESSNA 210 T210N 2073456 CE CONT O520 TSIO520* 17040 SO FUSELAGE CRACKED D K NONE O OTHER IN INSP/MAINT 1 NM 03 967CC 5661 21064534 HORIZONTAL STABILIZER WAS REMOVED FOR THE REPLACEMENT OF AFT REINFORCEMENTS. THE BULKHEAD ASSEMBLY PN1212133-1 WAS NOTI CED TO BE CRACKED AT LEFT AFT RELIEF CUTOUT, JUST FORWARD OF THE HORIZONTAL STABILIZER AFT ATTACHMENT. CRACK WAS ABOUT .3750 INCH LONG. PN 12121335 IS THE REPLACEMENT BULKHEAD ASSEMBLY NUMBER. 1 H 7 1 3O 3 O 3A21 E8CE 2001040900353 20010409 00353 CE 2001 4 9 20010322CW004 1 20010205 A 5510 12326241 FITTING CESSNA 210 T210N 2073456 CE CONT O520 TSIO520* 17040 SO HORIZONTAL STAB CRACKED D K NONE O OTHER IN INSP/MAINT 1 NM 03 967CC 3853 21064534 DURING ANNUAL INSPECTION THE HORIZONTAL STABILIZER ATTACHMENT POINT REINFORCEMENT ON THE LEFT SIDE WAS FOUND CRACKED. T HIS REINFORCEMENT WAS THE NEW STYLE STEEL PN 12326241 THAT WAS CRACKED. THIS AC IS USED FOR LOW LEVEL OVERLAND SURVEY A ND THESE REINFORCEMENT ARE INSPECTED EVERY 100 HOURS. THE RIGHT REINFORCEMENT WAS NOT CRACKED AT THIS TIME, BUT IT WAS CHANGED DUE TO CONVENIENCE AND HIGH TIME(3853). 1 H 7 1 3O 3 O 3A21 E8CE 2001040900354 20010409 00354 CE 2001 4 9 20010322CW005 1 20010215 A 5510 1016400123 BRACKET BEECH 200 B200 1152922 CE PWA PT6 PT6* 52043 EA HORIZONTAL STAB CRACKED B K NONE O OTHER IN INSP/MAINT 1 NE 05 333RD 6914 BB915 THE LT ATTACH BRACKET THAT SECURES THE HORIZONTAL STABILIZER TO THE VERTICAL FIN HAD A CRACK AT THE LOWER HUCKBOLT HOLE ATTACHING IT TO THE VERTICAL FIN. REPLACEMENT OF THE BRACKET WAS REQUIRED DUE TO THIS CRACK. AREA IS HARD TO SEE, LOCA TED ON THE FORWARD LEADING EDGE SIDE OF THE VERTICAL FIN. ONLY WAY TO INSPECT THIS AREA IS BY ACCESSING IT USING THE PA NEL ATOP THE HORIZONTAL STAB. THAT HAS THE BEACON LIGHT ON IT. ONCE THIS PANEL IS REMOVED, BY USE OF A MIRROR, THIS ARE A CAN BE INSPECTED AND SHOULD BE INSPECTED AT NORMAL INSPECTION INTERVALS. THERE IS NO POSITIVE CAUSE FOR THIS CRACK AT THIS TIME. PART WAS SENT FOR EVALUATION. IMPROPER SHIMMING UPON INSTALL COULD BE A CAUSE, BUT NOT CONFIRMED. 1 L 7 2 4T 3 T A24CE E2NE 2001040900355 20010409 00355 CE 2001 4 9 20010403CW020 1 20010213 A 2435 03601018 BEARING LUCAS RAYTHN DH125 HAWKER800 7450004 CE GARRTT TFE731 TFE731* 01518 WP STARTER GEN FAILED B KC2R K NONE O OTHER IN INSP/MAINT 1 GL 03 237RA 612 94326 258237 UNIT REMOVED BECAUSE OF EXCESS VIBRATION. ANIT DRIVE END BEARING HAD FAILED. THIS BEARING IS RETAINED AND DOES NOT MOV E. THE DRIVE END BEARING WHICH SHOULD FLOAT WAS RUSTED SOLID IN THE LINER BUT HAD NOT FAILED. BEARING SHOULD BE INSTAL LED WITH LUBE ON RACE TO PREVENT THIS SITUATION 2 L 7 2 4F 4 F RT A3EU E6WE 2001040900356 20010409 00356 SO 2001 4 9 20010322CW006 2 20010222 A 8520 CAMSHAFT CESSNA 303 T303 2073820 CE CONT O520 TSIO520AE 17040 SO ENGINE FAILED D C ABORTED TAKEOFF Y J ENGINE STOPPAGE WARNING INDICATION TO TAKEOFF 1 CE 01 9777C 4 T30300213 246694R ENGINE FAILED ON TAKE OFF, AIRCRAFT WAS AIRBORN. OWNER WAS ABLE TO MAKE A SAFE LANDING. FOUND ENGINE TO HAVE NO COMPRE SSION. REMOVED ROCKER BOX COVERS, FOUND ONLY ONE EXHAUST VALVE WOULD MOVE ON NR1 CYLINDER. CAMSHAFT BROKE BETWEEN EXHA UST AND INTAKE ON NR1 CYLINDER. 1 L 7 2 3O 3 O A34CE E8CE 2001040900357 20010409 00357 CE 2001 4 9 20010322CW007 1 20010115 A 3260 SAFETY SWITCH CESSNA 401 401 207590C CE CONT O520 IO520* 17032 SO MLG INOPERATIVE D K NONE O OTHER IN INSP/MAINT 1 SW 07 31DB 4010202 LANDING GEAR DOWN LIGHT DID NOT ILLUMINATE. SWITCH ACCT LEAF WAS BROKEN. 1 L 7 2 3O 3 O A7CE E5CE 2001040900360 20010409 00360 EA 2001 4 9 20010320CW003 2 20010216 A 8520 MAIN BEARING PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA ENGINE MAKING METAL D K NONE O OTHER IN INSP/MAINT 1 SO 05 3581C 318052091 L956861A WHILE PERFORMING A 100 HOUR ENGINE INSPECTION, LARGE METAL PRATICALS WHERE FOUND IN THE OIL SUCTION SCREEN. ALSO, AN EX CESSIVE AMOUNT OF METAL FOUND IN THE ENGINE OIL FILTER. SAMPLES OF METAL SENT FOR TESTING. DETERMINED METAL PARTICALS TO BE CRANK AND OR ROD BEARING MATERIAL. ENGINE REMOVE FROM SERVICE. NOTE: THIS IS THE SECOND ENGINE HAVE HAD THIS HA PPEN TO WITHIN THE LAST 1.5 YEARS. 1 L 7 2 3O 3 O A20SO E14EA 2001040900361 20010409 00361 EA 2001 4 9 20010320CW004 2 20010220 A 8520 03227091 BRACKET CESSNA 190 190 2072902 CE JACOBS R755 R7559 35003 EA ENGINE CORRODED D K NONE O OTHER IN INSP/MAINT 1 CE 03 195JA 3800 7504 THESE BRACKETS ARE MADE OF MAGNESIUM AND ARE CORRODING SEVERELY AND CRACKING AT THE MOUNTING FEET AND THE MAIN BEARING B OSS. SUGGEST DYE PENETRANT CHECK WITH PAINT REMOVED, AT EACH ANNUAL INSPECTION. REPLACE WITH AIRWORTHY BRACKETS OR ST C ALUMINUM BRACKETS. 1 H 7 1 3R 3 R NC A790 TC121 2001040900362 20010409 00362 NE 2001 4 9 C2XA01CL051 2 20010307 A 7261 ENGINE AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE NR 1 ENGINE OVERSERVICED A C2XA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 14834 193 CLE FLIGHT 3176 THE CREW REPORTED THAT ON STARTUP OF NR 1 ENGINE THERE WAS SMOKE IN THE COCKPIT. THE CREW SHUTDOWN THE ENGINE. MAINTENANCE INSPECTED AND FOUND THE NR 1 ENGINE WAS OVERSERVICED WITH OIL. MAINTENANCE SERVICED THE NR 1 ENGIN E TO PROPER LEVEL. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2001040900363 20010409 00363 SO 2001 4 9 C2XA01CL052 1 20010307 A 2530 CBC16707 RECEPTACLE EMB 145 EMB145ER SO GALLEY BURNED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 15932 145015 CLE FLIGHT 3992 THE CREW REPORTED A BURNING SMELL IN THE GALLEY. MAINTENANCE INSPECTED AND REPLACED THE OUTBOARD HOT JU G RECEPTACLE. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001040900364 20010409 00364 2001 4 9 RAIA00103006 4 20010307 A 3418 0861DT5 VANE EMB 145 EMB145ER SO LT FUSELAGE FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 803HK 1249 145077 7601-STL- STALL PROTECTION SYSTEM FAILED DURING TAXI. MAINTENANCE REPLACED LEFT STALL VANE. 2 L 7 2 4F RT T00011AT 2001040900365 20010409 00365 2001 4 9 RAIA00103007 4 20010307 A 3452 6226523207 TRANSPONDER AEROSP ATR42 ATR42300 8680920 EU COCKPIT INOPERATIVE A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 424TE 27521 124 7163-STL-CREW REPORTS BOTH TRANSPONDERS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED TRANSPONDER CONTROL HEAD. 2 H 7 2 4T RT A53EU 2001040900366 20010409 00366 WP 2001 4 9 DJFA200100012 2 20010227 A 7261 8310441 OIL FILTER AMD FALC50 FALCON50MYST 2730106 EU GARRTT TFE731 TFE731* 01518 WP ENGINE MISINSTALLED E DJFA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 EA 23 519CW 11 11 50019 P76160C ENGINE SHUTDOWN IN FLIGHT AFTER OIL PRESSURE INDICATION FLUCTUATION. 2 L 7 3 4F 4 F A46EU E6WE 2001040900367 20010409 00367 SO 2001 4 9 COMA0110041 1 20010307 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 259CA 21382 120252 EMERGENCY LIGHTS, ROWS 7 TO 10 ARE INOPERABLE. REPLACED THE EMERGENCY BATTERY. 2 L 7 2 4T RT A31SO 2001040900368 20010409 00368 EA 2001 4 9 COMA0160303 1 20010307 A 3020 300013000002 ANTI-ICE VALVE CNDAIR CL600 CL6002B19 EA RT ENGINE FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 914CA 14016 7012 RIGHT ENGINE COWL ANTI-ICE CAUTION MESSAGE. REPLACED THE ANTI-ICE VALVE. 2 L 7 2 4F RT A21EA 2001040900369 20010409 00369 EA 2001 4 9 20010404CW005 1 20010222 A 3244 256K433 TIRE CNDAIR CL601 CL6013A 8070802 EA GE CF34 CF34* NE MLG DELAMINATED B K NONE O OTHER IN INSP/MAINT 1 EA 21 601EC 263 MAR920488 5064 WHILE PERFORMING A POST FLIGHT INSPECTION, THE LEFT MAIN GEAR INBOARD TIRE SHOWED SIGNS OF TREAD SEPARATION FROM TIRE CO RE. SUSPECT DEFECT IN TIRE MATERIAL AT TIME OF MANUFACTURING. INSPECTED ALL OTHER TIRES ON AIRCRAFT AND NO DAMAGE OR D EFECTS WERE FOUND. 2 L 7 2 4F 4 F RT A21EA E15NE 2001040900370 20010409 00370 GL 2001 4 9 20010320CW006 3 20010214 A 6114 2A34C50N HUB CESSNA 182 182G 2072716 CE CONT O470 O470R 17026 SO MCAULY 2A34C 2A34C50 GL PROPELLER CRACKED B W59R K NONE O OTHER IN INSP/MAINT 1 WP 07 3107S 18255607 732897 EDDY CURRENT INSPECTION REVEALED A CRACK IN THREADS OR NR1 BLADE HUB SOCKET AT APPROX 7 OCLOCK POSITION WHEN VIEWED FROM SIDE WITH CYLINDER END POINTING UP AND APPROX 1.25 INCH IN LENGTH HUB WAS NOT MODIFIED TO OIL FILL CONFIGURATION. 1 H 7 1 3O 3 O NT 3A13 E273 5 C P3EA 2001040900371 20010409 00371 NM 2001 4 9 20010306CW003 1 20010130 A 2720 108713 SLIDE BOEING 737 737375 13844BN NM RUDDER CRACKED B AWXA K NONE O OTHER IN INSP/MAINT 1 NM 01 336AW 47551 23707 SLIDE IS CRACKED ON BOTH SIDES OF SHAFT, ABOUT 0.090IN FROM THE END AND THE SHAFT IS BENT. PROBABLE CAUSE IS EXCESSIVE STRESS AND FATIGUE DURING OPERATIONAL LOAD. INCREASE INSPECTION REQUIREMENTS FOR SERVO VALVE SLIDE AND REQUIRE THAT SLI DE BE EDDY CURRENT INSPECTED FOR CRACKS. 2 L 7 2 4F RT A16WE 2001040900372 20010409 00372 NM 2001 4 9 20010306CW004 1 20010130 A 2760 654494713 HOUSING BOEING 737 737 UTILSYS NM SPOILER ACTUATOR CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 30379 HOUSING IS CRACKED AND BROKEN AT THE BEARING LUG. OVERSTRESSED, FATIGUE, AND / OR POSSIBLE FLAW IN HOUSING DESIGN. H OUSING DESIGN NEEDS TO BE EVALUATED. 2 L 7 2 4F RT A16WE 2001040900373 20010409 00373 NM 2001 4 9 20010306CW005 1 20010130 A 2760 654494713 HOUSING BOEING 737 737 UTILSYS NM SPOILER ACTUATOR CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 30379 HOUSING IS CRACKED AND BROKEN AT THE BEARING LUG. PROBABLE CAUSE: OVERSTRESSED, FATIGUE, AND / OR POSSIBLE FLAW IN HOU SING DESIGN. HOUSING DESIGN NEEDS TO BE EVALUATED. 2 L 7 2 4F RT A16WE 2001040900374 20010409 00374 NM 2001 4 9 20010306CW006 1 20010122 A 2760 654494713 HOUSING BOEING 737 737 UTILSYS NM SPOILER ACTUATOR CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 30573 HOUSING IS CRACKED AT TWO LOCATIONS, ALONG THE RADIUS OF THE OUTSIDE SHOULDERS OPPOSITE THE PORTS. 2 L 7 2 4F RT A16WE 2001040900376 20010409 00376 EU 2001 4 9 KBMA88689 1 20010309 A 8012 0174078010 START VALVE SNIAS 350 AS350BA 8680817 EU RT ENGINE LEAKING E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 350SH 4522 2957 START DRAIN VALVE LEAKING. NOTE: REMOVAL FROM RIGHT ENGINE 4126. 1 G 7 1 3U NC H9EU 2001040900378 20010409 00378 NM 2001 4 9 20010306CW007 1 20010201 A 2760 654494715 HOUSING BOEING 737 737 UTILSYS NM SPOILER ACTUATOR CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 42465 HOUSING IS CRACKED AND BROKEN AT BEARING LUG. PROBABLE CAUSE: OVERSTRESSED, FATIGUE, AND / OR POSSIBLE FLAW IN HOUSI NG DESIGN. DESIGN OF HOUSING SHOULD BE EVALUATED. 2 L 7 2 4F RT A16WE 2001040900379 20010409 00379 NM 2001 4 9 20010306CW008 1 20010109 A 2760 654494713 HOUSING BOEING 737 737 UTILSYS NM SPOILER ACTUATOR BROKEN B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 39624 HOUSING IS CRACKED AND THE BEARING LUG HAS BROKEN OFF. OVERSTRESSED, FATIGUE, AND / OR POSSIBLE FLAW IN HOUSING DESIG N. 2 L 7 2 4F RT A16WE 2001040900380 20010409 00380 EU 2001 4 9 SABA010007 1 20010302 A 6120 CONTROL UNIT BAG JETSTM JETSTM3201 1500217 EU RT PROP OUT OF ADJ A SABA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 33 957AE 957 AIRCRAFT 957 ON FLIGHT 5121 FROM CLT TO HTS. DURING TAKEOFF ROLL THE RIGHT ENGINE ONLY MADE 98 PERCENT RPM. TAKEOFF WA S ABORTED. AIRCRAFT RETURNED TO THE GATE WITH NO OTHER PROBLEMS AND NO EMERGENCY PROCEDURES WERE USED. MAINTENANCE ADJ USTED THE X SCREW PER BAE MAINTENANCE MANUAL. A GROUND RUN WAS PERFORMED. OPS CHECK WAS GOOD. AIRCRAFT RETURNED TO SE RVICE. 2 L 7 2 4T RT A56EU 2001040900381 20010409 00381 NM 2001 4 9 20010406CW002 1 20010221 A 2761 654494713 HOUSING BOEING 737 737* NM SPOILER ACTUATOR CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 30757 HOUSING IS CRACKED. 2 L 7 2 4F RT A16WE 2001040900382 20010409 00382 NM 2001 4 9 20010406CW003 1 20010221 A 2761 654494710 HOUSING BOEING 737 737* NM SPOILER ACTUATOR CRACKED B IU2R K NONE O OTHER IN INSP/MAINT 1 NM 01 45828 HOUSING IS CRACKED. 2 L 7 2 4F RT A16WE 2001040900383 20010409 00383 NM 2001 4 9 20010406CW004 1 20010221 A 2913 123412 COVER BOEING 737 737* NM SHUTOFF VALVE CRACKED B IU2R K NONE O OTHER IN INSP/MAINT 1 NM 01 COVER HAS A CRACK FROM THE EDGE OF THE CENTER HOLE OUT TO THE EDGE OF THE COVER. 2 L 7 2 4F RT A16WE 2001040900384 20010409 00384 NM 2001 4 9 20010406CW005 1 20010220 A 2742 144490 PLATE BOEING 747 747* NM ACTUATOR CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 41974 MOUNTING LUGS CRACKED AND BROKEN ON THE PLATE. PROBABLE CAUSE, FATIGUE, OVERSTRESSED. 2 L 7 4 4F RT A20WE 2001040900385 20010409 00385 NM 2001 4 9 20010406CW006 1 20010219 A 2761 654494713 HOUSING BOEING 737 737* NM SPOILER ACTUATOR CRACKED B K NONE O OTHER IN INSP/MAINT 1 NM 01 25607 HOUSING IS CRACKED AND BROKEN AT THE BEARING MOUNT LUG. OVERSTRESSED, FATIGUE, AND OR POSSIBLE FLAW IN HOUSING DESIGN. 2 L 7 2 4F RT A16WE 2001040900388 20010409 00388 EA 2001 4 9 COMA0160325 1 20010319 A 5270 864807 PSEU CNDAIR CL600 CL6002B19 EA EE BAY MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 937CA 8059 7044 CARGO DOOR CAUTION MESSAGE. REPLACED THE PSEU. 2 L 7 2 4F RT A21EA 2001040900396 20010409 00396 WP 2001 4 9 MWEA010292 1 20010306 A 2751 29190801 SWITCH DOUG DC9 DC914 3022034 WP LT MLG WW INOPERATIVE A MWEA D RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 31 600ME 45725 TAKEOFF WARNING HORN WILL NOT SILENCE. REMOVED AND REPLACED THE FLAP SWITCH IN THE LEFT WHEEL WELL. 2 L 7 2 4F A6WE 2001040900397 20010409 00397 NM 2001 4 9 TSAA0152018 1 20010218 A 5230 6562254 DOOR BOEING 737 7372X6C 1384552 NM CARGO BAY CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 817AL 23292 IDENTIFIED CRACKS AT 3.25 INCH PROPAGATING FROM ONE RIVET TO ADJACENT RIVET ON MAIN CARGO DOOR AT BS 430, 2 INCHES BELOW STRINGER 14L CONFIRMED BY UTILIZING HFEC AND VISUAL METHOD. TRIM OUT THE CRACK DAMAGE, FABRICATED FILLERS FROM 2024-T3 , FABRICATED EXTERNAL DOUBLER ONE GAUGE THICKER THAN DOOR LOWER OUTER SKIN, AND INSTALLED FASTENERS PER SRM 51-30-2. IN ACCORDANCE WITH ECO 3211, RECEIVED 8110-3 APPROVAL. (M) 2 L 7 2 4F RT A16WE 2001040900399 20010409 00399 NM 2001 4 9 01FDEA00180 1 20010308 A 2610 656020916 CONTROL UNIT BOEING 727 7272S2F 1384O81 NM COCKPIT MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 211FE 22933 DURING CLIMB, FIRE WARN MASTER LIGHT ON GLARESHIELD CAME ON. AIR TURNBACK. CK WIRE FROM FIRE DET CNTRL UNIT M819 PIN 1 4 OF D1478 FOR A GROUND. WIRE CK GOOD WITH FLUKE. SUSP FIRE DET CNTRL UNIT TO BE THE PROBLEM. REMOVED AND REPLACED EN G FIRE DETECTION UNIT PER EA 1-2610-56855 OPS CK GOOD. FOUND LEAK ON INLET SIDE OF FUEL HEAT AIR VALVE. REPLACED GASKE TS PER B727 MM 73-14-011. OPS CK GOOD. 2 L 7 3 4F A3WE 2001040900400 20010409 00400 NE 2001 4 9 20010404CW006 2 20010312 A 7314 RG9570R196884511 PUMP PILATS PC12 PC1245 EU PWA PT6 PT6A60A 52043 NE ENGINE FAILED B ESMR O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 11 605TC 275 320 PCEPR0183 PILOT NOTICED EXCESSIVE CONSUMPTION OF FUEL COMPARED TO FLIGHT TIME AND LANDED. FOUND FUEL DRAINING FROM ENGINE COWLING AREA. PILOT PRESSURIZED FUEL SYSTEM, FOUND FUEL LEAKING FROM LOW PRESSURE FUEL PUMP GASKET BETWEEN PUMP REGULATOR AND PUMP BODY. THE INTERNAL SEAL BETWEEN REGULATOR AND PUMP BODY PROBABLY FAILED, THEN PRESSURIZED REGULATOR AREA TAKING O UT THE GASKET. 1 L 7 1 3T 4 T RT A78EU E4EA 2001040900401 20010409 00401 EU 2001 4 9 C2XA01IA149 1 20010308 A 5330 S5357110120000 SKIN AEROSP ATR42 ATR42320 8680930 EU FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14822 163 YUL - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE WING BOX SKIN WAS FOUND TO BE GOUGED. MAINTENANCE PERFORMED A REPAIR IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHANGE EC5330-01151, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001040900402 20010409 00402 EU 2001 4 9 C2XA01IA150 1 20010308 A 5714 S5397091627600 INTERCOSTAL AEROSP ATR42 ATR42320 8680930 EU WING BOX CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14822 163 YUL - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE WING BOX INTERCOSTAL AT STRINGER 1 LEFT WAS FOUND TO BE CRACKED BETWEEN FRAMES 23 & 24. MAINTENANCE REMOVED AND REPLACED THE AFFECTED INTERCOSTAL IN ACCORDANCE WITH ATR42-320 SRM 51- 25-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001040900403 20010409 00403 EU 2001 4 9 C2XA01IA151 1 20010308 A 5414 S5411079520000 SKIN AEROSP ATR42 ATR42320 8680930 EU RT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14822 163 YUL - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE RIGHT HAND NACELLE LEFT HAND FORWARD EDGING WAS FOUND TO BE CRA CKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGING IN ACCORDANCE WITH ATR42-320 SRM 54-12-61, & 51-25-03, AND T HE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001040900404 20010409 00404 EU 2001 4 9 C2XA01IA152 1 20010308 A 5410 S5411058620000 CHANNEL AEROSP ATR42 ATR42320 8680930 EU RT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14822 163 YUL - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE RIGHT HAND ENGINE TOP COWL WAS FOUND TO HAVE A CRACKED LEFT HAN D CHANNEL. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CHANNEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001040900405 20010409 00405 EU 2001 4 9 C2XA01IA153 1 20010308 A 5414 S5411079520000 SKIN AEROSP ATR42 ATR42320 8680930 EU LT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14822 163 YUL - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE LEFT HAND NACELLE LEFT HAND FORWARD EDGING WAS FOUND TO BE CRAC KED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGING IN ACCORDANCE WITH ATR42-320 SRM 51-25-03, AND THE AIRCRAFT W AS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001040900406 20010409 00406 EU 2001 4 9 C2XA01IA154 1 20010308 A 5410 S5411058620000 CHANNEL AEROSP ATR42 ATR42320 8680930 EU LT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14822 163 YUL - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE LEFT HAND CHANNEL ON THE LEFT HAND HALF MOON COWLING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CHANNEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI CE. 2 H 7 2 4T RT A53EU 2001040900408 20010409 00408 EU 2001 4 9 C2XA01IA155 1 20010308 A 5320 S5367131120600 ANGLE AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14822 163 YUL - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE FAIL SAFE AT FRAME 37 WAS FOUND TO BE CORRODED. MAINTENANCE RE MOVED AND REPLACED THE AFFECTED FAIL SAFE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001040900409 20010409 00409 EU 2001 4 9 C2XA01IA156 1 20010308 A 5714 S5397091635700 STRUCTURE AEROSP ATR42 ATR42320 8680930 EU WING BOX CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14822 163 YUL - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE STRUCTURE IN THE WING BOX AT FRAME 29A RIGHT WAS FOUND TO BE CO RRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRUCTURE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001040900410 20010409 00410 EU 2001 4 9 C2XA01IA157 1 20010308 A 5714 S5397091635600 STRUCTURE AEROSP ATR42 ATR42320 8680930 EU WING BOX CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14822 163 YUL - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE STRUCTURE AT FRAME 29A LEFT IN THE WING BOX WAS FOUND TO BE CRA CKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRUCTURE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001040900411 20010409 00411 WP 2001 4 9 AALA016019 1 20010217 A 3350 FUSE DOUG DC9 DC983 3022083 WP EMRGENCY LIGHT BLOWN A AALA K NONE L NO TEST NR NOT REPORTED 1 SW 21 871RA 49788 LAX-CCI - EMERGENCY LIGHTS SEATS 28 AFT INOPERATIVE. REMOVED AND REPLACED FUSE FOR AFT EMERGENCY LIGHTS, OPS CHECK GOOD . (M) 2 L 7 2 4F RT A6WE 2001040900412 20010409 00412 2001 4 9 AALA016020 4 20010224 A 2565 D29982113 SLIDE DOUG DC9 DC982 3022082 WP L1 DOOR LOOSE A AALA K NONE O OTHER NR NOT REPORTED 1 SW 21 823RA 49889 FOUND FORWARD ENTRY DOOR SLIDE PACK LOOSE IN DOOR. PACK LOCATED ON JETBRIDGE. RE-INSTALLED FORWARD ENTRY DOOR SLIDE. (M) 2 L 7 2 4F A6WE 2001040900413 20010409 00413 NM 2001 4 9 BJNA010205 1 20010221 A 3222 654620021 STRUT BOEING 737 737214 138446R NM NLG LEAKING A BJNA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 11 457TM 20156 NOSE LANDING GEAR SHOCK STRUT LEAKING. REMOVED AND REPLACED NOSE LANDING GEAR STRUT ASSEMBLY PER B737 MM 32-21-0. (M) 2 L 7 2 4F A16WE 2001040900414 20010409 00414 NM 2001 4 9 BJNA010206 1 20010221 A 3244 26010452 TIRE BOEING 737 737282 13844AT NM NLG DEFORMED A BJNA K NONE E VIBRATION/BUFFET CL CLIMB 1 WP 11 789TM 23046 WHEN GEAR IS RETRACTED MUCH VIBRATION, ALSO VIBRATION WHEN HIGH SPEED BEFORE ROTATION. INSPECTED NOSE TIRES AND FOUND T HEM GROSSLY OUT OF ROUND. REMOVED AND REPLACED NOSE TIRES PER BMM 32-45-21. (M) 2 L 7 2 4F RT A16WE 2001040900415 20010409 00415 NM 2001 4 9 BJNA010207 1 20010226 A 3350 1619 LIGHT BOEING 737 737282 13844AT NM EXTERIOR INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 NM 05 789TM 23046 FOUND EXTERIOR EMERGENCY LIGHT AT L1 DOOR INOPERATIVE. RELAMPED, OPS CHECK NORMAL, IAW BMM 33-51-61. (M) 2 L 7 2 4F RT A16WE 2001040900416 20010409 00416 EU 2001 4 9 20010405SG001 1 20010222 A 2750 FLAP AIRBUS 300 A300B4203 3930306 EU WINGS MALFUNCTIONED A WRNA K NONE F FLT CONT AFFECTED AP APPROACH 1 SO 05 820SC 154 DURING APPROACH, SLATS EXTENDED INITIALLY TO 16 DEGREES. SLATS RETRACTED WHEN 25 DEGREES FLAP WERE SELECTED. COULD''NT DUPLICATE ON GROUND. OPS CHECKED NORMAL IAW FIM 27-80-00. REQUIRES FURTHER INVESTIGATION. AIRCRAFT INSPECTED AND PRE PARED FOR FERRY FLIGHT IAW PROCEDURES, CHAPTER 11 TAI GMM. AIRCRAFT CONSIDERED AIRWORTHY FOR FLIGHT INTENDED. (M) 2 L 7 2 4F RT A35EU 2001040900417 20010409 00417 NM 2001 4 9 TSAA0133026 1 20010303 A 3350 86210066 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 809AL 21720 REPLACED FORWARD ENTRY IDENT LIGHT ASSEMBLY DUE TO BEING INOPERATIVE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F A16WE 2001040900418 20010409 00418 NM 2001 4 9 01FDEA00160 1 20010223 A 2782 SUPPORT BRACKET BOEING 727 727247 138408F NM LE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 233FE 21327 DURING ROUTINE INSP, NR 1 LEAD EDGE FLAP ACTUATOR, FWD OTBD UPPER FITTING SUPPORT BRACKET FOUND CRACKED.*S/D* REMOVED A ND REPLACED BRACKET PER IAW BAC 727 MM 27-81-001-4 AND BAC 727 SRM 51-10-1. 2 L 7 3 4F A3WE 2001040900419 20010409 00419 NM 2001 4 9 TSAA0133028 1 20010303 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 5 AND NR 6 EMERGENCY EXIT BATTERY PACKS DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F RT A16WE 2001040900420 20010409 00420 NM 2001 4 9 TSAA0133029 1 20010303 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED NR 1 AND NR 3 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4F RT A16WE 2001040900421 20010409 00421 NM 2001 4 9 TSAA0133031 1 20010303 A 3350 LIGHT BOEING 737 73725A 1384481 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 819AL 23791 REPLACED NR 1 FLOOR PROXIMITY LIGHT ASSY FOR RETIREMENT. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001040900422 20010409 00422 NM 2001 4 9 TSAA0133030 1 20010303 A 3350 LIGHT BOEING 737 737230 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 REPLACED NR 6 FLOOR PROXIMITY LIGHT ASSEMBLY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001040900423 20010409 00423 NM 2001 4 9 GAIA01106OP 1 20010307 A 3350 LIGHT BOEING 727 727224 1384076 NM CABIN LOOSE A GAIA K NONE O OTHER CR CRUISE 1 SW 07 69739 20667 FLT 2031 - RNO-IND - DURING CRUISE, THE EMERGENCY EXIT LIGHT ILLUMINATED. THE AIRCRAFT LANDED WITHOUT ANY FURTHER DIFFI CULITIES. FOUND THE EMERGENCY EXIT LIGHT TO BE LOOSE IN ITS FIXTURE. RESECURED AS REQUIRED. OPERATIONALLY CHECKS GOOD . THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001040900424 20010409 00424 NM 2001 4 9 GAIA01108OP 1 20010306 A 2421 GENERATOR BOEING 727 727223 1384074 NM ENGINE MALFUNCTIONED A GAIA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 SW 07 6827 20180 FLT 2071 - GEG-PHX - AFTER TAKEOFF, LOSS OF ALL GENERATORS OCCURRED. AIRCRAFT MADE AN UNEVENTFUL LANDING IN GEG. RAN E NGINES AND GENERATORS. LOADED GENERATORS UP ELECTRICALLY, HYDRAULICALLY AND PNEUMATICALLY. RAN FOR 15 MINUTES WITH NO DEFECTS NOTED, PER BOEING MM 24. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001040900425 20010409 00425 EU 2001 4 9 USAA010256 1 20010306 A 7120 2170746 NUT AIRBUS 330 A330322 3930325 EU ENGINE MOUNT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 4464 315 CLT - FOUND NUT CRACKED .5 INCH, FORWARD LEFT BARREL NUT, AFT LEFT ENGINE MOUNT. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER EA 69252. (M) 2 L 7 2 4F RT A46NM 2001040900426 20010409 00426 NM 2001 4 9 01FDEA00165 1 20010226 A 5320 RIB BOEING 727 727247 138408F NM LT MLG CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 233FE 21327 DURING ROUTINE INSP, LT MLG UPLOCK FRAME REINFORCING RIB AT BS 910 FOUND CRACKED. *S/D* REMOVED DOUBLER, STOP DRILL CR ACK. REINSTALL DOUBLER PER IAW BAC 727 SRM 51-30-2. 2 L 7 3 4F A3WE 2001040900427 20010409 00427 WP 2001 4 9 MWEA010293 1 20010309 A 5320 3913576501 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 CENTERLINE INTERCOSTAL LONGERON 30, STATION 237-256 HAS CORROSION. REMOVED INTERCOSTAL, FABRICATED REPAIR, LOCATED, DRI LLED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001040900428 20010409 00428 EU 2001 4 9 USAA010257 1 20010306 A 7120 2170746 NUT AIRBUS 330 A330322 3930325 EU ENGINE MOUNT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 4464 315 CLT - FOUND NUT CRACKED .5 INCH, FORWARD INBOARD BARREL NUT, AFT LEFT ENGINE MOUNT. DEFECTIVE PART REPLACED WITH IDENTI CAL PART NR PER EA 69252. (M) 2 L 7 2 4F RT A46NM 2001040900429 20010409 00429 WP 2001 4 9 USAAD01042 1 20010303 A 2913 AS66411LS666 PUMP DOUG DC9 DC931 3022065 WP RT ENGINE FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 965VJ 34399 47374 MHT-PIT - FLT 1770 - DURING CLIMB-OUT, THE RIGHT HYDRAULIC PRESSURE DROPPED FOLLOWED BY THE LEFT HYDRAULIC PRESSURE. TH E ALTERNATE GEAR EXTENSION WAS USED. THE AIRCRAFT LANDED WITHOUT INCIDENT AND WAS TOWED TO THE GATE. MAINTENANCE REPLA CED THE RIGHT ENGINE DRIVEN HYDRAULIC PUMP. (M) 2 L 7 2 4F A6WE 2001040900430 20010409 00430 WP 2001 4 9 USAAD01043 1 20010304 A 3260 SENSOR DOUG DC9 DC981 3022081 WP RT MLG DIRTY A USAA K NONE N FALSE WARNING CL CLIMB 1 EA 19 800US 48034 PBI-PIT - FLT 1575 - DURING DEPARTURE, UPON GEAR RETRACTION THE RIGHT MAIN GEAR LIGHT REMAINED RED. THE LANDING GEAR WA S CYCLED AND ALL WAS NORMAL. MAINTENANCE CLEANED THE LANDING GEAR INDICATION SENSORS AND RELEASED THE AIRCRAFT FOR SERV ICE. (M) 2 L 7 2 4F A6WE 2001040900431 20010409 00431 NM 2001 4 9 USAA010176 1 20010226 A 5210 SILL BOEING 757 7572B7 1384964 NM DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 621AU 25863 27200 CLT - FOUND DOOR SILL OUTER CHORD CORRODED 38 INCHES, DOOR SILL FROM BS 560-612. INSTALLED REPAIR FILLERS AND SUPPORT A NGLE PER EA 69073. (M) 2 L 7 2 4F RT A2NM 2001040900432 20010409 00432 NM 2001 4 9 USAA010175 1 20010226 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 618AU 47860 22210 CLT - FOUND SKIN CORRODED 1 INCH BY 1 INCH, STATION 1300 INNER SKIN IN FRONT UNDER CARGO FLOOR. REPAIRED DOUBLER PER SR M 53-00-01 FIG 203 AND EA 69182. (M) 2 L 7 2 4F RT A2NM 2001040900433 20010409 00433 NM 2001 4 9 USAA010238 1 20010217 A 5313 STRINGER BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 618AU 47860 22210 CLT - FOUND STRINGER CORRODED 1 INCH BY 2 INCHES, AFT CARGO FLOOR STR AFT OF STATION 340 UNDER S28R. CORROSION LEVEL 1, TASK NR C53-155-02. CUT OUT CORRODED AREA, FABRICATED NEW STRINGER SECTION PER TR 53-10-01. (M) 2 L 7 2 4F RT A2NM 2001040900434 20010409 00434 NM 2001 4 9 USAA010250 1 20010214 A 5311 FRAME BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 618AU 47860 22210 CLT - FOUND FRAME CRACKED .25 INCH, STATION 1600 STRINGER 26R. INSTALLED DOUBLER PER T/R NR 53-60-01 REV A. (M) 2 L 7 2 4F RT A2NM 2001040900435 20010409 00435 NM 2001 4 9 01FDEA00166 1 20010226 A 5320 TIE CLIP BOEING 727 727247 138408F NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 233FE 21327 DURING ROUTINE INSP THE FUSELAGE TIE CLIP AT BS 1070, STR 8L FOUND CRACKED. *S/D* REMOVED CLIP OUT OF ALLOWABLE LIMITS PER IAW BAC 727 SRM 53-10-1. TREATED AND PRIMED PER IAW BAC 727 SRM 51-10-2. 2 L 7 3 4F A3WE 2001040900436 20010409 00436 NM 2001 4 9 01FDEA00167 1 20010226 A 5320 WEB BOEING 727 727247 138408F NM TORQUE BOX CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 233FE 21327 DURING ROUTINE INSP, AFT AIRSTAIR RT TORQUE BOX WEB LIGHTENING HOLE FOUND CRACKED AT BS 1223. *S/D* STOP DRILL CRACK P ER BAC 727 SRM 51-40-2. FAB AND INSTALL PER IAW BAC 727 SRM 51-40-2. 2 L 7 3 4F A3WE 2001040900437 20010409 00437 WP 2001 4 9 MWEA010294 1 20010309 A 5320 59197415 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 TWO INTERCOSTALS BETWEEN STATION 503-522 BELOW AND OUTBOARD OF NR 4 SEAT TRACK ARE CRACKED ON THE FORWARD ENDS. REMOVED INTERCOSTALS, FABRICATED, LOCATED, DRILLED AND INSTALLED DOUBLERS AND INTERCOSTAL. 2 L 7 2 4F A6WE 2001040900438 20010409 00438 WP 2001 4 9 MWEA010295 1 20010309 A 5311 991151515 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 FRAME STATION 160 AT LONGERON 30 HAD 3 ENLARGED HOLES. REMOVED INTERCOSTAL, REMOVED DAMAGED FRAME, LOCATED, DRILLED, IN STALLED NEW FRAME AND REINSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001040900439 20010409 00439 NM 2001 4 9 USAA010174 1 20010226 A 5320 ANGLE BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND ANGLE CRACKED .25 INCH, STATION 1320, RBL 46 CABIN FLOOR SUPPORT. INSTALLED PART PER SRM 51-10-02. (M) 2 L 7 2 4F RT A2NM 2001040900440 20010409 00440 NM 2001 4 9 USAA010220 1 20010227 A 5320 FLANGE BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND WEB FLANGE CRACKED, TOP FLANGE WEB, AFT NUT PLATE HOLE STATION 480-500. FABRICATED NEW UPPER CHORD ANGLE PE R BOEING DWG 284N1020-33 AND SRM 53-00-51 AND 51-10-00. (M) 2 L 7 2 4F RT A2NM 2001040900441 20010409 00441 NM 2001 4 9 USAA010190 1 20010228 A 5320 ANGLE BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND ANGLE CRACKED .25 INCH, STATION 1260, RBL 22 CABIN FLOOR SUPPORT. REMOVED CRACK AND FABRICATED PER SRM 53-6 0-01. (M) 2 L 7 2 4F RT A2NM 2001040900442 20010409 00442 WP 2001 4 9 USAAD01031 1 20010216 A 3350 LIGHT DOUG DC9 DC981 3022081 WP CABIN MISINSTALLED A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 802US 48036 MCO - A CONFIGURATION DEVIATION WAS FOUND IN THE OVERHEAD EMERGENCY LIGHTS SYSTEM. THE LIGHT BULB IN THE RIGHT EMERGENC Y LIGHT ASSEMBLY AT SEAT ROW 31 WAS REMOVED, LEAVING THE UNIT BLAND, TO COMPLY WITH THE CORRECT CONFIGURATION. (M) 2 L 7 2 4F A6WE 2001040900443 20010409 00443 EU 2001 4 9 USAAF01005 1 20010131 A 3232 125005 ACTUATOR FOKKER F28 F28MK0100 4990807 EU NLG DOOR BROKEN A USAA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 EA 19 887US 22415 11349 PHL-SYR - FLT 768 - AFTER GEAR UP WAS SELECTED, A LOUD FLUTTERING NOISE WAS PRESENT WITH A NOSE LANDING GEAR INDICATION LIGHT. THE FLIGHT RETURNED TO PHL AND MADE A NORMAL LANDING. MAINTENANCE REPLACED THE NOSE LANDING GEAR DOOR ACTUATOR. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT 2001040900444 20010409 00444 EU 2001 4 9 USAAF01007 1 20010225 A 2611 SMOKE DETECTOR FOKKER F28 F28MK0100 4990807 EU LAVATORY ACTIVATED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 852US 11280 PIT-MKE - FLT 1078 - AFTER TAKEOFF, RECEIVED A LAVATORY SMOKE DETECTOR WARNING. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. (M) 2 L 7 2 4F RT 2001040900445 20010409 00445 NM 2001 4 9 USAASB01068 1 20010228 A 3397 WIRE BOEING 737 737201 1384454 NM CABIN DAMAGED A K NONE L NO TEST IN INSP/MAINT 1 EA 19 256AU 22798 MCO - THE LOW LEVEL EMERGENCY LIGHT AT SEAT ROW 15 WAS INOPERATIVE. MAINTENANCE CLEARED THE AIRCRAFT TO OPERATE PER MEL PROCEDURES. DURING THE MAINTENANCE OVERNIGHT THE WIRING TO THE EMERGENCY LIGHT WAS REPAIRED. (M) 2 L 7 2 4F A16WE 2001040900448 20010409 00448 NE 2001 4 9 01FDEA00178 2 20010307 A 7261 FILTER BOEING 727 72722 1384002 NM PWA JT8 JT8D7B 52053 NE NR 3 ENGINE DIRTY A FDEA J E A DUMP FUEL ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 151FE 19147 653814 NR 3 OIL BYPASS LIGHT CAME ON. COMPLIED WITH RED TABS AND SHUTDOWN ENGINE. OIL PRESS AND TEMP NORMAL. *S/D* CHANGE F ILTER PER 727-100 MM 79-00-000-2, CHANGE OIL PRESS DIFFERENTIAL SWITCH AS PRECAUTIONARY DUE TO HEAVY CARBON BUILD UP ON FILTER PER MM 79-33-002-4. RAN ENG PER JRH NO LEAKS NOTED AND ALL ENG PARAMETERS NORM. 2 L 7 3 4F 4 F A3WE E2EA 2001040900449 20010409 00449 EU 2001 4 9 KBMA88703 1 20010310 A 6720 350A33214501 PITCH LINK SNIAS 350 AS350B2 8680813 EU TAIL ROTOR CRACKED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 53SH 4989 2009 TAIL ROTOR PITCH LINK CRACKED AT SILENT BLOCK. 1 G 7 1 3U H9EU 2001040900450 20010409 00450 CE 2001 4 9 20010322CW008 1 20010215 A 2822 2017002 PUMP RKWELL NA265 NA26565 7630107 CE GARRTT TFE731 TFE7313R1D 01518 WP FUEL BOOST INOPERATIVE B KI2R K NONE O OTHER IN INSP/MAINT 1 CE 01 7NR 1951 1951 46544 BOOST PUMP QUIT RUNING IN FLIGHT. SUSPECT FROZEN BEARING. THIS WAS APPROX 50 HRS BEFORE REQUIRED TIME CHANGE. RECOMME NDATIONS: REVIEWING FREQUENCY OF FAILURES AND ADJUSTING TIME CHANGE. 2 L 7 2 4J 4 F A2WE E6WE 2001040900454 20010409 00454 EU 2001 4 9 20010322CW010 1 20010214 A 2435 03601018 BEARING LUCAS AMD FALC10 FALCON10 2730101 EU GARRTT TFE731 TFE731* 01518 WP STARTER GEN FAILED B O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 GL 03 43EC 447 2700 168 UNIT REMOVED FOR SEVERE VIBRATION. DRIVE END BEARING HAD FAILED. BEARING RACE WAS RUSTED IN LINER OF END BELL AND COUL D NOT FLOAT. RECOMMEND LUBRICATION ON BEARING RACE WHEN INSTALLED. 2 L 7 2 4F 4 F A33EU E6WE 2001040900455 20010409 00455 SO 2001 4 9 20010322CW011 1 20010215 A 3233 89075005 ACTUATOR PIPER PA46 PA46350P SO LYC O540 IO540* 41532 EA RT MLG STUCK D K NONE O OTHER IN INSP/MAINT 1 EA 07 49PK 1273 4622050 DURING NORMAL GEAR EXTENSION THE RT MLG DID NOT INDICATE LOCKED. AFTER CYCLING THE GEAR & FISH TAILING IT INDICATED LOC KED & A NORMAL LANDING OCCURED. THE ACTUATOR WAS REMOVED AND DISASSEMBLED AND FOUND THAT ONE OF FOUR PAWLS THAT INTERAL LY LOCK THE COLLAR WAS STICKING & NOT COMPLETING THE LOCK. THE ACTUATOR WAS OVERHAULED & BENCH CKD OK. IT WAS REINSTALL ED AND OPS CKD OK. THIS IS A RECURRING PROBLEM THROUGHOUT THE FLEET. IT IS RECOMMENDED THAT 500 HR. I.R.A.N BE MADE A SERVICE ITEM FOR CONTINUED AIRWORTHINESS. IT IS BELIEVED ALSO, TO BE COLD RELATED. 1 L 7 1 3O 3 O RT A25SO 1E4 2001040900456 20010409 00456 NM 2001 4 9 2001UALA00148 1 20010226 A 5270 WARNING LIGHT AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE COCKPIT ILLUMINATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 814UA 862 DOOR 1R PRESSURE LIGHT ILLUMINATED. *S/D* CHECKED THE GIRT BAR FOR DEBRIS, CYCLED THE DOOR CLOSED, AND ARMED AND DISAR MED THE DOOR. ALL OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2001070300066 20010703 00066 NM 2001 7 3 2001UALA00157 1 20010225 A 2730 CONTROL UNIT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE ELEVATOR MALFUNCTIONED A UALA O OTHER F FLT CONT AFFECTED LD LANDING 1 WP 29 667UA 29239 ON LANDING NOSE PITCHED UP WITHOUT YOKE DISPLACEMENT. *S/D* UNABLE TO DUPLICATE PITCH-UP CONDITION. ACCOMPLISHED FULL ELEVATOR AND SPOILER OPERATIONAL CHECKS PER MM'S. ACCOMPLISHED MECHANICAL CHECKS OF FLAP AND AILERON SYSTEMS. REVIEWE D INFORMATION FROM FLIGHT DATA RECORDED. ACCOMPLISHED MINIMUM THREE TEST FLIGHTS WITH WING OBSERVERS. ALL OPS CHECKS N ORMAL. NO SIGNIFICANT FINDINGS OR FAILURES NOTED. 2 L 7 2 4F 4 F RT A1NM E24NE 2001040900458 20010409 00458 NM 2001 4 9 01FDEA00186 1 20010311 A 7931 WARNING LIGHT BOEING 727 727233 138408A NM COCKPIT ILLUMINATED A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 220FE 20934 NR 2 OIL PRESSURE/FILTER BYPASS LIGHT STAY ON LONGER THAN NORM. INFLT ENGINE SHUTDOWN ACCOMPLISHED. 2 L 7 3 4F RT A3WE 2001040900459 20010409 00459 NM 2001 4 9 GAIA01078OP 1 20010228 A 2750 652661433 TRANSMISSION BOEING 727 7272J0 138407E NM LT FLAP BINDS A GAIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SW 07 281KH 21105 FLT 281 - JAX - DURING APPROACH, THE INBOARD TRAILING EDGE FLAP INDICATOR WILL NOT MOVE PAST FOUR DEGREES IN FLIGHT. PER FORMED ABNORMAL PROCEDURE. DECLARED AN EMERGENCY WITH APPROACH CONTROL. THE AIRCRAFT LANDED WITHOUT ANY FURTHER DIFFIC ULTIES. REMOVED AND REPLACED NR 4 FLAP TRANSMISSION IAW BOEING MM 27-51-41. ALSO, REMOVED AND REPLACED THE INBOARD FLA P POSITION INDICATOR. OPERATIONALLY CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2001040900460 20010409 00460 NM 2001 4 9 GAIA01079OP 1 20010302 A 2613 WARNING LIGHT BOEING 727 727251 138408H NM COCKPIT ACTIVATED A GAIA K NONE N FALSE WARNING CR CRUISE 1 SW 07 279US 21158 FLT 723 - ROC-TOL, LOSER AFT BODY OVERHEAT MOMENTARY ILLUMINATION. ISOLATED BY LOWER AFT BODY OVERHEAT ILLUMINATION CHE CKLIST. COULD NOT GET LIGHT TO RE-ILLUMINATE. AIRCRAFT MADE AN UNEVENTFUL LANDING IN TOL. INSPECTED AIR CONDITIONING AND ANTI-ICE DUCTS FOR LEAKS IN AFT AIRSTAIR AREA AND AFT BELLY PIT. NO LEAKS WERE NOTED. INSPECTED OVERHEAT DETECTION LOOPS WITH NO DEFECTS NOTED. OVERHEAT DETECTION SYSTEM OPS CHECK NORMAL DURING ENGINE RUN. AIRCRAFT WAS RETURNED TO S ERVICE. (M) 2 L 7 3 4F A3WE 2001040900461 20010409 00461 NM 2001 4 9 EIA2001012 1 20010222 A 2410 705117H HOUSING BOEING 747 747273C 1384896 NM NR 2 CSD CRACKED A EIAA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 09 470EV 20653 RJCC - NR 2 ENGINE INDICATED OIL QTY LEAK OF APPROX 1 HAL/HR DIVERTED TO RJCC. OIL QTY DROPPED BELOW ZERO, IFSD NR 2 EN GINE. PERFORMED WINDMILL INSPECTION, NO DEFECTS. FOUND NR 2 CSD FILTER HOUSING CRACKED AND HEAT DAMAGED. REPLACED CSD AND GARLOCK SEAL. LEAK AND OP CHECKS NORMAL. (M) 2 L 7 4 4F A20WE 2001040900462 20010409 00462 NE 2001 4 9 20010406SG001 2 20010222 A 7261 804278 GARLOCK SEAL BOEING 747 747273C 1384896 NM PWA JT9 JT9D7J 52054 NE NR 2 ENGINE DAMAGED A EIAA E A ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CR CRUISE 1 NM 09 470EV 20653 RJCC - NR 2 ENGINE INDICATED OIL QTY LEAK OF APPROX 1 HAL/HR DIVERTED TO RJCC. OIL QTY DROPPED BELOW ZERO, IFSD NR 2 EN GINE. PERFORMED WINDMILL INSPECTION, NO DEFECTS. FOUND NR 2 CSD FILTER HOUSING CRACKED AND HEAT DAMAGED. REPLACED CSD AND GARLOCK SEAL. LEAK AND OP CHECKS NORMAL. REF EIA2001012. (M) 2 L 7 4 4F 4 F A20WE E20EA 2001040900463 20010409 00463 NM 2001 4 9 EIA2001014 1 20010221 A 3350 69B4601024 MODULE BOEING 747 747132 1384882 NM CABIN MALFUNCTIONED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 KJFK - EMERGENCY LIGHTS WOULD NOT SHUTOFF. REPLACED EMERGENCY LIGHT MODULE. (M) 2 L 7 4 4F A20WE 2001040900464 20010409 00464 NM 2001 4 9 EIA2001013 1 20010222 A 7922 VALVE BOEING 747 747212B 1384886 NM FUEL SYS MALFUNCTIONED A EIAA E ENGINE SHUTDOWN M OVER TEMP CR CRUISE 1 NM 09 485EV 20712 PANC - FLT 2914 - NR 4 ENGINE OIL TEMP INCREASED TO ORANGE/YELLOW BAND. FOLLOWED PROCEDURES IN ABNORMALS. 10 MIN LATER OIL TEMP INCREASED TO RED ZONE. IFSD NR 4 ENGINE. AFTER SHUT DOWN OIL TEMP SLOWLY BEGAN TO DECREASE TO 55C AT LANDING . REPLACED NR 4 FUEL HEAT VALVE. INSPECTION NR 4 OIL TEMP BULB/OIL TEMP IND WIRING. NO DEFECTS NOTED. PERFORMED HIGH POWER ENG RUNS FOR 35 MIN. OIL TEMP REMAINED BELOW 90C. FUEL HEAT APPLIED, GEN ON LINE, AIRCRAFT FULLY POWERED. NO T EMP FLUX NOTED. SYSTEM CHECKS NORMAL. (M) 2 L 7 4 4F A20WE 2001040900465 20010409 00465 WP 2001 4 9 GTIA010020 1 20010119 A 2160 CONTROL VALVE DOUG DC9 DC982 3022082 WP AC BAY MALFUNCTIONED A GTIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 957AS 49126 ACY - FLT 529 - AFTER TAKEOFF IN CLIMB, RIGHT AIR CONDITIONING PACK WENT FULL HOT. MANUAL CONTROL WOULD NOT CONTROL VAL VE. SMOKE FILLED THE AIRCRAFT. WENT HP BLEED OFF ON RT PACK AND RAM AIR ON AND SMOKE CLEARED. LANDING WAS NOT OVERWEI GHT. INSPECTED RT ACM AND ASSOCIATED DUCTING. NO DEFECTS NOTED. OPERATED RT A/C SYSTEM USING APU AND ENGINE SUPPLY AI R. ALL SYSTEMS OPS CHECK GOOD. ALL IAW MD-80 MM 21-31-00. (M) 2 L 7 2 4F A6WE 2001040900469 20010409 00469 WP 2001 4 9 GTIA010039 1 20010213 A 3350 LIGHT DOUG DC9 DC931 3022065 WP CABIN LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 969NK 47268 DCA - FLT 139 - AISLE PATH LIGHT, RED LOOSE. REPOSITIONED AISLE PATH LIGHT IAW MM 33-53-01. (M) 2 L 7 2 4F A6WE 2001040900470 20010409 00470 WP 2001 4 9 GTIA010029 1 20010201 A 3350 110049 CHARGER DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 805NK 48087 DTW - FOUND FORWARD ROW 1 TO 9 EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED CHARGER ASSY FORWARD SYSTEM, OPS CHECK S GOOD PER IAW MD-80 MM 33-53-00. (M) 2 L 7 2 4F A6WE 2001040900471 20010409 00471 WP 2001 4 9 GTIA010024 1 20010121 A 3350 SIGN DOUG DC9 DC983 3022083 WP CABIN MALFUNCTIONED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 DALLR 53015 DTW - FLT 632 - EXIT ROW EXIT SIGNS NOT ILLUMINATED. OPS CHECK EMERGENCY EXIT ROW SIGNS IAW 33-50-00. OPS CHECK GOOD, NO OTHER DEFECTS NOTED. (M) 2 L 7 2 4F RT A6WE 2001040900472 20010409 00472 WP 2001 4 9 GTIA010022 1 20010119 A 3350 25503025 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 DALLQ 53014 LGA - FORWARD ENTRY EXIT IDENTIFIER, FORWARD RIGHT SERVICE DOOR EXIT IDENTIFIER, AND FOUR FLOOR TRACK LIGHTS FOR EMERGEN CY LIGHTING INOPERATIVE. T/S TO BATTERIES IN B5-205 CHARGER AS PER WD 33-51-14. REMOVED AND REPLACED BATTERIES IN B5-20 5 CHARGER. EMERGENCY LIGHTS OPS CHECK NORMAL AS PER MM 33-53-00. (M) 2 L 7 2 4F RT A6WE 2001040900473 20010409 00473 WP 2001 4 9 GTIA010019 1 20010119 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN MISSING A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 DALLQ 53014 FLL - FLT 705 - FLOOR PATH LIGHTING LOOSE AND ON RED LIGHT MISSING IN THE AFT OF THE CABIN. REPLACED COVER AND SECURED RED OF LIGHT PATH. OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 2001040900478 20010409 00478 NM 2001 4 9 20010406SG004 1 20010210 A 3350 900542 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 802MA 245 MID CABIN OVERHEAD EMERGENCY EXIT SIGN LIGHT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY IAW MM 33-50-21, OPS CHECK OK. (M) 2 H 7 2 4T RT A13NM 2001040900479 20010409 00479 NM 2001 4 9 20010406SG006 1 20010210 A 3350 900835A BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 802MA 245 FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IAW MM 33-50-21, OPS CHECK OK. (M) 2 H 7 2 4T RT A13NM 2001040900480 20010409 00480 NM 2001 4 9 20010406SG007 1 20010214 A 3350 1000677 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 803MA 22434 ON PREFLIGHT TRANSIT, FOUND AFT AREA EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED AFT AREA EMERGENCY EXIT LIG HT IAW MM 33-50-81, OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 2001040900483 20010409 00483 CE 2001 4 9 20010312CW012 1 20010107 A 3230 358100946012 WORM GEAR BEECH 36 A36 1151604 CE CONT O550 IO550* SO MLG DAMAGED E EWPA K NONE O OTHER IN INSP/MAINT 1 SO 07 714BM 32 E3345 LANDING GEAR EMERGENCY EXTENSION HANDLE CORNER HAS BEEN SANDED OFF AND HANDLE ENGAGED DURING NORMAL GEAR OPERATION. INT ERNAL INSPECTION FOUND DAMAGE TO INTERNAL LDG GEAR BOX DRIVE WORM GEAR, REQUIRING REPLACEMENT. 1 L 7 1 3O 3 O 3A15 E3SO 2001040900484 20010409 00484 CE 2001 4 9 20010312CW013 1 20010107 A 3230 358100946012 WORM GEAR BEECH 36 A36 1151604 CE CONT O550 IO550* SO MLG DAMAGED E EWPA K NONE O OTHER IN INSP/MAINT 1 SO 07 475JM 12 E3368 LANDING GEAR EMERGENCY EXTENSION HANDLE CORNER HAS BEEN SANDED OFF AND HANDLE COULD BE ENGAGED DURING NORMAL GEAR OPERAT ION. CAUSING DAMAGE TO INTERNAL LDG GEAR BOX DRIVE WORM GEAR. 1 L 7 1 3O 3 O 3A15 E3SO 2001040900485 20010409 00485 WP 2001 4 9 MWEA010301 1 20010312 A 5320 99579455 ANGLE DOUG DC9 DC932 3022066 WP CARGO BAY CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FORWARD CARGO DOOR JAMB AREAS OF LIGHT CORROSION ON TOP SIDE OF UPPER JAMB BOX AREA. CORROSION IS ON BOTH LOWER ANGLES FOR AFT DOOR HINGE MOUNT AND ON STRUCTURE WHERE ANGLES MOUNT. LOCATED, BACKDRILLED AND INSTALLED NEW ANGLES. 2 L 7 2 4F A6WE 2001040900486 20010409 00486 CE 2001 4 9 20010312CW010 1 20010125 A 3340 509230015 BRACKET CESSNA 310 T310Q 2074244 CE CONT O520 TSIO520C 17040 SO STROBE CRACKED B CM2R K NONE O OTHER IN INSP/MAINT 1 SW 15 7542Q 10544 310Q0042 AC WAS IN THE HANGAR FOR 50 HOUR INSPECTION. STROBE LIGHTS WERE TURNED ON AND AN EXPLOSION DAMAGED THE LEFT WING TIP TAN K. FWD FAIRING WAS BLOWN APART BY AN EXPLOSION. FOUND THE FWD TANK ACCESS PANEL SPOT WELDS FOR THE NAV/STROBE LIGHT BR ACKETS WERE CRACKED, ALLOWING GAS FUMES TO COLLECT IN THE NOSE CONE AND CAUSE THE EXPLOSION. 1 L 7 2 3O 3 O 3A10 E8CE 2001040900487 20010409 00487 CE 2001 4 9 2401N813JW 1 20010206 A 3260 446EN19 SQUAT SWITCH LEAR 25 25 5170506 CE GE CJ610 CJ6101 30006 NE RT MAIN GEAR INOPERATIVE E KKFA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 813JW 25038 LANDING GEAR WOULD NOT RETRAACT. AIRCRAFT RETURNED TO BASE. REPLACED RT SQUAT SWITCH WITH NEW. OPERATIONAL CHECK OF L ANDING GEAR EXTENSION AND RETRACTION SYSTEM PERFORMED SATISFACTORY. 2 L 7 2 4J 4 J A10CE 1E16 2001040900488 20010409 00488 WP 2001 4 9 MWEA010300 1 20010312 A 5321 995791822 FLOOR PANEL DOUG DC9 DC932 3022066 WP CABIN CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 PANEL F6 HAS MANY AREAS OF CORROSION, DENTS AND CRACKED HOLES. REMOVED FLOORBOARD SKIN, FABRICATED FLOOR PANEL, AND HAT CHANNELS. INSTALLED CHAFE STRIPS AND HAT CHANNELS. 2 L 7 2 4F A6WE 2001040900489 20010409 00489 WP 2001 4 9 13001N71CK 2 20010202 A 7320 21011425 COMPUTER LEAR 35 36A 5170603 CE GARRTT TFE731 TFE731* 01518 WP LT ENGINE INOPERATIVE E KKFA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 23 71CK O35 P74520C LT ENGINE RPM ROLLED BACK 40 PERCENT DURING CLIMB, UNEVENTFULL LANDING ACCOMPLISHED. REPLACED LEFT ENGINE FUEL COMPUTER WITH SERVICEABLE UNIT. GROUND RUN AND FLIGHT TEST SATISFACTORY 2 L 7 2 4F 4 F A10CE E6WE 2001040900491 20010409 00491 EU 2001 4 9 KBMA88691 1 20010310 A 6520 BUSHING SNIAS 350 AS350B2 8680813 EU T/R SPIDER WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 53SH 4989 2009 TAIL ROTOR SPIDER SPLIT BUSHINGS WORN BEYOND LIMITS. 1 G 7 1 3U H9EU 2001040900498 20010409 00498 CE 2001 4 9 20010328CW007 1 20010220 A 5751 502100213 HINGE BRACKET CESSNA 414 414 2075908 CE RT WING WRONG PART B Q2AR K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 17 414RJ 4140632 FOUND ON INSPECTION, OUTBOARD RIGHT AILERON NOT STREAMLINED WITH TRAILING EDGE OF WING (APPROX .2500 HIGH) INVESTIGATIO N REVEALED INCORRECT OUTBOARD HINGE BRACKET INSTALLED DURING PREVIOUS WING REPAIR CAUSED BY INCORRECT PRINT IN 414 PARTS CATALOG. THE HINGE WAS DESIGNED TO BE A LEFT INSTALLATION BUT WAS INSTALLED ON RIGHT WING. 1 L 7 2 3O RT A7CE 2001040900499 20010409 00499 GL 2001 4 9 20010328CW008 2 20010224 A 7261 6887190 ENGINE BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL ENGINE BAY MAKING METAL E ALGR O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 27574 2562 CAE834168 ENGINE CHIP ILLUMINATED ON CAUTION PANEL. 1 G 7 1 3U 3 U H2SW E4CE 2001040900500 20010409 00500 CE 2001 4 9 20010323CW012 1 20010219 A 5720 511131417 ANGLE CESSNA 425 425 2076018 CE PWA PT6 PT6A60A 52043 NE WING CRACKED B EIPR K NONE O OTHER IN INSP/MAINT 1 WP 07 926ES 10223 4250029 WHILE INSPECTING FOR FUEL LEAKS A CRACK APPROXIMATELY 2.5 INCHES IN LENGTH WAS FOUND IN THE LEFT CANTED RIB, JUST AFT OF THE FORWARD SPAR, BELOW THE TOP SKIN. RECOMMEND REPLACEMENT OF THE ANGLE. 1 L 7 2 3T 4 T RT A7CE E4EA 2001040900501 20010409 00501 NE 2001 4 9 20010328CW009 1 20010224 A 3252 071119209 TRANSPONDER SKRSKY S76 S76 8143010 NE ALLSN 250C 250C30S 03013 GL MLG MELTED E ALGR O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 03 705AL 760267 890011S IN CRUSE FLIGHT, SMOKE IN COCKPIT, ACRID SMELL IN COCKPIT. PHOTOCELL AND ADJACENT AREA OF CONTROL HEAD MELTED. 1 G 7 2 3U 3 U H1NE E1GL 2001040900502 20010409 00502 NE 2001 4 9 20010328CW010 1 20010303 A 2612 7630607902104 FIRE DETECTOR SKRSKY S76 S76 8143010 NE ALLSN 250C 250C30S 03013 GL NR 1 ENGINE WILL NOT TEST E ALGR K NONE L NO TEST IN INSP/MAINT 1 SW 03 705AL 760267 89001S FOUND DURING PRE-START CHECK, FLAME DETECTOR WOULD NOT TEST. 1 G 7 2 3U 3 U H1NE E1GL 2001040900503 20010409 00503 GL 2001 4 9 20010328CW011 2 20010209 A 7200 23005290 ENGINE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL NR 2 FAILED E ALGA A UNSCHED LANDING F X J FLT CONT AFFECTED ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SW 03 376AL 18806 760002 890874S IN CRUSE FLIGHT A LOUD NOISE WAS HEARD AND SHARP YAW WAS EXPERIENCED. NR 2 N1 WAS AT 10 PERCENT, T5 WAS INCREASING THRO UGH 800 DEGREES C AND NR 2 FIRE LIGHT ILLUMINATED. FAILED ENGINE WAS VERIFIED AND EMERGENCY CHECK LIST FOLLOWED. PRELI MINARY UNCONTAINED BURST OF ONE OR MORE TURBINE WHEELS, ENGINE HAS NOT BEEN EVALUATED. 1 G 7 2 3U 3 U H1NE E1GL 2001040900504 20010409 00504 EA 2001 4 9 20010323CW013 2 20010212 A 8520 STD705 BOLT PIPER PA28 PA28140 7102802 SO LYC O320 O320E2A 41508 EA CRANKSHAFT MISSING D K NONE O OTHER IN INSP/MAINT 1 SW 99 7146R 5214 2821852 L1386027A DURING OIL PUMP AD COMPLIANCE, FOUND BOLT HEAD MISSING FROM IDLER SHAFT MOUNT. THIS IDLER SYSTEM IS BETWEEN CAM AND CRA NKSHAFT. IF THIS FAILS ENGINE WILL STOP. THERE WERE NO SQUAKS ON THIS ENGINE FAILURE WAS IMMANENT WITH NO PRIOR INDICA TION. PROBABLE CAUSE UNKNOWN, COULD BE OVER TORQUE OR BOLT MATERIAL FATIGUE. SUGGEST INSPECTION OF GEARS DURING MAG RE MOVAL TO DETECT LOOSE SHAFT, DAMAGE TO CASE REQUIRED TEARDOWN AND REPAIR O F IDLER SEAT PAD, AND UPDATED TO 5/16(.3125)I NCH BOLT HOLES. 1 L 7 1 3O 3 O 2A13 E274 2001040900506 20010409 00506 CE 2001 4 9 20010326CW001 1 20010122 A 5511 115970279 RIB BEECH 99 B99 1154004 CE PWA PT6 PT6A27 52043 EA HARTZL HCB3T HCB3T* GL HORIZONTAL STAB CRACKED G K NONE O OTHER IN INSP/MAINT 1 NM 07 950AA 32041 U159 DURING AN UNRELATED REPAIR, IT WAS DISCOVERED THAT THE LEFT HORIZONTAL TIP RIB WAS CRACKED. RIB WAS REPAIRED AND ADOUBL ER WAS INSTALLED. CRACKS WERE STOP DRILLED AS NECESSARY. DUE TO VIBARATION, THE LEFT REGION OF THE HORIZONTAL STABILIZ ER ON MOST OF THESE AIRCRAFT, SUSTAIN SIMILAR SIGNS OF FATIGUE THROUGH CRACKING OR RIVITS LOOSENING. PROP BALANCING AND FLIGHT CONTROL BALANCE CHECKS WILL NOW BE PERFORMED ON A MORE FREQUENT BASIS. 1 L 7 2 3T 4 T A14CE E4EA 6 C P15EA 2001040900507 20010409 00507 2001 4 9 KBMA88681 4 20010304 A 3422 5050010902 GYRO SNIAS 350 AS350BA 8680817 EU COCKPIT MALFUNCTIONED E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 1188P 9826 2347 DIRECTIONAL GYRO IS CRACKED AND MALFUNCTIONS WHEN POWER IS APPLIED. 1 G 7 1 3U NC H9EU 2001040900508 20010409 00508 EU 2001 4 9 KBMA88682 1 20010304 A 7110 TL100AXE12650 LATCH SNIAS 350 AS350B2 8680813 EU RT ENG COWL BROKEN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 345SH 26 3345 RIGHT AFT ENGINE COWLING LATCH BROKEN. 1 G 7 1 3U H9EU 2001040900509 20010409 00509 EU 2001 4 9 KBMA88686 1 20010306 A 6520 350A33215300 BEARING SNIAS 350 AS350BA 8680817 EU TAIL ROTOR DELAMINATED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 2273A 2959 2273 TAIL ROTOR BEARINGS DELAMINATED 1 G 7 1 3U NC H9EU 2001040900510 20010409 00510 NE 2001 4 9 KBMA88688 2 20010309 A 7321 016448620 FUEL CONTROL SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE LEAKING E KBMA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 19 350SH 4522 2957 FUEL CONTROL UNIT LEAKING (AFT SEAL DRAIN). NOTE: INSTALLED SN A947B FROM ENGINE 4126. PERMANENTLY INSTALLED SN A148B . 1 G 7 1 3U 3 U NC H9EU E19EU 2001040900511 20010409 00511 EU 2001 4 9 KBMA88690 1 20010310 A 7712 305731366 INDICATOR SNIAS 350 AS350BA 8680817 EU COCKPIT INTERMITTENT E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 270SH 7545 1864 TORQUE INDICATOR INTERMITTENT IN FLIGHT. 1 G 7 1 3U NC H9EU 2001040900512 20010409 00512 EU 2001 4 9 KBMA88693 1 20010310 A 7110 350A58154321 HINGE SNIAS 350 AS350B2 8680813 EU ENGINE COWL DAMAGED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 53SH 4989 2009 ENGINE COWLING HINGE RIPPED, WORN OUT. 1 G 7 1 3U H9EU 2001040900513 20010409 00513 NE 2001 4 9 20010312CW006 2 20010130 A 7322 5655578 CARBURETOR DHAV DH82 DH82 2801000 GL PWA R985 R985* 52008 NE HARTZL HCB3R HCB3R304 GL ENGINE MALFUNCTIONED D K NONE O OTHER IN INSP/MAINT 1 SW 11 67673 1284 42160005 EM119 AFTER TRYING TO START ENGINE, PILOT SMELLED FUEL. FURTHER INVESTIGATION REVEALED A STUCK FLOAT OR NEEDLE VALVE OR SUNKE N FLOAT. 1 Q 7 1 3I 3 R EXPA1Q71 5E1 5 C P28EA 2001040900514 20010409 00514 2001 4 9 HNAA0100017 4 20010308 A 3442 066308601 INDICATOR DHAV DHC8 DHC8102 2809003 NM COCKPIT DEFECTIVE A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 912HA 26596 235 040 WHILE PARKING THE AIRCRAFT CREW NOTICED RADAR INDICATOR CRT WAS COVERED WITH GREEN LINES AND A BURNING SMELL COMING FROM THE INDICATOR. REPLACED RADAR INDICATOR. 2 H 7 2 4T RT A13NM 2001040900515 20010409 00515 NM 2001 4 9 HNAA0100016 1 20010308 A 3350 82410162001 CONTROL BOX DHAV DHC8 DHC8102 2809003 NM COCKPIT MALFUNCTIONED A HNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 07 916HA 072 ON TAXI OUT THE EMERGENCY LIGHTS FLICKERED ON. REPLACED THE EMERGENCY LIGHTS CONTROL BOX. 2 H 7 2 4T RT A13NM 2001040900516 20010409 00516 WP 2001 4 9 AT0100105 1 20010308 A 3350 LIGHT DOUG DC9 DC932 3022066 WP L1 DOOR INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 802AT 47177 FOUND L-1 DOOR PORTABLE EMERGENCY LIGHT ASSEMBLY INOPERATIVE. INSTALLED PORTABLE EMERGENCY LIGHT ASSEMBLY. 2 L 7 2 4F A6WE 2001040900517 20010409 00517 NM 2001 4 9 CALA0100224 1 20010313 A 5230 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14325 23455 INSPECTION FOUND C-1 DOOR OUTER SKIN DENTED JUST AFT OF DOOR HANDLE. THE DENTED SECTION OF SKIN WAS REMOVED AND A DOUBL ER WAS INSTALLED IAW SRM 52-00-01, FIGURE 203. 2 L 7 2 4F RT A16WE 2001040900518 20010409 00518 NM 2001 4 9 CALA0100226 1 20010314 A 5230 WEB BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 47332 23570 INSPECTION FOUND A 3 INCHES CRACK IN C-1 DOOR WEB INSIDE FORWARD OF LOWER AFT DOOR STOP. A NEW DOOR WEB WAS INSTALLED I AW SRM 51-30-2. 2 L 7 2 4F RT A16WE 2001040900519 20010409 00519 NM 2001 4 9 CALA0100227 1 20010314 A 5230 STRUCTURE BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 47332 23570 INSPECTION FOUND A 2 INCH CRACK IN LOWER T-CHORD OF C-1 DOOR. THE T-CHORD WAS REPLACED IAW SRM 51-30-2. 2 L 7 2 4F RT A16WE 2001040900522 20010409 00522 NE 2001 4 9 UPS01435269 2 20010313 A 7200 ENGINE BOEING 747 747121 1384871 NM PWA JT9 JT9D7A 52054 NE NR 3 ENGINE MALFUNCTIONED A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 01 691UP 19641 INSPECTION TYPE:PFLT DURING INITIAL ROTATION FOR T/O SMOKE (LITE SMOKE) ENTERED COCKPIT AND SPREAD INTO CABIN. PUT ON O XY MASKS, INCLUDING 1 ACM FOLLOWED SMOKE ELIMINATION CHECK LIST. SMOKE CLEARED IN SHORT TIME. ODOR, BUT NOT OF RUBBER OR ELEC WIRING. *S/D* T/S REVEALED NR 3 ENGINE HAD HIGH O2 CONSUMPTION. FOUND NR 3 ENGINE EVC OFF SCHEDULE AT START, AS CAUSE OF O2 LOSS. PERFORMED ENGINE/EVC TRIM AS PRESCRIBED BY AMM 71-00-00. FURHTER O2 LOSS NOTED ON ENGINE RUN. 2 L 7 4 4F 4 F A20WE E20EA 2001040900524 20010409 00524 CE 2001 4 9 20010327CW013 1 20010220 A 3340 40010027 LIGHT CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE RUDDER FAILED B K NONE L NO TEST IN INSP/MAINT 1 NM 09 477KM 5500353 BEACON NOT OSCILLATING. FOUND LAMPS INSTALLED INCORRECTLY AND CANTED SIDEWAYS, LAMPS RUBBED AND GROUND ON GLASS. GEARS OR MOTOR WORN OUT. 1 L 7 2 4F 4 F A22CE E1NE 2001040900525 20010409 00525 CE 2001 4 9 20010327CW014 1 20010201 A 2130 CHECK VALVE LEAR 24 24 5170302 CE GE CJ610 CJ6106 30006 NE CABIN PRESSURE FAILED E CJPA K NONE O OTHER IN INSP/MAINT 1 NM 03 241JA 131 251 CABIN COULD NOT MAINTAIN PRESSURIZATION AT FL350, MAINTENANCE PERFORMED A GROUND PRESSURIZATION FUNCTIONAL CHECK NORMALL Y. A PNEUMATIC CHECK VALVE DISCOVERED WITH BROKEN SPRING WAS REPLACED, HOWEVER, INITIAL FLIGHT TEST WAS NOT SUCCESSFUL. MAINTENANCE TROUBLESHOT SUSPECTED LOSS OF PRESSURIZED AIR FROM RIGHT ENGINE AND REPLACED NR2 ENGINE FUEL CONTROL TO CO RRECT IMPROPER BLEED VALVE SCHEDULING, WHICH RESULTED IN MAINTAINING A NORMAL BLEED AIR SUPPLY. TEST FLIGHT FOR PRESSUR IZATION WAS GOOD. 2 L 7 2 4J 4 J A10CE 1E16 2001040900526 20010409 00526 NM 2001 4 9 EISA20010049 1 20010214 A 5344 525951 HINGE BOEING 727 727223 1384074 NM CARGO DOOR ELONGATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND MAIN CARGO DOOR HINGE AREA HAS ELONGATED HOLES. REAMED HOLES FABRICATED AND INS TALLED FREEZE PLUG BUSHINGS AND RADIUS FILLER STRAP, ALODINED AND PRIMED IAW SRM 51-10-2, 51-30-2, AND FVCI DRAWING 53-0 1035-1. 2 L 7 3 4F A3WE 2001040900527 20010409 00527 WP 2001 4 9 TWAA0104602 1 20010311 A 3350 60030431 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9625W 53595 THE FWD OVERHEAD EMERGENCY LIGHTS AROUND THE LIFE RAFT CONTAINER WOULD NOT EXTINGUISH WITH POWER OFF THE AIRCRAFT. PLAC ED EMERGENCY LIGHT SWITCH TO ARM FOR A HALF HOUR THEN LIGHTS STAYED OFF. ON FOLLOW UP THE NEXT STATION REPLACED THE BAT TERY PACK. CHECK-C 10-6-00 STL. 2 L 7 2 4F RT A6WE 2001040900528 20010409 00528 WP 2001 4 9 TWAA0104603 1 20010310 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCONNECTED A TWAA K NONE O OTHER CR CRUISE 1 CE 05 914TW 49185 THE EGRESS LIGHTS AT ROW 5 THRU 15 CAME ON DURING FLIGHT. ALL THE LIGHTS WENT OUT WITH THE EMERGENCY LIGHT SWITCH TURNE D OFF. RECONNECTED THE BATTERY PACK AT ROW 5. CHECK-C 2-13-01 STL. 2 L 7 2 4F A6WE 2001040900529 20010409 00529 WP 2001 4 9 TWAA0104604 1 20010309 A 3350 60030451LB BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A TWAA K NONE O OTHER NR NOT REPORTED 1 CE 05 914TW 49185 THE EGRESS LIGHTS COME ON AT ROW 5 TO 15. REPLACED THE EMERGENCY LIGHT BATTERIES. CHECK-C 2-13-01 STL. 2 L 7 2 4F A6WE 2001040900530 20010409 00530 WP 2001 4 9 TWAA0104605 1 20010310 A 3350 58222 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A TWAA K NONE O OTHER CR CRUISE 1 CE 05 914TW 49185 THE EMERGENCY LIGHTS CAME ON DURING FLIGHT AT ROW 5 THRU 15. REPLACED THE BATTERY PACK. CHECK-C 2-13-01 STL. 2 L 7 2 4F A6WE 2001040900531 20010409 00531 WP 2001 4 9 TWAA0104606 1 20010308 A 3350 AC4A SIGN DOUG DC9 DC983 3022083 WP L2 DOOR MISSING A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9304C 49530 THE EXIT LIGHT WAS MISSING AT THE LEFT SIDE NUMBER 2 CABIN DOOR. INSTALLED NEW EXIT SIGN ABOVE THE DOOR FRAME. CHECK-C 2-05-01 JFK. 2 L 7 2 4F RT A6WE 2001040900533 20010409 00533 NM 2001 4 9 TWAA0104608 1 20010312 A 5753 SKIN BOEING 767 767205 1385121 NM T/E FLAP DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 650TW 23057 DURING CHECK-C THE RT WING OTBD T/E FLAP OTBD END, 48 INCHES FROM THE OTBD END AND 7.5 IN FROM THE T/E HAD A 5 IN BY 3.7 5 IN DELAMINATION. INSTALLED REPAIR 9 IN BY 21 IN WET LAYUP USING SRM 51-70-17 AS GUIDE. PRIMED AND PAINTED PER MM 51- 22-02. 2 L 7 2 4F RT A1NM 2001040900534 20010409 00534 NM 2001 4 9 01FDEA00199 1 20010315 A 5230 DOOR BOEING 727 72725C 138400H NM CARGO BAY UNLATCHED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 124FE 19360 AFT CARGO LIGHT ON AT 14,000. BOTH PACKS WERE ON AND PRESS WAS STABLE. NO YAW PROBLEMS NOTED. FOUND AFT FAIRING DOOR UNLATCHED. SECURED LATCH. OPS NORMAL. OK FOR SERVICE. 2 L 7 3 4F A3WE 2001040900535 20010409 00535 CE 2001 4 9 20010312CW016 1 20010124 A 3234 S8012FPO CONNECTOR LEAR 25 25 5170506 CE GE CJ610 CJ6105 30006 NE GEAR SELECTOR DAMAGED E KKFA K NONE O OTHER IN INSP/MAINT 1 GL 23 39CK 14335 005 LANDING GEAR WOULD NOT EXTEND NORMALLY. PERFORMED EMERGENCY GEAR EXTENSION. UNEVENTFULL LANDING ACCOMPLISHED. REPLACE D LOOSE SOCKET AT GEAR SELECTOR SWITCH CONNECTOR J115. OPERATIONAL CHECK OF LANDING GEAR EXTENSION AND RETRACTION SYSTE M PERFORMED SATISFACTORY. NO RECOMMENDATION TO PREVENT RECURRENCE. 2 L 7 2 4J 4 J A10CE 1E16 2001040900536 20010409 00536 NM 2001 4 9 HNA0100018 1 20010311 A 2720 85500015001 PUSHROD DHAV DHC8 DHC8102 2809003 NM RUDDER STRIPPED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 943HA 167 DURING INSPECTION, THE LOWER RUDDER RADIUS ROD FORWARD ROD END WAS FOUND LOOSE. THE THREADED PORTION OF THE PUSH ROD TH READS WERE FOUND STRIPPED AND CHAFED INTO THE ROD. 2 H 7 2 4T RT A13NM 2001040900538 20010409 00538 EA 2001 4 9 JBXA000255 1 20010308 A 3030 7858062 SENSOR CNDAIR CL600 CL6002B19 EA EE BAY MALFUNCTIONED A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 579ML 7277 DURING CLIMBOUT, LEFT AOA HEAT CAUTION LIGHT ILLUMINATED. COMPLIED WITH QRH ABNROMAL 1L5. NO CHANGE IN CAUTION LIGHT. PER DISPATCH/ MOC DIRECTION, RETURN TO KRDU. REMOVED AND REPLACED NR 1 AIR DATA SENSOR HEATER CONTROLLER IAW CL-65 AMM 30-31-15. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2001040900539 20010409 00539 EA 2001 4 9 COMA0160305 1 20010308 A 2611 473052 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA CARGO BAY MALFUNCTIONED A COMA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING AP APPROACH 1 SO 01 987CA 8331 7199 CARGO SMOKE WARNING. REPLACED THE CARGO SMOKE DETECTOR. 2 L 7 2 4F RT A21EA 2001040900541 20010409 00541 CE 2001 4 9 20010313CW001 1 20010220 A 3211 5842000213 TRUNNION CESSNA 414 414 2075908 CE NLG CRACKED B Q2AR K NONE O OTHER IN INSP/MAINT 1 SW 17 414RJ 6585 4140632 FOUND TRUNNION CASTING CRACKED. 1 L 7 2 3O RT A7CE 2001040900545 20010409 00545 WP 2001 4 9 ABXA010101 1 20010312 A 5414 995815434 SKIN DOUG DC9 DC932 3022066 WP PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 52416 47364 RIGHT PYLON ELECTRICAL BAY AFT UPPER SKIN TO VERTICAL WEB ANGLE WAS CRACKED AT THE OUTBOARD BOLT HOLE. MAINTENANCE INSP ECTED AND REPAIRED THE PYLON IAW DC-9 SRM 54-01 FIG 2 SHEET 3. 2 L 7 2 4F A6WE 2001040900546 20010409 00546 WP 2001 4 9 ABXA010100 1 20010312 A 5320 49125151 CAP DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 53416 47364 LONGERON END CAP AT FUSELAGE STATION 996, LONGERON 29L WAS CRACKED. MAINTENANCE INSPECTED AND REPLACED THE LONGERON END CAP IAW DC-9 SRM. 2 L 7 2 4F A6WE 2001040900547 20010409 00547 WP 2001 4 9 ABXA010099 1 20010312 A 5320 49124591 ANGLE DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 52416 47364 EXFOLIATION FOUND ON ATTACH ANGLE AT THE FORWARD CARGO DOOR PAN, FUSELAGE STATION 389. MAINTENANCE INSPECTED AND REPLAC ED THE ATTACH ANGLE IAW DC-9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 2001040900548 20010409 00548 WP 2001 4 9 ABXA010097 1 20010312 A 5320 99579123 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 52416 47364 INTERCOSTAL WAS CRACKED AT FUSELAGE STATION 440 LONGERON 29L. MAINTENANCE INSPECTED AND REPLACED THE INTERCOSTAL IAW DC -9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2001040900549 20010409 00549 WP 2001 4 9 ABXA010096 1 20010312 A 5320 99579073 BRACKET DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 52416 47364 FLOORBEAM OUTBOARD ATTACH BRACKET WAS CRACKED AT FUSELAGE STATION 389 RBL 50. MAINTENANCE INSPECTED AND REPLACED THE BR ACKET IAW DC-9 SRM 21-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2001040900550 20010409 00550 WP 2001 4 9 ABXA010095 1 20010312 A 5320 D0489820 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 52416 47364 CUSP WEB LOCATED AT FUSELAGE STATION 598R WAS CRACKED. MAINTENANCE INSPECTED AND REPLACED THE WEB IAW DC-9 SRM 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 2001040900553 20010409 00553 NM 2001 4 9 COOSDR010005 1 20010405 A 5330 SKIN BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 395AJ 21100 SECTION 43-STA720E+11/STA720D+3, S26R AND ST720E+5.25 S26L. INTERNAL FUSELAGE SKIN CORRODED. 2 L 7 3 4F 4 F RT A3WE E2EA 2001040900554 20010409 00554 WP 2001 4 9 ABXA010094 1 20010312 A 5220 995773419 CLIP DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 52416 47364 LEFT FORWARD EMERGENCY EXIT DOOR HAD A CRACKED ATTACH CLIP ON THE UPPER PAN, AFT OF THE RELEASE HANDLE. MAINTENANCE INS PECTED AND REPLACED THE ATTACH CLIP IAW DC-9 SRM 51-30-2, 51-30-5, AND 51-10-3B. 2 L 7 2 4F A6WE 2001040900555 20010409 00555 WP 2001 4 9 ABXA010090 1 20010312 A 5210 5910081101 DOOR DOUG DC9 DC932 3022066 WP ENTRY DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 52416 47364 LOWER FORWARD ENTRY DOOR WAS CRACKED BEHIND THE LOWER HINGE. MAINTENANCE INSPECTED AND REPLACED THE FORWARD ENTRY DOOR. 2 L 7 2 4F A6WE 2001040900556 20010409 00556 WP 2001 4 9 ABXA010089 1 20010312 A 2740 591096231 JACKSCREW DOUG DC9 DC932 3022066 WP HORIZ STAB CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 82480 2480 47364 HORIZONTAL STABILIZER JACKSCREW THREADS HAVE PITTING CORROSION AND THE SCREW WAS GOUGED. MAINTENANCE INSPECTED AND REPL ACED THE JACKSCREW ASSEMBLY AND ACME NUT IAW DC-9 MM. 2 L 7 2 4F A6WE 2001040900557 20010409 00557 NM 2001 4 9 COOSDR010006 1 20010405 A 5315 FLOORBEAM BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 395AJ 21100 MAIN CARGO CABIN BS 720A FLOOR BEAM UPPER CHORD CORRODED, BETWEEN RBL 60 INCHES AND LBL 60 INCHES, WL 208. 2 L 7 3 4F 4 F RT A3WE E2EA 2001040900558 20010409 00558 NM 2001 4 9 COOSDR010007 1 20010405 A 5330 SKIN BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 395AJ 21100 LOWER FUSELAGE, SKIN CORRODED BETWEEN BS 117B TO BS 1183 BETWEEN STR 25L AND STR 26L. 2 L 7 3 4F 4 F RT A3WE E2EA 2001040900559 20010409 00559 NM 2001 4 9 COOSDR010008 1 20010405 A 5313 STRINGER BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 395AJ 21100 AFT CARGO COMPARTMENT, STRINGER 30 CRACKED AT BS 950. 2 L 7 3 4F 4 F RT A3WE E2EA 2001040900560 20010409 00560 NM 2001 4 9 COOSDR010009 1 20010405 A 5315 FLOORBEAM BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 395AJ 21100 MAIN CARGO CABIN, BS 950F, FLOORBEAM UPPER CHORD CORRODED, BETWEEN RBL 62 IN AND LBL 62 IN, WL 208. 2 L 7 3 4F 4 F RT A3WE E2EA 2001040900561 20010409 00561 NM 2001 4 9 COOSDR010010 1 20010405 A 5315 FLOORBEAM BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 395AJ 21100 MAIN CARGO CABIN BS 1030 FLOORBEAM UPPER CHORD CORRODED, BETWEEN RBL 62IN AND LBL 62 IN, WL 208. 2 L 7 3 4F 4 F RT A3WE E2EA 2001040900562 20010409 00562 NM 2001 4 9 COOSDR010011 1 20010405 A 5315 FLOORBEAM BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 395AJ 21100 MAIN CARGO CABIN BS 1110 FLOORBEAM UPPER CHORD CORRODED, BETWEEN RBL 61 IN AND LBL 61 INCHES, WL 208. 2 L 7 3 4F 4 F RT A3WE E2EA 2001040900563 20010409 00563 NM 2001 4 9 COOSDR010012 1 20010405 A 5315 FLOORBEAM BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 395AJ 21100 MAIN CARGO CABIN BS 1130 FLOOR BEAM LOWER CHORD CORRODED, BETWEEN RBL 45 INCHES AND LBL 45 INCHES. 2 L 7 3 4F 4 F RT A3WE E2EA 2001040900564 20010409 00564 WP 2001 4 9 TWAA0104501 1 20010308 A 3350 408822101 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A TWAA K NONE O OTHER TX TAXI/GRND HDL 1 CE 05 914TW 49185 A SECTION OF EGRESS LIGHTING IN THE FIRST CLASS CABIN ILLUMINATED DURING TAXI AND WOULD NOT RESET. REPLACED THE BATTERI ES IN THE POWER SUPPLY. CHECK-C 2-13-01 STL. 2 L 7 2 4F A6WE 2001040900565 20010409 00565 SO 2001 4 9 GLBA2001058 1 20010310 A 2821 FILTER EMB 120 EMB120ER 3260203 SO FUEL SYS DIRTY A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 01 299UX 120299 ABORTED T/O - LEFT FUEL PRESSURE ANNUNCIATOR ILLUMINATED. REMOVED AND CLEANED LOW AND HIGH PRESSURE FUEL FILTERS, OPS C HECKED GOOD. 2 L 7 2 4T RT A31SO 2001040900566 20010409 00566 CE 2001 4 9 GLBA2001059 1 20010312 A 5210 SEAL BEECH 1900 1900D 1154162 CE PAX DOOR OUT OF POSITION A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 240GL UE240 RETURN TO BLOCK - PAX DOOR LEAKING AIR, INSPECTED FOUND DOOR SEAL OUT OF POSTION. RESECURED DOOR SEAL, PERFORMED TEST F LIGHT AND OPS CHECKED GOOD. 2 L 7 2 4T RT A24CE 2001040900567 20010409 00567 NM 2001 4 9 COOSDR010013 1 20010405 A 5315 FLOORBEAM BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 395AJ 21100 MAIN CARGO CABIN BS 950C FLOORBEAM UPPER CHORD CORRODED, BETWEEN RBL 62 IN AND LBL 62 IN. 2 L 7 3 4F 4 F RT A3WE E2EA 2001040900568 20010409 00568 NM 2001 4 9 COOSDR010014 1 20010405 A 5315 FLOORBEAM BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 395AJ 21100 MAIN CARGO CABIN BS 380 FLOORBEAM UPPER CHORD CORRODED, BETWEEN RBL 62 IN AND LBL 62 IN, WL 208. 2 L 7 3 4F 4 F RT A3WE E2EA 2001040900569 20010409 00569 NM 2001 4 9 COOSDR010015 1 20010405 A 5315 FLOORBEAM BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 395AJ 21100 MAIN CARGO CABIN BS 720D FLOORBEAM UPPER CHORD CORRODED, BETWEEN 45 IN AND LBL 60 IN, WL 208. 2 L 7 3 4F 4 F RT A3WE E2EA 2001040900570 20010409 00570 NM 2001 4 9 COOSDR010016 1 20010405 A 5315 FLOORBEAM BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 395AJ 21100 MAIN CARGO CABIN BS 1070, FLOORBEAM UPPER AND LOWER CHORD CORRODED, BETWEEN RBL 61 IN AND LBL 61 IN, WL 208. 2 L 7 3 4F 4 F RT A3WE E2EA 2001040900571 20010409 00571 WP 2001 4 9 ABXA010093 1 20010312 A 5320 29560321 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 52416 47364 EXFOLIATION CORROSION FOUND UNDER NUT PLATE ON FLOOR SUPPORT AT STA 851, BETWEEN LONGERON 28 AND 27L. MAINTENANCE REPLA CED THE BRACKET AT STA 851 IAW DC-9 SRM. 2 L 7 2 4F A6WE 2001040900572 20010409 00572 WP 2001 4 9 ABXA010092 1 20010312 A 5311 591141625 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 52416 47364 LEFT FUSELAGE FRAME AT STATION 718 WAS CRACKED. MAINTENANCE REPLACED THE FRAME IAW DC-9 SB 53-131 AND ABX REA D953-4016 6-MR. 2 L 7 2 4F A6WE 2001040900573 20010409 00573 WP 2001 4 9 ABXA010091 1 20010312 A 5530 591241 ATTACH ANGLE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 52416 47364 A CRACK WAS FOUND ON RIGHT SIDE OF VERTICAL STABILIZER, STABILIZER TO FUSELAGE ATTACH ANGLE. MAINTENANCE INSPECTED AND REPAIRED THE CRACKED ATTACH ANGLE IAW ABX REA D953-40145. 2 L 7 2 4F A6WE 2001040900574 20010409 00574 NM 2001 4 9 COOSDR010018 1 20010405 A 5730 SKIN BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE RT WING CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 395AJ 21100 RT WING, LOWER SURFACE AT WS 320, STRINGER 8 SKIN CORRODED. 2 L 7 3 4F 4 F RT A3WE E2EA 2001072500489 20010725 00489 EU 2001 7 25 SIMA0492 1 20010218 A 3350 1317 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST UK UNKNOWN 1 SW 21 904AE 340B314 DFW - FLT 3525 - CREW REPORTED FLOOR PROXIMITY EMERGENCY LIGHT AT SEAT 5BC IS INOPERATIVE. PUT ON MEL AT THIS TIME. MA INTENANCE REPLACED BULB AT SEAT 5BC. OPS CHECK AS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001040900575 20010409 00575 SO 2001 4 9 SIMA0286 1 20010128 A 5610 163500110 WINDSHIELD EMB 135 EMB135LR SO COCKPIT CRACKED A SIMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 21 711PP 145235 ORD - FLT 4035 - FIRST OFFICER WINDSCREEN OUTER PLY CRACKED IN SPIDER WEB FORMATION. REMOVED AND REPLACED WINDSCREEN IA W AMM. (M) 2 L 7 2 4F RT TOOO11AT 2001040900576 20010409 00576 SO 2001 4 9 C2XA01TY050 1 20010320 A 3350 66366 LIGHT EMB 135 EMB135LR SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17521 145378 TYS DURING A SCHEDULED INSPECTION THE AFT EMERGENCY FLOOR TRACK LIGHTING STRIP WAS FOUND INOPERATIVE. MAINTENANCE INSP ECTED THE LIGHTING STRIP AND FOUND THE WIRES PULLED LOOSE FROM THE ASSEMBLY. THE LIGHTING STRIP WAS REMOVED AND REPLACE D IAW EMB-145 33-50-12, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT TOOO11AT 2001040900578 20010409 00578 WP 2001 4 9 AALA016018 1 20010216 A 3397 WIRE DOUG DC9 DC987 3022087 WP AFT AIRSTAIR BROKEN A K NONE L NO TEST NR NOT REPORTED 1 SW 21 754RA 49641 CCI-RNO - FOUND FORWARD OVERHEAD EMERGENCY LIGHT IN AFT STAIRWELL INOPERATIVE. REPAIRED BROKEN WIRE AT LIGHT ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 2001041000009 20010410 00009 SO 2001 4 10 C2XA01TY010 1 20010204 A 5330 14521721005 PLATE EMB 145 EMB145 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 TYS - DURING A SCHEDULED 1C INSPECTION, FORWARD DIGITAL PLATE JUST AFT OF COCKPIT DOOR HAS CORROSION ON AND AROUND RIVET HEADS. MAINTENANCE REMOVED CORRODED AREA, MEASURED DAMAGED AREA, FOUND MAX DEPTH TO BE .008 INCH. NO FURTHER ACTION N EEDED. REF EMB REF GST-203/2001. REPAIRS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001041000011 20010410 00011 NM 2001 4 10 VNAA0102017 1 20010225 A 3010 001B5784A3103200 DUCT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT WING FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 328JS 14604 3030 DURING FLIGHT THE LEFT ENGINE INLET DEICE AND LEFT OUTBOARD WING DEICE FAILED. THE FLIGHT DIVERTED TO PIT WHERE HIGH WIN DS AND TURBULENCE CAUSED A MISSED APPROACH. THE FLIGHT CREW THEN DIVERTED FOR MORE FAVORABLE LANDING CONDITIONS AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE LEFT OUTBOARD WING LEADING EDGE AS SEMBLY AND REPLACED THE LEFT ENGINE INLET DEICER TUBE. REPORTED OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001041000012 20010410 00012 EU 2001 4 10 DHL2001366011 1 20010307 A 2760 A274101600400 POSITION SWITCH AIRBUS 300 A300B4203 3930306 EU SPOILER INOPERATIVE A DHLA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 01 366DH 249 ASYMMETRIC SPOILER INDICATION ON FLIGHT CONTROL CHK. GROUND VERIFIED PROPER OPS OF SPOILER. DEFERRED RIGHT O/B SPOILER IND PER MEL 27-15-01-1. DMI 4640. T/S PERFORMED. FOUND RIGHT OUTBOARD SPOILER PICK-OFF ROD SW FROZEN. REMOVED AND R EPLACED SPOILER PICK-OFF ROD SW PER MM 27-65-00. OPS CHECK GOOD. THIS CLEARS DMI 4640. 2 L 7 2 4F RT A35EU 2001041000014 20010410 00014 NE 2001 4 10 01FDEA00183 2 20010310 A 7261 LINE BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE LEAKING A FDEA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 220FE 20934 NR 2 LOW OIL PRESSURE BYPASS LIGHT CAME ON. FOLLOWED BY LOSS OF OIL QUANTITY SHUT DOWN NR 2 IN FLT PER CKLIST. *S/D* FOUND MAIN SCAVENGE OIL LINE LEAKING AT COUPLING NUT PACKINGS DETERIORATING. REMOVED AND REPLACED PACKINGS PER MM 79-20 -002-2, MAIN OIL FILTER PER MM 79-00-000-3 AND OIL FILTER BYPASS SWITCH PER MM 7+-33-002-4. 2 L 7 3 4F 4 F RT A3WE E2EA 2001041000015 20010410 00015 WP 2001 4 10 TWAA0104601 1 20010309 A 3350 58222 POWER SUPPLY DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9306T 49567 THE EGRESS LIGHTS WERE INOPERATIVE AFT OF THE AFT GALLEY. REPLACED THE POWER PACK. CHECK-C 2-23-01 STL. 2 L 7 2 4F 4 F RT A6WE E2EA 2001041000016 20010410 00016 SO 2001 4 10 C2XA01CL055 1 20010308 A 3030 CS500060D4A RELAY EMB 135 EMB135LR SO COCKPIT BURNED A C2XA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 27 16520 145372 CLE FLIGHT 4276 THE CREW REPORTED A BURNING SMELL ALONG WITH SMOKE IN THE COCKPIT. ALSO RECEIVED A TAT NR 2 INOP MESSAG E ON THE EICAS. THE SMOKE CLEARED AFTER 10 MINUTES. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTE NANCE REMOVED AND REPLACED A BURNT TAT 2 CURRENT SENSOR KO494 AND A BURNT SOCKET XKO494. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT TOOO11AT 2001041000017 20010410 00017 EU 2001 4 10 C2XA01CL056 1 20010308 A 3260 D228830001 SENSOR AEROSP ATR42 ATR42320 8680930 EU NLG FAILED A C2XA K NONE J WARNING INDICATION AP APPROACH 1 SW 27 34820 159 CLE FLIGHT 3158 THE CREW REPORTED THE LANDING GEAR SYSTEM 1 NOSE GEAR UNLOCK LIGHT ILLUMINATED UPON GEAR EXTENSION. THE LIGHT REMAINED ON UNTIL AFTER TOUCHDOWN. MAINTENANCE REMOVED AND REPLACED SYSTEM 1 PROXIMITY SENSOR. OPERATIONAL CHEC KS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A53EU 2001041000018 20010410 00018 EU 2001 4 10 C2XA01CL057 1 20010309 A 3260 141FL01D3 UPLOCK SWITCH AEROSP ATR42 ATR42320 8680930 EU NLG STUCK A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 34820 159 SYR FLIGHT 3185 THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT RETURNED TO SYR AND LA NDED WITHOUT INCIDENT. ALSO REPORTED A LOUD BANGING SOUND UPON TOUCHDOWN. MAINTENANCE REMOVED AND REPLACED THE NOSE LA NDING GEAR UPLOCK SWITCH AND LUBRICATED THE NOSE LANDING GEAR. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A53EU 2001041000019 20010410 00019 EU 2001 4 10 01FDEA00188 1 20010228 A 5530 A5557011120000 FITTING AIRBUS 310 A310203 EU VERTICAL STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 442FE 353 TRANSVERSE LOAD FITTING HAS INTERGRANULAR CORROSION, TOP LT AND RT ATTACH POINT TO FWD VERTICAL STAB FRONT SPAR. 2 L 7 2 4F RT A35EU 2001041000023 20010410 00023 WP 2001 4 10 MWEA010302 1 20010313 A 5523 3913064 FITTING DOUG DC9 DC914 3022034 WP LT ELEVATOR BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 LEFT ELEVATOR INBOARD CONTROL TAB ATTACH FITTING IS BENT. REMOVED, FABRICATED AND INSTALLED FITTING. 2 L 7 2 4F A6WE 2001041000024 20010410 00024 WP 2001 4 10 MWEA010303 1 20010313 A 5320 5911264501 FITTING DOUG DC9 DC914 3022034 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 STRINGER 23 HAS DEEP GOUGES AT FORWARD STRINGER TO TEE ATTACH HOLE. REMOVED GOUGES, SPOT FACED HOLES AND INSTALLED HAT BUSHING. 2 L 7 2 4F A6WE 2001041000025 20010410 00025 WP 2001 4 10 MWEA010305 1 20010313 A 5330 591142865 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 FUSELAGE AT STATION 1050 BELOW LONGERON 22 RIGHT WAS GOUGED. BLENDED AREA, FABRICATED, LOCATED, DRILLED AND INSTALLED D OUBLER. 2 L 7 2 4F A6WE 2001041000026 20010410 00026 WP 2001 4 10 MWEA010306 1 20010313 A 5321 995791820 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 FORWARD CABIN FLOORBOARD E1 HAD CRACK PROPAGATING FROM MIDDLE OUTBOARD HOLE. REMOVED FLOORBOARD, FABRICATED DOUBLER, FI LLER, LOCATED, INSTALLED AND REINSTALLED FLOORBOARD. 2 L 7 2 4F A6WE 2001041000027 20010410 00027 WP 2001 4 10 MWEA010307 1 20010313 A 5320 5917579135 ANGLE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 SUPPORT ANGLE IN LEFT LAV AREA AT APB AND VENTRAL DOOR JAMB 10 INCHES UP FROM CUSP LINE WAS CRACKED. REMOVED ANGLE, FAB RICATED NEW ANGLE LOCATED, DRILLED AND INSTALLED. 2 L 7 2 4F A6WE 2001041000028 20010410 00028 WP 2001 4 10 MWEA010308 1 20010313 A 5311 991224381 SPAR DOUG DC9 DC932 3022066 WP RT PYLON WRINKLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 RIGHT FORWARD PYLON SPAR WEB BETWEEN UPPER AND LOWER SPAR CAPS WAS WRINKLED IN EXCESS OF .125. REMOVED WEB, FABRICATED, LOCATED DRILLED AND INSTALLED NEW WEB. 2 L 7 2 4F A6WE 2001041000029 20010410 00029 WP 2001 4 10 MWEA010309 1 20010313 A 5311 991224381 SPAR DOUG DC9 DC932 3022066 WP LT PYLON WRINKLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 LEFT PYLON SPAR WEB BETWEEN UPPER AND LOWER SPAR CAPS WAS WRINKLED TO A DEPTH OF .125 INCH. REMOVED WEB AND DOUBLER, FA BRICATED, LOCATED, DRILLED AND INSTALLED NEW WEB AND DOUBLER. 2 L 7 2 4F A6WE 2001041000030 20010410 00030 WP 2001 4 10 MWEA010310 1 20010313 A 5512 5910403570 SKIN DOUG DC9 DC932 3022066 WP HORIZ STAB CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 LEFT BOTTOM SIDE OF HORIZONTAL STAB STATION XHR 6.6 SKIN HAS CHAFE MARKS. BLENDED CHAFES AND FOUND ONE OUT OF LIMITS. FABRICATED REPAIR DOUBLER, LOCATED, DRILLED AND INSTALLED. 2 L 7 2 4F A6WE 2001041000031 20010410 00031 WP 2001 4 10 MWEA010311 1 20010313 A 5311 59356509 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 FRAME AT STATION 737 LEFT SIDE AT LONGERON 18 HAD CRACK AT FORWARD FLANGE. FABRICATED REPAIR DOUBLER, SHIMS, LOCATED, D RILLED AND INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001041000032 20010410 00032 WP 2001 4 10 MWEA010312 1 20010313 A 5320 995821527 SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 AFT CARGO SUPPORT STRUT AT STATION 917, LONGERON 23 LEFT HAD CORROSION AROUND FASTENER HOLES. REMOVED CORROSION, FABRIC ATED DOUBLER, AND INSTALLED. 2 L 7 2 4F A6WE 2001041000033 20010410 00033 WP 2001 4 10 MWEA010313 1 20010313 A 5347 59108203 SEAT TRACK DOUG DC9 DC932 3022066 WP CABIN CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 NR 3 SEAT TRACK HAS NUMEROUS AREAS OF MODERATE CORROSION STATION 198 - 237. REMOVED DAMAGED SECTION, FABRICATED NEW SEA T TRACK, INSTALLED SEAT TRACK REPAIR. 2 L 7 2 4F A6WE 2001041000034 20010410 00034 NM 2001 4 10 UPS01235273 1 20010219 A 5744 ATTACH FITTING BOEING 727 72722C 138400F NM FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, RT WING - CRACK AT NR 7 FLAP TRACK ATTACH AREA O/B FASTENER ROW, THIRD HOLE FROM FRONT. REPAIR CA RRIED OUT IAW SRM 51-30-5 & SMRO WO 2001-006-013 UPS ENGINEERING FILE NR B727-5730-14010-A. 2 L 7 3 4F A3WE 2001041000035 20010410 00035 EA 2001 4 10 COMA0160311 1 20010312 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA CABIN MISWIRED A COMA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 SO 01 769CA 7292 EMERGENCY FLOOR LIGHTS ARE INOP ROWS 1 THRU 5. FOUND WIRING BACKWARDS, REPAIRED WIRING AND SYSTEM TEST SATISFACTORY. 2 L 7 2 4F RT A21EA 2001041000036 20010410 00036 EA 2001 4 10 COMA0160312 1 20010302 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 809CA 7366 EMERGENCY LIGHT AT CABIN ENTRANCE IS INOPERABLE. SECURED WIRE CONNECTION, LIGHT OPERATES NORMAL. 2 L 7 2 4F RT A21EA 2001041000037 20010410 00037 EA 2001 4 10 COMA0160313 1 20010304 A 2700 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT ACTIVATED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 977CA 7157 CONFIG AILERON AND CONFIG SPOILER DURING T/O. COULD NOT DUPLICATE. OPERATIONAL CHECKS NORMAL. 2 L 7 2 4F RT A21EA 2001041000038 20010410 00038 EA 2001 4 10 COMA0160314 1 20010303 A 3350 363782 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 964CA 7129 EMERGENCY FLOOR LIGHTING AT ROW 1 IS INOPERABLE. REPLACED THE FLEXIBLE LAMP ASSY. 2 L 7 2 4F RT A21EA 2001041000039 20010410 00039 EA 2001 4 10 COMA0160315 1 20010302 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA RT FLAP MALFUNCTIONED A COMA K NONE F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 SO 01 804CA 3410 7352 FLAPS FAIL MESSAGE. REPLACED THE RT FLAP BPSU. 2 L 7 2 4F RT A21EA 2001041000040 20010410 00040 WP 2001 4 10 TWAA0104702 1 20010311 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 911TW 49182 A DENT 18 IN BY 12 IN BY 0.500 INCHES WAS FOUND ON PREFLIGHT, 8 FEET FWD OF THE FWD CARGO DOOR AND 30 IN AFT OF THE DRAI N MAST. FRAME BETWEEN LONGERON 24R AND 25R REPAIRED. LONGERON 25R STA 247 TO 287 REPAIRED. LONGERON 26R STA 247 TO 2 87 REPAIRED. SKIN REPAIRED STA 247 TO 287. CHECK-C 8-20-00 STL. 2 L 7 2 4F A6WE 2001041000041 20010410 00041 WP 2001 4 10 TWAA0104703 1 20010308 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 928TW 48012 DURING CHECK-C MAINT IN THE FWD CABIN, CORROSION WAS FOUND ON FLOOR SUPORT AT STA 218, BL ZERO, LBL 18 IN. FABRICATED N EW FLOOR SUPPORT, INSTALLED. 2 L 7 2 4F A6WE 2001041000042 20010410 00042 WP 2001 4 10 TWAA0104704 1 20010309 A 5320 FLOOR SUPPORT DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 992Z 47095 DURING OP 15 MAINTENANCE CHECK, FLOOR SUPPORT AT STA 160 TO 200, RBL 47 IN, WAS CORRODED. FABRICATED NEW FLOOR SUPPO RT, TREATED, PAINTED AND INSTALLED FASTENERS. 2 L 7 2 4F A6WE 2001041000043 20010410 00043 WP 2001 4 10 TWAA0104705 1 20010309 A 5320 FLOOR SUPPORT DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 992Z 47095 DURING OP 15 MAINTENANCE CHECK FOUND FLOOR SUPPORT AT STA 200, RBL 20 IN TO 43 IN, WAS CORRODED. FABRICATED NEW FLOOR S UPPORT, TREATED, PAINTED AND INSTALLED FASTENERS. 2 L 7 2 4F A6WE 2001041000044 20010410 00044 WP 2001 4 10 TWAA0104706 1 20010309 A 5320 WEB DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 992Z 47095 DURING OP 15 MAINTENANCE CHECK, FOUND MEMBRANE UNDER FLOOR AT STA 160 TO 200, RBL 21 INCHES, WAS CRACKED AND CORRODED. REMOVED DAMAGED MEMBRANE BETWEEN STA 160 TO 200, RBL 0 INCHES TO 44 IN. MADE NEW MEMBRANE AND INSTALLED. 2 L 7 2 4F A6WE 2001041000045 20010410 00045 WP 2001 4 10 TWAA0104707 1 20010309 A 5320 ANGLE DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 992Z 47095 DURING OP 15 MAINT CHECK THE RIGHT GALLEY SERVICE DOOR FRAME WAS CORRODED INSIDE THE AFT LOWER CORNER, INSIDE FRAME TO F LOOR STRUCTURE. CUT AND REMOVED CORRODED SECTION OF CUSP ANGLE FROM STA 164 TO 229. FABRICATED NEW CUSP ANGLE AND SPLI CED PARTS, TREATED AND PRIMED AREA. INSTALLED CUSP ANGLE AND SPLICES. 2 L 7 2 4F A6WE 2001041000046 20010410 00046 NM 2001 4 10 DHL2001741500 1 20010309 A 7110 SKIN BOEING 727 7272Q9 138448M NM NOSE COWL CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 NR 1 ENGINE NOSE COWL EXTERNAL SKIN HAS CRACK BETWEEN TWO FASTENERS EXTENDING INTO EXISTING DOUBLER REPAIR 9:00 POSITION NACELLE STA 80. REMOVED EXISTING DOUBLER REPAIR PER 727 SRM 57-30-2. CUT OUT ACCESS HOLE 8 INCHES DIA PER SRM 54-30-3 FIG 3. CUT OUT DELAMINATED AREA IAW B727 SRM 54-30-3. ACCOMPLISHED NDT HFEC INSPECTION PER SRM 51-00-00, CRACK CONTAI NMENT CONFIRMED. MADE PARTS FROM 2024T3 .032 LOT 192552. PO 8319541 3 INCH X 11 IN FILLER. MATERIAL FOR DOUBLERS 2024- T-3 .040 LOT 220081 PO 83110438 3.5 X 20 2 EA PER B727 SRM 54-30-3 PG 8B. ALODINED AND PRIMED PARTS IAW B 727 SRM 51-30 -2. INSTALLED PARTS IAW B727 SRM 51-30-2. MADE PARTS FOR CUTOUT ACCESS HOLE FROM 2024 T3 .063. 2 L 7 3 4F RT A3WE 2001041000047 20010410 00047 EA 2001 4 10 JBXA000257 1 20010312 A 3020 300013000002 ANTI-ICE VALVE CNDAIR CL600 CL6002B19 EA RT ENGINE FAILED A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 571ML 7209 RT COWL ANTI ICE MESSAGE INFLT AT N2 RPM OF GREATER THAN 78 PERCENT. AIR RETURNED TO RDU. REMOVED AND REPLACED RT COWL ANTI ICE VALVE IAW CRJ AMM 30-22-01, OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2001082100160 20010821 00160 SO 2001 8 21 C2XA01IA159 1 20010309 A 3260 12041126001 HARNESS EMB 120 EMB120ER 3260203 SO RT MLG FAULTY A C2XA O OTHER N FALSE WARNING CR CRUISE 1 SW 27 15732 120195 IAH - FLIGHT 3420, THE CREW REPORTED THAT THE REPORTED THAT THE RIGHT GEAR SYSTEM-B INTRANSIT LIGHT ILLUMINATED INTERMIT TENTLY IN FLIGHT. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE INDICATION ON MEL 32-60-1B CONTROL NUMBER 007710, A ND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RETURNED TO IAH ON 03-15-01 WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED B-SYSTEM WIRE HARNESS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001041000048 20010410 00048 SO 2001 4 10 C2XA01IA160 1 20010307 A 3350 12021299501 LIGHT EMB 120 EMB120ER 3260203 SO EXTERNAL INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 27716 120128 SHV - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT WING EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPER ATIVE. MAINTENANCE PLACED THE EMERGENCY LIGHT ON MEL 33-50-1/1 C, CONTROL NUMBER 007686, AND THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE LEFT WING EXTERNAL EMERGENC Y EXIT LIGHT, REMOVED THE MEL 33-50-1/1 C CONTROL NUMBER 007686, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001041000049 20010410 00049 WP 2001 4 10 MWEA010316 1 20010313 A 5313 591140617 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 LONGERON 4 LEFT IS CRACKED WHERE IT ATTACHES TO FRAME AT STATION 160. REMOVED DAMAGED SECTION, LOCATED, DRILLED AND INS TALLED NEW SECTION AND SPLICES. 2 L 7 2 4F A6WE 2001041000050 20010410 00050 WP 2001 4 10 MWEA010317 1 20010313 A 5320 991555048 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 AFT CARGO COMPARTMENT FROM STATION 980-996 BETWEEN LONGERON 28-27 RIGHT HAD CORROSION AROUND NUT PLATES ON INTERCOSTAL. REMOVED INTERCOSTAL, LOCATED, DRILLED AND INSTALLED NEW INTERCOSTAL AND CLIPS. 2 L 7 2 4F A6WE 2001041000051 20010410 00051 WP 2001 4 10 MWEA010318 1 20010313 A 5522 991848058 DOUBLER DOUG DC9 DC932 3022066 WP RT ELEVATOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 RIGHT ELEVATOR AT STATION XHS 158.0 TOP SKIN HAD CRACKS WHERE PANEL 3616A MOUNTS. REMOVED CRACKED DOUBLER, FABRICATED, LOCATED, DRILLED AND INSTALLED NEW DOUBLER. 2 L 7 2 4F A6WE 2001041000052 20010410 00052 WP 2001 4 10 MWEA010319 1 20010313 A 5321 991559811 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 CABIN FLOORBOARD B-4 HAD ONE CRACKED SCREW HOLE. CUT OUT DAMAGE, FABRICATED, LOCATED AND INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F A6WE 2001041000053 20010410 00053 WP 2001 4 10 MWEA010320 1 20010313 A 5321 995791820 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 CABIN FLOORBOARD F1 HAD LITE CORROSION ON FORWARD END. REMOVED SKIN, FABRICATED AND INSTALLED NEW SKIN. 2 L 7 2 4F A6WE 2001041000054 20010410 00054 WP 2001 4 10 MWEA010321 1 20010313 A 5313 591141581 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 STATION 756 LONGERON 5 LEFT WAS CRACKED AT FRAME. REMOVED DAMAGED SECTION, FABRICATED NEW REPAIR PARTS. LOCATED, DRILL ED AND INSTALLED. 2 L 7 2 4F A6WE 2001041000055 20010410 00055 WP 2001 4 10 MWEA010322 1 20010313 A 5347 27726601 SEAT TRACK DOUG DC9 DC932 3022066 WP CABIN CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 NR 2 SEAT TRACK FROM STATION 200-237 HAD AREAS OF LITE CORROSION. BLENDED AN AREA OUT OF LIMITS AND REMOVED SECTION OF TRACK. FABRICATED NEW SEAT TRACK AND SPLICE, LOCATED, DRILLED AND INSTALLED. 2 L 7 2 4F A6WE 2001041000056 20010410 00056 WP 2001 4 10 MWEA010323 1 20010313 A 5330 59114004 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 NOSE SKIN CRACKED IN 4 PLACES AT STATION 58, LONGERON 20 RIGHT. REMOVED DAMAGED AREA, FABRICATED, LOCATED, DRILLED AND INSTALLED NEW REPAIR DOUBLER AND FILLER. 2 L 7 2 4F A6WE 2001041000057 20010410 00057 WP 2001 4 10 MWEA010324 1 20010313 A 5330 5910228136 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 FUSELAGE AT STATION 1097 BELOW LONGERON 22 RIGHT WAS GOUGED. BLENDED GOUGE, FABRICATED, LOCATED, DRILLED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001041000058 20010410 00058 WP 2001 4 10 MWEA010325 1 20010313 A 5240 99115829 BEAM DOUG DC9 DC932 3022066 WP SERVICE DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 AT GALLEY DOOR NR 4 HORIZONTAL BEAM WAS CRACKED ON LOWER HINGE FORWARD CORNER. STOP DRILLED CRACK, FABRICATED, LOCATED, DRILLED AND INSTALLED REPAIR PARTS. 2 L 7 2 4F A6WE 2001041000059 20010410 00059 NE 2001 4 10 01FDEA00182 2 20010309 A 7261 RELIEF VALVE BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE STUCK A FDEA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 25 220FE 20934 NR 2 OIL BYPASS LIGHT ILLUMINATED. SECURE ENG PER RED TAB PROC. REMOVED AND REPLACED MAIN OIL SCREEN, FOUND FILTER PRE SSURE RELIEF VALVE STUCK. REMOVED AND REPLACED VALVE PER PW JT8D72-009G518C-518D. INSP OIL SCREEN PER MM 79-00-000-2. NONE NOTED. LEAK AND OPS CK GOOD. 2 L 7 3 4F 4 F RT A3WE E2EA 2001041000060 20010410 00060 NM 2001 4 10 01FDEA00181 1 20010309 A 2613 WARNING LIGHT BOEING 727 727227 1384078 NM COCKPIT ILLUMINATED A FDEA O OTHER N FALSE WARNING CR CRUISE 1 SO 25 482FE 21464 LWR AFT BODY OVERHEAT LIGHT CAME ON. AFT TURN RIGHT PACK OFF, SYS TEST OK AND FLT CONT ON ONE PACK. RUNNING 3 ENG AND BOTH AC PACKS ON INSP PNEU DUCTS ON AFT BODY COMP AND KEEL BEAM AREA. NO LEAKS NOTED. INSP SENSING ELEMENT BY PROXIMIT Y TO PNEU DUCT. NO FAULT FOUND. AC OK FOR SERVICE. 2 L 7 3 4F A3WE 2001041000061 20010410 00061 NM 2001 4 10 CALA0100221 1 20010312 A 2550 PANEL BOEING 737 7373T0 1384582 NM CARGO BAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 47332 23570 INSPECTION FOUND AFT CARGO RIGHT TRANSITION PANEL CORRODED FROM STA 727-747. THE TRANSITION PANEL WAS REPLACED. 2 L 7 2 4F RT A16WE 2001041000062 20010410 00062 NM 2001 4 10 CALA0100222 1 20010312 A 5330 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17329 23459 INSPECTION FOUND FUSELAGE SKIN GOUGED AT STA 395, STRINGER 20-21R. A DOUBLER WAS INSTALLED. 2 L 7 2 4F RT A16WE 2001041000063 20010410 00063 NM 2001 4 10 CALA0100223 1 20010313 A 5330 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17329 23459 INSPECTION FOUND FUSELAGE SKIN GOUGED AT L-1 DOOR TORQUE TUBE UPPER HINGE AREA, BS 312 , S13L. THE GOUGED AREA OF SKIN WAS REMOVED AND NEW SKIN WAS INSTALLED. 2 L 7 2 4F RT A16WE 2001041000064 20010410 00064 WP 2001 4 10 CALA0100225 1 20010313 A 5310 BEAM DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14889 49118 INSPECTION FOUND MID CARGO DOOR JAMB BEAM CORRODED. A DOUBLER, SPACER, AND FASTENERS WERE INSTALLED. 2 L 7 2 4F A6WE 2001041000065 20010410 00065 NM 2001 4 10 0100862702 1 20010309 A 3350 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8877Z 21450 DURING OVERNIGHT CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE FROM ROW 8 - 13. MAINTENANCE REPLACED BATTERY, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 2001041000066 20010410 00066 NM 2001 4 10 0100876303 1 20010311 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 663US 23818 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT LEFT WALL OF NR 1 GALLEY, DOOR 3L FLIGHT ATTENDAN T SEAT, AND PASSENGER SEAT 75B. MAINTENANCE RECONNECTED WIRING. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001041000067 20010410 00067 NM 2001 4 10 0100886305 1 20010311 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 665US 23820 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE BETWEEN ROWS 25ABC-31ABC. MAINTENANCE RECONNECTED L OOSE WIRING. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001041000068 20010410 00068 NM 2001 4 10 0100895518 1 20010227 A 2751 WARNING SYSTEM BOEING 757 757251 1384970 NM COCKPIT ACTIVATED A NWAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 01 518US 23206 TRAILING EDGE FLAP DISAGREE WARNING LIGHT ILLUMINATED WHEN FLAPS EXTENDED FROM FLAPS 15. PERFORMED COM PROCEDURES AND D ECLARED AN EMERGENCY. AN UNEVENTFUL LANDING WAS MADE WITH FLAPS AT 20. MAINTENANCE PERFORMED OPERATIONAL CHECK OF FLAP S, CHECKED OK. 2 L 7 2 4F RT A2NM 2001041000069 20010410 00069 WP 2001 4 10 0100901228 1 20010224 A 2612 FIRE LOOP DOUG DC10 DC1030 3023501 WP NR 3 ENGINE FAULTY A NWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 01 228NW 46578 EN ROUTE, ENGINE FIRE LIGHT ON FORWARD PANEL FLASHED INTERMITTENTLY. NR 3 START LEVER, NR 3 ENGINE FIRE HANDLE, AND NR 3 ENGINE LOOP ''A'' ALL CAME ON INTERMITTENTLY AND INCREASED IN FREQUENCY AND INTENSITY. REPLACED A AND B FAN AND CORE LOOP ASSEMBLIES AND FORWARD AND AFT PYLON LOOPS. OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 2001041000070 20010410 00070 NE 2001 4 10 0100916613 2 20010301 A 7230 ENGINE BOEING 747 747251B 1384892 NM PWA JT9 JT9D7J 52054 NE NR 4 ENGINE STALLED A NWAA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. R A PARTIAL RPM/PWR LOSS FLAME/FIRE LD LANDING 1 GL 01 613US 20358 662633 DURING LANDING ROLLOUT (NKT) WHILE COMING OUT OF REVERSE THRUST, THE NR 4 ENGINE COMPRESSOR STALLED. THE EGT ROSE TO 12 91C AND THE CONTROL TOWER REPORTED FLAMES FROM THE ENGINE. THE CREW FOLLOWED ENGINE FIRE PROCEDURES AND DISCHARGED ONE FIRE BOTTLE. MAINTENANCE INSPECTED THE ENGINE WITH NO EVIDENCE OF EXTERNAL FIRE NOTED. THE AIRCRAFT WAS FERRIED AND T HE ENGINE WAS REPLACED. 2 L 7 4 4F 4 F A20WE E20EA 2001041000071 20010410 00071 NM 2001 4 10 0100926303 1 20010305 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 663US 23818 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE BETWEEN PASSENGER DOOR 3L AND ROW 41 AND BETWEEN DOOR 4R AND ROW 29. MAINTENANCE REPAIRED BROKEN WIRE AND RECONNECTED LOOSE CONNECTOR. OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 2001041000072 20010410 00072 WP 2001 4 10 TWAA0104801 1 20010313 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 969TW 53619 THE EGRESS LIGHT WAS EXPOSED AND INOPERATIVE AT ROW 10 AND 17. RE-CONNECTED LIGHT STRIP AT ROW 17 AND REPLACED LIGHT CO VER AT ROW 10 DEFERRED CORRECTIONS. THE NEXT STATION REPLACED THE COVER, (P/N 0105601-001), AND RE-CONNECTED THE LIGHT STRIP AT ROW 17. CHECK-C 7-28-00 JFK. 2 L 7 2 4F RT A6WE 2001041000073 20010410 00073 WP 2001 4 10 TWAA0104802 1 20010313 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 928TW 48012 DURING CHECK-C MAINTENANCE, THE CABIN FLOOR MEMBRANE HAD A HOLE WITH CRACK EMITTING FROM THE HOLE AT LBL 8.5 IN AND STA 180. ACCOMPLISHED EDDY CURRENT INSPECTION AND FOUND CRACK CONTAINED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 2001041000074 20010410 00074 WP 2001 4 10 TWAA0104803 1 20010313 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 928TW 48012 DURING CHECK-C MAINTENANCE FOUND CABIN FLOOR TRACK AT LBL 45 INCHES HAD MATERIAL REMOVED BEYOND LIMITS ON CORROSION REM OVAL, STA 1088 TO 1127. REPLACED TRACK FROM STA 1030 TO 1308. 2 L 7 2 4F A6WE 2001041000075 20010410 00075 NM 2001 4 10 CALA0100229 1 20010314 A 5313 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 47332 23570 INSPECTION FOUND A .5 INCH CRACK IN STRINGER 16L AND 16R AT STA 500C. STRINGER REPAIRS WERE INSTALLED. 2 L 7 2 4F RT A16WE 2001041000076 20010410 00076 NM 2001 4 10 CALA0100230 1 20010314 A 5347 SEAT TRACK BOEING 737 7373Q8 1384670 NM CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14384 26313 INSPECTION FOUND INBOARD RIGHT SEAT TRACK CORRODED AT STA 360, RBL 10. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED A ND A NEW SECTION WAS INSTALLED. 2 L 7 2 4F RT A16WE 2001041000077 20010410 00077 SO 2001 4 10 SWIA972424 1 20010309 A 2722 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RUDDER FAILED A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 217SW 120286 ON LANDING APPROACH AT APPROXIMATELY 130 KNOTS WITH THE YAW DAMPER OFF, UNABLE TO MOVE THE RIGHT RUDDER PEDAL TO THE RIG HT PAST APPROX .25 TRAVEL. NO ASSOCIATED RUDDER LIGHTS ILLUMINATED. REPLACED BLUE SYSTEM RUDDER LINEAR ACTUATOR. S /N IN 0142, S/N OUT 611 RUDDER SYSTEM CHECKED GOOD WITH NO LEAKS. 2 L 7 2 4T 4 T RT A31SO E20NE 2001041000078 20010410 00078 SO 2001 4 10 SWIA972425 1 20010312 A 2752 3203001007 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE T/E FLAPS FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 188SW 120039 FLAP DISAGREEMENT ON OUTBOARD FLAPS WHEN SELECTING FLAPS 45 DEGREES. REPLACED LEFT OUTBOARD FLAP ACTUATOR. FLAP OPS CH ECKS GOOD. P/N ON 3203001007, S/N ON 0738, S/N OFF 850. 2 L 7 2 4T 4 T RT A31SO E20NE 2001041000079 20010410 00079 SO 2001 4 10 SWIA972426 1 20010302 A 3020 BOOT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE ENGINE INLET CONTAMINATED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 569SW 120344 BOTH ENGINE AIR INLET DEICE BOOTS FAILED ON CLIMBOUT. RETURNED TO FIELD. PURGED MOISTURE FROM LEFT AND RIGHT INLET BOO T TUBING. PERFORMED RUNUP. NO FAILURE DURING TEST. 2 L 7 2 4T 4 T RT A31SO E20NE 2001041000080 20010410 00080 SO 2001 4 10 SWIA972427 1 20010307 A 2731 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE ELEVATOR TAB FAILED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 290SW 120317 ELEVATOR TRIM FROZE AT FL 230 IN LEVEL FLIGHT. REPLACED BOTH NUMBER ONE AND NUMBER TWO ELEVATOR TRIM TAB ACTUATORS. OPS CHECK GOOD. NR 1 P/N ON 5299-0, S/N ON 635, S/N OFF 678, NR 2 P/N ON 529901, S/N ON 702, S/N OFF 543. 2 L 7 2 4T 4 T RT A31SO E20NE 2001041000081 20010410 00081 EA 2001 4 10 SWIA972428 1 20010314 A 2910 HYDRAULIC LINE CNDAIR CL600 CL6002B19 EA ENGINE LEAKING A SWIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 07 408SW 7055 DURING CLIMBOUT, LOST HYDRAULIC SYSTEM ONE PRESSURE AND QUANTITY. RETURNED TO SLC. FOUND HYDRAULIC LINE FOR ENGINE D RIVEN HYDRAULIC PUMP PSI LINE IN PYLON TO BE LEAKING. REMOVED AND REPLACED LINE. OPS CHECK AND LEAK CHECKED GOOD. 2 L 7 2 4F RT A21EA 2001041000082 20010410 00082 2001 4 10 SWIA972429 4 20010310 A 3418 COMPUTER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE STALL WARNING FAULTY A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 229SW 120305 AFTER TAKEOFF STALL WARNING LIGHT WITH ASSOCIATED TRIPLE CHIME WENT ON THEN OFF. REPEATED EVERY FEW MINUTES, BUT NO STA LL WARNING PANEL LIGHT. REPLACED NUMBER TWO STALL WARNING COMPUTER WITH SERVICEABLE UNIT. ALSO, REPLACED STALL WARNING CONTROL PANEL WITH SERVICEABLE ASSEMBLY. ALL CHECKS AND TESTS FOUND GOOD. COMP SN ON 748, SN OFF 751, CONT PAN EL SN ON 120-092R, SN OFF 083366999. 2 L 7 2 4T 4 T RT A31SO E20NE 2001041000083 20010410 00083 NM 2001 4 10 CALA0100232 1 20010316 A 5330 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 47332 23570 INSPECTION FOUND SKIN CORRODED AT AFT PRESSURE BULKHEAD BETWEEN STRINGER 29L AND 29R. THE CORRODED AREA OF SKIN WAS CUT OUT AND A REPAIR WAS INSTALLED. 2 L 7 2 4F RT A16WE 2001041000084 20010410 00084 NM 2001 4 10 CALA0100233 1 20010316 A 5320 STIFFENER BOEING 737 7373T0 1384582 NM BULKHEAD CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 47332 23570 INSPECTION FOUND FORWARD FACE LOWER RADIAL STIFFENER CORRODED AT AFT PRESSURE BULKHEAD. THE STIFFENER WAS REMOVED AND R EPLACED. 2 L 7 2 4F RT A16WE 2001041000085 20010410 00085 WP 2001 4 10 CALA0100234 1 20010317 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72822 49482 INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 200 - 220 BETWEEN LONGERON 16R AND 18R. A REPAIR DOUBLER WAS INSTA LLED. 2 L 7 2 4F A6WE 2001041000086 20010410 00086 WP 2001 4 10 CALA0100235 1 20010318 A 5311 FRAME DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14062 47863 INSPECTION FOUND FRAME CORRODED AT STA 1139, LONGERON 51L. THE CORRODED SECTION OF FRAME WAS REMOVED AND A NEW SECTION WAS INSTALLED. 2 L 7 3 4F A22WE 2001041000087 20010410 00087 WP 2001 4 10 TWAA0104909 1 20010314 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT IN AFT CABIN FOUND FLOOR SUPPORT STRUCTURE CORRODED AT STA 1250, LBL 23 AND RBL 43. REMOVED CORROD ED SUPPORT AND REPLACED WITH NEW PART. INSTALLED WITH HI-LOK FASTENERS. 2 L 7 2 4F A6WE 2001041000088 20010410 00088 WP 2001 4 10 TWAA0104910 1 20010314 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 928TW 48012 DURING CHECK-C MAINT FOUND CABIN NUMBER 2 CHAIR TRACK HAD CORROSION GROUND BEYOND LIMITS AT STA 1034 TO 1308. REPLACED SEAT TRACK FROM STA 1032 TO 1308. 2 L 7 2 4F A6WE 2001041000089 20010410 00089 WP 2001 4 10 TWAA0104911 1 20010314 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 928TW 48012 DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR SUPPORT AT STA 210, RBL 10. FABRICATED NEW FLOOR SUPPORT AND INSTA LLED. 2 L 7 2 4F A6WE 2001041000090 20010410 00090 NM 2001 4 10 TWAA0104912 1 20010314 A 5753 SKIN BOEING 767 7673Y0 NM T/E FLAP DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 632TW 24953 DURING CHECK-C MAINT FOUND DENT ON RIGHT WING ON BOTTOM SIDE OF TRAILING EDGE FLAP, 4 IN BY 4 IN BY .6875 INCH, OUTBOA RD AND AFT OF RT MAIN GEAR. APPLIED WET LAY UP. APPLIED CONDUCTIVE COAT AND PRIMER. 2 L 7 2 4F RT A1NM 2001041000091 20010410 00091 WP 2001 4 10 TWAA0104913 1 20010315 A 5320 WEB DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 992Z 47095 DURING OP 15 MAINT CHECK FOUND MEMBRANE SKIN UNDER CABIN FLOOR AT STA 200 TO 218, RBL 57, WAS CORRODED. FABRICATED NEW MEMBRANE AND INSTALLED RIVETS AND BOLTS. 2 L 7 2 4F A6WE 2001041000092 20010410 00092 WP 2001 4 10 TWAA0104914 1 20010315 A 5310 BEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 928TW 48012 DURING OP 16 MAINT CHECK IN MID CARGO COMPT, THE LOWER DOOR BEAM HAD CORROSION REMOVAL GROUND BELOW 25 PERCENT AT STA 64 6. REPAIRED BEAM. 2 L 7 2 4F A6WE 2001041000093 20010410 00093 WP 2001 4 10 TWAA0104915 1 20010315 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINTENANCE FOUND CORROSION ON CHAIR TRACK 2 1/2 L AT STA 1117 TO 1136. REPLACED PART WITH NEW AND INST ALLED. 2 L 7 2 4F A6WE 2001041000094 20010410 00094 WP 2001 4 10 TWAA0104916 1 20010315 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINTENANCE FOUND CABIN FLOOR TRACK NUMBER 2, RBL 22, WAS CORRODED TOP AND BOTTOM AT STA 1136 TO 1307. REMOVED 16 FT LENGTH OF TRACK AND REPLACED WITH NEW TRACK. 2 L 7 2 4F A6WE 2001041000095 20010410 00095 WP 2001 4 10 TWAA0104901 1 20010316 A 3010 39244421 REGULATOR VALVE DOUG DC9 DC982 3022082 WP ANTI-ICE SYS MALFUNCTIONED A TWAA K NONE O OTHER NR NOT REPORTED 1 CE 05 952U 49266 WITH WING ANTI-ICE ON, HOT SMOKEY SMELL FILLED THE CABIN. REPLACED THE RIGHT ANTI-ICE PRESSURE REGULATING VALVE. CHEC K-C 3-3-01 STL. 2 L 7 2 4F A6WE 2001041000099 20010410 00099 WP 2001 4 10 UPS01835324 1 20010319 A 2611 BATTERY DOUG DC8 DC873F 302199F WP SMOKE DETECTOR DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE LOWER CARGO COMPARTMENT FIRE DETECTOR SN FA2392 HAS LOW BATTERY FAULT. SMOKE DECTOR REMOVED AND R EPLACED BATTERIES AT DETECTOR FA2392. FOUND D BATTERY LEVELS LOW. REPLACED BATTERIES, LOWER CARGO SMOKE DETECTOR SYST EM OPS CKS NORMAL, DEFERRAL M210845 CLEARED. 2 L 7 4 4F RT 4A25 2001041000100 20010410 00100 2001 4 10 UPS01235325 4 20010321 A 2565 SLIDE BOEING 727 72722C 138400F NM DOOR OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE IN ESCAPE SLIDE FELL OUT. RE-PACKED EMERGENCY ESCAPE SLIDE. 2 L 7 3 4F A3WE 2001041000101 20010410 00101 WP 2001 4 10 UPS01835329 1 20010225 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE, C2, 3, STA 280 AT LONG 33R INTERCOSTAL, FRAME, AND INTERCOSTAL ATTACH FITTINGS ARE CORRODED BEYOND L IMITS. REMOVED AND REPLACED FITTINGS. REPAIRED FRAME AND INTERCOSTAL. 2 L 7 4 4F RT 4A25 2001041000102 20010410 00102 WP 2001 4 10 UPS01835332 1 20010228 A 5347 5750864593 SEAT TRACK DOUG DC8 DC873F 302199F WP CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE, C2, 3, STA 585 - 595 LBL 60 SEAT TRACK IS CORRODED BEYOND LIMITS. REPAIRED SEAT TRACK. 2 L 7 4 4F RT 4A25 2001041000103 20010410 00103 WP 2001 4 10 UPS01835333 1 20010227 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP CABIN DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE C2, 3, STA 70 SEAT TRACK SCALLOP IS BROKEN AT LBL 48. REPAIRED SEAT TRACK. 2 L 7 4 4F RT 4A25 2001041000104 20010410 00104 WP 2001 4 10 UPS01835334 1 20010223 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE, C2, 3, STA 345 LONG 27L AND BATHTUB FITTING ARE CORRODED BEYOND LIMITS. REPAIRED LONGERON AND REPL ACED BATHTUB FITTINGS. 2 L 7 4 4F RT 4A25 2001041000105 20010410 00105 WP 2001 4 10 UPS01835335 1 20010223 A 5320 561385725 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE C2, 3, STA -60 CUSP TO FRAME TFITTING IS CORRODED BEYOND LIMITS AT LBL 60. REMOVED, FABRICATED, AND REPLACED FITTING. 2 L 7 4 4F RT 4A25 2001041000106 20010410 00106 WP 2001 4 10 UPS01835336 1 20010227 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE, C2, 3, STA 270 LBL 48 SEAT TRACK IS CORRODED BEYOND LIMITS. REPAIRED SEAT TRACK. 2 L 7 4 4F RT 4A25 2001041000107 20010410 00107 WP 2001 4 10 UPS01835337 1 20010227 A 5347 5889588502 SEAT TRACK DOUG DC8 DC873F 302199F WP CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE C2, 3, STA 1580 RBL 24 SEAT TRACK IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED SEAT TRACK. 2 L 7 4 4F RT 4A25 2001041000108 20010410 00108 WP 2001 4 10 UPS01835338 1 20010224 A 5320 38949101N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE C2, 3, STA 415 LOWER FRAME TO CUSP FITTING IS CRACKED. REMOVED AND REPLACED FITTING. 2 L 7 4 4F RT 4A25 2001041000109 20010410 00109 NM 2001 4 10 F3LA200100047 1 20010320 A 5330 SKIN BOEING 737 7372P6 NM FUSELAGE DENTED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 272 3512 21613 DURING C1 CHECK, INSPECTION REPORTED 2 DENTS ON RIGHT FUSELAGE SKIN AT STA 1016, STR 20R. MAINTENANCE REMOVED DAMA GED AREA, FABRICATED FILLER, REPAIRED DOUBLER, AND INSTALLED. 2 L 7 2 4F RT A16WE 2001041000110 20010410 00110 EU 2001 4 10 RAIA00103012 1 20010319 A 3260 842503 PSEU AEROSP ATR42 ATR42300 8680920 EU EE BAY FAILED A RAIA O OTHER O OTHER CL CLIMB 1 CE 03 424TE 23276 20680 124 7406-STL- DURING CLIMB LANDING GEAR WOULD NOT RETRACT. MAINTENANCE REMOVED AND REPLACED THE PROXIMITY BOX. 2 H 7 2 4T RT A53EU 2001041000111 20010410 00111 NE 2001 4 10 RAIA00103013 2 20010320 A 7322 31059006 FUEL CONTROL JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE NR2 ENGINE FAILED A RAIA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CE 03 568HK 7537 1601 41086 75111 7060-JLN- DURING TAKEOFF NR 2 ENGINE WOULD NOT PRODUCE TAKEOFF TORQUE. MAINTENANCE REMOVED AND REPLACED NR 2 FUEL CONTR OL IAW GARRETT TPE331-14 MAINTENANCE MANUAL. 2 L 7 2 4T 4 T RT A41NM E18NE 2001041000112 20010410 00112 NE 2001 4 10 GLBA2001061 2 20010319 A 7532 BLEED VALVE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ENGINE MALFUNCTIONED A GLBA K NONE R PARTIAL RPM/PWR LOSS DE DESCENT 1 CE 01 153GL UE153 RIGHT ENGINE COMPRESSOR STALLING. RECLASSED BLEED VALVE TEST FLIGHT SATISFACTORY. 2 L 7 2 4T 4 T RT A24CE E26NE 2001041000113 20010410 00113 EU 2001 4 10 QXEA0100287 1 20010311 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-LEFT HAND FUSELAGE HAS A SHARP DENT BETWEEN FRAME 50-2 AND STRINGER 6-8 APPROXIMATELY WL 220. REPAIRED IAW FOKKER S RM 53-02-06. 2 L 7 2 4F RT A20EU 2001041000114 20010410 00114 EU 2001 4 10 QXEA0100288 1 20010306 A 5240 DOOR FOKKER F28 F28MK4000 4990810 EU A/C SERVICE DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CORROSION FOUND IN HOLES AROUND PANEL 25C (GROUND SUPPLY AIR CONDITIONING SERVICE DOOR). REPAIRED IAW FOKKER SRM 51 -31-01 PAGE 13-14. 2 L 7 2 4F RT A20EU 2001041000115 20010410 00115 EU 2001 4 10 QXEA0100289 1 20010302 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CORROSION FOUND UNDER MARKER BEACON ANTENNA. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, AND SRM 51-01-01, PAGE 3, SR M 53-15-01. 2 L 7 2 4F RT A20EU 2001041000116 20010410 00116 EU 2001 4 10 QXEA0100290 1 20010302 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-DENT FOUND BETWEEN STRINGER 60 AND 61 FRAME 7305 AND FRAME 7805 ON RIGHT HAND SIDE OF FUSELAGE. REPAIRED IAW FOKKER SRM 53-02-02, PAGE 2, AND SRM 53-17-03, PAGE 7. 2 L 7 2 4F RT A20EU 2001041000117 20010410 00117 EU 2001 4 10 QXEA0100291 1 20010302 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-SKIN UNDER AFT DME ANTENNA HAS MINOR SURFACE CORROSION. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, AND SRM 53-01-01, PAGE 3, SRM 51-10-04, PAGE 7. 2 L 7 2 4F RT A20EU 2001041000118 20010410 00118 EU 2001 4 10 QXEA0100292 1 20010302 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-SKIN UNDER LOWER ATC ANTENNA HAS MINOR SURFACE CORROSION. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, SRM 53-15-01, A ND SRM 51-10-04, PAGE 7. 2 L 7 2 4F RT A20EU 2001041000119 20010410 00119 EU 2001 4 10 QXEA0100293 1 20010302 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-FUSELAGE SKIN UNDER AFT RADIO ALTIMETER ANTENNA HAS MINOR SURFACE CORROSION. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 3 AND SRM 51-10-04, PAGE 7, SRM 53-15-01. 2 L 7 2 4F RT A20EU 2001041000120 20010410 00120 EU 2001 4 10 QXEA0100294 1 20010302 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-FUSELAGE SKIN UNDER FORWARD RADIO ALTIMETER ANTENNA HAS MINOR SURFACE CORROSION. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, SRM 53-01-01, PAGE 3, SRM 51-10-04, PAGE 7. 2 L 7 2 4F RT A20EU 2001041000121 20010410 00121 EU 2001 4 10 QXEA0100295 1 20010301 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-FORWARD RADIO ALTIMETER BLANKING PLATE SKIN CUTOUT HAS MINOR SURFACE CORROSION STATION 386.023, BLI, WL-64.960. REP AIRED IAW FOKKER SRM 53-01-01, AND SRM 51-10-04, PAGE 9. 2 L 7 2 4F RT A20EU 2001041000122 20010410 00122 EU 2001 4 10 QXEA0100296 1 20010302 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-SKIN CRACKED AT CENTER CARGO DOOR HANDLE TORSION BOX. REPAIRED IAW FOKKER SRM 52-02-01, PAGE 3. 2 L 7 2 4F RT A20EU 2001041000123 20010410 00123 EU 2001 4 10 QXEA0100297 1 20010226 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-LONGITUDINAL BUTT JOINT CRACKED BETWEEN FRAME 3850 - 3960 AND STRINGER 61, FOUND CRACK AT STATION 4460. REPAIRED IA W FOKKER SRM 51-31-01 AND SRM 53-30-03. 2 L 7 2 4F RT A20EU 2001041000124 20010410 00124 EU 2001 4 10 QXEA0100298 1 20010302 A 5320 STIFFENER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK ON HORIZONTAL STIFFENER ON AFT SIDE OF FRAME 3870 ABOVE LEFT HAND BLEED AIR DUCT ACCESS THROUGH FORWARD CARGO PIT. REPAIRED IAW FOKKER SRM 53-03-01, PAGE 7 AND SRM 51-31-01, PAGE 14. 2 L 7 2 4F RT A20EU 2001041000125 20010410 00125 EU 2001 4 10 QXEA0100299 1 20010302 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-FUSELAGE SKIN CHAFED AT LOWER EDGE OF FUSELAGE FAIRING 91BD. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 3, AND SRM 51-1 0-04, PAGE 7. 2 L 7 2 4F RT A20EU 2001041000126 20010410 00126 EU 2001 4 10 MALA010278 1 20010318 A 7810 NF24668057 NOZZLE SAAB SF340 SF340A 7850100 EU LT ENGINE DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 89XJ 089 ON FLIGHT 2797, LT INTAKE LIGHT ILLUMINATED IN FLIGHT. AIR RETURN TO BIS. MAINTENANCE REPLACED LT EXHAUST NOZZLE P/N N F24668057, S/N ON L291478, S/N OFF L293501. REPLACED DE-ICE CONTROL UNIT P/N 44730-501, S/N ON A00311, S/N OFF A00482. OPS AND SECURITY CHECKS GOOD. 2 L 7 2 4T RT A52EU 2001041000127 20010410 00127 EU 2001 4 10 MALA010279 1 20010319 A 2434 51539007B GENERATOR SAAB SF340 340B 7860101 EU RT ENGINE DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 436XJ 436 ON FLIGHT 3116, RIGHT DC GENERATOR FAILED IN FLIGHT, ACCOMPLISHED ORH, COULD NOT GET BACK ONLINE. AIR RETURN TO MSP. M AINTENANCE REPLACED RIGHT DC GENERATOR P/N 51539-007B, S/N ON 98079, S/N OFF 97814 IAW AMM 24-30-00. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2001041000128 20010410 00128 EU 2001 4 10 DHL2001366012 1 20010316 A 7120 A5461149650000 SHIM AIRBUS 300 A300B4203 3930306 EU NR 2 ENG MOUNT CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 366DH 249 AFT ENGINE MOUNT ATTACH FITTING SHIM CORRODED, NR 2. REPLACED AFT ATTACH FITTING SHIM IAW M/M 54-42-25, PG 401. 2 L 7 2 4F RT A35EU 2001041000129 20010410 00129 EU 2001 4 10 DHL2001364011 1 20010113 A 7120 A5461000920001 SHIM AIRBUS 300 A300B4203 3930306 EU NR 1 ENG MOUNT CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH LT ENGINE NR 1 AFT ENG MOUNT HAS PITTED AND CORROSION ON PYLON SHIM. OPENED ACCESS PNL, REMOVED PRECOOLER, REMOVED PLEN UM PNL MM 72-20-01. STARTED REMOVAL OF ATTACHING HARDWARE, REMOVED AFT MOUNT AREA VIS INSP UPON SHIM REMOVAL, NO DEFECT S. REMOVED AND REPLACED NR 1 AFT MOUNT PYLON SHIM (IAW 54-42-25). INSTALLED PRECOOLER ON NR 1 PYLON MM 36-11-15, LEAK CHK OK. 2 L 7 2 4F RT A35EU 2001041000130 20010410 00130 EU 2001 4 10 QXEA0100302 1 20010311 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-SLIGHT CORROSION FOUND UNDER LOWER VHF COMM ANTENNA FORWARD POSITION. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, AND HORIZON AIR EA 4-53-1454. 2 L 7 2 4F RT A20EU 2001041000131 20010410 00131 EU 2001 4 10 QXEA0100303 1 20010306 A 5230 STRUCTURE FOKKER F28 F28MK4000 4990810 EU CARGO DOOR PUNCTURED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-PUNCTURE AT AFT LOWER RADIUS OF REAR CARGO DOOR. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, 14, AND SRM 51-31-03, P AGE 10, 11. 2 L 7 2 4F RT A20EU 2001041000132 20010410 00132 EU 2001 4 10 QXEA0100304 1 20010306 A 5230 ANGLE FOKKER F28 F28MK4000 4990810 EU CARGO DOOR BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-BROKEN REINFORCEMENT ANGLE AT FORWARD LOWER CORNER OF REAR CARGO DOOR. REPAIRED IAW FOKKER SRM 52-30-00 AND SRM 51- 31-03, PAGE 10, 11. 2 L 7 2 4F RT A20EU 2001041000133 20010410 00133 EU 2001 4 10 QXEA0100305 1 20010313 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-GOUGED SKIN AT FORWARD LOWER REAR CARGO DOOR APERTURE. REPAIRED IAW FOKKER SRM 52-01-01, PAGE 7 AND SRM 51-10-04. 2 L 7 2 4F RT A20EU 2001041000134 20010410 00134 EU 2001 4 10 QXEA0100306 1 20010306 A 5230 ANGLE FOKKER F28 F28MK4000 4990810 EU CARGO DOOR BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-BROKEN REINFORCEMENT ANGLE AT AFT LOWER CORNER OF REAR CARGO DOOR. REPAIRED IAW FOKKER SRM 51-31-03, PAGE 10, 11 AN D SRM 52-30-00. 2 L 7 2 4F RT A20EU 2001041000135 20010410 00135 EU 2001 4 10 SIMA0393 1 20010208 A 3310 LIGHT SAAB SF340 340B 7860101 EU COCKPIT MALFUNCTIONED A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 313AE 340B313 FLT 4580 - BOS - FLIGHT STATUS PANEL LIGHTS ALL FAILED AFTER TAKEOFF. RESET C/B, OPS CHECK GOOD IAW AMM. (M) 2 L 7 2 4T RT A52EU 2001041000136 20010410 00136 EU 2001 4 10 20010409SG001 1 20010221 A 2132 22250F060200 INDICATOR AEROSP ATR42 ATR42300 8680920 EU COCKPIT DEFECTIVE A SIMA B EMER. DESCENT P NO WARNING INDICATION CL CLIMB 1 SW 21 135MQ 135 MIA - FLT 5200 - CREW REPORTED THAT DURING CLIMB THROUGH 18,000 FEET, IT WAS NOTED THAT THE CABIN DIFF WAS INDICATING 1. 5 PSI. CABIN PRESSURE ROSE TO 10,000 AND AN EMERGENCY DESCENT PROCEDURE WAS APPLIED. ONCE MANUAL MODE WAS SELECTED, CA BIN FAILED TO PRESSURIZE IN EITHER AUTO OR MANUAL MODE. MAINTENANCE REMOVED AND REPLACED DIGITAL CONTROLLER AND CABIN/P RESSURE INDICATOR IAW ATR MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0522. (M) 2 H 7 2 4T RT A53EU 2001041000137 20010410 00137 NE 2001 4 10 20010410AP026 2 20010225 A 7200 ENGINE BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE NR 1 FAILED A MYWA E C ENGINE SHUTDOWN ABORTED TAKEOFF K X T FLUID LOSS ENGINE FLAMEOUT ENGINE CASE PENETRATION TO TAKEOFF 1 SO 19 804MA 22435 685520 AT TAKEOFF THRUST SETTING (ANV) LOUD EXPLOSION HEARD IN COCKPIT AND NR 1 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED AND O IL QUANTITY DECREASED TO 2 GAL THEN INCREASED TO 3 GAL AFTER SHUTDOWN. ABORTED TAKEOFF AND PERFORMED EMERGENCY ENGINE S HUTDOWN PROCEDURES PER AOM 2-1-2. RETURNED TO RAMP. OIL PRESSURE ALSO DECREASED TO 20 PSI AND CONTINUED TO DECREASE. DISCOVERED T3/T4 HAD SEPARATED FROM ENGINE CAUSING DAMAGE TO TAIL PIPE ASSY. REMOVED AND REPLACED NR 1 ENGINE. OPS CHE CK OK. LEAK CHECK OK IAW B727 MM 71-00. (M) 2 L 7 3 4F 4 F A3WE E2EA 2001041000138 20010410 00138 NM 2001 4 10 20010409SG002 1 20010227 A 7920 496142 LINE BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE CRACKED A MYWA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 887MA 21857 700297 IN FLIGHT NR 2 ENGINE BEGAN LOSING OIL AT RATE OF 1 QUART EVERY 9 MINUTES. REDUCED THRUST DID NOT AFFECT RATE. SHUT DO WN ENGINE WITH 1 GALLON REMAINING. ENGINE WINDMILLED 30 MINUTES, OIL PRESSURE 42 PSI. T/S ENGINE, FOUND NR 2 ENGINE NR 2 BEARING LINE CRACKED AT B-NUT FITTING. REMOVED AND REPLACED LINE. REMOVED AND REPLACED MAIN OIL SCREEN. PERFORMED ENGINE POWER RUN AT TAKEOFF POWER. NO LEAKS NOTED IAW 71-00-00 AND 79-00-00. RESERVICED OIL AS REQUIRED. (M) 2 L 7 3 4F 4 F A3WE E2EA 2001041000139 20010410 00139 NM 2001 4 10 20010409SG003 1 20010131 A 5751 SKIN BOEING 757 757* NM AILERON DELAMINATED A N8TA K NONE O OTHER IN INSP/MAINT 1 WP 19 508NA 26244 RIGHT AILERON UPPER SURFACE DELAMINATED 40 INCHES INBOARD OF OUTBOARD END 6 INCHES FORWARD OF TRAILING EDGE. REPAIRED I AW SRM. (M) 2 L 7 2 4F RT A2NM 2001041000140 20010410 00140 NM 2001 4 10 20010409SG004 1 20010208 A 2550 453N162513 TUBE BOEING 757 757* NM CARGO BAY CRACKED A N8TA K NONE O OTHER IN INSP/MAINT 1 WP 19 508NA 26244 BLOW OUT GRILL AFT CARGO COMPARTMENT RIGHT WALL, CRACKED AND BENT. REPLACED DAMAGED TUBES IAW BOEING DRAWING 453N1625. (M) 2 L 7 2 4F RT A2NM 2001041000141 20010410 00141 NM 2001 4 10 20010409SG005 1 20010202 A 5347 451N5700101 FITTING BOEING 757 757* NM CARGO BAY CORRODED A N8TA K NONE O OTHER IN INSP/MAINT 1 WP 19 508NA 26244 FOUND SURFACE CORROSION IN AREA OF NET TIE DOWN .050 INCH BY 1.5 INCH BY 1 NICH, BS 1442, RBL 22. REPLACED CARGO TIE DO WN FITTING. (M) 2 L 7 2 4F RT A2NM 2001041000142 20010410 00142 NM 2001 4 10 20010409SG006 1 20010219 A 2750 FSEU BOEING 757 757200 1384950 NM FLAP/SLAT FAILED A N8TA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 19 506NA 24771 DURING CLIMB, AT FLAP RETRACTION LE SLAT DISAGREE MESSAGE ON EICAS ILLUMINATED AND SLAT/FLAP POSITION INDICATOR INDICATE D SLATS NOT RETRACTED. RETURNED TO DEPARTURE STATION AND ACCOMPLISHED UNEVENTFUL LANDING. INVESTIGATION REVEALED BOTH FSEU''S FAULTED PDU SLAT XMITTER. RESET BOTH FSEU''S FLAPS/SLATS OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A2NM 2001041000143 20010410 00143 NM 2001 4 10 USAA010206 1 20010215 A 5510 FITTING BOEING 737 737301 1384611 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 38667 23555 PIT - FOUND FITTING CRACKED AND CORRODED .25 INCH BY .075 INCH PLUS DEEP, RIGHT HORIZONTAL STABILIZER FITTING FORWARD TO P SPAR LUG HORIZ SIDE. CORROSION LEVEL 1. MACHINED FITTING AND INSTALLED NEW BUSHINGS PER SRM 55-10-10, J3-90-09000-17 3. (M) 2 L 7 2 4F RT A16WE 2001041000144 20010410 00144 NM 2001 4 10 USAA010208 1 20010227 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FGUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FORWARD PRESSURE BULKHEAD CRACKED .25 INCH, STATION 178, WL 188, LBL .5, RBL .5 AFT SIDE. INSTALLED DOUBLER PER EA 69140. (M) 2 L 7 2 4F RT A16WE 2001041000145 20010410 00145 NM 2001 4 10 USAA010209 1 20010227 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FORWARD PRESSURE BULKHEAD CRACKED .5 INCH, STATION 178, WL 198, RBL 4.5 AFT SIDE. INSTALLED DOUBLER PER EA 69140 (MC 90-93852). (M) 2 L 7 2 4F RT A16WE 2001041000146 20010410 00146 NM 2001 4 10 USAA010210 1 20010227 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FORWARD PRESSURE BULKHEAD CRACKED .125 INCH, STATION 178, WL 198.5, LBL 5 AFT SIDE. INSTALLED DOUBLER PER E A 69140 (MK 90-938-52). (M) 2 L 7 2 4F RT A16WE 2001041000147 20010410 00147 NM 2001 4 10 USAA010211 1 20010227 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FORWARD PRESSURE BULKHEAD CRACKED .25 INCH, STATION 178, WL 198.5, RBL 6 AFT SIDE. INSTALLED DOUBLER PER EA 69140 (MK 90-93852). (M) 2 L 7 2 4F RT A16WE 2001041000148 20010410 00148 NM 2001 4 10 USAA010212 1 20010227 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FORWARD PRESSURE BULKHEAD CRACKED .375 INCH, BS 178, LBL 4, WL 200. INSTALLED DOUBLER PER EO 5300V153/SRM 5 3-10-08 FIG 211. (M) 2 L 7 2 4F RT A16WE 2001041000149 20010410 00149 NM 2001 4 10 USAA010213 1 20010227 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FORWARD PRESSURE BULKHEAD CRACKED .5 INCH, STATION 178, WL 201, LBL 5 AFT SIDE. INSTALLED DOUBLER PER EA 69 140. (M) 2 L 7 2 4F RT A16WE 2001041000150 20010410 00150 NM 2001 4 10 USAA010214 1 20010227 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM USELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FORWARD PRESSURE BULKHEAD CRACKED .25 INCH, STATION 178, WL 201, RBL 6 AFT SIDE. INSTALLED DOUBLER PER EA 6 9140 (MK 90-93852). (M) 2 L 7 2 4F RT A16WE 2001041000151 20010410 00151 NM 2001 4 10 USAA010215 1 20010227 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FORWARD PRESSURE BULKHEAD CRACKED .125 INCH, STATION 178, WL 206, RBL .5 AFT SIDE. INSTALLED DOUBLER PER EO 5300V153/SRM 53-10-08 FIG 211. (M) 2 L 7 2 4F RT A16WE 2001041000152 20010410 00152 NM 2001 4 10 USAA010216 1 20010227 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - FOUND BULKHEAD SKIN CRACKED .375 INCH, BS 178, WL 213, LBL 6. INSTALLED DOUBLER PER EO 5300V153/SRM 53-10-08 FIG 211. (M) 2 L 7 2 4F RT A16WE 2001041000153 20010410 00153 NM 2001 4 10 USAA010217 1 20010227 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - FOUND BULKHEAD CRACKED .375 INCH, BS 178, WL 213, RBL 6 STRAP. INSTALLED DOUBLER PER EO 5300V153 AND SRM 53-10-08 FIG 211. (M) 2 L 7 2 4F RT A16WE 2001041000154 20010410 00154 NM 2001 4 10 USAA010218 1 20010227 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FRAME CRACKED .25 INCH, BS 480 BETWEEN STRINGER 8/9 LT. FRAME REPAIRED PER SRM 53-10-14. INSTALLED DOUBLER . (M) 2 L 7 2 4F RT A16WE 2001041000155 20010410 00155 NM 2001 4 10 USAA010219 1 20010227 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FRAME CRACKED .80 INCH, BS 480 BETWEEN STRINGER 8/9 LEFT AT INBOARD RIVET. INSTALLED DOUBLER PER TYP REP 53 -10-14. (M) 2 L 7 2 4F RT A16WE 2001041000156 20010410 00156 NM 2001 4 10 USAA010225 1 20010221 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 32258 24554 CLT - FOUND SIDE CHORD CRACKED 1 INCH, RIGHT SIDE CHORD STATION 178 WL 207. INSTALLED DOUBLERS PER EA 68929/EO 5300V157 . (M) 2 L 7 2 4F RT A16WE 2001041000157 20010410 00157 NM 2001 4 10 USAA010226 1 20010221 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 32258 24554 CLT - FOUND SIDE CHORD CRACKED 1 INCH, STATION 178 AT WL 207 LEFT SIDE CHORD. INSTALLED DOUBLERS PER EO 5300V157. (M) 2 L 7 2 4F RT A16WE 2001041000158 20010410 00158 NM 2001 4 10 USAA010227 1 20010221 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 32258 24554 CLT - FOUND BULKHEAD CRACKED .5 INCH, BS 178, RBL 5.7, WL 180 AFT SIDE. INSTALLED DOUBLER PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2001041000159 20010410 00159 NE 2001 4 10 TSAA0172033 2 20010307 A 7200 ENGINE BOEING 737 7372T4 1384492 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE MALFUNCTIONED A TSAA E C D ENGINE SHUTDOWN ABORTED TAKEOFF RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 808AL 33824 5427 23445 FLT 531 - LNY-HNL - TAXIED TO RUNWAY. WHEN POWER ADVANCED FOR TAKEOFF, A LOUD BANG CAME FROM THE NR 1 ENGINE. ABORTED TAKEOFF AT APPROXIMATELY 20 KNOTS AND SHUT DOWN THE NR 1 ENGINE. NR 2 ENGINE NORMAL. RETURNED TO GATE. REMOVED AND RE PLACED THE NR 1 ENGINE IAW M-213, M-21-, AND M-215. OPS AND LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F A16WE E2EA 2001041000160 20010410 00160 NM 2001 4 10 TSAA0153034 1 20010305 A 5330 6546560 SKIN BOEING 737 7372S2C 138448G NM FUSELAGE DENTED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 806AL 49845 21927 IDENTIFIED DENT A BS 986.5, STRINGER 20L AND S22L. (M) 2 L 7 2 4F A16WE 2001041000161 20010410 00161 NM 2001 4 10 TSAA0153035 1 20010305 A 5311 66232562 FRAME BOEING 737 7372S2C 138448G NM FUSELAGE DENTED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 806AL 21927 IDENTIFIED DENT AT BS 986.5 FRAME BETWEEN STRINGER 23L AND 24L. (M) 2 L 7 2 4F A16WE 2001041000162 20010410 00162 NM 2001 4 10 GAIA01107OP 1 20010308 A 2910 6517840366 HYDRAULIC LINE BOEING 727 727223 1384074 NM RT WING CRACKED A GAIA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 6810 19485 FLT 7359 - OAK-MHR - DURING CLIMB, THE SYSTEM A HYDRAULIC QUANTITY STARTED TO DECREASE. THE CREW DECLARED AN EMERGENCY AND LANDED SAFELY IN MHR WITH NO FURTHER PROBLEMS. MAINTENANCE FOUND A CRACKED HYDRAULIC PRESSURE LINE TO THE RIGHT WIN G LEADING EDGE DEVICES. MAINTENANCE REPLACED THE LINE AND PRESSURE TESTED OK. THE AIRCRAFT WAS RETURNED TO SERVICE. ( M) 2 L 7 3 4F A3WE 2001041000163 20010410 00163 NM 2001 4 10 GAIA01109OP 1 20010215 A 5210 507945152 FRAME BOEING 727 727251 138408H NM PAX DOOR CRACKED A GAIA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 278US 21157 FLT 1805 - PHX - DURING CLIMB THROUGH 20,000 FEET, THE CREW NOTICED A LOUD AIR LEAK. CLIMBING THROUGH 24,000 FEET A LOU D BANG WAS HEARD AND THE CABIN PRESSURIZATION STARTED DEPRESSURIZING SLOWLY. ATC WAS ADVISED, AND THE CREW DID A PRECAU TIONARY RETURN TO PHX. THE AIRCRAFT LANDED WITHOUT ANY FURTHER DIFFICULTIES. REMOVED AND REPLACED THE L1 DOOR DUE TO A N AFT FRAME CRACK. THE L1 DOOR WAS RIGGED, AND OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001041000164 20010410 00164 NM 2001 4 10 KPVA20017 1 20010311 A 3350 10005511 LIGHT DHAV DHC8 DHC8103 1386005 NM COCKPIT WEAK A KPVA K NONE O OTHER IN INSP/MAINT 1 WP 13 808WP 846 026 HNL - FLIGHT COMPARTMENT EMERGENCY EXIT LIGHT WEAK. REMOVED AND REPLACED EXIT LIGHT ASSEMBLY IAW DHC-8 33-51-00 PAR 1A- 1B PAGE 201-202. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 2001041000165 20010410 00165 NM 2001 4 10 KPVA20016 1 20010310 A 3350 10005511 LIGHT DHAV DHC8 DHC8103 1386005 NM COCKPIT INOPERATIVE A KPVA K NONE L NO TEST IN INSP/MAINT 1 WP 13 807WP 292 023 HNL - DURING MAINTENANCE PRE-FLIGHT INSPECTION, COCKPIT EMERGENCY LIGHT DID NOT OPERATE AS REQUIRED. REMOVED AND REPLAC ED (PORTABLE EMERGENCY) LIGHT ASSY. OPS CHECK GOOD IAW PSM 1-8-2 CHAPTER 33-51-00 PAGE 201-202. (M) 2 H 7 2 4T RT A13NM 2001041000166 20010410 00166 WP 2001 4 10 Y2PA01003 1 20010214 A 2611 100064701 SMOKE DETECTOR DOUG DC9 DC932F 3022067 WP CARGO BAY FAULTY A Y2PA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 23 207US 47355 SAT - FOUND LOWER CARGO FIRE ANNUNCIATOR ILLUMINATED DURING CRUISE FLIGHT (FL330) ALONG WITH MASTER WARNING LIGHTS APPRO ACHING SAT VOR. CREW DECLARED EMERGENCY AND DIVERTED TO SAT AIRPORT, LANDING WITHOUT INCIDENT. ON THE GROUND IT WAS DE TERMINED THAT NO FIRE HAD ACTUALLY EXISTED AND MAINTENANCE WAS CONTACTED. MAINTENANCE IN SAT DETERMINED THAT TWO SMOKE SENSORS HAD FAILED IN THE LOWER CARGO SMOKE DETECTOR SYSTEM. ONE SENSOR HAD FAILED AND WAS JUST INOPERATAIVE. THE SECO ND SENSOR HAD FAILED AND WAS REPORTEING A FALSE FIRE WARNING. THIS WAS DETERMINED THROUGH THE SYSTEM BYTE TEST. THE SY STEM WAS DEFERRED IAW THE MEL UNTIL IT COULD RETURN TO A USA JET MX FACILITY FOR REPLACEMENT SENSOR UNITS. UPON RETURN 2 L 7 2 4F A6WE 2001041000167 20010410 00167 NE 2001 4 10 20010409SG007 2 20010304 A 7261 730969 PUMP BOEING 737 7373T5 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE DAMAGED A RJEF A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 23 501NG 22395 686323 SAL - FLT TA410 - DURING CRUISE OF FLIGHT, ENGINE NR 2 WAS SHUTDOWN DUE TO LOW OIL PRESSURE, AND HIGH OIL TEMPERATURE. AFTER UNEVENTFUL LANDING AT EL SALVADOR AIRPORT, MAINTENANCE TECHNICIANS PERFORMED INSPECTION AND FOUND IN ENGINE NR 2, THE MAIN OIL FILTER CONTAMINATED AND MAIN OIL PUMP DAMAGED. THE AIRCRAFT REMAINED ON GROUND FOR MAINTENANCE. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 2001041000168 20010410 00168 NM 2001 4 10 USAASB01062 1 20010226 A 2410 731753 CSD BOEING 737 737201 1384454 NM NR 1 ENGINE OVERSERVICED A USAA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 EA 19 257AU 22799 MCO - FLT 2802 - ON CLIMB-OUT FROM MCO, AT ABOUT 4,000 FEET, THE NR 1 ENGINE CSD HIGH OIL TEMPERATURE LIGHT ILLUMINATED. THE APU WAS ALREADY ON MEL SO THE FLIGHT RETURNED TO FIELD AT MCO. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED T O THE GATE NORMALLY. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE NR 1 ENGINE CSD OIL OVERSERVICED. SERVICED OIL TO PROPER LEVEL. RAN ENGINE. OIL TEMPERATURE CHECKS GOOD. CLEARED MEL ON APU BY REPLACING A LEAKING O-RING AT THE APU COMPRESSOR DISCHARGE PRESSURE T-FITTING. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 2001041000169 20010410 00169 NM 2001 4 10 USAASB01055 1 20010223 A 2910 HYDRAULIC LINE BOEING 737 737201 1384454 NM NR 1 ENGINE LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 253AU 22795 PIT - FLT 2622 - EN ROUTE FROM BWI TO MDW, AT FL280, FLIGHT EXPERIENCED A LOSS OF SYSTEM A HYDRAULIC QUANTITY FOLLOWED B Y A LOSS OF HYDRAUIC PRESSURE. CREW DECLARED AN EMERGENCY AND DIVERTED TO PIT. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND WAS TOWED TO THE GATE. MAINTENANCE FOUND THE NR 1 ENGINE HYDRAUILC PRESSURE HOSE LEAKING. REMOVED AND REPLACED PRE SSURE HOSE AND SYSTEM 'A' AND 'B' PRESSURE AND RETURN CASE DRAIN FILTERS AS PRECAUTIONARY. NO EVIDENCE OF DEBRIS NOTED. SERVICED HYDRAULIC SYSTEM AND PRESSURIZED HYDRAULIC SYSTEM. LEAK CHECK GOOD. ACCOMPLISHED GEAR SWING AND FREE FALL C HECK OF GEAR. CHECKS GOOD. RAN FLAPS THROUGH FULL TRAVEL IN BOTH NORMAL AND ALTERNATE MODES. SYSTEM CHECKS GOOD. RAN 2 L 7 2 4F A16WE 2001041000170 20010410 00170 NM 2001 4 10 USAASB01061 1 20010226 A 4990 O-RING BOEING 737 737201 1384454 NM APU LEAKING A USAA A UNSCHED LANDING P H NO WARNING INDICATION ELECT. POWER LOSS-50 PC CL CLIMB 1 EA 19 257AU 22799 BDL - FLT 2978 - EN ROUTE FROM PVD-BWI, THE NR 1 GENERATOR DROPPED OFF LINE AND WOULD NOT RESET. THE NR 1 GENERATOR DRI VE OIL TEMPERATURE ''IN'' INDICATION WAS OFF SCALE AND NO HIGH OIL TEMPERATURE LIGHT ILLUMINATED. AFTER PLACING APU ON LINE, THE APU LATER SHUTDOWN. FLIGHT DIVERTED TO BDL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE APU CO MPRESSOR DISCHARGE PRESSURE T-FITTING LEAKING AT O-RING. REMOVED AND REPLACED O-RING. RAN APU. OPERATIONAL CHECK GOOD AS FOR THE NR 1 GENERATOR DROPPING OFF LINE, MAINTENANCE REMOVED AND REPLACED THE NR 1 CSD (P/N 731753) AND THE NR 1 C SD OIL COOLER (P/N 6A47-000) DUE TO METAL CONTAMINATION FOUND IN THE FILTER AND ON THE MAGNET IN THE CSD. OPERATIONAL C 2 L 7 2 4F A16WE 2001041000171 20010410 00171 NM 2001 4 10 AALA20010364 1 20010301 A 5630 WINDOW BOEING 757 757223 1384957 NM R1 DOOR CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 690AA 25696 SJC - FOUND 1R ENTRY DOOR WINDOW CRACKING AND CRAZED. INSPECTED 1R WINDOW FOUND SUPERCICIAL SCRATCHES ON OUTER SURFACE OK FOR SERVICE PER MM 56-31-02-6. (M) 2 L 7 2 4F RT A2NM 2001041000172 20010410 00172 NM 2001 4 10 20010409SG008 1 20010209 A 2910 106056320 HYDRAULIC LINE BOEING 737 7372H6 NM NR 1 ENGINE DAMAGED A SOKF A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 23 235TA 21765 CCS - FLT TA610 - DURING CRUISE, THE HYDRAUIC SYSTEM ''A'' WAS LOSS, DUE TO THIS SITUATION, THE AIRCRAFT RETURNED TO CAR ACAS AIRPORT. AFTER LANDING, MAINTENANCE TECHNICIANS PERFORMED INSPECTION AND FOUND IN NR 1 ENGINE THE PRESSURE HOSE DA MAGED, IT WAS REMOVED AND REPLACED AS PER AMM 29-11-31. ALSO, THE CASE FILTER WAS REMOVED AND CHECKED AS PER AMM 29-11-4 1. ENGINE RUN-UP WAS PERFORMED WITH SATISFACTORY RESULTS, THE AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F A16WE 2001041000173 20010410 00173 EU 2001 4 10 AALA20010173 1 20010131 A 3230 VALVE AIRBUS 300 A300B4605R 3930308 EU MLG CONTAMINATED A AALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 21 33069 512 LHR - RIGHT MAIN GEAR SLOW TO RETRACT TRIGGERING ECAM WARNING AND DOOR OPEN LIGHT. STAYED ON FOR APPROX 1 MINUTE. AIRC RAFT HAS BEEN INSPECTED AND FOUND TO BE IN A SAFE CONDITION FOR FERRY FLIGHT FROM LHR TO JFK FOR FURTHER TROUBLESHOOTING AND REPAIR OF RIGHT MLG DUE TO SLOW RETRACTION. THIS FERRY FLIGHT IS AUTHORIZED BY SPOTTING MESSAGE NR 01-194. INSPEC TED RESTRICTOR VALVES FOR RIGHT MLG AND RT GEAR DOOR. CLEANED DEBRIS FROM BOTH VALVES. ACCOMPLISHED GEAR SWING SEVERAL TIMES. ALL CHECKS NORMAL. GREASED RIGHT MAIN GEAR TRUNNION. (M) 2 L 7 2 4F RT A35EU 2001041000174 20010410 00174 EU 2001 4 10 20010410AP027 1 20010201 A 2822 12272320002 PUMP FOKKER F27 F27MK600 4990706 EU FUEL BOOST FAILED A COEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 13 702FE 10350 ON ATTEMPTING TAKEOFF FROM OAK AT APPROXIMATELY 0200 (L), PILOT REPORTED THE WARNING LIGHT FOR THE LEFT NR 2 FUEL BOOST PUMP ILLUMINATED. AS THE NR 1 PUMP FOR THIS ENGINE WAS ALREADY DEFERRED, PILOT ELECTED TO ABORT THE TAKEOFF AND RETURN TO THE RAMP FOR MAINTENANCE. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM DURING A STATIC GROUND RUN, AND AIRCRAFT AGAIN ATTEMPTED TAKEOFF. DURING ACCELERATION THE LEFT NR 2 PUMP WARNING LIGHT ILLUMINATED AGAIN AND THE TAKEOFF RUN WAS AGAI N ABORTED. BOTH FUEL BOOST PUMPS WERE REPLACED ON THE LEFT SIDE OF THE AIRCRAFT, DMI CLEARED AND AIRCRAFT RETURNED TO S ERVICE. (M) 2 H 7 2 4T A817 2001041000175 20010410 00175 CE 2001 4 10 20010410AP028 1 20010216 A 2612 24409015 FIRE LOOP BEECH 1900 1900C 1154161 CE LT ENGINE INOPERATIVE A GUUA O OTHER N FALSE WARNING CL CLIMB 1 SO 19 181GA UB24 FLT 9137 - FLL - AFTER TAKEOFF, LEFT ENGINE FIREWALL FUEL VALVE ILLUMINATED INTERMITTENTLY. REMOVED AND REPLACED FORWAR D LEFT ENGINE FIRE LOOP. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4T RT A24CE 2001041000176 20010410 00176 CE 2001 4 10 20010410AP029 1 20010218 A 2150 1143840045 BLOWER BEECH 1900 1900C 1154161 CE RT WING FAILED A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 19 137GA UC105 FLT 9323 - TPA/RSW - DURING FLIGHT, UNKNOWN ODOR IN THE COCKPIT. REMOVED AND REPLACED CONDENSER BLOWER. (M) 2 L 7 2 4T RT A24CE 2001041000177 20010410 00177 WP 2001 4 10 HALA0100056 1 20010223 A 2421 073012ABD GCU DOUG DC9 DC951 3022051 WP LT & RT FAILED A HALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 WP 13 661HA 47796 FLT 184 - HNL - AIRCRAFT X-TIE LOCKOUT LIGHT CAME ON IN FLIGHT. IT CAUSED A DOUBLE GENERATOR FAILURE, RESET GENERATORS IN FILGHT. APU WAS RESTARTED SUCCESSFULLY. NORMAL LANDING. REPLACED RIGHT GCU. GROUND RAN BOTH ENGINES. OPS CHECK O K. RESET X-TIE LOCKOUT. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 2001041000178 20010410 00178 SW 2001 4 10 BSAA200100001 1 20010131 A 3213 2751540003 PIN SWRNGN SA227 SA227AC 8780603 SW RT MLG BROKEN A BSAA O OTHER E VIBRATION/BUFFET LD LANDING 1 NM 05 27465 AC755B ON LANDING ROLL OUT, THE AIRCRAFT STARTED VIBRATING AND PULLING TOWARD THE RIGHT SIDE OF THE RUNWAY. THE AIRCRAFT STAYE D ON THE RUNWAY AND WAS BROUGHT TO A FULL STOP. INVESTIGATION REVEALED THAT THE RIGHT MAIN GEAR WAS COCKED OFF TO THE S IDE 30 TO 45 DEGREES. TROUBLE TRACED TO UPPER RIGHT TORQUE LINK PIN BROKEN IN TWO PLACES. THE -001 PIN WAS REPLACED BY A -003 PIN AND HAS TWO ADDITIONAL HOLES DRILLED IN THE PIN. THE FAILED PIN SHOWS TWO AREAS OF POSSIBLE EXISTING CRACKS OR FLAWS. WHEN ONE SIDE OF THE PIN FAILED, THE OTHER SIDE WAS SUBJECTED TO HIGH STRESS CAUSING IT TO FAIL. (M) 2 L 7 2 4T RT A8SW 2001041000179 20010410 00179 EU 2001 4 10 NSVA0103 1 20010219 A 3260 CONNECTOR SAAB SF340 340B 7860101 EU DRAG BRACE DISCONNECTED A NSVA O OTHER N FALSE WARNING CL CLIMB 1 EA 27 350BE 340B197 EN ROUTE FROM IAD-MNZ, AFTER EXTENSION OF GEAR FOR LANDING THE CREW NOTED THAT THE DOWN AND LOCK INDICATOR FOR THE RT GE AR WAS INOPERATIVE. RETURNED TO IAD TO SEE IF THE TOWER COULD GIVE CONFIRMATION OF GEAR POSITION, HOWEVER IT WAS TO DAR K FOR THE TOWER TO SEE THE GEAR. ON FINAL APPROACH TO IAD THE GWPS SOUNDED UNSAFE GEAR WARNING. CREW EXECUTED EMERGENCY LANDING GEAR EXTENSION PROCEDURES. LANDING AT IAD WAS UNEVENTFUL. MECHANIC INSPECTED AND PINNED GEAR, SPECIAL FLIGHT PERMIT FROM IAD TO MNZ WAS ISSUED. UPON FURTHER INSPECTION A LOOSE CONNECTOR PLUG FOUND ON THE DRAG BRACE HARNESS WAS S ECURED. SYSTEM OPERATIONALLY CHECKED GOOD. (M) 2 L 7 2 4T RT A52EU 2001041000180 20010410 00180 NM 2001 4 10 TSAA0153020 1 20010216 A 5311 6545767103 FRAME BOEING 737 737282 13844AT NM FUSELAGE DENTED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 824AL 23045 IDENTIFIED DENT ON FRAME ASSEMBLY 5 INCHES BY 7 INCHES AT BS 360-380 STRINGER 17L. (M) 2 L 7 2 4F RT A16WE 2001041000181 20010410 00181 WP 2001 4 10 HALA0100055 1 20010225 A 2731 SPRING DOUG DC9 DC951 3022051 WP TRIM HANDLE BROKEN A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 649HA 47715 HNL - PRIMARY TRIM MOTOR HANDLE STICKS CAUSING MOTOR TO RUN AGAINST BRAKE, RESULTING IN MOTOR OVERHEAT AND SHUTDOWN. RT SUITCASE HANDLE ON PEDESTAL. REPLACED BROKEN RETURN SPRING. OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 2001041000182 20010410 00182 WP 2001 4 10 GTIA010033 1 20010203 A 2150 LIMITER DOUG DC9 DC982 3022082 WP CABIN TEMP FAILED A GTIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 957AS 49126 FLL - SMELLED SMOKE IN CABIN DURING FLIGHT. LIGHT MISTY SMOKE WITH SMELL. REMOVED AND REPLACED THERMAL TEMP LIMITER IA W MD-80 MM 21-65. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2001041000183 20010410 00183 WP 2001 4 10 GTIA010045 1 20010226 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 804NK 49104 LGA - FLT 752 - FOUND COCKPIT OVERHEAD EMERGENCY LIGHTS IS INOPERATIVE. RELAMPED COCKPIT OVERHEAD EMERGENCY LIGHT IAW 3 3-53-00. OPS CHECK NORMAL. (M) 2 L 7 2 4F A6WE 2001041000184 20010410 00184 2001 4 10 GTIA010044 4 20010224 A 2565 SLIDE DOUG DC9 DC981 3022081 WP PAX DOOR LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 ORD - FLT 781 - SLIDE PACK DOOR IS LOOSE. RE-INSTALLED SLIDE PACK ON L1 DOOR IAW MM 25-02-00. OPS CHECK OK. (M) 2 L 7 2 4F A6WE 2001041000185 20010410 00185 WP 2001 4 10 GTIA010043 1 20010223 A 5350 4913354501 TAIL CONE DOUG DC9 DC941 302207N WP AFT SEPARATED A GTIA O OTHER D INFLIGHT SEPARATION LD LANDING 1 GL 23 130NK 47604 DCA - FLT 72 - TAILCONE FELL OFF DURING LANDING. REMOVED AND REPLACED TAILCONE IAW MM 53-50-3, OPS CHECK NORMAL. (M) 2 L 7 2 4F A6WE 2001041000186 20010410 00186 NM 2001 4 10 GAIA01073BOP 1 20010223 A 2910 LINE BOEING 727 727224 1384076 NM HYS SYSTEM RUPTURED A GAIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 79748 22450 FLT 1805 - FWA-LAX - AT FL310, HYDRAULIC SYSTEM ''A'' PRESSURE AND QUANTITY WENT TO ZERO. AIRCRAFT MADE AN UNEVENTFUL L ANDING IN DEN. TROUBLESHOOT AND FOUND RUPTURED HYDRAULIC LINE IN RIGHT SIDE OF AFT AIRSTAIR. REMOVED AND REPLACED THE HYDRAULIC LINE PER B727 MM 20-10-5. LEAKS CHECKS GOOD ON GROUND. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001041000187 20010410 00187 NM 2001 4 10 P2EA01002 1 20010119 A 3260 WARNING SYSTEM BOEING 737 737230 NM MLG MALFUNCTIONED A P2EA O OTHER N FALSE WARNING AP APPROACH 1 CE 05 122NJ 22120 MCI - FLT 101 - DURING APPROACH WITH LANDING GEAR HANDLE DOWN, GEAR INDICATION OF 3 GREEN, 3 RED LIGHTS ON AND WARNIGN H ORN SOUNDING. ABORTED APPROACH AND WENT AROUND, CYCLED GEAR 2ND TIME ALL INDICATIONS NORMAL. TESTED GEAR LIGHTS AND HO RN IAW BOEING MM 32-61-0, COULD NOT DUPLICATE. ALL INDICATIONS NORMAL. (M) 2 L 7 2 4F RT A16WE 2001041000188 20010410 00188 NM 2001 4 10 GAIA01076OP 1 20010228 A 2612 FIRE LOOP BOEING 727 727259 138408J NM NR 3 ENGINE LOOSE A GAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 901RF 22476 FLT 1806 - DEN - NR 3 FIRE WARNING BELL AND LIGHT SOUNDED AND ILLUMINATED INTERMITTENTLY DURING CLIMB-OUT. THROTTLE WAS RETARDED AND WARNINGS CEASED. AIRCRAFT MADE AN UNEVENTFUL RETURN TO DEN. FOUND TWO CLAMPS LOOSE ON NR 3 ENGINE FIRE L OOP. RE-SET CLAMPS AND RAN ENGINES AT TAKEOFF POWER AND CRUISE POWER SETTINGS. COULD NOT DUPLICATE PROBLEM. SYSTEM OP ERATES GOOD ON GROUND. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001041000189 20010410 00189 NM 2001 4 10 GAIA01074OP 1 20010227 A 3260 ACCESSORY UNIT BOEING 727 727223 1384074 NM MLG MALFUNCTIONED A GAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 6831 20184 FLT 2021 - MHR - UPON GEAR RETRACTION, 3 GEAR UNSAFE LIGHTS ILLUMINATED. TAIL SKID AMBER LIGHT ILLUMINATED. AIRCRAFT M ADE AN UNEVENTFUL RETURN LANDING AT MHR. PINNED GEAR, CYCLED HANDLE TO FULL UP POSITION. RED INTRANSIT LIGHT ILLUMINAT ED AND UNSAFE HORNS SOUNDED AS DESIGNED. CYCLED GEAR HANDLE DOWN. THREE GREEN HORN SILENCED. RE-RACKED LANDING GEAR A CCESSORY BOX. OPERATIONALLY CHECK GOOD ON GROUND. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001041000190 20010410 00190 NM 2001 4 10 GAIA01075OP 1 20010223 A 7500 CLAMP BOEING 727 727223 1384074 NM NR 1 STRUT LEAKING A GAIA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 6827 20180 FLT 2507 - GEG-IND - AT 1000 FEET AGL, ENGINE AND WING HEAT OPENED. ONE MINUTE LATER NR 1 STRUT OVER HEAT LIGHT ILLUMIN ATED AS A/C CLIMBED THROUGH CLOUDS INTO CLEAR. ALL ANTI-ICE SYSTEMS CLOSED AND STRUT OVER HEAT LIGHT EXTINGUISHED. NOR MAL CONDITIONS THROUGHOUT REST OF FLIGHT. AIRCRAFT MADE AN UNEVENTFUL LANDING IN IND. FOUND SEVERAL LOOSE CLAMPS ON NR 1 ENGINE PYLON AREA. TIGHTENED ALL CLAMPS AS REQUIRED. NO LEAK NOTED ON GROUND RUN. OPS CHECK GOOD. AIRCRAFT WAS RE TURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001041000191 20010410 00191 2001 4 10 P2EA01001 4 20010102 A 3417 ADC BOEING 737 737247 138448D NM E/E BAY MALFUNCTIONED A P2EA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 912MP 19607 MCI - FLT 301 - AUTO PRESSURIZATION FAILED ON CLIMB-OUT, STANDBY PRESSURIZATION COULD NOT MAINTAIN PRESSURIZATION SCHEDU LE. AIRCRAFT RETURNED TO MCI WITH NO INCIDENT. REMOVED AND REPLACED NR 2 AIR DATA COMPUTER IAW MM 21-30-0, OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A16WE 2001041000193 20010410 00193 NM 2001 4 10 P2EA01003 1 20010217 A 2910 65445461468 LINE BOEING 737 7372B7 1384560 NM HYD SYSTEM WORN A P2EA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 CE 05 125NJ 22882 FLT 650 - MYR - DURING FLIGHT INBOUND TO MYR A SYSTEM HYDRAULIC QUANTITY WHEN TO 0, FOLLOWED BY A SYSTEM PRESSURE. DURI NG INSPECTION FOUND A SYSTEM WITH HYDRAULIC LINE LEAKING. REMOVED AND REPLACED TUBE ASSEMBLY. OPS CHECKED AND LEAK CHE CKED IAW BOEING MM 29-00A AND 29-09-308A. (M) 2 L 7 2 4F A16WE 2001041000194 20010410 00194 NM 2001 4 10 P2EA01004 1 20010222 A 5210 SEAL BOEING 737 737244 138448U NM PAX DOOR FAILED A P2EA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 620PC 19708 MCI - FLT 350 - WHILE IN CLIMB-OUT OF MCI, AIRCRAFT WOULD NOT PRESSURIZE, RETURN TO MCI. INSPECTION FOUND AIRCRAFT L1 D OOR SEAL NOT PROPERLY SEATED. RESECURED DOOR AND OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A16WE 2001041000195 20010410 00195 EU 2001 4 10 AALA20010187 1 20010204 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU NR 2 GALLEY INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1440A 11435 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT AT NR 2 GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SEGME NT AT NR 2 GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001041000196 20010410 00196 EU 2001 4 10 AALA20010189 1 20010202 A 4910 DUCT FOKKER F28 F28MK0100 4990807 EU APU LEAKING A AALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 SW 21 1431B 11416 ORD - FLT 844 - EN ROUTE ORD-HPN, SHORTLY AFTER ENGINE START FLIGHT ATTENDANT REPORTED SMOKE AND FUMES IN CABIN. RETURN ED ORD GATE WITHOUT FURTHER INCIDENT. REALIGNED APU AIR INLET. RAN BOTH PACKS. NO SMOKE OR ODOR NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001041000197 20010410 00197 NM 2001 4 10 AALA20010190 1 20010131 A 2913 S270T2017 PUMP BOEING 757 757223 1384957 NM NR 1 ENGINE LEAKING A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 685AA 25342 LGA - FLT 708 - EN ROUTE DFW-LGA, SHORTLY BEFORE ARRIVAL LEFT SIDE HYDRAULIC QUANTITY DECREASED TO ZERO. HYDRAULIC PRES SURE DECREASED. LANDED LGA WITHOUT FURTHER INCIDENT. REPLACED LEFT SIDE HYDRAULIC PUMP. ACCOMPLISHED LEAK CHECK PER T HE MM. NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001041000198 20010410 00198 NE 2001 4 10 AALA20010191 2 20010202 A 7532 714810 VALVE BOEING 727 727223 1384074 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE DEFECTIVE A AALA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SW 21 706AA 22463 IAD - FLT 371 - EN ROUTE IAD-DFW - DURING TAKEOFF, DETECTED A LOUD BANG AND VIBRATION AT CABIN. RETURNED IAD AND LANDED WITHOUT FURTHER INCIDENT. REPLACED NR 2 ENGINE BLEED VAVLE. ACCOMPLISHED HIGH POWER RUN. SYSTEM GROUND CHECKED NORMA L OPERATION. (M) 2 L 7 3 4F 4 F A3WE E2EA 2001041000199 20010410 00199 WP 2001 4 10 AALA20010192 1 20010203 A 2170 1808492 COALESCER BAG DOUG DC9 DC982 3022082 WP ACM BAY DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 495AA 49733 DFW - FLT 1293 - EN ROUTE DFW-SAT - SHORTLY AFTER TAKEOFF FLIGHT ATTENDANT REPORTED SMOKE AND FUMES IN AFT CABIN. DECLA RED EMERGENCY, RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED COALESCER BAGS. ACCOMPLISHED PACK BURNOUT PE R MM. NO SMOKE OR ODOR NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001041000200 20010410 00200 NM 2001 4 10 AALA20010143 1 20010125 A 3350 LIGHT BOEING 767 767223 1385123 NM CABIN INTERMITTENT A AALA O OTHER O OTHER CR CRUISE 1 SW 21 317AA 22319 JFK - FLT 142 - EN ROUTE JFK-LHR - DETECTED EMERGENCY EXIT LIGHT ILLUMINATE INTERMITTENTLY. LANDED LHR WITHOUT FURTHER INCIDENT. ACCOMPLISHED EMERGENCY EXIT LIGHT CHECK. NO DEFECTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001041000201 20010410 00201 NM 2001 4 10 AALA20010135 1 20010124 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 322AA 22323 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 25 A/B INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT CONN ECTOR AT 25 A/B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001041000202 20010410 00202 NM 2001 4 10 AALA20010137 1 20010124 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7667A 25301 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD SECTION EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STR IP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001041000203 20010410 00203 NM 2001 4 10 AALA20010136 1 20010124 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 183AN 29593 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 4 THROUGH 12 INOPERATIVE. REPLACED EMERGENCY EXIT LIGH T CONNECTORS AT SEAT 4 AND 12. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001041000204 20010410 00204 NM 2001 4 10 AALA20010134 1 20010123 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN INOPERATIVE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 694AN 26974 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SET 9D INOPERATIVE. REPAIRED EMERGENCY EXIT WIRE AT SEAT 9D . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001041000205 20010410 00205 NM 2001 4 10 AALA20010146 1 20010126 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 374AA 25201 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 28B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECT OR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001041000206 20010410 00206 NM 2001 4 10 AALA20010182 1 20010131 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN INOPERATIVE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 692AA 26972 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L1 AND L2 INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001041000207 20010410 00207 NM 2001 4 10 AALA20010168 1 20010131 A 3350 4001089 CONNECTOR BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 359AA 24040 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT WIRE AT 22H BROKEN. REPLACED EMERGENCY EXIT PIN AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001041000208 20010410 00208 NM 2001 4 10 AALA20010166 1 20010130 A 3350 020182000 LIGHT BOEING 767 767223 1385123 NM MID GALLEY DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 313AA 22316 BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT MID GALLEY DAMAGED. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001041000209 20010410 00209 NM 2001 4 10 AALA20010221 1 20010206 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 395AN 29432 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 29 AB INOPERATIVE. RE-PINNED EMERGENCY EXIT LIGHT CONN ECTOR AT SIDE WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001041000210 20010410 00210 EU 2001 4 10 AALA20010222 1 20010206 A 3350 CONNECTOR FOKKER F28 F28MK0100 4990807 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1411G 11369 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 7 THROUGH 11 INOPERATIVE. RE-SECURED EMERGENCY EXIT LI GHT CONNECTOR AT SEAT 8 AND 10. SYSTEM GROUND CHECKED NORMAL OPS. (M) 2 L 7 2 4F RT 2001041000211 20010410 00211 NM 2001 4 10 AALA20010223 1 20010206 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 621AM 24579 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 2EF INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT CONNE CTOR AT BIN 2EF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001041000212 20010410 00212 WP 2001 4 10 AALA20010224 1 20010206 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7547A 53029 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT CABIN INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMB LY AT SEAT ROW 29. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001041000213 20010410 00213 EU 2001 4 10 AALA20010225 1 20010207 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 1424M 11407 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT FORWARD CABIN INOPERATIVE. SPLICED EMERGENCY EXIT LIGHT FLO OR PROXIMITY LIGHT WIRE AT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001041000214 20010410 00214 WP 2001 4 10 AALA20010226 1 20010207 A 3350 SPLICE DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 455AA 49560 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT SPLICE AT AFT CABIN . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001041000215 20010410 00215 NM 2001 4 10 AALA20010227 1 20010204 A 2612 S332T1003 FIRE DETECTOR BOEING 767 767223 1385123 NM NR 2 ENGINE DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SW 21 332AA 22331 JFK - FLT 45 - EN ROUTE JFK-SFO - DETECTED FAILURE OF BOTH RIGHT SIDE ENGINE FIRE LOOP WARNING SYSTEM. AIR INTERUPTED, RETURNED JFK AND LANDED WITHOUT FURTHER INCIDENT. REPLACED RIGHT SIDE ENGINE LP 2 DETECTOR. PERFORMED LOOP RESISTANT C HECK. ACCOMPLISHED FIRE WARNING TEST PER THE MM. NO DEFECTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001041000216 20010410 00216 NM 2001 4 10 AALA20010228 1 20010206 A 2530 86901 OVEN BOEING 767 767323 1385205 NM NR 2 GALLEY DEFECTIVE A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 352AA 24033 LHR - FLT 91 - EN ROUTE LHR-ORD, DETECTED SMOKE AT NR 2 GALLEY. NR 2 OVEN CIRCUIT BREAKER PULLED. LANDED ORD WITHOUT F URTHER INCIDENT. REPLACED NR 2 GALLEY OVEN AND RESET CIRCUIT BREAKER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001041000217 20010410 00217 WP 2001 4 10 AALA20010229 1 20010206 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 70401 49312 LAX - DURING OVERNIGHT MAINTENANCE, AFT LEFT EMERGENCY LIGHT AT LOWER SIDE WALL INOPERATIVE. RE-CONNECTED EMERGENCY EXI T LIGHT WIRES AT SIDE WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001041000218 20010410 00218 WP 2001 4 10 AALA20010305 1 20010209 A 5310 STRUCTURE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7512A 49806 TUL - FOUND CRACKED AT STATION 486 AND 570. REMOVED DAMAGED AT STATION 486 AND 570 AND INSTALLED DOUBLER PER AARD 53-00 -00-02 FIG 1. (M) 2 L 7 2 4F A6WE 2001041000219 20010410 00219 WP 2001 4 10 AALA20010304 1 20010208 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7512A 49806 TUL - FOUND CORROSION ON SEAT TRACK NR 1 AT STATION 735. REMOVED MATERIAL THAT WAS BEYOND LIMITS AND INSTALLED SEAT TRA CK PLUG PER AARD 53-20-00-10. (M) 2 L 7 2 4F A6WE 2001041000220 20010410 00220 WP 2001 4 10 AALA20010306 1 20010209 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7512A 49806 TUL - FOUND HORIZONTAL SCRATCH 4 INCHES IN LENGTH 2 FEET AFT OF POSS ENTRY DOOR EVEN WITH BUTTON OF DOOR AND SHEAR TIE C RACKED. DAMAGED AREA CUTOUT AND SHEAR TIE REMOVED DOUBLER AND NEW SHEAR TIE INSTALLED PER SRM 53-04 FIG 12B AND 51-01. (M) 2 L 7 2 4F A6WE 2001041000221 20010410 00221 WP 2001 4 10 AALA20010307 1 20010213 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7512A 49806 TUL - FOUND CRACK IN FUSELAGE SKIN AT STATION 1401, 8 INCHES ABOVE THE NR 2 ENGINE PYLON. STOP DRILLED CRACK AND INSTAL LED DOUBLER PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2001041000222 20010410 00222 WP 2001 4 10 AALA20010309 1 20010209 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7512A 49806 TUL - FOUND CUSP WEB AT STATION 513-608 CRACKED. REMOVED DAMAGE AT 513 AND 608 AND INSTALLED DOUBLER PER AARD 53-00-00- 02. (M) 2 L 7 2 4F A6WE 2001041000223 20010410 00223 WP 2001 4 10 AALA20010310 1 20010208 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7512A 49806 TUL - FOUND GOUGE IN SEAT TRACK NR 4 STATION 340. REMOVED GOUGE SEAT TRACK NR 4 STATION 340. INSTALLED PLUG PER AARD 5 3-20-00-10. (M) 2 L 7 2 4F A6WE 2001041000224 20010410 00224 WP 2001 4 10 AALA20010311 1 20010208 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7512A 49806 TUL - FOUND .5 INCH CRACK AT FRAME 160 FASTENERS. LONG SPLICE SECTION PER SRM 53-02. (M) 2 L 7 2 4F A6WE 2001041000225 20010410 00225 WP 2001 4 10 AALA20010313 1 20010212 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7512A 49806 TUL - FOUND CRACK IN CUSP WEB AT STATION 795. REMOVED DAMAGED AREA AND INSTALLED REPAIR DUOBLER PER AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 2001041000226 20010410 00226 WP 2001 4 10 AALA20010314 1 20010218 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7512A 49806 TUL - FOUND SMALL DENT IN SKIN AT STATION 237 BETWEEN LONGERON 18-19L. INSTALLED DOUBLER AT DENT PER SRM 53-04 FIG 12B. (M) 2 L 7 2 4F A6WE 2001041000227 20010410 00227 WP 2001 4 10 AALA20010315 1 20010212 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7512A 49806 TUL - FOUND STATION 1200R FLOOR CUSP HAS HOLE OUTBOARD OF NR 6 SEAT TRACK. INSTALLED DOUBLER PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2001041000228 20010410 00228 WP 2001 4 10 AALA20010316 1 20010210 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7512A 49806 TUL - FOUND CORROSION ON NR 1 SEAT TRACK FROM 1174-1309. INSTALLED SERVICEABLE SEAT TRACK FROM STATION 1170-1309 AS PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2001041000229 20010410 00229 WP 2001 4 10 AALA20010317 1 20010216 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7512A 49806 TUL - FOUND FRAME CRACKED AT AIRSTAIR ACTUATOR BRACKET, STATION 1485. REPAIRED FRAME PER ESO 80559 DATED 2/16/2001. (M ) 2 L 7 2 4F A6WE 2001041000230 20010410 00230 WP 2001 4 10 AALA20010318 1 20010210 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7512A 49806 TUL - FOUND 2 INCHES BY 76 INCHES CORROSION ON LEFT CUSP STATION 1174. INSTALLED NEW SERVICEABLE LEFT CUSP STATION 1174 -1250 PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2001041000231 20010410 00231 WP 2001 4 10 AALA20010319 1 20010210 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7512A 49806 TUL - FUOND SEAT TRACK NR 6 CORRODED FROM STATION 303-798. INSTALLED NEW SEAT TRACK NR 6 FROM STATION 303-798 PER SRM 5 1-01. (M) 2 L 7 2 4F A6WE 2001041000232 20010410 00232 WP 2001 4 10 AALA20010320 1 20010211 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7512A 49806 TUL - FOUND CORROSION ON SEAT TRACK STATION 1174-1309. REMOVED AND REPLACED SECTION OF NR 2 SEAT TRACK STATION 1174-130 9 SRM 51-01. (M) 2 L 7 2 4F A6WE 2001041000233 20010410 00233 WP 2001 4 10 AALA20010321 1 20010205 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7512A 49806 TUL - FOUND RIGHT CUSP AT STATION 722. 6 INCHES INBOARD FROM WALL HAS CRACK. CUT OUT DAMAGE AND INSTALLED DOUBLER PER A ARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 2001041000234 20010410 00234 WP 2001 4 10 AALA20010322 1 20010205 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7512A 49806 TUL - FOUND CUSP CRACKED STATION 1290 JUST OUTBOARD NR 1 SEAT TRACK. INSTALLED NEW CUSP SHEET FROM STATION 1250-1309 LE FT PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2001041000235 20010410 00235 WP 2001 4 10 AALA20010323 1 20010209 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7512A 49806 TUL - FOUND LONGERON 2R CRACKED AT STATION 1418. INSTALLED NEW SECTION OF LONGERON EXTRUSION AS PER AARD 53-30-00-2, PA GE NR 1 AND NR 2. (M) 2 L 7 2 4F A6WE 2001041000236 20010410 00236 WP 2001 4 10 AALA20010267 1 20010126 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 242AA 49255 BOS - DURING OVERNIGHT INSPECTION, EMERGENCY EXIT LIGHT CONNECTOR PIN NOT SEATED. REINSTALLED EMERGENCY EXIT LIGHT CONN ECTOR PIN AT ROW 21. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001041000237 20010410 00237 WP 2001 4 10 AALA20010277 1 20010129 A 3350 CONTACTOR DOUG DC9 DC983 3022083 WP BATTERY DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 570AA 49352 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 18B, 20B, AND 20D INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT BATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001041000238 20010410 00238 WP 2001 4 10 AALA20010273 1 20010214 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 7508 49802 MIA - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001041000239 20010410 00239 WP 2001 4 10 AALA20010271 1 20010126 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 481AA 49656 PHX - DURING OVERNIGHT INSPECTION, EMERGENCY EXIT LIGHT CONNECTOR PIN NOT SEATED. RESEATED EMERGENCY EXIT LIGHT CONNECT OR PIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001041000240 20010410 00240 WP 2001 4 10 AALA20010269 1 20010127 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 294AA 49306 BOS - DURING OVERNIGHT INSPECTION, EMERGENCY LIGHT CONNECTOR HAS PIN NOT SEATED. RE-SEATED EMERGENCY EXIT LIGHT CONNECT OR PIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001041000241 20010410 00241 WP 2001 4 10 AALA20010268 1 20010129 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 21 7543A 53025 BOS - DURING OVERNIGHT INSPECTION, EMERGENCY EXIT LIGHT WIRE BROKEN. REPAIRED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001041000242 20010410 00242 WP 2001 4 10 AALA20010266 1 20010131 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 408AA 49319 SJC - DURING OVERNIGHT INSPECTION, EMERGENCY EXIT LIGHT ELECTRICAL CONNECTOR AT SEAT 20 DISCONNECTED. RE-CONNECTED EMER GENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001041000243 20010410 00243 WP 2001 4 10 AALA20010278 1 20010219 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 555AN 53085 DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT LIGHT DIM. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYST EM GROUND CHECKED NORMAL OPERATION. M) 2 L 7 2 4F A6WE 2001041000244 20010410 00244 NM 2001 4 10 AALA20010303 1 20010221 A 5310 STRUCTURE DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 1763 48553 TUL - FOUND CORROSION IN THE HOLES AND ON THE SURFACE OF THE RIGHT AFT MATING SURFACE OUTBOARD OF AFT HOLE. REMOVED COR ROSION PER ESO 41000 S/N 48553 DATED 2/21/2001. (M) 2 L 7 3 4F RT A22WE 2001041000245 20010410 00245 NM 2001 4 10 AALA20010348 1 20010221 A 5312 STIFFENER BOEING 727 727223 1384074 NM BULKHEAD CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 861AA 21088 TUL - FOUND VERTICAL STIFFENER ON BULKHEAD 1183 HAS CRACK FROM LOWER END BL 8. INSTALLED REPAIR PER DRAWING NR 65C29080 . INSTALLED BL 8 PREVENTATIVE MOD AND REPAIR KIT. (M) 2 L 7 3 4F A3WE 2001041000246 20010410 00246 NM 2001 4 10 AALA20010349 1 20010227 A 5210 SKIN BOEING 727 727223 1384074 NM PAX DOOR DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 861AA 21088 TUL - FOUND BLEND OUT OF AREA WITH NO EDGE DISTANCE TO FASTENERS. REMOVED DAMAGED SECTION OF SKIN EDGE AND INSTALLED RE PAIR DOUBLER PER SRM 52-00-3 FIG 4. (M) 2 L 7 3 4F A3WE 2001041000247 20010410 00247 NM 2001 4 10 AALA20010350 1 20010223 A 5320 PAN BOEING 727 727223 1384074 NM CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 861AA 21088 TUL - FOUND 40 INCH BY 2 INCH CORROSION ON FLOOR PAN ALONG HAT CHANNEL FROM STATION 1143-1183, RBL 27. REMOVED CORROSIO N, INSTALLED DOUBLER PER SRM 51-40-2. (M) 2 L 7 3 4F A3WE 2001041000248 20010410 00248 EU 2001 4 10 AALA20010359 1 20010228 A 5310 BEAM AIRBUS 300 A300B4605R 3930308 EU CABIN FLOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3075A 606 TUL - FOUND DOOR SILL BEAM CORRODED ON UPPER LIP AT FRAME 61. REMOVED CORROSION PER SRM 51-74-10 AND REPAIRED PER ESO 3 0595, DATED 28 FEB 2001. (M) 2 L 7 2 4F RT A35EU 2001041000249 20010410 00249 NM 2001 4 10 AALA20010302 1 20010221 A 5343 FITTING DOUG MD11 MD11 3023602 NM MLG TRUNNION CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 1763 48553 TUL - FOUND LEFT CENTER GEAR TRUNNION SUPPORT FITTING HAS CORROSION ON THE BOTTOM MATING SURFACE, FS 1520. REMOVED CORR OSION PER ESO 41000 S/N 48553 DATED 2/21/2001. (M) 2 L 7 3 4F RT A22WE 2001041000250 20010410 00250 WP 2001 4 10 AALA20010335 1 20010226 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG DISCHARGED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 469AA 49599 DFW - FLT 1571 - EN ROUTE DFW-TUS, SHORTLY AFTER TAKEOFF ATTEMPTED TO RAISE LANDED GEAR. LANDING GEAR WOULD NOT RETRACT . RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. SERVICED NOSE LANDING GEAR STRUT. ACCOMPLISHED GEAR RETRACTION PE R THE MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001041000251 20010410 00251 WP 2001 4 10 AALA20010336 1 20010224 A 2910 O-RING DOUG DC9 DC982 3022082 WP RUDDER LEAKING A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 582AA 53159 EWR - FLT 1704 - EN ROUTE ORD-EWR, DURING TAXI AIRCRAFT CABIN FILLED WITH SMOKE. DETECTED HYDRAULIC FLUID EMPTY. REPLA CED O-RING AT RUDDER SHUTOFF VALVE PLUG. ACCOMPLISHED LEAK CHECK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001041000252 20010410 00252 EU 2001 4 10 AALA20010337 1 20010226 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1409B 11367 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 9D INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PROXIMIT Y LIGHT SEGMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001041000253 20010410 00253 NM 2001 4 10 AALA20010338 1 20010226 A 3397 WIRE BOEING 727 727223 1384074 NM AFT VENT STAIR INOPERATIVE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 859AA 21086 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT VENTRAL STAIR INOPERATIVE. REPAIRED EMERGENCY EXIT WIRI NG AT AFT VENTRAL STAIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001041000254 20010410 00254 NM 2001 4 10 AALA20010339 1 20010210 A 2612 WARNING SYSTEM BOEING 777 777223 1385213 NM FWD CARGO BAY ACTIVATED A AALA F A ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 21 772AN 29580 DFW - FLT 157 - EN ROUTE DFW-KIX, DETECTED FORWARD CARGO FIRE INDICATION AT COCKPIT. DISCHARGED FIRE BOTTLES, DUMPED FU EL, RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. (M) 2 L 7 2 4F RT T00001SE 2001041000255 20010410 00255 WP 2001 4 10 AALA20010340 1 20010227 A 3350 LAMP DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7509 49803 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 14D TOO BRIGHT. REPLACED EMERGENCY EXIT LAMP AT SEAT 1 4D SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001041000256 20010410 00256 WP 2001 4 10 AALA20010341 1 20010227 A 3350 LAMP DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7509 49803 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 13D DIM. REPLACED EMERGENCY EXIT LAMP AT SEAT 13D. SY STEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001041000257 20010410 00257 NM 2001 4 10 AALA20010342 1 20010226 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 885AA 21524 DFW - FOUND DURING OVERNIGHT MAINTENANCE, FLOOR EMERGENCY EXIT LIGHT DIM AT COACH CLASS. REPAIRED EMERGENCY EXIT LIGHT STRIP AT COACH CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001041000258 20010410 00258 NM 2001 4 10 AALA20010343 1 20010225 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN INOPERATIVE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 397AN 29604 SEA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT REMAINED ILLUMINATED ON WOULD NOT RESET. REPAIRED EMERGENCY EX IT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001041000259 20010410 00259 WP 2001 4 10 AALA20010344 1 20010227 A 3222 O-RING DOUG DC9 DC982 3022082 WP NLG LEAKING A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 469AA 49599 DFW - FLT 1318 - EN ROUTE DFW-CMH, ON TAKEOFF, DETECTED NOSE GEAR LIGHT ILLUMINATE AT COCKPIT. RETURNED DFW AND LANDED WITHOUT INCIDENT. REPLACED O-RING AT NOSE LANDING GEAR SCHRADER VALVE. SERVICED STRUT. SWUNG NOSE LANDING GEAR PER TH E MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001041000260 20010410 00260 NM 2001 4 10 AALA20010345 1 20010227 A 2750 RELAY BOEING 767 767323 1385205 NM TE FLAPS FAILED A AALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 21 382AN 25451 LAX - LEADING EDGE FLAP ASSY EICAS AND LEADING EDGE LIGHT REMAINED ON AFTER FLAPS SELECTED TO ZERO LE FLAP ASSY. CHECKL IST RUN, FLAPS SELECTED BY ALT MEANS. REMOVED AND REPLACED RELAY K2307, REQUIRES OPS CHECK. ALSO, INSPECTED AND VERIFI ED WEAR LIMITS. FOUND WITHIN LIMITS. OPS CHECK NORMAL AS PER MM 27-81-24-6. ACCOMPLISHED OVERWEIGHT LANDING AS PER MM 05-51-35-2. (M) 2 L 7 2 4F RT A1NM 2001041000261 20010410 00261 NM 2001 4 10 AALA20010346 1 20010227 A 2421 GEN5103 GENERATOR BOEING 767 767323 1385205 NM LT ENGINE FAILED A AALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 21 372AA 25199 BHX - CLIMBING AT FL250, LEFT GENERATOR DRIVE LIGHT ILLUMINATED STEADY. ACCOMPLISHED ABNORMAL PROCEDURE AND DISCONNECTE D GEN DRIVE. REMOVED AND REPLACED LEFT IDG AS PER MM. OPS CHECK AND LEAK CHECK GOOD CLEARED MEL/MIC SHEET. (M) 2 L 7 2 4F RT A1NM 2001041000262 20010410 00262 NM 2001 4 10 AALA20010347 1 20010227 A 2422 INVERTER BOEING 767 767323 1385205 NM COCKPIT BURNED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 359AA 24040 CVR - FLT 950 - SMOKE IN COCKPIT AND CABIN MOST LIKELY RELATED TO STANDBY INVERTER. FOUND STANDBY INVERTER BLOWN. REPL ACED INVERTER AND OPS CHECKED PER MM. ALL CHECKS PER MM OK. STATIC INVERTER WAS SOURCE OF SMOKE IN THE CABIN. (M) 2 L 7 2 4F RT A1NM 2001041000263 20010410 00263 NM 2001 4 10 AALA20010361 1 20010228 A 2910 LINE BOEING 757 757223 1384957 NM MLG LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 21 670AA 25335 DFW - FLT 1881 - EN ROUTE AUS-SJC - LEFT HYDRAULIC SYSTEM QUANTITY DECREASED TO ZERO. DIVERTED DFW AND LANDED WITHOUT F URTHER INCIDENT. REPLACED RIGHT MAIN GEAR DOOR ACTUATOR HYDRAULIC FLEX LINE. SERVICED HYDRAULIC SYSTEM. PERFORMED LEA K CHECK. NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001041000264 20010410 00264 NE 2001 4 10 AALA20010362 2 20010227 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE NR 1 STALLED A AALA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SW 21 73444 49470 709765 DEN - FLT 1220 - EN ROUTE DEN-ORD, ON TAKEOFF, DETECTED NR 1 ENGINE COMPRESSOR STALL. RETURNED DEN AND LANDED WITHOUT F URTHER INCIDENT. REPLACED NR 1 ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F A6WE E9NE 2001041000265 20010410 00265 EU 2001 4 10 AALA20010363 1 20010228 A 2913 862536 PUMP FOKKER F28 F28MK0100 4990807 EU NR 1 ENGINE LEAKING A AALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 21 1420D 11403 BOS - FLT 1859 - EN ROUTE BOS-DCA, SHORTLY AFTER TAKEOFF BROUGHT GEAR AND FLAPS UP. FLAPS STOPPED AT SIX DEGREES. LOST HYDRAULIC PRESSURE. RETURNED BOS AND LANDED WITHOUT FURTHER INCIDENT. REPLACED NR 1 ENGINE HYDRAULIC PUMP. LEAK CHEC KS GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001041000266 20010410 00266 WP 2001 4 10 AALA20010202 1 20010121 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 TUL - FOUND CORROSION ON SEAT TRACK NR 2 STATION 1201. INSTALLED NEW SECTION OF NR 2 SEAT TRACK FROM STATION 1164-1309 PER SRM 53-05 FIG 4F. (M) 2 L 7 2 4F A6WE 2001041000267 20010410 00267 WP 2001 4 10 AALA20010203 1 20010121 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 TUL - FOUND 2 INCH BY 32 INCHES OF CORROSION ON FLOORBOARD SUPPORT AT STATION 200, RBL 10-42. REMOVED AND REPLACED FLOO RBOARD SUPPORT PER MM 51-00-00-8. (M) 2 L 7 2 4F A6WE 2001041000268 20010410 00268 WP 2001 4 10 AALA20010204 1 20010121 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 TUL - FOUND 2 INCH BY 4 INCHES OF CORROSION ON TOP SKIN OF FLOORBOARD STATION 146 RBL 24 APPROX. REMOVED AND REPLACED F LOORBOARD PER MM 53-20-01-2. (M) 2 L 7 2 4F A6WE 2001041000269 20010410 00269 WP 2001 4 10 AALA20010205 1 20010120 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 TUL - FOUND CORROSION 1 INCH BY 2 INCHES ON CUSP STATION 655-674 LEFT. INSTALLED DOUBLER FROM 661 TO 667 LEFT SIDE PER SRM 53-01 FIG 4-3. (M) 2 L 7 2 4F A6WE 2001041000270 20010410 00270 WP 2001 4 10 AALA20010206 1 20010119 A 5320 STRAP DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 TUL - FOUND CRACK IN TIE STRAP AT STATION 200 FRAME TO LONGERON 11 LEFT SIDE. INSTALLED DOUBLER PER AARD 53-10-00-11. (M) 2 L 7 2 4F A6WE 2001041000271 20010410 00271 WP 2001 4 10 AALA20010207 1 20010118 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 TUL - FOUND CRACK IN CUSP LEFT STATION 450 AT LIGHTENING HOLE. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SERM 53-01- 00. (M) 2 L 7 2 4F A6WE 2001041000273 20010410 00273 CE 2001 4 10 20010409CW013 1 20010101 A 5730 SKIN CESSNA 335 335 2075601 CE CONT O520 TSIO520* 17040 SO LT & RT WING WRINKLED D K NONE O OTHER IN INSP/MAINT 1 GL 17 2704U 3350005 AIRCRAFT WAS INSPECTED AND REPAIRED DUE TO HARD LANDING. ALL LANDING GEAR WERE REMOVED AND INSPECTED. LOWER WING SKINS WERE REPLACED ON BOTH WINGS DUE TO BEING WRINKLED. REPLACED. SEVERAL WHEEL WELL FORMERS WHICH WERE BENT. REINSTALLED LANDING GEAR AND RIGGED. AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3O 3 O 3A25 E8CE 2001041000277 20010410 00277 SO 2001 4 10 20010409CW018 1 20010315 A 2140 B4500 NOZZLE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA HEATER INOPERATIVE E WVBA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 AL 01 42WP 1031 1031 318252038 AIRCRAFT WAS HOLDING SHORT OF RUNWAY WHEN TOWER ALERTED PILOT OF CLOUD OF SMOKE FROM RIGHT SIDE OF AC. MECHANIC DETERMI NED THAT AC WAS SECURE FROM SMOKE/FLAME AND AC RETURNED TO BASE. IT WAS DETERMINED THAT THE HEATER HAD OVERTEMPED AND B ELCHED SMOKE BACK THROUGH THE BLOWER MOTOR INLET. A DECAY TEST WAS PERFORMED WITH NO LEAK DOWN DETECTED. THE IGNITOR U NIT WAS REPLACED. IGNITOR CLEANED. HEATER STILL RAN ROUGH. FUEL NOZZLE WAS REPLACED AND GROUND OPS AND LEAK CHECK APPE ARED NORMAL. NOZZLE PERMITTED EXCESS FUEL TO OT HEATER AND BELCH SMOKE/FUMES. 1 L 7 2 3O 3 O A20SO E14EA 2001041000278 20010410 00278 CE 2001 4 10 20010409CW019 1 20010301 A 2731 030A8521741 CONTROL CABLE MTSBSI MU2 MU2B35 5780411 CE GARRTT TPE331 TPE331* 01514 WP TRIM SEPARATED E K NONE O OTHER IN INSP/MAINT 1 SW 15 755MA 235 553 CABLE SEPARATED AT A 90 DEGREE TURN OVER PULLEY IN AFT TAIL CONE AREA 1 H 7 2 3T 3 T RT A10SW E2WE 2001041100001 20010411 00001 NM 2001 4 11 EISA20010003 1 20010127 A 3610 BACC10AD600W CLAMP BOEING BOEING 727 7272M7 138407S NM NR 3 ENGINE WORN A EISA K NONE J WARNING INDICATION CR CRUISE 1 SW 07 725RW 21502 NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED DURING FLIGHT. INSTALLED NEW CLAMPS ON DUCTS IN NR 3 STRUT. RAN UP TO POW ER, NO LIGHT. 2 L 7 3 4F A3WE 2001041100002 20010411 00002 WP 2001 4 11 MWEA010332 1 20010314 A 5320 992348461 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 FLOORBOARD SUPPORT AT STATION 200 BETWEEN AIRCRAFT CENTERLINE AND NR 3 SEAT TRACK IS CORRODED. REMOVED SUPPORT, FABRICA TED, LOCATED, DRILLED AND INSTALLED NEW SUPPORT. 2 L 7 2 4F A6WE 2001041100003 20010411 00003 NM 2001 4 11 EISA20010001 1 20010104 A 2611 74800 INDICATOR BOEING BOEING 727 727223 1384074 NM COCKPIT MALFUNCTIONED A EISA K NONE N FALSE WARNING CR CRUISE 1 SW 07 311NE 19703 LOWER CARGO COMPARTMENT FIRE DETECTION SYSTEM MAINTENANCE INDICATOR ILLUMINATED. GREEN SYSTEM OK LIGHT ILLUMINATED. RE SET SMOKE DETECTOR PER MAINTENANCE MANUAL 26-15-00, OPS CHECK GOOD. 2 L 7 3 4F A3WE 2001041100004 20010411 00004 NM 2001 4 11 EISA20010002 1 20010103 A 2133 10328051 OUTFLOW VALVE BOEING BOEING 727 727231 1384079 NM FUSELAGE OBSTRUCTED A EISA B A EMER. DESCENT UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 74318 20051 CLIMBING THROUGH 18000 FT CABIN STARTED TO CLIMB, UNABLE TO CONTROL IN AUTO OR MANUAL. DESCENDED TO 10000 FT, CABIN LEV ELED OFF AT 8000 FT. RETURNED TO AUSTIN. CORRRECTIVE ACTION: INSPECTED PRESSURIZATION SYSTEM FOUND DEBRIS IN OUT FLOW V ALVE, REMOVED DEBRIS FROM VALVE OPS CHECK NORMAL. 2 L 7 3 4F A3WE 2001041100009 20010411 00009 WP 2001 4 11 MWEA010337 1 20010314 A 5311 59114481 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FORWARD BAG PIT, FUSELAGE FRAME AT STATION 332 HAS LIGHT CORROSION IN LOWER FRAME CHANNEL ON AFT SIDE LONGERON 29 LEFT T O 28 RIGHT. REMOVED CORROSION, LOCATED, DRILLED AND INSTALLED REPAIR SPLICE. 2 L 7 2 4F A6WE 2001041100011 20010411 00011 NM 2001 4 11 EISA20010022 1 20010202 A 5720 ANGLE BOEING 727223 BOEING 727 727223 1384074 NM LT WING CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 19495 DURING ROUTINE C-CHECK INSPECTION FOUND ANGLE CRACKED AT STATION 92L WING ROOT. FABRICATED REPAIR ANGLE, ALODINED, PRIM ED, AND INSTALLED REPAIR ANGLE IAW SRM 51-30-2, 51-10-2, 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2001041100012 20010411 00012 NM 2001 4 11 EISA20010024 1 20010202 A 5320 651757931 ANGLE BOEING BOEING 727 727223 1384074 NM FUSELAGE CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ROUTINE C-CHECK INSPECTION FOUND CRACKED ANGLE UNDER FLOOR PANEL AT BS 300 RBL 10. REMOVED ANGLE, FABRICATED, AL ODINED, PRIMED, AND INSTALLED REPAIR ANGLE IAW SRM 51-30-2, 51-10-6, 51-40-4. 2 L 7 3 4F A3WE 2001041100013 20010411 00013 NM 2001 4 11 EISA200120025 1 20010202 A 5311 65224971 FRAME BOEING BOEING 727 727223 1384074 NM FUSELAGE CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ROUTINE C-CHECK, INSPECTION FOUND CRACK AT BS 298 RBL 14. FABRICATED REPAIR DOUBLER, ALODINED, PRIMED, AND INSTA LLED REPAIR IAW SRM 51-10-1 PARA 9, 51-40-3 FIG 1, 51-10-2, 51-30-2, M/M 20-10-20. 2 L 7 3 4F A3WE 2001041100014 20010411 00014 NM 2001 4 11 EISA20010004 1 20010202 A 2782 1U1095 STIFFENER BOEING BOEING 727 727223 1384074 NM SLAT CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ROUTINE C-CHECK INSPECTION, FOUND CRACK AT NR 2 SLAT ACTUATOR STIFFENER. REMOVED CRACKED STIFFENER, FABRICATED S TIFFENER, DOUBLER AND FILLER, ALODINED, PRIMED AND INSTALLED IAW SRM 51-30-2, 51-10-2, SB 57-0130, BSOPM 20-42-02. 2 L 7 3 4F A3WE 2001041100015 20010411 00015 NM 2001 4 11 EISA20010005 1 20010202 A 5754 FORMER BOEING BOEING 727 727223 1384074 NM SLAT CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ROUTINE C-CHECK INSPECTION FOUND CRACK AT NR 4 SLAT ACTUATOR INBOARD FORMER. STOP DRILLED CRACK, FABRICATED, REP AIR DOUBLER, ALODINED, PRIMED, AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-3, 51-30-2, 51-10-2. 2 L 7 3 4F A3WE 2001041100016 20010411 00016 NM 2001 4 11 EISA20010006 1 20010202 A 5744 65162211 SUPPORT FITTING BOEING BOEING 727 727223 1384074 NM SLAT DAMAGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ROUTINE C-CHECK INSPECTION FOUND OUTBOARD TRACK SUPPORT HAS ELONGATED HOLE. REAMED FITTING IAW SB 57-0134, ALODI NED AND PRIMED IAW SRM 51-10-2. 2 L 7 3 4F A3WE 2001041100017 20010411 00017 NM 2001 4 11 EISA20010007 1 20010202 A 5311 6522497 FRAME BOEING BOEING 727 727223 1384074 NM FUSELAGE DAMAGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ROUTINE C-CHECK INSPECTION FOUND ELONGATED HOLE AT BS 870. REAMED HOLE PER SB 53-0194 TO 402. 2 L 7 3 4F A3WE 2001041100018 20010411 00018 NM 2001 4 11 EISA20010008 1 20010202 A 5311 65561641 FRAME BOEING BOEING 727 727223 1384074 NM FUSELAGE CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ROUTINE C-CHECK INSPECTION FOUND BS 620 FRAME WEB HAS CRACK STARTING AT LOWER TOOLING HOLE AND EXTENDING DOWN THR OUGH FASTENER HOLE. CORRECTIVE ACTION: FABRICATED REPAIR DOUBLER, ALODINED, PRIMED AND INSTALLED REPAIR DOUBLER IAW SRM 51-10-2, 51-30-2, 51-40-2 FIG 1. 2 L 7 3 4F A3WE 2001041100019 20010411 00019 NM 2001 4 11 EISA20010009 1 20010202 A 5753 SKIN BOEING BOEING 727 727223 1384074 NM FLAP DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ROUTINE C-CHECK INSPECTION FOUND NR 4 AFT FLAP TRAILING EDGE DELAMINATED. REMOVED DELAMINATED AREAS OF FLAP TRAI LING EDGE, CLEANED, PREPPED, ALODINED, PRIMED, AND BONDED FIBERGLASS OVERLAYS IAW SRM 51-10-2, 57-50-1 FIG 3, 51-40-6 FI G 37. 2 L 7 3 4F A3WE 2001041100020 20010411 00020 NM 2001 4 11 EISA20010010 1 20010202 A 5523 657279919 SKIN BOEING BOEING 727 727223 1384074 NM ELEVATOR TAB DAMAGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ROUTINE C-CHECK INSPECTION FOUND HOLE IN LT ELEVATOR TAB UPPER SURFACE. CLEANED PREPPED AND POTTED .250 DIAMETER AREA, ALODINED, PRIMED, AND PAINTED. WEIGHT AND BALANCE IAW SRM 51-40-6 FIG 35, 51-10-2, 51-80-9 PG 1, 51-80 FIG 2, AN D M/M 27-30-1. 2 L 7 3 4F A3WE 2001041100021 20010411 00021 NM 2001 4 11 EISA20010011 1 20010202 A 5744 ATTACH FITTING BOEING BOEING 727 727223 1384074 NM LT WING CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ROUTINE C-CHECK INSPECTION FOUND CRACKS AT TOP OF LEFT WING AT NR 2, 3, AND 4 SPOILER ATTACH POINTS. STOP DRILL ED CRACKS, FABRICATED, INSTALLED, ALODINED, AND PRIMED REPAIR DOUBLERS, IAW SRM 51-10-2, 51-30-4 FIG 10, AND 51-30-2. 2 L 7 3 4F A3WE 2001041100022 20010411 00022 NM 2001 4 11 EISA20010013 1 20010202 A 5347 SEAT TRACK BOEING BOEING 727 727223 1384074 NM CABIN CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION ON SEAT TRACK FROM BS 580 TO BS 620 LBL 45.50. REMOVED CORRODED SEAT TRACK, FABRICATED TRACK SPLICE, DRILLED DEBURRED, COUNTERSUNK, ALODINED, PRIMED, AND INSTALLED IAW 53-10-1, 53-10-5 FIG 7, 51-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 2001041100023 20010411 00023 NM 2001 4 11 EISA20010015 1 20010202 A 7120 FABRICATED MOUNT BRACKET BOEING BOEING 727 727223 1384074 NM NR3 ENGINE DAMAGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ROUTINE C-CHECK INSPECTION FOUND NR 3 ENGINE AFT MOUNT LOWER FLANGE HAS ELONGATED HOLES. FABRICATED FREEZE PLUGS , STAP, ALODINED, PRIMED, AND INSTALLED REPAIR IAW EOI-DAL-00-0081H, AND SRM 51-10-2, 51-30-2. 2 L 7 3 4F A3WE 2001041100024 20010411 00024 NM 2001 4 11 EISA20010017 1 20010202 A 5347 65208247 SEAT TRACK BOEING BOEING 727 727223 1384074 NM CABIN CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION AROUND FASTENER HEADS ON SEAT TRACK FROM BS 480 TO BS 580. REMOVED CO RRODED SEAT TRACK SECTION, FABRICATED SEAT TRACK, SPLICE DRILLED, DEBURRED, COUNTER SUNK, ALODINED, PRIMED, AND INSTALLE D SEAT TRACK SPLICE IAW SRM 51-30-2, 51-10-2, 53-10-1 FIG 3, 53-10-5 FIG 7. 2 L 7 3 4F A3WE 2001041100027 20010411 00027 NM 2001 4 11 EISA20010018 1 20010202 A 5347 65208247 SEAT TRACK BOEING BOEING 727 727223 1384074 NM CABIN CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION AROUND SCREW HEADS ON SEAT TRACK LBL 24.50 FROM BS 640 TO BS 720. REM OVED CORRODED SEAT TRACK FABRICATED, TRIMMED, DRILLED, ALODINED, PRIMED, AND INSTALLED, SEAT TRACK SPLICE IAW SRM 53-10- 1, 53-10-5 FIG 7, 51-10-2, 51-30-2. 2 L 7 3 4F A3WE 2001041100028 20010411 00028 NM 2001 4 11 EISA20010019 1 20010202 A 5347 65208247 SEAT TRACK BOEING BOEING 727 727223 1384074 NM CABIN CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION ON SCREW HEADS ON SEAT TRACK RBL 24.50 FROM BS 480 TO BS 680. REMOVED SEAT TRACK, FABRICATED, TRIMMED, DRILLED, ALODINED, PRIMED, AND INSTALLED SEAT TRACK SPLICE, AT RBL 24.50 FROM BS 480 T O BS 680 IAW SRM 53-10-1 FIG 3, 53-10-5 FIG 7, 51-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 2001041100029 20010411 00029 NM 2001 4 11 EISA20010020 1 20010202 A 5754 FABRICATED ANGLE BOEING BOEING 727 727223 1384074 NM L/E FLAP CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ROUTINE C-CHECK INSPECTION FOUND ANGLE CRACKED IN LEFT WING LEADING EDGE OF NR 3 KRUEGER FLAP. REMOVED ANGLE, FA BRICATED AND INSTALLED REPAIR ANGLE, ALODINED AND PRIMED IAW SRM 51-40-3 FIG 1, 51-30-2. 2 L 7 3 4F A3WE 2001041100030 20010411 00030 NM 2001 4 11 EISA20010021 1 20010202 A 5347 65208247 SEAT TRACK BOEING BOEING 727 727223 1384074 NM CABIN CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION ON SEAT TRACK AT RBL 45.50 BS 700. REMOVED CORRODED SECTION, FABRICAT ED SEAT TRACK LOCATED HOLES, ALODINED, PRIMED, AND INSTALLED SEAT TRACK SPLICE IAW SRM 51-10-2, 51-10-6, 53-10-1, 51-10- 5 FIG 1, 53-10-2 FIG 7, 51-30-2. 2 L 7 3 4F A3WE 2001041100031 20010411 00031 NM 2001 4 11 EISA20010023 1 20010202 A 5311 65224971 FRAME BOEING BOEING 727 727223 1384074 NM FUSELAGE DAMAGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ROUTINE C-CHECK INSPECTION FOUND HOLE IN FRAME AT STRINGER 17L. FABRICATED REPAIR DOUBLER, ALODINED, REPAIRED, A ND INSTALLED REPAIR IAW SRM 51-30-2, 51-10-2, 53-10-4 FIG 1. 2 L 7 3 4F A3WE 2001041100033 20010411 00033 NM 2001 4 11 UPS01235534 1 20010328 A 5230 STIFFENER BOEING 727 72731C 1384011 NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C & SI, SUSPECT CRACK FWD CARGO DOOR INTERIOR AT HORIZONTAL STIFFENER LWR FLANGE IN CONTACT WITH INTER IOR SKIN FROM FWD END. REPLACED DOOR IAW NRC 320552 2 L 7 3 4F A3WE 2001041100034 20010411 00034 EU 2001 4 11 UPS01135474 1 20010329 A 2840 WARNING SYSTEM AIRBUS A300 A300F4622R 3930360 EU FUEL TANK ACTIVATED A IPXA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 128UP 0813 IN FLT, ECAM MSG AUTO TRIM TANK SYS INOP / FUEL GRAVITY FWD TRANSFER ONLY. ITEM TRANSFERED TO MEL M212201. PLACARD INST ALLED. ITEM CLEARED, PLACARD REMOVED. NOW AIRCRAFT RESTORED TO NORMAL OPERATING CONFIGURATION. 2 L 7 2 4F RT A35EU 2001041100035 20010411 00035 NM 2001 4 11 UPS01235463 1 20010328 A 5610 WINDSHIELD BOEING 727 72725C 138400H NM COCKPIT FAILED A IPXA O OTHER O OTHER CR CRUISE 1 SO 01 933UP 19857 FIRST OFFICERS WINDSHIELD SHATTERED. OLD WINDOW REMOVED NEW WINDOW PARTIALLY INSTALLED / R&R R1 WINDOW PER M/M 56-11-1 WINDOW HEAT OPS CHECK GOOD 2 L 7 3 4F A3WE 2001041100036 20010411 00036 NM 2001 4 11 UPS01235473 1 20010328 A 3350 LIGHT BOEING 727 727172C 1384058 NM COCKPIT LOOSE A IPXA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 916UP 19808 EMERGENCY EXIT LIGHT HOUSING IN COCKPIT IS LOOSE. ON T/O & LANDING HOUSING COME LOOSE & EMERGENCY EXIT LIGHT ILLUMINATED . REMOVED EMERGENCY EXIT LIGHT ASSY & REFITTED BASE TO LIGHT ASSY ENSURING PROPER FIT. LIGHT ASSY REINSTALLED TO A/ C SYS & LIGHT OPS CHECK NORMAL. 2 L 7 3 4F A3WE 2001041100037 20010411 00037 NM 2001 4 11 UPS01235475 1 20010330 A 2120 UNKNOWN BOEING 727 727185C 138406N NM COCKPIT ODOR A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 01 940UP 19826 SMOKE ODOR IN FLT DECK AREA. RAN ALL 3 ENGINES AND OPERATED ALL PACKES AT FULL HOT AND COLD. COULD NOT DUPLICATE. OPER ATED ALL NAV AND COMM EQUIPMENT. NO DEFECTS NOTED. OK TO CONTINUE SERVICE 2 L 7 3 4F A3WE 2001041100038 20010411 00038 NM 2001 4 11 UPS01435464 1 20010314 A 5347 SEAT TRACK BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C CORROSION ON UPPER DECK SEAT TRACK AT BS 530 - BS 580 RBL 64. SEAT TRACK REPLACED IAW SRM 53-10-05 2 L 7 4 4F A20WE 2001041100039 20010411 00039 NM 2001 4 11 UPS01435466 1 20010315 A 5311 FRAME BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, MAIN DECK FRAME WEB IS CRACKED AT CUT OUT FOR STR. AT BS 2120 STR 25 LT. REPAIR CARRIED OUT IAW Q UERY NOTE NUMBER 10/01 2 L 7 4 4F A20WE 2001041100040 20010411 00040 NM 2001 4 11 UPS01435467 1 20010315 A 5311 FRAME BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, MAIN DECK FRAME WEB IS CRACKED AT CUT OUT FOR STRINGER AT BS 2180 S 25 LT. REPAIR CARRIED OUT IAW QUERY NOTE NO.10/01 2 L 7 4 4F A20WE 2001041100041 20010411 00041 NM 2001 4 11 UPS01435468 1 20010316 A 5320 141U10429 STRAP BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, CRACK ON STRAP AT AFT AIDE OF FRONT PRESSURE BULKHEAD AT LBL AND RBL 25. CHORD REPLACED IAW EO B7 47-5310-3279-D 2 L 7 4 4F A20WE 2001041100042 20010411 00042 NM 2001 4 11 UPS01435469 1 20010312 A 5610 14160008 WINDOW BOEING 747 747123F NM COCKPIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, COCKPIT NR 3 RT WINDOW IS CRACKED. NR 3 RT COCKPIT WINDOW REPLACED IAW MM 56-11-02 2 L 7 4 4F A20WE 2001041100043 20010411 00043 NM 2001 4 11 UPS01435470 1 20010312 A 5610 14150008 WINDOW BOEING 747 747123F NM COCKPIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, COCKPIT NR 2 RT WINDOW IS CRACKED. NR 2 RT WINDOW REPLACED IAW MM 56-11-02 2 L 7 4 4F A20WE 2001041100044 20010411 00044 NM 2001 4 11 UPS01435341 1 20010211 A 5320 65B140561 SUPPORT BOEING 747 747259B NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 527UP 21730 INSPECTION TYPE:C STA 1329 LOWER FUSELAGE SUPPORT BETWEEN BODY GEAR DOORS IS CORRODED BEYOND LIMITS. REMOVED AND REPLAC ED SUPPORT IAW DWG 65B14056, AND SRM 51-10-02. 2 L 7 4 4F RT A20WE 2001041100045 20010411 00045 NM 2001 4 11 AWXA0001511 1 20010321 A 5312 65163007 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 FS 178 BULKHEAD WEB FROM FWD SIDE WL 234.1 CRACKED AT 4 FASTENERS RBL 9, 10.2, 11 AND 12. REMOVED FASTENERS; CUTOUT DAM AGED AREA; LOCATED, DRILLED, AND INSTALLED REPAIR DOUBLER AND FILLER IAW B737-300 SRM 53-10-08 PG 265-269, FIG 209. 2 L 7 2 4F RT A16WE 2001041100046 20010411 00046 NM 2001 4 11 EISA20010031 1 20010224 A 2782 CONNECTOR BOEING BOEING 727 727223 1384074 NM ACTUATOR LOOSE A EISA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CR CRUISE 1 SW 07 315NE 20190 NR 8 LEADING EDGE SLAT HAD BOTH AMBER LIGHTS ON IN AGREEMENT, PILOT STATED THAT HE COULD FEEL VIBRATION. THE AIRCRAFT O VERFLEW DFW TO IND. INSPECTED NR 8 ACTUATOR AND FOUND LOOSE CONNECTOR. TIGHTENED CONNECTOR ON ACTUATOR, OPS CHECK GOOD . 2 L 7 3 4F A3WE 2001041100047 20010411 00047 NE 2001 4 11 EISA20010034 2 20010302 A 7260 504898 FITTING PWA BOEING 727 727277 138408S NM PWA JT8 JT8D15 52051 NE NR 2 GEARBOX LOOSE A EISA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 275WC 20549 687406 INFLIGHT NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. ASSOCIATED PRESSURE INDICATED 10-12 PSI. ENGINE SHUT DOWN IAW EXPRESS ONE CHECKLIST, DIVERTED INTO OMA. REPLACED GEARBOX FITTING TO DIFFERENTIAL PRESSURE PORT IAW 72-61-00. NO DEF ECTS NOTED. 2 L 7 3 4F 4 F RT A3WE E2EA 2001041100048 20010411 00048 NM 2001 4 11 EISA20010027 1 20010220 A 2420 902F2425 PANEL BOEING 727 727225 1384077 NM COCKPIT FAULTY A EISA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SW 07 354PA 20624 ON CLIMBOUT NR 1 GENERATOR TRIPPED VOLTS AND FREQS WERE 0 AFTER RESETTING FR. DISCONNECTED CSD PER ABNORMALS, AIR TURNB ACK TO (CLT). REMOVED AND REPLACED NR 1 BUS PROTECTION PANEL, OPS CHECK OK PER M/M 24-20-01. 2 L 7 3 4F A3WE 2001041100049 20010411 00049 NM 2001 4 11 EISA20010028 1 20010222 A 2611 100064901 SENSOR BOEING 727 727223 1384074 NM CARGO BAY MALFUNCTIONED A EISA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SW 07 701NE 22459 ON TAKEOFF LOWER AFT CARGO SMOKE DETECTION LIGHT ILLUMINATED. CHECK AND INSPECTED LOWER AFT CARGO COMPARTMENT FOUND OK, DEACTIVATED ACO 00-26-37, ST3000 SYSTEM. 2 L 7 3 4F A3WE 2001041100050 20010411 00050 NM 2001 4 11 EISA20010038 1 20010214 A 5347 BAC1520792 SEAT TRACK BOEING BOEING 727 727223 1384074 NM CABIN CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION AT MAIN CABIN SEAT TRACK SECTION BS 910 TO BS 950 LBL 24.75. FABRICAT ED AND INSTALLED SEAT TRACK SPLICE AT BS 910 TO BS 950 LBL 24.75, ALODINED AND PRIMED SEAT TRACK SPLICE IAW SRM 53-10-5 FIG 7, 51-10-6, 51-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 2001041100051 20010411 00051 NM 2001 4 11 EISA20020039 1 20010214 A 5347 BAC1520792 SEAT TRACK BOEING BOEING 727 727223 1384074 NM CABIN CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION AT MAIN CABIN SEAT TRACK SECTION BS 920 TO BS 960 AT 0 BL. FABRICATED AND INSTALLED SEAT TRACK SPLICE AT BS 920 TO BS 960 0 BL, ALODINED AND PRIMED SEAT TRACK IAW SRM 51-10-5 FIG 7 AND FIG 2, 53-10-5, 51-10-6, 51-10-2. 2 L 7 3 4F A3WE 2001041100052 20010411 00052 NM 2001 4 11 MWEA010274 1 20010306 A 3010 3080700 ANTI-ICE SYSTEM DOUG MD88 MD88 3023688 NM LT WING INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 601ME 49762 LEFT OVERWING HEATER INOPERATIVE. REMOVED AND REPLACED HEATER BLANKET. 2 L 7 2 4F RT A6WE 2001041100053 20010411 00053 WP 2001 4 11 MWEA010389 1 20010324 A 7711 20470201 INDICATOR DOUG DC9 DC9* WP COCKPIT FAILED A MWEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 31 809ME 48071 ADVANCING THROTTLES FOR TAKE OFF, LEFT EPR GUAGE FLAGGED. TRIED ENGINE ANTI-ICE BUT NO HELP. WHEN ENGINE SHUT DOWN AT GATE GUAGE FLAGGED AGAIN. REMOVED AND REPLACED WITH SERVICABLE EPR INDICATOR IAW MM 77-10-00. 2 L 7 2 4F A6WE 2001041100054 20010411 00054 WP 2001 4 11 MWEA010371 1 20010326 A 5220 3913926521 FITTING DOUG DC9 DC914 3022034 WP VENTRAL DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 AFT VENTRAL PLUG DOOR FITTING LONGERON 20 HAS A CRACK INDICATION FROM ONE FASTENER. REMOVED FASTENER, FABRICATED NEW R EPAIR ANGLES, INSTALLED REPAIR ANGLES. 2 L 7 2 4F A6WE 2001041100055 20010411 00055 WP 2001 4 11 MWEA010372 1 20010326 A 5220 3913926525 FITTING DOUG DC9 DC914 3022034 WP VENTRAL DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 AFT VENTRAL PLUG DOOR FITTING LONGERON 12 HAS A CRACK INDICATION FROM ONE FASTENER. REMOVED FASTENER, FABRICATED NEW REPAIR, INSTALLED REPAIR ANGLE. 2 L 7 2 4F A6WE 2001041100056 20010411 00056 WP 2001 4 11 MWEA010373 1 20010326 A 5330 5911400 SKIN DOUG DC9 DC914 3022034 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FUSELAGE LEFT SIDE HAS A DENT AT STATION 58 AND 3 INCHES ABOVE LEFT FORWARD NLG DOOR HINGE. -- FABRICATED, DRILLED A ND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001041100057 20010411 00057 WP 2001 4 11 MWEA010374 1 20010326 A 5330 5911411 SKIN DOUG DC9 DC914 3022034 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 DENT IN FUSELAGE SKIN AT STATION 389, 2 INCHES BELOW LONGERON 19 RT, D=1.3, X=.020, D/X=65. REMOVED INTERCOSTAL, COLD FORMED SKIN, FABRICATED AND INSTALLED REPAIR DOUBLER, INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001041100058 20010411 00058 NM 2001 4 11 01FDEA00195 1 20010314 A 5311 6516342 FRAME BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 FRAME IS CRACKED AT CEILING SUPPORT BS 1030, LBL 33.5, WL 294. * S/D * CUT OUT CRACK AND REPAIRED PER IAW FEDEX EA 7-5 310-56295. 2 L 7 3 4F RT A3WE 2001041100059 20010411 00059 SO 2001 4 11 COMA0110052 1 20010312 A 5320 12005802001 SILL EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 21213 120264 DURING 2C CHECK TASK 131-01Z, THE FUSELAGE LT FORWARD FLOOR BEAM SILL WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCO RDANCE WITH EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001041100060 20010411 00060 WP 2001 4 11 MWEA010339 1 20010315 A 5321 995791917 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 CABIN FLOORBOARD B3 HAS AREAS OF CORROSION AROUND FASTENER HOLES. REMOVED SKIN, FABRICATED NEW SKIN AND SUPPORT, INSTAL LED SKIN. 2 L 7 2 4F A6WE 2001041100061 20010411 00061 WP 2001 4 11 MWEA010340 1 20010315 A 5320 99115505 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 REMOVED LEFT E&E DOOR JAMB INTERCOSTAL FOR OTHER MAINTENANCE AND FOUND CRACK. REMOVED INTERCOSTAL, FABRICATED NEW, LOCA TED, DRILLED AND INSTALLED NEW. 2 L 7 2 4F A6WE 2001041100062 20010411 00062 NM 2001 4 11 01FDEA00201 1 20010314 A 3231 DOOR BOEING 727 7272S2F 1384O81 NM NLG MALFUNCTIONED A FDEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 25 216FE 22937 WHEN GEAR WAS EXTENDED MANUALLY HAD RED DOOR LIGHT BUT NO GREEN LIGHT. CK VIEW PORT AND CONFIRM NOT DOWN. PERF OPS CK OF NOSE GEAR MANUAL EXT, BOTH POWER ON AND OFF. CYCLED 5 TIMES, NO DEFECT NOTED. OPS CK GOOD PER IAW MM 32-34-000-5 AN D MM 7-11-000-2. 2 L 7 3 4F A3WE 2001041100063 20010411 00063 NM 2001 4 11 01FDEA00197 1 20010314 A 5311 6516342 FRAME BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 FRAME IS CRACKED AT CEILING SUPPORT MOUNTING POINT BS 1030, RBL 33.5, WL 294. * S/D * FAB & R&R PER IAW FEDEX SRM 53-10 -4 FIG 2 AND FEDEX EA 7-5310-56296. 2 L 7 3 4F RT A3WE 2001041100064 20010411 00064 SO 2001 4 11 COMA0110048 1 20010312 A 5320 12046963001 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 7922 120264 DURING 2C CHECK TASK 131-01Z, THE FUSELAGE LT FORWARD FLOORBEAM BUTTSTRAP WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001041100065 20010411 00065 SO 2001 4 11 COMA0110050 1 20010312 A 5320 12005805003 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 7922 120264 DURING 2C CHECK TASK 131/132-01Z, THE FUSELAGE CENTER FORWARD FLOORBEAM BUTTSTRAP WAS FOUND CORRODED. THE PART WAS REPL ACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001041100066 20010411 00066 SO 2001 4 11 COMA0110053 1 20010312 A 5320 12046156001 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 21213 120264 DURING 2C CHECK TASK 132-01Z, THE FUSELAGE RT FORWARD FLOOR BEAM BUTTSTRAP WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001041100067 20010411 00067 SO 2001 4 11 COMA0110054 1 20010312 A 5315 12005807007 FLOORBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 21213 120264 DURING 2C CHECK TASK 131/132-01Z, THE FUSELAGE CENTER FORWARD FLOOR OMEGA BEAM WAS FOUND CORRODED. THE PART WAS REPAIRE D IN ACCORDANCE WITH EMB-120 STANDARD PRACTICES AND AERODESIGN REPORT 2181-12, REV IR, 3-4-01. 2 L 7 2 4T RT A31SO 2001041100068 20010411 00068 SO 2001 4 11 COMA0110056 1 20010312 A 5320 12004149002 CROSSBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 7922 120264 DURING 2C CHECK TASK 132-01Z, THE FUSELAGE RT FLOOR CROSSBEAM AT FRAME 16 WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001041100069 20010411 00069 SO 2001 4 11 COMA0110057 1 20010312 A 5720 12017054615 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 21213 120264 DURING 2C CHECK TASK 5720-522-011, THE LT WING LOWER SKIN SUPPORT AT RIB 8, AND STRINGER 10, WAS FOUND CRACKED. THE PAR T WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3813-1, REV IR, 11-5-00. 2 L 7 2 4T RT A31SO 2001041100070 20010411 00070 EU 2001 4 11 2001UALA00127 1 20010219 A 2133 OUTFLOW VALVE 90231570381 AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE PRESSURIZATION ERRATIC A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 430UA 568 RETURNED TO THE FIELD DUE TO A CABIN PRESSURIZATION PROBLEM. *S/D* FOUND OUTFLOW VALVE OPERATION ERRATIC. REPLACED TH E OUTFLOW VALVE. NO FURTHER DISCREPANCIES REPORTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2001041100071 20010411 00071 NE 2001 4 11 2001UALA00181 2 20010304 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE LT & RT ENGINE FLAMED OUT A UALA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 WP 29 666UA 29238 LEFT AND RIGHT ENGINE FLAMEOUT REPORTED AT FL240. RESTARTS ACCOMPISHED. DIVERTED KOA. EMERGENCY DECLARED. LANDED APP ROXIMATELY 24000 LBS OVERWEIGHT. 2 L 7 2 4F 4 F RT A1NM E24NE 2001041100072 20010411 00072 NM 2001 4 11 2001UALA00182 1 20010214 A 5347 SEAT TRACK BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 618UA 21878 MAIN CABIN SEAT TRACK FITTING CORRODED AT STATION 1421 T0 1471, RBL 90, UNDER FLANGE. REPLACED FITTING PER BAC DWG 146 T5204-2 AND INSTALLED FITTING PER SRM 51-40-2. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041100073 20010411 00073 NM 2001 4 11 2001UALA00183 1 20010214 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 618UA 21878 AFT PIT SHEAR TIE BETWEEN STR 39L AND 39R CORRODED. INSTALLED NEW SHEAR TIE PER BAC DRAWING 146T1206 AND SRM 51-40-2. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041100074 20010411 00074 NM 2001 4 11 2001UALA00185 1 20010221 A 5753 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE T/E FLAP DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7288U 21566 RIGHT INBOARD FLAP IS DELAMINATED AND LEFT INBOARD FORE FLAP UPPER SURFACE IS CHAFED. REMOVED AND REPLACED RIGHT INBOAR D FLAP PER MM 27-51-04. REPAIRED LEFT INBOARD FORE FLAP PER GN MM 1-0-1-66. 2 L 7 3 4F 4 F A3WE E2EA 2001041100075 20010411 00075 NM 2001 4 11 2001UALA00186 1 20010214 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 618UA 21878 AFT PIT SHEAR TIE CORRODED BS 1480. REPLACED SHEAR TIE REF: BAC 140T2102 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041100076 20010411 00076 NM 2001 4 11 2001UALA00189 1 20010214 A 5414 SPLICE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE PYLON CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 618UA 21878 NR 1 PYLON INBOARD SIDE BETWEEN 2 SIDE PANELS, ATTACH SPLICE IS CORRODED. REPLACED SPLICE PER SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041100077 20010411 00077 NM 2001 4 11 2001UALA00194 1 20010222 A 5754 SLAT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7450U 21904 NR 6 SLAT CRACKED UNDER ANTI-ICE DUCT. REPAIRED SLAT CRACK PER SM-OR-70-57-56-01-AR11. 2 L 7 3 4F 4 F A3WE E2EA 2001041100078 20010411 00078 NM 2001 4 11 2001UALA00199 1 20010228 A 5754 RIB BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE L/E SLAT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7448U 21902 NR 6 SLAT UNDER INBOARD PANEL RIB IS CRACKED. REPAIRED SLAT RIB PER SRM 70-57-56-01-JD. INSTALLED ACCESS PANELS PER GN MM 1-0-1-2. 2 L 7 3 4F 4 F A3WE E2EA 2001041100079 20010411 00079 NM 2001 4 11 2001UALA00200 1 20010222 A 5751 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE AILERON DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7450U 21904 THE AILERON SKIN IS DAMAGED AND STRETCHED. REPLACED UPPER AND LOWER AILERON SKIN PER BAC DWG 65-21766 AND SRM 51-30-2. REBALANCED SURFACE PER SRM 51-80-04. 2 L 7 3 4F 4 F A3WE E2EA 2001041100081 20010411 00081 NM 2001 4 11 2001UALA00212 1 20010221 A 5523 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE ELEVATOR TAB DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7288U 21566 LEFT ELEVATOR TAB IS DELAMINATED. REPAIRED TAB PER GN MM 1-0-1-24 AND CALCULATED WEIGHT AND BALANCE PER SRM 51-80-09. 2 L 7 3 4F 4 F A3WE E2EA 2001041100082 20010411 00082 SO 2001 4 11 COMA0110059 1 20010312 A 5320 12061603602 FLOOR SUPPORT EMB 120 EMB120RT SO FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 21213 120264 DURING 2C CHECK TASK 122-01Z, THE FUSELAGE RT FLOOR PROP AT FRAME 13 WAS FOUND CRACKED. THE PART WAS REPAIRED IN ACCORD ANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT NR 3647-1, REV IR, 5-3-00. 2 L 7 2 4T RT A31SO 2001041100083 20010411 00083 NM 2001 4 11 UPS01235527 1 20010321 A 5753 651920217 CARRIAGE BOEING 727 72731C 1384011 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C & SI, NR 1 FLAP TRACK CARRIAGE HAS CORROSION INSIDE SPINDLE BORE. REPLACED CARRIAGE 2 L 7 3 4F A3WE 2001041100084 20010411 00084 NM 2001 4 11 UPS01235528 1 20010321 A 5753 65192929 CARRIAGE BOEING 727 72731C 1384011 NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C & SI, NR 2 FLAP TRACK CARRIAGE HAS CORROSION INSIDE SPINDLE BORE. CARRIAGE ASSY REPLACED. 2 L 7 3 4F A3WE 2001041100085 20010411 00085 NM 2001 4 11 UPS01235529 1 20010328 A 5230 STRUCTURE BOEING 727 72731C 1384011 NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C & SI, SUSPECT CRACK ON DOOR FRAME INTERIOR FWD CARGO DOOR. DOOR REPLACED ON NRC320552 2 L 7 3 4F A3WE 2001041100086 20010411 00086 NM 2001 4 11 UPS01235530 1 20010327 A 5230 STIFFENER BOEING 727 72731C 1384011 NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C & SI, SUSPECT CRACK FWD CARGO DOOR VERTICAL STIFFENER AT FWD UPPER CORNER ADJACENT TO INTERIOR SKIN AND HINGE ATTACH POINT FWD, REPLACED DOOR ON NRC320552 2 L 7 3 4F A3WE 2001041100087 20010411 00087 NM 2001 4 11 UPS01235531 1 20010327 A 5230 STIFFENER BOEING 727 72731C 1384011 NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C & SI, CRACK IN FWD CARGO DOOR AT VERTICAL STIFFENER FWD UPPER CORNER SUPPORT ANGLE ADJACENT TO AFT H INGE AFT SIDE. REPLACED DOOR IAW NRC320552 2 L 7 3 4F A3WE 2001041100088 20010411 00088 NM 2001 4 11 UPS01235533 1 20010328 A 5230 STIFFENER BOEING 727 72731C 1384011 NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C & SI, SUSPECT CRACK HORIZONTAL STIFFENER AT FLANGE RADIUS IN CONTACT WITH INTERIOR SKIN 20 INCHS FWD OF AFT EDGE STIFFENER RUNS BETWEEN FWD AND AFT DOOR STOP ON FWD CARGO DOOR. REPLACED DOOR IAW NRC 320552 2 L 7 3 4F A3WE 2001041100089 20010411 00089 NM 2001 4 11 2001UALA00104 1 20010211 A 3350 1102833LB LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7264U 21411 THE CENTER OVERWING EXIT SIGN IS INOPERABLE. *S/D* REPLACED LIGHT ASSEMBLY L876. OPERATION CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001041100090 20010411 00090 2001 4 11 UPS01235445 4 20010321 A 2565 GIRT BAR BOEING 727 72722C 138400F NM ESCAPE SLIDE INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE: PREFLT, ESCAPE SLIDE GIRT BAR STOW HOOKS DO NOT HOLD BAR IN PLACE WHEN SLIDE IS DISENGAGED. REMOV ED MAIN ENTRY DOOR SLIDE COVER FOR REPAIR. INSTALLED MAIN ENTRY DOOR EVACUATION SLIDE AND COVER IAW B727 MM 25-60-03. 2 L 7 3 4F A3WE 2001041100091 20010411 00091 NM 2001 4 11 UPS01235446 1 20010322 A 2610 WARNING LIGHT BOEING 727 72727C 138400J NM COCKPIT ILLUMINATED A IPXA K NONE N L FALSE WARNING NO TEST IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: PREFLT, LWR CARGO FIRE DETECTION UNIT YELLOW MX LIGHT ILLUMINATED. TESTED LOWER SMOKE / FIRE DETEC TION SYSTEM. SYSTEM CHECKED OK. 2 L 7 3 4F A3WE 2001041100092 20010411 00092 NM 2001 4 11 UPS01435413 1 20010308 A 5210 65B135667 STOP FITTING BOEING 747 747121 1384871 NM PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - L1 DOOR FWD LOWER STOP FITTING CRACKED. STOP FITTING REPLACED AS PER SRM 51-10-01 P.8. 2 L 7 4 4F A20WE 2001041100093 20010411 00093 NM 2001 4 11 UPS01435414 1 20010308 A 3233 654U61343 FITTING BOEING 747 747121 1384871 NM RT MLG CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 TWO CRACKS REVEALED ON RT MLG ACTUATOR UPPER SUPPORT FITTING O/B LUG BORE BOTH BY APPROX. 1/8 INCH LO NG AS MARKED. SERVICEABLE SUPPORT FITTING REPLACED IAW SRM 51-10-01 P.8 AND BOEING SB 747-53-2298 FIG 3. 2 L 7 4 4F A20WE 2001041100094 20010411 00094 NM 2001 4 11 UPS01435415 1 20010309 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - BS 1007 S-3 RT STRINGER END FOUND CRACKED. STRINGER REPAIRED. 2 L 7 4 4F A20WE 2001041100095 20010411 00095 NM 2001 4 11 UPS01435416 1 20010311 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 M/D -BS 1352-1354 S18 RT, STRINGER END FOUND CRACK. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4 F OR WORK DETAIL. 2 L 7 4 4F A20WE 2001041100096 20010411 00096 NM 2001 4 11 UPS01435417 1 20010311 A 5320 SPLICE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 M/D - BS 1007 S1R , STRINGER END SPLICE FITTING FOUND CRACK. STRINGER END SPLICE FITTING REPLACED A S PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001041100097 20010411 00097 NM 2001 4 11 UPS01435418 1 20010311 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 M/D - BS 742 - 744 , S23 RT STRINGER END FOUND CRACK. STRINGER REPAIRED. 2 L 7 4 4F A20WE 2001041100098 20010411 00098 NM 2001 4 11 UPS01435420 1 20010311 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - M/D FLOORBEAM BS2220, RBL 57 UPPER CHORD CORRODED. FLOORBEAM REPAIRED AS PER SRM 53-10-01 FIG 1. BLEND OUT CORROSION. DEPTH 0.056 INCH , WIDTH 1 INCH , LENGTH 2 INCHES. 2 L 7 4 4F A20WE 2001041100099 20010411 00099 NM 2001 4 11 UPS01435421 1 20010311 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 FWD CARGO COMPT BS 800 LBL 40 FLOORBEAM UPPER SURFACE ANCHOR NUT ATTACH AREA FOUND CORRODED AS MARKED . FLOORBEAMS REPAIRED AS PER 51-40-04 FIG 2. BLENDED OUT CORROSION. DEPTH 0.030 INCH , WIDTH 1 INCH , LENGTH 2 INCHES. 2 L 7 4 4F A20WE 2001041100100 20010411 00100 NM 2001 4 11 UPS01435422 1 20010313 A 5210 STRUCTURE BOEING 747 747121 1384871 NM PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CRACK REVEALED ON R1 MAIN ENTRANCE DOOR LOWER CORNER BY APPROX. 1.5 INCH LONG AS MARKED. DOOR LWR CORNER REPAIRED AS PER SRM52-10-02 FIG 10. 2 L 7 4 4F A20WE 2001041100101 20010411 00101 NM 2001 4 11 UPS01435423 1 20010311 A 5347 SEAT TRACK BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 M/D - BS 2240 - 2280 LBL 11 SEAT FLANGE FOUND CHIPPED & CRACKED AS MARKED. SEAT TRACK REPAIRED AS P ER SRM 53-10-05 FIG 14. 2 L 7 4 4F A20WE 2001041100102 20010411 00102 NM 2001 4 11 UPS01435424 1 20010308 A 5210 DOUBLER BOEING 747 747121 1384871 NM PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - L1 DOOR LOWER HINGE DOUBLER FOUND CRACKED. DOUBLER REPLACED AS PER BOEING SB B747-52-2144 . 2 L 7 4 4F A20WE 2001041100103 20010411 00103 NM 2001 4 11 UPS01435425 1 20010309 A 5310 65B11751602 DOOR FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 M/D - R3 DR LOWER FWD CORNER REVEAL FOUND CRACKED. CORNER REVEAL REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001041100104 20010411 00104 NM 2001 4 11 TWAA0105001 1 20010319 A 3350 80741 LIGHT BOEING 767 7673Y0 NM CABIN MISSING A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 638TW 26205 THE EGRESS LIGHT WAS MISSING AT SEAT ROW 27-GH AND 34-AC. REPLACED MISSING LAMP ASSEMBLIES. CHECK-C 2-15-00. 2 L 7 2 4F RT A1NM 2001041100105 20010411 00105 NM 2001 4 11 TWAA0105002 1 20010318 A 3350 80741 LIGHT BOEING 767 7673Y0 NM CABIN MISSING A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 639TW 26208 THE EGRESS LIGHT WAS MISSING AT SEAT ROW 27-GH AND 34-AC. REPLACED THE LIGHT ASSEMBLIES. CHECK-C 2-10-00. 2 L 7 2 4F RT A1NM 2001041100106 20010411 00106 WP 2001 4 11 TWAA0105003 1 20010313 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 928TW 48012 DURING CHECK-C MAINT IN THE FWD CARGO COMPT, LONGERON 28L AT STA 294 WAS CORRODED. FABRICATED PARTS PER SRM 53-02. FIN ISHED REPAIR BY INSTALLING HI-LOKS PER SRM 53-02, FIG 18, SHEET 1 THRU 6. 2 L 7 2 4F A6WE 2001041100107 20010411 00107 WP 2001 4 11 TWAA0105004 1 20010312 A 5320 FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT FOUND FAIRING SUPPORT STRUCTURE BRACKET WAS CRACKED AT CENTER OF KEEL BEAM, STA 875. REPLACED CRAC KED TEE FITTING WITH NEW PER SPM 6-70-01, PAGE 3. 2 L 7 2 4F A6WE 2001041100108 20010411 00108 WP 2001 4 11 TWAA0105005 1 20010309 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT FOUND STATIC BURNS AT STA 61, 20 INCHES BELOW LONGERON 18R. CUT OUT AND INSTALLED DOUBLER REPAIR P ER SRM 53-04, PAGE 18. 2 L 7 2 4F A6WE 2001041100109 20010411 00109 NM 2001 4 11 UPS01435426 1 20010308 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - BS 920 S-24 RT TO S-25 RT FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 11. 2 L 7 4 4F A20WE 2001041100110 20010411 00110 NM 2001 4 11 UPS01435427 1 20010308 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - BS 920 S-25L FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 11. 2 L 7 4 4F A20WE 2001041100111 20010411 00111 NM 2001 4 11 UPS01435428 1 20010311 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 FWD CARGO COMPT STA 800 S45L TO S46L FRAME CHORD & WEB FOUND CORRODED. BS 800 STR 45L - 45R FRAME ATTACH LWR ''T'' CHORD AND WEB REPLACED AS PER SRM 5101 P.8. BLEND OUT CORROSION DEPTH 0.050 , WIDTH 1 INCH , LENGHT 2 INCHES. 2 L 7 4 4F A20WE 2001041100112 20010411 00112 NM 2001 4 11 UPS01435429 1 20010308 A 5347 SEAT TRACK BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - M/D FLOOR TIE DOWN TRACK (BS 1920-1940, LBL 97) CORRODED. SEAT TRACK REPLACED AS PER SRM 53- 10-05 FIG 1A. BLEND OUT CORROSION DEPTH 0.038 INCH , WIDTH 1 INCH , LENGTH 3 INCHES. 2 L 7 4 4F A20WE 2001041100113 20010411 00113 NM 2001 4 11 UPS01435430 1 20010308 A 5311 FRAME BOEING 747 747121 1384871 NM BULKHEAD CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CRACK REVEALED ON R/H BS 1000 BULKHEAD CHORD VERTICAL FLANGE AT LWR TENSION BOLT HOLE AT S-38 RT AREA BY APPROX. 0.050 INCH LONG AS MARKED. RT BS 1000 BULKHEAD CHORD VERTICAL FLANGE AT LWR TENSION BOLT HOLE CRACK CLEA RED. HFEC INSPECTED SATIS. NEW BOLT INSTALLED PER RS#R53-42-34640. 2 L 7 4 4F A20WE 2001041100114 20010411 00114 NM 2001 4 11 UPS01435431 1 20010309 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - BS 1007 S-3L STRINGER END FOUND CRACKED. STRINGER REPAIRED. 2 L 7 4 4F A20WE 2001041100115 20010411 00115 NM 2001 4 11 EISA20010012 1 20010202 A 5730 SKIN BOEING BOEING 727 727223 1384074 NM LT WING CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ROUTINE C-CHECK INSPECTION FOUND SKIN CRACKED ON LEFT WING ABOVE NR 4 SLAT. ROUTED OUT CRACK, FABRICATED REPAIR DOUBLER, PRIMED, ALODINED, AND INSTALLED DOUBLER IAW SRM 57-30-4, 51-10-2, 51-30-2. 2 L 7 3 4F A3WE 2001041100116 20010411 00116 NM 2001 4 11 EISA20010030 1 20010223 A 2782 U109592 ACTUATOR BOEING BOEING 727 727223 1384074 NM L/E SLAT MALFUNCTIONED A EISA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 07 6819 19494 ON DEPARTURE WHEN RETRACTING FLAPS FROM 5 TO 2 DEGREES NR 8 SLAT WAS STUCK, IN THE EXTEND POSITION. AMBER L/E FLAP LIGH T ILLUMINATED AND NR 8 SLAT ILLUMINATED. CYCLED AGAIN SLAT RETRACTED. REMOVED AND REPLACED NR 8 SLAT ACTUATOR PER M/M 27-80-00, OPS CHECK GOOD. 2 L 7 3 4F A3WE 2001041100117 20010411 00117 WP 2001 4 11 MWEA010338 1 20010315 A 5330 59114015N SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 BELLY SKIN FROM STATION 110-229 REQUIRED REMOVAL FOR OTHER MAINTENANCE AND FOUND CONDITION 3 BLENDOUT. REMOVED SKIN, FA BRICTED, LOCATED, DRILLED AND INSTALLED INTERNAL DOUBLER REPAIR. REINSTALLED SKIN. 2 L 7 2 4F A6WE 2001041100118 20010411 00118 SO 2001 4 11 COMA0110058 1 20010312 A 5720 12017064009 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 21213 120264 DURING 2C CHECK TASK 5720-561-01I, THE LT WING UPPER SKIN SUPPORT AT RIB 23, BETWEEN STRINGER 5A AND REAR SPAR, WAS FOUN D CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001041100119 20010411 00119 NM 2001 4 11 2001UALA00142 1 20010222 A 2432 GROUND WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BATTERY DAMAGED A UALA K NONE M OVER TEMP IN INSP/MAINT 1 WP 29 652UA 25390 APU BATTERY GROUND GD3072DC OVERHEATED. INSULATION BLANKETS HEAT DAMAGED. *S/D* ACCOMPLISHED DETAILED VISUAL INSPECTI ON OF ALL EFFECTED WIRE BUNDLES AND INSTALLATIONS LOCATED IN E6-1 SHELF AND P49 PANEL. ALL WIRING CHECKED OK, EXCEPT AP U BATTERY GROUND WIRE. REPLACED APU BATTERY GROUND BRACKET (P/N 287T0152-4), APU BATTERY GROUND WIRE W1048-007-1/0 AND GROUND GD3072DC HARDWARE. 2 L 7 2 4F 4 F RT A1NM E24NE 2001041100120 20010411 00120 NM 2001 4 11 2001UALA00190 1 20010304 A 5311 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 645UA 25280 AFT CARGO PIT AT BS 1197 +132 AT LBL 22-26, FRAME T-CAP IS CORRODED. REPLACED T-CAP PER BAC DWG 146T1060 AND INSTALLED PER SRM53-00-07, FIG 101. 2 L 7 2 4F 4 F RT A1NM E24NE 2001041100121 20010411 00121 NM 2001 4 11 2001UALA00201 1 20010307 A 2751 18196918 TRANSMITTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE T/E FLAP FAILED A UALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 29 510UA 24780 FLAP CONFIGURATION WARNING ON TAKEOFF. REJECTED TAKEOFF AT 95 KTS, FLAPS AT 15. *S/D* FAILED RIGHT TRAILING EDGE FLAP TRANSMITTER. REPLACED SAME AND OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041100122 20010411 00122 NM 2001 4 11 UPS01235274 1 20010216 A 2750 CONTROL VALVE BOEING 727 72722C 138400F NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C+SI, CORROSION ON T/E FLAP INPUT QUADRANT ABOVE FLAP CONTROL VALVE. REPAIR CARRIED OUT IAW MM 27-51-00 & MM 27-51-51. 2 L 7 3 4F A3WE 2001041100123 20010411 00123 NE 2001 4 11 SWIA972431 2 20010309 A 7321 EEC EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NR 2 ENGINE MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 271YV 120271 NUMBER TWO EEC DROPPED OFF LINE (AURAL WARNING, RED EEC LIGHT ILLUMINATED, MANUL LIGHT) DURING TAKEOFF. ABORTED TAKEOFF . NUMBER TWO NP REMAINED AT 80 PERCENT UNTIL EEC WAS TURNED OFF. DEFERRED PER MEL 73-21-1, MC 0179. INSPECTED, CLEANE D AND OHMED RIGHT ENGINE EEC SYSTEM. PERFORMED GROUND RUNS WITH NO DEFECTS NOTED. SYSTEM OPS NORMAL AT THIS TIME. PLA CARD REMOVED. 2 L 7 2 4T 4 T RT A31SO E20NE 2001041100124 20010411 00124 SO 2001 4 11 COMA0110060 1 20010312 A 5720 12017063009 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 21213 120264 DURING 2C CHECK TASK 5720-561-01I, THE LT WING UPPER SKIN SUPPORT AT RIB 23, BETWEEN STRINGERS 3A AND 4A, WAS FOUND CRAC KED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001041100125 20010411 00125 WP 2001 4 11 UPS01835298 1 20010318 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSLEAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE: PREFLT. PREVIOUS REPAIR BENT AND CRACKED AT STA 1580 LT 2 INCHES ABOVE FLOOR (FUSELAGE FRAME.) SUPPL EMENTAL: REMOVED DAMAGED REPAIR FABRICATED REPAIR DOUBLER AND INSTALLED DOUBLER PER E.O. DC8 5310 13993 2 L 7 4 4F RT 4A25 2001041100126 20010411 00126 NM 2001 4 11 UPS01235481 1 20010401 A 2611 SMOKE DETECTOR BOEING 727 72725C 138400H NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 MAIN CABIN SMOKE DETECTOR FAILED TO TEST. RELAMPED AND DISPATCHED AIRCRAFT 2 L 7 3 4F A3WE 2001041100127 20010411 00127 NM 2001 4 11 UPS01435465 1 20010329 A 5610 WINDOW BOEING 747 747123F NM COCKPIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE: PREFLT, R-1 WINDOW OUTER PANE CRACKED & SPIDER-WEBBED. INSTALLED WINDOW IN R1 POSITION IAW MM 56-10 2 L 7 4 4F A20WE 2001041100128 20010411 00128 NM 2001 4 11 UPS01635482 1 20010401 A 3610 PRIORITY VALVE BOEING 767 767300 1385204 NM LT ENGINE INOPERATIVE A IPXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 322UP 27748 ETOP DIVERSION - LT ENGINE PRV EICAS MSG AND ANN LT ON ICE IN PHL DIVERTED TO SDF. REMOVED AND REPLACED PRV CONTROLLER IAW MM 36-11-19 2 L 7 2 4F RT A1NM 2001041100129 20010411 00129 NM 2001 4 11 UPS01435432 1 20010309 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - BS 1007 S-2L STRINGER END FOUND CRACKED. STRINGER END REPAIRED. 2 L 7 4 4F A20WE 2001041100130 20010411 00130 NM 2001 4 11 UPS01435433 1 20010309 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - BS 1007 S-5L STRINGER END FOUND CRACKED. STRINGER END REPAIRED. 2 L 7 4 4F A20WE 2001041100131 20010411 00131 NM 2001 4 11 UPS01435434 1 20010308 A 5320 65B169522 FITTING BOEING 747 747121 1384871 NM BULKHEAD CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CRACKS REVEALED ON RT BS 1000 BULKHEAD ATTACHED BATH TUB FITTING AT SEVERAL FASTENER HOLES AS MARKED. RT BS 1000 BULKHEAD ATTACH BATH TUB FTG REPLACED AS PER SRM 51-10-01 P.8. 2 L 7 4 4F A20WE 2001041100132 20010411 00132 NM 2001 4 11 UPS01435435 1 20010308 A 5320 65B169521 FITTING BOEING 747 747121 1384871 NM BULKHEAD CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CRACKS REVEALED ON LT BS 1000 BULKHEAD ATTACHED BATH TUB FITTING AT SEVERAL FASTENER HOLE LOCATIONS A S MARKED. LT BS 1000 BULKHEAD ATTACH BATH TUB FTG REPLACED AS PER SRM 51-10-01 P.8. 2 L 7 4 4F A20WE 2001041100133 20010411 00133 NM 2001 4 11 UPS01435436 1 20010312 A 5320 65B381743 FITTING BOEING 747 747121 1384871 NM FUSLEAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CRACKS REVEALED ON AFT CARGO DOOR ROTARY ACTUATOR ATTACH FITTING AT BS 1820 AND 1900 AS PER ATTACHED FIGURE. REFER EO 747-5320-12180-A, AREA DEFECT RECTIFICATION CUTOUT. 2 L 7 4 4F A20WE 2001041100134 20010411 00134 NM 2001 4 11 UPS01435438 1 20010310 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 FWD CARGO COMPT BILGE AREA SKIN FOUND CORRODED AT FS 976-980 S45R- 46R AREA. FX SKIN REPAIRED AS P ER SRM 53-30-03 FIG 1. 2 L 7 4 4F A20WE 2001041100135 20010411 00135 NM 2001 4 11 UPS01435439 1 20010326 A 5320 FLOOR SUPPORT BOEING 747 747123F NM E/E BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C LOWER NOSE AREA E&E. LONGITUDINAL FLOOR SUPPORT TEE SECTION CRACKED AT BS410 LBL20 TEE SECTION RE PLACED IAW SRM 51-30-02 2 L 7 4 4F A20WE 2001041100136 20010411 00136 NM 2001 4 11 UPS01435443 1 20010313 A 5510 BRACKET BOEING 747 747123F NM HORIZONTAL STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C TAIL. CRACK IN ANGLE BRACKET ON RT HORIZONTAL STAB REAR SPAR AT STAB STA . 580 NEW BRACKET FABRICA TED AND FITTED IAW SRM 51-30-02 2 L 7 4 4F A20WE 2001041100137 20010411 00137 WP 2001 4 11 UPS01835405 1 20010306 A 5320 ATTACH ANGLE DOUG DC8 DC873F 302199F WP MLG DOOR HINGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C2, KEELBEAM AREA BETWEEN MLG DOORS STA 830, LT ATTACH ANGLE CRACKED. FABED AND INSTALLED NEW ATTACH ANGLE IAW DAC DWG 4645535 AND DC8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001041100138 20010411 00138 WP 2001 4 11 UPS01835408 1 20010311 A 5321 FLOORBOARD DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C2 FLOORBOARD STA 1040 BETWEEN RAILS E & F CORRODED REPAIRED AREA IAW DC8 SRM 53-2-3 2 L 7 4 4F RT 4A25 2001041100139 20010411 00139 WP 2001 4 11 UPS01835411 1 20010309 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE: C2, MAIN CABIN STA 880 PRESSURE DECK FLOORBEAM ON TRACK G RBL 65 IS OUT OF LI MITS AND HAS BARE METAL. REPAIRED AREA IAW TSRM STD-5310-001 2 L 7 4 4F RT 4A25 2001041100140 20010411 00140 WP 2001 4 11 UPS01835412 1 20010306 A 5320 FITTING DOUG DC8 DC873F 302199F WP LT MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C2 LT MLG WW CRACKED IN VERT LEG OF TRAPEZOIDAL FITTING FS 902 LONG 24 LT. STOP DRILLED CRACK IAW UP S EO DC8-5340-0748 2B CRACK CONDITION REPAI R PREVIOUSLYCOMPLIED WITH IAW UPS EO DC8-5340-0748 NO FURTHER ACTION REQUIR ED AT THIS TIME 2 L 7 4 4F RT 4A25 2001041100142 20010411 00142 WP 2001 4 11 UPS01835448 1 20010323 A 5220 STOP FITTING DOUG DC8 DC873F 302199F WP EMERGENCY EXIT MISSING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:PFLT BOTH OVERWING EXIT DOORS MISSING STOP FITTING ASSY/WILL NOT LATCH RESEATED IN SILL AND LATCHED INTO PLACE. M/M 52-20-00 2 L 7 4 4F RT 4A25 2001041100143 20010411 00143 WP 2001 4 11 UPS01835449 1 20010326 A 3350 LIGHT DOUG DC8 DC871F 302199D WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:PREFLT, BOTH COCKPIT & ENTRY DOOR EMERGENCY LIGHTS INOP REMOVED & REPLACED EMERGENCY BATTERY & REL AY UNIT. OPS CHECK GOOD. OK FOR SERVICE. 2 L 7 4 4F RT 4A25 2001041100144 20010411 00144 WP 2001 4 11 TWAA0105204 1 20010320 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT IN AFT CABIN FOUND CORROSION ON CHAIR TRACK AT SEVERAL PLACES, STA 1003 TO 1146. INSTALLED NEW TRA CK PER INSTALLATION PRINT 5930566. TREATED AREA WITH ALODINE AND PRIMER PER SRM 51-10-3, PAGE 16 AND 18. 2 L 7 2 4F A6WE 2001041100147 20010411 00147 WP 2001 4 11 TWAA0104908 1 20010314 A 5313 LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 992Z 47095 DURING OP 15 MAINT CHECK FOUND LONGERONS 17R, 12R, AND 16R WERE CRACKED AT STA 965. SPLICED IN NEW LONGERON FROM STA 96 5 TO 996 PER SRM 53-02, FIG 18. 2 L 7 2 4F A6WE 2001041100148 20010411 00148 NM 2001 4 11 HNAA0100019 1 20010315 A 7921 28E997 OIL COOLER DHAV DHC8 DHC8102 2809003 NM NR 2 ENGINE LEAKING A HNAA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 07 934HA 15350 201 139 NR 2 ENGINE LOST OIL PRESSURE. SHUT DOWN ENGINE IN FLIGHT AND RETURNED TO PHL. REMOVED AND REPLACED NR 2 OIL COOLER. 2 H 7 2 4T RT A13NM 2001041100149 20010411 00149 NM 2001 4 11 MWEA010366 1 20010322 A 3310 102ADP31 PANEL DOUG MD88 MD88 3023688 NM COCKPIT INOPERATIVE A MWEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 31 601ME 49762 ON TAKE OFF ROLL THE CABIN ALTITUDE AND MASTER WARNING ILLUMINATED AND CIRCUIT BREAKER T-36 POPPED. TROUBLESHOT TO OVE RHEAD ANNUNCIATOR PANEL. REMOVED AND REPLACED PANEL. 2 L 7 2 4F RT A6WE 2001041100150 20010411 00150 WP 2001 4 11 USAAD01036 1 20010220 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC981 3022081 WP PAX CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 802US 48036 EWR - FOUND SEVERAL CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED THE POWER SUPPLY AT SEAT 25. (M) 2 L 7 2 4F A6WE 2001041100151 20010411 00151 WP 2001 4 11 USAAD01037 1 20010220 A 3350 AD4002P BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 806US 48038 IND - THE CEILING EMERGENCY LIGHTS BETWEEN THE AFT LAVATORIES WERE INOPERATIVE. REPLACED BATTERIES AT B5-27 IN THE RIGH T LAVATORY CEILING. (M) 2 L 7 2 4F A6WE 2001041100152 20010411 00152 WP 2001 4 11 USAAD01038 1 20010221 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP PAX CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 824US 49143 TPA - THE FORWARD ENTRY ENTRY LIGHT WAS INOPERATIVE. REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F A6WE 2001041100153 20010411 00153 WP 2001 4 11 USAAD01032 1 20010217 A 3350 LIGHT DOUG DC9 DC981 3022081 WP ROW 20, 30, & 25 OUT OF POSITION A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 807US 48039 MCO - THE EMERGENCY LIGHTS AT ROWS 30, 25, AND 20 WERE FOUND TO BE OUT OF POSITION. THE LIGHTS WERE PLACED INTO THEIR C ORRECT POSITIONS. (M) 2 L 7 2 4F A6WE 2001041100154 20010411 00154 WP 2001 4 11 USAAD01035 1 20010220 A 3350 LIGHT DOUG DC9 DC981 3022081 WP CABIN MISINSTALLED A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 826US 48026 PIT - THE EMERGENCY LIGHTS AT ROWS 19, 24, AND 29 WERE INSTALLED AT THE WRONG POSITIONS. INSTALLED THE LIGHT ASSEMBLIES INTO THE CORRECT POSITIONS. (M) 2 L 7 2 4F A6WE 2001041100155 20010411 00155 WP 2001 4 11 ASAA0180087 1 20010223 A 3350 0105606003 LIGHT DOUG DC9 DC982 3022082 WP ROW 11 DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 967AS 49103 PHX - DURING PREFLIGHT CHECK, FOUND TWO EMERGENCY FLOOR TRACK LIGHTS DAMAGED AT ROW 11. REPLACED LIGHT ASSEMBLY AT ROW 11. TRACK LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001041100156 20010411 00156 NM 2001 4 11 ASAA0110099 1 20010219 A 3350 86210144 BATTERY BOEING 737 737290C 138448V NM MID CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING MAINTENANCE CHECK, FOUND EXIT LIGHTS AT ROWS 2, 3, 12, 14 AND 18 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY ON ROWS 2, 3, 12, 14, AND 18, AND REMOTE ASSEMBLY RECEIVER ON ROWS 2 AND 3 THEN LIGHTS OPERATED NORMALL Y. (M) 2 L 7 2 4F A16WE 2001041100157 20010411 00157 NM 2001 4 11 20010410AP030 1 20010219 A 3350 883200312 RECEIVER BOEING 737 737290C 138448V NM MID CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING MAINTENANCE CHECK, FOUND EXIT LIGHTS AT ROWS 2, 3, 12, 14 AND 18 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY ON ROWS 2, 3, 12, 14, AND 18, AND REMOTE ASSEMBLY RECEIVER ON ROWS 2 AND 3 THEN LIGHTS OPERATED NORMALL Y. REF ASAA0110099. (M) 2 L 7 2 4F A16WE 2001041100158 20010411 00158 WP 2001 4 11 ASAA0180088 1 20010226 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 13 TO 16. REPAIRED BROKEN WIRES AND TRAC K COVERS. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001041100159 20010411 00159 WP 2001 4 11 ASAA0180076 1 20010217 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 973AS 53449 SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS IN AFT PAX CABIN INOPERATIVE. REPAIRED WIRING. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001041100160 20010411 00160 WP 2001 4 11 ASAA0180086 1 20010223 A 3350 0105606005 LIGHT DOUG DC9 DC982 3022082 WP CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 934AS 49235 SEA - DURING PREFLIGHT CHECK, FOUND TWO EMERGENCY FLORO TRACK LIGHTS DAMAGED/MISSING AT ROWS 22. REPLACED LIGHT ASSEMBL IES AT ROW 22. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 2001041100161 20010411 00161 NM 2001 4 11 ASAA011079 1 20010209 A 5330 SKIN BOEING 737 737290C 138448V NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND PLUGGED HOLE ON SKIN PANEL AT BODY STATION 767, STRINGER 4L. REPAIRED PER PER. ( M) 2 L 7 2 4F A16WE 2001041100162 20010411 00162 NM 2001 4 11 UPS01235398 1 20010219 A 7160 DUCT BOEING 727 72730C 1384009 NM NR 2 ENGINE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:C CHECK NR 2 ENGINE INLET S DUCT INNER SKIN HAS CIRCUMFERENTIAL CRACKS 2 EA APPX 100-104 INCH FROM AFT EDGE. 1 EA 7 INCH Y SHAPED CRACK & 1 EA 1.5 INCH CRACK APPX 4 OCLOCK. CUT OUT DAMAGED AREA. INSTALLED REPAIR. HEAT TREA TED. 2 L 7 3 4F A3WE 2001041100163 20010411 00163 NM 2001 4 11 UPS01235399 1 20010219 A 7160 DUCT BOEING 727 72730C 1384009 NM NR 2 ENGINE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:C CHECK NR 2 ENGINE INLET S DUCT INNER SKIN HAS CIRCUMFERENTIAL CRACKS. 1 EA 4 INCH CRACK 93 INCHES FRO M AFT EDGE 4 OCLOCK. CUT OUT DAMAGED AREA. INSTALLED REPAIR. 2 L 7 3 4F A3WE 2001041100164 20010411 00164 NM 2001 4 11 UPS01235400 1 20010215 A 5311 FRAME BOEING 727 72730C 1384009 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:C CHECK LT W/W LWR SECTION OF BS 930 FRAME SHOWS CRACK TO AFT CENTER SECTION WHERE REPAIR NOT INSTALLED. ACCOMPLISHED STA 930 RT & LT FRAME REMOVAL & REPLACEMENT. 2 L 7 3 4F A3WE 2001041100165 20010411 00165 NM 2001 4 11 UPS01235402 1 20010226 A 5740 FITTING BOEING 727 72730C 1384009 NM L WING SPAR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:C CHECK LT WING FRONT SPAR INTERIOR & LBBL 70.5 TERMINAL FITTING ATTACH V SHAPE FITTING TO UPPER SHOW CR ACK MIGRATING FROM OB BOLT. REMOVED FITTING LT WING FRONT SPAR INTERIOR LBL 70.5 V SHAPE. INSTALLED LT WING UPPER FRON T SPAR CONER NEW FITTING & TORQUE BOLTS. 2 L 7 3 4F A3WE 2001041100166 20010411 00166 NM 2001 4 11 UPS01235403 1 20010323 A 5270 TERMINAL BOEING 727 7272A1 138407F NM CARGO DOOR DAMAGED A IPXA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 01 214UP 21342 AMBER MAIN CARGO DOOR LIGHT ILLUMINATED IN FLIGHT. FOLLOWED PROCEDURES PER AOM CH 2. DIVERTED FLIGHT TO FWA. DEFERED P ER MEL 52-4 AND COMPLIED WITH DMP VERIFYING THAT MAIN CARGO DOOR CLOSED AND LOCKED PRIOR TO DEPARTURE. ITEM DEFERRED M21 1761 PLACARD INSTLD T/S FOUND 1 EA BROKEN WIRE TERMINAL ON SWITCH S909 REPLACED WIRE TERMINAL AS REQUIRED. PRESSURIZED A /C AND OPS CHECKED CARGO DOOR SYSTEM IAW M/M 55-34-00. OPS CHECKED GOOD. CLEARED DEF LP 492291 2 L 7 3 4F A3WE 2001041100167 20010411 00167 NM 2001 4 11 UPS01435352 1 20010307 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - ABOVE MAIN DECK FLOOR BS 2320 LT FRAME (WL 20004) INNER FRAME CRACKED. FRAME REPAIRED AS PER SRM 51-40-03 FIG 1. 2 L 7 4 4F A20WE 2001041100168 20010411 00168 NM 2001 4 11 UPS01435353 1 20010307 A 5320 BRACKET BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - MAIN DECK LONG. FLOOR SUPPORT BRACKET CRACKED. BRACKET REPLACED 2 L 7 4 4F A20WE 2001041100169 20010411 00169 NM 2001 4 11 UPS01435354 1 20010308 A 5320 FLOOR SUPPORT BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - MAIN DECK LT O/B FLOOR SUPPORT (BS2320-2342, LBL 66-70) CORRODED. FLOOR SUPPORT REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001041100170 20010411 00170 NM 2001 4 11 UPS01435355 1 20010308 A 5210 65B135668 FITTING BOEING 747 747121 1384871 NM PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - R1 DOOR FWD LOWER STOP FITTING FOUND CRACKED. STOP FITTING REPLACED AS PER SRM 51-10-01 P .8. 2 L 7 4 4F A20WE 2001041100171 20010411 00171 NM 2001 4 11 UPS01435356 1 20010308 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - BS 560 S-24L FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 11. 2 L 7 4 4F A20WE 2001041100172 20010411 00172 NM 2001 4 11 UPS01435357 1 20010308 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - BS 740 S-23R STRINGER END FOUND CRACKED. STRINGER REPAIRED. 2 L 7 4 4F A20WE 2001041100173 20010411 00173 NM 2001 4 11 UPS01435358 1 20010308 A 5240 INTERCOSTAL BOEING 747 747121 1384871 NM SERVICE DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - R4 DOOR UPPER CENTER INTERCOSTAL WEB FOUND CRACKED, DOOR INTERCOSTAL WEB REPAIRED AS PER SRM 51-40-03 FIG 1. 2 L 7 4 4F A20WE 2001041100174 20010411 00174 NM 2001 4 11 UPS01435360 1 20010308 A 5347 SEAT TRACK BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 M/D - BS 320-340 RBL 11 SEAT TRACK FLANGE FOUND CORRODED. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2001041100175 20010411 00175 NM 2001 4 11 UPS01435362 1 20010308 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - BS 900 S-25L FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 4. 2 L 7 4 4F A20WE 2001041100176 20010411 00176 NM 2001 4 11 UPS01435363 1 20010308 A 5240 DOOR FRAME BOEING 747 747121 1384871 NM SERVICE DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - L4 DOOR FWD FRAME LOWER CORNER FOUND CRACKED. L4 DOOR FWD FRAME LOWER CORNER REPAIRED AS PER SRM 52-10-02 FIG 10. 2 L 7 4 4F A20WE 2001041100177 20010411 00177 NM 2001 4 11 UPS01435364 1 20010308 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - BS 980 S-25R FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG.11. 2 L 7 4 4F A20WE 2001041100178 20010411 00178 NM 2001 4 11 UPS01435365 1 20010308 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - BS 960 S-25R FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG.11. 2 L 7 4 4F A20WE 2001041100179 20010411 00179 NM 2001 4 11 UPS01435366 1 20010308 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - BS 940 S-24R TO S-25R FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG.11. 2 L 7 4 4F A20WE 2001041100180 20010411 00180 NM 2001 4 11 UPS01435367 1 20010309 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - BS 987 S-15R STRINGER END FOUND CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4. 2 L 7 4 4F A20WE 2001041100181 20010411 00181 NM 2001 4 11 UPS01435368 1 20010309 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - BS987 S-15L STRINGER END FOUND CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4. 2 L 7 4 4F A20WE 2001041100182 20010411 00182 NM 2001 4 11 UPS01435369 1 20010309 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - BS1007 S-1L STRINGER END FOUND CRACKED. STRINGER END ANGLE REPAIRED. 2 L 7 4 4F A20WE 2001041100183 20010411 00183 NM 2001 4 11 UPS01435370 1 20010309 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - BS1007 S-5R STRINGER END FOUND CRACKED. STRINGER REPAIRED. 2 L 7 4 4F A20WE 2001041100184 20010411 00184 NM 2001 4 11 UPS01435371 1 20010309 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - BS1007 S-1R STRINGER END FOUND CRACKED. STRINGER REPAIRED. 2 L 7 4 4F A20WE 2001041100185 20010411 00185 NM 2001 4 11 UPS01435372 1 20010309 A 5320 TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - BS 780 LT TENSION TIE FOUND CRACKED. TENSION TIE REPAIRED AS PER EO B747-5310-5890 FIG.2. 2 L 7 4 4F A20WE 2001041100186 20010411 00186 NM 2001 4 11 UPS01235476 1 20010323 A 5320 WEB BOEING 727 7272A1 138407F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 213UP 21341 INSPECTION TYPE: C, TWO CRACKS AND ONE MISSING FASTENER ON UPPER FLANGE OF WEB BETWEEN BS 400 AND BS 420, WL 206, BL 0. REMOVED WEB AND L ANGLE FABRICATED NEW WEB AND L ANGLE AND INSTALLED IAW SRM 51-10-3, 51-20-1, 51-20-2 AND 51-20-15 2 L 7 3 4F A3WE 2001041100188 20010411 00188 NM 2001 4 11 UPS01435514 1 20010308 A 5311 FRAME BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, RT WING MLG WW. CORROSION ON 1265 FRAME OUTER CHORD AT THE OVER WING LONGERON OUTER CHORD. 2 L 7 4 4F A20WE 2001041100189 20010411 00189 NM 2001 4 11 UPS01435515 1 20010307 A 5330 SKIN BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, MAIN DECK. CORROSION ON EXTERIOR SURFACE OF WING CENTER SECTION UPPER SKIN AT BS 1080 LBL.92 SKI N REPAIRED IAW QUERY NOTE 12/01 2 L 7 4 4F A20WE 2001041100190 20010411 00190 NM 2001 4 11 UPS01435516 1 20010307 A 5330 SKIN BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, MAIN DECK. CORROSION ON EXTERIOR SURFACE OF WING CENTER SECTION UPPER SKIN AT BS 1100 LBL 92. SKIN REPAIRED IN ACCORDANCE WITH QUERY NOTE 12/01 2 L 7 4 4F A20WE 2001041100191 20010411 00191 NM 2001 4 11 UPS01435517 1 20010306 A 5330 SKIN BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, MAIN DECK. CORROSION ON UPPER SURFACE OF CENTER WING AT BS 1140 RBL 45. SKIN REPAIRED IAW QUERY NOTE 12/01 2 L 7 4 4F A20WE 2001041100192 20010411 00192 NM 2001 4 11 UPS01435518 1 20010312 A 5330 SKIN BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, MAIN DECK. CORROSION ON EXTERIOR SURFACE OF WING CENTER SECTION UPPER SKIN AT BS 1140 RBL 58. SK IN REPAIRED IAW QUERY NOTE 12/01 2 L 7 4 4F A20WE 2001041100193 20010411 00193 NM 2001 4 11 UPS01435519 1 20010309 A 5330 SKIN BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, MAIN DECK CORROSION ON EXTERIOR SURFACE OF WING CENTER SECTION UPPER SKIN AT BS 1009 LBL 88. SKIN REPAIRED IAW QUERY NOTE 12/01 2 L 7 4 4F A20WE 2001041100194 20010411 00194 NM 2001 4 11 UPS01435520 1 20010320 A 5311 FRAME BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, AFT CARGO HOLD. CORROSION ON FRAME WEB AT BS 1940 AT STR. 43 LT. FRAME WEB REPAIRED IAW Q/NOTE 24/ 01 2 L 7 4 4F A20WE 2001041100195 20010411 00195 NM 2001 4 11 UPS01435521 1 20010307 A 5330 SKIN BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, MAIN DECK. CORROSION ON UPPER SURFACE OF CENTER WING SKIN AT BS 1241 RBL 25. CORROSION REWORKED I AW Q/NOTE 12/01 2 L 7 4 4F A20WE 2001041100196 20010411 00196 NM 2001 4 11 UPS01435522 1 20010320 A 5311 FRAME BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, FWD CARGO HOLD. FUSELAGE FRAME CRACKED AT BS 960 STR 31 RT. FRAME REPAIRED IAW QUERY NOTE 21/01 2 L 7 4 4F A20WE 2001041100197 20010411 00197 NM 2001 4 11 UPS01435523 1 20010320 A 5311 FRAME BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, FWD CARGO HOLD. CRACKING DUE TO CORROSION BULGE ON WEB OF FUSLAGE FRAME BS 680 ST 39-40 LT. FRAM E WEB REPAIRED IAW QUERY NOTE 21/01 2 L 7 4 4F A20WE 2001041100198 20010411 00198 NM 2001 4 11 UPS01435524 1 20010408 A 2611 SMOKE DETECTOR BOEING 747 747123F NM FWD CARGO HOLD FALSE ACTIVATION A IPXA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 673UP 20325 BTB-FWD CARGO COMPARTMENT SMOKE DET WARNING LIGHT ILLUMINATED. AWAITING LOG PAGE DEFERRED PER MEL 2 L 7 4 4F A20WE 2001041100199 20010411 00199 NM 2001 4 11 UPS01535538 1 20010407 A 3350 402112 GUARD BOEING 757 75724APF 1384969 NM LIGHT SWITCH INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 433UP 25464 EMERGENCY EXIT LIGHT SWITCH GUARD WILL NOT OPERATE PROPERLY. LIGHT SWITCH MUST BE POSITIONED MANUALLY REPLACED SWIT CH GUARD, OP CHECK OK 2 L 7 2 4F RT A2NM 2001041100200 20010411 00200 NM 2001 4 11 UPS01235327 1 20010321 A 3510 OXYGEN MASK BOEING 727 72730C 1384009 NM COCKPIT FAILED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 917UP 19310 D-SECOND OBSEVERS. O2 MASK INOP M-211583. R & R 02 MASK & CLEANED AUDIO JACK. CHECKS GOOD THIS CLEARS DFRL. 2 L 7 3 4F A3WE 2001041100201 20010411 00201 NM 2001 4 11 UPS01235331 1 20010319 A 3510 LINE BOEING 727 72725C 138400H NM CREW OXYGEN SYS LEAKING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:B REF L/P 640094 ITEM NR 1 FOUND OXY LEAKING AT OXY DISTRIBUTION TUBE B-NUT CONNECTED TO PRESSURE TRANSD UCER AND TO THE OTHER END B-NUT CONNECTED TO THE FOUR WAY FITTING. BAD LINE REMOVED, 02 TURNED OFF AT BOTTLE. REMOVED AND REPLACED 02 LINE (P/N 65-20901-88) IAW STANDARD PRACTICES. LEAK CHECKS GOOD. 2 L 7 3 4F A3WE 2001041100202 20010411 00202 NM 2001 4 11 UPS01435326 1 20010321 A 2612 FIRE DETECTOR BOEING 747 747200B NM NR 4 ENGINE MALFUNCTIONED A IPXA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SO 01 522UP 21936 INSPECTION TYPE:N/A NR 4 ENGINE FIRE DETECTION LIGHT ILLUMINATED REMOVED AND REPLACED NR 4 ENGINE UPPER AFT TEST DEC TECTOR ASSY. I.A.W. MMNL 26-11-00. OPERATIONAL CHK SYSTEM NORMAL. 1 L 7 4 4F RT A20WE 2001041100203 20010411 00203 WP 2001 4 11 TWAA0105104 1 20010316 A 5754 SKIN DOUG DC9 DC982 3022082 WP SLAT DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 909TW 49170 DURING CHECK-C MAINT ON LT WING MIDDLE OF NUMBER 4 SLAT HAD DENT FILLED WITH FILLER, 6 IN BY 4 IN. CLEANED AREA OF FILL ER AND ACCOMP NDT CHECK FOR CRACKS. NO CRACKS FOUND. REFILLED AREA PER SRM 57-03 FIG 14B, SHEET 2. ALSO SRM 57-40-102 PAGE 201 FOR APPROVED FILLER. 2 L 7 2 4F A6WE 2001041100204 20010411 00204 WP 2001 4 11 TWAA0105102 1 20010316 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT FOUND FLOOR SUPPORT CORRODED AT STA 160 TO 200, RBL 44. REPLACED FLOOR SUPPORT PER SPM 6-70-01 AND SRM 51-30-2. 2 L 7 2 4F A6WE 2001041100205 20010411 00205 WP 2001 4 11 TWAA0105103 1 20010319 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT FOUND FLOOR SUPPORT CORRODED AND BROKEN AT STA 180, RBL 9 IN TO RBL 44 INCHES. INSTALLED NEW FLOOR SUPPORT PER SPM 6-70-01 AND SRM 51-30. 2 L 7 2 4F A6WE 2001041100206 20010411 00206 NE 2001 4 11 TWAA0105101 2 20010319 A 7260 B4902 CHIP DETECTOR BOEING 767 767330 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE DETACHED A TWAA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 05 691LF 25137 4701 THE NUMBER 1 ENGINE EXPERIENCED AN OIL QUANTITY AND PRESSURE LOSS. ENGINE WAS SHUT DOWN AND FLIGHT LANDED AT IAD. THE CHIP DETECTOR FOR THE 1, 1.5, AND 2 BEARINGS WAS FOUND LAYING IN THE COWLING. THE ANGLE GEARBOX CHIP DETECTOR WAS NOT L OCKED IN PLACE. INSTALLED BOTH CHIP DETECTORS, SERVICED OIL, AND CHECKED THE MAIN OIL SCREEN. THE CHIP DETECTOR HOUSIN GS WERE LATER REPLACED. CHECK-C 9-23-00 LAX. 2 L 7 2 4F 4 F RT A1NM E24NE 2001041100207 20010411 00207 WP 2001 4 11 AALA20010208 1 20010125 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE TORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 TUL - FOUND CUSP TORN AROUND NUTPLATE AT 1307. FABRICATED AND INSTALLED FILLER PER ESO 80559 DATED 1/23/2001. (M) 2 L 7 2 4F A6WE 2001041100208 20010411 00208 WP 2001 4 11 AALA20010209 1 20010119 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 TUL - FOUND CORROSION ON LEFT CUSP, STATION 927-946. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER BETWEEN STATION 938-942 PER AARD 53-00-00-00. (M) 2 L 7 2 4F A6WE 2001041100209 20010411 00209 WP 2001 4 11 AALA20010210 1 20010119 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 TUL - FOUND CORROSION ON LEFT CUSP, STATION 636-655, UPPER SURFACE. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53 -00-00-02. (M) 2 L 7 2 4F A6WE 2001041100210 20010411 00210 WP 2001 4 11 AALA20010211 1 20010119 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 TUL - FOUND CORROSION ON LEFT CUSP, STATION 946-965. CUT OUT AND BLENDED DAMAGED AREA. INSTALLED DOUBLER, STATION 956- 962 PER AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 2001041100211 20010411 00211 WP 2001 4 11 AALA20010212 1 20010119 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 TUL - FOUND NR 1 SEAT TRACK, BROKEN AND CRACKED AT STATION 313. INSTALLED 1 NEW SEAT TRACK PLUG PER AARD 53-20-00-10. (M) 2 L 7 2 4F A6WE 2001041100212 20010411 00212 WP 2001 4 11 AALA20010213 1 20010118 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 TUL - FOUND SEAT TRACK NR 6 HAS CORROSION AT STATION 274-275. INSTALLED NEW SEAT TRACK PLUG PER AARD 53-20-00-10. (M) 2 L 7 2 4F A6WE 2001041100213 20010411 00213 WP 2001 4 11 AALA20010214 1 20010118 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSLEAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 TUL - FOUND SEAT TRACK NR 6 HAS CORROSION AT STATION 597-580. INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10. (M) 2 L 7 2 4F A6WE 2001041100214 20010411 00214 WP 2001 4 11 AALA20010215 1 20010123 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE TOOL DAMAGE A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 21 498AA 49736 TUL - FOUND DEEP TOOLING MARKS IN LONGERON 11L TOP SIDE STATION 456 AND 461. INSTALLED DOUBLER PER SRM 53-02 AND SRM 51 -10-1. (M) 2 L 7 2 4F A6WE 2001041100215 20010411 00215 NM 2001 4 11 01FDEA00187 1 20010314 A 2612 FIRE DETECTOR BOEING 727 727233 138408A NM APU CONTAMINATED A FDEA K NONE N FALSE WARNING CR CRUISE 1 SO 25 268FE 21674 DURING FLT (APU OFF) RED FIRE LIGHT IN APU FIRE HANDLE CAME ON. UPON ENTRY INTO E&E COMP. FOUND AREA EXTREMELY WET. R EMOVED APU FIRE DET OPS PWR UNIT, CLEANED AND DRIED AND REINSTALLED. TEST SYS ALL CK GOOD. NO LIGHTS CAME ON REF B727- 200 WDM. 2 L 7 3 4F RT A3WE 2001041100216 20010411 00216 NM 2001 4 11 UPS01435450 1 20010326 A 5512 SKIN BOEING 747 747259B NM HORIZONTAL STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 527UP 21730 INSPECTION TYPE:C, LEFT HORIZONTAL STAB L/E. IS CRACKED AT L/E. STA. 360 REPAIRED SKIN I.A.W. SRM. 55-10-03 FIG. 1 2 L 7 4 4F RT A20WE 2001041100217 20010411 00217 NM 2001 4 11 UPS01435451 1 20010311 A 5310 SHEAR TIE BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 FWD CARGO COMPT STA 820 STR 45L AND 46L SHEAR TIE CORRODED. DOME NUT PLATE REPLACED AS PER SRM 51-1 0-01 P.8. 2 L 7 4 4F A20WE 2001041100218 20010411 00218 NM 2001 4 11 UPS01435452 1 20010310 A 5310 SHEAR TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 M/D - BS 1220, STR 10R - 11R, FRAME ATTACH SHEAR TIE FOUND CRACK. SHEAR TIE ANGLE REPLACED AS P ER ARM 51-10-01 P.8 AND 51-30-02. 2 L 7 4 4F A20WE 2001041100219 20010411 00219 NM 2001 4 11 UPS01435453 1 20010308 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 AFT CARGO COMPT - FRAME ATTACH SKIN EDGE FOUND CRACKED AT RH STA 1520 STR 28R. THE SUBJECT FRAME PRE VIOUS REPAIRED AS PER SRM 53-10-04 FIG 39 & CONFIRM NO CRACK BEYOND FASTENER HOLE BY NDT. 2 L 7 4 4F A20WE 2001041100220 20010411 00220 NM 2001 4 11 UPS01435455 1 20010309 A 5320 ANGLE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 BODY CREASE BEAM STRUCTURE - FRAME ATTACH FWD ANGLE BEND RADIUS FOUND CRACKED AT BS 960 STRINGER 7L A S MARKED. ANGLE REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001041100221 20010411 00221 WP 2001 4 11 UPS01835456 1 20010327 A 3260 INDICATOR DOUG DC8 DC871F 302199D WP MLG INTERMITTENT A IPXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 713UP 46014 ON FINAL, GEAR DOWN & LOCK INDICATOR INTERMITTENT. DECLARED EMERGENCY. REPAIRED BROKEN WIRE AT PIN 5 (BLUE WIRE) CON N. P1-213 ON LT MLG DOWN LIMIT SWITCH & REPLACED CONNECTOR.CHECKED NORMALLY. 2 L 7 4 4F RT 4A25 2001041100222 20010411 00222 WP 2001 4 11 UPS01835457 1 20010327 A 2170 COALESCER BAG DOUG DC8 DC873F 302199F WP LEFT CONTAMINATED A IPXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 810UP 46001 AFTER TAKEOFF AND LEFT PACK TURNED ON, CAUSTIC FUMES FILLED COCKPIT. DECLARED EMERGENCY. RAN FUMES EVAC CHECKLIST WHILE RETURNING TO LAND . AIR TURN BACK. R & R LEFT WATER SEPARATOR SOCK, INSPECTED R-SOCK FOUND NO DEFECTS. LEFT SOCK FUEL FUME SOAKED. 2 L 7 4 4F RT 4A25 2001041100223 20010411 00223 EU 2001 4 11 QXEA0100300 1 20010306 A 5310 PRESSURE PANEL FOKKER F28 F28MK4000 4990810 EU NLG WW MISALIGNED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-NOSE LANDING GEAR BAY LEFT HAND SIDEWALL STATION 2650 LOWER CONNECTION ATTACH IS SITTING HIGH ON LOWER AFT CORNER AN D HI-LOK HOLES. REPAIRED IAW FOKKER SRM 53-11-00 AND SRM 51-31-01, PAGE 13 & 14. 2 L 7 2 4F RT A20EU 2001041100224 20010411 00224 EU 2001 4 11 QXEA0100301 1 20010310 A 5310 PRESSURE PANEL FOKKER F28 F28MK4000 4990810 EU NLG WW DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-NOSE LANDING GEAR BAY RIGHT HAND SIDEWALL HAS DENTS IN SKIN AT UPPER FORWARD AND AFT ACM ATTACH AREAS. REPAIRED IAW FOKKER SRM 53-02-18, PAGE 29 AND HORIZON AIR EA 4-53-1452. 2 L 7 2 4F RT A20EU 2001041100225 20010411 00225 EU 2001 4 11 QXEA0100307 1 20010302 A 3830 PAN FOKKER F28 F28MK4000 4990810 EU LAVATORY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CORROSION ON BOTTOM OF LAV DRAIN TUB INSIDE AFT CARGO PIT. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9 AND SRM 53-01-0 1, PAGE 6, AND SRM 51-10-04, PAGE 7. 2 L 7 2 4F RT A20EU 2001041100226 20010411 00226 EU 2001 4 11 QXEA0100308 1 20010302 A 5320 WEB FOKKER F28 F28MK4000 4990810 EU NLG WW MISREPAIRED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-NOSE LANDING GEAR BAY RIGHT HAND SIDE NON STANDARD REPAIR SIDE BOX WEBPLATE. REPAIRED IAW FOKKER SRM 53-11-00 AND S RM 53-11-00. 2 L 7 2 4F RT A20EU 2001041100227 20010411 00227 EU 2001 4 11 QXEA0100309 1 20010312 A 2530 POST FOKKER F28 F28MK4000 4990810 EU AFT GALLEY IMPROPER A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-AFT GALLEY CENTER FREIGHT POST LOWER ATTACHMENT TO FLOOR STRUCTURE IN NON CONFORMANCE, ALSO LOWER END OF FREIGHT POS T IS IN CONTACT WITH GUSTLOCK CABLE RUN. REPAIRED IAW HORIZON AIR EA 4-53-1457. 2 L 7 2 4F RT A20EU 2001041100228 20010411 00228 EU 2001 4 11 QXEA0100310 1 20010311 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-RIGHT HAND FUSELAGE HAS SHARP DENT LOCATED 5 INCHES DOWN AND 4 INCHES IN FROM TRAILING EDGE OF RIGHT HAND STUBWING. REPAIRED IAW FOKKER SRM 53-02-01. 2 L 7 2 4F RT A20EU 2001041100229 20010411 00229 EU 2001 4 11 QXEA0100311 1 20010311 A 5240 FLANGE FOKKER F28 F28MK4000 4990810 EU SERVICE DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK ON SERVICE EMERGENCY DOOR INNER FLANGE UPPER AFT CORNER. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, 14. 2 L 7 2 4F RT A20EU 2001041100230 20010411 00230 EU 2001 4 11 QXEA0100312 1 20010226 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-DENT FOUND TO BE BEYOND LIMITS, NON FLUSH REPAIR. REPAIRED IAW FOKKER SRM 53-02-02, AND SRM 53-01-01, PAGE 8. 2 L 7 2 4F RT A20EU 2001041100231 20010411 00231 EU 2001 4 11 QXEA0100313 1 20010228 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CASTELLATION CLIP ON FRAME 13815 AT STRINGER 43 CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 53-21-04, PAGE 8. 2 L 7 2 4F RT A20EU 2001041100232 20010411 00232 EU 2001 4 11 QXEA0100314 1 20010228 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CASTELLATION CLIP ON FRAME 12405 AT STRINGER 33 CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 53-21-04, PAGE 6. 2 L 7 2 4F RT A20EU 2001041100233 20010411 00233 WP 2001 4 11 NACA2001012 1 20010313 A 6120 322518 FUSE DOUG DC6 DC6A 3021706 WP HAMSTD 43E 43E60 NE PROP SYNC BOX BLOWN A NACA A UNSCHED LANDING O OTHER CL CLIMB 1 AL 03 43872 3314 1245 533294 173169 UNABLE TO CONTROL NR 2 PROPELLER WITH MASTER LEVER OR TOGGLES. REPLACED FUSE IN THE PROP SYNC BOX. 2 L 7 4 4R 6A3 6 C P871 2001041100234 20010411 00234 NM 2001 4 11 UPS01435342 1 20010211 A 5320 65B140562 SUPPORT BOEING 747 747259B NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 527UP 21730 INSPECTION TYPE:C2, 3, STA 1306 LOWER SUPPORT FRAME BETWEEN BODY DOORS IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SUPPORT FRAME IAW DWG 65B14056, AND SRM 51-30-02. 2 L 7 4 4F RT A20WE 2001041100235 20010411 00235 NM 2001 4 11 UPS01435343 1 20010304 A 5340 65B083204 FITTING BOEING 747 747121 1384871 NM FRAME CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6, CRACK AT BS 1265 RT NR 2 STOP AND FRAME INNER CHORD ATT FASTENER HOLE, APPROX .25 INCH LONG RUNNING I/B NR 2 STOP FITTING. REMOVED AND REPLACED PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001041100236 20010411 00236 NM 2001 4 11 UPS01435344 1 20010304 A 5340 65B08320 FITTING BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6, CRACK REVEALED AT BS 1265 LT NR 2 STOP FITTING AND FRAME INNER CHORD ATTACH HOLE APPROX .1875 INCH L ONG. STOP FITTING REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001041100237 20010411 00237 NM 2001 4 11 UPS01435346 1 20010307 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 M/D BS 2320 LT FRAME INNER FRAME FOUND CRACKED. FRAME REPAIRED PER SRM 51-40-03 FIG 1. 2 L 7 4 4F A20WE 2001041100238 20010411 00238 NM 2001 4 11 UPS01435348 1 20010307 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6, FWD CARGO RT FLOOR AREA AT BS 980 STR 39 WEB UPPER FRAME CRACKED THROUGH 1 UPPER FASTENER HOLE. REP AIRED PER SRM 53-10-04 FIG 52. 2 L 7 4 4F A20WE 2001041100239 20010411 00239 NM 2001 4 11 UPS01435350 1 20010211 A 5711 SPAR CAP BOEING 747 747259B NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 527UP 21730 INSPECTION TYPE:C, RIGHT WING FRONT SPAR LOWER CAP LOWER LEG IS CORRODED BEYOND LIMITS, 15 INCHES I/B OF STA FSSO, WS 13 22. REPAIRED LOWER SPAR CAP IAW SRM 57-30-03 FIG 4. 2 L 7 4 4F RT A20WE 2001041100240 20010411 00240 NM 2001 4 11 UPS01635277 1 20010313 A 3610 PRIORITY VALVE BOEING 767 76734AF 1385212 NM RT ENGINE INOPERATIVE A IPXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 301UP 27239 ABORTED T/O IN SDF FOR PRIORITY VALVE EICAS MESSAGE. TROUBLE SHOT TO PRV VALVE AFTER REACTIVATION OF SYS. R & R PRV V ALVE PER M/M 36-11-18 AND CHECKS PER M/M 36-11-18 ALL CHECK SNORMAL. THIS CLEARS M 211073. PLACARD REMOVED.LP636851 2 L 7 2 4F RT A1NM 2001041100241 20010411 00241 NM 2001 4 11 UPS01235508 1 20010404 A 3350 38931002 BATTERY BOEING 727 72751C 1384015 NM LIGHT PACK DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 902UP 18898 BOTH EMERGENCY EXIT LIGHT BATTERY PACK LIGHTS VERY DIM FADE TO NEAR FAILURE IN 30 SECONDS. REPLACED BOTH BATTERIES IN BOTH LIGHT PACKS AS REQUIRED STEADY ILLUMINATION OPS CK OK 2 L 7 3 4F A3WE 2001041100242 20010411 00242 NM 2001 4 11 UPS01435509 1 20010313 A 5311 FRAME BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, MAIN DECK. FRAME WEB IS CRACKED AT CUT OUT FOR STRINGER AT BS 360 S17 LT. REPAIR CARRIED OUT IAW Q UERY NOTE 8/01 2 L 7 4 4F A20WE 2001041100243 20010411 00243 NM 2001 4 11 UPS01435510 1 20010313 A 5311 FRAME BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, MAIN DECK. FRAME WEB IS CRACKED AT CUT OUT FOR STRINGER AT BS 360 S14 RT. REPAIR CARRIED OUT IAW QUERY NOTE 8/01 2 L 7 4 4F A20WE 2001041100244 20010411 00244 NM 2001 4 11 UPS01435511 1 20010320 A 5311 FRAME BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, FWD CARGO HOLD. CRACK ON INNER FLANGE OF FUSELAGE FRAME AT BS 500 S37-38 LT. REPAIR CARRIED OUT I AW EO B747-5310-14356-A 2 L 7 4 4F A20WE 2001041100245 20010411 00245 WP 2001 4 11 UPS01835495 1 20010305 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE: C2, AFT LWR CARGO PIT AT FS 1060 ABOVE LONG 33 RT - 36 FRAME IS CORRODED UND ER AND AROUND NUTPLATES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW 53-2-0 REMOVED FRAME CAP GUSSET & CLIP FOUND GUSSET DAMAGED, OUT OF LI MITS IAW 53-2-0 REC''''D LOCATED & DRILLED NEW FRAME CAP FAB REPAIR IAW STD 5310-602 FAB NEW GUSSET & CLIP IAW DAC DWG 9758507. 2 L 7 4 4F RT 4A25 2001041100246 20010411 00246 WP 2001 4 11 UPS01835498 1 20010305 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE: C2, AFT CARGO PIT AT FS 1140 ABOVE LONG 36 FRAME IS CORRODED. FABBED ALODINED & PRIMED & INSTALLED - 7 REPAIR ANGLE, FILLER, -3 BACK- UP ANGLE & -5 FRAME CAP IAW REO G07893 DC8 SRM 51-1-8 51-1-20D 2 L 7 4 4F RT 4A25 2001041100247 20010411 00247 WP 2001 4 11 UPS01835499 1 20010306 A 5312 BULKHEAD DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE: C2, RT AFT PRESSURE BULKHEAD CRACKED AT STA 1766, 11RT REPAIRED AREA IAW DAC DWG SRO 8530007 2 L 7 4 4F RT 4A25 2001041100248 20010411 00248 WP 2001 4 11 UPS01835500 1 20010306 A 5312 BULKHEAD DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE: C2, LT AFT PRESSURE BULKHEAD CRACKED STA 1766, 11LT REPAIRED AREA IAW DAC DWG SRO 8530007 2 L 7 4 4F RT 4A25 2001041100249 20010411 00249 WP 2001 4 11 UPS01835501 1 20010309 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE: C2, FRAME AT FS -67 HAS CORROSION AT CUSP AREA. REMOVED ''Z'' ANGLES AND INTERCOSTAL TO GET ACCESS TO FRAME CUT OFF DAMAGED SECTION OF FRAME IAW REO-G07891 FABED -17 FRAME SECTION IAW DAC DW G 5613784 FABED -27 -25 SPLICES IAW REO G07891 HEAT TREATED FRAME SE CTION AND SPLICES IAW TPS-1003 REV A ALODINED & PRIMED FRAME SECTION AND SPLICES IAW DC8 SRM 51-1-8 2 L 7 4 4F RT 4A25 2001041100250 20010411 00250 WP 2001 4 11 UPS01835502 1 20010305 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE: C2, AFT LWR CARGO PIT FS 1180 IN CEILING. FLOORBEAM END FITTING IS CRACKED. REMOVED INTERCOSTAL AN D FLOORBOARD TO GAIN ACCESS TO FASTENERS & REMOVED CRACKED FITTING LOCATED NEW FITTING PN 3754922-501 DIAW DC8 SRM 51-1- 21 & 51-3-0 2 L 7 4 4F RT 4A25 2001041100251 20010411 00251 WP 2001 4 11 UPS01835507 1 20010309 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE: C2, MAIN CARGO FLOOR SUPPORT AT STA 1684 LT SIDE AFT OF PANEL F210 CORRODED AROUND HOLES REMOVED S UPPORT FABBED NEW SUPPORT . 2 L 7 4 4F RT 4A25 2001041100252 20010411 00252 WP 2001 4 11 UPS01835512 1 20010405 A 2612 CONNECTOR DOUG DC8 DC873F 302199F WP NR 4 ENGINE LOOSE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:N/A CREW PREFLT- NR 4 ENGINE FIRE DETECTOR FAILED TEST, SECURED NR 4 ENGINE FIRE DETECTOR CORE LOOP CONNECTOR. 2 L 7 4 4F RT 4A25 2001041100253 20010411 00253 WP 2001 4 11 UPS01835458 1 20010327 A 2910 LINE DOUG DC8 DC873F 302199F WP NR 2 ENG HYD SYS BLOWN A IPXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SO 01 851UP 46051 ATB FOR HYD LOST IN FLT, FOUND NR 2 EDP FLEX LINE BLOWN. REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC PRESSURE LINE. R AN ENGINES, LEAK CHECKED. OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2001041100254 20010411 00254 NM 2001 4 11 UPS01435351 1 20010212 A 5754 65B350118 STRUCTURE BOEING 747 747259B NM RT WING LE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 527UP 21730 INSPECTION TYPE:C, RIGHT WING I/B FOREFLAP IS CORRODED BEYOND LIMITS WBL 128.4675 TO WBL 445. REMOVED AND REPLACED RIGH T I/B FOREFLAP. 2 L 7 4 4F RT A20WE 2001041100255 20010411 00255 2001 4 11 UPS01835349 4 20010319 A 2565 TAB DOUG DC8 DC871F 302199D WP ESCAPE SLIDE BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:N/A, MAIN CABIN SLIDE COVER LOCKING TAB BROKEN OFF. REMOVED AND REPLACED LOCKING TAB BRACKET ON SLIDE C ASE. THIS CLEARS M211497 PLACARD REMOVED. 2 L 7 4 4F RT 4A25 2001041100256 20010411 00256 NE 2001 4 11 NACA2001013 2 20010321 A 8530 356993 CYLINDER PWA CB3 DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE NR 2 ENGINE CRACKED A NACA E A ENGINE SHUTDOWN UNSCHED LANDING E K VIBRATION/BUFFET FLUID LOSS CR CRUISE 1 AL 03 99330 773 773 P36927 43576 P36927 SHUT DOWN NR 2 ENGINE DUE TO ROUGHNESS AND OIL LOSS. (NR 4 CYLINDER CRACKED). REPLACED CYLINDER NR 4 ON THE NR 2 ENGIN E. 2 L 7 4 4R 4 R 6A3 5E8 2001041100257 20010411 00257 NM 2001 4 11 TWAA0105201 1 20010321 A 3350 80741 LIGHT BOEING 767 7673Q8 NM CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 634TW 28132 THE CABIN EGRESS LIGHTS WERE INOPERATIVE AT THE END OF FIRST CLASS ON LEFT SIDE, RT SIDE ROW 24 TO 27, AND RT SIDE ROW 1 6 TO 22. REPLACED LIGHT SOCKET ON LT SIDE OF FIRST CLASS, RECONNECTED LIGHT PLUG AT ROW 24 RT SIDE, AND RECONNECTED LIG HT CONNECTOR AT ROW 22 RT SIDE. CHECK-C 10-25-00 LAX. 2 L 7 2 4F RT A1NM 2001041100258 20010411 00258 WP 2001 4 11 TWAA0105202 1 20010320 A 5347 CARGO TRACK DOUG DC9 DC931 3022065 WP FWD CARGO BAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 992Z 47095 DURING OP 15 MAINT CHECK IN THE FWD CARGO COMPT, THE RT FWD CARGO TRACK WAS BADLY CORRODED, STA 218 TO 370. MADE NEW TR ACK FROM STOCK. DRILLED HOLES FROM OLD TRACK AND COUNTERSUNK HOLES. TREATED AND PRIMED TRACK. ACCOMPLISHED PER SPM 6- 70-01. 2 L 7 2 4F A6WE 2001041100259 20010411 00259 WP 2001 4 11 TWAA0105203 1 20010320 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT FOUND CABIN FLOOR TRACK NUMBER 4, BETWEEN STA 200 AND 256, HAD CORROSION ON TOP AND BOTTOM OF FLANG E SURFACE. REMOVED OLD TRACK AND INSTALLED NEW PER SPM 6-70-01. INSTALLED HI-LOKS PER SRM 51-30-05. 2 L 7 2 4F A6WE 2001041100260 20010411 00260 WP 2001 4 11 TWAA0105205 1 20010214 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP AFT CARGO BAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 957U 49702 DURING CHECK-C MAINT IN AFT CARGO COMPT THE LT TIE DOWN TRACK WAS CORRODED FROM STA 1155 TO 1320. REMOVED CORROSION PER SPM 6-80-1. FABRICATED NEW TRACKS PER SPM 6-70-01 AND ORIGINALS. INSTALLED SPLICE AND TRACK PER SRM 53-05 FIG 4G. FA STENERS PER SRM 51-30-1. 2 L 7 2 4F A6WE 2001041100261 20010411 00261 EU 2001 4 11 MALA010281 1 20010316 A 3230 CONNECTOR SAAB SF340 340B 7860101 EU LANDING GEAR DIRTY A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 590MA 340B181 AFTER TO ON FLIGHT 3353, LANDING GEAR HANDLE WAS SELECTED UP, LANDING GEAR FAILED TO RETRACT. GEAR UNSAFE LIGHT REMAINE D ILLUMINATED, AND HYDRAULIC PUMP CONTINUED TO RUN. AIR RETURN TO BUF. MAINTENANCE CLEANED CANNON PLUGS AND UPLOCK SWI TCHES, PERFORMED OPS CHECK. ALL SYSTEMS CHECK NORMAL. 2 L 7 2 4T RT A52EU 2001041100262 20010411 00262 EU 2001 4 11 QXEA0100385 1 20010319 A 3350 5515900004 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 483US 11233 PDX-EXIT SIGN ABOVE GALLEY CABIN ENTRY HAS INOPERATIVE LETTERS. REMOVED AND REPLACED CIRCUIT BOARD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001041100263 20010411 00263 NM 2001 4 11 AWXA0001509 1 20010321 A 5320 BAC1517705 WEB BOEING 737 737277 1384570 NM CARGO BAY CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 AFT CARGO COMPARTMENT, AFT OF DOOR OPENING, WEB CRACKED AND TORN ALONG EDGE OF DOOR OPENING. REPAIRED TORQUE BOX WEB AT BS 847 STR 21R IAW B737-200 SRM 51-40-2 FIG 1. 2 L 7 2 4F RT A16WE 2001041100264 20010411 00264 NM 2001 4 11 AWXA0001510 1 20010321 A 5320 65465375 ANGLE BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 CRACK IN I/B LEG OF VERTICAL ANGLE BS 578 LBL 60. REMOVED AND REPLACED VERTICAL ANGLE IAW BOEING DWG 65-46537, B737-200 SRM 51-30-2 PG 2, 3, 8. 2 L 7 2 4F RT A16WE 2001041100265 20010411 00265 NM 2001 4 11 AWXA0001512 1 20010321 A 5311 65163004301 FRAME BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 LEFT SIDE CHORD AT WL 207 ON AFT SIDE OF BS 178 BULKHEAD CRACKED IN RADIUS. REMOVED LEFT SIDE WEB, REMOVED LEFT SIDE CH ORD; LOCATED, DRILLED AND INSTALLED NEW SIDE CHORD IAW B737-300 SRM 51-40-02 PG 1 AND 10; REINSTALLED WEB IAW B737-300 S RM 51-40-02 PG 1 AND 10. 2 L 7 2 4F RT A16WE 2001041100266 20010411 00266 NM 2001 4 11 AWXA0001513 1 20010321 A 5315 BAC1505100246 FLOORBEAM BOEING 737 7373S3 1384711 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 CABIN FLOORBEAM UPPER CHORD UPPER SURFACE CORRODED AT BS 312 RBL 13 WL 208. REMOVED UPPER CHORD SECTION OF FLOORBEAM AT BS 312 BL 18L - 24R WL 208; LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED NEW SECTION IAW B737-300 SRM 53-10-51 FIG 2 05. 2 L 7 2 4F RT A16WE 2001041100267 20010411 00267 NM 2001 4 11 AWXA0001514 1 20010321 A 5320 AND101341205 ANGLE BOEING 737 7373S3 1384711 NM FUSELAGE ELONGATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 FS 178 BULKHEAD AFT FACE FLOORBEAM LOWER ANGLE HAS ELONGATED HOLES WL 195 LBL 24. REMOVED FASTENERS, CUT OUT DAMAGE, FO RMED, DRILLED AND INSTALLED REPAIR DOUBLERS AND FILLER IAW B737-300 SRM 51-70-12 PG 1; HEAT TREATED ANGLES IAW TIMCO TPS -1003 REV A; TREATED AND PRIMED IAW B737-300 SRM 51-20-01 PG 1. 2 L 7 2 4F RT A16WE 2001041100268 20010411 00268 NM 2001 4 11 2001UALA00147 1 20010224 A 3350 20131 BATTERY PACK BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN DEFECTIVE A UALA K NONE O OTHER CR CRUISE 1 WP 29 617UA 21877 EEL LIGHTS IN BUSINESS CLASS AND OVERWING EXIT LIGHTS FLASH CONTINUOUSLY WITH SWITCH IN ARMED. *S/D* REPLACED BATTERY PACK AT M737 FOR TROUBLESHOOTING, NO HELP. SWAPPED BATTERY PACK AT M735 WITH M737, PROBLEM FOLLOWED. REPLACED BATTERY PACK M735. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041100269 20010411 00269 NM 2001 4 11 2001UALA00158 1 20010227 A 5330 SKIN BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 985UA 21747 SEVERAL FATIGUE CRACKS WERE FOUND IN THE FUSELAGE SKIN JUST AFT OF THE FORWARD GALLEY DOOR AND FORWARD OF THE STA 360 PR ODUCTION JOINT. *S/U* FASTENER HOLE CRACKED AT STR 15R WAS REPAIRED PER SRM 53-30-3, FIGURE 43. FASTENER HOLES CRACKE D AT STR 16R WERE REPAIRED PER SRM 53-30-3, FIGURE 6. 2 L 7 2 4F 4 F A16WE E2EA 2001041100270 20010411 00270 EU 2001 4 11 2001UALA00160 1 20010227 A 2822 PUMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUEL SYSTEM INTERMITTENT A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 423UA 504 WING BOOST PUMP FAILURE. *S/D* THE NR 2 FUEL BOOST PUMP WAS GROUND CHECKED WITH NO FAULTS FOUND. THE PUMP HAS NO HIST ORY OF BEING INOPERATIVE AND HAS FLOWN 2 FLIGHTS SINCE IT WAS CHECKED AS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2001041100271 20010411 00271 WP 2001 4 11 MWEA010365 1 20010323 A 5320 99579092 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE DEFORMED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 INTERCOSTAL AT LONGERON 26 RIGHT UPPER SIDE, BETWEEN STATION 427-433 NEEDS REMOVED FOR STATION 427 FRAME REPAIR. REMOV ED, RECONTOURED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001041100272 20010411 00272 NM 2001 4 11 UPS01435373 1 20010309 A 5320 TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - BS 800 LT TENSION TIE FOUND CRACKED. TENSION TIE REPAIRED AS PER EO B747-5310-5890 FIG 2. 2 L 7 4 4F A20WE 2001041100273 20010411 00273 NM 2001 4 11 UPS01435374 1 20010309 A 5320 TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - BS 820 LT TENSION TIE FOUND CRACKED. TENSION TIE REPAIRED AS PER EO B747 AS PER EO B747-5310 -5890 FIG 2. 2 L 7 4 4F A20WE 2001041100274 20010411 00274 NM 2001 4 11 UPS01435375 1 20010309 A 5320 TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - BS 860 LT TENSION TIE FOUND CRACKED. TENSION TIE REPAIRED AS PER EO B747-5310-5890 FIG 2. 2 L 7 4 4F A20WE 2001041100275 20010411 00275 NM 2001 4 11 UPS01435376 1 20010309 A 5320 TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - BS 880 LT TENSION TIE FOUND CRACKED. TENSION TIE REPAIRED AS PER EO B747-5310-5890 FIG 2. 2 L 7 4 4F A20WE 2001041100276 20010411 00276 NM 2001 4 11 UPS01435377 1 20010309 A 5320 TIE BOEING 747 747121 1384871 NM CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - BS 920 LT TENSION TIE FOUND CRACKED. TENSION TIE REPAIRED AS PER EO B747310890 FIG 2. 2 L 7 4 4F A20WE 2001041100277 20010411 00277 NM 2001 4 11 UPS01435378 1 20010309 A 5320 TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - BS 940 LT TENSION TIE FOUND CRACKED. TENSION TIE REPAIRED AS PER EO B747-5310-5890 FIG 2. 2 L 7 4 4F A20WE 2001041100278 20010411 00278 NM 2001 4 11 UPS01435379 1 20010309 A 5320 TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - BS 780 RT TENSION TIE FOUND CRACKED. TENSION TIE REPAIRED AS PER EO B747-5310-5890 FIG 2. 2 L 7 4 4F A20WE 2001041100279 20010411 00279 NM 2001 4 11 UPS01435380 1 20010309 A 5320 TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - BS 800 RT TENSION TIE FOUND CRACKED. TENSION TIE REPAIRED AS PER EO B747-5310-5890 FIG 2. 2 L 7 4 4F A20WE 2001041100280 20010411 00280 NM 2001 4 11 UPS01435381 1 20010309 A 5320 TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - BS 820 RT TENSION TIE FOUND CRACKED. TENSION TIE REPAIRED AS PER EO B747-5310-5890 FIG 2. 2 L 7 4 4F A20WE 2001041100281 20010411 00281 NM 2001 4 11 UPS01435382 1 20010309 A 5320 TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - BS 860 RT TENSION TIE FOUND CRACKED. TENSION TIE REPAIRED AS PER EO B747-5310-5890 FIG 2. 2 L 7 4 4F A20WE 2001041100282 20010411 00282 NM 2001 4 11 UPS01435383 1 20010309 A 5320 TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN BS 880 RT TENSION TIE FOUND CRACKED. TENSION TIE REPAIRED AS PER EO B747-5310-5890 FIG 2. 2 L 7 4 4F A20WE 2001041100283 20010411 00283 NM 2001 4 11 UPS01435384 1 20010309 A 5320 TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - BS 920 RT TENSION TIE FOUND CRACKED. TENSION TIE REPAIRED AS PER EO B747-5310-5890 FIG 2. 2 L 7 4 4F A20WE 2001041100284 20010411 00284 WP 2001 4 11 MWEA010367 1 20010323 A 5230 59101415 PAN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 FORWARD CARGO DOOR OUTER PAN HAD CRACKS COMING FROM A FASTENER HOLE. STOP DRILLED CRACKS, FABRICATED, LOCATED, DRILLE D AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001041100285 20010411 00285 NM 2001 4 11 UPS01435385 1 20010309 A 5320 TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - BS 940 RT TENSION TIE FOUND CRACKED. TENSION TIE REPAIRED AS PER EO B747-5310-5890 FIG 2. 2 L 7 4 4F A20WE 2001041100286 20010411 00286 NM 2001 4 11 UPS01435386 1 20010309 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 M/D FRAME CUP FOUND CRACKED AT BS 1660 JUST ABOVE STR 16R. FRAME CUP REPAIRED AS PER SRM 53-10-04 FIG 4. 2 L 7 4 4F A20WE 2001041100287 20010411 00287 NM 2001 4 11 UPS01435387 1 20010309 A 5210 65B0831916 FITTING BOEING 747 747121 1384871 NM PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 MAIN DECK - R3 DOOR FWD CUTOUT NR 5 STOP SUPPORT FITTING FOUND CRACKED. R3 DOOR FWD NO.5 STOP FITTIN G REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001041100288 20010411 00288 NM 2001 4 11 UPS01435388 1 20010309 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 MAIN DECK - FRAME CUP FOUND CRACKED AT BS 900 JUST ABOVE STR 22L. FRAME CUP REPAIRED AS PER SRM 53- 10-04 FIG 4. 2 L 7 4 4F A20WE 2001041100289 20010411 00289 NM 2001 4 11 UPS01435389 1 20010309 A 5310 DOOR FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 CABIN - R4 DOOR AFT LOWER FRAME CORNER CRACKED. DOOR LOWER CORNER REPAIRED AS PER SRM 52-10-02 FIG 10. 2 L 7 4 4F A20WE 2001041100290 20010411 00290 NM 2001 4 11 UPS01435390 1 20010309 A 5210 FITTING BOEING 747 747121 1384871 NM PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 MAIN DECK - R3 DOOR FWD CUTOUT NR 5 DOOR STOP SUPPORT FITTING FOUND CRACKED. REFER NRC 6124 FOR F ITTING REPLACEMENT DETAIL. 2 L 7 4 4F A20WE 2001041100291 20010411 00291 NM 2001 4 11 UPS01435391 1 20010309 A 5310 65B11751601 DOOR FRAME BOEING 747 747121 1384871 NM PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 MAIN DECK - L3 DOOR LOWER FWD CORNER REVEAL FOUND CRACKED. CORNER REVEAL REPLACED AS PER SRM 51-1 0-01. 2 L 7 4 4F A20WE 2001041100292 20010411 00292 NM 2001 4 11 UPS01435392 1 20010310 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 M/D - BS 1467 - 1478, STR 9R, STRINGER END FOUND CRACKED. STRINGER END ANGLE REPAIRED. 2 L 7 4 4F A20WE 2001041100293 20010411 00293 NM 2001 4 11 UPS01435393 1 20010310 A 5320 FLOOR SUPPORT BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 M/D - BS 1241-1265 LBL 116 O/B LONGITUDINAL FLOOR SUPPORT FOUND CORRODED. FLOOR SUPPORT REPLACED AS PER SRM 51-10-01. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT COR. DEPTH 0.036 INCH, WIDTH 1INCH , LENGTH 2 INCH. 2 L 7 4 4F A20WE 2001041100294 20010411 00294 NM 2001 4 11 UPS01435394 1 20010310 A 5310 SHEAR TIE BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 AFT CARGO COMPT - FRAME SHEAR TIE AFT FACE FOUND CORRODED AT STA 1680, BETWEEN STR 51 LT TO STR 51 RT . AFT CARGO COMPT SHEAR TIE CORROSION REMOVED & REPAIRED PER SRM 53-10-04 FIG 3A. BLEND OUT CORROSION DEPTH 0.030 INCH , WIDTH 1 INCH, LENGTH 2 INCH. 2 L 7 4 4F A20WE 2001041100295 20010411 00295 NM 2001 4 11 UPS01435395 1 20010311 A 5210 STRUCTURE BOEING 747 747121 1384871 NM PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 M/D - R2 DOOR FWD LWR CORNER FOUND CRACKED. DOOR FWD LWR CORNER REPAIRED AS PER SRM 52-10-02 FIG 10. 2 L 7 4 4F A20WE 2001041100296 20010411 00296 NM 2001 4 11 UPS01435396 1 20010311 A 5310 DOOR FRAME BOEING 747 747121 1384871 NM PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 M/D - R2 DOOR FWD EDGE MOST UPPER STOP CUTOUT AREA FOUND CRACKED. DOOR CUTOUT EDGE REPAIRED AS PER S RM 52-10-02 FIG 8. 2 L 7 4 4F A20WE 2001041100297 20010411 00297 WP 2001 4 11 MWEA010368 1 20010323 A 5415 59239371 FITTING DOUG DC9 DC932 3022066 WP LT PYLON CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 LEFT LOWER PYLON BEAVER TAIL FITTING BOTTOM SURFACE CORRODED. REMOVED DAMAGED FITTING, DRILLED UP NEW FITTING AND INST ALLED. 2 L 7 2 4F A6WE 2001041100298 20010411 00298 WP 2001 4 11 MWEA010369 1 20010323 A 5320 591013054 ANGLE DOUG DC9 DC932 3022066 WP BULKHEAD DAMAGED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 205ME 47601 AFT PRESSURE BULKHEAD TEE ANGLE AT STATION 996 HAD 2 AREAS OF MECHANICAL DAMAGE IN RADIUS AND SEVERAL AREAS OF DAMAGE ON FLANGE LONGERON 11 - 13 RIGHT. REMOVED T ANGLE, LOCATED, DRILLED AND INSTALLED NEW ANGLE. 2 L 7 2 4F A6WE 2001041100299 20010411 00299 NM 2001 4 11 UPS01435397 1 20010311 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C6 M/D - BS 1560, S24R-S25R FRAME O/B AREA FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 4. 2 L 7 4 4F A20WE 2001041100300 20010411 00300 NM 2001 4 11 UPS01235486 1 20010404 A 3510 SHUTOFF VALVE BOEING 727 727172C 1384058 NM CREW OXYGEN LEAKING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 916UP 19808 CREW PRE-FLIGHT CREW O2 SHUTOFF VALVE LEAKING. R&R SHUT OFF VALVE 2 L 7 3 4F A3WE 2001041600472 20010416 00472 NM 2001 4 16 UPS01235487 1 20010404 A 2750 CONTROL CABLE BOEING 727 727247 138408F NM TE FLAPS OUT OF RIG A IPXA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 01 207UP 21699 ATB-A/C ROLLS DURING FLAP RETRACTION. SUPPLEMENTAL MRR. ADJUSTED INBD AND OUTBD FLAPS FUSELAGE CABLES PER B727 MM-27-51 -00 2 L 7 3 4F A3WE 2001041100301 20010411 00301 NM 2001 4 11 UPS01235491 1 20010326 A 5230 FITTING BOEING 727 72731C 1384011 NM CARGO DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C & SI, TOP FWD CORNER FITTING CORRODED & CRACKED IN MAIN CARGO DOOR. TOP FWD CORNER FITTING REPLACED ON MCD IAW SRM 51-30-2 2 L 7 3 4F A3WE 2001041100302 20010411 00302 NM 2001 4 11 UPS01235492 1 20010326 A 5230 FITTING BOEING 727 72731C 1384011 NM CARGO DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C & SI, TOP AFT CORNER FITTING CORRODED & CRACKED ON MAIN CARGO DOOR. TOP AFT CORNER FITTING REPLACED ON MCD IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2001041100303 20010411 00303 NM 2001 4 11 UPS01235493 1 20010323 A 5350 FRAME BOEING 727 72731C 1384011 NM FAIRING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C & SI, LT WING TO BODY FAIRING NR 3335 HAS CORRODED FRAME. RIVETS REMOVED FROM CORRODED FRAME IAW SRM 51-30-2 CORRODED FRAME CUT OUT IAW SRM 51-10-6 REPAIR CARRIED OUT IAW SRM 51-40-3 FIG 1 2 L 7 3 4F A3WE 2001041100304 20010411 00304 NM 2001 4 11 UPS01435484 1 20010313 A 5315 FLOORBEAM BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, UPPER DECK FLOOR. CORROSION ON UPPER CHORD OF FLOORBEAM AT BS 520 LBL 46 TO LBL 64 CORROSION R EMOVED AND FOUND TO BE OUTSIDE LIMITS. REPAIRS ACCOMPLISHED IAW SRM 53-10-07 2 L 7 4 4F A20WE 2001041100305 20010411 00305 WP 2001 4 11 UPS01835489 1 20010401 A 3350 LIGHT DOUG DC8 DC873F 302199F WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 809UP 46109 EMERGENCY EXIT DISARM LIGHT DID NOT COME ON WHEN TURNED OFF. RELAMPED OP CHECK GOOD PER DC8 MM 33-50-02 2 L 7 4 4F RT 4A25 2001041100306 20010411 00306 WP 2001 4 11 UPS01835490 1 20010402 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 805UP 46117 EMERG LIGHTS INOP. REPLACED EMERG BATTERY PACK 60-1223-5 S/N 338N) 341(OFF) 2 L 7 4 4F RT 4A25 2001041100307 20010411 00307 WP 2001 4 11 UPS01835494 1 20010403 A 2560 SEAL DOUG DC8 DC871F 302199D WP COCKPIT PBE LEAKING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 PBE. IN FLIGHT DECK HAS AIR TIGHT SEAL BROKEN. R & R PBE IN FLIGHT DECK AS REQ''''D. OK FOR SERVICE. S/N 2 L 7 4 4F RT 4A25 2001041100308 20010411 00308 EU 2001 4 11 UPS01135461 1 20010328 A 2510 SHOULDER BELT AIRBUS A300 A300F4622R 3930360 EU COCKPIT SEATS INOPERATIVE A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 122UP 0807 INSPECTION TYPE:N/A CAPTAINS & FIRST OFFICERS SHOULDERS HARNESS RETRACT INTO SEATBACK. 2 L 7 2 4F RT A35EU 2001041100309 20010411 00309 NM 2001 4 11 UPS01235401 1 20010218 A 5330 LAP JOINT BOEING 727 72730C 1384009 NM FUSELAGE BULGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:C CK LAP JOINT 19RT HAS SKIN BULGE AT BS 620. CUT OUT DAMAGED SKIN LWR & UPPER AREA. INSTALLED REPAI R PART AT LAP JOINT STR 19 BS 620. 2 L 7 3 4F A3WE 2001041100310 20010411 00310 NM 2001 4 11 UPS01235459 1 20010306 A 5310 SHEAR TIE BOEING 727 727247 138408F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE:C. DISCOVERED SHEAR TIE AT BS 1148 LBL 10 WL 150 TO BE CORRODED SHEAR TIE FOUND TO BE CORRODED OUT OF LIMITS PER SRM 53-10-1 REMOVED OLD SHEAR TIE AND INSTALLED NEW SHEAR TIE PER SRM 51-30-2 AND 51-10-2 2 L 7 3 4F A3WE 2001041100311 20010411 00311 NM 2001 4 11 UPS01235460 1 20010320 A 5320 M264232 STIFFENER BOEING 727 7272A1 138407F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 213UP 21341 INSPECTION TYPE:C CORROSION IN RT MLG WW ON STIFFENER AND LOWER CHANNEL AT BS 919, WL 188, RBL 65 REMOVED CORRODED S TIFFENER, FABRICATED AND INSTALLED PER SRM 51-10-6, 51-30-2, 51-10-1 AND BOEING DRAWING 65-16335 PL AND SHT 2 AT BS 919, WL 188, RBL 65 2 L 7 3 4F A3WE 2001041100312 20010411 00312 WP 2001 4 11 UPS01835462 1 20010327 A 5610 SEAL DOUG DC8 DC871F 302199D WP COCKPIT WINDOW FAILED A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 715UP 45915 CAPTAINS CLEARVIEW SLIDING WINDOW SEAL BLOWN OUT. 2 L 7 4 4F RT 4A25 2001041100313 20010411 00313 WP 2001 4 11 MWEA010331 1 20010314 A 5313 5911401103 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 LONGERON 30 IS CRACKED AT STATION 200. REMOVED SECTION, FABRICATED, LOCATED, DRILLED AND INSTALLED NEW SECTION. 2 L 7 2 4F A6WE 2001041100314 20010411 00314 WP 2001 4 11 MWEA010326 1 20010314 A 5753 5935929501 STRUCTURE DOUG DC9 DC932 3022066 WP RT FLAP CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 RIGHT WING FLAP LEADING EDGE IS CHAFED 3 INCHES INBOARD OF FLAP HINGE FITTING. BLENDED RUB STRIP OUT OF LIMITS. REMOVE D DAMAGED SECTION, FABRICATED, LOCATED, DRILLED AND INSTALLED NEW SECTION. 2 L 7 2 4F A6WE 2001041100315 20010411 00315 WP 2001 4 11 MWEA010327 1 20010314 A 5320 591034311 DOUBLER DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 THE E&E BAY DOOR JAMB PAN DOUBLER WAS CORRODED BEYOND LIMITS. REMOVED, DOUBLER, LOCATED, DRILLED AND INSTALLED NEW DOUB LER. 2 L 7 2 4F A6WE 2001041100316 20010411 00316 WP 2001 4 11 MWEA010328 1 20010314 A 5347 59108205 SEAT TRACK DOUG DC9 DC932 3022066 WP CABIN CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 NR 4 SEAT TRACK AT STATION 200 WAS CORRODED. REMOVED SECTION, FABRICATED, LOCATED, DRILLED AND INSTALLED NEW SECTION. 2 L 7 2 4F A6WE 2001041100317 20010411 00317 WP 2001 4 11 MWEA010329 1 20010314 A 5320 9910078170 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 FLOORBOARD SUPPORT FORWARD OF NR 4 SEAT TRACK AT STATION 160-200 WAS CORRODED. REMOVED SUPPORT, FABRICATED, LOCATED, DR ILLED AND INSTALLED NEW SUPPORT. 2 L 7 2 4F A6WE 2001041100318 20010411 00318 WP 2001 4 11 MWEA010330 1 20010314 A 5320 992348463 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 FLOORBOARD SUPPORT BETWEEN NR 3 AND 4 SEAT TRACK WAS CORRODED. REMOVED SUPPORT, FABRICATED, LOCATED, DRILLED AND INSTAL LED NEW SUPPORT. 2 L 7 2 4F A6WE 2001041100319 20010411 00319 WP 2001 4 11 MWEA010333 1 20010314 A 5320 592420713 SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FORWARD BAG PIT AFT BULKHEAD, ONE VERTICAL SUPPORT FRAME IS CRACKED AT LOWER END. REMOVED DAMAGED SECTION, FABRICATED A ND INSTALLED NEW PART, SPLICE AND DOUBLERS. 2 L 7 2 4F A6WE 2001041100320 20010411 00320 WP 2001 4 11 MWEA010334 1 20010314 A 5320 99155409 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 INTERCOSTAL HAS LIGHT CORROSION BY TAP NUT PLATE AND TAP FLANGE IS BENT STATION 1004 APPROXIMATELY 22 INCHES RIGHT OF CL . CLEANED CORROSION, FABRICATED DOUBLE STACKED DOUBLER, INSTALLED STACKED ANGLE REPAIR. 2 L 7 2 4F A6WE 2001041100321 20010411 00321 WP 2001 4 11 MWEA010335 1 20010314 A 5321 995792926 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 CORROSION AND GOUGES ON FLOORBOARD A9 STATION 908. REMOVED HAT CHANNELS, FABRICATED NEW FLOOR PANEL SKIN AND HAT CHANNE LS. INSTALLED HAT CHANNELS AND FLOORBOARD INSULATION BAGS. 2 L 7 2 4F A6WE 2001041100322 20010411 00322 WP 2001 4 11 MWEA010336 1 20010314 A 5320 592420714 SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FORWARD BAG PIT AFT BULKHEAD SUPPORT FRAMES HAVE LIGHT CORROSION AROUND SOME SCREW HOLES. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLERS. 2 L 7 2 4F A6WE 2001041100323 20010411 00323 EU 2001 4 11 01FDEA00198 1 20010314 A 7830 WARNING LIGHT AIRBUS 310 A310222 3930315 EU COCKPIT ILLUMINATED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 451FE 303 ON T/O ROLL WITH MAX POWER SET, NR 2 REVERSER UNLOCK LIGHT CAME ON WITH ECAM WARN. AC RELEASED PER MEL 78-1. 2 L 7 2 4F RT A35EU 2001041100324 20010411 00324 SO 2001 4 11 COMA0110047 1 20010312 A 5320 12007089003 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 7922 120264 DURING 2C CHECK TASK 131/132-01Z, THE FUSELAGE CENTER FORWARD FLOORBEAM BUTTSTRAP WAS FOUND CORRODED. THE PART WAS REPL ACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 1671-1, REV A, 1-28-97. 2 L 7 2 4T RT A31SO 2001041100325 20010411 00325 NM 2001 4 11 EISA20010035 1 20010214 A 5523 TRIM TAB BOEING BOEING 727 727223 1384074 NM ELEVATOR DAMAGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND RT ELEVATOR TRIM TAB HAS HOLE WHERE SCREW WAS LOCATED. FABRICATED INSTALLED BUS HING, ALODINED AND PRIMED IAW REO-W00026, SRM 51-30-2, AND M/M 27-30-11. 2 L 7 3 4F A3WE 2001041100326 20010411 00326 NM 2001 4 11 EISA20010036 1 20010214 A 5755 651734742 SKIN BOEING BOEING 727 727223 1384074 NM SPOILER DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSP FOUND RIGHT WING NR 11 SPOILER UPPER SURFACE DELAMINATED. CLEANED AND PREPPED AREA, BONDED FIBERGLASS OVERLAYS, PRIMED AND PAINTED AREA IAW SRM 57-40-06, 51-50-6 FIG 1, AND M/M 27-61-1 AND 51-20-151. 2 L 7 3 4F A3WE 2001041100327 20010411 00327 NM 2001 4 11 EISA20010037 1 20010214 A 5320 BAC1503100174 WEB BOEING BOEING 727 727223 1384074 NM FUSELAGE CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND CRACK AT BS 1195 WL 290 FWD OF ACCESSORY COMPRT LEFT SIDE OF AFT ENTRY DOOR. FA BRICATED INSTALLED WEB REPAIR DOUBLER AND CHORD REPAIR ANGLES, ALODINED AND PRIMED IAW SRM 53-10-2, 51-40-2 FIG 2, 51-10 -2, M/M 51-20-11 AND BOEING DRAWING 65-23651. 2 L 7 3 4F A3WE 2001041100328 20010411 00328 2001 4 11 EISA20010029 4 20010215 A 2210 258580212 CONTROL BOX HONEYWELL BOEING 727 727225 1384077 NM COCKPIT SMOKE A EISA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 354PA 20624 SMOKE FROM AUTOPILOT CONTROL BOX, TURNED OFF AND PULLED CIRCUIT BREAKER. REMOVED AND REPLACED AUTO PILOT CONTROL HEAD P ER M/M 22-11-01, OPS CHECK NORMAL. 2 L 7 3 4F A3WE 2001041200001 20010412 00001 NM 2001 4 12 EISA20010041 1 20010214 A 5347 BAC1520841 SEAT TRACK BOEING BOEING 727 727223 1384074 NM UPPER CARGO BAY CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION ON MAIN CABIN CARGO COMPARTMENT LEFT O/B SEAT TRACK SECTION FROM BS 75 7 TO BS 852 LBL 45.5. FABRICATED AND INSTALLED SEAT TRACK SPLICE AT BS 757 TO BS 852 LBL 45.5, ALODINED AND PRIMED IAW SRM 53-10-5 FIG 2, 51-10-6, 53-10-1 FIG 3, 51-10-2, 51-30-2. 2 L 7 3 4F A3WE 2001041200002 20010412 00002 NM 2001 4 12 EISA20010042 1 20010214 A 5312 BULKHEAD BOEING BOEING 727 727223 1384074 NM FUSELAGE CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION AT AFT CARGO BULKHEAD BS 1060, WL 208. FABRICATED AND INSTALLED REPAI R FRAME DOUBLER, FILLER, AND REPAIR ANGLE, AT BS 1060 WL 208. ALODINED AND PRIMED IAW SRM 53-10-8 FIG 3, 51-10-2, 51-30 -2. 2 L 7 3 4F A3WE 2001041200003 20010412 00003 NM 2001 4 12 EISA20010043 1 20010214 A 5347 BAC1520792 SEAT TRACK BOEING BOEING 727 727223 1384074 NM UPPER CARGO BAY CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION ON MAIN CABIN CARGO COMPARTMENT LEFT O/B SEAT TRACK SECTION FROM BS 44 0 TO BS 480 LBL 45. FABRICATED AND INSTALLED SEAT TRACK SPLICE AT BS 440 TO BS 480 LBL 45, ALODINED AND PRIMED IAW SRM 53-10-1 FIG 3, 53-10-5 FIG 7, 53-30-3, 51-30-2, 51-10-2. 2 L 7 3 4F A3WE 2001041200004 20010412 00004 NM 2001 4 12 EISA20010044 1 20010214 A 5347 BAC1520841 SEAT TRACK BOEING BOEING 727 727223 1384074 NM CABIN CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION ON MAIN CABIN LEFT I/B SEAT TRACK SECTION FROM BS 757 TO BS 852 LBL 25 . FABRICATED AND INSTALLED SEAT TRACK SPLICE AT BS 757 TO BS 852 LBL 25, ALODINED AND PRIMED IAW SRM 53-10-1, 53-10-5 F IG 7, 51-10-2. 2 L 7 3 4F A3WE 2001041200005 20010412 00005 NM 2001 4 12 EISA20010045 1 20010214 A 5347 BAC1520792 SEAT TRACK BOEING BOEING 727 727223 1384074 NM UPPER CARGO BAY CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION ON MAIN CABIN CARGO COMPARTMENT LEFT I/B SEAT TRACK SECTION FROM BS 74 1 TO BS 757. FABRICATED AND INSTALLED SEAT TRACK SPLICE AT BS 741 TO BS 757 LBL 24. ALODINED AND PRIMED IAW SRM 51-10- 2, 53-10-5 FIG 7, 51-10-6, 51-30-2. 2 L 7 3 4F A3WE 2001041200006 20010412 00006 NM 2001 4 12 EISA20010046 1 20010214 A 5347 BAC1520792 SEAT TRACK BOEING BOEING 727 727223 1384074 NM UPPER CARGO BAY CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION ON MAIN CARGO COMPARTMENT RIGHT O/B SEAT TRACK SECTION FROM BS 580 TO BS 620. FABRICATED AND INSTALLED SEAT TRACK SPLICE AT BS 580 TO BS 640 RBL 45. ALODINED AND PRIMED IAW 51-10-2, 53-10- 5 FIG 7, 51-10-6, 51-30-2. 2 L 7 3 4F A3WE 2001041200007 20010412 00007 NM 2001 4 12 EISA20010047 1 20010214 A 5315 6520827 FLOORBEAM BOEING BOEING 727 727223 1384074 NM FUSELAGE CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND FLOORBEAM AT BS 1060 LOWER LEG CORRODED. FABRICATED AND INSTALLED 2 REPAIR ANGL ES, ALODINED AND PRIMED ANGLE REPAIRS IAW SRM 53-10-8 FIG 2, 51-10-2, 51-30-2. 2 L 7 3 4F A3WE 2001041200008 20010412 00008 NM 2001 4 12 EISA20010048 1 20010214 A 5320 BAC15171507 ANGLE BOEING BOEING 727 727223 1384074 NM FUSELAGE CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND Z-ANGLE CORRODED AT BS 570 TO BS 600, RBL 20. FABRICATED AND INSTALLED Z-ANGLE AND WEB REPAIR, ALODINED AND PRIMED IAW SRM 51-40-2 FIG1, 51-40-4, 53-10-2, 51-30-2, 51-10-2, AND M/M 51-20-11. 2 L 7 3 4F A3WE 2001041200009 20010412 00009 NM 2001 4 12 EISA20010050 1 20010214 A 5711 6516202 SPAR BOEING BOEING 727 727223 1384074 NM RT WING CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION AT RIGHT WING CENTER SECTION, REAR SPAR LOWER CHORD AND WEB. FABRICAT ED AND INSTALLED WEB REPAIR AND SPACERS AT RIGHT WING CENTER SECTION REAR SPAR LOWER CHORD AND WEB, ALODINED AND PRIMED IAW SRM 51-10-2, 51-30-2, SPM 20-10-23, 20-50-19, AND TIMCO REO-W00028. 2 L 7 3 4F A3WE 2001041200010 20010412 00010 NM 2001 4 12 2001UALA00175 1 20010304 A 3620 342B030000 THERMOSTAT AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE BLEED AIR FAILED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 805UA 783 NR 2 ENGINE BLEED AIR LOW TEMPERATURE INDICATION. SUPPLEMENTAL DATA UPDATE REPLACED FAN AIR VALVE THERMOSTAT. NO FURTH ER DISCREPANCIES NOTED SINCE THERMOSTAT REPLACEMENT. 2 L 7 2 4F 4 F RT A28NM E40NE 2001041200011 20010412 00011 NM 2001 4 12 2001UALA00193 1 20010223 A 3610 BACC10KH550R CLAMP BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE BLEED AIR SYS FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 784UA 26951 FORTY MINUTES AFTER TAKE-OFF, FLIGHT HAD MULTIPLE EICAS MESSAGES FOR THEIR RIGHT ENGINE NACELLE VENT VALVE. BLEED LOOP 2 WING R STATUS MSG, BLEED LEAK R, BLEED LOSS R AND PACK R. RESET THE BLEED BUT MESSAGES CAME BACK. RETURNED TO IAD AN D LANDED OVERWEIGHT. SUPPLEMENTAL DATA UPDATE FORWARD CLAMP ON RH PACK FLOW CONTROL VALVE FOUND BROKEN. THE HOT AIR LEA KAGE TRIPPED THE OVERTEMP DETECTION SYSTEM CONTRIBUTING TO THE MULTIPLE FLIGHT DECK MESSAGES.CLAMP WAS REPLACED PER AMM 21-51-01. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001041200012 20010412 00012 NM 2001 4 12 2001UALA00218 1 20010308 A 2460 BACC45FT188P7 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CIRCUIT BREAKER BROKEN A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 593UA 28144 120 KTS STBY BUS OFF LIGHT ILLUMINATED. SELECTED STBY POWER SELECTOR TO BATTERY, OFF LIGHT WENT OUT AND DISCHARGE LIGHT ILLUMINATED. SUPPLEMENTAL DATA UPDATE REPLACED BROKEN CONNECTOR AT DC STANDBY BUSS OFF CIRCUIT BREAKER 6A3. (BOEING SPE C BACC45FT18-8P7) 2 L 7 2 4F 4 F RT A2NM E17NE 2001041200013 20010412 00013 2001 4 12 C2XA2001BT036 4 20010317 A 3140 7013348935 DAU EMB 145 EMB145LR SO E&E BAY FALSE INDICATION A C2XA O OTHER N FALSE WARNING UK UNKNOWN 1 SW 27 14972 4823 4823 145151 CREW REPORTED, BAGGAGE FIRE EXT WARNING LIGHT WILL NOT EXTINGUISH. MAINTENANCE RERACKED THE NR 1 DAU BAGGAGE FIRE EXT W ARNING LIGHT EXTINGUISHED AND REMAINED OUT. OPS CHECKED GOOD IAW EMB145 MM 26-15-01. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2001041200014 20010412 00014 NE 2001 4 12 MWEA010564 2 20010409 A 7230 500050101 FAN DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE LT ENGINE DAMAGED A MWEA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 GL 31 701ME 49760 P725386D ENROUTE TO LAX, AT 31,000 FEET CRUISE ALTITUDE, FLIGHT ATTENDANTS REPORTED LOUD BANG FOLLOWED BY VIBRATION. NO PARAMETE R CHANGES NOTICED BY COCKPIT CREW. RETURNED TO MKE. FOUND NR 1 ENGINE C1 FAN DAMAGE. REMOVED AND REPLACED NR 1 ENGIN E. 2 L 7 2 4F 4 F RT A6WE E9NE 2001041200015 20010412 00015 WP 2001 4 12 01FDEA00218 1 20010320 A 3220 PIN DOUG DC10 DC1030F 3023504 WP NLG DEFECTIVE A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 322FE 47908 NOSE GEAR DID NOT RETRACT ON T/O. REMOVED AND REPLACED NOSE GEAR PIN. AC OK TO CONTINUE. 2 L 7 3 4F RT A22WE 2001041200016 20010412 00016 SO 2001 4 12 C2XA2001BT037 1 20010319 A 2611 SMOKE DETECTOR EMB 145 EMB145ER SO LAVATORY MALFUNCTIONED A C2XA O OTHER N FALSE WARNING CL CLIMB 1 SW 27 15932 145015 CREW REPORTED, LAV SMOKE WARNING AFTER DEPARTURE WITH NO INDICATION OF SMOKE IN LAV. MAINTENANCE INSPECTED AIRCRAFT AND PERFORMED OPERATIONAL CHECK OF LAV SMOKE DETECTION SYSTEM, OPS CHECKED GOOD IAW EMB145 MM REFERENCE 26-14-00. 2 L 7 2 4F RT T00011AT 2001041200017 20010412 00017 NM 2001 4 12 MWEA010565 1 20010409 A 5330 5953050513 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE SCRATCHED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 FUSELAGE SKIN IS SCRATCHED AT STATION 265 BETWEEN LONGERONS 26 LEFT AND 25 LEFT. BLENDED DAMAGED AREA AND INSTALLED REP AIR DOUBLER. 2 L 7 2 4F RT A6WE 2001041200018 20010412 00018 NE 2001 4 12 MWEA010566 2 20010409 A 7230 500050101 FAN DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217C 52053 NE LT ENGINE DAMAGED A MWEA O OTHER E J VIBRATION/BUFFET WARNING INDICATION DE DESCENT 1 GL 31 803ME 48029 P718459D ON DECENT, HEARD A LOUD BANG AND VIBRATION FOLLOWED. INSPECTED BOTH ENGINES. FOUND LEFT ENGINE WITH C1 DAMAGE. REMOVED AND REPLACED ENGINE. 2 L 7 2 4F 4 F A6WE E9NE 2001041200019 20010412 00019 NM 2001 4 12 ASAA0110085 1 20010209 A 5310 6550568503 DOOR FRAME BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND DOOR FRAME ANGLE AT BODY STATION 947-990, LEFT BUTTOCK LINE 51 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041200020 20010412 00020 WP 2001 4 12 AALA20010220 1 20010120 A 5345 FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 TUL - FOUND FORWARD GALLEY INBOARD TIEDOWN FITTING CORRODED 2 INCHES BY 8 INCHES, STATION 160. REMOVED AND REPLACED FOR WARD INBOARD GALLEY TIE DOWN FITTING PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2001041200021 20010412 00021 NM 2001 4 12 USAABB01009 1 20010211 A 3350 873100151REV9 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 613AU 27144 LAX - FOUND FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE AT ROW 33. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001041200022 20010412 00022 NM 2001 4 12 ASAA0110092 1 20010209 A 5320 6939162 BRACKET BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND WEB BRACKET AT BODY STATION 1121-1138, WATERLINE 260 CORRODED. REPAIRED PER SRM (M) 2 L 7 2 4F A16WE 2001041200023 20010412 00023 NM 2001 4 12 ASAA0140024 1 20010210 A 5311 65582802 FRAME BOEING 737 7374Q8 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 778AS 25110 PAE - DURING MAINTENANCE INSPECTION, FOUND CRACK IN FRAME AT FASTENER AT STATION 360, WATERLINE 270, AND BUTTLINE 63 LEF T. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2001041200024 20010412 00024 WP 2001 4 12 MWEA010227 1 20010405 A 5620 5912285507 PAN DOUG DC9 DC914 3022034 WP FUSELAGE WINDOW GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 REMOVE WINDOW PAN AT WINDOW NR 19 LEFT STATION 604- STATION 623, HAS DEEP NICKS AND GOUGES. REMOVED WINDOW PAN AND 4EA CLIP, LOCATED AND DRILLED NEW PAN, FABRICATED CLIPS, INSTALLED CLIP AND NEW PAN. 2 L 7 2 4F A6WE 2001041200025 20010412 00025 WP 2001 4 12 MWEA010245 1 20010405 A 5720 39133241 SPLICE DOUG DC9 DC914 3022034 WP CENTER TANK GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 CENTER TANK STRINGER NR 11 FORWARD SPLICE HAS 2 EA. HOLES WITH DEEP GOUGES. FABRICATED AND INSTALLED SPLICE. 2 L 7 2 4F A6WE 2001041200026 20010412 00026 WP 2001 4 12 MWEA010247 1 20010405 A 5710 39133241 SPLICE DOUG DC9 DC914 3022034 WP RT WING TANK NICKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 REMOVED STRINGER 14 FORWARD SPLICE P/N 3913324-1 TO FACILITATE OTHER MAINTENANCE. FOUND NICKS, DINGS, AND SCRATCHES. LOCATED, DRILLED, FABRICATED AND INSTALLED CENTER FORWARD 14 SPLICE. 2 L 7 2 4F A6WE 2001041200027 20010412 00027 WP 2001 4 12 MWEA010375 1 20010326 A 5230 59101415 PAN DOUG DC9 DC914 3022034 WP AFT CARGO DOOR GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 SEVERAL AREAS OF GOUGES ON TOP AND BOTTOM OF OUTER PAN IN THE RADIUS AFT CARGO DOOR. BLENDED GOUGES, FABRICATED, LOCAT ED, DRILLED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001041200028 20010412 00028 WP 2001 4 12 MWEA010376 1 20010326 A 5320 5911412 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FORWARD CARGO COMPARTMENT INTERCOSTAL ASSY BETWEEN STATION 408 AND 427, LEFT OF LONGERON 30 HAS CRACKS AND LIGHT CORROSI ON. REMOVED, FABRICATED AND INSTALLED NEW INTERCOSTAL. 2 L 7 2 4F A6WE 2001041200029 20010412 00029 WP 2001 4 12 MWEA010377 1 20010326 A 5320 5935024 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 INTERCOSTAL CRACKED (2 PLACES), LONGERON 5 LEFT, STATION 766-786. -- REMOVED, FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001041200030 20010412 00030 WP 2001 4 12 MWEA010378 1 20010326 A 5313 2777922 LONGERON DOUG DC9 DC914 3022034 WP FUSELAGE TOOL DAMAGE A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 TOOLING MARKS AT LONGERON 6 LEFT UPPER INNER SIDE BETWEEN STATION 218 AND 237. BLENDED, LOCATED AND DRILLED NEW SECTIO N OF LONGERON, INSTALLED LONGERON. 2 L 7 2 4F A6WE 2001041200031 20010412 00031 WP 2001 4 12 MWEA010379 1 20010326 A 5310 2912538 SHEAR TIE DOUG DC9 DC914 3022034 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 STATION 758, BETWEEN LONGERON 16 AND 17 RIGHT, DRILL DAMAGE, FIVE LOCATIONS, DAMAGE TO SHEAR TIE AND TO OUTBOARD FACR OF FRAME IN RADIUS. REMOVED, FABRICATED, LOCATED, DRILLED AND INSTALLED SHEAR TIE. 2 L 7 2 4F A6WE 2001041200032 20010412 00032 WP 2001 4 12 MWEA010380 1 20010326 A 5320 5956034501 ANGLE DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 FORWRD CARGO COMPARTMENT DOUBLER PLATE ON FRAME STATION 370 AT LONGERON 28 LEFT HAS AMISSING NUT PLATE, MISDRILLED HOLES AND BARE METAL. REMOVED DOUBLER PLATE, FABRICATED NEW GUSSET, LOCATED AND DRILLED HOLES, REMOVED CARGO TRACK SUPPORT A NGLE, LOCATED GUSSET, FABRICATED AND DRILLED SUPPORT ANGLE, INSTALLED SUPPORT ANGLE AND GUSSET. 2 L 7 2 4F A6WE 2001041200033 20010412 00033 WP 2001 4 12 MWEA010381 1 20010326 A 5310 2912538 SHEAR TIE DOUG DC9 DC914 3022034 WP FUSELAGE TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 TOOL DAMAGE IN RADIUS OF SHEAR TIE STATION 756 LONGERON 15-17 LEFT. REMOVED SHEAR TIE, FABRICATED, LOCATED, DRILLED AN D INSTALLED NEW SHEAR TIE. 2 L 7 2 4F A6WE 2001041200034 20010412 00034 WP 2001 4 12 MWEA010382 1 20010326 A 5311 935309531 FRAME DOUG DC9 DC914 3022034 WP FUSELAGE TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 TOOL DAMAGE ON FRAME, STATION 756, LONGERON 4 RIGHT. BLENDED TOOL MARKS, CUT OUT FRAME REPAIR, MADE FILLER, LOCATED HO LES ON FILLER, INSTALLED REPAIR, BRACKET AND FASTENERS. 2 L 7 2 4F A6WE 2001041200035 20010412 00035 WP 2001 4 12 MWEA010383 1 20010326 A 5753 5912154 SKIN DOUG DC9 DC914 3022034 WP TE FLAP DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 RIGHT FLAP INBOARD TRAILING EDGE HAS NUMEROUS SMALL DENTS ON LOWER SURFACE. REMOVED RIGHT INBOARD FLAP TRAILING EDGE AND EDGE LOWER SKIN, FABRICATED NEW SKIN, INSTALLED NEW FABRICATED LOWER SKIN, INSTALLED FLAP TRAILING EDGE. 2 L 7 2 4F A6WE 2001041200036 20010412 00036 WP 2001 4 12 MWEA010384 1 20010326 A 5753 5912146 SKIN DOUG DC9 DC914 3022034 WP RT TE FLAP CANNING A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 RIGHT FLAP HAS A DENT WITH OIL CANNING ON 3RD TRAILING EDGE SECTION. REMOVED FLAP TRAILING EDGE PANEL, CUT OUT DAMAGED A REA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER, INSTALLED NR 3 FLAP TRAILING EDGE AND GAP COVERS. 2 L 7 2 4F A6WE 2001041200037 20010412 00037 WP 2001 4 12 MWEA010385 1 20010326 A 5330 5911426 SKIN DOUG DC9 DC914 3022034 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 DENT IN FUSELAGE SKIN AT STATION 710-722 BETWEEN LONGERONS 8 TO 11 RIGHT. X=.024, D=3 INCHES. REMOVED OIL CAN AREA, FAB RICATED REPAIR DOUBLER AND FINGER DOUBLER, FABRICATED 4 SHIMS, INSTALLED REPAIR DOUBLER AND SHIMS. 2 L 7 2 4F A6WE 2001041200038 20010412 00038 WP 2001 4 12 MWEA010386 1 20010326 A 5320 9911499 STRUCTURE DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 REMOVED LOWER SHEAR CLIP ON BULKHEAD STRINGER 21-22 TO FACILITATE OTHER MAINTENANCE. BLENDED CORROSION, LOCATED, DRILL ED AND INSTALLED REPLACEMENT CLIP, DOME SEALED. 2 L 7 2 4F A6WE 2001041200039 20010412 00039 WP 2001 4 12 MWEA010387 1 20010326 A 5410 5923938 STIFFENER DOUG DC9 DC914 3022034 WP RT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 RIGHT PYLON SUPPORT STIFFNER HAS A CRACK, LOCATED ABOVE 13TH STAGE AIR DUCT. REMOVED FASTENER, FABRICATED AND INSTALLE D DOUBLER. 2 L 7 2 4F A6WE 2001041200040 20010412 00040 WP 2001 4 12 MWEA010388 1 20010326 A 5712 99116084 RIB DOUG DC9 DC914 3022034 WP RT WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 RIGH WING FUEL TANK, WING RIB CRACKED AT STATION 164 AT LOWER LEG INBOARD SIDE BETWEEN STRINGER 15 AND 16. FABRICATED, LOCATED, DRILLED AND INSTALLED PARTS. 2 L 7 2 4F A6WE 2001041200041 20010412 00041 NM 2001 4 12 2001UALA00177 1 20010303 A 3260 CIRCUIT BREAKER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NLG INDICATOR MALFUNCTIONED A UALA O OTHER N FALSE WARNING LD LANDING 1 WP 29 327UA 24147 NOSE GEAR UNSAFE LIGHT ON WHEN THE GEAR WAS EXTENDED FOR LANDING. SUPPLEMENTAL DATA UPDATE RESET BREAKER C404 AND NORMAL GEAR INDICATION RETURNED. REPLACED THE BREAKER AS A PRECAUTION. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041200042 20010412 00042 NM 2001 4 12 2001UALA00180 1 20010302 A 2530 OVEN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GALLEY CONTAMINATED A UALA F A ACTIVATE FIRE EXT. UNSCHED LANDING A FLAME/FIRE CL CLIMB 1 WP 29 521UA 24891 CABIN CREW REPORT FLAMES IN FORWARD GALLEY. SUPPLEMENTAL DATA UPDATE FLAMES IN GALLEY OVEN CAUSED BY PAPER STUCK IN VENT . REPLACED OVEN. NO DAMAGE TO AIRCRAFT. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041200043 20010412 00043 SO 2001 4 12 COMA0110061 1 20010312 A 5310 12034416002 SHEAR TIE EMB 120 EMB120RT SO FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 120264 DURING 2C CHECK TASK 5310-222-05I, THE RT FUSELAGE SKIN SUPPORT AT FRAME 9, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 660-1, REV IR, 2-16-93. 2 L 7 2 4T RT A31SO 2001041200044 20010412 00044 SO 2001 4 12 COMA0110062 1 20010312 A 5410 12003878001 STIFFENER EMB 120 EMB120RT SO NACELLE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 21213 120264 DURING 2C CHECK TASK 5410-442-04I, THE RT NACELLE FRAME 10 STIFFENER ANGLE, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001041200045 20010412 00045 SO 2001 4 12 COMA0110063 1 20010312 A 5320 12034416001 SUPPORT EMB 120 EMB120RT SO FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 120264 DURING 2C CHECK TASK 5310-221-05I, THE LT FUSELAGE SKIN SUPPORT AT FRAME 9, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 660-1, REV IR, 2-16-93. 2 L 7 2 4T RT A31SO 2001041200046 20010412 00046 SO 2001 4 12 COMA0110065 1 20010312 A 5330 12019737003 SKIN EMB 120 EMB120RT SO FUSELAGE GOUGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 21213 120264 DURING 2 YEAR CORROSION CHECK TASK 5310-132-CO1E, THE FUSELAGE LOWER SKIN WAS FOUND TO BE GOUGED JUST BELOW THE LAV DUMP VALVE DOUBLER. THE SKIN WAS REPAIRED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND EMBRAER REPAIR FAX GST-0738 /01. 2 L 7 2 4T RT A31SO 2001041200047 20010412 00047 SO 2001 4 12 COMA0110067 1 20010312 A 5320 12046158603 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 7922 120264 DURING 2C CHECK TASK 142-01Z, THE RT FLOORBEAM BUTTSTRAP WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH E MB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 2174-1, REV IR, 1-15-97. 2 L 7 2 4T RT A31SO 2001041200048 20010412 00048 SO 2001 4 12 COMA0110068 1 20010312 A 5413 12041441001 STRINGER EMB 120 EMB120RT SO LT NACELLE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 21213 120264 DURING 2C CHECK TASK 5410-432-04I, THE LEFT NACELLE OUTBOARD STRINGER NR 1 WAS FOUND TO BE CRACKED JUST AFT OF NACELLE F RAME 10. THE STRINGER WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001041200049 20010412 00049 SO 2001 4 12 COMA0110069 1 20010312 A 5320 12006159501 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 21213 120264 DURING 2C CHECK TASK 162-01Z, THE FORWARD RT FLOORBEAM BUTTSTRAP IN THE CARGO COMPARTMENT, WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001041200050 20010412 00050 SO 2001 4 12 COMA0110071 1 20010312 A 5320 12006218001 SUPPORT EMB 120 EMB120RT SO FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 21213 120264 DURING 2C CHECK TASK 261-01Z, THE FUSELAGE LT SKIN SUPPORT AT FRAME 40, BETWEEN STRINGERS 3L AND 4L, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001041200051 20010412 00051 SO 2001 4 12 COMA0110072 1 20010312 A 5310 12014309001 SUPPORT EMB 120 EMB120RT SO COCKPIT CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 21213 120264 DURING 2C CHECK TASK 5310-221-05I, THE FUSELAGE LT SKIN SUPPORT BEHIND AND ABOVE THE CAPTAIN''S DV WINDOW, BETWEEN FRAME S 12A AND 13, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001041200052 20010412 00052 SO 2001 4 12 COMA0110073 1 20010312 A 5310 12012545001 SUPPORT EMB 120 EMB120RT SO COCKPIT CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 21213 120264 DURING 2C CHECK TASK 5310-221-05I, THE FUSELAGE LT SKIN SUPPORT BEHIND THE CAPTAIN''S DV WINDOW, BETWEEN FRAMES 12A AND 13, WAS FOUND CRCKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001041200053 20010412 00053 SO 2001 4 12 COMA0110074 1 20010312 A 5320 12035891001 SUPPORT EMB 120 EMB120RT SO FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 21213 120264 DURING 2C CHECK TASK 232-01Z, THE FUSELAGE RT SKIN SUPPORT AT FRAME 13A, STRINGER 14R WAS FOUND CRACKED. THE PART WAS R EPAIRED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3653-2, REV IR, 11-7-00. 2 L 7 2 4T RT A31SO 2001041200054 20010412 00054 WP 2001 4 12 MWEA010403 1 20010328 A 5321 99579249 FLOOR PANEL DOUG DC9 DC914 3022034 WP FUSELAGE MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 FLOOR PANEL B6 HAS 2 REPAIRS OF WRONG TYPE. FABRICATED NEW SKIN AND HAT CHANNELS, LOCATED, DRILLED AND INSTALLED HAT C HANNELS. 2 L 7 2 4F A6WE 2001041200055 20010412 00055 WP 2001 4 12 MWEA010411 1 20010328 A 5321 995791819 FLOOR PANEL DOUG DC9 DC914 3022034 WP FUSELAGE MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 FLOOR PANEL A4 HAS A REPAIR OF THE WRONG TYPE. REMOVED HAT CHANNELS, FABRICATED NEW SKIN, INSTALLED HAT CHANNELS. 2 L 7 2 4F A6WE 2001041200056 20010412 00056 WP 2001 4 12 MWEA010421 1 20010328 A 5321 995791921 FLOORBOARD DOUG DC9 DC914 3022034 WP FUSELAGE BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FLOORBOARD E9 HAS ONE END THAT IS BENT AND HAS A CRACK BY A FASTENER. -- FABRICATED NEW SKIN, INSTALLED HAT CHANNELS A ND INSULATION. 2 L 7 2 4F A6WE 2001041200057 20010412 00057 SO 2001 4 12 COMA0110075 1 20010312 A 5720 12017063009 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 21213 120264 DURING 2C CHECK TASK 5720-552-01I, THE LT WING UPPER SUPPORT AT RIB 20, BETWEEN STRINGERS 3A AND 4A, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRCTICES. 2 L 7 2 4T RT A31SO 2001041200058 20010412 00058 SO 2001 4 12 COMA0110076 1 20010312 A 5720 12017060007 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 21213 120264 DURING 2C CHECK TASK 5720-552-01I, THE LT WING SUPPER SKIN SUPPORT AT RIB 20, BETWEEN STRINGERS 2A AND 3A, WAS FOUND CRA CKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001041200059 20010412 00059 SO 2001 4 12 COMA0110079 1 20010312 A 5320 12014241001 CROSSBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 21213 120264 DURING 2C CHECK TASK 131-01Z, THE FUSELAGE LT FLOOR CROSSBEAM AT FRAME 15 WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001041200060 20010412 00060 SO 2001 4 12 COMA0110080 1 20010312 A 5320 12046158003 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 21213 120264 DURING 2C CHECK TASK 141-01Z, THE FUSELAGE LT FLOORBEAM BUTT STRAP WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDA NCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 2174-1, REV IR, 1-15-97. 2 L 7 2 4T RT A31SO 2001041200061 20010412 00061 SO 2001 4 12 COMA0110081 1 20010312 A 5320 12061603601 FLOOR SUPPORT EMB 120 EMB120RT SO FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 21213 120264 DURING 2C CHECK TASK 121-01Z, THE FUSELAGE LT FLOOR PROP AT FRAME 13 WAS FOUND CRACKED. THE PART WAS REPAIRED IN ACCORD ANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3647-1, REV IR, 5-3-00. 2 L 7 2 4T RT A31SO 2001041200062 20010412 00062 EA 2001 4 12 COMA0160317 1 20010313 A 2621 365000183 FIRE BOTTLE CNDAIR CL600 CL6002B19 EA CARGO BAY LOW A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 983CA 14363 7169 CARGO FIRE BOTTLE LOW MESSAGE. REPLACED THE FIRE BOTTLE. 2 L 7 2 4F RT A21EA 2001041200063 20010412 00063 EA 2001 4 12 COMA0160318 1 20010313 A 3350 20131A BATTERY CNDAIR CL600 CL6002B19 EA CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 963CA 12018 7127 EMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY LIGHTS BATTERY. 2 L 7 2 4F RT A21EA 2001041200064 20010412 00064 EA 2001 4 12 COMA0160319 1 20010314 A 3397 6464 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN DEFECTIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 937CA 7044 EMERGENCY FLOOR LIGHTING AT ROW 8 IS INOPERABLE. REPLACED THE LIGHT CABLE ASSY. 2 L 7 2 4F RT A21EA 2001041200065 20010412 00065 WP 2001 4 12 MWEA010502 1 20010402 A 5312 4911484514N CLIP DOUG DC9 DC914 3022034 WP BULKHEAD CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 REMOVED SHEAR CLIP RIGHT WING ON BULKHEAD 69 BETWEEN STRINGER 12-13 TO FACILITATE OTHER MAINTENANCE. CLIP HAS TOOL DAM AGE, BLENDED CORROSION, REMOVED, LOCATED, DRILLED AND INSTALLED CLIP. 2 L 7 2 4F A6WE 2001041200066 20010412 00066 SO 2001 4 12 C2XA01IA161 1 20010315 A 3397 7287580507 WIRE EMB 145 EMB145LR 3260212 SO CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12921 145354 IAH - DURING 2A INSPECTION, THE AFT AISLE PATH LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN W IRE ON THE LIGHT STRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001041200067 20010412 00067 EU 2001 4 12 C2XA01IA162 1 20010312 A 2150 22044004 ACM AEROSP ATR42 ATR42320 8680930 EU AC BAY OVERHEATED A C2XA O OTHER M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 14815 104 IAH - FLIGHT 3431, THE CREW REPORTED THAT THE NUMBER TWO PACK OVERHEATED FOLLOWED BY A BURNING SMELL. MAINTENANCE REMOV ED AND REPLACED THE NUMBER TWO AIR CYCLE MACHINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001041200068 20010412 00068 2001 4 12 MWEA010341 4 20010315 A 3425 5223908001 ADI DOUG DC9 DC932 3022066 WP COCKPIT DEFECTIVE A MWEA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 31 206ME 47791 CAPTAINS ADI FOGGED OVER. REMOVED AND REPLACED CAPTAINS ADI, OPS CHECK GOOD. 2 L 7 2 4F A6WE 2001041200069 20010412 00069 WP 2001 4 12 MWEA010343 1 20010314 A 5311 99115076 FRAME DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 DAMAGE TO FRAME AT STATION 94.550. REMOVED DAMAGE AND INSTALLED REPAIR ANGLES. 2 L 7 2 4F A6WE 2001041200070 20010412 00070 WP 2001 4 12 MWEA010344 1 20010316 A 5320 5910160 WEB DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 WEB HAS NUMEROUS HOLES WITH IMPROPER SPACING STATION 503. REMOVED WEB, FABRICATED AND LOCATED NEW WEB, FABRICATED L-DOU BLER, INSTALLED DOUBLER AND WEB. 2 L 7 2 4F A6WE 2001041200071 20010412 00071 WP 2001 4 12 MWEA010345 1 20010316 A 5311 9958200 FRAME DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 STATION 525 FRAME HAS NUMEROUS HOLES WITH IMPROPER SPACING BETWEEN LONGERON 11-15 LEFT. PLUGGED HOLES, FABRICATED, LOCA TED, DRILLED AND INSTALLED REPAIR STRAP. 2 L 7 2 4F A6WE 2001041200072 20010412 00072 WP 2001 4 12 MWEA010346 1 20010316 A 5347 2772660 SEAT TRACK DOUG DC9 DC914 3022034 WP CABIN DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 SEAT TRACK NR 1 HAS ELONGATED IN LOWER FLANGE COMMON TO FLOOR SUPPORT AT STATION 642 LEFT. REMOVED SEAT TRACK, FABRICAT ED NEW SECTION OF SEAT TRACK AND SPLICE ASSEMBLY, INSTALLED SEAT TRACK. 2 L 7 2 4F A6WE 2001041200073 20010412 00073 WP 2001 4 12 MWEA010347 1 20010316 A 5320 3914617510 FLOOR SUPPORT DOUG DC9 DC914 3022034 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FLOOR SUPPORT AT STATION 566 LEFT SIDE BETWEEN SEAT TRACKS NR 1 AND NR 2 HAS ELONGATED HOLES AND IS BENT. REMOVED, FABR ICATED AND INSTALLED FLOOR SUPPORT. 2 L 7 2 4F A6WE 2001041200074 20010412 00074 WP 2001 4 12 MWEA010350 1 20010316 A 5320 59101607 WEB DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 WEB CRACKED, (P/N 5910160-7) AFT OF STATION 525, LONGERON 15 LEFT. REMOVED, FABRICATED, LOCATED, DRILLED AND INSTALLED WEB. 2 L 7 2 4F A6WE 2001041200075 20010412 00075 WP 2001 4 12 MWEA010351 1 20010316 A 5330 59114161 SKIN DOUG DC9 DC914 3022034 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FUSELAGE SKIN UNDER FAIRING RIB HAS MECHANICAL DAMAGE FROM SCREWS STATION 484 BETWEEN LONGERON 18 LEFT AND 19 LEFT. BLE NDED GOUGES, FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001041200076 20010412 00076 WP 2001 4 12 MWEA010352 1 20010316 A 5410 95400027 STIFFENER DOUG DC9 DC914 3022034 WP RT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 RIGHT PYLON OUTER LOWER STIFFENER HAS A 1 INCH CRACK AT STATION 858. FABRICATED AND INSTALLED DOUBLER AND ANGLES. 2 L 7 2 4F A6WE 2001041200077 20010412 00077 2001 4 12 01FDEA00202 4 20010315 A 3140 COMPUTER AIRBUS 300 A300F4605R 3930327 EU COCKPIT FAULTY A FDEA O OTHER G J MULTIPLE FAILURE WARNING INDICATION DE DESCENT 1 SO 25 667FE 771 ON T/O ECAM WENT CRAZY, GALLEY SHED ON, NR 1 PITCH TRIM DISCONNECTED AND WOULD NOT RESET. NR 1 PRESS REG FAILED. POS 1 LAND GEAR INOP, ACARS RINGER INOP, NR 1 FLT DIR INOP, APU LOOP-B FAULT. 2 L 7 2 4F RT A35EU 2001041200078 20010412 00078 EA 2001 4 12 SWIA972433 1 20010315 A 2916 RESERVOIR CNDAIR CL600 CL6002B19 EA HYD SYSTEM FAILED A SWIA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 NM 07 410SW 7066 AFTER TAKEOFF SELECTED GEAR UP AND HYDRAULIC NUMBER THREE LOW PRESSURE CAUTION CAME ON, FOLLOWED BY GEAR UP DISAGREE (BO TH MAIN GEAR). ALSO, NOSE DOOR OPEN WARNING MESSAGE CAME ON. NOTED NUMBER THREE HYDRAULIC SYSTEM FAILURE (3A & 3B PUMP PSI 0). RETURNED TO PSC. REPLACED HYDRAULIC NUMBER THREE RESERVOIR AND BOTH HYDRAULIC PUMPS. CHANGED FILTERS AND LEA K CHECK SYSTEM IAW 29-12-00. JACKED AIRCRAFT AND PERFORMED LANDING GEAR CHECK. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2001041200079 20010412 00079 2001 4 12 SWIA972435 4 20010311 A 3425 COMPARATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT FAILED A SWIA A UNSCHED LANDING I J FLT. ATTITUDE INST. WARNING INDICATION CL CLIMB 1 NM 07 292SW 120319 NUMBER ONE EHSI RED HDG FLAG AND HDG FAILURE DURING FLIGHT. RETURNED TO PDX. REPLACED NUMBER ONE AHC85 AND INITIALIZAT ION PROCEDURE WAS PERFORMED. SYSTEM OPS CHECK GOOD. ALL PANELS SECURE. P/N: 622-6190-204, S/N ON: 1121, S/N OFF: 1059. 2 L 7 2 4T 4 T RT A31SO E20NE 2001041200080 20010412 00080 NE 2001 4 12 SWIA972436 2 20010316 A 7321 ENGINE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE MALFUNCTIONED A SWIA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 NM 07 209SW 120269 LEFT ENGINE DID NOT SPOOL UP WITHIN NORMAL PARAMETERS AS DID THE RIGHT ENGINE ON TAKEOFF ROLL. AS A RESULT ABORTED TAKE OFF. RAN BOTH ENGINES TO TAKEOFF POWER SEVERAL TIMES. BOTH ENGINES ACCELERATED NORMAL. ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001041200081 20010412 00081 NM 2001 4 12 2001UALA00272 1 20010317 A 5230 TEE CHORD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 309UA 23670 FORWARD CARGO DOOR CROSSBEAM AFT END OUTER TEE CHORD CRACKED. REPAIRED CRACKED TEE CHORD. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041200082 20010412 00082 SO 2001 4 12 SWIA972437 1 20010318 A 2752 3203001007 ACTUATOR EMB 120 EMB120RT SO PWA 118 PW118 NE RT FLAP FAULTY A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 269UE 120194 EN ROUTE AT FL230 CONTROL FAULT LIGHT ILLUMINATED, WOULD NOT RESET. WEIGHTED FLAP AVERAGE WAS ZERO. LANDED WITH 0 DEGR EES FLAPS. FOUND RIGHT HAND OUTBOARD FLAP ACTUATOR EXTERNAL READING AT 820-R. REMOVED AND REPLACED ACTUATOR. OPS CHEC KS ACTUATOR IAW 27-50-00 RI I 27-307 P/N ON 3203001007, S/N ON 0315, S/N OFF 0971. REMOVED AND REPLACED FLAP ANNUNCIAT OR. OPS CHECK GOOD. P/N ON 3069001005, S/N ON 0037, S/N OFF 0010. FOUND INCORRECT (SOFTWARE LEVEL) FCU INSTALLED, REM OVED AND REPLACED OPS CHECK GOOD WITH NO FAULT FOUND ON GROUND IAW. P/N ON 307500-1007, S/N ON 0092, S/N OFF 0181. 2 L 7 2 4T 4 T RT A31SO E20NE 2001041200083 20010412 00083 SO 2001 4 12 C2XA01IA168 1 20010318 A 3397 W182000924 WIRE EMB 120 EMB120ER 3260203 SO CABIN DISCONNECTED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16724 120171 IAH - FLIGHT 2904, DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT A RED EMERGENCY AISLE PATH LIGHT WAS INOPERATIV E. MAINTENANCE RECONNECTED A WIRE ON THE AFFECTED LIGHT AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001041200084 20010412 00084 SO 2001 4 12 C2XA01IA166 1 20010314 A 4930 161544100 TANK EMB 120 EMB120ER 3260203 SO APU ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 58733 120197 IAH - FLIGHT 3420, THE CREW REPORTED THAT THE APU BLEED CAUSED A FUEL SMELL IN THE CABIN. MAINTENANCE DRAINED THE APU E PA TANK, OPERTAIONALLY CHECKED THE APU AND PACKS SYSTEM WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001041200085 20010412 00085 SO 2001 4 12 C2XA01IA167 1 20010312 A 3350 03092022 CONNECTOR EMB 120 EMB120ER 3260203 SO CABIN DISCONNECTED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 51726 120174 IAH - DURING MAINTENANCE INSPECTION, THE FORWARD ROW OF AISLE PATH EMERGENCY LIGHTS WAS FOUND TO BE INOPERATIVE. MAINTE NANCE RECONNECTED THE EMERGENCY LIGHTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001041200086 20010412 00086 NM 2001 4 12 EISA20010040 1 20010214 A 5347 BAC1520792 SEAT TRACK BOEING BOEING 727 727223 1384074 NM UPPER CARGO BAY CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION ON MAIN CABIN CARGO COMPARTMENT LEFT O/B SEAT TRACK SECTION BS 720C TO 720E LBL 45. FABRICATED AND INSTALLED SEAT TRACK SPLICE AT BS 720C TO BS 720E LBL 45, ALODINED AN DPRIMED IAW SRM 53-1 0-7 FIG 7, 53-10-5, 51-30-2. 2 L 7 3 4F A3WE 2001041200087 20010412 00087 NM 2001 4 12 2001UALA00219 1 20010311 A 5414 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 NR 2 ENGINE PYLON IB SKIN CRACKED AT FWD LIGHTING HOLE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REPAIRED SKIN PER MAINTENANCE MANUAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041200088 20010412 00088 WP 2001 4 12 MWEA010487 1 20010330 A 5531 5912125501 SPAR CAP DOUG DC9 DC932 3022066 WP VERTICAL STAB MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 209ME 47730 MISDRILLED HOLE GOING THROUGH SPAR CAP LEFT SIDE OF VERTICAL STABILIZER, BELOW HORIZONTAL STABILIZER LEADING EDGE. DRI LLED HOLE, FABRICATED AND INSTALLED BUSHINGS. 2 L 7 2 4F A6WE 2001041200089 20010412 00089 EU 2001 4 12 2001UALA00237 1 20010313 A 3610 ABS73772 SEAL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT ENGINE LEAKING A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 436UA 638 RIGHT WING AIR LEAK. SUPPLEMENTAL DATA UPDATE FOUND ENGINE BLEED AIR SUPPLY DUCT JOINT LEAK IN RIGHT HAND WING LEADING E DGE. REPLACED DETERIORATED SEAL. NO FURTHER FAULTS REPORTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2001041200090 20010412 00090 NM 2001 4 12 2001UALA00248 1 20010312 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 FUSELAGE REPAIR DOUBLER AT STA 1300 STR 24L DOES NOT MEET MINIMUM FASTENER SPACING. SUPPLEMENTAL DATA UPDATE MAJOR REPA IR ACCOMPLISHED.REPAIRED SKIN PER SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001042400190 20010424 00190 NM 2001 4 24 2001UALA00264 1 20010319 A 3350 D7170201 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN MISSING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 773UA 26929 EMERGENCY LIGHT AT 1E HANGING OUT OF SEAT. FOUND LIGHT ASSY MISSING. EMERGENCY FLOOR PROX LIGHT WILL NOT TEST ROW 1 T O 9. SUPPLEMENTAL DATA UPDATE PROBABLE CAUSE OF MISSING LIGHT ASSY: PASSENGER LUGGAGE OR GALLEY CART IMPACTED THE EEL LI GHT ASSY, CAUSING THE EEL LIGHT ASSY TO BECOME SEPARATED FROM THE SEAT ASSEMBLY. CORRECTIVE ACTION FOR MISSING LIGHT ASS EMBLY: REPLACED EEL LIGHT ASSY AT SEAT 1E. CAUSE OF EMERGENCY FLOOR PROX LIGHTS NOT TESTING IN ROWS 1 TO 9: FOUND BATT ERY PACK AT DOOR 1 RIGHT AT FAULT.CORRECTIVE ACTION FOR EMERGENCY FLOOR PROX LIGHTS NOT TESTING IN ROWS 1 TO 9:REPLACED BATTERY PACK ASSY AT DOOR 1 RIGHT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001041200091 20010412 00091 NM 2001 4 12 2001UALA00269 1 20010317 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 GOUGE IN FRAME AT STA 1500 STR 26L. 35 PERCENT MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME AT STA 1500 ST R 26L PER SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041200092 20010412 00092 WP 2001 4 12 MWEA010355 1 20010316 A 5620 5912285505 WINDOW FRAME DOUG DC9 DC914 3022034 WP CABIN CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 WINDOW FRAME BETWEEN STATION 525 - 544 (LEFT SIDE) IS CHAFED IN RADIUS. LOCATED, DRILLED AND INSTALLED NEW WINDOW RETAI NER. 2 L 7 2 4F A6WE 2001041200093 20010412 00093 NE 2001 4 12 QXEA0100281 2 20010316 A 7200 ENGINE DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE NR 1 & NR 2 ENG MALFUNCTIONED A QXEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 09 367PH 511 SEA - NR 1 AND 2 TORQUE SURGE 5 PERCENT TO 8 PERCENT ON CLIMB AND 3 PERCENT TO 5 PERCENT AT 65 PERCENT TORQUE. NO SURGE BELOW 60 PERCENT NOTED. CREW REQUESTED A RETURN TO SEA. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT DOWN FOR MAINTENA NCE. 2 H 7 2 4T 4 T RT A13NM E20NE 2001041200095 20010412 00095 NM 2001 4 12 2001UALA00271 1 20010317 A 5230 BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 309UA 23670 AFT CARGO DOOR LOWER CROSS BEAM CRACKED. REPAIRED CRACKED CROSS BEAM. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041200096 20010412 00096 NM 2001 4 12 2001UALA00273 1 20010319 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 501UA 24622 FUSELAGE SKIN DENTED AT STA 1600 BETWEEN STR 19LT AND 20LT. MAJOR REPAIR ACCOMPLISHED.REPAIRED SKIN PER SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041200097 20010412 00097 NM 2001 4 12 2001UALA00274 1 20010307 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CROWN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 FUSELAGE UPPER CROWN SKIN HAS A MATERIAL LOSS UNDER THE VHF ANTENNA. INSTALLED A DOUBLER TO THE AFFECTED AREA. MAJOR R EPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041200098 20010412 00098 NM 2001 4 12 2001UALA00275 1 20010319 A 5330 STRUCTURE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 916UA 25383 NR 2 VHF ANTENNA INTERIOR SUPPORT STRUCTURE SHOWS SIGNS OF FAILURE. REPLACED SUPPORT CHANNEL. MAJOR REPAIR ACCOMPLISHE D. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041200099 20010412 00099 WP 2001 4 12 MWEA010353 1 20010316 A 5330 59114113 SKIN DOUG DC9 DC914 3022034 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 DENT IN PRESSURIZED FUSELAGE SKIN AT STATION 251-276. 1 TO 3 INCHES ABOVE LONGERON 21 RIGHT, D=2.5 INCH, A=.030, B=.012, X=.042, D/X= 59, TOTAL LENGTH= 25.5 INCHES. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS. 2 L 7 2 4F A6WE 2001041200100 20010412 00100 NM 2001 4 12 DHL2001741501 1 20010310 A 7110 SKIN BOEING 727 7272Q9 138448M NM COWLING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 NR 3 ENGINE UPPER COWL, O/B NR 4 LATCH CUTOUT IS CRACKED IN 2 CORNERS. CUT OUT DAMAGED AREA AT NR 3 ENG UPPER COWL O/B NR 4 LATCH CUT-OUT CRACK AS PER B727 SRM 54-10-3 FIG 5 MAT LOSS 1 X.5 INCH. REMOVED EXISTING REPAIR IAW B727 SRM 51-30- 2. INSTALLED EXTERNAL DOUBLER REPAIR AS PER B727 SRM 54-10-3 FIG 5. MAT USED 2024T3 .050 5 X 10 INCH LOT 240318 PO 831 12055. ALODINED AND PRIMED AS PER B727 SRM 51-10-2. 2 L 7 3 4F RT A3WE 2001041200101 20010412 00101 NM 2001 4 12 DHL2001741502 1 20010309 A 5321 FLOORBOARD BOEING 727 7272Q9 138448M NM CABIN CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 CORROSION ON AND FLOOR SUPPORT STRUCTURE FROM FS STA 303 TO FS 344 AND FROM RBL 16 TO RBL 55 (UNDER FWD LAV). REMOVED C ORROSION AS PER B727 SRM 51-10-6 MATERIAL LOSS .030 FOUND OUT OF LIMITS AS PER B727 SRM 53-30-01. REPLACED FLOORBOARDS SUPPORT PO 8B12244 LOT 11154-1 AND 8311094 LOT 168979-1-1 P/N AND10137-1105 AND P/N BAC1505-100617 DIMENSION 28.75 X 2 I NCHES AND 15 X 2 INCHES IAW B727 SRM 53-30-8 FROM STA 312 RBL 16 TO RBL 50. ALODINED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED FLOORBOARD SUPPORT IAW B727 SRM 53-30-8 51-30-2 OK TO INSTALL FLOOR PANEL. FABRICATE AND INSTALLED NEW FLOOR PANEL AT FWD LAV FROM STA 303 TO 344 RBL 16-RBL 55 AS PER B727 SRM 53-20-1 FIG 1- MAT USED AE4155. 2 L 7 3 4F RT A3WE 2001041200102 20010412 00102 NM 2001 4 12 DHL2001741503 1 20010308 A 5320 FLOOR SUPPORT BOEING 727 7272Q9 138448M NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 CABIN FLOOR SUPPORT STA 743 LBL 24.75 TO 45.5 HAS A CRACK. REMOVED AND REPLACED MED STRAP-FLOOR SUPPORT STA 743 LBL 24. 75 TO 45.5. MAT USED 7075T6 .040 PO 8311935 LOT 219081 SIZE 16.5 X 2 INCHES AS PER B 727 SRM 51-20-2. TREATED, ALODINED AND PRIMER AS PER B727 SRM 51.10.6. 2 L 7 3 4F RT A3WE 2001041200103 20010412 00103 NM 2001 4 12 DHL2001741504 1 20010308 A 5320 WEB BOEING 727 7272Q9 138448M NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 CABIN FLOOR WEB CORRODED AT SEVERAL AREAS FROM STA 1183 TO 1148 LBL 24 TO LBL 62. CUT OUT DAMAGED AREAS AT CABIN FLOOR WEB STA 1183 TO 1148 LBL 24 TO LBL 62 IN SEVERAL SECTIONS IAW B727 SRM 51-40-2 FIG 1 MAT USING 2024-T3 .063 10 X 38 INCH ES PO 83110575 LOT 890YAFG.P. TREATED AND PRIMED REPAIR DOUBLER IAW B727 SRM 51-10-2. INSTALLED REPAIR DOUBLER IAW B72 7 SRM 51-40-2 PAGE 1. 2 L 7 3 4F RT A3WE 2001041200104 20010412 00104 NM 2001 4 12 DHL2001741505 1 20010312 A 2810 FUEL TANK BOEING 727 7272Q9 138448M NM CTR WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 CORROSION AT CTR WING TANK LWR SURFACE, INSIDE RT A/C BAY PLENUM, APPROX BS 830. REMOVED FASTENERS FOR ACCESS AS PER B7 27 SRM 51-30-2. REMOVED RT PRIMARY AND SECONDARY HEAT EXCHANGER AND PLENUM ASSY FOR SM ACCESS B727 MM 21-50-21. REMOVE D CORROSION AT CTR WING TANK LOWER SURFACE I/B A/C PLENUM FROM STA 830 TO 839 RBL 32 TO 23 INCHES AS PER B727 SRM 51-10- 6. PERFORMED HFEC INSPECTION AT AREA PER NDT PART 6,51-00-00 FIG 4. NO DEFECTS NOTED. PERFORMED THICKNESS CHECK OF L OWER SKIN BS 830 TO 839.0 RBL 32 TO 23 PER PANAMETRICS MANUAL 910-131B, LOWEST READINGS .109,SEVERAL AREAS OUT OF LIMITS . REMOVED INTERNAL DOUBLER RBL 32 TO RBL 13 STA 830 AS PER B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2001041200105 20010412 00105 NM 2001 4 12 DHL2001741506 1 20010309 A 5753 SKIN BOEING 727 7272Q9 138448M NM T/E FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 RT I/B MID FLAP UPPER SURFACE DELAMINATED AREA AT I/B TRAILING EDGE AREA (MKD). INSTALLED BOND REPAIR TO I/B MID FLAP U PPER SURFACE AT I/B TRAILING EDGE AREA AS PER B727 SRM 51-40-6 PAGE 7 MATERIAL USED ADHESIVE AF 163-2K 085 PO 2429 AND A LUMINUM 7075-T6 016 PO 3083 SIZE OF REPAIR 15 X 4 INCHES. 2 L 7 3 4F RT A3WE 2001041200106 20010412 00106 NM 2001 4 12 DHL2001741507 1 20010310 A 5711 SPAR BOEING 727 7272Q9 138448M NM RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 RIGHT WING LOWER SPAR HAS EXFOLIATED CORROSION UNDER CAVITY CUT OUT FOR NR 8 LEADING EDGE SLAT ACTUATOR. REMOVE L/E ACC ESS PANELS 6542, 6543, 6546, AND 6540 AT RIGHT WING LOWER SURFACE AS PER B727 SRM 51-30-2. REMOVED FUEL ACCESS PANELS 1 7, 18, 19 AT RIGHT WING LOWER SURFACE FOR ACCESS TO WORK AS PER B727 SRM 51-30-2. REMOVED FUEL DUMP PLUMBING AT RIGHT W ING STATION 738.50 IAW M/M B72728-31-31. REMOVED I/B AND O/B ANGLE ACTUATOR SUPPORT AND INNER BOX AT NR 8 LEADING EDGE FLAP AS PER B727 SRM 51-30-2. CUT OUT RT WING LOWER SPAR STA 749 TO STA 726.68 AS PER B727 SRM 57-10-6 21.75 INCHES LON G. REMOVED 4 L/E ACCESS PANEL SUPPORT W/S 740 TO 720 AS PER B727 SRM 51-30-2. REMOVED OLD SEALANT. 2 L 7 3 4F RT A3WE 2001041200107 20010412 00107 NM 2001 4 12 01FDEA00207 1 20010317 A 2121 215201 GASPER FAN BOEING 727 727233 138408A NM CABIN SHORTED A FDEA G O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 25 276FE 22041 AIR CREW SMELL SULFUR ODOR IN COCKPIT, DONNED 02 MASK AND SMOKE GOGGLES. FLT ENG THOUGHT ODOR WAS COMING FROM GASPER FA N. INSP AC AND CARGO WITH FIRE DEPT, NOTHING FOUND. AFT OFF LOAD PRESS AC HAD ELECTRICAL ODOR COMING OUT GASPER. GASP ER FAN CIRCUIT BREAKER POPPED AND WHEN RESET POPPED AGAIN. *S/D* REMOVED AND REPLACED GASPER FAN PER MM 21-23-011-4. 2 L 7 3 4F RT A3WE 2001041200108 20010412 00108 EU 2001 4 12 C2XAO1CLO61 1 20010319 A 3350 3011210 LIGHT AEROSP ATR42 ATR42320 8680930 EU PAX DOOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14829 181 CLE DURING LINE/WEEKLY INSPECTION MAINTANCE DISCOVERED PASSENGER DOOR STAIR EMERGENCY LIGHT INOPERATIVE. MAINTANCE REMO VED AND REPLACED EMERGENCY LIGHT ASSEMBLY. PERFORMED OPERATIONAL CHECKS AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001041200109 20010412 00109 SO 2001 4 12 C2XA01BT038 1 20010320 A 2611 FDS765A2 SMOKE DETECTOR EMB 145 EMB145ER SO LAVATORY FALSE INDICATION A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 15932 145015 FLIGHT CREW REPORTED, LAV SMOKE DETECTOR IS GIVING NUMEROUS FALSE WARNINGS IN FLIGHT. MAINTENANCE REMOVED AND REPLACED LAV SMOKE DETECTOR SENSOR IAW EMB145 MM REFERENCE 26-14-01, OPS CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2001041200110 20010412 00110 CE 2001 4 12 C2XAO1CL062 1 20010316 A 3260 GE327 WARNING LIGHT BEECH 1900 1900D 1154162 CE COCKPIT INOPERATIVE A C2XA K NONE L NO TEST NR NOT REPORTED 1 SW 27 81553 UE222 CLE FLIGHT 3108 THE CREW REPORTED BOTTOM RED GEAR UNSAFE LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED LAMP AND PERFORMED OPERATIONAL CHECKS. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 2001041200111 20010412 00111 WP 2001 4 12 MWEA010348 1 20010316 A 5347 995821223 SEAT TRACK DOUG DC9 DC914 3022034 WP CABIN DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 STATION 642 NR 1 SEAT TRACK HAS ONE HOLE ELONGATED IN THE SEAT TRACK BOTTOM FLANGE, COMMON TO INTERCOSTAL AND TEE. ALSO ONE CLIP BROKEN 4 INCHES INBOARD OF NR 1 SEAT TRACK. FABRICATED, LOCATED AND INSTALLED BUSHING AND STRAP. 2 L 7 2 4F A6WE 2001041200112 20010412 00112 WP 2001 4 12 MWEA010356 1 20010319 A 5320 9957729 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FABRICATE INTERCOSTAL AT STATION 642 AT NR 1 SEAT TRACK, HAS ELONGATED HOLE. REMOVED, FABRICATED, LOCATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001041200113 20010412 00113 SO 2001 4 12 COMA0110064 1 20010312 A 5720 12017063009 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 22886 120264 DURING 2C CHECK TASK 5720-561-01I, THE LT WING UPPER SUPPORT AT RIB 23, BETWEEN STRINGERS 2A AND 3A, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001041200114 20010412 00114 SO 2001 4 12 C2XA01CL058 1 20010316 A 5610 163500109 WINDSHIELD EMB 145 EMB145LR SO COCKPIT DEFECTIVE A C2XA A UNSCHED LANDING M OVER TEMP CR CRUISE 1 SW 27 18982 3138 145223 CLE FLIGHT 4263 THE CREW REPORTED THE CAPTAINS WINDSHIELD HEATING ELEMENT GLOWS ORANGE WHEN SELECTED AND SCORCH MARKS WE RE PRESENT. MAINTENANCE INSPECTED AND REPLACED THE CAPTAIN''S WINDSHIELD. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001041200115 20010412 00115 WP 2001 4 12 MWEA010480 1 20010329 A 5310 49122621 SPLICE DOUG DC9 DC914 3022034 WP FUSELAGE ELONGATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 LONGERON 1 SPLICE CAP HAS 4 EA. HOLES ELONGATED AND IN RADIUS OF LONG SPLICE CAP AT STATION 226 TO 230. REMOVED LONGER ON SPLICE CAP, CUT AND FABRICATED NEW SECTION OF STRAP AND SPLICE PLATE, CUT OUT DAMAGED SKIN, FABRICATED EXTERNAL DOUBL ER, INSTALLED SKIN PLUG, TAPERED FILLER, FINGER DOUBLERS AND EXTERNAL DOUBLER. 2 L 7 2 4F A6WE 2001041200116 20010412 00116 WP 2001 4 12 MWEA010481 1 20010329 A 5522 5918045 SKIN DOUG DC9 DC914 3022034 WP LT ELEVATOR WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 LEFT ELEVATOR UPPER SKIN WORN TO KNIFE EDGE AT FORWARD EDGE ABOVE NR 4 EYE BOLT ATTACH. FABRICATED AND INSTALLED REPAI R DOUBLER. 2 L 7 2 4F A6WE 2001041200117 20010412 00117 WP 2001 4 12 MWEA010484 1 20010329 A 5710 9919369501 STRUCTURE DOUG DC9 DC932 3022066 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 CORROSION AROUND FASTENER ON LOWER RIGHT WING TEE BETWEEN STRINGER 21 AND 20 (3 & 4 FROM FRONT). REMOVED CORROSION. 2 L 7 2 4F A6WE 2001041200118 20010412 00118 WP 2001 4 12 MWEA010485 1 20010329 A 5710 9919369501 STRUCTURE DOUG DC9 DC932 3022066 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 LIGHT CORROSION ON THE EDGE OF LEFT WING TEE CAP XCW 58 HORIZONTAL LEG AFT OF STRINGER 19. -- BLENDED CORROSION. 2 L 7 2 4F A6WE 2001041200119 20010412 00119 WP 2001 4 12 MWEA010486 1 20010329 A 5320 9911520387 ANGLE DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FORWARD BAG PIT, FRAME TO LONGERON ATTACH ANGLE AT STATION 218 AT LONGERON 30 HAS AREAS OF LIGHT CORROSION. BLENDED CO RROSION, REMOVED FASTENERS AND ANGLE, LOCATED, DRILLED AND INSTALLED ANGLE. 2 L 7 2 4F A6WE 2001041200120 20010412 00120 WP 2001 4 12 MWEA010453 1 20010328 A 5321 995791819 FLOOR PANEL DOUG DC9 DC932 3022066 WP FUSELAGE MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 209ME 47730 CABIN FLOOR PANEL A3 HAS AN AREA OF MISDRILLED HOLES AT AFT END. REMOVED FLOOR PANEL, FABRICATED NEW FLOOR BOARD, REPL ACED FLOOR PANEL. 2 L 7 2 4F A6WE 2001041200121 20010412 00121 WP 2001 4 12 MWEA010454 1 20010328 A 5321 995791819 FLOOR PANEL DOUG DC9 DC932 3022066 WP FUSELAGE MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 209ME 47730 CABIN FLOOR PANEL A2 HAS MISDRILLED HOLES ON ONE END INCLUDING CHANNELS. CUT AND REMOVED AFT 2 INCHES OF FLOOR BOARD S KIN, INSERTED SPLICE PLATE AND DOUBLER, CUT AND REMOVED AFT 4 INCHES OF HAT CHANNELS, SPLICED NEW HAT CHANNELS, ASSEMBLE D REPAIR PARTS TO FLOOR BOARD. 2 L 7 2 4F A6WE 2001041200122 20010412 00122 WP 2001 4 12 MWEA010482 1 20010328 A 5270 59103647 PLATE DOUG DC9 DC932 3022066 WP STAIR DOOR OUT OF ADJ A MWEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 31 207ME 47794 ON TAKE OFF ROLL, FORWARD STAIRWAY DOOR ANNUNCIATOR CAME ON. -- ADJUSTED SWITCH STRIKER PLATE, PRESSURIZED AIRCRAFT TO 7 PSI, LIGHT REMAINED OFF. 2 L 7 2 4F A6WE 2001041200123 20010412 00123 NM 2001 4 12 01FDEA00209 1 20010319 A 5311 6515928 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 FRAME DENTED AT 500, STR 22 LT, STR 25 LT. *S/D* REMOVED, REPLACED AND FAB PER FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 2001041200124 20010412 00124 NM 2001 4 12 01FDEA00210 1 20010319 A 5311 6515933 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 BS 600 FRAME DENTED STR 22 LT - 23 LT. *S/D* REMOVED AND REPLACED PER FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 2001041200125 20010412 00125 NM 2001 4 12 01FDEA00211 1 20010319 A 5311 6515929 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 FRAME DENTED AND GOUGED AT BS 520, STR 22 LT - 25 LT. *S/D* REMOVED AND REPLACED PER FED-EX 51-40-3, 51-30-2. ALODINE D AND PRIMED ANGLE PER FEDEX MM 51-20-151. 2 L 7 3 4F RT A3WE 2001041200126 20010412 00126 NM 2001 4 12 01FDEA00212 1 20010319 A 5311 6515937 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 FRAME DENTED AT BS 680 BETWEEN STR 23 LT AND 24 LT. *S/D* REMOVED AND REPLACED PER FED-EX SRM 51-40-3 FIG 1. 2 L 7 3 4F RT A3WE 2001041200127 20010412 00127 EA 2001 4 12 COMA0160320 1 20010316 A 3250 17300233 HARNESS CNDAIR CL600 CL6002B19 EA NLG WW DEFECTIVE A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 729CA 7265 STEERING INOPERABLE MESSAGE DURING T/O. REPLACED THE NWS WIRE HARNESS. 2 L 7 2 4F RT A21EA 2001041200128 20010412 00128 EA 2001 4 12 COMA0160321 1 20010316 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 EA CABIN LOOSE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 956CA 7105 FORWARD ORANGE SECTION OF EMERGENCY FLOOR LIGHTING IS INOP. SECURED LOOSE CONNECTION, SYSTEM TEST NORMAL. 2 L 7 2 4F RT A21EA 2001041200129 20010412 00129 2001 4 12 JBXA000258 4 20010319 A 3418 STALL WARNING CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTIONED A JBXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 05 583ML 7327 STALL FAIL CAUTION MESSAGE WHEN GEAR RETRACTED AFTER TAKEOFF. PERFORMED OPERATIONAL TEST OF STALL PROTECTION SYSTEM. O PS CHECK GOOD, NO FAULTS NOTED IAW AMM 27-35-01. 2 L 7 2 4F RT A21EA 2001041200130 20010412 00130 2001 4 12 JBXA000259 4 20010319 A 3418 3995100208 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING FAILED A JBXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 05 583ML 7327 STALL FAIL CAUTION MESSAGE WHEN GEAR RETRACTED AFTER TAKEOFF. REMOVED AND REPLACED STALL PROTECTION COMPUTER IAW AMM 27 -35-01, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2001041200131 20010412 00131 WP 2001 4 12 MWEA010534 1 20010409 A 5321 99579249 FLOOR PANEL DOUG DC9 DC932 3022066 WP FUSELAGE MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 209ME 47730 CABIN FLOOR PANEL B7 HAS MISDRILLED FASTNER HOLES AT ONE END. FABRICATED AND INSTALLED FLOOR PANEL REPAIR PARTS. 2 L 7 2 4F A6WE 2001041200132 20010412 00132 WP 2001 4 12 MWEA010535 1 20010409 A 5321 995792926 FLOOR PANEL DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 CABIN FLOOR PANEL F9 HAS AREAS OF LIGHT CORROSION AND MISSING PAINT ON TOP SIDE. FABRICATED AND INSTALLED PATCH AND FIL LER. 2 L 7 2 4F A6WE 2001041200133 20010412 00133 WP 2001 4 12 MWEA010536 1 20010409 A 5321 995792821 FLOOR PANEL DOUG DC9 DC932 3022066 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 CABIN FLOOR PANEL E15, SKIN IS DENTED AND A PIECE CRACKED OFF AT ONE EDGE. FABRICATED AND INSTALLED SKIN. 2 L 7 2 4F A6WE 2001041200134 20010412 00134 WP 2001 4 12 MWEA010537 1 20010409 A 5321 991559713 FLOOR PANEL DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 CABIN FLOOR PANEL A4, SKIN IS CRACKED AT FORWARD CORNER. FABRICATED AND INSTALLED FLOOR PANEL REPAIR PARTS. 2 L 7 2 4F A6WE 2001041200135 20010412 00135 WP 2001 4 12 MWEA010538 1 20010409 A 5321 99579120 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FLOOR BOARD F-2 HAS SEVERAL AREAS OF CORROSION ON TOP SURFACE AND CORROSION AROUND SOME OF THE FASTENER HOLES AND BOTTOM HAT CHANNELS HAVE MINOR CHAFTES AND CORROSION. FABRICATED AND INSTALLED TOP SKIN. 2 L 7 2 4F A6WE 2001041200136 20010412 00136 WP 2001 4 12 MWEA010539 1 20010409 A 5321 995791922 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FLOORBOARD B-8 HAS SEVERAL AREAS OF CORROSION ON TOP SURFACE AND CORROSION AROUND SOME OF THE FASTENER HOLES AND BOTTOM HAT CHANNELS HAVE MINOR CHAFES AND CORROSION. FABRICATED AND INSTALLED FLOOR BOARD REPAIR PARTS. 2 L 7 2 4F A6WE 2001041200137 20010412 00137 WP 2001 4 12 MWEA010540 1 20010409 A 5321 995791917 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FLOORBOARD B-1 HAS A SMALL CRACK IN TOP SURFACE WITH CORROSION AROUND SOME OF THE FASTENER HOLES AND BOTTOM HAT CHANNELS HAVE MINOR CHAFES AND CORROSION. FABRICATED AND INSTALLED FLOOR PANEL. 2 L 7 2 4F A6WE 2001041200138 20010412 00138 WP 2001 4 12 MWEA010541 1 20010409 A 5321 991559811 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FLOORBOARD E-6 HAS SEVERAL AREAS OF CORROSION ON TOP SURFACE WITH SOME FASTENERS PULLED THROUGH SKIN AND CORROSION AROUN D SOME OF THE FASTENER HOLES AND BOTTOM HAT CHANNELS HAVE MINOR CHAFES AND CORROSION. REMOVED AND REPLACED WITH FLOORBO ARD REPAIR. 2 L 7 2 4F A6WE 2001041200139 20010412 00139 WP 2001 4 12 MWEA010542 1 20010409 A 5321 991559714 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FLOORBOARD F-4 AFT OUTBOARD CORNER IS MISSING, HAS SEVERAL AREAS OF CORROSION ON TOP SURFACE AND AROUND SOME FASTENER HO LES AND BOTTOM HAT CHANNELS HAVE MINOR CHAFES AND CORROSION. FABRICATED AND INSTALLED SKIN FOR FLOORBOARD. 2 L 7 2 4F A6WE 2001041200140 20010412 00140 EU 2001 4 12 C2XA01CL059 1 20010317 A 2121 EVAC2423H COOLING FAN AEROSP ATR42 ATR42320 8680930 EU FUSELAGE MALFUNCTIONED A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 42836 11447 200 CLE FLIGHT 3116 THE CREW REPORTED A LIGHT HAZE AND ELECTRICAL BURNING SMELL IN COCKPIT DURING TAXI. THE AIRCRAFT RETURN ED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LEFT GROUND COOLING FAN. OPERATIONAL C HECKS WERE GOOD. MAINTENANCE ALSO INSPECTED THE NR 1 AND NR 2 ENGINES. NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEAS ED FOR SERVICE. 2 H 7 2 4T RT A53EU 2001041200141 20010412 00141 SO 2001 4 12 C2XA01CL060 1 20010318 A 2621 336000575 FIRE BOTTLE EMB 145 EMB145ER SO NR 2 ENGINE INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 14933 825 145018 CLE FLIGHT 4089 THE CREW REPORTED EXTINGUISHER BOTTLE-B INOP MESSAGE IN FLIGHT. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE FIRE BOTTLE. THE AIRCRAFT WAS RELEASED FOR SERVI CE. 2 L 7 2 4F RT T00011AT 2001041200142 20010412 00142 SO 2001 4 12 COMA0110066 1 20010312 A 5315 12006962001 FLOORBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 7922 120264 DURING 2C CHECK TASK 131-01Z, THE FUSELAGE LT FLOORBEAM T-SECTION AT FRAME 16 WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001041200143 20010412 00143 NM 2001 4 12 ASAA0110080 1 20010209 A 5310 65566552 DOOR FRAME BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND DOOR FRAME AT BODY STATION 790, STRINGER 20R-26R CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041200144 20010412 00144 NM 2001 4 12 ASAA0110081 1 20010209 A 5315 65671407 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BODY STATION 540-727B, LEFT BUTTOCK LINE 45.5 CORRODED. REPAIRED PER EA. (M) 2 L 7 2 4F A16WE 2001041200145 20010412 00145 NM 2001 4 12 ASAA0110082 1 20010209 A 5315 6567140 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BODY STATION 460, LEFT BUTTOCK LINE 10-53 CORRODED. REPAIRED PER EA. (M) 2 L 7 2 4F A16WE 2001041200146 20010412 00146 NM 2001 4 12 ASAA0110084 1 20010209 A 5315 6567140 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 420, LEFT BUTTOCK LINE 0-46 CORRODED. REPAIRED PER EA. (M) 2 L 7 2 4F A16WE 2001041200147 20010412 00147 NM 2001 4 12 ASAA0110083 1 20010209 A 5320 6546578574 ANGLE BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND CHORD ANGLE AT BS 1088-1156, ABOVE RIGHT HORIZONTAL STABILIZER AFT UPPER ATTACHMEN T POINT CRACKED. REMOVED AND REPLACED CORD ANGLE PER SRM. (M) 2 L 7 2 4F A16WE 2001041200148 20010412 00148 NM 2001 4 12 ASAA0110086 1 20010209 A 5347 BAC15201432 SEAT TRACK BOEING 737 737290C 138448V NM CABIN CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND SEAT TRACK AT BODY STATION 880-947, LEFT BUTTOCK LINE 24.75 CORRODED. REPAIRED PE R SRM. (M) 2 L 7 2 4F A16WE 2001041200149 20010412 00149 NM 2001 4 12 ASAA0110087 1 20010209 A 5347 BAC15201434 SEAT TRACK BOEING 737 737290C 138448V NM CABIN CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND SEAT TRACK AT BODY STATION 807-887, LEFT BUTTOCK LINE 45.5 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041200150 20010412 00150 WP 2001 4 12 AALA20010216 1 20010118 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 TUL - FOUND LONGERON 4L CRACKED AROUND FASTENER AT STATION 160. INSTALLED LONGERON REPAIR SPLICE PER SRM 53-02 FIG 18 A ND 53-14-1 FIG 3. (M) 2 L 7 2 4F A6WE 2001041200151 20010412 00151 WP 2001 4 12 AALA20010217 1 20010130 A 5320 STRUCTURE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 TUL - FOUND CRACK BS 1485R, UNDER RIGHT AIR STAIRS ACTUATOR APPROX 1 INCH LONG. INSTALLED SPLICE REPAIR PER ESO 80559 D ATED 29 JAN 2001. (M) 2 L 7 2 4F A6WE 2001041200152 20010412 00152 WP 2001 4 12 AALA20010218 1 20010121 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 TUL - FOUND HOLE IN CUSP WEB UNDER SEAT TRACK NR 6 STATION 1086. INSTALLED DOUBLER AT STATION 1086 IN CUSP WEB PER AARD 25-00-00-02. (M) 2 L 7 2 4F A6WE 2001041200153 20010412 00153 WP 2001 4 12 AALA20010219 1 20010121 A 5345 FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 TUL - FOUND INBOARD GALLEY TIE DOWN CORRODED STATION 218. REMOVED AND REPLACED GALLEY TIE DOWN PER SRM 53-01-00. (M) 2 L 7 2 4F A6WE 2001041200154 20010412 00154 WP 2001 4 12 AALA20010250 1 20010207 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 411AA 49322 TUL - FOUND CORROSION AT ATTACH FASTENER AND NUT CLIPS FROM 1211 TO 1322. REPLACED LEFT CARGO TIE DOWN TRACK STATION 10 07-1322, PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2001041200155 20010412 00155 WP 2001 4 12 AALA20010251 1 20010131 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 411AA 49322 TUL - FOUND CORROSION ON CHORD ANGLE STATION 1003 LONGERON 26L. REPAIRED ANGLE PER ESO 80559 DATED 1-30-01 CORROSION BL ENDED OUT AND DOUBLER INSTALLED. (M) 2 L 7 2 4F A6WE 2001041200156 20010412 00156 WP 2001 4 12 AALA20010252 1 20010202 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 411AA 49322 TUL - FOUND VISUAL INDICATION OF CRACK ON LONGERON 20R, STATION 1003. STOP DRILLED CRACK AND REPAIRED LONGERON PER AARD 53-10-00-18 PAGE 1 TO PAGE 3. (M) 2 L 7 2 4F A6WE 2001041200157 20010412 00157 WP 2001 4 12 AALA20010253 1 20010127 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 411AA 49322 TUL - FOUND NR 3 SEAT TRACK WORN, BS 296. INSTALLED SEAT TRACK PLUG PER SRM 53-05 PART 1. (M) 2 L 7 2 4F A6WE 2001041200158 20010412 00158 WP 2001 4 12 AALA20010254 1 20010129 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 411AA 49322 TUL - FOUND FUSELAGE SKIN CRACKED AT STATION 1380 BELOW L13R. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01 FI G 2 SHEET 3. (M) 2 L 7 2 4F A6WE 2001041200159 20010412 00159 WP 2001 4 12 AALA20010249 1 20010126 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 411AA 49322 TUL - FOUND DENT AND SCRATCH IN FUSELAGE BELOW RIGHT ENGINE 3 FEET ABOVE FRESH WATER DRAIN HOLE, FS 1309. REF ADL NR 00 24. INSTALLED TITANIUM SCUFF PLATE PER AARD 53-30-00-8 AND INTERNAL DOUBLER PER SRM 53-04 FIG 38. (M) 2 L 7 2 4F A6WE 2001041200160 20010412 00160 NM 2001 4 12 USAASB01059 1 20010225 A 5610 5717623116 SLIDING WINDOW BOEING 737 7373B7 1384580 NM COCKPIT CRACKED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 384US 29992 14603 22957 ALB - FLT 775 - ON CLIMB-OUT FROM ALB, EN ROUTE TO PIT, THE FIRST OFFICERS SLIDING WINDOWN ARCED AND THEN CRACKED. FLIG HT RETURNED TO FIELD AT ALB AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND RE PLACED THE FIRST OFFICERS SLIDING WINDOW PER MM 56-12-11. ALSO, AS PRECAUTIONARY, REMOVED AND REPLACED THE FIRST OFFICE RS SLIDING WINDOW HEAT CONTROL UNIT (P/N 83000-05602) PER MM 30-41-11. ADJUSTMENT AND OPERATIONAL TEST OF WINDOW GOOD. (M) 2 L 7 2 4F RT A16WE 2001041200161 20010412 00161 NM 2001 4 12 USAASB01060 1 20010225 A 2131 7638101 CONTROLLER BOEING 737 737301 1384611 NM E&E BAY FAULTY A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 575US 37037 23740 CLT - FLT 1262 - ON CLIMB-OUT FROM PBI, EN ROUTE TO PHL, PRESSURIZATION WAS UNCONTROLLABLE WITH THE RIGHT PACK AS THE LE FT PACK WAS ON MEL. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANC E REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER PER MM 21-31-21. OPS CHECK NORMAL. PERFORMED HULL LEAKAGE CHECK. LEAK RATE WITHIN LIMITS PER MM 05-51-91. CLEARED MEL ON LEFT PACK BY REMOVING AND REPLACING THE LEFT DUCT LIMIT SWITCH . OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2001041200162 20010412 00162 NM 2001 4 12 USAASB01056 1 20010224 A 5240 DOOR BOEING 737 7373B7 1384580 NM SERVICE DOOR NOT CLOSED A USAA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 EA 19 520AU 23706 PWM - FLT 1433 - ON CLIMB-OUT FROM PWM, EN ROUTE TO PIT, THE AIRCRAFT WOULD NOT PRESSURIZE. AT 5,000 FEET, THE CREW LEV ELED OFF AND TRIED TO PRESSURIZE. AIRCRAFT WOULD NOT PRESSURIZE IN AUTO, STANDBY OR MANUAL MODES. FLIGHT RETURNED TO F IELD AT PWM AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE AFT RIGHT SERVICE DO OR NOT CLOSED PROPERLY. OPENED AND CLOSED DOOR TO CONFIRM PROPER OPERATION. NO PROBLEMS NOTED. DOOR OPERATION CHECKS GOOD. (M) 2 L 7 2 4F RT A16WE 2001041200163 20010412 00163 NM 2001 4 12 USAASB01057 1 20010224 A 3610 1074845 REGULATOR BOEING 737 7374B7 1384702 NM NR 2 ENGINE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 427US 37570 24549 ORD - FLT 916 - ON CLIMB-OUT FROM ORD, EN ROUTE TO CLT, THE NR 2 ENGINE BLEED TRIP LIGHT ILLUMINATED. CAPTAIN TRIED TO RESET THE NR 2 ENGINE BLEED TRIP WITH NO HELP, AS LIGHT REMAINED ILLUMINATED. CABIN PRESSURE STARTED TO CLIMB WITH THE AIRCRAFT, SO THE CAPTAIN DECKED TO RETURN TO FIELD AT ORD. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DE CLARED. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE HIGH STAGE REGULATOR PER MM 36-11-86. PERFORMED OPERATIONAL T EST OF BLEED AIR CONTROL SYSTEM PER MM 36-11-05. OPERATIONAL TEST GOOD. (M) 2 L 7 2 4F RT A16WE 2001041200164 20010412 00164 NM 2001 4 12 USAASB01052 1 20010217 A 3350 AD20131A BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 584US 23743 GSO - MAINTENANCE FOUND SOME EMERGENCY LIGHTS IN THE CABIN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PA CK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001041200165 20010412 00165 CE 2001 4 12 C2XA01CL063 1 20010315 A 2612 MS3456KT14S7P CONNECTOR BEECH 1900 1900D 1154162 CE RT ENGINE DIRTY A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 87554 UE227 MDT FLIGHT 3133 THE CREW REPORTED RIGHT ENGINE FIRE LOOP TEST FAILED. MAINTENANCE CLEANED AND RESEATED RIGHT ENGINE FIR E LOOP CANNON PLUG. PERFORMED OPERATIONAL TEST AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 2001041200166 20010412 00166 NM 2001 4 12 USAABB01011 1 20010217 A 4900 7321387009 ACTUATOR BOEING 757 757225 1384959 NM APU INLET DOOR FAULTY A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 606AU 1832 22202 JAX - FLT 880 - EN ROUTE FLL-PIT, WITH THE LEFT IDG ON MEL AND THE APU OPERATING, THE CREW RECEIVED INDICATIONS THAT THE APU HAD PERFORMED AN AUTO-SHUTDOWN. THE CREW TRIED UNSUCCESSFULLY TO RESTART THE APU. THE FLIGHT DIVERTED TO JAX AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE IN JAX REPLACED THE INLET DOOR PROXIMITY SENSOR DEFECTIVE AND REPLACED IT. SUBSEQUENTLY, THE DOOR INLET ACTUATOR WAS REPLACED DUE TO THE APU INLET DOOR NOT OPENING. (M) 2 L 7 2 4F RT A2NM 2001041200167 20010412 00167 NM 2001 4 12 USAASB01035 1 20010203 A 3610 106498G0266180 HOSE BOEING 737 7373B7 1384580 NM NR 2 ENGINE FAILED A USAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 514AU 23700 YUL - FLT 0442 - EN ROUTE FROM PIT TO YUL, AT FL330, THE CABIN ALTITUDE WARNING HORN SOUNDED. CREW PERFORMED EMERGENCY PROCEDURES AND WHEN CABIN ALTITUDE CLIMED TO MORE THAN 10,000 FEET, THEY DECLARED AN EMERGENCY. CREW DESCENDED THE FLIG HTS TO FL100 AND WERE ABLE TO CONTROL CABIN ALTITUDE IN MANUAL AND STANDBY MODE. FLIGHT CONTINUED ONTO YUL AT FL100 AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE HOSE ASSY FROM THE 450 DEGREE THERMO STAT TO THE PRESSURE REGULATOR AND SHUTOFF VALVE (PRSOV). OPS CHECK GOOD. DUCT PRESSURE NORMAL PER MM 36-11-05. ACCOM PLISHED CHECK OUT OF PRESSURIZATION SYSTEM. PRESSURIZATION SYSTEM CHECKS NORMAL. (M) 2 L 7 2 4F RT A16WE 2001041200168 20010412 00168 NM 2001 4 12 USAASB01053 1 20010221 A 2781 654476028 SWITCH BOEING 737 7374B7 1384702 NM L/E SLAT FAULTY A USAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 EA 19 775AU 24933 CLT - FLT 540 - ON CLIMB-OUT FROM CLT, CREW RECEIVED A FORWARD LEADING EDGE SLAT INDICATION ALONG WITH A NR 3 SLAT OVERH EAD INTRANSIT LIGHT. CREW RECYCLED FLAPS TO FLAPS 1 PER CHECKLIST WITH NO HELP. FLIGHT RETURNED TO FIELD AT CLT AND LN DED WITH FLAP SETTING OF 15. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 3 LEADING EDGE SLAT AC TUATOR ROD END SWITCH PER MM 27-81-41. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001041200169 20010412 00169 NM 2001 4 12 USAASB01054 1 20010221 A 2910 HYDRAULIC LINE BOEING 737 7373B7 1384580 NM MLG WW RUPTURED A USAA A UNSCHED LANDING K J F FLUID LOSS WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 EA 19 511AU 23594 CLT - FLT 1507 - ON CLIMB-OUT, AT FL100, THE B HYDRAULIC SYSTEM LOW PRESSURE LIGHT ILLUMINATED WITH HYDRAULIC QUANTITY I NDICATING ZERO. CAPTAIN DECLARED AN EMERGENCY AND THE FLIGHT RETURED TO FIELD AT CLT. ON RETURN TO CLT, CREW SUSPECTS THE STANDBY HYDRAULIC PUMP FAILED AS IT FAILED TO MOVE THE FLAPS BEYOND FLAPS 10. FLIGHT LANDED WITHOUT FURTHER INCIDEN T AND WAS TOWED TO THE GATE DUE TO FEAR OF HOT BRAKES. MAINTENANCE FOUND THE HYDRAULIC FLEX LINE FROM THE B ELECTRIC PU MP TO THE HYD MODULE RUPTURED. REMOVED AND REPLACED FLEX LINE. ALSO, REMOVED AND REPLACED STANDBY HYDRAULIC PUMP (P/N 165W01020), B SYSTEM ELECTRIC HYDRAULIC PUMP (P/N MPEV3-056-9), NR 2 ENGINE HYDRAULIC PUMP (P/N 65075-06) AND ALL ASSOC 2 L 7 2 4F RT A16WE 2001041200170 20010412 00170 WP 2001 4 12 USAAD01030 1 20010216 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 827US 48049 TPA - DURING A TEST OF THE EMERGENCY LIGHTS, ROW 25 UNDER SEAT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. A BATTERY W AS REPLACED. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F A6WE 2001041200171 20010412 00171 NM 2001 4 12 USAABB01012 1 20010209 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 619AU 27198 SFO - FOUND ALL 10 FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2001041200172 20010412 00172 NM 2001 4 12 USAABB01008 1 20010211 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 613AU 27144 LAX - FOUND FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE AT ROW 6. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2001041200173 20010412 00173 2001 4 12 USAASB01013 4 20010120 A 3417 HG480B42 ADC BOEING 737 737301 1384611 NM E&E BAY FAULTY A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 588US 39156 23933 TPA - FLT 9230 - AFTER T/O, AT APPROX 500 FT, THE WINDSHEAR WARNING WITH AUDIO SOUNDED ALONG WITH STICK SHAKER ACTIVATIO N. AIRSPEED DROPPED TO 110 KNOTS ON THE CAPTS SIDE. WINDSHEAR RECOVERY PROCEDURES WERE PERFORMED. AIRSPEED FLUCTUATED FROM 110 TO 125 KNOTS. ALTIMETER QUIT AT 800 FT AND AIRSPEED WENT TO ZERO. FLT RETURNED TO FIELD AT TPA AND AT APPRX 500 FT ABOVE GROUND LEVEL, THE WINDSHEAR WARNING ACTIVATED AGAIN AND AIRSPEED BEGAN TO FLUCTUATE AT 80 KNOTS. FLIGHT LA NDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MX REMOVED AND REPLACED THE NR 1 DIGITAL AIR DATA COMPUTER P ER JOB CARD. LEAK CHECKED SYSTEM PER PITOT STATIC TEST BOX. SYSTEM CHECKS GOOD. ACCOMPLISHED EXCEEDING FLAPS DOWN SPE 2 L 7 2 4F RT A16WE 2001041200174 20010412 00174 NM 2001 4 12 USAABB01010 1 20010217 A 2433 60B401042 TRANSFORMER BOEING 757 7572B7 1384964 NM APU DEFECTIVE A USAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 EA 19 613AU 7770 27144 CLT - FL 1154 - APPROXIMATELY FORTY MINUTES AFTER TAKEOFF FROM MCO, AN ELECTRICAL SMELL WAS NOTED IN THE CABIN. SHORTLY AFTER, THE COCKPIT CREW NOTED IT ALSO. TEN MINUTES LATER, THE 21 AND 31 LAV SMOKE DETECTORS ACTIVATED. CREW PERFORMED HANDBOOK PROCEDURES. THE SMELL DISSIPATED. THE FLIGHT DIVERTED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENAN CE FOUND THE APU TRU TRIPPING ITS CIRCUIT BREAKER. THE TRU WAS REPLACED. (M) 2 L 7 2 4F RT A2NM 2001041200175 20010412 00175 WP 2001 4 12 USAAD01033 1 20010218 A 3350 9721050 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 826US 48026 IND - THE INTERIOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED TRANSMITTER BATTERIES. (M) 2 L 7 2 4F A6WE 2001041200176 20010412 00176 WP 2001 4 12 USAAD01034 1 20010219 A 3350 MISC0639 BATTERY PACK DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 826US 48026 PIT - THE OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) 2 L 7 2 4F A6WE 2001041200177 20010412 00177 SO 2001 4 12 C2XA01IA163 1 20010316 A 3397 W602009620 WIRE EMB 120 EMB120ER 3260203 SO CABIN GROUNDED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 27716 120128 IAH-FLIGHT 2976, DURING PREFLIGHT INSPECTION THE AFT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A GROUNDED WIRE FOR THE LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001041200178 20010412 00178 SO 2001 4 12 C2XA01IA164 1 20010313 A 3397 W220103924 WIRE EMB 120 EMB120ER 3260203 SO CABIN DISCONNECTED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 22727 120177 IAH-DURING PREFLIGHT INSPECTION THE FORWARD CABIN EXIT SIGN DID NOT ILLUMINATE. MAINTENANCE RECONNECTED A LOOSE WIRE ON THE LIGHT ASSEMBLY AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001041200179 20010412 00179 SO 2001 4 12 COMA0110070 1 20010312 A 5311 12022636501 FRAME EMB 120 EMB120RT SO FUSELAGE GOUGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 21213 120264 DURING 2C CHECK TASK 163-01Z, THE FUSELAGE FRAME 46A WAS FOUND TO BE GOUGED BY AN INTERIOR LINING SCREW AT FLOOR LEVEL O N THE LEFT SIDE. THE FRAME WAS REPAIRED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 2400=5, REV IR, 3-5-01. 2 L 7 2 4T RT A31SO 2001041200180 20010412 00180 SO 2001 4 12 COMA0110077 1 20010312 A 5720 12017062613 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 21213 120264 DURING 2C CHECK TASK 5720-552-01I, THE LT WING UPPER SKIN SUPPORT AT RIB 21, BETWEEN FR ON SPAR AND STRINGERS 2A, WAS FO UND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001041200181 20010412 00181 SO 2001 4 12 COMA0110078 1 20010312 A 5315 12004449001 FLOORBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 21213 120264 DURING 2C CHECK TASK 152-01Z, THE FUSELAGE RT FLOOR T-SECTION AT FRAME 36 WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001041200182 20010412 00182 EA 2001 4 12 COMA0160316 1 20010313 A 2613 6005912225 SWITCH CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 767CA 7285 WING OVERHEAT WARNING MESSAGE. REPLACED THE RT OVERHEAT STANDBY SWITCH. 2 L 7 2 4F RT A21EA 2001041200183 20010412 00183 WP 2001 4 12 MWEA010390 1 20010326 A 5712 591000644 FITTING DOUG DC9 DC932 3022066 WP RT WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 RIGHT WING TO FUSELAGE FITTING AT XOS 50 LONGERON 22 RIGHT WAS CRACKED. -- REMOVED FITTING, LOCATED, DRILLED, AND INST ALLED NEW FITTING. 2 L 7 2 4F A6WE 2001041200184 20010412 00184 WP 2001 4 12 MWEA010391 1 20010325 A 2913 A866411LS616 PUMP DOUG DC9 DC932 3022066 WP LT ENGINE INOPERATIVE A MWEA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 31 207ME 47794 LEFT HYDRAULIC QUANTITY DROPPED TO 1 1/2 QUARTS IN FLIGHT, LEFT ENGINE DRIVER HYDRAULIC PUMP LEAKING. REPLACE LEFT ENG INE DRIVEN HYDRAULIC PUMP. 2 L 7 2 4F A6WE 2001041200185 20010412 00185 WP 2001 4 12 MWEA010392 1 20010324 A 2760 H2026B SWITCH DOUG DC9 DC932 3022066 WP LT & RT WING INOPERATIVE A MWEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 31 216ME 47740 AFTER ENGINE START THE SPOILER DEPLOYED ANNUNCIATOR LIGHT CAME ON. REPLACED LEFT INBOARD AND RIGHT OUTBOARD SPOILER DE PLOYMENT SWITCHES. 2 L 7 2 4F A6WE 2001041200186 20010412 00186 WP 2001 4 12 MWEA010342 1 20010314 A 5330 5910072 SKIN DOUG DC9 DC914 3022034 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 HOLE IN SKIN AT STATION 94.550. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001041200187 20010412 00187 WP 2001 4 12 MWEA010399 1 20010327 A 5321 995791820 FLOOR PANEL DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FLOOR PANEL F3 HAS A CRACK AT FASTENER HOLE AT FORWARD END. FABRICATED AND LOCATED HOLES IN NEW SKIN, INSTALLED HAT CH ANNELS TO NEW SKIN. 2 L 7 2 4F A6WE 2001041200188 20010412 00188 WP 2001 4 12 MWEA010400 1 20010328 A 5321 995791917 FLOOR PANEL DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FLOOR PANEL B3 HAS AREAS OF LIGHT CORROSION. BLENDED AREAS OF CORROSION, REMOVED DAMAGED HAT SECTION, AND FABRICATED N EW HAT SECTION, INSTALLED NEW HAT CHANNEL TO SKIN. 2 L 7 2 4F A6WE 2001041200189 20010412 00189 WP 2001 4 12 MWEA010401 1 20010328 A 5321 995791917 FLOOR PANEL DOUG DC9 DC914 3022034 WP FUSELAGE MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 FLOOR PANEL B2 HAD WRONG TYPE REPAIR INSTALLED. REMOVED HAT CHANNELS FROM SKIN, DRILLED UP NEW SKIN, DRILLED UP NEW HA T CHANNELS, INSTALLED CHAFE STRIPS AND INSULATION. 2 L 7 2 4F A6WE 2001041200190 20010412 00190 WP 2001 4 12 MWEA010402 1 20010328 A 5321 995792118 FLOOR PANEL DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FLOOR PANEL F4 HAS MANY AREAS OF LIGHT CORROSION. REMOVED CORROSION, FABRICATED NEW FLOOR BOARD SKIN AND HAT CHANNEL, I NSTALLED HAT CHANNEL. 2 L 7 2 4F A6WE 2001041200191 20010412 00191 WP 2001 4 12 MWEA010404 1 20010328 A 5321 995791919 FLOOR PANEL DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FLOOR PANEL B8 HAS AREAS OF BARE METAL. REMOVED CORROSION ON UPPER SURFACE, DRILLED PUNCTURE AND INSTALLED RIVET, INST ALLED PROPER HARDWARE AND PROPER REPAIR OF PUNCTURE. 2 L 7 2 4F A6WE 2001041200192 20010412 00192 WP 2001 4 12 MWEA010405 1 20010328 A 5321 995791820 FLOOR PANEL DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FLOOR PANEL F5 HAS A SMALL CRACK ALONG THE EDGE. FABRICATED NEW SKIN AND LOCATED HOLES IN NEW SKIN, INSTALLED HAT CHAN NELS ON NEW SKIN. 2 L 7 2 4F A6WE 2001041200193 20010412 00193 WP 2001 4 12 MWEA010406 1 20010328 A 5321 995791820 FLOOR PANEL DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FLOOR PANEL F6 HAS AREAS OF LIGHT CORROSION. REMOVED CORROSION, LOCATED AND DRILLED NEW SKIN, INSTALLED HAT CHANNELS T O NEW SKIN. 2 L 7 2 4F A6WE 2001041200194 20010412 00194 WP 2001 4 12 MWEA010407 1 20010328 A 5321 995792926 FLOOR PANEL DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FLOOR PANEL F7 HAS AREAS OF LIGHT CORROSION. REMOVED CORROSION, REMOVED FLOOR BOARD SKIN, FABRICATED NEW SKIN, INSTALL ED NEW SKIN. 2 L 7 2 4F A6WE 2001041200195 20010412 00195 WP 2001 4 12 MWEA010408 1 20010328 A 5321 995791820 FLOOR PANEL DOUG DC9 DC914 3022034 WP FUSELAGE MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 FLOOR PANEL F2 HAS WRONG TYPE REPAIR INSTALLED. -- REMOVED HAT CHANNELS, FABRICATED NEW PANEL AND SKIN, INSTALLED HAT CHANNELS. 2 L 7 2 4F A6WE 2001041200196 20010412 00196 WP 2001 4 12 MWEA010409 1 20010328 A 5321 995791821 FLOOR PANEL DOUG DC9 DC914 3022034 WP FUSELAGE MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 FLOOR PANEL A5 HAS 2 REPAIRS DONE INCORRECTLY. REMOVED ONE REPAIR, REMOVED OLD SKIN, FABRICATED NEW SKIN, INSTALLED NE W SKIN. 2 L 7 2 4F A6WE 2001041200197 20010412 00197 WP 2001 4 12 MWEA010410 1 20010328 A 5321 995792925 FLOOR PANEL DOUG DC9 DC914 3022034 WP FUSELAGE MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 FLOOR PANEL A7 HAS TWO REPAIRS DONE INCORRECTLY. FABRICATED NEW FLOOR BOARD, REMOVED OLD SKIN AND INSTALLED NEW SKIN. 2 L 7 2 4F A6WE 2001041200198 20010412 00198 WP 2001 4 12 MWEA010413 1 20010328 A 5321 995791819 FLOOR PANEL DOUG DC9 DC914 3022034 WP FUSELAGE DENTED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 FLOOR PANEL A1 HAS A SMALL SHARP DENT. FABRICATED NEW SKIN, LOCATED HOLES IN NEW SKIN, INSTALLED HAT CHANNELS TO NEW S KIN. 2 L 7 2 4F A6WE 2001041200199 20010412 00199 WP 2001 4 12 MWEA010414 1 20010328 A 5321 995791819 FLOOR PANEL DOUG DC9 DC914 3022034 WP FUSELAGE MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 FLOOR PANEL A1 HAS THE WRONG TYPE REPAIR INSTALLED. FABRICATED TWO NEW HAT CHANNELS, REPAIRED GLASS HAT CHANNELS THAT WERE DAMAGED. 2 L 7 2 4F A6WE 2001041200200 20010412 00200 WP 2001 4 12 MWEA010415 1 20010328 A 5320 99579169 CHANNEL DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FLOORBOARD E4 HAS A CRACKED HAT CHANNEL. REMOVED OLD CHANNEL, FABRICATED AND INSTALLED NEW HAT CHANNEL. 2 L 7 2 4F A6WE 2001041200201 20010412 00201 WP 2001 4 12 MWEA010416 1 20010328 A 5321 99579169 FLOORBOARD DOUG DC9 DC914 3022034 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FLOORBOARD E4 TOP SURFACE HAS A DENT IN IT. REMOVED DAMAGED AREA AND FABRICATED FLUSH REPAIR, INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001041200202 20010412 00202 WP 2001 4 12 MWEA010417 1 20010328 A 5321 995792313 PANEL DOUG DC9 DC914 3022034 WP FUSELAGE SCRATCHED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FLOORBOARD B4 TOP SURFACE HAD SEVERAL SCRATCHES. BLENDED SCRATCHES, FABRICATED NEW PANEL, LOCATED AND DRILLED, INSTALL ED HATS AND INSULATION BLANKETS. 2 L 7 2 4F A6WE 2001041200203 20010412 00203 WP 2001 4 12 MWEA010418 1 20010328 A 5320 99579233 CHANNEL DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FLOORBOARD B5 HAS TWO HAT CHANNELS THAT ARE CRACKED. FABRICATED AND INSTALLED NEW HAT CHANNELS. 2 L 7 2 4F A6WE 2001041200204 20010412 00204 WP 2001 4 12 MWEA010419 1 20010328 A 5321 99579249 FLOORBOARD DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FLOORBOARD E8 HAS A CRACK AT ONE END. REMOVED CRACKED FLOOR BOARD, FABRICATED, LOCATED HOLES AND INSTALLED PATCH. 2 L 7 2 4F A6WE 2001041200205 20010412 00205 WP 2001 4 12 MWEA010420 1 20010328 A 5320 99579249 CHANNEL DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FLOORBOARD E7 HAS THREE CHANNELS WITH CRACKS. LOCATED AND DRILLED NEW SKIN, FABRICATED 5 HAT CHANNELS, INSTALLED HAT C HANNELS. 2 L 7 2 4F A6WE 2001041200206 20010412 00206 WP 2001 4 12 MWEA010412 1 20010328 A 5321 995791819 FLOOR PANEL DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FLOOR PANEL A3 HAS SEVER AREAS OF LIGHT CORROSION. REMOVED CORROSION AND HAT CHANNELS, FABRICATED NEW SKIN, INSTALLED HAT CHANNEL ON NEW SKIN, INSTALLED CHAFE STRIPS. 2 L 7 2 4F A6WE 2001041200207 20010412 00207 WP 2001 4 12 MWEA010422 1 20010328 A 5321 995791917 FLOORBOARD DOUG DC9 DC914 3022034 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FLOORBOARD E5 HAS NUMEROUS DENTS ON THE TOP SURFACE. REPAIRED DENTS. 2 L 7 2 4F A6WE 2001041200208 20010412 00208 WP 2001 4 12 MWEA010423 1 20010328 A 5321 995791917 FLOORBOARD DOUG DC9 DC914 3022034 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FLOORBOARD B1 TOP SURFACE HAS FOUR DENTS. FABRICATED NEW SKIN, HAT SECTIONS BLENDED, INSTALLED HAT SECTIONS, INSULATIO N AND CHAFE STRIPS. 2 L 7 2 4F A6WE 2001041200209 20010412 00209 WP 2001 4 12 MWEA010424 1 20010328 A 5320 995791921 CHANNEL DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FLOOR BOARD B7 HAS TWO HAT CHANNELS WITH CRACKED ENDS. FARICATED TWO NEW HAT CHANNELS. 2 L 7 2 4F A6WE 2001041200210 20010412 00210 WP 2001 4 12 MWEA010425 1 20010328 A 5321 995791921 FLOORBOARD DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FLOORBOARD B7 HAS LIGHT CORROSION AND CHAFE MARKS ON THE TOP SURFACE. BLENDED CORROSION AND CHAFE MARKS, FABRICATED NE W SKIN, INSTALLED HAT CHANNELS AND INSULATION. 2 L 7 2 4F A6WE 2001041200211 20010412 00211 WP 2001 4 12 MWEA010452 1 20010328 A 3610 577957 DUCT DOUG DC9 DC914 3022034 WP RT ENGINE SEPARATED A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 500ME 45711 RECEIVED RIGHT ENGINE FIRE WARNING, THEN WHEN SILENCE BELL BUTTON WAS PUSHED FIRE WARNING WENT AWAY. LOOP A TESTED NORMA L. LOOP B ALREADY DEFERRED. FOUND 13TH STAGE BLEED AIR DUCT TO FUEL HEAT VALVE MOUNTING FLANGE SEPERATED AT JOINT. REM OVED AND REPLACED AIR DUCT. 2 L 7 2 4F A6WE 2001041200212 20010412 00212 WP 2001 4 12 MWEA010455 1 20010328 A 5320 49120092 CLIP DOUG DC9 DC914 3022034 WP BULKHEAD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 REMOVED LOWER CLIP ON BULKHEAD 69 BETWEEN REAR SPAR AND STRINGER 11 TO FACILITATE OTHER MAINTENANCE. CLIP FOUND TO BE CRACKED, LOCATED, DRILLED AND INSTALLED REPLACEMENT CLIP. 2 L 7 2 4F A6WE 2001041200213 20010412 00213 WP 2001 4 12 MWEA010456 1 20010328 A 5320 4911499510 CLIP DOUG DC9 DC914 3022034 WP BULKHEAD CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 REMOVED LOWER SHEAR CLIP ON BULKHEAD 69, BETWEEN STRINGER 20-21 TO FACILITATE OTHER MAINTENANCE. -- CLIP HAS CORROSION PITS THROUGH RADIUS, LOCATED, DRILLED AND INSTALLED REPLACEMENT CLIP. 2 L 7 2 4F A6WE 2001041200214 20010412 00214 WP 2001 4 12 MWEA010457 1 20010328 A 5320 4911499510 CLIP DOUG DC9 DC914 3022034 WP BULKHEAD CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 REMOVED LOWER SHEAT CLIP ON BULKHEAD 69, BETWEEN STRINGER 18-19 TO FACILIATE OTHER MAINTENANCE. CLIP HAS CORROSION THR OUGH RADIUS, LOCATED AND DRILLED AND INSTALLED REPLACEMENT CLIP. 2 L 7 2 4F A6WE 2001041200215 20010412 00215 WP 2001 4 12 MWEA010458 1 20010328 A 5320 49120012 CLIP DOUG DC9 DC914 3022034 WP BULKHEAD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 REMOVED LOWER SHEAR CLIP ON BULKHEAD 69, STRINGER 16-17 TO FACILITATE OTHER MAINTENANCE. CLIP IS CRACKED AT END NEXT T O STRINGER 16, LOCATED, DRILLED AND INSTALLED REPLACEMENT CLIP. 2 L 7 2 4F A6WE 2001041200216 20010412 00216 WP 2001 4 12 MWEA010459 1 20010328 A 5320 4911499520 CLIP DOUG DC9 DC914 3022034 WP BULKHEAD CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 REMOVED LOWER SHEAR CLIP ON BULKHEAD 69, BETWEEN STRINGER 15-16 TO FACILITATE OTHER MAINTENANCE. CLIP HAS SEVERAL SPOT S OF LIGHT TO MODERATE CORROSION, BLENDED CORROSION, LOCATED AND DRILLED REPLACEMENT CLIP. 2 L 7 2 4F A6WE 2001041200217 20010412 00217 WP 2001 4 12 MWEA010460 1 20010328 A 5753 5912154 SKIN DOUG DC9 DC914 3022034 WP RT WING TE FLAP DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 RIGHT WING DENT AT FLAP NR 4 TRAILING EDGE SECTION UPPER SURFACE. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLER, INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001041200218 20010412 00218 WP 2001 4 12 MWEA010461 1 20010328 A 5321 995191820 FLOORBOARD DOUG DC9 DC914 3022034 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FLOOR BOARD F2 REQUIRES A RESKIN. FABRICATED NEW HAT CHANNELS, FABRICATED NEW SKIN AND LOCATED HOLES, INSTALLED HAT CH ANNELS ON NEW SKIN. 2 L 7 2 4F A6WE 2001041200219 20010412 00219 NM 2001 4 12 01FDEA00164 1 20010225 A 7160 FLANGE BOEING 727 727247 138408F NM NR 2 ENG INTAKE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 233FE 21327 DURING ROUTINE INSP NR 2 ENG INTAKE FLANGE 1342 BULKHEAD FOUND CRACKED BY LFEC AROUND FLANGE BOLTS IN 16 PLACES FROM 3 O ''CLOCK TO 10 O''CLOCK POSITION. *S/D* REMOVED AND REPLACED NR 2 ENG INTAKE DUCT MOUNTING FLANGE PER IAW FEDEX EO 7-54 30-7-2303. 2 L 7 3 4F A3WE 2001041200220 20010412 00220 NM 2001 4 12 ASAA0110088 1 20010209 A 5315 6567140 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BODY STATION 260, LEFT BUTTOCK LINE 12, RIGHT BUTTOCK LINE 14 CORRODE D. REPAIRED PER EA. (M) 2 L 7 2 4F A16WE 2001041200221 20010412 00221 NM 2001 4 12 ASAA0110089 1 20010209 A 5315 6567140 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BODY STATION 480, LEFT BUTTOCK LINE 42.5-46 CORRODED. REPAIRED PER E A. (M) 2 L 7 2 4F A16WE 2001041200222 20010412 00222 NM 2001 4 12 ASAA0110090 1 20010209 A 5315 6567140 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 947, RIGHT BUTTOCK LINE 36, LEFT BUTTOCK LINE 47 CORRODED. REPAIR ED PER EA. (M) 2 L 7 2 4F A16WE 2001041200223 20010412 00223 NM 2001 4 12 ASAA0110091 1 20010209 A 5315 6567140 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BODY STATION 500B, LEFT BUTTOCK LINE 0-45.5 CORRODED. REPAIRED PER E A. (M) 2 L 7 2 4F A16WE 2001041200224 20010412 00224 NM 2001 4 12 ASAA0110093 1 20010210 A 5347 65671407 SEAT TRACK BOEING 737 737290C 138448V NM CABIN CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND SEAT TRACK AT BS 727-727B, LEFT BUTTOCK LINE 40 CORRODED. REPAIRED PER EA. (M) 2 L 7 2 4F A16WE 2001041200225 20010412 00225 NM 2001 4 12 ASAA0110027 1 20010129 A 5310 654656311 SHEAR TIE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 967, STRINGER 24L-26L, CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041200226 20010412 00226 NM 2001 4 12 ASAA0110017 1 20010115 A 5330 6545775 SKIN BOEING 737 737290C 138448V NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DING OUT OF LIMITS AT BS 954, STRINGER 20R-21R. REMOVED DAMAGED SEC TION OF SKIN AND REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041200228 20010412 00228 NM 2001 4 12 ASAA0140023 1 20010210 A 5310 65465482526 SHEAR TIE BOEING 737 7374Q8 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 778AS 25110 PAE - DURING MAINTENANCE INSPECTION FOUND CORROSION ON SHEAR TIE AT STATION 767 WATERLINE 149 AND BUTTLINE 10 RIGHT AND LEFT SIDES. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2001041200229 20010412 00229 NM 2001 4 12 ASAA0110108 1 20010223 A 5210 65C34071 HINGE BOEING 737 737290C 138448V NM L1 DOOR LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING MAINTENANCE CHECK, FOUND L1 DOOR HARD TO CLOSE. LUBED HINGES, DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2001041200231 20010412 00231 2001 4 12 MWEA010438 4 20010325 A 3417 ADC DOUG MD88 MD88 3023688 NM E/E BAY MALFUNCTIONED A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 805ME 48031 DURING CLIMB, CAPTAINS AIRSPEED INDICATOR INTERMITTENTLY FLAGGED. PERFORMED SELF TEST AND RETURN TO SERVICE CHECKS ON NR 1 AND NR 2 CENTRAL AIR DATA COMPUTERS. INSPECTED WIRING ON CONECTOR PLUG FOR AIRSPEED INDICATOR. NO DEFECTS NOTED. 2 L 7 2 4F RT A6WE 2001041200232 20010412 00232 SO 2001 4 12 SWIA972430 1 20010306 A 7332 WARNING LIGHT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT ILLUMINATED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 271YV 120271 ON TAKEOFF FUEL AMBER LIGHT ILLUMINATED ON MAP. OVERHEAD RIGHT SIDE LOW PRESSURE LIGHT ILLUMINATED. BOTH RIGHT FUEL PU MPS CAME ON. LOW PRESSURE LIGHT REMAINED ILLUMINATED. RIGHT FRONT PUMP WILL NOT SHUT OFF. ABORTED TAKEOFF. REPLACED RELAY K0103 AND SECURED WIRES TO RIGHT FRONT FUEL BOOST PUMP SWITCH. CLEANED AND RE-SECURED RIGHT ENGINE FUEL LOW PSI S WITCH CANNON PLUG. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 2001041200233 20010412 00233 2001 4 12 SWIA972432 4 20010309 A 2213 CONTROL PANEL EMB 120 EMB120RT SO PWA 118 PW118 NE COCKPIT MALFUNCTIONED A SWIA K NONE F FLT CONT AFFECTED AP APPROACH 1 NM 07 130G 120130 WITH GEAR DOWN, FLAP 25 DEGREES, FLIGHT CONTROLS GET STUCK WHILE ATTEMPTING TO ROLL TO THE RIGHT. CHECKED AILERONS. CO ULD NOT DUPLICATE PROBLEM. SUSPECT AUTOPILOT DID NOT DISENGAGE. INSTALLED SERVICEABLE APP-65A. OPS CHECK GOOD AT THIS TIME. P/N: 622-6684-006, S/N ON: 2614, S/N OFF: 2628. 2 L 7 2 4T 4 T RT A31SO E20NE 2001041200234 20010412 00234 WP 2001 4 12 MWEA010543 1 20010409 A 5321 995791917 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 LEFT FLOORBOARD B9 HAS SKIN CRACKS AROUND RIVITS WHICH SECURES CHANNELS AT ONE END. FABRICATED AND INSTALLED SKIN SPLIC E AND FILLER. 2 L 7 2 4F A6WE 2001041200235 20010412 00235 WP 2001 4 12 MWEA010544 1 20010409 A 5321 995782757 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 COCKPIT CENTER FLOORBOARD HAS A CRACK AT A FASTENER HOLE, LOCATED ON THE RIGHT SIDE TOWARDS THE FORWARD END. FABRICATED AND INSTALLED FLOOR BOARD AND HAT CHANNELS. 2 L 7 2 4F A6WE 2001041200236 20010412 00236 WP 2001 4 12 MWEA010545 1 20010409 A 5321 995791917 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FLOORBOARD B-2 HAS 3 EACH CRACKED HOLES IN FORWARD END. FABRICATED AND INSTALLED FLOOR BOARD REPAIR PARTS. 2 L 7 2 4F A6WE 2001041200237 20010412 00237 WP 2001 4 12 MWEA010556 1 20010410 A 5713 5911280501 STRINGER DOUG DC9 DC932 3022066 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 LEFT WING INTERNAL: LIGHT TO MODERATE CORROSION ON THE FORWARD LOWER HORIZONTAL LEG OF STRINGER 22 INBOARD END. APPROXIM ATELY 3 INCHES FROM XCW 58. REMOVED AND REPLACED STRINGER. 2 L 7 2 4F A6WE 2001041200238 20010412 00238 WP 2001 4 12 MWEA010546 1 20010409 A 5321 995791921 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FLOORBOARD B-8 HAS 2 EA CRACKED HOLES IN FORWARD END. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER. 2 L 7 2 4F A6WE 2001041200239 20010412 00239 WP 2001 4 12 MWEA010547 1 20010409 A 5711 5911307506 SPAR DOUG DC9 DC932 3022066 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 RIGHT WING INTERNAL: LIGHT CORROSION ON LOWER HORIZONTAL LEG OF FORWARD SPAR, STARTING 3 INCHES OUTBOARD OF XCW58 FOR A STRETCH OF APPROXIMATELY 12 INCHES OUTBOARD. REMOVED CORROSION AND BLENDED AREA ACCEPTABLE PER MWE/BOEING TELEX #MWX-O RD-01-00206H. 2 L 7 2 4F A6WE 2001041200240 20010412 00240 WP 2001 4 12 MWEA010558 1 20010410 A 5321 991960013 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FLOORBOARD A-8 HAS 2 CRACKS AT FASTENER HOLES ON TOP SKIN. FABRICATED AND INSTALLED REPAIR DOUBLER AND FAIRING. 2 L 7 2 4F A6WE 2001041200241 20010412 00241 WP 2001 4 12 MWEA010548 1 20010409 A 5720 5912724501 WEB DOUG DC9 DC932 3022066 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 WEB SUPPORT ASSY AT STATION XRS 137 REMOVED TO FACILITATE OTHER MAINTENANCE. CORROSION PRESENT BY FASTENER HOLES. REMO VED AND REPLACED PART. 2 L 7 2 4F A6WE 2001041200242 20010412 00242 WP 2001 4 12 MWEA010549 1 20010409 A 5711 99194013 SPAR DOUG DC9 DC932 3022066 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 LEFT AUX SPAR WEB HAS INTERGRANULAR CORROSION. FABRICATED AND INSTALLED WEB. 2 L 7 2 4F A6WE 2001041200243 20010412 00243 WP 2001 4 12 MWEA010559 1 20010410 A 5313 59114267 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 LONGERON 13 LEFT CRACKED AT BULKHEAD, STATION 965 LOWER ATTACH POINT. REMOVED DAMAGED SECTION, FABRICATED REPAIR SPLICE , LONGERON SECTION, DRILLED AND INSTALLED. 2 L 7 2 4F A6WE 2001041200244 20010412 00244 WP 2001 4 12 MWEA010560 1 20010410 A 5210 591412147 ANGLE DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 PAX DOOR AFT END DOOR PAN SPLICE ANGLE HAD A CRACK AT CUT OUT FOR BAYONET. FABRICATED REPAIR ANGLE, LOCATED, DRILLED A ND INSTALLED. 2 L 7 2 4F A6WE 2001041200245 20010412 00245 WP 2001 4 12 MWEA010561 1 20010410 A 5313 591142515 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 LONGERON 29 LEFT WAS EXFOLIATED AT STATION 913 JUST AFT OF SPLICE. REMOVED DAMAGED AREA, LOCATED, DRILLED AND INSTALLED NEW LONGERON SPLICE AND LONGERON. 2 L 7 2 4F A6WE 2001041200246 20010412 00246 WP 2001 4 12 MWEA010562 1 20010410 A 5210 995575721 BEAM DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 PAX DOOR HAD A CRACK ON THE NR 6 BEAM LOWER SIDE AT CENTER OF DOOR. STOP DRILLED CRACK, FABRICATED LOCATED DRILLED AND ISNTALLED REPAIR DOUBLERS. 2 L 7 2 4F A6WE 2001041200247 20010412 00247 WP 2001 4 12 MWEA010563 1 20010410 A 5240 991157911 ANGLE DOUG DC9 DC932 3022066 WP SERVICE DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 FORWARD SERVICE DOOR UPPER BEAM FORWARD END AHD ANGLE THAT WAS CRACKED. REMOVED ANGLE, FABRICATED, LOCATED, DRILLED AND INSTALLED NEW ANGLE. 2 L 7 2 4F A6WE 2001041200248 20010412 00248 WP 2001 4 12 MWEA010533 1 20010409 A 5321 995791917 FLOOR PANEL DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 CABIN FLOOR PANEL B3 HAS TWO FASTENER HOLES CRACKED OUT. FABRICATED AND INSTALLED DOUBLERS AND FILLERS. 2 L 7 2 4F A6WE 2001041200249 20010412 00249 WP 2001 4 12 MWEA010550 1 20010409 A 5711 9919369501 SPAR DOUG DC9 DC932 3022066 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 RIGHT WING INTERNAL: LIGHT TO MODERATE CORROSION ON XCW 58 SPAR TEE LOWER LEG FORWARD OF STRINGER 16. REMOVED CORROSION ; WING TEE IS WITHIN SERVICEABLE LIMITS PER TELEX MWX-ORD-01-00200H DATED 07 MARCH 2001. 2 L 7 2 4F A6WE 2001041200250 20010412 00250 WP 2001 4 12 MWEA010551 1 20010409 A 5711 9919369501 SPAR DOUG DC9 DC932 3022066 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 RIGHT WING INTERNAL: FOUR AREAS OF LIGHT TO MODERATE CORROSION ON XCW 58 TEE LOWER LEG BETWEEN STRINGEER 21 AND 22. REM OVED CORROSION AND BLENDED AREAS; WING TEE IS WITHIN SERVICEABLE LIMITS PER MWX-ORD-01-00200H DATED 07 MARCH 2001. 2 L 7 2 4F A6WE 2001041200251 20010412 00251 WP 2001 4 12 MWEA010552 1 20010409 A 5711 9919369501 SPAR DOUG DC9 DC932 3022066 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 RIGHT WING INTERNAL: LIGHT CORROSION ON OUTBOARD EDGE OF XCW 58 SPAR TEE LOWER LEG, FORWARD OF STRINGER 22. REMOVED COR ROSION AND BLENDED AREA; WING TEE IS WITHIN SERVICEABLE LIMITS PER TELEX MWX-ORD-01-00200H DATED 07 MARCH 2001. 2 L 7 2 4F A6WE 2001041200252 20010412 00252 WP 2001 4 12 MWEA010553 1 20010409 A 5720 991001023 STIFFENER DOUG DC9 DC932 3022066 WP WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 REMOVED STIFFNER TO FACILITATE OTHER MAINTENANCE, STATION XRS 95. FOUND TOOLMARKS AND LIGHT CORROSION ON STIFFENER. F ABRICATED AND INSTALLED STIFFENER. 2 L 7 2 4F A6WE 2001041200253 20010412 00253 WP 2001 4 12 MWEA010554 1 20010409 A 5720 991001025 STIFFENER DOUG DC9 DC932 3022066 WP WING TOOL DAMAGE A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 209ME 47730 REMOVED STIFFENER TO FACILITATE OTHER MAINTENANCE, LEFT WING STATION XRS 85. FOUND TOOL MARKS AND LIGHT CORROSION ON S TIFFENER. FABRICATED AND INSTALLED STIFFENER. 2 L 7 2 4F A6WE 2001041200254 20010412 00254 WP 2001 4 12 MWEA010555 1 20010409 A 5711 59113571 SPAR DOUG DC9 DC932 3022066 WP WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 AFT SPAR SPLICE TEE REMOVED TO FACILITATE OTHER MAINTENANCE, STATION 111.5. FOUND CORROSION. FABRICATED AND INSTALLED SPLICE TEE. 2 L 7 2 4F A6WE 2001041200255 20010412 00255 WP 2001 4 12 MWEA010513 1 20010331 A 2170 1808492 COALESCER BAG DOUG DC9 DC932 3022066 WP TAIL SECTION CONTAMINATED A MWEA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 205ME 47601 UPON START OF APU AIR, HEAVY BURNING SMELL AND MIST FILLED CABIN WITH RIGHT PACK ON. CHANGED LEFT AND RIGHT WATER SEPA RATOR SOCKS. 2 L 7 2 4F A6WE 2001041200256 20010412 00256 WP 2001 4 12 MWEA010488 1 20010402 A 5312 59101631 BULKHEAD DOUG DC9 DC914 3022034 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 AFT PRESSURE BULKHEAD RIGHT SIDE FORWARD FACE 19 INCHES OUTBOARD OF DOOR CUT OUT 2 INCHES ABOVE NR 9 RADIAL HAS SMALL DE NTS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER. 2 L 7 2 4F A6WE 2001041200257 20010412 00257 WP 2001 4 12 MWEA010489 1 20010402 A 5210 591412155 PAN DOUG DC9 DC914 3022034 WP PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FORWARD PAX DOOR PAN IS CRACKED IN UPPER AFT CORNER. REMOVED ANGLE AND UPPER PAN, LOCATED AND DRILLED NEW ANGLE AND PA N, FABRICATED REPAIR ANGELS, INSTALLED REPAIR ANGLES AND PAN. 2 L 7 2 4F A6WE 2001041200258 20010412 00258 WP 2001 4 12 MWEA010490 1 20010402 A 5312 9915554 PLATE DOUG DC9 DC914 3022034 WP BULKHEAD MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 2 EA. T-PLATES AT BULKHEAD 218, 27 LEFT TO 28 LEFT AND 27 RIGHT TO 28 RIGHT HAVE MISDRILLED HOLES, OVERSIZE HOLES AND BA D PITCH. FARICATED AND INSTALLED 2 TEE PLATES. 2 L 7 2 4F A6WE 2001041200259 20010412 00259 WP 2001 4 12 MWEA010491 1 20010402 A 5320 99155549 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 INTERCOSTAL FROM STATION 218-237 STRINGER 27 LEFT TO 28 LEFT HAS CORROSION AND 2 EA OVERSIZE HOLES ON FORWARD END UPPER FLANGE. -- REMOVED INTERCOSTAL, FABRICATED AND INSTALLED INTERCOSTAL AND FITTING. 2 L 7 2 4F A6WE 2001041200260 20010412 00260 WP 2001 4 12 MWEA010492 1 20010402 A 5320 99155543 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 INTERCOSTAL FROM STATION 218-237 STRINGER 27 RIGHT TO 28 RIGHT HAS CORROSION AND MISDRILLED HOLES AND BAD PITCH ON FORWA RD END UPPER FLANGE. REMOVED INTERCOSTAL, FABRICATED AND INSTALLED NEW INTERCOSTAL. 2 L 7 2 4F A6WE 2001041200261 20010412 00261 WP 2001 4 12 MWEA010493 1 20010402 A 5320 99576591 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE TOOL DAMAGE A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 TOOL DAMAGE IN RAIDUS, STATION 513, LONGERON 10 RIGHT, DAMAGE IN INTERCOSTAL. BLENDED MATERIAL, FABRICATED INTERCOSTAL , LOCATED AND DRILLED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001041200262 20010412 00262 WP 2001 4 12 MWEA010494 1 20010402 A 5320 9911520 WEB DOUG DC9 DC914 3022034 WP FUSELAGE PUNCTURED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 STATION 218 BULKHEAD IN FORWARD CARGO COMPARTMENT REQUIRES REPLACEMENT IN ACCORDANCE WITH TELEX MWX-ORD-01-00083H 31JAN0 1. REPLACEMENT IS DUE TO NUMEROUS PUNCTURES IN WEB. FABRICATED ALL REQUIRED PARTS, FABRICATED TEE AND FLOOR SUPPORT, I NSTALLED TEE ANGLE, FABRICATED, LOCATED AND DRILLED GILLINER SUPPORT, INSTALLED ALL PARTS. 2 L 7 2 4F A6WE 2001041200263 20010412 00263 WP 2001 4 12 MWEA010495 1 20010402 A 5310 59114243 DOOR FRAME DOUG DC9 DC914 3022034 WP FUSELAGE BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 AFT SIDE OF CARGO DOOR JAMB AT STATION 756-761 IS BENT BACK ABOUT .065 BETWEEN LONGERONS 24 TO 26 RIGHT. FABRICATED RE PAIR DOUBLERS AND INSTALLED ASSEMBLED REPAIR. 2 L 7 2 4F A6WE 2001041200264 20010412 00264 WP 2001 4 12 MWEA010496 1 20010402 A 5230 9957666 DOUBLER DOUG DC9 DC914 3022034 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 CRACK IN RADIUS OF PANS INNER LATCH SUPPORT DOUBLER. FORWARD END OF DOORS INNTER PAN AFT CARGO DOOR. REMOVED LATCH SUP PORT DOUBLER, BLENDED DAMAGE, FABRICATED, LOCATED AND DRILLED AND INSTALLED PAN INTERCOSTAL. 2 L 7 2 4F A6WE 2001041200265 20010412 00265 WP 2001 4 12 MWEA010497 1 20010402 A 5310 591014216 GUSSET DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FORWARD CARGO COMPARTMENT DOUBLER PLATE ON DOOR JAMB WEBBING AT LONGERON 28 RIGHT FROM STATION 300 TO 318 HAS LIGHT CORR OSION AND MISDRILLED HOLES. REMOVED GUSSET, FABRICATED AND INSTALLED NEW GUSSET. 2 L 7 2 4F A6WE 2001041200266 20010412 00266 WP 2001 4 12 MWEA010498 1 20010402 A 5210 5910079515 STOP DOUG DC9 DC914 3022034 WP PAX DOOR GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 PAX DOOR, DOOR STOP, SCREW HOLE GOUGED, FORWARD SIDE OF JAMB, SECOND HOLE FROM BOTTOM. BLENDED GOUGE, FABRICATED, LOC ATED AND DRILLED AND INSTALLED FILLER AND DOUBLER. 2 L 7 2 4F A6WE 2001041200267 20010412 00267 WP 2001 4 12 MWEA010499 1 20010402 A 5710 49120052 SHEAR TIE DOUG DC9 DC914 3022034 WP RT WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 RIGHT WING FUEL TANK, SHEAR TIE CRACKED AT XRS 111 OUTBOARD SIDE, BETWEEN AFT SPAR AND STRINGER NR 11. REMOVED CRACKED SHEAR TIE, LOCATED AND DRILLED NEW SHEAR TIE AND CLIP, INSTALLED CLIP. 2 L 7 2 4F A6WE 2001041200268 20010412 00268 WP 2001 4 12 MWEA010500 1 20010402 A 5710 49114612 SHEAR TIE DOUG DC9 DC914 3022034 WP RT WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 RIGHT WING FUEL TANK, SHEAR TIE CRACKED AT XRS 164 OUTBOARD SIDE BETWEEN AFT SPAR AND STRINGER NR 1. REMOVED CRACKED S HEAR TIE, BLENDED OUT DRILL MARKS, FABRICATED, LOCATED, DRILLED AND INSTALLED NEW CLIP. 2 L 7 2 4F A6WE 2001041200269 20010412 00269 WP 2001 4 12 MWEA010501 1 20010402 A 5312 49120022 CLIP DOUG DC9 DC914 3022034 WP BULKHEAD CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 REMOVED LOWER SHEAR CLIP ON BULKHEAD 69 BETWEEN STRINGER 17-18 TO FACILITATE OTHER MAINTENANCE. -- CLIP HAS CORROSION CRACKS, BLENDED CORROSION, FARICATED, LOCATED AND DRILLED AND INSTALLED NEW CLIP. 2 L 7 2 4F A6WE 2001041200270 20010412 00270 WP 2001 4 12 MWEA010503 1 20010402 A 5312 4911484514N CLIP DOUG DC9 DC914 3022034 WP BULKHEAD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 REMOVED SHEAR CLIP ON BULKHEAD 69 RIGHT WING BETWEEN STRINGER 11-12 TO FACILITATE OTHER MAINTENANCE. CLIP IS CRACKED, REMOVED, LOCATED, DRILLED AND INSTALLED NEW SHEAR CLIP. 2 L 7 2 4F A6WE 2001041200271 20010412 00271 WP 2001 4 12 MWEA010504 1 20010402 A 5720 4912003502 CLIP DOUG DC9 DC914 3022034 WP XRS 111.5 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FOUND CLIP CRACKED AT XRS 111.5, STRINGER 21-22 OUTBOARD. -- FABRICATED SHEAR TIE, LOCATED, DRILLED AND INSTALLED CLIP . 2 L 7 2 4F A6WE 2001041200272 20010412 00272 WP 2001 4 12 MWEA010505 1 20010402 A 5313 99579485 LONGERON DOUG DC9 DC914 3022034 WP FUSELAGE TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 TOOLING MARKS ON LONGERON 1 UPPER LEFT SIDE, BETWEEN STATION 237 AND 252. REMOVED INTERCOSTAL AND FINGER DOUBLER, LOCA TED AND DRILLED LONGERON AND SPLICE, FABRICATED NEW FINGER DOUBLER, LOCATED AND DRILLED NEW INTERCOSTAL, INSTALLED LONGE RON, FINGER DOUBLER AND INTERCOSTAL. 2 L 7 2 4F A6WE 2001041200273 20010412 00273 WP 2001 4 12 MWEA010506 1 20010402 A 5311 9911520385 FRAME DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FORWARD CARGO COMPARTMENT FRAME STATION 218 AFT SIDE HAS AREAS OF LIGHT CORROSION FROM LONGERON 28 RIGHT TO 29 LEFT. F ABRICATED SPLICE DOUBLERS, FRAME FILLER, AND REPAIR PARTS, INSTALLED REPAIR PARTS. 2 L 7 2 4F A6WE 2001041200274 20010412 00274 WP 2001 4 12 MWEA010507 1 20010402 A 5310 591014211 DOOR FRAME DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FORWARD CARGO COMPARTMENT DOOR JAMB WEBBING BETWEEN STATION 305 AND 377 HAS AREAS OF LIGHT CORROISON ON TOP SIDE FORM LO NGERON 26 RIGHT TO 29 RIGHT. REMOVED AND BLENDED CORROSION AND FORWARD CARGO DOOR JAMB WEB, LOCATED, DRILLED AND INST ALLED NEW DOOR JAMB WEB. 2 L 7 2 4F A6WE 2001041200275 20010412 00275 WP 2001 4 12 MWEA010508 1 20010402 A 5542 591025629 SKIN DOUG DC9 DC914 3022034 WP RUDDER DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 DENT IN RUDDER SKIN AT STATION ZR 117 ON LEFT SIDE JUST AFT OF LEADING EDGE PANEL. FABRICATED SKIN PANEL AND SKIN, INS TALLED SKIN, FABRICATED AND INSTALLED NEW BALANCE TAG. 2 L 7 2 4F A6WE 2001041200276 20010412 00276 WP 2001 4 12 MWEA010509 1 20010402 A 5311 5910163184 FRAME DOUG DC9 DC914 3022034 WP FUSELAGE TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 MODERATE TOOL DAMAGE AROUND SIX FASTENERS, JUST AFT OF FRAME STATION 817, LONGERON 11 RIGHT. REMOVED FASTENERS AND DA MAGED SECTION, FABRICATED REPAIR FILLER, DOUBELRS AND FINGER DOUBLERS, INSTALLED REPAIR PARTS. 2 L 7 2 4F A6WE 2001041200277 20010412 00277 WP 2001 4 12 MWEA010510 1 20010402 A 5320 591015835 WEB DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FORWARD CARGO COMPARTMENT WEBBING SECTION HAS BN NUT INSTALLED WITH NO PITCH DISTANCE INCLUDING TWO IN THE EDGE OF FRAME STATION 377 FLANGE, LOCATED BETWEEN LONGERON 25 RIGHT AND 26 RIGHT. - REMOVED DAMAGED WEB, FABRICATED NEW WEB AND SPLI CE REPAIR, LOCATED, DRILLED AND INSTALLED WEB, SPLICE AND DOUBLER. 2 L 7 2 4F A6WE 2001041200278 20010412 00278 WP 2001 4 12 MWEA010511 1 20010402 A 5410 99577434 INTERCOSTAL DOUG DC9 DC914 3022034 WP RT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 RIGHT PYLON INTERCOSTAL AFT OF AFT SPAR HAS A CRACK ON UPPER END. REMOVED PYLON SKIN, FABRICATED TWO EACH REPAIR DOUBL ERS, INSTALLED DOUBLERS AND SKIN. 2 L 7 2 4F A6WE 2001041200279 20010412 00279 2001 4 12 MWEA010512 4 20010401 A 3418 80098717 TRANSDUCER DOUG DC9 DC932 3022066 WP LT FUSELAGE INOPERATIVE A MWEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 31 212ME 47701 STALL INDICATOR FAILURE ANNUNCIATOR CAME ON AT CLIMBOUT WITH INTERMEDIATE WINDSHEAR INOP LIGHT. REPLACED LEFT ANGLE OF ATTACH VANE. 2 L 7 2 4F A6WE 2001041200280 20010412 00280 NM 2001 4 12 01FDEA00189 1 20010314 A 5315 65861685 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 FWD LOWER FLANGE OF FLOORBEAM BS 1010 CORRODED BEYOND LIMITS. *S/D* REMOVED, REPLACED AND FAB PER IAW FEDEX SRM 53-10- 8. 2 L 7 3 4F RT A3WE 2001041200281 20010412 00281 NM 2001 4 12 0100956744 1 20010226 A 5310 WINDOW FRAME BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A NWAA K NONE O OTHER CL CLIMB 1 GL 01 644NW 24177 ON CLIMBOUT AT 9000 FT LOUD HISSING NOISE FROM AROUND FLIGHT COMPARTMENT WINDOW 3R. FLIGHT CONTINUED UNEVENTFULLY TO DE STINATION. MAINTENANCE PERFORMED INSPECTION OF 3R WINDOW AND FOUND INTERGRANNULAR CORROSION ON BOTTOM CORNER SILL. MAI NTENANCE PERFORMED REPAIR OF LOWER SILL AND SURROUNDING AREA PER EA 67-180110 REV A. REFERENCE LOG PAGES 8723892, 15787 98, 1578795, 1578796, 1578790 AND 8723890. 2 L 7 4 4F A20WE 2001041200282 20010412 00282 EA 2001 4 12 COMA0160322 1 20010315 A 3150 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 941CA 7050 T/O CONFIG MESSAGE DURING T/O. COULD NOT DUPLICATE. OPERATIONAL CHECK OF SYSTEM NORMAL. 2 L 7 2 4F RT A21EA 2001041200283 20010412 00283 WP 2001 4 12 MWEA010393 1 20010327 A 5320 99101541 WEB DOUG DC9 DC914 3022034 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 SUBFLOOR MEMBRANE HAS (3EA) HOLES ELONGATED OR CRACKED, STATION 642-645, LX 57. FABRICATED AND INSTALLED REPAIR DOUBLE R. 2 L 7 2 4F A6WE 2001041200284 20010412 00284 WP 2001 4 12 MWEA010394 1 20010327 A 5753 59121522 SKIN DOUG DC9 DC914 3022034 WP TE FLAP DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 LEFT FLAP TRAILING EDGE SKIN HAS A DENT APPROXIMATELY FROM WING STATION XRS 137.7 AND 6 INCHES UP FROM TRAILING EDGE. R EMOVED FLAP TRAILING EDGE PANEL, FABRICATED DOUBLER, INSTALLED REPAIR AND REINSTALLED TRAILING EDGE PANEL. 2 L 7 2 4F A6WE 2001041200285 20010412 00285 WP 2001 4 12 MWEA010395 1 20010327 A 5210 39151395 HINGE DOUG DC9 DC914 3022034 WP PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 HINGE ON PAX DOOR LOWER GATE IS CRACKED. DRILLED AND INSTALLED BLIND NUTS, FABRICATED AND DRILLED SEAL RETAINER. 2 L 7 2 4F A6WE 2001041200286 20010412 00286 WP 2001 4 12 MWEA010246 1 20010405 A 5711 99116034 SPAR DOUG DC9 DC914 3022034 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 REMOVE RIGHT LOWER WING TEE P/N 9911603-4 DUE TO NUMEROUS CORROSION DISCREPANCIES. REMOVED AND REPLACED RIGHT LOWER WI NG SPAR TEE. 2 L 7 2 4F A6WE 2001041200287 20010412 00287 WP 2001 4 12 MWEA010448 1 20010328 A 5347 59108203 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE MISSING A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 NR 3 SEAT TRACK IS MISSING A LOBE AT STATION 579. REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED AND INSTALLED REPL ACEMENT SECTION OF SEAT TRACK AND REPAIR SPLICE. 2 L 7 2 4F A6WE 2001041200288 20010412 00288 WP 2001 4 12 MWEA010449 1 20010328 A 5311 99124512 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FORWARD CARGO FRAME AT STATION 370 HAD MISDRILLED HOLES AND BLEND OUTS BETWEEN LONGERON 29 RIGHT TO LONGERON 25 RIGHT. REMOVED DOOR STOP FITTINGS, FORMED, LOCATED AND DRILLED DOUBLER REPAIR, FORMED STACK ANGLES, INSTALLED REPAIR ANGLES AN D DOOR STOP FITTINGS. 2 L 7 2 4F A6WE 2001041200289 20010412 00289 WP 2001 4 12 MWEA010451 1 20010328 A 5330 595468827 DOUBLER DOUG DC9 DC932 3022066 WP WINDOW BELT CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 STEEL DOUBLER PART NUMBER 575468827 ON INSIDE SURFACE OF OUTER WINDOW RETAINER LEFT SIDE IS CRACKED, DOUBLER IS LOCATED AT STATION Y128 AT UPPER AFT CORNER OF CLEARVIEW WINDOW FRAME. REMOVED CRACKED DOUBLER, FABRICATED AND INSTALLED NEW D OUBLER. 2 L 7 2 4F A6WE 2001041200290 20010412 00290 WP 2001 4 12 MWEA010396 1 20010327 A 5320 59101411 BRACKET DOUG DC9 DC914 3022034 WP CARGO DOORWAY WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FORWARD CARGO DOOR, TWO HINGE BRACKET (DOOR JAMB) WORN. DRILLED AND INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F A6WE 2001041200291 20010412 00291 WP 2001 4 12 MWEA010429 1 20010327 A 5311 27779305 FRAME DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 AFT CARGO BAY FRAME LOWER FLANGE HAS LIGHT CORROSION STATION 786 BETWEEN LONGERON 29 LEFT AND 29 RIGHT. BLENDED CORROI SON, CUT OUT DAMAGED AREA, FABRICATED FILLER, DOUBLER AND REPAIR PARTS, INSTALLED REPAIR PARTS. 2 L 7 2 4F A6WE 2001041200292 20010412 00292 WP 2001 4 12 MWEA010430 1 20010327 A 5311 995791739 FRAME DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 AFT CARGO BAY FRAME LOWER FLANGE HAS 1 INCH X 1 INCH AREA OF LIGHT CORROSION FRAME 756 ABOVE LONGERON 27 LEFT. BLENDED CORROSION, REMOVED DAMAGE, LOCATED, DRILLED AND INSTALLED REPAIR PARTS. 2 L 7 2 4F A6WE 2001041200293 20010412 00293 WP 2001 4 12 MWEA010462 1 20010328 A 5320 99100783 WEB DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 SEVERAL HOLES MISDRILLED IN SUB FLOOR STATION 160, XO TO LX40. -- FABRICATED DOUBLER, LOCATED AND DRILLED HOLES, INSTA LLED DOUBLER. 2 L 7 2 4F A6WE 2001041200294 20010412 00294 WP 2001 4 12 WEA010463 1 20010328 A 5740 59112802 FITTING DOUG DC9 DC914 3022034 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 RIGHT WING FUEL TANK, MODERATE CORROSION ON STRINGER NR 22 FORWARD LOWER LEG, BETWEEN XRS 58 AND 69. BLENDED CORROSION , LOCATED AND DRILLED LOWER FLANGE OF STRINGER, INSTALLED STRINGER. 2 L 7 2 4F A6WE 2001041200295 20010412 00295 WP 2001 4 12 MWEA010464 1 20010328 A 5320 99100783 WEB DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 SMALL CRACK IN SUBFLOOR UNDER NR 3 SEAT TRACK AT STATION 206. STOP DRILLED CRACKS, FABRICATED AND INSTALLED REPAIR DOU BLER. 2 L 7 2 4F A6WE 2001041200296 20010412 00296 WP 2001 4 12 MWEA010465 1 20010328 A 5315 4916414 FLOORBEAM DOUG DC9 DC914 3022034 WP FUSELAGE ELONGATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FLOORBEAM AT STATION 275 UNDER NR 4 SEAT TRACK, HAS AN ELONGATED HOLE. REMOVED DAMAGE ON FLOORBEAM, FABRICATED AND INST ALLED REPAIR PARTS. 2 L 7 2 4F A6WE 2001041200297 20010412 00297 WP 2001 4 12 MWEA010466 1 20010328 A 5320 99101541 WEB DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 CABIN CUSP MEMBRANE HAS A MISDRILLED HOLE AT SEAT TRACK NR 4 STATION 250. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001041200298 20010412 00298 WP 2001 4 12 MWEA010467 1 20010328 A 5320 99101541 WEB DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 CABIN FLOOR CUSP MEMBRANE HAS A MISDRILLED HOLE AT SEAT TRACK NR 4 OUTSIDE STATION 269. FABRICATED AND INSTALLED REPAI R DOUBLER, REMOVED DAMAGE TO CUSP MEMBRANE, FABRICATED AND INSTALLED FILLER. 2 L 7 2 4F A6WE 2001041200299 20010412 00299 WP 2001 4 12 MWEA010468 1 20010328 A 5320 5910942 WEB DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 CRACK LOCATED STATION 625 IN LEFT CUSP WEB STATION 623 TO 642. FABRICATED NEW CUSP WEB, INSTALLED WEB. 2 L 7 2 4F A6WE 2001041200300 20010412 00300 WP 2001 4 12 MWEA010469 1 20010328 A 5320 99100783 WEB DOUG DC9 DC914 3022034 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 GOUGES ON SUB FLOOR BETWEEN NR 2 SEAT TRACK AND CENTER FLOOR SUPPORT AT STATION 200 TO 218. DRILLED THROUGH GOUGE AND INSTALLED RIVET, REMOVED 2 EA LOOSE AND PREVIOUSLY DRILLED THROUGH LOCK FASTENERS AND INSTALLED RIVETS AND FASTENERS, FA BRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 2001041200301 20010412 00301 WP 2001 4 12 MWEA010470 1 20010328 A 5320 9957907 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 INTERCOSTAL STATION 294 LONGERON 29 RIGHT HAS PLUGGED HOLE IN RADIUS. REMOVED, FABRICATED, LOCATED AND DRILLED INTERCO STAL. 2 L 7 2 4F A6WE 2001041200302 20010412 00302 WP 2001 4 12 MWEA010471 1 20010328 A 5313 39203341 LONGERON DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 AFT CARGO BAY LONGERON 26 LEFT HAS LIGHT CORROSION FROM STATION 660 TO 720. CORROSION REMOVED, REMOVED DAMAGED SECTION OF LONGERON, REMOVED CRACKED SECTION OF FINGER DOUBLER, FABRICATED NEW SECTION OF FINGER DOUBLER, INSTALLED FINGER DOUB LER AND NEW SECTION OF LONGERON, FABRICATED NEW SPLICES, INSTALLED LONGERON AND SPLICES. 2 L 7 2 4F A6WE 2001041200303 20010412 00303 WP 2001 4 12 MWEA010472 1 20010328 A 5320 591016344 STIFFENER DOUG DC9 DC914 3022034 WP BULKHEAD GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 NR 9 AFT PRESSURE BULKHEAD RADIAL STIFFNER HAS NUMEROUS GOUGES. DRILLED AND INSTALLED NEW NR 9 RADIAL STIFFNER. 2 L 7 2 4F A6WE 2001041200304 20010412 00304 WP 2001 4 12 MWEA010473 1 20010328 A 5410 5923938 INTERCOSTAL DOUG DC9 DC914 3022034 WP RT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 RIHT PYLON MOST INBOARD INTERCOSTAL AFT OF AFT SPAR HAS A SMALL CRACK ON UPPER FLANGE APPROXIMATELY 18 INCHES AFT OF AFT SPAR. FABRICATED AND INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F A6WE 2001041200305 20010412 00305 WP 2001 4 12 MWEA010474 1 20010328 A 5311 9958214 FRAME DOUG DC9 DC914 3022034 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FORMER REMOVED TO FACILITATE OTHER MAINTENANCE AT STATION 718 BETWEEN LONGERON 7 RIGHT AND 11 RIGHT ON NRI 7052, TO BE R EINSTALLED ON THIS NRI. -- FABRICATED, LOCATED AND INSTALLED NEW FORMER. 2 L 7 2 4F A6WE 2001041200306 20010412 00306 WP 2001 4 12 MWEA010475 1 20010328 A 5313 49122621 LONGERON DOUG DC9 DC914 3022034 WP FUSELAGE MISALIGNED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 OFF CENTER HOLES ON LONGERON 1 JUST FORWARD OF STATION 229 COMMON TO LONGERON SPLICE ASSEMBLY. -- REMOVED DAMAGED SECT ION OF LONGERON, LOCATED AND DRILLED HOLES IN NEW SECTION OF LONGERON, INSTALLED LONGERON AND SPLICE. 2 L 7 2 4F A6WE 2001041200307 20010412 00307 WP 2001 4 12 MWEA010476 1 20010328 A 5313 27779223 LONGERON DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 AFT CARGO BAY LONERON 24 LEFT HAS AREA OF LIGHT CORROSION FROM STATION 756 TO 766. BLENDED CORROSION, REMOVED DAMAGED SECTION OF LONGERON, FABRICATED LONGERON REPAIR SECTION, FABRICATED REPAIR SPLICE, INSTALLED SPLICE AND LONGERON. 2 L 7 2 4F A6WE 2001041200308 20010412 00308 WP 2001 4 12 MWEA010477 1 20010328 A 5230 59101415 PAN DOUG DC9 DC914 3022034 WP CARGO DOOR GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 AFT CARGO DOOR OUTER PAN, LOWER SECTION (BOTTOM) HAS GOUGES IN RADIUS. FABRICATED AND INSTALLED DOUBLERS. 2 L 7 2 4F A6WE 2001041200309 20010412 00309 WP 2001 4 12 MWEA010478 1 20010328 A 5310 99115811 BEAM DOUG DC9 DC914 3022034 WP SERVICE DOOR MISINSTALLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 GALLEY SERVICE DOOR BEAM NR 3 BELOW HANDLE HAS B.N. NUTS AND RIVETS INSTALLED WITH INCORRECT PITCH DISTANCE IN SEVERAL P LACES. REMOVED INNER SKIN, REMOVED RIGHT AND LEFT STOP PADS AND RIGHT AND LEFT FRAME, REMOVED STIFFNER, LOCATED AND DR ILLED NEW BEAM, INSTALLED RIGHT AND LEFT FRAME, INSTALLED STIFFNER AND BEAM. 2 L 7 2 4F A6WE 2001041200310 20010412 00310 WP 2001 4 12 MWEA010479 1 20010328 A 5620 591228509E RETAINER DOUG DC9 DC914 3022034 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 STATION 633 WINDOW RETAINER BOTTOM SECTION HAS DENTS AND NICKS AND LIGHT SURFACE CORROSION RIGHT SIDE INTERIOR. REMOVE D INNER WINDOW PANE, BLENDED AREA, REMOVED INNER AND OUTER WINDOW RETAINERS, INSTALLED NEW INNER WINDOW RETAINER, INSTAL LED OUTER AND INNER WINDOWS. 2 L 7 2 4F A6WE 2001041200311 20010412 00311 SO 2001 4 12 SWIA972434 1 20010316 A 5753 FLAP TRACK EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE WINGS DIRTY A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 203SW 120240 WHEN FLAPS ARE SELECTED 45 DEGREES OUTBOARD PAIR OF FLAPS STOPS AT APPROXIMATELY 35 DEGREES (DISAGREEMENT). FLAPS EXTEN D TO 45 DEGREES AT APPROXIMATELY 120 - 125 KTS. CLEANED FLAP TRACK AND ROLLERS. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001041200312 20010412 00312 NM 2001 4 12 EISA20010061 1 20010214 A 5311 FRAME BOEING BOEING 727 727223 1384074 NM FUSELAGE MISDRILLED A EISA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND DOUBLE DRILLED HOLES AT BS 950A STRINGER 8R TO 9R. FABRICATED AND INSTALLED ANG LE REPAIR, ALODINED AND PRIMED ANGLE REPAIR IAW SRM 53-10-4 FIG 1, 51-10-2, 51-30-2. 2 L 7 3 4F A3WE 2001041200313 20010412 00313 WP 2001 4 12 MWEA010439 1 20010327 A 5320 9915558253 ANGLE DOUG DC9 DC932 3022066 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 GOUGES IN RADIUS AND AROUND RIVETS ON APB ANGLE BRACKET FOR UPPER RIGHT STIFFNER NEAR LONGERON 9 RIGHT. REMOVED FORMER , LOCATED FASTENER HOLES ON REPLACEMENT FORMER, INSTALLED FORMER. 2 L 7 2 4F A6WE 2001041200314 20010412 00314 WP 2001 4 12 MWEA010440 1 20010327 A 5347 59108203 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 CABIN SEAT TRACK NR 3 HAS AREAS OF MODERATE CORROSION ON TOP SIDE FROM STATION 237 TO 260. BLENDED CORROSION, REMOVED S EAT TRACK SECTION, DRILLED AND INSTALLED NEW SEAT TRACK SECTION. 2 L 7 2 4F A6WE 2001041200315 20010412 00315 WP 2001 4 12 MWEA010441 1 20010327 A 5347 59108203 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 CABIN SEAT TRACK NR 3 HAS AN AREA OF MODERATE CORROSION ON TOP SIDE AT STATION 375. CUT OUT SEAT TRACK, DRILLED SEAT T RACK, INSTALLED PLUG AND CHANNEL. 2 L 7 2 4F A6WE 2001041200316 20010412 00316 WP 2001 4 12 MWEA010442 1 20010327 A 5320 9910078873 PANEL DOUG DC9 DC932 3022066 WP FUSELAGE BROKEN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 CUSP PANEL HAS BROKEN OUT AREAS UNDER SEAT TRACK NR 4 AT STATION 203. REMOVED WEB FROM AIRFRAME, FABRICATED AND INSTA LLED NEW WEB. 2 L 7 2 4F A6WE 2001041200317 20010412 00317 WP 2001 4 12 MWEA010443 1 20010327 A 5313 591141277 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 LONGERON 29 RIGHT IS CORRODED FROM STATION 323-360. REMOVED DAMAGED SECTION OF LONGERON 29 RIGHT, FABRICATED NEW LONGE RON SECTION AND REPAIR SPLICE, INSTALLED LONGERON AND SPLICE. 2 L 7 2 4F A6WE 2001041200318 20010412 00318 WP 2001 4 12 MWEA010444 1 20010327 A 5347 591028205 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 NR 4 SEAT TRACK STATION 262 AND STATION 280 HAVE AREAS OF EXFOLIATION IN TOP TRACK CHANNEL. REMOVED SEAT TRACK, FABRICA TED NEW SECTION OF TRACK, DRILLED SPLICE HOLES, FABRICATED SEAT TRACK SPLICE REPAIR PARTS, INSTALLED SECTION OF SEAT TRA CK AND SPLICES. 2 L 7 2 4F A6WE 2001041200319 20010412 00319 NM 2001 4 12 01FDEA00200 1 20010314 A 5311 BAC15171062 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 FRAME 500 DENTED RBL 67, WL 212. *S/D* REMOVED AND REPLACED PER FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 2001041200320 20010412 00320 WP 2001 4 12 MWEA010445 1 20010327 A 5347 59108207 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 NR 1 SEAT TRACK HAS AREAS OF MODERATE CORROSION ON LOWER SIDE OF INBOARD FLANGE STATION 945 - 965. ALSO CORROSION IN TOP TRACK CHANNEL AT STATION 963. REMOVED SEAT TRACK, LOCATED AND DRILLED NEW SEAT TRACK, INSTALLED SEAT TRACK. 2 L 7 2 4F A6WE 2001041200321 20010412 00321 WP 2001 4 12 MWEA010446 1 20010327 A 5315 99581871 FLOORBEAM DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 CORROSION, GOUGES AND ELONGATED HOLES ON RIGHT LAV FLOORBEAM AT STATION 980. REMOVED DAMAGED SECTIONS OF BEAM TOP SURFA CE, BLENDED GOUGES, REMOVED CORROSION, FABRICATED FILLER AND WEAR PLATE, DRILLED ANGLE AND FILLER, INSTALLED ANGLE AND F ILLERS. 2 L 7 2 4F A6WE 2001041200322 20010412 00322 WP 2001 4 12 MWEA010397 1 20010327 A 5240 991007395 DOUBLER DOUG DC9 DC914 3022034 WP ACCESS DOOR CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FORWARD ACCESSORY DOOR PAN DOUBLER ON LEFT SIDE HAS A CHAFE MARK. FABRICATED AND INSTALLED NEW DOUBLER. 2 L 7 2 4F A6WE 2001041200323 20010412 00323 WP 2001 4 12 MWEA010398 1 20010327 A 5230 59101411 FITTING DOUG DC9 DC914 3022034 WP CARGO DOOR WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FORWARD CARGO DOOR AFT HINGE MOUNT ON FUSELAGE IS WORN. -- FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001041200324 20010412 00324 WP 2001 4 12 MWEA010426 1 20010327 A 5720 9915547510 BRACKET DOUG DC9 DC914 3022034 WP RT WING CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 RIGHT WING UPPER FILLET SUPPORT BRACKET IS CHAFFING, STATION 585. -- BLENDED CHAFE AREA, FABRICATED AND INSTALLED DOUB LER, INSTALLED CHAFE STRIP AND FILLET BRACKET. 2 L 7 2 4F A6WE 2001041200325 20010412 00325 WP 2001 4 12 MWEA010427 1 20010327 A 5315 4913414 FLOORBEAM DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 MODERATE CORROSION ON TOPSIDE OF FLOORBEAM, STATION 802, THIRTY FIVE INCHES LEFT OF CENTER. REMOVED OLD FILLER, FABRICA TED NEW FILLER, FABRICATED STAINLESS STEEL SHIM, INSTALLED FILLERS. 2 L 7 2 4F A6WE 2001041200326 20010412 00326 WP 2001 4 12 MWEA010428 1 20010327 A 5320 99101541 WEB DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 STATION 777 RIGHT SIDE OUTBOARD SECTION OF SUBFLOOR HAS A CRACK IN IT. STOP DRILLED CRACK, FABRICATED AND INSTALLED RE PAIR DOUBLER. 2 L 7 2 4F A6WE 2001041200327 20010412 00327 WP 2001 4 12 MWEA010431 1 20010327 A 5320 99100783 WEB DOUG DC9 DC914 3022034 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 GOUGES, CORROSION AND CRACKS ON SUBFLOOR JUST RIGHT OF CENTER FLOOR SUPPORT FROM STATION 160 TO 200. -- FABRICATED AND INSTALLED DOUBLER AND FILLER. 2 L 7 2 4F A6WE 2001041200328 20010412 00328 WP 2001 4 12 MWEA010432 1 20010327 A 5320 99101541 WEB DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 SEVERAL AREAS OF CRACKS ON RIGHT CABIN SUBFLOOR FROM STATION 218 TO 223. STOP DRILLED CRACKS IN AREA, FABRICATED AND IN STALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001041200329 20010412 00329 WP 2001 4 12 MWEA010433 1 20010327 A 5313 27779223 LONGERON DOUG DC9 DC914 3022034 WP FUSELAGE TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 TOOLING MARKS ON LOWER SECTION OF LONGERON 10 RIGHT AFT OF STATION 218. BLENDED TOOL MARKS, FABRICATED AND INSTALLED R EPAIR DOUBLER. 2 L 7 2 4F A6WE 2001041200330 20010412 00330 WP 2001 4 12 MWEA010434 1 20010327 A 5311 27779305 FRAME DOUG DC9 DC914 3022034 WP FUSELAGE TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 TOOLING MARKS ON FRAME STATION 237, LONGERON 5 RIGHT. BLENDED, FABRICATED REPAIR DOUBLER AND PLATE, CUT OUT DAMAGED ARE A, FABRICATED REPAIR FILLER, INSTALLED REPAIR PARTS. 2 L 7 2 4F A6WE 2001041200331 20010412 00331 WP 2001 4 12 MWEA010435 1 20010327 A 5320 5911406 WEB DOUG DC9 DC914 3022034 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 DRILL START AT STATION 205 ON PAX DOOR JAMB WEB JUST BELOW LONGERON 9 LEFT. FABRICATED REPAIR DOUBLER, AND DRILLED UP S KIN, INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001041200332 20010412 00332 WP 2001 4 12 MWEA010436 1 20010327 A 5311 1387619 FRAME DOUG DC9 DC914 3022034 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 THREE FASTENERS IN RADIUS OF FRAME REPAIR DOUBLER, STATION 817, LONGERON 4-5 LEFT. REMOVED BRACKET AND DAMAGED SPLICE ANGLE, INSTALLED BRACKET, DRILLED UP AND INSTALLED NEW SPLICE ANGLE. 2 L 7 2 4F A6WE 2001041200333 20010412 00333 WP 2001 4 12 MWEA010437 1 20010327 A 5321 995791820 FLOORBOARD DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FLOORBOARD F-1 STATION 237 TO 313 RBL 48 TO RBL 58 HAS CORROSION OUT OF LIMITS ON SKIN. REMOVED OLD SKIN, FABRICATED N EW SKIN, INSTALLED SKIN. 2 L 7 2 4F A6WE 2001041200334 20010412 00334 WP 2001 4 12 MWEA010447 1 20010321 A 5414 995815957 SKIN DOUG DC9 DC932 3022066 WP RT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FOUND ONE INCH LONG CRACK AT ATTACH POINT FOR RIGHT ENGINE PYLON PANEL 8105, AFT OUTBOARD NUTPLATE AREA. INSTALLED CRA CK REPAIR PER STRUCTURAL REPAIR MANUAL 54-01, FIGURE 2. 2 L 7 2 4F A6WE 2001041200335 20010412 00335 WP 2001 4 12 MWEA010450 1 20010328 A 5315 99581821 FLOORBEAM DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 FORWARD BAG PIT FLOOR BEAM AT STATION 427, 12 INCHES RIGHT OF CENTER LINE HAD CORROSION AROUND FASTENER HOLES. CUT OUT DAMAGED SECTION, FABRICATED BEAM ANGLE REPAIR, LOCATED, DRILLED AND INSTALLED. 2 L 7 2 4F A6WE 2001041200336 20010412 00336 NM 2001 4 12 EISA20010053 1 20010214 A 5313 STRINGER BOEING BOEING 727 727223 1384074 NM FUSELAGE GOUGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND GOUGE AT STRINGER 25L BS 400. FABRICATED AND INSTALLED REPAIR DOUBLERS AT BS 40 0 STR 25L, ALODINED AND PRIMED IAW SRM 53-10-1, 53-10-2, 53-10-3 FIG 2, 51-10-2, 51-30-2. 2 L 7 3 4F A3WE 2001041200337 20010412 00337 NM 2001 4 12 EISA20010056 1 20010214 A 5330 SKIN BOEING BOEING 727 727223 1384074 NM FUSELAGE CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND MAIN CABIN SKIN CRACKED AT BS 1096 STRINGER 1. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER AT BS 1096 STR 1, ALODINED AND PRIMED, IAW SRM 53-30-3 FIG 4, 51-10-2, 51-30-2. 2 L 7 3 4F A3WE 2001041200338 20010412 00338 NM 2001 4 12 EISA20010062 1 20010214 A 5753 SKIN BOEING BOEING 727 727223 1384074 NM FOREFLAP GOUGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND LEFT WING INBOARD FOREFLAP INBOARD END UPPER AND LOWER SURFACES GOUGED. FABRICA TED DOUBLER AND FILLER, BONDED REPAIR FILLER AND DOUBLER, ALODINED AND PRIMED REPAIRS AND PAINTED IAW SRM 51-10-2, 51-40 -20 FIG 17, 57-50-2, M/M 51-20-151, 51-51-11. 2 L 7 3 4F A3WE 2001041200339 20010412 00339 NM 2001 4 12 EISA20010063 1 20010214 A 5313 BAC1498140 STRINGER BOEING BOEING 727 727223 1384074 NM FUSELAGE CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND FORWARD CARGO COMPARTMENT, LOWER LOBE AREA STRINGER 25L CRACKED/CORRODED AT ATTA CH POINT AT BS 580. FABRICATED AND INSTALLED REPAIR STRINGER SPLICE, ALODINED AND PRIMED STRINGER SPLICE IAW SRM 53-10- 3 FIG 1, 53-10-2, 51-30-2, 51-10-2. 2 L 7 3 4F A3WE 2001041200340 20010412 00340 NM 2001 4 12 EISA20010064 1 20010214 A 5313 BAC1498131 STRINGER BOEING BOEING 727 727223 1384074 NM FUSELAGE CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND FORWARD CARGO COMPARTMENT, LOWER LOBE AREA STRINGER 27R BS 560 CORRODED. FABRIC ATED AND INSTALLED STRINGER SPLICE, ALODINED AND PRIMED IAW SRM 53-10-3 FIG 1, 51-30-2, 51-10-2, M/M 51-20-11. 2 L 7 3 4F A3WE 2001041200341 20010412 00341 NM 2001 4 12 EISA20010065 1 20010214 A 5753 652163476 SKIN BOEING BOEING 727 727223 1384074 NM FLAP PUNCTURED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND RIGHT TRAILING EDGE FLAP HAS PUNCTURE HOLE. FABRICATED REPAIR DOUBLE, SEPTUM AN D CONE FILLER, BONDED REPAIRS, ALODINED, SEALED, AND PRIMED AREA IAW SRM 51-40-20 FIG 18, 57-50-2, 51-10-2, M/M 51-20-15 1. 2 L 7 3 4F A3WE 2001041200342 20010412 00342 NM 2001 4 12 EISA20010066 1 20010214 A 5313 STRINGER BOEING BOEING 727 727223 1384074 NM FUSELAGE CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND CRACK AT FORWARD CARGO COMPARTMENT, LOWER LOBE, STRINGER 26L EITHER SIDE OF BS 5 40 FRAME. STOP DRILLED, FABRICATED AND INSTALLED REPAIR ANGLE, ALODINED AND PRIMED IAW SRM 51-10-1, 53-10-3, 51-10-2, 5 1-30-2. 2 L 7 3 4F A3WE 2001041200343 20010412 00343 WP 2001 4 12 MWEA010514 1 20010404 A 5230 59101575 SKIN DOUG DC9 DC932 3022066 WP CARGO DOOR GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 GOUGE ON INNER AFT CARGO DOOR SKIN JUST BELOW FORWARD HINGE FITTING. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001041200344 20010412 00344 WP 2001 4 12 MWEA010515 1 20010404 A 5310 99124511 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FORWARD CARGO DOOR JAMB AT STATION 427 BETWEEN LONGERON 28 AND 29 RIGHT, ONE NUTPLATE AND ONE BN FASTENER HAVE CORROSION AROUND THEM ON INNER SURFACE. FABRICATED AND INSTALLED STACKED ANGLE REPAIRS. 2 L 7 2 4F A6WE 2001041200345 20010412 00345 WP 2001 4 12 MWEA010516 1 20010404 A 5310 591014211 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FORWARD CARGO DOOR JAMB LOWER WEB HAS AREAS OF LIGHT CORROSION AND BARE METAL STATION 362 TO 434. ALSO ONE MISSING NUT P LATE AT STATION 412. REMOVED AND REPLACED WEB. 2 L 7 2 4F A6WE 2001041200346 20010412 00346 WP 2001 4 12 MWEA010517 1 20010404 A 5610 56441611 FRAME DOUG DC9 DC932 3022066 WP COCKPIT WINDOW CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 CRACK INDICATION FOUND ON RADIO GRAPH WHILE PERFORMING PCI 9228 ON CAPTAINS WINDOW RETAINER FRAME. (INDICATION IS AT UPP ER AFT CORNER APPROXIMATELY 2 INCHES LONG.) FABRICATED FILLER AND REMOVED AND REPLACED EXTERNAL DOUBLER. 2 L 7 2 4F A6WE 2001041200347 20010412 00347 NM 2001 4 12 EISA20010059 1 20010214 A 5315 6520827 FLOORBEAM BOEING BOEING 727 727223 1384074 NM FUSELAGE CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND FLOORBEAM AT BS 1130 CORRODED AT NUT PLATES FROM RBL 62.5 TO LBL 62.5. FABRICAT ED AND INSTALLED REPAIR ANGLE AND RADIUS FILLER, ALODINED AND PRIMED REPAIR PARTS IAW SRM 53-10-1 FIG 5, 51-10-6, 53-10- 8 FIG 8, 51-10-2, 51-30-2. 2 L 7 3 4F A3WE 2001041200348 20010412 00348 NM 2001 4 12 EISA20010069 1 20010316 A 2133 7110033 OUTFLOW VALVE GARRETTLTD BOEING 727 7272M7 138407S NM AFT FUSELAGE STUCK A EISA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 721RW 21200 AIRCRAFT WOULD NOT PRESSURIZE IN ANY MODE, DURING CLIMB. AIR TURNBACK. REMOVED AND REPLACED OUTFLOW VALVE AND PRESSURE CONTROLLER. OPS CHECK NORMAL. 2 L 7 3 4F A3WE 2001041200349 20010412 00349 NM 2001 4 12 EISA20010051 1 20010214 A 5315 6520827 FLOORBEAM BOEING BOEING 727 727223 1384074 NM FUSELAGE CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION AT BS 620 WL 208 RBL 65 TO RBL 70 FLOORBEAM UPPER CHORD LOWER SECTION. FABRICATED AND INSTALLED REPAIR ANGLE AT BS 620 WL 208 RBL 65 TO RBL 70, ALODINED AND PRIMED REPAIR ANGLE IAW SRM 53-1 0-8 FIG 3, 51-10-2, 51-30-2. 2 L 7 3 4F A3WE 2001041200350 20010412 00350 NM 2001 4 12 EISA20010052 1 20010214 A 5311 FRAME BOEING BOEING 727 727223 1384074 NM FUSELAGE GOUGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND GOUGE AT MAIN CABIN FRAME BS 1166 WL 210 LBL 63. FABRICATED AND INSTALLED REPAI R WEB AND FLOOR SUPPORT DOUBLER AND FILLER, AT BS 1166 WL 210 LBL 63, ALODINED AND PRIMED IAW SRM 51-10-2, 51-40-3 FIG 1 , 53-10-2. 2 L 7 3 4F A3WE 2001041200351 20010412 00351 NM 2001 4 12 EISA20010054 1 20010214 A 5315 6520827 FLOORBEAM BOEING BOEING 727 727223 1384074 NM FUSELAGE CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION UNDER NUT PLATE ON FLOOR ANGLE AT BS 1148 12 FT LEFT OF BL 0 UNDER FLO OR SIDE. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER AT BS 1148 LBL 12, ALODINED AND PRIMED IAW SRM 53-10-8 FIG 8, 51-10-2, 51-10-6, 53-10-1. 2 L 7 3 4F A3WE 2001041200352 20010412 00352 WP 2001 4 12 MWEA010518 1 20010404 A 5311 591016373 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FRAME 996 RIGHT SIDE ABOVE FLOOR FITTING HAS CORROSION. REMOVED AND REPLACED FRAME REPAIR. 2 L 7 2 4F A6WE 2001041200353 20010412 00353 WP 2001 4 12 MWEA010519 1 20010404 A 5320 9911840129 STIFFENER DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 STIFFENER 9911840-129 FOUND CRACKED WHILE COMPLYING WITH NRI 5469. LOCATED AT BOTTOM OF STATION FRAME 1087 AND LEFT AFT VENTRAL STAIR JAMB. 2 L 7 2 4F A6WE 2001041200354 20010412 00354 WP 2001 4 12 MWEA010520 1 20010404 A 5313 591142235 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 LONGERON 5 RIGHT HAS 2 OPEN HOLES WITH MODERATE CORROSION AT STATION 948. REMOVED AND REPLACED LONGERON AND 3 SPLICE. 2 L 7 2 4F A6WE 2001041200355 20010412 00355 WP 2001 4 12 MWEA010521 1 20010404 A 5320 9957908501 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 INTERCOSTAL AT STATION 419 LONGERON 27 RIGHT & 29 RIGHT HAS ELONGATED HOLES AND IS BENT. FABRICATED AND INSTALLED INTE RCOSTAL. 2 L 7 2 4F A6WE 2001041200356 20010412 00356 WP 2001 4 12 MWEA010522 1 20010404 A 5320 99579081 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 INTERCOSTAL AT STATION 409, LONGERON 27 RIGHT, 29 RIGHT AHS ELONGATED HOLES AND IS BENT. FABRICATED AND INSTALLED INT ERCOSTAL. 2 L 7 2 4F A6WE 2001041200357 20010412 00357 WP 2001 4 12 MWEA010523 1 20010404 A 5320 9957908501 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 INTERCOSTAL AT STATION 400, LONGERON 27 RIGHT AND 29 RIGHT HAS ELONGATED HOLES AND IS BENT. FABRICATED AND INSTALLED OUTBOARD TEE CLIP AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001041200358 20010412 00358 WP 2001 4 12 MWEA010524 1 20010404 A 5320 99579089 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 INTERCOSTAL AT STATION 380 LONGERON 27 RIGHT AND 29 RIGHT HAS ELONGATED HOLES AND DAMAGE. FABRICATED AND INSTALLED IN TERCOSTAL AND OUTBOARD TEE CLIP. 2 L 7 2 4F A6WE 2001041200359 20010412 00359 WP 2001 4 12 MWEA010525 1 20010404 A 5315 99115451 FLOORBEAM DOUG DC9 DC932 3022066 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FLOORBEAM DEEPLY GOUGED AT STATION 917, 4 INCHES RIGHT OF CENTER. FABRICATED AND INSTALLED REPAIR DOUBLERS AND BUMPER. 2 L 7 2 4F A6WE 2001041200360 20010412 00360 WP 2001 4 12 MWEA010526 1 20010404 A 5320 59101377 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 CENTER FLOOR SUPPORT INTERCOSTAL IS EXFOLIATED AT THE FORWARD END UPPER CAP, LOCATED AFT OF STATION 237 APPROXIMATELY 3 INCHES. (REF NRI 4956). FABRICATED AND INSTALLED FLOOR SUPPORT AND SPLICE SET. 2 L 7 2 4F A6WE 2001041200361 20010412 00361 WP 2001 4 12 MWEA010527 1 20010404 A 5321 995791921 FLOOR PANEL DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 CABIN FLOOR PANEL E10, FORWARD SIDE HAS CRACKS AROUND RIVETS WHICH SECURE CHANNELS AND FORWARD CORNER HOLE IS CRACKED OU T. FABRICATED AND INSTALLED FLOOR BOARD SKIN REPAIR. 2 L 7 2 4F A6WE 2001041200362 20010412 00362 WP 2001 4 12 MWEA010528 1 20010404 A 5321 995791921 FLOOR PANEL DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 CABIN FLOOR PANEL E10 FASTENER HOLE IS CRACKED OUT, LOCATED AT AFT END, LEFT SIDE. FABRICATED AND INSTALLED PANEL REPA IR. 2 L 7 2 4F A6WE 2001041200363 20010412 00363 WP 2001 4 12 MWEA010529 1 20010404 A 5321 995791921 FLOOR PANEL DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 CABIN FLOOR PANEL E10 HAS LIGHT CORROSION AROUND FASTENER HOLES BOTTOM SIDE AND MISSING SECTION OF CHAFE STRIP, LOCATED AFT LEFT CORNER. FABRICATED AND INSTALLED SECTION OF CHAFE STRIP. 2 L 7 2 4F A6WE 2001041200364 20010412 00364 WP 2001 4 12 MWEA010530 1 20010404 A 5321 995791917 PANEL DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 CABIN FLOOR PANEL B9 HAS ONE FASTENER HOLE CRACKED OUT. FABRICATED AND INSTALLED PANEL REPAIR PARTS. 2 L 7 2 4F A6WE 2001041200365 20010412 00365 WP 2001 4 12 MWEA010531 1 20010404 A 5321 995791917 FLOOR PANEL DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 CABIN FLOOR PANEL B9 HAS SKIN CRACKS AROUND RIVETS WHICH SECURE CHANNELS AT ONE END. FABRICATED AND INSTALLED PANEL RE PAIR PART. 2 L 7 2 4F A6WE 2001041200366 20010412 00366 WP 2001 4 12 MWEA010532 1 20010404 A 5321 995791917 FLOOR PANEL DOUG DC9 DC932 3022066 WP FUSELAGE PUNCTURED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 CABIN FLOOR PANEL B3 HAS A PUNCTURE HOLE IN SKIN AT FORWARD END. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER. 2 L 7 2 4F A6WE 2001041200367 20010412 00367 NM 2001 4 12 EISA20010055 1 20010214 A 5754 WEB BOEING BOEING 727 727223 1384074 NM NR 1 SLAT CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND LEFT WING NR 1 SLAT II/B WEB FOR ACTUATOR ATTACH POINT CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER, ALODINED, AND PRIMED IAW SRM 51-40-3, 51-10-2, 51-30-2, 27-81-11, SPM 20-50-01. 2 L 7 3 4F A3WE 2001041600001 20010416 00001 NM 2001 4 16 2001UALA00143 1 20010225 A 2133 71100305 OUTFLOW VALVE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN PRESSURE FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 7299U 21894 AIRCRAFT DIVERTED TO DTW WITH PRESSURIZATION PROBLEMS. *S/D* MAINTENANCE FOUND MANY SMALL DISCREPANCIES WITH THE SYSTE M AND REPLACED SOME COMPONENTS. REPLACED OUTFLOW VALVE AND CABIN PRESSURE CONTROLLER. 2 L 7 3 4F 4 F A3WE E2EA 2001041600002 20010416 00002 NM 2001 4 16 2001UALA00150 1 20010227 A 2760 MODULE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SPOILER CONTROL FAILED A UALA O OTHER F FLT CONT AFFECTED LD LANDING 1 WP 29 506UA 24627 ON FINAL APPROACH FLAPS 15 USING SPEEDBRAKE AIRCRAFT EXPERIENCED SIGNIFICANT ROLL RATE TO RIGHT WHEN USING LAST 2 INCHES OF SPEEDBRAKE TRAVEL. SUPPLEMENTAL DATA UPDATE ACCOMPLISHED SPOILER CONTROL MODULE BITE TEST. FAULT BALLS NR 1 AND NR 3 DISPLAYED. ACCOMPLISHED OPS CHECK AND ALL SYSTEMS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600003 20010416 00003 NE 2001 4 16 2001UALA00151 2 20010228 A 7230 COMPRESSOR BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE FAILED A UALA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 WP 29 935UA 26663 726117 NR 2 ENGINE FLAME-OUT. *S/D* FOUND N2 ROTATION FROZEN. THE ENGINE WAS REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600004 20010416 00004 NM 2001 4 16 2001UALA00159 1 20010226 A 2822 7276138 CIRCUIT BREAKER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE COCKPIT FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 7460U 21914 AFTER TAKEOFF THE NUMBER TWO FUEL TANK AFT BOOST PUMP FAILED. THE AIRCRAFT RETURNED TO DEN. *S/D* REPLACED THE CIRCUI T BREAKER. OPERATIONS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001041600006 20010416 00006 NM 2001 4 16 2001UALA00164 1 20010227 A 2121 2075621MOD COOLING FAN AIRESRCH 2075621MOD BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE AC BAY OVERHEATED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7458U 21912 SMOKE IN CABIN. *S//D* THE RIGHT PACK COOLING FAN OVERHEATED. REPLACED RIGHT PACK COOLING FAN. 2 L 7 3 4F 4 F A3WE E2EA 2001041600007 20010416 00007 NM 2001 4 16 2001UALA00167 1 20010228 A 5320 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 STA 1200 - 1220 BL 0 INTERCOSTAL CRACKED SEVERAL PLACES. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED UPPER ANGLE TO INT ERCOSTAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600008 20010416 00008 NM 2001 4 16 2001UALA00169 1 20010214 A 5347 8323721 STOP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE F/O SEAT TRACK BROKEN A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 611UA 21872 FIRST OFFICERS SEAT CAME OFF SEAT TRACK. *S/D* OUTBOARD TRACK ASSY STOP ON FIRST OFFICER''S SEAT WAS FOUND BROKEN. RE PLACED SEAT TRACK STOP. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041600009 20010416 00009 NM 2001 4 16 2001UALA00171 1 20010222 A 5330 65B0277763 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 40231 0 26876 DURING ROUTINE MNTC AT SFO, MECHANIC SAW LIGHT COMING INTO RIGHT SIDE APU BATTERY COMPARTMENT FROM OUTSIDE. UPON INVEST IGATION, IT WAS DISCOVERED THAT 65B02777-601 SKIN ASSY WAS CRACKED THRU AT APPROX 3 O''CLOCK POSITION. IT APPEARS THAT THE AFT STR 11(65B02777-63) TO STA 2658 BHD FLANGE ATTACH FASTENERS WERE MISSING, BUT WERE INSTALLED AT ONE TIME. HOLES WERE WORN OVERSIZED THRU STACK-UP. *S/D* REPAIRED 65B02777-63, FRAME FLANGE AND SKIN PER SRM. 2 L 7 4 4F 4 F RT A20WE E24NE 2001041600010 20010416 00010 NM 2001 4 16 01FDEA00193 1 20010314 A 5311 6516340 FRAME BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 FRAME IS CRACKED AT CEILING SUPPORT MOUNTING POINT BS 990, WL 294, RBL 33.5. *S/D* REMOVED AND REPLACED PER FEDEX EA 7 -5310-56291 AND SRM 53-10-4, FIG 2. 2 L 7 3 4F RT A3WE 2001041600011 20010416 00011 NM 2001 4 16 01FDEA00196 1 20010314 A 5311 6516344 FRAME BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 FRAME IS CRACKED AT CEILING SUPPORT CHANNEL ATTACH POINT BS 1070, RBL 33.5, WL 294. *S/D* REMOVED AND REPLACED PER FED EX SRM 53-10-4 FIG 2 & EA 7-5310-56293. 2 L 7 3 4F RT A3WE 2001041600012 20010416 00012 NM 2001 4 16 2001UALA00173 1 20010302 A 2120 D212100600000 DUCT AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE COOLING SYSTEM DAMAGED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 821UA 944 UNABLE TO PRESSURIZE AFTER TAKEOFF. *S/D* FOUND AVIONICS COOLING SYSTEM EXTRACT DUCT DAMAGED. REPLACED DUCT. NO FURT HER PRESSURIZATION PROBLEMS REPORTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2001041600013 20010416 00013 2001 4 16 2001UALA00174 4 20010303 A 3442 066500080405 TRANSCEIVER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE WEATHER RADAR INOPERATIVE A UALA A UNSCHED LANDING P NO WARNING INDICATION NR NOT REPORTED 1 WP 29 456UA 1128 WEATHER RADAR SYSTEM INOPERATIVE. SUPPLEMENTAL DATA UPDATE REPLACED WEATHER RADAR TRANSCEIVER AND CONTROL PANEL. NO FU RTHER FAULTS OCCURED. 2 L 7 2 4F 4 F RT A28NM E40NE 2001041600014 20010416 00014 NM 2001 4 16 2001UALA00176 1 20010228 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 FWD PIT FRAME FLANGE IS DENTED STA 600 BETWEEN STR 23L ABD 24L. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME PER S RM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600015 20010416 00015 NM 2001 4 16 2001UALA00178 1 20010304 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 MAJOR REPAIR. CABIN FLOORBEAM T-CAP CORROSION BS 1640 FROM LBL 9 TO RT SIDE CREASE BEAM. *S/D* MAJOR REPAIR ACCOMPLIS HED. REPAIRED FLOORBEAM T-CAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600016 20010416 00016 NM 2001 4 16 2001UALA00179 1 20010304 A 5320 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 MAJOR REPAIR. CABIN INTERCOSTAL CORROSION BS 1638 TO 1640 RBL 13. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED INTERCOS TAL PER SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600017 20010416 00017 NM 2001 4 16 2001UALA00184 1 20010304 A 2131 7638101 CONTROLLER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN PRESSURE FAILED A UALA O OTHER O OTHER CL CLIMB 1 WP 29 7451U 21905 AUTO PRESSURIZATION FAILED DURING CLIMB. *S/D* THE PRESSURE CONTROLLER FAILED. REPLACED THE ELECTRONIC PRESSURE CONTR OLLER. 2 L 7 3 4F 4 F A3WE E2EA 2001041600018 20010416 00018 2001 4 16 2001UALA00187 4 20010304 A 3416 HG480B3 ADC BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE E/E BAY FAILED A UALA O OTHER O OTHER CR CRUISE 1 WP 29 7288U 21566 DURING CRUISE THE CAPTAINS ALTIMETER AND AUTOPILOT WERE INOPERABLE. SUPPLEMENTAL DATA UPDATE MAINTENANCE REPLACED CAPTS AIR DATA COMPUTER - OPS CHECK NORMAL (REFERENCE AMIS ITEM 9522003) NO FURTHER PROBLEMS REPORTED. 2 L 7 3 4F 4 F A3WE E2EA 2001041600019 20010416 00019 NM 2001 4 16 2001UALA00188 1 20010303 A 3397 58631 WIRE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE EMER LIGHTS BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7263U 21410 EMERGENCY EXIT SIGN IS LOOSE AND EEL LIGHTING IS INOPERABLE. SUPPLEMENTAL DATA UPDATE ACCOMPLISHED CABLE ASSEMBLY INTER IM REPAIR PER MM 33-50-32. OPERATIONS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001041600020 20010416 00020 NM 2001 4 16 2001UALA00191 1 20010305 A 5730 BOLT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUEL PANEL IMPROPER PART A UALA A UNSCHED LANDING W K INADEQUATE Q C FLUID LOSS CL CLIMB 1 WP 29 317UA 23949 FUEL SEEPING FROM THE TOP OF THE RIGHT WING. *S/D* FOUND THE FUEL LEAK TO BE RESULTING FROM BOLTS BOTTOMING OUT IN THE DOME NUTS IN THE SUSPECTED PANEL. REPLACED THE PANEL. THE BOLTS HAVE BEEN SWITCHED OUT WITH SHORTER ONES IN ORDER TO ELIMINATE THE PROBLEM. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600021 20010416 00021 NM 2001 4 16 2001UALA00192 1 20010302 A 5320 141W8518 STIFFENER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 767UA 24120 0 26918 STA 246 BUCKLED VERTICAL STIFFENERS AT LBL - 7.88, 26.05, 48 RBL - 7.88, 13.55, 20, 29.5, 47,53. *S/D* REPLACED STIFFE NERS PER SRM 53-10-51, REPAIR 3. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001041600022 20010416 00022 EU 2001 4 16 2001UALA00196 1 20010306 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 466UA 1343 AFT FUSELAGE SKIN DAMAGED FROM STRINGER 40R TO STRINGER 41R. THIS IS CLASSIFIED AS A MAJOR REPAIR. *S/D* THE DAMAGED AREA WAS CUT OUT AND REPAIRED BY THE INSTALLATION OF A FILLER AND ONE EXTERNAL DOUBLER. AN INSPECTION WAS PERFORMED AND THE REPAIR WAS APPROVED. 2 L 7 2 4F 4 F RT A28NM E40NE 2001041600023 20010416 00023 NM 2001 4 16 2001UALA00197 1 20010217 A 5315 FLOORBEAM BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 797UA 13457 0 26924 CRACKED STA 246 FLOORBEAM MID CHORD AT CUTOUT- LBL 38.5, BUCKLED STIFFENERS STA 246 FLOORBEAM - RBL 7 AND 26. *S/D* REPAIR CRACK PER SRM 53-10-51, REPAIR 1, PAGE 201. REPLACED STIFFENERS PER SRM 53-10-51, REPAIR 3, PAGE 201. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001041600024 20010416 00024 NM 2001 4 16 2001UALA00198 1 20010304 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE TORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 598UA 28751 LOWER FUSELAGE SKIN TORN APPROX 10 INCHES BY 1.5 INCHES TWO FEET AFT OF E&E COMPARTMENT DOOR. STATION 510 BETWEEN S-27L AND S-28L. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE. ACCOMPLISHED SKIN REPAIR AND INSTALLED EXTERNAL DOUB LER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600025 20010416 00025 NM 2001 4 16 2001UALA00203 1 20010306 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 MAJOR REPAIR. GALLEY FLOOR SUPPORT CORRODED WITH EXCESSIVE MATERIAL REMOVED STA 331 TO 333, RBL 25 TO 37. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600026 20010416 00026 NM 2001 4 16 2001UALA00204 1 20010306 A 5320 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 CABIN FLOOR INTERCOSTAL REQUIRES REPLACEMENT STA 365 TO 377, RBL 57. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED INTERC OSTAL PER SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600027 20010416 00027 NM 2001 4 16 2001UALA00205 1 20010306 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 RIGHT CREASE BEAM INNER CHORD STA 324 AT RBL 61 HAS EXESSIVE MATERIAL REMOVED, (25 PERCENT) .018 FRAME, .071 CHORD ANGLE . REF SRM 51-40-02. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600028 20010416 00028 NM 2001 4 16 2001UALA00206 1 20010307 A 5320 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 AFT CABIN CENTER LINE INTERCOSTAL CRACKED BETWEEN STA 1580 TO 1600. *S/D* MAJOR REPAIR ACCOMPLISHED. L-ANGLE REPLACED . 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600029 20010416 00029 NM 2001 4 16 2001UALA00207 1 20010307 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 FWD CABIN FLOOR SUPPORT CHANNEL CORRODED FROM UNDER DOOR DRAIN PAN STA 324-344 RBL 58-60. *S/D* MAJOR REPAIR ACCOMPLIS HED. REPLACED FLOOR SUPPORT. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600030 20010416 00030 NM 2001 4 16 2001UALA00208 1 20010307 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 FWD PIT FRAME IS CRACKED AT STA 540 BETWEEN STR 24L AND 25L. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME PER SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600031 20010416 00031 NM 2001 4 16 2001UALA00209 1 20010307 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 MAJOR REPAIR. FWD GALLEY FLOOR CHANNEL CORRODED STA 331 - 333 RBL 5-21. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED FL OOR SUPPORT PER SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600032 20010416 00032 NM 2001 4 16 2001UALA00210 1 20010307 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 MAJOR REPAIR. FWD GALLEY FLOOR SUPPORT CHANNEL STA 310 - 324, RBL 39-41 IS CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT CHANNEL. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600033 20010416 00033 NM 2001 4 16 2001UALA00211 1 20010307 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 MAJOR REPAIR. FWD GALLEY TIE DOWN SUPPORT BEAM STA 324 TO 345 RBL 2 HAS EXCESSIVE MATERIAL LOSS, MEASURES .018 LOSS ON .110 ORIGINAL THICKNESS. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED SUPPORT BEAM PER SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600034 20010416 00034 NM 2001 4 16 2001UALA00213 1 20010307 A 3397 58791 WIRE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE PATH LIGHTS BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7445U 21899 EMERGENCY EXIT SIGN AT DOOR 1L HAS A BROKEN POWER STRIP. SUPPLEMENTAL DATA UPDATE POWER STRIP FAILED. REPLACED POWER STR IP. OPERATIONS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001041600035 20010416 00035 NM 2001 4 16 2001UALA00214 1 20010307 A 2130 39608831 CONTROL VALVE AIRESRCH 39271611MOD BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN PRESSURE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7279U 21557 DURING CLIMB AIRCRAFT EXPERIENCED A PRESSURIZATION PROBLEM. AIRCRAFT RETURNED TO DEN. *S/D* REPLACED NR 1, AND NR 3 E NGINE HI STAGE BLEED AIR MODULATING VALVES. REPLACED LEFT AND RIGHT FLOW CONTROL VALVES. 2 L 7 3 4F 4 F A3WE E2EA 2001041600036 20010416 00036 NM 2001 4 16 2001UALA00217 1 20010309 A 5412 BULKHEAD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 MAJOR REPAIR. NR 1 PYLON INNER WEB CASTING AT NAC STA 191.86 IS CRACKED AND DENTED. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED BULKHEAD. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600037 20010416 00037 EU 2001 4 16 01FDEA00206 1 20010317 A 3610 CONTROLLER AIRBUS 310 A310203 EU PNEUMATIC SYS MALFUNCTIONED A FDEA O OTHER J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 25 430FE 394 AT 2000 ON AP W/E & W ANTI-ICE ON, FLAPS DOWN, WHEN THROTTLES CAME BACK NR 2 BLD INLINE FOR ANTI-ICE. AT 500 23 SEC LAT ER MDC SMOKE RED ECAM WARN. *S/D* REMOVED AND REPLACED NR 2 PACK COALESCER BAG PER MM 21-51-16-3. REPLACED NR 1 CONTR OLLER PER MM 36-11-19-4. NR 2 SYS NEEDS CONTROLLER (P/N 627248-1). 2 L 7 2 4F RT A35EU 2001041600038 20010416 00038 NM 2001 4 16 01FDEA00213 1 20010319 A 5311 6516345 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 DENT ON THE FRAME BS 1090, STR 26L. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 2001041600039 20010416 00039 NM 2001 4 16 EISA20010057 1 20010214 A 5315 6520827 FLOORBEAM BOEING BOEING 727 727223 1384074 NM FUSELAGE GOUGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND GOUGE AT MAIN CABIN FLOORBEAM BS 950 AT RBL 7. FABRICATED AND INSTALLED ANGLES, FILLER AND FLOORBEAM T-CAP AT BS 950 RBL 45 TO LBL 45, ALODINED AND PRIMED IAW SRM 53-10-2, 51-10-2, 53-10-8 FIG 8, 51- 30-2. 2 L 7 3 4F A3WE 2001041600040 20010416 00040 NM 2001 4 16 EISA20010058 1 20010214 A 5320 STRAP BOEING BOEING 727 727223 1384074 NM FUSELAGE CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION ON FLOOR STRAP AT BS 1130 AND LBL 24.75 UNDERSIDE. FABRICATED AND INS TALLED FLOOR STRAP, ALODINED AND PRIMED IAW SRM 51-40-2 FIG 1, 51-10-2, 51-30-2. 2 L 7 3 4F A3WE 2001041600041 20010416 00041 NM 2001 4 16 EISA20010060 1 20010214 A 5730 G11331 SKIN BOEING BOEING 727 727223 1384074 NM RT WING DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ROUTINE C-CHECK INSPECTION FOUND DELAMINATION ON PANEL SKIN AT RT WING L/E AFT OF NR 5 KRUEGER FLAP. CLEANED PRE PPED AREA BONDED FIBERGLASS OVERLAY, PRIMED AND PAINTED AREA IAW SRM 51-40-9, M/M 51-20-51, 51-20-151. 2 L 7 3 4F A3WE 2001041600042 20010416 00042 NM 2001 4 16 EISA20010067 1 20010314 A 2751 2061111 INDICATOR BOEING BOEING 727 727225 1384077 NM COCKPIT FAILED A EISA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 361KP 20627 INBOARD FLAPS LOCKOUT OCCURRED BETWEEN 2 AND 5 DEGREES. AIR TURNBACK TO IND. REMOVED AND REPLACED INBOARD FLAP POSITIO N INDICATOR. 2 L 7 3 4F A3WE 2001041600043 20010416 00043 NM 2001 4 16 EISA20010068 1 20010315 A 7930 42D107A1 SWITCH BOEING 727 727223 1384074 NM NR 2 ENGINE FAULTY A EISA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 6819 19494 DURING CRUISE AT FL 310, NR 2 ENGINE OIL FILTER BYPASS LIGHT ON F/E PANEL ILLUMINATED. PERFORMED APPROPRIATE CHECKLIST NR 2 ENGINE SHUT DOWN. REMOVED AND REPLACED OIL FILTER BY PASS SWITCH, OPS CHECK GOOD PER M/M 79-33-2. 2 L 7 3 4F A3WE 2001041600044 20010416 00044 CE 2001 4 16 C2XA01CL064 1 20010320 A 2612 24412886 FIRE LOOP BEECH 1900 1900D 1154162 CE LT ENGINE INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 87554 UE227 CLE FLIGHT 3133 THE CREW REPORTED LEFT ENGINE FIRE LOOP WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE FI RE LOOP AND PERFORMED OPERATIONAL TEST. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 2001041600045 20010416 00045 WP 2001 4 16 MWEA010357 1 20010320 A 5320 3939735527 STIFFENER DOUG DC9 DC914 3022034 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 STIFFENER FOR INTERCOSTAL AT LONGERON 9 RIGHT, STATION 568 HAS DAMAGED HOLE. REMOVED BLACK AIR DUCT AND UPPER AFT STIFF ENER, LOCATED AND DRILLED NEW STIFFENER, INSTALLED NEW STIFFENER AND BLACK AIR DUCT. 2 L 7 2 4F A6WE 2001041600046 20010416 00046 WP 2001 4 16 MWEA010358 1 20010320 A 5330 59114017 SKIN DOUG DC9 DC914 3022034 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 DENT AT STATION 185 BETWEEN LONGERON 21 AND 22 RIGHT. REMOVED DAMAGE, FABRICATED FINGER DOUBLER AND PLUG FOR SKIN, INST ALLED FINGER DOUBLER AND PLUG. 2 L 7 2 4F A6WE 2001041600048 20010416 00048 NM 2001 4 16 2001UALA00121 1 20010217 A 2597 L1912617 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GALLEY DAMAGED A UALA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 WP 29 582UA 26702 ELECTRICAL SPARKS SEEN IN REAR GALLEY. *S/D* N43 CABLE FROM CONTROLLER TO CART WAS CRUSHED AND CABLE WAS DISCONNECTED FROM CONTROLLER CAUSING SPARKS IN THE REAR GALLEY. CABLE AND PIGTAIL DISCONNECT WERE REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600049 20010416 00049 NM 2001 4 16 2001UALA00122 1 20010216 A 2450 HARNESS BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE E&E BAY BURNED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7251U 21398 STRONG BURNING ODOR IN E&E COMPARTMENT. *S/D* APU FEEDER HARNESS BURNED AT FIREWALL CONNECTOR. REPLACED APU HARNESS W IRES PER GN-MM 2-0-15-1. 2 L 7 3 4F 4 F A3WE E2EA 2001041600050 20010416 00050 NM 2001 4 16 2001UALA00126 1 20010219 A 2824 CONNECTOR BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CROSS FEED VALVE MISWIRED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 957UA 26707 DIVERTED DUE TO A FUEL IMBALANCE. *S/D* INSPECTED CROSS FEED VALVE AND FOUND CONNECTOR D792 WITH WIRES CROSSED CAUSIN G THE VALVE TO OPERATE INCORRECTLY. MOVED WIRES TO CORRECT PIN POSITION IN D792 CONNECTOR. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600051 20010416 00051 NE 2001 4 16 2001UALA00133 2 20010220 A 7531 1074741 CONTROLLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BLEED AIR DEFECTIVE A UALA K NONE O OTHER CR CRUISE 1 WP 29 565UA 26669 RIGHT DUCT PRESSURE FLUCTUATING BETWEEN 25 PSI AND 40 PSI. EPR FLUCTUATES BETWEEN 1.16 AND 1.28 FL410. *S/D* REPLACED THE RT PRSOV AND PRSOV CONTROLLER. PROBLEM WAS MOST LIKELY CAUSED BY THE PRSOV CONTROLLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600052 20010416 00052 NM 2001 4 16 2001UALA00138 1 20010221 A 2612 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COCKPIT SHORTED A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 173UA 24380 APU FIRE HANDLE LIGHT ON INTERMITTENLY, ALSO EICAS MESSAGE BUT NO FIRE WARNING AURAL CREW DIVERTING. *S/D* INVESTIGAT ION INDICATES THAT THE INTERMITTENT FLICKERING OF THE APU FIRE HANDLE, ALSO KNOWN AS FIRE EXTINGUISHING SWITCH ASSEMBLY, APPEARS TO HAVE BEEN CAUSED BY SOME METAL SHAVINGS DROPPED INTO THE WIRE INTEGRATION UNIT (WIU). THE CULPRIT WAS APPAR ENTLY CONTACTING THE WIU POSTS ON AND OFF CAUSING THE LIGHTS TO FLICKER. SINCE THE AREA HAD BEEN CLEANED UP, HOWEVER TH E AIRPLANE HAS BEEN FLYING WITHOUT DISPLAYING THAT ANOMALY. 2 L 7 4 4F 4 F RT A20WE E24NE 2001041600053 20010416 00053 NM 2001 4 16 2001UALA00139 1 20010218 A 5414 313A1355203 PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 1 NACELLE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 NR 1 NACELLE STRUT PLUME SUPPRESSOR AFT PANEL CRACKED. *S/D* FOUND PLUME PANEL CRACKED. REPAIRED PANEL. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600054 20010416 00054 2001 4 16 2001UALA00141 4 20010221 A 3417 4040800906 ADC BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE E&E BAY MALFUNCTIONED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 617UA 21877 CAPT AND FIRST OFFICER ALTIMETER EXCEED LIMITS AT 10000 FEET AND 250 KTS. GREATER THAN 75 FOOT DIFFERENCE BETWEEN PILOT AND COPILOT ALTIMETERS . AT FL260, 140 FT DIFFERENCE SPEED 332 KTS AT FL310 CAPT ALTIMTER READS 31000 FO READS 30880 . STBY ALTIMETER 31104. PROBLEM RE-OCCURRED FLIGHT 0169-24. *S/D* 140FT DIFFERENCE BETWEEN PILOT AND COPILOT ALTIMET ERS AT FL260. REPAIRED LEAKS. REPLACED RIGHT AIR DATA COMPUTER. TESTED OK, NO FAULTS FOUND. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041600055 20010416 00055 NM 2001 4 16 2001UALA00220 1 20010310 A 3350 CONNECTOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN DIRTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 364UA 24533 EMERGENCY EXIT LIGHTING FROM ROW 17 TO ROW 22 IS INOPERATIVE. CLEANED CONNECTORS. OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2001042400188 20010424 00188 NM 2001 4 24 2001UALA00221 1 20010309 A 2612 65267381 DUCT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE BROKEN A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7459U 21913 AIRCRAFT RTFL DUE TO NR 1 ENGINE FIRE WARNING LIGHT. SUPPLEMENTAL DATA UPDATE FOUND ANTI-ICE DUCT BROKEN. REPLACED DU CT. NO LEAKS FOUND AFTER DUCT REPLACEMENT. RAN ENG AT TAKEOFF POWER. NO ENGINE FIRE WARNINGS RESULTED. FIRE SYSTEM O PERATION TESTED GOOD. 2 L 7 3 4F 4 F A3WE E2EA 2001041600056 20010416 00056 NM 2001 4 16 2001UALA00222 1 20010309 A 2530 OVEN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE GALLEY OVERHEATED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7282U 21560 SMOKE IN GALLEY. SUPPLEMENTAL DATA UPDATE GALLEY OVEN ADJACENT TO DOOR 1R OVERHEATED & EMITTED SMOKE. ELECTRICAL HOOK-U PS CHECKED AND FOUND NORMAL. GALLEY OVEN TAGGED UNSERVICEABLE AND REPLACED. SUBSEQUENT OVENS NOW CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001041600057 20010416 00057 NM 2001 4 16 2001UALA00223 1 20010301 A 5512 TIP CAP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE HORIZ STAB PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7467U 21921 RT STABILIZER AFT END TIP PUNCTURED. REPAIRED TIP PER SRM 51-40-09. 2 L 7 3 4F 4 F A3WE E2EA 2001041600058 20010416 00058 NM 2001 4 16 2001UALA00224 1 20010301 A 5532 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE VERTICAL STAB DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7467U 21921 RT VERTICAL FIN PANEL 9608 IS DELAMINATED. REPAIRED PANEL PER GN MM 1-0-1-24 AND GN MM 1-0-1-66. INSTALLED NEW CORE FI LLER AND REPLACED INNER AND OUTER SKIN. 2 L 7 3 4F 4 F A3WE E2EA 2001041600059 20010416 00059 NM 2001 4 16 2001UALA00225 1 20010228 A 5753 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT FOREFLAP GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7448U 21902 RT INBOARD FOREFLAP GOUGED AT OUTBOARD LOWER SURFACE. REPAIRED FOREFLAP PER SRM 57-50-04 FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2001041600060 20010416 00060 NM 2001 4 16 2001UALA00226 1 20010301 A 5754 RIB BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE L/E SLAT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7467U 21921 NR 5 SLAT ACTUATOR ATTACHMENT RIBS ARE CRACKED. REPLACED RIBS PER BAC DWG 65-17276, GN MM 1-0-0-23, AND INSTALLED PER S RM 51-30-02. 2 L 7 3 4F 4 F A3WE E2EA 2001041600061 20010416 00061 NM 2001 4 16 2001UALA00227 1 20010301 A 5755 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE SPOILER PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7467U 21921 RT WING NR 8 GROUND SPOILER PUNCTURED. REMOVED SPOILER PER MM 27-61-01. REMOVED DOUBLERS AND LOWER SKIN, REPAIRED SKIN PER GN MM 1-0-1-66, INSTALLED PANEL PER MM 27-61-01, AND RIG CHECKED PER MM 27-60-01. OPERATIONS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001041600063 20010416 00063 NM 2001 4 16 2001UALA00229 1 20010310 A 3230 COLLAR BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE BELLCRANK OUT OF ADJ A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 994UA 22384 LEFT GEAR UNSAFE LIGHT ILLUMINATED. SUPPLEMENTAL DATA UPDATE FOUND UPLOCK BELLCRANK RETAINING COLLAR OUT OF ALIGNMENT AN D CONTACTING MANUAL RELEASE LEVER. RE-ALIGNED AND SECURED COLLAR. OPERATIONAL CHECK AND MANUAL EXTENSION OF LANDING GEAR CHECKED NORMAL. 2 L 7 2 4F 4 F A16WE E2EA 2001041600064 20010416 00064 NM 2001 4 16 2001UALA00230 1 20010310 A 2822 O-RING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE JET PUMP LEAKING A UALA A UNSCHED LANDING K FLUID LOSS NR NOT REPORTED 1 WP 29 343UA 24247 FUEL WAS NOTICED LEAKING FROM THE TOP OF THE LEFT WING. *S/D* FOUND FUEL LEAKING FROM LEADING EDGE SPAR INBOARD OF NR 2 ENG. REPLACED O-RING ON LOWER JET PUMP. NO LEAKS WITH BOOST PUMPS PRESSURIZED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600065 20010416 00065 NM 2001 4 16 2001UALA00231 1 20010312 A 3230 COLLAR BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE BELLCRANK OUT OF ADJ A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 994UA 22384 LEFT GEAR UNSAFE LIGHT ILLUMINATED. SUPPLEMENTAL DATA UPDATE FOUND UPLOCK BELL CRANK RETAINING COLLAR OUT OF ALIGNMENT AND CONTACTING MANUAL RELEASE LEVER. RE-ALIGNED AND SECURED COLLAR. OPERATIONAL CHECK AND MANUAL EXTENSION OF LANDING GE AR CHECKED NORMAL. 2 L 7 2 4F 4 F A16WE E2EA 2001041600066 20010416 00066 NM 2001 4 16 2001UALA00232 1 20010312 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 MAJOR REPAIR. DAMAGE TO FUSELAGE SKIN AND STRINGER AT CREASE BEAM STA 600 - 630 ON LEFT SIDE AT FLOOR LINE. *S/D* MAJ OR REPAIR ACCOMPLISHED. REPAIRED FUSELAGE SKIN AND STRINGER PER SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600067 20010416 00067 NM 2001 4 16 2001UALA00233 1 20010312 A 5310 BAC146T1210 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 AFT PIT BS 1285 STRINGERS 37L - 38L SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041600068 20010416 00068 NM 2001 4 16 2001UALA00234 1 20010312 A 5310 BAC146T1211 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 AFT PIT BS 1307 STRINGERS 37L - 38L SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041600070 20010416 00070 NM 2001 4 16 2001UALA00236 1 20010312 A 5310 146T1210 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 AFT PIT BS 1285 STRI8NGERS 39L - 39R SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041600071 20010416 00071 NM 2001 4 16 2001UALA00238 1 20010301 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 913UA 25291 PREVIOUS REPAIRED AREA ON BS 178 WILL INTERFER WITH THE CHORD DOUBLER. THIS IS CONSIDERED A MAJOR REPAIR. INSTALLED DO UBLER TO AFFECTED AREA. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600072 20010416 00072 NM 2001 4 16 2001UALA00239 1 20010304 A 5345 MOUNT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RADAR ANTENNA CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 310UA 23671 STATION 178 IS CRACKED AT THE RADAR ANTENNA MOUNT. THIS IS CONSIDERED A MAJOR REPAIR. INSTALLED DOUBLER TO AFFECTED AR EA. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600073 20010416 00073 NM 2001 4 16 2001UALA00240 1 20010309 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 308UA 23669 DENT ON FUSELAGE AFT OF DOOR 1L AT STA 392, WL 210, AND STRINGER 16L NEEDS PERMANENT REPAIR. THIS IS CONSIDERED A MAJOR REPAIR. ACCOMPLISHED NON-DESTRUCTIVE TESTING, NO CRACKS FOUND. ALODINED, PRIMED, AND INSTALLED DOUBLER TO AFFECTED AR EA. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001042400189 20010424 00189 NM 2001 4 24 2001UALA00244 1 20010313 A 3350 69542801 LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE L2 DOOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7274U 21421 EMERGENCY LIGHT ASSEMBLY AT DOOR 2L WAS INOPERABLE. SUPPLEMENTAL DATA UPDATE REPLACED EMERGENCY LITE ASSEMBLY AT DOOR 2L . OPERATIONAL CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001041600074 20010416 00074 NM 2001 4 16 2001UALA00245 1 20010312 A 3260 1EN161RB1 SWITCH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE MLG INTERMITTENT A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 7269U 21416 DURING GEAR RETRACTION, THE RIGHT MAIN LANDING GEAR AND DOORS LIGHT REMAIN ILLUMINATED. LIGHT DISTINGUISHED WHEN THE GE AR WAS RECYCLED. SUPPLEMENTAL DATA UPDATE FOUND SWITCH INTERMITTENT AND CONNECTOR WITH BURNED PINS. REPLACED DOOR ACTU ATOR SWITCH & ASSOCIATED CONNECTOR. OPERATIONAL CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001041600075 20010416 00075 NM 2001 4 16 2001UALA00246 1 20010313 A 5400 WEB BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 NR 1 PYLON WEB CRACKED AT OUTBOARD DRAIN HOLE JUST FORWARD OF IDG CUTOUT INSIDE PANEL 441DT. INSTALLED REPAIR DOUBLER REF: SRM 54-53-02. 2 L 7 2 4F 4 F RT A1NM E24NE 2001041600076 20010416 00076 NM 2001 4 16 2001UALA00247 1 20010312 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE TOOL DAMAGE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 MAJOR REPAIR. STR 24L STA 1296 - 1304 HAS TOOLING DAMAGE. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED STRINGER PER SRM . 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600077 20010416 00077 NM 2001 4 16 2001UALA00250 1 20010313 A 5400 WEB BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 NR 1 PYLON UPPER WEB AT IDG CABLE HOLE ACCESS HAS 2 CRACKS AT NP HOLES. INSTALLED REPAIR DOUBLER REF: SRM 54-53-02. 2 L 7 2 4F 4 F RT A1NM E24NE 2001041600078 20010416 00078 NM 2001 4 16 2001UALA00251 1 20010313 A 5400 WEB BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 NR 2 PYLON UPPER WEB AT IDG CABLE HOLE ACCESS HAS TO CRACKS. INSTALLED REPAIR DOUBLER REF: 54-53-02. 2 L 7 2 4F 4 F RT A1NM E24NE 2001041600079 20010416 00079 NM 2001 4 16 2001UALA00252 1 20010313 A 5320 WEB BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 AFT PIT BS 1280 RBL 18 FLOOR WEB CORRODED. INSTALLED REPAIR DOUBLER REF: SRM 51-70-13 FIGURE 01. 2 L 7 2 4F 4 F RT A1NM E24NE 2001041600080 20010416 00080 EU 2001 4 16 2001UALA00254 1 20010314 A 2530 2710000101 OVEN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GALLEY SMOKE A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 440UA 702 SMOKE SMELL IN THE GALLEY. SUPPLEMENTAL DATA UPDATE OVENS R41 AND R42 WERE CLEANED OF DEBRIS. OPS CHECKED GOOD. NO FURT HER INCIDENTS. 2 L 7 2 4F 4 F RT A28NM E40NE 2001041600081 20010416 00081 NM 2001 4 16 2001UALA00255 1 20010309 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 308UA 23669 LEFT HAND OVERWING FRAME BS 616L IS CRACKED. REPAIRED OVERWING FRAME BS 616L. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600082 20010416 00082 NM 2001 4 16 2001UALA00256 1 20010314 A 2782 ACTUATOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LE FLAPS FAILED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 WP 29 371UA 24540 LEADING EDGE FLAP EXTENSION PROBLEM. SUPPLEMENTAL DATA UPDATE REPLACED THE NR 3 LEADING EDGE FLAP ACTUATOR. OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600083 20010416 00083 NM 2001 4 16 2001UALA00258 1 20010309 A 5320 FITTING BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE MLG WW CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7465U 21919 RT WHEEL WELL AT STA 870 REPAIR FITTING CRACKED UNDER TRAPEZOID FITTING. REPLACED CRACKED WEB PER BAC DWG 65-25370 AND INSTALLED PER SRM 51-30-02. 2 L 7 3 4F 4 F A3WE E2EA 2001041600084 20010416 00084 NM 2001 4 16 2001UALA00259 1 20010315 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 310UA 23671 FLOORBEAM HAS 27 PERCENT MATERIAL LOSS AT STA 294. REPAIRED FLOORBEAM. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001043000183 20010430 00183 NM 2001 4 30 2001UALA00260 1 20010315 A 4990 5725149002 CHIP DETECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU COMPRESSOR LEAKING A UALA A UNSCHED LANDING H K J ELECT. POWER LOSS-50 PC FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 541UA 25253 61231 STATUS MESSAGE, APU LOW OIL QTY DISPLAYED. APU SHUTDOWN. LEFT GENERATOR DEFERRED. SUPPLEMENTAL DATA UPDATE FOUND COMPRES SOR BEARING CHIP DETECTOR BODY LEAKING. REPLACED CHIP DETECTOR ASSEMBLY, SERVICED AND LEAK TESTED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600085 20010416 00085 NM 2001 4 16 2001UALA00261 1 20010315 A 2421 MR24121 IDG BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE LT GENERATOR FAILED A UALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION NR NOT REPORTED 1 WP 29 794UA 2899 26953 LOST LT ENGINE GENERATOR AFTER DEPARTURE FROM FRA. FLIGHT CONTINUED WITH APU RUNNING UNTIL APU SHUTDOWN. DIVERTED TO LHR WHERE OVERWEIGHT LANDING WAS MADE. THE APU GEN WAS SELECTED IN PLACE OF LEFT GEN. HOWEVER, THE APU HAD AN AUTO SHUTDOW N RESULTED IN A DIVERTION TO LHR. THE REMOVED IDG FINDING REPORT IS NOT AVAILABLE AT THIS TIME. HOWEVER, IT WAS SUSPEC TED THAT THE IDG EXCITER FAILURE COULD RENDER THE IDG INOPERATIVE. THE LEFT IDG WAS REPLACED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001041600086 20010416 00086 NM 2001 4 16 2001UALA00262 1 20010314 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 644UA 25094 LT EMERGENCY EXIT LIGHTING (EEL) IN FIRST CLASS IS DAMAGED. 2 L 7 2 4F 4 F RT A1NM E24NE 2001041600087 20010416 00087 NM 2001 4 16 2001UALA00263 1 20010309 A 5754 RIB BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE L/E SLAT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7465U 21919 NR 6 SLAT ACTUATOR MOUNT RIBS CRACKED ON BOTH INBOARD AND OUTBOARD SIDES. 2 L 7 3 4F 4 F A3WE E2EA 2001041600088 20010416 00088 EA 2001 4 16 COMA0160323 1 20010318 A 2810 FUEL CAP CNDAIR CL600 CL6002B19 EA RT WING LOOSE A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 427CA 7460 RT FUEL CAP CAME LOOSE DURING T/O. INSPECTED FUEL CAP AND STRUCTURE. REINSTALLED CAP. 2 L 7 2 4F RT A21EA 2001041600089 20010416 00089 2001 4 16 COMA0160324 4 20010319 A 3425 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA E&E BAY FALSE ACTIVATION A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 812CA 2487 7381 EFIS COMP MON CAUTION DURING T/O. REPLACED THE NR 2 AHARS. 2 L 7 2 4F RT A21EA 2001041600090 20010416 00090 EA 2001 4 16 COMA0160326 1 20010319 A 7732 6917M101 HARNESS CNDAIR CL600 CL6002B19 EA LT ENGINE FAULTY A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 409CA 7441 LEFT ENGINE VIBRATION INDICATION AT 3.0. REPLACED THE EVM HARNESS. 2 L 7 2 4F RT A21EA 2001041600091 20010416 00091 EA 2001 4 16 COMA0160327 1 20010319 A 3242 50105201 BRAKE CNDAIR CL600 CL6002B19 EA LT MLG LEAKING A COMA D RETURN TO BLOCK K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 991CA 3490 7216 SMOKE COMING FROM LT MLG. REPLACED THE LT OUTBOARD BRAKE ASSY. 2 L 7 2 4F RT A21EA 2001041600092 20010416 00092 2001 4 16 COMA0160328 4 20010319 A 3140 6229820008 COMPUTER CNDAIR CL600 CL6002B19 EA E&E BAY MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 963CA 1664 7127 ENGINE OUTLINE ON EICAS HYDRAULIC PAGE, ALTERNATES FROM CYAN TO WHITE THEN BACK TO CYAN. REPLACED THE NR 2 DCU. 2 L 7 2 4F RT A21EA 2001041600093 20010416 00093 WP 2001 4 16 CALA0100236 1 20010319 A 5320 BEAM DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14062 47863 INSPECTION FOUND GALLEY G1A-G5 RT SUPPORT BEAM CORRODED. A NEW SUPPORT BEAM WAS INSTALLED IAW SRM 51-35-00. 2 L 7 3 4F A22WE 2001041600094 20010416 00094 WP 2001 4 16 CALA0100237 1 20010319 A 5341 BOLT DOUG DC10 DC1030 3023501 WP RT WING SHEARED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14062 47863 INSPECTION FOUND BOLT SHEARED IN RT WING FORWARD SPAR TO FUSELAGE ATTACH ANGLE. THE BOLT WAS REPLACED IAW SRM 51-38-01. 2 L 7 3 4F A22WE 2001041600095 20010416 00095 WP 2001 4 16 CALA0100238 1 20010319 A 5330 SKIN DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14062 47863 INSPECTION FOUND FUSELAGE BELLY SKIN CORRODED AT STA 1364. THE CORRODED AREA OF SKIN WAS CUT OUT AND A REPAIR WAS INSTA LLED IAW SRM 53-40-00, FIGURE 20. 2 L 7 3 4F A22WE 2001041600096 20010416 00096 WP 2001 4 16 CALA0100239 1 20010320 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72822 49482 INSPECTION FOUND LT AFT FUSELAGE LOWER SKIN DENTED BELOW OUTFLOW VALVE. THE AREA WAS REFORMED IAW SRM 53-04, FIGURE 38. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, 51-10-4, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 2001041600097 20010416 00097 NM 2001 4 16 CALA0100240 1 20010321 A 5310 BELTFRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 47332 23570 INSPECTION FOUND A 1.125 INCH CRACK IN BELTFRAME LOWER SECTION AT STA 807, S28R. A REPAIR ANGLE WAS INSTALLED IAW SRM 5 3-00-07, FIGURE 201. 2 L 7 2 4F RT A16WE 2001041600098 20010416 00098 SO 2001 4 16 C2XA01IA169 1 20010319 A 3234 12038594501 CONTROL BOX EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A C2XA K NONE O OTHER CL CLIMB 1 SW 27 17720 120142 IAH - FLIGHT 2953, THE CREW REPORTED THAT THE MAIN LANDING GEAR WERE SLOW TO RETRACT. THE AIRCRAFT LANDED AT IAH WITHOU T INCIDENT AND MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL MODULE, AND THE AIRCRAFT WAS APPROVED FOR RETUR N TO SERVICE. 2 L 7 2 4T RT A31SO 2001041600099 20010416 00099 EU 2001 4 16 C2XA01IA170 1 20010316 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 86842 751 286 IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED SEVERAL AISLE PATH EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANC E REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001041600100 20010416 00100 SO 2001 4 16 C2XA01IA171 1 20010313 A 2720 6405451 PIN EMB 145 EMB145 SO CONNECTOR LOOSE A C2XA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SW 27 14930 145011 IAH - FLIGHT 3426, THE CREW REPORTED MULTIPLE UNCOMMANDED RUDDER DEFLECTIONS WITH THE YAW DAMPER ENGAGED. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND PIN 12 ON CONNECTOR J0881 TO BE LOOSE. MAINTENANCE RESECURED THE PIN, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001041600101 20010416 00101 WP 2001 4 16 MWEA010360 1 20010322 A 5712 991160416 RIB DOUG DC9 DC914 3022034 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 RIGHT WING FUEL TANK, MODERATE CORROSION ON LOWER RIB CAP AT STATION 69, FROM FORWARD TO AFT SPAR. REMOVED CORROSION, F ABRICATED TEE ANGLE, LOCATED AND DRILLED NEW RIB CAP, INSTALLED NEW TEE ANGLE. 2 L 7 2 4F A6WE 2001041600102 20010416 00102 EU 2001 4 16 QXEA0100315 1 20010228 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CASTELLATION CLIP ON FRAME 12405 AT STRINGER 31 CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, AND SRM 53-21-01 , PAGE 6. 2 L 7 2 4F RT A20EU 2001041600103 20010416 00103 EU 2001 4 16 QXEA0100316 1 20010228 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CASTELLATION CLIP ON FRAME 13815 AT STRINGER 42 CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 53-21-04, PAGE 6. 2 L 7 2 4F RT A20EU 2001041600104 20010416 00104 EU 2001 4 16 QXEA0100317 1 20010228 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACKED CASTELLATION AT FRAME 5805 AND STRINGER 40. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 53-21-04, PAGE 8. 2 L 7 2 4F RT A20EU 2001041600105 20010416 00105 EU 2001 4 16 QXEA0100318 1 20010228 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACKED CASTELLATION AT FRAME 7805 AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 53-21-04, PAGE 12. 2 L 7 2 4F RT A20EU 2001041600106 20010416 00106 EU 2001 4 16 QXEA0100320 1 20010228 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACKED CASTELLATION AT FRAME 8805 AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 13 AND SRM 53-16-04, PAG E 16. 2 L 7 2 4F RT A20EU 2001041600107 20010416 00107 EU 2001 4 16 QXEA0100321 1 20010228 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACKED CASTELLATION AT FRAME 9305 AND STRINGER 46. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 53-16-04, PAGE 16. 2 L 7 2 4F RT A20EU 2001041600108 20010416 00108 EU 2001 4 16 QXEA0100322 1 20010228 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACKED CASTELLATION AT FRAME 9305A AND STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 2001041600109 20010416 00109 EU 2001 4 16 QXEA0100323 1 20010228 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACKED CASTELLATION AT FRAME 9305B AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-16-04, PAGE 20 AND SRM 53-02-13, PA GE 4. 2 L 7 2 4F RT A20EU 2001041600110 20010416 00110 EU 2001 4 16 QXEA0100324 1 20010228 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACKED CASTELLATION AT FRAME 9305C AND STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 53-16-04, PAG E 20. 2 L 7 2 4F RT A20EU 2001041600111 20010416 00111 EU 2001 4 16 QXEA0100325 1 20010228 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACKED CASTELLATION AT FRAME 9305C AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 53-16-04, PAG E 20. 2 L 7 2 4F RT A20EU 2001041600112 20010416 00112 EU 2001 4 16 QXEA0100326 1 20010302 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CABIN SEAT RAIL RIGHT HAND INBOARD HAS MINOR CORROSION. REPAIRED IAW FOKKER SRM 51-10-01, PAGE 7. 2 L 7 2 4F RT A20EU 2001041600113 20010416 00113 EU 2001 4 16 QXEA0100327 1 20010302 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CABIN SEAT RAIL LEFT HAND HAS MINOR CORROSION. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 7 AND SRM 51-10-04, PAGE 9. 2 L 7 2 4F RT A20EU 2001041600114 20010416 00114 EU 2001 4 16 QXEA0100328 1 20010311 A 5755 BUSHING FOKKER F28 F28MK4000 4990810 EU SPEED BRAKE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-SPEED BRAKE ACTUATOR TO TOWER SUPPORT BUSHINGS WORN. REPAIRED IAW HORIZON AIR EA 4-53-1456. 2 L 7 2 4F RT A20EU 2001041600115 20010416 00115 EU 2001 4 16 QXEA0100329 1 20010311 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-DENTS FOUND ON LEFT HAND SIDE OF ZONE 400 AT FRAME 18075. REPAIRED IAW FOKKER SRM 53-02-05. 2 L 7 2 4F RT A20EU 2001041600116 20010416 00116 EU 2001 4 16 QXEA0100330 1 20010311 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CHAFING FOUND ON FRAME 18075 BETWEEN STRINGER 19 AND 20. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5 AND SRM 53-25-04. 2 L 7 2 4F RT A20EU 2001041600117 20010416 00117 EU 2001 4 16 QXEA0100331 1 20010311 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-FUSELAGE SKIN AROUND ACCESS PANEL 41B DAMAGED. REPAIRED IAW HORIZON AIR EA 4-53-1453. 2 L 7 2 4F RT A20EU 2001041600118 20010416 00118 EU 2001 4 16 QXEA0100332 1 20010309 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-FUSELAGE SKIN AROUND ACCESS PANEL 41C DAMAGED. REPAIRED IAW HORIZON AIR EA 4-53-1453. 2 L 7 2 4F RT A20EU 2001041600119 20010416 00119 EU 2001 4 16 QXEA0100333 1 20010306 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 17565 AT STRINGER 11. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 2001041600120 20010416 00120 EU 2001 4 16 QXEA0100334 1 20010306 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 17565 AT STRINGER 9. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5 AND SRM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 2001041600121 20010416 00121 EU 2001 4 16 QXEA0100335 1 20010306 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 17565 AT STRINGER 8. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 15 AND SRM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 2001041600122 20010416 00122 EU 2001 4 16 QXEA0100336 1 20010306 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 17565 AT STRINGER 7. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5 AND SRM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 2001041600123 20010416 00123 EU 2001 4 16 QXEA0100337 1 20010312 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 22293 AT STRINGER 21A. REPAIRED IAW HORIZON AIR EA 4-53-1458. 2 L 7 2 4F RT A20EU 2001041600124 20010416 00124 EU 2001 4 16 QXEA0100338 1 20010312 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-FRAME 41-2 CHAFING ON STRINGER 54. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 7 AND SRM 53-02-01, PAGE 7, AND SRM 51-31 -01, PAGE 13, 14. 2 L 7 2 4F RT A20EU 2001041600125 20010416 00125 EU 2001 4 16 QXEA0100339 1 20010311 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 32-2 AT STRINGER 51. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-30-02, AND SRM 53-10-05. 2 L 7 2 4F RT A20EU 2001041600126 20010416 00126 EU 2001 4 16 QXEA0100340 1 20010311 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 24-2 AT STRINGER 33. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 53-10-05, PAGE 601, AND SRM 51-3 0-02, PAGE 9, 10. 2 L 7 2 4F RT A20EU 2001041600127 20010416 00127 EU 2001 4 16 QXEA0100341 1 20010311 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 24-2 AT STRINGER 42. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 53-10-05, PAGE 601 AND SRM 51-30 -02, PAGE 9, 10. 2 L 7 2 4F RT A20EU 2001041600128 20010416 00128 EU 2001 4 16 QXEA0100342 1 20010311 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 16-2 AT STRINGER 42. REPAIRED IAW FOKKER SRM 53-26-04 AND SRM 53-02-13, AND SRM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 2001041600129 20010416 00129 EU 2001 4 16 QXEA0100343 1 20010311 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 20075 AT STRINGER 40. REPAIRED IAW FOKKER SRM 53-26-04 AND SRM 53-02-13, AND SRM 53-10-05, PAG E 601, AND SRM 51-30-02, PAGE 9, 10. 2 L 7 2 4F RT A20EU 2001041600130 20010416 00130 EU 2001 4 16 QXEA0100344 1 20010311 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 20075 AT STRINGER 35. REPAIRED IAW FOKKER SRM 53-26-04 AND SRM 53-02-13, SRM 53-10-05, PAGE 60 1, AND SRM 51-30-02, PAGE 9, 10. 2 L 7 2 4F RT A20EU 2001041600131 20010416 00131 EU 2001 4 16 QXEA0100345 1 20010306 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 17565 AT STRINGER 53A. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5 AND SRM 53-25-04, PAGE 5, AND SRM 53-10-05, PAGE 601 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001041600132 20010416 00132 EU 2001 4 16 QXEA0100346 1 20010306 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 17565 AT STRINGER 54. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5 AND SRM 53-25-04, PAGE 5, AND S RM 51-31-01, SRM 53-10-05, 601. 2 L 7 2 4F RT A20EU 2001041600133 20010416 00133 EU 2001 4 16 QXEA0100347 1 20010306 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 17565 AT STRINGER 23. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5 AND SRM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 2001041600134 20010416 00134 EU 2001 4 16 QXEA0100348 1 20010306 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 17565 AT STRINGER 21. REPAIRED IAW FOKKER SRM 51-30-02, PAGE 9,10 AND SRM 51-31-01, PAGE 13,14 , SRM 53-10-05, PAGE 601, AND SRM 53-25-04, PAGE 4. 2 L 7 2 4F RT A20EU 2001041600135 20010416 00135 EU 2001 4 16 QXEA0100349 1 20010306 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 17565 AT STRINGER 20. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5 AND SRM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 2001041600136 20010416 00136 EU 2001 4 16 QXEA0100350 1 20010306 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 17565 AT STRINGER 17. REPAIRED IAW FOKER SRM 53-02-13, PAGE 5, SRM 51-31-01, AND SRM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 2001041600137 20010416 00137 EU 2001 4 16 QXEA0100351 1 20010311 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 58.5 AT STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-13, SRM 53-10-05, PAGE 601, AND SRM 51-30-0 2, PAGE 9, 10. 2 L 7 2 4F RT A20EU 2001041600138 20010416 00138 EU 2001 4 16 QXEA0100352 1 20010311 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 58.5 AT STRINGER 46. REPAIRED IAW FOKKER SRM 53-02-13, SRM 53-10-05, PAGE 601, AND SRM 51-30-0 2, PAGE 9, 10. 2 L 7 2 4F RT A20EU 2001041600139 20010416 00139 EU 2001 4 16 QXEA0100353 1 20010306 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 50-2 AT STRINGER 46. REPAIRED IAW FOKKER SRM 53-26-04, PAGE 20, SRM 51-31-01, PAGE 13, 14 AND SRM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 2001041600140 20010416 00140 EU 2001 4 16 QXEA0100354 1 20010306 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 50-2 AT STRINGER 25. REPAIRED IAW FOKKER SRM 53-26-04, SRM 51-31-01, SRM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 2001041600141 20010416 00141 EU 2001 4 16 QXEA0100355 1 20010306 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 50-2 AT STRINGER 52. REPAIRED IAW FOKKER SRM 53-26-04, PAGE 20 AND SRM 51-31-01, PAGE 13, 14, AND SRM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 2001041600142 20010416 00142 EU 2001 4 16 QXEA0100356 1 20010306 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 50-2 AT STRINGER 50. REPAIRED IAW FOKKER SRM 53-26-04, PAGE 20, AND SRM 51-31-01, PAGE 13, 14 AND SRM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 2001041600143 20010416 00143 EU 2001 4 16 QXEA0100357 1 20010306 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 50-2 AT STRINGER 48. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5 AND SRM 53-10-05, PAGE 601, AND SRM 51-31-01, PAGE 13, 14. 2 L 7 2 4F RT A20EU 2001041600144 20010416 00144 EU 2001 4 16 QXEA0100358 1 20010306 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 50-2 AT STRINGER 24. REPAIRED IAW FOKKER SRM 53-26-04, PAGE 20 AND SRM 51-31-01, PAGE 13, 14 A ND SRM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 2001041600145 20010416 00145 EU 2001 4 16 QXEA0100359 1 20010306 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 50-2 AT STRINGER 27. REPAIRED IAW FOKKER SRM 53-26-04, PAGE 20, AND SRM 51-31-01 PAGE 13, 14, AND SRM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 2001041600146 20010416 00146 EU 2001 4 16 QXEA0100360 1 20010311 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 41-2 AT STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 6 AND SRM 51-31-01, PAGE 13, 14, A ND SRM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 2001041600147 20010416 00147 EU 2001 4 16 QXEA0100361 1 20010306 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 32-2 AT STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, AND SRM 51-31-01, PAGE 13, 14, AND SRM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 2001041600148 20010416 00148 EU 2001 4 16 QXEA0100362 1 20010306 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 32-2 AT STRINGER 23. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-31-01, AND SRM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 2001041600149 20010416 00149 EU 2001 4 16 QXEA0100363 1 20010306 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 32-2 AT STRINGER 27. REPAIRED IAW FOKKER SRM 53-02-13, SRM 51-31-01, AND SRM 53-10-05, PAGE 60 1. 2 L 7 2 4F RT A20EU 2001041600150 20010416 00150 EU 2001 4 16 QXEA0100364 1 20010306 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 32-2 AT STRINGER 48. REPAIRED IAW FOKKER SRM 53-02-13, SRM 51-31-01, AND SRM 53-10-05, PAGE 60 1. 2 L 7 2 4F RT A20EU 2001041600151 20010416 00151 EU 2001 4 16 QXEA0100365 1 20010311 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 41-2 AND STRINGER 64. REPAIRED IAW FOKKER SRM 53-26-04 AND SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001041600152 20010416 00152 EU 2001 4 16 QXEA0100366 1 20010311 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 32-2 AND STRINGER 5. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 53-26-04. 2 L 7 2 4F RT A20EU 2001041600153 20010416 00153 EU 2001 4 16 QXEA0100367 1 20010311 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 32-2 AND STRINGER 7. REPAIRED IAW FOKKER SRM 53-26-04 AND SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001041600154 20010416 00154 EU 2001 4 16 QXEA0100368 1 20010311 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 32-2 AND STRINGER 9. REPAIRED IAW FOKKER SRM 53-26-04 AND SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001041600155 20010416 00155 EU 2001 4 16 QXEA0100369 1 20010311 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 32-2 AND STRINGER 68. REPAIRED IAW FOKKER SRM 53-26-04 AND SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001041600156 20010416 00156 EU 2001 4 16 QXEA0100370 1 20010311 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 32-2 AND STRINGER 66. REPAIRED IAW FOKKER SRM 53-26-01 AND SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001041600157 20010416 00157 EU 2001 4 16 QXEA0100371 1 20010311 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND AT FRAME 32-2 AND STRINGER 11. REPAIRED IAW FOKKER SRM 53-26-04 AND SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001041600158 20010416 00158 EU 2001 4 16 QXEA0100372 1 20010311 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACK FOUND ON FRAME 50-2 AND STRINGER 9. REPAIRED IAW FOKKER SRM 53-26-04 AND SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001041600159 20010416 00159 EU 2001 4 16 QXEA0100373 1 20010312 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-FUSELAGE SKIN AFT OF FRAME 32-2 BETWEEN STRINGER 5 & 7 DAMAGED. REPAIRED IAW FOKKER SRM 53-02-02 AND SRM 53-00-00, PAGE 2. 2 L 7 2 4F RT A20EU 2001041600160 20010416 00160 EU 2001 4 16 QXEA0100374 1 20010308 A 5541 RIB FOKKER F28 F28MK4000 4990810 EU RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-RUDDER RIBS 3, 4, 5 CRACKED AND OR BROKEN. REPAIRED IAW FOKKER SRM 55-40-04, SRM 51-31-01, AND SRM 51-31-02. 2 L 7 2 4F RT A20EU 2001041600161 20010416 00161 EU 2001 4 16 QXEA0100375 1 20010308 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-UPPER FLUTTER DAMPER BOLT TOO LONG AND HAS WORN SUPPORT STRUCTURE ABOVE. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, 14, AND HORIZON AIR EA 4-35-282. 2 L 7 2 4F RT A20EU 2001041600162 20010416 00162 EU 2001 4 16 QXEA0100376 1 20010308 A 5542 DOUBLER FOKKER F28 F28MK4000 4990810 EU RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-RUDDER ACCESS PANEL 57Y RIGHT HAND DOUBLER CRACKED. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, 14. 2 L 7 2 4F RT A20EU 2001041600163 20010416 00163 EU 2001 4 16 QXEA0100377 1 20010302 A 5540 STRINGER FOKKER F28 F28MK4000 4990810 EU RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-RUDDER STRINGER 10 CRACKED AT RIB 4. REPAIRED IAW FOKKER SRM 55-02-07, PAGE 3. 2 L 7 2 4F RT A20EU 2001041600164 20010416 00164 EU 2001 4 16 QXEA0100378 1 20010308 A 5542 DOUBLER FOKKER F28 F28MK4000 4990810 EU RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-RUDDER ACCESS PANEL 57V DOUBLER CRACKED. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, 14. 2 L 7 2 4F RT A20EU 2001041600165 20010416 00165 EU 2001 4 16 QXEA0100379 1 20010312 A 5542 DOUBLER FOKKER F28 F28MK4000 4990810 EU RUDDER MISINSTALLED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 497US 11173 YYC-RUDDER ACCESS PANEL 57V DOUBLER PLATE WAS INCORRECTLY INSTALLED. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, 14. 2 L 7 2 4F RT A20EU 2001041600166 20010416 00166 EU 2001 4 16 QXEA0100380 1 20010226 A 5711 SPAR FOKKER F28 F28MK4000 4990810 EU LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-LEFT HAND WING FRONT SPAR CAPS (UPPER AND LOWER) HAVE LIGHT FRETTING BETWEEN STATION 1825 AND 6440. REPAIRED IAW FO KKER SRM 57-01-01. 2 L 7 2 4F RT A20EU 2001041600167 20010416 00167 EU 2001 4 16 MALA010285 1 20010301 A 5330 SKIN BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 504XJ E2311 FOUND DURING C-CHECK, DENT ON RT SIDE OF FUSELAGE AT STATION 238 BELOW CABIN WINDOW REQUIRED REINSPECT WITHIN 3000 CYCLE S OR REPAIR AT C-CHECK, REPAIR WAS ACCOMPLISHED DURING C-CHECK PER EO A53034 AND SRM 53-00-12. 2 H 7 4 4F RT A49EU 2001041600168 20010416 00168 EU 2001 4 16 MALA010286 1 20010306 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 504XJ E2311 FOUND DURING C-CHECK, NR 4 SEAT RAIL HAS EVIDENCE OF CORROSION BETWEEN FRAM 18 AND 4.0 INCHES PAST FRAME 20. NR 4 SEAT RAIL WAS REMOVED AND REPLACED BETWEEN THOSE LOCATIONS PER EO A53026 AND SRM 53-00-21-201. REPAIR ACCOMPLISHED DURING C-C HECK. 2 H 7 4 4F RT A49EU 2001041600169 20010416 00169 EU 2001 4 16 MALA010287 1 20010307 A 5260 C14648 HAND RAIL BAC 146 AVRO146RJ85A 1500097 EU AIRSTAIR CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 504XJ E2311 FOUND DURING C-CHECK, CORROSION FOUND ON FWD PART OF INBOARD AIRSTAIR RAIL. DEPTH OF CORROSION IS .047 AND .030 INBOARD AIRSTAIR RAIL WAS REMOVED AND REPLACED IAW SRM 51-43-00 AND 51-42-00. REPAIR ACCOMPLISHED DURING C-CHECK. 2 H 7 4 4F RT A49EU 2001041600170 20010416 00170 EU 2001 4 16 MALA010288 1 20010307 A 5260 C14647 HAND RAIL BAC 146 AVRO146RJ85A 1500097 EU AIR STAIR CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 504XJ E2311 FOUND DURING C-CHECK, CORROSION FOUND ON OUTBOARD AIRSTAIR RAIL. DEPTH OF CORROSION IS .045; .060; .025; .039; .085 ON F LANGE, DEPTH OF CORROSION IS .045 IN RADIUS. OUTBOARD AIRSTAIR RAIL WAS REMOVED AND REPLACED IAW SRM 51-43-00. REPAIR AC COMPLISHED DURING C-CHECK. 2 H 7 4 4F RT A49EU 2001041600171 20010416 00171 EU 2001 4 16 MALA010289 1 20010323 A 5270 HANDLE SAAB SF340 SF340A 7850100 EU PAX DOOR OUT OF ADJ A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 114XJ 340A114 FLIGHT 2826, DOOR HANDLE LIGHT ILLUMINATED IN FLIGHT. COULD NOT DETERMINE IF BOTTOM PIN WAS ALLIGNED. AIR RETURN TO DTW. MAINTENANCE CLEANED AND ADJUSTED DOOR HANDLE MICRO-SWITCH. PRESSURIZED AC TO 4.8 DIFFERENTIAL. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2001041600172 20010416 00172 NM 2001 4 16 TSAA0153019 1 20010217 A 5311 65C33722 FRAME BOEING 737 737282 13844AT NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 824AL 23045 IDENTIFIED CRACK AT RIGHT UPPER CHORD BS 727, STRINGER 18A AFT HOLE BY UTILIZING HFEC AND ULTRASONIC METHOD. REMOVED AN D REPLACED RIGHT UPPER CHORD ASSEMBLY CLEANED AND TREATED ALL EXPOSED AREAS AND APPLIED CORROSION INHIBITING COMPOUND IA W ECO 1785. AIRCRAFT RETURNED TO SERVICE.(M) 2 L 7 2 4F RT A16WE 2001041600173 20010416 00173 NM 2001 4 16 TSAA0153021 1 20010220 A 5311 65C340969 FRAME BOEING 737 737282 13844AT NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 824AL 23045 IDENTIFIED A CRACK AT 2 PLACES ON THE RIGHT SIDE OF BS 1156 CHORD BETWEEN WL 281-269. STOP DRILLED ENDS OF CRACKS, REMO VED FASTENERS ON AFFECTED CHORD ASSEMBLY AND INSTALLED REPAIR STIFFENER ANGLE IAW ECO 1822. APPLIED ALODINE AND PRIMER BMS 10-11 TYPE 1 PRIMER TO ALL BARE SURFACES AND CORROSION INHIBITING COMPOUND. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2001041600174 20010416 00174 EU 2001 4 16 MALA010290 1 20010326 A 3213 SEAL SAAB SF340 SF340A 7850100 EU LT MLG STRUT LEAKING A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 103XJ 340A103 AFTER TAKEOFF FROM MSP ON FLIGHT 3156, CONFIG WARNING, TCAS, OAT HEAT FAILURE. AIR RETURN TO MSP. MAINTENANCE FOUND LT MLG STRUT BELOW SERVICE LIMITS FOR NITROGEN, HYD. FLUID, EXTENSION CURVE, ALSO NOTED FLUID LEAKING FROM STRUT. REMOVED AND REPLACED SHOCK STRUT SEAL ON LT MLG IAW TASK CARD 3211-301. OPS CHECK AND LEAK CHECK GOOD. 2 L 7 2 4T RT A52EU 2001041600175 20010416 00175 EU 2001 4 16 MALA010291 1 20010326 A 3320 LIGHT SAAB SF340 SF340A 7850100 EU CABIN OVERHEATED A MALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 15 106XJ 106 ON PREFLIGHT INSPECTION OF FLIGHT 3103, CREW REPORTED ELECTRICAL BURNING SMELL IN CABIN. FOUND FWD CABIN OVERHEAD LIGHT AT FAULT. PULLED C/B AND DEFERRED. MAINTENANCE RELAMPED, DEFERRED OVERHEAD LIGHTS PER MEL 33-20-1 MX PROCEDURES COMPLI ED WITH CB CABIN GEN PULLED ENTERED INTO DMR MX NOTIFIED. 2 L 7 2 4T RT A52EU 2001041600176 20010416 00176 2001 4 16 MALA010292 4 20010326 A 3418 002OAKY COMPUTER SAAB SF340 340B 7860101 EU STALL WARNING DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 454XJ 454 DURING TO FROM DTW ON FLIGHT 2906, LT STALL FAIL LIGHT ON TAKEOFF, PULLED E-7 C/B ORH COMPLETE. AIR RETURN TO DTW, MAINT ENANCE REPLACED STALL WARNING. COMP. PN 0020AKY SN/OFF 01114, SN/ON 01001. ALL CHECKS GOOD. MAINTENANCE REQUESTS TEST F LIGHT SEE LOG PAGE 934000. 2 L 7 2 4T RT A52EU 2001041600177 20010416 00177 EU 2001 4 16 MALA010293 1 20010328 A 7120 FITTING SAAB SF340 SF340A 7850100 EU ENGINE MOUNTS DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 79XJ 079 DURING C-CHECK IN CWA, RT IB UPPER, LT OB LOWER DRAG STRUT FITTINGS HAVE EXCESSIVE CLEARANCE. LT NACELLE BOTTOM ENGINE MOUNT FITTING HOLE. RT NACELLE BOTTOM ENGINE MOUNT FITTING HOLES HAVE EXCESSIVE CLEARANCE. REPAIRED DEFECTS IAW EO #554 048, SAAB STATEMENT 340SDS001318. 2 L 7 2 4T RT A52EU 2001041600178 20010416 00178 2001 4 16 2001UALA00084 4 20010206 A 2210 COMPUTER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE AUTOPILOT MALFUNCTIONED A UALA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 WP 29 331UA 24192 AUTOPILOT A WOULD NOT ENGAGE. SUPPLEMENTAL DATA UPDATE REMOVED AND REPLACED BOTH A & B FLIGHT CONTROL COMPUTERS AND AUTO PILOT STABILIZER TRIM SERVOS. ALL OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600179 20010416 00179 NM 2001 4 16 2001UALA00265 1 20010317 A 2130 SELECTOR SWITCH BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN PRESSURE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 202UA 24717 UNABLE TO PRESSURIZE THE AIRCRAFT AFTER DEPARTURE. SUPPLEMENTAL DATA UPDATE CABIN PRESSURE SELECTOR FAILED. REPLACED THE CABIN PRESSURE SELECTOR PANEL. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600180 20010416 00180 2001 4 16 2001UALA00266 4 20010318 A 2350 SWITCH BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE AUDIO PANEL FAILED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 322UA 23954 AUDIO CYCLING BETWEEN ALL CHANNELS. SUPPLEMENTAL DATA UPDATE REPLACED AUDIO REPRODUCER AND RESET SWITCH. OPS CHECKED NO RMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600181 20010416 00181 NM 2001 4 16 2001UALA00267 1 20010317 A 2613 CONTROLLER BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE OVERHEAT SYSTEM FAILED A UALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 29 925UA 26646 DEVELOPED A WING BODY OVERHEAT CONDITION. SUPPLEMENTAL DATA UPDATE THE OVERHEAT UNIT ASSEMBLY (CONTROLLER) FAILED. REPLA CED FAILED OVERHEAT UNIT ASSEMBLY. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600182 20010416 00182 NM 2001 4 16 2001UALA00268 1 20010317 A 2613 CONTROLLER BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE OVERHEAT SYSTEM FAILED A UALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 29 925UA 26646 DEVELOPED A WING BODY OVERHEAT CONDITION. SUPPLEMENTAL DATA UPDATE THE OVERHEAT UNIT ASSEMBLY (CONTROLLER) FAILED. REPLA CED FAILED OVERHEAT UNIT ASSEMBLY. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600183 20010416 00183 NM 2001 4 16 2001UALA00276 1 20010314 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 916UA 25383 CIRCUMFERENTIAL FRAME, STA 482A HAS FOUR CRACKS AT APPROXIMATELY CENTER LINE BELOW FLOOR. ACCOMPLISHED FRAME REPAIR. M AJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600184 20010416 00184 NM 2001 4 16 2001UALA00277 1 20010319 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 CABIN FLOORBEAM WEB STA 324 RBL 44 HAS OVERSIZED HOLE. MAJOR REPAIR ACCOMPLISHED. INSTALLED FREEZE PLUB AND T-CAP REPAI R PER SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600185 20010416 00185 NM 2001 4 16 2001UALA00278 1 20010304 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 310UA 23671 DENT LOCATED AT STA 960 LOWER FUSELAGE CENTERLINE. REPAIRED DENT. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600186 20010416 00186 NM 2001 4 16 2001UALA00280 1 20010307 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 BS 178 BULKHEAD WEB CRACKED. ACCOMPLISHED BS 178 BULKHEAD WEB REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001043000184 20010430 00184 NM 2001 4 30 2001UALA00282 1 20010320 A 2121 36169596 COOLING FAN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT FAILED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 560UA 2683 0 26660 SMOKE IN THE COCKPIT AND CABIN. SUPPLEMENTAL DATA UPDATE FOUND COOLING FAN SHAFT SHEARED AND FAN HOUSING BROKEN. THIS I S THE LATEST -6 FAN WHICH WAS INSTALLED ON THIS APU. HONEYWELL IS WORKING ON THIS LONG TIME PROBLEM WHICH HAD CAUSED MA NY DELAYS AND DISCREPANCIES, RENDERING THE APU INOPERATIVE RESULTING IN APU REMOVALS. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600188 20010416 00188 NM 2001 4 16 2001UALA00284 1 20010320 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN TOOL DAMAGE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 CABIN FLOORBEAM UPPER CAP AT STA 740 BETWEEN LT AND RT SEAT TRACK HAS TOOLING DAMAGE. MAJOR REPAIR ACCOMPLISHED. REPAI RED T CAP WITH SPLICE PER SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600189 20010416 00189 NM 2001 4 16 2001UALA00285 1 20010306 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 BS 178 BULKHEAD VERTICAL CHORD AT LBL 5.7 IS CRACKED. REPAIRED VERTICAL CHORD. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600190 20010416 00190 NM 2001 4 16 2001UALA00286 1 20010304 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BULKHEAD CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 310UA 23671 BS 178 BULKHEAD AFT SIDE LBL 5.7 INBOARD CHORD CRACKED. REPAIRED CRACKED CHORD. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600192 20010416 00192 2001 4 16 2001UALA00288 4 20010321 A 3417 4061100901 ADC BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE E/E BAY FAILED A UALA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 WP 29 301UA 23642 LOSS OF THE CAPTAINS INSTRUMENTS. SUPPLEMENTAL DATA UPDATE FOUND THE CAPTAINS DIGITAL AIR DATA COMPUTER (DADC) TO HAVE F AULTS. REPLACED THE NR 1 DADC AND CONDUCTED AN OPERATIONAL CHECK. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600193 20010416 00193 NM 2001 4 16 2001UALA00289 1 20010321 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 BS 178 BULKHEAD CRACKED AT LBL 5.7 WL 218. REPAIRED CRACKED BULKHEAD. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600194 20010416 00194 NM 2001 4 16 2001UALA00290 1 20010321 A 5230 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 309UA 23670 AFT CARGO DOOR EXTERNAL SKIN DENTED ABOVE THE HANDLE AREA. REPAIRED DENTS ON AFT CARGO DOOR. MAJOR REPAIR ACCOMPLISHED . 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600195 20010416 00195 NM 2001 4 16 2001UALA00291 1 20010321 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 309UA 23670 AFT PIT BODY FRAME STA 787 RBL 16 GOUGED. REPAIRED FRAME. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600196 20010416 00196 NM 2001 4 16 2001UALA00292 1 20010321 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 STA 1016 RBL 4 AND LBL 4 HAS EXCESSIVE MATERIAL REMOVED FROM CORROSION REMOVAL. PERFORMED STA 1016 FLOORBEAM SPLICE REP AIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600197 20010416 00197 NM 2001 4 16 2001UALA00293 1 20010321 A 3610 SHUTOFF VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ENGINE BLEED LEAKING A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 598UA 28751 ENGINE BLEED DUCT PRESSURE SPLIT. SUPPLEMENTAL DATA UPDATE TWO PRSOV SYSTEM FLEX LINES, HIGH PRESURE SHUTOFF VALVE, HIGH PRESSURE CONTROLLER AND MUSCLE LINE O-RING WERE REPLACED. HIGH POWER RUN ACCOMPLISHED, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600198 20010416 00198 NE 2001 4 16 2001UALA00294 2 20010321 A 7200 ENGINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 FAILED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 418UA 8894 1596 485 V10409 NR 2 ENGINE FIRE INDICATION. SUPPLEMENTAL DATA UPDATE FIRE INDICATION CAUSED BY LIBERATED HIGH PRESSURE COMPRESSOR (HPC) AIRFOIL, CAUSING SIGNIFICANT DOWNSTREAM DAMAGE IN ENGINE CORE GAS PATH. THE AFFECTED ENGINE WAS REMOVED AND REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2001041600199 20010416 00199 NM 2001 4 16 2001UALA00295 1 20010320 A 5310 PLATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 507UA 24743 LOWER SURFACE OF DECK PLATE HAS TOOLING DAMAGE STA 1704 TO 1707 LBL 62. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISH ED. AFT DECK PLATE WAS BLENDED TO REMOVE TOOLING DAMAGE PER FORM 8110-3 . 2 L 7 2 4F 4 F RT A2NM E17NE 2001043000002 20010430 00002 NM 2001 4 30 2001UALA00296 1 20010321 A 2121 36169596 COOLING FAN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT FAILED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 560UA 2683 0 26660 SMOKE IN CABIN AND COCKPIT. SUPPLEMENTAL DATA UPDATE FOUND COOLING FAN SHAFT SHEARED AND FAN HOUSING BROKEN. THIS IS TH E LATEST CONFIGURATION (-6) WHICH WAS INSTALLED ON THIS APU ON JUNE 11, 1999. THIS HAS BEEN A LONG TIME PROBLEM, AND HO NEYWELL IS WORKING IN FIXING THESE COOLING FAN FAILURES RESULTING IN APU REMOVALS. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600200 20010416 00200 NM 2001 4 16 2001UALA00297 1 20010322 A 2120 REGULATOR BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 952UA 26699 AIRCRAFT UNABLE TO PRESSURIZE. SUPPLEMENTAL DATA UPDATE THE NR 1 ENGINE HIGH STAGE REGULATOR FAILED. REPLACED NR 1 ENGI NE HIGH STAGE REGULATOR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600201 20010416 00201 NM 2001 4 16 2001UALA00298 1 20010322 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 AFT CABIN STA 1661 RBL 0 TOP CAP OF FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR SPLICE PER AMM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600202 20010416 00202 NM 2001 4 16 2001UALA00299 1 20010322 A 5512 SKIN AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE HORIZONTAL STAB DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 830UA 1243 LOWER SKIN OF THE RIGHT HAND HORIZONTAL STABILIZER DAMAGED APPROXIMATELY 1.5 FEET FROM THE OUTBOARD TIP. SUPPLEMENTAL DA TA UPDATE INSTALLED STRINGER REPAIR AND SKIN DOUBLER. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A28NM E40NE 2001041600204 20010416 00204 NM 2001 4 16 2001UALA00301 1 20010322 A 5310 STRUCTURE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7289U 21567 FORWARD BILGE AREA BS 580 TO 600 STRINGER 28R CORRODED. 2 L 7 3 4F 4 F A3WE E2EA 2001043000003 20010430 00003 NM 2001 4 30 2001UALA00302 1 20010321 A 4910 38601822 SPUR GEAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COOLING FAN FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 551UA 25399 APU INOP. SUPPLEMENTAL DATA UPDATE REPLACED APU. FOUND STARTER AND COOLING FAN IDLER DRIVE GEAR BROKEN IN GEARBOX. GEA RBOX HOUSING HAS DAMAGE AND WILL PROBABLY BE SCRAPPED. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600205 20010416 00205 NM 2001 4 16 2001UALA00303 1 20010321 A 5320 ANGLE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7289U 21567 LEFT HAND PRESSURE BOX ANGLE CRACKED FORWARD SIDE STATION 760. 3RD NUTPLATE UP FORWARD SIDE. 2 L 7 3 4F 4 F A3WE E2EA 2001041600206 20010416 00206 NM 2001 4 16 2001UALA00304 1 20010322 A 5320 ANGLE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7289U 21567 FORWARD PIT BILGE AREA BS 580 TO 600 BETWEEN STRINGERS 27R AND 28R SUPPORT ANGLE CRACKED. 2 L 7 3 4F 4 F A3WE E2EA 2001041600207 20010416 00207 NM 2001 4 16 2001UALA00306 1 20010319 A 3350 LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7464U 21918 LEFT FORWARD OVERWING EMERGENCY EXIT LIGHT INOP. 2 L 7 3 4F 4 F A3WE E2EA 2001042400192 20010424 00192 NM 2001 4 24 2001UALA00307 1 20010320 A 2131 CONTROLLER 39271611MOD BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN PRESSURE MALFUNCTIONED A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 7287U 21565 CABIN PRESSURIZATION IN AUTO, CABIN PRESSURE CANNOT BE MAINTAINED (CABIN ALTITUDE RISES) IN DECENT. OK IF ENGINE POWER A DDED. PRESSURIZATION SYSTEM INADEQUATE WITH POWER BACK SAME FOR BOTH STANDBY AND AUTO. SUPPLEMENTAL DATA UPDATE FOUND L OW ENG BLEED PRESSURE AT IDLE. BOTH NR 1 & NR 3 HI PRESSURE VALVES REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 2001041600208 20010416 00208 NM 2001 4 16 2001UALA00308 1 20010320 A 5720 WEB BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7446U 21900 LEFT WING TRAILING EDGE VERTICAL SUPPORT WEB HAS CRACK WBL 249.3, INBOARD SIDE OF INBOARD AILERON. 2 L 7 3 4F 4 F A3WE E2EA 2001050300313 20010503 00313 2001 5 3 2001UALA00309 4 20010319 A 3454 51RV2B RECEIVER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE E/E BAY FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 7272U 21419 BOTH VOR NR 1 AND 2 OFF FLAGS DISPLAYED WITH CDI NEEDLES FLUX 10 - 20 DEGREES. SUPPLEMENTAL DATA UPDATE NR 1 NAV RECEI VER FAILED. REPLACED NR 1 NAV RECEIVER. OPERATIONS CHECK NR 1 & 2 NAV SATISFACTORY PER MM 42-20-02. 2 L 7 3 4F 4 F A3WE E2EA 2001042400193 20010424 00193 NM 2001 4 24 2001UALA00310 1 20010319 A 5270 STOP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE PAX DOOR OUT OF ADJ A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 7447U 21901 CREW REJECTED TAKEOFF AT 95 KNOTS DUE TO FORWARD DOOR LIGHT. SUPPLEMENTAL DATA UPDATE ADJUSTED DOOR STOPS AND CHECKED DO OR WARNING SYSTEM PER MAINTENANCE MANUAL. OPERATIONAL CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001042400194 20010424 00194 NM 2001 4 24 2001UALA00311 1 20010317 A 2780 CONTROLLER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LE FLAPS MALFUNCTIONED A UALA J A DUMP FUEL UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 WP 29 7461U 21915 FLIGHT RETURNED TO LAS WITH NR 2 LEADING EDGE FLAP PROBLEM. FLAP WOULD NOT RETRACT. SUPPLEMENTAL DATA UPDATE ADJUSTED NR 2 LEADING EDGE FLAP LINKAGE AND CYCLED FLAPS SEVERAL TIMES. CHECKS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001041600209 20010416 00209 EU 2001 4 16 MALA010300 1 20010112 A 2760 SPOILER BAC 146 AVRO146RJ85A 1500097 EU RIGHT CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 524XJ E2349 FOUND DURING C-CHECK, IN ST JOHNS NF. FOUND RUB (CHAFE) FOUND ON RT FWD FLAP (TOP) UNDER ROLL SPOILER. MAINTENANCE RUB BED CHAFE, REPAIRED IAW REF: BARA/AVR/5274/01. A DV INSPECTION REQUIRED EVERY 250 CYCLES, ADU AND EDDY CURRENT, REQUIRED AT 500 CYCLES WITH PERMANENT REPAIR WITHIN 1,000 CYCLES. 2 H 7 4 4F RT A49EU 2001041600210 20010416 00210 EU 2001 4 16 MALA010294 1 20010123 A 5330 SKIN BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE GOUGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 524XJ E2349 FOUND DURING C-CHECK, IN ST. JOHN''S NF, GOUGE IN A/C APPROXIMATELY 5 INCHES BELOW LT FWD DOOR APERTURE AND 1 INCH FWD OF FRAME 18. MAINTENANCE REPAIRED GOUGE, IAW BAE REPAIR LEAFLET HC537H9457. REPEAT INSPECTION ON INTERNAL AND EXTERNAL AREA EVERY 2,000 CYCLES. INSPECTION IS TO BE DETAILED VISUAL. 2 H 7 4 4F RT A49EU 2001041600211 20010416 00211 EU 2001 4 16 MALA010295 1 20010103 A 5260 HAND RAIL BAC 146 AVRO146RJ85A 1500097 EU AIRSTAIR CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 524XJ E2349 FOUND DURING C-CHECK, IN ST JOHNS, NF. IB FWD AIRSTAIR GUIDE RAIL CORRODED ON FWD. ENG. REPLACE WITH NEW RAIL. MAINTE NANCE REPLACED NEW AIRSTAIR GUIDE RAIL, REPLACED IAW BAE SRM PROCEDURES. 2 H 7 4 4F RT A49EU 2001041600212 20010416 00212 EU 2001 4 16 MALA010296 1 20010102 A 5330 SKIN BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 524XJ E2349 FOUND DURING C-CHECK, IN ST. JOHNS, NF. DENT ON LT SIDE APPROXIMATELY ONE FOOT AFT OF FWD ENTRY DOOR. REQUIRES FURTHER INSPECTION OR REPAIR. MAINTENANCE REPAIRED DENT IAW BAE REPAIR DWB HC536H9316 AND BAE REPAIR INSTRUCTION LEAFLET. 2 H 7 4 4F RT A49EU 2001041600213 20010416 00213 EU 2001 4 16 MALA010297 1 20010115 A 2760 LINE BAC 146 AVRO146RJ85A 1500097 EU SPOILER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 524XJ E2349 FOUND DURING C-CHECK, IN ST. JOHNS, NF. THE PRESSURE LINE FOR THE RT ROLL SPOILER AT RIB 12 IS CHAFED, REQUIRES REPLACE MENT; TPC REF: 29-10-03-50, ITEM 91, IN STOCK. MAINTENANCE REPLACED LINE AS PER AMM 20-09-121, CHECKED FOR OPERATION AS PER AMM 27-62-11. PERFORMED LEAK CHECK FOR PRESSURE LINE, RAISED FLAP TO ZERO, RAISED RT OB ROLL SPOILER AND INSPECT NE WLY INSTALLED LINE FOR RUBBING ON FLAP. 2 H 7 4 4F RT A49EU 2001041600214 20010416 00214 EU 2001 4 16 MALA010298 1 20010110 A 7603 TURNBUCKLE BAC 146 AVRO146RJ85A 1500097 EU THROTTLE CABLE OUT OF ADJ A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 524XJ E2349 FOUND DURING C-CHECK, IN ST. JOHNS, NF. NR 3 THROTTLE CABLE TURNBUCKLE FOUND BACKED OFF BEYOND LIMITS (6 THREADS EXPOSED ) REQUIRES ADJUSTMENT AND RETENSIONING. REF: MM 76-11-00 BLOCK 501(FUSELAGE TURNBUCKLES). MAINTENANCE ADJUSTED NR 3 THR UST CONTROL CABLE TURNBUCKLE, AND CIRCUIT TENSIONED TO WITHIN LIMITS AND SAFETIED IAW MM 76-11-00. BLOCK 501. 2 H 7 4 4F RT A49EU 2001041600215 20010416 00215 EU 2001 4 16 MALA010299 1 20010110 A 7603 MS212561 CLIP BAC 146 AVRO146RJ85A 1500097 EU THROTTLE CABLE MISINSTALLED A MALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 15 524XJ E2349 FOUND DURING C-CHECK, BY AIR ALTANTIC, IN ST JOHNS, NF. NR 1, 2, AND 4 THROTTLE CABLE TURNBUCKLES FOUND NOT SAFETIED PRO PERLY IN FUSELAGE. SAFETY CLIPS TO BE INSTALLED. MAINTENANCE SAFETIED RN 1, 2, AND 4 TURNBUCKLES PN MS21256-1 IAW STAND ARD PRCTICES. 2 H 7 4 4F RT A49EU 2001041600216 20010416 00216 EU 2001 4 16 MALA010301 1 20010328 A 3020 PRESSURE SWITCH BAC 146 AVRO146RJ85A 1500097 EU NR 4 ENGINE FAILED A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 524XJ E2349 NR 4 ENGINE INTAKE LOW PRESSURE LIGHT REMAINED ON DURING FLIGHT. ONLY AT FLIGHT IDLE CONDITIONS WOULD IT EXTINGUISH. M AINTENANCE DEFERRED NR 4 ENGINE INTAKE LO PRESS LIGHT PER MEL 30-20-2 (C). MAINTENANCE PROCEDURED COMPLIED WITH. ENTER ED INTO DMR, MXC NOTIFIED 1310, STEP D=388 DEGREES, STEP E 406 DEGREES, STEP J 383 DEGREES, STEP K=402 DEGREES. DISCONNE CTED PRESS SWITCH CONNECTOR PLUG. REPLACED PSI SWITCH. 2 H 7 4 4F RT A49EU 2001041600217 20010416 00217 EU 2001 4 16 MALA010302 1 20010329 A 5610 WINDSHIELD SAAB SF340 SF340A 7850100 EU COCKPIT FAILED A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 102XJ 340A102 WHILE IN CRUISE, 3095, CAPT SIDE OF WINDSHIELD SHATTERED. MAINTENANCE REPLACED CAPT. A SCREEN. OPS CHECK GOOD AT THIS T IME 2 L 7 2 4T RT A52EU 2001041600225 20010416 00225 NM 2001 4 16 ASAA0140017 1 20010202 A 5311 6516300302 FRAME BOEING 737 7374Q8 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 778AS 25110 PAE - DURING SI CHECK, FOUND CRACK 1 INCH LONG AT BS 178 SIDE CHORD AT WL 207, RBL 28 AND LBL 28. (M) 2 L 7 2 4F RT A16WE 2001041600226 20010416 00226 NM 2001 4 16 ASAA0110036 1 20010202 A 5330 6551625505 DOUBLER BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND BEAR STRAP AT STATION 967, STRINGER 24L-26L CRACKED. REPAIRED PER EA 5310-01899. (M) 2 L 7 2 4F A16WE 2001041600227 20010416 00227 NM 2001 4 16 ASAA0110035 1 20010202 A 5312 6520726 BULKHEAD BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND WEB AT STATION 178, RIGHT BUTTOCK LINE 11 CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041600228 20010416 00228 NM 2001 4 16 ASAA0110043 1 20010205 A 5320 655056825 WEB BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND CUSP WEB AT BS 947-986, STRINGER 17L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041600229 20010416 00229 NM 2001 4 16 ASAA0110042 1 20010205 A 5320 656739313 WEB BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND WEB AT BS 967-976, LEFT BUTTOCK LINES 39-46 CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041600230 20010416 00230 NM 2001 4 16 ASAA0110094 1 20010210 A 5311 6546578501 FRAME BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND CHORD AT BS 1138-1156, WATERLINE 260 CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041600231 20010416 00231 NM 2001 4 16 UIEA01006 1 20010308 A 5311 65B01708508 FRAME BOEING 747 747230B 1384889 NM FUSELAGE DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 508MC 85610 21644 UPON REMOVAL OF FRAME SPLICE DOUBLER IAW SB747-53A-2272, FOUND ELONGATED HOLES IN FRAME WEB AT BS 300 RIGHT, JUST ABOVE STRINGER 14R BETWEEN RBL 60 AND RBL 70. TRIMMED OUT EXISTING WEB IN AREA OF ELONGATED HOLES. MANUFACTURED FILLER, REPA IR DOUBLERS AND SPLICES. INSTALLED PER STANDARD PRACTICES. (M) 2 L 7 4 4F A20WE 2001041600232 20010416 00232 NM 2001 4 16 UIEA01010 1 20010308 A 5330 SKIN BOEING 747 747230B 1384889 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 508MC 85610 21644 DURING INSPECTION OF AFT LOWER LOBE CARGO DOOR CUTOUT, A CRACK WAS DISCOVERED AT THE UPPER FORWARD CORNER, STATION 1814 APPROX 1.3 INCH. TRIMMED OUT CRACK, MANUFACTURED FILLER AND EXTERNAL DOUBLER FROM .063 2024T3 ALUMINUM. INSTALLED PER SRM 53-30-03. (M) 2 L 7 4 4F A20WE 2001041600233 20010416 00233 NM 2001 4 16 UIEA01011 1 20010308 A 5311 141U102111 FRAME BOEING 747 747230B 1384889 NM FUSELAGE MISDRILLED A UIEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 15 508MC 85610 21644 DURING INSPECTION OF THE NOSE WHEEL FRAME STATIONS, FOUND NINE HOLES ON FRAME WEB BS 300 L/S SHORT EDGE DISTANCE. TRIMM ED AWAY AFFECTED AREA. MANUFACTURED FILLERS, REPAIR STRAPS AND DOUBLERS. INSTALLED PER SRM 53-10-04. (M) 2 L 7 4 4F A20WE 2001041600234 20010416 00234 NM 2001 4 16 UIEA01009 1 20010308 A 5311 65B01712519 FRAME BOEING 747 747230B 1384889 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 508MC 85610 21644 DURING ACCOMPLISHMENT OF SB 747-53-2272 FOUND ONE CRACKED HOLE BS 380 R/S AT STRINGER 14R. STOP DRILLED CRACK, INSTALLE D REPAIR DOUBLER PER STANDARD PRACTICES IN A NON-MANDATORY ZONE. AMOC APPROVED PER PAR 9 OF AD 91-11-01. (M) 2 L 7 4 4F A20WE 2001041600235 20010416 00235 WP 2001 4 16 ASAA0180097 1 20010307 A 3397 0105606003 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A K NONE O OTHER CR CRUISE 1 NM 01 975AS 53451 SEA - DURING CRUISE, TRACK LIGHTING CAME ON FOR A MOMENT. A CHECK OF THE EMERGENCY FLOOR TRACK LIGHTS FOUND THE LIGHTS AT ROWS 22 TO 24 INOPERATIVE. REPAIRED BROKEN WIRES. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001041600237 20010416 00237 NM 2001 4 16 ASAA0110041 1 20010205 A 5320 65596585 INTERCOSTAL BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL AT BS 967-986, LEFT BUTTOCK LINE 46 CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041600238 20010416 00238 NM 2001 4 16 ASAA0110077 1 20010209 A 5751 654645519 SKIN BOEING 737 737290C 138448V NM AILERON CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND LEADING EDGE OF LEFT AILERON CRACKED. REPAIRED PER EA. (M) 2 L 7 2 4F A16WE 2001041600239 20010416 00239 NM 2001 4 16 ASAA0110076 1 20010209 A 5330 6545778501 SKIN BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND SKIN PANEL AT BS 967, STRINGER 18R CRACKED. REPAIRED PER EA. (M) 2 L 7 2 4F A16WE 2001041600240 20010416 00240 NM 2001 4 16 ASAA0110075 1 20010209 A 5320 66232564 SPLICE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND FRAME SPLICE AT BS 947, STRINGER 25R CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041600241 20010416 00241 NM 2001 4 16 ASAA0110074 1 20010209 A 5310 6546563 SHEAR TIE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 907, STRINGER 27L-27R CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041600242 20010416 00242 NM 2001 4 16 ASAA0110073 1 20010209 A 5320 6545833212 FLOOR SUPPORT BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT ANGLE AT BS 269, LEFT BUTTOCK LINE 12 TO RIGHT BUTTOCK LINE 12 CORRO DED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041600243 20010416 00243 NM 2001 4 16 ASAA0110072 1 20010209 A 5320 6545833149 INTERCOSTAL BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL AT BS 269, LEFT BUTTOCK LINE 10 TO RIGHT BUTTOCK LINE 10 CORRODED. RE PAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041600244 20010416 00244 NM 2001 4 16 ASAA0110071 1 20010208 A 5320 6554906 BEAM BOEING 737 737290C 138448V NM FUSELAGE BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND CARGO BEAM AT BS 491-520, STRINGER 27R BROKEN OUT. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041600245 20010416 00245 NM 2001 4 16 ASAA0110070 1 20010208 A 5320 6016907 BEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND BEAM AT BS 727, LEFT BUTTOCK LINE 26 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041600246 20010416 00246 NM 2001 4 16 ASAA0110069 1 20010208 A 5311 6546550 FRAME BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 987, STRINGER 24L-24R CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041600247 20010416 00247 EA 2001 4 16 ASAA0110068 1 20010208 A 5320 65636052 INTERCOSTAL ACQCOR F22 F22 8850908 EA FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL AT BS 967-986, LEFT BUTTOCK LINE 39 CORRODED. REPAIRED PER SRM. (M) 1 H 7 1 3O NC 1A9 2001041600248 20010416 00248 NM 2001 4 16 ASAA0110067 1 20010208 A 5320 65673938 ANGLE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND ANGLE ON INTERCOSTAL AT BS 967-986, LEFT BUTTOCK LINE 39 CORRODED. REPAIRED PER S RM. (M) 2 L 7 2 4F A16WE 2001041600249 20010416 00249 NM 2001 4 16 ASAA0110063 1 20010207 A 5347 BAC15201433 SEAT TRACK BOEING 737 737290C 138448V NM CABIN CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND SEAT TRACK AT BS 887-907, BUTTOCK LINE 0 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041600250 20010416 00250 NM 2001 4 16 ASAA0110064 1 20010207 A 5320 693535214 CLIP BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND SHEAR CLIP AT BS 807, STRINGER 7R CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041600251 20010416 00251 NM 2001 4 16 ASAA0110065 1 20010207 A 5312 65C28106 BULKHEAD BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND AFT PRESSURE BULKHEAD AT BS 1016-1030, STRINGER 27L-27R CORRODED. REPAIRED PER EA . (M) 2 L 7 2 4F A16WE 2001041600252 20010416 00252 2001 4 16 MALA010303 4 20010324 A 2210 4068300904 COMPUTER BAC 146 AVRO146RJ85A 1500097 EU AUTOPILOT DEFECTIVE A MALA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 GL 15 514XJ E2330 DURING CLIMBOUT ON FLIGHT 3638 FROM MEM, LOST FD''S, YAW DAMPER INOP, WINDSHEAR INOP LIGHT ILLUMINATED APPROXIMATELY THR EE MINUTES LATER, LIGHTS WENT OUT. AP WAS THEN ENGAGED. CLIMBING THRU APPROXIMATELY 16,000 FT. AP DISENGAGED, AND YD I NOP, AND WINDSHEAR INOP CAME BACK ON. AIR RETURN TO MEM. MAINTENANCE REPLACED FGC IAW AMM 22-10-11 201. PN 4068300-904 SN/ON 98100337, AND SN/OFF 97070289. PERFORMED RTS TEST PASSED. NO OTHER DEFECTS NOTED. AP ENGAGES NORMALLY. 2 H 7 4 4F RT A49EU 2001041600253 20010416 00253 EU 2001 4 16 MALA010304 1 20010223 A 5330 SHIELD SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426XJ 426 FOUND DURING C-CHECK, NASHVILLE, TN. A GROUP OF DENTS AFT OF RT ICE SHIELD AT STA 345.0. REFER TO CELSIUS W/O 19430, TA SK 2523, AND SAAB STATEMENT 340 SDS001131. 2 L 7 2 4T RT A52EU 2001041600254 20010416 00254 EU 2001 4 16 MALA010305 1 20010226 A 5320 CHANNEL SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426XJ 426 FOUND DURING C-CHECK, NASHVILLE, TN. THREE U CHANNELS ARE CORRODED THAT TIE FLOORBOARDS 122DZ AND 122EZ TO FLOORBOARD 12 1AZ. REFER TO W/O 19430, TASK 1543. CORROSION DAMAGE OUT OF LIMITS, REF 51-10-10 ON ALL THREE U CHANNELS. FABED 3 NEW U CHANNELS FROM 2024T3-063. PER SAMPLE TREATED, PRIMED AND TOPCOATED. 2 L 7 2 4T RT A52EU 2001041600255 20010416 00255 EU 2001 4 16 MALA010306 1 20010226 A 5321 FLOORBOARD SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426XJ 426 FOUND DURING C-CHECK FROM, IN NASHVILLE, TN. FLOORBOARD FLANGE AT STA 231.0 HAS CORROSION. REFER TO W/O 19430, TASK 254 3. MAINTENANCE BLENDED OUT CORROSION IAW SRM 51-70-40. REMAINING MATERIAL OUT OF LIMITS, REMOVED SEVERAL CORRODED RIVET S, ALODINED BARE METAL, FABRICATED REPAIR ANGLE FROM 2024T3, ALODINED, PRIMED AND TOPCOATEDREPAIR AND FLANGE, INSTALLED NEW RIVETS AND REPAIR ANGLE. 2 L 7 2 4T RT A52EU 2001041600256 20010416 00256 EU 2001 4 16 MALA010307 1 20010228 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426XJ 426 FOUND DURING C-CHECK, NASHVILLE, TN. DENT ABOVE CAPT PITOT TUBE. MAINTENANCE REPAIRED DAMAGE ABOVE CAPT PITOT TUBE (UPPE R) FOR TOUCH UP PAINT 2 L 7 2 4T RT A52EU 2001041600257 20010416 00257 EU 2001 4 16 MALA010308 1 20010301 A 5753 SKIN SAAB SF340 340B 7860101 EU TE FLAP CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426XJ 426 FOUND DURING C-CHECK, IN NASHVILLE, TN. RT FLAP UPPER SURFACE PANEL 641AT IS CHAFED AFT OF THE FORWARD IB EXHAUST COWLIN G CHAFE STRIP. MAINTENANCE SMOOTHED OUT, CHECKED LIMIT.REMAINING MATERIAL IS WITHIN LIMITS OF S/B340-57-012, ALODINED, PRIMED, REPAIRED CHAFED AREA. 2 L 7 2 4T RT A52EU 2001041600258 20010416 00258 EU 2001 4 16 MALA010309 1 20010301 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426XJ 426 FOUND DURING C-CHECK, IN NASHVILLE, TN. GALLEY SEAT TRACK HAS SEVERAL AREAS OF CORROSION. SEAT TRACK AND PROFILE CORRODE D BEYOND LIMITS. LOCATED AND DRILLED NDW SEAT TRACK, ALODINED, PRIMED AND TOPCOATED, INSTALLED SEAT TRACK AND PROFILE I AW SRM 51-40-21,22 AND 27. 2 L 7 2 4T RT A52EU 2001041600259 20010416 00259 EU 2001 4 16 MALA010310 1 20010301 A 5321 FLOORBOARD SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426XJ 426 FOUND DURING C-CHECK, IN NASHVILLE,TN. FLOORBOARD FLANGE AT FS 272 FOR FLOOR PANEL 122CZ HAS CORROSION. MAINTENANCE BLE NDED OUT CORROSION, NEGLIGIBLE MATERIAL REMOVED. MATERIAL REMAINT WITHIN LIMITS, ALODINED BARE METAL, PRIMED AND PAINTE D AREA IAW SRM 51-20-43. 2 L 7 2 4T RT A52EU 2001041600260 20010416 00260 EU 2001 4 16 MALA010311 1 20010301 A 5320 FLOOR PANEL SAAB SF340 340B 7860101 EU FUSLEAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426XJ 426 FOUND DURING C-CHECK, NASHVILLE, TN. FOUND FLOOR PANEL FLANGE 122CZ BETWEEN FS STA 272.0 AND 288.0 HAS CORROSION. MAINT ENANCE BLENDED OUT CORROSION, MATERIAL REMOVED IS OUT OF LIMITS, REMOVED DAMAGED FLANGE, FABRICATED NEW FLANGE ANGLE FRO M 2024T .040 AS PER SAMPLE, ALODINED, PRIMED AND TOPCOATED. 2 L 7 2 4T RT A52EU 2001041600261 20010416 00261 EU 2001 4 16 MALA010312 1 20010301 A 5320 WEB SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426XJ 426 FOUND DURING C-CHECK, IN NASHVILLE, TN. SEVERAL AREAS OF CORROSION ON WEB STA 288.TO STA 294. MAINTENANCE BLENDED OUT CORROSION, WEB CORRODED BEYOND LIMITS. REMOVED DAMAGED WEB, LOCATED, DRILLED AND COUNTERSUNK HOLES IN NEW WEB, ALODINED AND PRIMED HOLES, INSTALLED NEW WEB IAW SRM 51-40-21. 2 L 7 2 4T RT A52EU 2001041600262 20010416 00262 EU 2001 4 16 MALA010313 1 20010301 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426XJ 426 FOUND DURING C-CHECK, IN NASHVILLE TN. CORROSION ON RT FLOOR SUPPORT FLANGE AT RBL 33, FS 595, MAINTENANCE REMOVED CORRO SION , TREATED W ALODINE 1200. MATERIAL REMAINING WITHIN ALLOWABLE LIMITS. ALODINED, PRIMED AND PAINTED FLANGES. 2 L 7 2 4T RT A52EU 2001041600263 20010416 00263 EU 2001 4 16 MALA010314 1 20010301 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426XJ 426 FOUND DURING C-CHECK, IN NASHVILLE, TN. CORROSION ON RT FLOOR SUPPORT FLANGE, AT RBL 33 FROM FS 500 THRU STA 535. MAINT ENANCE REMOVED CORROSION, TREATED W/ ALODINE 1200, MATERIAL REMAINING WITHIN ALLOWABLE LIMITS. ALODINE, PRIMED AND PAINT ED FLANGES. 2 L 7 2 4T RT A52EU 2001041600264 20010416 00264 EU 2001 4 16 MALA010315 1 20010301 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426XJ 426 FOUND DURING C-CHECK, IN NASHVILLE, TN. LT FLANGE CORRODED ON SEAT TRACK AT BL.0 FROM FUSELAGE STA 294 TO STA 500. MAINT ENANCE REMOVED CORROSION, TREATED WITH AOLDINE 1200, MATERIAL REMAINING WITHIN ALLOWABLE LIMITS. ALODINED, PRIMED AND PA INTED APPLIED AV100 TO SEAT TRACKS. 2 L 7 2 4T RT A52EU 2001041600265 20010416 00265 EU 2001 4 16 MALA010316 1 20010301 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426XJ 426 FOUND DURING C-CHECK, IN NASHVILLE, TN. CORROSION ON FLOOR SUPPORT AT LBL 33, FS 512. MAINTENANCE REMOVED CORROSION, TR EATED WITH ALODINE 1200. REMAINING MATERIALS WITHIN ALLOWABLE LIMITS. ALODINED, PRIMED AND PAINTED. 2 L 7 2 4T RT A52EU 2001041600266 20010416 00266 EU 2001 4 16 MALA010317 1 20010301 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426XJ 426 FOUND DURING C-CHECK, IN NASHVILLE, TN. IB FLANGE CORRODED ON SEAT TRACK AT LBL 18.3 FROM FUSELAGE STA 294-560. MAINTENA NCE REMOVED CORROSION, TRATED WITH ALODINE 1200, MATERIAL REMAINING OUT OF ALLOWABLE LIMITS REF SRM 53-70-60, 51-10-10. PRIMED, PAINTED SEAT TRACKS APPLIED AV100 ON FLANGES. 2 L 7 2 4T RT A52EU 2001041600267 20010416 00267 EU 2001 4 16 MALA010318 1 20010302 A 5330 SHIELD SAAB SF340 340B 7860101 EU FUSELAGE DELAMINATED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426XJ 426 FOUND DURING C-CHECK, IN NASHVILLE, TN RT ICE SHIELD 3RD FROM BOTTOM DELAMINATED AT UPPER EDGE AND HAS 2 GROUPS OF DENT S. MAINTENANCE REMOVED RH ICE SHIELD, NDT PER FFVNDT006EC AND 004UT. NO CRACKS NO DELAMINATION IN OR AROUND DENTS. DENTS ON FUSELAGE SKIN BENEATH 3RD ICE GUARD OUT OF LIMITS. INSTALLED ICE SHIELD. 2 L 7 2 4T RT A52EU 2001041600268 20010416 00268 EU 2001 4 16 MALA010319 1 20010302 A 5410 DUCT SAAB SF340 340B 7860101 EU LT NACELLE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426XJ 426 FOUND DURING C-CHECK, IN NASHVILLE, TN. LT ENGINE COWL DUCT IS CRACKED. MAINTENANCE STOP DRILLED CRACK, FABRICATED DOUB LER. NO CRACKS NOTED IAW FFVNDT006. INSTALLED REPAIR DOUBLER IAW SAAB STATEMENT 340SDS001131. 2 L 7 2 4T RT A52EU 2001041600269 20010416 00269 EU 2001 4 16 MALA010320 1 20010302 A 5410 HINGE SAAB SF340 340B 7860101 EU NACELLE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426XJ 426 FOUND DURING C-CHECK, IN NASHVILLE, TN. LT ENGINE HINGE COWL 453BR NACA DUCT IS CRACKED. MAINTENANCE STOPPED DRILLED CR ACK, FABRICATED DOUBLER REF EO340SDS001131. NO CRACKS NOTED IAW FFVNDT006, INSTALLED REPAIR DOUBLER. 2 L 7 2 4T RT A52EU 2001041600270 20010416 00270 EU 2001 4 16 MALA010321 1 20010305 A 3230 SCISSORS SAAB SF340 340B 7860101 EU LT MLG CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426XJ 426 FOUND DURING C-CHECK, LT MLG LEG HAS CORROSION IN THE UPPER SCISSOR LINK BORE, SEE IPM-12 FOR WORK ACCOMPLISHED ON LT ML G. PERFORMED EXTENSION AND RETRACTION CHECK. 2 L 7 2 4T RT A52EU 2001041600271 20010416 00271 EU 2001 4 16 MALA010322 1 20010305 A 3230 SCISSORS SAAB SF340 340B 7860101 EU RT MLG CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426XJ 426 FOUND DURING C-CHECK , IN NASHVILLE TN. RT MLG LEG HAS CORROSION AT UPPER SCISSOR LINES BORE. MAINTENANCE REMOVED RH ML G LEG, INSTALLED RH MLG LEG. INSTALLED RH MLG ASSY. PERFORMED EXTENSION AND RETRACTION CHECK GOOD. 2 L 7 2 4T RT A52EU 2001041600272 20010416 00272 NM 2001 4 16 ASAA0110062 1 20010207 A 5347 BAC15201433 SEAT TRACK BOEING 737 737290C 138448V NM CABIN CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND SEAT TRACK AT BS 540-649, RIGHT BUTTOCK LINE 45.5 CORRODED. REPAIRED PER SRM. (M ) 2 L 7 2 4F A16WE 2001041600273 20010416 00273 NM 2001 4 16 ASAA0110061 1 20010207 A 5320 69387871 ATTACH FITTING BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND ATTACH FITTING AT BS 727, STRINGER 27L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041600274 20010416 00274 NM 2001 4 16 ASAA0110060 1 20010207 A 5320 6567393 ANGLE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND ANGLE AT BS 986, LEFT BUTTOCK LINE 39 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041600275 20010416 00275 NM 2001 4 16 ASAA0110059 1 20010207 A 5320 6553844 FITTING BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND TIE DOWN AT BS 915-947, STRINGER 27L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041600276 20010416 00276 NM 2001 4 16 ASAA0110058 1 20010207 A 5330 6545775 SKIN BOEING 737 737290C 138448V NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND SKIN PANEL AT BS 867, STRINGER 21R DENTED BEYOND SRM LIMITS. REPAIRED PER SRM. ( M) 2 L 7 2 4F A16WE 2001041600277 20010416 00277 NM 2001 4 16 ASAA0110057 1 20010207 A 5313 BAC1498158 STRINGER BOEING 737 737290C 138448V NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND A STRINGER AT BS 937-977, STRINGER 27L. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041600278 20010416 00278 NM 2001 4 16 ASAA0110056 1 20010207 A 5311 6546550 FRAME BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 480, STRINGER 21L-22L CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041600279 20010416 00279 NM 2001 4 16 ASAA0110055 1 20010207 A 5320 BAC1493577 INTERCOSTAL BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL STRAP AT BS 312-352, RIGHT BUTTOCK LINE 24 CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041600280 20010416 00280 NM 2001 4 16 ASAA0110054 1 20010207 A 5320 654961915 INTERCOSTAL BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL AT BS 791, STRINGER 25L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041600281 20010416 00281 NM 2001 4 16 ASAA0110053 1 20010207 A 5330 6545775 SKIN BOEING 737 737290C 138448V NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND SKIN PANEL AT BS 197-203, STRINGER 26R-27R DENTED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041600282 20010416 00282 NM 2001 4 16 ASAA0110051 1 20010207 A 5320 651630019 ANGLE BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND L-ANGLE BRACKET AT BS 178, STRINGER 25L CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041600283 20010416 00283 NM 2001 4 16 ASAA0170001 1 20010304 A 3397 8100022608 WIRE BOEING 737 737790 13844CN NM CABIN DISCONNECTED A K NONE L NO TEST IN INSP/MAINT 1 NM 01 609AS 29752 SEA - DURING LINE MAINTENANCE, EMERGENCY TRACK LIGHTING COVER WAS FOUND MISSING AND WIRING WAS DISCONNECTED. REPLACED C OVER AND WIRING. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 2001041600286 20010416 00286 NM 2001 4 16 2001UALA00216 1 20010307 A 2120 7321161002 MODULE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE PRESSURIZATION LEAKING A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 797UA 26924 CREW VERBAL ON AIRCRAFT DESCENT AT 7K, ODOR IN THE FORWARD CABIN FLT DESK. CREW SAID IT SMELLS LIKE HOT OIL SMELL OR O ZONE CONVERTER. SUPPLEMENTAL DATA UPDATE THE PROBLEM WAS DUE TO FAULTY RH HYDRAULIC PNEUMATIC PRESSURIZATION MODULE. TH E PNEUMATIC DUCTING WAS CONTAMINATED BECAUSE THIS UNIT WAS ALLOWING A SMALL AMOUNT OF HYDRAULIC FLUID PASS THROUGH THE C HECK VALVE. THE MODULE WAS REPLACED, AND A VERY THOROUGH PNEUMATIC DUCTING AND PACK BURNOUT WAS ACCOMPLISHED. AIRCRAFT WAS RETURNED TO SERVICE WITHOUT FURTHER ODOR COMPLAINTS.THE ABOVE IS ALSO THE RESPONSE TO MRR NUMBER 2001UALA00163. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001042400195 20010424 00195 NM 2001 4 24 2001UALA00312 1 20010323 A 2840 INDICATOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 FUEL FLOW MALFUNCTIONED A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 7447U 21901 NR 3 FUEL FLOW INDICATOR ERRATIC FOLLOWED BY 28 VOLT DC CB POPPED THR0UGH 500 FEET . ELECTRICAL ODOR SMELL IN COCKPIT. FUEL FLOW WILL OPERATE OKAY BUT FUEL FLOW TRANSMITTER WILL REQUIRE REMOVAL FOR REPAIR DUE TO CHAFED WIRE BEHIND TRANSMI TTER. SUPPLEMENTAL DATA UPDATE FOUND CHAFED WIRES. SPLICED NEW WIRES IN PLACE OF CHAFED WIRES PER GN/MM2-0-15-1. SYSTE M CHECKED NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001043000004 20010430 00004 NM 2001 4 30 2001UALA00313 1 20010324 A 2421 10610661110612 CSD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 1 FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 349UA 24253 LOSS OF THE NR 1 GENERATOR. SUPPLEMENTAL DATA UPDATE THE NR 1 CSD (G6) (MR24117-2143) AND GENERATOR (G1) (MR24216-14611) UNITS WERE REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600287 20010416 00287 NM 2001 4 16 2001UALA00314 1 20010325 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 AFT PIT STA 887 RBL 42 FRAME HAS EXCESSIVE MATERIAL REMOVED. INSTALLED REPAIR STRAP. MAJOR REPAIR ACCOMPLISHED 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600288 20010416 00288 NM 2001 4 16 2001UALA00315 1 20010326 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 FORWARD CABIN FLOORBEAM UPPER CHORD STA 294.5 HAS EXCESSIVE MATERIAL LOSS. SPLICED IN NEW SECTION OF UPPER T-CHORD. MA JOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600289 20010416 00289 NM 2001 4 16 2001UALA00316 1 20010325 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 CABIN STA 1016 LBL 17 TO LBL 37 HAS CORROSION ON FLOOR BEAM. MANUFACTURED AND INSTALLED REPAIR PARTS. MAJOR REPAIR ACC OMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600290 20010416 00290 NM 2001 4 16 2001UALA00317 1 20010324 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 310UA 23671 STA 180 WL 207 FLOOR INTERCOSTAL CRACKED. REPAIRED FLOOR INTERCOSTAL. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001043000005 20010430 00005 NM 2001 4 30 2001UALA00318 1 20010326 A 2121 36169596 COOLING FAN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAILED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 560UA 2683 0 26660 SMOKE IN CABIN. SUPPLEMENTAL DATA UPDATE FOUND COOLING FAN SHAFT SHEARED AND FAN HOUSING BROKEN. THIS IS THE LATEST CON FIGURATION (-6) WHICH WAS INSTALLED ON THIS APU ON JUNE 11, 1999. THIS HAS BEEN A LONG TIME PROBLEM, AND HONEYWELL IS W ORKING ON FIXING THESE COOLING FAN FAILURES RESULTING IN APU REMOVALS. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600291 20010416 00291 NM 2001 4 16 2001UALA00319 1 20010326 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 STA 1640 STR 5L FRAME FLANGE WORN. MAJOR REPAIR ACCOMPLISHED.REPAIRED FRAME FLANGE PER AMM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600292 20010416 00292 NM 2001 4 16 2001UALA00320 1 20010326 A 5270 PROXIMITY SENSOR BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CARGO DOOR BLOCKED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 946UA 26687 ABORTED TAKE-OFF DUE TO A DOOR WARNING INDICATION. FOUND AFT CARGO DOOR BUNGEE CORD INTERFERING WITH THE DOOR PROX SENS OR. REROUTED THE BUNGEE AND OPERATION RETURNED TO NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600293 20010416 00293 NM 2001 4 16 2001UALA00321 1 20010326 A 5320 FLOOR SUPPORT BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 995UA 22399 FLOOR SUPPORT HAS CORROSION AROUND FASTENER HOLES AT RBL 20 AND BETWEEN STA 967 AND STA 986. REMOVED CORRODED FLOOR SUP PORT. FABRICATED, ALODINED, PRIMED, AND INSTALLED NEW FLOOR SUPPORT. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F A16WE E2EA 2001041600294 20010416 00294 NM 2001 4 16 2001UALA00322 1 20010327 A 5320 CHANNEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 CABIN SEAT TRACK LINK SUPPORT CHANNEL AT STA 520 RBL 24.75 IS CRACKED AT THE UPPER OUTBOARD FASTENER HOLE. REPAIRED THE LINK SUPPORT. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001042400196 20010424 00196 NM 2001 4 24 2001UALA00323 1 20010323 A 3510 80048004 REGULATOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE OXYGEN SYSTEM FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7455U 21909 AT DEPARTURE TIME CREW LOST ALL OXYGEN PRESSURE TO ALL MASKS IN THE FLIGHT DECK. SUPPLEMENTAL DATA UPDATE FOUND THAT PRE SSURE REDUCING REGULATOR WAS NOT LETTING AIR OUT OF PRESSURE REGULATOR VALVE. REPLACED CREW OXYGEN PRESSURE REDUCING R EGULATOR PER MAINTENANCE MANUAL. OPERATIONAL CHECK OK. 2 L 7 3 4F 4 F A3WE E2EA 2001070300074 20010703 00074 NM 2001 7 3 2001UALA00324 1 20010325 A 2421 UALMR24121 IDG BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE LT ENGINE FAILED A UALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION NR NOT REPORTED 1 WP 29 219UA 30551 ACFT RTB FOR NR 2 GEN INOP. *S/D* ELEC GEN OFF LT EICAS WAS DISPLAYED W/ASSOC MAINT MSGS 24-31591 & 24-31631. IDG FILT ER INDICATOR WAS FOUND POPPED. LT IDG WAS REPLACED TO CORRECT THE PROBLEM. THE PRELIMINARY FINDING REPORT OF THE IDG INDICATED A FAILURE IN THE ROTOR ANTIDRIVE BEARING. THE ROTOR SLEEVE RUBBED ON THE STATOR CAUSING DEBRIS TO CIRCULATE T HROUGHOUT THE IDG. THE DEBRIS PLUGGED THE CHARGE AND SCAVENGE FILTERS. THE DEBRIS FILLED OIL CIRCULATED THROUGHOUT THE INTERNAL COMPONENTS CAUSING THE PLANETARY GEARS TO SEIZE. THE HEAT GENERATED WITHIN THE UNIT CAUSING IDG THERMALLY TO DISCONNECT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001050300316 20010503 00316 NM 2001 5 3 2001UALA00325 1 20010325 A 7810 241050 EXHAUST PIPE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7459U 21913 656004 NR 1 ENGINE TAILPIPE CRACKED AT THE 11 OCLOCK POSITION. SUPPLEMENTAL DATA UPDATE CAUSE OF CRACKING UNDER INVESTIGATION. THE CRACKS WERE REPAIRED PER MM 78-34-05. 2 L 7 3 4F 4 F A3WE E2EA 2001041600295 20010416 00295 NM 2001 4 16 2001UALA00326 1 20010322 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 AFT PIT BS 1351 STRINGERS 38L - 39L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE REF: BAC140T2101 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001070300075 20010703 00075 NE 2001 7 3 2001UALA00327 2 20010322 A 7530 7765555 CONTROL VALVE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE NR 2 ENGINE OUT OF RIG A UALA A UNSCHED LANDING R M A PARTIAL RPM/PWR LOSS OVER TEMP FLAME/FIRE CL CLIMB 1 WP 29 603UA 21864 707543 COMPRESSOR STALL NR 2 ENG ON T/O. MAX EGT 815 DEG C. FLAMES OBSERVED BY TOWER PERSONNEL. REDUCED TO IDLE POWER, RTF. * S/D* ENGINE WAS REPLACED DUE TO OVERTEMP. DURING ENGINE PRE-REPAIR RUN, FOUND ENGINE VANE BLEED CONTROL (EVBC) WAS OUT OF TRIM. EVBC WILL BE OVERHAULED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041600296 20010416 00296 NM 2001 4 16 2001UALA00329 1 20010322 A 5320 ANGLE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 AFT PIT BS 1087 STRINGER 39L FORWARD OF BULKHEAD ANGLE GOUGED. MAJOR REPAIR ACCOMPLISHED REPLACED ANGLE REF: BAC146T107 4 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041600297 20010416 00297 NM 2001 4 16 2001UALA00330 1 20010327 A 5241 STOP FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 310UA 23671 FORWARD GALLEY DOOR AFT STOP FITTING FRAME IS CRACKED. REPAIRED FORWARD GALLEY DOOR AFT STOP FITTING FRAME. MAJOR REPA IR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600298 20010416 00298 NM 2001 4 16 2001UALA00331 1 20010327 A 5312 PRESSURE PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE MLG WW CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 310UA 23671 CABIN STA 664 AT LBL 30 WHEEL WELL PRESSURE DECK IS CRACKED. REPAIRED CRACKED PRESSURE DECK. MAJOR REPAIR ACCOMPLISHED . 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600299 20010416 00299 NM 2001 4 16 2001UALA00332 1 20010322 A 5320 STIFFENER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 CABIN FLOOR BEAM BS 246, RBL 66 VERTICAL STIFFINER CRACKED. MAJOR REPAIR ACCOMPLISHED REPLACED STIFFINER REF: BAC141T58 14. 2 L 7 2 4F 4 F RT A1NM E3NE 2001070300076 20010703 00076 NM 2001 7 3 2001UALA00333 1 20010327 A 2131 MOTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN PRESSURE FAILED A UALA O OTHER G MULTIPLE FAILURE CR CRUISE 1 WP 29 659UA 27114 BOTH PRESSURE CONTROLLERS FAILED. DESCENDED TO FL180. OPERATED NORMALLY IN MAN MODE. *S/D* 3/27/01 AT LHR, AUTO PRES S SYSTEM NR 2 WAS DEFERRED INOP. ACFT FLEW TO ORD WITH NO PRESSURIZATION FAULTS. DURING ORD-IAD LEG, FLIGHT CREW REPOR TED FAILURE OF BOTH AUTO CABIN PRESSURE CONTROLLERS. REPLACED NR 2 AC MOTOR. 3/29/01: DF534 WAS CREATED FOR AUTO PRESS SYSTEM NR 2. BITE ON BOTH NR 1 & 2 CPC SHOWED NR 2 AC MOTOR FAULT. 4/5/01: REPLACED NR 2 AC MOTOR (MR21324-142 OFF, -80 ON). ENGINEERING CALLOUT (EG3456) ACCOMPLISHED ON 4/18/01, PERFORMED WIRE CHECKS BETWEEN AC MOTORS AND CABIN PRESS CONTROLLERS. NO DISCREPANCIES WERE FOUND. 2 L 7 2 4F 4 F RT A1NM E24NE 2001041600300 20010416 00300 NM 2001 4 16 2001UALA00334 1 20010322 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 AFT PIT BS 1329 STRINGERS 36L - 37L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED REPLACED SHEAR TIE REF: BAC140T2102 A ND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041600301 20010416 00301 NM 2001 4 16 2001UALA00335 1 20010327 A 5340 FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE DOOR FRAME CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 310UA 23671 FORWARD GALLEY DOOR FRAME AT THE FOURTH FITTING FROM THE BOTTOM ON THE AFT SIDE IS CRACKED. REPAIRED THE FORWARD GALLEY DOOR FRAME. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600302 20010416 00302 NM 2001 4 16 2001UALA00336 1 20010327 A 5743 ATTACH FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE MLG BEAM DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 309UA 23670 EXCESSIVE MATERIAL REMOVED DURING BLEND OUT ON RT MAIN LANDING GEAR SUPPORT BEAM ATTACH FITTING. REPLACED THE RT MAIN L ANDING GEAR SUPPORT BEAM ATTACH FITTING. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600303 20010416 00303 NM 2001 4 16 2001UALA00337 1 20010327 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 309UA 23670 CABIN FLOORBEAM STA 947 HAS EXCESSIVE MATERIAL REMOVED. REPAIRED CABIN FLOORBEAM. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600304 20010416 00304 NM 2001 4 16 2001UALA00338 1 20010322 A 5320 STIFFENER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FLOORBEAM CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 CABIN FLOORBEAM BS 246 LBL 27 VERTICAL STIFFENER CRACKED. MAJOR REPAIR ACCOMPLISHED REPLACED STIFFENER REF: BAC141T5814 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041600306 20010416 00306 NM 2001 4 16 2001UALA00340 1 20010322 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 AFT PIT BS 1329 STRINGERS 39L - 39R SHEARTIE CORRODED. MAJOR REPAIR ACCOMPLISHED REPLACED SHEARTIE REF: BAC146T1212 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041600307 20010416 00307 NM 2001 4 16 2001UALA00341 1 20010322 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 AFT PIT BS 1329 STRINGERS 37L - 38L SHEARTIE CORRODED. MAJOR REPAIR ACCOMPLISHED REPLACED SHEARTIE REF: BAC140T2102 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041600308 20010416 00308 NM 2001 4 16 2001UALA00342 1 20010322 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 CABIN TRANSVERSE FLOORBEAM CORRODED BS 824 LBL 11. MAJOR REPAIR ACCOMPLISHED INSTALLED FLOORBEAM REPAIR REF: SRM 53-00 -51. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041600309 20010416 00309 NM 2001 4 16 2001UALA00343 1 20010322 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 AFT PIT SHEAR TIE AT BS 1351 STRINGER 38L CORRODED. MAJOR REPAIR ACCOMPLISHED FABRICATED AND INSTALLED SHEAR TIE IN ACC ORDANCE WITH SRM 51-20-02 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041600310 20010416 00310 NM 2001 4 16 2001UALA00344 1 20010324 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 FORWARD PIT BS 368 RBL 35 FLOORBEAM T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED INSTALLED T-CAP REPAIR REF: SRM 53-30-07 FIGURE 201. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041600311 20010416 00311 NM 2001 4 16 2001UALA00345 1 20010324 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 FORWARD PIT BS 742 STRINGERS 37L - 38L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED REPLACED SHEAR TIE REF: BAC143T121 4 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041600312 20010416 00312 EU 2001 4 16 2001UALA00346 1 20010328 A 2131 CONTROLLER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN PRESSURE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 414UA 472 CABIN PRESSURIZATION PROBLEM. SUPPLEMENTAL DATA UPDATE FOUND RED CAPS INSTALLED ON STATIC PORTS ON BOTH PRESSURE CONTROL LERS. REMOVED CAPS, AND PERFORMED OPERATIONAL TEST OF THE PRESSURE CONTROL AND MONITORING SYSTEM. TESTED GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2001041600313 20010416 00313 NM 2001 4 16 2001UALA00349 1 20010328 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 AFT CARGO PIT AT BS 1241 BETWEEN STRINGERS 39L AND 39R, SHEAR TIE IS CORRODED. MAJOR REPAIR ACCOMPLISHEDREPLACED SHEAR TIE PER SRM 51-40-02 AND BAC DWG 140T2102. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041600314 20010416 00314 NM 2001 4 16 2001UALA00350 1 20010328 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 AFT CARGO PIT AT BS 1263 BETWEEN STRINGERS 39L AND 39R, SHEAR TIE IS CORRODED. MAJOR REPAIR ACCOMPLISHEDREPLACED SHEAR TIE PER SRM 51-40-02 AND BAC DWG 140T1209. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041600315 20010416 00315 NM 2001 4 16 2001UALA00351 1 20010328 A 5320 SPLICE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 FORWARD CARGO PIT AT BS 434, STRINGER 38L SPLICE FITTING IS CORRODED. MAJOR REPAIR ACCOMPLISHED REPLACED SPLICE AT STRI NGER 38L PER SRM 51-40-02 AND BAC DWG 140T0115. 2 L 7 2 4F 4 F RT A1NM E3NE 2001050300317 20010503 00317 NM 2001 5 3 2001UALA00352 1 20010328 A 5320 DOUBLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE VHF ANTENNA MISDRILLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 506UA 24627 3 EACH FIELD FASTENERS ON LWR VHF ANTENNA DOUBLER HAVE NO EDGE DISTANCE TO FWD END OF CUTOUT. STA 1466 RBL 3.23. SUPPLEM ENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.THE CUTOUT EXTENDED FORWARD TO REMOVE SHORT ED HOLES. THE REPAIR TRIPLER AN D DOUBLER WERE EXTENDED TO MEET THE REQUIREMENT FOR THE APPROPRIATE NUMBER OF FASTENERS AROUND THE CUTOUT AREA. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600316 20010416 00316 NM 2001 4 16 2001UALA00353 1 20010328 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 AFT CARGO PIT AT BS 1329 BETWEEN STRINGERS 38L AND 39L, SHEAR TIE IS CORRODED. MAJOR REPAIR ACCOMPLISHEDREPLACED SHEAR TIE PER SRM 51-40-02 AND BAC DWG 140T2102. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041600317 20010416 00317 NM 2001 4 16 2001UALA00354 1 20010328 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 AFT CARGO PIT AT BS 1065 TO 1087, STRINGER 30R IS CRACKED UNDER END FITTING. MAJOR REPAIR ACCOMPLISHEDREPAIRED STRINGER PER SRM 53-00-03, FIG 202 AND INSTALLED PER SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001050300318 20010503 00318 NM 2001 5 3 2001UALA00356 1 20010328 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 AFT CABIN STA 1640 LBL 8 TO RBL 62 TOP CAP OF FLOOR BEAM HAS HEAVY CORROSION. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCO MPLISHED. CORROSION DAMAGE RESULTED IN REPLACEMENT OF THE DAMAGED SECTION OF THE UPPER CHORD. A REPLACEMENT SECTION OF THE UPPER CHORD WAS SPLICED IN WITH ANGLES AND STRAPS. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600319 20010416 00319 NM 2001 4 16 2001UALA00357 1 20010328 A 5753 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT WING TE FLAP MISREPAIRED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 506UA 24627 RIGHT WING OTBD FLAP UPPER SURFACE NEAR LEADING EDGE HAS SCAB PATCH REPAIR DIRECTLY BELOW NR 10 SPOILER. MAJOR REPAIR A CCOMPLISHED. ACCOMPLISHED FLUSH REPAIR PER SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600320 20010416 00320 NM 2001 4 16 2001UALA00358 1 20010328 A 5320 CHANNEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 CABIN FLOOR STA 366 RBL 10 FLOOR CHANNEL CORRODED AT FLOOR BEAM ATTACH POINT. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR CHANNEL. 2 L 7 2 4F 4 F RT A2NM E17NE 2001042400197 20010424 00197 NM 2001 4 24 2001UALA00359 1 20010327 A 2822 7276138 PUMP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 FUEL BOOST INOPERATIVE A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 7460U 21914 AIRCRAFT DIVERTED TO DEN DUE TO INOPERABLE NR 2 RIGHT FUEL BOOST PUMP INDICATION. SUPPLEMENTAL DATA UPDATE. REPLACED NR 2 AFT LEFT CIRCUIT BREAKER. 2 L 7 3 4F 4 F A3WE E2EA 2001041600321 20010416 00321 EU 2001 4 16 2001UALA00360 1 20010329 A 5230 BEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CARGO DOOR BENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 401UA 435 FORWARD CARGO DOOR AFT ACTUATOR MOUNT BEAM IS BENT. REPLACED ACTUATOR ATTACH BEAM. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A28NM E40NE 2001041600322 20010416 00322 NM 2001 4 16 2001UALA00361 1 20010328 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 310UA 23671 AFT PIT STA 787 RBL 30 FRAME HAS A DENT ABOVE STRINGER 24R. REPAIRED FRAME. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600323 20010416 00323 NM 2001 4 16 2001UALA00362 1 20010328 A 5312 PRESSURE PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE MLG WW CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 310UA 23671 CABIN STA 664 AT RBL 40 WHEEL WELL PRESSURE DECK IS CRACKED. REPAIRED CRACKED PRESSURE DECK. MAJOR REPAIR ACCOMPLISHED . 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600324 20010416 00324 NM 2001 4 16 2001UALA00363 1 20010328 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 310UA 23671 STA 277 STRINGER 11R HAS A LARGE AMOUNT OF MATERIAL LOSS. REPAIRED AFFECTED STRINGER. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600326 20010416 00326 NM 2001 4 16 2001UALA00365 1 20010329 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 CABIN STA 1016 RBL 17 TO RBL 37 HAS CORROSION ON THE FLOORBEAM. FLOOR BEAM REPAIRED. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600328 20010416 00328 NM 2001 4 16 2001UALA00367 1 20010330 A 5310 STRUCTURE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 AFT PIT SUPPORT STRUCTURE FOR THE VHF ANTENNA IS CORRODED BETWEEN STA 727D AND STA 727E. REPLACED CHANNEL SUPPORT STRUC TURE FOR THE VHF ANTENNA. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600329 20010416 00329 NM 2001 4 16 2001UALA00369 1 20010329 A 5315 KEELBEAM BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 995UA 22399 DAMAGED AREAS AT KEEL BEAM STA 680 AND STA 708. REPLACES FASTENERS AT DAMAGED AREAS. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F A16WE E2EA 2001041600330 20010416 00330 NM 2001 4 16 2001UALA00371 1 20010330 A 5415 BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 NR 2 ENGINE PYLON FAN COWL SUPPORT BEAM NAC STA 102 LT SIDE INNER ANGLE CRACKED AFT SIDE OF WEB NEAR CENTER CHORD. MAJO R REPAIR ACCOMPLISHED.REPLACED ANGLE PER SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600331 20010416 00331 NM 2001 4 16 2001UALA00372 1 20010329 A 3230 656021132 ACCESSORY UNIT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE MLG FAILED A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 7258U 21405 LANDING GEAR HANDLE COULD NOT BE RETRACTED INTO UP POSITION. LANDING GEAR HAD TO BE BROUGHT UP MANUALLY. SUPPLEMENTAL DA TA UPDATE REPLACED LANDING GEAR ACCESSORY UNIT. ACCOMPLISHED WIRING CHECK BETWEEN LEVER LATCH SOLENOID AND LANDING GEAR ACCESSORY UNIT. ALSO ACCOMPLISHED WIRING CHECK BETWEEN AIR /GROUND SENSORS AND LANDING GEAR ACCESSORY UNIT. FUNCTI ON TESTS OK. 2 L 7 3 4F 4 F A3WE E2EA 2001041600332 20010416 00332 2001 4 16 MALA010323 4 20010401 A 3417 62244010001 ADC SAAB SF340 SF340A 7850100 EU E/E BAY DEFECTIVE A MALA O OTHER G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 GL 15 106XJ 106 ON FLIGHT 3308 IN DTW. CAPT. AIRSPEED INDICATION AND CAPT ALTIMETER FAILED INFLIGHT. MAINTENANCE DRAINED AND PURGED NR 1 PITOT/STATIC SYSTEM, REPLACED AIR DATA COMPUTER, PN 622-44010-001 SN/ON 17465, PN/OFF 822-0370-123 SN/OFF 4127. ALL CHECKS GOOD IAW SF340 MM/CHAP 34. 2 L 7 2 4T RT A52EU 2001041600333 20010416 00333 EU 2001 4 16 MALA010324 1 20010308 A 5330 SHIELD SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430XJ 430 FOUND DURING C-CHECK, IN NASHVILLE, TN, SEVERAL DENTS AFT OF RT ICE SHIELD BETWEEN STA 354.0 TO STA 339. FOUND DENTS OUT OF ALLOWABLE LIMIT REF SAAB SRM 51-10-10. NDTPERFFVNDT006 & 004 BOND. NO CRACKS NO DELAMINATION NOTED. DENTS ARE ACCEP TABLE IAW SAAB DOCUMENT 340SDS001241. 2 L 7 2 4T RT A52EU 2001041600334 20010416 00334 EU 2001 4 16 MALA010325 1 20010308 A 5330 SHIELD SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430XJ 430 FOUND DURING C-CHECK, A GROUP OF DENTS AFT OF RH ICE SHIELD AT STA 357.0. MAINTENANCE FOUND DENTS OUT OF ALLOWABLE LIMI T REF SAAB SRM 51-10-10. NDTPERFFVNDT006EC & 004 BOND. NO CRACKS, NO DELAMINATION NOTED. DENTS ARE ACCEPTABLE IAW SAAB D OCUMENT 340SDS001241. 2 L 7 2 4T RT A52EU 2001041600335 20010416 00335 EU 2001 4 16 MALA010326 1 20010308 A 5320 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430XJ 430 FOUND DURING C-CHECK, CARGO COMPARTMENT LT SEAT TRACK AT LBL 18 BETWEEN STA 630 AND STA 686 HAS CORROSION. MAINTENANCE T HOROUGHLY CLEANED AREA IAW SRM 51-20-41, REMOVED CORROSION. IAW SRM 51-70-40, ALODINED BARE METAL, MATERIAL REMOVED IS WITHIN LIMITS OK TO PRIME AND PAINT. 2 L 7 2 4T RT A52EU 2001041600336 20010416 00336 EU 2001 4 16 MALA010327 1 20010309 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430XJ 430 FOUND DURING C-CHECK, CORROSION ON IB FLOOR SUPPORT FLANGE, SEAT TRACK LBL 18.3 FROM FS 465 THRU FS 630. MAINTENANCE REM OVED CORROSION FROM STA 465-630 AS WORKED IAW 51-70-40. MATERIAL REMOVED IS WITHIN LIMITS IAW SRM 53-70-60. ALODINED, PR IMED AND TOPCOATED AFFECTED AREAS AS NOTED.IAW SRM 51-20-42/43. 2 L 7 2 4T RT A52EU 2001041600337 20010416 00337 EU 2001 4 16 MALA010328 1 20010312 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430XJ 430 FOUND DURING C-CHECK, CORROSION ON FLOOR BOARD FLANGE BETWEEN STA 258.0 AND FS 236.5. MAINTENANCE REMOVED CORROSION, MAT ERIALS REMOVED IS OUT OF LIMITS, REMOVED OLD FLANGE, FABRICATED NEW FLANGE, PER SAMPLE. OK TO TREAT AND PRIME AND TOPCO AT. INSTALLED NEW FLANGE IAW SRM 51-40-21 2 L 7 2 4T RT A52EU 2001041600338 20010416 00338 EU 2001 4 16 MALA010329 1 20010312 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430XJ 430 FOUND DURING C-CHECK, GALLEY SEAT TRACK HAS CORROSION AT STA 272.0 MAINTENANCE REMOVED CORROSION AT GALLEY SEAT TRACK STA 272.0, NEGATIVE MATERIALS REMOVED, WITHIN LIMITS, ALODINED, PRIMED AND TOPCOATED. 2 L 7 2 4T RT A52EU 2001041600339 20010416 00339 EU 2001 4 16 MALA010330 1 20010312 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430XJ 430 FOUND DURING C-CHECK, CORROSION ON FLOOR BOARD FLANGE AT FS STA 231.0. MAINTENANCE REMOVED CORROSION, MATERIAL REMOVED A RE WITHIN LIMIT. OK TO ALODINE, PRIME AND PAINT. OK TO TREAT AND PRIME PLUS TOPCOAT. TREATED AND PAINTED IAW SRM 51-20 -43. 2 L 7 2 4T RT A52EU 2001041600340 20010416 00340 EU 2001 4 16 MALA010331 1 20010312 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430XJ 430 FOUND DURING C-CHECK, CORROSION ON FLOORBOARD FLANGE AT STA 258.0 FOR PANEL 121AZ. MAINTENANCE REMOVED CORROSION, MATERI AL REMOVED IS OUT OF LIMIT, REMOVED FWD FLANGE , AND FABRICATED NEW FWD FLANGE PER SAMPLE. FABRICATED NEW AFT FLANGE. O K TO TREAT, PRIME AND TOPCOAT BOTH FWD AND AFT FLANGES. ALODINED AND PAINTED 2 EA. FLANGES IAW SRM 51-20-42/43. 2 L 7 2 4T RT A52EU 2001041600341 20010416 00341 EU 2001 4 16 MALA010332 1 20010312 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430XJ 430 FOUND DURING C-CHECK, CORROSION ON FLOOR BOARD FLANGE AT FS STA 272 UNDER GALLEY FLOORBOARD PANEL 122BZ. MAINTENANCE REM OVED CORROSION FROM FLOORBOARD ANGLE, MAERIAL REMOVED IS BEYOND LIMITS PER SRM 51-10-10. REMOVED L ANGLE AT STA 272.0 IA W 51-40-21. FABRICATED NEW L ANGLE PER SAMPLE, TREATED, PRIMED AND TOPCOATED. 2 L 7 2 4T RT A52EU 2001041600342 20010416 00342 EU 2001 4 16 MALA010333 1 20010312 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430XJ 430 FOUND DURING C-CHECK, CORROSION ON FLOOR SUPPORT FLANGE RBL 33 AT FS 500 AND FS 535. MAINTENANCE REMOVED CORROSION, R EMAINING MATERIAL IS WITHIN LIMITS. TREATED, PRIMED AND TOPCOATED IAW SRM 51-20-42/43. 2 L 7 2 4T RT A52EU 2001041600343 20010416 00343 EU 2001 4 16 MALA010334 1 20010312 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430XJ 430 FOUND DURING C-CHECK, CORROSION ON FLOOR SUPPORT FLANGE AT RBL 33, STA 355. MAINTENANCE REMOVED CORROSION, MATERIAL REMO VED IS WITHIN LIMITS, TREATED, PRIMED AND TOPCOATED IAW SRM 51-20-42/43. 2 L 7 2 4T RT A52EU 2001041600344 20010416 00344 EU 2001 4 16 MALA010335 1 20010312 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430XJ 430 FOUND DURING C-CHECK, CORROSION ON FLOOR SUPPORT FLANGE AT LBL 33, STA 345 THRU FS 329. MAINTENANCE REMOVED CORROSION, MATERIAL REMOVED WITHIN LIMITS, TREATED, PRIMED AND TOPCOATED IAW SRM 51-20-42/43. 2 L 7 2 4T RT A52EU 2001041600345 20010416 00345 EU 2001 4 16 MALA010336 1 20010316 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430XJ 430 FOUND DURING C-CHECK, CORROSION ON WEB AND ON INBOARD FLOOR SUPPORT FLANGE, SEAT TRACK 18.3 FS 294.0 THRU FS 415. MAINT ENANCE REMOVED CORROSION FROM WEB AND IB FLOOR SUPPORT. MATERIAL REMOVED IS OUT OF LIMITS. CUT OUT DAMAGED SECTION OF S EAT TRACK IAW SRM 53-70-60. OPERATIONAL CHECK PERFORMED ON EMERGENCY LIGHTING IAW AMM 33-50-00-5. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2001041600346 20010416 00346 EU 2001 4 16 MALA010337 1 20010319 A 5711 7257110308 SPAR SAAB SF340 340B 7860101 EU RT WING CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430XJ 430 FOUND DURING C-CHECK, RT WING FWD SPAR LOWER CAP IB OF NACELLE IS CHAFED. MAINTENANCE LIGHTLY BLENDED AREAS IAW SRM 51-1 0-10, ALODINED BARE METAL IAW SRM 51-20-43. FOUND DEEP CORROSION PITS, OUT OF ALLOWABLE LIMIT REF SRM 51-10-10. REMOVED 611BR TO FOM IAW AMM 51-20-05. REINSTALLED LEADING EDGE FAW 57-20-05.PERFORM OPS CHECK OF LEADING EDGE. FAILED OPS CHE CK REFER TO W/O 19471, MR6525, REPLACMENT OF BOOT. 2 L 7 2 4T RT A52EU 2001041600347 20010416 00347 EU 2001 4 16 MALA010338 1 20010319 A 5711 7257110307 SPAR SAAB SF340 340B 7860101 EU LT WING CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430XJ 430 FOUND DURING C-CHECK, LT WING FWD SPAR LOWER CAP IB OF NACELLE IS CHAFED. MAINTENANCE LIGHTLY BLENDED AREA, ALODINED BAR E METAL IAW SRM 51-20-43. FOUND DEEP CORROSION PITS, OUT OF ALLOWABLE LIMIT REF SRM 51-10-10. REMOVED 511BL/CL/AL TO FO M, REINSTALLED I/ES 511AL, 511BL AND 511CL IAW AMM 57-20-05. PERFORMED OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2001041600348 20010416 00348 EU 2001 4 16 MALA010339 1 20010319 A 5410 DUCT SAAB SF340 340B 7860101 EU NACELLE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430XJ 430 FOUND DURING C-CHECK, COWL 463AL NACA DUCT IS CRACKED. MAINTENANCE REMOVED CRACK BY ROUTING METHODS IAW SRM 51-70-00; N DT REQUIRED FOR FURTHER CRACKING. NDT PER FFVNDT006EC NO CRACKS PAST ROUTE OUT. REPAIR IS ACCEPTABLE IAW SAAB DOCUMENT 340SDS001241. AREA IS PRIMED AND TREATED. 2 L 7 2 4T RT A52EU 2001041600349 20010416 00349 EU 2001 4 16 MALA010340 1 20010319 A 5410 DUCT SAAB SF340 340B 7860101 EU LT NACELLE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430XJ 430 FOUND DURING C-CHECK, LT COWL 453AL NACA DUCT IS CRACKED. MAINTENANCE REMOVED CRACK BY ROUTING METHODS IAW SRM 51-70-00 . NDT REQUIRED FOR FURTHER CRACKING. NDTPERFFVNDT006ED NO CRACKS PAST ROUT OUT. REPAIR IS ACCEPTABLE IAW SAAB DOCUMENT 3 40SDS001241.AREA IS PRIMED AND TREATED. 2 L 7 2 4T RT A52EU 2001041600350 20010416 00350 EU 2001 4 16 MALA010341 1 20010319 A 5410 DUCT SAAB SF340 340B 7860101 EU LT NACELLE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430XJ 430 FOUND DURING C-CHECK, LT COWL 453BR NACA DUCT HAS CRACKS. MAINTENANCE REMOVED CRACK BY ROUTING METHODS IAW SRM 51-70-00 ; NDT REQUIRED FOR FURTHER CRACKING. NDT PER FFVNDT006ED NO CRACKS. DAMAGE IS ACCEPTED AS IS AREA IS PRIMED AND TREATED REF SAAB SRM 340SDS001241. 2 L 7 2 4T RT A52EU 2001041600351 20010416 00351 EU 2001 4 16 MALA010342 1 20010319 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430XJ 430 FOUND DURING C-CHECK, CORROSION ON LT FLOOR SUPPORT FLANGE ON SEAT TRACK BLO STA 294 THRU STA 415. MAINTENANCE REMOVED C ORROSION FROM LT FLOOR SUPPORT FLANGE. MATERIAL REMOVED IS OUT OF LIMITS. SEAT TRACK BLO WILL BE REPLACED FROM STA 294.0 TO 686. SEE W/O 19471, TASK 1550 FOR CORRECTIVE ACTION. 2 L 7 2 4T RT A52EU 2001041600352 20010416 00352 EU 2001 4 16 MALA010343 1 20010319 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430XJ 430 FOUND DURING C-CHECK, CARGO COMPARTMENT SEAT TRACK AT BLO HAS CORROSION BETWEEN FS 630 TO FS 686. MAINTENANCE REMOVED C ORROSION FROM STA 630-686. FOUND TO BE OUT OF LIMIT REF SRM 53-70-60. SEAT TRACK BLO WILL BE REPLACED FROM STA 294 TO 68 6.SEE W/O 19471, TASK 1550, FOR CORRECTIVE ACTION. 2 L 7 2 4T RT A52EU 2001041600353 20010416 00353 EU 2001 4 16 MALA010344 1 20010319 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430XJ 430 FOUND DURING C-CHECK, CARGO COMPARTMENT SEAT TRACK AT RBL 18 HAS CORROSION. MAINTENANCE REMOVED CORROSION, CLEANED SEAT TRACK AREA, MATERIAL REMOVED IS OUT OF LIMITS. APPLIED SURFACE PROTECTION IAW SRM 51-20-42/43. MATERIAL REMOVED IS ACC EPTABLE IAW SAAB DOC 340SDS01241. 2 L 7 2 4T RT A52EU 2001041600354 20010416 00354 EU 2001 4 16 MALA010345 1 20010320 A 5347 7253725191 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430XJ 430 FOUND DURING C-CHECK BY CELSIUS, CORROSION ON LT FLOOR SUPPORT FLANGE, SEAT TRACK BLO FROM STA 465 THRU STA 630. MAINTE NANCE REMOVED CORROSION FROM STA 465-630. MATERIAL REMOVED IS OUT OF LIMITS. 2 L 7 2 4T RT A52EU 2001041600355 20010416 00355 EU 2001 4 16 MALA010358 1 20010330 A 2730 7227105712 CONTROL CABLE SAAB SF340 SF340A 7850100 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 79XJ 079 FOUND DURING 4K-INSPECTION, CWA. LT OB ELEVATOR CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED CABLE PN 7227105-712. 2 L 7 2 4T RT A52EU 2001041600356 20010416 00356 EU 2001 4 16 MALA010359 1 20010330 A 2720 7227105582 CONTROL CABLE SAAB SF340 SF340A 7850100 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 79XJ 079 FOUND DURING 4K-INSPECTION, CWA. RT AFT SINGLE RUDDER CABLE CHAFED IN CIRCUIT I. MX REMOVED AND REPLACED CABLE PN 7227 105-582. 2 L 7 2 4T RT A52EU 2001041600357 20010416 00357 EU 2001 4 16 MALA010360 1 20010330 A 2710 CONTROL CABLE SAAB SF340 SF340A 7850100 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 79XJ 079 FOUND DURING 4K-INSPECTION, CWA. LT AILERON FWD OB WING CABLE IS CHAFED, MX REMOVED AND REPLACED CABLE. 2 L 7 2 4T RT A52EU 2001041600358 20010416 00358 EU 2001 4 16 MALA010361 1 20010330 A 2720 CONTROL CABLE SAAB SF340 SF340A 7850100 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 79XJ 079 FOUND DURING 4K-INSPECTION, CWA. RT RUDDER OB CABLE IS CHAFED IN CIRCUIT I. MX REPLACED OB RUDDER CABLE. 2 L 7 2 4T RT A52EU 2001041600359 20010416 00359 EU 2001 4 16 MALA010362 1 20010330 A 7120 MOUNT SAAB SF340 SF340A 7850100 EU ENGINE WORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 79XJ 079 FOUND DURING 4K-INSPECTION, CWA. RT NACELLE IB AND OB ENGINE STRUTS HAVE EXCESSIVE PLAY. MX REAMED OB UPPER AND LOWER AND IB LOWER ATTACHMENTS TO SECOND OVERSIZE IAW SB340-54-027. RT IB UPPER FITTING EXCEEDED ALLOWABLE LIMITS. MX REPAIR ED FITTING IAW SAAB STATEMENT 340SDS001318. REPLACED STRUT UPPER FITTING. 2 L 7 2 4T RT A52EU 2001041600360 20010416 00360 EU 2001 4 16 MALA010346 1 20010330 A 2711 7227150121 LINKAGE SAAB SF340 SF340A 7850100 EU RT AILERON WORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 79XJ 079 FOUND DURING 4K-INSPECTION, IN CWA, CONNECTING LINKS AT RT AILERON TRIM TAB PUSH / PULL TUBES ARE WORN. MX REMOVED AND R EPLACED LINKS. PN 7227150121, PN 7227150-123. 2 L 7 2 4T RT A52EU 2001041600361 20010416 00361 EU 2001 4 16 MALA010347 1 20010330 A 2731 7227150125 LINKAGE SAAB SF340 SF340A 7850100 EU ELEVATOR TRIM WORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 79XJ 079 FOUND DURING 4K-INSPECTION, CWA, CONNECTING LINKS ARE WORN AT RT ELEVATOR TRIM TAB PUSH / PULL TUBES. MX REMOVED AND REP LACED LINKS. PN (2) 7227150-125. 2 L 7 2 4T RT A52EU 2001041600362 20010416 00362 EU 2001 4 16 MALA010348 1 20010328 A 3230 FITTING SAAB SF340 SF340A 7850100 EU DRAG STRUT DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 79XJ 079 FOUND DURING 4K-INSPECTION, CWA. RT IB UPPER DRAG STRUT FITTINGS HAVE EXCESSIVE CLEARANCE. LT NACELLE BOTTOM ENGINE MOU NT FITTING HOLE. RT NACELLE BOTTOM ENGINE MOUNT FITTING HOLES HAVE EXCESSIVE CLEARANCE. MX REPAIRED DEFECTS IAW EO 54058 , SAAB STATEMENT 340SDS001318. 2 L 7 2 4T RT A52EU 2001041600363 20010416 00363 EU 2001 4 16 MALA010349 1 20010328 A 3230 FITTING SAAB SF340 SF340A 7850100 EU DRAG STRUT DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 79XJ 079 FOUND DURING 4K-INSPECTION, CWA. LT OB LOWER DRAG STRUT FITTINGS HAVE EXCESSIVE CLEARANCE. LT NACELLE BOTTOM ENGINE MOU NT FITTING HOLE.LT NACELLE BOTTOM ENGINE MOUNT FITTINGS HOLES HAVE EXCESSIVE CLEARANCE. MX REPAIRED DEFECTS IAW EO S540 48, SAAB STATEMENT 340SDS001318. 2 L 7 2 4T RT A52EU 2001041600364 20010416 00364 EU 2001 4 16 MALA010350 1 20010316 A 5410 FASTENER SAAB SF340 SF340A 7850100 EU LT NACELLE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 79XJ 079 FOUND DURING 4K-INSPECTION, CWA. LT NACELLE OB & IB FWD SKIN HAS FASTENERS PULLING THROUGH SKIN AROUND NACELLE STA 203. MX COMPLETED REPAIR IAW MAL EO S54049. 2 L 7 2 4T RT A52EU 2001041600365 20010416 00365 EU 2001 4 16 MALA010351 1 20010330 A 7120 MOUNT SAAB SF340 SF340A 7850100 EU LT ENGINE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 79XJ 079 FOUND DURING 4K-INSPECTION, CWA. LT NACELLE LOWER ENGINE MOUNT OB HOLE HAS EXCESSIVE CLEARANCE BETWEEN BOLTS AND NACELLE . MX REPAIRED IAW EO S54048 AND SAAB STATEMENT 340SDS001318. 2 L 7 2 4T RT A52EU 2001041600366 20010416 00366 EU 2001 4 16 MALA010352 1 20010330 A 7120 BOLT SAAB SF340 SF340A 7850100 EU ENGINE MOUNT LOOSE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 79XJ 079 FOUND DURING 4K-INSPECTION, CWA. LT NACELLE OB LOWER ENGINE STRUT ATTACHMENT BOLT HAS AXIAL PLAY. MX REPAIRED IAW EO S5 4048 AND SAAB STATEMENT 340SDS001318. 2 L 7 2 4T RT A52EU 2001041600367 20010416 00367 EU 2001 4 16 MALA010353 1 20010330 A 2710 7227151522 CONTROL CABLE SAAB SF340 SF340A 7850100 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 79XJ 079 FOUND DURING 4K-INSPECTION, CWA. RT OB WING FWD AILERON CABLE IS CHAFED. MX REPLACED CABLE PN 7227151-522. 2 L 7 2 4T RT A52EU 2001041600368 20010416 00368 EU 2001 4 16 MALA010354 1 20010330 A 7120 BOLT SAAB SF340 SF340A 7850100 EU ENGINE MOUNT LOOSE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 79XJ 079 FOUND DURING 4K-INSPECTION, CWA. RT NACELLE LOWER ENGINE MOUNT BOLT HOLES HAVE EXCESSIVE CLEARANCE BETWEEN BOLTS AND NA CELLE FRAME. MX REPAIRED IAW EO S54048, AND SAAB STATEMENT 340SDS001318. 2 L 7 2 4T RT A52EU 2001041600369 20010416 00369 EU 2001 4 16 MALA010355 1 20010330 A 2730 7227705644 CONTROL CABLE SAAB SF340 SF340A 7850100 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 79XJ 079 FOUND DURING 4K-INSPECTION, CWA. LT IB CABIN ELEVATOR CABLE CHAFED. MX REMOVED AND REPLACED CABLE PN 7227705-644. 2 L 7 2 4T RT A52EU 2001041600370 20010416 00370 EU 2001 4 16 MALA010356 1 20010330 A 2720 7227150562 CONTROL CABLE SAAB SF340 SF340A 7850100 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 79XJ 079 FOUND DURING 4K-INSPECTION, CWA. LT OB RUDDER CABLE IN CIRCUIT I IS CHAFED. MX REMOVED AND REPLACED CABLE PN 7227150-56 2. 2 L 7 2 4T RT A52EU 2001041600371 20010416 00371 EU 2001 4 16 MALA010357 1 20010330 A 2730 7227105712 CONTROL CABLE SAAB SF340 SF340A 7850100 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 79XJ 079 FOUND DURING 4K-INSPECTION, CWA. RT OB ELEVATOR CABLE CHAFED IN CABIN. MX REMOVED AND REPLACED CABLE PN 7227105-712. 2 L 7 2 4T RT A52EU 2001041600372 20010416 00372 EU 2001 4 16 MALA010363 1 20010401 A 3010 3950FS2 EJECTOR VALVE SAAB SF340 SF340A 7850100 EU STAB DEICE FAILED A MALA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 GL 15 107XJ 340A107 ON CLIMBOUT FROM DTW ON FLIGHT 2800, STAB DEICE LIGHT WOULD NOT ILLUMINATE. TRIED MANUAL INFLATION AND LIGHT FLICKERED BUT DID NOT ILLUMINATE STEADY. TRIED AGAIN ON MANUAL AND AUTO AND ONLY GOT FLICKER. AIR TURNBACK TO DTW. MAINTENANCE R EPLACED EJECTOR VALVE FOR TAIL BOOT PN 3950FS2, SN/0764. ALL CHECKS GOOD AT THIS TIME IAW SF340MM. 2 L 7 2 4T RT A52EU 2001041600373 20010416 00373 EU 2001 4 16 MALA010365 1 20010323 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428XJ 428 FOUND DURING C-CHECK, CORROSION ON CARGO BAY SEAT TRACK AT LBL 18.3. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40. MA TERIAL OUT OF LIMITS REF SRM 53-70-60, 51-10-10. DAMAGE IS ACCEPTED AS IS, COMPLIED WITH SURFACE TREAT WENT AND PROTECT ION REF SAAB EO 340 SDS001346. 2 L 7 2 4T RT A52EU 2001041600374 20010416 00374 EU 2001 4 16 MALA010366 1 20010326 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428XJ 428 FOUND DURING C-CHECK, CORROSION ON FLOORBOARD FLANGE AT STA 231.0. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40. REMA INING MATERIAL IS OUT OF LIMITS REF SRM 51-10-10. FABRICATED REPAIR ANGLE PER PRINCIPLES OF SRM 51-70-20, ALODINED, PRIM ED AND TOPCOATED PER SRM 51-20-42/43, INSTALLED REPAIR ANGLE IAW SRM 51-40-21. 2 L 7 2 4T RT A52EU 2001041600375 20010416 00375 EU 2001 4 16 MALA010367 1 20010326 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428XJ 428 FOUND DURING C-CHECK, CORROSION IN CARGO AREA SEAT TRACK BL-0 FROM STA 608.0 THRU STA 658.5. REMOVED CORROSION IAW SR M 51-70-40. MATERIAL OUT OF LIMITS, REF SRM 53-70-60, 51-10-10. FABRICATED LAYED OUT AND DRILLED REPAIR DOUBLER , ALODIN ED AND PRIMED TOPCOATED AND INSTALLED REPAIR. 2 L 7 2 4T RT A52EU 2001041600376 20010416 00376 EU 2001 4 16 MALA010368 1 20010327 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428XJ 428 FOUND DURING C-CHECK, CORROSION ON SEAT TRACK AT LBL 18.3 ON FLOOR PANEL INBOARD FLANGE FROM STA 411-STA 440. REMOVED S URFACE CORROSION, TREATED W/ALODINE 1200, MATERIAL REMOVED IS WITHIN LIMITS IAW SRM 53-70-60. OK TO PRIME AND PAINT. AL ODINE, PRIME AND PAINTED SEAT TRACK AND FLANGES. IAW SRM 51-20-00. 2 L 7 2 4T RT A52EU 2001041600377 20010416 00377 EU 2001 4 16 MALA010369 1 20010327 A 5330 DOUBLER SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428XJ 428 FOUND DURING C-CHECK, CORROSION ON THE VHF ANTENNA MOUNTING DOUBLER ON THE LOWER FUSELAGE. MAINTENANCE REMOVED CORROSION ON ANTENNA MOUNTING DOUBLER, NEGLIGABLE AMOUNT OF MATERIAL REMOVED OK TO TREAT, ALODINE ANTENNA MOUNTING DOUBLER IAW SR M 51-20-03. 2 L 7 2 4T RT A52EU 2001041600378 20010416 00378 EU 2001 4 16 MALA010370 1 20010327 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428XJ 428 FOUND DURING C-CHECK, CORROSION ON FLOORBOARD FLANGE AT STA 272.0 THRU STA 288.0. MAINTENANCE REMOVED CORROSION AS REQU IRED, MATERIAL REMOVED IS OUT OF LIMITS. REMOVED ANGLE AT STA 272 TO 288, FABRICATED NEW ANGLE, PRIMED, ALODINED, AND P AINTED IAW SRM 51-20-42/43, INSTALLED ANGLE. 2 L 7 2 4T RT A52EU 2001041600379 20010416 00379 EU 2001 4 16 MALA010371 1 20010327 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428XJ 428 FOUND DURING C-CHECK BY CELSIUS, CORROSION ON FLOORBOARD FLANGE AT STA 272. AT FLOOR PANEL 122BZ. MAINTENANCE REMOVED C ORROSION AS REQUIRED. MATERIAL REMOVED IS OUT OF LIMITS. REMOVED ANGLE AT STA 272, FABRICATED NEW ANGLE, ALODINED, PRIM ED AND PAINTED. INSTALLED ANGLE IAW SRM 51-40-21 AND 23. 2 L 7 2 4T RT A52EU 2001041600380 20010416 00380 EU 2001 4 16 MALA010372 1 20010327 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428XJ 428 FOUND DURING C-CHECK, CORROSION ON GALLEY SEAT TRACK. MAINTENANCE REMOVED CORROSION AS REQUIRED, MATERIAL IS WITHIN LIM ITS. ALODINE, PRIME AND PAINTED GALLEY SEAT TRACK IAW SRM 51-20-00. 2 L 7 2 4T RT A52EU 2001041600381 20010416 00381 EU 2001 4 16 MALA010373 1 20010327 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428XJ 428 FOUND DURING C-CHECK, FLOORBOARD FLANGE BETWEEN STA 236.5 - STA 258.0 HAS CORROSION. MAINTENANCE REMOVED CORROSION AS R EQUIRED. REMAINING MATERIAL IS OUT OF LIMIT. REF SRM 51-10-10. REMOVED CORRODED ANGLE IAW 51-40-21. MATERIAL REMOVED FR OM INTERCOSTAL OUT OF LIMITS REF. SRM 51-10-10. 2 L 7 2 4T RT A52EU 2001041600382 20010416 00382 EU 2001 4 16 MALA010374 1 20010327 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428XJ 428 FOUND DURING C-CHECK, CORROSION ON FLOOR BOARD FLANGE AT STA 258.0 FOR FLOOR PANEL 121AZ. MAINTENANCE REMOVED CORROSION AS REQUIRED. REMAINING MATERIAL IS OUT OF LIMITS REF SRM 51-10-10. REMOVED CORRODED ANGLE. FABRICATED NEW ANGLE FOR F WD SIDE OF FRAME AT STA 258.0. FABRICATED REPAIR DOUBLER ,ALODINED, PRIMED AND PAINTED. INSTALLED REPAIR DOUBLER IAW SR M 51-40-21. 2 L 7 2 4T RT A52EU 2001041600383 20010416 00383 EU 2001 4 16 MALA010375 1 20010328 A 5320 7253721439 WEB SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428XJ 428 FOUND DURING C-CHECK, SEVERAL AREAS OF CORROSION ON WEB AT STA 288.0 TO STA 294.0. MAINTENANCE REMOVED CORROSION AS REQ UIRED. MATERIAL IS OUT OF LIMITS REF SRM 51-10-10. REMOVED WEB AS REQUIRED, LOCATED AND DRILLED NEW WEB IAW SRM 51-40-40 . INSTALLED NEW WEB IAW SRM 51-40-20/23. 2 L 7 2 4T RT A52EU 2001041600384 20010416 00384 EU 2001 4 16 MALA010376 1 20010328 A 5743 BUSHING SAAB SF340 340B 7860101 EU LT MLG TRUNNION CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428XJ 428 FOUND DURING C-CHECK, LT MLG OB TRUNNION PIN BUSHING HAS MIGRATED. MAINTENANCE REMOVED MIGRATING TRUNION PIN BUSHING ON LT OB MLG AND CLEANED AREA. INSTALLED TRUNION PIN BUSHINGS PER CMM 32-10-06. REFER TO IPM-12 FOR ALL REPAIRS DONE TO LH OB MLG. 2 L 7 2 4T RT A52EU 2001041600385 20010416 00385 EU 2001 4 16 MALA010377 1 20010329 A 5347 7253799383 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428XJ 428 FOUND DURING C-CHECK, CORROSION ON LT FLOOR SUPPORT FLANGE ON BLO SEAT TRACK STA 294, STA 339, STA 363, AND STA 371. MA INTENANCE REMOVED CORROSION FROM STA 294 TO 371. SEAT TRACK FLANGE BL0. MATERIAL REMAINING IS OUT OF ALLOWABLE LIMIT. R EF SRM 53-70-60/51-10-10 IN SEVERAL AREAS AS MARKED. PERFORMED CUT AT STA 330 SPLICED IN NEW TRACK STA 294 TO STA 330 AN D INSTALLED U-BEAM SPLICE REF. SAAB SRM 53-70-60. DAMAGED AREA AFT OF STA 330 TO STA 371 ARE ACCEPTED COMPLIED WITH SURF ACE TRATMENT AND PROCTION REF EO 340SDS001346. 2 L 7 2 4T RT A52EU 2001041600386 20010416 00386 EU 2001 4 16 MALA010378 1 20010329 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428XJ 428 FOUND DURING C-CHECK, CORROSION ON SEAT TRACK AT BLO, LT FLOOR PANEL FLANGE, FROM STA 411 THRU STA 465. MAINTENANCE REM OVED SURFACE CORROSION, TREATED W/ALODINE 1200 IAW SRM 51-20-42. MATERIAL REMOVED IS OUT OF LIMITS IAW SRM 53-70-60. DAM AGE IS ACCEPTED AS IS, COMPLIED WITH SURFACE TREATMENT AND PROTECTION REF SAAB EO 340SDS001346. 2 L 7 2 4T RT A52EU 2001041600387 20010416 00387 EU 2001 4 16 MALA010379 1 20010329 A 5330 SHIELD SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428XJ 428 FOUND DURING C-CHECK, LT FUSELAGE DENTS AFT OF ICE SHIELD BETWEEN SL1515 AND SL1517. MAINTENANCE INSPECTED AND FOUND DE NTS OUT OF LIMITS. DISTANCE BETWEEN DENTS CLOSER THAN 4 X L. NDT FOR CRACKS PER FFVNDT006 AND DISBOND INSPECTION PER SRM 51-10-10 REQUIREMENTS SHOWS NO CRACKS OR DELAMINATION. DENTS ARE ACCEPTED AS IS REF SAAB EO340SDS001346. 2 L 7 2 4T RT A52EU 2001041600388 20010416 00388 EU 2001 4 16 MALA010380 1 20010329 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428XJ 428 FOUND DURING C-CHECK, RT FUSELAGE DENTS BETWEEN STA 339 AND STA 363 AND SL1620 AND SL1622. MAINTENANCE INSPECTED AND FO UND DENTS OUT OF LIMITS. DISTANCE BETWEEN DENTS CLOSER THAN 4XL. NDT FOR CRACKS PER FFVNDT006 AND DISBOND INSPECTION PE R SRM 51-10-10 REQUIREMENTS SHOWS NO CRACKS OR DELAMINATION. DENTS ARE ACCEPTED AS IS REF. SAAB EO 340SDS001346. 2 L 7 2 4T RT A52EU 2001041600389 20010416 00389 EU 2001 4 16 MALA010381 1 20010329 A 5347 7253799383 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428XJ 428 FOUND DURING C-CHECK, CORROSION ON IB FLOOR SUPPORT FLANGE AND WEB ON LBL 18.3 SEAT TRACK STA 294, STA 339 AND STA 371. MAINTENANCE REMOVED CORROSION FROM STA 294 TO STA 371. SEAT TRACK FLANGE AND WEB LBL18.3. MATERIAL IS OUT OF ALLOWABLE LIMIT IN SEVERAL AREAS AS MARKED. PERFORMED CUT AT STA 330-SPLICED IN NEW TRACK STA 294 TO STA 330 AND INSTALLED U-BEAM SPLICE PN 7253799-379. REF. SAAB SRM 53-70-60. DAMAGE AREAS AFT OF STA 330 TO STA 371 ARE ACCEPTED AS IS. COMPLIED WIT H SURFACE TREATMENT AND PROTECTION REF EO340SDS001346. 2 L 7 2 4T RT A52EU 2001041600390 20010416 00390 EU 2001 4 16 MALA010382 1 20010328 A 3230 BUSHING SAAB SF340 340B 7860101 EU RT MLG TRUNNION LOOSE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428XJ 428 FOUND DURING C-CHECK, RT MLG OB TRUNION PIN BUSHING HAS MIGRATED. MAINTENANCE REMOVED MIGRATING TRUNION PIN BUSHINGS ON RT OB MLG AND CLEANED AREA. INSTALLED TRUNION PIN BUSHINGS PER CMM 32-10-06. 2 L 7 2 4T RT A52EU 2001041600391 20010416 00391 EU 2001 4 16 MALA010383 1 20010110 A 2720 CONTROL CABLE SAAB SF340 SF340A 7850100 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 27XJ 027 FROM CWA, DURING 4K INSPECTION, LT AFT SINGLE RUDDER CABLE IS CHAFED. REF TO 409 CARD 032208, MAINTENANCE REMOVED AND RE PLACED CABLE. 2 L 7 2 4T RT A52EU 2001041600392 20010416 00392 EU 2001 4 16 MALA010384 1 20010110 A 2720 CONTROL CABLE SAAB SF340 SF340A 7850100 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 27XJ 027 DURING 4K INSPECTION IN CWA, MAINTENANCE FOUND RT AFT SINGLE RUDDER CABLE IS CHAFED. REF TO 409 CARD 032209. MAINTENA NCE REPLACED CABLE. 2 L 7 2 4T RT A52EU 2001041600393 20010416 00393 EU 2001 4 16 MALA010385 1 20010110 A 2720 CONTROL CABLE SAAB SF340 SF340A 7850100 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 27XJ 027 DURING 4K INSPECTION, IN CWA, MAINTENANCE FOUND RT OB RUDDER CABLE IS CHAFED. REF TO 409 CARD 032210. MAINTENANCE REMO VED AND REPLACED CABLE. 2 L 7 2 4T RT A52EU 2001041600394 20010416 00394 EU 2001 4 16 MALA010386 1 20010110 A 2720 CONTROL CABLE SAAB SF340 SF340A 7850100 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 27XJ 027 DURING 4K INSPECTION IN CWA, MAINTENANCE FOUND LT OB RUDDER CABLE IS CHAFED. REF TO 409 CARD 032211. MAINTENANCE REMOVE D AND REPLACED CABLE. 2 L 7 2 4T RT A52EU 2001041600395 20010416 00395 2001 4 16 MALA010387 4 20010112 A 2562 ELT SAAB SF340 SF340A 7850100 EU CABIN WILL NOT TEST A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 27XJ 027 DURING 4K INSPECTION IN CWA, ELT WILL NOT TEST. REF 409 CARD 032284. MAINTENANCE REMOVED AND REPLACED ELT. 2 L 7 2 4T RT A52EU 2001041600396 20010416 00396 EU 2001 4 16 MALA010388 1 20010114 A 5347 SEAT TRACK SAAB SF340 SF340A 7850100 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 27XJ 027 DURING 4K INSPECTION IN CWA, LT CENTER AISLE SEAT TRACK CORRODED. REF TO 409 CARD 032268. MAINTENANCE REPAIRED SEAT TR ACK AT BL 18.3 FROM STA 294 TO STA 329.0 IAW EO 553060. 2 L 7 2 4T RT A52EU 2001041600397 20010416 00397 EU 2001 4 16 MALA010389 1 20010114 A 5414 SKIN SAAB SF340 SF340A 7850100 EU LT & RT NACELLE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 27XJ 027 DURING 4K INSPECTION IN CWA, LT AND RT NACELLE SKINS AND FRAMES WERE FOUND TO CRACKED AT NACELLE STA 203.0. REFER TO EO S54050. MAINTENANCE COMPLETED REPAIRS TO LT AND RT NACELLE AND FRAMES IAW SRS340 SDS001079. 2 L 7 2 4T RT A52EU 2001041600398 20010416 00398 EU 2001 4 16 MALA010390 1 20010117 A 5347 SEAT TRACK SAAB SF340 SF340A 7850100 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 27XJ 027 DURING 4K INSPECTION IN CWA, FOUND CORROSION ON LT IB CENTER AISLE SEAT TRACK UPPER FLOORBOARD FLANGE FROM STA 650.888 T O 686.888. REFER TO 409 CARD 32269. MAINTENANCE COMPLETED REPAIR IAW EO S53078. 2 L 7 2 4T RT A52EU 2001041600399 20010416 00399 EU 2001 4 16 MALA010391 1 20010117 A 5347 SEAT TRACK SAAB SF340 SF340A 7850100 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 27XJ 027 DURING 4K INSPECTION IN CWA, MAINTENANCE FOUND CORROSION ON RT CENTER AISLE SEAT TRACK IN CARGO COMPARTMENT STA 657 TO S TA 686.888. REFER TO EO S53078. MAINTENANCE REPAIRED IAW EO S53078. 2 L 7 2 4T RT A52EU 2001041600400 20010416 00400 EU 2001 4 16 MALA010392 1 20010403 A 5410 DRAG STRUT SAAB SF340 SF340A 7850100 EU LT & RT NACELLE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 27XJ 027 DURING 4K INSPECTION IN CWA, MAINTENANCE FOUND ELONGATED HOLES WERE NOTED IN LT AND RT NACELLE, IB AND OB DRAG STRUTS AN D FITTINGS. REF TO EO S54047. MAINTENANCE REPAIRED DRAG STRUTS AND FITTINGS IAW PROCEDURES CONTAINED IN SB340-57-027 AN D SRS 340 SDS001219 REV A-EOS54047. 2 L 7 2 4T RT A52EU 2001041600401 20010416 00401 EU 2001 4 16 MALA010393 1 20010404 A 3213 AXLE SAAB SF340 SF340A 7850100 EU NLG CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 27XJ 027 DURING 4K INSPECTION IN CWA, NLG AXLE FITTING IS CORRODED AT MATING SURFACE TO NOSE STRUT PISTON. REFER TO 409 CARD 122 801. MAINTENANCE REMOVED AND REPLACED AXLE FITTING. 2 L 7 2 4T RT A52EU 2001041600402 20010416 00402 NM 2001 4 16 UPS01235541 1 20010322 A 5330 LAP JOINT BOEING 727 72731C 1384011 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C+SI, BULGING AT LAP JOINT 1342 STR8L DETECTED, UPON INVESTIGATION CRACK A ND CORROSION WAS FOUND. RE PAIRED IAW SRM . 2 L 7 3 4F A3WE 2001041600403 20010416 00403 NM 2001 4 16 UPS01235542 1 20010322 A 5311 65224979 FRAME BOEING 727 72731C 1384011 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C+SI, DURING INSPECTION A CRACK WAS FOUND ON BS 930 RT FRAME RUNNING BETWEEN TWO FASTENERS HOLES BELOW STR 17. FRAME REPLACED. 2 L 7 3 4F A3WE 2001041600404 20010416 00404 NM 2001 4 16 UPS01235544 1 20010411 A 5753 CARRIAGE BOEING 727 72731C 1384011 NM NR 7 FLAP TRACK CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C+SI, NR 7 FLAP CARRIAGE HAS CORROSION INSIDE SPINDLE BORE. CARRIAGE ASSY REPLACED. 2 L 7 3 4F A3WE 2001041600405 20010416 00405 NM 2001 4 16 UPS01235545 1 20010320 A 5753 652165113 SUPPORT BRACKET BOEING 727 72731C 1384011 NM FLAP TRACK CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C+SI, NR 4 FLAP TRACK ATTACH LUG ON LWR SURFACE OF LT WING HAS LIGHT SURFACE CORROSION ON FACES OF LUG A ND DUR TO PREVIOUS REWORK HAS FREEZE PLUG INSERTED AND BUSHING FIT IS VERY LOOSE. NR 4 TRACK ATTACH LUG REPLACED. 2 L 7 3 4F A3WE 2001041600406 20010416 00406 NM 2001 4 16 UPS01235551 1 20010319 A 5320 BEAM BOEING 727 72731C 1384011 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C+SI, DURING INSPECTION A CRACK WAS FOUND ON BS 1183 VERTICAL BEAM AT 26,8 3 RT AT WATER LINE 262. REP AIRED IAW EO 727531106311 USING BOEING DWG 65C34406 AND KIT 6 5C34406-5 2 L 7 3 4F A3WE 2001041600407 20010416 00407 NM 2001 4 16 UPS01235552 1 20010321 A 5320 FITTING BOEING 727 72725C 138400H NM RT MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: C, RT WHEEL WELL BS 940 FRAME FITTING LWR HALF CRACKED INBD AFT SIDE INSTALLED UPPER AND LOWER BACK T O BACK BATH TUB FITTINGS. AS PER REF UPSMIA-01-0003F AND DRAWING 65-16337 AT RH STA 940 FITTING FLANGE 2 L 7 3 4F A3WE 2001041600408 20010416 00408 NM 2001 4 16 UPS01235553 1 20010321 A 5711 SPAR BOEING 727 72725C 138400H NM CENTER WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: C, WING CENTER SECTION FRONT SPAR T FITTING CRACKED LWR CHORD STA 740 LBL 42. REPLACED WING CENTER SEC TION FRONT SPAR T FITTING T LWR CHORD STA 74 0 LBL 42 IAW B727 SRM 51-30-2 2 L 7 3 4F A3WE 2001080600245 20010806 00245 NM 2001 8 6 UPS01435549 1 20010303 A 5311 FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:N/A CRACK ON NR 2 STRUT AFT BULKHEAD LEFT HAND CHORD AND FASTENER HOLE. *S/D* ACCOMPLISHED IAW EO MF-M AN-B747-5440-14107. 2 L 7 4 4F A20WE 2001073000039 20010730 00039 NM 2001 7 30 UPS01435550 1 20010303 A 5210 WEB BOEING 747 747212B 1384886 NM NR 3 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:N/A CRACKS ON NR 3 ENTRY DOOR LIGHTING HOLES. *S/D* ACCOMPLISHED REPAIR IAW EO 747-53-15-88270. 2 L 7 4 4F A20WE 2001041600409 20010416 00409 WP 2001 4 16 UPS01835539 1 20010323 A 5320 WEB DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C2 AT STA -67 SUB FLOOR RT SIDE CORROSION AT CUSP IN FLT DECK REPAIRED SUBFLOOR AT STA -67 AT CUSP A REA DAC DWG SRO 8530026 2 L 7 4 4F RT 4A25 2001041600410 20010416 00410 WP 2001 4 16 UPS01835548 1 20010411 A 5710 STRUCTURE DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 MX INSP-CRACK IN WING STRUCTURE JUST AFT OF LEFT MLG STRUT, MRR FILED AS OPEN. 2 L 7 4 4F RT 4A25 2001041600411 20010416 00411 NM 2001 4 16 2001UALA00242 1 20010312 A 2823 SHUTOFF VALVE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 FUEL TANK FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 7273U 21420 LOW FUEL INDICATION ON NR 2 TANK. AIRCRAFT DIVERTED TO DTW. SUPPLEMENTAL DATA UPDATE CROSSFEED SHUTOFF VALVE FAILED. REP LACED SHUTOFF VALVE. 2 L 7 3 4F 4 F A3WE E2EA 2001041600412 20010416 00412 NM 2001 4 16 2001UALA00243 1 20010312 A 2821 69186128 VENT LINE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 FUEL TANK LEAKING A UALA O OTHER K FLUID LOSS CL CLIMB 1 WP 29 7453U 21907 NR 3 FUEL TANK QUANTITY STEADILY DECREASED DURING CLIMB. SUPPLEMENTAL DATA UPDATE ELBOW VENT TUBE CRACKED. REPLACED VENT TUBE. 2 L 7 3 4F 4 F A3WE E2EA 2001041600413 20010416 00413 NM 2001 4 16 2001UALA00253 1 20010226 A 5315 141W851861 FLOORBEAM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 766UA 24045 0 26917 STA. 246 DISCREPANCIES: BUCKLED VERTICAL STIFFENERS AT RBL 7.88, 50.0 CRACKED VERTICAL STIFFENERS AT RBL 26.06, 38.0 CRA CKED MID CHORD AT RBL 38.0 CRACKED FLOORBEAM WEB AT RBL 38.0 SUPPLEMENTAL DATA UPDATE REPLACED STIFFENERS PER SRM 53-10- 51, REPAIR 3. REPAIRED MID CHORD PER SRM 53-10-51, REPAIR 2. REPAIRED WEB PER EVA G95-7683. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001041600414 20010416 00414 NM 2001 4 16 2001UALA00373 1 20010331 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 CABIN FLOORBEAM TOP SURFACE AT STA 365, CENTER TO RBL 61 CORRODED. MAJOR REPAIR ACCOMPLISHED.REPLACED T-ANGLE PER SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001043000012 20010430 00012 NM 2001 4 30 2001UALA00374 1 20010329 A 3320 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 9 A FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 766UA 26917 ABOVE 3A BURNING SMELL POSSIBLE ELECTRIC SMELL, VERYFAINT PER CREW. SUPPLEMENTAL DATA UPDATE PROBABLE CAUSE: FAILED L IGHT ASSEMBLY AND BULBDISCREPANCIES: FOUND CEILING LIGHT INOP AT SEAT 9A, FUSE INOP.CORRECTIVE ACTION: REPLACED CEILING LIGHT ASSY AND BULB. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001041600415 20010416 00415 NM 2001 4 16 2001UALA00375 1 20010330 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 AFT PIT FLOORBEAM IS CORRODED FROM STA 727 TO STA 947 RBL 13. REPLACED FLOOR SUPPORT BEAM FROM STA 727 TO STA 947 RBL 1 3. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600416 20010416 00416 NM 2001 4 16 2001UALA00376 1 20010402 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 FORWARD GALLEY DOOR FRAME CRACKED AT THE LOWER FORWARD CORNER UPPER OUTBOARD BOLT HOLE FOR THE STOP FITTING. REPAIRED C RACKED DOOR FRAME. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600417 20010416 00417 NM 2001 4 16 2001UALA00377 1 20010402 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 FORWARD GALLEY DOOR FRAME CRACKED AT THE LOWER AFT CORNER UPPER OUTBOARD BOLT HOLE FOR THE STOP FITTING. INSTALLED FRAM E KIT. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600418 20010416 00418 NM 2001 4 16 2001UALA00378 1 20010402 A 5210 SEAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE PAX DOOR MISDRILLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 310UA 23671 AFT ENTRY DOOR HAS MISDRILLED LOWER SEAL AT THE LOWER FRAME. REPAIRED AFT ENTRY DOOR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600419 20010416 00419 NM 2001 4 16 2001UALA00379 1 20010402 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 310UA 23671 BS 178 BULKHEAD WL 207 RBL 28 CHORD CRACKED. REPAIRED CHORD. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100020 20010521 00020 NM 2001 5 21 2001UALA00380 1 20010331 A 2420 GENERATOR BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE NR 2 FAILED A UALA C ABORTED TAKEOFF H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 WP 29 993UA 22383 NR 2 GENERATOR DROPPED OFF LINE. DRAINED THE CSD OIL TO PROPER LEVEL, AND CHECKED THE MAGNETIC OIL PLUG / FOUND CLEAN OF DEBRIS. FUNCTIONAL TEST ACCOMPLISHED. AIRCARFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A16WE E2EA 2001041600421 20010416 00421 NM 2001 4 16 2001UALA00382 1 20010411 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BETWEEN STRINGERS 38R - 39R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHEDFABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 51-40-02 AND BAC DRAWING 140T2102. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041600422 20010416 00422 NM 2001 4 16 2001UALA00383 1 20010330 A 3350 LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN LOOSE A UALA O OTHER O OTHER LD LANDING 1 WP 29 7450U 21904 EMERGENCY EXIT LIGHT FELL OFF DURING LANDING. SUPPLEMENTAL DATA UPDATE REINSTALLED EMERGENCY EXIT LIGHT. 2 L 7 3 4F 4 F A3WE E2EA 2001041600423 20010416 00423 NM 2001 4 16 2001UALA00384 1 20010331 A 5313 STRINGER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7297U 21892 STRINGER 22R AT STA 336 HAS DENT DAMAGE BEYOND ALLOWABLE LIMITS OF SRM 53-10-01. INSTALLED STRINGER REPAIR PER SRM 53- 10-03 FIGURE 1. MAJOR REPAIR ACCOMPLISHED. 2 L 7 3 4F 4 F A3WE E2EA 2001041600424 20010416 00424 NM 2001 4 16 2001UALA00385 1 20010330 A 5522 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT ELEVATOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7297U 21892 RT ELEVATOR EXTERIOR SKIN UPPER SURFACE HAS A HALF INCH CRACK ON THE INBOARD FORWARD SKIN. INSTALLED DOUBLER REPAIR PER SRM 55-20-03 FIGURE 4. CALCULATED WEIGHT AND BALANCE PER SRM 51-80-07. MAJOR REPAIR ACCOMPLISHED. 2 L 7 3 4F 4 F A3WE E2EA 2001041600425 20010416 00425 NM 2001 4 16 2001UALA00386 1 20010331 A 2761 ROD END BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE SLAT ACTUATOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7257U 21404 NR 5 SLAT ACTUATOR ROD END ATTACH POINT HAS AN EXISTING REPAIR WITH DOUBLE DRILLED HOLE AND CRACKED CORNERS. REPAIRED RIB PER EVA G07938 WHICH INCORPORATES A DOUBLER AND FILLER ON THE SLAT BEAM WEB. MAJOR REPAIR ACCOMPLISHED. 2 L 7 3 4F 4 F A3WE E2EA 2001041600426 20010416 00426 NM 2001 4 16 2001UALA00387 1 20010331 A 2761 ROD END BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE SLAT ACTUATOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7257U 21404 NR 5 SLAT ACTUATOR ROD END ATTACH POINT HAS AN EXISTING REPAIR WITH DOUBLE DRILLED HOLE AND CRACKED CORNERS. SUPPLEMENTA L DATA UPDATE REPAIRED RIB WITH DOUBLER AND FILLER ON THE SLAT BEAM WEB PER EVA G07938.MAJOR REPAIR ACCOMPLISHED. 2 L 7 3 4F 4 F A3WE E2EA 2001041600427 20010416 00427 NM 2001 4 16 2001UALA00388 1 20010402 A 5414 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 NR 2 PYLON INBOARD SKIN ACCESS CUTOUT CRACKED. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER REPAIR PER SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001070600041 20010706 00041 NM 2001 7 6 2001UALA00390 1 20010302 A 2913 271T4610 PUMP BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE HYD SYSTEM FAILED A UALA O OTHER F FLT CONT AFFECTED CL CLIMB 1 WP 29 666UA 29238 AFTER T/O DURING FLAP RETRACTION A LOUD METAL ON METAL SOUND WAS HEARD THROUGHOUT THE ACFT. THIS NOISE CONFIRMED BY FLT CREW WHILE FLAPS IN MOTION AND CEASED IMMEDIATELY WHEN FLAPS STOPPED. *S/D* INTERNAL FAILURE OF CENTER HYDRAULIC SYST EM AIR DRIVEN PUMP (ADP) CAUSED GRINDING SOUND IN PUMP. THIS PUMP IS ON DEMAND FOR T/O WITH BOTH LANDING GEAR AND TRAIL ING EDGE FLAP SYSTEMS OPERATIVE. REPLACED SUBJECT ADP WITH SERVICEABLE UNIT. 2 L 7 2 4F 4 F RT A1NM E24NE 2001052100021 20010521 00021 NM 2001 5 21 2001UALA00391 1 20010315 A 4970 38762121 SENSOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE APU FAILED A UALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION NR NOT REPORTED 1 WP 29 794UA 26953 LOST LEFT ENGINE GENERATOR AFTER DEPARTURE FROM FRA. AFTER DISCUSSION WITH MAINTENANCE, FLIGHT CONTINUED WITH APU RUNNI NG UNTIL APU SHUTDOWN. DIVERTED TO LHR WHERE OVERWEIGHT LANDING WAS MADE. AN OVER SPEED FAULT WAS DETECTED CAUSING AN A UTOMATIC SHUTDOWN OF THE APU. LINE MAINTENANCE ACCOMPLISHED FIM TASK 49-60-812. THE SPEED SENSOR CONNECTOR WAS CLEANED AND REINSTALLED. APU OPERATED NORMAL. HOWEVER, ACARS STILL DETECTED A FAULT COMING FROM THE SENSOR. ENGINEERING REQ UESTED THE SENSOR TO BE REPLACED. AFTER THE REPLACEMENT OF THE PART, FAULTS WERE STILL BEING DETECTED. THEREFORE, ANOT HER SENSOR REPLACEMENT WAS REQUESTED. THE SECOND SENSOR WAS ABLE TO FIX THE FAULTS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001041600428 20010416 00428 NM 2001 4 16 2001UALA00393 1 20010403 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 BS 178 BULKHEAD RT LOWER WEATHER RADAR ANTENNA MOUNT HAS THREE CRACKS. REPAIRED CRACKED WEATHER RADAR ANTENNA MOUNT. M AJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600429 20010416 00429 NM 2001 4 16 2001UALA00394 1 20010402 A 5330 SKIN BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 989UA 21751 RT FUSELAGE HAS EXISTING INTERIM REPAIR FROM BS 178 TO BS 191 AND FROM WL 190 TO WL 199. ACCOMPLISHED FINAL REPAIR. MA JOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F A16WE E2EA 2001041600430 20010416 00430 NM 2001 4 16 2001UALA00395 1 20010402 A 5330 SKIN BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 989UA 21751 LT FUSELAGE HAS EXISTING INTERIM REPAIR FROM BS 178 TO BS 191 AND FROM WL 190 TO WL 199. ACCOMPLISHED FINAL REPAIR. MA JOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F A16WE E2EA 2001041600431 20010416 00431 NM 2001 4 16 2001UALA00396 1 20010403 A 5743 FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE MLG DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 RT WING UPPER CHORD AND MAIN LANDING GEAR FITTING CRACKED. INSTALLED DOUBLER AND BOLTS. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600432 20010416 00432 NM 2001 4 16 2001UALA00397 1 20010403 A 5743 FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT WING DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 LT WING MAIN LANDING GEAR BEAM FITTING CRACKED. INSTALLED DOUBLER AND BOLTS. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600433 20010416 00433 NM 2001 4 16 2001UALA00398 1 20010403 A 5210 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE PAX DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 EXTERIOR DOOR HAS NUMEROUS DENTS. REPLACED EXTERIOR SKIN. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001042400198 20010424 00198 NM 2001 4 24 2001UALA00399 1 20010403 A 5315 141W8517 FLOORBEAM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUSLEAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 770UA 23920 0 26925 STA 246: FLOORBEAM UPPER WEB IS CRACKED AT RBL 8.5& 38.5. FLOORBEAM MID CHORD UPPER RADIUS IS CRACKED RBL 9,25,50 & LB L 8. FLOORBEAM MID CHORD IS CRKED RBL 38.5. FLOORBEAM MID CHORD UPPRER RADIUS IS CRKED RBL 44. CRKED STIFFNER AT FLOORBE AM RBL & LBL AT 26.06 FLR BM FWD VERT STIFFNER CRKED LBL38.5. FLOORBEAM AT LBL & RBL 7.88 BUCKLED STIFFNERS. SUPPLEMEN TAL DATA UPDATE REPLACED STIFFENERS PER SRM 53-10-51, REPAIR 3. REPAIRED WEBS PER EVA E97-0254A. REPAIRED MID-CHORD PER SRM 53-10-51, REPAIR 1 & 2. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001043000013 20010430 00013 NM 2001 4 30 2001UALA00400 1 20010403 A 4990 38760592 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU OIL SYSTEM FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 588UA 26717 APU OIL QUANTITY STATUS MESSAGE ILLUMINATED. RIGHT GENERATOR PREVIOUSLY DEFERRED. SUPPLEMENTAL DATA UPDATE ACCOMPLISHED APU OIL CONSUMPTION CHECK. APU WAS CHECKED ONCE FOR OIL CONSUMPTION AND EXTERNAL OIL LEAKS, AND NO DISCREPANCIES WERE F OUND. SUSPECT THE OIL LEVEL SWITCH TO BE GIVING ERRONEOUS INDICATION. REPLACED OIL LEVEL SWITCH. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600434 20010416 00434 EU 2001 4 16 2001UALA00401 1 20010403 A 3250 711TS06Y CONTROLLER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NLG STEERING FAILED A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 470UA 73 0 1427 LOST NOSE WHEEL STEERING AND BRAKING CONTROL. SUPPLEMENTAL DATA UPDATE REPLACED CAPTAINS STEERING TILLER. OPS CHECKS OK . 2 L 7 2 4F 4 F RT A28NM E40NE 2001041600435 20010416 00435 NM 2001 4 16 2001UALA00402 1 20010404 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 FORWARD PIT BS 500 FRAME CRACKED BETWEEN STRINGER 20R AND 21R. REPAIRED CRACKED FRAME. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600436 20010416 00436 NM 2001 4 16 2001UALA00404 1 20010331 A 6310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 AFT BULKPIT AT STA. 1417 BETWEEN STRINGERS 37L AND 38L SHEAR TIE IS CORRODED. MAJOR REPAIR ACCOMPLISHEDFABRICATED NEW S HEAR TIE PER BOEING DWG 140T2102. INSTALLED PER SRM 51-20-01. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041600437 20010416 00437 NM 2001 4 16 2001UALA00405 1 20010331 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 AFT PIT AT STA. 1395 STRINGERS 38L & 39L SHEAR TIE IS CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE PER BOEIN G DWG 140T2102 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041600438 20010416 00438 NM 2001 4 16 2001UALA00406 1 20010331 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 AFT PIT STA. 1219 FLOOR FRAME T-CAP HAS AREAS OF CORROSION FROM BL0 - LBL 46 ON UPPER AND LOWER FLANGES. MAJOR REPAIR A CCOMPLISHED. REPLACED UPPER T-CAP PER BOEING DWG 146T1060 AND SRM 51-40-01. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041600439 20010416 00439 NM 2001 4 16 2001UALA00407 1 20010331 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 AFT CARGO PIT AT STA. 1065 - 1087 STRINGER 33L IS CRACKED UNDER END FITTING RADIUS. MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW SECTION OF STRINGER PER SRM 51-20-01 AND SRM 53-00-03. TYPE II STRINGER AND HAT CHANNEL. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041600440 20010416 00440 NM 2001 4 16 2001UALA00408 1 20010331 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 FORWARD PIT STRINGER 37R BETWEEN STA. 412 AND 434 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER SPLICE SRM 53-10-03 FIGURE 201, BOEING DWG 140T0115. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041600441 20010416 00441 NM 2001 4 16 2001UALA00409 1 20010331 A 5320 SPLICE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 FORWARD PIT STA. 434 STRINGER 35R SPLICE HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SPLICE PER SRM 51-40-0 2 AND BOEING DWG 140T0115. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000014 20010430 00014 EU 2001 4 30 2001UALA00411 1 20010404 A 3040 HEATER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LT WINDSHIELD ARCED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 444UA 11150 824 LEFT WINDSHIELD HEAT STARTED ARCING ON DESCENT. SUPPLEMENTAL DATA UPDATE INSTALLED NEW LEFT WINDSHIELD. HEAT OPS CHECKE D GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2001061800006 20010618 00006 EU 2001 6 18 2001UALA00412 1 20010404 A 3510 MF100511 OXYGEN MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT LEAKING A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 453UA 1001 FLIGHT DECK LOW OXYGEN PRESSURE. *S/D* REMOVED CREW FULL FACE OXYGEN MASK (WITH SECONDARY REGULATOR) AND REPLACED. AL SO REMOVED AND REPLACED THE STOWAGE BOX. 2 L 7 2 4F 4 F RT A28NM E40NE 2001041600443 20010416 00443 NM 2001 4 16 2001UALA00413 1 20010404 A 5320 STIFFENER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BULKHEAD CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 STA 178 BULKHEAD BL 5.7 VERTICAL STIFFENER FORWARD CHORD IS CRACKED. REPAIRED CRACKED CHORD. MAJOR REPAIR ACCOMPLISHED . 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600444 20010416 00444 NM 2001 4 16 2001UALA00414 1 20010404 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 STA 178 BULKHEAD WEB CRACKED AT THE UPPER LT RADAR MOUNT LBL 5.9. REPAIRED CRACKED WEB. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600445 20010416 00445 NM 2001 4 16 2001UALA00415 1 20010404 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE MISDRILLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 312UA 23673 STA 480 FLOORBEAM RBL 50 - 60 HAS INCORRECT RIVET PATTERN. REPAIRED STA 480 FLOORBEAM. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600446 20010416 00446 NM 2001 4 16 2001UALA00416 1 20010404 A 3350 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 383UA 24658 EMERGENCY EXIT LIGHTING IS INOPERATIVE FROM ROW 12 THROUGH ROW 18. FOUND SIDEWALL TO EMERGENCY EXIT LIGHTING FEEDER STR IP DAMAGED. REPLACED THE FEEDER STRIP. OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2001070600042 20010706 00042 NM 2001 7 6 2001UALA00417 1 20010403 A 5210 258T11265 DOOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE AFT ENTRY STUCK A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 645UA 25280 UNABLE TO OPEN LEFT REAR ENTRY DOOR. *S/D* FOUND PAWL ON DOOR ASSIST REEL WHICH IS A SUBASSEMBLY OF COUNTERBALANCE ASS EMBLY ENGAGED. DISENGAGED PAWL AND OPERATIONAL CHECK PROVIDED SATISFACTORY SYSTEM OPERATION. 2 L 7 2 4F 4 F RT A1NM E24NE 2001041600447 20010416 00447 NM 2001 4 16 2001UALA00418 1 20010331 A 5313 STRINGER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7297U 21892 STRINGER 22R AT STA 336 HAS DENT DAMAGE BEYOND ALLOWABLE LIMITS OF SRM 53-10-01. SUPPLEMENTAL DATA UPDATE INSTALLED STR INGER REPAIR PER SRM 53-10-03 FIGURE 1. MAJOR REPAIR ACCOMPLISHED. 2 L 7 3 4F 4 F A3WE E2EA 2001071100021 20010711 00021 NM 2001 7 11 2001UALA00419 1 20010403 A 2550 PDU BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CARGO BAY SHORTED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 654UA 25392 AFT CARGO COMPARTMENT DRIVE 6R HAS POWER CABLE FRAYED WIRES AND WAS SMOKING. *S/D* CAPPED CIRCUIT BREAKER, C159 PER WD , REPLACED PDU PER MM. CHECK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2001071100022 20010711 00022 NM 2001 7 11 2001UALA00420 1 20010404 A 2913 326879210 PUMP BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE HYDRAULIC SYS FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 666UA 29238 ON GEAR RETRACTION DURING T/O FROM OGG, AIR DEMAND PUMP LOW PRESS LIGHT CAME ON. DIVERTED TO HNL. *S/D* REPLACED AIR DRIVEN PUMP. 2 L 7 2 4F 4 F RT A1NM E24NE 2001041600448 20010416 00448 NM 2001 4 16 2001UALA00421 1 20010405 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 FUSELAGE SKIN DENTED AT BS 650 JUST BELOW FLOORLINE STRINGER 17L. INSTALLED DOUBLER PER SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600449 20010416 00449 NM 2001 4 16 2001UALA00422 1 20010402 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 DENT IN FUSELAGE SKIN 42 INCHES AFT OF DOOR 2L, STRINGER 16L. INSTALLED DOUBLER AND REPAIRED STRINGER 16L BS 770-780 PE R SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600450 20010416 00450 NM 2001 4 16 2001UALA00423 1 20010405 A 5312 BULKHEAD BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 917UA 25384 STA 178 BULKHEAD CRACKED AT THE INBOARD LOWER SIDE OF THE WEATHER RADAR ANTENNA MOUNT LBL 5.7 WL 200. REPAIRED CRACKED WEATHER RADAR ANTENNA MOUNT. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600451 20010416 00451 NE 2001 4 16 2001UALA00424 2 20010405 A 7230 BLADE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 1 COMPRESSOR FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 398UA 24673 721713 NR 1 ENGINE COMPRESSOR STALL. SUPPLEMENTAL DATA UPDATE BORESCOPE INSPECTION REVEALED 7TH STAGE HIGH PRESSURE COMPRESSOR BLADE DAMAGE BEYOND LIMITS. THE ENGINE WAS REMOVED AND IS BEING SENT TO THE SHOP FOR TEARDOWN AND FURTHER ANALYSIS. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600452 20010416 00452 NM 2001 4 16 2001UALA00425 1 20010405 A 5743 FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT MLG CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 THE LEFT MLG SUPPORT BEAM OUTBOARD SUPPORT FITTING IS CRACKED. SUPPLEMENTAL DATA UPDATE INSTALLED DOUBLER AND BOLTS. MA JOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600453 20010416 00453 NM 2001 4 16 2001UALA00426 1 20010405 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 LT FUSELAGE DENTED AT STA 989 STRINGER 14L. REPAIRED STRINGER 14L. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600454 20010416 00454 NM 2001 4 16 2001UALA00427 1 20010404 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 CORROSION IN SHEAR TIE UNDER FRAME STA. 654 BETWEEN STRINGERS 39L AND 37R. MAJOR REPAIR ACCOMPLISHEDFABRICATED AND INST ALLED SHEAR TIE IN ACCORDANCE WITH B767 DRAWING 140T2103 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041600455 20010416 00455 NM 2001 4 16 2001UALA00428 1 20010404 A 5311 FRAME BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7297U 21892 FUSELAGE FRAME BS 783 RT HAS A CRACK AT FIRST HOLE BELOW CABIN FLOOR LINE. INSTALLED DOUBLER AND ANGLE REPAIR PER SRM 53-11-05 AND MM 53-11-08. MAJOR REPAIR ACCOMPLISHED. 2 L 7 3 4F 4 F A3WE E2EA 2001041600456 20010416 00456 NM 2001 4 16 2001UALA00429 1 20010404 A 2842 SENSOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUEL QUANTITY FAILED A UALA O OTHER N FALSE WARNING CL CLIMB 1 WP 29 7278U 21425 DURING CLIMB FUEL QUANTITY INDICATION WAS ERRATIC DURING FUEL TRANSFER FROM THE NR 1 FUEL TANK. SUPPLEMENTAL DATA UPDATE . REPLACED INDICATOR. 2 L 7 3 4F 4 F A3WE E2EA 2001050300320 20010503 00320 NM 2001 5 3 2001UALA00430 1 20010405 A 2131 CONTROLLER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN PRESSURE FAILED A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 7442U 21896 DURING DESCENT CABIN PRESSURE WAS ERRATIC. SUPPLEMENTAL DATA UPDATE SUSPECT CABIN PRESSURE CONTROLLER FAILED. REPLACED CABIN PRESSURE CONTROLLER. 2 L 7 3 4F 4 F A3WE E2EA 2001041600457 20010416 00457 CE 2001 4 16 CA010402002 1 20010314 A 3230 KP16BS BEARING BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA HARTZL HCB3T HCB3TN3 GL MLG CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING ROUTINE INSPECTION IT WAS NOTICED THAT THE LANDING GEAR WAS SLOW TO RETRACT. UPON FURTHER INSPECTION THE B EARING SUPPORTING THE RT DRIVE SHAFT WAS FOUND CORRODED AND STIFF. THIS BEARING ALSO CAUSED THE GEAR MOTOR TO BECOME WE AK AND NEEDED TO BE REPLACED. THIS AIRCRAFT IS NOT BEING OPERATED IN A CORROSIVE ENVIRONMENT BUT AT ONE TIME IT WAS AND THIS MAY BE THE CAUSE OF THIS. 1 L 7 2 3T 4 T A14CE E4EA 6 C P15EA 2001041600461 20010416 00461 SO 2001 4 16 CA010402009 1 20010313 A 3242 16403906 DISK PIPER PA31T PA31T 7103124 SO PWA PT6 PT6A28 EA RT MLG BRAKES CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) PROBLEM FOUND DURING INSPECTION. RT BRAKE FOUND CRACKED ALONG THE WEARING SURFACE. 1 L 7 2 3T 4 T A8EA E4EA 2001041600462 20010416 00462 WP 2001 4 16 CA010402010 1 20010301 A 3320 1502643 LIGHT LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE CABIN CEILING SHORTED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) AFT LOWR GALLEY CEILING LIGHT SHORT OUT (FIRST LIGHT ASSY IN FRONT OF GALLEY LIFT) CAUSING SMELL OR SMOKE IN CABIN . 2 L 7 3 4F 4 F A23WE E12EU 2001041600463 20010416 00463 WP 2001 4 16 CA010402011 1 20010228 A 2820 96851103 FUEL LINE LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE NR 2 ENGINE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) STEEL BRAIDED FLEX FUEL SUPPLY LINE, NR 2 ENGINE & APU, IN HYDRAULIC SERVICE CENTER COMPARTMENT LEAKING APPROXIMAT ELY 3 FEET FROM FORWARD END DUE TO INTERNAL RUPTURE. FUEL LINE IS UNDER INVESTIGATION BY ENGINEERING DEPARTMENT TO DETER MINE THE CAUSE. 2 L 7 3 4F 4 F A23WE E12EU 2001041600464 20010416 00464 WP 2001 4 16 CA010402012 1 20010303 A 3260 801813 PROXIMITY SENSOR LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21122B02 54555 NE LT MLG FAULTY W O OTHER N FALSE WARNING AP APPROACH 1 CA (CAN) DURING APPROACH AT YMX, NO GREEN LIGHT ILLUMINATE ON LT MLG DOWN & LOCK, PROXIMITY SENSOR AT FAULT, R&R C/OUT, GEA R WING C/OUT, CHECK SERVICEABLE. 2 L 7 3 4F 4 F A23WE E12EU 2001041600465 20010416 00465 NM 2001 4 16 CA010402013 1 20010303 A 3241 39617 VALVE BOEING 757 75723A 1384967 NM RROYCE RB211 RB211535E437 54555 NE RT ANTISKID SYS CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) R/H HYDRAULIC QUANTITY DECREASING DURING LAST MINUTE OF FLIGHT. FOUND DURING WALKAROUND, RT ANTI-SKID MODULE VALVE V35 IN WHEEL WELL CRACKED, VALVE REPLACED, LEAK CHECK CUT OUT AND ACFT BACK TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2001041600470 20010416 00470 NM 2001 4 16 CA010403010 1 20010219 A 5753 BACB10B131 BEARING BOEING 737 737242C 1384478 NM PWA JT8 JT8D9A 52048 NE RT FLAP BROKEN W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) DURING TAXI, FLAPS SELECTED WITH INDICATION PROBLEM. AIRCRAFT RETURNED TO GATE. FURTHER INVESTIGATION FOUND RT FLA P CARRIAGE BEARINGS WAS BROKEN IN 2 PIECES AND A SECOND BEARING SPLIT. NEW PARTS INSTALLED AND FLAP RIGGING CARRIED OUT I.A.W. MM. NO FURTHER INCIDENT DURING SUBSEQUENT FLIGHT. 2 L 7 2 4F 4 F A16WE E2EA 2001041600473 20010416 00473 NM 2001 4 16 UPS01235554 1 20010326 A 5711 SPAR BOEING 727 72731C 1384011 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C & SI, CRACK ON REAR SPAR WEB AT APPROX LBBL 16 AT TOP CORNER OF CUTOUT FOR ACCESS PANEL WEB REPA IR CARRIED OUT IAW SRM 51-40-2 FIG 1 2 L 7 3 4F A3WE 2001041600474 20010416 00474 NM 2001 4 16 UPS01235555 1 20010326 A 5320 SPLICE BOEING 727 72731C 1384011 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C & SI, SPLICE PLATE AT RBBL 70.5 UPPER & BS 870 CRACKED REPAIR CARRIED OUT IAW SRM 51-30-2 2 L 7 3 4F A3WE 2001041600475 20010416 00475 NM 2001 4 16 UPS01235556 1 20010320 A 5310 STRUCTURE BOEING 727 72731C 1384011 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C & SI, LT BS 910 CRACKED MRR FILED AS OPEN AWAITING LOG PAGE. CRACK REPAIRED IAW EO B727-5310-1896-B 2 L 7 3 4F A3WE 2001041600476 20010416 00476 NM 2001 4 16 UPS01235557 1 20010322 A 5753 FLAP TRACK BOEING 727 72731C 1384011 NM NR 5 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C & SI, NR 5 FLAP TRACK FWD ATTACH LUG CORRODED. REPLACED #5 FLAP TRACK FWD ATTACH LUG IAW DRG 65-2165 1 2 L 7 3 4F A3WE 2001041600477 20010416 00477 NM 2001 4 16 UPS01235558 1 20010322 A 5711 SPAR BOEING 727 72731C 1384011 NM CENTER WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C&SI SEVERAL RIVET HEADS POPPED ON THE CENTER SECTION REAR SPAR UPR CHORD & VERT. WEB AT LBL 37 LBL 17 . REPAIR CARRIED OUT IAW SRM 51-30-2 & SRM 51-30-01 2 L 7 3 4F A3WE 2001041600478 20010416 00478 NM 2001 4 16 UPS01235559 1 20010327 A 5530 HINGE BOEING 727 72731C 1384011 NM RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C & SI, UPPER RUDDER HINGE SUPPORT FITTING IN VERT STAB HAS SUSPECT CRACK AL ONG LH FLANGE AT FWD END. REPLACED RUDDER HINGE SUPPORT FITTING IAW SMRO EO 2001-010-003 UPS ENGINEERING FILE 727-27-20001 2 L 7 3 4F A3WE 2001041600479 20010416 00479 NM 2001 4 16 UPS01235560 1 20010321 A 5753 ATTACH FITTING BOEING 727 72731C 1384011 NM LT WING TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C & SI, NR 1 FLAP TRACK FWD ATTACH LUG HAS SURFACE CORROSION ON THE LUG I/B FACE, REPAIR CARRIED OUT I AW SMRO EO 2001-010-005 UPS ENGINEERING FILE 727-32-20001 2 L 7 3 4F A3WE 2001041600480 20010416 00480 NM 2001 4 16 UPS01235565 1 20010328 A 5710 PANEL BOEING 727 72731C 1384011 NM WS 270 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C & SI, RT WING & NR 1 FUEL PANEL HAS LIGHT SURFACE CORROSION ON LWR SURFACE, PANEL REPLACED IAW MM 28- 11-21 2 L 7 3 4F A3WE 2001041600481 20010416 00481 NM 2001 4 16 UPS01235566 1 20010321 A 5753 CARRIAGE BOEING 727 72731C 1384011 NM NR 8 FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C & SI, NR 8 FLAP CARRIAGE HAS CORROSION INSIDE SPINDLE BORE. CARRIAGE ASSY REPLACED IAW MM 27-51-13 2 L 7 3 4F A3WE 2001041600482 20010416 00482 NM 2001 4 16 UPS01235567 1 20010321 A 5753 CARRIAGE BOEING 727 72731C 1384011 NM NR 5 TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C & SI, NR 5 FLAP CARRIAGE HAS CORROSION INSIDE BORE OF SPINDLE. CARRIAGE REPLACED IAW OHM 57-58-02 2 L 7 3 4F A3WE 2001041600483 20010416 00483 NM 2001 4 16 UPS01235568 1 20010321 A 5753 CARRIAGE BOEING 727 72731C 1384011 NM NR 4 FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C & SI, NR 4 FLAP CARRIAGE HAS HEAVY SURFACE CORROSION INSIDE SPINDLE BORE. CARRIAGE ASSY REPLACED IA W MM 27-51-01 & OHM 57-58-02 2 L 7 3 4F A3WE 2001041600484 20010416 00484 NM 2001 4 16 UPS01235569 1 20010321 A 5753 PAD BOEING 727 72731C 1384011 NM NR 4 FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C & SI, NR 4 FLAP TRACK AFT MOUNT PAD, HEAVY SURFACE CORROSION ON PAD. CORROSION REMOVED FROM AFT MOUNT PAD WITHIN LIMITS IAW OHM 57-40-01 2 L 7 3 4F A3WE 2001041600485 20010416 00485 NM 2001 4 16 UPS01235570 1 20010321 A 5753 PAD BOEING 727 72731C 1384011 NM NR 5 FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C & SI, NR 5 FLAP TRACK, AFT MOUNT PAD HAS SURFACE CORROSION ON PAD SURFACE. REPAIR CARRIED OUT IAW UP S EO B727-5742-0651 2 L 7 3 4F A3WE 2001041600486 20010416 00486 NM 2001 4 16 UPS01235571 1 20010406 A 5330 SKIN BOEING 727 72731C 1384011 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C & SI, CORROSION ON LOWER SKIN & ON INTERNAL DOUBLER BS 1183 -1110 BETWEEN S20R & 21R REPAIR CARR IED OUT IAW SRM 51-10-6 & 53-30-3 2 L 7 3 4F A3WE 2001041600487 20010416 00487 NM 2001 4 16 UPS01235572 1 20010320 A 3270 CYLINDER BOEING 727 72731C 1384011 NM TAIL SKID CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C & SI, TAIL SKID CYLINDER HAS CORROSION ON OUTER SURFACE BELOW MID CLAMP. TAIL SKID CYLINDER REPLACED IAW MM 32-71-22 2 L 7 3 4F A3WE 2001041600488 20010416 00488 NM 2001 4 16 UPS01235573 1 20010402 A 5320 STIFFENER BOEING 727 72731C 1384011 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C & SI, LT MLG AFT BULKHEAD STIFFENER CRACKED AT LBL 45 APPROX. REPAIRED IAW SRM 51-40-3 2 L 7 3 4F A3WE 2001041600489 20010416 00489 NM 2001 4 16 UPS01235574 1 20010324 A 5320 STIFFENER BOEING 727 72731C 1384011 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C & SI, SUSPECT CRACK IN STIFFENER ON NOSE WW CEILING BL 0 BS 340. NEW STIFFENER INSTALLED IAW PRODUC TION DRWQING 65-18417 2 L 7 3 4F A3WE 2001041600490 20010416 00490 NM 2001 4 16 UPS01235575 1 20010327 A 5320 STIFFENER BOEING 727 72731C 1384011 NM BULKHEAD CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C & SI, SUSPECT CRACK IN RTH OB VERTICAL STIFFENER AFT PRESSURE BULKHEAD. REPAIR CARRIED OUT IAW UPS EO B727-5310-1109-E & UPS DRG. 66C33724 2 L 7 3 4F A3WE 2001041600491 20010416 00491 NM 2001 4 16 UPS01435563 1 20010413 A 2450 CONNECTOR BOEING 727 727* NM PDU SHORTED A IPXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 521UP 21944 21944 DURING GROUND LOADING OPERATIONS SMOKE WAS REPORTED COMING FROM 19L1 SMART WHEEL. MAINT REPORTED FINDING 19L1 PDU AND AS SOC WIRING SMOKING AT THIS POS. ELECTRICAL CONNECTOR WAS REMOVED AND STOWED C/B WAS PULLED AND COLLARED BY PVG MECH HE UN.THIS ITEM WAS PLACED ON DEFERRAL D213295. 2 L 7 3 4F RT A3WE 2001041600492 20010416 00492 WP 2001 4 16 MWEA010557 1 20010410 A 5532 591213011 SKIN DOUG DC9 DC932 3022066 WP VERTICAL STAB CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 VERTICAL STABILIZER SKIN JUST AFT OF LEFT LEADING EDGE SIDE ROLLER TRACK HAS A CHAFE MARK. FABRICATED AND INSTALLED HO RIZONTAL STAB CUTOUT PANEL. 2 L 7 2 4F A6WE 2001041600493 20010416 00493 WP 2001 4 16 MWEA010567 1 20010411 A 5220 59139311 HANDLE DOUG DC9 DC932 3022066 WP OVERWING EXIT INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 LEFT FORWARD OVERWING EXIT DOOR HAS A HANDLE THAT OPENS INTERMITTENLY. -- REMOVED AND REPLACED HOUSING ASSEMBLY. 2 L 7 2 4F A6WE 2001041600494 20010416 00494 WP 2001 4 16 MWEA010569 1 20010411 A 5711 59113073 SPAR DOUG DC9 DC932 3022066 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 LEFT WING INTERNAL, 4 AREAS OF LIGHT CORROSION ON BOTTOM HORIZONTAL LEG OF FORWARD SPAR FROM XCW 58 TO 12 INCHES OUTBOAR D OF XCW 58. -- BLENDED AREAS. AREAS ARE ACCEPTABLE FOR STRENGTH, IAW BOEING TELEX MWX-ORD-01-00147H DATE 21 FEB 01. 2 L 7 2 4F A6WE 2001041600495 20010416 00495 WP 2001 4 16 MWEA010570 1 20010411 A 5711 99193691 SPAR DOUG DC9 DC932 3022066 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 LEFT WING INTERNAL, LIGHT CORROSION ON XCW 58 TEE HORIZONTAL LEG BETWEEN STRINGER 12 AND 13. REMOVED CORROSION AND BLEN DED. BLENDOUTS ARE ACCEPTABLE FOR STRENGTH, IAW BOEING TELEX MWX-ORD-01-00171H DATED 2/28/01. 2 L 7 2 4F A6WE 2001041600496 20010416 00496 WP 2001 4 16 MWEA010571 1 20010411 A 5711 99193691 SPAR DOUG DC9 DC932 3022066 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 LEFT WING INTERNAL, LIGHT CORROSION ON XCW 58 TEE HORIZONTAL LEG BETWEEN STRINGER 15 AND 16. REMOVED CORROSION. BLEN DOUTS ARE ACCEPTABLE FOR STRENGTH, IAW BOEING TELEX MWX-ORD-01-00146H. 2 L 7 2 4F A6WE 2001041600497 20010416 00497 WP 2001 4 16 MWEA010572 1 20010411 A 5711 99193691 SPAR DOUG DC9 DC932 3022066 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 LIGHT CORROSION ON XCW 58 TEE LOWER SIDE JUST UNDER THE INBOARD FORWARD LOWER END OF STRINGER 22, LEFT WING INTERNAL. - - REMOVED CORROSION. BLEND OUT IS ACCEPTABLE FOR STRENGTH, IAW BOEING TELEX MWX-ORD-01-00146H. 2 L 7 2 4F A6WE 2001041600498 20010416 00498 WP 2001 4 16 MWEA010573 1 20010411 A 5743 5913663501 GUSSET DOUG DC9 DC932 3022066 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 LEFT TRUNNION LOWER GUSSET CORRODED, XRS 111. FABRICATED AND INSTALLED NEW GUSSET. 2 L 7 2 4F A6WE 2001041600499 20010416 00499 2001 4 16 MWEA010574 4 20010412 A 2350 F200211 SWITCH DOUG MD88 MD88 3023688 NM COCKPIT INOPERATIVE A MWEA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 GL 31 701ME 49760 CAPTAINS NR 1 COMM WAS INOPERATIVE AND THE MICROPHONE SWITCH WAS BROKEN. REMOVED AND REPLACED CAPTAINS PUSH TO TALK S WITCH. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A6WE 2001041600500 20010416 00500 WP 2001 4 16 MWEA010568 1 20010411 A 5347 3957317 CARGO TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FORWARD BAG PIT, CARGO TIE DOWN MOUNT FITTING AT STATION 365 BETWEEN LONGERON 30 AND LONGERON 29 RIGHT IS CORRODED. FA BRICATED AND INSTALLED FITTING. 2 L 7 2 4F A6WE 2001041600501 20010416 00501 EU 2001 4 16 MALA010395 1 20010319 A 3230 1175101 BOLT SAAB SF340 SF340A 7850100 EU MLG DEFECTIVE A MALA O OTHER P NO WARNING INDICATION LD LANDING 1 GL 15 103XJ 340A103 COMING INTO ROA FLIGHT 2779, GOT NO 3-GREEN INDICATOR LIGHT. THE CREW CALLED MAINTENANCE AND GOT OK FOR MANUAL EXTENSIO N AND RECIEVED 3-GREEN. LANDING GEAR WOULD NOT EXTEND EMERGENCY EXTENSION WAS NESSARY TO GET THE GEAR DOWN. AC WAS FERR IED GEAR DOWN DUE TO GEAR FAILURE. TO EXTEND IN NORMAL POSITION HAS TO USE EMERGENCY EXTENSION. AIR TURNBACK. MAINTENAN CE FOUND AC TO BE SAFE FOR A FERRY FLIGHT GEAR DOWN FORM ROA TO DTW. TIGHTEN LOOSE BACKSHELL CANNON PLUGS IN GEARWELL. REPLACED SEPERATION BOLTS LT, RT PN 117510-1 SN/OFF LT 1746, SN/ON 2436, SN/OFF RH 2434. BREAKAWAY WIRE EMG. HANDLE SWI NG GEARS 20 TIMES. ALL CHECK GOOD. 2 L 7 2 4T RT A52EU 2001041600502 20010416 00502 EU 2001 4 16 MALA010397 1 20010318 A 3020 FN24668057 NOZZLE SAAB SF340 SF340A 7850100 EU LT ENGINE DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 89XJ 089 ON FLIGHT 2797, LT INTAKE LIGHT ILLUMINATED IN FLIGHT. AIR TURNBACK TO BIS. REPLACED LT ENHAUST NOZZLE PN FN24668057, SN/ON L291478, SN/OFF L293501. REMAND REPLACED DE-ICE CONTROL UNIT PN 44730-501, SN/ON A00311, SN/OFF A00482. OPS AND S ECURITY CHECKS GOOD. 2 L 7 2 4T RT A52EU 2001041600503 20010416 00503 EU 2001 4 16 MALA010398 1 20010309 A 3040 MOTOR SAAB SF340 SF340A 7850100 EU WINDSHIELD WIPER FAILED A MALA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 GL 15 89XJ 089 DURING FLIGHT 3387, FIRST OFFICER WINDSHIELD WIPER WOULD NOT SHUT OFF IN FLIGHT, PULLED CIRCUIT BREAKER. MAINTENANCE REP LACED RT WINDSHIELD WIPER MOTOR RELAY (12ME). WITH SERVICEABLE UNIT. OPS CHECK GOOD AT THIS TIME. REMOVED FROM DMR, MAIN TENANCE NOTIFIED. 2 L 7 2 4T RT A52EU 2001041700001 20010417 00001 NM 2001 4 17 DHL2001740002 1 20010325 A 5751 DOUBLER BOEING 727 7272Q9 138448M NM LT WING AILERON LOOSE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 NR 19. LT WING TOP AILERON REPAIR IS COMING LOOSE FWD. AND INBD NR 7 SPOILER(DOT) RII CORRECTIVE ACTION: ACOMPLISHED REP AIR IAW AERONAUTICAL SOLUTIONS REPORT 00-003 IR 03-26-01 AND SRM 51-30-02.SEE ITEM 9M FOR REPLACEMENT INSTRUCTIONS. INTE RIM REPAIR INSTALLED TO WING SKIN PANEL,UPPER INBOARD L/H SIDE. THIS REPAIR MUST BE REPLACED WITH A PERMANENT REPAIR NO LATER THAN THE NEXT C CHECK APPROX JUNE 2002 (00-003 IR) TRANSFERED TO DMI 4888E OK PER GMM 3.5 A8A. PLACKARD. STATUS OPEN. 2 L 7 3 4F RT A3WE 2001041700003 20010417 00003 WP 2001 4 17 ASAA0180023 1 20010122 A 3350 60030451 LIGHT DOUG DC9 DC983 3022083 WP COCKPIT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 977AS 53453 LAX - DURING LINE CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHTS FOUND INOPERATIVE. REINSTALLED BATTERY PACK. EXIT LIGHTS OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001041700004 20010417 00004 NM 2001 4 17 ASAA0110011 1 20010109 A 5320 652072629 WEB BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND WEB CORRODED. REMOVED AND REPLACED WEB PER SRM. (M) 2 L 7 2 4F A16WE 2001041700006 20010417 00006 NM 2001 4 17 ASAA0140025 1 20010216 A 5320 654587545 SILL BOEING 737 7374Q8 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 778AS 25110 PAE - DURING SI CHECK, FOUND CORROSION ON MOPSILL. REPLACED MOPSILL IAW SRM. (M) 2 L 7 2 4F RT A16WE 2001041700007 20010417 00007 NM 2001 4 17 ASAA0140033 1 20010227 A 5310 6545815285 SHEAR TIE BOEING 737 7374Q8 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 778AS 25110 PAE - DURING SI CHECK, FOUND CORROSION ON SHEAR TIE AT STATION 767 TO WATERLINE 150 AND BUTT LINE 19. REMOVED AND REPLA CED SHEAR TIE IAW SRM. (M) 2 L 7 2 4F RT A16WE 2001041700009 20010417 00009 EU 2001 4 17 DHL2001367001 1 20010330 A 3610 CONNECTOR AIRBUS 300 A300B4203 3930306 EU NR 1 ENGINE OPEN A DHLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 367DH MSN265 REGULATOR FAULT NR 1 LIGHT ILLUMINATED. ABNORMAL PROCEDURES ACCOMPLISHED. REGULATOR FAULT REMAINED UNCORRECTED. HP MI IN-LINE, NO PRESSURE INDICATION. PLACED NR 1 ENGINE BLEED AIR SUPPLY SYS ON DMI 4944. MEL 36-11-01 S.P. 36-11-01. ACCO MPLISHED REG LOCKOUT. CORRECTIVE ACTION; DURING TROUBLESHOOTING, FOUND OPEN AT CONNECTOR 51HA TERMINAL B. REPAIRED SAM E IAW 20-53-00. PERFORMED OPERATIONAL TEST IAW 36-11-00 BLOCK 501. NO DEFECTS NOTED. THIS CLEARS DMI #4944. PLACARD REMOVED. STATUS - CLOSED. 2 L 7 2 4F RT A35EU 2001041700011 20010417 00011 SO 2001 4 17 20010411CW008 1 20010327 A 2421 ALU8521 ALTERNATOR PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540* 41533 EA ENGINE INOPERATIVE E WVBA O OTHER J WARNING INDICATION NR NOT REPORTED 1 AL 01 27755 53 317852148 PILOT REPORTED LEFT ALTERNATOR WARNING LIGHT ILLUMINATED AND COULD NOT RESET CIRCUIT BREAKER. UPON INSPECTION OF ALTERN ATOR, DISCOVERED THAT THE POSITIVE BATTERY LUG WAS LOOSE AND HAD CAUSED A SHORT TO THE CASE. THIS CAUSED BATTERY CABLE TO MELT AND TRIP BREAKER. ALTERNATOR AND CABLE END WERE REPLACED AND THE SYSTEM FUNCTIONALLY CHECKED SATISFACTORY. 1 L 7 2 3O 3 O A20SO E14EA 2001041700012 20010417 00012 CE 2001 4 17 20010411CW009 1 20010312 A 3230 95810017 MOTOR BEECH 36 A36 1151604 CE CONT O550 IO550* SO MLG FAILED E ML2R K NONE O OTHER IN INSP/MAINT 1 GL 11 497EB 93 E3296 PERFORMED NORMAL RETRACTION ON LANDING GEAR. GEAR RUN UP WITH NO DISCREPANCIES NOTED. SELECTED GEAR DOWN AND THE LANDI NG GEAR ACTURATOR WAS JAMMED IN THE UP POSITION AND THE LANDING GEAR MOTOR FAILED. ACTUATOR REQUIRED SEVERAL POUNDS OF FORCE TO HAND CRANK THE GEAR DOWN. SAFETY SWITCHES, AND DYNAMIC BRAKE RELAY WERE PREVIOUSLY FOUND TO BE RIGGED AND WORK ING CORRECTLY. 1 L 7 1 3O 3 O 3A15 E3SO 2001041700015 20010417 00015 WP 2001 4 17 20010411CW014 2 20010226 A 7310 8965471 TUBE BEECH 100 B100 1152919 CE GARRTT TPE331 TPE33110 01514 WP FUEL CONTROL DISCONNECTED E EGQA A UNSCHED LANDING K Y J FLUID LOSS ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 EA 17 105VY 5442 5442 BE109 P102225C DURING TAXI FOR TAKEOFF, THE RIGHT ENGINE EXPERIENCED AN UNCOMMANDED SHUTDOWN. AIRCRAFT WAS TAXIED BACK AND TURNED OVER TO MAINTENANCE. INSPECTION REVEALED THE P3 LINE DISCONNECTED AT THE FUEL CONTROL. THE LINE WAS RECONNECTED AND THE EN GINE GROUND RUN NORMALLY. THERE WAS NO SAFETY LOCKING FEATURE FOR THIS B NUT ON THE FUEL CONTROL. INADEQUATE TORQUE AT ENGINE BUILD SUSPECTED AS THE CAUSE. 1 L 7 2 4T 4 T A14CE E4WE 2001041700016 20010417 00016 EA 2001 4 17 20010406CW009 2 20010201 A 7314 PUMP PIPER PA31 PA31 7103102 SO LYC O540 O540* 41532 EA FUEL SYSTEM FAILED E DSFA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 25 430S 318252048 L270761A FUEL LEAK IN AREA OF FUEL PUMP ABOVE INJECTOR. CAUSED FIRE. HOSES WERE NOT REMOVED TO DETERMINE EXACT CAUSE. 1 L 7 2 3O 3 O A20SO E295 2001041700025 20010417 00025 EU 2001 4 17 CA010406003 1 20010315 A 3310 SD190470020 BALLAST FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU COCKPIT FAILED W G B A O2 MASK DEPLOYED EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA (CAN) PILOTS REPORTED THAT THEY NOTICED A TOXIC SMELL (ACRID ODOR) IN THE COCKPIT. OXYGEN MASKS WERE DONNED BY THE FLIGH T CREW AND AN EMERGENCY WAS DECLARED FOR PRIORITY LANDING. THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. THE CREW R EPORTS THE SMELL SEEMED TO BE COMING FROM THE OVERHEAD PANEL. THE AIRCRAFT WAS INSPECTED AND DEEMED SAFE FOR FERRY FLIGH T. AIRCRAFT CREW OXYGEN TOPPED UP AND THEN REPOSITIONED TO MAINTENANCE BASE. MAINTENANCE FOUND THE CENTRE RED FLARE SHIE LD LIGHT BALLAST TO BE A FAULT. THE BALLAST WAS REMOVED AND THE SYSTEM WAS MELD (33-02 - CAT.B). AIRCRAFT RETURNED TO SE RVICE WITH NO FURTHER INCIDENTS TO REPORT (MEL REMAINS IN AFFECT AT TIME OF WRITING SDR). 2 L 7 2 4F 4 F RT A20EU E2EU 2001041700026 20010417 00026 NM 2001 4 17 CA010406004 1 20010323 A 2120 65544709 DUCT BOEING 737 7372Q8 138448K NM PWA JT8 JT8D15 52051 NE A/C PACK BROKEN W O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CA (CAN) CREW REPORTED THAT THEY HAD A LOUD NOISE IN THE MID CABIN WHEN THE LEFT AIR CONDITIONING PACK WAS RUNNING. THEY AL SO NOTED THAT THE SMELL THAT WAS NOTICEABLE WHEN THE PACK WAS RUNNING. THE AIRCRAFT WAS REMOVED FROM SERVICE TO INVESTIG ATE THE CREW REPORT AND A FIBRE GLASS DUCT IN THE LEFT HAND MIX CHAMBER OF THE AIR CONDITIONING SYSTEM WAS FOUND TO HAVE A HOLE IN THE SIDE OF IT. THE DUCT WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2001041700027 20010417 00027 NM 2001 4 17 CA010406005 1 20010324 A 4900 87858101 CONNECTOR BOEING 737 737281 138448P NM PWA JT8 JT8D17 52049 NE APU DAMAGED W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA (CAN) THE AIRCRAFT WAS DEPARTING WHEN THE CREW EXPERIENCED AN APU FIRE INDICATION. THEY FOLLOWED PROCEDURES INCLUDING DI SCHARGING THE EXTINGUISHER BOTTLE THEN RETURNED TO BASE. THE APU WAS INSPECTED BY MAINTENANCE AND THERE WAS NO INDICATIO N OF FIRE DAMAGE. THE AIRCRAFT WAS DISPATCHED WITH THE APU ON MEL DUE TO THE DISCHARGED BOTTLE. AT THE NEXT AVAILABLE MA INTENANCE OPPORTUNITY, THE APU WAS INSPECTED AND REPAIRS MADE TO THE WIRING HARNESS ON THE APU BEFORE THE MEL WAS REMOVE D FROM THE AIRCRAFT.WIRE: P/N BMS 13-5515C1G18 2 L 7 2 4F 4 F A16WE E2EA 2001041700028 20010417 00028 CE 2001 4 17 CA010406006 1 20010323 A 5610 5042006934 WINDSHIELD BEECH 90 E90 1152914 CE PWA PT6 PT6A28 EA COCKPIT FAILED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA 3398 (CAN) TWENTY MINUTES OUT, LEVEL AT 21,000 FEET, RT WINDSHIELD SHATTERED. AIRCRAFT DESCENDED TO SAFE ALTITUDE, INNER PLY CONFIRMED FAILED. AIRCRAFT RETURNED TO BASE AT REDUCED SPEED AND PRESS DIFF. 1 L 7 2 3T 4 T 3A20 E4EA 2001041700030 20010417 00030 CE 2001 4 17 CA010406009 1 20010321 A 3260 1003810061 DOWNLOCK SWITCH BEECH 200 B200C 1152924 CE PWA PT6 PT6A42 52043 NE RT MLG INTERMITTENT W O OTHER N FALSE WARNING AP APPROACH 1 CA (CAN) ON FINAL APPROACH WHEN GEAR WAS SELECTED DOWN, RT GEAR LIGHT WOULD NOT COME ON. GEAR WAS SELECTED SEVERAL TIMES WI TH SOME RESULT. GO AROUND WAS UNDERTAKEN. RT GEAR WAS VISUALLY CHECKED IN THE DOWN POSITION AND ON THE NEXT APPROACH AIR CRAFT LANDED WITHOUT INCIDENT AND TAXIED TO THE HANGAR. RT MAIN GEAR DOWN LOCK SWITCH CONTACTS WERE FOUND TO HAVE FAILED . SWITCH WAS REPLACED, GEAR SWING COMPLETED AND CHECKED SERVICEABLE. 1 L 7 2 4T 4 T A24CE E4EA 2001041700033 20010417 00033 CE 2001 4 17 CA010406012 1 20010323 A 3234 LMD5001P RELAY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG SHORTED W O OTHER J WARNING INDICATION LD LANDING 1 CA 4799 (CAN) CREW REPORTED THAT LANDING GEAR FUNCTIONED NORMALLY BUT MOTOR WOULD NOT QUIT RUNNING. THE AIRCRAFT WAS FERRIED BAC K FOR REPAIRS. MAINTENANCE FOUND THE CONTROL RELAY STUCK (A SMACK PROVIDED THE INSPIRATION TO OPEN THE CONTACTS). THE RE LAY WAS REPLACED, THE GEAR SWUNG NUMEROUS TIMES AND THE AIRCRAFT RETURNED TO SERVICE. THIS RELAY IS LOCATED IN THE LEFT HAND TURTLE DECK OF THE 1900D, JUST AFT OF THE ENGINE COMPARTMENT. THE AREA IS PARTICULARLY HOSTILE FOR ELECTRICAL COMPO NENTS. 2 L 7 2 4T 4 T RT A24CE E26NE 2001041700035 20010417 00035 WP 2001 4 17 CA010406014 2 20010204 A 7250 31081251 TURBINE BLADES SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE ENGINE CRACKED W O OTHER E VIBRATION/BUFFET CR CRUISE 1 CA 2149 2149 (CAN) THIS ENGINE REMOVED FOR DIFFERENT REASON THAN HOT SECTION DAMAGE THAT FOUND LATER. DURING PREMATURE HOT SECTION I NSP ON ENGINE IT WAS FOUND THAT 6 CRACKS WERE FOUND ON 1ST STAGE TURBINE BLADES INITIATING FROM LEADING EDGE TIP CORNER & EXTENDING DOWN LEADING EDGE TOWARDS BLADE ROOT. EROSION CAN ALSO BE SEEN THROUGH PARENT MATERIAL. THESE BLADES DID NOT EVEN MAKE IT TO HOT SECTION INSP OF 3,500 HRS. IS NO LIFE ON THESE BLADES AT PRESENT. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 2001041700036 20010417 00036 EU 2001 4 17 CA010406015 1 20010403 A 2822 9688411404 PUMP PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL FUEL BOOST FAILED W O OTHER J WARNING INDICATION CR CRUISE 1 CA 690 690 (CAN) PILOT REPORTED FUEL BALANCING SYSTEM WAS NOT OPERATIONAL. BOOST PUMP REPLACED AND AIRCRAFT RETURNED TO SERVICE. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001041700038 20010417 00038 EU 2001 4 17 CA010409004 1 20010316 A 2434 9789601090 BRUSH HOLDER PILATS 5243212158 PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL STARTER GEN WORN W O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 CA 149 100318 (CAN) DURING CRUISE FLIGHT THE SECOND GENERATOR WENT OFF LINE, THE PILOT DID A RESET, THE GENERATOR CAME BACK ONLINE. AP PROXIMATELY FIVE MINUTES LATER IT WENT OFF LINE AGAIN. THIS TIME THE PILOT DID NOT TRY TO RESET. ONCE THE AIRCRAFT WAS B ACK ON THE GROUND THE PILOT TRYED A RESET ONCE MORE. HOWEVER, WAS NOT ABLE TO GET THE GENERATOR BACK ONLINE. THE BRUSH A SSY REPLACED, AND THE GENERATOR IS NOW SERVICEABLE. THIS GENERATOR HAD THE POST SB 24-016 BRUSHES. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001041700039 20010417 00039 2001 4 17 CA010409005 4 20010315 A 2215 KSA372 SERVO KING PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL AUTOPILOT FAILED W O OTHER P NO WARNING INDICATION AP APPROACH 1 CA 1886 4288 (CAN) AUTO PILOT WOULD FAIL TO CAPTURE THE HEADING BUG IN BOTH HEADING AND NAV MODE. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001041700040 20010417 00040 2001 4 17 CA010409006 4 20010320 A 3417 8800M ADC PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL E/E BAY FAILED W O OTHER J WARNING INDICATION CR CRUISE 1 CA 1572 (CAN) GPWS INOP WARNING LIGHT WOULD COME ON RANDOMLY IN FLIGHT. THE AIR DATA COMPUTER WAS REPLACED AND SOLVED THE PROBLE M. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001041700041 20010417 00041 2001 4 17 CA010409007 4 20010309 A 3418 9754421422 TRANSMITTER PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL AOA SYSTEM FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 1293 (CAN) WHILE PERFORMING A DAILY INSPECTION, THE VANE WAS FOUND CATCHING AT ONE SPOT, ROUGHNESS COULD BE HEARD INTERNALLY AND IT BECAME LOADED IN THE UP POSITION. ALHOUGH THE VANE WOULD STILL MOVE FREELY, A MANUFACTURER TECH. REP. ADVISED TO REPLACE THE TRANSMITTER. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001041700042 20010417 00042 EU 2001 4 17 CA010409008 1 20010309 A 2437 METER PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL VOLTAGE FAULTY W O OTHER N FALSE WARNING CR CRUISE 1 CA 1426 (CAN) PILOT REPORTED LOW VOLTAGE ON NR 2 BATTERY SYSTEM CHECKED AND IT WAS FOUND THE VOLT METER IN OVERHEAD ELECTRICAL P ANEL WAS AT FAULT. WE COULD NOT REPLACE JUST THE METER SO A PANEL WAS ORDERED AND REPLACED. THE OLD PANEL WHEN REMOVED W AS FOUND TO HAVE SOME BURNT MARKS ON IT BUT NO INDICATION OF FIRE OR HOT SPOTS AROUND THE AREA. THE CREWS HAD NOT REPORT ED SMELLING SMOKE IN THE COCKPIT. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001041700043 20010417 00043 EU 2001 4 17 CA010409009 1 20010309 A 5240 5711012353 STRUT PILATS 5711012141 PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL OIL COOLER DOOR BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 331 (CAN) THE SHOCK STRUT IS ACTUALLY AN ALUMINUM TUBE. THE SHOCK STRUT IS ATTACHEED TO THE FLAP STRUT WITH A STRAIGHT PIN. TWO SPRINGS KEEP THE FLAP DOOR CLOSED ALL THE TIME EXCEPT WHEN THE NLG IS DOWN. THE CONSTANT TENSION ON THE ALUMINUM SHO CK STRUT RESULTS IN PREMATURE WEAR AT THE HOLES. THE FAILRE OF THAT STRUT COULD LEAD TO HIGH OIL TEMERATURE ON THE GROUN D. THE FLAP STRUT END COULD POSSIBLY PIERCE THE SKIN WITH THE VIBRATION. THE PROBLEM RE-APPEARS EVERY 300-400 HOURS AFTE R THE PART IS REPLACED. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001041700063 20010417 00063 WP 2001 4 17 MWEA010580 1 20010413 A 3240 S1424 SWITCH DOUG DC9 DC932 3022066 WP PARKING BRAKE INOPERATIVE A MWEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 31 212ME 47701 TAKE OFF WARNING HORN CAME ON AT 105 KNOTS DURING TAKE OFF ROLL. ABORTED TAKE OFF. MAINTENANCE FOUND PARKING BRAKE SWIT CH INOPERATIVE AND REPLACED SWITCH. 2 L 7 2 4F A6WE 2001041700064 20010417 00064 NM 2001 4 17 MWEA010581 1 20010416 A 3340 5557 LIGHT DOUG MD88 MD88 3023688 NM NLG WW LOOSE A MWEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 31 810ME 48072 RIGHT NOSE WHEEL TAXI LIGHT RETAINING RING CAME LOOSE. -- RESECURED TAXI LIGHT. 2 L 7 2 4F RT A6WE 2001041700065 20010417 00065 EU 2001 4 17 MALA010400 1 20010411 A 2421 31342001 GENERATOR SAAB SF340 SF340A 7850100 EU LEFT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 109XJ 340A109 DURING FLIGHT 2932 LT AC GENERATOR LIGHT ILLUMINATED IN CRUISE, FOLLOWED ORH, LIGHT STAYED ON. AIR TURNBACK TO MSP. MA INTENANCE REPLACED LT AC GEN PN 31342-001, OPS CHECK NO GOOD. MAINTENANCE FOUND WIRE XA526-24, OPEN FROM LT GCU AND 139 VT. REPAIRED WIRE IN LT FLAP TRACK. OHM CHECK GOOD FROM GCU TO COCKPIT AC GENERATOR SWITCH, AND CHECKS GOOD OPEN TO GR OUND. OPS CHECK OF LT & RT AC GEN SYSTEM OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2001041700071 20010417 00071 EU 2001 4 17 MALA010401 1 20010411 A 2434 23020021 GENERATOR SAAB SF340 340B 7860101 EU RIGHT FAILED A MALA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 450XJ 450 RT GEN OVERTEMP AND RAMP PERSONNEL SHIGNALED SMOKE AND SPARKS FROM RIGHT SIDE ON FLIGHT 2747 OUT OF ATW. SHUTDOWN ENGIN E. MAINTENANCE REPLACED RT DC GENERATOR PN 23020-031 SN/ON 4307 SN/OFF 98275. OPS CHECK GOOD 2 L 7 2 4T RT A52EU 2001041700072 20010417 00072 NM 2001 4 17 UPS01235576 1 20010325 A 5312 PRESSURE PANEL BOEING 727 72731C 1384011 NM NLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C & SI, EVIDENCE OF CORROSION ON TOP PANEL NWW BS 312 RT, 2ND STIFFENER. REPAIR CARRIED OUT IAW SRM 51-30-2 & BOEING DRG. 65-18417 2 L 7 3 4F A3WE 2001041700073 20010417 00073 WP 2001 4 17 MWEA010576 1 20010416 A 5315 99154683 FLOORBEAM DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 CORROSION GOUGES AND ELONGATED HOLES ON RT LAV FLOORBEAMS AT STATION 996. FABRICATED AND INSTALLED FLOORBEAM ANGLE. 2 L 7 2 4F A6WE 2001041700079 20010417 00079 EU 2001 4 17 MALA010283 1 20010321 A 2435 23080031 STARTER GEN SAAB SF340 SF340A 7850100 EU RIGHT OVERTEMP A MALA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 GL 15 41XJ 041 ON FLIGHT 2723, AFTER START RT STARTER CAUGHT ON FIRE. BURNT COWLING. PILOT ACTUALLY PUT OUT FIRE USING HAND HELD EXTIN GUISHER. MAINTENANCE REPLACED STARTER GENERATOR DUE TO OVERTEMP P/N 23080-031, S/N OFF 3596, SN/ON 96075. IAW MEL TASK CARD 243103. OPS AND LEAK CHECK GOOD. CABLE EXTENDS APPEAR OVERTEMPED. NEEDS STARTER CABLE REPLACEMENT AND FIRE EXTIN GUISHER AT ROB 1C/D CABIN. SEE DISC 8 LOG PG 934734 FOR FERRY DISC. REMOVED AND REPLACED E-CABLES ENDS ON RT STARTER G EN. 2 L 7 2 4T RT A52EU 2001041700082 20010417 00082 EU 2001 4 17 MALA010284 1 20010321 A 3230 HP848430621 SELECTOR VALVE SAAB SF340 340B 7860101 EU MLG DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 GL 15 416XJ 416 ON FLIGHT 2861, WHILE ON APPROACH IN MSP THE GEAR DISCREPANCY LIGHT ILLUMINATED. AFTER GOING MISS APPROACH AND PERFORMI NG THE ORH, DISCOVERED THE F7 C/B WAS POPPED. LANDING CONTROL AFTER RESETTING IT WORKED FINE. MAINTENANCE REPLACED LAN DING GEAR SELECTOR VALVE P/N HP848430-621 S/N ON 1425, S/N OFF 0011. REF 409 CARD NR 088667 FOR DETAILS. 2 L 7 2 4T RT A52EU 2001041700090 20010417 00090 SW 2001 4 17 MV5R055N 1 20010313 A 3211 73005822 ANGLE GULSTM 690TP 690A 0141722 SW RT MLG CRACKED B MV5R K NONE O OTHER IN INSP/MAINT 1 GL 11 690TP 4552 11218 RIGHT MAIN LANDING GEAR INBOARD GEAR MOUNT SIDE BRACE TO WING ATTACHMENT ANGLE CRACKED. CRACK LOCATED AT THE AFT PORTIO N OF THE ANGLE EXTENDING ONE INCH FORWARD. 1 H 7 2 3T 2A4 2001041700091 20010417 00091 2001 4 17 20010413CW009 4 20010413 A 2210 439070202 RESISTOR CESSNA 414 414A 2075907 CE CONT O520 TSIO520* 17040 SO AUTOPILOT BROKEN B X0FR O OTHER O OTHER NR NOT REPORTED 1 WP 07 4838A 414A0102 AUTOPILOT WAS INOPERATIVE IN PITCH. THE PITCH RESISTOR WAS BROKEN CAUSING THE AUTOPILOT TO BE INOPERATIVE. THE PART IS ON THE CONTROL UNIT. 1 L 7 2 3O 3 O A7CE E8CE 2001041700094 20010417 00094 NM 2001 4 17 AWXA0001520 1 20010321 A 5753 658276415 SEAL BOEING 737 737277 1384570 NM PANEL MISINSTALLED A AWXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 28 188AW 22655 LT WING (WBL 92.5 - WBL 114) LWR INBOARD T/E PANEL BULB SEAL JUST INBOARD OF GEAR INSTALLED INCORRECTLY AND WRONG FASTEN ERS ARE CAUSING DAMAGE TO MLG SUPPORT BEAM. SUPPORT BEAM DAMAGED AREA BLENDED IAW SRM 57-20-1 FIG 5 - MAT LOSS .003; SE AL INSTALLATION CORRECTED IAW GENERAL MAINTENANCE PRACTICES. 2 L 7 2 4F RT A16WE 2001041700095 20010417 00095 NM 2001 4 17 AWXA0001529 1 20010321 A 5330 65458001329 SKIN BOEING 737 737277 1384570 NM FUSELAGE DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 22655 DENT IN FUSELAGE SKIN JUST FWD OF EQUIPMENT BAY DOOR AND AFT OF RADOME REQ''S TERMINATION REPAIR. AREA REPAIRED IAW SRM 53-30-3 FIG 6. 2 L 7 2 4F RT A16WE 2001041700106 20010417 00106 WP 2001 4 17 MWEA010361 1 20010322 A 5320 995791761 DOUBLER DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 AFT CARGO BAY FRAME U-CHANNEL DOUBLER HAS AREAS OF LIGHT CORROSION STATION 756, LONGERON 29-27 LEFT. BLENDED CORROSION, REMOVED, FABRICATED, LOCATED AND INSTALLED SPLICE. 2 L 7 2 4F A6WE 2001041700107 20010417 00107 WP 2001 4 17 MWEA010362 1 20010322 A 5320 99155714 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 800ME 45842 FASTENERS WITH NO SPACING OR EDGE DISTANCE ON DOUBLER INSIDE INTERCOSTAL AT LONGERON 9 RIGHT, BETWEEN STATION 237 AND 25 6. REMOVED AND FABRICATED INTERCOSTAL, FABRICATED DOUBLER AND PLATE, INSTALLED INTERCOSTAL, DOUBLER, AND PLATE. 2 L 7 2 4F A6WE 2001041700108 20010417 00108 NM 2001 4 17 DHL2001740001 1 20010323 A 3150 INDICATOR BOEING 727 7272Q9 138448M NM COCKPIT MALFUNCTIONED A DHLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 740DH 21930 S.O. ELEC. ANNUNCE. PANEL HAS OVEREXITED AND UNDEREXITED SYS. 1, LIGHTS ILLUMINATED WHEN RESET BUTTON IS PUSHED THE LIGH T EXTINGUISH AND THE LIGHT FOR NR 2 DIFF. FAULT LIGHT ILLUMINATES. WHEN RESET BUTTON IS RELEASED AND THE SAME NR 1 SYS. LIGHTS RE-ILLUMINATE LIGHTS DO SAME WITH GENERATOR ON OR OFF. CORRECTIVE ACTION; DEFERRED PER REF. MEL/CDL 24-12, CAT C. DMI 4848 ASSIGNED. PLACARD INSTALLED. STATUS OPEN. 2 L 7 3 4F RT A3WE 2001041700111 20010417 00111 SO 2001 4 17 C2XA01CL050 1 20010306 A 5610 WINDOW EMB 135 EMB135ER 3260203 SO COCKPIT LEAKING A C2XA E D ENGINE SHUTDOWN RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 16501 145145 CLE FLIGHT 3971 AFTER DEICING OF AIRCRAFT THE CREW REPORTED A HISS AND POP SOUND FOLLOWED BY SMOKE COMING FROM FIRST OFF ICER''S SIDE PANEL. THE ENGINES WERE SHUT DOWN AND ALL ELECTRICAL POWER WAS TURN OFF. MAINTENANCE INSPECTED AND FOUND DEICE FLUID HAD LEAKED THRU THE RIGHT SIDE WINDOW AND DOWN INTO THE TAT 2 SENSOR RELAY (KO494) AND THE PITOT STATIC SENS OR RELAY (KO054). THESE RELAY''S ARE BEHIND PANEL 224 ERW AND WERE FOUND TO BE BURNT. THE RELAYS WERE REPLACED ALONG W ITH THERE SOCKETS. MAINTENANCE ALSO COMPLIED WITH EA 2510-01030 SIDE CONSOLE PANEL AND STORM WINDOW SEALING IMPROVEMENT . ALL DEICE FLUID WAS REMOVED. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001041700122 20010417 00122 NM 2001 4 17 DHL2001702006 1 20010323 A 5230 NAS110626 BOLT BOEING 727 72730C 1384009 NM CARGO DOOR SHEARED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 MAIN CARGO DOOR WILL NOT CLOSE.CORRECTIVE ACTION: REPLACED SHEARED BOLTS AT FWD CAM LATCH PER MM 52-34-21. OPS CHECK G OOD. STATUS CLOSED. 2 L 7 3 4F A3WE 2001041700125 20010417 00125 NM 2001 4 17 0100962284 1 20010302 A 5730 SKIN BOEING 727 727251 138408H NM LT WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 284US 21323 DURING H-CHECK FOUND CRACK IN TWO FASTENER HOLES ON SKIN PANEL COMMON TO CHORD AT BS 760.95 AT LBL 70.5. REPAIRED PER E A 22-182198. 2 L 7 3 4F A3WE 2001041700127 20010417 00127 NM 2001 4 17 DLM11010365 1 20010304 A 3320 CONTROL PANEL DOUG MD11 MD11 3023602 NM CABIN FLOOR BURNED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 809DE 48480 FOUND WIRING HARNESS G013 DAMAGED WHILE TROUBLESHOOTING MCO C/NS C02271036 AND 333401016. NUMEROUS WIRES BURNED APROX 18 INCHES FROM P1-618 TO AFT ATTENDANT PANEL AT 4L DOOR. REPAIRED WIRES 141-22, 119-22, 114-20, 121-22, 97-22, 117-20, 23 -24, 1-22 AND 131-20 IAW M/M PROCEDURES.CONTROLS FROM AFT ATTENDANT PANEL NOW CHECK OK 2 L 7 3 4F RT A22WE 2001041700128 20010417 00128 NM 2001 4 17 DL73K010366 1 20010305 A 5310 65479592 DOOR FRAME BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 315DL 23087 C2 CARGO DOOR OPENING FORWARD FRAME WAS FOUND TO HAVE CRACKS IN THE UPPER FRAME BETWEEN STR 24R AND 26R. ADDITIONALLY, THE REINFORCEMENT STRAP WAS FOUDN CORRODED BETWEEN STR 24R AND 25R. THE FRAME WAS REPAIRED PER SRM 51-40-3 AND THE DAMAGED SECTION OF STRAP WAS REMOVED AND A NEW SECTION SPLICED IN. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001041700129 20010417 00129 NM 2001 4 17 DL72S010368 1 20010305 A 5330 65545839 SKIN BOEING 727 727225A 1384077 NM FUSELAGE PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8873Z 21291 THE FUSELAGE SKIN WAS PUNCTURED BY GROUND EQUIPMENT AT FS 1100 BETWEEN STRINGERS 19L & 20L. THE DAMAGE WAS REMOVE D WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUMDOUBLER INSTALLED PER ER/A 380183-14, REV A. 2 L 7 3 4F RT A3WE 2001041700139 20010417 00139 NM 2001 4 17 CA010404008 1 20010318 A 5610 WINDSHIELD BOEING 737 7372T5 NM PWA JT8 JT8D17 52049 NE COCKPIT LEAKING W A UNSCHED LANDING O OTHER CL CLIMB 1 CA (CAN) CLIMBING THROUGH 13,000 FEET, APPROXIMATELY 4 PSI CABIN PRESSURE, CAPTS WINDSHIELD POPPED WITH A NOTICEABLE PRESSU RIZATION LEAK. RETURNED. WINDOW INSPECTED, NO DEFECTS NOTED. WINDOW ATTACHED BOLTS WERE RETORQUED. AIRCRAFT PRESSURIZED TO 3 PSI, NO PRESSURIZATION LEAK NOTED. WINDOW RESEALED. 2 L 7 2 4F 4 F RT A16WE E2EA 2001041700140 20010417 00140 NM 2001 4 17 CA010404010 1 20010322 A 2710 654476112 CONTROL UNIT BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE AILERON LEAKING W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 48644 48644 (CAN) DURING FLIGHT A SYSTEM HYDRAULIC SYSTEM QUANTITY BEGAN TO DROP, AT A RATE OF 1 GALLON PER HOUR. DUE TO POOR WEATHE R ELECTED TO DIVERT. GEAR EXTENDED NORMALLY AND QUANTITY REMAINED STEADY. FLIGHT LANDED WITHOUT INCIDENT. FOUND A SYSTEM AILERON POWER CONTROL UNIT LEAKING. REPLACED PCU AS PER WORK CARD 51143. 2 L 7 2 4F 4 F A16WE E2EA 2001041700141 20010417 00141 NM 2001 4 17 CA010404011 1 20010202 A 5415 311T21592 FITTING BOEING 767 767375 NM GE CF6 CF680C2B6 30025 NE NR 2 PYLON CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 56995 56995 (CAN) DURING INSPECTION OF NR 2 RT PYLON, THE MIDSPAN FITTING FOUND CRACKED BETWEEN FASTENERS. NR 2 ENGINE REMOVED AS PE R WORK CRD 71125-2. NR 2 PYLON REMOVED AS PER WORK CARD 54102-2 FROM AIRCRAFT FOR REPAIR. NR 2 MIDSPAN FITTING RELACED A S PER ENGINEERING VARIANCE AUTHORIZATION 01-767-54-4020. PYLON REINSTALLED AS PER WORK CARD 54102-2. ENGINE REINSTALLED AS PER WORK CARD 71125-2. 2 L 7 2 4F 4 F RT A1NM E13NE 2001041700142 20010417 00142 EU 2001 4 17 CA010404014 1 20010316 A 2133 9599091121 OUTFLOW VALVE PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL CABIN PRESSURE FAILED W B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 2744 46A0090 (CAN) AIRCRAFT WAS REPORTED TO HAVE JUST REACHED CRUISING ALTITUDE AT FL 290. THE CABIN ALTITUDE WARNING LIGHT ON THE CA WS PANEL ILLUMINATED. THE CREW VERIFIED THAT THE CABIN ALTITUDE HAD CLIMBED TO ABOVE 10,700 FEET AND INITIATED AN EMERGE NCY DESCENT. THE AIRCRAFT RETURNED TO BASE. A TEST OF THE PRESSURIZATION CONTROL SYSTEM WAS PERFORMED BY MAINTENANCE. TH E TEST REQUIRES THE OUTFLOW VALVE TO FULLY CLOSE DURING A SEQUENCE OF EVENTS. THE VALVE FAILED TO CLOSE AS INDICATED IN THE PILATUS MAINTENANCE MANUAL, AND WAS SUBSEQUENTLY REPLACED.A GROUND TEST OF THE NEW VALVE, FOLLOWED BY A SATISFACTORY TEST FLIGHT AT 29,000 FEEET INDICATED THAT THERE WERE NO FURTHER PROBLEMS WITH THE PRESSURIZATION SYSTEM. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001041700144 20010417 00144 SO 2001 4 17 CA010405003 1 20010323 A 3246 16101900 WHEEL PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2B 41532 EA MLG CRACKED W O OTHER D INFLIGHT SEPARATION LD LANDING 1 CA (CAN) FLAT TIRE ON LANDING. FOUND INNER WHEEL HALF BROKEN. 1 L 7 2 3O 3 O A20SO E14EA 2001041700147 20010417 00147 GL 2001 4 17 20010411CW004 3 20010323 A 6110 106GAO COUNTERWEIGHT CESSNA 208 208B 2073701 CE PWA PT6 PT6A114 52043 NE MCAULY 3AF34C 3GFR34C703 GL PROPELLER DAMAGED E DEMA A UNSCHED LANDING E VIBRATION/BUFFET NR NOT REPORTED 1 CE 03 970FE 1812 1474 208B0093 17395 970514 AIRCRAFT ENCOUNTERED SEVERE VIBRATION ON CLIMB OUT. REQUESTED TO RETURN TO AIRPORT AND LANDED WITHOUT COMPLICATIONS. I NSPECTION OF VIBRATION FOUND THAT THE COUNTERWEIGHT FROM NR 2 PROP BLADE HAD COME LOOSE. INSPECTION SHOWED BOLT THAT HO LDS COUNTERWEIGHT HAD PULLED THREADS LOOSE FROM PROP BLADE SHANK. BOLT DID NOT BREAK LOOSE, STILL HAD TORQUE SEAL UNBRO KEN. BOLT DID NOT COME LOOSE. DAMAGE WAS DONE TO SPINNER AND WIRE HARNESS. PROBABLE CAUSE COULD HAVE BEEN BOLT TOO SH ORT OR OVERTORQUED 1 H 7 1 3T 3 T A37CE E4EA 5 C P60GL 2001041700149 20010417 00149 EU 2001 4 17 01FDEA00219 1 20010321 A 2612 FIRE WARNING AIRBUS 300 A300F4605R 3930327 EU COCKPIT ACTIVATED A FDEA F A ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 656FE 745 AT CR FOR APPROX 20 MIN FMS IND A FIRE. PROC IN QRH FOLLOWED FIRE HANDLE PULL AGENT DISCHARGED. IMMEDIATE LAND AT IND. FIRE LIGHT IN APU HANDLE EXT ON TOUCHDOWN. 2 L 7 2 4F RT A35EU 2001041700150 20010417 00150 2001 4 17 01FDEA00220 4 20010322 A 3452 TRANSPONDER AIRBUS 310 A310203 EU E&E BAY MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 428FE 248 AFT DEP LOST TRANSPONDER (1 & 2), NR 2 PITCH TRIM, NR 1 ATS, CAPT/STBY BY PROBE HEAT AND NR 2 PRESSURE CONTROLLER. ALSO ACARS DID NOT RECORD OFF OR ON TIMES CAPT SRS INOP. EVERYTHING APPEAR TO RESET UPON LANDING. 2 L 7 2 4F RT A35EU 2001041700151 20010417 00151 NM 2001 4 17 01FDEA00222 1 20010322 A 2612 656020916 CONTROL UNIT BOEING 727 7272S2F 1384O81 NM COCKPIT MALFUNCTIONED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 211FE 22933 IN CLIMB GOT AN INTERMITTENT FIRE WARN LIGHT, A FIRE BELL, AND MASTER FIRE WARN LIGHT. REMOVED AND REPLACED FIRE DETECT ION CONTROL UNIT AND RAN ALL 3 ENGINES PER IAW JRH CHPT 5. OPS CK GOOD. FIRE WARN TEST OK. REF EA 7-2610-56907. 2 L 7 3 4F A3WE 2001041700152 20010417 00152 2001 4 17 MWEA010364 4 20010321 A 3450 6223257001 RECEIVER DOUG DC9 DC932 3022066 WP NAV SYSTEM INOPERATIVE A MWEA D RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TX TAXI/GRND HDL 1 GL 31 207ME 47794 NR 2 NAV CIRCUIT BREAKER TRIPPED WHEN NR 2 ENGINE STARTED AND APU POWER SWITCHED TO ENGINE ELECTRICAL. REPLACED NR 2 NA V RECEIVER. 2 L 7 2 4F A6WE 2001041700153 20010417 00153 NE 2001 4 17 ARWA0010307 2 20010320 A 7260 777882 O-RING DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE GEARBOX LEAKING A ARWA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 SO 19 810BN 45905 671358 AT TOP OF DESCENT NR 3 ENGINE OIL PRESSURE GAUGE FLICKERS FULL SCALE HIGH AND LOW AND NR 3 ENGINE OIL PRESSURE LIGHT FLI CKERS ON AND OFF. ALL OTHER ENGINE PARAMETERS NORMAL. PRECAUTIONARY ENGINE SHUTDOWN. ON INSPECTION OF ENGINE, FOUND T OWER SHAFT SEAL LEAKING, REPLACE SEAL, LEAK CHECK, AND RUN-UP AND SYSTEM CHECK COMPLETED SATISFACTORY. 2 L 7 4 4F 4 F 4A25 1E8 2001041700154 20010417 00154 NM 2001 4 17 DHL2001741508 1 20010308 A 5755 SUPPORT BRACKET BOEING 727 7272Q9 138448M NM LT SPOILER CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 LT WING NR 7 SPOILER HINGE SUPPORT ROD IS LOOSE AND CORRODING AT LOWER ATTACH TO LOWER COVER PANEL SUPPORT RIB. REMOVED LOWER ATTACH SUPPORT BRACKET AT LEFT WING NR 7 SPOILER OUTBOARD HINGE SUPPORT ROD AS PER B727 SRM 51-30-2. FABRICATE N EW SUPPORT BRACKET AS PER B727 SRM 57-20-2 FIG 2 MATERIAL USED 7075-0 .050, 8 X 4 INCH LOT Z99214 PO 8319222 START OPEN THE HOLES AT NEW SUPPORT BRACKET AS PER SRM- B727 51-30-2. INSTALLED BRACKET PER SRM B727 51-30-2. HEAT TREATED TO 707 5 T6 AS PER GENERAL PROCESS SPECIFICATION 98 PSI 247 PS-01. ALODINED PRIMED AS PER B727 SRM 51-10-2. 2 L 7 3 4F RT A3WE 2001041700155 20010417 00155 WP 2001 4 17 ASAA0180092 1 20010302 A 3350 20131A BATTERY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 955AS 48080 PHX - DURING K-CHECK, DETERMINED THAT, WHEN TURNED ON, EMERGENCY FLOOR TRACK LIGHTS IN FORWARD CABIN AND AT ENTRY WAY DO NOT STAY ON. REPLACED ASSOCIATED BATTERY PER MIG-4 4438481. (M) 2 L 7 2 4F A6WE 2001041700156 20010417 00156 WP 2001 4 17 ASAA0180093 1 20010303 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE BETWEEN ROWS 20 AND 33. REPLACED ASSOCIATED BAT TERY PACK. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001041700157 20010417 00157 WP 2001 4 17 ASAA0180094 1 20010303 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN MALFUNCTIONED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 950AS 53023 SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS FROM ROW 29 THROUGH TAILCONE, WERE DETERMINED TO BE INOPERAT IVE. RESET ASSOCIATED BATTERY PACK. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001041700158 20010417 00158 WP 2001 4 17 ASAA0180095 1 20010306 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 954AS 49387 SEA - DURING LINE CHECK, EXTERIOR OVERWING EMERGENCY LIGHTS WERE DETERMINED TO BE INOPERATIVE. REMOVED AND REPLACED ASS OCIATED BATTERY PACKS. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 2001041700160 20010417 00160 NM 2001 4 17 ASAA0110040 1 20010205 A 5312 651630084 BULKHEAD BOEING 737 737290C 138448V NM FUSELAGE CRACKED A K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 DURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB AT BS 178, LEFT BUTTOCK LINE 6-18 CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041700161 20010417 00161 NM 2001 4 17 ASAA0110037 1 20010205 A 5311 6546560508 FRAME BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 947, STRINGER 24L-26L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041700162 20010417 00162 NM 2001 4 17 ASAA0110038 1 20010205 A 5330 6545775 SKIN BOEING 737 737290C 138448V NM FUSELAGE DENTED A K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND SKIN PANEL AT BS 912, STRINGER 21R DENTED BEYOND SRM LIMITS. REPAIRED PER SRM. (M ) 2 L 7 2 4F A16WE 2001041700163 20010417 00163 NM 2001 4 17 ASAA0110052 1 20010207 A 5320 6559658 DOUBLER BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND DOUBLER ON INTERCOSTAL AT BS 980-986, STRINGER 46L CORRODED. REPAIRED PER SRM. ( M) 2 L 7 2 4F A16WE 2001041700164 20010417 00164 NM 2001 4 17 ASAA0110044 1 20010206 A 5311 65465503 FRAME BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 787, STRINGER 17L-22L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041700165 20010417 00165 NM 2001 4 17 ASAA0110045 1 20010206 A 5310 6546563 SHEAR TIE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND CENTER SHEAR TIE AT BS 927, STRINGER 27L-27R CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041700166 20010417 00166 NM 2001 4 17 ASAA0110047 1 20010206 A 5313 BAC1498158 STRINGER BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER AT BS 727-739, STRINGER 25L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041700167 20010417 00167 NM 2001 4 17 ASAA0110020 1 20010126 A 5512 6573794518 SKIN BOEING 737 737290C 138448V NM HORIZ STAB CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND RIGHT HORIZONTAL STABILIZER CHAFED ON TRAILING EDGE OF STATION 121.5. REPAIRED PE R SRM. (M) 2 L 7 2 4F A16WE 2001041700168 20010417 00168 NM 2001 4 17 ASAA0110021 1 20010126 A 5320 65468127 FLOOR SUPPORT BOEING 737 737290C 138448V NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FLOOR SUPPORT HAS DOUBLER DRILLED HOLES AT BS 1006-1016, LBL 18. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041700169 20010417 00169 NM 2001 4 17 ASAA0110022 1 20010126 A 5320 69353646 TIE CLIP BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND TIE CLIP AT BS 867, STRINGER 20L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041700170 20010417 00170 NM 2001 4 17 ASAA0110023 1 20010129 A 5330 69530441 PLATE BOEING 737 737290C 138448V NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, SPLICE PLATE AT BS 727, STRINGER 4L CUT APPROXIMATELY TWO INCHES. REPAIRED PER EA 5330- 01502. (M) 2 L 7 2 4F A16WE 2001041700171 20010417 00171 NM 2001 4 17 ASAA0110025 1 20010129 A 5315 654681113 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND FLOORBEAM ANGLE AT BS 986, LBL 39, CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041700172 20010417 00172 NM 2001 4 17 ASAA0110026 1 20010129 A 5320 656739319 ANGLE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND LOWER ANGLE ATTACHED TO INTERCOSTAL AT BS 967-986, LBL 46, CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041700181 20010417 00181 NM 2001 4 17 ASAA0140007 1 20010119 A 5311 35301734 FRAME BOEING 737 7374Q8 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 776AS 25109 PAE - DURING SI CHECK, FOUND CRACK AT BS 178 LEFT AND RIGHT SIDE AT WL 205. REMOVED AND REPLACED BS 178 LEFT AND RIGHT SIDE CHORD PER EA 5310-01890. (M) 2 L 7 2 4F RT A16WE 2001041700182 20010417 00182 NM 2001 4 17 ASAA0140006 1 20010117 A 5315 654681179 FLOORBEAM BOEING 737 7374Q8 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 776AS 25109 PAE - DURING SI CHECK, FOUND CORROSION ON FLOORBEAM AT BS 986.6 RBL 44 TO LBL 31, WL 208 AROUND FASTENER HOLES. REPAIRE D FLOORBEAM IAW EA 5310-01891. (M) 2 L 7 2 4F RT A16WE 2001041700183 20010417 00183 NM 2001 4 17 ASAA0110105 1 20010202 A 5315 6545805501 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 294.5, RIGHT BUTTOCK LINE 24, LEFT BUTTOCK LINE 26 CORRODED. REPA IRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041700184 20010417 00184 NM 2001 4 17 ASAA0110006 1 20010103 A 5320 65466115 STIFFENER BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND CORROSION AT NUT CLIP HOLES ON UPPER AND LOWER SIDE OF FLOORBEAM STIFFENER. REMOV ED AND REPLACED FLOORBEAM STIFFENER PER SRM. (M) 2 L 7 2 4F A16WE 2001041700199 20010417 00199 EU 2001 4 17 SIMA0302 1 20010130 A 5610 7256100502 WINDSHIELD SAAB SF340 340B 7860101 EU COCKPIT CRACKED A SIMA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 236AE 340B236 BVT - FLT 5113 - DURING CRUISE, CREW REPORTED THE FIRST OFFICERS WINDSCREEN OUTER PANE SHATTERED. NO LOSS OF CABIN PRES SURE NOTED. AIRCRAFT DIVERTED TO BVT AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED FIRST OFFICERS WINDSCREEN IAW SAAB MM 56-10-05. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001041700200 20010417 00200 EU 2001 4 17 SIMA0274 1 20010127 A 3010 4D203701 TIMER SAAB SF340 340B 7860101 EU DE-ICE SYSTEM INOPERATIVE A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 280AE 340B280 DFW - FLT 3841 - EN ROUTE TO AMA, CREW REPORTED THE DE-ICE TIMER LIGHT CAME ON DURING OPERATION. FOLLOWED CHECKLIST AND COULD NOT INFLATE RIGHT WING BOOT MANUALLY OR IN AUTO. AIRCRAFT WAS LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REP LACED DE-ICE TIMER IAW SAAB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001041700201 20010417 00201 EU 2001 4 17 SIMA0266 1 20010126 A 2120 UNKNOWN SAAB SF340 340B 7860101 EU COCKPIT ODOR A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 382AE 340B382 ABI - FLT 3328 - CREW REPORTED A STRONG BURNING SMELL DURNIG CLIMB-OUT WITH OVERHEAD INTERMITTENTLY FLASHING. MAINTENAN CE COULD NOT DUPLICATE DISCREPANCY WITH OVERHEAD LIGHT. SUSPECT SMELL CAME FROM RESIDUAL COMPRESSOR WASH FLUID FROM THE PREVIOUS NIGHT MAINTENANCE VISIT. MAINTENANCE PERFORMED GROUND ENGINE RUNS AND COULD NOT DUPLICATE SMELL. AIRCRAFT WA S RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001041700202 20010417 00202 EU 2001 4 17 SIMA0341 1 20010203 A 5610 7256100501 WINDSHIELD SAAB SF340 340B 7860101 EU COCKPIT CRACKED A SIMA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 347SB 340B347 ALB - FLT 5087 - CREW REPORTED CAPTAINS FRONT WINDSHIELD CRACKED AT 19,000 FEET. AIRCRAFT DIVERTED TO ALB. MAINTENANCE REMOVED AND REPLACED LEFT FRONT WINDSHIELD IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVIC E. (M) 2 L 7 2 4T RT A52EU 2001041700203 20010417 00203 EU 2001 4 17 SIMA0323 1 20010201 A 5101 STRUCTURE SAAB SF340 340B 7860101 EU FUSELAGE VIBRATION A SIMA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SW 21 283AE 340B283 DURING CRUISE FLIGHT, A YAW VIBRATION WAS FELT OVER 230 KNOTS. AIRCRAFT TURNED BACK TO BOS. INSPECTED BOOTS, VORTEX GE NS, RUDDER AND TRIM TAB BEARINGS, CABLE TENSIONS IAW AMM. NO DEFECTS NOTED. PERFORMED FCF AND PASSED. AIRCRAFT RETURN ED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001041700213 20010417 00213 EU 2001 4 17 SIMA04516 1 20010214 A 3230 MS332010 CIRCUIT BREAKER SAAB SF340 340B 7860101 EU LT & RT MLG FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 254AE 340B254 SBP - DURING MBV INSPECTION, FOUND NO VOLTAGE TO PIN C AND D ON LEFT AND RIGHT MLG SEPARATION BOLTS. REMOVED AND REPLAC ED LEFT EMERGENCY EXTENSION CIRCUIT BREAKER IAW AMM 24-00-00. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001041700218 20010417 00218 EA 2001 4 17 WVBA2001019 2 20010402 A 8520 LW19340 CAMSHAFT PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA HARTZL HCE3Y HCE3YR2A GL ENGINE DAMAGED E WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 300ED 400 400 317852008 L231268A DJ11225A DURING INSPECTION, METAL CONTAMINATION WAS DISCOVERED IN THE OIL FILTER. A CHECK OF VALVELIFT WAS DONE AND IT WAS DISCO VERED THAT NR 3 AND NR 4 INTAKE LOBES WERE EXCESSIVE. NR 3 CLYINDER WAS REMOVED AND DAMAGE OBSERVED ON THE CAM LOBES AN D TAPPET FOLLOWERS. NOTE THIS IS THE 20TH ENGINE IN THREE YEARS. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 2001041700219 20010417 00219 GL 2001 4 17 20010411CW007 3 20010306 A 6110 D31561 COUNTERWEIGHT MCAULY BEECH 55 D55 1152730 CE CONT O520 IO520* 17032 SO MCAULY 2AF34C 2AF34C55 GL PROPELLER SEPARATED E XGNA C ABORTED TAKEOFF D E INFLIGHT SEPARATION VIBRATION/BUFFET TO TAKEOFF 1 SW 05 69RP 650 693805 TE766 693805 COUNTERWEIGHT DEPARTED LEFT PROP ON TAKEOFF ROLL. SPINNER AND BACKING PLATE WERE DESTROYED. PROP HUB WAS CRACKED IN TW O PLACES. NO OTHER DAMAGE TO AIRCRAFT OR ENGINE. ROTOR COUNTERWEIGHT WAS NOT FOUND. 1 L 7 2 3O 3 O 3A16 E5CE 5 C P5EA 2001041700220 20010417 00220 SO 2001 4 17 C2XA01TY051 1 20010320 A 5315 14521700001 FLOORBEAM EMB 145 EMB145LR SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13978 145180 TYS DURING A SCHEDULED INSPECTION THE LEFT OMEGA BEAM WAS FOUND TO HAVE CORROSION UNDER THE CARBON FIBER SUPPORT RAIL A T FRAME 20. MAINTENANCE REPAIRED THE OMEGA BEAM IAW EMB-145 SRM-53-21-10, EMB-145 SRM-51-40-02 AND EMB-145 CPM-51-21-03 ,04. THE REPAIR WAS SATISFACTORY, AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2001041700221 20010417 00221 SO 2001 4 17 C2XA01TY052 1 20010322 A 2612 3601133500 FIRE LOOP EMB 145 EMB145LR SO LT ENGINE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13978 3772 3772 145180 TYS DURING A SCHEDULED INSPECTION THE LEFT ENGINE FIRE LOOP WAS FOUND CHAFED, ON TOP SECTION OF ENGINE. MAINTENANCE RE MOVED AND REPLACED THE LEFT ENGINE FIRE LOOP IAW EMB-145 MM 26-11-01, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT WI LL BE RELEASED FOR SERVICE UPON COMPLETION OF INSPECTION. P/N 3601-133-500/230C-9.0M. 2 L 7 2 4T RT T00011AT 2001041700223 20010417 00223 SO 2001 4 17 C2XA01TY053 1 20010320 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13978 145180 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RIGHT HAND OMEGA BEAM TOP CAP BETWEEN FRAME 18 AND 23. MA INTENANCE REMOVED AND REPLACED THE RIGHT HAND OMEGA BEAM TOP CAP IAW EMB-145 SRM-51-40-02 AND EMB-145 CPM-51-21-06. THE REPAIR WAS SATISFACTORY, AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2001041700224 20010417 00224 SO 2001 4 17 C2XA01TY054 1 20010320 A 5315 14521700001 FLOORBEAM EMB 145 EMB145LR SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13978 145180 TYS DURING A SCHEDULED INSPECTION SEVERAL AREAS OF CORROSION WAS FOUND ON THE RIGHT HAND OMEGA BEAM BETWEEN FRAMES 19 A ND 22. MAINTENANCE REPAIRED THE RIGHT HAND OMEGA BEAM IAW EMB GST-0823/01, REPAIR WAS SATISFCATORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2001041700228 20010417 00228 NM 2001 4 17 C1HA200194009 1 20010321 A 7931 ST104Y TRANSMITTER BOEING 727 727290 138408W NM OIL SYSTEM FAILED A C1HA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 15 294AS 22146 NR 1 ENG OIL QTY AT 0 GALLONS, TEMP AT 135 DEGREES C IN THE YELLOW AND OIL PRESS IN THE GREEN TEMP AND PRESS FLUCTUATED IN AND OUT OF YELLOW ARC. FOUND T-FITTING LEAKING ON RT SIDE OF GEARBOX REPLACED OIL PRESS TRANSMITTER PER 79-32-1, OPS CK NORMAL. 2 L 7 3 4F A3WE 2001041700229 20010417 00229 EA 2001 4 17 COMA0160329 1 20010318 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 EA RT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 952CA 7092 RT LOWER WING PLANK CRACKED AT 2 LOCATIONS: 640 DB WS 95.950 AND 640 FB WS 136.676. BLENDED OUT DAMAGED AREAS AND ROTO -PEENED IAW REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 2001041700230 20010417 00230 EA 2001 4 17 COMA0160330 1 20010318 A 2750 601R930043 CONTROL HANDLE CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTIONED A COMA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 959CA 7356 7116 FLAPS FAIL MESSAGE DURING LANDING ROLL. REPLACED THE FLAP CONTROL LEVER. 2 L 7 2 4F RT A21EA 2001041700231 20010417 00231 EA 2001 4 17 COMA0160331 1 20010320 A 3030 7858062 SENSOR CNDAIR CL600 CL6002B19 EA E&E BAY MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 969CA 11678 7141 RT STATIC, PITOT, AND AOA HET CAUTION MESSAGE. REPLACED THE RT ADSHC. 2 L 7 2 4F RT A21EA 2001051800003 20010518 00003 NM 2001 5 18 DHL2001715003 1 20010327 A 3246 BEARING BOEING 727 727155C 138404Z NM MLG WHEEL SEPARATED A DHLA D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 SO 01 715DH 19618 VIBRATION DURING TAXI AND A/C REQUIRES HIGHER THAN NORMAL THRUST TO TAXI. NR 1 MAIN TIRE NUT AND BEARING SEPERATED. REPL ACED LT MLG LOWER CYLINDER ASSY. FOUND NR 1 MAIN T/W ASSY SLEEVE DAMAGED. REPLACED NR 1 T/W ASSY, NR 1 BRAKE, AND NR 2 W/T ASSY. 2 L 7 3 4F A3WE 2001041700232 20010417 00232 NM 2001 4 17 DHL2001701004 1 20010329 A 7931 INDICATOR BOEING 727 72730C 1384009 NM NR 3 OIL PRESS MALFUNCTIONED A DHLA E D ENGINE SHUTDOWN RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 701DH 19011 NR 3 LOW OIL PRESSURE LIGHT ILLUMINATED DURING TAXI. QUANITY AND PRESS NORMAL. TRANSFERRED TO DMI PER MEL 79-4. VISUALLY VERIFIED OIL QUANITY FULL, CONTROL 4933 PLACARD INSTALLED BULB REMOVED. STATUS-OPEN. 2 L 7 3 4F A3WE 2001041700233 20010417 00233 NM 2001 4 17 AWXA0001515 1 20010321 A 5330 6545877 DOUBLER BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 R1 DOOR JAMB, FWD UPPER CORNER BEAR STRAP INTERIOR SKIN HAS CRACK EMANATING FROM FIFTH FASTENER FROM TOP IN RADIUS. REM OVED FASTENERS, STOP DRILLED CRACK; FABBED AND INSTALLED REPAIR DUOBLERS IAW B737-300 SRM 51-40-02 PG 1 AND DWG 65C33800 . 2 L 7 2 4F RT A16WE 2001041700234 20010417 00234 NM 2001 4 17 AWXA0001516 1 20010321 A 5315 AND101341205 FLOORBEAM BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 FLOORBEAM LOWER ANGLE HAS ELONGATED/CRACKED FASTENER HOLES BS 178 RBL 24 WL 195. REMOVED FASTENERS; CUT OUT DAMAGE ON F LOORBEAM LOWER ANGLES; FORMED, CUT DRILLED AND INSTALLED REPAIR ANGLES AND FILLERS IAW B737-300 SRM 51-70-12 PG 1 2 L 7 2 4F RT A16WE 2001041700236 20010417 00236 NM 2001 4 17 AWXA0001517 1 20010321 A 5320 06720382 INTERCOSTAL BOEING 737 7373S3 1384711 NM FUSELAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 INTERCOSTAL ADJACENT TO SIDE CHORD AT WL 195 ON AFT RIGHT SIDE OF BS 178 BULKHEAD HAS (1) MISSING/LOOSE FASTENER. REMOV ED DAMAGED INTERCOSTAL; FORMED, LOCATED, DRILLED INTERCOSTAL IAW B737-300 SRM 51-40-02 PG 1; TREATED AND PRIMED IAW SRM 51-20-01 PG 1. 2 L 7 2 4F RT A16WE 2001041700237 20010417 00237 NM 2001 4 17 AWXA0001518 1 20010321 A 5320 654581951 WEB BOEING 737 737277 1384570 NM NLG WW CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 22655 NOSE GEAR RETRACT ACTUATOR SUPPORT BEAM WEB CRACKED AT FWD AREA AS MARKED. MADE AND INSTALLED WEB IAW DWG 65-45819. 2 L 7 2 4F RT A16WE 2001041700238 20010417 00238 NM 2001 4 17 AWXA0001519 1 20010321 A 5320 654581945 CHANNEL BOEING 737 737277 1384570 NM NLG WW CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 22655 NOSE GEAR RETRACT ACTUATOR SUPPORT BEAM AFT CHANNEL CRACKED IN RADIUS. GUSSET REPLACED IAW DWG 65-45819. 2 L 7 2 4F RT A16WE 2001041700239 20010417 00239 NM 2001 4 17 AWXA0001521 1 20010321 A 5311 651630087 FRAME BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 22655 FWD PRESSURE BLKHD SIDE CHORD CRACKED AT RT SIDE AND LT SIDE AT WL 207; RIVET MISSING FROM FLOOR WEB. RT SIDE CHORD (P/ N 65-16300-86) REPLACED IAW DWG 65-16300-40 AND SRM 51-30-2; LT SIDE CHORD (P/N 65-16300-87) REPLACED IAW DWG 65-16300 & SRM 51-30-2; WEB REPLACED IAW DWG 65-45833 AND SRM 51-30-2; MISSING RIVET REPLACED IAW SRM 51-30-2. 2 L 7 2 4F RT A16WE 2001041700240 20010417 00240 NM 2001 4 17 AWXA0001522 1 20010321 A 5321 65458333 FLOOR PANEL BOEING 737 737277 1384570 NM COCKPIT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 22655 COCKPIT FLOOR PANEL CORNER PIECE BROKEN OFF AT STA 188 WL 207 JUST BELOW -40 WEB AT RT SIDE. REPAIRED FLOOR PANEL IAW R EF DWG 65-45833 AND SRM 51-40-02 FIG 1 AND SRM 51-30-2. 2 L 7 2 4F RT A16WE 2001041700241 20010417 00241 NM 2001 4 17 AWXA0001523 1 20010321 A 5312 65163007 BULKHEAD BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 22655 FWD PRESSURE BLKHD CRACKED AT FASTENER HOLE AT RBL 12 WL 234; 2 CRACKS APPROX .0625 INCH BEYOND FASTENER HEAD. WEB REPA IRED IAW SRM 53-10-11 FIG 1 DET II AND SRM 51-30-2. 2 L 7 2 4F RT A16WE 2001041700242 20010417 00242 NM 2001 4 17 AWXA0001524 1 20010321 A 5320 6720381 INTERCOSTAL BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 22655 FWD PRESSURE BLKHD INTERCOSTAL CRACKED AT STA 178 WL 195 LT SIDE (1 INCH CRACK) FWD CORNER. REPLACED INTERCOSTAL IAW DW G 65-16300 AND SRM 51-30-2. 2 L 7 2 4F RT A16WE 2001041700243 20010417 00243 NM 2001 4 17 AWXA0001525 1 20010321 A 5312 65163007 BULKHEAD BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 22655 FWD PRESSURE BLKHD CRACKED (APPROX 2 INCHES) AT BL 0 WL 190. REPAIRED IAW SRM 53-10-11 FIG 4 DET II. 2 L 7 2 4F RT A16WE 2001041700244 20010417 00244 NM 2001 4 17 AWXA0001526 1 20010321 A 5330 6573748 SKIN BOEING 737 737277 1384570 NM FUSELAGE DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 22655 DENT AT BS 1064 STR 14L. REMOVED DOUBLER AND ASSESSED IAW SRM 53-30-1 FIG 1; INSTALLED NEW DOUBLER IAW SRM 53-30-3 FIG 17. 2 L 7 2 4F RT A16WE 2001041700245 20010417 00245 NM 2001 4 17 AWXA0001527 1 20010321 A 5315 6546816 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 22655 SURFACE CORROSION ON TOP OF CABIN FLOORBEAM AT BS 986.5. FLOORBEAM REPAIRED IAW SRM 53-10-9 FIG 2. 2 L 7 2 4F RT A16WE 2001041700246 20010417 00246 NM 2001 4 17 AWXA0001528 1 20010321 A 5330 6573743 SKIN BOEING 737 737277 1384570 NM FUSELAGE DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 22655 TWO DENTS COVERED BY REPAIR DOUBLERS BELOW CARGO BIN AT STA 460. OLD REPAIRS REMOVED, NDT CONFIRMED NO CRACKS IN CUTOUT AREAS; NEW REPAIRS FABBED AND INSTALLED IAW SRM 53-30-3 FIG 6. 2 L 7 2 4F RT A16WE 2001041700247 20010417 00247 NM 2001 4 17 AWXA0001530 1 20010321 A 7110 657377311 STIFFENER BOEING 737 737277 1384570 NM NR 1 COWL CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 22655 NR 1 ENG O/B COWL 4TH RIB FROM AFT AND 7TH, 8TH, AND 9TH CHAFING TO THE ENGINE. NR 4 AND 9 RIB REPAIRED IAW SRM 51-40-3 ; NR 7 AND 8 RIBS (STIFFENERS) BLENDED W/I SRM 54-10-1 FIG 1 LIMITS; AREAS ALODINED AND PRIMED IAW SRM 51-10-2 AND DWG 6 5-73773. 2 L 7 2 4F RT A16WE 2001041700248 20010417 00248 NM 2001 4 17 AWXA0001531 1 20010321 A 5330 65528733 SKIN BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 22655 USING HFEC .25 INCH CRACK FOUND AT DOOR 2L UPPER HINGE CUTOUT. CRACK REMOVED IAW SRM 52-00-2 FIG 6 (BEYOND LIMIT); NDT CHECKED. CRACK REMOVED IAW NDT PT.6 51-00-00; CRACK REPAIRED IAW ER 15-5210-01072-JS4. 2 L 7 2 4F RT A16WE 2001041700249 20010417 00249 NE 2001 4 17 JBXA00240 2 20010224 A 7230 65015 BLADE FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAY65015 54557 NE NR 2 ENGINE NICKED A JBXA K NONE O OTHER IN INSP/MAINT 1 SO 05 109ML 14698 11485 17519 NICK FOUND IN NR 2 ENGINE FAN BLADE ON POST FLIGHT INSPECTION. REMOVED AND REPLACED NR 2 ENGINE IAW MIDWAY AIRLINES WOR KCARDS F4624 AND 4622. 2 L 7 2 4F 4 F RT E25NE 2001041700250 20010417 00250 NM 2001 4 17 DHL2001741509 1 20010307 A 5754 PANEL BOEING 727 7272Q9 138448M NM L/E SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 NR 3 L/E SLAT ACTUATOR ROD END ATTACH AREA ADJACENT PANEL CRACKED. REMOVED INTERNAL PANEL AT NR 3 L/E SLOT ACTUATOR AS PER B 727 SRM 51-30-2. ROUTE OUT CRACK AS PER B 727 SRM 51-10-1, MAT LOSS .010. INSTALLED DOUBLER REPAIR AS PER B 727 SRM 51-40 2 FIG AT. USED 2024 T3 .040, 12 X 4.25 INCH LOT 192582 P/O 8319615. ALODINED AND PRIMED AS PER B 727 SRM 51-1 0-2. REINSTALLED PANEL AT NR 3 SLAT AS PER B 727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2001041700251 20010417 00251 NM 2001 4 17 DHL2001741510 1 20010308 A 2810 FUEL TANK BOEING 727 7272Q9 138448M NM CTR WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 CORROSION AT CTR WING TANK LOWER SURFACE, INSIDE RT A/C BAY PLENUM, APPROX BS 830. REMOVED FASTENERS FOR ACCESS AS PER B 727 SRM 51-30-2. REMOVED RT PRIMARY 7 SECONDARY HEAT EXCHANGER AND PLENUM ASY FOR S/M ACCESS B 727 MM 21-50-2. REMOV ED CORROSION AT CENTER WING TANK LWR SURFACE I/B A/C PLENUM FROM STA 830 TO 839 RBL 32 TO 23 US/PER B 727 SRM 51-10- 6. PERFORMED HFEC, INSPECTION AT AREA PER NDT PART 6,51-00-00 FIG 4, NO DEFECTS NOTED. PERFORMED THICKNESS CHECK OF LWR S KIN BS 830 TO 839.0 RBL 32 TO 23 PER PARAMETRICS MANUAL NR 910-131B, LOWEST READINGS. 109, SEVERAL AREAS OUT OF LIMITS. REMOVED INTERNAL DOUBLER RBL 32 TO RBL 13 STA 830 AS PER B 727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2001041700252 20010417 00252 NM 2001 4 17 2001UALA00368 1 20010330 A 5310 ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOORWAY MISDRILLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 310UA 23671 FORWARD CARGO DOOR REINFORCING ANGLES HAVE AREAS WITH SHORT EDGE DISTANCE. REPAIRED FORWARD CARGO DOOR. MAJOR REPAIR A CCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041700253 20010417 00253 SO 2001 4 17 C2XA01IA172 1 20010321 A 2530 CBC16707 RECEPTACLE EMB 145 EMB145ER SO GALLEY BURNED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 27 14938 145029 IAH-FLIGHT ATTENDANT REPORTED BURNT SMELL IN CABIN DURING DESENT AND FOR REMAINDER OF THE FLIGHT. MAINTENANCE REMOVED A ND REPLACED THE HOT JUG RECEPTACLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001041700257 20010417 00257 NM 2001 4 17 ASAA0110050 1 20010207 A 5320 65516985 SPLICE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE AT BS 907, STRINGER 20L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041700258 20010417 00258 NM 2001 4 17 ASAA0110028 1 20010129 A 5320 654795734 CHANNEL BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND CHANNEL AT BS 790-847, STRINGER 25R, CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041700259 20010417 00259 NM 2001 4 17 ASAA0110029 1 20010129 A 5320 BAC1493357 ANGLE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND ANGLE AT BS 887, STRINGER 22L-24, CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041700260 20010417 00260 WP 2001 4 17 ASAA0180024 1 20010122 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 967AS 49103 SEA - DURING LINE CHECK, FOUND OVERHEAD EMERGENCY LIGHTS IN ROWS 1 THROUGH 5 WERE FOUND INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERIES. LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 2001041700261 20010417 00261 NM 2001 4 17 ASAA0110012 1 20010109 A 5320 654583340 WEB BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND FLOOR WEB CRACKED. REMOVED, FABRICATED AND REPLACED FLOOR WEB PER SRM. (M) 2 L 7 2 4F A16WE 2001041700273 20010417 00273 NM 2001 4 17 ASAA0140021 1 20010208 A 5347 6546813101 SEAT TRACK BOEING 737 7374Q8 NM CABIN CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 778AS 25110 PAE - DURING SI CHECK, FOUND CORROSION OUT OF LIMITS ON SEAT TRACK FROM BS 360-480 AND RBL 24.75 AND WBL 208. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2001041700274 20010417 00274 NM 2001 4 17 ASAA0140030 1 20010227 A 5315 6545815285 FLOORBEAM BOEING 737 7374Q8 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 778AS 25110 PAE - DURING SI CHECK, FOUND CORROSION ON FLOORBEAM. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2001041700275 20010417 00275 NM 2001 4 17 ASAA0140026 1 20010216 A 5320 6545875520 STRAP BOEING 737 7374Q8 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 778AS 25110 PAE - DURING SI CHECK, FOUND CORROSION ON MOPSILL STRAP. REPLACED MOPSILL STRAP IAW SRM. (M) 2 L 7 2 4F RT A16WE 2001041700276 20010417 00276 NM 2001 4 17 ASAA0140031 1 20010227 A 5320 65C807351 SILL BOEING 737 7374Q8 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 778AS 25110 PAE - DURING SI CHECK, FOUND CORROSION ON MOPSILL. REMOVED AND REPLACED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2001041700277 20010417 00277 NM 2001 4 17 ASAA0140032 1 20010227 A 5315 6545808260 FLOORBEAM BOEING 737 7374Q8 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 778AS 25110 PAE - DURING SI CHECK, FOUND CORROSION ON UPPER CHORD OF FLOORBEAM. REMOVED AND REPLACED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2001041700278 20010417 00278 WP 2001 4 17 ASAA0180083 1 20010223 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 982AS 53473 PHX - DURING K-CHECK, FOUND LEFT AND RIGHT OVERWING EMERGENCY EXIT OVERHEAD LIGHTS INOPERATIVE. REMOVED AND REPLACED TH E TWO BATTERIES IN THE ASSOCIATED BATTERY PACK. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001041700279 20010417 00279 NM 2001 4 17 ASAA0110107 1 20010222 A 3350 8731002142 SIGN BOEING 737 737210C 1384459 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING MAINTENANCE CHECK, FOUND EXIT TO REAR SIGN ON SMOKE BARRIER INOPERATIVE. REMOVED AND REPLACED SIGN ASSEMBL Y THEN SIGN OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2001041700280 20010417 00280 NM 2001 4 17 ASAA0110109 1 20010223 A 3350 86210144 BATTERY BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, FOUND EXIT TO REAR SIGN ON SMOKE BARRIER INOPERATIVE. REPLACED REMOTE ASSEMBLY BATTERY, LIGHT FUNCTION NORMAL. (M) 2 L 7 2 4F RT A16WE 2001041700281 20010417 00281 NM 2001 4 17 ASAA0110110 1 20010224 A 3350 86210144 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS ON SEAT PALLET 6-10 INOPERATIVE. REPLACED REMOTE ASSEMBLY B ATTERY AND RECEIVER, LIGHTS FUNCTION NORMAL. (M) 2 L 7 2 4F RT A16WE 2001041700282 20010417 00282 NM 2001 4 17 20010417SG001 1 20010224 A 3350 883200312 RECEIVER BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS ON SEAT PALLET 6-10 INOPERATIVE. REPLACED REMOTE ASSEMBLY B ATTERY AND RECEIVER, LIGHTS FUNCTION NORMAL. REF ASAA0110110. (M) 2 L 7 2 4F RT A16WE 2001041700285 20010417 00285 WP 2001 4 17 ASAA0080504 1 20010220 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 PHX - DURING SCHEDULED 30K CHECK, THE UPPER SURFACE OF THE FLOOR WEB AT STATION 785, LONGERON 18R WAS FOUND TO BE CORROD ED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A6WE 2001041700286 20010417 00286 WP 2001 4 17 ASAA0080506 1 20010221 A 5313 993053812 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 PHX - DURING SCHEDULED 30K CHECK, FOUND STATION 570-577 LONGERON 18R WEB WAS FOUND TO BE CORRODED. REPAIRED PER SRM. ( M) 2 L 7 2 4F RT A6WE 2001041700292 20010417 00292 NM 2001 4 17 UPS01235578 1 20010328 A 5730 SKIN BOEING 727 72731C 1384011 NM CENTER WING BOX CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C & SI, WING CENTER SECTION UPPER SKIN CORROSION FOUND ON LWR SURFACE BETWEE N LBBL 49 & RBBL 45 AT BS 870 AND CORROSION FOUND IN 3 FASTENER HOLE S AT R BBL 61 - 64 AT BS 870. REPAIR CARRIED OUT IAW SMRO EO 2001-010-014 UPS ENGINEERING FILE NO. B727-5710-14405-A 2 L 7 3 4F A3WE 2001041700293 20010417 00293 NM 2001 4 17 UPS01235579 1 20010321 A 5753 CARRIAGE BOEING 727 72731C 1384011 NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C & SI, FLAP CARRIAGE NR 3 HAS CORROSION IN SPINDLE BORE. FLAP CARRIAGE REPLACED IAW MM 27-51-01 & OH M 57-58-02 2 L 7 3 4F A3WE 2001041700294 20010417 00294 NM 2001 4 17 UPS01235580 1 20010321 A 5753 CARRIAGE BOEING 727 72731C 1384011 NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C & SI, NR 6 FLAP CARRIAGE HAS CORROSION INSIDE SPINDLE BORE. NR 6 FLAP CARRIAGE REPLACED IAW MM 27-51 -03 2 L 7 3 4F A3WE 2001050100169 20010501 00169 NM 2001 5 1 UPS01235587 1 20010413 A 3510 DOOR BOEING 727 72725C 138400H NM OXYGEN SYSTEM WILL NOT TEST A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:N/A FWD FLIGHT ATTENDANT O2 DOOR WOULD NOT DEPLOY. PERFORMED E.O.727-3520-14476-A OPS CK FWD FLT ATTEND ANTS O2 MASK DOOR DROP CK. OPS CKS GOOD 2 L 7 3 4F A3WE 2001041700295 20010417 00295 NM 2001 4 17 UPS01235588 1 20010413 A 2610 BULB BOEING 727 72727C 138400J NM DETECT INDICATOR INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 914UP 19246 CARGO SMOKE DETECTOR TEST INOP. 2 BULBS INOP. R&R BULBS 2 L 7 3 4F A3WE 2001041700296 20010417 00296 NM 2001 4 17 UPS01435585 1 20010308 A 5313 LONGERON BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, LT MLG WW. CORROSION ON TOP CHORD OF LT OVERWING LONGERON A T BS 1241 LONGERON REPAIRED IAW DRA WING NO. 144U3542 2 L 7 4 4F A20WE 2001042400237 20010424 00237 NM 2001 4 24 UPS01435591 1 20010414 A 2612 FIRE LOOP BOEING 747 747123F NM NR 4 ENGINE INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 674UP 20100 NR 4 FIRE LOOP INOP. REPLACED NR 4 ENG LOWER FWD SENSING ELEMENT AND OPS CHECK NORMAL PER M M 26-11-02 THIS CLEARS M212481 2 L 7 4 4F A20WE 2001041700297 20010417 00297 NM 2001 4 17 UPS01635589 1 20010415 A 2612 FIRE LOOP BOEING 767 767300 1385204 NM LT ENGINE FALSE INDICATION A IPXA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 310UP 27762 LT ENGINE FIRE LOOP MESSAGE DISPLAYED. REF M212830, REMOVED AND REPLACED LT ENGINE FIRE LOOP LOWER FWD ELEMENTS. PER M M 2 6-11-01 OPS CHECKS GOOD. 2 L 7 2 4F RT A1NM 2001041700298 20010417 00298 WP 2001 4 17 UPS01835562 1 20010411 A 2710 AILERON DOUG DC8 DC871F 302199D WP WINGS LACK OF LUBE A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 748UP 45948 AILERONS STIFF. INSPECTED AILERON CONTROL SYSTEM AND FOUND AILERONS IN NEED OF LUBE. LUBRICATED AILERONS IAW 27-10-06 A ND PERFORMED AILERON SYS ADJ/TEST IA W MM 27-10-00. AILERONS CHECKED NORMAL OK FOR SERVICE 2 L 7 4 4F RT 4A25 2001041700299 20010417 00299 WP 2001 4 17 UPS01835581 1 20010403 A 5340 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE: C2, MLG WW PRESSURE DECK STIFFENER STA 960 LBL 48 HAS POPPED RIVETS AND CORROSION COMING FROM UNDERNEA TH. REMOVED & REPLACED FITTING IAW DAC DWG 3640087 AND DC8 SRM 51-1-21 AND 5 1-1-20D 2 L 7 4 4F RT 4A25 2001041700300 20010417 00300 WP 2001 4 17 UPS01835582 1 20010404 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE: C2, STATION Y=8, X=0 FLOOR WEB CRACKED & GOUGED AT SEVERAL AREAS D128. REMOVED FLOOR ATTACH ANGEL, CUT OUT DAMAGE IN WEB FABBED & INSTALLED FILLER & DOUBLER IAW DC8 SRM 53-2-0 FIG 23 AND 51-1-21 ALODINED & PRIME D IAW DC8 SRM 51-1-8 2 L 7 4 4F RT 4A25 2001041700301 20010417 00301 WP 2001 4 17 UPS01835583 1 20010403 A 5340 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE: C2, MAIN CABIN STA 780 RT SIDE, BY SEAT TRACK H BEAM FITTING. SUPPORT CRACKED. REMOVED AND REPLACED F ITTING IAW DC8 SRM 51-1-20 51-1-24 AND 51-3-0 2 L 7 4 4F RT 4A25 2001041700302 20010417 00302 WP 2001 4 17 UPS01835584 1 20010404 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE: C2, MAIN CABIN STA 920 LT FLOORBEAM CORRODED AT FRAME JOINT FWD AND AFT. REMOVED AND REPLACED FLOORBE AM STRAP IAW DAC DWG 5646864 ALODINED A ND PRIMED IAW DC8 SRM 51-1-8 2 L 7 4 4F RT 4A25 2001050100044 20010501 00044 WP 2001 5 1 UPS01835590 1 20010413 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 RT WING STATION 172.000 INBD OF NR 3 ENGINE. SKIN CRACKED RT WING LOWER SURFACE, SKIN CRACKED AT WS 172 AFT OF CENTER S PAR. JUST 8 INCHES I/B OF NR 4 MAIN TANK MID FUEL DRAIN VALVE. AREA (APPROX 7 1/4 INCHES) PERFORMED INTERIM REPAIR OF R T INNER WING AFT BOTTOM SKIN PANEL CRACK FOR PURPOSE OF FERRY FLIGHT PER E.O. DC-8-5730-14248C 2 L 7 4 4F RT 4A25 2001041700303 20010417 00303 WP 2001 4 17 MWEA010575 1 20010416 A 5311 99124512 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 STATION 427 FRAME FROM LONGERON 25 RIGHT THRU 28 RIGHT HAS SEVERAL DOUBLE DRILLED HOLES ON TOP FLANGE OF FRAME. FORMED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 2001041700304 20010417 00304 WP 2001 4 17 MWEA010577 1 20010416 A 5720 99100101 STIFFENER DOUG DC9 DC932 3022066 WP WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 XRS 86 WEB SUPPORT STIFFENER END TEE IS EXFOLIATED. FABRICATED AND INSTALLED END TEE. 2 L 7 2 4F A6WE 2001041700305 20010417 00305 WP 2001 4 17 MWEA010578 1 20010416 A 5711 5911301501 SPAR CAP DOUG DC9 DC932 3022066 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 LEFT WING INTERNAL HAS LIGHT CORROSION ON LOWER TEE CAP LEG FORWARD OF AFT SPAR AT APPROX XRS 67. LOCATED, DRILLED, AND DEBURRED HORIZONTAL FLANGE OF SPAR CAP AND VERTICAL FLANGE OF SPAR CAP. INSTALLED FASTENERS. 2 L 7 2 4F A6WE 2001041700306 20010417 00306 WP 2001 4 17 MWEA010579 1 20010416 A 5743 5919289517 TRUNNION DOUG DC9 DC932 3022066 WP LT MLG CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 LEFT MAIN LANDING GEAR TRUNNION: LIGHT CORROSION ON BOTH FACES OF SIDE BRACE OF ATTACH LUG. FABRICATED AND INSTALLED STRUT ASSY SHIMS. 2 L 7 2 4F A6WE 2001041700307 20010417 00307 2001 4 17 01FDEA00203 4 20010315 A 3140 COMPUTER AIRBUS 300 A300F4605R 3930327 EU COCKPIT FAULTY A FDEA O OTHER N FALSE WARNING TO TAKEOFF 1 SO 25 667FE 771 ON T/O ECAM WENT CRAZY, GALLEY SHED ON, NR 1 PITCH TRIM DISCONNECTED AND WOULD NOT RESET, NR 1 PRESSURE REG FAILED, POS 1 LAND GEAR INOP, ACARS RINGER INOP, NR 1 FLT DIRECTOR INOP. APU LOOP-B FAULT. 2 L 7 2 4F RT A35EU 2001041700308 20010417 00308 NM 2001 4 17 ASAA0110039 1 20010205 A 5311 6546560 FRAME BOEING 737 737290C 138448V NM FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 219, STRINGER 15R-16R CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001041700309 20010417 00309 NM 2001 4 17 ASAA0110046 1 20010206 A 5330 6545775 SKIN BOEING 737 737290C 138448V NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PHX - DURING SCHEDULED D-CHECK, FOUND SKIN PANEL AT BS 836, STRINGER 20L DENTED BEYOND SRM LIMITS. REPAIRED PER SRM. ( M) 2 L 7 2 4F A16WE 2001041800001 20010418 00001 SO 2001 4 18 DHL2001741004 1 20010327 A 5610 5893543109 WINDSHIELD GRUMAV G21 G21A 3951204 SO COCKPIT FAILED A DHLA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 741 B97 CAPT WINDSHIELD SHATTERED AT FLIGHT LEVEL 350. ABNORMAL PROCEDURES ACCOMPLISHED. R&R L-1 WINDOW WITH SERVICABLE UNIT PE R M/M 56-11-11. A/C OK FOR SERVICE. STATUS - CLOSED. 1 H 7 2 3R TC654 2001041800004 20010418 00004 WP 2001 4 18 DHL2001806541 1 20010306 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - FWD CARGO COMPARTMENT FLOOR SUPPORT ANGLE CRACKED 2 INCHES AT STA 500, L-33L TO L-34L. PERFORMED STOP HOLE. F ABRICATED DOUBLER AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1B. STATUS-CLOSED 2 L 7 4 4F RT 4A25 2001041800005 20010418 00005 WP 2001 4 18 DHL2001806542 1 20010309 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP COCKPIT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - FLIGHT COMPARTMENT 676C FLOOR PANEL SKIN CRACKED. PERFORMED STOP HOLE IAW SRM 53-2-3 FIG 10. FABRICATED DOU BLER IAW SRM 53-2-3 FIG 10, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 53-2-3 FIG 10. STATUS-CLOSED . 2 L 7 4 4F RT 4A25 2001041800006 20010418 00006 WP 2001 4 18 DHL2001806543 1 20010309 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP COCKPIT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECKED - FLIGHT COMPARTMENT #676B FLOOR PANEL SKIN CRACKED. PERFORMED STOP HOLE IAW SRM 53-2-3 FIG 10. FABRICATED DOUBLER IAW SRM 53-2-3 FIG 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER USING NEW FASTNERS IAW SRM 51-1-21 PAGE 1. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800007 20010418 00007 WP 2001 4 18 DHL2001806544 1 20010309 A 5520 STRUCTURE DOUG DC8 DC873F 302199F WP ELEVATOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK 0- TAIL CONE INTERIOR PART, SIDE, RT AT STA 1920, SHOWS 1/2 INCH CRACK AND RIVETS LOOSE IN ELEVATOR TORQUE TUBE PROTECTOR. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1. PERFORMED STOP HOLE IAW SRM 53-2-0 FIG 1B. FABRICATED DOUBLER IAW SRM 53-2-0 FIG 1B. TREATED AND PAINTED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1B. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800008 20010418 00008 WP 2001 4 18 DHL2001806546 1 20010318 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - MAIN CARGO AFT BULKHEAD INTERCOASTAL DOUBLER CRACKED 1 INCH AT STA 1760.00 L-6R. STOP DRILLED IAW SRM 53-2- 0 FIG 18. FABRICATED DOUBLER IAW SRM 53-2-0 FIG 1B. TREATED, PRIMED IAW SRM 51-1-8B AND INSTALLED DOUBLER IAW SRM 53-2 -0 FIG 1B. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800010 20010418 00010 WP 2001 4 18 DHL2001806547 1 20010312 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - MAIN CARGO 1 INCH CRACK IN CENTRAL WING FLOOR ''D'' STA 878.000. CUT OUT DAMAGED AREA OF FLOOR PANEL ''D'' A T STA 878 FABRICATED FILLER AND DOUBLER IAW SRM 53-2-3 PAGE 39/40 CLEANED, TREATED & PRIMED IAW SRM 51-1-8B PAGE 1-12. INSTALLED FILLER AND DOUBLER IAW SRM 53-2-3 PAGE 39/40, SRM 51-1-15 PAGE 1, SRM 51-1-21 PAGE 1. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800011 20010418 00011 WP 2001 4 18 DHL2001806548 1 20010316 A 5320 ANGLE DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - MAIN CARGO COMPT FLOOR E COUPLING ANGLE CRACKED 1 INCH STA 720.00. REMOVED ANGLE DETERIORATED IAW SRM 51-3-0 . FABRICATED ANGLE IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED, AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE IAW SRM 53-2- 0 FIG 1B. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800012 20010418 00012 WP 2001 4 18 DHL2001806549 1 20010313 A 2550 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECKED - MAIN CARGO 2 INCH CRACK IN CENTRAL WING FLOOR D STA 866.00. CUT OUT DAMAGED AREA OF FLOOR PANEL D AT STA 86 6.00, FABRICATED FILLER & DOUBLER ANGLES IAW SRM 53-2-3 PAGE 39, 40. CLEANED, TREATED, & PRIMED IAW SRM 51-1-8B. INS TALLED FILLER & DOUBLER & ANGLES IAW SRM 53-2-3 PAGE 39, 40. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800013 20010418 00013 NM 2001 4 18 DHL2001742004 1 20010411 A 5320 SILL BOEING 727 727225 1384077 NM CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AFT BAGGAGE PIT DOOR FWD SILL PLATE FWD CORNER CRACKED. DEFFERD PER GMM 3.5 CAT 1 REF GMM 20.2 PAGE 1 PARAG C ITEM C ON DMI 5135E.THIS SDR REMAINS OPEN. 2 L 7 3 4F A3WE 2001041800015 20010418 00015 WP 2001 4 18 DHL2001806500 1 20010304 A 5320 SUPPORT BRACKET DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - FWD CARGO COMPT SIDE WALL SUPPORT ANGLE CRACKED 1/2 INCH AT STATION 180 L-31 RT. CORRECTIVE ACTION: PERFORMED STOP HOLE, FABRICATED REINFORCING ANGLE (STEEL 301, 1/2 H, 0.032 INCH) AND INSTALLED IAW SRM 53-2-0, FIG. 1B. STATUS - CLOSED 2 L 7 4 4F RT 4A25 2001041800016 20010418 00016 NM 2001 4 18 DL73K010381 1 20010307 A 3310 20131A BATTERY PACK BOEING 737 737247 138448D NM CABIN DISCHARGED A DALA O OTHER O OTHER CR CRUISE 1 SO 27 375DL 23602 PASSENGER SEAT 17C AND ALL SEAT EPATH LITES AFT OF IT ARE INOP. FOUND BATTERY PACK INOP. DAL P/N 337101963 2 L 7 2 4F A16WE 2001041800017 20010418 00017 NE 2001 4 18 DL76L010382 2 20010308 A 7314 82550112 PUMP BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE LOOSE A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 187DN 17347 27582 727621 A/C DIV SNN DUE FUEL QTY DISCREPANCY BETWEEN FUEL TOTALIZER AND FMS FUEL REALITY. INCREASE THROUGH OUT FLT ACCOMPANIED BY INCREASING FUEL IMBALANCE WITH EXCESSIVE CONSUMPTION FROM RT WING. FOUND 2 EA FASTENER LOOSE AT FUEL PUMP FLANG FITTI NG AFT LINE TO FUEL OIL COOLER OUTLET. REMOVED LINE AT PUMP CONNECTOR AND FOUND PACKING DAMAGED. REPLACED PACKING AND SE CURED FLANGE BOLTS. ENG RUN LK CK NO LKS FOUND. PUMP AND ATTACHING BOLTS REMOVED FOR EVALUATION. 2 L 7 2 4F 4 F RT A1NM E24NE 2001041800018 20010418 00018 NM 2001 4 18 DL767010383 1 20010308 A 3260 387 BULB BOEING 767 767232 1385132 NM MLG INDICATOR BURNED OUT A DALA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SO 27 108DL 22220 LT MAIN LANDING GEAR NOT INDICATING GREEN WHEN LANDING GEAR IS DOWN AND LOCKED. RELAMPED LT MAIN GEAR DOWNLOCK GREEN LI TE RECONFIGED A/C TO NORM GEAR MODE ALL CKS OK 2 L 7 2 4F RT A1NM 2001041800019 20010418 00019 NM 2001 4 18 DL733010386 1 20010307 A 2497 WIRE BOEING 737 737330 NM OVERHEAD CHAFED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 241DL 23833 ON TOUCHDOWN SHOWER OF SPARKS FROM O/H PANEL BETWEEN F/C GALLEY AND FLT DECK.CONTRACT MTC FOUND WIRE BUNDLE W132 BURNE D. FOUND SAME WIRING BUNDLE RUBBING ON PANEL LATCH CAUSING WIRES TO SHORT OUT. REPAIRED WIRING. 2 L 7 2 4F RT A16WE 2001041800020 20010418 00020 2001 4 18 DL76S010388 4 20010310 A 3410 PROBE BOEING 767 767332 1382001 NM LT NOSE AREA MALFUNCTIONED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 124DE 23438 RTB FOR INSP. DUE TO SMOKE COMING FROM LT NOSE AREA OVER RADOME. J/C VISUAL INSPECTION OF NLG AREA, FWD AND MAIN E/E C OMPARTMENTS. ALSO VISUALLY INSPECTED OF LT / RT ACM AREAS AND RADAR ANTENNA AREA. NO ANOMALIES NOTED-ALL HYD QTYS NORMA L, NO HYD LEAKS FOUND. REPLACED TAT PROBE AS PRECAUTION PER M/M. PERF CADC BITE TEST. NO ABNORMAL CONDITIONS NOTED. RAN BOTH ACMS AND PNEU.SYS, ALL CK NORMAL 2 L 7 2 4F RT A1NM 2001041800021 20010418 00021 NM 2001 4 18 DL76L010389 1 20010310 A 2121 FAN BOEING 767 767332 1382001 NM E/E BAY OVERHEATED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 183DN 27110 AFTER APPROX 5 HRS FLT TIME AT FL 310 NOTICED VERY FAINT ELECTRICAL SMELL. 5 MINS LATER L REC FAN EICAS MSG AND INOP LT IN LT RECIRC FAN SW CAME ON CB DNOT POP. CA - FOUND CB BOPPED ON CB PANEL IN MEC RMVD AND REPLD LT RECIFAN OPS CK GOOD ALL CBS RESET. 2 L 7 2 4F RT A1NM 2001041800022 20010418 00022 NE 2001 4 18 DLM88010390 2 20010310 A 7320 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE CRACKED A DALA F ACTIVATE FIRE EXT. R PARTIAL RPM/PWR LOSS LD LANDING 1 SO 27 963DL 31975 0 49982 718044 FLIGHT CREW REPORTED NR 1 LOST POWER ABOUT 15 MILES OUT OF CAE ENGINE WAS NOT SHUT DOWN UNTIL AFTER TOUCHDOWN. DURNING I NSP MTC FOUND FUEL MISTING INTO THE COLD STREAM ON START ATTEMPT. PRIMARY FUEL MANIFOLD CRACKED. REPLACED SAME 2 L 7 2 4F 4 F RT A6WE E9NE 2001041800023 20010418 00023 NM 2001 4 18 DL76K010391 1 20010310 A 3350 LP7265001 LIGHT BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 171DZ 29690 ON L/O FOUND EMERGENCY EXIT LIGHTS OUT AT SEATS 11FG,26AB,36AB. RELAMPED EMERGENCY EXIT LIGHTS AT SEATS 11FG, 26AB,36AB , OPS CK. GOOD. 2 L 7 2 4F RT A1NM 2001041800024 20010418 00024 NM 2001 4 18 DL72S010392 1 20010310 A 3350 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 533DA 22046 ON L/O FOUND FWD ESCAPE PATH FLOOR LIGHTS ROWS 20 TO 26 INOPERATIVE. SECURED CONNECTON AT SEAT 20D AND REPLACED BATTERY M9027 PACK- OPS NML NOW. 2 L 7 3 4F A3WE 2001041800025 20010418 00025 NM 2001 4 18 DLM88010393 1 20010310 A 3350 FUSE DOUG MD88 MD88 3023688 NM POWER SUPPLY BLOWN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 969DL 53172 ON L/O FOUND FWD CBN WHITE EMERGENCY LIGHTS INOP AT SEAT ROWS 10,11,12,13. REPAIRED DAMAGED WIRE AT SEATROW 1R--RPLCD PWR SUPPLY PER M/M. ALL LIGHTS CK GOOD 2 L 7 2 4F RT A6WE 2001041800026 20010418 00026 2001 4 18 DL757010395 4 20010311 A 2565 GIRT BAR BOEING 757 757232 1384965 NM PAX DOOR BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 646DL 24217 L 4 DOOR GIRT BAR BROKEN AND GUST ASSIST BOTTLE ACTIVATED C/A REPLACED L 4 DOOR GIRT BAR AND DOOR ASSIST BOTTLE. REPL ACED L4 DOOR SLIDE PRECAUTIONARY. (IT DID NOT DEPLOY,DUE TO MALFUNCTIONING GIRT BAR.) ORIGINAL PROBLEM WAS FLT ATT COUL D NOT ARM L4 DOOR. BWI MTC ARMED DOOR AND OPENED, ACTIVATING ASSIST BOTTLE. A/C FERRIED TO ATL FOR MTC. 2 L 7 2 4F RT A2NM 2001041800027 20010418 00027 WP 2001 4 18 DLL10010397 1 20010311 A 2530 OVEN LKHEED 1011 10113851 5265010 WP GALLEY OVERHEATED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 730DA 193C1199 TWO PBES USED DUE SMOKE FROM OVERTEMP OVENS IN LOWER GALLEY- PLS REPLACE PBES ATL MAINT F/A TOOK 2 CABIN PBES TO LO WER GALLEY PLS CHECK ALL PBES FOR PROPER LOCATION. CA-AS PER F/A VERBAL OVENS ON FOR EXTENDED PERIOD DUE TO FROZEN MEA LS. INSPECTED OVENS FOUND 6 OVERHEAT WD TRAPPED. RESET SAME OPS CKD OVEN. CKS OK. REPLACD PBE KITS. 2 L 7 3 4F A23WE 2001041800028 20010418 00028 NM 2001 4 18 DL72W010399 1 20010311 A 2910 651782119 MODULE BOEING 727 727247 138408F NM MLG FAILED A DALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 2816W 20872 LOSS OF SYSTEM A FLUID AND PRESSURE SHORTLY AFTER LDG GEAR WAS SELECTED DN. ALL 3 GREEN DN LOCK LGTS ILLUM AND RED DR L GT REMAINED ILLUM. THE L/R GEAR DR AND TAIL SKID AMBER ANNUNCIATORS ON S/O PNL REMAINED ILLUM. FOLLOWED HYD LOSS PRO CEDURES PER POM. UNEVENTFUL FLAP 15 LDG. FOUND A SYSTEM HYD PRESSURE MODULE CHECK VALVE FAILED. FAILED VALV E ALSO DAMAGED AN A SYSTEM RETURN LINE. RPLACED PRESSURE MODULE AND INSTALLED TEMPORARY LINE. 2 L 7 3 4F A3WE 2001041800029 20010418 00029 NM 2001 4 18 DL764010400 1 20010311 A 3350 SOCKET BOEING 767 767* NM CABIN CORRODED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 834MH 29707 DURING PRE-DEPARTURE CHECK FOUND LT OVERWING EXTERIOR EXIT EMERGENCY LIGHT BULB INOP. REPLACED BULB AND BULB HOLDER. O PS NORMAL. USED SPARE BULB HOLDER. BULB HOLDER AND BULB HAD CORROSION RENDERING LIGHT INOP. 2 L 7 2 4F RT A1NM 2001041800030 20010418 00030 NM 2001 4 18 DL72W010401 1 20010312 A 5312 6516312180 BULKHEAD BOEING 727 727247 138408F NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W 21057 CRACKS WERE FOUND IN THE WEBS AND FAIL SAFE CHORDS OF THE FS294.5 BULKHEAD. CRACKS WERE EMANATING FROM FASTENER LOCATI ONS AT WL 180 AND LBL 14. ONE WEB AND THE CHORDS WEREREPLACED AND ONE OF THE WEBS WAS SPLICED. THE DAMAGE WAS FOUND AT HMV. 2 L 7 3 4F A3WE 2001041800031 20010418 00031 NM 2001 4 18 DL72W010402 1 20010312 A 5311 651634021 FRAME BOEING 727 727247 138408F NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W 21057 CRACKS WERE FOUND IN TWO LOCATIONS OF THE FS 990 FRAME. ONEWAS AT STR 28R AND THE OTHER AT STR 29R. THE CRACKS WERE CUT OUT AND A DOUBLER INSTALLED. THE DAMAGE WAS FOUND AT HMV. 2 L 7 3 4F A3WE 2001041800032 20010418 00032 NM 2001 4 18 DLM11010403 1 20010310 A 3520 OXYGEN MASK DOUG MD11 MD11 3023602 NM CABIN DEPLOYED A DALA G O2 MASK DEPLOYED O OTHER TX TAXI/GRND HDL 1 SO 27 812DE 48601 UPON ENGINE SHUT DOWN ALL OVERHEAD MASKS DEPLOYED WITH AIR SYSTEM IN MANUAL AT AC POWER TRANSFER - NO FAULTS FOUND - UNA BLE TO DUPLICATE 2 L 7 3 4F RT A22WE 2001041800033 20010418 00033 2001 4 18 DHL2001807008 4 20010406 A 2211 2588788905 COMPUTER DOUG DC8 DC873 302199C WP AUTOPILOT UNSERVICEABLE A DHLA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 01 807DH 45990 AUTOPILOT OVER BANKS IN TURNS AND OVERTURNS BY 15 DEG. AND GAINS 100 FT IN TURNS AND LOSES 150 FT IN ROLLOUT. R&R ROLL C HANNEL COMPTR IAW 22-12-0 CHECKED OPERATION OK. 2 L 7 4 4F RT 4A25 2001041800034 20010418 00034 NM 2001 4 18 DHL2001724003 1 20010409 A 5312 PRESSURE PANEL BOEING 727 727228 NM NLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 A-CHECK - FOUND CONFIRMED CRACK LT SIDE OF NLG WW 10 INCHES FWD OF CENTER BULKHEAD, 2 INCHES ABOVE AND 5 INCHES FWD OF D OOR COUNTER WEIGHT, BETWEEN STA 283 TO 286. APPROX 4 INCHES LONG. STOPPED DRILL CRACK IAW 6727 SRM 51-10-1. INSTALLED REPAIR DOUBLER IAW B727 SRM 51-30-2. PRESSURIZATION OF REPAIR AND ACCESS PANEL. OPS CHECK, OK. STATUS-CLOSED. 2 L 7 3 4F A3WE 2001041800035 20010418 00035 WP 2001 4 18 DHL2001806533 1 20010310 A 5530 ANGLE DOUG DC8 DC873F 302199F WP VERTICAL STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - VERT. STAB. LE INNER RIB REINFORCING ANGLE CRACKED 1/2 INCH ZF 86.000 RT. REMOVED CRACK REINFORCING ANGLE IAW SRM 51-1-21 PAGE 1. FABRICATED ANGLE IAW SRM 55-1-1 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 5-1-8B. INSTALLED ANGLE IAW SRM 51-1-21 PAGE 1. STATUS CLOSED. 2 L 7 4 4F RT 4A25 2001041800036 20010418 00036 WP 2001 4 18 DHL2001806534 1 20010317 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - FWD. CARGO COMPT. FLOOR SUPPORT ANGLE CRACKED 2 INCH AT STA 580. L-34 LT. PERFORMED STOP HOLE. FABRICATED D OUBLER AND INSTALLED IAW SRM 53-2-0 FIG 1B. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800037 20010418 00037 WP 2001 4 18 DHL2001806535 1 20010312 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - FWD CARGO COMPART. FLOOR SUPPORT ANGLE CRACKED 1 INCH AT STA 600. L-35LT. PERFORMED STOP DRILL IAW SRM 53-1-0 FIG 1B. FABRICATED REINFORCING ANGLE IAW SRM 53-2-0 FIG 1B. INSTALLED REINFORCING ANGLE IAW SRM 53-2-0 FIG 1B. STATU S-CLOSED. 2 L 7 4 4F RT 4A25 2001041800038 20010418 00038 WP 2001 4 18 DHL2001806536 1 20010310 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - FWD CARGO COMPARTMENT LT FLOOR SUPPORT ANGLE CRACKED 3 INCH AT STA 520.00 L-33L TO L34L. STOP DRILLED AND FA BRICATED DOUBLER AND INSTALLED IAW SRM 53-2-5 PAGE 6M. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800039 20010418 00039 NM 2001 4 18 DL72W010404 1 20010311 A 5753 6519270 SHIM BOEING 727 7272Q8 138407W NM RT WING TE FLAP LOOSE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831L 21826 INSPECTIONS OF THE INBD FLAP INBD TRACK ON THE RT WING PER AD 90-07-05 REVEALED A LAMINATED SHIM WHICH HAD MIGRATED MOR E THAN THE .25 INCH ALLOWED. THE MIGRATED SHIM WAS REMOVED AND REPLACED AND THE ATTACH BOLTS RE-TORQUED PER THE REQUIREMENTS ON THE AD AND ER/A 380279-14AD. 2 L 7 3 4F A3WE 2001041800040 20010418 00040 NM 2001 4 18 DL757010405 1 20010312 A 2120 UNKNOWN BOEING 757 757232 1384965 NM CABIN ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 687DL 27586 DURING CRUISE FLT FLT. ATTNDS. RERORTED OIL ODOR IN AFT GALLEY. APU WAS NOT RUNNING. UPON FLT ARRIVAL AND AFTER 15/30 MINS. FROM ENG SHUTDOWN INSPS OF INLET/EXHAUST AND EXTERNAL LEAKS OF BOTH ENG OK. BOTH ENGS OIL QTY CK FULL -MTC FOUND N O HISTORY CHAPTS 21-36 OR ENGS GROUPS ATA -OIL CONSUMPTION RECORDS GOOD -NO ODORS AT GATE MCO-INSP OF AFT GALLEY AND EQ . OK. 2 L 7 2 4F RT A2NM 2001041800041 20010418 00041 NM 2001 4 18 DL73K010406 1 20010309 A 5330 654658531 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 301DL 23073 FUSELAGE / FS 1138 / STRG. 12R / HORIZ STAB CUTOUT : CRACK REPAIR INSPECTIONS OF THE FUSELAGE STRUCTURE AROUND THE HORIZ ONTAL STABILIZER CUTOUT PER BAC S/B 737-53-1134 REVEALED A .5 INCH CRACK IN THE SKIN AND UNDERLYING STRINGER STRAP JUST FWD OF FS 1138 AND JUST ABOVE STRINGER 12R. A 3 INCH CRACK WAS FOUND IN THE STRINGER STRAP AND FRAME STRAP AT THE FS 1 138 FRAME AND S-12R INTERECTION. THE SKIN WAS CUTOUT AND NEW SECTIONSOF STRINGER AND FRAME STRAP SPLICED IN PER ER/A 380 221-14. 2 L 7 2 4F RT A16WE 2001041800042 20010418 00042 NM 2001 4 18 DL73K010407 1 20010312 A 3040 CONTROLLER BOEING 737 737232 1384475 NM WINDOW HEAT FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 304DL 23076 ELECTRIAL CONNECTOR TO RIGHT FWD WINDOW BEGAN SMOKING, TURNED OFF WINDOW HEAT SMOKE STOPPED. / REPLACED R1 WINDOW AND W INDOW HEAT CONTROLLER PER M/M. OPNL TEST OF WINDOW HEAT GOOD 2 L 7 2 4F RT A16WE 2001041800043 20010418 00043 NM 2001 4 18 DL75A010409 1 20010312 A 3350 WIRE BOEING 757 757212 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 750AT 23126 EMERGENCY LIGHT INOP AT SEAT ROW 33DEF. REPAIRED BROKEN WIRE AT SEAT ROW 33DEF, EMERGENCY LIGHT OPS CK. GOOD 2 L 7 2 4F RT A2NM 2001041800044 20010418 00044 2001 4 18 DLM11010410 4 20010312 A 2210 FUEL CONTROL DOUG MD11 MD11 3023602 NM AUTOPILOT FAILED A DALA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 27 807DE 48478 ON TAKE OFF AFTER PROF SELECTED AT 1000FT AGL AUTO THROTTLES RETARDED THROTTLES 1 AND 3 - REPLACED FCC 1 2 L 7 3 4F RT A22WE 2001041800045 20010418 00045 2001 4 18 DHL2001727004 4 20010406 A 2211 25858027 CONTROLLER BOEING 727 727228 NM COCKPIT FAILED A DHLA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SO 01 727DH 20204 AUTOPILOT MANUAL PITCH CONTROL DOES NOT MAINTAIN CONSISTENT CLIMBS OR DECENTS. REMOVED AND REPLACED AUTO PILOT HEAD PANE L PER B727 M/M SEC 22-11-181, OPS CK. GOOD. 2 L 7 3 4F A3WE 2001041800046 20010418 00046 NE 2001 4 18 DL757010411 2 20010313 A 7310 PW2037RTC ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 MALFUNCTIONED A DALA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 686DA 44846 0 27589 716326 ON TAKEOFF ROLL LEFT ENGINE DID NOT REACH TAKEOFF POWER LEFT ENGINE INDICATED 1.09 EPR RIGHT ENGINE 1.26 EPR TRIED TO R UN UP LEFT ENGINE FARTHER LEFT OIL PRESSURE RED WARNING INDICATED HIGH OIL PRESSURE STOPPED TAKEOFF ROLL AT VERY LOW SPE ED LESS THAN 40 KNOTS. FOUND CUT O RING BETWEEN FUEL FLOW TRANSMITTER AND FUEL DISTRUBUSTION MANIFOLD LINE REPLACED O-R ING RAN PER PFHB ALL IND NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041800047 20010418 00047 NM 2001 4 18 DLM90010413 1 20010312 A 2822 PUMP DOUG MD90 MD9030 3023690 NM FUEL BOOST FAILED A DALA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 SO 27 908DA 53388 BOTH CENTER BOOST PUMP B PHASE C/BS POPPED IN FLIGHT. TRIED RESETTING BUT POPPED AGAIN. TROUBLESHOOTING CNTR BOOST PUMP C/BS POPPING. REPLACED BOTHCNTR BOOST PUMPS. OPS CHECKS NORMAL AND ACCESS PANELS INSTALLED. 2 L 7 2 4F RT A6WE 2001041800048 20010418 00048 NM 2001 4 18 DL76S010414 1 20010312 A 5330 146T32621 SKIN BOEING 767 767332 1382001 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 122DL 23436 THE FUSELAGE SKIN WAS FOUND WITH A 9.5 INCH CRACK ADJACENT TO THE LOWER AFT VHF ANTENNA AT FS 1197+95 BETWEEN STRINGERS 39L & 39R. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 380276-14, REV A. 2 L 7 2 4F RT A1NM 2001041800049 20010418 00049 NM 2001 4 18 DL757010415 1 20010313 A 3340 331001542 LIGHT BOEING 757 757232 1384965 NM EXTERIOR BURNED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 675DL 25980 AFTER GEAR RETRACTION AND EXTENSION, A VERY STRONG ODOR OF BURNING RUBBER FILLED COCKPIT AND CABIN. ALL INSTRUMENT IND ICATIONS NORMAL. FOUND RT RUNWAY TURNOFF SWITCH FUSED. REPLACED PANEL, NO FURTHER SMELL. INSPECTED WHEEL WELLS, WHEEEL S, TIRES AND BRAKES ALL O.K. A/C O.K. FOR SERVICE. 2 L 7 2 4F RT A2NM 2001041800050 20010418 00050 NM 2001 4 18 DLM88010416 1 20010313 A 3350 HARNESS DOUG MD88 MD88 3023688 NM CABIN DISCONNECTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 907DL 49538 SEAT 34C/D WIRE HARNESS LOOSE ON FLOOR. FOUND BY FAA INSPECTOR. DETERMINED SEAT EMERGENCY LIGHTING WIRE HARNESS DISCONNE CTED BETWEEN ROW 31C/D AND 34C/D. RECONNECTED AND SECURED WIRING. ALL EMERGENCY LIGHTS NOW CHECK NRML. 2 L 7 2 4F RT A6WE 2001041800051 20010418 00051 NM 2001 4 18 DL73K010417 1 20010313 A 5330 SKIN BOEING 737 737247 138448D NM WINDOW BELT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 381DL 23608 FOUND ON O1 LETTER CK 1/4 MIN CRACK IN L-1 WINDOW CUTOUT AT UPPER OUTBD CORNER. REPAIRED PER SRM 53-30-3. 2 L 7 2 4F A16WE 2001041800052 20010418 00052 NM 2001 4 18 DL757010418 1 20010313 A 2420 INVERTER BOEING 757 757232 1384965 NM CABIN ODOR A DALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DE DESCENT 1 SO 27 6704Z 30396 ON INITIAL DESCENT STBY INVERTER STATUS MESSAGE APPEARED FOLLOWED BY FAINT ODOR THROUGHOUT CABIN. C/A REPLACE D STATIC INVERTER 2 L 7 2 4F RT A2NM 2001041800053 20010418 00053 NM 2001 4 18 DL72S010419 1 20010313 A 3350 LIGHT BOEING 727 727232 1384082 NM CABIN WILL NOT TEST A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 516DA 21432 EMERG LIGHT AT REAR EXIT WOULD NOT TEST - REPLACED LIGHT RACK 2 L 7 3 4F A3WE 2001041800054 20010418 00054 NM 2001 4 18 DL73E010420 1 20010311 A 5311 6516300301 FRAME BOEING 737 737247 138448D NM BULKHEAD CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 380DL 23607 THE FS 178 BULKHEAD LT AND RT SIDE CHORDS WERE FOUND CRACKEDWHILE ACCOMPLISHING INSPECTIONS PER S/B 737-53A1173. THE CHO RDS WERE REPLACED PER ERA 397346-14AD AT CV. 2 L 7 2 4F A16WE 2001041800055 20010418 00055 NM 2001 4 18 DL733010421 1 20010314 A 5330 6545800602 SKIN BOEING 737 73735B NM FUSELAGE PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 222DZ 23971 THE FUSELAGE SKIN WAS DAMAGED BY GROUND EQUIPMENT BETWEEN FS 312 & 331 AND BETWEEN STRINGERS 21R & 22R. THE DAMAGE WAS REMOVED WITH A 17 INCH X 6 INCH CUTOUT. THE CUTOUT WAS REPAIREDWITH AN EXTERNAL ALUMINUM DOULBER INSTALLED PER ER/A 380282-14, REV A. 2 L 7 2 4F RT A16WE 2001041800056 20010418 00056 EU 2001 4 18 RAIA00103015 1 20010323 A 7722 30238452 TERMINAL JETAIR JETSTM JETSTM4101 1500501 EU RT EGT DEFECTIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 558HK 41071 EWR- DURING TAXI RIGHT HAND IEC CAPTION ILLUMINATED/RIGHT HAND ENGINE EGT FLUX. MAINTENANCE REMOVED AND REPLACED RIGHT HAND ENGINE EGT HARNESS TERMINAL IAW J41 MAINTENANCE MANUAL. 2 L 7 2 4T RT A41NM 2001041800057 20010418 00057 EU 2001 4 18 DHL2001363002 1 20010323 A 2761 3050544 ACTUATOR AIRBUS 300 A300B4203 3930306 EU RT SPOILER FAILED A DHLA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 363DH 085 RIGHT SPOILER STUCK AT 15 DEG. DEFERRED RIGHT OUTBOARD ROLL SPOILER IAW MEL 27-62-01-1. DMI 4859. 2 L 7 2 4F RT A35EU 2001041800058 20010418 00058 WP 2001 4 18 DHL2001804001 1 20010407 A 2612 FIRE LOOP DOUG DC8 DC873F 302199F WP NR 2 ENGINE MALFUNCTIONED A DHLA E J B A ENGINE SHUTDOWN DUMP FUEL EMER. DESCENT UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 804DH 46124 RECEIVED FIRE WARNING, ENGINE NR 2 DURING CRUISE. FOLLOWED PROCEDURE AND SECURED ENGINE. WARNING DID NOT REAPPEAR (ALL ENGINE INSTRUMENTS NORMAL DURING EVENT). R&R LEFT O/B FIRE BOTTLE AND DEFEARED B LOOP. STATUS-OPEN. 2 L 7 4 4F RT 4A25 2001041800059 20010418 00059 NM 2001 4 18 DL733010396 1 20010311 A 2130 SENSOR BOEING 737 7373B7 1384580 NM RIGHT PACK FAILED A DALA O OTHER G MULTIPLE FAILURE CL CLIMB 1 SO 27 951WP 22951 IR - AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. CABIN CLIMBED AT 1500-2000 FPM. OUTFLOW VLV SHOWED FULL CLOSED AND ST BY MODE NO CHANGE. CABIN PRESSURE STABILIZED AT SAME FLT LEVEL. CA - FOUND RIGHT PACK 35 DEGREE TEMP INOP. REPLACED SA ME. 2 L 7 2 4F RT A16WE 2001041800060 20010418 00060 SO 2001 4 18 C2XA01TY058 1 20010323 A 5311 14521446413 FRAME EMB 145 EMB145LR SO FUSELAGE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13978 145180 TYS DURING A SCHEDULED INSPECTION, FRAME NR 80 WAS FOUND TO BE CHAFED BY THE APU FIRE BOTTLE DISCHARGE LINE. MAINTENAN CE REPAIRED FRAME NR 80 IAW EMB-GST-0872/01, REPAIR WAS SATISFACTORY. AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSP ECTION. 2 L 7 2 4T RT T00011AT 2001041800061 20010418 00061 WP 2001 4 18 ABXA010106 1 20010324 A 2611 100012703 CONTROL UNIT DOUG DC9 DC932 3022066 WP FIRE DETECTION FAULTY A ABXA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 903AX 332 47427 A LOWER CARGO FIRE ANNUNCIATOR ILLUMINATED ON SHORT FINAL APPROACH. THE FLIGHT CREW DECLARED AN EMERGENCY AND LANDED WI THOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND DEFERRED THE CARGO SMOKE DETECTION SYSTEM IAW DC-9 MEL. ON 03/25/01, MAINTENANCE REPLACED THE SMOKE DETECTOR CENTRAL CONTROL UNIT AND REMOVED THE DEFERRAL. 2 L 7 2 4F A6WE 2001041800062 20010418 00062 NM 2001 4 18 DL72W010423 1 20010314 A 5754 ANGLE BOEING 727 727247 138408F NM NR 8 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 294WA 22112 COVE SKIN ATTACH ANGLE CRACKED BELOW TAI DUCT NBR 8 SLAT. REPAIR PER MM 57-54-000-8 2 L 7 3 4F A3WE 2001041800063 20010418 00063 NM 2001 4 18 DL72S010424 1 20010314 A 3350 900835A BATTERY PACK BOEING 727 727225A 1384077 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8891Z 21860 RT WING EMERG EXIT EXTERIOR LITE INOP REPLACED BATTERY PACK RT WING EMERG EXIT-OPS CKS GOOD 2 L 7 3 4F RT A3WE 2001041800064 20010418 00064 NM 2001 4 18 DLM90010425 1 20010314 A 2740 JACKSCREW DOUG MD90 MD9030 3023690 NM HORIZONTAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 902DA 53382 HORIZONTAL STAB JACKSCREW FAILED OPEN 5936AD INSPECTION. LIGHT CORROSION FOUND ON LOWER 4 THREADS OF JACKSCREW CA: REPL ACED JACKSCREW ASSY 2 L 7 2 4F RT A6WE 2001041800065 20010418 00065 2001 4 18 DL757010426 4 20010315 A 3442 TRANSCEIVER BOEING 757 757232 1384965 NM WX RADAR FAILED A DALA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 SO 27 652DL 24392 TCAS AND WX RADAR DISPLAYS INOP. TCAS DISPLAY STUCK IN 10M RANGE. ABOVE AND BELOW SW. INOP. UNABLE TO GET ANY WEATHER INFORMATION. REPLACED WX RADAR TRANSCEIVER AND WX RADAR INDICATOR, SYS. GROUND CHECKS NORMAL 2 L 7 2 4F RT A2NM 2001041800066 20010418 00066 NM 2001 4 18 DL733010427 1 20010314 A 5311 FRAME BOEING 737 737347 1384647 NM BULKHEAD CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3301 23181 THE LT AND RT SIDE CHORDS OF THE FS 178 BULKHEAD WERE FOUND CRACKED NEAR WL 207. THE CRACKS ARE LESS THAN 3 INCHES IN L ENGTH.THE CRACKS WERE STOP DRILLED AND REPAIRED WITH A TEMPORARY ANGLE REPAIR PER B737-300 SRM 53-10-08, FIG. 208 AND E R/A 380283-14AD. 2 L 7 2 4F RT A16WE 2001041800067 20010418 00067 NM 2001 4 18 DL72W010428 1 20010314 A 5312 BULKHEAD BOEING 727 727247 138408F NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 294WA 22112 THE FS 1183 BULKHEAD WEB WAS FOUND WITH A 1 INCH LONG CRACK AT RBL 26 AND WL 169. THE CRACK WAS STOP DRILLED AND REPAI RED WITH A TITANIUM DOUBLER PER ER/A 380315-14. 2 L 7 3 4F A3WE 2001041800068 20010418 00068 CE 2001 4 18 C2XA01CL065 1 20010324 A 2612 24412886 FIRE LOOP BEECH 1900 1900D 1154162 CE RT ENGINE BROKEN A C2XA E ENGINE SHUTDOWN N FALSE WARNING AP APPROACH 1 SW 27 87557 UE246 CLE FLIGHT 3032 THE CREW REPORTED THE RIGHT FIRE LOOP AND FIRE T-HANDLE FLICKERED DURING FLIGHT FOR ABOUT 30 SECONDS AND STOPPED. ON FINAL APPROACH THE T-HANDLE STAYED ILLUMINATED AND THE MASTER WARNING ILLUMINATED. THE AIRCRAFT LANDED WI THOUT FURTHER INCIDENT AND THE CREW SHUT DOWN THE RIGHT ENGINE ON THE RUNWAY. THE CREW REPORTED THERE WAS NO FIRE DETEC TED. MAINTENANCE INSPECTED AND FOUND THE RIGHT FIRE LOOP TO BE BROKEN. THE FIRE LOOP WAS REPLACED AND OPERATIONAL CHEC KS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 2001041800069 20010418 00069 NM 2001 4 18 SWAA010697 1 20010308 A 3350 079123 COVER BOEING 737 7373A4 1384585 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 EEPLS TRACK COVER LOOSE AT ROW 3. SECURED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001041800070 20010418 00070 NM 2001 4 18 SWAA010698 1 20010308 A 3350 079123 COVER BOEING 737 7375H4 138449D NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 506SW 24183 EEPLS TRACK COVER MISSING AT MID CABIN. INSTALLED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001041800071 20010418 00071 NM 2001 4 18 SWAA010699 1 20010308 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 515SW 25154 EEPLS INOP AT ROW 11. REPAIRED EEPLS WIRING PER MM. 2 L 7 2 4F RT A16WE 2001041800072 20010418 00072 NM 2001 4 18 DL72S010429 1 20010315 A 2530 5334E OVEN BOEING 727 727232 1384082 NM GALLEY INOPERATIVE A DALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 534DA 22047 AIR-TURN-BACK DUE TO ELECTRICAL BURNING SMELL IN FWD GALLEY AREA. SLC MECHANIC FOUND FWD GALLEY OVEN TO BE THE CAUSE. REPLACED GALLEY OVEN. 2 L 7 3 4F A3WE 2001041800073 20010418 00073 NM 2001 4 18 DL757010430 1 20010314 A 2613 DETECTOR BOEING 757 757232 1384965 NM OVERHEAT FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 621DL 22911 FWD EQUIP COOLING OVERHEAT MSG. EQUIP COOLING SWITCH WILL NOT LATCH IN THE -ALTN- POSITION. REPLACED LOW FLOW SENSOR AN D OVERHEAT DETECTOR 2 L 7 2 4F RT A2NM 2001041800074 20010418 00074 NM 2001 4 18 DL72L010431 1 20010305 A 4990 APU BOEING 727 727232 1384082 NM APU BAY LEAKING A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 502DA 44637 21304 ON GROUND PREFLT OPERATING A/C PACKS CREATES AN ODOR AND HAZE IN AFT CABIN. ALL COCKPIT INDICATIONS NORMAL AFTER PACK OF F. RE-CYCLED LEFT PACK ONLY AND ODOR / HAZE REAPPEARED. CORRECTED OIL LEAK AT APU. 2 L 7 3 4F A3WE 2001041800075 20010418 00075 2001 4 18 DL777010432 4 20010314 A 2220 AUTOPILOT SYS BOEING 777 777232 1385232 NM COCKPIT MALFUNCTIONED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 860DA 29951 ON DECENT, MAX SPEED AUTOPILOT EICAS LT ILLUMINATED. AS WENT ABOUT 2 KNOTS HIGH INTO RED-OVERSPEED WARNING TRIED TO SOUN D BUT WAS MUFFLED SOUNDING. AN ELECTRICAL SMELL ON LEFT SIDE OF COCKPIT WAS NOTICED SUSPECT OVERSPEED SHAKER FAILURE. T/ S AP MTC MSG PER FIM SUGGESTED SEQUENCE ERROR NO ACTION NEEDED FOR FAULT. ALSO PERFORMED WEU SYSTEM TEST ON MAT TO VERIF Y SPEAKER OPN. TEST PASSED PERFORMED STALL WARNING TEST OF STICK SHAKER MOTORS ALL OK. NO ELECTRIC OR BURNING SMELL NOTE D OK FOR SERVICE 2 L 7 2 4F RT T00001SE 2001041800076 20010418 00076 NE 2001 4 18 DLM88010433 2 20010315 A 7250 JT8D219 TURBINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE FAILED A DALA C ABORTED TAKEOFF E J VIBRATION/BUFFET WARNING INDICATION TO TAKEOFF 1 SO 27 996DL 31552 53363 725394 ON TAKEOFF CREW NOTICED NOISE AND VIBRATION WHICH SEEMED TO BE COMING FROM BACK OF ACFT. RT HYD SYS PRESSURE AND QTY LOS T THEN WHILE TURNING DOWNWIND NOTICED RT ENGINE EPR FLUX FOLLOWED BY REV UNLOCK LIGHT AND BLUE LOCKED LIGHT. EXCESSIVE VIBS APPEARED AND CREW DECIDED TO RUN ENGINE AT IDLE DUE TO CONCERNS THAT REV MIGHT HAVE DEPLOYED. ENG NOT SHUT DOWN AN D LANDING NOT HARD. ALTERNATE GEAR EXTENSION ACCOMPLISHED. ENGINE FAILED. NTSB INVESTIGATING. 2 L 7 2 4F 4 F RT A6WE E9NE 2001041800077 20010418 00077 2001 4 18 SWAA010700 4 20010308 A 2565 D31354 SLIDE BOEING 737 7377H4 NM ENTRY DOOR OUT OF TOLERANCE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 796SW 27889 FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001041800078 20010418 00078 NM 2001 4 18 SWAA010701 1 20010308 A 5312 6517583 BULKHEAD BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 513SW 24190 DURING SCHEDULED D-CHECK AT DALFORT, FOUND 2 BS FWD BULKHEAD VERTICAL BEAM WEB CRACKS AT BS 184, RBL 17.1. REPAIRED VER TICAL BEAM WEB PER SWA RA. 2 L 7 2 4F RT A16WE 2001041800079 20010418 00079 NM 2001 4 18 SWAA010702 1 20010308 A 5312 6517583 BULKHEAD BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 513SW 24190 DURING SCHEDULED D-CHECK AT DALFORT, FOUND 2 FWD BULKHEAD VERTICAL BEAM WEB CRACKS BETWEEN BS 179 & BS 183, RBL 17.1. R EPAIRED VERTICAL BEAM WEB PER SWA RA. 2 L 7 2 4F RT A16WE 2001041800080 20010418 00080 NM 2001 4 18 SWAA010680 1 20010307 A 3350 BR2013 LIGHT BOEING 737 7372H4 138448C NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 EEPLS DAMAGED AT ROW 14. REPAIRED EEPLS PER MM. 2 L 7 2 4F A16WE 2001041800081 20010418 00081 NM 2001 4 18 DLM88010434 1 20010315 A 4990 36280 APU DOUG MD88 MD88 3023688 NM APU BAY LEAKING A DALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 976DL 9341 53257 PASSING FL 220 WE GOT A RT ICE PROT TEMP HIGH LIGHT WE CLOSED THE RT CROSSFEED VALVE THEN GOT A RT AIR COND TEMP HILIGHT FOLLOWED BY SMOKE IN THE CABIN AND COCKPIT FOLLOWED CK LIST SMOKE STOPPED. FOUND APU OIL LEAKING INTO APU INLET C/W OP N 5088 UNABLE TO FIND SOURCE OF APU OIL LEAK UNABLE TO CLEAN APU INLET THIS STA T/S PACK SYS RAN ADJUST/TEST AND AUGMENT ATION VALVE CK PER M/M AND PFHB ALL CKS NORMAL. APU FWD TO MCO/PLAC FOR OIL CONTAMINATION. 2 L 7 2 4F RT A6WE 2001041800082 20010418 00082 NM 2001 4 18 DL757010435 1 20010315 A 5330 143N34003 SKIN BOEING 757 757232 1384965 NM FUSELAGE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 604DL 22811 THE FUSELAGE SKIN WAS FOUND DENTED AND GOUGED BETWEEN FS 519& 531 AND BETWEEN STRINGERS 27L & 28L. THE DAMAGED WAS REMOV ED WITH A 10.5 INCH X 4 INCH CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 3801 76-14, REV A. 2 L 7 2 4F RT A2NM 2001041800083 20010418 00083 NM 2001 4 18 DL757010436 1 20010315 A 5330 146N34303 SKIN BOEING 757 757232 1384965 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 604DL 22811 THE FUSELAGE SKIN WAS FOUND DENTED AT FS 1598 JUST BELOW THE STRINGER 20L SKIN LAP SPLICE. THE DENT WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 380096-14, REV B. 2 L 7 2 4F RT A2NM 2001041800084 20010418 00084 NM 2001 4 18 DL733010437 1 20010315 A 5330 654658560 SKIN BOEING 737 737347 1384647 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 302WA 23182 INSPECTIONS OF THE HORIZONTAL STABILIZER CUTOUT SURROUND STRUCTURE REVEALED A CRACK IN THE STRINGER 12L STRAP. ADDIT IONAL TOOLING DAMAGE WAS FOUND ON THE STRINGER 12L UPPER CHORD. THE DAMAGED SECTION OF CHORD WAS REMOVED. THESTRAP WAS REPAIRED WITH A DOUBLER AND A NEW SECTION OF STRINGER CHORD SPLICED WITH AN ALUMINUM ANGLE PER ER/A 380274-14, REV A. 2 L 7 2 4F RT A16WE 2001041800085 20010418 00085 NM 2001 4 18 DL76L010438 1 20010315 A 5315 146T51161 FLOORBEAM BOEING 767 767332 1382001 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 190DN 28447 THE LOWER CHORD AREA OF THE FS 1439 FLOOR BEAM WAS FOUND WITH SEVERAL CRACKS BETWEEN LBL 20 AND LBL 30 CAUSED BY IMPACT WITH CARGO. THE DAMAGED AREA OF LOWER CHORD WAS REMOVED WITH A 7.25 INCH LONG CUTOUT. THE BEAM WAS REPAIRED WITH AN ALUMINUM WEB DOUBLER AND 2 ALUMINUM REPAIR CHANNELS PER ER/A 380302-14, REV A. 2 L 7 2 4F RT A1NM 2001041800086 20010418 00086 NM 2001 4 18 DLM88010439 1 20010316 A 2910 38005041 LINE DOUG MD88 MD88 3023688 NM HYD SYSTEM LEAKING A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 906DL 9208 0 P80426 49537 IRREG: DURING APPROACH TO LANDING WITH WING A/I (TAIL SELECTED) AND APU ON STRONG FUMES IN AFT LAV (CAPTS SIDE) AND SMO KE DET CAME ON - FOUND HYDRAULIC LINE LEAKING IN TAIL COMPARTMENT - TIGHTENED SAME - PERFORMED DUCT BURNOUT 2 L 7 2 4F RT A6WE 2001041800087 20010418 00087 NM 2001 4 18 SWAA010681 1 20010307 A 5330 65C35775 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING WALK AROUND INSPECTION, FOUND 3 EXTERNAL FUSELAGE SKIN CRACK AT BS 760, BELOW STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001041800088 20010418 00088 NM 2001 4 18 SWAA010682 1 20010307 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 386SW 26601 EEPLS WIRES EXPOSED AND NUMEROUS TRACK COVERS MISSING. SECURED WIRING AND INSTALLED TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 2001041800089 20010418 00089 2001 4 18 SWAA010683 4 20010307 A 2565 D31354 SLIDE BOEING 737 7377H4 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 708SW 27842 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001041800090 20010418 00090 NM 2001 4 18 SWAA010684 1 20010307 A 5315 6546804 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 967, RBL 18 TO RBL 28. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F A16WE 2001041800091 20010418 00091 NM 2001 4 18 SWAA010685 1 20010307 A 5311 6546546 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 13R. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2001041800092 20010418 00092 SO 2001 4 18 C2XA01TY056 1 20010322 A 4910 14533997001 FIREWALL EMB 145 EMB145LR SO APU GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13978 145180 TYS DURING A SCHEDULED INSPECTION THE APU FIRE WALL WAS FOUND GOUGED ADJACENT TO THE BYPASS VALVE. MAINTENANCE REPAIRE D THE DAMAGED AREA IAW EMB GST-0429/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF I NSPECTION. 2 L 7 2 4T RT T00011AT 2001041800093 20010418 00093 SO 2001 4 18 C2XA01TY057 1 20010322 A 4910 12015565502 FAIRING EMB 145 EMB145LR SO APU CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13978 145180 TYS DURING A SCHEDULED INSPECTION THE APU COWLING UPPER RIGHT HAND FAIRING WAS FOUND CRACKED ALONG THE ATTACHMENT FLANG E. MAINTENANCE REMOVED AND REPLACED THE FAIRING IAW EMB GST-0835/01 AND EMB-145 CPM-51-21-06. AIRCRAFT WILL BE RELEASE D UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2001041800094 20010418 00094 NM 2001 4 18 DL757010440 1 20010316 A 2421 IDG BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE FAULTY A DALA C ABORTED TAKEOFF H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 SO 27 605DL 22812 716550 AT ROTATION LOST RT GEN AND ASSOCIATED HYD. T/S PER FIM. RPLCD RT GCU & RT IDG PER M/M. IDG LK CKS OK RAN RT ENG, GEN WI LL NOT PICK UP BUS. BITE CKD BPCU, FAULT OPEN PHASE TRIP MAIN BUS. IDG NEEDS DISCONNECT TEST. RPLCD BUS PWR CTL UNIT, R AN ENG, CONNECTED & RAN GEN. LOAD CKS OK.DISCONNECTED GEN & RECONNECTED SAME & LOAD CKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041800095 20010418 00095 NM 2001 4 18 DLM11010441 1 20010316 A 2530 72077500 OVEN DOUG MD11 MD11 3023602 NM GALLEY SMOKE A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 804DE 48475 OVEN MID GALLEY RIGHT SIDE PRODUCES HEAVY SMOKE-MAYBE SPILLED FOOD. CABIN SERVICE CLEANED SPILLED FOOD FROM INTERIOR OF OVEN HEATED OVEN 15 MIN. NO SMOKE 2 L 7 3 4F RT A22WE 2001041800096 20010418 00096 NM 2001 4 18 DL76L010442 1 20010316 A 3350 SOCKET BOEING 767 767332 1382001 NM CABIN SHORTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 188DN 27583 EMERGENCY LIGHTS INOP BOTH SIDES FROM ROW 22-30. FOUND EMERGENCY LTS SOCKET AT SEAT 24AB SHORTING OUT. REPLACED SO CKET ASSY AND REPLACED BLOWN FUSE ON POWER SUPPLYCHARGER. OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 2001041800097 20010418 00097 NM 2001 4 18 DLM88010444 1 20010316 A 5330 ANGLE DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DL 49532 FOUND ON H2 LETTER CK 1 INCH CRACK IN VERT STAB ATTACH STRAP AT AFT SIDE OF CANTED FRAME 1388 LBL12. REPAIRED PER SRM 55 -02 FIG 26. 2 L 7 2 4F RT A6WE 2001041800098 20010418 00098 NM 2001 4 18 DL76S010445 1 20010317 A 2780 SLAT BOEING 767 767332 1382001 NM WING MALFUNCTIONED A DALA O OTHER J WARNING INDICATION DE DESCENT 1 SO 27 117DL 23276 LEADING EDGE ASSYM EICAS MESSAGE CAME ON WITH LEADING EDGE LIGHT AT 250 KTS. FLAP INDICATION SHOWED HALFWAY BETWEEN UP A ND 1 DEG. WITH WING A/I ON. LOWERED FLAPS AND SLATS INSP ALL AREAS NO DEFECTS NOTED. RAN ALL SYST. SEVERAL TIMES OPERAT ION AND INDICATIONS NORMAL 2 L 7 2 4F RT A1NM 2001041800099 20010418 00099 NM 2001 4 18 SWAA010687 1 20010307 A 3350 BR2013 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED A1 CHECK, FOUND EEPLS INOP AT ROW 4. SECURED WIRING CONNECTOR PER MM. 2 L 7 2 4F A16WE 2001041800100 20010418 00100 NM 2001 4 18 SWAA010689 1 20010307 A 5753 6546453 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBD T/E AFT FLAP DELAMINATED AT INBD AFT CORNER. REMOVED AND REPLACED AFT FL AP PER MM. 2 L 7 2 4F RT A16WE 2001041800101 20010418 00101 NM 2001 4 18 SWAA010690 1 20010307 A 3397 BR2013 WIRE BOEING 737 7372H4 138448C NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 073SW 22673 EEPLS WIRING EXPOSED. SECURED WIRING PER MM. 2 L 7 2 4F A16WE 2001041800102 20010418 00102 NM 2001 4 18 SWAA010691 1 20010307 A 5754 6573714 SKIN BOEING 737 7373H4 1384600 NM L/E SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 398SW 27692 DURING SCHEDULED C4 CHECK, FOUND NR 2 L/E SLAT SKIN CRACKED AT 2 FASTENER HOLES, 18 OUTBD OF ACTUATOR. REPAIRED SLAT PE R SRM. 2 L 7 2 4F RT A16WE 2001041800103 20010418 00103 2001 4 18 SWAA010692 4 20010306 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 398SW 27692 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001041800104 20010418 00104 NM 2001 4 18 0100976633 1 20010320 A 2612 FIRE WARNING BOEING 747 747227B 1384888 NM COCKPIT FALSE INDICATION A NWAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 01 633US 21991 DURING TAKEOFF, THE NR 3 ENGINE FIRE DETECTION LIGHT FLICKERED ON AND OFF. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. INSPECTED AND TESTED THE NR 3 ENGINE FIRE DETECTION SYSTEM WITH NO FAULTS FOUND. 2 L 7 4 4F A20WE 2001041800105 20010418 00105 EU 2001 4 18 0100983203 1 20010312 A 2910 D2905880203401 HYDRAULIC LINE AIRBUS 320 A320211 3930320 EU RT WING LEAKING A NWAA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 303US 34 DURING CRUISE, RECEIVED HYD G RSVR LO LVL AND HYD G SYS LO PR MESSAGES. SELECTED THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP AND PTU OFF PER COM PROCEDURES. DURING APPROACH AT FINAL DESTINATION, SELECTED PTU ON RESTORING GREEN SYSTEM PRESSURE T O EXTEND LANDING GEAR AND LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED LEAKING HYDRAULIC LINE AT RIGHT WING AFT SPAR. LEAK CHECK OK. 2 L 7 2 4F RT A28NM 2001041800106 20010418 00106 2001 4 18 0100993257 4 20010317 A 2565 SLIDE AIRBUS 320 A320212 EU L2 DOOR FAILED A NWAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 01 357NW 830 DURING AIRCRAFT EVACUATION FOLLOWING ABORTED TAKEOFF AND RUNWAY EXCURSION, THE SLIDE RAFT ASSEMBLY FAILED TO DEPLOY AT D OOR 2L. 2 L 7 2 4F RT A28NM 2001041800107 20010418 00107 WP 2001 4 18 0101011154 1 20010316 A 3320 LIGHT DOUG DC10 DC1040 3023508 WP CABIN INTERMITTENT A NWAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 01 154US 46763 DURING TAXI OUT, LEFT AFT CABIN READING LIGHTS WERE FLASHING. FLASHING STOPPED AFTER RESETTING READING LIGHT AND CALL L IGHT CIRCUIT BREAKERS BUT FLIGHT ATTENDANT NOTED ELECTRICAL SMOKE. AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT. REP LACED OVERHEAD DECODER AT SEAT 36AB. 2 L 7 3 4F A22WE 2001041800108 20010418 00108 NE 2001 4 18 0101026634 2 20010318 A 7321 FUEL CONTROL BOEING 747 747227B 1384888 NM PWA JT9 JT9D7Q 52054 NE NR 4 ENGINE FAILED A NWAA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 GL 01 634US 22234 702145 WHILE IN CRUISE, THE NR 4 ENGINE FLAMED OUT. ALL ENGINE PARAMETERS ROLLED BACK WITH FUEL FLOW INDICATING ZERO. AFTER D ESCENDING TO FL280, TWO RESTART ATTEMPTS WERE MADE, BOTH UNSUCCESSFUL. THE FLIGHT DIVERTED TO ANC AND LANDED WITHOUT INC IDENT. MAINTENANCE REPLACED THE FUEL CONTROL AND ENGINE FUEL PUMP. ENGINE OPERATIONAL CHECK WAS WITHIN LIMITS. 2 L 7 4 4F 4 F A20WE E3NE 2001041800109 20010418 00109 NM 2001 4 18 DL72S010446 1 20010317 A 3350 0201875003 HARNESS BOEING 727 727225A 1384077 NM CABIN DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8873Z 21291 SEAT 30D EMERGENCY LIGHT INOP.// FOUND DAMAGED WIRING HARNESS, REPLACED HARNESS SECTION. OPS CK OK. 2 L 7 3 4F RT A3WE 2001041800110 20010418 00110 NM 2001 4 18 DL73K010447 1 20010317 A 3350 BPS73 POWER SUPPLY BOEING 737 737232 1384475 NM CABIN SHORTED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 320DL 23092 FOUND EMER. LIGHT FROM ROW 10 - 16 INOP - REPLACED POWER SUPPLY 2 L 7 2 4F RT A16WE 2001041800111 20010418 00111 NM 2001 4 18 DLM88010448 1 20010318 A 2150 A/C PACK DOUG MD88 MD88 3023688 NM CABIN CONTAMINATED A DALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 914DL 49545 IMMEDIATELY AFTER T/O , SMOKE DETECTOR IN AFT LAV WENT OFF. AFT F/A REPORTED SMOKE SMELL AS ELECTRICAL. FWD F/A COULD SM ELL SMOKE AS WELL. BY THE TIME WE RETURNED FOR LANDING, SMOKE DISSAPATED. PERFORMED DUCT BURN OUT 2 L 7 2 4F RT A6WE 2001041800112 20010418 00112 NM 2001 4 18 DL73K010449 1 20010318 A 4920 APU BOEING 737 737232 1384475 NM APU BAY ODOR A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 320DL 32090 23092 NA ACRID SMOKE SMELL LIKE BURNING RUBBER EMINATING FROM ROW 3 TO ROW 5 AREA IN CABIN. PASSENGERS COMPLAINED ABOUT SMELL. FL IGHT ATTENDANTS ALSO COMPLAINED OF SMELL WHICH EVENTUALLY WAS DETECTABLE FROM COCKPIT. FOUND OILY SMELL IN COCKPIT FROM APU AIR PERFORMED DUCT BURNOUT 2 L 7 2 4F RT A16WE 2001041800113 20010418 00113 NM 2001 4 18 DL72S010450 1 20010318 A 3350 S106 BATTERY BOEING 727 727225A 1384077 NM AIRSTAIR UNSERVICEABLE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8875Z 21293 AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT WILL NOT TEST. REPLACED BATTERIES NOW CKS NML 2 L 7 3 4F RT A3WE 2001041800114 20010418 00114 NM 2001 4 18 DL76G010451 1 20010319 A 3350 LIGHT BOEING 767 767332 1382001 NM LT OVERWING INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1610D 30594 LT EXTERIOR AFT OVER WING EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY. LIGHT OPS NML 2 L 7 2 4F RT A1NM 2001041800115 20010418 00115 NM 2001 4 18 SWAA010693 1 20010307 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 701GS 27836 DURING SCHEDULED C4 CHECK, FOUND EEPLS TRACK COVERS CRACKED AT ROWS 8, 9, 12, 19, 20 & 23. REMOVED AND REPLACED TRACK C OVERS PER MM. 2 L 7 2 4F RT A16WE 2001041800116 20010418 00116 NM 2001 4 18 SWAA010695 1 20010307 A 5315 6546804 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 312, LBL 13 TO RBL 11. REPAIRED FLOORBEAM UPPER CH ORD PER SRM. 2 L 7 2 4F A16WE 2001041800117 20010418 00117 NM 2001 4 18 SWAA010696 1 20010307 A 5310 AND10134 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD SHEAR TIE CRACKED AT FWD FASTENER HOLE, LT SIDE, WL 208. REPAIRED SH EAR TIE ANGLE PER SWA RA. 2 L 7 2 4F RT A16WE 2001041800118 20010418 00118 NM 2001 4 18 SWAA010666 1 20010306 A 3350 100031 LIGHT BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 092SW 22964 OVERHEAD EMERGENCY EXIT LIGHT LOOSE AT OVERWING EXIT. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 2001041800119 20010418 00119 NM 2001 4 18 SWAA010667 1 20010305 A 5311 6546546 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, RBL 65, WL 208. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2001041800120 20010418 00120 NM 2001 4 18 SWAA010669 1 20010306 A 5312 6517582 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM WEBS CRACKED AT LBL 17.1, WL 230 & RBL 17.1, WL 182. R EMOVED AND REPLACED BEAM WEB PER BFG ER. 2 L 7 2 4F RT A16WE 2001041800121 20010418 00121 NM 2001 4 18 SWAA010670 1 20010306 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 500C+2, STR 15L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001041800122 20010418 00122 NM 2001 4 18 SWAA010671 1 20010305 A 3350 100031 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED C1 CHECK, FOUND AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2001041800123 20010418 00123 NM 2001 4 18 SWAA010672 1 20010306 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 624SW 27934 DURING SCHEDULED SERVICE CHECK, FOUND 1 EEPLS BULB INOP AT MID CABIN. RELAMPED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001041800124 20010418 00124 NM 2001 4 18 SWAA010673 1 20010306 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 630WN 27705 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT AFT CABIN. RELAMPED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001041800125 20010418 00125 NM 2001 4 18 DLM88010452 1 20010319 A 3010 DUCT DOUG MD88 MD88 3023688 NM ANTI ICE SYSTEM CONTAMINATED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 923DL 49705 FUMES FROM WING ANTI-ICE SYSTEM SET OFF SMOKE DETECTORS IN BOTH AFT LAVS - COULD NOT DUPLICATE - PERFORMED DUCT BURNOUT AS PRECAUTION 2 L 7 2 4F RT A6WE 2001041800126 20010418 00126 NM 2001 4 18 DL733010453 1 20010319 A 3260 310FW0410 UPLOCK SENSOR BOEING 737 737347 1384647 NM NOSE GEAR FAILED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 313WA 23599 ON TAKEOFF SLC NOSE GEAR UNSAFE LIGHT ON RETRACTION. RED LIGHT STAYED ON. REPLACED NOSE UPLOCK SENSOR S846. PERFORM ED GEAR SWING OPS CHECKED NORMAL. 2 L 7 2 4F RT A16WE 2001041800127 20010418 00127 NM 2001 4 18 DL733010454 1 20010315 A 5312 654583340 BULKHEAD BOEING 737 737347 1384647 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3301 23181 BS 178 BULKHEAD FLOOR SUPPORT STRUCTURE WEB CRACKED AT WL 207 AND LBL 25. ER/A 380305-14AD ORIGINAL ISSUE 2 L 7 2 4F RT A16WE 2001041800128 20010418 00128 NM 2001 4 18 DL757010455 1 20010316 A 5415 012N88883 FITTING BOEING 757 757232 1384965 NM NR 1 PYLON TOOL DAMAGE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 604DL 22811 NR 1 PYLON / NACELLE ATTACH SUPPORT SIDE LINK FITTING MISDRILLED HOLE AT NR 2 ATTACH HOLE THROUGH SIDE LINK FITTING, WIN G LOWER SKIN AND WING FRONT SPAR LOWER CHORD. 2 L 7 2 4F RT A2NM 2001041800129 20010418 00129 NM 2001 4 18 DL73K010456 1 20010316 A 5312 BULKHEAD BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 238WA 23186 DURING REPETITIVE INSPECTIONS, BS 178 BULKHEAD WEB FOUND WITH ADDTIONAL CRACKS. EXISTING REPAIR REMOVED, AND NEW REPAIR INSTALLED TO INCORPORATE EXISTING AND NEW DAMAGE LOCATIONS. EXISTING REPAIR DOCUMENT HAS BEEN SUPERCEDED BY ER/A 37992 4-14AD. 2 L 7 2 4F A16WE 2001041800130 20010418 00130 NM 2001 4 18 SWAA010676 1 20010305 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 520SW 25319 DURING SCHEDULED C2 CHECK, FOUND EEPLS INOP AND TRACK COVERS BROKEN/LOOSE IN SEVERAL AREAS. REPAIRED EEPLS AND REMOVED AND REPLACED TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 2001041800131 20010418 00131 2001 4 18 SWAA010677 4 20010305 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY AND SVC DOOR EMERGENCY EVAC SLIDE ASSY''S OUT OF ADJUST. RE-ADJUSTED EVAC SL IDE ASSY''S PER MM. 2 L 7 2 4F RT A16WE 2001041800132 20010418 00132 NM 2001 4 18 SWAA010678 1 20010304 A 3320 059341 BALLAST BOEING 737 7373A4 1384585 NM CABIN INOPERATIVE A SWAA K NONE L B NO TEST SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 676SW 23288 ELECTRIC BURNING ODOR AT ROWS 17 TO 18, RIGHT SIDE. FOUND WINDOW LIGHT BALLAST INOP. REMOVED AND REPLACED BALLAST PER MM. 2 L 7 2 4F RT A16WE 2001041800133 20010418 00133 NM 2001 4 18 SWAA010679 1 20010306 A 5330 6545776 DOUBLER BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED D-CHECK, FOUND INTERNAL FUSELAGE SKIN DOUBLER CORRODED AT BS 967, LBL 3 TO LBL 7. REPAIRED SKIN PER BF G ER. 2 L 7 2 4F RT A16WE 2001041800134 20010418 00134 NM 2001 4 18 SWAA010748 1 20010313 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 389SW 26592 EEPLS INOP BETWEEN ROWS 11 & 17, AND TRACK COVERS MISSING AT ROWS 12 & 15. REPAIRED EEPLS EXCEPT 1 LIGHT AND TRACK COVE RS. DEFERRED PER MEL. AT BWI (FLT 203) REPLACED LIGHT AND TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 2001041800135 20010418 00135 NM 2001 4 18 DL73E010457 1 20010317 A 5313 6546877144 STRINGER BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 377DL 23604 FUSELAGE STRINGER 18A SHEAR WEB CRACKED ON RH SIDE OF AIRCRAFT AT STA. 727. CRACK IS 1.0 INCH AND EXTENDS FORWARD FROM THE INBOARD/ AFT FASTENER LOCATION. CRACK IS TYPICAL OF S/B 737-53-1066. 2 L 7 2 4F A16WE 2001041800136 20010418 00136 NM 2001 4 18 DL757010458 1 20010320 A 5310 146N85124 DOOR FRAME BOEING 757 757232 1384965 NM CARGO DOOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 604DL 22811 ADDITIONAL DAMAGE FOUND AT EXISTING REPAIR ON C-2 DOOR SURROUND AFT FRAME INNER CHORD. EXISTIND REPAIR WILL BE REMOVED AND REPLACED WITH A NEW REPAIR SCHEME. THIS ER/A SUPERCEDED BY ER/A 379988-14. 2 L 7 2 4F RT A2NM 2001041800137 20010418 00137 NM 2001 4 18 DLM88010459 1 20010320 A 2910 LINE DOUG MD88 MD88 3023688 NM HYD SYSTEM LEAKING A DALA C ABORTED TAKEOFF K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TO TAKEOFF 1 SO 27 906DL 49537 ON T/O SMOKE/ODOR IN AIRCRAFT. SMOKE ALARM GOING OFF IN AFT LAV. SMOKE STOPPED AT ALT. SMOKE AND ALARM STARTED AGAIN ON FINAL APPROACH FOUND REVERSER STOW LINE IN AFT FUSELAGE LEAKING AT SWAGE RE-SWAGED RT SIDE REVERSER STOW LINE LK AND O PS WITH NO DEFECTS NOTED. PERFORMED OPN 5088 DUCT BURNOUT. NO SMOKENOTED 2 L 7 2 4F RT A6WE 2001041800138 20010418 00138 NM 2001 4 18 DL73K010460 1 20010317 A 5510 BEARING BOEING 737 737232 1384475 NM HORIZONTAL STAB WORN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 316DL 23088 WHILE PERFORMING JIC5957 FOUND PIVOT BEARING PLAY TO BE OUT OF LIMITS. IN THE PROCCESS OF REMOVING BEARING HOUSING FOUN D SAFETY WIRE BROKEN AND KEEPER BACKED OFF APROX 1/4 INCH 2 L 7 2 4F RT A16WE 2001041800139 20010418 00139 NE 2001 4 18 DL757010461 2 20010321 A 7310 PW2037RTC O-RING BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE LEAKING A DALA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 644DL 35038 23998 716540 RT ENGINE FUEL PUMP FILTER CASE LEAKING. REPLACED DAMAGED O-RING. LEAK CK OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041800140 20010418 00140 NM 2001 4 18 SWAA010750 1 20010313 A 5311 6558280 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND AFT SVC DOOR UPPER STUB FRAME CRACKED AT BS 955, WL 256. REMOVED AND REPLACED STUB FRAM E PER SRM. 2 L 7 2 4F A16WE 2001041800141 20010418 00141 NM 2001 4 18 SWAA010751 1 20010312 A 5311 6546569 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 947, STR 17R. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2001041800142 20010418 00142 NM 2001 4 18 SWAA010752 1 20010313 A 5330 6545890 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACK AT BS 343, ABOVE STR 17L. REPAIRED SKIN PER BFG ER. 2 L 7 2 4F RT A16WE 2001041800143 20010418 00143 2001 4 18 SWAA010753 4 20010313 A 2565 61621469 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED 1/4D CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY FRAYED AT INBD EDGES. REMOVED AND REPLAC ED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001041800144 20010418 00144 NM 2001 4 18 SWAA010754 1 20010313 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED 1/4D CHECK, FOUND 6 BS 178 BULKHEAD WEB CRACKS AT RBL 5.0 TO LBL 7.0, WL 199 TO WL 207. REPAIRED BULKH EAD WEB PER SWA RA. 2 L 7 2 4F RT A16WE 2001041800145 20010418 00145 NM 2001 4 18 DL72S010462 1 20010321 A 7931 ST104Z TRANSMITTER BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE FAILED A DALA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SO 27 524DA 21584 700687 NBR 2 ENG OIL PRESSURE READ IN RED ON CLIMBOUT FROM OMA. REPLACED OIL PRESSURE TRANSMITTER 2 L 7 3 4F 4 F A3WE E2EA 2001041800146 20010418 00146 2001 4 18 DL733010463 4 20010322 A 2565 CASE BOEING 737 7373B7 1384580 NM ESCAPE SLIDE DISLODGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947WP 23376 CABIN SERVICE OPENED R1 DOOR AND SLIDE AND CASE FELL OFF OF THE DOOR. WHEN IT CONTACTED THE GROUND THE SLIDE DEPLOYED. G IRT BAR WAS ATTACHED TO SLIDE COVER. - REPLACED SAME 2 L 7 2 4F RT A16WE 2001041800147 20010418 00147 NM 2001 4 18 DLM90010464 1 20010321 A 3350 07912 LENS DOUG MD90 MD9030 3023690 NM ROW 14 MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 914DN 53394 FLOOR EMER LT AT ROW 14 LENSE MISSING. RPLCD LENSE. 2 L 7 2 4F RT A6WE 2001041800148 20010418 00148 NM 2001 4 18 DLM90010465 1 20010321 A 3350 BULB DOUG MD90 MD9030 3023690 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 914DN 53394 OVERHEAD EMERGENCY LIGHT AT ROW 1R INOP. RELAMPED. CHKS GOOD. 2 L 7 2 4F RT A6WE 2001041800149 20010418 00149 NM 2001 4 18 DL73E010466 1 20010322 A 5311 65479592 FRAME BOEING 737 7372S3 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 367DL 21774 A CRACK WAS FOUND IN THE WEB OF THE FS 795 FRAME BETWEEN STR 23R AND 24R. THE CRACK WAS CUT OUT AND REPAIRED PER SRM 51 -40-3, FIGURE 1. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001041800150 20010418 00150 NM 2001 4 18 DL72E010468 1 20010322 A 2750 ACTUATOR BOEING 727 727247 138408F NM TE FLAPS LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 831WA 21483 DURING APPROACH LOST A SYSTEM HYD PRESS. MANUALLY EXTENDED GEAR. FOUND FLAP HYD MOTOR LEAKING FLUID. REPLACED FLAP HYD MOTOR, AND CASE DRAIN CHECK VALVE PER MM. INSPECTED CASE DRAIN FILTERS, NO METAL FOUND. PERFORMED ENG RUN, OPS CHECKS NORMAL. 2 L 7 3 4F A3WE 2001041800151 20010418 00151 NM 2001 4 18 DL72L010469 1 20010322 A 5320 ANGLE BOEING 727 727232 1384082 NM LT MLG WW CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 503DA 21305 FOUND ON B2 LETTER CK FWD ANGLE CRACKED AT STA 910 ABOVE MLG UPLOCK IN THE LT MLG WW. REPAIRED PER MM 53-11-000-8. 2 L 7 3 4F A3WE 2001041800152 20010418 00152 NM 2001 4 18 DL72W010470 1 20010322 A 3350 RPS1 POWER SUPPLY BOEING 727 727247 138408F NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 294WA 22112 F/C SEAT ROWS EMER LIGHTS INOP. REPLACED POWER SUPPLY AND BATTERY PACK. OPS CKS NML 2 L 7 3 4F A3WE 2001041800153 20010418 00153 NM 2001 4 18 DL73K010472 1 20010323 A 2450 941D3352 CIRCUIT BREAKER BOEING 737 737232 1384475 NM COCKPIT FAILED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 309DL 23081 DURING T/S FOR ITEM ON LT AC BUS WOULD NOT COME ON LINE. FOUND APU GEN C/B WITH BURNED / SCORCHED TERMINALS AT THE B-1/2 /3 POSITIONS. REPLACED APU GEN C/B AS PRECAUTION. 2 L 7 2 4F RT A16WE 2001041800154 20010418 00154 NM 2001 4 18 DL73K010473 1 20010323 A 7120 MOUNT BOEING 737 737232 1384475 NM ENGINE WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 301DL 23073 ENGINE MOUNT SUPPORT FITTING HAD MIGRATING BEARINGS RESULTING IN OVERSIZED MOUNT HOLES. REPAIR PER ER/A 401250-14AD. 2 L 7 2 4F RT A16WE 2001041800155 20010418 00155 NM 2001 4 18 DL73K010474 1 20010323 A 7120 MOUNT BOEING 737 737232 1384475 NM ENGINE WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 301DL 23073 FWD ENGINE MOUNT WAS FOUND WITH MIGRATING BEARINGS THAT RESULTED IN OVERSIZED MOUNT HOLES. REPAIR PER ER/A 401250-14AD 2 L 7 2 4F RT A16WE 2001041800156 20010418 00156 NM 2001 4 18 DL73K010475 1 20010323 A 7120 MOUNT BOEING 737 737232 1384475 NM ENGINE WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 302DL 23047 FWD ENGINE MOUNT FOUND WITH MIGRATING BEARING RESULTING IN OVERSIZED MOUNT HOLES. REPAIR PER ER/A 401250-14AD. 2 L 7 2 4F RT A16WE 2001041800157 20010418 00157 NM 2001 4 18 DLM88010476 1 20010322 A 2150 8597221 GASKET DOUG MD88 MD88 3023688 NM LT ACM BAY CRACKED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 903DL 49534 TAIL COMPT TEMP HIGH LIGHT ILLUMINATED ON CLIMB OUT. H.P BLEED SELECTED OFF. AFTER 2 MINS LIGHT EXTINGUISHED, DIVERT TO CVG TO AVOID ICING CONDITIONS. FOUND TUBE ON LT FLOW CONTROL VLV WITH CRACKED FLARE. RPLCD TUBE. ALSO FOUND DUCT SENSOR COVER PLATE GASKET BLOWN ON BLEED DUCT. REPLACED GASKET. RAN ENGS AND PACKS, NO LEAKS NOTED AND NO HIGH T EMP LIGHT. OK FOR SERVICE. 2 L 7 2 4F RT A6WE 2001041800158 20010418 00158 NM 2001 4 18 DL757010477 1 20010323 A 5754 SLAT TRACK BOEING 757 757232 1384965 NM LT WING DAMAGED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 653DL 24393 LE FLAP ASSY ON FLAP RETRACTION - DECLARED EMERGENCY AND LANDED WITH NO INCIDENT. MTC IN WORK - FOUND NR 2 LE SLAT TRACK BROKEN LOOSE ON ARRIVAL. 2 L 7 2 4F RT A2NM 2001041800159 20010418 00159 NM 2001 4 18 DLM88010478 1 20010322 A 3520 GENERATOR DOUG MD88 MD88 3023688 NM PAX CABIN FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 970DL 43173 RIGHT HAND PASSENGER CHEMICAL OXYGEN GENERATOR UNIT FAILED TO FIRE DURING ACTIVATION, PRIOR TO DISPOSAL IN HAZARDOUS WAS TE DRUM. TRIED SEVERAL TIMES TO ACTIVATE. GENERATOR WAS BEING REPLACED DUE TO TIME. MANUFACTURE DATE-9-89.LOT NO.1314. 2 L 7 2 4F RT A6WE 2001041800160 20010418 00160 NM 2001 4 18 DL76G010480 1 20010323 A 3610 79275515 CONTROLLER BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 1 ENGINE FAILED A DALA A UNSCHED LANDING L NO TEST CL CLIMB 1 SO 27 1611B 30595 706140 IR - L ENG BLEED OFF LIGHT CAME ON AFTER T.O. AT 2000FT. L DUCT PRESS <10 PSI. SYSTEM RECOVERED A FEW MIN LATER ONLY T O PRESENT AGAIN AT TOP OF CLIMB. L REV DID NOT OPEN ON LNDG. NO L ANTI-ICE. NO LT ENG BLEED FAULTS ON BITE MODULE. USI NG PNEUMATIC TEST EQUIPTMENT PER MM - PRC FAILED. REPLACED SAME AND CHKS OK PER MM. ENG RUN OK. LT ENG ANTI-ICE AND T/R OPS OK. ETOPS CATEGORY ''''B'''': DIVERSION OR TURNBACK 2 L 7 2 4F 4 F RT A1NM E13NE 2001041800161 20010418 00161 NM 2001 4 18 DLM11010481 1 20010323 A 2121 6054578 FAN DOUG MD11 MD11 3023602 NM PAX OUTLET FAN OVERHEATED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 803DE 48474 DIVERTED INTO CDB FOR SMOKE SMELL IN CABIN. WITH CABIN BUSES OFF SMELL DIMINISED. FOUND PAX OUTLET FAN AT FAULT. DEACTIV ATED SAME. FAN R/R IN ANC ON LOG PAGE 379080001. FAN P/N 605457-8 S/N 18-7444 2 L 7 3 4F RT A22WE 2001041800162 20010418 00162 NM 2001 4 18 DHL2001702009 1 20010411 A 2760 SWITCH BOEING 727 72730C 1384009 NM SPEED BRAKE OUT OF ADJ A DHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 702DH 19793 TAKEOFF WARNING HORN SOUNDED DURING T/O ROLL 60 KTS. TAKEOFF REJECTED. VERIFIED T/O CONFIGURATION WAS CORRECTED. 2ND T/O NORMAL. FOUND SPEED BRAKE TAKEOFF WARNING SWITCH OUT OF ADJUSTMENT. ADJUSTED SWITCH S194 AND TESTED IAW MM 31-26- 25 P401-403. OPS CHECK GOOD. STATUS-CLOSED. 2 L 7 3 4F A3WE 2001041800163 20010418 00163 EA 2001 4 18 COMA0160333 1 20010322 A 5610 NP1393215 WINDSHIELD CNDAIR CL600 CL6002B19 EA COCKPIT CRACKED A COMA O OTHER O OTHER CR CRUISE 1 SO 01 915CA 4477 7013 PILOTS WINDSHIELD SHATTERED. REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 2001041800164 20010418 00164 NM 2001 4 18 DHL2001741517 1 20010309 A 5321 FLOORBOARD BOEING 727 7272Q9 138448M NM CABIN CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 CORROSION ON FLOORBOARDS AND FLOOR SUPPORT STRUCTURE FROM FS STA 303 TO FS 344 AND FROM RBL 16 TO RBL 55 (UNDER FWD LAV) . REMOVED CORROSION AS PER B727 SRM 51-10-6 MATERIAL LOSS .030 FOUND OUT OF LIMITS AS PER B727 SRM 53-30-1. REPLACED F LOORBOARDS SUPPORT PO 8312244 LOT 11154-1 AND 83110094 LOT 168979-1-1 P/N AND10137-1105 AND P/N BAC1505-100617 DIMENSION S 28.75 X 2 INCH AND 15 X 2 INCH IAW B727 SRM 53-30-8 FROM STA 312 RBL 16 TO RB 50. ALODINED AND PRIMED IAW B727 SRM 51 -10-2. INSTALLED FLOORBOARD SUPPORT IAW B727 SR 53-30-8 51-30-2. OK TO INSTALL FLOOR PANEL. FABRICATE AND INSTALL NEW FLOOR PANEL AT FWD LAV FROM STA 330 TO 344 RBL 16-RBL 55 AS PER B727 SRM 53-20-1 FIG 1. MAT USED AE4155-811162 24. 2 L 7 3 4F RT A3WE 2001041800165 20010418 00165 WP 2001 4 18 DHL2001806562 1 20010313 A 3010 DIFFUSER DOUG DC8 DC873F 302199F WP LT WING ANTI-ICE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LT WING LE ANTI-ICE DIFFUSERS 1-1/2 INCH CRACK AT UPPER PART STA XFS 745.950. PERFORMED STOP HOLE AND FABRIC ATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B PAGES 1-12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800166 20010418 00166 WP 2001 4 18 DHL2001806563 1 20010313 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LH WING L/E RIB UPPER PART 1 INCH CRACK AT STA XFS 766.500. PERFORMED STOP HOLE AND FABRICATED DOUBLER IAW S RM 57-2-0 PAGES 9. 10. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B PAGES 1-12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 PAGES 9, 10. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800167 20010418 00167 WP 2001 4 18 DHL2001806564 1 20010313 A 3010 DIFFUSER DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LT WING LE ANTI-ICE DIFFUSER LOWER PART 1/2 INCH CRACK AT STA XFS 760-250. PERFORMED STOP HOLE AND FABRICATE D DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. ST ATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800168 20010418 00168 WP 2001 4 18 DHL2001806566 1 20010313 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LT WING LE RIB UPPER PART 1/2 INCH CRACK AT STA XFS 803.730. PERFORMED STOP HOLE AND FABRICATED DOUBLERS IAW S RM 57-2-0 PAGE 9, 10. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B, PAGES 1-12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 PAGE 9/10. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800169 20010418 00169 WP 2001 4 18 DHL2001806567 1 20010311 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LT WING LE RIB UPPER PART 1 INCH CRACK AT STA XFS 785.800. PERFORMED STOP DRILL AND FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B, AND INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 F IG 2. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800170 20010418 00170 WP 2001 4 18 DHL2001806568 1 20010312 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LT WING LE RIB UPPER PART 1 INCH CRACK AT STA XFS 822.500. PERFORMED STOP DRILL AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B, PAGES 1-12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. ST ATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800171 20010418 00171 WP 2001 4 18 DHL2001806569 1 20010313 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LH WING L/E RIB UPPER PART 1/2 INCH CRACK AT STA XFS 822. PERFORMED STOP DRILL AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8, PAGES 12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS -CLOSED. 2 L 7 4 4F RT 4A25 2001041800172 20010418 00172 WP 2001 4 18 DHL2001806570 1 20010313 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LT WING LE RIB UPPER PART 1 INCH CRACK AT STA XFS 860. PERFORMED STOP DRILL AND FABRICATED DOUBLERS IAW SR M 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B, PAGES 1-12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATU S-CLOSED. 2 L 7 4 4F RT 4A25 2001041800173 20010418 00173 NM 2001 4 18 SWAA010756 1 20010313 A 5754 65C26686 SKIN BOEING 737 7373Q8 1384670 NM L/E SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 663SW 23256 DURING SCHEDULED C3 CHECK, FOUND NR 1 L/E SLAT SKIN CRACKED AT AFT ROW OF FASTENERS, INBD OF OUTBD AUX TRACK. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001041800174 20010418 00174 NM 2001 4 18 SWAA010757 1 20010313 A 5754 65C26686 SKIN BOEING 737 7373Q8 1384670 NM L/E SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 663SW 23256 DURING SCHEDULED C3 CHECK, FOUND NR 2 L/E SLAT SKIN CRACKED AT 3 FASTENER HOLES ON AFT ROW. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001041800175 20010418 00175 NM 2001 4 18 SWAA010758 1 20010312 A 3350 BR2013 COVER BOEING 737 7375H4 138449D NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 525SW 26567 DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVERS MISSING. INSTALLED TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 2001041800176 20010418 00176 NM 2001 4 18 SWAA010759 1 20010313 A 5330 6545768 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CANNING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 513SW 24190 DURING SCHEDULED D-CHECK AT DALFORT, FOUND EXTERNAL FUSELAGE SKIN OIL CANNED AT PREVIOUS REPAIR, BS 370, BETWEEN STR 24R & 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001041800177 20010418 00177 NM 2001 4 18 SWAA010760 1 20010311 A 2751 W180420722B WIRE BOEING 737 7373H4 1384600 NM RT WING CHAFED A SWAA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 652SW 27722 DECLARED EMERGENCY. DURING CRUISE NOTICED SPLIT FLAP INDICATION. ACFT HANDLED NORMALLY. FOLLOWED QRH - NORMAL LANDING . REPAIRED SHORTED WIRE BETWEEN CONNECTORS D4867P & D229 PER BAC WDM. 2 L 7 2 4F RT A16WE 2001041800179 20010418 00179 2001 4 18 SWAA010762 4 20010312 A 2565 D31354 SLIDE BOEING 737 7373K2 13844BA NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 340LV 23738 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001041800180 20010418 00180 2001 4 18 SWAA010726 4 20010311 A 3414 2083111 INDICATOR BOEING 737 7373G7 1384595 NM COCKPIT INOPERATIVE A SWAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 07 690SW 23783 ABORTED TAKEOFF AT 80 KTS, CAPT''S ASI INOP. REMOVED AND REPLACED MACH AIRSPEED INDICATOR PER MM, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2001041800181 20010418 00181 NM 2001 4 18 SWAA010727 1 20010311 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 639SW 27712 EEPLS WIRING EXPOSED AT OVERWING EXIT ROW. SECURED WIRING PER MM. 2 L 7 2 4F RT A16WE 2001041800182 20010418 00182 2001 4 18 SWAA010728 4 20010311 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 FWD SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001041800183 20010418 00183 2001 4 18 SWAA010729 4 20010310 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 395SW 27689 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001041800184 20010418 00184 NM 2001 4 18 SWAA010730 1 20010311 A 3397 BR2013 WIRE BOEING 737 7375H4 138449D NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 EEPLS WIRING EXPOSED AT ROW 7. INSTALLED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001041800185 20010418 00185 NM 2001 4 18 SWAA010732 1 20010311 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 627SW 27935 DURING SCHEDULED A2 CHECK, FOUND NUMEROUS EEPLS BULBS INOP. RELAMPED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001041800186 20010418 00186 NM 2001 4 18 SWAA010733 1 20010310 A 3350 6556633 LENS BOEING 737 7373T0 1384582 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 684WN 23941 DURING SCHEDULED A2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2001041800187 20010418 00187 2001 4 18 SWAA010734 4 20010312 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 080SW 22675 AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001041800188 20010418 00188 NM 2001 4 18 SWAA010735 1 20010312 A 5312 6516300 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED SPECIAL VISIT, FOUND 3 BS 178 BULKHEAD WEB CRACKS AT LBL 6.5, WL 191 TO 194, & RBL 5, WL 192 TO 200. R EPAIRED BULKHEAD WEB PER SRM. 2 L 7 2 4F A16WE 2001041800189 20010418 00189 NM 2001 4 18 SWAA010736 1 20010312 A 5315 6546804 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 294, LBL 27 TO RBL 38. REPAIRED FLOORBEAM UPPER CH ORD PER SRM. 2 L 7 2 4F A16WE 2001041800190 20010418 00190 2001 4 18 SWAA010738 4 20010312 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001041800191 20010418 00191 NM 2001 4 18 SWAA010739 1 20010312 A 5311 6546569 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 1006, BETWEEN STR 20L & 21L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001041800192 20010418 00192 NM 2001 4 18 SWAA010740 1 20010312 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/4D CHECK, FOUND LT KEEL BEAM CORRODED ON OUTBD FLANGE, BS 708 TO BS 727. REPAIRED KEEL BEAM OUTBD FL ANGE PER BFG ER. 2 L 7 2 4F RT A16WE 2001041800193 20010418 00193 NM 2001 4 18 SWAA010741 1 20010312 A 5743 6552235 FITTING BOEING 737 7375H4 138449D NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 513SW 24190 DURING SCHEDULED D-CHECK AT DALFORT, FOUND RT MLG BEAM ATTACH FITTING. REMOVED AND REPLACED MLG BEAM FITTING PER SWA RA . 2 L 7 2 4F RT A16WE 2001041800194 20010418 00194 NM 2001 4 18 SWAA010743 1 20010312 A 3350 BR2013 CONNECTOR BOEING 737 7375H4 138449D NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP BETWEEN ROWS 10 & 14. RECONNECTED EEPLS WIRING PER MM. 2 L 7 2 4F RT A16WE 2001041800195 20010418 00195 NM 2001 4 18 SWAA010744 1 20010310 A 5320 963089 STIFFENER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD STIFFENER CRACKED AT LBL 25, WL 195. REMOVED AND REPLACED STIFFEN ER PER SRM. 2 L 7 2 4F A16WE 2001041800196 20010418 00196 NM 2001 4 18 SWAA010747 1 20010312 A 5330 65C35775 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING WALK AROUND INSPECTION, FOUND 4 EXTERNAL FUSELAGE SKIN CRACK AT BS 747, BELOW STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001041800197 20010418 00197 NM 2001 4 18 SWAA010704 1 20010309 A 3350 BR2013 LENS BOEING 737 7372T4 1384492 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 EEPLS LENS COVER MISSING AT ROW 18. INSTALLED LENS PER MM. 2 L 7 2 4F A16WE 2001041800198 20010418 00198 NM 2001 4 18 SWAA010705 1 20010309 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM ENTRY DOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 EMERGENCY EXIT LIGHT LENS MISSING AT FWD ENTRY DOOR. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2001041800199 20010418 00199 NM 2001 4 18 SWAA010707 1 20010309 A 5315 6546804 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 328, RBL 11 TO RBL 55. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F A16WE 2001041800200 20010418 00200 NM 2001 4 18 SWAA010708 1 20010309 A 5310 6547978 CREASE BEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM LOWER WEB SURFACE CORRODED AT NUT PLATE HOLES, BS 464 TO BS 474, RBL 65. RE PAIRED CREASE BEAM WEB PER SRM. 2 L 7 2 4F A16WE 2001041800201 20010418 00201 NM 2001 4 18 SWAA010709 1 20010309 A 5315 6546804 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 1016, LBL 36 TO RBL 36. REPAIRED FLOORBEAM PER SRM . 2 L 7 2 4F A16WE 2001041800202 20010418 00202 NM 2001 4 18 SWAA010710 1 20010309 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVER BROKEN AT ROW 8 & MISSING AT ROW 9. INSTALLED TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 2001041800203 20010418 00203 NM 2001 4 18 SWAA010711 1 20010309 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED C2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LOOSE AT ROW 5 DEF. SECURED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001041800204 20010418 00204 NM 2001 4 18 SWAA010713 1 20010309 A 5753 6546435 SKIN BOEING 737 7375H4 138449D NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 DURING SCHEDULED SPECIAL VISIT, FOUND RT WING T/E AFT FLAP DELAMINATED AT T/E. REMOVED AND REPLACED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2001041800205 20010418 00205 2001 4 18 SWAA010715 4 20010310 A 2565 D31354 SLIDE BOEING 737 7377H4 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 712SW 27846 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FALLING OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001041800206 20010418 00206 NM 2001 4 18 SWAA010716 1 20010310 A 3350 101074 SIGN BOEING 737 7372H4 138448C NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED RON CHECK, FOUND EMERGENCY EXIT SIGN BROKEN AT RT OVERWING HATCH. REMOVED AND REPLACED EXIT SIGN PER M M. 2 L 7 2 4F A16WE 2001041800207 20010418 00207 NM 2001 4 18 SWAA010717 1 20010310 A 3350 300432 LIGHT BOEING 737 7372H4 138448C NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SERVICE CHECK, FOUND AFT RT EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM . 2 L 7 2 4F A16WE 2001041800208 20010418 00208 NM 2001 4 18 SWAA010718 1 20010310 A 3350 BR2013 LIGHT BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED A2 CHECK, FOUND EEPLS LOOSE AT ROW 1. SECURED EEPLS PER MM. 2 L 7 2 4F A16WE 2001041800209 20010418 00209 NM 2001 4 18 SWAA010720 1 20010310 A 2560 65C168209 RETAINER BOEING 737 7373H4 1384600 NM ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 311SW 23333 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMEGENCY EVAC SLIDE GIRT RETAINER RIVETS LOOSE. SECURED GIRT RETAINER P ER MM. 2 L 7 2 4F RT A16WE 2001041800210 20010418 00210 NM 2001 4 18 SWAA010721 1 20010310 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 311SW 23333 DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT LIGHT LENS LOOSE AT LT OVERWING EXIT. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2001041800211 20010418 00211 NM 2001 4 18 SWAA010722 1 20010310 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED 1/4D CHECK, FOUND STR 28L CLIP CRACKED AT BS 867. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001041800212 20010418 00212 NM 2001 4 18 SWAA010723 1 20010309 A 2450 915F2134 PANEL BOEING 737 7373H4 1384600 NM COCKPIT OVERHEATED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 642WN 27715 AIR TURNBACK, DECLARED EMERGENCY. ELECTRICAL FUMES AND SMOKE IN COCKPIT WHILE CLIMBING THROUGH FL 250. REMOVED AND REP LACED BUS PROTECTION PANEL, ACCOMPLISHED COCKPIT CHECK AND ENG RUNS, OPS CHECK GOOD PER MM. 2 L 7 2 4F RT A16WE 2001041800213 20010418 00213 SO 2001 4 18 C2XA01TY059 1 20010323 A 5330 14523055001 SKIN EMB 145 EMB145LR SO FUSELAGE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13978 145180 TYS DURING A SCHEDULED INSPECTION THE LEFT ENGINE INTERNAL SKIN AT FRAMES NR 66 AND 67 WAS FOUND CHAFED BY A BLEED LINE ADEL CLAMP. MAINTENANCE REPAIRED DAMAGED AREA BY INSTALLING A DOUBLER IAW EMB-GST-0869/01, REPAIR WAS SATISFACTORY. T HE AIRCRAFT WILL RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2001041800214 20010418 00214 NM 2001 4 18 SWAA010703 1 20010308 A 5312 6517583 BULKHEAD BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 513SW 24190 DURING SCHEDULED D-CHECK AT DALFORT, FOUND 2 CRACKS AT FWD BULKHEAD VERTICAL BEAM WEBS BS 180, LBL 17.1 & BS 179.5, LBL 5.7. REPAIRED VERTICAL BEAM WEBS PER SWA RA. 2 L 7 2 4F RT A16WE 2001041800216 20010418 00216 NM 2001 4 18 SWAA010674 1 20010306 A 5743 6552235 FITTING BOEING 737 7375H4 138449D NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 513SW 24190 DURING SCHEDULED D-CHECK AT DALFORT, FOUND LT MLG BEAM FITTING CORRODED. REMOVED AND REPLACED BEAM FITTING PER MM. 2 L 7 2 4F RT A16WE 2001041800217 20010418 00217 NM 2001 4 18 SWAA010675 1 20010306 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED A1 CHECK, FOUND EEPLS INOP AT ROW 1 AND TRACK COVERS CRACKED AT ROWS 1 & 10. RELAMPED EEPLS AND REMOVE D AND REPLACED TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 2001041800218 20010418 00218 NM 2001 4 18 SWAA010749 1 20010313 A 3350 BR2013 LENS BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 506SW 24183 EEPLS LENS LOOSE AT ROW 7. REMOVED AND REPLACED EEPLS TRACK COVER AND LENS PER MM. 2 L 7 2 4F RT A16WE 2001041800219 20010418 00219 NM 2001 4 18 SWAA010755 1 20010313 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED A2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHTS INOP AT ROWS 12 DEF & 18 ABC. RELAMPED LIGHTS PER MM. 2 L 7 2 4F RT A16WE 2001041800220 20010418 00220 NM 2001 4 18 SWAA010761 1 20010313 A 2910 3290002 HYDRAULIC LINE BOEING 737 7373L9 1384470 NM NLG W/W LEAKING A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 658SW 23332 AIR TURNBACK, NLG RED WARNING LIGHT ILLUMINATED AFTER TAKEOFF/GEAR RETRACTION. LOUD NOISE FROM DRAG CONTINUED UNTIL GEA R HANDLE PLACED IN DOWN POSITION. ALL INDICATIONS THEN APPEARED NORMAL. FOUND NLG UPLOCK HYDRAULIC LINE LEAKING. REMO VED AND REPLACED HYDRAULIC LINE AND CYCLED GEAR, OP''S CHECK GOOD PER MM. 2 L 7 2 4F RT A16WE 2001041800221 20010418 00221 NM 2001 4 18 SWAA010686 1 20010307 A 5755 6573730 SKIN BOEING 737 7372H4 138448C NM SPOILER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND NR 7 SPOILER DELAMINATED AT LOWER SURFACE, OUTBOARD END. REPAIRED SPOILER PER SRM. 2 L 7 2 4F A16WE 2001041800222 20010418 00222 NM 2001 4 18 SWAA010688 1 20010307 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM CORRODED AT BS 500D, LT SIDE. REPAIRED KEEL BEAM PER BFG ER. 2 L 7 2 4F RT A16WE 2001041800223 20010418 00223 NM 2001 4 18 SWAA010694 1 20010307 A 5311 6546569 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 951, BELOW STR 12L. REPAIRED FRAME WEB PER SRM. 2 L 7 2 4F A16WE 2001041800224 20010418 00224 NM 2001 4 18 SWAA010668 1 20010306 A 5315 6546804 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 46 TO RBL 46. REPAIRED FLOORBEAM PER SWA RA. 2 L 7 2 4F A16WE 2001041800225 20010418 00225 2001 4 18 SWAA010731 4 20010311 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY FRAYED & STRAPS UNGLUED. REMOVED AND R EPLACED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001041800226 20010418 00226 NM 2001 4 18 SWAA010737 1 20010312 A 2560 6557463 BRACKET BOEING 737 7372H4 138448C NM CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKETS CORRODED. REMOVED AND REPLACED FW D AND AFT GIRT BRACKETS PER SRM. 2 L 7 2 4F A16WE 2001041800227 20010418 00227 NM 2001 4 18 SWAA010742 1 20010312 A 5743 6567172 FITTING BOEING 737 7375H4 138449D NM RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 513SW 24190 DURING SCHEDULED D-CHECK AT DALFORT, FOUND RT MLG SUPPORT BEAM STABILIZER BEAM FITTING CORRODED. REMOVED AND REPLACED B EAM FITTING PER MM. 2 L 7 2 4F RT A16WE 2001041800228 20010418 00228 NM 2001 4 18 SWAA010745 1 20010311 A 3230 65448106 ACTUATOR BOEING 737 7372H4 138448C NM LT MLG MALFUNCTIONED A SWAA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 062SW 22060 LT MLG LIGHT ILLUMINATED AFTER TAKEOFF AND LT GEAR EXTENDS WHEN HANDLE RETURNED TO NEUTRAL POSITION. REMOVED AND REPLAC ED LT MLG UPLOCK ACTUATOR AND HYDRAULIC MODULE PER MM. 2 L 7 2 4F A16WE 2001041800229 20010418 00229 NM 2001 4 18 SWAA010706 1 20010309 A 3350 BR2013 LENS BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 506SW 24183 EEPLS LENS LOOSE AT ROW 7. SECURED EEPLS LENS PER MM. 2 L 7 2 4F RT A16WE 2001041800230 20010418 00230 NM 2001 4 18 SWAA010712 1 20010309 A 5754 65C26686 SKIN BOEING 737 7373H4 1384600 NM L/E SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED C2 CHECK, FOUND NR 6 L/E SLAT SKIN CRACKED AT LOWER AFT ROW OF FASTENERS, 24 INBD OF ACTUATOR. REPAIRE D SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001041800231 20010418 00231 2001 4 18 SWAA010714 4 20010307 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001041800232 20010418 00232 2001 4 18 SWAA010719 4 20010310 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 311SW 23333 DURING SCHEDULED C4 CHECK, FOUND AFT SVC AND FWD ENTRY DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY''S PER MM. 2 L 7 2 4F RT A16WE 2001041800233 20010418 00233 EU 2001 4 18 QXEA0100381 1 20010309 A 5755 FITTING FOKKER F28 F28MK4000 4990810 EU RT SPOILER LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-RIGHT HAND NR 2 LIFT DUMPER SPIGOT LOOSE IN SPAR BRACKET. REPAIRED IAW FOKKER SRM 27-63-00, PAGE 402 AND HORIZON AI R EA 4-57-546. 2 L 7 2 4F RT A20EU 2001041800234 20010418 00234 EU 2001 4 18 QXEA0100382 1 20010314 A 2752 ROD FOKKER F28 F28MK4000 4990810 EU T/E FLAP CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-LEFT HAND WING STATION 7306 TRAILING EDGE STRUT ROD CRACKED. REPAIRED IAW FOKKER SRM 51-31-05, PAGE 8, 9 AND HORIZO N AIR EA 4-57-540. 2 L 7 2 4F RT A20EU 2001041800235 20010418 00235 EU 2001 4 18 QXEA0100383 1 20010312 A 5751 SKIN FOKKER F28 F28MK4000 4990810 EU LT AILERON DELAMINATED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-LEFT HAND AILERON TRAILING EDGE HAS DELAMINATION FROM OUTBOARD END AT EXITING DOUBLER. REPAIRED IAW FOKKER SRM 51-7 0-00, PAGE 14 AND SRM 57-50-41, PAGE 1. 2 L 7 2 4F RT A20EU 2001041800236 20010418 00236 EU 2001 4 18 QXEA0100384 1 20010312 A 5751 SKIN FOKKER F28 F28MK4000 4990810 EU LT AILERON DELAMINATED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-LEFT HAND AILERON TRAILING EDGE HAS 5 DISBONDS FROM OUTBOARD END AT EXITING DOUBLER ON TOP SKIN. REPAIRED IAW FOKKE R SRM 51-70-00, PAGE 13 AND SRM 57-50-41, PAGE 1. 2 L 7 2 4F RT A20EU 2001041800237 20010418 00237 EU 2001 4 18 QXEA0100419 1 20010319 A 5210 CABLE FOKKER F28 F28MK4000 4990810 EU PAX DOOR DEFECTIVE A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 486US 11237 SEA - MAIN CABIN DOOR FOUND DIFFICULT TO OPEN IN MANUAL MODE. REMOVED AND REPLACED MAIN CABIN DOOR MECHANICAL RELEASE C ABLE. RII COMPLIED WITH. AIRCRAFT STILL OUT OF SERVICE FOR UNRELATED MAINTENANCE. 2 L 7 2 4F RT A20EU 2001041800239 20010418 00239 NM 2001 4 18 DHL2001702007 1 20010330 A 5210 5717623095 WINDSHIELD BOEING 727 72730C 1384009 NM COCKPIT FAILED A DHLA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 702DH 19793 L-2 WINDSHIELD CRACKED DURING CRUISE FLIGHT. CORRECTIVE ACTION: REPLACED L-2 WINDOW IAW B727 MM 56-12-11. OPS CK SERV ICABLE PRESSURIZED A/C ON GROUND. NO LEAKS NOTED. STATUS CLOSED. 2 L 7 3 4F A3WE 2001041800240 20010418 00240 WP 2001 4 18 DHL2001706550 1 20010316 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - MAIN CARGO D FLOOR AT STA 887.000 CRACKED 2 INCHES. CUTOUT DAMAGED AREA OF FLOOR PANEL D AT STA 887 AND FAB RICATED FILLER AND DOUBLER IAW SRM 53-2-3 PAGE 39-40. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B, PAGES 1,12&13. INSTA LLED FILLER AND DOUBLER IAW SRM 53-2-3 PAGE 39-40. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800241 20010418 00241 WP 2001 4 18 DHL2001806551 1 20010318 A 5320 WEB DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - MAIN CARGO SUB-FLOOR AT STA 8.000 RBL 46 CRACKED 3 1/4 INCHES. PERFORMED STOP HOLE AND FABRICATED DOUBLER I AW SRM 53-1-0 FIG 1B. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 53-2-0 FIG. 1B. STATUS-CLOSE D. 2 L 7 4 4F RT 4A25 2001041800242 20010418 00242 WP 2001 4 18 DHL2001806552 1 20010319 A 5320 ANGLE DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - MAIN CARGO FLOOR SUPPORT ANGLE CRACKED 1/2 INCH AND DEFORM BL 0 AT STA 8.000. REMOVED CRACKED FLOOR SUPPORT ANGLE AND FABRICATED FLOOR SUPPORT ANGLE IAW SRM 53-2-0 PAGE 2E/2F. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INST ALLED FLOOR SUPPORT ANGLE IAW SRM 53-2-0 PAGE 2E/2F. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800245 20010418 00245 2001 4 18 DHL2001804002 4 20010406 A 2216 61574317 SERVO DOUG DC8 DC873F 302199F WP AUTOPILOT FAILED A DHLA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 01 804DH 46124 AUTO PILOT SERVO INDICATOR FOR ELEV ERRATIC IN SMOOTH FLIGHT. R&R ELEVATOR SERVO. CHECKED NORMAL IAW 22-10-00 ON GND. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800246 20010418 00246 WP 2001 4 18 DHL2001806553 1 20010318 A 5320 WEB DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - MAIN CARGO SUB-FLOOR SHOWS 02 EA CRACKS 3/8 AND 5/8 RBL 8 1/2 INCHES STA 25.000. PERFORMED STOP HOLE AND FA BRICATED DOUBLER IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED, AND PRIMED IAW SRM 51-1-8B AND INSTALLED DOUBLER IAW SRM 53-2 -0 FIG 1B. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800247 20010418 00247 WP 2001 4 18 DHL2001806554 1 20010318 A 5320 WEB DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - MAIN CARGO COMPARTMENT SUB-FLOOR SHOWS 02 EA CRACKS 1/4 INCH RBL 52 STA 55.000. PERFORMED STOP HOLE IAW 53-2 -0 FIG 1B. FABRICATED DOUBLER IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1B. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800248 20010418 00248 WP 2001 4 18 AALA20010445 1 20010306 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND SMOOTH DENT IN FUSELAGE SKIN AT STATION 238 BETWEEN LONGERON 17L AND 18L. ADL NR 5130030. INSTALLED TWO RO W INTERNAL .032 2024-T3 DOUBLER PER SRM 53-04 FIG 38 SHEET 22. (M) 2 L 7 2 4F A6WE 2001041800249 20010418 00249 WP 2001 4 18 AALA20010446 1 20010305 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND BLEND OUT OF LIMITS AT STATION 289 L24R ON FUSELAGE SKIN. INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M) 2 L 7 2 4F A6WE 2001041800250 20010418 00250 WP 2001 4 18 AALA20010447 1 20010305 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND LONGERON L2 CRACKED AT STATION 1418. INSTALLED NEW SECTION OF LONGERON PER AARD 53-30-00-2. (M) 2 L 7 2 4F A6WE 2001041800251 20010418 00251 WP 2001 4 18 AALA20010448 1 20010305 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND SKIN CRACKED AT FASTENER HOLE FUSE STATION 1380 L14L. STOP DRILLED CRACK. INSTALLED DOUBLER PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2001041800252 20010418 00252 WP 2001 4 18 AALA20010449 1 20010306 A 5320 FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND CRACK FROM BOLT HOLE ATTACH AT CUSP TO EDGE OF FITTING LEFT. INSTALLED FABRICATED PART SHOP ORDER 2202530 D ATED 2/28/2001 USING HI-LOCKS TO ZEE FRAME ATTACHMENT SRM 53-01. (M) 2 L 7 2 4F A6WE 2001041800253 20010418 00253 WP 2001 4 18 AALA20010450 1 20010306 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND CRACK IN CUSP RT FS 218 OUTBOARD OF NR 5 SEAT TRACK. INSTALLED SERVICEABLE CUSP SHEET FROM FS 218 TO FS 237 SRM 53-01. (M) 2 L 7 2 4F A6WE 2001041800254 20010418 00254 WP 2001 4 18 AALA20010451 1 20010228 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND FORWARD PAX DOOR JAMB AFT INNER WEB TONGUE CRACKED AT LONGERON 15. TRIMMED OFF TONGUE AND INSTALLED REPAIR STRAP PER AARD 53-10-00-11. (M) 2 L 7 2 4F A6WE 2001041800255 20010418 00255 2001 4 18 DHL2001802004 4 20010413 A 2210 AUTOPILOT SYS DOUG DC8 DC873F 302199F WP COCKPIT MALFUNCTIONED A DHLA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 01 802DH 46076 AUTOPILOT WILL NOT DISCONNECT USING TRIM SWITCHES ON YOKE. DEFEATED AUTOPILOT SYSTEM PER MEL 22-1. AUTOPILOT PLACARDE D DMI 5171. STATUS-OPEN 2 L 7 4 4F RT 4A25 2001041800256 20010418 00256 WP 2001 4 18 AALA20010456 1 20010304 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND CORROSION ON G2 GALLEY SUPPORT FITTING AT STATION 218 RBL 11. REMOVED GALLEY SUPPORT. INSTALLED NEW G2 GAL LEY FLOOR SUPPORT FITTING PER SRM 51-01-00. (M) 2 L 7 2 4F A6WE 2001041800257 20010418 00257 WP 2001 4 18 AALA20010464 1 20010306 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND DENT IN FUSELAGE SKIN T SHEAR TIE AT STATION 389 BETWEEN LONGERON 21 AND LONGERON 22L, ADL NR 5130037. COLD WORKED METAL BACK TO WITHIN LIMITS AND INSTALLED TWO ROW DOUBLER PER SRM 53-04 FIG 38. (M) 2 L 7 2 4F A6WE 2001041800258 20010418 00258 WP 2001 4 18 AALA20010452 1 20010228 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND NR 1 SEAT TRACK HAS CORROSION 1.5 INCH BY .5 INCH BY .050 AT STATION 1235 TO 1236. BLENDED OUT CORROSION, I NSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10. (M) 2 L 7 2 4F A6WE 2001041800259 20010418 00259 WP 2001 4 18 AALA20010453 1 20010228 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - DENT APPROX 1 INCH DIAMETER WITH GOUGE APPROX .25 INCH LONG ON LEFT SIDE BELOW NR 8 WINDOW STATION 327 BETWEEN L23 AND L24. CUT OUT DAMAGE 2.25 INCH DIAMETER CIRCLE. FABRICATED .032 TITANIUM DOUBLER 8 INCH BY 8 INCH PER SRM 53-04 FI G 8. (M) 2 L 7 2 4F A6WE 2001041800260 20010418 00260 WP 2001 4 18 AALA20010454 1 20010302 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND CORROSION ON LEFT CUSP STATION 617 TO STATION 636. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER AARD 53-0 0-00-02 STATION 617-636. (M) 2 L 7 2 4F A6WE 2001041800261 20010418 00261 WP 2001 4 18 AALA20010455 1 20010302 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND CORROSION ON LEFT CUSP SEVERAL PLACES FROM STATION 635-652. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD N R 53-00-00-2. (M) 2 L 7 2 4F A6WE 2001041800262 20010418 00262 WP 2001 4 18 AALA20010457 1 20010304 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND CORROSION ON SUBFLOOR DIRECTLY UNDERNEATH G-2 GALLEY SUPPORT FITTING. CUT OUT AREA AND INSTALLED NEW FABRIC ATED DOUBLER AT G2 GALLEY SUPPORT FITTING PER SRM 53-01-00. (M) 2 L 7 2 4F A6WE 2001041800263 20010418 00263 WP 2001 4 18 AALA20010458 1 20010303 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND CORROSION 3 INCHES BY 16 INCHES, ON CUSP STATION 734-750 LEFT SIDE. REMOVED AND INSTALLED DOUBLER PER SRM 5 3-01 FIG 4-3. (M) 2 L 7 2 4F A6WE 2001041800264 20010418 00264 WP 2001 4 18 AALA20010459 1 20010303 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND 1.5 INCH BY 1.5 INCH DENT IN SKIN FS 243, ADL NR 5130005. COLD WORK DENT TO WITHIN LIMITS AND INSTALLED DOU BLER INSIDE PER 53-04 FIG 38. (M) 2 L 7 2 4F A6WE 2001041800265 20010418 00265 WP 2001 4 18 AALA20010460 1 20010305 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND CORROSION ON CUSP FORWARD OF STATION 200 RIGHT SIDE RBL 58. DOUBLER REPAIR PER SRM 53-01 FIG 4-3. (M) 2 L 7 2 4F A6WE 2001041800266 20010418 00266 WP 2001 4 18 AALA20010461 1 20010305 A 5345 MOUNT DOUG DC9 DC982 3022082 WP FWD LAVATORY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND CORROSION ON FORWARD LAVATORY INBOARD AFT MOUNT, FS 253. INSTALLED NEW MOUNT PLATE SRM 51-01-00. (M) 2 L 7 2 4F A6WE 2001041800267 20010418 00267 WP 2001 4 18 AALA20010462 1 20010303 A 5310 BEAM DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND 1 INCH BY 20 INCHES OF CORROSION ON AFT CARGO DOOR JAMB BEAM ACROSS BOTTOM OF OPENING, FS 1155-1212. REMOVE D AND REPLACED DOOR JAMB BEAM PER 51-01. (M) 2 L 7 2 4F A6WE 2001041800268 20010418 00268 WP 2001 4 18 AALA20010463 1 20010307 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND CUSP ON LEFT SIDE AT STATION 1280 HAS 3 CRACKS PROTRUDING FROM HOLE. ROUTED OUT DAMAGED HOLE AND INSTALLED DOUBLER ON CUSP PER AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 2001041800269 20010418 00269 WP 2001 4 18 AALA20010465 1 20010228 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND CORROSION ON SEAT TRACK NR 7 AT STATION 1199, 1203. REMOVED CORROSION AND REPLACED CORRODED SEAT TRACK PLUG PER SRM 53-05. (M) 2 L 7 2 4F A6WE 2001041800270 20010418 00270 WP 2001 4 18 AALA20010466 1 20010312 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND CORROSION ON NR 2 SEAT TRACK STATION 1306-1214. REPLACED SEAT NR 2 TRACK STATION 1174 TO STATION 1309 PER S RM 53-05 PART 1 EK 4F SHEET 1. (M) 2 L 7 2 4F A6WE 2001041800271 20010418 00271 NM 2001 4 18 01FDEA00204 1 20010313 A 5210 ADA37541 STOP FITTING DOUG MD11 MD11F 3023600 NM R3 DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 603FE 48459 CABIN R3 DOOR PLUG AFT LWR STOP FITTING FOUND CRACKED. *S/D* REMOVED AND REPLACED PER SRM 51-31-01, VOL II, IAW DWG NO ADA 3462. HOLES TRANSFERRED TO NEW STOP FITTING AS PER SRM 51-35-01, VOL II. 2 L 7 3 4F RT A22WE 2001041800272 20010418 00272 2001 4 18 DHL2001702008 4 20010329 A 8300 717000 GEARBOX BOEING 727 72730C 1384009 NM NR 2 ENGINE LEAKING A DHLA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 702DH 19793 IN CRUISE FLIGHT LOW OIL PRESS LIGHT ILLUMINATED. OIL PRESSURE FLUCTUATING BETWEEN 20-40 PSI. PERFORMED OIL PRESS BELO W 40 PSI ABNORMAL CHECKLIST AND DISCOVERED ZERO OIL QUANTITY. PERFORMED IN FLIGHT ENG SHUTDOWN ABNORMAL PROCEDURE. OIL PRESS INDICATION ZERO, WITH ENGINE WINDMILLING 18 PERCENT N1, 27 PERCENT N2 FOR APPROX 30 MIN THRUST WAS NOT DECREASING PRIOR TO SHUTDOWN.CORRECTIVE ACTION: STATUS - R&R NR 2 ENGINE ACCY GEARBOX PER M/M JT8D-72-60 PERFORMED TEST B LEAK AN D OPS CK GOOD. STATUS-CLOSED. 2 L 7 3 4F A3WE 2001041800273 20010418 00273 WP 2001 4 18 DHL2001806565 1 20010313 A 3010 DIFFUSER DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LT WING LE ANTI-ICE DIFFUSER LOWER PART 1-1/2 INCH CRACK AT STA XFS 728. PERFORMED STOP HOLE AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STAT US-CLOSED. 2 L 7 4 4F RT 4A25 2001041800274 20010418 00274 WP 2001 4 18 DHL2001806555 1 20010313 A 5712 RIB DOUG DC8 DC873F 302199F WP WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - WING LE RIB UPPER PART 1 INCH CRACK AT STA 803.730. PERFORMED STOP HOLE AND FABRICATED DOUBLERS IAW SRM 57-2 -0 P1, 9, 10. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B PAGES 1-12, 13. INSTALLED DOUBLERS IAW SRM 57-2-0 PAGE 10. STA TUS-CLOSED 2 L 7 4 4F RT 4A25 2001041800275 20010418 00275 WP 2001 4 18 DHL2001806556 1 20010311 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LT WING LE RIB UPPER PART 1 INCH CRACK AT STA XFS 785.800. PERFORMED STOP DRILL AND FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B AND INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG2. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800276 20010418 00276 WP 2001 4 18 DHL2001806557 1 20010313 A 3010 DIFFUSER DOUG DC8 DC873F 302199F WP LT WING LE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LT WING LE ANTI-ICE DIFFUSER, 1 INCH CRACK AT UPPER PART STA XFS 766.500 - XFS 766.950. PERFORMED STOP HOLE. AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 57 -2-0 FIG 2. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800277 20010418 00277 WP 2001 4 18 DHL2001806558 1 20010312 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LT WING LE RIB 1 INCH CRACK AT UPPER PART STA XFS 822.500. PERFORMED STOP DRILL AND FABRICATED DOUBLER IAW S RM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B PAGES 1-12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STA TUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800278 20010418 00278 WP 2001 4 18 DHL2001806559 1 20010118 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LT WING LE RIB UPPER PART CRACKED 1/2 INCH AT STA XFS 822. PERFORMED STOP DRILL AND FABRICATED DOUBLER IAW S RM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B PAGES 12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATU S-CLOSED. 2 L 7 4 4F RT 4A25 2001041800279 20010418 00279 WP 2001 4 18 DHL2001806560 1 20010319 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LT WING LE RIB UPPER PART 1 INCH CRACK AT STA XFS 860. PERFORMED STOP DRILL AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B PAGES 1-12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS -CLOSED. 2 L 7 4 4F RT 4A25 2001041800280 20010418 00280 WP 2001 4 18 DHL2001806561 1 20010313 A 3010 DIFFUSER DOUG DC8 DC873F 302199F WP LT WING ANTI-ICE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LT WING LE ANTI-ICE DIFFUSER LWR PART 1/2 INCH CRACK AT STA XFS 766.250. PERFORMED STOP HOLE AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B PAGES 1-12, 13. INSTALLED DOUBLER IAW SRM 57-2- 0 FIG 2. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800281 20010418 00281 NM 2001 4 18 DHL2001707005 1 20010410 A 3340 77T1352 LIGHT BOEING 727 72722 1384002 NM RT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 RIGHT TAIL NAV LIGHT ASSY DAMAGED BY BAGGAGE CART. REPLACED RT WING TIP ASSY IAW MM 57-20-0. STATUS: CLOSED. 2 L 7 3 4F A3WE 2001041800283 20010418 00283 EU 2001 4 18 USAASA01006 1 20010219 A 3250 CONTROL UNIT AIRBUS 320 A320214 EU NLG STEERING FAILED A USAA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 EA 19 114UW 1148 AUA-PHL - FLT 654 - AFTER EXITING THE RUNWAY, THE AIRCAFT LOST NOSE WHEEL STEERING AND SYSTEM 2 BRAKING. AS A RESULT, T HE AIRCRAFT HAD TO BE TOWED TO THE GATE. MAINTENANCE PERFORMED BITE CHECK. THE BITE CHECK AND GROUND CHECK WERE NORMAL . (M) 2 L 7 2 4F RT A28NM 2001041800285 20010418 00285 WP 2001 4 18 DHL2001801003 1 20010331 A 2910 A602035509 REGULATOR DOUG DC8 DC873F 302199F WP HYD SYSTEM INOPERATIVE A DHLA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 801DH 46033 HYDRAULIC FLUID GUAGE INDICATED FLUID LOSS IN FLIGHT. PERFORMED ABNORMAL PROCEDURE. CORRECTIVE ACTION: FOUND ASPIRATO R REGULATOR LEAKING, REPLACED SAME PER 29-10-03. SERVICED SYSTEM, CYCLED FLIGHT CONTROLS, SERVICED SYSTEM AGAIN. CK NO RMAL, PER 29-10-0. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800288 20010418 00288 NM 2001 4 18 DHL2001745001 1 20010330 A 5210 5717623095 WINDSHIELD BOEING 727 727224 1384076 NM COKCPIT CRACKED A DHLA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 745DH 20665 L-2 WINDSHIELD CRACKED DURING CRUISE FLIGHT. CORRECTIVE ACTION: REPLACED L-2 WINDOW IAW B727 MM 56-12-11. OPS CK SERV ICABLE PRESSURIZED A/C ON GROUND. NO LEAKS NOTED. STATUS CLOSED. 2 L 7 3 4F A3WE 2001041800289 20010418 00289 NM 2001 4 18 DHL2001745002 1 20010330 A 2612 FIRE DETECTOR BOEING 727 727224 1384076 NM CARGO BAY FALSE INDICATION A DHLA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 745DH 20665 LOWER CARGO FIRE WARNING SOUNDED DURING CRUISE, DURING DESCENT, WARNING EXTINGUISHED, THEN CAME ON AGAIN DOWNWIND THEN OFF AGAIN ON LANDING. CORRECTIVE ACTION: TESTED LOWER FIRE WARNING ON GRND IAW 727MM 26-16-00. OPS TEST CHECKS SERVI CEABLE, NO DEFECTS NOTED. STATUS-CLOSED. 2 L 7 3 4F A3WE 2001041800290 20010418 00290 NM 2001 4 18 DHL2001720009 1 20010330 A 2913 5718607 PUMP BOEING 727 727228 NM HYD SYSTEM FAILED A DHLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 720DH 19544 DURING PREDEPARTURE NR 2 HYD B SYS PUMP INOP. CORRECTIVE ACTION: REPLACED NR 2 HYD ''B'' SYSTEM ELECTRIC PUMP AND RES ET NR 2 HYD PUMP FAULT DETECTOR. OPS CK GOOD IAW MM 29-12-11, MM 29-12-0, WDM 29-21-01. 2 L 7 3 4F A3WE 2001041800291 20010418 00291 EU 2001 4 18 DHL2001363005 1 20010402 A 5330 FRAME AIRBUS 300 A300B4203 3930306 EU FUSELAGE BENT A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH MAIN CARGO COMPARTMENT, STA 1499 STR. 7R, FRAME BENT AND GILL LINER TORN. CUT OUT DAMAGED AREA AT I/B SIDE OF FRAME AT S TA. 1499, STR.7R. FABRICATED REPAIR ANGLE. FABRICATED FRAME SHEER CLIP. PERFORMED NDT CUTOUT FRAME- NO CRACK INDICATI ON. INSTALLED NEW REINFORCEMENT J ANGLER DOUBLER AND EXTERIOR SKIN ATTACHMENT CLIP 2 L 7 2 4F RT A35EU 2001041800292 20010418 00292 2001 4 18 C1HA200182002 4 20010315 A 3442 MI5851641 ANTENNA BOEING 727 7272S7 138407Z NM FUSELAGE FAILED A C1HA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 682CA 22019 STABILIZATION ON WX RADAR IS INOP DURING TURB FLIGHT AND WHILE TURNING AIRCRAFT OR PITCH CHANGES OF AIRCRAFT. OVERWEIGH T LANDING WAS SMOOTH. REPLACED RADAR ANTENNA AND OPS CHECKED GOOD PER 34-41-22. PHASE 1 OVERWEIGHT LANDING INSPECTION COMPLIED WITH PER 5- 51-271. 2 L 7 3 4F A3WE 2001041800295 20010418 00295 EU 2001 4 18 DHL2001363001 1 20010306 A 2760 26V10TT4B01 TRANSMITTER AIRBUS 300 A300B4203 3930306 EU RT SPOILER MALFUNCTIONED A DHLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 363DH 085 DURING FLIGHT CONTROL CHK, RIGHT SPOILER ONLY INDICATES 7 DEG DEFLECTION. TRANSFERRED TO DM 4626 PER MEL 27-15-01-1 CAT B. SPECIAL PROCEDURE COMPLIED WITH. REMOVED AND REPLACED RT OUTER SPOILER POSITION TRANS IAW MM 27-15-11. OPS CK GOO D. PLACARD REMOVED. MXC NOTIFIED. DMI 4626 CLEARED. 2 L 7 2 4F RT A35EU 2001041800296 20010418 00296 NM 2001 4 18 C1HA200181002 1 20010302 A 3020 39270811 CONTROL VALVE BOEING 727 7272S7 138407Z NM ANTI-ICE SYS FAILED A C1HA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 681CA 22020 ENG NR 2 DUCT OVERHEAT LIGHT ILLUMINATED ON CLIMBOUT PERFORMED CHECKLIST REDUCED POWER AND TURNED ENG NR 2 ANTI-ICE OFF WHEN NO LONGER NEEDED. REMOVED AND REPLACED THERMOSTATIC CONTROL VALVE PER MM 30-21-21, PERFORMED HIGH POWER ENGINE RUN , OPS CHECKED GOOD AND NO LEAKS NOTED. 2 L 7 3 4F A3WE 2001041800297 20010418 00297 NM 2001 4 18 AWXA0001532 1 20010323 A 2782 6544517 ACTUATOR BOEING 737 73733A 1384673 NM L/E FLAP FAILED A AWXA O OTHER J WARNING INDICATION CR CRUISE 1 WP 28 167AW 56913 11211 23628 IAH - EMERGENCY LANDING - 3/18/01 - EN ROUTE FROM PHX TO IAH PRIOR TO DESCENT THE L/E FLAP TRANSIT AMBER LIGHT CAME ON A ND REMAINED ILLUMINATED; THE CREW LANDED IN IAH W/ FLAPS 15 PER THE QRH. MAINTENANCE FOUND THE SLAT CONTROL VALVE CABLE TENSIONS HIGH AND ADJUSTED IAW AMM 27-51-22 PG 406; AFTER THE AIRCRAFT RETURNED TO PHX ON A MAINTENANCE FERRY A COMPLET E TEST WAS PERFORMED ON THE L/E SLAT SYSTEMS. THE NR 1 KRUEGER FLAP ACT WAS REPLACED DUE TO EXCEEDING LEAK DOWN AND DRO OP LIMITS AND CABLES WFFA & WFFB ADJUSTED IAW AMM 27-51-00 PG 509; THE FOLLOWING COMPONENTS WERE ALSO REPLACED AS A PREC AUTION: HYD FUSE - PNEUDRAULICS INC. - P/N 6273-5 - LOC: MLG W/W; HYD.FUSE - DOWTY AEROSPACE - P/N 10-62204-5. 2 L 7 2 4F RT A16WE 2001041800301 20010418 00301 EA 2001 4 18 COMA0160332 1 20010322 A 2750 7455001 CONTROL HANDLE CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTIONED A COMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 01 936CA 780 7043 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FLAP CONTROL LEVER. 2 L 7 2 4F RT A21EA 2001041800307 20010418 00307 EU 2001 4 18 DHL2001366013 1 20010322 A 2822 PUMP AIRBUS 300 A300B4203 3930306 EU FUEL FAILED A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 366DH 249 TANK NR 2, PUMP NR 2 SHOWED AMBER AS WE WERE CLEARED FOR T/O AT JFK. TAXIED CLEAR OF 31L AFTER CANCELING T/O CLEARANCE AND RAN ABNORMAL PROCEDURE. T/S TO A BAD PUMP NR 2 PRESS SWITCH TRANSFERRED TO DMI 4852 IAW MEL 28-21-01-C CAT ''C'' PL ACARDED MXC NOTIFIED. 2 L 7 2 4F RT A35EU 2001041800308 20010418 00308 SO 2001 4 18 C2XA01BT041 1 20010319 A 3320 MS3470L106P SOCKET EMB 145 EMB145 SO CABIN SHORTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 14925 145004 CREW REPORTED BEFORE PUSHBACK PASSENGER IN SEAT 1A NOTICED SMOKE COMING FROM THE UPPER CABIN LIGHTING DIRECTLY OVER SEAT 1A. IND MECHANIC INSPECTED DISCONNECTED SHORTED LIGHT ASSY AND REMOVED BULB AND PLACARD 1A LATERAL LIGHT ON TO PLACARD 009968 MEL 33-20-00. ON 03/21/2001 BDL MAINTENANCE REMOVED AND REPLACED LATERAL LIGHT SOCKET OVERHEAD OF SEAT 1A AND R EPLACED BULB. OPS CHECKED GOOD IAW EMB145 MM 33-21-00, PLACARD REMOVED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2001041800310 20010418 00310 SO 2001 4 18 C2XA01BT042 1 20010322 A 2611 FDS765A2 SMOKE DETECTOR EMB 145 EMB145LR SO LAVATORY DEFECTIVE A C2XA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 27 13949 145057 APU BLEED CAUSES LAV SMOKE DETECTOR TO GO OFF. MEL 49-52-02, PLACARD 007786. MAINTENANCE REMOVED AND REPLACED LAV SMOK E DETECTOR IAW EMB145 MM 26-14-00. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2001041800311 20010418 00311 WP 2001 4 18 DHL2001802003 1 20010322 A 3000 SWITCH DOUG DC8 DC873F 302199F WP ANTI-ICE SYS FAULTY A DHLA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 802DH 46076 UNABLE TO MAINTAIN CABIN PRESS WITH FLOWS AT MAX MANUAL CONTROL FULL CLOSED. FOUND FAULTY SCOOP ANTI-ICE SWITCH CAUSING LT SCOOP VALVE TO INTERMITTINGLY STICK IN THE OPEN POSITION. REPLACED SWITCH PER MM 20-50-1. ALSO REPLACED LT SCOOP V ALVE AS PRECAUTION PER MM 30-20-2. OPS CK GOOD. OK FOR SERVICE. 2 L 7 4 4F RT 4A25 2001041800312 20010418 00312 NM 2001 4 18 DHL2001740003 1 20010403 A 3150 WARNING LIGHT BOEING 727 7272Q9 138448M NM NR 1 ENGINE ILLUMINATED A DHLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 740DH 21930 UPON NR 1 ENGINE STARTUP UNDER EXCITED SYSTEM NR 1, LIGHT ILLUMINATED ON S/O AUX PANEL. DEFERRED PER MEL 24-1. DMI 498 8 PLACARD INSTALLED. SP C/W. STATUS-OPEN. 2 L 7 3 4F RT A3WE 2001041800313 20010418 00313 NM 2001 4 18 DHL2001707003 1 20010330 A 5755 651734840 PANEL BOEING 727 72722 1384002 NM SPOILER DEBONDED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 UPON ROUTINE A-CHECK INSPECTION, FOUND THE 10 FLIGHT SPOILER PANEL LOWER SKIN SEPARATED FROM PANEL. THE OUTBOARD EDGE W AS COMPLETELY OPEN AND APPEARED THAT SKIN BONDING HAD FAILED. WHEN ATTEMPTING TO MOVE THE PANEL BY HAND, THE PANEL WOUL D BUCKLE UNDER PRESSURE. REMOVED AND REPLACED PANEL, AND PART SENT TO STORES FOR EVALUATION. STATUS-CLOSED. 2 L 7 3 4F A3WE 2001041800314 20010418 00314 NM 2001 4 18 DL76S010370 1 20010302 A 5330 141T32214 SKIN BOEING 767 767332 1382001 NM FUSELAGE TOOL DAMAGE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 125DL 24075 DURING ACCOMPLISHMENT OF A SRM SKIN REPAIR, TOOLING DAMAGE OCCURRED TO STR 39L. THIS DOCUMENT PROVIDES A REPAIR OF BOTH THE STRINGER AND SKIN. THE DAMAGE IS LOCATED AT STA 355. CORRECTIVE ACTION: ER/A 397313-14 2 L 7 2 4F RT A1NM 2001041800315 20010418 00315 NM 2001 4 18 DL76L010371 1 20010306 A 3350 BATTERY BOEING 767 767332 1382001 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 192DN 28449 EMERGNCY BATTERY CHARGER AT ROWS 6 A& B FAILED. REPLACED BATTERY CHARGER. 2 L 7 2 4F RT A1NM 2001041800316 20010418 00316 NE 2001 4 18 DL757010372 2 20010306 A 7200 ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 FAILED A DALA E C ENGINE SHUTDOWN ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SO 27 698DL 5538 29911 728728 ON TAKEOFF AT 1,200FT AGL, RIGHT ENG FAILED WITH A LOUD BANG AND AN EGT SPIKE TO 747 DEG C. MTC IN PROGRESS - ENG CHAN GE DUE 2 L 7 2 4F 4 F RT A2NM E17NE 2001041800317 20010418 00317 NM 2001 4 18 DLM90010373 1 20010306 A 3240 BRAKE DOUG MD90 MD9030 3023690 NM NR 2 OVERHEATED A DALA O OTHER M A J OVER TEMP FLAME/FIRE WARNING INDICATION LD LANDING 1 SO 27 911DA 3087 53391 AFTER LDG LT OUTBD BRAKE TEMP 575 LT INBD 500 DEGREES. LINEMAN REPORTED A FLAME FROM LEFT INBOARD BRAKE THAT WENT OUT AF TER A FEW SECONDS - REPLACED BRAKE 2 L 7 2 4F RT A6WE 2001041800318 20010418 00318 NM 2001 4 18 DLM88010374 1 20010306 A 3397 WIRE DOUG MD88 MD88 3023688 NM SEAT 31 BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 980DL 53267 SEAT 31DE E-PATH LIGHT INOP FOUND WIRES BROKEN TO LIGHT ASSY. REPAIRED WIRES BY SPLICING WIRES OPS CHK NML 2 L 7 2 4F RT A6WE 2001041800319 20010418 00319 WP 2001 4 18 DHL2001806501 1 20010308 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE DETERIORATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 FLIGHT CABIN 1/2 INCH CRACK ON 680 FLOOR MIDDLE PART IN LT ANGLE AT STA-12.000. REMOVED FASTNERS IAW SRM 51-1-21, REMOVE D DETERIORATED ANGLE IAW SRM 53-2-3. FABRICATED NEW ANGLE IAW SRM 52-3-3. CLEANED, TREATED, AND PRIMED IAW SRM 51-1-8B . INSTALLED NEW ANGLE IAW SRM 53-2-3 FIG 10; INSTALLED FASTNERS (RIVETS) IAW SRM 51-1-21 PAGE 1. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800320 20010418 00320 WP 2001 4 18 DHL2001806502 1 20010306 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 FWD CARGO COMPT - FLOOR SUPPORT ANGLE CRACKED 3 INCH AT STA 260, L-33 RT.PERFORMED STOP HOLE, FABRICATED DOUBLER (STEEL 301 1/4 H 0.040 INCH) AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1B. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800321 20010418 00321 WP 2001 4 18 DHL2001806530 1 20010308 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP COCKPIT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - FLIGHT CABIN 1/2 INCH CRACK ON 680 FLOOR MIDDLE PART IN RT ANGLE AT STA - 12.000. REMOVED FASTNERS IAQ SRM 5 1-1-21 PAGE 1. REMOVED DETERIORATED ANGLE IAW SRM 53-2-3 FIG 10. FABRICATED NEW ANGLE IAW 53-7-3 FIG 10 CLEANED, TRE ATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE IAW 53-2-3 FIG 10. INSTALLED RIVETS IAW SRM 51-1-21 PAGE 1. STATUS-C LOSED. 2 L 7 4 4F RT 4A25 2001041800322 20010418 00322 NM 2001 4 18 DLM11010375 1 20010305 A 5230 46265022 CONTROL UNIT DOUG MD11 MD11 3023602 NM CARGO DOOR DAMAGED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 810DE 48565 FOUND CENTER CARGO COMPARTMENT CARGO CONTROL UNIT DAMAGED DUE TO AN OVERHEAT CONDITION. ITEM WAS DISCOVERD WHILE WORKING AN MCO ON A DAMAGED CONNECTOR TO A POWER DRIVE UNIT IN THE CENTER CARGO BAY. IT APPEARS THAT THE OVERHEAT CONDITION WA S THE RESULT OF SHORTED WIRING AT THE POWER DRIVE UNIT CONNECTOR. THE CONNECTOR AND WIRING WERE REPAIRED AND THE CONTRO L UNIT REPLACED WITH NO FURTHER PROBLEMS. 2 L 7 3 4F RT A22WE 2001041800323 20010418 00323 NM 2001 4 18 DL73K010376 1 20010307 A 2751 INDICATOR BOEING 737 737232 1384475 NM TE FLAPS MALFUNCTIONED A DALA L ABORTED APPROACH N FALSE WARNING LD LANDING 1 SO 27 320DL 23092 ON GO AROUND FLAPS WOULD NOT RETRACT ABOVE 25 DEGREES NO ASSYMETRY NOTED. CORRECTIVE ACTION: FOUND EXTREME AMT OF I CE ON TE FLAPS DEICED FLAPS AND RAN THRU SEVERAL CYCLES OPS OK VISUAL CK OF FLAPS AND TORQUE TUBES FOUND OK REPLACED FLA P IND PRECAUTION OPS OK NOTE AIRCRAFT EXECUTED GO AROUND DUE TRAFFIC ON RUNWAY 2 L 7 2 4F RT A16WE 2001041800324 20010418 00324 NM 2001 4 18 DL73K010377 1 20010306 A 5314 6546877130 KEELBEAM BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 330DL 23102 THE RT STRINGER 18A SHEAR BEAM WAS FOUND WITH A WEB CRACK AT FS 727. THE CRACK IS TYPICAL OF THOSE FOUND IN BAC S/B 73 7-53-1066, HOWEVER THE S/B IS NOT EFFECTIVE FOR THIS AIRCRAFT. THE CRACK WAS STOP DRILLED AND REPAIRED WITH A STEEL RE PAIR CHANNEL PER ER/A 380238-14, REV A. 2 L 7 2 4F RT A16WE 2001041800325 20010418 00325 NM 2001 4 18 DL72S010378 1 20010305 A 5330 6554583161 SKIN BOEING 727 727232 1384082 NM FUSELAGE TORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 524DA 21584 THE FUSELAGE SKIN AND UNDERLYING TRIPLER WERE BADLY DAMAGED BY GROUND EQUIPMENT AT AN OUTFLOW VALVE CUTOUT BETWEEN FS 11 66 & 1183 AND BETWEEN STRINGERS 26R & 21R. THE SKIN AROUND THE OUTFLOW VALVE WAS CUT AWAY AND THE TRIPLER REMOVED. A N EW TRIPLER WAS INSTALLED AND A NEW SECTION OF SKIN SPLICE IN WITH AN EXTERNAL ALUMINUM SPLICE DOUBLER PER ER/A 380144-1 4, REV A. 2 L 7 3 4F A3WE 2001041800326 20010418 00326 2001 4 18 DL733010379 4 20010307 A 3421 INDICATOR BOEING 737 737347 1384647 NM COCKPIT FAILED A DALA O OTHER O OTHER CR CRUISE 1 SO 27 312WA 23598 STANDBY ATTITUDE INDICATOR FAILED ENROUTE. REPLACED STBY ATT INDICATOR. OPS NML 2 L 7 2 4F RT A16WE 2001041800327 20010418 00327 NM 2001 4 18 DLM88010380 1 20010307 A 2611 SA308C SMOKE DETECTOR DOUG MD88 MD88 3023688 NM LAVATORY INTERMITTENT A DALA O OTHER N FALSE WARNING CR CRUISE 1 SO 27 944DL 49817 FWD LAV SMOKE ALARM WENT OFF 3 TIMES DURING FLT WITH NO ONE OR NO SMOKE IN LAV. REPLACED FIRST CLASS LAV SMOKE DETECTO R - CKS OK 2 L 7 2 4F RT A6WE 2001041800328 20010418 00328 WP 2001 4 18 DHL2001806503 1 20010313 A 5510 37014272 FITTING DOUG DC8 DC873F 302199F WP HORIZONTAL STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 RT HORIZONTAL STABILIZER, LE INTERIOR LWR FITTING CRACKED 1 IN AT STA XFS 60.REMOVED CRACKED FITTING AT STA. XFS.60 OF R T HORIZONTAL STAB LE INTERIOR IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED, & PRIMED AREA IAW SRM 51-1-8 PAGE 12-13. INS TALLED NEW FITTING IAW SRM 51-1-20D PAGE 9. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800329 20010418 00329 WP 2001 4 18 DHL2001806512 1 20010317 A 5340 37502571 FITTING DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 FWD. CARGO COMPARTMENT - FITTING CRACKED 3 INCH BETWEEN STA. 440.000 AND STA. 460.000. L-31L REMOVED CRACKED FITTING F ROM FWD CARGO COMPT. STA. 440-460 L-31L IAW SRM 51-1-20D PAGE 21 CLEANED, TREATED, AND PRIMED IAW SRM 51-1-8 PAGE 12-15 INSTALLED NEW FITTING IAW SRM 51-1-20, PAGE 9. 2 L 7 4 4F RT 4A25 2001041800330 20010418 00330 WP 2001 4 18 DHL2001806513 1 20010316 A 5340 37502571 FITTING DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 FWD CARGO COMPARTMENT - FITTING CRACKED 6 INCHES BETWEEN STA 600.000 AND STA 620.000. L-31R. REMOVED CRACKED FITTING ( FWD CARGO COMPT STA 600-620, L-31R) IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED, AND PRIMED AREA IAW SRM 51-1-8 PAGE 12- 13. INSTALLED FITTING NEW IAW SRM 51-1-20D PAGE 9 PER TO N/R 0821 FOR ORIGINAL CERTIFICATE. (REF. SDR #DHL2001806513.) STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800331 20010418 00331 WP 2001 4 18 DHL2001806514 1 20010308 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 FWD CARGO COMPARTMENT FLOOR SUPPORT ANGLE CRACKED 1 INCH AT STA 180. L-31LT. PERFORMED STOP-HOLE TO ANGLE CRACKED IAW SRM 53-2-0 PAGE 2E/2F FIG . R/R FASTENERS IAW SRM 51-1-21 PAGE 1. CONDITIONED AND INSTALLED DOUBLER IAW SRM 53-2-0 P AGE 11. INSTALLED FASTENERS IAW SRM 51-1-20D, PAGE 9. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800332 20010418 00332 WP 2001 4 18 DHL2001806515 1 20010307 A 2820 BOLT DOUG DC8 DC873F 302199F WP FULE LINE MISINSTALLED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 806DH 46002 NR 1 ENGINE FUEL LINE BOLTS AT RT SIDE OF PYLON SHOW SAFETY IMPROPER. SAFETIED PROPERLY NR 1 ENGINE FUEL LINE BOLTS (P YLON RT. SIDE) IAW CFMI MM 70-00-40, PAGE 201, PARA 4. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800333 20010418 00333 WP 2001 4 18 DHL2001806504 1 20010308 A 5320 SUPPORT DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 FWD.CARGO BAY SIDE WALL SUPPORT ANGLE CRACKED 2 INCHES AT STA.180 L-32 RT. CORRECTIVE ACTION. PERFORMED STOP HOLE AND FA BRICATED SUPPORT ANGLE (STEEL 301 1/2 H 0.032) IAW SRM 53-2-0 FIG 18 AND INSTALLED IAW SRM 53-2-0 FIG 10 STATUS CLOSED. 2 L 7 4 4F RT 4A25 2001041800334 20010418 00334 WP 2001 4 18 DHL2001806505 1 20010307 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AFT CARGO-TUBING SUPPORT ANGLE BROKEN STA.1460 LT. REMOVED DAMAGED ANGLE (STA.1460 LT) IAW.SRM 51-1-21 PAGE1 FABRICATED NEW ANGLE IAW.SRM 53-2-0 PAGE 12 CLEANED,TREATED & PRIMED IAW-SRM 51-1-88 INSTALLED NEW ANGLE IAW-SRM51-1-21 PAGE1 STAT US CLOSED 2 L 7 4 4F RT 4A25 2001041800335 20010418 00335 NM 2001 4 18 DHL2001742003 1 20010403 A 2720 65415965 COVER BOEING 727 727225 1384077 NM RUDDER PEDALS BINDING A DHLA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 742DH 21290 F/O RUDDER PEDAL ADJ PROBLEM. FOUND FIBERGLASS FAIRING BINDING ON PEDALS. RE-TAPED FAIRING AND OP CHECKED FOR RUDDER P EDAL PER M/M 27-20-0. DMI 4836E IN EFFECT. STATUS-OPEN. 2 L 7 3 4F A3WE 2001041800336 20010418 00336 WP 2001 4 18 DHL2001806516 1 20010318 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP FUSELAGE BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 FWD CARGO COMPARTMENT SHOWS FLOOR SUPPORT BROKEN BETWEEN STA 120-180, L34L. REMOVED BROKEN FLOOR SUPPORTING ANGLE BETWE EN STA 120.00 AND STA 180.00, L-34L.IAW SRM 51-1-21. FABRICATED NEW FLOOR SUPPORTING ANGLE IAW SRM 53-2-0 FIG 1B. CLE ANED, TREATED, AND PRIMED IAW SRM 51-18B PAGE 12 AND 13. INSTALLED FLOOR SUPPORTING ANGLE IAW SRM 51-1-21 STATUS-CLOSED . 2 L 7 4 4F RT 4A25 2001041800338 20010418 00338 WP 2001 4 18 DHL2001806506 1 20010310 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - FWD CARGO COMPARTMENT FLOOR SUPPORT ANGLE CRACKED 1 INCH AT STA. 220 L-35 LT CORRECTIVE ACTION: PERFORMED STOP HOLE. FABRICATED REINFORCING ANGLE AND INSTALLED IAW SRM 53-2-3 FIG 10. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800339 20010418 00339 WP 2001 4 18 DHL2001806507 1 20010308 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 FWD CARGO COMPT FLOOR SUPPORT ANGLE CRACKED 1 INCH AT STA. 120 L-33RH.PERFORMED STOP HOLE,FABRICATED REINFORCING ANGLE A ND INSTALLED IAW.SRM 53-20-0 FIG.1B STATUS CLOSED 2 L 7 4 4F RT 4A25 2001041800340 20010418 00340 EU 2001 4 18 DHL2001364012 1 20010411 A 3242 C200601004 BRAKE AIRBUS 300 A300B4203 3930306 EU NR 7 OVERHEATED A DHLA C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SO 01 364DH 0141 UPON TAKEOFF, BRAKES HOT LIGHT CAME ON MWP, REJECTED TAKEOFF NR 3 BRAKE WAS INDICATING 300C AND BRAKE NR 7, 250C. R&R NR 7 BRAKE ASSY IAW MM 32-42-27. OPS & LEAK CHK OK. DEACTIVATED NR 3 BRAKE AND DEFERRED IAW MEL 32-42-09-1 CAT C, ENTE RED AS DMI 5122. R&R NR 7 + NR 3 BRAKE ASSEMBLIES. DMI CLOSED. STATUS-CLOSED 2 L 7 2 4F RT A35EU 2001041800341 20010418 00341 WP 2001 4 18 DHL2001806537 1 20010306 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - FWD CARGO COMPARTMENT FLOOR SUPPORT PLATE CRACKED 1 INCH STA 420 - 440, L-33R TO L-34R. FABRICATED DOUBLER I AW SRM 53-2-3 PAGE 1. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 530203 PAGE 1, SRM 51-1-2 1 PAGE 1. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800342 20010418 00342 WP 2001 4 18 DHL2001806538 1 20010309 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - FWD. CARGO COMPARTMENT FLOOR SUPPORT ANGLE CRACKED 1 1/2 INCH AT STA 420.000, L33L-L-34L. REMOVED FASTENERS IAW SRM 51-1-21 FIG 1. FABRICATED DOUBLER WITH STEEL IAW SRM 53-2-3 FIG 10. TREATED AND PRIMED IAW SRM 51-1-8 PAGE 12- 13. INSTALLED DOUBLER IAW SRM 51-1-21 PAGE 1. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800343 20010418 00343 WP 2001 4 18 DHL2001806539 1 20010307 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - FWD CARGO COMPARTMENT FLOOR SUPPORT ANGLE CRACKED 3 INCH STA 420, L-30LT TO L-31LT. FABRICATED REINFORCING AN GLE IAW SRM 53-2-3 FIG 10 AND INSTALLED REINFORCING ANGLE IAW SRM 51-1-21 PAGE21. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800344 20010418 00344 NM 2001 4 18 01FDEA00221 1 20010322 A 2781 CONNECTOR BOEING 727 727232 1384082 NM L/E FLAP FAULTY A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 499FE 21018 NR 4 LEAD EDGE FLAP WOULD NOT RETRACT WHEN FLAPS MOVED FROM 5 DEG TO 2 DEG. *S/D* REPLACED PLUG OPS CK GOOD. CHANGED CANNON PLUG D904 IAW WDM 27-81-02. RAN NR 1 ENG PER 727 JRH CK LWDT WING LEAD EDGE DISTRIBUTION MANIFOLD FOR LEAKS PER MM 30-13-000-5. NONE FOUND. 2 L 7 3 4F A3WE 2001041800345 20010418 00345 EA 2001 4 18 HNAA0100020 1 20010320 A 2434 GENERATOR DHAV DHC8 DHC8311 1386006 EA NR 1 ENGINE FAILED A HNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 07 343EN 340 AT 9000 FT, CREW REPORTED A LOUD EXPLOSION AND SIMULTANEOUSLY NR 1 DC GENERATOR DROPPED OFF LINE. NO VISIBLE LIGHTNING IN AREA AND LIGHT PRECIP ON RADAR. THE F/A REPORTED SEEING A BRIGHT FLASH AND LOUD BOOM IN THE ROW 2 AREA OF THE CABIN. CREW COMPLETED IN-FLIGHT LIGHTNING CHECK AND RETURNED TO CLT. 2 H 7 2 4T RT A13NM 2001041800346 20010418 00346 EU 2001 4 18 DHL2001365002 1 20010402 A 5280 DOOR AIRBUS 300 A300B4203 3930306 EU NLG VIBRATION A DHLA J A DUMP FUEL UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 01 365DH 149 EXCESSIVE VIBRATION CAUSED RETURN TO DFW. VIBRATION WAS EXCESSIVE AS LONG AS GEAR WAS RETRACTED. ON GEAR EXTENSION VIB RATION LESSENED.REMOVED LEFT HAND NOSE GEAR DOOR AND LT & RT AFT NOSE GEAR DOORS TO COMPLY WITH REVISED CDL 52-10 PER MM 32-00-00 PG 437 & 32-22-13. REF ITEM 1P L/P 216049. STATUS-OPEN. 2 L 7 2 4F RT A35EU 2001041800360 20010418 00360 WP 2001 4 18 DHL2001806531 1 20010319 A 5753 RIB DOUG DC8 DC873F 302199F WP RT WING TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - RT WING INBOARD FLAP INTERIOR SKIN RIB SHOWS CRACKS AT STA XRS 162.263. STOP DRILLED IAW SRM 57-2-0 FIG 2. F ABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. S TATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800361 20010418 00361 WP 2001 4 18 DHL2001806532 1 20010307 A 5320 SUPPORT BRACKET DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - FWD. CARGO COMPT SIDE WALL SUPPORT ANGLE CRACKED 1 INCH AT STA 160 L-31RT. REMOVED FASTENERS IAW SRM 51-1-20 D PAGE 21. FABRICATED DOUBLER ANGLE IAW SRM 53-7-0 FIG 1B. TREATED, AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER ANG LE IAW SRM 53-2-0 FIG 1B. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800365 20010418 00365 NM 2001 4 18 DHL2001715004 1 20010410 A 5320 65186214 SILL BOEING 727 727155C 138404Z NM DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 FAA INSPECTION FOUND LWR BELLY DOOR FWD THRESHOLD SILL-PLATE CRACKED.REMOVED OLD SILL-PLATE AND INSTALLED SERVICABLE PLA TE IAW M/M 53-13-0. STATUS-CLOSED. 2 L 7 3 4F A3WE 2001041800366 20010418 00366 WP 2001 4 18 DHL2001806540 1 20010306 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - FWD CARGO COMPT. FLOOR SUPPORT ANGLE CRACKED 2 INCH AT STA 460, L-31LT TO L-32LT. PERFORMED STOP HOLE AND FA BRICATED DOUBLER AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1B. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800367 20010418 00367 2001 4 18 DHL2001363004 4 20010414 A 2200 COMPUTER AIRBUS 300 A300B4103 3930104 EU AFCS FAILED A DHLA O OTHER O OTHER AP APPROACH 1 SO 01 363DH 085 AUTOPILOTS NR 1 AND NR 2 TRIPPED OFF REPEATEDLY DURING APPROACH. AFCS SHOWS BOTH LOGIC MONITOR COMPUTERS TRIPPED. RE SET AFCS AND RESEATED BOTH LOGIC MONITOR COMPUTERS AND OPS CHECK BOTH AUTOPILOT PER 22-10-00 GOOD. STATUS-CLOSED. 2 L 7 2 4F RT A35EU 2001041800368 20010418 00368 2001 4 18 DHL2001362011 4 20010414 A 2210 AUTOPILOT SYS AIRBUS 300 A300B4103 3930104 EU E/E BAY FAILED A DHLA O OTHER O OTHER CR CRUISE 1 SO 01 362DH 84 NR 1 AUTOPILOT WILL NOT ENGAGE, NR 2 A/P OPERATES NORMALLY. DEFERRED NR 1 AUTOPILOT AS PER MEL 22-11-01. 2 L 7 2 4F RT A35EU 2001041800369 20010418 00369 WP 2001 4 18 DHL2001806571 1 20010318 A 5320 WEB DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - MAIN CARGO SUBFLOOR SHOWS 02 EA CRACKS 3/8 AND 5/8 RBL 8 1/2 STA 25.000. PERFORMED STOP HOLE AND FABRICATED DOUBLER IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1B . STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800371 20010418 00371 EU 2001 4 18 QXEA0100319 1 20010228 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 YYC-CRACKED CASTELLATION AT FRAME 8305 AND STRINGER 41. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 53-16-04, PAGE 16. 2 L 7 2 4F RT A20EU 2001041800373 20010418 00373 EU 2001 4 18 C2XA01IA173 1 20010321 A 2120 SMOKE AEROSP ATR42 ATR42320 8680930 EU CABIN DETECTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 99838 259 IAH - FLIGHT 3499, THE CREW REPORTED A FAINT SMELL AND SMOKE IN THE CABIN DURING TAXI AFTER SHUTTING DOWN THE NUMBER ONE ENINE. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE ENGINES AND AIR CONDITIONING SYSTEM WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001041800374 20010418 00374 SO 2001 4 18 C2XA01IA174 1 20010320 A 5755 PE640424601605 BUSHING EMB 145 EMB145ER SO SPOILER CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14942 145037 IAH - DURING C-CHECK INSPECTION, THE LEFT WING SPOILER CENTER ATTACH BUSHING WAS FOUND TO BE RUSTY. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUSHING, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001041800375 20010418 00375 SO 2001 4 18 C2XA01IA175 1 20010320 A 5315 14521725013 FLOORBEAM EMB 145 EMB145ER SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14942 145037 IAH - DURING C-CHECK INSPECTION, THE RIGHT HAND OUTBOARD FLOORBEAM WAS FOUND TO BE CORRODED FROM FRAME 18 TO FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IN ACCORDANCE WITH EMB145 SRM51-40-02, AND THE AIRCRAFT WAS APPR OVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001041800376 20010418 00376 SO 2001 4 18 C2XA01IA176 1 20010320 A 5315 14522226003 FLOORBEAM EMB 145 EMB145ER SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14942 145037 IAH - DURING C-CHECK INSPECTION, THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED FROM FRAME 59 TO FRAME 61. MAINTENANCE R EMOVED AND REPLACED THE AFFECTED FLOORBEAM IN ACCORDANCE WITH EMB 145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RE TURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001041800377 20010418 00377 SO 2001 4 18 C2XA01IA177 1 20010322 A 3350 3025103 LIGHT EMB 145 EMB145LR SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13970 145146 IAH - DURING A-CHECK INSPECTION, THE RIGHT HAND OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001041800378 20010418 00378 EU 2001 4 18 RAIA00103014 1 20010322 A 3260 AIR135864 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU NLG FAILED A RAIA O OTHER P NO WARNING INDICATION CR CRUISE 1 CE 03 563HK 0 0 41079 5382-RIC- DURING FLIGHT NOSE LANDING GEAR INTRANSIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR MICRO SWITCH IAW J41 MAINTENANCE MANUAL. 2 L 7 2 4T RT A41NM 2001041800379 20010418 00379 WP 2001 4 18 CALA0100241 1 20010322 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72822 49482 INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 200 - 220 BETWEEN LONGERON 17L AND 18L. THE SKIN WAS REPAIRED IAW ECRA 5330-02471. 2 L 7 2 4F A6WE 2001041800380 20010418 00380 WP 2001 4 18 CALA0100242 1 20010322 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72822 49482 INSPECTION FOUND E&E BAY OVERHEAD FLOOR WEB PANEL HAD CORROSION BLEEDING OUT FROM THE FLOORBEAM AND LOWER SURFACE OF WEB PANEL AT STA 200, RBL 10. THE FLOOR PANEL WAS REMOVED FOR ACCESS AND THE CORROSION WAS REMOVED IAW SRM 51-10-3. THE C ORROSION WAS FOUND OUT OF LIMITS IAW SRM 51-10-3. THE FLOOR SUPPORT WAS REMOVED FOR ACCESS IAW SRM 51-30-2. A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 4, SHEET 3 AND 51-30-2. THE SUPPORT AND FLOOR PANEL WERE INSTALLED IAW ECRA 5100-01 844. 2 L 7 2 4F A6WE 2001041800381 20010418 00381 WP 2001 4 18 CALA0100243 1 20010322 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72822 49482 INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 463 BETWEEN LONGERON 16R AND 17R. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, VIEW E, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 2001041800382 20010418 00382 WP 2001 4 18 DHL2001806508 1 20010307 A 5350 FAIRING DOUG DC8 DC873F 302199F WP WING TO BODY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK.- LT WING TO FUSELAGE FAIRING SUPPORT ANGLE CRACKED 3/4 INCH AT STA. 640 L-21LT. TO L-22 LT. REMOVED FAIRING SUP PORT ANGLE IAW SRM.51-1-21 PAGE 1 FABRICATED ANGLE IAW. SRM 53-2-0 FIG 1B CLEANED,TREATED & PRIMED IAW SRM 51-1-8B INST ALLED ANGLE IAW.SRM 51-1-21 PAGE 1 STATUS CLOSED. 2 L 7 4 4F RT 4A25 2001041800383 20010418 00383 WP 2001 4 18 CALA0100244 1 20010322 A 5510 SUPPORT DOUG DC10 DC1030 3023501 WP HORIZ STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14062 47863 INSPECTION FOUND A 1.5 INCH CRACK IN LT HORIZONTAL STABILIZER SECONDARY PIVOT SUPPORT. THE PIVOT SUPPORT WAS REPLACED I AW EA 5310-03417 AND ECRA 5310-04118. 2 L 7 3 4F A22WE 2001041800384 20010418 00384 NM 2001 4 18 CALA0100245 1 20010322 A 5320 FLOOR SUPPORT BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14384 26313 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 500D BETWEEN STRINGER 26L AND 26R IN FORWARD CARGO AREA. THE FLOOR SUPPO RT WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND 53-30-53. 2 L 7 2 4F RT A16WE 2001041800385 20010418 00385 SO 2001 4 18 C2XA01TY055 1 20010321 A 5751 14569009408 ATTACH FITTING EMB 145 EMB145LR SO RT AILERON GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13978 145180 TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND AILERON TO PCA ATTACH FITTING WAS FOUND GOUGED AND CHAFED. MAINTENANC E REMOVED AND REPLACED THE ATTACH FITTING IAW EMB GST-0903/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEAS ED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2001041800386 20010418 00386 NM 2001 4 18 QXEA0100417 1 20010316 A 2611 7504311 WARN PANEL DHAV DHC8 DHC8202 2809007 NM COCKPIT FAULTY A QXEA K NONE N FALSE WARNING CR CRUISE 1 NM 09 353PH 6126 6126 496 SEA-SMOKE WARNING LIGHT ILLUMINATED INTERMITTANTLY DURING FLIGHT. REMOVED AND REPLACED WARNING LIGHT PANEL AND WARNING LIGHT CONTROL UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001041800387 20010418 00387 NM 2001 4 18 DHL2001741511 1 20010319 A 5711 SPAR BOEING 727 7272Q9 138448M NM RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 RIGHT WING, LOWER SPAR HAS EXFOLIATED CORROSION UNDER CAVITY CUTOUT FOR NR 8 LEADING EDGE SLATACTUATOR. REMOVED L/E ACC ESS PANELS 6542; 6543 6546 AND 6540 AT RIGHT WING LOWER SURFACEAS PER B727 SRM 51-30-2. REMOVED FUEL ACCESS PANELS AT RT WING LOWER SURFACE FOR ACCESS TO WORK AS PER B 727 SRM 51-30 2. 7702-7701-7618. REMOVED FUEL DUMP PLUMBING AT WING STATION 738.50 IAW M/M B-727 28-31-31. REMOVED I/B AND O/B ANGLE ACTUATOR SUPPORT AND INNER BOX AT NR 8 LEADING EDGE S LAP AS PER B727 SRM 51-30-2. CUT OUT RT WING LOWER SPAR STA 749 TO STA 726.68 AS PER B 727 SRM 57-10-6 21.75 INCHES LO NG. REMOVED 4 L/E ACCESS PANEL SUPPORT WS 740 TO 720 AS PER B727 SRM 51-30-2. REMOVED OLD SEALANT. 2 L 7 3 4F RT A3WE 2001041800388 20010418 00388 NM 2001 4 18 DHA2001741512 1 20010307 A 5320 WEB BOEING 727 7272Q9 138448M NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 CABIN FLOOR WEB 1183 TO 1166 RBL 24 TO 45 HAS SEVERAL ELONGATED HOLES AND CORROSION AT FASTENERS. CUT OUT DAMAGED AREA AT CABIN FLOOR WEB STA 1183 TO STA 1166 RBL 24 TO 45 IN SEVERAL SECTIONS IAW B727 SRM 51-40-2. INSTALLED DOUBLER REPAIR AT CABIN FLOOR WEB STA 1183 TO 1166 & RBL 24 TO RBL 45. MAT USED 2024 T3 .080 PO 8319589 LOT 130164 SIZE 2 X 1 IAW B72 7 SRM 51-40-2. TREATED AND PRIMED REPAIR DOUBLER IAW B727 SRM 51-10-2. 2 L 7 3 4F RT A3WE 2001041800389 20010418 00389 NM 2001 4 18 DHA2001741513 1 20010315 A 7110 SKIN BOEING 727 7272Q9 138448M NM COWLING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 NR 1 ENG UPPER COWL OUTER SKIN DAMAGED AT 3RD LATCH CUTOUT FROM OUTBOARD FWD SIDE. REMOVED LOWER ROW OF FASTENERS AND S TOP DRILL CRACK AS PER SRM 51-10-1 (COWL SKIN) NR 1 ENG 0.50, FABRICATED DOUBLER AS PER SRM 54-10-3 MATERIAL 7075-T6 ML 207155, INSTALLED DOUBLER REPAIR AT NR 1 ENG UPPER COWL OUTER SKIN 3RD LATCH FROM OUTBOARD FWD SIDE AS PER SRM 51-10-2. TREATED AND PRIMED AS PER SRM 51-10-2. MATERIAL USED 7075T6 .050 MAT SIZE 12 X 6 INCHES PO 207155 AS PER B727 SRM 54-1 0-3. NR 1 ENGINE UPPER COWL OUTER SKIN DAMAGED AT 3RD LATCH CUTOUT FROM OUTBOARD FWD SIDE. REMOVAL OF FASTENERS AND ST OP DRILL CRACK AS PER SRM 51-10-1. 2 L 7 3 4F RT A3WE 2001041800390 20010418 00390 NM 2001 4 18 DHL2001741514 1 20010314 A 7110 ATTACH ANGLE BOEING 727 7272Q9 138448M NM COWLING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 NR 3 ENGINE LOWER COWL LEFT I/B SIDE FWD NR 1 LATCH CUTOUT ATTACH ANGLE CRACKED AT O/B RADIUS. REMOVED ATTACH ANGLE AT LEFT I/B SIDE FWD OF NR 1 LATCH CUTOUT AS PER B727 SRM 51-30-2. FABRICATE NEW ATTACH ANGLE AS PER B727 SRM 54-10-2 FIG 2. MAT USED 7075 -O .050 16 X 4 INCHES LOT 299214 PO 8319222. HEAT TREATED TO 7075 T6 AS PER GENERAL PROCESS SPECIFICA TIONS 98PMS1.247PS-01. TRIMMED ATTACH ANGLE, PICKED-UP HOLES, DEBUR, TREATED AND PRIMED AS PER B727 SRM 51-10-1 & 51-10 -2. INSTALLED ATTACH ANGLE AT NR 3 ENG LOWER COWL LEFT I/B SIDE FWD NR 1 LATCH CUTOUT AS PER B727SRM 51-30-2. 2 L 7 3 4F RT A3WE 2001041800391 20010418 00391 NM 2001 4 18 DHL2001741515 1 20010315 A 7110 SKIN BOEING 727 7272Q9 138448M NM COWLING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 NR 3 ENGINE UPPER COWL O/B AFT CORNER SKIN AND ATTACH SUPPORT FOR RUB SEAL RETAINER ARE GOUGED AND CRACKED. STOP DRILLE D CRACKS PER B727 SRM 51-10-1 ON THE NR 3 ENGINE UPPER COWL O/B AFT CORNER SKIN. PERFORMED HFEC INSP PER B727 NDT MANUA L PART 6-51-00-00 FIG 4. NO CRACKS INDICATED PAST STOP DRILL. FABRICATED REPAIR DOUBLER USING 2024-T3 .040 6 X 12 INCH ES IAW B727 SRM 54-10-3 PG 22. TREATED AND PRIMED REPAIR DOUBLER IAW B727 SRM 51-10-2. LOT 241561 & LOT 8F0ZK14TO. IN STALLED REPAIR DOUBLER IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2001041800392 20010418 00392 NM 2001 4 18 DHL2001741516 1 20010309 A 5320 FLOOR SUPPORT BOEING 727 7272Q9 138448M NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 FWD LAV COMPARTMENT FLOOR SUPPORT CORRODED IN SEVERAL AREAS AND AROUND NUT PLATES (BLUE WATER STAINS). REMOVED CORROSIO N AS PER B727 SRM 51-10-6. MATERIAL LOSS .030 FOUND OUT OF LIMITS AS PER B727 SRM 53-30-1. CUT OUT DAMAGED AREA ON FLOO RBEAM AT BS 312RBL 39 INCHES 3.5 X .75 INCH AS PER B727 SRM 53-10-8. FABRICATED FLOORBEAM REPAIR MATERIAL USED 7075 T6 .080 & 7075T6 .050. PO 83112244 LOT# BV12MTBR & LOT761D6 687, PO 83110094 AS PER B727 SRM 53-10-8. LENGTH OF REPAIR 15 X 1 & 13 X 1 X 1. TREATED AND PRIMED AREA AS PER B727SRM 51-10-2. INSTALLED FLOORBEAM REPAIR MAT USED7075-T6.080, 7075 -T6 .050 PO 83112244 LOT BV12MTOR AND LOT 76106687 PO 83110094 IAW B727 SRM 53-10-8. 2 L 7 3 4F RT A3WE 2001041800393 20010418 00393 WP 2001 4 18 DHL2001806517 1 20010316 A 5710 FAIRING DOUG DC8 DC873F 302199F WP LT WING BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LT WING TE LOWER FAIRING BROKEN 1 INCH AT XW 106.000. PERFORMED STOP HOLE AND FABRICATED DOUBLER IAW SRM 57- 2-0 PAGE 1B. CLEANED, TREATED, AND PRIMED IAW SRM 51-1-0 PAGE 12-13. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 1B. STATUS- CLOSED. 2 L 7 4 4F RT 4A25 2001041800394 20010418 00394 SO 2001 4 18 C2XA01IA179 1 20010323 A 5280 12036136001 HINGE FITTING EMB 120 EMB120ER 3260203 SO LT MLG DOOR BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16724 120171 ILE- ON POSTFLIGHT INSPECTION THE CREW FOUND THE LEFT OUTBOARD MAIN GEAR DOOR AFT HINGE BROKEN. MAINTENANCE REMOVED THE LEFT OUTBOARD AFT MAIN LANDING GEAR DOOR, AND THE AIRCRAFT WAS FERRIED FROM ILE TO IAH. IAH MAINTENANCE REPLACED THE A FT HINGE FITTING ON THE LEFT HAND AFT OUTBOARD MAIN LANDING GEAR DOOR AND INSTALLED THE DOOR ON THE AIRCRAFT. OPS CHECK /GEAR SWINGS, CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001041800395 20010418 00395 EA 2001 4 18 JBXA000260 1 20010324 A 2913 PUMP CNDAIR CL600 CL6002B19 EA NR ENGINE LEAKING A JBXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 05 578ML 7270 HYDRAULIC NR 2 LOW PRESSURE IN FLIGHT AIR-RETURN TO RDU. REMOVED AND REPLACED NR 2 HYDRAULIC ENGINE DRIVEN PUMP AND HIG H PRESSURE RETURN LINE IAW CRJ AMM 29-11-52. LEAK AND OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2001041800396 20010418 00396 NM 2001 4 18 PCAA0103020 1 20010322 A 5610 0780306 WINDSHIELD DHAV DHC8 DHC8102 2809003 NM COCKPIT CRACKED A PCAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 13 808EX 13748 299 SYR-FLIGHT 3593. IN CRUISE FLIGHT AT 15,000 FT EAST OF SYR, FIRST OFFICERS WINDSCREEN CRACKED AND BECAME TOTALLY DISTOR TED. EMERGENCY DECLARED AND FLIGHT DIVERTED TO SYR, LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED FIRST OFFICE RS WINDSHIELD IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL. OPERATIONAL CHECK OF WINDSHIELD GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001041800397 20010418 00397 SO 2001 4 18 C2XA01IA180 1 20010320 A 3260 12038594001 MODULE EMB 120 EMB120ER 3260203 SO COCKPIT FAULTY A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 40717 120133 IAH- RED GEAR SYSTEM-A REMAINED ILLUMINATED IN FLIGHT. IAH- MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL M ODULE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001041800398 20010418 00398 WP 2001 4 18 DHL2001806518 1 20010308 A 5320 SUPPORT BRACKET DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - FWD. CARGO. COMPARTMENT LINING SUPPORT ANGLE AT STA 220 L-33L SHOWS CRACK OF 1/2 INCH. PERFORMED STOP HOLE AN D FABRICATED DOUBLER IAW SRM 53-2-0 PAGE 2E/2F FIG 1B. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B PAGE 1-2. INSTALLED DOUBLER IAW SRM 53-2-0 PAGE 2E/2F. STATUS CLOSED. 2 L 7 4 4F RT 4A25 2001041800399 20010418 00399 WP 2001 4 18 DHL2001806519 1 20010306 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP CARGO BAY BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - AFT CARGO COMPARTMENT - LOWER RT FLOOR PANEL BROKEN 2 INCH. REMOVED DAMAGED FLOOR PANEL IAW SRM 51-3-0. FABRI CATED NEW FLOOR PANEL IAW SRM 53-2-3 FIG 10. CLEANED, TREATED, AND PRIMED IAW SRM 51-1-8B PAGE 12-13. INSTALLED FLOOR PANEL IAW SRM 51-3-0 PAGE 2 AND 3. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800401 20010418 00401 WP 2001 4 18 ABXA010105 1 20010319 A 5320 SB095301662992 STIFFENER DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 948AX 56762 47065 AFT PRESSURE BULKHEAD LEFT HOIZONTAL STIFFENER WERE CRACKED ADJACENT TO LONGERON 14 AND 15L. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2001041800402 20010418 00402 WP 2001 4 18 DHL2001806520 1 20010314 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - FWD. CARGO COMPARTMENT FLOOR PANEL SUPPORTING ANGLE CRACKED 3 INCHES, STA. 220.00 L-33 R.REMOVED DAMAGED AREA IAW SRM 53-2-0 PAGE 11. FABRICATED DOUBLER IAW SRM 53-2-0 PAGE 11. INSTALLED DOUBLER IAW SRM 53-2-0 PAGE 11. STATUS-C LOSED. 2 L 7 4 4F RT 4A25 2001041800403 20010418 00403 WP 2001 4 18 DHL2001806521 1 20010318 A 5320 ANGLE DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - FWD. CARGO BAY TRANSVERSAL ANGLE CRACKED 1/2 INCH AT STA 260 L-33RT. PERFORMED STOP HOLE, FABRICATED DOUBLER I AW SRM 53-2-0 FIG 1B. CLEANED, TREATED, AND PRIMED IAW SRM 51-1-8B AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1B. STATUS -CLOSED. 2 L 7 4 4F RT 4A25 2001041800404 20010418 00404 WP 2001 4 18 DHL2001806522 1 20010317 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - FWD. CARGO COMPARTMENT - FLOOR SUPPORT ANGLE CRACKED 2 INCHES AT STA 200 L-35RT. PERFORMED STOP HOLE, FABRICA TED DOUBLER AND INSTALLED IAW SRM 53-2-0 FIG 1B. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800405 20010418 00405 WP 2001 4 18 01FDEA00223 1 20010323 A 3230 LANDING GEAR DOUG DC10 DC1010F 3022111 WP RT MLG MALFUNCTIONED A FDEA O OTHER E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 25 052FE 47806 AT APPROX 3000 FT IN CLIMBOUT RMG UNSAFE LIGHT ILLUM. S/O PNL LIGHT REMAIN OFF. PILOT NOTICED AIRFRAME VIBRATION IN SE AT AND CONTROL WHEEL. LG RECYCLED. ALL GEAR LIGHTS WENT OUT AND VIBRATION CEASED. 2 L 7 3 4F A22WE 2001041800406 20010418 00406 NM 2001 4 18 01FDEA00225 1 20010323 A 2781 40173 POSITION SWITCH BOEING 727 727232 1384082 NM L/E FLAP FAILED A FDEA J A DUMP FUEL UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 499FE 21018 WHILE RETRACT FLAPS NR 4 L/E DEVICE WOULD NOT RETRACT WHEN FLAPS MOVED FROM 5 DEG TO 2 DEG. DUMP FUEL. COULD NOT DUPLI CATE. AS PRECAUTIONARY REMOVED AND REPLACED NR 4 L/E FLAP POSITION SWITCH REF B727-200 MM 27-82-001-4. REMOVED AND REP LACED CONTROL MODULE AT S/O''''S STATION MM 27-82-031-4. PERF OPS OF FLAPS NUMEROUS TIMES, OPS NORMAL. 2 L 7 3 4F A3WE 2001041800407 20010418 00407 NM 2001 4 18 01FDEA00226 1 20010323 A 3230 LANDING GEAR BOEING 727 727233 138408A NM NLG & MLG MALFUNCTIONED A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 272FE 22037 LANDING GEAR FAILED TO RETRACT. RAN CKLIST, CK CB AND WAS NOT POPPED, ATTEMPT 2ND RETRACT AND WAS SUCCESSFUL. PERF LG HANDLE LOCK SYS ADJUSTMENT AND TEST PER 727-200 MM 32-31-011-5. CK OK. NO BINDING OR STICKING NOTED DURING ACTUATION. 2 L 7 3 4F RT A3WE 2001050100172 20010501 00172 NM 2001 5 1 01FDEA00228 1 20010324 A 5531 RIB BOEING 727 72722 1384002 NM RUDDER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 168FE 18865 DURING ROUTINE INSP HFEC IND THE LWR RUDDER, THRUST HINGE RIB FITTING WAS CRACKED AT FWD RIGHT SIDE. *S/D* REMOVED AND REPLACED RUDDER THRUST HINGE RIB PER IAW FEDEX EO 7-5550-7-2303C PART 2. 2 L 7 3 4F A3WE 2001041800408 20010418 00408 WP 2001 4 18 ABXA010104 1 20010319 A 5320 3917624511 FITTING DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 948AX 56762 47065 RIGHT LOWER VENTRAL DOOR STOP FITTING WAS CRACKED. MAINTENANCE INSPECTED AND REPLACED THE DOOR STOP FITTING IAW DC-9 SR M 51-30-2. 2 L 7 2 4F A6WE 2001041800409 20010418 00409 WP 2001 4 18 ABXA010103 1 20010319 A 5320 INTERCOSTAL DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 948AX 56762 47065 INTERCOSTAL WAS CRACKED AT FASTENER HOLE ON AFT SIDE OF FUSELAGE STATION 1143, JUST OUTBOARD OF LEFT RUDDER TORQUE TUBE VERTICAL ATTACH FITTING. MAINTENANCE INSPECTED AND REPAIRED THE INTERCOSTAL IAW DC-9 SUPPLEMENTAL SRM AND SRM 51-30-5. 2 L 7 2 4F A6WE 2001041800410 20010418 00410 WP 2001 4 18 ABXA010102 1 20010319 A 5312 591030391N1 CAP DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 948AX 56762 47065 NR 6 AFT PRESSURE BULKHEAD TEE CAP APPEARED TO BE CRACKED AT LONGERON 14L. MAINTENANCE INSPECTED AND REPLACED THE TEE S ECTION IAW ABX EA 53120037-004 AND EA 53120037-006. 2 L 7 2 4F A6WE 2001041800411 20010418 00411 SO 2001 4 18 C2XA01BT040 1 20010322 A 3350 7287580503 LIGHT EMB 145 EMB145LR SO CABIN INOPERATIVE A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 16981 145208 CREW REPORTED AFT ROW EMERGENCY LIGHT STRIP INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AFT ROW EMERGENCY LIGHT STRIP IAW EMB145 MM 33-50-08 OPS. CHECKED SYSTEM GOOD. 2 L 7 2 4T RT T00011AT 2001041800412 20010418 00412 WP 2001 4 18 01FDEA00231 1 20010325 A 3234 CONTROL HANDLE DOUG DC10 DC1010F 3022111 WP COCKPIT DIRTY A FDEA O OTHER N FALSE WARNING DE DESCENT 1 SO 25 051FE 47805 ON INITIAL GEAR EXT, NEITHER SET OF GEAR LIGHTS TURN GREEN, ALL LIGHT STAY RED. GEAR WAS RAISED AND RE-EXTENDED AND ALL LIGHTS IND NORMAL (GREEN). CLEANED MECHANISM ON GEAR HANDLE. OPS CK NORM PER MM 32-31-02. 2 L 7 3 4F A22WE 2001041800413 20010418 00413 WP 2001 4 18 DHL2001806509 1 20010308 A 3330 LIGHT DOUG DC8 DC8F54 3021926 WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK-FWD CARGO BAY LIGHT BASE CRACKED 1 INCH AT STA.100 LBL.17. REMOVED FASTENER IAW.SRM.51-1-21. FABRICATED DOUBLE R IAW SRM 53-2-0 FIG.2 CLEANED,TREATED & PRIMED IAW.SRM.51-1-88 INSTALLED DOUBLER & FASTENERS (NEW) IAW.SRM51-1-21 PAGE 21 STATUS CLOSED 2 L 7 4 4F 4A25 2001041800414 20010418 00414 WP 2001 4 18 DHL2001806510 1 20010320 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK: FWD.CARGO BAY. FLOOR SUPPORT ANGLE CRACKED 1 INCH AT STA.480 L-31 TO L-32 RT. PREFORMED STOP HOLE,FABRICATED DO UBLER AND INSTALLED IAW. SRM 53-02-0 FIG 1B. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800415 20010418 00415 WP 2001 4 18 DHL2001806511 1 20010309 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK-AFT-CARGO BAY FLOOR SUPPORT ANGLE CRACKED 1/4AT STA.1380 L-31RT TO L-32RT. PERFORMED STOP HOLE, FABRICATED DOUB LER AND INSTALLED IAW.SRM.53-2-0 FIG.1B STATUS CLOSED 2 L 7 4 4F RT 4A25 2001041800416 20010418 00416 2001 4 18 DHL2001362010 4 20010404 A 2210 B5FM1 COMPUTER AIRBUS 300 A300B4103 3930104 EU NR 1 MALFUNCTIONED A DHLA O OTHER O OTHER CR CRUISE 1 SO 01 362DH 84 AUTO PILOT NUMBER ONE WILL NOT ENGAGE IN MAN, OR CMD MODES. REPLACED NR 1 AP/FD LOGIC & MONITOR COMP WITH A SERV. UNIT. OPS CK IS GOOD IAW MM 22-13-34. COMPUTER P/N B5FM1, S/N OFF 213, S/N ON 433. STATUS-CLOSED. 2 L 7 2 4F RT A35EU 2001041800417 20010418 00417 2001 4 18 DHL2001363003 4 20010404 A 2200 B3BM2 COMPUTER AIRBUS 300 A300B4203 3930306 EU NR 1 MALFUNCTIONED A DHLA O OTHER O OTHER CR CRUISE 1 SO 01 363DH 085 AUTOPILOT NR 1 WILL NOT ALLOW CWS ROLL COMMAND IN CMD OR MAN MODE. SWAPPED A/P LONG COMPUTERS IAW MM 22-12-34 FOR TROUB LESHOOTING PURPOSES. OPS CHECKED NR 1 SYS IAW MM 22-11-00. NO DEFECTS NOTED. STATUS CLOSED. 2 L 7 2 4F RT A35EU 2001041800418 20010418 00418 WP 2001 4 18 DHL2001806523 1 20010309 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - FWD. CARGO COMPARTMENT - FLOOR SUPPORT ANGLE CRACKED 1 INCH AT STA 380 L-31R. REMOVED CRACKED ANGLE AT STA 3 80 L-31R IAW SRM 51-1-8 PAGE 21. FABRICATED ANGLE IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8, P AGE 12, 13. INSTALLED ANGLE IAW SRM 51-1-20D PAGE 9. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800419 20010418 00419 WP 2001 4 18 DHL2001806524 1 20010316 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - FWD CARGO COMPARTMENT - FLOOR SUPPORT ANGLE CRACKED 1/2 INCH AT STA 360.000 L-33R. PERFORMED STOP HOLE IAW SRM 53-2-0 FIG 1B. FABRICATED DOUBLER AND INSTALLED IAW SRM 53-2-0 FIG 1B. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800420 20010418 00420 WP 2001 4 18 DHL2001806525 1 20010308 A 5310 RIB DOUG DC8 DC873F 302199F WP TAIL CONE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - TAIL CONE LOWER INTERNAL PART RIB CRACKED 2 INCHES AT STA 1910.000. REMOVED RIVETS IAW SRM 51-1-21 PAGE 1. P ERFORMED STOP HOLE IAW SRM 53-3-0 FIG 1B. FABRICATED DOUBLER IAW SRM 53-2-0 FIG 1B. TREATED AND PRIMED IAW SRM 51-1-8B . INSTALLED DOUBLER IAW SRM 53-02-0 FIG 1B. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800421 20010418 00421 WP 2001 4 18 DHL2001806526 1 20010308 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - FWD CARGO COMPARTMENT FLOOR SUPPORT ANGLE AT STA 100.000 NEAR L-33R SHOWS CRACK OF 3 INCH. PERFORMED STOP HOL E IAW SRM 53-2-0 FIG 1B. FABRICATED DOUBLER IAW SRM 51-1-8C. INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1B. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800422 20010418 00422 WP 2001 4 18 DHL2001806527 1 20010309 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - FLIGHT COMPARTMENT 683 FLOOR PANEL SKIN CRACKED. PERFORMED STOP HOLE IAW SRM 53-2-3 FIG 10. FABRICATED DOUBL ER IAW SRM 53-2-3 FIG. 10. TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 53-2-3 FIG 10. STATUS-CLOSE D. 2 L 7 4 4F RT 4A25 2001041800423 20010418 00423 WP 2001 4 18 DHL2001806528 1 20010324 A 5753 SUPPORT DOUG DC8 DC873F 302199F WP TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - RH WING OUTBOARD FLAP. SUPPORT ARM PROTECTOR SHOWS 1 INCH CRACK AT STA XRS 230. REMOVED PROTECTOR FROM SUPP ORT ARM IAW SRM 51-1-21 PAGE 1. FABRICATED NEW PROTECTOR IAW SRM 53-2-0 FIG 2. TREATED AND PRIMED IAW SRM 51-1-8B. IN STALLED NEW PROTECTOR IAW SRM 51-1-21 PAGE 1. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041800424 20010418 00424 WP 2001 4 18 DHL2001806529 1 20010327 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - MAIN CARGO COMPARTMENT. FLOOR SUPPORT U ANGLE CRACKED 1 INCH BL 0 STA 1734-1760. REMOVED CRACKED U ANGLE IA W SRM 51-1-20 PAGE 21. FABRICATED ANGLE IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED, AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE IAW SRM 53-2-0 FIG 1B. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001041900002 20010419 00002 NM 2001 4 19 01FDEA00192 1 20010314 A 5315 65C26018 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 CORROSION ON 720A FLOORBEAM UPPER SURFACE OF UPPER FLANGE AT RBL 5 & 11. *S/D* REMOVED AND REPLACED PER SRM 51-10-1 FI G 4, 53-10-8 FIG 3 AND EA 7-5310-56300. 2 L 7 3 4F RT A3WE 2001041900003 20010419 00003 NM 2001 4 19 01FDEA00194 1 20010314 A 5320 SUPPORT BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 CEILING SUPPORT IS CRACKED FRAME HAS A DOUBLE HOLE AT BS 1130, WL 294. *S/D* REPAIRED PER FEDEX SRM 51-20-1, 51-40-3 F IG 1 AND EA 7-5310-56294. 2 L 7 3 4F RT A3WE 2001041900004 20010419 00004 NM 2001 4 19 SWAA010746 1 20010312 A 2131 7612688 CONTROLLER BOEING 737 7373H4 1384600 NM CABIN PRESSURE FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 324SW 23414 CLIMBING THROUGH FL350, AURAL WARNING INTERMITTENTLY SOUNDED AND CABIN PRESSURE BEGAN PASSING 10,000 FT. DESCENDED TO 1 0,000 FT AND DIVERTED TO TPA. MX FERRY TO DAL FOR REPAIRS. REPAIRED THE FOLLOWING DISCREPANCIES; NOSE RADOME HINGE CUT OUTS RESEALED, FWD ENTRY DOOR FWD & AFT LOWER CORNER SEALS REPAIRED, FWD CARGO DOOR SEAL REPAIRED, AFT CARGO DOOR SCUFF PLATES RESEALED, AFT ENTRY DOOR LOWER AFT CORNER & UPPER HINGE ARM RESEALED, LT OVERWING EMERGENCY EXIT READJUSTED, REMO VED AND REPLACED PRESSURE CONTROLLER (P/N 761268-8, S/N HG846) PER MM. 2 L 7 2 4F RT A16WE 2001041900005 20010419 00005 NM 2001 4 19 SWAA010724 1 20010309 A 3260 S138 SWITCH BOEING 737 7377H4 NM MLG W/W FAULTY A SWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 781WN 30601 DIVERSION, LANDING GEAR AURAL WARNING HORN SOUNDED INTERMITTENTLY DURING FLIGHT. ALL SYSTEMS FUNCTIONING NORMAL. REMOV ED AND REPLACED FLAP - LANDING GEAR WARNING SWITCH PER MM. RESET PSEU LATCHES AND RAN BITE CHECK WITH NO FAULTS. 2 L 7 2 4F RT A16WE 2001041900006 20010419 00006 NM 2001 4 19 SWAA010725 1 20010309 A 5310 6546575 SHEAR TIE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND VERTICAL STRAP CRACKED AT BS 1138, ABOVE STR 12R. REMOVED AND REPLACED VERTICAL STAP PE R SRM. 2 L 7 2 4F A16WE 2001041900007 20010419 00007 NM 2001 4 19 SWAA010785 1 20010316 A 3350 610478 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED SPECIAL VISIT, FOUND FWD ENTRY AND SVC DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY P ACK PER MM. 2 L 7 2 4F A16WE 2001041900008 20010419 00008 NM 2001 4 19 SWAA010786 1 20010316 A 5330 6545770 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACKED AT APPROX BS 645, STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001041900009 20010419 00009 NM 2001 4 19 SWAA010787 1 20010316 A 5320 6546804 STRINGER CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND 3 STR CLIPS CRACKED AT BS 727B, STR 8L & 9L, & BS 807, STR 5L. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F A16WE 2001041900010 20010419 00010 NM 2001 4 19 SWAA010788 1 20010316 A 5315 6546804 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED T BS 986, LBL 45. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F A16WE 2001041900011 20010419 00011 2001 4 19 SWAA010789 4 20010318 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 316SW 23338 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001041900012 20010419 00012 NM 2001 4 19 SWAA010790 1 20010316 A 5330 6545766 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 662SW 23255 DURING SCHEDULED SERVICE CHECK, FOUND 3.75 EXTERNAL FUSELAGE SKIN CRACK AT BS 500D, STR 12L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001041900013 20010419 00013 NM 2001 4 19 SWAA010791 1 20010316 A 5312 6516300 BULKHEAD BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 528SW 26570 DURING SCHEDULED SPECIAL VISIT, FOUND 3 BS 178 BULKHEAD WEB CRACKS AT WL 234, RBL 9.0 & WL 187, RBL 1.0 & LBL 1.0. REPA IRED BULKHEAD WEB PER SRM. 2 L 7 2 4F RT A16WE 2001041900014 20010419 00014 NM 2001 4 19 SWAA010792 1 20010316 A 5312 6517583 BULKHEAD BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 528SW 26570 DURING SCHEDULED SPECIAL VISIT, FOUND 1.0 FWD BULKHEAD VERTICAL BEAM WEB CRACK AT BS 180, RBL 17.1, WL 228. REPAIRED VE RTICAL BEAM WEB PER SWA RA. 2 L 7 2 4F RT A16WE 2001041900015 20010419 00015 NM 2001 4 19 SWAA010793 1 20010316 A 5513 183A8410 FITTING BOEING 737 7377H4 NM ELEVATOR TAB ELONGATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 725SW 27857 DURING SCHEDULED C4 CHECK, FOUND LT ELEVATOR TAB ATTACH FITTING MAST OUTBD INPUT ROD LUG BOLT HOLE ELONGATED. REMOVED A ND REPLACED ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2001041900016 20010419 00016 2001 4 19 SWAA010794 4 20010316 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22731 WHEN CLOSING AFT ENTRY DOOR, EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001041900017 20010419 00017 2001 4 19 SWAA010795 4 20010316 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 AFT ENTRY AND SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY''S PER MM. 2 L 7 2 4F A16WE 2001041900018 20010419 00018 NM 2001 4 19 SWAA010796 1 20010316 A 3397 079123 WIRE BOEING 737 7373H4 1384600 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 652SW 27722 EEPLS WIRING EXPOSED. INSTALLED EEPLS TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001041900019 20010419 00019 2001 4 19 SWAA010797 4 20010316 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 520SW 25319 FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001041900020 20010419 00020 NM 2001 4 19 SWAA010798 1 20010316 A 5320 6567740 FITTING BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND BS 663 FORGED FITTING CRACKED AT STR 3L & STR 3R. REPAIRED FORGED FITTING PER SRM. 2 L 7 2 4F A16WE 2001041900021 20010419 00021 NM 2001 4 19 SWAA010799 1 20010317 A 7711 D4582J CONNECTOR BOEING 737 7372H4 138448C NM NR 1 ENGINE LOOSE A SWAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 07 060SW 21812 ABORTED TAKEOFF, EPR INDICATORS FAILED ON NR 1 & 2 ENGINES DURING ROLLOUT. FOUND NR 1 ENG EPR TRANSMITTER CONNECTOR LOO SE. SECURED CONNECTOR PER MM. 2 L 7 2 4F A16WE 2001041900022 20010419 00022 NM 2001 4 19 SWAA010800 1 20010317 A 2910 R115551 HYDRAULIC LINE BOEING 737 7372H4 138448C NM NR 2 ENGINE LEAKING A SWAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 074SW 22674 NR 2 ENG A HYDRAULIC PUMP LOW PRESS LIGHT ILLUMINATED DURING FLIGHT. REMOVED AND REPLACED NR 2 ENG FLEX HOSE FROM ENG D RIVEN PUMP TO QUICK DISCONNECT. REMOVED AND REPLACED CASE DRAIN FILTER, NO CONTAMINATION NOTED PER MM. 2 L 7 2 4F A16WE 2001041900023 20010419 00023 2001 4 19 SWAA010771 4 20010314 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED RON CHECK, AFT ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED EVAC S LIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001041900024 20010419 00024 2001 4 19 SWAA010772 4 20010315 A 2565 61620468 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF TOLERANCE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 643SW 27716 FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001041900025 20010419 00025 NM 2001 4 19 SWAA010773 1 20010314 A 2560 65C16820 RETAINER BOEING 737 7372H4 138448C NM ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 063SW 22061 DURING SCHEDULED C3 CHECK, FOUND FWD AND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINERS LOOSE. SECURED RETAINER S PER MM. 2 L 7 2 4F A16WE 2001041900026 20010419 00026 NM 2001 4 19 SWAA010774 1 20010314 A 2560 6557463 BRACKET BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 063SW 22061 DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET LOOSE. SECURED BRACKET PER MM. 2 L 7 2 4F A16WE 2001041900027 20010419 00027 NM 2001 4 19 SWAA010775 1 20010315 A 5311 6516301 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17L & STR 17R. REPAIRED FRAMES PER SRM. 2 L 7 2 4F A16WE 2001041900028 20010419 00028 NM 2001 4 19 SWAA010776 1 20010315 A 5311 BAC1490 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CHORD CORRODED AT BS 270, LBL 11 TO RBL 11, WL 208. REPAIRED FRAME CHORD PER SRM. 2 L 7 2 4F A16WE 2001041900029 20010419 00029 NM 2001 4 19 SWAA010777 1 20010315 A 5320 65C27314 STRINGER CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND STR CLIPS CRACKED AT BS 727B, STR 6L & BS 747 STR 7R. REMOVED AND REPLACED STR CLIPS PE R SRM. 2 L 7 2 4F A16WE 2001041900030 20010419 00030 NM 2001 4 19 SWAA010778 1 20010314 A 5754 65C26686 SKIN BOEING 737 7373H4 1384600 NM L/E SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED C4 CHECK, FOUND NR 1 L/E SLAT LOWER SKIN CRACKED AT 2 FASTENER HOLES, AFT ROW, OUTBD MAIN TRACK. REPAI RED SLAT SKIN. 2 L 7 2 4F RT A16WE 2001041900031 20010419 00031 NM 2001 4 19 SWAA010779 1 20010314 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED CHECK, FOUND 3.25 EXTERNAL FUSELAGE SKIN CRACK AT BS 787, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001041900032 20010419 00032 NM 2001 4 19 SWAA010780 1 20010314 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED C4 CHECK, FOUND 5 EXTERNAL FUSELAGE SKIN CRACK AT BS 500, STR 10L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001041900033 20010419 00033 NM 2001 4 19 SWAA010781 1 20010314 A 5330 65C35786 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED C4 CHECK, FOUND 2 EXTERNAL FUSELAGE SKIN CRACKS AT BS 500B, STR 10R, 1 IN LENGTH & BS 500C, STR 10R, 3 IN LENGTH. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001041900034 20010419 00034 NM 2001 4 19 SWAA010782 1 20010314 A 5330 6545773 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED C4 CHECK, FOUND 2.5 EXTERNAL FUSELAGE SKIN CRACK AT BS 727B, STR 10L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001041900035 20010419 00035 NM 2001 4 19 SWAA010783 1 20010314 A 5330 6545769 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED C4 CHECK, FOUND 6 EXTERNAL FUSELAGE SKIN CRACK AT BS 420, STR 26L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001041900036 20010419 00036 NM 2001 4 19 SWAA010784 1 20010314 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED C4 CHECK, FOUND 1.25 EXTERNAL FUSELAGE SKIN CRACK AT BS 927, STR 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001041900037 20010419 00037 NM 2001 4 19 SWAA010763 1 20010314 A 5312 6517582 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD LT VERTICAL BEAM WEB CRACKED AT AT WL 228, EXITING BLANKET ATTACH HOLE. REPAIRED VERTICAL BEAM WEB PER BFG ER. 2 L 7 2 4F A16WE 2001041900038 20010419 00038 NM 2001 4 19 SWAA010764 1 20010314 A 5312 6516300 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED SPECIAL VISIT, FOUND .75 INCH BS 178 BULKHEAD WEB CRACK AT WL 182, LT SIDE. REPAIRED BULKHEAD WEB PER BFG ER. 2 L 7 2 4F A16WE 2001041900039 20010419 00039 NM 2001 4 19 SWAA010765 1 20010314 A 5312 6516300 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT RBL 10 TO RBL 10.5, WL 208. REPAIRED BULKHEAD WEB PER SR M. 2 L 7 2 4F A16WE 2001041900040 20010419 00040 NM 2001 4 19 SWAA010766 1 20010314 A 5311 6546546 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 794.3, AFT CARGO DOOR NR 1 LOWER STOP. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2001041900041 20010419 00041 NM 2001 4 19 SWAA010767 1 20010314 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND STR 4L CRACKED AT BS 695. REPAIRED STR PER SRM. 2 L 7 2 4F A16WE 2001041900042 20010419 00042 NM 2001 4 19 SWAA010768 1 20010314 A 3350 65C34691 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED C4 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2001041900043 20010419 00043 NM 2001 4 19 SWAA010769 1 20010314 A 5330 6545778 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED C4 CHECK, FOUND 4 INCH EXTERNAL FUSELAGE SKIN CRACK AT BS 927, STR 21R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001041900044 20010419 00044 NM 2001 4 19 SWAA010770 1 20010314 A 5310 573149 WINDOW POST BOEING 737 7373H4 1384600 NM COCKPIT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED 1/4D CHECK, FOUND WINDOW POST CRACKED AT LT SIDE, BETWEEN CAPT''S NR 1 & NR 2 WINDOWS. REPAIRED WINDOW POST PER SRM. 2 L 7 2 4F RT A16WE 2001041900045 20010419 00045 2001 4 19 SWAA010801 4 20010316 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 616SW 27699 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. RE-INSTALLED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001041900046 20010419 00046 NM 2001 4 19 SWAA010802 1 20010318 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 632SW 27707 EEPLS TRACK COVER LOOSE AT OVERWING EXIT. SECURED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001041900047 20010419 00047 NM 2001 4 19 SWAA010803 1 20010317 A 5754 65C26686 WEDGE BOEING 737 7372H4 138448C NM L/E SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SERVICE CHECK, FOUND NR 3 L/E SLAT CRACKED AT T/E WEDGE, 66 OUTBD FROM INBD END. REMOVED AND REPLACED NR 3 SLAT PER MM. 2 L 7 2 4F A16WE 2001041900048 20010419 00048 NM 2001 4 19 SWAA010804 1 20010318 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED A2 CHECK, FOUND 3 EXTERNAL FUSELAGE SKIN CRACK AT BS 483, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001041900049 20010419 00049 NM 2001 4 19 SWAA010805 1 20010318 A 3350 300432 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 329SW 23693 DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL EGRESS LIGHT INOP AT AFT SVC DOOR. RELAMPED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001041900050 20010419 00050 NM 2001 4 19 SWAA010806 1 20010318 A 5753 6546434 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 614SW 28033 DURING SCHEDULED C2 CHECK, FOUND RT WING INBD AFT T/E FLAP DISBONDED AT RT LOWER SIDE. REMOVED AND REPLACED AFT FLAP PE R MM. 2 L 7 2 4F RT A16WE 2001041900051 20010419 00051 NM 2001 4 19 SWAA010807 1 20010318 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 338SW 23960 EMERGENCY FLASHLIGHT INOP IN AFT CABIN. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001041900052 20010419 00052 NM 2001 4 19 SWAA010808 1 20010319 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND STR 27L CORRODED AT BS 947. REPAIRED STR PER SRM. 2 L 7 2 4F A16WE 2001041900053 20010419 00053 NM 2001 4 19 SWAA010809 1 20010319 A 5320 65C27314 STRINGER CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND STR 19L CLIP CRACKED AT BS 520. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F A16WE 2001041900054 20010419 00054 NM 2001 4 19 SWAA010810 1 20010319 A 5311 6558280 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND BS 360 FUSELAGE FRAME CRACKED BETWEEN STR 19R & 20R. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2001041900055 20010419 00055 NM 2001 4 19 SWAA010811 1 20010319 A 5320 65C27314 STRINGER CLIP BOEING 737 7372H4 138448C NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND 6 STR CLIPS CRACKED AT BS 727A, STR 7L, BS 747, STR 6L & 7L, BS 767, STR 7L, BS 787, STR 10R, & BS 807, STR 7L. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F A16WE 2001041900056 20010419 00056 NM 2001 4 19 SWAA010812 1 20010319 A 5752 6546455 TAB BOEING 737 7373H4 1384600 NM LT AILERON DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED 1/4D CHECK, FOUND LT AILERON TAB DELAMINATED AROUND HINGE POINTS. REMOVED AND REPLACED AILERON TAB PER MM. 2 L 7 2 4F RT A16WE 2001041900057 20010419 00057 NM 2001 4 19 SWAA010813 1 20010319 A 5310 6545409 PRESSURE PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 664, LBL 31. REPAIRED BEADED PRESSURE WEB PER TI-3 53-046. 2 L 7 2 4F RT A16WE 2001041900058 20010419 00058 NM 2001 4 19 SWAA010815 1 20010318 A 5320 BAC1503 STIFFENER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 683SW 24008 DURING SCHEDULED SERVICE CHECK, FOUND BS 663 BULKHEAD VERTICAL STIFFENERS CRACKED AT RBL 6.15 & LBL 6.15. REPAIRED STIF FENERS PER SWA RA. 2 L 7 2 4F RT A16WE 2001041900059 20010419 00059 NM 2001 4 19 SWAA010816 1 20010318 A 5512 65C25727 SKIN BOEING 737 7373Q8 1384670 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED C2 CHECK, FOUND 2.5 INCH LONG CRACK AT RT HORIZ STAB SKIN, BS 147.90, REAR SPAR. REPAIRED SKIN PER SRM . 2 L 7 2 4F RT A16WE 2001041900060 20010419 00060 NM 2001 4 19 SWAA010817 1 20010319 A 5330 65C27257 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AND DOUBLER CRACKED AT FWD ENTRY DOOR LOWER AFT CUTOUT CORNER. REPAIRED SKIN AND DOUBLER PER SWA RA. 2 L 7 2 4F RT A16WE 2001041900061 20010419 00061 NM 2001 4 19 SWAA010818 1 20010319 A 5320 BAC1514 STIFFENER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND BS 1016 BULKHEAD RADIAL STIFFENER ZEE ANGLE CRACKED AT STR 9L, LBL 5. REPAIRED STIFFENE R ZEE ANGLE PER SRM. 2 L 7 2 4F A16WE 2001041900062 20010419 00062 NM 2001 4 19 SWAA010819 1 20010317 A 7711 W002 CONNECTOR BOEING 737 7372H4 138448C NM EPR INDICATOR LOOSE A SWAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 07 082SW 22731 ABORTED TAKEOFF AT 40 KNOTS, NR 2 ENG EPR INDICATOR INOP. CLEANED CONNECTOR AT EPR INDICATOR PER MM. OPS CHECK GOOD. 2 L 7 2 4F A16WE 2001041900063 20010419 00063 NM 2001 4 19 SWAA010820 1 20010320 A 2560 P4010021 BATTERY BOEING 737 7372H4 138448C NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 060SW 21812 FWD INBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2001041900064 20010419 00064 2001 4 19 SWAA010821 4 20010320 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM NETRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 AFT ENTRY AND SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY''S PER MM. 2 L 7 2 4F A16WE 2001041900065 20010419 00065 2001 4 19 SWAA010822 4 20010317 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 AFT SVC DOOR EMERGENCY EVAC SLIDE ASSY OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001041900066 20010419 00066 NM 2001 4 19 SWAA010823 1 20010320 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 394SW 27380 EEPLS TRACK COVERS MISSING AT ROWS 14 & 15. INSTALLED TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 2001041900067 20010419 00067 NM 2001 4 19 SWAA010824 1 20010320 A 5312 6517583 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT LBL 17.1, WL 234. REMOVED AND REPLACED VER TICAL BEAM WEB PER BFG ER. 2 L 7 2 4F A16WE 2001041900068 20010419 00068 NM 2001 4 19 SWAA010825 1 20010320 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND STR 27L CORRODED AT BS 967. REPAIRED STR PER SRM. 2 L 7 2 4F A16WE 2001041900069 20010419 00069 NM 2001 4 19 SWAA010826 1 20010320 A 5320 65C27314 STRINGER CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND 4 STR CLIPS CRACKED AT BS 807, STR 5L & 13R, BS 727B, STR 7R & BS 847, STR 4R. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F A16WE 2001041900070 20010419 00070 NM 2001 4 19 SWAA010827 1 20010320 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 942, STR 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001041900071 20010419 00071 NM 2001 4 19 SWAA010828 1 20010320 A 5753 6546434 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 649SW 27719 DURING SCHEDULED C3 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED ON UPPER SKIN. REMOVED AND REPLACED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2001041900072 20010419 00072 2001 4 19 SWAA010829 4 20010319 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 649SW 27719 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE AS SY PER MM. 2 L 7 2 4F RT A16WE 2001041900073 20010419 00073 NM 2001 4 19 SWAA010830 1 20010320 A 3350 207377 LENS BOEING 737 7377H4 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 709SW 27843 DURING SCHEDULED A1 CHECK, FOUND EEPLS LENS MISSING AT FWD ENTRY. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2001041900074 20010419 00074 NM 2001 4 19 SWAA010831 1 20010320 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 385SW 26600 EEPLS TRACK COVER MISSING AT ROW 11. INSTALLED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001041900075 20010419 00075 NM 2001 4 19 SWAA010832 1 20010319 A 5310 6545819139 PRESSURE PANEL BOEING 737 7373H4 1384600 NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED 1/4D CHECK, FOUND NLG W/W BOX VERTICAL WEB CRACKED AT BS 233, BL 0. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001041900076 20010419 00076 NM 2001 4 19 SWAA010833 1 20010320 A 5330 6545773 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND FUSELAGE WINDOW BELT SKIN CRACKED AT WINDOW 10L, FWD UPPER CORNER. REPAIRED SKIN PER SR M. 2 L 7 2 4F A16WE 2001041900077 20010419 00077 NM 2001 4 19 SWAA010834 1 20010320 A 5330 6545773 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND FUSELAGE WINDOW BELT SKIN CRACKS AT WINDOWS 24L, 25L, 26L, 27L, 28L & 29L, FWD LOWER COR NERS. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001041900078 20010419 00078 NM 2001 4 19 SWAA010835 1 20010319 A 5330 6545773 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND FUSELAGE WINDOW BELT SKIN CRACKS AT WINDOWS 24L, 25L, 28L & 29L, AFT UPPER CORNERS. REP AIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001041900079 20010419 00079 NM 2001 4 19 SWAA010836 1 20010320 A 5330 6545773 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND FUSELAGE WINDOW BELT SKIN CRACKS AT WINDOWS 6R AND 11R, AFT LOWER CORNERS. REPAIRED SKI N PER SRM. 2 L 7 2 4F A16WE 2001041900080 20010419 00080 NM 2001 4 19 SWAA010837 1 20010321 A 5330 65C35775 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 091SW 22963 DURING WALKAROUND INSPECTION, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 727C+10, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001041900081 20010419 00081 2001 4 19 SWAA010838 4 20010321 A 2565 D31354 SLIDE BOEING 737 7377H4 NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 708SW 27842 FWD SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001041900082 20010419 00082 NM 2001 4 19 SWAA010839 1 20010321 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 713SW 27847 EEPLS TRACK COVER LOOSE AT ROW 1. SECURED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001041900083 20010419 00083 NM 2001 4 19 SWAA010840 1 20010320 A 5320 6551698 SPLICE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND STR 4L SPLICE CRACKED AT BS 908. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F A16WE 2001041900084 20010419 00084 NM 2001 4 19 SWAA010841 1 20010320 A 5330 6545766 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND FUSELAGE WINDOW BELT SKIN CRACKS AT WINDOWS 3L, 8L & 11L, FWD UPPER CORNERS. REPAIRED S KIN PER SRM. 2 L 7 2 4F A16WE 2001041900085 20010419 00085 NM 2001 4 19 SWAA010842 1 20010320 A 5330 6545766 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND FUSELAGE WINDOW BELT SKIN CRACKED AT WINDOW 10L, AFT LOWER CORNER. REPAIRED SKIN PER SR M. 2 L 7 2 4F A16WE 2001041900086 20010419 00086 NM 2001 4 19 SWAA010843 1 20010320 A 5330 6545766 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND FUSELAGE WINDOW BELT SKIN CRACKED AT WINDOW 9R, UPPER FWD CORNER. REPAIRED SKIN PER SRM . 2 L 7 2 4F A16WE 2001041900087 20010419 00087 NM 2001 4 19 SWAA010844 1 20010320 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVER LOOSE AT AFT GALLEY. SECURED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001041900088 20010419 00088 NM 2001 4 19 SWAA010845 1 20010321 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED C3 CHECK, FOUND 1.5 EXTERNAL FUSELAGE SKIN CRACK AT BS 460, STR 4R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001041900089 20010419 00089 NM 2001 4 19 SWAA010846 1 20010321 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED C3 CHECK, FOUND 3 EXTERNAL FUSELAGE SKIN CRACKS AT BS 500A, STR 10R, 2 LONG, BS 480, STR 10L, 3 LONG & BS 380, STR 10L, 1.75 LONG. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001041900090 20010419 00090 NM 2001 4 19 SWAA010847 1 20010320 A 3350 57771 CAP BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED C3 CHECK, FOUND EEPLS FWD END CAP MISSING. INSTALLED END CAP PER MM. 2 L 7 2 4F RT A16WE 2001041900091 20010419 00091 NM 2001 4 19 SWAA010848 1 20010320 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED C3 CHECK, FOUND 3 EXTERNAL FUSELAGE SKIN CRACK AT BS 480, STR 4L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001041900092 20010419 00092 NM 2001 4 19 SWAA010849 1 20010320 A 5512 65C25727 SKIN BOEING 737 7373H4 1384600 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED C3 CHECK, FOUND .75 INCH LONG RT HORIZ STAB LOWER SKIN CRACK AT AFT SPAR, 64 OUTBOARD OF FUSELAGE. REP AIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001041900093 20010419 00093 NM 2001 4 19 SWAA010850 1 20010320 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED C3 CHECK, FOUND 3 EXTERNAL FUSELAGE SKIN CRACKS AT STR 20L, BS 747, 1.5 LONG, BS 787+5, 2.25 LONG & BS 787+13, 2.5 LONG. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001041900094 20010419 00094 NM 2001 4 19 SWAA010851 1 20010321 A 5754 65C26686 WEDGE BOEING 737 7373H4 1384600 NM L/E SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 312SW 23334 DURING SCHEDULED C4 CHECK, FOUND LT WING NR 3 L/E SLAT T/E WEDGE DISBONDED, 75 PERCENT OF PANEL. REMOVED AND REPLACED N R 3 SLAT PER MM. 2 L 7 2 4F RT A16WE 2001041900095 20010419 00095 NM 2001 4 19 SWAA010852 1 20010321 A 5753 6546486 PANEL BOEING 737 7375H4 138449D NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 509SW 24186 DURING SCHEDULED C2 CHECK, FOUND RT WING INBOARD T/E FLAP WEDGE PANEL DELAMINATED. REMOVED AND REPLACED WEDGE PANEL PER MM. 2 L 7 2 4F RT A16WE 2001041900096 20010419 00096 NM 2001 4 19 SWAA010853 1 20010321 A 5315 6546804 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 513SW 24190 DURING SCHEDULED D-CHECK AT DALFORT, FOUND FLOORBEAM CORRODED AT BS 980, FROM RBL 22 TO OUTBOARD END. REPAIRED FLOORBEA M PER SRM. 2 L 7 2 4F RT A16WE 2001041900097 20010419 00097 NM 2001 4 19 SWAA010854 1 20010321 A 5311 BAC1505 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 528SW 26570 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD VERTICAL CHORD CRACKED AT LBL 5.7, WL 184.5. REPAIRED CHORD PER S RM. 2 L 7 2 4F RT A16WE 2001041900098 20010419 00098 NM 2001 4 19 SWAA010855 1 20010321 A 5315 6545410 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED 1/4D CHECK, FOUND BS 663 CENTER WING BOX LONGITUDINAL FLOORBEAM TEE CHORD CRACKED AT BL 0.7. REPAIRED FLOORBEAM TEE CHORD PER SWA RA. 2 L 7 2 4F RT A16WE 2001041900099 20010419 00099 NM 2001 4 19 SWAA010856 1 20010321 A 5523 83A8400 FITTING BOEING 737 7377H4 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 710SW 27844 DURING SCHEDULED SERVICE CHECK, FOUND LT ELEVATOR TAB NR 1 HINGE BUSHINGS AND FITTING WORN. REMOVED AND REPLACED NR 1 H INGE BOLT, BUSHINGS (P/N 183A8410) AND FITTING PER MM. 2 L 7 2 4F RT A16WE 2001041900100 20010419 00100 2001 4 19 SWAA010857 4 20010321 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 601WN 27695 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001041900101 20010419 00101 NM 2001 4 19 SWAA010858 1 20010322 A 3350 079123 COVER BOEING 737 7375H4 138449D NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 EEPLS TRACK COVER CRACKED AT ROW 3. REMOVED AND REPLACED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001041900102 20010419 00102 NM 2001 4 19 SWAA010859 1 20010321 A 5320 BAC1490 ATTACH ANGLE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD SKIN ATTACH ANGLE CRACKED AT WL 218, RT SIDE. REMOVED AND REPLACED ATTA CH ANGLE PER SRM. 2 L 7 2 4F A16WE 2001041900103 20010419 00103 NM 2001 4 19 SWAA010860 1 20010322 A 5312 6546576 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT STR 15L SPLICE. REPAIRED BULKHEAD WEB PER SRM. 2 L 7 2 4F A16WE 2001041900104 20010419 00104 NM 2001 4 19 SWAA010861 1 20010322 A 5330 6545766 SKIN BOEING 737 7372H4 138448C NM FUSLEAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND FUSELAGE WINDOW BELT SKIN CRACKS AT WINDOWS 5L, 7L & 9L, FWD UPPER CORNERS. REPAIRED SK IN PER SRM. 2 L 7 2 4F A16WE 2001041900105 20010419 00105 NM 2001 4 19 SWAA010862 1 20010322 A 5330 6545766 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND FUSELAGE WINDOW BELT SKIN CRACKED AT WINDOW 8L, AFT LOWER CORNER. REPAIRED SKIN PER SRM . 2 L 7 2 4F A16WE 2001041900106 20010419 00106 NM 2001 4 19 SWAA010863 1 20010322 A 5330 6545766 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND FUSELAGE WINDOW BELT SKIN CRACKS AT WINDOWS 8R & 12R, FWD UPPER CORNERS. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001041900107 20010419 00107 NM 2001 4 19 SWAA010864 1 20010322 A 5330 65C35775 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001041900108 20010419 00108 NM 2001 4 19 SWAA010865 1 20010322 A 2560 6557463 BRACKET BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT FLOOR BRACKET LOOSE. SECURED BRACKET PE R MM. 2 L 7 2 4F RT A16WE 2001041900109 20010419 00109 NM 2001 4 19 SWAA010866 1 20010322 A 3350 100031 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED C3 CHECK, FOUND AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2001041900110 20010419 00110 NM 2001 4 19 SWAA010867 1 20010321 A 5330 6545775 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 DURING SCHEDULED C2 CHECK, FOUND 3 INCH LONG EXTERNAL FUSELAGE SKIN CRACK AT BS 767, STR 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001041900111 20010419 00111 NM 2001 4 19 SWAA010868 1 20010321 A 5330 65C35775 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 DURING SCHEDULED C2 CHECK, FOUND 1.5 INCH LONG EXTERNAL FUSELAGE SKIN CRACK AT BS 760, STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001041900112 20010419 00112 NM 2001 4 19 SWAA010869 1 20010321 A 5754 65C266021 SKIN BOEING 737 7373Q8 1384670 NM L/E SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED C2 CHECK, FOUND NR 2 L/E SLAT SKIN DISBONDED. REMOVED AND REPLACED NR 2 SLAT PER MM. 2 L 7 2 4F RT A16WE 2001041900113 20010419 00113 NM 2001 4 19 SWAA010870 1 20010321 A 3350 BR2013 LIGHT BOEING 737 7373T5 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED C1 CHECK, FOUND EEPLS INOP AND END CAP MISSING AT AFT GALLEY. RELAMPED AND INSTALLED END CAP PER MM. 2 L 7 2 4F RT A16WE 2001041900114 20010419 00114 NM 2001 4 19 SWAA010871 1 20010321 A 5755 HINGE BOEING 737 7373T5 NM L/E SLAT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 9715V 23061 DURING SCHEDULED C1 CHECK, FOUND INBOARD GROUND SPOILER OUTBOARD HINGE BROKEN IN TWO PIECES AND INBOARD HINGE BEARING WO RN. REMOVED AND REPLACED GROUND SPOILER PER MM. 2 L 7 2 4F RT A16WE 2001041900115 20010419 00115 NM 2001 4 19 SWAA010872 1 20010321 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED C3 CHECK, FOUND 3.25 INCH LONG EXTERNAL FUSELAGE SKIN CRACK AT BS 727D, STR 19R. REPAIRED SKIN PER SRM . 2 L 7 2 4F RT A16WE 2001041900116 20010419 00116 NM 2001 4 19 SWAA010873 1 20010322 A 2560 A170033 STRAP BOEING 737 7372H4 138448C NM FLASHLIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 AFT CABIN EMERGENCY FLASHLIGHT STRAP MISSING. INSTALLED STRAP PER MM. 2 L 7 2 4F A16WE 2001041900117 20010419 00117 2001 4 19 SWAA010874 4 20010322 A 2565 D31354 SLIDE BOEING 737 7377H4 NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 720WN 27854 AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001041900118 20010419 00118 NM 2001 4 19 SWAA010875 1 20010322 A 5523 DAS414A1 BEARING BOEING 737 7377H4 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 717SA 27851 DURING SCHEDULED SERVICE CHECK (SWA SI 11038-55), FOUND NR 1, 2 & 4 RT ELEVATOR TAB BEARINGS WORN. REMOVED AND REPLACED BEARINGS PER D&M ENTERPRISES WORK ORDER SSR:011. 2 L 7 2 4F RT A16WE 2001041900119 20010419 00119 NM 2001 4 19 SWAA010876 1 20010322 A 5523 DAS414A1 BEARING BOEING 737 7377H4 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 717SA 27851 DURING SCHEDULED SERVICE CHECK (SWA SI 11038-55), FOUND NR 2 & 4 LT ELEVATOR TAB BEARINGS WORN. REMOVED AND REPLACED BE ARINGS PER D&M ENTERPRISES WORK ORDER SSR:011. 2 L 7 2 4F RT A16WE 2001041900120 20010419 00120 NM 2001 4 19 DHL2001703002 1 20010323 A 2930 INDICATOR BOEING 727 72730C 1384009 NM COCKPIT INOPERATIVE A DHLA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 703DH 19010 A-SYSTEM HYDRAULIC QUANTITY INDICATOR INOP. PLACED ON DEFERRAL PER DMI 4858. MEL REF 29-14 CAT C. 2 L 7 3 4F A3WE 2001041900121 20010419 00121 NM 2001 4 19 VNAA0103008 1 20010307 A 3250 2304000001 CONTROL UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NLG STEERING LEAKING A VNAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 07 429JS 7292 3043 DURING APPROACH UPON SELECTING GEAR DOWN THE FLIGHT CREW RECEIVED A NOSE WHEEL STEERING AND NOSE WHEEL POWER UP FAIL MES SAGE. THE FLIGHT CREW ADVISED THE TOWER THAT A MISSED APPROACH WAS REQUIRED TO COMPLETE THE CHECKLIST. THE FLIGHT CREW THEN RE-ENTERED THE APPROACH AND THE TOWER HAD EMERGENCY VEHICLES RESPOND. THE LANDING WAS MADE WITHOUT INCIDENT. MAI NTENANCE INSPECTED AND REPLACED THE HYDRAULIC STEERING CONTROL MANIFOLD IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32 -50-00. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001041900122 20010419 00122 NM 2001 4 19 VNAA0103009 1 20010308 A 3350 321473 POWER SUPPLY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST NR NOT REPORTED 1 GL 07 461PS 577 3075 THE FLIGHT CREW REPORTED THAT THE FORWARD SECTION OF THE EMERGENCY FLOOR LIGHTING WOULD NOT OPERATE. MAINTENANCE INSPEC TED AND REPLACED THE 4LK POWER SUPPLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-00. OPERATIONAL CHECKS WERE C OMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001041900123 20010419 00123 NM 2001 4 19 VNAA0103010 1 20010310 A 3250 2342500000 HARNESS DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NLG STEERING DEFECTIVE A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 434JS 14809 3051 AFTER TAKING THE RUNWAY FLIGHT 4168 RECEIVED A PROXIMITY SYSTEM FAIL WARNING MESSAGE. THE FLIGHT CREW THEN CLEARED THE RUNWAY. MAINTENANCE INSPECTED THE AIRCRAFT AND FERRIED THE AIRCRAFT TO CAK FOR REPAIRS. UPON APPROACH TO CAK FLIGHT 94 23 RECEIVED A NOSE WHEEL STEERING WARNING MESSAGE UPON LOWERING THE LANDING GEAR. THE FLIGHT CREW PERFORMED A MISSED AP PROACH TO COMPLETE THE CHECKLIST AND THE CAPTAIN DECLARED AN EMERGENCY. THE AIRCRAFT LANDED AND WAS SHUTDOWN ON THE RUN WAY AND WAS TOWED. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR ELECTRICAL HARNESS IN ACCORDANCE WITH DORNIER MAINT ENANCE MANUAL 32-20-00. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001041900125 20010419 00125 NM 2001 4 19 VNAA0103013 1 20010315 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST NR NOT REPORTED 1 GL 07 457PS 10634 95 3048 CREW REPORTED EMERGENCY LIGHTS BETWEEN ROWS 3 AND 5 WERE NOT WORKING. MAINTENANCE REPLACED EMERGENCY BATTERY AT 5LK IN ACCORDANCE WITH MAINTENANCE MANUAL 33-50-00. THE LIGHTS CHECKED GOOD. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001041900126 20010419 00126 NM 2001 4 19 VNAA0103012 1 20010314 A 5270 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT ACTIVATED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 436JS 3052 AS THE AIRCRAFT WAS TAXIING ONTO THE RUNWAY, THE FLIGHT RECEIVED A PROXI DOOR FAIL WARNING MESSAGE FOR THE MAIN CABIN DO OR. THE FLIGHT CREW EXITED THE RUNWAY AND RETURNED TO THE GATE. THE FLIGHT CREW CYCLED THE MAIN CABIN DOOR PROXI SENSO R CIRCUIT BREAKERS AND THE MESSAGE CLEARED. THE AIRCRAFT WAS REBOARDED AND DEPARTED WITHOUT ANY FURTHER PROBLEMS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001041900127 20010419 00127 2001 4 19 VNAA0103011 4 20010312 A 3418 84321 STICK SHAKER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FAILED A VNAA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 GL 07 459PS 12793 3070 AFTER THE FLIGHT CREW PERFORMED THE STALL STICK PUSHER TEST THE ELEVATOR CONTROL WOULD NOT MOVE PAST NEUTRAL FROM THE N OSE DOWN POSITION. MAINTENANCE INSPECTED AND FOUND THE STICK PUSHER ENGAGED. MAINTENANCE DISCONNECTED AND SECURED THE STICK PUSHER UNIT FOR THE PURPOSE OF A FERRY FLIGHT. AN UNEVENTFUL FERRY FLIGHT WAS COMPLETED TO PIT WHERE MAINTENANCE REPLACED THE STICK PUSHER UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-33-03. OPERATIONAL CHECKS WERE COMPLET ED AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001041900128 20010419 00128 NM 2001 4 19 QXEA0100401 1 20010314 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-RIGHT OUTBOARD FORWARD SEAT TRACK REQUIRES REPLACEMENT DUE TO CORROSION REMOVAL BLENDING BEYOND LIMITS. REPAIRED IA W DHC-8 SRM 51-40-11 AND RD-8-53-1102. 2 H 7 2 4T RT A13NM 2001041900129 20010419 00129 NM 2001 4 19 QXEA0100402 1 20010314 A 5620 WINDOW FRAME DHAV DHC8 DHC8102 2809003 NM CABIN CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-CHAFING AT LOWER APERTURE OF LEFT HAND MAIN CABIN WINDOW AT STATION 501. REPAIRED IAW DHC-8 RD-8-53-655 AND SRM 51- 20-11, PAGE 3. 2 H 7 2 4T RT A13NM 2001041900130 20010419 00130 NM 2001 4 19 QXEA0100404 1 20010317 A 5510 VORTEX GEN DHAV DHC8 DHC8102 2809003 NM HORIZ STAB UNAPPROVED PART A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-INBOARD VORTEX GENERATOR ON RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN IS NOT APPROVED PART FOR THIS AIRCRAFT. REP AIRED IAW HORIZON AIR EA 9-55-144. 2 H 7 2 4T RT A13NM 2001041900131 20010419 00131 NM 2001 4 19 QXEA0100405 1 20010312 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-DENT PROTRUDING IN LOWER EMPENNAGE SKIN LEFT OF TAIL SKID BUMPER, 12 INCHES FORWARD OF COMPOSITE TAIL CONE. REPAIRE D IAW DHC-8 SRM 53-30-24, PAGE 1. 2 H 7 2 4T RT A13NM 2001041900132 20010419 00132 NM 2001 4 19 QXEA0100407 1 20010312 A 3233 ACTUATOR DHAV DHC8 DHC8102 2809003 NM LT MLG CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-LEFT HAND LANDING GEAR RETRACTION ACTUATOR FRETTING MOUNTING PADS HAVE PITTING. REPAIRED IAW HORIZON AIR EA 9-54-27 9, SRM 32-30-11, PAGE 202 AND SRM 51-20-16, PAGE 4. 2 H 7 2 4T RT A13NM 2001041900133 20010419 00133 NM 2001 4 19 QXEA0100408 1 20010318 A 5414 SKIN DHAV DHC8 DHC8102 2809003 NM NACELLE TORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-LEFT HAND NACELLE OUTBOARD LOWER CORNER S/M TORN WHERE MAIN LANDING GEAR FORWARD HINGE ATTACH POINT. REPAIRED IAW D HC-8 RD-8-54-729. 2 H 7 2 4T RT A13NM 2001041900135 20010419 00135 EU 2001 4 19 AALA20010297 1 20010212 A 2520 RDAX4413 MODULE AIRBUS 300 A300B4605R 3930308 EU SEAT ARCED A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 70074 517 LHR - FLT 108 - EN ROUTE BOS-LHR - PASSENGER REPORTED ELECTRICAL ARCING UNDER SEAT AT 23C. SHUT DOWN SYSTEM AT MASTER S WITCH. LANDED LHR WITHOUT FURTHER INCIDENT. REPLACED ELECTRONIC BOX AT SEAT 23C. SYSTEM GROUND CHECKED NORMAL OPERATI ON. (M) 2 L 7 2 4F RT A35EU 2001041900136 20010419 00136 EU 2001 4 19 AALA20010240 1 20010213 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU R3 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14053 420 JFK - DURING OVERNIGHT MAINTENANCE, OVERHEAD R3 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AS SEMBLY AT R3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2001041900137 20010419 00137 WP 2001 4 19 AALA20010372 1 20010305 A 3397 WIRE DOUG DC9 DC982 3022082 WP TAILCONE DAMAGED A K NONE O OTHER IN INSP/MAINT 1 SW 21 456AA 49561 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT TAILCONE DIM. REPAIRED EMERGENCY EXIT LIGHT WIRE AT TAILCON E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001041900138 20010419 00138 NM 2001 4 19 AALA20010373 1 20010224 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 887AA 21526 TUL - FOUND FUSELAGE SKIN CRACKED AND CORRODED STATION 1130 AT STRINGER 29R. CUT OUT 2 INCH BY 3 INCH AREA OF SKIN AND INSTALLED DOUBLER REPAIR PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 2001041900139 20010419 00139 NM 2001 4 19 AALA20010374 1 20010226 A 5730 SKIN BOEING 727 727223 1384074 NM WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 887AA 21526 TUL - FOUND LOWER WING SKIN HAS AREA OF CORROSION ABOVE LEFT PRIMARY HEAT EXCHANGER, STATION 820, LBL 25. REMOVED CORRO SION, INSTALLED DOUBLER AND TRIPLER PER SRM 57-30-3. (M) 2 L 7 3 4F A3WE 2001041900140 20010419 00140 NM 2001 4 19 AALA20010375 1 20010226 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 887AA 21526 TUL - FOUND LIGHTS DIM, STATION 560-1030. REPLACED DAMAGED STRIP PER MM 33-60-098-4. (M) 2 L 7 3 4F A3WE 2001041900141 20010419 00141 WP 2001 4 19 AALA20010369 1 20010303 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A K NONE L NO TEST IN INSP/MAINT 1 SW 21 449AA 49475 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT STAIRWELL INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE A T SIDE WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001041900142 20010419 00142 WP 2001 4 19 AALA20010384 1 20010307 A 3320 SOCKET DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 476AA 49651 RDU - FLT 1176 - PRIOR TO GATE DEPARTURE DETECTED STRONG ELECTRICAL BURNING SMELL AT MID CABIN. TURNED OFF ALL POWER. REPLACED FLUORESCENT LAMP HOLDER AND BULB AT SEAT 10DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001041900143 20010419 00143 WP 2001 4 19 AALA20010413 1 20010312 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 577AA 53154 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 20D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 20D. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001041900144 20010419 00144 WP 2001 4 19 AALA20010412 1 20010312 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 577AA 53154 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 14D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 14D. S YSTEM GROUND CHECKED NORMAL OPEATION. (M) 2 L 7 2 4F A6WE 2001041900145 20010419 00145 WP 2001 4 19 AALA20010411 1 20010312 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 577AA 53154 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 11D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 11D. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001041900146 20010419 00146 WP 2001 4 19 AALA20010410 1 20010312 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 577AA 53154 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 10D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 10D. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001041900147 20010419 00147 WP 2001 4 19 AALA20010409 1 20010312 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 577AA 53154 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 2D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 2D. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001041900148 20010419 00148 WP 2001 4 19 AALA20010408 1 20010312 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 577AA 53154 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 5E DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 5E. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001041900149 20010419 00149 WP 2001 4 19 AALA20010407 1 20010312 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 577AA 53154 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 4E DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 4E. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001041900150 20010419 00150 WP 2001 4 19 AALA20010406 1 20010312 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 577AA 53154 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 3E DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 3E. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001041900151 20010419 00151 WP 2001 4 19 AALA20010398 1 20010310 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 555AN 53085 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEATS 4D, 8D, 11D, AND 21D, DIM. REPLACED EMERGENCY EXIT LI GHT AT 4D, 8D, 11D, AND 21D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001041900152 20010419 00152 WP 2001 4 19 AALA20010402 1 20010311 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP L1 DOOR BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 445AA 49471 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L1 DOOR BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT L 1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001041900153 20010419 00153 WP 2001 4 19 AALA20010414 1 20010309 A 3320 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 7532A 49924 ORD - FLT 2253 - ON TAXI OUT, FLIGHT ATTENDANT REPORTED SMOKE AT 9E AND 9F READING LIGHT. REPLACED OVERHEAD READING LIG HT AT 9E AND 9F. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001041900154 20010419 00154 WP 2001 4 19 AALA20010405 1 20010311 A 3397 WIRE DOUG DC9 DC982 3022082 WP COCKPIT LOOSE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 236AA 49251 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT COCKPIT OVERHEAD PANEL INOPERATIVE. RE-SECURED EMERGENCY EX IT LIGHT WIRE AT OVERHEAD COCKPIT PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001041900155 20010419 00155 WP 2001 4 19 AALA20010396 1 20010309 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 489AA 49682 TUL - FOUND DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT STAIR DOOR DIM. REPLACED EMERGENCY EXIT LIGHT BAT TERY PACK AT AFT STAIR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001041900156 20010419 00156 NM 2001 4 19 AALA20010377 1 20010305 A 2910 40914125 HYDRAULIC LINE BOEING 757 757223 1384957 NM LT MLG LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 696AN 26976 LAX - FLT 364 - EN ROUTE FLL-LAX, DETECTED LEFT SIDE HYDRAULIC SYSTEM DECREASE TO ZERO. LANDED LAX WITHOUT FURTHER INCI DENT. REPLACED LEFT GEAR DOWN LOCK LINE. SERVICED HYDRAULIC SYSTEM. LEAKS CHECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001041900157 20010419 00157 NM 2001 4 19 AALA20010391 1 20010301 A 5310 TORQUE BOX BOEING 727 727223 1384074 NM FUSELAGE PUNCTURED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 878AA 21390 TUL - FOUND HOLE PUNCTURED IN LEFT DOOR FRAME UPPER TORQUE BOX STATION 440, FOR E/E DOOR. ROUTED OUT HOLE, DYE CHECKED FOR CRACKS AND INSTALLED DOUBLER PER SRM 51-40-2. (M) 2 L 7 3 4F A3WE 2001041900158 20010419 00158 NM 2001 4 19 AALA20010390 1 20010303 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 878AA 21390 TUL - FOUND 2 INCH BY 7 INCH LARGE SCRAPE BETWEEN STRINGER 21R AND 22R, STATION 1125 TO 1135. DYE CHECKED FOUND NO CRAC KS. MEASURED DEPTH .025. INSTALLED 2024-T3 .071 DOUBLER 53-30. (M) 2 L 7 3 4F A3WE 2001041900159 20010419 00159 NM 2001 4 19 AALA20010389 1 20010303 A 5310 SHEAR TIE BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 878AA 21390 TUL - FOUND SHEAR TIE CORRODED STRINGER 26R, STATION 1148. REMOVED CORRODED SHEAR TIE AND REPLACED WITH NEW PART 51-10- 3. (M) 2 L 7 3 4F A3WE 2001041900160 20010419 00160 NM 2001 4 19 AALA20010388 1 20010303 A 5313 STRINGER BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 878AA 21390 TUL - FOUND STATION 1144 STRINGER 26R CORRODED 2 INCHES BY 12 INCHES. CUT OUT CORRODED STRINGER AND INSTALLED STRINGER SPLICE PER SRM 53-10-3 PAGE 3. (M) 2 L 7 3 4F A3WE 2001041900161 20010419 00161 NM 2001 4 19 AALA20010426 1 20010306 A 5312 BULKHEAD BOEING 727 727223 1384074 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 878AA 21390 TUL - FOUND CRACK IN WEB AT 870 BULKHEAD OUTBOARD OF LOWER CASTING. INSTALLED DOUBLER ON 870 BULKHEAD PER AARD 53-20-00 -2. (M) 2 L 7 3 4F A3WE 2001041900162 20010419 00162 NM 2001 4 19 AALA20010379 1 20010306 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 907AN 29509 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 12 AND 13D DIM. REPLACED EMERGENCY LIGHT BULB AT SEAT 12D A ND 13D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2001041900163 20010419 00163 WP 2001 4 19 EIA2001064 1 20010228 A 5320 WEB DOUG DC9 DC933F 302207A WP FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - LEFT CUSP WEB FROM FS 756-775 CORRODED AND ELONGATED HOLES. REPLACED CUSP WEB PER EO 53-DC9-978-00 REV B. (M ) 2 L 7 2 4F A6WE 2001041900164 20010419 00164 WP 2001 4 19 EIA2001062 1 20010228 A 5311 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - SED HOLE IN FRAME 317 APPROX CENTER OF HOLE TO EDGE OF PART 235D HOLE FS 617 2.5 INCH BELOW L15L. REPAIRED FR AME PER ECRA 933-53-070-2. (M) 2 L 7 2 4F A6WE 2001041900165 20010419 00165 WP 2001 4 19 EIA2001061 1 20010228 A 5311 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE GOUGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FASTENER GOUGING EDGE OF FRAME FS 617 5.5 INCH ABOVE L16L. REPAIRED FRAME PER ECRA 933-53-070-2. (M) 2 L 7 2 4F A6WE 2001041900166 20010419 00166 WP 2001 4 19 EIA2001059 1 20010228 A 5320 WEB DOUG DC9 DC933F 302207A WP FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FORWARD PIT DOOR AFT TORQUE WEB FS 427-434 L24R TO L29R, NUMEROUS INCORRECTLY INSTALLED FASTENERS, NUTPLATE HO LES ELONGATED AND SURFACE CORROSION UNDER NUTPLATES. REPAIRED FORWARD PIT DOR AFT TORQUE WEB PER ECRA 933-53-065-2. (M ) 2 L 7 2 4F A6WE 2001041900167 20010419 00167 WP 2001 4 19 EIA2001058 1 20010228 A 5220 WEB DOUG DC9 DC933F 302207A WP EMER EXIT DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND RIGHT FORWARD EMERGENCY EXIT DOOR INTERIOR WEB, CRACKED FLANGED CUTOUT. REPAIRED DOOR PER ECRA 933-52-0 54-2 REV A. (M) 2 L 7 2 4F A6WE 2001041900168 20010419 00168 WP 2001 4 19 EIA2001056 1 20010228 A 5320 WEB DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - CUSP WEB CRACKED FORWARD SIDE AT FRAME ATTACH POINT FS 737-756 LEFT. REPLACED CUSP WEB PER EO 53-DC9-978-00 R EV B. (M) 2 L 7 2 4F A6WE 2001041900169 20010419 00169 WP 2001 4 19 EIA2001048 1 20010228 A 5311 99187721 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND BS 1132L STRINGER 25L FRAME CORRODED AT END OF FRAME. REPLACED FRAME PER DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2001041900170 20010419 00170 WP 2001 4 19 EIA2001043 1 20010228 A 5320 STRUCTURE DOUG DC9 DC933F 302207A WP FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND AFT PIT STATION 935-965, 28L-28R SEVERAL AREAS OF SURFACE CORROSION. REMOVED CORROSION AND REPAIRED PER ECRA 933-53-069-2. (M) 2 L 7 2 4F A6WE 2001041900171 20010419 00171 WP 2001 4 19 EIA2001041 1 20010228 A 5320 5913055 FITTING DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND LEFT HORIZ FRAME TO CENTER TANK FRONT SPAR CRACKED STATION 598. REMOVED DAMAGED FITTING, DRILLED AND LO CATED NEW FITTING, SEALED AND INSTALLED FASTENERS PER SRM 51-30-1 PAGE 1 FIG 1-3, SRM 51-10-1 PAGE 4-6, SRM 51-20-0 PAGE 3. (M) 2 L 7 2 4F A6WE 2001041900172 20010419 00172 WP 2001 4 19 EIA2001040 1 20010228 A 5311 9922042U506 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND FORWARD PIT RIGHT STATION 484 SUPPORT STRUT FRAME ATTACH CONSTANT SECTION CRACKED. LOCATED AND DRILLED PER SRM 51-10-4. REPLACED SUPPORT STUT FRAME ATTACH CONSTANT SECTION PER SRM 51-30-5 AND 51-30-2. (M) 2 L 7 2 4F A6WE 2001041900173 20010419 00173 WP 2001 4 19 EIA2001039 1 20010228 A 5320 5913055504 FITTING DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND RIGHT HORIZONTAL FRAME TO CENTER TANK FRONT SPAR CRACKED FS 598. REPLACED FITTING PER DC9 SRM 51-30-01 PAGE 1 AND 51-10-04. (M) 2 L 7 2 4F A6WE 2001041900174 20010419 00174 WP 2001 4 19 EIA2001038 1 20010228 A 5320 WEB DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND MAIN CABIN AT FS 522 RBL 54.5 CUSP WEB CRACKED UNDER SEAT TRACK. STOP DRILLED CRACKS, FABRICATED AND IN STALLED DOUBLER PER EO 53-DC9-978-00 REV B. (M) 2 L 7 2 4F A6WE 2001041900175 20010419 00175 WP 2001 4 19 AALA20010247 1 20010129 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 411AA 49322 TUL - FOUND CORROSION BEYOND LIMIT ON SEAT TRACK NR 1 AT STA 825. INSTALLED REPAIR PER AARD 53-20. (M) 2 L 7 2 4F A6WE 2001041900176 20010419 00176 WP 2001 4 19 AALA20010380 1 20010303 A 4900 5940405503 APU DOUG DC9 DC983 3022083 WP TAIL LEAKING A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 76200 53290 DFW - FLT 1507 - EN ROUTE DFW-YVR, FLIGHT ATTENDANT DETECTED HEAVY SMOKE IN CABIN. DECLARED EMERGENCY. RETURNED DFW, A ND LANDED WITHOUT FURTHER INCIDENT. REPLACED APU. REPLACED ACM HEAT EXCHANGERS. REPLACED WATER SEPARATORS BAGS. ACCO MPLISHED PACK BURNOUT PER THE MM. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2001041900177 20010419 00177 WP 2001 4 19 AALA20010416 1 20010228 A 5310 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 TUL - FOUND GOUGE IN LIGHTENING HOLE AROUND DOOR CUTOUT, STATION 629-636 STRINGER 24R. REPAIRED GOUGE PER SRM 51-70-4 ( WEB). (M) 2 L 7 2 4F RT A6WE 2001041900178 20010419 00178 WP 2001 4 19 AALA20010417 1 20010306 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 TUL - FOUND CORROSION ON SUBFLOOR AT APPROX STATION 188 UNDER FLOORBOARD SUPPORT ANGLE AT FORWARD ENTRY DOOR. INSTALLED DOUBLER PER AARD 53-00-00-02 AND SRM 53-01 FIG 4 SHEET 3. (M) 2 L 7 2 4F RT A6WE 2001041900179 20010419 00179 WP 2001 4 19 AALA20010418 1 20010228 A 5310 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 TUL - FOUND FORWARD DOOR STOP HOLE IN DOOR BEAM IS WORN, BS 655. INSTALLED DOUBLER AND HI-LOCKS PER AARD 53-10-00-16. (M) 2 L 7 2 4F RT A6WE 2001041900180 20010419 00180 WP 2001 4 19 AALA20010427 1 20010228 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 TUL - FOUND TOOLING MARKS IN WEB, VERTICAL, STATION 905 LBL 51.5. INSTALLED DOUBLER PER SRM 51-70-4. (M) 2 L 7 2 4F RT A6WE 2001041900181 20010419 00181 WP 2001 4 19 AALA20010428 1 20010222 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 TUL - FOUND DENT IN RADIUS OF BELL FRAME STATION 1098 3 INCHES LEFT OF NR 1 LONG. INSTALLED DOUBLER REPAIR STATION 1098 PER AARD 53-10-00-14. (M) 2 L 7 2 4F RT A6WE 2001041900182 20010419 00182 WP 2001 4 19 AALA20010429 1 20010224 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 TUL - FOUND FRAME WORN STATION 1418 AT LONGERON 21R. BLENDED OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-03. (M) 2 L 7 2 4F RT A6WE 2001041900183 20010419 00183 WP 2001 4 19 AALA20010430 1 20010224 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 TUL - FOUND AREA OF DAMAGE FUSELAGE SKIN WITH DENT AND GOUGES STATION 251 LONGERON 3L INTERIM REPAIR (PREVIOUSLY), ACCOM PLISHED PER SRM 53-04. REMOVED CLASS 3 REPAIR DOUBLER AND INSTALLED INTERNAL FINGER DOUBLER AND EXTERNAL DOUBLER PER SR M 53-04 FIG 38 SHEET 25. (M) 2 L 7 2 4F RT A6WE 2001041900184 20010419 00184 WP 2001 4 19 AALA20010431 1 20010223 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CHAFED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 TUL - FOUND WEAR MARK IN FRAME FROM HYD LINE CLAMP. BLENDED OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-03 FIG 5. (M) 2 L 7 2 4F RT A6WE 2001041900185 20010419 00185 WP 2001 4 19 AALA20010432 1 20010223 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 TUL - FOUND CRACK BETWEEN LIGHTENING HOLES ON RIGHT CUSP AT 1302 9 INCHES INBOARD OF FUSELAGE. INSTALLED DOUBLER PER SR M 53-01 AND AARD 53-00-00-02. (M) 2 L 7 2 4F RT A6WE 2001041900186 20010419 00186 WP 2001 4 19 AALA20010434 1 20010221 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 TUL - FOUND CORROSION ON SEAT TRACK NR 4 AT STATION 234-235. BLENDED OUT CORROSION PER SRM 51-10-3. INSTALLED PLUG REP AIR PER SRM 53-05 FIG 4A ALODINED AND PRIMED PER SRM 51-10-3. (M) 2 L 7 2 4F RT A6WE 2001041900187 20010419 00187 WP 2001 4 19 AALA20010435 1 20010306 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND CORROSION AND BULGING WITH CRACK STATION 207 TO STATION 211 RBL 58. CUT OUT CORRODED CUSP AREA, BLENDED COR ROSION ON CUSP TEE PER SRM 51-10-3. INSTALLED DOUBLER FROM STATION 200 TO 217 RBL 58 PER AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 2001041900188 20010419 00188 WP 2001 4 19 AALA20010436 1 20010307 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - REMOVED WEB STATION 1148 TO 1219, LONGERON 26R TO 30R FOM FOUND OUT OF LIMITS CORROSION ON WEB DURING REMOVAL. RE MOVED OLD WEB AND INSTALLED NEW WEB PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2001041900189 20010419 00189 WP 2001 4 19 AALA20010437 1 20010306 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND DENT ACROSS SHEAR TIE STATION 302 BETWEEN 13L AND 18L, ADL NR 5130036. COLD WORKED DENT TO WITHIN LIMITS AN D INSTALLED TWO ROW DOUBLER PER SRM 53-04 FIG 38. DYE CHECK SHOWS NO CRACKS PERMANENT REPAIR. (M) 2 L 7 2 4F A6WE 2001041900190 20010419 00190 WP 2001 4 19 AALA20010438 1 20010309 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND CORROSION ON CUSP FS 1150-1225. INSTALLED NEW CUSP SHEET STATION 1150-1225 SRM 53-01 SRM 51-01. (M) 2 L 7 2 4F A6WE 2001041900191 20010419 00191 WP 2001 4 19 AALA20010439 1 20010307 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND RIGHT TIEDOWN TRACK HAS SEVERAL AREAS WITH LIGHT CORROSION AFT CARGO STATION 1231-1322. INSTALLED RIGHT AFT TIEDOWN TRACK FROM 1212 TO 1338, SRM 51-01. (M) 2 L 7 2 4F A6WE 2001041900192 20010419 00192 WP 2001 4 19 AALA20010440 1 20010309 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND NR 2 SEAT TRACK CORRODED 1 INCH BY 92 INCHES, LEFT SIDE OF MOUNTING FLANGE AND TOP OF TRACK, STATION 1214 TO 1306. INSTALLED NEW NR 2 SEAT TRACK FROM STATION 1174 TO 1309 IAW SRM 53-05 PART 1 FIG 4F, SHEET 1. (M) 2 L 7 2 4F A6WE 2001041900193 20010419 00193 WP 2001 4 19 AALA20010441 1 20010309 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND CRACK IN CUSP RIGHT SIDE STATION 1220. INSTALLED DOUBLER PER SRM 53-04. (M) 2 L 7 2 4F A6WE 2001041900292 20010419 00292 2001 4 19 HEEA071978 4 20010405 A 3442 4000023 TRANSCEIVER BELL 407 407 1182206 SW WX RADAR SYS INOPERATIVE E K NONE L NO TEST IN INSP/MAINT 1 SW 03 740PH 53435 INOPERATIVE. PERFORMED PRELIMINARY INSPECTION AND TESTED. FOUND NO TRANSMIT. REPLACED ICS U402, U403 AND U404. REPAIR ED. ALIGNED TRANSMITTER AND RECEIVER. BENCH CHECK GOOD. 1 G 7 1 3U O H2SW 2001042000031 20010420 00031 WP 2001 4 20 AALA20010442 1 20010305 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND VISUAL INDICATION OF CRACK LONGERON 20 STATION 993 ABOVE FASTENER AND FORWARD. STOP DRILLED CRACK. INSTALL ED ANGLE DOUBLER PER AARD 53-10-00-18. (M) 2 L 7 2 4F A6WE 2001042000032 20010420 00032 WP 2001 4 20 AALA20010443 1 20010306 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND CORROSION 2 INCHES BY 19 INCHES INSIDE SEAT TRACK NR 6 FROM STATION 237-256. INSTALLED NEW SECTION OF SEAT TRACK FROM STATION 215-302 PER SRM 53-05 FIG 4F. (M) 2 L 7 2 4F A6WE 2001042000033 20010420 00033 WP 2001 4 20 AALA20010444 1 20010306 A 5320 FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND CORROSION ON GALLEY G-2 SUPPORT FITTING AT STATION 215, RBL 58. INSTALLED NEW FITTING AT STATION 215, RBL 5 8. (M) 2 L 7 2 4F A6WE 2001042000034 20010420 00034 WP 2001 4 20 EIA2001115 1 20010228 A 5230 PAN DOUG DC9 DC933F 302207A WP CARGO DOOR GOUGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - MCD UPPER PAN FROM STATION 304 TO STATION 446, FASTENER RIDING ON RIVETS AND RIVETS GOUGING ON ANGLES INSIDE C ARGO DOOR AT APPROX L9L. REPAIRED PAN PER ECRA 933-52-086-2. (M) 2 L 7 2 4F A6WE 2001042000035 20010420 00035 WP 2001 4 20 EIA2001065 1 20010228 A 5230 SKIN DOUG DC9 DC933F 302207A WP CARGO DOOR CHAFED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - MAIN CARGO DOOR FS 370, 2.5 INCHES BELOW WALKING BEAM, SKIN CHAFED. REPAIRED SKIN PER ECRA 933-52-088-2. (M) 2 L 7 2 4F A6WE 2001042000052 20010420 00052 NM 2001 4 20 DL76L010422 1 20010314 A 2910 LINE BOEING 767 767332 1382001 NM HYD SYSTEM SEVERED A DALA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 27 178DN 25143 AFTER LANDING GOT ANTI-SKID EICAS FOLLOWED SHORTLY BY RT HYD QTY EICAS. FOUND LT GEAR STRUT DOOR DAMAGED AND ONE HYD LIN E SEVERED. REPLACED LINE. 2 L 7 2 4F RT A1NM 2001042000053 20010420 00053 NM 2001 4 20 QXEA0100397 1 20010314 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-SEAT TRACK REQUIRES REPLACEMENT DUE TO CORROSION BEYOND LIMITS. REPAIRED IAW DHC-8 SRM 51-40-00 AND RD-8-53-3403. 2 H 7 2 4T RT A13NM 2001042000054 20010420 00054 NM 2001 4 20 DL72S010482 1 20010323 A 5320 CHANNEL BOEING 727 727232 1384082 NM NOSE GEARWELL CRACKED A DALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 538DA 22076 CHANNEL P/N 534201717:ATTACH POINT FOR NOSE GEAR RETRACT ACTUATOR SHEARED ON GEAR EXTENSION CAUSING A_SYSTEM COMPLETE FL UID LOSS. REPLACED SAME 2 L 7 3 4F A3WE 2001042000055 20010420 00055 NM 2001 4 20 DL72E010484 1 20010324 A 2782 ACTUATOR BOEING 727 727247 138408F NM NR 3 KRUEGER JAMMED A DALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 27 283WA 21485 AFTER TAKEOFF NR 3 KRUEGER FLAP DID NOT RETRACT. REPLACED KRUEGER FLAP ACTUATOR AND SHUTTLE VALVE LEAK AND OPS CHECK OK PER OPN 7054.RII 2 L 7 3 4F A3WE 2001042000056 20010420 00056 NM 2001 4 20 DL757010485 1 20010324 A 3350 SIGN BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 M6715 30486 FOUND GALLEY AND L4 SERVICE DOOR EXIT SIGNS INOP. REPLACED POWER SUPPLY AND BATT. OPS NML. 2 L 7 2 4F RT A2NM 2001042000057 20010420 00057 NM 2001 4 20 DL73K010486 1 20010324 A 2761 654496116 ACTUATOR BOEING 727 727227 1384078 NM NMB 1 BROKEN A DALA O OTHER J WARNING INDICATION LD LANDING 1 SO 27 237WA 23185 NR 1 O/B SPOLIER ACTUATOR FAILED AND DUMPED -A- HYDRAULIC SYSTEM ON LANDING. A/C HAD TO BE TOWED FROM TAXIWAY. 2 L 7 3 4F A3WE 2001042000058 20010420 00058 WP 2001 4 20 DLL10010487 1 20010325 A 2500 H22625 CONTROL UNIT LKHEED 1011 10113851 5265010 WP OVERHEAD BIN DISCONNECTED A DALA J A DUMP FUEL UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 SO 27 733DS 193C1224 ON CLIMB OUT OVER HEAD BIN SEAT ROW 28 ABC OPENED IN CTR SECTION CAUSING BAG TO FALL OUT STRIKING PASSENGER IN HEAD. SN UBBER ASSY BECAME DISCONNECTED FROM OVERHEAD BIN FRAME AT SNUBBER ASSY. CTR O/H BIN DOOR ROW 28 ABC REMOVED BOTH DOOR L ATCH MECHANISMS CK OK WHEN DOOR OPENED SNUBBER ASSY CAME DISC AT MOUNTING STUD ON FRAME. 2 L 7 3 4F A23WE 2001042000059 20010420 00059 NM 2001 4 20 DLM11010489 1 20010324 A 3350 POWER SUPPLY DOUG MD11 MD11 3023602 NM CABIN ROW 38C INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 802DE 48473 WITH A/C POWER ON,EMERGENCY LIGHTS AT ROWS 30-35 STAYED ILLUMINATED WITH EMERGENCY LIGHTS SELECTED OFF. REMOVED AND REPL ACED POWER SUPPLY AND BATTERY. CHECKS OK 2 L 7 3 4F RT A22WE 2001042000060 20010420 00060 NM 2001 4 20 DL72E010491 1 20010325 A 3350 BATTERY PACK BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2829W 21481 RT OVERWING EMERGENCY EVAC LIGHT INOP. REPLACED BATT PACK OPS NML. 2 L 7 3 4F A3WE 2001042000061 20010420 00061 NM 2001 4 20 DLM88010492 1 20010325 A 3397 WIRE DOUG MD88 MD88 3023688 NM SEAT 24D PINCHED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 996DL 53363 CHECK FOUND SEAT 24D EMERGENCY LIGHTS INOP. FOUND PINCHED WIRE REPAIRED SAME - EMERGENCY LIGHTS NOW OP NML. 2 L 7 2 4F RT A6WE 2001042000062 20010420 00062 NM 2001 4 20 DLM11010493 1 20010326 A 2530 OVEN DOUG MD11 MD11 3023602 NM AFT GALLEY ODOR A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 801DE 48472 FLT ATT NOTIFIED CREW SMOKE SMELL IN AFT GALLEY. TURNED GALLEY POWER OFF. SMELL CONTINUED SMOKE DISAPEARED. ACTIVATED CA BIN BUS SWITCH TO OFF POSITION. FIRE SERVICE INSPECTED AREA ABOVE AFT GALLEY WITH THERMAL IMAGE DEVICE. NIL HOT SPOTS / DAMAGE NOTED.AREA ALSO INSPECTED BY MTC NO DAMAGE OR SMELL DETECTED. ALL CB PANELS CHECKED ALL CIRCUIT BREAKERS SET RAN ALL GALLEY EQUIPMENT AND LIGHTS IN AREA FOR 1.5 HRS. CONT FROM ITEM 002 SLIGHT SMELL FROM RT DOUBLE OVEN. OVEN AND G-7 C HILLER FWD TO MEL REF LOG ITEMS 006/007 2 L 7 3 4F RT A22WE 2001042000063 20010420 00063 NM 2001 4 20 DL738010494 1 20010326 A 5270 WARNING LIGHT BOEING 737 737832 13844CF NM SERVICE DOOR ILLUMINATED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 394DA 30562 DISCONTINUED TAKE OFF AT 110 KTS ON THE BRAKES AT 80 KTS .AFT ENTRY SERVICE DOOR LIGHT ILLUMINATED THEN WHEN OUT AFTER A /C CAME TO A FULL STOP FLT ATT. RECYCLED DOOR AND SAID THAT THE HANDLE WAS UP A LITTLE BIT. 2 L 7 2 4F RT A16WE 2001042000064 20010420 00064 NM 2001 4 20 DL757010495 1 20010323 A 5330 143N35212 SKIN BOEING 757 757232 1384965 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 604DL 22811 DOUBLER REPAIR AT HMV, AND EXISTING REPAIR DOUBLER WAS REMOVED FROM THE VHF ANTENNA CUTOUT AREA BETWEEN FS 720 & 740 AN D BETWEEN STRINGERS 28L & 28R. THE CUTOUT AND FASTENER HOLES WERE HFEC INSPECTED TO ENSURE NO CRACKS. THE BAC S/B 757 -53A0053MOD DOUBLER WAS INSTALLED WITH DEVIATIONS TO ACCOUNT FOR THE PREVIOUS REPAIR. THE MOD/REPAIR WAS ACCOMPLISHED P ER ER/A 379686-14, REV B. 2 L 7 2 4F RT A2NM 2001042000065 20010420 00065 NM 2001 4 20 DL757010496 1 20010325 A 5330 141N321612 SKIN BOEING 757 757232 1384965 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 6704Z 30396 THE FUSELAGE SKIN WAS FOUND DENTED AND GOUGED IN SEVERAL AREAS BETWEEN FS 200 & 231 AND BETWEEN STRINGER 26R AND BL0.THE DAMAGE WAS REMOVED WITH AN 8.5 INCHES X 8.5 INCHES CUTOUT AND A 10.5 INCHES X 13.75 INCHES CUTOUT. BOTH CUTOUTS WERE R EPAIRED WITH A SINGLE EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 380375 -14, REV A. 2 L 7 2 4F RT A2NM 2001042000066 20010420 00066 NM 2001 4 20 DLM11010497 1 20010326 A 2520 831620405 OVEN DOUG MD11 MD11 3023602 NM AFT GALLEY SMOKE A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 801DE 48472 IN FLIGHT, FLIGHT ATTENDANT REPORTS SMELL AND SMOKE IN AFT GALLEY. AIRCRAFT DEVERTED TO LONDON (LGW). MAINTENANCE RAN OV ENS AND CHILLER, FOUND SMELL COMING FROM CHILLER AND RIGHT AFT OVEN. DISCONNECTED CANNON PLUGS AND PULLED C/B ON BOTH CO MPONENTS. MAINTENANCE IN ATLANTA (ATL) REMOVED AND REPLACED THE AFT CHILLER AND RIGHT AFT OVEN. RAN BOTH NO PROBLEMS NOT ED ETOPS CATEGORY ''B'': DIVERSION OR TURNBACK 2 L 7 3 4F RT A22WE 2001042000067 20010420 00067 NM 2001 4 20 DL72E010498 1 20010326 A 3350 900835A BATTERY PACK BOEING 727 727247 138408F NM L2 DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 830WA 21482 INTERIOR L2 DOOR EMER LITE INOPERATIVE - REPLACED POWER SUPPLY BATTERY PACK. 2 L 7 3 4F A3WE 2001042000068 20010420 00068 NM 2001 4 20 DL73E010499 1 20010327 A 5330 654577416 SKIN BOEING 737 7372S3 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 367DL 21774 A CRACK WAS FOUND IN THE FUSELAGE SKIN AT FS 727B AND STR 16L. THE CRACK WAS CUT OUT AND REPAIRED PER SRM 53-30-3. TH E DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001042000069 20010420 00069 NM 2001 4 20 DL73K010500 1 20010327 A 5743 6545321432 FITTING BOEING 737 737232 1384475 NM REAR SPAR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 316DL 23088 CORROSION WAS FOUND IN A FASTENER HOLE OF THE UPPER ROW COMMON TO THE REAR SPAR UPPER CAP OF THE MLG SUPPORT BEAM O/B AF T FITTING. ANOTHER FASTENER HOLE WAS MISDRILLED WHILE REPLACING THE AFT FITTING. THE FASTENER HOLES WERE OVERSIZED AND BUSHED PER ERA 397386-14 AT HMV. 2 L 7 2 4F RT A16WE 2001042000070 20010420 00070 NE 2001 4 20 DL757010501 2 20010327 A 7200 ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 MAKING METAL A DALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SO 27 694DA 34028 29726 716563 AT SOME POINT IN CLIMB DURING ADVANCEMENT OF THROTTLES CREW REPORTS RT ENG BANG/STALL AND PARAMETERS ROLLED BACK. AT TH AT POINT FUEL CUTOFF INITIATED BY CREW. FLT 579 WAS ORGINALLY CVG TO SJU BUT DIV INTO ATL. UPON ARRVL ATL MTC REPORTING METAL IN TAILPIPE AND VSV SYSTEM PARTS BROKEN - REPLACED ENGINE 2 L 7 2 4F 4 F RT A2NM E17NE 2001042000071 20010420 00071 NM 2001 4 20 DL757010503 1 20010327 A 2121 731376 COOLING FAN BOEING 757 757232 1384965 NM NR 1 BURNED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 665DN 25013 GOT BURNING RUBBER SMELL 3 HRS INTO FLT,AT 350 EQUIP COOLING OVHT LIGHT CAME ON 10 MIN LATER DIVERTED TO LAS - REPLACED NUMBER 1 AIR SUPPLY FAN 2 L 7 2 4F RT A2NM 2001042000072 20010420 00072 NM 2001 4 20 DL764010504 1 20010319 A 3411 MODULE BOEING 767 767432ER NM STATIC AIR FAILED A DALA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 SO 27 835MH 29708 AT FL330 EICAS CAUTION AND ADVISORY MESSAGE - SINGLE AIR DATA, NO AUTO LAND, RUDDER RATIO, AILERON LOCKOUT, L AIR DATA. REPLACED STATIC AIR MODULE 2 L 7 2 4F RT A1NM 2001042000073 20010420 00073 NM 2001 4 20 DL757010505 1 20010326 A 5310 146N851210 DOOR FRAME BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 604DL 22811 IN ORDER TO REPLACE A CORRODED C2 DOOR SILL CHORD, THE FS 1440 OPENING FRAME WAS CUT AND REMOVED BETWEEN THE LOWER DOOR SILL AND STRINGER 26R. THE FRAME CHORDS WERE SPLICED WITH ALUMINUM REPAIR ANGLES AND THE WEB WITH AN ALUMINUM DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 379988-14, REV A. 2 L 7 2 4F RT A2NM 2001042000074 20010420 00074 NM 2001 4 20 QXXEA0100388 1 20010316 A 5280 DOOR DHAV DHC8 DHC8102 2809003 NM NLG DELAMINATED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-RIGHT HAND FORWARD NOSE LANDING GEAR DOOR COMPOSITE IS DELAMINATED ON FORWARD EDGE OF DOOR. REPAIRED IAW DHC-8 SRM 32-20-21, PAGE 211 AND SRM 32-30-00, PAGE 204. 2 H 7 2 4T RT A13NM 2001042000075 20010420 00075 CE 2001 4 20 GLBA2001056 1 20010307 A 2134 1143840391 PRESSURE SWITCH BEECH 1900 1900D 1154162 CE CABIN PRESSURE FAILED A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 01 219GL UE219 ABORTED T/O - RIGHT ENVIROMENTAL FAILURE. REPLACED PRESSURE SWITCH, OPS CHECKED SYSTEM GOOD. 2 L 7 2 4T RT A24CE 2001042000077 20010420 00077 CE 2001 4 20 GLBA2001053 1 20010305 A 2422 SPC10PW INVERTER BEECH 1900 1900D 1154162 CE AC SYSTEM INOPERATIVE A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 01 192GL UE192 LEFT INVERTER FAILED IN FLIGHT. REPLACED INVERTER AND REPAIRED WIRE. 2 L 7 2 4T RT A24CE 2001042000078 20010420 00078 CE 2001 4 20 GLBA2001055 1 20010306 A 2130 1143800595 SHUTOFF VALVE BEECH 1900 1900D 1154162 CE CABIN PRESSURE FAILED A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 01 96UX UE96 ABORTED T/O - RIGHT ENVIROMENTAL FAILURE. REPLACED PRSOV, OPS CHECKED SYSTEM GOOD. 2 L 7 2 4T RT A24CE 2001042000080 20010420 00080 NM 2001 4 20 A6WA200100018 1 20010314 A 3060 A56362 BRUSH BLOCK DORNER DO32 DO328100 2996000 NM RT PROPELLER DIRTY A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 338PH 1887 1887 3029 RIGHT PROP HEAT FAIL. MAINTENANCE CLEANED BRUSH BLOCK ASSEMBLY. 2 H 7 2 4T RT A45NM 2001042000081 20010420 00081 NM 2001 4 20 AWXA0001558 1 20010327 A 5280 141N090679 SKIN BOEING 757 7572S7 1384962 NM NLG DOOR GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 905AW 23567 NOSE WHEEL WELL LEFT AFT DOOR FWD HINGE POINT SKIN IS GOUGED AFT SIDE OF HINGE. REPAIRED IAW ER 19-5310-01061-JS2. 2 L 7 2 4F RT A2NM 2001042000082 20010420 00082 NM 2001 4 20 A6WA200100019 1 20010323 A 3260 870004MODB PSEU DORNER DO32 DO328100 2996000 NM NLG MALFUNCTIONED A A6WA O OTHER N FALSE WARNING LD LANDING 1 GL 31 328ML 3084 DURING GEAR EXTENSION NOSE GEAR UNSAFE INDICATED. C/W EMERGENCY GEAR EXTENSION PROCEDURE. RECEIVED NOSE GEAR DOWN LOCK ED INDICATION. MAINTENANCE REMOVED AND REPLACED PSEU, OPS CHECKED GOOD. 2 H 7 2 4T RT A45NM 2001042000083 20010420 00083 NM 2001 4 20 A6WA200100020 1 20010325 A 2121 011389502 COOLING FAN DORNER DO32 DO328100 2996000 NM A/C BAY FAILED A A6WA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 31 350AD 2362 431 3050 AFTER TAKEOFF CLEARANCE, SMOKED FILLED COCKPIT. COMPLIED WITH SMOKE IN COCKPIT EMERGENCY CHECKLIST. NO CAS MESSAGES AP PEARED. RIGHT AIR CONDITIONING PACK NOT OPERATED. PACK SELECTED OFF PER RIGHT HX FAN MEL. RECEIVED RIGHT PACK FAIL AN D RIGHT PACK OVERHEAT MESSAGES. MAINTENANCE REMOVED AND REPLACED RIGHT GROUND COOLING FAN. 2 H 7 2 4T RT A45NM 2001042000084 20010420 00084 EU 2001 4 20 A6WA200100021 1 20010315 A 2781 WARNING LIGHT BAG BAE146 BAE146200A 1500266 EU COCKPIT ILLUMINATED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 609AW E2070 FAULT LIGHT ILLUMINATED FLAPS STUCK AT 18 DEGREES. MAINTENANCE CLEARED FAULT USING BAE SUPPLEMENT. RAN FLAPS, OPS CHEC KED GOOD. 2 H 7 4 4F RT A49EU 2001042000085 20010420 00085 2001 4 20 A6WA200100022 4 20010317 A 2565 D31050105 SLIDE BAG BAE146 BAE146200A 1500266 EU SERVICE DOOR DEFECTIVE A A6WA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 292UE 19092 19092 E2087 FOUND FWD SERVICE DOOR EVACUATION SLIDE DEPLOYMENT CABLE NOT ATTACHED AND BOTTLE VALVE CABLE MISROUTED. DEPLOYMENT CABL E CONNECTION PIECES MISSING. MAINTENANCE REMOVED AND REPLACED EVACUATION SLIDE ASSEMBLY. 2 H 7 4 4F RT A49EU 2001042000087 20010420 00087 SO 2001 4 20 C2XA01IA158 1 20010312 A 4920 4501968B APU EMB 145 EMB145LR SO TAIL LEAKING A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 13949 145057 IAH - FLIGHT 4197, THE CREW REPORTED THAT AT INITIAL POWER UP WITH THE APU RUNNING, SMOKE WAS NOTICED IN THE CABIN WITH A LAV SMOKE WARNING. MX PLACED THE APU ON MEL 49-32-02 CONTROL NUMBER 007738, AND THE AIRCRAFT WAS APPROVED FOR RETURN T O SERVICE. ON 03/16/01 THE AIRCRAFT RETURNED TO IAH WHERE MX PERFORMED AN OPERATIONAL CHECK OF THE LAV SMOKE DETECTOR W ITH NO DEFECTS NOTED. MX REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE DISCREPANCY REPEATE D ON FLIGHT 4267 03/16/01, AND MX REMOVED AND REPLACED THE LAV SMOKE DETECTOR, AND RELEASED THE AIRCRAFT FOR RETURN TO S ERVICE. THE DISCREPANCY REPEATED AGAIN ON FLIGHT 4203, WHERE MAINTENANCE PLACED THE APU ON MEL. 2 L 7 2 4T RT T00011AT 2001042000088 20010420 00088 NM 2001 4 20 VNAA0103015 1 20010319 A 3260 2291000001 HARNESS DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT MLG DEFECTIVE A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 461PS 12368 0 3075 AFTER BEGINNING THE TAKEOFF ROLL THE FLIGHT CREW RECEIVED A PROXIMITY FAIL WARNING INDICATION. THE FLIGHT CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE INSPECTED THE AIRCRAFT AND IT WAS FERRIED TODAY. THE FERRY FLIGHT WA S COMPLETED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR WIRING HARNESS IN ACCORDANCE WITH DORNIER MANUAL 32-61-04. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001042000089 20010420 00089 NM 2001 4 20 VNAA0103016 1 20010321 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST NR NOT REPORTED 1 GL 07 458PS 7908 0 3068 THE FLIGHT CREW FOUND THAT THE ROW SIX EMERGENCY LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REPLACED THE 5LK EMERGENCY BAT TERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RETURNE D TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001042000090 20010420 00090 EA 2001 4 20 JBXA000261 1 20010322 A 3010 6243843 THERMOSWITCH CNDAIR CL600 CL6002B19 EA ANTI-ICE SYS FAILED A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 572ML 7224 FLT 930 RDU/DCA ON CLIMBOUT HAD WING OVERHEAT MESSAGE. AIRCRAFT RETURNED AND LANDED AT RDU. REMOVED PANEL 620ML, REMOV ED AND REPLACED TEMP SWITCHES 2S4HA, 2S5HA, 2S6HA. TEMP SENSORS 2RT2HA, 2RTHA AND REINSTALLED PANEL. OPERATIONAL CHECK GOOD IAW CL-65 MM 30-12-12 AND 30-12-14. 2 L 7 2 4F RT A21EA 2001042000091 20010420 00091 EA 2001 4 20 COMA0160334 1 20010323 A 5320 ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 7014 L-ANGLE CRACKED FS 484.00 AND ONE RIVET SHEARED ON INTERCOSTAL OUTBOARD EO, OUTBOARD OF RBL 27. REPAIRED L-ANGLE AT FS 484.00 AND REPLACED ONE SHEARED RIVET IAW WVAC EO 601R-53-2328. 2 L 7 2 4F RT A21EA 2001042000092 20010420 00092 EA 2001 4 20 COMA0160335 1 20010323 A 5530 600210617 BUSHING CNDAIR CL600 CL6002B19 EA VERTICAL STAB WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 797CA 7344 LEFT VERTICAL STAB PIVOT POINT BUSHING WORN. REMOVED AND REPLACED BUSHING IAW CRJ AMM 20-26-00-910-803, REAMED BUSHING IAW CRJ DRAWING 600-21061. MACHINED FLANGE IAW WVAC EO 601R-55-2325. 2 L 7 2 4F RT A21EA 2001042000093 20010420 00093 EA 2001 4 20 COMA0160336 1 20010323 A 5551 600R55110221 BUSHING CNDAIR CL600 CL6002B19 EA HORIZ STAB WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 797CA 7344 HORIZONTAL STAB LEFT OUTBOARD PIVOT POINT BUSHING WORN. REMOVED AND REPLACED BUSHING IAW CRJ AMM 20-26-00-910-803. REA MED BUSHING IAW REO 601R-55-11-022 REV A. 2 L 7 2 4F RT A21EA 2001042000094 20010420 00094 EA 2001 4 20 COMA0160337 1 20010323 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 7014 L-ANGLE AND INTERCOSTAL CRACKED FS 484.00 OUTBOARD OF LBL 27. REPAIRED L-ANGLE AND INTERCOSTAL AT FS 484.0 ON LBL 27 AN D OUTBOARD OF LBL 27, IAW WVAC EO 601R-53-2328. 2 L 7 2 4F RT A21EA 2001042000095 20010420 00095 EA 2001 4 20 COMA0160338 1 20010324 A 5753 CAP CNDAIR CL600 CL6002B19 EA FLAP CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 797CA 7344 LEFT INBOARD FLAP HAS CHAFED VANE CAP ON INBOARD END. BLENDED CHAFED AREA IAW CANADAIR REO 601R-57-52-004 AND PAINTED I AW CRJ SRM 51-21-16. 2 L 7 2 4F RT A21EA 2001042000096 20010420 00096 SO 2001 4 20 GLBA2001064 1 20010326 A 7714 3033515 SENSOR EMB 120 EMB120 3260201 SO RT ENGINE INOPERATIVE A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 01 96ZK 12096 ABORTED T/O, RIGHT NH INDICATOR FAILED. REPLACED NH SENSOR, OPS CHECKED SYSTEM GOOD. 2 L 7 2 4T RT A31SO 2001042000097 20010420 00097 WP 2001 4 20 TWAA0105401 1 20010325 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 964TW 53614 THE EMERGENCY EXIT LIGHTS OVER THE LT AND RT FWD OVERWING EXIT DOORS WERE INOPERATIVE. REPLACED THE BATTERY PACK. CHEC K-C 5-6-00 STL. 2 L 7 2 4F RT A6WE 2001042000098 20010420 00098 NM 2001 4 20 TWAA0105402 1 20010325 A 3350 BATTERY PACK BOEING 757 757231 1384950 NM CABIN DISCHARGED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 708TW 28480 THE EGRESS EXIT INDICATORS AT MID FWD CABIN AREA WERE INOPERATIVE. MAINTENANCE FOUND OPERATION NORMAL. BATTERY PACK MA Y HAVE HAD A LOW CHARGE AND CHARGED UP. CHECK-C 3-1-01 JFK. 2 L 7 2 4F RT A2NM 2001042000099 20010420 00099 WP 2001 4 20 TWAA0105403 1 20010321 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9405T 53141 THE EGRESS LIGHTING WAS INOPERATIVE FROM ROW 7 TO 14. SECURED LOOSE WIRING CONNECTOR AT ROW 9. CHECK-C 10-23-00 STL. 2 L 7 2 4F RT A6WE 2001042000100 20010420 00100 NM 2001 4 20 TWAA0105404 1 20010323 A 3350 767 LIGHT BOEING 757 757231 1384950 NM EXTERIOR INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 716TW 28484 THE EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE AT THE RT SIDE NUMBER 1 CABIN DOOR AND AT THE LT SIDE NUMBER 4 CABIN DOOR. REPLACED THE LAMP AT BOTH LOCATIONS. CHECK-C 4-14-00 LAX. 2 L 7 2 4F RT A2NM 2001042000101 20010420 00101 WP 2001 4 20 TWAA0105406 1 20010321 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT FOUND CABIN FLOOR MEMBRANE CRACKED AT STA 332 TO 351, RBL 54 INCHES. INSTALLED REPAIR DOUBLER PER SRM 53-01 FIG 4. INSTALLED FORMER RING FITTING PER SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 2001042000102 20010420 00102 WP 2001 4 20 TWAA0105407 1 20010321 A 5280 DOOR DOUG DC9 DC982 3022082 WP RT MLG CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT FOUND RT MAIN WHEEL WELL DOOR, FWD INBD CORNER OF THE DOOR CRACKED. INSTALLED DOUBLER PER SRM 52-0 5, FIG 28. 2 L 7 2 4F A6WE 2001042000103 20010420 00103 WP 2001 4 20 TWAA0105408 1 20010322 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT FOUND CABIN SEAT TRACK NUMBER 6 HAD CORROSION BETWEEN STA 389 AND 769. REPLACED TRACK SECTIONS. S PLICED PER SRM 53-05, FIG 4D. 2 L 7 2 4F A6WE 2001042000104 20010420 00104 WP 2001 4 20 TWAA0105409 1 20010322 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT IN THE AFT LAV AREA, THE CABIN FLOOR SUPPORT WAS CORRODED, STA 1307, LBL 18 INCHES. INSTALLED NEW FLOOR SUPPORT PER SRM 51-30-1. 2 L 7 2 4F A6WE 2001042000105 20010420 00105 WP 2001 4 20 TWAA0105410 1 20010322 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT RBL 8 TO RBL 45, STA 200. FABRICATED AND INSTALLED FLOOR SUPPO RT PER SPM 6-70-01 AND SRM 53-14-1, 51-30 AND 51-10-3. 2 L 7 2 4F A6WE 2001042000106 20010420 00106 WP 2001 4 20 TWAA0105411 1 20010323 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT FOUND CABIN MEMBRANE CRACKED AT STA 253 TO 275, RBL 54 INCHES. REPAIRED CRACKED MEMBRANE PER SRM 5 3-01, FIG 4 SHEET 3. INSTALLED RIVETS PER SRM 51-30-2. TREATED MATERIAL PER SRM 51-10-3, PAGE 46 ITEM 3. 2 L 7 2 4F A6WE 2001042000107 20010420 00107 WP 2001 4 20 TWAA0105412 1 20010323 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT NUMBER 5 CABIN FLOOR TRACK WAS CORRODED AT STA 237. REPLACED TRACK FROM STA 200 TO 247, PER SRM 53 -05 FIG 4. 2 L 7 2 4F A6WE 2001042000108 20010420 00108 SO 2001 4 20 SWIA972439 1 20010314 A 5753 FLAP TRACK EMB 120 EMB120RT SO PWA 118 PW118 NE WING DIRTY A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 137H 120137 FLAP DISAGREEMENT IN FLIGHT DURING FLAP RETRACTION. FOUND FLAP TRACKS AND ROLLERS DIRTY. CLEANED ALL TRACKS AND ROLLER S. OPERATED FLAPS NUMEROUS TIMES. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042000109 20010420 00109 2001 4 20 SWIA972440 4 20010318 A 2216 SERVO EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE ELEVATOR TRIM BINDING A SWIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 07 199SW 120237 AFTER AUTOPILOT DISCONNECTED, CAPTAINS SIDE NOTICED BINDING OF TRIM (ELEVATOR) BETWEEN 3 AND 6 UNITS. TRIM WHEEL WOULD BIND THEN RELEASE. ALTITUDE 6000 FEET WITH NO MOISTURE. INSPECTED ENTIRE ELEVATOR TRIM SYSTEM FOR DEFECTS. NONE NOTED . ALL TESTS AND FUNCTIONAL CHECKS FOUND ELEVATOR TRIM SYSTEM OPERATING NORMAL. REPLACED ELEVATOR TRIM SERVO WITH A SER VICEABLE UNIT AS A PRECAUTION. S/N OFF 3715, ON 4545. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042000110 20010420 00110 SO 2001 4 20 SWIA972441 1 20010319 A 2750 CONTROL UNIT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FLAPS MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 205SW 120260 DURING DESCENT AND DURING CLIMBOUT FLAP ADVANCED SWS AND CONTROL FAULT INDICATIONS (BOTH NACELLE PAIRS FLASHING) ILLUMIN ATED WITHOUT HAVING SELECTED FLAP MOVEMENT (RESET PER QRH PROCEDURE). REPLACED FLAP CONTROL UNIT. OPS CHECK GOOD. P/N ON 347200-1001, S/N ON 6148, S/N OFF 0208. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042000111 20010420 00111 EA 2001 4 20 SWIA972443 1 20010321 A 2760 SPOILER CNDAIR CL600 CL6002B19 EA WINGS OUT OF RIG A SWIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 07 413SW 7102 AIRPLANE ROLLS LEFT WITH 1/4 FLIGHT SPOILER OUT. INDICATES 9 LEFT, 8 RIGHT. REMOVED AND REPLACED LEFT HAND FLIGHT SPOI LER INBOARD ACTUATOR IAW 27-63-01. REMOVED AND REPLACED RIGHT HAND FLIGHT SPOILER OUTBOARD ACTUATOR. LEAK CHECK GOOD. STILL HAS SPLIT. HYDRAULIC SYSTEM NUMBER TWO CAUSES 3 DEGREE SPLIT IN FLIGHT. ADJUSTED RIGGING OF RIGHT SPOILER INBO ARD PCU IAW MM 27-62-01-803-801. OPS CHECK GOOD.P/N ON (LT) 27000-7, S/N ON 355, S/N OFF 709, P/N OFF (RT) 27000-7, S/N ON 909, S/N OFF 910. 2 L 7 2 4F RT A21EA 2001042000112 20010420 00112 SO 2001 4 20 SWIA972444 1 20010321 A 5270 SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FUEL DOOR OUT OF ADJ A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 290SW 120317 FUEL DOOR CAMLOCK IS LOOSE (ON RIGHT HAND SIDE). ABORTED TAKEOFF. ADJUSTED SWITCH ON INBOARD FUELING DOOR. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042000113 20010420 00113 CE 2001 4 20 GLBA2001062 1 20010319 A 2460 727725 CIRCUIT BREAKER BEECH 1900 1900D 1154162 CE COCKPIT FAILED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 251GL UE251 LEFT AC BUS FAIL IN FLIGHT. REPLACED CIRCUIT BREAKER, OPS CHECKED GOOD. 2 L 7 2 4T RT A24CE 2001042000114 20010420 00114 SO 2001 4 20 C2XA01IA181 1 20010325 A 3350 1317 LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 40717 120133 ABI- ON POSTFLIGHT INSPECTION THE CREW OBSERVED THE EXTERNAL EMERGENCY LIGHT ON THE FORWARD LEFT SIDE INOPERATIVE, AND T HE AIRCRAFT WAS RELEASED IAW MEL 32-60-1 CATAGORY B. IAH- MAINTENANCE REMOVED AND REPLACED THE LEFT EXTERNAL FORWARD EM ERGENCY LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001042000115 20010420 00115 SO 2001 4 20 C2XA01IA178 1 20010323 A 4950 4501968B APU EMB 145 EMB145LR SO TAIL LEAKING A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 13949 145057 IAH- APU BLEED PUTTING SMOKE IN CABIN AND LAV. MAINTENANCE REMOVED AND REPLACED THE APU ASSEMBLY IAW EMB145 MAINTENANCE MANUAL 49-10-01, LEAK AND OPERATIONAL CHECK GOOD AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001042000116 20010420 00116 NM 2001 4 20 AWXA0001536 1 20010326 A 5315 BAC1518338 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 FLOORBEAM AT FS 520 RBL 24.75 HAS A CRACK IN THE RADIUS OF UPPER CHORD EXTENDING PAST STOP DRILL. REMOVED EXISTING DOUB LERS; VERIFIED CRACK LENGTH; STOP DRILLED CRACK; VERIFIED CRACK TERMINATION AT STOP DRILL. REINSTALLED DOUBLERS IAW SRM 51-30-2 PG 1. 2 L 7 2 4F RT A16WE 2001042000117 20010420 00117 NM 2001 4 20 CALA0100252 1 20010325 A 3230 65448105 ACTUATOR BOEING 737 7373Q8 1384670 NM RT MLG INOPERATIVE A CALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 09 14384 18573 26313 THE RT MLG RED LIGHT REMAINED ILLUMINATED WITH NO GREEN LIGHT WHEN GEAR WAS EXTENDED ON APPROACH TO IAH. A MANUAL GEAR EXTENSION WAS PERFORMED SUCCESSFULLY AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT MLG UPLOCK ACTU ATOR AT FAULT. THE UPLOCK ACTUATOR WAS REPLACED IAW MM 32-32-41. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2001042000118 20010420 00118 SO 2001 4 20 C2XA01IA182 1 20010325 A 3350 RPS1B BATTERY PACK EMB 145 EMB145LR SO CABIN DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17984 145246 IAH - FLIGHT 3823, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS FROM ROW 12 ON ILLUMINA TED WHEN THE EMERGENCY LIGHT SWITCH WAS PLACED IN THE ARM POSITION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERG ENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001042000119 20010420 00119 SO 2001 4 20 C2XA01IA183 1 20010312 A 4930 CAV180 PLUG EMB 120 EMB120ER 3260203 SO APU LEAKING A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 58733 120197 IAH - FLIGHT 2479, THE CREW REPORTED A STRONG FUEL SMELL AFTER DEPARTURE FROM CLL. THE AIRCRAFT LANDED AT IAH WITHOUT I NCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE APU EPA TANK DRAIN PLUG, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001042000120 20010420 00120 NE 2001 4 20 SABA010008 2 20010326 A 7260 WARNING LIGHT DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE COCKPIT ILLUMINATED A SABA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 33 883CC 162 AIRCRAFT 883CC ON FLIGHT 5157 CVG/CLT. DURING TAKEOFF ROLL THE RIGHT ENGINE OIL PRESSURE GAUGE WENT TO 40 PSI AND THE L OW OIL PRESSURE WARNING LIGHT ILLUMINATED. TAKEOFF WAS ABORTED, THE AIRCRAFT RETURNED TO THE GATE WITH NO OTHER PROBLEM S. NO EMERGENCY WAS DECLARED. MAINTENANCE ADDED TWO QUARTS OF OIL TO THE RIGHT ENGINE. A GROUND RUN WAS PERFORMED. G ROUND RUN WAS GOOD, AND OPS CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2001042000121 20010420 00121 EU 2001 4 20 DHL2001362009 1 20010326 A 5330 SKIN AIRBUS 300 A300B4103 3930104 EU FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 84 RT FUSELAGE FWD OF LOWER CARGO DOOR FRAME 1383 SKIN SURFACE HAS A DENT (ADJACENT AFT OF ICE LIGHT). E&E COMP, RT AFT OF AC BATTS, REPOSITIONED FOR SM ACCESS, RELAY BOX 251VU AND 252VU PER A300 MM 25-54-00. NO CANNON PLUGS DISCONNECTED. C UT OUT GOUGED/DAMAGED AREA APPROX 1 X 3.5 INCHES IAW A300 SRM-53-10-10. BLENDED GOUGE, OUT OF LIMITS IAW A300 SRM 53-10 -10. FABRICATED DOUBLER AND TRIPLER. DRILLED AND COUNTERSUNK HOLES FOR FASTENERS. INSTALLED AND SEALED IAW A300 SRM 5 3-10-10 AND AVITAS RO AVHM 208RO-1. OK TO REINSTALL INSULATION BLANKETS AND REPOSITION ITEMS THAT WERE RELOCATED TO GAI N ACCESS FOR REPAIR INSIDE OF E & E COMPARTMENT IAW A300 SRM 53-10-10. REINSTALLED INSULATION BLANKET. 2 L 7 2 4F RT A35EU 2001042000122 20010420 00122 NM 2001 4 20 0101036641 1 20010326 A 5320 WEB BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 641NW 21941 DURING PCK FOUND CRACK ON CARGO FLOOR WEB AT BS 1960 LBL 18. REPAIRED PER EA 66-181884. 2 L 7 4 4F A20WE 2001042000123 20010420 00123 EU 2001 4 20 RAIA00103016 1 20010326 A 3244 AH52688 TIRE JETAIR JETSTM JETSTM4101 1500501 EU NLG BLOWN A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 572HK 41091 5406-EWR- NOSE LANDING GEAR TIRES BLEW OUT ON TAKEOFF. MAINTENANCE REMOVED AND REPLACED THE NOSE TIRES IAW J41 MAINTENA NCE MANUAL. 2 L 7 2 4T RT A41NM 2001042000124 20010420 00124 NM 2001 4 20 AWXA0001533 1 20010326 A 5230 65C36231 SKIN BOEING 737 7373Y0 1384671 NM CARGO DOOR DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 DENT NR 1, 16 INCHES FROM FWD EDGE OF AFT CARGO DOOR 31 INCHES UP FROM BTM - 2.0 INCHES WIDE, .125 INCH DEEP - OUT OF L IMITS; DENT NR 2, 35 INCHES FROM FWD EDGE 27 INCHES UP FROM BTM - 1.25 INCH WIDE .093 DEP - OUT OF LIMITS. REMOVED AND FABBED AFT CARGO DOOR OUTER SKIN IAW DWG 65-47952, SRM 52-30-01. 2 L 7 2 4F RT A16WE 2001042000125 20010420 00125 NM 2001 4 20 AWXA0001534 1 20010326 A 5310 6545409602 TEE CHORD BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 MAIN WHEEL WELL FWD BLKHD UPPER T-CHORD CRACKED AT FS 663.75 LBL 24 AND RBL 24. REPAIRED IAW BOEING DWG 65C37732, B737- 200 SRM 51-30-2 PGS 2-3, 5, 7-9 AND AWA ER 15-5702-01073-JS3. 2 L 7 2 4F RT A16WE 2001042000126 20010420 00126 NM 2001 4 20 AWXA0001535 1 20010326 A 5320 6545833U40 WEB BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 CRACKED FLOOR WEB AT FS 179-180 LBL 38 WL 207. REMOVED AND REPLACED WEB IAW SRM 51-30-2 PGS 2 & 8. 2 L 7 2 4F RT A16WE 2001042000127 20010420 00127 NM 2001 4 20 AWXA0001537 1 20010326 A 5230 BAC15031430 SKIN BOEING 737 737277 1384570 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 AFT CARGO DOOR INNER SKIN CRACKED AT 3 PLACES, AT LIGHTNING HOLES IN CENTER SKIN BETWEEN BEAMS 2 AND 3. REPAIRED CRACKS IN INNER SKIN IAW SRM 51-20-1 PG 10A AND 51-30-2 PG 2. 2 L 7 2 4F RT A16WE 2001042000128 20010420 00128 NM 2001 4 20 AWXA0001538 1 20010326 A 5311 651758365 FRAME BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 FS 178 BLKHD WEB VERTICAL CHORD IS CRACKED AT LBL 5.7 WL 173 - 174.5. REPAIRED VERT CHORD IAW SRM 53-10-08 PG 221-252 F IG 205. 2 L 7 2 4F RT A16WE 2001042000129 20010420 00129 NM 2001 4 20 AWXA0001539 1 20010326 A 5312 65163007 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 FS 178 BLKHD WEB IS CRACKED AT RBL 4.8 WL 198.7 AND 199.3 AND 199.9. REMOVED FASTENERS; CUT OUT DAMAGED AREA; LOCATED, DRILLED AND INSTALLED DOUBLER AND FILLER IAW SRM 53-10-08 PG 1-11 FIG 211. 2 L 7 2 4F RT A16WE 2001042000130 20010420 00130 NM 2001 4 20 AWXA0001540 1 20010326 A 5312 65163007 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 FS 178 BLKHD WEB IS CRACKED AT LBL 1.5 WL 205.8 BELOW T-ANGLE. REMOVED FASTENERS; CUT OUT DAMAGED AREA; LOCATED, DRILLE D AND INSTALLED DOUBLER AND STRAP IAW SRM 53-10-08 PG 1-11 FIG 211. 2 L 7 2 4F RT A16WE 2001042000131 20010420 00131 NM 2001 4 20 AWXA0001541 1 20010326 A 5312 65163007 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 FS 178 BLKHD CENTER WEB IS CRACKED AT RBL 1.0 WL 205.5. REMOVED FASTENERS; CUT OUT DAMAGED AREA; LOCATED, DRILLED AND I NSTALLED DOUBLER AND STRAP IAW SRM 53-10-08 PG 1-11 FIG 211. 2 L 7 2 4F RT A16WE 2001042000132 20010420 00132 NM 2001 4 20 AWXA0001542 1 20010326 A 5312 65163007 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 FS 178 BLKHD CENTER WEB IS CRACKED AT LBL 7 WL 200.75 TO 201.25. REMOVED FASTENERS; CUT OUT DAMAGED AREA; LOCATED, DRIL LED AND INSTALLED DOUBLER AND STRAP IAW SRM 53-10-08 PG 1-11 FIG 211. 2 L 7 2 4F RT A16WE 2001042000133 20010420 00133 NM 2001 4 20 AWXA0001543 1 20010326 A 5312 65163007 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 FS 178 BLKHD CENTER WEB IS CRACKED AT LBL 4.8 WL 198.4 AND WL 201.2 - 201.5. REMOVED FASTENERS; CUT OUT DAMAGED AREA; L OCATED, DRILLED AND INSTALLED DOUBLER AND STRAP IAW SRM 53-10-08 PG 1-11 FIG 211. 2 L 7 2 4F RT A16WE 2001042000134 20010420 00134 NM 2001 4 20 AWXA0001544 1 20010326 A 5312 65163007 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 FS 178 BLKHD CENTER WEB IS CRACKED (2 CRACKS) AT LBL 1.5 WL 187.25-188 AND AT RBL 1.5 WL 187-188.25. REMOVED FASTENERS; CUT OUT DAMAGED AREA; LOCATED, DRILLED AND INSTALLED DOUBLER AND STRAP IAW SRM 53-10-08 PG 1-11 FIG 211. 2 L 7 2 4F RT A16WE 2001042000135 20010420 00135 NM 2001 4 20 AWXA0001545 1 20010326 A 5320 6545833U40 WEB BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 FLOOR STRUCTURE AT WL 207 AFT SIDE OF FS 178 BLKHD HAS A CRACK EXTENDING O/B TOWARDS SIDE CHORD. REMOVED AND REPLACED W EB (WL 180 - 225 LBL 18 AND RBL 18) IAW SRM 51-40-02 PG 1. 2 L 7 2 4F RT A16WE 2001042000136 20010420 00136 NM 2001 4 20 AWXA0001546 1 20010326 A 5312 65163007 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 FS 178 BLKHD CENTER WEB IS CRACKED AT 2 PLACES LBL 10.8 AND 11.7 WL 234.1. REMOVED FASTENERS; CUT OUT DAMAGED AREA; LOC ATED, DRILLED AND INSTALLED DOUBLER AND STRAP IAW SRM 53-10-08 PG 1-11 FIG 211. 2 L 7 2 4F RT A16WE 2001042000137 20010420 00137 SO 2001 4 20 C2XA01CL066 1 20010325 A 2612 14534156401 MODULE EMB 135 EMB135ER 3260203 SO COCKPIT INOPERATIVE A C2XA K NONE L NO TEST NR NOT REPORTED 1 SW 27 19503 3503 145176 CLE FLIGHT 3355 THE CREW REPORTED THE BAGGAGE FIRE DETECT LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE FIRE DETECT O VERHEAD MODULE. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001042000138 20010420 00138 NM 2001 4 20 01FDEA00234 1 20010324 A 3610 CLAMP BOEING 727 727225 1384077 NM NR 2 ENGINE LOOSE A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 467FE 21449 DURING CLIMB AT 8000 FT MSL WITH PWR SET NR 3 ENG FIRE LIGHT ILLUMINATED ALONG WITH FIRE BELL. NR 3 THROTTLE WAS RETARD ED TO IDLE FIRE LIGHT AND BELL WENT OUT. FOUND LOOSE CLAMP ON 13TH STAGE PNEUMATIC BALL JOINT IN PYLON. TORQUED CLAMP, LEAK CK GOOD. 2 L 7 3 4F A3WE 2001042000139 20010420 00139 WP 2001 4 20 EIA2001109 1 20010228 A 5315 3912825500N FLOORBEAM DOUG DC9 DC933F 302207A WP FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND FS 207 LEFT FLOORBEAM UPPER CHORD CONTAINS ELONGATED HOLE. REPAIRED CHORD PER ECRA 933-53-101-2. (M) 2 L 7 2 4F A6WE 2001042000140 20010420 00140 WP 2001 4 20 TWAA0105405 1 20010321 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT RBL 8, STA 180 TO 200. REMOVED FLOOR SUPPORT AND FABRICATED NE W PER SRM 53-14-01, FIG 11 SHEET 1. TREATED PER SRM 51-10-03. SEALED PER SRM 51-20-0. INSTALLED PER SRM 51-30-01. 2 L 7 2 4F A6WE 2001042000141 20010420 00141 NM 2001 4 20 QXEA0100392 1 20010314 A 5320 ANGLE DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-CORROSION ON ANGLE AT STATION 600, WL 100. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2001042000142 20010420 00142 WP 2001 4 20 CALA0100246 1 20010323 A 5310 BEAM DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72822 49482 INSPECTION FOUND MID CARGO DOOR JAMB BEAM CORRODED. THE CORROSION WAS REMOVED. A DOUBLER WAS INSTALLED IAW ECRA 5310-0 3027. 2 L 7 2 4F A6WE 2001042000143 20010420 00143 WP 2001 4 20 CALA0100247 1 20010323 A 5311 FRAME DOUG DC9 DC982 3022082 WP RT W/W CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72822 49482 INSPECTION FOUND A 1 INCH CRACK IN RIGHT W/W FORWARD FRAME AT I/B LEADING EDGE NEXT TO KEEL BEAM. REPAIR DOUBLERS WERE INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-4, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 2001042000144 20010420 00144 WP 2001 4 20 EIA2001108 1 20010228 A 5320 99100789 ANGLE DOUG DC9 DC933F 302207A WP FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND FS LEFT L18L EXFOLIATION CORROSION ON CUSP TEE. REPAIRED CUSP TEE PER ECRA 933-53-064-2 REV B. (M) 2 L 7 2 4F A6WE 2001042000145 20010420 00145 WP 2001 4 20 EIA2001107 1 20010228 A 5320 WEB DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND MAIN CABIN FS 237-294 CUSP WEB CONTAINS EXFOLIATION CORROSION AND CRACK AT LBL 56 FS 275. REPLACED CUSP WEB PER EO 53-978-00 REV B. (M) 2 L 7 2 4F A6WE 2001042000146 20010420 00146 WP 2001 4 20 CALA0100248 1 20010323 A 5311 FRAME DOUG DC9 DC982 3022082 WP LT W/W CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72822 49482 INSPECTION FOUND A 1 INCH CRACK IN LEFT W/W LOWER FORWARD FRAME I/B NEXT TO KEEL BEAM. REPAIR DOUBLERS WERE INSTALLED I AW 53-01, FIGURE 2, 51-10-4, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 2001042000147 20010420 00147 WP 2001 4 20 CALA0100249 1 20010324 A 5342 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72822 49482 INSPECTION FOUND A CRACK IN AFT FUSELAGE TO VERTICAL STABILIZER ANGLE AT AFT END RT SIDE. THE CRACKED AREA WAS REMOVED IAW SRM 53-05, FIGURE 23. DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-10-3, 53-05, FIGURE 23, AND 51-20-0. 2 L 7 2 4F A6WE 2001042000148 20010420 00148 WP 2001 4 20 CALA0100250 1 20010324 A 5342 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72822 49482 INSPECTION FOUND A CRACK IN AFT FUSELAGE TO VERTICAL STABILIZER ANGLE AT AFT END LT SIDE. THE CRACKED AREA WAS REMOVED IAW SRM 53-05, FIGURE 23. DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-05, FIGURE 23, 51-10-3, 51-20-0, AND 51-30-5. 2 L 7 2 4F A6WE 2001042000149 20010420 00149 WP 2001 4 20 CALA0100251 1 20010324 A 5753 SKIN DOUG DC9 DC982 3022082 WP T/E FLAP GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72822 49482 INSPECTION FOUND RIGHT T/E INBOARD FLAP LOWER SKIN AFT OF MLG PITTED AND GOUGED. THE INBOARD T/E FLAP WAS REMOVED IAW M M 27-50-00. THE INBOARD T/E FLAP WEDGE WAS RESKINNED IAW SRM 51-10-4, 51-30-2, AND 57-50-9. THE INBOARD T/E FLAP WEDGE WAS REINSTALLED IAW MM 27-50-00 AND SRM 51-30-1. A REPAIR DOUBLER WAS INSTALLED ON OUTBOARD T/E IAW SRM 57-01, FIGURE 3, 51-10-4, AND 51-30-8. 2 L 7 2 4F A6WE 2001042000150 20010420 00150 NM 2001 4 20 CALA0100253 1 20010326 A 5330 SKIN BOEING 737 737824 13844BZ NM FUSELAGE PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13248 28808 THE AIRCRAFT HAD GROUND DAMAGE. THE FUSELAGE SKIN WAS PUNCTURED ON L/H SIDE FORWARD OF WING ROOT FAIRING AT STA 500D-50 0E, STRINGER 18-20L. THE AIRCRAFT WAS PREPARED FOR A MAINTENANCE FERRY FLIGHT TO CLE IAW ECRA 5330-03046. A PERMANENT SKIN REPAIR WAS PERFORMED AT CLE IAW SRM 53-00-01, REPAIR 3. 2 L 7 2 4F RT A16WE 2001042000151 20010420 00151 NE 2001 4 20 HNAA0100021 2 20010322 A 7261 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENGINE LACK OF LUBE A HNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 07 922HA 094 120344 DURING TAKEOFF ROLL, NR 2 ENGINE OIL PRESSURE FLUXED INTO THE YELLOW ARC. THERE WERE NO ASSCOIATED WARNING LIGHTS. CRE W ABORTED TAKEOFF. SERVICED NR 2 ENGINE WITH THREE QUARTS OF OIL. 2 H 7 2 4T 4 T RT A13NM E20NE 2001042000152 20010420 00152 WP 2001 4 20 EIA2001096 1 20010228 A 5330 PANEL DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND FS 449 RIGHT SERVICE PANEL 5019 LOWER PANEL SKIN CRACKED. REPAIRED PANEL SKIN PER ECRA 933-53-107-2. ( M) 2 L 7 2 4F A6WE 2001042000153 20010420 00153 WP 2001 4 20 EIA2001095 1 20010228 A 5347 CARGO TRACK DOUG DC9 DC933F 302207A WP CARGO BAY CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND FORWARD PIT FS 441 TO FS 467 LBL 27 SEAT TRACK UPPER CHORD CORRODED. REPAIRED SEAT TRACK PER ECRA 933-5 3-097-2. (M) 2 L 7 2 4F A6WE 2001042000154 20010420 00154 WP 2001 4 20 TWAA0105501 1 20010326 A 3350 408822101 BATTERY DOUG DC9 DC932 3022066 WP COCKPIT DISCHARGED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 998R 47030 THE COCKPIT OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY. CHECK-C 2-4-01 STL. 2 L 7 2 4F A6WE 2001042000155 20010420 00155 NM 2001 4 20 TWAA0105502 1 20010327 A 3350 363674 LIGHT BOEING 757 7572Q8 1384972 NM CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 710TW 28169 THE EGRESS LIGHT WAS INOPERATIVE BY THE LEFT SIDE LAV AND AT SEAT ROW 1 LEFT SIDE. REPLACED THE LAMP AT BOTH LOCATIONS. CHECK-C 5-4-00 LAX. 2 L 7 2 4F RT A2NM 2001042000156 20010420 00156 WP 2001 4 20 TWAA0105503 1 20010323 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 906TW 49160 DURING CHECK-C MAINT IN THE FWD CARGO COMPT FOUND CORROSION AT LONGERON 28R, FROM STA 349 TO 357. REPLACED LONGERON PER SRM 53-02, FIG 18. INSTALLED FASTENERS PER SRM 51-30-03. PRIMED AND PAINTED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001042000157 20010420 00157 WP 2001 4 20 TWAA0105504 1 20010323 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 906TW 49160 DURING CHECK-C MAINT IN FWD CARGO COMPT FOUND CORROSION AT INTERCOSTAL ABOVE LONGERON 29R, STA 354 TO 360. REPLACED INT ERCOSTAL PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-3. PRIMED AND PAINTED PER SRM 51-10-03. 2 L 7 2 4F A6WE 2001042000158 20010420 00158 WP 2001 4 20 TWAA0105506 1 20010324 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 906TW 49160 DURING CHECK-C MAINT FOUND CHAIR TRACK AT RBL 24 INCHES WITH HEAVY CORROSION AT STA 200 TO 218 ON FLANGES. REPLACED COR RODED CHAIR TRACK WITH NEW PER SPM 6-70-01, PAGE 3. 2 L 7 2 4F A6WE 2001042000159 20010420 00159 WP 2001 4 20 TWAA0105507 1 20010325 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 906TW 49160 DURING CHECK-C MAINT FOUND FLOOR SUPPORT CORRODED AT STA 1250, LBL 24 INCHES TO 48 IN LBL. REMOVED FLOOR SUPPORT. INST ALLED NEW SUPPORT WITH FASTENERS PER SRM 51-30-3. 2 L 7 2 4F A6WE 2001042000160 20010420 00160 WP 2001 4 20 EIA2001089 1 20010228 A 5315 FLOORBEAM DOUG DC9 DC933F 302207A WP FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND FS 756 FLOORBEAM UPPER CHORD FORWARD 2 SEAT TRACK ATTACHMENT HOLES ELONGATED TO .312. REPAIRED FLOORBEA M PER ECRA 933-53-104-2. (M) 2 L 7 2 4F A6WE 2001042000161 20010420 00161 WP 2001 4 20 EIA2001088 1 20010228 A 5230 99211662 FRAME DOUG DC9 DC933F 302207A WP CARGO DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - MCD STATION 389 L16L TO L17L LOWER CLOSEOUT WEB AREA INTERIOR FRAME CRACKED. REPLACED FRAME PER DC9 SRM 51-30 -2 AND 51-30-5. (M) 2 L 7 2 4F A6WE 2001042000162 20010420 00162 WP 2001 4 20 EIA2001087 1 20010228 A 5230 99211661 FRAME DOUG DC9 DC933F 302207A WP CARGO DOOR GOUGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - MCD STATION STATION 351 L17L LOWER CLOSEOUT WEB AREA INTERIOR FRAME GOUGED JUST ABOVE WALKING BEAM. REPLACED FRAME PER DC9 SRM 51-30-2 AND 51-30-5. (M) 2 L 7 2 4F A6WE 2001042000163 20010420 00163 WP 2001 4 20 EIA2001086 1 20010228 A 5311 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND FS 718 LBL 55 FRAME UPPER FLANGE 3 ELONGATED HOLES AT FLOOR LINE. REPAIRED FRAME PER ECRA 933-53-106-2. (M) 2 L 7 2 4F A6WE 2001042000164 20010420 00164 WP 2001 4 20 EIA2001085 1 20010228 A 5230 FITTING DOUG DC9 DC933F 302207A WP CARGO DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND FS 413.062 MCD LOWER FITTING CRACKED. REPLACED FITTING PER DC9 SRM 51-30-5 PAGE 1-30. (M) 2 L 7 2 4F A6WE 2001042000165 20010420 00165 WP 2001 4 20 TWAA0105508 1 20010323 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 928TW 48012 DURING CHECK-C MAINT AT LT AFT LAV FOUND CORROSION ON FORE AND AFT SIDES OF FORMER, STA 1338, FROM CUSP TO LONGERON 21L. REMOVED CORROSION AND INSTALLED REPAIR PER SRM 51-70-4. 2 L 7 2 4F A6WE 2001042000166 20010420 00166 WP 2001 4 20 TWAA0105509 1 20010326 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 906TW 49160 DURING CHECK-C MAINT IN THE FWD CARGO COMPT FOUND CRACK AT INTERCOSTAL TIE ANGLE AT FWD SIDE OF STA 229 FORMER BETWEEN L ONGERON 27L AND 28L. REMOVED AND REPLACED ANGLE PER SPM 6-70-01. REPLACED FASTENERS PER SRM 51-30-02 AND SRM 51-30-05. 2 L 7 2 4F A6WE 2001042000167 20010420 00167 WP 2001 4 20 TWAA0105510 1 20010326 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 906TW 49160 DURING CHECK-C MAINT IN THE FWD CARGO COMPT A CRACK WAS FOUND AT INTERCOSTAL TIE ANGLE AT FWD SIDE OF STA 229 FORMER BET WEEN LONGERON 27R AND 28R. REPLACED ANGLE PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-01. 2 L 7 2 4F A6WE 2001042000168 20010420 00168 WP 2001 4 20 TWAA0105511 1 20010326 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT CORRODED AT STA 200, LBL 4 TO RBL 4. REPLACED FLOOR SUPPORT PER SPM 6-70 -01 AND SRM 53-14-1. 2 L 7 2 4F A6WE 2001042000169 20010420 00169 WP 2001 4 20 TWAA0105512 1 20010326 A 5320 BRACE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT IN MID CARGO COMPT, FOUND CORROSION ON CORNER BRACE AT STA 693, RBL 7 IN. REPLACED BRACE PER SRM 5 1-30-5. 2 L 7 2 4F A6WE 2001042000170 20010420 00170 WP 2001 4 20 TWAA0105513 1 20010326 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 909TW 49170 DURING CHECK-C MAINT AT STA 1155, LBL 24 TO 42, THE FLOOR CAP HAD HEAVY CORROSION TOP SIDE. FLOORBEAM CAP GROUND BEYOND LIMITS. REPLACED SUPPORT CAP PER SPM 6-70-1. 2 L 7 2 4F A6WE 2001042000171 20010420 00171 WP 2001 4 20 EIA2001082 1 20010228 A 5321 FLOOR PANEL DOUG DC9 DC933F 302207A WP CABIN CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND FLOOR PANEL NR 33 FROM FS 503-775 LBL 38 TO LBL 45 DOUBLER AND SEVERAL FASTENERS CRACKED. REPAIRED FLOO R PANEL PER ECRA 933-53-091-2. (M) 2 L 7 2 4F A6WE 2001042000172 20010420 00172 WP 2001 4 20 EIA2001080 1 20010228 A 5532 59121665 FAIRING DOUG DC9 DC933F 302207A WP ELEVATOR DELAMINATED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND RIGHT ELEVATOR BOTTOM FAIRING WORN WITH DELAMINATION PRESENT AND RIVETS POPPED. METAL AND METAL LAMINAT ED HOT BOND REPAIR MADE PER ECRA 933-55-080-2 REV A AND DC9 SRM 51-70-2 PAGE 183. (M) 2 L 7 2 4F A6WE 2001042000173 20010420 00173 WP 2001 4 20 EIA2001079 1 20010228 A 5320 5912995504 PAN DOUG DC9 DC933F 302207A WP FUSELAGE GOUGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND SEVEN GOUGES IN EMERGENCY EXIT PAN FS 658-680 L15R TO L16R. REPLACED EMERGENCY EXIT PAN PER DC9 SRM 51- 10-4 PAGE 1-24 AND 51-30-2 PAGE 1-14. (M) 2 L 7 2 4F A6WE 2001042000174 20010420 00174 WP 2001 4 20 EIA2001076 1 20010228 A 5320 INTERCOSTAL DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND MAIN CABIN FS 155 RIGHT L12R INTERCOSTAL CRACKED. REPAIRED INTERCOSTAL PER ECRA 933-53-099-2. (M) 2 L 7 2 4F A6WE 2001042000175 20010420 00175 WP 2001 4 20 EIA2001075 1 20010228 A 5532 FAIRING DOUG DC9 DC933F 302207A WP ELEVATOR DELAMINATED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND LEFT ELEVATOR BOTTOM FAIRING WORN, DELAMINATION PRESENT, RIVETS POPPED AND FINGER DOUBLERS PEELING UP. METAL AND METAL LAMINATED HOT BOND REPAIR MADE PER ECRA 933-55-080-2. (M) 2 L 7 2 4F A6WE 2001042000176 20010420 00176 WP 2001 4 20 EIA2001074 1 20010228 A 5330 SKIN DOUG DC9 DC933F 302207A WP FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND FS 370 AND FS 427 L29R TO L30R, TWO AREAS OF PITTING CORROSION ON SKIN. BOTH AREAS BLENDED AND OUT LIMI TS WITH VISIBLE PITTING CORROSION STILL PRESENT. REPAIRED SKIN PER ECRA 933-53-105-2. (M) 2 L 7 2 4F A6WE 2001042000177 20010420 00177 WP 2001 4 20 EIA2001073 1 20010228 A 5311 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND FS 39 TO FS 45 RBL 18 CORRODED ON RIGHT OUTBOARD NOSE GEAR WHEEL WELL CUTOUT FRAME. REPAIRED FRAME PER ECRA 933-53-056-2. (M) 2 L 7 2 4F A6WE 2001042000178 20010420 00178 WP 2001 4 20 EIA2001072 1 20010228 A 5311 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND FS 44-48 LBL 18 CORROSION ON LEFT OUTBOARD NOSE GEAR WHEEL WELL CUTOUT FRAME. REPAIRED FRAME PER ECRA 9 33-53-056-2. (M) 2 L 7 2 4F A6WE 2001042000179 20010420 00179 WP 2001 4 20 EIA2001071 1 20010228 A 5320 59105373 WEB DOUG DC9 DC933F 302207A WP FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND FS 658-680 RIGHT CORROSION ON WEB P/N 5910537-3 AT LOWER AFT EMERGENCY EXIT. REPLACED WEB PER SRM 53-01 , 51-10-4, 51-10-3 AND 51-30-2. (M) 2 L 7 2 4F A6WE 2001042000180 20010420 00180 WP 2001 4 20 EIA2001070 1 20010228 A 5330 SKIN DOUG DC9 DC933F 302207A WP FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND NOSE WHEEL WELL FS 58 TO FS 69 RIGHT CORROSION PITTING IN SKIN. REPAIRED SKIN PER ECRA 933-53-093-2. ( M) 2 L 7 2 4F A6WE 2001042000181 20010420 00181 WP 2001 4 20 EIA2001069 1 20010228 A 5311 9923407501N FRAME DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND FS 658 LEFT L8L-18L FRAME CRACKED AT LOWER END OUTBOARD FLANGE JUST ABOVE CENTER TANK. REPLACED FS 658 LEFT FRAME PER SRM 51-30-5 AND 51-30-2. (M) 2 L 7 2 4F A6WE 2001042000182 20010420 00182 WP 2001 4 20 EIA2001066 1 20010228 A 5320 WEB DOUG DC9 DC933F 302207A WP FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND CORROSION ON CUSP WEB LOWER SURFACE UNDER NUTPLATES FOR LBL 54.5 SEAT TRACK FLANGE BOLTS FS 699-718. RE PLACED CUSP WEB PER EO 53-DC9-978-00 REV B. (M) 2 L 7 2 4F A6WE 2001042000183 20010420 00183 WP 2001 4 20 GTIA010038 1 20010212 A 3350 60030431 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 603CA 49508 ACY - FOUND EMERGENCY LIGHTING BATTERY POWER SUPPLY IN ENTRANCE FORWARD GALLEY INOPERATIVE. REMOVED AND REPLACED EMERGE NCY LIGHTING POWER SUPPLY IN FORWARD GALLEY ENTRANCE WAY IAW MD-80 33-50. OPS CHECK NORMAL. (M) 2 L 7 2 4F A6WE 2001042000184 20010420 00184 NE 2001 4 20 GTIA010048 2 20010202 A 7200 ENGINE DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217A 52053 NE RT ENGINE FAILED A GTIA O OTHER J Y WARNING INDICATION ENGINE STOPPAGE NR NOT REPORTED 1 GL 23 806NK 48051 696424 PBI - FLT 509 - RIGHT ENGINE FAILED. THE RIGHT OIL STRAINER CLOGGING LIGHT CAME ON. ALL INDICATIONS WERE NORMAL. REF MM 71-00, TASK-CARD NR 0191, INSTALLED SERVICEABLE ENGINE. (M) 2 L 7 2 4F 4 F A6WE E9NE 2001042000185 20010420 00185 WP 2001 4 20 TWAA0105505 1 20010323 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 906TW 49160 DURING CHECK-C MAINT IN FWD CARGO COMPT FOUND CORROSION AT LONGERON 29R, STA 352 TO 360. INSTALLED NEW LONGERON PER SPM 6-70-01. INSTALLED SPLICE PER SRM 53-02, FIG 18. INSTALLED FASTENERS PER SRM 51-30-03. PRIMED AND PAINTED PER SRM 51 -10-3. 2 L 7 2 4F A6WE 2001042000202 20010420 00202 EA 2001 4 20 COMA0160340 1 20010326 A 5320 60034017373 ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 943CA 7062 VERTICAL J-ANGLE CLIP INSIDE CBP1 AT LBL 9 IS CRACKED. REPAIRED IAW WVAC EO 601R-53-2337A. 2 L 7 2 4F RT A21EA 2001042000208 20010420 00208 NM 2001 4 20 QXEA0100410 1 20010313 A 5280 BRACKET DHAV DHC8 DHC8102 2809003 NM RT MLG CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-NACELLE WHEEL WELL RIGHT HAND AT STATION 240.76 AFT DOOR ACTUATOR BRACKET IS CHAFED AND HAS RTV HANGING OFF. REPAIR ED IAW HORIZON AIR EA 9-54-283. 2 H 7 2 4T RT A13NM 2001042000233 20010420 00233 EA 2001 4 20 COMA0160339 1 20010326 A 5320 601R31171 ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 943CA 7062 THE ANGLES AT RBL 27 AND LBL 27 AND INTERCOSTALS AT BL 36 (LT AND RT) AT FS 484 ARE CRACKED. REPAIRED LEFT AND RIGHT AN GLES AT RBL 27 AND LBL 27 INTERCOSTAL AT BL/36 (LEFT AND RIGHT) AT FS 484 IAW WVAC EO 601R-53-2334B. 2 L 7 2 4F RT A21EA 2001042000236 20010420 00236 NM 2001 4 20 QXEA0100411 1 20010322 A 5414 RIVET DHAV DHC8 DHC8102 2809003 NM RT NACELLE LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-RIGHT NACELLE HAS FOUR LOOSE RIVETS BOTTOM OUTBOARD OF OIL COOLER. REPAIRED IAW HORIZON AIR EA 9-54-290A AND DHC-8 RD-8-54-057. 2 H 7 2 4T RT A13NM 2001042000237 20010420 00237 NM 2001 4 20 QXEA0100412 1 20010316 A 5411 RIB DHAV DHC8 DHC8102 2809003 NM RT NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-RIGHT NACELLE OUTBOARD STIFFENER/RIB CHAFED IN TWO AREAS XN141.95 AND ZN18.0. REPAIRED IAW HORIZON AIR EA 9-54-287 AND DHC-8 SRM 53-00-16, PAGE 4. 2 H 7 2 4T RT A13NM 2001042000238 20010420 00238 NM 2001 4 20 QXEA0100413 1 20010316 A 5411 RIB DHAV DHC8 DHC8102 2809003 NM RT NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-RIGHT NACELLE OUTBOARD STIFFENER/RIB CHAFED AT XN137.35 AND ZN17.0. REPAIRED IAW HORIZON AIR EA 9-54-288 AND DHC-8 SRM 51-20-11. 2 H 7 2 4T RT A13NM 2001042000239 20010420 00239 NM 2001 4 20 QXEA0100415 1 20010321 A 5220 STOP DHAV DHC8 DHC8102 2809003 NM EMERGENCY EXIT WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-RIGHT HAND FORWARD EMERGENCY EXIT DOOR STOPS HAVE STEP WEAR. REPAIRED IAW DHC-8 RD-8-52-349. 2 H 7 2 4T RT A13NM 2001042000244 20010420 00244 NM 2001 4 20 QXEA0100416 1 20010317 A 5230 FRAME DHAV DHC8 DHC8102 2809003 NM CARGO DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-CHAFE DAMAGE TO FRAME FOR SEAL RETAINER ON BAGGAGE DOOR AT X597.0 AFT SIDE OF DOOR. REPAIRED IAW DHC-8 SRM 51-20-31 AND HORIZON AIR EA 9-52-115. 2 H 7 2 4T RT A13NM 2001042000245 20010420 00245 NM 2001 4 20 QXEA0100386 1 20010309 A 5313 RIVET DHAV DHC8 DHC8102 2809003 NM STRINGER MISSING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-2 RIVETS MISSING AT RIGHT HAND STRINGER 32 AND FRAME CLIP STATION 426. REPAIRED IAW DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2001042000246 20010420 00246 NM 2001 4 20 QXEA0100387 1 20010308 A 3220 LANDING GEAR DHAV DHC8 DHC8102 2809003 NM NLG GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-NOSE LANDING GEAR LOWER MEMBER FORWARD FACE IS GOUGED AT Z70.00. REPAIRED IAW DHC-8 RD8-32-289. 2 H 7 2 4T RT A13NM 2001042000247 20010420 00247 NM 2001 4 20 QXEA0100389 1 20010316 A 5280 SPACER DHAV DHC8 DHC8102 2809003 NM NLG MISSING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-RIGHT HAND FORWARD NOSE LANDING GEAR DOOR SPRING HAS SPACERS MISSING AT DOOR BRACKET ATTACH POINT. REPAIRED IAW DHC -8 SRM 32-20-21, PAGE 205 AND SRM 32-30-00, PAGE 204. 2 H 7 2 4T RT A13NM 2001042000248 20010420 00248 NM 2001 4 20 QXEA0100390 1 20010319 A 5320 FLOOR SUPPORT DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-CORROSION ON SUPPORT STRUCURE FOR FLOOR PANEL 131C8 ON THE MOST OUTBOARD SECTION OF SUPPORT STRUCTURE, AROUND THE NU T PLATE HOLE. REPAIRED IAW DHC-8 RD8-53-832 AND HORIZON AIR EA 9-53-613. 2 H 7 2 4T RT A13NM 2001042000249 20010420 00249 NM 2001 4 20 QXEA0100391 1 20010314 A 5321 SKIN DHAV DHC8 DHC8102 2809003 NM FLOORBOARD CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-CORROSION ON TOP AND BOTTOM OF FLOORBOARD SKIN AT 2 NUT PLATES, STATION 599, WL100. REPAIRED IAW DHC-8 SRM 51-20-16 , SRM 51-20-36 AND SRM 51-40-00. 2 H 7 2 4T RT A13NM 2001042000256 20010420 00256 NM 2001 4 20 QXEA0100394 1 20010313 A 7603 CONTROL CABLE DHAV DHC8 DHC8102 2809003 NM NR 1 ENGINE BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX- NR 1 ENGINE POWER CONTROL CABLE HAS A BROKEN STRAND JUST FORWARD OF PULLEY. REPAIRED IAW DHC-8 SRM 76-10-14, PAGE 211. 2 H 7 2 4T RT A13NM 2001042000257 20010420 00257 NM 2001 4 20 QXEA0100396 1 20010314 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-DUE TO THE MULTIPLE WRITE-UPS ON SEAT TRACK NR 4 REQUIRES REPLACEMENT. REPAIRED IAW DHC-8 SRM 51-40-00, SRM 51-40-1 1, AND RD-8-53-3403. 2 H 7 2 4T RT A13NM 2001042000258 20010420 00258 NM 2001 4 20 QXEA0100398 1 20010316 A 5240 SKIN DHAV DHC8 DHC8102 2809003 NM SERVICE DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-RIGHT HAND FORWARD SERVICE EMERGENCY DOOR DENTED AT STATION Z143.00 AND X262.00, AFT OF DOOR WINDOW. REPAIRED IAW H ORIZON AIR EA 9-52-114. 2 H 7 2 4T RT A13NM 2001042000259 20010420 00259 NM 2001 4 20 QXEA0100399 1 20010315 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-NR 7 SEAT TRACK RIGHT HAND INBOARD STATION 182-424 REQUIRES REMOVAL DUE TO MULTIPLE WRITE-UPS. REPAIRED IAW HORIZON AIR EA 9-53-612 AND DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2001042000260 20010420 00260 NM 2001 4 20 QXEA0100400 1 20010314 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-CORROSION .024 INCH REMOVED FROM BOTTOM OF SEAT TRACK AFT OF STATION 467. RIGHT HAND OUTBOARD SEAT TRACK CORROSION OUT OF LIMITS. REPAIRED IAW DHC-8 SRM 51-40-11 AND RD-8-53-1102. 2 H 7 2 4T RT A13NM 2001042000261 20010420 00261 NM 2001 4 20 QXEA0100395 1 20010313 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-PITTING CORROSION ON LEFT HAND OUTBOARD SEAT TRACK STATION 370. REPAIRED IAW DHC-8 SRM 51-40-11 AND RD-8-53-1102. 2 H 7 2 4T RT A13NM 2001042000267 20010420 00267 NM 2001 4 20 AWXA0001549 1 20010327 A 5311 6546538552 FRAME BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 FUSELAGE FRAME CRACKED IN RADIUS AFT SIDE AT FS 597 RBL 65 WL 206. REPLACED FRAME IAW B737-200 SRM 51-30-2 PG 2. 2 L 7 2 4F RT A16WE 2001042000268 20010420 00268 NM 2001 4 20 AWXA0001550 1 20010327 A 5312 65163007 BULKHEAD BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 CRACK IN 178 BLKHD WEB AT LBL 11.5 WL 218.5 BENEATH U-CHANNEL REINFORCEMENT. REPAIRED CRACK IAW B737-200 SRM 53-10-11 F IG 1 PG 1-4 & 6. 2 L 7 2 4F RT A16WE 2001042000274 20010420 00274 NM 2001 4 20 AWXA0001551 1 20010327 A 5240 143N61004 SKIN BOEING 757 7572S7 1384962 NM L2 DOOR DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 905AW 23567 L2 DOOR FWD LWR CORNER EDGE SKIN HAS 2 DENTS. CUT OUT DAMAGED SKIN, NDT - NO CRACKS. FABBED DOUBLER AND FILLER IAW SRM 52-10-01; INSTALLED REPAIR PARTS IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2001042000275 20010420 00275 NM 2001 4 20 AWXA0001553 1 20010327 A 5313 143N3110 STRINGER BOEING 757 7572S7 1384962 NM FUSELAGE DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 905AW 23567 AFTER REMOVING DOUBLER AT STA 626 STR 16L, FOUND STR 16L DENTED. CUT OUT DAMAGE; FABBED AND INSTALLED REPAIR SPLICE IAW SRM 53-00-03 FIG 201. 2 L 7 2 4F RT A2NM 2001042000276 20010420 00276 NM 2001 4 20 AWXA0001554 1 20010327 A 5330 143N33208 SKIN BOEING 757 7572S7 1384962 NM FUSELAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 905AW 23567 DAMAGED RIVETS AND SKIN FWD OF L2 DOOR FS 620-640. CUT OUT DAMAGE AND REPAIRED IAW SRM 53-00-01 FIG 204, SRM 51-40-02. 2 L 7 2 4F RT A2NM 2001042000277 20010420 00277 NM 2001 4 20 AWXA0001555 1 20010327 A 5240 146N6130 SKIN BOEING 757 7572S7 1384962 NM R4 DOOR WRINKLED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 905AW 23567 R4 DOOR SKIN EDGE WRINKLED AT FWD LWR CORNER. CUT OUT DAMAGED AREA, NDT - NO CRACKS. FABBED AND INSTALLED FILLER AND D OUBLER IAW SRM 52-10-01. 2 L 7 2 4F RT A2NM 2001042000278 20010420 00278 NM 2001 4 20 AWXA0001556 1 20010327 A 5320 146N5391 FITTING BOEING 757 7572S7 1384962 NM CARGO BAY CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 905AW 23567 AFT CARGO COMPARTMENT ANCHOR FITTING AT FS 1380 LBL 23 HAS EXFOLIATION CORROSION AROUND FITTING. REMOVED STRUCTURE TO G AIN ACCESS TO REPAIR AREA IAW SRM 51-40-02; REMOVED DMGD SECTION OF SIDE PANEL; FABBED REPAIR SECTION AND REPAIR DOUBLER ; INSTALLED PARTS IAW SRM 51-70-13; INSTALLED ACCESS STRUCTURE IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2001042000279 20010420 00279 NM 2001 4 20 AWXA0001557 1 20010327 A 5410 311N50418 ATTACH ANGLE BOEING 757 7572S7 1384962 NM NR 2 PYLON CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 905AW 23567 NR 2 PYLON AFT BLKHD ATTACH ANGLE IS CRACKED AT PP STA 200. REMOVED ANGLE IAW SRM 51-40-02; FABBED REPLACEMENT ANGLE IA W DWG 311N5041; INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2001042000280 20010420 00280 NM 2001 4 20 AWXA0001559 1 20010327 A 5320 143N3370 FLOOR SUPPORT BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 905AW 23567 FWD CARGO COMPARTMENT FLOOR SUPPORT BEAM AT FS 543 AND LBL 8 IS DENTED AND CRACKED. REMOVED DAMAGED AREA; FABBED REPAIR ANGLE AND 1 FLOOR SUPPORT IAW SRM 51-70-12 AND 53-30-53; TREATED AND PRIMED REPAIR PARTS; INSTALLED REPAIR ANGLE AND RE PLACEMENT SUPPORT IAW SRM 51-70-12 AND 51-40-02. 2 L 7 2 4F RT A2NM 2001042000281 20010420 00281 NM 2001 4 20 AWXA0001560 1 20010327 A 5320 146N8722 BRACKET BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 905AW 23567 CABIN STA 1671 RBL 65 DOOR SILL ANGLE BRACKET HAS CORROSION. REMOVED CORROSION - FOUND OUT OF LIMITS; CUT OUT DAMAGE; F ABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-70-13. 2 L 7 2 4F RT A2NM 2001042000283 20010420 00283 EU 2001 4 20 QXEA0100421 1 20010326 A 3350 5515800106 LENS FOKKER F28 F28MK4000 4990810 EU EXIT SIGN BROKEN A QXEA K NONE O OTHER NR NOT REPORTED 1 NM 09 475AU 11222 SEA - FORWARD OVERHEAD EXIT SIGN FOUND TO HAVE A BROKEN LENS COVER. REMOVED AND REPLACED EXIT SIGN ASSEMBLY. OPERATION AL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001042000284 20010420 00284 EU 2001 4 20 QXEA0100422 1 20010320 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN DEFECTIVE A QXEA K NONE O OTHER NR NOT REPORTED 1 NM 09 478US 11227 PDX - FORWARD CABIN EXIT SIGN WAS REPORTED DIM. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RET URNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001042000285 20010420 00285 WP 2001 4 20 EIA2001099 1 20010228 A 5311 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND FS 90 LEFT FORWARD BULKHEAD FRAME CORRODED UNDER F/O SIDE CONSOLE AREA. REPAIRED FRAME PER ECRA 933-53- 092-2. (M) 2 L 7 2 4F A6WE 2001042000286 20010420 00286 WP 2001 4 20 EIA2001090 1 20010228 A 5315 FLOORBEAM DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND FS 389 RBL 53 FLOORBEAM UPPER CHORD CRACKED. REPAIRED FLOORBEAM PER ECRA 933-53-102-2. (M) 2 L 7 2 4F A6WE 2001042000287 20010420 00287 WP 2001 4 20 EIA2001081 1 20010228 A 5330 592176469 SKIN DOUG DC9 DC933F 302207A WP FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND GASH IN SKIN TWO PLACES 1 INCH BY .4 INCH AND 2.3 INCH BY .3 INCH AT FS 301, L18L LOWER FORWARD CORNER O F MAIN CARGO DOOR OPENING. REPAIRED SKIN PER ECRA 933-53-051-2. (M) 2 L 7 2 4F A6WE 2001042000288 20010420 00288 SO 2001 4 20 SWIA972445 1 20010306 A 2720 RUDDER PEDAL EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT BINDING A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 187SW 120037 RIGHT RUDDER PEDAL BINDS AND IS NOISY WITH FORWARD MOVEMENT. APPLIED LUBRICANT TO RUDDER TRIM ACTUATOR CLUTCH MECHANISM . OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042300001 20010423 00001 NM 2001 4 23 01FDEA00190 1 20010314 A 5310 BAC14902770 SHEAR TIE BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 CORROSION (SPEC C53-111-01,3) ON FRAME SHEAR TIE BS AT BS 950D BETWEEN STR 29L AND STR 28L. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-10-1 FIG 1, 53-10-4 FIG 15. 2 L 7 3 4F RT A3WE 2001042300002 20010423 00002 NM 2001 4 23 01FDEA00205 1 20010314 A 5710 ARB2850502 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 603FE 48459 RT WING L/E STA XFS 1004, NR 16 SLAT TRACK SUPPORT FITTING CRACKED. *S/D* REMOVED AND REPLACED PER DWG ARB2850. 2 L 7 3 4F RT A22WE 2001042300003 20010423 00003 NM 2001 4 23 01FDEA00214 1 20010319 A 5330 65184201 SKIN BOEING 727 727233 138408A NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 A TEMPORARY REPAIR IS INSTALLED ON FUSELAGE AT BS 216, STR 17R. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-30-3 FIG 5 . 2 L 7 3 4F RT A3WE 2001042300004 20010423 00004 NM 2001 4 23 01FDEA00216 1 20010319 A 5330 6572702 SKIN BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 CORROSION (C53-111-01, 2) ON SKIN UNDER LEVELING COMPOUND BS 684 O/B OF STR 27R. *S/D* REMOVED AND REPLACED PER IAW FE DEX SRM 53-30-3 FIG 3. 2 L 7 3 4F RT A3WE 2001042300005 20010423 00005 NM 2001 4 23 01FDEA00233 1 20010326 A 5320 65861851 WEB BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 CORROSION (C53-132-01, -1) BS 850, WL 162, LBL 10. *S/D* REMOVED AND REPLACED PER FEDEX SRM 51-10-2, 51-30-2 AND 51-30 -5. ALODINED, PRIMED AND PAINTED PER FEDEX PER MM 51-21-152. 2 L 7 3 4F RT A3WE 2001042300006 20010423 00006 NM 2001 4 23 AWXA0001547 1 20010327 A 2760 WARNING SYSTEM BOEING 757 7572G7 1384963 NM COCKPIT ACTIVATED A AWXA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 WP 28 909AW 24522 D: PHX - AIR TURNBACK - 3/26/01 - IN FLIGHT EICAS SPOILERS DISPLAYED WITH SPOILERS DOWN; AILERON DISPLACEMENT OBSERVED A S FLAPS RETRACTED AND THEN EXTENDED FOR LANDING; FLAPS 20 USED FOR LANDING. ON DEBRIEF OF FLIGHT CREW, REPORTED LEFT WI NG HEAVY. MAINTENANCE VISUALLY INSPECTED FLAPS AND SPOILERS - NO DEFECTS NOTED. TROUBLESHOT IAW FIM 27-09-00 FIG 105; SCM 3R FAULTS PCA FAULT; RESET THE FAULTBALL AND OPERATED THE SPOILERS AND FAULT DID NOT RETURN. AS A PRECAUTION MEL 27 -61-1 CONDITION 1 WAS APPLIED AND SPOILERS 4 AND 9 DEACTIVATED IN THE DOWN POSITION. 2 L 7 2 4F RT A2NM 2001042300007 20010423 00007 NM 2001 4 23 AWXA0001548 1 20010327 A 2910 BACV10CD2 CHECK VALVE BOEING 737 7373G7 1384595 NM NLG FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 157AW 23779 ORD - AIR TURNBACK - 3/26/01 - AFTER TAKEOFF ON LANDING GEAR RETRACTION THE NOSE LANDING GEAR WOULD NOT RETRACT AND THE AIRCRAFT RETURNED TO ORD MAKING AN UNEVENTFUL LANDING. THE AIRCRAFT WAS MAINTENANCE FERRIED TO PHX. MAINTENANCE TROUBL ESHOT AND FOUND A NOSE GEAR UP HYDRAULIC LINE CHECK VALVE FAILED. MAINTENANCE REPLACED BOTH NOSE LANDING GEAR UP LINE C HECK VALVES AND GEAR RETRACT TEST WAS NORMAL. 2 L 7 2 4F RT A16WE 2001042300008 20010423 00008 EU 2001 4 23 QXEA0100420 1 20010321 A 3220 200725001 LANDING GEAR FOKKER F28 F28MK4000 4990810 EU NLG FAILED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 482US 1456 1456 11231 YEG - ON GEAR EXTENTION, NOSE LANDING GEAR INDICATED NOT DOWN AND LOCKED. CYCLED GEAR, ALL INDICATION NORMAL. REMOVED AND REPLACED NOSE LANDING GEAR ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001042300009 20010423 00009 SO 2001 4 23 SWIA972446 1 20010305 A 3030 ANTI-ICE SYSTEM EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT AOA FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 579SW 120347 LEFT AOA HEAT FAILS IN FLIGHT, EVERY 5 TO 15 SECONDS. RETURNED TO LAX. INSTALLED NEW AOA RELAYS K0185 AND K0187. RAN FOR 20 MINUTES. OPS CHECK GOOD ON GROUND AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042300010 20010423 00010 SO 2001 4 23 SWIA972447 1 20010306 A 5230 DOOR SEAL EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CARGO BAY UNSECURE A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 298SW 120328 AFTER DEPARTURE FROM BOI CLIMBING THROUGH 20,000 FEET LOST PRESSURIZATION. FLIGHT ATTENDANT HEARD LOUD NOISE COMING FRO M CARGO AREA. RETURNED TO BOI. FOUND CARGO DOOR SEAL NOT SECURED. INSTALLED SEAL IAW MM 52-30-01. PRESSURIZATION CHE CK OK. OK FOR SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042300011 20010423 00011 SO 2001 4 23 SWIA972448 1 20010306 A 5270 SWITCH EMB 120 EMB120RT SO PWA 118 PW118 NE CARGO DOOR OUT OF ADJ A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 156CA 120156 CARGO DOOR OPEN INDICATIONS ON CLIMBOUT, RED LIGHT ON MAP AND TRIPLE CHIME. RETURNED TO SEA. ADJUSTED CARGO DOOR MICRO SWITCH. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042300012 20010423 00012 SO 2001 4 23 SWIA972449 1 20010316 A 2731 SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE ELEVATOR FAILED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 204SW 120243 RECEIVED TRIM AURAL WARNING ON TAKEOFF ROLL WITH TRIM SET AT 35 PERCENT. ABORTED TAKEOFF. REPLACED RIGHT ELEVATOR PROP SWITCH IAW 27-32-05. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042300013 20010423 00013 EA 2001 4 23 SWIA972450 1 20010322 A 2760 SPOILER CNDAIR CL600 CL6002B19 EA LT WING OUT OF RIG A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 413SW 7102 TAKEOFF CONFIG OK ADVISORY NOT ON. AT 70 PERCENT THRUST TAKEOFF CONFIG SPOILERS WARNING COMES ON. ABORTED TAKEOFF. AD JUSTED RIGGING ON LEFT OUTBOARD FLIGHT SPOILER OUTBOARD PCU IAW MM 27-62-01. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2001042300014 20010423 00014 SO 2001 4 23 SWIA972451 1 20010323 A 2910 TUBE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE HYD SYSTEM BROKEN A SWIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 07 187SW 120037 LEFT HYDRAULIC SYSTEM (GREEN) LOW RESERVOIR PRESSURE, LOW LEVEL, MAIN PUMP LOW PRESS LIGHTS ON. RETURNED TO SLC REPAIRE D BROKEN MAIN HYDRAULIC PUMP PRESSURE TUBE AT LEFT HYDRAULIC COMPARTMENT FIRE WALL IAW EMB 120 MM 20-10-04. OPS AND LEA K CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042300015 20010423 00015 EA 2001 4 23 SWIA972452 1 20010323 A 3610 COUPLING CNDAIR CL600 CL6002B19 EA BLEED AIR LOOSE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 405SW 7029 LEFT 14TH DUCT WARNING ILLUMINATED AFTER TAKEOFF. FOLLOWED QRH RETURNED TO AIRPORT FOR LANDING. RAN THE LEFT ENGINE AN D FOUND THE LEFT 14TH STAGE PYLON SECTION BLEED AIR TUBE FORWARD CHECK BAND COUPLING LOOSE. TIGHTENED CLAMP RAN ENGINE IAW MM 21-00-00. BLEED AIR TUBE LEAK CHECKS GOOD IAW MM 30-20-01. RAN ENGINE FOR 30MINS WITH NO 14TH DUCT WARNING MES SAGE NOTED. 2 L 7 2 4F RT A21EA 2001042300016 20010423 00016 2001 4 23 SWIA972453 4 20010324 A 3425 INDICATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT FAILED A SWIA A UNSCHED LANDING I J FLT. ATTITUDE INST. WARNING INDICATION CL CLIMB 1 NM 07 292SW 120319 CAPTAIN HDG 70 DEGREES FROM FO EHSI FAIL AND HDG FLAGS DISPLAYED AS WELL AS COMP FLAG CAPTAIN ADI AND FAIL FLAG FO RMI 2 /23/01. RETURNED TO FAT. COULD NOT DUPLICATE COMPLAINT. REPLACED K0395 AND K0397 TO TROUBLESHOOTING. SYSTEM OP CHECK S GOOD IAW MM 34-21-00. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042300017 20010423 00017 SO 2001 4 23 SWIA972454 1 20010325 A 2731 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE ELEVATOR TRIM DEFECTIVE A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 586SW 120354 DURING FLIGHT TRIM JUMPS AND AIRCRAFT PITCH ATTITUDE CHANGES ABRUPTLY. HAPPEN WITH AP ON EITHER SIDE. AT FREEZING TEM PERATURES, TRIM WHEEL IS VERY DIFFICULT TO MOVE. ON GROUND AND WARMER TEMPS IT MOVES FREELY. REMOVED AND REPLACED ELEV ATOR TRIM ACTUATORS ON LEFT AND RIGHT SIDES WITH SERVICEABLE UNITS IAW MM 27-32-02. P/N ON RIGHT 5299-1, S/N ON 043330, S/N OFF 834, P/N ON LEFT 5299-1, S/N ON 830, S/N OFF 734. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042300018 20010423 00018 SO 2001 4 23 SWIA972455 1 20010325 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FLAP FAULTY A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 186SW 120034 INTERMITTENT CONTROL FAULT FOR ALMOST THE ENTIRE FLIGHT, OUTBOARD FLAP INDICATING FLASHING. REMOVED AND REPLACED LEFT O UTBOARD FLAP ACTUATOR PER MM 27-50-09 AND RII 27-307. OPS CHECKS GOOD, NO LEAKS. P/N ON 320300-1007, S/N ON 0864, S/N OFF 0552. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042300019 20010423 00019 NM 2001 4 23 SCNA01318 1 20010321 A 5320 FLOOR SUPPORT BOEING 727 7272J4 1384006 NM FUSELAGE CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 290SC 20764 DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON FLOOR SUPPORT AT STA 1070 THROUGH 1090 LBL 12. REMOVED CORROSION IAW B727 SRM 511006. REMOVED FLOOR SUPPORT IAW B727 SRM 513002. FABRICATED NEW FLOOR SUPPORT FROM B AC 15064417 7075 T6. TREATED AND PRIMED IAW B727 SRM 511002 AND MM 512002. INSTALLED IAW B727 SRM 513002. 2 L 7 3 4F RT A3WE 2001042300020 20010423 00020 NM 2001 4 23 F3LA200100049 1 20010326 A 2120 65841571 MANIFOLD BOEING 737 737317 138447P NM COCKPIT BROKEN A F3LA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 EICHH 282 23177 DURING FLIGHT FROM LAX TO DEN, FLIGHT CREW REPORTED SPARKS, ARCING AND SMOKE COMING FROM BEHIND CAPTAIN''S INSTRUMENT PA NEL. AIRCRAFT DIVERTED TO LAS AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE CAPTAIN''S INSTRUMENT COOLING MANIFOL D BROKEN AND THE COOLING AIR DUCT INSULATION CHAFED, WHICH EXPOSED THE METAL DUCT AND CREATED A SHORT. AN INTERIM REPAI R WAS ACCOMPLISHED PER EA 21-737-009 AND RW 258 WAS ISSUED TO REPLACE THE MANIFOLD AND THE DUCT AT THE NEXT C-CHECK. 2 L 7 2 4F RT A16WE 2001042300021 20010423 00021 SO 2001 4 23 C2XA01CL067 1 20010324 A 3250 CONTROL UNIT EMB 145 EMB145LR SO NLG OUT OF ADJ A C2XA K NONE O OTHER LD LANDING 1 SW 27 19966 145131 PIT FLIGHT 4141 ON LANDING IN PITT THE AIRCRAFT SKIDDED OFF THE RUNWAY. MAINTENANCE INSPECTED AIRCRAFT FOR DAMAGE AND N O DAMAGE WAS FOUND. MAINTENANCE ALSO FOUND THE AIRCRAFT WAS PULLING TO THE RIGHT ON TAXI. FOUND THE STEERING CONTROL W HEEL WAS OFF 7 DEGREES. THE NOSEWHEEL STEERING TILLER WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. THE STEERING CONT ROL MODULE AND STEERING MANIFOLD WERE REPLACED FOR PRECAUTIONARY REASONS. 2 L 7 2 4T RT T00011AT 2001042300022 20010423 00022 WP 2001 4 23 ARWA0010308 1 20010323 A 3241 WARNING LIGHT DOUG DC8 DC863F 302198F WP COCKPIT ERRATIC A ARWA D RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 19 661AV 45969 ABORT TAKEOFF BELOW IAS AT BGI DUE THE ANTI-SKID LIGHT FLICKERING ON/OUT. FOLLOW CHECKLIST FOR ATO. CHECKED ANTI-SKID SYSTEM, CONTROL MONITOR, AND RESET ANTI-SKID SWITCH. LIGHT CHECK NORMAL. COULD NOT DUPLICATE, CONTINUE WITH SCHEDULE D EPARTURE WITHOUT FURTHER PROBLEM. 2 L 7 4 4F 4A25 2001042300023 20010423 00023 CE 2001 4 23 C2XA01CL068 1 20010328 A 2910 LINE BEECH 1900 1900D 1154162 CE HYD SYSTEM LOOSE A C2XA K NONE O OTHER CL CLIMB 1 SW 27 87557 UE246 CLE FLIGHT 3032 THE CREW REPORTED AFTER TAKEOFF THE LANDING GEAR RELAY CIRCUIT BREAKER POPPED. MAINTENANCE INSPECTED AN D TIGHTENED THE PRESSURE LINE ON THE LANDING GEAR ACCUMULATOR AND SERVICED THE HYDRAULIC SYSTEM. OPERATIONAL CHECKS WER E GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT A24CE 2001042300024 20010423 00024 EU 2001 4 23 RAIA00103017 1 20010326 A 3241 CONTROL BOX JETAIR JETSTM JETSTM4101 1500501 EU ANTI- SKID FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 555HK 41072 5358-EWR-DURING TAXI IN LEFT HAND MAIN LANDING GEAR BRAKES LOCKED UP DUE TO ANTI-SKID FAILURE NR 1 MAIN TIRE IS FLAT. M AINTENANCE REMOVED AN REPLACED NR 1 AND 2 MAIN LANDING GEAR TIRE IAW J41 MAINTENANCE MANUAL. 2 L 7 2 4T RT A41NM 2001042300025 20010423 00025 NM 2001 4 23 F3LA200100050 1 20010327 A 5753 69378536 ATTACH FITTING BOEING BOEING 737 7372Y5 1384554 NM FOREFLAP BROKEN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 921WA 119 652 23039 DURING A-CHECK, MAINTENANCE REPORTED LT WING OTBD FOREFLAP OTBD ATTACH LINK BROKEN. REPLACED LT WING OTBD FOREFLAP. 2 L 7 2 4U RT A16WE 2001042300026 20010423 00026 NM 2001 4 23 AWXA0001561 1 20010327 A 5320 146N5318 FLOOR SUPPORT BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 905AW 23567 CABIN STA 1690-1720 RBL 12 FLOOR BOARD SUPPORT CORRODED. REMOVED, FABBED REPLACEMENT SUPPORT AND INSTALLED REPLACEMENT PART IAW SRM 51-40-02, 51-30-01 AND DWG 146N5180. 2 L 7 2 4F RT A2NM 2001042300027 20010423 00027 NM 2001 4 23 AWXA0001563 1 20010327 A 5330 143N33208 SKIN BOEING 757 7572S7 1384962 NM FUSELAGE DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 905AW 23567 DENT IN FUSELAGE SKIN AT FS 460 STR 19L .050 DEEP X .50 WIDE OUT OF LIMITS IAW SRM 53-00-01 FIG 101. CUT OUT DAMAGE AND REPAIRED SKIN IAW SRM 53-00-01 FIG 204. 2 L 7 2 4F RT A2NM 2001042300028 20010423 00028 EA 2001 4 23 COMA0160341 1 20010326 A 5320 601R311719 ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 943CA 7062 THE ANGLES AT RBL 27 AND LBL 27 AND INTERCOSTALS AT BL36 (LT AND RT) AT FS 484 ARE CRACKED. REPAIRED LEFT AND RIGHT ANG LES AT RBL 27 AND LBL 27 INTERCOSTALS AT BL/36 (LEFT AND RIGHT) AT FS 484 I/A/W WVAC EO 601R-53-2334A. 2 L 7 2 4F RT A21EA 2001042300029 20010423 00029 EA 2001 4 23 COMA0160343 1 20010324 A 3350 59465 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 969CA 7141 EMERGENCY FLOOR LIGHTS, ROW 2 TO 5, ARE INOPERABLE. REPLACED FLOOR LIGHTS CABLE ASSY. 2 L 7 2 4F RT A21EA 2001042300030 20010423 00030 EA 2001 4 23 COMA0160344 1 20010323 A 2750 FLAP CNDAIR CL600 CL6002B19 EA WING MALFUNCTIONED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 958CA 7111 FLAPS FAIL MESSAGE, FLAPS STUCK AT ZERO. COULD NOT DUPLICATE. C/W INSP OF FLAP SYSTEM PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2001042300031 20010423 00031 EA 2001 4 23 COMA0160345 1 20010323 A 5610 NP1393216 WINDSHIELD CNDAIR CL600 CL6002B19 EA COCKPIT CRACKED A COMA O OTHER O OTHER CR CRUISE 1 SO 01 809CA 2991 7366 COPILOTS WINDSHIELD CRACKED DURING FLIGHT. REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 2001042300032 20010423 00032 EA 2001 4 23 COMA0160346 1 20010323 A 3260 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT ACTIVATED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 982CA 7168 RIGHT MLG DISAGREE WARNING. COULD NOT DUPLICATE. OPERATIONAL CHECKS WERE SATISFACTORY. 2 L 7 2 4F RT A21EA 2001042300033 20010423 00033 EA 2001 4 23 COMA0160347 1 20010323 A 2721 601R5122623 PANEL CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTIONED A COMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 01 991CA 7216 RUDDER TRIM WENT FULL NOSE LEFT UNCOMMANDED. REPLACED THE RUDDER TRIM SWITCH PANEL. 2 L 7 2 4F RT A21EA 2001042300034 20010423 00034 EA 2001 4 23 COMA0160348 1 20010323 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 947CA 7077 EMERGENCY LIGHT AT ROW 5 IS INOPERABLE. REPLACED LIGHT BULB. 2 L 7 2 4F RT A21EA 2001042300035 20010423 00035 WP 2001 4 23 TWAA0105601 1 20010328 A 3350 1315 LIGHT DOUG DC9 DC982 3022082 WP ACCESSORY BAY INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 951U 49245 THE AFT ACCESSORY COMPT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE LAMPS. CHECK-C 9-8-00 STL. 2 L 7 2 4F A6WE 2001042300036 20010423 00036 WP 2001 4 23 TWAA0105602 1 20010328 A 3350 408822101 BATTERY DOUG DC9 DC982 3022082 WP COCKPIT DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 951U 49245 THE COCKPIT EMERGENCY FLOOD LIGHTS WERE INOPERATIVE. REPLACED THE BATTERIES. CHECK-C 9-8-00 STL. 2 L 7 2 4F A6WE 2001042300037 20010423 00037 NE 2001 4 23 TWAA0105603 2 20010328 A 7250 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE RT ENGINE FAILED A TWAA A E UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 CE 05 9304C 49530 1404 DURING CLIMB THE RT ENGINE HAD A COMPRESSOR STALL, LOST ENGINE OIL, AND STARTED TO SPOOL DOWN. THE ENGINE WAS SHUT DOWN AND FLIGHT DIVERTED TO JFK. THE ENGINE WAS CHANGED. CHECK-C 2-5-01 JFK. 2 L 7 2 4F 4 F RT A6WE E9NE 2001042300038 20010423 00038 WP 2001 4 23 TWAA0105604 1 20010327 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 992Z 47095 DURING OP 15 MAINT CHECK FOUND CRACK IN SKIN AT STA 1087, LONGERON 4R. ACCOMP HIGH FREQ EDDY CURRENT AND CONFIRMED .75 INCH CRACK PER 51-00-03 PART 6. REPAIRED PER SRM 53-04, FIG 27. 2 L 7 2 4F A6WE 2001042300039 20010423 00039 WP 2001 4 23 TWAA0105605 1 20010327 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 909TW 49170 DURING CHECK-C MAINT FOUND CORROSION ON FORMER SUPPORT ATTACHED TO LONGERON 29L, AND BETWEEN STA 427 THRU 446. REPLACED FORMER SUPPORT WITH NEW. USED RIVET AND HI-LOK PER SPM 6-70-01, SRM 51-30-5 AND 51-30-2. 2 L 7 2 4F A6WE 2001042300040 20010423 00040 WP 2001 4 23 TWAA0105606 1 20010327 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT IN THE AFT CABIN FOUND CORROSION AND CRACKS IN MEMBRANE AT STA 1174 TO 1250, LBL 45 INCHES. REMOVE D CORROSION AND DAMAGED AREA. MADE DOUBLER REPAIR AND INSTALLED PER SRM 53-01, WEB REPAIR. 2 L 7 2 4F A6WE 2001042300041 20010423 00041 EU 2001 4 23 RAIA00103018 1 20010327 A 3244 AHA1837 TIRE JETAIR JETSTM JETSTM4101 1500501 EU LT MLG BLOWN A RAIA K NONE O OTHER LD LANDING 1 CE 03 555HK 41072 9549-ROC-AIRCRAFT PULLED HARD TO THE LEFT AS IF LEFT HAND MAIN LANDING GEAR TIRES LOCKED UP, AIRCRAFT WAS UNABLE TO TAXI . MAINTENANCE REMOVED AND REPLACED NR 1 MAIN LANDING GEAR WHEEL ASSEMBLY IAW J41 MAINTENANCE MANUAL. 2 L 7 2 4T RT A41NM 2001042300042 20010423 00042 EU 2001 4 23 RAIA00103019 1 20010327 A 3244 AHA1837 TIRE JETAIR JETSTM JETSTM4101 1500501 EU LT MLG BLOWN A RAIA K NONE O OTHER LD LANDING 1 CE 03 555HK 41072 9549-ROC-AIRCRAFT PULLED TO LEFT AS IF LEFT HAND MAIN LANDING GEAR TIRES LOCKED UP, AIRCRAFT WAS UNABLE TO TAXI. MAINTE NANCE REMOVED AND REPLACED THE NR 2 MAIN LANDING GEAR WHEEL ASSEMBLY IAW J41 MAINTENANCE MANUAL. 2 L 7 2 4T RT A41NM 2001042300043 20010423 00043 EU 2001 4 23 RAIA00103020 1 20010327 A 3242 320511 CONTROL VALVE JETAIR JETSTM JETSTM4101 1500501 EU BRAKE SYS FAILED A RAIA K NONE O OTHER LD LANDING 1 CE 03 555HK 10006 10006 41072 9549-ROC-AIRCRAFT PULLED TO THE LEFT AS IF LEFT HAND MAIN LANDING GEAR TIRES LOCKED UP, AIRCRAFT WAS UNABLE TO TAXI. MA INTENANCE REMOVED AND REPLACED THE DUAL BRAKE CONTROL VALVE IAW J41 MAINTENANCE MANUAL. 2 L 7 2 4T RT A41NM 2001042300044 20010423 00044 EU 2001 4 23 RAIA00103021 1 20010326 A 3241 CONTROL BOX JETAIR JETSTM JETSTM4101 1500501 EU ANTI-SKID FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 555HK 41072 5358-EWR-DURING TAXI IN LEFT HAND MAIN LANDING GEAR BRAKES LOCKED UP DUE TO ANTI SKID FAILURE NR 2 MAIN TIRE WAS FLAT. MAINTENANCE REMOVED AND REPLACED NR 2 MAIN LANDING GEAR TIRE IAW J41 MAINTENANCE MANUAL. 2 L 7 2 4T RT A41NM 2001042300045 20010423 00045 EU 2001 4 23 QXEA0100423 1 20010326 A 3230 71538 SELECTOR VALVE FOKKER F28 F28MK4000 4990810 EU NLG LEAKING A QXEA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 497US 38204 38204 11173 BOI - FLIGHT CREW REPORTED UNSAFE GEAR INDICAION DURING EXTENTION CYCLE UPON APPROACH. CYCLED GEAR, NO CHANGE IN INDICA TION. CREW USED ALTERNATE GEAR EXTENTION METHOD. GEAR EXTENDED AND INDICATED DOWN AND LOCKED WITHOUT INCIDENT. MAINTE NANCE FOUND THE NOSE GEAR SELECTOR VALVE SHAFT LEAKING. REMOVED AND REPLACED NOSE GEAR SELECTOR VALVE. OPERATIONAL GEA R SWINGS CHECK GOOD. LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001042300046 20010423 00046 NM 2001 4 23 PCAA0103022 1 20010323 A 3350 BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 812EX 312 MDT- DURING ROUTINE MAINTENANCE VISIT 2 RED EGRESS LIGHTS ON CABIN FLOOR FOUND INOPERATIVE. ALL EMERGENCY LIGHT BATTERI ES REPLACED DUE TO BEING DEAD/WEAK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001042300047 20010423 00047 NM 2001 4 23 DLM90010506 1 20010326 A 3260 INDICATOR DOUG MD90 MD9030 3023690 NM COCKPIT FALSE INDICATION A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 904DA 53384 AFTER RAISING GEAR RT MAIN RED LIGHT REMAINED ON. ALL GREENSOUT, GEAR DOOR LIGHT OUT, LOWERED LANDING GEAR PER CKLIST AL L 3 GREEN ON, ALL REDS OUT BUT DOOR LIGHT REMAINED ON FOR APPROX. 2 MIN. LANDING GEAR DOOR LIGHT FLICKERED ON/OFF UNTI L A/C WAS SLOWED FOR APPROACH DOOR LIGHT WENT OUT - JACKED A/C AND SWUNG GEAR - TESTED PROX SWITCHES - NO TROUBLE FOUND - UNABLE TO DUPLICATE 2 L 7 2 4F RT A6WE 2001042300048 20010423 00048 NM 2001 4 23 DL72L010507 1 20010327 A 3350 S106 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 511DA 21313 ON LAYOVER FOUND OVERHEAD CENTER AISLE EMERGENCY EXIT LIGHT AT ROW 25 INOP - REPLACED BATTERIES 2 L 7 3 4F A3WE 2001042300049 20010423 00049 NM 2001 4 23 DL76G010508 1 20010317 A 2820 FLOW VALVE BOEING 767 7673P6 1385105 NM WING FAILED A DALA O OTHER O OTHER NR NOT REPORTED 1 SO 27 1501P 24983 A/C RESTRICTED FROM ETOPS OPERATIONS DUE TO REPETITIVE FUEL MIGRATION HISTORY. FOUND MOTIVE FLOW VALVE MALFUNCTION. REP LACED SAME. 2 L 7 2 4F RT A1NM 2001042300050 20010423 00050 NM 2001 4 23 0101046641 1 20010328 A 5330 STRAP BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 641NW 21941 DURING PCK, FOUND CORROSION ON FUSELAGE SKIN STRAP AT BS 1960 LBL 4. REPAIRED PER EA 66-182916. 2 L 7 4 4F A20WE 2001042300051 20010423 00051 NM 2001 4 23 0101052284 1 20010226 A 5540 WEB BOEING 727 727251 138408H NM RUDDER CHAFED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 284US 21323 DURING H-CHECK, FOUND CHAFING ON THE BOTTOM WEB OF LOWER RUDDER. REPAIRED PER EA 22-182193. 2 L 7 3 4F A3WE 2001042300052 20010423 00052 NM 2001 4 23 0101062284 1 20010214 A 5532 SKIN BOEING 727 727251 138408H NM VERTICAL STAB CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 284US 21323 DURING H-CHECK, FOUND CRACK ON THE LT VERTICAL FIN SKIN AT FIN STA 13.7 STRINGER 10. REPAIRED PER EA 22-182196. 2 L 7 3 4F A3WE 2001042300053 20010423 00053 NM 2001 4 23 0101072284 1 20010221 A 5315 FLOORBEAM BOEING 727 727251 138408H NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 284US 21323 DURING H-CHECK, FOUND CORROSION ON FLOORBEAM AT BS 380 BETWEEN RBL 2 AND RBL 65. REPAIRED PER EA 22-182195. 2 L 7 3 4F A3WE 2001042300054 20010423 00054 NM 2001 4 23 0101082284 1 20010223 A 5315 FLOORBEAM BOEING 727 727251 138408H NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 284US 21323 DURING H-CHECK, FOUND CORROSION ON FLOORBEAM AT BS 1110 RBL 25 TO LBL 45. REPAIRED PER EA 22-182194. 2 L 7 3 4F A3WE 2001042300055 20010423 00055 NM 2001 4 23 0101092284 1 20010228 A 5315 FLOORBEAM BOEING 727 727251 138408H NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 284US 21323 DURING H-CHECK, FOUND CORROSION ON TOP OF FLOORBEAM AT BS 1130 LBL 50. REPAIRED PER EA 22-182192. 2 L 7 3 4F A3WE 2001042300056 20010423 00056 SO 2001 4 23 SWIA972456 1 20010326 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT FLAP FAILED A SWIA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 186SW 120034 FLAP CONTROL FAULT ON TAXI OUT. COULD NOT RESET. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR IAW 27-50-09. OPS AND LEAK CHECK GOOD. P/N ON 320300-1007, S/N ON 1093, S/N OFF 1146. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042300057 20010423 00057 SO 2001 4 23 SWIA972457 1 20010325 A 2130 CONTROLLER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CABIN PRESSURE MALFUNCTIONED A SWIA O OTHER O OTHER CL CLIMB 1 NM 07 308SW 120326 PRESSURIZATION SYSTEM UNABLE TO MAINTAIN THE CABIN ALTITUDE SELECTED. OPERATED AUTO PRESSURIZATION WITH TEST BOX, OPERA TION NORMAL. NO LEAKS FOUND AT EXITS OR BOTH ECS PACKS ENTERING CABIN. COULD NOT DUPLICATE. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042300058 20010423 00058 SO 2001 4 23 SWIA972458 1 20010326 A 2750 CONTROL UNIT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FLAP MALFUNCTIONED A SWIA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 188SW 120039 FLAP DISAGREEMENT ON INBOARD FLAPS DURING TAXI IN. REMOVED FLAP CONTROL UNIT AND RE-RACKED. OPS CHECK OK. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042300059 20010423 00059 2001 4 23 SWIA972459 4 20010322 A 2210 CONTROL PANEL EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 576SW 120345 BOTH CAPTAINS AND FIRST OFFICER''S YAW DAMPER FAILED TO ENGAGE. TRIM FAIL LIGHT ILLUMINATED (RED TRIM FAIL LIGHT ON MAP ). BURNING SMELL IN COCKPIT. EN ROUTE FRESNO, DIVERTED TO BURBANK AIRPORT. DETERMINED AUTOPILOT CONTROL PANEL SOURCE OF BURNING SMELL. REPLACED APP65A CONTROL PANEL. OPERATED SYSTEMS FOR EXTENDED PERIOD OF TIME WITH NO FURTHER FAILURES . OPS CHECK GOOD. S/N ON: 713, S/N OFF: 7129. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042300060 20010423 00060 NM 2001 4 23 QXEA0100424 1 20010327 A 7931 INDICATOR DHAV DHC8 DHC8202 2809007 NM COCKPIT INOPERATIVE A QXEA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 NM 09 364PH 5797 524 SEA - AT 14,000 FEET NR 2 ENGINE OIL PRESSURE DROPPED TO APPROXIMATELY 42 PSI AND TEMPERATURE READ APPROXIMATELY 80. AS PER CHECKLIST ENGINE NR 2 WAS SHUT DOWN TO START FEATHER. AIRCRAFT LANDED WITHOUT INDICIDENT. REMOVED AND REPLACED IN DICATOR S/N 8092. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001042300061 20010423 00061 EU 2001 4 23 RAIA00103022 1 20010328 A 7712 30000000044 TORQUE SENSOR AEROSP ATR42 ATR42300 8680920 EU NR 2 ENGINE FAILED A RAIA K NONE O OTHER AP APPROACH 1 CE 03 424TE 14215 14215 124 7438-STL-DURING FINAL APPROACH NR 2 ENGINE WHEN INTO FEATHER. MAINTENANCE REMOVED AND REPLACED THE NR 2 TORQUE SIGNAL C ONDITIONER IAW ATR42 MAINTENANCE MANUAL. 2 H 7 2 4T RT A53EU 2001042300062 20010423 00062 WP 2001 4 23 CALA0100254 1 20010327 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72822 49482 INSPECTION FOUND MAIN CABIN FLOOR PANEL CORRODED AT STA 256-313, LBL 22-44. THE PANEL WAS REMOVED AND A NEW PANEL WAS I NSTALLED IAW ECRA 5320-01265 AND SRM 51-30-1. 2 L 7 2 4F A6WE 2001042300063 20010423 00063 WP 2001 4 23 CALA0100255 1 20010327 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72822 49482 INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 200-220 BETWEEN LONGERON 18 L AND 19L. THE DENTED AREA WAS CUT OUT IAW SRM 53-04, FIGURE 25. A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-01, FIGURE 25, 51-10-3, AND 53-04, FIGU RE 25. REINSTALLED ALL REMOVED PARTS IAW SRM 51-30-01 AND 51-30-02. SPLICED CUSP WEB IAW SRM 53-01. 2 L 7 2 4F A6WE 2001042300064 20010423 00064 NM 2001 4 23 CALA0100256 1 20010327 A 5347 SEAT TRACK BOEING 737 737524 1384721 NM CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17627 27531 INSPECTION FOUND SEAT TRACK CORRODED AT BS 344, LBL 44. THE SEAT TRACK SECTION WAS REPAIRED IAW SRM 53-00-52, FIGURE 20 2. 2 L 7 2 4F RT A16WE 2001042300065 20010423 00065 WP 2001 4 23 CALA0100257 1 20010327 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72822 49482 INSPECTION FOUND A 6 INCH CRACK IN MAIN CABIN DOOR TORQUE BOX WEB TANG AT FS 200, LBL 54. THE TORQUE BOX WEB TANG WAS R EPAIRED IAW EA 9-5314-2-A0880 AND ECRA 5310-04121. 2 L 7 2 4F A6WE 2001042300066 20010423 00066 WP 2001 4 23 CALA0100258 1 20010327 A 5230 SKIN DOUG DC9 DC982 3022082 WP CARGO DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72822 49482 INSPECTION FOUND FORWARD CARGO DOOR DENTED ON OUTER SKIN. THE CARGO DOOR WAS REMOVED IAW MM 52-31-00. THE DOOR WAS REP AIRED IAW SRM 53-04, FIGURE 38 AND 51-10-3. THE DOOR WAS REINSTALLED IAW MM 52-31-00. 2 L 7 2 4F A6WE 2001042300067 20010423 00067 WP 2001 4 23 CALA0100259 1 20010328 A 5310 BEAM DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72822 49482 INSPECTION FOUND AFT CARGO PIT DOOR JAMB BEAM CORRODED. A NEW BEAM WAS INSTALLED IAW SRM 51-30-4 AND 51-30-5. TWO DOOR STOP BRACKETS AND 3 SCUFF PLATE STRAPS WERE INSTALLED IAW SRM 51-30-5 AND 51-30-2. 2 L 7 2 4F A6WE 2001042300068 20010423 00068 NM 2001 4 23 CALA0100260 1 20010328 A 5347 SEAT TRACK BOEING 737 737524 1384721 NM CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17627 27531 INSPECTION FOUND SEAT TRACK CORRODED AT BS 344-380, RBL 22. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALL ED IAW SRM 53-00-52. 2 L 7 2 4F RT A16WE 2001042300069 20010423 00069 EU 2001 4 23 QXEA0100427 1 20010326 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 491US 11156 BOI - MID CABIN EXIT SIGN REPORTED TO HAVE INOPERATIVE LAMPS. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001042300070 20010423 00070 NM 2001 4 23 QXEA0100425 1 20010327 A 3350 10005511 SIGN DHAV DHC8 DHC8202 2809007 NM COCKPIT INOPERATIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 349PH 486 PDX - FLIGHT COMPARTMENT EMERGENCY EXIT SIGN REPORTED INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001042300071 20010423 00071 EU 2001 4 23 QXEA0100426 1 20010327 A 3350 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 486US 11237 PDX - THE EXIT SIGN OVER THE FLIGHT COMPARTMENT DOOR WAS REPORTED INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATI ONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001042300072 20010423 00072 NM 2001 4 23 HNAA0100022 1 20010327 A 3232 BOLT DHAV DHC8 DHC8102 2809003 NM MLG DOOR MISSING A HNAA K NONE J WARNING INDICATION CR CRUISE 1 EA 07 935HA 142 NR 1 MLG FWD DOOR CAME OPEN IN FLIGHT. FOUND DOOR ACTUATING ROD TO DOOR HINGE HARDWARE MISSING. REPLACED HARDWARE. 2 H 7 2 4T RT A13NM 2001042300073 20010423 00073 WP 2001 4 23 ABXA010107 1 20010328 A 2710 TORQUE TUBE DOUG DC8 DC863 302198A WP RT AILERON BROKEN A ABXA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 23 821AX 67327 45930 46116 THE RIGHT AILERON TORQUE TUBE WAS REPORTED TO BE BROKEN AT EWR. *S/D* THE AIRCRAFT ON DEPARTURE AND ARRIVAL HAD RIGHT ROLL TENDENCY THAT REQUIRED APPROX 30 DEGREES WINGS LEFT YOKE INPUT TO MAINTAIN LEVAL WINGS. MAINTENANCE INSPECTED AND FOUND THE RIGHT OUTBOARD AILERON TORSION BAR TO BE BROKEN AND REPLACED THE OUTBOARD AILERON ASSEMBLY IAW DC-8 MM 27-11-0 2. 2 L 7 4 4F 4A25 2001042300074 20010423 00074 WP 2001 4 23 0101109873 1 20010324 A 2710 110370 DRAIN VALVE DOUG DC9 DC951 3022051 WP RT SLANT PANEL CLOGGED A NWAA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 01 782NC 48107 EN ROUTE FROM DFW TO DTW, THE AILERON FLIGHT CONTROLS FROZE. AIRCRAFT DESCENDED TO A LOWER ALTITUDE AND CONTROL RETURNE D. FLIGHT DIVERTED TO MEM AND MADE A NORMAL SAFE LANDING. MAINTENANCE FOUND THE RIGHT SLANT PANEL DRAIN VALVE CLOGGED. CLEARED OBSTRUCTION AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2001042300075 20010423 00075 2001 4 23 0101111162 4 20010323 A 2230 ACCELEROMETER DOUG DC10 DC1040 3023508 WP AUTOPILOT FAILED A NWAA K NONE O OTHER CR CRUISE 1 GL 01 162US 46771 WITH NR 1 AUTOPILOT IN COMMAND AND IAS HOLD ENGAGED AT FL 250, AIRCRAFT BEGAN A RAPID DESCENT AND NR 1 AUTOPILOT DISCONN ECTED. AIRCRAFT LEVELED OFF AT FL 237 AND FLIGHT CONTINUED WITH MANUAL CONTROL. FLIGHT LANDED AT MCO WITHOUT INCIDENT. REPLACED ACCELEROMETER AND PITCH COMPUTER. NR 1 AUTOPILOT MEL. 2 L 7 3 4F A22WE 2001042300076 20010423 00076 WP 2001 4 23 0101121233 1 20010321 A 2170 COALESCER BAG DOUG DC10 DC1030 3023501 WP A/C BAY DIRTY A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 233NW 46640 ON CLIMBOUT OF AMS, FLIGHT ATTENDANTS NOTICED FUMES INITIALLY STRONG BUT DID NOT DISSIPATE AFTER 50 MINUTES IN FLIGHT. FLIGHT RETURNED TO AMS AND LANDED WITHOUT INCIDENT. REPLACED ALL THREE COALESCER SOCKS AND PERFORMED BURNOUT PROCEDURE. OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 2001042300077 20010423 00077 NM 2001 4 23 0101136730 1 20010325 A 2611 SMOKE DETECTOR BOEING 747 7472J9F 1384806 NM UPPER CARGO BAY MALFUNCTIONED A NWAA K NONE N FALSE WARNING CR CRUISE 1 GL 01 630US 21668 DURING CRUISE, RECEIVED A FIRE WARNING FROM THE NR 3 DETECTOR IN THE MAIN DECK CARGO COMPARTMENT. WARNING QUIT AFTER 40 MINUTES AND AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE A-SMOKE DETECTOR IN THE NR 3 P OSITION. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2001042300078 20010423 00078 WP 2001 4 23 0101151233 1 20010324 A 2612 FIRE WARNING TSCP7004B DOUG DC10 DC1030 3023501 WP COCKPIT ACTIVATED A NWAA F D ACTIVATE FIRE EXT. RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 01 233NW P90321 46640 AFTER PUSHBACK, THE APU FIRE LIGHT ILLUMINATED. FIRE BOTTLE DISCHARGED INTO THE APU COMPARTMENT. MAINTENANCE REPLACED THE APU AND FIRE BOTTLE. 2 L 7 3 4F A22WE 2001042300079 20010423 00079 NM 2001 4 23 0101166302 1 20010329 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 662US 23720 DURING LINE CHECK, FOUND EMERGENCY FLOOR PATH LIGHTING INOPERATIVE IN B-ZONE ON LEFT SIDE. RECONNECTED LOOSE CONNECTION . OPERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001042300080 20010423 00080 NM 2001 4 23 0101176623 1 20010328 A 3350 POWER SUPPLY BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 623US 21705 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE IN ZONE-D. REPLACED D-ZONE POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F A20WE 2001042300081 20010423 00081 NE 2001 4 23 0101149615 2 20010323 A 7321 CONTROL UNIT DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9 52048 NE LT & RT ENGINE MALFUNCTIONED A NWAA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 615NW 47129 LT657609 DURING TAKEOFF ROLL, TWO ENGINE COMPRESSOR STALLS WERE HEARD BY THE FLIGHT CREW. IT WAS NOT DETERMINED WHICH ENGINE OR BOTH EXPERIENCED THE COMPRESSOR STALLS. THE TAKEOFF WAS ABORTED AT 120 KNOTS WITHOUT INCIDENT. MAINTENANCE REPLACED TH E FUEL CONTROL UNITS LOCATED ON THE LEFT AND RIGHT ENGINES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F 4 F A6WE E2EA 2001042300082 20010423 00082 EU 2001 4 23 C2XA01BT043 1 20010330 A 3350 3011210 LIGHT AEROSP ATR42 ATR42320 8680930 EU PAX DOOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15818 153 DURING 4A INSPECTION MAINTENANCE FOUND PASSENGER DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED PASSENGER DOOR EMERGENCY LIGHT ASSY IAW ATR42 JIC 33-51-24. OPS CHECKED GOOD. 2 H 7 2 4T RT A53EU 2001042300083 20010423 00083 NM 2001 4 23 01FDEA00232 1 20010329 A 2612 894120 FIRE LOOP BOEING 727 7272S2F 1384O81 NM NR3 ENGINE FAULTY A FDEA K NONE N FALSE WARNING CL CLIMB 1 SO 25 211FE 22933 PASS 12,000 FT GOT AN INTERMITTENT FIRE LIGHT ON THE NR 3 ENGINE. RECEIVED FIRE BELL MOMENTARILY. REPLACED LWR FIRE DE TECTOR ELEMENT REF MM 26-11-012-4. OPS CK OK. 2 L 7 3 4F A3WE 2001042300084 20010423 00084 NM 2001 4 23 01FDEA00235 1 20010329 A 5531 65168463 SPAR BOEING 727 727233 138408A NM VERTICAL STAB CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 VERTICAL STAB MIDSPAR CHORD (STR 7) IS CHAFED, LT SIDE 3 INCHES FROM FRONT OF SLIDE SEAL FRONT TRACK. *S/D* REPAIRED A REA PER FEDEX SR 27-55-008. 2 L 7 3 4F RT A3WE 2001042300085 20010423 00085 NM 2001 4 23 01FDEA00236 1 20010329 A 5315 BAC1518332 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 CORROSION ON FLOORBEAM AT BS 328, LBL 30-45, WL 208. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 53-10-8. 2 L 7 3 4F RT A3WE 2001042300086 20010423 00086 EU 2001 4 23 01FDEA00237 1 20010329 A 3230 LANDING GEAR AIRBUS 300 A300F4605R 3930327 EU LANDING GEAR FAILED A FDEA A UNSCHED LANDING P NO WARNING INDICATION TO TAKEOFF 1 SO 25 685FE 803 LANDING GEAR WOULD NOT RETRACT AFT DEPART IAH. WHEEL WELL DOORS OPENED. PERF SYS BITE, NO FAULTS FOUND, DEFERRED NR 1 POS IND SYS ON MEL 32-2. 2 L 7 2 4F RT A35EU 2001042300087 20010423 00087 WP 2001 4 23 01FDEA00239 1 20010329 A 2750 FLAP DOUG DC10 DC1010 3022110 WP WINGS FAULTY A FDEA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 25 390FE 46624 LAND PHASE, SEL FLAPS 15 DEG, RT FLAPS TRACKED TO 15 DEG, LEFT FLAP TAPE IND ONLY 5 DEG. CREW RAN NO FLAPS/ASYM FLAPS W ITH SLATS EMERGENCY CKLIST. FLAP OVRD GUARD HANDLE NEEDS NEW SAFETY WIRE. DURING SPLIT FLAP IND, NO ADVERSE FLT CHARAC TERISTICS. 2 L 7 3 4F A22WE 2001042300088 20010423 00088 WP 2001 4 23 01FDEA00240 1 20010330 A 2120 UNKNOWN DOUG DC10 DC1010 3022110 WP CABIN ODOR A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 390FE 46624 DURING CLIMBOUT NOTICED ACRID FUMES EMANATING FROM AIR CONDITION SYS, PROCEED TO COMPLY WITH EMERGENCY CKLIST AND RETURN TO DEP AIRPORT. 2 L 7 3 4F A22WE 2001042300089 20010423 00089 WP 2001 4 23 CALA0100261 1 20010329 A 5754 SKIN DOUG DC9 DC982 3022082 WP RT SLAT DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72822 49482 INSPECTION FOUND RT NR 3 SLAT LEADING EDGE SKIN CREASED. THE INNER SKIN WAS REMOVED IAW SRM 51-30-8. THE SLAT SKIN WAS REPAIRED IAW ECRA 5754-01039. REINSTALLED INNER SKIN IAW SRM 51-30-8. REINSTALLED ANTI-ICE DUCT IAW MM 30-10-00. LEA K AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A6WE 2001042300090 20010423 00090 NM 2001 4 23 CALA0100262 1 20010329 A 5320 FLOOR SUPPORT BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17627 27531 INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 344-360, RBL 11. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WA S INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001042300091 20010423 00091 NM 2001 4 23 CALA0100263 1 20010329 A 5320 ATTACH ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND FLOOR SUPPORT ATTACH ANGLES CRACKED AT STA 540, RIGHT OF AIRCRAFT CENTERLINE AND LEFT OF AIRCRAFT CENTE RLINE. THE CRACKS WERE 1 INCH LONG. THE TWO FLOOR SUPPORT ATTACH ANGLES WERE REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001042300092 20010423 00092 WP 2001 4 23 CALA0100264 1 20010330 A 3230 59516395001 BUNGEE CYLINDER DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A CALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SW 09 16813 48066 WHEN GEAR WAS LOWERED FOR LANDING ON APPROACH TO ORD THREE RED UNSAFE LIGHTS WERE ILLUMINATED. A GO-AROUND WAS PERFORME D AND QRH PROCEDURES WERE ACCOMPLISHED WITH SUCCESSFUL GEAR EXTENSION. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENAN CE TROUBLESHOOTING FOUND THE NOSE GEAR NOT EXTENDING HYDRAULICALLY. MAINTENANCE FOUND THE NOSE GEAR BUNGEE CYLINDER AT FAULT. THE BUNGEE CYLINDER WAS REMOVED AND REPLACED IAW MM 32-32-7. THE LANDING GEAR CONTROL VALVE WAS REPLACED AS A P RECAUTIONARY MEASURE AND THE SYSTEM WAS TESTED IAW MM 32-32-01. 2 L 7 2 4F A6WE 2001042300093 20010423 00093 NM 2001 4 23 CALA0100265 1 20010329 A 5552 251A24362 ATTACH FITTING BOEING 737 737824 13844BZ NM LT ELEVATOR WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16217 28777 WHEN PERFORMING WORK CARD 99-5550-1-0006 MAINTENANCE FOUND THE LT ELEVATOR TAB MECHANISM O/B TAB ROD ATTACH FITTING WORN AND I/B WAS STARTING TO WEAR. THE LT ELEVATOR TAB MECHANISM ASSEMBLY WAS REMOVED AND REPLACED IAW MM 27-31-34. 2 L 7 2 4F RT A16WE 2001042300094 20010423 00094 EA 2001 4 23 COMA0160350 1 20010325 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 940CA 7048 OVERHEAD EMERGENCY LIGHT AFT CABIN IS INOP. REPLACED THE LIGHT BULB. 2 L 7 2 4F RT A21EA 2001042300095 20010423 00095 EA 2001 4 23 COMA0160352 1 20010326 A 5324 POST CNDAIR CL600 CL6002B19 EA CABIN CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 943CA 7062 INBOARD AND OUTBOARD POSTS AT RBL 9 AND LBL 9 AT FS 559 ARE CRACKED AT APPROXIMATELY WL 45. CAUSE UNKNOWN. DAMAGED ARE AS REMOVED AND REPAIRED IAW WVAC EO 601R-53-2335B. 2 L 7 2 4F RT A21EA 2001042300096 20010423 00096 WP 2001 4 23 ARWA0010309 1 20010330 A 3260 SENSOR LKHEED 1011 1011385115 5265015 WP LT MLG OUT OF ADJ A ARWA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 19 308GB 193U1133 TRUCK LIGHT REMAINS ON AFTER TAKEOFF. GEAR WOULD NOT RETRACT. AIR TURNBACK. AIRCRAFT LANDED WITHOUT INCIDENT. ADJUST ED TRUCK SENSOR LEFT MLG, COMPLETED LANDING GEAR RETRACTION AND ALL SYSTEMS CHECK OK IAW MM 32-30-00. 2 L 7 3 4F A23WE 2001042300097 20010423 00097 NM 2001 4 23 AWXA0001564 1 20010330 A 5315 6545410145 FLOORBEAM BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 CABIN FLOOR SUPPORT UPPER T-ANGLE AND WEB CRACKED AT FS 663.75 BL 0. FABBED, DRILLED AND INSTALLED REPAIR WEB SPLICE PL ATES AND ANGLES IAW AWA ER 5702-01074-JS5 AND B737-300 SRM 51-10-02 PG 15 AND 51-40-02 PG 10. 2 L 7 2 4F RT A16WE 2001042300098 20010423 00098 NM 2001 4 23 AWXA0001565 1 20010330 A 5311 6546533503 FRAME BOEING 737 7373S3 1384711 NM FUSELAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 STA 500 FRAME ELONGATED HOLES IN LOWER WEB BETWEEN STR 28R AND 28L. FABBED, DRILLED AND INSTALLED REPAIR DOUBLER, FILL ERS AND CLIPS IAW AWA ER 03-5332-01087-DD1. 2 L 7 2 4F RT A16WE 2001042300099 20010423 00099 EU 2001 4 23 AWXA0001566 1 20010330 A 5230 D52371190002 HANDLE AIRBUS 320 A320231 3930325 EU CARGO DOOR MISALIGNED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 C1 DOOR UPPER LOCKING SHAFT AFT SUPPORT FITTING BORE FOUND IN MISALIGNMENT TO SHAFT. REPAIRED IAW AWA ER 26-5231-01087- 5-S51. 2 L 7 2 4F RT A28NM 2001042300100 20010423 00100 CE 2001 4 23 DJFA00115 1 20010320 A 7110 45A3517622 COWLING BEECH MU300 400A 1155402 CE NR 2 ENGINE BUCKLED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 440CW 3596 RK40 COWLING BUCKELED, RIGHT SIDE LOWER INBOARD. 2 H 7 2 4F RT A16SW 2001042300101 20010423 00101 WP 2001 4 23 TWAA0105701 1 20010328 A 3350 58222 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A TWAA K NONE O OTHER CR CRUISE 1 CE 05 929TW 48014 THE EGRESS LIGHTS BEHIND ROW 29 WERE FLASHING. REPLACED THE POWER SUPPLY. CHECK-C 3-30-00 STL. 2 L 7 2 4F A6WE 2001042300102 20010423 00102 NM 2001 4 23 TWAA0105702 1 20010329 A 3350 6100928 LIGHT BOEING 767 7673Q8 NM CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 634TW 28132 THE EGRESS LIGHT AT SEAT 24J AND THE EMERGENCY LIGHT ABOVE SEAT 34G WERE INOPERATIVE. REPLACED THE LAMP, P/N 6100928, A T SEAT 24J, AND THE LAMP, P/N 1317, ABOVE SEAT 34G. CHECK-C 10-25-00 LAX. 2 L 7 2 4F RT A1NM 2001042300103 20010423 00103 WP 2001 4 23 TWAA0105703 1 20010326 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT FOUND CORROSION ON STA 1338 AFT PRESSURE BULKHEAD LOWER TEE. REPLACED FUSELAGE SKIN STA 1311 TO 13 38, LONGERON 21R TO 26R, PER ARA 17647 AND SRM 53-04 FIG 12C. 2 L 7 2 4F A6WE 2001042300104 20010423 00104 SO 2001 4 23 C2ZA01IA184 1 20010328 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145LR SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13955 145075 BNA-DURING POST FLIGHT INSPECTION THE CREW THE OVERWING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY POWER SUPPLY, PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM AND CHECK GOO D. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001042300105 20010423 00105 SO 2001 4 23 C2XA01IA185 1 20010327 A 2170 645001RR151 O-RING EMB 120 EMB120ER 3260203 SO WATER SEPARATER LEAKING A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 16724 120171 IAH-FLIGHT 3422 DURING CLIMBOUT THE CREW REPORTED SMOKE IN THE CABIN, WITH RIGHTHAND DUCT LEAK WARNING. THE NR 2 ENGINE WAS SHUT DOWN AS A PRECAUTION. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE WATER SEPARATOR O-RING, PERFORMED AN OPERATIONAL CHECK OF THE PACKS SYSTEM WITH NO DEFECTS NOTED. THE AIR CRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001042300106 20010423 00106 CE 2001 4 23 GLBA2001065 1 20010324 A 7714 1303800445 INDICATOR BEECH 1900 1900D 1154162 CE COCKPIT FAILED A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 251GL 224 UE251 N1 INDICATOR FAILED. REPLACED INDICATOR. 2 L 7 2 4T RT A24CE 2001042300107 20010423 00107 SO 2001 4 23 GLBA2001066 1 20010326 A 3260 TARGET EMB 120 EMB120ER 3260203 SO LT MLG OUT OF ADJ A GLBA K NONE N FALSE WARNING CR CRUISE 1 CE 01 299UX 120299 LEFT MAIN GEAR UNSAFE LIGHT WITH GEAR SELECTED UP. INSPECTED FOUND LEFT UPLOCK PROX SENSOR TARGET OUT OF ADJUSTMENT. O PS CHECKED GEAR SYSTEM GOOD. RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 2001042300108 20010423 00108 NE 2001 4 23 GLBA2001068 2 20010329 A 7314 1143890425 PUMP BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ENGINE FAILED A GLBA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 01 154GL 2230 UE154 RIGHT FUEL PRESSURE ANNUNCIATOR ILLUMINATED. REPLACED ENGINE DRIVEN FUEL PUMP, OPS CHECKED SYSTEM GOOD. RETURNED TO SE RVICE. 2 L 7 2 4T 4 T RT A24CE E26NE 2001042300109 20010423 00109 WP 2001 4 23 SCNA01023 1 20010324 A 3242 50007097 BRAKE DOUG DC10 DC1015 3022118 WP MLG FIRE A SCNA K NONE A FLAME/FIRE LD LANDING 1 GL 15 153SY 48276 AFTER LANDING AT MCO THE CREW WAS NOTIFIED THAT THE NUMBER EIGHT BRAKE WAS ON FIRE. REMOVED AND REPLACED NUMBER EIGHT B RAKE, TIRE, AND BRAKE SLEEVE. OPERATIONAL CHECKS GOOD. 2 L 7 3 4F A22WE 2001042300110 20010423 00110 WP 2001 4 23 SCNA01024 1 20010318 A 5270 SWITCH DOUG DC10 DC1015 3022118 WP CARGO BAY DIRTY A SCNA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 15 151SY 48295 DURING TAKEOFF ROLL AT MCO (85KTS) THE FORWARD CENTER CARGO A-SYSTEM LIGHT ILLUMINATED. PLACED A-SYSTEM LIGHT ON MEL. CLEANED SWITCHES AND OPERATIONAL CHECKS GOOD. 2 L 7 3 4F A22WE 2001042300112 20010423 00112 NM 2001 4 23 0101186641 1 20010309 A 5320 BEAM BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 641NW 21941 DURING PCK, FOUND CRACK IN VERTICAL SUPPORT BEAM LOWER END AT BS 987 RBL 10. REPAIRED PER EA 66-181879. 2 L 7 4 4F A20WE 2001042300113 20010423 00113 NM 2001 4 23 0101196626 1 20010304 A 5315 FLOORBEAM BOEING 747 747251B 1384892 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 626US 21708 DURING LINE CHECK FOUND CRACK ON FLOORBEAM LOWER CHORD AT BS 1900 RBL 110. REPAIRED PER EA 66-181515. 2 L 7 4 4F A20WE 2001042300114 20010423 00114 WP 2001 4 23 0101201146 1 20010129 A 5315 FLOORBEAM DOUG DC10 DC1040 3023508 WP FUSELAGE DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 146US 46755 DURING M-CHECK, MAIN CABIN FLOORBEAM AT BS 1293 WAS FOUND SEVERED AT LBL 106 AND CRACKED AT RBL 106 JUST INSIDE OF NR 3 LT AND NR 3 RT DOORS. REPAIRED PER EA 11-180795. 2 L 7 3 4F A22WE 2001042300115 20010423 00115 WP 2001 4 23 ABXA010108 1 20010331 A 2710 5924667 MIXER BOX DOUG DC9 DC941 302207N WP AILERON CONTROL BINDING A ABXA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 GL 23 969AX 56452 47464 DURING PRE-DEPARTURE CHECKS, THE AILERON CONTROL YOKE WOULD BIND WHEN RETURNING FROM LEFT TO CENTER POSITIONS. MAINTENA NCE INSPECTED, CLEANED, AND LUBRICATED THE LEFT AND RIGHT AILERON MIXER ASSEMBLIES. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001042300116 20010423 00116 WP 2001 4 23 ABXA010109 1 20010331 A 5246 59589451 DOOR DOUG DC9 DC932 3022066 WP NACELLE MISSING A ABXA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 GL 23 981AX 69779 47273 DURING MAINTENANCE WALKAROUND INSPECTION, THE NR 2 ENGINE OIL SERVICE DOOR WAS NOTED TO BE MISSING FROM THE AIRCRAFT. M AINTENANCE INSPECTED THE NR 2 ENGINE AND AIRFRAME FOR DAMAGE. NONE WAS NOTED. A REPAIR WAS COMPLETED IAW ABX REA D954- 40560, AND A DEFERRAL WAS INITIATED FOR THE ITEM. *S/D* ON 04/03/01 MAINTENANCE INSPECTED AND REPLACED THE LOWER NR 2 ENGINE OIL ACCESS DOOR IAW DC-9 SRM 51-30-1. THE DEFERRAL WAS REMOVED FROM THE AIRCRAFT. 2 L 7 2 4F A6WE 2001042300117 20010423 00117 EA 2001 4 23 A6WA200100023 2 20010325 A 7200 ENGINE BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502* 41580 EA NR 1 ENGINE POWER LOSS A A6WA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 31 179US E2041 LF05061 ON CLIMBOUT IN ICING CONDITIONS, NR 1 ENGINE POWER DECAYED WITH TAIL AND WING ANTI-ICE ON N1 WENT TO 82 PERCENT, N2 WENT TO 84 PERCENT. MAINTENANCE INSPECTED ALL CHIP DETECTORS, BLEED BAND ACTUATOR, OPS CHECK GOOD. NO DEFECTS NOTED. 2 H 7 4 4F 4 F RT A49EU E6NE 2001042300118 20010423 00118 2001 4 23 A6WA200100024 4 20010327 A 2565 CABLE BAG BAE146 BAE146200A 1500266 EU SLIDE DETACHED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 290UE 8167 8167 0839 E2080 FWD PAX SLIDE DEPLOY CABLE NOT ATTACHED TO GIRT BAR. MAINTENANCE REMOVED AND REPLACED EVACUATION SLIDE ASSEMBLY. 2 H 7 4 4F RT A49EU 2001042300119 20010423 00119 2001 4 23 A6WA200100025 4 20010329 A 2565 D31050105 SLIDE BAG BAE146 BAE146300A 1500267 EU DOOR FAILED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 615AW 28403 28403 E3141 SLIDE DID NOT DEPLOY, HUNG LIMP. MAINTENANCE REMOVED AND REPLACED EVACUATION SLIDE AFTER PULLING PULL HANDLE TO INFLATE . 2 H 7 4 4F RT A49EU 2001042300120 20010423 00120 NM 2001 4 23 AT0100106 1 20010402 A 3350 CONNECTOR BOEING 737 7372L9 1384497 NM CABIN DAMAGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 737Q 21279 FOUND FORWARD CABIN OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPAIRED BENT PIN AT BATTERY PACK CONNECTOR IAW 737WDM 33-51- 01. 2 L 7 2 4F RT A16WE 2001042300121 20010423 00121 WP 2001 4 23 AT0100107 1 20010308 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP CABIN CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 FOUND CABIN FLOORPANEL NR 4699 CORRODED. REPLACED FLOORPANEL SKIN IAW DC9 SRM 53-21 FIG 2D, 51-10-02, 51-10-0351-10-04, 51-20-01, AND 51-30-02. 2 L 7 2 4F A6WE 2001042300122 20010423 00122 WP 2001 4 23 AT0100108 1 20010306 A 5230 SKIN DOUG DC9 DC932 3022066 WP CARGO DOOR DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 FOUND DENT IN AFT CARGO DOOR BS 937-959R. FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 53-04 FIG 12C. 2 L 7 2 4F A6WE 2001042300123 20010423 00123 WP 2001 4 23 AT0100109 1 20010308 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 FOUND FLOORBOARD 4698 CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 53-05, 51-10-02, 51-10-04, AN D 51-20. 2 L 7 2 4F A6WE 2001042300124 20010423 00124 WP 2001 4 23 AT0100110 1 20010309 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP FUSELAGE CHAFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 FOUND FLOORBEAM AT BS 446 CHAFED BEYOND LIMITS. INSTALLED REPAIR ANGLE IAW DC9 SRM 53-05 FIG 20A. 2 L 7 2 4F A6WE 2001042300125 20010423 00125 WP 2001 4 23 AT0100111 1 20010309 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 FOUND FLOORBOARD CORRODED BEYOND LIMITS AT BS 129 RBL 17-42. FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 51-70-04 AND 5 1-10-03. 2 L 7 2 4F A6WE 2001042300126 20010423 00126 WP 2001 4 23 AT0100112 1 20010308 A 5543 SKIN DOUG DC9 DC932 3022066 WP RUDDER TAB DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 FOUND RUDDER TAB DENTED. FABRICATED AND INSTALLED FILLER AND DOUBLERS IAW DC9 SRM 51-70-02 AND 55-40-01. 2 L 7 2 4F A6WE 2001042300127 20010423 00127 WP 2001 4 23 AT0100113 1 20010323 A 5310 DOOR FRAME DOUG DC9 DC932 3022066 WP CARGO BAY CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 FOUND CRACK IN AFT CARGO DOOR JAMB. REPAIRED CRACK IAW REO-L00420 AND EO 09-5310-29-61496. 2 L 7 2 4F A6WE 2001042300128 20010423 00128 WP 2001 4 23 AT0100114 1 20010305 A 5280 SKIN DOUG DC9 DC932 3022066 WP LT MLG DOOR CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 847AT 47555 FOUND TWO CRACKS IN LEFT WHEEL WELL DOOR AT AFT UPPER SKIN. REMOVED EXISTING DOUBLER REPAIR, STOP DRILLED 3 CRACKS, HFE C INSPECTED. FABRICATED INTERNAL AND EXTERNAL DOUBLER IAW DC9 52-05 FIGURE 4 50-01 FIGURE 2. 2 L 7 2 4F A6WE 2001042300129 20010423 00129 WP 2001 4 23 AT0100115 1 20010306 A 5532 SKIN DOUG DC9 DC932 3022066 WP VERTICAL STAB CHAFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 847AT 47555 FOUND UPPER VERTICAL STAB PANEL CHAFING ON FORWARD STRUCTURE. BLENDED CHAFED AREAS, FOUND TO BE OUT OF LIMITS. FABRICA TED REPAIR SECTIONS AND INSTALLED IAW DC9 SRM 55-01 FIGURE 2 AND 51-10-2. 2 L 7 2 4F A6WE 2001042300130 20010423 00130 WP 2001 4 23 AT0100116 1 20010318 A 5311 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 847AT 47555 FOUND CORROSION FORWARD ON FRAME AT BS 1121. REMOVED AND REPLACED AT BS 1121 CANTED FRAME RIGHT SIDE IAW TIMCO SERVICE ORDER 151104-22132. 2 L 7 2 4F A6WE 2001042300131 20010423 00131 WP 2001 4 23 AT0100117 1 20010302 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 847AT 47555 FOUND .25 INCH CRACK ON FUSELAGE SKIN AT BS 160 LONGERON 23L. CUT OUT CRACKED AREA, FABRICATED REPAIR DOUBLERS AND INST ALLED IAW DCI SRM 53-01 FIGURE 38, DRAWING 3R09530129 AND EO 09-5330-E1714. 2 L 7 2 4F A6WE 2001042300132 20010423 00132 EU 2001 4 23 SABA010009 1 20010328 A 7332 1103P0645 SWITCH BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE331* 01514 WP LT ENGINE DEFECTIVE A SABA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 33 958AE 958 AIRCRAFT 958 ON FLIGHT 5141 CLT TO LYH. DURING TAKEOFF ROLL THE LEFT ENGINE LOW FUEL PRESSURE WARNING LIGHT CAME ON. T HE TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE WITH NO OTHER PROBLEMS. NO EMERGENCY PROCEDURES USED. MAINTEN ANCE REMOVED AND REPLACED THE LEFT ENGINE FUEL PRESSURE TRANSDUCER AND LOW FUEL PRESSURE WARNING SWITCH. OPS CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 3 T RT A56EU E2WE 2001042300133 20010423 00133 WP 2001 4 23 IXXA0100010 1 20010321 A 2910 AE246010J0134 HYDRAULIC LINE DOUG DC8 DC862 3021970 WP NR 3 ENGINE DEFECTIVE A IXXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 11 21CX 68387 1841 45955 DURING CLIMBOUT FROM AVB, THE FLIGHT CREW NOTICED A DECLINE IN THE MAIN HYDRAULIC QUANTITY AND PRESSURE INDICATION SYSTE MS. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND RETURNED TO AVB FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED T HE AIRCRAFT LOCATING A DEFECTIVE HYDRAULIC PRESSURE LINE ON THE NUMBER THREE ENGINE HYDRAULIC PUMP. MAINTENANCE REPLACE D THE LINE AND PERFORMED A SUCCESSFUL OPERATIONAL CHECK IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETU RNED TO SERVICE. 2 L 7 4 4F 4A25 2001042300134 20010423 00134 WP 2001 4 23 IXXA0100012 1 20010331 A 8012 350515422 STARTER DOUG DC8 DC871F 302199D WP ENGINE DEFECTIVE A IXXA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 11 827BX 81517 49 45971 EN ROUTE FROM TOL TO LAX, THE FLIGHT CREW NOTICED A DECLINE IN THE NUMBER TWO ENGINE OIL QUANTITY SYSTEM. THE FLIGHT CR EW SECURED THE ENGINE FOLLOWING COMPANY PROCEDURES FOR PRECAUTIONARY MEASURES. THE FLIGHT CONTINUED TO LAX FOR AN UNEVE NTFUL LANDING. MAINTENANCE INSPECTED THE ENGINE LOCATING A DEFECTIVE PNEUMATIC STARTER. MAINTENANCE REPLACED THE START ER IN ACCORDANCE WITH THE MAINTENANCE MANUAL AND PERFORMED A SUCCESSFUL OPERATIONAL CHECK. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2001042300135 20010423 00135 GL 2001 4 23 C2XA01BT044 2 20010327 A 7230 COMPRESSOR EMB 145 EMB145ER SO ALLSN AE300 AE3007A GL NR 2 ENGINE LEAKING A C2XA O OTHER J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 15932 7737 145015 CAE310026 LAV SMOKE WARNING EICAS AND ALARM IN CABIN AFTER TAKEOFF. WARM PACK SMELL, NO VISIBLE SMOKE OR FIRE AIRCRAFT RELEASED I AW MEL 26-14-00 PLACARD 012059. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE AFTER FINDING EVIDENCE OF OIL LEAKAGE IN ENGINE COMPRESSOR SECTION IAW TASK CARD 6271001. OPS CHECKS AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001042300136 20010423 00136 NM 2001 4 23 CALA0100266 1 20010330 A 5320 ANGLE BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17627 27531 INSPECTION FOUND R-2 DOOR Z-ANGLE CORRODED AT BS 947-1000. THE Z-ANGLE WAS REMOVED AND A NEW Z-ANGLE WAS INSTALLED IAW SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A16WE 2001042300137 20010423 00137 NM 2001 4 23 CALA0100267 1 20010330 A 5320 ATTACH ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT ATTACH ANGLE AT STA 540 BETWEEN RT SEAT TRACKS. THE ATTACH ANGLE WAS R EMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001042300138 20010423 00138 NM 2001 4 23 CALA0100268 1 20010330 A 5730 SKIN BOEING 737 7373T0 1384582 NM RT WING GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND RT WING UPPER L/E SKIN GOUGED ABOVE O/B END OF NR 5 SLAT. THE SKIN WAS REPAIRED IAW ECRA 5721-01048. 2 L 7 2 4F RT A16WE 2001042300139 20010423 00139 NM 2001 4 23 CALA0100269 1 20010330 A 5523 DAS414A1508 BEARING BOEING 737 737824 13844BZ NM ELEVATOR TAB WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17229 28793 INSPECTION OF LEFT ELEVATOR TAB IAW EA 5550-01218 FOUND NR 3 HINGE BEARING WORN. THE NR 3 HINGE BEARING WAS REMOVED AND REPLACED IAW MM 27-31-40. 2 L 7 2 4F RT A16WE 2001042300140 20010423 00140 NM 2001 4 23 CALA0100270 1 20010331 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND A 2 INCH CRACK IN FLOOR INTERCOSTAL AT STA 500D-520, BL 0. THE INTERCOSTAL WAS REMOVED AND A NEW INTER COSTAL WAS INSTALLED IAW SRM 51-40-00. 2 L 7 2 4F RT A16WE 2001042300141 20010423 00141 NM 2001 4 23 CALA0100271 1 20010331 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND FLOORBEAM T-CHORD CORRODED AT SCREW HOLES, STA 947.5, LBL 4. THE T-CHORD WAS REMOVED AND REPLACED IAW SRM 51-40-00 AND 53-00-51. 2 L 7 2 4F RT A16WE 2001042300142 20010423 00142 NM 2001 4 23 CALA0100272 1 20010401 A 5754 SKIN BOEING 737 7373T0 1384582 NM NR 3 SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND TWO .25 INCH CRACKS EXTENDING FROM RIVETS ON LOWER SURFACE OF NR 3 SLAT SKIN AT ACTUATOR. A REPAIR WAS INSTALLED ON NR 3 SLAT IAW BOEING DRAWING 65C30133. 2 L 7 2 4F RT A16WE 2001042300143 20010423 00143 NM 2001 4 23 CALA0100273 1 20010401 A 5523 183A81004 BUSHING BOEING 737 737824 13844BZ NM ELEVATOR TAB WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16234 28946 INSPECTION FOUND RT ELEVATOR TAB RODS TO ELEVATOR TAB MAST FITTING, BOLT, AND BUSHING WORN. THE RT ELEVATOR TAB WAS REM OVED AND REPLACED IAW MM 27-31-31. 2 L 7 2 4F RT A16WE 2001042300144 20010423 00144 NM 2001 4 23 CALA0100274 1 20010401 A 5345 MOUNT BOEING 737 737524 1384721 NM GALLEY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17627 27531 INSPECTION FOUND G-2 GALLEY FORWARD INBOARD LOWER MOUNT CORRODED AT STA 336, RBL 12. THE MOUNT WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 2001050300252 20010503 00252 NM 2001 5 3 01FDEA00247 1 20010331 A 5330 SKIN BOEING 727 72725C 138400H NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 124FE 19360 DURING INSP FUSELAGE SKIN AT BS 249, WL 245 WAS FOUND CRACKED AT FASTENER HOLE BENEATH THE PILOTS NR 3 WINDOW. *S/D* R EPAIRED SKIN PER IAW FEDEX EA 7-5330-57216. 2 L 7 3 4F A3WE 2001042300145 20010423 00145 NM 2001 4 23 01FDEA00250 1 20010402 A 5270 SWITCH BOEING 727 727227 1384078 NM CARGO DOOR LOOSE A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 484FE 21466 ON CLIMBOUT, PASS 5000 FT MAIN CARGO DOOR LIGHT ILLUMINATED. LIGHT FLICKERED OCCASIONALLY. DEPRESS CABIN AND LIGHT WEN T OUT. CK ALL LATCH SWITCHES, FOUND S9039 LATCH SW LOOSE. TIGHTENED MOUNTING SCREWS, PRESS A/C. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2001042300146 20010423 00146 NM 2001 4 23 01FDEA00251 1 20010401 A 2710 AILERON DOUG MD11 MD11F 3023600 NM LT WING MALFUNCTIONED A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 610FE 48603 AT 8000 FT ON DEPART RECEIVED A LEVEL 2 AIL DEFLECT DISAG ALERT ON CONFIG PAGE, LEFT AILERON WAS DROOPING, CREATING A RI GHT TURN. ADJUSTED LOB TO NEUTRAL POS PER MM 27-10-00. CYCLED FLAPS AND AILERONS 3X''S, NIL ALERTS AND SYNOPTIC DISPLA Y SHOW NEUTRAL. 2 L 7 3 4F RT A22WE 2001042300147 20010423 00147 GL 2001 4 23 C2XA01BT045 2 20010331 A 7530 23070418 LINE EMB 145 EMB145ER SO ALLSN AE300 AE3007A GL BLEED VALVE DEFECTIVE A C2XA O OTHER R M PARTIAL RPM/PWR LOSS OVER TEMP CL CLIMB 1 SW 27 14943 145040 ENGINE NR 2 WILL NOT HOLD ITT AT CLIMB THRUST. MAXIMUM CONTINUOUS EXCEEDED 930 DEGREES MAXIMUM. MAINTENANCE REMOVED AN D REPLACED LOWER BLEED CONTROL VALVE LINE IAW ROLLSROYCE MM 75-31-25, OPS CHECKED GOOD. ITT DID NOT EXCEED LIMITS, NO F URTHER ACTION REQUIRED IAW ROLLS ROYCE MM 77-00-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001042300148 20010423 00148 NM 2001 4 23 01FDEA00191 1 20010314 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 CORROSION (C53-224-04) AT FASTENER HOLES IN FLOORBEAM BS 1130, RBL 36-42 AND BL 0 - LBL 25, WL 201. *S/D* REPAIRED PER FEDEX EA 7-5310-56290. 2 L 7 3 4F RT A3WE 2001042300149 20010423 00149 SO 2001 4 23 C2XA01CL069 1 20010329 A 3246 13889 BEARING EMB 135 EMB135ER 3260203 SO NLG WHEEL FAILED A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 27506 145206 CLE FLIGHT 3806 AFTER LANDING IN CVG THE CREW REPORTED THE LEFT NOSE WHEEL DID NOT LOOK LIKE IT WAS INSTALLED CORRECTLY. MAINTENANCE INSPECTED AND FOUND THE LEFT NOSE WHEEL BEARING HAD FAILED. THE NOSE WHEEL ASSEMBLY WAS REPLACED ALONG WI TH THE NOSE STRUT SLIDING TUBE. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001042300150 20010423 00150 SO 2001 4 23 C2XA01CL070 1 20010328 A 3350 CONNECTOR EMB 145 EMB145LR SO CABIN DIRTY A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 14920 145380 CLE FLIGHT 3897 THE CREW REPORTED THE MID CABIN EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND CLEANED AND RESEATED THE CANNON PLUG ON THE LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2001042300151 20010423 00151 NM 2001 4 23 TWAA0105801 1 20010401 A 3350 CONNECTOR BOEING 757 757231 1384950 NM CABIN DIRTY A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 719TW 28487 THE EGRESS LIGHT WAS INOPERATIVE AT CABIN ROW 25. CLEANED AND SECURED FLEX LAMP CONNECTION. CHECK-C 1-5-01 LAX. 2 L 7 2 4F RT A2NM 2001042300152 20010423 00152 NM 2001 4 23 TWAA0105802 1 20010331 A 3350 363674 LIGHT BOEING 757 757231 1384950 NM CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 715TW 28483 THE EGRESS LIGHT WAS INOPERATIVE AT ROW 1. REPLACED THE FLEX LAMP. CHECK-C 10-14-2000 LAX. 2 L 7 2 4F RT A2NM 2001042300153 20010423 00153 NM 2001 4 23 TWAA0105803 1 20010330 A 3350 767 LIGHT BOEING 767 7673Y0 NM CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 640TW 25411 THE EXTERIOR EMERGENCY EXIT LIGHT AT THE AFT RT SIDE NUMBER 3 AND 4 DOORS WERE INOPERATIVE. REPLACED THE LAMPS AT BOTH PLACES. CHECK-C 5-15-00. 2 L 7 2 4F RT A1NM 2001042300154 20010423 00154 WP 2001 4 23 TWAA0105804 1 20010327 A 5312 BULKHEAD DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT FOUND CORROSION ON PRESSURE BULKHEAD AT STA 1338, BETWEEN STRINGER 25R AND 26R. REMOVED AND REPLAC ED TIE FITTING. INSTALLED FASTENERS PER DRAWING 5911429. 2 L 7 2 4F A6WE 2001042300155 20010423 00155 WP 2001 4 23 TWAA0105805 1 20010327 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 906TW 49160 DURING CHECK-C MAINT, THE RT FWD SERVICE DOOR LOWER HINGE AREA INSIDE THE DOOR FORMER ANGLE WAS CRACKED 2 INCHES LONG. REPLACED DOOR FORMER AND RIGGED PER DRAWING 176379. 2 L 7 2 4F A6WE 2001042300156 20010423 00156 WP 2001 4 23 TWAA0105806 1 20010329 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT IN THE AFT CABIN CORROSION WAS FOUND ON NUMBER 2 FLOOR TRACK, FROM STA 1136 TO 1307. CLEANED CORRO SION PER SPM 6-80-01 AND SRM 53-05. TREATED PER SRM 51-10-3 FROM STA 1136 TO 1174. CHANGED TRACK FROM STA 1174 TO 1307 PER SRM 51-30-02. USED RIVETS PER SRM 51-30. 2 L 7 2 4F A6WE 2001042300157 20010423 00157 WP 2001 4 23 TWAA0105807 1 20010330 A 5345 FITTING DOUG DC9 DC982 3022082 WP GALLEY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT IN THE FWD CABIN, THE RT GALLEY HOLD DOWN WAS CORRODED AT STA 160, RBL 51. REPLACED CASTING PER SR M 51-10-4 AND SPM 06-70-01. 2 L 7 2 4F A6WE 2001042300158 20010423 00158 WP 2001 4 23 TWAA0105808 1 20010330 A 5345 FITTING DOUG DC9 DC982 3022082 WP GALLEY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT IN THE FWD CABIN THE RT GALLEY HOLD DOWN WAS CORRODED AT STA 160, RBL 45. REPLACED CASTING PER SRM 51-10-4 AND SPM 06-70-01. 2 L 7 2 4F A6WE 2001042300159 20010423 00159 WP 2001 4 23 TWAA0105809 1 20010330 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE BROKEN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT IN THE AFT CARGO COMPT, THE FLOOR SUPPORT WAS BROKEN AND CORRODED BETWEEN STA 1155 AND 1147, BETWEE N LONGERON 29R AND 30R. REMOVED OLD PART AND INSTALLED NEW PER SPM 6-70-01. FASTENER INSTALLATION PER SRM 51-30-5. 2 L 7 2 4F A6WE 2001042300160 20010423 00160 WP 2001 4 23 TWAA0105810 1 20010328 A 5320 BEAM DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 909TW 49170 DURING CHECK-C MAINT IN THE LT GEAR WHEEL WELL FAIRING BEAM FWD OF CENTER KEEL ON LT SIDE HAD A 3 INCH CRACK. INSTALLED NEW FAIRING BEAM. INSTALLED PER SPM 6-70-01 PAGE 2 AND 3, PER DRAWING 5930584-163 AND 5930584. INSTALLED AD RIVETS PE R SRM 51-30-2 PAGE 1 AND 3. INSTALLED HI-LOKS PER SRM 51-30-5 PAGE 1 AND 3. TORQUED HI-LOKS PER SRM 51-30-1 PARAGRAPH 6. 2 L 7 2 4F A6WE 2001042300161 20010423 00161 NM 2001 4 23 AWXA0001567 1 20010402 A 2133 322684003 OUTFLOW VALVE BOEING 737 7373G7 1384595 NM CABIN PRESSURE FAILED A AWXA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 28 322AW 8547 25400 SJC - AIR TURNBACK - 3/26/01 - THE AIRCRAFT EXPERIENCED A VIBRATION FROM THE LEFT SIDE OF THE FUSELAGE AND RETURNED TO S JC. TECHNICIANS WERE SENT FROM PHX WHO PERFORMED A VISUAL INSPECTION OF THE AIRCRAFT - FOUND NO DISCREPANCIES. REMOVED AND REPLACED THE FWD OUTFLOW VALVE AS THE MOST LIKELY CAUSE; ALSO REPLACED THE EQUIPMENT COOLING VALVE AS A PRECAUTION; NO FURTHER VIBRATIONS NOTED. PART: VALVE, EQUIP. COOLING EXHAUST - MFG: ABLE CORP. - P/N: 31040 - S/N: 1149 - LOC: FWD E/E COMP - COND: PRECAUTION - T.T.: 2576 - T.C.: 1680 2 L 7 2 4F RT A16WE 2001042300162 20010423 00162 2001 4 23 AWXA0001568 4 20010402 A 2210 SC47003 ACTUATOR AIRBUS 320 A320231 3930325 EU YAW DAMPNER LEAKING A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 622AW 7840 054 D: PHX - AIR TURNBACK - 3/31/01 - EN ROUTE FROM PHX TO BOS THE AIRCRAFT LOST GREEN HYDRAULIC SYSTEM QUANTITY AND RETURNE D TO PHX MAKING AN UNEVENTFUL LANDING. MAINTENANCE FOUND THE LT YAW DAMP SERVO ACTUATOR LEAKING AT THE OUTPUT SHAFT; TH E SERVO ACTUATOR WAS REPLACED; LEAK CHECKS AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A28NM 2001042300163 20010423 00163 EU 2001 4 23 RAIA00103023 1 20010329 A 2761 TY176301 ACTUATOR JETAIR JETSTM JETSTM4101 1500501 EU SPOILER FAILED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 571HK 13475 13475 41090 7224-STL-TOCWS ACTIVATION UPON TAKEOFF AND TESTS UNSATISFACTORY WITH ALL 7 PARAMETERS SET CORRECTLY. MAINTENANCE REMOVE D AND REPLACED THE LEFT HAND SPOILER ACTUATOR IAW J41 MAINTENANCE MANUAL. 2 L 7 2 4T RT A41NM 2001042300164 20010423 00164 NM 2001 4 23 F3LA200100051 1 20010330 A 5540 ANGLE BOEING 737 7372P6 NM RUDDER CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 272 3512 21613 DURING C-1 CHECK, INSPECTION REPORTED CRACK IN ANGLE, VERTICAL STABILIZER AT APPROXIMATELY RUDDER STA 86.59. MAINTENANC E FABRICATED AND INSTALLED REPAIR ANGLES PER SRM 51-40-4. 2 L 7 2 4F RT A16WE 2001042300165 20010423 00165 NM 2001 4 23 QXEA0100428 1 20010329 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 SEA - DURING SCHEDULED INSPECTION, A DENT ON THE BOTTOM FUSELAGE AREA AT STATION X445.500 WAS FOUND. DAMAGE WAS FOUND T O BE A DENT 1 X 2 X .030 IN DEPTH. REPAIRED IN ACCORDANCE WITH A ENGINEERING APPROVED REPAIR DRAWING RII COMPLIED WITH. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001042300166 20010423 00166 NM 2001 4 23 QXEA0100429 1 20010330 A 5415 STRUT DHAV DHC8 DHC8202 2809007 NM NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - DURING INSPECTION, FOUND TWO CHAFED AREA''S IN LOWER INBOARD ENGINE NACELLE SUPPORT STRUT. REPAIRED IN ACCORDANCE WITH ENGINEERING APPROVED REPAIR DRAWING RII COMPLIED WITH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001042300167 20010423 00167 EU 2001 4 23 QXEA0100430 1 20010328 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 476US 11224 SEA - BOTH THE FORE AND AFT EXIT SIGNS FOUND INOPERATIVE. REMOVED AND REPLACED EXIT SIGN CIRCUIT BOARDS. OPERATIONAL C HECKS GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001042300168 20010423 00168 EU 2001 4 23 QXEA0100431 1 20010328 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 476US 11224 SEA - BOTH THE FORE AND AFT EXIT SIGNS FOUND INOPERATIVE. REMOVED AND REPLACED EXIT SIGN CIRCUIT BOARDS. OPERATIONAL C HECKS GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001042300169 20010423 00169 EU 2001 4 23 QXEA0100432 1 20010328 A 3350 XB864041 LIGHT FOKKER FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 477AU 11226 SEA - DURING INSPECTION, FOUND EXCAPE PATH LIGHT ON SEAT 3A/B INOPERATIVE. REMOVED AND REPLACED SEAT LIGHT ASSEMBLY OPE RATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001042300170 20010423 00170 EU 2001 4 23 QXEA0100433 1 20010328 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 498US 11181 SEA - THE EXIT SIGN ABOVE THE FLIGHT COMPARTMENT DOOR WAS FOUND INOPERATIVE. REMOVED AND REPLACED EXIT SIGN ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001042300171 20010423 00171 SO 2001 4 23 C2XA01IA186 1 20010328 A 3260 CONNECTOR EMB 120 EMB120ER 3260203 SO RT MLG DIRTY A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 17728 120182 TYR - FLIGHT 2916, THE CREW REPORTED A SMOKE SMELL IN THE CABIN. MAINTENANCE CLEANED THE WEIGHT ON WHEELS PROXIMITY SWI TCH CANNON PLUG, OPERATIONALLY CHECKED THE PAX SYSTEM WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001042300172 20010423 00172 WP 2001 4 23 ABXA010110 1 20010330 A 3232 ACTUATOR DOUG DC8 DC863 302198A WP RT MLG OUT OF ADJ A ABXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 818AX 84699 2025 46075 AFTER TAKEOFF, THE CREW RECORDED A LANDING GEAR UNSAFE LIGHT WAS ILLUMINATED. THE GEAR AND DOOR LATCH SELECTOR INDICATED THAT THE RIGHT MAIN LANDING GEAR DOOR WAS NOT LATCHED. THE CREW RE-CYCLED THE LANDING GEAR. AFTER RE-CYCLE THE MAIN LAN DING GEAR AND DOOR LATCHING SELECTOR INDICATED THE LEFT AND RIGHT MAIN LANDING GEAR DOORS AND THE RIGHT MAIN LANDING GEA R AS UNLATCHED. MAINTENANCE INSPECTED AND REPLACED THE RIGHT MAIN LANDING GEAR TRIM (BOGIE) CYLINDER ASSEMBLEY AND INSPE CTED AND REPLACED THE RIGHT MAIN LANDING GEAR DOOR PROXIMITY SENSOR TARGET PADDLE. THE LEFT MAIN LANDING GEAR DOOR ACTU ATOR WAS ADJUSTED AND THE DOOR ROLLER WAS ALIGNED WITH THE UPLATCH MECHANISM. OPERATIONAL CHECKS WERE COMPLETED. 2 L 7 4 4F 4A25 2001042300173 20010423 00173 NM 2001 4 23 A6WA200100026 1 20010331 A 6120 CONNECTOR DORNER DO32 DO328100 2996000 NM PCU FAULTY A A6WA E ENGINE SHUTDOWN O OTHER DE DESCENT 1 GL 31 329PH 3007 HL332 DURING DESCENT THE LEFT ENGINE SURGED SEVERAL TIMES. RETARDED POWER LEVER. C/W INFLIGHT SHUTDOWN OF LEFT ENGINE. MAIN TENANCE REMOVED AND REPLACED PCU ELECTRICAL CONNECTOR. 2 H 7 2 4T RT A45NM 2001042300174 20010423 00174 WP 2001 4 23 ABXA010111 1 20010330 A 2420 976J2544 CONTROL PANEL DOUG DC9 DC941 302207N WP COCKPIT FAILED A ABXA O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 959AX 82610 12 47761 IN CRUISE, THE AIRCRAFT EXPERIENCED A RIGHT GENERATOR FAILURE WITH A CROSS TIE LOCKOUT. THE GENERATOR WAS RESET AND IT FAILED AGAIN. THE CREW DECLARED AN EMERGENCY. MAINTENANCE INSPECTED AND DEFERRED THE RIGHT A/C GENERATOR IAW DC-9 MEL. ON 03/31/01 MAINTENANCE INSPECTED AND REPLACED THE GENERATOR CONTROL PANEL AND REMOVED THE DEFERRAL FROM THE AIRCRAFT. 2 L 7 2 4F A6WE 2001042300175 20010423 00175 WP 2001 4 23 ABXA010116 1 20010328 A 5312 5910130392 TEE CHORD DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 51479 47511 THE AFT PRESSURE BULKHEAD NR 2 TEE CAP SHOWED A CRACK INDICATION WITH HIGH FREQUENCY EDDY CURRENT, ADJACENT TO LONGERON 14R. MAINTENANCE INSPECTED AND REPLACED THE NR 2 TEE CAP IAW DC-9 SRM 53-03 FIG 37A. 2 L 7 2 4F A6WE 2001042300176 20010423 00176 WP 2001 4 23 ABXA010115 1 20010328 A 5330 59114111 SKIN DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 51479 47511 A CRACK WAS LOCATED AT THE FORWARD LOWER CARGO DOOR CUTOUT, UPPER FORWARD CORNER. CRACK WAS RADIATING FROM EDGE .2187 L ONG. CRACK WAS LOCATED IN THE EXTERIOR SKIN, VERIFIED BY EDDY CURRENT. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW ABX EA 53100110. 2 L 7 2 4F A6WE 2001042300177 20010423 00177 WP 2001 4 23 ABXA010114 1 20010328 A 5330 99234343 DOUBLER DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 51479 47511 PANEL 5114 CUT OUT HAD CORROSION AROUND NUT PLATES AND BULGED BETWEEN SKIN AND DOUBLER. MAINTENANCE INSPECTED AND REPLA CED THE INTERNAL DOUBLER IAW DOUGLAS DRAWING 9923434 AND DC-9 SRM. 2 L 7 2 4F A6WE 2001042300178 20010423 00178 WP 2001 4 23 ABXA010113 1 20010328 A 5521 5910412510 SPAR DOUG DC9 DC941 302207N WP ELEVATOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 51479 47511 THE RIGHT ELEVATOR REAR SPAR HAD LEVEL 2 CORROSION, FORWARD OF GEAR TAB. MAINTENANCE INSPECTED AND REPLACED THE RIGHT E LEVATOR IAW DC-9 MM 27-30-02. 2 L 7 2 4F A6WE 2001042300179 20010423 00179 WP 2001 4 23 ABXA010112 1 20010328 A 5330 591142837 SKIN DOUG DC9 DC941 302207N WP FUSELAGE BULGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 51479 47511 FUSELAGE SKIN WAS NOTED TO BE BULGING AT STATION 1072. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC9 SRM 53-01 FI G 4. 2 L 7 2 4F A6WE 2001042300180 20010423 00180 NE 2001 4 23 ARWA0010401 2 20010401 A 7200 ENGINE LKHEED 1011 1011385114 WP RROYCE RB211 RB211524B02 54555 NE NR 2 ENGINE VIBRATION A ARWA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 19 260FA 193A1158 NR 2 ENGINE VIBRATION EXCEEDED 2.5 UNITS IN BOTH A & B VIBRATION SELECTIONS. ENGINE SHUT DOWN PLUS RETURNED TO MIA TIME 00:35Z. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED CHIP DETECTORS, EXHAUST COLLECTOR NO DEFECT NOTED. LUBED CLAPPERS . PERFORMED BOROSCOPE INSPECTION ON COMPRESSOR STAGE 6 HP, STAGE 7 HPT REAR FACE NO DEFECT FOUND. ACCOMPLISHED ENGINE RUN UP TEST NR 11 ALL VIBRATION INDICATION WAS WITHIN MM LIMITS IAW MM 71-00-00 PAGE 216. 2 L 7 3 4F 4 F A23WE E12EU 2001042300181 20010423 00181 2001 4 23 A6WA200100027 4 20010329 A 2565 D31050105 SLIDE BAG BAE146 BAE146200A 1500266 EU PAX DOOR UNSERVICEABLE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 607AW 6839 6839 E2052 FOUND THE FWD PAX DOOR EVACUATION SLIDE CABLE RELEASE NOT ATTACHED TO GIRT BAR. MAINTENANCE REMOVED AND REPAIRED EVACUA TION SLIDE. 2 H 7 4 4F RT A49EU 2001042300182 20010423 00182 NM 2001 4 23 QXEA0100435 1 20010309 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-CORROSION ON OUTBOARD FLANGE OF RIGHT HAND INBOARD SEAT TRACK, STATION 580-600 (CARGO PIT). REPAIRED IAW DHC-8 SRM 51-20-16, SRM 51-20-36, AND RD-8-53-784. 2 H 7 2 4T RT A13NM 2001042300183 20010423 00183 NM 2001 4 23 QXEA0100436 1 20010323 A 5230 DOOR DHAV DHC8 DHC8102 2809003 NM CARGO BAY OUT OF TOLERANCE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-RIGGED MCD, DOOR IS NOT WITHIN CLEARANCE LIMITS OF STOP 4. REPAIRED IAW HORIZON AIR EA 9-52-116. 2 H 7 2 4T RT A13NM 2001042300184 20010423 00184 NM 2001 4 23 QXEA0100437 1 20010323 A 5230 DOOR DHAV DHC8 DHC8102 2809003 NM CARGO BAY OUT OF TOLERANCE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 PDX-RIGGED MCD, DOOR IS NOT WITHIN CLEARANCE LIMITS OF STOP 2. REPAIRED IAW HORIZON AIR EA 9-52-116. 2 H 7 2 4T RT A13NM 2001042300185 20010423 00185 WP 2001 4 23 ABXA010117 1 20010405 A 2740 2715413 SHAFT DOUG DC8 DC863 302198A WP FUSELAGE SHEARED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 THE HORIZONTAL STABILIZER OPERATING BULKHEAD, LEFT SIDE AFT END, HAD A SHEARED SHAFT. 2 L 7 4 4F 4A25 2001042300186 20010423 00186 WP 2001 4 23 ABXA010121 1 20010409 A 5347 59108205 SEAT TRACK DOUG DC9 DC932 3022066 WP CABIN CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 984AX 68919 47258 SEAT TRACK AT FUSELAGE STATION 200 RBL 44 WAS FOUND TO BE CORRODED. MAINTENANCE INSPECTED AND REPLACED THE SEAT TRACK F ROM FS 145 TO FS 200, IAW DC-9 SRM 51-30-1. 2 L 7 2 4F A6WE 2001042300187 20010423 00187 WP 2001 4 23 ABXA010120 1 20010409 A 5311 9919619503 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 984AX 68919 47258 FUSELAGE FRAME AT STATION 737 LEFT SIDE WAS FOUND TO BE CRACKED. MAINTENANCE INSPECTED AND REPLACED THE MAIN FRAME AT S TA 737 IAW ABX EA 53400325-001. 2 L 7 2 4F A6WE 2001042300188 20010423 00188 WP 2001 4 23 ABXA010119 1 20010409 A 5347 59108207 SEAT TRACK DOUG DC9 DC932 3022066 WP CABIN CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 984AX 68919 47258 SEAT TRACK LOCATED AT FUSELAGE STATION 160 LBL 44 WAS EXFOLIATED. MAINTENANCE INSPECTED AND REPLACED THE SEAT TRACK FRO M FS 160 TO FS 218 IAW DC-9 SRM 51-30-1. 2 L 7 2 4F A6WE 2001042300189 20010423 00189 NM 2001 4 23 ABXA010118 1 20010405 A 2897 AG1025AA05 WIRE BOEING 767 767205 1385121 NM FUEL TANK PROBE CHAFED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 713AX 60042 23058 LEFT WING FUEL QUANTITY PROBE WIRING AT ACCESS PANEL 531BB WAS CHAFED DOWN TO BARE WIRE. MAINTENANCE INSPECTED AND REPL ACED THE LEFT AUX FUEL QUANTITY WIRING HARNESS. 2 L 7 2 4F RT A1NM 2001042300190 20010423 00190 EA 2001 4 23 FWRA2001001 2 20010403 A 8520 LW19341 CAMSHAFT PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA HARTZL HCE3Y HCE3YR2A GL RT ENGINE DAMAGED E FWRA K NONE O OTHER IN INSP/MAINT 1 AL 01 222CC 1497 8052095 RL258768A DJ8596A DURING DISASSEMBLY OF ENGINE DUE TO A CRACK IN CRANKCASE FOUND ONE CAMSHAFT LOBE GONE AND ONE TAPPET BODY DAMAGED. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 2001042300191 20010423 00191 EU 2001 4 23 SIMA0694 1 20010227 A 5320 S5367128100001 BRACKET AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE PAX DOOR SPRING ATTACH BRACKETS BETWEEN FRAMES 39 AND 40 LEFT C ORRODED. MAINTENANCE REMOVED AND REPLACED THE ATTACH BRACKETS IAW SRM 51-25-04. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001042300192 20010423 00192 EU 2001 4 23 20010420SG001 1 20010227 A 5320 S5367127200201 BRACKET AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE PAX DOOR SPRING ATTACH BRACKETS BETWEEN FRAMES 39 AND 40 LEFT C ORRODED. MAINTENANCE REMOVED AND REPLACED THE ATTACH BRACKETS IAW SRM 51-25-04. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0694. (M) 2 H 7 2 4T RT A53EU 2001042300193 20010423 00193 EU 2001 4 23 SIMA0693 1 20010226 A 5320 S52678008100 FLOOR SUPPORT AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT AND RIGHT FLOOR ZEE MEMBER BETWEEN FRAMES 39 ND 41 CORRODE D. MAINTENANCE REMOVED AND REPLACED THE ZEE MEMBERS IAW SRM 51-25-04. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001042300194 20010423 00194 EU 2001 4 23 20010420SG002 1 20010226 A 5320 S53678008216 FLOOR SUPPORT AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT AND RIGHT FLOOR ZEE MEMBER BETWEEN FRAMES 39 ND 41 CORRODE D. MAINTENANCE REMOVED AND REPLACED THE ZEE MEMBERS IAW SRM 51-25-04. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0693. (M) 2 H 7 2 4T RT A53EU 2001042300195 20010423 00195 EU 2001 4 23 SIMA0642 1 20010305 A 3350 0341516 FUSE AEROSP ATR72 ATR72212 EU CABIN BLOWN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 426AT 426 DFW - DURING SCHEDULED PS-2 CHECK, MAINTENANCE FOUND A FLOOR PROXIMITY LIGHT AT 6AB AND THE PASSENGER DOOR EMERGENCY LIG HT TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE FOR THE FLOOR LIGHT AND REPLACED A FUSE IN THE POWER SUPPLY. OP''S CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001042300196 20010423 00196 WP 2001 4 23 DHL2001806545 1 20010313 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - AFT FUSELAGE EXTERIOR-UPPER PART VERTICAL STABILIZER TO FUSELAGE ANGLE SHOWS CORROSION, STA FS 000 RT SIDE.COR RECTIVE ACTION - REMOVED LEVEL I CORROSION FROM AFT FUSELAGE EXTERIOR UPPER PART VERTICAL STABILIZER TO FUSELAGE ANGLE S TA FS 000 RH IAW SRM 51-1-8 PAGE 17 AND 18 LESS 2%. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B PAGE 1 AND 2 TO 12. ST ATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300197 20010423 00197 EU 2001 4 23 SIMA0692 1 20010228 A 5320 S5367800826801 FLOOR SUPPORT AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT FLOOR SUPPORTS BETWEEN FRAMES 38-39 AND 39-40 CORRODED, AN D THE RIGHT FLOOR SUPPORTS BETWEEN FRAMES 38-39 AND 36-38 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORTS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001042300198 20010423 00198 EU 2001 4 23 20010420SG003 1 20010228 A 5320 S5367800826901 FLOOR SUPPORT AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT FLOOR SUPPORTS BETWEEN FRAMES 38-39 AND 39-40 CORRODED, AN D THE RIGHT FLOOR SUPPORTS BETWEEN FRAMES 38-39 AND 36-38 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORTS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0692. (M) 2 H 7 2 4T RT A53EU 2001042300199 20010423 00199 EU 2001 4 23 20010420SG004 1 20010228 A 5320 S5367800920102 FLOOR SUPPORT AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT FLOOR SUPPORTS BETWEEN FRAMES 38-39 AND 39-40 CORRODED, AN D THE RIGHT FLOOR SUPPORTS BETWEEN FRAMES 38-39 AND 36-38 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORTS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0692. (M) 2 H 7 2 4T RT A53EU 2001042300200 20010423 00200 EU 2001 4 23 20010420SG005 1 20010228 A 5320 S5367800021451 FLOOR SUPPORT AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT FLOOR SUPPORTS BETWEEN FRAMES 38-39 AND 39-40 CORRODED, AN D THE RIGHT FLOOR SUPPORTS BETWEEN FRAMES 38-39 AND 36-38 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORTS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0692. (M) 2 H 7 2 4T RT A53EU 2001042300201 20010423 00201 EU 2001 4 23 SIMA0691 1 20010226 A 5320 S53671217336 TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE PAX DOOR DRAIN TRACK AND SERVICE DOOR DRAIN TRACK BETWEEN FRAME S 36 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE DRAIN TRACKS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SER VICE. (M) 2 H 7 2 4T RT A53EU 2001042300202 20010423 00202 EU 2001 4 23 20010420SG006 1 20010226 A 5320 S53671217336 TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE PAX DOOR DRAIN TRACK AND SERVICE DOOR DRAIN TRACK BETWEEN FRAME S 36 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE DRAIN TRACKS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SER VICE. REF SIMA0691 (M) 2 H 7 2 4T RT A53EU 2001042300203 20010423 00203 EU 2001 4 23 SIMA0697 1 20010226 A 5320 S5367121729402 SILL AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - FOUND DURING CPCP-2 INSPECTION MAINTENANCE, REPORTED THE PAX DOOR SILL PLATE BETWEEN FRAME 36 AND 39 CORRODED. MA INTENANCE REMOVED AND REPLACED THE SILL PLATE IAW SRM 51-25-04. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001042300204 20010423 00204 EU 2001 4 23 SIMA0696 1 20010227 A 5330 S5367130501000 SKIN AEROSP ATR72 ATR72212 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-2 INSPECTION MAINTENANCE CLEARED TDMI NR 260MQ5301D5, DENT IN RIGHT SIDE OF FUSELAGE AT FRAME 40 STRIN GER 17. MAINTENANCE REPAIRED THE DENT IAW SRM 53-00-00. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001042300206 20010423 00206 WP 2001 4 23 DHL2001806572 1 20010319 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP CABIN CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - MAIN CARGO FLOOR SUPPORT ANGLE CRACKED 1/2 INCH AND DEFORMED BL.0 AT STA 8.000. REMOVED CRACKED FLOOR SUPPOR T ANGLE AND FABRICATED FLOOR SUPPORT ANGLE. IAW SRM 53-2-0 PAGE 2E/2F. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. I NSTALLED FLOOR SUPPORT ANGLE IAW SRM 53-2-0 PAGE 2E/2F. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300207 20010423 00207 WP 2001 4 23 DHL2001806573 1 20010312 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LT WING L/E RIB UPPER PART 1/2 INCH CRACK AT STA XFS 660. PERFORMED STOP DRILL AND FAVRICATE REINFORCING ANGL E IAW SRM 53-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2 . STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300208 20010423 00208 EU 2001 4 23 DHL2001364014 1 20010414 A 5320 FLANGE AIRBUS 300 A300B4203 3930306 EU DOOR FRAME SEAL CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 0141 FWD CARGO DOOR JAMB SEAL FLANGE CRACKED AT FWD LOWER CORNER. TRIMMED CRACK DAMAGE & FABRICATED REPAIR ANGLE DOUBLER IA W SRM A300 51-41-30. ALODINED & PRIMED IAW SRM A300 51-40-12. INSTALLED REPAIR ANGLE DOUBLER IAW SRM A300 51-41-30. T OUCHED-UP PAINT IN REPAIR AREA IAW SRM A300 51-40-12. REINSTALLED DOOR JAMB CLOSEOUT PNLS IAW SRM A300 51-30-30. STATU S-CLOSED. 2 L 7 2 4F RT A35EU 2001042300209 20010423 00209 WP 2001 4 23 DHL2001806574 1 20010313 A 3010 DIFFUSER DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LT WING L/E ANTI-ICE DIFFUSER 1 INCH CRACK AT LWR. PART STA XFS 728.750. PERFORMED STOP HOLE AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B AND INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300210 20010423 00210 WP 2001 4 23 DHL2001806575 1 20010313 A 3010 DIFFUSER DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LT WING L/E ANTI-ICE DIFFUSER HAS A 1/2 INCH CRACK AT LWR PART STA XFS 747.500. PERFORMED STOP HOLE AND FABRI CATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300211 20010423 00211 WP 2001 4 23 DHL2001806576 1 20010311 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK, LT WING L/E RIB LOWER PART HAS A 1/2 INCH CRACK AT STA XFS 803.750.PERFORMED STOP DRILL AND FABRICATED REINFO RCING ANGLE IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57- 2-0 FIG 2. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300212 20010423 00212 WP 2001 4 23 DHL2001806577 1 20010311 A 5700 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LT WING L/E RIB UPPER PART HAS A 1/2 INCH CRACK AT STA XFS 785.250. PERFORMED STOP DRILL AND FABRICATED REIN FORCING ANGLE IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 5 7-2-0 FIG 2. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300213 20010423 00213 WP 2001 4 23 DHL2001806578 1 20010311 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LT WING L/E RIB UPPER PART HAS A 1 INCH CRACK AT STA XFS 822.950. PERFORMED STOP DRILL AND FABRICATED REINFO RCING ANGLE IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57- 2-0 FIG 2. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300214 20010423 00214 WP 2001 4 23 DHL2001806579 1 20010311 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LT WING L/E RIB UPPER PART HAS A 1 INCH CRACK AT STA XFS 841.250. PERFORMED STOP DRILL AND FABRICATED REINFO RCING ANGLE IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57- 2-0 FIG 2. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300215 20010423 00215 WP 2001 4 23 DHL2001806580 1 20010311 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LT WING L/E RIB UPPER PART HAS A 1/2 INCH CRACK AT STA XFS 041.950.PERFORMED STOP DRILL AND FABRICATED DOUBLE R IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300216 20010423 00216 WP 2001 4 23 DHL2001806581 1 20010313 A 3010 DIFFUSER DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LT WING ANTI-ICE DIFFUSER UPPER PART HAS A 1 INCH CRACK AT STA XFS 728.720. PERFORMED STOP DRILL AND FABRICAT ED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IA W SRM 57-2-0 FIG 2. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300217 20010423 00217 WP 2001 4 23 DHL2001806582 1 20010308 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BULKHEAD CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - AFT BULKHEAD LINING SUPPORT ANGLE LOWER PART AT STA 1766.000 CRACKED 1 INCH. REMOVED CRACKED LINING SUPPORT ING ANGLE IAW SRM 53-2-5 PAGE 6A. FABRICATED NEW SUPPORTING ANGLE IAW SRM 53-2-5 PAGE 6A. TREATED AND PRIMED IAW SRM 51 -1-8B AND INSTALLED NEW LINING SUPPORTING ANGLE IAW SRM 53-2-5 PAGE 6A. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300218 20010423 00218 WP 2001 4 23 DHL2001806584 1 20010318 A 5320 WEB DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - MAIN CARGO COMPARTMENT SUBFLOOR SHOWS 02 EA CRACKS 1/4 INCH. RBL 52 STA 55.000. PERFORMED STOP HOLE IAW SRM 53-2-0 FIG 1B. FABRICATED DOUBLER IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. AND INSTALLED DOUB LER IAW SRM 53-2-0 FIG 1B. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300219 20010423 00219 NM 2001 4 23 DL73K010488 1 20010325 A 2700 TORQUE TUBE BOEING 737 737232 1384475 NM ELEVATOR STUCK A DALA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SO 27 321DL 23093 ELVEATOR JAMMED AND STUCK IN FLIGHT CONTINUED STICKING AND RELEASING THROUGH REST OF FLIGHT DIVERTED TO ATL TRIED ISOLA TED A AND B DID NOT HELP. REPLACED ELEVATOR INPUT TORQUE TUBE 2 L 7 2 4F RT A16WE 2001042300220 20010423 00220 NM 2001 4 23 DL72W010509 1 20010328 A 2121 GASPER FAN BOEING 727 727247 138408F NM CABIN FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 2816W 20872 PAX REPORTED ELECT SMELL IN CABIN, STRONGEST NEAR ROW 14 OCCURED JUST PRIOR TO LANDING AND DURING TAXI TO GATE.A PAX IN THE VICINITY OF ROW 14 ALSO MENTIONED THE SOUND OF HYD PUMPS GETTING LOUDER JUST PRIOR TO LANDING. FOUND GASPER FAN BAD. REPLACED SAME. 2 L 7 3 4F A3WE 2001042300221 20010423 00221 NM 2001 4 23 DL72S010510 1 20010327 A 7120 MOUNT BOEING 727 727232 1384082 NM NR 3 PYLON DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 528DA 21702 INSPECTION OF THE NR 3 ENGINE PYLON FWD ENGINE MOUNT ATTACH FITTING HOLES PER AD 97-05-08 FOUND 2 HOLES OUT OF LIMITS. THE HOLES WERE HFEC INSPECTED TO ENSURE NO CRACKS AND OVERSIZED TO THE NEXT ALLOWABLE SIZE OF FED EX S/B 2000-5410A01 . LARGER DIAMETER BOLTS WERE THEN INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 380396-14AD. 2 L 7 3 4F A3WE 2001042300222 20010423 00222 NM 2001 4 23 DL757010511 1 20010327 A 5330 146N37505 SKIN BOEING 757 757232 1384965 NM FUSELAGE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 636DL 23763 INSPECTION OF AN EXISTING SKIN REPAIR BETWEEN FS 1681 & 1701 AND BETWEEN STRINGERS 18L & 19L REVEALED GOUGE DAMAGE TO TH EREPAIR. THE REPAIR WAS REMOVED AND THE FUSELAGE SKIN CUT TO REMOVE ALL REPAIR FASTENER HOLES AND DAMAGE. THE FINAL CUTOUT WAS 10.5 INCHES X 10.5 INCHES. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER PER ER/A 380355-14, REV A. 2 L 7 2 4F RT A2NM 2001042300223 20010423 00223 NM 2001 4 23 DL73K010512 1 20010327 A 5330 SKIN BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 237WA 23185 A TYPICAL CRACK WAS FOUND IN THE LOWER AFT CORNER OF THE FWD GALLEY DOOR OPENING. THE CRACK WAS 1.4 INCHES LONG IN THE SKIN AND BONDED DOUBLER ONLY (BEAR STRAP NOT CRACKED). THE CRACK WAS ROUTED OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER PER B737-200 SRM 53-30-03 FIG. 26 AND ER/A 380408-14, REV A. 2 L 7 2 4F A16WE 2001042300224 20010423 00224 NM 2001 4 23 DLM88010514 1 20010328 A 4990 38005041 APU DOUG MD88 MD88 3023688 NM APU BAY LEAKING A DALA D RETURN TO BLOCK K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 903DE 9200 0 P80524 53380 SMOKE ALARM GOING OFF IN AFT LAV HAZE OBSERVED BY FLT ATTENDENT - REPLACED APU FOR OIL LEAK - PERFORMED DUCT BURNOUT 2 L 7 2 4F RT A6WE 2001042300225 20010423 00225 NM 2001 4 23 DLM88010515 1 20010328 A 3397 WIRE DOUG MD88 MD88 3023688 NM SEAT 10D BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 944DL 49817 EMERGENCY LIGHT INOP IN SEAT 10D ON L/O INSPECTION. REPLACED LIGHT ASSY CHECKS OK 2 L 7 2 4F RT A6WE 2001042300226 20010423 00226 NM 2001 4 23 DL72S010516 1 20010329 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 8 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 410DA 21222 1/2 INCH CRACK IN NR 8 L/E SLAT COVE SKIN ANGLE AT ANTI-ICE DUCT CUTOUT REPAIRED PER MM 57-54-000-8 2 L 7 3 4F A3WE 2001042300227 20010423 00227 2001 4 23 DL73K010517 4 20010330 A 3423 2591201922 COUPLER BOEING 737 737232 1384475 NM COMPASS FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 315DL 23087 NR 2 COMPASS SYSTEM IS THIRTY DEGREES OFF CAPTS HEADING AND WILL NOT SLAVE UP AND STAY SLAVED. REPLACED NR 2 COMPASS CO UPLER OP CHECKS NORMAL. ITEM CAUSED AIR TURN BACK 2 L 7 2 4F RT A16WE 2001042300228 20010423 00228 NM 2001 4 23 DL73E010518 1 20010330 A 5315 FLOORBEAM BOEING 737 7372S3 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 367DL 21774 DURING ACCOMPLISHMENT OF INSPECTION PER S/B 737-57-1210. A CRACK WAS FOUND IN THE PANEL ATTACH HOLE AT FS 660. THE CRA CK WAS CUT OUT AND THE AREA REPAIRED BY S/B 737-57-1210.THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001042300229 20010423 00229 NM 2001 4 23 DL73K010519 1 20010330 A 5343 654654319 ATTACH FITTING BOEING 737 737232 1384475 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 316DL 23088 THE LT MLG STRUT SUPPORT FITTING FRAME AT FS 685 HAD CORROSION AT THE SIDE STRUT ATTACH LUG LOCATED AT LBL 68.5 AND WL 1 88.5. CORROSION WAS FOUND IN THE BORE AND BOTH FACES. CORROSION WAS REMOVED AND A REPAIR SLEEVE INSTALLED.THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001042300230 20010423 00230 NM 2001 4 23 DL76G010521 1 20010330 A 2560 CHARGER BOEING 767 7673P6 1385105 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 152DL 24984 LEFT EMERGENCY SLIDE SQUIB TEST FAILED DURING EPDC TEST. REPLACED CHARGER M00962 AND BATTERY. ESCAPE SLIDE SQUIBS TES T GOOD. 2 L 7 2 4F RT A1NM 2001042300231 20010423 00231 2001 4 23 DLM11010522 4 20010330 A 3460 4059050912 FMC DOUG MD11 MD11 3023602 NM FWD E/E BAY FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 804DE 48475 IN CRUISE LAV SMOKE AND CREW REST SMOKE DETECTORS TRIPPED. ELECTRICAL SMELL NOTED IN COCKPIT FWD AND MID CABINS. SMOKE ALSO NOTED IN CREW REST AREA. T/S FOUND FMC 2 INOP. FOUND EVIDENCE OF ELECTRICAL SMOKE ON TOP OF UNIT. REMOVED AND RE PLACED UNIT RTS PASSED RAN ALL GALLEY EQUIP AND IFE NO SMOKE/SMELL NOTED CHECKED GOOD. 2 L 7 3 4F RT A22WE 2001042300232 20010423 00232 NM 2001 4 23 DL72S010523 1 20010330 A 2913 PUMP BOEING 727 727232 1384082 NM NR 1 AND 2 B HYD FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 538DA 22076 DURING CLIMB CHECK SWITCHED THE NR 1 B ELECTRIC PUMP OFF AND NOTICED PRESSURE FLUCTUATION ON B SYSTEM GUAGE. TURNED NR 1 ELEC PUMP BACK ON AND SEVERAL SECONDS LATER LOW NR 1 PUMP LOW PRESSURE LIGHT ILLUMINATED AND SYSTEM PRESSURE DROPPED TO 2200 PSI- UPON EXAM FOUND NR 1B ELECTRIC PUMP C/B POPPPED-PERFORMED POM PROCEDURE-LANDED IN ATL. REPLACED B SYSTEM H YD. PUMPS, CKS GD. 2 L 7 3 4F A3WE 2001042300233 20010423 00233 NM 2001 4 23 DL76L010524 1 20010330 A 3350 POWER SUPPLY BOEING 767 767332 1382001 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 171DN 24759 ON L/O FOUND EXT EMERGENCY SLIDE LIGHT ON 2L INOP. REPLACED POWER SUPPLY. 2 L 7 2 4F RT A1NM 2001042300234 20010423 00234 NM 2001 4 23 DL76L010526 1 20010331 A 2530 FAN BOEING 767 767332 1382001 NM GALLEY OVEN FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 192DN 28449 ABOUT 2 HOURS INTO FLT. THERE WAS A SLIGHT ACRID SMELL IN THE COCKPIT. RECIRC FANS WERE TURNED OFF ,SMELL STOPPED. W HILE TROUBLE SHOOTING FOUND THAT SMELL WAS NO LONGER PRESENT WITH FWD GALLEY POWER OFF. INSPECTED FWD GALLEY AREA & LOWER COCKPIT FLOOR. FOUND LOWER OVEN IN FWD. GALLEY WITH DEFECTIVE FAN. REPLACED OVEN. 2 L 7 2 4F RT A1NM 2001042300235 20010423 00235 NM 2001 4 23 DL733010527 1 20010331 A 3211 ATTACH FITTING BOEING 737 737347 1384647 NM NLG BROKEN A DALA O OTHER E VIBRATION/BUFFET AP APPROACH 1 SO 27 304WA 23345 DURING GEAR EXTENSION THE NOSEGEAR DID NOT EXTEND. THE VALVES COULD BE HEARD SHIFTING BUT THE NOSEGEAR REMAINED UP. TH E GEAR WAS CYCLED 3 TIMES WITHOUT MOVING THE NOSE GEAR. THE MLG OPERATED NORMALLY. FOLLOWED POM PROCEDURES ON THE 4TH ATTEMPT THE NOSEGEAR CAME DOWN NORMALLY WITH PROPER INDICATION AND LOCKED. FOUND NLG LOCK ACTUATOR DAMAGED. REPLACED NOSEGEAR ACT PER MM.SWING NLG CHECKS OK. 2 L 7 2 4F RT A16WE 2001042300236 20010423 00236 NM 2001 4 23 DL777010528 1 20010401 A 2530 COFFEEMAKER BOEING 777 777232 1385232 NM AFT GALLEY SHORTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 860DA 29951 REAR COFFEE MAKER SHORTED OUT REPLACED DISPENSER. 2 L 7 2 4F RT T00001SE 2001042300237 20010423 00237 NM 2001 4 23 DL72E010529 1 20010401 A 3350 900835A BATTERY PACK BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 282WA 21484 FOUND AFT EMERGENCY EXIT BATTERY DEAD. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 2001042300238 20010423 00238 NM 2001 4 23 DL72L010530 1 20010401 A 3350 SEAT BELT BOEING 727 727232 1384082 NM SEAT 11 WORN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 510DA 21312 EXIT PATH LITE AT SEAT ROW 11 DEF INOPERATIVE. REPLACED SEAT HARNESS. CKS NML. 2 L 7 3 4F A3WE 2001042300239 20010423 00239 NM 2001 4 23 DL73K010532 1 20010402 A 5343 65465445001 FITTING BOEING 737 737232 1384475 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 316DL 23088 THE LT MLG STRUT SUPPORT FITTING FRAME INSTALLATION HAD CORROSION LOCATED IN THE BORE. THE FITTING IS LOCATED AT FS 6 95, LBL 68.5 AND WL 188.5. THE CORROSION WAS REMOVED AND A REPAIR SLEEVE INSTALLED. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001042300240 20010423 00240 NM 2001 4 23 DL73K010533 1 20010402 A 5342 FITTING BOEING 737 737232 1384475 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 316DL 23088 CORROSION WAS FOUND IN THE BORE AND FACES OF THE LT AND RT FUSELAGE CLEVIS LUGS FOR THE HORIZONTAL STABILIZER. THE COR ROSION WAS REMOVED AND NEW BUSHINGS WERE INSTALLED PER ERA 397371-14AD AT HMV. 2 L 7 2 4F RT A16WE 2001042300241 20010423 00241 NM 2001 4 23 DL73K010534 1 20010402 A 5551 FITTING BOEING 737 737232 1384475 NM HORIZOTAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 316DL 23088 CORROSION WAS FOUND ON THE LT AND RT HORIZONTAL STABILIZER ATTACH FITTINGS ON BOTH THE BORES AND FACES. THE CORROSION W AS REMOVED AND NEW BUSHINGS INSTALLED PER 397372-14 AT HMV. 2 L 7 2 4F RT A16WE 2001042300242 20010423 00242 NM 2001 4 23 DL73K010535 1 20010402 A 5342 6546585503 STRAP BOEING 737 737232 1384475 NM HORIZONTAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 316DL 23088 CRACKS WERE FOUND AT THE CUTOUT IN THE FUSELAGE FOR THE HORIZONTAL STABILIZER SIMILIAR TO THE TYPICAL CRACKS OF S/B 737 -53-1134. CRACKS WERE FOUND IN THE LT & RT STINGER 12 STRAP, FS 1140, AND THE LT & RT FS 1138 FRAME STRAPS. THE DAMAGE WAS REPAIRED PER SRM 53-00-01, FIGURE 22 AND 53-30-3, FIG. 30. 2 L 7 2 4F RT A16WE 2001042300243 20010423 00243 NM 2001 4 23 DL76S010536 1 20010328 A 5720 111T20055 STIFFENER BOEING 767 767332 1382001 NM WING CENTER BOX CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 128DL 24078 THE WING CENTER SECTION FRONT SPAR VERTICAL STIFFENER LOCATED AT LBL 10.94 WAS FOUND CRACKED AT ITS TOP END. THE DAMAGE WAS IN THE WEB OF THE STIFFENER AT THE OVERWING LONGITUDINAL FLOORBEAM TO STIFFENER JOINT. 2 L 7 2 4F RT A1NM 2001042300244 20010423 00244 NM 2001 4 23 DL757010537 1 20010330 A 5315 146N51114 FLOORBEAM BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 604DL 22811 THE UPPER CAP OF THE FS 1681 FLOOR BEAM WAS FOUND WITH NUMEROUS AREAS OF CORROSION ALONG ITS LENGTH. THE UPPER CAP WAS TRIMMED OFF ALONT ITS FULL LENGTH FROM LBL 60 TO RBL 60. A NEW CAP WAS FABRICATED FROM AN ALUMINUM EXTRUSION AND INSTAL LED PER ER/A 380020-14, REV A. 2 L 7 2 4F RT A2NM 2001042300245 20010423 00245 NM 2001 4 23 DL757010538 1 20010330 A 5320 143N85122 SILL BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 604DL 22811 THE C1 DOOR OPENING LOWER SILL WAS CORRODED, REQUIRING REPLACEMENT OF THE SILL OUTER CHORD. TO FACILITATE INSTALLATI ON OF A NEW CHORD, THE FS 620 CLOSING FRAME OUTER CHORD AND WEB WERE CUT BETWEEN STRINGERS 25R & 26R AND A SECTION TEMPO RARILY REMOVED FOR ACCESS. THE SECTIONS WERE REINSTALLED WITH ALUMINUM ANGLE CHORD SPLICES AND AN ALUMINUM DOUB LER WEB SPLICE INSTALLED PER ER/A 380263-14. 2 L 7 2 4F RT A2NM 2001042300246 20010423 00246 NM 2001 4 23 DL73K010539 1 20010401 A 5330 654577561 SKIN BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 THE FUSELAGE SKIN WAS FOUND WITH A 3 INCH CRACK JUST BELOW STRINGER 18 RT AT APPROXIMATELY FS 760. THE CRACK LOCATION W AS FWD OF AN EXISTING REPAIR FOR SIMILAR CRACKING. THE NEW CRACK WAS REMOVED WITH A 3 INCHES X 1.5 INCHES CUTOUT AND TH E EXISTINGREPAIR REMOVED. THE 2 CUTOUTS OF THE PREVIOUS REPAIR AND ALL FASTENER HOLES WERE HFEC INSPECTED WITH NO CRA CKING. THEDAMAGED AREAS WERE REPAIRED WITH AN ALUMINUM DOUBLER PER ERA 2 L 7 2 4F A16WE 2001042300247 20010423 00247 NM 2001 4 23 DL76L010540 1 20010402 A 3600 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 178DN 8359 25143 ON T/O GOT RT HP BLEED AND FOLLOWED POM. RETURNED TO CVG. REPLACED NBR 2 ENG HPSO VALVE PER MM 36-11-07-4-03 NO FURTH ER FAULTS. 2 L 7 2 4F 4 F RT A1NM E24NE 2001042300248 20010423 00248 NM 2001 4 23 DL72L010541 1 20010402 A 5720 STIFFENER BOEING 727 727232 1384082 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 512DA 21314 IB SPAR STIFFENER IS CRACKED AT NR 2 SLAT IB TRACK. REPAIR PER M/M 57-20-021-8 2 L 7 3 4F A3WE 2001042300249 20010423 00249 NE 2001 4 23 DL76L010542 2 20010402 A 7297 WIRE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE BROKEN A DALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 27 178DN 41737 25143 724178 RIGHT ENGINE HPSOV ON TAKEOFF ROLL, RETURN TO CVG. . REPAIRED BROKEN WIRE ON D4208P RAN ENGINE LEAK AND OPS CHECKS G OOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2001042300250 20010423 00250 NM 2001 4 23 DLM88010543 1 20010402 A 4990 O-RING DOUG MD88 MD88 3023688 NM APU CHIP DETECT LEAKING A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 929DL 10104 49716 AFT CABIN SMOKE DETECTERS GOING OFF IN FLIGHT. FOUND 1 AFT SMOKE DETECTOR BAD AND APU OIL LEAK.NO ODER NOTICED IN CABIN . PERFORMED OP 5088 T/S FOR SMOKE IN CABIN AND PERFORMED DUCT BURN OUT.REPLACED SMOKE DET. 2 L 7 2 4F RT A6WE 2001042300251 20010423 00251 NM 2001 4 23 DLM88010544 1 20010402 A 2150 LINE DOUG MD88 MD88 3023688 NM HYD SYSTEM LEAKING A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 27 978DL 53259 BAD ODOR IN CABIN DURING TAKEOFF AND LANDING. FOUND HYDRAULIC LINE LEAKING ON LEFT THRUST REVERSER CONTROL VALVE. TI GHTENED LINE. PERFORMED OPN 5088 DUCT BURNOUT 2 L 7 2 4F RT A6WE 2001042300252 20010423 00252 NM 2001 4 23 DL757010545 1 20010401 A 3350 BPS73 BATTERY PACK BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 603DL 22810 FOUND ON LO FC EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK OPS NORMAL 2 L 7 2 4F RT A2NM 2001042300253 20010423 00253 NM 2001 4 23 DL72S010546 1 20010402 A 5310 65561001 DOOR FRAME BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 528DA 21702 INSPECTION OF THE C1 DOOR OPENING FWD FRAME AT FS 560 PER AD 99-23-13 REVEALED 3 CRACKS IN THE WEB (1 BELOW THE NR 4 S TOP AND 2 BELOW THE NR 1 STOP). THE WEB WAS CUT AT THE NR 6 STOP AND THE UPPER SECTION WITH THE CRACKS REMOVED. WEB RE MOVAL REVEALED SEVERAL CORRODED FASTENER HOLES IN THE INNER CHORD WHICH WAS THEN CUT TO REMOVE THE DAMAGED SECTION. NEW SECTIONS OF WEB AND CHORD WERE SPLICED PER SRM 51-40. 2 L 7 3 4F A3WE 2001042300254 20010423 00254 NM 2001 4 23 DLM11010547 1 20010403 A 2750 CONTROL UNIT DOUG MD11 MD11 3023602 NM TE FLAPS FAILED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 815DE 48624 RIGHT OUTBOARD FLAP POS INDICATOR INOP. RESET FCC NR 1 ALSO RESET FLAP INDICATION CKS OK 2 L 7 3 4F RT A22WE 2001042300255 20010423 00255 NM 2001 4 23 DLM11010549 1 20010402 A 2530 COMPRESSOR DOUG MD11 MD11 3023602 NM GALLEY CHILLER OVERHEATED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 807DE 48478 PRIOR TO DEPARTURE FWD GALLEY CHILLER COMPRESSOR MAKING VERY LOUD NOISE AND GETTING WARM HOT / SMOKE - REPLACED CHILLE R. 2 L 7 3 4F RT A22WE 2001042300256 20010423 00256 NM 2001 4 23 DLM88010550 1 20010403 A 2910 AS15308K0254 HOSE DOUG MD88 MD88 3023688 NM RT HYD SYS CHAFED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 918DE 49959 DURING FLT RT HYD QTY WENT TO ZERO WIH LOSS OF PRESSURE. MTC FOUND HYD HOSE WITH HOLE IN IT FROM CHAFING. REPLACED RT SY STEM HYDRAULIC FILTER SUPPLY LINE - REPLACED FILTER AND ENGINE DRIVEN PUMP 2 L 7 2 4F RT A6WE 2001042300257 20010423 00257 NM 2001 4 23 DL72S010551 1 20010403 A 2751 INDICATOR BOEING 727 727232 1384082 NM COCKPIT STUCK A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 531DA 21814 UPON FLAP RETRACTION OUTBOARD FLAPS REMAINED AT 5 DEG. INBOARD WENT TO 2 DEG. AND L/E FLAP LIGHT REMAINED AMBER. RAN CH ECK LIST. REPLACED OTBD FLAP INDICATOR. RAN FLAPS SEVERAL TIMES OPERATION CKS OK. 2 L 7 3 4F A3WE 2001042300258 20010423 00258 2001 4 23 DL76K010552 4 20010403 A 2565 BATTERY PACK BOEING 767 767332 1382001 NM RT SLIDE DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 171DZ 29690 DURING TRANSIT CHECK. FOUND RIGHT EMERGENCY ESCAPE SLIDE TEST ONE INOP. REPLACED RIGHT EMERGENCY OVERWING ESCAPE SLIDE BATTERY PACK.OPERATION NOW NORMAL. 2 L 7 2 4F RT A1NM 2001042300259 20010423 00259 NM 2001 4 23 DL72S010553 1 20010403 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM FWD CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 538DA 22076 FOUND EMERGENCY EXIT LIGHT BATTERY DISCHARGED. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 2001042300260 20010423 00260 NM 2001 4 23 DL73E010554 1 20010404 A 5330 65457789 SKIN BOEING 737 7372S3 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 367DL 21774 A CRACK WAS FOUND IN THE LOWER HINGE CUTOUT OF THE AFT GALLEY DOOR. THE CRACK WAS COMMON TO THE SKIN, BONDED DOUBLER A ND THE BEAR STRAP. THE CRACK WAS CUT OUT AND A DOUBLER / TRIPLER INSTALLED AT HMV. 2 L 7 2 4F RT A16WE 2001042300261 20010423 00261 NM 2001 4 23 DL73E010555 1 20010404 A 5330 6545775581 SKIN BOEING 737 7372S3 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 367DL 21774 TWO CRACKS WERE FOUND IN THE FUSELAGE SKIN NEAR FS 727B, STR 17 RT AND 727A, STR 18 RT. THE CRACKS WERE CUT OUT AND AN EXTERNAL DOUBLER WAS INSTALLED PER B737-200 SRM 53-30-3, FIG6. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001042300262 20010423 00262 NM 2001 4 23 DL73K010556 1 20010404 A 5311 652072354 FRAME BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 316DL 23088 A CRACK WAS FOUND IN THE FS 492 FRAME AT STR 24 RT IN THE FLANGE. THE LENGTH OF THE CRACK IS 2.05 INCHES. THE CRACK WAS CUTOUT AND A REPAIR WAS INSTALLED PER SRM 51-40-3. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001042300263 20010423 00263 NM 2001 4 23 DL73E010557 1 20010404 A 5311 6516300301 FRAME BOEING 737 7372S3 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 367DL 21774 CRACKS WERE FOUND IN THE FS 178 BULKHEAD LT AND RT SIDE CHORDS. ADDITIONALLY, TWO CRACKS WERE FOUND IN THE CENTER WEB AT LBL 12/WL 218 AND RBL 12/WL 234. THE WEB WAS REPAIRED PER SRM 53-10-11, FIG. 1 AND THE CHORDS WERE REPLACED PER ERA 397408-14AD. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001042300264 20010423 00264 NM 2001 4 23 DL73K010558 1 20010405 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 322DL 23094 A SMALL CRACK WAS FOUND IN THE UPPER AFT CORNER OF THE L2 DOOR CUTOUT SKIN. THE CRACK WAS REMOVED WITH .25 INCH X .8 IN CH TRIMOUT IN THE OUTER LAYER OF SKIN ONLY. THE TRIMOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 38047 7-14, REV A. 2 L 7 2 4F RT A16WE 2001042300265 20010423 00265 NM 2001 4 23 DL76L010559 1 20010404 A 5754 SKIN BOEING 767 767332 1382001 NM NR 1 SLAT DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 197DN 28454 OUTBOARD MOST 54 INCHES OF THE LE SKIN OF THE NR 1 SLAT WAS FOUND DAMAGED BY IMPACT. REPAIR PER ER/A 371936-14 REV B 2 L 7 2 4F RT A1NM 2001042300266 20010423 00266 NM 2001 4 23 DL757010560 1 20010405 A 2120 UNKNOWN BOEING 757 757* NM CABIN ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 900PC 28446 ON SHORT FINAL F/AS REPORTED ODOR AFT OF FIRST CLASS CABIN THAT SMELLED LIKE BURNING HAIR. INSPECTED WIRE BUNDLES ABOVE CEILING PANELS. RAN PACKS AND WARM AND COLD. INSPECTED LIGHT FIXTURES ABOVE STORAGE BINS. INSPECTED GALLEYS. ALL WIRE BUNDLES AND EQUIP. CHECKS. COULD NOT DUPLICATE ODOR IN FIRST CLASS. 2 L 7 2 4F RT A2NM 2001042300268 20010423 00268 NM 2001 4 23 DL757010562 1 20010405 A 2150 A/C PACK BOEING 757 757232 1384965 NM RIGHT ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 6710E 30482 HOT PACK ODOR APPARENT THROUGH WHOLE AIRCRAFT DURING T/O WITH NORMAL POWER. NO WARNING LIGHTS OR OTHER INDICATIONS. REPLACED RT PACK FLOW CONTROL VALVE PER MM. RAN PACKS OFF OF ENGINES AT FULL HOT AND COLD. NO TROUBLE FOUND. 2 L 7 2 4F RT A2NM 2001042300269 20010423 00269 NM 2001 4 23 DLM11010563 1 20010405 A 2530 OVEN DOUG MD11 MD11 3023602 NM AFT GALLEY SMOKE A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 801DE 48472 OVENS IN AFT GALLEY STARTED TO SMOKE. OVENS CLEANED AND OPERATED FOR 15 MINUTES. CHECKS OK 2 L 7 3 4F RT A22WE 2001042300270 20010423 00270 NM 2001 4 23 DL76S010564 1 20010327 A 5315 111T50485 FLOORBEAM BOEING 767 767332 1382001 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 126DL 24076 CRACKS FOUND IN THE RBL 54.75 OVERWING LONGITUDINAL FLOORBEAM AT FS 788 IN THE UPPER CHORD. THE CHORD WILL BE TRIMMED A ND A NEW SECTION SPLICED IN. 2 L 7 2 4F RT A1NM 2001042300271 20010423 00271 NM 2001 4 23 DL757010565 1 20010405 A 5330 141N38501 SKIN BOEING 757 757232 1384965 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 604DL 22811 THE FUSELAGE SKIN AND UNDERLYING BUTT SPLICE STRAP WERE FOUND DENTED AT FS 297 BELOW STRINGER 17L. THE DAMAGED AREA OF SKIN WAS REMOVED WITH A CUTOUT AND THE BUTT SPLICE STRAP WAS CUT NEAR WL 216 AND A NEW SECTION INSTALLED. THE SKIN WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND THE NEW BUTT STRAP WAS SPLICED TO THE ORIGINAL WITH AN ALUMINUM DOUBLER PER ER/A 380006-14, REV A. 2 L 7 2 4F RT A2NM 2001042300273 20010423 00273 NM 2001 4 23 DL757010567 1 20010406 A 5330 146N370062 SKIN BOEING 757 757232 1384965 NM FUSELAGE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 604DL 22811 THE FUSELAGE SKIN WAS FOUND WITH SEVERAL DENTS AND GOUGES AROUND THE LOWER PORTION OF THE R4 DOOR CUTOUT. THERE WERE ALSO SEVERAL EXISTING REPAIRS IN THE AREA. TO REMOVE THE DAMAGE AND ELIMINATE THE EXISTING REPAIS, THE ENTIRE SKIN PANEL WAS REMOVED. A NEW SKIN PANEL WAS INSTALLED PER ER/A 380033-14. 2 L 7 2 4F RT A2NM 2001042300274 20010423 00274 NM 2001 4 23 DLM88010568 1 20010406 A 3610 LINE DOUG MD88 MD88 3023688 NM NLG WW CRACKED A DALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 909DL 49540 UPON ROTATION, NOTICED UNUSUAL SMELL, AS WE CLIMBED THROUGH 4000 FEET. SMELL RESEMBLED BURNING AND BECAME STRONGER. ON DESCENT, SMELL BECAME INTERMITTENT, MOST NOTABLE IN MID / AFT CABIN. ONE FLIGHT ATTENDANT COMPLAINED OF SLIGHT STINGING TONOSE AND MOUTH. FOUND HYDRAULIC LINE TO BRAKE BOOSTER VALVE CRACKED. REPLACED SAME 2 L 7 2 4F RT A6WE 2001042300275 20010423 00275 NM 2001 4 23 DL757010569 1 20010406 A 2121 FAN BOEING 757 757232 1384965 NM AFT CARGO BAY INOPERATIVE A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 613DL 22820 SMOKE REPORTED MID CABIN GALLEY RIGHT AFTER TAKEOFF. FOUND EICAS STATUS MSG SHOWING THAT NR 2 AFT EQUIP EXHAUST FAN INOP . NR 2 AFT EQUIP EXHAUST FAN FWD TO MCO AND PLAC. 2 L 7 2 4F RT A2NM 2001042300276 20010423 00276 NM 2001 4 23 DLM88010570 1 20010406 A 2120 UNKNOWN DOUG MD88 MD88 3023688 NM CABIN ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 988DL 53339 ON T/O ROLL AFT F/A SMELLED ELECTRICAL OR RUBBER BURNING. NO SMOKE BUT HAZE IN CABIN - THOROUGHLY INSPECTED AIRCRAFT - NTF - PERFORMED OPN 5088 DUCT BURNOUT. 2 L 7 2 4F RT A6WE 2001042300277 20010423 00277 2001 4 23 DLM88010571 4 20010406 A 3442 219101132 DISPLAY DOUG MD88 MD88 3023688 NM COCKPIT FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 966DL 53115 CREW REPORTS BURNED SMELL IN COCKPIT. FOUND RADAR DISPLAY BURNED, ALSO FOUND CAPTS MCDU OVERHEATED. REPLACED DISPLAY AN D MCDU. CHECKS GOOD. ALSO REPLACED INST. COOLING FAN, ALL CHECK GOOD. 2 L 7 2 4F RT A6WE 2001042300278 20010423 00278 NM 2001 4 23 DL72W010572 1 20010407 A 2100 7110035 CONTROLLER BOEING 727 727247 138408F NM CABIN PRESSURE MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 2815W 20871 CLIMBING THROUGH 17,000 FT.IN AUTO MODE AIRCRAFT CABIN ALT. PRESSURE CLIMBED THROUGH 10,000FT RAPIDLY. FOLLOWED LOSS OF PRESSURIZATION, CHECKLISTS AND WAS ABLE TO REGAIN CABIN CONTROL AFTER CYCLING LEFT PACK. STBY.MODE WORKED FINE AFTER THA T. 2 L 7 3 4F A3WE 2001042300279 20010423 00279 WP 2001 4 23 DLL10010573 1 20010407 A 2750 FLAP LKHEED 1011 10113851 5265010 WP WINGS MALFUNCTIONED A DALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 27 728DA 193C1173 FLAP / SLAT LOCK LIGHT CAME ON IN CRUISE. UNABLE TO LOWER FLAPS. ALL SLATS EXTENDED. RAN WIRES FROM COMPARATOR TO AS SEMETRY TRANSDUCER BOTH WINGS USING A MEGGER MTR. ALSO SHOOK DOWN WIRE BUNDLES FROM WING TIP TO WING ROOT BOTH WINGS. NO TROUBLE FOUND. RAN FLAPS SEVERAL TIMES ALL CHECKS NORMAL. 2 L 7 3 4F A23WE 2001042300280 20010423 00280 NM 2001 4 23 DL72W010574 1 20010407 A 3350 900835A BATTERY BOEING 727 727247 138408F NM RT / LT FUSELAGE DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 297WA 22534 DURING LAYOVER CHECK FOUND RT CENTER OVERWING EMERGENCY LIGHT INOP. ALSO FOUND LT AFT OVERWING EMERGENCY LIGHT INOP. RE PLACED BATTERIES AT BOTH LIGHTS OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2001042300281 20010423 00281 NM 2001 4 23 DLM88010575 1 20010407 A 3350 BATTERY PACK DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SO 27 919DL 49584 ON LO FOUND SEAT EMERGENCY LIGHT INOP. REPLACED BATTERIES. CHECKS GOOD. 2 L 7 2 4F RT A6WE 2001042300282 20010423 00282 NM 2001 4 23 DLM88010578 1 20010408 A 2910 AS15308K0254 LINE DOUG MD88 MD88 3023688 NM HYD SYSTEM LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 933DL 49720 LEFT HYDRAULIC QUANTITY DECREASED INFLIGHT FROM 11 QUARTS TO 4 QUARTS. FOLLOWED POM PROCEDURE AND QUANTITY INCREASED TO 19 QUARTS. TURNED LEFT ENGINE AND AUXILLARY AND TRANSFER PUMPS BACK ON AND QUANTITY WENT SLOWLY BACK TO ZERO AND PRESSUR E ZERO. REPLACED LINE FROM THRUST REVERSER BYPASS VALVE TO CASE DRAIN FILTERS. REPLACED CASE DRAIN FILTERS AND TRANSFE R PUMPFILTER. LEAK CHECKS GOOD. 2 L 7 2 4F RT A6WE 2001042300283 20010423 00283 NM 2001 4 23 DLM88010579 1 20010408 A 3230 519164605509 VALVE DOUG MD88 MD88 3023688 NM MLG LEAKING A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 979DL 53266 STRONG SMELL REPORTED BY FLIGHT ATTENDANTS AND NOTICED ALL THE WAY IN THE COCKPIT. SMELLED LIKE RUBBER FROM TIRES. THIS OCCURED RIGHT AFTER GEAR RETRACTION AND VERY QUICKLY DISSAPATED. REPLACED LANDING GEAR CONTROL VALVE. LEAK CHECKS GOOD. PERFORMED OPERATION 5088 DUCT BURNOUT 2 L 7 2 4F RT A6WE 2001042300284 20010423 00284 NM 2001 4 23 DL72S010580 1 20010408 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM LT OVERWING DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 544DA 22493 LT OVERWING EMERGENCY EXIT LIGHT FLASHING. REMOVED AND REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 2001042300285 20010423 00285 NM 2001 4 23 DL73K010581 1 20010409 A 5330 SKIN BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 381DL 23608 A 3 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN JUST BELOW STRINGER 18 RT JUST AFT OF FS 727B. THE CRACK WAS REMOVED W ITH A CUTOUT IN THE SKIN. THE SKIN WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 380422-14. 2 L 7 2 4F A16WE 2001042300286 20010423 00286 NM 2001 4 23 DL73K010582 1 20010409 A 5330 654576988 SKIN BOEING 737 737232 1384475 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 316DL 23088 CORROSION WAS FOUND IN THE FUSELAGE SKIN AND BEAR STRAP AT FS 490 BETWEEN STR 27R/28R. THE DAMAGE WAS CUT OUT AND A REPAIR DOUBLER INSTALLED. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001042300287 20010423 00287 NM 2001 4 23 DL73K010583 1 20010409 A 5312 BULKHEAD BOEING 737 737232 1384475 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 316DL 23088 CORROSION WAS FOUND ON THE BS 1016 PRESSURE BULKHEAD WEB AT BL 0. REPAIR WAS ACCOMPLISHED PER S/B 737-53A1075. THE DAM AGE WAS FOUND DURING HMV. 2 L 7 2 4F RT A16WE 2001042300288 20010423 00288 NM 2001 4 23 DL73K010584 1 20010409 A 5311 654653122 FRAME BOEING 737 737232 1384475 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 316DL 23088 LOWER LOBE FRAME AT FS 500 WAS FOUND CORRODED AT THE INBD FLANGE BETWEEN STR 25R/26R. THE FLANGE WAS CUT OUT AND A REPA IR ANGLE INSTALLED. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001042300289 20010423 00289 NM 2001 4 23 DL76G010585 1 20010409 A 7600 EEC BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 2 ENGINE MALFUNCTIONED A DALA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 SO 27 1609 4513 30574 706112 ON DESCENT OUT OF 10,000 FEET, THE CREW NOTICED THE RT ENGINE ROLLING BACK AND FLAMED OUT. CREW WAS ABLE TO RESTART THE ENGINE SUCCESSFULLY. NO WATER IN FUEL SUMPS. RAN ENG AND VERIFIED CONT AND ENGINE PARAMETERS NML EEC REPLACED. CHECK ED WIRING AND POWER SPAR VALVE NTF VLV ACT REMOVED PRECAUTION.RPLD SPAR VLV RPL RT ENG FUEL T SW PER 76-11-00-2-N. REP LACED RT ENGINE EEC RESET PIMU PERFORMED ENG RUN.NO FAULTS RECORDED ALL ENG PARAMETERS ARE NORMAL.MCO AND PLACARD REMOVE D. 2 L 7 2 4F 4 F RT A1NM E13NE 2001042300290 20010423 00290 2001 4 23 DL76G010586 4 20010410 A 2210 6224717003 CONTROL PANEL BOEING 767 7673P6 1385105 NM COCKPIT OVERHEATED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 1501P 24983 RT AUTOPILOT ENGAGE SWITCH SMOKED WHEN ENGAGED. DISCONNECTED SAME AND ENGAGED LEFT AUTOPILOT FOR REMAINDER OF FLT. RE PLACED A/P MODE CONTROL PANEL AND PERFORMED OPS CKS. ALL OKAY. 2 L 7 2 4F RT A1NM 2001042300291 20010423 00291 NM 2001 4 23 DL73K010587 1 20010410 A 5313 652072625 STRINGER BOEING 737 737232 1384475 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 316DL 23088 CORROSION WAS FOUND ON STR 26 RT AT APPROXIMATLEY FS 500+12. THE AFTMOST END OF THE STRINGER WAS CUT OFF AND A NEW SECT ION WAS SPLICED IN. THE CORROSION WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001042300292 20010423 00292 NM 2001 4 23 DL76G010588 1 20010410 A 2900 HYDRAULIC SYSTEM BOEING 767 7673P6 1385105 NM MAIN LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 153DL 24985 CENTER SYSTEM HYD QTY STARTED DROPPING RAPIDLY. TURNED OFF CENTER SYS PUMPS AS PER POM. .35 FLUID STILL IN SYS IN CRUIS E. SERVICED CENTER SYS TO FULL. RAN ALL FLT CONTROLS, FLAPS, GEAR, RUDDER, ELEV, AND STAB. NO LEAKS FOUND. DUE TO PR EV CTR SYSTEM HYD LEAK. 2 L 7 2 4F RT A1NM 2001042300293 20010423 00293 NM 2001 4 23 DL76L010590 1 20010410 A 2420 GENERATOR BOEING 767 767332 1382001 NM RT ENGINE FAILED A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 27 175DN 24803 RT GENERATOR OFF LIGHT AND EICAS MESSAGE CAME ON AFTER T/O. STARTED APU AND GOT A GOOD ELEC FROM THE GENERATOR. RE PLACED RT GEN PER M/M. OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 2001042300294 20010423 00294 NM 2001 4 23 DL72S010591 1 20010410 A 3350 LIGHT BOEING 727 727232 1384082 NM CARGO DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 544DA 22493 EMERGENCY LIGHT ON AFT CARGO DOOR INOPERATIVE. REPLACED LIGHT RACK 2 L 7 3 4F A3WE 2001042300295 20010423 00295 NM 2001 4 23 DL72S010593 1 20010409 A 5330 65545743 SKIN BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 518DA 21469 INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE YIELDED CRACK INDICATIONS. INTERNAL MFEC INSPECTION CONFIRMED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL AT FS 383 & 384. THE CRACKED AREA WAS ROUTED OUT AND A REPAIR DOUBLER AND STRUCTURAL FILLER INSTALLED PER B727 SRM 53-30-3, FIG. 5 AND ER/A 380513-14AD. 2 L 7 3 4F A3WE 2001042300296 20010423 00296 NM 2001 4 23 DL73K010594 1 20010409 A 5330 SKIN BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 381DL 23608 A 1.25 INCH CRACK WAS FOUND IN THE SKIN AT THE UPPER HINGE CUTOUT OF THE R2 DOOR OPENING. THE UNDERLYING BEAR STRAP WAS UNDAMAGED. THE CRACK WAS ROUTED OUT OF THE SKIN AND REPAIRED WITH AN EXTERNAL STEEL DOUBLER PER ER/A 380475-14. 2 L 7 2 4F A16WE 2001042300297 20010423 00297 NM 2001 4 23 DLM11010595 1 20010411 A 3320 BULB DOUG MD11 MD11 3023602 NM CABIN OVERHEATED A DALA H DEACTIVATE SYST/CIRCUITS M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 801DE 48472 LIGHT BY 4L DOOR WAS EXTREMELY HOT AND THE FLIGHT ATTENDANT SMELLED BURING PLASTIC UNTIL SHE TURNED IT OFF. INSPECTED A ND RELAMPED OPS NORMAL 2 L 7 3 4F RT A22WE 2001042300298 20010423 00298 NM 2001 4 23 DL757010596 1 20010411 A 2121 FAN BOEING 757 757232 1384965 NM E/E BAY FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 668DN 25141 EQUIPMENT OVERHEAT LIGHT ON AND ALSO HAD A LIGHT ODOR IN COCKPIT. REPLACED NR 1 FWD EQUIPMENT COOLING FAN AND CLEANED FILTER.OPS OK. 2 L 7 2 4F RT A2NM 2001042300299 20010423 00299 NM 2001 4 23 DLM11010597 1 20010411 A 2530 4110001137 COFFEEMAKER DOUG MD11 MD11 3023602 NM MID GALLEY SHORTED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 803DE 48474 MID GALLEY COFEEMAKER SHORTED OUT. (283) VISIBLE SPARKS FLEW, C/B POPPED. REPLACED COFFEEMAKER 2 L 7 3 4F RT A22WE 2001042300300 20010423 00300 NM 2001 4 23 DL73K010598 1 20010411 A 3350 1619 BULB BOEING 737 737232 1384475 NM CABIN BURNED OUT A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 303DL 23075 R2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED. 2 L 7 2 4F RT A16WE 2001042300301 20010423 00301 NM 2001 4 23 DL76S010599 1 20010410 A 5410 311T17303 BRACE BOEING 767 767332 1382001 NM NR 1 AND 2 PYLON CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 128DL 24078 THE BUSHINGS IN THE FORWARD AND AFT LUGS OF THE NR 1 AND 2 PYLON DIAGONAL BRACES WERE FOUND ROTATED / MIGRATED. THIS CO NDITION WAS FOUND DURING REMOVAL/INSTALLATION OF THE PYLON WHICH HAD BEEN REMOVED FOR OTHER REWORK. REMOVAL OF THE BUSH INGS REVEALED MINOR CORROSION IN THE FWD BORES. 2 L 7 2 4F RT A1NM 2001042300302 20010423 00302 NM 2001 4 23 DL72W010601 1 20010411 A 5330 SKIN BOEING 727 7272Q8 138407W NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831L 21826 THE FUSELAGE SKIN WAS FOUND WITH A SMALL BULGE AND CRACK AT FS 1030 AND STRINGER 30. THE DAMAGE WAS REMOVED WITH A 1.5 INCHES X 1.5 INCHES CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 380542-14, REV A. 2 L 7 3 4F A3WE 2001042300303 20010423 00303 2001 4 23 DL757010602 4 20010412 A 2210 COMPUTER BOEING 757 757232 1384965 NM AUTO FLIGHT OVERHEATED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 619DL 22909 CENTER AUTOPILOT DISCONNECTED APPROXIMATELY 1.5 HRS IN CRUISE FLIGHT. THIS WAS FOLLOWED BY NO-LAND 3 AND ELECTRICALINSUL ATION ACIDIC SMELL IN COCKPIT THEN THROUGHOUT CABIN WITH NO EVIDENCE OF SMOKE. THE SMELL DISSIPATED AFTER 15 MINUT ES. THE RIGHT AUTOPILOT WAS ENGAGED WITH NO PROBLEM. FOUND THE CENTER FCC INOP WITH BURNING SMELL. REPLACED SAME. NO OT HER DEFECTS WERE FOUND. RAN MCDP TEST ON NEW FCC. ALL CHECKS WERE NORMAL OK FOR SERVICE 2 L 7 2 4F RT A2NM 2001042300304 20010423 00304 NM 2001 4 23 DL757010604 1 20010412 A 2121 FAN BOEING 757 757232 1384965 NM E/E BAY SEIZED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 620DL 22910 A/C 620 FLT 739 DECLARED AN EMERGENCY AND DIVERTED TO MEM DUE TO HOT ELECTRICAL ODOR IN COCKPIT. NO ABNORMAL INDI CATIO NS OR EICAS MESSAGES. UPON ARRIVAL CONTRACT MTC FOUND THE FWD EQUIPMENT COOLING SUPPLY FAN NBR 1 DPN 216001013 SERIAL NB R 1997 AT FAULT (BEARING FAILURE AND SEIZING). REPLACED SAME 2 L 7 2 4F RT A2NM 2001042300305 20010423 00305 2001 4 23 DL75A010605 4 20010412 A 2565 D30656132 SLIDE BOEING 757 757212 NM PAX DOOR DISLODGED A DALA O OTHER L NO TEST TX TAXI/GRND HDL 1 SO 27 752AT 23128 3L ENTRY DOOR OPENED WHILE ARMED, SLIDE DID NOT DEPLOY, IT FELL ON SERVICE TRUCK - REPLACED SAME 2 L 7 2 4F RT A2NM 2001042300306 20010423 00306 NM 2001 4 23 DL76S010606 1 20010412 A 3350 LIGHT BOEING 767 767332 1382001 NM FUSELAGE INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 136DL 23146 ON L/O FOUND RIGHT OVERWING FORWARD EMERGENCY LIGHT INOP. RELAMPED 2 L 7 2 4F RT A1NM 2001042300307 20010423 00307 NM 2001 4 23 DL76S010607 1 20010412 A 3350 20131A BATTERY PACK BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 138DL 25409 ON SERVICE CHECK FOUND LEFT AFT EXTERIOR EMERGENCY LIGHTS INOP. R/R BATTERY PACK CHECKS GOOD 2 L 7 2 4F RT A1NM 2001042300308 20010423 00308 2001 4 23 DLM11010608 4 20010413 A 2330 PROJECTOR DOUG MD11 MD11 3023602 NM NR 2 OVERHEATED A DALA O OTHER M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 803DE 48474 NR 2 PROJECTOR OVERHEATED AND EMITTED FUMES BEFORE DEPARTURE - REPLACED SAME 2 L 7 3 4F RT A22WE 2001042300309 20010423 00309 NE 2001 4 23 DLM88010610 2 20010413 A 7510 13277503 DUCT DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE CRACKED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 934DL 49721 718247 WHILE CLIMBING THRU 11K FT NR 2 ENG FIREALOOP ILLUMINATED AT 13K FT NR 2 FIREBELL WARNING HANDLE ILLUMINATED. THROTTLE W AS RETARDED TO IDLE AND LIGHT EXTINGUISHED. UPON ENG INSP FOUND DUCT BETWEEN 13TH STAGE DUCT AND NOSE COWL ANTI ICE VALVE CRACKED. REPLACED DUCT AND PERFORMED ENG RUN PER PFHB. LEAK CHECKED GOOD. 2 L 7 2 4F 4 F RT A6WE E9NE 2001042300310 20010423 00310 NM 2001 4 23 DL72W010611 1 20010411 A 5320 ANGLE BOEING 727 727247 138408F NM RT WHEEL WELL CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 290WA 22108 DUE SRM PERMANANT REPAIR OF CRACK IN THE BS 870 SUPPORT ANGLE RT WHEEL WELL. REPLACED KEEL BEAM SUPPORT ANGLE PER SRM 5 3-10-9D. 2 L 7 3 4F A3WE 2001042300311 20010423 00311 NM 2001 4 23 DL764010612 1 20010413 A 2752 256T62004 ACTUATOR BOEING 767 767* NM RT WING MALFUNCTIONED A DALA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SO 27 831MH 29702 TE FLAP DISAGREE ON TAKEOFF. FLAPS STOPPED RETRACTING AT 10DEG. FLAPS EXTENDED TO 20 DEG. WITH ALTN FLAPS SYSTEM. FOUN D ROTARY ACTUATOR BRAKE TRIPPED ON RT OUTBOARD FLAP GEAR BOX ROTARY FLAP ACTUATOR ON INBOARD SIDE TRIPPED. REPLACED ROT ARY ACTUATOR MFR. NBR. 256T6200-4 ETOPS CATEGORY ''B'': DIVERSION OR TURNBACK 2 L 7 2 4F RT A1NM 2001042300312 20010423 00312 NM 2001 4 23 DLM88010613 1 20010413 A 3350 0105643001 SOCKET DOUG MD88 MD88 3023688 NM CABIN FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 939DL 49812 FOUND GALLEY 1R EMERGENCY LIGHT NOT WORKING. REPLACED BROKEN LIGHT SOCKET. 2 L 7 2 4F RT A6WE 2001042300314 20010423 00314 NM 2001 4 23 DLM88010615 1 20010414 A 2130 DUCT DOUG MD88 MD88 3023688 NM WATER SEPARATOR RUPTURED A DALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 27 966DL 53115 FLOW LIGHT CAME ON DURING CLIMBOUT WHEN LEVEL AT 12000FT CABIN CONTINUED TO CLIMB THRU 8000 FT CABIN RATE UNCONTROLLABLE . FOUND RT WATER SEPERATOR AFT FLEX DUCT RUPTURED - REPLACED SAME 2 L 7 2 4F RT A6WE 2001042300315 20010423 00315 NM 2001 4 23 DL73K010617 1 20010414 A 3350 S283T0143 POWER SUPPLY BOEING 737 737232 1384475 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 302DL 23047 RT AFT AISLE EMERGENCY LIGHT INOP. REPLACED BATTERY POWER SUPPLY CKS NORMAL 2 L 7 2 4F RT A16WE 2001042300316 20010423 00316 NE 2001 4 23 DL78K010618 2 20010414 A 7200 CFM567 ENGINE BOEING 737 737832 13844CF NM GE CFM56 CFM567B24 NE NR 2 FAILED A DALA C ABORTED TAKEOFF Y J ENGINE STOPPAGE WARNING INDICATION TO TAKEOFF 1 SO 27 399DA 926 0 30379 876581 SPOOLING UP NR 2 ENG , AT 40 PERCENT FOR TAKE OFF, AIRCRAFT SHUDDERED. ENGINE SHUT DOWN ON ITS OWN AND ENGINE FAIL LIGH T ILLUMINATED. ENGINE OVERTEMPED. ENGINE CHANGED. 2 L 7 2 4F 4 F RT A16WE E00055EN 2001042300317 20010423 00317 NM 2001 4 23 DL72S010621 1 20010415 A 3350 CONNECTOR BOEING 727 727225A 1384077 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 805EA 22436 RED EMERGENCY LIGHT INOPERATIVE INBD SIDE OF FWD COAT CLOSET. FOUND WIRE PULLED FRM CONNECTOR. REPAIRED CONNECTOR 2 L 7 3 4F RT A3WE 2001042300318 20010423 00318 NM 2001 4 23 DL76S010622 1 20010415 A 5330 146T32521 SKIN BOEING 767 767332 1382001 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 136DL 23146 AN EXISTING SKIN REPAIR WAS FOUND WITH A DENT AREA AT THE UPPER EDGE ROW OF THE REPAIR AT BS 1197+78. THE EXISTING REPAIR WAS REMOVED AND ALL UNDELYING DAMGE CUTOUTS COMBINED INTO ONE CUTOUT EXTENDING FROM STRINGER 38L TO STRINGER 36L. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B767 SRM 53-00-01, FIG. 212 AND ER/A 380365-14. 2 L 7 2 4F RT A1NM 2001042300319 20010423 00319 NE 2001 4 23 DL76L010623 2 20010416 A 7200 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 FAILED A DALA A UNSCHED LANDING E R J VIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SO 27 181DN 40225 0 25986 724314 COMPRESSOR STALL ON RIGHT ENGINE AT 31000FT. STALL WAS FELT BY FLIGHT CREW. CONTINUED TO ATL FOR RIGHT ENGINE CHANGE. S MALL AMOUNTS OF METAL FOUND IN TAILPIPE. 2 L 7 2 4F 4 F RT A1NM E24NE 2001042300320 20010423 00320 NM 2001 4 23 DLM88010625 1 20010416 A 5210 SEAL DOUG MD88 MD88 3023688 NM PAX DOOR LEAKING A DALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 27 955DL 49886 AIRPLANE WOULD NOT PRESSURIZE AFTER T/O RETURNED TO LAND CVG EXCESSIVE WIND NOISE AT 2L DOOR - SECURED SEAL AND REPLACED FILLER 2 L 7 2 4F RT A6WE 2001042300321 20010423 00321 NM 2001 4 23 DL757010626 1 20010416 A 3397 WIRE BOEING 757 757232 1384965 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 643DL 23997 PAX SEAT 6CD EMERGENCY LITES INOPERATIVE. REPAIRED BROKEN WIRE 2 L 7 2 4F RT A2NM 2001042300322 20010423 00322 NM 2001 4 23 DL738010627 1 20010416 A 3350 D71702001 CHARGER BOEING 737 737832 13844CF NM ROW 16 INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 390DA 30536 INTERIOR EMERGENCY LIGHTS INOPERATIVE AT ROW 16ABC. REPLACED CHARGER AND BATTERY COMBINATION. 2 L 7 2 4F RT A16WE 2001042300323 20010423 00323 NM 2001 4 23 DL73E010628 1 20010416 A 3350 BATTERY BOEING 737 737247 138448D NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 373DL 23520 AFT RT SLIDE EMERGENCY LT INOPERATIVE AND 1 CABIN AISE EMER. LT I INOPERATIVE. REPLACED BATTERY 2 L 7 2 4F A16WE 2001042300324 20010423 00324 NM 2001 4 23 DL73E010629 1 20010416 A 3350 LIGHT BOEING 737 737247 138448D NM ESCAPE SLIDE CORRODED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 373DL 23520 AFT LEFT SLIDE EMERGENCY LT INOPERATIVE. REPLACED LIGHT ASSY 2 L 7 2 4F A16WE 2001042300325 20010423 00325 NM 2001 4 23 DL72S010548 1 20010403 A 7930 INDICATOR BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE INOPERATIVE A DALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 545DA 52649 22494 700711 NR 1 ENG LOW OIL PRESSURE / BYPASS LIGHT ILLUMINATED IN FLIGHT INSPECTED MAIN OIL FILTER FOUND APPRECIABLE COKE DEPOS RA N ENGINE WITH NEW FILTER INSPECTED FOUND VERY LITTLE COKE NOMETAL FOUND AT ANY TIME REPLACED SEC FILTER OIL PRESS INDIC NML. 2 L 7 3 4F 4 F A3WE E2EA 2001042300326 20010423 00326 CE 2001 4 23 20010417CW012 1 20010311 A 8120 S1891805 CLAMP GARRTT CESSNA 421 421C 2076016 CE CONT O520 TSIO520* 17040 SO TURBOCHARGER BROKEN D DYVA K NONE O OTHER IN INSP/MAINT 1 NM 07 4119M 1298 SJR0103R 421C1029 ENROUTE, CRUISE. LT ENGINE TURBOCHARGER DAMAGED, BROKEN SHAFT AND SEIZED. PILOT FEATHERED LEFT PROP, SECURED ENGINE A ND HAD SINGLE ENG LANDING. LANDED SAFELY. TANG PORTION OF CLAMP FOUND BROKEN OFF. 1 L 7 2 3O 3 O A7CE E8CE 2001042300327 20010423 00327 CE 2001 4 23 20010417CW013 1 20010313 A 5751 99130000617 SKIN BEECH 90 F90 1152909 CE AILERON CRACKED B R2JR K NONE O OTHER IN INSP/MAINT 1 EA 21 994RD 5981 LA119 DURING PHASE 2 INSPECTION, FOUND 6 INCH CRACK AT TOP AILERON SKIN. SKIN WAS CLOSE TO FAILURE. 1 L 7 2 4T A31CE 2001042300328 20010423 00328 2001 4 23 DHL2001364013 4 20010417 A 3414 CONNECTOR AIRBUS 300 A300B4203 3930306 EU AIRSPEED INDICAT DIRTY A DHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 364DH 0141 AT BEGINNING OF TAKEOFF ROLL F/O AIRSPEED INDICATOR RED FLAG APPEARED & ''''0'''' KNOTS INDICATED. CAPTAINS AIRSPEED IN DICATOR NORMAL & INDICATING 80 KNOTS. REMOVED INDICATOR, CLEANED RESEATED BOTH CONNECTOR PLUGS. PERFORMED AIR DATA SE LF-TEST. AMM 34-12-22 PAGE 403. NO DEFECTS NOTED. STATUS-CLOSED. 2 L 7 2 4F RT A35EU 2001042300329 20010423 00329 2001 4 23 DHL2001709003 4 20010417 A 2210 AUTOPILOT SYS BOEING 727 72782C 1384026 NM COCKPIT MALFUNCTIONED A DHLA K NONE O OTHER CR CRUISE 1 SO 01 709DH 19968 WITH AUTOPILOT AND ALT HOLD ENGAGED, A/C GAINS ABOUT 300 FT AN HOUR IN BOTH A & B MODE AND WITH AUX 1 NORMAL AND AUX VGS SELECTED. TRANSFERRED ITEM TO DEFERRAL-ALT, SELECT MODE - DMI 5201 PER MEL 27-1-3, PLACARD INSTALLED. STATUS-OPEN 2 L 7 3 4F A3WE 2001042300330 20010423 00330 NM 2001 4 23 DHL2001745003 1 20010417 A 3241 425270 CONTROL UNIT BOEING 727 727224 1384076 NM ANTI SKID SYS MALFUNCTIONED A DHLA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 745DH 20665 WITH ANTI-SKID ON, AND BRAKE PEDALS AT MECHANICAL STOPS, ANTI-SKID WOULD NOT ENGAGE OR CYCLE. R & R ANTI-SKID CONTROL BOX WITH SERVICABLE UNIT IAW MM 32-42-0. STATUS-CLOSED. P/N OFF 42-527D, S/N OFF 1802, P/N ON 42-527D, S/N ON 1647. PC T 100434, POS ONLY. 2 L 7 3 4F A3WE 2001042300331 20010423 00331 WP 2001 4 23 DHL2001806785 1 20010316 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP FUSELAGE BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - MAIN CARGO NR 3 TRACK SHOWS A BREAK OF 2 INCH AND POINTS OF CORROSION BETWEEN STA 640.000 - STA 718.000. REMOV ED DAMAGED AREA OF FLOOR TRACK 3 RT AND FABRICATED SPLICE IAW SRM 53-2-3 PAGE 49-50. FABRICATED TRACK IAW SRM 53-2-3 PA GE 49-50. CLEANED, TREATED & PRIMED IAW SRM 51-1-8 PAGES 1-12, 13. INSTALLED SPLICE + TRACK IAW SRM 53-2-3 PAGE 49-50. 2 L 7 4 4F RT 4A25 2001042300332 20010423 00332 WP 2001 4 23 DHL2001806585 1 20010316 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - MAIN CARGO NR 3 TRACK SHOWS A BREAK OF 2 INCHES AND POINTS OF CORROSION BETWEEN STA 640.000 - STA 718.000. R EMOVED DAMAGED AREA OF FLOOR TRACK 3 RT AND FABRICATED SPLICE IAW SRM 53-2-3 PAGE 49-50. FABRICATED TRACK IAW SRM 53-2 -3 PAGE 49-50. CLEANED, TREATED & PRIMED IAW SRM 51-1-8 PAGES 1-12, 13. INSTALLED SPLICE + TRACK IAW SRM 53-2-3 PAGE 4 9-50. 2 L 7 4 4F RT 4A25 2001042300333 20010423 00333 2001 4 23 DHL2001709004 4 20010418 A 2210 25858043 CONTROL UNIT BOEING 727 72782C 1384026 NM AUTOPILOT MALFUNCTIONED A DHLA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SO 01 709DH 19968 ANYTIME THE AUTOPILOT ELEVATOR IS ENGAGED IN A SYSTEM MODE, THE AIRCRAFT PITCHES ERATICALLY UP AND DOWN. R / R PITCH CH ANNEL CONTROL IAW MM 22-11-01. SECURITY CHECK IS GOOD. STATUS-CLOSED. 2 L 7 3 4F A3WE 2001042300334 20010423 00334 2001 4 23 DHL2001721001 4 20010418 A 2210 CONTROL UNIT BOEING 727 727228 NM AUTOPILOT MALFUNCTIONED A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 721DH 19545 BOTH AUTOPILOT ON - IN MAN MODE/HDG SEL INGAGED USING HDG BUG TO TURN AND CLIMB AT SAME TIME - A/C BANKED 30 DEG AND THE PITCH WOULD TEMPORARILY BECOME ERRATIC PITCHING UP THEN DOWN +/- 5-7 DEG. RE RACKED PITCH CHANNEL SYSTEM. OPS GOOD W ITH COMPANY EQUIPMENT IAW 22-11-01. STATUS-CLOSED. 2 L 7 3 4F A3WE 2001042300335 20010423 00335 2001 4 23 DHL2001745004 4 20010418 A 2210 COMPUTER BOEING 727 727224 1384076 NM AUTOPILOT MALFUNCTIONED A DHLA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 745DH 20665 AUTOPILOT ENGAGED/DISENGAGED PADDLE LEVERS WILL NOT MOVE TO THE ENGAGED POSITION IN BOTH A AND B MODE. A & B MODE DEAC TIVATED ON AIRCRAFT. PLACARD MUST HAVE BEEN MISSED BY CREW. SYSTEM OPERATES NORMAL PER BMM REF 22-11-1. STATUS-CLOSED . 2 L 7 3 4F A3WE 2001042300336 20010423 00336 WP 2001 4 23 DHL2001804003 1 20010418 A 3240 26014112 WHEEL DOUG DC8 DC873F 302199F WP NR 3 MLG SEPARATED A DHLA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 804DH 46124 WHEEL ON RIGHT MAIN FELL OFF DURING TAXI-IN AFTER LANDING. REMOVED NR 3 WHEEL HALF & NR 4 MAIN WHEEL ASSY. INSPECTED A XLES & SURROUNDING AREA. NO DEFECTS NOTED. REPLACED NR 3 & 4 MAIN WHEEL ASSY IAW 32-40-1. P/N''S OFF & ON: 2601411-2. NR 3 S/N OFF: B2583/H277 AND S/N ON: H1127/H0785 PCT:0133258. NR 4 S/N OFF: BH1170/BH1643 AND S/N ON: B2296/B2296 PC T:0135995. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300338 20010423 00338 WP 2001 4 23 DHL2001806586 1 20010326 A 5753 ANGLE DOUG DC8 DC873 302199C WP TE FLAPS CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LH OUTBD FLAP SLIDING COVER HOUSING ANGLE CRACKED AT STA XRS 367.REMOVED CRACKED ANGLE IAW SRM 51-3-0 PAGE 1. FABRICATED NEW ANGLE IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-3-0 PAGE 1. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300339 20010423 00339 WP 2001 4 23 DHL2001806587 1 20010305 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - FUSELAGE NOSE SECTION EXTERNAL SKIN CRACKED 1 INCH AT FS -40.0 L-32 RT. PERFORMED STOP HOLE. FABRICATED DOU BLER IAW SRM 53-2-0 FIG 1B PAGE 77/78. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1B. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300340 20010423 00340 WP 2001 4 23 DHL2001806588 1 20010326 A 5753 ANGLE DOUG DC8 DC873F 302199F WP TE FLAPS CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LT OUTBD FLAP SLIDING COVER HOUSING ANGLE CRACKED AT STA XRS 247.REMOVED ANGLE CRACKED IAW SRM 51-1-21 PAGE 1. FABRICATED NEW ANGLE WITH EXTRUSION 7075 T6 IAW SRM 57-2-0 FIG 2. TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-1-21 PAGE 1. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300341 20010423 00341 WP 2001 4 23 DHL2001806589 1 20010318 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - MAIN CARGO COMPARTMENT - FRAME DEFORMED STA 1580.000 L-20 LT. REMOVED FASTENERS IAW SRM 51-1-20D PAGE 21. RE MOVED DAMAGED FRAME IAW SRM 53-20 PAGE 25 THRU 27. FABRICATED NEW FRAME IAW SRM 53-2-0 PAGE 25 THROUGH 27. PERFORMED T HERMAL TREATMENT TO NEW FRAME IAW DPS 7. 00-1. AND INSTALLED FRAME USING NEW FASTENERS IAW SRM 51-1-20D PAGE 9. STATUS -CLOSED. 2 L 7 4 4F RT 4A25 2001042300342 20010423 00342 WP 2001 4 23 DHL2001806590 1 20010309 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - COCKPIT - 682 FLOOR PANEL SUPPORT ANGLES LWR EDGE CRACKED 1/2 INCH AT STA -12.000. PERFORMED STOP HOLE IAW SR M 53-2-0 FIG 1B. FABRICATED REINFORCING ANGLE IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INST ALLED REINFORCING ANGLES IAW SRM 53-2-0 FIG 1B. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300343 20010423 00343 WP 2001 4 23 DHL2001806591 1 20010328 A 5751 RIB DOUG DC8 DC873F 302199F WP AILERON CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LT WING AILERON INTERIOR LATERAL RIB ACCESS DOOR FRAME CRACKED 4 INCHES, STA XA 425. REMOVED LATERAL RIB ACCE SS DOOR FRAME IAW SRM 51-1-21 PAGE 1. CLEANED, TREATED AND PRIMED AILERON INTERIOR LATERAL RIB ACCESS DOOR FRAME AT STA XA 425 IAW SRM 51-1-8B. INSTALLED NEW RIB ACCESS DOOR FRAME IAW SRM 51-1-21 PAGE 1. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300344 20010423 00344 WP 2001 4 23 DHL2001806592 1 20010314 A 5315 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP FUSELAGE BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - MAIN CARGO FLOOR SUPPORT ANGLE AT STA 8.000 RBL 46 BROKEN. STOP DRILLED IAW SRM 53-2-0 FIG 1B. FABRICATED RE INFORCING ANGLE. 2 L 7 4 4F RT 4A25 2001042300345 20010423 00345 NE 2001 4 23 DHL2001727005 2 20010417 A 7530 6522444803 DUCT BOEING 727 727228 NM PWA JT8 JT8* 52044 NE 8TH STAGE BENT A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 ON CLIMB-OUT LT DUCT PRESS 46PSI RT 64PSI WITH ENG NR 1 EPR 1.88 AND NR 3 AT 1.84 WITH ENG ANTI-ICE ON. AFTER ENG NR 3 STRUT OHEAT PROB WAS STABILIZED. SEE 2P BELOW WITH ENG NR 3 BLEED-OFF AND NR 2 BLEED-0N DUCT PRESSURES WERE MATCHED AT 32 PSI WITH ENG NR 1 AT 1.76 EPR AND NR 2 AT 1.78 EPR. PERFORMED HI PRESS BLEED CONTROL (SYS OPS CHECK AND FOUND NO DE FECTS AS PER MM 36-12-01 SEC 2 TEST & JRH 6.5. REPAIRED FLANGE ON NR 3 ENG AIR DUCT. SEE ITEM 2P IAW BAC OHM 36-10-01. NO LEAKS NOTED. ACCOMPLISHED DUCT BLEED AIR CHECK PER DHL JRH 6.5. NO LEAKS NOTED. NEEDLES MATCHED. STATUS CLOSED. 2 L 7 3 4F 4 F A3WE E2EA 2001042300347 20010423 00347 2001 4 23 DHL2001365003 4 20010420 A 2210 B7CM1 COMPUTER AIRBUS 300 A300B4203 3930306 EU AUTO THROTTLES MALFUNCTIONED A DHLA O OTHER O OTHER CR CRUISE 1 SO 01 365DH 149 AUTO THROTTLE SYSTEM DIS-ENGAGED NUMEROUS TIMES IN CRUISE FLIGHT. COULD NOT DUPLICATE ON GROUND. REPLACED AUTO THROTT LE COMPUTER FOR TROUBLE-SHOOTING IAW M/M 22-31-34. ALL P/NS B7CM1, S/N OFF 158. S/N ON 197. STATUS-CLOSED. 2 L 7 2 4F RT A35EU 2001042300348 20010423 00348 WP 2001 4 23 DHL2001806593 1 20010316 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 MAIN CARGO BAY SPLICE FITTING CRACKED 2 INCH AT STA 900 - 920 L-1. REMOVED CRACKED SPLICE FITTING AT STA 900 - 920 L-1 IAW SRM 51-1-200 PAGE 21. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PAGE 9. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300349 20010423 00349 WP 2001 4 23 DHL2001806594 1 20010323 A 5320 FITTING DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - AFT CARGO COMPARTMENT. FITTING CRACKED 1 INCH BETWEEN L-25L AND L-23L. STA 1180.000. REMOVED FITTING CRACK ED FROM AFT CARGO COMPARTMENT BETWEEN L-25L AND L-27L IAW SRM 51-1-21 PAGE 21. CLEANED, TREATED AND PRIMED IAW SRM 51-1 -8B. INSPECTED NEW FITTING IAW SRM 51-1-2D PAGE 9. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300350 20010423 00350 NE 2001 4 23 20010420CW013 1 20010303 A 2612 7630607902 FIRE DETECTOR SKRSKY S76 S76 8143010 NE ALLSN 250C 250C30S 03013 GL NR 1 ENGINE INOPERATIVE B ALGR O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 03 705AL 760267 DURING PRESTART CHECK, FLAME DETECTOR WOULD NOT TEST. 1 G 7 2 3U 3 U H1NE E1GL 2001042300351 20010423 00351 SW 2001 4 23 20010420CW014 1 20010323 A 6510 407340339103 BEARING BELL 407 407 SW ALLSN 250C 250C47B GL T/R DRIVESHAFT DAMAGED B ALGR O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 03 417AL 5418 53054 CAE847018 ON THE 2ND SHUT DOWN OF THE DAY, LOUD NOISES AND EXCESSIVE VIBRATION WERE NOTED. FORWARD BEARING ON THE NR 2 TAILROTOR DRIVESHAFT, (OIL COOLER BLOWER) HAD AN UNCONTAINED FAILURE. BLOWER DECK AND SUPPORTING STRUCTURE CRACKED AFT ENGINE FIR EWALL AND IMPELLER HOUSING. 1 G 7 1 3U 3 U O H2SW E1GL 2001042300352 20010423 00352 SW 2001 4 23 20010420CW015 1 20010222 A 5330 206050136184 SKIN PANEL BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL FUSELAGE DEBONDED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 15Q 159 2235 AFTER LANDING AND WALK AROUND, RIGHT SKID PANEL METAL STRIP WAS FOUND DEBONDED FROM SKID PANEL. 1 G 7 1 3U 3 U H2SW E4CE 2001042300353 20010423 00353 NE 2001 4 23 20010420CW016 1 20010301 A 6320 7635109041043 QUILL SKRSKY S76A SKRSKY S76 S76A 8143006 NE TMECA ARRIEL ARRIEL1A 60030 NE BLOWER DRIVE DAMAGED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 521AL 6902 352 A08100128 760132 DURING PHASE INSPECTION, FOUR LARGE CHIPS WERE FOUND ON RIGHT HAND CHIP PLUG AND ONE LARGE CHIP ON THE LEFT HAND CHIP PL UG. THE BLOWER ASSEMBLY QUILL WAS PULLED AND TWO TEETH FOUND DAMAGED. 1 G 7 2 3U 3 U H1NE E19EU 2001042300355 20010423 00355 NE 2001 4 23 20010420CW018 1 20010322 A 6321 7636309101108 CALIPER SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL ROTOR BRAKE STUCK B ALGR O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 03 518AL 760134 DURING RUN UP PRIOR TO 135 REVENUE FLIGHT. SMOKE COMING OUT OF INTAKE COWLING AREA, NOTIFIED FLIGHT CREW WHO SHUT DOWN THE AIRCRAFT. MAINTENANCE FOUND ONE ROTOR BRAKE PUCK STUCK OUT AGAINST THE DISC CAUSING SMOKE. 1 G 7 2 3U 3 U H1NE E1GL 2001042300356 20010423 00356 WP 2001 4 23 DHL2001806595 1 20010329 A 5312 PRESSURE PANEL DOUG DC8 DC873F 302199F WP NLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - NLG WHEEL WELL INTERNAL COVER CRACKED 1/2 INCH AT FS 10.000. DRILLED STOP HOLE IAW SRM 53-2-0 FIG 1B. FABRI CATED DOUBLER IAW SRM 53-2-0 FIG 1B. TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1B. ST ATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300357 20010423 00357 WP 2001 4 23 DHL2001806596 1 20010329 A 5330 SKIN DOUG DC8 DC873F 302199F WP TAIL CONE BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - TAIL CONE EXTERIOR LT SIDE UPPER PART SKIN 02 EA BREAKS 1/2 INCH STA 1861-1868. CUT TAIL CONE EXTERIOR RH SI DE UPPER PART SKIN AT STA 1868.168 IAW SRM 53-2-3 PAGE 7. FABRICATED FILLER IAW SRM 53-2-3 PAGE 1-2. TREATED AND PRIM ED IAW SRM 51-1-8B. FABRICATED DOUBLER IAW SRM 53-2-3 PAGE 1-2. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300358 20010423 00358 WP 2001 4 23 DHL2001806597 1 20010329 A 5320 FITTING DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - MAIN CARGO COMPARTMENT - FITTING BETWEEN EXTRUSION AND WEB CRACKED 1/2 AT STA 305.000 L-21R. REMOVED CRACKED FITTING AT STA 305 L-21R IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FIT TING IAW SRM 51-1-20D PAGE 9. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300359 20010423 00359 WP 2001 4 23 DHL2001806598 1 20010315 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - MAIN CARGO COMPT. SEAT TRACK 1 LH LUGS BROKEN (STA 504 - 512). CUT OUT DAMAGED AREA OF SEAT TRACK (STA 504-5 12) AND FABRICATED SPLICE IAW SRM 53-2-3 PAGE 49-50 FABRICATED TRACK (P/N 52772660) IAW SRM 53-2-3 PAGE 49-50. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8 PAGE 1 TO 12-13. AND INSTALLED SPLICE + TRACK IAW SRM 53-2-3 PAGE 49-50. STATUS-CLO SED. 2 L 7 4 4F RT 4A25 2001042300360 20010423 00360 WP 2001 4 23 DHL2001806599 1 20010318 A 5753 SKIN DOUG DC8 DC873F 302199F WP TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - RT WING FLAP JOINT DELAMINATED. R/R JOINT FLAP IAW MM 57-20-1 PAGE 204-214. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300361 20010423 00361 WP 2001 4 23 DHL2001806600 1 20010313 A 5320 FITTING DOUG DC8 DC873F 302199F WP BULKHEAD CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - RT REAR PRESSURE BULKHEAD TEE FITTING SHOWS CRACK OF 3 INCH WITH STOP DRILL. FABRICATED REINFORCEMENT ANGLE IAW SRM 51-1-8B FIG 1B. TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCEMENT ANGLE IAW SRM 53-2-0 FIG 1B. STATU S-CLOSED. 2 L 7 4 4F RT 4A25 2001042300362 20010423 00362 WP 2001 4 23 DHL2001806601 1 20010326 A 5753 SKIN DOUG DC8 DC873F 302199F WP RT WING TE FLAP MISREPAIRED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - RT WING O/B FLAP T/E AT STA XW 454.000 SHOWS REPAIR IMPROPER. REMOVED T/E WITH REPAIR IMPROPER IAW SRM 51-1-21 PAGE 1. FABRICATED NEW T/E IAW SRM 52-2-0 FIG 2D. TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW T/E IAW SRM 51- 1-21 PAGE 1. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300363 20010423 00363 WP 2001 4 23 DHL2001806602 1 20010328 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - FWD CARGO COMPART FITTING CRACKED 1/2 INCH, STA 300 L-27 LT. REMOVED CRACKED FITTING (STA 300 L-27L) IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PAGE 9. ST ATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300364 20010423 00364 WP 2001 4 23 DHL2001806603 1 20010312 A 5753 SKIN DOUG DC8 DC873F 302199F WP LT WING TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECKED - LT WING L/E LWR SKIN SURFACE CRACKED 1/2 INCH AT STA XFS 585. CUT OUT DAMAGED AREA OF LT WING L/E LWR SKIN XFS 585 AND FABRICATED FILLER AND DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALL ED FILLER AND DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300365 20010423 00365 WP 2001 4 23 DHL2001806604 1 20010324 A 5320 FITTING DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - FWD CARGO COMPT. FITTING CRACKED 1 INCH AT STA 200 L-25 RT. REMOVED CRACKED FITTING AT STA 200 L-25 RT (FWD C ARGO COMPT) IAW SRM 51-3-0 PAGE 1, 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-3- 0 PAGE 1, 2. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300366 20010423 00366 WP 2001 4 23 DHL2001806605 1 20010321 A 5320 FITTING DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - FWD CARGO COMPARTMENT FITTING CRACKED 4 INCH BETWEEN STA 600.000 AND STA 620.000 L-32R. R/R FITTING CRACKED IAW SRM 51-1-200 PAGE 21. CLEANED TREATED AND PRIMED FWD CARGO COMPT FITTING BETWEEN STA 600.000 AND STA 620.000 L-32R IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PAGE 9. 2 L 7 4 4F RT 4A25 2001042300367 20010423 00367 WP 2001 4 23 DHL2001806606 1 20010321 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - FWD CARGO COMPARTMENT - FITTING BETWEEN FRAME AND BEAM SHOWS CORROSION AT STA 822.000, L-21R. R/R FITTING CO RRODED IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED MAIN CARGO COMPARTMENT FITTING BETWEEN FRAME AND BEAM AT S TA 827.000 L-21R IAW SRM 51-1-20D PAGE 9. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300368 20010423 00368 WP 2001 4 23 DHL2001806607 1 20010309 A 2824 CONTROL VALVE DOUG DC8 DC873F 302199F WP FUEL TANK MISINSTALLED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - RT FWD TANK, LEVEL CONTROL VALVE ELECTRICAL PLUG IMPROPERLY SAFETIED. SAFETIED PROPERLY LEVEL CONTROL VALVE ELECT PLUG (RT FWD TANK) IAW MM 20-18-0 PAGE 201-215. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300369 20010423 00369 WP 2001 4 23 DHL2001806608 1 20010329 A 5320 FITTING DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - FWD CARGO COMPARTMENT FITTING CRACKED 1 INCH AT STA 280 L-21RT. REMOVED CRACKED FITTING AT STA 280 L-21R IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PAGE 9 . STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300370 20010423 00370 WP 2001 4 23 DHL2001806609 1 20010311 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LT WING L/E RIB UPPER PART HAS A 1/2 INCH CRACK AT STA XFS 747.000. PERFORMED STOP DRILL AND FABRICATED RE INFORCING ANGLE IAW SRM 57-2-0 FIG 2 CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INBSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042300371 20010423 00371 WP 2001 4 23 DHL2001806550 1 20010316 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - MAIN CARGO D FLOOR AT STA 887.000 CRACKED 2 INCHES. CUTOUT DAMAGED AREA OF FLOOR PANEL D AT STA 887 AND FABR ICATED FILLER AND DOUBLER IAW SRM 53-2-3 PAGE 39-40. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B, PAGES 1,12&13. INSTAL LED FILLER AND DOUBLER IAW SRM 53-2-3 PAGE 39-40. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042400001 20010424 00001 NM 2001 4 24 01FDEA00224 1 20010323 A 2130 CONTROL VALVE BOEING 727 727227 1384078 NM CABIN PRESSURE FAILED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 478FE 21395 AFT T/O CABIN PRESS DID NOT WORK, PSID NEVER WENT ABOVE 1 PSID. PERF RED TABS WITH BOTH AC PACKS ON ENG BLD 1 & 3 OPEN. CARGO HEAT OUTFLOW VALVE CLOSED. CABIN PRESS WAS 1000 FT LWR THAN AC ALTITUDE. *S/D* VERIFIED OUTFLOW VALVE, CARGO HEAT OUTFLOW VALVE OPERATION. SAFETY VALVES CLOSED. CK FOR LEAKS AND BLOWN DUCTS IN DISTRIBUTION BAY (NONE FOUND), NEG PRESS VALVE CK GOOD. REMOVED AND REPLACED RT FLOW CONTROL AND MODULATION VALVE AS PER MM 36-12-061. REMOVED GILLINER AND ADJUST HORZ PUSHROD PER IAW 52-11-001-5. 2 L 7 3 4F A3WE 2001042400002 20010424 00002 NM 2001 4 24 PCAA0103021 1 20010325 A 3231 UPLOCK DHAV DHC8 DHC8102 2809003 NM LT MLG MALFUNCTIONED A PCAA K NONE J WARNING INDICATION NR NOT REPORTED 1 EA 13 805EX 228 MDT- CREW REPORTED THAT AFTER GEAR RETRACTION LEFT HAND FORWARD MAIN LANDING GEAR DOOR CLOSES AND THEN OPENS WHEN FLAPS SELECTED TO 15 DEGREES. MAINTENANCE REPLACED LEFT MAIN GEAR DOOR HYDRAULIC FLEX LINE, REPLACED STAB STAY ACTUATOR, AND REPLACED DOOR UPLOCK HOOK ASSEMBLY. RIGGED DOOR AND ACTUATOR ASSEMBLY. ALSO REPLACED WERE RELAYS 3261-K9 AND 3261-K12. OPERATIONAL TEST OF SYSTEM GOOD. FLIGHT TEST SATISFACTORY. 2 H 7 2 4T RT A13NM 2001042400003 20010424 00003 NM 2001 4 24 01FDEA00238 1 20010330 A 2611 473925 CONTROL UNIT BOEING 727 72722 1384002 NM CARGO BAY MALFUNCTIONED A FDEA F ACTIVATE FIRE EXT. B N SMOKE/FUMES/ODORS/SPARKS FALSE WARNING TX TAXI/GRND HDL 1 SO 25 147FE 19080 WHILE HOLDING FOR T/O DURING CROSSBLEED START OF NR 3 ENG. AFT CARGO SMOKE WARNING AND BELL ACTIVATED. FIRED NR 1 FIRE BOTTLE INTO AFT CARGO COMPARTMENT. WARNING STAY ON. INPS AFT CARGO COMP. NO FIRE OR SMOKE. *S/D* REMOVED AND REPLA CED AFT CARGO COMP CONTROL ELECTRONICS UNIT PER MM 26-16-012. SYS CK OK. REPLACED AFT NR 1 FIRE BOTTLE PER MM 26-16-01 4-2. 2 L 7 3 4F A3WE 2001042400004 20010424 00004 NM 2001 4 24 01FDEA00241 1 20010330 A 5315 6540271 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 CORROSION ON LWR CHORD OF FLOORBEAM BS 1010, LBL 12-15 AROUND NUT PLATE HOLES. *S/D* REMOVED AND REPLACED PER FEDEX SR M 53-10-8 FIG 8. 2 L 7 3 4F RT A3WE 2001042400005 20010424 00005 NM 2001 4 24 01FDEA00242 1 20010330 A 5315 65208353 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 CORROSION ON LWR CHORD OF FLOORBEAM AT BS 1070, RBL 25 AT NUT PLATES. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 51- 10-6, 53-10-8 FIG 2. 2 L 7 3 4F RT A3WE 2001042400006 20010424 00006 NM 2001 4 24 01FDEA00243 1 20010330 A 5320 6516350386 BEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 FOUND CORROSION ON I-BEAM AT BS 1182, RBL 25, WL 204. *S/D* OUT OF LIMITS PER FEDEX SRM 53-10-1. REMOVED AND REPLACED PER FEDEX SRM 51-30-2. 2 L 7 3 4F RT A3WE 2001042400007 20010424 00007 CE 2001 4 24 DJFA00116 1 20010320 A 7110 45A3517622 COWLING BEECH MU300 400A 1155402 CE NR 2 ENGINE BUCKLED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 440CW 3596 RK40 COWLING BUCKELED, RIGHT SIDE LOWER INBOARD. 2 H 7 2 4F RT A16SW 2001042400008 20010424 00008 NM 2001 4 24 01FDEA00249 1 20010331 A 3610 652663928 DUCT BOEING 727 72722 1384002 NM NR 3 ENGINE FAILED A FDEA K NONE J WARNING INDICATION CL CLIMB 1 SO 25 181FE 18868 NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUM. DURING CLIMBOUT 17000 FT NR 1 BLD OPEN, NR 2 BLD CLOSED. LIGHT EXTINGUISHED W HILE RUNNING CKLIST FOR STRUT OVERHEAT LIGHT. *S/D* REPLACED DUCT ASSY PER MM 36-00-001-2. OPS AND LEAK CK OK. 2 L 7 3 4F A3WE 2001042400009 20010424 00009 SO 2001 4 24 C2XA01IA187 1 20010330 A 3260 922FS2AGNZ735 PROXIMITY SWITCH EMB 120 EMB120ER 3260203 SO NLG INOPERATIVE A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 17728 120182 IAH - FLIGHT 3412, THE CREW REPORTED THAT THE NOSE GEAR SYSTEM B-TRANSIT / UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE PLACED THE INDICATION ON MEL 32-60-1 CAT B CO NTROL NUMBER 012105, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RETURNED TO IAH ON 04/02/01 WHER E MAINTENANCE REMOVED AND REPLACED THE B-SYSTEM NOSE LANDING GEAR PROXIMITY SWITCH. REMOVED THE MEL, AND THE AIRCRAFT W AS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001042400010 20010424 00010 SO 2001 4 24 C2XA01IA188 1 20010329 A 2121 EVAC523C2 COOLING FAN EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 16723 120169 IAH - FLIGHT 3436, DURING PRE-FLIGHT THE CREW REPORTED SMOKE IN THE COCKPIT. THE AIRCRAFT WAS EVACUATED WITHOUT INCIDEN T. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND GROUND COOLING FAN, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. 2 L 7 2 4T RT A31SO 2001042400011 20010424 00011 SO 2001 4 24 C2XA01TY060 1 20010330 A 5311 14525516001 FRAME EMB 145 EMB145LR SO FUSELAGE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15980 145202 TYS DURING A SCHEDULED INSPECTION, FRAME 63 BETWEEN STRINGERS 7 AND 8 WAS FOUND TO BE CHAFED. MAINTENANCE REPAIRED DAM AGED AREA IAW EMB GST-0967/01, REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2001042400012 20010424 00012 SO 2001 4 24 C2XA01CL071 1 20010401 A 5210 MS21042L3 NUT EMB 145 EMB145 SO CABIN DOOR WORN A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 12957 145080 MSP FLIGHT 4089 THE CREW REPORTED THE MAIN CABIN DOOR WOULD NOT OPEN FROM THE INSIDE. MAINTENANCE INSPECTED AND FOUND T HE BOLT AND NUT ON THE INTERNAL HANDLE ASSEMBLY TO BE WORN. THE HARDWARE WAS REPLACED AND OPERATIONAL CHECKS OF THE DOO R WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. BOLT P/N IS AN3-13A. 2 L 7 2 4F RT T00011AT 2001042400013 20010424 00013 SO 2001 4 24 C2XA01TY061 1 20010330 A 5330 12020334044 SKIN EMB 135 EMB135ER 3260203 SO FUSELAGE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14508 145220 TYS DURING A SCHEDULED INSPECTION, THE LEFT HAND AFT FUSELAGE SKIN AT FRAME 74 BETWEEN STRINGERS 15L AND 17L WAS FOUND TO BE DAMAGED. MAINTENANCE REPAIRED THE DAMAGED AREA IAW EMB SST-1031/00, REPAIR WAS SATISFACTORY. AIRCRAFT RELEASED F OR SERVICE. 2 L 7 2 4F RT T00011AT 2001042400014 20010424 00014 CE 2001 4 24 C2XA01CL072 1 20010402 A 6123 5038912147 SWITCH BEECH 1900 1900D 1154162 CE RT ENGINE FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16540 10843 UE172 SBN FLIGHT 3190 THE CREW REPORTED THE RIGHT AUTO FEATHER SYSTEM WOULD NOT TEST. MAINTENANCE INSPECTED AND REPLACED THE RIGHT ENGINE LOW PRESSURE SWITCH. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT A24CE 2001042400015 20010424 00015 SO 2001 4 24 C2XA01TY062 1 20010331 A 3250 13BF7184 POTENTIOMETER EMB 145 EMB145 SO NLG STEERING FAILED A C2XA O OTHER J WARNING INDICATION LD LANDING 1 SW 27 19966 145131 MEM FLIGHT 3694. THE PILOT REPORTED THAT AFTER LANDING THEY RECEIVED A LANDING GEAR GROUND MESSAGE AND THE AIRCRAFT SL IGHTLY VEERED TO THE RIGHT. MAINTENANCE INSPECTED THE LANDING GEAR SYSTEM AND AFTER EXTENSIVE TROUBLESHOOTING THE AIRCR AFT WAS TEST FLOWN TO TYS. THE TEST FLIGHT WAS UNSATISFACTORY, MAINTENANCE REMOVED AND REPLACED THE RUDDER PEDAL POTENT IOMETER IAW EMB-145-MM 32-50-02, OPERATIONAL CHECKS AND TEST FLIGHT WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001042400016 20010424 00016 SO 2001 4 24 RAIA00103024 1 20010401 A 3234 22270100001 SELECTOR VALVE EMB 145 EMB145ER SO HYD BAY FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 803HK 6193 6193 145077 7607-CHS-DURING TAXI A LOUD THUMPING NOISE IN COCKPIT FLOOR COMING FROM HYDRAULIC COMPARTMENT AREA. MAINTENANCE REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW J41 MAINTENANCE MANUAL. 2 L 7 2 4F RT T00011AT 2001042400017 20010424 00017 SO 2001 4 24 RAIA00103025 1 20010402 A 3260 852701 DOWNLOCK SWITCH EMB 145 EMB145ER SO LT MLG FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 803HK 6193 6193 145077 7607-CHS-DURING TAXI A LOUD THUMPING NOISE IN COCKPIT FLOOR. MAINTENANCE REMOVED AND REPLACED LEFT HAND MAIN LANDING GE AR DOWN LOCK SWITCH IAW J41 MAINTENANCE MANUAL. 2 L 7 2 4F RT T00011AT 2001042400018 20010424 00018 2001 4 24 SWIA972460 4 20010324 A 3418 PANEL EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 194SW 120120 STALL WARNING ON TAKEOFF ROLL. ABORTED TAKEOFF. REMOVED AND REPLACED STALL WARNING TEST PANEL IAW EMB120 MM 27-34-08. OPS CHECK GOOD. P/N: 120-34428-505, S/N ON: 120290, S/N OFF: 120269. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042400019 20010424 00019 SO 2001 4 24 SWIA972461 1 20010327 A 5240 FUEL DOOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT WING UNLATCHED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 583SW 120351 ABORTED TAKEOFF DUE TO DOOR WARNING LIGHT (SERVICE DOOR). FOUND OUTBOARD FUEL DOOR LATCH OPEN. SECURED. GROUND CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042400020 20010424 00020 SO 2001 4 24 SWIA972462 1 20010326 A 3150 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT ACTIVATED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 292SW 120319 ON TAKEOFF ROLL HEARD TRIPLE CHIME AURAL WARNING FOR TRIM. RESET AURAL WARNING UNIT. PERFORMED OPS CHECK OF TRIM SEVER AL TIMES. OPS CHECK NORMAL. COULD NOT DUPLICATE PROBLEM ON GROUND. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042400021 20010424 00021 SO 2001 4 24 SWIA972463 1 20010328 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE T/E FLAP FAILED A SWIA K NONE F FLT CONT AFFECTED LD LANDING 1 NM 07 194SW 120120 INBOARD FLAPS REMAIN AT 25 DEGREES AFTER LANDING WITH FLAP HANDLE AT 0 DEGREES. REMOVED AND REPLACED RT I/B FLAP ACUTAT OR. USED BEAKOUT BOX. ACTUATOR POS BAD AT 15-25 DEGREES SETTING. REF MM 27-50-07 & RII 27-307. NO LEAKS NOTED. OPS CHECK GOOD. ALL OPENED PANELS SECURED. P/N: 320300-1005, S/N ON: 0030, S/N OFF: 0067. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042400023 20010424 00023 SO 2001 4 24 SWIA972465 1 20010326 A 3233 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT MLG OUT OF ADJ A SWIA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 NM 07 251YV 120251 LEFT MAIN LANDING GEAR WOULD NOT RETRACT WITH HANDLE UP, RED GEAR LIGHTS, WITH A VIBRATION IN THE AIRFRAME. RETURN TO F IELD. ADJUSTED LEFT MAIN GEAR ACTUATOR IAW EMB MM 32-32-10. OPS CHECK GOOD. PERFORMED GEAR SWING WITH NO DEFECTS NOTE D. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042400024 20010424 00024 SO 2001 4 24 SWIA972466 1 20010326 A 3150 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT ACTIVATED A SWIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 NM 07 251YV 120251 TAKEOFF TRIM WARNING. ABORTED AND RETURNED TO GATE. RESET AURAL WARNING UNIT. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042400025 20010424 00025 SO 2001 4 24 SWIA972467 1 20010330 A 2752 3203001007 ACTUATOR EMB 120 EMB120RT SO PWA 118 PW118 NE T/E FLAP FAILED A SWIA K NONE F FLT CONT AFFECTED DE DESCENT 1 NM 07 269UE 120194 WHEN SELECTING FLAPS 15 DEGREES AND 25 DEGREES AIRCRAFT ROLLS TO THE RIGHT WITH NO FLAP WARNING INDICATIONS. REMOVED AN D REPLACED RIGHT OUTBOARD FLAP ACTUATOR. OPS CHECK GOOD. P/N: 320300-1007, S/N ON: 0706, S/N OFF: 0931. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042400026 20010424 00026 SO 2001 4 24 SWIA972468 1 20010330 A 2750 3075001007 FCU EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE T/E FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 07 188SW 120039 IN DESCENT THROUGH 18,000 FLAP/ADV SWS LIGHT ILLUMINATED AS WELL AS CONTROL FAULT INBOARD FLAP LIGHTS (2ND FROM TOP) FLA SHING (QRH PROCEDURE UNSUCCESSFUL). CAPT AUTOPILOT DISCONNECTED. TRY TO RE-ENGAGE AND AC PITCHED NOSE DOWN AT RAPID RA TE. REMOVED AND REPLACED THE FLAP CONTROL COMPUTER IAW MM 27-50-06. OPERATED THE FLAPS, COULD NOT DUPLICATE THE PROBLE M AFTER FECU REPLACMENT OPS CHECKS GOOD. P/N ON 307500-1007, S/N ON 0102, S/N OFF 0193. OPERATED THE NR 1 AUOTPILOT SY STEM IAW MM 22-10-00. COULD NOT DUPLICATE THE PROBLEM. NO PITCH TENDANCIES NOTED AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042400027 20010424 00027 NE 2001 4 24 SWIA972469 2 20010330 A 7320 FUEL LINE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE LOOSE A SWIA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 NM 07 291SW 120318 DURING APPLICATION OF TAKEOFF POWER LEFT ENGINE LAGGED BEHIND. THE AUTO FEATHER NOT ARMED WARNING OCCURRED. TIGHTENED LOOSE P3 LINE AT LEFT HMU. PERFORMED POWER ASSURANCE RUN. LEFT AND RIGHT ENGINES ADVANCED EQUAL AND MATCHED PW MM 72-0 0-00 PG 509. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042400028 20010424 00028 SO 2001 4 24 SWIA972470 1 20010331 A 3260 WARNING LIGHT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT ILLUMINATED A SWIA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 NM 07 294SW 120321 ON APPROACH TO SEA, GEAR HANDLE SELECTED DOWN, WHEN THAT WAS DONE. F/O NOTICED OUTBOARD ANTI-SKID INOP LIGHT CAME ON. ALSO, GEAR INDICATED ALL ''A'' AND ''B'' GREEN ON AND ALL''A'' RED LIGHTS ON, PUT GEAR UP FOR GO AROUND, CYCLED GEAR DOW N (ON DOWN WIND LEG) PER QRH. RECEIVED GOOD INDICATOR AND LANDED. CYCLED GEAR, GROUND OPS CHECK GOOD IAW MM 32-60-00. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042400030 20010424 00030 EA 2001 4 24 SWIA972472 1 20010331 A 5610 NP1393216 WINDSHIELD CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT CRACKED A SWIA K NONE O OTHER DE DESCENT 1 NM 07 426SW 7468 FIRST OFFICER''''S WINDSHIELD SHATTERED. CABIN DIFFERENTIAL PRESSURE ON 7.3, NO PRESSURE LOSS. REMOVED AND REPLACED W INDSHIELD WITH SERVICEABLE UNIT IAW MM 56-11-01. C/W PRESSURIZATION CHECK. LEAK CHECK GOOD. P/N: NP139321-6, S/N ON: 00083H3538, S/N OFF: 00165H9933, P/N: 601R33033-10. 2 L 7 2 4F 4 F RT A21EA E15NE 2001042400031 20010424 00031 SO 2001 4 24 SWIA972473 1 20010331 A 3260 UP12041126001 PROXIMITY SENSOR EMB 120 EMB120RT SO PWA 118 PW118 NE RT MLG FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 1117H 120117 ON TAKEOFF, RIGHT MAIN GEAR RED ''A'' LIGHT REMAINED ON AND ALL GEAR CAME UP BUT ALL DOORS STAYED OPEN. NO CHANGE WHEN GEAR HANDLE WAS CYCLED. REMOVED AND REPLACED RIGHT HAND MAIN LANDING GEAR PROXIMITY SENSOR (''A'' DOWN AND ''A'' UP). OPS CHECK GOOD IAW MM 32-60-00. P/N ON UP120-41126-001, P/N ON DOWN120-41127-00. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042400032 20010424 00032 SO 2001 4 24 SWIA972474 1 20010328 A 5240 FUEL DOOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT WING UNLATCHED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 216SW 120285 SERVICED DOOR LIGHT CAME ON ON TAKEOFF ROLL. ABORTED TAKEOFF. FOUND A CAMLOCK POPPED OPEN ON FUEL SERVICE DOOR. SECUR ED LOCK. SERVICE LIGHT OUT. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042400033 20010424 00033 SO 2001 4 24 SWIA972475 1 20010401 A 5753 FLAP TRACK EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE T/E FLAPS DIRTY A SWIA A UNSCHED LANDING F FLT CONT AFFECTED AP APPROACH 1 NM 07 197SW 120186 FLAPS WOULD NOT EXTEND TO 45 DEGREES INBOUND TO CARLSBAD. COMPLIED WITH QRH PROCEDURE FOR FLAP DISAGREEMENT. RETURNED TO LAX. EXAMINED FLAP TRACKS AND ROLLERS FOR OUTBOARD FLAPS AND CLEANED AS NEEDED. OPERATED FLAP SYSTEMS 12 TIMES IAW 27-50-00 AND OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042400034 20010424 00034 SO 2001 4 24 SWIA972476 1 20010331 A 5270 TARGET EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE CARGO DOOR OUT OF ADJ A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 197SW 120186 CARGO DOOR LIGHT ILLUMINATED ON TAKEOFF ROLL. ABORTED TAKEOFF. LIGHT GOES ON AND OFF INTERMITTENTLY. ADJUSTED STRIKE R PLATE ON CARGO LIGHT SWITCH. CYCLED DOOR NUMEROUS TIMES. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042400035 20010424 00035 EU 2001 4 24 AWXA0001569 1 20010402 A 5347 D53112782 SEAT TRACK AIRBUS 320 A320232 3930326 EU CABIN CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 641AW 453 SEAT TRACK CORRODED AT FWD END FR 20 - Y1292 Z120. REPAIRED IAW A320 SRM 53-11-15 FIG 203. 2 L 7 2 4F RT A28NM 2001042400036 20010424 00036 EU 2001 4 24 AWXA0001570 1 20010402 A 5347 D53112782 SEAT TRACK AIRBUS 320 A320232 3930326 EU CABIN CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 641AW 453 SEAT TRACK CORRODED AT FWD END FR 20 - Y765 Z120. REPAIRED IAW A320 SRM 53-11-15 FIG 203. 2 L 7 2 4F RT A28NM 2001042400037 20010424 00037 NM 2001 4 24 AWXA0001571 1 20010402 A 5553 6549558506 FITTING BOEING 737 737277 1384570 NM VERTICAL STAB DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 DURING MAINTENANCE CHECK REMOVAL OF BOLT, RIGHT O/B FWD VERT FIN ATTACH LUG BOLT HOLE WAS DAMAGED AT FS 1088. REMOVED A ND REPLACED LUG AWA ER 15-5383-00029-JS1A. 2 L 7 2 4F RT A16WE 2001042400038 20010424 00038 NM 2001 4 24 AWXA0001572 1 20010402 A 5315 654541046 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 FLOORBEAM REPAIR RBL 25 BS 675 CRACKED. REMOVED AND REPLACED FLOORBEAM REPAIR AT RBL 25 BS 675 IAW B737-200 SRM 51-20-1 PG 13 FIG 2; AND COMPARTMENT BS 500 FRAME IAW SRM 51-40-02 AND 51-70-11 FIG 1 PG 1-6. 2 L 7 2 4F RT A16WE 2001042400039 20010424 00039 NM 2001 4 24 AWXA0001573 1 20010402 A 5320 65C3453719 WEB BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 CRACK IN LWR FLOOR SUPPORT FLANGE AND WEB BS 704-717 BL 0. REPAIRED CRACK IAW B737-200 SRM 51-40-4 PG 1-4 AND SB 737-57 -1210 PG 44-47. 2 L 7 2 4F RT A16WE 2001042400040 20010424 00040 NM 2001 4 24 AWXA0001575 1 20010402 A 5240 65458711 PAN BOEING 737 737277 1384570 NM R1 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 FWD GALLEY DOOR PAN CRACKED AT UPPER HINGE CUTOUT. REPAIRED DOOR PAN IAW AWA ER 15-5210-01086-GF2. 2 L 7 2 4F RT A16WE 2001042400041 20010424 00041 NM 2001 4 24 AWXA0001576 1 20010402 A 5312 6551542 PRESSURE PANEL BOEING 737 737277 1384570 NM LT MLG WW CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 LT WHEEL WELL UPPER PRESSURE WEB CRACKED AT BS 664 LBL 34 AND BS 673 LBL 31. REPAIRED CRACKS IAW AWA ER 15-5702-01082-G F2. 2 L 7 2 4F RT A16WE 2001042400042 20010424 00042 NM 2001 4 24 AWXA0001577 1 20010402 A 5411 6553553152 RIB BOEING 737 737277 1384570 NM NR 2 PYLON CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 RT PYLON L/E FAIRING FWD SEAL RETAINER AND RIB CHAFED BEYOND LIMITS. FORMED, DRILLED AND INSTALLED REPAIR ANGLE IAW SRM 51-40-3 PG1-5 AND 51-30-2 PG 2 & 3. 2 L 7 2 4F RT A16WE 2001042400043 20010424 00043 NM 2001 4 24 AWXA0001578 1 20010402 A 5311 6546538551 FRAME BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 CRACK IN ANGLE AT BS 597 LBL 69 WL 203. REMOVED FRAME AND WEBS; REPLACED FRAME AND REINSTALLED WEBS IAW SRM 51-30-5 PG 4 & 5 AND 51-30-2 PG 1. 2 L 7 2 4F RT A16WE 2001042400044 20010424 00044 NM 2001 4 24 AWXA0001580 1 20010402 A 5753 6571902335 RIB BOEING 737 737277 1384570 NM MID FLAP CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 LEFT I/B MID FLAP I/B RIB CHAFED. CUT OUT DAMAGED AREA; CUT, FITTED, DRILLED AND INSTALLED REPAIR FILLER, PLATE AND DOU BLER IAW B737-200 SRM 51-30-2 PG 2, 3, 8, 9, 13 & 14 AND 57-50-4 PG 8 & 9 FIG 4. 2 L 7 2 4F RT A16WE 2001042400045 20010424 00045 NM 2001 4 24 AWXA0001581 1 20010402 A 5320 6546818 ANGLE BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 ANGLE CRACKED AT FS 663 BLKHD WL 207. REMOVED AND REPLACED ANGLE IAW B737-200 SRM 51-40-4 PG 1 FIG 1 AND 51-30-2 PG 1. 2 L 7 2 4F RT A16WE 2001042400046 20010424 00046 NM 2001 4 24 AWXA0001582 1 20010402 A 5320 6516301 ATTACH ANGLE BOEING 737 7373S3 1384711 NM FUSELAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 FS 178 BLKHD WL 195 RBL 24-28 ATTACH ANGLE HAS ELONGATED HOLES. REMOVED AND REPLACED ANGLE AND CLIP IAW BOEING DWG 65-1 6301 AND SRM 51-40-02 PG 10. 2 L 7 2 4F RT A16WE 2001042400047 20010424 00047 NM 2001 4 24 AWXA0001584 1 20010402 A 5311 6546803 FRAME BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 FWD CARGO COMPARTMENT STA 500 FRAME HAS A .125 INCH CRACK AT RBL 5. FABBED REPAIR ANGLE AND FILLER; LOCATED, DRILLED AN D INSTALLED REPAIR IAW B737-300 SRM 51-40-02 AND 51-70-11 FIG 1 PG 1 - 6. 2 L 7 2 4F RT A16WE 2001042400048 20010424 00048 NM 2001 4 24 AWXA0001583 1 20010402 A 5753 654647019 RIB BOEING 737 7373S3 1384711 NM MID FLAP CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 RIB AND CHAFE STRIP WORN THROUGH ON I/B END OF LEFT O/B MID FLAP. REMOVED AND REPLACED RIB AND CHAFE STRIP IAW B737-300 SRM 51-40-02 PG 3 & 6 AND 51-40-05 PG 2. 2 L 7 2 4F RT A16WE 2001042400049 20010424 00049 NM 2001 4 24 AWXA0001585 1 20010402 A 5312 6550781 PRESSURE PANEL BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 CRACK IN LT WHEEL WELL PRESSURE PANEL AT FS 663 LBL 34. TRIMMED OUT DAMAGED AREA; FABBED, DRILLED AND INSTALLED REPAIR DOUBLER, FILLER, STIFFENER AND CHANNEL IAW AWA ER 03-5710-01073-JS1. 2 L 7 2 4F RT A16WE 2001042400050 20010424 00050 EA 2001 4 24 COMA0160353 1 20010331 A 5553 600210615 BUSHING CNDAIR CL600 CL6002B19 EA VERTICAL STAB WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 981CA 9837 7163 RT VERTICAL STAB BUSHING IS MIGRATED AT HORIZ STAB PIVOT POINT. REMOVED MIGRATED BUSHING. MACHINED FLANGE OF NEW BUSHI NG P/N 600-21061-7 TO .077 IAW WVAC EO 601R-55-2353. INSTALLED MACHINED BUSHING IAW CRJ AMM 20-26-0-910-803. REAMED BU SHING TO TOLERANCE 1.5001 IAW DWG 600-21-29. 2 L 7 2 4F RT A21EA 2001042400051 20010424 00051 EA 2001 4 24 COMA0160354 1 20010328 A 5320 BEAM CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 943CA 7062 VERTICAL BEAM AT RBL 27 AND LBL 27 FS 409.0 + 128 INBOARD LOWER FASTENERS CRACKED. REPAIRED BOTH BEAMS IAW WVAC EO 601R -53-2336C. 2 L 7 2 4F RT A21EA 2001042400052 20010424 00052 EA 2001 4 24 COMA0160355 1 20010328 A 5553 601R55310025 BUSHING CNDAIR CL600 CL6002B19 EA VERTICAL STAB WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 941CA 7050 RIGHT VERT STAB BUSHING AT HORZ STAB PIVOT POINT WORN. REMOVED AND REPLACED BUSHING P/N 601R-55-31-001-5 IAW CRJ AMM 20 -26-00-910-803. MACHINED BUSHING IAW WVAC EO 601R-55-2345. BORE WITHIN TOLERANCE IAW CRJ DRAWING 600-21058. REAMED BU SHING IAW CRJ DRAWING 600-21029. 2 L 7 2 4F RT A21EA 2001042400053 20010424 00053 NM 2001 4 24 PCAA0103023 1 20010328 A 3060 7826895 BRUSH BLOCK DHAV DHC8 DHC8102 2809003 NM RT ENGINE SHORTED A PCAA K NONE O OTHER DE DESCENT 1 EA 13 830EX 1161 46 155 ALB- FLIGHT 3945 CREW REPORTED EMERGENCY LIGHTS FLICKER IN DESCENT. MAINTENANCE FOUND RIGHT PROP DEICING BRUSH BLOCK SH ORTED AND OVERHEATING AT BACKING PLATE. BRUSH BLOCK AND DEICE CABLE ASSEMBLY REPLACED. OPERATIONAL CHECK GOOD. AIRCRA FT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001042400054 20010424 00054 NM 2001 4 24 PCAA0103024 1 20010330 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 812EX 312 BGM- DURING ROUTING MAINTENANCE VISIT, SEVERAL EMERGENCY PATHWAY LIGHTS FOUND INOPERATIVE. BROKEN WIRES UNDER FLOOR REP AIRED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001042400055 20010424 00055 NM 2001 4 24 HNAA0100023 1 20010402 A 5755 FASTENER DHAV DHC8 DHC8102 2809003 NM RT SPOILER MISSING A HNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 07 940HA 156 OUTBOARD ROLL SPOILER DOES NOT COME UP WHEN TURNING CONTROL WHEEL TO THE RIGHT. (NO INDICATION ON PFCS) MAINTENANCE FO UND HARDWARE MISSING WT THE CENTER HINGE POINT OF RIGHT HAND OUTBOARD SPOILER. REPLACED HARDWARE AND REPAIRED DAMAGE TO BRACKET. 2 H 7 2 4T RT A13NM 2001042400056 20010424 00056 CE 2001 4 24 GLBA2001069 1 20010331 A 5270 SWITCH BEECH 1900 1900D 1154162 CE CARGO DOOR DIRTY A GLBA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 01 94UX UE94 CARGO DOOR ANNICIATOR ILLUMINATED IN FLIGHT. CLEANED MICROSWITCHES, OPS CHECKED GOOD. 2 L 7 2 4T RT A24CE 2001042400057 20010424 00057 CE 2001 4 24 GLBA2001070 1 20010401 A 2140 9938001001 BYPASS VALVE BEECH 1900 1900D 1154162 CE RT ACM INOPERATIVE A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 01 261GL 10793 UE261 CABIN HEAT NOT WORKING. REMOVED AND REPLACED ACM BYPASS VALVE, OPS CHECKED GOOD. 2 L 7 2 4T RT A24CE 2001042400058 20010424 00058 CE 2001 4 24 GLBA2001071 1 20010401 A 3260 WARNING LIGHT BEECH 1900 1900D 1154162 CE COCKPIT MALFUNCTIONED A GLBA O OTHER P NO WARNING INDICATION AP APPROACH 1 CE 01 195GL UE195 NOSE GEAR LIGHTS TOOK TWO CYCLES TO ILLUMINATE. INSPECTED GEAR SYSTEM CND. 2 L 7 2 4T RT A24CE 2001042400059 20010424 00059 NE 2001 4 24 GLBA2001072 2 20010401 A 7261 PW118A ENGINE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT ENGINE FLUCTUATES A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 297UX 23088 67 120297 115173 ENGINE OIL FLUCUATION ON CLIMBOUT. REMOVED AND REPLACED ENGINE. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042400060 20010424 00060 WP 2001 4 24 TWAA0105902 1 20010328 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 909TW 49170 DURING CHECK-C MAINT FOUND EXCESSIVE CORROSION ON NUMBER 1 FLOOR TRACK SECTION STA 798 TO 1030, PRODUCTION SPLICES. REM OVED AND REPLACED FLOOR TRACK FROM PRODUCTION SPLICE AT STA 798 TO PRODUCTION SPLICE STA 1030, PER SPM 6-70-01 AND SRM 5 1-30-1. PAINTED TRACK PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001042400061 20010424 00061 WP 2001 4 24 TWAA0105903 1 20010328 A 5312 BULKHEAD DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 909TW 49170 DURING CHECK-C MAINT FOUND CORROSION ON AFT PRESSURE BULKHEAD AT STA 1338, JUST AFT OF END OF LONGERON 30. CORROSION WA S ON TRIANGULAR DOUBLER AT LOWER END OF AFT PRESSURE BULKHEAD AT 0BL. CLEANED CORROSION PER SPM 6-80-01 AND FOUND BEYON D LIMITS. REMOVED CORRODED DOUBLER AND FABRICATED NEW PART AND INSTALLED PER SPM 6-70-01 AND DRAWING 5910130. PRIMED A ND PAINTED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001042400062 20010424 00062 WP 2001 4 24 TWAA0105904 1 20010329 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 909TW 49170 DURING CHECK-C MAINT FOUND CORROSION ON INTERCOSTAL IN FWD CARGO COMPT, STA 434 TO 446, AT LONGERON 29R. REMOVED CORROD ED PART AND REPLACED PER SPM 6-70-01. 2 L 7 2 4F A6WE 2001042400063 20010424 00063 WP 2001 4 24 TWAA0105905 1 20010329 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 909TW 49170 DURING CHECK-C MAINT FOUND CORROSION ON LONGERON 20L, STATION 218 TO 224. REMOVED AND REPLACED LONGERON FROM STA 200 TO 224, FACTORY SPLICE TO FWD END, PER SPM 6-70-01, AND SRM 51-30-1. USED SRM 51-30-5 FOR FASTENER INSTALLATION. 2 L 7 2 4F A6WE 2001042400064 20010424 00064 WP 2001 4 24 TWAA0105906 1 20010329 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 909TW 49170 DURING CHECK-C MAINT FOUND CORROSION IN CABIN TRACK NUMBER 1, STA 1234 TO 1236. REPLACED TRACK NUMBER 1 AT STA 1234 TO 1236 WITH NEW. TRANSFERRED FASTENER HOLES PER SRM 51-10-3. INSTALLED PER SRM 51-30-1. PRIMED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001042400065 20010424 00065 WP 2001 4 24 TWAA0105907 1 20010329 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 909TW 49170 DURING CHECK-C MAINT FOUND CORROSION IN CABIN TRACK NUMBER 1 AT STA 1202 TO 1208. REPLACED TRACK NUMBER 1 AT STA 1202 T O 1208 WITH NEW. TRANSFERRED FASTENERS HOLES PER SRM 51-10-4. INSTALLED PER SRM 51-30-1. PRIMED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001042400066 20010424 00066 WP 2001 4 24 TWAA0105908 1 20010328 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 992Z 47095 DURING OP 15 MAINT CHECK FOUND CORROSION ON SKIN AT STA 351 ON RT SIDE AT LONGERON 29R. INTERIM REPAIR WAS INSTALLED. REPAIRED PER SRM 53-04, FIG 38, SHEET 24, AND ARA 17539. 2 L 7 2 4F A6WE 2001042400067 20010424 00067 WP 2001 4 24 TWAA0105909 1 20010329 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 992Z 47095 DURING OP 15 MAINT CHECK FOUND FUSELAGE SKIN CRACKED AT STA 1079, CANTED BULKHEAD, LONGERON 3L AND 5L. INSTALLED REPAIR DOUBLER PER SRM 53-04, FIG 27, PAGE 143 AND SRM 51-01, PAGE 2 PARAGRAPH 3. 2 L 7 2 4F A6WE 2001042400068 20010424 00068 WP 2001 4 24 TWAA0105910 1 20010329 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT FOUND DENT IN FUSELAGE FROM STA 229 TO 234, BETWEEN LONGERON 24L AND 25L. DENT WAS 5 INCHES BY 1.7 50 BY 0.020 DEEP. REPAIRED DENT IN FUSELAGE PER SRM 53-04, PAGE 37 FIG 12B. 2 L 7 2 4F A6WE 2001042400069 20010424 00069 WP 2001 4 24 TWAA0105911 1 20010323 A 5312 BULKHEAD DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 928TW 48012 DURING CHECK-C MAINT AT THE AFT LT LAVATORY, CORROSION WAS FOUND ON THE AFT PRESSURE BULKHEAD, STA 1338 FROM CUSP TO LON GERON 21L. REMOVED CORROSION. INSTALLED REPAIR DOUBLERS ON AFT PRESSURE BULKHEAD PER ARA 17570, PAGE 1 AND 2. 2 L 7 2 4F A6WE 2001042400070 20010424 00070 WP 2001 4 24 TWAA0105912 1 20010329 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT FOUND DENT IN FUSLEAGE AT STA 237, BETWEEN LONGERON 24L AND 25L. DENT WAS 1 INCH BY 2 IN BY 0.050 DEEP. REPAIRED DENT PER 53-04, PAGE 37 FIG 12B. 2 L 7 2 4F A6WE 2001042400071 20010424 00071 NM 2001 4 24 TWAA0105901 1 20010329 A 5414 SKIN BOEING 767 7673Y0 NM NR 2 PYLON DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 632TW 24953 ON THE NUMBER 2 PYLON, THE INBD SIDE PANEL JUST AFT OF THE HYD ACCESS PANEL HAD A HOT BOND REPAIR THAT WAS LOOSE. INSTA LLED EXTERNAL DOUBLER 0.063 301 1/2 STAINLESS STEEL WET WITH PRC SECURED WITH HI-LOKS PER SRM 54-53-70, FIG 203 SHEET 1 TO 10. CHECK-C 3-10-01 LAX. 2 L 7 2 4F RT A1NM 2001042400072 20010424 00072 CE 2001 4 24 GLBA2001073 1 20010402 A 2910 HYDRAULIC LINE BEECH 1900 1900D 1154162 CE RT MLG LEAKING A GLBA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 CE 01 211UX UE211 RIGHT MAIN GEAR HYDRAULIC HOSE LEAKING. 2 L 7 2 4T RT A24CE 2001042400073 20010424 00073 WP 2001 4 24 NACA2001015 1 20010313 A 5330 SKIN DOUG DC6 DC6A 3021706 WP FUSELAGE CRACKED A NACA K NONE O OTHER IN INSP/MAINT 1 AL 03 43872 533294 CRACK IN FUSELAGE SKIN AT STA R89 LONGERON R24. REMOVED INTERNAL DOUBLER, SAFETY SEALS, AND AFT SECTION OF LONGERON R24 (8 INCHES). REMOVED SECTION OF SKIN FOR CORROSION. INSTALLED NEW INTERNAL DOUBLER, LONGERON SPLICE AND LAP SEAM REPAI R PER DC-6 O/H MANUAL CHAPTER 12 AND NAC DRAWING FOR UPPER LAP SEEM REPAIR. 2 L 7 4 4R 6A3 2001042400074 20010424 00074 SO 2001 4 24 C2XA01IA189 1 20010330 A 3231 SV14H11004 SOLENOID VALVE EMB 120 EMB120ER 3260203 SO LANDING GEAR DR FAILED A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 16723 120169 IAH - FLIGHT 3423, THE CREW REPORTED THAT THE LANDING GEAR DOORS WILL NOT CLOSE. THE AIRCRAFT LANDED AT IAH WITHOUT INC IDENT WHERE MAINTENANCE REMOVED AND REPLACED THE GEAR DOOR SOLENOID VALVE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO S ERVICE. 2 L 7 2 4T RT A31SO 2001042400075 20010424 00075 SO 2001 4 24 C2XA01IA190 1 20010331 A 3260 922AA2YA6PZ722 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO LT MLG OUT OF ADJ A C2XA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 27 58733 120197 IAH - FLIGHT 3244, THE CREW REPORTED THAT THE SYSTEM-A GEAR INDICATION LIGHT ILLUMINATED ON TAKEOFF ROLL. THE CREW ABOR TED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE ADJUSTED THE LEFT MAIN LANDING GEAR A-SYSTEM PROXIMITY SENSOR, AND TH E AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001042400076 20010424 00076 NE 2001 4 24 RAIA00104001 2 20010402 A 7310 3035681 FUEL FILTER AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW124B NE RT ENGINE CLOGGED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 722TE 220 124172 7320-STL-DURING TAKEOFF RIGHT HAND ENGINE FUEL CLOG LIGHT CAME ON. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND ENGI NE FUEL FILTER IAW ATR72 MAINTENANCE MANUAL. 2 H 7 2 4T 4 T RT A53EU E2ONE 2001050300251 20010503 00251 NM 2001 5 3 01FDEA00244 1 20010331 A 5711 SPAR BOEING 727 72725C 138400H NM CNTR WING BOX CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 124FE 19360 DURING ROUTINE INSP, THE AFT FACE OF THE CENTER WING TANK FOUND CORRODED 9 INCHES UP FROM BOTTOM OF THE TANK AT RBL 9. *S/D* REPAIRED REAR SPAR PER IAW FEDEX EA 7-5710-57223. 2 L 7 3 4F A3WE 2001042400077 20010424 00077 NM 2001 4 24 01FDEA00252 1 20010403 A 3610 CLAMP BOEING 727 727225 1384077 NM BLEED AIR LOOSE A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SO 25 461FE 22548 AFT LEVEL OFF LWR AFT BODY O/H LIGHT ILLUM, RED TAB PROC UTILIZED AND LIGHT EXT. SECURED CLAMP AT PURGE BLD LINE ON NR 1 ENG BLD AIR CLEANER, NO LEAKS NOTED. PERF O/H DETECT ADJUST AND TEST AND OPS CK NORM PER B727 MM 26-14-000-5. 2 L 7 3 4F A3WE 2001042400078 20010424 00078 WP 2001 4 24 01FDEA00253 1 20010403 A 2780 SLAT DOUG DC10 DC1030F 3023504 WP WING FAILED A FDEA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 303FE 46802 DURING SLAT EXT BEFORE LAND SLAT DISAGREE STAY ILLUMINATED. RED TAB WERE ACCOMPLISH AND A NO SLAT WITH FLAPS LAND WAS A CCOMPLISH. REMOVED AND REPLACED S1-379 PER MM 27-84-02-2 PG 201. FUNCTIONAL CK GOOD PER PARAGRAPH 3. ACFT OK FOR CONT SERVICE. 2 L 7 3 4F RT A22WE 2001042400079 20010424 00079 NM 2001 4 24 01FDEA00254 1 20010403 A 5320 651630616 STIFFENER BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 CORROSION ON FWD RT CORNER OF NOSE WHEEL WELL STIFFENER BS 227, WL 165, RBL 20. *S/D* REPAIRED PER FEDEX SRM 51-40-4. 2 L 7 3 4F RT A3WE 2001050300249 20010503 00249 NM 2001 5 3 01FDEA00246 1 20010331 A 5711 SPAR BOEING 727 72725C 138400H NM CTR FUEL TANK CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 124FE 19360 DURING ROUTINE INSP, THE CTR FUEL TANK AFT WEB FOUND CORRODED ON THE AFT FACE FROM LBL 15 TO LBL 18, 6-8 IN UP FROM BOTT OM OF TANK. *S/D* REPAIRED REAR SPAR WEB PER IAW FEDEX EA 7-5710-57223. 2 L 7 3 4F A3WE 2001042400080 20010424 00080 SO 2001 4 24 C2XA01TY063 1 20010401 A 4910 12013413501 SKIN EMB 145 EMB145LR SO APU COWLING DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15980 145202 TYS DURING A SCHEDULED INSPECTION THE APU COWLING L-PROFILE WAS FOUND TO BE DAMAGED. MAINTENANCE REPAIRED THE APU COWL ING IAW EMB GST-0971/01, REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED FOR SERVICE UPON COMPLETION OF INSPECTI ON. 2 L 7 2 4T RT T00011AT 2001042400081 20010424 00081 SO 2001 4 24 C2XA01TY064 1 20010401 A 5320 14521718003 ANGLE EMB 145 EMB145LR SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15980 145202 TYS DURING A SCHEDULED INSPECTION THE AFT LEFT HAND RAMP ANGLE ON THE LEFT OMEGA BEAM WAS FOUND TO CORRODED AT FRAME 20 . MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW EMB-145 SRM-51-30-01, 51-40-02 AND EMB-145 CPM-51-21-03. THE REP AIR WAS SATISFACTORY, AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2001042400082 20010424 00082 SO 2001 4 24 C2XA01TY065 1 20010401 A 5350 12043610003 SKIN EMB 145 EMB145LR SO TAIL CONE NICKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15980 145202 TYS DURING A SCHEDULED INSPECTION THE TAIL CONE WAS FOUND TO BE NICKED BEYOND MANUFACTURES LIMITS. MAINTENANCE REPAIRE D THE TAIL CONE IAW EMB GST-0994/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSP ECTION 2 L 7 2 4T RT T00011AT 2001042400083 20010424 00083 EU 2001 4 24 C2XA01BT047 1 20010404 A 5320 S5397142420101 INTERCOSTAL AEROSP ATR42 ATR42320 8680930 EU FUSELAGE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 25811 094 DURING C-CHECK INSPECTION FOUND INTERCOSTAL BETWEEN FRAME 27A AND 28A STRINGER 17 TORN. MAINTENANCE REMOVED AND REPLACE D INTERCOSTAL IAW ATR42 SRM 51-25-01. 2 H 7 2 4T RT A53EU 2001042400084 20010424 00084 NM 2001 4 24 0101216743 1 20010220 A 5320 STRAP BOEING 747 747249F 1384849 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 643NW 22245 DURING L-CHECK, FOUND CRACK IN LT FRAME INNER STRAP AT BS 2231 STR 25L. REPAIRED PER EA 67-165014. 2 L 7 4 4F A20WE 2001042400085 20010424 00085 WP 2001 4 24 0101221146 1 20010215 A 5310 DOUBLER DOUG DC10 DC1040 3023508 WP FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 146US 46755 DURING M-CHECK, FOUND CORROSION ON FORWARD CARGO DOOR JAMB DOUBLER AT BS 910 ABOVE L43R. REPAIRED PER EA 11-180797. 2 L 7 3 4F A22WE 2001042400086 20010424 00086 WP 2001 4 24 0101231146 1 20010228 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 146US 46755 DURING M-CHECK, FOUND CORROSION ON VERTICAL LEG OF LONGERON AT NUMBER 3 AIR CONDITIONING EXHAUST DOOR CUTOUT AT BS 515-5 20 JUST ABOVE THE LOWER EDGE. REPAIRED PER EA 11-180800. 2 L 7 3 4F A22WE 2001042400087 20010424 00087 WP 2001 4 24 0101241141 1 20010301 A 5330 SKIN DOUG DC10 DC1040 3023508 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 141US 46750 DURING LINE CHECK, FOUND CRACK IN NOSE LANDING GEAR CUTOUT RT FORWARD CORNER SKIN AT BS 464. REPAIRED PER EA 11-182711. 2 L 7 3 4F A22WE 2001042400088 20010424 00088 EU 2001 4 24 C2XA01BT048 1 20010404 A 5313 S5397140220300 STRINGER AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 25811 094 DURING C-CHECK INSPECTION FOUND FRAME 27A, STRINGER 14R TO BE CRACKED. MAINTENANCE REPAIRED THE STRINGER IAW ATR42 SRM 53-91-43 FIGURE 405. 2 H 7 2 4T RT A53EU 2001042400089 20010424 00089 EU 2001 4 24 C2XA01BT049 1 20010404 A 5320 S5397142420001 INTERCOSTAL AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 25811 094 DURING C-CHECK INSPECTION FOUND IN WHEEL WELL, INTERCOSTAL BETWEEN FRAME 27A AND FRAME 28A AT STRINGER 17L TO BE CRACKED . MAINTENANCE REMOVED AND REPLACED INTERCOSTAL IAW ATR42 SRM 51-25-01. 2 H 7 2 4T RT A53EU 2001042400090 20010424 00090 EU 2001 4 24 C2XA01BT050 1 20010404 A 5315 S5367240820200 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 25811 094 DURING C-CHECK INSPECTION FOUND FLOORBEAM AT FRAME 39 TO BE BADLY CORRODED. MAINTENANCE REPAIRED FLOORBEAM AT FRAME 39 IAW ATR42 SRM 53-00-00 PAGE 438 AND 439. 2 H 7 2 4T RT A53EU 2001042400091 20010424 00091 EU 2001 4 24 C2XA01BT051 1 20010404 A 5347 S5367800120200 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 25811 094 DURING C-CHECK INSPECTION FOUND RIGHTHAND INBOARD SEAT TRACK TO BE CORRODED AT FRAME 36. MAINTENANCE REPAIRED SEAT TRAC K AT FRAME 36 IAW ATR42 SRM 53-00-00 FIGURE 437. 2 H 7 2 4T RT A53EU 2001042400092 20010424 00092 EU 2001 4 24 C2XA01BT052 1 20010404 A 5320 S53678008268 INTERCOSTAL AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 25811 094 DURING C-CHECK FOUND BOTH FORWARD AND AFT INTERCOSTALS UNDER SERVICE DOOR THRESHOLD TO BE CORRODED. MAINTENANCE FABRICA TED NEW FORWARD AND AFT INTERCOSTALS IAW ATR42 SRM 53-67-70 AND INSTALLED FORWARD AND AFT INTERCOSTALS IAW ATR42 SRM 51- 25-01. 2 H 7 2 4T RT A53EU 2001042400093 20010424 00093 NM 2001 4 24 AWXA0001586 1 20010403 A 5320 6520726 WEB BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 FWD CARGO PIT STA 492.4 AFT OF CARGO SCUFF PLATE CLOSE OUT WEB CRACKED. CUT OUT CRACK; HFEC - NO CRACKS NOTED. FABBED DOUBLER AND SHIM IAW SRM 51-70-13 FIG 1; INSTALLED REPAIR IAW 51-70-13 FIG 1. 2 L 7 2 4F RT A16WE 2001042400094 20010424 00094 NM 2001 4 24 AWXA0001587 1 20010403 A 5320 6720382 INTERCOSTAL BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 INTERCOSTAL CRACKED 1.0 INCH FS 180 WL 195 RBL 24. REMOVED CRACKED INTERCOSTAL IAW SRM 51-4-02; FABBED NEW PART IAW DWG 65-16300; TREATED AND PRIMED AND INSTALLED INTERCOSTAL IAW SRM 51-4-02 AND 51-20-01. 2 L 7 2 4F RT A16WE 2001042400095 20010424 00095 NM 2001 4 24 AWXA0001588 1 20010403 A 5320 65C273085 FLOOR SUPPORT BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 AFT CARGO COMPT STA 887 LONG 25L CIRCUMFERENTIAL HAS CORROSION. REMOVED CIRCUMFERENTIAL FLOOR SUPPORT; FABBED IAW DWG 6 5C27308; ALODINED AND PRIMED IAW SRM 51-20-01 AND INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001042400096 20010424 00096 NM 2001 4 24 AWXA0001589 1 20010403 A 5230 6547952309 STIFFENER BOEING 737 7373Y0 1384671 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 LWR FWD STIFFENER CAP CRACKED AND BROKEN AT UPPER END AFT CARGO DOOR BS 834. REPLACED IAW DWG 65-47952, SRM 51-10-02 AN D 52-30-01. 2 L 7 2 4F RT A16WE 2001042400097 20010424 00097 NM 2001 4 24 AWXA0001590 1 20010403 A 5230 6547952514 WEB BOEING 737 7373Y0 1384671 NM CARGO DOOR GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 AFT CARGO DOOR LWR AFT STIFFENER WEB HAS DEEP TOOLING MARKS AND GOUGES AT UPPER END. FABBED STIFFENER WEB IAW DWG 65-47 952, SRM 51-10-02 AND 52-30-01. 2 L 7 2 4F RT A16WE 2001042400098 20010424 00098 NM 2001 4 24 AWXA0001591 1 20010403 A 5320 69374024 ANGLE BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 CABIN FS 303 STR 17R CREASE BEAM, ANGLE CRACKED. REMOVED FLOOR BOARDS IAW M/M 53-21-00; REMOVED AND REPLACED CRACKED AN GLE IAW SRM 51-40-02; REINSTALLED FLOOR BOARDS IAW MM 53-21-00. 2 L 7 2 4F RT A16WE 2001042400099 20010424 00099 NM 2001 4 24 AWXA0001592 1 20010403 A 4910 6550938269 DUCT BOEING 737 7373Y0 1384671 NM APU CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 APU INLET DUCT FWD I/B LWR CORNER CRACKED. REPAIRED PART BY WELDING PER BAC 5975 IAW ENGINEERING RESPONSE; HFEC INSPECT ED - NO CRACKS NOTED. 2 L 7 2 4F RT A16WE 2001042400100 20010424 00100 NM 2001 4 24 AWXA0001593 1 20010403 A 4910 6550938269 DUCT BOEING 737 7373Y0 1384671 NM APU CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 INSIDE SKIN CRACKED AT RIVET IN APU INLET DUCT FOR I/B Z-ANGLE STIFFENER TOP END. REPAIRED PART BY WELDING PER BAC 5975 IAW ENGINEERING RESPONSE; HFEC INSPECTED - NO CRACKS NOTED. 2 L 7 2 4F RT A16WE 2001042400101 20010424 00101 NM 2001 4 24 AWXA0001594 1 20010403 A 5320 65C3760727 STIFFENER BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 VERT STIFFENER CRACKED 2 PLACES FS 178 WL 184 ON I/B AND O/B EXTRUSION LATERAL FLANGES. REPAIRED DAMAGED AREA OF STIFFE NERS IAW SRM 53-10-08; RECONNECTED HORIZ STAB FWD CONTROL MECHANISM TO FWD BLKHD 178; RETENSIONED CABLES STA AND STB IAW MM 27-41-01; CHAIN MECHANISM MOVEMENT GOOD IAW MM 27-41-00; OPS CHECKED GOOD. 2 L 7 2 4F RT A16WE 2001042400102 20010424 00102 NM 2001 4 24 AWXA0001595 1 20010403 A 5311 651630086 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 FUSELAGE RT SIDE CHORD AT WL 207 STA 178 CRACKED. INSTALLED NEW CHORD IAW SRM 51-40-02 PG 1, 2, 9, 10 W/ REF TO DWG 65- 16300 SHEET 5 FRAME 1-7. 2 L 7 2 4F RT A16WE 2001042400103 20010424 00103 NM 2001 4 24 AWXA0001596 1 20010403 A 5311 651630086 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 FUSELAGE LT SIDE CHORD AT WL 207 STA 178 CRACKED. INSTALLED NEW CHORD IAW SRM 51-40-02 PG 1, 2, 9, 10 W/ REF TO DWG 65- 16300 SHEET 5 FRAME 1-8. 2 L 7 2 4F RT A16WE 2001042400104 20010424 00104 NM 2001 4 24 AWXA0001597 1 20010404 A 2910 271N61191 HYDRAULIC LINE BOEING 757 7572S7 1384962 NM LT MLG LEAKING A AWXA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 WP 28 906AW 23568 PHX - EMERGENCY LANDING - 3/28/01 - ON FINAL APPROACH INTO PHX THE AIRCRAFT LOST LEFT HYDRAULIC SYSTEM PRESSURE AND QUAN TITY; THE AIRCRAFT LANDED W/O INCIDENT. MAINTENANCE FOUND THE LT MAIN LANDING GEAR DOWNLOCK ACTUATOR LINE LEAKING AND R EPLACED IT; NO OTHER LEAKS WERE FOUND. 2 L 7 2 4F RT A2NM 2001042400105 20010424 00105 NE 2001 4 24 AWXA0001598 2 20010404 A 7321 FMU500MK4 FMU AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NR 2 ENGINE FAILED A AWXA C ABORTED TAKEOFF X ENGINE FLAMEOUT TO TAKEOFF 1 WP 28 628AW 20777 3754 67 V0208 SEA - ABORTED TAKEOFF - 4/2/01 - NR 2 ENGINE FLAMEOUT. ON TAKEOFF AFTER SETTING TAKEOFF POWER AND ABOUT 60 KTS THERE WA S A SURGE ON NR 2 ENGINE AND IT SHUT DOWN; THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. THE POST FLIGHT REPORT FA ULTED THE NR 2 ENGINE FUEL METERING UNIT (FMU); MAINTENANCE PERFORMED BITE CHECKS ON THE NR 2 ENGINE FADEC & EEC W/ NO F AULTS REPORTED. MAINTENANCE REPLACED THE NR 2 ENGINE FMU IAW AWA TASK CARD RSM71304; ENGINE RUNS AND FUNCTIONAL CHECKS WERE GOOD. 2 L 7 2 4F 4 F RT A28NM E311NE 2001042400106 20010424 00106 WP 2001 4 24 TWAA0106001 1 20010403 A 3350 408822101 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9402W 53138 THE OVERHEAD EMERGENCY LIGHTS IN THE COCKPIT AND FORWARD ENTRY WERE INOPERATIVE. REPLACED THE BATTERIES IN THE BATTERY PACK. CHECK-C 12-14-00 MCI. 2 L 7 2 4F RT A6WE 2001042400107 20010424 00107 WP 2001 4 24 TWAA0106002 1 20010329 A 5320 TIE CLIP DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 906TW 49160 DURING CHECK-C MAINT IN THE AFT CABIN FOUND CORROSION AT TIE CLIP FROM FLOORBEAM AT STA 1338 TO LONGERON 18L. REMOVED C ORROSION PER SPM 6-80-1. FABRICATED AND INSTALLED NEW TIE CLIP PER DRAWING 9910154-21 AND PAINTED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001042400108 20010424 00108 WP 2001 4 24 TWAA0106003 1 20010329 A 5320 BRACKET DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 906TW 49160 DURING CHECK-C IN THE AFT CABIN FOUND CORROSION AT BRACKET FOR FUEL LINE HOUSING CLAMP AT STA 1316, ABOVE LONGERON 18L. REMOVED CORROSION PER SPM 6-80-1. INSTALLED NEW BRACKET PER SRM 51-30. PAINTED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001042400109 20010424 00109 NM 2001 4 24 QXEA0100434 1 20010403 A 2120 UNKNOWN DHAV DHC8 DHC8202 2809007 NM GALLEY ODOR A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 345PH 476 PDX - F/A REPORTED SMELLING GAS FROM BEVERAGE CART RECEPTICLE. INSP GALLEY AREA FOR EVIDENCE OF FUEL, NONE NOTED. RAMP AGENTS CHANGE GALLEY TRASH BIN. NO OTHER DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001042400110 20010424 00110 SO 2001 4 24 C2XA01IA191 1 20010402 A 3350 110049 CHARGER EMB 145 EMB145ER SO CABIN DEFECTIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14930 145011 IAH - DURING MAINTENANCE INSPECTION, THE LEFT HAND EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE RE MOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY CHARGER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001042400111 20010424 00111 SO 2001 4 24 C2XA01IA192 1 20010402 A 3350 276005 FUSE EMB 145 EMB145ER SO CABIN BLOWN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15926 145005 IAH - FLIGHT 4213, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED SEVERAL EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENA NCE REMOVED AND REPLACED A BLOWN FUSE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001042400112 20010424 00112 SO 2001 4 24 C2XA01IA193 1 20010403 A 3350 D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15713 120114 IAH - FLIGHT 3471, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT SEVERAL EMERGENCY LIGHTS REMAINED ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001042400113 20010424 00113 SO 2001 4 24 C2XA01IA194 1 20010402 A 2150 8152402 ACM EMB 145 EMB145LR SO A/C BAY FAILED A C2XA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 13992 145284 IAH - FLIGHT 4054, DURING TAXI THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN DURING TAXI. THE CREW SHUT DOWN THE NUM BER ONE PACK, AND RETURNED TO THE GATE WHERE MAINTENANCE PLACED THE NUMBER ONE PACK ON MEL 21-51-00 CONTROL NUMBER 01219 9, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RETURNED TO IAH ON FLIGHT 4175, WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE AIR CYCLE MACHINE, REMOVED MEL CONTROL NUMBER 012199, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001042400114 20010424 00114 EU 2001 4 24 C2XA01CL073 1 20010404 A 3260 CONNECTOR AEROSP ATR42 ATR42320 8680930 EU COCKPIT DIRTY A C2XA O OTHER N FALSE WARNING AP APPROACH 1 SW 27 14828 179 CLE FLT 3076 THE CREW REPORTED GEAR UNLOCK LIGHT ON NOSE GEAR SYSTEM REMAINED ILLUMINATED AFTER LANDING GEAR EXTENSION. AIRCRAFT LANDED WITH OUT FURTHER INCIDENT. MAINTENANCE CLEANED CANNON PLUG FOR DOWNLOCK INDICATION. OPERATIONAL CHECK S WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001042400115 20010424 00115 SO 2001 4 24 C2XA01TY066 1 20010405 A 5320 14522459003 ANGLE EMB 145 EMB145LR SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15980 145202 TYS DURING A SCHEDULED INSPECTION THE LEFT HAND OMEGA BEAM RAMP ANGLE WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPL ACED THE RAMP ANGLE IAW EMB-145 SRM-51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETIO N OF INSPECTION. 2 L 7 2 4T RT T00011AT 2001042400116 20010424 00116 SO 2001 4 24 C2XA01TY067 1 20010402 A 5315 14590141001 FLOORBEAM EMB 145 EMB145LR SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15980 145202 TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REPAIRED OMEGA BEAM IAW EMB GST-1030/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTI ON. 2 L 7 2 4T RT T00011AT 2001042400117 20010424 00117 SO 2001 4 24 C2XA01TY068 1 20010402 A 7110 14576010001 STIFFENER EMB 145 EMB145LR SO LT COWLING CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15980 145202 TYS DURING A SCHEDULED INSPECTION THE LEFT ENGINE UPPER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED. MAINTENANCE REPA IRED THE COWLING IAW EMB GST-0999/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INS PECTION. 2 L 7 2 4T RT T00011AT 2001042400118 20010424 00118 SO 2001 4 24 C2XA01TY069 1 20010402 A 5230 14522493001 SKIN EMB 145 EMB145LR SO CARGO DOOR CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15980 145202 TYS DURING A SCHEDULED INSPECTION THE CARGO DOOR SKIN WAS FOUND CHAFED AT THE EDGES OF EXTERNAL HANDLE CUTOUT. MAINTE NANCE REPAIRED THE DAMAGED AREA IAW EMB GST-0998/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON CO MPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2001042400119 20010424 00119 SO 2001 4 24 C2XA01TY070 1 20010402 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15980 145202 TYS DURING A SCHEDULED INSPECTION THE RIGHT OMEGA BEAM TOP CAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 19 AND 22. MAIN TENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB-145 SRM-51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RE LEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2001042400120 20010424 00120 EU 2001 4 24 RAIA00104002 1 20010402 A 3010 B1181175 HOSE JETAIR JETSTM JETSTM4101 1500501 EU HORIZ STAB FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 563HK 41079 9540-PVD-DURING TAXI AIRFRAME DEICE FAULTED IN AUTO AND MANUAL MODES. MAINTENANCE REMOVED AND REPLACED RIGHT HAND HORIZ ONTAL LEADING EDGE DEICE HOSE IAW J41 MAINTENANCE MANUAL. 2 L 7 2 4T RT A41NM 2001042400121 20010424 00121 EU 2001 4 24 C2XA01CL074 1 20010404 A 3620 6411343 SWITCH AEROSP ATR42 ATR42320 8680930 EU BLEED AIR FAILED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 17831 185 CLE FLIGHT 3061 THE CREW REPORTED A SMELL OF SMOKE IN THE COCKPIT DURING FLIGHT.THE AIRCRAFT RETURNED TO CLEVELAND AND L ANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND PERFORMED ENGINE RUNS NO SMOKE SMELL WAS NOTED. DURING RUNS TH E NR 1 BLEED FAULTED AND WOULD NOT RESET. MAINTENANCE REPLACED THE NR 1 BLEED AIR OVER TEMPATURE SWITCHES AND OPERATIO NAL CHECKS WERE GOOD. P/N 641134-3, S/N C038. 2 H 7 2 4T RT A53EU 2001042400122 20010424 00122 NE 2001 4 24 C1HA200194010 2 20010321 A 7200 JT8D17 ENGINE BOEING 727 727290 138408W NM PWA JT8 JT8D17 52049 NE NR 1 ENGINE OVERTEMP A C1HA E A ENGINE SHUTDOWN UNSCHED LANDING K M J FLUID LOSS OVER TEMP WARNING INDICATION CR CRUISE 1 GL 15 294AS 22146 696766 NR 1 ENG AT CRUISE ENG TEMP CLIMBED TO 145C OIL QUANTITY DROP TO UNDER 1 GAL. ENG SHUT DOWN ENG OIL TEMP WENT PAST RED LINE. AIRCRAFT RETURNED TO ORIGINATING STA. REMOVED AND REPLACED NR 1 ENG. 2 L 7 3 4F 4 F A3WE E2EA 2001042400123 20010424 00123 NM 2001 4 24 C1HA200195002 1 20010323 A 5210 SEAL BOEING 727 727290 138408W NM L1 DOOR LEAKING A C1HA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 295AS 22147 CABIN DOOR SEAL LEAKS (L1) AIR RETURN. REFORMED SEAL REPAIR ON SEAL AT LOWER THRESHOLD AREA PER 52-00-01. 2 L 7 3 4F A3WE 2001042400124 20010424 00124 NM 2001 4 24 C1HA200185002 1 20010404 A 2910 HYDRAULIC LINE BOEING 727 7272S7 138407Z NM HYDRAULIC MODULE LEAKING A C1HA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 685CA 22492 AFTER PUSH BACK AND INITIAL TAXI OUT A-PRESS FLUCTUATED AND QTY DROP TO 2.4 GAL. RETURNED TO GATE. FOUND A-SYSTEM HYDR AULIC MODULE LINE LEAKING. RE-TORQUED LINE, SERVICED SYSTEM, LEAK CHECKED GOOD. 2 L 7 3 4F A3WE 2001042400125 20010424 00125 NM 2001 4 24 C1HA200186003 1 20010331 A 3242 CONTROL UNIT BOEING 727 7272S7 138407Z NM BRAKE ASSY LEAKING A C1HA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 15 686CA 22021 LOST BOTH B-SYSTEM HYDRAULIC PUMPS, LOW PRESS LIGHTS CAME ON IN FLT. AT FL260 B-QUANTITY NORMAL LOSS OF A-QUANTITY. FL IGHT DIVERTED. AUTOBRAKE CONTROL MODULE DISCOVERED LEAKING AT PLUG ON AFT I/B SIDE OF AUTOBRAKE CTRL MODULE. RE-SEALED MODULE. REMOVED AND REPLACED B-PUMPS, REMOVED AND REPLACED FILTERS LEAK AND OPS CHECKS GOOD. 2 L 7 3 4F A3WE 2001042400126 20010424 00126 NM 2001 4 24 C1HA200184003 1 20010329 A 2611 473597402 SMOKE DETECTOR BOEING 727 7272S7 138407Z NM CARGO BAY FAILED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 684CA 22491 AFT CARGO SMOKE DETECTOR TEST FAILED. FOUND NR 5 SMOKE DETECTOR BAD. REMOVED AND REPLACED NR 5 SMOKE DETECTOR PER 26-2 5-01, OPS CHECK NORMAL. 2 L 7 3 4F A3WE 2001042400128 20010424 00128 NM 2001 4 24 C1HA200186004 1 20010402 A 3350 BATTERY BOEING 727 7272S7 138407Z NM AFT AIRSTAIR DISCHARGED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 686CA 22021 AFT AIRSTAIR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERIES, OPS CHECK GOOD. 2 L 7 3 4F A3WE 2001042400129 20010424 00129 NM 2001 4 24 C1HA200195003 1 20010403 A 3350 10101141 LIGHT BOEING 727 727290 138408W NM AFT AIRSTAIR INOPERATIVE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 295AS 22147 AFT AIRSTAIR EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, CHECKS GOOD. 2 L 7 3 4F A3WE 2001042400130 20010424 00130 NM 2001 4 24 C1HA200185003 1 20010403 A 2611 SMOKE DETECTOR BOEING 727 7272S7 138407Z NM LAVATORY INOPERATIVE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 685CA 22492 RIGHT LAV SMOKE DETECTOR INOP. REMOVED AND REPLACED SMOKE DETECTOR, CHECKS GOOD. 2 L 7 3 4F A3WE 2001042400131 20010424 00131 WP 2001 4 24 TWAA0106102 1 20010329 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 906TW 49160 DURING CHECK-C MAINT FOUND CORROSION ON TOP SIDE OF FLOORBEAM, STA 1250, BL 25L THRU 40L. REMOVED CORROSION PER SRM 60- 70-1. REPLACED FLOOR SUPPORT PER DRAWING 593054 AND SRM 51-30-5. TREATED AND PAINTED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001042400132 20010424 00132 WP 2001 4 24 TWAA0106103 1 20010329 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 906TW 49160 DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT CORRODED AT STA 1154, LBL 24 TO 48. REMOVED CORROSION PER SPM 6-70-01. REPLACED THE FLOOR SUPPORT PER DRAWING 5930544 AND SRM 51-30-5. TREATED AND PAINTED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001042400133 20010424 00133 WP 2001 4 24 TWAA0106104 1 20010402 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 906TW 49160 DURING CHECK-C MAINT IN AFT CARGO COMPT FOUND CORROSION ON AFT SIDE OF FORMER WEB STA 1338, FROM LONGERON 30 TO 23L, AFT SIDE. FABRICATED NEW PART PER DRAWING 9915561, AND SRM 51-10-3 FOR PAINT. INSTALLED PER SRM 51-3 AND 51-10-4. 2 L 7 2 4F A6WE 2001042400134 20010424 00134 WP 2001 4 24 TWAA0106105 1 20010402 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 906TW 49160 DURING CHECK-C MAINT IN THE AFT CARGO COMPT, STA 1231, FROM LONGERON 24L TO 28R, CORROSION WAS FOUND ON THE FORMER, LOWE R AFT SIDE. REMOVED CORROSION PER SPM 6-80-1. PRIMED PER SRM 51-10-3. INSTALLED FASTENERS PER SRM 51-30-5 AND SRM 51- 30-2. 2 L 7 2 4F A6WE 2001042400135 20010424 00135 WP 2001 4 24 TWAA0106106 1 20010330 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT FOUND CABIN MEMBRANE 7 INCHES INBD OF FWD PASSENGER ENTRY AND 11 INCHES FWD OF STA 200, HAD CORROSI ON. REPLACED CORROSION AREA PER SRM 51-70-4. 2 L 7 2 4F A6WE 2001042400136 20010424 00136 WP 2001 4 24 AT0100118 1 20010403 A 3350 AD4002P BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 823AT 47529 FOUND FORWARD CABIN OVERHEAD EMERGENCY LIGHTS FAILED TO ILLUMINATE. REPLACED BATTERIES IN BATTERY PACK IAW DC9 MM 33-53 . 2 L 7 2 4F A6WE 2001042400137 20010424 00137 EU 2001 4 24 01FDEA00255 1 20010405 A 7830 WARNING LIGHT AIRBUS 310 A310222 3930315 EU COCKPIT ILLUMINATED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 451FE 303 ON T/O AS PWR WAS ADVANCED ECAM WARN AND NR 2 ENG REVR UNLOCK LIGHT ILLUM. REJECT T/O AND LIGHT AND WARN WENT AWAY AFT PWR REDUCED. THRUST REVERSER UNDER MEL 78-1. 2 L 7 2 4F RT A35EU 2001042400138 20010424 00138 NM 2001 4 24 0101256641 1 20010314 A 5414 SKIN BOEING 747 747212B 1384886 NM NR 4 PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 641NW 21941 DURING H-CHECK, FOUND CRACK ON THE NUMBER 4 PYLON INBOARD STRUT SKIN. REPAIRED PER EA 66-181950. 2 L 7 4 4F A20WE 2001042400141 20010424 00141 EU 2001 4 24 QXEA0100441 1 20010405 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN DEFECTIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 SEA - THE FORWARD EXIT SIGN ABOVE THE FLIGHT COMPARTMENT DOOR WAS FOUND DIM UPON INSPECTION. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001042400142 20010424 00142 EU 2001 4 24 AWXA0001599 1 20010409 A 5320 D53112818200 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 641AW 453 CORROSION ON FLOOR SUPPORT FWD OF FR 20 -Y35 TO -Y40 Z120. REPAIRED IAW A320 SRM 53-00-14 FIG 206 PG 229-234. 2 L 7 2 4F RT A28NM 2001042400143 20010424 00143 NM 2001 4 24 AWXA0001600 1 20010409 A 5320 657N4326 FLOOR SUPPORT BOEING 757 7572G7 1384963 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 909AW 24522 R-1 SERVICE DOOR FLOOR AREA STRUCTURE - CORROSION AROUND FASTENER HOLES FOR FLOORBOARDS ON CHORD ASSY, RBL 62 BS 339-363 . REMOVED DAMAGED AREA; FABBED REPAIR ANGLE DOUBLER; INSTALLED REPAIR IAW SRM 53-00-51. 2 L 7 2 4F RT A2NM 2001042400144 20010424 00144 EU 2001 4 24 AWXA0001601 1 20010409 A 3350 321452 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN FAULTY A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 622AW 82 054 PHX - 4/5/01 - DURING MAINTENANCE OPERATIONAL CHECK ESCAPE PATH LIGHTS AT SEAT ROW 3L, 7L & 26L AS WELL AS OVERHEAD LIGH T AT 11L FAILED TO ILLUMINATE. THE EMERGENCY LIGHT POWER SUPPLY UNIT AT POSITION NR 4 WAS REPLACED AND FUNCTIONAL CHECK S WERE GOOD. 2 L 7 2 4F RT A28NM 2001042400145 20010424 00145 NM 2001 4 24 AWXA0001602 1 20010409 A 5220 D25270552035009 PANEL AIRBUS A319 A319132 NM EMERG EXIT DOOR UNSECURE A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 803AW 931 LAS - ABORTED TAKEOFF - 4/7/01 - AT APPROX 40 KIAS ECAM MESSAGE FOR THE LEFT EMERGENCY OVERWING EXIT DOOR OPEN ILLUMINAT ED AND THE TAKEOFF WAS ABORTED. A PAX REPORTED THE EMERGENCY DOOR HANDLE ACCESS COVER FELL OFF DURING INITIAL TAKEOFF R OLL. MAINTENANCE INSPECTED THE PANEL (FLAP ASSY HANDLE) AND DOOR; NO DISCREPANCIES NOTED. MAINTENANCE REINSTALLED PANE L AND THE AIRCRAFT WAS RETURNED TO SERVICE W/ NO FURTHER DISCREPANCIES. 2 L 7 2 4F RT A28NM 2001042400146 20010424 00146 NM 2001 4 24 AWXA0001603 1 20010409 A 5310 6545409602 TEE CHORD BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 MAIN WHEEL WELL FWD BLKHD UPPER T-CHORD CRACKED AT FS 663.75 RBL 24. REPAIRED IAW BOEING DWG 65C37732, SRM 51-30-2 PG 2 - 3, 5, 7 - 9 AND AWA ER 15-5702-01073-JS3. 2 L 7 2 4F RT A16WE 2001042400147 20010424 00147 NM 2001 4 24 AWXA0001604 1 20010409 A 5315 6546533503 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 FLOORBEAM REPAIR RBL 25 BS 675 CRACKED. REMOVED AND REPLACED FLOORBEAM REPAIR IAW B737-200 SRM 51-20-1 PG 13 FIG 2, 51- 40-02 AND 51-70-11 FIG 1 PG 1-6. 2 L 7 2 4F RT A16WE 2001042400148 20010424 00148 NM 2001 4 24 AWXA0001605 1 20010409 A 5230 65479527 BEAM BOEING 737 737277 1384570 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 AFT CARGO DOOR LWR CROSS BEAM CRACKED AT FWD END. REPAIRED IAW EO 52-33-01 REV D AND SRM 51-30-2 PG 2-3 AND 51-20-1 PG 13. 2 L 7 2 4F RT A16WE 2001042400149 20010424 00149 NM 2001 4 24 AWXA0001606 1 20010409 A 5320 6545833640 WEB BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 FLOOR STRUCTURE AT WL 207 AFT SIDE OF FS 178 BLKHD HAS A CRACK EXTENDING O/B FWD SIDE CHORD. REMOVED AND REPLACED WEB O N AFT SIDE OF BLKHD WL 180 - 225, RBL 18 IAW SRM 51-40-02 PG 1. 2 L 7 2 4F RT A16WE 2001042400150 20010424 00150 NM 2001 4 24 AWXA0001607 1 20010409 A 5315 BAC1505100246 FLOORBEAM BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 REMOVE BLOCK ON BOTTOM SIDE OF UPPER FWD LIP OF FLOORBEAM AT LBL 45.5 FOR FURTHER CRACK INSPECTION BS 520. INSPECTED AN D REPAIRED CRACK IAW EO 53-14-12 REV C. 2 L 7 2 4F RT A16WE 2001042400151 20010424 00151 NM 2001 4 24 AWXA0001608 1 20010410 A 5230 146N6882 ANGLE BOEING 757 7572G7 1384963 NM CARGO DOOR CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 909AW 24522 AFT CARGO DOOR FWD EDGE ANGLE CHAFED AT LWR END APPROX 1.9 INCH LONG BY 0.3 INCH WIDE. REMOVED DAMAGED AREA; FABBED AND INSTALLED REPAIR PARTS IAW SRM 52-30-02 FIG 3 AND SRM 51-70-13 FIG 1. 2 L 7 2 4F RT A2NM 2001042400152 20010424 00152 EU 2001 4 24 SIMA06622 1 20010307 A 5720 S5701062000800 LINK AEROSP ATR42 ATR42300 8680920 EU LT WING UNSERVICEABLE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 314AM 314 SAW - DURING MBV-2 INSPECTION MAINTENANCE REPORTED THE LEFT FORWARD LOWER WING TO FUSELAGE JUNTION ROD (DOG BONE) HAD AN EXCESSIVELY TIGHT BEARING AND PITTED BUSHING. MAINTENANCE REMOVED AND REPLACED THE JUNCTION ROD IAW JIC 57-15-21-RAI-1 0000-006. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001042400153 20010424 00153 EU 2001 4 24 SIMA0664 1 20010307 A 3320 EO33601 SOCKET AEROSP ATR42 ATR42300 8680920 EU CABIN BURNED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 223AT 223 MIA - FLT 5335 - BURNING WIRE SMELL IN CABIN. OVERHEAD LIGHT SOCKET BURNED. REMOVED BULB. REMOVED AND REPLACED LIGHT SOCKET IAW AMM. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 2001042400154 20010424 00154 EU 2001 4 24 SIMA0663 1 20010307 A 3350 LP1670 LIGHT AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 135MQ 135 MIA - FLT 5221 - EMERGENCY FLOOR LIGHT INOPERATIVE AT 3B, MEL 33-30 ISSUED. MAINTENANCE REPLACED BULB AT SEAT 3B. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001042400155 20010424 00155 NE 2001 4 24 EIA2001015 2 20010314 A 7200 ENGINE DOUG DC9 DC915F 3022037 WP PWA JT8 JT8D7A 52053 NE RT ENGINE FAILED A EIAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 NM 09 916F 47044 KFAR - RIGHT ENGINE FAILED IN FLIGHT. (M) 2 L 7 2 4F 4 F A6WE E2EA 2001042400156 20010424 00156 NM 2001 4 24 EIA2001017 1 20010111 A 5330 SKIN BOEING 747 747SR46 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 HKG-HAECO - FOUND FUSELAGE BS 1840-1845, STRINGER 51R FUSELAGE SKIN FOUND SURFACE CORROSION. CORROSION REMOVED, TRIMMED OFF DAMAGED SKIN AND STRINGER DOUBLER, NDT INSPECTED. REPAIR DOUBLER INSTALLED AT BS 1820-1860 STRINGER 51R PER SRM 53 -30-03 FIG 37 AND SRWS 918068. (M) 2 L 7 4 4F A20WE 2001042400157 20010424 00157 NM 2001 4 24 EIA2001018 1 20010113 A 5414 DOUBLER BOEING 747 747212B 1384886 NM NR 2 PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 485EV 20712 HKG-HAECO - NR 2 PYLON RIGHT EXIT DOUBLER CRACKED AT NAC STATION 222. REMOVED CRACKED DOUBLER, FARRIED OUT NDT INSPECTI ON SKIN AREA. CONFIRMED CRACK FREE. FABRICTED AND INSTALLED NEW DOUBLER PER SRM 54-30-03 FIG 35 AND 36. (M) 2 L 7 4 4F A20WE 2001042400158 20010424 00158 NM 2001 4 24 EIA2001016 1 20010110 A 5753 65B1704710 FITTING BOEING 747 747273C 1384896 NM FOREFLAP CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 SIN-SASCO - FOUND RIGHT WING INBOARD FOREFLAP CENTER TRACK ATTACH FITTING CRACKED. NEW FITTING INSTALLED AS PER SRM 51- 30-02 AND RIGHT WING INBOARD FOREFLAP REINSTALLED PER MM 27-51-02. (M) 2 L 7 4 4F A20WE 2001042400159 20010424 00159 NM 2001 4 24 EIA2001022 1 20010126 A 5310 PRESSURE PANEL BOEING 747 747132 1384882 NM NLG WW CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 HKG-HAECO - FOUND NLG WHEEL WELL RIGHT VERTICAL BEAM WEB CRACKED AT FASTENER HOLES BETWEEN BS 300-320 AT FIVE LOCATIONS. REPLACED RIGHT VERTICAL WEB PER BSB 53A2293. (M) 2 L 7 4 4F A20WE 2001042400160 20010424 00160 NM 2001 4 24 EIA2001023 1 20010126 A 5730 BUTT JOINT BOEING 747 747132 1384882 NM WING CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 HKG-HAECO - FOUND M/D WING CENTER SECTION UPPER SKIN SURFACE BUTT JOINT CORRODED AT BS 1140 LBL 11 TO RBL 11. CORROSION REMOVED, NDT INSPECTED, AREA REWORKED AND REPROTECTED, WITHIN SRM LIMITS PER BOEING MSG EVR-HKG-01-00005H AND RS R-57-1 4-34583. (M) 2 L 7 4 4F A20WE 2001042400161 20010424 00161 NM 2001 4 24 EIA2001024 1 20010126 A 5730 BUTT JOINT BOEING 747 747132 1384882 NM WING CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 HKG-HAECO - FOUND M/D WING CENTER SECTION UPPER SKIN SURFACE BUTT JOINT CORRODED AT BS 1140 LBL 75 - LBL 92. REMOVED CO RROSION, NDT INSPECTED, REWORKED AND REPROTECTED AREA. WITHIN SRM LIMITS PER BOEING MSG EVR-HKG-01-00004H AND RS R-57-1 4-34584. (M) 2 L 7 4 4F A20WE 2001042400162 20010424 00162 NM 2001 4 24 EIA2001025 1 20010126 A 5330 SKIN BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 HKG-HAECO - FOUND FX RIGHT UPPER SKIN AT BS 2658 STRINGER 7R CRACKED. TRIMMED OFF CRACKED SKIN, NDT INSPECTED, REPAIRED SKIN PER SRM 53-30-03. (M) 2 L 7 4 4F A20WE 2001042400163 20010424 00163 NM 2001 4 24 EIA20001026 1 20010126 A 7160 FLANGE BOEING 747 747132 1384882 NM NR 2 NOSE COWL CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 HKG-HAECO - FOUND CRACKED ATTACHMENT FLANGE FASTENER HOLE AT NR 2 ENG NOSE COWL ATTACHMENT RING. OVERSIZED HOLE TO REMO VE CRACK, NDT INSPECTED, INSTALLED REPAIR FREEZE PLUG PER BOEING MSG EVR-HKG-01-00005F, 00007H, 00007F, 00010H, BSB 71-2 290 AND RS R-54-00-34591. (M) 2 L 7 4 4F A20WE 2001042400164 20010424 00164 NM 2001 4 24 EIA2001027 1 20010126 A 5320 65B111176 FITTING BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 HKG-HAECO - FOUND BS 1480 STRINGER 34R END FITTING CRACKED. REPLACED STRINGER 34R END FITTING PER SRM 51-10-01. (M) 2 L 7 4 4F A20WE 2001042400165 20010424 00165 NM 2001 4 24 EIA2001028 1 20010126 A 5310 TIE BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 HKG-HAECO - FOUND M/D BS 880 RT TENSION TIE CRACKED AT FRAME ATTACHMENT AREA. TRIMMED OFF CRACKED AREA, NDT INSPECTED A ND REPAIRED TENSION TIE PER BSB 53-237. (M) 2 L 7 4 4F A20WE 2001042400166 20010424 00166 NM 2001 4 24 EIA2001029 1 20010126 A 5313 65B043681 STRINGER BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 HKG-HAECO - FOUND M/D BS 1740 STRINGER 3L CRACKED. TRIMMED OFF CRACKED AREA, NDT INSPECTED, REPAIRED STRINGER 3L PER BO EING MSG EVR-HKG-01-00003H AND RS R-53-61-34588. (M) 2 L 7 4 4F A20WE 2001042400167 20010424 00167 NM 2001 4 24 EIA2001030 1 20010126 A 5313 STRINGER BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 HKG-HAECO - FOUND M/D BS 1920 STRINGER 2L CRACKED. STOP HOLE DRILLED, NDT INSPECTED, AND REPAIRED STRINGER 2L PER SRM 5 3-10-03 FIG 2. (M) 2 L 7 4 4F A20WE 2001042400168 20010424 00168 NM 2001 4 24 EIA2001031 1 20010126 A 5313 65B043689 STRINGER BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 HKG-HAECO - FOUND M/D BS 1960 STRINGER 3R CRACKED. TRIMMED OFF CRACKED AREA, NDT INSPECTED, REPAIRED STRINGER 3R PER BO EING MSG EVR-HKG-01-00003H AND RS R-53-61-34587. (M) 2 L 7 4 4F A20WE 2001042400169 20010424 00169 NM 2001 4 24 EIA2001032 1 20010126 A 5313 STRINGER BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 HKG-HAECO - M/S BS 1480-1500 STRINGER 1R CRACKED. DRILLED STOP HOLES, NDT INSPECTED, AND REPAIRED STRINGER 1R PER SRM 5 3-10-03 FIG 3. (M) 2 L 7 4 4F A20WE 2001042400170 20010424 00170 NM 2001 4 24 EIA2001033 1 20010126 A 5313 STRINGER BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 HKG-HAECO - FOUND M/D BS 1840 STRINGER 1R CRACKED. STOP HOLE DRILLED, NDT INSPECTED, AND REPAIRED STRINGER 1R PER SRM 5 3-10-03 FIG 2. (M) 2 L 7 4 4F A20WE 2001042400171 20010424 00171 NM 2001 4 24 EIA2001034 1 20010126 A 5320 FITTING BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 HKG-HAECO - FOUND BS 1000 STRINGER 45L END FITTING CRACKED. REPLACED STRINGER 45L END FITTING PER SRM 51-10-01. (M) 2 L 7 4 4F A20WE 2001042400172 20010424 00172 NM 2001 4 24 EIA2001035 1 20010126 A 5310 STOP FITTING BOEING 747 747132 1384882 NM L5 DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 HKG-HAECO - FOUND M/D 5L FORWARD CUTOUT NR 2 STOP FITTING CRACKED. REPLACED NR 2 STOP FITTING PER SRM 51-10-01. (M) 2 L 7 4 4F A20WE 2001042400173 20010424 00173 NM 2001 4 24 EIA2001036 1 20010126 A 5330 SKIN BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 HKG-HAECO - FOUND AFT CARGO DOOR FORWARD AND AFT UPPER DOOR CUTOUTS CRACKED AT FUSELAGE SKIN AT BS 1814 AND BS 1916 STRI NGER 27R. TRIMMED OFF BOTH FORWARD AND AFT CRACKED CORNER SKINS, 4 LAYERS OF REPAIR DOUBLERS INSTALLED PER BOEING MSG E VR-HKG-01-00009H, 00006F, 00011H, BSB 53A2248, PRELIMINARY SRM 53-30-03 FIG 60, AND RS R-53-61-34592. (M) 2 L 7 4 4F A20WE 2001042400174 20010424 00174 NM 2001 4 24 EIA2001037 1 20010126 A 5330 SKIN BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 HKG-HAECO - FOUND CRACKED REVEALED AT LEFT FUSELAGE SKIN AT BS 1698 AND STRINGER 34L AT TOP ROW FASTENER HOLE APPROX .06 0 INCH LONG AT 2 O''CLOCK POSITION. (M) 2 L 7 4 4F A20WE 2001042400175 20010424 00175 NM 2001 4 24 EIA2001021 1 20010126 A 5310 PRESSURE PANEL BOEING 747 747132 1384882 NM NLG WW CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 HKG-HAECO - FOUND LEFT NLG WHEEL WELL VERTICAL BEAM WEB AT BS 300 AND BS 320 CRACKED AT INSULATION BLANKET STANDOFF HOLE BELOW NR 1 CUP. REPLACED LEFT WEB PER BSB 53A2293. (M) 2 L 7 4 4F A20WE 2001042400176 20010424 00176 NM 2001 4 24 EIA2001020 1 20010126 A 5320 FLOOR SUPPORT BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 HKG-HAECO - FOUND M/D BS 140 LBL 45 FLOOR SUPPORT WEB CRACKED. STOP HOLE DRILLED, NDT INSPECTED, REPAIRED FLOOR SUPPORT WEB PER SRM 51-40-02. (M) 2 L 7 4 4F A20WE 2001042400177 20010424 00177 NM 2001 4 24 EIA2001019 1 20010126 A 5320 FLOOR SUPPORT BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 HKG-HAECO - FOUND M/D BS 360 LBL 96 FLOOR SUPPORT WEB CRACKED. FLOOR SUPPORT WEB REPAIRED PER SRM 51-40-02. (M) 2 L 7 4 4F A20WE 2001042400178 20010424 00178 NE 2001 4 24 EIA2001116 2 20010320 A 7200 ENGINE BOEING 747 747132 1384882 NM PWA JT9 JT9D7F 52054 NE NR 1 ENGINE FAILED A EIAA O OTHER Y ENGINE STOPPAGE CR CRUISE 1 NM 09 481EV 19896 689487 CGK - NR 1 ENGINE SHUTDOWN IN FLIGHT AT 39,000 FEET, ON DESCENT TRIED TO START. N2 56 PERCENT EGT CLIMBED TO 948 RAPIDL Y. ENGINE SHUTDOWN AFTER GOING THROUGH TURBULENCE. WINDMILLING CHECK PERFORMED, CHIP DETECTORS CHECKED GOOD. REPLACED OIL FILTER AND FUEL FILTER. 3.5 BLEED VALVE CHECKED GOOD. ALL ENGINE START AND RUNUP PARAMETERS CHECKED NORMAL PER 71- 00-00. (M) 2 L 7 4 4F 4 F A20WE E20EA 2001042400179 20010424 00179 SO 2001 4 24 SIMA0261 1 20010126 A 5610 WINDSHIELD EMB 145 EMB145LR SO COCKPIT CRACKED A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 630AE 145132 IND - FLT 4048 - IN CRUISE, CAPTAIN''S WINDSHIELD SHATTERED. CREW DECLARED AN EMERGENCY AND LANDED IN IND. (M) 2 L 7 2 4T RT T00011AT 2001042400180 20010424 00180 WP 2001 4 24 USAAD01047 1 20010313 A 3350 8732030153 MODULE DOUG DC9 DC981 3022081 WP CABIN FAILED A USAA K NONE O OTHER AP APPROACH 1 EA 19 813US 48093 PIT-BUF - FLT 1055 - APPROXIMATELY 5 MINUTES BEFORE LANDING THE CABIN EMERGENCY LIGHTS STARTED TO FLICKER, AND CONTINUED UNTIL AFTER THE AIRCRAFT WAS PARKED AND THE TERMINAL. MAINTENANCE REPLACED THE FORWARD EMERGENCY LIGHT CONTROL MODULE. (M) 2 L 7 2 4F A6WE 2001042400181 20010424 00181 WP 2001 4 24 USAAD01051 1 20010315 A 3350 9721050 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 813US 48093 PIT - THE LOW LEVEL EMERGENCY LIGHT FLICKER INTERMITTENTLY. MAINTENANCE REPLACED THE EXIT IDENTIFIER EMERGENCY LIGHT BA TTERIES. (M) 2 L 7 2 4F A6WE 2001042400182 20010424 00182 WP 2001 4 24 USAAD01050 1 20010313 A 3350 8732030153 MODULE DOUG DC9 DC981 3022081 WP CABIN FAILED A USAA K NONE O OTHER DE DESCENT 1 EA 19 813US 48093 YYZ-PHL - FLT 1103 - DURING DESCENT, THE CABIN EMERGENCY LIGHTS FLICKERED. MAINTENANCE REPLACED THE AFT LOW LEVEL CONTR OL MODULE. (M) 2 L 7 2 4F A6WE 2001042400183 20010424 00183 WP 2001 4 24 USAAD01048 1 20010313 A 3222 1D3224044REVC PISTON DOUG DC9 DC981 3022081 WP NLG DEFECTIVE A USAA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 EA 19 808US 48040 BOS-CLT - FLT 1045 - AFTER TAKEOFF, AS THE LANDING GEAR WAS BEING RAISED, A VIBRATION BEGAN AND THE INTENSITY INCREASED WITH AIRSPEED. THE LANDING GEAR WAS LOWERED, BUT THE NOSE GEAR UNSAFE LIGHT ILLUMINATED AND THE MECHANICAL INDICATOR SH OWED UNSAFE. QRH PROCEDURES WERE FOLLOWED AND THE NOSE GEAR INDICATED SAFE. THE AIRCRAFT RETURNED TO THE FIELD AND LAN DED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR STUT PISTON ASSEMBLY. (M) 2 L 7 2 4F A6WE 2001042400185 20010424 00185 WP 2001 4 24 UPS01835561 1 20010411 A 5710 STRUCTURE DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 CRACK IN WING STRUCTURE AFT OF LEFT MLG REF DC8-5720-14401-A D213157 COMPLETE AT NEXT C CHECK UPS01835548 VOIDED DUE T O DUPLICATION OF MRR 2 L 7 4 4F RT 4A25 2001042400186 20010424 00186 NM 2001 4 24 USAASB01063 1 20010224 A 3350 AD20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 390US 23312 GSO - MAINTENANCE FOUND SOME CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OP S CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001120600136 20011206 00136 NM 2001 12 6 USAASB01066 1 20010225 A 3411 106145819 PITOT TUBE BOEING 737 7373B7 1384580 NM PITOT/STATIC SYS FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 531AU 24478 PHL - FLT 738 - ON CLIMB-OUT FROM PHL, CREW REPORTED LOSS OF VNAV AND NOTED INCREASING DISCREPANCIES BETWEEN CAPTAINS AN D F/O'S AIRSPEED AND ALTIMETERS. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. AIRSPEED AND ALT IMETER SPLITS WERE NOTED AS FOLLOWS AT 25,000 FEET 30 KNOTS/1,500 FOOT DIFFERENCE, AT 5,000 FEET 10 KNOT/150 FOOT DIFFER ENCE AND AT 1,000 FEET 5 KNOT/50 FOOR DIFFERENCE. MAINTENANCE REMOVED AND REPLACED CAPTAINS UPPER LEFT PITOT STATIC PRO BE AND STATIC PORT LINE (P/N 41075-0065). OPERATIONAL CHECK AND LEAK CHECK GOOD PER MM 34-11. AIRSPEED AND ALTIMETERS WITHIN LIMITS PER MM 34-12. (M) 2 L 7 2 4F RT A16WE 2001042400187 20010424 00187 WP 2001 4 24 DHL2001806583 1 20010317 A 5320 WEB DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - MAIN CARGO COMPARTMENT SUBFLOOR CRACKED 1 3/4 INCH RBL 20, STA 55.000. STOP DRILLED IAW SRM 53-2-3 PAGE 39-4 0. FABRICATED DOUBLER IAW SRM 53-2-3 PAGE 39-40. TREATED AND PRIMED IAW SRM 51-1-8B. AND INSTALLED DOUBLER IAW SRM 53 -2-3 PAGE 39-40. STATUS-CLOSED. 2 L 7 4 4F RT 4A25 2001042400191 20010424 00191 NM 2001 4 24 2001UALA00305 1 20010318 A 2751 2061121 INDICATOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE TE FLAPS FAILED A UALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 WP 29 7299U 21894 CREW REPORTS AN OUTBOARD FLAP ASYMMETRIC LOCK OUT, OUTBOARD INDICATOR IS SPLIT, ONE SIDE IS 15 DEGREES OTHER SIDE IS 20 DEGREES, INBOARD FLAPS OK AND HANDLE IS AT 15 DEGREES. SUPPLEMENTAL DATA UPDATE REMOVED AND REPLACE OUTBOARD FLAP INDIC ATOR PER MAINTENANCE MANUAL. OPERATIONAL CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001042400199 20010424 00199 NM 2001 4 24 2001UALA00431 1 20010409 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 AFT CABIN FRAME BS 1681 STR 17R WL 208 IS EXFOLIATED. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME PER SRM. INSTALLED DO UBLER ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001042400200 20010424 00200 NM 2001 4 24 2001UALA00432 1 20010409 A 5320 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 CREASE BEAM WEB STA 1021 STR 17L HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB PER SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001042400201 20010424 00201 NM 2001 4 24 2001UALA00433 1 20010406 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 310UA 23671 AFT PIT FRAME IS CRACKED AT STA 787 AND RBL 20. REPAIRED FRAME USING ANGLE AND FILLERS. MAJOR REPAIR ACCOMPLISHED 2 L 7 2 4F 4 F RT A16WE E2GL 2001042400202 20010424 00202 NM 2001 4 24 2001UALA00434 1 20010406 A 5310 STRAP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 ELECTRICAL EQUIPMENT COMPARTMENT COOLING AIR EXHAUST FUSELAGE TEAR STRAP IS CUT IN TWO PLACES. FUSELAGE SKIN DOUBLER IN STALLED TO AFFECTED AREA. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001042400203 20010424 00203 NM 2001 4 24 2001UALA00435 1 20010407 A 5743 FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT MLG GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 LEFT MAIN GEAR HANGER BEAM FITTING BORE GOUGED. REPLACED THE LEFT MAIN LANDING GEAR HANGER BEAM FITTING. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001042400204 20010424 00204 NM 2001 4 24 2001UALA00436 1 20010407 A 5530 FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE VERTICAL STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 VERTICAL STABILIZER RIGHT HAND FORWARD FAIL SAFE LUG IS CORRODED. BORE OF FAIL SAFE LUG REAMED AND BUSHING INSTALLED. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001042400205 20010424 00205 NM 2001 4 24 2001UALA00437 1 20010407 A 5530 FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE VERTICAL STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 VERTICAL STABILIZER RIGHT HAND REAR ATTACH FITTING AFT FAIL SAFE LUG IS CORRODED. FAIL SAFE LUG BORE REAMED AND BUSHING INSTALLED. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001042400206 20010424 00206 NM 2001 4 24 2001UALA00438 1 20010407 A 5530 FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE VERTICAL STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 VERTICAL STABILIZER RIGHT HAND ATTACH LUGS ARE CORRODED. BUSHINGS REMOVED AND FITTINGS WERE REAMED TO REMOVE THE CORROS ION. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001042400207 20010424 00207 NM 2001 4 24 2001UALA00439 1 20010407 A 5530 FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE VERTICAL STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 VERTICAL STABILIZER LEFT HAND ATTACH LUGS ARE CORRODED. LUGS WERE REAMED TO REMOVE CORROSION AND BUSHINGS WERE MANUFACT URED AND INSTALLED. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001042400208 20010424 00208 NM 2001 4 24 2001UALA00440 1 20010407 A 5530 FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE VERTICAL STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 VERTICAL STABILIZER ATTACH POINT LEFT HAND FAIL SAFE LUG ON FUSELAGE SIDE IS CORRODED. LUG REAMED TO REMOVE CORROSION A ND A BUSHING WAS MANUFACTURED AND INSTALLED. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001042400209 20010424 00209 NM 2001 4 24 2001UALA00441 1 20010407 A 5530 FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE VERTICAL STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 VERTICAL STABILIZER ATTACH POINT LEFT HAND FORWARD FAIL SAFE LUG IS CORRODED. LUG WAS REAMED TO REMOVE CORROSION AND TH E BUSHING WAS REPLACED. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001042400210 20010424 00210 NM 2001 4 24 2001UALA00442 1 20010408 A 5330 SKIN BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 992UA 22089 AFT CARGO DOOR AFT DOOR FRAME LIP EXTERIOR SKIN APPROXIMATELY 19 INCHES FROM THE BOTTOM IS DEFORMED AND HAS A GOUGE. RE PAIRED DAMAGED AREA. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F A16WE E2EA 2001042400211 20010424 00211 NM 2001 4 24 2001UALA00443 1 20010409 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 STA 178 BULKHEAD RIGHT HAND LOWER RADAR ANTENNA MOUNT HAS INCORRECT REPAIR. REMOVED OLD DOUBLER AND INSTALLED NEW DOUBL ER. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001042400212 20010424 00212 NM 2001 4 24 2001UALA00444 1 20010409 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 STA 178 BULKHEAD CRACKED AT UPPER RIGHT HAND RADAR ANTENNA MOUNT NEAR UPPER OUTBOARD RIGHT HAND ATTACH RBL 5.9 REPAIRED AFFECTED AREA. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001042400213 20010424 00213 NM 2001 4 24 2001UALA00445 1 20010409 A 5330 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 STA 178 BULKHEAD WEB CRACKED AT UPPER RIGHT HAND RADAR ANTENNA MOUNT OUTBOARD OF LOWER ATTACH HOLE. REMOVED DAMAGED ARE A AND INSTALLED REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001042400214 20010424 00214 NM 2001 4 24 2001UALA00447 1 20010312 A 5320 141W8519 STIFFENER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 791UA 16497 0 26933 STA. 246 BUCKLED FWD STIFFENER AT:LBL - 7.88 RBL - 7.88 STA. 246 CRACKED FWD STIFFENER AT: RBL 26.06 SUPPLEMENTAL DAT A UPDATE REPLACED STIFFENERS PER SRM 53-10-51, REPAIR 3. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001042400215 20010424 00215 NM 2001 4 24 2001UALA00448 1 20010406 A 5311 FRAME BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 AFT PIT BS 1285 FRAME T-CAP AT LBL 12-33 T-CAP IS CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 51-40-02 AND BAC DRAWING 140T1210. 2 L 7 2 4F 4 F RT A1NM E3NE 2001042400216 20010424 00216 NM 2001 4 24 2001UALA00449 1 20010405 A 5311 FRAME BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 AFT PIT AT BS 1175 BODY LINE 0 RBL 25 FRAME T-CAP HAS AREAS OF CORROSION. MAJOR REPAIR ACCOMPLISHED.FABRICATED AND INST ALLED REPAIR IN ACCORDANCE WITH SRM 51-40-02 AND 53-00-07. 2 L 7 2 4F 4 F RT A1NM E3NE 2001042400217 20010424 00217 2001 4 24 2001UALA00450 4 20010408 A 2565 M961 BATTERY PACK BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LT OVERWING DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 611UA 21872 LEFT OVERWING SLIDE SQUIB WILL NOT TEST. REPLACED LEFT HAND OVERWING SLIDE BATTERY PACK OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E3NE 2001052100022 20010521 00022 2001 5 21 2001UALA00451 4 20010406 A 3454 RECEIVER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE VOR SYSTEM FAILED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 7457U 21911 AIRCRAFT DIVERTED TO STL DUE TO NAVIGATION SYSTEM FAILURE IN ROUTE. STATIC WICKS AND NAV RECEIVER FAILED. FOUND TWO BAD STATIC DISCHARGE WICKS AND NR 1 VOR RECEIVER TO BE WEAK. REPLACED STATIC WICKS AND NR 1 VOR RECEIVER. SYSTEM CHECKS NO RMAL PER MAINTENANCE MANUAL. 2 L 7 3 4F 4 F A3WE E2EA 2001042400218 20010424 00218 EU 2001 4 24 2001UALA00453 1 20010409 A 5610 WINDSHIELD AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT CRACKED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 436UA 638 CAPTAINS WINDSHIELD CRACKED. REPLACED CRACKED WINDSHIELD AND NR 1 WINDOW HEAT CONTROL. 2 L 7 2 4F 4 F RT A28NM E40NE 2001043000015 20010430 00015 NM 2001 4 30 2001UALA00454 1 20010409 A 2780 CONTROL UNIT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LE FLAPS MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 365UA 24534 NR 3 LEADING EDGE FLAP INDICATION PROBLEM. SUPPLEMENTAL DATA UPDATE REPLACED LEADING EDGE FLAP EXTEND PROXIMITY SENSOR S 173. 2 L 7 2 4F 4 F RT A16WE E2GL 2001042400219 20010424 00219 NM 2001 4 24 2001UALA00455 1 20010409 A 5241 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 FORWARD GALLEY DOOR SKIN AT THE LOWER HINGE ARM CUTOUT IS CRACKED. REPAIRED CRACKED SKIN. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001042400220 20010424 00220 NM 2001 4 24 2001UALA00456 1 20010409 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 FORWARD GALLEY DOOR AFT EDGE FRAME AT LOWER STOP FITTING ATTACHMENT HAS APPROXIMATELY A .050 INCH CRACK AT THE FASTENER HOLE. REPLACED LOWER FRAME SECTION USING BOEING DOOR FRAME REPAIR KIT. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001042400221 20010424 00221 NM 2001 4 24 2001UALA00457 1 20010409 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 STA 178 BULKHEAD REPAIR LOWER CENTER AREA REPAIR PATCH HAS ONE ROW OF FASTENERS BETWEEN DAMAGED REMOVAL AREA LOWER LEFT HAND RADAR MOUNT. DOUBLER REPAIR REPLACED WITH APPROPRIATE REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001042400222 20010424 00222 NM 2001 4 24 2001UALA00459 1 20010409 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 STA 294 FLOORBEAM UPPER CAP HAS EXCESS MATERIAL REMOVED AT RBL 38. ACCOMPLISHED FLOORBEAM REPAIR. MAJOR REPAIR ACCOMPL ISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001042400223 20010424 00223 NM 2001 4 24 2001UALA00460 1 20010410 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 EXCESS MATERIAL LOSS AT STA 947 FLOORBEAM RBL 16, 20, 25, 36, AND 37. FABRICATED AND INSTALLED REPAIR STRAP. MAJOR REP AIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001050300321 20010503 00321 NM 2001 5 3 2001UALA00461 1 20010408 A 2421 GENERATOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE RT ENGINE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 787UA 26939 LOST RT ENG GEN PRIOR TO ENTERING ETOPS. RIGHT GENERATOR CONTROL BREAKER (GCB) OPEN OR GENERATOR CONTROL SWITCH OFF AN D ENGINE NOT SHUT DOWN. DIVERT TO LHR. SUPPLEMENTAL DATA UPDATE ELEC GEN SYS R EICAS MESSAGE WAS DISPLAYED WITH ASSOCIA TED MAINTENANCE MESSAGES 24-30032, GENERATOR CONTROL UNIT (R) HAS AN INTERNAL FAULT AND 24-31612, INTEGRATED DRIVE GENER ATOR (R) EXCITER FIELD CURRENT IS OUT OF RANGE. BOTH THE RIGHT GCU AND IDG WERE REPLACED. THE FIX WAS REPLACEMENT OF T HE RIGHT IDG. THE SHOP FINDING REPORTED THAT THE IDG EXCITER LEAD WIRES FAILED. THIS UNIT WILL BE MODIFIED TO INCORPOR ATE HAMILTON SUNDSTRAND SERVICE BULLETINS WHICH HAVE NOT BEEN ACCOMPLISHED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001042400224 20010424 00224 NM 2001 4 24 2001UALA00462 1 20010410 A 5412 BULKHEAD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 NACELLE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 NR 2 PYLON AFT BULKHEAD NACELLE STA 201.02 RIGHT HAND SIDE VERTICAL FLANGE LOWER CORNER HAS EXCESSIVE MATERIAL LOSS. FA BRICATED AND INSTALLED REPAIR CRES PLATES. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 2001042400225 20010424 00225 NM 2001 4 24 2001UALA00463 1 20010410 A 5322 ANGLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 MID CABIN SUPPORT STRUCTURE ADJACENT TO DOOR 2R BS 740 TO BS 760 RBL 62 HAS EXCESSIVE MATERIAL LOSS. REMOVED AND REPLAC ED TWO ANGLES. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 2001042400226 20010424 00226 NM 2001 4 24 2001UALA00464 1 20010410 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 CREASE BEAM WEB STA 1076 STRINGER 17R HAS EXCESSIVE MATERIAL LOSS. REMOVED AND REPLACED AFFECTED CREASE BEAM WEB. MAJO R REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 2001042400227 20010424 00227 NM 2001 4 24 2001UALA00465 1 20010410 A 5410 WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 567UA 26673 NR 1 PYLON WEB CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLERS TO THE AFFECTED AREA. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 2001071100024 20010711 00024 NM 2001 7 11 2001UALA00466 1 20010410 A 2750 285T004953 FSEU BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE E/E BAY FAULTY A UALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 WP 29 606UA 21867 T/E DISAGREE AT 800 AGL. AMBER ALERT. LANDING UNEVENTFUL. *S/D* T/E DISAGREE WAS A NUISANCE MESSAGE GENERATED BY FLA P STAB POSITION MODULE (FSEU). REPLACED FSEU WITH SERVICEABLE UNIT AND OPS CHECKED PER MM 27-51-01. CYCLED FLAPS SEVER AL TIMES, ALL OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 2001050300322 20010503 00322 EU 2001 5 3 2001UALA00468 1 20010411 A 7722 6A5878 HARNESS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE CHAFED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 409UA 3640 462 V10670 NR 2 ENGINE EXHAUST GAS TEMPERATURE OVERTEMP INDICATION. SUPPLEMENTAL DATA UPDATE EXHAUST GAS TEMPERATURE (EGT) HARNESS EXHIBITED UNUSUAL PHYSICAL CHAFING. REPLACED THE EGT HARNESS. 2 L 7 2 4F 4 F RT A28NM E40NE 2001042400228 20010424 00228 NM 2001 4 24 2001UALA00469 1 20010411 A 5410 WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 567UA 26673 NR 2 PYLON WEB IS CRACKED OUT OF THE FORWARD RIGHT HAND CUTOUT, ABOVE THE FORWARD MOUNT, AT THE ONE OCLOCK POSITION. MA NUFACTURED AND INSTALLED DOUBLERS. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 2001042400229 20010424 00229 NM 2001 4 24 2001UALA00470 1 20010410 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 AFT CARGO PIT AT BS 1241 BETWEEN STRINGERS 36L AND 37L, SHEAR TIE IS CORRODED. MAJOR REPAIR ACCOMPLISHED REPLACED SHEAR TIE PER BAC DRAWING 140T21023 AND INSTALLED PER SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001042400230 20010424 00230 NM 2001 4 24 2001UALA00471 1 20010410 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 MAIN CABIN FLOORBEAM T-CAP HAS DOUBLE DRILLED HOLES BS 790 TO 880 LBL 33. MAJOR REPAIR ACCOMPLISHEDFABRICATED AND INSTA LLED REPAIR IN ACCORDANCE WITH SRM 53-00-51 AND 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001042400231 20010424 00231 NM 2001 4 24 2001UALA00472 1 20010410 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 AFT PIT BS 1153 BETWEEN STRINGERS 39L AND 39R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHEDFABRICATED AND INSTALLED REP AIR IN ACCORDANCE WITH BAC DRAWING 140T2102 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001042400232 20010424 00232 NM 2001 4 24 2001UALA00473 1 20010410 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 AFT PIT BS 1395 STRINGERS 37R TO 38R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T2102 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001042400236 20010424 00236 NM 2001 4 24 UPS01235615 1 20010417 A 2750 CONNECTOR BOEING 727 727173C 1384059 NM TE FLAPS LOOSE A IPXA A UNSCHED LANDING F N FLT CONT AFFECTED FALSE WARNING CL CLIMB 1 SO 01 938UP 19506 INSPECTION TYPE:N/A ATB-OUTBD FLAPS WOULD NOT MOVE ON INITIAL EXTENSION AT MCI. SECURED CONNECTORPLUG IN RT W/W, OPS C HECK GOOD 2 L 7 3 4F A3WE 2001050100267 20010501 00267 NM 2001 5 1 UPS01435613 1 20010417 A 2612 FIRE LOOP BOEING 747 747123F NM NR 4 ENGINE INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:N/A PREFLIGHT NR 4 ENGINE FIRE WARNING FAILED TO TEST WHEN MOVING TEST SWITCH TO UPPER POSITION NR 4 ENG NACELLE IND AND FIRE HANDLE INOP AND WHEN TO DOWN POSITION ONLY NR 1 FIRE HANDLE TESTS REPAIRED BROKEN TERMINAL END S ON LOWER NR 4 FWD FIRE LOOP REF WDM 26-11-04 ENG FIRE DETECTION SYS OPS CKS GOOD IAW M/M 26-11-04 2 L 7 4 4F A20WE 2001042400238 20010424 00238 NM 2001 4 24 UPS01535614 1 20010417 A 2750 CONTROL VALVE BOEING 757 75724APF 1384969 NM TE FLAPS WORN A IPXA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 01 432UP 25463 ATB-AIRFRAME VIBRATION DURING FLAP RETRACTION. PER WN 578203 R&R FLAP POWER DRIVE UNIT, CONTROL VALVE PER MM 27-51-28 C HECKED FLAP CONTROL CABLE FROM COCKPIT TO CONTROL VALVE. OPERATED FLAPS THROUGH SEVERAL FULL CYCLE AND CKD ALL TRANSMISS IONS & BALL SCREWS FOR VIBRATION. CKD LEADING EDGE DEVICES THROUGH FULL TRAVEL ALL ITEMS CKD PER MM 27-51-00 NO DEFECTS NOTED. 2 L 7 2 4F RT A2NM 2001042400239 20010424 00239 WP 2001 4 24 UPS01835592 1 20010330 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 RIGHT WING L/E. UPPER RIB IS CRACKED AT FASTENER END AT XFS 772.5. REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2001042400240 20010424 00240 WP 2001 4 24 UPS01835593 1 20010330 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 RIGHT WING L/E. UPPER RIB IS CRACKED AT FASTENER END AT XFS 722.5. REPAIRED RIB I.A.W. SRM. 57-2- 0 FIG. 2 2 L 7 4 4F RT 4A25 2001042400241 20010424 00241 WP 2001 4 24 UPS01835594 1 20010404 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 LEFT WING L/E. UPPER RIB IS CRACKED AT XFS 327. REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2001042400242 20010424 00242 WP 2001 4 24 UPS01835595 1 20010330 A 5730 576958929 DOUBLER DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 LEFT WING L/E. INTERNAL DOUBLER IS CRACKED AT XW 257.5. REMOVED,FABRICATED,AND REPLACED DOUBLER I. A.W. DWG. 5769589,AND SRM. 51-1-20D,51-1-21 2 L 7 4 4F RT 4A25 2001042400243 20010424 00243 WP 2001 4 24 UPS01835597 1 20010330 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 LEFT WING L/E. UPPER RIB IS CRACKED AT XS 442.185. REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2001042400244 20010424 00244 WP 2001 4 24 UPS01835598 1 20010331 A 5720 97532977 ANGLE DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 LEFT WING L/E. ATTACH ANGLE IS CRACKED AT XW454. REMOVED, FABRICATED, AND REPLACED ANGLE I.A.W. D WG. 9753297,AND SRM. 51-1-20D,51-1-21 2 L 7 4 4F RT 4A25 2001042400245 20010424 00245 WP 2001 4 24 UPS01835600 1 20010330 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 LEFT WING L/E. UPPER RIB IS CRACKED AT XFS 347.75. REPAIRED RIB I.A.W. SRM. 57-2-0 ,FIG. 2 2 L 7 4 4F RT 4A25 2001042400246 20010424 00246 WP 2001 4 24 UPS01835601 1 20010330 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 LEFT WING L/E. UPPER RIB IS CRACKED AT XFS 372.750. REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2001042400247 20010424 00247 WP 2001 4 24 UPS01835602 1 20010330 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 LEFT WING L/E. UPPER RIB IS CRACKED AT XW 466.651. REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2001042400248 20010424 00248 WP 2001 4 24 UPS01835603 1 20010330 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 LEFT WING L/E. UPPER RIB IS CRACKED AT XS 448.581. REPAIRED RIB I.A.W. SRM.57-2-0 FIG.2 2 L 7 4 4F RT 4A25 2001042400249 20010424 00249 WP 2001 4 24 UPS01835604 1 20010330 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 LEFT WING L/E. UPPER RIB IS CRACKED AT XFS 366.5 REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2001042400250 20010424 00250 WP 2001 4 24 UPS01835605 1 20010328 A 5320 3755842505N FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 STA. 1180 BATHTUB BETWEEN LONG. 27L-28L IS CRACKED REMOVED AND REPLACED FITTING I.A.W. DWG. 375 5842,AND SRM. 53-2-0 FIG. 2D 2 L 7 4 4F RT 4A25 2001042400251 20010424 00251 WP 2001 4 24 UPS01835606 1 20010402 A 5310 SHEAR TIE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 STA. 660 SHEAR TIE CLIP IS CRACKED BETWEEN LONG. 26L-27L REPAIRED SHEARTIE I.A.W. SRM. 53-2-0 FIG. 2A 2 L 7 4 4F RT 4A25 2001042400252 20010424 00252 WP 2001 4 24 UPS01835607 1 20010328 A 5320 375841501 FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 STA. 1180 LONG. 34R BATHTUB FITTING IS CRACKED REMOVED AND REPLACED FITTING I.A.W. DWG. 37558 41,AND SRM. 53-2-0 FIG. 2D 2 L 7 4 4F RT 4A25 2001042400253 20010424 00253 WP 2001 4 24 UPS01835608 1 20010328 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 LEFT WING AUX. TANK UPPER SKIN IS CORRODED BEYOND LIMITS AT XFS 193, 8-10 INCHES AFT OF L/E. RE PAIRED SKIN I.A.W. SRM. 57-2-0 FIG. 2A 2 L 7 4 4F RT 4A25 2001042400254 20010424 00254 WP 2001 4 24 UPS01835609 1 20010329 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 RT AUX TANK UPPER SKIN IS CORRODED BEYOND LIMITS BETWEEN XFS 20-26.25 REPAIRED SKIN I.A.W. SRM. 5 7-2-0 FIG. 37 & 38,AND DHM. ENGINEERING RESPONSE. 2 L 7 4 4F RT 4A25 2001042400255 20010424 00255 WP 2001 4 24 UPS01835610 1 20010329 A 5512 SKIN DOUG DC8 DC871F 302199D WP HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 RT. H-STAB. L/E. SKIN IB. SIDE OF STA. XFS 178 IS CORRODED BEYOND LIMITS. REPAIRED SKIN I.A.W. SRM . 55-2-1 FIG. 4 2 L 7 4 4F RT 4A25 2001042400256 20010424 00256 WP 2001 4 24 UPS01835611 1 20010329 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 RT. WING L/E. UPPER SKIN IS CORRODED BEYOND LIMITS XFS 603.75 AT IB SLING ATTACH POINT. REPAIRED SKIN I.A.W. SRM. 57-3-0 FIG. 18,AND E.O. DC8-5720-7767-A 2 L 7 4 4F RT 4A25 2001042400258 20010424 00258 2001 4 24 20010418CW006 4 20010327 A 6122 JAM-NUT CESSNA 310 T310R 2074246 CE CONT O520 TSIO520* 17040 SO GOVERNOR CRACKED D K NONE O OTHER IN INSP/MAINT 1 GL 07 5466J 17 900136 310R0264 GOVERNOR JAM NUT AS INSTALLED BY OVERHAULER RESULTED IN CRACKED STOP WHEN ADJUSTED AND RETIGHTENED. GOVERNOR STOP ARM H AS A FLAT SURFACE AND CURVED SURFACE THROUGH WHICH THE STOP BOLT IS ATTACHED. TRADITIONALLY WE HAVE SEEN THE JAM NUT ON THE FLAT SURFACE. BECAUSE THE STOP IS MADE OF PLASTIC WHEN THE JAM NUT IS TIGHTENED ON THE ROUNDED SURFACE RATHER THAN THE FLAT SURFACE IT IS EASY TO OVERTIGHTEN AND CAUSE A CRACK RESULTING IN THE POSSIBLE LOSS OF STOP BOLT. A POSSIBLE O VER SPEED COULD RESULT. JAM NUT SHOULD BE INSTALLED ON FLAT SIDE. 1 L 7 2 3O 3 O 3A10 E8CE 2001042400274 20010424 00274 CE 2001 4 24 20010419CW015 1 20010316 A 7500 5097010115 TUBE BEECH 100 A100 1152915 CE PWA PT6 PT6A27 52043 EA LT WING PUNCTURED B EWCR K NONE O OTHER IN INSP/MAINT 1 SO 05 38P 8904 B231 INSTALL BLEED AIR TUBE IN LEFT WING CENTER SECTION. USING ICE PICK ON SUSPECT COROSION BLISTERS, TUBE COULD BE PUNCTURE D EASILY. TUBE REMOVED FOR REPLACEMENT, 1 PIN HOLE ON TOP OF TUBE. HOLES LOCATED 8 TO 9 INCHES INBOARD OF COUPLING HO SE END OF TUBE. 1 L 7 2 3T 4 T A14CE E4EA 2001042400275 20010424 00275 SO 2001 4 24 20010419CW016 1 20010316 A 3211 67054008 TRUNNION PIPER PA32 PA32301 7103207 SO LYC O540 IO540* 41532 EA MLG CRACKED B EWCR K NONE O OTHER IN INSP/MAINT 1 SO 05 239A 639 3246022 CRACK ACROSS FRONT OF TRUNNION 1.5 INCHES LONG AND IN 3.6250 UP FROM BOTTOM. 1 L 7 1 3O 3 O A3SO 1E4 2001042400276 20010424 00276 EA 2001 4 24 20010419CW017 2 20010316 A 7414 M3327 ROTOR SLICK PIPER PA32 PA32301 7103207 SO LYC O540 IO540K1G5 41532 EA MAGNETO CORRODED B EWCR K NONE O OTHER IN INSP/MAINT 1 SO 05 239A 244 98100093 3246022 L2572548A ROTATING MAGNET SHAFT CORRODED WITH PITTING. IMPULSE COUPLING IN SAME CONDITION. LEFT SIDE OF ACCESSORY CASE APPEARS T O COLLECT MORE MOISTURE TO CREATE THIS CONDITION. THIS IS 2ND MAG ON THIS ENGINE SINCE NEW. 1 L 7 1 3O 3 O A3SO 1E4 2001042400281 20010424 00281 EA 2001 4 24 20010420CW004 2 20010209 A 7414 M3117 ROTOR SLICK PIPER PA32 PA32300 7103212 SO LYC O540 IO540K1A5 41532 EA MAGNETO BROKEN E GSBA K NONE O OTHER IN INSP/MAINT 1 AL 01 76RL 98020638 327540024 PILOT REPORTED ENGINE DIES DURING MAG CHECK. TIMING CHECK REVEALED POINTS NOT OPENING AND CLOSING. MAGNETO CHANGE FOR OVERHAUL ASSEMBLY. FOUND ROTOR SHAFT SNAPPED AT BEARING CAP. 1 L 7 1 3O 3 O A3SO 1E4 2001042400283 20010424 00283 EA 2001 4 24 20010420CW005 2 20010226 A 8500 ENGINE PIPER PA32 PA32300 7103212 SO LYC O540 IO540K1A5 41532 EA NACELLE FAILED E GSBA K NONE O OTHER IN INSP/MAINT 1 AL 01 107TA 4422 422 327540099 L1198848A ENGINE HAD FAILURE. THRU THE NR 2 CONNECTING ROD AND DESTROYED CASE, CAM AND OTHER CYLINDERS AND RODS BEFORE STOPPING. FOUND ONE BROKEN CONNECT ROD BOLT BROKEN IN NR2 CYLINDER. NO SIGN OF OTHER. 1 L 7 1 3O 3 O A3SO 1E4 2001042400284 20010424 00284 NE 2001 4 24 20010420CW006 2 20010420 A 7414 DISTRIBUTOR BOSCH BEECH 18 H18 1151012 CE PWA R985 R985* 52008 NE LT MAGETO BROKEN E GSBA K NONE O OTHER IN INSP/MAINT 1 AL 01 228A BB26248 BA629 LEFT MAGNETO, LEFT ENGINE FAILED CHECK DURING RUN UP. MAINTENANCE DISCOVERED SEVERAL BROKEN/ UNSERVICEABLE PARTS INSIDE MAGNETO WHEN DISTRIBUTOR COVER REMOVED DURING TROUBLESHOOTING. 1 L 7 2 3R 3 R A765 5E1 2001042400290 20010424 00290 SO 2001 4 24 20010420CW012 2 20010420 A 8530 IO520MB HOUSING CESSNA 310 310R 2074245 CE CONT O520 IO520MB 17032 SO PUSH ROD CRACKED D K NONE K FLUID LOSS IN INSP/MAINT 1 EA 09 1852E 310R1587 266054R LT ENGINE NOT PRODUCING POWER, LEAKING OIL OUT LEFT LEFT TOP GRATE. INSPECTED, FOUND CASE CRACKED BELOW NR 1 CYLINDER A ROUND PUSH ROD HOUSING ASSEMBLY AND NR 1 CYLINDER BOTH TOP AND BOTTOM FORWARD CYLINDER DOWN NUTS BROKEN OFF. REMOVED AND REPLACED ENGINE. 1 L 7 2 3O 3 O 3A10 E5CE 2001042400291 20010424 00291 NM 2001 4 24 UPS01235618 1 20010327 A 5754 BRACKET BOEING 727 72731C 1384011 NM NR 6 SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C & SI, RT WING NR 6 SLAT - I/B SLAT TRACK - O/B TRACK TO SLAT SKIN SUPPORTIN G ANGLE CRACKED REPL ACED BRACKET IAW MM 27-81-11 2 L 7 3 4F A3WE 2001042400292 20010424 00292 NM 2001 4 24 UPS01235619 1 20010301 A 5310 DOOR FRAME BOEING 727 72731C 1384011 NM CARGO DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C&SI ON REMOVAL OF MCD UPPER BEAM ON DOOR FOUND CORRODED. CORROSION FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-6 MCD UPPER BEAM REPLACED IAW SRM 51-80-2 WITH REF TO BOEING DRG 65- 25337 & 65-36524 & SMRO EO 2001-010-015 UPS E NGINEERING FILE NO. 727-21-0018 2 L 7 3 4F A3WE 2001042400293 20010424 00293 NM 2001 4 24 UPS01235620 1 20010321 A 5240 FRAME BOEING 727 72731C 1384011 NM GALLEY DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C&SI CRACK FOUND ON MID GALLEY DOOR AT AFT UPPER FRAME GALLEY DOOR AT AFT UPPER FRAME REPAIRED IAW S RM ADDENDUM UPS EO B727 -5240-4626 APPENDIX D 2 L 7 3 4F A3WE 2001042400294 20010424 00294 NM 2001 4 24 UPS01235621 1 20010327 A 5714 WEB BOEING 727 72730C 1384009 NM WING BOX CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 918UP 19008 INSPECTION TYPE:C LOWER F.S. AT WING CENTER SECTION BETWEEN BS 775 TO BS 800 AND RBL 13 WEBS CRACKED AND CORRODED. REMO VE WEB AT LWR FUSELAGE CENTER SECTION BETWEEN 767 TO 830 RBL13 AS PER B727 SRM 51-30-02 REMEOVED AND REPLACED DAMAGE WE B LOWER CENTER WING SECTION BS 775 TO 800 RBL 13 AS PER SRM 51-30-02. 2 L 7 3 4F A3WE 2001042400295 20010424 00295 NM 2001 4 24 UPS01235622 1 20010327 A 5714 WEB BOEING 727 72730C 1384009 NM WING BOX CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 918UP 19008 INSPECTION TYPE:C LOWER F.S. AT WING CENTER SECTION APROX BETWEEN BS 800 TO 810 AND LBL 13 WEB IS CORRODED. REMOVE W EB AT LWR FUSELAGE CENTER SECTION BETWEEN BS 800 TO BS 810 LBL 13 WEB AS PER B727 SRM 51-30-2. REPLACED DAMAGED WEB LOW ER CENTER WING AT BS 800 TO 810 LBL 13 WEB AS PER B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2001042400296 20010424 00296 NM 2001 4 24 UPS01235623 1 20010327 A 5714 WEB BOEING 727 72730C 1384009 NM WING BOX CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 918UP 19008 INSPECTION TYPE:C LOWER F.S. AT WING CENTER SECTION APROX 770 AND LBL 13 WEB IS CORRODED. REMOVED WEB AT LOWER FUSELAGE CENTER SECTION AT BS 770 AND LBL13 WEB AS PER B727 SRM 51-30-02. REPLACED DAMAGE WEB LOWER CENTER WING AT BS 770 AND L BL 13 WEB AS PER B 727 SRM 51-30-2. 2 L 7 3 4F A3WE 2001042400297 20010424 00297 NM 2001 4 24 UPS01235624 1 20010329 A 5313 STRINGER BOEING 727 72730C 1384009 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 918UP 19008 INSPECTION TYPE: C, FWD CARGO COMPT BETWEEN STA 680 AND 660, LT SIDE STRINGER 24, CORROSION. CUT OUT SECTION AT BAD ST RINGER AREA STA 680 TO STA 660 LT STRINGER 24 INSTALLED REPAIR AS PER B727 SRM 53-10-3 FIG 1 SIDE OF STRINGER DOUBLER REPAIR 11 1/4 INCHES. 2 L 7 3 4F A3WE 2001042400298 20010424 00298 NM 2001 4 24 UPS01235625 1 20010328 A 5314 KEELBEAM BOEING 727 72730C 1384009 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 918UP 19008 INSPECTION TYPE:C, RT SIDE OF KEELBEAM APU CUT OUT FWD END HAS A DOUBLER CRACKED AT BS 874 NEXT TO HORIZONTAL STIFFENER . REMOVED OLD DOUBLER REPAIR OF KEEL BEAM AREA AND INSTALLED NEW DOUBLER REPAIR AT SAME AREA BS 874 AS PER B727 SRM 51- 10-01. 2 L 7 3 4F A3WE 2001042400299 20010424 00299 NM 2001 4 24 UPS01235626 1 20010326 A 5330 PRESSURE PANEL BOEING 727 72730C 1384009 NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 918UP 19008 INSPECTION TYPE: C, NOSE WHEEL WELL RT SIDE CRACKED AT BS 286.5 TO BS 294.5 WL 160 LOOKING FROM INSIDE TUNNEL. CUT OUT DAMAGE AREA, NDT CUT OUT, AND INSTALLED DOUBLER REPAIR AS PER B727 SRM 51-40-2 FIG.1 2 L 7 3 4F A3WE 2001042400300 20010424 00300 NM 2001 4 24 UPS01235628 1 20010326 A 5347 SEAT TRACK BOEING 727 72730C 1384009 NM FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 918UP 19008 INSPECTION TYPE: C, MAIN CARGO DECK FUSELAGE STATION 1130 LBL 45 SEAT TRACK TONGUES ARE NICKED AND GOUGED REPLACED DAMA GED SECTION OF SEAT TRACK FROM BS 1110 TO STA 1130 LBL 45 2 L 7 3 4F A3WE 2001042400301 20010424 00301 NM 2001 4 24 UPS01235631 1 20010420 A 5610 WINDOW BOEING 727 72727C 138400J NM COCKPIT OUT OF ADJ A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 914UP 19246 CAPT L2 WINDOW UNLATCHES W/O PRESSING UNLATCH LEVER ADJUSTED LOCKING AND SERATION PLATE. 2 L 7 3 4F A3WE 2001042400302 20010424 00302 NM 2001 4 24 UPS01235633 1 20010418 A 3350 LIGHT BOEING 727 72727C 138400J NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 908UP 19114 EMERG EXIT LIGHT INOP. REPLACED BULB OP CHECKS GOOD 2 L 7 3 4F A3WE 2001042400303 20010424 00303 NM 2001 4 24 UPS01535632 1 20010420 A 2910 SWITCH BOEING 757 75724APF 1384969 NM LEFT FAILED A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 451UP 27739 ENG START MAIN CARGO SMOKE DETECTION INDICATED SMOKE ALONG WITH ACRI D ODOR IN COCKPIT T/S TO LEFT HYDRAULIC ACMP SW ITCH FAILED R&R SWITCH 2 L 7 2 4F RT A2NM 2001042400304 20010424 00304 NM 2001 4 24 UPS01635630 1 20010419 A 2710 CONTROL ROD BOEING 767 767322 1385200 NM AILERONS LACK OF LUBE A IPXA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 SO 01 317UP 27745 AILERONS FEEL STIFF LIKE THERE IS NO HYD PWR CLEANED AND LUBED CENTERING MECHANISM SYSTEM CHECKS GOOD 2 L 7 2 4F RT A1NM 2001042400305 20010424 00305 WP 2001 4 24 UPS01835596 1 20010328 A 5340 37584951N FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 STA. 1240, LONG. 35L INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG.3758495,AND SRM. 51-1-20D 2 L 7 4 4F RT 4A25 2001050100045 20010501 00045 WP 2001 5 1 UPS01835627 1 20010420 A 2150 A/C PACK DOUG DC8 DC871F 302199D WP LEFT SMOKE A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 01 730UP 46030 LT PACK TRIP LIGHT CAME ON IN FLIGHT FOLLOWED BY A STRONG SMELL OF ELECTRICAL SMOKE. SMOKE SMELL WENT AWAY AFTER PERFOR MING SMOKE OF UNKNOWN ORIGIN CHECKLIST. PERFORMED OPERATIONAL CHECK PER MM 21-60-00 ON TEMP CONTROL ON LEFT PACK SYSTEM CHECK NORMAL NO LEAKS OR SMOKE IN COCKPIT 2 L 7 4 4F RT 4A25 2001042400306 20010424 00306 WP 2001 4 24 UPS01835629 1 20010418 A 2611 SMOKE DETECTOR DOUG DC8 DC873F 302199F WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 818UP 46108 CREW-PREFLIGHT MULTIPLE SMOKE DETECTORS INOP IN PIT 34. R&R BATT CLEARED DEFERRAL 2 L 7 4 4F RT 4A25 2001042400311 20010424 00311 CE 2001 4 24 20010423CW007 1 20010308 A 3230 594H007 LINK CESSNA 425 425 2076018 CE PWA PT6 PT6A60A 52043 NE MLG CORRODED B K NONE O OTHER IN INSP/MAINT 1 GL 25 1226B 0222 DURING PHASE INSPECTION CORROSION WAS FOUND INSIDE THE LIGHTENING BORE OF THE AXLE LINK ASSEMBLY ON BOTH MAIN GEAR AT TH E UPPER END.(KNEE). CORROSION WAS REMOVED AND AFTER MEASURING REMAINING THICKNESS THE PARTS WERE FOUND WITHIN PRODUCTIO N TOLERANCES. THE BLENDED AREAS WERE REQUIRED TO BE SHOT PEENED BEFORE BEING RETRUNED TO SERVICE. 1 L 7 2 3T 4 T RT A7CE E4EA 2001042400312 20010424 00312 CE 2001 4 24 20010423CW008 1 20010308 A 3230 5941108 LINK CESSNA 425 425 2076018 CE PWA PT6 PT6A60A 52043 NE MLG CORRODED D K NONE O OTHER IN INSP/MAINT 1 GL 25 1226B 0222 DURING PAHSE INSPECTION CORROSION WAS FOUND INSIDE THE LIGHTENING BORE OF THE AXLE LINK ASSEMBLY ON BOTH MAIN GEAR AT TH E UPPER END (KNEE). CORROSION WAS REMOVED AND AFTER MEASURING REMAINING THICKNESS THE PARTS WERE FOUND WITHIN PRODUCTI ON TOLERANCES. THE BLENDED AREA WERE REQUIRED TO BE SHOT PEENED BEFORE BEING RETURNED TO SERVICE. 1 L 7 2 3T 4 T RT A7CE E4EA 2001042400313 20010424 00313 CE 2001 4 24 20010423CW009 1 20010307 A 3230 SM50D7 RELAY BEECH 58 58 1152740 CE CONT O520 IO520* 17032 SO DYNAMIC BRAKE INOPERATIVE E BSYA K NONE O OTHER IN INSP/MAINT 1 GL 07 58TA TH596 GEAR WOULD NOT GO UP ALL THE WAY. FOUND DYNAMIC BRAKE RELAY OPENING UP UNDER A LOAD IN THE UP POSITION. REMOVED AND RE PLACED RELAY. OPS CHECKED GOOD. 1 L 7 2 3O 3 O 3A16 E5CE 2001042400314 20010424 00314 CE 2001 4 24 20010423CW010 1 20010307 A 7602 5038901223 CONTROL CABLE BEECH 58 58 1152740 CE CONT O520 IO520C 17032 SO MIXTURE CONTROL BROKEN E K NONE O OTHER IN INSP/MAINT 1 GL 07 58WA TH201 RIGHT ENGINE SHUT DOWN IN FLIGHT, FOUND RIGHT MIXTURE CABLE BROKEN. REMOVED AND REPLACED CABLE. OPS CHECKS GOOD. 1 L 7 2 3O 3 O 3A16 E5CE 2001042400315 20010424 00315 CE 2001 4 24 20010423CW011 1 20010423 A 2140 D83A28 HEATER BEECH 95 95B55 1152729 CE CONT O470 IO470* 17026 SO NOSE BAY FAILED D K NONE L NO TEST IN INSP/MAINT 1 SW 09 1848W TC1534 HEATER FAILED DECAY TEST. AFTER CONVERSATION WITH HEATER REPAIR FACILITY, THEY STATED 85 TO 90 PERCENT FAILED ON TEST AT OVERHAUL . 1 L 7 2 3O 3 O RT 3A16 E1CE 2001042400316 20010424 00316 CE 2001 4 24 20010423CW012 1 20010329 A 7160 LW127984S274 HOSE CESSNA 206 T206H CE LYC O540 TIO540A1A 41532 EA LT ENGINE BURNED D K NONE O OTHER IN INSP/MAINT 1 EA 25 2379W 110 T20608157 L1041661A DURING THIS AIRCRAFTS FIRST INSPECTION, THE TURBO BREATHER HOSE WAS FOUND ROUTED NEXT TO THE EXHAUST SYSTEM AND BURNED, CAUSING AN OIL LEAK. FAILURE OF THIS HOSE WILL CAUSE OIL SYSTEM LEAKAGE AND SUBSEQUENT ENGINE FAILURE. NO POSITIVE RESP ONSE FROM ENGINE OR AIRFRAME MANUFACTURER. 1 H 7 1 3O 3 O A4CE E14EA 2001050100266 20010501 00266 NM 2001 5 1 UPS01235658 1 20010421 A 2710 CONTROL ROD BOEING 727 72722C 138400F NM WING AILERON LACK OF LUBE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:IN AILERON STIFF IN LEFT TURNS AILERON SPRING CARTRIDGE FOUND OUT OF RIG. RE-ADJUSTED I.A.W. B727 M .M.27-61-21. SPRING CARTRIDGE OPS CHECKS SERV. CONTROL WHEEL INPUTS (FORCE) THE SAME LEFT AND RIGHT NOTE: MIXER CONTROL ROD AND SPD BRK INPUT ROD REMOVED AND REINSTALLED ON SPOILER MIXER FOR T/S NO CHANGE 2 L 7 3 4F A3WE 2001042400319 20010424 00319 NM 2001 4 24 UPS01435636 1 20010407 A 5310 SHEAR TIE BOEING 747 747SR46 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 CABIN - SHEAR TIE FOUND CRACKED AT STN 2340 STR- 4R TO 5R. SHEAR TIE REPLACED PER SRM 51-10-01 2 L 7 4 4F A20WE 2001042400320 20010424 00320 NM 2001 4 24 UPS01435637 1 20010408 A 5347 SEAT TRACK BOEING 747 747SR46 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 CABIN SEAT TRACK I/B FLANGE FOUND CRACKED AT STN 996-997 RBL 33. SEAT TRACK REPAIRED PER SRM 53-10-0 5 FIG. 1A 2 L 7 4 4F A20WE 2001042400321 20010424 00321 NM 2001 4 24 UPS01435638 1 20010421 A 3397 WIRE BOEING 747 747200B NM CABIN DAMAGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:N/A EMERGENCY LIGHT INOP UPPER DECK EXIT FWD PANEL REPAIRED PULLED WIRE, OPS CK GOOD 1 L 7 4 4F RT A20WE 2001042400322 20010424 00322 NM 2001 4 24 UPS01435640 1 20010414 A 5310 SHEAR TIE BOEING 747 747SR46 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 CABIN - SHEAR TIE FOUND CRACK AT STA 1800 S-4R TO S-5R. SHEAR TIE REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001042400323 20010424 00323 NM 2001 4 24 UPS01435641 1 20010421 A 5320 FLOOR SUPPORT BOEING 747 747SR46 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 BULK CARGO COMPT - FLOOR PANEL SUPPORT LOWER SURFACE FOUND CORROSION AT STA 1920 LBL0 AS MARKED. FLOO R PANEL SUPPORT REPAIRED AT BULK CARGO COMPTMENT BETWEEN STA 1920 TO 1925 BL 0. 2 L 7 4 4F A20WE 2001042400324 20010424 00324 NM 2001 4 24 UPS01435654 1 20010420 A 3220 DOOR BOEING 747 747212B 1384886 NM NOSE GEAR MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:IN NOSE GEAR DOORS HARD TO CLOSE CLOSED DOORS 2 L 7 4 4F A20WE 2001050100170 20010501 00170 2001 5 1 UPS01435656 4 20010419 A 2210 AUTOPILOT SYS BOEING 747 747212B 1384886 NM COCKPIT MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:IN AUTO PILOT PITCHES IN LEVEL FLT. P1 TARGET ALERT H197877 IN LEVEL FLIGHT AUTOPILOT PULSED YOKE FORE/A FT WHEN AUTOPILOT WAS DISENGAGED LARGE FORCES IN THE PITCH AXIS WERE BEING HELF W AUTOPILOT REF LOGPAGE 575644 BLOCK 2 W RITE UP REMOVED AND REPLACED CADC (CAPT SIDE) PER MM 34 12 00 AUTOPILOT CHECKS NORMAL PER MM 22 10 00 2 L 7 4 4F A20WE 2001050100043 20010501 00043 NM 2001 5 1 UPS01635634 1 20010420 A 2760 ACTUATOR BOEING 767 767300 1385204 NM SPOILER LEAKING A IPXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 323UP 27749 CENTER HYDRAULIC QTY DECREASED TO 0.07. SYSTEM DEPRESSURIZED AND LEAK CONTINUED. ***MRR FILED AS OPEN*** AWAITING LOG P AGE CORRECTIVE ACTION ENTRIES FOUND SPOILER ACTUTATOR LEAKING AT PLUG BELOW SERVO VALVE ON ACTUATOR JUST OUTBOARD OF INBOARD AILERON. REPLACED O-RINGS & SERVICED CENTER HYD SYSTEM. OP''S CHK''S OK. - NO LEAKS. 2 L 7 2 4F RT A1NM 2001042400325 20010424 00325 WP 2001 4 24 UPS01835642 1 20010331 A 5320 45976432N FITTING DOUG DC8 DC871F 302199D WP CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 STA. 100 UPPER FRAME TO CUSP FITTING IS CRACKED AND CORRODED BEYOND LIMITS AT LONG. 21R REMOVED AND REPLACED FITTING I.A.W. DWG. 4597643,AND SRM. 51-1-20D 2 L 7 4 4F RT 4A25 2001042400326 20010424 00326 WP 2001 4 24 UPS01835643 1 20010411 A 5510 SKIN DOUG DC8 DC871F 302199D WP HORIZONTAL STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 LEFT HORIZONTAL STAB. L/E. SKIN IS CRACKED AND DENTED BEYOND LIMITS XFS 150. REPAIRED SKIN I.A.W . SRM. 55-2-1 FIG. 4 2 L 7 4 4F RT 4A25 2001042400327 20010424 00327 CE 2001 4 24 20010423CW016 1 20010404 A 2820 1560014S290 LINE CESSNA 206 U206F 2073333 CE CONT O520 IO520* 17032 SO FUEL SYSTEM LEAKING B R2JR K NONE K FLUID LOSS IN INSP/MAINT 1 EA 21 5VA U20603223 FOUND FUEL RETURN LINE LEAKING THROUGH THE STEEL BRAID. HOSE IS LESS THAN 3 YEARS OLD, WITH NO VISIBLE DAMAGE. EVEN TH OUGH THIS TYPE HOSE IS APPROVED FOR FUEL, AVIATION FUEL SEEMS TO DETERIOATE IT. HOSE HAS STEEL BRAID EXTERIOR. 1 H 7 1 3O 3 O A4CE E5CE 2001042400328 20010424 00328 CE 2001 4 24 20010423CW018 1 20010320 A 2750 WIRE CESSNA 421 421C 2076016 CE CONT O520 GTSIO520* 17032 SO TE FLAPS BROKEN B K NONE O OTHER IN INSP/MAINT 1 GL 17 171N 421C0461 FLAPS FAILED AND TRAVELED BEYOND STOP SWITCHES. ONLY THING THAT WAS FOUND WAS A BROKEN WIRE WHERE THE QUADRENT SWITCHES ARE LOCATED. MANY PARTS HAD TO BE REPLACED. BRACKETS, PULLEYS, RODS CABLES, CHAINS, BELLCRANKS, ACTUATOR AND BOLTS. AFTER REPAIR, OPERATION WAS NORMAL. 1 L 7 2 3O 3 O A7CE E7CE 2001042400329 20010424 00329 GL 2001 4 24 R7MR32756 2 20010315 A 7320 23072731 HMU BELL 407 407 SW ALLSN 250C 250C47B GL ENGINE INOPERATIVE B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 407SJ 390 390 53422 CAE847459 AIRCRAFT FAILED TO START. SUSPECT START VALVE NOT HOLDING PRIME. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2001042400330 20010424 00330 EU 2001 4 24 R7MR32724 1 20010302 A 7120 L633M2001106 MOUNT UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206A NE ENGINE COLLAPSED B R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 135SJ 594 EC1350054 PART COLLAPSED. REMOVED AND REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2001042400331 20010424 00331 EU 2001 4 24 R7MR32723 1 20010315 A 2435 23081057 STARTER GEN UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206A NE ENGINE MALFUNCTIONED B R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 135SJ 49 EC1350054 COMMENTATOR MALFUNCTIONING. REMOVED AND REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2001042400332 20010424 00332 NE 2001 4 24 R7MR32758 2 20010322 A 7250 70BM041720 TURBINE WHEEL SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE ENGINE RATCHETING B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 397LG 106 3268 EXCESSIVE RUBBING CAUSING MR TO RACHET. REPLACED WITH RENTAL UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E00054EN 2001042400333 20010424 00333 NE 2001 4 24 R7MR32737 2 20010217 A 7200 PW206B ENGINE UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE ENGINE BAY FOD B R7MA K NONE C F.O.D. IN INSP/MAINT 1 NM 07 135SJ 1646 EC1350054 FOREIGN OBJECT DAMAGE. DAMAGE OCCURRED PRIOR TO TAKING DELIVERY OF AIRCRAFT. SUSPECT RIVET FRAGMENTS ENTERED ENGINE DU RING FINAL PHASE OF AIRFRAME ASSEMBLY. 1 G 7 2 3U 3 U O H88EU E42NE 2001042400334 20010424 00334 NE 2001 4 24 R7MR32736 2 20010217 A 7200 PW206B ENGINE UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE LEFT FOD B R7MA K NONE C F.O.D. IN INSP/MAINT 1 NM 07 135SJ 1646 EC1350054 PCEBB0045 FOREIGN OBJECT DAMAGE. DAMAGE OCCURRED PRIOR TO TAKING DELIVERY OF AIRCRAFT. SUSPECT RIVET FRAGMENTS ENTERED ENGINE DU RING FINAL PHASE OF AIRFRAME ASSEMBLY. 1 G 7 2 3U 3 U O H88EU E42NE 2001042400335 20010424 00335 NE 2001 4 24 R7MR32735 2 20010220 A 7200 PW206B ENGINE UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE LEFT FOD B R7MR K NONE C F.O.D. IN INSP/MAINT 1 NM 07 135N 50 EC1350086 PCEBB0068 FOREIGN OBJECT DAMAGE. DAMAGE OCCURRED PRIOR TO TAKING DELIVERY OF AIRCRAFT. SUSPECT RIVET FRAGMENTS ENTERED ENGINE DU RING FINAL PHASE OF AIRFRAME ASSEMBLY. 1 G 7 2 3U 3 U O H88EU E42NE 2001042400337 20010424 00337 NE 2001 4 24 R7MR32733 2 20010315 A 7200 PW206B ENGINE UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE LEFT FOD B R7MR K NONE C F.O.D. IN INSP/MAINT 1 NM 07 426AE 7 EC1350159 PCEBB0093 FOREIGN OBJECT DAMAGE. DAMAGE OCCURRED PRIOR TO TAKING DELIVERY OF AIRCRAFT. SUSPECT THAT RIVET FRAGMENTS ENTERED ENGI NE DURING FINAL PHASE OF AIRFRAME ASSEMBLY. 1 G 7 2 3U 3 U O H88EU E42NE 2001042400338 20010424 00338 NE 2001 4 24 R7MR32732 2 20010315 A 7200 PW206B ENGINE UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE RIGHT FOD B R7MR K NONE C F.O.D. IN INSP/MAINT 1 NM 07 426AE 7 EC1350159 PCEBB0094 FOREIGN OBJECT DAMAGE. DAMAGE OCCURRED PRIOR TO TAKING DELIVERY OF AIRCRAFT. SUSPECT THAT RIVET FRAGMENTS ENTERED ENGI NE DURING FINAL PHASE OF AIRFRAME ASSEMBLY. 1 G 7 2 3U 3 U O H88EU E42NE 2001042400339 20010424 00339 NM 2001 4 24 R7MR32759 1 20010312 A 5320 900R1103001113 BUMPER BLOCK DOUG MD900 MD900 3027375 NM PWA PW206 PW206A NE BEAM CRACKED B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 901CF 1234 90000012 LATERAL CRACK BEYOND SERVICEABLE LIMITS. REMOVED AND REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U NC H19NM E42NE 2001042500001 20010425 00001 NM 2001 4 25 01FDEA00248 1 20010404 A 5270 SWITCH BOEING 727 727233 138408A NM CARGO DOOR FAULTY A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 223FE 20935 WHILE LEVEL FLT 330 MAIN CARGO DOOR LIGHT ILLUM ON 2ND OFF PNL. FOLLOW RED TAB HOWEVER, LIGHT REMAIN ON. *S/D* REMOVE D AND REPLACED LATCH WARN SWITCH 9034 PER BOEING STANDARD WIRING PRACTICES MANUAL CHPT 20. OPS CK OK PER MM 52-70-001-5 . 2 L 7 3 4F RT A3WE 2001042500008 20010425 00008 WP 2001 4 25 0101269983 1 20010329 A 4940 GTCP8598DCA APU DOUG DC9 DC932 3022066 WP APU BAY FIRE A NWAA F ACTIVATE FIRE EXT. A FLAME/FIRE IN INSP/MAINT 1 GL 01 983US 50455 3088 47282 DURING APU MAINTENANCE BETWEEN FLIGHTS, AN APU COMPARTMENT FIRE WAS REPORTED. NR 1 AIRCRAFT FIRE BOTTLE WAS DISCHARGED AND THE FIRE WAS EXTINGUISHED. MAINTENANCE REMOVED THE APU AND INSPECTED APU COMPARTMENT FINDING NO DAMAGE. REPLACED TH E APU AND NR 1 FIRE BOTTLE. 2 L 7 2 4F A6WE 2001042500009 20010425 00009 2001 4 25 0101276626 4 20010331 A 2330 SMOKE BOEING 747 747251B 1384892 NM CABIN DETECTED A NWAA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 626US 21708 DURING FLIGHT, THE FLIGHT ATTENDANT SMELLED SMOKE IN FORWARD GALLEY ENTERTAINMENT CENTER AREA. SMOKE AND FUMES WERE COM ING FROM PASSENGER ENTERTAINMENT SYSTEM. REMOVED POWER FROM SYSTEM AND DIVERTED TO ANC AND LANDED WITHOUT INCIDENT. RE MOVED THE NR 1 AND NR 2 VCRS. SMOKE SMELL REMAINED AND UNABLE TO DETERMINE EXACT LOCATION OF SMOKE AND SMELL. SEALED C ANNON PLUGS, TYWRAPPED, AND DEFERRED SYSTEM PER MEL 23-30A. SPECIFIC PART CAUSING PROBLEM TO BE DETERMINED. 2 L 7 4 4F A20WE 2001042500010 20010425 00010 EU 2001 4 25 0101283206 1 20010331 A 2121 EVT3454H FAN AIRBUS 320 A320211 3930320 EU AVIONICS BAY FAILED A NWAA H DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DE DESCENT 1 GL 01 306US 30441 10414 60 DURING DESCENT, AN ELECTRICAL BURNING ODOR WAS NOTICED IN THE COCKPIT FOLLOWED BY VENT BLOWER FAULT MESSAGE. COMPLIED W ITH COM PROCEDURES, DECLARED AN EMERGENCY, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE AVIONICS VENTILATION I NLET BLOWER FAN AND SYSTEM FILTER. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 2001042500011 20010425 00011 NM 2001 4 25 CALA0100275 1 20010402 A 5320 PANEL BOEING 737 737524 1384721 NM CARGO BAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17627 27531 INSPECTION FOUND LT TRANSITION PANELS IN ABB CORRODED AT STA 787-867, S24L AND AT STA 907-947.50, S24L. THE TRANSITION PANELS WERE REPLACED IAW SRM 53-60-53. 2 L 7 2 4F RT A16WE 2001042500012 20010425 00012 NM 2001 4 25 CALA0100276 1 20010402 A 5313 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND A .25 INCH CRACK AT FASTENER IN STRINGER 16L AT STA 500C. THE CRACKED AREA OF STRINGER WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-00-03. 2 L 7 2 4F RT A16WE 2001042500013 20010425 00013 NM 2001 4 25 CALA0100277 1 20010404 A 5330 SKIN BOEING 737 737524 1384721 NM FUSELAGE GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17627 27531 INSPECTION FOUND GOUGES IN FORWARD LOWER CORNER OF C-2 DOOR CUTOUT (EXTERNAL SKIN) AT STA 796. A REPAIR WAS INSTALLED I AW ECRA 5330-03050. 2 L 7 2 4F RT A16WE 2001042500014 20010425 00014 NM 2001 4 25 CALA0100278 1 20010404 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND FLOORBEAM CORRODED ON UPPER SURFACE AROUND SCREW HOLES AT STA 1016, LBL 0-36. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A NEW FLOORBEAM SECTION WAS INSTALLED IAW ECRA 5310-03851. 2 L 7 2 4F RT A16WE 2001042500015 20010425 00015 NM 2001 4 25 CALA0100279 1 20010405 A 5411 FRAME BOEING 737 7373T0 1384582 NM NR 1 PYLON GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND NR 1 ENGINE PYLON FORWARD O/B UPPER CHORD GOUGED. THE NR 1 ENGINE PYLON O/B UPPER CHORD WAS REPAIRED I AW ECRA 5440-01221 AND EA 04-5440-0836. 2 L 7 2 4F RT A16WE 2001042500016 20010425 00016 NM 2001 4 25 CALA0100280 1 20010405 A 5720 STIFFENER BOEING 737 7373T0 1384582 NM WING GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND VERTICAL T-SUPPORT (STIFFENER) ON AFT SPAR JUST I/B OF MLG SUPPORT BEAM O/B FITTING GOUGED AT WS 133. A NEW STIFFENER WAS INSTALLED IAW SRM 51-40-5 AND 51-40-6. 2 L 7 2 4F RT A16WE 2001042500017 20010425 00017 NM 2001 4 25 CALA0100281 1 20010405 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03851. 2 L 7 2 4F RT A16WE 2001042500018 20010425 00018 NM 2001 4 25 PCAA0104025 1 20010402 A 3220 88303 CAP DHAV DHC8 DHC8102 2809003 NM NLG BROKEN A PCAA K NONE O OTHER TX TAXI/GRND HDL 1 EA 13 819EX 016 PIT-FLIGHT 3528 CREW REPORTED NOSE WHEEL STRUT RING BROKEN. MAINTENANCE REPLACED BROKEN PISTON CAP AND LINK, AND SERVIC ED IN ACCORDANCE WITH DASH 8 MAINTENANCE MANUAL 32-20-01. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001042500019 20010425 00019 NM 2001 4 25 PCAA0104027 1 20010404 A 3350 KCD4N RELAY DHAV DHC8 DHC8102 2809003 NM RELAY PANEL INTERMITTENT A PCAA K NONE O OTHER CR CRUISE 1 EA 13 830EX 155 PIT-FLIGHT 3555 CREW REPORTED EMERGENCY LIGHTS FLICKER IN FLIGHT. MAINTENANCE SWAPPED AC CONTACTOR BOXES WITH ANOTHER A IRCRAFT FOR TROUBLESHOOTING. CLEANED ALL CANNON PLUGS ON BOXES, REPLACED RIGHT TRANSFORMER RECTIFIER UNIT CIRCUIT BREAK ER AND REPLACED PROPELLER HEAT RELAY 3061-K2. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001042500020 20010425 00020 SO 2001 4 25 SWIA972477 1 20010326 A 5240 FASTENER EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE FUEL DOOR LOOSE A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 284YV 120284 SERVICE DOOR WARNING LIGHT ON TAKEOFF ROLL. TAKEOFF ABORTED. INBOARD FUEL DOOR CAM LOCK LOOSE. RESECURED, OPS CHECK G OOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042500021 20010425 00021 SO 2001 4 25 SWIA972478 1 20010329 A 5270 WARNING LIGHT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT FALSE INDICATION A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 292SW 120319 CARGO DOOR LIGHT ILLUMINATED IN FLIGHT AND RETURNED TO FIELD. VISUALLY CHECKED CARGO DOOR UPON ARRIVAL AND FOUND TO BE SECURED. VERIFIED DOOR WARNING WORKS. PERFORMED INSPECTION ON CARGO DOOR LIGHT SWITCHES AND PERFORMED NUMEROUS CYCLES ON CARGO DOOR. COULD NOT DUPLICATE FAILURE. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042500022 20010425 00022 2001 4 25 SWIA972480 4 20010327 A 2211 DAMPER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE AUTOPILOT MALFUNCTIONED A SWIA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 292SW 120319 YAW DAMPER ENGAGED ON TAXI, WILL NOT DISCONNECT. REMOVED AND REPLACED APP65A WITH SERVICEABLE UNIT. OPS CHECK GOOD. P /N: 622-6684-006, S/N ON: 2614, S/N OFF: 344. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042500023 20010425 00023 SO 2001 4 25 SWIA972481 1 20010329 A 2730 WIRE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TAIL CHAFED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 199SW 120237 TRIM AURAL WARNING DURING TAKEOFF ROLL. ABORTED TAKEOFF. FOUND AURAL CB POPPED. INSPECTED ELEVATOR TRIM PROXIMITY SEN SORS WIRING ON TOP OF TAIL. FOUND WIRES CHAFING ON STEEL BRAIDED WIRE SHROUD. INSULATED BARE WIRES AND RESET AURAL WAR NING CB. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042500024 20010425 00024 2001 4 25 SWIA972482 4 20010402 A 3417 ADC CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE COCKPIT FAILED A SWIA A UNSCHED LANDING I FLT. ATTITUDE INST. CR CRUISE 1 NM 07 413SW 7102 ADC NR 1 INOP. IAS/ALT/VS BLANK FOR 20 MINS QRH. RETURNED TO SLC. REMOVED AND REPLACED NR 1 ADC IAW 34-12-01. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2001042500025 20010425 00025 SO 2001 4 25 SWIA972483 1 20010404 A 3350 BATTERY PACK EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE CABIN DISCHARGED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 284YV 120284 EMERGENCY EXIT SIGNS AT ROWS 5 AND 6 DO NOT ILLUMINATE. INSTALLED SERVICEABLE MIDDLE BATTERY PACK IAW 33-50-00. OPS CH ECK GOOD. S/N ON 1335, S/N OFF 1089. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042500026 20010425 00026 EU 2001 4 25 C2XA01BT055 1 20010404 A 5347 S5367800120100 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 25811 094 DURING C-CHECK INSPECTION FOUND RIGHTHAND SEAT TRACK CORRODED AT FRAME 36. MAINTENANCE REPAIRED THE SEAT TRACK IAW ATR4 2 SRM 53-00-00 FIGURE 437. 2 H 7 2 4T RT A53EU 2001042500027 20010425 00027 EU 2001 4 25 C2XA01BT056 1 20010404 A 5347 S5367800121400 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 25811 094 DURING C-CHECK INSPECTION FOUND LEFTHAND SEAT TRACK BETWEEN FRAMES 36 AND 39 TO BE CORRODED. MAINTENANCE FABRICATED NEW SEAT TRACK IAW ATR42 SRM 53-63-00 FIGURE 101. REMOVED AND REPLACED SEAT TRACK IAW ATR42 SRM 51-25-04. 2 H 7 2 4T RT A53EU 2001042500028 20010425 00028 NM 2001 4 25 PCAA0104026 1 20010405 A 5210 85210276101 BUSHING DHAV DHC8 DHC8102 2809003 NM PAX DOOR MISSING A PCAA K NONE O OTHER TX TAXI/GRND HDL 1 EA 13 818EX 235 LGA-FLIGHT 3704 CREW REPORTED PASSENGER DOOR WILL NOT OPEN. MAINTENANCE FOUND THREADED BUSHING MISSING ON HANDRAIL ASSE MBLY. INSTALLED INTERIM REPAIR ON DOOR. DOOR OPERATES NORMALLY. AIRCRAFT RETURNED TO SERVICE. CORRECT BUSHING INSTAL LED LATER THAT DAY. 2 H 7 2 4T RT A13NM 2001042500029 20010425 00029 EU 2001 4 25 C2XA01IA195 1 20010404 A 3350 3011210 LIGHT AEROSP ATR42 ATR42320 8680930 EU PAX DOOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 42836 200 IAH - DURING MAINTENANCE INSPECTION, THE PASSENGER DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R EMOVED AND REPLACED THE PAX DOOR LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001042500030 20010425 00030 SO 2001 4 25 C2XA01IA197 1 20010405 A 3231 12012347003 LATCH EMB 120 EMB120ER 3260203 SO LT MLG DOOR BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12715 120125 CLL - FLIGHT 3532, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE LAFT MAIN LANDING GEAR OUTBOARD FORWARD DOOR WOULD NOT LATCH. MAINTENANCE REMOVED AND REPLACED THE AFFECTED GEAR DOOR LATCH, AND THE AIRCRAFT WAS APPROVED FOR RETU RN TO SERVICE. 2 L 7 2 4T RT A31SO 2001042500031 20010425 00031 NM 2001 4 25 01FDEA00259 1 20010407 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 168FE 18865 DURING ROUTINE INSP, BS 640 FLOORBEAM FOUND CORRODED AT 5 SEAT TRACK. CUT OUT DAMAGED AREA. FAB AND INSTALL REPAIR PER IAW BAC 727 SRM 53-10-8. 2 L 7 3 4F A3WE 2001042500032 20010425 00032 NM 2001 4 25 01FDEA00260 1 20010407 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 168FE 18865 DURING ROUTINE INSP, BS 660 FLOORBEAM FOUND CORRODED AT NR 5 SEAT TRACK. CUT OUT DAMAGED AREA. FAB AND INSTALL REPAIR PER IAW BAC 727 SRM 53-10-8. 2 L 7 3 4F A3WE 2001042500033 20010425 00033 NM 2001 4 25 SWAA010877 1 20010323 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 644SW 28329 EEPLS LOOSE AT EXIT ROW. SECURED EEPLS TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001042500034 20010425 00034 NM 2001 4 25 SWAA010878 1 20010323 A 3350 207377 LENS BOEING 737 7375H4 138449D NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 524SW 26566 EEPLS LENS MISSING AT ROW 7. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2001042500035 20010425 00035 2001 4 25 SWAA010879 4 20010323 A 2565 6557463 BRACKET BOEING 737 7377H4 NM CABIN OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 737JW 27869 FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. RE-ADJUSTED GIRT BRACKET PER MM. 2 L 7 2 4F RT A16WE 2001042500036 20010425 00036 NM 2001 4 25 SWAA010880 1 20010323 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND STR 21L CORRODED AT BS 911. REPAIRED STR PER SRM. 2 L 7 2 4F A16WE 2001042500037 20010425 00037 2001 4 25 SWAA010881 4 20010323 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001042500038 20010425 00038 NM 2001 4 25 SWAA010882 1 20010323 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED C2 CHECK, FOUND 1.5 INCH LONG EXTERNAL FUSELAGE SKIN CRACK AT BS 727E, STR 22L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001042500039 20010425 00039 NM 2001 4 25 SWAA010883 1 20010323 A 3350 2013A BATTERY PACK BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 513SW 24190 DURING SCHEDULED D-CHECK AT DALFORT, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2001042500040 20010425 00040 NM 2001 4 25 SWAA010884 1 20010322 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 602SW 27953 EMERGENCY EXIT LIGHT LENS LOOSE AT AFT CABIN. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2001042500041 20010425 00041 NM 2001 4 25 SWAA010885 1 20010324 A 3350 101073 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 637SW 27710 FWD ENTRY DOOR EMERGENCY EXIT LIGHT ASSY LOOSE. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001042500042 20010425 00042 NM 2001 4 25 SWAA010886 1 20010323 A 5330 6545778 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 DURING WALKAROUND INSPECTION, FOUND EXTERNAL FUSELAGE SKIN CRACKED AT STR 22R, BS 927 & 947.5. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001042500043 20010425 00043 NM 2001 4 25 SWAA010887 1 20010324 A 5330 65C35775 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED SERVICE CHECK, FOUND 1.25 INCH LONG EXTERNAL FUSELAGE SKIN CRACK AT 758, STR 19R. REPAIRED SKIN PER SR M. 2 L 7 2 4F RT A16WE 2001042500044 20010425 00044 NM 2001 4 25 SWAA010888 1 20010324 A 5330 6545778 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED SERVICE CHECK, FOUND 1.5 INCH LONG EXTERNAL FUSELAGE SKIN CRACK AT BS 944, STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001042500045 20010425 00045 NM 2001 4 25 SWAA010889 1 20010324 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED SERVICE CHECK, FOUND 2.25 EXTERNAL FUSLEAGE SKIN CRACK AT BS 524, ABOVE STR 10R. REPAIRED SKIN PER BAC SB & SWA RA. 2 L 7 2 4F RT A16WE 2001042500046 20010425 00046 NM 2001 4 25 SWAA010890 1 20010324 A 5330 65C35765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED SERVICE CHECK, FOUND 2.25 INCH LONG EXTERNAL FUSELAGE SKIN CRACK AT BS 500+4, STR 10L. REPAIRED SKIN P ER BAC SB. 2 L 7 2 4F RT A16WE 2001042500047 20010425 00047 NM 2001 4 25 SWAA010891 1 20010324 A 5315 6545410 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED 1/4D CHECK, FOUND BS 660 CENTER WING BOX LONGITUDINAL FLOORBEAM TEE CHORD CRACKED AT BL 0. REPAIRED FL OORBEAM TEE CHORD PER SWA RA. 2 L 7 2 4F RT A16WE 2001042500048 20010425 00048 2001 4 25 SWAA010892 4 20010323 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 376SW 26584 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001042500049 20010425 00049 2001 4 25 SWAA010893 4 20010323 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 376SW 26584 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY AND SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY''S OUT OF ADJUST. RE-ADJUSTED EV AC SLIDE ASSY''S PER MM. 2 L 7 2 4F RT A16WE 2001042500050 20010425 00050 NM 2001 4 25 SWAA010894 1 20010325 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 655WN 28400 TWO EEPLS LAMPS INOP AND WIRING EXPOSED AT OVERWING EMERGENCY EXIT. REPAIRED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001042500051 20010425 00051 NM 2001 4 25 SWAA010895 1 20010323 A 5330 6545767 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACK AT RADIO ALTIMETER ANTENNA AFT CUTOUT, FWD FASTENER HOLES. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001042500052 20010425 00052 NM 2001 4 25 SWAA010896 1 20010324 A 2150 20405011 ACM BOEING 737 7373H4 1384600 NM A/C BAY FAILED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 314SW 23336 AIR TURNBACK, DECLARED EMERGENCY. SMOKE AND FUMES NOTICED IN CABIN AFTER TAKEOFF. REMOVED AND REPLACED LT AIR CYC MACH INE, RECIRC FAN (P/N 64505-1), COALESCER BAGS, AND HEPA FILTER PER MM. PERFORMED 5 MIN ENG POWER RUN AND PRESSURIZED AC FT, ALL SYS OPS CHECK GOOD PER MM. 2 L 7 2 4F RT A16WE 2001042500053 20010425 00053 NM 2001 4 25 SWAA010897 1 20010323 A 3240 6544510 LINE BOEING 737 7372H4 138448C NM LT MLG LEAKING A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 063SW 22061 AIR TURNBACK, LOST B-HYDRAULIC SYS AFTER TAKEOFF. REMOVED AND REPLACED NR 1 BRAKE LINE, INSPECTED BOTH B-PUMP CASE DRAI N FILTERS, SERVICED SYSTEM AND PERFORMED LEAK CHECK PER MM. 2 L 7 2 4F A16WE 2001042500054 20010425 00054 NM 2001 4 25 SWAA010898 1 20010323 A 3350 15AT48 SWITCH BOEING 737 7377H4 NM COCKPIT INTERMITTENT A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 744SW 29490 EMERGENCY EXIT NOT ARMED LIGHT ILLUMINATING INTERMITTENTLY ON P-5 PANEL. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH PE R MM. 2 L 7 2 4F RT A16WE 2001042500055 20010425 00055 NM 2001 4 25 SWAA010899 1 20010324 A 5330 65C35770 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED SPECIAL VISIT, FOUND 3 LONG EXTERNAL FUSELAGE SKIN CRACK AT BS 578, ABOVE STR 10. REPAIRED SKIN PER SR M. 2 L 7 2 4F A16WE 2001042500056 20010425 00056 NM 2001 4 25 SWAA010900 1 20010325 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 513SW 24190 DURING SCHEDULED D-CHECK AT DALFORT, FOUND EEPLS INOP IN SEVERAL LOCATIONS. RELAMPED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001042500057 20010425 00057 NM 2001 4 25 SWAA010901 1 20010324 A 5720 6567172 FITTING BOEING 737 737317 138447P NM LT WING WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED SERVICE CHECK, FOUND LT MLG WALKING BEAM FWD ATTACH FITTING ON REAR SPAR WORN AT WBL 135.505. REMOVED AND REPLACED BEAM FITTING PER MM. 2 L 7 2 4F RT A16WE 2001042500058 20010425 00058 2001 4 25 SWAA010902 4 20010325 A 2565 65C168209 RETAINER BOEING 737 7373H4 1384600 NM ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 624SW 27934 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT RETAINER HOOK LOOSE. SECURED RETAINER PER S RM. 2 L 7 2 4F RT A16WE 2001042500059 20010425 00059 NM 2001 4 25 SWAA010903 1 20010325 A 3397 079123 WIRE BOEING 737 7373H4 1384600 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 389SW 26592 EEPLS WIRES EXPOSED AT EMERGENCY EXIT. INSTALLED EEPLS TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001042500060 20010425 00060 NM 2001 4 25 SWAA010904 1 20010325 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 394SW 27380 EEPLS LOOSE AT ROW 16. SECURED EEPLS TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001042500061 20010425 00061 2001 4 25 SWAA010905 4 20010326 A 2565 2302294152 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF TOLERANCE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED RON CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001042500062 20010425 00062 NM 2001 4 25 SWAA010906 1 20010325 A 3350 079123 COVER BOEING 737 7375H4 138449D NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 EEPLS TRACK COVERS MISSING AT ROWS 7 &10. REPLACED TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 2001042500063 20010425 00063 NM 2001 4 25 SWAA010907 1 20010325 A 3350 BR2013 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 067SW 22356 DURING SCHEDULED C1 CHECK, FOUND EEPLS END CAP MISSING AND WIRING EXPOSED AT FWD GALLEY. REPLACED END CAP AND SECURED W IRING PER MM. 2 L 7 2 4F A16WE 2001042500064 20010425 00064 NM 2001 4 25 SWAA010908 1 20010324 A 5320 6517583 BEAM BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED SPECIAL VISIT, FOUND 2 BS 178 BULKHEAD VERTICAL BEAM CRACKS AT RBL 5.7, BETWEEN WL 182 TO WL 188. REPA IRED VERTICAL BEAM PER SRM & BFG ER. 2 L 7 2 4F A16WE 2001042500065 20010425 00065 NM 2001 4 25 SWAA010909 1 20010324 A 5312 6517582 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT RBL 17.1, WL 228. REPAIRED VERTICAL BEAM WEB PER BFG ER. 2 L 7 2 4F A16WE 2001042500066 20010425 00066 NM 2001 4 25 SWAA010910 1 20010326 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND STR 23L CORRODED AT BS 910. REPAIRED STR SECTION PER SRM. 2 L 7 2 4F A16WE 2001042500067 20010425 00067 NM 2001 4 25 SWAA010911 1 20010326 A 5320 65C27314 STRINGER CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND 2 STR CLIPS CRACKED AT BS 727B, STR 6L & BS 747, STR 7R. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F A16WE 2001042500068 20010425 00068 NM 2001 4 25 SWAA010912 1 20010325 A 3350 207377 LENS BOEING 737 7377H4 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 740SW 29276 DURING SCHEDULED C1 CHECK, FOUND EEPLS LENS BROKEN AT ROW 1. REMOVED AND REPLACED EEPLS LENS PER MM. 2 L 7 2 4F RT A16WE 2001042500069 20010425 00069 NM 2001 4 25 SWAA010913 1 20010325 A 3350 207377 LENS BOEING 737 7377H4 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 729SW 27861 DURING SCHEDULED C3 CHECK, FOUND EEPLS RED LENS MISSING. INSTALLED RED LENS PER MM. 2 L 7 2 4F RT A16WE 2001042500070 20010425 00070 2001 4 25 SWAA010914 4 20010325 A 3441 HG1050AD04 IRU BOEING 737 7373T0 1384582 NM E&E BAY FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 684WN 23941 DIVERSION, NR 2 IRU FAULT LIGHT ILLUMINATED DURING CRUISE. REMOVED AND REPLACED NR 2 IRU PER MM, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2001042500071 20010425 00071 NM 2001 4 25 SWAA010915 1 20010325 A 2751 10619264 INDICATOR BOEING 737 7373G7 1384595 NM COCKPIT MALFUNCTIONED A SWAA O OTHER O OTHER LD LANDING 1 SW 07 670SW 23784 DECLARED EMERGENCY, L/E AND T/E DEVICES WOULD NOT EXTEND. A AND B HYD SYSTEM NORMAL. EXTENDED FLAPS USING ALT FLAP SYS TEM. CLEANED FLAP POS IND AND OPERATED FLAPS PER MM AT HOU. REMOVED AND REPLACED FLAP POS INDICATOR FOR MX CONVENIENCE PER MM. 2 L 7 2 4F RT A16WE 2001042500072 20010425 00072 NM 2001 4 25 SWAA010916 1 20010326 A 5312 6517582 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 378SW 26585 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB STAND OFF HOLE CRACKED AT RBL 17.1, UPPER SECTIO N. REPAIRED VERTICAL BEAM WEB PER SWA RA. 2 L 7 2 4F RT A16WE 2001042500073 20010425 00073 2001 4 25 SWAA010979 4 20010401 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 AFT ENTRY AND SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY''S PER MM. 2 L 7 2 4F A16WE 2001042500074 20010425 00074 2001 4 25 SWAA010980 4 20010401 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 607SW 27927 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001042500075 20010425 00075 NM 2001 4 25 SWAA010981 1 20010329 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 623SW 27933 RT OVERWING EMERGENCY EXIT LIGHT LOOSE. SECURED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001042500076 20010425 00076 NM 2001 4 25 SWAA010982 1 20010401 A 3350 101073 LIGHT BOEING 737 7373Y0 1384671 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664WN 23495 DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR EMERGENCY EXIT LIGHT FRAME CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001042500077 20010425 00077 NM 2001 4 25 SWAA010983 1 20010331 A 3350 20131A BATTERY PACK BOEING 737 7373A4 1384585 NM CABIN DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHTS DIM AT AFT CABIN. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2001042500078 20010425 00078 2001 4 25 SWAA010984 4 20010331 A 2565 D31354 SLIDE BOEING 737 737317 138447P NM ENTRY DOOR OUT OF TOLERANCE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001042500079 20010425 00079 NM 2001 4 25 SWAA010985 1 20010331 A 3350 079123 COVER BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 EEPLS TRACK COVERS LOOSE AT ROWS 13 & 14. SECURED TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 2001042500080 20010425 00080 NM 2001 4 25 SWAA010986 1 20010402 A 3350 207377 LENS BOEING 737 7375H4 138449D NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 EEPLS CLEAR LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2001042500081 20010425 00081 NM 2001 4 25 SWAA010987 1 20010401 A 3350 65C27095 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 080SW 22675 DURING SCHEDULED C2 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EXIT LIGHT BATTERY PACKS LOOSE. SECURED BATTERY PACKS PE R MM. 2 L 7 2 4F A16WE 2001042500082 20010425 00082 NM 2001 4 25 SWAA010988 1 20010401 A 3350 BR2013 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 080SW 22675 DURING SCHEDULED C2 CHECK, FOUND EEPLS END CAP MISSING AND TRACK LOOSE AT FWD SECTION. INSTALLED END CAP AND SECURED TR ACK PER MM. 2 L 7 2 4F A16WE 2001042500083 20010425 00083 NM 2001 4 25 SWAA010989 1 20010401 A 5330 6545769 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND INTERNAL FUSELAGE SKIN CORRODED UNDER SHEAR TIE AT BS 520, BETWEEN STR 28L & 28R. REPAI RED SKIN PER SRM. 2 L 7 2 4F A16WE 2001042500084 20010425 00084 NM 2001 4 25 SWAA010990 1 20010401 A 5330 6516352 DOUBLER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR CUTOUT BEAR STRAP CRACKED AT BS 442, RBL 34. REPAIRED STRAP PER SRM. 2 L 7 2 4F A16WE 2001042500085 20010425 00085 NM 2001 4 25 SWAA010991 1 20010402 A 5310 6546529 SHEAR TIE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 460, BETWEEN STR 27R & 28R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F A16WE 2001042500086 20010425 00086 NM 2001 4 25 SWAA010992 1 20010402 A 5754 6573714 SLAT BOEING 737 7372H4 138448C NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND NR 2 L/E SLAT DELAMINATED AT AFT INBD CORNER. REPAIRED SLAT PER SRM. 2 L 7 2 4F A16WE 2001042500087 20010425 00087 NM 2001 4 25 SWAA010993 1 20010402 A 5754 6573714 SLAT BOEING 737 7372H4 138448C NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND NR 3 L/E SLAT DELAMINATED AT T/E INBOARD CORNER. REPAIRED SLAT PER SRM. 2 L 7 2 4F A16WE 2001042500088 20010425 00088 NM 2001 4 25 SWAA010994 1 20010331 A 2133 7110033 HEATER BOEING 737 7373H4 1384600 NM OUTFLOW VALVE INOPERATIVE A SWAA K NONE O OTHER DE DESCENT 1 SW 07 347SW 24374 DURING DESCENT, CABIN PRESS ERRATIC IN AUTO & STANDBY MODES. FOUND OUTFLOW VALVE HEATER INOP CAUSING OUTFLOW VALVE TO F REEZE. REMOVED AND REPLACED AFT HEATER AND OUTFLOW VALVE PER MM. PERFORMED PACK CONFIDENCE CHECK PER SWA SAM 728 & CAB IN PRESS CONTROLLER TEST PER SWA SAM 729. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2001042500089 20010425 00089 NM 2001 4 25 SWAA010995 1 20010331 A 5720 6962014 STIFFENER BOEING 737 7373H4 1384600 NM WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED RON CHECK, FOUND WING CENTER SECTION REAR SPAR ZEE STIFFENER CRACKED AT LBL 6.15. REPAIRED STIFFENER P ER SWA RA. 2 L 7 2 4F RT A16WE 2001042500090 20010425 00090 NM 2001 4 25 SWAA010996 1 20010402 A 5311 BAC1503 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND BS 1156 BULKHEAD FRAME CHORD CRACKED AT LBL 1, 6 O''CLOCK POSITION. REPAIRED FRAME CHOR D PER SRM. 2 L 7 2 4F A16WE 2001042500091 20010425 00091 NM 2001 4 25 SWAA010997 1 20010401 A 3350 079123 COVER BOEING 737 7373T5 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVER LOOSE AT AFT SECTION. SECURED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001042500092 20010425 00092 NM 2001 4 25 SWAA010998 1 20010401 A 5754 6546431 FLAP BOEING 737 7373T5 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD FOREFLAP DELAMINATED AT T/E, INBOARD CORNER. REMOVED AND REPLACED FOR EFLAP PER MM. 2 L 7 2 4F RT A16WE 2001042500093 20010425 00093 NM 2001 4 25 SWAA010999 1 20010402 A 3350 612825 CHARGER BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 502SW 24179 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT AFT 7 ROWS. REMOVED AND REPLACED EEPLS CHARGER ASSY PER MM. 2 L 7 2 4F RT A16WE 2001042500094 20010425 00094 NM 2001 4 25 SWAA011000 1 20010401 A 5753 65C372563 FRAME BOEING 737 7373Y0 1384671 NM LT FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664WN 23495 DURING SCHEDULED 1/4D CHECK, FOUND LT WING INBD FLAP, OUTBD TRACK, UPPER ACCESS PANEL AFT APERTURE FRAME CRACKED. REPAI RED PER SWA RA. 2 L 7 2 4F RT A16WE 2001042500095 20010425 00095 NM 2001 4 25 SWAA011001 1 20010331 A 5330 6545890 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664WN 23495 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR AFT LOWER CORNER SKIN CUTOUT CRACKED, 1 IN LENGTH. REPAIRED SKIN AND SKIN DOUBLER PER SWA RA. 2 L 7 2 4F RT A16WE 2001042500096 20010425 00096 NM 2001 4 25 SWAA011002 1 20010402 A 5312 6517582 BULKHEAD BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 514SW 25153 DURING SCHEDULED D-CHECK AT DALFORT, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT RBL 17.1, UPPER SECTION. REMOVE D AND REPLACED VERTICAL BEAM WEB PER SWA RA. 2 L 7 2 4F RT A16WE 2001042500097 20010425 00097 NM 2001 4 25 SWAA010939 1 20010328 A 2751 181738 TRANSMITTER BOEING 737 7373G7 1384595 NM LT/RT FLAPS MALFUNCTIONED A SWAA O OTHER J WARNING INDICATION LD LANDING 1 SW 07 670SW 23784 DECLARED EMERGENCY, L/E & T/E FLAPS WOULD NOT EXTEND USING NORMAL METHOD. EXTENDED NORMALLY USING ALT FLAP SYSTEM. REM OVED AND REPLACED LT AND RT FLAP POS TRANSMITTERS PER MM. OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 2001042500098 20010425 00098 NM 2001 4 25 SWAA010940 1 20010328 A 3350 079123 COVER BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 EEPLS TRACK COVER LOOSE IN FWD SECTION. SECURED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001042500099 20010425 00099 NM 2001 4 25 SWAA010941 1 20010328 A 5755 ABYT8102H BEARING BOEING 737 7372H4 138448C NM RT SPOILER OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULED C2 CHECK, FOUND NR 5 SPOILER OUTBD BEARING MIGRATED OUT OF CASTING. REMOVED AND REPLACED NR 5 SPOILER PER MM. 2 L 7 2 4F A16WE 2001042500100 20010425 00100 NM 2001 4 25 SWAA010942 1 20010328 A 3350 57771 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULED C2 CHECK, FOUND EEPLS END CAP MISSING AT AFT CABIN. INSTALLED END CAP PER MM. 2 L 7 2 4F A16WE 2001042500101 20010425 00101 2001 4 25 SWAA010943 4 20010328 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASS Y PER MM. 2 L 7 2 4F A16WE 2001042500102 20010425 00102 NM 2001 4 25 SWAA010944 1 20010328 A 5240 6545871 DOOR FRAME BOEING 737 7372H4 138448C NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR FRAME CRACKED AT LOWER AFT CORNER. REPAIRED DOOR FRAME PER SRM. 2 L 7 2 4F A16WE 2001042500103 20010425 00103 NM 2001 4 25 SWAA010945 1 20010329 A 5310 6546529 SHEAR TIE BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME SHEAR TIE CORRODED AT BS 520, BETWEEN STR 28R & 28L. REMOVED AND REPLACE D FRAME SHEAR TIE PER SRM. 2 L 7 2 4F A16WE 2001042500104 20010425 00104 NM 2001 4 25 SWAA010958 1 20010328 A 3350 6556681 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 646SW 28331 DURING SCHEDULED C4 CHECK, FOUND RT EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001042500105 20010425 00105 NM 2001 4 25 SWAA010960 1 20010328 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 730SW 27862 DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVER CRACKED AT ROW 1. REMOVED AND REPLACED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001042500106 20010425 00106 NM 2001 4 25 SWAA010930 1 20010328 A 3350 079123 COVER BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 EEPLS TRACK COVER LOOSE IN FWD SECTION. SECURED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001042500107 20010425 00107 NM 2001 4 25 SWAA010931 1 20010327 A 3350 610478 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED C1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2001042500108 20010425 00108 NM 2001 4 25 SWAA010938 1 20010328 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 638SW 27711 DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVER LOOSE AT ROW 11. SECURED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001042500109 20010425 00109 NM 2001 4 25 SWAA010917 1 20010326 A 3350 BR2013 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 394SW 27380 EEPLS TRACK COVER LOOSE AT ROW 18. REPAIRED EEPLS WIRING AND SECURED TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 2001042500110 20010425 00110 NM 2001 4 25 SWAA010918 1 20010325 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 625SW 27701 EEPLS INOP AT ROW 21. RECONNECTED EEPLS WIRING PER MM. 2 L 7 2 4F RT A16WE 2001042500111 20010425 00111 NM 2001 4 25 SWAA010919 1 20010325 A 3350 6556633 LENS BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 619SW 28035 LT OVERWING EMERGENCY EXIT LIGHT LENS COVER BROKEN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2001042500112 20010425 00112 NM 2001 4 25 SWAA010925 1 20010326 A 3350 6556633 COVER BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 503SW 24180 DURING SCHEDULED C4 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT COVER LOOSE. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001042500113 20010425 00113 NM 2001 4 25 SWAA011037 1 20010405 A 3350 079123 COVER BOEING 737 7375H4 138449D NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 519SW 25318 DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVER CRACKED AT FWD SECTION. REMOVED AND REPLACED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001042500114 20010425 00114 NM 2001 4 25 SWAA011019 1 20010404 A 3397 BR2013 WIRE BOEING 737 7377H4 1384404 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 714CB 27848 EEPLS WIRING EXPOSED AT ROW 1. SECURED WIRING PER MM. 2 L 7 2 4F RT A16WE 2001042500115 20010425 00115 NM 2001 4 25 SWAA011020 1 20010403 A 3397 BR2013 WIRE BOEING 737 7372H4 138448C NM CABIN DISCONNECTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 087SW 22903 DURING SCHEDULED C3 CHECK, FOUND EEPLS DIM BETWEEN ROWS 5 & 20. RECONNECTED EEPLS WIRES PER BAC WDM. 2 L 7 2 4F A16WE 2001042500116 20010425 00116 NM 2001 4 25 SWAA011021 1 20010403 A 3397 079123 WIRE BOEING 737 7372H4 138448C NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 087SW 22903 DURING SCHEDULED C3 CHECK, FOUND EEPLS WIRING EXPOSED AT ROW 16. INSTALLED TRACK COVER PER MM. 2 L 7 2 4F A16WE 2001042500117 20010425 00117 NM 2001 4 25 SWAA011023 1 20010403 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 645SW 28330 DURING SCHEDULED C4 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 16 DEF. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2001042500118 20010425 00118 NM 2001 4 25 SWAA011024 1 20010404 A 3350 BR2013 LIGHT BOEING 737 7373A4 1384585 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED A1 CHECK, FOUND EEPLS INOP AT ROW 9. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2001042500119 20010425 00119 NM 2001 4 25 SWAA011025 1 20010403 A 3350 6556633 LENS BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED C3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2001042500120 20010425 00120 NM 2001 4 25 SWAA011027 1 20010404 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 750SA 29802 DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVER CRACKED AT EMERGENCY EXIT ROW. REMOVED AND REPLACED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001042500121 20010425 00121 NM 2001 4 25 SWAA011028 1 20010404 A 3350 BR9442 LENS BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 606SW 27926 EMERGENCY EXIT LIGHT LENS CRACKED AT FWD F/A STATION. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2001042500122 20010425 00122 NM 2001 4 25 SWAA011005 1 20010402 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 372SW 26599 AFT ENTRY DOOR EMERGENCY EXIT LIGHT LENS COVER MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001042500123 20010425 00123 NM 2001 4 25 SWAA011006 1 20010403 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 396SW 27690 EEPLS TRACK COVERS LOOSE AT EMERGENCY EXIT ROW. SECURED TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 2001042500124 20010425 00124 NM 2001 4 25 SWAA011008 1 20010403 A 3350 300432 LIGHT BOEING 737 7372H4 138448C NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL EMERGENCY EXIT LIGHT INOP AT LT AFT LOWER FUSELAGE. RELAMPED LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 2001042500125 20010425 00125 NM 2001 4 25 SWAA010974 1 20010331 A 3397 BR2013 WIRE BOEING 737 7375H4 138449D NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 EEPLS WIRING EXPOSED AT ROW 12. REPAIRED EEPLS WIRING PER MM. 2 L 7 2 4F RT A16WE 2001042500126 20010425 00126 NM 2001 4 25 P5CA0100508 1 20010323 A 5753 SKIN BOEING 747 7472U3B NM T/E MIDFLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 923FT 22769 DELAMINATION FOUND ON LT WING, T/E INBOARD MID FLAP BOTTOM SKIN WITH BULGES. REPAIRED PER SRM 51-40-15. 2 L 7 4 4F RT A20WE 2001042500127 20010425 00127 NE 2001 4 25 P5CA0100482 2 20010228 A 7200 BEARING BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR2 ENGINE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 662857 DAMAGE FOUND ON NR 2 ENG LT TANGENTIAL BEARING. REPLACED TANGENTIAL LINK AND BEARING PER MM 71-21-04 ITEM 13. 2 L 7 4 4F 4 F A20WE E20EA 2001042500128 20010425 00128 NM 2001 4 25 P5CA0100483 1 20010226 A 5311 FRAME BOEING 747 7472U3B NM FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 922FT 22768 CRACK FOUND ON 1265 FRAME RT AND LT SIDE. REPAIRED PER SB 747-53A-2416. 2 L 7 4 4F RT A20WE 2001042500129 20010425 00129 NM 2001 4 25 P5CA0100484 1 20010228 A 5313 STRINGER BOEING 747 7472U3B NM FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 922FT 22768 CRACK 2.1 LONG BS 1000 LHS STR 46. REPAIRED PER SB747-53-2316. 2 L 7 4 4F RT A20WE 2001042500130 20010425 00130 NM 2001 4 25 P5CA0100466 1 20010225 A 2612 33603903P FIRE WARNING BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE NR 2 ENGINE ACTIVATED A P5CA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION TO TAKEOFF 1 WP 23 806FT 21827 702264 NR 2 ENG FIRE DET LIGHT AND FAULT LIGHT CAME ON A-LOOP WITH A FIRE WARNING. ENGINE SHUT DOWN AND BOTTLE FIRED. REPLACE D NR 2 LFT FIRE BOTTLE. P/N ON 33603903P, S/N M2621 2 L 7 4 4F 4 F A20WE E3NE 2001042500131 20010425 00131 NM 2001 4 25 P5CA0100467 1 20010213 A 5753 SKIN BOEING 747 747122 1384872 NM MID FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 DELAMINATION FOUND ON LEFT O/B MID FLAP. REPAIRED PER PAO-LGB01-00045F. 2 L 7 4 4F A20WE 2001042500132 20010425 00132 NM 2001 4 25 P5CA0100468 1 20010221 A 5230 SKIN BOEING 747 7472U3B NM CARGO DOOR DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 922FT 22768 DENT FOUND ON AFT CARGO DOOR EXT SKIN AT LOWER FWD SECTION AT INSP PANEL. REPAIRED PER SRM 52-00-03. 2 L 7 4 4F RT A20WE 2001042500133 20010425 00133 NM 2001 4 25 P5CA0100469 1 20010221 A 5310 STOP FITTING BOEING 747 7472U3B NM DOOR FRAME CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 922FT 22768 CRACK ON LT DOOR STOP AFT SIDE ON WEB DOOR FRAME. REPAIRED PER SRM 53-10-04. 2 L 7 4 4F RT A20WE 2001042500134 20010425 00134 NM 2001 4 25 P5CA0100470 1 20010221 A 5330 SKIN BOEING 747 7472U3B NM FUSELAGE DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 922FT 22768 DENT FOUND ON FUSELAGE SKIN RT SIDE EXT SURFACE AT BS 450 S37R. REPAIRED PER SRM 53-30-03. 2 L 7 4 4F RT A20WE 2001042500135 20010425 00135 NM 2001 4 25 P5CA0100471 1 20010221 A 5330 SKIN BOEING 747 7472U3B NM FUSELAGE DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 922FT 22768 DENT FOUND ON FUSELAGE SKIN LT SIDE EXTERIOR SURFACE AT BS 630 S39L. REPAIRED PER SRM 53-30-03. 2 L 7 4 4F RT A20WE 2001042500136 20010425 00136 NM 2001 4 25 P5CA0100472 1 20010221 A 5330 SKIN BOEING 747 7472U3B NM FUSELAGE DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 922FT 22768 DENT FOUND ON FUSELAGE SKIN LT BS 510 S28L. REPAIRED PER SRM 53-30-03. 2 L 7 4 4F RT A20WE 2001042500137 20010425 00137 WP 2001 4 25 AT0100120 1 20010324 A 5270 WARNING LIGHT DOUG DC9 DC932 3022066 WP COCKPIT FALSE INDICATION A ZZDA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 15 832AT 47451 AFT CABIN DOOR LIGHT ILLUMINATED IN FLIGHT CAUSING AIR RETURN. ACTIVATED DOOR SEVERAL TIMES WITH NO DISCREPANCIES. 2 L 7 2 4F A6WE 2001042500138 20010425 00138 NM 2001 4 25 CALA0100292 1 20010406 A 5210 BEAM BOEING 737 7373T0 1384582 NM PAX DOOR GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND L-1 DOOR INNER DOOR CHORD BEAM GOUGED IN UPPER TORQUE TUBE SLEEVE BAY AT STA 312. THE CHORD BEAM WAS R EMOVED AND A NEW CHORD BEAM WAS INSTALLED IAW SRM 52-10-02 AND 51-30-02. 2 L 7 2 4F RT A16WE 2001042500139 20010425 00139 EA 2001 4 25 COMA0160356 1 20010408 A 5311 6003603024 FRAME CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 999CA 7230 RIGHT FS 718 FRAME BETWEEN STRINGERS 10 AND 12 CRACKED. REPAIRED CRACK IAW CANADAIR REO 601R-53-61-193A. 2 L 7 2 4F RT A21EA 2001042500140 20010425 00140 EA 2001 4 25 COMA0160357 1 20010407 A 5311 6003603023 FRAME CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 999CA 7230 LEFT FS 718 FRAME BETWEEN STRINGERS 10 AND 12 CRACKED. REPAIRED CRACK IAW CANADAIR REO 601R-53-61-193 REVA. 2 L 7 2 4F RT A21EA 2001042500141 20010425 00141 WP 2001 4 25 TWAA0106216 1 20010331 A 5210 STOP FITTING DOUG DC9 DC982 3022082 WP ENTRY DOOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 906TW 49160 DURING CHECK-C MAINT AT AFT ENTRY DOOR, THE LT BOTTOM DOOR STOP CASTING WAS CRACKED. INSTALLED NEW CASTING. FASTENERS INSTALLED PER SRM 51-30-02 AND 51-30-5. 2 L 7 2 4F A6WE 2001042500142 20010425 00142 WP 2001 4 25 TWAA0106223 1 20010403 A 5210 WEB DOUG DC9 DC982 3022082 WP PAX DOOR CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT ON THE FWD ENTRY DOOR, CORROSION WAS FOUND ON MEMBRANE AFT SIDE OF STA 160, LONGERON 18L. UT INSP INDICATES 40 PER CENT MATERIAL LOSS. REPAIRED PER ARA 17574. 2 L 7 2 4F A6WE 2001042500143 20010425 00143 WP 2001 4 25 TWAA0106209 1 20010402 A 5230 BEAM DOUG DC9 DC982 3022082 WP CARGO DOOR CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 928TW 48012 DURING CHECK-C MAINT IN THE AFT CARGO COMPT, THE LOWER CARGO DOOR BEAM HAD CORROSION. REMOVED AND REPLACED BEAM PER DOU GLAS PRINT 5930483, SRM 51-30-5, SRM 51-30-02, AND 51-60-0. 2 L 7 2 4F A6WE 2001042500144 20010425 00144 EU 2001 4 25 QXEA0100438 1 20010404 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 477AU 11226 SEA - UPON INSPECTION, FOUND FORWARD EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED EXIT SIGN CIRCUIT BOARD. OP ERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001042500145 20010425 00145 EU 2001 4 25 QXEA0100439 1 20010405 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN DEFECTIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 483US 11233 SEA - EMERGENCY EXIT LIGHT OVER FLIGHT COMPARTMENT DOOR DIM. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001042500146 20010425 00146 EU 2001 4 25 QXEA0100440 1 20010404 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 486US 11237 PDX - EXIT SIGN OVER FLIGHT COMPARTMENT DOOR WAS FOUND WITH ONE SEGMENT BURNT OUT. REMOVED AND REPLACED SIGN. OPERATIO NAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001042500147 20010425 00147 SO 2001 4 25 SWIA972484 1 20010405 A 5270 SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE ENTRY DOOR OUT OF ADJ A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 207SW 120266 ON TAKEOFF FORWARD DOOR LIGHT BLINKED ON WITH WARNING. ADJUSTED THE MICROSWITCH FOR THE FORWARD DOOR LIGHT. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042500148 20010425 00148 WP 2001 4 25 ABXA010123 1 20010407 A 3231 5704066 ROD DOUG DC8 DC861 3021952 WP RT MLG DOOR BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 55050 45891 THE RIGHT MAIN LANDING GEAR FLYING DOOR CONNECTING ROD WAS BROKEN. MAINTENANCE INSPECTED AND REPLACED THE RIGHT MAIN LA NDING GEAR FLYING DOOR CONNECTING ROD, IAW DC-8 MM 32-12-01. 2 L 7 4 4F 4A25 2001042500149 20010425 00149 WP 2001 4 25 TWAA0106305 1 20010404 A 5240 STOP FITTING DOUG DC9 DC982 3022082 WP SERVICE DOOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 906TW 49160 DURING CHECK-C MAINT IN THE AFT CABIN, THE AFT ENTRY DOOR STOP CASTING WAS CRACKED ON RT SIDE, 18 INCHES ABOVE FLOOR RBL 17 INCHES. REPLACED BRACKET WITH NEW PER SPM 6-70-01 AND SRM 51-30-2 PAGE 1. 2 L 7 2 4F A6WE 2001042500150 20010425 00150 WP 2001 4 25 TWAA0106306 1 20010404 A 5240 STOP FITTING DOUG DC9 DC982 3022082 WP SERVICE DOOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 906TW 49160 DURING CHECK-C MAINT IN THE AFT CABIN, THE AFT CABIN ENTRY DOOR STOP CASTING WAS CRACKED ON RT SIDE, 36 INCHES ABOVE FLO OR RBL 17 INCHES. REPLACED BRACKET PER SRM 51-70-01 AND SRM 51-30-02 PAGE 1. 2 L 7 2 4F A6WE 2001042500151 20010425 00151 WP 2001 4 25 TWAA0106307 1 20010403 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT IN FWD CARGO COMPT FOUND CORROSION ON FWD CARGO DOOR LOWER JAMB. REMOVED LOWER FWD CARGO DOOR FLOO R PAN AND INSTALLED FLOOR PAN WITH HI-LOKS PER SRM 53-05. 2 L 7 2 4F A6WE 2001042500152 20010425 00152 EU 2001 4 25 QXEA0100442 1 20010406 A 5210 A26350411 CABLE FOKKER F28 F28MK4000 4990810 EU DOOR INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX-WITH AIRSTAIR DOOR HANDLE IN ALTERNATE POSITION, CAN''''T PUSH OPEN AIRSTAIR DOOR. REMOVED AND REPLACED PASSENGER D OOR ACTUATOR MECHANICAL RELEASE CABLE FROM INBOARD HANDLE TO CABLE TENSION BALANCE LINK. OPERATIONAL CHECK GOOD. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001042500153 20010425 00153 WP 2001 4 25 EIA2001110 1 20010228 A 5330 ACCESS PANEL DOUG DC9 DC933F 302207A WP CENTER FUEL TANK CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 MZJ-EAC - FOUND LEFT CENTER FUEL TANK ACCESS, CORROSION ON 41 HOLES. REPAIRED LEFT CENTER FUEL TANK ACCESS PER ECRA 933 -53-081-2. (M) 2 L 7 2 4F A6WE 2001042500154 20010425 00154 SO 2001 4 25 C2XA01TY073 1 20010410 A 5220 14527698001 SKIN EMB 145 EMB145LR SO EMGER EXIT DR DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18982 145223 TYS DURING A SCHEDULED INSPECTION THE LEFT HAND EMERGENCY EXIT DOOR INNER SKIN WAS FOUND TO BE SCRATCHED. MAINTENANCE REPAIRED THE DOOR SKIN IAW EMB GST-1175/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2001042500155 20010425 00155 SO 2001 4 25 C2XA01TY074 1 20010410 A 5220 14527698001 SKIN EMB 145 EMB145LR SO EMERG EXIT DR DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18982 145223 TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND EMERGENCY EXIT DOOR INNER SKIN WAS FOUND TO BE SCRATCHED. MAINTENANCE REPAIRED THE DOOR SKIN IAW EMB GST-1175/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2001042500156 20010425 00156 SO 2001 4 25 C2XA01TY077 1 20010411 A 5230 14522493001 SKIN EMB 145 EMB145LR SO CARGO DOOR CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18982 145223 TYS DURING A SCHEDULED INSPECTION THE CARGO DOOR HANDLE CUTOUT SKIN WAS FOUND TO BE CHAFED. MAINTENANCE REPAIRED THE D OOR SKIN IAW EMB GST-1174/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2001042500157 20010425 00157 SO 2001 4 25 SWIA972496 1 20010326 A 5210 DOOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE ENTRY DOOR OUT OF ADJ A SWIA K NONE O OTHER CR CRUISE 1 NM 07 199SW 120237 EXCESSIVE LOUD HISSING THROUGH FORWARD CABIN DOOR. FLIGHT ATTENDANT REPORTS HE CAN SEE DAYLIGHT THROUGH BOTTOM RIGHT SI DE OF FORWARD DOOR. SHIM FORWARD BOTTOM CORNER OF CABIN DOOR. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042500158 20010425 00158 SO 2001 4 25 RAAAO1E404 1 20010411 A 5230 SKIN LKHEED 188 188C 5262604 SO CARGO DOOR TORN A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 4 MAINTENANCE CHECK, FOUND FWD BAGGAGE PIT DOOR SKIN TORN AT LOWER AFT EDGE. REPAIRED PER L-188 SRM 53-2-1 FIG 2. M-54 # 162 2 L 7 4 4T 4A22 2001042500159 20010425 00159 SO 2001 4 25 C2XA01IA209 1 20010407 A 5210 14540853401 DOOR EMB 145 EMB145LR SO ENTRY DOOR OUT OF RIG A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15980 145202 IAH - FLIGHT 3300, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE MAIN CABIN DOOR INDICATED CLOSED AND LOCKED WHILE OPEN. MAINTENANCE RIGGED THE CABIN DOOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002022700100 20020227 00100 NM 2002 2 27 WRLA200103 1 20010302 A 2710 96010215 TRANSMITTER DOUG MD11 MD11 3023602 NM FLAP HANDLE FAILED A WRLA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 27 273WA 48519 AFTER TAKEOFF, DEFLECTED AILERONS WOULD NOT RETRACT, AIR RETURNED TO KSEA BASE. MAINTENANCE PROCEDURES COMPLIED WITH, A IRCRAFT DEPARTED. FLAP HANDLE POSITION TRANSMITTER POSITION TRANSMITTER WAS CHANGED TO CORRECT PROBLEM. FLAP HANDLE PO SITION TRANSMITTER. (M) 2 L 7 3 4F RT A22WE 2001042500160 20010425 00160 NM 2001 4 25 WRLA200105 1 20010313 A 2612 710113 FIRE LOOP DOUG MD11 MD11 3023602 NM NR 3 ENGINE MALFUNCTIONED A WRLA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 275WA 48631 PASSING FLIGHT LEVEL 230, ON CLIMB-OUT RECEIVED ENGINE FIRE WARNING ON NR 3 ENGINE, ENGINE SHUT DOWN, NO OTHER FIRE INDI CATION FIRE WARNING LIGHT STAYED ON FOR 20 MINUTES. FOUND FDCU3 FAULTING BOTH A AND B LOOP DETERMINED THE R4 RESPONDER B LOOP DEFECT REMOVED AND REPLACED SAME P/N ON 7101-13 S/N ON 40784 UNABLE TO DETERMINE S/N OFF. B LOOP RTS CONNECTOR D 5018J TO BE THE CLOSE PINS 1-2. CLEANED SAME AND RECONNECTED PRECAUTIONARY REPLACED NR 3 FDCU P/N ON 8038-03-03, S/N ON 920, P/N OFF 8038-02-03, S/N OFF 541. FDCU3 RTS CHECK ACCOMPLISHED WITH NO DEFECTS NOTED. COWLS CLOSED AND SECURED NR 3 ENGINE RUN ACCOMPLISHED ALL INDICATIONS NIL. NO ALERTS. (M) 2 L 7 3 4F RT A22WE 2001042500161 20010425 00161 NM 2001 4 25 WRLA200104 1 20010310 A 7931 4059011910 INDICATOR DOUG MD11 MD11 3023602 NM NR 3 INOPERATIVE A WRLA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 277WA 48743 NR 3 OIL INDICATION WENT FROM 9 QUARTS AT LEVEL OFF TO 3 QUARTS IN TWO MINUTES, SHUT DOWN ENGINE AND RETURNED BASE. SER VICED 1 QT DEFERRED NR 3 OIL QUANTITY INDICATION PER MEL M70MR10-17 MR MEL 79-31-1. NR 3 ENGINE OIL PRESSURE INDICATED NORMAL EN ROUTE WIMM-OEJN NO OIL ADDED IND. ON DISPLAY 28 QUARTS IND SYSTEM NORMAL DMI CLEARED. THE NR 3 DISPLAY ELECT RONIC UNIT WAS ON MEL 31-61-1 REF THE ATTACHED MD 11 MEL PAGE. LANDING WAS PRECAUTIONARY TO ASSURE PROPER OIL QUANTITY. (M) 2 L 7 3 4F RT A22WE 2001042500162 20010425 00162 WP 2001 4 25 HALA0100062 1 20010228 A 2910 SHUTOFF VALVE DOUG DC10 DC1010 3022110 WP NR 2 ENGINE LEAKING A HALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 13 152AA 46707 HNL - FLT 152 - NR 2 ENGINE BOTH HYD PRESS LOW LIGHTS CAME ON AS FLUID QUANTITY DECREASED TO ZERO. REPLACED 1-3 NON-REV ERSIBLE SHUTOFF VALVES. LEAK AND OPS CHECK OK. (M) 2 L 7 3 4F A22WE 2001042500167 20010425 00167 NE 2001 4 25 ASOA01028 2 20010311 A 7261 311489201 VALVE AEROSP ATR72 ATR72212 EU PWA PW120 PW127 NE RT ENGINE INOPERATIVE A ASOA D RETURN TO BLOCK B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 SO 11 630AS 336 127155 FLT 4100 - ON THE GROUND WHILE IN HOTEL MODE FOR A FLIGHT FROM ATL TO TRI, CREW EXPERIENCED SMOKE IN THE CABIN. MAINTEN ANCE FOUND THE RIGHT ENGINE EMITTING OIL OUT OF THE CASE VENT DRAIN. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE 2.5 SWITCHING VALVE. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 2001042500168 20010425 00168 NM 2001 4 25 UIEA01008 1 20010308 A 5311 65B01711158 FRAME BOEING 747 747230B 1384889 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 508MC 85610 21644 DURING ACCOMPLISHEMENT OF SB 747-53-2272 FOUND TWO CRACKED HOLE BS 360 R/S AT STRINGER 14R AND STRINGER 15R. STOP DRILL ED CRACK, INSTALLED REPAIR DOUBLERS PER STANDARD PRACTICES IN A NON-MANDATORY ZONE. AMOC APPROVED PER PAR 9 OF AD 91-11 -01. (M) 2 L 7 4 4F A20WE 2001042500169 20010425 00169 NM 2001 4 25 UIEA01007 1 20010308 A 5311 65B01711163 FRAME BOEING 747 747230B 1384889 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 508MC 21644 DURING ACCOMPLISHMENT OF SB 747-53-2272 FOUND ONE CRACKED HOLE BS 360 LEFT ABOVE STRINGER 15L. STOP DRILLED CRACK, INST ALLED REPAIR DOUBLERS PER STANDARD PRACTICES IN A NON-MANDATORY ZONE. AMOC APPROVED PER PAR (9) OF AD 91-11-01. (M) 2 L 7 4 4F A20WE 2001042500170 20010425 00170 NM 2001 4 25 UIEA01005 1 20010306 A 5311 65B01352 FRAME BOEING 747 7472F6B 1384807 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 535MC 79763 21833 DURING THE CURRENT A-CHECK, LOWER LOBE FORWARD CARGO DOOR FRAME BS 560 AT STRINGER 38R WAS FOUND CRACKED. CUTOUT SECTIO N OF CRACKED AREA FROM S37 AND S39. MANUFACTURED FILLER, REPAIR ANGLES, DOUBLERS AND ASSOCIATED FILLERS. INSTALLED IAW ATLAS EO 4753A125. (M) 2 L 7 4 4F A20WE 2001042500171 20010425 00171 NM 2001 4 25 20010425AP002 1 20010222 A 2611 160117301 BATTERY BOEING 727 72751C 1384015 NM CARGO BAY DISCHARGED A RYNA K NONE N FALSE WARNING IN INSP/MAINT 1 CE 07 413EX 19206 FOUND LOWER CARGO SMOKE DETECTOR PANEL, AMBER MAINTENANCE LIGHT ILLUMINATED. REMOVED AND REPLACED BATTERIES IN FORWARD AND AFT CARGO COMPARTMENTS SMOKE DETECTORS. SYSTEM TEST NORMAL. (M) 2 L 7 3 4F A3WE 2001042500172 20010425 00172 NM 2001 4 25 20010425AP003 1 20010218 A 2611 1864 BULB BOEING 727 72782C 1384026 NM COCKPIT BURNED OUT A RYNA K NONE N FALSE WARNING IN INSP/MAINT 1 CE 07 528PC 19597 MAIN CABIN SMOKE DETECTOR HAS 1 BACKGROUND LIGHT INOPERATIVE. REMOVED AND REPLACED ONE BACKGROUND LIGHT IN MAIN CABIN S MOKE DETECTOR INDICATOR ON FLIGHT ENGINEERS PANEL. SYSTEM TEST NORMAL. (M) 2 L 7 3 4F A3WE 2001042500173 20010425 00173 NM 2001 4 25 MASA01024 1 20010305 A 5520 85510031004 GUST LOCK DHAV DHC8 DHC8202 2809007 NM ELEVATOR LOOSE A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 434YV 434 DURING ROUTINE MAINTENANCE, THE ELEVATOR GUST LOCK PLATES WERE FOUND TO HAVE LOOSE AND SMOKING JO-BOLTS. A REPAIR WAS C OMPLIED WITH IAW RO DHC82-55-0004GJT (DEHAVILLAND RD 8-55-112). OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 2001042500174 20010425 00174 CE 2001 4 25 20010425AP004 1 20010218 A 2120 1143840045 BLOWER BEECH 1900 1900C 1154161 CE RT WING ODOR A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 19 137GA UC105 FLT 9323 - TPA-RSW - DURING FLIGHT, UNKNOWN SMELL IN THE COCKPIT. REMOVED AND REPLACED CONDENSOR BLOWER. (M) 2 L 7 2 4T RT A24CE 2001042500175 20010425 00175 NM 2001 4 25 20010425AP005 1 20010319 A 3230 6552811109 ACCESSORY UNIT BOEING 737 7372H6 NM MLG FAILED A SOKF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 235TA 21765 MSY - FLT 671 - AFTER TAKEOFF, AT MSY STATION THE LANDING GEAR DIDN''T RETRACTED, THE AIRCRAFT RETURNED TO MSY STATION FOR MAINTENANCE. AT EL SALVADOR STATION, THE LANDING GEAR ACCESSORY UNIT AND GEAR CONTROL LEVER LOCK SOLENOID WERE REPL ACED PER AMM 32-09-100 AND AMM 32-31-31. RETRACTION AND EXTENSION OF THE LANDING GEARS WERE PERFORMED PER AMM 32-31-0, WITH NORMAL RESULTS. THE AIRCRAFT RETURNED TO OPERATION. (M) 2 L 7 2 4F A16WE 2001042500176 20010425 00176 NM 2001 4 25 20010425AP006 1 20010319 A 3230 A42006028305 SOLENOID VALVE BOEING 737 7372H6 NM MLG FAILED A SOKF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 235TA 21765 MSY - FLT 671 - AFTER TAKEOFF, AT MSY STATION THE LANDING GEAR DIDN''T RETRACTED, THE AIRCRAFT RETURNED TO MSY STATION FOR MAINTENANCE. AT EL SALVADOR STATION, THE LANDING GEAR ACCESSORY UNIT AND GEAR CONTROL LEVER LOCK SOLENOID WERE REPL ACED PER AMM 32-09-100 AND AMM 32-31-31. RETRACTION AND EXTENSION OF THE LANDING GEARS WERE PERFORMED PER AMM 32-31-0, WITH NORMAL RESULTS. THE AIRCRAFT RETURNED TO OPERATION. (M) 2 L 7 2 4F A16WE 2001042500177 20010425 00177 NM 2001 4 25 20010425AP007 1 20010308 A 3300 BPS73 POWER SUPPLY BOEING 757 757200 1384950 NM CABIN INOPERATIVE A N8TA K NONE L NO TEST IN INSP/MAINT 1 WP 19 513NA 26962 NUMEROUS ESCAPE PATH LIGHTING LIGHTS ON SEATS NOT WORKING. REPAIRED WIRING AT POWER SUPPLY AND REPLACED POWER SUPPLY. (M) 2 L 7 2 4F RT A2NM 2001042500178 20010425 00178 NM 2001 4 25 20010425AP008 1 20010316 A 3200 AS11504D0232 HOSE BOEING 757 757236 NM LT MLG WW RUPTURED A N8TA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 19 526NA 24794 LOST LEFT HYDRAULIC SYSTEM IN FLIGHT, RETURNED TO STATION AND MADE AN UNEVENTFUL LANDING. INSPECTION REVEALED BURST HOS E ASSEMBLY IN LEFT MLG WHEEL WELL. REPLACED HOSE, SERVICED SYSTEM AND OPERATIONAL CHECKED GOOD. (M) 2 L 7 2 4F RT A2NM 2001042500179 20010425 00179 NM 2001 4 25 20010425AP009 1 20010311 A 2800 D45525001 SWITCH BOEING 757 757236 NM RT ENGINE FAILED A N8TA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION TX TAXI/GRND HDL 1 WP 19 544NA 6382 29942 AFTER ENGINE START, RIGHT ENGINE AUTO SHUTDOWN WITH EICAS MESSAGE RT ENG SPAR VALVE AND SPAR VALVE LIGHT. REMOVED AND R EPLACED RIGHT ENGINE SHUTOFF SWITCH IN FIRE CONTROL PANEL. (M) 2 L 7 2 4F RT A2NM 2001042500180 20010425 00180 SO 2001 4 25 ASOA01026 1 20010308 A 3310 12030182001 RHEOSTAT EMB 120 EMB120RT SO GLARESHIELD FAILED A ASOA G O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 246AS 120100 FLT 4869 - DURING FLIGHT FROM DFW-FSM, CREW NOTICED SMOKE COMING FROM THE F/O SIDE OF THE AUDIO CONTROL PANEL. THE CAPT AIN AND F/O DONNED MASKS AND GOGGLES. NO EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED SAFELY IN FSM. MAINTENANCE FOUND THE F/O CHART HOLDER RHEOSTAT CONTACTS SHORTING TO THE GLARESHIELD STRUCTURE. MAINTENANCE REMOVED EXCESSIVE SOLDER AND APPLIED NON-CONDUCTIVE ANTI-CHAFE COMPOUND TO RHEOSTAT CONTACTS. NO FURTHER DEFECTS WERE NOTED. OPS CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001042500196 20010425 00196 WP 2001 4 25 USAAD01049 1 20010313 A 2170 V1211 COALESCER BAG DOUG DC9 DC981 3022081 WP A/C BAY CONTAMINATED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 807US 48039 CLT-EWR - FLT 554 - AFTER TAKEOFF, SMOKE APPEARED IN THE REAR CABIN. THE LEFT AIR CONDITIONING PACK WAS TURNED OFF AND THE SMOKE DISSIPATED. THE AIRCRAFT CONTINUED TO ITS DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE RELEASED THE AIRCRAFT WITH THE LEFT AIR CONDITIONING PACK INOPERATIVE UNDER THE MEL PROCEDURES. DURING OVERNIGHT MAINTENANCE THE AIR CONDITIONING WATER SEPARATOR BAG WAS REPLACED FOR CONTAMINATION AND THE AREA CLEANED. (M) 2 L 7 2 4F A6WE 2001042500197 20010425 00197 2001 4 25 USAAD01052 4 20010114 A 2565 HANDLE DOUG DC9 DC982 3022082 WP SLIDE RELEASE MISSING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 824US 49143 BWI - THE FORWARD GALLEY SERVICE DOOR EMERGENCY EVACUATION SLIDE MANUAL RELEASE WAS NOT ATTACHED TO THE LANYARD. MAINTE NANCE SECURED THE MANUAL RELEASE. (M) 2 L 7 2 4F A6WE 2001042500198 20010425 00198 WP 2001 4 25 USAA010258 1 20010228 A 5310 SHEAR TIE DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 826US 52843 48026 BOS - FOUND SHEAR TIE CORRODED .75 INCH BY 2 INCH, STATION 1287 BETWEEN LONGERON 28L TO 28R. CORROSION LEVEL 1. BURNIS HED, TREATED AND PRIMED CORROSION. CUT OUT SECTION OF SHEAR TIE AND REPLACED PER OM-26. (M) 2 L 7 2 4F A6WE 2001042500199 20010425 00199 NM 2001 4 25 USAASB01073 1 20010304 A 2130 72073735 RELIEF VALVE BOEING 737 7374B7 1384702 NM CABIN PRESSURE FAILED A USAA G B A O2 MASK DEPLOYED EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 775AU 29543 24933 PHL - FLT 2178 - EN ROUTE FROM PHL-NAS, CLIMBING THROUGH FL140, THE PRESSURIZATION SYSTEM WENT TO STANDBY MODE. CABIN A LTITUDE CLIMBED TO 14,000 FEET AND THE OXYGEN MASKS DEPLOYED. PRESSURIZATION WAS CONTROLLABLE. CREW ACCOMPLISHED CHECK LIST AND CLOSED OUTFLOW VALVE THEN DESCENDED FLIGHT TO FL080 AND RETURNED TO FIELD AT PHL. FLIGHT LANDED WITHOUT FURTHE R INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE TROUBLESHOT SYSTEM TO THE RIGHT SAFETY RELIEF VALVE. REMOVED AND R EPLACED SAFETY RELIEF VALVE PER MM 21-32-21. ALSO, FOUND AFT OUTFLOW VALVE FAILING. REMOVED AND REPLACED AFT OUTFLOW V ALVE (P/N 711003-3) PER MM 21-31-11. AS PRECAUTIONARY, REMOVED AND REPLACED OVERHEAD CABIN PRESSURE SELECTOR PANEL (P/N 2 L 7 2 4F RT A16WE 2001042500200 20010425 00200 NM 2001 4 25 USAASB01074 1 20010306 A 5210 DOOR BOEING 737 7373B7 1384580 NM AFT PAX NOT CLOSED A USAA A UNSCHED LANDING P W NO WARNING INDICATION INADEQUATE Q C CL CLIMB 1 EA 19 520AU 23706 IAH - FLT 744 - ON CLIMB-OUT FROM IAH, CAPTAIN REPORTED THEY COULD NOT GET THE CABIN TO PRESSURIZE. AT 8,000 FEET, FLIG HT ATTENDANT ADVISED CAPTAIN THAT THE AFT SERVICE DOOR WAS NOT CLOSED. NO DOOR INDICATION WAS NOTED IN COCKPIT. FLIGHT RETURNED TO FIELD AT IAH AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE AFT SE RVICE DOOR NOT FULLY CLOSED. CHECK OPERATION OF DOOR. DOOR CHECKS GOOD. PRESSURIZED AIRCRAFT. PRESSURIZATION CHECKS GOOD. A MEL HAS BEEN ISSUED FOR THE AFT SERVICE DOOR WARNING LIGHT SYSTEM. (M) 2 L 7 2 4F RT A16WE 2001042500201 20010425 00201 NM 2001 4 25 USAASB01069 1 20010301 A 3350 CHARGER BOEING 737 737301 1384611 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 352US 23555 DCA - MAINTENANCE FOUND THE THIRD BULLNOSE EMERGENCY LIGHT IN THE CABIN INOPERATIVE. MAINTENANCE REPAIRED THE GROUND ON PIN 16 OF PLUG D2962 AT STATION 462. OPERATIONAL CHECK GOOD. REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY (P/N 2 012-1) AT STATION 622, RT SIDE, AS PRECAUTIONARY. (M) 2 L 7 2 4F RT A16WE 2001042500202 20010425 00202 NM 2001 4 25 USAASB01071 1 20010302 A 3350 20121 POWER SUPPLY BOEING 737 737301 1384611 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 576US 23741 GSO - MAINTENANCE FOUND THE EMERGENCY LIGHT AT SEAT ROW 16 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPP LY ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001042500203 20010425 00203 NM 2001 4 25 USAASB01070 1 20010301 A 3350 20121 POWER SUPPLY BOEING 737 7374B7 1384702 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 432US 24554 TPA - MAINTENANCE FOUND THE AFT RIGHT INTERIOR OVERWING EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POW ER SUPPLY ASSEMBLY FOR THE AFT RIGHT INTERIOR OVERWING EXIT SIGN. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001042500204 20010425 00204 NM 2001 4 25 USAASB01067 1 20010228 A 3350 AD20131A BATTERY PACK BOEING 737 737401 1384701 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 423US 23990 LGA - MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY LIGHT AND HATCH LIGHT EXTINGUISHES AFTER SIXTY SECONDS DURING TEST. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002022100032 20020221 00032 NE 2002 2 21 USAAF01009 2 20010319 A 7200 ENGINE FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAY65015 54557 NE LEFT FAILED A USAA A UNSCHED LANDING E J Y VIBRATION/BUFFET WARNING INDICATION ENGINE STOPPAGE CL CLIMB 1 EA 19 893US 11373 PIT-TOL - FLT 841 - WHILE CLIMBING THROUGH FL180, THE CREW FELT A VIBRATION IN THE AIRCRAFT. THEN, RECEIVED A VIBRATION WARNING INDICATION FOR THE LEFT ENGINE. POWER WAS PULLED BACK ON THE LEFT ENGINE. WHILE THE POWER WAS BEING REMOVED, THE LEFT ENGINE FAILED. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO FIELD, LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE. OPERATION AND LEAK CHECKED OK. (M) 2 L 7 2 4F 4 F RT E25NE 2001042500206 20010425 00206 NM 2001 4 25 USAASB01075 1 20010308 A 3397 WIRE BOEING 737 737201 1384454 NM CABIN DAMAGED A K NONE L NO TEST IN INSP/MAINT 1 EA 19 264AU 22961 LGA - THE LOW LEVEL EMERGENCY LIGHT AT SEAT ROW 7 WAS INOPERATIVE. MAINTENANCE REPAIRED THE EMERGENCY LIGHT WIRING TO T HE SEAT ROW EMERGENCY LIGHT. (M) 2 L 7 2 4F A16WE 2001042500207 20010425 00207 NM 2001 4 25 USAASB01078 1 20010315 A 3350 900835A BATTERY PACK BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 241US 22443 BDL - MAINTENANCE FOUND THE LOW LEVEL EMERGENCY LIGHTS FROM ROWS 10 TO 14 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 2001042500208 20010425 00208 NM 2001 4 25 USAASB01079 1 20010316 A 3350 900835A BATTERY PACK BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 241US 22443 BWI - MAINTENANCE FOUND THE EMERGENCY LIGHTS INOPERATIVE AT THE EMERGENCY EXIT. MAINTENANCE REMOVED AND REPLACED THE BA TTERY PACK. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A16WE 2001042500209 20010425 00209 NM 2001 4 25 USAASB01081 1 20010318 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM MID CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 779AU 24996 BOS - MAINTENANCE FOUND THE LOW LEVEL EMERGENCY LIGHTS FOR SEAT ROWS 6 THROUGH 9 INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED THE M1479 CHARGER ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001042500210 20010425 00210 NM 2001 4 25 USAASB01082 1 20010316 A 3397 WIRE BOEING 737 7374B7 1384702 NM CABIN DAMAGED A K NONE L NO TEST IN INSP/MAINT 1 EA 19 434US 24556 LGA - MAINTENANCE FOUND THE TWO ESCAPE PATH EMERGENCY LIGHTS MOUNTED ON THE FORWARD COAT CLOSET INOPERATIVE. MAINTENANC E REPAIRED WIRES IN THE FORWARD COAT CLOSET. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001042500211 20010425 00211 EU 2001 4 25 USAAF01008 1 20010307 A 2170 5391 COALESCER BAG FOKKER F28 F28MK0100 4990807 EU A/C BAY CONTAMINATED A USAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 EA 19 898US 11398 CLT-PIT FLT 1240 - AFTER TAKEOFF, BOTH LAVATORY SMOKE DETECTORS BEGAN ALERTING. A SMELL OF SMOKE WAS ALSO PRESENT IN TH E REAR CABIN AREA. THE AIR CONDITIONING PACKS WERE SWITCHED TO MANUAL, FULL COLD, TO COOL THE CLIMBING PACK TEMPERATURE S. TEMPERATURES WERE REDUCED, HOWEVER, THE LAVATORY SMOKE DETECTORS CONTINUED TO ALERT. THE FLIGHT RETURNED TO FIELD A ND LANDED WITHOUT INCIDENT. MAINTENANCE OPERATED BOTH PACKS FROM BOTH ENGINES AND THE APU, AND COULD NOT DUPLICATE THE PROBLEM. REPLACED THE WATER SEPARATOR BAGS AS A PRECAUTION. OK FOR SERVICE. (M) 2 L 7 2 4F RT 2001042500212 20010425 00212 2001 4 25 USAASB01076 4 20010310 A 3417 ADC BOEING 737 737401 1384701 NM NR 2 FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 415US 23883 CLT - FLT 2138 - ON CLIMB-OUT FROM CLT, EN ROUTE TO IAH, CAPTAIN REPORTED THAT THE NR 2 AIR DATA COMPUTER HAD FAILED RES ULTING IN LOSS OF THE FIRST OFFICERS ALTIMETER AND AIRSPEED INDICATIONS. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WIT HOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE RE-RACKED THE NR 2 AIR DATA COMPUTER AND CHECKES SECURIT Y OF PITOT AND STATIC CONNECTIONS. BITE TEST NORMAL. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2001042500213 20010425 00213 NM 2001 4 25 USAASB01077 1 20010315 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 532AU 24479 PHL - MAINTENANCE FOUND THE EMERGENCY EXIT SIGN ABOVE THE AFT LEFT ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPL ACED THE BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001042500214 20010425 00214 NM 2001 4 25 UHLA003185 1 20010228 A 3350 OL3071BPCGPL BULB DHAV DHC8 DHC8315 2809010 NM CABIN BLOWN A UHLA K NONE L NO TEST IN INSP/MAINT 1 NE 03 801SA 393 BUF - DURING NIGHT MAINTENANCE CHECK, TWO FORWARD EMERGENCY AISLE LIGHT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED TWO FORWARD EMERGENCY LIGHT BULBS IAW DMM 33-51-00. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 2001042500215 20010425 00215 EA 2001 4 25 UHLA003227 1 20010313 A 3350 1014001 CONNECTOR DHAV DHC8 DHC8311 1386006 EA CEILING DIRTY A UHLA K NONE L NO TEST IN INSP/MAINT 1 NE 03 802SA 19599 250 BUF - DURING OVERNIGHT MAINTENANCE, THE OVERHEAD MAIN CABIN DOOR EXIT SIGN WAS INOPERATIVE. MAINTENANCE CLEANED AND RES ECURED THE CONNECTOR AT THE EXIT SIGN AND OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A13NM 2001042500216 20010425 00216 EA 2001 4 25 UHLA013150 1 20010218 A 3297 WIRE DHAV DHC8 DHC8311 1386006 EA RT NACELLE BROKEN A K NONE J WARNING INDICATION IN INSP/MAINT 1 NE 03 802SA 250 FLT 492 - BUF-BD - RIGHT AMBER MAIN GEAR DOOR LIGHT ILLUMINATED AFTER THE GEAR WERE SELECTED UP. MAINTENANCE CONTROL RE QUESTED THAT THEY RETURN TO BUF. AIRCRAFT LANDED WITH NO FURTHER PROBLEMS. BUF MAINTENANCE FOUND RIGHT GEAR DOOR SENSO R OUT OF LIMITS AND K-14 RELAY DEFECTIVE. THE SENSOR WAS READJUSTED AND K-14 RELAY WAS REPLACED. A MAINTENANCE CHECK F LIGHT WAS PERFORMED, NO DEFECTS NOTED. AIRCRAFT WAS RELEASE FOR SERVICED. PROBLEM REOCCURED SEE MRRS OF 2/21/01 ANDS 2 /23/01 AND 2/25/01 WO 4994 MAINTENANCE TRACED WIRING FOR RIGHT MAIN UPLOCK SENSOR AND FOUND THREE PINCHED WIRES. ABLE T O DUPLICATE PROBLEM BY FLEXING WIRES. REPAIRED WIRES AND CYCLED GEAR. OPS CHECKS AND CHECK FLIGHT BOTH GOOD. (M) 2 H 7 2 4T RT A13NM 2001042500217 20010425 00217 EA 2001 4 25 UHLA013169 1 20010221 A 3297 WIRE DHAV DHC8 DHC8311 1386006 EA RT NACELLE BROKEN A O OTHER J WARNING INDICATION LD LANDING 1 NE 03 802SA 19512 250 FLIGHT 287 - TTN-BUF - CREW NOTICED THE RIGHT GEAR DOOR LIGHT ILLUMINATING WHILE APPROACHING BUF. CREW LANDED WITHOUT A NY INCIDENTS. BUF MAINTENANCE TROUBLESHOT SYSTEM, WIRING, DOOR AND GEAR SENSOR/TARGET GAPS. PERFORMED SIX GEAR SWINGS. NO DEFECTS NOTED. AIRCRAFT WAS RELEASED TO SERVICE. MAINTENANCE TRACED WIRING FOR THE RIGHT MAIN UPLOCK SENSOR AND F OUND 3 PINCHED WIRES. ABLE TO DUPLICATE PROBLEM BY FLEXING WIRES. REPAIRED WIRES AND CYCLED GEAR. OPS CHECK AND CHECK FLIGHT BOTH GOOD. (M) 2 H 7 2 4T RT A13NM 2001042500218 20010425 00218 WP 2001 4 25 CALA0100353 1 20010413 A 5230 SKIN DOUG DC9 DC982 3022082 WP CARGO DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND AFT PIT DOOR EXTERNAL SKIN DENTED. THE DENTED AREA WAS CUTOUT AND DOUBLER AND FILLER WERE INSTALLED IA W SRM 52-05. 2 L 7 2 4F A6WE 2001042500219 20010425 00219 NM 2001 4 25 CALA0100359 1 20010413 A 5230 DOOR FRAME BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND A 2.5 INCH CRACK IN AFT CARGO DOOR FORWARD FRAME SPLICE, THROUGH HOLE FOR TENSION PULLEY FOR COUNTER BA LANCE MECHANISM, APPROXIMATELY 3.5 INCH FROM CENTERLINE OF DOOR. THE AFT CARGO DOOR WAS REMOVED AND THE FORWARD UPPER A ND LOWER FRAME SECTIONS WERE REPLACED IAW SRM 51-40-2 AND 52-30-02. THE DOOR WAS REINSTALLED IAW CARD 03-5230-1-4003. 2 L 7 2 4F RT A16WE 2001042500220 20010425 00220 EU 2001 4 25 SIMA07814 1 20010228 A 5730 S5241055700200 ACCESS PANEL AEROSP ATR72 ATR72212 EU LT WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AT 274 SAW - DURING CPCP-4 INSPECTION MAINTENANCE REPORTED THE UPPER LEFT WING FUEL CELL ACCESS PANEL 522CT AND 521DT CORRODED. MAINTENANCE REMOVED AND REPLACED BOTH PANELS IAW JIC 57-00-00-OAC-10000-017. (M) 2 H 7 2 4T RT A53EU 2001042500221 20010425 00221 EU 2001 4 25 20010425AP010 1 20010228 A 5730 S5241055200200 ACCESS PANEL AEROSP ATR72 ATR72212 EU LT WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AT 274 SAW - DURING CPCP-4 INSPECTION MAINTENANCE REPORTED THE UPPER LEFT WING FUEL CELL ACCESS PANEL 522CT AND 521DT CORRODED. MAINTENANCE REMOVED AND REPLACED BOTH PANELS IAW JIC 57-00-00-OAC-10000-017. REF SIMA07814. (M) 2 H 7 2 4T RT A53EU 2001042500222 20010425 00222 EU 2001 4 25 SIMA07813 1 20010227 A 5320 S5367800920002 INTERCOSTAL AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AT 274 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE LEFT INTERCOSTAL BETWEEN FRAMES 36 AND 38 CORRODED, THE LEFT FLO OR SUPPORT BETWEEN FRAMES 38 AND 39 CORRODED. THE RIGHT INTERCOSTAL BETWEEN FRAMES 36 AND 38 CORRODED, AND TEH SERVICE DOOR DRAIN TRACK BETWEEN FRAMES 36 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTALS, FLOOR SUPPORT, A ND DRAIN TRACK IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001042500223 20010425 00223 EU 2001 4 25 20010425AP011 1 20010227 A 5320 S5367800826801 FLOOR SUPPORT AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AT 274 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE LEFT INTERCOSTAL BETWEEN FRAMES 36 AND 38 CORRODED, THE LEFT FLO OR SUPPORT BETWEEN FRAMES 38 AND 39 CORRODED. THE RIGHT INTERCOSTAL BETWEEN FRAMES 36 AND 38 CORRODED, AND TEH SERVICE DOOR DRAIN TRACK BETWEEN FRAMES 36 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTALS, FLOOR SUPPORT, A ND DRAIN TRACK IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA07813. (M) 2 H 7 2 4T RT A53EU 2001042500224 20010425 00224 EU 2001 4 25 20010425AP012 1 20010227 A 5320 S5367800920102 INTERCOSTAL AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AT 274 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE LEFT INTERCOSTAL BETWEEN FRAMES 36 AND 38 CORRODED, THE LEFT FLO OR SUPPORT BETWEEN FRAMES 38 AND 39 CORRODED. THE RIGHT INTERCOSTAL BETWEEN FRAMES 36 AND 38 CORRODED, AND TEH SERVICE DOOR DRAIN TRACK BETWEEN FRAMES 36 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTALS, FLOOR SUPPORT, A ND DRAIN TRACK IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA07813. (M) 2 H 7 2 4T RT A53EU 2001042500225 20010425 00225 EU 2001 4 25 20010425AP013 1 20010227 A 5320 S5367121729501 SILL DRAIN AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AT 274 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE LEFT INTERCOSTAL BETWEEN FRAMES 36 AND 38 CORRODED, THE LEFT FLO OR SUPPORT BETWEEN FRAMES 38 AND 39 CORRODED. THE RIGHT INTERCOSTAL BETWEEN FRAMES 36 AND 38 CORRODED, AND TEH SERVICE DOOR DRAIN TRACK BETWEEN FRAMES 36 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTALS, FLOOR SUPPORT, A ND DRAIN TRACK IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA07813. (M) 2 H 7 2 4T RT A53EU 2001042500226 20010425 00226 EU 2001 4 25 SIMA07812 1 20010310 A 5315 S53672406208 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AT 274 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAM 29 HAD ELONGATED HI-LOCK HOLES AT LEFT INBOARD SEAT TRACK ATTACH POINT AND FLOORBEAM 36 MISDRILLED AT LEFT FLIGHT ATTENDANT SEAT TRACK ATTAH POINT. MAINTENANCE REPAIRED BOTH FLO ORBEAMS IAW SRM 53-00-00 FIGURE 429. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001042500227 20010425 00227 EU 2001 4 25 20010425AP014 1 20010310 A 5315 S5337241123402 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE MISDRILLED A SIMA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 21 274AT 274 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAM 29 HAD ELONGATED HI-LOCK HOLES AT LEFT INBOARD SEAT TRACK ATTACH POINT AND FLOORBEAM 36 MISDRILLED AT LEFT FLIGHT ATTENDANT SEAT TRACK ATTAH POINT. MAINTENANCE REPAIRED BOTH FLO ORBEAMS IAW SRM 53-00-00 FIGURE 429. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA07812. (M) 2 H 7 2 4T RT A53EU 2001042500228 20010425 00228 EU 2001 4 25 SIMA07811 1 20010227 A 5315 S53672406208 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AT 274 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAMS 36, 38 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAMS IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001042500229 20010425 00229 EU 2001 4 25 20010425AP015 1 20010227 A 5315 S53672407252 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AT 274 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAMS 36, 38 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAMS IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA07811 (M) 2 H 7 2 4T RT A53EU 2001042500230 20010425 00230 EU 2001 4 25 20010425AP016 1 20010227 A 5315 S53672408254 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AT 274 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAMS 36, 38 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAMS IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA07811 (M) 2 H 7 2 4T RT A53EU 2001042500231 20010425 00231 EU 2001 4 25 SIMA09110 1 20010401 A 5347 EPNE95300013019 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE RIGHT FLIGHT ATTENDANT, LEFT FLIGHT ATTENDANT, LEFT AFT INBOARD, AND LEFT AFT OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9 5300-02-013. A IRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001042500232 20010425 00232 EU 2001 4 25 20010425AP017 1 20010401 A 5347 EPNE95300013023 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE RIGHT FLIGHT ATTENDANT, LEFT FLIGHT ATTENDANT, LEFT AFT INBOARD, AND LEFT AFT OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9 5300-02-013. A IRCRAFT WAS RETURNED TO SERVICE. REF SIMA09110. (M) 2 H 7 2 4T RT A53EU 2001042500233 20010425 00233 EU 2001 4 25 20010425AP018 1 20010401 A 5347 EPNE95300013017 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE RIGHT FLIGHT ATTENDANT, LEFT FLIGHT ATTENDANT, LEFT AFT INBOARD, AND LEFT AFT OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9 5300-02-013. A IRCRAFT WAS RETURNED TO SERVICE. REF SIMA09110. (M) 2 H 7 2 4T RT A53EU 2001042500234 20010425 00234 EU 2001 4 25 20010425AP019 1 20010401 A 5347 EPNE95300013018 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE RIGHT FLIGHT ATTENDANT, LEFT FLIGHT ATTENDANT, LEFT AFT INBOARD, AND LEFT AFT OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9 5300-02-013. A IRCRAFT WAS RETURNED TO SERVICE. REF SIMA09110. (M) 2 H 7 2 4T RT A53EU 2001042500235 20010425 00235 EU 2001 4 25 SIMA0919 1 20010401 A 5320 S5367121729402 SILL AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE RIGHT FLIGHT ATTENDANT, LEFT FLIGHT ATTENDANT, LEFT AFT INBOARD, AND LEFT AFT OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9 5300-02-013. A IRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001042500236 20010425 00236 EU 2001 4 25 20010425AP020 1 20010401 A 5320 S5367121729801 SILL DRAIN AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE RIGHT FLIGHT ATTENDANT, LEFT FLIGHT ATTENDANT, LEFT AFT INBOARD, AND LEFT AFT OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9 5300-02-013. A IRCRAFT WAS RETURNED TO SERVICE. REF SIMA0919. (M) 2 H 7 2 4T RT A53EU 2001042500237 20010425 00237 EU 2001 4 25 SIMA0916 1 20010401 A 5330 S5367240620402 DOUBLER AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED DOUBLER ON FRAME 36 LEFT SIDE AT FLOOR LEVEL CORRODED. MAINTENANCE REMOVED AND REPLACED THE DOUBLER IAW SRM 51-25-04. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001042500238 20010425 00238 EA 2001 4 25 UHLA013158 1 20010223 A 3297 WIRE DHAV DHC8 DHC8311 1386006 EA RT NACELLE BROKEN A K NONE J WARNING INDICATION IN INSP/MAINT 1 NE 03 802SA 19512 250 FLT 201 - TTN-BUF - DURING CRUISE, RIGHT MAIN DOOR AND RIGHT GEAR UNSAFE LIGHT ILLUMINATED. A THUMP WAS FELT WITH EACH CYCLE, CYCLED 7 TIMES IN FLIGHT. MAINTENANCE TRACED WIRING FOR THE RIGHT MAIN UPLOCK SENSOR AND FOUND 3 PINCHES WIRES I N THE RIGHT WHEEL WELL. ABLE TO DUPLICATE PROBLEM BY FLEXING WIRES. REPAIRED WIRES AND CYCLED GEAR. OPS CHECK AND CHE CK FLIGHT BOTH GOOD. (M) 2 H 7 2 4T RT A13NM 2001042500239 20010425 00239 WP 2001 4 25 GTIA010047 1 20010224 A 5350 TAIL CONE DOUG DC9 DC941 302207N WP FUSELAGE DISLODGED A GTIA O OTHER O OTHER LD LANDING 1 GL 23 130NK 47604 MYR - FLT 303 - TAILCONE CAME OFF ON LANDING. TAILCONE RELEASE SYSTEM EVACUATED AND REPAIRED BY BOEING. REPLACED EXTER IOR CABLE FITTING AND RIGHT LOWER LOCKING PIN. TAILCONE WAS FIT FOR CLEARANCES AND DROP CHECK PERFORMED AS PER DC-9 MM 53-50-3. (M) 2 L 7 2 4F A6WE 2001042500240 20010425 00240 NM 2001 4 25 AALA20010188 1 20010116 A 7100 ENGINE BOEING 767 767223 1385123 NM RIGHT LEAKING A AALA A UNSCHED LANDING K FLUID LOSS NR NOT REPORTED 1 SW 21 330AA 22330 MSP - RIGHT ENGINE LEAKING OIL IN FLIGHT, REACHING 5 QUARTS DURING DIVERT TO MSP. PRESTART 17 QUARTS, AFTER SHUTDOWN 12 QUARTS. OIL LEAK VISUALLY NOTED ON POST FLIGHT INSPECTION. AIRCRAFT HAS BEEN INSPECTED AND FOUND TO BE IN SAFE CONDIT ION FOR FERRY FLIGHT FROM MSP TO SFO FOR REPAIR OF RIGHT ENGINE. REMOVED AND REPLACED RIGHT ENGINE PER CARD 71-94-01. OPS AND LEAK CHECK GOOD EPR CARD 71-95-18. (M) 2 L 7 2 4F RT A1NM 2001042500241 20010425 00241 NM 2001 4 25 20010425AP021 1 20010307 A 7931 INDICATOR BOEING 737 737242 1384477 NM NR 2 ENGINE MALFUNCTIONED A EGEF O OTHER N FALSE WARNING LD LANDING 1 SO 23 127GU 22074 GUA - FLT 514 - ENGINE NR 2 LOW OIL PRESSURE LIGHT CAME ON, AND OIL PRESSURE INDICATOR SHOWED 30 PSI. ENGINE WAS SECURE D. CONDITION OCCURRED AFTER LANDING AT GUA. VERIFIED THAT NO WINDMILLING CONDITION EXITS. A TROUBLESHOOTING WAS ACCOM PLISHED, ACCORDING TO PW ENGINE MM 72-00 TROUBLESHOOTING 02A, PARAGRAPH ''F'' (OIL PRESSURE PROBLEMS); LOW OR NO OIL PRE SSURE; TABLE VI, AND FIGURES 118 AND 119. AIRCRAFT REMAINS ON GROUND FOR COMPLETE INSPECTION. (M) 2 L 7 2 4F A16WE 2001042500242 20010425 00242 EU 2001 4 25 FJT01039381 1 20010302 A 7710 1680540 COMPUTER BAG JETSTM JETSTM3201 1500217 EU RT ENGINE MALFUNCTIONED A FJTA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SO 03 938AE 938 RDU - FLT 1524 - AIRCRAFT WAS EN ROUTE FROM EWN TO RDU, WHEN THE RIGHT ENGINE STARTED TO HAVE TORQUE AND TEMPERATURE FLU CTUATIONS. NORMAL PROCEDURES WERE FOLLOWED AND THE ENGINE WAS SHUTDOWN. THE CAPTAIN DECLARED AN EMERGENCY AND PROCEEDE D TO RDU WERE THE AIRCRAFT LANDED SAFELY WITHOUT FURTHER INCIDENTS. ENGINE GROUND RUNS CONFIRMED THE FLUCTUATING TORQUE AND TEMPERATURE. THE RIGHT SRL COMPUTER WAS TURNED OFF AND THE ENGINE THE MAINTAINED CONSTANT TORQUE AND TEMPERATURE. THE RIGHT ENGINE SRL COMPUTER WAS MEL''D IAW MEL PROCEDURES. THE AIRCRAFT RETURNED TO SERVICE. THE MEL WAS CLEARED LA TER THE DAY BY REPLACING THE RIGHT PROPELLER MONOPOLE. SEVERAL ENGINE RUNS WERE PERFORMED, WITH NO DISCREPANCIES NOTED. 2 L 7 2 4T RT A56EU 2001042500243 20010425 00243 EU 2001 4 25 SIMA0554 1 20010224 A 2612 472326 FIRE LOOP SAAB SF340 340B 7860101 EU RT NACELLE CHAFED A SIMA F E A ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 388AE 340B388 TUL - FLT 3735 - CREW REPORTED THE RIGHT ENGINE FIRE DETECT FAIL FOLLOWED BY RIGHT ENGINE FIRE INDICATION. CREW SHUT DO WN ENGINE AND SHOT ENGINE FIRE BOTTLES. MAINTENANCE FOUND A FIRE LOOP CHAFED AND NO EVIDENCE OF FIRE. FIRE LOOP WAS RE MOVED AND REPLACED, OPS CHECK WAS GOOD. FIRE BOTTLES WERE REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001042500244 20010425 00244 EU 2001 4 25 SIMA0893 1 20010330 A 5320 S5367121721002 PLATE AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE PLATE ON TOP OF THE CREASE BEAM JUST FORWARD OF FLOORBEAM 36 LE FT CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PLATE IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVI CE. (M) 2 H 7 2 4T RT A53EU 2001042500245 20010425 00245 EU 2001 4 25 SIMA0894 1 20010330 A 5315 S5367240620802 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAMS 36 AND 38 CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AN D REPLACED THE FLOORBEAMS IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001042500246 20010425 00246 EU 2001 4 25 20010425AP022 1 20010330 A 5315 S5367240725201 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAMS 36 AND 38 CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AN D REPLACED THE FLOORBEAMS IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001042500247 20010425 00247 EU 2001 4 25 SIMA07816 1 20010227 A 5347 EPNE95300013013 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AT 274 SAW - DURING CPCP-8 INSPECTION MAINTENANCE REPORTED THE LEFT FORWARD INBOARD, LEFT MIDDLE OUTBOARD, LEFT AFT OUTBOARD, L EFT AFT INBOARD, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT INBOARD, RIGHT AFT OUTBOARD, AND RIGHT FORWARD INBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-05300-013. AIRCRAFT WAS RETU RNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001042500248 20010425 00248 EU 2001 4 25 20010425AP023 1 20010227 A 5347 S53570203202 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AT 274 SAW - DURING CPCP-8 INSPECTION MAINTENANCE REPORTED THE LEFT FORWARD INBOARD, LEFT MIDDLE OUTBOARD, LEFT AFT OUTBOARD, L EFT AFT INBOARD, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT INBOARD, RIGHT AFT OUTBOARD, AND RIGHT FORWARD INBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-05300-013. AIRCRAFT WAS RETU RNED TO SERVICE. REF SIMA07816. (M) 2 H 7 2 4T RT A53EU 2001042500249 20010425 00249 EU 2001 4 25 20010425AP024 1 20010227 A 5347 S53678001224 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AT 274 SAW - DURING CPCP-8 INSPECTION MAINTENANCE REPORTED THE LEFT FORWARD INBOARD, LEFT MIDDLE OUTBOARD, LEFT AFT OUTBOARD, L EFT AFT INBOARD, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT INBOARD, RIGHT AFT OUTBOARD, AND RIGHT FORWARD INBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-05300-013. AIRCRAFT WAS RETU RNED TO SERVICE. REF SIMA07816. (M) 2 H 7 2 4T RT A53EU 2001042500250 20010425 00250 EU 2001 4 25 20010425AP025 1 20010227 A 5347 EPNE95300013017 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AT 274 SAW - DURING CPCP-8 INSPECTION MAINTENANCE REPORTED THE LEFT FORWARD INBOARD, LEFT MIDDLE OUTBOARD, LEFT AFT OUTBOARD, L EFT AFT INBOARD, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT INBOARD, RIGHT AFT OUTBOARD, AND RIGHT FORWARD INBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-05300-013. AIRCRAFT WAS RETU RNED TO SERVICE. REF SIMA07816. (M) 2 H 7 2 4T RT A53EU 2001042500251 20010425 00251 EU 2001 4 25 20010425AP026 1 20010227 A 5347 EPNE95300013023 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AT 274 SAW - DURING CPCP-8 INSPECTION MAINTENANCE REPORTED THE LEFT FORWARD INBOARD, LEFT MIDDLE OUTBOARD, LEFT AFT OUTBOARD, L EFT AFT INBOARD, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT INBOARD, RIGHT AFT OUTBOARD, AND RIGHT FORWARD INBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-05300-013. AIRCRAFT WAS RETU RNED TO SERVICE. REF SIMA07816. (M) 2 H 7 2 4T RT A53EU 2001042500252 20010425 00252 EU 2001 4 25 20010425AP027 1 20010227 A 5347 EPNE95300013019 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AT 274 SAW - DURING CPCP-8 INSPECTION MAINTENANCE REPORTED THE LEFT FORWARD INBOARD, LEFT MIDDLE OUTBOARD, LEFT AFT OUTBOARD, L EFT AFT INBOARD, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT INBOARD, RIGHT AFT OUTBOARD, AND RIGHT FORWARD INBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-05300-013. AIRCRAFT WAS RETU RNED TO SERVICE. REF SIMA07816. (M) 2 H 7 2 4T RT A53EU 2001042500253 20010425 00253 EU 2001 4 25 20010425AP028 1 20010227 A 5347 S53678001226 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AT 274 SAW - DURING CPCP-8 INSPECTION MAINTENANCE REPORTED THE LEFT FORWARD INBOARD, LEFT MIDDLE OUTBOARD, LEFT AFT OUTBOARD, L EFT AFT INBOARD, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT INBOARD, RIGHT AFT OUTBOARD, AND RIGHT FORWARD INBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-05300-013. AIRCRAFT WAS RETU RNED TO SERVICE. REF SIMA07816. (M) 2 H 7 2 4T RT A53EU 2001042500254 20010425 00254 EU 2001 4 25 20010425AP029 1 20010227 A 5347 S53678001225 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AT 274 SAW - DURING CPCP-8 INSPECTION MAINTENANCE REPORTED THE LEFT FORWARD INBOARD, LEFT MIDDLE OUTBOARD, LEFT AFT OUTBOARD, L EFT AFT INBOARD, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT INBOARD, RIGHT AFT OUTBOARD, AND RIGHT FORWARD INBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-05300-013. AIRCRAFT WAS RETU RNED TO SERVICE. REF SIMA07816. (M) 2 H 7 2 4T RT A53EU 2001042500255 20010425 00255 EU 2001 4 25 20010425AP030 1 20010227 A 5347 EPNE95300013012 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AT 274 SAW - DURING CPCP-8 INSPECTION MAINTENANCE REPORTED THE LEFT FORWARD INBOARD, LEFT MIDDLE OUTBOARD, LEFT AFT OUTBOARD, L EFT AFT INBOARD, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT INBOARD, RIGHT AFT OUTBOARD, AND RIGHT FORWARD INBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-05300-013. AIRCRAFT WAS RETU RNED TO SERVICE. REF SIMA07816. (M) 2 H 7 2 4T RT A53EU 2001042500256 20010425 00256 EU 2001 4 25 SIMA07815 1 20010225 A 5210 S5217620421002 PAN AEROSP ATR72 ATR72212 EU PAX DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AT 274 SAW - DURING CPCP-8 INSPECTION, MAINTENANCE REPORTED THE PAX DOOR LOWER PAN CORRODED AND DENTED IN TWO PLACES. MAINTENA NCE REMOVED AND REPLACED THE LOWER PAN IAW SRM 52-11-00. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001042500257 20010425 00257 SO 2001 4 25 SIMA0773 1 20010318 A 2720 3621001007 CONTROL UNIT EMB 145 EMB145 SO HORIZONTAL STAB INOPERATIVE A SIMA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SW 21 613AE 145081 ORD - FLT 4117 - CREW REPORTED THAT THE PITCH TRIM 1 FAILED AT ABOUT 3000 AGL AND 220 KIAS AFTER TAKEOFF. CREW ALSO NOT ED THAT THE STANDY TRIM DID NOT WORK. MAINTENANCE REMOVED AND REPLACED THE HSCU. OPERATIONAL CHECK WAS GOOD AND AIRCRA FT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001042500258 20010425 00258 SO 2001 4 25 SIMA0874 1 20010328 A 3350 66364 LIGHT EMB 145 EMB145LR SO CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 619AE 145101 XNA - FLT 3687 - CREW REPORTED AISLE FLOOR LIGHTING STRIP BETWEEN ROWS 14 AND 16 INOPERATIVE. REMOVED AND REPLACED FLOO R LIGHTING STRIP BETWEEN ROWS 14 AND 16 IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT T00011AT 2001042500259 20010425 00259 SO 2001 4 25 SIMA0736 1 20010314 A 7100 ENGINE EMB 145 EMB145 SO NR 2 FAILED FAILED A SIMA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION LD LANDING 1 SW 21 613AE 145081 ORF - FLT 4365 - CREW REPORTED UPON TOUCH DOWN AND THRUST REVERSERS DEPLOYED, A LOUD BANG WAS HEARD FOLLOWED BY THE NR 2 ENGINE SHUTTING DOWN. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE IAW EMB MM. OPERATIONAL AND LEAK CHECKS WERE G OOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001042500260 20010425 00260 EU 2001 4 25 SIMA0787 1 20010315 A 5347 1289 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 332AE 340B332 SBP - FOUND SEAT 11BC SN79521 HAS CORRODED HARDWARE AT INBOARD FLOOR ATTACHMENT. REMOVED AND REPLACED BOTTOM TIE ASSEMB LY AND ALL ATTACHING HARDWARE IAW B/E AERO SB 25-20-1289. (M) 2 L 7 2 4T RT A52EU 2001042500261 20010425 00261 EU 2001 4 25 SIMA0786 1 20010315 A 5260 7253710871 TRACK SAAB SF340 340B 7860101 EU AIR STAIR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 332AE 340B332 SBP - AIR STAIR TRACK HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED AIRSTAIR TRACK AND SUPPORT ANGLES IAW SAAB S RM 51-40-21. (M) 2 L 7 2 4T RT A52EU 2001042500262 20010425 00262 EU 2001 4 25 20010425AP031 1 20010315 A 5260 7253710133 SUPPORT FITTING SAAB SF340 340B 7860101 EU AIR STAIR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 332AE 340B332 SBP - AIR STAIR TRACK HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED AIRSTAIR TRACK AND SUPPORT ANGLES IAW SAAB S RM 51-40-21. REF SIMA0786 (M). 2 L 7 2 4T RT A52EU 2001042500263 20010425 00263 EU 2001 4 25 20010425AP032 1 20010315 A 5260 7253710135 TRACK SAAB SF340 340B 7860101 EU AIR STAIR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 332AE 340B332 SBP - AIR STAIR TRACK HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED AIRSTAIR TRACK AND SUPPORT ANGLES IAW SAAB S RM 51-40-21. REF SIMA0786. (M) 2 L 7 2 4T RT A52EU 2001042500264 20010425 00264 EU 2001 4 25 SIMA0772 1 20010318 A 2750 HP14161005 VALVE SAAB SF340 340B 7860101 EU TE FLAPS INOPERATIVE A SIMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 21 243AE 340B243 BOS - FLT 4893 - ON APPROACH FLAPS WOULD NOT EXTEND FOLLOW ABNORMAL PROCEDURE FOR FLAPS FAULT. MAINTENANCE REMOVED AND REPLACED FLAP CONTROL VALVE IAW SAAB MM 27-51-15. OPS CHECK WAS GOOD AND AIRCRAFT WAS RELEASED FOR A FUNCTIONAL CHECK F LIGHT. FCF WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001042500265 20010425 00265 EU 2001 4 25 SIMA07810 1 20010227 A 5311 S5367240725601 FRAME AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AT 274 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FRAME 38 CORRODED. MAINTENANCE REMOVED AND REPLACED THE LOWER SEGME NT OF FRAME 38 IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001042500266 20010425 00266 EU 2001 4 25 SIMA0789 1 20010228 A 5320 S5337129320201 PLATE AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AT 274 SAW - DURING CPCP-4 INSPECTION MAINTENANCE REPORTED THE FORWARD CARGO DRAIN TRACK AND DRAIN TRACK SUPPORT PLATE BETWEEN FRAMES 13 AND 17 CORRODED. MAINTENANCE REMOVED AND REPLACED THE DRAIN TRACK AND PLATE IAW SRM 51-25-02. AIRCRAFT WAS R ETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001042500267 20010425 00267 EU 2001 4 25 20010425AP033 1 20010228 A 5320 S5337129320001 PLATE AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AT 274 SAW - DURING CPCP-4 INSPECTION MAINTENANCE REPORTED THE FORWARD CARGO DRAIN TRACK AND DRAIN TRACK SUPPORT PLATE BETWEEN FRAMES 13 AND 17 CORRODED. MAINTENANCE REMOVED AND REPLACED THE DRAIN TRACK AND PLATE IAW SRM 51-25-02. AIRCRAFT WAS R ETURNED TO SERVICE. REF SIMA0789. (M) 2 H 7 2 4T RT A53EU 2001042500268 20010425 00268 EU 2001 4 25 SIMA0788 1 20010307 A 5330 S53571304202 SKIN AEROSP ATR72 ATR72212 EU FUSELAGE CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING MBV-1 INSPECTION MAINTENANCE REPORTED CRACK INDICATIONS DURING EDDY CURRENT ROTO TEST OF THE LEFT AND RIGHT WING TO FUSELAGE ATTACH POINTS AT FRAME 25 AND STRINGER 7. MAINTENANCE REPAIRED THE HOLES IAW EO E2-53MR-113. AIRCRAF T WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001042500269 20010425 00269 EU 2001 4 25 20010425AP034 1 20010307 A 5330 S53571303202 SKIN AEROSP ATR72 ATR72212 EU FUSELAGE CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING MBV-1 INSPECTION MAINTENANCE REPORTED CRACK INDICATIONS DURING EDDY CURRENT ROTO TEST OF THE LEFT AND RIGHT WING TO FUSELAGE ATTACH POINTS AT FRAME 25 AND STRINGER 7. MAINTENANCE REPAIRED THE HOLES IAW EO E2-53MR-113. AIRCRAF T WAS RETURNED TO SERVICE. REF SIMA0788. (M) 2 H 7 2 4T RT A53EU 2001042500270 20010425 00270 EU 2001 4 25 SIMA0781 1 20010304 A 5315 S5337241122402 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE OVERSIZED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAM 20 AND 21 HAD MISDRILLED HI-LOCK HOLES AT OUTBOARD SEAT TRACK AT TACH POINT. MAINTENANCE REPAIRED BOTH SEAT TRACKS IAW SRM 53-00-00 FIGURE 435. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001042500271 20010425 00271 EU 2001 4 25 20010425AP035 1 20010304 A 5315 S5337241122402 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAM 20 AND 21 HAD MISDRILLED HI-LOCK HOLES AT OUTBOARD SEAT TRACK AT TACH POINT. MAINTENANCE REPAIRED BOTH SEAT TRACKS IAW SRM 53-00-00 FIGURE 435. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0781. (M) 2 H 7 2 4T RT A53EU 2001042500272 20010425 00272 EU 2001 4 25 SIMA0783 1 20010304 A 5315 S5337241122402 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAM 20 AND 21 HAD MISDRILLED HI-LOCKS HOLES AT OUTBOARD SEAT T RACK ATTACH POINT. MAINTENANCE REPAIRED BOTH SEAT TRACKS IAW SRM 53-00-00 FIGURE 435. AIRCRAFT WAS RETURNED TO SERVICE . (M) 2 H 7 2 4T RT A53EU 2001042500273 20010425 00273 EU 2001 4 25 20010425AP036 1 20010304 A 5315 S5337241122402 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAM 20 AND 21 HAD MISDRILLED HI-LOCKS HOLES AT OUTBOARD SEAT T RACK ATTACH POINT. MAINTENANCE REPAIRED BOTH SEAT TRACKS IAW SRM 53-00-00 FIGURE 435. AIRCRAFT WAS RETURNED TO SERVICE . REF SIMA0783. (M) 2 H 7 2 4T RT A53EU 2001042500274 20010425 00274 EU 2001 4 25 SIMA0785 1 20010228 A 5330 S5216301200 SKIN AEROSP ATR72 ATR72212 EU FUSELAGE CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE PAX DOOR INNER SKIN CRACKED NEXT TO THE PRESSURE RELIEF DOOR AND THE U PPER PAN CORRODED. MAINTENANCE REPAIRED THE INNER SKIN IAW SRM 52-11-00 AND 51-25-02, AND REPAIRED THE UPPER PAN IAW SR M 52-11-00 FIGURE 911. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001042500275 20010425 00275 EU 2001 4 25 20010425AP037 1 20010228 A 5210 S5217620421002 PAN AEROSP ATR72 ATR72212 EU PAX DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE PAX DOOR INNER SKIN CRACKED NEXT TO THE PRESSURE RELIEF DOOR AND THE U PPER PAN CORRODED. MAINTENANCE REPAIRED THE INNER SKIN IAW SRM 52-11-00 AND 51-25-02, AND REPAIRED THE UPPER PAN IAW SR M 52-11-00 FIGURE 911. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0785. (M) 2 H 7 2 4T RT A53EU 2001042500276 20010425 00276 SO 2001 4 25 SIMA0892 1 20010330 A 2740 3621001007 CONTROL UNIT EMB 145 EMB145LR SO HORIZONTAL STAB INOPERATIVE A SIMA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 21 617AE 145093 DFW - FLT 3756 - DURING CRUISE INTO DFW, CREW NOTED PITCH TRIM 1 FAIL ON EICAS; LOST OF AP; LOST OF PITCH TRIM ON BOTH Y OKES. STANDBY PITCH AT THIS POINT WAS STILL WORKING. UPON DESCENT INTO DFW CREW STILL HAD PREVIOUS ITEMS BUT NOW STAND BY IS NOT WORKING. CREW DECLARED AN EMERGENCY LANDING. LANDED SAFELY. NO FURTHER INCIDENTS WERE REPORTED. REMOVED AN D REPLACED BACK UP PITCH TRIM SWITCH AND HSCU IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT T00011AT 2001042500277 20010425 00277 SO 2001 4 25 20010425AP038 1 20010330 A 2731 9939015 CONTROL UNIT EMB 145 EMB145LR SO PITCH TRIM INOPERATIVE A SIMA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 21 617AE 145093 DFW - FLT 3756 - DURING CRUISE INTO DFW, CREW NOTED PITCH TRIM 1 FAIL ON EICAS; LOST OF AP; LOST OF PITCH TRIM ON BOTH Y OKES. STANDBY PITCH AT THIS POINT WAS STILL WORKING. UPON DESCENT INTO DFW CREW STILL HAD PREVIOUS ITEMS BUT NOW STAND BY IS NOT WORKING. CREW DECLARED AN EMERGENCY LANDING. LANDED SAFELY. NO FURTHER INCIDENTS WERE REPORTED. REMOVED AN D REPLACED BACK UP PITCH TRIM SWITCH AND HSCU IAW AMM. OPS CHECK GOOD. REF SIMA0892. (M) 2 L 7 2 4T RT T00011AT 2001042500278 20010425 00278 SO 2001 4 25 SIMA0698 1 20010310 A 3010 D3899926FA98SN CONNECTOR EMB 145 EMB145 SO ANTI-ICE SYSTEM DAMAGED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 611AE 145074 DFW - FLT 3951 - CREW REPORTED BLEED LEAK 1 AND WING 1 ANTI-ICE FAIL ON EICAS. MAINTENANCE COULD NOT DUPLICATE DISCREPA NCY FOR THE BLEED PROBLEM. GROUND RAN AIRCAFT WITH NO DEFECTS NOTED. MAINTENANCE REMOVED AND REPLACED CANNON PLUG FOR LEFT WING BURST SWITCH. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001042500279 20010425 00279 SO 2001 4 25 SIMA0621 1 20010303 A 3610 S2U3222 SEAL EMB 145 EMB145LR SO NR 2 BLEED LEAKING A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 616AE 145092 DFW - FLT 3593 - DURING CRUISE FLIGHT, CREW REPORTED NR 2 BLEED LEAK. AIRCRAFT WAS RETURNED TO DFW. MAINTENANCE REPLAC ED THE BLEED DUCT SEALS. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001042500280 20010425 00280 SO 2001 4 25 SIMA0841 1 20010324 A 2731 CONTROL UNIT EMB 145 EMB145LR SO PITCH TRIM MALFUNCTIONED A SIMA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SW 21 615AE 145087 ORD - FLT 4225 - CREW REPORTED THE NR 1 PITCH TRIM TO BE INOPERATIVE. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPE RATIONAL CHECK WAS GOOD IAW EMB MM AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001042500281 20010425 00281 SO 2001 4 25 SIMA0835 1 20010324 A 7710 WARNING SYSTEM EMB 145 EMB145LR SO POWER INDICATION MALFUNCTIONED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 643AE 145200 DFW - FLT 3627 - DURING TAKEOFF ROLL AT APPROXIMATELY 10 KNOTS CREW AN ENGINE 1 LOW N1 WARNING. TAKEOFF WAS ABORTED AND AIRCRAFT WAS RETURNED TO THE GATE. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. ENGINE GROUND RUNS WERE PERFORMED IAW EMB MM 71-00-011 WITH NO DEFECTS REPORTED. (M) 2 L 7 2 4T RT T00011AT 2001042500282 20010425 00282 SO 2001 4 25 SIMA0681 1 20010309 A 3150 WARNING SYSTEM EMB 145 EMB145LR SO EICAS ACTIVATED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 608AE 145068 GRR - FLT 4405 - ON TAKEOFF ROLL OF 90 KNOTS HAD EICAS MESSAGE OF REV DISAGREE, RETURNED TO GATE FOR MAINTENANCE. NOTE THE MESSAGE WENT AWAY VERY QUICK. INSPECTOR AND OPS CHECK IAW AMM. COULD NOT DUPLICATE PROBLEM. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001042500283 20010425 00283 EU 2001 4 25 SIMA0641 1 20010305 A 6100 78249052 PCU SAAB SF340 340B 7860101 EU RT ENGINE MALFUNCTIONED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 400BR 340B400 DFW - FLT 3251 - RIGHT PROP WENT TO FEATHER WHEN POWER WAS ADVANCED FOR TAKEOFF, THERE WAS NO TORQUE INDICATION AT THIS POINT. PROP CAME OUT OF FEATHER WHEN THE AUTOCOARSEN WAS TURNED OFF, STILL WITH NO TORQUE INDICATION. RAI RIGHT ENGINE PCU IAW HAMILTON STANDARD MM 61-22-00, OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001042500284 20010425 00284 SO 2001 4 25 SIMA07817 1 20010319 A 7830 ROD EMB 145 EMB145LR SO THRUST REVERSER OUT OF ADJ A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 712AE 145247 ORD - FLT 4230 - DURING TAKEOFF ROLL, CREW NOTED T/REV DISAGREE MSG ON EICAS. CREW ABORTED TAKEOFF AND RETURNED TO GATE SAFELY. NO FURTHER INCIDENTS WERE REPORTED. SYSTEM WAS LATER MEL''D. MAINTENANCE ADJUSTED NR 2 UPPER SHELL ACTUATOR ROD IAW ENGINEERING ORDER EB-78-00-011. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001042500285 20010425 00285 SO 2001 4 25 SIMA0904 1 20010331 A 3350 CONNECTOR EMB 135 EMB135LR SO CABIN LOOSE A SIMA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 21 730KW 145346 ORD - FLT 4421 - CREW REPORTED REAR OVERHEAD EMERGNCY LIGHT INOPERATIVE. RESECURED LOOSE CANNON PLUG ON LIGHT ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT TOOO11AT 2001042500286 20010425 00286 NE 2001 4 25 SIMA0911 2 20010401 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT OVERHEATED A SIMA O OTHER M J OVER TEMP WARNING INDICATION DE DESCENT 1 SW 21 236AE 340B236 JFK - FLT 5192 - ON DESCENT, RIGHT ENGINE RED OVERTEMP LIGHT ILLUMINATED CREW UNABLE TO DETERMINE HOW HIGH THE TEMPERATU RE WENT TO FDR PULLED. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 2001042500287 20010425 00287 SO 2001 4 25 SIMA0915 1 20010401 A 3010 ANTI-ICE SYSTEM EMB 135 EMB135LR SO COCKPIT ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 707EB 145195 ORF - FLT 4973 - CREW REPORTED THAT DURING FLIGHT WHEN ANTI-ICE SYSTEM TURNED ON THEY NOTICED A BURN SMELL IN THE COCKPI T. WHEN THE ANTI-ICE SYSTEM WENT OFF THE SMELL WNT AWAY. (M) 2 L 7 2 4F RT TOOO11AT 2001042500288 20010425 00288 2001 4 25 SIMA0902 4 20010331 A 3418 0861DTS SENSOR EMB 135 EMB135LR SO CABIN FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 737MW 145396 ORD - FLT 4149 - SPS 1 INOPERATIVE, STICK PUSHER FAIL ICAS, SPS ADVANCE FAL ICAS. RETURN TO FIELD ORD. REPLACED LT RT AOA SENSORS. (M) 2 L 7 2 4F RT TOOO11AT 2001042500290 20010425 00290 SO 2001 4 25 SIMA0771 1 20010318 A 4950 4950958 VALVE EMB 135 EMB135LR SO APU INOPERATIVE A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 716AE 145264 ORF - FLT 4971 - CREW REPORTED DURING CLIMB-OUT OF BOS, AN EXHAUST SMELL WAS NOTED IN FLIGHT COMPARTMENT AND IN CABIN. AIRCRAFT WAS LANDED IN ORF WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE APU BLEED VAVLE. O PERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001042500291 20010425 00291 SO 2001 4 25 SIMA0737 1 20010314 A 7830 M83726 RELAY EMB 145 EMB145LR SO THRUST REVERSER FAILED A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 712AE 145247 ORD - FLT 4123 - DURING TAKEOFF ROLL, AFTER 80 KNOTS BUT PRIOR TO Y1 CREW RECEIVED THE NR 2 REVERSER DISAGREE MESSAGE. TAKEOFF WAS ABORTED. MESSAGE CLEARED DURING THE ABORT. MAINTENANCE REPLACED RELAY K0640. OPERATIONAL CHECK WAS GOOD A ND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001042500292 20010425 00292 SO 2001 4 25 SIMA0763 1 20010317 A 2731 362200101 CONTROL UNIT EMB 135 EMB135LR SO HORIZONTAL STAB FAILED A SIMA O OTHER S AFFECT SYSTEMS CL CLIMB 1 SW 21 726AE 145314 ORD - FLT 9754 - AFTER TAKEOFF, WITH PITCH TRIM SET AT +8, THE PILOT ATTEMPTED TO RETRIM. PITCH TRIM MOVED FROM +8 TO + 6 AND THEN FAILED. BACKUP TRIM WORKED NORMAL. MAINTENANCE REMOVED AND REPLACED THE HSCU. OPERATIONAL CHECK WAS GOOD A ND AIRCRAFT WAS RELEASED FOR A FUNCTIONAL CHECK FLIGHT. FCF WAS SATISFACTORY AND WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001042500293 20010425 00293 EU 2001 4 25 SIMA0918 1 20010401 A 5260 S5217640600001 STEP AEROSP ATR72 ATR72212 EU PAX DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE FORTH AND TOP STEP ON PASSENGER DOOR CORRODED. MAINTENANCE REMO VED AND REPLACED THE STEPS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001042500294 20010425 00294 EU 2001 4 25 20010425AP039 1 20010401 A 5260 S5217640600001 STEP AEROSP ATR72 ATR72212 EU PAX DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE FORTH AND TOP STEP ON PASSENGER DOOR CORRODED. MAINTENANCE REMO VED AND REPLACED THE STEPS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0918 (M) 2 H 7 2 4T RT A53EU 2001042500295 20010425 00295 EU 2001 4 25 SIMA0917 1 20010401 A 5210 S5217630120000 SKIN AEROSP ATR72 ATR72212 EU PAX DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE PAX DOOR UPPER INNER SKIN CRACKED AND CORRODED AND THE LOWER PAN CORRODED. MAINTENANCE REPAIRED THE INNER SKIN IAW SRM 52-11-10 FIGURE 411 AND REPAIRED THE LOWER PAN IAW SRM 52-11-00 FIGURE 411. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001042500296 20010425 00296 EU 2001 4 25 20010425AP040 1 20010401 A 5210 S5217620421005 PAN AEROSP ATR72 ATR72212 EU PAX DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE PAX DOOR UPPER INNER SKIN CRACKED AND CORRODED AND THE LOWER PAN CORRODED. MAINTENANCE REPAIRED THE INNER SKIN IAW SRM 52-11-10 FIGURE 411 AND REPAIRED THE LOWER PAN IAW SRM 52-11-00 FIGURE 411. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0917 (M) 2 H 7 2 4T RT A53EU 2001042500297 20010425 00297 EU 2001 4 25 SIMA0905 1 20010331 A 3260 141FL01D3 SWITCH AEROSP ATR72 ATR72212 EU NLG FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 494AE 494 DFW - FLT 3400 - NOSE WHEEL UNLOCK LIGHT ON AFTER GEAR RETRACTION. REMOVED AND REPLACED NOSE LANDING GEAR LIMIT SWITCH IAW AMM. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 2001042500298 20010425 00298 EU 2001 4 25 SIMA09111 1 20010401 A 5753 GUIDE AEROSP ATR72 ATR72212 EU RT FLAP CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING MBV-1 INSPECTION MAINTENANCE REPORTED THE RIGHT INBOARD FLAP NR 4, NR 3, NR 2, NR 1 CAM GUIDES CORRODED, P/ NS S5751204920500, S5751211020400. THE LEFT OUTBOARD FLAP NR 3, NR 2, NR 1 AND LEFT INBOARD FLAP NR 5, NR 4, NR 3, NR 2 , NR 1 CAM GUIDES CORRODED. MAINTENANCE REMOVED AND REPLACED THE CAM GUIDES IAW JIC 57-53-12-RAI-1000-001. AIRCRAFT WA S RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001042500299 20010425 00299 EU 2001 4 25 SIMA0903 1 20010331 A 3260 C245890001 UPLOCK SENSOR AEROSP ATR72 ATR72212 EU LT MLG LEAKING A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 410AT 410 DFW - FLT 3706 - UPON GEAR RETRACTION LEFT MAIN GEAR CYCLED BETWEEN LOCKED AND UNLOCKED POSITION APPROX 9 TIMES WITH LOU D BANGING NOISE ASSOCIATED WITH EACH CYCLED BEFORE LOCKING UP. REMOVED AND REPLACED UPLOCK BOX IAW MM 32-31-00 GEAR RET RACTION AND MEASUREMENT CHECKED GOOD OK FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001050300253 20010503 00253 NM 2001 5 3 01FDEA00278 1 20010416 A 5210 50794577 DOOR FRAME BOEING 727 7272S2F 1384O81 NM ENTRY DOOR GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 215FE 22936 FWD ENTRY DOOR FWD SIDE FRAME GOUGED ON I/B FLANGE 2 INCHES BELOW UPPER LATCH CRANK. *S/D* BLENDED AND REPAIRED DAMAGE PER IAW FEDEX EA 7-5210-54049, SRM 51-10-6. 2 L 7 3 4F A3WE 2001042500300 20010425 00300 NM 2001 4 25 USAASB01084 1 20010322 A 2420 6130200003 HARNESS BOEING 737 737201 1384454 NM NR 1 GENERATOR FAILED A USAA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 EA 19 244US 22752 BOS - FLT 2993 - ON CLIMB-OUT FROM BOS, EN ROUTE TO FLL, THE NR 1 GENERATOR BUS OFF LIGHT ILLUMINATED. CREW TRIED TO RE SET GENERATOR WITH NO HELP. THE APU WAS ALREADY ON MEL SO THE FLIGHT RETURNED TO FIELD AT BOS AND LANDED WITHOUT FURTHR INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REPAIRED THE NR 1 ENGINE GENERATOR FEEDER CABLES AT LEADING EDGE OF LEFT WING, INBOARD SIDE, PER BOEING STANDARD PRACTICE 20-30-13 AND 20-61-19. INSTALLED NEW CABLES AND FIREWALL DISCONNE CT. OPS CHECK GOOD. CLEARED MEL ON APU BY REMOVING AND REPLACING THE APU LOAD STAT (P/N 129552-11). (M) 2 L 7 2 4F A16WE 2001042500301 20010425 00301 NM 2001 4 25 AALA20010611 1 20010321 A 3350 SOCKET BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 608AA 27446 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 5E INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET A T SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001042500302 20010425 00302 NM 2001 4 25 USAA010263 1 20010302 A 5312 BULKHEAD BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND BULKHEAD CRACKED .25 INCH, STATION 178, RBL 10.5, WL 234. REMOVED DAMAGE, INSTALLED DOUBLER. (M) 2 L 7 2 4F A16WE 2001042500303 20010425 00303 NM 2001 4 25 USAA010264 1 20010302 A 5312 BULKHEAD BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND BULKHEAD CRACKED 1 INCH, STATION 178 LBL 7, WL 213.5. REMOVED DAMAGE, INSTALLED DOUBLER. (M) 2 L 7 2 4F A16WE 2001042500304 20010425 00304 NM 2001 4 25 USAA010265 1 20010307 A 5312 BULKHEAD BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND BULKHEAD CRACKED 1 INCH, BS 178, RBL 5.7. REMOVED CRACKED AREA, INSTALLED DOUBLER. (M) 2 L 7 2 4F A16WE 2001042500305 20010425 00305 NM 2001 4 25 AALA20010565 1 20010319 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39367 25194 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 22H INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT CONNE CTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001042500306 20010425 00306 NM 2001 4 25 AALA20010566 1 20010319 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39367 25194 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 23B INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT CONNECT OR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001042500308 20010425 00308 NM 2001 4 25 AALA20010616 1 20010324 A 2810 S343T000340 VALVE BOEING 737 737823 13844BZ NM FUEL CROSS FEED DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 909AN 29511 MIA - FLT 723 - EN ROUTE MIA-MAR, SHORTLY AFTER TAKEOFF FUEL MIGRATED FROM LEFT TANK TO THE RIGHT TANK UN-COMMANDED. RE TURNED MIA AND LANDED WITHOUT FURTHER INCIDENT. REPLACED FUEL CROSS FEED VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION . (M) 2 L 7 2 4F RT A16WE 2001042500309 20010425 00309 WP 2001 4 25 AALA20010572 1 20010322 A 3350 8034001 BATTERY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 400AA 49311 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 4 THROUGH 7 DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042500310 20010425 00310 NM 2001 4 25 USAA010266 1 20010226 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 241US 52896 22443 TPA - FOUND SKIN CRACKED 1 INCH, EQUIPMENT COOLING EXHAUST STATION 380 STRINGER 28L. INSTALLED .100 2024 T3 CLAD DOUBLE R IAW TYPICAL REPAIR 53-30-04. (M) 2 L 7 2 4F A16WE 2001042500311 20010425 00311 NM 2001 4 25 USAA010267 1 20010228 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50584 22757 TPA - FOUND SKIN CRACKED 2.5 INCHES, STATION 951, STRINGER 20L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6. (M) 2 L 7 2 4F A16WE 2001042500312 20010425 00312 NM 2001 4 25 USAA010295 1 20010320 A 5313 STRINGER BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 47321 22962 TPA - FOUND STRINGER CRACKED 1.25 INCH, STRINGER 27, STATION BS 947. INSTALLED PART PER SRM 53-10-3 FIG 1. (M) 2 L 7 2 4F A16WE 2001042500313 20010425 00313 EU 2001 4 25 USAAF01012 1 20010326 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 EA 19 886US 11346 RDU - THE RIGHT SERVICE DOOR EXIT LIGHT WAS INOPERATIVE IN STANDBY AND EMEGENCY LIGHTING. MAINTENANCE REPAIRED TWO BROK EN WIRES ON THE BACK OF THE EXIT LIGHT ASSEMBLY. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT 2001042500314 20010425 00314 EU 2001 4 25 SIMA0622 1 20010303 A 3241 WARNING LIGHT SAAB SF340 340B 7860101 EU ANTI-SKID SYSTEM ILLUMINATED A SIMA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 SW 21 301AE 340B301 DFW - FLT 3769 - ON APPROACH, WHEN GEAR WAS LOWERED CREW RECEIVED AN ANTI-SKID CAUTION INDICATION ON CWP. MAINTENANCE C OULD NOT DUPLICATE DISCREPANCY. OPS CHECK WAS PERFORMED WITH NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001042500315 20010425 00315 NM 2001 4 25 USAA010294 1 20010208 A 5313 STRINGER BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 618AU 47860 22210 CLT - FOUND STRINGER CORRODED 8 INCHES, STATION 1320 AND 1340 RIGHT OF OBL TOP OF STRINGER. REPAIRED PER TYPICAL 53-10- 01 PART B. (M) 2 L 7 2 4F RT A2NM 2001042500316 20010425 00316 NM 2001 4 25 USAA010331 1 20010320 A 5320 INTERCOSTAL BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND INTERCOSTAL CRACKED .5 INCH, BS 1671, RBL 12. FABRICATED NEW ANGLE PER SRM 53-60-51 AND 51-40-00. (M) 2 L 7 2 4F RT A2NM 2001042500317 20010425 00317 NM 2001 4 25 USAA010286 1 20010301 A 5320 INTERCOSTAL BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND INTERCOSTAL CRACKED .5 INCH, BS 1671 AT RBL 12. INSTALLED NEW ANGLE 51-40-00. (M) 2 L 7 2 4F RT A2NM 2001042500318 20010425 00318 NM 2001 4 25 USAA010290 1 20010219 A 5320 PAN BOEING 757 757225 1384959 NM CABIN FLOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND FLOOR PAN CORRODED 12 INCHES BY 12 INCHES, STATION 1716 LBL 7 LBL .5. INSTALLED DOUBLER PER EA 69219. (M) 2 L 7 2 4F RT A2NM 2001042500319 20010425 00319 NM 2001 4 25 USAA010285 1 20010220 A 5320 CHANNEL BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND HAT CHANNEL 2 INCHES BY 4 INCHES, STATION 310 TO STATION 324 RBL 42. INSTALLED NEW HAT CHANNEL SRM 51-30-02 . (M) 2 L 7 2 4F RT A2NM 2001042500320 20010425 00320 NM 2001 4 25 USAA010346 1 20010326 A 5320 STRAP BOEING 757 757225 1384959 NM STABILIZER CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND STABILIZER STRAP CRACKED 2 INCHES, STATION 365 TO STATION 377, RBL 20. REMOVED AND REPLACED STABILIZER STRA P PER SRM 53-10-51. (M) 2 L 7 2 4F RT A2NM 2001042500321 20010425 00321 NM 2001 4 25 USAA010270 1 20010220 A 5300 FRAME BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND 2 SQUARE INCHES OF CORROSION, 4 INCHES ABOVE FORWARD ENTRY DOOR SILL PLATE STATION 377.7. FABRICATED STRAP PER DRAWING 141N8322, SRM 51-20-1. (M) 2 L 7 2 4F RT A2NM 2001042500322 20010425 00322 NM 2001 4 25 USAA010289 1 20010222 A 5320 FLANGE BOEING 757 757225 1384959 NM FUSLEAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND FLANGE CRACKED .5 INCH, STATION 480 AND STATION 500 RBL 9. FABRICATED FLANGE AND INSTALLED PER SRM 53-30-51 . (M) 2 L 7 2 4F RT A2NM 2001042500323 20010425 00323 NM 2001 4 25 USAA010325 1 20010320 A 5313 STRINGER BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND STRINGER CRACKED .5 INCH, STATION 640 PLUS 4 INCHES STRINGER 16L. INSTALLED NEW STRINGER SECTION PER SRM 53 -00-03. (M) 2 L 7 2 4F RT A2NM 2001042500324 20010425 00324 NM 2001 4 25 USAA010330 1 20010320 A 5320 WEB BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND SUPPORT WEB CRACKED 1.3 INCHES, STATION 660, STRINGER 14R. INSTALLED DOUBLER PER SRM 51-70-11. (M) 2 L 7 2 4F RT A2NM 2001042500325 20010425 00325 NM 2001 4 25 USAA010326 1 20010320 A 5320 WEB BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND SUPPORT WEB CRACKED 1.3 INCH, STATION 660, STRINGER 14L. INSTALLED DOUBLER PER SRM 51-70-11. (M) 2 L 7 2 4F RT A2NM 2001042500326 20010425 00326 NM 2001 4 25 USAA010291 1 20010221 A 5320 WEB BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND SUPPORT WEB CRACKED 1.3 INCHES, STATION 660, STRINGER 14L. INSTALLED DOUBLER PER SRM 51-70-11. (M) 2 L 7 2 4F RT A2NM 2001042500327 20010425 00327 NM 2001 4 25 USAA010288 1 20010221 A 5320 WEB BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND SUPPORT WEB CRACKED 1.3 INCHES, STATION 660, STRINGER 14R. INSTALLED DOUBLER. (M) 2 L 7 2 4F RT A2NM 2001042500328 20010425 00328 NM 2001 4 25 USAA010327 1 20010320 A 5320 FRAME BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND FRAME CRACKED .25 INCH, STATION 690 STRINGER 7R. REMOVED DAMAGE INSTALLED DOUBLER, ANGLE RADIUS PER EA 6930 3. (M) 2 L 7 2 4F RT A2NM 2001042500329 20010425 00329 NM 2001 4 25 USAA010328 1 20010320 A 5320 ANGLE BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND OUTER CHORD ANGLE CRACKED 1 INCH, STATION 1300 BETWEEN STRINGER 21L-20L. FABRICATED AND INSTALLED NEW CHORD ANGLE PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 2001042500330 20010425 00330 NM 2001 4 25 USAA010269 1 20010303 A 5347 SEAT TRACK BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND SEAT TRACK CORRODED 1 INCH BY 1 INCH, INBOARD FLANGE RBL 24 STATION 1320. INSTALLED NEW SEAT TRACK AND DOUB LER. (M) 2 L 7 2 4F RT A2NM 2001042500331 20010425 00331 NM 2001 4 25 USAA010281 1 20010216 A 5320 INTERCOSTAL BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND INTERCOSTAL CRACKED 2 INCHES, STATION 1320 LBL 45. REMOVED AND REPLACED 52-60-51. (M) 2 L 7 2 4F RT A2NM 2001042500332 20010425 00332 NM 2001 4 25 USAA010333 1 20010320 A 5320 ANGLE BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND ANGLE CRACKED .25 INCH, STATION 1320 CABIN FLOOR SUPPORT. FABRICATED AND INSTALLED PER BOEING DWG 140N2502. (M) 2 L 7 2 4F RT A2NM 2001042500333 20010425 00333 NM 2001 4 25 USAA010334 1 20010320 A 5320 INTERCOSTAL BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND INTERCOSTAL CRACKED 2 INCHES, STATION 1320, LBL FLOOR. FABRICATED NEW WEB PER REPAIR DOCUMENT 52-60-51. (M ) 2 L 7 2 4F RT A2NM 2001042500334 20010425 00334 NM 2001 4 25 USAA010282 1 20010216 A 5320 ANGLE BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND ANGLE CRACKED .25 INCH, STATION 1320 CABIN FLOOR. FABRICATED NEW ANGLE PER BOEING DRAWING 140N2502. (M) 2 L 7 2 4F RT A2NM 2001042500335 20010425 00335 NM 2001 4 25 USAA010283 1 20010216 A 5320 INTERCOSTAL BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND INTERCOSTAL CRACKED .5 INCH, STATION 1320-1340 BL 0 UPPER CHORD. INSTALLED WEB FILLER. (M) 2 L 7 2 4F RT A2NM 2001042500336 20010425 00336 NM 2001 4 25 USAA010332 1 20010320 A 5320 INTERCOSTAL BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND INTERCOSTAL CRACKED .5 INCH, STATION 1320-1340, BL 0 UPPER CHORD. INSTALLED WEB AND FILLER PER SRM 51-00-10 AND 53-60-51. (M) 2 L 7 2 4F RT A2NM 2001042500337 20010425 00337 NM 2001 4 25 USAA010262 1 20010204 A 5312 BULKHEAD BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND PRESSURE BULKHEAD CRACKED 6.5 INCHES, BS 1016 PLUS 1 AT STRINGER 6L. INSTALLED FILLER, DOUBLER AND SHIMS. (M) 2 L 7 2 4F A16WE 2001042500338 20010425 00338 NM 2001 4 25 USAA010296 1 20010320 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 50739 22881 TPA - FOUND SKIN CRACKED .75 INCH, LOWER HINGE BETWEEN STRINGER 9 AND 10 RT AFT STATION 947. INSTALLED DOUBLER PER SRM 53-30-3 FIG 33. (M) 2 L 7 2 4F A16WE 2001042500339 20010425 00339 NM 2001 4 25 USAA010298 1 20010320 A 5320 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND TIE CLIP CRACKED .5 INCH, TIE CLIP STATION 663, STRINGER 10L. REPLACED WITH NEW PART PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2001042500340 20010425 00340 NM 2001 4 25 USAA010299 1 20010320 A 5320 STIFFENER BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND CORROSION ON CHANNEL STIFFENER 6 FEET, FORWARD LOWER SIDE AFT BULKHEAD AFT STATION 1016, BL 0. INSTALLED DO UBLER AND REPAIR ANGLES PER EA 69123. (M) 2 L 7 2 4F A16WE 2001042500341 20010425 00341 NM 2001 4 25 USAA010300 1 20010320 A 5312 BULKHEAD BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND HORIZ WEB CRACKED 1 INCH, BS 178 BULKHEAD, WL 207, RBL 29. REMOVED AND REPLACED WEB PER EO 5300V157. (M) 2 L 7 2 4F A16WE 2001042500342 20010425 00342 NM 2001 4 25 USAA010347 1 20010326 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND SKIN CRACKED 5 INCHES, STATION 727A PLUS 16 INCHES ABOVE STRINGER 17L. INSTALLED FILLER AND DOUBLER PER EA 69166. (M) 2 L 7 2 4F A16WE 2001042500343 20010425 00343 NM 2001 4 25 USAASB01094 1 20010329 A 3350 6013211 POWER SUPPLY BOEING 737 737201 1384454 NM CARGO BAY FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 265AU 22962 BOS - PILOT REPORTED THAT THE AFT LEFT AND AFT RIGHT EMERGENCY ESCAPE SLIDE LIGHTS WERE INOPERATAIVE. MAINTENANCE REMOV ED AND REPLACED THE POWER SUPPLY AND THE BATTERY PACK (P/N 61-0478-9). OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 2001042500344 20010425 00344 EU 2001 4 25 USAAF01006 1 20010219 A 3350 59257 INVERTER FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 869US 11314 IND - MAIN ENTRANCE DOOR, SERVICE DOOR AND GALLEY AISLE FLOOR PROXIMITY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED I NVERTER A AND THE OUTBOARD MARKER LIGHT ASSEMBLY. OPS CHECKED OK. (M) 2 L 7 2 4F RT 2001042500345 20010425 00345 EU 2001 4 25 USAAF01011 1 20010324 A 3350 59257 INVERTER FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 851US 11278 IND - A SECTION OF THE RIGHT FORWARD OVERWING LOW LEVEL EMERGENCY LIGHTS, AND A SECTION OF THE LEFT AFT OVERWING LOW LEV EL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED AN INVERTER. OPS CHECKED OK. (M) 2 L 7 2 4F RT 2001042500346 20010425 00346 NM 2001 4 25 USAA010329 1 20010320 A 5320 STRAP BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND STRAP CRACKED 2 INCHES, STATION 1380, RBL 46. REPAIR PLATE PER SRM 53-10-51. (M) 2 L 7 2 4F RT A2NM 2001042500348 20010425 00348 NM 2001 4 25 USAA010287 1 20010219 A 5320 WEB BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND WEB CRACKED .5 INCH, STATION 1661-1681, RBL 10.5. INSTALLED NEW WEB 53-60-51. (M) 2 L 7 2 4F RT A2NM 2001042500349 20010425 00349 NM 2001 4 25 USAA010324 1 20010320 A 5313 STRINGER BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 618AU 47860 22210 CLT - FOUND STRINGER CORRODED 8 INCHES, BETWEEN STATION 1320/1340. REPAIR ANGLES PER TR 53-10-01 PART B. (M) 2 L 7 2 4F RT A2NM 2001042500350 20010425 00350 NM 2001 4 25 USAA010293 1 20010302 A 5320 ANGLE BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 618AU 47860 22210 CLT - FOUND TRANSITION ANGLE CORRODED 20 INCHES, STATION 1340 STATION 1360 WS 27R. REPAIRED PER SRM 51-40-02. (M) 2 L 7 2 4F RT A2NM 2001042500351 20010425 00351 NM 2001 4 25 USAASB01090 1 20010327 A 5210 DOOR BOEING 737 7373B7 1384580 NM PAX NOT CLOSED A USAA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 EA 19 520AU 23706 PWM - FLT 2271 - ON CLIMB-OUT FROM PWM, THE A/C WOULD NOT PRESSURIZE. CREW ASSUMED IT WAS A MALFUNCTION OF THE PRESSURI ZATION SYSTEM SINCE THERE WAS NO DOOR WARNING LIGHT INDICATION. AT 4,000 FEET, CAPTAIN ELECTED TO RETURN TO FIELD AT PW M. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND WITH NO EMERGENCY BEING DECLARED. ONCE PARKED, CAPTAIN WAS INFORMED BY F LIGHT ATTENDANT THAT THE AFT RIGHT SERVICE DOOR APPEARED TO BE AJAR. CAPTAIN RECYCLED DOOR WHILE IN COMMUNICATION WITH FIRST OFFICER IN COCKPIT. DOOR WARNING INDICATOR LIGHTS OPERATED NORMALLY AND DOOR APPEARED TO SEAL PROPERLY. MX CONFI RMED THAT THE AFT RIGHT SERVICE DOOR WAS NOT LATCHED AND FULLY CLOSED. CYCLED AFT RIGHT SERVICE DOOR AND CONFIRMED DOOR 2 L 7 2 4F RT A16WE 2001042500352 20010425 00352 NM 2001 4 25 USAASB01091 1 20010327 A 2530 5000387D4 COFFEEMAKER BOEING 737 737301 1384611 NM FWD GALLEY SHORTED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 346US 14775 23515 MIA - FLT 1191 - EN ROUTE FROM CLT-MIA, FLIGHT ATTENDANT REPORTED A SCORCHING SMELL IN THE FORWARD GALLEY APPROXIMATELY TEN MINUTES BEFORE LANDING AT MIA. OVENS WERE NOT IN USE AT THE TIME. COFFEE MAKER CIRCUIT BREAKERS WERE ALL PULLED AN D GALLEY POWER WAS TURNED OFF. SMELL DISSIPATED IMMEDIATELY. FLIGHT LANDED AT MIA WITHOUT FURTHER INCIDENT. MAINTENAN CE COULD NOT FIND ANY BURNING SMELL IN FORWARD GALLEY. REPLACED FORWARD GALLEY NR 1 COFFEE MAKER AS PRECAUTIONARY. (M) 2 L 7 2 4F RT A16WE 2001042500353 20010425 00353 NE 2001 4 25 USAASB01085 2 20010322 A 7532 2760000101 BLEED VALVE BOEING 737 737201 1384454 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE FAULTY A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 243US 22445 LGA - FLT 2721 - ON TAKEOFF FROM LGA, EN ROUTE TO FLL, THE AUTO THROTTLE DISENGAGED AND THE NR 1 ENGINE EPR PULLED BACK TO 1.88. THERE WAS NO RESPONSE TO THROTTLE MOVEMENT. CONDITIONS WERE A BLEEDS-OFF NON-PRESSURIZED TAKEOFF. THEN ON CL IMB-OUT, AFTER BLEED RECONFIGURATION, A LOUD BANG WAS HEARD. A MINUTE LATER, FLIGHT ATTENDANT REPORTED TO CREW OF SMOKE IN THE MID CABIN. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT LGA. FLIGHT LANDED WITHOUT FURTHER INCIDENT AS SMOKE DISSIPATED. MAINTENANCE ACCOMPLISHED A FULL POWER RUN-UP OF BOTH ENGINES AS PER MM 71-09-231. ALL THROTTLE MOVEM ENTS AND EPR INDICATIONS WERE NORMAL. HOWEVER, MAINTENANCE FOUND THE NR 2 ENGINE 13TH STAGE BLEED VALVE HUNG UP AND SLO 2 L 7 2 4F 4 F A16WE E2EA 2001042500354 20010425 00354 NM 2001 4 25 USAASB01088 1 20010326 A 3230 MODULE BOEING 737 7372B7 1384560 NM MLG MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 285AU 23132 FLL - FLT 2719 - AFTER TAKEOFF FROM FLL, THE LANDING GEAR WOULD NOT RETRACT. FLIGHT RETURNED TO FIELD AT FLL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE RERACKED THE LANDING GEAR ACCESSORY MODULE. ACCOMPL ISHED MAIN LANDING GEAR SAFETY SENSOR CHECK PER MM 32-09-200. CHECKS OK PER MM. (M) 2 L 7 2 4F A16WE 2001042500355 20010425 00355 NM 2001 4 25 USAA010261 1 20010305 A 5312 BULKHEAD BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND BULKHEAD WEB CRACKED .125 INCH, BS 178, RBL 5, WL 189, 190 AND 191.5. REMOVED DAMAGE INSTALLED DOUBLER PER EA 69132. (M) 2 L 7 2 4F A16WE 2001042500356 20010425 00356 WP 2001 4 25 AALA20010586 1 20010325 A 3350 SOCKET DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 561AA 53091 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 4E DIM. REPLACED EMERGENCY EXIT LIGHT SOCKET AT SEAT 4 E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042500357 20010425 00357 WP 2001 4 25 UPS01835644 1 20010331 A 5320 37503491 STRAP DOUG DC8 DC871F 302199D WP CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 STA. 465 STRAP IN MIDDLE OF LONG. 33R IS CRACKED REMOVED,FABRICATED,AND REPLACED STRAP I.A.W. DWG. 3750349,AND SRM. 51-1-20D,51-1-21 2 L 7 4 4F RT 4A25 2001042500358 20010425 00358 WP 2001 4 25 UPS01835645 1 20010328 A 5320 3755843501N FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 STA. 1150 BETWEEN LONG. 35R-34R BATHTUB FITTING IS CRACKED REMOVED AND REPLACED FITTING I.A.W. DWG. 3755843,AND SRM. 53-2-0 FIG. 2D 2 L 7 4 4F RT 4A25 2001042500359 20010425 00359 WP 2001 4 25 UPS01835646 1 20010326 A 5320 9754022503N FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 STA. 280 LOWER FLOORBEAM TO CUSP FITTING IS CRACKED AT LONG. 21R REMOVED AND REPLACED FITTING I .A.W. DWG. 9754022,AND SRM. 51-1-20D,& 51-1-21 2 L 7 4 4F RT 4A25 2001042500360 20010425 00360 WP 2001 4 25 UPS01835647 1 20010328 A 5314 KEELBEAM DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 LT. KEEL BEAM WEB IS CRACKED AT STA. 879. REPAIRED WEB I.A.W. SRM. 53-2-0 FIG. 23 2 L 7 4 4F RT 4A25 2001042500361 20010425 00361 WP 2001 4 25 UPS01835648 1 20010327 A 5340 37558272N FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 STA. 280 BANANA FITTING IS CRACKED AT LONG. 33R REMOVED AND REPLACED FITTING I.A.W. DWG.3755827 ,AND SRM. 51-1-20D 2 L 7 4 4F RT 4A25 2001042600001 20010426 00001 WP 2001 4 26 AALA016025 1 20010301 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP ROWS 17-20 DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 754RA 49641 CCI-LAX - SEAT MOUNTED EMERGENCY EXIT LIGHTS AT ROWS 17, 18, 19 AND 20 NOT WORKING. INSTALLED NEW BATTERY PACK, ALL EME RGENCY LIGHTS WORK OK. (M) 2 L 7 2 4F RT A6WE 2001042600002 20010426 00002 WP 2001 4 26 AALA016026 1 20010306 A 3350 6011779 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 834RA 53124 EMERGENCY EXIT LIGHTS 4 ROWS ON THE RIGHT SIDE ARE E N, EMERGENCY EXIT SIGN AT TAIL CONE DOOR IS ALSO ON. REPLACED POWE R SUPPLY FOR ASSOC ROWS, PERFORMED OPS CHECKS. OPS CHECKS OK PER MM. (M) 2 L 7 2 4F RT A6WE 2001042600003 20010426 00003 WP 2001 4 26 AALA016027 1 20010228 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP AFT EXIT LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 871RA 49788 LAX-CCI - EMERGENCY LIGHT AT SEATS 28D, 29D AND 30D AND AFT EXIT INOPERATIVE WHEN TESTING. REPLACED BAT5014 AT SEAT 29D . NO HELP. REPLACED BATTERY PACK ASY AT AFT EXIT LIGHT. LIGHTS TESTED OK. (M) 2 L 7 2 4F RT A6WE 2001042600004 20010426 00004 WP 2001 4 26 AALA016028 1 20010312 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN FAILED A K NONE L NO TEST IN INSP/MAINT 1 SW 21 871RA 49788 LAX - MAINTENANCE ENTRY, EMERGENCY FLOOR LIGHT ROWS 24 TO REAR INOPERATIVE. CHECKED ALL WIRING AT SEAT 29DEF, CHECKS NO RMAL. REMOVED PLACARD CLEARED MIC. (M) 2 L 7 2 4F RT A6WE 2001042600005 20010426 00005 NM 2001 4 26 USAASB01093 1 20010329 A 3350 20131A BATTERY PACK BOEING 737 737301 1384611 NM FWD CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 576US 23741 LGA - MAINTENANCE FOUND THE FORWARD ENTRY DOOR EMERGENCY EXIT LIGHTS WEAK. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001042600006 20010426 00006 NM 2001 4 26 USAASB01092 1 20010329 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM MID CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 531AU 24478 GSO - MAINTENANCE FOUND THE EXTERIOR OVERWING EMERGENCY EXIT LIGHT, RIGHT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND RE PLACED THE BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001042600007 20010426 00007 NM 2001 4 26 USAASB01087 1 20010325 A 3350 20131A BATTERY PACK BOEING 737 737301 1384611 NM FWD CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 590US 23935 CLT - PILOT REPORTED THAT NUMEROUS EMERGENCY EVACUATION LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE ASSOCITED BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001042600008 20010426 00008 NM 2001 4 26 USAASB01080 1 20010318 A 2701 CONTROL COLUMN BOEING 737 737201 1384454 NM COCKPIT SEIZED A USAA L ABORTED APPROACH F FLT CONT AFFECTED DE DESCENT 1 EA 19 248US 22755 LGA-PBI - FLT 2693 - DURING A DESCENDING TURN THE CONTROL COLUMN SEIZED. NEITHER THE CAPTAIN NOR THE FIRST OFFICER COUL D MOVE THE CONTROL COLUMN FOR SEVERAL SECONDS. AFTER A GO-AROUND THE AIRCRAFT LANDED WITHOUT INCIDENT. (M) 2 L 7 2 4F A16WE 2001042600009 20010426 00009 NM 2001 4 26 AALA20010403 1 20010311 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 608AA 27446 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 30 DAMAGED. REPLACED EMERGENCY EXIT LIGHT STRIP AT ROW 30. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001042600010 20010426 00010 NM 2001 4 26 AALA20010404 1 20010312 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 329AA 22329 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 35B INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT CONNE CTOR AT SIDE WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001042600011 20010426 00011 NM 2001 4 26 AALA20010397 1 20010310 A 3350 PIN BOEING 767 767223 1385123 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 315AA 22317 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 22B INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT CONNECT OR PIN AT SIDE WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001042600012 20010426 00012 NM 2001 4 26 AALA20010574 1 20010322 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 647AM 24605 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 15 THROUGH 23 DIM. ACCOMPLISHED OPS CHECK PER THE MM. NO FAULTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001042600013 20010426 00013 NM 2001 4 26 AALA20010588 1 20010324 A 3350 LAMP BOEING 777 777223 1385213 NM CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 784AN 29588 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 9G DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 9G. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001042600014 20010426 00014 NM 2001 4 26 AALA20010589 1 20010324 A 3350 P4010049 BATTERY BOEING 767 767223 1385123 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 336AA 22334 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ILGHT AT ROW 2 THROUGH 10 DIM. REPLCED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001042600015 20010426 00015 NM 2001 4 26 AALA20010592 1 20010322 A 3350 LAMP BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 636AM 24594 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 5E TOO BRIGHT. REPLACED EMERGENCY EXIT LIGHT AT SEAT 5 E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001042600016 20010426 00016 NM 2001 4 26 AALA20010594 1 20010320 A 3350 LIGHT BOEING 777 777223 1385213 NM R1 DOOR BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 770AN 29578 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT R1 DOOR BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT R 1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001042600017 20010426 00017 NM 2001 4 26 AALA20010598 1 20010325 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 693AA 26973 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 31D INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT CONNE CTOR AT SEAT 31D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001042600018 20010426 00018 NM 2001 4 26 AALA20010602 1 20010324 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 692AA 26972 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT CONNECTOR. SYSTE M GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001042600019 20010426 00019 NM 2001 4 26 AALA20010609 1 20010321 A 3350 CONNECTOR BOEING 757 757223 1384957 NM L2 DOOR DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 665AA 25299 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L2 DOOR INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT CONNECTOR AT L2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001042600020 20010426 00020 NM 2001 4 26 AALA20010610 1 20010321 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 355AA 24036 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 26 A/B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSE MBLY AT SEAT 26 A/B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001042600021 20010426 00021 NM 2001 4 26 AALA20010423 1 20010306 A 5310 DOUBLER BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 894AA 22010 TUL - FOUND DOUBLER CORRODED STATION 294 RIGHT SIDE OF DOGHOUSE UPPER CHORD. REMOVED AND REPLACED DOUBLER (RADIUS FILLE R BLOCK) ON UNDER SIDE OF PREVIOUSLY INSTALLED REPAIR ANGLE 7075-T6 .250 .75 INCH WIDE BY 6 INCHES LONG. RE-INSTALLED E XISTING FASTENERS PER SRM 51-40-4 PAGE 2. (M) 2 L 7 3 4F A3WE 2001042600022 20010426 00022 NM 2001 4 26 AALA20010422 1 20010312 A 5511 SPAR BOEING 727 727223 1384074 NM HORIZONTAL STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 894AA 22010 TUL - FOUND CORROSION ON LEFT HORIZONTAL STAB AFT SPAR ON TOP APPROX 15 INBOARD OF ELEVATOR PCU. REPAIRED AREA PER ESO 11697 DATED 3-7-2001. (M) 2 L 7 3 4F A3WE 2001042600023 20010426 00023 NM 2001 4 26 AALA20010419 1 20010309 A 5310 DOOR FRAME BOEING 727 727223 1384074 NM CARGO BAY CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 894AA 22010 TUL - FOUND FORWARD CARGO DOOR CRACKED AFT FRAME STATION 620 AT SERVICE LIGHT SWITCH CUTOUT. REPAIRED CRACK IN FRAME WE B STATION 620 FORWARD DOOR CUTOUT PER SRM 51-40-2 FIG 1. (M) 2 L 7 3 4F A3WE 2001042600024 20010426 00024 NM 2001 4 26 AALA20010433 1 20010221 A 5310 STRUCTURE BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 861AA 21088 TUL - FOUND CORROSION AROUND FASTENER AT BS 950D STRINGER 29R. INSTALLED STRAP PER ESO 11697 2-21-2001. (M) 2 L 7 3 4F A3WE 2001042600026 20010426 00026 WP 2001 4 26 AALA20010535 1 20010310 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND EDGE OF LEFT AFT EMERGENCY EXIT DOOR CUTOUT AREA WORN ON INBOARD SIDE, LOWER EDGE BS 916. INSTALLED DOUBLER PER ESO 80559, DATD 3-9-2001. (M) 2 L 7 2 4F A6WE 2001042600027 20010426 00027 WP 2001 4 26 AALA20010536 1 20010310 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND SEVERAL AREAS OF CORROSION ON CUSP FROM STATION 630 TO STATION 710. INSTALLED NEW CUSP SHEET FROM STATION 5 98 TO 712 PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2001042600028 20010426 00028 WP 2001 4 26 AALA20010585 1 20010325 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 561AA 53091 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 9D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 9D. SYS TEM GROUND HECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600029 20010426 00029 WP 2001 4 26 AALA20010584 1 20010325 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 561AA 53091 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 13D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 13D. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600030 20010426 00030 WP 2001 4 26 AALA20010583 1 20010325 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 561AA 53091 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 10D DIM. REPLACED EMERGENCY EXIT LIGHT AT SET 10D. SY STEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600031 20010426 00031 NM 2001 4 26 AT0100119 1 20010311 A 5330 SKIN BOEING 737 737284 138448R NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 470AT 21501 FOUND AFT LAV SERVICE PANEL SKIN AT BS 976-1006 CORRODED BEYOND LIMITS. INSTALLED REPAIR IAW B737 53-10-03 FIG 1 AND 53 -10-02 FIG 9. 2 L 7 2 4F A16WE 2001042600032 20010426 00032 NM 2001 4 26 F3LA200100052 1 20010405 A 2133 OUTFLOW VALVE BOEING 737 737228 13844AG NM CABIN PRESSURE OBSTRUCTED A F3LA G A O2 MASK DEPLOYED UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 234TR 23004 AIR TURNBACK. FLT CREW REPORTED PRESSURIZATION NORMAL THROUGH 10,000 FT ACFT WENT TO STANDBY MODE AND CABIN PRESSURE CONTINUED TO CLIMB. SET STANDBY MODE AT 5.6 PSI AND CABIN STILL CONTINUED TO CLIMB. MANUALLY CLOSED OUTFLOW VALVE AND SUBSEQUENTLY OXYGEN MASKS DEPLOYED. RETURNED TO MDW AND LANDED WITHOUT INCIDENT. MX INSPECTED ACFT AND FOUND A 12 INCH PIECE OF INSULATION PROTRUDING FROM OUTFLOW VALVE. REMOVED INSULATION, PERFORMED CABIN LEAKAGE TEST PER MM 5-51-91, PG 202 AND CHECKED OK. ACFT WAS FERRIED TO DEN FOR MAINTENANCE AND TO RESTOW OXYGEN MASKS. UPON ARRIVAL IN DEN, OXYGEN M ASKS WERE RESTOWED, PASSENGER OXYGEN BOTTLE WAS REPLACED, A SERVICE CHECK WAS ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001042600033 20010426 00033 CE 2001 4 26 GLBA2001077 1 20010403 A 2120 UNKNOWN BEECH 1900 1900D 1154162 CE CABIN ODOR A GLBA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CE 01 211UX UE211 BURNING ODOR REPORTED. INSPECTED CND. 2 L 7 2 4T RT A24CE 2001042600034 20010426 00034 EA 2001 4 26 JBXA000262 1 20010406 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 EA MLG OUT OF ADJ A JBXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 05 590ML 7385 GEAR DISAGREE MSG WHEN GEAR SELECTED UP. FOUND MLG UPLOCK PROXIMITY SENSOR AND TARGET OUT OF RANGE. ADJUSTED MLG UPLOC K PROX SENSOR RT IAW AMM 32-61-05 OPS CHECK GOOD. OPS CHECK GOOD OF PROX SYSTEM IAW AMM 32-61-00. 2 L 7 2 4F RT A21EA 2001042600035 20010426 00035 SO 2001 4 26 C2XA01IA196 1 20010404 A 2120 12007740007 HOSE EMB 120 EMB120ER 3260203 SO ACM LOOSE A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 15725 120173 IAH - FLIGHT 3454, THE CREW REPORTED SMOKE IN THE CABIN SHORTLY AFTER DEPARTURE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE RESECURED A LOOSE HOSE ON THE LEFT HAND AIR CYCLE MACHINE, AND THE AIRCRAFT WAS AP PROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001042600036 20010426 00036 NM 2001 4 26 01FDEA00256 1 20010406 A 2613 CONTROL UNIT BOEING 727 727225 1384077 NM NR 3 ENGINE FAULTY A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SO 25 461FE 22548 LWR AFT BODY O/H LIGHT CAME ON. TURN OFF R/PACK AND NR 3 ENG BLD AND O/H LIGHT WENT OUT. REMOVED AND REPLACED CONTROL UNIT PER 727-200 MM 26-14-000-1. RAN A/C ENG 3 PER JET RUN HDBK. NO O/H LIGHT. OPS CK GOOD. 2 L 7 3 4F A3WE 2001042600037 20010426 00037 NM 2001 4 26 USAASB01086 1 20010323 A 2120 655447015 DUCT BOEING 737 737201 1384454 NM A/C BAY FAILED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 243US 22445 PBI - FLT 2990 - EN ROUTE FROM LGA TO PBI, APPROXIMATELY ONE HOUR INTO FLIGHT, THE FLIGHT ATTENDANT ADVISED THE CREW OF AN ELECTRICAL SMELL IN MID-CABIN. CREW COOLED DOWN CABIN AND SMELL DISSIPATED. FLIGHT ATTENDANT ADVISDED THAT ONLY A F AINT ODOR REMAINED. FLIGHT CONTINUED AND LANDED AT PBI WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. S/D - MAI NTENANCE REMOVED AND REPLACED THE DUCT ASSEMBLY (P/N 65-54467-1) AND THE LEFT SIDE MIX CHAMBER DUCT ASSEMBLY IN THE AIR CONDITIONING DISTRIBUTION BAY. ALSO, REMOVED AND REPLACED BOTH THE LEFT AND RIGHT WATER SEPARATOR BAGS (P/N V121-1) PER MM. RAN BOTH PACKS AND LEAK CHECKED. NO LEAKS NOTED. (M) 2 L 7 2 4F A16WE 2001042600038 20010426 00038 NM 2001 4 26 01FDEA00261 1 20010407 A 5347 SEAT TRACK BOEING 727 72722 1384002 NM CABIN CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 168FE 18865 DURING ROUTINE INSP, FWD LWR CARGO BIN LT SEAT TRACK FOUND CORRODED AT BS 680. REMOVED, REPLACED AND FAB PER IAW BAC 72 7 SRM 53-10-5. 2 L 7 3 4F A3WE 2001042600039 20010426 00039 NM 2001 4 26 01FDEA00263 1 20010406 A 5520 PLATE BOEING 727 72725C 138400H NM RT ELEVATOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 124FE 19360 DURING ROUTINE INSP, RT ELEVATOR REAR SPAR NR 4 SHEAR PLATE FOUND CRACKED. REMOVED, REPLACED AND FAB PER IAW BAC 727 SR M 51-20-2, 51-30-2. 2 L 7 3 4F A3WE 2001042600041 20010426 00041 NM 2001 4 26 01FDEA00265 1 20010406 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM CABIN CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 124FE 19360 DURING ROUTINE INSP, NR 2 SEAT TRACK FOUND CORRODED BS 610. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 53-10-5. 2 L 7 3 4F A3WE 2001042600042 20010426 00042 NM 2001 4 26 SWAA010937 1 20010327 A 5330 65C35775 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED C4 CHECK, FOUND 2 LONG EXTERNAL FUSELAGE SKIN CRACK AT BS 727D, STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001042600043 20010426 00043 NM 2001 4 26 SWAA010920 1 20010326 A 5330 65C33756 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 312, STR 20R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001042600044 20010426 00044 NM 2001 4 26 SWAA010929 1 20010327 A 3260 6546990 MODULE BOEING 737 7372H4 138448C NM COCKPIT ERRATIC A SWAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 068SW 22357 DIVERSION, DURING LANDING GEAR RETRACTION, THE GEAR RED INDICATOR LIGHTS ILLUMINATED, AURAL WARNING SOUNDED AND REMAINED ON UNTIL FLAPS WERE RETRACTED. CYCLED GEAR AND 3 GREEN AND 3 RED LIGHTS ILLUMINATED. CYCLED GEAR AGAIN AND RED LIGHTS EXTINGUISHED. REMOVED AND REPLACED LANDING GEAR MODULE PER MM, OPS CHECK GOOD. 2 L 7 2 4F A16WE 2001042600045 20010426 00045 NM 2001 4 26 SWAA010946 1 20010329 A 5312 6516300 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD VERTICAL CHORD RADIUS CRACKED AT RBL 6, WL 184. REPAIRED BULKHEAD VERTI CAL CHORD PER SRM. 2 L 7 2 4F A16WE 2001042600046 20010426 00046 NM 2001 4 26 SWAA010947 1 20010329 A 5320 6515198 SPLICE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND STR 14R SPLICE CRACKED AT BS 540. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F A16WE 2001042600047 20010426 00047 NM 2001 4 26 SWAA010948 1 20010329 A 5315 6546804 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 360, LBL 11 TO RBL 65. REPAIRED FLOORBEAM UPPER CH ORD PER BFG ER. 2 L 7 2 4F A16WE 2001042600048 20010426 00048 NM 2001 4 26 SWAA010949 1 20010329 A 5315 6546804 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 947, LBL 48. REPAIRED FLOORBEAM UPPER CHORD PER BFG ER. 2 L 7 2 4F A16WE 2001042600049 20010426 00049 NM 2001 4 26 SWAA010950 1 20010328 A 5330 6545769 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BL 0, BS 444 TO BS 447. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001042600050 20010426 00050 NM 2001 4 26 SWAA010951 1 20010329 A 5310 6546550 DOOR FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR FWD FUSELAGE FRAME CRACKED AT BS 794, RBL 29. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2001042600051 20010426 00051 NM 2001 4 26 SWAA010952 1 20010329 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 727B+12, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001042600052 20010426 00052 NM 2001 4 26 SWAA010954 1 20010329 A 5743 6567172 FITTING BOEING 737 7372H4 138448C NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED D-CHECK, FOUND LT MLG AFT STABILIZER BEAM FITTING CORRODED. REMOVED AND REPLACED BEAM FITTING PER MM. 2 L 7 2 4F A16WE 2001042600053 20010426 00053 NM 2001 4 26 SWAA010955 1 20010328 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 378SW 26585 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED AT RBL 1, WL 218. REPAIRED BULKHEAD WEB PER SRM. 2 L 7 2 4F RT A16WE 2001042600055 20010426 00055 NM 2001 4 26 SWAA010957 1 20010329 A 5753 6546435 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 624SW 27934 DURING SCHEDULED 1/2D CHECK, FOUND RT WING OUTBD T/E AFT FLAP SKIN DELAMINATED ON LOWER SIDE, 6 OUTBD FROM INBD END. RE MOVED AND REPLACED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2001042600056 20010426 00056 2001 4 26 SWAA010959 4 20010328 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM ENTRY DOOR OUT OF TOLERANCE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 512SW 24189 DURING SCHEDULED RON CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVA C SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001042600057 20010426 00057 NM 2001 4 26 SWAA010961 1 20010329 A 5523 183A8410 BUSHING BOEING 737 7377H4 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 762SW 27876 DURING SCHEDULED A2 CHECK (SWA SI 11038-55), FOUND RT ELEVATOR TAB OUTBD HINGE FITTING HAS EXCESSIVE PLAY. REMOVED AND REPLACED ELEVATOR TAB BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2001042600058 20010426 00058 NM 2001 4 26 SWAA010962 1 20010329 A 5542 173A0100 SKIN BOEING 737 7377H4 NM RUDDER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 762SW 27876 DURING SCHEDULED A2 CHECK, FOUND 12 X 6 DELAMINATION ON RUDDER, LT SIDE, 35 ABOVE BOTTOM, 12 AFT OF L/E. MX FERRIED AIR CRAFT TO HOU. REMOVED AND REPLACED RUDDER PER MM. 2 L 7 2 4F RT A16WE 2001042600059 20010426 00059 2001 4 26 SWAA011033 4 20010404 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001042600060 20010426 00060 NM 2001 4 26 SWAA010963 1 20010329 A 2131 7638102 CONTROLLER BOEING 737 7373H4 1384600 NM CABIN PRESSURE LOOSE A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 339SW 24090 AIR TURNBACK, CABIN CLIMBED NORMAL TO 1000 FT THEN ABRUPTLY CLIMBED AND RETURNED TO NORMAL. AT 15,000 FT, CABIN DEPRESS URIZED, NO HELP IN STANDBY OR NORMAL MODE. FOUND CABIN PRESS CONTROLLER LOOSE IN RACK. SECURED CONTROLLER AND PRESSURI ZED AIRCRAFT PER MM. OPS CHECK GOOD. PERFORMED PACK CONFIDENCE CHECK PER SWA SAM 728. 2 L 7 2 4F RT A16WE 2001042600061 20010426 00061 NM 2001 4 26 SWAA011017 1 20010330 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED LAP JOINT MODIFICATION, FOUND APPROX 5 EXTERNAL FUSELAGE SKIN CRACK BETWEEN BS 500 & BS 500A, STR 4L. REPAIRED SKIN PER SWA ACO. 2 L 7 2 4F A16WE 2001042600062 20010426 00062 NM 2001 4 26 SWAA010968 1 20010330 A 5311 6516301 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME LOWER CHORD CRACKED AT BS 188, RBL 31. REPAIRED FRAME CHORD PER SRM. 2 L 7 2 4F A16WE 2001042600063 20010426 00063 NM 2001 4 26 SWAA010977 1 20010329 A 5520 BEARING BOEING 737 7372H4 138448C NM ELEVATOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 4744A 23053 DURING SCHEDULED D-CHECK, FOUND LT ELEVATOR PCU UPPER ATTACH BEARING LOOSE. REMOVED AND REPLACED ELEVATOR PCU PER MM. 2 L 7 2 4F A16WE 2001042600064 20010426 00064 NM 2001 4 26 P5CA0100507 1 20010323 A 5754 FLAP BOEING 747 7472U3B NM WING WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 923FT 22769 WEAR FOUND ON LEADING EDGE FLAPS - NR 2 - WS 1423, NR 4-WS 1280, NR 7-WS 972, NR 8-WS889, NR 9-WS807. REPAIRED PER SRM 51-40-15. 2 L 7 4 4F RT A20WE 2001042600066 20010426 00066 NM 2001 4 26 P5CA0100479 1 20010226 A 5330 SKIN BOEING 747 7472U3B NM FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 922FT 22768 CRACK FOUND BS 434 STR 26 & 27. REPAIRED PER SRM 53-30-02. 2 L 7 4 4F RT A20WE 2001042600067 20010426 00067 NM 2001 4 26 P5CA0100514 1 20010328 A 5540 BALANCE WEIGHT BOEING 747 7472U3B NM RUDDER CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 923FT 22769 LEVEL 1 CORROSION FOUND ON BALANCE WEIGHT SEVEN ON UPPER RUDDER. REPAIRED PER S/L 747-55-07. 2 L 7 4 4F RT A20WE 2001042600068 20010426 00068 NM 2001 4 26 P5CA0100517 1 20010326 A 5751 BALANCE WEIGHT BOEING 747 7472U3B NM AILERON CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 923FT 22769 LEVEL 1 CORROSION FOUND ON BALANCE WEIGHT ONE LEFT OUTBOARD AILERON NR 3 POSITION. REPAIRED PER S/L 747-55-07. 2 L 7 4 4F RT A20WE 2001042600069 20010426 00069 NM 2001 4 26 P5CA0100520 1 20010326 A 5320 INTERCOSTAL BOEING 747 7472U3B NM FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 923FT 22769 CRACK FOUND ON INTERCOSTAL BULK CARGO BS 2040 LBL-30. REPAIRED PER SRM 53-10-07. 2 L 7 4 4F RT A20WE 2001042600070 20010426 00070 NM 2001 4 26 P5CA0100527 1 20010327 A 5730 FAIRING BOEING 747 747122 1384872 NM WING DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 DAMAGE FOUND ON NR 6 CANOE FIXED FAIRING WBL 353. FAIRING REPAIRED PER SRM 51-40-08. 2 L 7 4 4F A20WE 2001042600071 20010426 00071 NM 2001 4 26 CALA0100285 1 20010406 A 5551 ATTACH FITTING BOEING 737 7373T0 1384582 NM HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND LT FORWARD UPPER HORIZONTAL STABILIZER ATTACH FITTING HAD CORROSION BETWEEN BUSHING AND FITTING. A NEW OVERSIZED BUSHING WAS INSTALLED IAW SRM 55-10-06. 2 L 7 2 4F RT A16WE 2001042600072 20010426 00072 NM 2001 4 26 CALA0100291 1 20010406 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND FLOORBEAM CORRODED ON UPPER SURFACE AROUND SCREW HOLES AT STA 967, RBL 27, LBL 6, AND LBL 27. REPAIR S TRAPS AND SHIMS WERE INSTALLED IAW SRM 53-00-51, FIGURE 203, 51-20-01, AND 51-30-01. 2 L 7 2 4F RT A16WE 2001042600073 20010426 00073 NM 2001 4 26 CALA0100296 1 20010406 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND DIAGONAL FLOOR SUPPORT CORRODED AROUND FASTENER HOLES AT STA 986-1016 IN RT AFT LAV AREA. THE DIAGONAL FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001042600074 20010426 00074 NM 2001 4 26 CALA0100298 1 20010406 A 5320 PAN BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND FLOOR PAN CORRODED AT STA 1016 TO AFT PRESSURE BULKHEAD, BL 0 TO RBL 48. THE FLOOR PAN WAS REMOVED AND A NEW FLOOR PAN WAS INSTALLED IAW SRM 51-10-02, DRAWING 65C32677, AND DRAWING 65-52878. 2 L 7 2 4F RT A16WE 2001042600075 20010426 00075 NM 2001 4 26 CALA0100304 1 20010406 A 5330 SKIN BOEING 737 737524 1384721 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17627 27531 INSPECTION FOUND SKIN DENTED AT AFT CARGO DOOR JAMB LT SIDE OPENING 13 INCHES UP FROM BOTTOM EDGE, STA 847. A DOUBLER A ND TRIPLER WAS INSTALLED IAW ECRA 5330-03051. 2 L 7 2 4F RT A16WE 2001042600076 20010426 00076 NM 2001 4 26 CALA0100308 1 20010407 A 5415 ANGLE BOEING 737 7373T0 1384582 NM NR 2 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND A 1 INCH CRACK IN NR 2 ENGINE O/B LOWER PYLON ANGLE AT NAC STA 278. A DOUBLER WAS INSTALLED ON THE ANG LE IAW SRM 51-40-00. 2 L 7 2 4F RT A16WE 2001042600077 20010426 00077 WP 2001 4 26 AALA20010582 1 20010325 A 3350 LAMP DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7506 49800 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 17D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 17D. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600078 20010426 00078 WP 2001 4 26 AALA20010581 1 20010325 A 3350 LAMP DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7506 49800 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 7D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 7D. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600079 20010426 00079 WP 2001 4 26 AALA20010580 1 20010325 A 3350 LAMP DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7506 49800 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 13D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 13D. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600080 20010426 00080 WP 2001 4 26 AALA20010579 1 20010325 A 3350 LAMP DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7506 49800 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ILGHT AT SEAT 18D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 18D. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600081 20010426 00081 WP 2001 4 26 AALA20010578 1 20010325 A 3350 LAMP DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7506 49800 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 20D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 20D. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600082 20010426 00082 WP 2001 4 26 AALA20010590 1 20010324 A 3350 8034001 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 553AA 53083 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY EXIT LIGHT DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. SYST EM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600083 20010426 00083 WP 2001 4 26 AALA20010597 1 20010323 A 3350 LAMP DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7528A 49920 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 7D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 7D. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600084 20010426 00084 NM 2001 4 26 USAASB01083 1 20010320 A 5210 DOOR BOEING 737 737301 1384611 NM MAIN PAX NOT CLOSED A USAA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 EA 19 300AU 23228 BWI - FLT 1568 - ON CLIMB-OUT FROM DCA, AT APPROXIMATELY 4,500 FEET, THE FLIGHT ATTENDANT ADVISED CREW OF A LOUD AIR NOI SE COMING FROM THE FORWARD ENTRY DOOR. SIMULATANEOUSLY, THE CREW WAS UNABLE TO PRESSURIZE THE AIRCRAFT. FLIGHT DIVERTE D TO BWI AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MX FOUND THE FORWARD ENTRY DOOR NOT CLOSED PR OPERLY. A 1 INCH GAP WAS EVIDENT BETWEEN THE DOOR AND THE AIRCRAFT SKIN ALONG THE ENTIRE AFT EDGE. THE FORWARD SIDE OF DOOR WAS SECURED PROPERLY. DOOR WARNING LIGHT OPERATED NORMALLY. CYCLED DOOR SEVERAL TIMES. OPS CHECK GOOD. ALSO, F OUND THE AFT ENTRY DOOR SEAL COMING LOOSE. RESECURED DOOR SEAL. PRESSURIZED AIRCRAFT. PRESSURIZATION CHECKED GOOD WIT 2 L 7 2 4F RT A16WE 2001042600085 20010426 00085 EU 2001 4 26 USAASA01008 1 20010308 A 3350 1013101 SIGN AIRBUS 320 A320214 EU PAX CABIN INOPERATIVE A USAA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 19 108UW 1061 PHL-DEN - FLT 125 - THE EMERGENCY OVERWING EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EXIT SIGN ASSEMBL Y. OPERATIONALLY CHECKED GOOD. (M) 2 L 7 2 4F RT A28NM 2001042600086 20010426 00086 NM 2001 4 26 USAABB01015 1 20010213 A 3350 873100151REV9 LIGHT BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 608AU 22204 LAX - FOUND FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE AT ROW 5. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001042600087 20010426 00087 NM 2001 4 26 USAABB01014 1 20010312 A 3350 3020412 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 621AU 27200 BOS - FOUND R-1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001042600088 20010426 00088 NM 2001 4 26 USAABB01013 1 20010312 A 3350 LIGHT BOEING 757 7572B7 1384964 NM EXTERIOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 621AU 27200 BOS - FOUND L2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE CLEANED THE LIGHT ASSEMBLY CONTACTS. LIGHT WORKE D NORMALLY. (M) 2 L 7 2 4F RT A2NM 2001042600089 20010426 00089 WP 2001 4 26 USAAD01059 1 20010321 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC982 3022082 WP PAX CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 822US 49139 IND - THE CEILING EMERGENCY LIGHTS AT SEAT ROWS 15, 16 AND 17 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGH T POWER SUPPLY. (M) 2 L 7 2 4F A6WE 2001042600090 20010426 00090 WP 2001 4 26 USAAD01045 1 20010309 A 3350 9721055 BATTERY DOUG DC9 DC982 3022082 WP PAX CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 830US 49443 IND - THE LOW LEVEL EMERGENCY LIGHTS FAILED THE LIGHT TEST. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIE S. (M) 2 L 7 2 4F A6WE 2001042600091 20010426 00091 WP 2001 4 26 USAAD01055 1 20010317 A 3350 AD4002P BATTERY DOUG DC9 DC982 3022082 WP PAX CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 815US 48095 BOS - THE CENTER SECTION OF THE CEILING EMERGENCY LIGHTS AND THE OVERWING EXIT EMERGENCY LIGHTS WERE INOPERATIVE. MAINT ENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001042600093 20010426 00093 NM 2001 4 26 AALA20010571 1 20010320 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 878AA 21390 TUL - FOUND 31 INCHES BY 24 INCHES OF CORROSION ON LOWER SKIN OF CENTER WING STATION 834 TO 845 LBL 20-35 ABOVE HEAT EXC HANGER. REMOVED CORROSION AND INSTALLED DOUBLER PER ESO 11697 DATED 3-20-01. (M) 2 L 7 3 4F A3WE 2001042600094 20010426 00094 NM 2001 4 26 SWAA010932 1 20010328 A 5311 6546529 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, BL 25, WL 154. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2001042600095 20010426 00095 NM 2001 4 26 SWAA010933 1 20010328 A 5330 6545778 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND AFT SVC DOOR LOWER HINGE FUSELAGE SKIN CUTOUT CRACKED. REPAIRED SKIN PER BFG ER. 2 L 7 2 4F A16WE 2001042600096 20010426 00096 NM 2001 4 26 SWAA010934 1 20010328 A 5320 65C27314 STRINGER CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND 6 STR CLIPS CRACKED AT BS 727A, STR 7L, BS 747, STR 6L &7L, BS 807, STR 7L, BS 767, STR 7L & BS 787, STR 10R. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F A16WE 2001042600097 20010426 00097 NM 2001 4 26 SWAA010935 1 20010328 A 5520 DAS1026A1 BEARING BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 638SW 27711 DURING SCHEDULED C2 CHECK, LT ELEVATOR FAILED HINGE PLAY INSPECTION. REMOVED AND REPLACED ELEVATOR PUSH ROD BEARING PER MM. 2 L 7 2 4F RT A16WE 2001042600098 20010426 00098 NM 2001 4 26 SWAA010936 1 20010328 A 5315 6546804 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CRACKED AT BS 947, LBL 55. REPAIRED FLOORBEAM PER T1-253-024 & T1 -453-037. 2 L 7 2 4F A16WE 2001042600099 20010426 00099 CE 2001 4 26 GLBA2001063 1 20010324 A 5753 ROLLER BEECH 1900 1900D 1154162 CE FLAPS STUCK A GLBA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CE 01 260GL UE260 FLAPS STUCK AT 17 PERCENT. REPLACED FLAP SWITCH ROLLERS AND LINK OPS CHECKED SYSTEM GOOD. RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 2001042600100 20010426 00100 NM 2001 4 26 SWAA010921 1 20010327 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 378SW 26585 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED AT RBL 5, WL 201. REPAIRED BULKHEAD WEB PER SRM. 2 L 7 2 4F RT A16WE 2001042600101 20010426 00101 NM 2001 4 26 SWAA010922 1 20010326 A 5753 6546435 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 615SW 27698 DURING SCHEDULED C2 CHECK, FOUND RT WING OUTBD T/E FLAP DELAMINATED AT INBD END. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2001042600102 20010426 00102 2001 4 26 SWAA010923 4 20010326 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 624SW 27934 DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESSURE IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001042600103 20010426 00103 NM 2001 4 26 SWAA010924 1 20010327 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664WN 23495 DURING SCHEDULED SERVICE CHECK, FOUND 2.5 INCH LONG EXTERNAL FUSELAGE SKIN CRACK AT BS 727E, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001042600104 20010426 00104 2001 4 26 SWAA010926 4 20010326 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 503SW 24180 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001042600105 20010426 00105 NM 2001 4 26 SWAA010927 1 20010326 A 5330 6545778 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 503SW 24180 DURING SCHEDULED C4 CHECK, FOUND 3 INCH LONG EXTERNAL FUSELAGE SKIN CRACK AT BS 947, STR 22R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001042600106 20010426 00106 NM 2001 4 26 SWAA010928 1 20010326 A 2131 7638102 CONTROLLER BOEING 737 7373H4 1384600 NM CABIN PRESSURE INOPERATIVE A SWAA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 323SW 23344 DIVERSION, CABIN FAILED TO PRESSURIZE DURING FLIGHT. PRESS CONTROLLER AUTO MODE ALREADY ON MEL. REMOVED AND REPLACED C ABIN PRESS CONTROLLER PER MM, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2001042600107 20010426 00107 NM 2001 4 26 SWAA011029 1 20010404 A 5330 65C35773 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND FUSELAGE WINDOW BELT SKIN CRACKED AT WINDOW 30R, LOWER FWD CORNER. REPAIRED SKIN PER BF G ER. 2 L 7 2 4F A16WE 2001042600108 20010426 00108 NM 2001 4 26 SWAA011030 1 20010404 A 5330 65C35773 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND FUSELAGE WINDOW BELT SKIN CRACK AT WINDOW 28R, UPPER AFT CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001042600109 20010426 00109 NM 2001 4 26 SWAA011031 1 20010404 A 5330 6545766 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND FUSELAGE WINDOW BELT SKIN CRACKS AT WINDOWS 1L, 2L & 3L, UPPER FWD CORNERS. REPAIRED SK IN PER BFG ER. 2 L 7 2 4F A16WE 2001042600110 20010426 00110 NM 2001 4 26 SWAA011032 1 20010405 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED A1 CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 400, STR 4L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001042600111 20010426 00111 2001 4 26 SWAA011034 4 20010404 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 357SW 26594 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY AND SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF VIEW. REPOSITIONE D EVAC SLIDE ASSY''S PER MM. 2 L 7 2 4F RT A16WE 2001042600112 20010426 00112 NM 2001 4 26 SWAA011035 1 20010405 A 5754 65C26686 SKIN BOEING 737 7373Y0 1384671 NM L/E SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664WN 23495 DURING SCHEDULED 1/4D CHECK, FOUND NR 1 L/E SLAT SKIN CRACKED AT OUTBD LOWER END. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001042600113 20010426 00113 NM 2001 4 26 SWAA011036 1 20010404 A 5320 6551698 SPLICE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 514SW 25153 DURING SCHEDULED D-CHECK AT DALFORT, FOUND STR SPLICE CRACKED BETWEEN FASTENER HOLES AT BS 907, STR 4R. REMOVED AND REP LACED STR SPICE PER SRM. 2 L 7 2 4F RT A16WE 2001042600114 20010426 00114 NM 2001 4 26 SWAA011038 1 20010404 A 5552 183A8300 FITTING BOEING 737 7377H4 NM ELEVATOR TAB DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 713SW 27847 DURING SCHEDULED SERVICE CHECK (SWA SI 11038-55), FOUND MIGRATED BEARING AT LT ELEVATOR TAB CONTROL OUTBD ATTACH POINT T O ELEVATOR. REPAIRED TAB CONTROL ATTACH FITTING PER D&M ENTERPRISES WO 014. 2 L 7 2 4F RT A16WE 2001042600115 20010426 00115 NM 2001 4 26 SWAA011039 1 20010404 A 5523 DAS414A1 BEARING BOEING 737 7377H4 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 713SW 27847 DURING SCHEDULED SERVICE CHECK (SWA SI 11038-55), FOUND NR 1 RT ELEVATOR TAB BEARING WORN. REMOVED AND REPLACED BEARING PER MM AND D&M ENTERPRISES INV SSR012. 2 L 7 2 4F RT A16WE 2001042600116 20010426 00116 NM 2001 4 26 AALA20010542 1 20010311 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 891AA 22007 TUL - FOUND DEEP GOUGE AND DENT IN SKIN STATION 715 BELOW STRINGER 20R. INSTALLED DOUBLER PER SRM 53-30-1. (M) 2 L 7 3 4F A3WE 2001042600117 20010426 00117 NM 2001 4 26 AALA20010550 1 20010312 A 5730 SKIN BOEING 727 727223 1384074 NM WING BOX CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 878AA 21390 TUL - FOUND CORROSION ON LOWER SKIN OF CENTER WING STATION 832-834 RBL 16.20-32.20. REMOVED CORROSION AND INSTALLED DOU BLER PER SRM 57-30-3. (M) 2 L 7 3 4F A3WE 2001042600118 20010426 00118 NM 2001 4 26 AALA20010023 1 20010103 A 3350 SWITCH DOUG MD11 MD11 3023602 NM COCKPIT DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1761R 48551 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT INOPERATIVE. REPLACED LEFT SIDE EMERGENCY EXIT LIGH T SWITCH AT COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 2001042600119 20010426 00119 NM 2001 4 26 SWAA011040 1 20010404 A 5523 183A84102 BUSHING BOEING 737 7377H4 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 713SW 27847 DURING SCHEDULED SERVICE CHECK (SWA SI 11038-55), FOUND NR 2, 3 & 4 RT ELEVATOR TAB HINGE BUSHINGS WORN. REMOVED AND RE PLACED BUSHINGS PER MM AND D&M ENTERPRISES INV SSR013. 2 L 7 2 4F RT A16WE 2001042600120 20010426 00120 NM 2001 4 26 SWAA011041 1 20010404 A 5523 183A84102 BUSHING BOEING 737 7377H4 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 713SW 27847 DURING SCHEDULED SERVICE CHECK (SWA SI 11038-55), FOUND NR 1, 2, 3 & 4 LT ELEVATOR TAB BUSHINGS WORN. REMOVED AND REPLA CED BUSHINGS PER MM AND D&M ENTERPRISES INV SSR013. 2 L 7 2 4F RT A16WE 2001042600121 20010426 00121 NM 2001 4 26 SWAA011018 1 20010404 A 5751 6545645 SKIN BOEING 737 7372H4 138448C NM AILERON DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 068SW 22357 ON WALKAROUND, FOUND LT WING AILERON SKIN DELAMINATED ON UPPER AND LOWER SURFACE, OUTBD END. REMOVED AND REPLACED AILER ON PER MM. 2 L 7 2 4F A16WE 2001042600122 20010426 00122 NM 2001 4 26 AALA20010039 1 20010108 A 3350 CONNECTOR DOUG MD11 MD11 3023602 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1762B 48552 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT AISLE LIGHT AT FIRST CLASS CABIN INOPERATIVE. REPLACED EMERGENCY EXI T LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 2001042600123 20010426 00123 NM 2001 4 26 AALA20010366 1 20010301 A 3350 CONNECTOR DOUG MD11 MD11 3023602 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1766A 48597 DFW - DURING OVERNIGHT MAINTENANCE, FLOOR PATH EMERGENCY EXIT LIGHT AT RIGHT AFT CABIN DIM. REPLACED FLOOR PATH EMERGEN CY EXIT LIGHT CONNECTOR AT SEAT 38C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 2001042600124 20010426 00124 NM 2001 4 26 AALA20010526 1 20010312 A 3397 WIRE DOUG MD11 MD11 3023602 NM R2 DOOR BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 21 1766A 48597 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT R2 DOOR DIM. REPAIRED EMERGENCY EXIT WIRE SPLICE AT R2 DOOR . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 2001042600125 20010426 00125 NM 2001 4 26 AALA20010527 1 20010312 A 3397 WIRE DOUG MD11 MD11 3023602 NM CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 21 1766A 48597 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 20G THROUGH 38G DIM. REPAIRED EMERGENCY EXIT LIGHT WIR E SPLICE AT SEAT 38G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 2001042600126 20010426 00126 NM 2001 4 26 AALA20010528 1 20010312 A 3397 WIRE DOUG MD11 MD11 3023602 NM CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 21 1766A 48597 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 8G THROUGH 15G DIM. REPAIRED EMERGENCY EXIT LIGHT WIRE SPLICE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 2001042600127 20010426 00127 NM 2001 4 26 AALA20010529 1 20010312 A 3350 LIGHT DOUG MD11 MD11 3023602 NM CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1766A 48597 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT FIRST CLASS CABIN DIM. REPLACED EMERGENCY EXIT LIGHT STRIP AT FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 2001042600128 20010426 00128 EU 2001 4 26 AALA20010559 1 20010315 A 2612 K0038A RELAY FOKKER F28 F28MK0100 4990807 EU TAIL INOPERATIVE A AALA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 1411G 11369 DFW - FLT 581 - EN ROUTE ORD-SAT, DETECTED APU FIRE WARNING LIGHT AT MFDU. DISCHARGED APU FIRE BOTTLE. DIVERTED DFW AN D LANDED WITHOUT FURTHER INCIDENT. REPLACED APU TAIL PIPE OVERHEAT DETECTOR RELAY. SYSTEM GROUND CHECKED NORMAL OPERAT ION. (M) 2 L 7 2 4F RT 2001042600129 20010426 00129 2001 4 26 SWAA011022 4 20010404 A 2565 63550101 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF TOLERANCE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED SERVICE CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED E VAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001042600130 20010426 00130 NM 2001 4 26 SWAA011026 1 20010403 A 5753 6546434 FLAP BOEING 737 7375H4 138449D NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED C3 CHECK, FOUND LT WING INBD AFT FLAP DELAMINATED AT INBD END. REMOVED AND REPLACED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2001042600131 20010426 00131 WP 2001 4 26 AALA20010555 1 20010309 A 4990 5940405503 APU DOUG DC9 DC982 3022082 WP APU BAY LEAKING A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 489AA 49682 DFW - FLT 421 - EN ROUTE DFW-SEA, SHORTLY AFTER TAKEOFF, CABIN FILLED WITH SMOKE. RETURNED DFW AND LANDED WITHOUT FURTH ER INCIDENT. REPLACED APU. PERFORMED PACK BURNOUT PER MM. LEAK CHECKED GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600132 20010426 00132 WP 2001 4 26 AALA20010554 1 20010312 A 2120 UNKNOWN DOUG DC9 DC982 3022082 WP COCKPIT ODOR A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 493AA 49731 ORD - FLT 538 - EN ROUTE LAS-ORD, WHEN WINDSHIELD ANTI-FOG TURNED ON DETECTED A BURNING SMELL. TURNED OFF WINDSHIELD AN TI-FOG. LANDED ORD WITHOUT FURTHER INCIDENT. OPERATED ANTI-FOG APPROXIATELY THREE HOURS. NO SMOKE OR ODOR NOTED. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600133 20010426 00133 WP 2001 4 26 AALA20010511 1 20010317 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7538A 49992 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT AT SEAT 24, 25, AND 26 INOPERATIVE. CLEANED EMERGENCY EXIT LIGH T CONNECTOR AT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600134 20010426 00134 WP 2001 4 26 AALA20010508 1 20010316 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 76200 53290 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PORTABLE LIGHT DIM. REPLACED EMERGENCY EXIT PORTABLE LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001042600135 20010426 00135 WP 2001 4 26 AALA20010504 1 20010315 A 3397 WIRE DOUG DC9 DC982 3022082 WP OVERWING BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 21 77421 49333 RDU - DURING OVERNIGHT MAINTENANCE, LEFT SIDE OVERWING EMERGENCY EXIT LIGHT DIM. REPAIRED EMERGENCY EXIT LIGHT GROUND W IRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600136 20010426 00136 WP 2001 4 26 AALA20010503 1 20010314 A 3350 LAMP DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 490AA 49683 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 8E TOO BRIGHT. REPLACED EMERGENCY EXIT IGHT AT SEAT 8E . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600137 20010426 00137 WP 2001 4 26 AALA20010500 1 20010315 A 3350 LAMP DOUG DC9 DC982 3022082 WP AFT LAVATORY MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 432AA 49350 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT AT AFT LAVATORY DIM. REPLACED EMERGENCY EXIT LIGHT AT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600138 20010426 00138 WP 2001 4 26 AALA20010499 1 20010315 A 3350 LAMP DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 587AA 53250 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 21D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 21D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600139 20010426 00139 WP 2001 4 26 AALA20010496 1 20010315 A 3350 LAMP DOUG DC9 DC982 3022082 WP TAILCONE MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 409AA 49320 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT TAIL CONE DIM. REPLACED EMERGENCY EXIT LIGHT AT TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600140 20010426 00140 WP 2001 4 26 AALA20010495 1 20010315 A 3350 LAMP DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 409AA 49320 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 10 DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 10. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600141 20010426 00141 WP 2001 4 26 AALA20010494 1 20010315 A 3350 CHARGER DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 587AA 53250 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT AT SEAT ROW 13 THROUGH 15 DIM. REPLACED EMERGENCY EXIT LIGHT CHARGE R ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600142 20010426 00142 WP 2001 4 26 AALA20010491 1 20010315 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 443AA 49469 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT FIRST CLASS DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK AT FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600143 20010426 00143 WP 2001 4 26 AALA20010487 1 20010315 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 419AA 49331 DFW - DURING OVERNIGHT MAINTENANCE, PORTABLE EMERGENCY EXIT LIGHT AT L1 DOOR INOPERATIVE. REPLACED PORTABLE EMERGENCY E XIT LIGHT ASSEMBLY AT L1 DOOR. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600144 20010426 00144 WP 2001 4 26 AALA20010483 1 20010315 A 3350 4000792 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 468AA 49598 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 9 INOPERTIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT ROW 9. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600145 20010426 00145 NM 2001 4 26 SWAA011003 1 20010402 A 2910 65C26839 HYDRAULIC LINE BOEING 737 7373H4 1384600 NM HYD SYSTEM BROKEN A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 341SW 24091 DIVERSION, LOST B-HYDRAULIC SYSTEM PRESS AND FLUID. REMOVED AND REPLACED BROKEN HYDRAULIC LINE AT B-SYSTEM ELECTRIC PUM P PER MM. 2 L 7 2 4F RT A16WE 2001042600146 20010426 00146 NM 2001 4 26 SWAA011004 1 20010403 A 5330 6545800 SKIN BOEING 737 7373T5 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD UPPER CORNER OF AIRSTAIR DOOR CUTOUT. REPAIRED SKIN PER S WA RA. 2 L 7 2 4F RT A16WE 2001042600147 20010426 00147 2001 4 26 SWAA011007 4 20010402 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 635SW 27708 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001042600148 20010426 00148 NM 2001 4 26 SWAA011009 1 20010403 A 5330 6545857 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACK AT AFT ENTRY DOOR, UPPER FWD HINGE CUTOUT. REPAIRED SKIN PER BFG ER . 2 L 7 2 4F A16WE 2001042600149 20010426 00149 NM 2001 4 26 SWAA011010 1 20010403 A 5311 6546539 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT BS 616, RT SIDE, WL 202. REPAIRED FRAME PER BFG ER. 2 L 7 2 4F A16WE 2001042600150 20010426 00150 2001 4 26 SWAA011011 4 20010403 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SEVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001042600151 20010426 00151 NM 2001 4 26 SWAA011012 1 20010402 A 5310 6546558 SHEAR TIE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 908, BELOW STR 14R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F A16WE 2001042600152 20010426 00152 NM 2001 4 26 SWAA011013 1 20010402 A 5330 65C35770 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED 1/2D CHECK, FOUND 4 FUSELAGE SKIN CRACKS, UNDER PREVIOUS REPAIR, AT BS 663.75, BETWEEN STR 4R & STR 3L. REPAIRED SKIN PER SRM & T1-A51-002. 2 L 7 2 4F A16WE 2001042600153 20010426 00153 NM 2001 4 26 SWAA011014 1 20010403 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 355SW 25250 DURING SCHEDULED D-CHECK, FOUND FUSELAGE T-CHORD CORRODED AT BS 328, RBL 42 & RBL 49, LOWER SURFACE. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001042600154 20010426 00154 WP 2001 4 26 AALA20010481 1 20010312 A 3350 SOCKET DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 494AA 49732 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 4E INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET A SSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600155 20010426 00155 WP 2001 4 26 AALA20010480 1 20010312 A 3350 LAMP DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 499AA 49737 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 4E DIM. REPLACED EMERGENCY EXIT LIGHT AT 4E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600156 20010426 00156 WP 2001 4 26 AALA20010479 1 20010312 A 3350 LAMP DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 499AA 49737 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 7D DIM. REPLACED EMERGENCY EXIT LIGHT AT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600157 20010426 00157 WP 2001 4 26 AALA20010478 1 20010312 A 3350 LAMP DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 499AA 49737 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 13D DIM. REPLACED EMERGENCY EXIT LIGHT AT 13D. SYSTEM GROU ND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600158 20010426 00158 WP 2001 4 26 AALA20010477 1 20010312 A 3350 LAMP DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 499AA 49737 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 23D DIM. REPLACED EMERGENCY EXIT LIGHT AT 23D. SYSTEM GROU ND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600159 20010426 00159 WP 2001 4 26 AALA20010476 1 20010312 A 3350 LAMP DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 499AA 49737 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 26D DIM. REPLACED EMERGENCY EXIT LIGHT AT 26D. SYSTEM GROU ND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600160 20010426 00160 WP 2001 4 26 AALA20010475 1 20010312 A 3350 LAMP DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 499AA 49737 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT ILGHT AT 27D DIM. REPLACED EMERGENCY EXIT LIGHT AT 27D. SYSTEM GROUN D CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600161 20010426 00161 NM 2001 4 26 SWAA011015 1 20010402 A 5753 6546435 FLAP BOEING 737 7375H4 138449D NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 507SW 24184 DURING SCHEDULED C3 CHECK, FOUND LT WING OUTBD T/E AFT FLAP DISBONDED AT INBD END. REMOVED AND REPLACED AFT FLAP PER MM . 2 L 7 2 4F RT A16WE 2001042600162 20010426 00162 2001 4 26 SWAA011016 4 20010402 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 512SW 24189 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001042600163 20010426 00163 2001 4 26 SWAA010964 4 20010330 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF TOLERANCE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 063SW 22061 DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED E VAC SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001042600164 20010426 00164 NM 2001 4 26 SWAA010965 1 20010330 A 5312 6517582 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT RBL 17.5, WL 226. REPAIRED VERTICAL BEAM W EB PER SRM. 2 L 7 2 4F A16WE 2001042600165 20010426 00165 NM 2001 4 26 SWAA010966 1 20010330 A 5330 6545857 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER BFG ER. 2 L 7 2 4F A16WE 2001042600166 20010426 00166 NM 2001 4 26 AALA20010471 1 20010311 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 773AN 29583 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT SEATS 25 THROUGH 30 DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001042600167 20010426 00167 WP 2001 4 26 AALA20010473 1 20010312 A 3350 LAMP DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 499AA 49737 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 30D DIM. REPLACED EMERGENCY EXIT LIGHT BULB AT SEAT 30 D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600168 20010426 00168 NM 2001 4 26 AALA20010558 1 20010313 A 3230 4080070 LINE BOEING 757 757223 1384957 NM MLG LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 624AA 24582 LAX - FLT 2490 - EN ROUTE LAX-DFW, LOST LEFT SIDE HYDRAULIC SYSTEM. RETURNED LAX AND LANDED WITHOUT FURTHER INCIDENT. REPLACED LEFT SIDE MAIN LANDING GEAR DOWN LOCK ACTUATOR RETURN LINE. LEAK CHECKS GOOD. SYSTEM GROUND CHECKED NORMAL OP ERATION. (M) 2 L 7 2 4F RT A2NM 2001042600169 20010426 00169 NM 2001 4 26 AALA20010557 1 20010314 A 2910 S271T0054 SWITCH BOEING 757 757223 1384957 NM NR 2 ENGINE DEFECTIVE A AALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 611AM 24487 TUL - FLT 1805 - EN ROUTE TUL-DFW, DETECTED RIGHT SIDE HYDRAULIC QUANTITY LOW. RETURNED TUL GATE WITHOUT FURTHER INCIDE NT. REPLACED NR 2 SIDE ENGINE DIFFERENTIAL PRESSURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001042600170 20010426 00170 EU 2001 4 26 AALA20010570 1 20010321 A 2530 251000307 OVEN AIRBUS 300 A300B4605R 3930308 EU CABIN DIRTY A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 14065 508 LHR - FLT 0092 - EN ROUTE EWR-LHR, DETECTED SMOKE AT BUSINESS CLASS OVEN. TURNED OFF OVEN. LANDED LHR WITHOUT FURTHER INCIDENT. CLEANED BUSINESS CLASS OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2001042600171 20010426 00171 NM 2001 4 26 AALA20010612 1 20010321 A 2810 PACKING BOEING 757 757223 1384957 NM NR 2 ENGINE LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 601AN 27052 MIA - FLT 687 - EN ROUTE MIA-SXM - SHORTLY AFTER TAEKOFF DETECTED VAPOR STREAM OF FUEL AT RIGHT ENGINE. RETURNED MIA AN D LANDED WITHOUT FURTHER INCIDENT. REPLACED NR 2 ENGINE FUEL FLOW PRESSURE SWITCH PACKING AND FUEL DIFFERENTIAL PRESSURE SWITCH PACKING. (M) 2 L 7 2 4F RT A2NM 2001042600172 20010426 00172 NM 2001 4 26 AALA20010617 1 20010319 A 5730 SKIN BOEING 727 727223 1384074 NM WING BOX CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 868AA 21373 TUL - FOUND CORROSION ON LOWER CENTER SECTION WING SKIN ABOVE RIGHT PRIMARY HEAT EXCHANGER (LOWER SKIN). REMOVED CORROS ION AND INSTALLED DOUBLER AND TRIPLER PER SRM 57-30-3. (M) 2 L 7 3 4F A3WE 2001042600173 20010426 00173 NM 2001 4 26 AALA20010618 1 20010316 A 5313 STRINGER BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 868AA 21373 TUL - FOUND CORROSION ON STRINGER 28R OUTBOARD SIDE STATION 677. REMOVED CORRODED SECTION OF STRINGER. INSTALLED STRIN GER REPAIR PER SRM 53-10-3, AND MM 51-20-0. (M) 2 L 7 3 4F A3WE 2001042600174 20010426 00174 NM 2001 4 26 AALA20010619 1 20010321 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 868AA 21373 TUL - FOUND DENT AT FUSELAGE SKIN ABOVE STRINGER 24R AT STATION 340. REMOVED DAMAGED AREA, INSTALLED DOUBLER PER SRM 53 -30-3 PART 1. (M) 2 L 7 3 4F A3WE 2001042600175 20010426 00175 NM 2001 4 26 SWAA010967 1 20010330 A 5320 6551698 SPLICE BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND 2 STR SPLICES CORRODED AT BS 907, STR 21L & STR 23L. REMOVED AND REPLACED STR SPLICES P ER SRM. 2 L 7 2 4F A16WE 2001042600176 20010426 00176 NM 2001 4 26 SWAA010969 1 20010330 A 5315 6546804 FLOORBEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664WN 23495 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAMS CORRODED AT BS 750, RBL 3.0 & BS 767, LBL 7.5. REPAIRED FLOORBEAMS PER SW A RA. 2 L 7 2 4F RT A16WE 2001042600177 20010426 00177 NM 2001 4 26 SWAA010970 1 20010330 A 5320 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664WN 23495 DURING SCHEDULED 1/4D CHECK, FOUND STR 26L CLIP CRACKED AT BS 867. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001042600178 20010426 00178 NM 2001 4 26 SWAA010971 1 20010330 A 5312 6516300 BULKHEAD BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664WN 23495 DURING SCHEDULED 1/4D CHECK, FOUND 3 BS 178 BULKHEAD WEB CRACKS AT LBL 12, WL 234, LBL 13.5, WL 234 & RBL 5, WL 195. RE PAIRED BULKHEAD WEB CRACKS PER SRM. 2 L 7 2 4F RT A16WE 2001042600179 20010426 00179 NM 2001 4 26 SWAA010972 1 20010330 A 5312 6516300 BULKHEAD BOEING 737 7373Y0 1384671 NM FUSELAGE CANNING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664WN 23495 DURING SCHEDULED 1/4 CHECK, FOUND BS 178 BULKHEAD WEB OIL CANNED AT PREVIOUS REPAIR, WL 190, BL 0. REPAIRED BULKHEAD WE B PER SRM. 2 L 7 2 4F RT A16WE 2001042600180 20010426 00180 NM 2001 4 26 SWAA010973 1 20010329 A 5230 57094 SEAL BOEING 737 7373H4 1384600 NM CARGO DOOR OUT OF POSITION A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 346SW 24153 AIR TURNBACK, CABIN DIFFICULT TO PRESSURIZE. REPOSITIONED AFT CARGO DOOR PRESSURE SEAL PER MM. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2001042600181 20010426 00181 NM 2001 4 26 AALA20010382 1 20010306 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 352AA 24033 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 38H, 25B, 2B, 3B, 7B AND 8B INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 38H AND 25B. REPAIRED CONNECTOR AT 2B AND 3B, 7B AND 8B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001042600182 20010426 00182 NM 2001 4 26 AALA20010401 1 20010309 A 3350 LAMP BOEING 777 777223 1385213 NM CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 788AN 30011 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT COACH CLASS DIM. REPLACED EMERGENCY EXIT LIGHT AT COACH CLA SS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001042600183 20010426 00183 NM 2001 4 26 USAASB01089 1 20010326 A 3260 189929 SENSOR BOEING 737 7372B7 1384560 NM MLG FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 285AU 23132 FLL - FLT 2992 - AFTER TAKEOFF FROM FLL, THE LANDING GEAR WOULD NOT RETRACT AS GEAR LEVER WOULD NOT MOVE PAST NEUTRAL. GEAR WARNING HORN AND AIR-GROUND SENSOR ALARMS SOUNDED AS CREW RETRACTED FLAPS PER QUICK REF HANDBOOK PROCEDURES. CREW WOULD NOT ISOLATE PROBLEM. FLIGHT RETURNED TO FIELD AT FLL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLA RED. AIRCRAFT WAS MAINTENANCE FERRIED TO TPA WHERE MAINTENANCE JACKED AIRCRAFT AND CYCLED GEAR NORMALLY SEVERAL TIMES. INSPECTED LANDING GEAR SAFETY SWITCHES AND FOUND AIR SAFETY SENSOR GAP EXCESSIVE. ADJUSTED LANDING GEAR SAFETY SENSOR AND TESTED OK PER MM 32-09-200. (M) 2 L 7 2 4F A16WE 2001042600184 20010426 00184 NM 2001 4 26 AALA20010629 1 20010319 A 5320 SUPPORT BRACKET BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 892AA 22008 TUL - FOUND STRINGER TO FRAME SUPPORT BRACKET (U-CHANNEL) CORRODED ON BOTTOM JUST ABOVE BELLY SKIN STRINGER 27R STATION 560. REMOVED CORROSION, ALODINED AND PRIMED. (M) 2 L 7 3 4F A3WE 2001042600185 20010426 00185 NM 2001 4 26 AALA20010630 1 20010319 A 5310 SHEAR TIE BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 892AA 22008 TUL - FOUND CORROSION ON SHEAR TIE STATION 540 STRINGER 27R. REMOVED CORROSION, ALODINED AND PRIMED PER MM 51-20-0. (M ) 2 L 7 3 4F A3WE 2001042600186 20010426 00186 NM 2001 4 26 AALA20010631 1 20010325 A 5313 STRINGER BOEING 727 727223 1384074 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 892AA 22008 TUL - FOUND STRINGER 18A CRACKED ABOVE AND BELOW FLANGE AT STATION 940 RIGHT. REMOVED AND REPLACED STRINGER 18A RIGHT P ER SERVICE BULLETIN 727-53-0172. (M) 2 L 7 3 4F A3WE 2001042600187 20010426 00187 NM 2001 4 26 AALA20010632 1 20010321 A 5710 STRUCTURE BOEING 727 727223 1384074 NM RT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 892AA 22008 TUL - FOUND RIGHT WING LOWER LEADING EDGE CHORD EXTENSION HAS HEAVY AREA OF CORROSION, UNDER INBOARD END OF STUB ACCESS. REMOVED CORROSION AND REPAIRED PER AARD 57-30-00-2. (M) 2 L 7 3 4F A3WE 2001042600188 20010426 00188 NM 2001 4 26 AALA20010621 1 20010320 A 2910 5490418 LINE BOEING 767 767223 1385123 NM NR 2 ENGINE LEAKING A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 315AA 22317 BWI - FLT 174 - EN ROUTE RDU-LGW, DETECTED RIGHT SIDE HYDRAULIC SYSTEM FAILURE. DIVERTED BWI AND LANDED WITHOUT FURTHER INCIDENT. REPLACED RIGHT SIDE ENGINE HYDRAULIC PUMP PRESSURE INE. SERVICED RIGHT HYDRAULIC SYSTEM. RAN BOTH ENGINES. NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001042600189 20010426 00189 NM 2001 4 26 AALA20010472 1 20010311 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 773AN 29583 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L1 DOOR DAMAGED. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001042600190 20010426 00190 NM 2001 4 26 AALA20010530 1 20010314 A 3350 BATTERY BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 789AN 30252 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 37G THROUGH 43G DIM. CHARGED EMERGENCY EXIT LIGHT BATT ERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001042600191 20010426 00191 NM 2001 4 26 SWAA010975 1 20010331 A 3350 6104789 BATTERY PACK BOEING 737 7372K6 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2001042600192 20010426 00192 NM 2001 4 26 SWAA010976 1 20010331 A 5752 6546455 TAB BOEING 737 7373Y0 1384671 NM AILERON DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664WN 23495 DURING SCHEDULED 1/4D CHECK, FOUND RT WING AILERON TAB INBD T/E DELAMINATED. REMOVED AND REPLACED AILERON TAB PER MM. 2 L 7 2 4F RT A16WE 2001042600193 20010426 00193 NM 2001 4 26 SWAA010978 1 20010401 A 3240 52701010 VALVE BOEING 737 7377H4 NM BRAKE SYS FAILED A SWAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 724SW 27856 DURING TAXI INTO POSITION FOR TAKEOFF, BRAKES LOCKED UP & RTO LIGHT ILLUMINATED. AIRCRAFT WOULD NOT MOVE. TOWED AIRCRA FT BACK TO GATE. REMOVED AND REPLACED ANTI-SKID CONTROL UNIT AND PARKING BRAKE VALVE PER MM. C/W BITE CHECK AND SPEED BRAKE RTO TEST PER MM, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2001042600194 20010426 00194 NM 2001 4 26 VNAA0103017 1 20010330 A 3350 362624 LIGHT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN INOPERATIVE A VNAA K NONE L NO TEST NR NOT REPORTED 1 GL 07 457PS 3048 THE FLIGHT CREW REPORTED THAT THE EMERGENCY FLOOR PATHWAY LIGHT WOULD NOT ILLUMINATE ADJACENT TO THE CABIN SEAT ROW 7 P OSITION. MAINTENANCE REPLACED THE FLOOR PATHWAY LIGHT STRIP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-12. OP ERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001042600195 20010426 00195 NM 2001 4 26 AALA20010421 1 20010312 A 5511 SPAR BOEING 727 727223 1384074 NM HORIZONTAL STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 894AA 22010 TUL - FOUND CORROSION ON RIGHT HORIZ STAB AFT SPAR, ON TOP APPROX 30 INCHES OUTBOARD OF ELEVATOR PCU. REPAIRED AREA PER ESO 11697 DATED 3-7-01. (M) 2 L 7 3 4F A3WE 2001042600196 20010426 00196 WP 2001 4 26 AALA20010537 1 20010313 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND DENT WITH GOUGE IN FUSELAGE SKIN STATION 503, BETWEEN LONGERON 21R AND 22R. REPAIRED PER ESO 80559 03/08/20 01 AND REVISION DATED 3/12/01, USING 38 HI-LOCKS WITH REMAINDER OF THE FASTENER AS RIVITS. (M) 2 L 7 2 4F A6WE 2001042600197 20010426 00197 NM 2001 4 26 USAA010259 1 20010312 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 42739 23742 PIT - FOUND SKIN CRACKED 1.5 INCH LONG CRACK, RIGHT SIDE, STATION 727D AT STRINGER 23 RT. CUT OUT DAMAGE, INSTALLED EXT ERNAL DOUBLER PER SRM 53-00-01 FIG 201. (M) 2 L 7 2 4F RT A16WE 2001042600198 20010426 00198 EA 2001 4 26 JBXA000263 1 20010406 A 2913 PUMP CNDAIR CL600 CL6002B19 EA NR 1 ENGINE FAILED A JBXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 05 575ML 7256 NR 1 HYDRAULIC SYSTEM LOST ALL PRESSURE AND FLUID AT 26,000 FEET. RETURNED TO RDU. REMOVED AND REPLACED ALL NR 1 SYSTE M HYDRAULIC FILTERS IAW CRJ AMM 29-11-09, 29-11-40, AND 29-11-46. REMOVED AND REPLACED NR 1 SYSTEM ENGINE DRIVEN HYDRAU LIC PUMP IAW CRJ AMM 29-11-01. REMOVED AND REPLACED NR 1 ENGINE DRIVEN PUMP PRESSURE LINE IAW CRJ AMM 29-11-52. REPAIR ED NR 1 SYSTEM RETURN LINE IAW CRJ AMM 20-22-00. PERFORMED OPS AND LEAK TEST OF NR 1 HYDRAULIC SYSTEM IAW CRJ AMM 29-10 -00. ALL OPS AND LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2001042600199 20010426 00199 EU 2001 4 26 RAIA00104006 1 20010408 A 2422 PC125123B INVERTER JETAIR JETSTM JETSTM4101 1500501 EU AVIONICS BAY FAILED A RAIA O OTHER J WARNING INDICATION CL CLIMB 1 CE 03 554HK 5788 5788 41067 5330-BWI-DURING CLIMB RIGHT HAND INVERTER FAILED. MAINTENANCE REMOVED AND REPLACED RIGHT HAND INVERTER IAW J41 MAINTENA NCE MANUAL. 2 L 7 2 4T RT A41NM 2001042600200 20010426 00200 2001 4 26 RAIA00104003 4 20010407 A 3418 0020BN4 COMPUTER EMB 145 EMB145 SO AVIONICS BAY FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 801HK 5951 5951 145053 7601-STL-DURING TAXI SPS MASTER CAUTION ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE STALL PROTECTION COMPUTER IAW EMB145 MAINTENANCE MANUAL. 2 L 7 2 4F RT T00011AT 2001042600201 20010426 00201 2001 4 26 RAIA00104004 4 20010407 A 3418 0861DT5 VANE EMB 145 EMB145 SO RT AOA FAILED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 801HK 7019 7019 145053 7601-STL-DURING TAKEOFF SPS MASTER CAUTION WARNING ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND ANGLE O F ATTACK VANE IAW EMB145 MAINTENANCE MANUAL. 2 L 7 2 4F RT T00011AT 2001042600202 20010426 00202 EU 2001 4 26 RAIA00104005 1 20010407 A 3010 14157015404 BOOT JETAIR JETSTM JETSTM4101 1500501 EU RT WING LEAKING A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 564HK 41081 5393-BWI-DURING TAXI CCT1 AND CCT3 FAULTED IN AUTO AND MANUAL. MAINTENANCE REMOVED AND REPLACED RIGHT HAND WING LEADING EDGE IAW J41 MAINTENANCE MANUAL. 2 L 7 2 4T RT A41NM 2001042600203 20010426 00203 NM 2001 4 26 USAA010235 1 20010219 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND FRAME CRACKED .25 INCH, FRAME 807 STRINGER 13L. REMOVED DAMAGE AND INSTALLED DOUBLERS PART 1 AND 2 IAW SRM 53-10-4. (M) 2 L 7 2 4F A16WE 2001042600204 20010426 00204 NM 2001 4 26 USAA010187 1 20010228 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 50739 22881 TPA - FOUND SKIN CRACKED .75 INCH, LOWER HINGE CUTOUT BETWEEN STRINGER 9 AND 10R AFT STATION 947. INSTALLED DOUBLER PER SRM 53-30-3 FIG 33N AND TR 53-30-11. (M) 2 L 7 2 4F A16WE 2001042600205 20010426 00205 SO 2001 4 26 C2XA01BT046 1 20010328 A 3240 WARNING SYSTEM EMB 145 EMB145 SO COCKPIT ACTIVATED A C2XA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 SW 27 14974 145161 CREW REPORTED AFTER RETRACT GOT BRAKE OVERHEAT MESSAGE. RE-EXTENDED LANDING GEAR TO COOL, GEAR WOULD NOT RETRACT. AIRC RAFT AIR RETURNED TO EWR. MAINTENANCE OPS CHECKED SYSTEM GOOD. GEAR WOULDN''T RETRACT IN FLIGHT BECAUSE AIRCRAFT WAS G OING OVER 200 KNOTS. GEAR CHECKED OK FOR SERVICE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2001042600206 20010426 00206 NM 2001 4 26 VNAA0104002 1 20010403 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST NR NOT REPORTED 1 GL 07 438JS 10261 12 3056 THE FLIGHT CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT OPERATE IN THE AFT SECTION OF THE CABIN. MAINTENANCE INSPE CTED AND REPLACED THE 7LK BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-00. OPERATIONAL CHECKS WERE COMPLE TED AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001042600207 20010426 00207 NM 2001 4 26 VNAA0104001 1 20010403 A 3350 363674 LIGHT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN INOPERATIVE A VNAA K NONE L NO TEST NR NOT REPORTED 1 GL 07 423JS 3032 THE FLIGHT CREW REPORTED THAT THE EMERGENCY FLOOR PATHWAY LIGHTING STRIP WOULD NOT ILLUMINATE ADJACENT TO SEAT 1D/F. MA INTENANCE INSPECTED AND RESECURED THE LIGHT STRIP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-12. OPERATIONAL C HECKS WERE COMPLETED AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001042600208 20010426 00208 NM 2001 4 26 VNAA0103019 1 20010331 A 5610 SPSDO328311 WINDOW DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT CRACKED A VNAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 426JS 3649 0 3038 DURING CLIMBOUT THE FLIGHT CREW REPORTED THAT THE FIRST OFFICERS SIDE WINDOW HAD CRACKED. THE FLIGHT CREW RETURNED TO T HE FIELD AND MADE AN UNEVENTFUL LANDING. MAINTENANCE REPLACED THE SIDE WINDOW IN ACCORDANCE WITH DORNIER MAINTENANCE MA NUAL 56-10-00. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001042600209 20010426 00209 NM 2001 4 26 VNAA0103018 1 20010330 A 3350 362624 LIGHT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN INOPERATIVE A VNAA K NONE L NO TEST NR NOT REPORTED 1 GL 07 442JS 3060 THE FLIGHT CREW REPORTED THAT THE EMERGENCY FLOOR PATHWAY LIGHT WOULD NOT ILLUMINATE ADJACENT TO THE CABIN SEAT ROW 4 POSITION. MAINTENANCE REPLACED THE FLOOR PATHWAY LIGHT STRIP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-12. O PERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001042600210 20010426 00210 NE 2001 4 26 VNAA0104003 2 20010405 A 7532 311671504 BLEED VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 460PS 12714 2624 3061 AS THE FLIGHT CREW APPLIED TAKEOFF POWER THE RIGHT ELECTRONIC ENGINE CONTROL UNIT WOULD FAIL. THE FLIGHT CREW EXITED TH E RUNWAY WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT ENGINE INTERCOMPRESSOR BLEED VAVLE IN ACCORDANC E WITH DORNIER MAINTENANCE MANUAL 75-10-00. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001042600211 20010426 00211 2001 4 26 GLBA2001074 4 20010402 A 3416 066306200 ALTIMETER BEECH 1900 1900D 1154162 CE COCKPIT FAILED A GLBA A UNSCHED LANDING I FLT. ATTITUDE INST. CL CLIMB 1 CE 01 247GL 94 94 UE247 CAPTAINS ALTIMETER FAILED INFLIGHT. REPLACED INDICATOR. 2 L 7 2 4T RT A24CE 2001042600212 20010426 00212 NM 2001 4 26 P5CA0100506 1 20010323 A 5753 SKIN BOEING 747 7472U3B NM T/E FLAP CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 923FT 22769 DAMAGE FOUND ON LT WING, T/E OUTBOARD FOREFLAP O/B AREA LEADING EDGE CHAFED. REPAIRED PER SRM 51-40-15. 2 L 7 4 4F RT A20WE 2001042600213 20010426 00213 NM 2001 4 26 P5CA0100473 1 20010226 A 5313 STRINGER BOEING 747 7472U3B NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 922FT 22768 LEVEL 1 CORROSION FOUND ON STR 51L AT STA 1000. REPAIRED PER SRM 53-10-03. 2 L 7 4 4F RT A20WE 2001042600214 20010426 00214 NM 2001 4 26 P5CA0100474 1 20010226 A 5313 STRINGER BOEING 747 7472U3B NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 922FT 22768 LEVEL 1 CORROSION FOUND STR 51R STA 1000 KWD TIE. REPAIRED PER SRM 53-10-03. 2 L 7 4 4F RT A20WE 2001042600215 20010426 00215 NM 2001 4 26 P5CA0100475 1 20010226 A 5330 SKIN BOEING 747 7472U3B NM FUSELAGE DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 922FT 22768 DENT AT 3 LOCATIONS STA 1830 TO 1840 STR 39L TO 40L. REPAIRED PER SRM 53-30-03. 2 L 7 4 4F RT A20WE 2001042600216 20010426 00216 NM 2001 4 26 P5CA0100477 1 20010226 A 5330 SKIN BOEING 747 7472U3B NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 922FT 22768 LEVEL 1 CORROSION BETWEEN STA 1700-1720 STR 50L AND51L. REPAIRED PER 53-30-03. 2 L 7 4 4F RT A20WE 2001042600217 20010426 00217 NM 2001 4 26 P5CA0100478 1 20010226 A 5330 SKIN BOEING 747 7472U3B NM FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 922FT 22768 CRACK FOUND AT BS 1000 STR 46-47 RT 1.8 LONG. REPAIRED PER S/B 747-53-2316. 2 L 7 4 4F RT A20WE 2001042600218 20010426 00218 NM 2001 4 26 P5CA0100480 1 20010226 A 5320 INTERCOSTAL BOEING 747 7472U3B NM FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 922FT 22768 CRACK 2.25 INCH FOUND ON INTERCOSTAL BS 434 STR 26. REPAIRED PER SRM 53-30-02. 2 L 7 4 4F RT A20WE 2001042600219 20010426 00219 NM 2001 4 26 P5CA0100481 1 20010220 A 5320 PANEL BOEING 747 7472U3B NM BULKHEAD CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 922FT 22768 CRACK FOUND ON CANTED PRESSURE BULKHEAD LEFT CLOSURE PANEL AT WEB AND DOUBLER STA 1240 LBL 75. REPAIRED PER 8110-3 AND SRM 51-10-01. 2 L 7 4 4F RT A20WE 2001042600220 20010426 00220 NM 2001 4 26 P5CA0100509 1 20010323 A 5330 SKIN BOEING 747 7472U3B NM FUSELAGE DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 923FT 22769 FUSELAGE SKIN DENTED AT BS 2309-STRINGER 22 RIGHT, BS 2318-STRINGER 22 LEFT, BS 2324-STRINGER 21 LEFT. REPAIRED PER SRM 51-40-01. 2 L 7 4 4F RT A20WE 2001042600221 20010426 00221 WP 2001 4 26 AALA20010596 1 20010323 A 3350 LAMP DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7528A 49920 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 23D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 23D. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600222 20010426 00222 WP 2001 4 26 AALA20010595 1 20010323 A 3350 8034001 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7526A 49918 DFW - FOUND DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT CABIN DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600223 20010426 00223 WP 2001 4 26 AALA20010601 1 20010326 A 3350 LAMP DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 442AA 49468 TUL - FOUND DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT AT SEAT 15D TOO BRIGHT. REPLACED EMERGENCY EXIT LIGHT AT SEAT 15D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600224 20010426 00224 WP 2001 4 26 AALA20010608 1 20010323 A 3350 LAMP DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14551 53033 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 21D TOO BRIGHT. REPLACED EMERGENCY EXIT LIGHT AT SEAT 21D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600225 20010426 00225 WP 2001 4 26 AALA20010607 1 20010320 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 221AA 49172 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 16D BROKEN. REPLACED EMEGENCY EXIT LIGHT ASSEMBLY AT S EAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600226 20010426 00226 NM 2001 4 26 AALA20014013 1 20010309 A 5753 BEARING BOEING 777 777223 1385213 NM TE FLAPS LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 775AN 29584 AFW - FOUND RIGHT INBOARD FLAP OUTBOARD SUPPORT FITTING OUTBOARD TOP MOUNT BEARING LOOSE. REMOVED GOUGES AND REAM BORE TO 1.81-1.84 INCH DIAMETER. FABRICATE REPAIR BUSHING PER REF REPAIR 5-1 WITH THE FOLLOWING DEVIATIONS. BUSHING WALL TH ICKNESS TO BE A MINIMUM OF 0.30, SHANK .255 INCH. OMIT PENETRANT INSPECTION PRIOR TO NICKEL STRIKE/CAD PLATE. REAM BUS HING TO 1.750 INCH DIAMETER AFTER INSTALLATION. (M) 2 L 7 2 4F RT T00001SE 2001042600227 20010426 00227 WP 2001 4 26 AALA20010371 1 20010305 A 3350 HARNESS DOUG DC9 DC982 3022082 WP AFT AIRSTAIR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7530 49922 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT HAR NESS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600228 20010426 00228 WP 2001 4 26 AALA016029 1 20010315 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 871RA 49788 RNO-CCI- FOUND SEATS 24-32 EMERGENCY LIGHT INOPERATIVE. FOUND SHORTED BLACK WIRE AT SEAT 30FED. REPAIRED, SYSTEM OPS C HECKS GOOD PER MM. (M) 2 L 7 2 4F RT A6WE 2001042600229 20010426 00229 WP 2001 4 26 AALA016031 1 20010320 A 2170 1808492 COALESCER BAG DOUG DC9 DC983 3022083 WP A/C BAY CONTAMINATED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 881RA 49941 SJC - CREW REPORTED UNKNOWN PETROLEUM SMELL IN FLIGHT COMING FROM ROW 7. DECLARED EMERGENCY. PER CREW DEBRIEF SUSPECT PASSENGER HAD BUTANE LIGHTER OR REFILL THAT LEAKED. MAINTENANCE CHANGED COALESCER BAGS AND ACCOMPLISHED PACK CHECK. (M ) 2 L 7 2 4F RT A6WE 2001042600230 20010426 00230 WP 2001 4 26 AALA016030 1 20010312 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN CHAFED A O OTHER L NO TEST NR NOT REPORTED 1 SW 21 871RA 49788 LAX - EMERGENCY SEAT MOUNT LIGHTS STAY ON ROW 28-31. REPAIRED CHAFED WIRE AT SEAT 29 FED. ALSO, RELACED CHARGER (P/N 2 60BC1011) AT AFT ENTRY DOOR. (M) 2 L 7 2 4F RT A6WE 2001042600231 20010426 00231 2001 4 26 AALA016033 4 20010316 A 2565 D29985103 SLIDE DOUG MD90 MD9030 3023690 NM AFT GALLEY DOOR DISCHARGED A AALA O OTHER O OTHER NR NOT REPORTED 1 SW 21 901RA 53489 LAX-CCI - AFT GALLEY SERVICE DOOR SLIDE PRESSURE GAUGE NEEDLE IS OUT OF GREEN ZONE. REMOVED AND REPLACED AFT GALLEY SER VICE DOOR SLIDE. (M) 2 L 7 2 4F RT A6WE 2001042600232 20010426 00232 WP 2001 4 26 AALA016034 1 20010323 A 3350 BR9661105 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 832RA 53044 CCI-RNO - L1 EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. OPS CHECKS NORMAL. (M) 2 L 7 2 4F RT A6WE 2001042600233 20010426 00233 WP 2001 4 26 AALA016035 1 20010323 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 21 832RA 53044 CCI-RNO - EMERGENCY EXIT LIGHT AT SEAT 1EF INOPERATIVE. REPAIRED BROKEN WIRE TO 1EF EMERGENCY EXIT LIGHT ASSEMBLY. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 2001042600234 20010426 00234 WP 2001 4 26 AALA016032 1 20010321 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 823RA 49889 DURING ENGINE START EMERGENCY LIGHTS ARM AND CHARGE CIRCUIT BREAKER AT OVERHEAD A-14 POPPED. REPLACED SWITCH S-387, CIR CUIT BREAKER B1-21. ALSO, REPLACED BATTERY PACK ASSEMBLY AFT CATWALK. EMERGENCY LIGHT SYSTEM OPS CHECKS NORMAL. (M) 2 L 7 2 4F A6WE 2001042600235 20010426 00235 WP 2001 4 26 20010426AP001 1 20010321 A 3350 S387 SWITCH DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 823RA 49889 DURING ENGINE START EMERGENCY LIGHTS ARM AND CHARGE CIRCUIT BREAKER AT OVERHEAD A-14 POPPED. REPLACED SWITCH S-387, CIR CUIT BREAKER B1-21. ALSO, REPLACED BATTERY PACK ASSEMBLY AFT CATWALK. EMERGENCY LIGHT SYSTEM OPS CHECKS NORMAL. REF A ALA016032. (M) 2 L 7 2 4F A6WE 2001042600236 20010426 00236 WP 2001 4 26 20010426AP002 1 20010321 A 3350 B141 CIRCUIT BREAKER DOUG DC9 DC982 3022082 WP CABIN TRIPPED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 823RA 49889 DURING ENGINE START EMERGENCY LIGHTS ARM AND CHARGE CIRCUIT BREAKER AT OVERHEAD A-14 POPPED. REPLACED SWITCH S-387, CIR CUIT BREAKER B1-21. ALSO, REPLACED BATTERY PACK ASSEMBLY AFT CATWALK. EMERGENCY LIGHT SYSTEM OPS CHECKS NORMAL. REF A ALA016032. (M) 2 L 7 2 4F A6WE 2001042600237 20010426 00237 SO 2001 4 26 C2XA01BT031 1 20010309 A 7100 14531138401 TUBE EMB 145 EMB145 SO NR 1 ENGINE LEAKING A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SW 27 16594 145072 EWR - FLT 3811 - CREW REPORTED NR 1 BLEED VALVE LIGHT AND LOST NR 1 ENGINE SHORTLY AFTER TAKEOFF. AIRCRAFT AIR RETURNED TO EWR SAFELY. MAINTENANCE TROUBLESHOT NR 1 ENGINE SHUTDOWN AND REMOVED AND REPLACED NR 1 ENGINE 9TH STAGE CHECK VALVE AND BLEED AIR TUBE. AIRCRAFT RAN AND OPS CHECKED GOOD. RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001042600238 20010426 00238 SO 2001 4 26 C2XA01BT030 1 20010302 A 7100 14531138401 TUBE EMB 145 EMB145LR SO NR 1 ENGINE FAULTY A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SW 27 16954 145072 EWR - FLT 3811 - CREW REPORTED NR 1 BLEED VALVE LIGHT AND LOST NR 1 ENGINE SHORTLY AFTER TAKEOFF. AIRCRAFT AIR RETURNED TO EWR SAFELY. MAINTENANCE TROUBLESHOT NR 1 ENGINE SHUTDOWN AND REMOVED AND REPLACED NR 1 ENGINE 9TH STAGE CHECK VALVE AND BLEED AIR TUBE. AIRCRAFT RAN AND OPS CHECKED GOOD. RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001042600239 20010426 00239 EA 2001 4 26 20010426AP003 2 20010318 A 7532 BLEED VALVE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA RT ENGINE FAILED A GUUA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 19 152GA UC143 FLT 9363 - FLL/EYW - EN ROUTE TO EYW, SHUTDOWN RIGHT ENGINE DUE TO BAD SURGING OF ENGINE, PLUS/MINUS 700 LBS OF TORQUE. TROUBLESHOT RIGHT ENGINE AND FOUND BLEED VALVE CLOSING EARLY. RECLASSED BLEED VALVE. PERFORMED ENGINE RUNS. OPS CHEC K NORMAL. NO EVIDENCE OF SURGING OBSERVED. (M) 2 L 7 2 4T 4 T RT A24CE E4EA 2001042600240 20010426 00240 NM 2001 4 26 BJNA010304 1 20010326 A 3350 1012721 LIGHT BOEING 737 737214 138446R NM CABIN INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 457TM 20156 FOUND ROW 12 AISLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT AT ROW 12 AISLE, OPS CHECK NORMAL IAW BMM 33-51-11. (M) 2 L 7 2 4F A16WE 2001042600241 20010426 00241 NM 2001 4 26 BJNA010305 1 20010328 A 3350 6013211 BATTERY BOEING 737 737214 138446R NM CABIN INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 NM 05 457TM 20156 FOUND LEFT ROW 1 THROUGH 6 SEATS, INOPERTIVE EMERGENCY EXIT LIGHTS. REMOVED AND REPLACED BATTERY POWER SUPPLY UNIT PER BMM 33-51-11, OPS CHECK NORMAL. (M) 2 L 7 2 4F A16WE 2001042600242 20010426 00242 NM 2001 4 26 BJNA010303 1 20010313 A 3350 B99851 GUARD BOEING 737 737282 13844AT NM LIGHT SWITCH BROKEN A BJNA K NONE L NO TEST IN INSP/MAINT 1 NM 05 233TM 23043 FOUND EMERGENCY LIGHT SWITCH GUARD SPRING BROKEN. REMOVED AND REPLACED GUARD ON EMERGENCY LIGHT SWITCH P5 PANEL 33-5-01 , OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2001042600243 20010426 00243 NM 2001 4 26 BJNA010301 1 20010310 A 3350 LIGHT BOEING 737 737282 13844AT NM CABIN INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 NM 05 233TM 23043 EMERGENCY FLOOR TRACK FORWARD SECTION INOPERATIVE. CLEANED CONNECTOR ON POWER SUPPLY, OPS TESTED PER LOCTITE LUMINESCEN T SYSTEM COMPONENT MANUAL 33-50-01. (M) 2 L 7 2 4F RT A16WE 2001042600244 20010426 00244 NM 2001 4 26 BJNA010302 1 20010310 A 2810 SEAL BOEING 737 737282 13844AT NM ACCESS PANEL LEAKING A BJNA O OTHER K FLUID LOSS CR CRUISE 1 NM 05 789TM 23046 FUEL LEAKING FROM RIGHT WING IN FLIGHT, ALSO ON GROUND FROM OUTSIDE INSPECTION PANEL. REMOVED ACCESS PANEL AT SURGE TAN K FOUND SEAL COMING LOOSE, CLEANED PANEL RESEALED AND CURED SEALANT FOR 4 HOURS. REINSTALLED ACCESS PANEL PER MM 28-11- 011-4, LEAK CHECKED GOOD. (M) 2 L 7 2 4F RT A16WE 2001042600245 20010426 00245 2001 4 26 WRLA200106 4 20010319 A 2565 5WD230100201 SLIDE DOUG DC10 DC1030 3023501 WP PAX DOOR DEPLOYED A WRLA K NONE L NO TEST IN INSP/MAINT 1 EA 27 14075 46922 DEPLOYED L1 SLIDE PER WORLD AIRWAYS WORK CARD NON ROUTINE TASK CARD AND DC-10 AIRCRAFT MAINTENANCE MANUAL. SLIDE FAILED TO FULLY DEPLOY DUE TO 2 EACH RETENTION CABLES BEING HUNG UP IN THEIR RETAINERS, ALSO DUE TO THE FAILURE TO FULLY DEPLO Y, THE PRESSURE RELIEF VALVE OPENED RELEASING PRESSURE FROM THE SLIDE. WHEN THE SLIDE CABLES WERE RELEASED, THE SLIDE F ELL OPEN, HANGING LOOSELY FROM THE SIDE OF THE AIRCRAFT. SLIDE LAST OVERHAULED 06-2000. REMOVED AND REPLACED L1 DOOR S LIDE. (M) 2 L 7 3 4F A22WE 2001042600246 20010426 00246 NM 2001 4 26 GAIA01113OP 1 20010330 A 3350 106004110 LIGHT BOEING 727 727251 138408H NM CABIN INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 278US 21157 DURING A ROUTINE INSPECTION BEING PERFORMED AT PDX, IT WAS DISCOVERED THAT THE EMERGENCY LIGHT ASSEMBLY AT THE L1 DOOR A PPEARS TO BE DISCHARGED. REMOVED AND REPLACED THE L1 DOOR EMERGENCY LIGHT ASSEMBLY. OPERATIONALLY CHECKED NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001042600247 20010426 00247 NM 2001 4 26 UIEA01030 1 20010326 A 5730 65B10534149 PANEL BOEING 747 7472D7B 1384803 NM LT WING DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 524MC 78323 21784 DURING ROUTINE INSPECTION, FOUND LEFT SIDE UNDER WING VAPOR BARRIER PANEL DELAMINATED IN SEVERAL AREAS FROM LBL 29.98 TO 103.95. DELAMINATED AREAS SANDWICHED WITH ALUMINUM PLATES AND THROUGH BOLTED. REPAIR AREA TO BE REINSPECTED FOR STRUC TURAL INTERGRITY AND SECURITY AT EVERY 2A CHECK. PANEL REPLACEMENT NOT TO EXCEED 18 MONTHS FROM 3/26/01. (M) 2 L 7 4 4F RT A20WE 2001042600248 20010426 00248 NM 2001 4 26 UIEA01028 1 20010326 A 5311 65B046002 FRAME BOEING 747 7472D7B 1384803 NM FUSELAGE DENTED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 524MC 78323 21784 DURING ROUTINE INSPECTION, FOUND BS 1780 FRAME DENTED AND DEFORMED AT STRINGER 15R. TRIMMED AWAY DAMAGED AREA. FABRICA TED FILLER, NEW SHEAR TIE, REPAIR DOUBLE AND SPLICES. INSTALLED PER STANDARD PRACTICES. (M) 2 L 7 4 4F RT A20WE 2001042600249 20010426 00249 NM 2001 4 26 UIEA01029 1 20010326 A 5330 SKIN BOEING 747 7472D7B 1384803 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 524MC 21784 DURING ROUTINE HFEC INSPECTION, FOUND SKIN CRACKED .33 INCH AT RADIUS CUT OUT, UPPER FORWARD CORNER OF LOWER LOBE AFT CA RGO COMPARTMENT DOOR FRAME, BS 1815, AT STRINGER 15R. TRIMMED AWAY CRACK AREA FABRICATED FILLER AND REPAIR DOUBLERS PE R SRM 53-30-03 FIG 60 TYPE 2 AS REPAIR REFERENCE SCHEME. INSTALLED PER STANDARD PRACTICES. (M) 2 L 7 4 4F RT A20WE 2001042600250 20010426 00250 EA 2001 4 26 ASOA01027 1 20010310 A 5610 NP1393215 WINDSHIELD CNDAIR CL600 CL6002B19 EA CABIN CRACKED A ASOA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 11 858AS 1886 7417 FLT 4496 - CAPTAINS FRONT WINDSHIELD CRACKED WHILE ON THE GROUND AFTER FLIGHT FROM DFW TO CHS. MAINTENANCE REMOVED AND REPLACED CAPTAINS FRONT WINDSHIELD. HEATING AND PRESSURIZATION TESTS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001042600251 20010426 00251 SO 2001 4 26 MASA01012 1 20010125 A 3030 M6106 RELAY EMB 145 EMB145LR SO E/E BAY FAILED A MASA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 831MJ 145273 FLT 9519 - BHM-DCA - RETURNED TO FIELD AFTER THE COCKPIT STARTED FILLING UP WITH SMOKE. AN EMERGENCY WAS DECLARED AND T HE AIRCRAFT MADE AN UNEVENTFUL LANDING. MX TROUBLESHOT AND FOUND THE RELAY PROBE HEATER CONTROL RELAY SHORTED. MAINTEN ANCE IN BHM PULLED AND BANDED THE CIRCUIT BREAKER. THE DISCREPANCY WAS MEL''D. IN DCA MAINTENANCE REMOVED AND REPLACED THE RELAY AND SOCKET. OPS CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001042600252 20010426 00252 WP 2001 4 26 AALA20010562 1 20010319 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14551 53033 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 13D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 13D. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600253 20010426 00253 WP 2001 4 26 AALA20010561 1 20010317 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN SHORTED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 513AA 49890 DFW - FLT 1674 - EN ROUTE SEA-DFW, PASSENGER DETECTED SMOKE AT ROW 19DE OVERHEAD LIGHT. TURNED OVERHEAD LIGHT OFF. LAN DED DFW WITHOUT FURTHER INCIDENT. INSPECTED LIGHT ASSEMBLY AND WIRING. NO DEFECTS NOTED. NO SMOKE OR ODOR NOTED. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600254 20010426 00254 2001 4 26 AALA20010556 4 20010310 A 3421 4056510903 DISPLAY DOUG DC9 DC982 3022082 WP COCKPIT FAILED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 455AA 49560 DTW - FLT 494 - EN ROUTE ORD-DTW, DETECTED SMOKE BEHIND CAPTAINS ATTITUDE INDICATOR. LANDED DTW WITHOUT FURTHER INCIDEN T. REPLACED CAPTAINS SYMBOL GENERATOR AND CAPTAINS PRIMARY FLIGHT DISPLAY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M ) 2 L 7 2 4F A6WE 2001042600255 20010426 00255 WP 2001 4 26 AALA20010525 1 20010316 A 3350 LAMP DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 276AA 49273 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 7D TOO BRIGHT. REPLACED EMERGENCY EXIT LIGHT AT SEAT 7 D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001042600257 20010426 00257 NM 2001 4 26 AALA20010543 1 20010310 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 891AA 22007 TUL - FOUND DENT AND GOUGE IN SKIN STATION 501 BELOW STRINGER 28R DEPTH OF GOUGE OUT OF LIMITS DYE CHECKED GOUGE. NO CR ACKS FOUND. INSTALLED DOUBLER AT STATION 501 BELOW STRINGER 28R PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 2001042600258 20010426 00258 NM 2001 4 26 AALA20010544 1 20010315 A 5711 SPAR BOEING 727 727223 1384074 NM WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 891AA 22007 TUL - FOUND CORROSION ON LOWER CHORD OF FRONT SPAR BELOW ACTUATOR FOR THE NR 2 SLAT, WS 629. REMOVED CORROSION AND INST ALLED DOUBLER STRAP PER SRM 57-30-00. (M) 2 L 7 3 4F A3WE 2001042600259 20010426 00259 NM 2001 4 26 AALA20010545 1 20010312 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 891AA 22007 TUL - FOUND LOWER HINGE ON FORWARD ENTRY DOOR BODY SKIN CRACKED. ROUTED OUT CRACK ON LOWER HINGE OF FORWARD ENTRY DOOR, INSTALLED DOUBLER PER S/B 727-53-198. (M) 2 L 7 3 4F A3WE 2001042600260 20010426 00260 NM 2001 4 26 AALA20010547 1 20010315 A 5310 STRUCTURE BOEING 727 727223 1384074 NM FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 891AA 22007 TUL - FOUND 2ND FASTENER HOLE ABOVE CREASE ANGLE STATION 760.95 ELONGATED ESO REQUIRED. REPAIRED HOLE AT STATION 760.95 PER ESO 11697, DATED 3-14-2001. (M) 2 L 7 3 4F A3WE 2001042600261 20010426 00261 NM 2001 4 26 AALA20010548 1 20010315 A 5711 SPAR CAP BOEING 727 727223 1384074 NM WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 891AA 22007 TUL - FOUND NR 6 L/E FLAP GAP PANEL SPAR CAP CORRODED. INSTALLED DOUBLER PER BOEING REPAIR DOCUMENT 57-30-00-2, PATES 1 -3. (M) 2 L 7 3 4F A3WE 2001042600262 20010426 00262 NM 2001 4 26 AALA20010541 1 20010311 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 891AA 22007 TUL - FOUND DENT IN SKIN, STATION 410 BELOW STRINGER 24L, ADL NR 0029. INSTALLED DOUBLER STATION 410 BELOW STRINGER 24L PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 2001042600263 20010426 00263 SO 2001 4 26 SWIA972479 1 20010326 A 2750 FLAP EMB 120 EMB120RT SO PWA 118 PW118 NE WING MALFUNCTIONED A SWIA K NONE F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 130G 120130 OUTBOARD FLAPS DO NOT EXTEND PAST 35 DEGREES WHEN SELECTED TO 45 DEGREES. INSPECTED OUTBOARD FLAPS AND TRACK SYSTEM. ALL FOUND GOOD. CLEANED CONNECTORS AT BOTH LEFT AND RIGHT ACTUATORS. PERFORMED SEVERAL FUNCTIONAL CHECKS WITH NO FAULT S FOUND. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042600264 20010426 00264 EU 2001 4 26 C2XA01CL075 1 20010405 A 3260 842503A PSEU AEROSP ATR42 ATR42320 8680930 EU RT MLG FAILED A C2XA O OTHER N FALSE WARNING AP APPROACH 1 SW 27 34817 20503 20503 152 CLE FLIGHT 3238 THE CREW REPORTED THE RIGHT MAIN GEAR UNLOCK LIGHT ILLUMINATED INTERMITTENTLY DURING FLIGHT. THE AIRCRA FT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT. OPERATIONA L CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A53EU 2001042600265 20010426 00265 EU 2001 4 26 C2XA01BT053 1 20010404 A 5410 S5411061920300 CHANNEL AEROSP ATR42 ATR42320 8680930 EU RT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 25811 094 DURING C-CHECK INSPECTION FOUND RIGHTHAND LOWER NACELLE HAS THE LEFTHAND UPPER CHANNEL CRACKED. MAINTENANCE FABRICATED NEW EDGING IAW ATR42 SRM 54-12-61 FIGURE 106 AND REMOVED AND REPLACED IAW ATR42 SRM 51-25-03. 2 H 7 2 4T RT A53EU 2001042600266 20010426 00266 EU 2001 4 26 C2XA01BT054 1 20010404 A 5410 S5411058620100 CHANNEL AEROSP ATR42 ATR42320 8680930 EU RT COWLING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 25811 094 DURING C-CHECK INSPECTION FOUND RIGHTHAND ENGINE HALF MOON COWL (446AT) HAS LEFTHAND CHANNEL CRACKED. MAINTENANCE REMOV ED THE DAMAGED CHANNEL AND NEW CHANNEL FABRICATED IAW ATR42 SRM 54-12-61 FIGURE 101. INSTALLED IAW ATR42 SRM 51-25-01. 2 H 7 2 4T RT A53EU 2001042600267 20010426 00267 EU 2001 4 26 C2XA01BT057 1 20010404 A 5330 S5337140020000 SKIN AEROSP ATR42 ATR42320 8680930 EU FUSELAGE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 25811 094 DURING C-CHECK INSPECTION FOUND THREE SCRATCHES BETWEEN FRAMES 15 AND 17 AT STRINGER 19L. MAINTENANCE REPAIRED DAMAGE I AW CONTINENTAL EXPRESS EC 5330-01153. 2 H 7 2 4T RT A53EU 2001042600268 20010426 00268 EU 2001 4 26 C2XA01BT058 1 20010403 A 3260 D22924010 PROXIMITY SWITCH AEROSP ATR42 ATR42320 8680930 EU LT MLG FAULTY A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 14821 160 EWR CO3433 CREW REPORTED LEFT UNLOCK LIGHT ILLUMINATED WITH GEAR RETRACTED ON SYSTEM NR 2 (NO DOWNLOCK INDICATION WITH GEAR EXTENDED). MAINTENANCE REMOVED AND REPLACED LEFT DOWNLOCK PROXIMITY SWITCH IAW ATR42 MM 32-61-00. OPS CHECKED GOO D. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001042600269 20010426 00269 CE 2001 4 26 DJFA00117 1 20010402 A 2163 1298362 SENSOR BEECH MU300 400A 1155402 CE CABIN PRESSURE FAILED E DJFA B EMER. DESCENT B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 EA 23 445CW RK45 AIRCRAFT WAS FLYING AT FL330, HEARD A LOUD BANG AND THE CABIN RATE NEEDLE FLUCTUATED. SUSPECTED LOST PRESSURIZATION. I NITIATED AN EMERGENCY DESCENT PROCEDURES. CABIN STARTED FILLING WITH BLACK SMOKE. ALSO NOTICED THE ACM FAIL LIGHT CAME ON. DECLARED AN EMERGENCY AND LANDED AT NEWARK WITHOUT INCIDENT. THE PROBLEM WAS CAUSED BY THE ACM COALESCER BAG FREE ZING AND THE NOISE WAS THE BYPASS VALVE POPPING OPEN. THE FREEZING OF THE COALESCER BAG WAS DO TO THE TEMP SENSOR FAILE D. 2 H 7 2 4F RT A16SW 2001042600270 20010426 00270 NM 2001 4 26 P5CA0100510 1 20010323 A 5330 SKIN BOEING 747 7472U3B NM FUSELAGE DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 923FT 22769 FUSELAGE SKIN DENTED BS 2298-STRINGER 21 RIGHT, BS 2288 TO 2300 - STRINGERS 22 TO 23 LEFT, BS 2303 - STRINGER 23 LEFT, B S 2306 - STRINGER 24 LEFT. REPAIRED PER SRM 51-40-01. 2 L 7 4 4F RT A20WE 2001042600271 20010426 00271 NM 2001 4 26 P5CA0100511 1 20010323 A 5330 SKIN BOEING 747 7472U3B NM FUSELAGE DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 923FT 22769 FUSELAGE SKIN DENTED BS 2298-STRINGER 24 LEFT, BS 2433-STRINGER 24L TO S25 LEFT, BS 2184-STRINGER 23L TO S24 LEFT, BS 21 91 - STRINGER 23L TO S24 LEFT. REPAIRED PER SRM 51-40-01. 2 L 7 4 4F RT A20WE 2001042600272 20010426 00272 NM 2001 4 26 P5CA0100512 1 20010323 A 5320 INTERCOSTAL BOEING 747 7472U3B NM FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 923FT 22769 CRACK FOUND ON INTERCOSTALS BS 1960- RBL 30, BS 1960- BL 0, BS 1960- RBL 7.5, BS 1980- LBL 37.5. REPAIRED PER SRM 53-10 -07. 2 L 7 4 4F RT A20WE 2001042600273 20010426 00273 NM 2001 4 26 P5CA0100513 1 20010323 A 5730 SKIN BOEING 747 7472U3B NM LT WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 923FT 22769 LEVEL 1 CORROSION FOUND ON LT WING L/E TOP WING SKIN WS 586 - WBL 470 BULGING AROUND FASTENERS. REPAIRED PER SRM 57-10- 01, 51-30-02. 2 L 7 4 4F RT A20WE 2001042600274 20010426 00274 NM 2001 4 26 P5CA0100515 1 20010326 A 5520 BALANCE WEIGHT BOEING 747 7472U3B NM ELEVATOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 923FT 22769 LEVEL 1 CORROSION FOUND ON BALANCE WEIGHT TWO RIGHT OUTBOARD ELEVATOR. REPAIRED PER S/L 747-55-07. 2 L 7 4 4F RT A20WE 2001042600275 20010426 00275 NM 2001 4 26 P5CA0100516 1 20010326 A 5520 BALANCE WEIGHT BOEING 747 7472U3B NM ELEVATOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 923FT 22769 LEVEL 1 CORROSION FOUND ON BALANCE WEIGHT THREE LEFT OUTBOARD ELEVATOR. REPAIRED PER S/L 747-55-07. 2 L 7 4 4F RT A20WE 2001042600276 20010426 00276 NM 2001 4 26 P5CA0100518 1 20010326 A 5313 STRINGER BOEING 747 7472U3B NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 923FT 22769 LEVEL 1 CORROSION FOUND ON BS 1765-STRINGER 49R, BS 1640-STRINGER 48L, BS 1920-STRINGER 49L. REPAIRED PER SRM 51-10-01. 2 L 7 4 4F RT A20WE 2001042600277 20010426 00277 NM 2001 4 26 P5CA0100519 1 20010326 A 5330 SKIN BOEING 747 7472U3B NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 923FT 22769 LEVEL 1 CORROSION FOUND ON FUSELAGE SKIN BS 2060-STRINGER 46R. REPAIRED PER SRM 51-10-01. 2 L 7 4 4F RT A20WE 2001042600278 20010426 00278 NM 2001 4 26 P5CA0100521 1 20010326 A 5313 STRINGER BOEING 747 7472U3B NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 923FT 22769 LEVEL 1 CORROSION FOUND ON BS 1700-STR 44 RIGHT, BS 1775- STR 48 RIGHT. SECTION REPLACED PER SRM 53-30-03. 2 L 7 4 4F RT A20WE 2001042600279 20010426 00279 NM 2001 4 26 P5CA0100522 1 20010326 A 5330 SKIN BOEING 747 7472U3B NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 923FT 22769 LEVEL 1 CORROSION FOUND ON FUSELAGE SKIN BS 1319 WL 214 AND WL 227. REPAIRED PER SRM 51010-01. 2 L 7 4 4F RT A20WE 2001042600280 20010426 00280 NM 2001 4 26 P5CA0100523 1 20010326 A 5540 BALANCE WEIGHT BOEING 747 7472U3B NM RUDDER CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 923FT 22769 LEVEL 1 CORROSION FOUND ON BALANCE WEIGHT ONE UPPER RUDDER. REPAIRED PER S/L 747-55-07. 2 L 7 4 4F RT A20WE 2001042600281 20010426 00281 NM 2001 4 26 P5CA0100524 1 20010327 A 5730 PANEL BOEING 747 747122 1384872 NM LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LT WING PANEL WBL 461 OF INBOARD AILERON HAS LOOSE FIBERGLASS. REPAIR CARRIED OUT IAW SRM 51-40-08. 2 L 7 4 4F A20WE 2001042600282 20010426 00282 NM 2001 4 26 P5CA0100525 1 20010327 A 5753 SKIN BOEING 747 747122 1384872 NM T/E FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 DELAMINATION FOUND ON RT WING INBOARD LOWER FLAP WBL 163. REPAIRED PER SRM 51-40-08. 2 L 7 4 4F A20WE 2001042600283 20010426 00283 NM 2001 4 26 P5CA0100526 1 20010327 A 5730 FAIRING BOEING 747 747122 1384872 NM WING DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 DAMAGE FOUND ON FIX FAIRING IN FRONT OF NR 6 CANOE. FAIRING REPAIRED PER SRM 51-40-08. 2 L 7 4 4F A20WE 2001042600284 20010426 00284 NM 2001 4 26 P5CA0100528 1 20010327 A 5730 PANEL BOEING 747 747122 1384872 NM RT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 RT WING PANEL BEHIND NR 1 INBOARD SPOILER WBL 264 FIBERGLASS COWLING LOOSE. FIBERGLASS PANEL REPAIRED AS PER SRM 51-40- 08. 2 L 7 4 4F A20WE 2001042600285 20010426 00285 NM 2001 4 26 P5CA0100529 1 20010327 A 5730 PANEL BOEING 747 747122 1384872 NM RT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 RT WING PANEL BEHIND NR 2 INBOARD SPOILER FIBERGLASS COMING LOOSE. FIBERGLASS PANEL REPAIRED PER SRM 51-40-08. 2 L 7 4 4F A20WE 2001042600286 20010426 00286 NM 2001 4 26 P5CA0100530 1 20010323 A 5730 PANEL BOEING 747 747122 1384872 NM LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LT WING PANEL ON L/EDGE OF FUSELAGE WBL 150 HAS LOOSE FIBERGLASS. REPAIRED CARRIED OUT PER SRM 51-40-08. 2 L 7 4 4F A20WE 2001042600287 20010426 00287 NM 2001 4 26 P5CA0100531 1 20010323 A 5730 PANEL BOEING 747 747122 1384872 NM LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LT PANEL DIRECTLY BEHIND FLYING PANEL LT WING WBL 197 HAS LOOSE FIBERGLASS. REPARIED CARRIED OUT IAW SRM 51-40-08. 2 L 7 4 4F A20WE 2001042600288 20010426 00288 NM 2001 4 26 P5CA0100532 1 20010323 A 5730 PANEL BOEING 747 747122 1384872 NM LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LT WING PANEL THAT IS BEHIND FLYING PANEL HAS FIBERGLASS COMING LOOSE STA 197. REPAIRED CARREID OUT IAW SRM 51-40-08. 2 L 7 4 4F A20WE 2001042600289 20010426 00289 EU 2001 4 26 YENA0104 1 20010405 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A YENA K NONE O OTHER IN INSP/MAINT 1 EA 15 507JB 1240 DURING WALKAROUND FOUND DAMAGE TO AIRCRAFT SKIN BETWEEN FRAMES 61-62 AND STRINGERS P41 AND P43. AIRCRAFT MAINTENANCE FE RRY FROM OAK TO JFK FOR REPAIR. ACCOMPLISHED MAJOR REPAIR PER SRM 53-00-11, FIG 202 AND 209. 2 L 7 2 4F 4 F RT A28NM E40NE 2001042600290 20010426 00290 EU 2001 4 26 C2XA01BT060 1 20010406 A 3610 CLAMP AEROSP ATR42 ATR42320 8680930 EU BLEED AIR LOOSE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 25811 094 IAD/EWR---CO3411, CREW REPORTED NR 1 ENGINE BLEED LEAK, AND BURNING SMELL NOTED IN FLIGHT. AIRCRAFT RAN AND INSPECTED A ND MAINTENANCE FERRIED TO EWR. EWR MAINTENANCE TIGHTENED DUCT CLAMP, RAN ENGINE FOR 30 MINUTES, NO FAULT NOTED AT THIS TIME IAW ATR42 MM 36-22-00. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001042600291 20010426 00291 EU 2001 4 26 C2XA01BT061 1 20010409 A 2120 UNKNOWN AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE CABIN ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 25811 094 EWR---CO3145, CREW REPORTED STRONG ODOR OF AN ELECTRICAL NATURE DURING LAST HOUR OF FLIGHT. EWR MAINTENANCE PERFORMED V ISUALLY INSPECTION OF ELECTRICAL RELAY RACKS IAW ATR42 WIRING MANUAL CHAPTER 20 CHECKS GOOD. VISUALLY INSPECTED ENGINE( S) NR 1 AND 2 BLEED DUCTING, RAN ENGINES WITH NR 1 PACK ON. ALL CHECKS GOOD IAW ATR42 JIC 72-00-00. AIRCRAFT RELEASED TO SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2001042600292 20010426 00292 NM 2001 4 26 SWAA010953 1 20010329 A 5312 6546568 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND BS 1016 BULKHEAD WEB SPLICE CRACKED AT AFT SIDE, STR 7R, FIRST TWO FASTENER HOLES FROM C ENTER RING. REPAIRED BULKHEAD WEB PER SRM. 2 L 7 2 4F A16WE 2001042600293 20010426 00293 WP 2001 4 26 AT0100121 1 20010328 A 2170 COALESCER BAG DOUG DC9 DC932 3022066 WP A/C BAY DIRTY A ZZDA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 SO 15 839AT 47089 AIRCRAFT HAD CHEMICAL SMELL AND AFT LEFT SMOKE DETECTORS SOUNDED. REPLACED BOTH COALESCER BAGS AND RAN ENGINES. 2 L 7 2 4F A6WE 2001042600294 20010426 00294 NM 2001 4 26 CALA0100282 1 20010406 A 5330 SKIN BOEING 737 737524 1384721 NM FUSELAGE GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17627 27531 INSPECTION FOUND UPPER RT AND LT AFT FUSELAGE SKIN GOUGED BETWEEN RUDDER SEAL AND VORTEX GENERATOR AT STA 1104. DOUBLER S WERE INSTALLED IAW SRM 53-00-01, FIGURE 202. 2 L 7 2 4F RT A16WE 2001042600295 20010426 00295 NM 2001 4 26 CALA0100283 1 20010406 A 5320 WEB BOEING 737 7373T0 1384582 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND AFT CARGO DOOR AFT LOWER FRAME WEB DENTED AT STA 847. THE DENTED AREA WAS REMOVED AND A NEW REPAIR WEB WAS INSTALLED IAW SRM 51-70-13 AND 51-40-02. 2 L 7 2 4F RT A16WE 2001042600296 20010426 00296 WP 2001 4 26 CALA0100284 1 20010406 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND FORWARD ENTRY SUBFLOOR CORRODED AT FS 218 - 225, LBL 42. A DOUBLER WAS INSTALLED IAW SRM 53-20-0 AND 5 1-30-2. 2 L 7 2 4F A6WE 2001042600297 20010426 00297 NM 2001 4 26 CALA0100286 1 20010406 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND FLOOR SUPPORT CORRODED AROUND SCREW HOLES AT STA 951, RBL 24 - 48. THE FLOOR SUPPORT WAS REMOVED AND R EPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001042600298 20010426 00298 NM 2001 4 26 CALA0100287 1 20010406 A 5551 ATTACH FITTING BOEING 737 7373T0 1384582 NM HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND RT UPPER FORWARD HORIZONTAL STABILIZER ATTACH FITTING FWD AND AFT BUSHINGS HAD CORROSION BETWEEN BUSHIN GS AND FITTINGS. NEW OVERSIZED BUSHINGS WERE INSTALLED IAW SRM 55-10-06. 2 L 7 2 4F RT A16WE 2001042600299 20010426 00299 NM 2001 4 26 CALA0100288 1 20010406 A 5330 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND EXTERIOR FUSELAGE SKIN DENTED BELOW LAP SEAM AT STA 1010, S20R. THE DENTED AREA WAS CUT OUT AND A REPA IR PLATE WAS INSTALLED IAW SRM 53-00-01, FIGURE 202 AND 207. 2 L 7 2 4F RT A16WE 2001042600300 20010426 00300 NM 2001 4 26 CALA0100289 1 20010406 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND GOUGES ON TOP OF SEAT TRACK AT STA 344-400, LBL 25. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53 -00-52. 2 L 7 2 4F RT A16WE 2001042600301 20010426 00301 NM 2001 4 26 CALA0100290 1 20010406 A 5315 FLOORBEAM BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17627 27531 INSPECTION FOUND FLOORBEAM CORRODED AROUND FASTENER HOLES AT STA 947, LBL 20.5. A REPAIR WAS INSTALLED IAW ECRA 5320-01 668. 2 L 7 2 4F RT A16WE 2001042600302 20010426 00302 NM 2001 4 26 CALA0100293 1 20010406 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND ANGLED FLOOR SUPPORT CORRODED AT AFT END AT STA 986.5-1006, RT SIDE. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001042600303 20010426 00303 NM 2001 4 26 CALA0100294 1 20010406 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM LAVATORY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND AFT RT LAV FORWARD WALL SUPPORT CORRODED AT I/B END. THE WALL SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001042600304 20010426 00304 NM 2001 4 26 CALA0100295 1 20010406 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND AFT RT LAV FLOOR SUPPORT BEAM CORRODED AROUND FASTENER HOLES AT STA 998-1016, RBL 36. THE FLOOR SUPPOR T BEAM WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001042600305 20010426 00305 NM 2001 4 26 CALA0100297 1 20010406 A 5320 THRESHOLD BOEING 737 7373T0 1384582 NM R2 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND R-2 DOOR THRESHOLD CHORD CORRODED AT STA 977. THE R-2 DOOR THRESHOLD CHORD WAS REMOVED AND REPLACED IA W SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001042600306 20010426 00306 NM 2001 4 26 CALA0100299 1 20010406 A 5311 FRAME BOEING 737 737524 1384721 NM FUSELAGE CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17627 27531 INSPECTION FOUND FRAME CHAFED BY APU PNEUMATIC DUCT AFT OF STA 1040. INSTALLED DOUBLERS IAW ECRA 5310-04124. 2 L 7 2 4F RT A16WE 2001042600307 20010426 00307 NM 2001 4 26 CALA0100300 1 20010406 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM LAVATORY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND FORWARD LOWER WALL SUPPORT OF AFT LT LAV CORRODED AT STA 996. THE WALL SUPPORT WAS REMOVED AND REPLACE D IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001042600308 20010426 00308 NM 2001 4 26 CALA0100301 1 20010406 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 986.5-1006, LBL 10-20 AND AT STA 996-1006, LBL 36. THE FLOOR SUPPORTS W ERE REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001042600309 20010426 00309 NM 2001 4 26 CALA0100302 1 20010406 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND FLOOR SUPPORT CORRODED AT SCREW HOLES AT STA 1006-1016, LBL 36. THE FLOOR SUPPORT WAS REMOVED AND REPL ACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001042600310 20010426 00310 NM 2001 4 26 CALA0100303 1 20010406 A 5320 WEB BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND LEFT O/B SUBFLOOR CORRODED AT STA 986-1016. THE SUBFLOOR WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001042600311 20010426 00311 NM 2001 4 26 CALA0100305 1 20010406 A 5320 STRAP BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND METAL STRAP CORRODED AT EYEBOLT AREA OF TANK HOLD DOWN ROD AT STA 1016, LBL 27. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001042600312 20010426 00312 NM 2001 4 26 CALA0100306 1 20010406 A 5320 STRAP BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND METAL STRAP CORRODED BETWEEN STA 1006 AND APB, LBL 18. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-1 0-02. 2 L 7 2 4F RT A16WE 2001042600313 20010426 00313 NM 2001 4 26 CALA0100307 1 20010406 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND AFT RIGHT LAV FLOOR SUPPORTS CORRODED AROUND FASTENER HOLES AT STA 1006-1016, RBL 18 AND RBL 27. THE F LOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001042600314 20010426 00314 NM 2001 4 26 CALA0100309 1 20010407 A 5743 ATTACH FITTING BOEING 737 7373T0 1384582 NM RT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND RIGHT MLG STAB LINK AFT ATTACH FITTING ON GEAR BEAM CORRODED. THE ATTACH FITTING WAS REMOVED AND A NEW ATTACH FITTING WAS INSTALLED IAW MM 57-15-00. 2 L 7 2 4F RT A16WE 2001042600315 20010426 00315 NM 2001 4 26 CALA0100310 1 20010407 A 5320 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND A .0625 INCH CRACK AT FASTENER ON UNDER SIDE OF LEFT CREASE BEAM STIFFENER ANGLE AT STA 1000. THE CREA SE BEAM STIFFENER ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001042600316 20010426 00316 NM 2001 4 26 CALA0100311 1 20010407 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND AFT RIGHT LAV FLOOR SUPPORT CORRODED AT STA 1016, RBL 6. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IA W SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001042600317 20010426 00317 NM 2001 4 26 CALA0100312 1 20010407 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND FLOOR SUPPORT CORRODED AROUND SCREW HOLES AT STA 967-986.5, LBL 20. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND ECRA 5310-03585. 2 L 7 2 4F RT A16WE 2001042600318 20010426 00318 NM 2001 4 26 AALA20010531 1 20010314 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 789AN 30252 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ASSEMBLY AT L1 DOOR DAMAGED. REPLACED EMERGENCY EXIT LIGHT ASS EMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001042600319 20010426 00319 NM 2001 4 26 AALA20010533 1 20010318 A 3350 PIN BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 602AN 27053 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 13 INOPERATIVE. RE-SECURED EMERGENCY EXIT CONNECTOR PIN . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001042600320 20010426 00320 NM 2001 4 26 AALA20010518 1 20010317 A 3350 SPLICE BOEING 767 767223 1385123 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 334AA 22332 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 24A LOOSE CONNECTION. REPLACED EMERGENCY EXIT LIGHT SP LICE AT SEAT 24A. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001042600321 20010426 00321 NM 2001 4 26 AALA20010512 1 20010317 A 3350 LAMP BOEING 777 777223 1385213 NM CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 770AN 29578 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 3D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 3D. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001042600322 20010426 00322 NM 2001 4 26 AALA20010513 1 20010317 A 3350 LAMP BOEING 777 777223 1385213 NM CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 770AN 29578 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 4D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 4D. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001042600323 20010426 00323 NM 2001 4 26 AALA20010514 1 20010317 A 3350 LAMP BOEING 777 777223 1385213 NM CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 770AN 29578 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 27C DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 27C. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001042600324 20010426 00324 NM 2001 4 26 AALA20010515 1 20010317 A 3350 LAMP BOEING 777 777223 1385213 NM CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 770AN 29578 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 34C DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 34C. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001042600325 20010426 00325 NM 2001 4 26 AALA20010516 1 20010317 A 3350 LAMP BOEING 777 777223 1385213 NM CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 770AN 29578 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 35C DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 35C. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001042600326 20010426 00326 NM 2001 4 26 AALA20010509 1 20010317 A 3350 LAMP BOEING 777 777223 1385213 NM CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 770AN 29578 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT IGHT AT SEAT 3G DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 3G. SYST EM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001042600327 20010426 00327 NM 2001 4 26 AALA20010510 1 20010317 A 3350 LAMP BOEING 777 777223 1385213 NM CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 770AN 29578 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 36G DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 36G. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001042600328 20010426 00328 NM 2001 4 26 AALA20010493 1 20010315 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 621AM 24579 DFW - DURING OVERNIGHT MAINTENANCE, AFT EMERGENCY EXIT LIGHT AT L2 DOOR DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK AT L3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001042600329 20010426 00329 NM 2001 4 26 AALA20010488 1 20010316 A 3397 WIRE BOEING 767 767223 1385123 NM CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 21 334AA 22332 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 36B BROKEN WIRES. REPAIRED EMERGENCY EXIT LIGHT WIRES AT SEAT 36B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001042600330 20010426 00330 NM 2001 4 26 AALA20010489 1 20010316 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 334AA 22332 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L2 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTO R AT SIDE WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001082300002 20010823 00002 EU 2001 8 23 F3LA200100048 2 20010326 A 7200 ENGINE BOEING 737 7373Q8 1384670 NM CFMINT CFM56 CFM563C1 13802 EU NR 1 ENGINE MALFUNCTIONED A F3LA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 03 319FL 22365 2466 26301 726115 DURING CLIMBOUT, FLIGHT CREW REPORTED SMOKE IN COCKPIT AND CABIN. DECLARED AN EMERGENCY AND RETURNED TO DEN WITHOUT INC IDENT. MAINTENANCE REPLACED NR 1 ENGINE. AN ADDENDUM WILL BE ISSUED WHEN CAUSE OF FAILURE IS KNOW. ADDENDUM: PERFORM ED BORESCOPE INSPECTION, PERFORMANCE RUN AND ACCOMPLISHED AN ENGINE WASH. NO DAMAGE OR DEFECTS WERE FOUND. 2 L 7 2 4F 4 F RT A16WE E21EU 2001042600331 20010426 00331 NM 2001 4 26 01FDEA00230 1 20010324 A 5320 INTERCOSTAL BOEING 727 72722 1384002 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 168FE 18865 DURING ROUTINE INSP, INTERCOSTAL AT BS 738 AT THE NR 5 SEAT TRACK FOUND CRACKED. *S/D* STOP DRILLED INTERCOSTAL. REMO VED, REPLACED AND FAB PER IAW BAC 727 SRM 51-40-2. 2 L 7 3 4F A3WE 2001042600332 20010426 00332 NM 2001 4 26 AALA20010490 1 20010315 A 3350 CONNECTOR BOEING 767 767323 1385205 NM RT WING DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 370AA 25197 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT RIGHT SIDE AFT WING INOPERATIVE. CLEANED EMERGENCY EXIT LIG HT AT RIGHT WING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001042600333 20010426 00333 NM 2001 4 26 AALA20010485 1 20010314 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 327AA 22327 LAX - DURING OVERNIGHT MAINTENANCE, AFT RIGHT SIDE EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED AFT RIGHT SIDE EMERGENCY E XIT LIGHT AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001042600334 20010426 00334 NM 2001 4 26 AALA20010486 1 20010314 A 3350 400875 LAMP BOEING 767 767223 1385123 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 327AA 22327 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 31HJ INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT HOLDER ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001042600335 20010426 00335 NM 2001 4 26 AALA20010482 1 20010317 A 3397 WIRE BOEING 767 767223 1385123 NM CABIN LOOSE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 334AA 22332 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 24A/B LOOSE CONNECTION. REPAIRED EMERGENCY EXIT LIGHT SPLICE AT SEAT 24A/B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001042600336 20010426 00336 NM 2001 4 26 AALA20010386 1 20010307 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 678AN 29428 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTO R. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001042600337 20010426 00337 NM 2001 4 26 AALA20010387 1 20010307 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 678AN 29428 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 31 CONNECTOR BROKEN. REPLACED EMERGENCY EXIT LIGHT CON NECTOR AT SEAT 31. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001042600338 20010426 00338 NM 2001 4 26 AALA20010381 1 20010306 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 653A 24611 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT 16F INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT CONNECTOR AT 16F. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001042600339 20010426 00339 NM 2001 4 26 AALA20010370 1 20010306 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 366AA 25193 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 22H INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT CONNE CTOR AT SEAT 22H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001042600340 20010426 00340 NM 2001 4 26 AALA20010368 1 20010302 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 604AA 27055 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT ILGHT AT SEAT 1ABC INOPERATIVE. REPLACED OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 1ABC. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001042600341 20010426 00341 NM 2001 4 26 AALA20010399 1 20010309 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 788AN 30011 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L1 DOOR DAMAGED. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001042600342 20010426 00342 NM 2001 4 26 AALA20010400 1 20010309 A 3350 LAMP BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 788AN 30011 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT BUSINESS CLASS DIM. REPLACED EMERGENCY EXIT LIGHT AT BUSINE SS CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001042600343 20010426 00343 WP 2001 4 26 AALA20010538 1 20010308 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND CORROSION ON CUSP AT STATION 1155 LBL 48 25 BY 3 BY .040. REMOVED CORROSION, CUTOUT PIECE OF CUSP. INSTALL ED DOUBLER PER AARD 51-60-00-05. (M) 2 L 7 2 4F A6WE 2001042600344 20010426 00344 WP 2001 4 26 AALA20010539 1 20010315 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 513AA 49890 TUL - FOUND CORROSION ON METAL FLOORBOARD STATION 148 RBL 18. INSTALLED NEW SERVICEABLE FLOORBOARD AND FASTENERS AND SE ALED AROUND EDGES SRM 51-01. (M) 2 L 7 2 4F A6WE 2001042600345 20010426 00345 WP 2001 4 26 AALA016021 1 20010227 A 3350 0105606004 MODULE DOUG DC9 DC983 3022083 WP AFT FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 871RA 49788 LAX - EMERGENCY LIGHT REMAINS ON AT ROW 28. REPLACED LEFT AFT EMERGENCY LIGHT MODULE. ACCOMPLISHED REQUIRED CHECKS MM SYSTEM CHECKED NORMAL. (M) 2 L 7 2 4F RT A6WE 2001042600346 20010426 00346 WP 2001 4 26 AALA016022 1 20010225 A 3350 BR50447 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 871RA 49788 CCI-LAX - EMERGENCY LIGHT INOPERATIVE BETWEEN SEAT ROW 28-31. BATTERY PACK ABOVE SEAT 28 REPLACED AND FUSE CHANGED AT A FT LEFT BATTERY PACK, LEFT LAVATORY POSITION. OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 2001042600347 20010426 00347 WP 2001 4 26 AALA016023 1 20010303 A 3350 4097023 LIGHT DOUG DC9 DC983 3022083 WP AFT CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 871RA 49788 LAST FOUR ROWS RIGHT SIDE OF AIRCRAFT EMERGENCY LIGHTS CAME ON AND WOULD NOT GO OUT. REMOVED AND REPLACED AFT EMERGENCY EXIT LIGHT ASSY PER MM. OPS CHECK NORMAL ON LAST FOUR ROWS RIGHT SIDE OF AIRCRAFT. (M) 2 L 7 2 4F RT A6WE 2001042600348 20010426 00348 WP 2001 4 26 AALA20016024 1 20010306 A 5220 591015933 DOOR DOUG DC9 DC987 3022087 WP EMERGENCY EXIT MISINSTALLED A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 755RA 49727 AFTER TAKEOFF, FLIGHT ATTENDANT ADVISED LOUD NOISE AD FLOW FROM LEFT AFT OVERWING EXIT. RETURNED FOR LANDING. FOUND AF T LEFT OVERWING EMERGENCY EXIT DOOR NOT PROPERLY SEATED. RE-SEATED DOOR AND PRESSURIZED AIRCRAFT TO 6 PSI. DOOR CHECKE D GOOD WITH NO LEAKS NOTED, OK FOR SERVICE. (M) 2 L 7 2 4F RT A6WE 2001042600349 20010426 00349 NM 2001 4 26 01FDEA00262 1 20010407 A 5320 SUPPORT BOEING 727 72722 1384002 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 168FE 18865 DURING ROUTINE INSP, FLOORBEAM SUPPORT STRAP AT BS 304, STR 18R, RBL 35 FOUND CRACKED. REMOVED, REPLACED AND FAB PER IA W BAC 727 SRM 51-20-1, 51-30-2. 2 L 7 3 4F A3WE 2001042600350 20010426 00350 WP 2001 4 26 USAAD01046 1 20010312 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 801US 48037 IND - THE LOW LEVEL EMERGENCY LIGHTS FAILED THE LIGHT TEST. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIE S. (M) 2 L 7 2 4F A6WE 2001042600351 20010426 00351 WP 2001 4 26 USAAD01058 1 20010321 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 812US 48092 MCO - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE, AND THE LIGHTS AT SEAT ROWS 16, 20, 25 AND 30 WERE IN THE WRONG P OSITION. MAINTENANCE REPOSITIONED THE LOW LEVEL EMERGENCY LIGHT ASSEMBLIES AND REPLACED THE BATTERIES. (M) 2 L 7 2 4F A6WE 2001042600352 20010426 00352 WP 2001 4 26 USAAD01056 1 20010320 A 3350 8732030153 MODULE DOUG DC9 DC981 3022081 WP PAX CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 819US 48099 IND - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE AFT CONTROL MODULE. (M) 2 L 7 2 4F A6WE 2001042600353 20010426 00353 WP 2001 4 26 USAAD01057 1 20010318 A 3350 4TL115 SWITCH DOUG DC9 DC981 3022081 WP PAX CABIN INTERMITTENT A USAA O OTHER O OTHER AP APPROACH 1 EA 19 813US 48093 IND-PIT - FLT 1130 - THE EMERGENCY LIGHTS CAME ON INTERMITTENTLY THE LAST 5 MINUTES OF THE FLIGHT. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT TRANSMITTER MODULE, OVERHEAD EMERGENCY LIGHT POWER SUPPLIES, AND THE FLIGHT ATTENDANT EME RGENCY LIGHT SWITCH. (M) 2 L 7 2 4F A6WE 2001042600354 20010426 00354 NM 2001 4 26 USAA010224 1 20010220 A 5313 655129814 STRINGER BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND STRINGER AND TIE CLIP CRACKED .250 INCH, BS 520 STRINGER 19L. REMOVED AND REPLACED TIE CLIP AND INSTALLED S TRINGER 18 INCH SECTION PER SRM 53-10-03, 51-10-01, 51-10-02. (M) 2 L 7 2 4F A16WE 2001042600355 20010426 00355 NM 2001 4 26 20010426AP004 1 20010220 A 5320 654576773 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 22756 CLT - FOUND STRINGER AND TIE CLIP CRACKED .250 INCH, BS 520 STRINGER 19L. REMOVED AND REPLACED TIE CLIP AND INSTALLED S TRINGER 18 INCH SECTION PER SRM 53-10-03, 51-10-01, 51-10-02. REF USAA010224. (M) 2 L 7 2 4F A16WE 2001042600356 20010426 00356 NM 2001 4 26 USAA010234 1 20010219 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND SKIN DOUBLER CRACKED 8 INCHES BY 11 INCHES, 727 PLUS 16 S 27R. INSTALLED DOUBLER PER SRM 53-30-03. (M) 2 L 7 2 4F A16WE 2001042600357 20010426 00357 NM 2001 4 26 USAA010236 1 20010219 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND FRAME CRACKED 2 INCHES, FS 767 AT STRINGER 13L. INSTALLED REPAIR DOUBLERS PART 1 AND 2 IAW SRM 53-10-4. (M ) 2 L 7 2 4F A16WE 2001042600358 20010426 00358 NM 2001 4 26 USAA010237 1 20010219 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND SKIN CRACKED 1 INCH, BS 380 AT E/E EQUIPMENT COOLING DUCT OUTLET. INSTALLED INTERIOR SKIN DOUBLER PER T/R 5 3-30-04. (M) 2 L 7 2 4F A16WE 2001042600359 20010426 00359 NM 2001 4 26 USAA010246 1 20010215 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND FLOOR FRAME CORRODED 12 SQUARE INCHES, BS 947.5 LBL 30 - RBL 49. FABRICATED T-CAP AND SPLICE PARTS PER 53-1 0-9. CORROSION LEVEL 1, TASK NR C53-107-02. (M) 2 L 7 2 4F A16WE 2001042600360 20010426 00360 NM 2001 4 26 USAA010247 1 20010215 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND FLOOR FRAME CORRODED 4 SQUARE INCHES, STATION 987.5 LBL 14, RBL 15, RBL 24. REPLACED T-CAP FROM LEFT AND RI GHT EXTREMITIES PER TYP REP 53-60-01. CORROSION LEVEL 1, TASK NR C53-107-02. (M) 2 L 7 2 4F A16WE 2001042600361 20010426 00361 NM 2001 4 26 USAA010248 1 20010203 A 5320 INTERCOSTAL BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND INTERCOSTAL CORRODED 2 SQUARE INCHES, BS 987.9, LBL 20 TO STATION 1016, LBL 6. FABRICATED NEW INTERCOSTAL P ER 51-30-0 AND 51-10-1. CORROSION LEVEL1, TASK NR C53-107-02. (M) 2 L 7 2 4F A16WE 2001042600362 20010426 00362 NM 2001 4 26 USAA010249 1 20010214 A 5320 ANGLE BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND CHORD ANGLE CRACKED .5 INCH, STATION 663 RBL 24, WL 201.5. INSTALLED REPAIR ANGLES PER DRW 65C37732, EA 689 73. (M) 2 L 7 2 4F A16WE 2001042600363 20010426 00363 NM 2001 4 26 USAA010252 1 20010215 A 5310 SHEAR TIE BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND SHEAR TIE CRACKED .5 INCH, BS 967 AT STRINGER 7L. FABRICATED AND INSTALLED NEW SHEAR TIE PER SRM 53-10-4 FI G 8. (M) 2 L 7 2 4F A16WE 2001042600364 20010426 00364 NM 2001 4 26 USAA010253 1 20010215 A 5320 693535214 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND TIE CLIP CRACKED .125 INCH, BS 616 STRINGER 1. MODIFIED PART NR INSTALLED. (M) 2 L 7 2 4F A16WE 2001042600365 20010426 00365 NM 2001 4 26 USAA010254 1 20010215 A 5320 693535214 CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND CLIP CRACKED .125 INCH, STATION 616 STRINGER 3 LEFT. MODIFIED PART NR INSTALLED. (M) 2 L 7 2 4F A16WE 2001042600366 20010426 00366 NM 2001 4 26 USAA010255 1 20010214 A 5313 STRINGER BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND STRINGER CRACKED .5 INCH, STRINGER 15L BS 520-540. REPLACED STRINGER SECTION IAW SRM 53-10-3. (M) 2 L 7 2 4F A16WE 2001042600367 20010426 00367 NM 2001 4 26 USAA010198 1 20010302 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 257AU 49060 22799 BOS - FOUND SKIN CRACKED 1.375 INCH, STATION 807 ABOVE STRINGER 19L. INSTALLED DOUBLER AT STATION 807 STRINGER 19L. (M ) 2 L 7 2 4F A16WE 2001042600368 20010426 00368 NM 2001 4 26 USAA010188 1 20010228 A 5210 WEB BOEING 737 737201 1384454 NM PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND DOOR WEB CRACKED .5 INCH, AFT SERVICE DOOR TORQUE BOX WEB BS 947 BELOW STRINGER 11R. INSTALLED DOUBLER PER TR 53-30-07A. (M) 2 L 7 2 4F A16WE 2001042600369 20010426 00369 NM 2001 4 26 USAA010199 1 20010216 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 255AU 49888 22797 BOS - FOUND SKIN CRACKED 1.5 INCH, STATION 765, STRINGER 18L. CUT OUT DAMAGE AND INSTALLED 11 INCHES BY 6.75 INCHES SOL ID RIVITS DOUBLER PER SRM 53-30-3 FIG 6. (M) 2 L 7 2 4F A16WE 2001042600370 20010426 00370 NM 2001 4 26 USAA0102000 1 20010214 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 253AU 47639 22795 BOS - FOUND SKIN CRACKED 1.375 INCH CRACK, BETWEEN STATION 747 AND 767 ABOVE STRINGER 18R. INSTALLED DOUBLER AT STATION 747 AND 767 ON STRINGER 18R AND 19R PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 2001042600371 20010426 00371 NM 2001 4 26 USAA010201 1 20010209 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 261AU 47593 22867 BOS - FOUND SKIN CRACKED .75 INCH, BETWEEN STATION 787/807 STRINGER 19L. INSTALLED DOUBLER INCORPORATED PREVIOUS PATCH PER SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 2001042600372 20010426 00372 NM 2001 4 26 USAA010221 1 20010220 A 5320 672038502 INTERCOSTAL BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND INTERCOSTAL CRACKED 1 INCH, 178 BULKHEAD, RBL 26, WL 195. MODIFIED PART INSTALLED PER EA 68934. (M) 2 L 7 2 4F A16WE 2001042600373 20010426 00373 NM 2001 4 26 USAA010222 1 20010220 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND CHORD VERTICAL CRACKED .9 INCH IN INBOARD RADIUS, RBL 5-7, WL 184, BS 178 BULKHEAD. INSTALLED VERTICAL CHOR D REPAIR PARTS PER EA 68935/EO5300V155. (M) 2 L 7 2 4F A16WE 2001042600374 20010426 00374 NM 2001 4 26 USAA010223 1 20010220 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND VERTICAL CHORD CRACKED 1 INCH OUTBOARD RADIUS AND 1.8 INCH INBOARD, BS 178 BULKHEAD, LBL 5-7, WL 184. INSTA LLED VERTICAL CHORD REPAIR PARTS PER EA 68935/EO 5300V155. (M) 2 L 7 2 4F A16WE 2001042600375 20010426 00375 NM 2001 4 26 USAA010271 1 20010213 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FLOORBEAM CORRODED 1 INCH IN SEVERAL AREAS, STATINO 312, BL 0 RBL 12, LBL 7, 32, 39. REPLACED T-CAP. (M) 2 L 7 2 4F RT A16WE 2001042600376 20010426 00376 NM 2001 4 26 USAA010312 1 20010320 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FLOORBEAM CORRODED 2 INCHES, STATION 312, BL 0, RBL 12, LBL 7, 32, 39. REPLACED T-CAP PER SRM 53-10-51. (M ) 2 L 7 2 4F RT A16WE 2001042600377 20010426 00377 NM 2001 4 26 USAA010313 1 20010320 A 5347 SEAT TRACK BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND SEAT TRACK CORRODED .250 INCH BY 1.5 INCH, BS 340, RBL 24. INSTALLED NEW SECTION PER SRM 53-00-52. (M) 2 L 7 2 4F RT A16WE 2001042600378 20010426 00378 NM 2001 4 26 USAA010314 1 20010320 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 50420 24559 CLT - FOUND FLOORBEAM T-CAP CORRODED 3 INCHES, BS 312 FROM LBL 33 TO RBL 10. SPLICED IN NEW T-CAP SECTION PER SRM 53-10 -51. (M) 2 L 7 2 4F RT A16WE 2001042700001 20010427 00001 2001 4 27 COMA0160342 4 20010324 A 2210 DAMPENER CNDAIR CL600 CL6002B19 EA AUTOPILOT MALFUNCTIONED A COMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 01 767CA 7285 RAPID YAW OSCILATIONS DURING CLIMB. COULD NOT DUPLICATE. SYSTEM TEST SATISFACTORY, NO FAULTS CODES IN COMPUTER. 2 L 7 2 4F RT A21EA 2001042700002 20010427 00002 2001 4 27 ARWA0010310 4 20010330 A 3442 GUIDE DOUG DC8 DC862 3021970 WP RADAR LOOSE A ARWA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 19 1808E 46105 RADAR WILL NOT PAINT WEATHER. AIRCRAFT DIVERTED TO MIAMI AND LANDED WITHOUT INCIDENT. TIGHTENED WAVE GUIDE; OPS CHECK NORMAL IAW MM 34-41-0. 2 L 7 4 4F 4A25 2001042700003 20010427 00003 NM 2001 4 27 01FDEA00257 1 20010407 A 3020 SENSING ELEMENT DOUG MD11 MD11F 3023600 NM NR 3 ENGINE FAULTY A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 617FE 48748 LEVEL 3 ENG 2 A-ICE DUCT ALERT IND. SHUTDOWN ENG 3. *S/D* REMOVED AND REPLACED SENSING ELEMENT D190 (LOWER SIDE) PER MD11 MM 30-22-11-4. 2 L 7 3 4F RT A22WE 2001042700004 20010427 00004 WP 2001 4 27 CNMA200100002 1 20010321 A 5410 AVB731817 FITTING DOUG DOUG DC10 DC1010 3022110 WP NR 2 PYLON BROKEN A CNMA K NONE O OTHER IN INSP/MAINT 1 SW 07 450AX 46942 DURING MAINTENANCE REMOVAL OF NR 2 ENGINE, THE LEFT AFT LIFTING FITTING WAS BROKEN CAUSING DAMAGE TO THE CENTER BOX STRU CTURE AT THE TOP OF THE ENGINE BAY OF NR 2 PYLON - ( REFERENCE DC10 IPC 54-12-02, PG 7). THE CAUSE OF THE FAILURE OF TH E LIFTING FITTING HAS NOT BEEN DETERMINED. PRELIMINARY INSPECTION OF THE FAILED FITTING SHOWS NO EVIDENCE OF FATIGUE, C RACK, OR CORROSION. ALL DAMAGE WAS REMOVED AND NEW WEB FILLER WAS FABRICATED. THE LT AVB7318-11 STIFFENER AND BOTH LT AND RT AVB7318-17 FITTINGS WERE REPLACED WITH NEW OEM PARTS. RT FITTING WAS ONLY REPLACED AS A PRECAUTION DUE TO SUSTAIN ING AN EXCESS LOAD. 2 L 7 3 4F A22WE 2001042700005 20010427 00005 NM 2001 4 27 CALA0100314 1 20010408 A 5320 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND Z-ANGLE CORRODED O/B OF AFT LAV AND GALLEY (L-2 DOOR AREA). THE Z-ANGLE WAS REMOVED AND A NEW Z-ANGLE WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001042700006 20010427 00006 NM 2001 4 27 CALA0100315 1 20010408 A 5320 WEB BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND MAIN DECK SUBFLOOR CORRODED JUST FORWARD OF AFT PRESSURE BULKHEAD AT STA 1010, LBL 4. THE SUBFLOOR WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001042700007 20010427 00007 WP 2001 4 27 TWAA0106217 1 20010401 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 906TW 49160 DURING CHECK-C MAINT FOUND INTERCOSTAL CORRODED BETWEEN STA 1237 AND 1250, LONGERON 25L. REMOVED CORROSION PER SPM 6-80 -01. PRIMED AND PAINTED PER SRM 51-10-3. INSTALLED THE INTERCOSTAL BETWEEN STA 1237 AND 1250 PER SRM 51-30-02. 2 L 7 2 4F A6WE 2001042700008 20010427 00008 WP 2001 4 27 TWAA0106218 1 20010401 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 906TW 49160 DURING CHECK-C MAINT FOUND CORROSION ON LT MEMBRANE, BETWEEN STA 1136 THRU 1155. REMOVED CORROSION AS REQUIRED PER SPM 6-80-01, PAGE 3 FIG 2. TREATED AND PRIMED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001042700009 20010427 00009 WP 2001 4 27 TWAA0106219 1 20010403 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 906TW 49160 DURING CHECK-C MAINT FOUND CABIN AUX TRACK CORRODED, LBL 38 IN, STA 1098 TO STA 1136. REPLACED CORRODED TRACK PER SRM 5 3-24-0. REINSTALLED BOLTS IN CHAIR TRACK PER SRM 51-30-1. 2 L 7 2 4F A6WE 2001042700010 20010427 00010 WP 2001 4 27 TWAA0106220 1 20010330 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT FOUND RT COCKPIT FLOOR AREA BETWEEN STA 133 TO 160, AND 26 IN RBL, MEMBRANE HAD CORROSION. REMOVED CORROSION THEN FABRICATED NEW WEB PER IPC 53-14-1. INSTALLED PER 51-30-2, 51-16-3, AND 51-70-4. 2 L 7 2 4F A6WE 2001042700011 20010427 00011 WP 2001 4 27 TWAA0106221 1 20010330 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT IN THE FWD CABIN FOUND CORROSION BELOW GALLEY DRAIN STA 148 TO 160, RBL 44 TO RBL 54. REMOVED CORR ODED MEMBRANE. FABRICATED NEW MEMBRANE PER IPC 53-14-1. INSTALLED PER 51-30-2. TREATED PER 51-10-3 AND 51-70-4. 2 L 7 2 4F A6WE 2001042700012 20010427 00012 WP 2001 4 27 TWAA0106222 1 20010330 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT BETWEEN STA 160 AND 200, 6 INCHES INBD OF PASSENGER FWD ENTRY, HAD CORROS ION ON FLANGE TOP AND BOTTOM. FABRICATED NEW FLOOR SUPPORT. REPLACED NEW FLOOR SUPPORT PER SRM 53-40-00. 2 L 7 2 4F A6WE 2001042700013 20010427 00013 WP 2001 4 27 TWAA0106224 1 20010403 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 909TW 49170 DURING CHECK-C MAIN FOUND CORROSION IN TRACK NUMBER 3, STA 1094 TO 1280. REMOVED AND REPLACED CHAIR TRACK WITH NEW FROM STA 1088 TO 1309. SPLICED AT 1088 PER SRM 53-05, FIG 4F USING SPLICES WITH HI-LOKS PER SRM 51-30-5. INSTALLED TRACK W ITH SCREWS AND NUTS TORQUED PER SRM 51-30-1. 2 L 7 2 4F A6WE 2001042700014 20010427 00014 WP 2001 4 27 TWAA0106225 1 20010404 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 906TW 49160 DURING CHECK-C MAINT FOUND AFT CABIN FLOOR TRACK CORRODED AT LBL 24, STA 1049 TO 1307, AND STA 1221 TO 1309. REMOVED SE AT TRACK FROM STA 1049 TO 1309. INSTALLED NEW SEAT TRACK WITH NEW PER 6-80-61. 2 L 7 2 4F A6WE 2001042700015 20010427 00015 WP 2001 4 27 TWAA0106226 1 20010404 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 906TW 49160 DURING CHECK-C MAINT IN FWD CABIN FOUND CORROSION ON MEMBRANE AROUND FLT ATTEND CHAIR MOUNT STA 164, BL 42L, AND AT STA 194, LBL 3 INCHES. REMOVED CORRODED MEMBRANE AND REPAIRED PER SRM 53-01 PAGE 18. TREATED AND PAINTED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001042700016 20010427 00016 WP 2001 4 27 TWAA0106227 1 20010404 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 906TW 49160 DURING CHECK-C MAINT IN THE AFT CARGO COMPT, FOUND CORROSION ON FWD SIDE OF STA 1193 FORMER, BETWEEN LONGERON 30 AND 29R . REMOVED CORROSION PER SPM 6-80-01. PAINTED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001042700017 20010427 00017 WP 2001 4 27 TWAA0106228 1 20010404 A 5345 FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 906TW 49160 DURING CHECK-C MAINT IN FWD CABIN FOUND CORROSION AROUND LAV MOUNT HOLES AT STA 219 AND BL 16L. REMOVED CORROSION PER SPM 6-80-01. PAINTED AND TREATED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001042700018 20010427 00018 WP 2001 4 27 TWAA0106229 1 20010404 A 5330 DOUBLER DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 906TW 49160 DURING CHECK-C MAINT IN THE ELECTRONIC COMPT, FOUND CORROSION ON DRAIN MAST DOUBLER AT STA 207, BETWEEN LONGERON 28R AND 29R. REMOVED CORROSION PER SPM 6-80-1. REPLACED DOUBLER PER 6-70-1. PAINTED PER SRM 51-10-3. INSTALLED FASTENERS PE R SRM 51-30-2 AND 51-30-1. 2 L 7 2 4F A6WE 2001042700019 20010427 00019 WP 2001 4 27 TWAA0106230 1 20010404 A 5320 SUPPORT BRACKET DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 906TW 49160 DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND CORROSION ON SUPPORT BRACKET AT STA 1148, ABOVE LONGERON 20R. FABRICA TED NEW SUPPORT ANGLE PER PART REMOVED USING SPM 6-70-01, FROM 7075T6 PER SRM 51-14-3 AND DRAWING 5930483. INSTALLED HI -LOKS PER SRM 51-30-05. 2 L 7 2 4F A6WE 2001042700020 20010427 00020 WP 2001 4 27 TWAA0106203 1 20010330 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT FOUND IN CABIN AT FWD PASSENGER ENTRY AT STA 200, 8 IN INBD, MEMBRANE HAD A 1 INCH CRACK. REPLACED WITH NEW MEMBRANE WHERE AREA WAS CRACKED PER SRM 51-70-4. 2 L 7 2 4F A6WE 2001042700021 20010427 00021 WP 2001 4 27 TWAA0106204 1 20010402 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT FOUND FLOOR SUPPORT CORRODED AT LBL 4, STA 180 TO 200. REPLACED FLOOR SUPPORT PER SRM 51-10-4, SRM 51-30-1, AND SPM 6-70-1. 2 L 7 2 4F A6WE 2001042700022 20010427 00022 WP 2001 4 27 TWAA0106205 1 20010402 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT FOUND ON COCKPIT RT SIDE, BETWEEN STA 120 TO 148 AND 51 INCH RBL, FLOOR/WALL SUPPORT HAD CORROSION. MADE NEW ANGLE USING 0.040 7075T6. TRIMMED AND DRILLED TO AIRCRAFT PER 6-70-01 AND DRAWING 9936533. 2 L 7 2 4F A6WE 2001042700023 20010427 00023 WP 2001 4 27 TWAA0106206 1 20010402 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 909TW 49170 DURING CHECK-C MAINT FOUND IN CABIN THE SEAT TRACK HAD SEVERAL AREAS OF CORROSION, RBL 54, STA 341 TO 794. CORROSION RE MOVED BY REMOVING OLD TRACK AND INSTALLING NEW SECTIONS, SPLICING IN AT 341 PER SRM 53-05, FIG 4F. ALSO AT STA 570 AND FACTORY SPLICES AT STA 796. SURFACE TREATMENT PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001042700024 20010427 00024 WP 2001 4 27 TWAA0106207 1 20010402 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 909TW 49170 DURING CHECK-C MAINT IN THE AFT CARGO COMPT, THE RT TIE DOWN TRACK HAD CORROSION AT STA 1136 TO 1155. REPLACED TIE DOWN TRACK PER SRM 51-30-1 AND SRM 51-30-2, STA 1041 TO 1155. 2 L 7 2 4F A6WE 2001042700025 20010427 00025 WP 2001 4 27 TWAA0106208 1 20010402 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 909TW 49170 DURING CHECK-C MAINT IN THE AFT CARGO COMPT, THE RT TIE DOWN TRACK HAD CORROSION AT STA 1136 TO 1155, AND LONGERON 28R H AD CORROSION. REPLACED TIE DOWN TRACK PER SRM 51-30-1 AND SRM 51-30-2. CHANGED SUPPORT BRACKET PER DRAWING 593660. TR EATED AND PRIMED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001042700026 20010427 00026 WP 2001 4 27 TWAA0106210 1 20010330 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 992Z 47095 DURING OP 15 MAINT CHECK FOUND POSSIBLE CRACK IN SKIN AT STA 1104, LONGERON 5L TO 4L. COMPLIED WITH ARA 17573 REFERRING TO LISTED SRM 53-04, FIG 27 AND SRM 51-01 PARAGRAPH 3B1. 2 L 7 2 4F A6WE 2001042700027 20010427 00027 WP 2001 4 27 TWAA0106211 1 20010330 A 5320 FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT FOUND STRINGER TIE FITTING HAD CORROSION AT STA 1338, STRINGER 21R. REPLACED STRINGER 21R TIE FITT ING PER SRM 51-30-05. 2 L 7 2 4F A6WE 2001042700028 20010427 00028 WP 2001 4 27 TWAA0106212 1 20010330 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT FOUND CORROSION ON LONGERON 26R, BETWEEN STA 1338 AND 1322. INSTALLED NEW LONGERON AND SPLICE PER SRM 53-02, PAGE 49 AND ARA 17645, STA 1297 TO 1338. 2 L 7 2 4F A6WE 2001042700029 20010427 00029 WP 2001 4 27 TWAA0106213 1 20010302 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 DURING CHECK-C MAINT THE LOWER Y CHORD SECTION AT STA 1338, STRINGER 24R TO 24L, HAD CORROSION. INSTALLED Y-CHORD PER S RM 53-03 FIG 37A, AND ARA 17647A, STRINGER 23R TO 23L. 2 L 7 2 4F A6WE 2001042700030 20010427 00030 WP 2001 4 27 TWAA0106214 1 20010330 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 906TW 49160 DURING CHECK-C MAINT IN THE AFT CABIN, FOUND CORROSION AT TOP OF FLOORBEAM, STA 1338, LBL 18 IN THRU 54 INCHES. REMOVED CORROSION PER SPM 6-80-01. TREATED METAL PER SPM 61-103. INSTALLED ANGLE REPAIR PER SRM 53-05, PAGE 31 FIG B. 2 L 7 2 4F A6WE 2001042700031 20010427 00031 WP 2001 4 27 TWAA0106215 1 20010330 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 906TW 49160 DURING CHECK-C MAINT IN THE AFT FUSELAGE, 4 CRACKS WERE FOUND AROUND FASTENERS AT STA 1463 ON WEB AT END OF RBL 8 INCHES . STOP DRILLED CRACKS. INSTALLED DOUBLER PER SRM 53-01 FIG 4. INSTALLED FASTENERS PER SRM 51-30-01. PRIMED AREA PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001042700032 20010427 00032 SO 2001 4 27 C2XA01CL076 1 20010406 A 3246 13889 BEARING EMB 145 EMB145 SO NLG FAILED A C2XA K NONE E VIBRATION/BUFFET TX TAXI/GRND HDL 1 SW 27 19966 145131 MCI FLIGHT 4107 THE CREW REPORTED DURING TAXI TO THE GATE A LOUD SQUEAL AND VIBRATION WAS FELT FROM THE NOSE GEAR. MAI NTENANCE INSPECTED AND FOUND THE RIGHT NOSE WHEEL BEARING HAD FAILED AND CAUSED DAMAGE TO THE STRUT AXLE.BOTH NOSE WHEEL ASSEMBLY''S WERE REPLACED ALONG WITH THE NOSE LANDING GEAR ASSEMBLY. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001042700033 20010427 00033 SW 2001 4 27 PNSA010301 1 20010329 A 3150 WARNING LIGHT FRCHLD SA227 SA227DC 3377521 SW COCKPIT ILLUMINATED A PNSA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 AL 03 892DC DC892B RT SAS FAIL LIGHT WOULD NOT EXTINGUISH. ABORTED TAKEOFF, RETURNED TO GATE. RESET SAS MODULE, OPS CHECK OK. 2 L 7 2 4T RT A18SW 2001042700034 20010427 00034 SW 2001 4 27 PNSA010302 1 20010306 A 7603 FRICTION RING SWRNGN SA227 SA227AC 8780603 SW COCKPIT MALFUNCTIONED A PNSA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 AL 03 640PA AC759B SPEED LEVER SLIPPED BACK DURING TAKEOFF. ABORTED TAKEOFF. RESET FRICTION LOCK. SUBSEQUENT TAKEOFFS WERE OK. 2 L 7 2 4T RT A8SW 2001042700035 20010427 00035 SW 2001 4 27 PNSA010303 1 20010303 A 7400 ENGINE SWRNGN SA227 SA227AC 8780603 SW RT ENGINE MALFUNCTIONED A PNSA K NONE O OTHER TX TAXI/GRND HDL 1 AL 03 650PA AC775B RT ENGINE WOULD NOT START. NO IGNITION. TROUBLESHOT SYSTEM. NO FAULT FOUND. OPERATIONAL CHECK OK. 2 L 7 2 4T RT A8SW 2001042700036 20010427 00036 EA 2001 4 27 SWIA972485 1 20010405 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT CRACKED A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 418SW 7446 FIRST OFFICER''S WINDSHIELD SHATTERED INFLIGHT AT FL250. INSIDE LAYER DID NOT DELAMINATE. NO CABIN PRESSURE LOSS. REM OVED AND REPLACED COPILOT''S WINDSHIELD IAW MM 56-11-01, CHECKS GOOD. P/N: NP-139321-10, S/N ON: 0107343239, S/N OFF: 0013047097. 2 L 7 2 4F 4 F RT A21EA E15NE 2001042700037 20010427 00037 SO 2001 4 27 SWIA972486 1 20010402 A 3350 BATTERY PACK EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CABIN DISCHARGED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 212SW 120276 AFT EMERGENCY LIGHTS DO NOT TEST. REMOVED AND REPLACED NR 4 EMERGENCY BATTERY PACK IAW 33-50-02. OPS CHECKS GOOD. P/N D366-04-001, S/N OFF 891 ON 1166. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042700038 20010427 00038 SO 2001 4 27 SWIA972487 1 20010402 A 3260 HARNESS EMB 120 EMB120RT SO PWA 118 PW118 NE NLG FAULTY A SWIA K NONE J WARNING INDICATION CL CLIMB 1 NM 07 1117H 120117 AFTER TAKEOFF, RIGHT MAIN GEAR SYSTEM-A RED LIGHT REMAINED ILLUMINATED. GEAR RETRACTED, BUT GEAR DOORS REMAINED OPEN. RECYCLED GEAR, BUT RIGHT MAIN GEAR SYSTEM-A RED LIGHT RE-ILLUMINATED AND GEAR DOORS WOULD NOT CLOSE. 4-2-01 (PDX) - SWIN G LANDING GEAR. ABLE TO DUPLICATE PROBLEM. SWAPPED LEADS ''A'' UP AND ''B'' UP. ''B'' RED LIGHT ILLUMINATED WITH GEAR IN UP POSITION. DEFERRED RED ''B'' LIGHT PER MEL 32-60-1A. 4-4-01 (PDX) - FOUND RT ''A'' HARNESS TO BE BAD BY SHAKING IT WHILE GEAR IS UP. REMOVED AND REPLACED HARNESS ''A'' UP, PER MM 32-61-01. CYCLED GEAR 15 TIMES AND SHOOK ALL HARNE SSES. GEAR SYS OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042700039 20010427 00039 2001 4 27 SWIA972488 4 20010406 A 3417 ADC CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 413SW 7102 EFIS COMPARATOR MONITOR MESSAGE ILLUMINATED INFLIGHT WITH IAS FLAGS ON BOTH SIDES. CAPTAIN''S AIRSPEED NOTED 40 TO 50 K NOTS LESS THAN FIRST OFFICER''S. AFTER ONE MINUTE MACH TRIM AND STALL FAIL MESSAGES APPEARED. (CAT II) PURGED PITOT/ST ATIC SYSTEM REMOVED AND REPLACED NR 1 ADC. P/N 822-0372-140, S/N OFF 1022, S/N ON 1478 CAT II IAW 34-13-01. 2 L 7 2 4F RT A21EA 2001042700040 20010427 00040 SO 2001 4 27 SWIA972489 1 20010406 A 3260 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT MLG FAULTY A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 190SW 120050 ON TAKEOFF THE LEFT LANDING GEAR FAILED TO RETRACT. UPON RECYCLING, THE GEAR WOULD NOT EXTEND. RETURNED TO SLC. REMOV ED AND REPLACED A SYSTEM DOWNLOCK PROX SENSOR AND B-SYSTEM DOWNLOCK PROX SENSOR AND CANNON PLUG AT P0136 WITH SERVICEABL E UNIT IAW EMB 120 MM 32-61-01, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042700041 20010427 00041 SO 2001 4 27 C2XA01IA198 1 20010406 A 3350 7287580501 LIGHT EMB 145 EMB145LR SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16919 145393 IAH-DURING A-CHECK, THE MECHANIC NOTED THE AISLE PATH LIGHTING AT SEAT 9A WAS INOPERATIVE. IAH-MAINTENANCE REMOVED AND REPLACED THE AISLE EMERGENCY LIGHT AT SEAT 9A AND THE OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM WAS SATISFACTOR Y. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001042700042 20010427 00042 SO 2001 4 27 C2XA01IA199 1 20010407 A 3350 AD2047 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15732 120195 IAH-DURING POSTFLIGHT THE CREW OBSERVED THAT THE LAST SECTION OF EMERGENCY LIGHTS WAS NOT ILLUMINATED. IAH-MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY BATTERY, PERFORMED AN OPERATIONAL CHECK WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001042700045 20010427 00045 WP 2001 4 27 ARWA0010402 1 20010404 A 3220 LANDING GEAR DOUG DC8 DC862F 3021972 WP NLG COLLAPSED A ARWA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 791AL 46150 EMERGENCY TURNBACK DUE TO NOSE GEAR MALFUNCTION. ON ROLLOUT NOSE GEAR COLLAPSED AT 70 KTS. EMERGENCY UNITS APPLIED FOA M FIRE PROTECTION ON RUNWAY AND PURPLE DRY CHEMICAL WAS USED IN COCKPIT AREA PRECAUTIONARY. 2 L 7 4 4F 4A25 2001042700046 20010427 00046 WP 2001 4 27 ARWA0010403 1 20010407 A 2421 31229000 GENERATOR DOUG DC8 DC862 3021970 WP NR 2 ENGINE MALFUNCTIONED A ARWA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 19 802BN 45909 NR 2 GENERATOR FIELD RELAY TRIPS AND WILL NOT RESET.CORRECTIVE ACTION: REMOVED AND REPLACED NR 2 GENERATOR OPERATIONAL C HECK NORMAL DURING RUN UP IAW MM 24-20-1 & 71-00 2 L 7 4 4F 4A25 2001042700048 20010427 00048 EA 2001 4 27 COMA0160358 1 20010404 A 5320 601R31527181 ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 982CA 9807 7168 ANGLE P/N 601R-31527-181 CORRODED AT LOWER LONGERON, PASSENGER DOOR ANGLE LOCATED AT STR 17 FS 342.7 - 317.70. FABRICAT ED ANGLE - 181 AND INSTALLED IAW WVAC EO 601R-53-2366. 2 L 7 2 4F RT A21EA 2001042700049 20010427 00049 EA 2001 4 27 COMA0160359 1 20010410 A 5320 601R311719172 INTERCOSTAL CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 918CA 18723 7018 FS 484 ANGLES CRACKED T LBL 27 INBOARD AND OUTBOARD. REPAIRED INTERCOSTALS AND ANGLES AT FS 484 IAW WVAC EO 601R-53-237 5. 2 L 7 2 4F RT A21EA 2001042700050 20010427 00050 NM 2001 4 27 CALA0100316 1 20010408 A 5345 MOUNT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND AFT GALLEY AFT I/B MOUNT CORRODED AT STA 967, LBL 14. THE GALLEY MOUNT WAS REMOVED AND REPLACED IAW SR M 51-40-02 AND 51-10-02. 2 L 7 2 4F RT A16WE 2001042700051 20010427 00051 NM 2001 4 27 CALA0100317 1 20010409 A 2742 251N205110 ACTUATOR BOEING 757 757224 1384958 NM HORIZ STAB WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 58101 28934 27291 INSPECTION FOUND HORIZONTAL STABILIZER ACTUATOR GIMBAL WORN BEYOND LIMITS. THE ACTUATOR WAS REMOVED AND REPLACED IAW MM 27-41-10. 2 L 7 2 4F RT A2NM 2001042700052 20010427 00052 NM 2001 4 27 CALA0100318 1 20010409 A 5320 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND Z-ANGLE CORRODED AT R-2 DOOR ENTRY. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001042700053 20010427 00053 NM 2001 4 27 CALA0100319 1 20010409 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1006 - 1016, LBL 4 - 10. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001042700054 20010427 00054 NM 2001 4 27 CALA0100320 1 20010409 A 5743 656717217 FITTING BOEING 737 7373T0 1384582 NM LT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND LT MLG STAB LINK AFT ATTACH FITTING ON GEAR BEAM CORRODED. THE FITTING WAS REMOVED AND REPLACED IAW MM 51-40-04. 2 L 7 2 4F RT A16WE 2001042700055 20010427 00055 NM 2001 4 27 CALA0100321 1 20010409 A 5320 WEB BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND MAIN DECK SUBFLOOR CORRODED BETWEEN RUBBER SEAL OF APB, STA 1016, RBL 2. THE SUBFLOOR WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001042700056 20010427 00056 WP 2001 4 27 TWAA0106301 1 20010409 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9305N 49395 THE AFT CABIN EXIT IDENTIFIER FAILED TO ILLUMINATE. REPAIRED A BROKEN WIRE IN CEILING OF AFT LEFT LAVATORY. CHECK-C 2- 5-01 JFK. 2 L 7 2 4F RT A6WE 2001042700057 20010427 00057 WP 2001 4 27 TWAA0106302 1 20010408 A 3397 58531 WIRE DOUG DC9 DC982 3022082 WP CABIN WORN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 922TW 48013 THE EGRESS LIGHTS WERE INOPERATIVE FROM CABIN ROW 15 TO 21. REPLACED POWER FLEX CABLE. CHECK-C 6-10-00 JFK. 2 L 7 2 4F A6WE 2001042700058 20010427 00058 WP 2001 4 27 TWAA0106303 1 20010409 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 969TW 53619 THE EGRESS LIGHTS WERE INOPERATIVE IN FIRST CLASS AND AT ROW 12 TO 24, AND THE OVERHEAD EMERGENCY LIGHTS WERE INOPERATIV E AT ROW 15 TO 22. REPLACED LIGHT MODULE P/N 0105606-003 IN FIRST CLASS. FOR THE EGRESS LIGHTS AT ROW 12 TO 24 AND THE OVERHEAD EMERGENCY LIGHTS, REPLACED THE POWER SUPPLY 60-0304-51LB AND CELLS P/N 408822-101 AT EACH LOCATION. CHECK-C 7 -28-00 JFK. 2 L 7 2 4F RT A6WE 2001042700059 20010427 00059 WP 2001 4 27 TWAA0106304 1 20010404 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 906TW 49160 DURING CHECK-C MAINT IN THE AFT CARGO COMPT, FOUND CORROSION ON FORMER AT STA 1155 BETWEEN LONGERON 25L THRU 27L. REMOV ED PART FROM AIRCRAFT. REMOVED CORROSION PER SPM 6-80-1. FINISH RESTORED BY PAINT DEPT. RE-INSTALLED PART ON ACFT WIT H ORIGINAL TYPE FASTENERS AND INSTALLED PER SRM 51-30-5. 2 L 7 2 4F A6WE 2001042700060 20010427 00060 WP 2001 4 27 TWAA0106308 1 20010404 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT FOUND INTERCOSTAL CORRODED OTBD OF STA 1322, STRINGER 28L. FORMED NEW INTERCOSTAL PER SPM 6-70-01. INSTALLED PER SRM 51-30-5, 51-30-7, 51-10-4, AND 51-10-2A. 2 L 7 2 4F A6WE 2001042700061 20010427 00061 WP 2001 4 27 TWAA0106309 1 20010330 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT FOUND IN CABIN AT STA 160, 42 IN LBL, FLOOR SUPPORT HAD CORROSION. REPLACED FLOOR SUPPORT PER SRM 51-70-0. 2 L 7 2 4F A6WE 2001042700062 20010427 00062 WP 2001 4 27 TWAA0106310 1 20010405 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT IN AFT CARGO COMPT FOUND FRAME AT STA 1309 WAS CORRODED FRONT AND BACK BETWEEN LONGERON 28R TO 28L. SPLICED FRAME REPAIR PER SRM 53-03, FIG 2A. 2 L 7 2 4F A6WE 2001042700063 20010427 00063 WP 2001 4 27 TWAA0106311 1 20010404 A 5320 ATTACH ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING CHECK-C MAINT FOUND FRAME ATTACH ANGLE CORRODED AT FWD SIDE STA 1309, BETWEEN LONGERON 29L AND 29R. REPLACED FRA ME ATTACH ANGLE PER SRM 53-03, FIG 3. 2 L 7 2 4F A6WE 2001042700064 20010427 00064 WP 2001 4 27 TWAA0106312 1 20010404 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 908TW 49169 DURING OP 16 MAINT CHECK IN FWD CABIN FOUND CORROSION ON FLOOR MEMBRANE AT STA 200, RBL 45 TO 55. FABRICATED MEMBRANE S TA 200, RBL 45 IN TO 55 IN PER SRM 53-14-1. TREATED PER SRM 51-10-3. INSTALLED PER SRM 53-01, PAGE 9 WITH RIVETS PER S RM 51-30-2, WET WITH SEALER PER SRM 51-20-0. 2 L 7 2 4F A6WE 2001042700065 20010427 00065 WP 2001 4 27 TWAA0106313 1 20010404 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 909TW 49170 DURING CHECK-C MAINT FOUND CABIN CHAIR TRACK CORROSION AT LBL 24 INCHES, STA 1127 TO 1309. INSTALLED NEW FLOOR TRACK FR OM STA 1088 TO 1309. INSTALLED SPLICE AT STA 1088 PER SRM 53-05 PAGE 106, FIG 4F SHEET 1. SECURED TRACK WITH BOLTS, MS 250 WASHERS AND NUTS PER SRM 51-60-0, 51-30-1, AND SRM 51-30-5. 2 L 7 2 4F A6WE 2001042700066 20010427 00066 NM 2001 4 27 C8GA20010005 1 20010406 A 2424 902F2425 GCU BOEING 727 7272A1 138407F NM NR 1 ENGINE CONTAMINATED A C8GA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 15 287SC 71 21345 FLT BX742 FROM TOL TO OMA. NR 1 IN LINE FOR TAKEOFF, NR 1 GENERATOR HAD A 3 LIGHT TRIP WITH A BRIEF LOSS OF NR 2 & 3 GC B''S AND ESSENTIAL POWER (SELECTED ON NR 3 AT THE TIME). CREW REPORTED SMELLING SMOKE IN THE COCKPIT. AIRCRAFT RETURNE D TO BLOCKS WITHOUT INCIDENT. FOUND WATER FROM HEAVY RAIN IN THE NR 1 GENERATOR CONTROL UNIT (GCU). REPLACED GCU. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2001042700067 20010427 00067 SO 2001 4 27 C2XA01CL077 1 20010407 A 3030 CS500060D4A RELAY EMB 135 EMB135LR SO COCKPIT BURNED A C2XA K NONE J WARNING INDICATION AP APPROACH 1 SW 27 17513 145292 CLE-FLT 3800 THE CREW REPORTED TAT NR 2 HEAT INOPERTATIVE MESSAGE ON SHORT FINAL. ACCOMPANIED BY A STRONG BURNING SMEL L IN COCKPIT AND CABIN. MAINTENANCE REPLACED RELAY KO494 AND CONNECTORS XK0494 AND XK0054. PERFORMED OPERATIONAL CHECK S AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT TOOO11AT 2001042700068 20010427 00068 SO 2001 4 27 C2XA01TY071 1 20010407 A 3350 3025103 LIGHT EMB 145 EMB145 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16927 145006 TYS DURING A SCHEDULED INSPECTION THE FWD RIGHT HAND EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY IAW EMB-145 MM 33-50-07, OPEATIONAL CHECKS WERE SATISFACTORY. THE AIRCRAFT WA S RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001042700069 20010427 00069 SO 2001 4 27 C2XA01TY072 1 20010408 A 3350 3025101 LIGHT EMB 145 EMB145ER SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15941 145035 TYS DURING A SCHEDULED INSPECTION THE FWD RIGHT HAND EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY IAW EMB-145 MM 33-50-07, OPERATIONAL CHECKS WERE SATISFACTORY. THE AIRCRAFT W AS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001042700070 20010427 00070 CE 2001 4 27 GLBA2001078 1 20010410 A 3246 114800121 BEARING BEECH 1900 1900D 1154162 CE NLG FAILED A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 01 211UX 4709 885 UE211 NOSE WHEEL BEARINGS FAILED ON T/O, WHEEL SEPARATED FROM AIRCRAFT. REPLACED NOSE LANDING GEAR AND WHEEL ASSEMBLY. 2 L 7 2 4T RT A24CE 2001042700071 20010427 00071 CE 2001 4 27 GLBA2001079 1 20010410 A 3060 BRUSH BLOCK BEECH 1900 1900D 1154162 CE LT PROP OUT OF ADJ A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 201YQ UE201 LEFT PROP DEICE AMPS LOW. CLEANED AND RESHIMMED BRUSH BLOCK, OPS CHECKED SYSTEM GOOD. RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 2001042700072 20010427 00072 WP 2001 4 27 ZW0A0100101 1 20010410 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 921TW 49101 THE EGRESS LIGHTS WERE INOPERATIVE FROM CABIN ROW 28 TO 33. DRIED MOISTURE ON CABLE, REPLACED THE AFT FLEX CABLE P/N 58 53-1, AND REPLACED THE AFT POWER SUPPLY P/N 5822-2. CHECK-C 3-24-01 STL. 2 L 7 2 4F RT A6WE 2001042700073 20010427 00073 WP 2001 4 27 ZW0A0100102 1 20010404 A 5350 BRACKET DOUG DC9 DC982 3022082 WP FAIRING CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 909TW 49170 DURING CHECK-C MAINT ON RT WING L/E THE INBD L/E FAIRING ATTACH BRACKETS WERE CRACKED, INBD OF ZERO L/E SLAT. REMOVED 2 BROKEN BRACKETS. FABRICATED NEW BRACKETS PER DRAWING 5937452 AND SRM 51-30-5. INSTALLED PER SPM 6-70-01. TREATED AND PAINTED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001042700074 20010427 00074 WP 2001 4 27 ZW0A0100103 1 20010406 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 909TW 49170 DURING CHECK-C MAINT FOUND CORROSION ON AFT FACE AND TROUGH OF FORMER AT STA 1309, LONGERON 25L TO 28R. REMOVED LIGHT C ORROSION PER SPM 6-80-01. ALODINED AND PRIMED PER SRM 51-10-3. REINSTALLED FLOOR SUPPORT BRACKET AND REINSTALLED LONGE RON FASTENERS AS NEEDED. 2 L 7 2 4F A6WE 2001042700075 20010427 00075 WP 2001 4 27 ZW0A0100104 1 20010406 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT FOUND CRACK ON LONGERON 4L AT STA 160. REMOVED AND INSTALLED NEW LONGERON PER SPM 6-70-01 PAGE 3 P ARA 4. INSTALLED RIVETS PER SRM 51-30-02. INSTALLED HI-LOKS PER SRM 51-30-05. 2 L 7 2 4F A6WE 2001042700076 20010427 00076 WP 2001 4 27 ZW0A0100105 1 20010409 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT FOUND CABIN TRACK CORRODED AT LBL 55 INCHES, STA 995 TO 1136. REMOVED CORROSION PER SPM 6-80-01 PA GE 3. INSTALLED AND REPLACED SEAT TRACK PER SPM 6-70-01 PAGE 1, AND SRM 53-05 FIG 4F SHEET 5. 2 L 7 2 4F A6WE 2001042700077 20010427 00077 WP 2001 4 27 ZW0A0100106 1 20010409 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT CORRODED AT STA 200, RBL 47 IN TO 58 IN. FLOOR SUPPORT CORRODED BEYOND L IMITS. FABRICATED NEW FLOOR SUPPORT PER SPM 6-70-01 PAGE 2 AND PAGE 3, AND DRAWING 9936534. CORROSION TREATED NEW FLOO R SUPPORT PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001042700078 20010427 00078 WP 2001 4 27 ZW0A0100107 1 20010409 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT FOUND GOUGE IN FUSELAGE SKIN BELOW LAV SERVICE PANEL, CURRENTLY HAVING SURFACE PATCH INSTALLED. CU T OUT SKIN AND INSTALLED DOUBLER PER SRM 53-04, PAGE 37, FIG 12B. TREATED AND SEALED REPAIR PER SRM 51-10-03 AND COMPLI ED WITH ET 009. 2 L 7 2 4F A6WE 2001042700079 20010427 00079 WP 2001 4 27 ZW0A0100108 1 20010330 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 908TW 49169 DURING CHECK-C MAINT FOUND IN LT CABIN BETWEEN STA 160 AND 200, 6 INCHES INBD OF FWD PASSENGER ENTRY, FLOOR MEMBRANE HAD CORROSION. REPLACED DAMAGED CORRODED PART PER SRM 51-70-4. 2 L 7 2 4F A6WE 2001042700080 20010427 00080 WP 2001 4 27 ZW0A0100109 1 20010408 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 908TW 49169 DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND CORROSION ON AFT RT CARGO TIE DOWN TRACK. INSTALLED NEW TRACK PER SPM 6-70-01, ITEM 4. INSTALLED NEW FASTENERS PER SRM 51-30. 2 L 7 2 4F A6WE 2001042700081 20010427 00081 WP 2001 4 27 ZW0A0100110 1 20010306 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 909TW 49170 DURING CHECK-C MAINT AT CABIN STA 1129 TO 1309, FLOOR TRACK AT LBL 42 IN, FOUND INBD AND OTBD FLANGES HAD CORROSION. RE MOVED TRACK NUMBER 2 AT STA 1309 TO 1129. REPLACED TRACK WITH NEW. DRILLED HOLES PER SRM 51-10-4. INSTALLED PER SRM 5 1-30-1. PRIMED PER SRM 51-10-3 PAGE 16. SEALED PER SRM 51-10-0. 2 L 7 2 4F A6WE 2001042700082 20010427 00082 WP 2001 4 27 ZW0A0100111 1 20010405 A 5315 FLOORBEAM DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 992Z 47095 DURING OP 15 MAINT CHECK AT STA 965, RBL 5 INCHES AND RBL 14 INCHES, BOTTOM OF CABIN FLOORBEAM HAD A BULGE. REMOVED COR RODED SECTIONS OF FLOORBEAM. INSTALLED REPAIR DOUBLERS AND ANGLES PER SRM 53-05, FIG 79, AND ARA 17099. 2 L 7 2 4F A6WE 2001042700083 20010427 00083 WP 2001 4 27 ZW0A0100112 1 20010406 A 5320 ANGLE DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 992Z 47095 DURING OP 15 MAINT CHECK FOUND POSSIBLE CRACK IN SUPPORT ANGLE AT STA 1046, LONGERON 3L. ACCOMP NDT USING HFEC PER 51-0 0-03, PART 6 AND FOUND 1 .25 IN LONG CRACK. INSTALLED DOUBLER PER SRM 53-05, PAGE 506, FIG 23B, AND SRM 51-30-5. 2 L 7 2 4F A6WE 2001042700084 20010427 00084 WP 2001 4 27 ZW0A0100113 1 20010330 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT FOUND CORROSION ON INTERCOSTAL BETWEEN STA 1250 AND 1271, LONGERON 25L. INSTALLED FASTENERS PER SR M 51-30-02. INSTALLED NEW INTERCOSTAL PER SPM 6-70-01 AND SRM 51-30-02. 2 L 7 2 4F A6WE 2001042700085 20010427 00085 SO 2001 4 27 C2XA01IA200 1 20010407 A 3231 12043270501 CONTROL BOX EMB 120 EMB120ER 3260203 SO LANDING GEAR INOPERATIVE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 16723 120169 EFD - FLIGHT 3353, THE CREW REPORTED THAT THE FORWARD LANDING GEAR DOORS WOULD NOT CLOSE. THE AIRCRAFT LANDED AT EFD WI THOUT INCIDENT WHERE MAINTENANCE CLEANED THE HYDRAULIC SOLENOID VALVE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI CE. THE DISCREPANCY REOCCURRED ON 04/08/01 FLIGHT 3353 AT EFD WHERE MAINTENANCE RESET THE GEAR DOOR EMERGENCY SELECTOR SWITCH, AND THE AIRCRAFT WAS AGAIN APPROVED FOR RETURN TO SERVICE. ON FLIGHT 4371, THE GEAR DOORS WERE AGAIN FOUND TO R EMAIN OPEN. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL RELAY BOX, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. NO FURTHER INCIDENTS HAVE BEEN REPORTED TO DATE. 2 L 7 2 4T RT A31SO 2001042700086 20010427 00086 SO 2001 4 27 C2XA01IA201 1 20010408 A 3260 12041126001 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO RT MLG FAULTY A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 27 51726 120174 SHV - FLT 3340, THE CREW REPORTED RIGHT MAIN LANDING GEAR SYSTEM ''B'' RED LIGHT ILLUMINATED IN FLT. THE ACFT LANDED AT SHV WITHOUT INCIDENT. MX CLEANED THE LANDING GEAR PROXIMITY SWITCHES, OPERATIONALLY CHECKED WITH NO DEFECTS FOUND, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. THE DISCREPANCY REOCCURED ON 04/09/01 AT IAH WHERE MX PLACED THE SYSTEM ' 'B'' INDICATION ON MEL 32-60-01B CONTROL 012399, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 04/10/01 THE A CFT RETURNED TO IAH WHERE MX REMOVED AND REPLACED THE SYSTEM ''B'' PROXIMITY SENSOR ON THE RIGHT MAIN LANDING GEAR, OPER ATIONALLY CHECKED WITH NO DEFECTS NOTED. REMOVED THE MEL. 2 L 7 2 4T RT A31SO 2001042700087 20010427 00087 SO 2001 4 27 C2XA01IA202 1 20010206 A 5720 12061345009 SUPPORT EMB 120 EMB120ER 3260203 SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15732 120195 SJK - DURING C-CHECK INSPECTION, TWO WING SKIN SUPPORTS ON RIB 19, AND ONE SKIN SUPPORT ON RIB 20 OF THE LEFT WING WERE FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORTS IN ACCORDANCE WITH EMB-120 SRM 57-20-0 7, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001042700088 20010427 00088 SO 2001 4 27 C2XA01IA203 1 20010206 A 5711 12037485001 SPAR EMB 120 EMB120ER 3260203 SO LT&RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15732 120195 SJK - DURING C-CHECK INSPECTION, THE LEFT HAND AND RIGHT HAND SPAR CAPS WERE FOUND TO BE CRACKED AT RIB 17 USING EDDY CU RRENT INSPECTION. MAINTENANCE PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH EMB-120 SRM 57-20-05, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001042700089 20010427 00089 SO 2001 4 27 C2XA01IA204 1 20010206 A 3350 1011191 LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15732 120195 SJK - DURING C-CHECK INSPECTION, ONE CEILING EMERGENCY EXIT LIGHT AND ONE FLOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INO PERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CEILING EMERGENCY EXIT LIGHT, AND OPERATIONALLY CHECKED THE FLO OR EMERGENCY EXIT LIGHT WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001042700090 20010427 00090 EU 2001 4 27 C2XA01IA205 1 20010411 A 3350 3011180 POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 97841 280 IAH - DURING MAINTENANCE INSPECTION, THE AFT SECTION OF AISLE PATH EMERGENCY EXIT LIGHTS WAS FOUND TO BE INOPERATIVE. M AINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO S ERVICE. 2 H 7 2 4T RT A53EU 2001042700091 20010427 00091 SO 2001 4 27 C2XA01IA206 1 20010411 A 5713 12016085001 STRINGER EMB 120 EMB120ER 3260203 SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16731 120190 IAH - DURING MAINTENANCE INSPECTION STRINGER 10 ON THE RIGHT WING WAS FOUND TO BE CRACKED AT ACCESS PANEL 622DB. MAINTE NANCE PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHANGE EC5710-01010, AND THE AIRCRAF T WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001042700092 20010427 00092 NM 2001 4 27 01FDEA00268 1 20010411 A 2710 ACTUATOR DOUG MD11 MD11 3023602 NM AILERON FAILED A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 596FE 48554 AFT FLAP RETRACTION, AILERON DISAGREE ALERT DISPLACY. RED TAB PROC ACCOMP. DEFLECTED AILERON SYS INOP. RIGHT O/B ACT FAILED AND REPLACED WITH FIXED PUSHROD PER METHOD B. 2 L 7 3 4F RT A22WE 2001042700094 20010427 00094 WP 2001 4 27 RRXA010025 1 20010227 A 3230 57146745001 CONTROL VALVE DOUG DC8 DC873F 302199F WP MLG FAILED A RRXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 605AL 46106 AFTER TAKEOFF, GEAR UPLATCH CHECK FAILURE. REMOVED AND REPLACED MAIN GEAR CONTROL VALVE IAW M/M 32-32-1 RIGGED IAW M/M 32-31-0 P208. NO LEAKS NOTED ON PRESSURE CHECKS. PERFORMED EXTENSION AND RETRACT ON CHECKS PER M/M 32-30-0. CYCLED GE AR THREE TIMES NO FURTHER PROBLEMS NOTED ON GEAR SWING. 2 L 7 4 4F RT 4A25 2001042700095 20010427 00095 WP 2001 4 27 RRXA010026 1 20010303 A 7722 CONNECTOR DOUG DC8 DC862F 3021972 WP NR 1 EGT FAULTY A RRXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 15 996CF 46162 ON TAKEOFF ROLL, NR 1 EGT WENT TO ZERO. AFTER REDUCING POWER TO IDLE, RETURNED TO NORMAL. REMOVED AND REPLACED NR 1 EG T BULKHEAD CONNECTORS. PERFORMED ENGINE RUN, NR 1 EGT OPERATION CHECKED NORMAL IAW DC-8 MM 77-20-0. 2 L 7 4 4F 4A25 2001042700096 20010427 00096 WP 2001 4 27 RRXA010027 1 20010324 A 3231 DOOR DOUG DC8 DC871F 302199D WP NLG MALFUNCTIONED A RRXA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 15 8085U 45975 LOUD NOISE AND BUFFET FROM NOSE SECTION. RIGHT NOSE LANDING GEAR DOOR IN OPEN POSITION WHEN AIRCRAFT TAXIED IN. INSPEC TED NOSE GEAR DOORS FOR CONDITION AND OPERATION NO DEFECTS NOTED. RE-SET POSITION, AIRCRAFT OK FOR FURTHER FLIGHT DC-8 M/M 32-20-00. 2 L 7 4 4F RT 4A25 2001042700097 20010427 00097 WP 2001 4 27 RRXA010028 1 20010324 A 2133 A42G64753 OUTFLOW VALVE DOUG DC8 DC871F 302199D WP CABIN PRESSURE FAILED A RRXA A UNSCHED LANDING O OTHER DE DESCENT 1 WP 15 801GP 46039 ON DESCENT, CABIN BEGAN TO CLIMB. WENT TO MAX RATE ON AUTO CONTROLLER AND MAX FLOW ON PACKS, WOULD NOT STOP CLIMB, CABI N COULD NOT BE CONTROLLED MANUALLY EITHER. ANY ATTEMPT TO MANUALLY CONTROL PRESSURE CAUSED CABIN TO CLIMB HIGHER, MANUA L LEVER COULD NOT BE MOVED PAST 3/4 CLOSED. REMOVED AND REPLACED OUTFLOW VALVE ACT IAW M/M 21-33-01. REMOVED AND REPLA CED PRESS MANUAL CONTROL LEVER LIMIT SWITCH IAW EMERY M/M 21-32-06. BOTH AUTO AND MANUAL PRESSURIZATION SYSTEM OPS GOOD IAW EMERY 21-30-01. 2 L 7 4 4F RT 4A25 2001042700098 20010427 00098 WP 2001 4 27 RRXA010029 1 20010329 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 APPROX 3 INCH TEAR IN FUSELAGE SKIN AT FWD LOWER CORNER BELOW CARGO DOOR DURING FWD DOOR GUARD INSTALLATION. REPAIRED D AMAGED AREA AT LOWER FORWARD CORNER OF MCD JAMB IAW GUIDELINES OF EWA ENGINEERING MEMO ML329011 THIS TEMPORARY REPAIR LI MITED TO 1000 CYCLES 2 L 7 4 4F RT 4A25 2001042700099 20010427 00099 2001 4 27 RRXA010030 4 20010328 A 3420 19769101 INDICATOR DOUG DC8 DC873F 302199F WP COCKPIT FAULTY A RRXA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 15 2674U 46062 IN FLIGHT, SAI SHOWS A 20 DEG RIGHT BANK AND 5 DEG TO 6 DEG NOSE UP IN LEVEL FLIGHT. SAI WILL THEN RETURN TO A 3 DEG RI GHT BANK AND 5 DEG''''S TO 6 DEG''''S NOSE UP. REMOVED AND REPLACED STANDBY ATTITUDE INDICATOR. OPS CHECKS NORMAL IAW MM CH 34-00-00. 2 L 7 4 4F RT 4A25 2001042700100 20010427 00100 WP 2001 4 27 RRXA010031 1 20010408 A 7714 8DJ324WAC1 INDICATOR DOUG DC8 DC873F 302199F WP COCKPIT FAULTY A RRXA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 15 605AL 46106 NR 4 ENGINE DURING SPOOL UP, N1 RPM INDICATOR HANGS UP BETWEEN 50 TO 70 PERCENT. REMOVED AND REPLACED NR 4 N1 INDICATOR IAW DC-8 MM CH 77-00. OPS CHECKS GOOD ON ENGINE RUN-UP. 2 L 7 4 4F RT 4A25 2001042700101 20010427 00101 WP 2001 4 27 RRXA010033 1 20010410 A 7722 INDICATOR DOUG DC8 DC862F 3021972 WP COCKPIT FAULTY A RRXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 15 997CF 46154 ON TAKEOFF ROLL NR 1 ENG EGT TEMP WENT TO 575 DEGREES AND WAS CLIMBING OUTSIDE TEMP 22 EPR 1.88 N1 & FF WERE EVEN ACFT S PEED WAS 70 KNOTS. PERFORMED EGT INDICATOR AND HARNESS TEST IAW MM 77-20-4, & BARFIELD TEST SET INSTRUCTIONS FOUND NR 1 EGT INDICATOR TO READ 30 DEGREES - 40 DEGREES HIGH ABOVE 500 DEGREES. REMOVED AND REPLACED NR 1 EGT INDICATOR IAW MM 77-20-1. PERFORMED GROUND RUN IAW EWA RUN UP HANDBOOK, OPS CK GOOD. 2 L 7 4 4F 4A25 2001042700102 20010427 00102 WP 2001 4 27 ABXA010129 1 20010411 A 5311 99234362 FRAME DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 57301 47499 THE FUSELAGE MAIN FRAME AT FS 756 WAS CRACKED AT THE FWD BOLT INBD VERTICAL FLANGE. MAINTENANCE INSPECTED AND REPAIRED THE FRAME IAW ABX REA D953-40627-SB. 2 L 7 2 4F A6WE 2001042700103 20010427 00103 WP 2001 4 27 ABXA010128 1 20010411 A 5311 99234361 FRAME DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 57301 47499 THE FUSELAGE MAIN FRAME AT FS 756 WAS CRACKED AT THE FORWARD BOLT INBD VERTICAL FLANGE. MAINTENANCE INSPECTED AND REPAI RED THE FRAME IAW ABX REA D953-40627-SB. 2 L 7 2 4F A6WE 2001042700104 20010427 00104 WP 2001 4 27 ABXA010127 1 20010411 A 5510 3918022501 SUPPORT FITTING DOUG DC9 DC941 302207N WP HORIZONTAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 57301 47499 THE RIGHT HORIZONTAL STABILIZER SUPPORT FITTING WAS CRACKED ABOVE AND AFT OF THE ELEVATOR CONTROL VALVE ON THE ELEVATOR TRAILING EDGE. MAINTENANCE INSPECTED AND REPLACED THE FITTING IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 2001042700105 20010427 00105 WP 2001 4 27 ABXA010126 1 20010411 A 5330 5911401117 SKIN DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 57301 47499 THE FUSELAGE SKIN WAS CRACKED AT LONGERON 22L FS 194 BELOW THE AIRSTAIR DOOR CUTOUT. MAINTENANCE INSPECTED AND REPAIRED THE FUSELAGE IAW DC-9 SRM 53-04 FIG 12B. 2 L 7 2 4F A6WE 2001042700106 20010427 00106 WP 2001 4 27 ABXA010125 1 20010411 A 5312 5910130273 BULKHEAD DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 57301 47499 THE AFT PRESSURE BULKHEAD PRESSURE DOME SKIN WAS CRACKED ON THE RIGHT SIDE OF THE DOOR CUTOUT. MAINTENANCE INSPECTED AN D REPAIRED THE CRACK IAW DC-9 SRM 53-05. 2 L 7 2 4F A6WE 2001042700107 20010427 00107 WP 2001 4 27 ABXA010124 1 20010411 A 2700 59571191 ARM DOUG DC9 DC941 302207N WP FLIGHT CONTROL CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 THE LONGITUDINAL TRIM ARM WAS PITTED ON THE UPPER SIDE AT THE CABLE ATTACH BOLT, AFT OF FUSELAGE STATION 218, RBL 40. M AINTENANCE INSPECTED AND REPLACED THE SECTOR ARM. 2 L 7 2 4F A6WE 2001042700108 20010427 00108 NM 2001 4 27 SCNA01025 1 20010406 A 3350 LIGHT BOEING 727 7272M7 138407S NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 294SC 21202 DURING A MAINTENANCE LINE CHECK THE RIGHT FORWARD GALLEY DOOR EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. REMOVED AND REP LACED LAMP AT R1 DOOR OVERHEAD EMERGENCY EXIT. 2 L 7 3 4F A3WE 2001042700109 20010427 00109 NM 2001 4 27 SCNA01026 1 20010406 A 3350 BATTERY BOEING 727 727227 1384078 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 275AF 22092 DURING A MAINTENANCE LINE CHECK THE OVERHEAD EMERGENCY EXIT LIGHT BETWEEN THE AFT LAVS WAS FOUND INOPERATIVE. REMOVED A ND REPLACED THE EMERGENCY EXIT LIGHT BATTERY AND CHARGER ASSEMBLY BETWEEN THE AFT LAVS. 2 L 7 3 4F A3WE 2001042700110 20010427 00110 NM 2001 4 27 SCNA01027 1 20010410 A 3150 WARNING SYSTEM BOEING 727 727259 138408J NM COCKPIT ACTIVATED A SCNA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 15 289SC 20765 DURING TAKEOFF ROLLOUT OF LAS, THE TAKEOFF WARNING HORN SOUNDED WHEN THE THROTTLES WERE ADVANCED, ALL CONTROLS WERE FOUN D TO BE IN PROPER POSITION. CHECKED TAKEOFF WARNING SYSTEM, NO TROUBLE FOUND. 2 L 7 3 4F A3WE 2001042700111 20010427 00111 SO 2001 4 27 C2XA01TY075 1 20010410 A 5311 14523050401 FRAME EMB 145 EMB145LR SO FUSELAGE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18982 145223 TYS DURING A SCHEDULED INSPECTION, FRAME 64 BETWEEN STRINGER 6R AND 7R WAS FOUND TO BE CHAFED. MAINTENANCE REPAIRED TH E FRAME IAW EMB GST-1177/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2001042700112 20010427 00112 SO 2001 4 27 C2XA01TY076 1 20010411 A 5320 14533823007 STIFFENER EMB 145 EMB145LR SO FUSELAGE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18982 145223 TYS DURING A SCHEDULED INSPECTION THE EXTERNAL FUSELAGE STIFFENER (T-REINFORCEMENT) AT STRINGER 19L CENTER FUSEALGE IV WAS FOUND TO BE CHAFED. MAINTENANCE REPAIRED THE STIFFENER IAW EMB GST-1207/01, THE REPAIR WAS SATISFACTORY. THE AIRCR AFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2001042700113 20010427 00113 NM 2001 4 27 C8GA20010006 1 20010412 A 5610 BACB10B131 BEARING BOEING 727 727227 1384078 NM WINDOW LOOSE A C8GA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 15 308AS 43005 22002 FLT EB941 FROM MSY TO MCI. AFTER TAKEOFF, CREW HEARD A LOUD SQUEAL FROM THE R2 WINDOW. AIRCRAFT RETURNED TO MSY AND LA NDED WITHOUT INCIDENT. FOUND THE R2 WINDOW AFT TRACK LOWER ROLLER BEARING LOOSE. RESECURED BEARING. OPS AND LEAK CHEC K GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2001042700114 20010427 00114 2001 4 27 SWIA972490 4 20010407 A 2215 SERVO EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE AUTOPILOT BINDING A SWIA K NONE F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 581SW 120349 ELEVATOR BINDING MILDLY WITH FORWARD MOVEMENT. REPLACED ELEV AUTOPILOT SERVO IAW 22-10-05. OPS CHECK GOOD. P/N: 622- 5734-002, S/N ON: 7488, S/N OFF: 10041. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042700115 20010427 00115 2001 4 27 SWIA972491 4 20010407 A 3417 ADC CNDAIR CL600 CL6002B19 EA COCKPIT FAILED A SWIA K NONE I FLT. ATTITUDE INST. TX TAXI/GRND HDL 1 NM 07 410SW 7066 ADC1 FAILURE, MAC TRIM FAILURE, IAS 1 FAIL, FD FAILURE - CAT II. REMOVED AND REPLACED NR 1 ADC 850A AND NR 1 ADC DRAIN ASSEMBLY. OPS CHECK GOOD IAW 34-13-01. CAT II OK FOR CAT II. P/N: 822-0372-140, S/N ON: 2145, S/N OFF: 1102. 2 L 7 2 4F RT A21EA 2001042700116 20010427 00116 SO 2001 4 27 SWIA972492 1 20010410 A 2731 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE ELEVATOR TRIM FAULTY A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 566SW 120341 TAKEOFF AURAL WARNING FOR TRIM WHEN POWER LEVERS ARE ADVANCED NO MATTER WHERE TRIM IS SET IN GREEN ARC. REMOVED AND REP LACED RIGHT ELEVATOR TRIM PROXIMITY SENSOR. OPS CHECK GOOD IAW 27-32-05. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042700117 20010427 00117 SO 2001 4 27 SWIA972493 1 20010407 A 3233 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NLG OUT OF ADJ A SWIA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CR CRUISE 1 NM 07 217SW 120286 DURING CRUISE AT FL 260 NOSE GEAR RED A LIGHT ILLUMINATED. WHEN LANDING GEAR WAS RECYCLED IT EXTENDED NORMALLY; HOWEVER , WHEN RETRACTED BOTH RED A & B LIGHTS REMAINED ILLUMINATED AND VIBRATION AND NOISE WERE NOTICEABLE. GEAR EXTENDED NORM ALLY. ADJUSTED NOSE LANDING GEAR ACTUATING CYLINDER IAW EMB120 MM 32-32-11. PERFORMED OPERATIONAL CHECK IAW EMB120 MM 32-30-00. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042700119 20010427 00119 2001 4 27 SWIA972495 4 20010322 A 2210 SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE AUTOPILOT FAULTY A SWIA K NONE F FLT CONT AFFECTED CR CRUISE 1 NM 07 251YV 120251 AUTOPILOT TRANSFER SWITCH WILL NOT TRANSFER FROM FIRST OFFICER SIDE. WHEN AUTOPILOT IS ENGAGED, TRIM WHEEL RAPIDLY TRIM S NOSE UP. INSPECTED AND REPLACED LAMPS AND F/O''S TRANSFER SWITCH. FOUND LOOSE SCREW INSIDE. REPAIRED, OPS CHECKS GO OD. AUTOPILOT TESTS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042700120 20010427 00120 2001 4 27 SWIA972497 4 20010329 A 2340 INTERPHONE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CABIN INOPERATIVE A SWIA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 07 295SW 120322 FLIGHT ATTENDANT HANDSET SMOKING AND INOPERATIVE. REMOVE AND REPLACE FLIGHT ATTENDANT HANDSET. OPS CHECK GOOD IAW 23-3 0-1. P/N: 5096-1-2, S/N ON: 669. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042700121 20010427 00121 SO 2001 4 27 SWIA972499 1 20010405 A 3350 BATTERY PACK EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CABIN DISCHARGED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 565SW 120340 FIRST THREE ROWS OF EMERGENCY LIGHTS DO NOT ILLUMINATE. ALSO FORWARD EXIT SIGNS DO NOT ILLUMINATE. REPLACED FORWARD (N R 1) EMERGENCY LIGHT BATTERY PACK. GROUND CHECK NORMAL. P/N D366-04-001, S/N ON 883, S/N OFF 397. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042700122 20010427 00122 NM 2001 4 27 CALA0100322 1 20010410 A 5541 RIB BOEING 737 737824 13844BZ NM RUDDER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14235 28947 INSPECTION FOUND A 1.38 INCH CRACK IN RIG PIN HOLE BOSS ON RIB WEB AT STA 56.48. A REPAIR WAS INSTALLED IAW ECRA 5530-0 1292, REV A PART 3. 2 L 7 2 4F RT A16WE 2001042700123 20010427 00123 NM 2001 4 27 CALA0100323 1 20010410 A 5552 251A243010 ATTACH FITTING BOEING 737 737724 NM ELEVATOR TAB WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 54711 28782 INSPECTION FOUND LT ELEVATOR TAB MECHANISM O/B ATTACH POINT FOR TAB ROD WORN. THE LT ELEVATOR TAB CRANK ASSEMBLY AND EL EVATOR TAB PUSH ROD WERE REMOVED AND REPLACED IAW MM 27-31-34. 2 L 7 2 4F RT A16WE 2001042700124 20010427 00124 NM 2001 4 27 CALA0100324 1 20010411 A 5315 DOUBLER BOEING 737 7373T0 1384582 NM FUSELAGE GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND FWD ENTRYWAY FLOORBEAM AFT FLANGE OUTER DOUBLE STACK REPAIR DOUBLER GOUGED IN RADIUS AND ON HORIZONTAL FLANGE AT STA 312, RBL 24. THE DOUBLER WAS REMOVED AND A REPAIR ANGLE WAS INSTALLED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 2001042700125 20010427 00125 NM 2001 4 27 CALA0100325 1 20010411 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND SEAT TRACK CORRODED AT STA 179-294, RBL 45. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTAL LED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001042700126 20010427 00126 NM 2001 4 27 AALA20010576 1 20010322 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 647AM 24605 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT AT ROW 5 DIM. ACCOMPLISHED EMERGENCY LIGHT OPERATIONA L CHECKS PER THE MM. NO FAULTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001042700127 20010427 00127 NM 2001 4 27 AALA20010420 1 20010312 A 5511 SPAR BOEING 727 727223 1384074 NM HORIZONTAL STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 894AA 22010 TUL - FOUND CORROSION ON RIGHT HORIZ STABILIZER AFT SPAR ON TOP APPROX 6 INCHES OUTBOARD OF ELEVATOR PCU. REPAIRED AREA PER ESO 11697, DATED 3-7-01. (M) 2 L 7 3 4F A3WE 2001042700128 20010427 00128 WP 2001 4 27 USAAD01064 1 20010326 A 3260 WARNING LIGHT DOUG DC9 DC981 3022081 WP COCKPIT ILLUMINATED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 809US 48041 PBI-PIT - FLT 1575 - THE NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED DURING GEAR RETRACTION. THE FLIGHT RETURNED TO PBI AND LANDED WITHOUT INCIDENT. S/D - MAINTENANCE SECURED THE NOSE LANDING GEAR DOORS AND PERFORMED AN OVERWEIGHT LANDING INSPECTION. (M) 2 L 7 2 4F A6WE 2001042700129 20010427 00129 NM 2001 4 27 USAA010315 1 20010320 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 50420 24559 CLT - FOUND FLOORBEAM T-CAP CORRODED 4 INCHES, BS 340 FROM LBL 10 TO RBL 10. CORROSION LEVEL 1C53-107-02. SPLICED IN N EW T-CAP PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2001042700130 20010427 00130 NM 2001 4 27 USAA010316 1 20010320 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 50420 24559 CLT - FOUND FLOORBEAM CORRODED 1 INCH BY 10 INCHES, STATION 967 FROM LBL 32 TO RBL 32. CORROSION LEVEL 1 C53-107-02. I NSTALLED REPAIR DOUBLER PER SRM 53-00-51 FIG 202. (M) 2 L 7 2 4F RT A16WE 2001042700131 20010427 00131 NM 2001 4 27 USAA010260 1 20010308 A 5711 SPAR BOEING 737 737301 1384611 NM WING DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 587US 23932 PIT - FOUND REAR SPAR WITH PLY SEPARATION .5 INCH BY .5 INCH, BOTTOM INBOARD SPAR END. REMOVED SPLINTER PLY THEN COMPLE TED 2 WET LAY UP THEN RESEALED EDGES PER EA 70365 AND SRM 51-70-17. (M) 2 L 7 2 4F RT A16WE 2001042700132 20010427 00132 NM 2001 4 27 USAA010268 1 20010305 A 5330 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 412US 36306 23881 CLT - FOUND SKIN CRACKED 2 INCHES, 3 INCHES FORWARD OF 727 F 1 INCH ABOVE STRINGER 26R. INSTALLED DOUBLER. (M) 2 L 7 2 4F RT A16WE 2001042700133 20010427 00133 NM 2001 4 27 USAA010272 1 20010215 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FRAME CRACKED .25 INCH, BS 400 BETWEEN STRINGER 8 AND 9 LEFT. FRAME REPAIR SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 2001042700134 20010427 00134 NM 2001 4 27 USAA010273 1 20010215 A 5320 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND ANGLE CRACKED 2 INCHES, STATION 298 LOWER FRAME DOOR INBOARD CORNER. INSTALLED DOUBLER. (M) 2 L 7 2 4F RT A16WE 2001042700135 20010427 00135 NM 2001 4 27 USAA010274 1 20010214 A 5311 BAC15171470 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FRAME CRACKED .5 INCH, STATION 440 RIGHT SIDE STRINGER 8R AND 9R. INSTALLED DOUBLER. (M) 2 L 7 2 4F RT A16WE 2001042700136 20010427 00136 NM 2001 4 27 USAA010275 1 20010214 A 5311 1131754 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FRAME CRACKED .5 INCH, STATION 380 FRAME RIGHT SIDE STRINGER 8R AND 9R. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001042700137 20010427 00137 NM 2001 4 27 USAA010276 1 20010215 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND SKIN CRACKED .750 AND .250 INCH, STATION 10 RBL OF 0. INSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F RT A16WE 2001042700138 20010427 00138 NM 2001 4 27 USAA010277 1 20010214 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 32136 23882 CLT - FOUND FRAME CRACKED .5 INCH, STATION 400 FRAME RIGHT SIDE BETWEEN STRINGER 8R AND 9R. REMOVED DAMAGED, REPAIRED T R 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001042700139 20010427 00139 NM 2001 4 27 USAA010278 1 20010214 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FRAME CRACKED .5 INCH, STATION 480 FRAME RIGHT SIDE BETWEEN STRINGER 8R AND 9R. INSTALLED FRAME DOUBLER. ( M) 2 L 7 2 4F RT A16WE 2001042700140 20010427 00140 NM 2001 4 27 USAA010279 1 20010215 A 5311 FRAME BOEING 737 7374B7 1384702 NM BULKHEAD CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND SIDE CHORD .5 INCH, BS 178 LEFT SIDE CHORD WL 207. REMOVED DAMAGE AND SPLICED IN NEW CHORD PER EO 5300V157 PLUS EO 69141. (M) 2 L 7 2 4F RT A16WE 2001042700141 20010427 00141 NM 2001 4 27 USAA010280 1 20010226 A 5320 STRAP BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND STRAP CRACKED .875 INCH, BS 300 STRINGER 10L. REPLACED CRACKED STRAP PER SRM 51-40-00, 51-40-02. (M) 2 L 7 2 4F RT A16WE 2001042700142 20010427 00142 NM 2001 4 27 USAA010292 1 20010227 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 507AU 45575 23382 CLT - FOUND SKIN CRACKED 2.25 INCH, BS 330 FORWARD SERVICE DOOR CUT OUT. REPAIRED PER SRM 53-10-01 FIG 2. (M) 2 L 7 2 4F RT A16WE 2001042700143 20010427 00143 NM 2001 4 27 USAA010297 1 20010320 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 588US 40053 23933 TPA - FOUND SKIN CRACKED .25 INCH, LOWER LOBE FUSELAGE SKIN DIRECTLY AFT COOLING FAN CUTOUT. INSTALLED REPAIR DOUBLER P ER TR 53-30-07. (M) 2 L 7 2 4F RT A16WE 2001042700144 20010427 00144 NM 2001 4 27 USAA010301 1 20010320 A 5330 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 412US 36306 23881 CLT - FOUND FUSELAGE SKIN CRACKED 2 INCHES, 3 INCHES FORWARD OF 727F 1 INCH ABOVE STRINGER 26R. INSTALLED DOUBLER PER S RM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2001042700145 20010427 00145 NM 2001 4 27 USAA010302 1 20010320 A 5311 FRAME BOEING 737 7374B7 1384702 NM BULKHEAD CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND CHORD SIDE CRACKED .5 INCH, BS 178 BULKHEAD LEFT SIDE CHORD WL 207. INSTALLED REPLACEMENT PER EO 5300V157 A ND EA 69141. (M) 2 L 7 2 4F RT A16WE 2001042700146 20010427 00146 NM 2001 4 27 USAA010303 1 20010320 A 5320 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND ANGLE CRACKED 2 INCHES, FORWARD SERVICE DOOR FRAME LOWER FORWARD INBOARD STATION 298. INSTALLED DOUBLER PER SRM 51-70-11 FIG 1. (M) 2 L 7 2 4F RT A16WE 2001042700147 20010427 00147 NM 2001 4 27 USAA010304 1 20010320 A 5320 STRAP BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND STRAP CRACKED .875 INCH, BS 300 STRINGER 10L. REPLACED CRACKED STRAP PER SRM 51-40-00 AND 51-40-02. (M) 2 L 7 2 4F RT A16WE 2001042700148 20010427 00148 NM 2001 4 27 USAA010305 1 20010320 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FRAME CRACKED .5 INCH, STATION 380 FRAME RIGHT SIDE BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER TR 53 -10-14. (M) 2 L 7 2 4F RT A16WE 2001042700149 20010427 00149 NM 2001 4 27 USAA010306 1 20010320 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FRAME CRCKED .25 INCH, BS 400 BETWEEN STRINGER 8 AND 9 LT. FRAME REPAIR PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 2001042700150 20010427 00150 NM 2001 4 27 USAA010307 1 20010320 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FRAME CRACKED .5 INCH, STATION 400 FRAME RIGHT SIDE BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER TR 53 -10-14. (M) 2 L 7 2 4F RT A16WE 2001042700151 20010427 00151 NM 2001 4 27 USAA010308 1 20010320 A 5311 BAC15171470 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FRAME CRACKED .5 INCH, STATION 440 FRAME RIGHT SIDE BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER TR 53 -10-14. (M) 2 L 7 2 4F RT A16WE 2001042700152 20010427 00152 NM 2001 4 27 USAA010309 1 20010320 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND FRAME CRACKED .5 INCH, STATION 480 FRAME RIGHT SIDE BETWEEN STRINGER 8R AND 9R. INSTALLED FRAME DOUBLER REP AIR PER TR 53-10-04. (M) 2 L 7 2 4F RT A16WE 2001042700153 20010427 00153 NM 2001 4 27 USAA010310 1 20010320 A 5414 SKIN BOEING 737 7374B7 1384702 NM NR 1 PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND SKIN CRACKED 1 INCH, NR 1 ENGINE PYLON PANEL NR 5724L CUTOUT. INSTALLED REPAIR DOUBLER PER TR 54-50-07 FIG 2 STEP 4. (M) 2 L 7 2 4F RT A16WE 2001042700154 20010427 00154 NM 2001 4 27 USAA010311 1 20010320 A 5414 SKIN BOEING 737 7374B7 1384702 NM NACELLE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 32136 24557 CLT - FOUND SKIN CRACKED .75 INCH BY .25 INCH, ACCESS PANEL NR 5828 CUTOUT NACELLE STATION 10 RBL OF 0. INSTALLED REPAI R DOUBLER PER TR 54-30-07. (M) 2 L 7 2 4F RT A16WE 2001042700155 20010427 00155 NM 2001 4 27 USAA010317 1 20010320 A 5320 STRAP BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 50420 24559 CLT - FOUND STABILIZER STRAP .5 INCH CRACK, STATION 344, LBL 45. INSTALLED DOUBLER PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2001042700156 20010427 00156 NM 2001 4 27 USAA010318 1 20010320 A 5320 TIE CLIP BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 50420 24559 CLT - FOUND TIE CLIP CRACKED .125 INCH, STATION 663, STRINGER 10R. REPAIRED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001042700157 20010427 00157 NM 2001 4 27 USAA010319 1 20010320 A 5320 TIE CLIP BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 50420 24559 CLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 663, STRINGER 10L. REPAIRED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001042700158 20010427 00158 NM 2001 4 27 USAA010320 1 20010320 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 50420 24559 CLT - FOUND FRAME CRACKED .25 INCH, STATION 727D, STRINGER 8R-9R. INSTALLED FRAME REPAIR PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001042700159 20010427 00159 NM 2001 4 27 USAA010321 1 20010320 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 50420 24559 CLT - FOUND FRAME CRACKED .25 INCH, STATION 787, STRINGER 8L AND 9L. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001042700160 20010427 00160 NM 2001 4 27 USAA010322 1 20010320 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 50420 24559 CLT - FOUND FRAME CRACKED .5 INCH, STATION 907, STRINGER 8L-9L. INSTALLED FILLER AND REPAIR DOBLER PER TR 53-10-14. (M ) 2 L 7 2 4F RT A16WE 2001042700161 20010427 00161 NM 2001 4 27 USAA010323 1 20010320 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 507AU 45575 23382 CLT - FOUND FUSELAGE SKIN CRACKED 2.25 INCH, FORWARD SERVICE DOOR CUTOUT LOWER AFT CORNER BS 330. FABRICATED AND INSTAL LED REPAIR PARTS PER SRM 53-10-01 FIG 202. (M) 2 L 7 2 4F RT A16WE 2001042700162 20010427 00162 SO 2001 4 27 C2XA01BT035 1 20010312 A 4920 4501968B APU EMB 145 EMB145ER SO TAIL FAULTY A C2XA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 27 14945 4298 145049 EWR - FLT 3605 - CREW REPORTED, STRONG ODOR OF FUEL IN COCKPIT AND CABIN DURING APU START IN FLIGHT. MAINTENANCE REMOVE D AND REPLACED THE APU. OPS CHECKED GOOD. NO SMELL OF FUEL NOTED. AIRCRAFT MEL CLEARED AND RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001042700163 20010427 00163 WP 2001 4 27 USAAD01063 1 20010323 A 3213 STRUT DOUG DC9 DC982 3022082 WP NLG DISCHARGED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 825US 49237 PIT-ABE - FLT 1422 - THE NOSE LANDING GEAR WOULD NOT RETRACT. THE FLIGHT RETURNED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICED THE NOSE GEAR AND PERFORMED SEVERAL GEAR SWING. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F A6WE 2001042700164 20010427 00164 NM 2001 4 27 USAABB01019 1 20010402 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 601AU 22193 SFO - FOUND ALL FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED ALL THE BATTERIES (10 EACH). (M) 2 L 7 2 4F RT A2NM 2001042700165 20010427 00165 WP 2001 4 27 USAAD01066 1 20010329 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 828US 48028 IND - ALL SEAT LIGHTS HAD INOPERATIVE GREEN LIGHTS. MAINTENANCE REPLACED ALL SEAT BATTERIES. (M) 2 L 7 2 4F A6WE 2001042700166 20010427 00166 WP 2001 4 27 USAAD01065 1 20010329 A 3350 9721050 BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 828US 48028 IND - THE LEFT FORWARD ENTRY AND RIGHT FORWARD SERVICE DOORS EMERGENCY EXIT ID LIGHTS WERE INOPERATIVE. MAINTENANCE REP LACED BATTERIES AND THE LEFT FORWARD EMERGENCY EXIT ID LIGHT ASSEMBLY. (M) 2 L 7 2 4F A6WE 2001042700167 20010427 00167 WP 2001 4 27 USAAD01071 1 20010330 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 810US 48042 BOS - THE SEAT MOUNTED EMERGENCY LIGHT BATTERIES WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F A6WE 2001042700168 20010427 00168 WP 2001 4 27 USAAD01070 1 20010329 A 3350 86210151 BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 828US 48028 IND - THE GREEN LIGHT ON THE AFT EXIT BETWEEN LAVATORIES WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY ON THE LIGHT AND CONTROL MODULE. (M) 2 L 7 2 4F A6WE 2001042700169 20010427 00169 WP 2001 4 27 USAAD01069 1 20010329 A 3350 8732030153 MODULE DOUG DC9 DC981 3022081 WP PAX CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 828US 48028 IND - THE GREEN LIGHTS IN THE LEFT AND RIGHT EMERGENCY EXIT ROWS WERE INOPERATIVE. MAINTENANCE REPLACED THE CONTROL MOD ULE IN THE MID CABIN. (M) 2 L 7 2 4F A6WE 2001042700170 20010427 00170 WP 2001 4 27 USAAD01068 1 20010329 A 3350 8732030153 MODULE DOUG DC9 DC981 3022081 WP PAX CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 828US 48028 IND - THE GREEN LIGHTS IN THE AFT CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE CONTROL MODULE AND BATTERY. (M) 2 L 7 2 4F A6WE 2001042700171 20010427 00171 WP 2001 4 27 USAAD01067 1 20010329 A 3350 9721050 BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 828US 48028 IND - THE IDENTIFICATION LIGHT AT THE AFT LEFT LAVATORY POSITION WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND LIGHT BULB. (M) 2 L 7 2 4F A6WE 2001102500139 20011025 00139 WP 2001 10 25 USAAD01060 1 20010910 A 3350 9721055 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 830US 49443 THE LOW LEVEL EMERGENCY LIGHTS AND THE RIGHT AFT EMERGENCY EXIT LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LE VEL EMERGENCY LIGHT BATTERIES AND THE RIGHT AFT EMERGENCY EXIT LIGHT ASSEMBLY. (M) 2 L 7 2 4F A6WE 2001042700172 20010427 00172 WP 2001 4 27 USAAD01062 1 20010323 A 3350 873100272 LIGHT DOUG DC9 DC981 3022081 WP PAX CABIN FAILED A USAA O OTHER O OTHER LD LANDING 1 EA 19 813US 48093 EWR-PIT - FLT 689 - THE EMERGENCY LIGHT CAME ON DURING LANDING. MAINTENANCE REPLACED THE AFT GALLEY RECEIVER. (M) 2 L 7 2 4F A6WE 2001042700173 20010427 00173 WP 2001 4 27 USAAD01075 1 20010403 A 3350 9721055 BATTERY DOUG DC9 DC982 3022082 WP PAX CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 823US 49142 IND - TWO LOW LEVEL EMERGENCY LIGHTS AND TWO SECTIONS OF CEILING EMERGENCY LIGHTS WERE INOPERATAIVE. THE LOW LEVEL EMER GENCY LIGHT FOR SEAT ROW 25 WAS LOCATED AT SEAT ROW 26. MAINTENANCE REPLACED THE LOW LEVEL AND CEILING EMERGENCY LIGHT BATTERIES AND RELOCATED THE LOW LEVEL LIGHT ASSEMBLY TO THE PROPER ROW. (M) 2 L 7 2 4F A6WE 2001042700174 20010427 00174 WP 2001 4 27 20010427AP001 1 20010403 A 3350 AD4002P BATTERY DOUG DC9 DC982 3022082 WP PAX CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 823US 49142 IND - TWO LOW LEVEL EMERGENCY LIGHTS AND TWO SECTIONS OF CEILING EMERGENCY LIGHTS WERE INOPERATAIVE. THE LOW LEVEL EMER GENCY LIGHT FOR SEAT ROW 25 WAS LOCATED AT SEAT ROW 26. MAINTENANCE REPLACED THE LOW LEVEL AND CEILING EMERGENCY LIGHT BATTERIES AND RELOCATED THE LOW LEVEL LIGHT ASSEMBLY TO THE PROPER ROW. REF USAAD01075. (M) 2 L 7 2 4F A6WE 2001042700175 20010427 00175 WP 2001 4 27 USAAD01074 1 20010402 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 800US 48034 IND - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001042700176 20010427 00176 WP 2001 4 27 USAAD01073 1 20010331 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 814US 48094 IND - THE LOW LEVEL EMERGENCY LIGHTS WILL NOT TEST PROPERLY. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001042700177 20010427 00177 WP 2001 4 27 USAAD010172 1 20010330 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC982 3022082 WP PAX CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 820US 49119 PIT - THE ENTRY WAY EMERGENCY LIGHTS WILL NOT STAY OFF WHEN ELECTICAL POWER IS REMOVED FROM THE AIRCRAFT. MAINTENANCE R EPLACED THE EMERGENCY LIGHT POWER SUPPLY. (M) 2 L 7 2 4F A6WE 2001042700178 20010427 00178 NM 2001 4 27 USAASB0108 1 20010318 A 2700 65759606 CONNECTOR BOEING 737 737201 1384454 NM AILERONS DAMAGED A USAA L ABORTED APPROACH F FLT CONT AFFECTED DE DESCENT 1 EA 19 248US 51003 22755 LGA-PBI - FLT 2693 - DURING A DESCENDING TURN THE CONTROL COLUMN SEIZED. NEITHER THE CAPT NOR THE F O COULD MOVE THE CO NTROL COLUMN FOR SEVERAL SECONDS. AFTER A GO-AROUND THE AIRCRAFT LANDED W/O INCIDENT. MX REPLACED THE A/B AILERON PCUS , AUTOPILOT MODE CONTROL PANEL, YAW DAMP COUPLER, AILERON POSITION SENSOR. THE A/C WAS TEST FLOWN TO TPA WITH NO DIFFIC ULTIES. THE FOLLOWING WAS COMPLETED FOR ENGINEERING EVALUATION. A AND B HYD MODULES AND THE ROLL CHANNEL COMPUTER WERE REPLACED, AND FLUID SAMPLES WERE TAKEN FROM THE A AND B HYD SYSTEMS. A BENT PIN IN CONNECTOR D4462P WAS REPAIRED. AFT ER RELEASE FOR SERVICE THE PROBLEM REPEATED AND THE AILERON CENTERING SPRING AND TRIM MECHANISM. 2 L 7 2 4F A16WE 2001042700179 20010427 00179 EU 2001 4 27 USAASA01009 1 20010321 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320214 EU PAX CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 108UW 1061 BOS - THE AIRCRAFT FAILED THE EMERGENCY EXIT LIGHT TEST. MAINTENANCE REPLACED THE LEFT OVERWING EMERGENCY POWER SUPPLY UNIT. OPS CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2001042700180 20010427 00180 EU 2001 4 27 USAAF01013 1 20010330 A 3350 6040681 BATTERY FOKKER F28 F28MK0100 4990807 EU PAX CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 889US 11358 PIT - THE FORWARD ENTRANCE DOOR AND SERVICE DOOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY SU PPLY ASSEMBLY. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT 2001042700181 20010427 00181 EU 2001 4 27 USAAF01014 1 20010403 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU PAX CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 880US 11331 GSO - THE AFT OVERHEAD CEILING AND BOTH LAVATORY EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK N R 1 EIGHT. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT 2001042700182 20010427 00182 NM 2001 4 27 GAIA01081ST 1 20010204 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE BULGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BULGING SKIN AND DISHED FASTENER HEADS ALONG STRINGER 24R BS 22 0. ACCOMPLISHED FUSELAGE SKIN LAP REPAIR BS 220 STRINGER 24R IAW B727 SRM 53-30-3 FIG 5. (M) 2 L 7 3 4F A3WE 2001042700183 20010427 00183 NM 2001 4 27 GAIA01082ST 1 20010204 A 5720 ANGLE BOEING 727 727223 1384074 NM RT WING CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHT STAR, IT WAS DISCOVERED A PREVIOUS REPAIR CRACKED AT RIGHT WING T/E STATION 120 AT INB OARD GROUND SPOILER ACTUATOR SUPPORT. ACCOMPLISHED FABRICATION AND INSTALLATION OF T/E ANGLE IAW B727 SRM 51-40-3 FIG 1 AND 51-30-2. (M) 2 L 7 3 4F A3WE 2001042700184 20010427 00184 NM 2001 4 27 GAIA01083ST 1 20010204 A 5311 65198615 FRAME BOEING 727 727223 1384074 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BULGING SKIN/DISHED FASTENER HEADS ALONG FUSELAGE SKIN BS 295-3 60 AT LEFT LOWER NOSE CHORD. ACCOMPLISHED NOSE WHEEL WELL LEFT LOWER CHORD REPLACEMENT IAW B727 SRM 53-10-4 AND 51-30-2 , 51-20-4. (M) 2 L 7 3 4F A3WE 2001042700185 20010427 00185 NM 2001 4 27 GAIA01084ST 1 20010402 A 5310 SHEAR TIE BOEING 727 727223 1384074 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED LEFT LOWER NOSE CHORD ATTACH ANGLE (SHEAR TIE) AT BS 312 HAS HE AVY CORROSION AND IS CRACKED. ACCOMPLISHED FABRICATION AND INSTALLATION OF SHEAR TIE REPAIR IAW B727 SRM 53-10-4 AND 51 -30-2. (M) 2 L 7 3 4F A3WE 2001042700186 20010427 00186 NM 2001 4 27 GAIA01085ST 1 20010402 A 5312 BULKHEAD BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED A CRACK ON RIGHT WALL ON NWW AT BS 257 AT APPROX WL 180. ACCOM PLISHED BULKHEAD REPAIR BS 257 WL 180 IAW B727 SRM 51-40-2 AND 51-30-2. (M) 2 L 7 3 4F A3WE 2001042700187 20010427 00187 NM 2001 4 27 GAIA01086ST 1 20010402 A 5312 BULKHEAD BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED A CRACK ON RIGHT WALL OF NWW AT BS 265 AT APPROX WL 180. ACCOM PLISHED BULKHEAD REPAIR BS 265 WL 180 IAW B727 SRM 51-40-2 AND 51-30-2. (M) 2 L 7 3 4F A3WE 2001042700188 20010427 00188 NM 2001 4 27 GAIA01087ST 1 20010402 A 5711 FRAME BOEING 727 727223 1384074 NM RT WING CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED RIGHT WING UPPER SPAR LEADING EDGE CORRODED AT WS 90. ACCOMPLI SHED RIGHT WING UPPER SPAR CHORD REPAIR WS 130-139 PER REPAIR ORDER FASI-007RO-1 REV I/R DATED MAR 27, 2001 AND STRUCTUR AL SUBSTANTIATION REPORT AVHM--125 REV I/R DATED 3/27/2001. (M) 2 L 7 3 4F A3WE 2001042700189 20010427 00189 NM 2001 4 27 GAIA01088ST 1 20010402 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED CRACK IN FUSELAGE SKIN BS 240 STRINGER 18L. ACCOMPLISHED FUSEL AGE SKIN REPAIR BS 240 STRINGER 18L IAW B727 SRM 53-30-3 FIG 3. (M) 2 L 7 3 4F A3WE 2001042700190 20010427 00190 NM 2001 4 27 GAIA01089ST 1 20010402 A 5730 SKIN BOEING 727 727223 1384074 NM RT WING CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED RIGHT WING AT WS 224 UPPER SURFACE EXFOLIATED. ACCOMPLISHED RI GHT WING FIXED L/E SKIN REPAIR IAW B727 SRM 57-30-4 FIG 1. (M) 2 L 7 3 4F A3WE 2001042700191 20010427 00191 NM 2001 4 27 GAIA01090ST 1 20010402 A 5313 STRINGER BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED STR 15R IS CRACKED AT BS 720A PLUS 10 INCHES, FORWARD OF THE WI NG SCANNING LIGHT. ACCOMPLISHED STRINGER REPAIR BS 720A PLUS 10 INCHES STRINGER 15R IAW B727 SRM 53-10-3 FIG 5. (M) 2 L 7 3 4F A3WE 2001042700192 20010427 00192 NM 2001 4 27 GAIA01091ST 1 20010402 A 5313 STRINGER BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED STRINGER 15L IS CRACKED AT BS 720A PLUS 10 INCHES, FORWARD OF T HE WING SCANNING LIGHT. ACCOMPLISHED STRINGER REPAIR BS 720A PLUS 10 INCHES STRINGER 15R IAW B727 SRM 53-10-3 FIG 5. ( M) 2 L 7 3 4F A3WE 2001042700193 20010427 00193 NM 2001 4 27 GAIA0192ST 1 20010402 A 5313 STRINGER BOEING 727 727223 1384074 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 1070 STRINGER 22L UPPER FLANGE IS CORRODED. ACCOMPLISHED ST RINGER REPAIR BS 1070 STRINGER 22L IAW B727 SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 2001042700194 20010427 00194 NM 2001 4 27 GAIA01093ST 1 20010402 A 5311 FRAME BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 1166 FRAME RIGHT IS CRACKED AND DENTED AT WL 215. ACCOMPLIS HED FUSELAGE FRAME REPAIR BS 1166 WL 215 IAW B727 SRM 51-40-3 FIG 1. (M) 2 L 7 3 4F A3WE 2001042700195 20010427 00195 NM 2001 4 27 GAIA01094ST 1 20010402 A 5311 FRAME BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 520 RIGHT FRAME IS CRACKED AND DENTED AT WL 215. ACCOMPLISH ED FUSELAGE FRAME REPAIR BS 520 RIGHT WL 215 IAW B727 SRM 51-40-3 FIG 1. (M) 2 L 7 3 4F A3WE 2001042700196 20010427 00196 NM 2001 4 27 GAIA01095ST 1 20010402 A 5311 FRAME BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 540 RIGHT FRAME IS CRACKED AND DENTED AT WL 215. ACCOMPLISH ED FUSELAGE FRAME REPAIR BS 540 RIGHT WL 215 IAW B727 SRM 51-40-3 FIG 1. (M) 2 L 7 3 4F A3WE 2001042700197 20010427 00197 NM 2001 4 27 GAIA01096ST 1 20010402 A 5347 BAC1520792 SEAT TRACK BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED SEAT TRACK CRACKED AT BS 520 LBL 45.50 AS VIEWED FROM THE FORWARD CARGO BAY. ACCOMPLISHED SEAT TRACK REPAIR BS 480-690 LBL 45.50 IAW B727 SRM 53-10-5 FIG 1. (M) 2 L 7 3 4F A3WE 2001042700198 20010427 00198 NM 2001 4 27 GAIA01097ST 1 20010402 A 5754 SKIN BOEING 727 727223 1384074 NM LT WING SLAT CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED LEFT WING NR 3 SLAT INBOARD OF NR 2 TRACK FRONT SPAR STATION 46 7 SKIN IS CRACKED. ACCOMPLISHED SKIN REPAIR NR 3 SLAT FSS 467 IAW B727 SRM 57-30-4. (M) 2 L 7 3 4F A3WE 2001042700199 20010427 00199 NM 2001 4 27 GAIA01098ST 1 20010402 A 5522 SKIN BOEING 727 727223 1384074 NM RT ELEVATOR CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION OF FLIGHTSTAR, IT WAS DISCOVERED NR 3 O/B STATIC DISCHARGER ON RIGHT ELEVATOR HAS CORROSION ON A ND AROUDN EXISTING DOUBLER AND T/E METAL HAS STATIC DISCHARGE DAMAGE TO IT. ACCOMPLISHED RIGHT ELEVATOR UPPER SKIN REPA IR IAW B727 SRM 55-20-3 FIG 2. (M) 2 L 7 3 4F A3WE 2001042700200 20010427 00200 NM 2001 4 27 GAIA01099ST 1 20010402 A 5713 STRINGER BOEING 727 727223 1384074 NM LT WING CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED LEFT WING UPPER STRINGER NR 13 CRACKED AT FORWARD AND AFT RIB A TTACH FLANGES AT WS 629 RIB. ACCOMPLISHED LEFT WING UPPER VENT STRINGER REPAIR WS 629 STRINGER 13 IAW B727 SB 727-57-A1 59 REV 3 FIG 2. (M) 2 L 7 3 4F A3WE 2001042700201 20010427 00201 NM 2001 4 27 GAIA01100ST 1 20010402 A 5712 RIB BOEING 727 727223 1384074 NM LT WING CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED CANTED RIB AT WBL 90.0 LEFT WING INSIDE HIP TANK UPPER ANGLE IS CRACKED. ACCOMPLISHED CANTED RIB UPPER CHORD REPAIR WBL 90.0 LEFT IAW B727 SRM 51-40-4. (M) 2 L 7 3 4F A3WE 2001043000001 20010430 00001 WP 2001 4 30 CALA0100355 1 20010413 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND AFT PIT RT CUSP WEB CRACKED AT STA 1271-1287, RBL 56. THE CRACK WAS STOP DRILLED IAW SRM 51-10-4. A D OUBLER WAS INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 2001043000006 20010430 00006 NM 2001 4 30 2001UALA00498 1 20010410 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 AFT CARGO PIT AT BS 1241 BETWEEN STRINGERS 37L TP 39L, SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED REPLACED SHEAR TIE PER BAC DRAWING 140T2102 AND INSTALLED PER SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001052100023 20010521 00023 NM 2001 5 21 2001UALA00510 1 20010401 A 2750 FLAP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT WING OUT OF ADJ A UALA O OTHER E VIBRATION/BUFFET CR CRUISE 1 WP 29 7254U 21401 CREW REPORTED AIRFRAME VIBRATION AT HIGHER SPEEDS. NO VIBRATION AT LOWER SPEEDS. SUPPLEMENTAL DATA UPDATE RIGHT HAND I NBOARD AFT FLAP ECCENTRIC REQUIRED ADJUSTMENT. NO PARTS REPLACED. SYSTEM CHECKS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001043000007 20010430 00007 CE 2001 4 30 GLBA2001082 1 20010414 A 2162 WARNING LIGHT BEECH 1900 1900D 1154162 CE COCKPIT FALSE INDICATION A GLBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 01 219GL UE219 RIGHT & LEFT ENVIROMENTAL FAIL ANNUNCIATOR ILLUMINATED ON T/O, PERFORMED PRESSURE AND TEMP.TESTS COULD NOT DUPLICATE, O PS CHECKED GOOD 2 L 7 2 4T RT A24CE 2001043000009 20010430 00009 NM 2001 4 30 2001UALA00536 1 20010417 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 BS 368 STRINGERS 37L TO 38L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANC E WITH BAC DRAWING 141T1221. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000010 20010430 00010 EU 2001 4 30 2001UALA00347 1 20010328 A 2911 ACCUMULATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYD SYSTEM FAILED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 452UA 955 AILERON PROBLEM. SUPPLEMENTAL DATA UPDATE BLUE HYDRAULIC SYSTEM ACCUMULATOR FAILED INTERNAL LEAK TEST ON AIRCRAFT. REPL ACED BLUE HYDRAULIC ACCUMULATOR (P/N SB209L1A1-1483), AND BLUE AILERON SERVOCONTROL (P/N 31073-110). 2 L 7 2 4F 4 F RT A28NM E40NE 2001071200090 20010712 00090 NM 2001 7 12 2001UALA00546 1 20010417 A 3210 161T12251 LINK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT MLG MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 LT MAIN LANDING GEAR HAS EVIDENCE OF CONTACTING UPPER WING PANEL DURING RETRACTION. *S/D* STABILIZING LINK WAS FOUND M ISSING, ALLOWING UPSTOP FTG TO ROTATE FREELY, THEREBY CAUSING A PRELOAD BETWEEN GEAR AND GEAR DOOR. THIS CAUSED THE O VER-RETRACTION. LINK WAS POSSIBLY LEFT OFF DURING BRAKE ROD INSPECTION. 2 L 7 2 4F 4 F RT A1NM E24NE 2001043000016 20010430 00016 WP 2001 4 30 ZW0A0100208 1 20010410 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT ON FWD LT FUSELAGE, FOUND CHERRY RIVETED REPAIR AT STA 275, LT SIDE. REPAIRED AREA PER SRM 53-04, FIG 12C. 2 L 7 2 4F A6WE 2001043000017 20010430 00017 WP 2001 4 30 ZW0A0100210 1 20010410 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT IN THE FWD CABIN, FOUND CORROSION ON FLOOR SUPPORT AT BL 56 INCHES, AND FROM STA 160 TO 200. REMOV ED VISIBLE CORROSION PER SPM 6-80-01. NEW SUPPORT FABRICATED FROM EXTRUSION PER MATERIAL SPECIFICATIONS IN SRM 53-14-1, FIG 11. TREATED PART PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001043000018 20010430 00018 EU 2001 4 30 RAIA00104007 1 20010415 A 7931 81071100010 SENSOR AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW124B NE NR1 ENGINE FAILED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 721TE 18158 18158 217 124169 7014-SGF-DURING TAKEOFF NR 1 ENGINE HAD HIGH OIL INDICATION. MANTENANCE REMOVED AND REPLACED NR 1 ENGINE OIL PRESSURE S ENSOR IAW ATR72 MAINTENANCE MANUAL. 2 H 7 2 4T 4 T RT A53EU E2ONE 2001043000019 20010430 00019 EU 2001 4 30 RAIA00104008 1 20010416 A 2120 23095002 SEAL JETAIR JETSTM JETSTM4101 1500501 EU AIR DISTRIBUTION DAMAGED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 558HK 41071 5402-EWR-DURING TAXI LEFT DUCT FAIL LIGHTS ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND GAMAH DUCT SEAL IAW J41 MAINTENANCE MANUAL. 2 L 7 2 4T RT A41NM 2001043000020 20010430 00020 EU 2001 4 30 RAIA00104009 1 20010416 A 2435 23095002 STARTER GEN JETAIR JETSTM JETSTM4101 1500501 EU NR 2 ENGINE FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 560HK 6232 186 41076 7498-STL-NR 2 GENERATOR FELL OFF LINE, WARNING CAPTION ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE NR 2 STARTER G ENERATOR IAW J41 MAINTENANCE MANUAL. 2 L 7 2 4T RT A41NM 2001043000021 20010430 00021 WP 2001 4 30 ABXA010152 1 20010307 A 5347 SEAT TRACK DOUG DC8 DC863F 302198F WP CABIN CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 85679 46041 THE SEAT TRACK AT FUSELAGE STATION 920 HAD A CORRODED FASTENER HOLE. MAINTENANCE INSPECTED AND INSTALLED A NEW SEAT TRA CK AT STATION 870 - 940 IAW DC-8 SRM 51-3-0 AND 51-1-21. 2 L 7 4 4F 4A25 2001043000022 20010430 00022 WP 2001 4 30 ABXA010151 1 20010313 A 5720 FITTING DOUG DC8 DC863F 302198F WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 85679 46041 THE RIGHT WING LOWER FORWARD TRAPEZOID FITTING WAS CRACKED. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM 57 -2-7. 2 L 7 4 4F 4A25 2001043000023 20010430 00023 WP 2001 4 30 ABXA010150 1 20010416 A 5720 FITTING DOUG DC8 DC863F 302198F WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 85679 46041 THE LEFT WING LOWER TRAPEZOID FITTING WAS CRACKED. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM 57-5-2. 2 L 7 4 4F 4A25 2001043000024 20010430 00024 WP 2001 4 30 ABXA010149 1 20010311 A 5347 SEAT TRACK DOUG DC8 DC863F 302198F WP MAIN CARGO BAY CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 85679 46041 THE MAIN CARGO COMPARTMENT SEAT TRACK AT RBL 30, STATION 1723 - 1746 WAS CORRODED. MAINTENANCE INSPECTED AND INSTALLED A NEW SEAT TRACK IAW DC-8 SRM 51-3-0 AND ZANTOP DRAWING 86302. 2 L 7 4 4F 4A25 2001043000025 20010430 00025 WP 2001 4 30 ABXA010148 1 20010312 A 5313 9754931 LONGERON DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 85679 46041 CORROSION WAS FOUND AT THE FORWARD LOWER CARGO PIT BETWEEN STA 280 AND 300, LONGERON 28L. MAINTENANCE INSPECTED AND REP AIRED THE AREA IAW DC-8 SRM 51-1-8 AND DAC DRAWING 9754931. 2 L 7 4 4F 4A25 2001043000026 20010430 00026 NE 2001 4 30 ARWA0010404 2 20010417 A 7230 ENGINE LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B02 54555 NE NR 3 ENGINE VIBRATION A ARWA E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SO 19 308GB 193U1133 NR3 ENGINE VIBRATION UNITS WENT ABOVE 2.5 SHORTLY AFTER LEVEL OFF IN CRUISE. 04:50Z SHUTDOWN ENGINE IN ACCORDANCE WITH A BNORMAL VIBRATION CHECKLIST. HIGH VIBRATION READING WAS ONLY IN THE LOW SELECTION ALL OTHER READINGS WERE NORMAL.CORRECT IVE ACTION: PERFORMED BOROSCOPE INSPECTION IAW L1011 MM VOLUME I FORM PAGE 3-9-1 THRU 3-9-5 NO DISCREPANCIES FOUND. CLEA NED FIR TREE AND LUBED MID-SPANS PER MM 72-31-05, PERFORMED TEST NR11 VIBRATION SURVEY. VIBRATION WITHIN LIMITS. 2 L 7 3 4F 4 F A23WE E12EU 2001043000027 20010430 00027 WP 2001 4 30 ABXA010147 1 20010312 A 5313 LONGERON DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 85679 46041 CORROSION WAS FOUND ON LONGERON 33L BETWEEN FUSELAGE STA 320 - 340 IN LOWER CARGO PIT. MAINTENANCE INSPECTED AND REPAIR ED THE AREA IAW DC-8 SRM 53-2-0. 2 L 7 4 4F 4A25 2001043000028 20010430 00028 WP 2001 4 30 ABXA010146 1 20010311 A 5330 SKIN DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 85679 46041 THE FUSELAGE EXTERIOR SKIN WAS FOUND TO BE CRACKED AT STA 1720 LONGERON 17-18R. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM 53-2-1. 2 L 7 4 4F 4A25 2001043000029 20010430 00029 WP 2001 4 30 ABXA010145 1 20010311 A 5330 SKIN DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 85674 46041 THE FUSELAGE EXTERIOR SKIN AT STATION 1750 LONGERON 15R-16R WAS FOUND TO BE CRACKED BETWEEN FASTENERS. MAINTENANCE INSP ECTED AND REPAIRED THE AREA IAW DC-8 SRM 53-2-1. 2 L 7 4 4F 4A25 2001043000030 20010430 00030 NM 2001 4 30 CALA0100331 1 20010411 A 5755 SKIN BOEING 737 7373T0 1384582 NM SPOILER DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND LT WING NR 2 FLIGHT SPOILER DENTED ON LOWER SURFACE. THE DENTED AREA WAS REMOVED AND A DOUBLER WAS INS TALLED IAW SRM 57-70-01 AND MM 27-61-11. 2 L 7 2 4F RT A16WE 2001043000031 20010430 00031 SO 2001 4 30 RAAA01E405 1 20010411 A 5311 FRAME LKHEED 188 188C 5262604 SO FUSELAGE BENT A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 4 MAINTENANCE CHECK, FOUND FORMER BENT IN BETWEEN STR 34 & 36. REPAIRED FORMER PER SRM 53-2-3. 2 L 7 4 4T 4A22 2001043000032 20010430 00032 WP 2001 4 30 0101341232 1 20010407 A 7931 TRANSMITTER DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 1 ENGINE FAULTY A NWAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 01 232NW 46961 455926 DURING TAKEOFF ROLL, THE NR 1 ENGINE OIL PRESSURE INDICATION DROPPED TO 15 PSI. THE TAKEOFF WAS ABORTED AND THE AIRCRAF T RETURNED TO THE GATE. MAINTENANCE REPLACED THE OIL PRESSURE TRANSMITTER AND THE OIL PRESSURE INDICATOR. AN ENGINE RU N WAS PERFORMED TO HIGH POWER WITH NORMAL INDICATIONS. 2 L 7 3 4F 4 F A22WE E23EA 2001043000033 20010430 00033 EU 2001 4 30 QXEA0100443 1 20010408 A 4910 38075412 APU FOKKER F28 F28MK4000 4990810 EU APU BAY MALFUNCTIONED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 492US 9927 843 11159 PDX-SMELL OF SMOKE COMING FROM FRESH AIR. NO SMELL FROM DUCTS NOTED. REMOVED AND REPLACED APU. OPERATIONAL AND LEAK CHEC KS ARE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001043000034 20010430 00034 NM 2001 4 30 2001UALA00281 1 20010320 A 2432 30874001 BATTERY BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN DISCHARGED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 328UA 24148 BOTH DC LIGHTS ILLUMINATED. SUPPLEMENTAL DATA UPDATE THE M6 AIRCRAFT BATTERY (MR24349-445), AND M5 BATTERY CHARGER (MR24 315-011) WERE REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2001043000035 20010430 00035 CE 2001 4 30 GLBA2001075 1 20010403 A 2722 ACTUATOR BEECH 1900 1900D 1154162 CE RUDDER TRIM STIFF A GLBA K NONE F FLT CONT AFFECTED CR CRUISE 1 CE 01 254GL UE254 RUDDER TRIM STIFF. CLEANED AND LUBRICATED RUDDER TRIM ACTUATORS, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001043000036 20010430 00036 CE 2001 4 30 GLBA2001076 1 20010403 A 2751 SWITCH BEECH 1900 1900D 1154162 CE FLAPS OUT OF ADJ A GLBA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CE 01 240GL UE240 FLAPS STUCK AT 17 PERCENT. CLEANED AND ADJUSTED LEFT FLAP SPLIT SWITCH, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001043000037 20010430 00037 NM 2001 4 30 2001UALA00446 1 20010406 A 2131 CONTROLLER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN PRESSURE FAILED A UALA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 321UA 23953 LOSS OF CABIN PRESSURE. SUPPLEMENTAL DATA UPDATE THE CABIN PRESSURE K8 RELAY HAD A FAILED TRANSISTOR. REPLACED THE CAB IN PRESSURE CONTROLLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100064 20010521 00064 2001 5 21 2001UALA00492 4 20010415 A 2330 176422CY777 VIDEO UNIT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN FAILED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 799UA 26926 ELECTRICAL ODOR AND SMOKE REPORTED IN AFT CABIN. FLIGHT DIVERTED AND LANDED UNDER AMBER ALERT INTO SNN (SHANNON, IRELAN D). MAINT CHECK SEAT FOR FAILED SEAT VIDEO DISTRIBUTION UNITS IN AFT CABIN AREA. SUPPLEMENTAL DATA UPDATE THE VIDEO DIST RIBUTION UNIT AT SEAT 35FG FAILED. THE UNIT AND THE ASSOCIATED SEAT TO SEAT CABLE WERE REPLACED. THE UNIT WAS OPENED A T THE COMPONENT SHOP AND FOUND TO HAVE DAMAGE TO THE POWER SUPPLY. PRELIMINARY REPORT INDICATES A SHORT IN THE POWER SU PPLY. EXACT CAUSE WILL BE DETERMINED AT THE VENDORS FACILITY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001050300323 20010503 00323 NM 2001 5 3 2001UALA00493 1 20010413 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA O OTHER L NO TEST NR NOT REPORTED 1 WP 29 187UA 26876 EMERGENCY EXIT LIGHTS-FLOOR LIGHT DAMAGED. SUPPLEMENTAL DATA UPDATE CAUSE: WIRE W2086-005-20 (REF. WDM33-51-52 PAGE 3 S HEET 1) 2 INCHES FROM CONNECTOR DX321 LOCATED AT DR4L. REPAIRED WIRE PER GNMM 2-0-15-1 PAGE 7. 2 L 7 4 4F 4 F RT A20WE E24NE 2001043000039 20010430 00039 NM 2001 4 30 2001UALA00494 1 20010411 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 MID CABIN FLOOR STRUCTURE SUPPORT ADJACENT TO DOOR 2R BS740 TO BS760 RBL 62 HAS EXCESSIVE MATERIAL LOSS. REPLACED ANGLE S PER SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001043000040 20010430 00040 NM 2001 4 30 2001UALA00495 1 20010410 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 1439 STRINGER 38R TO 39R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T2102 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000041 20010430 00041 NM 2001 4 30 2001UALA00496 1 20010410 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 CORROSION IN STRINGER S35R BETWEEN FRAMES STATION 610 TO 632. MAJOR REPAIR ACCOMPLISHED INSTALLED REPAIR PER SRM 53-00- 03, FIGURE 204. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000042 20010430 00042 NM 2001 4 30 2001UALA00497 1 20010411 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 CREASE BEAM WEB STA 1076 STR 17R HAS EXCESSIVE MATERIAL LOSS. REPLACED CREASE BEAM PER SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001043000043 20010430 00043 NM 2001 4 30 AWXA0001611 1 20010416 A 7722 BACC45FN2255S CONNECTOR BOEING 737 7373S3 1384711 NM EGT SHORTED A AWXA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 28 312AW 24060 PHX - AIR TURNBACK - 4/9/01 - ON CLIMBOUT NR 1 EGT GAUGE NEEDLE DROPPED TO 0; THE CREW RESET THE NR 1 EGT CIRCUIT BREAKE R AND THE NEEDLE DROVE UP TO THE ASSUMED TEMP THEN DROPPED BACK DOWN. THE AIRCRAFT RETURNED TO PHX FOR REPAIR; THIS PRO BLEM HAD SOME RECENT HISTORY. MAINTENANCE FOUND DURING TROUBLESHOOTING SOCKETS 17 & 18 ON CONNECTOR D4012J SHORTING TOG ETHER; AN ENGINEERING REPAIR WAS ISSUED TO MOVE WIRE V152-9264-24R FROM PIN LOCATION NR 18 TO SPARE PIN POSITION NR 35; THE CONNECTOR HAS BEEN SCHEDULED FOR REPLACEMENT AT THE NEXT C-CHECK. NO FURTHER DISCREPANCIES HAVE BEEN NOTED. 2 L 7 2 4F RT A16WE 2001043000044 20010430 00044 EU 2001 4 30 AWXA0001612 1 20010416 A 2930 WARNING LIGHT AIRBUS 320 A320231 3930325 EU COCKPIT ILLUMINATED A AWXA O OTHER J WARNING INDICATION CR CRUISE 1 WP 28 628AW 67 PHX - EMERGENCY LANDING - 4/10/01 - EN ROUTE FROM ORD TO PHX THE FLIGHT CREW GOT AN ECAM WARNING AND CAUTION LIGHT FOR T HE GREEN HYD SYSTEM RESERVOIR OVERHEAT. THE CREW CALLED AN EMERGENCY LANDING; THE CREW CYCLED THE GREEN HYD SYSTEM SWIT CH AND THE GREEN SYSTEM FUNCTIONED NORMALLY AND THE WARNINGS CLEARED AS WELL. AN UNEVENTFUL LANDING. MAINTENANCE PERFO RMED HYDRAULIC INTERNAL LEAK CHECK WHICH CHECKED GOOD. PERFORMED CONTINUITY CHECK THAT CHECKED GOOD. THE GREEN HYD SYS TEM LOW PRESS AND HIGH PRESS FILTERS WERE REMOVED AND REPLACED. NO DEBRIS WAS FOUND IN EITHER FILTER. 2 L 7 2 4F RT A28NM 2001043000045 20010430 00045 WP 2001 4 30 ABXA010144 1 20010313 A 5320 3616789 FITTING DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 85679 46041 CORROSION WAS FOUND AT THE FORWARD AIR-CONDITIONING PRESSURE COMPARTMENT AT THE RIGHT CUSP FITTING. CORROSION WAS FOUND UNDER AND AROUND THE NUT PLATES. MAINTENANCE INSTALLED A NEW FITTING IAW DC-8 SRM 51-1-20 AND 51-3-0. 2 L 7 4 4F 4A25 2001043000046 20010430 00046 WP 2001 4 30 ABXA010143 1 20010309 A 5711 STRUCTURE DOUG DC8 DC863F 302198F WP LT WING LEAKING A ABXA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 23 814AX 85679 46041 THE SPAR CAP WAS FOUND TO BE LEAKING FUEL JUST INBOARD OF THE NR 1 PYLON AT WS 444. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW ABX REA D857-40311MR. 2 L 7 4 4F 4A25 2001043000047 20010430 00047 WP 2001 4 30 ABXA010142 1 20010313 A 5320 4711722504 FITTING DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 85679 46041 CORROSION WAS FOUND ON END FITTING AT FUSELAGE STATION 8-28 LONGERON 27R IN THE FORWARD AIR-CONDITIONING COMPARTMENT. M AINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM 51-1-8, 51-2-0 AND DAC DRAWING 4711722. 2 L 7 4 4F 4A25 2001043000048 20010430 00048 WP 2001 4 30 ABXA010141 1 20010312 A 5320 FITTING DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 85679 46041 CORROSION WAS FOUND ON FITTING AT THE LEFT MLG WHEEL WELL AT FUSELAGE STATION 857. MAINTENANCE INSPECTED AND REPAIRED T HE AREA IAW ABX REA D853-40267-MR AND DC-8 SRM 53-2-0. 2 L 7 4 4F 4A25 2001043000049 20010430 00049 NM 2001 4 30 01FDEA00267 1 20010410 A 3222 SEAL BOEING 727 727233 138408A NM NLG FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 262FE 21624 ON PREFLT INSP NOSE GEAR STRUT FULLY COMPRESSED. TAIL STAND OVER PRESSURIZED. ON GEAR RETRACTION THE RED DOORS & AMBER NOSE GEAR LIGHT REMAIN ILLUM. *S/D* REMOVED NOSE INNER CYLINDER, INSTALL SEALS PER 727 200 MM 32-21-001. REMOVED PIS TON TUBE ASSY PER 727-200 MM 32-21-001-8. ALL IND NORMAL. 2 L 7 3 4F RT A3WE 2001043000050 20010430 00050 NM 2001 4 30 CALA0100341 1 20010412 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND A 3 INCH CRACK IN FORWARD CARGO COMPARTMENT FLOOR SUPPORT AT STA 500 ABOVE S27R. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-40-02 AND 51-40-03. 2 L 7 2 4F RT A16WE 2001043000051 20010430 00051 WP 2001 4 30 CALA0100351 1 20010413 A 5730 SKIN DOUG DC9 DC982 3022082 WP LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND A 2.3 INCH CRACK IN LT WING LEADING EDGE SKIN O/B OF NR 7 SLAT TRACK. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 51-30-5 AND ECRA 5721-01064. 2 L 7 2 4F A6WE 2001043000052 20010430 00052 NM 2001 4 30 JBXA000264 1 20010415 A 2910 FITTING BOEING 737 737* NM HYDRAULIC PUMP LOOSE A JBXA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 05 314ML 30271 SYSTEM-A HYDRAULICS DECREASED FROM 103 PERCENT TO 55 PERCENT INFLIGHT, RETURNED TO BASE. UPON INSPECTION OF NR 1 ENGINE HYDRAULIC PUMP, FOUND QUICK RELEASE FITTING LOOSE, CAUSING LOSS OF FLUID. RESECURED QUICK RELEASE FITTING ON NR 1 ENGI NE DRIVEN PUMP. SERVICED SYSTEM-A HYDRAULICS AND OPERATIONALLY CHECKED PUMP IAW BOEING AMM 29-11-11, OPS CHECKED GOOD A ND NO LEAKS NOTED. 2 L 7 2 4F RT A16WE 2001043000053 20010430 00053 NM 2001 4 30 ZW0A0100201 1 20010412 A 3350 LIGHT BOEING 757 757231 1384950 NM CABIN MISSING A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 711ZX 28481 THE FIRST CLASS EGRESS LIGHTS HAD A SEGMENT MISSING AND WIRES EXPOSED. SPLICED IN ELECTRICAL CONNECTORS P/N 65801-003 A ND 91F9705, AND STOWED WIRES. CHECK-C 5-23-00 LAX. 2 L 7 2 4F RT A2NM 2001043000054 20010430 00054 NM 2001 4 30 ZW0A0100202 1 20010416 A 3350 CONNECTOR BOEING 757 757231 1384950 NM CABIN LOOSE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 717TW 28485 THE EGRESS LIGHT IN FRONT OF THE D-LAVATORY WAS INOPERATIVE. TIGHTENED A LOOSE CONNECTOR. CHECK-C 9-6-00 LAX. 2 L 7 2 4F RT A2NM 2001043000055 20010430 00055 NM 2001 4 30 ZW0A0100203 1 20010415 A 2612 FIRE WARNING BOEING 757 757231 1384950 NM COCKPIT FALSE INDICATION A ZW0A F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 CE 13 716TW 28484 AFT CARGO COMPARTMENT FIRE WARNING WAS INDICATED. CREW DISCHARGED BOTH FIRE BOTTLES BUT WARNING REMAINED ON. NO PROBLE M FOUND ON GROUND AFTER REMOVAL OF LARGE SHIPMENT OF HOT CHILI PEPPERS. CARGO DETECT BITE ACCOMPLISHED PER FM 26-16-00. CHECK-C 4-14-00 LAX. 2 L 7 2 4F RT A2NM 2001043000056 20010430 00056 WP 2001 4 30 ZW0A0100204 1 20010405 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT FOUND IN CABIN, CORROSION ON INTERCOSTAL AND CLIP AT LONGERON 16R, STA 160 TO 165. REMOVED CORROSI ON PER SPM 6-80-01. 2 L 7 2 4F A6WE 2001043000057 20010430 00057 WP 2001 4 30 ZW0A0100206 1 20010405 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT IN AFT CARGO COMPT, FOUND CORROSION ON UPPER EDGE OF FORMER AT STA 1271 BETWEEN RBL 6 AND LBL 6. R EMOVED CORROSION PER SPM 6-80-01. 2 L 7 2 4F A6WE 2001043000058 20010430 00058 WP 2001 4 30 ZW0A0100207 1 20010410 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT FOUND CORROSION AROUND FLIGHT ATTENDANT CHAIR MOUNT ON MEMBRANE AT STA 164 AND BL 15L. CUT OUT DAM AGED AND CORRODED AREA. INSTALLED FILLER AND DOUBLER PER SRM 53-01, PAGE 19, FIG 4 SHEET 3. SEALED AROUND EDGES. 2 L 7 2 4F A6WE 2001043000059 20010430 00059 WP 2001 4 30 ZW0A0100209 1 20010410 A 5320 ATTACH ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT FOUND COCKPIT FLOOR PANEL ATTACH ANGLE CRACKED AT STA 121, LBL 2 INCHES. INSTALLED NEW ANGLE PER S PM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-05. 2 L 7 2 4F A6WE 2001043000060 20010430 00060 EA 2001 4 30 SWIA972503 1 20010412 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN DAMAGED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 416SW 7089 EMERGENCY LIGHTS OUT FROM ROW 5 TO 8. REPAIRED WIRES AT ROW 8, DEFERRED ROW 6. REMOVED LIGHT STRIP AT ROW 6, PLUGGED IN RIGHT DIRECTION. OPS CHECK SATISFACTORY. 2 L 7 2 4F RT A21EA 2001043000061 20010430 00061 SO 2001 4 30 SWIA972505 1 20010413 A 3350 BATTERY PACK EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CABIN DISCHARGED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 209SW 120269 FORWARD EMERGENCY LIGHTS DO NOT ILLUMINATE. REMOVE AND REPLACE THE FORWARD EMERGENCY LIGHTS BATTERY PACK. P/N D366-04- 001, S/N ON 7720, OFF 891. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001043000062 20010430 00062 SO 2001 4 30 C2XA01IA214 1 20010413 A 3260 852701 PROXIMITY SWITCH EMB 145 EMB145LR SO RT MLG OUT OF ADJ A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 15980 145202 SLP - FLIGHT 4054, THE CREW REPORTED THAT AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO SL P WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE RIGHT MAIN LANDING GEAR WEIGHT ON WHEELS PROXIMITY SWITCH, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001043000063 20010430 00063 2001 4 30 ABXA010137 4 20010412 A 3418 9650041029 COMPUTER DOUG DC9 DC941 302207N WP STALL WARNING FAULTY A ABXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 953AX 85329 4253 47608 DURING ROTATION AT SJU THE CREW NOTED A STALL WARNING WITH STICK SHAKER ACTIVATION. THE CREW FOLLOWED ABNORMAL PROCEDUR ES, DECLARED AN EMERGENCY AND RETURNED TO THE FIELD AT SJU. MAINTENANCE INSPECTED AND REPLACED THE LT STALL WARNING COM PUTER. 2 L 7 2 4F A6WE 2001043000064 20010430 00064 SO 2001 4 30 C2XA01IA215 1 20010411 A 3350 AD3127 BATTERY PACK EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15730 120187 IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT SEVERAL EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001043000065 20010430 00065 SO 2001 4 30 C2XA01IA216 1 20010412 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145LR SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13978 145180 IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT SEVERAL EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001043000066 20010430 00066 NE 2001 4 30 CNMA200100012 2 20010414 A 7261 FILTER DOUG DC10 DC1010 3022110 WP GE CF6 CF66K 30020 NE ENGINE CLOGGED A CNMA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SW 07 450AX 46942 451342 NR 2 ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED IN FLIGHT. PERFORMED OIL STRAINER CLOG LIGHT ABNORMAL CHECKLIST. CLOG LIGHT REMAINED ILLUMINATED. ENGINE WAS SHUTDOWN BY FLIGHT CREW. MX REPLACED OIL STRAINER FILTER AND OIL CLOG LIGHT SWI TCH. 2 L 7 3 4F 4 F A22WE E23EA 2001052100001 20010521 00001 NM 2001 5 21 01FDEA00274 1 20010412 A 5320 FITTING BOEING 727 72725C 138400H NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 124FE 19360 DURING ROUTINE INSP STRINGER 18L END FITTING AT BS 1183 FOUND CORRODED. *S/D* REMOVED AND REPLACED STR T-FITTING PER I AW BAC 727 SRM 51-30-2. 2 L 7 3 4F A3WE 2001043000067 20010430 00067 WP 2001 4 30 UPS01835649 1 20010328 A 5313 LONGERON DOUG DC8 DC871F 302199D WP AFT CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 STA. 1260-1280 LONG. 35L IS CRACKED. REPAIRED LONGERON I.A.W. 8110-3 APPROVED DH SK 797-370 2 L 7 4 4F RT 4A25 2001043000068 20010430 00068 WP 2001 4 30 UPS01835651 1 20010330 A 5313 LONGERON DOUG DC8 DC871F 302199D WP LT MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 STA. 879-902,LONG. 24L IS CRACKED. REPAIRED LONG. I.A.W. SRM. 53-2-2 FIG. 5 2 L 7 4 4F RT 4A25 2001043000069 20010430 00069 WP 2001 4 30 UPS01835652 1 20010331 A 5320 3755822505N FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 STA. 300 BETWEEN LONG. 29L-30L BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FIT TING I.A.W. DWG. 3755822,AND SRM. 51-1-20D 2 L 7 4 4F RT 4A25 2001043000070 20010430 00070 WP 2001 4 30 UPS01835653 1 20010331 A 5320 3755822505N FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 STA. 300 BETWEEN LONG. 28L-29L BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FI TTING I.A.W. DWG. 3755822,AND SRM.51-1-20D 2 L 7 4 4F RT 4A25 2001050100171 20010501 00171 WP 2001 5 1 UPS01835657 1 20010420 A 5210 SEAL DOUG DC8 DC871F 302199D WP PAX DOOR FAILED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:N/A COULD NOT MAINTAIN CABIN PRESSURE WITH BOTH PACKS ***SUPPLEMENTAL MRR*** SEALED R2 DOOR AND R1 W INDOW PRESS CHECKED GOOD IAW 21-31-00 2 L 7 4 4F RT 4A25 2001052100063 20010521 00063 2001 5 21 2001UALA00452 4 20010409 A 3442 066500080405 RADAR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE WX SYSTEM FAILED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 470UA 1427 FAILURE OF THE WEATHER RADAR. WEATHER RADAR TRANSCEIVER WAS REPLACED AND THE SYSTEM CHECKED GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2001043000072 20010430 00072 NM 2001 4 30 2001UALA00475 1 20010410 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 AFT PIT BS 1395 STRINGERS 38L TO 39L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED FABRICATED AND INSTALLED REPAIR IN A CCORDANCE WITH BAC DRAWING 140T2102 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000073 20010430 00073 NM 2001 4 30 2001UALA00476 1 20010410 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 AFT BS 1395 STRINGERS 39L TO 39R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED FABRICATED AND INSTALLED REPAIR IN ACCOR DANCE WITH BAC DRAWING 140T2102 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000074 20010430 00074 NM 2001 4 30 2001UALA00477 1 20010410 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 1395 STRINGERS 36L TO 37L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED FABRICATED AND INSTALLED REPAIR IN ACCORDANC E WITH BAC DRAWING 140T2102 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000075 20010430 00075 NM 2001 4 30 2001UALA00478 1 20010410 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 FORWARD PIT BS 522 STRINGERS 33L TO 34L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED INSTALLED NEW SHEAR TIE IN ACCORD ANCE WITH SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000076 20010430 00076 NM 2001 4 30 2001UALA00480 1 20010410 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 FORWARD PIT BS 742 STRINGERS 38R TO 39R SHEAR TIE CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED FABRICATE D AND INSTALLED NEW SHEAR TIE IN ACCORDANCE WITH BAC DRAWING 140T2102 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000077 20010430 00077 NM 2001 4 30 2001UALA00481 1 20010410 A 5311 FRAME BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 STATION 560 STRINGER 38L FRAME LOWER FLANGE CORRODED. MAJOR REPAIR ACCOMPLISHED FABRACATED AND INSTALLED REPAIR IN ACCO RDANCE WITH SRM 53-00-07 AND51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000078 20010430 00078 NM 2001 4 30 2001UALA00482 1 20010410 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 742 STRINGER 39L TO 39R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED FABRACATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T2102 ANDSRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000079 20010430 00079 NM 2001 4 30 2001UALA00483 1 20010410 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 STATION 1241 STRINGER 39L TO 39R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED FABRACATED AND INSTALLED REPAIR IN ACCOR DANCE WITH BAC DRAWING 140T2102 ANDSRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000080 20010430 00080 NM 2001 4 30 2001UALA00484 1 20010411 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 918UA 25385 FUSELAGE SKIN DENTED AT STA 887 STRINGER 21RT. DAMAGED AREA WAS CUT OUT AND A REPAIR PLATE AND FILLER WERE INSTALLED. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001043000081 20010430 00081 NM 2001 4 30 2001UALA00499 1 20010410 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSLEAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 1241 TO 1263 STRINGER 39R CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SR M 53-00-03 FIGURE 202 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000082 20010430 00082 NM 2001 4 30 2001UALA00500 1 20010410 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 1285 TO 1307 STRINGER 34R CORRODED. MAJOR REPAIR ACCOMPLISHEDFABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 53-00-03 FIGURE 204. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000083 20010430 00083 NM 2001 4 30 2001UALA00501 1 20010410 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 1540 TO 1562 STRINGER 28R CORRODED. MAJOR REPAIR ACCOMPLISHED.FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 53-00-03 FIGURE 202 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000084 20010430 00084 NM 2001 4 30 2001UALA00502 1 20010410 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 1540 TO 1562 STRINGER 32R CORRODED. MAJOR REPAIR ACCOMPLISHED.FABRICATED AND INSTALLED NEW REPAIR IN ACCORDANCE WITH SRM 53-00-03 FIGURE 202 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000085 20010430 00085 NM 2001 4 30 2001UALA00503 1 20010410 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 390 TO 412 STRINGERS 27L TO 28L DENT WITH CREASE IN AIRCRAFT SKIN. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALL ED REPAIR IN ACCORDANCE WITH SRM 53-00-01 FIGURE 206. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000086 20010430 00086 NM 2001 4 30 2001UALA00504 1 20010410 A 5311 FRAME BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 764 FRAME CORRODED BETWEEN STRINGS 39R TO 35R. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDA NCE WITH SRM 53-00-07 FIGURE 202. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000087 20010430 00087 NM 2001 4 30 2001UALA00505 1 20010410 A 5311 FRAME BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 1263 BL0-LBL 30 FRAME T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 146T1209-5 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000088 20010430 00088 SO 2001 4 30 SWIA972498 1 20010330 A 2710 AILERON EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE WING STIFF A SWIA K NONE F FLT CONT AFFECTED CR CRUISE 1 NM 07 227SW 120304 AIRCRAFT FEELS EXTREMELY STIFF IN ROLLING TO RIGHT. REQUIRES 3+ UNITS OF AILERON TRIM TO FLY STRAIGHT AND LEVEL. INSPE CTED AILERON TRIM SYSTEM IAW EMB MM 27-12. ALSO INSPECTED AILERON CONTROL SYSTEM PER EMB MM 27-11. ALL CHECKS AND TEST S FOUND AILERON CONTROL AND TRIM SYSTEM TO BE FUNCTIONING NORMALLY. NO DEFECTS FOUND. 2 L 7 2 4T 4 T RT A31SO E20NE 2001043000090 20010430 00090 NM 2001 4 30 2001UALA00507 1 20010414 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 917UA 25384 FUSELAGE SKIN DENTED EXCESSIVE MATERIAL REMOVED AT FUSELAGE STA 415 STRINGER 2RT. ACCOMPLISHED FUSELAGE SKIN FLUSH REPA IR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001060600011 20010606 00011 NM 2001 6 6 2001UALA00508 1 20010415 A 3610 39271611 VALVE 39271611 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE FAILED A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 7454U 21908 NR 3 ENGINE STRUT OVERHEAT LIGHT CLIMBING THROUGH 8000 FEET FROM MIA. *S/D* REPLACED NR 3 13TH STAGE MOD VALVE. OPERA TIONS CHECK NORMAL, NO FURTHER PROBLEMS REPORTED. 2 L 7 3 4F 4 F A3WE E2EA 2001043000091 20010430 00091 NM 2001 4 30 2001UALA00509 1 20010415 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7269U 21416 EXTERNAL FUSELAGE SKIN HAS EXCESSIVE MATERIAL REMOVED . STATION 219.818 INCHES BELOW STRINGER 25L. MAJOR REPAIR ACCOMP LISHED. DOUBLER INSTALLED PER SAM 53-30-3, FIGURE 1. 2 L 7 3 4F 4 F A3WE E2EA 2001052100024 20010521 00024 NM 2001 5 21 2001UALA00511 1 20010412 A 5315 141W8517 FLOORBEAM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 781UA 19318 26945 DISCREPANCIES: STA. 246 BUCKLED STIFFENER AT LBL - 7, RBL - 26.06, 50.0STA. 246 CRACKED STIFFENER AT LBL - 38.5STA. 246 CRACKED MID-CHORD AT LBL - 7 REPAIRED MID-CHORD PER SRM 53-10-51, REPAIR 2.REPLACED CRACKED AND BUCKLED STIFFENERS PER SRM 53-10-51, REPAIR 3. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001060600012 20010606 00012 NM 2001 6 6 2001UALA00512 1 20010410 A 5315 141W8517 FLOORBEAM BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 785UA 18365 0 26954 STA 246 MID-CHORD HORIZ LEG CRACKED AT RBL 38.5. *S/D* REPAIRED PER SRM 53-10-51, REPAIR 2. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001043000092 20010430 00092 NM 2001 4 30 2001UALA00513 1 20010416 A 5320 ANGLE BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE BULKHEAD CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 987UA 21749 T ANGLE CRACKED ON THE FORWARD BULKHEAD OF THE LEFT WHEEL-WELL AT STA 663 LBL 54. REPLACED 12 INCH T ANGLE STIFFENER. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F A16WE E2EA 2001043000093 20010430 00093 NM 2001 4 30 2001UALA00514 1 20010406 A 5311 FRAME BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 AFT PIT FRAME STATION 1351 T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WIT H SRM 53-11-99 AND 51-40-01. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000094 20010430 00094 NM 2001 4 30 2001UALA00515 1 20010313 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 AFT PIT LT FRAME STA 1400 STR 28L TOP OF FRAME DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE PER MM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001043000095 20010430 00095 NM 2001 4 30 2001UALA00517 1 20010315 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE TOOL DAMAGE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 AFT PIT RT SIDE STR 27 STA 1590 HAS TOOL DAMAGE. MAJOR REPAIR ACCOMPLISHED.INSTALLED STRINGER SPLICE PER SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001043000096 20010430 00096 NM 2001 4 30 2001UALA00519 1 20010315 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 MID CABIN FLOORBEAM WEB STA 700 LBL 25 CRACKED. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLERS ON FLOORBEAM PER SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001060100161 20010601 00161 NM 2001 6 1 2001UALA00520 1 20010416 A 7500 CLAMP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE LEAKING A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 7299U 21894 700253 NR 1 ENGINE STRUT OVERHEAT LIGHT CAME ON AFTER ENGINE WAS RUNNING FOR 4 MINUTES AT 1.90 EPR WITH BLEED OFF. LIGHT GOES OFF IF THROTTLE RETARDED TO 1.60. *S/D* THE 13TH STAGE PNEUMATIC DUCT WAS LEAKING AT A CLAMP. THE CLAMP WAS REPLACED AND ENGINE TESTED WITH NO FAULT. OVERHEAT DETECTION MODULE WAS REPLACED AS PRECAUTIONARY MEASURE. 2 L 7 3 4F 4 F A3WE E2EA 2001043000097 20010430 00097 NM 2001 4 30 CALA0100326 1 20010411 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM CABIN GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND LEFT O/B SEAT TRACK GOUGED AT STA 540-727, LBL 46. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-20-01 AND 51-40-00. 2 L 7 2 4F RT A16WE 2001043000098 20010430 00098 NM 2001 4 30 CALA0100327 1 20010411 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE BENT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND AFT PIT DOOR CUTOUT LOWER INTERCOSTAL BENT AT FORWARD FRAME TO AFT FRAME, STA 794-849, LBL 24. THE INT ERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-40-2. 2 L 7 2 4F RT A16WE 2001043000099 20010430 00099 NM 2001 4 30 CALA0100328 1 20010411 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM CABIN GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND LEFT O/B SEAT TRACK GOUGED AND WORN AT STA 480-520, LBL 46. THE DAMAGED SECTION OF SEAT TRACK WAS REMO VED AND A NEW SECTION OF TRACK WAS INSTALLED IAW SRM 53-00-52, 51-21-01, AND ECRA 5100-01844. 2 L 7 2 4F RT A16WE 2001043000100 20010430 00100 NM 2001 4 30 CALA0100329 1 20010411 A 5313 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND A .5 INCH CRACK IN STRINGER 28R AT STA 440. THE CRACKED SECTION OF STRINGER WAS CUT OUT AND A J-ANGLE REPAIR WAS INSTALLED IAW SRM 53-00-03. 2 L 7 2 4F RT A16WE 2001043000101 20010430 00101 NM 2001 4 30 CALA0100330 1 20010411 A 5330 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND THREE CREASES IN LT FUSELAGE EXTERIOR SKIN ALONG LAP SEAM AT STA 275, S19L. THE SKIN WAS REPAIRED IAW SRM 53-00-01. 2 L 7 2 4F RT A16WE 2001043000102 20010430 00102 NM 2001 4 30 CALA0100332 1 20010411 A 5755 SKIN BOEING 737 7373T0 1384582 NM SPOILER DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND LT WING NR 3 FLIGHT SPOILER DENTED ON TOP SURFACE. THE DENTED AREA WAS REMOVED AND A DOUBLER WAS INSTA LLED IAW SRM 57-70-01, FIGURE 204 AND 51-20-01. 2 L 7 2 4F RT A16WE 2001043000103 20010430 00103 NM 2001 4 30 CALA0100333 1 20010411 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL UPPER FLANGE AT BS 380 - 400, LBL 23. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 53-30, 51-21-01, AND 51-40-02. 2 L 7 2 4F RT A16WE 2001043000104 20010430 00104 NM 2001 4 30 CALA0100334 1 20010411 A 5411 FRAME BOEING 737 7373T0 1384582 NM NR 2 PYLON WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND RT ENGINE PYLON FORWARD O/B UPPER CHORD WORN. THE CHORD WAS REPAIRED IAW ECRA 5440-01221 AND EA 04-544 0-0836. 2 L 7 2 4F RT A16WE 2001043000105 20010430 00105 NM 2001 4 30 CALA0100335 1 20010411 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND UPPER SURFACE OF FLOORBEAM CORRODED AT STA 986.5. THE CORRODED SECTION OF FLOORBEAM T-CAP WAS REMOVED AND A NEW SECTION WAS INSTALLED USING REPAIR STRAP AND ANGLES IAW SRM 51-40-00 AND ECRA 5310-03851. 2 L 7 2 4F RT A16WE 2001043000106 20010430 00106 NM 2001 4 30 CALA0100336 1 20010411 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND A 1 INCH CRACK IN FORWARD ENTRYWAY INTERCOSTAL AT FLOORBEAM ATTACH AREA, STA 312, BL 0. THE INTERCOSTA L WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001043000107 20010430 00107 NM 2001 4 30 CALA0100337 1 20010411 A 5320 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND R-1 DOOR I/B CHORD O/B L-ANGLE CORRODED ON TOP AND BOTTOM SURFACES AT STA 312, S18R. THE L-ANGLE WAS R EMOVED AND REPLACED IAW SRM 51-40-02 AND 51-10-02. 2 L 7 2 4F RT A16WE 2001043000108 20010430 00108 SO 2001 4 30 RAAA01E401 1 20010411 A 5730 SKIN LKHEED 188 188C 5262604 SO RT WING CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 4 MAINTENANCE CHECK, FOUND CORROSION IN NR 1 UPPER WING PLANK NUT PLATE HOLES FOR WING TO FUSELAGE F ILLET. REPAIRED PLANK PER LUNDBY DESIGN SERVICE DWG 188372 AND L-188 SRM 51-2-12. 2 L 7 4 4T 4A22 2001043000109 20010430 00109 SO 2001 4 30 RAAA01E402 1 20010411 A 5730 SKIN LKHEED 188 188C 5262604 SO RT WING CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 4 MAINTENANCE CHECK, FOUND RT WING LOWER NR 2 PLANK CRACKED AT MOUNTING SCREW HOLE NR 3 TANK OVERFLO W VALVE WS 128. REPAIRED IAW LDS DWG 188370 AND L-188 SRM 51-2-14. 2 L 7 4 4T 4A22 2001043000110 20010430 00110 SO 2001 4 30 RAAA01E403 1 20010411 A 5311 FRAME LKHEED 188 188C 5262604 SO FUSELAGE CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 4 MAINTENANCE CHECK FOUND CORROSION ON FORMER BETWEEN PREVIOUS REPAIR AND FORMER. REPAIRED PER LKHE ED DRAWING 841811. 2 L 7 4 4T 4A22 2001043000111 20010430 00111 SO 2001 4 30 RAAA01E406 1 20010411 A 5311 FRAME LKHEED 188 188C 5262604 SO FUSELAGE BENT A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED #4 MAINTENANCE CHECK, FOUND FORMER BENT IN BETWEEN STR 36 & 39. REPAIRED FORMER PER L-188 SRM 53-2-3. 2 L 7 4 4T 4A22 2001043000112 20010430 00112 SO 2001 4 30 C2XA01IA207 1 20010407 A 5520 14524987403 HINGE PIN EMB 145 EMB145ER SO ELEVATOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14945 145049 IAH - DURING C-CHECK INSPECTION, THE RIGHT HAND ELEVATOR HINGE PIN WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND RE PLACED THE AFFECTED HINGE PIN IN ACCORDANCE WITH EMB-145 M/M 55-10-00-400-801-A, AND THE AIRCRAFT WAS APPROVED FOR RETUR N TO SERVICE. 2 L 7 2 4F RT T00011AT 2001043000113 20010430 00113 SO 2001 4 30 C2XA01IA208 1 20010407 A 5520 KSC270720V BEARING EMB 145 EMB145ER SO ELEVATOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14945 145049 IAH - DURING C-CHECK INSPECTION, THE LEFT HAND AND RIGHT HAND ELEVATOR SPHERICAL BEARINGS WERE FOUND TO BE CORRODED. MA INTENANCE REMOVED AND REPLACED THE AFFECTED SPHERICAL BEARINGS IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING AUTHOR IZATION EA5510-01016, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001043000114 20010430 00114 NM 2001 4 30 0101295522 1 20010404 A 3260 43467410332206 ANNUNCIATOR BOEING 757 757251 1384970 NM COCKPIT SMOKE A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 01 522US 23616 UPON ARRIVAL TO GATE, FLIGHT CREW NOTICED SMOKE COMING FROM THE LANDING GEAR CONTROL HANDLE OPENING. FIRE EQUIPMENT WAS CALLED OUT. AFTER SHUTDOWN OF ENGINE, APU, AND UTILITY BUSSES, THE SMOKE STOPPED. MAINTENANCE REPLACED THE LEFT LANDI NG GEAR DOWN ANNUNCIATION AND THE PROXIMITY SWITCH ELECTRONICS UNIT. LANDING GEAR INDICATION NORMAL. 2 L 7 2 4F RT A2NM 2001043000115 20010430 00115 WP 2001 4 30 0101319973 1 20010410 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP TAIL INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9340 47346 DURING LINE CHECK, FOUND CATWALK EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED AFT COMPARTMENT POWER SUPPLY. OPERA TIONAL CHECK OK. 2 L 7 2 4F A6WE 2001043000116 20010430 00116 NM 2001 4 30 0101326301 1 20010410 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 661US 23719 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE FROM DOOR 3R TO SEAT 27H AND FROM SEAT 28 TO 48. SE CURED CONNECTIONS AT ROW 26 AND AT SEAT 48. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001043000117 20010430 00117 WP 2001 4 30 0101331147 1 20010404 A 3610 CLAMP DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE BLEED AIR FAILED A NWAA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION CR CRUISE 1 GL 01 147US 46756 686167 WHILE IN CRUISE AT FL260, THE NR 2 ENGINE FIRE WARNING ACTIVATED. THE ENGINE WAS SECURED PER COM AND ONE FIRE BOTTLE WA S DISCHARGED. AN EMERGENCY WAS DECLARED WITH THE FLIGHT LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED THE TWO PNEUMAT IC DUCT CLAMPS WHICH SECURE THE ENGINE 8TH STAGE PNEUMATIC CHECK VALVE. ENGINE RUN AND LEAK CHECK GOOD. 2 L 7 3 4F 4 F A22WE E20EA 2001043000118 20010430 00118 NM 2001 4 30 0101356633 1 20010410 A 2530 SMOKE BOEING 747 747227B 1384888 NM GALLEY DETECTED A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 633US 21991 DURING CRUISE, NOTICED WHITE SMOKE AND ELECTRICAL SMELL COMING FROM THE NR 2 COFFEEMAKER IN NR 1 GALLEY. SMOKE AND SMEL L DIMINISHED AFTER PULLING THE GALLEY CIRCUIT BREAKERS. MAINTENANCE COLLARED THE CIRCUIT BREAKER. LOG PAGE CURRENTLY D EFERRED FOR ADDITIONAL MAINTENANCE. FINAL REPAIR NOT YET COMPLETED. 2 L 7 4 4F A20WE 2001043000119 20010430 00119 SO 2001 4 30 C2XAO1IA210 1 20010411 A 3350 C36601100 BATTERY PACK EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15730 120187 IAHH - DURING POST-FLIGHT INSPECTION, THE CREW REPORTED SEVERAL EMERGENCY EXIT LIGHTS TO BE INOPERATIVE. MAINTENANCE RE MOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001043000120 20010430 00120 SO 2001 4 30 C2XA01IA211 1 20010412 A 2120 UNKNOWN EMB 120 EMB120ER 3260203 SO CABIN ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 58733 120197 IAH - FLIGHT 3035, THE CREW REPORTED A STRONG FUEL ODOR FROM THE APU. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE AIR CONDITIONING SYSTEM USING THE APU BLEED AIR WITH NO DEFECTS NOTED , AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001043000122 20010430 00122 NM 2001 4 30 USAASB01095 1 20010329 A 3040 8300005602 CONTROL UNIT BOEING 737 7372B7 1384560 NM HEATER FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 285AU 39948 23132 RSW - FLT 2635 - EN ROUTE FROM ORF TO FLL, THE LEFT FORWARD WINDOW HEAT OVERHEAT LIGHT ILLUMINATED. CREW REPORTED THAT THE WINDOW BEGAN TO FOG UP AND THAT THEY WERE UNABLE TO RESET CIRCUIT BREAKER. FLIGHT DIVERTED TO RSW AND LANDED WITHOU T FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE L1 WINDOW HEAT CONTROL UNIT AND RESET THE CIRCUIT BREAKER. OP S CHECK GOOD. (M) 2 L 7 2 4F A16WE 2001043000123 20010430 00123 SO 2001 4 30 C2XA01TY078 1 20010410 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN ODOR A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 16961 5317 145103 CAE311032 TYS FLIGHT 4355. THE CREW REPORTED THAT DURING TAKEOFF ROLL THE RT ENGINE OIL PRESSURE WENT TO 116 PSI AND THERE WAS A STRONG ODOR IN THE COCKPIT AND CABIN. THE CREW REJECTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE INSPECTED T HE ENGINE AND PERFORMED GROUND RUN OPERATIONAL CHECKS IAW ROLLSROYCE MM 72-00-00, ALL PARAMETER WERE WITHIN LIMITS AND N O ODOR WAS DETECTED IN COCKPIT OR CABIN. THE AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2001043000124 20010430 00124 EU 2001 4 30 XNA01007 1 20010411 A 3411 PITOT LINE AIRBUS 300 A300B4203 3930306 EU PITOT SYS OBSTRUCTED A TC8A C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 23 473AS 203 ABORTED T/O AT 120 KTS. CAPTS AIRSPEED HAD NO INDICATION AT 70 KTS AND INDICATED APPROX 90 TO 100 KTS W/FO''S STBY AIRS PEED AT 120 KTS. AFTER ABORT W/FO''S INDICATING 70-80 KTS, CAPT''S WAS STUCK AT 100, THEN CAME DOWN BELOW 60 KTS. FLUS HED CAPT''S PITOT SYSTEM IAW A300 MM 34-11-10 FOUND DEBRIS IN LINES. TIGHTENED UP CAPT''S PITOT SYSTEM. ACCOMPLISHED S YS LEAK CHECK IAW A300 MM 34-11-00 & ACCOMPLISHED AIR DATA COMPLETATION CHECK IAW A300 MM 34-11-40. ALL SYSTEMS NORMAL. 2 L 7 2 4F RT A35EU 2001043000125 20010430 00125 NM 2001 4 30 HNAA0100024 1 20010411 A 3320 BR63031023 BALLAST DHAV DHC8 DHC8102 2809003 NM CABIN OVERHEATED A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 EA 07 927HA 117 F/A NOTICED SMOKE AND ELECTRICAL SMELL IN CABIN. FOUND CENTER OVERHEAD LIGHT AT ROW 8 DIM AND BALLAST EXTREMELY HOT TO THE TOUCH. REPLACED THE LUMINAIRE/BALLAST ASSY. 2 H 7 2 4T RT A13NM 2001043000126 20010430 00126 WP 2001 4 30 ABXA010130 1 20010409 A 2740 591096233 JACKSCREW DOUG DC9 DC933F 302207A WP HORIZ STAB CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 41741 47413 THE HORIZONTAL STABILIZER JACKSCREW WAS FOUND TO HAVE PITTING CORROSION ON THE UPPER THREE THREADS. THE 26TH THREAD FRO M THE BOTTOM OF THE JACKSCREW WAS ALSO NOTED TO BE CHIPPED. MAINTENANCE REPLACED THE JACKSCREW ASSEMBLY IAW DC-9 MM 27- 40-01. 2 L 7 2 4F A6WE 2001043000127 20010430 00127 NM 2001 4 30 2001UALA00485 1 20010410 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 1131 STRINGERS 34R TO 35R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED FABRACATED AND INSTALLED REPAIR IN ACCORDANC E WITH BAC DRAWING 140T2102 ANDSRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000128 20010430 00128 NM 2001 4 30 2001UALA00486 1 20010410 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 1417 STRINGERS 38R TO 39R SHEAR TIE CIRRIDED. MAJOR REPAIR ACCOMPLISHEDFABRACATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T2102 ANDSRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000129 20010430 00129 NM 2001 4 30 2001UALA00487 1 20010410 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 1417 STRINGERS 39L TO 39R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED FABRACATED AND INSTALLED SHEAR TIE IN ACCORD ANCE WITH BAC DRAWING 140T2102 ANDSRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000130 20010430 00130 NM 2001 4 30 2001UALA00488 1 20010410 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 1373 STRINGERS 36L TO 37L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED FABRACATED AND INSTALLED REPAIR IN ACCORDANC E WITH BAC DRAWING 140T2102 ANDSRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000131 20010430 00131 NM 2001 4 30 2001UALA00489 1 20010410 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 1439 STRINGERS 39L TO 39R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED FABRACATED AND INSTALLED REPAIR IN ACCORDANC E WITH BAC DRAWING 140T2102 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071100026 20010711 00026 NM 2001 7 11 2001UALA00490 1 20010406 A 2730 FILTER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE ELEVATOR FAILED A UALA O OTHER F FLT CONT AFFECTED IN INSP/MAINT 1 WP 29 607UA 21868 EICAS R ELEV IND NOT MOVING ON CONTROL CHECK. SEVERAL ATTEMPTS, STICK GAVE A JUMP AND NOW INDICATOR FUNCTIONS, BUT CONT ROLS SPONGY. *S/D* LOSS OF ELEV EICAS INDICATION WAS ATTRIBUTED TO A FAILED IN-LINE ELECTRICAL FILTER (L-C FILTER) AN D SPLICE. THE SPONGY FEEL OF THE ELEV CONTROLS WAS ATTRIBUTED TO AN OUT OF RIG CONDITION OF THE ELEV POWER CONTROL ACTU ATORS (PCA'S). THE SUBJECT L-C FILTER WAS REPLACED AND RESPLICED PER WDM BOTH ELEV POSITION TRANSMITTERS WERE ADJUSTED PER MM . THE ELEV PCA RIGGING WAS CHECKED AND CORRECTED AS REQUIRED PER MM . A ELEV INPUT LINKAGE BELLCRANK WAS FOUND OUT OF SERVICEABLE LIMITS AND WAS REPLACED. THE BELLCRANK DID NOT CONTRIBUTE TO THE LOSS OF ELEV INDICATION. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000132 20010430 00132 NM 2001 4 30 ABXA010131 1 20010413 A 2913 3508807 PUMP BOEING 767 767281 1385109 NM NR 1 ENGINE FAILED A ABXA O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 773AX 697 22788 THE LEFT HYDRAULIC QUANTITY WENT TO ZERO IN FLIGHT. THE LEFT ENGINE PRIMARY HYDRAULIC PRESSURE LIGHT ILLUMINATED. MAIN TENANCE INSPECTED AND REPLACED THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP IAW B767 MM 29-11-05. 2 L 7 2 4F RT A1NM 2001043000133 20010430 00133 NM 2001 4 30 CALA0100338 1 20010412 A 5743 658411916 BEARING BOEING 737 7373T0 1384582 NM RT MLG FROZEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND RT MLG SUPPORT BEAM HAD LOOSE BEARING HOUSING AND FROZEN BEARING AT MOUNT FITTING. REMOVED NR 5 FLAP T RACK WITH TRANSMISSION, REMOVED FITTING AND INSTALLED NEW BEARING. REINSTALLED NR 5 FLAP TRACK WITH TRANSMISSION. MAIN TENANCE WAS PERFORMED IAW MM 27-51-71, PAGE 410-411 AND ECRA 5750-03524. 2 L 7 2 4F RT A16WE 2001043000134 20010430 00134 WP 2001 4 30 CALA0100339 1 20010412 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND L-1 DOOR FUSELAGE EXTERNAL SURFACE OF GUST LOCK LATCH SKIN CRACKED. REMOVED REPAIR FASTENERS AND INSTA LLED DOUBLERS IAW SRM 53-04, FIGURE 24, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 2001043000135 20010430 00135 NM 2001 4 30 CALA0100340 1 20010412 A 5511 RIB BOEING 737 7373T0 1384582 NM HORIZ STAB WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND RT ELEVATOR CENTER BALANCE HAD WEAR MARKS ON I/B WALL (HOR STAB RIB) AT STA 66.54. THE WORN AREA WAS R EMOVED IAW SRM 57-70-10, PARA 4B. FILLER AND DOUBLER WERE INSTALLED IAW SRM 51-70-10, PARA 5 & 9. REINSTALLED SEALS RE MOVED FOR REPAIR IAW MM 27-31-41. 2 L 7 2 4F RT A16WE 2001043000136 20010430 00136 NM 2001 4 30 CALA0100342 1 20010412 A 5320 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND A .5 INCH CRACK IN FORWARD ENTRYWAY L-ANGLE AT FLOORBEAM AFT FLANGE ATTACH POINT, STA 344, LBL 10. THE L-ANGLE ON TOP OF INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-0. 2 L 7 2 4F RT A16WE 2001043000137 20010430 00137 NM 2001 4 30 CALA0100343 1 20010412 A 5320 CHANNEL BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND CHANNEL CORRODED AT L-1 DOOR THRESHOLD CUSP WEB, L18L. THE CHANNEL WAS REMOVED AND REPLACED IAW SRM 51 -40-02. 2 L 7 2 4F RT A16WE 2001043000138 20010430 00138 WP 2001 4 30 CALA0100344 1 20010412 A 5321 INSERT DOUG DC9 DC982 3022082 WP FLOOR PANEL CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND CABIN FLOOR PANEL HAD CORRODED INSERTS. A NEW PANEL WAS INSTALLED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001043000139 20010430 00139 WP 2001 4 30 CALA0100345 1 20010412 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND RT CABIN FLOOR PANEL AT FS 886-927 HAD TWO EDGE CRACKS AND WEAR IN CENTER OF PANEL. A NEW PANEL WAS IN STALLED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001043000140 20010430 00140 NM 2001 4 30 CALA0100346 1 20010412 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND RIGHT O/B MAIN CABIN SEAT TRACK CORRODED AT STA 540-727. THE CORRODED SECTION OF SEAT TRACK WAS REMOVE D AND REPLACED IAW SRM 53-00-52. 2 L 7 2 4F RT A16WE 2001043000141 20010430 00141 WP 2001 4 30 UPS01835599 1 20010330 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 LEFT WING L/E. UPPER RIB IS CRACKED AT XFS. 360.250. REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2001043000142 20010430 00142 WP 2001 4 30 CALA0100347 1 20010412 A 5321 INSERT DOUG DC9 DC982 3022082 WP FLOOR PANEL CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND LT CABIN FLOOR PANEL AT FS 1079-1124 HAD CORRODED INSERTS. A NEW PANEL WAS INSTALLED IAW ECRA 5320-012 65. 2 L 7 2 4F A6WE 2001043000143 20010430 00143 NM 2001 4 30 CALA0100348 1 20010412 A 5320 WEB BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND FORWARD END OF FLOOR PAN CORRODED AT STA 986.5-1016, RBL 36-48. THE CORRODED FLOOR PAN WEB WAS REMOVED AND A NEW FLOOR PAN WEB WAS INSTALLED IAW SRM 51-10-2, 51-40-01, AND DRAWING 65C32677. 2 L 7 2 4F RT A16WE 2001043000144 20010430 00144 NM 2001 4 30 CALA0100349 1 20010412 A 5320 PAN BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND FLOOR PAN AT STA 1016 TO AFT PRESSURE BULKHEAD CORRODED AT BL 0 TO LBL 48. THE FLOOR PAN WAS REMOVED A ND A NEW FLOOR PAN WAS INSTALLED IAW SRM 51-10-02, DRAWING 65-52878 AND DRAWING 65C32677. 2 L 7 2 4F RT A16WE 2001043000145 20010430 00145 NM 2001 4 30 CALA0100350 1 20010412 A 5320 WEB BOEING 737 7373T0 1384582 NM CARGO BAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND FORWARD CARGO COMPARTMENT DOOR OPENING LOWER SUPPORT PANEL (SILL WEB) CORRODED AT STA 440-490, S25R. T HE SILL WEB WAS REMOVED AND A NEW SILL WEB WAS INSTALLED IAW SRM 51-40-5, 51-40-6, AND 51-40-8. 2 L 7 2 4F RT A16WE 2001043000146 20010430 00146 WP 2001 4 30 CALA0100352 1 20010413 A 5321 INSERT DOUG DC9 DC982 3022082 WP FLOOR PANEL CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND AFT END OF LEFT I/B FLOOR PANEL CORRODED AROUND SCREW HOLES AT FS 1003-1079. A NEW FLOOR PANEL WAS INS TALLED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001043000147 20010430 00147 NM 2001 4 30 GAIA01101ST 1 20010402 A 5320 INTERCOSTAL BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED INTERCOSTAL TO FRAME ATTACH ANGLE IS CRACKED AT STRINGER 22L BS 720D. ACCOMPLISHED INTERCOSTAL REPAIR BS 720D STRINGER 22L IAW B727 SRM 53-10-2 FIG 3. (M) 2 L 7 3 4F A3WE 2001043000148 20010430 00148 NM 2001 4 30 GAIA01102ST 1 20010402 A 5320 ANGLE BOEING 727 727223 1384074 NM TAIL SKID CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED TAIL SKID UPPER ATTACH T-CHORD CORRODED AND 2 EACH VERTICAL SUP PORT ANGLES CORRODED. ACCOMPLISHED TAIL SKID UPPER ATTACH T-CHORD REPAIR AND TWO EACH VERTICAL STIFFENERS IAW B727 SRM 51-40-3 FIG 1. (M) 2 L 7 3 4F A3WE 2001043000149 20010430 00149 NM 2001 4 30 GAIA01103ST 1 20010402 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE GOUGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED GOUGE ON FUSELAGE EXTERNAL SKIN AT BS 218 STRINGER 19L ACCOMPL ISHED FUSELAGE SKIN REPAIR IAW B727 SRM 53-30-3 FIG 5. (M) 2 L 7 3 4F A3WE 2001043000150 20010430 00150 NM 2001 4 30 GAIA01104ST 1 20010402 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE GOUGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED DENTS/GOUGES ON FUSELAGE SKIN T BS 430 1 INCH BELOW STRINGER 25 L. ACCOMPLISHED FUSELAGE SKIN REPAIR IAW B727 SRM 53-30-3 FIG 1. (M) 2 L 7 3 4F A3WE 2001043000151 20010430 00151 NM 2001 4 30 GAIA01105ST 1 20010402 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE GOUGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED DENT IN FUSELAGE SKIN AT BS 670 BETWEEN STRINGER 23-24L. ACCOM PLISHED FUSELAGE SKIN REPAIR IAW B727 SRM 53-30-3 FIG 1. (M) 2 L 7 3 4F A3WE 2001043000152 20010430 00152 NM 2001 4 30 GAIA01115ST 1 20010402 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE GOUGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED DENT IN FUSELAGE SKIN AT BS 590 BETWEEN STRINGER 24-25L. ACCOM PLISHED FUSELAGE SKIN REPAIR IAW B727 SRM 53-30-3 FIG 1. (M) 2 L 7 3 4F A3WE 2001043000153 20010430 00153 NM 2001 4 30 GAIA01116ST 1 20010402 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE GOUGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED GOUGES IN FUSELAGE SKIN AT BS 205 BETWEEN STRINGER 25-26L. ACC OMPLISHED FUSELAGE SKIN REPAIR IAW B727 SRM 53-30-3 FIG 1. (M) 2 L 7 3 4F A3WE 2001043000154 20010430 00154 NM 2001 4 30 GAIA01117ST 1 20010402 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE GOUGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED GOUGES ON FUSELAGE SKIN AT BS 258 ON STRINGER 16L. ACCOMPLISHE D FUSELAGE SKIN REPAIR IAW B727 SRM 53-30-3 FIG 3A. (M) 2 L 7 3 4F A3WE 2001043000155 20010430 00155 2001 4 30 USAABB01016 4 20010323 A 2565 60B1002624 CABLE BOEING 757 7572B7 1384964 NM PAX DOOR SLIDE BROKEN A K NONE O OTHER IN INSP/MAINT 1 EA 19 624AU 27245 SFO - WHILE OPENING THE L4 DOOR FROM OUTSIDE THE AIRCRAFT, THE SLIDE DEPLOYMENT SEQUENCE BEGAN (THE DOOR ASSIST BOTTLE A CTIVATED). MAINTENANCE FOUND THE DOOR DISARM CABLE BROKEN AND REPLACED IT. (M) 2 L 7 2 4F RT A2NM 2001043000156 20010430 00156 2001 4 30 USAABB01017 4 20010328 A 2565 GIRT BAR BOEING 757 757225 1384959 NM PAX DOOR SLIDE DISLODGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 600AU 22192 CLT - DURING A TEST OF THE R3 DOOR EMERGENCY ESCAPE SLIDE, THE GIRT BAR POPPED OUT OF THE FLOOR BRACKETS. (M) 2 L 7 2 4F RT A2NM 2001043000157 20010430 00157 NM 2001 4 30 USAABB01018 1 20010329 A 3610 BLEED AIR SYS BOEING 757 7572B7 1384964 NM CABIN ODOR A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 623AU 27244 CLT - FLT 40 - AFTER TAKEOFF, CREW NOTED AN ODOR IN THE COCKPIT AND CABIN. FLIGHT RETURNED TO CLT AND LANDED WITH NO FU RTHER INCIDENT. MAINTENANCE RAN THE ENGINES AND OPERATED THE GENERATORS AT MAX LOAD (GALLEYS, IFE, ECT). NO FAULTS WER E PRESENT. ALL CIRCUIT BREAKER PANELS AND ELECTRICAL LOAD CENTRS WRE CHECKED WITH NO DISCREPANCIES NOTED. THE ODOR WAS ISOLATED TO THE RIGHT BLEED SYSTEM, AND THE ODOR DISSIPATED AS THE ENGINE RAN. NO ABNORMAL ENGINE PARAMETERS WERE NOTE D. THIS ENGINE HAD BEEN INSTALLED THE PREVIOUS NIGHT. (M) 2 L 7 2 4F RT A2NM 2001043000158 20010430 00158 EU 2001 4 30 USAABA01002 1 20010330 A 5270 WARNING SYSTEM AIRBUS 330 A330323 EU RT PAX DOOR ACTIVATED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 671UW 323 JAX - FLT 2 EN ROUTE MIA-PHL, CREW RECEIVED THE ECAM WARNING DOOR RT AFT CABIN AND THE ASSOCIATED LIGHT. NO PRESSURIZAT ION PROBLEMS WERE EVIDENT. FLIGHT DIVERTED TO JAC AND LANDED WITHOUT FURTHER INCIDENT. (M) 2 L 7 4 4F RT A46NM 2001043000159 20010430 00159 NM 2001 4 30 USAA010335 1 20010326 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 50420 24559 CLT - FOUND FLOORBEAM CORRODED 2 INCHES BY .102 INCHES, STATION 987 BETWEEN RBL 54 AND LBL 48. INSTALLED REPAIR TO T-CA P, SRM 53-00-01 AND TR 53-60-01. CORROSION LEVEL 1, C53-107-02. (M) 2 L 7 2 4F RT A16WE 2001043000160 20010430 00160 NM 2001 4 30 USAA010336 1 20010326 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 50420 24559 CLT - FOUND FRAME CRACKED .250 INCH, STATION 400 BETWEEN S8L AND S9L. INSTALLED REPAIR DOUBLER, TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001043000161 20010430 00161 NM 2001 4 30 USAA010338 1 20010326 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 50420 24559 CLT - FOUND FRAME CRACKED .250 INCH, STATION 787 BETWEEN S8L AND S9L. INSTALLED REPAIR DOUBLER, TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001043000162 20010430 00162 NM 2001 4 30 USAA010339 1 20010326 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 50420 24559 CLT - FOUND FRAME .250 CRACKED, STATION 867 BETWEEN S8L AND S9L. INSTALLED REPAIR DOUBLER, TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001043000163 20010430 00163 NM 2001 4 30 USAA010340 1 20010326 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 50420 24559 CLT - FOUND FRAME CRACKED .250 INCH, STATION 440 BETWEEN S8R AND S9R. INSTALLED DOUBLER, TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001043000164 20010430 00164 NM 2001 4 30 USAA010341 1 20010326 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 50420 24559 CLT - FOUND FRAME CRACKED .250 INCH, STATION 480 BETWEEN S8R AND S9R. INSTALLED DOUBLER, TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001043000165 20010430 00165 NM 2001 4 30 USAA010342 1 20010326 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 50420 24559 CLT - FOUND FRAME CRACKED .250 INCH, STATION 500D BETWEEN S8R AND S9R. INSTALLED DOUBLER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001043000166 20010430 00166 NM 2001 4 30 USAA010343 1 20010326 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 50420 24559 CLT - FOUND FRAME CRACKED .250 INCH, STATION 727D BETWEEN S8R AND S9R. INSTALLED DOUBLER, TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001043000167 20010430 00167 NM 2001 4 30 USAA010345 1 20010326 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 50420 24559 CLT - FOUND FRAME CRACKED .250 INCH, STATION 827 BETWEEN S8L AND S9L. INSTALLED DOUBLER, TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001043000168 20010430 00168 NM 2001 4 30 USAA010337 1 20010326 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 50420 24559 CLT - FOUND FRAME CRACKED .250 INCH, STATION 747, BETWEEN S8L AN S9L. INSTALLED REPAIR DOUBLER, TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001043000169 20010430 00169 NM 2001 4 30 USAA010344 1 20010326 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 50420 24559 CLT - FOUND FRAME CRACKED .250 INCH, STA 747 BETWEEN S8R AND S9R. INSTALLED DOUBLER. (M) 2 L 7 2 4F RT A16WE 2001043000170 20010430 00170 NM 2001 4 30 AWXA0001609 1 20010413 A 5315 BAC1518338 FLOORBEAM BOEING 757 7572G7 1384963 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 909AW 24522 FLOORBEAM AT BS 350 HAS CORROSION AND BARE METAL AROUND FLOORBOARD FASTENERS HOLES ON THE UPPER AND LOWER SURFACE OF THE TOP FLANGE FROM LBL 60 RBL 60. REMOVED EXISTENT SPLICE CHORD IAW SRM 51-40-02; FABBED EXISTENT SPLICE CHORD IAW SRM 53 -00-51; INSTALLED SPLICE IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2001043000171 20010430 00171 NM 2001 4 30 AWXA0001610 1 20010413 A 5320 655479712 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 FS 277 AT 14R LONGERON HAS .75 INCH CRACK IN INTERCOSTAL WEB. REMOVED DAMAGED AREA IAW SRM 51-70-01, NDT - NO CRACKS. FABBED AND INSTALLED ANGLE AND SHIM REPAIR IAW SRM 51-70-11; TREATED AND PRIMED IAW SRM 51-20-01. 2 L 7 2 4F RT A16WE 2001043000172 20010430 00172 NM 2001 4 30 USAA010359 1 20010405 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 33516 22953 CLT - FOUND FRAME CRACKED .250 INCH, STATION 500A BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER. (M) 2 L 7 2 4F RT A16WE 2001043000173 20010430 00173 CE 2001 4 30 GLBA2001080 1 20010411 A 2131 13037432 CONTROLLER BEECH 1900 1900D 1154162 CE CABIN PRESSURE MALFUNCTIONED A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 170GL 3591 2154 UE170 CABIN PRESSURIZATION SPIKED SEVERAL TIMES AFTER T/O. REPLACED PRESSURE CONTROLLER, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001043000174 20010430 00174 SO 2001 4 30 SWIA972500 1 20010410 A 4950 CONTROL VALVE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE APU FAILED A SWIA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 561SW 120335 ON THE GROUND W/APU RUNNING, CABIN SMOKE DETECTOR IS ACTIVATED. ISOLATED SOURCE TO BE LEFT PACK. APU LOAD CONTROL VALV E CLOSED LIGHT ILLUMINATES WITH SWITCH IN OPEN POSITION. UPON TROUBLESHOOTING, FOUND VENTURI TUBE ASSEMBLY CRACKED. RE MOVED AND REPLACED WITH SERVICEABLE UNIT. WASHED HEAT EXCHANGERS, RAN COOLING FAN FOR 30 MINS, RAN AIRCRAFT. DISCREPAN CIES STILL EXISTS. P/N 120-50481-001. ISOLATED SOURCE TO APU. REPLACED APU LOAD CONTROL VALVE AND RAN APU. OPS CHECK GOOD. P/N ON 109812-1, S/N ON P-112C, P/N OFF 109812-9, S/N OFF 2276. 2 L 7 2 4T 4 T RT A31SO E20NE 2001043000175 20010430 00175 EA 2001 4 30 SWIA972501 1 20010412 A 2740 CONTROL UNIT CNDAIR CL600 CL6002B19 EA HORIZ STAB CONTAMINATED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 410SW 7066 STAB TRIM CHANNEL 2 WILL NOT ENGAGE. WITH STAB TRIM CHANNEL 1 ENGAGED, THE MACH TRIM WILL NOT ENGAGE. REMOVE AND REPLA CE MOTOR CONTROL UNIT (MCU) HORIZONTAL STABILIZER TRIM ACTUATOR IAW 27-42-01. FOUND HORIZONTAL STABILIZER CONTROL UNIT (HSTCU) WET WITH WATER. REMOVE AND REPLACE HSTCU IAW 27-41-01. OPS CHECK GOOD. COMPLIED WITH OPS CHECK OF MACH TR IM IAW 27-35-25. OPS CHECK GOOD AT THIS TIME. MCU: P/N ON 7026-2, S/N ON 218, S/N OFF 328, HSTA: P/N ON 8396-3, S /N ON 281, S/N OFF 910, HSTCU: P/N ON 7060-8, P/N OFF 7060-7, S/N ON 174, S/N OFF 350. 2 L 7 2 4F RT A21EA 2001043000176 20010430 00176 SO 2001 4 30 SWIA972502 1 20010412 A 2150 VENTURI EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT A/C PACK BLOWN A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 07 298SW 120328 INFLIGHT, WHEN PACKS (A/C) ARE SELECTED TO NORM, A BURNING PACK ODOR OCCURS. INSPECTED A/C PACKS. FOUND RIGHT VENTURI BLOWN OUT. REPLACED WITH SERVICEABLE UNIT. RAN BOTH PACKS. NO DISCREPANCIES NOTED AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 2001043000177 20010430 00177 NM 2001 4 30 EIA2001183 1 20010312 A 5210 SKIN BOEING 747 747273C 1384896 NM PAX DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND MED L3 DOOR CRACKED AT UPPER HINGE CUTOUT LOWER CORNER APPROX .125 INCH LENGTH. REPAIRED L3 DOOR UPPE R HINGE CUTOUT SKIN PER BSB 747-52-2144 FIG 5. (M) 2 L 7 4 4F A20WE 2001043000178 20010430 00178 NM 2001 4 30 01FDEA00272 1 20010412 A 5320 65401174 FITTING BOEING 727 72725C 138400H NM RT MLG WW CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 124FE 19360 DURING ROUTINE INSP, RT MAIN GEAR DOOR TO WING FAIRING ROLLER FITTING FOUND CRACKED. ** S/D ** R&R FITTING PER IAW BA C 727 SRM 51-30-2. 2 L 7 3 4F A3WE 2001043000179 20010430 00179 NM 2001 4 30 USAA010367 1 20010405 A 5320 695335214 TIE CLIP BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 33516 22953 CLT - FOUND TIE CLIP CRACKED .250 INCH, STATION 787, STRINGER 10L. REPLACED PART PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2001043000180 20010430 00180 NM 2001 4 30 USAA010369 1 20010405 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 33516 22953 CLT - FOUND FLOORBEAM CORRODED LBL 8-14, STATION 312, LBL 8 TO RBL 14. REPAIRED PER SRM 53-10-51, FIG 205. (M) 2 L 7 2 4F RT A16WE 2001043000181 20010430 00181 NM 2001 4 30 AALA20010693 1 20010329 A 5330 SKIN BOEING 727 727227 1384078 NM FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 729AA 20736 TUL - FOUND STATION 1120 BETWEEN STRINGER 15L AND 16L DEEP DENT AND GOUGE. REMOVED DAMAGED AREA AND REPAIRED WITH FLUSH PATCH AS PER RM 53-30-3 PART 1. (M) 2 L 7 3 4F A3WE 2001043000182 20010430 00182 NM 2001 4 30 2001UALA00479 1 20010410 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 FORWARD PIT BS 742 STRINGERS 38R TO 39R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED INSTALLED NEW SHEAR TIE IN ACCORD ANCE WITH SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000185 20010430 00185 WP 2001 4 30 CALA0100363 1 20010414 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND A 2 INCH CRACK IN LT CUSP WEB AT LIGHTENING HOLE, STA 1295. A DOUBLER WAS INSTALLED IAW SRM 53-05, FIG URE 96, 51-10-4, 51-10-5, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 2001043000186 20010430 00186 2001 4 30 20010430AP001 4 20010325 A 2565 D31516113 SLIDE AIRBUS 320 A320214 EU PAX DOOR DISLODGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 GBXKA 714 R-1 EMERGENCY EVACUATION SLIDE PULLED FROM DOOR. REPLACED R-1 EMERGENCY EVACUATION DOOR SLIDE FOR PRECAUTIONARY PURPOSE S. (M) 2 L 7 2 4F RT A28NM 2001043000187 20010430 00187 2001 4 30 20010430AP002 4 20010324 A 2565 D31516113 SLIDE AIRBUS 320 A320231 3930325 EU PAX DOOR DEPLOYED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 GCVYE 394 FLT 962 - MSP - R1 DOOR EMERGENCY EVACUATION SLIDE WAS INADVERTENTLY DEPLOYED WHILE ACCOMPLISHING OTHER MAINTENANCE. RE MOVED AND REPLACED R1 DOOR EMERGENCY EVAUCATION SLIDE. SYSTEM OPERATES NORMAL. (M) 2 L 7 2 4F RT A28NM 2001043000188 20010430 00188 2001 4 30 20010430AP003 4 20010325 A 2565 D31516113 SLIDE AIRBUS 320 A320214 EU PAX DOOR INOPERATIVE A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 GBXKA 714 R1 EMERGENCY EVACUATION SLIDE PULLED FROM DOOR BUT DID NOT INFLATE WHILE PERFORMING SCHEDULED MAINTENANCE. REPLACED R1 EMERGENCY EVACUATION DOOR SLIDE. SYSTEM OPERATES NORMAL. (M) 2 L 7 2 4F RT A28NM 2001043000189 20010430 00189 NM 2001 4 30 20010430AP004 1 20010316 A 2612 SWITCH BOEING 727 727222 1384073 NM FIRE DETECTION DAMAGED A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 7638U 19911 FLT 19, POSITIONED ON LRD DURING ENGINE AND FIREWALL FIRE TEST THE FIRE HORN JUST CHIRPS. REMOVED AND REPLACED FIRE WAR NING BELL CUT OUT SWITCH. SYSTEM OPERATES NORMAL. (M) 2 L 7 3 4F A3WE 2001043000190 20010430 00190 NM 2001 4 30 20010430AP005 1 20010316 A 2611 SMOKE DETECTOR BOEING 727 727222 1384073 NM CARGO BAY MALFUNCTIONED A RYNA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 07 7639U 19912 FLT 34 - EN ROUTE TO ICT, DIVERTED INTO STL FOR MAIN CARGO SMOKE DETECTOR LIGHT ILLUMINATED. CARGO SMOKE LIGHT EXTINGUI SHED ON TOUCH DOWN. PILOT DECLARED AN EMERGENCY AND LANDED STL WITHOUT FURTHER INCIDENT. PERFORMED INSPECTION OF SMOKE DETECTION SYSTEM AN FOUND NO DEFECTS. SYSTEM SELF TEST GOOD. SYSTEM OPERATES NORMAL. (M) 2 L 7 3 4F A3WE 2001043000191 20010430 00191 NM 2001 4 30 GAIA01118ST 1 20010402 A 5730 SKIN BOEING 727 727223 1384074 NM LT WING DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED SEVERAL SMALL DENTS AT LEFT WING L/E UPPER SURFACE AT APPROX WS 90. ACCOMPLISHED LEFT WING FIXED L/E SKIN REPAIR WS 90 IAW B727 SRM 57-30-4 FIG 8. (M) 2 L 7 3 4F A3WE 2001043000192 20010430 00192 NM 2001 4 30 GAIA01119ST 1 20010402 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM FUSELAGE GOUGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED SEAT TRACK BS 995 LBL 24.75 TRACK GOUGED. ACCOMPLISHED SEAT TR ACK REPAIR BS 950-1035 LBL 24.75 IAW B727 SRM 53-10-5 FIG 1. (M) 2 L 7 3 4F A3WE 2001043000193 20010430 00193 NM 2001 4 30 GAIA01120ST 1 20010402 A 5311 FRAME BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 1166 FRAME LEFT IS DENTED AT WL 210. ACCOMPLISHED FUSELAGE FRAME REPAIR BS 1166 WL 215 IAW B727 SRM 51-40-3 FIG 1. (M) 2 L 7 3 4F A3WE 2001043000194 20010430 00194 NM 2001 4 30 GAIA01121ST 1 20010402 A 5311 FRAME BOEING 727 727223 1384074 NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING AT LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 360 FRAME IS DENTED BETWEEN STRINGER 4-5R. ACCOMPLISHED FU SELAGE FRAME REPAIR BS 360 BETWEEN STRINGER 4-5 R IAW B727 SRM 53-10-4 2. (M) 2 L 7 3 4F A3WE 2001043000195 20010430 00195 NM 2001 4 30 GAIA01122ST 1 20010402 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE GOUGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED DENT IN FUSELAGE IN FUSELAGE SKIN AT BS 383, 1 INCH ABOVE STRIN GER 25L. ACCOMPLISHED FUSELAGE SKIN REPAIR IAW B727 SRM 53-30-3 FIG 14. (M) 2 L 7 3 4F A3WE 2001043000196 20010430 00196 NM 2001 4 30 GAIA01080ST 1 20010402 A 5230 6022684 FRAME BOEING 727 727223 1384074 NM CARGO DOOR CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT THE C3 DOOR LOWER CHORD IS CRACKED AT AFT END. ACCOMPLISH ED C3 CARGO DOOR LOWER CHORD REMOVAL AND REPLACEMENT IAW B727 SRM 52-30-1 FIG AND 51-30-2, 51-20-4. (M) 2 L 7 3 4F A3WE 2001043000197 20010430 00197 EA 2001 4 30 MASA01025 1 20010309 A 3350 GE1317 BULB CNDAIR CL600 CL6002B19 EA EXTERIOR INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77331 7331 DURING ROUTINE MAINTENANCE, AN EXTERIOR EMERGENCY LIGHT ON LEFT SIDE OF FUSELAGE WAS INOPERATIVE. REMOVED AND REPLACED THE LIGHT BULB. OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001043000198 20010430 00198 EA 2001 4 30 MASA01026 1 20010309 A 3320 1317 BULB CNDAIR CL600 CL6002B19 EA CABIN BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17358 7358 DURING OVERNIGHT MAINTENANCE, THAT AN AFT AISLE CEILING EMERGENCY EXIT LIGHT WAS INOPERATIVE. THE BULB OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001043000199 20010430 00199 EA 2001 4 30 MASA01029 1 20010324 A 3320 1317 BULB CNDAIR CL600 CL6002B19 EA CABIN BURNED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77331 7331 FLT 5881 - BNA-PHL - MAINTENANCE DISCOVERED ONE CEILING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED BULB. OP CHE CKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001043000200 20010430 00200 EA 2001 4 30 MASA01031 1 20010325 A 2560 4530150 ELT CNDAIR CL600 CL6002B19 EA TAIL CONE FAILED A MASA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 07 77260 7260 DURING OVERNIGHT MAINTENANCE, THE ELT CAUTION MESSAGE WAS ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE ELT. OPS C HECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001043000201 20010430 00201 EU 2001 4 30 C2XA01IA212 1 20010410 A 2121 EVCTA325A FAN AEROSP ATR42 ATR42320 8680930 EU CARGO BAY SHORTED A C2XA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 42836 200 IAH- DURING FLIGHT THE CREW NOTED THE PAX VENT POWER SUPPLY CIRCUIT BREAKER POPPED; WHEN THE CIRCUIT BREAKER WAS RESET A STRONG ELECTRIC BURNING SMELL WAS PRESENT. THE CREW PULLED THE CIRCUIT BREAKER AND THE SMELL DISSIPATED. IAH- MAINTEN ANCE REMOVED AND REPLACED THE PAX VENT FAN, AND PERFORMED AN OPERATIONAL CHECK OF THE FAN WITH NO DEFECTS NOTED. THE AI RCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001043000202 20010430 00202 NM 2001 4 30 20010430AP006 1 20010328 A 3150 WARNING SYSTEM BOEING 757 757200 1384950 NM LE/TE FLAPS ACTIVATED A N8TA O OTHER N FALSE WARNING AP APPROACH 1 WP 19 513NA 26962 ON APPROACH, IN LANDING CONFIGURATION, LE SLAT DISAGREE AND TE FLAP DISAGREE EICAS MESSAGE ILLUMINATED. EXTENDED USING ALTERNATE EXTENSION. ACCOMPLISHED OPERATIONAL CHECK OF THE FLAP AND SLAT SYSTEM. NO FAULTS FOUND BITE CHECK OF FSEU. NO FAULTS FOUND. NO EICAS MESSAGES. (M) 2 L 7 2 4F RT A2NM 2001043000203 20010430 00203 EU 2001 4 30 20010430AP007 1 20010308 A 2130 354971008 SEQUENCE VALVE AIRBUS 300 A300B4203 3930306 EU COCKPIT INOPERATIVE A WRNA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 823SC MSN207 AT 500 FT WHEN PACS WERE TURNED ON, CABIN WENT INTO A DIVE APPROXIMATELY 1500 FEET PER MINUTE. CABIN ALTITUDE AT 9000 F EET WAS APPROXIMATELY 3000 FEET BELOW SEA LEVEL. DIFFERENTIAL PRESSURE 8.5 PSI. AIRCRAFT WAS PRESSURIZED WITH MANUAL D EPRESSION. FUEL DUMP WAS PERFORMED TO OBTAIN LANDING WEIGHT. AIRCRAFT LANDED NORMAL. REMOVED AND REPLACED PRESSURE RE GULATOR SEQUENCE BOX. PRESSURIZATION CHECK ON GROUND IAW MM 21-31-00. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A35EU 2001043000204 20010430 00204 EA 2001 4 30 MASA01030 1 20010324 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA CEILING BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7291Z 7291 DURING OVERNIGHT, THAT AN AFT AISLE CEILING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE BULB OP CHEC KS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001043000205 20010430 00205 NM 2001 4 30 USAA010357 1 20010405 A 5320 693535214 TIE CLIP BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 33516 22953 CLT - FOUND STRINGER TIE CLIP CRACKED .250 INCH, STATION 706, STRINGER 10L. REPLACED PART. (M) 2 L 7 2 4F RT A16WE 2001043000206 20010430 00206 NM 2001 4 30 USAA010358 1 20010405 A 5320 693535214 TIE CLIP BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 33516 22953 CLT - FOUND STRINGER TIE CLIP CRACKED, BS 663, STRINGER 10L. REPLACED PART. (M) 2 L 7 2 4F RT A16WE 2001043000207 20010430 00207 NM 2001 4 30 USAA010360 1 20010405 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 33516 22953 CLT - FOUND SKIN DENTED 1.25 INCH AND .875 INCH BY .0715 INCH DEEP, STATION 639, STRINGER 8R. INSTALLED DOUBLER PER T/R B737-300-53-30-02. (M) 2 L 7 2 4F RT A16WE 2001043000208 20010430 00208 NM 2001 4 30 USAA010361 1 20010405 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 33516 22953 CLT - FOUND STATION CRACKED .250 INCH, STATION 500C, BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER. (M) 2 L 7 2 4F RT A16WE 2001043000209 20010430 00209 NM 2001 4 30 01FDEA00269 1 20010412 A 3610 DUCT CLAMP BOEING 727 7272S2F 1384O81 NM PWA JT8 JT8D217C 52053 NE NR 1 ENGINE LOOSE A FDEA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION AP APPROACH 1 SO 25 216FE 22937 715017 ON FINAL NR 1 FIRE WARN ILLUM. ENG SHUTDOWN. FIRE BOTTLE DISCHARGED. FOUND DUCT CLAMP LOOSE WITH AIR LEAK. TIGHTENE D CLAMP PER STANDARD MAINTENANCE PRACTICES. RAN ENG, NO LEAKS NOTED. REMOVED AND REPLACED OIL FILTER PER P&W MM 72-61- 55, RAN ENG PER JET RUN HDBK. NO LEAKS NOTED. 2 L 7 3 4F 4 F A3WE E9NE 2001070200025 20010702 00025 EU 2001 7 2 01FDEA00273 1 20010327 A 5311 FRAME AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 456FE 318 CORROSION ON FRAME 80. *S/D* Removed and replaced FRAME STR 23 LT and 35 RT PER EA 6-5310-41803 & ABI 19R539-7059813 & 19R53970599. 2 L 7 2 4F RT A35EU 2001043000210 20010430 00210 EU 2001 4 30 01FDEA00270 1 20010413 A 3231 DOOR AIRBUS 310 A310203 EU NLG NOT CLOSED A FDEA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 SO 25 423FE 281 AFT T/O ECAM L/GEAR DOOR NOT CLOSED AMBER NOSE GEAR DOOR LIGHT ON. AS SPEED INCREASE LOUD NOISE AND VIBRATION FROM NOSE WHEEL AREA. 2 L 7 2 4F RT A35EU 2001043000211 20010430 00211 WP 2001 4 30 ABXA010133 1 20010323 A 2740 591096233 JACKSCREW DOUG DC9 DC932 3022066 WP HORIZ STAB CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 901AX 364 47381 THE HORIZONTAL STABILIZER JACKSCREW ASSEMBLY WAS FOUND TO HAVE PITTING CORROSION ON THE THREADED AREA. MAINTENANCE REPL ACED THE JACKSCREW ASSEMBLY IAW DC-9 MM 27-40-01. 2 L 7 2 4F A6WE 2001043000212 20010430 00212 WP 2001 4 30 ABXA010132 1 20010319 A 2740 59109625 JACKSCREW DOUG DC9 DC932 3022066 WP HORIZ STAB CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 984AX 83003 3003 47258 THE HORIZONTAL JACKSCREW ASSEMBLY WAS FOUND TO HAVE CORROSION ABOVE THE GIMBLE. MAINTENANCE INSPECTED AND REPLACED THE JACKSCREW ASSEMBLY IAW DC-9 MM 27-40-01. 2 L 7 2 4F A6WE 2001043000213 20010430 00213 WP 2001 4 30 01FDEA00277 1 20010416 A 3260 WARNING LIGHT DOUG DC10 DC1030 3023501 WP COCKPIT ILLUMINATED A FDEA O OTHER J WARNING INDICATION TO TAKEOFF 1 SO 25 318FE 46837 AFT T/O RED NOSE GEAR IND LIGHT STAY ILLUM. 2 L 7 3 4F A22WE 2001043000214 20010430 00214 SO 2001 4 30 C2XA01IA213 1 20010412 A 3260 12038594001 MODULE EMB 120 EMB120ER 3260203 SO COCKPIT FALSE INDICATION A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 15726 120174 IAH- DURING FLIGHT THE CREW NOTED THAT THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT SYSTEM-B WAS ILLUMINATED INFLIGHT AND TH E AIRCRAFT MADE A NORMAL LANDING WITHOUT INCIDENT. IAH- MAINTENANCE REMOVED AND REPLACED THE MODULE ASSEMBLY, INDICATIO N/CONTROL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001060600013 20010606 00013 NM 2001 6 6 2001UALA00521 1 20010416 A 7810 24105029 EXHAUST PIPE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7264U 21411 700316 NR 2 ENGINE EXHAUST TAILPIPE HAS A 16 INCH CRACK AT THE 6 OCLOCK POSITION NEAR THE ACOUSTIC PANEL. *S/D* THE CAUSE OF THE CRACKING IS STILL UNDER INVESTIGATION WITH THE MANUFACTURE OF THE TAILPIPE. THE TAILPIPES HAVE BEEN MODIFIED BY A S TC FOR THE STAGE 3 HUSHKIT REQUIREMENTS. THE CORRECTIVE ACTION IS THE WELDING OF THE CRACKS PER THE MM 70-78-34-05. 2 L 7 3 4F 4 F A3WE E2EA 2001043000215 20010430 00215 NM 2001 4 30 2001UALA00522 1 20010418 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 FLOORBEAM CAP STA 310.5 RBL 44 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR ON T-CAP PER AMM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001043000216 20010430 00216 NM 2001 4 30 2001UALA00524 1 20010418 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 FLOOR BEAM STA 324 BL 0 AND RBL 58 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED T-CAP REPAIR PER AMM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001043000217 20010430 00217 NM 2001 4 30 2001UALA00525 1 20010418 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 FUSELAGE SKIN DENTED LEFT SIDE AT FLOOR LINE BETWEEN STA 460 TO STA 492 STR 17L. MAJOR REPAIR ACCOMPLISHED.INSTALLED DO UBLER PER SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001043000218 20010430 00218 NM 2001 4 30 2001UALA00526 1 20010416 A 5320 STRINGER CLIP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 FORWARD PIT STATION 478, STRINGER CLIP HAS OBLONG HOLES. MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP PER BOEING DRAWING 14 0T2101. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000219 20010430 00219 NM 2001 4 30 2001UALA00527 1 20010417 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 929UA 26652 DEEP GOUGE THROUGH THE FIRST LAYER OF SKIN JUST ABOVE THE FORWARD CARGO DOOR OPENING. BLENDED OUT THE DAMAGED AREA AND INSTALLED A DOUBLER. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001043000220 20010430 00220 NM 2001 4 30 2001UALA00528 1 20010417 A 5320 STRAP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 FAIL SAFE STRAP BS 1270 TO 1370 RBL 90.5 CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORD ANCE WITH BAC DRAWING 146T8511 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000221 20010430 00221 NM 2001 4 30 2001UALA00529 1 20010417 A 5310 DOOR FRAME BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CARGO BAY CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 BULK PIT DOOR SILL UPPER CHORD CORRODED ON INBOARD LEG STATION 1417 TO 1424 ABOVE STRINGERS 32L TO 33L. MAJOR REPAIR AC COMPLISHEDFABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 146T8511 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000222 20010430 00222 NM 2001 4 30 2001UALA00530 1 20010417 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 FLOORBEAM CORRODED UNDER MID GALLEY STATION 824 RBL 8. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN AC CORDANCE WITH SRM 53-00-51. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000223 20010430 00223 NM 2001 4 30 2001UALA00531 1 20010417 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 STATION 355 STRINGERS 35L TO 34L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCO RDANCE WITH BAC DRAWING 141T1221 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000225 20010430 00225 NM 2001 4 30 2001UALA00533 1 20010417 A 5320 STRINGER CLIP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 STATION 355 STRINGER 37L STRINGER CLIP IS CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCOR DANCE WITH SRM 51-40-02 AND GN/MM 1-0-0-23. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000226 20010430 00226 NM 2001 4 30 2001UALA00534 1 20010417 A 5320 STRINGER CLIP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 STATION 355 STRINGER 38L STRINGER CLIP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDAN CE WITH SRM 51-40-02 AND GN/MM 1-0-0-23. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000227 20010430 00227 NM 2001 4 30 2001UALA00535 1 20010417 A 5311 FRAME BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 BS 390 FRAME T-CAP HAS DOUBLE DRILLED HOLE AT LBL 29. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACC ORDANCE WITH 53-00-07 FIGURE 204. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000228 20010430 00228 NM 2001 4 30 2001UALA00537 1 20010417 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 BS 1065 TO 1087 STRINGER CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 51- 40-02 AND 53-00-03. 2 L 7 2 4F 4 F RT A1NM E3NE 2001043000229 20010430 00229 NM 2001 4 30 2001UALA00538 1 20010417 A 5313 STRINGER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 STRINGER 32R AT BS 1200 HAS A FIGURE EIGHT SHAPED FASTENER HOLE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHEDREPAI RED PER SRM 51-20-07 AND SRM 53-00-01. 2 L 7 2 4F 4 F RT A1NM E24NE 2001043000230 20010430 00230 NM 2001 4 30 2001UALA00539 1 20010414 A 7110 PANEL BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT NACELLE SEPARATED A UALA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 WP 29 645UA 25280 AFTER ROTATION CREW REPORTED HAD LEFT ENG PANEL LOOSE AND FLOATING AROUND LEADING EDGE , AIRCRAFT LANDED AT JFK AMBER AL ERT FOUND DAMAGE TO CORE COWL AND LEADING EDGE. 2 L 7 2 4F 4 F RT A1NM E24NE 2001050300325 20010503 00325 NM 2001 5 3 2001UALA00541 1 20010419 A 5311 FRAME BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 1307 LBL 16.5 T-CAP HAS HOLE DRILLED IN RADIUS. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND I NSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 146T1211 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001060600014 20010606 00014 NM 2001 6 6 2001UALA00543 1 20010418 A 7810 24105029 EXHAUST PIPE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7281U 21559 NR 1 ENGINE TAILPIPE CRACKED JUST AFT OF FORWARD FLANGE AT 9 O''CLOCK POSITION. *S/D* THE CAUSE OF THE CRACKING IS STI LL UNDER INVESTIGATION WITH THE MANUFACTURE OF THE TAILPIPE. THE CORRECTIVE ACTION WAS THE REPLACEMENT OF THE TAILPIPE. 2 L 7 3 4F 4 F A3WE E2EA 2001060100160 20010601 00160 NM 2001 6 1 2001UALA00544 1 20010418 A 2120 BACC10KH550R CLAMP BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE A/C BAY BROKEN A UALA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION NR NOT REPORTED 1 WP 29 798UA 26928 EICAS BLEED LOSS WING RIGHT INDICATION, FOLLOWED BY RIGHT ISOLATION VALVE CLOSURE, THEN FINALLY THE LOSS OF THE RIGHT AI R CONDITIONING PACK LEAD TO FLIGHT DIVERTING TO MIA. *S/D* FOUND FWD BAND CLAMP FAILED AT LWR RT FLOW CONTROL VLV. TH IS CAUSED AIR LEAK, WHICH CAUSED THE RT PACK AND RT BLEED TO SHUTDOWN. REPLACED CLAMP, THEN A/C RETURNED TO REVENUE SER VICE WITHOUT FURTHER INCIDENT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001043000231 20010430 00231 NM 2001 4 30 2001UALA00545 1 20010420 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO BAY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 FORWARD CARGO DOOR LOWER AFT CORNER FRAME CRACKED. REPLACED CRACKED FRAME. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100025 20010521 00025 NM 2001 5 21 2001UALA00547 1 20010419 A 2920 651784914 HYDRAULIC LINE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE HYDRAULIC SYS LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 7284U 21562 CREW REPORTED THAT B HYDRAULIC SYSTEM QUANTITY READ ZERO. NO LOW PRESSURE LIGHTS ILLUMINATED. SUPPLEMENTAL DATA UPDATE REPLACED B SYSTEM HYDRAULIC TUBE ON FILTER MODULE. SERVICED HYDRAULIC SYSTEM. CHECKS OK. 2 L 7 3 4F 4 F A3WE E2EA 2001043000232 20010430 00232 NM 2001 4 30 2001UALA00548 1 20010420 A 5320 140T2112 STOP BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CARGO BAY DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 671UA 30026 REAR CARGO CONTAINER DOOR STOP FITTING BROKEN LOOSE FROM DOOR FRAME STRUCTURE. MAJOR REPAIR ACCOMPLISHED. REMOVED AND R EPLACED STOP FITTING 140T2112 WITH SERVICEABLE PART, RIGGED S160 PROX SWITCH PER MM52-35-43, CHECKED DOOR STOP RIG PER M M52-35-00. REPLACED ALL SHEARED FASTENERS AS REQUIRED REF IPC 52-34-53. 2 L 7 2 4F 4 F RT A1NM E24NE 2001043000233 20010430 00233 NM 2001 4 30 2001UALA00549 1 20010420 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 FLOORBEAM CORRODED STA 1669-1673 RLB 40. MAJOR REPAIR ACCOMPLISHED.INSTALLED NEW FLOOR BEAM PER SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001043000234 20010430 00234 NM 2001 4 30 2001UALA00550 1 20010420 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 CREASE BEAM DAMAGED INBOARD ANGLE RIGHT SIDE STA 1130-1133. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPAIRED DAMAGE SECTION OF CREASE BEAM USING SRM 51-70-12 TYPICAL EXTRUDED SECTION REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2001043000235 20010430 00235 NM 2001 4 30 2001UALA00554 1 20010423 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 FRAME DAMAGED AT STA 365 ADJACENT TO STR 17R. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.INSTALLED FRAME DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2001043000236 20010430 00236 SO 2001 4 30 SIMA20011032 1 20010413 A 2731 3094343 SWITCH EMB 145 EMB145 SO CAPTAIN YOKE REVERSED A SIMA A UNSCHED LANDING W F INADEQUATE Q C FLT CONT AFFECTED CL CLIMB 1 SW 21 642AE 2 DURING CLIMB-OUT, CAPTAIN NOTED HIS PITCH TRIM SWITCH DOING THE OPPOSITE OF WHAT WAS COMMANDED. FIRST OFFICER AND STA ND BY SWITCHES OPERATED NORMAL. AIRCRAFT WAS RETURNED TO CRP SAFELY WITH NO FURTHER INCIDENTS REPORTED. C/A- MAINTEN ANCE REMOVED AND REPLACED THE PILOTS TRIM SWITCH IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SE RVICE. 2 L 7 2 4F RT T00011AT 2001043000237 20010430 00237 NE 2001 4 30 C8GA20010007 2 20010412 A 7412 103538754 EXCITER BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE INOPERATIVE A C8GA O OTHER X ENGINE FLAMEOUT DE DESCENT 1 SO 15 808EA 3447 22439 656881 FLT 722 FROM TOL TO CLT. UPON INITIAL DESCENT TO CLT, NR 2 ENGINE FLAMED OUT. TWO ATTEMPTS TO AIR RESTART FAILED. AIR CRAFT CONTINUED TO CLT AND LANDED WITHOUT INCIDENT. PERFORMED ENGINE INSPECTION OF FILTERS AND SENSE LINES. NO DEFECTS NOTED. FOUND NR 2 EXCITER BOX INOPERATIVE. REPLACED EXCITER BOX. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2001043000238 20010430 00238 WP 2001 4 30 ABXA010136 1 20010122 A 2740 591096231 BEARING DOUG DC9 DC931 3022065 WP HORIZ STAB WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 66098 47269 THE HORIZONTAL STABILIZER JACKSCREW BEARING FREE PLAY EXCEEDED LIMITATIONS. MAINTENANCE INSPECTED AND REPLACED THE JACK SCREW ASSEMBLY IAW DC-9 MM 27-40-01. 2 L 7 2 4F A6WE 2001043000239 20010430 00239 WP 2001 4 30 ABXA010135 1 20010312 A 2740 591096235 JACKSCREW DOUG DC9 DC941 302207N WP HORIZ STAB WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 51473 47511 THE HORIZONTAL STABILIZER JACKSCREW END PLAY AND FREE PLAY EXCEEDED LIMITATIONS. MAINTENANCE REPLACED THE JACKSCREW ASS EMBLY IAW DC-9 MM 27-40-01. 2 L 7 2 4F A6WE 2001043000240 20010430 00240 WP 2001 4 30 ABXA010134 1 20010118 A 2740 59109625 JACKSCREW DOUG DC9 DC941 302207N WP HORIZ STAB CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 54436 1900 47608 THE HORIZONTAL STABILIZER JACKSCREW THREADS WERE FOUND TO HAVE PITTING CORROSION. MAINTENANCE REPLACED THE JACKSCREW AS SY IAW DC-9 MM 27-40-01. 2 L 7 2 4F A6WE 2001043000241 20010430 00241 WP 2001 4 30 IXXA0100013 1 20010413 A 3230 UPLOCK DOUG DC8 DC871F 302199D WP MLG DIRTY A IXXA O OTHER N FALSE WARNING CL CLIMB 1 SW 11 823BX 82177 1878 46064 EN ROUTE FROM BRO TO TOL, THE LANDING GEAR UNSAFE WARNING LIGHT ILLUMINATED. THE FLIGHT CREW CYCLED THE LANDING GEAR BU T THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECT ED THE LANDING GEAR, CLEANED AND LUBRICATED THE GEAR UPLATCH MECHANISMS AND PERFORMED A SUCCESSFUL OPERATIONAL CHECK IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2001043000242 20010430 00242 EA 2001 4 30 JBXA000265 1 20010413 A 2760 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT FALSE ACTIVATION A JBXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 05 590ML 7385 INBOARD AND OUTBOARD GROUND SPOILERS FAULT STATUS MESSAGE. SPOILERON MESSAGE FIRST, THEN CLEARED FOLLOWED BY STALL FAIL CAUTION MESSAGE. PERFORMED OPERATIONAL TEST OF SPOILERS AND SPOILER ELECTRONIC CONTROL UNIT SYSTEMS, NO PROBLEMS FOUND AT THIS TIME. OPS CHECK GOOD IAW CRJ AMM 27-61-05. 2 L 7 2 4F RT A21EA 2001043000243 20010430 00243 WP 2001 4 30 AALA20010658 1 20010403 A 3350 8039001 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 253AA 49286 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 7 THROUGH 11 DIM. RE-SEATED EMERGENCY EXIT LIGHT BATTER Y PACK AT ROW 7. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001043000244 20010430 00244 WP 2001 4 30 AALA20010659 1 20010401 A 3350 P2010031302 LIGHT DOUG DC9 DC982 3022082 WP FWD LAVATORY DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 576AA 53153 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AISLE MARKER AT FORWARD LAVATORY INOPERATIVE. REPLACED EMERGEN CY EXIT LIGHT ASSEMBLY. (M) 2 L 7 2 4F A6WE 2001043000245 20010430 00245 WP 2001 4 30 AALA20010660 1 20010401 A 3350 P4010051111 MODULE DOUG DC9 DC982 3022082 WP AFT SLIDE DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 407AA 49318 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT SLIDE INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT MODULE . SYSTEM GRUOND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001043000246 20010430 00246 WP 2001 4 30 AALA20010657 1 20010401 A 3350 4000792 LIGHT DOUG DC9 DC982 3022082 WP FWD LAVATORY INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 576AA 53153 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT MARKER AT FORWARD LAVATORY INOPERATIVE. REPLACED EMERGENCY EXI T LIGHT ASSEMBLY AT FORWARD LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001043000247 20010430 00247 WP 2001 4 30 AALA20010666 1 20010401 A 3350 LAMP DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 510AM 49804 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 4E DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 4E. SYST EM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001043000249 20010430 00249 NM 2001 4 30 AALA20010656 1 20010326 A 2120 AAP2711 DUCT BOEING 757 757223 1384957 NM CABIN LEAKING A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 648AA 24606 BGI - FLT 984 - EN ROUTE BGI-MIA - DETECTED LOUD NOISE IN CABIN. RETURNED BGI AND LANDED WITHOUT FURTHER INCIDENT. REP LACED AIR CONDITIONING DUCT. ACCOMPLISHED LEAK CHECK. LEAK CHECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001043000250 20010430 00250 2001 4 30 AALA20010560 4 20010316 A 2397 4103646 CABLE BOEING 777 777223 1385213 NM CABIN SHORTED A H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 785AN 30005 LHR - FLT 56 - EN ROUTE MIA-LHR, DETECTED SMOKE AT SEAT 27A VIDEO MONITOR. TURNED OFF VIDEO MONITOR AT SEAT 27A. LANDE D LHR WITHOUT FURTHER INCIDENT. REPLACED SEAT CABLE AT SEAT 27A. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001043000251 20010430 00251 NM 2001 4 30 AALA20010633 1 20010221 A 3610 1836M64G03 DUCT DOUG MD11 MD11 3023602 NM NR 3 ENGINE RUPTURED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 1756 48491 DFW - FLT 946 - SHORTLY AFTER TAKEOFF, NR 3 AIR SYSTEM DIFFERENTIAL MESSAGE ILLUMINATED. NR 3 BLEED AIR PRESSURE OFF LI GHT ALSO ILLUMINATED. LANDED DFW WITHOUT FURTHER INCIDENT. REPLACED NR 3 INBOARD DUCT. LEAK CHECKS GOOD. SYSTEM GROU ND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 2001043000252 20010430 00252 NM 2001 4 30 AALA20010614 1 20010321 A 2612 FIRE DETECTOR DOUG MD11 MD11 3023602 NM APU BAY MALFUNCTIONED A AALA F D ACTIVATE FIRE EXT. RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 21 1761R 48551 DFW - FLT 963 - EN ROUTE DFW-GRU - AT GATE DURING ENGINE START APU COMPRESSOR STALLED SEVERAL TIMES ACCOMPANIED BY APU F IRE WARNING INDICATION. ACCOMPLISHED EMERGENCY PROCEDUES PER CHECKLIST. APU LIGHT EXTINGUISHED AFTER PROCEDURES ACCOMP LISHED. REPLACED APU FIRE BOTTLE AND SQUIB. ACCOMPLISHED TROUBLESHOOTING PROCEDURES. NO EVIDENCE OF FIRE FOUND. RAN APU. NO FAULTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 2001043000253 20010430 00253 NM 2001 4 30 AALA20010634 1 20010214 A 3610 1836M64G03 DUCT DOUG MD11 MD11 3023602 NM NR 3 ENGINE RUPTURED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 1767A 48598 DFW - FLT 946 - SHORTLY AFTER TAKEOFF, NR 3 MANIFOLD FAIL LIGHT ILLUMINATED. LANDED DFW WITHOUT FURTHER INCIDENT. REPL ACED NR 3 INBOARD DUCT PYLON. LEAK CHECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 2001043000254 20010430 00254 WP 2001 4 30 AALA20010534 1 20010314 A 5312 BULKHEAD DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 126AA 46947 TUL - FOUND FORWARD SIDE OF BULKHEAD AND STIFFENER HAS CORROSION 10 INCHES UP FROM FLOOR. INSTALLED REPAIR DOUBLERS PER ESO 7349 DATED 03-09-2001. (M) 2 L 7 3 4F A22WE 2001043000255 20010430 00255 WP 2001 4 30 AALA20010376 1 20010302 A 5330 SKIN DOUG DC10 DC1010 3022110 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 126AA 46947 TUL - FOUND SKIN AT FORWARD CARGO ABOUT 48R TO 43R, FS 1059 TO 1150 OUT OF LIMITS. INSTALLED CLASS I REPAIR DOUBLER PER SRM 53-30-00 VOL I. (M) 2 L 7 3 4F A22WE 2001043000256 20010430 00256 NM 2001 4 30 KPVA20018 1 20010330 A 3350 6104781 POWER SUPPLY DHAV DHC8 DHC8103 1386005 NM CABIN INOPERATIVE A KPVA K NONE L NO TEST IN INSP/MAINT 1 WP 13 803WP 141 HNL - FOUND ON DAILY INSPECTION, EMERGENCY LIGHTS AT REAR OVERHEAD CEILING LIGHT AND LEFT AFT EGRESS LIGHT, WILL NOT COM ON DURING TEST. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AT 3351 PS3 IAW DHC-8 MM 33-51-00 PAGE 201 PAR 1. O PS CHECK GOOD IAW DHC-8 MM 33-51-01 PAGES 201-202 PAR 2A. NO DEFECTS. (M) 2 H 7 2 4T RT A13NM 2001043000257 20010430 00257 NM 2001 4 30 GAIA01114ST 1 20010402 A 5753 652163480 SKIN BOEING 727 727214 138407R NM RT WING TE FLAP DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 751US 21513 DURING MAINTENANCE, IT WAS DISCOVERED THAT THE RIGHT INBOARD AFT FLAP HAS A SMALL HOLE IN THE UPPER SKIN. REMOVED DAMAG ED AREA AND REPAIRED IAW THE B727 SRM CHAPTER 57-50-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001043000258 20010430 00258 NM 2001 4 30 EIA2001125 1 20010323 A 5412 BULKHEAD BOEING 747 747273C 1384896 NM ENGINE BAY CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 HKG-HAECO - FOUND 4 CRACKS AT NR 2 ENGINE STRUT REAR ENGINE MOUNT BULKHEAD WEB, FROM FRAME WEB ADJACENT TO REPAIR ANGLE, 1 AT FORWARD SIDE AND 3 AT AFT SIDE. REPAIRED BULKHEAD WEB PER RS R-54-53-34641. CONTINUE DETAIL VISUAL AND HFEC INSP ECTION OF B/H IAW SB 747-54A2202. (M) 2 L 7 4 4F A20WE 2001043000259 20010430 00259 NM 2001 4 30 EIA2001126 1 20010323 A 5412 BULKHEAD BOEING 747 747273C 1384896 NM NR 3 NACELLE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 HKG-HAECO - NR 3 STRUT REAR ENGINE MOUNT BULKHEAD AFT SIDE OF FRAME WEB CRACKED AT OUTBOARD LOWER AREA ADJACENT TO REPAI R ANGLE, APPROX .375 INCH LENGTH. STOP DRILLED HOE PER SRM 51-10-01. INSPECT STOP DRILLED HOLE BY HFEC EVERY 600 FLT C YCLES PER SB 747-54A2202. (M) 2 L 7 4 4F A20WE 2001043000260 20010430 00260 NM 2001 4 30 EIA2001127 1 20010323 A 5412 BULKHEAD BOEING 747 747273C 1384896 NM NR 4 NACELLE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 HKG-HAECO - NR 4 STRUT REAR ENGINE MOUNT BULKHEAD FORWARD SIDE OF FRAME WEB CRACKED AT OUTBOARD LOWER AREA, ADJACENT TO REPAIR ANGLE, APPROX .375 INCH LENGTH. REPAIRED BULKHEAD WEB PER RS R-54-53-34641. CONTINUE DETAIL VISUAL AND HFEC INS PECTION PER SB 747-54A2202. (M) 2 L 7 4 4F A20WE 2001043000261 20010430 00261 NM 2001 4 30 EIA2001128 1 20010323 A 5711 SPAR BOEING 747 747273C 1384896 NM RT WING CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 HKG-HAECO - FOUND RT WING REAR SPAR WEB, WBL 445 WEB OUTBOARD VERTICAL CHANNEL CRACKED. REPLACED VERTICAL STIFFENER PER SRM 51-10-01. (M) 2 L 7 4 4F A20WE 2001043000262 20010430 00262 NM 2001 4 30 EIA2001129 1 20010323 A 5410 ANGLE BOEING 747 747273C 1384896 NM NR 3 NACELLE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 FOUND NR 3 PYLON REAR ENGINE MOUNT BULKHEAD LEFT TOP LONGERON, REPAIR ANGLE ON FRAME TOP END CRACKED. NDT INSPECTED ARE A, DEFECTIVE BRACKET REPLACED PER SRM 51-10-01. (M) 2 L 7 4 4F A20WE 2001043000263 20010430 00263 NM 2001 4 30 EIA2001130 1 20010323 A 5310 SHEAR TIE BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 HKG-HAECO - FOUND THREE VERTICAL BEAM ATTACH SHEAR TIE CLIPS CRACKED, FUSELAGE RIGHT NOSE GEAR TUNNEL SIDEWALL. REPLACE D DEFECTIVE SHEAR TIE CLIPS PER SRM 51-10-01. (M) 2 L 7 4 4F A20WE 2001043000264 20010430 00264 NM 2001 4 30 EIA2001131 1 20010327 A 5412 BULKHEAD BOEING 747 747121 1384871 NM NR 2 PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 HKG-HAECO - NR 2 PYLON REAR ENGINE MOUNT BULKHEAD WEB CRACKED AT FORWARD AND AFT SIDE. STOP DRILLED CRACKS, NDT INSPECT ED, INSTALLED NEW ANGLE CHORD AND OVERSIZED HI-LOCKS PER BOEING MSG 2 L 7 4 4F A20WE 2001043000265 20010430 00265 NM 2001 4 30 EIA2001121 1 20010321 A 5315 FLOORBEAM BOEING 747 747128 1384894 NM FUSELAGE MISDRILLED A EIAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - FOUND FS 474 RIGHT OUTBOARD FLOORBEAM NUTPLATE HOLE DOUBLE DRILLED AT RBL 90. REPAIRED BEAM PER B747 SRM 51-2 0-01 AND ECRA 3203-53-33-2. (M) 2 L 7 4 4F A20WE 2001043000266 20010430 00266 NM 2001 4 30 EIA2001120 1 20010321 A 5530 STRUCTURE BOEING 747 747128 1384894 NM VERTICAL STAB CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - FOUND VERTICAL STAB INTERIOR CORROSION ON FORWARD FLANGE OF T-CHORD AT FIN STATION 570 RIGHT. FABRICATED AND INSTALLED CHORD PER B747 SRM 51-30-02 AND 51-10-02. (M) 2 L 7 4 4F A20WE 2001043000267 20010430 00267 NM 2001 4 30 EIA2001119 1 20010321 A 5410 STRUCTURE BOEING 747 747128 1384894 NM NR 4 PYLON CHAFED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - FOUND NR 4 PYLON LOWER EDGE CHAFED BELOW REPAIR DOUBLER AT RIGHT OUTBOARD SIDE, AFT OF AFT ENGINE MOUNT. REPA IRED NR 4 PYLON PER ECRA 3203-54-024-2. (M) 2 L 7 4 4F A20WE 2001043000268 20010430 00268 NM 2001 4 30 EIA2001118 1 20010321 A 5520 STRUCTURE BOEING 747 747128 1384894 NM RT ELEVATOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - FOUND RIGHT INBOARD ELEVATOR, UPPER SURFACE LE CRACK AT RIVET HEAD, 24 INCHES OUTBOARD OF INBOARD EDGE. REPAI RED RIGHT INBOARD ELEVATOR PER ECRA 3203-55-035-2. (M) 2 L 7 4 4F A20WE 2001043000269 20010430 00269 NM 2001 4 30 EIA2001117 1 20010321 A 5314 PANEL BOEING 747 747128 1384894 NM KEELBEAM CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - FOUND SURFACE CORROSION EXT SURFACE 191JJ KEEL BEAM PNL AND CRACK AT ONE SCREW HOLE. FABRICATED AND INSTALLED NEW PANEL PER B747 SRM 51-20-01 FIG 7. (M) 2 L 7 4 4F A20WE 2001043000270 20010430 00270 NM 2001 4 30 EIA2001124 1 20010321 A 5340 FITTING BOEING 747 747128 1384894 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - FOUND FS 660 RBL 117 WL 199 FLOORBEAM FITTING HAS .250 DIAMETER HOLE BROKEN OUT OF EDGE OF UPT T-CAP AFT FLANG E. REPAIRED FITTING PER ECRA 3203-53-20-2. (M) 2 L 7 4 4F A20WE 2001043000271 20010430 00271 NM 2001 4 30 USAA010362 1 20010405 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 33516 22953 CLT - FOUND FRAME CRACKED .250 INCH, STATION 727C, BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001043000272 20010430 00272 NM 2001 4 30 USAA010363 1 20010405 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 33516 22953 CLT - FOUND FRAME CRACKED .250 INCH, STATION 480, STRINGER 8L AND 9L. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001043000273 20010430 00273 NM 2001 4 30 USAA010365 1 20010405 A 5510 1137587 BEAM BOEING 737 7373B7 1384580 NM HORIZONTAL STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 33516 22953 CLT - FOUND THRUSTBEAM CRACKED 4 INCHES, HORIZONTAL STAB CENTER SECTION, RIGHT THRUST BEAMS. REPLACED THRUST BEAM SRM 5 1-10-02 AND 51-40-02. (M) 2 L 7 2 4F RT A16WE 2001043000274 20010430 00274 NM 2001 4 30 USAA010366 1 20010405 A 5320 693535214 TIE CLIP BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 33516 22953 CLT - FOUND TIE CLIP CRACKED .250 INCH, STATION 807, STRINGER 10L. REPLACED PART PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2001043000275 20010430 00275 NM 2001 4 30 USAA010368 1 20010405 A 5320 695335214 TIE CLIP BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 33516 22953 CLT - FOUND TIE CLIP CRACKED .250 INCH, STATION 827, STRINGER 10L. REPLACED PART PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2001043000276 20010430 00276 NM 2001 4 30 USAA010370 1 20010405 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 33516 22953 CLT - FOUND FRAME CRACKED .500 INCH, STATION 400, BETWEEN STRINGER 8L-9L. DOUBLER INSTALLED PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001043000277 20010430 00277 NM 2001 4 30 CALA0100367 1 20010415 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND FLOORBEAM CORRODED ON UPPER SURFACE AROUND SCREW HOLES AT STA 967, RBL 27, LBL 6, AND LBL 27. REPAIR S TRAPS AND SHIMS WERE INSTALLED IAW SRM 53-00-51, FIGURE 203, 51-20-01, AND 51-30-01. 2 L 7 2 4F RT A16WE 2001043000278 20010430 00278 WP 2001 4 30 CALA0100372 1 20010412 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DELAMINATED A CALA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND CENTER FLOOR PANEL AT STA 946 - 1003 DELAMINATED AND LT FLOOR PANEL DELAMINATED AT STA 927 - 1003. THE FLOOR PANELS WERE REMOVED AND REPLACED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001043000279 20010430 00279 EA 2001 4 30 SWIA972504 1 20010411 A 3030 ANTI-ICE SYSTEM CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE PITOT SYS MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 418SW 7446 AFTER TAKEOFF RIGHT STATIC HEAT, RIGHT PITOT HEAT, TAT PROBE HEAT AND RIGHT AOA HEAT WARNINGS ILLUMINATED. RETURNED TO SLC. RESET HEAT SYSTEM FOR RIGHT PITOT STATIC, TAT PROBES, AND AOA SYSTEM. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2001043000280 20010430 00280 NM 2001 4 30 CALA0100381 1 20010416 A 5755 6545321606 FITTING BOEING 737 7373T0 1384582 NM RT SPOILER GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND RT WING AFT SPAR SPOILER FITTING GOUGED AT WS 133. THE SPOILER FITTING WAS REPLACED IAW ECRA 5750-0351 7 AND AMS EA 04-5750-0842. 2 L 7 2 4F RT A16WE 2001043000281 20010430 00281 NM 2001 4 30 01FDEA00258 1 20010406 A 5730 SKIN BOEING 727 72725C 138400H NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 124FE 19360 DURING ROUTINE INSP, RT WING UPPER SKIN LEAD EDGE FOUND CRACKED AT WS 46, 8 INCHES FWD OF THE FWD WING SPAR.** S/D ** FAB & REPAIR PER IAW BAC 727 SRM 57-30-4 & SRM 51-30-2. 2 L 7 3 4F A3WE 2001043000282 20010430 00282 NE 2001 4 30 HNAA0100025 2 20010413 A 7200 PW120 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE NR 2 ENGINE DEFECTIVE A HNAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 07 927HA 30825 979 117 120432 SMOKE IN CABIN AND FLIGHT COMPARTMENT, SMELLED LIKE HOT DUCT. DECLARED EMERGENCY AND DIVERTED TO BUFFALO. AIRCRAFT FER RIED TO SBY. FOUND OIL IN HEAT EXCHANGER AND AIR CYCLE MACHINE DUCTING. REMOVED AND REPLACED ACM AND HEAT EXCHANGER. ON 15 APRIL PROBLEM RECURRED. ON GROUND RUN WHEN NR 2 ENGINE BLEEDS FLOW AT MAX AND MANUALLY SELECTING TEMP TO WARM, AI RCRAFT FILLED UP WITH OIL MIST. NR 2 ENGIND REMOVED AND REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 2001043000283 20010430 00283 WP 2001 4 30 CALA0100354 1 20010413 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND R-1 DOOR RT CUSP ANGLE CORRODED AT FS 216. THE CORRODED SECTION OF CUSP ANGLE WAS REMOVED AND A NEW CU SP ANGLE AND SPLICES WERE INSTALLED IAW SRM 53-05, FIGURE 55. 2 L 7 2 4F A6WE 2001043000284 20010430 00284 NM 2001 4 30 CALA0100356 1 20010413 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 967-986.5, LBL 18 AND RBL 18. THE FLOOR SUPPORT WAS REMOVED AND REPLACE D IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001043000285 20010430 00285 NM 2001 4 30 CALA0100357 1 20010413 A 5320 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT INTERCOSTAL ANGLE AT STA 927-947, BL 0. REMOVED CRACKED ANGLE ON INTER COSTAL AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F RT A16WE 2001043000286 20010430 00286 NM 2001 4 30 CALA0100358 1 20010413 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE BENT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND INTERCOSTAL IN FORWARD CARGO COMPARTMENT BENT ON UPPER SURFACE AT STA 440-460, S28R. THE INTERCOSTAL W AS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001043000287 20010430 00287 NM 2001 4 30 CALA0100360 1 20010413 A 5320 ATTACH ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND FORWARD CARGO COMPARTMENT AFT PRESSURE BULKHEAD RT PANEL LOWER ATTACH ANGLE CORRODED AT STA 500D, S26R. THE ATTACH ANGLE WAS REMOVED AND TWO REPAIR ANGLES WERE INSTALLED IAW SRM 51-70-12 AND 51-40-02. 2 L 7 2 4F RT A16WE 2001043000288 20010430 00288 NM 2001 4 30 CALA0100361 1 20010413 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED AT STA 907-947. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52 , FIGURE 204. 2 L 7 2 4F RT A16WE 2001043000289 20010430 00289 NM 2001 4 30 CALA0100362 1 20010414 A 5511 SPAR BOEING 757 757224 1384958 NM HORIZ STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 58101 27291 INSPECTION FOUND A 1.5 INCH CRACK IN LT HORIZONTAL STABILIZER LEADING EDGE LOWER CHORD/AUX SPAR AT FSS 155.849. THE ARE A WAS REPAIRED IAW ECRA 5512-01003. 2 L 7 2 4F RT A2NM 2001043000290 20010430 00290 WP 2001 4 30 CALA0100364 1 20010414 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND FLOORBEAM CORRODED AT AND UNDER NUT PLATES AT STA 1309, BL 0 TO LBL 54. 2 L 7 2 4F A6WE 2001043000291 20010430 00291 WP 2001 4 30 CALA0100365 1 20010415 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND CABIN LEFT O/B SEAT TRACK CORRODED AT FS 1136. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INS TALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-1. 2 L 7 2 4F A6WE 2001043000292 20010430 00292 NM 2001 4 30 CALA0100366 1 20010415 A 5523 HINGE BOEING 737 737724 NM ELEVATOR TAB WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33714 28785 INSPECTION FOUND LEFT ELEVATOR TAB I/B NR 1 HINGE POINT WORN. THE ELEVATOR TAB WAS REMOVED AND REPLACED IAW MM 27-31-00 . 2 L 7 2 4F RT A16WE 2001043000293 20010430 00293 NM 2001 4 30 CALA0100368 1 20010416 A 5315 FLOORBEAM BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14628 27532 INSPECTION FOUND FLOORBEAM CORRODED AROUND NUT PLATE HOLES AT STA 986, RBL 4. THE CORROSION WAS CLEANED AND A STRAP REP AIR WAS INSTALLED IAW SRM 53-00-51, FIGURE 203. 2 L 7 2 4F RT A16WE 2001043000294 20010430 00294 WP 2001 4 30 CALA0100369 1 20010416 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND SHEAR TIE ON AFT SIDE OF FRAME IN AFT PIT CORRODED AT STA 1155 BETWEEN LONGERON 30 AND 29R. A T-ANGLE WAS INSTALLED IAW 51-10-4, 51-10-3, AND 51-30-5. 2 L 7 2 4F A6WE 2001043000295 20010430 00295 WP 2001 4 30 CALA0100370 1 20010412 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND CABIN FLOOR PANEL BBB DELAMINATED. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001043000296 20010430 00296 WP 2001 4 30 CALA0100371 1 20010412 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND CENTER FLOOR PANEL DELAMINATED AT FS 1309 - 1322. A NEW PANEL WAS INSTALLED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001043000297 20010430 00297 WP 2001 4 30 CALA0100373 1 20010412 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND FLOOR PANELS DELAMINATED AT CENTER SECTION FS 1079 - 1174, RT SECTION AT FS 1117 - 1174, AND CENTER SEC TION AT FS 1117 - 1174. THE FLOOR PANELS WERE REPLACED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001043000298 20010430 00298 WP 2001 4 30 CALA0100374 1 20010412 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND RT FLOOR PANEL AT STA 866 - 886 DELAMINATED AND FLOOR PANEL AT STA 886 - 946 DELAMINATED. THE FLOOR PA NELS WERE REPLACED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001043000299 20010430 00299 WP 2001 4 30 CALA0100375 1 20010412 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND MAIN CABIN FORWARD ENTRY FLOOR PANELS A, C, D, E, F, G, H, I, AND J DELAMINATED. THE FLOOR PANELS WERE REPLACED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001043000300 20010430 00300 WP 2001 4 30 CALA0100376 1 20010412 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND FORWARD ENTRY FLOOR PANELS M, N, O, AND P DELAMINATED. THE FLOOR PANELS WERE REPLACED IAW ECRA 5320-01 265. 2 L 7 2 4F A6WE 2001043000301 20010430 00301 WP 2001 4 30 CALA0100377 1 20010412 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND LT CABIN FLOOR PANEL DELAMINATED AT FS 769 - 826. THE PANEL WAS REPLACED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001043000302 20010430 00302 NM 2001 4 30 HNAA0100026 1 20010413 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST UK UNKNOWN 1 EA 07 925HA 111 EMERGENCY LIGHTS OUT NR 3 & 4, FRONT RED LIGHTS. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY BASE. 2 H 7 2 4T RT A13NM 2001043000303 20010430 00303 EA 2001 4 30 COMA0160360 1 20010415 A 5320 ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 926CA 7027 ANGLES AT FS 484 BL 27 (LT & RT) FOUND CRACKED. FABRICATED REPLACEMENT ANGLES AND INSTALLED IAW WVAC EO 601R-53-2385. 2 L 7 2 4F RT A21EA 2001043000304 20010430 00304 NM 2001 4 30 USAA010371 1 20010405 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 33516 22953 CLT - FOUND FRAME CRACKED .75 INCH, STATION 727E, BETWEEN STRINGER 8L-9L. DOUBLER INSTALLED. (M) 2 L 7 2 4F RT A16WE 2001043000305 20010430 00305 NM 2001 4 30 USAA010372 1 20010405 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 33516 22953 CLT - FOUND FRAME CRACKED .250 INCH, STATION 727C BETWEEN STRINGER 8R-9R. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001043000306 20010430 00306 NM 2001 4 30 USAA010373 1 20010405 A 5311 1131754 FRAME BOEING 737 7373B7 1384580 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 33516 22953 CLT - FOUND FRAME CRACKED .250 INCH, STATION 480, BETWEEN STRINGER 8R-9R. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001043000307 20010430 00307 WP 2001 4 30 USAAD01080 1 20010411 A 3260 WARNING SYSTEM DOUG DC9 DC982 3022082 WP MLG ACTIVATED A USAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 19 815US 48095 CLT-EWR - FLT 1744 - AFTER TAKEOFF AND LANING GEAR RETRACTION, THE LEFT GEAR RED UNSAFE LIGHT AND THE AMBER GEAR DOOR OP EN LIGHT REMAINED ILLUMINATED. THE LANDING GEAR WAS CYCLED WITH NO CHANGE, BUT GEAR DOWN INDICATIONS WERE NORMAL. THE AIRCRAFT CONTINUED TO THE DESTINATION AND LANDED WITHOUT INCIDENT. (M) 2 L 7 2 4F A6WE 2001043000308 20010430 00308 WP 2001 4 30 USAAD01079 1 20010409 A 3230 39370291 LINK DOUG DC9 DC981 3022081 WP RT MLG BROKEN A USAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 19 803US 48035 CMH-DCA - FLT 835 - AFTER TAKEOFF, WITH THE LANDING GEAR HANDLE RAISED THE RIGHT GEAR RED UNSAFE LIGHT AND THE AMBER GEA R DOOR OPEN LIGHT REMAINED ILLUMINATED. QRH PROCEDURES WERE FOLLOWED, ALL LIGHTS EXTINGUISHED WITH THE GEAR DOWN BUT NO CHANGE WITH THE GEAR UP. THE FLIGHT CONTINUED TO THE DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED TH E RIGHT LANDING GEAR LOWER RETRACT/EXTEND LINK. (M) 2 L 7 2 4F A6WE 2001043000309 20010430 00309 NM 2001 4 30 USAASB01099 1 20010410 A 3350 20131A BATTERY PACK BOEING 737 7374B7 1384702 NM CEILING DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 436US 24558 ALB - MAINTNANCE FOUND THE SEAT MOUNTED EMERGENCY EVACUATION LIGHTS, FROM SEAT ROWS 20 TO 23 INOPERATIVE. MAINTENANCE R EMOVED AND REPLACED THE BATTERY PACK IN THE AFT GALLEY CEILING, LEFT SIDE. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001043000310 20010430 00310 EU 2001 4 30 USAAF01010 1 20010323 A 2120 UNKNOWN FOKKER F28 F28MK0100 4990807 EU CABIN ODOR A USAA A UNSCHED LANDING E B VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 889US 11358 CLT-MEM - FLT 896 - A LOUD NOISE, WITH SUBSEQUENT VIBRATION AND METAL BURNING ODOR , WAS HEARD DURING FLIGHT. THE FLIGH T DIVERTED TO CHA AND LANDED WITHOUT INCIDENT. (M) 2 L 7 2 4F RT 2001043000311 20010430 00311 WP 2001 4 30 AALA20010670 1 20010401 A 2913 31495 PUMP DOUG DC9 DC982 3022082 WP NR 2 ENGINE LEAKING A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 552AA 53034 DFW - FLT 320 - EN ROUTE DFW-DEN, DETECTED RIGHT SIDE HYDRAULIC PUMP FAILURE DURING CLIMB-OUT. RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED RIGHT SIDE HYDRAULIC PUMP. SERVICED HYRAULIC SYSTEM. RAN ENGINES. LEAK CHECKS GOO D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001043000312 20010430 00312 NM 2001 4 30 USAA010364 1 20010405 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 33516 22953 CLT - FOUND FLOORBEAM CORRODED 58 INCHES, STATION 1016, LBL 29 TO RBL 29. LEVEL 2 CORROSION. REPAIR STRAP INSTALLED PE R SRM 53-00-51 AND 51-10-2. (M) 2 L 7 2 4F RT A16WE 2001043000313 20010430 00313 NM 2001 4 30 USAA010356 1 20010405 A 5320 693535214 TIE CLIP BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 33516 22953 CLT - FOUND STRINGER TIE CLIP CRACKED .250 INCH, STATION 597, STRINGER 9L. REPLACED PART. (M) 2 L 7 2 4F RT A16WE 2001043000314 20010430 00314 NM 2001 4 30 AALA20010655 1 20010323 A 5330 STRINGER BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 868AA 21373 TUL - FOUND CORROSION UNDER STRINGER 28R STATION 950F TO 970 RIVET HEADS BROKEN AND SKIN BULGING ON EXTERIOR SIDE. INST ALLED REPAIR DOUBLER IAW ESO 11697 DATED 3/20/01 AT 950F-970 STRINGER 28 RT. (M) 2 L 7 3 4F A3WE 2001043000315 20010430 00315 NM 2001 4 30 AALA20010654 1 20010315 A 5730 SKIN BOEING 727 727223 1384074 NM WING CENTER BOX CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 891AA 22007 TUL - FOUND WING CENTER SECTION, ABOVE LEFT PRIMARY HEAT EXCHANGER LOWER WING SKIN HAS HEAVY CORROSION 2 INCHES AFT OF S -5C SKIN BUTT JOINT LBL 18. BLENDED OUT CORROSION AND REPAIRED PER RM 57-30-3 PAGE 28. (M) 2 L 7 3 4F A3WE 2001043000316 20010430 00316 NM 2001 4 30 AALA20010690 1 20010403 A 5532 SKIN BOEING 727 727227 1384078 NM VERTICAL STAB SCRATCHED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 729AA 20736 TUL - LOWER LEFT VERTICAL STABILIZER HAS DEEP SCRATCH 3 INCHES BY .25 INCH JUST ABOVE TAIL NR. INSTALLED DOUBLER PER SR M 53-30-3 FIG 1. (M) 2 L 7 3 4F A3WE 2001043000317 20010430 00317 NM 2001 4 30 AALA20010691 1 20010403 A 5532 SKIN BOEING 727 727227 1384078 NM VERTICAL STAB SCRATCHED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 729AA 20736 TUL - FOUND DEEP SCRATCH 3 INCHES BY .5 INCH IN LOWER LEFT VERTICAL STABILIZER SKIN JUST ABOVE AIRCRAFT TAIL NR. INSTAL LED DOUBLER PER SRM 55-30-3, FIG 1. (M) 2 L 7 3 4F A3WE 2001043000318 20010430 00318 NM 2001 4 30 AALA20010692 1 20010403 A 5532 SKIN BOEING 727 727227 1384078 NM VERTICAL STAB SCRATCHED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 729AA 20736 TUL - FOUND DEEP SCRATCH 3 INCHES BY .25 INCH IN LOWER LEFT VERTICAL STABILIZER SKIN BETWEEN TAIL NR. INSTALLED DOUBLE R PER SRM 55-30-3, FIG 1. (M) 2 L 7 3 4F A3WE 2001043000319 20010430 00319 NM 2001 4 30 AALA20010694 1 20010401 A 5330 SKIN BOEING 727 727227 1384078 NM FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 729AA 20736 TUL - FOUND DENT IN FORWARD FUSELAGE SKIN STATION 370, STRINGER 18R. DYE CHECKED AREA, ONE CRACK FOUND. STOP DRILLED P ER SRM 51-10-1. INTALLED REPAIR DOUBLER PER RM 53-30-3. (M) 2 L 7 3 4F A3WE 2001043000320 20010430 00320 NM 2001 4 30 AALA20010695 1 20010402 A 5330 SKIN BOEING 727 727227 1384078 NM FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 729AA 20736 TUL - FOUND GOUGES IN SKIN OF FUSELAGE STRINGER 14L BETWEEN STATION 1106 AND STATION 1109. BLENDOUT OF GOUGES BEYOND LI MITS MINOR REPAIR. INSTALLED PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 2001043000321 20010430 00321 NM 2001 4 30 AALA20010686 1 20010402 A 5313 STRINGER BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 893AA 22009 TUL - FOUND STRINGER 29L CORRODED OUTBOARD SIDE STATION 1006 TO STATION 1010. INSTALLED NEW STRINGER SPLICE AND STRINGE R CLIP PER SRM 53-10-3 AND STRINGER 29L OUTBOARD SIDE STATION 1006-1010. (M) 2 L 7 3 4F A3WE 2001043000322 20010430 00322 NM 2001 4 30 AALA20010687 1 20010402 A 5313 STRINGER BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 893AA 22009 TUL - FOUND CORROSION 1 INCH BY 20 INCHES ON STRINGER AND SPLICE STRINGER 27R STATION 1010 TO 1014. INSTALLED REPAIR OF .063 17-7PH CRES, ANGLES AS PER ESO 11697 DATED 3-30-01. (M) 2 L 7 3 4F A3WE 2001043000323 20010430 00323 NM 2001 4 30 AALA20010688 1 20010329 A 5730 SKIN BOEING 727 727223 1384074 NM WING CENTER BOX CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 893AA 22009 TUL - FOUND CORROSION ON LOWER SURFACE OF CENTER WING SKIN RBL 30 BETWEEN S4C AND S5C CORROSION WAS REMOVED BY BLENDOUT AND A REPAIR WAS ACCOMPLISHED WITH DEVIATIONS PER ESO 11697 DATED 2/29/00. REMOVED DOUBLER PER ESO 11697 DATED 2/20/00 AND INSTALLED DOUBLER PER SRM 57-30-03 FIG 10. (M) 2 L 7 3 4F A3WE 2001043000324 20010430 00324 NM 2001 4 30 AALA20010689 1 20010401 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 893AA 22009 TUL - FOUND HFEC CRACK AT LOWER AFT CORNER OF DOOR CUTOUT FROM FASTENER TOWARD CUTOUT RADIUS, FS 417-419. CRACK INDICAT ION IN SKIN. REPAIRED PER BOEING S/B 727-53-188 LISTED ON PATTERN CARD NR 5708 PAGE NR 1. (M) 2 L 7 3 4F A3WE 2001043000325 20010430 00325 EA 2001 4 30 COMA0160361 1 20010404 A 5320 601R31527181 ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 982CA 9807 7168 ANGLE P/N 601R-31527-181 CORRODED AT LOWER LONGENON, PASSENGER DOOR ANGLE LOCATED AT STR 17 FS 342.7 - 317.70. FABRICAT ED ANGLE - 181 AND INSTALLED IAW WVAC EO 601R-53-2366. 2 L 7 2 4F RT A21EA 2001043000326 20010430 00326 EA 2001 4 30 JBXA000266 1 20010416 A 3234 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 EA NLG WW FAILED A JBXA L A ABORTED APPROACH UNSCHED LANDING J WARNING INDICATION LD LANDING 1 SO 05 591ML 7388 UPON APPROACH INTO LGA NOSE DIAGREE MESSAGE ON EICAS, NOSE GEAR FAILED TO EXTEND NORMALLY. A/C DIVERTED TO SWF WHERE EM ERGENCY GEAR HANDLE WAS PULLED. A/C LANDED WITH OUT INCIDENT. LANDING GEAR WAS PINNED AND MAINTENANCE FERRIED TO RDU. TROUBLSHOOTING INDICATED NOSE LANDING GEAR SELECTOR TO BE FAULTY. REMOVED AND REPLACED NOSE LANDING GEAR SELECTOR VALV E IAW CL-65 AMM 32-33-10. JACKED NOSE GEAR, SWUNG NOSE GEAR SEVERAL TIMES AND NO FAULTS NOTED. 2 L 7 2 4F RT A21EA 2001043000327 20010430 00327 WP 2001 4 30 CALA0100378 1 20010413 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND LT FLOOR PANEL DELAMINATED AT FS 1031 - 1155. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001043000328 20010430 00328 WP 2001 4 30 CALA0100379 1 20010413 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND RT CABIN FLOOR PANEL DELAMINATED AT FS 1250 - 1309. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-0126 5. 2 L 7 2 4F A6WE 2001043000329 20010430 00329 NM 2001 4 30 CALA0100380 1 20010416 A 5320 STIFFENER BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND A 1 INCH CRACK IN VERTICAL STIFFENER 18 INCHES ABOVE RT KEEL BEAM AT MAIN WHEEL WELL FORWARD BULKHEAD, STA 663, RBL 6. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 57-10-60 AND 51-10-01. 2 L 7 2 4F RT A16WE 2001043000330 20010430 00330 NM 2001 4 30 CALA0100382 1 20010416 A 5753 SKIN BOEING 737 737524 1384721 NM FLAP GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14628 27532 INSPECTION FOUND NR 1 MID FLAP SKIN GOUGED BY NR 2 FAIRING PRELOAD PAD. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5753-01 152. 2 L 7 2 4F RT A16WE 2001043000331 20010430 00331 WP 2001 4 30 CALA0100383 1 20010416 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND AFT PIT INTERCOSTAL CRACKED AT FS 1332 BETWEEN LONGERON 27R AND 28R, BELOW RT CARGO TRACK. THE INTERCO STAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2, 51-10-3, 51-10-4, AND 51-30-5. 2 L 7 2 4F A6WE 2001043000332 20010430 00332 WP 2001 4 30 CALA0100384 1 20010416 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND CABIN LT CENTER SEAT TRACK CORRODED AT FS 1120 - 1220. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-2, 51-30-1, 51-10-3, AND 53-05. 2 L 7 2 4F A6WE 2001050100001 20010501 00001 WP 2001 5 1 UPS01835687 1 20010403 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2 AFT PIT FWD ENTRY CARGO DOOR STA 1220 LONG 34R FITTING CRACKED RMVD CRACKED FITTING IAW DC8 SRM 5 1-1-20D RECD LOCATED & DRILLED NEW FITTING & REPAIR ANGLES IAW DC8 SRM 53-2-0 AND INSTALLED IAW DC8 SR M 51-1-20D 2 L 7 4 4F RT 4A25 2001050100002 20010501 00002 WP 2001 5 1 UPS01835688 1 20010403 A 5320 PAN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2 AFT PIT AFT ENTRY DOOR CRACKED TOP OF SCUFF PLATE STA 1410 L34R. REMOVED DOOR SCUFF PLATE SEAL COMP RESSOR LWR HOLAF FABBED REPAIR IN STALLED NEW SEAL COMPRESSOR INSTALLED REPAIR & SCUFF PLATE IAW DC8 S RM 51-1-21 &51-1- 20D 2 L 7 4 4F RT 4A25 2001051800035 20010518 00035 WP 2001 5 18 UPS01835706 1 20010424 A 2622 EXTINGUISHER DOUG DC8 DC871F 302199D WP CABIN LEAKING A IPXA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:N/A PORTABLE FIRE EXTINGUISHER LEAKING NEEDS RECHARGE. REMOVED AND REPLACED FIRE EXTINGUISHER IN COURIE R AREA. 2 L 7 4 4F RT 4A25 2001050100003 20010501 00003 EU 2001 5 1 20010417CW008 1 20010129 A 2432 RETAINER AMD FALC50 FALCON50MYST 2730106 EU GARRTT TFE731 TFE731* 01518 WP BATTERY WRONG PART B JGVR K NONE O OTHER IN INSP/MAINT 1 CE 09 35RZ 113 UPON INSPECTION OF UNIT FOUND ALL THREE BATTERY CELL RETAINERS LOOSE. REMOVED RETAINERS AND FOUND BATTERY CELLS PHYSICA LLY TOO SHORT TO MAKE PROPER CONTACT WITH BATTERY HOLDER TERMINALS. BATTERY CELL PART NUMBERS NOT FOUND. REPLACEMENT O F CELLS WITH PART NUMBERS SPECIFIED IN MFG MANUAL. 2 L 7 3 4F 4 F A46EU E6WE 2001050100005 20010501 00005 EU 2001 5 1 20010417CW010 1 20010129 A 2432 166241 RETAINER AMD FALC50 FALCON50MYST 2730106 EU GARRTT TFE731 TFE731* 01518 WP BATTERY WRONG PART B JGVR K NONE O OTHER IN INSP/MAINT 1 CE 09 35RZ 113 UPON INSPECTION FOUND ALL 3 CELLS UNAUTHORIZED. BATTERY CELL PART NUMBER NOT FOUND. REPLACEMENT OF CELLS WITH PART NU MBER SPECIFIED IN MFG MANUAL. 2 L 7 3 4F 4 F A46EU E6WE 2001050100006 20010501 00006 EU 2001 5 1 RAIA00104010 1 20010412 A 2612 FIRE WARNING JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT FALSE ACTIVATION A RAIA F ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 CE 03 563HK 12907 12907 41079 5404-EWR-DURING CLIMB LEFT HAND ENGINE FIRE INDICATION AT 2000 FEET, FIRE BOTTLE WAS BLOWN AND WARNING LIGHT WENT OUT. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND FIRE BOTTLE, BOTH SQUIBS AND LEFT HAND ENGINE FIRE LOOP IAW J41 MAINTENAN CE MANUAL. 2 L 7 2 4T RT A41NM 2001050100008 20010501 00008 EA 2001 5 1 20010411CW011 1 20010306 A 2752 SC14000062 BEARING EATON CNDAIR CL600 CL6002B19 EA FLAP ACTUATOR LACK OF LUBE B VK6R K NONE O OTHER IN INSP/MAINT 1 GL 09 1350 THRUST BEARING FAILURE DUE TO LACK OF LUBRICATION AND POSSIBLE PRELOAD CONDITION. 2 L 7 2 4F RT A21EA 2001050100009 20010501 00009 WP 2001 5 1 ZW0A0100401 1 20010417 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 9630A 53561 THE EGRESS FLOOR PATH LIGHT WAS INOPERATIVE BETWEEN ROWS 21 AND 22. REPLACED THE LIGHT MODULE. CHECK-C 4-21-00 STL. 2 L 7 2 4F RT A6WE 2001050100010 20010501 00010 WP 2001 5 1 ZW0A0100402 1 20010416 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT IN THE AFT CARGO COMPT THE RT TIE DOWN TRACK WAS CORRODED AT STA 1117 TO 1155. REMOVED AND REPLACE D TIE DOWN TRACK AS REQUIRED PER SPM 6-70-01. TREATED, PRIMED, AND PAINTED PER SRM 51-10-3. INSTALLED FASTENERS PER SR M 51-30-1 AND 51-30-02. 2 L 7 2 4F A6WE 2001050100011 20010501 00011 WP 2001 5 1 ZW0A0100403 1 20010416 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT IN FWD CABIN, FOUND CORROSION ON FLOOR SUPPORT AT STA 160 THRU STA 200, LBL 7 INCHES. MADE NEW FLO OR SUPPORT PER SAMPLE PER SPM 6-70-01, REF IPC 53-40-00 FIG 80, ITEM 215. INSTALLED SUPPORT USING SCREWS, WASHERS, AND NUTS AND INSTALLED PER SRM 51-30-1, PAGE 11, 12, AND 13. 2 L 7 2 4F A6WE 2001050100012 20010501 00012 EU 2001 5 1 MALA010402 1 20010413 A 2450 BUSS SAAB SF340 SF340A 7850100 EU COCKPIT MALFUNCTIONED A MALA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 GL 15 27XJ 027 INFLIGHT ON FLIGHT 2913, THE RT MAIN BUS LIGHT ILLUMINATED. NO BUS-TIE CONNECT OCCURRED, ALL RIGHT MAIN BUS EQUIPMENT W AS LOST. ORH WAS COMPLETED. STANBY 26V INVERTER WAS SELECTED AS PER QRH, 20 - 30 SECONDS LATER RT SIDE EQUIPMENT WAS RE STORED. RIGHT MAIN BUS LIGHT WAS EXTINGQUISHED. AIR RETURN TO LAF. MAINTENANCE RAN ENGINES, POWERED BOTH BUS. 2 L 7 2 4T RT A52EU 2001050100013 20010501 00013 EU 2001 5 1 MALA010403 1 20010413 A 2750 8519M3 FCU SAAB SF340 340B 7860101 EU FLAPS FAULTY A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 417XJ 340B417 DURING FLIGHT 2828 FROM DTW, FLAPS CYCLE BETWEEN 0-2-3 DEGREES EVERY 1 TO 2 MINUTES DURING CRUISE. FLIGHT AND FLIGHT LV L 220, INDICATED SPEED OF 180-185. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED EIE FLAP CONTROL UNIT P/N 8519M3 , S/N OFF 061, S/N ON 484 AND FLAP CONTROL VALVE P/N MP1416100-5, S/N OFF 1365, S/N ON 1606. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2001050100014 20010501 00014 EU 2001 5 1 20010411CW015 1 20010103 A 2431 23761 BATTERY SAFT AMD FALCON FALCON20 2730103 EU GE CF700 CF700* 30010 NE TEMP PROBE IMPROPER PART E JGVA K NONE O OTHER IN INSP/MAINT 1 CE 09 312K 324 IMPROPER TEMPERATURE PROBE INSTALLED FOR THIS PN BATTERY. TEMERATURE PROBES HAVE BEEN ROUTINELY INSTALLED WITHOUT SPECI FIC APPROVAL TO DO SO. 2 L 7 2 4F 4 F RT A7EU E7EA 2001050100015 20010501 00015 NM 2001 5 1 20010501AP002 1 20010312 A 5310 SHEAR TIE BOEING 747 747273C 1384896 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND FASTENER HOLE CRACK ON MED R5 BS 2231 STRINGER 24R-25R, ONE CRACK ON AFT INNER CHORD AFT ANGLE, ONE CR ACK ON INNER CHORD FORWARD ANGLE, AND TWO CRACKS ON DOOR REVEAL. OVERSIZED CRACKED FASTENER HOLE, TRIMMED OFF CRACKED C HORD AND REVEAL, NDT INSPECTED, INSTALLED REPAIR DOUBLER AND FILLERS PER BOEING MSG AND RS R-53-62-34623. REF EIA200117 7. (M) 2 L 7 4 4F A20WE 2001050100016 20010501 00016 NM 2001 5 1 EIA2001176 1 20010312 A 5320 FITTING BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND BS 1000 BULKHEAD SEAT TRACK ATTACH SHEAR TIE FITTING CRACKED. REPLACED SHEAR TIE FITTING PER SRM 51-1 0-01. (M) 2 L 7 4 4F A20WE 2001050100017 20010501 00017 NM 2001 5 1 EIA2001175 1 20010312 A 5313 STRINGER BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND FORWARD CARGO STATION 980 STRINGER 38L CRACKED. REPAIRED STATION 980 STRINGER 38L PER SRM 53-10-03. (M) 2 L 7 4 4F A20WE 2001050100018 20010501 00018 NM 2001 5 1 EIA2001174 1 20010312 A 5313 STRINGER BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND FORWARD CARGO STATION 980 STRINGER 38R CRACKED. REPAIRED STATION 980 STRINGER 38R PER SRM 53-10-03. ( M) 2 L 7 4 4F A20WE 2001050100019 20010501 00019 NM 2001 5 1 EIA2001173 1 20010312 A 5330 SKIN BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND FUSELAGE SKIN CRACKED AT STATION 2658 RIGHT WL 316 TO 319. TRIMMED OFF CRACK, NDT INSPECTED, REPAIRED SKIN PER SRM 53-30-03. (M) 2 L 7 4 4F A20WE 2001050100020 20010501 00020 NM 2001 5 1 EIA2001172 1 20010312 A 5330 SKIN BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND BS 980 LEFT SKIN LAYER CRACKED AT LOWER DRAG SPLICE FITTING AND SHIM INSIDE BATHTUB FITTING AT STRINGE R 38L. TRIMMED OFF CRACKS, NDT INSPECTED, REPLACED SHIM AND REPAIRED SKIN PER SRM 53-30-03. (M) 2 L 7 4 4F A20WE 2001050100021 20010501 00021 NM 2001 5 1 20010501AP003 1 20010312 A 5320 SHIM BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND BS 980 LEFT SKIN LAYER CRACKED AT LOWER DRAG SPLICE FITTING AND SHIM INSIDE BATHTUB FITTING AT STRINGE R 38L. TRIMMED OFF CRACKS, NDT INSPECTED, REPLACED SHIM AND REPAIRED SKIN PER SRM 53-30-03. REF EIA2001172. (M) 2 L 7 4 4F A20WE 2001050100022 20010501 00022 NM 2001 5 1 EIA2001171 1 20010312 A 5210 65B1356425 FITTING BOEING 747 747273C 1384896 NM PAX DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND MED L1 DOOR AFT UPPER STOP FITTING CRACKED. REPLACED STOP FITTING PER SRM 51-10-01. (M) 2 L 7 4 4F A20WE 2001050100023 20010501 00023 NM 2001 5 1 EIA2001170 1 20010312 A 5320 65B1117615 DOOR FRAME BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND MED L3 DOOR FORWARD CUTOUT REVEAL CRACKED. REPLACED REVEAL PANEL PER SRM 51-10-01. (M) 2 L 7 4 4F A20WE 2001050100024 20010501 00024 NM 2001 5 1 EIA2001169 1 20010312 A 5320 STOP FITTING BOEING 747 747273C 1384896 NM NR 6 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND MED R3 DOOR FORWARD CUTOUT NR NR 6 STOP FITTING CRACKED. REPLACED NR 6 STOP FITTING PER EO 53-747-154 2-99 REV A. (M) 2 L 7 4 4F A20WE 2001050100025 20010501 00025 NM 2001 5 1 EIA2001168 1 20010312 A 5310 DOOR FRAME BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND MED L2 DOOR FORWARD CUTOUT LOWER REVEAL CRACKED. STOP DRILLED, NDT INSPECTED, REPAIRED REVEAL PER SRM 51-40-03 FIG 1. (M) 2 L 7 4 4F A20WE 2001050100026 20010501 00026 NM 2001 5 1 EIA2001166 1 20010312 A 5311 141U1054113 FRAME BOEING 747 747273C 1384896 NM BS 500 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND BS 500 STRINGER 14L FRAME WEB CRACKED. BS 500 FRAME WEB FROM STRINGER 0 TO STRINGER 18L REPLACED PER E O 53-747-1143-91 REV E AND DWG 624U0003 SH 25H. (M) 2 L 7 4 4F A20WE 2001050100027 20010501 00027 NM 2001 5 1 EIA20011165 1 20010312 A 5311 141U105357 FRAME BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND BS 480 STRINGER 14L FRAME WEB CRACKED. BS 480 FRAE WEB FROM STRINGER 0 TO STRINGER 16L REPLACED PER E O 53-747-1143-91 REV E AND DWG 624U0003 SH 24H. (M) 2 L 7 4 4F A20WE 2001050100028 20010501 00028 NM 2001 5 1 EIA2001164 1 20010312 A 5315 FLOORBEAM BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 FOUND BS 330 RBL 58 BELOW FLOORBEAM WEB CRACKED. TRIMMED OFF CRACK, NDT INSPECTED, REPAIRED FLOORBEAM WEB AND UPPER CHO RD PER DWG 65B28068. (M) 2 L 7 4 4F A20WE 2001050100029 20010501 00029 NE 2001 5 1 20010427CW007 1 20010206 A 6230 643520536101 SHAFT SKRSKY S64 S64F NE PWA JFTD12 JFTD12A4A 52047 NE MAIN ROTOR CRACKED B JYDR K NONE O OTHER IN INSP/MAINT 1 NM 09 223AC 2228 64086 DURING OVERHAUL, MAGNETIC PARTICLE INSPECTION REVEALED MULTIPLE INDICATION IN THE LOWER SPLINE AREA OF MAIN ROTOR SHAFT. LONGEST INDICATION MEASURED APPROX .500 INCH IN LENGTH, BEGINNING IN THE ROOT AREA EXTENDING OVER SPLINE FACE, DOWN TO THE NEXT ADJACENT ROOT AREA, INCLUDING UP TO THREE CRACKS ON SAME SPLINE. 2 G 7 2 4U 4 U H6EA E15EA 2001050100030 20010501 00030 NE 2001 5 1 20010427CW008 2 20010118 A 7230 370930 SEAL PWA SKRSKY S64 S64E 8142604 NE PWA JFTD12 JFTD12A4A 52047 NE COMPRESSOR CRACKED E JYDR K NONE O OTHER IN INSP/MAINT 1 NM 09 176AC 2375 672603 64003 672603 ENGINE DISASSEMBLED FOR REPAIR OF COMPRESSOR. AT DISASSEMBLY, 9TH STAGE DISK DOUBLE LIPPED REAR ROTATING AIRSEAL, WAS F OUND TO BE CRACKED IN 3 PLACES, APPROXIMATELY 0 , 30, AND 120 DEGREES. ENGINE WAS OPERATED UNDER NORMAL CONDITIONS A ND NO ABNORMALITIES WERE FOUND DURING ENGINE PRE RUN PRIOR TO DISASSEMBLY. BELIEVE CRACKING MAY BE FROM THE TIGHT FIT F OUND DURING INSTALLATION AND REMOVAL OF THE SEAL FROM THE DISK EVEN WHEN HOT AND COLD PRACTICES ARE USED. 2 G 7 2 4U 4 U H4EA E15EA 2001050100031 20010501 00031 NM 2001 5 1 EIA2001163 1 20010312 A 5315 FLOORBEAM BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND BS 330 LBL 72 BELOW FLOORBEAM WEB CRACKED. TRIMMED OFF CRACK, NDT INSPECTED, REPAIRED FLOORBEAM WEB A ND UPPER CHORD PER DWG 65B28068 SH 5. (M) 2 L 7 4 4F A20WE 2001050100032 20010501 00032 NM 2001 5 1 EIA2001162 1 20010312 A 5311 141U100841 FRAME BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND BS 360 STRINGER 3L FRAME CRACKED. FOUND BS 360 FRAME FROM STRINGER 0 TO STRINGER 14L REPLACED PER EO 53-747-1143-91 REV E AND DWG 624U0003 SH 9K. (M) 2 L 7 4 4F A20WE 2001050100033 20010501 00033 NM 2001 5 1 EIA2001161 1 20010312 A 5311 141U105166 FRAME BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND BS 440 FRAME STRINGER 10A RIGHT CRACKED. FOUND BS 440 FRAME FROM STRINGER 0 TO STRINGER 16R REPLACED PER EO 53-747-1143-91 REV E AND DWG 624U0003 SH 22R. (M) 2 L 7 4 4F A20WE 2001050100034 20010501 00034 NM 2001 5 1 EIA2001160 1 20010312 A 5313 STRINGER BOEING 747 747273C 1384896 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND FORWARD CARGO COMPARTMENT AT BS 800 STRINGER 47R CORRODED. BLENDED OUT CORROSION AND REPAIRED STRINGE R PER SRM 53-10-03. (M) 2 L 7 4 4F A20WE 2001050100035 20010501 00035 NM 2001 5 1 EIA2001159 1 20010312 A 5347 SEAT TRACK BOEING 747 747273C 1384896 NM FUSELAGE BROKEN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND BS 1260 RBL 11 SEAT TRACK FLANGE BROKEN. REPLACED SEAT TRACK ASSY FROM BS 1000 TO BS 1265 RBL 11 PER SRM 51-10-01. (M) 2 L 7 4 4F A20WE 2001050100036 20010501 00036 NM 2001 5 1 EIA2001157 1 20010312 A 5330 SKIN BOEING 747 747273C 1384896 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND BS 1470 PRESSURE DECK WEB SKIN CORRODED AT LBL 34 FLOORBEAM LOWER CHORD. REMOVED CORROSION, NDT INSPE CTED, AND INSTALLED REPAIR DOUBLER PER BOEING MSG EVR-HKG-01-00038H / 00029F / 00019H / 00025F AND RS R-53-48-34616. (M ) 2 L 7 4 4F A20WE 2001050100037 20010501 00037 NM 2001 5 1 EIA2001156 1 20010312 A 5315 FLOORBEAM BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND STATION 330 RIGHT FLOORBEAM WEB CRACKED. TRIMMED OFF CRACK, NDT INSPECTED, REPAIRED WEB AND UPPER CHO RD PER DWG 65B28068 SH 5. (M) 2 L 7 4 4F A20WE 2001050100038 20010501 00038 NM 2001 5 1 EIA2001155 1 20010312 A 5315 FLOORBEAM BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND STATION 330, LEFT FLOORBEAM WEB CRACKED. TRIMMED OFF CRACK, NDT INSPECTED, REPAIRED WEB AND UPPER CHO RD PER DWG 65B28068 SH 5. (M) 2 L 7 4 4F A20WE 2001050100039 20010501 00039 NM 2001 5 1 EIA2001154 1 20010312 A 5311 FRAME BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND R1 AFT LOWER CORNER AT BS 488 STRINGER 25 CRACKED ON AFT SIDE OF FRAME WEB AT NR 1 STOP FITTING AREA. REPAIRED WEB BETWEEN STRINGER 23R TO STRINGER 30R PER EO 53-747-1626-01 PART 2. (M) 2 L 7 4 4F A20WE 2001050100040 20010501 00040 NM 2001 5 1 EIA2001153 1 20010312 A 5312 BULKHEAD BOEING 747 747273C 1384896 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 FOUND BS 1350 RIGHT BLG WW BULKHEAD WEB CORRODED AT WL 190 AND RBL 115. REMOVED CORROSION, NDT INSPECTED, SHOT PEENED R EWORKED AREA, INSTALLED INBOARD CHORD WITH FILLER AND REPAIRED WEB PER BOEING MSG AND RS R-53-48-34637. (M) 2 L 7 4 4F A20WE 2001050100041 20010501 00041 NM 2001 5 1 EIA2001152 1 20010312 A 5313 STRINGER BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND BS 300-320 RIGHT STRINGER 8 CRACKED. REPLACED STRINGER PER SRM 51-30-02 AND 51-10-01 PAGE 8. (M) 2 L 7 4 4F A20WE 2001050100042 20010501 00042 NM 2001 5 1 EIA2001149 1 20010312 A 5311 FRAME BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND BS 300 RT BETWEEN STRINGER 10A AND STRINGER 13A WEB CRACKED. REPAIRED SHEAR WEB PER SRM 51-40-02. (M ) 2 L 7 4 4F A20WE 2001050100046 20010501 00046 WP 2001 5 1 ABXA010139 1 20010320 A 5730 37578571 STRUCTURE DOUG DC8 DC863F 302198F WP RT WING LEAKING A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 85679 46041 A FASTENER WAS FOUND TO BE LEAKING FUEL AT STA 795. MAINTENANCE REPAIRED THE AREA IAW REA D857-40312MR AND DC-8 SRM. 2 L 7 4 4F 4A25 2001050100047 20010501 00047 WP 2001 5 1 ABXA010138 1 20010310 A 5311 561560441 FRAME DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 85679 46041 A CRACK 4.5 INCH LONG WAS FOUND ON THE NOSE WHEEL WELL AFT DOOR FORWARD HINGE FRAME. MAINTENANCE REPAIRED THE CRACK IAW REA D853-40280MR. 2 L 7 4 4F 4A25 2001050100048 20010501 00048 WP 2001 5 1 UPS01835680 1 20010405 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 STA. 140 FLOORBEAM IS CORRODED BEYOND LIMITS BETWEEN RBL. 50 AND RBL. 60. REPAIRED FLOORBEAM I.A.W . 8110-3 APPROVED DH SK 779-363 2 L 7 4 4F RT 4A25 2001050100049 20010501 00049 NM 2001 5 1 EISA20010072 1 20010320 A 2130 1106P12 SWITCH BOEING BOEING 727 7272M7 138407S NM CABIN FAULTY A EISA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 07 725RW 21502 AUTO PACK SYSTEM TRIPPED AT TAKEOFF POWER. REMOVED AND REPLACED AUTO PACK TRIP SWITCHES PER M/M 21-11-11, 21-30, OPS CH ECK NORMAL. 2 L 7 3 4F A3WE 2001050100050 20010501 00050 NM 2001 5 1 EISA20010074 1 20010408 A 3270 MS250114 SWITCH BOEING BOEING 727 727223 1384074 NM TAIL SKID STUCK A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 311NE 19703 AFTER GEAR RETRACTION TAIL SKID ANNUNCIATOR LIGHT ILLUMINATED WHEN GEAR HANDLE PLACED TO OFF. CYCLED GEAR, SAME INDICAT ION. AIR TURNBACK TO PDX. CORRECTIVE ACTION: CLEANED AND LUBED TAIL SKID SWITCHES, SYSTEM OPS CHECK NORMAL PER M/M 32-7 1. 2 L 7 3 4F A3WE 2001050100051 20010501 00051 NM 2001 5 1 EISA20010070 1 20010312 A 5753 652163476 FLAP BOEING 727 727223 1384074 NM RT WING DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ROUTINE B-CHECK INSPECTION, FOUND RT INBOARD LOWER FLAP HAS DELAMINATED AREA. BONDED FIBERGLASS OVERLAYS TO REPA IR DOUBLER AND FILLER, ALODINED, SEALED AND PRIMED IAW SRM 51-40-5, 51-40-2, 57-50-1 AND M/M 51-20-151. 2 L 7 3 4F A3WE 2001050100052 20010501 00052 NM 2001 5 1 EISA20010071 1 20010305 A 5347 BAC1520792 SEAT TRACK BOEING 727 727223 1384074 NM CABIN CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6815 19490 DURING ROUTINE B-CHECK INSPECTION FOUND CRACK IN SEAT TRACK BETWEEN BS 520 AND BS 540 AT LBL 45. FABRICATED AND INSTALL ED SEAT TRACK SPLICE, ALODINED AND PRIMED IAW SRM 51-10-2, 53-10-5 FIG 1, AND SOPM 20-50-01. 2 L 7 3 4F A3WE 2001061300026 20010613 00026 WP 2001 6 13 ERYA258211 2 20010412 A 7230 BLADE RAYTHN DH125 HAWKER800 7450004 CE GARRTT TFE731 TFE7315R 01518 WP NR 1 ENGINE BROKEN E ERYA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 CE 07 91DV 2725 2725 258211 P91535 LEVEL CRUISE AT FL-390 VMC CONDITIONS. LOUD NOISE (BANG) FROM NR 1 ENGINE. N1 IMMEDIATELY DROPPED TO ABOUT 17 PERCENT. EMERGENCY WAS DECLARED, ENGINE SHUTDOWN CONDUCTED, AIRCRAFT WAS LANDED AT ELP. ENGINE IS BEING CHANGED. AT ENGINE DI SASSEMBLY FOUND: 2ND STAGE LPC ROTOR ASSEMBLY; ONE OF THE DOVETAILS BROKE OFF CAUSING RELEASE OF TWO BLADES AND THE SUB SEQUENT DAMAGE TO OTHER ENGINE COMPONENTS. 2 L 7 2 4F 4 F RT A3EU E6WE 2001050100053 20010501 00053 WP 2001 5 1 JWC101 1 20010314 A 4920 3600550 CAP DOUG DC10 DC1030 3023501 WP APU COMPRESSOR FAILED D F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 NM 07 335SJ 47843 FIRE WARNING WHEN STARTING APU, DURING LANDING RUN. FIRE DRILL CARRIED OUT. FIRE EVENT COMFIRMED BY GROUND INSPECTION. DEFECT FAILURE OF APU COMPRESSOR END CAP. PARTS OF THE END CAP PIERCED APU BAY ROOF SLOWER SURFACE OF STABILIZER CENT ER SECTION TORQUE BOX HOLE APPROX 5.5 INCHES X 1.25 INCHES. 2 L 7 3 4F A22WE 2001050100054 20010501 00054 WP 2001 5 1 ZW0A0100301 1 20010416 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 9615W 53562 THE RT AFT OVERWING EXIT EGRESS RED LIGHT DID NOT ILLUMINATE. RECONNECTED EGRESS LIGHT AT THE AFT OVERWING EXIT. CHECK -C 7-14-00 STL. 2 L 7 2 4F RT A6WE 2001050100055 20010501 00055 NM 2001 5 1 ZW0A0100302 1 20010417 A 3350 767 LIGHT BOEING 757 757231 1384950 NM EXTERIOR INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 724TW 288488 FOUND EXTERIOR EXIT LIGHT INOPERATIVE AT THE RT SIDE AFT, LT SIDE AFT, AND THE RT SIDE FWD CABIN DOORS. REPLACED LAMP A T THE RT SIDE FWD DOOR AND CLEANED OUT CORROSION IN LIGHT ASSEMBLY AT THE OTHER TWO DOORS. CHECK-C 2-28-01 LAX. 2 L 7 2 4F RT A2NM 2001050100056 20010501 00056 WP 2001 5 1 ZW0A0100303 1 20010411 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT THE FWD E AND E COMPT FORMER WAS CORRODED BELOW DOOR SILL AND BEHIND EQUIPMENT RACK, STA 168, STRIN GER 18R TO 21R. FORMER CORRODED BEOND LIMITS. INSTALLED NEW FORMER AND FRAME STIFFENER PER DRAWING 9911616 AND SPM 6-7 0-01. 2 L 7 2 4F A6WE 2001050100057 20010501 00057 WP 2001 5 1 ZW0A0100304 1 20010411 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT IN AFT CARGO COMPT, BETWEEN STA 1287 AND 1306, LONGERON 28R WEB MEMBRANE WAS CORRODED IN TWO PLACES . REMOVED OLD MEMBRANE AND REPLACED WITH NEW PER SERVICE BULLETIN 53-246 AND SRM 53-05, FIG 97. 2 L 7 2 4F A6WE 2001050100058 20010501 00058 WP 2001 5 1 ZW0A0100305 1 20010411 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT IN AFT CABIN, FOUND CORROSION AT FLOOR PAN, STA 1297, BETWEEN 5 AND 6 TRACK. REMOVED OLD MEMBRANE AND REPLACED WITH NEW PER SERVICE BULLETIN 53-246 AND SRM 53-05, FIG 97. 2 L 7 2 4F A6WE 2001050100059 20010501 00059 WP 2001 5 1 ZW0A0100306 1 20010410 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 909TW 49170 DURING CHECK-C MAINT FOUND CORROSION ON NUMBER 2 GALLEY OUTBOARD TIE DOWN TRACK, STA 212. FOUND CORRODED BEYOND LIMITS. REMOVED AND INSTALLED NEW FITTING PER SPM 6-70-01. FASTENERS PER SRM 51-10-4. PAINTED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001050100060 20010501 00060 WP 2001 5 1 ZW0A0100308 1 20010410 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 909TW 49170 DURING CHECK-C MAINT FOUND CORROSION ON STA 1287 FORMER FROM LONGERON 18L TO 24R. REPLACED FORMER FRAME FROM 18L TO 24R AT STA 1287 WITH NEW PER SRM 53-05. INSTALLED FASTENERS PER SRM 51-30-0. INSTALLED WET AND TREATED AND PAINTED PER SR M 51-10-3. 2 L 7 2 4F A6WE 2001050100061 20010501 00061 WP 2001 5 1 ZW0A0100309 1 20010411 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 909TW 49170 DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR MEMBRANE AND FLOOR SUPPORT STRUCTURE, STA 148 TO 218. REMOVED CORRO DED FLOOR SUPPORTS AND MEMBRANE, STA 148 TO 218, LBL 15 TO RBL 57, PER SPM 6-70-01 AND SRM 53-01, FIG 2. 2 L 7 2 4F A6WE 2001050100062 20010501 00062 WP 2001 5 1 ZW0A0100310 1 20010411 A 5345 FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 909TW 49170 DURING CHECK-C MAINT FOUND CORROSION ON NUMBER 1 GALLEY TIE DOWN FITTINGS. REPLACED TIE DOWN FITTINGS PER SPM 6-70-01. 2 L 7 2 4F A6WE 2001050100063 20010501 00063 WP 2001 5 1 ZW0A0100311 1 20010411 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 909TW 49170 DURING CHECK-C MAINT FOUND CORROSION ON CUSP ANGLE AT FWD SERVICE DOOR, STA 160 TO 200. REMOVED CORRODED SECTION OF CUS P ANGLE AND INSTALLED CUSP REPAIR SECTION PER SRM 53-05, FIG 55. 2 L 7 2 4F A6WE 2001050100064 20010501 00064 NM 2001 5 1 ZW0A0100312 1 20010413 A 5753 SKIN BOEING 757 757231 1384950 NM FLAP DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 715TW 28483 ON THE LT WING, THE LOWER INBD CORNER OF THE INBD AFT FLAP HAD BOTTOM SURFACE WITH IMPACT DAMAGE. AREA WAS APPROX 8 IN BY 6 IN WITH CRACK. INSTALLED 14 BY 15 INCH WET LAYUP PER SRM 57-53-01, FIG 201. CHECK-C 10-14-00 LAX. 2 L 7 2 4F RT A2NM 2001050100065 20010501 00065 WP 2001 5 1 ZW0A0100313 1 20010412 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP COCKPIT WORN A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT FOUND CAPTAINS SEAT TRACK WORN, FWD OTBD. REPAIRED SEAT TRACK PER SRM 53-05, FIG 92, AND DRAWING C O4216. 2 L 7 2 4F A6WE 2001050100066 20010501 00066 WP 2001 5 1 ZW0A0100315 1 20010412 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT IN FWD CABIN, FOUND CORROSION ON FLOOR SUPPORT AT STA 218 AND BL 0. MADE FLOOR SUPPORT PER DRAWING 9936535-31 USING MATERIAL 2929169, 7075-T6 EXTRUSION. 2 L 7 2 4F A6WE 2001050100067 20010501 00067 WP 2001 5 1 ZW0A0100317 1 20010413 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT FOUND DEEP CORROSION ON LONGERON 23R, WITH PITS IN BOTTOM END TIE, STA 1320 TO 1338. REPLACED LONG ERON 23R WITH NEW. SEALED PART DURING INSTALLATION PER SRM 51-20-00. REPLACED EXISTING HI-LOKS WITH HL 329 AND HLT 429 PER SRM 51-60-0 FIG 4. REINSTALLED RIVETS PER SRM 51-30-02. 2 L 7 2 4F A6WE 2001050100068 20010501 00068 WP 2001 5 1 ZW0A0100318 1 20010416 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 909TW 49170 DURING CHECK-C MAINT IN AFT CARGO COMPT FOUND CORROSION ON AFT END OF RT TIE DOWN TRACK, STA 1322 TO 1212. REMOVED AND REPLACED TRACK PER SRM 51-30-2. INSTALLED PER SRM 51-10-5 AND 51-10-1. TREATED AND PAINTED PER SRM 51-10-30, STA 1322 TO 1212. 2 L 7 2 4F A6WE 2001050100069 20010501 00069 WP 2001 5 1 ZW0A0100319 1 20010411 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 909TW 49170 DURING CHECK-C MAINT IN AFT CARGO COMPT STA 1211 TO 1320, THE RT HOLD DOWN TRACK HAD CORROSION. REMOVED AND REPLACED TR ACK PER SRM 51-30-2. INSTALLED PER SRM 51-10-5 AND 51-10-1. TREATED AND PAINTED PER SRM 5-10-30, STA 1211 TO 1320. 2 L 7 2 4F A6WE 2001050100070 20010501 00070 WP 2001 5 1 ZW0A0100320 1 20010416 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 909TW 49170 DURING CHECK-C MAINT IN THE AFT CARGO COMPT THE LT TIE DOWN TRACK HAD CORROSION AT SCREW HOLES, STA 1041 TO 1193. REMOV ED OLD TRACK AND INSTALLED NEW TRACK PER SRM 53-05. INSTALLED FASTENERS PER SRM 51-30-2 AND 51-30-2, STA 1041 TO 1212. 2 L 7 2 4F A6WE 2001050100071 20010501 00071 WP 2001 5 1 ZW0A0100321 1 20010412 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 909TW 49170 DURING CHECK-C MAINT IN THE AFT CARGO COMPT, THE LT TRACK WAS CORRODED, STA 1193 TO 1322. REMOVED TRACK FROM SPLICES TO AFT END OF BIN, AND INSTALLED NEW TRACK PER SRM 51-10-5 AND 51-10-1. 2 L 7 2 4F A6WE 2001050100072 20010501 00072 EU 2001 5 1 20010424CW007 1 20010320 A 2913 704A34310006 PUMP SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE HYDRAULIC SYS INOPERATIVE D O OTHER O OTHER NR NOT REPORTED 1 WP 19 352HH 2714 1B PILOT REPORTED HYDRAULIC LIGHT ILLUMINATION DURING FLIGHT, IMMEDIATELY SHUT DOWN HYDRAULIC SYSTEM. ON THE GROUND, PILOT STARTED THE AIRCRAFT FOR MAINTENANCE RUN AND HOVERED THE AIRCRAFT FEELING FULL HYDRAULIC CONTROL. MECHANICS REMOVED HY DRAULIC PUMP AND REPLACED BOTH THE PUMP AND SPLINED SHAFT AS PRECAUTIONARY MEASURES. SHAFT SHOWED SIGNS OF WEAR AND POS SIBLE SLIPPAGE, PUMP OPERATED NORMALLY. AIRCRAFT WAS RUN AGAIN WITH NO FURTHER FAULT FOUND. 1 G 7 1 3U 3 U NC H9EU E19EU 2001050100073 20010501 00073 SO 2001 5 1 C2XA01IA218 1 20010415 A 3350 7287103503 CONTROLLER EMB 145 EMB145ER SO COCKPIT INOPERATIVE A C2XA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 27 14945 145049 IAH - DURING MAINTENANCE INSPECTION, THE EMERGENCY LIGHT NOT ARMED MESSAGE APPEARED ON THE EICAS DISPLAY. MAINTENANCE R EMOVED AND REPLACED THE CABIN LIGHT CONTROLLER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001050100074 20010501 00074 SO 2001 5 1 C2XA01IA219 1 20010418 A 3350 20131A POWER SUPPLY EMB 145 EMB145 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13964 145123 IAH - DURING 4-A INSPECTION, THE NUMBER FIVE AND SIX FLOOR EMERGENCY LIGHTS, AND THE LEFT HAND DOOR EMERGENCY LIGHT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT POWER SUPPLY, AND THE AIRCR AFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001050100075 20010501 00075 SO 2001 5 1 C2XA01IA220 1 20010419 A 5300 12019737003 SKIN EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16718 120136 IAH - DURING MAINTENANCE INSPECTION, THE BELLY SKIN WAS FOUND TO BE CRACKED AROUND THE VHF 2 ANTENNA. MAINTENANCE CUT O UT THE DAMAGED SECTION OF SKIN AND PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH EMBRAER FAX GST-1268-01 AND EMB-120 SRM 53-20-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001050100076 20010501 00076 WP 2001 5 1 MWEA010582 1 20010417 A 5320 39125091 DOUBLER DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 INTERCOSTAL AT LONGERON 29 RIGHT, STATION 351-362 HAD LIGHT CORROSION ON LOWER FLANGE AND TOP DOUBLER. REMOVED CORROSIO N, REMOVED TOP DOUBLER, DRILLED AND INSTALLED NEW TOP DOUBLER. 2 L 7 2 4F A6WE 2001050100077 20010501 00077 WP 2001 5 1 MWEA010583 1 20010417 A 5310 S1761367 FITTING DOUG DC9 DC932 3022066 WP CARGO BAY CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FORWARD CARGO DOOR JAMB TEE FITTING WAS EXFOLIATED INSIDE BOX STRUCTURE TOP OF DOOR JAMB. REMOVED FITTING, FABRICATED, AND INSTALLED NEW TEE FITTING. 2 L 7 2 4F A6WE 2001050100078 20010501 00078 WP 2001 5 1 MWEA010584 1 20010417 A 5310 99579071 FITTING DOUG DC9 DC932 3022066 WP CARGO BAY CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FORWARD CARGO DOOR JAMB, FOUND T-FITTING CORRODED INSIDE BOX STRUCTURE TOP OF DOOR JAMB ABOVE AFT STOP FITTING. REMOVED BRACKET, FABRICATED, DRILLED, AND INSTALLED NEW FITTING. 2 L 7 2 4F A6WE 2001050100079 20010501 00079 WP 2001 5 1 MWEA010585 1 20010417 A 5320 99579453 BRACKET DOUG DC9 DC932 3022066 WP CARGO BAY CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 AT FORWARD CARGO DOOR JAMB FOUND LIGHT CORROSION ON L-BRACKET INSIDE BOX STRUCTURE. REMOVED BRACKET, DRILLED AND INSTAL LED NEW BRACKET. 2 L 7 2 4F A6WE 2001050100080 20010501 00080 WP 2001 5 1 MWEA010587 1 20010417 A 5320 991963815 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 CABIN INTERCOSTAL BETWEEN FLOORBEAM AT STATION 351-370 INBOARD OF NR 1 SEAT TRACK HAS CORROSION AROUND NUT PLATES. REMO VED FABRICATED, DRILLED, AND INSTALLED NEW INTERCOSTAL. 2 L 7 2 4F A6WE 2001050100081 20010501 00081 WP 2001 5 1 MWEA010588 1 20010417 A 5321 995791822 FLOOR PANEL DOUG DC9 DC932 3022066 WP CABIN CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FLOORBOARD D-5 CHAFE FLEXIBLE JOINT HAD CRACKED HOLES. REMOVED FLEXIBLE JOINT. FABRICATED AND INSTALLED NEW JOINT. 2 L 7 2 4F A6WE 2001050100082 20010501 00082 WP 2001 5 1 MWEA010589 1 20010417 A 5320 591014211 CLIP DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 SEVERAL CLIPS (6) REQUIRED REPLACEMENT BETWEEN STATION 370 - 427. REMOVED CLIPS, FABRICATED AND INSTALLED NEW CLIPS. 2 L 7 2 4F A6WE 2001050100083 20010501 00083 WP 2001 5 1 MWEA010590 1 20010417 A 5720 9919348501 STRUCTURE DOUG DC9 DC932 3022066 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 AT LEFT WING FOUND CORROSION ON LOWER TEE CAP HORIZONTAL LEG BETWEEN STRINGER 13 AND 14. REMOVED CORROSION, SUBMITTED B LENDOUTS TO BOEING AND ARE ACCEPTABLE PER TELEX MWX-ORD-01-00146H DATED 21, FEB, 2001. PLACED ON WATCH ITEM 5616 FOR RE PETITIVE INSPECTION. 2 L 7 2 4F A6WE 2001050100084 20010501 00084 WP 2001 5 1 MWEA010591 1 20010417 A 5720 4917060507 CLIP DOUG DC9 DC932 3022066 WP WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 CORROSION FOUND ON OUTBOARD OF XCW 58 LOWER TEE CAP, HORIZONTAL LEG BETWEEN STRINGER 23. REMOVED 2 CLIPS FOR OUT OF LIM ITS CORROSION. FABRICATED DRILLED AND INSTALLED NEW CLIPS. 2 L 7 2 4F A6WE 2001050100085 20010501 00085 WP 2001 5 1 MWEA010592 1 20010417 A 5720 9911486506 FITTING DOUG DC9 DC932 3022066 WP RT WING GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND DEEP GOUGES ON FITTING AT STATION XRS 353 BETWEEN STRINGER 11 AND AFT SPAR RIGHT WING. REMOVED FITTING, FABRICATE D, DRILLED AND INSTALLED NEW FITTING. 2 L 7 2 4F A6WE 2001050100086 20010501 00086 WP 2001 5 1 MWEA010594 1 20010417 A 5711 9910010351 SPAR DOUG DC9 DC932 3022066 WP LT WING GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 REMOVED LEFT WING SPAR WEB AT TRUNNION AND FOUND GOUGES OUT OF LIMITS. FABRICATED, DRILLED AND INSTALLED NEW WEB SECTIO N. 2 L 7 2 4F A6WE 2001050100087 20010501 00087 WP 2001 5 1 MWEA010595 1 20010417 A 5310 591016380 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND CORROSION ON SKIN SPLICE DOUBLER AND FORWARD SIDE OF RIGHT LAV FLOORBEAM AT STATION 996. REMOVED SHEAR TIE, LOCAT ED, DRILLED, AND INSTALLED NEW SHEAR TIE. 2 L 7 2 4F A6WE 2001050100088 20010501 00088 WP 2001 5 1 MWEA010596 1 20010417 A 5321 995792117 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FLOORBOARD A-5 HAD AREAS OF CORROSION AROUND HOLES AND ON HAT CHANNELS. REMOVED FLOORBOARD, FABRICATED PANEL, HAT CHANN ELS, ASSEMBLED AND INSTALLED TOGETHER. 2 L 7 2 4F A6WE 2001050100089 20010501 00089 WP 2001 5 1 RRXA010032 1 20010411 A 2450 BUSS DOUG DC10 DC1010F 3022111 WP ACCESS BAY CONTAMINATED A RRXA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 WP 15 68047 47801 GEN-B OFF LIGHT CAME ON, AC LOAD ZERO ALT WITH AC BUS TIE 3 ISON LIGHT AND RT EMER PWR. NO CODE TO COVER PROBLEM. FOUN D MOISTURE ON DC POWER CENTER IN CACC. REMOVED MOISTURE AND RAN ALL 3 ENGINES IAW DC-10 ENGINE RUN HANDBOOK. NO FAULTS NOTED ON ELECTRICAL SYS TEST. 2 L 7 3 4F A22WE 2001050100090 20010501 00090 WP 2001 5 1 MWEA010597 1 20010417 A 5321 99579249 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FLOORBOARD E-9 HAD SEVERAL AREAS OF CORROSION AROUND FASTENER HOLES AND ON HAT CHANNELS. REMOVED FLOORBOARD, FABRICATED SKIN, REMOVED CORROSION FROM HAT CHANNELS, ASSEMBLED NEW SKIN AND CHANNELS. 2 L 7 2 4F A6WE 2001050100091 20010501 00091 WP 2001 5 1 MWEA010598 1 20010417 A 5321 995791819 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FLOORBOARD A-1 HAD SEVERAL FASTENERS PULLED THRU AND CORROSION; CHAFES AROUND HAT CHANNELS. REMOVED FLOORBOARD, FABRICA TED NEW FLOORBOARD, REMOVED CORROSION FROM HAT CHANNELS, FABRICATED ONE NEW HAT CHANNEL AND INSTALLED ALL. 2 L 7 2 4F A6WE 2001050100092 20010501 00092 WP 2001 5 1 MWEA010600 1 20010417 A 5320 992190419 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 INTERCOSTAL BETWEEN STATION 945 - 965 AT CENTERLINE OF AIRCRAFT BELOW SUPPORT IS CRACKED. REMOVED INTERCOSTAL, FABRICAT ED, DRILLED, AND INSTALLED NEW PART. 2 L 7 2 4F A6WE 2001050100093 20010501 00093 WP 2001 5 1 MWEA010601 1 20010417 A 5711 59911305503 SPAR DOUG DC9 DC932 3022066 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 RIGHT WING INTERNAL AFT LOWER SPAR TEE HAD HEAVY CORROSION. FABRICATED REPAIR FILLERS, INSTALLED IAW BOEING TELEX MWX-O RD-01-00272H, DATED 03 APRIL 2001. PLACED ON WATCH ITEM 5720 FOR FINAL DISPOSITION. 2 L 7 2 4F A6WE 2001050100094 20010501 00094 WP 2001 5 1 MWEA010602 1 20010417 A 5320 991554027 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 INTERCOSTAL AT STATION 1018 AND RBL 15 TO 25 CORRODED AND CRACKED. REMOVED AND REPLACED INTERCOSTAL. 2 L 7 2 4F A6WE 2001050100095 20010501 00095 WP 2001 5 1 MWEA010603 1 20010417 A 5320 99579081 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 INTERCOSTAL AT STATION 390 LONGERON 27 RIGHT - 29 RIGHT HAS ELONGATED HOLES AND IS BENT. FABRICATED AND INSTALLED INTER COSTAL AND INBOARD AND OUTBOARD TEE CLIPS. 2 L 7 2 4F A6WE 2001050100096 20010501 00096 WP 2001 5 1 MWEA010604 1 20010417 A 5321 991559713 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FLOORBOARD A-4 HAS SEVERAL AREAS OF CORROSION ON TOP SURFACE AND CORROSION AROUND SOME OF THE FASTENER HOLES AND BOTTOM HAT CHANNELS HAVE MINOR CHAFES AND CORROSION. REMOVED CORROSION AND CHAFING. REPAIRED FLOOR PANEL IAW DC9 SRM 51-30-2 AND DRW 9915597 & SRM 53-05 FIG 1. 2 L 7 2 4F A6WE 2001050100097 20010501 00097 WP 2001 5 1 MWEA010605 1 20010417 A 5321 995791821 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FLOORBOARD A-6 HAS SEVERAL AREAS OF CORROSION ON TOP SURFACE AND CORROSION AROUND SOME OF THE FASTENER HOLES AND BOTTOM HAT CHANNELS HAVE MINOR CHAFES AND CORROSION. FABRICATED AND INSTALLED FLOORBOARD SKIN AND HAT CHANNELS. 2 L 7 2 4F A6WE 2001050100098 20010501 00098 WP 2001 5 1 MWEA010607 1 20010416 A 3260 833703 SENSOR DOUG DC9 DC981 3022081 WP NLG OUT OF RIG A MWEA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 GL 31 810ME 48072 ON GEAR RETRACTION NOSE GEAR UNSAFE LIGHT CAME ON WITH A VIBRATION. AIRCRAFT RETURNED AND LANDED OVERWEIGHT. OVERWEIGH T LANDING INSPECTION COMPLIED WITH. NO DEFECTS NOTED. NOSE LANDING GEAR DOWNLOCK TARGET AND UPLOCK PROXIMITY SENSOR RI GGED OUT OF TOLERANCE. RIG TO WITHIN LIMITS. 2 L 7 2 4F A6WE 2001050100099 20010501 00099 EU 2001 5 1 20010423CW001 1 20010322 A 6120 FE1595413C GEAR AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE HAMSTD 14SF 14SF5 NE PROP BRAKE FAILED B QM7R K NONE O OTHER IN INSP/MAINT 1 EA 07 315CR 1999 252 121062 910340 THE BEARING FAILED ON THE PROP BRAKE SPLINE SHAFT CAUSING THE RETAINING RING TO DISENGAGE FROM ITS SLOT. THE CONFIGURAT ION OF THE PROP BRAKE HOUSING KEPT THE SPLINE FROM DISENGAGING WITH THE REDUCTION GEARBOX BUT DID ALLOW AN EXCESSIVE AMO UNT OF OIL BLOW BY. THIS FAULT HAD NO NOTICEABLE EFFECT DURING FLIGHT AND WAS ONLY IDENTIFIED AFTER MAINTENANCE ACTION TO FIX THE OIL LEAK. THE PROP BRAKE WAS 501 HOURS FROM OVERHAUL LIMITS. 2 H 7 2 4T 4 T RT A53EU E20NE 6 C P7NE 2001050100100 20010501 00100 WP 2001 5 1 20010423CW002 1 20010329 A 7921 16498 OIL COOLER DOUG DC3 DC3C 3021457 WP PWA R1830 R1830* 52020 NE RT ENGINE FAILED E VLLA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 05 932H 231 34368 SHORTLY AFTER DEPARTURE, STARTED TO LOOSE OIL PRESSURE ON RIGHT ENGINE. SHUT DOWN ENGINE AND RETURNED TO AIRPORT. SUS PECT HIGH PRESSURE, COLD OIL MAY HAVE CAUSED FAILURE OF THE COOLER. 2 L 7 2 4R 4 R A669 5E4 2001050100101 20010501 00101 NM 2001 5 1 ABXA010167 1 20010214 A 5311 FRAME BOEING 767 767205 1385121 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 713AX 60042 23058 CORROSION WAS FOUND ON THE FWD PIT FRAME AT BS 764, LBL 8. MAINTENANCE INSPECTED AND REPAIRED THE FRAME IAW B767 SRM 53 -00-07 AND 51-20-01. 2 L 7 2 4F RT A1NM 2001050100102 20010501 00102 NM 2001 5 1 ABXA010166 1 20010214 A 5313 143T300176 STRINGER BOEING 767 767205 1385121 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 713AX 60042 23058 CORROSION WAS FOUND ON STRINGER 39R AT THE AFT END BETWEEN BS 456 AND 478. MAINTENANCE INSPECTED AND REPLACED THE STRIN GER IAW BOEING DRAWING 143T3220 AND B767 SRM. 2 L 7 2 4F RT A1NM 2001050100103 20010501 00103 NM 2001 5 1 ABXA010165 1 20010206 A 5313 146T3003 STRINGER BOEING 767 767205 1385121 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 713AX 60042 23058 CORROSION WAS FOUND ON STRINGER 35L AT THE AFT BULK PIT BS 1461-1480 FRAME 636. MAINTENANCE INSPECTED AND REPLACED THE STRINGER IAW B767 SRM. 2 L 7 2 4F RT A1NM 2001050100104 20010501 00104 NM 2001 5 1 ABXA010164 1 20010126 A 5313 1498205 STRINGER BOEING 767 767205 1385121 NM FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 713AX 60042 23058 STRINGER 19 WAS FOUND TO BE CRACKED AT STA 390L FRAME 481. MAINTENANCE INSPECTED AND REPLACED THE STRINGER IAW B767 SRM . 2 L 7 2 4F RT A1NM 2001050100105 20010501 00105 NM 2001 5 1 ABXA010163 1 20010122 A 5313 STRINGER BOEING 767 767205 1385121 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 713AX 60042 23058 STRINGER 39R AT BS 1373 IN AFT LOWER CARGO AREA FRAME 400 WAS FOUND TO BE CORRODED. MAINTENANCE INSPECTED AND REPLACED THE STRINGER IAW B767 SRM. 2 L 7 2 4F RT A1NM 2001050100106 20010501 00106 NM 2001 5 1 20010423CW003 1 20010326 A 7430 IGNITION SWITCH DOUG MD11 MD11 3023602 NM GE CF6 CF680C2D1F 30025 NE NR 2 ENGINE FAILED A A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 03 105EV 48544 PILOT REPORTED NR 2 ENGINE, LOW RPM WARNING APPEARED, LEVEL 2 WITH N 1 25 PER CENT, EGT, 100 THEN WENT TO 0. NR 2 , 40 PER CENT, OIL QTY 20, RECOVERED AFTER IGN OVRD SELECTED DURING STARTED DESCENT. MAINTENANCE RAN NR 2 ENGINE WIT H BOTH A AND B IGNITION SYSTEM. NO FAULT NOTED, NO FAULT LOGED IN CFDS. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 3 4F 4 F RT A22WE E31N3 2001050100107 20010501 00107 WP 2001 5 1 ZW0A0100205 1 20010405 A 5320 STRUCTURE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT FOUND IN CABIN, CORROSION AROUND RIVETS AT BL 0, FROM STA 160 THRU 200. REMOVED CORROSION PER SPM 6-80-01. REPLACED FASTENERS PER SRM 51-30-02. PAINTED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001050100108 20010501 00108 NE 2001 5 1 20010419CW002 2 20010416 A 8500 R20007M2 ENGINE DHAV DHC7 DHC7* EA PWA R2000 R2000* 52023 NE HAMSTD 43D 43D50 NE NR 1 FAILED D G2OC E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 AL 05 2225C 639754 P108448 AFTER DEPARTURE, AT CLIMB POWER, THE NR 1 THRUST METER BEGAN A REDUCTION FOLLOWED BY A DROP IN OIL PRESSURE AND AN INCRE ASE IN OIL TEMPERATURE. THE CAPTAIN SHUT DOWN AND SECURED THE NR 1 ENGINE. THE AIRCRAFT CREW DECLARED AN EMERGENCY. THE AIRCRAFT RETURNED TO AIRPORT AND LANDED WITHOUT FURTHER INCIDENT. UPON INSPECTION BY MAINTENANCE, THE PROP WAS DI FFICULT TO ROTATE AND A CONSIDERABLE AMOUNT OF METAL WAS FOUND IN THE OIL SUMP. THE ENGINE WILL BE REPLACED DUE TO INTE RNAL FAILURE. A TEAR DOWN REPORT WILL BE COMPLETED BY OVERHAUL FACILITY. 2 H 7 4 4T 4 R RT A20EA 5E5 6 C P8879 2001050100110 20010501 00110 EU 2001 5 1 RAIA00104015 1 20010418 A 2422 PC125123B INVERTER JETAIR JETSTM JETSTM4101 1500501 EU NR 1 FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 562HK 12082 11116 41078 5355-ROC- DURING TAXI NR 1 INVERTER FAILED. MAINTENANCE REMOVED AND REPLACED NR 1 INVERTER IAW J41 MAINTENANCE MANUAL. 2 L 7 2 4T RT A41NM 2001050100111 20010501 00111 NM 2001 5 1 ABXA010153 1 20010417 A 2910 27271200101 HYDRAULIC LINE BOEING 767 767281 1385109 NM HYDRAULIC SYS BROKEN A ABXA O OTHER J K WARNING INDICATION FLUID LOSS AP APPROACH 1 GL 23 786AX 37543 23019 THE RIGHT HYDRAULIC QUANTITY WAS NOTED TO HAVE DECREASED TO 0.14. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT FUR THER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE HYDRAULIC PRESSURE LINE TO THE LEFT OUTBOARD AILERON ACTUATOR IAW 767 MM 27-11-73. 2 L 7 2 4F RT A1NM 2001050100112 20010501 00112 WP 2001 5 1 ABXA010154 1 20010417 A 3260 H1410051 DOWNLOCK SWITCH DOUG DC9 DC941 302207N WP RT MLG STUCK A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 971AX 57243 47497 DURING CLIMBOUT A RED GEAR UNSAFE LIGHT ILLUMINATED FOR THE RIGHT MAIN LANDING GEAR. THE CREW COMPLIED WITH THE ABNORMA L CHECKLIST AND CONTINUED OPERATIONS. MAINTENANCE INSPECTED AND FOUND THE RIGHT MAIN LANDING GEAR DOWNLOCK SWITCH TO BE STICKING. MAINTENANCE REPLACED THE SWITCH IAW DC-9 MM 32-60-80. 2 L 7 2 4F A6WE 2001050100113 20010501 00113 WP 2001 5 1 CALA0100385 1 20010417 A 5320 STRAP DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND AFT CARGO COMPARTMENT LOWER TORQUE BOX REPAIR STRAP CORRODED AT FS 1155-1212, LONGERON 28R. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-30-05, 51-10-3, AND ECRA 5310-03027. 2 L 7 2 4F A6WE 2001050100114 20010501 00114 WP 2001 5 1 CALA0100386 1 20010417 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND THE THIRD I/B FROM LEFT SEAT TRACK CORRODED AT FS 1098 - 1309, LBL 22. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-5, 51-30-01, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 2001050100115 20010501 00115 NM 2001 5 1 CALA0100391 1 20010418 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND INTERCOSTAL CRACKED AT LOWER AFT CORNER OF AFT CARGO DOOR CUTOUT. A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001050100116 20010501 00116 WP 2001 5 1 CALA0100392 1 20010418 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND INTERCOSTAL CORRODED AT LOWER FLANGE IN FORWARD CARGO AREA AT FS 427-466, LONGERON 29R. THE INTERCOSTA L WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-5. 2 L 7 2 4F A6WE 2001050100117 20010501 00117 NM 2001 5 1 CALA0100393 1 20010418 A 5320 WEB BOEING 737 7373T0 1384582 NM CARGO BAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND AFT BAGGAGE BIN THRESHOLD WEB CORRODED ON UPPER SURFACE. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-1 0-02. 2 L 7 2 4F RT A16WE 2001050100118 20010501 00118 NM 2001 5 1 CALA0100394 1 20010418 A 5320 STRAP BOEING 737 7373T0 1384582 NM CARGO BAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND CORROSION IN LOWER STRAP DOUBLER FORWARD LOWER CORNER CARGO DOOR CUTOUT AT THRESHOLD PLATE AFT CARGO. THE STRAP DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001050100119 20010501 00119 NM 2001 5 1 CALA0100395 1 20010418 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND INTERCOSTAL CORRODED AT STA 747 - 767, RT SIDE. REPLACED INTERCOSTAL IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001050100120 20010501 00120 NM 2001 5 1 CALA0100387 1 20010417 A 5345 MOUNT BRACKET BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND AFT LEFT LAV FLOOR MOUNT BRACKET CORRODED AT STA 1016, LBL 6. THE FLOOR MOUNT BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001050100121 20010501 00121 NM 2001 5 1 CALA0100388 1 20010417 A 5320 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND AFT BAGGAGE BIN RT SUPPORT Z-ANGLE CORRODED AT STA 727 - 767. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001050100122 20010501 00122 WP 2001 5 1 CALA0100389 1 20010417 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND SECOND I/B FROM LEFT SEAT TRACK CORRODED AT FS 1079 - 1309, LBL 44. THE SEAT TRACK WAS REMOVED AND A N EW TRACK WAS INSTALLED IAW SRM 51-30-1, 51-30-2, 51-10-3, AND 51-30-5. 2 L 7 2 4F A6WE 2001050100124 20010501 00124 NM 2001 5 1 CALA0100396 1 20010418 A 5320 CHANNEL BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND SUPPORT CHANNEL CORRODED AT STA 727A - 727B. THE CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001050100125 20010501 00125 NM 2001 5 1 CALA0100397 1 20010418 A 2612 G718505 WARN PANEL BOEING 737 7373T0 1384582 NM COCKPIT FAULTY A CALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 09 10323 4141 23374 THE CARGO FIRE LIGHT ILLUMINATED WHILE EN ROUTE FROM IAH TO YYZ. NO BELL SOUNDED. THE CARGO FIRE SYSTEM TESTED NORMALL Y, BUT THE LIGHT REMAINED ON AFTER TEST. RESET ALL CIRCUIT BREAKERS FOR CARGO FIRE SYSTEM, BUT THE FIRE LIGHT WOULD NOT GO OUT. THE AIRCARFT WAS DIVERTED TO SDF WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. TH E COCKPIT FIRE SUPRESSION SYSTEM PANEL WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW MM 26-16-10, PAGE 209. 2 L 7 2 4F RT A16WE 2001050100126 20010501 00126 NM 2001 5 1 ABXA010162 1 20010119 A 5315 FLOORBEAM BOEING 767 767205 1385121 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 713AX 60042 23058 CORROSION WAS FOUND ON FLOORBEAM CAP AT STATION 303 RBL 63. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW BOEING DRAW ING 141T5112 AND B767 SRM. 2 L 7 2 4F RT A1NM 2001050100127 20010501 00127 NM 2001 5 1 ABXA010161 1 20010117 A 5315 FLOORBEAM BOEING 767 767205 1385121 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 713AX 60042 23058 CORROSION WAS FOUND ON TOP LEG OF FLOOR BEAM FRAME 207, STATION 1518 LBL 25. MAINTENANCE INSPECTED AND REPAIRED THE ARE A IAW ABX REA B653-39290-MR. 2 L 7 2 4F RT A1NM 2001050100128 20010501 00128 NM 2001 5 1 ABXA010160 1 20010113 A 5320 140T011516 SPLICE BOEING 767 767205 1385121 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 713AX 60042 23058 STRINGER SPLICE FITTING 25R AT STATION 434 FRAME 111 WAS FOUND TO BE CORRODED. MAINTENANCE INSPECTED AND REPLACED THE F ITTING IAW B767 SRM. 2 L 7 2 4F RT A1NM 2001050100129 20010501 00129 NM 2001 5 1 ABXA010159 1 20010113 A 5320 140T011516 SPLICE BOEING 767 767205 1385121 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 713AX 60042 23058 STRINGER SPLICE FITTING 31L STATION 434, FRAME 110 WAS FOUND TO BE CORRODED. MAINTENANCE INSPECTED AND REPLACED THE FIT TING IAW BOEING DRAWING 140T115 AND B767 SRM. 2 L 7 2 4F RT A1NM 2001050100130 20010501 00130 NM 2001 5 1 ABXA010158 1 20010111 A 5315 FLOORBEAM BOEING 767 767205 1385121 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 713AX 60042 23058 CORROSION WAS FOUND ON THE TOP OF FLOORBEAM CAP AT FRAME 087, STA 287, LBL 0 THROUGH LBL 20. MAINTENANCE INSPECTED AND REPLACED THE CAP IAW BOEING DRAWING 141T5111 AND B767 SRM. 2 L 7 2 4F RT A1NM 2001050100131 20010501 00131 EU 2001 5 1 GXPA0105 1 20010301 A 3260 CONNECTOR AMD FALC20 FALCON 2720302 EU GE CF700 CF700* 30010 NE MLG DOOR DIRTY E GXPA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 25 613GA 77 AIRCRAFT RETURNED TO AIRPORT DUE TO GEAR DOORS WOULD NOT CLOSE AFTER TAKE OFF. CORRECTIVE ACTION: CLEANED ALL LANDING GEAR SWITCH PLUGS AND PERFORMED RETRACTION TEST NUMEROUS TIMES. 2 L 7 2 4F 4 F A7EU E7EA 2001050100132 20010501 00132 NM 2001 5 1 ABXA010157 1 20010111 A 5315 141T511145 FLOORBEAM BOEING 767 767205 1385121 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 713AX 60042 23058 CORROSION WAS FOUND ON BEAM CAP AT STATION 287 BL 0- RBL 70. MAINTENANCE REPLACED THE CAP IAW B767 SRM. 2 L 7 2 4F RT A1NM 2001050100133 20010501 00133 WP 2001 5 1 UPS01835655 1 20010421 A 2611 SMOKE DETECTOR DOUG DC8 DC871F 302199D WP CARGO BAY FALSE INDICATION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 SMOKE DETECTOR INOP. DEF M213526 M213526 4/20 PIT 33 SMOKE DETECTOR 2ND FROM FRONT S/N 6631 FALSE WARNING REPLACED S MOKE DETER S/N OFF 6631 ON 3094 REPLACED CM, PRECAUTIONALY OPS. CHECK O.K. 2 L 7 4 4F RT 4A25 2001050100134 20010501 00134 EU 2001 5 1 C2XA01BT062 1 20010413 A 2612 FIRE WARNING AEROSP ATR42 ATR42320 8680930 EU COCKPIT FALSE INDICATION A C2XA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 27 34817 152 EWR CO2996, CREW REPORTED NR 1 ENGINE FIRE INDICATION DURING TAXI. NO FIRE, RETURNED TO THE GATE. MAINTENANCE INSPECTE D AIRCRAFT PERFORMED DETAIL VISUAL INSPECTION FOUND NO EVIDENCE OF FIRE. PERFORMED ENGINE RUN ON NR 1 ENGINE FOR 15 MIN UTES. NO FAULT FOUND IAW ATR42 MM 72-00-00. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001050100135 20010501 00135 CE 2001 5 1 C2XA01CL078 1 20010410 A 6123 5038912129 SWITCH BEECH 1900 1900D 1154162 CE RT ENGINE MALFUNCTIONED A C2XA K NONE O OTHER AP APPROACH 1 SW 27 87555 UE234 CLE FLIGHT 3190 THE CREW REPORTED THAT ON APPROACH THE RIGHT PROP CYCLED IN AND OUT OF FEATHER. THE TORQUE GAUGE CYCLED UP AND DOWN APPROXIMITY 800 LBS. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND THE NR 2 ENGINE AUTOFEATHER LOW PRESSURE SWITCH TRIPS HIGH. THE SWITCH WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. THE AI RCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT A24CE 2001050100136 20010501 00136 CE 2001 5 1 C2XA01CL080 1 20010414 A 6123 MS252531 SWITCH BEECH 1900 1900D 1154162 CE COCKPIT FAILED A C2XA K NONE L NO TEST CR CRUISE 1 SW 27 81556 UE239 CLE FLIGHT 3197 THE CREW REPORTED THE LEFT AUTOFEATHER DOES NOT ARM WHILE INFLIGHT. MAINTENANCE REPLACED THE LEFT ENGIN E POWER LEVER SWITCH. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT A24CE 2001050100137 20010501 00137 SO 2001 5 1 C2XA01CL079 1 20010412 A 3350 20131A BATTERY PACK EMB 145 EMB145LR SO CABIN DISCHARGED A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 13968 6607 53 145138 SDF FLIGHT 4077 THE CREW REPORTED THE LAST THREE ROWS OF EMERGENCY FLOOR AISLE PATH LIGHTING WAS INOPERATIVE. MAINTENAN CE REPLACED THE NR 3 EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE . 2 L 7 2 4T RT T00011AT 2001050100138 20010501 00138 CE 2001 5 1 20010413CW001 1 20010228 A 2431 019504000 SENSOR CESSNA 650 650 2076802 CE GARRTT TFE731 TFE731* 01518 WP BATTERY DEFECTIVE B JGVR K NONE O OTHER IN INSP/MAINT 1 CE 09 790QS 6507090 TEMPERATURE SENSOR CONNECTOR PINS FOUND TO BE RECESSED EXCESSIVELY. DEFECT FOUND DURING INSPECTION OF BATTERY. THIS C ONDITION PROVIDES ONLY MINIMAL CONTACT BETWEEN MATING PINS. 2 L 7 2 4F 4 F A9NM E6WE 2001050100139 20010501 00139 SO 2001 5 1 GLBA2001083 1 20010415 A 8010 32540 RELAY EMB 120 EMB120ER 3260203 SO COCKPIT SHORTED A GLBA K NONE O OTHER IN INSP/MAINT 1 CE 01 297UX 120297 SPARKS FROM RT SIDE START CONTACT PANEL DURING NR 2 ENGINE START/INSP. FOUND START CONTACT RELAY SHORTED. REPLACED REL AY, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A31SO 2001050100140 20010501 00140 NM 2001 5 1 QXEA0100444 1 20010416 A 2612 FIRE LOOP DHAV DHC8 DHC8202 2809007 NM FIRE DETECTION FAULTY A QXEA K NONE N FALSE WARNING CL CLIMB 1 NM 09 359PH 514 SEA - FLIGHT CREW REPORTED A MASTER FIRE WARNING INDICATION IN CONJUNCTION WITH A B-LOOP DETECTOR FAULT DURING CLIMBOUT . INDICATION LASTED 20 SECONDS. INSPECTED ENGINE AREA, NO DEFECTS NOTED. PLACED B-LOOP DETECTION CIRCUIT ON DEFERRED MAINTENANCE LIST. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001050100141 20010501 00141 EU 2001 5 1 QXEA0100445 1 20010415 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 477AU 11226 SEA - UPON INSPECTION, FOUND OVERWING EXIT SIGN TO HAVE INOPERATIVE LAMPS. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001050100142 20010501 00142 EU 2001 5 1 QXEA0100446 1 20010415 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 483US 11233 BOI - FORWARD EXIT SIGN FOUND TO HAVE INOPERATIVE LAMPS. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIR CRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001050100144 20010501 00144 WP 2001 5 1 27314101 2 20010309 A 7261 30607016 PUMP ISRAEL 1125 ASTRASPX 4500205 EU GARRTT TFE731 TFE731* 01518 WP LT ENGINE LEAKING A QRRR K NONE K FLUID LOSS IN INSP/MAINT 1 EA 13 273RA 1240 097 113143 OIL PUMP LEAKING THRU CASE DUE TO WORMING. REMOVED AND REPLACED PUMP. 2 L 7 2 4F 4 F RT A16NM E6WE 2001050100145 20010501 00145 EU 2001 5 1 QXEA0100447 1 20010415 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 494US 11167 SEA - THE FORWARD EXIT SIGN WAS REPORTED TO BE PARTIALLY INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHEC KS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001050100146 20010501 00146 EU 2001 5 1 QXEA0100448 1 20010413 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 496US 11169 GEG - EMERGENCY EXIT SIGN ABOVE FLIGHT COMPARTMENT DOOR INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECK S GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001050100147 20010501 00147 NM 2001 5 1 01FDEA00279 1 20010416 A 5330 65458310 SKIN BOEING 727 7272S2F 1384O81 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 215FE 22936 DENT IN FUSELAGE SKIN AT BS 1040, STR 15R. *S/D* FOUND DENT IN SKIN OUT OF LIMITS PER IAW FEDEX SRM 53-30-1. REPAIRED SKIN PER FEDEX SRM 53-30-3 FIG 3. 2 L 7 3 4F A3WE 2001050100148 20010501 00148 NM 2001 5 1 01FDEA00280 1 20010416 A 5330 6554579 SKIN BOEING 727 7272S2F 1384O81 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 215FE 22936 DENT IN FUSELAGE SKIN, BS 1040 BETWEEN STR 4L AND STR 15L. *S/D* REMOVED AND REPLACED SKIN PER IAW FEDEX EA 7-5330-572 14 & FEDEX SRM 53-30-3 FIG 24. 2 L 7 3 4F A3WE 2001050100149 20010501 00149 EU 2001 5 1 01FDEA00281 1 20010415 A 3234 SELECTOR VALVE AIRBUS 300 A300F4605R 3930327 EU COCKPIT MALFUNCTIONED A FDEA L ABORTED APPROACH O OTHER AP APPROACH 1 SO 25 656FE 745 LANDING GEAR WOULLD NOT EXTEND NORM ON APPR TO EWR. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE 3GA PRE AMM 32-31- 12. JACKED AC AND CYCLED LANDING GEAR SEVERAL TIMES. CK BOTH SYS 1 & 2 WITH NO DISCREP NOTED. 2 L 7 2 4F RT A35EU 2001050100150 20010501 00150 WP 2001 5 1 27314102 2 20010309 A 7261 3060701 PUMP ISRAEL 1125 ASTRASPX 4500205 EU GARRTT TFE731 TFE731* 01518 WP RT ENGINE LEAKING B QRRR K NONE K FLUID LOSS IN INSP/MAINT 1 EA 13 273RA 1410 097 OIL PUMP LEAKING THRU CASE DUE TO WORMING. REMOVED AND REPLACED OIL PUMP. 2 L 7 2 4F 4 F RT A16NM E6WE 2001050100151 20010501 00151 NM 2001 5 1 01FDEA00282 1 20010417 A 2130 VALVE BOEING 727 727227 1384078 NM A/C BAY FAILED A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 479FE 21461 LEFT PACK INOP. CARGO HEAT OUTFLOW VALVE CLOSED. AC UNABLE TO MAINTAIN PRESS. REMOVED AND REPLACED LEFT PACK VALVE. OPS CHECK NORM OF BOTH LEFT AND RIGHT PACK PRESS AC NORMAL. REMOVED PLACARD TO THE LEFT PACK. 2 L 7 3 4F A3WE 2001050100152 20010501 00152 NM 2001 5 1 01FDEA00284 1 20010418 A 2612 FIRE WARNING BOEING 727 72722 1384002 NM COCKPIT FALSE ACTIVATION A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 149FE 19087 FIRE WARNING BELL CAME ON IMMED AFT T/O. ENG FIRE AND WHEEL WELL FIRE SYS TEST NORMAL. APU FIRE SYS DID NOT. INSP APU FIRE SYS AND APU. FOUND SYS TO TEST NORM AND NO PROBLEMS IN THE APU AREA. TEST APU SEVERAL TIMES AND SYS CK GOOD. OK FOR SERVICE. ALL ENG TEST GOOD. 2 L 7 3 4F A3WE 2001050100153 20010501 00153 SO 2001 5 1 C2XA01CL081 1 20010417 A 3231 22250100003 SOLENOID VALVE EMB 135 EMB135ER 3260203 SO NLG FAILED A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 16501 145145 CLE FLIGHT 3960 AFTER LANDING GEAR RETRACTION CREW REPORTED LOUD AIR NOISE COMING FROM NOSE LANDING GEAR AREA. NOISE INCREASED WITH AIRSPEED. AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITH OUT FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR DOOR SOLENOID VALVE. PERFORMED OPERATIONAL CHECKS AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2001050100154 20010501 00154 EU 2001 5 1 RAIA00104013 1 20010412 A 2612 51228318 FIRE LOOP JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE CHAFED A RAIA F ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 CE 03 563HK 41079 5404-EWR-DURING CLIMB LEFT HAND FIRE INDICATION AT 2000 FEET, FIRE BOTTLE WAS BLOWN AND WARNING LIGHT WENT OUT. MAINTEN ANCE REMOVED AND REPLACED THE LEFT HAND FIRE BOTTLE, BOTH SQUIBS AND THE LEFT HAND ENGINE FIRE LOOP IAW J41 MAINTENANCE MANUAL. 2 L 7 2 4T RT A41NM 2001050100155 20010501 00155 EU 2001 5 1 JBXA00267 1 20010418 A 2131 CONTROLLER FOKKER F28 F28MK0100 4990807 EU CABIN PRESSURE MALFUNCTIONED A JBXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 05 110ML 11486 CABIN WILL NOT PRESSURIZE AFTER TAKEOFF. COULD NOT CONTROL MANUALLY. PULLED AND RESET C/B FOR CABIN PRESSURE CONTROLLE R. PERFORMED OPERATIONAL CHECK OF CABIN PRESSURE CONTROLLER IAW F-100 AMM 21-31-02. ALL OPERATIONAL CHECKS GOOD AT THI S TIME. 2 L 7 2 4F RT 2001050100157 20010501 00157 NM 2001 5 1 PCAA0104028 1 20010412 A 2720 82760050005 SPRING DHAV DHC8 DHC8102 2809003 NM RUDDER BROKEN A PCAA K NONE O OTHER NR NOT REPORTED 1 EA 13 EICHP 258 PHL-FLIGHT 3812 CREW REPORTED LEFT RUDDER PEDALS HAVE VERY LITTLE SPRING TENSION. MANTENANCE REPLACED AFT RUDDER FEEL SPRING IN ACCORDANCE WITH ALERT SERVICE BULLETN A8-27-82 AND DASH 8 MAINT MANUAL 27-20-01 OPERATIONAL AND VISUAL CHECK G OOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001050100158 20010501 00158 NM 2001 5 1 PCAA0104029 1 20010416 A 3097 WIRE DHAV DHC8 DHC8102 2809003 NM NR 2 BRUSH BLK DAMAGED A PCAA K NONE N FALSE WARNING CL CLIMB 1 EA 13 830EX 155 PIT-FLIGHT 3942 CREW REPORTED THE EMERGENCY FLOOR LIGHTS FLICKER DURING CLIMBOUT IN CONJUNCTION WITH NR 2 PROP, BLADES 1 AND 3 ANTI-ICE LIGHT ILLUMINATION. MAINTENANCE FOUND AND REPAIRED BARE WIRE ON NR 2 BRUSH BLOCK WIRE HARNESS. ALSO FO UND AND REPAIRED DAMAGED WIRE ON FLIGHT ATTENDANTS CONTROL PANEL FOR EMERGENCY LIGHT SWITCH. RAN AIRCRAFT, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001050100159 20010501 00159 EU 2001 5 1 RAIA00104014 1 20010417 A 3240 JS308 ARM JETAIR JETSTM JETSTM4101 1500501 EU PARKING BRAKE BROKEN A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 564HK 41081 5364-RIC- DURING TAXI TAKEOFF CONFIG WARNING LIGHT LIGHT ILLUMINATED. MAINTENANCE FOUND DEFECTIVE ROCKER ARM BROKEN AT PARKING BRAKE HANDLE. MAINTENANCE REMOVED AND REPLACED THE ARM IAW J41 MAINTENANCE MANUAL. 2 L 7 2 4T RT A41NM 2001050100160 20010501 00160 2001 5 1 20010413CW008 4 20010320 A 2210 CONTROL PANEL CESSNA 560 560XL CE PWA 545 PW545A NE AUTO PILOT CONTAMINATED B K NONE O OTHER IN INSP/MAINT 1 SW 99 83SD 235 5605091 AFTER SITTING IN RAIN, ON DEPARTURE, AIRCRAFT CLIMBED TO 38,000 FT. AFTER APPROX 10 MIN THE AUTO PILOT KICKED OUT. PIL OT REPORTED CONTROLS FELT STUCK. PILOT APPLIED PRESSURE TO CONTROLS AND THEY BECAME UNSTUCK AND OPERATED OK. LANDED OK . MAINTENANCE REMOVED AC PANEL AND HAD ABOUT GAL OF WATER DRAIN OUT. THE RIB AT APPROX STA 449.00 DOES NOT HAVE DRAIN HOLE AT BOTTOM TO ALLOW WATER TO FLOW FWD TO FUSELAGE DRAIN PORTS. CONTROL CABLE PULLEYS WERE SETTING IN WATER. BELIEV E WATER FROZE CAUSED CONTROL PROBLEM. ORDER WAS ISSUED TO DRILL HOLE IN RIB SO ANY WATER IN AREA WOULD DRAIN FORWARD TO FUSELAGE DRAIN PORTS. 2 L 7 2 4F 4 F RT A22CE E00059EN 2001050100161 20010501 00161 SO 2001 5 1 SWIA972509 1 20010416 A 5751 FAIRING EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE AILERON DEPARTED A SWIA K NONE D E INFLIGHT SEPARATION VIBRATION/BUFFET CR CRUISE 1 NM 07 237SW 120314 IN FLIGHT, FELT STRANGE VIBRATION FOR A FEW SECONDS. UPON CONDUCTING POST FLIGHT INSPECTION, FOUND A SECTION OF UPPER A ILERON FAIRING MISSING. REMOVED DAMAGED LEFT AILERON UPPER FAIRING AND REPLACED WITH SERVICEABLE UNIT. 2 L 7 2 4T 4 T RT A31SO E20NE 2001050100162 20010501 00162 SO 2001 5 1 LR7A01009 1 20010416 A 5320 3375082 FITTING LKHEED 382 382G 526414U SO FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2324 4606 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC05297 FOUND FS 737E - 745E INTERCOSTAL FITTING CORRODED AT WL 143, LBL 60. REPLACED FITTING IAW SMP 581-53-40 PG 10. 2 H 7 4 4T A1SO 2001050100163 20010501 00163 SO 2001 5 1 LR7A01015 1 20010416 A 5330 SKIN LKHEED 382 382G 526414U SO FUSELAGE DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2324 4606 DURING SCHEDULED C3 INSPECTION CARRY OVER ITEM 00679 DUE, REF ED 00-0022-2. FUSELAGE RT SIDE SKIN DENTED FS 812E/WL 152 AND FS 812E/WL 164. REPAIRED IAW SRM SMP 583-51-140-11. 2 H 7 4 4T A1SO 2001050100164 20010501 00164 SO 2001 5 1 LR7A01023 1 20010416 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2324 4606 DURING SCHEDULED C3 INSPECTION PER JOB CARD HSP53224 FOUND FS 497 OVERHEAD BULKHEAD WEB CRACKED AT WL 267, RBL 58. REPA IRED IAW SRM SMP 583-53-40-35A. 2 H 7 4 4T A1SO 2001050100165 20010501 00165 SO 2001 5 1 LR7A01026 1 20010416 A 5320 356182356122 FITTING LKHEED 382 382G 526414U SO FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2324 4606 DURING SCHEDULED C3 INSPECTION NR 2011 ACCOMPLISHMENT FOUND FS 737E AND 757E FLOORBEAM END FITTINGS CORRODED AT WL 146, LBL 61. REPLACED FITTINGS PER SRM SMP 583-51-10 PG 6. 2 H 7 4 4T A1SO 2001060600002 20010606 00002 EU 2001 6 6 01FDEA00286 1 20010504 A 7830 THRUST REVERSER AIRBUS 300 A300F4605R 3930327 EU NR 2 ENGINE MALFUNCTIONED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 675FE 789 ON T/O ROLL, ECAM WARN NR 2 ENGINE REVERSER PRESSURIZED, REJECT T/O. 2 L 7 2 4F RT A35EU 2001050100166 20010501 00166 WP 2001 5 1 MWEA010586 1 20010417 A 5320 S1416036S BRACKET DOUG DC9 DC932 3022066 WP CARGO BAY CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 AT FORWARD CARGO DOOR JAMB FOUND LIGHT CORROSION ON L-BRACKET, INSIDE BOX STRUCTURE. REMOVED BRACKET, DRILLED AND INSTA LLED NEW BRACKET. 2 L 7 2 4F A6WE 2001050100167 20010501 00167 WP 2001 5 1 MWEA010599 1 20010417 A 5313 591141277 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 LONGERON 28 RIGHT IS CORRODED FROM STATION 323 - 360. REMOVED DAMAGED SECTION, FABRICATED SECTION, REPAIR SPLICE, DRILL ED AND INSTALLED. 2 L 7 2 4F A6WE 2001050100168 20010501 00168 WP 2001 5 1 UPS01835751 1 20010405 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2 MAIN CABIN TRACK B ST 1450 TO 1470 CORRODED. CUT SEAT 1430 TO 1470 IAW DC8 EO 5320-8309 AND REPAIR IA W WITH SAME 2 L 7 4 4F RT 4A25 2001050100173 20010501 00173 NM 2001 5 1 EIA2001186 1 20010312 A 5210 FRAME BOEING 747 747273C 1384896 NM PAX DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 DURING BSB 53A2451, BS 800 LEFT DOOR EDGE FRAME FOUND CRACKED AT FORWARD FRAME INNER CHORD ANGLE AND FASTENER HOLE BETWE EN STRINGER 16L AND STRINGER 17L. TRIMMED OFF CRACKS ON BOTH ANGLE AND STRAP, OVERSIZED FASTENER HOLE, FREEZE PLUGGED, NDT INSPECTED, AND INSTALLED EXTERNAL REPAIR DDOUBLER AND INTERNAL STEEL STRAPS PER BOEING MSG AND RS R-53-22-34619. (M ) 2 L 7 4 4F A20WE 2001050100174 20010501 00174 NM 2001 5 1 EIA2001158 1 20010312 A 5711 SPAR BOEING 747 747273C 1384896 NM WING CENTER BOX CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 FOUND BS 1241 LEFT AND RIGHT WING CENTER SECTION REAR SPAR WEB AFT SURFACE AT BULKHEAD FTG AREA CORRODED AND BLENDOUT EX CEEDS SRM LIMITS. REMOVED CORROSION AND REPAIRED PER BSB 57-2263. SECTION OF PX WEB ANGLE TRIMMED FOR ACCESS, NEW SECT ION SPLICEDIN PER BOEING MSG AND RS R-57-12-34638. (M) 2 L 7 4 4F A20WE 2001050100175 20010501 00175 EU 2001 5 1 20010424CW011 1 20010326 A 6310 4639202011 CLUTCH BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE TRANSMISSION DAMAGED D O OTHER O OTHER NR NOT REPORTED 1 CE 03 440SL 3969 80 7158 PILOT STARTED NR 1 ENGINE, AND RAN UP TO GROUND IDLE. PILOT STARTED NR 2 ENGINE, AND RAN UP TO GROUND IDLE. PILOT FELT THUD AND HIGH FREQ VIBRATION IN THE AIRCRAFT. PILOT THEN SHUT BOTH ENGINES DOWN. THEN INSPECTED ENGINE COMPARTMENTS, AND FOUND NR 2 ENGINE TO TRANSMISSION DRIVE SHAFT TO BE BENT AND TWISTED. MAINTENANCE CONTACTED TECH SUPPORT. TECH SUP PORT FELT THAT THE CLUTCH DID NOT ENGAGE UNTIL NR 2 ENGINE WAS AT GROUND IDLE. TWISTING THE DRIVE SHAFT, WHEN IT DID EN GAGE. 1 G 7 2 3U 3 U H13EU E5NE10 2001050100176 20010501 00176 NM 2001 5 1 20010413CW012 1 20010326 A 2700 22277 CONTROL ROD AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE LT WING SEPARATED E VO2R K NONE O OTHER IN INSP/MAINT 1 GL 19 375SC 4716 023 METAL END OF CONTROL ROD IS SEPARATING FROM CARBON FIBER. A MOVEMENT OF .003 IN WAS OBSERVED DURING OPERATION OF SYSTE M DURING C INSPECTION PART SENT FOR EVALUATION. 2 K 7 3 4F 4 F RT A50NM E44NE 2001050100177 20010501 00177 NM 2001 5 1 01FDEA00271 1 20010413 A 2130 32167441 VALVE BOEING 727 727227 1384078 NM A/C BAY FAILED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 479FE 21461 ON CLIMBOUT WITH BOTH PACKS ON CABIN BEGAN TO CLIMB TO 10,000 FT. STARTED A DESCENT, A/C REMAIN UNPRESSURIED UNTIL LAND . *S/D* REMOVED AND REPLACED LT PACK VALVE. OPS CK OF BOTH PACK LT & RT PRESS. AC NORMAL ON GROUND AS PER MM. REMOV ED PLACARD. 2 L 7 3 4F A3WE 2001050100178 20010501 00178 SW 2001 5 1 20010426CW004 1 20010417 A 2150 412AC7007 CONDENSER BELL 412 412EP 1182205 SW PWA PT6 PT6* 52043 EA A/C BAY MISLOCATED D K NONE O OTHER IN INSP/MAINT 1 SW 99 911FR 36248 BELL PITCH CHANGE LINK ANTIROTATIONAL BRACKETS CAME IN CONTACT WITH AIRCONDITIONER CONDENSER DURING A NORMAL LANDING, RE SULTING IN BENT REPHAZING LEVERS (FLIGHT CONTROL). PROBABLE CAUSE: TRANSMISSION HAS A GREATER AMOUNT OF TRAVEL ON ITS PYLON MOUNTS, THAN THERE IS CLEARANCE BETWEEN ROTATING COMPONENTS AND FIXED CONDENSER. RECOMMENDATIONS: PROVIDE ENOUG H CLEARANCE TO CONDENSER, SO THAT TRANSMISSION MOVEMENT CAN NOT CAUSE CONTACT. 1 G 7 2 4U 3 T H4SW E2NE 2001050100179 20010501 00179 NM 2001 5 1 01FDEA00276 1 20010414 A 2120 CLAMP BOEING 727 727247 138408F NM NR 3 ENGINE LOOSE A FDEA O OTHER J WARNING INDICATION CR CRUISE 1 SO 25 233FE 21327 NR 3 ENGINE STRUT O/H LIGHT ILLUMINATED. RED TABS ACCOMPLISHED. FOUND AIR LEAK ON INBOARD HEAT EXCHANGER CLAMP. LOOSE NED ALL CLAMPS, TRYING TO PROPERLY SEAT INBD CLAMP. REMOVED INBD CLAMP PER STANDARD MAINT PRACT. REMOVED AND REPLACED SEALS AND DUCT ASSY PER STAND MAINT. NO LEAKS NOTED. OK FOR SERVICE. 2 L 7 3 4F A3WE 2001050100180 20010501 00180 NM 2001 5 1 ABXA010156 1 20010110 A 5315 14T3T10605 FLOORBEAM BOEING 767 767205 1385121 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 713AX 60042 23058 CORROSION WAS FOUND ON T-CAP AT STA 632, RBL 20. MAINTENANCE REPLACED THE T-CAP IAW B767 SRM. 2 L 7 2 4F RT A1NM 2001050100181 20010501 00181 NM 2001 5 1 ABXA010155 1 20010110 A 5315 143T10603 FLOORBEAM BOEING 767 767205 1385121 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 713AX 60042 23058 CORROSION WAS FOUND ON T-CAP AT STA 434 RBL 44. MAINTENANCE REPLACED THE T-CAP IAW B767 SRM. 2 L 7 2 4F RT A1NM 2001050100183 20010501 00183 NE 2001 5 1 20010416CW003 2 20010213 A 7414 DAM33200A MAGNETO DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE NR 4 ENGINE FAILED H B2OB K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 AL 01 44911 878 10461 P1041Y7 FOUND COIL BURNED OUT. BURNED ELECTRIC SMELL. 2 L 7 4 4R 4 R A762 5E5 2001050100184 20010501 00184 WP 2001 5 1 20010416CW004 1 20010216 A 6123 MOTOR DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE FEATHERING SYS WEAK H B2OB K NONE O OTHER IN INSP/MAINT 1 AL 01 44911 2500 10461 P175525 BENCHED GOOD, BUT WAS NOT STRONG ENOUGH WITH A LOAD. 2 L 7 4 4R 4 R A762 5E5 2001050100185 20010501 00185 NE 2001 5 1 20010416CW005 2 20010212 A 8530 446888 CYLINDER DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE NR 4 ENGINE WORN H B2OB K NONE O OTHER IN INSP/MAINT 1 AL 01 44911 875 10461 P104147 VALVE CHECK SHOWS EXCESS WOBBLE IN EX GUIDE. 2 L 7 4 4R 4 R A762 5E5 2001050100186 20010501 00186 NM 2001 5 1 UPS01435714 1 20010406 A 5311 FRAME BOEING 747 747SR46 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 CABIN - FRAME FOUND CRACKED AT STA 1416 BETWEEN STR 24L TO STR 25L. REPAIRED FRAME AS PER SRM 53-10-0 1 FIG 11. 2 L 7 4 4F A20WE 2001050100187 20010501 00187 NM 2001 5 1 UPS01435715 1 20010408 A 5315 FLOORBEAM BOEING 747 747SR46 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C3 UPPER DECK FLOOR BEAM UPPER CHORD AT BS 360 LBL 24-54 FOUND FOUR FLOORBEAM PANEL ATTACHMENT HOLES C RACKED AS MARKED. REPAIRED CRACKED HOLES PER SB 747-53A2431 FIG 9. THE REPETITIVE INSPECTION TO BE FOLLWED BY UPS & TO B E BODIED IN 3000 FLT CYCLES PER EO B747-5320-12407-B (CUSTOMER HAD BEEN INFORMED). 2 L 7 4 4F A20WE 2001050100188 20010501 00188 NM 2001 5 1 UPS01435716 1 20010408 A 5315 FLOORBEAM BOEING 747 747SR46 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 UPPER DECK FLOORBEAM UPPER CHORD AT BS 340 LBL 32 FOUND ONE EACH FLOOR PANEL ATTACHMENT HOLE CRACKED AS MARKED. REPAIRED CRACKED HOLES AS PER SB 747-53A2431 FIG 9. 2 L 7 4 4F A20WE 2001050100189 20010501 00189 NM 2001 5 1 UPS01435717 1 20010408 A 5315 FLOORBEAM BOEING 747 747SR46 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 UPPER DECK FLOORBEAM UPPER CHORD AT BS 380 RBL 32-36 FOUND PANEL ATTACHMENT HOLES CRACKED AS MARKED. REPAIRED FLOOR BEAM CRACKED HOLES AS PER SB 747-53A2431 FIG 9 . 2 L 7 4 4F A20WE 2001050100190 20010501 00190 NM 2001 5 1 UPS01435718 1 20010408 A 5315 FLOORBEAM BOEING 747 747SR46 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 UPPER DECK FLOORBEAM UPPER CHORD AT BS 380 LBL 32-36 FOUND TWO EACH , FLOOR PANEL ATTACHMENT HOLES C RACKED AS MARKED. REPAIRED FLOOR BEAM CRACKED HOLES PER SB 747-53A2431 FIG 7. 2 L 7 4 4F A20WE 2001050100191 20010501 00191 NM 2001 5 1 UPS01435719 1 20010408 A 5315 FLOORBEAM BOEING 747 747SR46 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C3 UPPER DECK FLOORBEAM UPPER CHORD AT BS 360 RBL 18-58 FOUND EIGHT FLOOR PANEL ATTACHMENT HOLES CRACK ED AS MARKED. REPAIRED FLOORBEAM CRACKED HOLES PER SB 747-53A2431 FIG 9. 2 L 7 4 4F A20WE 2001050100192 20010501 00192 NM 2001 5 1 UPS01435720 1 20010408 A 5315 FLOORBEAM BOEING 747 747SR46 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C3 UPPER DECK FLOORBEAM UPPER CHORD AT BS 340 RBL 44-55 FOUND THREE EACH FLOOR PANEL ATTACHMENT HOLES CRACKED AS MARKED. REPAIRED FLOORBEAM UPPER HCORD (AFT SIDE) CRACKED HOLES AS PER SB 747-53A2431 FIG.9. 2 L 7 4 4F A20WE 2001050100193 20010501 00193 WP 2001 5 1 20010416CW008 1 20010216 A 7714 AN55311 TACH GENERATOR DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE ENGINE NR 1 INOPERATIVE H B2OB K NONE O OTHER IN INSP/MAINT 1 AL 01 44911 1588 10461 BROKEN WIRE WHERE CONNECTOR PLUG CONNECTS. 2 L 7 4 4R 4 R A762 5E5 2001050100194 20010501 00194 NM 2001 5 1 UPS01435721 1 20010406 A 5210 HINGE BOEING 747 747SR46 NM PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 M/D - L1 DOOR BODY T/T LOWER HINGE UPP BEARING SUPPORT FTG FOUND CRACKED AT BS 440 WL 178. REPLAC ED L1 DOOR HINGE BODY TORQUE TUBE LOWER HINGE FTG PER SRM 51-10-01 DOOR RIGGING & OPERATIONAL TEST DONE PER MM FOUND SAT IS. 2 L 7 4 4F A20WE 2001050100195 20010501 00195 NM 2001 5 1 UPS01435722 1 20010407 A 5310 DOOR FRAME BOEING 747 747SR46 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 M/D - L5 DOOR FWD CUTOUT REVEAL FOUND CRACKED AT UPPER HINGE LOWER AREA. REPLACED L5 DOOR FWD CUTOUT REVEAL AS PER SRM 51-10-01 DOOR RIGGING & OPERATIONAL TEST DONE PER MM 52-11-01 FOUND SATIS. 2 L 7 4 4F A20WE 2001050100196 20010501 00196 NM 2001 5 1 UPS01435724 1 20010407 A 5310 DOOR FRAME BOEING 747 747SR46 NM PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C3 M/D - L2 DOOR FWD CUTOUT LOWER REVEAL FOUND CRACKED. L2 DOOR FWD CUTOUT LOWER REVEAL AND FRAME REP AIRED AS PER SRM 53-10-04 FIG.84. 2 L 7 4 4F A20WE 2001050100197 20010501 00197 NM 2001 5 1 UPS01435725 1 20010406 A 5310 FRAME BOEING 747 747SR46 NM PAX WINDOW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 FX - COCKPIT R3 WINDOW FRAME FOUND CRACKED AT AFT EDGE LOWER AREA. SKIN REPAIED AS PER SRM 53-30-03 FIG 49. 2 L 7 4 4F A20WE 2001050100198 20010501 00198 NM 2001 5 1 UPS01435726 1 20010412 A 5310 DOOR FRAME BOEING 747 747SR46 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C3 CRACK REVEALED ON THE BOTTOM FORWARD CORNER VERTICAL BEAM OF DOOR 5L, DOOR 5L FWD CORNER VERTICAL B EAM REPAIRED AS PER SRM 52-10-02 FIG 10 2 L 7 4 4F A20WE 2001050100199 20010501 00199 NM 2001 5 1 UPS01435727 1 20010404 A 5311 FRAME BOEING 747 747SR46 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 M/D - BS 140 BULKHEAD RING FOUND CRACKED AT STR 20R. M/D BS 140 BULKHEAD OUTER RING CHORD REPAIRED IA W UPS EO 747-5310-3079-D APPENDIX B FIG 4. 2 L 7 4 4F A20WE 2001050100200 20010501 00200 NM 2001 5 1 UPS01435728 1 20010407 A 5210 FITTING BOEING 747 747SR46 NM PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 M/D- L3 DOOR FWD CUTOUT NR 6 STOP FITTING FOUND CRACKED. REPLACED NR 6 DOOR STOP FITTING AS PER SRM 51-10-01; DOOR ADJUSTMENT & RIGGING AS PER MM 52-11-01 BE COMPLIED WITH FOUND SATIS. 2 L 7 4 4F A20WE 2001050100201 20010501 00201 NM 2001 5 1 UPS01435729 1 20010405 A 5210 FITTING BOEING 747 747SR46 NM PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C3 M/D- L3 DOOR FWD CUTOUT NR 2 STOP FTG FOUND CRACKED. REPLACED NR 2 STOP FITTING PER SRM 51-10-01 D OOR ADJUSTMENT & RIGGING PER MM BE COMPLIED WITH FOUND SATIS. 2 L 7 4 4F A20WE 2001050100202 20010501 00202 NM 2001 5 1 UPS01435730 1 20010407 A 5313 STRINGER BOEING 747 747SR46 NM CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 CABIN - STRINGER END FOUND CRACK AT 1730 - 1731 STR-8L. STRINGER REPAIRED AS PER SRM 53-10-03 FIG .5 2 L 7 4 4F A20WE 2001050100203 20010501 00203 NM 2001 5 1 UPS01435731 1 20010408 A 5315 FLOORBEAM BOEING 747 747SR46 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 COCKPIT LATERAL FLOORBEAM UPPER CHORD CORRODED AROUND FASTENER HOLES. U/D BS 420 LBL 11 TO LBL 30 F LOORBEAM REPAIR AS PER SRM 53-10-07 FIG.8 2 L 7 4 4F A20WE 2001050100204 20010501 00204 NM 2001 5 1 UPS01435732 1 20010408 A 5315 FLOORBEAM BOEING 747 747SR46 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 U/D - BS 660 LBL 38 FLOORBEAM FOUND CORROSION. U/D BS 660 LBL 38 FLOORBEAM REPAIR AS PER SRM 53-10- 01 FIG.1. 2 L 7 4 4F A20WE 2001050100205 20010501 00205 NM 2001 5 1 UPS01435733 1 20010408 A 5321 FLOOR PANEL BOEING 747 747SR46 NM CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C3 BULK CARGO COMPT - FLOOR PANEL SUPPORT LOWER SURFACE FOUND CORROSION AT FS LBL 30 AS MARKED. FLOOR PANEL SUPPORT REPAIRED AT BULK CARGO COMPT FX 1920- FS 1926 LBL 30 AS PER SRM 53-10-07 FIG 20. 2 L 7 4 4F A20WE 2001050100206 20010501 00206 NM 2001 5 1 UPS01435734 1 20010401 A 5347 SEAT TRACK BOEING 747 747SR46 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C3 U/D - BS 670-690 LBL 65 SEAT TRACK LIPS CORRODED. SEAT TRACK REPAIR AT LBL 65 FROM BS 670-690 AS PE R SRM 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2001050100207 20010501 00207 NM 2001 5 1 UPS01435735 1 20010408 A 5347 SEAT TRACK BOEING 747 747SR46 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C3 U/D - BS 600-660 LBL 64 SEAT TRACK FLANGE CORRODED. SEAT TRACK REPAIR AT LBL 65 FROM BS 600-660 AS P ER SRM 53-10-05 FIG 1A 2 L 7 4 4F A20WE 2001050100208 20010501 00208 NM 2001 5 1 UPS01435736 1 20010408 A 5347 SEAT TRACK BOEING 747 747SR46 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 U/D - BS 520-530 LBL 48 SEAT CROWN FOUND CORRODED. U/D SEAT TRACK REPAIR AT LBL 48 FROM BS 520- BS 5 30 AS PER SRM 53-10-01 FIG 1. 2 L 7 4 4F A20WE 2001050100209 20010501 00209 NM 2001 5 1 UPS01435737 1 20010408 A 5347 SEAT TRACK BOEING 747 747SR46 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C3 U/D - BS 590 LBL 48 SEAT TRACK FLANGE CORRODED. U/D SEAT TRACK REPAIR AT LBL 48 BS 590 AS PER SRM 53-10-01 FIG.1. 2 L 7 4 4F A20WE 2001050100210 20010501 00210 NM 2001 5 1 UPS01435738 1 20010408 A 5347 SEAT TRACK BOEING 747 747SR46 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C3 U/D - BS 620-660 LBL 48 SEAT TRACK FLANGE CORRODED. U/D BS 620-660 LBL 48 SEAT TRACK REPAIRED AS PE R SRM 53-10-01 FIG.1 2 L 7 4 4F A20WE 2001050100211 20010501 00211 NM 2001 5 1 UPS01435739 1 20010408 A 5347 SEAT TRACK BOEING 747 747SR46 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C3 U/D - BS 580 - 600 LBL 48 SEAT TRACK FLANGE CORRODED. U/D BS 580-600 LBL 48 SEAT TRACK REPAIRED AS PER SRM 53-10-01 FIG.1. 2 L 7 4 4F A20WE 2001050100212 20010501 00212 NM 2001 5 1 UPS01435740 1 20010408 A 5347 SEAT TRACK BOEING 747 747SR46 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 U/D - BS 710 LBL 28 SEAT TRACK FLANGE CORRODED. U/D BS 710 LBL 28 SEAT TRACK REPAIRED AS PER SRM 53 -10-01 FIG.1. 2 L 7 4 4F A20WE 2001050100213 20010501 00213 NM 2001 5 1 UPS01435741 1 20010408 A 5347 SEAT TRACK BOEING 747 747SR46 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C3 U/D - BS 660-680 LBL 28 SEAT TRACK CROWN AND FLANGE CORRODED. U/D BS 660-680 LBL 28 SEAT TRACK CROW N REPAIRED AS PER SRM 53-10-01 FIG.1. 2 L 7 4 4F A20WE 2001050100214 20010501 00214 NM 2001 5 1 UPS01435742 1 20010408 A 5347 SEAT TRACK BOEING 747 747SR46 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 U/D - BS 600-660 LBL 28 SEAT TRACK FLANGE CORRODED. U/D BS 600-660 LBL 28 SEAT TRACK FLANGE REPAIRED AS PER SRM 53-10-01 FIG.1. 2 L 7 4 4F A20WE 2001050100215 20010501 00215 NM 2001 5 1 UPS01435743 1 20010408 A 5347 SEAT TRACK BOEING 747 747SR46 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 U/D - BS 560-580 LBL 28 SEAT TRACK CORRODED. U/D BS 560-580 LBL 28 SEAT TRACK REPAIRED AS PER SRM 53 -10-01 FIG.1. 2 L 7 4 4F A20WE 2001050100216 20010501 00216 NM 2001 5 1 UPS01435744 1 20010408 A 5347 SEAT TRACK BOEING 747 747SR46 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 U/D - BS 540 LBL 28 SEAT TRACK CROWN CORRODED. U/D BS 540 LBL 28 SEAT TRACK CROWN REPAIRED AS PER SR M 53-10-01 FIG.1 2 L 7 4 4F A20WE 2001050100217 20010501 00217 NM 2001 5 1 UPS01435749 1 20010425 A 5712 RIB BOEING 747 747SR46 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 RT - CORROSION CRACK IS REVEALED AT ILES 630.72 RIB AS MARKED. RT RIB WAS REPAIRED AS PER SRM 51-40- 02 AFTER CORROSION REMOVED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001050700541 20010507 00541 NM 2001 5 7 UPS01635750 1 20010427 A 2710 AILERON BOEING 767 767300 1385204 NM WINGS BINDING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 323UP 27749 WHEN CHECKING FLIGHT CONTROLS BEFORE ENGINE START, THE RIGHT OUTBOARD AILERON STUCK IN THE FULL UP POSITION WITH CONTROL YOKE IN NEUTRAL. ORDERED RIGHT AILERON (OUTBOARD) INBD PCA. EMP 25110 ACCOMPLISHED FIM B-767 27-11-00 NO PROBLEMS FOUN D PCU OPERATE NORMALLY. LUBRICATED AILERON HINGES FOR PRECAUTIONARY SYSTEM 1 CHECKS NORMAL A/C OK FOR SERVICE (NO EICAS MESSAGES FOUND) 2 L 7 2 4F RT A1NM 2001050100218 20010501 00218 WP 2001 5 1 UPS01835708 1 20010328 A 5320 37558452N FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 STA. 1160 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG. 36 TO 35R. REMOVED AND REPLACED FITTING I.A.W. DWG. 3755845,AND SRM. 53-2-0 FIG. 2D 2 L 7 4 4F RT 4A25 2001050100219 20010501 00219 WP 2001 5 1 UPS01835709 1 20010329 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE: C2,3 STA. 1580 FLOORBEAM IS CORRODED BEYOND LIMITS AT RBL. 48. REPAIRED FLOORBEAM I.A.W. 8110-3 APPRO VED DH SK 797-605 2 L 7 4 4F RT 4A25 2001050100220 20010501 00220 WP 2001 5 1 UPS01835710 1 20010329 A 5230 PAN DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 C-PIT DOOR PAN IS CRACKED AT STA. 1180 AT LONG. 32R APPROX. REPAIRED PAN I.A.W. SRM. 52-2-0 FIG. 4 2 L 7 4 4F RT 4A25 2001050100221 20010501 00221 WP 2001 5 1 UPS01835711 1 20010330 A 5320 3610130501N FITTING DOUG DC8 DC871F 302199D WP A/C BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 STA. 70 LOWER CUSP TO FRAME FITTING IS CORRODED BEYOND LIMITS AT LONGERON 21R. REMOVED AND REPLAC ED FITTING I.A.W. DWG. 3610130,AND SRM. 51-1-21, 51-3-0 2 L 7 4 4F RT 4A25 2001050100222 20010501 00222 WP 2001 5 1 UPS01835745 1 20010330 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 FUSELAGE EXTERNAL SKIN IS CORRODED BEYOND LIMITS AT STA. 857 BETWEEN LONGERON 16R-17R. REPAIRED SK IN I.A.W. SRM. 53-2-0 FIG. 22A 2 L 7 4 4F RT 4A25 2001050100223 20010501 00223 WP 2001 5 1 UPS01835746 1 20010329 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 RIGHT WING L/E. UPPER SKIN IS CORRODED BEYOND LIMITS BETWEEN XFS 341 TO XOLDI 6.225. REPAIRED SKIN I.A.W. 8110-3 APPROVED DH SK 797-486 2 L 7 4 4F RT 4A25 2001050100224 20010501 00224 WP 2001 5 1 UPS01835747 1 20010329 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 RIGHT WING AUX. TANK UPPER SKIN IS CORRODED BEYOND LIMITS AT XFS 193. REPAIRED SKIN I.A.W. SRM. 57 -2-1 FIG. 37 & 38 2 L 7 4 4F RT 4A25 2001050100225 20010501 00225 WP 2001 5 1 UPS01835748 1 20010328 A 5730 SKIN DOUG DC8 DC871F 302199D WP LEFT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 LEFT WING L/E. UPPER SKIN IS CORRODED BEYOND LIMITS AT XFS 760. REPAIRED SKIN I.A.W. SRM. 57-2-1 FI G. 38 2 L 7 4 4F RT 4A25 2001050100226 20010501 00226 WP 2001 5 1 UPS01835752 1 20010405 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2 MAIN CABIN STA 1306 AT X=0 (TRACK D) TRACK SCALLOP IS WORN AS MARKED. TRIMMED OUT DAMAGED AREA AND IN STALLED PLUG IAW DC8 SRM 53-2-3 2 L 7 4 4F RT 4A25 2001050100227 20010501 00227 WP 2001 5 1 UPS01835753 1 20010405 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE: C2, AFT CARGO PIT AT FS 1420 AT BL0 IN CEILING AT D PIT DOOR COVER ATTACH BRACKET IS CRACKED REMOVE D CRACKED ATTACH ANGLE IAW DC8 SRM 51-1-21 AND 51-1-20D CVD NEW P ART 5616673-64 ANGLE LOCATED AND DRILLED HOLES IAW DC8 SRM 51-1-24 INSTALLED ANGLE IAW DC8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001050100228 20010501 00228 WP 2001 5 1 UPS01835754 1 20010403 A 5230 FITTING DOUG DC8 DC873F 302199F WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2 FWD PIT FWD DOOR STA 280 LONG 31R FITTING CRACKED AND CORRODED INSIDE TORQUE BOX. REMOVED FITTING IA W DC8 SRM 51-1-21 DRILLED NEW FITTING IAW DC8 SRM 51- 1-24 AND DC8 SRM 51-1-20D INSTALLED NEW FITTING IAW DC8S RM 51-1-2 0D 2 L 7 4 4F RT 4A25 2001050100229 20010501 00229 WP 2001 5 1 UPS01835755 1 20010403 A 5320 STIFFENER DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2 FS 1800 TAIL SECTION UPPER TORQUE BOX FWD STIFFENER CRACKED. FABBED NEW STIFFENER PER TIMCO REO G079 73 2 L 7 4 4F RT 4A25 2001050100230 20010501 00230 WP 2001 5 1 UPS01835756 1 20010403 A 5320 STRUCTURE DOUG DC8 DC873F 302199F WP CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2 FLC C1 DOOR TORQUE BOX AREA STA 280 L33R UPPER FLANGE HAS CORROSION. REMOVED CORROSION, REMOVED WEB ZEE FITTING FABED DOUBLER & MODIFIED ZEE FITTI NG IAW REO G07967 INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001050100231 20010501 00231 WP 2001 5 1 20010411CW005 2 20010306 A 7200 ENGINE CASA C212 C212CC 2410204 EU GARRTT TPE331 TPE33110R 0517 WP HARTZL HCB4M HCB4M GL NR 2 MAKING METAL E EHAA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 99 422CA 7077 3976 238 P37098C CDA4145 ON DOWNWIND LEG AT 2000 FT PILOT NOTICED NR 2 ENGINE TORQUE GAGE READ 0. COPILOT VISUAL OF NR 2 PROP REPORTED AS FEATH ERED EMERGENCY HANDLE ACTIVATED AND UNEVENTFUL LANDING MADE. SUBSQUENT ENGINE START FAILED. NEXT START ATTEMPT FOLLO WING DAY FOR TROUBLESHOOTING NORMAL, AFTER 2 MINUTE GROUND RUN NR 2 ENGINE CHIP DETECTOR ILLUMINATED AND ENGINE WAS SHUT DOWN. OIL FILTER INSPECTION REVEALED NO METAL CONTENT. ENGINE REMOVED FROM SERVICE. 2 H 7 2 4T 4 T A43EU E4WE 6 C P56GL 2001050100232 20010501 00232 WP 2001 5 1 UPS01835660 1 20010329 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 STA. 1766 LONG. 17L IS CRACKED AND CORRODED REPAIRED LONGERON I.A.W. SRM.53-2-2 FIG. 10 2 L 7 4 4F RT 4A25 2001050100233 20010501 00233 WP 2001 5 1 ZW0A0100314 1 20010412 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT IN AFT CARGO COMPT FOUND CORROSION ON LONGERON 30 BETWEEN STA 1003 AND 1022. CORROSION REMOVED BY SPOT FACE AND BLEND PER ARA 17738, SRM 51-10-3 PARA 35, AND SPM 6-80-01 PARA 3. PRIMED AND PAINTED PER SRM 51-10. INST ALLED NEW FASTENERS PER SRM 51-60-0, FIG 4 AND TABLE 15 SRM 51-30-0, AND SRM 51-20-0. 2 L 7 2 4F A6WE 2001050100234 20010501 00234 SO 2001 5 1 C2XA01IA217 1 20010413 A 3350 1317 LIGHT EMB 145 EMB145ER SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14945 145049 IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED AN EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE AFFECTED LIGHT BULB AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001050100235 20010501 00235 SW 2001 5 1 20010425CW004 1 20010320 A 6320 206040150029 CASE BELL 206 206B 1181511 SW ALLSN 250B 250B* GL TRANSMISSION CRACKED B PN1R K NONE O OTHER IN INSP/MAINT 1 EA 17 16EP 7456 3081 DURING A NORMAL 4500 HOUR TRANSMISSION OVERHAUL THE LOWER CASE WAS FOUND CRACKED ON ALL 4 SUPPORT WEBS, CAUSING THE CASE TO BE UNAIRWORTHY. 1 G 7 1 3U 3 T H2SW E10CE 2001050100236 20010501 00236 WP 2001 5 1 ABXA010140 1 20010310 A 5320 STIFFENER DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 85679 46041 THE RIGHT MLG WHEEL WELL HORIZONTAL PRESSURE WEB WAS FOUND TO BE CORRODED. A STIFFENER WAS FOUND TO BE BULGING AT STA 9 02 RBL 56 THROUGH 65. MAINTENANCE REPAIRED THE AREA IAW REA D853-40284, DAC DRAWING 5645332 AND DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 2001050100237 20010501 00237 NM 2001 5 1 01FDEA00288 1 20010419 A 3260 LIGHT BOEING 727 7272S2F 1384O81 NM COCKPIT INOPERATIVE A FDEA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SO 25 210FE 22932 RIGHT AND LEFT MLG IND LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT BULBS PER MAINT PRACT. OPS CK GOOD. 2 L 7 3 4F A3WE 2001050100238 20010501 00238 SO 2001 5 1 SWIA972506 1 20010414 A 5610 LATCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT DIRTY A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 578SW 120346 DURING CRUISE FLIGHT AT 22,000 FT CAPTAIN DV WINDOW LOCKING PIN SLOWLY STARTED RAISING. DESCENDED AND DIVERTED FLIGHT T O LAS WHILE MANUALLY HOLDING DV WINDOW SHUT. FOUND CAPTAIN''S DV WINDOW RELEASE LATCH GUMMED UP. CLEANED AND LUBRICATE D. OPS CHECK OF CAPTAIN''S DV WINDOW SATISFACTORY IAW CH 56-10-00. 2 L 7 2 4T 4 T RT A31SO E20NE 2001050100239 20010501 00239 NM 2001 5 1 0101365523 1 20010412 A 2913 PUMP BOEING 757 757251 1384970 NM HYDRAULIC SYS LEAKING A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 523US 17971 8107 23617 AFTER TAKEOFF, THE NR 2 CENTER HYDRAULIC PUMP PRESSURE LIGHT AND EICAS MESSAGE ILLUMINATED. THIS WAS SHORTLY FOLLOWED B Y NR 1 CENTER HYDRAULIC PUMP PRESSURE LIGHT AND EICAS MESSAGE. CENTER HYDRAULIC SYSTEM QUANTITY THEN FELL TO ZERO. FOL LOWED COM PROCEDURES. RETURNED TO MSP FOR AN UNEVENTFUL LANDING. MAINTENANCE REPLACED THE CENTER ELECTRIC HYDRAULIC PU MP AND SERVICED THE CENTER SYSTEM. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A2NM 2001050100240 20010501 00240 NM 2001 5 1 0101375534 1 20010413 A 2612 FIRE DETECTOR BOEING 757 757251 1384970 NM LT ENGINE MALFUNCTIONED A NWAA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 GL 01 534US 24265 ON ENGINE START, THE LEFT ENGINE FIRE WARNING OCCURRED. WARNINGS STOPPED AFTER FIRE SWITCH WAS PULLED AND ONE BOTTLE DI SCHARGED. MAINTENANCE CHECKED ENGINE, DUCTING, AND FUEL AND OIL LINES FOR EVIDENCE OF FIRE WITH NONE FOUND. REPLACED T HE NR 1, 2, 3, AND 4 LEFT ENGINE FIRE DETECTORS. ALSO REPLACED THE LEFT ENGINE LOOP 2 DETECTOR CARD M681, THE NR 1 AFOL TS FIRE DETECTION SYSTEM CARD M10224, AND THE NR 1 FIRE EXTINGUISHER BOTTLE. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A2NM 2001050100241 20010501 00241 SO 2001 5 1 SWIA972507 1 20010413 A 2910 HYDRAULIC LINE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE HYDRAULIC SYS LEAKING A SWIA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 562SW 120336 DURING FLIGHT, LOSS OF FLUID QUANTITY WAS NOTED ON GREEN HYDRAULIC SYSTEM. ON DEPARTURE, QUANTITY WAS APPROXIMATELY 7/8 ON GAUGE. APPROX 30-35 MINUTES INTO FLIGHT, RESERVOIR LOW LEVEL LIGHT ILLUMINATED; QTY WAS IN YELLOW ARC. CONSTANT DE CREASE IN QUANTITY WAS NOTED FOR THE DURATION OF THE FLIGHT. UPON LANDING, FLUID QUANTITY WAS IN YELLOW ARC; FLUID PRES SURE REMAINED IN GREEN ARC DURING ALL PHASED/NO CAUTION SIGNS OBSERVED. MANUAL GEAR EXTENSION PERFORMED OUT OF CONCERN FOR PARTIAL GEAR EXTENSION (FREE FALL). AN EMERGENCY WAS DECLARED AS A PRECAUTION. INSTALLED NEW LEFT ENGINE DRIVEN PU MP MAIN PRESSURE LINE (120-35694-025) PER EMB 120 MM 20-10-04. REPLENISHED RESERVOIR, LEAK CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001050100242 20010501 00242 SO 2001 5 1 SWIA972508 1 20010413 A 2751 3471001001 ANNUNCIATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT FAULTY A SWIA K NONE F FLT CONT AFFECTED CL CLIMB 1 NM 07 565SW 120340 FLAP DISAGREEMENT LIGHT ILLUMINATES AFTER FLAP RETRACTION. RETURNED FLAP HANDLE TO 15 DEGREES SETTING AND THEN SELECTED FLAPS UP. AGAIN DISAGREEMENT LIGHT REMAINED ILLUMINATED. FLAP POSITION INDICATOR DISPLAYS APPROX 2 DEGREES. REPLACED FLAP ANNUNCIATOR UNIT. OPS CHECK GOOD. P/N 347100-1001, S/N ON 0157, OFF 0078. 2 L 7 2 4T 4 T RT A31SO E20NE 2001050100243 20010501 00243 SO 2001 5 1 LR7A01006 1 20010416 A 5520 35719125 COUNTERWEIGHT LKHEED 382 382G 526414U SO ELEVATOR CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2324 4606 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC2704 FOUND LT ELEVATOR OUTBD WEIGHT ASSY CORRODED AT FS 1090, HSS 316, WL 278. REPLACED COUNTERWEIGHT ASSY IAW AC 43.13-1B AND SMP 581-91-00-10 PG 209. 2 H 7 4 4T A1SO 2001050100244 20010501 00244 SO 2001 5 1 LR7A01007 1 20010416 A 5520 35719125 COUNTERWEIGHT LKHEED 382 382G 526414U SO ELEVATOR CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2324 4606 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC2704 FOUND RT ELEVATOR OUTBD WEIGHT ASSY CORRODED AT FS 1090, HSS 316, WL 278. REPLACED COUNTERWEIGHT ASSY IAW AC 43.13-1B AND SMP 581-91-00-10 PG 209. 2 H 7 4 4T A1SO 2001050100245 20010501 00245 SO 2001 5 1 LR7A01008 1 20010416 A 5315 3375081 FITTING LKHEED 382 382G 526414U SO FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2324 4606 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC05297 FOUND FS 729 - 737 INTERCOSTAL FITTING CORRODED AT WL 143, LBL 60. REPLACED FITTING IAW SMP 581-53-40 PG 10. 2 H 7 4 4T A1SO 2001050100246 20010501 00246 SO 2001 5 1 LR7A01010 1 20010416 A 5321 STIFFENER LKHEED 382 382G 526414U SO FLOOR PANEL DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2324 4606 DURING SCHEDULED C3 INSPECTION DURING NR 2006 ACCESS FOUND LT, CENTER AND RT FS 740E - 817E FLOOR PANELS WITH DAMAGED S TIFFENERS AT LBL 52 - LBL 15, LBL 15 - RBL 15 AND RBL 15 - RBL 52 AT WL 146. FABRICATED AND REPLACED FLOOR PANELS IAW S RM SMP 583-53-40-05. 2 H 7 4 4T A1SO 2001050100247 20010501 00247 SO 2001 5 1 LR7A01011 1 20010416 A 5330 SKIN LKHEED 382 382G 526414U SO FUSELAGE DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2324 4606 DURING SCHEDULED C3 INSPECTION CARRY OVER ITEM 00679 DUE, REF ED 00-0022-2. FUSELAGE BELLY SKIN DENTED FS 317E/RBL 5 - 12, FS 322E/RBL 18, FS 328E/LBL 3, FS 337E/LBL 6, FS 337E/LBL 9, FS 339E/RBL 11, FS 764E/LBL 50, FS 775E/LBL 44 AND FS 7 53E/RBL 37. FABRICATED AND REPLACED 2 SKIN PANELS FS 245 - FS 339E AND FS 737E - 777E, LBL 60 TO RBL 60 IAW SRM SMP 583 -53-10 PG 2. 2 H 7 4 4T A1SO 2001050100248 20010501 00248 SO 2001 5 1 LR7A01012 1 20010416 A 5330 SKIN LKHEED 382 382G 526414U SO FUSELAGE DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2324 4606 DURING SCHEDULED C3 INSPECTION CARRY OVER ITEM 00679 DUE, REF ED 00-0022-2. FUSELAGE LT SIDE SKIN DENTED FS 742E/WL 152 , FS 754E/WL 146-161, FS 761E/WL 152 AND FS 771E/WL 155. REPAIRED IAW SRM SMP 583-51-140-11. 2 H 7 4 4T A1SO 2001050100249 20010501 00249 SO 2001 5 1 LR7A01013 1 20010416 A 5330 SKIN LKHEED 382 382G 526414U SO FUSELAGE DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2324 4606 DURING SCHEDULED C3 INSPECTION CARRY OVER ITEM 00679 DUE, REF ED 00-0022-2. FUSELAGE BELLY SKIN DENTED FS 257/RBL 11-17 . REPAIRED IAW SRM SMP 583-51-140-12. 2 H 7 4 4T A1SO 2001050100250 20010501 00250 SO 2001 5 1 LR7A01014 1 20010416 A 5330 SKIN LKHEED 382 382G 526414U SO FUSELAGE DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2324 4606 DURING SCHEDULED C3 INSPECTION CARRY OVER ITEM 00679 DUE, REF ED 00-0022-2. FUSELAGE BELLY SKIN DENTED FS 721/RBL 46. REPAIRED IAW SRM SMP 583-51-140-12. 2 H 7 4 4T A1SO 2001050100251 20010501 00251 SO 2001 5 1 LR7A01016 1 20010416 A 5330 SKIN LKHEED 382 382G 526414U SO FUSELAGE DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2324 4606 DURING SCHEDULED C3 INSPECTION CARRY OVER ITEM 00679 DUE, REF ED 00-0022-2. FUSELAGE LT SIDE SKIN DENTED FS 715/WL 165 AND FS 722/WL 157. REPAIRED IAW SRM SMP 583-51-140-12. 2 H 7 4 4T A1SO 2001050100252 20010501 00252 SO 2001 5 1 LR7A01017 1 20010416 A 5320 BEAM LKHEED 382 382G 526414U SO FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2324 4606 DURING SCHEDULED C3 INSPECTION PER JOB CARD HSP5369 FOUND LT MLG WHEEL WELL FS 577 VERTICAL BEAM CORRODED AT WL 185 - 18 7, LBL 70. REPAIRED IAW LAC MEA 382-53-01-011. 2 H 7 4 4T A1SO 2001050100253 20010501 00253 SO 2001 5 1 LR7A01019 1 20010416 A 5320 ANGLE LKHEED 382 382G 526414U SO FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2324 4606 DURING SCHEDULED C3 INSPECTION PER JOB CARD HSP5369 FOUND LMLG WHEEL WELL FS 537 BOW BEAM LOWER SUPPORT BRACKET CORRODED AT WL 150, LB 64. L-ANGLE FABRICATED AND REPLACED IAW SRM SMP 583-51-10 PG 4. 2 H 7 4 4T A1SO 2001050100254 20010501 00254 SO 2001 5 1 LR7A01020 1 20010416 A 5320 STIFFENER LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2324 4606 DURING SCHEDULED C3 INSPECTION PER JOB CARD HSP53126 FOUND FS 480 PRESSURE FAIRING INNER STIFFENER CRACKED ALONG 4 FASTE NER HOLES AT WL 280, LBL 18. REPAIRED IAW SRM SMP 583-53-40-35C. 2 H 7 4 4T A1SO 2001050100255 20010501 00255 SO 2001 5 1 LR7A01021 1 20010416 A 5347 SEAT TRACK LKHEED 382 382G 526414U SO COCKPIT WORN A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2324 4606 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC2560 FOUND FS 130 PILOT''S OUTBD SEAT TRACK WORN AT WL 203, LBL 28. REPAI RED IAW LAC MEA 382-53-99-164 R1. 2 H 7 4 4T A1SO 2001050100256 20010501 00256 SO 2001 5 1 LR7A01022 1 20010416 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2324 4606 DURING SCHEDULED C3 INSPECTION PER JOB CARD HSP53224 FOUND FS 497 OVERHEAD BULKHEAD WEB CRACKED AT WL 266, LBL 58. REPA IRED IAW SRM SMP 583-53-40-35A. 2 H 7 4 4T A1SO 2001050100257 20010501 00257 SO 2001 5 1 LR7A01024 1 20010416 A 5320 BEAM LKHEED 382 382G 526414U SO FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2324 4606 DURING SCHEDULED C3 INSPECTION NR 2034 ACCOMPLISHMENT FOUND LT MLG WHEEL WELL FS 588 VERTICAL BEAM CORRODED AT WL 185 - 187, LBL 70. REPAIRED IAW LAC MEA 382-53-01-012. 2 H 7 4 4T A1SO 2001050100258 20010501 00258 SO 2001 5 1 LR7A01025 1 20010416 A 5310 PRESSURE PANEL LKHEED 382 382G 526414U SO FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2324 4606 DURING SCHEDULED C3 INSPECTION PER JOB CARD HSP53126 FOUND FS 477 - 517 PRESSURE FAIRING CORRODED AT RT CWS 23.5 TO 61.5 , WL 276 TO WL 282. REPAIRED IAW LAC MEA 382-53-01-013. 2 H 7 4 4T A1SO 2001050100259 20010501 00259 SO 2001 5 1 LR7A01027 1 20010416 A 5320 LS5112 ANGLE LKHEED 382 382G 526414U SO FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2324 4606 DURING SCHEDULED C3 INSPECTION NR 2011 ACCOMPLISHMENT FOUND FS 737E - 750E CHINE ANGLE CORRODED AT WL 146, LBL 61. FABR ICATED AND REPLACED CHINE ANGLE PER SRM SMP 583-53-40-26. 2 H 7 4 4T A1SO 2001050100260 20010501 00260 SO 2001 5 1 LR7A01028 1 20010416 A 5320 3723519 CAP LKHEED 382 382G 526414U SO FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2324 4606 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC05297 FOUND FS 597 - 737 CHINE CAP CORRODED AT WL 146, LBL 58 AROUND 25K D -RING HOLE. REPLACED CHINE CAP PER SRM SMP 583-51-10 PG 4. 2 H 7 4 4T A1SO 2001050100261 20010501 00261 SO 2001 5 1 LR7A01029 1 20010417 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 1168 5025 DURING CARGO DOOR CLOSURE PRIOR TO DEPARTURE FOUND FS 968 BULKHEAD ASSY AND BRACE BROKEN AT BL 0, WL 280 AT ACTUATOR ATT ACH DUE FITTING P/N 3303522-1 CRACKED. REPAIRED UPPER BULKHEAD IAW SRM SMP 583-53-50-06. REPLACED BRACE AND FITTING IA W SRM SMP 583-51-40 PG 4, PARA G. 2 H 7 4 4T A1SO 2001060600001 20010606 00001 NM 2001 6 6 01FDEA00285 1 20010504 A 2613 CONTROL UNIT BOEING 727 727225 1384077 NM OVERHEAT DETECT FAILED A FDEA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 25 461FE 22548 IN CR LWR AFT BODY OVERHEAT LIGHT ILLUM. PERFORMED RED TABS. REMOVED AND REPLACED OVERHEAT DETECTION CONTROL UNIT PER MM 26-12-011-05. SYSTEM CHECK NORMAL. 2 L 7 3 4F A3WE 2001050100262 20010501 00262 NM 2001 5 1 UPS01M35712 1 20010411 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 250UP INSPECTION TYPE:C MAIN DECK, SEAT TRACK, LBL27 CORRODED AT BS 840 - BS 915. CORROSION CLEANED FOUND STA 816 AND 909 OUT OF LIMIT. NEW SEAT TRACK FROM STA 816 - 909 LBL27 REPLACED PER SRM53-70-00 FIG.1 VOL.I REV.28 2 L 7 3 4F RT A22WE 2001050100263 20010501 00263 NM 2001 5 1 UPS01M35713 1 20010411 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 250UP INSPECTION TYPE: C, MAIN DECK SEAT TRACK LBL27 CORRODED AT BS840-BS915 CORROSION CLEANED FOUND STA 816 AND 909 OUT OF LIMIT NEW SEAT TRACK FROM STA816 TO STA909 LBL27 REPLACED 2 L 7 3 4F RT A22WE 2001050100264 20010501 00264 CE 2001 5 1 20010411CW006 1 20010321 A 7603 2300003261 CONTROL CABLE LEAR 24 24 5170302 CE GE CJ610 CJ610* 30006 NE LT ENGINE BINDING E CJPA K NONE O OTHER IN INSP/MAINT 1 NM 03 241JA 1280 131 LT THROTTLE BINDING WHEN ADVANCED FOR TAKEOFF POWER. FOUND BINDING OF LEFT AFT ENGINE THROTTLE CONTROL DUE TO POSSIBLE E XCESSIVE ROUTING OF CONTROL TO CONFORM TO NACELLE SIZE. REROUTED CONTROL TO INCREASE RADIUS OF BEND INSIDE NACELLE AND CONTROL OPERATED NORMALLY. 2 L 7 2 4J 4 J A10CE 1E16 2001050100265 20010501 00265 WP 2001 5 1 UPS01835659 1 20010328 A 5320 5643483502N FITTING DOUG DC8 DC871F 302199D WP MAIN CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 STA. 879 RBL. 63 CUSP TO FRAME FITTING BELOW FLOOR PANEL IS CORRODED BEYOND LIMITS REMOVED AND REPLACED FITTING I.A.W. DWG. 5643483,AND SRM. 51-1-20D, 51-1-21 2 L 7 4 4F RT 4A25 2001050100268 20010501 00268 NM 2001 5 1 EIA2001123 1 20010321 A 5315 FLOORBEAM BOEING 747 747128 1384894 NM FUSELAGE MISDRILLED A EIAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - FOUND FS 460 RBL 19 DOUBLE DRILLED HOLE IN FLOORBEAM AFT FLANGE. REMOVED DAMAGED SECTION OF FLOORBEAM UPPER C HORD FROM BL 0 TO RBL 45, FABRICATED NEW UPPER CHORD SECTION 1 AND 2 SPLICE ANGLES, 3 STRAPS, 6 AND 7 FILLERS, AND INSTA LLED PER SRM 53-10-07 FIG 8 AND 51-30-02. (M) 2 L 7 4 4F A20WE 2001050100269 20010501 00269 NM 2001 5 1 EIA2001122 1 20010321 A 5531 SPAR BOEING 747 747128 1384894 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - FOUND WEB AT FINS STATION 570, 39 INCHES FROM LE, AND WEB FORWARD SPAR AT FIN STATION 570 CORRODED. INSTALLED FRONT SPAR WEB REPAIR AT STATION 570 PER B747 SRM 55-30-05 FIG 1. REPLACED INBOARD L-CHORD AND WEB ON LE RIB AT STATIO N 570 PER B747 SRM 51-20-01 AND 51-30-02. (M) 2 L 7 4 4F A20WE 2001050100270 20010501 00270 NM 2001 5 1 EIA2001198 1 20010312 A 5330 SKIN BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND S41 MOD AT ZONE 1, BS 340-393 STRINGER 6R LAP JOINT FOUND SEVERAL SKIN CRACKS INCLUDING ONE AT UPPER B ONDED DOUBLER. (M) 2 L 7 4 4F A20WE 2001050100271 20010501 00271 NM 2001 5 1 EIA2001197 1 20010312 A 5330 SKIN BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND S41 MOD AT ZONE 1, BS 340, STRINGER 5L TO STRINGER 9L FX SKIN FOUND 12 FASTENER HOLES CRACKED. (M) 2 L 7 4 4F A20WE 2001050100272 20010501 00272 NM 2001 5 1 EIA2001196 1 20010312 A 5330 SKIN BOEING 747 747273C 1384896 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND S41 MOD AT ZONE 1, BS 320-340 LEFT EXTERNAL DOUBLER BETWEEN STRINGER 2L TO STRINGER 5L FOUND 3 FASTENE R HOLES OVERSIZED. (M) 2 L 7 4 4F A20WE 2001050100273 20010501 00273 NM 2001 5 1 EIA2001194 1 20010312 A 5310 STRUCTURE BOEING 747 747273C 1384896 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND BS 2360 B/H MOD, FOUND 2 EXISTING REPAIR DOUBLER INSTALLED ON FORWARD AND AFT SIDE OF B/H APU CUTOUT. REMOVED EXISTING WEB REPAIR PARTS AND REPLACED WITH MODIFIED PARTS. (M) 2 L 7 4 4F A20WE 2001050100274 20010501 00274 NM 2001 5 1 EIA2001193 1 20010312 A 5320 65B105177 SPLICE BOEING 747 747273C 1384896 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND BS 1000 STRINGER 38L, ON REMOVAL OF EXTERIOR DRAG SPLICE FITTINGS FOUND HEAVY CORROSION ON FAYING SURF ACE ATTACH LUGS. REPLACED BS 1000 STRINGER 38L EXTERIOR DRAG SPLICE FITTINGS PER SRM 51-10-01. (M) 2 L 7 4 4F A20WE 2001050100275 20010501 00275 NM 2001 5 1 20010501AP001 1 20010312 A 5320 65B1051775 SPLICE BOEING 747 747273C 1384896 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND BS 1000 STRINGER 38L, ON REMOVAL OF EXTERIOR DRAG SPLICE FITTINGS FOUND HEAVY CORROSION ON FAYING SURF ACE ATTACH LUGS. REPLACED BS 1000 STRINGER 38L EXTERIOR DRAG SPLICE FITTINGS PER SRM 51-10-01. REF EIA2001193. (M) 2 L 7 4 4F A20WE 2001050100276 20010501 00276 NM 2001 5 1 EIA2001192 1 20010312 A 5712 RIB BOEING 747 747273C 1384896 NM LT WING CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND LT WING SURGE TANK WS 1516 UPPER RIB STRINGER 6 AFT BOLT HOLE CRACKED. REPAIRED UPPER RIB CHORD PER S RM 57-10-05 FIG 4. (M) 2 L 7 4 4F A20WE 2001050100277 20010501 00277 NM 2001 5 1 EIA2001191 1 20010312 A 5720 WEB BOEING 747 747273C 1384896 NM RT WING CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND RT WING NR 3 MAIN TANK MID SPAR UPPER WEB 1 FASTENER EDGE CRACKED FROM WS 382-411. TRIMMED OFF CRACKE D AREA, NDT INSPECTED, INSTALLED FREEZE PLUG AND REPAIRED MID SPAR WEB PER RM 571-0-06. (M) 2 L 7 4 4F A20WE 2001050100278 20010501 00278 NM 2001 5 1 EIA2001190 1 20010312 A 5720 WEB BOEING 747 747273C 1384896 NM LT WING CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND LT WING NR 2 MAIN TANK MID SPAR UPPER WEB 1 FASTENER EDGE CRACKED FROM WS 150-353. TRIMMED OFF CRACKE D AREA, NDT INSPECTED, INSTALLED FREEZE PLUG AND REPAIRED MID SPAR WEB PER SRM 57-10-06. (M) 2 L 7 4 4F A20WE 2001050100279 20010501 00279 NM 2001 5 1 EIA2001189 1 20010312 A 5720 WEB BOEING 747 747273C 1384896 NM LT WING CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - LT WING NR 2 MAIN TANK MID SPAR UPPER WEB FASTENER EDGE CRACKED FROM WS 382-411. TRIMMED OFF CRACKED AREA, NDT INSPECTED, INSTLALED FREEZE PLUG AND REPAIRED MID SPAR WEB PER SRM 57-10-06. (M) 2 L 7 4 4F A20WE 2001050100280 20010501 00280 NM 2001 5 1 EIA2001188 1 20010312 A 5720 WEB BOEING 747 747273C 1384896 NM LT WING CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND LT WING NR 2 MAIN TANK MID SPAR UPPER WEB 1 FASTENER EDGE CRACKED BETWEEN WS 440-469. TRIMMED CRACKED AREA, NDT INSPECTED, REPAIRED WEB PER SRM 57-10-06 FIG 5. (M) 2 L 7 4 4F A20WE 2001050100281 20010501 00281 NM 2001 5 1 EIA2001187 1 20010312 A 5310 65B1569711 SHEAR TIE BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND BS 1000 LBL 78 CENTER TANK UPPER SHEAR TIE CRACKED. REPLACED CENTER TANK UPPER SHEAR TIE AT LBL 78 PE R SRM 51-10-01. (M) 2 L 7 4 4F A20WE 2001050100282 20010501 00282 NM 2001 5 1 EIA2001185 1 20010312 A 5320 WEB BOEING 747 747273C 1384896 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND WLG W/W STATION 1264 RBL 120 MOST OUTBOARD VERTICAL WEB CORRODED. REMOVED CORROSION, REPAIRED FRAME W EB PER BSB 747-53-2416. (M) 2 L 7 4 4F A20WE 2001050100283 20010501 00283 NM 2001 5 1 EIA2001184 1 20010312 A 5330 SKIN BOEING 747 747273C 1384896 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FX AT STATION 100 STRINGER 45R TO STRINGER 46R SKIN DOUBLER CORRODED. REPLACED DOUBLER PER SRM 51-10-01. ( M) 2 L 7 4 4F A20WE 2001050100284 20010501 00284 NM 2001 5 1 EIA2001182 1 20010312 A 5315 FLOORBEAM BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND BS 1480 M/D PX WEB CORRODED AND CRACKED ON UPPER MATING SURFACE AT RBL 58 FLOORBEAM LOWER CHORD. TRIM MED OFF WEB SKIN FROM BS 1475 TO BS 1480 RBL 57-66, NDT INSPECTED, INSTALLED 3 REPAIR DOUBLERS PER BOEING MSG AND RS R-5 3-48-34631. (M) 2 L 7 4 4F A20WE 2001050100285 20010501 00285 NM 2001 5 1 EIA2001181 1 20010312 A 5315 FLOORBEAM BOEING 747 747273C 1384896 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FORWARD CARGO COMPT AT BS 840 RBL 5 FLOORBEAM UPPER CHORD FOUND DAMAGED. SLIGHTLY TRIMMED OUT DAMAGE, NDT I NSPECTED AND REPAIRED CHORD PER SRM 51-10-01. (M) 2 L 7 4 4F A20WE 2001050100286 20010501 00286 NM 2001 5 1 EIA2001180 1 20010312 A 5310 DOOR FRAME BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND MED BS 1670 R4 DOOR FORWARD CUTOUT LOWER REVEAL CRACKED. STOP DRILLED, NDT INSPECTED, REPAIRED M/D R4 DOOR FORWARD CUTOUT LOWER REVEAL AT BS 1670 BETWEEN STRINGER 22R TO 25R PER SRM 53-10-04 FIG 84. (M) 2 L 7 4 4F A20WE 2001050100287 20010501 00287 NM 2001 5 1 EIA2001179 1 20010312 A 5230 SKIN BOEING 747 747273C 1384896 NM CARGO DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND AFT CARGO DOOR CUTOUT MOD, FX SKIN FASTENER HOLES CRACKED AT UPPER FORWARD AND AFT CORNERS. TRIMMED O FF CRACKS, NDT INSPECTED, INSTALLED 4 LAYERS OF REPAIR DOUBLERS AND REPAIRED UPPER FORWARD AND AFT CUTOUT CORNERS. (M) 2 L 7 4 4F A20WE 2001050100288 20010501 00288 NM 2001 5 1 EIA2001178 1 20010312 A 5320 ANGLE BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND FASTENER HOLE CRACK ON MED R5 BS 2231 STRINGER 24R-25R, ONE CRACK ON AFT INNER CHORD AFT ANGLE, ONE CR ACK ON INNER CHORD FORWARD ANGLE, AND TWO CRACKS ON DOOR REVEAL. OVERSIZED CRACKED FASTENER HOLE, TRIMMED OFF CRACKED C HORD AND REVEAL, NDT INSPECTED, INSTALLED REPAIR DOUBLER AND FILLERS PER BOEING MSG AND RS R-53-62-34623. (M) 2 L 7 4 4F A20WE 2001050100290 20010501 00290 CE 2001 5 1 20010419CW010 1 20010319 A 2435 BEARING LEARSIEGLER RKWELL NA265 NA26565 7630107 CE GARRTT TFE731 TFE7313R1D 01518 WP STARTER/GEN FAILED D A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 03 921CC 298 46567 PILOT REPORTED DURING FLIGHT THE LT GEN HOT ANNUCIATOR LIGHT AND MASTER CAUTION LIGHT ILLUMINATED. LEFT ENGINE WAS SHUT DOWN SINCE THE GENERATOR HOT ANNUNICATOR LIGHT WOULD NOT GO OUT. UPON RETURING TO DEPARTURE AIRPORT,RIGHT STARTER/GEN ERATOR FAILED. ON THIS AIRPLANE WITH BOTH GENERATORS OFF LINE AND THE LANDING GEAR IN THE RETRACTED POSITION, THE SECON DARY BUS WILL AUTOMATICALLY DISCONNECT, REDUCING PILOT WORK LOAD. PILOTS WERE ABLE TO RESET THE RIGHT GENERATOR AND SEC ONDARY BUS, TO HAVE THE RT GEN FALL OFF LINE AFTER 2 MINUTES AFTER RESETTING. REPLACED LT STARTER/GEN SYSTEM. NO PROBL EM WAS FOUND WITH RT GEN SYSTEM. 2 L 7 2 4J 4 F A2WE E6WE 2001050100291 20010501 00291 NM 2001 5 1 F3LA200100053 1 20010419 A 5315 FLOORBEAM BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3498 23177 DURING C-6 CHECK, INSPECTION REPORTED SURFACE CORROSION OF FLOORBEAM AT STA 312 AFT OF COCKPIT DOOR. MAINTENANCE DETERM INED CORROSION OUT OF LIMITS PER SRM 51-70-12. REMOVED FLOORBEAM, FABRICATED AND INSTALLED REPLACEMENT FLOORBEAM PER SR M 53-00-51. 2 L 7 2 4F RT A16WE 2001050100292 20010501 00292 WP 2001 5 1 MWEA010627 1 20010419 A 3260 UPLOCK DOUG DC9 DC932 3022066 WP LT MLG OUT OF ADJ A MWEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 31 401ME 47133 AFTER TAKEOFF WITH GEAR SELECTED UP, LEFT GEAR UNSAFE (RED) LIGHT REMAINED ON. CREW CYCLED GEAR WITH SAME RESULT. RETU RNED TO MCI AND LANDED WITH THREE GREEN LIGHTS, NO RED. MAINTENANCE ADJUSTED DOOR LATCH MECHANISM AND PERFORMED GEAR SW ING. SYSTEM CHECKED GOOD. 2 L 7 2 4F A6WE 2001050100293 20010501 00293 2001 5 1 31101147KH 4 20010316 A 2297 WIRE LEAR LEAR 24 24 5170302 CE GE CJ610 CJ610* 30006 NE PITCH RELAY BOX SHORTED E A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 147KH 610879 24147 SHORTLY AFTER DEPARTURE, FLIGHT CREW NOTED A PUSH FORWARD ON THE YOKE. AIRCRAFT RETURNED TO AIRPORT AND LANDED. MAINTE NANCE PERSONNEL DISCOVERED A WIRE CHAFFED AND SHORTED TO GROUND GOING TO THE PITCH DISCONNECT BOX. WIRING WAS REPAIRED AND SYSTEM TESTED EXTENSIVELY. 2 L 7 2 4J 4 J A10CE 1E16 2001050100294 20010501 00294 NM 2001 5 1 01FDEA00245 1 20010331 A 5714 STIFFENER BOEING 727 72725C 138400H NM CTR WING TANK CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 124FE 19360 DURING ROUTINE INSP THE VERTICAL STIFFENER AT LBL 14 ON THE AFT SIDE OF THE CTR WING TANK FOUND CORRODED 2 IN FROM TOP O F THE STIFFENER. 2 L 7 3 4F A3WE 2001050100295 20010501 00295 WP 2001 5 1 ZW0A0100307 1 20010410 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 909TW 49170 DURING CHECK-C MAINT FOUND CORROSION ON FLOOR TRACK NUMBER 5, RBL 54, STA 275 TO 294 AND 313 TO 332. REMOVED CORRODED S ECTION OF TRACK FROM FWD END, STA 212 TO STA 341, AND REPLACED SECTION PER SRM 53-05, FIG 4F WITH SPLICE AT STA 341. SU RFACE TREATMENT APPLIED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001051000262 20010510 00262 EU 2001 5 10 UPS01135766 1 20010429 A 3510 OXYGEN BOTTLE AIRBUS A300 A300F4622R 3930360 EU CABIN DISCHARGED A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 127UP 0812 INSPECTION TYPE:N/A PILOT REPORTS CREW O2 BOTTLE EMPTY ****SUPPLEMENTAL MRR*** SERVICED BOTTLE 2 L 7 2 4F RT A35EU 2001050100296 20010501 00296 NM 2001 5 1 UPS01235761 1 20010404 A 5260 STRUCTURE BOEING 727 72725C 138400H NM AFT AIRSTAIRS CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:C AFT AIRSTAIRS HAS 5 INCH CRACK. REPAIRED BY E.O. B72752102687, NEEDS PERMANENT REPAIR. CUT-OUT CRACK ED AREA OF SKIN 1.25 X 4 AND INSTALL FLUSH DOUBLER REPAIR 3 X 7 TO LT TOP CORNER I/A/W B727 SRM 52-10-2 FIG.4 REMOVED AN D REPLACED O/B VERTICAL WEB, HORIZONTAL SUPPORT ANGLE AND VERTICAL SUPPORT ANGLE DUE TO EXISTING DAMAGE. 2 L 7 3 4F A3WE 2001050100297 20010501 00297 NM 2001 5 1 UPS01235762 1 20010404 A 5330 SKIN BOEING 727 72725C 138400H NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:C FUSELAGE NOSE SECTION LT SIDE BS 235.8 WL 220 STR 15L SKIN CRACKED AROUND FASTENER. NDT INSP. CUT-OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR AT LT SIDE BS 235.8 WL 220 STR 15L AS PER B727 SRM 53-30-3 FIG.3 MATERIAL USE D 2024-T3 .063 9.5 X 18 LOT 869121 PO 83111644. 2 L 7 3 4F A3WE 2001050100298 20010501 00298 NM 2001 5 1 UPS01235763 1 20010404 A 5330 SKIN BOEING 727 72725C 138400H NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE: C, FUSELAGE NOSE SECTION RT SIDE BS 203.8 WL 219.5 STR.15R SKIN CRACKED AROUND FASTENERS (2EA) NDT INS P. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR AT R/H SIDE BS 203.8 WL 219.5 STR.15R AS PER B727 SRM 53-30-3 FIG. 3 MATERIAL USED 2024-T3 .063 FOR EXTERNAL DOUBLER 9.25 X 10.25 LOT240328 PO 83112055, MATERIAL USED FOR FILLER 2024-T3 . 050 2.5 X 1 PO 83110438 LOT303423. 2 L 7 3 4F A3WE 2001050100299 20010501 00299 2001 5 1 UPS01435764 4 20010429 A 2210 259102705 CARD BOEING 747 747123F NM AUTOPILOT DEFECTIVE A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 677UP 20391 INSPECTION TYPE :W/E, ON DEPARTURE THE CREW BEGAN TO NOTICE A SLIGHT ELECTRICAL SMELL, NOTHING OUT OF ORDINARY WAS NOTI CED, APPROACHING LEVEL OFF SMELL DISAPPEARED. SHORTLY AFTER ''B'' A/P DISENGAGED FOR NO APPARANT REASON. COULD NOT REEN GAGE A/P B, NOTE: B A/P PADDLESTICK SWITCH W/ENGAGE BUT A/P W/NO T HOLD ALT. OR COURSE, PULLED B A/P CB & CONTINUED FLT. REPLACED MONITOR & LOGIC UNIT AS PER MM 22-11-07, OPS CKS GOOD, PERF ORMED T/S TREE IN 22-15-00 WITH NO DEFECTS NOTED NO ABNORMAL SMELL N OTED IN COCKPIT 2 L 7 4 4F A20WE 2001050300312 20010503 00312 NM 2001 5 3 UPS01535767 1 20010428 A 5210 DOOR SEAL BOEING 757 75724APF 1384969 NM CREW DOOR TORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 CREW ENTRY DOOR SEAL TORN REF: D205294. PARTIAL TEAR, INNER SEAL OF CREW ENTRY DOOR. REPAIRED TEAR ON CREW ENTRY DOOR. OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2001050100300 20010501 00300 WP 2001 5 1 UPS01835757 1 20010403 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2 SEAT TRACK B EXFOLIATED STA 1140. REPAIRED IAW EO DC8-5320-8309 2 L 7 4 4F RT 4A25 2001050100301 20010501 00301 WP 2001 5 1 UPS01835758 1 20010403 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2 FLC AT STA 70 INTERCOSTAL AT APPROX RBL 27 TO RBL 35 CRACKED & CORRODED ***CPCP*** REMOVED INTERC OSTAL. FABBED INTERCOSTAL IAW DAC DWG 5613064 ALODINED & PR IMED IAW DC8 SRM 51-1-8 INSTALLED IAW DC8 SRM 51-1-20D & 51 -1-21 2 L 7 4 4F RT 4A25 2001050100302 20010501 00302 WP 2001 5 1 UPS01835759 1 20010409 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2 AFT PIT AT FS 1220 L33R FITTING IS CORRODED ***CPCP*** REMOVED CORROSION IAW DC8 SRM 51-1-8 ORIGI NAL THICKNESS 0.125 MINIMUM REMAINING THICKNESS IS 0.063 & FOUND TO BE OUT OF LIMITS RMVD CORROSION LOCATED & DRILL NEW FITTING IAW DC8 SRM 51-1-21 AND INSTALLED FIT TING IAW DC8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001050100303 20010501 00303 WP 2001 5 1 UPS01835760 1 20010409 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2 AFT PIT AT FS 1160 L33R FITTING IS CORRODED ***CPCP*** REMOVED CORROSION AND FOUND TO BE OUT OF L IMIT REMOVE OLD FITTING INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D & 51-3-2 2 L 7 4 4F RT 4A25 2001050100304 20010501 00304 WP 2001 5 1 ZW0A0100316 1 20010412 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT IN FWD CABIN FOUND CORROSION ON FLOOR SUPPORT AT STA 200, FROM BL 0 THRU BL 5L. FABRICATED NEW PAR T PER SRM 53-14-1, FIG 11. INSTALLED RIVETS PER SRM 51-30-2, HI-LOKS PER SRM 51-30-5. REF PRINT 9936535. 2 L 7 2 4F A6WE 2001050100305 20010501 00305 CE 2001 5 1 20010416CW019 1 20010316 A 3244 301320870 TIRE LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP RT MLG DELAMINATED D O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 EA 21 99FN 071 RP74189 TREAD COMPLETELY SEPARATED FROM TIRE CAUSING DAMAGE TO WHEEL AND GEAR DOOR ASSEMBLIES. INCIDENT OCCURED AT TAKE OFF FRO M DEPLOYED LOCATION, CREW HEARD AN UNUSUAL NOISE. ALL PARAMETERS NORMAL AND RECOVERED. AIRCRAFT LANDED AND TIRE DID N OT DEFLATE. ASSUME TIRE IS DEFECTIVE FROM MANUFACTURER, NEED TO DETERMINE CAUSE. ASSEMBLY HAS A TOTAL OF 20 LANDINGS. 2 L 7 2 4F 4 F A10CE E6WE 2001050100306 20010501 00306 CE 2001 5 1 20010419CW014 1 20010329 A 3000 VALVE BEECH B300 B300B350C CE PWA PT6 PT6A65AR 52043 NE DE ICE SYSTEM STUCK B LX5R K NONE O OTHER IN INSP/MAINT 1 GL 19 97I11 FL267 LEFT BRAKE DEICE VALVE STUCK IN ON POSITION. 2 L 7 2 4T 4 T RT A24CE E4EA 2001050100307 20010501 00307 2001 5 1 AWXA0001614 4 20010418 A 3442 6225129021 CONTROL UNIT AIRBUS A319 A319132 NM COCKPIT INOPERATIVE A AWXA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 28 810AW 6874 1835 1116 IAH - DIVERTED FLIGHT - 4/14/01 - EN ROUTE FROM PHX TO ATL THE WEATHER RADAR WENT INOPERATIVE AND THE AIRCRAFT WAS DIVER TED TO IAH DUE TO WEATHER. IN IAH THE WEATHER RADAR WAS PLACED ON MEL 34-31-01 CONDITION 1; ON 4/16/01 TROUBLESHOOTING WAS PERFORMED IN SAN AND THE RADAR CONTROL UNIT WAS REPLACED IAW AMM 34-41-12-401 AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A28NM 2001050100308 20010501 00308 EU 2001 5 1 AWXA0001615 1 20010418 A 5310 D53480020 PLATE AIRBUS 320 A320231 3930325 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 643AW 315 LT CABIN FR 68 O/B SHEAR PLATE CRACKED. FABBED AND INSTALLED SHEAR PLATE IAW DWG 53480020. 2 L 7 2 4F RT A28NM 2001050100309 20010501 00309 EU 2001 5 1 AWXA0001616 1 20010418 A 5347 D53112782 SEAT TRACK AIRBUS 320 A320231 3930325 EU CABIN CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 643AW 315 NR 3 SEAT TRACK FRAME 20 CORRODED. SEAT TRACK FABBED IAW DWG NR 53112782; INSTALLED IAW SRM 51-72-11. 2 L 7 2 4F RT A28NM 2001050100310 20010501 00310 EU 2001 5 1 AWXA0001617 1 20010418 A 5320 D53110858 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 643AW 315 FLOOR PANEL SUPPORT Y 254 LT FR 16-20 CORRODED. FABBED AND INSTALLED NEW FLOOR SUPPORT IAW DWG 531128182. 2 L 7 2 4F RT A28NM 2001050100311 20010501 00311 EU 2001 5 1 AWXA0001618 1 20010418 A 5320 D53110858 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 643AW 315 FLOOR PANEL SUPPORT Y 254 RT FR 16-20 CORRODED. CORROSION REMOVED IAW SRM 51-74-00 - FOUND TO BE OUT OF LIMITS; FABBED AND INSTALLED FLOOR PANEL SUPPORT IAW SRM 53-11-14 AND DWG D53110858. 2 L 7 2 4F RT A28NM 2001050100312 20010501 00312 EU 2001 5 1 AWXA0001619 1 20010418 A 5411 D54530032200 RIB AIRBUS 320 A320231 3930325 EU NR2 PYLON CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 643AW 315 NR 2 PYLON RIB NR 14 CRACKED. DAMAGED RIB REPLACED IAW SRM 51-72-11 AND REPAIR ACTION IAW AWA ER 26-5453-01103-JS3. 2 L 7 2 4F RT A28NM 2001050100313 20010501 00313 EU 2001 5 1 AWXA0001620 1 20010419 A 5347 D53112782 SEAT TRACK AIRBUS 320 A320232 3930326 EU CABIN CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 641AW 453 SEAT TRACK CORRODED AT FWD END FR20 -Y765 Z120. REPAIRED IAW A320 SRM 53-11-15 FIG 203 FROM FR20 TO FR23. 2 L 7 2 4F RT A28NM 2001050100314 20010501 00314 EU 2001 5 1 AWXA0001621 1 20010419 A 5347 D53112782 SEAT TRACK AIRBUS 320 A320232 3930326 EU CABIN CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 641AW 453 SEAT TRACK CORRODED AT FWD END FR20 -Y1292 Z120. REPAIRED IAW A320 SRM 53-11-15 FIG 203 FROM FR20 TO FR23. 2 L 7 2 4F RT A28NM 2001050100315 20010501 00315 EU 2001 5 1 AWXA0001622 1 20010419 A 5320 D53112818200 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 641AW 453 CORROSION ON FLOOR SUPPORT FWD OF FR20 -Y35 TO -Y40 Z120. REPAIRED IAW A320 SRM 53-00-14 FIG 206 PG 229 - 234. 2 L 7 2 4F RT A28NM 2001050100316 20010501 00316 WP 2001 5 1 ZW0A0100501 1 20010417 A 5320 CLIP DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT IN THE ELECTRONIC COMPT FOUND CORROSION ON CLIPS AT STA 130 AND 160, BOTH OTBD OF LONGERON 28R. CO RRODED CLIPS REMOVED. NEW CLIPS FABRICATED PER DRAWING 911550. TREATED PER SRM 51-10-3. INSTALLED PER SRM 51-30-5 AND 51-60-00. 2 L 7 2 4F A6WE 2001050100317 20010501 00317 WP 2001 5 1 ZW0A0100502 1 20010407 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT AT RT MLG WHEEL WELL DOOR, FOUND A ONE INCH CRACK IN RADIUS OF UPPER END OF FORMER, SECOND AFT OF T HE DOOR. ACCOMP NDT STOP DRILL PER 51-00-03, PART 6. MADE REPAIR DOUBLER AND STOP DRILLED CRACK AND INSTALLED REPAIR P ER SRM 52-01, FIG 2. 2 L 7 2 4F A6WE 2001050100318 20010501 00318 WP 2001 5 1 ZW0A0100503 1 20010417 A 5280 RIB DOUG DC9 DC982 3022082 WP RT MLG DOOR CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT ON RT MLG DOOR, THE OTBD CORNER AT Y-948 HAD A CRACK IN THE RIB. ACCOMP NDT STOP DRILL PER 51-00-0 3, PART 6. STOP DRILLED CRACK PER SRM 51-02 FIG 2. MADE REPAIR PER SRM 52-01, FIG 2. 2 L 7 2 4F A6WE 2001050100319 20010501 00319 WP 2001 5 1 ZW0A0100504 1 20010418 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT IN THE FWD CABIN FOUND FLOOR SUPPORT WITH CORROSION BETWEEN STA 160 AND 200, LBL 54 INCHES. REMOVE D CORRODED FLOOR SUPPORT. MADE NEW OUT OF SAME MATERIAL PER SPM 6-78-01. RE-INSTALLED WITH SEALER PER SRM 51-30-2. 2 L 7 2 4F A6WE 2001050100320 20010501 00320 WP 2001 5 1 ZW0A0100505 1 20010418 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT IN CABIN FOUND TRACK CORRODED AT LBL 48 INCHES, STA 1183 TO 1308. REPLACED CHAIR TRACK PER SPM 6-7 0-01. PRIMED AND PAINTED PER SRM 51-10-3. INSTALLED FASTENERS PER SRM 51-30-01. 2 L 7 2 4F A6WE 2001050100321 20010501 00321 WP 2001 5 1 ZW0A0100506 1 20010418 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT IN THE AFT GALLEY AREA, FOUND CORROSION ON NUMBER 2 CHAIR TRACK OTBD FLANGE, FROM STA 1231 TO 1308. INSTALLED NEW CHAIR TRACK PER SPM 6-70-01. PRIMED AND PAINTED PER SRM 51-10-3. INSTALLED FASTENERS PER SRM 51-30-01. 2 L 7 2 4F A6WE 2001050100322 20010501 00322 WP 2001 5 1 ZW0A0100507 1 20010418 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT IN THE AFT CARGO BILGE, FOUND CORROSION ON BOTH SIDE OF THE INTERCOSTAL BETWEEN STA 1309 AND 1323, LBL 17 INCHES. REMOVED AND REPLACED INTERCOSTAL WITH NEW. INTERCOSTAL INSTALLED PER SRM 51-30-0 AND SEALED PER SRM 51- 20-0. INTERCOSTAL LOCATED BETWEEN STA 1309 AND 1323, LBL 17 IN. 2 L 7 2 4F A6WE 2001050100323 20010501 00323 SO 2001 5 1 C2XA01IA221 1 20010317 A 5711 12002289002 SPAR CAP EMB 120 EMB120ER 3260203 SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17728 120182 EMB - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE RIGHT WING SPAR CAP WAS FOUND TO BE CRACKED BETWEEN RIBS 17 AND 18. MAINTENANCE REPAIRED THE WING SPAR IN ACCORDANCE WITH EMB-120 SRM 57-20-05, AND THE AIRCRAFT WAS APPROVED FOR RETU RN TO SERVICE. 2 L 7 2 4T RT A31SO 2001050100324 20010501 00324 SO 2001 5 1 C2XA01IA222 1 20010418 A 3231 12032943001 SEQUENCE VALVE EMB 120 EMB120ER 3260203 SO NLG WW OUT OF ADJ A C2XA K NONE O OTHER UK UNKNOWN 1 SW 27 17728 120182 IAH - FLIGHT 2913, THE CREW REPORTED THAT THE NOSE LANDING GEAR DOORS WOULD NOT CLOSE. THE AIRCRAFT LANDED AT IAH WITHO UT INCIDENT WHERE MAINTENANCE CLEANED AND ADJUSTED THE AFFECTED GEAR DOOR SEQUENCE VALVE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001050100325 20010501 00325 NM 2001 5 1 01FDEA00287 1 20010418 A 3260 INDICATOR DOUG MD11 MD11F 3023600 NM RT MLG FAULTY A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 620FE 48791 ON GEAR RETRACTION RT MG IND SHOW RED CONFIG PAGE SHOW RED ALSO. FOLLOW CKLIST RECYCLED GEAR, NO HELP. DOWN IND, ALL NM L. 2 L 7 3 4F RT A22WE 2001050100326 20010501 00326 EU 2001 5 1 01FDEA00291 1 20010419 A 3260 WARNING LIGHT AIRBUS 300 A300F4605R 3930327 EU COCKPIT ILLUMINATED A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 652FE 735 AFT T/O NOSE GEAR DOOR DID NOT CLOSE, BOTH NOSE DOOR LIGHT ON. CYCLED GEAR IN FLT, LIGHT OUT RETRACT NORM. 2 L 7 2 4F RT A35EU 2001050100327 20010501 00327 EU 2001 5 1 01FDEA00290 1 20010420 A 2611 WARNING SYSTEM AIRBUS 300 A300F4605R 3930327 EU COCKPIT ACTIVATED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 656FE 745 ON T/O CRC SOUNDED WITH RED ECAM DISPLAYED. MIN EQUP BAY SMOKE WARN ON ECAM. 2 L 7 2 4F RT A35EU 2001050100328 20010501 00328 NM 2001 5 1 20010417CW001 1 20010305 A 2782 69358521 SLEEVE BOEING BOEING 737 737* NM BLOCKING VALVE CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 7649K SLEEVE 145 IS CRACKED. FATIGUE AS PROBABLE CAUSE. 2 L 7 2 4F RT A16WE 2001050100329 20010501 00329 NM 2001 5 1 20010417CW002 1 20010305 A 2782 69358521 SLEEVE BOEING BOEING 737 737* NM BLOCKING VALVE CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 6826 SLEEVE 145 IS CRACKED. FATIGUE IS PROBABLE CAUSE. 2 L 7 2 4F RT A16WE 2001050100330 20010501 00330 NM 2001 5 1 20010417CW003 1 20010301 A 2782 BLOCK BOEING BOEING 737 737* NM SLAT ACTUATOR CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 0590 SLEEVE 145 IS CRACKED AND APPEARS TO BE OCCURRING UNDER NORMAL USE. 2 L 7 2 4F RT A16WE 2001050100331 20010501 00331 NM 2001 5 1 20010417CW004 1 20010305 A 3240 69778552 SPRING BOEING 737 737* NM BRAKE SYSTEM BROKEN B K NONE O OTHER IN INSP/MAINT 1 NM 01 SPRINGS PN 6977855-2 ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM. IMPROPER HEAT TREATING OR INCORRECT ALLOYS IN THE SPRING S. REMOVED AND REPLACED SPRINGS. 2 L 7 2 4F RT A16WE 2001050100332 20010501 00332 NM 2001 5 1 20010417CW005 1 20010308 A 2761 654494714 HOUSING BOEING BOEING 737 737* NM SPOILER ACTUATOR CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 5302 HOUSING IS CRACKED APPROX. 1.30 INCHES IN LENGTH. 2 L 7 2 4F RT A16WE 2001050100333 20010501 00333 NM 2001 5 1 20010417CW006 1 20010320 A 2730 401606223 HOUSING BOEING 727 727* NM ELEVATOR CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 HOUSING ASSEMBLY IS CRACKED ON THE SEAL PLATE SURFACE. PROBABLE CAUSE IS HOUSING ASSEMBLY IS MADE FROM MAGNESIUM ALLOY AND IS EXTREMELY SUSCEPTIBLE TO DISSIMILAR METAL CORROSION AND CRACKS. 2 L 7 3 4F RT A3WE 2001050100334 20010501 00334 NM 2001 5 1 UPS01435661 1 20010417 A 5753 65B1565013 SHAFT BOEING 747 747SR46 NM LT WING TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 LT & RT WING T/E I/B AFT FLAP DRIVE GENEVA CAM ROLLER SHAFTS NR 3,5 & 6 PITTING CORROSION FOUND. ROLLER SHAFTS REPLACED IAW MM 27-51-39. 2 L 7 4 4F A20WE 2001050100335 20010501 00335 NM 2001 5 1 20010417CW007 1 20010313 A 3230 65446924 HOUSING BOEING BOEING 737 737* NM MLG MODULE CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 HOUSING IS CRACKED IN D PRIORITY PORT. FATIGUE IS PROBABLE CAUSE. 2 L 7 2 4F RT A16WE 2001050100336 20010501 00336 NM 2001 5 1 UPS01435662 1 20010417 A 5753 65B1565011 SHAFT BOEING 747 747SR46 NM RT FLAP TRACK CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 RT WING NR 8 FLAP TRACK GENEVA CAM ROLLER SUPPORT ROD CORRODED. RT WING NR 8 FLAP TRACK AFT ROLLER SUPPORT SHAFT & ROLLER REPLACED IAW MM 27-51-40. 2 L 7 4 4F A20WE 2001050100337 20010501 00337 NM 2001 5 1 UPS01435663 1 20010419 A 5320 FLOOR SUPPORT BOEING 747 747SR46 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C3, AFT CARGO BAY- FLOOR PANEL SUPPORT FOUND CRACK AT STA 1976 RBL 30 AS MARKED. FLOOR PANEL SUPPORT R EPAIRED AS PER SRM 53-10-07 FIG 20. 2 L 7 4 4F A20WE 2001050100338 20010501 00338 NM 2001 5 1 UPS01435664 1 20010412 A 5310 SHEAR TIE BOEING 747 747SR46 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C3 CABIN - SHEAR TIE FOUND CRACK AT STA 1820 S-4R TO S-5R. CRACKED SHEAR TIE REPLACED PER SRM 51-10 -01. 2 L 7 4 4F A20WE 2001050100339 20010501 00339 NM 2001 5 1 UPS01435665 1 20010412 A 5310 SHEAR TIE BOEING 747 747SR46 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 CABIN - SHEAR TIE FOUND CRACK AT STA 1920 S-4R TO S-5R. SHEAR TIE REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001050100340 20010501 00340 NM 2001 5 1 UPS01435666 1 20010414 A 5310 65B11751602 DOOR FRAME BOEING 747 747SR46 NM PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 R3 DR CUTOUT FWD LOWER CORNER REVEAL CRACKED AS MARKED. R3 DR CUTOUT FWD LOWER CORNER REVEAL REPL ACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001050100341 20010501 00341 NM 2001 5 1 UPS01435667 1 20010417 A 5320 CHANNEL BOEING 747 747SR46 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 CABIN - ''U'' CHANNEL I/B FLANGE FOUND CRACKED AT STA 994-995 LBL 75. U CHANNEL REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001050100342 20010501 00342 NM 2001 5 1 UPS01435668 1 20010417 A 5320 FLOOR SUPPORT BOEING 747 747SR46 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 M/D - BS 1350-1370 LBL 116 MOST O/B LONGITUDINAL FLR SUPPORT FOUND CRACKED AS MARKED. M/D BS 1350 -1370 LBL 116 FLOOR SUPPORT REPAIRED AS PER SRM 51-40-03 FIG 1. 2 L 7 4 4F A20WE 2001050100343 20010501 00343 NM 2001 5 1 UPS01435670 1 20010414 A 5310 65B11751601 DOOR FRAME BOEING 747 747SR46 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 L3 DR CUTOUT FWD LOWER CORNER REVEAL CRACKED AS MARKED. L3 DR CUTOUT FWD LOWER CORNER REVEAL REPL ACED AS PER AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001050100344 20010501 00344 NM 2001 5 1 UPS01435671 1 20010421 A 5410 FRAME BOEING 747 747SR46 NM NR 4 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 NR 4 PYLON PYLON AFT TORQUE BULKHEAD O/B VERTICAL CHORD, CRACK FOUND AT 2ND FASTENER HOLE (FROM LOWER ) RUNNING O/B APPROX. 0.100 INCH LONG. NR 4 PYLON AFT TORQUE BULKHEAD O/B VERTICAL CHORD CRACKED HOLE O/SIZE FASTENER INSTALLED WITH FREEZE PLUG IAW UPS-HKG-01-00015H AND UPS-HK-01-00016. 2 L 7 4 4F A20WE 2001050100345 20010501 00345 NM 2001 5 1 UPS01435672 1 20010422 A 5320 SUPPORT BOEING 747 747SR46 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 FX - AFT BODY FAIRING SUPPORT SURFACE CORROSION AT STA 1540 FROM LBL 40 - RBL 60 AS MARKED. SUPP ORT REPAIRED AS PER SRM 53-50-04 FIG 2. 2 L 7 4 4F A20WE 2001050100346 20010501 00346 NM 2001 5 1 UPS01435673 1 20010423 A 5320 SUPPORT BOEING 747 747SR46 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 FX - BODY FAIRING SUPPORT SURFACE CORROSION AT LBL 58 FROM STA 1170-1230. LT STA 1170-1230 LBL 58 BODY FAIRING SUPPORT SURFACE REPLACED AS PER SRM 51-40-04 FIG 1. 2 L 7 4 4F A20WE 2001050100347 20010501 00347 NM 2001 5 1 UPS01435674 1 20010423 A 5311 FRAME BOEING 747 747SR46 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 CABIN - FRAME FOUND CRACK AT STA 560 BETWEEN STR 23L TO STR 24L. FRAME REPAIRED AS PER SRM 53-10- 04 FIG 11. 2 L 7 4 4F A20WE 2001050100348 20010501 00348 NM 2001 5 1 UPS01435676 1 20010421 A 5313 STRINGER BOEING 747 747SR46 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 AFT CARGO - BILGE AREA STA 1750 STR 51R SURFACE CORROSION. AFT CARGO - BS 1750-1770 STR 51R REPAIRED AS PER SRM 53-10-03 FIG 8. 2 L 7 4 4F A20WE 2001050100349 20010501 00349 NM 2001 5 1 UPS01435677 1 20010423 A 5310 DOOR FRAME BOEING 747 747SR46 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 M/D - R2 DOOR FWD CUTOUT REVEAL FOUND CRACKED. NR 2 RT DOOR LWR REVEAL AND FRAME INNER CHORD STRA P REPAIRED AS PER SRM 53-10-04 FIG 84. 2 L 7 4 4F A20WE 2001050100350 20010501 00350 NM 2001 5 1 UPS01435678 1 20010421 A 5320 FLOOR SUPPORT BOEING 747 747SR46 NM CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 BULK CARGO COMPT - FLOOR SUPPORT CORROSION REVEALED AT STA 1940, LBL 55 AS MARKED. FLOOR SUPPORT BETWEEN STA 1920 TO STA 1950 LBL 55 REPAIRED AS PER 53-10-07 FIG 20. 2 L 7 4 4F A20WE 2001050100351 20010501 00351 NM 2001 5 1 UPS01435689 1 20010421 A 5240 BEAM BOEING 747 747SR46 NM PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 CRACK REVEALED ON THE FWD BOTTOM OF HORIZONTAL BEAM OF DOOR 4L. 4L DOOR FWD BOTTOM OF HORIZONTAL BEA M REPAIRED AS PER SRM 52-10-02 FIG 10. 2 L 7 4 4F A20WE 2001050100352 20010501 00352 NM 2001 5 1 UPS01435691 1 20010424 A 5320 SUPPORT BOEING 747 747SR46 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 AFT CARGO - STA 1913 BALLMAT SUPPORT SURFACE CORR AT RBL 30, RBL 40 & RBL 60. REPAIR AS PER SRM 51- 40-03 FIG 1. 2 L 7 4 4F A20WE 2001050100353 20010501 00353 NM 2001 5 1 UPS01435692 1 20010423 A 5320 SUPPORT BOEING 747 747SR46 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 FX - BODY FAIRING SUPPORT UPPER & LWR SURFACE CORR AT STA 1480 FROM LBL 55 - RBL 40. STA 1480 LBL 55 - RBL 40 BODY FAIRING SUPPORT REPLACED AS PER SRM 51-10-01 P.8. 2 L 7 4 4F A20WE 2001050100354 20010501 00354 NM 2001 5 1 UPS01435693 1 20010423 A 5320 65B08351U8 FITTING BOEING 747 747SR46 NM PAX DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 M/D - R3 DOOR FWD CUTOUT NR 6 STOP FITTING CRACKED. NR 6 STOP FITTING REPLACED AS PER SRM 51-10-01. ` 2 L 7 4 4F A20WE 2001050100355 20010501 00355 NM 2001 5 1 UPS01435695 1 20010424 A 5312 141U11075 PRESSURE PANEL BOEING 747 747SR46 NM NLG W/W CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 NOSE WHEEL WELL VERTICAL BEAM LT BS 300 FRAME WEB FOUND NR 2 STAND OFF HOLE CRACK (COUNT FROM TOP APP ROX. 1/4 INCH IN LENGTH AT 7 O/C POSN AS MARKED. (LOOKING FWD) VERTICAL BEAM WEB REPLACED IAW BOEING SB 747-53A2293, PR OCEDURE 3 PART IV PER DRAWING 624U0005 SHEET 1 & 13. 2 L 7 4 4F A20WE 2001050100356 20010501 00356 NM 2001 5 1 UPS01435697 1 20010424 A 5320 65B140561 SUPPORT BOEING 747 747SR46 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 FX - STA 1404 LBL 16 - RBL 16 KEEL BEAM PANEL SUPPORT FIND WITH CORRODED. SUPPORT REPLACED AS PER 5 1-10-01. 2 L 7 4 4F A20WE 2001050100357 20010501 00357 NM 2001 5 1 UPS01435698 1 20010421 A 5330 SKIN BOEING 747 747SR46 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 FX - EXTERIOR SKIN STA 2160 STR 46R CORR CRACK REVEALED ***CPCP*** FX - EXTERIOR SKIN AT STA 2160 STR-46R REPAIRED AS PER SRM 53-30-03 FIG 1. 2 L 7 4 4F A20WE 2001050100358 20010501 00358 NM 2001 5 1 UPS01435699 1 20010423 A 5320 65B140581 SUPPORT BOEING 747 747SR46 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 FX - STA 1465 LBL 16 - RBL 16 KEEL BEAM PANEL SUPPORT FOUND WITH CORRODED. ***CPCP*** SUPPORT REP LACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001050100359 20010501 00359 NM 2001 5 1 UPS01435700 1 20010425 A 5310 DOOR FRAME BOEING 747 747SR46 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 CABIN - R5 DOOR FWD LOWER CORNER FOUND CRACKED. R5 DOOR FWD LOWER CORNER REPAIRED AS PER SRM 52-1 0-02 FIG 1B. 2 L 7 4 4F A20WE 2001050100360 20010501 00360 NM 2001 5 1 UPS01435701 1 20010424 A 5220 BEAM BOEING 747 747SR46 NM EMERGENCY DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C6 CRACK REVEALED ON THE FWD BOTTOM OF HORIZONTAL BEAM OF DOOR 2L. 2L DOOR FWD BOTTOM OF HORIZONTAL BEAM REPAIRED AS PER SRM 52-10-02 FIG 10. 2 L 7 4 4F A20WE 2001050100361 20010501 00361 NM 2001 5 1 UPS01435702 1 20010423 A 5315 FLOORBEAM BOEING 747 747SR46 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 M/D - BS 2240 LBL 40-75 FLOORBEAM UPPER SURFACE FOUND CORROSION FLOORBEAM REPAIRED AS PER SRM 53-1 0-07 FIG 9. 2 L 7 4 4F A20WE 2001050100362 20010501 00362 NM 2001 5 1 UPS01435703 1 20010423 A 5320 SUPPORT BOEING 747 747SR46 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C3 FX - STA 1426 LBL 16 - RBL 16 KEEL BEAM PANEL SUPPORT FOUND WITH CORRODED. SUPPORT REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001050100364 20010501 00364 NM 2001 5 1 UPS01635707 1 20010425 A 3350 LIGHT BOEING 767 767300 1385204 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 331UP 27757 INSPECTION TYPE:N/A EMER EXIT LIGHT ON FLIGHT DECK ILLUM WITH OVRHD EMER LIGHTS SW IN AR MED. WOULD NOT EXTINGUISH UNLES S SW IS MOVED TO OFF POSITION. LIGHTI NG LIGHTING WENT OUT DURING CRUISE WITH SW IN ARM. IN DESCENT MALFUN CTION RE-OCCU RED REMOVED AND REPLACED EMERG EXIT LIGHT SW PANEL ASSY CHECKS GOOD 2 L 7 2 4F RT A1NM 2001050100365 20010501 00365 WP 2001 5 1 UPS01835679 1 20010330 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 STA. 920 LONG. 18R EXTERNAL SKIN IS CORRODED BEYOND LIMITS. REPAIRED SKIN I.A.W. 8110-3 APPROVED DH SK 797-908 2 L 7 4 4F RT 4A25 2001050100366 20010501 00366 WP 2001 5 1 UPS01835681 1 20010404 A 5320 FITTING DOUG DC8 DC873F 302199F WP CUSP MEMBRANE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2 CORROSION ON UPPER SURFACE OF CUSP FITTING AT & BETWEEN FS 110 - 1120. REMOVED FITTING INSTALLED NEW FITTING PN 4643162 PO 355728 2 L 7 4 4F RT 4A25 2001050100367 20010501 00367 WP 2001 5 1 UPS01835682 1 20010417 A 5720 FITTING DOUG DC8 DC873F 302199F WP WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2, NR 2 MAIN FUEL TANK STRINGER SPLICE FITTING PN 3704841 IS CRACKED. LOCATED & DRILLED NEW FITTING I AW DC8 SRM 51-1-24 INSTALLED NEW FITT ING IAW DC8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001050100368 20010501 00368 WP 2001 5 1 UPS01835683 1 20010404 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2 AFT CARGO PIT FS 1220 AT LONG 31R INSIDE X SLIDE DOOR AFT TORQUE BOX FITTING IS CORRODED. REMOVED C ORROSION IAW DC8 SRM 51-1-8 FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0 RMVD FITTING IAW DC8 SRM 51-1-21 RCVD LOCATED D RILLED IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001050100369 20010501 00369 WP 2001 5 1 UPS01835684 1 20010423 A 5720 BRACKET DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2 LT WING LE SECTION BETWEEN NR 1 & 2 ENGINE SLOT DOOR ACTUATOR ATTACH BRACKET IS CRACKED APPROX 50 IN CHES FROM OTBD LWR SIDE RMVD OB SECTION OF LT OB SLOT, SETAINER & SEAL FABBED NEW ATTACH BRA CKET FITTING IAW DAC DW G 4770278 INSTALLED NEW ATTACH FITTING REINST ALLED OB SECTION OF OB SLOT, SEAL & RETAINER IAW UPS DC8 MM 2702 270 0 & 5 1-3-0 OPS CHECK GOOD 2 L 7 4 4F RT 4A25 2001050100370 20010501 00370 WP 2001 5 1 UPS01835685 1 20010404 A 5320 SUPPORT DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2 STANTION SUPPORT CRACKED ATTACHED TO FRAME STA 1060 RH SIDE AFT PIT. REMOVED CRACKED STANTION SUPPOR T STRUT IAW DC8 SRM 51-1-20D RCVD NEW SU PPORT PN 3773077-509N W/ PO 355450 LOCATED & DRILLED HOLES IAW DC8 S RM 51-1-24 INSTALLED STANTION IAW DC8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001050200073 20010502 00073 CE 2001 5 2 20010409CW020 1 20010301 A 2435 23080023 STARTER GEN LEAR 35 31 5170530 CE GARRTT TFE731 TFE73123B WP RT ENGINE FAILED B A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 NE 01 202LC 892 147 P99414 AFTER TAKEOFF VIBRATION COMING FROM RIGHT SIDE OF AIRCRAFT. BROUGHT RIGHT ENGINE TO IDLE, NO CHANGE. 2 L 7 2 4F 4 F RT A10CE E6WE 2001050200074 20010502 00074 EU 2001 5 2 GXPA0106 1 20010306 A 2130 CONTROL UNIT AMD FALCON FALCON20 2730103 EU GE CF700 CF700* 30010 NE CABIN PRESSURE MALFUNCTIONED E GXPA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 25 183GA 147 AIRCRAFT RETURNED TO AIRPORT DUE TO PRESSURIZATION PROBLEM. REMOVED AND REPLACED CABIN PRESSURE CONTROLER. 2 L 7 2 4F 4 F RT A7EU E7EA 2001050200075 20010502 00075 EU 2001 5 2 20010411CW002 1 20010326 A 2435 BEARING BRAERO DH125 BAE125800A 1500285 EU GARRTT TFE731 TFE7315R 01518 WP STARTER GEN FAILED E KWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 13 255RB 650 650 258059 P91236 FRONT END BEARING FAILED ON STARTER GENERATOR, IN FLIGHT. 2 L 7 2 4F 4 F RT A3EU E6WE 2001050200076 20010502 00076 NM 2001 5 2 20010411CW003 1 20010319 A 3230 655790142 TRUNNION BOEING 727 727223 1384074 NM RT MLG DAMAGED E AALA K NONE O OTHER IN INSP/MAINT 1 SO 19 705AA 22462 SEVERE DAMAGE TO THE AFT TRUNNION SPUD AREA. 2 L 7 3 4F A3WE 2001050200078 20010502 00078 2001 5 2 DL777010520 4 20010330 A 2330 130902016 CONNECTOR BOEING 777 777232 1385232 NM SEAT 52 ARCED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 862DA 29734 FOUND PLUG J1 CONNECTOR P1 AT SEAT 52AB ARCED. ACTIVATED IFE SYSTEM CLEARED MCO 445269003 REMOVED AND REPLACED AVU AT SE AT 52 A/B-P/N 1301273-11 AND SEAT TO SEAT CABLE P/N 130902-016. 2 L 7 2 4F RT T00001SE 2001050200079 20010502 00079 WP 2001 5 2 0101389156 1 20010416 A 3230 59516395001 BUNGEE CYLINDER DOUG DC9 DC914 3022034 WP NLG FAULTY A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 8915E 45832 ON APPROACH FOR LANDING, THE NOSE LANDING GEAR DID NOT EXTEND NORMALLY. THE MAIN LANDING GEAR OPERATED FINE AND THE HY DRAULIC SYSTEM PRESSURE WAS NORMAL. COMPLIED WITH COM PROCEDURES WITH THE NOSE GEAR EXTENDED. GEAR DOOR OPEN LIGHT WAS OUT OF VIEW AND LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED THE NOSE LANDING GEAR BUNGEE CYLINDER, BUNGEE SPRING, AND THE LANDING GEAR CONTROL VALVE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001050200080 20010502 00080 NE 2001 5 2 0101399140 2 20010411 A 7260 CARBON SEAL DOUG DC9 DC914 3022034 WP PWA JT8 JT8D7 52053 NE GEARBOX LEAKING A NWAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 930RC 45729 57621 AIRCRAFT DIVERTED TO MSP DUE LOSS OF OIL QUANTITY. DURING CRUISE, THE RIGHT ENGINE OIL QUANTITY STEADILY DROPPED FROM 1 6 QTS TO 0 QTS WHILE THE OIL TEMPERATURE AND PRESSURE REMAINED NORMAL. THE ENGINE SHUT DOWN WHEN LOW OIL PRESSURE LIGHT ILLUMINATED BUT WINDMILLED FOR APPROXIMATELY 10 MINUTES WITH ENGINE BELOW 10 PSI AFTER PREVIOUS ENGINE SHUTDOWN. MAINT ENANCE SERVICED RIGHT ENGINE WITH 17 QTS OF OIL. RAN ENGINE WITH OIL COMING OUT OF DRAIN MAST. DISCONNECTED AFT DRAIN LINES FROM MAST AND FOUND OIL COMING FROM THE FUEL PUMP/FUEL CONTROL CARBON SEAL. REPLACED THE FUEL PUMP AND CARBON SEA L. PERFORMED WINDMILL INSPECTION. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F 4 F A6WE E2EA 2001050200081 20010502 00081 NM 2001 5 2 0101406635 1 20010413 A 3350 BATTERY BOEING 747 747227B 1384888 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 635US 21682 DURING LINE CHECK, FOUND ZONE-E EMERGENCY ESCAPE PATH FLOOR LIGHTING INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LI GHT BATTERY. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F A20WE 2001050200082 20010502 00082 NM 2001 5 2 0101416308 1 20010416 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 668US 24223 DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE BETWEEN LAV AT ROW 22HJK AND NR 3 PASSEN GER DOOR AND BETWEEN ROW 25ABC AND PASSENGER DOOR 3L. REPAIRED WIRING AT DOOR 2R AND REPLACED LIGHT ASSEMBLY AT ROW 25A BC. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001050200083 20010502 00083 NM 2001 5 2 0101426635 1 20010419 A 3350 BATTERY PACK BOEING 747 747227B 1384888 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 635US 21682 DURING LINE CHECK, MAINTENANCE FOUND E-ZONE EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. REPLACED THE BATTERY PACK. OPE RATIONAL CHECK NORMAL. 2 L 7 4 4F A20WE 2001050200084 20010502 00084 NM 2001 5 2 CALA0100398 1 20010420 A 3230 S272U8607 FUSE BOEING 737 737824 13844BZ NM NLG WW CONTAMINATED A CALA O OTHER O OTHER LD LANDING 1 SW 09 36247 28807 NOSE GEAR WOULD NOT EXTEND WHEN PUTTING LANDING GEAR DOWN. FOLLOWED QRH PROCEDURE - NOSE GEAR EXTENDED MANUALLY. BLEE D HYDRAULIC RATE FUSE (EXTENSION). AIR INSIDE SYSTEM. REFERENCE TELEGRAPHIC SERVICE LETTER M7200-00-00442. NO EXISTI NG FAULTS ON PSEU. SWUNG GEAR, OPS CHECK OK. 2 L 7 2 4F RT A16WE 2001050200085 20010502 00085 CE 2001 5 2 GLBA2001084 1 20010419 A 2120 1143800595 VALVE BEECH 1900 1900D 1154162 CE RT PRSOV FAILED A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 01 219GL UE219 RIGHT HAND ENVIRO BLEED FAIL ANNUNCIATOR ILLUMINATED ON TAKEOFF.R&R RIGHT HAND PRSOV 2 L 7 2 4T RT A24CE 2001050200086 20010502 00086 WP 2001 5 2 ABXA010168 1 20010420 A 5313 LONGERON DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 LONGERON 6L WAS CRACKED AT THE U-CHANNEL, STA 230. 2 L 7 4 4F 4A25 2001050200087 20010502 00087 WP 2001 5 2 ABXA010169 1 20010419 A 5311 FRAME DOUG DC8 DC863 302198A WP FUSELAGE DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 AFT PIT FLOORBEAM FRAME AT STA 1000 HAD AN ELONGATED HOLE. 2 L 7 4 4F 4A25 2001050200088 20010502 00088 WP 2001 5 2 ABXA010170 1 20010420 A 5313 LONGERON DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 LONGERON CRACKED AT CARGO DOOR ACTUATOR U-CHANNEL. 2 L 7 4 4F 4A25 2001050200089 20010502 00089 WP 2001 5 2 ABXA010171 1 20010420 A 5313 LONGERON DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 LONGERON 4L CRACKED AT CARGO DOOR ACTUATOR U-CHANNEL STA 134. 2 L 7 4 4F 4A25 2001050200090 20010502 00090 WP 2001 5 2 ABXA010172 1 20010403 A 5720 FITTING DOUG DC8 DC863 302198A WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 RIGHT WING JACK POINT CRACKED AT XRS 139. 2 L 7 4 4F 4A25 2001050200091 20010502 00091 WP 2001 5 2 ABXA010173 1 20010408 A 5320 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 RIGHT MAIN LANDING GEAR WHEEL WELL TRAPEZOID FITTING AT STA 860 WAS CRACKED. 2 L 7 4 4F 4A25 2001050200092 20010502 00092 NM 2001 5 2 ZW0A0100601 1 20010419 A 8011 STARTER BOEING 767 76733AER 1385230 NM PWA 4060 PW4060 52119 NE RT ENGINE FAILED A ZW0A E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 CE 13 637TW 25403 4717 DURING ENGINE START GROUND CREW REPORTED RT ENGINE FIRE. CREW SHUT DOWN THE ENGINE AND FIRED BOTH FIRE EXTINGUISHING BO TTLES. ENGINE STARTER REPORTED TO HAVE FAILED RELEASING OIL WHICH CAUGHT ON FIRE, CAUSING CONSIDERABLE DAMAGE TO THE EN GINE AND COWL. CHECK-C 1-17-01 LAX. 2 L 7 2 4F 4 F RT A1NM E24NE 2001050200093 20010502 00093 NE 2001 5 2 ZW0A0100602 2 20010420 A 7261 ENGINE BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE LT ENGINE LEAKING A ZW0A E A ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CR CRUISE 1 CE 13 702TW 28162 4954 THE LEFT ENGINE OIL QUANTITY DECREASED IN FLIGHT. OIL PRESSURE EVENTUALLY DECREASED TO RED LINE. ENGINE WAS SHUT DOWN, AN UNSCHEDULED LANDING MADE AT DTW. CHECK-C 10-17-99 LAX. 2 L 7 2 4F 4 F RT A2NM E17NE 2001050200094 20010502 00094 NM 2001 5 2 ZW0A0100603 1 20010413 A 5751 SKIN BOEING 717 717200 1383700 NM AILERON CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 405TW 405TW DENTS DUE TO HAIL DAMAGE WERE FOUND ON LT AILERON UPPER SURFACE, FWD OF THE INBD TAB, HAD CRACK 1 INCH LONG. REPAIRED P ER SRM 57-00-00 FIG 201, AND COMPUTER BALANCE ACCOMPLISHED. NO CHECK-C. 2 L 7 2 4F TR A6WE 2001050200095 20010502 00095 WP 2001 5 2 ZW0A0100604 1 20010413 A 5751 SKIN DOUG DC9 DC983 3022083 WP AILERON CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9304C 49530 HAIL DAMAGE CAUSED H-SHAPE CRACK IN RT AILERON, 17 INCHES FROM OTBD EDGE AND 3.5 IN FROM THE T/E CRACKS ARE .75 IN LONG. RT AILERON CRACK REPAIRED PER SRM 51-70-1A, NUMBER 11. CHECK-C 2-5-01 JFK. 2 L 7 2 4F RT A6WE 2001050200096 20010502 00096 EU 2001 5 2 C2XA01BT064 1 20010420 A 3350 CM44 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 34820 159 BTV---CO2930, DURING 3A INSPECTION MAINTENANCE FOUND EXTERIOR LEFTHAND FORWARD EMERGENCY LIGHT INOPERATIVE. RELAMPED EX TERIOR LEFTHAND FORWARD EMERGENCY LIGHT. OPS CHECKED GOOD. 2 H 7 2 4T RT A53EU 2001050200097 20010502 00097 WP 2001 5 2 MWEA010608 1 20010419 A 5310 99577397 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 SHEAR TIE CRACKED AT STATION 945 BELOW LONGERON 15 RIGHT. REMOVED DAMAGED SECTION, FABRICATED NEW SECTION AND REPAIR SP LICES. LOCATED, DRILLED, AND INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001050200098 20010502 00098 WP 2001 5 2 MWEA010609 1 20010419 A 5320 99234843 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 CABIN SUBFLOOR BETWEEN CENTERLINE AND RIGHT FLOOR SUPPORT FORWARD OF NR 4 SEAT TRACK HAD AREAS OF CHAFES AND LIGHT CORRO SION. BLENDED, REMOVED CORROSION, FABRICATED, LOCATED, DRILLED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 2001050200099 20010502 00099 WP 2001 5 2 MWEA010610 1 20010419 A 5347 59108205 SEAT TRACK DOUG DC9 DC932 3022066 WP CABIN CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 NR SEAT TRACK HAD SEVERAL AREAS OF MODERATE CORROSION AND BARE METAL AT STATION 200 - 229. REMOVED SEAT TRACK, CUT, FO RMED, LOCATED, DRILLED AND INSTALLED NEW SEAT TRACK AND SPLICE REPAIR. 2 L 7 2 4F A6WE 2001050200100 20010502 00100 WP 2001 5 2 MWEA010611 1 20010419 A 5320 99100787 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 SUBFLOOR AT STATION 218 BETWEEN CENTER LINE AND NR 3 SEAT TRACK HAD AREAS OF MODERATE CORROSION. BLENDED, REMOVED CORRO SION, FABRICATED, LOCATED, DRILLED, AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 2001050200101 20010502 00101 WP 2001 5 2 MWEA010612 1 20010419 A 5311 995774025 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 AT RIGHT KEEL AREA, FUSELAGE FRAME STATION 617 WAS CRACKED AT OUTBOARD ATTACH. REMOVED, LOCATED, DRILLED, AND INSTALLED NEW FRAME. 2 L 7 2 4F A6WE 2001050200102 20010502 00102 WP 2001 5 2 MWEA010613 1 20010419 A 5315 99115451 FLOORBEAM DOUG DC9 DC932 3022066 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 GOUGE ON BOTTOM OF FLOORBEAM AT STATION 408, 2 INCHES RIGHT OF CENTER INTERCOSTAL. BLENDED GOUGE, FABRICATED, LOCATED, DRILLED, AND INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001050200103 20010502 00103 WP 2001 5 2 MWEA010614 1 20010419 A 5320 99101409 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 SUBFLOOR WAS CRACKED AT STATION 218 OUTBOARD OF NR 4 SEAT TRACK NEAR PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR, STOP DRI LLED CRACK, FABRICATED NEW REPAIR DOUBLER, DRILLED AND INSTALLED. 2 L 7 2 4F A6WE 2001050200104 20010502 00104 WP 2001 5 2 MWEA010615 1 20010419 A 5320 99234843 WEB DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 CABIN SUBFLOOR AT STATION 200 BETWEEN SEAT TRACKS 3 AND 4 HAD A DRILL STOP. FABRICATED, DRILLED, INSTALLED REPAIR DOUBL ER. 2 L 7 2 4F A6WE 2001050200105 20010502 00105 WP 2001 5 2 MWEA010616 1 20010419 A 5313 59114279 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 LONGERON 17 LEFT WAS CRACKED AT STATION 980 UPPER AND LOWER ATTACH POINTS. REMOVED DAMAGED SECTION, FABRICATED, DRILLED AND INSTALLED NEW LONGERON. 2 L 7 2 4F A6WE 2001050200106 20010502 00106 WP 2001 5 2 MWEA010617 1 20010419 A 5313 59114279 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 LONGERON 17 RIGHT WAS CRACKED AT STATION 965. REMOVED DAMAGED SECTION, FABRICATED DRILLED, INSTALLED NEW SECTION. 2 L 7 2 4F A6WE 2001050200107 20010502 00107 WP 2001 5 2 MWEA010618 1 20010419 A 5313 59114267 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 LONGERON 13 RIGHT WAS CRACKED AT STATION 965. REMOVED DAMAGED SECTION, FABRICATED, DRILLED AND INSTALLED NEW SECTION. 2 L 7 2 4F A6WE 2001050200108 20010502 00108 WP 2001 5 2 MWEA010619 1 20010419 A 5320 591142745 DOUBLER DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 DOUBLER PLATE WAS CRACKED AT STATION 975 RIGHT LAVATORY AREA ABOVE LONGERON 17 RIGHT. REMOVED DOUBLER, FABRICATED, DRIL LED, AND INSTALLED NEW DOUBLER. 2 L 7 2 4F A6WE 2001050200109 20010502 00109 WP 2001 5 2 MWEA010620 1 20010419 A 5311 99578753 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 DAMAGE ON FRAME RADIUS STATION 207 AFT SIDE LONGERON 17 LEFT. FABRICATED AND INSTALLED REPAIR ANGLES. 2 L 7 2 4F A6WE 2001050200110 20010502 00110 WP 2001 5 2 MWEA010621 1 20010419 A 5311 995821519 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 FRAME CORRODED, STATION 917, LONGERON 30. FOUND CRACK JUST AFT OF OUTBOARD FASTENER HOLE. FABRICATED AND INSTALLED FRA ME SPLICES AND DOUBLERS. 2 L 7 2 4F A6WE 2001050200111 20010502 00111 WP 2001 5 2 MWEA010622 1 20010419 A 5320 99234843 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 FOUND 2 CRACKED NUT PLATE HOLES IN SUBFLOOR BENEATH THE NR 4 SEAT TRACK BETWEEN STATION 200 - 218. FABRICATED AND INSTA LLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001050200112 20010502 00112 WP 2001 5 2 MWEA010623 1 20010419 A 5312 991224345 BULKHEAD DOUG DC9 DC932 3022066 WP FUSELAGE CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 PYLON FORWARD BULKHEAD, AT STATION 965, WEB THAT CONNECTS RIGHT AND LEFT BULKHEADS TOGETHER IS CHAFED IN BOTH CORNERS. FABRICATED AND INSTALLED STACKED ANGLE REPAIR. 2 L 7 2 4F A6WE 2001050200113 20010502 00113 WP 2001 5 2 MWEA010624 1 20010419 A 5310 995823869 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 REPAIR DOUBLER CRACKED ON SHEAR TIE REPAIR AT STATION 980 AND BELOW LONGERON 14 LEFT. REMOVED AND REPLACED SHEAR TIE. FABRICATED AND INSTALLED LONGERON TO FRAME ATTACHMENT ANGLES, SHEAR TIE SPLICE STRAPS, AND RADIUS FILLERS. 2 L 7 2 4F A6WE 2001050200114 20010502 00114 WP 2001 5 2 MWEA010625 1 20010419 A 5310 995823870 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 SHEAR TIE CRACKED AT STATION 980, BELOW LONGERON 14 RIGHT AND ABOVE 16 RIGHT. FABRICATED AND INSTALLED -45 DOUBLER, L-A NGLES, STRAPS, AND RADIUS FILLERS. 2 L 7 2 4F A6WE 2001050200115 20010502 00115 WP 2001 5 2 MWEA010626 1 20010419 A 5310 991224319 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 SHEAR TIE CRACKED AT STATION 965, BETWEEN LONGERON 13 AND 14 RIGHT. FABRICATED AND INSTALLED SHEAR TIE REPAIR. 2 L 7 2 4F A6WE 2001052200111 20010522 00111 SO 2001 5 22 C2XA01BT065 1 20010416 A 3350 20131A BATTERY PACK EMB 145 EMB145 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 13964 145123 EWR--CO4095, CREW REPORTED EMERGENCY BATTERY PACKS INOPERATIVE. MAINTENANCE TROUBLESHOT PROBLEM AND FOUND BATTERY POWER PACKS DEFECTIVE. REMOVED AND REPLACED ALL EMERGENCY LIGHT BATTERY POWER PACKS. OPS CHECKED SYSTEM GOOD. 2 L 7 2 4F RT T00011AT 2001050200116 20010502 00116 SO 2001 5 2 C2XA01BT066 1 20010409 A 3350 66361 CONNECTOR EMB 145 EMB145LR SO CABIN DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14977 145175 YUL---DURING MODIFICATION WORK IN YUL MAINTENANCE FOUND FLOOR PROXIMITY STRIP (EMERGENCY LIGHT TRACK) THREE STRIP CONNEC TORS DAMAGED. REMOVED AND REPLACED EMERGENCY LIGHT TRACK IAW AMM 33-50-12. CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2001050200117 20010502 00117 SO 2001 5 2 C2XA01BT059 1 20010407 A 3222 1170C000001 TORQUE LINK EMB 145 EMB145LR SO NLG DEFECTIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 16976 3976 3976 145171 EWR---CO4361, CREW REPORTED AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. ALSO, HAD EICAS MESSAGE LG AIR/GND FAIL. MA INTENANCE FOUND NOSE LANDING GEAR LEG WOULD NOT FULLY EXTEND CAUSING THE LANDING GEAR NOT TO RETRACT AND THE LG AIR/GND FAILURE MESSAGE ON THE EICAS. REMOVED AND REPLACED NOSE LANDING GEAR LEG IAW EMB145 MM 32-20-01. OPS AND LEAKED CHECKE D GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2001050200118 20010502 00118 NM 2001 5 2 QXEA0100492 1 20010417 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY MALFUNCTIONED A QXEA K NONE N FALSE WARNING CR CRUISE 1 NM 09 356PH 6060 2384 502 PDX - THE MASTER WARNING AND SMOKE DETECTION LIGHTS ILLUMINATED MULTIPLE TIMES DURING FLIGHT. REMOVED AND REPLACED NR 1 SMOKE DETECTOR IN REAR BAGGAGE COMPARTMENT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001050200119 20010502 00119 NM 2001 5 2 QXEA0100493 1 20010418 A 2530 841005 PSEU DHAV DHC8 DHC8102 2809003 NM GALLEY DEFECTIVE A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 831PH 26102 11008 328 SEA - AN ELECTRICAL TYPE SMELL WAS NOTED IN THE GALLEY. FOUND SMELL TO BE FROM A DEFECTIVE PSEU. REMOVED AND REPLACED PSEU. COMPLIED WITH BITE TEST. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001050200120 20010502 00120 NM 2001 5 2 QXEA0100494 1 20010416 A 3610 DUCT DHAV DHC8 DHC8202 2809007 NM BLEED AIR CRACKED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 345PH 476 SEA - STRONG FISH TYPE SMELL IN THROUGHOUT AIRCRAFT. FOUND BLEED AIR DUCTING CRACKED. REMOVED AND REPLACED DUCTS. OPE RATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001050200121 20010502 00121 EU 2001 5 2 QXEA0100495 1 20010417 A 2611 SMOKE WARNING FOKKER F28 F28MK4000 4990810 EU COCKPIT FALSE ACTIVATION A QXEA K NONE N FALSE WARNING NR NOT REPORTED 1 NM 09 491US 11156 SEA - FLIGHT CREW REPORTED INTERMITTENT SMOKE DETECTION AURAL WARNING EMINATING FROM CARGO COMPARTMENT. NO DEFECTS WERE FOUND UPON INSPECTION. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001050200122 20010502 00122 EU 2001 5 2 QXEA0100497 1 20010417 A 3397 WIRE FOKKER F28 F28MK4000 4990810 EU CABIN BROKEN A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 498US 11181 SEA - ESCAPE PATH LIGHTING FOUND INOPERATIVE. FOUND BROKEN WIRE. REPAIRED WITH SPLICE. NO PARTS REPLACED. OPERATIONA L CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001050200123 20010502 00123 EA 2001 5 2 JBXA000268 1 20010422 A 2611 473052 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA CARGO BAY FAULTY A JBXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 05 579ML 7277 CARGO SMOKE INDICATION IN FLIGHT, DECLARED EMERGENCY INTO MIA (FALSE INDICATION). ISSUED MEL FOR CARGO COMPARTMENT EMPT Y FOR FLIGHT FROM MIA - RDU. REMOVED AND REPLACED BOTH CARGO SMOKE DETECTORS, AND BOTH CARGO FIRE BOTTLESIAW CL-65 AMM 26-15-01, AND 26-25-01 RESPECTIVELY. 2 L 7 2 4F RT A21EA 2001050200124 20010502 00124 SO 2001 5 2 C2XA01IA223 1 20010421 A 3350 AD2047 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17728 120182 IAH- DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHTS WERE NOT ILLUMINATED IN THE FRONT PART OF THE CABIN. MAI NTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY BATTERY, PERFORMED AN OPERATIONAL TEST OF THE EMERGENCY LIGHTING. CHEC KED GOOD AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001050200125 20010502 00125 EU 2001 5 2 MALA010404 1 20010407 A 2720 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433XJ 433 DURING 4K INSPECTION IN CWA, AFT RUDDER CABLE OF LT DUAL CIRCUIT I IS CHAFED. MX REPLACED AFT LT CABLE OF CIRCUIT IAW 2 7-21-25. RIGGED CIRCUIT I IAW SFE AMM 27-21-00. REFER TO 409 NR 123628 FOR TRAVEL CHECKS OF RUDDER. 2 L 7 2 4T RT A52EU 2001050200126 20010502 00126 EU 2001 5 2 MALA010405 1 20010408 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433XJ 433 DURING 4K INSPECTION IN CWA, RT CENTER AISLE SEAT TRACK BL 0 BETWEEN STA 632 TO 645 HAS CORROSION. MAINTENANCE COMPLETE D REPAIR IAW EO S53077. 2 L 7 2 4T RT A52EU 2001050200127 20010502 00127 EU 2001 5 2 MALA010406 1 20010408 A 2720 7227105562 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433XJ 433 DURING 4K INSPECTION IN CWA, RHOB CABLE OF RUDDER DUAL CIRCUIT I IS CHAFED. MX INSTALLED RHOB EIE56 DUAL CIRCUIT I CABL E P/N 7227105-562 IAW SF340 AMM 27-21-25. SEE CONTINUATION CARD FOR DETAILS. SEE 409 CARD 123628 FOR RIGGING. 2 L 7 2 4T RT A52EU 2001050200128 20010502 00128 EU 2001 5 2 MALA010407 1 20010409 A 2720 7227105562 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433XJ 433 DURING 4K INSPECTION IN CWA, LHOB CABLE OF RUDDER DUAL CIRCUIT IS CHAFED. MX REPLACED OB RUDDER CABLE LT DUAL CIRCUIT P /N 7227105-562. FOR RIG AND TRAVEL CHECKS SEE 409 NR 123628. 2 L 7 2 4T RT A52EU 2001050200129 20010502 00129 EU 2001 5 2 MALA010408 1 20010409 A 2730 7227105712 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433XJ 433 DURING 4K INSPECTION IN CWA, FWD RHOB ELEVATOR SYSTEM IS CHAFED. MX INSTALLED SERVICEABLE CABLE IN RHOB FWD ELEVATOR P/ N 7227105-712 FOR RIGGING SEE 409 NR 123628. FOR STEERING PLUG INSTALL SEE 409 NR 122727 CONT CARD 35450, DISC 2 CABLE INSTALLED IAW SF340 AMM 27-31-15-4. 2 L 7 2 4T RT A52EU 2001050200130 20010502 00130 EU 2001 5 2 MALA010409 1 20010409 A 2730 7227705644 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433XJ 433 FOUND DURING 4K INSPECTION IN CWA, LHOB ELEVATOR SYSTEM IS CHAFED. MX INSTALLED LHOB ELEVATOR CABLE IAW SF340 AMM 27-31 -15-4, P/N 7227705-644. 2 L 7 2 4T RT A52EU 2001050200131 20010502 00131 EU 2001 5 2 MALA010410 1 20010409 A 2730 7227705644 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433XJ 433 DURING 4K INSPECTION IN CWA, LHIB CABLE OF ELEVATOR SYSTEM IS CHAFED. MX INSTALLED NEW FWD LHIB ELEVATOR CABLE IAW SF34 0AMM 27-31-15-4 P/N 7227705-644, FOR RIG SEE 409 NR 123629, FOR STEERING PLUG INSTALL SEE 409 NR 122727. 2 L 7 2 4T RT A52EU 2001050200132 20010502 00132 EU 2001 5 2 MALA010411 1 20010409 A 2720 7227105582 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433XJ 433 FOUND DURING 4K INSPECTION IN CWA, AFT RUDDER CABLE OF DUAL CIRCUIT I IS CHAFED (RH RUDDER SYSTEM). MX REPLACED AFT RUD DER CABLE OF CIRCUIT I IAW SF3AMM 27-21-25 P/N 7227105-582. 2 L 7 2 4T RT A52EU 2001050200133 20010502 00133 EU 2001 5 2 MALA010412 1 20010410 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433XJ 433 FOUND DURING 4K INSPECTION, LT CENTER AISLE SEAT TRACK LBL 18.3. FROM APPROXIMATELY STA 297 TO 329, HAS CORROSION. MX R EPLACED SEAT TRACK SECTION IAW GEN REPAIR EO S53060 AND SRM 51-00-00. 2 L 7 2 4T RT A52EU 2001050200134 20010502 00134 EU 2001 5 2 MALA010413 1 20010410 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433XJ 433 DURING 4K INSPECTION IN CWA, RT CENTER FLOOR BOARD FLANGE ON SEAT TRACK HAS CORROSION. MAINTENANCE REPLACED SEAT TRACK SECTION FROM STA 297 TO STA 329. MX REPLACED IAW EO53060. 2 L 7 2 4T RT A52EU 2001050200135 20010502 00135 EU 2001 5 2 MALA010414 1 20010411 A 2710 7227105623 CONTROL CABLE SAAB SF340 340B 7860101 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433XJ 433 FOUND DURING 4K INSPECTION, FWD RT IB CABLE OF AILERON SYSTEM IS CHAFED. MX REPLACED FWD RT IB AILERON CABLE P/N 722710 5-623 IAW SAAB AMM 27-11-01 SEE 409 NR 12627 FOR RIGGING. 2 L 7 2 4T RT A52EU 2001050200136 20010502 00136 EU 2001 5 2 MALA010415 1 20010411 A 2710 7227105613 CONTROL CABLE SAAB SF340 340B 7860101 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433XJ 433 FOUND DURING 4K INSPECTION IN CWA, FWD LHOB CABLE IS CHAFED. MX REPLACED FWD LHOB AILERON CABLE P/N 7227105-613 IAW SAA B AMM 27-11-01. SEE 409 123627 FOR RIGGING. 2 L 7 2 4T RT A52EU 2001050200137 20010502 00137 EU 2001 5 2 MALA010416 1 20010411 A 2730 7227105644 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433XJ 433 FOUND DURING 4K INSPECTION IN CWA, FWD RHIB CABLE OF ELEVATOR SYSTEM IS CHAFED. MX INSTALLED FWD RHIB ELEVATOR CABLE P/ N 7227105-644 IAW AMM 27-31-15, SEE CONT CARD 035450 FOR DETAILS. 2 L 7 2 4T RT A52EU 2001050200138 20010502 00138 EU 2001 5 2 MALA010417 1 20010411 A 2710 7227105614 CONTROL CABLE SAAB SF340 340B 7860101 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433XJ 433 FOUND DURING 4K INSPECTION LHIB FWD CABLE OF AILERON SYSTEM IS CHAFED. MX REPLACED LHIB FWD AILERON CABLE P/N 7227105-6 14 IAW SAAB AMM 27-11-01. SEE 409 NR 123627 FOR RIGGING. 2 L 7 2 4T RT A52EU 2001050200139 20010502 00139 EU 2001 5 2 MALA010418 1 20010411 A 2730 7227105712 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433XJ 433 FOUND DURING 4K INSPECTION IN CWA, FWD LHOB CABLE OF ELEVATOR SYSTEM IS CHAFED. MX REPLACED FWD LHOB ELEVATOR FUSELAGE CABLE P/N 7227105-712 IAW SF340AMM 27-31-15-4, FOR RIGGING SEE 409 CARD NR 123629, FOR STEERING PLUG INSTALL SEE 409 NR 122727. 2 L 7 2 4T RT A52EU 2001050200140 20010502 00140 2001 5 2 HNAA0100027 4 20010421 A 3425 7003360941 COMPUTER DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A HNAA A UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 07 917HA 33055 26 075 IN FLIGHT, NR 2 AHRS FLAGGED AND GOR ELECTRICAL SMELL IN COCKPIT AND CABIN. REPLACED 2 AHRS UNIT. 2 H 7 2 4T RT A13NM 2001050200141 20010502 00141 WP 2001 5 2 ABXA010174 1 20010408 A 5312 BULKHEAD DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 THE RIGHT MAIN LANDING GEAR WHEEL WELL FORWARD OUTBOARD LOWER BULKHEAD PANEL WAS CRACKED. 2 L 7 4 4F 4A25 2001050200142 20010502 00142 WP 2001 5 2 ABXA010175 1 20010409 A 5320 INTERCOSTAL DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 INTERCOSTAL CRACKED AT FS 975 AT LONGERON 28R. 2 L 7 4 4F 4A25 2001050200143 20010502 00143 WP 2001 5 2 ABXA010176 1 20010409 A 5320 INTERCOSTAL DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 INTERCOSTAL AT LONGERON 25R FS 960 IN THE RIGHT MAIN LANDING GEAR WHEEL WELL IS CRACKED. 2 L 7 4 4F 4A25 2001050200144 20010502 00144 WP 2001 5 2 ABXA010177 1 20010412 A 5320 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 LEFT FRAME FITTING AT FS 700 BELOW LONGERON L21 WAS CRACKED. 2 L 7 4 4F 4A25 2001050200145 20010502 00145 WP 2001 5 2 ABXA010178 1 20010414 A 5320 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 BATH TUB FITTING CRACKED IN FORWARD CARGO PIT AT FS 300 L27 - L28. 2 L 7 4 4F 4A25 2001050200146 20010502 00146 WP 2001 5 2 ABXA010179 1 20010417 A 5320 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 Z-FITTING CRACKED IN AFT LOWER CARGO BAY AT FS 1680 FROM L34R TO L35R. 2 L 7 4 4F 4A25 2001050200147 20010502 00147 WP 2001 5 2 ABXA010180 1 20010417 A 5320 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 Z-FITTING CRACKED AT STA 1200 LONGERON 33R-34R. 2 L 7 4 4F 4A25 2001050200148 20010502 00148 WP 2001 5 2 ABXA010181 1 20010420 A 5311 564024027 FRAME DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 FRAME CRACKED COMPLETELY THROUGH AT FUSELAGE STA 1620 LONGERON 24L. 2 L 7 4 4F 4A25 2001050200149 20010502 00149 NM 2001 5 2 QXEA0100449 1 20010403 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- RIGHT OUTBOARD SEAT TRACK HAS MILD CORROSION AT STATION 539. REPAIRED IAW DHC-8 SRM 51-20-36 AND 51-20-16. 2 H 7 2 4T RT A13NM 2001050200150 20010502 00150 NM 2001 5 2 QXEA0100450 1 20010403 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- RIGHT OUTBOARD SEAT TRACK HAS MILD CORROSION AT STATION 521. REPAIRED IAW DHC-8 SRM 51-20-36, 51-20-16 AND RD 8-53 -1342. 2 H 7 2 4T RT A13NM 2001050200151 20010502 00151 NM 2001 5 2 QXEA0100451 1 20010408 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- RIGHT OUTBOARD SEAT TRACK HAS PITTING CORROSION AT STATION 436.500. REPAIRED IAW DHC-8 RD 8-53-1342 AND HORIZON AI R EA 2-53-261. 2 H 7 2 4T RT A13NM 2001050200152 20010502 00152 NM 2001 5 2 QXEA0100452 1 20010408 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- RIGHT OUTBOARD SEAT TRACK HAS CORROSION AT STATION 376.110. REPAIRED IAW DHC-8 RD 8-53-1342 AND HORIZON AIR EA 2-5 3-261. 2 H 7 2 4T RT A13NM 2001050200153 20010502 00153 NM 2001 5 2 QXEA0100453 1 20010408 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- RIGHT HAND OUTBOARD SEAT TRACK HAS PITTING CORROSION AT STATION 342.300. REPAIRED IAW DHC-8 SRM 51-20-16, RD 8-53- 1342 AND HORIZON AIR EA 2-53-261. 2 H 7 2 4T RT A13NM 2001050200154 20010502 00154 NM 2001 5 2 QXEA0100454 1 20010408 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- RIGHT HAND OUTBOARD SEAT TRACK HAS PITTING CORROSION AT STATION 366.050. REPAIRED IAW DHC-8 SRM 51-20-16, RD 8-53- 1342 AND HORIZON AIR EA 2-53-261. 2 H 7 2 4T RT A13NM 2001050200155 20010502 00155 NM 2001 5 2 QXEA0100455 1 20010402 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- RIGHT HAND CENTER SEAT TRACK AT STATION 531.500 HAS LIGHT PITTING CORROSION. REPAIRED IAW DHC-8 RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001050200156 20010502 00156 NM 2001 5 2 QXEA0100456 1 20010402 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- RIGHT HAND CENTER SEAT TRACK AT STATION 510.000 TO 521.000 HAS LIGHT PITTING CORROSION. REPAIRED IAW DHC-8 RD 8-53 -1342. 2 H 7 2 4T RT A13NM 2001050200157 20010502 00157 NM 2001 5 2 QXEA0100457 1 20010402 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- RIGHT HAND CENTER SEAT TRACK AT STATION 487.500 HAS LIGHT PITTING CORROSION. REPAIRED IAW DHC-8 RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001050200158 20010502 00158 NM 2001 5 2 QXEA0100458 1 20010402 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- RIGHT HAND CENTER SEAT TRACK AT STATION 467.00 HAS LIGHT PITTING CORROSION. REPAIRED IAW DHC-8 RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001050200159 20010502 00159 NM 2001 5 2 QXEA0100459 1 20010402 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- RIGHT HAND CENTER SEAT TRACK AT STATION 424.124 HAS A GOUGE AND IS MISSING PAINT. REPAIRED IAW DHC-8 RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001050200160 20010502 00160 NM 2001 5 2 QXEA0100460 1 20010404 A 5310 DOOR FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- RIGHT HAND EMERGENCY EXIT FRAME HAS POWDER CORROSION ON BOTTOM FRAME AT STATION 242.200. REPAIRED IAW SRM 53-00-16 . 2 H 7 2 4T RT A13NM 2001050200161 20010502 00161 NM 2001 5 2 QXEA0100461 1 20010404 A 5310 DOOR FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- RIGHT HAND EMERGENCY EXIT FRAME HAS POWDER CORROSION ON BOTTOM FRAME AT STATION 234.500. ALODINED AND PRIMED AREA. 2 H 7 2 4T RT A13NM 2001050200162 20010502 00162 NM 2001 5 2 QXEA0100462 1 20010404 A 5310 DOOR FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- RIGHT HAND EMERGENCY EXIT FRAME HAS POWDER CORROSION ON BOTTOM FRAME AT STATION 222.700. ALODINED AND PRIMED AREAS . 2 H 7 2 4T RT A13NM 2001050200163 20010502 00163 NM 2001 5 2 QXEA0100463 1 20010408 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- DUE TO CORROSION AT STATION 333.3 AND STATION 355.950, REPLACE RIGHT CENTER FORWARD SEAT TRACK. REPAIRED IAW DHC-8 SRM 51-40-00, 51-40-11 AND RD 8-53-4472. 2 H 7 2 4T RT A13NM 2001050200164 20010502 00164 NM 2001 5 2 QXEA0100464 1 20010406 A 5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- CARGO BAY CENTER FLOORBOARD AFT SUPPORT BRACKET IS CORRODED AROUND NUT PLATE AND SUPPORT BRACKET AT STATION X600.00 . REPAIRED IAW DHC-8 SRM 51-40-11 AND 51-20-16. 2 H 7 2 4T RT A13NM 2001050200165 20010502 00165 NM 2001 5 2 QXEA0100465 1 20010403 A 5347 CARGO TRACK DHAV DHC8 DHC8202 2809007 NM CARGO BAY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- CARGO BAY RIGHT HAND INBOARD SEAT TRACK AT STATION X564.500 TO X600.00 INBOARD AND OUTBOARD CHANNELS HAVE LIGHT SUR FACE CORROSION. REPAIRED IAW DHC-8 SRM 51-20-36 AND RD 8-53-284. 2 H 7 2 4T RT A13NM 2001050200166 20010502 00166 NM 2001 5 2 QXEA0100466 1 20010408 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- LEFT HAND OUTBOARD SEAT TRACK HAS SMALL NICKS/GOUGES ON TOP FLANGE 3 INCHES FORWARD OF STATION X270.500. REPAIRED IAW SRM 51-20-16 AND HORIZON AIR EA 2-53-262. 2 H 7 2 4T RT A13NM 2001050200167 20010502 00167 NM 2001 5 2 QXEA0100467 1 20010408 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- LEFT HAND OUTBOARD SEAT TRACK HAS SMALL NICKS/GOUGES ON THE TOP FLANGE 5 INCHES AFT OF STATION X291.400. REPAIRED IAW DHC-8 SRM 51-20-16 AND HORIZON AIR EA 2-53-262. 2 H 7 2 4T RT A13NM 2001050200168 20010502 00168 NM 2001 5 2 QXEA0100468 1 20010408 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- LEFT HAND OUTBOARD SEAT TRACK HAS AN AREA 3 INCHES LONG WITH SMALL NICKS/GOUGES AT 1 INCH FORWARD STATION X312.350 ON TOP FLANGE. REPAIRED IAW DHC-8 SRM 51-20-16 AND HORIZON AIR EA 2-53-262. 2 H 7 2 4T RT A13NM 2001050200169 20010502 00169 NM 2001 5 2 QXEA0100469 1 20010408 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- SMALL NICKS/GOUGES ON LEFT HAND OUTBOARD SEAT TRACK TOP FLANGE AT 5.5 INCHES FORWARD STATION X333.300. REPAIRED IA W DHC-8 SRM 51-20-16 AND HORIZON AIR EA 2-53-262. 2 H 7 2 4T RT A13NM 2001050200170 20010502 00170 NM 2001 5 2 QXEA0100470 1 20010408 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- SMALL NICKS/GOUGES ON LEFT HAND OUTBOARD SEAT TRACK TOP FLANGE AT STATION X342.300. REPAIRED IAW DHC-8 SRM 51-20-1 6 AND HORIZON AIR EA 2-53-262. 2 H 7 2 4T RT A13NM 2001050200171 20010502 00171 NM 2001 5 2 QXEA0100471 1 20010408 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- LEFT HAND OUTBOARD SEAT TRACK HAS SMALL CHAFE ON TOP FLANGE 7.5 INCHES AFT OF STATION X354.250. REPAIRED IAW DHC-8 SRM 51-20-16 AND HORIZON AIR EA 2-53-262. 2 H 7 2 4T RT A13NM 2001050200172 20010502 00172 NM 2001 5 2 QXEA0100472 1 20010408 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- LEFT HAND OUTBOARD SEAT TRACK HAS SMALL AREA WITH A GOUGE ON TOP FLANGE 1.5 INCHES AFT STATION X405.737. REPAIRED IAW DHC-8 SRM 51-20-16 AND HORIZON AIR EA 2-53-262. 2 H 7 2 4T RT A13NM 2001050200173 20010502 00173 NM 2001 5 2 QXEA0100473 1 20010408 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- SMALL NICKS/GOUGES IN TOP FLANGE OF LEFT HAND OUTBOARD SEAT TRACK AT STATION X501.00. REPAIRED IAW DHC-8 SRM 51-20 -16 AND HORIZON AIR EA 2-53-262. 2 H 7 2 4T RT A13NM 2001050200174 20010502 00174 NM 2001 5 2 QXEA0100474 1 20010403 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- SMALL AREA OF LIGHT FRETTING IN TOP FLANGE OF LEFT HAND OUTBOARD SEAT TRACK 6.5 INCHES AFT OF STATION X510.00. REP AIRED IAW DHC-8 SRM 51-20-36 AND RD 8-53-3644. 2 H 7 2 4T RT A13NM 2001050200175 20010502 00175 NM 2001 5 2 QXEA0100475 1 20010405 A 5320 SILL DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- MAIN CABIN DOOR SILL ON AIRFRAME FLOOR ATTACH BOLT HOLES HAVE EVIDENCE OF LIGHT CORROSION. REPAIRED IAW DHC-8 SRM 51-10-00, 51-40-11, 51-20-36, 51-00-04 AND 51-00-06. 2 H 7 2 4T RT A13NM 2001050200176 20010502 00176 NM 2001 5 2 QXEA0100476 1 20010405 A 5320 NUT PLATE DHAV DHC8 DHC8202 2809007 NM FRAME CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- NUT PLATE HAS EVIDENCE OF CORROSION AT OUTBOARD FRAME 252.700 ON UNDER SIDE OF FRAME WHERE THE ENTRY FLOOR PANEL AT TACHES TO FRAME. REPAIRED IAW DHC-8 SRM 51-10-00, 51-00-06, 51-00-04, 51-20-16, 51-20-36 AND 51-40-11. 2 H 7 2 4T RT A13NM 2001050200177 20010502 00177 NM 2001 5 2 QXEA0100477 1 20010410 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- DUE TO CORROSION ON OUTBOARD FLOOR SUPPORT FLANGE FOR INBOARD EDGE OF PANEL 131DZ, REPLACED LEFT HAND INBOARD FORWA RD SEAT TRACK. REPAIRED IAW DHC-8 SRM 51-40-11, 51-40-00 AND RD 8-53-4472. 2 H 7 2 4T RT A13NM 2001050200178 20010502 00178 NM 2001 5 2 QXEA0100478 1 20010410 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- DUE TO PITTING CORROSION ON INBOARD FLOOR SUPPORT FLANGE AT STATION X488.500, REPLACE LEFT HAND INBOARD AFT SEAT TR ACK. REPAIRED IAW DHC-8 SRM 51-40-00, 51-40-11 AND RD 8-53-4472. 2 H 7 2 4T RT A13NM 2001050200179 20010502 00179 NM 2001 5 2 QXEA0100480 1 20010407 A 5310 STOP FITTING DHAV DHC8 DHC8202 2809007 NM CARGO BAY GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- CARGO DOOR BOTH UPPER DOOR STOPS ON APERTURE HAS GOUGES ON DOOR FRAME. REPAIRED IAW HORIZON AIR EA 2-53-264. 2 H 7 2 4T RT A13NM 2001050200180 20010502 00180 NM 2001 5 2 QXEA0100481 1 20010404 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- CARGO DOOR UPPER OUTER SKIN IS GOUGED IN FIVE SPOTS. REPAIRED IAW DHC-8 SRM 51-00-06, 51-00-04 AND HORIZON AIR EA 2-52-89. 2 H 7 2 4T RT A13NM 2001050200181 20010502 00181 NM 2001 5 2 QXEA0100482 1 20010405 A 5511 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- FRAME FLANGE IS CRACKED .5 INCH AT THE INTERSECTION OF FRAME 4 AND STRINGER 4P. REPAIRED IAW DHC-8 RD 8-55-199. 2 H 7 2 4T RT A13NM 2001050200182 20010502 00182 NM 2001 5 2 QXEA0100483 1 20010406 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- FRAME FLANGE IS CRACKED .3 INCH IN THE INTERSECTION OF FRAME 4 AND STRINGER 4S. REPAIRED IAW DHC-8 SRM 51-00-06 AN D RD 8-55-199. 2 H 7 2 4T RT A13NM 2001050200183 20010502 00183 NM 2001 5 2 QXEA0100484 1 20010409 A 7110 RIB DHAV DHC8 DHC8202 2809007 NM COWLING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- ENGINE PANEL 424AR RIB IS CHAFED. REPAIRED IAW HORIZON AIR EA 2-71-128. 2 H 7 2 4T RT A13NM 2001050200184 20010502 00184 NM 2001 5 2 QXEA0100485 1 20010405 A 5720 ATTACH ANGLE DHAV DHC8 DHC8202 2809007 NM LT WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- LEFT HAND WING STATION YW171.40 FORWARD SURFACE OF FRONT SPAR HAS GOUGE WORK ON ATTACHING ANGLE TO NACELLE. REPAIR ED IAW DHC-8 SRM 51-20-00, 51-20-11, 51-00-06, 51-20-16 AND 51-20-36. 2 H 7 2 4T RT A13NM 2001050200185 20010502 00185 NM 2001 5 2 QXEA0100486 1 20010407 A 5720 SUPPORT DHAV DHC8 DHC8202 2809007 NM LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- LEFT HAND WING TRAILING EDGE SUPPORT ANGLE, STATION YW175.0 HAS CHAFE DAMAGE. REPAIRED IAW HORIZON AIR EA 2-57-91. 2 H 7 2 4T RT A13NM 2001050200186 20010502 00186 NM 2001 5 2 QXEA0100487 1 20010406 A 5753 SKIN DHAV DHC8 DHC8202 2809007 NM LT FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- LEFT HAND OUTBOARD FLAP UPPER SKIN, STATION YW175.0 HAS CHAFE DAMAGE. REPAIRED IAW DHC-8 SRM 51-00-06, 51-20-16 AN D RD 8-57-1022. 2 H 7 2 4T RT A13NM 2001050200187 20010502 00187 NM 2001 5 2 QXEA0100488 1 20010407 A 5720 SUPPORT DHAV DHC8 DHC8202 2809007 NM RT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- RIGHT HAND WING TRAILING EDGE SUPPORT ANGLE, STATION YW175.0 HAS CHAFE DAMAGE. REPAIRED IAW HORIZON AIR EA 2-57-91 . 2 H 7 2 4T RT A13NM 2001050200188 20010502 00188 NM 2001 5 2 QXEA0100489 1 20010406 A 5753 SKIN DHAV DHC8 DHC8202 2809007 NM RT FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- RIGHT HAND OUTBOARD FLAP UPPER SKIN, STATION YW175.0 HAS CHAFE DAMAGE. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-57 -1022. 2 H 7 2 4T RT A13NM 2001050200189 20010502 00189 NM 2001 5 2 QXEA0100490 1 20010405 A 5730 PANEL DHAV DHC8 DHC8202 2809007 NM RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- RIGHT WING PANELS 623AT SCREW HOLES ARE CORRODED. REPAIRED IAW DHC-8 SRM 51-20-26, 51-20-16 AND RD 8-57-1420. 2 H 7 2 4T RT A13NM 2001050200190 20010502 00190 NM 2001 5 2 QXEA0100491 1 20010405 A 3213 ARM DHAV DHC8 DHC8202 2809007 NM NLG STRUT GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX- NOSE LANDING GEAR STRUT TRAILING ARM HAS GOUGES AND SCRATCHES ON UPPER FORWARD SECTION FROM TOOLBAR. REPAIRED IAW DHC-8 SRM 32-20-01 AND RD 8-32-289. 2 H 7 2 4T RT A13NM 2001050200191 20010502 00191 NM 2001 5 2 PCAA0104030 1 20010419 A 2720 82710038101 FITTING DHAV DHC8 DHC8102 2809003 NM COCKPIT CRACKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 841EX 249 MDT- DURING ROUTINE MAINTENANCE VISIT AN INSPECTION OF RUDDER PEDAL ADJUSTMENT FITTING PER ALERT SERVICE BULLETIN A8-27- 91 REVEALED THE CAPTAINS FITTING WAS CRACKED. FITTING WAS REPLACED IN ACCORDANCE WITH DEHAVILLAND MAINTENANCE MANUAL 27 -20-00. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001050200192 20010502 00192 SO 2001 5 2 COMA0110082 1 20010418 A 5713 12016085001 STRINGER EMB 120 EMB120RT SO LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING INTERNAL INVESTIGATION OF A CRACK IN LEFT WING STRINGER NR 8, STRINGER NR 10 WAS ALSO FOUND TO BE CRACKED 6 INCHE S OUTBOARD OF RIB NR 8. THE STRINGER WAS REPAIRED AT THIS TIME PER AERODESIGN REPORT NR 3949-1, REV IR 3/27/01. OK FOR SERVICE. 2 L 7 2 4T RT A31SO 2001050200193 20010502 00193 SO 2001 5 2 COMA0110083 1 20010418 A 5713 12016079001 STRINGER EMB 120 EMB120RT SO LT WING CRACKED A COMA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING C-CHECK TASK 5720-522-02E ON 3/23/2001, TWO RIVETS WERE FOUND LEAKING FUEL ON THE LEFT WING LOWER SKIN NEAR RIB N R 8. INTERNAL INVESTIGATION FOUND STRINGER NR 8 TO BE CRACKED 6 INCHES INBOARD OF RIB NR 8. EMBRAER GAVE COMAIR APPROV AL TO OPERATE THE AIRCRAFT FOR 100 HOURS PER FAX GST-0936-01. THE STRINGER WAS REPAIRED AT THIS TIME PER AERODESIGN REP ORT NR 3949-1, REV IR 3/27/01. OK FOR SERVICE. 2 L 7 2 4T RT A31SO 2001050200194 20010502 00194 SO 2001 5 2 COMA0110084 1 20010418 A 5210 12026545001 FITTING EMB 120 EMB120RT SO PAX DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 811-02Z, THE PASSENGER DOOR FORWARD LOWER STRUCTURAL CONNECTING FITTING WAS FOUND TO BE CRACKED. T HE FITTING WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200195 20010502 00195 SO 2001 5 2 COMA0110085 1 20010418 A 5210 12021068002 CHANNEL EMB 120 EMB120RT SO PAX DOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2 C-CHECK TASK 811-02Z, THE PASSENGER DOOR FORWARD VERTICAL CHANNEL WAS FOUND TO BE CORRODED. THE CHANNEL WAS RE PLACED PER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200196 20010502 00196 NM 2001 5 2 CALA0100400 1 20010421 A 5522 65C2574683 SKIN BOEING 737 7373T0 1384582 NM ELEVATOR DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 LEFT ELEVATOR UPPER SURFACE HAS SMALL DAMAGED AREA (.25 INCH HOLE). INSTALLED COMPOSITE REPAIR PER EC/RA 5523-01025 AND SRM 51-70-17. CALCULATED WEIGHT AND BALANCE, NO WEIGHTS ADDED. 2 L 7 2 4F RT A16WE 2001050200197 20010502 00197 NM 2001 5 2 CALA0100401 1 20010421 A 5330 6518420 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 61304 23355 PILOTS OUTBOARD WINDOW POST CRACKED AT TOP OUTBOARD CORNER (.75 INCH). INSTALLED REPAIR DOUBLER ON PST PER SRM 53-10-01 FIG 210. 2 L 7 2 4F RT A16WE 2001050200198 20010502 00198 NM 2001 5 2 CALA0100402 1 20010423 A 5414 311A1459 ACCESS PANEL BOEING 737 7373T0 1384582 NM LT PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 61304 23355 LEFT ENGINE PYLON UPPER OUTBOARD ACCESS PANEL CRACKED AT CUTOUT (.75 INCH). STOP DRILLED CRACK AND INSTALLED A REPAIR D OUBLER PER EC/RA 5430C01230. 2 L 7 2 4F RT A16WE 2001050200199 20010502 00199 WP 2001 5 2 CALA0100403 1 20010423 A 5320 602820415 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 AFT PIT FLOORBOARD SUPPORT IS CORRODED AT STATION 1193 - 1212 ABOVE THE TORQUE BOX WEB UPPER AND LOWER SIDES. REMOVED F LOOR SUPPORT. FABRICATED AND INSTALLED NEW SUPPORT PER SRM 51-10-4. TREATED AND PRIMED PER SRM 51-30-2 AND 3. 2 L 7 2 4F A6WE 2001050200200 20010502 00200 WP 2001 5 2 CALA0100404 1 20010423 A 5320 BRACKET DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 AFT PIT AFT TORQUE BOX WEB ATTACH BRACKET CORRODED. REMOVED, FABRICATED, AND INSTALLED NEW ATTACH BRACKET PER SRM 51-30 -2, 51-10-4, AND 51-10-3 AND 5. 2 L 7 2 4F A6WE 2001050200201 20010502 00201 WP 2001 5 2 CALA0100405 1 20010421 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 TAIL COMPARTMENT SHEAR TIE CRACKED AT STATION 1418 AND LONGERON 1. REMOVED SHEAR TIE, FABRICATED AND INSTALLED A SPLICE . TREATED AND PRIMED SHEAR TIE AND INSTALLED PER SRM 51-10-4, 53-03 FIG 3, 51-10-3, AND 51-30-5. 2 L 7 2 4F A6WE 2001050200202 20010502 00202 WP 2001 5 2 CALA0100406 1 20010421 A 5320 J0602283 PAN DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 FOWARD CARGO PIT DOOR CUT-OUT LOWER PAN CORRODED. REMOVED AND REPLACED PAN PER SRM 53-05 FIG 44, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 2001050200203 20010502 00203 WP 2001 5 2 CALA0100407 1 20010421 A 5230 STIFFENER DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 FORWARD CARGO DOOR AFT LOWER INNER STRUCTURE STIFFENER CRACKED (1 INCH). REMOVED DAMAGED STIFFENER. FABRICATED AND INS TALLED NEW STIFFENER PER SRM 51-30-2, 51-10-4, 51-30-5 AND 51-10-3. 2 L 7 2 4F A6WE 2001050200204 20010502 00204 WP 2001 5 2 CALA0100408 1 20010421 A 5230 BRACKET DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 FORWARD CARGO DOOR AFT LOWER CENTER INNER BRACKET IS CRACKED (1 INCH). REMOVED BRACKET. FABRICATED AND INSTALLED NEW B RACKET PER SRM 51-30-5, 51-10-4 AND 51-10-3. 2 L 7 2 4F A6WE 2001050200205 20010502 00205 WP 2001 5 2 CALA0100409 1 20010421 A 5230 BRACKET DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 FORWARD CARGO DOOR FORWARD LOWER INNER STRUCTURE BRACKET CRACKED (1 INCH). REMOVED BRACKET. FABRICATED NEW BRACKET AND ANGLE, INSTALLED PER SRM 51-30-2, 51-10-3, AND 51-30-5. 2 L 7 2 4F A6WE 2001050200206 20010502 00206 WP 2001 5 2 CALA0100410 1 20010421 A 5320 609530 SUPPORT FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 AFT ACCESSORY COMPARTMENT RIGHT LOWER END FS 1485 AND BELOW AFT STAIR TORQUE TUBE SUPPORT IS CRACKED. REMOVED AND REPLA CED SUPPORT FITTING PER SRM 51-30-2, 51-30-5, 51-10-4, 51-10-3, AND 51-30-1 AND 5. 2 L 7 2 4F A6WE 2001050200207 20010502 00207 WP 2001 5 2 CALA0100411 1 20010421 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 AFT CARGO TORQUE WEB AFT OF DOOR CUTOUT FS 1215 HAS A HOLE PUNCTURED IN THE WEB. REMOVED AND REPLACED DAMAGED TORQUE WE B PER SRM 51-30-5, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 2001050200208 20010502 00208 WP 2001 5 2 CALA0100412 1 20010420 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 FLOORBEAM CORRODED AT AND UNDER NUT PLATE LOCATIONS AT STATION 1322 AND LBL 0 - LBL 54. REMOVED NUT PLATES AND CUT OUT DAMAGED AREAS. INSTALLED REPAIR ANGLES AND FILLERS PER SRM 51-30-2, 53-01 FIG 1, 53-05 FIG 204, 51-10-3, AND 53-05 FIG 202. 2 L 7 2 4F A6WE 2001050200209 20010502 00209 WP 2001 5 2 CALA0100413 1 20010420 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 MID CARGO THRESHOLD SUPPORT IS CORRODED. REMOVED DAMEGED SUPPORT. FABRICATED AND INSTALLED NEW SUPPORT PER SRM 51-30-1 , 51-10-4, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 2001050200210 20010502 00210 WP 2001 5 2 CALA0100414 1 20010420 A 5230 SKIN DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 FORWARD CARGO DOOR EXTERNAL SKIN CRACKED AT LOWER FORWARD END (.5 INCH). STOP DRILLED CRACK. FABRICATED AND INSTALLED A REPAIR DOUBLER PER SRM 51-10-4, 51-30-3 AND 51-30-2. 2 L 7 2 4F A6WE 2001050200211 20010502 00211 SO 2001 5 2 COMA0110086 1 20010418 A 5210 12028448001 ATTACH ANGLE EMB 120 EMB120RT SO PAX DOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 811-02Z, THE PASSENGER DOOR FORWARD LOWER ATTACHING ANGLE FOR THE VERTICAL AND LONGITUDINAL CHANNEL S WAS FOUND TO BE CORRODED. THE ANGLE WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200212 20010502 00212 SO 2001 5 2 COMA0110087 1 20010418 A 5210 12039384002 CHANNEL EMB 120 EMB120RT SO PAX DOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 811-02Z, THE PASSENGER DOOR FORWARD LOWER VERTICAL CHANNEL WAS FOUND TO BE CORRODED. THE CHANNEL W AS REPLACED PER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200213 20010502 00213 SO 2001 5 2 COMA0110088 1 20010418 A 5315 12006962001 FLOORBEAM EMB 120 EMB120RT SO FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 131-01Z, THE FUSELAGE LEFT FORWARD FLOOR SUPPORTING T-SECTION AT FRAME NR 16, WAS FOUND TO BE CRACK ED. THE T-SECTION WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200214 20010502 00214 SO 2001 5 2 COMA0110089 1 20010418 A 5320 12004733001 ANGLE EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 131/132-01Z, THE FUSELAGE FORWARD FLOOR SUPPORTING Z-SECTION AT FRAME 13 WAS FOUND TO BE CORRODED. THE Z-SECTION WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200215 20010502 00215 SO 2001 5 2 COMA0110090 1 20010418 A 5210 12026563601 DOOR FRAME EMB 120 EMB120RT 3260202 SO PAX DOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 811-02Z, THE PASSENGER DOOR LOWER LONGITUDINAL FRAME, WAS FOUND TO BE CORRODED. THE FRAME WAS REPL ACED PER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200216 20010502 00216 SO 2001 5 2 COMA0110091 1 20010418 A 5320 12004149002 CROSSBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 151-01Z, THE LEFT FLOOR SUPPORT CROSSBEAM AT FRAME 36, INSIDE THE CABIN, WAS FOUND TO BE CORRODED. THE CROSSBEAM WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200217 20010502 00217 SO 2001 5 2 COMA0110092 1 20010418 A 5315 12007089603 FLOORBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 7134 120267 DURING 2C-CHECK TASK 131-01Z, THE FORWARD LEFT FLOOR SUPPORT T-SECTION AT FRAME 16 INSIDE THE CABIN ,WAS FOUND TO BE COR RODED. THE T-SECTION WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200218 20010502 00218 SO 2001 5 2 COMA0110093 1 20010418 A 5320 12043600001 SUPPORT EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 242-01Z, THE RIGHT SIDEWALL SEAT TRACK SUPPORT INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SUPP ORT WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200219 20010502 00219 SO 2001 5 2 COMA0110094 1 20010418 A 5320 12043599001 SUPPORT EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 232-01Z, THE FORWARD RIGHT SIDEWALL SEAT TRACK SUPPORT INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SUPPORT WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200220 20010502 00220 SO 2001 5 2 COMA0110095 1 20010418 A 5320 12005803001 SILL EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 132-01Z, THE FOWARD RIGHT FLOOR SUPPORT SILL INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SILL W AS REPLACED PER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200221 20010502 00221 SO 2001 5 2 COMA0110096 1 20010418 A 5320 12007089603 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 7134 120267 DURING 2C-CHECK TASK 131/132-01Z, THE FORWARD CENTER FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICE AND AERODESIGN REPORT 1671-1, REV A, 1/28/97. 2 L 7 2 4T RT A31SO 2001050200222 20010502 00222 SO 2001 5 2 COMA0110097 1 20010418 A 5320 12027289501 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 7134 120267 DURING 2C-CHECK TASK 131-01Z, THE FORWARD LEFT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE B UTTSTRAP WAS REPLACED PER SRM STANDARD PRACTICES AND AERODESIGN REPORT 1671-2, REV IR 12/4/96. 2 L 7 2 4T RT A31SO 2001050200223 20010502 00223 SO 2001 5 2 COMA0110098 1 20010418 A 5320 12046963001 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 7134 120267 DURING 2C-CHECK TASK 131-01Z, THE LEFT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200224 20010502 00224 SO 2001 5 2 COMA0110099 1 20010418 A 5320 12005805003 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 7134 120267 DURING 2C-CHECK TASK 131/132-01Z, THE CENTER FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUT TSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200225 20010502 00225 SO 2001 5 2 COMA0110100 1 20010418 A 5320 12046156601 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 7134 120267 DURING 2C-CHECK TASK 132-01Z, THE RIGHT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRA P WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200226 20010502 00226 SO 2001 5 2 COMA0110101 1 20010418 A 5320 12043603001 SUPPORT EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 243-01Z, THE LEFT SIDEWALL SUPPORT SECTION INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SUPPORTI NG SECTION WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200227 20010502 00227 SO 2001 5 2 COMA0110102 1 20010418 A 5320 12006664002 SILL EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 142-01Z, THE RIGHT FLOOR SUPPORT SILL INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SILL WAS REPL ACED PER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200228 20010502 00228 SO 2001 5 2 COMA0110103 1 20010418 A 5320 12006664004 SILL EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 142-01Z, THE RIGHT FLOOR SUPPORT SILL INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SILL WAS REPL ACED PER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200229 20010502 00229 SO 2001 5 2 COMA0110104 1 20010418 A 5320 12046158002 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 142-01Z, THE RIGHT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRA P WAS REPLACED PER EM-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200230 20010502 00230 SO 2001 5 2 COMA0110105 1 20010418 A 5320 12046158003 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 142-01Z, THE RIGHT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRA P WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200231 20010502 00231 SO 2001 5 2 COMA0110106 1 20010418 A 5320 12046158003 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 141-01Z, THE LEFT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200232 20010502 00232 SO 2001 5 2 COMA0110107 1 20010418 A 5320 12046158001 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 141-01Z, THE LEFT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200233 20010502 00233 SO 2001 5 2 COMA0110108 1 20010418 A 5320 12046163005 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 151-01Z, THE AFT LEFT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTS TRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200234 20010502 00234 WP 2001 5 2 ABXA010185 1 20010419 A 5320 FITTING DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 FITTING CRACKED AND CORRODED AT FS 1690 LONGERON 36 AFT SIDE OF SPLICE. 2 L 7 4 4F 4A25 2001050200235 20010502 00235 WP 2001 5 2 ABXA010186 1 20010419 A 5320 SPLICE DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 SPLICE FITTING AT FS 1050 LONGERON 31L IS CRACKED. 2 L 7 4 4F 4A25 2001050200236 20010502 00236 WP 2001 5 2 ABXA010187 1 20010419 A 5320 FITTING DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 A FITTING AFT OF THE PRODUCTION SPLICE IS CORRODED. 2 L 7 4 4F 4A25 2001050200237 20010502 00237 WP 2001 5 2 ABXA010188 1 20010419 A 5320 FITTING DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 FITTING IS CRACKED AND CORRODED AT FS 1690 LONGERON 34R AFT SIDE OF SPLICE. 2 L 7 4 4F 4A25 2001050200238 20010502 00238 WP 2001 5 2 ABXA010182 1 20010418 A 5313 57501981 LONGERON DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 CORROSION FOUND ON UPPER SURFACE OF LONGERON 24 AT FS 920. CORROSION EXTENDS UNDER FITTING IN LEFT MAIN LANDING GEAR WH EEL WELL. 2 L 7 4 4F 4A25 2001050200239 20010502 00239 WP 2001 5 2 ABXA010183 1 20010418 A 5313 57501481 LONGERON DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 LONGERON 24 IN LEFT MAIN LANDING GEAR WHEEL WELL HAS CORROSION ON UPPER SURFACE, BETWEEN STA 879 AND 902. 2 L 7 4 4F 4A25 2001050200240 20010502 00240 WP 2001 5 2 ABXA010184 1 20010418 A 5320 SPLICE DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 FITTING AT PRODUCTION SPLICE FS 1690 32R WAS CRACKED. 2 L 7 4 4F 4A25 2001050200241 20010502 00241 SO 2001 5 2 COMA0110109 1 20010418 A 5320 12027929001 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 151/152-01Z, THE AFT CENTER FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PACTICES. 2 L 7 2 4T RT A31SO 2001050200242 20010502 00242 SO 2001 5 2 COMA0110110 1 20010418 A 5320 12046163003 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2-C CHECK TASK 152-01Z, THE AFT RIGHT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUT TSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200243 20010502 00243 SO 2001 5 2 COMA0110111 1 20010418 A 5320 12046163001 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2-C CHECK TASK 152-01Z, THE AFT RIGHT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUT TSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200244 20010502 00244 SO 2001 5 2 COMA0110112 1 20010418 A 5320 12006159501 SILL EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 162-01Z, THE FORWARD RIGHT FLOOR SUPPORT SILL INSIDE THE CARGO COMPARTMENT WAS FOUND TO BE CORRODED . THE SILL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200245 20010502 00245 SO 2001 5 2 COMA0110113 1 20010418 A 5320 12006157007 SILL EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2-C CHECK TASK 164-01Z, THE AFT RIGHT FLOOR SUPPORT SILL INSIDE THE CARGO COMPARTMENT WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3661-1, REV IR, 5/15/00. 2 L 7 2 4T RT A31SO 2001050200246 20010502 00246 SO 2001 5 2 COMA0110114 1 20010418 A 5210 12021058001 CHANNEL EMB 120 EMB120RT SO PAX DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 811-02Z, THE U-CHANNEL INSIDE THE PASSENGER DOOR WAS FOUND TO BE CRACKED. THE CHANNEL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200247 20010502 00247 SO 2001 5 2 COMA0110115 1 20010418 A 5310 12034416002 SHEAR TIE EMB 120 EMB120RT SO FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 120267 DURING 2C-CHECK TASK 222-01Z, THE FUSELAGE SKIN SUPPORT ON RIGHT SIDE OF COCKPIT AT FRAME NR 9 WAS FOUND TO BE CRACKED. THE SKIN SUPPORT WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 660-1, REV IR, 2/16/93. 2 L 7 2 4T RT A31SO 2001050200248 20010502 00248 NM 2001 5 2 C8GA20010008 1 20010420 A 2750 FLAP BOEING 727 727223 1384074 NM WINGS FLUTTER A C8GA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 15 713AA 50869 22469 FLT BX1110 FROM MCO TO MEM. AFTER TAKEOFF IN CRUISE, AIRCRAFT EXPERIENCED SHUDDERING AT SPEEDS ABOVE 240 KNOTS. THE AI RCRAFT DIVERTED TO JAX AND LANDED WITHOUT FURTHER INCIDENT. INSPECTED AILERONS, ELEVATORS, STAB, RUDDER, AND FLAPS. AL L FOUND NORMAL. ALSO INSPECTED BODY DOORS AND FAIRINGS FOR LOOSENESS. NO DEFECTS NOTED. FOUND TRAILING EDGE FLAPS DRO OPING. ADJUSTED T/E FLAPS IAW 27-51-0. OPS CHECK AND LOCAL ACCEPTANCE FLIGHT CHECK GOOD AT ALL ALTITUDES AND SPEEDS. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2001050200249 20010502 00249 SO 2001 5 2 COMA0110116 1 20010418 A 5310 12034416001 SHEAR TIE EMB 120 EMB120RT SO FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 120267 DURING 2C-CHECK TASK 221-01Z, THE FUSLEAGE SKIN SUPPORT ON LEFT SIDE OF COCKPIT AT FRAME NR 9 WAS FOUND TO BE CRACKED. THE SKIN SUPPORT WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 660-1, REV IR, 2/16/93. 2 L 7 2 4T RT A31SO 2001050200250 20010502 00250 SO 2001 5 2 COMA0110117 1 20010418 A 5210 12021059001 CHANNEL EMB 120 EMB120RT SO PAX DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 811-02Z, THE CHANNEL INSIDE THE PASSENGER DOOR WAS FOUND TO BE CRACKED. THE CHANNEL WAS REPLACED P ER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200251 20010502 00251 SO 2001 5 2 COMA0110118 1 20010418 A 5320 12048716001 BRACKET EMB 120 EMB120RT SO CARGO BAY CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 262-01Z, THE AFT CARGO DOOR TRACK UPPER MOUNTING BRACKET WAS FOUND TO BE CRACKED. THE BRACKET WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 1657-3, REV IR, 6/12/00. 2 L 7 2 4T RT A31SO 2001050200252 20010502 00252 SO 2001 5 2 COMA0110119 1 20010418 A 5310 12012545001 SHEAR TIE EMB 120 EMB120RT SO FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 221-01Z, THE LEFT FUSELAGE SKIN SUPPORT JUST BEHIND CAPTAIN''S DV WINDOW, BETWEEN FRAMES 12A AND 23 , WAS FOUND TO BE CRACKED. THE SUPPORT WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200253 20010502 00253 SO 2001 5 2 COMA0110120 1 20010418 A 5310 12035891001 SHEAR TIE EMB 120 EMB120RT SO FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 232-01Z, THE RIGHT FUSELAGE SKIN SUPPORT AT FRAME NR 13A AND STRINGER NR 14R, WAS FOUND TO BE CRACK ED. THE SUPPORT WAS REPAIRED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3653-2, REV IR, 11/7/00. 2 L 7 2 4T RT A31SO 2001050200254 20010502 00254 WP 2001 5 2 CALA0100415 1 20010423 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 EXTERNAL FUSELAGE. SKIN DENTED AT STA 256 LGL 30 BY DRAIN HOLE. CUT OUT DAMAGED AREA IAW 53-04 FIG 12B. FAB''D REPAIR DOUBLERS IAW 53-04 FIG 12B. DRILLED AND COUNTERSUNK IAW 51-10-04. TREATED AND PRIMED IAW 51-10-3 AND INSTALLED ALL PER 51-30-2, 4, 5. 2 L 7 2 4F A6WE 2001050200255 20010502 00255 SO 2001 5 2 COMA0110121 1 20010418 A 5720 12031657001 ANGLE EMB 120 EMB120RT SO LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 5320-243-01I, THE LEFT WING UPPER SKIN ATTACH ANGLE FOR FAIRING NR 193 WAS FOUND TO BE CRACKED. TH E ANGLE WAS REPAIRED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 1126-21, REV IR, 7/6/99. 2 L 7 2 4T RT A31SO 2001050200256 20010502 00256 SO 2001 5 2 COMA0110122 1 20010418 A 5320 12061603602 FLOOR SUPPORT EMB 120 EMB120RT SO FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 5310-122-01I, THE RIGHT FUSELAGE FLOOR PROP AT FRAME NR 13 WAS FOUND TO BE CRACKED. THE FLOOR PROP WAS REPAIRED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3647-1, REV IR, 5-3-00. 2 L 7 2 4T RT A31SO 2001050200257 20010502 00257 SO 2001 5 2 COMA0110123 1 20010418 A 5320 12061603601 FLOOR SUPPORT EMB 120 EMB120RT SO FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 5310-121-01I, THE LEFT FUSELAGE FLOOR PROP AT FRAME NR 13 WAS FOUND TO BE CRACKED. THE FLOOR PROP WAS REPAIRED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3647-1, REV IR, 5-3-00. 2 L 7 2 4T RT A31SO 2001050200258 20010502 00258 SO 2001 5 2 COMA0110124 1 20010418 A 5720 12017063609 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK 5720-552-01I, THE LEFT WING UPPER SKIN SUPPORT AT RIB 21, BETWEEN STRINGER NR 2 AND 3, WAS FOUND TO BE C RACKED. THE SKIN SUPPORT WAS REMOVED AND REPLACED PER EMB-120 SRM STANDRAD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200259 20010502 00259 SO 2001 5 2 COMA0110125 1 20010418 A 5720 12017062613 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK 5720-552-01I, THE LEFT WING UPPER SKIN SUPPORT AT RIB NR 21, BETWEEN FRONT SPAR AND STRINGER NR 2, WAS F OUND TO BE CRACKED. THE SKIN SUPPORT WAS REMOVED AND REPLACED PER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200260 20010502 00260 SO 2001 5 2 COMA0110126 1 20010418 A 5753 12040327007 SKIN EMB 120 EMB120RT SO T/E FLAP CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 120267 DURING 2C-CHECK (NO SPECIFIC TASK APPLIES), THE LEFT NACELLE FLAP LOWER SKIN WAS FOUND TO BE CRACKED AT ACCESS PANEL NR 436AB CUTOUT. THE NACELLE FLAP WAS REMOVED AND REPLACED PER EMB-120 MM 27-50-03. 2 L 7 2 4T RT A31SO 2001050200261 20010502 00261 SO 2001 5 2 COMA0110127 1 20010418 A 5720 12017063609 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 5710-652-01I, THE RIGHT WING UPPER SKIN SUPPORT ON RIB NR 21, BETWEEN STRINGERS NR 2 AND 3, WAS FOU ND TO BE CRACKED. THE SKIN SUPPORT WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200262 20010502 00262 SO 2001 5 2 COMA0110128 1 20010418 A 5413 12041440002 STRINGER EMB 120 EMB120RT SO RT NACELLE DENTED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 5410-442-04I, THE RIGHT NACELLE OUTBOARD STRINGER NR 1 WAS FOUND TO BE DENTED BY THE GEAR DOOR TENS IONER. THE STRINGER WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES AND EMBRAER REPAIR GST-1034/01, DATED 3/30/01. 2 L 7 2 4T RT A31SO 2001050200263 20010502 00263 NE 2001 5 2 C2XA01CL082 2 20010422 A 7261 PW121 ENGINE AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE RT ENGINE LEAKING A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 14828 20564 7806 179 CLE FLIGHT 3091 THE CREW REPORTED SMOKE IN CABIN. MAINTENANCE INSPECTED AND FOUND THE NR 2 ENGINE TO BE LEAKING OIL INT ERNALLY. THE ENGINE WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2001050200264 20010502 00264 SO 2001 5 2 COMA0110129 1 20010418 A 5330 12019737003 SKIN EMB 120 EMB120RT SO FUSELAGE GOUGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2 YEAR CORROSION CHECK TASK 5310-132-C01E, THE LOWER RH FUSELAGE SKIN WAS FOUND GOUGED JUST BELOW THE LAV DUMP VA LVE DOUBLER. THE SKIN WAS REPAIRED PER EMBRAER SRM STANDARD PRACTICES AND REPAIR FAX GST-0992/01, DATED 3/28/01. 2 L 7 2 4T RT A31SO 2001050200265 20010502 00265 SO 2001 5 2 COMA0110130 1 20010418 A 5320 12006664003 SILL EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 20574 120267 DURING 2C-CHECK TASK 141-01Z, THE AFT LEFT FLOOR SUPPORT SILL INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SILL WAS R EPLACED PER EMB-120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 2001050200266 20010502 00266 EU 2001 5 2 YENA0105 1 20010423 A 3350 1012881 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN MISSING A YENA K NONE O OTHER IN INSP/MAINT 1 EA 15 507JB 1240 ROW 1ABC EMERGENCY LIGHT BULB MISSING WITH TERMINAL PIN BROKEN OFF. 2 L 7 2 4F 4 F RT A28NM E40NE 2001050200267 20010502 00267 WP 2001 5 2 ZW0A0100704 1 20010420 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT FOUND FLOOR SUPPORT CORRODED AT STA 1155, LONGERON 30 TO 29R. REPLACED FLOOR SUPPORT PER SPM 6-70- 01. 2 L 7 2 4F A6WE 2001050200268 20010502 00268 WP 2001 5 2 ZW0A0100705 1 20010419 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT FOUND CABIN FLOOR BEAM, LT SIDE OF TOP CAP, WAS CORRODED OUT AT STA 1250. REMOVED SUPPORT ANGLE AN D FABRICATED NEW AND INSTALLED WITH HI-LOKS PER SPM 6-70-01. 2 L 7 2 4F A6WE 2001050200269 20010502 00269 WP 2001 5 2 ZW0A0100706 1 20010419 A 5342 ATTACH ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT FOUND VERTICAL STABILIZER RT SIDE OF DORSAL FIN, AFT END OF VERTICAL STAB TO FUSELAGE ATTACH ANGLE, AFT OF PREVIOUS REPAIR HAD ANGLE WITH A 2 INCH CRACK. TRIMMED OFF BROKEN PART. MADE FILLER AND DOUBLER PER SRM 53-05, FIG 23A, AND INSTALLED. 2 L 7 2 4F A6WE 2001050200270 20010502 00270 WP 2001 5 2 ZW0A0100707 1 20010419 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT FOUND A 1.5 INCH CRACK IN WEBBING AT STA 1266, LONGERON 18L, ONE INCH OTBD OF NUMBER 1 CHAIR TRACK. INSTALLED WEB DOUBLER PER SRM 53-01, FIG 2 AND SRM 51-30-2. 2 L 7 2 4F A6WE 2001050200271 20010502 00271 WP 2001 5 2 ZW0A0100708 1 20010419 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT IN THE AFT ACCY COMPT, FOUND CORROSION AND RUSTED FASTENERS BETWEEN SKIN AND FORMERS AT STA 1437, B ETWEEN LONGERON 19R AND 17R. REMOVED CORROSION PER SRM 51-10-3 AND SPM 6-80-01. INSTALLED DOUBLER REPAIR PER SRM 53-01 , PAGE 9 FIG 2. 2 L 7 2 4F A6WE 2001050200272 20010502 00272 WP 2001 5 2 ZW0A0100709 1 20010418 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT FOUND CORROSION ON FORMER AT STA 1320, LONGERON 27R TO 18L, AT STA 1320 FROM RBL 17 IN TO RBL 21 IN CORROSION ON BOTTOM OF FORMER FWD SIDE, AND STA 1323 FROM LBL 7 IN TO LBL 32 IN FWD SIDE OF FORMER WAS CORRODED. INSTA LLED NEW FORMER RING. INSTALLED PER DRAWING 9936664 AND SRM 51-30-02. REPLACED FORMER RING AT STA 1320 FROM LONGERON 1 8L TO 18R. 2 L 7 2 4F A6WE 2001050200273 20010502 00273 WP 2001 5 2 ZW0A0100701 1 20010419 A 3350 7732 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ZW0A K NONE L NO TEST NR NOT REPORTED 1 CE 13 9616G 53563 EGRESS LIGHTING WAS INOPERATIVE AT ROW 30, ROWS 11 TO 15, AND ROW 17. REPLACED LAMP P/N 7732 AT ROW 30, REPLACED WIRE H ARNESS P/N 0105606-003 FOR ROWS 11 TO 20, AND RECONNECTED HARNESS AT ROW 17. CHECK-C 8-18-00 JFK. 2 L 7 2 4F RT A6WE 2001050200274 20010502 00274 NM 2001 5 2 ZW0A0100702 1 20010420 A 3350 S417N5094 LENS BOEING 767 7673Y0 NM R2 DOOR MISSING A ZW0A K NONE O OTHER NR NOT REPORTED 1 CE 13 632TW 24953 THE EGRESS LIGHTING RED EXIT INDICATOR WAS MISSING AT THE RT SIDE NUMBER 2 PASSENGER DOOR AREA. REPLACED THE LENS. CHE CK-C 3-22-01 LAX. 2 L 7 2 4F RT A1NM 2001050200275 20010502 00275 NM 2001 5 2 ZW0A0100703 1 20010419 A 3397 WIRE BOEING 767 7673Y0 NM CABIN DISCONNECTED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 632TW 24953 THE INTERIOR EMERGENCY EXIT LIGHTS WERE INOPERATIVE ON RT SIDE OF CABIN, ROW 32 TO 40. RECONNECTED WIRING AT THE AFT TR ACK AREA. CHECK-C 3-22-01 LAX. 2 L 7 2 4F RT A1NM 2001050200276 20010502 00276 CE 2001 5 2 20010423CW015 1 20010326 A 5210 MJV3 DOOR SEAL CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE PAX DOOR MALFUNCTIONED B R2JR K NONE O OTHER IN INSP/MAINT 1 EA 21 92SS 1785 5600388 AFTER FLIGHT, CABIN DOOR SEAL SLOW TO DEFLATE, FOUND DOOR SEAL VALVE STRIKING AND AN911-1 FITTING IN INLET OF VALUE, CO RRODED. REPLACED VALVE AND INSTALLED AN911-1J FITTING. 2 L 7 2 4F 4 F RT A22CE E25EA 2001050200277 20010502 00277 NE 2001 5 2 MWEA010629 2 20010421 A 7261 541556 OIL FILTER DOUG DC9 DC915 3022036 WP PWA JT8 JT8D7B 52053 NE LT ENGINE CLOGGED A MWEA E ENGINE SHUTDOWN J WARNING INDICATION TX TAXI/GRND HDL 1 GL 31 300ME 45718 LEFT OIL STRAINER CLOGGING ANNUNCIATOR ILLUMINATED. REPLACED LEFT ENGINE OIL FILTER. 2 L 7 2 4F 4 F A6WE E2EA 2001050200278 20010502 00278 CE 2001 5 2 20010423CW017 1 20010317 A 2910 5407002340 TUBE LEAR 60 60LEAR 5170707 CE HYD SYSTEM CRACKED D K NONE K FLUID LOSS IN INSP/MAINT 1 GL 17 600LC 3740 021 A SMALL HYDRAULIC LEAK WAS FOUND IN WHEEL WELL. TIGHTENED B-NUT AND LEAK BECAME WORSE. REMOVED TUBE AND FOUND CRACK AR OUND CIRCUMFERENCE AT FLARE. THIS TUBE IS ABOUT 3 FEET LONG AND IS ONLY SURPPORTED 4 INCHES FROM OPPOSITE END OF CRACK. 2 L 7 2 4F RT A10CE 2001050200279 20010502 00279 EA 2001 5 2 SWIA972519 1 20010419 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT CRACKED A SWIA K NONE O OTHER DE DESCENT 1 NM 07 427SW 7497 ON DESCENT THROUGH 17,000, LEFT WINDSHIELD SHATTERED. NO LOSS OF PRESSURIZATION AND NO OTHER STRUCTURAL DAMAGE NOTED. REMOVED AND REPLACED LEFT WINDSHIELD IAW RII 56-401 AND MM 56-11-01. OPS CHECKS GOOD. P/N ON PPG-WP-139321-9, S/N ON 0103248940, P/N OFF 601R33033-13, S/N OFF 01008H7144. 2 L 7 2 4F 4 F RT A21EA E15NE 2001050200281 20010502 00281 CE 2001 5 2 20010424CW002 1 20010317 A 7830 6000100 TUBE LEAR 60 60LEAR 5170707 CE THRUST REVERSER CRACKED D K NONE K FLUID LOSS IN INSP/MAINT 1 GL 17 600LC 3740 021 SMALL HYDRAULIC LEAK WAS FOUND IN AFT HYDRAULIC AREA NEAR FUEL FILTERS. TIGHTENED B NUT AND LEAK BECAME WORSE. REMOVED TUBE AND FOUND CRACK AT FLARE AROUND CIRCUMFERENCE. THIS TUBE NEEDS BETTER SUPPORT. 2 L 7 2 4F RT A10CE 2001050200282 20010502 00282 CE 2001 5 2 20010424CW003 1 20010317 A 3310 76880394 LIGHT LEAR 60 60LEAR 5170707 CE COCKPIT BURNED D K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 17 600LC 3765 021 DISCREPANCY ON AIRCRAFT INDICATED THE PANEL WAS DIM. UPON REMOVAL OF OVERLAY, ARCING WAS NOTED ON CIRCUIT BREAKER UNDER NEATH AND A BURNED HOLE WAS IN THE BACKSIDE OF THE OVERLAY. 2 L 7 2 4F RT A10CE 2001050200283 20010502 00283 SO 2001 5 2 20010424CW004 1 20010206 A 5280 4205907 HINGE PIPER PA31T PA31T 7103124 SO PWA PT6 PT6* 52043 EA MLG DOOR CRACKED D K NONE O OTHER IN INSP/MAINT 1 NM 09 700LT 5190 31T7920046 ON POST FLIGHT, FOUND FORWARD HINGE ON LEFT MAIN LANDING GEAR OUTBOARD DOOR BROKEN. REMOVED DOOR, FOUND REAR HINGE CRAK ED IN SAME AREA. REMOVED RIGHT OUTBOARD DOOR, FOUND CRACKED PAINT IN SAME AREA AS BROKEN HINGE. REPLACED ALL HINGES. 1 L 7 2 3T 3 T A8EA E2NE 2001050200284 20010502 00284 2001 5 2 20010424CW005 4 20010120 A 8300 MS927609 NUT BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA ACCESS GEARBOX FRETTED A FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 575P UC95 PCE32327 DURING FLIGHT AT CRUISE, LOW FUEL PRESSURE AND LOW OIL PRESSURE WARNING LIGHTS CONFIRMED LOW OIL PRESSURE ON GAGE. OIL WAS NOTED COMING OUT OF EXHAUST. CREW SHUT DOWN ENGINE. DURING TEARDOWN, ACCESSORY GEARBOX COUPLING WAS FOUND SHEARED, SUGGESTED COUPLING SHEARED OWED TO A MS927609 NUT THAT CAME LOOSE AND JAMMED BETWEEN GEARS. 2 L 7 2 4T 4 T RT A24CE E4EA 2001050200285 20010502 00285 CE 2001 5 2 20010424CW006 1 20010412 A 2435 632617 GEAR CONT CESSNA 337 337G 2075730 CE CONT O360 IO360GB 17025 SO STARTER ADAPTER SHEARED D K NONE O OTHER IN INSP/MAINT 1 SO 15 724AS 277 8508 33701792 352972 DETAILED INVESTIGATION OF THE STARTER DRIVE REVEALED THAT ALL OF THE GEAR TEETH WERE WORN EXCESSIVELY ON ONE OF THE BEVE L GEARS WHICH DRIVES THE VACUUM PUMP. 1 H 7 2 3O 3 O A6CE E1CE 2001050200286 20010502 00286 CE 2001 5 2 20010424CW010 1 20010403 A 3710 632617D BEVEL GEAR CESSNA 337 337G 2075730 CE CONT O360 IO360GB 17025 SO MCAULY 2AF34C D2AF34C307 GL VACUUM PUMP SHEARED D O OTHER O OTHER NR NOT REPORTED 1 SO 15 726AS 725 33701661 813015R 771909 PILOT REPORTED LOSS OF INSTRUMENT VACUUM FROM REAR ENGINE DURING BEFORE TAKEOFF GROUND RUN UP. INVESTIGATION REVEALED T HAT THE VACUUM PUMP WAS STILL SERVICEABLE. FURTHER INVESTIGATION REVEALED THAT ALL OF THE GEAR TEETH WERE SHEARED OFF O F ONE OF THE BEVEL GEARS WHICH DRIVES THE VACUUM PUMP. 1 H 7 2 3O 3 O A6CE E1CE 5 C P5EA 2001050200287 20010502 00287 WP 2001 5 2 20010424CW012 2 20010225 A 7250 30720142 TURBINE BLADES LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE731* 01518 WP 3RD STG FAILED E EXOA O OTHER E M J VIBRATION/BUFFET OVER TEMP WARNING INDICATION LD LANDING 1 SO 17 556HJ 9240 028 85221 ON LANDING ROLLOUT, CREW NOTICED, VIBRATION, TEMPERATURE, AND RPM FLUCTUATING. ENGINE SHUTDOWN DETERMINED, THIRD STAG E TURBINE BLADE FAILED. 2 L 7 2 4F 4 F A10CE E6WE 2001050200288 20010502 00288 CE 2001 5 2 RU3A0101 1 20010404 A 2120 SMOKE BEECH 300 300BEECH 1152930 CE PWA PT6 PT6A60A 52043 NE CABIN DETECTED H A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 99 72 FF7 ACRID FOUL SMELLING SMOKE PERMEATED CABIN, ENVIROMENTAL TEMP CIRCUIT BREAKER POPPED. DECLARED EMERGENCY AND DIVERTED. SMOKE DISSIPATED. CABIN TEMP INCREASED BECAUSE FORWARD AND AFT BLOWER MOTORS WERE INOPERATIVE. DID NOT REQUEST CRASH E QUIPMENT. LANDED UNEVENTFULLY. MECHANIC COULD NOT DUPLICATE AFTER 30 MINUTE RUN UP WITH CREW PRESENT. ALL SYSTEMS OPE RATING. AIRCRAFT RETURNED TO AIRWORTHY CONDITION. 2 L 7 2 4T 4 T A24CE E4EA 2001050200289 20010502 00289 EA 2001 5 2 20010425CW001 1 20010321 A 5610 6003303025 WINDSHIELD CNDAIR CL600 CL600* EA COCKPIT CRACKED E EXOA O OTHER O OTHER DE DESCENT 1 SW 17 65HJ 1360 1038 ON DESCENT WINDSHIELD CRACKED AND DELAMINATED WITH SEVERAL LARGE PIECES, APPROX 75 PER CENT OF IT DEPARTING AIRCRAFT (OU TER LAYER). THE REMAINING WINDSHELD MAKING EXTREMELY HIGH LEVELS OF NOISE AND THE AIRCRAFT SEEMED TO VIBRATE SLIGHTLY. 2 L 7 2 4F RT A21EA 2001050200290 20010502 00290 CE 2001 5 2 20010425CW002 1 20010322 A 3411 DRAIN LINE RAYTHN BEECH 1900 1900D 1154162 CE PITOT/STATIC DRN CORRODED B JGVR K NONE O OTHER IN INSP/MAINT 1 CE 09 9UP 258147 FOUND 4 PITOT/ STATIC DRAINS LEAKING DURING 24 MONTH PITOT/STATIC SYSTEM CERTIFICATION. FOUND LEFT AFT DRAIN RESERVOIR AND LINE CORRODED. FOUND DRAIN LINE ON RIGHT SIDE CHAFING ON ELEVATOR PRIMARY CONTROL CABLE. CORROSION ON FITTINGS AND DRAIN BODIES AS FOUND. REPLACED DRAIN INSERTS. (PHOTOS) 2 L 7 2 4T RT A24CE 2001050200291 20010502 00291 SO 2001 5 2 20010425CW003 1 20010405 A 2460 PISTON CONT PIPER PA34 PA34220T 7103420 SO CONT O360 LTSIO360RB SO CONTROLLER STUCK B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 9299E DGN9687 3449043 819507R THE CONTROLLER PISTON STICK IN. A SPLIT IN POWER SETTING IN FLIGHT AND ON THE GROUND CONTROLLER REPLACED. 1 L 7 2 3O 3 O A7SO E9CE 2001050200292 20010502 00292 GL 2001 5 2 20010425CW005 3 20010327 A 6110 A3496 SPRING HARTZL BEECH 1900 1900C 1154161 CE HARTZL HCB4M HCB4M GL PROPELLER CRACKED B ME4R K NONE O OTHER IN INSP/MAINT 1 SO 19 125BA 12192 UB6 FW778 DURING DISASSEMBLY AND VISUAL INSPECTION, SPRING WAS FOUND CRACKED IN HALF, IAW AIRCREW, NO DISCREPANCY WAS NOTED DURING INCOMING FLIGHT. PROPELLER HUB REPLACED, SPRING REPLACED, PROPELLER REASSEMBLED AND INSTALLED ON THE AIRCRAFT WITH NO DISCREPANCIES NOTED. 2 L 7 2 4T RT A24CE 6 C P56GL 2001050200293 20010502 00293 SO 2001 5 2 20010425CW006 1 20010315 A 7920 AE7010201K0240 HOSE PIPER PA31T PA31T2 7103127 SO PWA PT6 PT6A60 52043 NE OIL COOLER BURST B E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 CE 01 410CA 112 31T8166005 PCE92300 IN FLIGHT THE LEFT ENGINE OIL COOLER HOSE BURST CAUSING A LOSS OF OIL AND A PRECAUTIONARY ENGINE SHUTDOWN. THE PILOT MA DE AN UNEVENTFUL LANDING. BEIN THAT THIS WAS THE SECOND SUCH HOSE THAT HAS FAILED IN THIS METHOD ON THISAIRCRAFT PROBLE M IS SUSPECTED ING THE MANUFACTURING PROCESS. 1 L 7 2 3T 4 T RT A8EA E4EA 2001050200295 20010502 00295 CE 2001 5 2 20010425CW008 1 20010312 A 2720 CONTROL CABLE BEECH 36 A36 1151604 CE CONT O550 IO550* SO RUDDER CHAFED B K NONE O OTHER IN INSP/MAINT 1 GL 11 497EB 93 E3296 RIGHT RUDDER CABLE IS CHAFFING ON LONGERON JUS AFT OF FIRST PULLEY AT F.S. 83. 090 DOWN LINE FROM RUDDER PEDAL BELLCRANK . CABLE SHOULD PASS THROUGH FIRST LIGHTENING HOLE JUST AFT OF PULLEY. CABLE CURRENTLY PASSES THROUGH SECOND LIGHTENING HOLE, CAUSING CABLE TO CHAFE LONGERON. 1 L 7 1 3O 3 O 3A15 E3SO 2001050200296 20010502 00296 WP 2001 5 2 UPS01835686 1 20010404 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2 MAIN CABIN STA 920 LT FLOORBEAM CORRODED AT FRAME JOINT FWD AND AFT. REMOVED AND REPLACED FLOOR BEA M STRAP IAW DAC DWG 5646864 ALODINED & PRIMED IAW DC8 SRM 51-1-8 2 L 7 4 4F RT 4A25 2001050200297 20010502 00297 SO 2001 5 2 20010425CW010 2 20010322 A 8550 CH48108 FILTER BEECH 58 58P 1152744 CE CONT O520 TSIO520L 17040 SO OIL SYSTEM CHIPPED G A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 07 1563L TJ84 509228 PILOT REPORTED LOW OIL PRESSURE AND HIGH TEMPERATURES. INVESTIGATION REVEALED METAL PIECES HOLDING OPEN THE OIL TEMPERA TURE CONTROL VALVE. THE METAL PIECES WERE TRACED TO THE OIL FILTER. UPON REMOVING THE TOP FROM THE OIL FILTER WE OBSER VED PIECES MISSING FROM THE FLANGE THAT RETAINS THE RUBBER BACK FLOW VALVE. THE PIECES REMOVED FROM THE TEMPERATURE CON TROL VALVE APPEARED TO MATCH THE MISSING AREA OF THE OIL FILTER FLANGE. NOT ALL OF THE MISSING FLANGE CAN BE ACCOUNTED FOR AND FERRUS PARTICLES WERE FOUND IN THE FILTER MEDIA. 1 L 7 2 3O 3 O A23CE E8CE 2001050200299 20010502 00299 EA 2001 5 2 20010425CW012 2 20010121 A 7200 PT6A65 ENGINE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA RIGHT FAILED E YADA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 AL 03 45GL 14625 7219 UC45 PCE32413 ON RETURN LEG OF ROUND TRIP, PILOT NOTICED AN ORANGE FLASH FRO THE RIGHT HAND ENGINE. ENGINE ITT STARTED RISING AND THE POWER STARTED RISING AND THE POWER STARTED SURGING. THE ENGINE WAS SECURED AND FEATHERED 45 MINUTES OUT. MADE UNEVENT FUL LANDING. NO DETERMINATION OF THE CAUSE OF FAILURE HAS MADE AT THIS TIME. THE OIL FILTER WAS CONTAMINATED WITH META LLIC PARTICLES AND THE COMPRESSOR SECTION WAS SEIZED UP. ENGINE HAS BEEN REMOVED AND REPLACED. 2 L 7 2 4T 4 T RT A24CE E4EA 2001050200300 20010502 00300 CE 2001 5 2 20010425CW013 1 20010116 A 2612 24412886 FIRE LOOP BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE RT ENGINE CHAFED E YADA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 AL 03 1553C UC24 WITHIN MINUTES OF DEPARTURE, RIGHT ENGINE FIRE WARNING LIGHT CAME ON. PILOT REPORTED NO FLAMES, DID NOT USE EXTINGUISHE R. SHUT DOWN RIGHT ENGINE. NO ABNORMAL ENGINE INSTRUMENTS. AIRCRAFT LAND OVER MAXIMUM LANDING WEIGHT. MAINTENANCE FO UND HEAVY CHAFED SPOT ON FORWARD ENGINE FIRE LOOP, AT A LOOP CLAMP LOCATION. IT APPEARS THAT THE CLAMP CAME LOOSE AND A LLOWED THE LOOP TO CONTACT THE CLAMP BRACKET, REPLACED FORWARD FIRE LOOP. 2 L 7 2 4T 4 T RT A24CE E4EA 2001050200302 20010502 00302 CE 2001 5 2 20010425CW015 1 20010222 A 7921 10656D OIL COOLER BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA NR 2 ENGINE CRACKED B YADA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 AL 03 5632C 785 UC81 PCE32586 FLIGHT CREW PERFORMED IN-FLIGHT SHUTDOWN OF THE NR 2 ENGINE ONE HALF HOUR PRIOR TO REACHING THE DESTINATION AIRPORT, DUE TO LOW ENGINE OIL PRESSURE INDICATION. UNEVENTFUL LANDING. A SUSPECTED OIL LEAK WAS REPAIRED AND THE AIRCRAFT DEPARTE D AND AGAIN THE NR 2 ENGINE WAS SECURED PRIOR TO ARRIVAL AT DESTINATION. AN UNEVENTFUL LANDING WAS PERFORMED. AGAIN, A SUSPECTED OIL LEAK WAS REPAIRED AND AIRCRAFT RETURNED. 2 L 7 2 4T 4 T RT A24CE E4EA 2001050200304 20010502 00304 EA 2001 5 2 20010425CW017 2 20010402 A 7411 ES103825881 COIL CONT PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA IGNITION SYS CRACKED D K NONE O OTHER IN INSP/MAINT 1 EA 03 27329 303 5010586 317752150 L360561A DURING ROUTINE MAINTENANCE ON DUAL MAGNETO, A CRACK WAS FOUND ON THE RIGHT IGNITION COIL OUTER INSULATION COVERING. THE CRACK STARTED FROM THE HIGH TENSION OUTLET CLIP AND RAN ALONG THE MOLD LINE APPROX .25. BOTH SIDES OF THE CLIP HAD THE SAME TYPE OF CRACK, TWO ALTOGETHER. MAGNETO OPERATION WAS NORMAL PRIOR TO INSPECTION. 1 L 7 2 3O 3 O A20SO E14EA 2001050200305 20010502 00305 SW 2001 5 2 MV5R055N1 1 20010406 A 3220 ESIO119 BLOCK GULSTM 690TP 695A 7630519 SW GARRTT TPE331 TPE331* 01514 WP NOSE GEAR SEPARATED B MV5R K NONE O OTHER IN INSP/MAINT 1 GL 11 695GG 135 96036 NOSE GEAR SEARING ATTACHMENT BLOCK PIN HAD SEPERATED FROM THE BLOCK. THE ROLL PIN THAT SECURES THE PIN TO THE BLOCK HAD SHEARED, INSPECTION OF THE ROLL PIN INDICATED THAT THE SHEAR WAS IN A DOWNWARD DIRECTION. 1 H 7 2 4T 3 T 2A4 E2WE 2001050200306 20010502 00306 SO 2001 5 2 WVBA2001022 1 20010417 A 2140 A23DO4 REGULATOR ELECTROSYS PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA HEATER LEAKING B WVBA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 AL 01 42WP 120 WAV113FR 318252038 PILOT REPORTED FRONT HEATER INOPERATIVE. IT WAS FOUND THAT THE FUEL PRESSURE REGULATOR, FOR THE FRONT COMBUSTION HEATER WAS LEAKING FROM THE TOP GASKET UNIT, WAS REPLACED . HEATER OPERATIONS CHECK APPEARED NORMAL. 1 L 7 2 3O 3 O A20SO E14EA 2001050200307 20010502 00307 NM 2001 5 2 EIA2001167 1 20010312 A 5311 141U105166 FRAME BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND BS 440 STRINGER 14R FRAME WEB CRACKED. BS 440 FRAME WEB FROM STRINGER 0 TO STRINGER 16R REPLACED PER EO 53-747-1143-91 REV E AND DWG 624U0003 SH 22R. (M) 2 L 7 4 4F A20WE 2001050200308 20010502 00308 NM 2001 5 2 EIA2001151 1 20010312 A 5311 FRAME BOEING 747 747273C 1384896 NM BS 500 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND BS 500 RIGHT STRINGER 31 FRAME JOINT PREVIOUS CRACK REPAIR. REMOVED PREVIOUS REPAIR, NDT INSPECTED. INSTALLED REPAIR DOUBLER, STRAP WITH EXTENDED PROFILE, AND FILLER PER BOEING MSG EVR-HKG-01-00021H/00015F AND RS R-53-12 -34606. (M) 2 L 7 4 4F A20WE 2001050200309 20010502 00309 WP 2001 5 2 AALA20010424 1 20010219 A 5330 SKIN DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 126AA 46947 TUL - FOUND PITTING AND CORROSION ON SKIN UNDER SHEAR TIE BETWEEN STRINGER 51L AND 52L UNDER STATION 824. ALODINED, PAI NTED, AND REPLACED CORRODED AREA IAW SRM 53-20-00 VI CLASS II REPAIR, PER ESO 7349 DATE 3-5-01. (M) 2 L 7 3 4F A22WE 2001050200310 20010502 00310 WP 2001 5 2 AALA20010672 1 20010326 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 TUL - FOUND NR 6 SEAT TRACK HAS CORROSION STATION 215. REMOVED AND REPLACED SEAT TRACK FROM STATION 210-323 PER SRM 53- 05 PART 1 FIG 4E SHT 1,5. (M) 2 L 7 2 4F RT A6WE 2001050200311 20010502 00311 WP 2001 5 2 AALA20010673 1 20010322 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 TUL - FOUND FUSELAGE SKIN CRACKED AT RIVET HOLE STATION 1380 LONGERON 14L. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2001050200312 20010502 00312 WP 2001 5 2 AALA20010674 1 20010316 A 5320 SPLICE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 TUL - FOUND RIGHT CUSP SPLICE CORRODED STATION 1162-1165. REMOVED CORROSION FABRICATED AND INSTALLED NEW SPLICE/DOUBLER PER SRM 53-01 AND AARD 53-00-00-02. (M) 2 L 7 2 4F RT A6WE 2001050200313 20010502 00313 WP 2001 5 2 AALA20010675 1 20010321 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 TUL - FOUND DEEP DRILL BIT GOUGE IN LONGERON 9R, STATION 313. INSTALLED LONGERON REPAIR AS PER SRM 53-02 PAGE 48-53. ( M) 2 L 7 2 4F RT A6WE 2001050200314 20010502 00314 WP 2001 5 2 AALA20010676 1 20010321 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE TOOL DAMAGE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 TUL - FOUND TOOLING MARK IN FRAME STATION 313 LONGERON 9R. INSTALLED J-ANGLE REPAIR AS PER AARD 53-10-00-14. (M) 2 L 7 2 4F RT A6WE 2001050200315 20010502 00315 WP 2001 5 2 AALA20010677 1 20010325 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 TUL - FOUND CUSP UNDER NR 6 SEAT TRACK DAMAGED STATION 297 TO 310 RT. SPLICED IN NEW SECTION OF CUSP FROM STATION 289 T O 313 RIGHT IAW SRM 53-01 FIG 4. (M) 2 L 7 2 4F RT A6WE 2001050200316 20010502 00316 NM 2001 5 2 EIA2001134 1 20010312 A 5320 WEB BOEING 747 747273C 1384896 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND BS 1241 REAR SPAR WEB UPPER EDGE AT RBL 75.89 AND RBL 98.55, HEAVY CORROSION/BLENDOUT EXCEEDS SRM LIMI TS. CORROSION REMOVED, HFEC INSPECTED BLENDOUT AREA, HFEC INSPECTED ALL OPEN HOLES. FLAP/SHOT PEENED BLENDOUT REGIONS AND REPAIR ANGLE. REPLACED SPLICED ANGLE AND REPAIRED WEB PER BOEING MSG AND RS R-57-12-34634. (M) 2 L 7 4 4F A20WE 2001050200317 20010502 00317 NM 2001 5 2 EIA2001133 1 20010312 A 5730 SKIN BOEING 747 747273C 1384896 NM WING CENTER BOX CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND BS 1241 WING CENTER SECTION UPPER SURFACE AT RBL 57 TO RBL 103 AND LBL 11 TO LBL 33 CORRODED. BLENDE D OUT CORROSION, NDT INSPECTED, REWORKED AND REPORTECTED BLENDOUT REGIONS PER BOEING MSG EVR-HKG-01-00043F/00068H/00069H / AND RS R-57-14-34635. (M) 2 L 7 4 4F A20WE 2001050200318 20010502 00318 NM 2001 5 2 P2EA01022 1 20010405 A 5320 CHANNEL BOEING 737 7372B7 1384560 NM FUSELAGE CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 125NJ 22882 SJO - DURING C-CHECK, FOUND CORROSION ON CHANNEL SUPPORT BETWEEN BS 986 AND 1006 AND BETWEEN STRINGER 25L AND 26L. (M) 2 L 7 2 4F A16WE 2001050200319 20010502 00319 NM 2001 5 2 P2EA01021 1 20010404 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSLEAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 125NJ 22882 SJO - DURING C-CHECK, FOUND SKIN CRACKED AT STRINGER 19R AT BS 765. (M) 2 L 7 2 4F A16WE 2001050200320 20010502 00320 NM 2001 5 2 P2EA001016 1 20010404 A 5330 SKIN BOEING 737 737244 138448U NM FUSELAGE CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 OKC - DURING C-CHECK, FOUND THE INTERNAL SKIN AT FUSELAGE STATION 322 BETWEEN STRINGERS 28-29 RIGHT HAS CORROSION. (M) 2 L 7 2 4F A16WE 2001050200321 20010502 00321 NM 2001 5 2 P2EA001015 1 20010404 A 5330 SKIN BOEING 737 737244 138448U NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 OKC - FOUND DURING C-CHECK, FORWARD FUSELAGE SKIN AT STATION 196.5 TO 203.5 AT LBL 3 WITH CRACK .75 INCH IN LENGTH. (M) 2 L 7 2 4F A16WE 2001050200322 20010502 00322 NM 2001 5 2 P2EA001013 1 20010329 A 5730 SKIN BOEING 737 737244 138448U NM LT WING CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 OKC - DURING C-CHECK, FOUND THE LEFT WING CENTER SECTION LOWER SKIN SURFACE ABOVE THE LEFT RAM AIR DUCT WITH CORROSION O UT OF LIMITS. (M) 2 L 7 2 4F A16WE 2001050200323 20010502 00323 NM 2001 5 2 P2EA001012 1 20010325 A 5730 SKIN BOEING 737 737244 138448U NM RT WING CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 OKC - DURING C-CHECK, FOUND THE RIGHT WING CENTER SECTION LOWER SKIN SURFACE ABOVE THE RIGHT RAM AIR DUCT WITH CORROSION OUT OF LIMITS. (M) 2 L 7 2 4F A16WE 2001050200324 20010502 00324 NM 2001 5 2 P2EA001014 1 20010330 A 5730 SKIN BOEING 737 737244 138448U NM RT WING CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 OKC - DURING C-CHECK, FOUND THE RIGHT WING LEADING EDGE AT NR 6 LEADING EDGE SLAT ANTI-ICE TUB CUTOUT WITH CRACK, LENGTH .25 INCH. (M) 2 L 7 2 4F A16WE 2001050200325 20010502 00325 NM 2001 5 2 P2EA001068 1 20010328 A 5753 SKIN BOEING 737 737244 138448U NM RT WING TE FLAP DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 DURING C-CHECK, FOUND THE RIGHT WING INBOARD MID-FLAP OUTBOARD EDGE WITH DELAMINATION, LENGTH 6.5 INCH, WIDTH 1 INCH. ( M) 2 L 7 2 4F A16WE 2001050200326 20010502 00326 NM 2001 5 2 P2EA001009 1 20010328 A 5753 SKIN BOEING 737 737244 138448U NM LT WING TE FLAP DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 OKC - DURING C-CHECK, FOUND THE LEFT WING OUTBOARD MID-FLAP INBAORD EDGE WITH DELAMINATION, LENGTH 2 INCHES, WIDTH 1 INC H. (M) 2 L 7 2 4F A16WE 2001050200331 20010502 00331 NM 2001 5 2 KPVA20019 1 20010406 A 3350 1000551 LIGHT DHAV DHC8 DHC8103 1386005 NM COCKPIT BROKEN A KPVA O OTHER O OTHER CR CRUISE 1 WP 13 807WP 023 FLT 1127 - HNL - OVERHEAD DOME LIGHT FELL OUT AND BROKE DURING FLIGHT. REMOVED AND REPLACED PORTABLE EMERGENCY LIGHT AS SEMBLY. OPS CHECK GOOD IAW PSM 1-8-2 CH 33-51-00 PAGE 201-202. (M) 2 H 7 2 4T RT A13NM 2001050200332 20010502 00332 WP 2001 5 2 USAAD01077 1 20010405 A 3350 1001191 LIGHT DOUG DC9 DC981 3022081 WP PAX CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 806US 48038 IND - THE MAIN ENTRY DOOR WALK-AROUND AND THE LOW LEVEL EMERGENCY LIGHTS AT THE FORWARD SERVICE DOOR AND SEAT ROW 11 WER E INOPERATIVE. THE AFT LOW LEVEL EMERGENCY LIGHT RECEIVER WAS INOPERATIVE. MAINTENANCE REPLACED THE MAIN ENTRY DOOR WA LK-AROUND LIGHT ASSEMBLY, THE LOW LEVEL LIGHT BATTERIES, AND THE AFT LOW LEVEL EMERGENCY LIGHT RECEIVER. (M) 2 L 7 2 4F A6WE 2001050200333 20010502 00333 WP 2001 5 2 AALA20010613 1 20010321 A 4990 B-NUT DOUG DC9 DC982 3022082 WP APU BAY LOOSE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 422AA 49334 ORD-BDL - FLT 1460 - EN ROUTE SHORTLY AFTER TAKEOFF DETECTED SMOKE AND HAZE IN COCKPIT AND CABIN. RETURNED ORD AND LAND ED WITHOUT FURTHER INCIDENT. REPLACED WATER SEPARATOR BAGS. TIGHTENED OIL COOLER SYSTEM B-NUT LINE AT LEFT SIDE APU CO MPARTMENT. PERFORMED PACK BURNOUT CHECKS PER THE MM. NO SMELL OR SMOKE NOTED. LEAK CHECKS GOOD. SYSTEM GROUND CHECKE D NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001050200334 20010502 00334 WP 2001 5 2 AALA20010622 1 20010323 A 3222 59100448 STRUT DOUG DC9 DC982 3022082 WP NLG LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 448AA 49474 MIA-ATL - FLT 1130 - SHORTLY AFTER TAKEOFF UNABLE TO RETRACT NOSE LANDING GEAR. RETURNED MIA AND LANDED WITHOUT FURTHER INCIDENT. REPLACED NOSE LANDING GEAR STRUT. ACCOMPLISHED LEAK CHECK. NO LEAKS NOTED. SWUNG NOSE LANDING GEAR. SYST EM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001050200335 20010502 00335 WP 2001 5 2 AALA20010615 1 20010322 A 3231 DOOR DOUG DC9 DC982 3022082 WP NLG OUT OF ADJ A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 430AA 49342 DFW-GRU - FLT 1663 - EN ROUTE SHORTLY AFTER TAKEOFF DETECTED A LOUD VIBRATION AT FORWARD PART OF AIRFRAME. RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. READJUSTED NOSE LANDING GEAR DOOR. SYTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001050200336 20010502 00336 NM 2001 5 2 AALA20010563 1 20010319 A 3350 LAMP BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 941AN 29534 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 23D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 23D. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2001050200337 20010502 00337 NM 2001 5 2 AALA20010603 1 20010321 A 3350 SOCKET BOEING 737 737* NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 912AN 29513 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 18 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET AT ROW 18. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2001050200338 20010502 00338 NM 2001 5 2 AALA20010564 1 20010319 A 3350 LAMP BOEING 737 737823 13844BZ NM CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 941AN 29534 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LGIHT AT SEAT 17D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 17D. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2001050200339 20010502 00339 WP 2001 5 2 AALA20010635 1 20010328 A 3350 8039001 BATTERY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70425 49337 DFW- DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 8, 9, AND 10 DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY AT SEAT 8, 9 AND 10. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001050200340 20010502 00340 WP 2001 5 2 AALA20010636 1 20010327 A 3350 8039001 BATTERY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 3515 49892 DFW - DURING OVERNIGHT MAINTNANCE, CEILING MOUNTED EMERGENCY EXIT LIGHT AT ROW 27 THROUGH 29 DIM. REPLACED CEILING MOUN TED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001050200341 20010502 00341 WP 2001 5 2 AALA20010637 1 20010327 A 3350 8039001 BATTERY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 287AA 49299 DFW - DURING OVERNIGHT MAINTENANCE, CEILING MOUNTED EMERGENCY EXIT LIGHT AT ROW 7 THROUGH 10 DIM. REPLACED CEILING MOUN TED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001050200342 20010502 00342 WP 2001 5 2 AALA20010638 1 20010327 A 3350 8039001 BATTERY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7528A 49920 DURING OVERNIGHT MAINTENANCE, CEILING MOUNTED EMERGENCY EXIT LIGHT AT ROW 23 THROUGH 26 DIM. REPLACED EMERGENCY EXIT LI GHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001050200343 20010502 00343 WP 2001 5 2 AALA20010640 1 20010328 A 3350 8039001 BATTERY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 482AA 49675 DURING OVERNIGHT MAINTENANCE, CEILING MOUNTED EMERGENCY EXIT LIGHT AT ROW 27 THROUGH 29 DIM. REPLACED CEILING MOUNTED E MERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001050200344 20010502 00344 WP 2001 5 2 AALA20010645 1 20010329 A 3350 8039001 BATTERY DOUG DC9 DC982 3022082 WP TAIL INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 420AA 49332 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT TAILCONE DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTE M GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001050200345 20010502 00345 WP 2001 5 2 AALA20010646 1 20010329 A 3350 SOCKET DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 573AA 53092 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 7D DIM. REPLACED EMERGENCY EXIT LIGHT FLOOR PATH SOCKE T. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001050200346 20010502 00346 NM 2001 5 2 EIA2001148 1 20010312 A 5320 WEB BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - DOOR HORIZ WEB CRACKED AT CTR 07 BEAM NR 1 AREA. REPAIRED WEB PER SRM 51-40-02 FIG 2. (M) 2 L 7 4 4F A20WE 2001050200347 20010502 00347 NM 2001 5 2 EIA2001147 1 20010312 A 5311 141U100715 FRAME BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND FLOORBEAM LEFT BS 340 CRACKED AT FRAME FASTENER HOLE, RUNNING OUTBOARD 4TH FASTENER HOLE. REPLACED LE FT BS 340 FRAME BETWEEN STRINGER 0-14L PER EO 53-747-1143-91 REV E AND DWG 624U0003 SH 8D. (M) 2 L 7 4 4F A20WE 2001050200348 20010502 00348 NM 2001 5 2 EIA2001146 1 20010312 A 5315 FLOORBEAM BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND FLOORBEAM RIGHT BS 380 CRACKED AT FLOORBEAM WEB FASTENER HOLE THROUGH THICKNESS, RUNNING UPWARD. TRIM MED OFF CRACK, NDT INSPECTED AND REPAIRED PER EO 53-747-1625-01 REV A AND BSB 53A2429 FIG 5. (M) 2 L 7 4 4F A20WE 2001050200349 20010502 00349 NM 2001 5 2 EIA2001145 1 20010312 A 5315 FLOORBEAM BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND FLOORBEAM LEFT BS 420 CRACKED AT FLOORBEAM WEB FASTENER HOLE THROUGH THICKNESS, RUNNING INBOARD. TRIM MED OFF CRACK, NDT INSPECTED, AND REPAIRED FLOORBEAM WEB PER SRM 53-10-07 FIG 11. (M) 2 L 7 4 4F A20WE 2001050200350 20010502 00350 NM 2001 5 2 EIA2001144 1 20010312 A 5315 FLOORBEAM BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND FLOORBEAM RIGHT BS 420 CRACKED AT FLOORBEAM WEB FASTENER HOLE THROUGH THICKNESS, RUNNING DOWNWARD. TR IMMED OFF CRACK, NDT INSPECTED, AND REPAIRED FLOORBEAM WEB PER SRM 53-10-07 FIG 11. (M) 2 L 7 4 4F A20WE 2001050200351 20010502 00351 NM 2001 5 2 EIA2001143 1 20010312 A 5311 141U105548 FRAME BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAEC0 - FOUND FLOORBEAM RIGHT BS 520 CRACKED AT WEB AND FRAME FASTENER HOLE THROUGH THICKNESS, RUNNING INBOARD AND O UTBOARD. REPAIRED U/D FLOORBEAM WEB BS 520 RBL 60 TO RBL 98 PER SRM 53-10-07 FIG 11. REPLACED RT BS 520 FRAME BETWEEN STRINGER 0-14R PER EO 53-747-1143-91 REV E AND DWG 624U0003 SH 26F. (M) 2 L 7 4 4F A20WE 2001050200352 20010502 00352 NM 2001 5 2 EIA2001142 1 20010312 A 5315 FLOORBEAM BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND FLOORBEAM LEFT BS 360 CRACKED AT UPPER CHORD FASTENER HOLE THROUGH THICKNESS, RUNNING UPWARD. TRIMMED OFF CRACK, NDT INSPECTED, REPAIRED UPPER CHORD PER EO 53-747-1625-01 REV A AND BSB 53-2429 FIG 4 AND DWG 141U0044 SH 3. (M) 2 L 7 4 4F A20WE 2001050200353 20010502 00353 NM 2001 5 2 EIA2001141 1 20010312 A 5320 65B167813 FITTING BOEING 747 747273C 1384896 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND BS 1241 LEFT AND RIGHT REAR SPAR KICK FITTINGS CORRODED. REMOVED CORROSION, NDT INSPECTED, FLAP/SHOT PEENED BLENDOUT REGION. REWORKED KICK FITTINGS AND INSTALLED BUSHING PER BOEING MSG EVR-HKG-01-00018H AND RS R-57-12-34 600. (M) 2 L 7 4 4F A20WE 2001050200354 20010502 00354 NM 2001 5 2 20010502AP001 1 20010312 A 5320 65B167814 FITTING BOEING 747 747273C 1384896 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND BS 1241 LEFT AND RIGHT REAR SPAR KICK FITTINGS CORRODED. REMOVED CORROSION, NDT INSPECTED, FLAP/SHOT PEENED BLENDOUT REGION. REWORKED KICK FITTINGS AND INSTALLED BUSHING PER BOEING MSG EVR-HKG-01-00018H AND RS R-57-12-34 600. REF EIA2001141 (M) 2 L 7 4 4F A20WE 2001050200355 20010502 00355 NM 2001 5 2 EIA2001140 1 20010312 A 5320 SUPPORT BRACKET BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND AT BS 2598 LEFT SUPPORT FRAME FOUND 3 FASTENER HOLES CRACKED BETWEEN STRINGER 11L-12L, LBL 35-40, WL 3 15-320. OVERSIZED CRACKED HOLES, NDT INSPECTED, AND INSTALLED FREEZE PLUGS PER BOEING MSG EVR-HKG-01-00047H/00037F/0002 6F/00027H, BSB 53A2427, AND RS R-53-83-34629. (M) 2 L 7 4 4F A20WE 2001050200356 20010502 00356 NM 2001 5 2 EIA2001139 1 20010312 A 5311 FRAME BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND STRINGER 41 MOD, BS 500 FRAME AT STRINGER 31L CRACKED. TRIMMED OFF CRACK, NDT INSPECTED, REPAIRED STR AP AND INSTALLED DOUBLER PER BOEING MSG EVR-HKG-01-00020H/00013F AND RS R-53-12-34602. (M) 2 L 7 4 4F A20WE 2001050200357 20010502 00357 NM 2001 5 2 EIA2001138 1 20010312 A 5313 STRINGER BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND BS 400-520 STRINGER 6R TOP ROW FASTENERS, 5 HOLES CRACKED. STOP DRILLED HOLES, NDT INSPECTED AND REPA IRED DOUBLER PER EO 53-747-1089-91. (M) 2 L 7 4 4F A20WE 2001050200358 20010502 00358 NM 2001 5 2 EIA2001137 1 20010312 A 5313 STRINGER BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND BS 400-520 STRINGER 6L TOP ROW FASTENERS, 32 HOLES CRACKED. STOP DRILLED HOLES, NDT INSPECTED AND REP AIRED DOUBLER PER EO 53-747-1089-91. (M) 2 L 7 4 4F A20WE 2001050200359 20010502 00359 NM 2001 5 2 EIA2001136 1 20010312 A 5210 65BU60751635 STOP FITTING BOEING 747 747273C 1384896 NM R1 DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND R1 DOOR FORWARD LOWER, AFT UPPER, AND AFT LOWER STOP FITTINGS CRACKED, P/NS 65BU60751635, 65B1356618, 65B1356426. STOP FITTINGS REPLACED PER SRM 51-10-01. (M) 2 L 7 4 4F A20WE 2001050200360 20010502 00360 NM 2001 5 2 EIA2001135 1 20010312 A 5410 65B07795U23 FITTING BOEING 747 747273C 1384896 NM NR 1 ENGINE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG-HAECO - FOUND NR 1 ENGINE PYLON DIAGONAL BRACE AFT FITTING CRACKED FROM AFT LEFT ATTACH BOLT HOLE TO OUTBOARD AFT SI DE, AND LEFT 2ND FROM AFT BOLT HEAD BROKEN OFF. REPLACED DIAGONAL BRACE FITTING WITH TAPER SHIM INSTALLED PER BSB 57-22 88, BSB 57A2308, BOEING MSG EVR-HKG-01-00046H/00033F, AND RS R-54-54-34621. (M) 2 L 7 4 4F A20WE 2001050300005 20010503 00005 2001 5 3 MALA010422 4 20010423 A 3416 4039892909 ALTIMETER BAC 146 AVRO146RJ85A 1500097 EU COCKPIT DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 530XJ E2364 DURING FLIGHT NR 3460 OUT OF MSP, CAPT''S ALTIMETER FAILED RIGHT AFTER LIFT-OFF. AFTER LANDING RED OFF FLAG DISAPPEARED , HOWEVER WHEN ALTIMETER SETTING MOVED OFF CURRENT READING RED FLAG RETURNED. AIR RETURN TO MSP. MAINTENANCE REPLACED NR 1 ALTIMETER P/N 4039892-909, SN/ON 97054077, S/N OFF 99074747. NR 1 ALTIMETER OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 2001050300006 20010503 00006 2001 5 3 MALA010423 4 20010422 A 3442 CONNECTOR SAAB SF340 340B 7860101 EU WEATHER RADAR CONTAMINATED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 415XJ 340B415 ON FLIGHT 2877 OUT OF RHI, WEATHER RADAR WET AND TILT AND STABILIZATOR INOP. AIR TURNBACK TO RHI. MAINTENANCE DRIED RA DAR AND CANNON PLUGS. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2001050300007 20010503 00007 SO 2001 5 3 20010430CW006 2 20010405 A 8530 TSIO520VB LIFTER CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO LEFT ENGINE SPALLED D K NONE O OTHER IN INSP/MAINT 1 SW 99 2651S 1120 402C0342 290159R LEFT ENGINE, MECHANIC WAS CHANGING LEAKY PUSHROD TUBE SEALS AND REMOVED LIFTERS TO BLEED OUT OIL. NOTED FACE OF LIFTER TO BE SEVERELY SPALLED. ASSOCIATED CAM LOBE WAS WORN AND STEPPED. REMOVAL OF REMAINING LIFTERS REVEALED VARIED DEGREES OF SPALLING ON ALL INTAKE LIFTERS. NO DAMAGE WAS NOTED ON EXHAUST LIFTERS. ALL INTAKE CAM LOBES SHOWED SIGNS OF WEAR. THERE WERE NO SYMTOMS OF THIS PROBLEM. 1 L 7 2 3O 3 O A7CE E8CE 2001050300008 20010503 00008 NM 2001 5 3 UPS01235775 1 20010420 A 5330 SKIN BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE: C, ON HFEC INSPECTION CRACKS FOUND ON FUSELAGE SKIN AT BS 235.8 BETWEEN SL 223 & 225 LT. SKIN REPAIR CARRIED OUT IAW SRM 530 FIG 3 2 L 7 3 4F A3WE 2001050300009 20010503 00009 NM 2001 5 3 UPS01235780 1 20010419 A 5320 WEB BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE: C, SURFACE CORROSION FOUND ON LOWER SURFACE OF HORIZONTAL WEB S18A RT, BETWEEN BS 880 & 950. ALL REP AIRS CARRIED OUT IAW SRM 51-10-6, 51-10-1, 51-10-2, 51-30-2 & SMRO EO 2001-013-001 UPS ENGINEERING FILE NO 727-53-20015 2 L 7 3 4F A3WE 2001050300010 20010503 00010 NM 2001 5 3 UPS01235782 1 20010430 A 3350 BATTERY BOEING 727 727247 138408F NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 208UP 21701 EMERGENCY EXIT BATTERY DISCHARGED. REMOVED AND REPLACED BATTERY 2 L 7 3 4F A3WE 2001050700530 20010507 00530 NM 2001 5 7 UPS01235785 1 20010502 A 2610 WARNING SYSTEM BOEING 727 72751C 1384015 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 904UP 18946 COMPT SHOWS-TD DELAY FOR FIRE WARNING BELL INDICATOR INOP COCKPIT FIRE BELL WILL NOT SOUND WITH THE ENG FIRE DETECTION P ANEL TEST SWITCH IN A,B,OR A/B THIS APPLIES TO ACTUATING EITHER THE ENG TEST SWITCH OR WHEEL WELL TEST SWITCH. CLEAN ED AND RESECURED WIRING AT TB 224 56 AND 57. TEST VOLTAGE, OK SYSTEM OK PER 26-11-02. 2 L 7 3 4F A3WE 2001050300011 20010503 00011 NM 2001 5 3 UPS01435784 1 20010501 A 3240 BRAKE ASSY BOEING 747 747200B NM MLG INOPERATIVE A IPXA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 522UP 21936 WHILE EXITING RAMP NO NORMAL BRAKES AVAILABLE MOMENTARILY. INSPECTED ALL SYSTEM FOR LEAKS, NONE FOUND. PERFORMED OPERA TION OF BRAKE SYSTEM ON NR 4, NR 1 AND RESERVE SYSTEM. FOUND NORMAL IAW MM 32-40-00. OK FOR SERVICE. 1 L 7 4 4F RT A20WE 2001050700540 20010507 00540 NM 2001 5 7 UPS01535787 1 20010502 A 2810 FUEL CELL BOEING 757 75724APF 1384969 NM RIGHT LEAKING A IPXA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 461UP 28265 RT DRY BAY HAS RUNNING FUEL LEAK ON RIGHT WING INBD OF NR 2 ENGINE. ISOLATED FUEL LEAK AT NR 4 DRY BAY AT I/B BULKHEAD (WE-204.5) AT FWD SIDE OF STRINGER S-15L. CLEANED AND RESEALED INTERNALLY USING TWO PART SEALING METHOD IAW MM 28-11-0 0 LEAK CHECK DUE. 2 L 7 2 4F RT A2NM 2001050300012 20010503 00012 WP 2001 5 3 UPS01835768 1 20010328 A 5730 SKIN DOUG DC8 DC871F 302199D WP LEFT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE: C1, 3, LEFT WING CENTER L/E SKIN IS CRACKED AT XW 257.5 REPAIRED SKIN I.A.W. E.O. DC8-5720-7767-A 2 L 7 4 4F RT 4A25 2001050300013 20010503 00013 WP 2001 5 3 UPS01835769 1 20010330 A 5340 37544731N FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 STA. 390 LONG. 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG. 3754473-1N, AND SRM. 51-1-20D 2 L 7 4 4F RT 4A25 2001050300014 20010503 00014 SO 2001 5 3 WVBA2001021 1 20010417 A 3245 0923150 TUBE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA SIDEWALL UNSERVICEABLE B WVBA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 AL 01 3582P 40 318052103 PILOT TAXIED OUT TO RUNWAY AND REPORTED NOSE TIRE WENT FLAT. AIRCRAFT WAS RECOVERED AFTER INSTALLING NEW WHEEL ASSEMBL Y. IT WAS FOUND THAT THE TUBE HAD A HOLE IN THE SIDE WALL OPPOSITE THE VALVE STEM. THIS IS THE SECOND FLAT RELATED TO A TUBE. 1 L 7 2 3O 3 O A20SO E14EA 2001050300015 20010503 00015 SO 2001 5 3 SWIA972531 1 20010424 A 2710 AILERON EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE WING JAMMED A SWIA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 199SW 120237 AILERONS JAMMED, WILL NOT DEFLECT FOR A LEFT TURN ON TAXI. TIGHTENED SCREW THAT BACKED OUT ON RIGHT AILERON INSPECTION PANEL. CHECKED AILERONS FOR FREEDOM OF MOVEMENT IN BOTH DIRECTIONS. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001050300016 20010503 00016 SO 2001 5 3 SWIA972532 1 20010420 A 3060 RCCB EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE ANTI-ICE SYS FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 290SW 120317 RIGHT PROP HEAT INOP ON BOTH TIMER 1 AND TIMER 2. RETURNED TO FAT. REPLACED RCCB IAW EMB120 MM 30-60-00. OPS CHECK GO OD. P/N: SM600BA, S/N ON: MP01173, S/N OFF: 27735. 2 L 7 2 4T 4 T RT A31SO E20NE 2001050300017 20010503 00017 SO 2001 5 3 SWIA972514 1 20010415 A 5270 FUEL DOOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE WING UNSECURE A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 290SW 120317 RECEIVED SERVICE DOOR WARNING DURING TAKEOFF ROLL. ABORTED AND RETURNED TO GATE. SECURED FUEL DOOR. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001050300018 20010503 00018 EA 2001 5 3 SWIA972520 1 20010420 A 3010 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT FALSE INDICATION A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 423SW 7456 WING OVERHEAT MESSAGE ON TAKEOFF. ABORTED AT APPROXIMATELY 100 KTS. MESSAGE EXTINGUISHED. OPERATED THE WING ANTI ICE SYSTEM ON THE GROUND AT TAKEOFF POWER. COULD NOT DUPLICATE THE PROBLEM. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2001050300019 20010503 00019 SO 2001 5 3 20010430CW007 2 20010405 A 8530 628488 LIFTER CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO RT ENGINE SPALLED D K NONE O OTHER IN INSP/MAINT 1 EA 25 2651S 1120 0342 290160R RIGHT ENGINE, DAMAGE NOTED TO LEFT ENGINE PROMPTED INSPECTION OF THIS ENGINE. REMOVAL OF LIFTER ASSEMBLIES FROM RANDOM CYLINDERS REVEALED SPALLING TO THE LIFTER FALES AND DAMAGE AND WEAR TO THE ASSOCIATED CAM LOBES. THIS DAMAGE WAS NOTED ON THE INTAKE LIFTERS ONLY. 1 L 7 2 3O 3 O A7CE E8CE 2001050300021 20010503 00021 SO 2001 5 3 SWIA972533 1 20010415 A 2434 GENERATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE VIBRATION A SWIA K NONE E VIBRATION/BUFFET CR CRUISE 1 NM 07 562SW 120336 VIBRATION FELT FROM LEFT ENGINE DURING OPERATION. REMOVED AND REPLACED LEFT ENGINE HYD PUMP. (NO FIX). PUMP OPS CHECK S GOOD IAW 29-13-00. REMOVED AND REPLACED LEFT AUX GEN. VIBRATION FIXED, NO DEFECTS. OPS CHECKS GOOD. PUMP - P/N ON PV3-022-2A, S/N ON MX503650, OFF MX375399. AUX GEN P/N ON 30091-010, S/N ON 90007, OFF 677. 2 L 7 2 4T 4 T RT A31SO E20NE 2001050300024 20010503 00024 SO 2001 5 3 C2XA01TY081 1 20010421 A 5230 14522493001 SKIN EMB 135 EMB135ER 3260203 SO CARGO DOOR CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16502 145166 TYS DURING A SCHEDULED INSPECTION THE CARGO DOOR SKIN WAS FOUND CHAFED AROUND THE EXTERIOR HANDLE. MAINTENANCE ACCOMPL ISHED A BLEND REPAIR IAW EMB GST-1314/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001050300025 20010503 00025 SO 2001 5 3 C2XA01TY082 1 20010421 A 2710 14569000425 BRACKET EMB 135 EMB135ER 3260203 SO LT WING GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16502 145166 TYS DURING A SCHEDULED INSPECTION THE LEFT AILERON ACTUATOR ATTACH BRACKET WAS FOUND GOUGED ON THE SECOND FROM INBOARD FITTINGS. MAINTENANCE ACCOMPLISHED A BLEND REPAIR IAW EMB-GST-1299/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001050300026 20010503 00026 SO 2001 5 3 C2XA01TY083 1 20010422 A 5315 14522459001 FLOORBEAM EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16502 145166 TYS DURING A SCHEDULED INSPECTION THE RIGHT OMEGA RAMP ANGLE WAS FOUND CORRODED AT FRAME 20. MAINTENANCE REMOVED AND R EPLACED THE RAMP ANGLE IAW EMB-135 SRM-51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLE TION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001050300027 20010503 00027 SO 2001 5 3 C2XA01TY084 1 20010422 A 2742 14521904420 FITTING EMB 135 EMB135ER 3260203 SO HORIZ STAB GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16502 145166 TYS DURING A SCHEDULED INSPECTION THE RIGHT HORIZONTAL ACTUATOR SUPPORT FITTING WAS FOUND GOUGED. MAINTENANCE ACCOMPLI SHED A BLEND REPAIR IAW EMB GST-1340/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001050300028 20010503 00028 EU 2001 5 3 RAIA00104016 1 20010423 A 2432 16566 BATTERY AEROSP ATR72 ATR72202 8680940 EU CARGO BAY DISCHARGED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 722TE 15312 50 220 7170-STL-DURING TAXI EMERGANCY BATTERY LIGHT REMAINS ON. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY IAW ATR 72 MAINTENANCE MANUAL. 2 H 7 2 4T RT A53EU 2001050300029 20010503 00029 SO 2001 5 3 C2XA01TY085 1 20010422 A 5315 145217132003 FLOORBEAM EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16502 145166 TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND OMEGA BEAM WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION AT FRAME 20. MAINTENANCE REPAIRED THE OMEGA BEAM IAW EMB-GST-3120/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPO N COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001050300030 20010503 00030 SO 2001 5 3 C2XA01TY086 1 20010423 A 5415 14528167001 MOUNT EMB 135 EMB135ER 3260203 SO LT PYLON CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16502 145166 TYS DURING A SCHEDULED INSPECTION THE LEFT ENGINE PYLON FORWARD YOKE MOUNT WAS FOUND CHAFED. MAINTENANCE ACCOMPLISHED A BLEND REPAIR IAW EMB GST-1365/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPE CTION. 2 L 7 2 4F RT T00011AT 2001050300031 20010503 00031 EU 2001 5 3 MALA010396 1 20010415 A 7931 522794 INDICATOR SAAB SF340 SF340A 7850100 EU COCKPIT DEFECTIVE A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 114XJ 340A114 DURING CLIMBOUT ON FLIGHT 2802, OUT OF DTW RIGHT ENGINE OIL PRESSURE GAUGE WENT TO ZERO. DURING RETURN THE GAUGE FLICKE RED BACK ON A COUPLE OF TIMES, BUT THEN WENT OUT AGAIN. RIGHT OIL TEMP WORKED FINE. MAINTENANCE ADDED 1 QUART OF OIL T O RT ENGINE, REPLACED RT ENG OIL PRESS/TEMP INDICATOR WITH SERVICABLE UNIT P/N 522794, S/N/OFF 06871426, S/N ON 05861331 . FUNCTIONAL CHECKS ARE GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2001050300032 20010503 00032 EU 2001 5 3 MALA010419 1 20010416 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU E/E BAY MALFUNCTIONED A MALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 15 423XJ 423 AVIONICS SMOKE CAUTION LIGHT ILLUMINATED INTERMITTENTLY DURING PREFLIGHT. NO ACTUAL SMOKE, FUMES OR ODORS WERE DETECTED . MAINTENACE REPLACED AVIONICS SMOKE DETECTOR P/N 72-111211-000, S/N OFF A5331, S/N ON A5322. ALL CHECKS GOOD AT THIS TIME IAW SF340 NR 26. 2 L 7 2 4T RT A52EU 2001050300033 20010503 00033 EU 2001 5 3 MALA010420 1 20010413 A 2750 8519ME CONTROL UNIT SAAB SF340 340B 7860101 EU T/E FLAPS MALFUNCTIONED A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 417XJ 340B417 DURING FLIGHT 2828, OUT OF DTW, FLAPS CYCLE BETWEEN 0-3 DEGREES EVERY 1-2 MINUTES DURING CRUISE. FLIGHT AND FLT LVL 220 , INDICATED SPEED OF 180-185. AIR RETURN TO DTW. MAINTENANCE REPLACED FLAP CONTROL UNIT AND FLAP CONTROL VALVE. CONTR OL UNIT P/N 8519M3, S/N OFF 061, S/N ON 484. FLAP CONTROL VALVE P/N MP1416100-5, S/N OFF 1365, S/N ON 1606. ALL CHECKS GOOD IAW SF340MM CHAP 27-51-00-5. 2 L 7 2 4T RT A52EU 2001050300034 20010503 00034 2001 5 3 MALA010421 4 20010420 A 3417 8220370123 ADC SAAB SF340 SF340A 7850100 EU E/E BAY FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 48XJ 048 DURING FLIGHT 2739 OUT OF MSP AT 14,000 FT THE FOLLOWING INDICATIONS WERE NOTED: CAP SIDE AIRSPEED INDICATION LOST, FLI GHT DIRECTORS LOST AND FLAGGED, TCAS YELLOW FLAG ON TCAS INDICATOR, RUDDER LIMIT LIGHT ILLUMINATED, TAS INDICATION LOST, OUTSIDE AIR TEMP INDICATOR LOST ATC SAID MODE C INDICATION LOST. ALL INDICATIONS RESTORED TO NORMAL DURING DESCENT THR OUGHT 8,000 FT AND THEN FAILED AGAIN AT 4000 FT. MAINTENANCE PURGED THE NR 1 PITOT SYSTEM WITH DRY NITROGEN, NO MOISTUR E FOUND. REPLACED ADC P/N 822-0370-123, S/N/ON 2939, P/N OFF 622-4401-001, S/N OFF 17234. FAR 91.411 C/W ON 4-18-1 TO 55,000 FT BY COLLINS TEST GOOD. FD, TCAS, RUDDER LIMITER, TAS, OAT ALL TEST GOOD IAW SAAB MM. 2 L 7 2 4T RT A52EU 2001050300035 20010503 00035 EU 2001 5 3 C2XA01CL084 1 20010420 A 3350 OL3042BP LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 16824 166 CLE FLIGHT 3158 THE CREW REPORTED THE RIGHT SIDE LOWER EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED BULBS ON THE RIGHT SIDE LOWER EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A53EU 2001050300036 20010503 00036 EA 2001 5 3 JBXA00269 1 20010421 A 2752 853D10018 ACTUATOR CNDAIR CL600 CL6002B19 EA T/E FLAP FAILED A JBXA O OTHER J WARNING INDICATION DE DESCENT 1 SO 05 589ML 7376 FLAPS FAIL CAUTION MESSAGE ON EICAS. FLAPS FAILED AT 37 DEGREES. ACCOMPLISHED FLAPS FAIL QRH PROCEDURE AND CALCULATION PRIOR TO LANDING. REMOVED AND REPLACED RT OUTBOARD /INBOARD H3 FLAP ACTUATOR IAW CRM AMM 27-53-05, OPS CK GOOD. 2 L 7 2 4F RT A21EA 2001050300037 20010503 00037 EA 2001 5 3 JBXA000270 1 20010422 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 EA COCKPIT ILLUMINATED A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 589ML 7376 CARGO DOOR LIGHT CAME ON IN FLIGHT. RETURNED TO MIA. ADDED MEL 52-70-4 CARGO DOOR INDICATION. 2 L 7 2 4F RT A21EA 2001050300038 20010503 00038 EU 2001 5 3 JBXA000271 1 20010421 A 7931 CONNECTOR FOKKER F28 F28MK0100 4990807 EU TRANSDUCER DIRTY A JBXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 05 109ML 11485 AIRCRAFT INDICATED LOW OIL PRESSURE (NR 2 ENGINE) ON MFDU. FOLLOWED PROCEDURE AND MFDU SHOWED HIGH TGT INDICATION. FOL LOWED PROCEDURE AND RETURNED TO RDU. CLEANED CANNON PLUG ON OIL PRESSURER TRANSDUCER IAW AMM 79-32-01, TGT WITHIN LIMIT S OF AMM 71-00-00 . ENGINE RUN PERFORMED IAW 71-00-00. PERFORMED TGT TEST PART IAW 71-00-00. ALL INDICATIONS NORMAL A T THIS TIME. 2 L 7 2 4F RT 2001050300039 20010503 00039 NE 2001 5 3 20010427CW003 2 20010323 A 7200 CF650C2 ENGINE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 2 CONTAMINATED I M8BB K NONE O OTHER IN INSP/MAINT 1 WP 33 10MB 65388 47907 455393 DURING A CHECK, BOROSCOPE INSPECTION, FOUND METAL AT TAILPIPE OF NR 2 ENGINE. METALLURGICAL ANALYSIS IDENTIFIED MET AL TO BE INCONEL 718 AND SUGGESTED POSSIBEL SOURCE TO BE FROM LPT INTERSTAGE SEALS.AMOUNT OF METAL WAS SIGNIFICANT AND O EM RECOMMENDED ENGINE REPLACEMENT. 2 L 7 3 4F 4 F A22WE E23EA 2001050300040 20010503 00040 WP 2001 5 3 20010427CW004 1 20010323 A 2780 P1969174 PULLEY DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 2 SLAT BROKEN I M8BB O OTHER O OTHER TX TAXI/GRND HDL 1 WP 33 10MB 47907 AFTER LANDING , FLIGHT ENGINEER NOTICE RT DROOPED LEADING EDGE NOT RETRACTED AND FLUSHED WITH ADJACENT SLAT SURFACES. F OUND SUBJECT PULLEY BROKEN, CAUSING NR 2 SLAT EXTEND/TIE CABLE DISLODGED. ALL OF THE NR 2 SLAT CABLES WERE REPLACED DUR ING C CHECK AND PULLEYS CONDITION WERE CHECKED GOOD AND SERVICEABLE THEN. 2 L 7 3 4F 4 F A22WE E23EA 2001050300042 20010503 00042 SO 2001 5 3 20010427CW005 1 20010410 A 7830 7013348924 COMPUTER GULSTM GV GV SO RROYCE BR700 BR700710A110 NE ELECTRONICS RACK INCORRECT E UG8A O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 23 5102 1175 551 AFTER DEPLOYING AND STOWING THE THRUST REVERSERS THE THRUST REVERSER MISCOMPARE ANNUNCIATOR ILLUMINATED MOMENTARILY. AP PARENT CAUSE WAS DCU DATA LATCH UP. CONFIRMED BOTH T/RS TO BE STOWED PROPERLY AND RESET DCU, NR 1 AND NR 2 WITH NO FURT HER OCCURRENCE. 2 L 7 2 4F 4 F RT A12EA E00057EN 2001050300043 20010503 00043 NE 2001 5 3 20010427CW006 2 20010411 A 7310 M259881160 O-RING GULSTM G1159 GIV 3980115 SO RROYCE BR700 BR700710A110 NE RT ENGINE SPLIT E UG8A O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 23 5101 128 550 11236 AFTER DEPLANING PASSENGERS , CREW NOTICED A FUEL LEAK AT THE RIGHT HAND ENGINE. IT WAS REPORTED AS DRAINING FROM THE CO WLING. AN INSPECTOR AND MECHANIC WERE DISPATCHED AND FOUND A FAULTY ORING AT THE LOW PRESSURE FUEL FILTER BOWL. THE OR ING WAS REPLACED AND A SUCCESSFUL LEAK CHECK ACCOMPLISHED. 2 L 7 2 4F 4 F RT A12EA E00057EN 2001050300045 20010503 00045 WP 2001 5 3 ABXA010194 1 20010319 A 5320 DOUBLER DOUG DC8 DC863 302198A WP FUSELAGE BULGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 70572 46079 FINGER DOUBLER FS 80 ON TOP SIDE OF CUSP WEB BULGED AND FASTENERS WERE SHEARED. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM. 2 L 7 4 4F 4A25 2001050300047 20010503 00047 NM 2001 5 3 AWXA0001632 1 20010423 A 5754 656304611H FLAP BOEING 737 737301 1384611 NM LT L/E WING PUNCTURED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 23258 LEFT O/B KRUEGER FLAP PUNCTURED AT ACTUATOR MOUNT. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER IAW AWA EO 03-5743-01106- TB1. 2 L 7 2 4F RT A16WE 2001050300048 20010503 00048 EA 2001 5 3 20010501CW002 2 20010409 A 8500 STUD PIPER PA32 PA32260 7103206 SO LYC O540 O540E4B5 41532 EA GOVERNOR MISINSTALLED E BTHA K NONE O OTHER IN INSP/MAINT 1 AL 01 4803S 321188 L2265040A DURING ENGINE INSTALLATION AFTER OVERHAUL, FOUND ALL 4 GOVERNOR HOLD DOWN STUDS NOT SCREWED FAR ENOUGH INTO CASE. STUDS HAD TO BE TURNED IN .2500 FURTHER TO ALLOW GOVERNOR TO MATE WITH ENGINE. 1 L 7 1 3O 3 O A3SO E295 2001050300049 20010503 00049 EA 2001 5 3 20010501CW003 2 20010409 A 8530 LW67113 ARM PIPER PA32 PA32R300 7103213 SO LYC O540 IO540K1A5 41532 EA ROCKER WORN A BTHA K NONE O OTHER IN INSP/MAINT 1 AL 01 4352F 338 32R7680441 L774448A DURING VALVE CLEARANCE INSPECTION, FOUND NR 6 INTAKE ROCKER ARM FACE WHERE IT CONTACTS ROTATER CAP, WORN SEVERELY .1250 AND BADLY PITTED. ENGINE HAS BEEN ON OIL ANALYSIS SINCE OVERHAUL WITH NO PROBLEMS NOTED. ALL OTHER ROCKER ARMS FOUND N ORMAL. PROBABLE CAUSE IS THAT A WORN UNAIRWORTHY PART WAS PUT IN ENGINE DURING OVERHAUL. 1 L 7 1 3O 3 O A3SO 1E4 2001050300050 20010503 00050 NM 2001 5 3 AWXA0001638 1 20010423 A 5312 651630084 BULKHEAD BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 23258 FS 178 BLKHD CRACKED AT WL 201.5 LBL 5. REPAIRED AREA IAW B737-300 SRM 53-10-08 FIG 211 PG 1-11 AND 51-21-41 PG 701-702 AND 51-40-02 PG 2-4, 6-8, 10-11. 2 L 7 2 4F RT A16WE 2001050300051 20010503 00051 NM 2001 5 3 AWXA0001642 1 20010423 A 5320 651630084 WEB BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 23258 COCKPIT FLOOR CRACKED AT FS 180 WL 207 LBL 23. REMOVED AND REPLACED WEB IAW B737-300 SRM 51-40-02 PG 2-4, 6-8, 10-11, 1 6-17. 2 L 7 2 4F RT A16WE 2001050300052 20010503 00052 EU 2001 5 3 QXEA0100629 1 20010423 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 11234 BOI-EMERGENCY EXIT SIGN IN AFT CABIN HAS BURNT OUT BULBS. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECK GOOD. AIR CRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001050300053 20010503 00053 CE 2001 5 3 20010501CW004 1 20010405 A 5510 12324002 BRACKET CESSNA 210 210L 2073448 CE CONT O520 IO520* 17032 SO HORIZONTAL STAB CORRODED H K NONE O OTHER IN INSP/MAINT 1 SO 15 59299 16742 21060199 DURING ANNUAL INSPECTION FOUND EXFOLIATION ON RIGHT HORIZONTAL STAB ATTACH BRACKET. 1 H 7 1 3O 3 O 3A21 E5CE 2001050300054 20010503 00054 2001 5 3 DHL2001366014 4 20010424 A 2230 COMPUTER AIRBUS 300 A300B4203 3930306 EU E/E BAY MALFUNCTIONED A DHLA K NONE O OTHER CR CRUISE 1 SO 01 366DH 249 AUTO THROTTLE DISENGAGES (DISARMS) IN CRUISE FLIGHT (SWITCH ON GLARESHIELD). RE-RACKED AUTO THROTTLE COMPUTER. OPS CHE CKED GOOD. 2 L 7 2 4F RT A35EU 2001050300055 20010503 00055 NM 2001 5 3 DHL2001741005 1 20010424 A 2611 SMOKE DETECTOR BOEING 727 7272Q9 138448M NM CARGO BAY MALFUNCTIONED A DHLA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 741DH 21931 CARGO SMOKE ANNUNCIATOR ILLUMINATED IN FLIGHT. CHECKED CONNECTIONS ON NR 5 TEST SW. NO DEFECTS FOUND. SYS OPS NORMAL ON GND PER MM 26-17-1000. 2 L 7 3 4F RT A3WE 2001050300056 20010503 00056 2001 5 3 DHL2001804004 4 20010421 A 3417 9B8101015 ADC DOUG DC8 DC873F 302199F WP E/E BAY MALFUNCTIONED A DHLA K NONE O OTHER CR CRUISE 1 SO 01 804DH 46124 AFTER AIRSPEED INDICATORS DECREASED TO ZERO THE A/C BEGAN TO OSCILLATE IN PITCH (+/- 150FT) ALT HOLD REMAINED INOP. PIT CH DUMP MODE OK. NAV SELECT OK. AUTO PILOT OK BELOW 1800 FT. REPLACED DADC AND TESTED PER SMM 34-11-31. PITOT STATIC LEAK TEST FAILED. FOUND ALT PITOT LINE IN NOSE COMPARTMENT LEAKING. REPLACED LINE. PERFORMED LEAK CHECK ON PITOT SYS TEM. LEAK CKS GOOD. DADC CHECKS GOOD. REF ITEM 1P THIS L/P A/P OPS NORMAL PER MM 22-10-0. 2 L 7 4 4F RT 4A25 2001050300057 20010503 00057 EU 2001 5 3 JBXA000272 1 20010422 A 7931 APTE173RM75G TRANSMITTER FOKKER F28 F28MK0100 4990807 EU NR 2 ENGINE FAILED A JBXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 05 109ML 11485 RETURNED TO RDU DUE TO NR 2 ENGINE LOW OIL PRESSURE INDICATION. REMOVED AND REPLACED NR 2 ENGINE OIL PRESSURE TRANSMITT ER IAW 77-47-01. PERFORMED GROUND RUN OF ENGINE NR 2 AT DIFFERENT POWER SETTINGS. COULD NOT DUPLICATE LOW OIL PRESSURE . REF MDW NRC 14811 FOR WORK PERFORMED. 2 L 7 2 4F RT 2001050300058 20010503 00058 NM 2001 5 3 DHL2001702010 1 20010424 A 2750 DT2RA7 SWITCH BOEING 727 72730C 1384009 NM COCKPIT STUCK A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 702DH 19793 TAKEOFF WARNING HORN SOUNDED WHEN TAKEOFF THRUST WAS APPLIED WITH FLAPS AT 15, SPEED BRAKE STOWED, AND STAB TRIM AT 5.5. TAKEOFF WAS DISCONTINUED. FOUND TAKEOFF WARNING SWITCH STUCK. REMOVED AND REPLACED SWITCH. TESTED SYSTEM IAW DHL MM 27-51-191. 2 L 7 3 4F A3WE 2001050300059 20010503 00059 WP 2001 5 3 01FDEA00296 1 20010424 A 2920 AGK7002553 HYDRAULIC LINE DOUG DC10 DC1030F 3023504 WP CARGO BAY LEAKING A FDEA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 25 315FE 48313 EVIDENCE OF HYD LEAK COMING FROM AFT CARGO COMPARTMENT. *S/D* REPAIRED PIPE ASSY AGK7002-553 PER MM 20-10-01-2 AND REP LACED PNEU DUCT INSULATION BLANKETS. 2 L 7 3 4F RT A22WE 2001050300060 20010503 00060 WP 2001 5 3 MWEA010633 1 20010424 A 5240 4917889501 HINGE DOUG DC9 DC932 3022066 WP DOOR WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 AFT PRESSURE BULKHEAD DOOR UPPER HINGE LOBES ARE WORN. REMOVED AND REPLACED UPPER HINGE LINK. 2 L 7 2 4F A6WE 2001050300061 20010503 00061 WP 2001 5 3 MWEA010635 1 20010424 A 5230 39132492 FITTING DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 NR 2 BEAM END FITTING IS CRACKED ON FORWARD END. REMOVED AND REPLACED END FITTING. 2 L 7 2 4F A6WE 2001050300062 20010503 00062 WP 2001 5 3 MWEA010636 1 20010424 A 5230 39132392 PAN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 FORWARD CARGO DOOR OUTER PAN IS CRACKED UNDER FORWARD STOP FITTING AREA. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001050300063 20010503 00063 WP 2001 5 3 MWEA010637 1 20010424 A 5320 99576641 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 INTERCOSTAL WEB IS CRACKED UNDER LOWER FORWARD STOP FITTING. FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001050300064 20010503 00064 WP 2001 5 3 MWEA010638 1 20010424 A 5310 J06011917 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 LEFT SIDE SHEAR TIE IS CRACKED AT STATION 980 ABOVE LONGERON 15 ON FORWARD SIDE. REMOVED AND REPLACED SHEAR TIE. 2 L 7 2 4F A6WE 2001050300065 20010503 00065 EU 2001 5 3 QXEA0100496 1 20010416 A 3220 200725001 LANDING GEAR FOKKER F28 F28MK4000 4990810 EU NLG MALFUNCTIONED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 09 476US 40378 5492 11224 PDX - SMELL OF BURNING RUBBER NOTED AFTER TAKEOFF. REMOVED AND REPLACED NOSE LANDING GEAR, NOSE TIRES, AND ADJUSTED STE ERING CABLES. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001050300066 20010503 00066 WP 2001 5 3 MWEA010640 1 20010424 A 5410 991550032 ANGLE DOUG DC9 DC932 3022066 WP RT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 RIGHT PYLON WEB ATTACH ANGLE CRACKED AT STATION 1038 JUST INBOARD OF AFT ENGINE MOUNT. FABRICATED AND INSTALLED ATTACH ANGLE. 2 L 7 2 4F A6WE 2001050300067 20010503 00067 WP 2001 5 3 MWEA010641 1 20010424 A 5712 99193507 RIB DOUG DC9 DC932 3022066 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 LEFT WING LOWER RIB CAP HAS MODERATE CORROSION ON UPPER SURFACE INBOARD SIDE AT XRS 91 BETWEEN STRINGER 17 AND 22. FABR ICATED AND INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F A6WE 2001050300068 20010503 00068 WP 2001 5 3 MWEA010642 1 20010424 A 5415 SRO954000212 ATTACH ANGLE DOUG DC9 DC932 3022066 WP RT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 RIGHT HAND PYLON UPPER ATTACH ANGLE IS CRACKED, STATION 980. FABRICATED AND INSTALLED ANGLE AND SPLICE STRAPS. 2 L 7 2 4F A6WE 2001050300069 20010503 00069 WP 2001 5 3 MWEA010630 1 20010424 A 5320 9915565155 ANGLE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 NR 2 BEAM ON AFT PRESSURE BULKHEAD HAD A CRACKED ATTACH ANGLE. REMOVED ANGLE, FABRICATED, DRILLED, AND INSTALLED NEW AN GLE. 2 L 7 2 4F A6WE 2001050300070 20010503 00070 WP 2001 5 3 MWEA010631 1 20010424 A 5230 39250471 STOP FITTING DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 AFT CARGO DOOR LOWER CENTER STOP FITTING ON DOOR WAS CRACKED. REMOVED FITTING, DRILLED AND INSTALLED NEW FITTING. 2 L 7 2 4F A6WE 2001050300071 20010503 00071 WP 2001 5 3 MWEA010632 1 20010424 A 5230 39250471 FITTING DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 AFT CARGO DOOR NR 2 BEAM AFT END FITTING WAS CRACKED. REMOVED FITTING, DRILLED, AND INSTALLED NEW FITTING. 2 L 7 2 4F A6WE 2001050300072 20010503 00072 WP 2001 5 3 MWEA010634 1 20010424 A 5312 591013085 BULKHEAD DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 LEFT LOWER VENTRAL DOOR CORNER HAS CRACK INDICATION ON RADIOGRAPH APPROXIMATELY 1.25 INCH LONG. TRIMMED AND LOCATED DOU BLERS IAW SERVICE BULLETIN DC9 53-137. INSTALLED DOUBLERS IAW SERVICE BULLETIN DC9 53-137 AND PLACED ON WI 5728 FOR REP ETITIVE INSPECTION. 2 L 7 2 4F A6WE 2001050300073 20010503 00073 WP 2001 5 3 MWEA010643 1 20010424 A 5330 5910228 SKIN DOUG DC9 DC914 3022034 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 DENT IN AFT FUSELAGE STATION 958 APPROXIMATELY LONGERON 16 RIGHT. REPAIRED IN ACCORDANCE WITH 53-01 FIGURE 4. 2 L 7 2 4F A6WE 2001050300074 20010503 00074 NM 2001 5 3 AWXA0001623 1 20010423 A 5315 654680324 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 CRACK SUSPECTED AFT SIDE OF FLOORBEAM STA 520 LBL 24.75 - NDT CONFRIMED CRACK. REPAIRED IAW ENG REPAIR 03-5321-01111-BA 1. 2 L 7 2 4F RT A16WE 2001050300075 20010503 00075 NM 2001 5 3 AWXA0001624 1 20010423 A 5230 65C80735149 CROSSBEAM BOEING 737 7373G7 1384595 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 FWD CARGO DOOR LWR CROSS BEAM CRACKED AT AFT AND FWD SIDE. CARGO DOOR REMOVED IAW MM 52-31-00 PG 401-407; REMOVED FASTE NERS ON LWR INNER SKIN; REMOVED DAMAGED WEB AND T-CHORD; INSTALLED NEW WEB AND T-CHORD IAW SRM 51-40-02; REINSTALLED INN ER SKIN IAW SRM 51-40-02; REINSTALLED DOOR IAW W/C R8M52001 AND RIGGED IAW W/C R8M52001. WEB - P/N: 65C46921-183. 2 L 7 2 4F RT A16WE 2001050300076 20010503 00076 WP 2001 5 3 ABXA010189 1 20010320 A 5311 FRAME DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 FRAME LINK FLANGE CORRODED AT STA 1000 ABOVE LONGERON 36. 2 L 7 4 4F 4A25 2001050300077 20010503 00077 WP 2001 5 3 ABXA010190 1 20010402 A 5730 PANEL DOUG DC8 DC863 302198A WP WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 PANEL 505F BOLT HOLES HAVE CRACK INDICATIONS FOUND DURING NDT INSPECTION. 2 L 7 4 4F 4A25 2001050300078 20010503 00078 WP 2001 5 3 ABXA010191 1 20010320 A 5311 FRAME DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 AFT CARGO PIT FRAME AT FS 1480 ABOVE LONGERON 36 FRAME IS CORRODED. 2 L 7 4 4F 4A25 2001050300079 20010503 00079 WP 2001 5 3 ABXA010192 1 20010320 A 5320 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 Z-FITTING IN AFT CARGO PIT AT FS 1220 LONGERON 34L-35L IS CORRODED. 2 L 7 4 4F 4A25 2001050300080 20010503 00080 WP 2001 5 3 ABXA010193 1 20010319 A 5320 3755845 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 70572 46079 AFT CARGO PIT AT FS 1150 INSIDE FWD TORQUE BOX LONGERON 35R-36R WAS CORRODED. MAINTENANCE REPAIRED THE AREA IAW DC-8 SR M 53-2-0. 2 L 7 4 4F 4A25 2001050300081 20010503 00081 WP 2001 5 3 ABXA010195 1 20010318 A 5313 LONGERON DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 LONGERON 24L FS 980 CRACKED BETWEEN FASTENERS ON TOP SIDE. MAINTENANCE REPAIRED THE AREA IAW DC-8 SRM. 2 L 7 4 4F 4A25 2001050300082 20010503 00082 WP 2001 5 3 ABXA010196 1 20010324 A 5320 DOUBLER DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 70572 46079 ALC STATION 1220-1228 LONGERON 30R-31R TORQUE BOX INTERNAL DOUBLER HAD DEEP EXFOLIATION CORROSION. MAINTENANCE REPAIRED THE AREA IAW ABX REA D853-40368. 2 L 7 4 4F 4A25 2001050300083 20010503 00083 WP 2001 5 3 ABXA010197 1 20010320 A 5311 FRAME DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 70572 46079 AFT CARGO PIT FRAME AT FS 1120 ABOVE LONGERON 35R-36R WAS CORRODED UNDER AND AROUND NUT PLATES. MAINTENANCE REPAIRED TH E AREA IAW DC-8 SRM 53-2-0. 2 L 7 4 4F 4A25 2001050300084 20010503 00084 WP 2001 5 3 ABXA010198 1 20010317 A 5330 SKIN DOUG DC8 DC863 302198A WP FUSELAGE DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 70572 46079 FUSELAGE EXTERIOR SKIN CREASED AND GOUGED AT STA 115-120 LONGERON 21R-23R. MAINTENANCE REPAIRED THE AREA IAW DC-8 SRM 5 3-2-1. 2 L 7 4 4F 4A25 2001050300085 20010503 00085 NM 2001 5 3 AWXA0001625 1 20010423 A 5240 6545871 SKIN BOEING 737 7373G7 1384595 NM SERVICE DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 FWD SERVICE DOOR OUTER SKIN CRACKED AT LWR HINGE CUTOUT, FWD UPPER CORNER. FWD SERVICE DOOR REMOVED AND REPLACED IAW MM 52-41-00 PG 401-406; CRACK REPAIRED IAW SRM 52-00-01 FIG 202; EDGE SEALED IAW SRM 51-10-01; POINTED IAW MM 51-29-99. 2 L 7 2 4F RT A16WE 2001050300086 20010503 00086 EU 2001 5 3 C2XA01BT067 1 20010424 A 3350 44 LIGHT AEROSP ATR42 ATR42320 8680930 EU EXTERIOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14832 187 BTV---CO3014, DURING LINE CHECK AND WEEKLY CHECK MAINTENANCE FOUND RIGHTHAND AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHTHAND AFT EMERGENCY LIGHT BULP IAW ATR42 STANDARD PRACTICES. 2 H 7 2 4T RT A53EU 2001050300087 20010503 00087 NM 2001 5 3 AWXA0001626 1 20010423 A 5240 65C807351 STRUCTURE BOEING 737 7373G7 1384595 NM SERVICE DOOR CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 AFT SERVICE DOOR INNER SILL CHORD CORRODED FROM APPROX BS 960-986.5. CORROSION REMOVED - MAT LOSS IN EXCESS IAW SRM 53- 60-15 FIG 101 PG 104 LIMITS; INNER SILL CHORD REPLACED BY NEW CHORD; DRAIN TROUGH REINSTALLED; DRAIN TROUGH FITTINGS INS TALLED IAW EO 53-15-15. 2 L 7 2 4F RT A16WE 2001050300089 20010503 00089 SO 2001 5 3 SWIA972511 1 20010418 A 3150 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT FALSE ACTIVATION A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 205SW 120260 ON TAKEOFF ROLL WITH POWER AT 100 PERCENT TORQUE, GOT A T6 WARNING. BOTH ENGINES T6 GAUGES WERE LESS THAN 816 DEGREES. NO RED LIGHTS CAME ON THE GAUGE. ABORTED TAKEOFF. REPLACED AURAL WARNING COMPUTER. PERFORMED OPS CHECKS. OPS CHECKS GOOD. P/N 8-0557-11, S/N ON 0427, S/N OFF 0467. 2 L 7 2 4T 4 T RT A31SO E20NE 2001050300090 20010503 00090 SO 2001 5 3 SWIA972512 1 20010417 A 5270 SWITCH EMB 120 EMB120RT SO PWA 118 PW118 NE DOOR OUT OF ADJ A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 1117H 120117 ON TAKEOFF ROLL, PRIOR TO V1 TRIPLE CHIME, DOORS AURAL WARNING SOUNDED. TAKEOFF WAS ABORTED. AIRCRAFT RETURNED TO GATE . (FORWARD DOOR LIGHT ILLUMINATED). DEFERRED FORWARD DOOR WARNING SYSTEM IAW MEL 52-70-1C. 4-19-01 PDX FOUND LOWER M ICROSWITCH COVER MISSING, REPLACED. CHECKED AND ADJUSTED MICROSWITCH ROLLER SPRING TENSION. VISUALLY CHECKED WIRING AT MICROSWITCH AND FORWARD HINGE ON PAX DOOR. NO DISCREPANCIES NOTED. DOOR WARNING OPERATION CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001050300091 20010503 00091 EA 2001 5 3 SWIA972513 1 20010417 A 2163 SENSOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE CABIN TEMP MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 07 409SW 7056 DISPLAY COOL MESSAGE CAME ON CLIMBING THROUGH 12,000 FEET. TRIED FLT ALT AND STBY POSITIONS ON DISPLAY FAN. MESSAGE RE MAINED FOR ABOUT 10 MINUTES. VERIFIED FAN OPERATION IN ALL POSITIONS AND AIR FLOW GOOD, NO LEAKS. REPLACED AIRFLOW SEN SOR. OPS CHECK GOOD ON GROUND. P/N: 009519-04. 2 L 7 2 4F 4 F RT A21EA E15NE 2001050300092 20010503 00092 2001 5 3 SWIA972515 4 20010416 A 3414 INDICATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT FAULTY A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 234SW 120308 HIGH SPEED AURAL WARNING ON TAKEOFF ROLL AT APPROXIMATELY 60 KIAS. ABORTED TAKEOFF. REPLACED NR 1 AIRSPEED INDICATOR. OPS CHECK GOOD. LEAK CHECKS GOOD. P/N ON 39948-E2903 OFF 329ASI, S/N ON 496 OFF AJ126. 2 L 7 2 4T 4 T RT A31SO E20NE 2001050300093 20010503 00093 EA 2001 5 3 SWIA972516 1 20010406 A 3030 ANTI-ICE SYSTEM CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE AOA VANE MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 07 409SW 7056 RIGHT AOA VANE CAUTION MESSAGE CAME ON IN FLIGHT. RETURNED TO SLC. CYCLED POWER. RAN 20 MINUTES. RIGHT AOA HEAT OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2001050300095 20010503 00095 SO 2001 5 3 SWIA972518 1 20010410 A 2131 CONTROLLER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CABIN PRESSURE MALFUNCTIONED A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 293SW 120320 LOSS OF CABIN PRESS AT 17K SUDDEN TOTAL LOSS. RETURNED TO SEA. RE-SAFTIED MANUAL OUTLFOW VALVE TO THE CLOSED POSITION DUE TO THE MANUAL PRESSURIZATION PREVIOUS DEFERRAL. AUTO PRESSURIZATION OPS CHECK GOOD ON GROUND AT THIS TIME. INSTALL ED NEW AUTO CONTROLLER. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001050300096 20010503 00096 EA 2001 5 3 SWIA972521 1 20010420 A 2740 SWITCH CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT FAULTY A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 416SW 7089 STABILIZER TRIM AND MACH TRIM CAUTION MESSAGE CAME ON AFTER TAKEOFF. FOLLOWED QRH, WOULD NOT RE-ENGAGE. AIRCRAFT RETUR NED TO THE FIELD. CAT II. REMOVED AND REPLACED FIRST OFFICER''S PITCH TRIM DISCONNECT SWITCH IAW MM 27-41-30. PERFORM ED STABILIZER TRIM OPS AND FUNCTIONAL CHECKS IAW MM 27-40-00-710-801. OPS CHECKS GOOD, NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A21EA E15NE 2001050300097 20010503 00097 NE 2001 5 3 SWIA972522 2 20010420 A 7321 CONNECTOR EMB 120 EMB120RT SO PWA 118 PW118 NE LT EEC CONTAMINATED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 1105G 120105 POWER LEVER SPLIT OF 2 INCHES ON T/O, ABORTED. TRIED STATIC EVERYTHING WORKED. TOOK OFF, LEFT EEC FAILED. DEFERRED PER MEL 73-21-1. CLEANED OIL FROM LEFT SIGNAL CONDITIONER CANNON PLUGS. REPAIRED AUXILIARY GENERATOR DRAIN LINE. OPS CH ECKS GOOD. CONDUCTED TRIM CHECK TRIM GOOD IAW EMB MM 73-21-00. 2 L 7 2 4T 4 T RT A31SO E20NE 2001050300098 20010503 00098 SO 2001 5 3 SWIA972523 1 20010420 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE T/E FLAP FAILED A SWIA A UNSCHED LANDING K J F FLUID LOSS WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 NM 07 233SW 120307 COMPLETE LOSS OF BLUE SYSTEM HYDRAULICS AT SBP, COMPLIED WITH QRH. RETURNED TO LAX AND LANDED FLAPS 0 DEGREES. INSPECT ED AND FOUND T6 CAP SCREWS OF RIGHT NACELLE ACTUATOR LOCK PIN SOLENOID SHEARED OFF. INSTALLED SERVICEABLE RIGHT NACELLE FLAP ACTUATOR IAW MM 27-50-00, SEE RII 27-307. CYCLED FLAPS NUMEROUS TIMES, OPS CHECKS GOOD. NO LEAKS NOTED. 2 L 7 2 4T 4 T RT A31SO E20NE 2001050300099 20010503 00099 SO 2001 5 3 SWIA972524 1 20010420 A 3020 BOOT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 229SW 120305 OVER VTU IN ICING CONDITIONS, BOTH ENGINE DEICE BOOTS FAILED. RECYCLED SWITCHES, LEFT ENGINE DEICE BOOT FAILED AND RIGH T ONE WORKED NORMALLY. RETURNED TO LAX. REPLACED LEFT ENGINE INLET DUCT WITH SERVICEABLE UNIT. S/N OFF 080 ON 213. R AN ENGINE, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001050300100 20010503 00100 SO 2001 5 3 SWIA972525 1 20010421 A 3010 BOOT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE ANTI-ICE SYS FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 212SW 120276 RIGHT INBOARD STABILIZER BOOT FAILS IN BOTH TIMERS 1 AND 2 IN BOTH THE HEAVY AND LIGHT POSITIONS. RETURNED TO SLC. REM OVED AND REPLACED LEFT WING INBOARD DEICE BOOT IAW MM 30-10-00 AND RII 30-301. OPS CHECK GOOD. P/N ON P29S-705135-25, S/N ON MP19510, S/N OFF MB26310. 2 L 7 2 4T 4 T RT A31SO E20NE 2001050300101 20010503 00101 NM 2001 5 3 01FDEA00293 1 20010423 A 2612 FIRE LOOP DOUG MD11 MD11F 3023600 NM NR 1 ENGINE FAULTY A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 582FE 48420 AFT T/O LEVEL 1 ALERT FIRE DET NR 1 FAIL ILLUMINATED. NR 1 ENG A-LOOP DEFERRED. *S/D* REMOVED AND REPLACED LWR RAIL W HICH INCLUDED DH8 & DH5 PER MD11 MM 26-11-03-4 B-LOOP. CHECK GOOD. 2 L 7 3 4F RT A22WE 2001050300102 20010503 00102 SO 2001 5 3 C2XA01CL083 1 20010414 A 3397 W192883222 WIRE EMB 145 EMB145ER 3260211 SO CABIN BROKEN A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 14933 145018 CLE FLIGHT NR 3623 THE CREW REPORTED AISLE PATH EMERGENCY LIGHTS BY SEATS 8 AND 9 INOPREATIVE. MAINTENANCE REPAIRED B ROKEN WIRE AND OPERATIOMAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2001050300103 20010503 00103 SO 2001 5 3 C2XA01TY079 1 20010420 A 5330 14523058001 SKIN EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16502 145166 TYS DURING A SCHEDULED INSPECTION THE FUSELAGE SKIN WAS FOUND CORRODED AT FRAME 67 ON STRINGER 17R. MAINTENANCE REPAIR ED THE DAMAGE AREA IAW EMB-135 SRM 53-31-01, REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001050300104 20010503 00104 NM 2001 5 3 01FDEA00294 1 20010423 A 3260 WARNING SYSTEM DOUG MD11 MD11F 3023600 NM COCKPIT MALFUNCTIONED A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 592FE 48550 RED NOSE GEAR WARN LIGHT ILLUM. RECYCLED GEAR LIGHT GREEN ON 2ND ATTEMPT. INSP DOWN PROX AND LOCK PROX SENSOR FOUND NO RMAL. PROX SWITCH ELECTRONICS UNIT. TEST PASSED NO SIGNS OF LEAKAGE OR DAMAGE ON UNLOCK CYLINDER AND CK VALVE PER FIM 32-30-06-02. AC OK FOR SERVICE. 2 L 7 3 4F RT A22WE 2001050300105 20010503 00105 SO 2001 5 3 C2XA01TY080 1 20010421 A 5320 14522460013 FLOOR SUPPORT EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16502 145166 TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND OMEGA BEAM TOP CAP BETWEEN FRAMES 18 AND 22 WAS FOUND GOUGED AND CORRO DED. MAINTENANCE REMOVED AND REPLACED THE OMEGA BEAM TOP CAP IAW EMB-135 SRM-51-40-02, THE REPAIR WAS SATISFACTORY. TH E AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001050300106 20010503 00106 NM 2001 5 3 AWXA0001627 1 20010423 A 5315 654681192 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 FLOORBEAM CORRODED AFT GALLEY AREA STA 986.5. BLENDED BEYOND LIMITS IAW SRM 53-60-51 FIG 101; PREVIOUS T-CAP REPAIR REP LACED AND SPLICED IAW SRM 51-70-12. 2 L 7 2 4F RT A16WE 2001050300108 20010503 00108 WP 2001 5 3 01FDEA00283 1 20010223 A 5510 ALC750212 ANGLE DOUG DC10 DC1030F 3023504 WP HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 NR 3 RT LEAD EDGE ASSY FOR HORIZONTAL HAS 7 INCH STRESS CRACK, RUNNING THRU HOLES ON UPPER FLANGE. *S/D* REMOVED AND RE PLACED T-ANGLE REF SRM 55-10-00. RE-INSTALLED NR 3 RT LEADING EDGE ASSY. 2 L 7 3 4F RT A22WE 2001050300110 20010503 00110 NM 2001 5 3 AWXA0001630 1 20010423 A 5315 6546568 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 23258 FS 1016 LBL 7 FLOORBEAM UPPER CAP CORRODED. REMOVED CORROSION; TREATED AND INSTALLED REPAIR IAW B737-300 SRM 53-00-51 F IG 203 PG 211-215 AND 53-60-51 FIG 101 PG 109. 2 L 7 2 4F RT A16WE 2001050300111 20010503 00111 CE 2001 5 3 20010501CW005 1 20010417 A 3246 11512 WHEEL CESSNA 210 2105 2073404 CE CONT O470 IO470* 17026 SO NLG CRACKED D K NONE O OTHER IN INSP/MAINT 1 EA 23 8279Z 5239 5239 2050279 MAGNESIUM 5.00-5 TYPE III WHEEL HALVES. FOUND CRACKS ADJAVENT TO THRU BOLT BOSSES AT PERIMETER ON BOTH WHEEL HALVES. PO SSIBLE CAUSES, HARD LANDINGS OR OVER TORQUING. 1 H 7 1 3O 3 O 3A21 E1CE 2001050300113 20010503 00113 EU 2001 5 3 C2XA01CL086 1 20010424 A 3260 D228830001 PROXIMITY SWITCH AEROSP ATR42 ATR42320 8680930 EU NLG FAULTY A C2XA O OTHER N FALSE WARNING AP APPROACH 1 SW 27 14833 188 DTW FLIGHT 3143 THE CREW REPORTED LANDING GEAR SYSTEM NR 2 INDICATES AURAL AND LOCAL ALERTS ACTIVATED, NOSE GEAR DID NO T INDICATE DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT FURTHER PROBLEMS. INDICATION PLACED ON MEL. CLE - MAINTENANCE REM OVED AND REPLACED SYSTEM PROXIMITY SWITCH ON NOSE LANDING GEAR. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001050300115 20010503 00115 WP 2001 5 3 MWEA010648 1 20010425 A 5311 5911448503 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 FRAME CORRODED, STATION 852, LONGERON 30, AFT SIDE OF FRAME. FABRICATED AND INSTALLED FRAME REPAIR PARTS. 2 L 7 2 4F A6WE 2001050300117 20010503 00117 CE 2001 5 3 20010501CW008 1 20010403 A 7603 5038901223 THROTTLE CABLE BEECH 58 58 1152740 CE CONT O520 IO520CB 17032 SO LT ENGINE BROKEN A BSYA K NONE O OTHER IN INSP/MAINT 1 GL 07 1653W TH252 LEFT ENGINE THROTTLE CABLE STUCK AT HALF THROTTLE, FOUND BROKEN THROTTLE CABLE, REMOVED AND REPLACED CABLE ASSEMBLY. OPS CHECK GOOD. 1 L 7 2 3O 3 O 3A16 E5CE 2001050300118 20010503 00118 NM 2001 5 3 ABXA010205 1 20010421 A 3330 60B4002613 TRANSFORMER BOEING 767 767281 1385109 NM CARGO BAY FAILED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 785AX 37955 23018 THE UPPER CARGO COMPARTMENT LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE UPPER CARGO LIGHTS TRANSFOR MER AND WIRING IAW B767 MM. 2 L 7 2 4F RT A1NM 2001050300119 20010503 00119 WP 2001 5 3 ABXA010206 1 20010424 A 3230 49516351 SPRING DOUG DOUG DC9 DC941 302207N WP NLG BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX N6356 47499 DURING THE PREFLIGHT INSPECTION MAINTENANCE FOUND THE NOSE LANDING GEAR OVER CENTER SPRING TO BE BROKEN. A MAINTENANCE FERRY WAS ISSUED AND COMPLETED FROM FSD TO ILN. ILN MAINTENANCE INSPECTED AND REPLACED THE NOSE LANDING GEAR OVER CENTE R BUNGEE SPRING IAW DC-9 MM 32-21-03. 2 L 7 2 4F A6WE 2001050300120 20010503 00120 CE 2001 5 3 20010426CW002 1 20010322 A 3010 9091010017 DUCT BEECH 90 C90A 1152911 CE PWA PT6 PT6* 52043 EA ANTI ICE SYSTEM BROKEN B VY2R K NONE O OTHER IN INSP/MAINT 1 SO 17 988P0 992 LJ1526 FOUND RIGHT HAND ENGINE INLET LIP HEAT FLEX DUCT, ON LEFT HAND EXHAUST STACK. FOUND BROKEN COMPLETELY OFF. BREAK IS AT LOWER END WHERE FLEX DUCTING ATTACHES TO FITTING. POSSIBLE FIRE HAZZARD. 1 L 7 2 3T 3 T RT 3A20 E2NE 2001050300122 20010503 00122 CE 2001 5 3 20010501CW010 1 20010403 A 3260 CTJ120E06E513 BLOCK LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP SELECTOR SWITCH INOPERATIVE D BSYA K NONE O OTHER IN INSP/MAINT 1 GL 07 31WR 313 LANDING GEAR WOULD NOT RETRACT. COULD NOT DUPLICATE ON GROUND. CHANGED GEAR SELECTOR SWITCH AND JUNCTION BLOCK FOR PRE CAUTIONARY MEASURES, OPS CHECKED GOOD. 2 L 7 2 4F 4 F A10CE E6WE 2001050300123 20010503 00123 CE 2001 5 3 20010501CW011 1 20010403 A 3260 8858K44 SELECTOR SWITCH LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP MLG INOPERATIVE D BSYA K NONE O OTHER IN INSP/MAINT 1 GL 07 31WR 313 LANDING GEAR WOULD NOT RETRACT. COULD NOT DUPLICATE ON GROUND. CHANGED GEAR SELECTOR SWITCH AND JUNCTION BLOCK FOR PRE CAUTIONARY MEASURES, OPS CHECKED GOOD. 2 L 7 2 4F 4 F A10CE E6WE 2001050300124 20010503 00124 WP 2001 5 3 20010501CW012 2 20010403 A 7200 ENGINE LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP LEFT MALFUNCTIONED D BSYA K NONE O OTHER IN INSP/MAINT 1 GL 07 56JA 342 LP74242 LEFT ENGINE CAUSING SMOKE IN CABIN. TROUBLE SHOT ENGINE TO NR 4 AND NR 5 CARBON SEALS. REMOVED AND REPLACED ENGINE. 2 L 7 2 4F 4 F A10CE E6WE 2001050300125 20010503 00125 NM 2001 5 3 CALA0100417 1 20010425 A 5320 WEB BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 CRACK AT LIGHTENING HOLE ON VERTICAL WEB AT LBL 23 APPROX 6 INCHES AFT OF 178 BULKHEAD AND 10 INCHES BELOW COCKPIT FLOOR . REPAIRED PER EC/RA 5320-01671. 2 L 7 2 4F RT A16WE 2001050300126 20010503 00126 SO 2001 5 3 20010501CW013 2 20010403 A 7414 103493505 MAGNETO BEECH 58 58 1152740 CE CONT O520 IO520C 17032 SO LEFT ENGINE INOPERATIVE D BSYA K NONE O OTHER IN INSP/MAINT 1 GL 07 36673 TH1143 L816914R LEFT ENGINE RUNNING ROUGH, FOUND LEFT MAGNETO DEAD. REMOVED AND REPLACED MAGNETO, CLEANED AND GAPPED PLUGS. GROUND RU N, OK. 1 L 7 2 3O 3 O 3A16 E5CE 2001050300127 20010503 00127 NM 2001 5 3 AWXA0001631 1 20010423 A 5320 6546812186 FLOOR SUPPORT BOEING 737 737301 1384611 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 23258 FS 993 RBL 17 FLOOR SUPPORT UPPER CAP CORRODED. REMOVED AND REPLACED FLOOR SUPPORT IAW B737-300 SRM 53-60-51 PG 108-114 AND 51-40-08 PG 1-6. 2 L 7 2 4F RT A16WE 2001050300128 20010503 00128 NM 2001 5 3 AWXA0001633 1 20010423 A 5310 65C2684321 PRESSURE PANEL BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 23258 LEFT WHEEL WELL PRESSURE WEB CRACKED AT FS 663 LBL 32. INSTALLED REPAIR CHANNEL IAW AWA ER 03-5716-0110-552. 2 L 7 2 4F RT A16WE 2001050300129 20010503 00129 NM 2001 5 3 AWXA0001634 1 20010423 A 5312 651630084 BULKHEAD BOEING 737 737301 1384611 NM FUSELAGE GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 23258 FS 178 BLKHD GOUGED AT WL 205 RBL 24. REPAIRED AREA IAW B737-300 SRM 51-40-02 PG 6-8, 10, 11 AND 51-20-01 PG 1-11 AND 5 3-40-08 FIG 209 PG 266-267 AND 53-10-08 FIG 101 PG 102-103. 2 L 7 2 4F RT A16WE 2001050300130 20010503 00130 WP 2001 5 3 IXXA0100015 1 20010126 A 5730 56123851 SKIN DOUG DC8 DC871F 302199D WP LT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 827BX 81468 2962 45971 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON LEFT WING OUTER WING SKIN PANEL AT STATION XRS 533.3, STRINGE R 62 END FITTING. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA. FABRICATION AND INSTALLATION AN REPAIR FILLER, DOUBLER AND TRIPLER IN ACCORDANCE WITH FAA DER APPROVED DRAWINGS 3759035-1, 5612385-507 AND DACO STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2001050300131 20010503 00131 WP 2001 5 3 IXXA0100016 1 20010418 A 2910 37193455001 SWIVEL DOUG DC8 DC871F 302199D WP HYD SYSTEM LEAKING A IXXA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 11 824BX 79644 1111 45946 AFTER TAKEOFF FROM TOL, THE FLIGHT CREW NOTICE A DECLINED IN THE MAIN HYDRAULIC QUANTITY SYSTEM. THE FLIGHT RETURNED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT LOCATING A RUPTURED LEFT AILERON SWIVEL GLAND. MAIN TENANCE REPACKED THE SWIVEL GLAND AND PERFORMED A SUCCESSFUL OPERATIONAL CHEKCK IN ACCORDANCE WITH THE MAINTENANCE MANUA L. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2001050300132 20010503 00132 WP 2001 5 3 IXXA0100017 1 20010424 A 3260 UPLOCK SENSOR DOUG DC8 DC871F 302199D WP MLG WW DIRTY A IXXA O OTHER N FALSE WARNING CL CLIMB 1 SW 11 826BX 83063 951 45998 EN ROUTE FROM SJC TO TOL, THE LANDING GEAR UNSAFE AND DOOR WARNING LIGHTS ILLUMINATED AFTER GEAR RETRACTION. THE FLIGHT CREW CYCLED THE LANDING GEAR AND THE WARNING INDICATING LIGHTS EXTINGUISHED. THE FLIGHT CONTINUED TO TOL FOR AN UNEVEN TFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT, CLEANED AND LUBRICATING THE GEAR UPLATCH MECHANISMS AND PERFORMED A S UCESSFUL OPERATIONAL CHECK IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2001050300133 20010503 00133 WP 2001 5 3 IXXA0100014 1 20010125 A 5713 5643545508 STRINGER DOUG DC8 DC871F 302199D WP RT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 827BX 81468 2962 45971 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED AT THE RIGHT WING STRINGER 54 AT WING STATION 510. REPAIR ACCOM PLISHED REMOVAL OF THE DAMAGED AREA. FABRICATION AND INSTALLATION OF A CHANNEL FILLER AND TWO REPAIR ANGLES IN ACCORDAN CE WITH FAA DER APPROVED DRAWING 5643545-508 AND DACO STRUCTURAL REPAIR MANUAL 57-2-2, 51-1-1, 51-1-5, 51-1-27. 2 L 7 4 4F RT 4A25 2001050300134 20010503 00134 SO 2001 5 3 C2XA01CL085 1 20010422 A 3350 20131A BATTERY EMB 145 EMB145LR SO CABIN DISCHARGED A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 13964 2534 19 145123 CLE FLIGHT 4058 THE CREW REPORTED EMERGENCY LIGHTS OUT ON AISLE PATH LIGHTING. MAINTENANCE REPLACED THE NR 3 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001050300136 20010503 00136 NM 2001 5 3 AWXA0001635 1 20010423 A 5312 651630084 BULKHEAD BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 23258 FS 178 BLKHD CRACKED AT WL 234 LBL 8 - 11.5. REPAIRED AREA IAW B737-300 SRM 53-10-08 PG 265-269 AND 51-40-02 PG 3-4 & 9 -11 AND 51-20-01 PG 1-10. 2 L 7 2 4F RT A16WE 2001050300137 20010503 00137 NM 2001 5 3 AWXA0001636 1 20010423 A 5312 651630084 BULKHEAD BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 23258 FS 178 BLKHD CRACKED AT WL 234 RBL 8 - 11.5. REPAIRED AREA IAW B737-300 SRM 53-10-08 PG 265-269 AND 51-40-02 PG 3-4 & 9 -11 AND 51-20-01 PG 1-10. 2 L 7 2 4F RT A16WE 2001050300138 20010503 00138 NM 2001 5 3 AWXA0001637 1 20010423 A 5312 651630084 BULKHEAD BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 23258 FS 178 BLKHD CRACKED AT WL 200 LBL 5. REPAIRED AREA IAW B737-300 SRM 53-10-08 FIG 211 PG 1-11 AND 51-21-41 PG 701-702 A ND 51-40-02 PG 2-4, 6-8, 10-11. 2 L 7 2 4F RT A16WE 2001050300139 20010503 00139 NM 2001 5 3 AWXA0001639 1 20010423 A 5312 651630084 BULKHEAD BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 23258 FS 178 BLKHD CRACKED AT WL 201.5 LBL 6.5. REPAIRED AREA IAW B737-300 SRM 53-10-08 FIG 211 PG 1-11 AND 51-21-41 PG 701-7 02 AND 51-40-02 PG 2-4, 6-8, 10-11. 2 L 7 2 4F RT A16WE 2001050300140 20010503 00140 NM 2001 5 3 AWXA0001640 1 20010423 A 5312 651630084 BULKHEAD BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 23258 FS 178 BLKHD CRACKED AT WL 200 RBL 5. REPAIRED AREA IAW B737-300 SRM 53-10-08 FIG 211 PG 1-11 AND 51-21-41 PG 701-702 A ND 51-40-02 PG 2-4, 6-8, 10-11. 2 L 7 2 4F RT A16WE 2001050300142 20010503 00142 NM 2001 5 3 AWXA0001641 1 20010423 A 5320 651630084 WEB BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 23258 COCKPIT FLOOR CRACKED AT FS 180 WL 207 RBL 23. REMOVED AND REPLACED WEB IAW B737-300 SRM 51-40-02 PG 2-4, 6-8, 10-11, 1 6-17. 2 L 7 2 4F RT A16WE 2001050300145 20010503 00145 NM 2001 5 3 QXEA0100626 1 20010421 A 2120 DUCT DHAV DHC8 DHC8202 2809007 NM CABIN OUT OF POSITION A QXEA B EMER. DESCENT O OTHER CR CRUISE 1 NM 09 375PH 529 PDX-EN-ROUTE TO LMT AT FLIGHT LEVEL 21,000 FEET, HEARD A LOUD POP AND THEN EXPERIENCED A RAPID DEPRESSURIZATION. DESCEN T TO FLIGHT LEVEL 10,000 FEET. UPON INSPECTION, FOUND RIGHT HAND DUCT BLOWN OFF OF RECIRCULATION FAN. REINSTALLED DUCT AND TIGHTENED ALL FOUR CLAMPS ON FAN INTAKE AND OUTLET. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001050300146 20010503 00146 EU 2001 5 3 QXEA0100627 1 20010423 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 11234 BOI-EMERGENCY EXIT SIGN ABOVE COCKPIT DOOR HAS BURNT OUT BULBS. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOO D. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001050300147 20010503 00147 EU 2001 5 3 QXEA0100628 1 20010423 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 11234 BOI-EMERGENCY EXIT SIGN AT CABIN ENTRYWAY HAS BURNT OUT BULBS. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001050300150 20010503 00150 EA 2001 5 3 SWIA972526 1 20010410 A 5610 WINDOW CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT CRACKED A SWIA K NONE O OTHER LD LANDING 1 NM 07 405SW 7029 ON LANDING THE RIGHT SIDE WINDOW CRACKED. REMOVED AND REPLACED RIGHT SIDE SIDE WINDOW IAW 56-12-01; RII 56-401. OPS CH ECK GOOD. P/N ON PPG-NP-139322-6, S/N ON 00320H3690, S/N OFF 92016H6381. 2 L 7 2 4F 4 F RT A21EA E15NE 2001050300151 20010503 00151 SO 2001 5 3 SWIA972528 1 20010423 A 2133 OUTFLOW VALVE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CABIN PRESSURE FAULTY A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 297SW 120327 WHEN AUTOMATIC PRESSURIZATION REACHES 4.0 PSI, CABIN RATE GOES UP AND DOWN 72000 FT/MIN. REPLACED PNEUMATIC OUTFLOW VAL VE IAW CARD RII 21-303. OPS CHECK GOOD. P/N: 2093K010800, S/N ON: 075, S/N OFF: 395. 2 L 7 2 4T 4 T RT A31SO E20NE 2001050300152 20010503 00152 SO 2001 5 3 SWIA972529 1 20010421 A 2710 BELLCRANK EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT AILERON OBSTRUCTED A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 288SW 120316 ON DOWNWIND THE AILERONS FROZE FOR 12 SECONDS, WE WERE UNABLE TO MOVE YOKE. ON BASE TURN THE AILERONS FROZE FOR 5 SECON DS AND ON FINAL THE AILERONS FROZE FROM APPROX 200 FT AGL UNTIL 20 SECONDS AFTER ROLLOUT. AUTOPILOT WAS CONFIRMED DISCO NNECTED BY BOTH PILOTS. WHEN AILERONS WERE FROZEN THE YOKE WAS NEUTRAL AND UNMOVEABLE BY BOTH PILOTS. REMOVED UPPER AND LOWER ACCESS PANELS TO LEFT AND RIGHT AILERONS. INSPECTED YOKE CHAIN DRIVE. NO DEFECTS NOTED. FOUND PANEL MISSING 2 SCREWS ON LT AILERON JUST FWD OF THE TRIM TAB. LEADING EDGE WAS BENT FORWARD AND IMPEDING TRAVEL ON LEFT AILERON BELLCR ANK. RE-SECURED PANEL. SCREW HOLES ARE NOT ELONGATED. CLOSED ALL PANELS. CONTROL DISCONNECT LIGHTS OUT ON MAP. 2 L 7 2 4T 4 T RT A31SO E20NE 2001050300153 20010503 00153 SO 2001 5 3 SWIA972530 1 20010419 A 7714 INDICATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT DEFECTIVE A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 294SW 120321 NL GAUGE RIGHT ENGINE APPROACHED RED ARC DURING CLIMBOUT. TORQUE WAS REDUCED. NH AND ALL OTHER INDICATIONS REMAINED NO RMAL (T6 APPROX 690-700, NH APPROX 95 PERCENT). AFTER ENGINE SHUTDOWN, GAUGE MOMENTARILY STUCK AT 10 PERCENT NL. DURIN G FLIGHT, NL RIGHT SIDE STAYED 10 PERCENT HIGHER THAN NL LEFT SIDE. REPLACED RIGHT NH/NL INDICATOR WITH SERVICEABLE UNI T. OPS CHECK GOOD AT THIS TIME. P/N ON AND OFF SEDL-OC29M, S/N ON 191, S/N OFF B232. 2 L 7 2 4T 4 T RT A31SO E20NE 2001050300162 20010503 00162 EU 2001 5 3 QXEA0100498 1 20010404 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- SHARP DENT IN FUSELAGE SKIN AT RIGHT HAND AIR CYCLE MACHINE INLET FORWARD END IN UNPRESSURIZED AREA. REPAIRED IAW FOKKER SRM 53-02-02 FIGURE 1 AND 51-31-01 PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001050300163 20010503 00163 EU 2001 5 3 QXEA0100499 1 20010324 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- SHARP DENT IN FUSELAGE SKIN 5 INCHES ABOVE ACCESS PANEL 24B AND 4 INCHES AFT OF STATION 2750 IS BEYOND LIMITS. REP AIRED IAW FOKKER SRM 53-02-01 PAGE 3 AND 51-31-01 PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001050300164 20010503 00164 EU 2001 5 3 QXEA0100500 1 20010402 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACK ON FRAME 2650 AT STRINGER 18. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2. 2 L 7 2 4F RT A20EU 2001050300165 20010503 00165 EU 2001 5 3 QXEA0100501 1 20010403 A 5310 WINDOW POST FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- REMOVED WINDOW POST NR 2 REPAIR FOR INSPECTION AND NDT. REPAIRED IAW HORIZON AIR EA 4-53-1474. 2 L 7 2 4F RT A20EU 2001050300166 20010503 00166 EU 2001 5 3 QXEA0100502 1 20010406 A 5310 STRUCTURE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACK AT STATION 1550 AND STRINGER 72. REPAIRED IAW HORIZON AIR EA 4-53-1466. 2 L 7 2 4F RT A20EU 2001050300167 20010503 00167 EU 2001 5 3 QXEA0100503 1 20010327 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- MINOR CORROSION UNDER MARKER BEACON ANTENNA ON FUSELAGE SKIN. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9. 2 L 7 2 4F RT A20EU 2001050300168 20010503 00168 EU 2001 5 3 QXEA0100504 1 20010329 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- MINOR CORROSION ON FUSELAGE SKIN UNDER FORWARD RADIO ALTIMETER ANTENNA. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9. 2 L 7 2 4F RT A20EU 2001050300169 20010503 00169 EU 2001 5 3 QXEA0100505 1 20010406 A 2150 DUCT FOKKER F28 F28MK4000 4990810 EU ACM ERODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- LEFT HAND AIR CYCLE MACHINE INLET ERRODED. REPAIRED IAW FOKKER SRM 51-10-05, 51-31-01 AND 51-31-05. 2 L 7 2 4F RT A20EU 2001050300170 20010503 00170 EU 2001 5 3 QXEA0100506 1 20010404 A 2150 DUCT FOKKER F28 F28MK4000 4990810 EU ACM ERODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- RIGHT HAND AIR CYCLE MACHINE INLET ERRODED. REPAIRED IAW FOKKER SRM 51-31-01 PAGES 13 AND 14 AND 51-31-04. 2 L 7 2 4F RT A20EU 2001050300171 20010503 00171 EU 2001 5 3 QXEA0100507 1 20010405 A 5310 BEAM FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- 18MM LONG CRACK LOWER RADIUS OF BEAM 3 AT BUTT LINE 55R FRONT SIDE OF REAR PRESSURE BULKHEAD. REPAIRED IAW HORIZON AIR EA 4-53-1227. 2 L 7 2 4F RT A20EU 2001050300172 20010503 00172 EU 2001 5 3 QXEA0100509 1 20010324 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- RIGHT HAND FUSELAGE SKIN DENTED AFT OF MID CARGO DOOR STATION 8805-9305 AND STRINGERS 64 AND 65. REPAIRED IAW FOKK ER SRM 53-02-02 PAGE 2 AND 51-31-01 PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001050300173 20010503 00173 EU 2001 5 3 QXEA0100510 1 20010326 A 5310 PRESSURE PANEL FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- NOSE LANDING GEAR BAY TOP COVER IS CRACKED ON LEFT HAND SIDE OF STATIONS 2996 - 3050L. REPAIRED IAW HORIZON AIR EA 4-53-1459. 2 L 7 2 4F RT A20EU 2001050300174 20010503 00174 EU 2001 5 3 QXEA0100511 1 20010324 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- SHARP DENT IN FUSELAGE SKIN AT STATION 5805, 3INCHES FORWARD OF FORWARD CARGO DOOR. REPAIRED IAW FOKKER SRM 53-02- 02 FIGURE 1 AND 51-31-01 PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001050300175 20010503 00175 EU 2001 5 3 QXEA0100512 1 20010330 A 5312 BULKHEAD FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- FRONT PRESSURE BULKHEAD REAR SIDE BELOW FLOOR, RIGHT OF CENTER AT BEAM 3 HAS MINOR SURFACE CORROSION. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9. 2 L 7 2 4F RT A20EU 2001050300176 20010503 00176 EU 2001 5 3 QXEA0100513 1 20010330 A 5312 BULKHEAD FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- FRONT PRESSURE BULKHEAD REAR SIDE BELOW FLOOR RIGHT OF CENTER AT BEAM 2 HAS MINOR SURFACE CORROSION. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9. 2 L 7 2 4F RT A20EU 2001050300177 20010503 00177 EU 2001 5 3 QXEA0100514 1 20010331 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- DAMAGE TO LEFT HAND FUSELAGE SKIN BETWEEN 5305 AND 7305 BETWEEN STRINGERS 14 AND 18. REPAIRED IAW HORIZON AIR EA 4 -53-1460. 2 L 7 2 4F RT A20EU 2001050300178 20010503 00178 EU 2001 5 3 QXEA0100516 1 20010324 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- MID CARGO DOOR COMING FORWARD IS GOUGED AND BLENDED BEYOND LIMITS. REPAIRED IAW FOKKER SRM 53-02-16. 2 L 7 2 4F RT A20EU 2001050300179 20010503 00179 EU 2001 5 3 QXEA0100517 1 20010405 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- AFT CARGO PIT CRACKED CASTELLATION AT FRAME 13815A AND STRINGER 1-2. REPAIRED IAW FOKKER SRM 53-02-13, 53-22-04 AN D 51-31-01. 2 L 7 2 4F RT A20EU 2001050300180 20010503 00180 EU 2001 5 3 QXEA0100518 1 20010406 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED CASTELLATION IN REAR CARGO PIT AT FRAME 13815A AND STRINGER 73 AND 72. REPAIRED IAW FOKKER SRM 53-02-13, 5 3-22-04 AND 51-31-01. 2 L 7 2 4F RT A20EU 2001050300181 20010503 00181 EU 2001 5 3 QXEA0100519 1 20010406 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED CASTELLATION IN REAR CARGO PIT AT FRAME 13815B AND STRINGER 2 AND 3. REPAIRED IAW FOKKER SRM 53-22-04 AND 51-31-01. 2 L 7 2 4F RT A20EU 2001050300182 20010503 00182 EU 2001 5 3 QXEA0100520 1 20010406 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED CASTELLATION IN REAR CARGO PIT AT FRAME 13815B AND STRINGER 72 AND 73. REPAIRED IAW FOKKER SRM 53-22-04 AN D 51-31-01. 2 L 7 2 4F RT A20EU 2001050300183 20010503 00183 EU 2001 5 3 QXEA0100521 1 20010404 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED CLIP AT FRAME 8305 AND STRINGER 70. REPAIRED IAW FOKKER SRM 53-02-01, 53-02-13, 54-31-01 AND 51-30-02. 2 L 7 2 4F RT A20EU 2001050300184 20010503 00184 EU 2001 5 3 QXEA0100522 1 20010331 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED CASTELLATION AT FRAME 5805 AND STRINGER 16 AND 17 (LEFT HAND FUSELAGE SKIN). REPAIRED IAW HORIZON AIR EA 4 -53-1461. 2 L 7 2 4F RT A20EU 2001050300185 20010503 00185 EU 2001 5 3 QXEA0100524 1 20010326 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- FUSELAGE SKIN TO FRAME IS CRACKED AT FORWARD CARGO PIT FRAME 7305 AND STRINGER 1. REPAIRED IAW FOKKER SRM 53-02-13 AND 51-31-01 PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001050300186 20010503 00186 EU 2001 5 3 QXEA0100525 1 20010327 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED CLIP IN FORWARD CARGO PIT FRAME 9305 AND STRINGER 66. REPAIRED IAW FOKKER SRM 51-31-01 PAGE 13 AND 14. 2 L 7 2 4F RT A20EU 2001050300187 20010503 00187 EU 2001 5 3 QXEA0100526 1 20010329 A 5310 DOOR FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- FORWARD CARGO PIT FORWARD DOOR AFT LOWER CORNER OF APERTURE HAS MINOR SURFACE AROUND SCREW HOLES. REPAIRED IAW FOK KER SRM 51-10-04 PAGE 9. 2 L 7 2 4F RT A20EU 2001050300188 20010503 00188 EU 2001 5 3 QXEA0100527 1 20010329 A 5310 DOOR FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- FORWARD CARGO PIT AFT DOOR AFT LOWER CORNER OF APERTURE HAS MINOR SURFACE CORROSION AROUND SCREW HOLES. REPAIRED I AW FOKKER SRM 51-10-04 PAGE 9. 2 L 7 2 4F RT A20EU 2001050300189 20010503 00189 SO 2001 5 3 20010427CW009 1 20010329 A 2913 1159SCH5057 PUMP GULSTM G1159 GIV 3980115 SO RROYCE BR700 BR700710A110 NE HYDRAULIC SYS UNSERVICEABLE D K NONE O OTHER IN INSP/MAINT 1 GL 15 23M 178 1022 L11261 HYDRAULIC PUMP CASE DRAIN FILTER SAMPLES FOR LEFT ENGINE DID NOT PASS THE PATCH TEST. REPLACED PUMP WITH SERVICEABLE UN IT, BLED AIRCRAFT SYSTEMS AND RETURNED AIRCRAFT TO SERVICE. WE WILL CONTINUE SAMPLE SYSTEM FLUID AS REQUIRED. 2 L 7 2 4F 4 F RT A12EA E00057EN 2001050300190 20010503 00190 EU 2001 5 3 QXEA0100528 1 20010329 A 5310 DOOR FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- FORWARD CARGO PIT FORWARD DOOR FORWARD LOWER CORNER OF APERTURE HAS MINOR SURFACE CORROSION AROUND SCREW HOLES. RE PAIRED IAW FOKKER SRM 51-10-04 PAGE 9. 2 L 7 2 4F RT A20EU 2001050300191 20010503 00191 EU 2001 5 3 QXEA0100529 1 20010330 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- FORWARD CARGO PIT FRAME 8305 AT STRINGER 3 TOP FLANGE OF FRAME IS DENTED. REPAIRED IAW HORIZON AIR EA 4-53-1462. 2 L 7 2 4F RT A20EU 2001050300192 20010503 00192 EU 2001 5 3 QXEA0100530 1 20010329 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- FORWARD CARGO PIT FORGED STRINGER 2 AT FRAME 9305C HAS SURFACE CORROSION. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9. 2 L 7 2 4F RT A20EU 2001050300193 20010503 00193 EU 2001 5 3 QXEA0100532 1 20010329 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- FORWARD CARGO PIT FRAME 8305 AT STRINGER 73 BOTTOM SIDE OF UPPER FLANGE HAS SURFACE CORROSION AROUND ANCHOR NUT. R EPAIRED IAW FOKKER SRM 51-10-04 PAGE 9. 2 L 7 2 4F RT A20EU 2001050300194 20010503 00194 EU 2001 5 3 QXEA0100533 1 20010329 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- FORWARD CARGO PIT FRAME 9305 AT STRINGER 3 HAS MINOR SURFACE CORROSION ON TOP SURFACE OF UPPER FLANGE. REPAIRED IA W FOKKER SRM 51-10-04 PAGE 9. 2 L 7 2 4F RT A20EU 2001050300195 20010503 00195 EU 2001 5 3 QXEA0100535 1 20010406 A 5260 ANGLE FOKKER F28 F28MK4000 4990810 EU ENTRY STAIRS CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- MAIN CABIN DOOR ENTRANCE WAY SECOND STEP BOTTOM INBOARD ANGLE CORRODED. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9. 2 L 7 2 4F RT A20EU 2001050300196 20010503 00196 EU 2001 5 3 QXEA0100536 1 20010406 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR TORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- REAR CARGO DOOR INSIDE SKIN TORN BY BOTTOM MID SECTION ALONG RIVET LINE. REPAIRED IAW FOKKER SRM 52-30-00, 52-02-0 5 PAGE 3 AND 51-31-05 PAGES 8 AND 10. 2 L 7 2 4F RT A20EU 2001050300197 20010503 00197 EU 2001 5 3 QXEA0100539 1 20010330 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- MINOR CORROSION FOUND UNDER LOWER COMM ANTENNA. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9. 2 L 7 2 4F RT A20EU 2001050300198 20010503 00198 EU 2001 5 3 QXEA0100540 1 20010405 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- MINOR CORROSION FOUND UNDER LOWER TRANSPONDER ANTENNA. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9. 2 L 7 2 4F RT A20EU 2001050300199 20010503 00199 EU 2001 5 3 QXEA0100542 1 20010404 A 5312 BULKHEAD FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACK ON REAR PRESSURE BULKHEAD AT BEAM 2 BL425R - BL1050R. REPAIRED IAW HORIZON AIR EA''S 4-92-21 A&B AND 4-53-14 73. 2 L 7 2 4F RT A20EU 2001050300208 20010503 00208 SO 2001 5 3 20010501CW021 1 20010202 A 2421 ACY6412R ALTERNATOR PIPER PA32 PA32301 7103207 SO LYC O540 IO540K1G5 41532 EA ENGINE MISALIGNED A PNSA K NONE O OTHER IN INSP/MAINT 1 AL 03 81052 148 328206023 L2394248A ALTERNATOR SLIP RING TO BRUSH ALIGNMENT OFF. BRUSHES STEPPED WITH NORMAL WEAR IN LENGTH. THE BRUDH TO SLIP RING STEP W EAR IS AT INSULATOR OF THE TWO SLIP RINGS. IN WHICH IT UNSEATED PRESSURE TO THE SLIP RING. STEP IS ABOUT .0156 WIDE. 1 L 7 1 3O 3 O A3SO 1E4 2001050300212 20010503 00212 NM 2001 5 3 2001UALA00561 1 20010418 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 1461 STRINGERS 39L TO 39R SHEAR TIE CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHEDFABRICATED AND INSTAL LED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T2102. 2 L 7 2 4F 4 F RT A1NM E3NE 2001052100026 20010521 00026 NM 2001 5 21 2001UALA00568 1 20010420 A 5540 66139641 BUSHING BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RUDDER WORN A UALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 29 7254U 21401 AIRCRAFT RETURNED TO GSO DUE TO AIRFRAME VIBRATION. SUPPLEMENTAL DATA UPDATE UPPER RUDDER TRAILING EDGE PLAY OUT OF LIMI T. REPLACED BOLTS, AND BUSHING. RUDDER TRAILING EDGE PLAY WITHIN LIMIT. 2 L 7 3 4F 4 F A3WE E2EA 2001050300215 20010503 00215 SO 2001 5 3 20010503CW007 1 20010228 A 2742 1159SCC20043 ACTUATOR MOOG GULSTM G1159 GIV 3980115 SO RROYCE TAY TAYMK6118 NE HORIZONTAL STAB INOPERATIVE D O OTHER O OTHER NR NOT REPORTED 1 EA 25 440CP 1644 87906 1118 PILOT SELECTED 10 DEGREES FLAPS, FLAPS MOVED TO THE SETTING BUT HORIZONTAL STABILIZER DID NOT AGREEE WITH FLAP SETTING. PILOT SELECTED FULL FLAPS DOWN SETTING BUT FLAPS WOULD NOT MOVE. MAINTENANCE CREW FOUND THAT A/C HORZ STAB ACTUATOR WA S INOPERATIVE. ON REMOVAL OF STABILIZER ACTUATOR, IT WAS FOUND THE UNIT HAD TO BE DISASSEMBLED WHILE IN A/C BECAUSE THE ACTUATOR FAILED THE FULL EXTENDED POSITION. ON DISASSEMBLY, ACTUATOR WAS FOUND CORRODED INTERNALLY TO THE POINT WHERE IT HAMPERED ITS REMOVAL FROM A/C. THE A/C HORZ STAB ACTUATOR IS AN ON CONDITION COMPONENT. NO ROUTINE MAINTENANCE OR I NTERNAL INSPECTION IS REQUIRED. IMPENDING FAILURE IS NOT EVIDENT IN THE EVENT OF SEAL FAILURE. 2 L 7 2 4F 4 F RT A12EA A25NE 2001050300217 20010503 00217 NM 2001 5 3 2001UALA00580 1 20010425 A 3211 BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT MLG GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 LEFT HAND AFT LANDING GEAR SUPPORT BEAM FORWARD SIDE IS GOUGED. REPAIRED GOUGED LANDING GEAR SUPPORT BEAM. MAJOR REPAI R ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001050300218 20010503 00218 NM 2001 5 3 2001UALA00585 1 20010425 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 AFT PIT FRAME STA 827 RBL 20 HAS A HOLE IN THE WEB. ACCOMPLISHED WEB CUTOUT AND INSTALLED A DOUBLER. MAJOR REPAIR ACCO MPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001050300219 20010503 00219 NM 2001 5 3 2001UALA00591 1 20010426 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 314UA 23675 AFT CABIN FLOORBEAM STA 986 TOP CAP RBL 49 HAS EXCESSIVE MATERIAL REMOVED. SPLICED IN A NEW UPPER CHORD. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001050300220 20010503 00220 NM 2001 5 3 01FDEA00297 1 20010406 A 5311 53FX13491 FRAME BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 LWR CARGO COMPT PERF HFEC INSP FOUND 1 CRACK APPROX 1.5 INCH AT BS 600 JUST ABOVE S-20L AT I/B RADIUS SUB FRAME UNDER CA RGO DOOR SPOOL FITTING. ** S/D ** R&R & FAB PER FDW DWG 53FX1349. PER SRM 51-10-01 & FDX DFWG 53FX1371. 2 L 7 3 4F RT A3WE 2001050300221 20010503 00221 CE 2001 5 3 20010502CW003 1 20010327 A 3411 S10711 PITOT LINE CESSNA 207 207A 2073604 CE CONT O520 IO520* 17032 SO RT WING CHAFED C YADA K NONE O OTHER IN INSP/MAINT 1 AL 03 9874M 20700745 FOLLOWING REPAIR FROM LANDING ACCIDENT, ON FIRST FLIGHT AFTER REPAIRS, PILOT REPORTED AIRSPEED APPEARED TO INDICATE 30 K NOTS LOW. POST FLIGHT MAINTENANCE REVELED A CHAFE HOLE IN PITOT LINE IN LEFT WING AT A NOSE RIB. 1 H 7 1 3O 3 O A16CE E5CE 2001050300222 20010503 00222 SW 2001 5 3 20010502CW007 1 20010403 A 3340 4609383 RELAY BELL 214 214ST 1182106 SW GE CT7TS CT71 30030 NE SEARCH LIGHT MALFUNCTIONED E ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 392AL 28114 DURING COOL DOWN AFTER LANDING, AN ELECTRICAL SMELL WAS NOTED. SEARCH LIGHT RELAY WAS FOUND TO BE THE CAUSE OF THE SMEL L. 2 G 7 2 4U 4 U H10SW E8NE 2001050300223 20010503 00223 WP 2001 5 3 AALA20010678 1 20010322 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 TUL - FOUND CLASS III TEMP REPAIR INSTALLED ON FUSELAGE FROM STATION 446-490 STRINGER 21R AND 22R. DENT IN SKIN STATION 503 STRINGER 21R HAS ADL STICKER. CUTOUT DAMAGED FROM STATION 447-490, 4 INCHES ABOVE STRINGER 21R TO STRINGER 22R AT STATION 503 3 INCH DIAMETER. INSTALLED PERM CLASS 1 DOUBLER INTERNAL AND EXT PER ESO 80559 DATED 3-19-01. (M) 2 L 7 2 4F RT A6WE 2001050300224 20010503 00224 WP 2001 5 3 AALA20010681 1 20010323 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 TUL - FOUND FUSELAGE SKIN CRACKED AT RIVET HOLE STATION 1380 LONGERON 14R. INSTALLED DOUBLER IAW SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2001050300226 20010503 00226 EU 2001 5 3 QXEA0100541 1 20010331 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC-MINOR CORROSION FOUND UNDER UPPER NAV/COM ANTENNA. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 AND 53-01-01. 2 L 7 2 4F RT A20EU 2001050300227 20010503 00227 NM 2001 5 3 CALA0100399 1 20010422 A 2540 FLOOR PANEL BOEING 737 737824 13844BZ NM AFT LAVATORY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 54241 28953 AFT LAV HAS CORROSION AT FLOOR UNDER THRESHOLD PLATE AT AFT END AT MOUNT LUG FOR LAV MODULE TO FLOOR. REMOVED THRESHOLD AND CORROSION BUILD-UP, REPAIRED HONEYCOMB AND INSTALLED ONE NEW INSERT. REINSTALLED THRESHOLD PER SRM 51-10-02 PARA 1 1. 2 L 7 2 4F RT A16WE 2001050300228 20010503 00228 NE 2001 5 3 20010426CW014 2 20010409 A 7260 37C301961P102 DRIVE SHAFT AMD FALCON FALCON20 2730103 EU GE CF700 CF7002D2 30010 NE ENGINE BROKEN E GXPA O OTHER R X J PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT WARNING INDICATION NR NOT REPORTED 1 GL 25 178GA 9072 6105 163 245411 AT FL310 A SUDDEN LOSS OF POWER, FLAME OUT AND OIL PRESSURE, FUEL PRESSURE, HYDRAULIC PRESSURE, WARNINGS. OPERATOR SUS PECTS FAILURE OF HORIZONTAL GEARBOX DRIVE SHAFT. EMERGENCY LANDING. 2 L 7 2 4F 4 F RT A7EU E7EA 2001050300231 20010503 00231 WP 2001 5 3 AALA20010679 1 20010322 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 TUL - FOUND NR 1 SEAT TRACK CORRODED AND PITTED STATION 1237. REMOVED CORROSION, OUT OF LIMITS. TRIMMED RETAINING IAW ESO 80569 DATED 3-21-2001 TREATED AND PRIMED AREA. (M) 2 L 7 2 4F RT A6WE 2001050300232 20010503 00232 WP 2001 5 3 AALA20010680 1 20010322 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 TUL - FOUND AREAS OF CORROSION LEFT CUSP STATION 641-655. CUTOUT DAMAGED AREAS AND INSTALLED DOUBLER PER SRM 53-01 FIG 4 SHEET 3. (M) 2 L 7 2 4F RT A6WE 2001050300233 20010503 00233 NM 2001 5 3 01FDEA00298 1 20010424 A 2613 WARNING LIGHT DOUG MD11 MD11F 3023600 NM COCKPIT ILLUMINATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 615FE 48767 NR 2 ENG COWL ANTI-ICE DUCT O/H IND CAME ON IN CLIMB. 2 L 7 3 4F RT A22WE 2001050300234 20010503 00234 WP 2001 5 3 01FDEA00299 1 20010424 A 5270 WARNING LIGHT DOUG DC10 DC1010F 3022111 WP COCKPIT ILLUMINATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 053FE 47807 AFT T/O MAIN CARGO -A- LIGHT BLINK INTERMITTENTLY. RELEASE FOR SERVICE PER MEL/CDL. 2 L 7 3 4F A22WE 2001050300235 20010503 00235 WP 2001 5 3 ARWA0010405 1 20010418 A 3260 H141003 DOWNLOCK SWITCH DOUG DC8 DC863F 302198F WP RT MLG FAULTY A ARWA K NONE N FALSE WARNING DE DESCENT 1 SO 19 441J 45988 BEFORE LANDING WHEN LANDING GEAR LEVER SELECTED TO GEAR DOWN THE RIGHT LANDING GEAR GREEN LIGHT DID NOT ILUMINATE. LIGH T TOOK APPROX 2 MINUTES TO ILLUMINATE. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR DOWN AND LOCK SWITCH AND CANNON PLUG. LANDING GEAR OPERATIONAL CHECK PERFORMED ALL CKD NORMAL IAW MM 32-30-0 & 32-60-0. 2 L 7 4 4F 4A25 2001050300238 20010503 00238 CE 2001 5 3 20010502CW002 1 20010411 A 7603 08502638 THROTTLE CONTROL CESSNA 310 310Q 2074242 CE CONT O470 IO470* 17026 SO RIGHT ENGINE BROKEN D O OTHER O OTHER AP APPROACH 1 EA 07 121LA 5276 310Q0973 DURING APPROACH FOR LANDING, RIGHT ENGINE THROTTLE CONTROL MOVEMENT HAD NO RESPONSE IN ENGINE POWER. CONTROL FELT NORMA L. ENGINE FEATHERED AND AIRCRAFT MADE A NORMAL LANDING. INSPECTION REVEALED THROTTLE CABLE BROKE ABOUT 12 INCHES AFT O F THROTTLE ASSEMBLY. BREAK OCCURED INSIDE CONTROL HOUSING. 1 L 7 2 3O 3 O 3A10 E1CE 2001050300239 20010503 00239 SO 2001 5 3 WVBA2001023 1 20010419 A 3260 487862 DOWNLOCK SWITCH PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA LT MLG FAILED E WVBA O OTHER J WARNING INDICATION AP APPROACH 1 AL 01 27755 317852148 PILOT REPORTED LEFT MAIN GEAR INDICATED NOT LOCKED ON APPROACH. AIRCRAFT DID A FLYBY AND GEAR WAS OBSERVED DOWN AND LOC KED. AIRCRAFT MADE A NORMAL LANDING. UPON INSPECTING THE DOWN LOCK SWITCH, A WORE WAS FOUND TO HAVE A BREAK IN IT. A REPAIR WAS ACCOMPLISHED WITH A IN LINE CONNECTOR (BUTT SPLICE). A GEAR RETRACTION TEST WAS PERFORMED AND THE AIRCRAFT R ETURNED TO SERVICE. 1 L 7 2 3O 3 O A20SO E14EA 2001050300240 20010503 00240 NM 2001 5 3 F3LA200100054 1 20010423 A 3350 110049 POWER SUPPLY BOEING 737 7372P6 NM CABIN DISCHARGED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 272 22 21613 PRIOR TO DEPARTURE, FLIGHT CREW REPORTED EMERGENCY AISLE PATH LIGHTING IN FWD CABIN INOPERATIVE. REPLACED FWD EMERGENCY AISLE PATH LIGHTING POWER SUPPLY. 2 L 7 2 4F RT A16WE 2001050300241 20010503 00241 NM 2001 5 3 F3LA200100055 1 20010424 A 5313 STRINGER BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3498 23177 DURING C-6 CHECK, INSPECTION REPORTED STRINGER 21-L AT STA 727D IN AFT CARGO COMPARTMENT CORRODED. REPLACED DAMAGED STR INGER PER SRM 53-00-03. 2 L 7 2 4F RT A16WE 2001050300243 20010503 00243 EU 2001 5 3 RAIA00104017 1 20010424 A 2613 57228532 FIRE LOOP JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILED A RAIA O OTHER N FALSE WARNING CL CLIMB 1 CE 03 563HK 41079 RIC-DURING CLIMB RIGHT HAND ENGINE FIRE LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED RIGHT HAND ENGINE FIRE LOOP IAW J41 MAINTENANCE MANUAL. 2 L 7 2 4T RT A41NM 2001050300244 20010503 00244 2001 5 3 RAIA00104018 4 20010424 A 3418 C850176 SENSOR JETAIR JETSTM JETSTM4101 1500501 EU STALL WARNING FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 564HK 76140 130 41081 EWR-DURING TAXI RIGHT HAND STALL CAPTION ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE ANGLE OF ATTACK SENSOR IAW J 41 MAINTENANCE MANUAL. 2 L 7 2 4T RT A41NM 2001050300245 20010503 00245 EU 2001 5 3 RAIA00104019 1 20010424 A 3241 140149 TRANSDUCER JETAIR JETSTM JETSTM4101 1500501 EU NR 4 WHEEL FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 565HK 41082 STL-DURING TAXI ANTI-SKID CAPTION LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED NR 4 ANTI-SKID WHEEL SPEED TRANSD UCER IAW J41 MAINTENANCE MANUAL. 2 L 7 2 4T RT A41NM 2001050300246 20010503 00246 WP 2001 5 3 IXXA0100018 1 20010424 A 2121 FAN DOUG DC8 DC862 3021970 WP A/C BAY DEFECTIVE A IXXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 11 31CX 45911 EN ROUTE FROM HIK TO JON, THE FLIGHT CREW EXPERIENCED SMOKE IN THE AIRCRAFT. THE FLIGHT CREW SECURED THE RIGHT RECIRULA TION FAN, THE SMOKE SUBSIDED. THE FLIGHT CONTINUED TO JON FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAF T WHICH REVEALED THE RIGHT RECIRULATION FAN DEFECTIVE. MAINTENANCE PLACED THE FAN ON DEFERRAL AND THE AIRCRAFT WAS RETU RNED TO SERVICE. 2 L 7 4 4F 4A25 2001050300250 20010503 00250 WP 2001 5 3 AALA016040 1 20010401 A 3350 BR9194501 LIGHT DOUG DC9 DC983 3022083 WP TAILCONE INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 833RA 53045 CCI-LAX - TAILCONE MID EMERGENCY LIGHTS INOPERATIVE, 3 ASSY''S. REPLACED 2 EMERGENCY LIGHT ASSEMBLIES AND RELAMPED 1 AS SEMBLY. OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 2001050300254 20010503 00254 NM 2001 5 3 2001UALA00389 1 20010325 A 2841 VALVE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE RT FUEL TANK MISWIRED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 611UA 21872 RIGHT TANK INDICATE LESS FUEL THAN LEFT TANK - WITH FUEL FLOW INDICATED AND FUEL USED EACH ENGINE THE SAME. SUSPECT TH AT THE RIGHT TANK IS FEEDING LEFT ENGINE EVEN THOUGH X-FEED CLOSE. CHRONIC PROBLEM . SUPPLEMENTAL DATA UPDATE CROSSFEED VALVE WIRES WERE FOUND TO BE SWAPPED AT D4942J. WIRES CORRECTED AND CHECKS OF SYSTEMS ASSOCIATED WITH D4942 PERFORMED. S YSTEM OPERATION NORMAL TO DATE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001050300256 20010503 00256 EU 2001 5 3 QXEA0100508 1 20010403 A 5310 STRUCTURE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- 10 MM LONG CRACK IN RADIUS OF UPPER CONSOLE AT BEAM 2 BUTT LINE 425R, FRONT SIDE OF REAR PRESSURE BULKHEAD. REPAIR ED IAW FOKKER SRM 51-31-02 PAGE 9 AND 10 AND 51-31-01 PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001050300257 20010503 00257 EU 2001 5 3 QXEA0100515 1 20010408 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- SUPPORT STRUCTURE AND FRAME 14755 CORRODED AND HAS BROKEN ANCHOR NUTS. REPAIRED IAW HORIZON AIR EA 4-53-1469. 2 L 7 2 4F RT A20EU 2001050300258 20010503 00258 EU 2001 5 3 QXEA0100523 1 20010329 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- MINOR CORROSION ON FUSELAGE SKIN UNDER LOWER VHF COMM ANTENNA. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9. 2 L 7 2 4F RT A20EU 2001050300259 20010503 00259 NM 2001 5 3 2001UALA00551 1 20010421 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 CABIN FLOORBEAM UPPER CHORD CORRODED STATION 365.25 BETWEEN BL 0 TO RBL 62. MAJOR REPAIR ACCOMPLISHED.INSTALLED T-CAP R EPAIR PER SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001050300260 20010503 00260 NM 2001 5 3 2001UALA00552 1 20010421 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 CABIN FLOORBEAM CORRODED STA 345 RBL 45 AROUND FASTENER HOLES. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR STRAP PER SR M. 2 L 7 2 4F 4 F RT A2NM E17NE 2001050300261 20010503 00261 NM 2001 5 3 2001UALA00553 1 20010421 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 CABIN FLOORBEAM CORRODED STA 1640 RBL 10 TO CREASE BEAM. MAJOR REPAIR ACCOMPLISHED. INSTALLED T-CAP REPAIR PER SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001050300262 20010503 00262 NM 2001 5 3 2001UALA00555 1 20010423 A 5310 DOOR FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 AFT CARGO DOOR INTERNAL FRAME CRACKED. STA 1410 AT HOLE FOR SWITCH. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER PER SRM . 2 L 7 2 4F 4 F RT A2NM E17NE 2001050300263 20010503 00263 NM 2001 5 3 2001UALA00556 1 20010420 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE MISREPAIRED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 STA 727E BETWEEN STRINGER 14L AND 13L HAS BEEN INCORRECTLY REPAIRED. REMOVED THE EXISTING INCORRECT REPAIR AND MANUFACT URED AND INSTALLED THE CORRECT PARTS. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001050300264 20010503 00264 EU 2001 5 3 QXEA0100531 1 20010329 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- FORWARD CARGO PIT FORGED STRINGER 73 AT FRAME 9305C HAS SURFACE CORROSION. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 . 2 L 7 2 4F RT A20EU 2001050300266 20010503 00266 WP 2001 5 3 AALA20010682 1 20010326 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 TUL - FOUND LONGERON 22L CORRODED (BLOW OUT). REPAIRED AREA WITH LONGERON SPLICE PER SRM 53-02 PAGE 50. (M) 2 L 7 2 4F RT A6WE 2001050300267 20010503 00267 WP 2001 5 3 AALA20010683 1 20010324 A 5330 ACCESS PANEL DOUG DC9 DC983 3022083 WP CENTER TANK DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 TUL - FOUND 16 HOLES ON CENTER TANK LEFT, RIGHT ACCESS PLATE LANDINGS ELONGATED. REPAIRED 16 HOLES IN LEFT RIGHT ACCESS PANEL LANDINGS PER ESO 80559 DATED 3-23-01. (M) 2 L 7 2 4F RT A6WE 2001050300268 20010503 00268 WP 2001 5 3 AALA20010684 1 20010323 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 TUL - FOUND SKIN DENTED AT STATION 237 LEFT LONGERON 18. REPAIRED PER SRM 53-04 AND AARD 320. (M) 2 L 7 2 4F RT A6WE 2001050300269 20010503 00269 WP 2001 5 3 AALA20010685 1 20010316 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 TUL - FOUND CORROSION ON SEAT TRACK NR 1. PERFORMED SEAT TRACK REPAIR PLUG PER 53-05 FIG 4A. (M) 2 L 7 2 4F RT A6WE 2001050300270 20010503 00270 WP 2001 5 3 USAAD01076 1 20010405 A 3350 9721055 BATTERY DOUG DC9 DC982 3022082 WP PAX CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 816US 48096 BOS - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001050300271 20010503 00271 WP 2001 5 3 USAAD01078 1 20010405 A 3260 7951248502 SENSOR DOUG DC9 DC981 3022081 WP NLG FAILED A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 19 814US 48094 CLT-PIT - FLT 374 - AFTER LANDING GEAR RETRACTION TO THE NOSE GEAR RED LIGHT REMAINED ILLUMINATED. THE LANDING GEAR WAS CYCLED AND THE LIGHT WENT OUT. THE AIRCRAFT CONTINUED TO ITS DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REP LACED THE NOSE LANDING GEAR DOWN LOCK PROXIMITY SENSOR AND PERFORMED SUCCESSFUL NOSE LANDING GEAR RETRACTION AND EXTENSI ON CHECK. (M) 2 L 7 2 4F A6WE 2001050300272 20010503 00272 NM 2001 5 3 USAASB01096 1 20010329 A 2913 6507506 PUMP BOEING 737 7374B7 1384702 NM NR 1 ENGINE LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 775AU 32662 24933 MIA - FLT 1975 - EN ROUTE FROM CLT TO MBJ, FLYING OVER CUBA, CAPTAIN REPORTED THAT THE NR 1 ENGINE HYDRAULIC PRESSURE LI GHT FLICKERED AND THAT HE WAS LOSING A-SYSTEM HYDRAULIC FLUID. THE FLIGHT WAS 45 MINUTES FROM MBJ OR MIA, AND AFTER DIS CUSSION, CAPTAIN AGREED TO DIVERT TO MIA. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND LANDED WITHOUT FURTHER INCIDENT AT MIA. AFTER LANDING, THE AIRCRAFT WAS TOWED TO GATE. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. REMOVED AND REPLACED HYDRAULIC PUMP PER MM 29-15-12. SERVICED A-SYSTEM HYDRAULI C RESERVOIR TO FULL. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001050300273 20010503 00273 2001 5 3 S2YA01001 4 20010116 A 3416 06603062000 ALTIMETER BEECH 1900 1900D 1154162 CE NR 1 INOPERATIVE A S2YA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 13 901SK UE90 FLT 2044 - MKE-CWA - DURING FLIGHT, THE CAPTAINS ALTIMETER FLAG APPEARED IN FLIGHT. THE CREW MADE AN AIR-TURN-BACK AND AN UNEVENTFUL LANDING IN MKE. MAINTENANCE REPLACED THE CAPTAINS ALTIMETER, OPS CHECKED IT AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A24CE 2001050300274 20010503 00274 CE 2001 5 3 S2YA01002 1 20010119 A 3230 571302 MOTOR BEECH 1900 1900D 1154162 CE MLG INOPERATIVE A S2YA O OTHER J WARNING INDICATION AP APPROACH 1 GL 13 85SK 16605 UE85 FLT 1900 - MKG-MKE - DURING APPROACH, THE CRWE SELECTED GEAR DOWN BUT DID ACHEIVE DOWN AND LOCKED. THE CREW EMERGENCY H AND PUMPED THE GEAR DOWN AND GOT THREE GREEN. JUST TO BE SURE THE CREW MADE A FLY-BY TO CONFIRM THE GEAR DOWN AND AN UN EVENTFUL LANDING IN MKE. MAINTENANCE PINNED THE GEAR TO TAXI THE A/C. MAINTENANCE INSPECTED THE SYSTEM AND REPLACED TH E LANDING GEAR MOTOR. MAINTENANCE CHECKED THE OPERATION AND THE RIGGING OF THE LANDING GEAR AND RETURNED THE AIRCRAFT T O SERVICE. (M) 2 L 7 2 4T RT A24CE 2001050300275 20010503 00275 CE 2001 5 3 S2YA01003 1 20010206 A 3230 1013880175 LINE BEECH 1900 1900D 1154162 CE MLG BROKEN A S2YA L ABORTED APPROACH K FLUID LOSS AP APPROACH 1 GL 13 841SK UE84 FLT 1350 - TVC-MKE - DURING APPROACH, THE CREW SELECTED GEAR DOWN BUT DID ACHIEVE DOWN AND LOCKED. THE HYDRAULICS LOW A NNUNCIATOR ILLUMINATED AND THE CIRCUIT BREAKER FOR THE LANDING GEAR MOTOR TRIPPED. THE CREW DID A MISSED APPROACH AND E MERGENCY HAND PUMPED THE GEAR DOWN. THE CREW ACHIEVED THREE GREEN AND MADE AN UNEVENTFUL LANDING IN MKE. MAINTENANCE P INNED THE GEAR TO TAXI THE A/C. MAINTENANCE INSPECTED THE SYSTEM AND REPLACED THE LEFT LANDING GEAR DOWN ACTUATOR LINER . MAINTENANCE CHECKED THE OPERATION AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A24CE 2001050300276 20010503 00276 CE 2001 5 3 S2YA01004 1 20010208 A 2130 1143800595 SHUTOFF VALVE BEECH 1900 1900D 1154162 CE CABIN PRESSURE FAILED A S2YA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 13 79SK UE79 FLT 1001 - MKE-STL - SHORTLY AFTER TAKEOFF, THE CREW COULD NOT PRESSURIZE THE CABIN AND MADE AN AIR-TURN-BACK. THE CREW TOLD MAINTENANCE THEY COULD NOT LATCH THE FO DOCUMENT WINDOW. MAINTENANCE FIXED THE WINDOW AND RETURNED THE A/C TO SER VICE. SHORTLY AFTER THE SECOND TAKEOFF, THE CREW COULD NOT PRESSURIZE THE CABIN AND MADE AN AIR-TURN-BACK. MAINTENANCE INSPECTED THE SYSTEM AND FOUND A BAD CHECK VALVE AT THE ACM. MAINTENANCE REPLACED THE CHECK VALVE AND CHANGED THE RT P RSOV. MAINTENANCE OPS CHECKED THE SYSTEM AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A24CE 2001050300277 20010503 00277 CE 2001 5 3 S2YA01005 1 20010311 A 3260 SWITCH BEECH 1900 1900D 1154162 CE MLG OUT OF ADJ A S2YA O OTHER J WARNING INDICATION AP APPROACH 1 GL 13 91SK UE91 FLT 1111 - MKE-CHM - DURING APPROACH, THE CREW SELECTED GEAR DOWN BUT DID ACHIEVE DOWN AND LOCKED ON THE NOSE GEAR. THE CREW FLEW BY THE TOWER TO VERIFY THE NOSE GEAR WAS DOWN. THE CREW THEN EMERGENCY HAND PUMPED THE GEAR DOWN BUT DID NOT ACHIEVE THREE GREEN. THE CREW MADE AN UNEVENTFUL LANDING AND THE NOSE GEAR DOWN AND LOCK ILLUMINATED AFTER LANDING IN CMH. THE AIRCRAFT WAS FERRIED BACK TO MKE. MAINTENANCE INSPECTED THE SYSTEM AND ADJUSTED THE NOSE GEAR DRAG BRACE DOWN LOCK SWITCHES. MAINTENANCE CHECKED THE OPERATION OF THE LANDING GEAR AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A24CE 2001050300278 20010503 00278 CE 2001 5 3 S2YA01006 1 20010323 A 5610 10138402518 WINDSHIELD BEECH 1900 1900D 1154162 CE COCKPIT ODOR A S2YA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 13 91SK 4477 UE91 FLT 1426 - MKE-CMH - DURING CRUISE, THE FLIGHT CREW NOTICED A STRANGE ODOR IN THE COCKPIT. THE CREW MADE AN AIRTURN BAC K AND LANDING AT MKE WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE GROUND TERMINAL ON THE RIGHT WI NDSHIELD BURNED. MAINTENANCE REPLACED THE RIGHT WINDSHIELD AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A24CE 2001050300279 20010503 00279 WP 2001 5 3 AALA016041 1 20010402 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 832RA 53044 CCI-LAX - EMERGENCY LIGHTS DOOR L1 INOPERATIVE. REPLACED FUSE, OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 2001050300280 20010503 00280 WP 2001 5 3 AALA016042 1 20010408 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 822RA 49932 EMERGENCY FLOOR LIGHTING SYSTEM BETWEEN ROWS 25-28 CAME ON UNCOMMANDED. BOTH PILOTS AND FA SWITCHES RECYCLED WITH NO AF FECT. FOUND LOOSE GROUND WIRE OF PLUG AT SEAT 26F, SECURED. OPS CHECKED LIGHTS, WORKING NORMAL. (M) 2 L 7 2 4F A6WE 2001050300281 20010503 00281 WP 2001 5 3 AALA016036 1 20010325 A 3241 26088921 BRAKE ASSY DOUG DC9 DC983 3022083 WP NR 1 ASSY FAILED A AALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 871RA 49788 SNA - AFTER LANDING, NOISE REPORTED BY ANOTHER AIRCRAFT L OUTBOARD ANTI-SKID LIGHT ILLUMINATED DURING TAXI AIRCRAFT WAS STOPPED AND TOWED TO GATE. NR 1 MAIN TIRE WAS FLAT. REMOVED AND REPLACED NR 1 BRAKE ASSEMBLY AND BOTH NR 1 AND NR 2 WH EEL ASSEMBLY. PERFORMED ANIT-SKID WHEEL SPIN-UP AND OPS CHECK GOOD. INSPECTED ENGINE INLET NO DAMAGE NOTED. (M) 2 L 7 2 4F RT A6WE 2001050300282 20010503 00282 WP 2001 5 3 20010503AP001 1 20010325 A 3246 ETY2132545 WHEEL DOUG DC9 DC983 3022083 WP MLG DAMAGED A AALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 871RA 49788 SNA - AFTER LANDING, NOISE REPORTED BY ANOTHER AIRCRAFT L OUTBOARD ANTI-SKID LIGHT ILLUMINATED DURING TAXI AIRCRAFT WAS STOPPED AND TOWED TO GATE. NR 1 MAIN TIRE WAS FLAT. REMOVED AND REPLACED NR 1 BRAKE ASSEMBLY AND BOTH NR 1 AND NR 2 WH EEL ASSEMBLY. PERFORMED ANIT-SKID WHEEL SPIN-UP AND OPS CHECK GOOD. INSPECTED ENGINE INLET NO DAMAGE NOTED. REF AALA0 16036. (M) 2 L 7 2 4F RT A6WE 2001050300283 20010503 00283 2001 5 3 AALA016037 4 20010328 A 2565 D29985103 SLIDE DOUG DC9 DC983 3022083 WP GALLEY DOOR DISLODGED A AALA O OTHER O OTHER NR NOT REPORTED 1 SW 21 834RA 53124 SJS - FLIGHT ATTENDANT ADVISES METAL PIECE OF SLIDE MECHANISM FELL OFF OF AFT GALLEY DOOR DURING ARMING PROCEDURE. SECU RED LOOSE PIECE AND REINSTALLED SLIDE LOCK MECHANISM, OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 2001050300284 20010503 00284 2001 5 3 AALA016038 4 20010329 A 2565 D29983113 SLIDE DOUG DC9 DC983 3022083 WP GALLEY DOOR DISLODGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 836RA 53046 LAX - EMERGENCY SLIDE AT FORWARD GALLEY IS FALLING OUT OF ITS CONTAINER. REINSTALLED SLIDE OK FOR SERVICE. (M) 2 L 7 2 4F RT A6WE 2001050300285 20010503 00285 WP 2001 5 3 AALA016039 1 20010404 A 2120 20495055 DUCT DOUG DC9 DC983 3022083 WP A/C PACK LOOSE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 832RA 53044 CLIMBING OUT OF FLT LVL 290, FLIGHT ATTENDANTS REPORTED SMOKE IN THE CABIN ALONG WITH AN UNUSUAL SMELL. COCKPIT CREW CO NFIRMED VERY HAZY CABIN AIR WITH AN OILY SMELL. CONDITIONS WERE GETTING WORSE SO DIVERTED TO FRESNO (FAT). SMELL AND S MOKE BEGAN TO CLEAR DURING DESCENT AND CABIN WAS CLEAR OF BOTH BY LANDING. ACCOMPLISHED CABIN SMOKE EMERGENCY PROCEDURE DURING DESCENT. FOUND ODOR EMINATING FROM LEFT FLOW PACK. PLACARDED INOPERATIVE PER MEL 21-1A. VERIFIED PROPER OPERA TION. FOUND BLOWN DUCT AT OUTLET OF LEFT FLOW PACK. (M) 2 L 7 2 4F RT A6WE 2001050300286 20010503 00286 NM 2001 5 3 P2EA01028 1 20010408 A 5330 SKIN BOEING 737 737297 1384480 NM FUSELAGE PUNCTURED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 5WM 22629 MDW - FLT 350 - PUNCTURE THROUGH SKIN AT BS 933, WL 203 BETWEEN STRINGER 20L AND 21L. REPAIRED IAW SRM 53-30-3. (M) 2 L 7 2 4F A16WE 2001050300287 20010503 00287 EU 2001 5 3 SIMA0875 1 20010328 A 3350 GE3071 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 905AE 340B319 DFW - FLT 3524 - EMERGENCY FLOOR LIGHT AT 5BC OUT. REMOVED AND REPLACED BULB IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001050300288 20010503 00288 2001 5 3 SIMA0895 4 20010330 A 3425 6226190113 COMPUTER SAAB SF340 340B 7860101 EU COCKPIT FAILED A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 323AE 340B323 DFW - FLT 3285 - NR 2 AHRS FAILED IN FLIGHT FOR 5 MINUTES. THEN APPEARED TO WORK NORMAL. REMOVED AND REPLACED NR 2 AHR S COMPUTER AND OPS CHECK GOOD AIW 34-21-05. (M) 2 L 7 2 4T RT A52EU 2001050300289 20010503 00289 EU 2001 5 3 SIMA0932 1 20010403 A 3350 6837BPF BULB SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 286AE 340B286 BOS - FLT 5122 - CREW REPORTED AN EMERGENCY FLOOR LIGHT AT ROW 7BC TO BE INOPERATIVE. MAINTENANCE REPLACED BULB AT ROW 7BC IAW SAAB AMM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050300290 20010503 00290 EU 2001 5 3 SIMA0735 1 20010314 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY FAILED A SIMA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 250AE 340B250 BFL - FLT 3000 - AFTER TAKEOFF, CARGO SMOKE LIGHT ILLUMINATED AT 8,000 FEET. CREW DISCHARGED CARGO FIRE BOTTLE, THE LIG HT WENT OUT AFTER 2 MINUTES AND CREW RETURNED TO BFL. NO EVIDENCE FOUND OF FIRE OR SMOKE AFTER RETURN TO GATE. REMOVED AND REPLACED FORWARD AND AFT SMOKE DETECTORS (S/N A4289 AND A4237) IAW AMM 26-23-00. OPS CHECK GOOD. NR 2 FIRE BOTTLE WAS REMOVED AND REPLACED. (M) 2 L 7 2 4T RT A52EU 2001050300291 20010503 00291 EU 2001 5 3 SIMA0734 1 20010314 A 3350 3071BPE LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 326AE 340B326 PWM - FLT 4482 - FOUND SEAT 4A FLOOR PROXIMITY EMERGENCY LIGHT PATH MARKING LIGHT IS INOPERATIVE. PUT ON MEL AT THIS TI ME. MAINTENANCE REPLACED BULB AT SET 4A. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050300292 20010503 00292 EU 2001 5 3 SIMA0751 1 20010316 A 3350 3071BPEGPL BULB SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 283AE 340B283 JFK - FLT 5045 - CREW REPORTED INTERIOR EMERGENCY LIGHTS WORKING INTERMITTENTLY. MAINTENANCE PERFORMED OPERATIONAL CHEC K OF EMERGENCY LIGHT AND FOUND EMERGENCY LIGHT AT SEAT 8BC FLICKERING. BULB WAS REPLACED AND AIRCRAFT WAS RETURNED TO S ERVICE. (M) 2 L 7 2 4T RT A52EU 2001050300293 20010503 00293 EU 2001 5 3 SIMA0752 1 20010316 A 3350 GE1317 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 272AE 340B272 DFW - FLT 3811 - CREW REPORTED EMERGENCY FLOOR LIGHT AT SEAT 9BC TO BE INOPERATIVE. MAINTENANCE REPLACED BULB AT ROW 9B C. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050300294 20010503 00294 EU 2001 5 3 SIMA0934 1 20010403 A 3350 74331 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA O OTHER L NO TEST NR NOT REPORTED 1 SW 21 376AE 340B376 DFW - FLT 3818 - FLOOR PROXIMITY LIGHT STRIP AT ROW 3 IS BROKEN. MAINTENANCE REPLACED FLOOR PROXIMITY LIGHT STRIP AT RO W 3A. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050300295 20010503 00295 WP 2001 5 3 MWEA010639 1 20010424 A 5310 J0601199 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 RIGHT SIDE SHEAR TIE IS CRACKED AT STATION 945 BETWEEN LONGERON 15 - 16. REMOVED AND REPLACED SHEAR TIE. 2 L 7 2 4F A6WE 2001050300296 20010503 00296 SO 2001 5 3 AL03200101158 1 20010115 A 2421 ALU8521R ALTERNATOR PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA ENGINE DEFECTIVE A PNSA K NONE O OTHER IN INSP/MAINT 1 AL 03 28KE 85 318152049 LEFT VOLTAGE REGULATOR CIRCUIT BREAKER WAS POPPING AS SOON AS AIRCRAFT POWER WAS APPLIED. TROUBLESHOT SYSTEM, FOUND ALT ERNATOR TO BE INTERNALLY GROUNDING. ALTERNATOR ALSO HAD BURNED ELECTRICAL SMELL COMING FROM INSIDE. 1 L 7 2 3O 3 O A20SO E14EA 2001050300297 20010503 00297 SO 2001 5 3 AL032001B6473 1 20010201 A 8011 MZ4222 STARTER PIPER PA32 PA32301 7103207 SO LYC O540 IO540K1C5 41532 EA ENGINE MALFUNCTIONED A PNSA K NONE O OTHER IN INSP/MAINT 1 AL 03 8429N 33 33 328106089 L2216448A STARTER MALFUNCTIONED, WOULD NOT ENGAGE. 1 L 7 1 3O 3 O A3SO 1E4 2001050300298 20010503 00298 SO 2001 5 3 AL03200101165 1 20010116 A 8011 MZ4222 STARTER PIPER PA32 PA32301 7103207 SO LYC O540 IO540K1C5 41532 EA ENGINE MALFUNCTIONED A PNSA K NONE O OTHER IN INSP/MAINT 1 AL 03 8429N 100 328106089 L2216448A STARTER WAS MAKING LOUD GRINDING/ DRAGGING NOISE SINCE SHORTLY AFTER INSTALL. AS TIME PROGRESSED NOISES CONTINUED AND P ERFORMANCE DIMINISHED. 1 L 7 1 3O 3 O A3SO 1E4 2001050300299 20010503 00299 EU 2001 5 3 SIMA0935 1 20010403 A 3350 BV033020250 SOCKET SAAB SF340 340B 7860101 EU CABIN SHORTED A SIMA O OTHER O OTHER CR CRUISE 1 SW 21 304AE 340B304 PIT - FLT 5049 - CREW REPORTED AN ELECTRICAL SMELL AROUND SEAT 11A. INSPECTED AREA AND PUT ON MEL AT THIS TIME. MAINTE NANCE REPLACED FLOURESCENT LAMP HOLDER, AT SEAT 11A. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE (M) 2 L 7 2 4T RT A52EU 2001050300300 20010503 00300 EU 2001 5 3 SIMA0957 1 20010405 A 2120 UNKNOWN SAAB SF340 340B 7860101 EU COCKPIT ODOR A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 356SB 340B356 BOS - FLT 4622 - CREW REPORTED SMOKE COMING UP FROM FLOOR ON THE FIRST OFFICERS SIDE WITH A STRONG ODOR OF BURNING ELECT RICAL INSULATION. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT WIRING AND ELECTRICAL BOXES WERE INSPECTED UND ER FLOOR, SIDE WALL, AND INSTRUMENT PANEL WITH NO DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR A FUNCTIONAL CHECK FLIGHT. FCF WAS SATISFACTORY AND AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050300301 20010503 00301 EU 2001 5 3 SIMA200109805 1 20010408 A 3350 3071BPEGPL LIGHT SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 312AE 340B312 SBP - FOUND SEAT 3B EMERGENCY LIGHT FAILS TO ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT AT 3B IAW SAAB AMM 33-50- 20. (M) 2 L 7 2 4T RT A52EU 2001050300302 20010503 00302 EU 2001 5 3 SIMA200109901 1 20010409 A 2460 D43636 SPLICE SAAB SF340 340B 7860101 EU CABIN CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 SBP - FOUND WIRE BUNDLE UNDER FLOOR BY SEATS 3 BC HAS CHAFED WIRES BY BL 18.3 RIGHT SEAT TRACK. REPAIRED CHAFED WIRES L N99 AND LN100 IAW SAAB WM 20-20-35, WIRE BUNDLE IS COMMON TO THE EMERGENCY LIGHT SYSTEM. OPS CHECK OF EMERGENCY LIGHT SY STEM CHECKED GOOD IAW SAAB AMM 33-50-00. (M) 2 L 7 2 4T RT A52EU 2001050300303 20010503 00303 EU 2001 5 3 SIMA0754 1 20010316 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 272AE 340B272 DFW - FLT 3811 - FOUND OVERHEAD EMERGENCY LIGHT AT ROW 3 BC IS INOPERATIVE. MAINTENANCE REPAIRED WIER IAW SAAB MM 33-50 -00. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050300304 20010503 00304 EU 2001 5 3 SIMA0761 1 20010317 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA O OTHER L NO TEST UK UNKNOWN 1 SW 21 335AE 340B335 BFL - FLT 3130 - FOUR ADJACENT FLOOR EMERGENCY LIGHT FAILED TO TEST. MAINTENANCE REMOVED AND REPLACED BATTERY PACKS AT 20LN, 21LN, 22LN, AND 23LN, (S/N 18435, 18173, 17498, 19527). OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050300305 20010503 00305 EU 2001 5 3 SIMA07818 1 20010319 A 3350 OL307BPEGPL BULB SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 304AE 340B304 JFK - FLT 5106 - FOUND LOWER EMERGENCY LIGHT FOR EMERGENCY EXIT DOOR IS INOPERATIVE. MAINTENANCE REPLACED BULB. OPS CH ECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050300306 20010503 00306 EU 2001 5 3 SIMA0843 1 20010325 A 2120 UNKNOWN SAAB SF340 340B 7860101 EU CABIN ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 320AE 340B320 SAN - FLT 3043 - CREW REPORTED STRONG ODOR OF BURNED ELECTRICAL WIRING NEAR ROW 8. MAINTENANCE COULD NOT DUPLICATE DISC REPANCY. CABIN LIGHTS. BALLAST, AND WIRING NEAR ROW 8, RECIRCULATION FANS AND AIR CONDITIONING WERE INSPECTED WITH NO DEFECTS WERE FOUND AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050300307 20010503 00307 EU 2001 5 3 SIMA0844 1 20010325 A 3350 1317 BULB SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 904AE 340B314 DFW - FLT 3356 - CREW REPORTED THE OVERHEAD EMERGENCY LIGHT AT SEAT 11A AND FLOOR EMERGENCY LIGHT AT SEAT 8A TO BE INOPE RATIVE. MAINTENANCE REPLACED THE BULBS AT BOTH POSITIONS. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERV ICE. (M) 2 L 7 2 4T RT A52EU 2001050300308 20010503 00308 EU 2001 5 3 20010503AP002 1 20010325 A 3350 8GS500542405 BULB SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 904AE 340B314 DFW - FLT 3356 - CREW REPORTED THE OVERHEAD EMERGENCY LIGHT AT SEAT 11A AND FLOOR EMERGENCY LIGHT AT SEAT 8A TO BE INOPE RATIVE. MAINTENANCE REPLACED THE BULBS AT BOTH POSITIONS. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERV ICE. REF SIMA0844. (M) 2 L 7 2 4T RT A52EU 2001050300309 20010503 00309 EU 2001 5 3 SIMA0562 1 20010225 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 536AT 536 DFW - DURING SCHEDULED PS CHECK MAINTENANCE REPORTED EVERY OTHER EMERGENCY FLOOR LIGHT WAS INOPERATIVE AND ALL OTHERS WE RE DIM. MAINTENANCE REMOVED AND REPLACED ALL FOUR POWER SUPPLY UNIT BATTERY PACKS, (S/N''S 1654, 1745, 1382, 1381). OP S CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001050300310 20010503 00310 EU 2001 5 3 SIMA0563 1 20010225 A 3350 1317 BULB AEROSP ATR72 ATR72212 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 545AT 545 DURING SCHEDULED PS CHECK, MAINTENANCE REPORTED THE PASSENGER DOOR LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED BULB I N THE LIGHT ASSEMBLY. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001050300311 20010503 00311 NM 2001 5 3 UPS01235777 1 20010418 A 5220 HOUSING BOEING 727 72722C 138400F NM RT EMERG. EXIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE: C, CORROSION ON OPERATING HANDLE HOUSING ON AFT RT EMERGENCY EXIT. OPERATING HOUSING REPLACED IAW S RM 51-30-2 & PER DRW 50-7978 2 L 7 3 4F A3WE 2001050300319 20010503 00319 SO 2001 5 3 20010503CW002 1 20010329 A 2913 1159SCH5059 PUMP GULSTM GV GV SO RROYCE BR700 BR700710A110 NE HYDRAULIC SYS DEFECTIVE B O OTHER O OTHER NR NOT REPORTED 1 GL 15 73M 48 547 R11203 FLUID CONTAMINATION IN RIGHT ENGINE PUMP WAS THE LATEST MODEL AND WAS NEW AT INSTALLATION AND HAS ONLY BEEN OPERATED FOR 48.4 HOURS. WE ARE GETTING BETTER TIME OUT OF THE OLD STYLE PUMPS. 2 L 7 2 4F 4 F RT A12EA E00057EN 2001050300326 20010503 00326 NM 2001 5 3 01FDEA00292 1 20010420 A 2913 PUMP DOUG MD11 MD11F 3023600 NM NR 2 ENGINE OVERTEMP A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 617FE 48748 AFT T/O HYD NR 2 LEFT PUMP OFF FOR HIGH TEMP. SWITCH TO AUTO PUMPS TURNED OFF, TEMP WENT BACK UP AGAIN. 2 L 7 3 4F RT A22WE 2001050300327 20010503 00327 WP 2001 5 3 MWEA010628 1 20010420 A 5521 591041251 SPAR CAP DOUG DC9 DC932 3022066 WP ELEVATOR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 ELEVATOR S/N ESA5 REQUIRED A SPAR CAP REPLACEMENT TO CLEAR CARRY OVER 2401. REMOVED AND INSTALLED NEW SPAR. 2 L 7 2 4F A6WE 2001050300334 20010503 00334 CE 2001 5 3 20010430CW009 1 20010402 A 2910 244110010 PIVOT CESSNA 172 172RG 2072438 CE LYC O360 O360A1D 41514 EA LEFT MLG CRACKED D WIWR K NONE O OTHER IN INSP/MAINT 1 WP 07 9516B 2841 172RG0847 WHILE REPLACING THE RIGHT PIVOT, IT WAS DECIDED TO INSPECT THE LEFT PIVOT ON THIS AIRCRAFT. THE PIVOT SHOWED NO SIGNS O F CRACKING UNTIL ZYGLO TYPE DYE PENETRANT WAS USED UNDER A BLACK LIGHT. THIS REVEALED A TOTAL OF 11 CRACKS THAT RADIATE D OUTWARD FROM THE SPLINES OF THE PIVOT ASSEMBLY. THIS PIVOT WAS ONE OF THE NEW STYLE PIVOTS THAT WAS SUPPOSED TO HAVE A HIGHER RESISTANCE TO FATIGUE. 1 H 7 1 3O 3 O 3A17 E286 2001050300337 20010503 00337 CE 2001 5 3 20010430CW010 1 20010327 A 2131 1305304 CONTROLLER RAYTHN DH125 HAWKER800XP CE GARRTT TFE731 TFE731* 01518 WP CABIN PRESSURE MALFUNCTIONED D K NONE O OTHER IN INSP/MAINT 1 CE 07 729TA 2275 258374 MODERATE LOSS OF PRESSURIZATION OCCURED AT FL330. THE CAUSE WAS OBVIOUSLY A MALFUNCTION OF THE CONTROLLERBECAUSE ONCE R EPLACED THE AIRCRAFT OPERATED FINE. 2 L 7 2 4F 4 F RT A3EU E6WE 2001050300338 20010503 00338 2001 5 3 20010430CW011 4 20010410 A 3416 42230510141 MODULE LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP ALTIMETER DEFECTIVE A DELA K NONE L NO TEST IN INSP/MAINT 1 CE 03 360LJ 45 360 DURING A PREFLIGHT, NR 1 ALTIMETER C/B TRIPPED AND WOULD NOT RESET. AFTER TROUBLESHOOTING FOUND SDC MODULE DEFECTIVE WI TH MOISTURE. THE TRIP WAS MOVET TO A LR55-119. REPLACED SDC MODULE, REPAIRED AVIONIC BOY SEDL. TESTED D/C FOUND OK. 2 L 7 2 4F 4 F A10CE E6WE 2001050300341 20010503 00341 WP 2001 5 3 ABXA010203 1 20010424 A 3350 LIGHT DOUG DC8 DC863 302198A WP COCKPIT INOPERATIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 823AX 46122 THE EMERGENCY LIGHT AMBER LIGHT WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT AMBER LIGH T BULBS IAW DC-8 MM 33-00-00. 2 L 7 4 4F 4A25 2001050300342 20010503 00342 WP 2001 5 3 ABXA010202 1 20010423 A 3350 60030451 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 984AX 47258 THE COCKPIT OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERIE S AND RETURNED THE AIRCRAFT TO SERVICE. ON 04/24/01 MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY P/N 6 0-0304-51, S/N 11413. 2 L 7 2 4F A6WE 2001050300343 20010503 00343 WP 2001 5 3 ABXA010201 1 20010424 A 5714 591046449 ANGLE DOUG DC9 DC933F 302207A WP CNTR WING BOX CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 44451 47465 AN L-ANGLE AT FS 637 LBL 44 THROUGH LBL 54 WAS CORRODED ON THE UPPER SIDE OF THE CENTER FUEL TANK PANEL. MAINTENANCE RE PAIRED THE AREA IAW DC-9 SRM 51-30-1, 51-30-5 AND DOUGLAS DRAWING 5910464. 2 L 7 2 4F A6WE 2001050300344 20010503 00344 WP 2001 5 3 ABXA010200 1 20010424 A 5711 59104641 SPAR DOUG DC9 DC933F 302207A WP WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 THE REAR SPAR UPPER PLANK WAS FOUND TO HAVE INTERGRANULAR CORROSION, BELOW AND ADJACENT TO SLAT PANEL 24 INCHES TO THE L EFT OF THE KEEL. MAINTENANCE REPAIRED THE AREA IAW ABX REA D957-40679. 2 L 7 2 4F A6WE 2001050300345 20010503 00345 WP 2001 5 3 ABXA010199 1 20010425 A 5313 LONGERON DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 LONGERON 24L WAS FOUND TO BE CRACKED AT FS 960. 2 L 7 4 4F 4A25 2001050300346 20010503 00346 WP 2001 5 3 MWEA010644 1 20010425 A 5230 59101415 PAN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 FORWARD CARGO DOOR HAS A CRACK ON AFT SIDE OF OUTER PAN BETWEEN 2 LOWER STOP PADS. FABRICATED AND INSTALLED REPAIR DOUB LER. 2 L 7 2 4F A6WE 2001050300347 20010503 00347 WP 2001 5 3 MWEA010645 1 20010425 A 5280 59101618 SKIN DOUG DC9 DC932 3022066 WP RT MLG DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 RIGHT MAIN LANDING GEAR DOOR CRACKED AT UPPER FORWARD INBOARD CORNER. FABRICATED AND INSTALLED REPAIR SHIM AND REPAIR D OUBLER. 2 L 7 2 4F A6WE 2001050300348 20010503 00348 WP 2001 5 3 MWEA010646 1 20010425 A 5320 39146771 SPLICE DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 LONGERON 30, SPLICE CORRODED, STATION 795-814. BLENDED CORROSION ON LONGERON. BLEND IS WITHIN LIMITS. MAINTENANCE REM OVED AND REPLACED SPLICE. 2 L 7 2 4F A6WE 2001050300349 20010503 00349 WP 2001 5 3 MWEA010647 1 20010425 A 5311 59114481 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 FRAME CORRODED, STATION 833, LONGERON 30, AFT SIDE OF FRAME. FABRICATED AND INSTALLED FRAME REPAIR PARTS. 2 L 7 2 4F A6WE 2001050300350 20010503 00350 WP 2001 5 3 MWEA010649 1 20010425 A 5310 995773925 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 SHEAR TIE CRACKED AT STATION 945, BETWEEN LONGERON 14 AND 15 LEFT. FABRICATED AND INSTALLED FORMER. 2 L 7 2 4F A6WE 2001050300351 20010503 00351 WP 2001 5 3 MWEA010650 1 20010425 A 5320 591142529 STRAP DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 BUTT SPLICE STRAP IS DAMAGED. STRAP IS LOCATED IN AFT BAG PIT STATION 823 LONGERON 26 LEFT THROUGH 26 RIGHT. FABRICATE D AND INSTALLED BUTT SPLICE DOUBLER. 2 L 7 2 4F A6WE 2001050300352 20010503 00352 WP 2001 5 3 MWEA010651 1 20010425 A 5330 591142125 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 AFT CARGO SKIN IS CRACKED AT STATION 803 BETWEEN LONGERON 29 RIGHT AND 30, FROM SKIN SPLICE FORWARD TO THE FASTENER. FA BRICATED AND INSTALLED REPAIR DOUBLER, FILLER, AND FINGER DOUBLER. 2 L 7 2 4F A6WE 2001050300353 20010503 00353 WP 2001 5 3 MWEA010652 1 20010425 A 5320 591970727 DOUBLER DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 LONGERON NR 30 STATION 803-995. TWO DOUBLERS ARE CRACKED. FABRICATED AND INSTALLED DOUBLERS. 2 L 7 2 4F A6WE 2001050300354 20010503 00354 WP 2001 5 3 MWEA010653 1 20010425 A 5320 3913291501 SPLICE DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 LONGERON NR 30 SPLICE AT STATION 955 IS CORRODED. REMOVED AND REPLACED LONGERON SPLICE. 2 L 7 2 4F A6WE 2001050300355 20010503 00355 WP 2001 5 3 MWEA010654 1 20010425 A 5542 9957485507 SKIN DOUG DC9 DC932 3022066 WP RUDDER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 RUDDER SKIN IS CRACKED AT RIB NR 3 LEFT SIDE. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER. 2 L 7 2 4F A6WE 2001050300356 20010503 00356 WP 2001 5 3 MWEA010655 1 20010425 A 5313 59197079 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 LIGHT CORROSION, LONGERON 30, STATION 917. REMOVED AND REPLACED LONGERON. 2 L 7 2 4F A6WE 2001050300357 20010503 00357 2001 5 3 NACA2001016 4 20010420 A 6122 5U1881 GOVERNOR PWA CB3 DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE HAMSTD 43E 43E60 NE NR 3 ENGINE FAILED A NACA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CR CRUISE 1 AL 03 43872 2310 399 P32304 533294 P32304 N192656 NR 3 PROPELLER UNCONTROLLABLE, NR 3 ENGINE RUNAWAY, 3300RPM. REPLACED PROPELLER GOVERNOR, INSPECTED ALL OIL SCREENS/CET ERFUGE, NO DEFECTS. OVERSPEED WITHIN LIMITS. 2 L 7 4 4R 4 R 6A3 5E8 6 C P871 2001050300358 20010503 00358 WP 2001 5 3 ABXA010204 1 20010425 A 3240 BRAKE DOUG DC8 DC863F 302198F WP MLG DEFECTIVE A ABXA K NONE O OTHER LD LANDING 1 GL 23 811AX 46113 THE BRAKES WERE SPONGY AND INEFFECTIVE ON LANDING. 2 L 7 4 4F 4A25 2001050300359 20010503 00359 EA 2001 5 3 COMA0160362 1 20010424 A 5320 601R31171 ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 933CA 16868 7040 THE ANGLES AT BL27 (LT & RT) AND INTERCOSTALS AT BL 36 (LT & RT) AT FS 484 ARE CRACKED. INSTALLED NEW SERVICEABLE LT & RT INBOARD AND OUTBOARD 484 ANGLES IAW WVAC EO 601R-53-2413A. 2 L 7 2 4F RT A21EA 2001050300360 20010503 00360 NM 2001 5 3 AWXA0001628 1 20010424 A 5310 6545409245 PRESSURE PANEL BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 169AW 23630 LEFT MLG W/W PRESSURE WEB CRACKED AT BS 663 APPROX BL 32. REMOVED UPPER ATTACH CHANNEL; TRIMMED OUT DAMAGED PORTION OF WEB; FABBED REPAIR -1 DOUBLER, -2 FILLER AND -3 STIFFENER; TREATED AND PRIMED REPAIR PARTS; INSTALLED REPAIR AND THE UPP ER ATTACH CHANNEL IAW AWA ER 03-5716-01101-SSIA. 2 L 7 2 4F RT A16WE 2001050300361 20010503 00361 NM 2001 5 3 AWXA0001629 1 20010424 A 5312 65163007 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 169AW 23630 HFEC INDICATES CRACK AT FASTENER HOLE LBL 10 WL 234.1 BS 179 BLKHD WEB FORWARD SIDE. CUT OUT DAMAGED SKIN AREA; LOCATED , DRILLED AND INSTALLED REPAIR DOUBLER AND FILLER IAW B737-300 SRM 53-10-08. 2 L 7 2 4F RT A16WE 2001050300362 20010503 00362 NM 2001 5 3 AWXA0001644 1 20010424 A 5312 65163007 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 169AW 23630 HFEC INDICATES .5 INCH CRACK EMANATING FROM BENEATH STRAP IN WEB BS 178 BLKHD RBL 6.8 WL 212.5 CONFIRMED 10X VISUAL. CU T OUT DAMAGED WEB AREA; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER AND FILLER IAW B737-300 SRM 53-10-08. 2 L 7 2 4F RT A16WE 2001050300363 20010503 00363 NM 2001 5 3 AWXA0001645 1 20010425 A 3150 MS252531 SWITCH BOEING 737 737277 1384570 NM COCKPIT BROKEN A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 188AW 22655 OAK - ABORTED TAKEOFF - 4/21/01 - AS POWER WAS APPLIED FOR TAKEOFF, THE CONFIGURATION WARNING HORN SOUNDED AND THE TAKEO FF WAS ABORTED; THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE TROUBLESHOT AND FOUND THE SPEED BRAKE TAKEOFF WARNING SW ITCH (S651) BROKEN. THE SWITCH WAS REPLACED AND FUNCTIONALLY CHECKED GOOD. 2 L 7 2 4F RT A16WE 2001050300364 20010503 00364 WP 2001 5 3 CALA0100416 1 20010424 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 LEFT CUSP ANGLE CORRODED AT STATION 1322-1338. CUSP ANGLE REPAIRED PER EA 9-5314-2-A0873. FABRICATED REPAIR ANGLE FROM .050 7075T6. INSTALLED PER SRM 51-30-02 AND EC/RA 5310-04134. 2 L 7 2 4F A6WE 2001050300365 20010503 00365 NM 2001 5 3 CALA0100418 1 20010425 A 5311 6546547675 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 CRACK IN FRAME STATION 727 AT S 14L. REPAIRED PER EC/RA 5310-04133. 2 L 7 2 4F RT A16WE 2001050300366 20010503 00366 NM 2001 5 3 2001UALA00557 1 20010418 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 1175 STRINGERS 39R TO 39L SHEAR TIE CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.FABRICATED AND INSTA LLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T2102 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001050300367 20010503 00367 NM 2001 5 3 2001UALA00558 1 20010421 A 5310 STRUCTURE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 STA 400 LBL 50 NUT CLIP HOLE IS ELONGATED. REMOVED DAMAGE AND INSTALLED AN ANGLE REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001050300368 20010503 00368 NM 2001 5 3 2001UALA00559 1 20010422 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 FUSELAGE SKIN DAMAGED AND BONDED DOUBLER SEPERATED FROM SKIN ABOVE STRINGER 4R STA 569. THE DAMAGED AREA WAS CUT OUT AN D A SKIN DOUBLER WAS INSTALLED. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001050300369 20010503 00369 NM 2001 5 3 2001UALA00560 1 20010420 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 CABIN FRAME CRACKED AT STA 727C BELOW STRINGER 14L. REPAIRED CRACKED FRAME. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001050300370 20010503 00370 NM 2001 5 3 2001UALA00562 1 20010420 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 314UA 23675 BS 178 BULKHEAD WEB CRACKED AT RBL 1 AND LBL 1 AT WL 187 IN TWO PLACES. INSTALLED A DOUBLER TO THE AFFECTED AREA. MAJO R REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001050300371 20010503 00371 NM 2001 5 3 2001UALA00563 1 20010422 A 5240 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 314UA 23675 FORWARD GALLEY DOOR LOWER AFT CORNER CRACKED FROM BOTH SIDES OF FASTENER HOLE ON DOOR FRAME. SPLICE REPAIR ACCOMPLISHED TO DAMAGED AREA. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001050300372 20010503 00372 NM 2001 5 3 2001UALA00564 1 20010420 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE MISREPAIRED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 STA 344 RBL 13 CABIN FLOOR BEAM HAS INCORRECT REPAIR. REMOVED INCORRECT REPAIR. INSTALLED ANGLE DOUBLER WITH STRAP REP AIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001050300373 20010503 00373 NM 2001 5 3 2001UALA00565 1 20010420 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 RIGHT HAND FUSELAGE INTERCOSTAL CRACKED AT STA 278 BETWEEN STRINGER 14R HAT CHANNEL AT THE FORWARD INBOARD RADIUS. REPL ACED INTERCOSTAL AND STRINGER CLIP. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001071100027 20010711 00027 NM 2001 7 11 2001UALA00566 1 20010420 A 3350 8100033901 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE L NO TEST UK UNKNOWN 1 WP 29 773UA 26929 EMERGENCY LIGHT ON SEAT 19G INOP. *S/D* BULB IN FLOOR PROXIMITY LIGHT ASSY FAILED. REPLACED FLOOR PROXIMITY LIGHT ASS Y. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001050300374 20010503 00374 2001 5 3 2001UALA00567 4 20010423 A 2330 VIDEO UNIT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 191UA 26880 WHEN VIDEO CLOSET DOOR WAS PULLED UP IT HIT SOMETHING BEHIND THE VIDEO EQUIPMENT, SPARKS AND ELECTRICAL SMELL REPORTED B Y CREW. VIDEO SYSTEM IS INOP. 2 L 7 4 4F 4 F RT A20WE E24NE 2001053100295 20010531 00295 NM 2001 5 31 2001UALA00570 1 20010422 A 3350 6012541LB BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7294U 21572 BOTH LT ESCAPE HATCH EMERGENCY EXIT SIGNS ARE INOPERABLE. *S/D* BATTERY PACK FAILED. REPLACED BATTERY PACK. OPERATIO NS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001050300375 20010503 00375 NM 2001 5 3 2001UALA00571 1 20010423 A 5754 RIB BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE SLAT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7258U 21405 NR 3 SLAT ACTUATOR INBOARD RIB IS CRACKED. REPAIRED PER SM OR 70-57-56-01-AR5. MAJOR REPAIR ACCOMPLISHED. 2 L 7 3 4F 4 F A3WE E2EA 2001050300376 20010503 00376 NM 2001 5 3 2001UALA00572 1 20010424 A 5522 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT ELEVATOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7466U 21920 RT ELEVATOR OUTBOARD TRAILING EDGE HAS LIGHTNING DAMAGE. SKIN IS CRACKED, MELTED, PUNCTURED AND STATIC WICK IS MISSING. REPAIRED ELEVATOR PER SM OR 70-55-20-03-JD, AND INSTALLED REPAIR PER SRM 51-30-02. MAJOR REPAIR ACCOMPLISHED. 2 L 7 3 4F 4 F A3WE E2EA 2001060100162 20010601 00162 NE 2001 6 1 2001UALA00573 2 20010424 A 7532 5840207104 BLEED VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE MALFUNCTIONED A UALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 29 590UA 28708 727195 AFTER POWER REDUCED TO CLIMB THRUST THE LEFT ENGINE EXPERIENCED A COMPRESSOR STALL. *S/D* REPLACED 14TH STAGE BLEED VA LVE (BEANPOT) PRECAUTIONARY. 2 L 7 2 4F 4 F RT A2NM E17NE 2001061800007 20010618 00007 NM 2001 6 18 2001UALA00574 1 20010424 A 7331 MR73364 POWER SUPPLY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUEL SYSTEM INOPERATIVE A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 7256U 21403 FUEL FLOW INDICATION FOR ALL ENGINES WENT TO ZERO TWICE IN FLIGHT. AIRCRAFT DIVERTED TO MCI. *S/D* THE CAUSE OF THE F UEL FLOW INDICATION TO READ ZERO IS THE FUEL FLOW POWER SUPPLY UNIT. THERE IS ONLY ONE POWER SUPPLY UNIT FOR ALL THREE INDICATORS. THE FUEL FLOW POWER SUPPLY UNIT WAS REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 2001053100296 20010531 00296 NM 2001 5 31 2001UALA00575 1 20010424 A 3397 362624 WIRE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7448U 21902 FIRST CLASS FLOOR EMERGENCY LIGHTS ARE INOPERABLE. *S/D* LIGHT ASSY CABLE SHORTED. TROUBLESHOT AND FOUND EEL STRIP SH ORTED. REPLACED LIGHT ASSY CABLE. 2 L 7 3 4F 4 F A3WE E2EA 2001050300377 20010503 00377 NM 2001 5 3 2001UALA00576 1 20010423 A 5311 FAILSAFE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 REMOVED FAILSAFE STRAP TO FACILITATE STRINGER REPAIR STATION 368 STRINGERS 37R TO 39R. MAJOR REPAIR ACCOMPLISHEDCUT OUT REQUIRED SECTION, FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 51-70-12. 2 L 7 2 4F 4 F RT A1NM E3NE 2001050300378 20010503 00378 NM 2001 5 3 2001UALA00577 1 20010424 A 5320 SPLICE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 STATION 1439 FRAME SPLICE CORRODED AT STRINGERS 25R TO 26R. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW FRAME SPLICE IN AC CORDANCE WITH SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001050300379 20010503 00379 NM 2001 5 3 2001UALA00578 1 20010424 A 5311 FRAME BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 1131 LBL 40-45 FRAME T-CAP IS CORRODED. MAJOR REPAIR ACCOMPLISHEDFABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 146T203-5 ANDSRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001050300380 20010503 00380 NM 2001 5 3 2001UALA00579 1 20010424 A 5320 FITTING BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 1373 STRINGER 39L END FITTING IS CORRODED. MAJOR REPAIR ACCOMPLISHEDFABRICATED AND INSTALLED REPAIR IN ACCORDANCE WI TH BAC DRAWING 146T3240 AND BAC DRAWING 146T3006. 2 L 7 2 4F 4 F RT A1NM E3NE 2001050300381 20010503 00381 NM 2001 5 3 2001UALA00581 1 20010425 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE TOOL DAMAGE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 STA 178 WL 211 RBL 28 AFT FACE HAS TOOL DAMAGE. REPAIRED DAMAGED AREA. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001050300382 20010503 00382 NM 2001 5 3 2001UALA00582 1 20010425 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 STA 178 BULKHEAD CRACKED AT LBL 1 AND RBL 1 WL 188. CUT OUT THE DAMAGED AREA AND INSTALLED A DOUBLER. MAJOR REPAIR ACC OMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001050300383 20010503 00383 NM 2001 5 3 2001UALA00583 1 20010425 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 STA 178 BULKHEAD CRACKED AT LOWER RIGHT HAND RADAR MOUNT. CUT OUT DAMAGED AREA AND INSTALLED A DOUBLER. MAJOR REPAIR A CCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001050300384 20010503 00384 NM 2001 5 3 2001UALA00584 1 20010425 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 STA 178 BULKHEAD CRACKED AT THE LOWER LEFT HAND RADAR MOUNT. CUT OUT THE DAMAGED AREA AND INSTALLED A DOUBLER. MAJOR R EPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001050300385 20010503 00385 NM 2001 5 3 2001UALA00586 1 20010425 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 AFT PIT STA 787 FRAME DENTED AT STRINGER 26R. REPAIRED DAMAGED AREA. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001050300387 20010503 00387 NM 2001 5 3 2001UALA00588 1 20010426 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 FUSELAGE STA 195 WL 207 RBL 30 STRINGER 17 CREASE BEAM WEB IS CRACKED. REPLACEMENT WEB MANUFACTURED AND INSTALLED. MAJ OR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001050300388 20010503 00388 EA 2001 5 3 20010427CW001 1 20010405 A 5610 6003303025 WINDSHIELD CNDAIR CL600 CL6001A11 1900302 EA LYC ALF502 ALF502* 41580 EA COCKPIT CRACKED E EXOA O OTHER O OTHER CR CRUISE 1 SO 17 63HJ 783 1021 DURING CRUISE FLIGHT, LEFT WINDSHIELD CRACKED. CREW CALLED MAINTENANCE. MAINTENANCE ADVISED TO TURN HEAT OFF. DELAMI NATION STOPPED, CONTINUED TO DESTINATION. 2 L 7 2 4F 4 F RT A21EA E6NE 2001050300390 20010503 00390 NM 2001 5 3 2001UALA00589 1 20010426 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 STA 616 RIGHT HAND FRAME INNER CHORD CRACKED AT THE LOWER END BELOW THE CREASE BEAM. CUT OUT THE DAMAGED AREA OF THE CH ORD AND INSTALLED A STIFFENING ANGLE. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001050300391 20010503 00391 NM 2001 5 3 2001UALA00590 1 20010426 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 AFT PIT STA 827 FRAME ABOVE STRINGER 24L IS DENTED. REPAIRED DAMAGED AREA. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001050300392 20010503 00392 NM 2001 5 3 2001UALA00592 1 20010426 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 314UA 23675 AFT CABIN FLOORBEAM TOP CAP STA 947 RBL 18 TO RBL 38 HAS EXCESSIVE MATERIAL REMOVED. REMOVED DAMAGE AND INSTALLED FABRI CATED REPAIR PARTS. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001050300393 20010503 00393 NM 2001 5 3 2001UALA00593 1 20010321 A 5311 FRAME BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 AFT PIT BS 1329 LBL 8-25 FRAME T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED REPLACED T-CAP REF: BAC 146T1210 AND SRM 51-4 0-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001052100065 20010521 00065 NE 2001 5 21 2001UALA00594 2 20010426 A 7321 8228305 EEC PWA PW40903 BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE LT ENGINE OUT OF TOLERANCE A UALA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 WP 29 786UA 14713 14713 222001 26938 222001 ON T/O, WHEN ENGAGING AT UPON THRUST APPLICATION, LT ENG LAGGED BEHIND RT, ADDED THROTTLE MANUALLY, EVENTUALLY ALL THE W AY TO STOP EPR WAS PEGGED 1.395 (1.444=REDUCED TO) WITH RT ENG. AT 1.44. ENGS NORMAL OPS AT SETTING OF CLIMB. REPLACED ELECTRONIC ENGINE CONTROL AND ACCOMPLISHED HIGH POWER RUN-UP. EEC INTERNAL PRESSURE SENSOR FOR P2 WAS FOUND HIGH OUT OF LIMITS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001050300395 20010503 00395 CE 2001 5 3 20010502CW008 1 20010409 A 3234 644183864 HANDLE BEECH 18 E18S 1151006 CE PWA R985 R985* 52008 NE MLG HANDLE MISREPAIRED B ABOR A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 GL 15 16U 14561 BA394 DURING TAKEOFF, AT AROUND 70 KNOTS AIRSPEED, THE LANDING GEAR RETRACTED WITHOUT A COMMAND FROM THE PILOT. MAINTENANCE F OUND THE GEAR SELECTOR WHEN MOVED TO DOWN AND LOCK POSITION WOULD NOT ALWAYS FULLY ENGAGE INTO THE DOWN AND LOCK DETENT. THIS WAS CAUSED BY A SMALL WASHER GETTING CAUGHT IN THE DOWN AND LOCK DETENT GROOVE CAUSING THE GEAR HANDLE TO SIT RIG HT ON THE EDGE OF THE DETENT AND WIGH VERY SLIGHT FINGER PRESSURE APPLIED TO THE GEAR HANDLE, IT WILL POP UP INTO THE GE AR UP POSITION. THE DEFECTIVE HANDLE HAD A SMALL WASHER INSTALLED, AND THE SERVICEABLE HANDLES HAD A LARGE AREA WASHER INSTALLED, THAT CNA NOT GET CAUGHT IN THE DETENT GROOVE. 1 L 7 2 3R 3 R A765 5E1 2001050700001 20010507 00001 NM 2001 5 7 ERKR200100066 1 20010326 A 5330 592480296 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DENTED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 12FQ 49766 DENTED SKIN AT STATION 540 - 560, BETWEEN L17 AND L18 RIGHT HAND SIDE. ADDRESS REPAIR OF EXISTING DENTED SKIN LOCATED A T STATION 540 - 560, BETWEEN L17-L18, RIGHT HAND SIDE PER ECRA N12FQ-53-MD88-009-EAC. 2 L 7 2 4F RT A6WE 2001050700002 20010507 00002 NM 2001 5 7 ERKR200100065 1 20010326 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 12FQ 49766 REPAIR-SKIN PANEL, STATION 560, STRINGER 27 RIGHT. THIS DOCUMENT PROVIDES REPAIR INSTRUCTIONS FOR REPLACEMENT OF AN EXI STING REPAIR WITH A PERMANENT REPAIR AT THE SUBJECT LOCATION. THE SKIN PANEL WAS FOUND TO HAVE AN UNDOCUMENTED REPAIR I N THE AREA OF AN INTERNAL SKIN DOUBLER PER ECRA N12FQ-53-MD88-010-EAC. 2 L 7 2 4F RT A6WE 2001050700003 20010507 00003 NM 2001 5 7 ERKR200100069 1 20010326 A 5510 3912060503 HINGE DOUG MD88 MD88 3023688 NM HORIZ STAB CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 12FQ 49766 REPAIR - CORROSION, HORIZONTAL STABILIZER HINGE - SIDE LOAD FITTING. THIS DOCUMENT PROVIDES REPAIR INSTRUCTIONS FOR COR ROSION FOUND AT THE HORIZONTAL STABILIZER HINGE SIDE LOAD FITTING. THE CORROSION IS IN THE AREA OF THE 2.0 INCHES DIAME TER COUNTERBORE. THE SIDE LOAD FITTING (P/N IS 3912060-503) PER ECRA N12FQ-55-MD88-003-EAC REV A. 2 L 7 2 4F RT A6WE 2001050700004 20010507 00004 NM 2001 5 7 ERKR200100070 1 20010326 A 5730 9937581505 PANEL DOUG MD88 MD88 3023688 NM LT WING CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 12FQ 49766 REPAIR- CORROSION, LEFT LOWER FORWARD WING PANEL, XFS=129.847. THIS DOCUMENT PROVIDES REPAIR INSTRUCTIONS FOR CORROSION FOUND COMMON TO THE LOWER SURFACE OF THE LEFT WING FORWARD PANEL, (P/N 9937581-505). REPAIR IS ACCOMPLISHED BY BLENDIN G OUT THE CORROSION AND INSTALLING AN EXTERNAL REPAIR DOUBLER PER ECRA N12FQ-57-MD88-004-EAC. 2 L 7 2 4F RT A6WE 2001050700005 20010507 00005 NM 2001 5 7 ERKR200100071 1 20010327 A 5754 65B0113514 FLAP BOEING 747 747100 NM LT WING L/E DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 911 20781 A 5.5 X 9.5 INCH HOLE TORE IN THE FOLDING NOSE ASSY, 2 LINKS ASSY''S .5 INCH IN DIAMETER AND 12 INCHES IN LENGTH BROKEN BY THE OUTBOARD SCISSOR LINK AND ONE BROKEN BY THE INBOARD SCISSOR ON THE NR 7 LEADING EDGE VARIABLE CAMBER FLAP, LEFT W ING. RECOMMENDATION IS TO ADD IT TO THE AGING FLEET INSPECTIONS. 2 L 7 4 4F RT A20WE 2001050700006 20010507 00006 NM 2001 5 7 ERKR200100072 1 20010327 A 5754 65B0113516 HINGE BOEING 747 747100 NM L/E FLAP CRACKED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 911 20781 CRACK ON THE INBOARD HINGE OF THE FOLDING NOSE ASSEMBLY ON THE NR 2 LEADING EDGE VARIABLE CAMBER FLAP LEFT WING. RECOMM ENDATION IS TO ADD IT TO THE AGING FLEET INSPECTIONS. 2 L 7 4 4F RT A20WE 2001050700007 20010507 00007 NM 2001 5 7 ERKR200100073 1 20010327 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 WINDOW AT STATION 210 RIGHT HAND SIDE HAS CORROSION ON AND AROUND WINDOW CASTING. REMOVED LIGHT SURFACE CORROSION PER B 747 56-20-01, ALODINED PER B747 SRM 51-10-02, PRIMED PER B747 SOPM 20-41-02, RESEALED PER B747 SOPM 20-50-19. 2 L 7 4 4F A20WE 2001050700008 20010507 00008 NM 2001 5 7 ERKR200100074 1 20010327 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 MAIN DECK RT STATION 300 TO 320 AND BETWEEN S-20R AND S-22R WINDOW FORGING HAS CORROSION UNDER FORGING. CLEANED AND TRE ATED CORROSION PER SRM 51-10-01, SRM 56-20-01, 51-10-01, SRM 51-30-02, SOPM 20-10-03 PG 1-24, SOPM 20-41-02 PG 1. 2 L 7 4 4F A20WE 2001050700009 20010507 00009 NM 2001 5 7 ERKR200100075 1 20010327 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 MAIN DECK RT SIDE BETWEEN STATION 320 TO 340 WINDOW FORGING BETWEEN S-20R AND S-22R HAS CORROSION UNDER FORGING. REMOVE D LIGHT SURFACE CORROSION PER B747 SRM 51-10-01. WINDOW FORGING IS FOUND TO BE WITHIN LIMITS PER B747 SRM 56-20-01. 2 L 7 4 4F A20WE 2001050700010 20010507 00010 NM 2001 5 7 ERKR200100076 1 20010327 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 MAIN DECK RT FROM STA 360 TO 380 BETWEEN S-20R AND S-22R WINDOW FORGING HAS CORROSION UNDER FORGING. REMOVED, CLEANED C ORROSION CHECKED LIMITS AND REINSTALLED WINDOW FORGING PER 747 SRM 51-10-01, SRM 56-20-01, SRM 51-10-02, 51-30-02, SOPM 20-10-03, SOPM 20-41-02, MM 56-21-01. 2 L 7 4 4F A20WE 2001050700011 20010507 00011 NM 2001 5 7 ERKR200100077 1 20010327 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 MAIN DECK RT SIDE FROM STA 380 TO STA 400 BETWEEN S-20R AND S-22R WINDOW FORGING HAS CORROSION UNDER FORGING. REMOVED W INDOW FORGING, REMOVED LIGHT SURFACE CORROSION WITHIN LIMITS, INSTALLED WINDOW FORGING AND SEALED PER SRM 51-30-02, SOPM 20-50-01, SRM 51-10-06, SOPM 20-10-03. 2 L 7 4 4F A20WE 2001050700012 20010507 00012 NM 2001 5 7 EISA20010073 1 20010320 A 2150 32167441 A/C PACK BOEING 727 727225 1384077 NM FUSELAGE MALFUNCTIONED A EISA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 356PA 20626 CABIN PRESSURE UNSTABLE, DIVERTED INTO (BNA). RAN ENGINES AND A/C FOR LEAKS, NONE FOUND. CABIN PRESSURE OPS CHECK NORM AL. 2 L 7 3 4F A3WE 2001050700013 20010507 00013 NE 2001 5 7 SWIA972510 2 20010417 A 7320 CONTROL CABLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT ENGINE OUT OF ADJ A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 416SW 7089 AT TAKEOFF N1 SETTING NOTICED HIGHER THAN NORMAL ITT TEMPS ON RIGHT ENGINE. ALSO AT GROUND IDLE, NOTICED HIGHER THAN NO RMAL N1 SPEEDS AT 28 PERCENT. ADJUSTED RIGHT ENGINE VG ACTUATOR FEED BACK CABLE IAW 72-00-00 SPECIAL PROCEDURE 07. RAN CHECK A/C, ALL RAN NORMAL. 2 L 7 2 4F 4 F RT A21EA E15NE 2001050700014 20010507 00014 NE 2001 5 7 01FDEA00295 2 20010424 A 7200 JT8D17AQM ENGINE BOEING 727 727227 1384078 NM PWA JT8 JT8D17 52049 NE NR 3 ENGINE LEAKING A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 490FE 21493 NR 3 ENG DURING CLIMBOUT, LOW OIL PRESS/FILTER BYPASS LIGHT ILLUM. FOLLOWED RED TAB THRU ENG SHUTDOWN. PREVIOUS WRITE- UP ON NR 3 OIL PRESS. *S/D* REMOVED AND REPLACED NR 3 ENG PER WORK CARD 70T0001-03. 2 L 7 3 4F 4 F A3WE E2EA 2001050700015 20010507 00015 NM 2001 5 7 ERKR200100078 1 20010424 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 MAIN DECK RT SIDE FROM STA 400 TO 420 BETWEEN S-20R AND S-22R WINDOW FORGING HAS CORROSION UNDER FORGING. REMOVED WINDO W FORGING, REMOVED CORROSION FOUND IT IN LIMITS PER SRM 51-10-01 & SRM 56-20-01. ALODINED AND PRIMED PER SRM 51-10-02. INSTALLED WINDOW FORGING AND SEALED PER SRM 51-30-02 & SOPM 20-050-01. 2 L 7 4 4F A20WE 2001050700016 20010507 00016 NM 2001 5 7 ERKR200100079 1 20010424 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 MAIN CABIN WINDOW FORGING AT STA 560 TO 580 RT HAS CORROSION ON UPPER FRD CORNER COMING OUT FROM UNDER SEALANT. REMOVED SEALANT AND LIGHT CORROSION WITHIN LIMITS. ALODINED AND PRIMED, RESEALED WITH BMS 5-95 SEALANT PER 747 SRM 51-10-01, 5 1-10-02, 56-20-01, AND 747 SOPM 20-41-02. 2 L 7 4 4F A20WE 2001050700017 20010507 00017 NM 2001 5 7 ERKR200100080 1 20010424 A 5620 65B041655 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 CORROSION ON WINDOW FRAME AT STA 950 RIGHT AFT LOWER CORNER. REMOVED WINDOW FORGING, REMOVED CORROSION FROM WINDOW FRAM E PER SRM 51-10-01. FOUND WINDOW FRAME TO BE OUT OF LIMITS PER SRM 56-20-01. REMOVED AND REPLACED WINDOW FRAME PER SR M 51-10-01, SRM 51-30-05, SRM 51-30-02 & SOPM 20-41-02. 2 L 7 4 4F A20WE 2001050700018 20010507 00018 NM 2001 5 7 ERKR200100081 1 20010424 A 5620 65B041657 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 RIGHT WINDOW AT STA 1070 HAS CORROSION ON AND AROUND WINDOW CASTING. REMOVED WINDOW FORGING PER 747 SRM 51-30-02 WINDOW FORGING FOUND TO BE OUT OF LIMITS PER 747 SRM 56-20-02. REMOVED WINDOW FORGING AND REPLACED WITH NEW FORGING PER 747 SRM 51-30-02, 51-10-02, SOPM 20-41-02. 2 L 7 4 4F A20WE 2001050700019 20010507 00019 NM 2001 5 7 ERKR200100082 1 20010424 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 WINDOW FORGING BETWEEN STA 1080 - 1100 HAS CORROSION COMING OUT FROM UNDER THE SEALANT IN THE MAIN CABIN ON THE RIGHT SI DE. REMOVED WINDOW FORGING PER 747 SRM 56-20-01, REMOVED CORROSION WITHIN LIMITS PER 747 SRM 56-20-01. REINSTALLED WIN DOW FORGING PER 747 SRM 51-30-02. 2 L 7 4 4F A20WE 2001050700020 20010507 00020 NM 2001 5 7 ERKR200100083 1 20010424 A 5620 65B041657 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 MAIN DECK RT SIDE FROM STA 1438 TO 1460 BETWEEN S-20R AND S-22R WINDOW FORGING HAS CORROSION UNDER FORGING. REMOVED WIN DOW FORGING PER 747 SRM 51-10-01. REMOVED CORROSION ON FORGING AND FOUND TO BE OUT OF LIMITS PER 747 SRM 56-20-01. INS TALLED NEW WINDOW FORGING AND SEALED PER 747 SRM 51-10-01, SRM 51-30-05 & SRM 51-30-06. 2 L 7 4 4F A20WE 2001050700021 20010507 00021 NM 2001 5 7 ERKR200100084 1 20010424 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 MAIN CABIN LT SIDE BETWEEN STA 180 TO 200 AND BETWEEN S-20L AND S-22L WINDOW FORGING HAS CORROSION ON UPPER FASTENERS. REMOVED UPPER FASTENERS AND REMOVED LIGHT SURFACE CORROSION FROM FORGING PER 747 SRM 51-10-01. INSTALLED NEW FASTENERS PER 747 SRM 51-30-02 AND SOPM 20-41-02. 2 L 7 4 4F A20WE 2001050700022 20010507 00022 EA 2001 5 7 SWIA972527 1 20010423 A 2710 AILERON CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE WING JAMMED A SWIA K NONE F FLT CONT AFFECTED AP APPROACH 1 NM 07 413SW 7102 AT ABOUT 1000 FT ON FINAL JUST AFTER TURNING AUTOPILOT OFF AILERONS WERE LOCKED UP. AFTER ABOUT 15 TO 20 SECONDS THEY B ECAME NORMAL. OPERATED AUTOPILOT WITH ALL 3 HYDRAULIC SYSTEMS, ALSO WITH INDIVIDUAL SYSTEMS ARMED, CONTROL AND INDICATI ON NORMAL. AP DISCONNECT SWITCHES CAPTS AND F/OS AND FCP ALL CHECK GOOD WITH WARNINGS AND FLIGHT CONTROLS (AILERON) DIS CONNECTED NORMAL. OVERRIDE OF AILERONS NORMAL, NO PHYSICAL ABNORMALITIES NOTED ON FLIGHT CONTROL SURFACE. REF CL600 MM 22-11-21, 22-11-02. 2 L 7 2 4F 4 F RT A21EA E15NE 2001050700023 20010507 00023 NM 2001 5 7 ERKR200100085 1 20010425 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 MAIN CABIN LT SIDE BETWEEN STA 200 TO 220 AND BETWEEN S-20L AND S-22L WINDOW HAS CORROSION UNDER FORGING ON AFT SIDE. RE MOVED SEALANT AND REMOVED LIGHT SURFACE CORROSION PER 747 SRM 51-10-01. TREATED AND PRIMED AND SEALED PER 747 SRM 51-10- 02 AND SOPM 20-41-02. 2 L 7 4 4F A20WE 2001050700024 20010507 00024 NM 2001 5 7 ERKR200100086 1 20010425 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 MAIN DECK LT SIDE FROM STA 320 TO 340 BETWEEN S-20L AND S-22L WINDOW FORGING HAS CORROSION UNDER FORGING. REMOVED WINDO W FORGING, CLEANED SURFACE CORROSION, FOUND TO BE WITHIN LIMITS PER 747 SRM 56-20-01. ALODINED AND PRIMED PER 747 SRM 5 1-10-03 AND SOPM 20-41-02 AND INSTALLED WINDOW FORGING PER 747 SRM 51-30-02. 2 L 7 4 4F A20WE 2001050700025 20010507 00025 NM 2001 5 7 ERKR200100087 1 20010425 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 MAIN DECK LT SIDE FROM STA 380 TO 400 BETWEEN S-20L AND S-22L WINDOW FORGING HAS CORROSION UNDER FORGING. REMOVED WINDO W FORGING PER 747 SRM 51-30-02. REMOVED LIGHT SURFACE CORROSION PER 747 SRM 51-10-01 AND FOUND TO BE WITHIN LIMITS PER 747 SRM 56-20-01. ALODINED AND PRIMED PER 747 SRM 51-10-02 AND SOPM 20-41-02. INSTALLED WINDOW FORGING PER 747 SRM 51- 30-02. 2 L 7 4 4F A20WE 2001050700026 20010507 00026 NM 2001 5 7 ERKR200100088 1 20010425 A 5330 SKIN BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 SURFACE CORROSION ON SKIN AROUND PAX WINDOW FORGING STA 500 TO 520 AND S-20L TO S-22L. ALSO ON UNDER SIDE OF S-22L AND UPPERSIDE OF S-20L MAIN CABIN LT SIDE. REMOVED WINDOW AND FORGING PER 747 SOPM 20-50-01. REMOVED CORROSION ON FORGING AND FUSELAGE SURFACE PER 747 SRM 51-10-01 FOUND TO BE WITHIN LIMITS PER 747 SRM 56-20-01. REPLACED WINDOW FORGING PER 7 47 SRM 51-30-01. 2 L 7 4 4F A20WE 2001050700027 20010507 00027 NM 2001 5 7 ERKR200100089 1 20010425 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 CORROSION BETWEEN S-20L AND WINDOW FORGING AT STA 530 MAIN CABIN LT SIDE. REMOVED LIGHT SURFACE CORROSION WITHIN LIMITS PER 747 SRM 56-20-01. ALODINED PER 747 SRM 51-10-02 AND PRIMED PER 747 SOPM 20-41-02. 2 L 7 4 4F A20WE 2001050700028 20010507 00028 NM 2001 5 7 ERKR200100090 1 20010425 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 MAIN CABIN WINDOW FORGING AT STA 660 - 680 LEFT HAND HAS CORROSION IN SEVERAL SPOTS COMING OUT FROM UNDER SEALANT. REMO VED SEALANT AND REMOVED CORROSION PER 747 SRM 51-10-01, WITHIN LIMITS PER 747 SRM 56-20-01. ALODINED PER 747 SRM 51-10- 02 AND PRIMED PER 747 SOPM 20-41-02 AND RESEALED PER 747 SRM 51-10-06. 2 L 7 4 4F A20WE 2001050700029 20010507 00029 NM 2001 5 7 ERKR200100091 1 20010425 A 5620 65B0701010 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 WINDOW AT STA 670 LEFT HAS CORROSION ON AND AROUND WINDOW CASTING. REMOVED WINDOW FORGING PER 747 SRM 51-30-02. REMOVE D CORROSION FROM PITTED AREAS OF FRAME OUTER SURFACE PER 747 SRM 55-20-01, OUT OF LIMITS PER 747 SRM 56-20-01. REPLACED WINDOW FORGING PER 747 SRM 51-30-02 AND 51-10-01 AND SOPM 20-41-02 AND PER ECRA 3203-53-47-2. 2 L 7 4 4F A20WE 2001050700030 20010507 00030 NM 2001 5 7 ERKR200100092 1 20010425 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 MAIN CABIN AT STA 986 LT SIDE WINDOW FORGING HAS 2 AREAS OF CORROSION JUST ABOVE S-22L. BLENDED OUT CORROSION PER 747 S RM 51-10-01, MINIMUM MATERIAL REMOVED. ALODINED PER 747 SRM 51-10-02 AND PRIMED PER 747 SOPM 20-41-02 AND SEALED PER 74 7 SRM 51-10-06. 2 L 7 4 4F A20WE 2001050700031 20010507 00031 NM 2001 5 7 ERKR200100093 1 20010425 A 5620 65B041659 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 WINDOW AT STA 1010 LEFT HAS CORROSION ON AND AROUND WINDOW CASTING. REMOVED WINDOW FORGING PER 747 SRM 51-30-02. REMOV ED CORROSION PER 747 SRM 51-10-01 OUT OF LIMITS PER 747 SRM 56-10-02. REPLACED WINDOW FORGING AND SEALED PER 747 SRM 51 -30-02 AND 51-10-06. 2 L 7 4 4F A20WE 2001050700032 20010507 00032 NM 2001 5 7 ERKR200100094 1 20010425 A 5620 65B04165603 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 MAIN DECK LT BETWEEN STA 1060 AND 1080 BETWEEN S-20L AND S-22L WINDOW FORGING HAS CORROSION FWD BOTTOM CORNER. REMOVED WINDOW FORGING PER 747 SRM 51-30-02, REMOVED CORROSION ON WINDOW FORGING FOUND TO BE OUT OF LIMITS PER 747 SRM 56-20-01. INSTALLED NEW WINDOW FORGING PER 747 SRM 51-30-05 AND 51-30-02. 2 L 7 4 4F A20WE 2001050700033 20010507 00033 EU 2001 5 7 QXEA0100543 1 20010331 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- MINOR CORROSION FOUND UNDER AFT DME ANTENNA. REPAIRED IAW FOKKER SRM 53-01-01. 2 L 7 2 4F RT A20EU 2001050700034 20010507 00034 EU 2001 5 7 QXEA0100544 1 20010406 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- FRAME 13815A HAS MINOR CORROSION BETWEEN STRINGERS 1 AND 74. REPAIRED IAW FOKKER SRM 53-22-04. 2 L 7 2 4F RT A20EU 2001050700035 20010507 00035 EU 2001 5 7 QXEA0100545 1 20010404 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- REAR PRESSURE BULKHEAD FLOORBEAM SUPPORT ANGLE IS CRACKED AT STATION 19275 BL425R. REPAIRED IAW FOKKER SRM 53-24-0 5, 51-31-01 AND 51-32-01. 2 L 7 2 4F RT A20EU 2001050700036 20010507 00036 EU 2001 5 7 QXEA0100546 1 20010403 A 5320 BRACKET FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- REAR PRESSURE BULKHEAD PULLEY REINFORCEMENT BRACKET FORWARD SIDE CRACKED. REPAIRED IAW FOKKER SRM 53-24-04 AND 51- 31-01. 2 L 7 2 4F RT A20EU 2001050700037 20010507 00037 EU 2001 5 7 QXEA0100547 1 20010401 A 5240 CABLE FOKKER F28 F28MK4000 4990810 EU SERVICE DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- SERVICE EMERGENCY DOOR RELEASE CABLES DAMAGED. REPAIRED IAW FOKKER SRM 52-40-01. 2 L 7 2 4F RT A20EU 2001050700038 20010507 00038 EU 2001 5 7 QXEA0100548 1 20010322 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CANNING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- FUSELAGE SKIN OIL CANNED FORWARD OF DORSAL FIN AT STATION 17845-18270 AND STRINGER 34 AND 33 ON ROOF. REPAIRED IAW FOKKER SRM 53-02-02. 2 L 7 2 4F RT A20EU 2001050700039 20010507 00039 EU 2001 5 7 QXEA0100549 1 20010327 A 5240 TRACK FOKKER F28 F28MK4000 4990810 EU SERVICE DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- SERVICE EMERGENCY DOOR FORWARD LOWER TRACK DENTED. REPAIRED IAW HORIZON AIR EA 4-52-444. 2 L 7 2 4F RT A20EU 2001050700040 20010507 00040 EU 2001 5 7 QXEA0100550 1 20010402 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- EXFOLIATING CORROSION ON FRAME SPLICE AT STATION 13353 AND STRINGER 31, FORWARD AND AFT OF FRAME. REPAIRED IAW FOK KER SRM 51-31-01 PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001050700041 20010507 00041 EU 2001 5 7 QXEA0100551 1 20010331 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- EXFOLIATING CORROSION ON FRAME SPLICE AT STATION 13353 AND STRINGER 45, FORWARD AND AFT SIDE OF FRAME. REPAIRED IA W FOKKER SRM 51-10-4 PAGE 9. 2 L 7 2 4F RT A20EU 2001050700042 20010507 00042 EU 2001 5 7 QXEA0100552 1 20010402 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CORROSION ON FORWARD SIDE OF FRAME 11905 LT BETWEEN STRINGERS 28-31. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 AND 53 -01-01. 2 L 7 2 4F RT A20EU 2001050700043 20010507 00043 EU 2001 5 7 QXEA0100553 1 20010324 A 5320 ATTACH ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- ATTACH ANGLE CRACKED FORWARD OF STATION 4900 AT CHANNEL 6 INBOARD FROM SERVICE EMERGENCY DOOR UNDER FORWARD GALLEY. REPAIRED IAW FOKKER SRM 53-11-05 AND 51-32-01. 2 L 7 2 4F RT A20EU 2001050700044 20010507 00044 WP 2001 5 7 ABXA010207 1 20010425 A 3310 53989 RHEOSTAT DOUG DC9 DC933F 302207A WP COCKPIT DEFECTIVE A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 23 932AX 44455 47465 THE CAPTAIN''S MAP LIGHT WAS SMOKING. MAINTENANCE DEFERRED THE MAP LIGHT PER THE DC-9 MEL AND RETURNED THE AIRCRAFT TO SERVICE. ON 04/26/01 MAINTENANCE INSPECTED AND REPLACED THE CAPTAIN''S MAP LIGHT RHEOSTAT IAW DC-9 MM 33-10-00. 2 L 7 2 4F A6WE 2001050700045 20010507 00045 NM 2001 5 7 ERKR200100095 1 20010426 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 MAIN DECK LT FROM STA 1160 TO 1180 AND BETWEEN S-20L AND S-22L WINDOW FORGING HAS CORROSION UNDER FORGING. REMOVED WIND OW FORGING PER 747 SRM 51-30-02 AND REMOVED CORROSION PER 747 SRM 51-10-01. MINIMUM MATERIAL REMOVED. ALODINED AND PRI MED PER 747 SRM 51-10-02 AND SOPM 20-41-02. REINSTALLED WINDOW FORGING PER 747 SRM 51-30-02. 2 L 7 4 4F A20WE 2001050700046 20010507 00046 NM 2001 5 7 ERKR200100096 1 20010426 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 MAIN CABIN LT SIDE BETWEEN STA 1394 AND STA 1416 S-20L AND S-22L HAS CORROSION AT WINDOW FORGING. REMOVED WINDOW FORGIN G PER 747 SRM 51-30-02 AND REMOVED CORROSION PER 747 SRM 51-10-01 AND FOUND TO BE WITHIN ALLOWABLE LIMITS PER 747 SRM 56 -20-01. ALODINED PER 747 SRM 51-10-02 AND PRIMED PER 747 SOPM 20-41-02. INSTALLED WINDOW FORGING PER 747 SRM 51-30-02. 2 L 7 4 4F A20WE 2001050700047 20010507 00047 NE 2001 5 7 NACA2001017 2 20010424 A 7411 10553991 COIL PWA CB3 DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE NR 16 CYLINDER SHORTED A NACA E A ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 AL 03 43872 75 P28737 533294 P28737 FEATHERED NR 2 ENGINE AT 1935 DUE TO BACKFIRING AND RUNNING ROUGH. REPLACED THE NR 16 CYLINDER IGNITION COIL. 2 L 7 4 4R 4 R 6A3 5E8 2001050700048 20010507 00048 NM 2001 5 7 ERKR200100097 1 20010426 A 5620 65B041655 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 MAIN CABIN LT SIDE BETWEEN STA 1438 AND STA 1460 S-20L AND S-22L HAS CORROSION AT WINDOW FORGING LOWER AFT SIDE. REMOVE D WINDOW FORGING PER 747 SRM 51-30-05. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER 747 SRM 51-10-01. REPLACED WIND OW FORGING PER 747 SRM 51-30-05. ALODINED WINDOW FORGING PER 747 SRM 51-10-01 AND PRIMED PER 747 SOPM 20-41-02. 2 L 7 4 4F A20WE 2001050700049 20010507 00049 WP 2001 5 7 DHL2001802005 1 20010425 A 2612 FIRE WARNING DOUG DC8 DC873F 302199F WP COCKPIT FALSE ACTIVATION A DHLA E ENGINE SHUTDOWN N FALSE WARNING AP APPROACH 1 SO 01 802DH 46076 NR 4 ENG FIRE LIGHT AND BELL CAME ON. PERFORMED PHASE ONE ITEMS. FIRE LIGHT WENT OUT. SHORT TEST INDICATED GOOD. INS PECTED NR 4 ENG FIRE LOOPS. NO DEFECTS NOTED. DUE TO HISTORY DEFFERED NR 4 ENG A LOOP FIRE DETECTION PER MEL 26-2-3. DMI 5331. PERFORMED SPEC PROCEDURES LOOP B OPERATIVE. PLACARD INSTALLED. 2 L 7 4 4F RT 4A25 2001050700050 20010507 00050 WP 2001 5 7 DHL2001801004 1 20010422 A 2760 56519772 PULLEY BRACKET DOUG DC8 DC873F 302199F WP RT SPOILER DEFECTIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 801DH 46033 ON POST FLIGHT FOUND A SPOILER ON RT WING EXTENDED AND WILL NOT RETRACT. REMOVED AND REPLACED SPOILER PULLEY BRACKET RT W/W IAW MM 20-16-0. COMPLIED WITH FUNCTIONAL TESTS IAW DC-8 MM 27-60-0, 27-63-0, 32-43-0 WITH NO DEFECTS NOTED. RIG C HECK ACCOMPLISHED PER 27-60-0. 2 L 7 4 4F RT 4A25 2001050700051 20010507 00051 2001 5 7 DHL2001364015 4 20010425 A 2210 AUTOPILOT SYS AIRBUS 300 A300B4203 3930306 EU COCKPIT INOPERATIVE A DHLA K NONE O OTHER UK UNKNOWN 1 SO 01 364DH 0141 NR 2 PITCH TRIM INOP. DEFERRED NR 2 PITCH TRIM PER MEL 22-11-03. TRANSFERRED TO DMI LOG CONTROL 5336. 2 L 7 2 4F RT A35EU 2001050700052 20010507 00052 WP 2001 5 7 DHL2001806610 1 20010304 A 5210 SKIN DOUG DC8 DC873F 302199F WP ENTRY DOOR DEFORMED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - ENTRY DOOR FWD UPPER CORNER DEFORMED FS 60.000. REMOVED FASTENERS IAW SRM 51-1-20D PAGE 21. CUT OUT DEFORMED SKIN IAW EO DHL 010325, ED 2388, EO 2001047. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FILLER AND DOUBLER (ALCLAD 7075 T6 0.050/0.063) IAW EO DHL010325, ED 2388, EO 2001097. CLEANED, TREATED AND PRIMED AND APPLIED (PR C) SEALANT ON REWORKED AREA IAW SRM 51-1-8B, SRM 51-1-15 PAGE 1. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW EO DHL 010325, ED 2388, EO 2001097, SRM 51-1020D PAGE 9. 2 L 7 4 4F RT 4A25 2001050700053 20010507 00053 WP 2001 5 7 DHL2001806611 1 20010328 A 5755 SPOILER DOUG DC8 DC873F 302199F WP RT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - RT WING REMOVAL AND INSTALLATION OF NR 1 GROUND SPOILER DUE TO UPPER SKIN DELAMINATED BETWEEN XW 5.000 AND XW 47.000. REMOVED NR 1 GROUND SPOILER (DELAMINATED) IAW MM 27-61-1 PAGE 201 TO 204. INSTALLED NR 1 GROUND SPOILER AFTER ITS REPAIR MADE IN USA IAW MM 27-61-1 PAGE 202, 203, 204, 205 AND 206. OPS CHECK WILL COMPLY WITH N/R 2635. 2 L 7 4 4F RT 4A25 2001050700054 20010507 00054 NM 2001 5 7 ERKR200100098 1 20010426 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 MAIN CABIN LT SIDE BETWEEN STA 1580 AND STA 1600 S-20L AND S-22L HAS CORROSION AT WINDOW FORGING LOWER AFT SIDE. REMOVE D LIGHT SURFACE CORROSION MINIMUM MATERIAL LOSS PER 747 SRM 51-10-01. ALODINED PER 747 SRM 51-10-02 AND PRIMED PER 747 SOPM 20-41-02. 2 L 7 4 4F A20WE 2001050700055 20010507 00055 EU 2001 5 7 C2XA01BT068 1 20010424 A 2121 EVCTA325AB FAN AEROSP ATR42 ATR42320 8680930 EU FUSELAGE FAULTY A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 93840 20769 271 IAD/EWR---CO3411, CREW REPORTED (IN IAD) THAT ON POST FLIGHT (WALKAROUND) ELECTRICAL FAN SMELL IN FORWARD CABIN. MAINTE NANCE FOUND FAULTY VENT FAN, AIRCRAFT PLACED ON MEL (CIRCUIT BREAKER PULLED AND TAGGED) IAW MEL 21-70-01 PLACARD NUMBER 012782, AIRCRAFT RETURNED TO SERVICE. ARRIVED IN EWR ON CO3486, EWR MAINTENANCE REMOVED AND REPLACED FORWARD VENT FAN I AW ATR42 AMM 21-26-21. OPS CHECKED GOOD, MEL/PLACARD CLEARED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001050700061 20010507 00061 WP 2001 5 7 RRXA10694 1 20010409 A 5720 NUT PLATE DOUG DC8 DC873 302199C WP LT WING DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING MAINTENANCE VSIT FOUND LT WING L/E FUEL TANK ATTACH SCREW TO LONG DAMAGE TO NUT PLATE AT XW-0 TO XW200 (EO), DAMA GE EXCEEDED LIMITATIONS IAW DC-8 SRM. 2 L 7 4 4F RT 4A25 2001050700062 20010507 00062 WP 2001 5 7 RRXA10695 1 20010320 A 5347 SEAT TRACK DOUG DC8 DC873 302199C WP CABIN WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 952-957 AND X-57, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. 2 L 7 4 4F RT 4A25 2001050700063 20010507 00063 WP 2001 5 7 RRXA10696 1 20010320 A 5347 SEAT TRACK DOUG DC8 DC873 302199C WP CABIN WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT RAIL AT STA 972-979 AND X-47.5, DAMAGE EXCEEDED LIMITATIONS IAW DC- 8 SRM. 2 L 7 4 4F RT 4A25 2001050700064 20010507 00064 WP 2001 5 7 RRXA10697 1 20010320 A 5347 SEAT TRACK DOUG DC8 DC873 302199C WP CABIN WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 1125 - 1135 AND X-0, DAMAGE EXCEEDED LIMITATIONS IAW D C-8 SRM. 2 L 7 4 4F RT 4A25 2001050700065 20010507 00065 WP 2001 5 7 RRXA10698 1 20010320 A 5347 SEAT TRACK DOUG DC8 DC873 302199C WP CABIN WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 1123 - 1131 AND X-22.5, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. 2 L 7 4 4F RT 4A25 2001050700066 20010507 00066 WP 2001 5 7 RRXA10699 1 20010320 A 5347 SEAT TRACK DOUG DC8 DC873 302199C WP CABIN WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 1542 - 1546 AND X+22.5, DAMAGE EXCEEDED LIMITATIONS IA W DC-8 SRM. 2 L 7 4 4F RT 4A25 2001050700067 20010507 00067 WP 2001 5 7 RRXA10700 1 20010320 A 5347 SEAT TRACK DOUG DC8 DC873 302199C WP CABIN WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 1568 - 1620 AND X+47, DAMAGE EXCEEDED LIMITATION IAW D C-8 SRM. 2 L 7 4 4F RT 4A25 2001050700068 20010507 00068 WP 2001 5 7 RRXA10701 1 20010320 A 5347 SEAT TRACK DOUG DC8 DC873 302199C WP CABIN WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 1125 - 1135 AND X-47, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. 2 L 7 4 4F RT 4A25 2001050700069 20010507 00069 WP 2001 5 7 RRXA10702 1 20010320 A 5230 DOUBLER DOUG DC8 DC873 302199C WP CARGO DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND CRACK BEYOND STOP DRILL DAMAGE TO B-PIT DOOR AT BOTTOM FWD DOUBLER, DAMAGE EXCEEDED LIM ITATIONS IAW DC-8 SRM. 2 L 7 4 4F RT 4A25 2001050700070 20010507 00070 WP 2001 5 7 RRXA10703 1 20010320 A 5522 SKIN DOUG DC8 DC873 302199C WP ELEVATOR CHAFED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND 8 INCHES WEAR/RUBB SPOT DAMAGE TO LT ELEVATOR AT MID SECTION, DAMAGE EXCEEDED LIMITATIO NS IAW DC-8 SRM. 2 L 7 4 4F RT 4A25 2001050700071 20010507 00071 WP 2001 5 7 RRXA10704 1 20010321 A 5347 SEAT TRACK DOUG DC8 DC873 302199C WP CABIN WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 1390 AND X-47, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SR M. 2 L 7 4 4F RT 4A25 2001050700072 20010507 00072 WP 2001 5 7 RRXA10705 1 20010321 A 5347 SEAT TRACK DOUG DC8 DC873 302199C WP CABIN WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 1402 - 1412 AND X-47, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. 2 L 7 4 4F RT 4A25 2001050700073 20010507 00073 WP 2001 5 7 RRXA10706 1 20010321 A 5347 SEAT TRACK DOUG DC8 DC873 302199C WP CABIN WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 1540 - 1560 AND X=0, DAMAGE EXCEEDED LIMITATIONS IAW D C-8 SRM. 2 L 7 4 4F RT 4A25 2001050700074 20010507 00074 WP 2001 5 7 RRXA10707 1 20010321 A 5347 SEAT TRACK DOUG DC8 DC873 302199C WP CABIN WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACKS AT STA 930 - 980 AND X+47.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. 2 L 7 4 4F RT 4A25 2001050700075 20010507 00075 WP 2001 5 7 RRXA10708 1 20010321 A 5347 SEAT TRACK DOUG DC8 DC873 302199C WP CABIN WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 970 - 978 AND X+23, DAMAGE EXCEEDED LIMITATIONS IAW DC -8 SRM. 2 L 7 4 4F RT 4A25 2001050700076 20010507 00076 WP 2001 5 7 RRXA10709 1 20010319 A 5321 FLOOR PANEL DOUG DC8 DC873 302199C WP CARGO BAY CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO MAIN CARGO COMP FLOOR PANEL AT STA 505 - 506 AND X-1.5, DAMAGE EXCE EDED LIMITATIONS IAW DC-8 SRM. 2 L 7 4 4F RT 4A25 2001050700077 20010507 00077 WP 2001 5 7 RRXA10710 1 20010319 A 5347 SEAT TRACK DOUG DC8 DC873 302199C WP CABIN WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 765 - 779 AND X=0, DAMAGE EXCEEDED LIMITATIONS IAW DC- 8 SRM. 2 L 7 4 4F RT 4A25 2001050700078 20010507 00078 WP 2001 5 7 RRXA10711 1 20010322 A 5347 SEAT TRACK DOUG DC8 DC873 302199C WP COCKPIT WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT F/E''S LT SIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. 2 L 7 4 4F RT 4A25 2001050700079 20010507 00079 WP 2001 5 7 RRXA10712 1 20010322 A 5347 SEAT TRACK DOUG DC8 DC873 302199C WP COCKPIT DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND ELONGATED HOLE DAMAGE TO SEAT TRACK LOCK HOLE AT F/E RIGHT SEAT DAMAGE EXCEEDED LIMITAT IONS IAW DC-8 SRM. 2 L 7 4 4F RT 4A25 2001050700080 20010507 00080 WP 2001 5 7 RRXA10713 1 20010322 A 5347 SEAT TRACK DOUG DC8 DC873 302199C WP CABIN WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 1030 - 1050 AND X+23, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. 2 L 7 4 4F RT 4A25 2001050700081 20010507 00081 WP 2001 5 7 RRXA10714 1 20010322 A 5347 SEAT TRACK DOUG DC8 DC873 302199C WP CABIN WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 1120 - 1140 AND X+23, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. 2 L 7 4 4F RT 4A25 2001050700082 20010507 00082 WP 2001 5 7 RRXA10715 1 20010322 A 5347 SEAT TRACK DOUG DC8 DC873 302199C WP CABIN WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 520 - 540 AND X+47, DAMAGE EXCEEDED LIMITATIONS IAW DC -8 SRM. 2 L 7 4 4F RT 4A25 2001050700083 20010507 00083 WP 2001 5 7 RRXA10716 1 20010322 A 5347 SEAT TRACK DOUG DC8 DC873 302199C WP CABIN WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 767 - 780 AND X+47, DAMAGE EXCEEDED LIMITATIONS IAW DC -8 SRM. 2 L 7 4 4F RT 4A25 2001050700084 20010507 00084 WP 2001 5 7 RRXA10717 1 20010322 A 5347 SEAT TRACK DOUG DC8 DC873 302199C WP CABIN WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 767 - 780 AND X+23, DAMAGE EXCEEDED LIMITATIONS IAW DC -8 SRM. 2 L 7 4 4F RT 4A25 2001050700085 20010507 00085 WP 2001 5 7 RRXA10718 1 20010322 A 5315 FLOORBEAM DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO MAIN CARGO COMP FLOOR BEAM AT STA 200 LT OF L22, DAMAGE EXCEEDED LIMITA TIONS IAW DC-8 SRM. 2 L 7 4 4F RT 4A25 2001050700086 20010507 00086 WP 2001 5 7 RRXA10719 1 20010328 A 5347 SEAT TRACK DOUG DC8 DC873 302199C WP CABIN DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND BROKEN LOBE DAMAGE TO SEAT TRACKS AT STA 640 AND X+47, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. 2 L 7 4 4F RT 4A25 2001050700087 20010507 00087 WP 2001 5 7 RRXA10720 1 20010328 A 5347 SEAT TRACK DOUG DC8 DC873 302199C WP CABIN DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND BROKEN LOBE DAMAGE TO SEAT TRACK AT STA 120 AND X+23, DAMAGE EXCEEDED LIMITATIONS IAW D C-8 SRM. 2 L 7 4 4F RT 4A25 2001050700088 20010507 00088 WP 2001 5 7 RRXA10721 1 20010326 A 5320 STIFFENER DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND CRACKED DAMAGE TO W/W VERT STIFFENER AT STA 940 AND WING ROOT, DAMAGE EXCEEDED LIMITATI ONS IAW DC-8 SRM. 2 L 7 4 4F RT 4A25 2001050700089 20010507 00089 WP 2001 5 7 RRXA10722 1 20010326 A 5752 SKIN DOUG DC8 DC873 302199C WP AILERON TAB DENTED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND DENT DAMAGE TO RT AILERON AT O/B CONTROL TAB, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. 2 L 7 4 4F RT 4A25 2001050700090 20010507 00090 WP 2001 5 7 RRXA10723 1 20010326 A 5347 SEAT TRACK DOUG DC8 DC873 302199C WP CABIN WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 1120 - 1140 AND X+47.5, DAMAGE EXCEEDED LIMITATIONS IA W DC-8 SRM. 2 L 7 4 4F RT 4A25 2001050700091 20010507 00091 WP 2001 5 7 RRXA10724 1 20010417 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SKIN AT STA 70 - 110 AND BELOW STR 31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. 2 L 7 4 4F RT 4A25 2001050700092 20010507 00092 WP 2001 5 7 RRXA10725 1 20010418 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 32R AT STA 100, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. 2 L 7 4 4F RT 4A25 2001050700093 20010507 00093 WP 2001 5 7 RRXA10726 1 20010405 A 5713 STRINGER DOUG DC8 DC871F 302199D WP RT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997GE 45667 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO STR 63 RT WING AT STA XFS 463, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM . REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-2-2 FIG 3D. 2 L 7 4 4F RT 4A25 2001050700094 20010507 00094 WP 2001 5 7 RRXA10727 1 20010405 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997GE 45667 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO RT WING SKIN AT STA XFS 463 AND STR 63, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 EO 01-195. 2 L 7 4 4F RT 4A25 2001050700095 20010507 00095 WP 2001 5 7 RRXA10728 1 20010409 A 5753 WEB DOUG DC8 DC871F 302199D WP FLAP CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996GE 45996 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LEFT WING I/B FLAP WEB AT XCW64 (EO), DAMAGE EXCEEDED LIMITATIONS IAW D C-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 EO 01-104. 2 L 7 4 4F RT 4A25 2001050700096 20010507 00096 CE 2001 5 7 C2XA01CL087 1 20010417 A 2612 24412886 FIRE LOOP BEECH 1900 1900D 1154162 CE RT ENGINE BROKEN A C2XA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 27 87552 UE216 CLE FLIGHT 3048 THE CREW REPORTED THE NR 2 ENGINE FIRE T-HANDLE LIGHTS FLICKERED ON WHILE TAXIING. MAINTENANCE REPLACED THE RIGHT ENGINE FORWARD FIRE LOOP. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT A24CE 2001050700097 20010507 00097 NM 2001 5 7 ERKR200100099 1 20010426 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 UPPER DECK WINDOW FORGING 2L HAS CORROSION PROTRUDING BOTTOM EDGE STA 620 TO STA 640 LEFT SIDE AT S-10L TOP SIDE. REMOV ED WINDOW FORGING PER 747 SRM 51-30-02. REMOVED CORROSION ON FORGING PER 747 SRM 51-10-01. FORGING IS WITHIN LIMITS PE R ECRA 3203-53-047-2. REINSTALLED WINDOW FORGING PER 747 SRM 51-30-02 AND ECRA 3203-53-047-2. 2 L 7 4 4F A20WE 2001050700098 20010507 00098 SO 2001 5 7 LR7A01030 1 20010425 A 5230 SKIN LKHEED 382 382G 526414U SO CARGO DOOR DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 5025 DURING SCHEDULED B2 INSPECTION CARRY OVER ITEM 01129 DUE, REF LOCKHEED SES GLD-1720 DISPOSITION DATED 03/26/01. AFT CAR GO DOOR SKIN DENTED AT FS 1010, BL 0. REPAIRED IAW SRM SMP 583-51-140-12. 2 H 7 4 4T A1SO 2001050700099 20010507 00099 WP 2001 5 7 MWEA010656 1 20010426 A 5312 5910130105 BULKHEAD DOUG DC9 DC915 3022036 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 LEFT SIDE AFT PRESSURE BULKHEAD SIDE STATION Z=34, 6 INCHES OUTBOARD OF DOOR CUTOUT FINGER DOUBLER IS CRACKED AROUND Z-R IVETS. ALSO AT STATION 40 FINGER DOUBLER HAS CRACK AROUND 1 RIVET. FABRICATED AND INSTALLED FINGER DOUBLER. 2 L 7 2 4F A6WE 2001050700100 20010507 00100 EA 2001 5 7 COMA0160363 1 20010426 A 5411 RIB CNDAIR CL600 CL6002B19 EA PYLON CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 933CA 16868 7040 THE LT PYLON AT FS 605 IS CRACKED AT THE OUTBOARD LOWER FLANGE. REPAIRED DAMAGED AREA TO THE LT PYLON RIB AT FS 605 AT THE OUTBOARD LOWER FLANGE IAW WVAC EO 601R-54-2401A. 2 L 7 2 4F RT A21EA 2001050700101 20010507 00101 WP 2001 5 7 CALA0100419 1 20010425 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 LEFT FUSELAGE SKIN AFT OF GROUND FLOOD LIGHT CREASED. REPAIRED FUSELAGE SKIN PER SRM 53-04 FIG 12B. 2 L 7 2 4F A6WE 2001050700102 20010507 00102 WP 2001 5 7 CALA0100420 1 20010425 A 5321 4017T40001BB9 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 MAIN CABIN FLOOR PANEL FS 1250 - 1309 CENTER HAS TORN INSERTS AND DAMAGED CORNERS. FABRICATED NEW FLOOR PANEL PER EC/RA 5320-01265. MATERIAL USED 4017T4000001BB-9. 2 L 7 2 4F A6WE 2001050700103 20010507 00103 WP 2001 5 7 CALA0100421 1 20010425 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 SHEAR TIE CRACKED AT STATION 1309 LGL 13 AND 14L. STOP DRILLED CRACK. FABRICATED AND INSTALLED DOUBLER PER EA 9-5314-2 -A0872 AND SRM 51-30-5. 2 L 7 2 4F A6WE 2001050700104 20010507 00104 WP 2001 5 7 CALA0100422 1 20010425 A 5320 FITTING DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 AFT CARGO DOOR CUTOUT AREA AFT LOWER CORNER FITTING CORRODED. REMOVED FITTING FROM CORNER. FABRICATED AND INSTALLED FI TTING PER SRM 51-30-5. 2 L 7 2 4F A6WE 2001050700105 20010507 00105 WP 2001 5 7 CALA0100423 1 20010425 A 5230 SUPPORT DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 FORWARD CARGO DOOR AFT LOWER INNER STIFFENER UPPER SUPPORT IS CRACKED. REMOVED DAMAGED STIFFENER. FABRICATED AND INSTA LLED NEW STIFFENER PER SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-5. 2 L 7 2 4F A6WE 2001050700106 20010507 00106 2001 5 7 DHL2001742005 4 20010425 A 2210 LIGHT BOEING 727 727225 1384077 NM AUTOPILOT INOPERATIVE A DHLA K NONE O OTHER CR CRUISE 1 SO 01 742DH 21290 AUTOPILOT HEADING SELECT LIGHT INOPERATIVE. WORD HDG SEL LIGHTS. RELAMPED HEADING SELECT LIGHT SEGMENT. OP''S CHECK G OOD PER MM 22-00. 2 L 7 3 4F A3WE 2001050700107 20010507 00107 2001 5 7 DHL2001367002 4 20010405 A 2212 AUTOPILOT SYS AIRBUS 300 A300B4203 3930306 EU COCKPIT MALFUNCTIONED A DHLA K NONE O OTHER CR CRUISE 1 SO 01 367DH MSN265 AT FL 290 NR 2 AUTOPILOT LEVELS OFF 200 FT HIGH THEN CONTINUES TO DRIFT HIGHER. NR 1 A/P NORMAL. PERFORMED A/P COMPLEM ENTARY TEST AND SYSTEM OP TEST ON NR 2 A/P. SYSTEM CHECKS OK PER MM 22-12-01. NO FAULT CODES NOTED. 2 L 7 2 4F RT A35EU 2001050700108 20010507 00108 WP 2001 5 7 DHL2001806612 1 20010403 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - AFT PAX ENTRY DOOR LWR AFT JAMB CORNER SHOWS 1 CRACK 1.5 INCH STA 1660.000 BETWEEN L-20 LT AND L-21 LT. CUT O UT DAMAGED AREA, FABRICATED FILLER AND DOUBLER (ALCLAD 7075 T6 0.090/ 0.125) IAW SRM 53-2-0 PAGE 123, 124, FIG 18. CLE ANED, TREATED, AND PRIMED IAW SRM 51-1-8B. APPLIED (PRC0 SEALENT IAW SRM 51-1-15 PAGE 1. INSTALLED FILLER AND DOUBLER IAW SRM 53-2-0 PAGE 123; 124. 2 L 7 4 4F RT 4A25 2001050700109 20010507 00109 NM 2001 5 7 ERKR200100100 1 20010426 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 UPPER DECK WINDOW FORGING 2R HAS CORROSION PROTRUDING AROUND TOP EDGE STA 620 TO 640 RIGHT SIDE AT S-8R BOTTOM SIDE. RE MOVED WINDOW FORGING PER 747 SRM 51-30-02, REMOVED CORROSION ON FORGING PER 747 SRM 51-10-01. FORGING IS WITHIN LIMITS PER ECRA 3203-53-047-2. REINSTALLED WINDOW FORGING PER 747 SRM 51-30-02 AND ECRA 3203-53-047-2. 2 L 7 4 4F A20WE 2001050700110 20010507 00110 NM 2001 5 7 AWXA0001646 1 20010426 A 5330 143N3320 DOUBLER BOEING 757 7572G7 1384963 NM FUSELAGE DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 909AW 24522 DENT IN PREVIOUS REPAIR AT STA 619, 5 INCHES ABOVE STR 17L ON FUSELAGE EXTERIOR. REMOVED EXISTING REPAIR DOUBLER; FABBE D AND INSTALLED REPAIR DOUBLER IAW AWA ER 19-5331-01104-SS1. 2 L 7 2 4F RT A2NM 2001050700111 20010507 00111 NM 2001 5 7 AWXA0001647 1 20010426 A 5320 6547977509 WEB BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 23258 LT CUSP WEB HAS CRACK APPROX 2 INCHES LONG AT FS 638 STR 17L. CUT OUT DAMAGED AREA; INSTALLED FILLER AND DOUBLER IAW B7 37-300 SRM 51-70-13 PG 1-3. 2 L 7 2 4F RT A16WE 2001050700112 20010507 00112 NM 2001 5 7 AWXA0001648 1 20010426 A 5230 6547977509 WEB BOEING 737 737301 1384611 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 23258 FWD CARGO DOOR - CRACK IN LWR WEB INSIDE LWR AFT ACCESS HOLE. CUT OUT DAMAGED AREA; INSTALLED FILLER AND DOUBLER IAW AW A ER 03-5231-01106-TB2. 2 L 7 2 4F RT A16WE 2001050700113 20010507 00113 NM 2001 5 7 AWXA0001649 1 20010426 A 5312 65163007 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CANNING A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 169AW 23630 FS 178 OIL CANNING AT WL 188-207 LBL 5 TO RBL 5. LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW B737-300 SRM 53-10-0 8 PG 1-11. 2 L 7 2 4F RT A16WE 2001050700114 20010507 00114 NM 2001 5 7 AWXA0001651 1 20010426 A 5320 6545803 WEB BOEING 737 73733A 1384673 NM FUSELAGE PUNCTURED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 169AW 23630 PUNCTURE IN VERT WEB RBL 44 FS 311.CUT OUT DAMAGED AREA; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW SRM 51-70-11 PG 1 AND 51-20-01 PG 1 AND 51-40-02 PG 3 & 4. 2 L 7 2 4F RT A16WE 2001050700115 20010507 00115 NM 2001 5 7 AWXA0001652 1 20010426 A 5312 65163007 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 169AW 23630 FS 178 BLKHD HAS 1.5 INCH CRACK AT WL 200.3 LBL 5. CUT OUT DAMAGD AREA; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER A ND FILLER IAW SRM 53-10-08 TR 53-15 PG 1-11. 2 L 7 2 4F RT A16WE 2001050700116 20010507 00116 NM 2001 5 7 AWXA0001653 1 20010426 A 5312 65163007 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 169AW 23630 FS 178 BLKHD HAS 1 INCH CRACK AT WL 206 RBL .6-1.8. CUT OUT DAMAGED AREA; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW SRM 53-10-08 TR 53-15 PG 1-11. 2 L 7 2 4F RT A16WE 2001050700117 20010507 00117 NM 2001 5 7 AWXA0001654 1 20010426 A 5312 65163007 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 169AW 23630 FS 178.5 BLKHD CRACK AT WL 188 LBL 5.7. CUT OUT DAMAGED AREA; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW AWA ER 03-5313-01109-TB1. 2 L 7 2 4F RT A16WE 2001050700118 20010507 00118 EU 2001 5 7 QXEA0100630 1 20010425 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU EXIT SIGN FAULTY A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487US 11238 PDX-NUMEROUS EMERGENCY EXIT LIGHTS IN FORWARD CABIN AND GALLEY ARE INOPERATION. RELAMPED AND REPLACED EXIT SIGN CIRCUIT BOARDS IN FORWARD CABIN AND GALLEY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001050700119 20010507 00119 EU 2001 5 7 QXEA0100631 1 20010422 A 5210 DOOR FOKKER F28 F28MK4000 4990810 EU PAX DOOR OUT OF ADJ A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX-AIRSTAIR DOOR WILL NOT PUSH OPEN FROM INSIDE PASSENGER CABIN WITH DOOR HANDLE IN ALTERNATE POSITION. INSPECTED MAIN CABIN DOOR ACTUATING MECHANISM FORWARD FRICTION MECHANISM EXCESSIVELY TIGHT. ADJUSTED AND TESTED. ALTERNATE MODE CHEC KS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001050700120 20010507 00120 NE 2001 5 7 01FDEA00301 2 20010425 A 7230 COMPRESSOR DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE NR 1 ENGINE STALLED A FDEA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 SO 25 311FE 46871 NR 1 ENG SHUTDOWN IN FLT DUE TO COMPRESSOR STALLS DURING PWR REDUCTIONS. 2 L 7 3 4F 4 F RT A22WE E23EA 2001050700121 20010507 00121 EU 2001 5 7 01FDEA00302 1 20010425 A 3230 LANDING GEAR AIRBUS 300 A300F4605R 3930327 EU NLG MALFUNCTIONED A FDEA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 25 655FE 742 ON FINAL APPR NOSE GEAR DID NOT SHOW DOWN ON SYS 1 & 2, SYS 3 IND GEAR DOWN. AFT GO AROUND GEAR RECYCLED AND ALL ID WER E GREEN. 2 L 7 2 4F RT A35EU 2001050700122 20010507 00122 EU 2001 5 7 01FDEA00303 1 20010426 A 7830 WARNING LIGHT AIRBUS 310 A310222 3930315 EU COCKPIT ILLUMINATED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 450FE 162 NR 2 REVERSE UNLOCK LIGHT CAME ON AT T/O. 2 L 7 2 4F RT A35EU 2001070200026 20010702 00026 NM 2001 7 2 01FDEA00300 1 20010405 A 3260 TARGET DOUG MD11 MD11F 3023600 NM NLG UNSERVICEABLE A FDEA K NONE N FALSE WARNING AP APPROACH 1 SO 25 592FE 48550 ON APPROACH NOSE GEAR UNSAFE ON EXT. Removed and replaced TARGET Per MM 32-61-17-4. RESECURED RIVETS PER SMP. CLEAN A LL TARGETS and SENSORS PRECAUTIONARY. AC OK FOR SERVICE. 2 L 7 3 4F RT A22WE 2001050700123 20010507 00123 WP 2001 5 7 0101479855 1 20010421 A 3230 59516395001 BUNGEE CYLINDER DOUG DC9 DC951 3022051 WP NLG MALFUNCTIONED A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 764NC 47717 DURING APPROACH INTO JAX, THE NOSE LANDING GEAR DID NOT EXTEND NORMALLY. COMPLIED WITH COM PROCEDURES AND NOSE GEAR EXT ENDED USING ALTERNATE (MANUAL) METHOD. AN UNEVENTFUL LANDING WAS MADE. MAINTENANCE REPLACED THE NOSE LANDING GEAR BUNG EE CYLINDER AND RESHIMMED THE PROXIMITY SENSOR. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2001050700124 20010507 00124 WP 2001 5 7 0101489606 1 20010419 A 3231 ROLLER DOUG DC9 DC932 3022066 WP RT MLG DOOR LOOSE A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 606NW 47225 DURING APPROACH INTO MSP, THE LANDING GEAR INDICATED DOWN AND LOCKED. THEN THE RIGHT MAIN GEAR INTERMITTENTLY INDICATED BOTH DOWN TO UNSAFE WITH ACCOMPANYING WARNING HORN. GROUND OBSERVER REPORTED THE RIGHT MAIN GEAR AS NOT DOWN AND LOCKE D WHEN CREW HAD A GREEN SAFE LIGHT. COM PROCEDURES AND CYCLING OF GEAR RESULTED IN A DOWN AND LOCKED CONDITION BOTH IND ICATED AND VISUALLY. LANDING WAS NORMAL. MAINTENANCE FOUND THE RIGHT MAIN GEAR DOOR ROLLER LOOSE. ADJUSTED AND SECURE D ROLLER. OPERATIONAL CHECK NORMAL AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001050700125 20010507 00125 EU 2001 5 7 0101493247 1 20010425 A 2916 RESERVOIR AIRBUS 320 A320212 EU HYD SYSTEM LACK OF LUBE A NWAA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 01 347NW 408 DURING APPROACH, RECEIVED HYD G RSVR LO LVL MESSAGE. PERFORMED COM PROCEDURE, GRAVITY EXTENDED LANDING GEAR, AND LANDED WITHOUT INCIDENT. MAINTENANCE RESERVICED THE GREEN HYDRAULIC SYSTEM. LEAK AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A28NM 2001050700126 20010507 00126 WP 2001 5 7 0101501159 1 20010418 A 2170 COALESCER BAG DOUG DC10 DC1040 3023508 WP A/C BAY CONTAMINATED A NWAA A UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 159US 46768 DURING TAXI OUT, LAV-C SMOKE ALARM SOUNDED ACCOMPANIED BY AN OILY ODOR IN CABIN. STARTED REMAINING ENGINE AND RAN ALL T HREE PACKS. ODOR DISSIPATED AND FLIGHT DEPARTED. DURING CLIMB ODOR RETURNED AND REMAINED BETWEEN DOOR 2 AND 3. RETURN ED TO SEA AND LANDED WITHOUT INCIDENT. MAINTENANCE DEFERRED THE NR 3 PACK AND REPLACED NR 1 AND NR 2 COALESCERS. OPERA TIONAL CHECK NORMAL. 2 L 7 3 4F A22WE 2001050700127 20010507 00127 WP 2001 5 7 0101511233 1 20010422 A 2742 CASE DOUG DC10 DC1030 3023501 WP RT STAB MOTOR SPLIT A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 233NW 69252 29652 46580 DURING CLIMBOUT OF LGW, NR 3 HYDRAULIC SYSTEM ELEVATOR OFF LIGHT ILLUMINATED. FOLLOWED COM PROCEDURES AND RETURNED TO L GW LANDING WITHOUT INCIDENT. FOUND RIGHT STABILIZER DRIVE MOTOR CASE SPLIT. REPLACED MOTOR AND FILTERS AND SERVICED NR 3 HYDRAULIC SYSTEM. OPERATIONAL CHECK NORMAL. 2 L 7 3 4F A22WE 2001050700128 20010507 00128 NM 2001 5 7 0101526626 1 20010417 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 626US 21708 DURING LINE CHECK, MAINTENANCE FOUND ZONE-D EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. REPLACED ZONE-D BATTERY PACK. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F A20WE 2001050700129 20010507 00129 EU 2001 5 7 C2XA01BT069 1 20010427 A 3350 LP1670 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14830 184 BTV---CO2930, DURING 2A INSPECTION MAINTENANCE FOUND EMERGENCY LIGHT ON FLOOR INOPERATIVE AT SEAT 6B. REMOVED AND REPLA CED EMERGENCY LIGHT BULB AT FLOOR LIGHT (6B). OPS CHECKED GOOD IAW ATR42 STANDARD PRACTICES. 2 H 7 2 4T RT A53EU 2001050700130 20010507 00130 EU 2001 5 7 C2XA01BT070 1 20010427 A 3350 3011210 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14830 184 BTV---CO2930, DURING 2A INSPECTION, MAINTENANCE FOUND PASSENGER DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED PASSENGER DOOR EMERGENCY LIGHT ASSY IAW ATR42 JIC 33-51-24. OPS CHECKED GOOD. 2 H 7 2 4T RT A53EU 2001050700131 20010507 00131 EU 2001 5 7 C2XA01CL088 1 20010424 A 3397 NSA935041BE20 WIRE AEROSP ATR42 ATR42320 8680930 EU CABIN BROKEN A C2XA K NONE O OTHER UK UNKNOWN 1 SW 27 14821 160 CLE FLIGHT 3109 THE CREW REPORTED EMERGENCY LIGHTS IN CABIN ILLUMINATE WITH MAIN CABIN DOOR OPEN. MAINTENANCE REPARIED WIRE BEHIND FLIGHT ATTENDANTS CONTROL PANEL. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A53EU 2001050700132 20010507 00132 NM 2001 5 7 CALA0100424 1 20010426 A 5210 ARM BOEING 737 7373T0 1384582 NM L1 DOOR OUT OF ADJ A CALA K NONE O OTHER NR NOT REPORTED 1 SW 09 17329 23459 L1 DOOR WILL NOT CLOSE. ADJUSTED L1 DOOR GUIDE ARM. OPS CHECK OK. 2 L 7 2 4F RT A16WE 2001050700133 20010507 00133 WP 2001 5 7 CALA0100425 1 20010427 A 5510 K55B2216 BEARING DOUG DC9 DC982 3022082 WP HORIZ STAB WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 RIGHT HORIZONTAL STAB SUPPORT BEARING HAS EXCESSIVE PLAY AND BOLT CORRODED. REMOVED HORIZONTAL STAB, REMOVED AND REPLAC ED STAB ATTACH PLATE BUSHINGS AND BEARINGS. REMOVED AND REPLACED HINGE PLATES PER 55-10-00 AND CARD 08-5530-1-0006. 2 L 7 2 4F A6WE 2001050700134 20010507 00134 NM 2001 5 7 CALA0100426 1 20010427 A 5210 SKIN BOEING 757 757224 1384958 NM L1 DOOR DENTED A CALA K NONE O OTHER TX TAXI/GRND HDL 1 SW 09 67134 29283 RAMP REPORTED DENT IN L1 DOOR (2 INCHES X 3 INCHES). REPAIRED PER SRM 53-00-01. 2 L 7 2 4F RT A2NM 2001050700135 20010507 00135 NM 2001 5 7 CALA0100427 1 20010425 A 2424 766300E GCU BOEING 767 767424ER NM RT ENGINE FAILED A CALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 09 59053 2074 271 29448 RIGHT GENERATOR CONTROL OFF LIGHT CAME ON IN FLIGHT. STARTED APU BUT APU GENERATOR OFF LIGHT CAME ON. REPLACED RIGHT G ENERATOR CONTROL UNIT. 2 L 7 2 4F RT A1NM 2001050700136 20010507 00136 2001 5 7 RAIA00104020 4 20010426 A 3425 7003360948 COMPUTER JETAIR JETSTM JETSTM4101 1500501 EU AVIONICS BAY FAILED A RAIA D RETURN TO BLOCK I FLT. ATTITUDE INST. TX TAXI/GRND HDL 1 CE 03 556HK 11694 1349 41073 5407-RIC- FIRST OFFICERS (RIGHT) ATTITUDE HEADING REFERENCE SYSTEM (AHRS) FAILED DURING TAXI. MAINTENANCE INSPECTED AND REPLACED RIGHT AHRS COMPUTER. 2 L 7 2 4T RT A41NM 2001050700137 20010507 00137 SO 2001 5 7 C2XA01CL089 1 20010424 A 2530 CBC16707 RECEPTACLE EMB 135 EMB135ER 3260203 SO GALLEY BURNED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 14508 145220 YYZ FLIGHT 3898 THE CREW REPORTED A BURNING SMELL FROM THE LEFT COFFEE JUG. MAINTENANCE REPLACED THE LEFT COFFEE JUG RE CEPTACLE CONNECTOR. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001050700138 20010507 00138 SO 2001 5 7 C2XA01IA224 1 20010425 A 5320 14522226003 STRAP EMB 145 EMB145LR SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13949 145057 IAH - DURING C-CHECK INSPECTION, THE CENTER BUTT STRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 59 AND 60. MAINTENANCE R EMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IN ACCORDANCE WITH E,B-145 SRM 51-40-02, AND THE AIRCRAFT WAS APP ROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001050700139 20010507 00139 SO 2001 5 7 C2XA01IA225 1 20010425 A 3350 20131A BATTERY PACK EMB 145 EMB145LR SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13949 145057 IAH - DURING C-CHECK INSPECTION, THE BOTH OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK IN ACCORDANCE WITH EMB-145 M/M 33-50-00-710-001-A00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001050700140 20010507 00140 SO 2001 5 7 C2XA01IA228 1 20010425 A 3350 3025103 LIGHT EMB 145 EMB145LR SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13949 145057 IAH - DURING C-CHECK INSPECTION, BOTH OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BOTH LIGHT ASSEMBLIES, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001050700141 20010507 00141 SO 2001 5 7 C2XA01IA226 1 20010425 A 3350 3025103 LIGHT EMB 145 EMB145LR SO EXTERIOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13949 145057 IAH - DURING C-CHECK INSPECTION, THE FORWARD RIGHT HAND EXTERNAL EMERGENCY EXIT LIGHT WAS FOUND TO BE CORRODED. MAINTEN ANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001050700142 20010507 00142 SO 2001 5 7 C2XA01IA227 1 20010425 A 3350 3025103 LIGHT EMB 145 EMB145LR SO EXTERIOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13949 145057 IAH - DURING C-CHECK INSPECTION, THE FORWARD LEFT HAND EXTERNAL EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINT ENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001050700143 20010507 00143 SO 2001 5 7 C2XA01TY087 1 20010423 A 5320 14521718003 ANGLE EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16502 145166 TYS DURING A SCHEDULED INSPECTION THE LEFT OMEGA BEAM AFT RAMP ANGLE FORWARD OF FRAME 20 WAS FOUND CORRODED. MAINTENAN CE REMOVED AND REPLACED THE RAMP ANGLE IAW EMB-135 SRM-51-30-01, REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001050700144 20010507 00144 SO 2001 5 7 C2XA01TY088 1 20010424 A 5315 14521700001 FLOORBEAM EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16502 145166 TYS DURING A SCHEDULED INSPECTION THE LEFT HAND OMEGA BEAM AFT OF FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE ACCOM PLISHED A SPLICE REPAIR IAW EMB-135 SRM-53-21-10, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPL ETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001050700145 20010507 00145 WP 2001 5 7 IXXA0100022 1 20010426 A 2612 898464 SENSING ELEMENT DOUG DC8 DC871F 302199D WP NR 2 ENGINE SHORTED A IXXA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 11 827BX 81644 176 45971 EN ROUTE FROM TOL TO LAX, THE NUMBER TWO ENGINE FIRE WARNING SHORT CIRCUIT LIGHT ILLUMINATED INTERMITTENTLY. THE FLIGHT CREW SECURED THE ENGINE FOLLOWING COMPANY PROCEDURES AND RETURNED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPEC TED THE ENGINE FIRE WARNING SYSTEM WHICH REVEALED A SHORTED FIRE SENSING ELEMENT. MAINTENANCE REPLACED THE SENSING ELEM ENT AND PERFORMED A SUCCESSFUL OPERATIONAL TEST IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2001050700146 20010507 00146 SO 2001 5 7 C2XA01TY089 1 20010425 A 5320 14521721005 PLATE EMB 135 EMB135ER 3260203 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16502 145166 TYS DURING A SCHEDULED INSPECTION THE FORWARD DIGITAL PLATE JUST AFT OF FLIGHT DECK WAS FOUND TO BE CORRODED. MAINTENA NCE ACCOMPLISHED A SLICE REPAIR IAW EMB-GST-1266/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON CO MPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001050700147 20010507 00147 SO 2001 5 7 C2XA01TY090 1 20010425 A 5210 14533994401 BRACKET EMB 135 EMB135ER 3260203 SO PAX DOOR CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16502 145166 TYS DURING A SCHEDULED INSPECTION THE MAIN CABIN DOOR, HANDLE BRACKET WAS FOUND TO BE CHAFED. MAINTENANCE REPAIRED THE DAMAGED AREA IAW EMB-GST-1405/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPEC TION. 2 L 7 2 4F RT T00011AT 2001050700148 20010507 00148 NM 2001 5 7 F3LA200100056 1 20010423 A 5751 6546454504 AILERON BOEING 737 7372L9 1384497 NM RT WING DELAMINATED A F3LA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 NM 03 271FL 57 22734 PRIOR TO DEPARTURE, MAINTENANCE REPORTED OTBD SIDE OF RT AILERON DELAMINATED. REPLACED AILERONS IN LT AND RT POSITIONS PER MM 27-11-11, RIGGED AILERONS, AND PERFORMED OPERATIONAL CHECK PER MM 27-11-11. 2 L 7 2 4F RT A16WE 2001050700149 20010507 00149 NM 2001 5 7 F3LA200100057 1 20010426 A 5315 TEE CHORD BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3498 23177 DURING C-6 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM UPPER TEE CHORD AT STA 1016, LBL 33. CLEANED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-51. FABRICATED AND INSTALLED REPAIR PER SRM 53-00-51, 51-40-02 AND SOPM 20-41- 02. 2 L 7 2 4F RT A16WE 2001050700150 20010507 00150 SO 2001 5 7 C2XA01TY091 1 20010426 A 2740 3622001013 ACTUATOR EMB 145 EMB145 SO HORIZ STAB INOPERATIVE A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 27 29917 16 16 145414 ORF FLIGHT 3365. PILOT REPORTED THAT EN ROUTE TO ORF THE AUTO TRIM ALONG WITH THE PITCH TRIM NR 1 FAILED. FIFTEEN MIN UTES LATER THE BACK-UP TRIM SYSTEM NR 2 FAILED AND THE SYSTEM STUCK AT +1. THE CREW ACCOMPLISHED A EMERGENCY LANDING WI THOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE SYSTEM AND FOUND THE HORIZONTAL STABILIZER ACTUATOR INOPERATIVE. THE ACTUATOR WAS REMOVED AND REPLACED IAW EMB-145 MM 27-40-02, ALL OPERATIONAL AND LEAK CHECKS WERE SATISFCATORY. THE AIRC RAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001050700151 20010507 00151 WP 2001 5 7 ZW0A0100803 1 20010423 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT IN FWD CABIN FOUND CORROSION ON FLOOR SUPPORT AT STA 200, FROM RBL 9 INCHES THRU RBL 46 INCHES. FA BRICATED NEW FLOOR SUPPORT PER DRAWING 9936534. APPLIED ALODINE PER SRM 51-10-3 PAGE 18. PRIMED AND TOP COAT PER SRM 5 1-10-3, PAGE 16. RE-INSTALLED NEW FLOOR SUPPORT PER SRM 51-30 AND SRM 5-10-4, AT STA 200, FROM RBL 9 IN TO RBL 46 INCHE S. 2 L 7 2 4F A6WE 2001050700152 20010507 00152 WP 2001 5 7 ZW0A0100804 1 20010424 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT FOUND CABIN TRACK NUMBER 5 WAS CORRODED AT STA 200 TO 247, RBL 45 INCHES. INSTALLED NEW TRACK PER SPM 6-70-1. INSTALLED FASTENERS PER SRM 51-30-01. 2 L 7 2 4F A6WE 2001050700153 20010507 00153 WP 2001 5 7 ZW0A0100805 1 20010425 A 5320 CASTING DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 924TW 49100 DURING CHECK-C MAINT IN NLG WELL FOUND CRACK IN CASTING AT STA 69.5, APPROX 16 IN LBL AT GEAR WELL CEILING HEIGHT. REPL ACED CASTING P/N 4912385-1 WITH NEW CASTING 4912385-501 PER SRM 51-01 AND SPM 6-70-01 PAGE 3. 2 L 7 2 4F A6WE 2001050700154 20010507 00154 WP 2001 5 7 ZW0A0100806 1 20010421 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT FOUND CORROSION UNDER NUMBER 1 GALLEY DRAIN PAN OTBD AFT CORNER. FABRICATED NEW MEMBRANE FROM 7075 -T6 PER SRM 53-14-1, FIG 11. INSTALLED PER SRM 51-30 AND 51-10-4. 2 L 7 2 4F A6WE 2001050700155 20010507 00155 WP 2001 5 7 ZW0A0100807 1 20010421 A 5345 MOUNT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT NUMBER 1 GALLEY TIE DOWN AT BL 10.5R, BL 45R AND BL 51R, HAD CORROSION. INSTALLED GALLEY TIE DOWNS PER SRM 51-30 AND 51-10-4. 2 L 7 2 4F A6WE 2001050700156 20010507 00156 WP 2001 5 7 ZW0A0100808 1 20010423 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT IN AFT CARGO COMPT, THE LT TIE DOWN TRACK WAS CORRODED FROM STA 1212 TO STA 1231. REPLACED LT SIDE TIE DOWN TRACK FROM STA 1002 TO STA 1320, PER SRM 51-30 AND SRM 51-10-4. INSTALLED FASTENERS PER SRM 51-30-5. 2 L 7 2 4F A6WE 2001050700157 20010507 00157 WP 2001 5 7 ZW0A0100809 1 20010423 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT IN THE AFT CARGO BIN AT STA 1220 TO 1332, THE LT TIE DOWN TRACK WAS CORRODED IN SEVERAL PLACES. RE PLACED TIE DOWN TRACK STA 1002 TO 1320, LT SIDE, PER SRM 51-30 AND SRM 51-10-4. ORDERED NEW SPLICE KIT TO PICK UP FASTE NERS HOLES FROM NEW TRACK AND INSTALLED SPLICE PER SRM 25-52-00, FIG 3. INSTALLED FASTENERS PER SRM 51-30-5. 2 L 7 2 4F A6WE 2001050700158 20010507 00158 WP 2001 5 7 ZW0A0100810 1 20010425 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT FOUND NUMBER 3 CABIN FLOOR TRACK WITH CORROSION ON FLANGE BETWEEN STA 1231 AND 1271. NEW TRACK FAB RICATED FROM EXTRUSION AND INSTALLED FROM STA 1136 TO 1309 PER SPM 6-70-01. 2 L 7 2 4F A6WE 2001050700159 20010507 00159 WP 2001 5 7 ZW0A0100811 1 20010425 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT IN AFT CARGO COMPT FOUND CORROSION ON FORMER AT STA 1231, LONGERON 27L TO 28L. REMOVED CORRODED FO RMER AND SPLICED NEW PER SRM 53-03, FIG 2A. 2 L 7 2 4F A6WE 2001050700160 20010507 00160 WP 2001 5 7 ZW0A0100812 1 20010425 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT FOUND FLOOR ATTACH ANGLE CORRODED AT STA 351 TO 446, RBL 8. REPLACED FLOOR SUPPORT WITH NEW PER DR AWING 5936587. REPLACED BOLTS, NUTS AND WASHERS PER SRM 51-30-1. REINSTALLED RIVETS PER SRM 51-30-2. 2 L 7 2 4F A6WE 2001050700161 20010507 00161 WP 2001 5 7 ZW0A0100813 1 20010425 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT FOUND CORROSION ON LT CARGO TRACK AT STA 1155 TO 1218. INSTALLED NEW TRACK AND INSTALLED FASTENERS PER SRM 51-30 FROM STA 1010 TO STA 1218, AND SRM 53-05 FIG 4. 2 L 7 2 4F A6WE 2001050700162 20010507 00162 WP 2001 5 7 ZW0A0100802 1 20010426 A 3350 58222 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 931TW 49527 THE EGRESS LIGHTS IN THE FWD COACH CABIN WERE INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 12-28-00 STL. 2 L 7 2 4F RT A6WE 2001050700163 20010507 00163 WP 2001 5 7 ZW0A0100814 1 20010425 A 5530 ATTACH ANGLE DOUG DC9 DC982 3022082 WP VERTICAL STAB CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT THE DORSAL FIN ATTACH ANGLE WAS CRACKED ON LT SIDE, STA 1405 TO 1427. REPLACED ATTACH ANGLE WITH N EW. INSTALLED RIVETS PER SRM 51-30-2. 2 L 7 2 4F A6WE 2001050700164 20010507 00164 WP 2001 5 7 ZW0A0100815 1 20010426 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT FOUND SEAT TRACK BOTTOM CORRODED AT STA 1155 TO STA 1308, AT LBL 22. TRACK REMOVED FROM STA 1136 T O 1308. NEW SECTION FABRICATED FROM EXTRUSION AND INSTALLED PER SPM 6-70-1. 2 L 7 2 4F A6WE 2001050700165 20010507 00165 WP 2001 5 7 ZW0A0100816 1 20010420 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT IN THE AFT CARGO COMPT, STA 1320, FROM RBL 17 IN TO LBL 17 IN, THE FLOOR SUPPORT WAS CORRODED. REP LACED FLOOR SUPPORT WITH NEW. TREATED PER SRM 51-10-3. RE-INSTALLED RIVETS PER SRM 51-30-2. RE-INSTALLED HI-LOKS PER SRM 51-30-5. 2 L 7 2 4F A6WE 2001050700166 20010507 00166 WP 2001 5 7 ZW0A0100817 1 20010423 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT IN THE AFT CARGO COMPT THE LT TIE DOWN TRACK WAS CORRODED FROM STA 1003 TO 1222. INSTALLED NEW TRA CK PER SRM 53-05-4G, PER SRM 51-30-5, 51-30-2, 51-30-1 AND SPM 6-70-01. 2 L 7 2 4F A6WE 2001050700167 20010507 00167 WP 2001 5 7 ZW0A0100818 1 20010420 A 5320 SPLICE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT FOUND CORROSION AT AFT END OF LONGERON SPLICE BETWEEN FORMERS 1297 AND 1309 LONGERON 25L. REPLACED LONGERON 25L SPLICE WITH NEW BETWEEN STA 1297 TO 1309 PER SPM 6-70-01 AND SRM 53-02 FIGURE 18. INSTALLED FASTENERS PER SRM 51-30-5 AND SRM 51-30-02. 2 L 7 2 4F A6WE 2001050700168 20010507 00168 WP 2001 5 7 ZW0A0100819 1 20010420 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT FROM STA 1211 TO 1323, RT TIE DOWN TRACK WAS CORRODED IN SEVERAL PLACES. REMOVED CORROSION BY INST ALLING NEW PART WITH SCREWS PER SRM 51-30-01 AND SPM 6-70-01. 2 L 7 2 4F A6WE 2001050700169 20010507 00169 WP 2001 5 7 ZW0A0100820 1 20010421 A 5320 SPLICE DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND LT TIE DOWN TRACK SPLICE CORRODED AT STA 1221. CORRODED SPLICE REMOVE D FROM ACFT AND REPLACED WITH NEW. INSTALLED PER DRAWING 5926660 AND SRM 51-60-0. FINISH PER 51-10-3. 2 L 7 2 4F A6WE 2001050700170 20010507 00170 NM 2001 5 7 ZW0A0100801 1 20010425 A 3350 767 LIGHT BOEING 757 757231 1384950 NM CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 715TW 28483 THE EMERGENCY LIGHT ABOVE CABIN SEAT 6C WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 10-14-00 LAX. 2 L 7 2 4F RT A2NM 2001050700171 20010507 00171 EU 2001 5 7 MALA010424 1 20010426 A 7110 725450188 COWLING SAAB SF340 SF340A 7850100 EU LT ENGINE LOOSE A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 106XJ 106 DURING FLIGHT 2737 OUT OF MSP, LT ENGINE COWLING CAME LOOSE INFLIGHT. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLA CED UPPER FAIRING P/N 7254501-88 AND PROP IAW SAAB 340 JOB CARD 6110-303. REINSTALLED FIGURE 8 COWL AS REQUIRED. RE-SC UFFED METAL, PRIMED AND PAINTED IAW SAAB AMM 51-20-00. 2 L 7 2 4T RT A52EU 2001050700172 20010507 00172 EU 2001 5 7 MALA010425 1 20010426 A 2434 23080031 GENERATOR SAAB SF340 SF340A 7850100 EU LT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 991XJ 091 ON FLIGHT 3333 FROM MSP, LEFT DC GENERATOR FAILED, FOLLOWED QRH, RESET C/B, J3 AND J4 AS PER MX STILL INOP. AIR RETURN TO MSP. MAINTENANCE REPLACED LEFT DC GEN P/N 23080-031, S/N ON 6754, S/N OFF 99283. COMPLETED JOB CARD 243103. OPERAT IONAL AND LEAK CHECK GOOD. 2 L 7 2 4T RT A52EU 2001050700173 20010507 00173 2001 5 7 DHL2001743003 4 20010426 A 3425 FLIGHT DIR BOEING 727 727225 1384077 NM COCKPIT MALFUNCTIONED A DHLA K NONE O OTHER AP APPROACH 1 SO 01 743DH 22438 COPILOT''S FLIGHT DIRECTOR GIVES ERRONEOUS COMMANDS (S-TURNS THROUGH LOCALIZER); NEVER STABILIZES. TESTED SYSTEM W/T-30 TEST BOX AND ALL LOCAL FREQUENCIES WITH NORMAL AND AUX NAV SETTINGS IAW B727 MM 34-31-02. NO DEFECTS NOTED. 2 L 7 3 4F A3WE 2001050700174 20010507 00174 2001 5 7 DHL2001804005 4 20010426 A 2210 2588788905 COMPUTER DOUG DC8 DC873F 302199F WP AUTO-PILOT SYS DEFECTIVE A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 804DH 46124 IN LEVEL FLIGHT AT CRUISE ALTITUDE THE AUTOPILOT ROWS THE AIRCRAFT 2 DEG LEFT AND RIGHT CONTINUOUSLY. REMOVED AND REPLA CED ROLL CHANNEL COMPUTER PER MM 22-12-1. OPS NORMAL. 2 L 7 4 4F RT 4A25 2001050700175 20010507 00175 2001 5 7 DHL2001804006 4 20010426 A 2210 2588788905 COMPUTER DOUG DC8 DC873F 302199F WP COCKPIT MALFUNCTIONED A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 804DH 46124 AUTOPILOT ELEVATOR SERVO TRIM METER OSCILLATES FULL DEFLECTION UP AND DOWN WHILE AIRCRAFT IS LEVEL FLIGHT. RERACKED PIT CH CHANNEL COMPUTER. SYSTEM OP CHECKS NORMAL PER MM 22-13-1. 2 L 7 4 4F RT 4A25 2001050700176 20010507 00176 2001 5 7 DHL2001807009 4 20010427 A 2210 AUTOPILOT SYS DOUG DC8 DC873 302199C WP COCKPIT DEFECTIVE A DHLA K NONE O OTHER CR CRUISE 1 SO 01 807DH 45990 AUTOPILOT WILL NOT ENGAGE. DMI 5372 - ASSIGNED CVG MX CTRL, MEL 22-1. PLACARD INSTALLED. 2 L 7 4 4F RT 4A25 2001050700177 20010507 00177 2001 5 7 DHL2001727011 4 20010426 A 2213 AUTOPILOT SYS BOEING 727 727228 NM COCKPIT ERRATIC A DHLA K NONE O OTHER CR CRUISE 1 SO 01 727DH 20204 DURING HEADING CHANGES, AIRCRAFT BANKS ERRATICALLY IN SHORT, JERKY MOTION. AUTOPILOT ON. DEFERRED AUTOPILOT SYSTEM PER MEL 22-1-2 CAT-C. DMI 5360. PLACARD INSTALLED. 2 L 7 3 4F A3WE 2001050700178 20010507 00178 WP 2001 5 7 DHL2001806613 1 20010403 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - AFT PAX ENTRY DOOR LWR FWD JAMB CORNER SHOWS 1 CRACK 3.0 INCHES STA 1600.000 BETWEEN L-20 LT AND L-21 LT. CUT OUT DAMAGED AREA, FABRICATED FILLER AND (2 EA) DOUBLERS (FROM ALCLAD 7075 T6 0.090, 0.125) IAW SRM 53-2-0 PAGE 125, 126 FIG 1B. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B, AND APPLIED (PRC) SEALANT IAW SRM 51-1-15 PAGE 1. INSTALLED FILL ER AND DOUBLERS IAW SRM 53-2-0 PAGE 125, 126. 2 L 7 4 4F RT 4A25 2001050700179 20010507 00179 WP 2001 5 7 DHL2001806614 1 20010401 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - NLG W/W LT AFT CORNER SKIN CRACKED 0.125 INCH LENGTH STA 8.000 L33 LT. CUT OUT DAMAGED SKIN IAW EO DHL 010331 , EO 2406, EO 2001075 FABRICATED FILLER AND DOUBLER (ALCLAD 7075 T6 0.050, 0.06) IAW SRM DHL 010331, EO 2406, EO 2001075 . CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. APPLIED (PRC) SEALANT ON REWORK AREA IAW SRM 51-1-15 PAGE 1. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW EO DHL 010331, EO 2406, EO 2001075, SRM 51-1-20D PAGE 9. 2 L 7 4 4F RT 4A25 2001050700180 20010507 00180 WP 2001 5 7 DHL2001806615 1 20010402 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - EXT FUSELAGE SKIN AT STA 1440.000 L-30 AND 31 RT SHOWS CRACK OF .5 INCH. REMOVED FASTENERS IAW SRM 51-1-21 PA GE 1. CUT OUT DAMAGED SKIN IAW EO DHL 010314, EO 2340, EO 2001095. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FILLER AND DOUBLER (ALCLAD 7075 T6 0.071/0.080) IAW 010314, EO 2340, EO 2001095. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW EO DHL 010314, EO 2340, EO 2001095, SRM 51-1-21 P AGE 1. APPLIED (PRC) SEALANT ON REWORKED AREA IAW SRM 51-1-15 PAGE 1. 2 L 7 4 4F RT 4A25 2001050700181 20010507 00181 NM 2001 5 7 DHL2001741006 1 20010427 A 2611 SMOKE DETECTOR BOEING 727 7272Q9 138448M NM CARGO BAY MALFUNCTIONED A DHLA O OTHER N FALSE WARNING DE DESCENT 1 SO 01 741DH 21931 CARGO SMOKE LIGHT CAME ON, ON INITIAL DESCENT. REMAINED ON UNTIL TOUGHDOWN. NO SMOKE OBSERVED BY CREW IN CARGO AREA. RESET CONNECTOR ON CARGO SMOKE DETECTOR. PERFORMED OPS CHECK, OK FOR CONTINUID SERVICE. 2 L 7 3 4F RT A3WE 2001050700182 20010507 00182 WP 2001 5 7 ZW0A0100822 1 20010422 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT ON THE AFTER BODY FOUND A CRACK AND INTERIM REPAIR IN RT CANTED WEB VENT BOX SUPPORT, STA 1465. FA BRICATED NEW SUPPORT PER DRAWING 520923 AND INSTALLED PER SRM 51-30. TREATED PARTS PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001050700183 20010507 00183 WP 2001 5 7 ZW0A0100823 1 20010423 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT IN THE AFT CARGO COMPT, AT STA 1211 AND LONGERON 28R, BOTTOM OF CARGO DOOR JAMB, FOUND ANGLE HAD CO RROSION. INSTALLED NEW ANGLE PER SPM 6-70-01. 2 L 7 2 4F A6WE 2001050700184 20010507 00184 WP 2001 5 7 ZW0A0100824 1 20010424 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT AT STA 1155 AND LONGERON 28R, BOTTOM OF CARGO DOOR JAM, FOUND ANGLE HAD CORROSION. INSTALLED NEW A NGLE PER SPM 6-70-01. 2 L 7 2 4F A6WE 2001050700185 20010507 00185 WP 2001 5 7 ZW0A0100825 1 20010425 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT SEAT TRACK BOTTOM FOUND CORRODED AT STA 1155 TO 1250, LBL 22 INCHES. NEW TRACK FABRICATED FROM EXT RUSION AND INSTALLED FROM STA 1136 TO 1309, PER SPM 6-70-01. 2 L 7 2 4F A6WE 2001050700186 20010507 00186 WP 2001 5 7 ZW0A0100826 1 20010425 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT FOUND CABIN FLOOR BEAM AT STA 1155 TO 1611 LBL HAD CORROSION. REMOVED OLD FLOOR SUPPORT AND FABRIC ATED NEW FROM EXTRUDED STOCK. INSTALLED WITH HI-LOKS PER SPM 6-70-01. 2 L 7 2 4F A6WE 2001050700187 20010507 00187 WP 2001 5 7 ZW0A0100827 1 20010422 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT ON LT FUSELAGE SKIN FOUND DENT 2 IN BY 3 IN BY 0.125 INCHES AT STA 230, BETWEEN LONGERON 17L AND 18 L. CUT OUT DAMAGED AREA AND REPAIRED BY INSTALLING DOUBLERS AND NEW SKIN PER SRM 53-04, FIG 12C. 2 L 7 2 4F A6WE 2001050700188 20010507 00188 WP 2001 5 7 ZW0A0100828 1 20010420 A 5712 RIB DOUG DC9 DC982 3022082 WP RT WING CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT ON RT WING THE L/E RIB JUST INBOARD OF JACK PAD HAD 1 INCH CRACK ON LOWER FWD END. INSTALLED DOUBL ER PER SERVICE BULLETIN 57-10. 2 L 7 2 4F A6WE 2001050700189 20010507 00189 WP 2001 5 7 ZW0A0100829 1 20010420 A 5712 RIB DOUG DC9 DC982 3022082 WP RT WING CHIPPED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT ON RT WING L/E THE AFT LOWER END OF RIB HAD METAL CHIP MISSING, JUST OTBD OF JACKPAD. INSTALLED DO UBLER PER SERVICE BULLETIN ENG TASK 57-10. 2 L 7 2 4F A6WE 2001050700190 20010507 00190 WP 2001 5 7 ZW0A0100830 1 20010420 A 5712 CLIP DOUG DC9 DC982 3022082 WP RT WING CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT ON RT WING L/E RIB JUST FWD OF JACKPAD HAD A 2 INCH CRACK IN ATTACH CLIP. REPAIRED PER SERVICE BUL LETIN 57-10. 2 L 7 2 4F A6WE 2001050700191 20010507 00191 WP 2001 5 7 ZW0A0100831 1 20010420 A 5730 SKIN DOUG DC9 DC982 3022082 WP RT WING CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT RT WING L/E SKIN HAD TEMPORARY REPAIR FOR SKIN CRACKS. INSTALLED PERMANENT REPAIR PER SERVICE BULL ETIN 57-170. 2 L 7 2 4F A6WE 2001050700192 20010507 00192 WP 2001 5 7 ZW0A0100832 1 20010420 A 5720 CLIP DOUG DC9 DC982 3022082 WP RT WING CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT ON RT WING THE RIB JUST INBD OF JACKPAD HAD A 2 INCH CRACK IN ATTACH CLIP. REPAIRED PER SERVICE BU LLETIN 57-170. 2 L 7 2 4F A6WE 2001050700193 20010507 00193 WP 2001 5 7 ZW0A0100833 1 20010420 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT IN FWD CABIN FOUND FLOOR AT STA 218, BL 0, HAD CORROSION. REMOVED CORRODED SUPPORT AND REPLACED WI TH SERVICEABLE SUPPORT. INSTALLED WITH SAME TYPE FASTENERS AND TREATED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001050700194 20010507 00194 EU 2001 5 7 QXEA0100554 1 20010325 A 5320 CHANNEL FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CHANNEL CRACKED FORWARD OF STATION 3820-3450, RIGHT HAND SIDE UNDER GALLEY FLOOR. REPAIRED IAW FOKKER SRM 53-11-05 , 53-02-14 AND 51-31-01 PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001050700195 20010507 00195 EU 2001 5 7 QXEA0100555 1 20010328 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- LEFT HAND AT FRAME 6305 AND STRINGER 19 HAS CRACKED CASTELLATION. REPAIRED IAW FOKKER SRM 53-02-12. 2 L 7 2 4F RT A20EU 2001050700196 20010507 00196 EU 2001 5 7 QXEA0100556 1 20010331 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- LEFT HAND AT FRAME 5805 AND STRINGER 19 HAS CRACKED CASTELLATION. REPAIRED IAW HORIZON AIR EA 4-53-1461. 2 L 7 2 4F RT A20EU 2001050700197 20010507 00197 EU 2001 5 7 QXEA0100557 1 20010331 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- LEFT HAND AT FRAME 5805 AND STRINGER 18 HAS CRACKED CASTELLATION. REPAIRED IAW HORIZON AIR EA 4-53-1461. 2 L 7 2 4F RT A20EU 2001050700198 20010507 00198 EU 2001 5 7 QXEA0100558 1 20010403 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- DENT AND SCRATCH BETWEEN FRAME 15635 AND 16060 BETWEEN STRINGER 68 AND 67, FORWARD OF REAR CARGO DOOR APERTURE. RE PAIRED IAW FOKKER SRM 53-02-04, 51-31-01 AND HORIZON AIR EA 4-53-1471. 2 L 7 2 4F RT A20EU 2001050700199 20010507 00199 EU 2001 5 7 QXEA0100559 1 20010328 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED CASTELLATION AT FRAME 15205 AND STRINGER 57. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001050700200 20010507 00200 EU 2001 5 7 QXEA0100560 1 20010328 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED CASTELLATION AT FRAME 15205 AND STRINGER 45. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001050700201 20010507 00201 EU 2001 5 7 QXEA0100561 1 20010328 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED CASTELLATION AT FRAME 15205 AND STRINGER 40. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001050700202 20010507 00202 EU 2001 5 7 QXEA0100562 1 20010328 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED CASTELLATION AT FRAME 15205 AND STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001050700203 20010507 00203 EU 2001 5 7 QXEA0100563 1 20010328 A 5320 WASHER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED RIVET WASHER IN CABIN AT FRAME 15205 AND STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001050700204 20010507 00204 EU 2001 5 7 QXEA0100564 1 20010328 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED CASTELLATION AT FRAME 14755 AND STRINGER 58A. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001050700205 20010507 00205 EU 2001 5 7 QXEA0100565 1 20010328 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED CLIP AT FRAME 14755 AND STRINGER 57. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001050700206 20010507 00206 EU 2001 5 7 QXEA0100566 1 20010328 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED CASTELLATION AT FRAME 14755 AND STRINGER 56. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001050700207 20010507 00207 EU 2001 5 7 QXEA0100567 1 20010328 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED CASTELLATION AT FRAME 14755 AND STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001050700208 20010507 00208 EU 2001 5 7 QXEA0100568 1 20010328 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED CASTELLATION AT FRAME 14755 AND STRINGER 40. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001050700209 20010507 00209 EU 2001 5 7 QXEA0100569 1 20010328 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED CASTELLATION AT FRAME 14755 AND STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001050700210 20010507 00210 EU 2001 5 7 QXEA0100570 1 20010328 A 5320 WASHER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED RIVET WASHER IN CABIN AT FRAME 14755 AND STRINGER 34. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001050700211 20010507 00211 EU 2001 5 7 QXEA0100571 1 20010328 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED CASTELLATION AT FRAME 14755 AND STRINGER 28. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001050700212 20010507 00212 EU 2001 5 7 QXEA0100572 1 20010328 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED CASTELLATION AT FRAME 13815 AND STRINGER 57. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001050700214 20010507 00214 EU 2001 5 7 QXEA0100574 1 20010328 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED CASTELLATION AT FRAME 12875 AND STRINGER 33. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001050700215 20010507 00215 EU 2001 5 7 QXEA0100575 1 20010329 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED CASTELLATION AT FRAME 12875 AND STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-11. 2 L 7 2 4F RT A20EU 2001050700216 20010507 00216 EU 2001 5 7 QXEA0100576 1 20010328 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED CASTELLATION AT FRAME 12405 AND STRINGER 46. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001050700217 20010507 00217 EU 2001 5 7 QXEA0100577 1 20010328 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED CASTELLATION AT FRAME 12405 AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001050700218 20010507 00218 EU 2001 5 7 QXEA0100578 1 20010328 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- RIGHT HAND INBOARD SEAT TRACK CORRODED BETWEEN STATION 10753 AND 11253. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9. 2 L 7 2 4F RT A20EU 2001050700219 20010507 00219 EU 2001 5 7 QXEA0100579 1 20010328 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- RIGHT HAND INBOARD SEAT TRACK CORRODED BETWEEN STATION 8805 AND 10753. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-40-1. 2 L 7 2 4F RT A20EU 2001050700220 20010507 00220 EU 2001 5 7 QXEA0100580 1 20010328 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- RIGHT HAND INBOARD SEAT TRACK CORRODED BETWEEN STATIONS 6565 AND 7305. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-40-1. 2 L 7 2 4F RT A20EU 2001050700221 20010507 00221 EU 2001 5 7 QXEA0100581 1 20010328 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- RIGHT HAND INBOARD SEAT TRACK IS CORRODED BETWEEN STATIONS 7305 AND 8065. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-40-1. 2 L 7 2 4F RT A20EU 2001050700222 20010507 00222 EU 2001 5 7 QXEA0100582 1 20010328 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- RIGHT HAND INBOARD SEAT TRACK CORRODED BETWEEN STATIONS 8065 AND 8565. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-40-1. 2 L 7 2 4F RT A20EU 2001050700223 20010507 00223 EU 2001 5 7 QXEA0100583 1 20010328 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- LEFT HAND INBOARD SEAT TRACK IS CORRODED BETWEEN STATIONS 9805 AND 10253. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-40-1. 2 L 7 2 4F RT A20EU 2001050700224 20010507 00224 EU 2001 5 7 QXEA0100584 1 20010328 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- LEFT HAND INBOARD SEAT TRACK IS CORRODED BETWEEN STATIONS 8805 AND 9305. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 A ND 53-40-1. 2 L 7 2 4F RT A20EU 2001050700225 20010507 00225 EU 2001 5 7 QXEA0100586 1 20010330 A 5320 SPLICE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CORROSION ON FRAME SPLICE ANGLES AT FRAME 11905 AND STRINGER 45 FORWARD AND AFT RIGHT HAND SIDES. REPAIRED IAW FOK KER SRM 51-31-01 PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001050700226 20010507 00226 EU 2001 5 7 QXEA0100587 1 20010328 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED CASTELLATION AT FRAME 10346 AND STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001050700227 20010507 00227 EU 2001 5 7 QXEA0100588 1 20010328 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED CASTELLATION AT FRAME 10966 AND STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001050700228 20010507 00228 EU 2001 5 7 QXEA0100589 1 20010331 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED CASTELLATION AT FRAME 6805 AND STRINGER 19. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001050700229 20010507 00229 EU 2001 5 7 QXEA0100590 1 20010331 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED CASTELLATION AT FRAME 7305 AND STRINGER 18. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001050700230 20010507 00230 EU 2001 5 7 QXEA0100591 1 20010331 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED CASTELLATION AT FRAME 7305 AND STATION 19. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001050700231 20010507 00231 EU 2001 5 7 QXEA0100592 1 20010331 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- FUSELAGE FRAME ATTACH ANGLES CRACKED AT FRAME 5305 AND STRINGERS 16 AND 17. REPAIRED IAW FOKKER SRM 53-02-01. 2 L 7 2 4F RT A20EU 2001050700232 20010507 00232 EU 2001 5 7 QXEA0100594 1 20010328 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- FUSELAGE SKIN DENTED ON RIGHT HAND SIDE ON THE ROOF OF STATION 20285 THROUGH 20785 AND STRINGERS 37 AND 38 BY DORSA L FIN. REPAIRED IAW FOKKER SRM 53-02-02 PAGE 2. 2 L 7 2 4F RT A20EU 2001050700233 20010507 00233 EU 2001 5 7 QXEA0100595 1 20010323 A 5240 DOOR FOKKER F28 F28MK4000 4990810 EU HYD SERVICE DR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- HYDRAULIC SERVICE PANEL DOOR REBATE CRACKED AT FORWARD END CENTER AND UPPER CORNER AND BENT LOWER FORWARD CORNER. REPAIRED IAW HORIZON AIR EA 4-52-442. 2 L 7 2 4F RT A20EU 2001050700234 20010507 00234 EU 2001 5 7 QXEA0100596 1 20010328 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- DENT IN FUSELAGE SKIN LEFT HAND SIDE, AFT OF FIRE BOTTLE DISCHARGE AT STATION 19775 AND STRINGERS 12 AND 13 FOUND B EYOND LIMITS. REPAIRED IAW FOKKER SRM 53-02-02 PAGE 2. 2 L 7 2 4F RT A20EU 2001050700235 20010507 00235 EU 2001 5 7 QXEA0100597 1 20010404 A 4910 DOOR FRAME FOKKER F28 F28MK4000 4990810 EU APU INLET CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- TWO CRACKS AT APU AIR INLET DOOR SURROUND TOP AND BOTTOM AFT CORNERS. REPAIRED IAW FOKKER SRM 53-02-07 PAGE 7, 53- 26-01 PAGE 8, 51-31-01 PAGES 13 AND 14 AND 51-31-05 PAGES 8-10. 2 L 7 2 4F RT A20EU 2001050700236 20010507 00236 EU 2001 5 7 QXEA0100598 1 20010417 A 5755 SUPPORT BRACKET FOKKER F28 F28MK4000 4990810 EU SPEEDBRAKE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- SPEEDBRAKE UPPER HINGE SUPPORT BRACKET IS CRACKED. REPAIRED IAW HORIZON AIR EA 4-53-1476. 2 L 7 2 4F RT A20EU 2001050700237 20010507 00237 EU 2001 5 7 QXEA0100599 1 20010401 A 5512 SKIN FOKKER F28 F28MK4000 4990810 EU HORIZ STAB CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CORROSION FOUND ON LEFT HAND HORIZONTAL STAB BOTTOM SKIN FORWARD OF PANEL 52E. REPAIRED IAW FOKKER SRM 51-10-04 PA GE 9. 2 L 7 2 4F RT A20EU 2001050700238 20010507 00238 EU 2001 5 7 QXEA0100600 1 20010328 A 5511 RIB FOKKER F28 F28MK4000 4990810 EU HORIZ STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- HORIZONTAL STAB LEADING EDGE 51A HAS A CRACK AT NUMBER 1 RIB. REPAIRED IAW HORIZON AIR EA 4-55-286. 2 L 7 2 4F RT A20EU 2001050700239 20010507 00239 EU 2001 5 7 QXEA0100601 1 20010406 A 5512 SKIN FOKKER F28 F28MK4000 4990810 EU HORIZ STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- HORIZONTAL STAB LEADING EDGE 51B HAS CRACKS AT OUTBOARD AND FLANGE CORNERS. REPAIRED IAW HORIZON AIR EA 4-55-287. 2 L 7 2 4F RT A20EU 2001050700240 20010507 00240 EU 2001 5 7 QXEA0100602 1 20010406 A 5512 SKIN FOKKER F28 F28MK4000 4990810 EU HORIZ STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- HORIZONTAL STAB LEADING EDGE 51C HAS CRACKS AT INBOARD AND FLANGE CORNER. REPAIRED IAW HORIZON AIR EA 4-55-287. 2 L 7 2 4F RT A20EU 2001050700241 20010507 00241 EU 2001 5 7 QXEA0100603 1 20010402 A 5542 SKIN FOKKER F28 F28MK4000 4990810 EU RUDDER DELAMINATED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- RUDDER TRAILING EDGE TO BE REPLACED DUE TO EXCESSIVE DELAMINATION. REPAIRED IAW FOKKER SRM 51-10-05. 2 L 7 2 4F RT A20EU 2001050700242 20010507 00242 EU 2001 5 7 QXEA0100604 1 20010330 A 5511 RIB FOKKER F28 F28MK4000 4990810 EU HORIZ STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- HORIZONTAL STAB LEADING EDGE 51B HAS A CRACK ON RIB 6. REPAIRED IAW HORIZON AIR EA 4-55-286. 2 L 7 2 4F RT A20EU 2001050700243 20010507 00243 EU 2001 5 7 QXEA0100605 1 20010330 A 5511 RIB FOKKER F28 F28MK4000 4990810 EU HORIZ STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- HORIZONTAL STAB LEADING EDGE 51B HAS A CRACK ON RIB 5. REPAIRED IAW HORIZON AIR EA 4-55-286. 2 L 7 2 4F RT A20EU 2001050700244 20010507 00244 EU 2001 5 7 QXEA0100606 1 20010328 A 5511 RIB FOKKER F28 F28MK4000 4990810 EU HORIZ STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- HORIZONTAL STAB LEADING EDGE 51A HAS A CRACK ON RIB 2. REPAIRED IAW HORIZON AIR EA 4-55-286. 2 L 7 2 4F RT A20EU 2001050700245 20010507 00245 EU 2001 5 7 QXEA0100607 1 20010328 A 5511 RIB FOKKER F28 F28MK4000 4990810 EU HORIZ STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- HORIZONTAL STAB LEADING EDGE 51A IS CRACKED ON RIB 4. REPAIRED IAW HORIZON AIR EA 4-55-286. 2 L 7 2 4F RT A20EU 2001050700246 20010507 00246 EU 2001 5 7 QXEA0100608 1 20010328 A 5511 RIB FOKKER F28 F28MK4000 4990810 EU HORIZ STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- HORIZONTAL STAB LEADING EDGE 51A HAS A CRACK ON RIB 5. REPAIRED IAW HORIZON AIR EA 4-55-286. 2 L 7 2 4F RT A20EU 2001050700247 20010507 00247 EU 2001 5 7 QXEA0100609 1 20010328 A 5511 RIB FOKKER F28 F28MK4000 4990810 EU HORIZ STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- HORIZONTAL STAB LEADING EDGE 51A HAS A CRACK ON RIB 6. REPAIRED IAW HORIZON AIR EA 4-55-286. 2 L 7 2 4F RT A20EU 2001050700248 20010507 00248 EU 2001 5 7 QXEA0100610 1 20010426 A 5541 RIB FOKKER F28 F28MK4000 4990810 EU RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- RIB 4 THROUGH 2 HAS SMALL CRACKS AT TRAILING EDGE RUDDER. REPAIRED IAW FOKKER SRM 55-02-01 PAGE 4, 55-02-07 PAGE 3 AND 51-31-01 PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001050700249 20010507 00249 EU 2001 5 7 QXEA0100611 1 20010405 A 5530 ANGLE FOKKER F28 F28MK4000 4990810 EU VERTICAL STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED ANGLE ON VERTICAL STAB ABOVE RIB 3 AND 2 BELOW RUDDER. REPAIRED IAW FOKKER SRM 55-31-04 AND 51-31-01. 2 L 7 2 4F RT A20EU 2001050700250 20010507 00250 EU 2001 5 7 QXEA0100612 1 20010330 A 5540 BRACKET FOKKER F28 F28MK4000 4990810 EU RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED RIB FAIRING BRACKET BELOW RIB 12 ON RUDDER. REPAIRED IAW FOKKER SRM 55-40-04 AND 51-31-01 PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001050700251 20010507 00251 EU 2001 5 7 QXEA0100613 1 20010328 A 5511 RIB FOKKER F28 F28MK4000 4990810 EU HORIZ STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- HORIZONTAL STAB LEADING EDGE 51A HAS A CRACK ON RIB 8. REPAIRED IAW HORIZON AIR EA 4-55-286. 2 L 7 2 4F RT A20EU 2001050700252 20010507 00252 EU 2001 5 7 QXEA0100614 1 20010330 A 5511 RIB FOKKER F28 F28MK4000 4990810 EU HORIZ STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- HORIZONTAL STAB LEADING EDGE 51B HAS A CRACK ON RIB 1. REPAIRED IAW FOKKER SRM 55-02-02. 2 L 7 2 4F RT A20EU 2001050700253 20010507 00253 EU 2001 5 7 QXEA0100615 1 20010401 A 5540 STRINGER FOKKER F28 F28MK4000 4990810 EU RUDDER DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- RIGHT HAND RUDDER STRINGER AT ACCESS PANEL 57Y DAMAGED. REPAIRED IAW FOKKER SRM 55-40-04, 55-02-07, 51-31-01 AND 5 1-30-02. 2 L 7 2 4F RT A20EU 2001050700254 20010507 00254 EU 2001 5 7 QXEA0100616 1 20010404 A 5531 RIB FOKKER F28 F28MK4000 4990810 EU VERTICAL STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- VERTICAL STAB RIB 8 IS CRACKED ON THE RIGHT HAND SIDE. REPAIRED IAW HORIZON AIR EA 4-55-284. 2 L 7 2 4F RT A20EU 2001050700255 20010507 00255 EU 2001 5 7 QXEA0100617 1 20010325 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU RT WING DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- DENT ON RIGHT HAND LEADING EDGE 62D BEYOND LIMITS. REPAIRED IAW FOKKER SRM 57-02-03. 2 L 7 2 4F RT A20EU 2001050700256 20010507 00256 EU 2001 5 7 QXEA0100618 1 20010401 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- LEFT HAND UPPER AFT SKIN PANEL REBATE IS CRACKED BETWEEN WS 2635-3100 AT FALSE SPAR. REPAIRED IAW HORIZON AIR EA 4 -57-548. 2 L 7 2 4F RT A20EU 2001050700257 20010507 00257 EU 2001 5 7 QXEA0100619 1 20010330 A 5730 SKIN PANEL FOKKER F28 F28MK4000 4990810 EU WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- REBATE ON ACCESS PANEL 73B NEEDS INVESTIGATION ON PREVIOUS REPAIR. REPAIRED IAW HORIZON AIR EA 4-57-550. 2 L 7 2 4F RT A20EU 2001050700258 20010507 00258 EU 2001 5 7 QXEA0100620 1 20010406 A 5755 HINGE FOKKER F28 F28MK4000 4990810 EU SPOILER WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- LEFT HAND NUMBER 5 LIFTDUMPER INBOARD ATTACHMENT HINGE BRACKET BOLT ANTI SPIN BASES WORN. REPAIRED IAW FOKKER SRM 27-63-01 AND HORIZON AIR EA 4-57-552. 2 L 7 2 4F RT A20EU 2001050700259 20010507 00259 EU 2001 5 7 QXEA0100621 1 20010403 A 5753 SKIN FOKKER F28 F28MK4000 4990810 EU RT FLAP VANE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- RIGHT HAND INBOARD FLAP VANE DENT IN LEADING EDGE OUTBOARD END. REPAIRED IAW FOKKER SRM 51-11-4 PAGE 2 AND 51-31-0 4 PAGES 10 AND 11. 2 L 7 2 4F RT A20EU 2001050700260 20010507 00260 EU 2001 5 7 QXEA0100622 1 20010405 A 5720 ATTACH ANGLE FOKKER F28 F28MK4000 4990810 EU LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- LEFT HAND WING INBOARD TRAILING EDGE UPPER ATTACH ANGLE TO 5280 BEAM IS CRACKED. REPAIRED IAW FOKKER SRM 51-32-01, 51-32-01 AND 51-35-02. 2 L 7 2 4F RT A20EU 2001050700261 20010507 00261 EU 2001 5 7 QXEA0100623 1 20010405 A 5755 BRACKET FOKKER F28 F28MK4000 4990810 EU SPOILER DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- RIGHT HAND NUMBER 1 LIFTDUMPER BRACKET MOUNTING HOLES REQUIRE REAMING FOR OVERSIZED BOLT. REPAIRED IAW HORIZON AIR EA 4-57-551. 2 L 7 2 4F RT A20EU 2001050700262 20010507 00262 EU 2001 5 7 QXEA0100624 1 20010405 A 5755 BRACKET FOKKER F28 F28MK4000 4990810 EU SPOILER DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- RIGHT HAND NR 2 LIFTDUMPER SPIGOT MOUNTING BRACKET REQUIRES REAMING FOR OVERSIZE BOLTS. REPAIRED IAW HORIZON AIR E A 4-57-551. 2 L 7 2 4F RT A20EU 2001050700263 20010507 00263 EU 2001 5 7 QXEA0100632 1 20010327 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED CLIP AT FORWARD CARGO PIT FRAME 9305 AND STRINGER 66. REPAIRED IAW FOKKER SRM 51-31-01 PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001071700104 20010717 00104 NM 2001 7 17 PCAA0104032 1 20010424 A 5315 85310380 FLOORBEAM DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 847EX 333 DURING SCHEDULED A INSPECTION NOSE GEAR WHEEL WELL FLOOR BEAM AT STATION X97 FOUND CRACKED. REPAIR STRAP INSTALLED PER DEHAVILLAND REPAIR DRAWING RD8-53-5817 AS AN INTERIM REPAIR. RD8-53-1336 IS REQUIRED TO BE INSTALLED WITHIN NEXT 250 HR S. PERMANENT REPAIR INSTALLED TO FLOORBEAM ON MAINTENANCE WORK RELEASE DATED 19 JUNE 2001. REPAIR ACCOMPLISHED IN ACCO RDANCE WITH DEHAVILLAND REPAIR DRAWING RD8-53-2376. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001050700264 20010507 00264 NM 2001 5 7 PCAA0104031 1 20010424 A 2433 TRANSFORMER DHAV DHC8 DHC8102 2809003 NM NR 2 FAULTY A PCAA K NONE O OTHER TO TAKEOFF 1 EA 13 806EX 263 MDT- FLIGHT 3909 CREW REPORTED EMERGENCY LIGHTS ILLUMINATED DURING TAKE-OFF ROLL FOR APROXIMATELY 5 SECONDS THEN EXTINGU ISHED. MAINTENANCE REPLACED EMERGENCY LIGHT CONTROL BOX. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. PROBL EM REOCCURED ON FLIGHT 3889/LGA BUT LIGHTS DID NOT EXTINGUISH UNTIL NR 2 ENGINE WAS SHUT DOWN. ISSUED MEL FOR NR 2 TRAN SFORMER RECTIFIER UNIT (TRU) OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001050700265 20010507 00265 NM 2001 5 7 PCAA0104033 1 20010424 A 3350 SWITCH DHAV DHC8 DHC8102 2809003 NM COCKPIT INTERMITTENT A PCAA K NONE O OTHER CR CRUISE 1 EA 13 806EX 263 LGA FLIGHT 3889 CREW REPORTED EMERGENCY LIGHTS ILLUMINATED INTERMITTANTLY IN FLIGHT AND DID NOT GO OUT UNTIL NR 2 ENGINE SHUT DOWN. MEL ISSUED FOR NR 2 TRANSFORMER RECTIFIER UNIT (TRU) OPERATIONAL CHECK NORMAL AIRCRAFT RETURNED TO SERVICE. PROBLEM REOCCURED ON FLT 3889/SYR, WITH NOTATION OF LOW SECONDARY BUSS VOLTAGE. MAINTENANCE REPLACED TRU AND SWAPPED GENERATOR CONTROL UNITS LEFT AND RIGHT. OPERATIONAL CHECK GOOD. PROBLEM REOCCURED FLIGHT 3865/LGA WHERE EMERGENCY LIGHTS ILLUMINATED 5 MINUTES AFTER TAKEOFF AND REMAINED ILLUMINATED IN FLIGHT. MEL ISSUED FOR RIGHT TRU MAINTENANCE FOUND INT ERMITTANT EMERGENCY LIGHT SWITCH IN COCKPIT AND REPLACED SWITCH. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001050700266 20010507 00266 NM 2001 5 7 PCAA0104034 1 20010425 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHT FOD A PCAA K NONE O OTHER CR CRUISE 1 EA 13 806EX 263 PVD FLIGHT 3634 CREW REPORTED EMERGENCY LIGHTS COME ON IN LIGHT. MAINTENANCE REPLACED CIRCUIT BREAKER C-3 RIGHT SECOND ARY BUSS. GROUND RUN CHECK GOOD. PROBLEM REOCCURRED FLIGHT 3800/SYR WHERE EMERGENCY LIGHTS INTERMITTANTLY ILLUMINATED IN FLIGHT. MAINTENANCE CHECKED WIRING BETWEEN FLIGHT ATTENDANT EMERGANCY LIGHT SWITCH AND CONTROL BOX. FOUND CANNON PL UG J73 TO BE FILLED WITH DEBRIS. PINS ON CANNON PLUG J73 REPLACED, CANNON PLUG REINSTALLED. OPERATIONAL CHECK GOOD IN HANGAR AND ON GROUND RUN AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001050700267 20010507 00267 NM 2001 5 7 01FDEA00305 1 20010426 A 7931 ST104Z TRANSMITTER BOEING 727 7272S2F 1384O81 NM NR 3 ENGINE DEFECTIVE A FDEA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SO 25 203FE 22925 689875 AFT T/O NR 3 OIL PRESS DROPPED TO 20 PSI ALL OTHER ENG IND NORM. REMOVED AND REPLACED NR 3 ENG OIL PRESS TRANSMITTER PE R 727-200 MM 79-33-001-2, RUN ENG PER JET RUN HDBK 5A. NO LEAKS FOUND. 2 L 7 3 4F A3WE 2001050700268 20010507 00268 EU 2001 5 7 01FDEA00306 1 20010427 A 3150 WARNING LIGHT AIRBUS 310 A310222 3930315 EU COCKPIT ILLUMINATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 422FE 346 AFT DEPART NR 1 GEN FAULT LIGHT CAME ON. AFT ECAM PROC AND DISCONNECT GEN IDG FAULT LIGHT ILLUM. 2 L 7 2 4F RT A35EU 2001052100014 20010521 00014 NM 2001 5 21 01FDEA00307 1 20010426 A 5320 SPLICE BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 270FE 22035 DURING ROUTINE INSP THE FAIL-SAFE CHORD SPLICE AT BS 560, STR 21L FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB SPLIC E PLATE PER IAW BAC 727 SRM 51-20-1, 51-30-2. 2 L 7 3 4F RT A3WE 2001052100016 20010521 00016 NM 2001 5 21 01FDEA00308 1 20010426 A 5320 SPLICE BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 270FE 22035 DURING ROUTINE INSP THE FAIL-SAFE CHORD SPLICE AT BS 580, STR 21L FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB SPLIC E PLATE PER IAW BAC 727 SRM 51-20-1, 51-30-2. 2 L 7 3 4F RT A3WE 2001052100015 20010521 00015 NM 2001 5 21 01FDEA00309 1 20010426 A 5320 SPLICE BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 270FE 22035 DURING ROUTINE THE FAIL-SAFE CHORD SPLICE AT BS 540, STR 21L FOUND CRACKED. *S/D* REMOVED AND FAB PER IAW BAC 727 SRM 51-20-1, 51-30-2. 2 L 7 3 4F RT A3WE 2001052100017 20010521 00017 NM 2001 5 21 01FDEA00310 1 20010426 A 5320 SPLICE BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 270FE 22035 DURING ROUTINE INSP, THE FAIL-SAFE CHORD SPLICE AT BS 520, STR 21L FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-20-1, 51-30-2. 2 L 7 3 4F RT A3WE 2001052100018 20010521 00018 NM 2001 5 21 01FDEA00311 1 20010426 A 5320 SPLICE BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 270FE 22035 DURING ROUTINE INSP THE FAIL-SAFE CHORD SPLICE AT BS 600, STR 21L FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB PER I AW 727 SRM 51-20-1, 51-30-2. 2 L 7 3 4F RT A3WE 2001052100019 20010521 00019 NM 2001 5 21 01FDEA00312 1 20010426 A 5320 SPLICE BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 270FE 22035 DURING ROUTINE INSP THE FAIL-SAFE CHORD SPLICE AT BS 500, STR 21L FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB SPLIC E PLATE PER IAW BAC 727 SRM 51-20-1, 51-30-2. 2 L 7 3 4F RT A3WE 2001050700269 20010507 00269 NM 2001 5 7 01FDEA00313 1 20010426 A 5320 SILL BOEING 727 727233 138408A NM CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 270FE 22035 DURING ROUTINE INSP LWR SILL INBOARD RADIUS OF MCD CUTOUT FOUND CRACKED AT BS 600. 2 L 7 3 4F RT A3WE 2001050700270 20010507 00270 NM 2001 5 7 01FDEA00314 1 20010426 A 5320 SILL BOEING 727 727233 138408A NM CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 270FE 22035 DURING ROUTINE INSP LWR SILL INBOARD RADIUS OF MCD CUTOUT FOUND CRACKED AT BS 580. 2 L 7 3 4F RT A3WE 2001050700271 20010507 00271 NM 2001 5 7 01FDEA00315 1 20010426 A 5320 SILL BOEING 727 727233 138408A NM CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 270FE 22035 DURING ROUTINE INSP LWR SILL INBOARD RADIUS OF MCD CUTOUT FOUND CRACKED AT BS 560. 2 L 7 3 4F RT A3WE 2001050700272 20010507 00272 NM 2001 5 7 01FDEA00316 1 20010426 A 5320 SILL BOEING 727 727233 138408A NM CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 270FE 22035 DURING ROUTINE INSP LWR SILL INBOARD RADIUS OF THE MCD CUTOUT FOUND CRACKED AT BS 540. 2 L 7 3 4F RT A3WE 2001050700273 20010507 00273 NM 2001 5 7 01FDEA00317 1 20010426 A 5320 SILL BOEING 727 727233 138408A NM CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 270FE 22035 DURING ROUTINE INSP LWR SILL INBOARD RADIUS OF MCD CUTOUT FOUND CRACKED AT BS 520. 2 L 7 3 4F RT A3WE 2001050700274 20010507 00274 NM 2001 5 7 01FDEA00318 1 20010426 A 5320 SILL BOEING 727 727233 138408A NM CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 270FE 22035 DURING ROUTINE INSP LWR SILL INBOARD RADIUS OF MCD CUTOUT FOUND CRACKED AT BS 500. 2 L 7 3 4F RT A3WE 2001050700275 20010507 00275 EA 2001 5 7 JBXA000273 1 20010429 A 2751 TRANSMITTER CNDAIR CL600 CL6002B19 EA T/E FLAP OUT OF RIG A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 586ML 7341 AFTER T/O FLAP INDICATION CHANGED FROM WHITE TO AMBER. FOUND FLAP POSITION FAULT IN STALL PROTECTION COMPUTER. REACTIV ATED RT FLAP POSITION INDICATOR IAW AMM 27-54-00. RIGGED THE RT FLAP POSITION TRANSMITTER IAW AMM 27-55-01, OPS CHECK G OOD NO FAULTS IN SPC. 2 L 7 2 4F RT A21EA 2001050700276 20010507 00276 2001 5 7 SWAA011110 4 20010411 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 063SW 22061 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001050700277 20010507 00277 2001 5 7 SWAA011111 4 20010411 A 2565 D31354 SLIDE BOEING 737 7372T4 1384492 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001050700278 20010507 00278 NM 2001 5 7 SWAA011112 1 20010410 A 5551 6551524 FITTING BOEING 737 7372H4 138448C NM HORIZ STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND HORIZ STAB CENTER SECTION AFT SPAR UPPER HINGE HOUSING ATTACH LUGS CORRODED AT RT SIDE, INBOARD AND OUTBOARD FACES. REPAIRED FITTING PER BFG ER. 2 L 7 2 4F A16WE 2001050700279 20010507 00279 NM 2001 5 7 SWAA011113 1 20010411 A 3350 65C34691 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED C3 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 12 DEF. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2001050700280 20010507 00280 NM 2001 5 7 SWAA011114 1 20010410 A 5553 6546872 FITTING BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 355SW 25250 DURING SCHEDULED D-CHECK, FOUND VERT STAB AFT PRIMARY CLEVIS, AFT LUG FACE AND BORE, CORRODED. REPAIRED FITTING PER BFG ER. 2 L 7 2 4F RT A16WE 2001050700281 20010507 00281 NM 2001 5 7 SWAA011115 1 20010410 A 5553 6547450 FITTING BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 355SW 25250 DURING SCHEDULED D-CHECK, FOUND VERT STAB FWD PRIMARY CLEVIS, FACE & BORE, CORRODED. REPAIRED FITTING PER BFG ER. 2 L 7 2 4F RT A16WE 2001050700282 20010507 00282 2001 5 7 SWAA011116 4 20010411 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 631SW 27706 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001050700283 20010507 00283 NM 2001 5 7 SWAA011117 1 20010410 A 2560 P2070004 RETAINER BOEING 737 7373A4 1384585 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED C4 CHECK, FOUND FWD SECTION EMERGENCY FLASHLIGHT HOLDER LOOSE. SECURED FLASHLIGHT HOLDER PER MM. 2 L 7 2 4F RT A16WE 2001050700284 20010507 00284 NM 2001 5 7 SWAA011118 1 20010410 A 3397 079123 WIRE BOEING 737 7375H4 138449D NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 528SW 26570 DURING SCHEDULED C4 CHECK, FOUND EEPLS WIRING EXPOSED AT ROW 14. INSTALLED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001050700285 20010507 00285 2001 5 7 SWAA011119 4 20010410 A 2565 6557463 BRACKET BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 528SW 26570 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD MOUNT BRACKET LOOSE. SECURED BRACKET PER SRM. 2 L 7 2 4F RT A16WE 2001050700286 20010507 00286 NM 2001 5 7 SWAA011120 1 20010411 A 5230 65C36183 SKIN BOEING 737 7373H4 1384600 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED C3 CHECK, FOUND FWD CARGO DOOR .25 INCH SKIN CRACK AT DOOR HANDLE CUTOUT, AFT UPPER CORNER. REPAIRED D OOR SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001050700287 20010507 00287 NM 2001 5 7 SWAA011099 1 20010409 A 2913 731442 PUMP BOEING 737 7373H4 1384600 NM HYD SYSTEM OVERHEATED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 388SW 26591 AIR TURNBACK. A SYSTEM HYD ELECTRIC PUMP OVERHEAT LIGHT ILLUMINATED. REMOVED AND REPLACED A HYD PUMP AND ELECTRICAL CO NNECTOR PER MM. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2001050700288 20010507 00288 NM 2001 5 7 SWAA011100 1 20010409 A 3350 6104781 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 074SW 22674 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2001050700289 20010507 00289 NM 2001 5 7 SWAA011101 1 20010410 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND STR 4L CRACKED AT BS 907. REPAIRED STR PER SRM. 2 L 7 2 4F A16WE 2001050700290 20010507 00290 NM 2001 5 7 SWAA011103 1 20010409 A 5754 65C26602 SKIN BOEING 737 7373H4 1384600 NM L/E SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 602SW 27953 DURING SCHEDULED C4 CHECK, FOUND NR 5 L/E SLAT DELAMINATED. REMOVED AND REPLACED SLAT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001050700291 20010507 00291 NM 2001 5 7 SWAA011104 1 20010409 A 2560 P2070004 RETAINER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 621SW 28037 DURING SCHEDULED C1 CHECK, FOUND FLASHLIGHT HOLDER LOOSE IN FWD SECTION. SECURED FLASHLIGHT HOLDER PER MM. 2 L 7 2 4F RT A16WE 2001050700292 20010507 00292 NM 2001 5 7 SWAA011105 1 20010410 A 3350 AD201318 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 621SW 28037 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT AFT CABIN. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2001050700293 20010507 00293 NM 2001 5 7 SWAA011106 1 20010410 A 3350 6556633 LENS BOEING 737 7373A4 1384585 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED 1/2D CHECK, FOUND LT AND RT OVERWING EMERGENCY LIGHT LENSES CRACKED. REMOVED AND REPLACED LENSES PER M M. 2 L 7 2 4F RT A16WE 2001050700294 20010507 00294 NM 2001 5 7 SWAA011107 1 20010410 A 5311 6558280 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 514SW 25153 DURING SCHEDULED D-CHECK AT DALFORT, FOUND FUSELAGE FRAME CRACKED AT BS 360, BETWEEN STR 14R & 15R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001050700295 20010507 00295 NM 2001 5 7 SWAA011108 1 20010409 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 769SW 30588 DURING SCHEDULED C3 CHECK, FOUND EEPLS FLOOR TRACKS CRACKED AT ROWS 1 & 11. REMOVED AND REPLACED TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 2001050700296 20010507 00296 NM 2001 5 7 SWAA011109 1 20010410 A 5523 BACB28AK04 BUSHING BOEING 737 7377H4 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 703SW 27837 DURING SCHEDULED SPECIAL VISIT (SWA SI 11038-55), RT ELEVATOR TAB FAILED FREE PLAY CHECK AT NR 4 HINGE (BUSHINGS WORN). REMOVED AND REPLACED ELEVATOR TAB PER MM DUE TO EXCESSIVE PAINT LOSS. 2 L 7 2 4F RT A16WE 2001050700297 20010507 00297 NM 2001 5 7 SWAA011072 1 20010408 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 639SW 27712 AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001050700298 20010507 00298 2001 5 7 SWAA011073 4 20010408 A 2565 D31354 SLIDE BOEING 737 7377H4 NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 401WN 29813 FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001050700299 20010507 00299 2001 5 7 SWAA011074 4 20010408 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 366SW 26577 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED EVAC SLIDE A SSY PER MM. 2 L 7 2 4F RT A16WE 2001050700300 20010507 00300 NM 2001 5 7 SWAA011075 1 20010408 A 5753 6546435 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 604SW 27955 DURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBD AFT FLAP DELAMINATED ON INBOARD END, UPPER AND LOWER SURFACES. REMO VED AND REPLACED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2001050700301 20010507 00301 NM 2001 5 7 SWAA011076 1 20010407 A 5313 BAC1498 STRINGER BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED 1/2D CHECK, FOUND STR 27R CORRODED BETWEEN BS 1006 & 1016. REPAIRED STR PER SRM. 2 L 7 2 4F RT A16WE 2001050700302 20010507 00302 NM 2001 5 7 SWAA011077 1 20010408 A 5320 6551698 SPLICE BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED 1/2D CHECK, FOUND STR 24L CORRODED AT BS 907. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2001050700303 20010507 00303 NM 2001 5 7 SWAA011078 1 20010409 A 3350 207377 LENS BOEING 737 7373A4 1384585 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 680AA 23505 EEPLS LENS LOOSE AT ROW 8. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2001050700304 20010507 00304 NM 2001 5 7 SWAA011079 1 20010408 A 5320 6962014 STIFFENER BOEING 737 7372H4 138448C NM MLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED C2 CHECK, FOUND BS 663.5 VERTICAL STIFFENER CRACKED AT LBL 6.15. REPAIRED VERTICAL STIFFENER PER SWA RA . 2 L 7 2 4F A16WE 2001050700305 20010507 00305 NM 2001 5 7 SWAA011080 1 20010409 A 5311 6546529 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 492, WL 156, RT SIDE. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2001050700306 20010507 00306 NM 2001 5 7 SWAA011081 1 20010409 A 5320 BAC1498 FITTING BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D CHECK, FOUND STRINGER END FITTING CRACKED AT BS 360, STR 5L. R&R STR END FITTING PER SRM. 2 L 7 2 4F A16WE 2001050700307 20010507 00307 NM 2001 5 7 SWAA011082 1 20010409 A 5330 6545877 BEAR STRAP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D CHECK, FOUND FUSELAGE BEAR STRAP CRACKED AT FWD ENTRY DOOR CUTOUT, UPPER FORWARD CORNER, APPROX 1 IN LENGTH. REPAIRED BEAR STRAP PER SWA ACO. 2 L 7 2 4F A16WE 2001050700308 20010507 00308 NM 2001 5 7 SWAA011083 1 20010409 A 5320 6517583 BEAM BOEING 737 7373H4 1384600 NM BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED 1/4D CHECK, FOUND 2 EA. BS 178 BULKHEAD VERTICAL BEAM CRACKS AT LBL 5.7, INBD & OUTBD RADIUS, WL 184.RE PAIRED VERTICAL BEAM PER SRM. 2 L 7 2 4F RT A16WE 2001050700309 20010507 00309 NM 2001 5 7 SWAA011084 1 20010409 A 5311 6978062 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 355SW 25250 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492, WL 160, R/H SIDE, INSIDE RADIUS. REPAIRED FRAME PER SR M. 2 L 7 2 4F RT A16WE 2001050700310 20010507 00310 NM 2001 5 7 SWAA011085 1 20010409 A 5330 65C35765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 355SW 25250 DURING SCHEDULED D CHECK, FOUND EXTERNAL FUSELAGE SKIN CREASED AT BS 360+11, STR 5L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001050700311 20010507 00311 NM 2001 5 7 SWAA011086 1 20010409 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 355SW 25250 DURING SCHEDULED D CHECK, FOUND FLOOR BEAM CORRODED AT BS 986.5, RBL 35 TO RBL 45. R&R FLOORBEAM PER T1-453-037. 2 L 7 2 4F RT A16WE 2001050700312 20010507 00312 NM 2001 5 7 SWAA011087 1 20010408 A 5752 6546455 BUSHING BOEING 737 7373H4 1384600 NM AILERON TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 627SW 27935 DURING SCHEDULED C4 CHECK, FOUND RT WING AILERON TAB BUSHINGS WORN AT THREE HINGES. R&R AILERON TAB PER MM. 2 L 7 2 4F RT A16WE 2001050700313 20010507 00313 NM 2001 5 7 SWAA011088 1 20010408 A 5315 6546804 FLOORBEAM BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 46 TO LBL 15. REPAIRED FLOORBEAM PER SWA T1. 2 L 7 2 4F RT A16WE 2001050700314 20010507 00314 NM 2001 5 7 SWAA011089 1 20010409 A 5330 6545857 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR LOWER HINGE CUTOUT, FWD CORNER. REPAI RED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001050700315 20010507 00315 NM 2001 5 7 SWAA011090 1 20010408 A 2910 6546858 HYDRAULIC LINE BOEING 737 7372H4 138448C NM NR 1 ENGINE LEAKING A SWAA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SW 07 094SW 23053 DECLARED EMERGENCY DURING DESCENT, A SYSTEM HYDRAULICS FAILED. FOUND PRESS LINE LEAKING FROM NR 1 ENGINE HYD PUMP. R&R PRESS LINE PER MM. NO METAL NOTED IN SYS, LEAK & OPS CHECK GOOD. 2 L 7 2 4F A16WE 2001050700316 20010507 00316 NM 2001 5 7 SWAA011091 1 20010408 A 5320 65C31240 DOUBLER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME DOUBLER CRACKED AT AFT CARGO DOOR FWD CUTOUT, BS 794, WL 159. R&R FRAME D OUBLER PER SRM. 2 L 7 2 4F A16WE 2001050700317 20010507 00317 NM 2001 5 7 SWAA011092 1 20010409 A 5551 6551524 FITTING BOEING 737 7372H4 138448C NM HORIZ STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D CHECK, FOUND HORIZ STAB CENTER SECTION AFT SPAR LOWER HINGE HOUSING ATTACH FITTING CORRODED AT OUTBD LUG, INBD FACE, LT SIDE. REPAIRED FITTING PER BFG ER. 2 L 7 2 4F A16WE 2001050700318 20010507 00318 NM 2001 5 7 SWAA011093 1 20010409 A 5551 6551524 FITTING BOEING 737 7372H4 138448C NM HORIZ STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D CHECK, FOUND LT HORIZ STAB CENTER SECTION REAR SPAR HINGE HOUSING LOWER INBD ATTACH CLEVIS CORRODED A T OUTBD FACE. REPAIRED FITTING PER BRG ER. 2 L 7 2 4F A16WE 2001050700319 20010507 00319 NM 2001 5 7 SWAA011094 1 20010409 A 5743 6567172 FITTING BOEING 737 7373H4 1384600 NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 355SW 25250 DURING SCHEDULED D CHECK, FOUND LT WING MLG BEAM SUPPORT LINK FITTING CORRODED ON LUG FACE. R&R BEAM FITTING PER MM. 2 L 7 2 4F RT A16WE 2001050700320 20010507 00320 2001 5 7 SWAA011095 4 20010409 A 2565 6945736 BRACKET BOEING 737 7373A4 1384585 NM SERVICE DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED 1/2D CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE FWD ATTACH BRACKET BROKEN. R&R BRACKET PER MM. 2 L 7 2 4F RT A16WE 2001050700321 20010507 00321 NM 2001 5 7 SWAA011096 1 20010408 A 5315 6546804 FLOORBEAM BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED 1/2D CHECK, FOUND FLOOR BEAM UPPER CHORD CORRODED AT BS 328, RBL 14 & RBL 28. REPAIRED FLOORBEAM PER SR M. 2 L 7 2 4F RT A16WE 2001050700322 20010507 00322 NM 2001 5 7 SWAA011097 1 20010408 A 2560 6557463 BRACKET BOEING 737 7373A4 1384585 NM CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR MOUNT BRACKETS CORRODED ON CABIN FLOOR. R&R BRACKETS PER SRM. 2 L 7 2 4F RT A16WE 2001050700323 20010507 00323 NM 2001 5 7 SWAA011098 1 20010409 A 7933 ST104Z TRANSMITTER BOEING 737 7372H4 138448C NM PWA JT8 JT8* 52044 NE NR 1 ENGINE FAULTY A SWAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 102SW 23108 707433 AIR TURNBACK, NR1 ENG OIL OVERTEMP INDICATION. SHUT DOWN ENGINE. R&R OIL FILTER, OIL TEMP BULB & PRESSURE TRANSMITTER P ER MM. PERFORMED BREATHER PRESSURE CHECK PER SWA SAM 146. NO DEFECTS NOTED. 2 L 7 2 4F 4 F A16WE E2EA 2001050700324 20010507 00324 2001 5 7 SWAA011042 4 20010405 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 074SW 22674 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001050700325 20010507 00325 NM 2001 5 7 SWAA011043 1 20010406 A 2782 6544651 ACTUATOR BOEING 737 7372H4 138448C NM L/E SLAT FAILED A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 105SW 23249 AIR TURNBACK, NR 4 L/E SLAT WOULD NOT RETRACT. VISUALLY VERIFIED SLAT NOT RETRACTED. R&R SLAT ACTUATOR PER MM. OPS & LE AK CHECK GOOD. 2 L 7 2 4F A16WE 2001050700326 20010507 00326 2001 5 7 SWAA011044 4 20010406 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 647SW 27717 FWD DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. READJUSTED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001050700327 20010507 00327 NM 2001 5 7 SWAA011045 1 20010406 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 653SW 28398 EEPLS TRACK COVER LOOSE AT ROW 14. R&R TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001050700328 20010507 00328 NM 2001 5 7 SWAA011046 1 20010405 A 3350 BR2013 LIGHT BOEING 737 7373Y0 1384671 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 665WN 23497 EEPLS LOOSE NEAR FWD SECTION. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001050700329 20010507 00329 2001 5 7 SWAA011047 4 20010406 A 2565 22D22900 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE ASSY PRESS IND OUT OF LIMITS. R&R EVAC SLIDE A SSY PER MM. 2 L 7 2 4F A16WE 2001050700330 20010507 00330 NM 2001 5 7 SWAA011048 1 20010408 A 3350 610478 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SERVICE CHECK, FOUND RT WING EXTERNAL EMERGENCY EGRESS LIGHT INOP. R&R BATTERY ASSY PER MM. 2 L 7 2 4F A16WE 2001050700331 20010507 00331 NM 2001 5 7 SWAA011049 1 20010406 A 5330 6545768 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 091SW 22963 DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 380, BELOW STR 14R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001050700332 20010507 00332 NM 2001 5 7 SWAA011050 1 20010405 A 5754 6546431 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 324SW 23414 DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBD FORE FLAP DISBONDED. R&R FORE FLAP PER MM. 2 L 7 2 4F RT A16WE 2001050700333 20010507 00333 NM 2001 5 7 SWAA011051 1 20010406 A 5754 65C26686 WEDGE BOEING 737 7373H4 1384600 NM L/E SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED C1 CHECK, FOUND NR 2 L/E SLAT T/E WEDGE DELAMINATED 4 X 18 ON UPPER SURFACE. R&R SLAT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001050700334 20010507 00334 2001 5 7 SWAA011052 4 20010405 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 642WN 27715 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. READJUSTED EVAC SLIDE ASSY P ER MM. 2 L 7 2 4F RT A16WE 2001050700335 20010507 00335 NM 2001 5 7 SWAA011053 1 20010405 A 5753 6546435 FLAP BOEING 737 7373A4 1384585 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED 1/2D CHECK, FOUND RT WING AFT FLAP DELMINATED AT INBD EDGE & CRACKED AT FWD EDGE IN FRONT OF FIRST SET OF FLIGHT BEARINGS. R&R AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2001050700336 20010507 00336 NM 2001 5 7 SWAA011054 1 20010406 A 5315 6546804 FLOORBEAM BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED 1/2D CHECK, FOUND FLOOR BEAM CORRODED AT BS 312, LBL 10 TO RBL 10. REPAIRED FLOOR BEAM PER SWA T1. 2 L 7 2 4F RT A16WE 2001050700337 20010507 00337 NM 2001 5 7 SWAA011055 1 20010406 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED SERVICE CHECK, FOUND 2 EXTERNAL FUSELAGE SKIN CRACK, L/H SIDE, AFT OF WING TO BODY FAIRING. REPAIR ED SKIN PER SRM. 2 L 7 2 4F A16WE 2001050700338 20010507 00338 NM 2001 5 7 SWAA011056 1 20010407 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 394SW 27380 EEPLS TRACK COVER MISSING AT MID CABIN. INSTALLED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001050700339 20010507 00339 NM 2001 5 7 SWAA011057 1 20010407 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED 1/4D CHECK, FOUND L/H KEEL BEAM FLANGE CORRODED AT BS 500D+2, OUTBD SURFACE. REPAIRED KEEL BEAM PER SRM . 2 L 7 2 4F RT A16WE 2001050700340 20010507 00340 NM 2001 5 7 SWAA011058 1 20010406 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SVC DOOR UPPER FWD CUTOUT. REPAIRED SKIN PER BAC SB. 2 L 7 2 4F RT A16WE 2001050700341 20010507 00341 NM 2001 5 7 SWAA011059 1 20010407 A 5312 6517582 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKS AT LBL 17.1, WL 226 & RBL 17.1, AT RETAINER HOLE, 3 ABOVE LOWER EDGE OF BEAM. REPAIRED VERTICAL BEAM WEBS PER BFG ER. 2 L 7 2 4F RT A16WE 2001050700342 20010507 00342 NM 2001 5 7 SWAA011060 1 20010406 A 5320 BAC1503 STIFFENER BOEING 737 7373Y0 1384671 NM MLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664WN 23495 DURING SCHEDULED 1/4 CHECK, FOUND BS 663.5 VERTICAL STIFFENER CRACKED AT RBL 6.15. R&R VERTICAL STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 2001050700343 20010507 00343 NM 2001 5 7 SWAA011061 1 20010407 A 5753 6546435 FLAP BOEING 737 7373Y0 1384671 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664WN 23495 DURING SCHEDULED 1/4D CHECK, FOUND RT WING OUTBD AFT FLAP DELAMINATED AT INBD END. R&R AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2001050700344 20010507 00344 NM 2001 5 7 SWAA011062 1 20010406 A 3350 65C34691 LIGHT BOEING 737 7373Q8 1384670 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED C2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 18 ABC. RELAMPED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001050700345 20010507 00345 2001 5 7 SWAA011063 4 20010406 A 2565 1061323469 SLIDE BOEING 737 7373A4 1384585 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. R&R EVAC SLIDE ASSY PER MM . 2 L 7 2 4F RT A16WE 2001050700346 20010507 00346 NM 2001 5 7 SWAA011064 1 20010406 A 3350 57771 CAP BOEING 737 7373A4 1384585 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED C3 CHECK, FOUND EEPLS END CAP MISSING AT FWD SECTION. INSTALLED END CAP PER MM. 2 L 7 2 4F RT A16WE 2001050700347 20010507 00347 NM 2001 5 7 SWAA011065 1 20010407 A 3350 610478 BATTERY PACK BOEING 737 7373A4 1384585 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED C3 CHECK, FOUND EEPLS INOP AT AFT SECTION. R&R BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2001050700348 20010507 00348 NM 2001 5 7 SWAA011066 1 20010406 A 5754 65C26602 SLAT BOEING 737 7373A4 1384585 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED C3 CHECK, FOUND NR 5 L/E SLAT DELAMINATED AT OUTBD UPPER T/E SURFACE. R&R NR 5 SLAT PER MM. 2 L 7 2 4F RT A16WE 2001050700349 20010507 00349 NM 2001 5 7 SWAA011067 1 20010407 A 5312 6516300 BULKHEAD BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT RBL 6.8, WL 201. REPAIRED BULKHEAD WEB PER SRM. 2 L 7 2 4F RT A16WE 2001050700350 20010507 00350 NM 2001 5 7 ERKR200100101 1 20010501 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 UPPER DECK WINDOW FORGING 1R HAS CORROSION PROTRUDING AROUND EDGES STA 560 TO STA 580 RIGHT SIDE S-8R TO S-10R. REMOVED UPPER DECK WINDOW FORGING FOUND IT WITHIN LIMITS PER ECRA 3203-53-047-2. ALODINED WINDOW FORGING PER 747 SRM 51-10-02 AND PRIMED WINDOW FORGING PER 747 SOPM 20-41-02. INSTALLED WINDOW FORGING PER 747 SRM 51-30-02. 2 L 7 4 4F A20WE 2001060600015 20010606 00015 NE 2001 6 6 2001UALA00595 2 20010423 A 7321 8228305039 EEC PWA PW40903 BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE LT ENGINE INADEQUATE A UALA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 WP 29 207UA 8155 1291 222103 30213 222103 TAKEOFF AT ORD LT ENG EPR 1.51 RIGHT ENG 1.48 EPR. RT THROTTLE SLIGHTLY AHEAD OF LT THROTTLE. AFTER THRUST REDUCTION, EVERYTHING MATCHED UP AND THROTTLES MARRIED UP. *S/D* PRELIM STATUS 5/4/2001: INSP ENG & ACCOMP POWER ASSURANCE RUN, NO DISCREP FOUND. PLAN TO RPL EEC PRECAUTIONARY. UNDER INVESTIGTION. REMOVED RT EEC, P2 SENSOR TESTED W/IN LIMITS. EEC SOFTWARE SCN9 CONTAINS T/O RATING TABLE ERROR THAT CAN CAUSE THRUST LIMIT SHORTFALL WHEN HIGH AIRSPEED IS SENSED FROM PT 2 BEFORE THROTTLE REACHES T/O POS. INTERIM PROBLEM MGMT: P2 SENSOR MONITORING, FULL STOP T/O PROC IN HEADWINDS. FINAL FIX WILL BE NEW EEC SOFTWARE TO BE DEVLP''''D. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001050700352 20010507 00352 WP 2001 5 7 UPS01835770 1 20010331 A 5320 3750330505N FITTING DOUG DC8 DC871F 302199D WP LOWER CARGO CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 STA. 450 LONG. 36 SPLICE FITTING IS CRACKED REMOVED AND REPLACED FITTING I.A.W. DWG. 3750330,AN D SRM. 51-1-20D 2 L 7 4 4F RT 4A25 2001050700353 20010507 00353 WP 2001 5 7 UPS01835771 1 20010402 A 5730 576960040 DOUBLER DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE: C2,3. RIGHT WING OB L/E. INTERNAL WRAPAROUND DOUBLER IS CRACKED AT XFS 572.5. REMOVED, FABRICATED, AND REPLACED DOUBLER I.A.W. DWG. 5769600,AND SRM. 51-1-21 2 L 7 4 4F RT 4A25 2001050700354 20010507 00354 WP 2001 5 7 UPS01835772 1 20010101 A 5730 576958930 DOUBLER DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 RIGHT WING L/E. INTERNAL WRAPAROUND DOUBLER IS CRACKED AT XFS 297.5 REMOVED,FABRICATED,AND REPL ACED DOUBLER I.A.W. DWG. 5769589,AND SRM. 51-1-21,51-1-20D 2 L 7 4 4F RT 4A25 2001050700355 20010507 00355 EU 2001 5 7 DHL2001367003 1 20010427 A 3610 REGULATOR VALVE AIRBUS 300 A300B4203 3930306 EU BLEED AIR FAILED A DHLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 367DH MSN265 NR 1 ENGINE REGULATOR FAULT LIGHT ILLUMINATED ON TAXI - COMPLETED ABNORMAL PROCEDURE PER AOM. LIGHT REMAINS ON.TRANSFERR ED NR 1 ENG BLEED PRESS REG TO DMI NR 5362 IAW MEL 36-11-06 CAT-C. PLACARDED , MXC NOTIFIED. *** REMOVED AND REPLACED PNEUMATIC REGULATOR PER 36-11-14. PERFORMED BITE CK PER 36-11-00. PERFORMED ENGINE RUN (JRH 16.5) LEAK CHK GOOD. DMI CLEARED. STATUS-CLOSED. 2 L 7 2 4F RT A35EU 2001050700357 20010507 00357 NM 2001 5 7 CA010423002 1 20010413 A 2424 915F2125 GCU BOEING 737 737217 1384464 NM PWA JT8 JT8D17A 52049 NE NR 1 ENGINE FAILED W O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 CA 48962 48962 UZ2297HJLN (CAN) NR 1 ENGINE GENERATOR FAILED INBOUND, NR 1 GENERATOR CONTROL PANEL REPLACED AS PER WORK CARD. 2 L 7 2 4F 4 F A16WE E2EA 2001050700358 20010507 00358 NM 2001 5 7 CA010423003 1 20010324 A 2910 82950010175 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) A HYDRAULIC LEAK DISCOVERED DURING ROUTINE MAINTENANCE RESULTED IN THE REPLACEMENT OF THE LT FLIGHT SPOILER UNLOAD ING TUBE ASSEMBLY. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001050700359 20010507 00359 NM 2001 5 7 CA010423004 1 20010325 A 2910 82920010307 TUBE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 34968 (CAN) INVESTIGATON OF SKYDROL LEAKING FROM THE PASSENGER SERVICE UNIT AT SEAT/ROW 5CD REVEALED THAT TUBE ASSEMBLIES 8292 0010-307 (GEAR DOWN), AND 82920010-263 (GEAR UP), WERE LEAKING FROM PIN HOLES IN FACTORY BENDS. THE LINES WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. DISSECTION OF THE LINES REVEALED SEVERAL SPOTS OF CORROSION ON THE INSIDE OF T HE LINES IN THE VICINITY OF THE LEAKS. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001050700366 20010507 00366 EA 2001 5 7 CA010423013 1 20010405 A 3211 AN620A BOLT DHAV DHC6 DHC6100 EA PWA PT6 PT6A20 52043 EA ATTACH FITTING SHEARED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA (CAN) BOLT ATTACHING LUG TIE ASSEMBLY (C6UFM1038-27) SHEARED. SEE DHC 1 PC + 32-15-100, ITEM 470 OF DHC-6-100. 1 H 7 2 3T 3 T A9EA E4EA 2001050700371 20010507 00371 EU 2001 5 7 CA010424007 1 20010319 A 2910 GHC1003 POWERPACK C632A0201052 UROCOP EC120 EC120B 8680987 EU TMECA ARRIUS ARRIU2F NE HYDRAULIC SYS SEIZED W E ENGINE SHUTDOWN F FLT CONT AFFECTED IN INSP/MAINT 1 CA 278 M178 (CAN) DURING NORMAL GROUND RUN-UP, HYDRAULIC TEST WAS CARRIED OUT, HYDRAULIC PRESSURE FAILED TO RETURN TO NORMAL. SHAFT BETWEEN THE HYDRO-PACK (P/N C632A2156201) WAS FOUND SHEARED AND THE PACK SEIZED.MANUFACTURES TECH REP TO ATTEND AND REPL ACE THE SHAFT AND PACK. 1 G 7 2 3U 3 U NC R0001RD E34NE 2001050700373 20010507 00373 EU 2001 5 7 CA010425005 1 20010405 A 2750 D9311 CONTACTOR BRAERO 748 HS7482B 1500248 EU TE FLAPS INTERMITTENT W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA (CAN) ON APPROACH, CREW SELECTED FLAPS TO APPRAOCH FROM 15 DEGREES. FLAPS FAILED TO MOVE. HANDLE SELECTED & DE-SELECTED SEVERAL TIMES, FLAPS OPERATED NORMALLY. FOUND UP SIDE OF REVERSING CONTACTOR FAILING INTERMITTENTLY. REPLACED CONTACTOR, NO FURTHER PROBLEMS. 2 L 7 2 3T A24EU 2001050700376 20010507 00376 EU 2001 5 7 CA010426008 1 20010330 A 2530 TERMINAL BLOCK AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FWD GALLEY MELTED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 15783 15783 (CAN) THE FORWARD GALLEY OVENS WERE FOUND TO BE INOPERATIVE BY THE FLIGHT ATENDANTS ON THE FLIGHT. THE ENGINEERS TROUBLE SHOOTING THE DEFECT FOUND FWD GALLEY FEEDER D BREAKER POPPED. FURTHER INVESTIGATION FOUND TERMINAL BLOCK 2752VT STUD 8 M ELTED, AND THE TERMINAL BLOCK STUD MISSING THE HOLD DOWN NUT. THE TERMINAL BLOCK, WIRE TERMINAL CONNECTORS WERE REPLACED AND THE ADJACENT WIRES INSPECTED AND FOUND IN SERVICEABLE CONDITION.THE AIRCRAFT HAD BEEN IN FOR IMPORTATION AND RECONF IGURATION BY AN FAA REPAIR STATION WHICH WAS COMPLETED ON 26 FEB 2001. 2 L 7 2 4F 4 F RT A28NM E311NE 2001050700383 20010507 00383 EA 2001 5 7 CA010430002 1 20010321 A 2752 854D10012 ACTUATOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAPS FAILED W O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 CA (CAN) FLAP FAIL CAUTION MESSAGE WHEN FLAP SELECTED TO 30 DEGREES FOR LANDING (FLAP LOCK OUT). REPLACED NR 4 RT FLAP ACTU ATOR AND NR 1 & 2 LT FLAP ACTUATORS ALSO REPLACED RT NR 4 FLEX SHAFT CABLE AND NR 1 & 5 LT FLEX SHAFT. WINTERIZATION OF THE SYSTEM ALSO COMPLETED. RIGGING AND OPERATION CHECK CARRIED OUT. SYSTEM FOUND SERVICEABLE. L/H ACTUATOR P/N 854D100-1 1 LT FLEX SHAFT NR 4 P/N 857SD100-7 RT FLEX SHAFT NR 1 P/N 857SD100-15 R/H FLEX SHAFT NR 5 P/N 857SD100-9 2 L 7 2 4F 4 F RT A21EA E15NE 2001050700384 20010507 00384 EA 2001 5 7 CA010430004 1 20010319 A 2750 8551009 PSU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAPS FAILED W O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) FLAP FAIL CAUTON MESSAGE ON LANDING ROLL OUT AT 70 KNOTS. RESET ATTEMPTED WITHOUT ANY SUCCESS, FLAP TWIST INSPECTI ON CARRIED OUT AND FOUND R/H END BPSU BREAK AWAY TORQUE BEYOND LIMITS.REPLACED AND RIGGED BOTH B.P.S.US.PSU P/N 855100-9 S/N 147 (R/H) AND 357 (L/H) 2 L 7 2 4F 4 F RT A21EA E15NE 2001050700386 20010507 00386 EU 2001 5 7 CA010430009 1 20010308 A 2780 DISPLAY AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE COCKPIT ECAM FAILED W H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED AP APPROACH 1 CA (CAN) SLAT ECAM (ELECTRONIC CENTRALIZED MONITORING SYSTEM)WARNING MESSAGE ON APPROACH. FLIGHT LANDED WITH NO SLATS WITH FLAP A THREE POSITION AS PER QRHI.RESET OF THE SYSTEM ON THE GROUND COMPLETED, SYSTEM FOUND SERVICEABLE. 2 L 7 2 4F 4 F RT A28NM E29NE 2001050700387 20010507 00387 EU 2001 5 7 CA010430012 1 20010327 A 5280 SEAL AIRBUS A340 A340313 EU CFMINT CFM56 CFM565C4 13802 NE MLG DOOR FAULTY W O OTHER N FALSE WARNING CL CLIMB 1 CA (CAN) CENTER RIGHT END LANDING GEAR DOOR WARNING MESSAGE SHOWING THE DOOR NOT CLOSED.DOOR UPLOCK AND DOOR ACTUATOR CHANG ED WITHOUT ANY SUCCESS. FOUND TO BE THE DOOR ZONE 2 SEALS AT FAULT.REPOSITION OF THE NR 2 SEALS LT AND RT, GEAR SWING CA RRIED OUT AND CHECK SERVICEABLE. 2 L 7 4 4F 4 F RT A197 E37NE 2001050700388 20010507 00388 WP 2001 5 7 CA010430015 1 20010407 A 5230 RETAINER LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21122B02 54555 NE CARGO DOOR BROKEN W A UNSCHED LANDING O OTHER CL CLIMB 1 CA (CAN) AFTER TAKEOFF AT 20,000 FEET, AIRCRAFT EXPERIENCED PRESSURIZATION PROBLEMS AND CREW COULD HEAR A KNOCKING SOUND AG AINST THE FUSELAGE ON THE RT SIDE. CREW PERFORMED RAPID DE-PRESSURIZATION DRILL AND REGAINED CONTROL OF PRESSURIZATION. CREW DUMPED FUEL AND DIVERTED TO LAND THE AIRCRAFT.MAINTENANCE FOUND SEAL RETAINER AND CARGO DOOR SEAL DAMAGED AND EXTRU DED FROM THE AIRCRAFT. MAINTENANCE REPLACED THE SEAL AND RETAINER AND RETURNED THE AIRCRAFT TO SERVICE. 2 L 7 3 4F 4 F A23WE E12EU 2001050700390 20010507 00390 WP 2001 5 7 CA010430017 1 20010409 A 5270 PROXIMITY SWITCH LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE CARGO DOOR OUT OF ADJ W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA (CAN) DURING CLIMB C1A CARGO DOOR OPEN LIGHT CAME ON AT 6.5 DIFF PRESSURE, AIRCRAFT RETURNED TO BASE. DURING DESCENT THE LITE EXTINGUISHED AT 4.5 DIFF PRESSURE.MAINTENANCE INSPECTED DOOR CLOSING AND LOOKING MECHANISM NO FAULT FOUND. DOOR RI GGING CHECKED FOUND THE PROXIMITY SWITCHES AT THE MAXIMUM TOLERANCE OF AMM, SWITCHES READJUSTED TO THE MINUMUM LIMITS AN D AIRCRAFT RELEASED FOR A TEST FLIGHT.TEST FLIGHT FOUND THE SYSTEM SERVICEABLE. 2 L 7 3 4F 4 F A23WE E12EU 2001050700404 20010507 00404 EU 2001 5 7 SIMA0564 1 20010225 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 545AT 545 DFW - DURING SCHEDULED PS CHECK MAINTENANCE, REPORTED THE AFT FLOOR PROXIMITY LIGHT HAD EVERY OTHER LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK IN POWER SUPPLY UNIT 73WL. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED T O SERVICE. (M) 2 H 7 2 4T RT A53EU 2001050700405 20010507 00405 EU 2001 5 7 SIMA0955 1 20010405 A 2420 1030032 SENSOR AEROSP ATR72 ATR72212 EU RT NACELLE INOPERATIVE A SIMA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 SW 21 533AT 533 DFW - FLT 3565 - CREW REPORTED THE NR 1 DC GENERATOR FAULTED AFTER TAKEOFF. SYSTEM WOULD NOT RESET PER AOM PROCEDURES. MAINTENANCE REMOVED AND REPLACED THE HALL EFFECT SENSOR IN THE RIGHT NACELLE. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETU RNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001050700406 20010507 00406 EU 2001 5 7 SIMA0956 1 20010405 A 3350 5211309111 LIGHT AEROSP ATR72 ATR72212 EU GALLEY DAMAGED A SIMA O OTHER O OTHER DE DESCENT 1 SW 21 308AE 309 MIA - FLT 5350 - FLIGHT ATTENDANT REPORTED THE FIRST FLOOR PROXIMITY EMERGENCY LIGHT IN THE GALLEY AREA TO BE IN NEED OF REPAIR. MAINTENANCE REPLACED THE LIGHT ASSEMBLY IN THE GALLEY AREA. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO S ERVICE. (M) 2 H 7 2 4T RT A53EU 2001050700407 20010507 00407 EU 2001 5 7 SIMA0541 1 20010223 A 2611 WARNING SYSTEM SAAB SF340 340B 7860101 EU COCKPIT FALSE ACTIVATION A SIMA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 21 397AE 340B397 SBP - LAVATORY SMOKE WARNING ALONG WITH MASTER WARNING SOUNDED IN CRUISE AND THEN SELF EXTINGUISHED AFTER ABOUT ONE SECO ND. MAINTENANCE CLEANED LAVATORY SMOKE DETECTOR. OPS CHECK WAS GOOD IAW SAAB AMM 26-13-00. NO FURTHER ACTION REQUIRED . AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050700408 20010507 00408 EU 2001 5 7 SIMA0543 1 20010223 A 2400 31342001 GENERATOR SAAB SF340 340B 7860101 EU RT ENGINE INOPERATIVE A SIMA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SW 21 387AE 340B387 DFW - FLT 3257 - FOUND CREW REPORTED THE RIGHT AC GENERATOR FAILED IN FLIGHT, RESET AND STILL FAILED. CREW RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED RIGHT AC GENERATOR IAW SAAB MM. OPS AND LEAK WAS GOOD AND AIRCRAFT WAS RETURNE D TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050700409 20010507 00409 EU 2001 5 7 SIMA0551 1 20010224 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 250AE 340B250 LAX - FLT 3085 - CREW REPORTED EMERGENCY FLOOR LIGHTS AT ROW 6 AND 7 EXTINGUISH AFTER 40 SECONDS. MAINTENANCE REMOVED A ND REPLACED POWER SUPPLY UNIT 22LN IAW SAAB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050700410 20010507 00410 EU 2001 5 7 SIMA0552 1 20010224 A 3350 MS274061 SWITCH SAAB SF340 340B 7860101 EU F/A PANEL INOPERATIVE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 278AE 340B278 LAX - FLT 3110 - FLIGHT ATTENDANT CONTROL PANEL EMERGENCY ARMED LIGHT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT SWITCH IAW SAAB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050700412 20010507 00412 EU 2001 5 7 SIMA0631 1 20010304 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 904AE 340B314 TYR - FLT 3738 - DURING PRE-FLIGHT, THE FLIGHT ATTENDANT INFORMED THE CREW THAT TWO EMERGENCY LIGHTS WERE INOPERATIVE. AIRCRAFT WAS FERRIED TO DFW FOR MAINTENANCE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN POWER SUPPLY UNIT 21L N. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050700413 20010507 00413 EU 2001 5 7 SIMA0632 1 20010304 A 3411 PITOT LINE SAAB SF340 340B 7860101 EU PITOT STATIC SYS CONTAMINATED A SIMA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 SW 21 254AE 340B254 SBA - FLT 3146 - CREW REPORTED DURING CRUISE AT 19,000 FT, BOTH THE FIRST OFFICER AND STANDBY AIRSPEED INDICATORS WENT T O ZERO. EMERGENCY WAS DECLARED AND AIRCRAFT DIVERTED TO SBA. BOTH AIRSPEED INDICATORS RESUMED WHILE DESCENDING THROUGH 10,000 FEET. MAINTENANCE DRAINED AND PURGED WATER FROM PITOT SYSTEM. PERFORMED PITOT STATIC LEAK CHECK AND RETURNED A IRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050700414 20010507 00414 EU 2001 5 7 SIMA0633 1 20010304 A 3320 BV033020250 SOCKET SAAB SF340 340B 7860101 EU CABIN BROKEN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 247AE 340B247 SBP - FOUND FLUORESCENT SOCKETS AT WINDOW SEATS 5C AND 12A ARE BROKEN. REPLACED LAMP SOCKETS IAW SAAB AMM 33-21-20. (M ) 2 L 7 2 4T RT A52EU 2001050700415 20010507 00415 EU 2001 5 7 20010504AP001 1 20010304 A 3320 BV033000250 SOCKET SAAB SF340 340B 7860101 EU CABIN BROKEN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 247AE 340B247 SBP - FOUND FLUORESCENT SOCKETS AT WINDOW SEATS 5C AND 12A ARE BROKEN. REPLACED LAMP SOCKETS IAW SAAB AMM 33-21-20. RE F SIMA0633. (M) 2 L 7 2 4T RT A52EU 2001050700416 20010507 00416 EU 2001 5 7 SIMA0699 1 20010310 A 3350 3071BPGEGPC BULB SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA O OTHER O OTHER UK UNKNOWN 1 SW 21 273AE 340B273 DFW - FLT 3819 - FOUND EMERGENCY LIGHT OUT AT SEAT 9B. REPLACED BULB, OPS CHECK WAS GOOD. (M) 2 L 7 2 4T RT A52EU 2001050700417 20010507 00417 EU 2001 5 7 SIMA0725 1 20010313 A 3350 1317 LAMP SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 268AE 340B268 JFK - FLT 5068 - EMERGENCY LIGHT OUT AT SEAT 14A IS INOPERATIVE. MAINTENANCE REPLACED LAMP AT SEAT 14A IAW SF340 MM 33- 50-00. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050700418 20010507 00418 SO 2001 5 7 SIMA200109802 1 20010408 A 7800 WARNING SYSTEM EMB 135 EMB135LR SO NR 2 ENGINE ACTIVATED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 734EK 145371 ORD - FLT 4097 - ENGINE 2 REV DISAGREE CAUTION CAME ON DURING TAKEOFF ROLL, MEL 7802 OPENED. (M) 2 L 7 2 4F RT TOOO11AT 2001050700421 20010507 00421 NE 2001 5 7 SIMA200101003 2 20010110 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE NR 1 AND 2 MALFUNCTIONED A SIMA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SW 21 394AE 340B394 LRD - FLT 3301 - POWER ROLL BACK, FL 200; -18C; SOLID IMC. NO BREAK IN CLOUDS. ENGINE ANTI-ICE ON. OBSERVED A POWER R OLLBACK AND RELIGHT ON NR 1 ENGINE. APPROX 1 OR 2 MINUTES LATER OBSERVED SIMILAR ROLLBACKS OF BOTH ENGINES. EACH ENGINE ROLLED BACK AND RELIT 2 OR 3 TIMES IN RAPID SUCCESSION. COMMENCED DESCENT TO 8000 (+10 OAT) AND NO FURTHER DISCREPANCI ES NOTED. INSPECTED NR 1 AND 2 ENGINE IAW GE MM 72-00 FAULT ISOL. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M ) 2 L 7 2 4T 4 T RT A52EU E8NE 2001050700422 20010507 00422 EU 2001 5 7 SIMA200100802 1 20010108 A 2910 7229162045 TUBE SAAB SF340 340B 7860101 EU RT LANDING GEAR LEAKING A SIMA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 280AE 340B280 DFW - FLT 3787 - LOSS OF HYDRAULIC QUANTITY AND MAIN ACCUMULATOR PRESSURE FOLLOWED BY LOSS OF OUTBOARD AND INBOARD BRAKE PRESSURE AFTER LANDING. REMOVED AND REPLACED HYDRAULIC LINE FROM DOWNLOCK TO SWIVEL ON RT SIDE IAW AMM (LANDING GEAR E XPLOSIVE WERE REMOVED AND REPLACED). OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001050700424 20010507 00424 SO 2001 5 7 SIMA200101301 1 20010113 A 2400 CS50006004A RELAY EMB 135 EMB135LR SO COCKPIT INOPERATIVE A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 730KW 145346 BOS - FLT 4745 - CREW REPORTED ELECTRICAL SMELLING SMOKE IN COCKPIT. LANDED IN BOS WITHOUT INCIDENT. MAINTENANCE REPLA CED THE TAT 2 CURRENT SENSOR RELAY AND SOCKET XK0494. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE (M) 2 L 7 2 4F RT TOOO11AT 2001050700425 20010507 00425 SO 2001 5 7 20010504AP002 1 20010113 A 3320 S5009140 SOCKET EMB 135 EMB135LR SO COCKPIT DAMAGED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 730KW 145346 BOS - FLT 4745 - CREW REPORTED ELECTRICAL SMELLING SMOKE IN COCKPIT. LANDED IN BOS WITHOUT INCIDENT. MAINTENANCE REPLA CED THE TAT 2 CURRENT SENSOR RELAY AND SOCKET XK0494. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIM A200101301. (M) 2 L 7 2 4F RT TOOO11AT 2001050700428 20010507 00428 EU 2001 5 7 SIMA200100101 1 20010101 A 3350 8GS00542405 BULB SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 180AE 340B180 DFW - FLT 3322 - CREW REPORTED FLOOR PROXIMITY EMERGENCY LIGHT NEXT TO SEAT 4B IS INOPERATIVE. MAINTENANCE REPLACED FLO OR EMERGENCY LIGHT BULB AT SEAT 4B. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050700429 20010507 00429 EU 2001 5 7 SIMA200100301 1 20010103 A 3110 CONNECTOR SAAB SF340 340B 7860101 EU COCKPIT DIRTY A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 343SB 340B343 JFK - FLT 5102 - CREW REPORTED SMOKE FROM FIRST OFFICERS SIDE EFIS AREA DURING START UP. MAINTENANCE INSPECTED AND FOUN D EXCESSIVE DUST ACCUMLATION ON RIGHT SIDE FLOURESCENT TUBE ELECTRICAL CONNECTORS. MAINTENANCE CLEANED CONNECTORS AND F LOOD LIGHT CONTROL SWITCHES. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050700430 20010507 00430 EU 2001 5 7 SIMA200100801 1 20010108 A 3350 1317 BULB SAAB SF340 340B 7860101 EU CABIN BURNED OUT A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 344SB 340B344 YUL - FLT 4748 - FOUND 4A OVERHEAD LIGHT INOPERATIVE ISSUED MEL 33-13 AUTH 010220 CAT C. REMOVED AND REPLACED OVERHEAD EMERGENCY LIGHT IAW SAAB AMM 33-52-00. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001050700432 20010507 00432 EU 2001 5 7 SIMA200103001 1 20010130 A 5610 8103731 WINDSHIELD SAAB SF340 340B 7860101 EU COCKPIT CRACKED A SIMA O OTHER O OTHER CR CRUISE 1 SW 21 313AE 340B313 BOS - FLT 4617 - DURING CRUISE, FLIGHT CREW REPORTED THE CAPTAINS WINDSCREEN CRACKED. REMOVED AND REPLACED WINDSHIELD I AW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001050700433 20010507 00433 SO 2001 5 7 SIMA200103503 1 20010204 A 3610 A7257226 O-RING EMB 145 EMB145LR SO RT WING LEAKING A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 624AE 145111 ORD - FLT 4047 - AFTER DEPARTURE FROM ORD RT/ENG BLEED LEAK LIGHT ILLUMINATED. CREW ELECTED TO RETURN TO ORD. REMOVED AND REPLACED O-RING AT RIGHT OVERWING BLEED IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT T00011AT 2001050700434 20010507 00434 SO 2001 5 7 SIMA200102003 1 20010120 A 2740 3621001007 CONTROL UNIT EMB 145 EMB145LR SO HORIZONTAL STAB FAILED A SIMA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SW 21 622AE 145108 CID - FLT 3954 - AFTER TAKEOFF, THE CAPTAIN AND FIRST OFFICERS YOKE TRIM SWITCHES FAILED. REMVOED AND REPLACED HORIZONT AL STABILIZER CONTROL UNIT IAW AMM. OPS CHECK GOOD. FCF GOOD. (M) 2 L 7 2 4T RT T00011AT 2001050700435 20010507 00435 EU 2001 5 7 SIMA200102802 1 20010128 A 5610 163500110 WINDSHIELD STBROS SD3 SD360 8100606 EU COCKPIT CRACKED A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 711PK SH3696 ORD - FLT 4035 - DURING TAKEOFF, FIRST OFFICERS WINDSCREEN OUTER PLY CRACKED. REMOVED AND REPLACED WINDSHIELD IAW AMM. OPS CHECK GOOD. (M) 2 H 7 2 4T A41EU 2001050700436 20010507 00436 SO 2001 5 7 SIMA200103601 1 20010205 A 7830 ACTUATOR EMB 145 EMB145LR SO THRUST REVERSER MALFUNCTIONED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 608AE 145068 SGF - FLT 3560 - ON TAKEOFF ROLL, HAD TR1 DISAGREE, ABORTED TAKEOFF AND RETURNED TO GATE. ENGINE 1 THRUST REVERSER PUT ON MEL AT THIS TIME. MAINTENANCE ADJUSTED UPPER AND LOWER T/R ACTUATORS ON NR 1 ENGINE IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001050700437 20010507 00437 SO 2001 5 7 SIMA200102703 1 20010127 A 2740 3622001001 ACTUATOR EMB 145 EMB145LR SO HORIZONTAL STAB FAILED A SIMA A UNSCHED LANDING P F NO WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 SW 21 622AE 145108 MEM - FLT 3256 - DURING CLIMB, CREW REPORTED CHATTERING NOISE FROM RELAYS FOLLOWED BY THE PITCH TRIM SWITCHES FOR THE FI RST OFFICER AND THE CAPTAIN NOT RESPONDING. CREW RETURNED TO MEM. DURING RETURN CREW HEARD ONE CLICK FROM A RELAY FOLL OWED BY BOTH FIRST OFFICER AND CAPTAINS PITCH TRIM SWITCHES WORKING. AIRCRAFT WAS LANDED SAFELY. REMOVED AND REPLACED HORIZONTAL STABILIZER CONTROL ACTUATOR IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT T00011AT 2001050700438 20010507 00438 SO 2001 5 7 SIMA200103201 1 20010201 A 3411 PITOT LINE EMB 145 EMB145 SO PITOT STATIC SYS CONTAMINATED A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 610AE 145073 HOU - FLT 3618 - ON TAKEOFF ROLL, AIRSPEED SPLIT OF 7 KNOTS, CAPTAIN WAS 80 KNOTS AND F/OS WAS 73 KNOTS. RETURNED TO GA TE FOR REPAIR. FERRIED A/C TO DFW. MOISTURE IN NUM 2 PITOT LINES. AIR OUT SYSTEM WITH NITROGEN. OPS CHECK GOOD. (M) 2 L 7 2 4F RT T00011AT 2001050700439 20010507 00439 SO 2001 5 7 SIMA200101802 1 20010118 A 3350 RPS1B BATTERY PACK EMB 145 EMB145LR SO CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 643AE 145200 CRP - FLT 3856 - FLOOR PROXIMITY EMERGENCY LIGHTS AT SEAT ROWS 8-11 ARE INOPERATIVE. MAINTNANCE REMOVED AND REPLACED BA TTERY PACK. OPS CHECK AS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001050700440 20010507 00440 2001 5 7 SIMA200101401 4 20010119 A 3417 INDICATOR EMB 135 EMB135LR SO COCKPIT MALFUNCTIONED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 719AE 145276 CMH - FLT 4544 - DURING TAKEOFF ROLL, CREW NOTED E1 N1 LOW SPEED INDICATION. CREW RETURN TO GATE SAFELY. NO FURTHER IN CIDENTS WERE REPORTED. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. INDICATION WENT AWAY WHEN AIRCRAFT RETURNED TO GAT E. RESET FADECS. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001050700441 20010507 00441 EU 2001 5 7 SIMA200102202 1 20010101 A 5315 S5337241122402 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AT 431 SAW - DURING MBV-1 INSPECTION MAINTENANCE REPORTED FLOORBEAM 32 HAD AN OVERSIZED HI-LOCK HOLES AT THE LEFT AFT SEAT TRAC K ATTACH POINT. MAINTENANCE REPAIRED THE FLOORBEAM IAW SRM 53-00-00 FIGURE 429. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001050700442 20010507 00442 EU 2001 5 7 SIMA200102201 1 20010101 A 5315 S5337241122402 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AT 431 SAW - DURING MBV-1 INSPECTION MAINTENANCE REPORTED FLOORBEAM 30 HAD AN OVERSIZED HI-LOCK HOLES AT THE LEFT AFT SEAT TRAC K ATTACH POINT. MAINTENANCE REPAIRED THE FLOORBEAM IAW SRM 53-00-00 FIGURE 435. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001050700443 20010507 00443 EU 2001 5 7 SIMA200102002 1 20010120 A 2150 A/C PACK AEROSP ATR72 ATR72212 EU A/C BAY STUCK A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 498AT 498 CRP - FLT 3858 - CREW REPORTED AFTER TAKEOFF BOTH PACKS STUCK OPEN. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. AIRCR AFT POWER WAS REMOVED THEN AIRCRAFT WAS RESTARTED WITH NO DEFECTS NOTED. (M) 2 H 7 2 4T RT A53EU 2001050700444 20010507 00444 EU 2001 5 7 SIMA200102701 1 20010124 A 5230 S5237651922251 HINGE AEROSP ATR42 ATR42300 8680920 EU CARGO DOOR CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 255AE 254 SAW - AIRCRAFT FERRIED TO SAW FROM MCO FOR REPAIR. CARGO DOOR FORWARD PIANO HINGE HAD FOUR CRACKED LUGS FOUND DURING RE INSPECT OF TDMI 255520198. MAINTENANCE REMOVED AND REPLACED THE FORWARD HINGE IAW CMM 52-31-00. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001050700445 20010507 00445 EU 2001 5 7 SIMA200102102 1 20010121 A 3350 3011151 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 223AT 223 MCO - FLT 10 - DURING OVERNIGHT MAINTENANCE, SEVERAL FLOOR PROXIMITY EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAI NTENANCE REMOVED AND REPLACED BATTERY PACK IN POWER SUPPLY UNIT 29WL. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO S ERVICE. (M) 2 H 7 2 4T RT A53EU 2001050700446 20010507 00446 EU 2001 5 7 SIMA200101803 1 20010118 A 2121 EVCTA465B FAN SAAB SF340 340B 7860101 EU CABIN BURNED A SIMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 370AM 340B370 DFW - FLT 3669 - FOUND CREW REPORTED LEFT RECIRCULATION FAN TO BE INOPERATIVE. WHEN TURNED ON CABIN FILLED WITH SMOKE, AIRCRAFT WAS EVACUATED. MAINTENANCE REMOVED AND REPLACED LEFT RECIRCULATION FAN AND FILTER. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050700447 20010507 00447 SO 2001 5 7 SIMA200101801 1 20010118 A 3110 S5009140 SOCKET EMB 145 EMB145LR SO COCKPIT FAILED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 647AE 145222 CRW - FLT 4020 - FOUND CREW REPORTED NR 2 PITOT FAIL ON EICAS AND THAN HAD AN ELECTRICAL SMELL THROUGHOUT CABIN AND COCK PIT. CREW MADE AN EMERGENCY LANDING WITHOUT INCIDENT IN CRW. MAINTENANCE REMOVED AND REPLACED RELAY AND SOCKET. OPS C HECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001050700448 20010507 00448 SO 2001 5 7 20010504AP003 1 20010118 A 3110 MS2774318 RELAY EMB 145 EMB145LR SO COCKPIT FAILED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 647AE 145222 CRW - FLT 4020 - CREW REPORTED NR 2 PITOT FAIL ON EICAS AND THAN HAD AN ELECTRICAL SMELL THROUGHOUT CABIN AND COCKPIT. CREW MADE AN EMERGENCY LANDING WITHOUT INCIDENT IN CRW. MAINTENANCE REMOVED AND REPLACED RELAY AND SOCKET. OPS CHECK W AS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001050700449 20010507 00449 EU 2001 5 7 SIMA200101201 1 20010112 A 3350 44 BULB AEROSP ATR72 ATR72212 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 308AE 309 MIA - FLT 5236 - MAIN CABIN DOOR EMERGENCY ENTRY LIGHT IS INOPERATIVE. MAINTENANCE REPLACED ENTRY EMERGENCY LIGHT BULB. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001050700450 20010507 00450 EU 2001 5 7 SIMA200100601 1 20010106 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 541AT 541 SGF - FOUND EMERGENCY BATTERY PACK LOCATION 4A AND B INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IAW 33-41-21. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 2001050700451 20010507 00451 EU 2001 5 7 SIMA200101602 1 20010116 A 3350 LIGHT AEROSP ATR72 ATR72212 EU CABIN LOOSE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 DFW - FLT 3826 - EMERGENCY FLOOR LIGHT IN AFT GALLEY IS LOOSE FROM FLOORBOARD. MAINTENANCE RESECURED LIGHT ASSEMBLY TO FLOORBOARD. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001050700452 20010507 00452 EU 2001 5 7 SIMA200102801 1 20010128 A 2435 O-RING AEROSP ATR42 ATR42300 8680920 EU NR 2 ENGINE S/G DAMAGED A SIMA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SW 21 141AE 141 MIA - FLT 5277 - DURING FLIGHT, THE NR 2 ENGINE WAS SHUTDOWN DUE TO LOW OIL PRESSURE AND BOTH OIL LIGHTS FLASHING. MAIN TENANCE INSPECTED ENGINE AND FOUND THE STARTER GENERATOR DRIVE SHAFT O-RING WAS DAMAGED. MAINTENANCE REPLACED THE O-RIN G ON STARTER GENERATOR SHAFT. OPS AND LEAK CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERIVCE. (M) 2 H 7 2 4T RT A53EU 2001050700453 20010507 00453 EU 2001 5 7 SIMA200101501 1 20010115 A 3350 3011210 LIGHT AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 293AT 293 MIA - FLT 5229 - CREW REPORTED EXTERIOR EMERGENCY LIGHT IN PASSENGER DOOR IS INOPERATIVE. MAITNENANCE REMOVED AND REPLA CED LIGHT ASSEMBLY IAW ATR MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001050700454 20010507 00454 SO 2001 5 7 SIMA200101804 1 20010118 A 2731 SW3094301 SWITCH EMB 145 EMB145LR SO PITCH TRIM FAILED A SIMA O OTHER F FLT CONT AFFECTED LD LANDING 1 SW 21 635AE 145158 CID - FLT 4236 - CREW REPORTED PITCH TRIM 1 FAIL ON APPROACH. MAINTENANCE REMOVED AND REPLACED CAPTAIN AND FIRST OFFICE RS PITCH TRIM YOKE SWITCHES AND THE HSCU. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001050700455 20010507 00455 SO 2001 5 7 20010504AP004 1 20010118 A 2740 3621001007 CONTROL UNIT EMB 145 EMB145LR SO HORIZONTAL STAB FAILED A SIMA O OTHER F FLT CONT AFFECTED LD LANDING 1 SW 21 635AE 145158 CID - FLT 4236 - CREW REPORTED PITCH TRIM 1 FAIL ON APPROACH. MAINTENANCE REMOVED AND REPLACED CAPTAIN AND FIRST OFFICE RS PITCH TRIM YOKE SWITCHES AND THE HSCU. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200101804. (M) 2 L 7 2 4T RT T00011AT 2001050700456 20010507 00456 EU 2001 5 7 SIMA200102702 1 20010127 A 3350 192411A FUSE SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 266AE 340B266 SBP - FLT 3207 - EMERGENCY LIGHT ABOVE SEAT 11A IS INOPERATIVE. MAINTENANCE REPLACED BULB AT SEAT 11A AND FUSE AT POSIT ION 76LN. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050700457 20010507 00457 EU 2001 5 7 20010504AP005 1 20010127 A 3350 1317 BULB SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 266AE 340B266 SBP - FLT 3207 - EMERGENCY LIGHT ABOVE SEAT 11A IS INOPERATIVE. MAINTENANCE REPLACED BULB AT SEAT 11A AND FUSE AT POSIT ION 76LN. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200102702. (M) 2 L 7 2 4T RT A52EU 2001050700458 20010507 00458 EU 2001 5 7 SIMA200103301 1 20010202 A 3350 1317 BULB SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 278AE 340B278 SBP - MAINTENANCE REPORTED EMERGENCY LIGHT AT SEATS 5BC IS INOPERATIVE. MAINTENANCE REPLACED BULB AT SEAT 5BC. OPERATI ONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050700459 20010507 00459 EU 2001 5 7 SIMA200103502 1 20010204 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 906AE 340B348 DFW - FLT 3613 - FOUND FLOOR PROXIMITY LIGHT AT SEAT POSITION 4B IS INOPERATIVE. PUT ON MEL AT THIS TIME. (M) 2 L 7 2 4T RT A52EU 2001050700460 20010507 00460 EU 2001 5 7 SIMA200102805 1 20010128 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 548AT 548 DFW - FOUND EMERGENCY LIGHTS WILL NOT COME ON WITH EXTERNAL POWER, MAIN BATTERIES OFF. MAINTENANCE REMOVED AND REPLACED BATTERY PACK FOR POWER SUPPLY UNIT AT OVERHEAD BIN 1AB. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVIC E. (M) 2 H 7 2 4T RT A53EU 2001050700461 20010507 00461 EU 2001 5 7 SIMA200102804 1 20010128 A 3320 EO33601 SOCKET AEROSP ATR72 ATR72212 EU CABIN BURNED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 440AM 440 MCO - FLT 5262 - CREW REPORTED AN ELECTRICAL BURNING SMELL IN FLIGHT. AIRCRAFT RETURN TO MCO. MAINTENANCE FOUND AN OVE RHEAD FLUORESCENT TUBE SOCKET DAMAGED. SOCKET WAS REMOVED AND REPLACED IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRC RAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001050700463 20010507 00463 EU 2001 5 7 SIMA200101002 1 20010110 A 3040 2311M961 MOTOR SAAB SF340 340B 7860101 EU WINDSHIELD WIPER FAILED A SIMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 211NE 340B211 DFW - FLT 3583 - ELECTRICAL SMOKE SMELL IN COCKPIT. FOUND CAPTAINS SIDE WIPER MOTOR TO BE THE SOURCE. REPLACED WIPER M OTOR IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001050700464 20010507 00464 EU 2001 5 7 SIMA200100401 1 20010104 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 332AE 340B332 LAX - FLT 3015 - CREW REPORRED THE EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPS CHECK OF EMERGENCY LIGHTS WAS COMPLIED WITH IAW SAAB MM 33-50-00. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050700465 20010507 00465 EU 2001 5 7 SIMA200101902 1 20010119 A 3350 1317 BULB SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 305AE 340B305 JFK - FLT 5060 - CREW REPORTED THREE FLOOR PROXIMITY LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED THREE BULBS AT POSI TION 4B, 9B, AND 11B. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050700466 20010507 00466 EU 2001 5 7 SIMA200102101 1 20010121 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 312AE 340B312 BFL - FLT 3130 - FLOOR PROXIMITY EMERGENCY ESCAPE MARKING SYSTEM LIGHT AT 8B EXIT AND 9B ARE INOPERATIVE LIGHTS 3B AND 4 B ARE INTERMITTENT, CABIN OVERHEAD LIGHTS EMERGENCY ARE INTERMITTENT AT 3C, 5C, 4A, 9A, 11A. FERRIED AIRCRAFT TO LAX FOR REPAIRS. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLIES 20LN, 21LN, 22LN, 23LN, AND 24LN, (S/N''S 184 35, 18070, 18419, 18434, 19438). OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050700467 20010507 00467 EU 2001 5 7 SIMA200102001 1 20010120 A 3350 1317 BULB SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 177AE 340B177 SHV - FLT 3315 - FOUND OVERHEAD EMERGENCY LIGHT AT SEAT 5BC IS INOPERATIVE. MAINTENANCE REPLACED BUBL IN LIGHT ASSEMBLY . OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050700468 20010507 00468 EU 2001 5 7 SIMA200104301 1 20010212 A 3350 LIGHT AEROSP ATR72 ATR72212 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 420AT 420 MIA - MAINTENANCE EMERGENCY LIGHT ASSEMBLY IN THE GALLEY AREA IS LOOSE. PUT ON MEL AT THIS TIME. MAINTENANCE RESECURED LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001050700469 20010507 00469 EU 2001 5 7 SIMA200103501 1 20010204 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 231AE 340B231 DFW - FLT 3329 - FOUND OVERHEAD EMERGENCY LIGHT AT 7A IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY UNI T IAW SAAB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050700470 20010507 00470 EU 2001 5 7 SIMA200104101 1 20010210 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 345SB 340B345 SYR - FLT 4863 - FOUND CREW REPORTED OVERHEAD LIGHT AT SEAT 12C IS INOPERATIVE. PUT ON MEL AT THIS TIME. (M) 2 L 7 2 4T RT A52EU 2001050700471 20010507 00471 EU 2001 5 7 SIMA200104801 1 20010217 A 3350 66362 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 397AE 340B397 PSP - FLT 3092 - CREW REPORTED FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE AT SEAT 4A AND 5A. MAINTENANCE REPLACED FLO OR LIGHT STRIP AT SEATS 4A AND 5A. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050700472 20010507 00472 NM 2001 5 7 20010503CW010 1 20010311 A 3244 TIRE BOEING 737 737222 1384473 NM NR 4 DEFLATED E KNNB O OTHER O OTHER LD LANDING 1 WP 25 135TA 19940 LANDING, NR 4 TIRE DEFLATED. TIRE HAS FLAT SPOT AND HOLE ON TREAD SURFACE FROM SKIDDING DURING LANDING. REMOVED AND RE PLACED BURST TIRE INSPECTION WAS PERFORMED. NO FURTHER DISCREPANCIES WERE NOTED. 2 L 7 2 4F A16WE 2001050700473 20010507 00473 CE 2001 5 7 20010503CW011 1 20010325 A 3231 DOOR CESSNA 500 550 2076604 CE PWA JT15 JT15D1 52060 NE NLG OUT OF RIG E UG8A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 225J 5500283 DURING CLIMB, GEAR WOULD NOT LOCK UP. PER COCKPIT GEAR LIGHT INDICATION. APPARENT CAUSE IS GEAR RIGGING. RIGGED NOSE LANDING GEAR DOORS. OPERATIONAL CHECK NORMAL. 1 L 7 2 4F 4 F A22CE E1NE 2001050700474 20010507 00474 EA 2001 5 7 WVBA2001020 2 20010405 A 8520 5015 STUD PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA RT ENGINE LEAKING E WVBA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 01 792FC 317552108 L245068A DURING INSPECTION EXCESSIVE OIL WAS OBSERVED IN BOTTOM OF COWLING OF RIGHT ENGINE. THE LEAK WAS TRACED TO THE TWO FORWA RD HOLD DOWN STUDS OF NR 2 CYLINDER. NOTE THESE ARE NOT THRU STUDS. THE CYLINDER WAS REMOVED AND OIL OBSERVED LEAKING FROM AROUND THE THREADS. THE STUDS WERE REMOVED BREAKING TORQUE WAS 8FT LBS. STUDS WERE REINSTALLED TO SPECS BUT STUD HEIGHT WAS INCORRECT. OVER SIZE STUDS WERE INSTALLED TO SPECS. RUN UP AND LEAK CHECK GOOD. UNABLE TO DETERMNE IF CASE OR STUDS CAUSED LEAKS. 1 L 7 2 3O 3 O A20SO E14EA 2001050700475 20010507 00475 SO 2001 5 7 SIMA200104601 1 20010215 A 3040 HEATER EMB 145 EMB145LR SO WINDSHIELD FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 635AE 145158 ORD - FLT 4114 - IN CRUISE WINDSHIELD 1 HEAT FAILED. RETURN TO ORD FOR MAINTENANCE REPAIR. MAINTENANCE COMPLIED WITH E NGINEERING ORDER EM 3000-018, WINDSHIELD HEATING IMPROVEMENT. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001050700476 20010507 00476 EU 2001 5 7 SIMA200101202 1 20010112 A 2434 23080031 GENERATOR SAAB SF340 340B 7860101 EU LEFT ENGINE INOPERATIVE A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 297AE 340B297 ALB - FLT 5012 - CREW REPORTED THE LEFT DC GENERATOR LIGHT ILLUMINATED IN FLIGHT. RESET PER AOM, GENERATOR LIGHT STILL REMAINED ILLUMINATED. MAINTENANCE REMOVED AND REPLACED LEFT DC GENERATOR IAW SAAB MM. OPS AND LEAK CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050700477 20010507 00477 EU 2001 5 7 SIMA200101204 1 20010112 A 2530 38512 CONNECTOR SAAB SF340 340B 7860101 EU GALLEY BURNED A SIMA O OTHER B S SMOKE/FUMES/ODORS/SPARKS AFFECT SYSTEMS DE DESCENT 1 SW 21 335AE 340B335 FAT- FLT 3105 - CREW REPORTED A STRONG BURNED PLASTIC SMELL DURING DESCENT INTO FAT. MAINTENANCE FOUND HOT JUG RECEPTIC LE BURNED. HOT JUGS PUT ON MEL AT THIS TIME. MAINTENANCE REPLACED AIRFRAME CONNECTOR FOR THE HOT JUGS. AIRCRAFT WAS R ETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050700478 20010507 00478 SO 2001 5 7 SIMA200102803 1 20010128 A 2150 A/C PACK EMB 145 EMB145LR SO A/C BAY CONTAMINATED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 619AE 145101 ORD - FLT 4256 - FOUND CREW REPORTED SMOKE IN CABIN AFTER TAKEOFF WHEN TURNING ON BLEED SYSTEM. FOUND PACKS TO BE SATUR ATED WITH GLYCOL. CLEANED LINES IAW AMM. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001050700479 20010507 00479 EU 2001 5 7 SIMA200103504 1 20010204 A 3350 192411A FUSE SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 906AE 340B348 DFW - FLT 3765 - FOUND CREW REPORTED OVERHEAD EMERGENCY LIGHT AT 11A TO BE INOPERATIVE. MAINTENANCE REPLACED FUSE 76LN IAW SAAB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050700480 20010507 00480 NM 2001 5 7 ASAA0110187 1 20010403 A 3350 86210144 BATTERY BOEING 737 737210C 1384459 NM MID CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 SEA - DURING MAINTENANCE CHECK, FOUND BATTERY FOR SMOKE BARRIER EMERGENCY EXIT LIGHT DISCHARGED. REMOVED AND REPLACED B ATTERY PACK AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2001050700481 20010507 00481 WP 2001 5 7 ASAA0180117 1 20010328 A 3350 6011779 LIGHT DOUG DC9 DC982 3022082 WP OVERWING EXIT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 951AS 24630 49111 PHX - DURING LINE CHECK, EXTERIOR EMERGENCY LIGHTS WERE DETERMINED TO BE INOPERATIVE. REMOVED AND REPLACED EXTERNAL EME RGENCY LIGHT BATTERY. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 2001050700483 20010507 00483 WP 2001 5 7 ASAA0180114 1 20010324 A 3350 0105606005 LIGHT DOUG DC9 DC982 3022082 WP CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 954AS 49387 PDX - DURING PRE-FLIGHT CHECK, FOUND AN EMERGENCY FLOOR TRACK LIGHT BROKEN AT ROW 6. REPLACED LIGHT ASSEMBLY AT ROW 6. TRACK LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001050700484 20010507 00484 NM 2001 5 7 ASAA0110151 1 20010324 A 3350 883200312 RECEIVER BOEING 737 737298C 1384490 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 8 WOULD NOT TEST PROPERLY. REMOVED AND REPLAC ED REMOTE ASSEMBLY RECEIVER AND BATTERY THEN LIGHTS ILLUMINATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 2001050700485 20010507 00485 NM 2001 5 7 20010504AP006 1 20010324 A 3350 86210144 BATTERY BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 8 WOULD NOT TEST PROPERLY. REMOVED AND REPLAC ED REMOTE ASSEMBLY RECEIVER AND BATTERY THEN LIGHTS ILLUMINATED NORMALLY. REF ASAA0110151. (M) 2 L 7 2 4F RT A16WE 2001050700486 20010507 00486 NM 2001 5 7 ASAA0110150 1 20010323 A 3350 8821004 BATTERY PACK BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS SLOW TO ILLUMINATE. REMOVED AND REPLACED TWO BATTERY PACKS THEN LIGHTS ILLUMINATED NORMALLY. (M) 2 L 7 2 4F A16WE 2001050700487 20010507 00487 NM 2001 5 7 ASAA0140038 1 20010323 A 3350 8100022602 CONNECTOR BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 776AS 25109 SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTING INOPERATIVE AT ROW 15/16 ABC. RECONNECTED EMERGENCY TRACK LIGHT WIRES. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2001050700488 20010507 00488 NM 2001 5 7 ASAA0140039 1 20010324 A 3350 8100022607 LIGHT BOEING 737 7374Q8 NM AFT MID CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 763AS 25100 FAI - BEFORE FLIGHT, FOUND EMERGENCY FLOOR TRACK LIGHTS AT AFT MID CABIN INOPERATIVE. RECONNECTED WIRES, OPS CHECKS GOO D. (M) 2 L 7 2 4F RT A16WE 2001050700489 20010507 00489 2001 5 7 ASAA0180105 4 20010316 A 2565 3961899501 LANYARD DOUG DC9 DC982 3022082 WP PAX DOOR SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 954AS 49387 SEA - DURING PRE-FLIGHT CHECK, L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD BETWEEN GIR T BAR AND SLIDE COVER. (M) 2 L 7 2 4F A6WE 2001050700490 20010507 00490 WP 2001 5 7 ASAA0180096 1 20010303 A 5320 991199215 CHANNEL DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 951AS 49111 OAK - DURING C-CHECK, FOUND RT C-CHANNEL, AFT OF MOVEABLE CEILING, CRACKED AT FUS CANT STATION 1485. REMOVED AND REPLAC ED CRACKED C-CHANNEL. (M) 2 L 7 2 4F A6WE 2001050700491 20010507 00491 2001 5 7 ASAA0180089 4 20010227 A 2565 4A30852 GIRT BAR DOUG DC9 DC983 3022083 WP EMERGENCY SLIDE INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 982AS 53473 LAX - DURING PRE-FLIGHT CHECK. L-2 DOOR EMERGENCY SLIDE GIRT BAR WAS FOUND TO BE IMPROPERLY INSTALLED. RE-INSTALLED GIR T BAR PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001050700492 20010507 00492 2001 5 7 ASAA0180090 4 20010227 A 2565 3753213 LATCH DOUG DC9 DC983 3022083 WP EMERGENCY SLIDE UNLATCHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 BUR - DURING PRE-FLIGHT CHECK, R1 DOOR EMERGENCY SLIDE PACK COVER LATCH WAS FOUND UNLATCHED. RE-LATCHED SLIDE PACK COVE R. (M) 2 L 7 2 4F RT A6WE 2001050700493 20010507 00493 WP 2001 5 7 ASAA0180091 1 20010228 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 955AS 48080 PHX - DURING K-CHK, FOUND FUSELAGE SKIN DENT AT APPROX FS 294, LONGERON 24L. REPAIRED DENT WITH INTERNAL FINGER DOUBLER AND SKIN PLUG IAW SRM 53-04, FIG 38. (M) 2 L 7 2 4F A6WE 2001050700494 20010507 00494 2001 5 7 ASAA0180101 4 20010310 A 2565 3961899501 LANYARD DOUG DC9 DC983 3022083 WP ESCAPE SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 969AS 53063 SEA - DURING PRE-FLIGHT CHECK, R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE PULLED OUT OF PLACE. REINSTALLED LANYAR D PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001050700495 20010507 00495 WP 2001 5 7 ASAA0180104 1 20010314 A 5610 5613217520 WINDOW DOUG DC9 DC982 3022082 WP COCKPIT DISLODGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 954AS 49387 SFO - DURING PREFLIGHT CHECK, FIRST OFFICERS SLIDING CLEARVIEW WINDOW CAME OUT OF ITS TRACK. PUT WINDOW BACK INTO TRACK . WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001050700496 20010507 00496 WP 2001 5 7 ASAA0180018 1 20010122 A 5311 991960431 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 981AS 53472 PHX - DURING K-CHECK, AFT CARGO BAY FRAME AT FS 1250, LONGERON 29L-28R, WAS FOUND TO BE CORRODED. FABRICATED AND INSTAL LED NEW FRAME SECTINO AND SPLICES. (M) 2 L 7 2 4F RT A6WE 2001050700497 20010507 00497 WP 2001 5 7 ASAA0180022 1 20010123 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 981AS 53472 PHX - DURING K-CHECK, FOUND LONGERON 30, IN MID CARGO BAY AT FS 579, WAS FOUND TO BE CORRODED AT FASTENERS COMMON TO FUS ELAGE SKIN. FABRICATED AND INSTALLED NEW LONGERON SECTION WITH SPLICE REPAIR. (M) 2 L 7 2 4F RT A6WE 2001050700498 20010507 00498 WP 2001 5 7 ASAA0180021 1 20010122 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 981AS 53472 PHX - DURING K-CHECK, FOUND LONGERON 30, AT FS 1287 IN THE AFT CARGO BAY, WAS FOUND TO BE CORRODED. FABRICATED AND REPL ACED SECTION OF LONGERON WITH SPLICE REPAIR. (M) 2 L 7 2 4F RT A6WE 2001050700499 20010507 00499 WP 2001 5 7 ASAA0180020 1 20010122 A 5320 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 981AS 53472 PHX - DURING K-CHECK, MID CARGO BAY UPPER FLANGE OF INTERCOSTAL AT FS 522-541, LONGERON 29 RT, WAS FOUND TO BE CORRODED. FABRICATED AND INSTALLED NEW INTERCOSTAL. (M) 2 L 7 2 4F RT A6WE 2001050700500 20010507 00500 WP 2001 5 7 ASAA0180064 1 20010213 A 5347 5936663505 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 982AS 53473 PHX - DURING K-CHECK, FOUND CORROSION ON RIGHT CARGO TRACK AT FS 1212-1322 IN AFT CARGO BAY. REMOVED AND REPLACED CORRO DED CARGO TRACK. (M) 2 L 7 2 4F RT A6WE 2001050700501 20010507 00501 WP 2001 5 7 ASAA0180002 1 20010104 A 2150 20495054 A/C PACK DOUG DC9 DC983 3022083 WP A/C BAY CONTAMINATED A ASAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 01 961AS 29643 21152 53075 LAX - FLT 285 - DURING CLIMB THROUGH 3000 FEET, STRONG CHEMICAL/OIL ODOR NOTED IN PASSENGER CABIN. RETURNED TO LAX. RE PLACED AIR CONDITIONING SYSTEM RIGHT COOLING TURBINE ASSEMBLY. SYSTEM THEN OP CHECKED OK. (M) 2 L 7 2 4F RT A6WE 2001050700502 20010507 00502 WP 2001 5 7 ASAA0180098 1 20010308 A 5610 5613217520 WINDOW DOUG DC9 DC982 3022082 WP COCKPIT INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 954AS 49387 ANC - DURING PREFLIGHT CHECK, FIRST OFFICERS SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. REALIGNED WINDOW GUIDE. WINDOW T HEN OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 2001050700503 20010507 00503 WP 2001 5 7 ASAA0180074 1 20010219 A 5210 5910081167 DOOR DOUG DC9 DC982 3022082 WP ENTRANCE OUT OF ADJ A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 935AS 31237 3701 49236 SEA - DURING LINE CHECK, FORWARD ENTRY L1 DOOR WAS DETERMINED TO BE HARD TO CLOSE WITH EXTERIOR HANDLE. REMOVED CENTER LINER. ADJUSTED DOOR PER MM 52-11-00. REINSTALLED LINER. DOOR LEAKED CHECKED OK. (M) 2 L 7 2 4F A6WE 2001050700504 20010507 00504 WP 2001 5 7 ASAA0180035 1 20010124 A 5347 5936663505 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 981AS 53472 PHX - DURING K-CHECK, AFT CARGO BAY TIE DOWN TRACK AT FS 1231-1287, WAS FOUND TO BE CORRODED. REMOVED AND REPLACED TRAC K AIW SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2001050700505 20010507 00505 WP 2001 5 7 ASAA0180043 1 20010124 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 981AS 53472 PHX - DURING K-CHECK, MID CARGO BAY LOWER AFT FRAME AT FS 522, FROM LONGERON 28R TO 28L, WAS FOUND TO BE HEAVILY CORRODE D. REPLACED CORRODED SECTION USING SPLICE REPAIR PER SRO 9530057. (M) 2 L 7 2 4F RT A6WE 2001050700506 20010507 00506 WP 2001 5 7 ASAA0180036 1 20010124 A 5310 991960433 SHEAR TIE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 981AS 53472 PHX - DURING K-CHECK, AFT CARGO BAY SHEAR TIE AT FS 1250, LONGERON 28L-28R, WAS FOUND TO BE CORRODED. REMOVED AND REPLA CED WITH NEWLY FABRICATED SHEAR TIE IAW SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2001050700507 20010507 00507 WP 2001 5 7 ASAA0180037 1 20010124 A 5347 593666091 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 981AS 53472 PHX - DURING K-CHECK, AFT CARGO BAY LEFT CARGO TRACK SPLICES AT FS 1220 WERE FOUND TO BE CORRODED. REMOVED AND REPLACED SPLICES (P/N''S 5936660-91, 93, 95, 97) IAW SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2001050700508 20010507 00508 WP 2001 5 7 ASAA0180038 1 20010124 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 981AS 53472 PHX - DURING K-CHECK, CABIN SEAT TRACK AT FS 246, 22 INCHES FROM RBL, WAS FOUND TO BE CORRODED. REPAIRED SEAT TRACK WIT H SPLICE REPAIR IAW SRM 53-05, FIG 4F. (M) 2 L 7 2 4F RT A6WE 2001050700509 20010507 00509 WP 2001 5 7 ASAA0180019 1 20010122 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 981AS 53472 PHX - DURING K-CHECK, AFT CARGO BAY TIE-DOWN TRACK AT FS 1090-1220, STRINGER 27L, WAS FOUND TO BE CORRODED. FABRICATED AND INSTALLED NEW CARGO TIE-DOWN TRACK. (M) 2 L 7 2 4F RT A6WE 2001050700510 20010507 00510 WP 2001 5 7 ASAA0180078 1 20010220 A 5320 59360713 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 982AS 53473 PHX - DURING K-CHECK, FOUND AFT CARGO BAY FRAME TO INTERCOSTAL ANGLE CORRODED AT FS 1155, RBL 3. REMOVED CORRODED ANGLE , FABRICATED AND INSTALLED NEW ANGLE PER ASA DWG 5936071. (M) 2 L 7 2 4F RT A6WE 2001050700511 20010507 00511 WP 2001 5 7 ASAA0180079 1 20010221 A 5320 9936696 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 982AS 53473 PHX - DURING K-CHECK, FOUND WEAR MARK ON OUTER RADIUS OF TRIANGLE INTERCOSTAL AT FS 1385, LBL 48. FABRICATED AND INSTAL LED A DOUBLER REPAIR PER SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2001050700512 20010507 00512 WP 2001 5 7 ASAA0180080 1 20010220 A 5330 C23AL230007 DOUBLER DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 982AS 53473 PHX - DURING K-CHECK, FOUND CLAIRCOM (PAX PHONE) ANTENNA MOUNT INTERNAL DOUBLER, LOCATED IN THE AFT CARGO BAY, CORRODED. REMOVED CORRODED DOUBLER. FABRICATED AND INSTALLED A REPLACEMENT DOUBLER PER SRM 51-30-2 AND DWG C23AL-2300. (M) 2 L 7 2 4F RT A6WE 2001050700513 20010507 00513 WP 2001 5 7 ASAA0180084 1 20010223 A 5210 5910081167 DOOR DOUG DC9 DC983 3022083 WP MAIN PAX INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 961AS 30117 2004 53075 SEA - DURING PRE-FLIGHT CHECK, L1 DOOR (FWD LT CREW/PAX DOOR) WAS FOUND TO BE DIFFICULT TO OPEN AND CLOSE. REMOVED AND REPLACED L1 DOOR. DOOR THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001050700514 20010507 00514 WP 2001 5 7 ASAA0180075 1 20010218 A 5350 3913359557 CABLE DOUG DC9 DC982 3022082 WP TAILCONE DISCONNECTED A K NONE L NO TEST IN INSP/MAINT 1 NM 01 951AS 49111 SEA - DURING LANDING, ''TAILCONE MISSING'' ANNUNCIATOR ILLUMINATED. SUBSEQUENT INSPECTION REVEALED THE EXTERNAL RELEASE HANDLE CABLE HAD BECOME DISCONNECTED. RECONNECTED RELEASE CABLE PER MM 53-50-00. (M) 2 L 7 2 4F A6WE 2001050700515 20010507 00515 WP 2001 5 7 ASAA0180085 1 20010225 A 5610 5613217519 WINDOW DOUG DC9 DC983 3022083 WP COCKPIT INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 LAX - DURING PREFLIGHT CHECK, CAPTAINS SLIDING CLEARVIEW WINDOW WAS FOUND TO BE DIFFICULT TO CLOSE. LUBRICATED WINDOW. WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001050700516 20010507 00516 WP 2001 5 7 ASAA0180081 1 20010221 A 5210 5910081167 DOOR DOUG DC9 DC983 3022083 WP MAIN PAX OUT OF ADJ A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 961AS 30117 2004 53075 SEA - DURING PRE-FLIGHT CHECK, L1 DOOR INTERNAL HANDLE WAS FOUND TO BE RUBBING AGAINST THE FORWARD LAVATORY WALL. READJ USTED DOOR PER MM 52-11-0. (M) 2 L 7 2 4F RT A6WE 2001050700517 20010507 00517 WP 2001 5 7 ASAA0180066 1 20010214 A 5320 593607111 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 982AS 53473 PHX - DURING K-CHECK, FOUND AFT CARGO BAY INTERCOSTAL AT FS 1149-1155, RBL 3, CORRODED. REMOVED AND REPLACED INTERCOSTA L, REF DWG 5936071. (M) 2 L 7 2 4F RT A6WE 2001050700518 20010507 00518 2001 5 7 ASAA0180082 4 20010222 A 2565 3961899501 LANYARD DOUG DC9 DC982 3022082 WP ESCAPE SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 934AS 49235 LAX - DURING PRE-FLIGHT CHECK, R1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD BETWEEN GIR T BAR AND SLIDE COVER. (M) 2 L 7 2 4F A6WE 2001050700519 20010507 00519 WP 2001 5 7 ASAA0180106 1 20010319 A 3350 0105606005 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 964AS 53078 SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT AFT END OF 1ST CLASS CABIN INOPERATIVE. REPLAED LIGHT JU MPER (CONNECTOR). LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001050700520 20010507 00520 WP 2001 5 7 ASAA0180108 1 20010319 A 3350 0105606003 MODULE DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST CR CRUISE 1 NM 01 949AS 53022 SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROWS 13, 14, 15 AND 16. REPAIRED CONNECTION AT ROW 15. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001050700521 20010507 00521 WP 2001 5 7 ASAA0180109 1 20010320 A 3350 0105606005 LIGHT DOUG DC9 DC983 3022083 WP CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 YVR - DURING PREFLIGHT CHECK, FOUND AN EMERGENCY FLOOR TRACK LIGHT BROKEN AT ROW 6. REPLACED LIGHT ASSEMBLIES AT ROW 6. LGIHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001050700522 20010507 00522 WP 2001 5 7 ASAA0180111 1 20010321 A 3350 60030451 BATTERY DOUG DC9 DC983 3022083 WP AFT CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 PDX - DURING LINE CHECK, OVERHEAD EMERGENCY LIGHTS IN AFT CABIN NEAR DOOR WERE DETERMINED TO BE INOPERATIVE. REMOVED AN D REPLACED BATTERIES WITHIN ASSOCIATED BATTERY PACK ASSEMBLY. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001050700523 20010507 00523 WP 2001 5 7 ASAA0180110 1 20010321 A 3350 PR2 LAMP DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 974AS 53450 PDX - DURING LINE CHECK, PORTABLE EMERGENCY LIGHT ASSEMBLY WAS DETERMINED TO BE INOPERATIVE. REPLACED LAMP (BULB) WITHI N LIGHT ASSEMBLY. LIGHT THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001050700525 20010507 00525 WP 2001 5 7 ASAA0180100 1 20010311 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 973AS 53449 SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROWS 4-12 CABIN INOPERATIVE. REPLACED BATTERIES. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001050700526 20010507 00526 EU 2001 5 7 20010504AP007 1 20010119 A 2710 VL35B3 ACTUATOR AIRBUS 300 A300B4203 3930306 EU AILERON FAILED A WRNA J A DUMP FUEL UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 05 823SC MSN207 LOW SPEED AILERON FAILED TO DISCONNECT IN AUTO AND MANUAL. DMI NR 1452 CLEARED BY REMOVING AND REPLACING OF AILERON PIC KOFF PER 27-11-63 ALTERNATE PROCEDURE. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A35EU 2001050700527 20010507 00527 EU 2001 5 7 20010504AP008 1 20010113 A 2710 VL35B3 ACTUATOR AIRBUS 300 A300B4203 3930306 EU LT AILERON FAILED A WRNA J A DUMP FUEL UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 05 823SC MSN207 LOW SPEED AILERON WOULD NOT DISCONNECT IN AUTO OR MANUAL. LEFT LOW SPEED AILERON ACTUATOR REMOVED AND SENT TO REPAIR FA CILITY. ACTUATOR REINSTALLED AND OPS CHECKED GOOD IAW 27-11-47. AIRCRAFT RETURNED TO SERVICE. DMI NR 1442 CLEARED. ( M) 2 L 7 2 4F RT A35EU 2001050700528 20010507 00528 EU 2001 5 7 20010504AP009 1 20010115 A 2710 VL35B3 ACTUATOR AIRBUS 300 A300B4203 3930306 EU LT AILERON INOPERATIVE A WRNA J A DUMP FUEL UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 05 823SC MSN207 LOW SPEED AILERON FAILED TO DISCONNECT IN AUTO AND IN DISCONNECT POSITION AFTER SLAT RETRACTION. FUEL DUMPED, 40,000 LB S. AIRCRAFT RETURNED TO LOCKBORNE. LANDING NORMAL. ASSIGNED DMI NR 1452 IAW MEL 27-11-01, CAT ''B'' EXPIRES 1-18-01. LOCKOUT PROCEDURES COMPLIED WITH. (M) 2 L 7 2 4F RT A35EU 2001050700529 20010507 00529 NM 2001 5 7 GAIA01124OP 1 20010409 A 3350 1000679 BATTERY BOEING 727 727225 1384077 NM L1 DOOR DISCHARGED A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 936PG 22441 DURING MAINTENANCE, IT WAS DISCOVERED THAT THE EMERGENCY LIGHT ASSEMBLY AT THE L1 DOOR APPEARS TO BE DISCHARGED. REMOVE D AND REPLACED THE L1 DOOR EMERGENCY LIGHT ASSEMBLY. OPERATIONALLY CHECKED NORMAL. THE AIRCRAFT WAS RETURNED TO SERVIC E. (M) 2 L 7 3 4F A3WE 2001050700531 20010507 00531 NM 2001 5 7 UPS01235790 1 20010420 A 5755 CASTING BOEING 727 72722C 138400F NM WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C, NR 7 SPOILER SUPPORT CASTING IS CORRODED BEYOND LIMITS. NR 7 SPOILER CASTING REMOVED & REPLACED I AW DRW 65-16216 & IAW SRM 51- 10-2 2 L 7 3 4F A3WE 2001050700532 20010507 00532 NM 2001 5 7 UPS01235792 1 20010421 A 3210 CASTING BOEING 727 72722C 138400F NM LT GEAR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C, LT GEAR OPERATED DOOR SEQUENCE VALVE SUPPORT CASTING CRACKED. CASTING REPLACED IAW MM 32-32-31 2 L 7 3 4F A3WE 2001050700533 20010507 00533 NM 2001 5 7 UPS01235798 1 20010420 A 5755 RIB BOEING 727 72722C 138400F NM WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C, NR 7 SPOILER, SUPPORT RIB ON I/B SIDE ATACHED TO MLG BEAM IS CORRODED BEYOND LIMITS. REPLACED SUPPOR T RIB IAW SRM 51-30-2 2 L 7 3 4F A3WE 2001050700534 20010507 00534 NM 2001 5 7 UPS01235799 1 20010420 A 5755 SUPPORT BOEING 727 72722C 138400F NM NR 7 SPOILER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C, NR 7 SPOILER, I/B END HINGE SUPPORT ATTACHED TO SPOILER SUPPORT BEAM I S CORRODED BEYOND LIMITS. /BE ND HINGE REPLACED IAW SRM 51-30-02 2 L 7 3 4F A3WE 2001050700535 20010507 00535 NM 2001 5 7 UPS01235802 1 20010423 A 2710 CASTING BOEING 727 72722C 138400F NM AILERONS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C, LT O/B AILERON LOCKOUT MECHANISM, MAIN SUPPORT CASTING HAS EVIDENCE OF CORROSION ON NUMEROUS BUSHING AREAS. CASTING REPLACED IAW SRM 51-30-02 & DRAWINGS 65-21776 & 65-21779 2 L 7 3 4F A3WE 2001050700536 20010507 00536 NM 2001 5 7 UPS01235805 1 20010423 A 5312 PRESSURE PANEL BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE: C, EVIDENCE OF CORROSION, NOSE WHEEL WELL TORQUE BOX WDF PANHEL BS 294 - 309 . REPAIR CARRIED OUT I AW SRM 53-10-9 2 L 7 3 4F A3WE 2001050700537 20010507 00537 NM 2001 5 7 UPS01235807 1 20010418 A 5313 STRINGER BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE: C, CORROSION FOUND AT BS 870 LT ON S18A LWR AFT ATTACH BOLT LOCATION. REPAIR CARRIED OUT IAW SRM 51-1 0-6 & SHANNON MRO EO 2001-013-002 UPS ENGINEERING FILE NO 727-53-20016 2 L 7 3 4F A3WE 2001050700538 20010507 00538 NM 2001 5 7 UPS01235808 1 20010418 A 5313 STRINGER BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C CORROSION FOUND ON S18A LT AT BS 890 TO 940 HORIZ. FLANGE AT BODY F AIRING SUPPORT. REPAIR CARRIED OU T IAW SRM 51-30-2 51-30-6 & SMRO EO 2001-013-002 UPS ENGINEERING FILE NO 727-53-20016 2 L 7 3 4F A3WE 2001050700539 20010507 00539 NM 2001 5 7 UPS01235809 1 20010420 A 2710 65244019 CASTING BOEING 727 72722C 138400F NM AILERON GEARBOX CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE: C, EVIDENCE OF CORROSION ON LEFT OUTBOARD AILERON TURNAROUND GEARBOX CASTING. REPLACED GEARBOX CASTING IAW 27-10-131 2 L 7 3 4F A3WE 2001051000263 20010510 00263 NM 2001 5 10 UPS01235813 1 20010502 A 2730 ELEVATOR BOEING 727 72727C 138400J NM FLIGHT DECK BINDING A IPXA O OTHER F FLT CONT AFFECTED IN INSP/MAINT 1 SO 01 910UP 19117 INSPECTION TYPE:N/A ELEVATORS BINDING AND MAKING A LOUD NOISE ***SUPPLEMENTAL MRR*** LUBED RUB STRIPS OPS CHECK GOOD . 2 L 7 3 4F A3WE 2001050700542 20010507 00542 NM 2001 5 7 UPS01635811 1 20010503 A 3510 STRAP BOEING 767 767300 1385204 NM 02 BOTTLES CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 331UP 27757 DURING MAINT INSP FOUND 02 BOTTLE STRAP CRACKED. R&R 02 BOTTLE STRAP 2 L 7 2 4F RT A1NM 2001050700543 20010507 00543 WP 2001 5 7 UPS01835778 1 20010501 A 7100 ENGINE DOUG DC8 DC873F 302199F WP NR 4 FLAMED OUT A IPXA E ENGINE SHUTDOWN X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SO 01 801UP 46101 APPROX 2 MIN AFTER LEVEL OFF AT FL350 + 273IAS, NR 4 ENG FLAMES OUT. I MMEDIATE X-FEED DID NOT RE-LIGHT IT. 2 NORMAL AIR START ATTEMPTS WERE TRIED IAW CHECKLIST PROCEDURES. BOTH UNSUCCESSFUL. PERFORMED IDLE CHECK, POWER ASSURANCE CHECK, P MC DROPCHECK ACCELERATION CHECK AND IDLE SPEED CHECK ALL IAW MM 71-00-00 ENGINE NR 4 OPS CHECKS NORMAL. 2 L 7 4 4F RT 4A25 2001050700544 20010507 00544 WP 2001 5 7 UPS01835786 1 20010502 A 7100 ENGINE DOUG DC8 DC871F 302199D WP NR 1 FLAMED OUT A IPXA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SO 01 709UP 45914 NR 1 ENGINE FLAMEOUT IN CRUISE FLT THEN RESTARTED. ACCOMPLISHED TROUBLESHOOTING PROCEDURES: VISUAL INSP, ROTATION OF F AN, INSPECTED MAGNETIC CHIP DETECTORS, SUMPED FUEL TANK AND INSPECTED NR 1 ENGINE FUEL FILTER, NO CONTAMINATES NOTED. RE F AMM 71-00-00 AND AMM 73-10-02 2 L 7 4 4F RT 4A25 2001050700545 20010507 00545 WP 2001 5 7 UPS01835795 1 20010503 A 3350 TL1156M SWITCH DOUG DC8 DC873F 302199F WP OVERHEAD PANEL INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE: PREFLT, FOUND DURING EMERGENCY LIGHT TEST. SWITCH INTERNALLY BAD DUE TO LIGHTS REMAIN ON WITH SWITCH O N OFF OR DISARMED POSITION. RESET TO S.W. MAKE LIGHT TO TURN OFF. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH AT OVERHE AD PANEL I/A/W WDM. 33-50-01 PAGE 4. AND PERFORMED TEST AS PER 30-50-01(MM). OPS CHECK NORMAL. 2 L 7 4 4F RT 4A25 2001050700546 20010507 00546 WP 2001 5 7 UPS01835797 1 20010503 A 2100 BUSS DOUG DC8 DC871F 302199D WP COCKPIT OPEN A IPXA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 706UP 46056 BTB-FOR SMOKE IN COCKPIT DUCT OVERHEAT LIGHT ON. SMOKE IN COCKPIT LEFT PACK TEMP GAUGE PEGGED FULL HOT. LEFT PACK WAS NEVER TURNED ON. SUSPECT LOSE OF NR 1 BUS OPENING LEFT PACK VALVE, RUN BOTH PACKS NO DEFECTS NOTED. 2 L 7 4 4F RT 4A25 2001050700547 20010507 00547 WP 2001 5 7 UPS01835814 1 20010503 A 3350 LIGHT DOUG DC8 DC873F 302199F WP COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 812UP 46112 EMERGENCY EXIT ARM/DISARM LIGHT INOPERATIVE. RELAMPED AND OPS CHECK GOOD 2 L 7 4 4F RT 4A25 2001050800001 20010508 00001 NM 2001 5 8 SWAA011102 1 20010410 A 5551 6551524 FITTING BOEING 737 7372H4 138448C NM HORIZ STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D CHECK, FOUND RT HORIZ STAB CENTER SECTION REAR SPAR LOWER CLEVIS AFT LUG, AFT FACE, CORRODED. REPAIRE D FITTING PER BFG ER. 2 L 7 2 4F A16WE 2001050800002 20010508 00002 NM 2001 5 8 SWAA011068 1 20010407 A 5315 65C33971 FLOORBEAM BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED 1/2D CHECK, FOUND FLOOR BEAM CORRODED AT BS 294, BL 0 TO LBL 19. REPAIRED FLOOR BEAM PER SWA T1. 2 L 7 2 4F RT A16WE 2001050800003 20010508 00003 NM 2001 5 8 SWAA011069 1 20010406 A 5312 6517582 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM WEBS CRACKED AT RBL 17.1, WL 181 & LBL 17.1, WL 234. REPAI RED VERTICAL BEAM WEB PER SRM. 2 L 7 2 4F A16WE 2001050800004 20010508 00004 NM 2001 5 8 SWAA011070 1 20010405 A 2120 65C280023 DUCT BOEING 737 7373Y0 1384671 NM CARGO BAY RUPTURED A SWAA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 682SW 23496 DIVERTED, UNABLE TO MAINTAIN CABIN PRESSURE. FOUND CLAMP LOOSE ON LT WATER SEPERATOR & MUFFLER/DUCT ASSY RUPTURED IN FWD CARGO BAY, BEHIND AFT WALL. SECURED CLAMP AND R&R DUCT ASSY PER MM. OPS CHECK NORMAL PER MM. 2 L 7 2 4F RT A16WE 2001050800005 20010508 00005 NM 2001 5 8 SWAA011071 1 20010406 A 5411 BAC1505 FRAME BOEING 737 7373Y0 1384671 NM NR 2 PYLON CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664WN 23495 DURING SCHEDULED 1/4D CHECK, FOUND NR 2 ENGINE PYLON FRAME CRACKED AT STA 351.88. R&R FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001050800006 20010508 00006 NM 2001 5 8 SWAA011121 1 20010412 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 391SW 27378 EEPLS WIRING EXPOSED & LENS MISSING AT OVERWING EXIT. SECURED WIRING & INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2001050800007 20010508 00007 NM 2001 5 8 SWAA011122 1 20010412 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 627SW 27935 EEPLS WIRING EXPOSED AT ROW 14. SECURED EEPLS WIRING PER MM. 2 L 7 2 4F RT A16WE 2001050800008 20010508 00008 NM 2001 5 8 SWAA011123 1 20010412 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 080SW 22675 DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 837, STR 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001050800009 20010508 00009 NM 2001 5 8 SWAA011124 1 20010412 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 355SW 25250 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500, LBL 6 TO RBL 2, WL 148. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001050800010 20010508 00010 NM 2001 5 8 SWAA011125 1 20010412 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 DURING SCHEDULED C4 CHECK, FOUND EEPLS WIRING EXPOSED AT ROW 11. SECURED EEPLS WIRING PER MM. 2 L 7 2 4F RT A16WE 2001050800011 20010508 00011 2001 5 8 SWAA011126 4 20010413 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001050800012 20010508 00012 NM 2001 5 8 SWAA011127 1 20010413 A 2913 623337 PUMP BOEING 737 7373H4 1384600 NM NR 1 ENGINE FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 389SW 26592 AIR TURNBACK, DURING GEAR RETRACTION, NR 1 ENG HYD PUMP FAILED. NO LOSS OF HYD FLUID. R&R NR 1 HYD PUMP & CASE DRAIN FI LTER PER MM, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2001050800013 20010508 00013 NM 2001 5 8 SWAA011128 1 20010413 A 3350 079123 COVER BOEING 737 7375H4 138449D NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 EEPLS TRACK COVER MISSING NEAR OVERWING EXIT. INSTALLED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001050800014 20010508 00014 NM 2001 5 8 SWAA011129 1 20010413 A 3350 BR9442 COVER BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 389SW 26592 DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT LIGHT COVER CRACKED AT FWD GALLEY. R&R LIGHT COVER PER MM. 2 L 7 2 4F RT A16WE 2001050800015 20010508 00015 NM 2001 5 8 SWAA011130 1 20010413 A 3350 6556633 LENS BOEING 737 7373G7 1384595 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED C2 CHECK, FOUND RT OVERWING EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2001050800016 20010508 00016 NM 2001 5 8 SWAA011131 1 20010413 A 5523 BACB28AK04 BUSHING BOEING 737 7377H4 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 744SW 29490 DURING SCHEDULED SERVICE CHECK (SWA SI 11038-55), FOUND RT ELEVATOR TAB BUSHING WORN AT NR 4 HINGE POINT. R&R BUSHING PE R D&M ENTERPRISES SSR #015. 2 L 7 2 4F RT A16WE 2001050800017 20010508 00017 NM 2001 5 8 SWAA011132 1 20010413 A 5523 BACB28AK04 BUSHING BOEING 737 7377H4 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 744SW 29490 DURING SCHEDULED CHECK (SWA SI 11038-55), FOUND LT ELEVATOR TAB BUSHINGS WORN AT NR 2, NR 3 & NR 4 HINGE POINTS. R&R BUS HINGS PER D&M ENTERPRISES SSR NR 015. 2 L 7 2 4F RT A16WE 2001050800018 20010508 00018 NM 2001 5 8 SWAA011133 1 20010414 A 5330 6552988 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED A2 CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 920, STR 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001050800019 20010508 00019 NM 2001 5 8 SWAA011134 1 20010414 A 5310 6558280 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 355SW 25250 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14L & 15L. R&R SHEAR TIE PER SRM & BAC DWG. 2 L 7 2 4F RT A16WE 2001050800020 20010508 00020 NM 2001 5 8 SWAA011135 1 20010412 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 355SW 25250 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 9L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001050800021 20010508 00021 NM 2001 5 8 SWAA011136 1 20010414 A 3350 BR9442 COVER BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 608SW 27928 EMERGENCY EXIT LIGHT COVER BROKEN IN FWD SECTION. R&R LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001050800022 20010508 00022 NM 2001 5 8 SWAA011137 1 20010413 A 5320 AND10134 STIFFENER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D CHECK, FOUND FWD BULKHEAD STIFFENER CRACKED AT BS 188, WL 208, LBL 25. REPAIRED STIFFENER PER BFG ER . 2 L 7 2 4F A16WE 2001050800023 20010508 00023 NM 2001 5 8 SWAA011138 1 20010412 A 5320 65C25721 ANGLE BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED 1/2D CHECK, FOUND BS 616 FRAME SUPPORT ANGLE CRACKED AT WING TERMINAL ATTACHMENT POINT. REPAIRED ANGLE PER SWA TI-153-018. 2 L 7 2 4F RT A16WE 2001050800024 20010508 00024 2001 5 8 SWAA011209 4 20010423 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001050800025 20010508 00025 NM 2001 5 8 SWAA011210 1 20010423 A 5320 65C27314 STRINGER CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 13R. R&R STR CLIP PER SRM. 2 L 7 2 4F A16WE 2001050800026 20010508 00026 NM 2001 5 8 SWAA011211 1 20010423 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN BULGED AT BS 727+15, STR 27L. REPAIRED SKIN PER BFG ER. 2 L 7 2 4F A16WE 2001050800027 20010508 00027 NM 2001 5 8 SWAA011212 1 20010422 A 3350 BR2013 LENS BOEING 737 7372T4 1384492 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED C3 CHECK, FOUND EEPLS FLOOR TRACK BROKEN AT ROW 15, LENS MISSING AT ROW 20 & END CAP MISSING AT AFT SEC TION. REPLACED TRACK COVER, LENS & END CAP PER MM. 2 L 7 2 4F A16WE 2001050800028 20010508 00028 NM 2001 5 8 SWAA011213 1 20010422 A 3350 65C27095 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY PACK LOOSE AT AFT CABIN. SECURED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2001050800029 20010508 00029 2001 5 8 SWAA011214 4 20010423 A 2565 D3159147B SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 611SW 27697 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. R&R EVAC SLIDE ASSY P ER MM. 2 L 7 2 4F RT A16WE 2001050800030 20010508 00030 NM 2001 5 8 SWAA011215 1 20010423 A 3350 61422 CHARGER BOEING 737 7373A4 1384585 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP. R&R BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2001050800031 20010508 00031 NM 2001 5 8 SWAA011216 1 20010423 A 5315 6546804 FLOORBEAM BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED 1/2D CHECK, FOUND FLOOR BEAM CORRODED AT BS 328, LBL 12. REPAIRED FLOOR BEAM PER SRM. 2 L 7 2 4F RT A16WE 2001050800032 20010508 00032 2001 5 8 SWAA011217 4 20010422 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001050800033 20010508 00033 NM 2001 5 8 SWAA011218 1 20010421 A 3350 65C34691 LENS BOEING 737 7373Y0 1384671 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 682SW 23496 BULLNOSE EMERGENCY EXIT LIGHT LENS BROKEN AT ROW 9 DEF. R&R LENS PER MM. 2 L 7 2 4F RT A16WE 2001050800034 20010508 00034 NM 2001 5 8 SWAA011219 1 20010422 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 641SW 27714 FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS BROKEN. R&R LENS PER MM. 2 L 7 2 4F RT A16WE 2001050800035 20010508 00035 2001 5 8 SWAA011220 4 20010422 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 355SW 25250 DURING SCHEDULED D CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. R&R SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001050800036 20010508 00036 NM 2001 5 8 SWAA011221 1 20010422 A 3350 BR2013 LIGHT BOEING 737 7377H4 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 751SW 29803 EEPLS INOP AT FWD SECTION. REPAIRED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001050800037 20010508 00037 NM 2001 5 8 SWAA011193 1 20010419 A 3350 079123 COVER BOEING 737 7373T0 1384582 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 684WN 23941 EEPLS FLOOR TRACK COVER BROKEN AT ROW 8. R&R TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001050800038 20010508 00038 NM 2001 5 8 SWAA011194 1 20010419 A 3350 655633 LIGHT BOEING 737 7375H4 138449D NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 525SW 26567 R/H OVERWING EMERGENCY EXIT LIGHT OUT OF POSITION. REPOSITIONED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001050800039 20010508 00039 NM 2001 5 8 SWAA011195 1 20010420 A 3350 BR2013 COVER BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 EEPLS TRACK COVER BROKEN AT ROW 1. R&R TRACK COVER & BULB PER MM. 2 L 7 2 4F RT A16WE 2001050800040 20010508 00040 NM 2001 5 8 SWAA011196 1 20010420 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED SERVICE CHECK, FOUND 2 LONG EXTERNAL FUSELAGE SKIN CRACK AT BS 540, BETWEEN STR 15L & 16L. REPAIRED SKI N PER SRM. 2 L 7 2 4F RT A16WE 2001050800041 20010508 00041 NM 2001 5 8 SWAA011197 1 20010420 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 625SW 27701 DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY EXIT LIGHT LENS CRACKED AT FWD SECTION. R&R LENS PER MM. 2 L 7 2 4F RT A16WE 2001050800042 20010508 00042 NM 2001 5 8 SWAA011198 1 20010420 A 3350 6104789 BATTERY PACK BOEING 737 7373A4 1384585 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED SERVICE CHECK, FOUND OVERWING EMERGENCY EXITS LIGHTS INOP. R&R BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2001050800043 20010508 00043 NM 2001 5 8 SWAA011199 1 20010420 A 5315 6546804 FLOORBEAM BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED 1/2D CHECK, FOUND FLOOR BEAM CORRODED AT BS 987, LBL 40 TO RBL 40. REPAIRED FLOOR BEAM PER SRM . 2 L 7 2 4F RT A16WE 2001050800044 20010508 00044 NM 2001 5 8 SWAA011200 1 20010420 A 5315 6546804 FLOORBEAM BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED 1/2D CHECK, FOUND FLOOR BEAM CORRODED AT BS 312, RBL 36 TO LBL 36. REPAIRED FLOOR BEAM PER SRM. 2 L 7 2 4F RT A16WE 2001050800045 20010508 00045 NM 2001 5 8 SWAA011201 1 20010420 A 5754 65C26686 SKIN BOEING 737 7373TO 138447G NM L/E SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 697SW 23838 DURING SCHEDULED C4 CHECK, FOUND NR 6 L/E SLAT SKIN CRACKED AT AFT ROW OF FASTENERS, 4 FROM OUTBD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2001050800046 20010508 00046 NM 2001 5 8 SWAA011202 1 20010419 A 3350 767 LIGHT BOEING 737 7377H4 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 783SW 29809 DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL EMERGENCY LIGHT INOP AT RT WING. RELAMPED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001050800047 20010508 00047 NM 2001 5 8 SWAA011203 1 20010421 A 2913 6915863 PUMP BOEING 737 7372H4 138448C NM NR 1 ENGINE VIBRATES A SWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 07 073SW 22673 AIR TURNBACK, DURING CLIMB OUT DETECTED ABNORMAL ENGINE VIBRATION FROM NR 1 ENGINE, ABOVE 1.7 EPR. R&R NR 1 ENG HYD PUMP & CASE DRAIN FILTER PER MM. OPS & LEAK CHECK GOOD. 2 L 7 2 4F A16WE 2001050800048 20010508 00048 NM 2001 5 8 SWAA011204 1 20010421 A 2751 106079113 INDICATOR BOEING 737 7372H4 138448C NM COCKPIT INOPERATIVE A SWAA O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 SW 07 086SW 22827 DECLARED EMERGENCY, DURING FLAP EXTENSION, T/E FLAPS STOPPED AT APPROX 1/2 DEGREE WITH NO L/E DEVICES. T/E & L/E FLAPS EXTENDED NORMALLY WITH ALT FLAP SWITCH. R&R FLAP POS INDICATOR PER MM. OPS CHECK GOOD. 2 L 7 2 4F A16WE 2001050800049 20010508 00049 2001 5 8 SWAA011205 4 20010420 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 AFT SVC DOOR EMERGENCY EVAC SLIDE ASSY OUT OF ADJUST. READJUSTED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001050800050 20010508 00050 NM 2001 5 8 SWAA011206 1 20010421 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED SERVICE CHECK, FOUND 3 LONG EXTERNAL FUSELAGE SKIN CRACK AT BS 440, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001050800051 20010508 00051 NM 2001 5 8 SWAA011207 1 20010421 A 5754 6546430 SKIN BOEING 737 7373H4 1384600 NM L/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED C2 CHECK, FOUND LT WING INBD FOREFLAP DELAMINATED ON UPPER SURFACE. R&R FOREFLAP PER MM. 2 L 7 2 4F RT A16WE 2001050800052 20010508 00052 NM 2001 5 8 SWAA011208 1 20010420 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED C2 CHECK, FOUND 5 LONG EXTERNAL FUSELAGE SKIN CRACK AT BS 500D, ABOVE STR 10L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001050800053 20010508 00053 NM 2001 5 8 SWAA011184 1 20010419 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 706SW 27840 EEPLS TRACK COVER MISSING AT ROW 9. INSTALLED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001050800054 20010508 00054 NM 2001 5 8 SWAA011185 1 20010418 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 714CB 27848 EEPLS TRACK COVER MISSING. INSTALLED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001050800055 20010508 00055 NM 2001 5 8 SWAA011186 1 20010419 A 5320 65C27314 STRINGER CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D CHECK, FOUND 2 EA. STR CLIPS CRACKED AT BS 380, STR 21L & 22L. R&R STR CLIPS PER SRM. 2 L 7 2 4F A16WE 2001050800056 20010508 00056 NM 2001 5 8 SWAA011187 1 20010418 A 3350 110049 POWER SUPPLY BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY & SVC DOOR EMERGENCY EXIT LIGHTS INOP. R&R POWER SUPPLY PER MM. 2 L 7 2 4F A16WE 2001050800057 20010508 00057 NM 2001 5 8 SWAA011188 1 20010418 A 5753 6546435 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 328SW 23692 DURING SCHEDULED C2 CHECK, FOUND LT WING INBD AFT FLAP DELAMINATED AT INBD END. R&R AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2001050800058 20010508 00058 NM 2001 5 8 SWAA011189 1 20010419 A 5312 6516300 BULKHEAD BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT LBL 11, WL 218. REPAIRED BULKHEAD WEB PER SRM. 2 L 7 2 4F RT A16WE 2001050800059 20010508 00059 NM 2001 5 8 SWAA011190 1 20010417 A 5315 6546804 FLOORBEAM BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED 1/2D CHECK, FOUND FLOOR BEAM CORRODED AT BS 1008, LBL 30. REPAIRED FLOOR BEAM PER SRM. 2 L 7 2 4F RT A16WE 2001050800060 20010508 00060 NM 2001 5 8 SWAA011191 1 20010419 A 3350 BR2013 COVER BOEING 737 7373T0 1384582 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 684WN 23941 EEPLS TRACK COVER BROKEN AT ROW 8. R&R EEPLS TRACK COVER AND 1 EA. LENS PER MM. 2 L 7 2 4F RT A16WE 2001050800061 20010508 00061 NM 2001 5 8 SWAA011177 1 20010417 A 3350 57771 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED C1 CHECK, FOUND EEPLS END CAP MISSING AT AFT SECTION. INSTALLED END CAP PER MM. 2 L 7 2 4F A16WE 2001050800062 20010508 00062 NM 2001 5 8 SWAA011178 1 20010416 A 5743 6567172 FITTING BOEING 737 7373H4 1384600 NM RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 355SW 25250 DURING SCHEDULED D CHECK, FOUND RT WING MLG STAB SUPPORT BEAM FITTING CORRODED. R&R BEAM FITTING PER MM. 2 L 7 2 4F RT A16WE 2001050800063 20010508 00063 NM 2001 5 8 SWAA011179 1 20010416 A 5320 6517583 BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 625SW 27701 DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 182, LBL 5.7. REPAIRED VERTICAL BEAM WEB PER SWA RA. 2 L 7 2 4F RT A16WE 2001050800064 20010508 00064 NM 2001 5 8 SWAA011180 1 20010417 A 5753 6546435 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 639SW 27712 DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBD AFT FLAP LOWER SURFACE DELAMINATED AT INBD END. R&R AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2001050800065 20010508 00065 NM 2001 5 8 SWAA011181 1 20010418 A 5320 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED 1/2D CHECK, FOUND 2 EA. STR CLIPS CRACKED AT BS 663, STR 10R & 10L. R&R STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001050800066 20010508 00066 NM 2001 5 8 SWAA011182 1 20010418 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 642WN 27715 EMERGENCY EXIT LIGHT LENS OUT OF POSITION. REPOSITIONED LENS PER MM. 2 L 7 2 4F RT A16WE 2001050800067 20010508 00067 NM 2001 5 8 SWAA011183 1 20010418 A 5523 BACB28AK04 BUSHING BOEING 737 7377H4 NM LT/RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 744SW 29490 DURING SCHEDULED C4 CHECK (SWA SI 11038-55), LT & RT ELEVATOR TAB FAILED FREE PLAY CHECK. R&R BOTH ELEVATOR TAB ATTACH F ITTING BOLTS AND BUSHINGS. 2 L 7 2 4F RT A16WE 2001050800068 20010508 00068 NM 2001 5 8 SWAA011164 1 20010415 A 3397 BR2013 WIRE BOEING 737 7372H4 138448C NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 EEPLS LOOSE & WIRES EXPOSED AT EMERGENCY EXIT ROW. REPAIRED & RELAMPED EEPLS PER MM. 2 L 7 2 4F A16WE 2001050800069 20010508 00069 2001 5 8 SWAA011165 4 20010416 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 AFT DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001050800070 20010508 00070 2001 5 8 SWAA011166 4 20010417 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 312SW 23334 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001050800071 20010508 00071 NM 2001 5 8 SWAA011167 1 20010417 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 725SW 27857 EEPLS TRACK COVER MISSING. INSTALLED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001050800072 20010508 00072 NM 2001 5 8 SWAA011168 1 20010416 A 3397 BR2013 WIRE BOEING 737 7372K6 1364440 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED C4 CHECK, FOUND EEPLS TRACK COVER LOOSE & WIRING EXPOSED AT AFT SECTION. INSTALLED TRACK COVER & END CA P PER MM. 2 L 7 2 4F RT A16WE 2001050800073 20010508 00073 2001 5 8 SWAA011169 4 20010417 A 2565 1061323469 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. R&R EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001050800074 20010508 00074 NM 2001 5 8 SWAA011170 1 20010417 A 3350 6556633 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 615SW 27698 DURING SCHEDULED A2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2001050800075 20010508 00075 2001 5 8 SWAA011171 4 20010416 A 2565 D31354 SLIDE BOEING 737 7373Y0 1384671 NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664WN 23495 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. READJUSTED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001050800076 20010508 00076 NM 2001 5 8 SWAA011172 1 20010417 A 5320 6517583 BEAM BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM CRACKED AT LBL 5.7, WL 184. REPAIRED VERTICAL BEAM PER SRM. 2 L 7 2 4F RT A16WE 2001050800077 20010508 00077 NM 2001 5 8 SWAA011173 1 20010417 A 5753 6546435 FLAP BOEING 737 7373G7 1384595 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 683SW 24008 DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBD AFT FLAP DELAMINATED AT INBD END. R&R AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2001050800078 20010508 00078 NM 2001 5 8 SWAA011174 1 20010417 A 5754 65C26686 SKIN BOEING 737 7373G7 1384595 NM L/E SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 683SW 24008 DURING SCHEDULED C2 CHECK, FOUND NR 2 L/E SLAT LOWER SKIN CRACKED AT AFT ROW OF FASTENERS, 20 INBD OF ACTUATOR. REPAIRED SLAT SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001050800079 20010508 00079 NM 2001 5 8 SWAA011175 1 20010417 A 5753 0570006 SKIN BOEING 737 7373G7 1384595 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 683SW 24008 DURING SCHEDULED C2 CHECK, FOUND RT WING INBD AFT FLAP DELAMINATED ON UPPER SURFACE. R&R AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2001050800080 20010508 00080 NM 2001 5 8 SWAA011176 1 20010416 A 5512 65C27494 SKIN BOEING 737 737317 138447P NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED C1 CHECK, FOUND 1.25 CRACK AT LT HORIZ STAB LOWER SKIN, FWD OF REAR SPAR ACCESS PANEL NR 9107L. REPAIRE D SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001050800081 20010508 00081 NM 2001 5 8 SWAA011139 1 20010415 A 3350 BR9442 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 378SW 26585 EMERGENCY EXIT LIGHT LENS MISSING FROM FWD BULKHEAD, LT SIDE. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2001050800082 20010508 00082 NM 2001 5 8 SWAA011140 1 20010414 A 2131 7612608 CONTROLLER BOEING 737 7373H4 1384600 NM CABIN PRESSURE FAILED A SWAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 390SW 26593 DIVERTED, DECLARED EMERGENCY, AT FL 370, PRESSURIZATION AURAL WARNING SOUNDED. PRESS VALVE CLOSED, EMERGENCY DESCENT KE PT CABIN ALT BELOW 11,500FT. R&R PRESS CONTROLLER PER MM, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2001050800083 20010508 00083 NM 2001 5 8 SWAA011141 1 20010414 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 627SW 27935 EEPLS TRACK COVER MISSING AT ROW 2. REPLACED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001050800084 20010508 00084 NM 2001 5 8 SWAA011142 1 20010415 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 700GS 27835 EEPLS TRACK COVER LOOSE AT ROW 8. SECURED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001050800085 20010508 00085 NM 2001 5 8 SWAA011143 1 20010414 A 5230 65C36231 SKIN BOEING 737 7373H4 1384600 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 395SW 27689 DURING SCHEDULED SERVICE CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT FWD LOWER CORNER. REPAIRED DOOR SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001050800086 20010508 00086 NM 2001 5 8 SWAA011144 1 20010414 A 3350 101073 LIGHT BOEING 737 7377H4 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 712SW 27846 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT LT FWD SECTION. RELAMPED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001050800087 20010508 00087 NM 2001 5 8 SWAA011145 1 20010415 A 5523 BACB28AK04 BUSHING BOEING 737 7377H4 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 712SW 27846 DURING SCHEDULED SERVICE CHECK (SWA SI 11038-55), FOUND LT & RT ELEVATOR TABS LOOSE AT INBD HINGES. R&R ELEVATOR TAB BUS HINGS & HARDWARE PER MM. 2 L 7 2 4F RT A16WE 2001050800088 20010508 00088 NM 2001 5 8 SWAA011146 1 20010416 A 3350 65C27093 LENS BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 AFT ENTRY DOOR EMERGENCY EXIT LIGHT LENS COVER LOOSE. SECURED LENS COVER PER MM. 2 L 7 2 4F A16WE 2001050800089 20010508 00089 NM 2001 5 8 SWAA011147 1 20010415 A 5330 6545773 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED SPECIAL VISIT, FOUND EXTERNAL FUSELAGE SKIN CRACKED AT BS 727B, STR 10L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001050800090 20010508 00090 NM 2001 5 8 SWAA011148 1 20010415 A 5330 6545766 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED SPECIAL VISIT, FOUND EXTERNAL FUSELAGE SKIN CRACKED AT BS 500B, STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001050800091 20010508 00091 NM 2001 5 8 SWAA011149 1 20010416 A 5240 6545871 DOOR FRAME BOEING 737 7373H4 1384600 NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 625SW 27701 DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR FRAME CUTOUTS CRACKED AT AFT STOPS NR3 & NR4. REPAIRED DOOR FRAME PER SW A TI. 2 L 7 2 4F RT A16WE 2001050800092 20010508 00092 NM 2001 5 8 SWAA011150 1 20010415 A 5754 65C26686 SKIN BOEING 737 737317 138447P NM L/E SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED C1 CHECK, FOUND NR3 L/E SLAT LOWER SKIN CRACKED AT INBD AUX TRACK. REPAIRED SLAT SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001050800093 20010508 00093 NM 2001 5 8 SWAA011151 1 20010416 A 5315 6546804 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 514SW 25153 DURING SCHEDULED D CHECK AT DALFORT, FOUND FLOOR BEAM CORRODED AT BS 986, RBL 18 TO RBL 40. REPAIRED FLOOR BEAM PER SRM. 2 L 7 2 4F RT A16WE 2001050800094 20010508 00094 NM 2001 5 8 SWAA011152 1 20010416 A 5311 6546529 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 514SW 25153 DURING SCHEDULED D CHECK AT DALFORT, FOUND FUSELAGE FRAME CRACKS EXTENDING FROM FASTENER HOLES AT BS 400, BELOW STR 8L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001050800095 20010508 00095 NM 2001 5 8 SWAA011153 1 20010414 A 2751 6554401 SENSOR BOEING 737 7372H4 138448C NM L/E FLAP FAULTY A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 102SW 23108 AIR TURNBACK, NR 4 KRUGER FLAP IN TRANSIT LIGHT WOULD NOT EXTINGUISH AT FLAPS 10 DEG POSITION. R&R NR 4 KRUGER FLAP DOWN SENSOR PER MM & BAC WDM. OPS CHECK GOOD. 2 L 7 2 4F A16WE 2001050800096 20010508 00096 2001 5 8 SWAA011154 4 20010415 A 3442 MI5851622 INDICATOR BOEING 737 7372H4 138448C NM COCKPIT INOPERATIVE A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 102SW 23108 AIR TURNBACK, WX RADAR INDICATOR INOP OUT DURING TAKEOFF. R&R WX RADAR INDICATOR PER MM, OPS CHECK GOOD. 2 L 7 2 4F A16WE 2001050800097 20010508 00097 NM 2001 5 8 SWAA011155 1 20010414 A 5523 BACB28U6B30 BUSHING BOEING 737 7375H4 138449D NM ELEVATOR TAB WORN A SWAA O OTHER F E FLT CONT AFFECTED VIBRATION/BUFFET CL CLIMB 1 SW 07 506SW 24183 FLT CONTROL VIBRATION FELT ABOVE 230 KTS. VIBRATION INCREASES WITH POSITIVE ANGLE OF ATTACK. R&R LT ELEVATOR TAB INBD H INGE BUSHINGS & HARDWARE PER MM. 2 L 7 2 4F RT A16WE 2001050800098 20010508 00098 2001 5 8 SWAA011156 4 20010413 A 2565 6567380 CONTAINER BOEING 737 737301 1384611 NM SERVICE DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 AFT SERVICE DOOR EMERGENCY EVAC SLIDE CONTAINER CAME LOOSE. INSPECTED SLIDE & RESECURED CONTAINER. 2 L 7 2 4F RT A16WE 2001050800099 20010508 00099 NM 2001 5 8 SWAA011157 1 20010416 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 355SW 25250 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKS AT BS 727D, STR 9L & 9R. REPAIRED FRAMES PER SRM & BFG ER. 2 L 7 2 4F RT A16WE 2001050800100 20010508 00100 NM 2001 5 8 SWAA011158 1 20010413 A 5311 6546557 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 355SW 25250 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKS AT BS 867, STR 9L & 9R. REPAIRED FRAMES PER SRM & BFG ER. 2 L 7 2 4F RT A16WE 2001050800101 20010508 00101 NM 2001 5 8 SWAA011159 1 20010413 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 355SW 25250 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 827 & BS 907, STR 9L. REPAIRED FRAMES PER SRM & BFG ER. 2 L 7 2 4F RT A16WE 2001050800102 20010508 00102 NM 2001 5 8 SWAA011160 1 20010411 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 355SW 25250 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 400, BS 480 & BS 787, STR 9R. REPAIRED FRAMES PER SRM & BF G ER. 2 L 7 2 4F RT A16WE 2001050800103 20010508 00103 NM 2001 5 8 SWAA011161 1 20010415 A 5753 6546486 WEDGE BOEING 737 737317 138447P NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED C1 CHECK, FOUND LT WING INBD MID FLAP T/E WEDGE PANEL DISBONDED. R&R T/E WEDGE PER MM. 2 L 7 2 4F RT A16WE 2001050800104 20010508 00104 NM 2001 5 8 SWAA011162 1 20010415 A 3350 101073 LIGHT BOEING 737 737317 138447P NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED C1 CHECK, FOUND 3 EA. BULBS INOP IN AFT ENTRY DOOR EMERGENCY EXIT LIGHT. RELAMPED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001050800105 20010508 00105 2001 5 8 SWAA011163 4 20010416 A 2565 65C19901 CABLE BOEING 737 737317 138447P NM EVAC SLIDE MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT CABLE ASSY MISROUTED. REPOSITIONED CABLE ASSY PE R MM. 2 L 7 2 4F RT A16WE 2001050800106 20010508 00106 NM 2001 5 8 SWAA011223 1 20010424 A 2560 P2070001 FLASHLIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 691WN 23781 EMERGENCY FLASHLIGHT INOP AT AFT CABIN. R&R FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2001050800107 20010508 00107 NM 2001 5 8 SWAA011224 1 20010423 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 635SW 27708 EEPLS INOP AT ROW 14. REPAIRED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001050800108 20010508 00108 NM 2001 5 8 SWAA011225 1 20010422 A 3350 BR2013 LIGHT BOEING 737 7377H4 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 716SW 27850 EEPLS LOOSE AT FWD SECTION. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001050800109 20010508 00109 NM 2001 5 8 SWAA011226 1 20010424 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 716SW 27850 EEPLS TRACK COVER LOOSE AT FWD SECTION. R&R TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001050800110 20010508 00110 2001 5 8 SWAA011227 4 20010423 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY P ER MM. 2 L 7 2 4F A16WE 2001050800111 20010508 00111 NM 2001 5 8 SWAA011228 1 20010424 A 5330 6545769 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 446, FWD OF AFT RADIO ALTIMETER ANTENNA. REPAIRED SKIN PER S RM. 2 L 7 2 4F A16WE 2001050800112 20010508 00112 NM 2001 5 8 SWAA011229 1 20010424 A 5315 6546804 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOOR BEAM WEB CRACKED AT BS 707 TO BS 713, LBL 25. REPAIRED FLOOR BEAM PER SRM. 2 L 7 2 4F A16WE 2001050800113 20010508 00113 NM 2001 5 8 SWAA011230 1 20010424 A 5320 6551698 SPLICE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D CHECK, FOUND STR SPLICE CAP CRACKED AT BS 907, STR 4L. R&R SPLICE CAP PER SRM. 2 L 7 2 4F A16WE 2001050800114 20010508 00114 NM 2001 5 8 SWAA011231 1 20010423 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED C3 CHECK, FOUND 2.5 LONG FUSELAGE SKIN CRACK AT BS 510, STR 12 R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001050800115 20010508 00115 NM 2001 5 8 SWAA011232 1 20010424 A 5315 6546804 FLOORBEAM BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED 1/2D CHECK, FOUND FLOOR BEAMS CORRODED AT BS 360, LBL 12 TO RBL 64 & BS 344, RBL 60 TO LBL 64. REPAIRE D FLOOR BEAMS PER SRM. 2 L 7 2 4F RT A16WE 2001050800116 20010508 00116 NM 2001 5 8 SWAA011233 1 20010424 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 519SW 25318 DURING SCHEDULED A2 CHECK, FOUND EEPLS INOP AT FWD SECTION. RELAMPED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001050800117 20010508 00117 NM 2001 5 8 SWAA011234 1 20010424 A 5523 BACB28AK04 BUSHING BOEING 737 7377H4 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 748SW 29800 DURING SERVICE CHECK (SWA SI 11038-55), FOUND EXCESSIVE PLAY AT RT ELEVATOR TAB ATTACH BOLTS AT NR2, NR3 & NR4 HINGES. R &R ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2001050800118 20010508 00118 2001 5 8 SWAA011235 4 20010425 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 394SW 27380 FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE. RESECURED EVAC SLIDE CASE TO DOOR PER MM. 2 L 7 2 4F RT A16WE 2001050800119 20010508 00119 2001 5 8 SWAA011236 4 20010425 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 641SW 27714 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001050800120 20010508 00120 NM 2001 5 8 SWAA011237 1 20010425 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D CHECK, FOUND 2 EA CRACKS AT STR 11R, BS 484 & BS 500+4. REPAIRED STR PER SRM & BAC DWG. 2 L 7 2 4F A16WE 2001050800121 20010508 00121 NM 2001 5 8 SWAA011238 1 20010425 A 5320 65C27314 STRINGER CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D CHECK, FOUND STR CLIP CRACKED AT BS 301, STR 9L. R&R STR CLIP PER SRM. 2 L 7 2 4F A16WE 2001050800122 20010508 00122 NM 2001 5 8 SWAA011239 1 20010425 A 5551 6551524 FITTING BOEING 737 7372H4 138448C NM HORIZ STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D CHECK, FOUND LT HORIZ STAB CENTER SECTION AFT SPAR UPPER CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED F ITTING PER BFG ER. 2 L 7 2 4F A16WE 2001050800123 20010508 00123 NM 2001 5 8 SWAA011240 1 20010425 A 5551 6551524 FITTING BOEING 737 7372H4 138448C NM HORIZ STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D CHECK, FOUND RT HORIZ STAB CENTER SECTION FRONT SPAR UPPER CLEVIS AFT LUG CORRODED. REPAIRED FITTING PER BFG ER. 2 L 7 2 4F A16WE 2001050800124 20010508 00124 NM 2001 5 8 SWAA011241 1 20010424 A 5330 6545857 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA T1-353 -041. 2 L 7 2 4F RT A16WE 2001050800125 20010508 00125 NM 2001 5 8 SWAA011242 1 20010424 A 3350 BR2013 TRACK BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 511SW 24188 DURING SCHEDULED C4 CHECK, FOUND EEPLS TRACK LOOSE AT ROWS 3 & 7. REPAIRED TRACK PER MM. 2 L 7 2 4F RT A16WE 2001050800126 20010508 00126 NM 2001 5 8 SWAA011243 1 20010424 A 3350 BR2013 LIGHT BOEING 737 7377H4 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 705SW 27839 DURING SCHEDULED C3 CHECK, FOUND EEPLS LIGHT INOP AT ROW 15. RELAMPED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001050800127 20010508 00127 NM 2001 5 8 SWAA011244 1 20010424 A 5330 6552880 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 680AA 23505 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA RA. 2 L 7 2 4F RT A16WE 2001050800128 20010508 00128 2001 5 8 SWAA011245 4 20010424 A 2565 65C16820 RETAINER BOEING 737 7373A4 1384585 NM SERVICE DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 680AA 23505 DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER LOOSE. SECURED RETAINER PER MM. 2 L 7 2 4F RT A16WE 2001050800129 20010508 00129 2001 5 8 SWAA011246 4 20010425 A 2565 D31354 SLIDE BOEING 737 7372T4 1384492 NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. READJUSTED EMERGENCY EVAC SLIDE PE R MM. 2 L 7 2 4F A16WE 2001050800130 20010508 00130 NM 2001 5 8 SWAA011247 1 20010425 A 3397 BR2013 WIRE BOEING 737 7375H4 138449D NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 519SW 25318 EEPLS TRACK WIRES EXPOSED. RESECURED EEPLS WIRES PER MM. 2 L 7 2 4F RT A16WE 2001050800131 20010508 00131 2001 5 8 SWAA011248 4 20010425 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 316SW 23338 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001050800132 20010508 00132 2001 5 8 SWAA011249 4 20010426 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. R&R EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001050800133 20010508 00133 NM 2001 5 8 SWAA011250 1 20010425 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 390SW 26593 EEPLS TRACK COVER LOOSE AT MID CABIN. R&R TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001050800134 20010508 00134 2001 5 8 SWAA011251 4 20010425 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001050800135 20010508 00135 NM 2001 5 8 SWAA011252 1 20010425 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM SERVICE DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 067SW 22356 FWD SVC DOOR EMERGENCY EXIT LIGHT INOP. R&R EMERGENCY EXIT LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 2001050800136 20010508 00136 NM 2001 5 8 SWAA011253 1 20010426 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 FUSELAGE SKIN CRACKED AT BS 967, STR 21L AND BS 927, STR 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001050800137 20010508 00137 NM 2001 5 8 SWAA011254 1 20010426 A 5541 65C25842 SPAR BOEING 737 7373A4 1384585 NM RUDDER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED 1/2D CHECK, FOUND RUDDER FWD SPAR CRACKED AT STA 27.95. REPAIRED PER BFG ER. 2 L 7 2 4F RT A16WE 2001050800138 20010508 00138 NM 2001 5 8 SWAA011255 1 20010426 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 DURING SCHEDULED SERV CHECK FOUND 2 CRACK IN FUSELAGE SKIN AT BS 727E, STR 22R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001050800139 20010508 00139 NM 2001 5 8 SWAA011256 1 20010425 A 5320 BAC1503 STIFFENER BOEING 737 7373A4 1384585 NM MLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED SERVICE CHECK FOUND VERTICAL STIFFNER CRACKED IN MLG WW BULKHEAD AT BS 663, LBL 6.5. REPAIRED STIFFNER PER SWA RA. 2 L 7 2 4F RT A16WE 2001050800140 20010508 00140 NM 2001 5 8 SWAA011257 1 20010426 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 626SW 27702 DURING SCHEDULED 1/2D CHECK, FOUND FLOOR BEAM CRACKED AT BS 787, RBL 13. REPAIRED FLOOR BEAM PER SRM. 2 L 7 2 4F RT A16WE 2001050800141 20010508 00141 NM 2001 5 8 SWAA011258 1 20010426 A 5553 6553834 ATTACH FITTING BOEING 737 7375H4 138449D NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 514SW 25153 DURING SCHEDULED D CHECK, FOUND VERTICAL STAB ATTACH FITTING DRAG ANGLE CORRODED AT LT FWD LUG. R&R LH FWD DRAG ANGLE PE R SRM. 2 L 7 2 4F RT A16WE 2001050800142 20010508 00142 NM 2001 5 8 SWAA011259 1 20010426 A 5553 6546872 ATTACH FITTING BOEING 737 7375H4 138449D NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 514SW 25153 DURING SCHEDULED D CHECK, VERTICAL STAB ATTACH FITTING RT AFT OUTBD LUG CORRODED. REPAIRED PER DLF XEA. 2 L 7 2 4F RT A16WE 2001050800143 20010508 00143 NM 2001 5 8 SWAA011260 1 20010425 A 5320 BAC1498 ANGLE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D CHECK, FOUND ANGLE CRACKED BS 301, STR14L. R&R ANGLE PER SRM. 2 L 7 2 4F A16WE 2001050800144 20010508 00144 2001 5 8 SWAA011309 4 20010501 A 2565 65C16820 RETAINER BOEING 737 7373H4 1384600 NM ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM. 2 L 7 2 4F RT A16WE 2001050800145 20010508 00145 NM 2001 5 8 SWAA011310 1 20010501 A 3350 655663 LENS BOEING 737 7373Q8 1384670 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 317WN 24068 DURING SCHEDULED C3 CHECK, FOUND LT & RT OVERWING EMERGENCY EXIT LIGHT LENSES LOOSE. SECURED LENSES PER MM. 2 L 7 2 4F RT A16WE 2001050800146 20010508 00146 NM 2001 5 8 SWAA011311 1 20010430 A 3397 BR2013 WIRE BOEING 737 7375H4 138449D NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 519SW 25318 EEPLS TRACK WIRING EXPOSED AT MID CABIN. SECURED EEPLS WIRING PER MM. 2 L 7 2 4F RT A16WE 2001050800147 20010508 00147 2001 5 8 SWAA011312 4 20010502 A 2565 D31591 SLIDE BOEING 737 7373G7 1384595 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CASE. REINSTALLED SLIDE IN CASE PER MM. 2 L 7 2 4F RT A16WE 2001050800148 20010508 00148 2001 5 8 SWAA011313 4 20010501 A 2565 C31591 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 623SW 27933 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRES IND OUT OF LIMITS. R&R EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001050800149 20010508 00149 NM 2001 5 8 SWAA011314 1 20010501 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 EEPLS TRACK WIRING EXPOSED AT MID CABIN. RESECURED EEPLS WIRING PER MM. 2 L 7 2 4F RT A16WE 2001050800150 20010508 00150 2001 5 8 SWAA011315 4 20010501 A 2565 D31354 SLIDE BOEING 737 7372T4 1384492 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 AFT ENTRY DOOR AND AFT SVC DOOR EMERGENCY EVAC SLIDES PRES IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDES PER MM. 2 L 7 2 4F A16WE 2001050800151 20010508 00151 NM 2001 5 8 SWAA011316 1 20010502 A 2731 6545166 ROD END BOEING 737 7377H4 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 720WN 27854 DURING RON,AD 11052-55 FOUND LT ELEVATOR TRIM TAB CONTROL ROD ENDS WORN. R&R TAB CONTROL ROD ENDS PER MM. 2 L 7 2 4F RT A16WE 2001050800152 20010508 00152 NM 2001 5 8 SWAA011317 1 20010501 A 5240 6545871 DOOR FRAME BOEING 737 7373H4 1384600 NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 627SW 27935 DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR FWD FRAME CRACKED AT CUTOUT FOR NR 3 STOP. REPAIRED FRAME PER SWA TR. 2 L 7 2 4F RT A16WE 2001050800153 20010508 00153 NM 2001 5 8 SWAA011318 1 20010502 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 091SW 22963 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 25L. REPAIRED SKIN PER SRM 2 L 7 2 4F A16WE 2001050800154 20010508 00154 NM 2001 5 8 SWAA011319 1 20010501 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 745, ABOVE STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001050800155 20010508 00155 NM 2001 5 8 SWAA011320 1 20010502 A 5311 6546543 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 767 & BS 787, STR 13L. REPAIRED FRAMES PER SRM. 2 L 7 2 4F A16WE 2001050800156 20010508 00156 NM 2001 5 8 SWAA011321 1 20010502 A 5330 6545771 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 308SA 23498 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 517, STR 13L REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001050800157 20010508 00157 NM 2001 5 8 SWAA011322 1 20010501 A 5311 6545877 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, BETWEEN STR 19R & 20R. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2001050800158 20010508 00158 NM 2001 5 8 SWAA011323 1 20010502 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D CHECK, FOUND CORROSION ON STRINGER 20L, BS 847. REPAIRED STR PER SRM. 2 L 7 2 4F A16WE 2001050800159 20010508 00159 NM 2001 5 8 SWAA011324 1 20010501 A 5311 6547853 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D CHECK, FOUND CORROSION ON AFT CARGO COMPT FRAME AT BS 847, INBD OF STR 22R, WL 167, RBL 61. REPAIRED FRAME PER SRM & BAC SB. 2 L 7 2 4F A16WE 2001050800160 20010508 00160 NM 2001 5 8 SWAA011302 1 20010429 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 644SW 28329 EEPLS FLOOR TRACK COVER LOOSE AT FWD CABIN. R&R TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001050800161 20010508 00161 2001 5 8 SWAA011303 4 20010430 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRES IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLI DE ASSY PER MM. 2 L 7 2 4F A16WE 2001050800162 20010508 00162 NM 2001 5 8 SWAA011304 1 20010501 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 312SW 23334 EMERGENCY FLASHLIGHT INOP IN AFT CABIN LOWER POSITION. R&R EMERGENCY FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2001050800163 20010508 00163 NM 2001 5 8 SWAA011305 1 20010501 A 3350 079123 COVER BOEING 737 7375H4 138449D NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24182 DURING RON, FOUND EEPLS TRACK COVER MISSING AT MID CABIN. INSTALLED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001050800164 20010508 00164 2001 5 8 SWAA011306 4 20010430 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRES IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC S LIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001050800165 20010508 00165 2001 5 8 SWAA011307 4 20010430 A 2565 65C16820 RETAINER BOEING 737 7373Y0 1384671 NM ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 665WN 23497 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. RESECURED GIRT BAR HOOK PER MM . 2 L 7 2 4F RT A16WE 2001050800166 20010508 00166 NM 2001 5 8 SWAA011308 1 20010501 A 3397 BR2013 WIRE BOEING 737 7375H4 138449D NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 519SW 25318 EEPLS TRACK WIRES EXPOSED AT MID CABIN. RESECURED EEPLS WIRES PER MM. 2 L 7 2 4F RT A16WE 2001050800167 20010508 00167 2001 5 8 SWAA011278 4 20010429 A 3418 6554792 SENSOR BOEING 737 7372H4 138448C NM STALL WARNING MALFUNCTIONED A SWAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 07 092SW 22964 ABORTED TAKEOFF, STALL WARNING CONTROL COLUMN SHAKER ACTIVATED. R&R AOA VANE PER MM. 2 L 7 2 4F A16WE 2001050800168 20010508 00168 NM 2001 5 8 SWAA011279 1 20010428 A 3350 207377 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING RON FOUND EEPLS FLOOR TRACK HAD LENS MISSING. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2001050800169 20010508 00169 NM 2001 5 8 SWAA011280 1 20010429 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 EEPLS TRACK WIRING EXPOSED. RESECURED EEPLS WIRES PER MM. 2 L 7 2 4F RT A16WE 2001050800170 20010508 00170 NM 2001 5 8 SWAA011281 1 20010429 A 3350 101073 LIGHT BOEING 737 7373H4 1384600 NM SERVICE DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 397SW 27691 FWD SVC DOOR EMERGENCY EXIT LIGHT BROKEN. R&R EMERGENCY EXIT LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001050800171 20010508 00171 NM 2001 5 8 SWAA011282 1 20010429 A 5230 65C36183 SKIN BOEING 737 7373H4 1384600 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 618WN 28034 DURING SCHEDULED A2 CHECK, FOUND SKIN CRACKED ON AFT CARGO DOOR AT LWR FWD CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001050800172 20010508 00172 NM 2001 5 8 SWAA011283 1 20010428 A 5320 BAC1503 STIFFENER BOEING 737 7373T5 NM MLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 667SW 23063 DURING SCHEDULED SERVICE CHECK, FOUND VERTICAL STIFFENER CRACKED IN MLG WW BULKHEAD AT BS 663 RBL 6.4. REPAIRED STIFFENE R PER SWA RA. 2 L 7 2 4F RT A16WE 2001050800173 20010508 00173 NM 2001 5 8 SWAA011284 1 20010429 A 5312 6517582 BULKHEAD BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED 1/2D CHECK, FOUND BS 178 VERTICAL BEAM WEBS CRACKED AT LBL 17.1 & RBL 17.1 WL 228. REPAIRED VERTICAL B EAM WEBS PER BFG ER. 2 L 7 2 4F RT A16WE 2001050800174 20010508 00174 NM 2001 5 8 SWAA011285 1 20010429 A 3350 101073 LIGHT BOEING 737 7373A4 1384585 NM ENTRY DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT BROKEN. R&R EMERGENCY EXIT LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001050800175 20010508 00175 NM 2001 5 8 SWAA011286 1 20010427 A 3350 BR2013 TRACK BOEING 737 7373T0 1384582 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 684WN 23941 DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK LOOSE AT ROW 15. RESECURED TRACK PER MM. 2 L 7 2 4F RT A16WE 2001050800176 20010508 00176 NM 2001 5 8 SWAA011287 1 20010430 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 635SW 27708 EEPLS INOP AT ROWS 4 TO 7 AND LOOSE AT ROW 9. REPAIRED AND RESECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001050800177 20010508 00177 NM 2001 5 8 SWAA011288 1 20010430 A 3397 BR2013 WIRE BOEING 737 7375H4 138449D NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 519SW 25318 EEPLS TRACK WIRING EXPOSED. RESECURED EEPLS WIRING PER MM. 2 L 7 2 4F RT A16WE 2001050800178 20010508 00178 NM 2001 5 8 SWAA011289 1 20010429 A 3350 57771 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 073SW 22673 DURING SCHEDULED C3 CHECK, FOUND EEPLS END CAP MISSING ON AFT END. INSTALLED END CAP PER MM. 2 L 7 2 4F A16WE 2001050800179 20010508 00179 NM 2001 5 8 SWAA011290 1 20010429 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 743SW 29279 DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK COVERS CRACKED AT VARIOUS LOCATIONS FROM ROW 1 TO ROW 19. R&R TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 2001050800180 20010508 00180 NM 2001 5 8 SWAA011291 1 20010429 A 5754 65C30462 SKIN BOEING 737 7373H4 1384600 NM L/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 633SW 27936 DURING SCHEDULED C3 CHECK, FOUND LT WING INBD FOREFLAP DELAMINATED ON UPPER SURFACE. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2001050800181 20010508 00181 NM 2001 5 8 SWAA011292 1 20010429 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D CHECK, FOUND STRINGER 6R CRACKED AT BS 1010. REPAIRED STR PER SRM. 2 L 7 2 4F A16WE 2001050800182 20010508 00182 NM 2001 5 8 SWAA011293 1 20010430 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B, STRINGER 4R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001050800183 20010508 00183 NM 2001 5 8 SWAA011294 1 20010428 A 5752 WES04B10GC BEARING BOEING 737 7373H4 1384600 NM AILERON TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 627SW 27935 DURING SCHEDULED 1/2D CHECK, FOUND PLAY AT LH WING AILERON TAB, OTBD HINGE BRACKET. R&R BEARING PER MM. 2 L 7 2 4F RT A16WE 2001050800184 20010508 00184 2001 5 8 SWAA011295 4 20010430 A 3425 4050270905 INDICATOR BOEING 737 7373H4 1384600 NM COCKPIT OVERHEATED A SWAA K NONE B M SMOKE/FUMES/ODORS/SPARKS OVER TEMP DE DESCENT 1 SW 07 399WN 27693 DURING DESCENT DETECTED ELECTRIAL BURNING SMELL IN COCKPIT. R&R CAPT HORIZ SIT IND PER MM. 2 L 7 2 4F RT A16WE 2001050800185 20010508 00185 NM 2001 5 8 SWAA011296 1 20010428 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D CHECK, FOUND FUSELAGE BELLY SKIN CRACKED BS 520, RBL 5. REPAIRED FUSELAGE SKIN PER SRM. 2 L 7 2 4F A16WE 2001050800186 20010508 00186 NM 2001 5 8 SWAA011297 1 20010430 A 5320 6551698 SPLICE BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE ANGLE CORRODED AT BS 906, STR 22 L. REPAIRED SPLICE ANGLE PER SRM. 2 L 7 2 4F A16WE 2001050800187 20010508 00187 NM 2001 5 8 SWAA011298 1 20010429 A 5311 6546546 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 747, BS 787 AND BS 807 ON STRINGER 13R. REPAIRED FRAMES PE R SRM. 2 L 7 2 4F A16WE 2001050800188 20010508 00188 NM 2001 5 8 SWAA011299 1 20010430 A 5320 65C27314 STRINGER CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 13R. REPAIRED STR CLIP PER SRM. 2 L 7 2 4F A16WE 2001050800189 20010508 00189 NM 2001 5 8 SWAA011300 1 20010430 A 5311 6551261 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D CHECK, FOUND FWD SVC DOORWAY FWD STUB FRAME CRACKED AT BS 295, RBL 56 AND WL 209. R&R STUB FRAME PER SRM. 2 L 7 2 4F A16WE 2001050800190 20010508 00190 NM 2001 5 8 SWAA011301 1 20010430 A 5320 6551698 SPLICE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 7L. REPAIRED STR SPLICE PER SRN. 2 L 7 2 4F A16WE 2001050800191 20010508 00191 NM 2001 5 8 SWAA011261 1 20010427 A 3350 BR2013 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 635SW 27708 EEPLS TRACK COVER MISSING ROWS 9&15. REPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2001050800192 20010508 00192 2001 5 8 SWAA011262 4 20010427 A 2565 D31591 SLIDE BOEING 737 7373Q8 1384670 NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. R&R EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001050800193 20010508 00193 NM 2001 5 8 SWAA011263 1 20010427 A 3350 BR2013 LIGHT BOEING 737 7377H4 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 700GS 27835 EEPLS TRACK LIGHTING LOOSE AT ROW 8. RESCURED EEPLS LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001050800194 20010508 00194 NM 2001 5 8 SWAA011264 1 20010427 A 5311 6546529 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, WL 207. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2001050800195 20010508 00195 NM 2001 5 8 SWAA011265 1 20010427 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D CHECK, FOUND 2 EA STRINGERS CORRODED AT BS 1008, 26R & 27L. REPAIRED STR PER SRM. 2 L 7 2 4F A16WE 2001050800196 20010508 00196 NM 2001 5 8 SWAA011266 1 20010427 A 5310 6546529 SHEAR TIE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 480, STR 14R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F A16WE 2001050800197 20010508 00197 NM 2001 5 8 SWAA011267 1 20010427 A 5522 65C25745 SKIN BOEING 737 7373H4 1384600 NM ELEVATOR DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 607SW 27927 DURING SCHEDULED C3 CHECK, FOUND LT ELEVATOR DELAMINATED IN THREE AREAS. REPAIRED LT ELEVATOR PER SRM. 2 L 7 2 4F RT A16WE 2001050800198 20010508 00198 NM 2001 5 8 SWAA011268 1 20010427 A 5522 65C27494 SKIN BOEING 737 7373H4 1384600 NM ELEVATOR DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 626SW 27702 DURING SCHEDULED 1/2D CHECK, FOUND LT ELEVATOR UPPER SKIN DELAMINATED AT STA 120. REPAIRED UPPER SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001050800199 20010508 00199 NM 2001 5 8 SWAA011269 1 20010428 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM ENTRY DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EMERGENCY LIGHT INOP. R&R EMERGENCY LIGHT PER MM. 2 L 7 2 4F A16WE 2001050800200 20010508 00200 NM 2001 5 8 SWAA011270 1 20010429 A 3350 BR2013 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 629SW 27704 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS TRACK TO HAVE MISSING AND CRACKED COVERS AT ROWS 7, 9, 12 AND 13. R&R TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 2001050900005 20010509 00005 NM 2001 5 9 AWXA0001650 1 20010426 A 5312 65163007 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 169AW 23630 FS 178 BLKHD HAS 1 INCH CRACK AT WL 197-198 LBL 4.8. CUT OUT DAMAGED WEB; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER AND FILLER IAW BOEING 737-300 SRM 53-10-08 TR 53-15 PG 1-11. 2 L 7 2 4F RT A16WE 2001050900006 20010509 00006 NM 2001 5 9 VNAA0104004 1 20010409 A 3243 AC69965 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE APRKING BRAKE FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 431JS 7758 0 3028 THE FLIGHT CREW RECEIVED A EMERGENCY PARKING BRAKE ACCUMULATOR LOW PRESSURE WARNING MESSAGE DURING FLIGHT. THE FLIGHT C REW REFERENCED THE QUICK REFERENCE HANDBOOK AND RETURNED TO THE FIELD. THE LANDING WAS MADE WITHOUT INCCIDENT. MAINTEN ANCE INSPECTED AND REPLACED THE EMERGENCY PARKING BRAKE VALVE IN ACCORDANCE WITH DONIER MAINTENANCE MANUAL 32-43-02. OP ERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001050900007 20010509 00007 NM 2001 5 9 VNAA0104007 1 20010412 A 2432 DTSP400L BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE E/E BAY OVERHEATED A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 460PS 12084 3061 WHILE EN ROUTE FROM PIT TO AZO, THE CREW RECEIVED A BATTERY OVERHEAT INDICATION ON THE RED WARNING PANEL. THE CREW FOLL OWED THE QUICK REFERENCE HANDBOOK AND CONTACTED MAINTENANCE CONTROL. THE CREW REPORTED THAT THE FLIGHT WOULD DIVERT INT O CAK. WHILE ON APPROACH THE INDICATION BECAME INTERMITTENT AND ON FINAL THE INDICATION HAD EXTINGUISHED. MAINTENANCE INSPECTED AND REPLACED THE RIGHT SIDE MAIN BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE FLIGHT CONTINUED TO AZO WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001050900008 20010509 00008 NM 2001 5 9 VNAA0104006 1 20010410 A 7603 001A761A1010100 SWITCH DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CONDITION LEVER FAULTY A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 460PS 3061 DURING THE TAKEOFF ROLL THE FLIGHT CREW RECEIVED A RIGHT ELECTRONIC ENGINE CONTROL FAIL MESSAGE. THE FLIGHT CREW ABORTE D THE TAKEOFF AND EXITED THE RUNWAY WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE RIGHT CONDITI ON LEVER MICROSWITCH RACK ASSEMBLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 76-11-05. OPERATIONAL CHECKS WERE COMP LETED AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001050900009 20010509 00009 NM 2001 5 9 VNAA0104008 1 20010415 A 3260 LIGHT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT INOPERATIVE A VNAA O OTHER N FALSE WARNING DE DESCENT 1 GL 07 460PS 3061 DURING DESCENT, FLIGHT 4065 HAD NO LEFT HAND GEAR DOWN INDICATION. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND C ONFIRMED THAT THE BULB WAS INOPERABLE. FLIGHT 4065 DID A GO AROUND AND HAD ATC CONFIRM GEAR WAS DOWN. FLIGHT 4065 EXEC UTED THE LANDING WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND GEAR INDICATION BULB IN AC CORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001050900010 20010509 00010 NM 2001 5 9 VNAA0104010 1 20010417 A 5270 WARNING LIGHT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT ILLUMINATED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 458PS 3068 BEFORE LEVELING OFF AT 24,000 FEET, THE CREW RECEIVED A RED WARNING PANEL INDICATION FOR THE MAIN CABIN DOOR. THE CREW CALLED MAINTENANCE CONTROL AND REFERENCED THE QUICK REFERENCE HANDBOOK WHICH INSTRUCTED THEM TO LAND AT THE NEAREST AIRP ORT. FLIGHT 4190 LANDED IN ROCHESTER WITHOUT ANY FURTHER INCIDENTS. OUTSTATION MAINTENANCE INSPECT THE AIRCRAFT AND FO UND NO DEFECTS. THE AIRCRAFT WAS FERRIED TO PIT WHERE MAINTENANCE TROUBLESHOT AND INSPECTED THE AIRCRAFT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. NO DEFECTS COULD BE FOUND. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAF T WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001050900012 20010509 00012 2001 5 9 VNAA0104012 4 20010418 A 3418 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT ACTIVATED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 433JS 3047 FLIGHT 4009 BEGAN THE TAKEOFF ROLL AND THE CREW RECEIVED A LEFT HAND ANGLE OF ATTACK FAIL CAS MESSAGE AND A SHAKER FAIL CAS MESSAGE. THE CREW ABORTED TAKEOFF AND CLEARED THE RUNWAY. AFTER FLIGHT 4009 CLEARED THE RUNWAY THE INDICATION EXTI NGUISHED. FLIGHT 4009 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4009 DEPARTED WITHOUT ANY FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001050900013 20010509 00013 NM 2001 5 9 VNAA0104014 1 20010420 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 458PS 9418 3068 THE CREW REPORTED THAT THE EMERGENCY LIGHTING WAS NOT OPERATING IN THE FIRST FLOORING STRIP. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY IN THE 5LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001050900014 20010509 00014 NM 2001 5 9 VNAA0104015 1 20010421 A 5270 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FALSE INDICATION A VNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 437JS 3055 WHILE CLIMBING THROUGH 14,000 FEET, THE CREW RECEIVED AN EMERGENCY ACCESS DOOR INDICATION ON THE RED WARNING PANEL. THE CREW REFERENCED THE QUICK REFERENCE HANDBOOK AND THE HANDBOOK DIRECTED THE CREW TO LAND AT THE NEAREST AIRPORT. THE CR EW CONFIRMED THE DOOR WAS THERE AND THAT IT WAS ONLY AN INDICATION PROBLEM. FLIGHT 4072 LANDED AT MGW WITH NO FURTHER I NCIDENT. OUTSTATION MAINTENANCE INSPECTED THE DOOR AND THE CREW PERFORMED OPERATIONAL CHECKS WHICH WERE GOOD. THE AIRC RAFT WAS RELEASED FOR SERVICE AND FLIGHT 4072 CONTINUED ON TO CHS WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001050900015 20010509 00015 NM 2001 5 9 VNAA0104016 1 20010423 A 2432 DTSP400L BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE E/E BAY OVERHEATED A VNAA L ABORTED APPROACH J M WARNING INDICATION OVER TEMP AP APPROACH 1 GL 07 439JS 8604 3057 WHILE TURNING ON FINAL, THE CREW NOTICED THERE WASN''T THREE GEAR LOCKED DOWN INDICATIONS. THE CREW INITIATED THE A GO AROUND AND CONTACTED MAINTENANCE CONTROL. THE PROBLEM WAS THEN CORRECTED. THE CREW ALSO RECEIVED A NR 1 BATTERY OVERHE AT WARNING ON THE RED WARNING PANEL. FLIGHT 4097 HAD TO DO TWO MORE GO AROUNDS DUE TO TRAFFIC. FLIGHT 4097 LANDED WITH NO FURTHER INCIDENTS. THE AIRCRAFT WAS FERRIED TO PIT WHERE THE NR 1 BATTERY WAS REPLACED IN ACCORDANCE WITH DORNIER M AINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001050900016 20010509 00016 WP 2001 5 9 MWEA010659 1 20010427 A 5310 J06011940 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 RIGHT SIDE SHEAR TIE IS CRACKED AT STATION 980 ABOVE LONGERON 15. REMOVED AND REPLACED SHEAR TIE. 2 L 7 2 4F A6WE 2001050900017 20010509 00017 WP 2001 5 9 MWEA010660 1 20010427 A 5347 995787115 SEAT TRACK DOUG DC9 DC932 3022066 WP COCKPIT DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 CAPTAINS AFT, INBOARD SEAT TRACK LOCKING HOLES ARE ELONGATED. FABRICATED AND INSTALLED REPAIR STRAP. 2 L 7 2 4F A6WE 2001050900018 20010509 00018 WP 2001 5 9 MWEA010662 1 20010427 A 5311 SR095300953 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 STATION 980 RIGHT SIDE FRAME IS CRACKED ON LOWER LEG AT LONGERON 17 RIGHT. FABRICATED AND INSTALLED DOUBLERS. 2 L 7 2 4F A6WE 2001050900019 20010509 00019 WP 2001 5 9 MWEA010663 1 20010427 A 5347 995787113 SEAT TRACK DOUG DC9 DC932 3022066 WP COCKPIT DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 CAPTAINS AFT SEAT TRACKS LOCKING HOLES ARE ELONGATED. FABRICATED AND INSTALLED REPAIR STRAP. 2 L 7 2 4F A6WE 2001050900020 20010509 00020 WP 2001 5 9 MWEA010664 1 20010427 A 5347 995787113 SEAT TRACK DOUG DC9 DC932 3022066 WP COCKPIT DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 F/O''S AFT OUTBOARD SEAT TRACK LOCKING HOLES ARE ELONGATED. FABRICATED AND INSTALLED REPAIR STRAP. 2 L 7 2 4F A6WE 2001050900021 20010509 00021 WP 2001 5 9 MWEA010657 1 20010427 A 5230 591014119 PAN DOUG DC9 DC915 3022036 WP CARGO DOOR CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 FORWARD CARGO DOOR PAN, AFT SIDE MODERATELY CHAFED ON RADIUS, NEXT TO DOOR LATCH. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001050900022 20010509 00022 WP 2001 5 9 MWEA010658 1 20010427 A 5311 991224672 FRAME DOUG DC9 DC915 3022036 WP FUSELAGE CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 FRAME IS CHAFED ON FORWARD SIDE IN AFT ACCCESSORY AT STATION 860 BETWEEN LONGERONS LEFT 5 AND LEFT 6. FABRICATED AND IN STALLED FRAME REPAIR PARTS. 2 L 7 2 4F A6WE 2001050900023 20010509 00023 WP 2001 5 9 MWEA010665 1 20010430 A 5320 99577373 INTERCOSTAL DOUG DC9 DC915 3022036 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 INTERCOSTAL AT STATION 817 AND LONGERON 3 LEFT IS CRACKED ON LOWER FLANGE. FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 2001050900024 20010509 00024 SO 2001 5 9 C2XA01CL090 1 20010427 A 3350 7287580505 LIGHT EMB 135 EMB135ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 14505 145192 CLE FLIGHT 3863 THE CREW REPORTED THE EMERGENCY FLOOR LIGHTS FROM SEAT 2A TO 6A WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY FLOOR LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001050900025 20010509 00025 WP 2001 5 9 CNMA200100013 1 20010427 A 3610 CLAMP DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE BLEED AIR LOOSE A CNMA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 630AX 46596 528116 AFTER TAKEOFF, NR 3 ENGINE FIRE WARNING ILLUMINATED AT CRUISE POWER. REDUCED POWER AND INDICATION CEASED. ACCOMPLISHED EMERGENCY PROCEDURES AND SHUT ENGINE DOWN. RETURNED TO ORIGINATING AIRPORT. INSPECTED ENGINE. FOUND LOOSE CLAMP ON P NEUMATIC DUCT AT TURBINE MIDFRAME AREA. REALIGNED DUCT, RETIGHTENED CLAMP, AND SAFETIED. PERFORMED GROUND ENGINE RUN. ALL PARAMETERS NORMAL. 2 L 7 3 4F 4 F A22WE E23EA 2001050900026 20010509 00026 EU 2001 5 9 C2XA01BT072 1 20010418 A 5311 S535726601200 FRAME AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26826 172 DURING 4C INSPECTION IN YUL, MAINTENANCE FOUND LEFT AND RIGHT HAND FRAME 25 CRACKED IN ONE PLACE ON EACH SIDE AROUND HYD RAULIC LINE FEED THROUGH. REPAIRED FRAME IAW COX EC 5310-01182. OK FOR SERVICE. 2 H 7 2 4T RT A53EU 2001050900027 20010509 00027 EU 2001 5 9 C2XA01BT073 1 20010418 A 5315 S5317220625801 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26826 172 DURING 4C INSPECTION IN YUL, MAINTENANCE FOUND CORROSION ON FLOORBEAM AT FRAME 9 ON CAPTAINS SIDE. CENTER FRAME 9 REMOV ED AND REPLACED IAW COX EC5310-01183. OK FOR SERVICE. 2 H 7 2 4T RT A53EU 2001050900028 20010509 00028 EU 2001 5 9 C2XA01BT074 1 20010418 A 5315 S5367221520200 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26826 172 DURING 4C INSPECTION IN YUL, MAINTENANCE FOUND THE FLOORBEAM AT FRAME 36 TO BE CORRODED BETWEEN BOTH CENTER SEAT TRACKS. CLEANED CORROSION, TREATED, AND INSTALLED REINFORCEMENT STRAP IAW COX EC5310-01037. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T RT A53EU 2001050900029 20010509 00029 EU 2001 5 9 C2XA01BT075 1 20010418 A 5320 S5367121720402 WEB AEROSP ATR42 ATR42320 8680930 EU FUSELAGE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26826 172 DURING 4C INSPECTION IN YUL, MAINTENANCE FOUND THAT THE PASSENGER DOOR FORWARD BOTTEM SPRING FITTING BROKE OFF WITH PART OF THE CREASE BEAM WHEN TENSION WAS APPLIED. MAINTENANCE MANUFACTURED A WEB IAW ATR42 SRM 53-67-70, WEB AND CREASE BEA M REMOVED AND REPLACED IAW ATR42 SRM 51-25-02 AND SRM 51-25-03. PASSENGER DOOR READJUSTED IAW ATR42 JIC 51-11-00 ADJ 10 000-001. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T RT A53EU 2001050900030 20010509 00030 EU 2001 5 9 C2XA01BT076 1 20010418 A 5320 S53678008268 INTERCOSTAL AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26826 172 DURING 4C INSPECTION IN YUL, MAINTENANCE FOUND UNDER PASSENGER DOOR THRESHOLD INTERCOSTAL BETWEEN FRAME 38 AND FRAME 39 TO BE CORRODED. REMOVED OLD INTERCOSTAL AND FABRICATED NEW INTERCOSTAL AND INSTALLED IAW ATR42 SRM 53-67-70 FIGURE 122 AND ATR42 SRM 51-25-01. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T RT A53EU 2001050900031 20010509 00031 EU 2001 5 9 C2XA01BT077 1 20010418 A 5330 S53872100120100 SKIN AEROSP ATR42 ATR42320 8680930 EU FUSELAGE DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26826 172 DURING 4C INSPECTION IN YUL, MAINTENANCE FOUND DENT FORWARD OF FRAME 43 BETWEEN STRINGERS 11 AND 12 ON THE RIGHTHAND SID E. REPAIRED IAW ATR42 SRM 53-00-00 FIGURE 408. OK FOR SERVICE. 2 H 7 2 4T RT A53EU 2001050900032 20010509 00032 EU 2001 5 9 C2XA01BT078 1 20010419 A 5280 D602602 HINGE FITTING AEROSP ATR42 ATR42320 8680930 EU RT MLG LOOSE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26826 172 DURING 4C INSPECTION IN YUL, MAINTENANCE FOUND RIGHTHAND MAIN LANDING GEAR DOOR HAS PLAY AT THE AFT HINGE FITTING AND LA NDING GEAR STRUT BOGEY. REMOVED RIGHTHAND MAIN GEAR DOOR, MAIN LANDING GEAR BARREL ATTACHMENT LUG REPAIRED IAW EXELTECH EO 42-32-27, REINSTALLED RIGHTHAND MAIN GEAR DOOR IAW ATR42 JIC 52-81-00 RAI 10000-009. 2 H 7 2 4T RT A53EU 2001050900033 20010509 00033 EU 2001 5 9 C2XA01BT079 1 20010419 A 5280 D602592 HINGE FITTING AEROSP ATR42 ATR42320 8680930 EU RT MLG LOOSE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26826 172 DURING 4C INSPECTION IN YUL, MAINTENANCE FOUND LEFTHAND MAIN LANDING GEAR DOOR HAS EXCESSIVE PLAY AT FORWARD AND AFT HIN GE FITTINGS AND AT DOOR ROD END. LEFTHAND MAIN GEAR DOOR REMOVED, LEFTHAND MAIN GEAR DOOR BEARINGS REMOVED AND REPLACED IAW ATR42 JIC 20-26-12, MAIN LANDING GEAR BARREL LUGS REPAIRED IAW EXELTECH EO 42-32-27, LEFTHAND MAIN GEAR DOOR REINST ALLED IAW ATR42 JIC 32-31-55. 2 H 7 2 4T RT A53EU 2001050900034 20010509 00034 WP 2001 5 9 AT0100122 1 20010406 A 2170 COALESCER BAG DOUG DC9 DC932 3022066 WP A/C BAY DIRTY A ZZDA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 15 831AT 47674 HOT OILY SMELL WAS NOTED AT 9000 FT. REPLACED COALESCER BAGS AND SEALS. 2 L 7 2 4F A6WE 2001050900035 20010509 00035 WP 2001 5 9 AT0100123 1 20010323 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP CABIN CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 837AT 45774 FOUND CABIN FLOOR PANEL AT BS 485-579 HAS SURFACE CORROSION. REMOVED CORROSION, MATERIAL LOSS OUT OF LIMITS. CUT, DRIL LED, TREATED, PRIMED, AND INSTALLED HAT AND SKIN PANEL SECTIONS IAW DC9 SRM 53-21-0 FIGURE 4, 52-30-2. 2 L 7 2 4F A6WE 2001050900036 20010509 00036 WP 2001 5 9 AT0100124 1 20010328 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP CABIN CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 837AT 45774 FOUND CABIN FLOOR PANEL NR 79 HAS A SURFACE CORROSION. REMOVED CORROSION, FABRICATED, TREATED, AND INSTALLED FLOOR PANE L IAW DC9 51-10-3, 53-21-0, 51-30-2. 2 L 7 2 4F A6WE 2001050900037 20010509 00037 WP 2001 5 9 AT0100125 1 20010325 A 3211 FITTING DOUG DC9 DC932 3022066 WP LT MLG CHAFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 837AT 45774 FOUND LEFT ATTACH FITTING FOR MLG CHAFED AT BS 735. BLENDED CHAFED AREA, TREATED, AND INSTALLED IAW DC9 SRM 51-10-6, 51 -10-3 DPS 4-999-2 AND TIMCO REO L00425. 2 L 7 2 4F A6WE 2001050900038 20010509 00038 WP 2001 5 9 CALA0100429 1 20010427 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 MID CARGO INTERCOSTAL AT FS 769-786 OUTBOARD OF LONG 28R IS CORRODED. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-10-3, 51-10-2, AND 51-10-5. 2 L 7 2 4F A6WE 2001050900039 20010509 00039 WP 2001 5 9 CALA0100430 1 20010428 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 AFT CARGO INTERCOSTAL AT 28L FROM STATION 1309 - 1320 HAS CORROSION. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-30-02, 51-30-05, AND 51-10-3. 2 L 7 2 4F A6WE 2001050900040 20010509 00040 WP 2001 5 9 CALA0100431 1 20010429 A 3350 RPS12 CHARGER DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14816 49370 EMERGENCY LIGHTS AT REAR GALLEY DOOR AND TAIL CONE DOOR INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY VASE PER MM 33-53-00 PG 407. 2 L 7 2 4F A6WE 2001050900041 20010509 00041 WP 2001 5 9 CALA0100432 1 20010430 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 L1 AFT TORQUE BOX WEB TANGS AT LONG 12 AND 15 ARE CRACKED. REPAIRED CRACKS. FABRICATED AND INSTALLED REPAIR FILLERS AN D DOUBLERS PER SRM 51-30-02 AND EC/RA 5310-04129. 2 L 7 2 4F A6WE 2001050900042 20010509 00042 WP 2001 5 9 CALA0100433 1 20010430 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 MID CARGO INTERCOSTAL HAS CORROSION AT FS 617-636 AT 29L. REMOVED DAMAGED SECTION. INSTALLED NEW INTERCOSTAL PER SRM 5 3-01 FIG 2 SHEET 3, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 2001050900043 20010509 00043 NM 2001 5 9 DHL2001701005 1 20010428 A 2750 BUSHING BOEING 727 72730C 1384009 NM T/E FLAP OUT OF ADJ A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 701DH 19011 A/C REQUIRES 5 DEG RT BANK TO MAINTAIN STRAIGHT FLIGHT. ADJUSTED ECCENTRIC BUSHINGS OF RIGHT WING INBOARD AFT FLAP PER MM 27-51-2. 2 L 7 3 4F A3WE 2001050900044 20010509 00044 2001 5 9 DHL2001365004 4 20010428 A 2210 AUTOPILOT SYS AIRBUS 300 A300B4203 3930306 EU COCKPIT MALFUNCTIONED A DHLA K NONE O OTHER AP APPROACH 1 SO 01 365DH 149 NR 1 AUTOPILOT WOULD NOT STAY ENGAGED DURING APPROACH. RESEATED NR 1 LOGIC COMPUTER AND PERFORMED OPS TEST PER MM 22-13 -00. CHECKED GOOD ON GROUND. 2 L 7 2 4F RT A35EU 2001050900045 20010509 00045 2001 5 9 DHL2001365006 4 20010428 A 2210 AUTOPILOT SYS AIRBUS 300 A300B4203 3930306 EU COCKPIT MALFUNCTIONED A DHLA K NONE O OTHER AP APPROACH 1 SO 01 365DH 149 NR 2 AUTOPILOT WOULD NOT STAY ENGAGED DURING APPROACH. RESEATED NR 2 LOGIC COMPUTER AND PERFORMED OPS TEST PER 22-13-00 . CHECKED GOOD ON GROUND. 2 L 7 2 4F RT A35EU 2001050900046 20010509 00046 NM 2001 5 9 DHL2001712005 1 20010429 A 3260 DOWNLOCK SWITCH BOEING 727 72729 1384007 NM NLG OUT OF POSITION A DHLA O OTHER N FALSE WARNING LD LANDING 1 SO 01 712DH 19401 DURING GEAR EXTENSION, NOSE GEAR INTRANSIT LIGHT AND GEAR DOWN LIGHT DID NOT ILLUMINATE. RAN ABNORMAL PROCEDURE 6.2 67 LIGHT STAYED OUT. VERIFIED NOSE GEAR DOWN THRU VIEWING PORT. AFTER GEAR WAS VERIFIED DOWN AND LOCKED, WHEN POWER WAS R EDUCED, GEAR WARNING HORN WENT OFF. REPOSITIONED LOCK SWITCH WIRE BUNDLE MOUNT AND CLAMP, REATTACHED THE SEPARATED WIRE S AT THE LOCK SWITCH AND OPS CK'D PER 32-61-71 OK. 2 L 7 3 4F A3WE 2001050900047 20010509 00047 NM 2001 5 9 DHL2001724004 1 20010427 A 2611 SMOKE WARNING BOEING 727 727228 NM COCKPIT FALSE INDICATION A DHLA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 724DH 19862 LOWER CARGO SMOKE MX LIGHT ILLUMINATED. PERFORMED SYSTEM ADV/TEST PER 26-16-0, PAGE 501. SYS OFF LIGHT EXTINGUISHED AN D DID NOT COME BACK ON. 2 L 7 3 4F A3WE 2001050900048 20010509 00048 2001 5 9 DHL2001701007 4 20010427 A 2210 SENSOR BOEING 727 72730C 1384009 NM ELEVATOR LOOSE A DHLA K NONE O OTHER CR CRUISE 1 SO 01 701DH 19011 AT FL330 AT M.78 YOKE OSCILLATES BACK AND FORTH WITH AUTO-PILOT SELECTED ON SERVO-A. TIGHTENED CRANK ON A-SYS ELEVATOR POSITION SENSOR IAW B727 22-11-77 OP CK GOOD. NORMAL ON GROUND IAW B727 M/M 22-11-71. 2 L 7 3 4F A3WE 2001050900049 20010509 00049 NM 2001 5 9 DHL2001709005 1 20010428 A 3350 BATTERY BOEING 727 72782C 1384026 NM CABIN DISCHARGED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 709DH 19968 EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED ALL DOOR EMER EXIT BATTERIES WITH SERVICABLE. OPS CHECK GOOD I AW MM 33-50-01. 2 L 7 3 4F A3WE 2001050900050 20010509 00050 WP 2001 5 9 AT0100126 1 20010326 A 5743 ATTACH FITTING DOUG DC9 DC932 3022066 WP RT WING CHAFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 837AT 45774 FOUND RIGHT ATTACH FITTING FOR MLG CHAFED AT BS 737. BLENDED CHAFED AREA, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51- 10-3, 51-10-6 TIMCO REO L-00426 AND DRS 4-999-2. 2 L 7 2 4F A6WE 2001050900051 20010509 00051 NM 2001 5 9 HNAA0100028 1 20010427 A 5310 PRESSURE PANEL DHAV DHC8 DHC8102 2809003 NM NLG WW CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 938HA 32670 152 DURING INSPECTION, (NOSE LANDING GEAR BAY) THE FORWARD LEFT HAND SIDE OF NOSE WHEEL BAY WAS CRACKED AT J-CHANNEL SIDEWAL L. REPAIRED IAW RD8-53-675. 2 H 7 2 4T RT A13NM 2001050900052 20010509 00052 NE 2001 5 9 MWEA010667 2 20010427 A 7314 378200 PUMP DOUG DC9 DC915 3022036 WP PWA JT8 JT8D7B 52053 NE RT ENGINE FAILED A MWEA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 GL 31 300ME 45718 6573957B DURING CRUISE RIGHT ENGINE UNSPOOLED TO 75 PERCENT. REMOVED AND REPLACED RIGHT ENGINE FUEL PUMP. 2 L 7 2 4F 4 F A6WE E2EA 2001050900053 20010509 00053 SO 2001 5 9 SWIA972534 1 20010419 A 3241 CAP EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT MLG WHEEL FAULTY A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 581SW 120349 DURING TAKEOFF ROLL, THE BRAKES MAP AND THE LEFT ANTI-SKID INOP LIGHTS CAME ON. ABORTED TAKEOFF AND RETURNED TO THE GAT E. REPLACED LEFT OUTBOARD BRAKE WHEEL HUB CAP ASSEMBLY. GROUND CHECK TEST NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 2001050900054 20010509 00054 SO 2001 5 9 SWIA972535 1 20010429 A 2722 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RUDDER FAILED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 215SW 120281 RUDDER BLUE SYSTEM INOP. (PILOT REPORTED RUDDER ACTUATOR LOCKED UP IN FLIGHT.) RUDDER PCU STARTING TO LEAK AND TESTS O N THE LOW END OF THE RUDDER HEALTH CHECK FOR BLUE SYSTEM. REMOVED AND REPLACED BLUE SYSTEM RUDDER ACTUATOR IAW EMB MM 2 7-22-024. PERFORMED RUDDER HYDRAULIC SYSTEM HEALTH CHECK IAW EMB MM 27-22-00 TO C/W FCD 00-09-27R2. RUDDER HEALTH CHEC K PASSED. OPS CHECK GOOD OF RUDDER SYSTEM. ALL PANELS VERIFIED CLOSED. LEAK CHECK GOOD. REMOVED RUDDER PCU AND INSTA LLED SERVICEABLE UNIT IAW MM 27-22-11 AND RII 27-312. OPS AND LEAK CHECK GOOD. ALSO PERFORMED RUDDER HEALTH CHECK IAW MM 27-22-00. CHECKED GOOD. P/N: 32100-1003, S/N ON: 0215A, S/N OFF: 0287. 2 L 7 2 4T 4 T RT A31SO E20NE 2001050900055 20010509 00055 2001 5 9 SWIA972536 4 20010428 A 3418 COMPUTER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE E/E BAY FAULTY A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 235SW 120310 AT 1500 FT AGL STALL WARNING AURAL ACTIVATED. UPON LANDING STALL WARNING AURAL ACTIVATED AGAIN. REPLACED NR 2 STALL WA RNING COMPUTER. ALL FUNCTIONAL CHECKS OF THE STALL WARNING SYSTEM FOUND GOOD (S/N ON 633, S/N OFF 770). 2 L 7 2 4T 4 T RT A31SO E20NE 2001050900056 20010509 00056 EA 2001 5 9 SWIA972537 1 20010427 A 2760 PCU CNDAIR CL600 CL6002B19 EA SPOILER FAULTY A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 411SW 7067 ABORTED TAKEOFF DUE TO FLIGHT SPOILER WARNING EICAS MESSAGE WITH TAKEOFF CONFIG OK. MESSAGE FOR FLIGHT SPOILER WARNING AT APPROX 80 N1. PERFORMED AN OPS CHECK OF THE FLIGHT SPOILER WARNING AT 80 PERCENT N1 AND TAKEOFF CONFIGURATION. OK, NO WARNING NOTED. REMOVED AND REPLACED LEFT FLIGHT SPOILER OUTBOARD PCU IAW MM 27-62-01. P/N ON 27000-7, S/N ON 0474, S/N OFF 0514. 2 L 7 2 4F RT A21EA 2001050900057 20010509 00057 NE 2001 5 9 ARWA74100 2 20010426 A 7230 COMPRESSOR DOUG DC8 DC863 302198A WP PWA JT3D JT3D7 52039 NE NR 3 ENGINE STALLED A ARWA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 19 345JW 46042 671393 TAKEOFF ROLL WAS ABORTED AT 65 KNOTS DUE TO COMPRESSOR STALL ON NR 3 ENGINE. PERFORMED TEST OF COMPRESSOR BLEED VALVE I AW MM 75-30-3, FOUND NORMAL. CHECKED ON ENGINE RUN UP IAW MM 71-00, FOUND NORMAL OPERATION NO COMPRESSOR STALL NOTED. 2 L 7 4 4F 4 F 4A25 1E8 2001050900058 20010509 00058 EU 2001 5 9 JBXA000274 1 20010430 A 3150 WARNING SYSTEM FOKKER F28 F28MK0100 4990807 EU COCKPIT ACTIVATED A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 107ML 11450 AFTER TAKEOFF GRD/FLT FAULT STALL CMPTR FAULT LIFT DUMPER FAULT. PERFORMED OPERATIONAL CHECK OF PSEU IAW F-100 AMM 31-4 1-00 NO FAULTS NOTED. CYCLED GROUND FLIGHT RELAY BREAKER NO FAULTS NOTED AT THIS TIME. 2 L 7 2 4F RT 2001050900059 20010509 00059 EU 2001 5 9 JBXA000275 1 20010429 A 3230 VALVE FOKKER F28 F28MK0100 4990807 EU LT MLG OUT OF ADJ A JBXA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 05 105ML 11475 UPON GEAR RETRACTION LEFT GEAR REMAINED DOWN WOULD NOT RETRACT. REINSPECTED AIR/GROUND TEST VALVE FOUND VALVE JUST OFF OF DETENT. REPOSITIONED TEST VALVE IN THE FULL FLIGHT DETENT AND SAFETIED VALVE IAW AMM 32-00-00-710-813A. 2 L 7 2 4F RT 2001050900060 20010509 00060 EU 2001 5 9 JBXA000276 1 20010430 A 2740 WARNING LIGHT FOKKER F28 F28MK0100 4990807 EU COCKPIT ILLUMINATED A JBXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 05 106ML 11477 WHEN LEVELING AT 31,000 FT JAMMED STAB AMBER WARNING ON MFDU. PERFORMED AFCAS TEST IAW AMM 22-11-00, NO FAULTS FOUND. OPERATIONAL CHECK OF FLIGHT CONTROL SERVO VALVES STICKING CIRCUIT IAW AMM 27-00-00 AND OPERATIONAL TEST OF STABILIZER JA M SWITCH IAW AMM 27-43-00, NO FAULTS FOUND. CLEANED AND REINSTALLED JAM SWITCH CANNON PLUG, ALL OPS CHECKS GOOD. 2 L 7 2 4F RT 2001050900061 20010509 00061 NM 2001 5 9 SABA010011 1 20010427 A 3231 DOOR DHAV DHC8 DHC8102 2809003 NM LT MLG MALFUNCTIONED A SABA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 883CC 162 AIRCRAFT 883 ON FLIGHT 5018 FROM CLT TO OAJ. AFTER TAKEOFF THE LEFT FORWARD MAIN LANDING-GEAR DOOR FAILED TO CLOSE WHEN THE LANDING-GEAR WAS RETRACTED. THE LANDING GEAR WAS EXTENDED, AND ALL INDICATIONS WERE NORMAL. THE AIRCRAFT RETURNED TO CLT AND LANDED WITH NO OTHER PROBLEMS. NO INFLIGHT EMERGENCY WAS DECLARED AND NO EMERGENCY PROCEDURES WERE USED. M AINTENANCE PERFORMED AN LANDING GEAR RETRACTION TEST. ALL SYSTEMS CHECKED NORMAL. OPS CHECK WAS GOOD. AIRCRAFT RETURN ED TO SERVICE. 2 H 7 2 4T RT A13NM 2001050900062 20010509 00062 WP 2001 5 9 MWEA010668 1 20010501 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 FUSELAGE SKIN UNDER AFT CARGO DOOR EXTERIOR SKUFF PLATE IS CORRODED. REMOVED CORROSION, FABRICATED, LOCATED, DRILL AND INSTALLED REPAIR DOUBLERS AND FILLER. 2 L 7 2 4F A6WE 2001050900063 20010509 00063 WP 2001 5 9 MWEA010669 1 20010501 A 5330 5910280 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 AT STATION 980 RIGHT, THERE IS A SMALL CRACK EXTENDING FROM A FASTENER BETWEEN LONGERON 14 RIGHT AND 16 RIGHT. REMOVED DAMAGED AREA, FABRICATED FILLERS, DOUBLER AND FINGER DOUBLER, INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001050900064 20010509 00064 NM 2001 5 9 SCNA01028 1 20010307 A 4920 GTCP8598CK APU BOEING 727 7272M7 138407S NM FUSELAGE FIRE A SCNA F ACTIVATE FIRE EXT. J A WARNING INDICATION FLAME/FIRE UK UNKNOWN 1 GL 15 294SC 21202 APU FIRE INDICATION, DISCHARGED THE APU FIRE BOTTLE. REMOVED AND REPLACED APU AND APU FIRE BOTTLE. 2 L 7 3 4F A3WE 2001050900065 20010509 00065 NM 2001 5 9 SCNA01029 1 20010404 A 3350 BATTERY BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 284SC 21438 DURING A MAINTENANCE LINE INSPECTION THE FORWARD EMERGENCY TRACK LIGHTS WERE FOUND INOPERATIVE. REMOVED AND REPLACED BA TTERY AND ASSEMBLY. 2 L 7 3 4F RT A3WE 2001050900066 20010509 00066 NM 2001 5 9 SCNA01030 1 20010418 A 2710 65178234 CONTROL UNIT BOEING 727 727282 138408T NM AILERON FAILED A SCNA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 15 281SC 21949 DURING CLIMBOUT FROM LAS THE A-SYSTEM HYDRAULICS FAILED. REMOVED AND REPLACED THE AILERON HYDRAULIC SYSTEM MODULAR UNIT . 2 L 7 3 4F RT A3WE 2001050900067 20010509 00067 NM 2001 5 9 SCNA01031 1 20010427 A 3610 80550012 DUCT BOEING 727 727259 138408J NM NR 2 ENGINE LEAKING A SCNA F J A ACTIVATE FIRE EXT. DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 289SC 20765 DURING CLIMBOUT ENGINE NUMBER TWO HAD A FIRE INDICATION, FOLLOWED CHECKLIST, DUMPED FUEL AND RETURNED TO MSP. REMOVED A ND REPLACED THE THE LEFT FIRE BOTTLE, REMOVED AND REPLACED 13TH STAGE SADDLE DUCT LEAK CHECK GOOD ON SADDLE 13TH STAGE S ADDLE DUCT. 2 L 7 3 4F A3WE 2001050900068 20010509 00068 WP 2001 5 9 SCNA01032 1 20010428 A 3213 AXLE DOUG DC10 DC1015 3022118 WP MLG DAMAGED A SCNA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 15 153SY 48276 ON ARRIVAL TO THE GATE THE NUMBER EIGHT WHEEL AND BRAKE WERE FOUND TO BE SMOKING. THE WHEEL IS ALSO NOT SITTING ON THE AXLE STRAIGHT. REMOVED AND REPLACED AXLE, SLEEVE AND NUT, AS WELL AS THE ASSOCIATED WHEEL AND BRAKE. 2 L 7 3 4F A22WE 2001050900069 20010509 00069 WP 2001 5 9 SCNA01033 1 20010428 A 3610 DUCT DOUG DC10 DC1015 3022118 WP A/C BAY LEAKING A SCNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 153SY 48276 DURING CLIMBOUT FROM MSP THE NUMBER THREE PNEUMATIC FAIL LIGHT ILLUMINATED. FOUND DUCT AAM7235-501 LEAKING AFT OF AFT W ALL NUMBER THREE PACK BAY. PERFORMED REPAIR OF CHAFED DUCT, REPOSITIONED AND LEAK CHECKED. 2 L 7 3 4F A22WE 2001050900070 20010509 00070 NE 2001 5 9 A6WA200100028 2 20010427 A 7210 PW119CRGB GEARBOX PWA DORNER DO32 DO328100 2996000 NM PWA 119 PW119C NE LT ENGINE DEFECTIVE A A6WA E ENGINE SHUTDOWN O OTHER DE DESCENT 1 GL 31 330PH 9875 3235 PCE116037 3008 PCE116037 DESCENT OUT OF FL240, LT ENGINE SURGED FROM 0 PERCENT TO 30 PERCENT TORQUE AND LT PROP IMMEDIATELY WENT TO 103 PERCENT N P. FLEW FOR 4 MINUTES WITH ENGINE AT FLT IDLE AND NP AT 103 PERCENT. ENGINE SURGED 2ND TIME CAUSING ACFT TO YAW. ELEC TED TO SHUTDOWN ENGINE. MAX NP WAS 106 PERCENT. PROP WAS IN A PITCH LOCK SITUATION AND THEN FEATHERED NORMALLY. MAINT ENANCE REMOVED AND REPLACED LT ENGINE. 2 H 7 2 4T 4 T RT A45NM E20NE 2001050900071 20010509 00071 EU 2001 5 9 A6WA200100029 1 20010422 A 5520 ELEVATOR BAG BAE146 BAE146300A 1500267 EU TAIL CONTAMINATED A A6WA K NONE F FLT CONT AFFECTED CL CLIMB 1 GL 31 614AW E3132 PITCH OSCILLATION OCCURRED ON CLIMBOUT. MAINTENANCE DRAINTED WATER FROM ELEVATORS. 2 H 7 4 4F RT A49EU 2001050900072 20010509 00072 EU 2001 5 9 A6WA200100030 1 20010422 A 5520 ELEVATOR BAG BAE146 BAE146200A 1500266 EU TAIL CONTAMINATED A A6WA K NONE F FLT CONT AFFECTED CL CLIMB 1 GL 31 183US E2043 PITCH OSCILLATION OCCURRED ON CLIMBOUT. MAINTENANCE DRAINED WATER FROM ELEVATORS. 2 H 7 4 4F RT A49EU 2001050900073 20010509 00073 NM 2001 5 9 ABXA010210 1 20010501 A 3350 1000679 SIGN BOEING 767 767200 1385120 NM COCKPIT INOPERATIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 767AX 38064 22785 THE COCKPIT EMERGENCY EXIT LIGHT SIGN WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EXIT LIGHT SIGN. 2 L 7 2 4F RT A1NM 2001050900074 20010509 00074 WP 2001 5 9 ABXA010209 1 20010417 A 2782 VTA03440 ROD END DOUG DOUG DC9 DC941 302207N WP SLAT ACTUATOR BROKEN A ABXA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 GL 23 976AX 55492 47596 DURING A SERVICE CHECK, MAINTENANCE FOUND THE UPPER LEFT OUTBOARD SLAT ACTUATOR ROD END TO BE BROKEN. DAMAGE WAS ALSO N OTED UNDER THE LEFT INBOARD SLAT AND UPPER WING PANEL 1142A. MAINTENANCE REPLACED THE SLAT ACTUATOR ROD END ASSY IAW DC -9 MM 27-80-05. THE DAMAGE UNDER THE LEFT INBOARD SLAT WAS BLENDED OUT PER THE DC-9 SRM AND WING PANEL 1142A WAS REPLAC ED. 2 L 7 2 4F A6WE 2001050900075 20010509 00075 WP 2001 5 9 ABXA010208 1 20010426 A 3350 60030451 POWER SUPPLY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 953AX 9795 254 47608 THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE DURING THE CREW PREFLIGHT INSPECTION. MAINTENANCE REPLACED THE EMERGE NCY LIGHT POWER SUPPLY, IAW DC-9 MM 33-53-02. 2 L 7 2 4F A6WE 2001050900076 20010509 00076 WP 2001 5 9 ZW0A0100901 1 20010427 A 3246 WHEEL DOUG DC9 DC932 3022066 WP LT MLG FAILED A ZW0A O OTHER O OTHER LD LANDING 1 CE 13 995Z 47027 DURING LANDING THE LEFT LANDING GEAR INBD WHEEL RIM FAILED. SOME METAL SEPARATED AND THE TIRE ROLLED OFF THE RIM DAMAGI NG SOME AREAS OF THE GEAR INCLUDING THE GEAR WIRE HARNESS. CHECK-C 1-20-01 STL. 2 L 7 2 4F A6WE 2001050900077 20010509 00077 NM 2001 5 9 ZW0A0100902 1 20010426 A 3350 BATTERY PACK BOEING 767 7673Y0 NM CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 632TW 24953 THE EGRESS RED LIGHT COVER WAS MISSING AT THE RT SIDE NUMBER 2 CABIN DOOR AND AT ROW 43 LT SIDE, AND THE EGRESS LIGHTS W ERE INOPERATIVE AT THE AFT GALLEY. REPLACED THE RED LENS, P/N 81000-22703, AT BOTH LOCATIONS. AT THE AFT GALLEY REPLAC ED THE BATTERY PACK P/N 2013-1A, A LAMP P/N 6100928, AND DRIED AREA OF WATER. CHECK-C 3-22-01 LAX. 2 L 7 2 4F RT A1NM 2001050900078 20010509 00078 WP 2001 5 9 ZW0A0100903 1 20010428 A 3350 0105607301 LENS DOUG DC9 DC983 3022083 WP CABIN MISSING A ZW0A K NONE O OTHER NR NOT REPORTED 1 CE 13 9618A 53565 THE EGRESS LIGHT RED LENS WAS MISSING AT ROW 21. REPLACED THE RED LENS. CHECK-C 10-12-00 STL. 2 L 7 2 4F RT A6WE 2001050900079 20010509 00079 WP 2001 5 9 ZW0A0100904 1 20010428 A 3350 408822101 BATTERY DOUG DC9 DC983 3022083 WP CABIN NOT SEATED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 9307R 49663 THE EGRESS LIGHTING WAS INOPERATIVE IN THE FIRST CLASS CABIN. RESEATED THE POWER SUPPLY BATTERIES. CHECK-C 1-26-01 MCI . 2 L 7 2 4F RT A6WE 2001050900080 20010509 00080 NM 2001 5 9 ZW0A0100905 1 20010430 A 3350 8039251 POWER SUPPLY BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 413TW 55080 THE EGRESS LIGHTING WAS INOPERATIVE AT ROWS 15 THRU 19. REPLACED THE POWER SUPPLY. NO CHECK-C. 2 L 7 2 4F TR A6WE 2001050900081 20010509 00081 NM 2001 5 9 ZW0A0100906 1 20010430 A 5330 SKIN BOEING 767 7673Y0 NM FUSELAGE DENTED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 639TW 26208 DURING CHECK-C MAINT FOUND DENT IN FUSELAGE APPROX STA 1502 AND STRINGER 28L. DENT 6 IN LONG BY 4 IN WIDE AND 0.218 DE EP, BELOW THE L4 CABIN DOOR. INSTALLED A 15 IN BY 19 IN REAIR DOUBLER PER SRM 53-00-01. 2 L 7 2 4F RT A1NM 2001050900082 20010509 00082 NM 2001 5 9 ZW0A0100907 1 20010430 A 5313 STRINGER BOEING 767 7673Y0 NM FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 639TW 26208 DURING CHECK-C MAINT FOUND STRINGER 27L CRACKED AT STA 1502. INSTALLED AN 18 INCH DOUBLER REPAIR PER SRM 53-00-03. 2 L 7 2 4F RT A1NM 2001050900083 20010509 00083 NE 2001 5 9 SWIA972538 2 20010429 A 7321 FUEL CONTROL EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ENGINE MALFUNCTIONED A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 295SW 120322 RIGHT ENGINE HAD TORQUE FLUCTUATIONS ON TAKEOFF ROLL. OPERATED RT ENGINE AND LT ENGINE. TRIMMED RT ENGINE AS NECESSARY . NO FURTHER DEFECTS NOTED. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001050900085 20010509 00085 WP 2001 5 9 0101461157 1 20010418 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 157US 46766 DURING H-CHECK, FOUND CORROSION ON L43R AT BS 1783-1786. REPAIRED PER EA 11-182576. 2 L 7 3 4F A22WE 2001050900086 20010509 00086 NM 2001 5 9 SWAA011271 1 20010427 A 2560 P2070004 RETAINER BOEING 737 7373T0 1384582 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 684WN 23941 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY FLASHLIGHT HOLDER LOOSE, FWD INBD LIGHT. SECURED HOLDER PER MM. 2 L 7 2 4F RT A16WE 2001050900087 20010509 00087 NM 2001 5 9 SWAA011272 1 20010427 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 746SW 29798 DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVER CRACKED AT FWD CABIN. R&R TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001050900088 20010509 00088 2001 5 9 SWAA011273 4 20010428 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 089SW 22904 AFT SVC DOOR EMERGENCY EVAC SLIDE PRES IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001050900089 20010509 00089 NM 2001 5 9 SWAA011274 1 20010427 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 FUSELAGE SKIN CRACKED BS 380, STR 4L AND BS 460 STR 4L. MX FERRY TO PHX AND REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001050900090 20010509 00090 2001 5 9 SWAA011275 4 20010427 A 2565 D31591 SLIDE BOEING 737 7373G7 1384595 NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 FWD SVC DOOR EMERGENCY EVAC SLIDE PRES IND OUT OF LIMITS. R&R EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001050900091 20010509 00091 NM 2001 5 9 SWAA011276 1 20010428 A 3260 6555797 UPLOCK SENSOR BOEING 737 7373A4 1384585 NM RT MLG OUT OF ADJ A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 673AA 23251 AIR TURNBACK, RT GEAR UNSAFE LIGHT ILLUMINATED WITH GEAR HANDLE IN THE OFF POSITION. ADJUSTED RT GEAR UPLOCK SENSOR PER MM. 2 L 7 2 4F RT A16WE 2001050900092 20010509 00092 NM 2001 5 9 SWAA011277 1 20010427 A 2761 65C26864 ACTUATOR BOEING 737 7373H4 1384600 NM SPOILER CRACKED A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 359SW 26596 AIR DIVERSION, A HYDRAULIC SYSTEM FAILED DURING FLIGHT. R&R NR 1 GRD SPOILER ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2001050900210 20010509 00210 SW 2001 5 9 HEEA072712 1 20010419 A 6300 BUSHING BELL 206 206L3 1182108 SW DRIVE LINK WORN E K NONE O OTHER IN INSP/MAINT 1 SW 03 6251X TR062 51552 MAIN ROTOR DRIVE LINK HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2001050900233 20010509 00233 WP 2001 5 9 CALA0100428 1 20010427 A 5311 593639518 FRAME DOUG DC9 DC982 3022082 WP FS1000/RBL60 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 RIGHT WHEEL WELL APPROX STATION 1000 RBL 60 MLG AFT FRAME IS WORN AND CRACKED. REMOVED AND REPLACED DAMAGED FRAME PER S RM 51-30-2, 51-10-4, 51-10-2, AND 51-30-5. 2 L 7 2 4F A6WE 2001050900234 20010509 00234 EU 2001 5 9 SIMA20011085 1 20010418 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 548AT 548 JAN - FLT 3350 - CREW REPORTED EMERGENCY LIGHT BATTERY NOT ABLE TO TAKE CHARGE. EMERGENCY EXIT LIGHTS DO NOT WORK. MAI NTENANCE REMOVED AND REPLACED THE BATTERY PACK IN POWER SUPPLY UNIT 43WL. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001050900235 20010509 00235 EU 2001 5 9 SIMA20011081 1 20010418 A 3350 LIGHT AEROSP ATR72 ATR72212 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 410AT 410 MIA - FLT 5318 - CREW REPORTED THE FORWARD FLOOR PROXIMITY EMERGENCY LIGHT TO BE INOPERATIVE. PUT ON MEL AT THIS TIME. (M) 2 H 7 2 4T RT A53EU 2001050900236 20010509 00236 NE 2001 5 9 SIMA20011093 2 20010419 A 7200 ENGINE AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE LT ENGINE FAILED A SIMA E ENGINE SHUTDOWN Y B J ENGINE STOPPAGE SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION LD LANDING 1 SW 21 314AM 8330 314 120379 MIA - FLT 5356 - DURING LANDING, THE CREW REPORTED HEARING A BANG FROM THE NR 1 ENGINE, FOLLOWED BY MILD SMOKE IN THE CO CKPIT AND A LOW OIL PRESSURE LIGHT. CREW SHUT DOWN THE NR 1 ENGINE AND REQUESTED CFR. CFR MET THE AIRCRAFT AT THE END OF THE LANDING ROLL. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE IAW ATRMM. OPS AND LEAK CHECKS WERE GOOD AND AIRCRAF T WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 2001050900238 20010509 00238 EU 2001 5 9 SIMA20011101 1 20010420 A 2910 AE706458H HYDRAULIC LINE SAAB SF340 340B 7860101 EU NLG WW RUPTURED A SIMA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SW 21 349SB 340B349 LAX - FLT 3035 - CREW REPORTED A LOSS OF HYDRAULIC FLUID. AOM PROCEDURES WERE FOLLOWED, GEAR WAS BLOWN DOWN AND AIRCRAF T WAS LANDED SAFELY. MAINTENANCE FOUND A HYDRAULIC LINE IN THE NOSE WHEEL WELL RUPTURED. LINE WAS REPLACED, LEAK CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050900239 20010509 00239 SO 2001 5 9 SIMA0912 1 20010401 A 3240 0871HT3MOD3 SENSOR EMB 145 EMB145 SO RT MLG BRAKE FAILED A SIMA C ABORTED TAKEOFF M OVER TEMP TO TAKEOFF 1 SW 21 642AE OMA - FLT 4174 - NR 2 BRAKE TEMP INDICATION WENT HIGH ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE. INDICATION RET URNED TO NORMAL. ISSUED MEL 3202 AUTH 040027. REMOVED AND REPLACED NR 1 BRAKE TEMP SENSOR IAW AMM OPS CHECK GOOD. (M) 2 L 7 2 4F RT T00011AT 2001050900240 20010509 00240 2001 5 9 SIMA200109801 4 20010408 A 3160 7021170951 DISPLAY EMB 145 EMB145LR SO COCKPIT MALFUNCTIONED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 628AE 145124 CVG - FLT 4093 - AFTER AIRCRAFT WAS POWERED FOR SOMETIME, THE CREW STARTED SMELLING SOMETHING IN COCKPIT ONLY. INSPECTE D AREA AND COULD NOT FIND WHERE SMELL WAS COMING FROM. SENDING MTX FROM CMH. REMOVED AND REPLACED EICAS DISPLAY UNIT I AW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT T00011AT 2001050900241 20010509 00241 SO 2001 5 9 SIMA200110203 1 20010412 A 3150 WARNING SYSTEM EMB 145 EMB145LR SO COCKPIT MALFUNCTIONED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 603AE 145055 ORD - FLT 4027 - DURING TAKEOFF, CREW NOTED SPS 1 INOPERATIVE IND FOLLOWED BY AN AOA FAIL CAUTION. CREW ABORTED TAKEOFF . RETURNED TO GATE SAFELY AND IND DID DISAPPEAR AT THIS TIME. NO FURTHER INCIDENTS WERE REPORTED. PERFORMED STALL PRO TECTION SYSTEM, OPS CHECK IAW AMM. SYSTEM OK. (M) 2 L 7 2 4T RT T00011AT 2001050900242 20010509 00242 EU 2001 5 9 SIMA20011103 1 20010420 A 3234 DH9H12001 CONTROL HANDLE SAAB SF340 340B 7860101 EU COCKPIT FAULTY A SIMA O OTHER N FALSE WARNING AP APPROACH 1 SW 21 317AE 340B317 JFK - FLT 5133 - RIGHT MAIN DOWN AND LOCKED LIGHT DID NOT COME ON WHEN GEAR WAS SELECTED DOWN. CREW RAN NORMAL CHECKLIS T LIGHT DID NOT COME ON. PILOT PRESSED FIRMLY ON BULB ASSEMBLY AND GOT THE GREEN LIGHT. MAINTENANCE REMOVED AND REPLAC ED THE LANDING GEAR CONTROL HANDLE IAW SAAB MM 32-30-00. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050900243 20010509 00243 EU 2001 5 9 SIMA20011078 1 20010417 A 5311 7253813007 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 278AE 340B278 ABI - MAINTENANCE FOUND FRAME 658.5 TO HAVE WEB DAMAGE ON THE RIGHT ABOVE WL 73.5. LOWER PORTION FRAME WAS REMOVED AND REPLACED IAW SAAB SRM 72LK3079 AND CPM 72LKS5585. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050900244 20010509 00244 EU 2001 5 9 SIMA20011077 1 20010417 A 5311 7253720272 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 278AE 340B278 ABI - MAINTENANCE FOUND THE LOWER FACE OF FRAME 401, BL 0.0 WERE FOUND TO BE CORRODED BEYOND SRM LIMITS. MAINTENANCE RE PAIRED DAMAGE IAW SAAB STATEMENT 340SDS001437 AND CURRENT SAAB 340 SRM STANDARD PRACTICES. (M) 2 L 7 2 4T RT A52EU 2001050900245 20010509 00245 EU 2001 5 9 SIMA20011076 1 20010417 A 3020 6124100 DUCT SAAB SF340 340B 7860101 EU RT NACELLE FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 317AE 340B317 JFK - FLT 5137 - CREW REPORTED DURING CLIMB-OUT, RIGHT INTAKE LIGHT CAME ON. RETURNED TO JFK. MAINTENANCE REMOVED AND REPLACED THE RIGHT LOWER DUCT IAW SAAB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050900246 20010509 00246 EU 2001 5 9 SIMA20011062 1 20010416 A 2131 21179662 CONTROLLER SAAB SF340 340B 7860101 EU COCKPIT FAILED A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 214DA 340B214 DFW - FLT 3305 - CREW REPORTED PRESSURIZATION WAS ERRATIC IN BOTH AUTO AND MANUAL MODES. AIRCRAFT STAYED PRESSURIZED ON GROUND. PRESSURIZATION WAS PUT ON MEL AT THIS TIME. MAINTENANCE REMOVED AND REPLACED THE PRESSURE CONTROLLER IAW SAAB MM 21-31-10. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050900247 20010509 00247 EU 2001 5 9 SIMA20011033 1 20010413 A 6120 201108000011 CONTROL UNIT AEROSP ATR72 ATR72212A 8680902 EU NR 1 ENGINE INOPERATIVE A SIMA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 21 541AM 541 DFW - FLT 3535 - AFTER TAKEOFF FROM DFW AT ABOUT 4,000 FEET THE CREW SELECTED THE POWER MANAGEMENT SWITCH FROM TAKEOFF T O CLIMB, THR NR 1 ENGINE TORQUE WENT TO 70 PERCENT AND THE PROPELLER SPEED WENT TO 100 PERCENT. THE CREW RETURNED TO DF W AND LANDED WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED PROPELLER INTERFACE UNIT IAW ATR MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001050900248 20010509 00248 NE 2001 5 9 SIMA20011034 2 20010413 A 7321 6071T20P16 CONTROL UNIT SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE FAILED A SIMA O OTHER X ENGINE FLAMEOUT AP APPROACH 1 SW 21 330AE 340B330 LAX - FLT 3048 - CREW REPORTED THE NR 1 ENGINE FAILED IN FLIGHT DURING SHORT FINAL. MAINTENANCE REMOVED AND REPLACED TH E DIGITAL ELECTRONIC CONTROL UNIT FOR THE LEFT ENGINE IAW THE GEE MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO S ERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 2001050900249 20010509 00249 GL 2001 5 9 SIMA20011041 2 20010414 A 7200 ENGINE EMB 145 EMB145LR SO ALLSN AE300 AE3007A GL NR 1 ENGINE OVERTEMP A SIMA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 SW 21 720AE 145279 CHA - FLT 4418 - CREW REPORTED TO FIELD DUE TO NR 1 ENGINE TRYING TO OVERTEMP. AT CLIMB, NR 1 ENGINE WAS AT 800 DEGREES AND THE NR 2 AT 697 DEGREES. (M) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2001050900250 20010509 00250 EU 2001 5 9 SIMA20011042 1 20010414 A 7712 311649902 SENSOR AEROSP ATR72 ATR72212 EU NR 2 ENGINE FAILED A SIMA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 21 425MJ 425 MIA - FLT 5265 - CREW REPORTED A RIGHT ENGINE POWER LOSS AT 1200 FEET. POWER LOSS LASTED APPROX 3-5 SECONDS THEN GRADUA LLY RETURNED TO NORMAL. MAINTENANCE REMOVED AND REPLACED THE TWO TORQUE SENSOR (S/N''S CH771, CH395) ON THE RIGHT ENGIN E IAW PWC MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001050900251 20010509 00251 EU 2001 5 9 SIMA20011043 1 20010414 A 6120 6071T20P16 CONTROL UNIT SAAB SF340 340B 7860101 EU RT ENGINE INOPERATIVE A SIMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 21 398AE 340B398 DFW - FLT 3677 - CREW REPORTED TAKEOFF DUE TO NO TORQUE PROPELLER SPEED INDICATIONS FOR THE RIGHT ENGINE. MAINTENANCE R EMOVED AND REPLACED THE DIGITAL ELECTRONIC CONTROL UNIT FOR THE RIGHT ENGINE IAW SAAB MM. OPS CHECKS WERE GOOD AND AIRC RAFT WAS RETURNE TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050900252 20010509 00252 GL 2001 5 9 SIMA20011044 2 20010414 A 7313 23065950A NOZZLE EMB 145 EMB145LR SO ALLSN AE300 AE3007A GL LT ENGINE CLOGGED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 634AE 145150 CRP - FLT 3575 - CREW REPORTED A SMELL IN COCKPIT WITH ENGINE ANTI-ICE SELECTED ON. MAINTENANCE REMOVED AND REPLACED AL L FUEL NOZZLES ON THE LEFT ENGINE IAW RR MM. LEAK CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2001050900253 20010509 00253 NE 2001 5 9 SIMA20011051 2 20010415 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE OVERTEMP A SIMA O OTHER M OVER TEMP AP APPROACH 1 SW 21 231LN 340B231 GEE785602 DCA - FLT 5059 - DURING GO AROUND, RIGHT OVERTEMP LIGHT CAME ON FOR LESS THAN 1 SECOND. RETARDED POWER LEVER AND LIGHT WENT OUT OUTSIDE AIR TEMP 19 MODERATE RAIN. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE ASSEMBLY IAW AE WORK CARD 490 3. OPS AND LEAK CHECK WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 2001050900254 20010509 00254 NE 2001 5 9 SIMA20011072 3 20010417 A 6111 7725362 BEARING SAAB SF340 340B 7860101 EU HAMSTD 14RF 14RF19 NE LT PROP WORN A SIMA K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 SW 21 231LN 340B231 890551 DFW - CREW REPORTED A SEVERE VIBRATION FROM THE LEFT PROPELLER AT ALL POWER SETTINGS AND PROPELLER SPEEDS. MAINTENANCE FOUND THE NR 4 BLADE IN THE LEFT PROPELLER WITH AN EXTREMELY WORN BLADE PITCH CHANGE BEARING AND PIN. PROPELLER BLADE W AS REMOVED AND REPLACED. BALANCE WAS CHECKED AND FOUND TO BE WITHIN LIMITS. ALL WORK WAS DONE IAW HS MM. OPS AND LEAK CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 6 C P11NE 2001050900255 20010509 00255 EU 2001 5 9 SIMA20011056 1 20010415 A 7600 M835362024M RELAY SAAB SF340 340B 7860101 EU LT APR FAILED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 266AE 340B266 SAN - FLT 3210 - AFTER ARMING THE APR SYSTEM ON TAKEOFF ROLL, THE LEFT APR LIGHT DID NOT ILLUMINATE. PUT ON MEL AT THIS TIME. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. RELAY 43KA WAS REPLACED AS A PRECAUTION. OPS CHECK OF APR SYSTEM WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050900256 20010509 00256 EU 2001 5 9 SIMA200110102 1 20010411 A 7600 7239060053 PANEL SAAB SF340 340B 7860101 EU COCKPIT FAILED A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 397AE 340B397 DFW - FLT 3343 - DURING TAKEOFF ROLL, THE APR LIGHT DID NOT COME ON. ABORTED TAKEOFF. PERFORMED LOWER LAMPS TEST AND B OTH LIGHTS WORKED. REMOVED AND REPLACED CTOT PANEL IAW SAAB MM. OPS CHECK GOOD IAW WORK CARD NR 2813. (M) 2 L 7 2 4T RT A52EU 2001050900257 20010509 00257 EU 2001 5 9 SIMA200110101 1 20010411 A 7600 WARNING LIGHT SAAB SF340 340B 7860101 EU COCKPIT ILLUMINATED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 236AE 340B236 BGR - FLT 4913 - AIRCRAFT ABORTED TAKEOFF AT BEGINNING OF ROLL, DUE TO NO APR LIGHTS ILLUMINATING. PERFORMED GROUND RUN UP IAW AMM. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050900258 20010509 00258 EU 2001 5 9 SIMA20011071 1 20010413 A 5311 7253813485 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 278AE 340B278 DURING MAIN BASE VISIT, MAINTENANCE FOUND FRAME 677 TO BE DAMAGED ON THE RIGHT SIDE ABOVE WL 73.5. FRAME WAS REPLACED I AW SAAB SRM AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050900259 20010509 00259 EU 2001 5 9 SIMA20011031 1 20010413 A 3230 HP848430621 CONTROL VALVE SAAB SF340 340B 7860101 EU MLG FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 359SB 340B359 ISP - FLT 4622 - CREW REPORTED THE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. MAINTENANCE REMOVED AND REPLACED THE L ANDING GEAR CONTROL VALVE IAW SAAB MM 32-31-20. OPS AND LEAK CHECK WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001050900260 20010509 00260 SO 2001 5 9 SIMA20011057 1 20010415 A 2740 3621001007 CONTROL UNIT EMB 135 EMB135LR SO HORIZ STAB FAILED A SIMA A UNSCHED LANDING F FLT CONT AFFECTED TO TAKEOFF 1 SW 21 724AE 145301 ORD - FLT 4139 - CREW REPORTED PITCH TRIM ON CAPTAINS AND FIRST OFFICERS YOKE TO BE INOPERATIVE AFTER TAKEOFF. MAINTENA NCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNT IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001050900261 20010509 00261 2001 5 9 SWAA011325 4 20010503 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CASE. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001050900262 20010509 00262 2001 5 9 SWAA011326 4 20010502 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 623SW 27933 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRES IND OUT OF LIMITS. R&R EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001050900263 20010509 00263 2001 5 9 SWAA011327 4 20010502 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY & AFT SVC DOORS EMERGENCY EVAC SLIDES PRES IND OUT OF VIEW. REPOSITIONED EMER GENCY EVAC SLIDES PER MM. 2 L 7 2 4F A16WE 2001050900264 20010509 00264 NM 2001 5 9 SWAA011328 1 20010502 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 870, BELOW STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001050900265 20010509 00265 NM 2001 5 9 SWAA011329 1 20010502 A 5523 BACB28AK04 BUSHING BOEING 737 7377H4 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 730SW 27862 DURING SCHEDULED SERVICE CHECK , SWA SI 11038-55, FOUND BOTH LT & RT ELEVATOR, NR 3 & NR 4 TAB HINGE BUSHINGS WORN. R&R BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2001050900266 20010509 00266 NM 2001 5 9 SWAA011330 1 20010501 A 5753 6546435 FLAP BOEING 737 7373Y0 1384671 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 665WN 23497 DURING SCHEDULED C2 CHECK, FOUND RT WING OTBD AFT FLAP DELAMINATED AT INBD CORNER. R&R FLAP ASSY PER MM. 2 L 7 2 4F RT A16WE 2001050900267 20010509 00267 NM 2001 5 9 SWAA011331 1 20010501 A 5330 6545871 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 665WN 23497 DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR CUT OUT FUSELAGE SKIN CRACKED AT LWR AFT CORNER. REPAIRED FUSELAGE SKIN PE R SRM. 2 L 7 2 4F RT A16WE 2001050900268 20010509 00268 NM 2001 5 9 SWAA011332 1 20010501 A 5551 181A2001 ATTACH FITTING BOEING 737 7377H4 NM HORIZ STAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 710SW 27844 DURING SCHEDULED C4 CHECK, FOUND HORIZONTAL STABILIZER CENTER SECTION FWD SPAR LT LWR ATTACH LUG WORN. REPAIRED PER SWA RA. 2 L 7 2 4F RT A16WE 2001050900269 20010509 00269 2001 5 9 SWAA011333 4 20010504 A 2565 65C16820 RETAINER BOEING 737 7373H4 1384600 NM ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 643SW 27716 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM. 2 L 7 2 4F RT A16WE 2001050900270 20010509 00270 2001 5 9 SWAA011334 4 20010504 A 2565 65C16820 RETAINER BOEING 737 7373H4 1384600 NM SERVICE DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 643SW 27716 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM. 2 L 7 2 4F RT A16WE 2001050900271 20010509 00271 2001 5 9 SWAA011335 4 20010504 A 2565 65C16820 RETAINER BOEING 737 7373H4 1384600 NM SERVICE DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 630WN 27705 DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM. 2 L 7 2 4F RT A16WE 2001050900272 20010509 00272 2001 5 9 SWAA011336 4 20010505 A 2565 65C16820 RETAINER BOEING 737 7373Y0 1384671 NM ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 682SW 23496 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM. 2 L 7 2 4F RT A16WE 2001050900273 20010509 00273 NM 2001 5 9 SWAA011337 1 20010504 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 388SW 26591 DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EXIT LIGHT LENS CRACKED. R&R LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2001050900274 20010509 00274 NM 2001 5 9 SWAA011338 1 20010504 A 3350 6104781 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 067SW 22356 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. R&R LT OVERWING LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 2001050900275 20010509 00275 NM 2001 5 9 SWAA011339 1 20010505 A 3350 6104789 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED SERVICE CHECK, FOUND WING ROOT OVERWING EMERGENCY EXIT LIGHTS INOP. R&R BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2001050900276 20010509 00276 NM 2001 5 9 SWAA011340 1 20010505 A 3397 BR2013 WIRE BOEING 737 7372T4 1384492 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 EEPLS TRACK WIRES EXPOSED AT ROW 5. RESECURED EEPLS WIRES PER MM. 2 L 7 2 4F A16WE 2001050900277 20010509 00277 2001 5 9 SWAA011341 4 20010504 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRES IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001050900278 20010509 00278 2001 5 9 SWAA011342 4 20010504 A 2565 D31354 SLIDE BOEING 737 7377H4 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 756SA 27872 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CASE. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001050900279 20010509 00279 2001 5 9 SWAA011343 4 20010504 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CASE. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001050900280 20010509 00280 2001 5 9 SWAA011344 4 20010505 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. R&R EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001050900281 20010509 00281 NM 2001 5 9 SWAA011345 1 20010504 A 5330 6545774 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 727E+17, STR 21L. REPAIRED SKIN PER SWA RA. 2 L 7 2 4F RT A16WE 2001050900282 20010509 00282 NM 2001 5 9 SWAA011346 1 20010504 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 937, ABOVE STR 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001050900283 20010509 00283 NM 2001 5 9 SWAA011347 1 20010504 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D+10, BELOW STR 11L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001050900284 20010509 00284 NM 2001 5 9 SWAA011348 1 20010504 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING WALK AROUND INSPECTION, FOUND 4 INCH LONG FUSELAGE SKIN CRACK AT BS 528, BELOW STR 6R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001050900285 20010509 00285 NM 2001 5 9 SWAA011349 1 20010505 A 2731 DAS414A1 BEARING BOEING 737 7377H4 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 706SW 27840 DURING SCHEDULED PM CHECK ( SI-11079-27 ), FOUND RT ELEVATOR TAB, OTBD AFT ROD END BEARING WORN. R&R ROD END BEARING PER MM. 2 L 7 2 4F RT A16WE 2001050900286 20010509 00286 NM 2001 5 9 SWAA011350 1 20010504 A 5330 6545890 BEAR STRAP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D CHECK, FOUND BEAR STRAP CRACKED AT BS 304, LBL 70 AND WL 258. REPAIRED STRAP PER BFG ER. 2 L 7 2 4F A16WE 2001050900287 20010509 00287 NM 2001 5 9 SWAA011351 1 20010504 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 512SW 24189 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER 18R CRACKED AT BS 1076, REPAIRED STR PER SRM. 2 L 7 2 4F RT A16WE 2001051000009 20010510 00009 WP 2001 5 10 0101431146 1 20010126 A 5320 BEAM DOUG DC10 DC1040 3023508 WP FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 146US 46755 DURING M-CHECK, FOUND CORROSION ON LOWER END OF BEAM AT BS 1521 PRESSURE BULKHEAD. REPAIRED PER EA 11-182647. 2 L 7 3 4F A22WE 2001051000010 20010510 00010 NM 2001 5 10 0101446641 1 20010208 A 5330 SKIN BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 641NW 21941 DURING H-CHECK, FOUND CORROSION ON SKIN PANEL INSTALLATION AT BS 1480 TO 1740 S46L-S46R. REPAIRED PER EA 66-181955. 2 L 7 4 4F A20WE 2001051000011 20010510 00011 WP 2001 5 10 0101451157 1 20010323 A 5310 DOOR FRAME DOUG DC10 DC1040 3023508 WP FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 157US 46766 DURING H-CHECK, FOUND CORROSION ON FORWARD FRAME OF CENTER CARGO DOOR JAMB AT BS 1708 BETWEEN L42R AND L44R. REPAIRED P ER EA 11-183322. 2 L 7 3 4F A22WE 2001051000012 20010510 00012 NM 2001 5 10 CALA0100434 1 20010501 A 5240 6545949536 SKIN BOEING 737 7373Q8 1384670 NM R1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19382 26311 R1 DOOR SKIN LOWER HINGE CUTOUT CRACKED (1 INCH). REPAIRED R1 DOOR CUTOUT PER SRM 52-00-01 PG 203, 204. DOOR OPERATES NORMALLY. 2 L 7 2 4F RT A16WE 2001051000013 20010510 00013 WP 2001 5 10 CALA0100435 1 20010501 A 2752 5936709 FITTING DOUG DC9 DC982 3022082 WP FLAP ACTUATOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 LEFT WHEEL WELL INBOARD FLAP ACTUATOR ATTACHMENT FITTING IS CRACKED (1 X .25 INCH). REMOVED AND REPLACED FITTING PER SR M 51-30-5 AND 51-10-4. 2 L 7 2 4F A6WE 2001053100131 20010531 00131 CE 2001 5 31 GLBA2001086 1 20010429 A 2131 13037432 CONTROLLER BEECH 1900 1900D 1154162 CE CABIN PRESSURE INOPERATIVE A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 100UX 94 UE100 WOULD NOT PRESSURIZE ON CLIMBOUT. REPLACED PRESSURE CONTROLLER. 2 L 7 2 4T RT A24CE 2001051000014 20010510 00014 CE 2001 5 10 GLBA2001087 1 20010429 A 2120 UNKNOWN BEECH 1900 1900D 1154162 CE COCKPIT ODOR A GLBA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CE 01 226GL UE226 BURNING ODOR ON T/O AND DURING LANDING WITH GEAR SELECTED DOWN. INSPECTED FOUND PRP GOVERNOR GASKET LEAKING. REPLACED GASKET. 2 L 7 2 4T RT A24CE 2001051000015 20010510 00015 EU 2001 5 10 0101533208 1 20010428 A 2910 O-RING AIRBUS 320 A320211 3930320 EU HYD SYSTEM LEAKING A NWAA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 308US 107 DURING CRUISE, RECEIVED HYD Y RSVR LO LVL MESSAGE. PERFORMED COM PROCEDURES AND CONTINUED TO FINAL DESTINATION WITH A N ORMAL LANDING. MAINTENANCE REPLACED O-RING AT ENGINE NR 2 PYLON CHECK VALVE. LEAK CHECK OK. 2 L 7 2 4F RT A28NM 2001051000016 20010510 00016 GL 2001 5 10 0101551211 2 20010428 A 7260 GEARBOX DOUG DC10 DC1030 3023501 WP GE CF6 CF650C 30018 GL NR 3 ENGINE LEAKING A NWAA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 211NW 46868 528118 DURING CRUISE, THE NR 3 ENGINE OIL QUANTITY DECREASED TO ZERO AND OIL PRESSURE DROPPED INTO THE RED WITH THE LOW OIL PRE SSURE WARNING LIGHT ILLUMINATED. THE ENGINE WAS SHUT DOWN AND THE FLIGHT DIVERTED TO MNL. THE LANDING WAS WITHOUT INCI DENT. MAINTENANCE REPLACED THE NR 3 ENGINE ANGLE GEARBOX. ENGINE RUN AND OIL LEAK CHECK WAS OK. 2 L 7 3 4F 4 F A22WE A23EA 2001051000017 20010510 00017 WP 2001 5 10 0101579947 1 20010424 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8938 47161 DURING LINE CHECK, FOUND CATWALK EMERGENCY LIGHT INOPERATIVE IN TAIL COMPARTMENT. MAINTENANCE REPLACED THE BATTERY PACK . OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 2001051000018 20010510 00018 EU 2001 5 10 RAIA00105001 1 20010501 A 7714 31055863 TRANSDUCER JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE RT ENGINE FAILED A RAIA O OTHER J WARNING INDICATION TO TAKEOFF 1 CE 03 557HK 11574 11574 41074 75081 EWR-DURING TAKEOFF RIGHT HAND IEC FAULT LIGHT LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND ENGINE SPEED TRANSDUCER IAW ALLIED SIGNAL MAINTENANCE MANUAL 77-10-10. 2 L 7 2 4T 4 T RT A41NM E18NE 2001051000019 20010510 00019 WP 2001 5 10 MWEA010670 1 20010501 A 5230 3614118503 PAN DOUG DC9 DC982 3022082 WP CARGO DOOR GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 FORWARD CARGO DOOR HANDLE RECESS PAN IS GOUGED UNDER THE HANDLE. REMOVED CARGO DOOR HANDLE AND INSTALLED NEW CARGO DOOR HANDLE. 2 L 7 2 4F A6WE 2001051000020 20010510 00020 WP 2001 5 10 MWEA010671 1 20010501 A 5230 3926046501 FITTING DOUG DC9 DC981 3022081 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 AFT CARGO DOOR LOWER AFT INTERCOSTAL END FITTING IS CRACKED. DRILLED OUT LOWER AFT INTERCOSTAL AND CLIPS, DRILLED UP AN D INSTALLED NEW CLIPS. 2 L 7 2 4F A6WE 2001051000021 20010510 00021 WP 2001 5 10 MWEA010672 1 20010501 A 5230 591014167 PAN DOUG DC9 DC981 3022081 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 AFT CARGO DOOR OUTER PAN IS CRACKED IN THE RADIUS AT THE LOWER AFT STOP AREA. FABRICATED, DRILLED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001051000022 20010510 00022 WP 2001 5 10 MWEA010673 1 20010501 A 5230 995766444 INTERCOSTAL DOUG DC9 DC981 3022081 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 AFT CARGO DOOR LOWER AFT INTERCOSTAL IS CRACKED. REMOVED CRACKED INTERCOSTAL, DRILLED UP NEW AFT CARGO DOOR LOWER AFT I NTERCOSTAL, INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001051000023 20010510 00023 WP 2001 5 10 MWEA010674 1 20010501 A 5310 59127561 DOOR FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 E&E COMPARTMENT DOOR JAMB FORWARD EDGE HAS LIGHT/MODERATE CORROSION AROUND SEVERAL FASTENERS. BLENDED CORROSION, REMOVE D E&E DOOR JAMB, DRILLED NEW DOOR PAN, DRILLED DOOR STOP IN NEW PAN, INSTALLED NEW E&E COMPARTMENT DOOR JAMB AND DOOR ST OPS. 2 L 7 2 4F A6WE 2001051000024 20010510 00024 WP 2001 5 10 MWEA010675 1 20010501 A 5330 592081423 DOUBLER DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 FORWARD ENTRANCE STAIR DRAIN INTERNAL DOUBLER STATION 210 BETWEEN LONGERON 22 RIGHT & 23 RIGHT HAS EXFOLIATION CORROSION . LOCATED AND DRILLED AND INSTALLED FORWARD ENTRANCE STAIR DRAIN INTERNAL DOUBLER. 2 L 7 2 4F A6WE 2001051000025 20010510 00025 WP 2001 5 10 MWEA010676 1 20010501 A 3800 59220133 PANEL DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 FORWARD LAVATORY SERVICE PANEL HAS LIGHT CORROSION AND DEEP GOUGES AROUND DRAIN VALVE OPENING. BLENDED TOOL GOUGES, LOC ATED, DRILLED AND INSTALLED NEW PAN. 2 L 7 2 4F A6WE 2001051000026 20010510 00026 WP 2001 5 10 MWEA010677 1 20010501 A 5320 99578453 INTERCOSTAL DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 INTERCOSTAL IN E&E COMPARTMENT STATION 207-218 BETWEEN LONGERON 29 RIGHT AND 30 RIGHT HAS MODERATE CORROSION ON TOP, ALS O GOES UNDER PLASTIC CHAFE STRIP. REMOVED INTERCOSTAL, LOCATED AND INSTALLED NEW INTERCOSTAL. 2 L 7 2 4F A6WE 2001051000027 20010510 00027 WP 2001 5 10 MWEA010678 1 20010501 A 5311 99115173 FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 E&E COMPARTMENT FRAME STATION 180 HAS MODERATE CORROSION IN SEVERAL AREAS ON FORWARD AND AFT SIDE TO INCLUDE AREA UNDER PLASTIC CHAFE STRIP. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001051000028 20010510 00028 WP 2001 5 10 MWEA010679 1 20010501 A 5313 4912583501 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 LONGERON 30 IN FORWARD PIT HAS MODERATE CORROSION STATION 218-237. BLENDED CORROSION ON LONGERON, LOCATED AND DRILLED N EW SPLICE, FABRICATED EXTERNAL DOUBLER, INSTALLED DOUBLER AND SPLICE. 2 L 7 2 4F A6WE 2001051000029 20010510 00029 WP 2001 5 10 MWEA010680 1 20010501 A 5313 99579004 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 REWORK PREVIOUS REPAIR AT LONGERON 15 LEFT BETWEEN STATION 1230 AND 1220. REMOVED PREVIOUS REPAIR, DRILLED 4 HOLES, FAB RICATED 4 SPACERS AND REPAIR ANGLES, LOCATED AND DRILLED NEW INTERCOSTAL, INSTALLED REPAIR ANGLE, INTERCOSTAL AND FASTEN ERS. 2 L 7 2 4F A6WE 2001051000030 20010510 00030 WP 2001 5 10 MWEA010681 1 20010501 A 5320 49113832 FITTING DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 STATION 1174 FRAME FITTING AT THE FLOORLINE IS HEAVILY CORRODED. REMOVED FRAME FITTING, LOCATED, DRILLED AND INSTALLED NEW FRAME FITTING. 2 L 7 2 4F A6WE 2001051000031 20010510 00031 WP 2001 5 10 MWEA010682 1 20010501 A 5347 593054767 SEAT TRACK DOUG DC9 DC981 3022081 WP CABIN CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 NR SEAT RAIL HAS MODERATE CORROSION FROM STATION 200 TO 237. BLENDED CORROSION, CUT AND REMOVED SEAT TRACK NR 2 FROM 20 0-248, FABRICATED SEAT TRACK SPLICE, INSTALLED SEAT TRACK AND SPLICE REPAIR. 2 L 7 2 4F A6WE 2001051000032 20010510 00032 WP 2001 5 10 MWEA010684 1 20010501 A 5320 5912492IN PAN DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 MODERATE CORROSION UNDER RIV-NUT AND FORWARD SERVICE DOOR JAMB ANGLE, AREA LOCATED BY FORWARD LOWER CORNER OF DOOR JAMB, STATION 169. REMOVED CORROSION AND G1 DOOR PAN, DRILLED UP AND INSTALLED NEW DOOR PAN. 2 L 7 2 4F A6WE 2001051000033 20010510 00033 WP 2001 5 10 MWEA010685 1 20010501 A 5320 59360651 ANGLE DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 AFT CARGO PIT INTERNAL LOWER DOOR JAMB FRAME ANGLE AT STATION 1165 IS CORRODED. REMOVED INTERCOSTAL, BLENDED CORROSION, LOCATED, DRILLED AND INSTALLED BEAM ATTACH FITTING, REINSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001051000034 20010510 00034 WP 2001 5 10 MWEA010686 1 20010501 A 5313 592480215 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 LONGERON 17 LEFT HAS SEVERAL CRACKS UNDER FRAMES FROM STATION 237 TO 427. REMOVED, LOCATED, DRILLED AND INSTALLED NEW L ONGERON. 2 L 7 2 4F A6WE 2001051000035 20010510 00035 WP 2001 5 10 MWEA010687 1 20010501 A 5313 5936053501 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 CENTER CARGO COMPARTMENT HAS SEVERAL AREAS OF TOOLING MARKS AND CORROSION ON LONGERON 29 LEFT FROM STATION 636 TO 693. REMOVED CORROSION, BLENDED TOOL MARKS, REMOVED LONGERON. 2 L 7 2 4F A6WE 2001051000036 20010510 00036 WP 2001 5 10 MWEA010688 1 20010501 A 5313 59360531 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 CENTER CARGO COMPARTMENT LONGERON 30 FROM STATION 693 TO 788 HAS SEVERAL AREAS OF CORROSION AND TOOLING MARKS. REMOVED CORROSION, DRILLED AND INSTALLED NEW LONGERON. 2 L 7 2 4F A6WE 2001051000037 20010510 00037 WP 2001 5 10 MWEA010689 1 20010501 A 5313 5936053501 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 CENTER CARGO COMPARTMENT LONGERON 29 LEFT FROM STATION 693 TO 788 HAS SEVERAL AREAS OF TOOLING MARKS AND CORROSION. REM OVED CORROSION, REMOVED LONGERON, FABRICATED AND INSTALLED LONGERON. 2 L 7 2 4F A6WE 2001051000038 20010510 00038 WP 2001 5 10 MWEA010690 1 20010501 A 5310 99360737 SHEAR TIE DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 AFT CARGO COMPARTMENT FRAME 1155 HAS CORROSION ON IT AT LONGERON 29 RIGHT. FABRICATED FRAME BRACKET, REMOVED INTERCOSTA L, DRILLED AND INSTALLED NEW SHEAR TIE, INSTALLED BRACKET, AND REINSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001051000039 20010510 00039 WP 2001 5 10 MWEA010691 1 20010501 A 5310 593063850IN DOOR FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 AFT CARGO DOOR LOWER JAMB FRAME CORRODED. BLENDED CORROSION, REMOVED INTERCOSTAL, REMOVED LOCATED AND DRILLED DOOR JAMB BEAM, REINSTALLED INTERCOSTAL, FABRICATED AND INSTALLED ATTACH ANGLE. 2 L 7 2 4F A6WE 2001051000040 20010510 00040 WP 2001 5 10 MWEA010692 1 20010501 A 5320 9910078191 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 LIGHT CORROSION ON FLOOR SUPPORT FIVE INCHES RIGHT OF CENTER AND AT STATION 200. REMOVED CORROSION, REMOVED, FABRICATED NEW TRACK SECTION, FABRICATED REPAIR, INSTALLED REPAIR AND NEW TRACK SECTION. 2 L 7 2 4F A6WE 2001051000041 20010510 00041 EU 2001 5 10 AWXA0001655 1 20010501 A 5610 NP1653113 WINDSHIELD AIRBUS 320 A320231 3930325 EU COCKPIT CRACKED A AWXA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 28 629AW 19585 076 DEN - DIVERTED FLIGHT - 5/1/01 - FLT 58 - EN ROUTE FROM LAS TO JFK THE CAPTAIN''S NR 1 WINDSHIELD OUTER PANE CRACKED AND THE AIRCRAFT MADE AN UNSCHEDULED LANDING IN DEN. IN DEN MAINTENANCE REMOVED AND REPLACED THE CAPTAIN''S NR 1 WINDSHIEL D IAW AMM 56-11-11-400-001 AND PERFORMED AN OPERATIONAL CHECK OF THE WINDOW HEAT IAW AMM 30-42-00-710-001; THE OPERATION AL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2001051000042 20010510 00042 NM 2001 5 10 AWXA0001656 1 20010501 A 5313 42516C02761 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 MAIN CABIN FS 500C STR 16R AT WING ICE LIGHT, STR CRACKED. FABBED AND INSTALLED STR REPAIR IAW AMW ER 03-5314-01093-6F1 AND SRM 51-20-01 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001051000043 20010510 00043 NM 2001 5 10 AWXA0001657 1 20010501 A 5313 42516C02771 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 MAIN CABIN FS 500C STR 16L AT WING ICE LIGHT, STR CRACKED. FABBED AND INSTALLED STR REPAIR IAW AMW ER 03-5314-01093-6F1 AND SRM 51-20-01 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001051000044 20010510 00044 NM 2001 5 10 AWXA0001658 1 20010501 A 5313 42516C02781 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 MAIN CABIN FS 500D STR 16L AT WING ICE LIGHT, STR CRACKED. FABBED AND INSTALLED STR REPAIR IAW AMW ER 03-5314-01093-6F1 AND SRM 51-20-01 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001051000045 20010510 00045 NM 2001 5 10 AWXA0001659 1 20010501 A 5347 6546813 SEAT TRACK BOEING 737 7373G7 1384595 NM CABIN CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 SEAT TRACK FLANGE CORRODED FS 294 RBL 45 WL 207. REMOVED CORROSION OUT OF LIMITS IAW SRM 53-00-52; FABBED AND INSTALLED REPAIR DOUBLER STRAP IAW SRM 53-00-51 FIG 203. 2 L 7 2 4F RT A16WE 2001051000046 20010510 00046 NM 2001 5 10 AWXA0001660 1 20010501 A 5312 65163007 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 CENTER WEB CRACKED FS 178 WL 202 1.0 INCH LONG AT LBL 5.0. HFEC IAW B737 BTM 51-00-00 FIG 23 CRACKED. NOTED STOP DRILL 1/4 - NDT VERIFIED CRACK TERMINATED. HFEC VERIFIED CRACK TERMINATED; FABBED 2 EACH FILLER AND DOUBLER IAW SRM 53-10-08 AND INSTALLED PARTS IAW SRM 51-40-2 AND 53-10-08 FIG 210; TREATED AND PRIMED SRM 51-20-01. 2 L 7 2 4F RT A16WE 2001051000047 20010510 00047 NM 2001 5 10 AWXA0001661 1 20010501 A 5312 65163007 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 CENTER WEB CRACKED FS 178 WL 187 LBL 0.7 AND RBL 0.7 1.0 INCH LONG. NDT HFEC IAW B737 NTM PT 6 51-00-00 FIG 23. CRACK NOTED STOP DRILLED .25 INCH - VERIFIED NDT CHECKED - VERIFIED CRACK TERMINATED; FABBED 2 EACH FILLER AND DOUBLER IAW SRM 53-10-08; INSTALLED PARTS; TREATED AND PRIMED IAW SRM 53-10-08 AND 51-40-01 AND 51-20-01. 2 L 7 2 4F RT A16WE 2001051000048 20010510 00048 EU 2001 5 10 RAIA00105002 1 20010421 A 7712 30005000044 TORQUE SENSOR AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE NR 2 ENGINE FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 422TE 21309 2250 106 120660 7320-STL-DURING TAXI NR 2 ECU FAULT LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED NR 2 TORQUE SIGNAL CONDITIONER IAW ATR42 MAINTENANCE MANUAL. 2 H 7 2 4T 4 T RT A53EU E20NE 2001051000049 20010510 00049 EU 2001 5 10 RAIA00105003 1 20010424 A 3610 ASNA21414007 O-RING AEROSP ATR42 ATR42300 8680920 EU BLEED AIR BROKEN A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 422TE 106 7122-STL-DURING TAXI NR 2 BLEED HAD AN OVER TEMP AND LEAK WARNING. MAINTENANCE REMOVED AND REPLACED THE O-RING AT THE W ING TO FUSALAGE DUCT CONNECTION IAW ATR42 MAINTENANCE MANUAL. 2 H 7 2 4T RT A53EU 2001051000050 20010510 00050 NM 2001 5 10 AWXA0001662 1 20010501 A 5315 6545812 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 AT LBL 2 FS 328 HAS CORROSION AT FASTENER HOLE AFT FLANGE. REMOVED CORROSION IAW SRM 53-00-51 FIG 203. FOUND OUT OF LI MITS. FABBED AND INSTALLED REPAIR STRAP IAW SRM 53-00-51 FIG 203. 2 L 7 2 4F RT A16WE 2001051000051 20010510 00051 EU 2001 5 10 C2XA01BT080 1 20010502 A 3350 LP1670 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14828 179 BTV---CO3014, DURING LINE AND WEEKLY CHECK IN BTV MAINTENANCE FOUND THE EMERGENCY AISLE PATH LIGHTING AT SEAT 7AB IS INO PERATIVE. REMOVED AND REPLACED BULB IN EMERGENCY LIGHT ASSY AT 7AB IAW ATR42 CMM 33-52-10. OPS CHECKED GOOD. 2 H 7 2 4T RT A53EU 2001051000052 20010510 00052 NM 2001 5 10 AWXA0001663 1 20010501 A 5311 65163004301 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 FWD PRESSURE BLKHD BS 178 AFT SIDE LT SIDE CRACKED AT SIDE CHORD WL 207 1 INCH LONG. REMOVED DAMAGED AREA ON SIDE CHANN EL IAW ER 03-5312-01099-DL1; REPAIRED SIDE CHORD IAW ER 03-5312-01099-DL1. 2 L 7 2 4F RT A16WE 2001051000053 20010510 00053 NM 2001 5 10 AWXA0001664 1 20010501 A 5312 65163007 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 CENTER WEB CRACKED FS 178 WL 202 1.1 INCH LONG AND WL 198 1.0 INCH LONG AT RBL 5.0. CUT OUT DAMAGE AND INSTALLED DOUBLE R AND FILLER REPAIR IAW SRM 53-10-08 FIG 203; HFEC INDICATES NO CRACKS FOUND. 2 L 7 2 4F RT A16WE 2001051000054 20010510 00054 NM 2001 5 10 AWXA0001665 1 20010501 A 5510 DHM42516T00338 BUSHING BOEING 737 7373G7 1384595 NM HORIZ STAB WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 PLATING WORN ON LT HORIZ STAB UPPER AFT ATTACH BUSHING (ON STAB) BS 1145. REMOVED BUSHING IAW CMM 55-10-06; CLEANED LUG AND SLEEVE; FOUND NO DAMAGE OR CORROSION. TREATED AND PRIMED AREA IAW SRM 51-20-01; NDT NOTED NO CRACKS. INSTALLED FA BBED BUSHING, SEALED BUSHING AND HONED BUSHING ID TO 1.3787 INCH IAW CMM 55-10-06. 2 L 7 2 4F RT A16WE 2001051000055 20010510 00055 NM 2001 5 10 AWXA0001666 1 20010501 A 5320 65596642 SPLICE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 FS 360 AT STR SPLICE 4R HAS 2 CRACKS .25 INCH. REMOVED AND REPLACED STR SPLICE. 2 L 7 2 4F RT A16WE 2001051000056 20010510 00056 NM 2001 5 10 AWXA0001667 1 20010501 A 5320 66244912 ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 INTERCOSTAL ATTACH ANGLE AT AFT/UPPER SIDE OF R1 DOOR FRAME (WL 268 BS 347) IS CRACKED (1.5 INCH LONG). REMOVED AND REP LACED INTERCOSTAL TEE ANGLE IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001051000057 20010510 00057 WP 2001 5 10 ABXA010211 1 20010405 A 5250 5956574177 TRACK DOUG DC9 DC933F 302207A WP COCKPIT DOOR LOOSE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 52322 47384 THE COCKPIT DOOR WAS HARD TO CLOSE AND THE LATCH JAMS IN THE CLOSED POSITION. MAINTENANCE INSPECTED AND FOUND THE UPPER DOOR TRACK LOOSE. THE DOOR TRACK WAS TIGHTENED AS REQUIRED IAW DC-9 MM. 2 L 7 2 4F A6WE 2001051000058 20010510 00058 NE 2001 5 10 ABXA010212 2 20010430 A 7200 ENGINE DOUG DC9 DC941 302207N WP PWA JT8 JT8D15 52051 NE NR 2 ENGINE FAILED A ABXA O OTHER Y ENGINE STOPPAGE LD LANDING 1 GL 23 967AX 47509 686248 THE RIGHT ENGINE (NR 2) EXPERIENCED AN UNCOMMANDED SHUT DOWN DURING THE LANDING FLARE. MAINTENANCE COMPLETED VISUAL INS PECTIONS OF THE INTAKE AND EXHAUST. NO DEFECTS WERE NOTED. THE RIGHT ENGINE FUEL FILTER WAS REPLACED AS A PRECAUTION. NO DEFECTS WERE NOTED WITH THE REMOVED FILTER. THE MOISTURE TRAP WAS INSPECTED AND DRAINED, AND THE PS4 LINE WAS INSPE CTED. NO DEFECTS WERE NOTED. MAINTENANCE SUMPED THE FUEL TANKS AND COMPLETED PROCEDURES FOR ENGINE FLAME-OUT PER PRATT AND WHITNEY JT8D MM. GROUND ENGINE RUNS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F A6WE E2EA 2001051000059 20010510 00059 NM 2001 5 10 AWXA0001668 1 20010501 A 5553 65538341 FITTING BOEING 737 7373G7 1384595 NM VERTICAL STAB CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 VERT STABILIZER LT AFT O/B ATTACH FITTING LUG HAS CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-40-02 AND 51-10-02 . 2 L 7 2 4F RT A16WE 2001051000060 20010510 00060 NM 2001 5 10 AWXA0001669 1 20010501 A 5510 DHM42516T003211 BUSHING BOEING 737 7373G7 1384595 NM HORIZ STAB WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 PLATING WORN ON LT HORIZ STAB CENTER AFT ATTACH BUSHINGS (ON STAB) BS 1145. REMOVED BUSHINGS IAW CMM 55-10-06. CLEANED SLEEVES - FOUND NO CORROSION OR DAMAGE; TREATED AND PRIMED IAW SRM 51-20-01; NDT VERIFIED NO CRACKS. INSTALLED FABBED BUSHINGS, SEALED AND HONED ID TO 1.3785 INCH IAW CMM 55-10-06. 2 L 7 2 4F RT A16WE 2001051000061 20010510 00061 NM 2001 5 10 AWXA0001670 1 20010501 A 5510 DHM42516T00345 BUSHING BOEING 737 7373G7 1384595 NM HORIZ STAB WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 PLATING WORN ON LT HORIZ STAB FWD LOWER ATTACH BUSHINGS (ON STAB) BS 1100. REMOVED BUSHINGS IAW CMM 55-10-06; CLEANED L UG AND SLEEVE, FOUND NO CORROSION OR DAMAGE. TREATED AND PRIMED IAW SRM 51-20-01; NDT VERIFIED NO CRACKS. INSTALLED FA BBED BUSHINGS, SEALED AND HONED ID TO .8784 INCH IAW CMM 55-10-06. 2 L 7 2 4F RT A16WE 2001051000062 20010510 00062 WP 2001 5 10 UPS01835773 1 20010331 A 5310 3755822505N FITTING DOUG DC8 DC871F 302199D WP LOWER CARGO CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C2,3 STA 320 BATHTUB FITTING IS CRACKED BETWEEN LONG. 29L-30L REMOVED AND REPLACED FITTING I.A.W. DW G. 3755822,AND SRM.51-1-20D 2 L 7 4 4F RT 4A25 2001051000063 20010510 00063 NM 2001 5 10 AWXA0001671 1 20010501 A 5510 DHM42516T00262 BUSHING BOEING 737 7373G7 1384595 NM HORIZ STAB WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 PLATING WORN ON LT HORIZ STAB FWD UPPER ATTACH BUSHINGS (ON STAB) BS 1100. REMOVED BUSHINGS IAW CMM 55-10-06. CLEANED LUG AND SLEEVE, FOUND NO CORROSION OR DAMAGE. TREATED AND PRIMED IAW SRM 51-20-01; NDT VERIFIED NO CRACKS. INSTALLED F ABBED BUSHINGS, SEALED AND HONED ID TO 1.0037 INCH IAW CMM 55-10-06. 2 L 7 2 4F RT A16WE 2001051000064 20010510 00064 EU 2001 5 10 MALA010427 1 20010429 A 3020 NH24668169 DUCT SAAB SF340 340B 7860101 EU RT INTAKE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 420XJ 420 DURING FLIGHT 3385 FROM MSP, RT INTAKE CAUTION LIGHT ILLUMINATED EN ROUTE TO BISMARCK AT 16,000 FT, CYCLED ON 15 SECOND INTERVALS. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED LOWER INLET DUCT P/N NH24668-169, S/N ON L155349, S/N O FF L291266 IAW 71-60-05-4. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2001051000065 20010510 00065 NM 2001 5 10 AWXA0001672 1 20010501 A 5510 DHM42516T003114 BUSHING BOEING 737 7373G7 1384595 NM HORIZ STAB WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 PLATING WORN ON LT HORIZ STAB LOWER AFT ATTACH BUSHINGS (ON STAB) BS 1145. REMOVED BUSHINGS IAW CMM 55-10-06. CLEANED LUG AND SLEEVE, FOUND NO CORROSION OR DAMAGE. TREATED AND PRIMED IAW SRM 51-20-01; NDT VERIFIED NO CRACKS. INSTALLED F ABBED BUSHINGS, SEALED AND HONED ID TO 1.5037 INCH IAW CMM 55-10-06. 2 L 7 2 4F RT A16WE 2001051000066 20010510 00066 NM 2001 5 10 AWXA0001673 1 20010501 A 5347 DHM42516003504 SEAT TRACK BOEING 737 7373G7 1384595 NM CABIN CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 CABIN SEAT TRACK UNDER FWD GALLEY AREA HAS PITTED CORROSION BS 328 - 360 AND RBL 55. REMOVED FLOORBOARD; REMOVED, FABBE D AND INSTALLED CABIN SEAT TRACK IAW SRM 51-40-02 AND 53-00-52. REINSTALLED FLOORBOARD IAW CARD E1025007 AND SRM 53-30- 52 AND 53-00-52. 2 L 7 2 4F RT A16WE 2001051000069 20010510 00069 NM 2001 5 10 AWXA0001674 1 20010501 A 5320 65458851 TIE CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 E & E COMPT STA 328 LONGERON 21L FRAME TIE CLIP CRACKED. REMOVED TIE CLIP IAW SRM 51-40-02; FABBED TIE CLIP IAW ENG SUP PORT; TREATED AND PRIMED TIE CLIP IAW SRM 51-20-01; INSTALLED TIE CLIP IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001051000070 20010510 00070 NM 2001 5 10 AWXA0001675 1 20010501 A 5320 6925966 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 INTERCOSTAL CRACKED LBL 46 AT FLOORBEAM UPPER FLANGE FS 328. REMOVED INTERCOSTAL; CUT OUT DAMAGE IAW SRM 51-70-11; FABB ED ANGLE REPAIR IAW SRM 51-70-11; INSTALLED INTERCOSTAL IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001051000074 20010510 00074 NM 2001 5 10 AWXA0001676 1 20010501 A 5512 657378337 SKIN BOEING 737 737301 1384611 NM FUSELAGE DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 23258 SEVERAL DENTS IN LT HORIZ STAB STA 95.66 - 104.66. INSTALLED REPAIR IAW ER 03-5515-01117-TB1. 2 L 7 2 4F RT A16WE 2001051000075 20010510 00075 NM 2001 5 10 AWXA0001677 1 20010501 A 5320 6546812187 FLOOR SUPPORT BOEING 737 737301 1384611 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 23258 STA 1015 LBL 8 FLOOR SUPPORT UPPER CAP CORRODED. REMOVED AND INSTALLED FLOOR SUPPORT IAW B737 SRM 51-40-02 PG 16-17. 2 L 7 2 4F RT A16WE 2001051000076 20010510 00076 NM 2001 5 10 AWXA0001678 1 20010501 A 5410 0640027 BUSHING BOEING 737 737301 1384611 NM NR 2 PYLON OUT OF POSITION A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 23258 NR 2 ENGINE PYLON O/B MID SPAR BUSHING HAS MIGRATED .095 INCHES. REPLACED BUSHINGS IAW SB 54-1037 PARAGRAPH 1D, AWA ER 03-5410-0111D-JS1. P/N: 311A1151-12, 311A1151-13. 2 L 7 2 4F RT A16WE 2001051000077 20010510 00077 EA 2001 5 10 COMA0160364 1 20010426 A 5320 6013600130 ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 929CA 17304 7035 THE FRAME AT FS 640 HAS A CRACKED ANGLE ON THE RIGHT SIDE AT THE ENGINE SUPPORT AREA. REMOVED CRACKED ANGLE P/N 601-360 01-30 AND INSTALLED A NEW ANGLE P/N 601-36001-30 IAW WVAC EO 601R-53-2390. 2 L 7 2 4F RT A21EA 2001051000078 20010510 00078 NM 2001 5 10 AWXA0001679 1 20010501 A 5315 6545808285 FLOORBEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 169AW 23630 CORROSION ON AFT CORNER OF TRACK SECTION AND UPPER FLANGE OF FLOORBEAM AT BS 294 RBL 12-14; CORROSION REMOVAL OUT OF LIM ITS. REMOVED FLOORBEAM T-CAP SECTION; LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED NEW T-CAP UPPER CORD IAW B737 SRM 51-40-05 PG 7 AND 51-20-05 PG 1 AND 53-10-51 PG 221-223. 2 L 7 2 4F RT A16WE 2001051000079 20010510 00079 NE 2001 5 10 NACA2001018 2 20010430 A 7250 618703 DISK PWA 7B BOEING 727 72723 1384004 NM PWA JT8 JT8D NE ENGINE VIBRATION A NACA E A ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 AL 03 930FT 19299 2917 948945 19387 948945 MI AT ANC AT 2102Z, ENGINE SHUTDOWN DUE TO SEVERE VIBRATION. REMOVED AND REPLACED NR 1 ENGINE. 2 L 7 3 4F 4 F A3WE E2EA 2001051000080 20010510 00080 NM 2001 5 10 AWXA0001681 1 20010501 A 5330 6545298813 SKIN BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 169AW 23630 BLIND RIVET REPAIR FORWARD OF AFT PRESSURE BLKHD BS 1012 STR 23L WL 182. REMOVED DOUBLER REPAIR WITH BLIND FASTENERS; F ORMED AND INSTALLED REPAIR DOUBLER IAW B737 SRM 51-20-01, 53-00-01 FIG 202 PG 204. 2 L 7 2 4F RT A16WE 2001051000081 20010510 00081 NM 2001 5 10 AWXA0001682 1 20010501 A 5311 6516300301 FRAME BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 169AW 23630 FS 178 BLKHD CRACK AT WL 187-230 CENTER OF RADIUS. REMOVED, LOCATED, DRILLED AND INSTALLED NEW SIDE CHORD IAW B737-300 SRM 51-10-02 PG 15 & 51-40-02 PG 1, 10. 2 L 7 2 4F RT A16WE 2001051000082 20010510 00082 NM 2001 5 10 AWXA0001683 1 20010501 A 5312 6516300301 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 169AW 23630 FS 178 BLKHD CRACKED AT WL 234.1 RBL 7.8-9.7. CUT OUT DAMAGED AREA, LOCATED, DRILLED, AND INSTALLED REPAIR DOUBLER IAW B737-300 SRM 53-10-08 PG 265-269. 2 L 7 2 4F RT A16WE 2001051000083 20010510 00083 NM 2001 5 10 AWXA0001684 1 20010501 A 5312 65163007 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 169AW 23630 FS 178 BLKHD CRACK AT WL 202.5 RBL 4.8. CUT OUT DAMAGED AREA, LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW B737-30 0 SRM 53-10-08 TR 53-15 PG 1-11. 2 L 7 2 4F RT A16WE 2001051000084 20010510 00084 NM 2001 5 10 AWXA0001685 1 20010501 A 5230 65C36232 SKIN BOEING 737 73733A 1384673 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 169AW 23630 AFT CARGO COMPT UPPER LINER SKIN CRACKED AT CENTER LIGHTENING HOLE. LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW B 737-300 SRM 51-40-02 PG 3. 2 L 7 2 4F RT A16WE 2001051000085 20010510 00085 NM 2001 5 10 AWXA0001686 1 20010501 A 5312 65163007 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 169AW 23630 FS 178 BLKHD CRACKED 2 PLACES LBL 4 & 1.2, RBL 8 WL 187-188. CUT OUT DAMAGED AREA, LOCATED, DRILLED AND INSTALLED REPAI R DOUBLER IAW B737-300 SRM 53-10-08 TR 53-15 PG 1-11. 2 L 7 2 4F RT A16WE 2001051000086 20010510 00086 NM 2001 5 10 AWXA0001688 1 20010501 A 5320 6545833U40 WEB BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 169AW 23630 FS 178 COCKPIT FLOOR WEB CRACKED AT RBL 23 WL 207. REMOVED DAMAGED AREA, LOCATED, DRILLED AND INSTALLED NEW WEB SECTION IAW B737-300 SRM 51-40-02 PG 1-6 & 51-10-02 PG 15. 2 L 7 2 4F RT A16WE 2001051000087 20010510 00087 NM 2001 5 10 AWXA0001689 1 20010501 A 5320 65C313927 STIFFENER BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 169AW 23630 FS 294 TEE CAP STIFFENER CORRODED RBL 28-43. REMOVED DAMAGED AREA, LOCATED, DRILLED AND INSTALLED NEW TEE CAP STIFFENER IAW B737-300 SRM 51-40-02 PG 1-10. 2 L 7 2 4F RT A16WE 2001051000088 20010510 00088 NM 2001 5 10 AWXA0001690 1 20010501 A 5230 65C25180 STRUCTURE BOEING 737 73733A 1384673 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 169AW 23630 FS 837 AFT CARGO DOOR, CRACK AT LWR CROSS BEAM, LOWER TEE, VERT LEG, 3RD HI-LOK FROM END BEAM. REMOVED DAMAGED AREA, LO CATED, DRILLED AND INSTALLED REPAIR FILLERS, DOUBLERS AND STRAPS IAW AWA EO 52-33-01 REV D PG 1-15. 2 L 7 2 4F RT A16WE 2001051000089 20010510 00089 NM 2001 5 10 AWXA0001692 1 20010501 A 5312 65163007 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 169AW 23630 BS 178 BLKHD WEB RBL 5 WL 200 HAS A .60 INCH CRACK EMANATING FROM BENEATH THE STRAP. CUT OUT DAMAGED WEB AREA; LOCATED, DRILLED, INSTALLED REPAIR DOUBLER AND FILLER IAW B737 SRM 53-10-08 TR 53-15 PG 1-11. 2 L 7 2 4F RT A16WE 2001051000090 20010510 00090 WP 2001 5 10 ZW0A0101001 1 20010427 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT FOUND NUMBER 1 CABIN SEAT TRACK WITH CORROSION, STA 1104 TO 1136. REPLACED SEAT TRACK PER SRM 53-0 5, FIG 4F. 2 L 7 2 4F A6WE 2001051000091 20010510 00091 WP 2001 5 10 ZW0A0101002 1 20010427 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT IN THE AFT CARGO COMPT, INTERCOSTAL AT STA 1237, BETWEEN LONGERON 24L AND 25L, HAD CORROSION. REMO VED CORROSION PER SPM 6-80-01. REINSTALLED INTERCOSTAL PER SRM 51-30-05 AND 51-30-02. 2 L 7 2 4F A6WE 2001051000092 20010510 00092 WP 2001 5 10 ZW0A0101003 1 20010430 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT IN FWD CABIN FOUND NUMBER 2 FLOOR TRACK AT STA 207 HAD CORROSION. CUT NUMBER 2 TRACK AT STA 247. REPLACED WITH NEW FROM STA 200 TO 247. SPLICED PER SRM 53-05-4F. 2 L 7 2 4F A6WE 2001051000093 20010510 00093 WP 2001 5 10 ZW0A0101004 1 20010430 A 5522 FAIRING DOUG DC9 DC982 3022082 WP ELEVATOR DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT ON RT ELEVATOR FOUND HOLE IN LINKAGE FAIRING ON LOWER SIDE, JUST FWD OF FWD HALF PANEL NUMBER 3616. REPAIRED AREA PER SRM 51-70-3 AND ARA 17747. BALANCE CALCULATION PER SRM 55-20-2 AND FOUND WITHIN LIMITS. 2 L 7 2 4F A6WE 2001051000094 20010510 00094 WP 2001 5 10 ZW0A0101005 1 20010426 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT BL 45R AND BETWEEN STA 160 THRU 200. FABRICATED NEW FLOOR SUPP ORT PER DRAWING 9936534 AND SPM 6-70-01 PAGE 2 ITEM 4A (1) AND PAGE 3 (2). CORROSION TREATED PART PER SRM 51-10-3. INS TALLED FLOOR SUPPORT PER SPM 6-70-01 PAGE 3B FROM STA 160 TO 200, BL 45R AND DRAWING 936534. 2 L 7 2 4F A6WE 2001051000095 20010510 00095 WP 2001 5 10 ZW0A0101007 1 20010426 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT FOUND CORROSION ON MEMBRANE AT STA 151 AND RBL 45R. CUT OUT DAMAGED SECTION OF MEMBRANE FROM STA 1 48 AND 160 RBL 40 IN TO RBL 59 IN. REPAIRED PER SRM 53-14-1 FIG 11 AND DRAWING 5930536. 2 L 7 2 4F A6WE 2001051000096 20010510 00096 WP 2001 5 10 ZW0A0101008 1 20010426 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT FOUND CORROSION ON MEMBRANE AT BL 52R THRU 58R, STA 168 THRU 200. CUT OUT DAMAGED SECTION OF MEMBR ANE FROM STA 168 TO 200 AND REPAIRED PER SRM 51-70-4 AND DRAWING 5930536. 2 L 7 2 4F A6WE 2001051000097 20010510 00097 WP 2001 5 10 ZW0A0101009 1 20010426 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT FOUND MEMBRANE AT STA 240, RBL 46 IN, WAS CRACKED. NEW MEMBRANE FABRICATED IN SHOP PER INTER SHOP WORK TICKET 837502 AND DRAWING 9930538. INSTALLED MEMBRANE PER SPM 6-70-01 PAGE 3 ITEM 4B, AND DRAWING 9930538. CORROS ION TREATED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001051000098 20010510 00098 WP 2001 5 10 ZW0A0101010 1 20010426 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT FOUND CORROSION ON MEMBRANE AFT OF STA 200, BL 46R THRU BL 57R. INSTALLED NEW MEMBRANE FROM STA 20 0 TO 220, RBL 46 TO RBL 59, PER DRAWING 9930538 AND SRM 51-70-4 FIG 1. 2 L 7 2 4F A6WE 2001051000099 20010510 00099 2001 5 10 SWIA972540 4 20010501 A 3418 STALL WARNING CNDAIR CL600 CL6002B19 EA COCKPIT FALSE ACTIVATION A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 408SW 7055 STALL FAIL CAUTION MESSAGE ON EICAS DURING CLIMBOUT. FOLLOWED QRH PROCEDURES. RETURNED TO SLC. RESET CIRCUIT BREAKERS CBP1, Q2 AND CBP4, C7. STALL FAIL MESSAGE WENT AWAY. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2001051000100 20010510 00100 SO 2001 5 10 SWIA972541 1 20010429 A 3060 BRUSH BLOCK EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT PROP FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 569SW 120344 RIGHT PROP INOP LIGHT ILLUMINATED ON TIMER 1 & 2. RETURNED TO FIELD. REPLACED RT ENGINE BRUSH BLOCK. OPS CHECK GOOD 3 0-60-00, 71-00-00. UPDATE BOI: REMOVED AND REPLACED RIGHT ENGINE OIL DEICE PRESSURE SWITCH IAW EMB120 MM 79-00-00. O PS CHECK IAW EMB120 MM 30-60-00. P/N: 1153P0013-01, S/N ON: 1061, S/N OFF: 0504. 2 L 7 2 4T 4 T RT A31SO E20NE 2001051000101 20010510 00101 NE 2001 5 10 SWIA972542 2 20010501 A 7321 PROBE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ENGINE FAILED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 204SW 120243 RIGHT EEC FAILED ON TAKEOFF ROLL. CLEANED CANNON PLUGS. REMOVED AND REPLACED NH PROBE IAW EMB MM 77-12-00. OPS CHECK GOOD. P/N: 3039242, S/N ON: CH12555, S/N OFF: CH17516. 2 L 7 2 4T 4 T RT A31SO E20NE 2001051000102 20010510 00102 NM 2001 5 10 PCAA0104035 1 20010429 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM COCKPIT GROUNDED A PCAA K NONE O OTHER CR CRUISE 1 EA 13 806EX 263 ALB-FLT 3589 EMERGENCY LIGHTS ILLUMINATED IN FLIGHT IN ARMED POSITION. MAINTENANCE CHECKED ALL WIRING FROM CIRCUIT BRE AKER TO OVERHEAD CEILING ROW 1. INSPECTED WIRES AT SHUNT CANNON PLUG IN NOSE AREA AND NR 1 AND NR 2 TRANSFORMER RECTIF IER UNITS. REPLACED MATRIX BLOCKS 4 AND 5 ON 9811-TB14. EMERGENCY LIGHT CONTROL BOX REPLACED. EMERGENCY LIGHT BATTERI ES IN POSITIONS 400, 500, AND 600 REPLACED. FOUND TERMINATED WIRE 7A22 SHORTING TO GROUND AT COCKPIT EMERGENCY LIGHT BO X. WIRE REPAIRED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001051000103 20010510 00103 WP 2001 5 10 ABXA010213 1 20010502 A 3210 57591015505 FITTING DOUG DC8 DC863 302198A WP LT MLG CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 THE LEFT MAIN LANDING GEAR FORWARD LUG IS CORRODED AND GOUGED INSIDE THE BORE. 2 L 7 4 4F 4A25 2001051000104 20010510 00104 WP 2001 5 10 ABXA010214 1 20010502 A 3211 5611425 TRUNNION DOUG DC8 DC863 302198A WP LT MLG CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 THE LEFT MAIN LANDING GEAR TRUNNION FORWARD FITTING HAS CORROSION IN BOTH FWD BORES. 2 L 7 4 4F 4A25 2001051000105 20010510 00105 SO 2001 5 10 C2XA01IA229 1 20010427 A 3234 8271013 CONTROL HANDLE EMB 145 EMB145LR SO COCKPIT INOPERATIVE A C2XA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SW 27 13988 145265 IAH - FLIGHT 4196, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LAN DED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL HANDLE, AND THE AIRCRAFT WAS APPROVED F OR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001051000106 20010510 00106 SO 2001 5 10 C2XA01IA230 1 20010430 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145ER SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14942 145037 IAH - FLIGHT 4152, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT SEVERAL AISLE PATH EMERGENCY LIGHTS WERE INOPERA TIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY, AND THE AIRCRAFT WAS APPROVED FOR RET URN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001051000107 20010510 00107 SO 2001 5 10 C2XA01IA231 1 20010501 A 3350 12021299001 LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 57734 120199 IAH - DURING MAINTENANCE INSPECTION, THE RIGHT HAND OUTBOARD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R EMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001051000108 20010510 00108 EU 2001 5 10 C2XA01IA232 1 20010427 A 3350 AD3127 POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 42836 200 EFD - DURING MAINTENANCE INSPECTION, THE EMERGENCY LIGHT PAD WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001051000109 20010510 00109 SO 2001 5 10 C2XA01IA233 1 20010424 A 3350 12021299501 LIGHT EMB 120 EMB120ER 3260203 SO EXTERIOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 51726 120174 IAH - DURING MAINTENANCE INSPECTION, THE RIGHT HAND EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R EMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001051000110 20010510 00110 SO 2001 5 10 C2XA01IA234 1 20010429 A 3230 LANDING GEAR EMB 135 EMB135LR SO NLG & MLG MALFUNCTIONED A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 15527 BPT - DURING TRAINING FLIGHT 838, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE PERFORMED OPERATIONAL CHECKS ON THE LANDING GEAR EXTENSION / RETRACTION SYSTEM WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT TOOO11AT 2001051000111 20010510 00111 CE 2001 5 10 GLBA200189 1 20010501 A 2120 DUCT BEECH 1900 1900D 1154162 CE CENTER WING DAMAGED A GLBA O OTHER J WARNING INDICATION CR CRUISE 1 CE 01 211UX UE211 LEFT HAND BLEED AIR FAIL, CABIN HIGH ALT ANN (ICING CONDITIONS). REPAIRED EVA TUBING LEFT CENTER WING, OPS CHECKED GOOD . 2 L 7 2 4T RT A24CE 2001051000112 20010510 00112 NM 2001 5 10 A6WA200100031 1 20010501 A 2133 2099J020900 OUTFLOW VALVE DORNER DO32 DO328100 2996000 NM CABIN PRESSURE DIRTY A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 329ML 3087 CABIN ALTITUDE RWP CAME ON WHILE CLIMBING OUT WHEN PASSING THROUGH 10K, ALSO TRIED MAN PRESSURIZATION ACFT STILL WOULD N OT PRESSURIZE. MAINTENANCE CLEANED OUTFLOW VALVE FILTER PLUG AND PRESSURIZED ACFT, OPS CHECK GOOD. 2 H 7 2 4T RT A45NM 2001051000113 20010510 00113 NM 2001 5 10 C8GA20010009 1 20010427 A 5297 WIRE BOEING 727 727223 1384074 NM E/E DOOR SWITCH BROKEN A C8GA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SO 15 898AA 52321 22014 FLT 001 FROM MIA TO PTY. AFTER TAKEOFF ROTATION, CREW HEARD A LOUD NOISE IN THE COCKPIT AND WAS UNABLE TO PRESSURIZE AI RCRAFT. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. FOUND THE E&E COMPARTMENT DOOR OPEN. UPON FURTHER INSPE CTION, FOUND A BROKEN WIRE AT TERMINAL IN THE E&E BAY DOOR SWITCH. INSTALLED NEW TERMINAL IAW STANDARD PRACTICES 20-11 AND OPS CHECK DOR SYSTEM IAW MM 52-40-0. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2001051000114 20010510 00114 SO 2001 5 10 SWIA972543 1 20010502 A 2133 REGULATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CABIN PRESSURE FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 209SW 120269 A/C WOULD NOT PRESSURIZE. TRIED MANUAL CONTROLLER. STILL WOULD NOT PRESSURIZE. LEFT PACK PRESSURE REGULATOR SHUT OFF V ALVE LOW PRESSURE. REPLACED PRESSURE REGULATOR AND SHUT OFF VALVE IAW 21-50-01. P/N: 3214414-3, S/N ON: 693, S/N OFF : 949. PERFORMED FUNCTIONAL CHECK OF PRESSURIZATION SYSTEM IN AUTO/MAN IAW 21-30-00-501, PARAGRAPHS A-E. FUNCTION CHE CK OK. 2 L 7 2 4T 4 T RT A31SO E20NE 2001051000115 20010510 00115 WP 2001 5 10 ASAA0180077 1 20010219 A 5347 6019609 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 982AS 53473 PHX - DURING K-CHECK, FOUND AFT CARGO BAY CARGO TRACK CORRODED BETWEEN FS 1088 AND 1221, AT BL 15. REMOVED CORRODED TRA CK. FABRICATED AND INSTALLED NEW TRACK PER SRM 53-24-0. (M) 2 L 7 2 4F RT A6WE 2001051000116 20010510 00116 WP 2001 5 10 UPS01835788 1 20010420 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C1,3 RIGHT WING LOWER SKIN IS CRACKED AT XRS 172 BETWEEN STRINGERS 56 & 58. REPAIRED SKIN I.A.W. 8110-3 DH SK 707-212 2 L 7 4 4F RT 4A25 2001051000117 20010510 00117 WP 2001 5 10 UPS01835789 1 20010424 A 5713 STRINGER DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C1,3 RIGHT WING STRINGER 58 IS CRACKED AT XRS 172. REPAIRED STRINGER I.A.W. SRM. 57-2-2 FIG. 3D 2 L 7 4 4F RT 4A25 2001051000185 20010510 00185 NM 2001 5 10 UPS01235812 1 20010420 A 5755 69396331 HINGE BOEING 727 72722C 138400F NM SPOILER PANEL CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C BOTH END HINGES ON NR 7 SPOILER PANEL ARE CORRODED BEYOND LIMITS. REPLACED HINGES IAW SRM 51-30-02 2 L 7 3 4F A3WE 2001060100047 20010601 00047 NM 2001 6 1 UPS01635815 1 20010506 A 4920 APU BOEING 767 76734AF 1385212 NM APU BAY SHUTDOWN A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 322UP 27748 INSPECTION TYPE:ETOP PILOT REPORT-APU AUTO SHUTDOWN. *S/D* REMOVED AND REPLACED APU PER TC NR 6004. RUN CK AND LEAK C HECK PERFORMED, ALL OK OPS GOOD. CLEARED MMOC NOTIFIED PLACARD REMOVED. 2 L 7 2 4F RT A1NM 2001051800042 20010518 00042 NM 2001 5 18 UPS01635816 1 20010507 A 5313 STRINGER BOEING 767 767300 1385204 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 314UP 27742 CRACK FOUND DURING HFEC INSP OF GOUGE AT STA 460 STR 31R REMOVED FASTNERS IN AREA COMMON TO REPAIR REINSTALLED FASTNERS IAW BOEING 767 SRM 51-40-00 INTERIM REPAIR HAS BEEN RECLASSIFIED AS PERMANENT REPAIR PER BOEING AND UPS EO B767 5330-142 62 2 L 7 2 4F RT A1NM 2001051000186 20010510 00186 WP 2001 5 10 UPS01835817 1 20010505 A 3510 REGULATOR DOUG DC8 DC873F 302199F WP CAPTAINS O2 INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 813UP 46059 CREW PREFLIGHT -CAPTAINS O2 REGULATOR FAILED. R&R CAPTS 02 REGULATOR 2 L 7 4 4F RT 4A25 2001051000187 20010510 00187 WP 2001 5 10 UPS01835818 1 20010502 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 RIGHT WING OB. L/E. UPPER RIB IS CRACKED AT XFS 841.25 REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2001051000188 20010510 00188 WP 2001 5 10 UPS01835819 1 20010501 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE: C1, 3. LEFT WING L/E. UPPER RIB IS CRACKED AT XFS 750 REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2001051000189 20010510 00189 WP 2001 5 10 UPS01835820 1 20010501 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1, 3. LEFT WING L/E. LOWER RIB IS CRACKED AT XFS 397.750 REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2001051000190 20010510 00190 WP 2001 5 10 UPS01835821 1 20010501 A 5712 RIB DOUG DC8 DC873F 302199F WP LEFT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1, 3. LEFT WING L/E. UPPER RIB IS CRACKED AT XFS 778.750 REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2001051000191 20010510 00191 WP 2001 5 10 UPS01835822 1 20010501 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1, 3. LEFT WING L/E. UPPER RIB IS CRACKED AT XFS 772.5 REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2001051000192 20010510 00192 WP 2001 5 10 UPS01835823 1 20010501 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE: C1 ,3. LEFT WING L/E. UPPER RIB IS CRACKED AT XFS 766.25 REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2001051000193 20010510 00193 WP 2001 5 10 UPS01835824 1 20010430 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE: C1, 3. LEFT WING OB. L/E. LOWER SKIN HAS INTERGRANULAR CORROSION BETWEEN XFS 710-716.25 ***CPCP*** REPAIRED SKIN I.A.W. E.O. DC8-5720-4087,AND SRM. 51-1-20D,51-1-21 2 L 7 4 4F RT 4A25 2001051000194 20010510 00194 WP 2001 5 10 UPS01835825 1 20010501 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE: C1, 3. LEFT WING OB L/E. UPPER SKIN IS CORRODED BEYOND LIMITS AT XFS 628.75 ***CPCP*** REPAIRED SK IN I.A.W. SRM. 57-2-1 FIG. 38 2 L 7 4 4F RT 4A25 2001051000195 20010510 00195 WP 2001 5 10 UPS01835826 1 20010430 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE: C1, 3. LEFT WING L/E. LOWER SKIN IS CORRODED BEYOND LIMITS AT XFS 635 ***CPCP*** REPAIRED SKIN I.A .W. E.O. DC8-5720-4087-B APPX. C 2 L 7 4 4F RT 4A25 2001051000196 20010510 00196 2001 5 10 SWIA972548 4 20010504 A 2211 COMPUTER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE AUTOPILOT SYS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 07 290SW 120317 WHEN DISCONNECTING AUTOPILOT, AIRCRAFT INSTANTLY ROLLED HARD RIGHT. REQUIRED AN UNUSUAL AMOUNT OF OPPOSING LEFT AILERON TRIM AND AIRCRAFT WAS SLOW TO RECOVER. INSPECTED AUTO PILOT COMPUTER NR 2 RACK CONNECTOR AND WIRING. NO DEFECTS NOTED . REPLACED NR 2 APC-65 FOR TROUBLESHOOTING. A/P OPS CHECKS GOOD IAW 22-10-00. P/N ON 622-8315-402, S/N ON 3997, S/N O FF 1423. 2 L 7 2 4T 4 T RT A31SO E20NE 2001051000197 20010510 00197 EU 2001 5 10 SIMA20011054 1 20010415 A 7722 ENGINE SAAB SF340 340B 7860101 EU LT ENGINE OVERHEATED A SIMA C ABORTED TAKEOFF M OVER TEMP TO TAKEOFF 1 SW 21 312AE 340B312 PSP - FLT 3238 - CREW REPORTED, THE LEFT ENGINE ITT REACHED 934 DEGREES DURING TAKEOFF. ABORTED TAKEOFF AS PER AOM (927 DEGREES). MAINTENANCE FOUND ITT VALVE TO BE WITHIN LIMITS IAW GE MM 72-00-00 SPECIAL PROCEDUERS PAGE 246. ITT FELL WI THIN AREA ''A''. NO INSPECTION WAS REQUIRED AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001051000198 20010510 00198 SO 2001 5 10 SIMA20011055 1 20010415 A 2740 3621001007 CONTROL UNIT EMB 145 EMB145LR SO HORIZ STAB FAILED A SIMA K NONE F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SW 21 628AE 145124 DFW - FLT 3758 - DURING CRUISE FLIGHT CREW REPORTED EICAS MESSAGE PITCH TRIM 2 INOPERATIVE, AND BACK UP TRIM INOPERATIVE CAME ON. BOTH MESSAGES STAYED ON UNTIL TOUCHDOWN THEN CLEARED. MAINTENANCE REMOVED AND REPLACED HORIZONTAL STABILIZER CONTROL UNIT IAW EMB MM. AIRCRAFT WAS RELEASED FOR FUNCTIONAL CHECK FLIGHT. FCF WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001051000199 20010510 00199 SO 2001 5 10 SIMA20011053 1 20010415 A 7830 WARNING SYSTEM EMB 135 EMB135LR SO COCKPIT ACTIVATED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 730AE 145346 CMH - FLT 4983 - CREW REPORTED NR 1 THRUST REVERSER DISAGREE MESSAGE DURING TAKEOFF. THRUST REVERSER PUT ON MEL AT THIS TIME. (M) 2 L 7 2 4F RT TOOO11AT 2001051000200 20010510 00200 EU 2001 5 10 SIMA0896 1 20010330 A 3233 AIR123784 PIN SAAB SF340 340B 7860101 EU LT MLG BROKEN A SIMA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 903AE 340B282 FSM - FLT 3371 - CREW REPORTED NO DOWN AND LOCKED INDICATION FOR THE LEFT MLG, ALSO NO INTRANSIT OR GREEN LIGHT AND HYDR AULIC PUMP RUNS CONTINUOUSLY. MAINTENANCE FOUND AFT MLG ACTUATOR PIN (BOLT) BROKEN. MAINTENANCE REPLACED THE MLG TRUNN ION, MLG STRUT, DRAG BRACE, AND THE MLG ACTUATOR DUE TO DAMAGE FROM THE ACTUATOR PIN BREAKING. NEW PIN WAS INSTALLED. OPS AND LEAK CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001051000201 20010510 00201 EU 2001 5 10 SIMA09113 1 20010401 A 3220 ARD4313 PIN SAAB SF340 340B 7860101 EU NLG SHEARED A SIMA O OTHER E VIBRATION/BUFFET CL CLIMB 1 SW 21 335AE 340B335 SBP - FLT 3042 - AFTER TAKEOFF, WHEN GEAR WAS SELECTED UP CREW REPORTED A VIBRATION IN THE AIRCRAFT. A MODERATELY LOUD NOISE WAS HEARD AFTER GEAR RETRACTED. DURING LANDING CREW EXPERIENCED NOSEWHEEL SHIMMY DURING ROLLOUT. MAINTENANCE FOU ND THE BOLT THAT HOLDS A CAM IN PLACE THROUGH CENTER LINK SHEARED OFF. DRAG BRACE AND LINK WERE ALSO FOUND TO HAVE DAMA GE. DRAGE BRACE ASSEMBLY AND LINK WERE REMOVED AND REPLACED AND NEW BOLT INSTALLED. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001051000202 20010510 00202 EU 2001 5 10 SIMA200109903 1 20010409 A 5347 7253799383 SEAT TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 SBP - FOUND BL 18.3 LEFT SEAT TRACK HAS CORROSION AT SEAT 3A FLOOR FLANGE AND FORWARD REINFORCEMENT ANGLE. REMOVED AND REPLACED ANGLE CLIP AND FABRICATED SPLICE REPAIR IAW SAAB SRM 53-70 AND SAAB AMM 51-40. (M) 2 L 7 2 4T RT A52EU 2001051000203 20010510 00203 EU 2001 5 10 20010509SG001 1 20010409 A 5320 ANGLE SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 SBP - FOUND BL 18.3 LEFT SEAT TRACK HAS CORROSION AT SEAT 3A FLOOR FLANGE AND FORWARD REINFORCEMENT ANGLE. REMOVED AND REPLACED ANGLE CLIP AND FABRICATED SPLICE REPAIR IAW SAAB SRM 53-70 AND SAAB AMM 51-40. REF SIMA200109903. (M) 2 L 7 2 4T RT A52EU 2001051000204 20010510 00204 EU 2001 5 10 SIMA200109904 1 20010409 A 5311 7253721447 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 SBP - FOUND LEFT GALLEY SUPPORT FLOOR FRAME HAS SOME CORRODED RIVETS, INBOARD FRAME, AND BEAM. REMOVED AND REPLACED FRA ME AND BEAM IAW SAAB SRM 51-40. (M) 2 L 7 2 4T RT A52EU 2001051000205 20010510 00205 EU 2001 5 10 20010509SG002 1 20010409 A 5320 7253721427 BEAM SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 SBP - FOUND LEFT GALLEY SUPPORT FLOOR FRAME HAS SOME CORRODED RIVETS, INBOARD FRAME, AND BEAM. REMOVED AND REPLACED FRA ME AND BEAM IAW SAAB SRM 51-40. REF SIMA200109904. (M) 2 L 7 2 4T RT A52EU 2001051000206 20010510 00206 EU 2001 5 10 SIMA200109905 1 20010409 A 5730 7257502251 RING SAAB SF340 340B 7860101 EU RT WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 SBP - FOUND RIGHT WING ACCESS PANEL 621 CT HAS CORROSION ON THE PROTECTION RING. REMOVED AND REPLACED PROTECTION RING I AW SAAB AMM 57-30. (M) 2 L 7 2 4T RT A52EU 2001051000207 20010510 00207 EU 2001 5 10 SIMA200109906 1 20010409 A 5260 7253710871 TRACK SAAB SF340 340B 7860101 EU AIRSTAIRS CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 SBP - FOUND RAIL ASSEMBLY FOR AIRSTAIR IS CORRODED. REMOVED AND REPLACED RAIL IAW SAAB SRM 51-40. (M) 2 L 7 2 4T RT A52EU 2001051000208 20010510 00208 EU 2001 5 10 20010509SG003 1 20010409 A 5260 7253710135 BRACKET SAAB SF340 340B 7860101 EU AIRSTAIRS CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 SBP - FOUND RAIL ASSEMBLY FOR AIRSTAIR IS CORRODED. REMOVED AND REPLACED RAIL IAW SAAB SRM 51-40. REF SIMA200109906. (M) 2 L 7 2 4T RT A52EU 2001051000209 20010510 00209 EU 2001 5 10 SIMA200109907 1 20010409 A 2520 D1121F10137A SEAT SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 SBP - FOUND SEAT 3A IS CORRODED. REMOVED AND REPLACED SEAT ASSEMBLY IAW EO G1-2500-093-R5 PART 1. (M) 2 L 7 2 4T RT A52EU 2001051000210 20010510 00210 EU 2001 5 10 SIMA200109908 1 20010409 A 2520 D1121F10337A SEAT SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 SBP - FOUND SEAT 4A IS CORRODED. REMOVED AND REPLACED SEAT ASSEMBLY IAW EO G1-2500-93-R5 PART 1. (M) 2 L 7 2 4T RT A52EU 2001051000211 20010510 00211 EU 2001 5 10 SIMA200109909 1 20010409 A 2520 SEAT SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 SBP - FOUND SEAT 4BC IS CORRODED. REMOVED AND REPLACED SEAT ASSEMBLY IAW EO G1-2500-093-R5 PART 1. (M) 2 L 7 2 4T RT A52EU 2001051000212 20010510 00212 EU 2001 5 10 SIMA200109910 1 20010409 A 2520 D1121F10337A SEAT SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 SBP - FOUND SEAT 5A IS CORRODED. REMOVED AND REPLACED SEAT ASSEMBLY IAW EO G1-2500-093-R5 PART 1. (M) 2 L 7 2 4T RT A52EU 2001051000213 20010510 00213 EU 2001 5 10 SIMA200109911 1 20010409 A 2520 D2121F10437A SEAT SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 SBP - FOUND SEAT 5BC IS CORRODED. REMOVED AND REPLACED SEAT ASSEMBLY IAW EO G1-2500-093-R5 PART 1. (M) 2 L 7 2 4T RT A52EU 2001051000214 20010510 00214 EU 2001 5 10 SIMA200109912 1 20010409 A 2520 D1121F10337A SEAT SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 SBP - FOUND SEAT 6A IS CORRODED. REMOVED AND REPLACED SEAT ASSEMBLY IAW EO G1-2500-093-R5 PART 1. (M) 2 L 7 2 4T RT A52EU 2001051000215 20010510 00215 NE 2001 5 10 SIMA200109927 3 20010409 A 6140 58787158010 INDICATOR AEROSP ATR72 ATR72212 EU HAMSTD 247 247F1 NE COCKPIT FAILED A SIMA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SW 21 355AT 355 MIA - FLT 5339 - NR 1 NP GAUGE FAILED AFTER TAKEOFF IN FLIGHT. REMOVED AND REPLACED NP INDICATOR GAUGE IAW 61-42-81. O PS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 6 C P1BO 2001051000216 20010510 00216 EU 2001 5 10 SIMA20011073 1 20010417 A 3350 LIGHT AEROSP ATR72 ATR72212 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 426AT 426 MIA - FLT 3701 - FOUND CREW REPORTED THE CABIN INTERIOR EMERGENCY EXIT PATH LIGHTING NEXT TO ROW 6 TO BE INOPERATIVE. M AINTENANCE REINSTALLED LOOSE BULB IN EXIT EMERGENCY LIGHT AT ROW 6. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SER VICE. (M) 2 H 7 2 4T RT A53EU 2001051000217 20010510 00217 EU 2001 5 10 20010508CW015 1 20010419 A 2121 SCREW SNIAS 350 AS350B2 8680813 EU A/C BAY WORN B TU3R K NONE O OTHER IN INSP/MAINT 1 WP 07 955TV 20012 3246 THE AIR CONDITIONING SYSTEM WAS INSTALLED ON THE AIRCRAFT UNDER STC SH3509SW. DURING AN INSPECTION, THE AIR CONDITIONER CIRCUIT BREAKER WAS POPPED. THE CIRCUIT BREAKER WAS RESET AND THE SYSTEM FUNCTIONALY TESTED. SPARKS WERE SEEN AT THE BACK OF THE FAN ASSEMBLY. ON DISASSEMBLY, FOUND ONE RETAINING SCREW HAD LOOSENED ENOUGH TO CONTACT THE ARMATURE AND WOR E OVER HALF THROUGH WHILE SPINNING AND HAD LODGED IN THE ARMATURE TO NOT ALLOW THE ARMATURE TO SPIN. 1 G 7 1 3U H9EU 2001051000218 20010510 00218 WP 2001 5 10 GTIA010076 1 20010211 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP PAX DOOR INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 805NK 48087 DTW - FOUND PASSENGER ENTRY DOOR LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT IAW MD-80 MM 33-50.00. OPS CH ECK GOOD. (M) 2 L 7 2 4F A6WE 2001051000219 20010510 00219 WP 2001 5 10 GTIA010075 1 20010322 A 7333 8TJ85G PACKING DOUG DC9 DC982 3022082 WP LT ENGINE LEAKING A GTIA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 23 602CA 49415 ORD - FLT 781 - PRIOR TO ATC, NOTIFIED THE CREW THAT FLUID LEAKING FROM LEFT ENGINE. RETURNED TO GATE FOR MAINTENANCE. REPLACED F/F TRANSMITTER PACKING IAW MM 73-31-00. (M) 2 L 7 2 4F A6WE 2001051000220 20010510 00220 2001 5 10 GTIA010069 4 20010313 A 2565 SLIDE DOUG DC9 DC982 3022082 WP L1 DOOR OUT OF POSITION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48087 DTW - FLT 506 - L1 SLIDE PACK FELL OFF DOOR. REINSTALLED SLIDE PACK REF MD-80 MM 25-62-00. (M) 2 L 7 2 4F A6WE 2001051000221 20010510 00221 2001 5 10 GTIA010067 4 20010315 A 2230 2587781901 SERVO DOUG DC9 DC981 3022081 WP AUTOPILOT SYS FAULTY A GTIA K NONE O OTHER TO TAKEOFF 1 GL 23 811NK 48017 LGA - FLT 384 - ON TAKEOFF, AUTOTHROTTLES STOPPED SHORT OF FLEX POWER. DID NOT REDUCE WHEN CLIMB POWER SELECTED RAPID, SMALL CHANGES IN CRUISE. DID NOT ATTEMPT TO USE THEM ON DESCENT AND APPROACH. REMOVED AND REPLACED AUTO THROTTLES SERV O PER MM 22-01. PERFORMED DFGS RTS PER MM 22-01-05. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2001051000222 20010510 00222 2001 5 10 GTIA010066 4 20010302 A 2230 7771492 AUTOPILOT SYS DOUG DC9 DC981 3022081 WP COCKPIT MALFUNCTIONED A GTIA K NONE O OTHER TO TAKEOFF 1 GL 23 811NK 48017 DTW - FLT 656 - AUTOTHROTTLES ON TAKEOFF, WHEN CLIMB POWER WAS SELECTED. THROTTLES STAYED AT TAKEOFF POWER. SET MANUAL LY THEN REAPPLIED AUTO THROTTLES. AT LEVEL OFF, THROTTLES STAYED SET TO CLIMB POWER. REMOVED AND REPLACED TRI IND, SYS TEM OPS CHECK GOOD IAW MD-80 MM 34-18-02. THIS CLEARS DMI NR 108049-1. (M) 2 L 7 2 4F A6WE 2001051000223 20010510 00223 WP 2001 5 10 GTIA010055 1 20010304 A 3350 110049 CHARGER DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 969ML 47268 MYR - FLT 616 - FOUND AFT EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT CHARGER IAW DC-9 MM 3 3-53-00. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2001051000224 20010510 00224 2001 5 10 GTIA0100161 4 20010314 A 2211 COMPUTER DOUG DC9 DC932 3022066 WP AUTOPILOT SYS MALFUNCTIONED A GTIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 GL 23 133NK 48111 FLL - FLT 267 - AUTO-PILOT VERTICAL SPEED MODE MALFUNCTIONED WITH VSI SET TO RN 500 FPM. A/C CLIMBS AT NR 2000-2500 FPM . SAME PROBLEM IN CLIMB AND DESCENT. RE-RACK PITCH COMPUTER SELF TEST NORMAL IAW MM 22-12-0. UNABLE TO DUPCLICATE. ( M) 2 L 7 2 4F A6WE 2001051000225 20010510 00225 WP 2001 5 10 GTIA010060 1 20010307 A 3350 TRACK DOUG DC9 DC932 3022066 WP CABIN DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 133NK 48111 DTW - EMERGENCY FLOOR TRACK LIGHTING CARGO TAPE. REPAIRED WIRING AND REPLACED COVERS AS REQUIRED PER MM 33-50-00 TO CLE AR C/O NR 102420-4. EMERGENCY FLOOR TRACK LIGHTING CARGO TAPE. (M) 2 L 7 2 4F A6WE 2001051000226 20010510 00226 WP 2001 5 10 GTIA010059 1 20010304 A 3350 110049 CHARGER DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 969ML 47268 ACY - FLT 616 - AFT EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT CHARGER IAW DC-9 MM 33- 53-0, OPS CHECKS GOOD. (M) 2 L 7 2 4F A6WE 2001051000227 20010510 00227 WP 2001 5 10 GTIA010058 1 20010315 A 3242 BRAKE DOUG DC9 DC982 3022082 WP MLG INOPERATIVE A GTIA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 23 957AS 49126 RSW - FLT 1525 - FOUND APPEARS AS IF NR 1 BRAKE IS NOT OPERATING. BLED AIR FROM NR 1 BRAKE ASSEMBLY IAW MD-80 MM 32-40- 00. GROUND CHECK GOOD. (M) 2 L 7 2 4F A6WE 2001051000228 20010510 00228 WP 2001 5 10 GTIA010053 1 20010305 A 3350 COVER DOUG DC9 DC983 3022083 WP CABIN BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 ORD - FLT 781 - EMERGENCY EXIT LIGHTING C1 DEF PORTION BROKEN. RE-INSTALLED FLOOR TRACK COVER AT 1 DEF EMERGENCY LIGHT COVER. OPS CHECK OK IAW MM 33-53-01. (M) 2 L 7 2 4F RT A6WE 2001051000229 20010510 00229 WP 2001 5 10 GTIA010052 1 20010303 A 3350 TRACK DOUG DC9 DC983 3022083 WP CABIN OUT OF POSITION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FLL - FLT 784 - FLOOR STRIP LIGHTS POPPED UP NEAR ROW 11, WIRES EXPOSED. RESEATED ELT FLOOR STRIP AT ROW 11. OPS CHECK NORMAL AT THIS TIME PER ATA 33-51. (M) 2 L 7 2 4F RT A6WE 2001051000230 20010510 00230 WP 2001 5 10 GTIA010051 1 20010307 A 3350 LIGHT DOUG DC9 DC981 3022081 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 817NK 48018 FLT 679 - AFT LEFT AND RIGHT EMERGENCY EXIT DOOR EMERGENCY LIGHTS DON''T WORK. REWIRED BATTERY PACK B5-25 FOR AFT EMERG ENCY EXIT DOORS LIGHTS. OPS CHECK OK, REF MM 33-53-00. (M) 2 L 7 2 4F A6WE 2001051000231 20010510 00231 WP 2001 5 10 GTIA010050 1 20010305 A 3350 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48016 ORD - FLT 223 - AIRCRAFT FLOOR TRACK LIGHTING ILLUMINATED AND DRAINED WHEN APU GENERATOR DROPPED OFF LINE. RECHARGED EM ERGENCY LIGHTING SYSTEM AS REQUIRED. ALL WORK IAW MX-80 MM. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2001051000232 20010510 00232 WP 2001 5 10 GTIA010090 1 20010403 A 3350 COVER DOUG DC9 DC931 3022065 WP CABIN MISSING A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 969ML 47268 DTW - FOUND TRACK COVER MISSING AT SEAT ROW 9A. CUT TRACK AND REPLACED AT SEAT ROW 9A IAW DC-9 MM 33-50-00. (M) 2 L 7 2 4F A6WE 2001051000233 20010510 00233 WP 2001 5 10 GTIA010087 1 20010404 A 3297 WIRE DOUG DC9 DC983 3022083 WP MLG BROKEN A C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 23 DALLQ 53014 FLT 706 - LGA - WHEEL NOT TURNING LIGHT CAME ON AT 60 KNOTS. ABORTED TAKEOFF. PERFORMED T/S AS PER MM 32-43-00. SELF TEST SHOWED OB ANTI-SIDE FAILURE. PERFORMED BITE-TEST, FAILED LEFT OUTBOARD TRANSDUCER. FOUND BROKEN WIRE AT P1 AND D OF P1-196 AS PER WD 32-41-00. REPAIRED WIRING AT CONNECTOR P1-196. REINSTALLED TRANSDUCER. OPS CHECK NORMAL AS PER MM 32-43-02. (M) 2 L 7 2 4F RT A6WE 2001051000234 20010510 00234 WP 2001 5 10 GTIA010086 1 20010408 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DAMAGED A K NONE L NO TEST IN INSP/MAINT 1 GL 23 DALLQ 53014 DTW - FLT 476 - EMERGENCY FLOOR PATH LIGHTING HAS SEVERAL LIGHTS INOPERATIVE. REPAIR WIRING FOR FLOOR TRACK LIGHTING IA W MD-80 MM 33-50-00. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 2001051000235 20010510 00235 EA 2001 5 10 UHLA013309 1 20010325 A 3350 6104769 POWER SUPPLY DHAV DHC8 DHC8311 1386006 EA CABIN INOPERATIVE A UHLA K NONE L NO TEST IN INSP/MAINT 1 NE 03 802SA 250 FLT 525 - BED-TTN - CREW NOTICED THAT SOME OF THE EMERGENCY LIGHTS WHERE OUT DURING THERE PRE-FLIGHT. MAINTENANCE REMOV ED AND REPLACED EMERGENCY POWER SUPPLY. EMERGENCY LIGHT SYSTEM, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 2001051000236 20010510 00236 NM 2001 5 10 UIEA01039 1 20010413 A 7700 94002007 DISPLAY BOEING 747 7472D7B 1384803 NM COCKPIT FAILED A UIEA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 EA 15 527MC 22471 DURING CRUISE FLIGHT, RIGHT ENGINE INSTRUMENT DISPLAY FAILED, NR 2 EGT SPIKED UP AND FLIGHT CREW REPORTED SMOKE IN COCKP IT AND ELECTRICAL BURNING ODOR. SMOKE CLEARED AND FLIGHT CONTINUED TO DESTINATION. REMOVED AND REPLACED RIGHT ENGINE I NSTRUMENT DISPLAY SCREEN. (M) 2 L 7 4 4F RT A20WE 2001051000237 20010510 00237 NE 2001 5 10 20010509SG004 2 20010412 A 7230 COMPRESSOR LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE NR 1 ENGINE STALLED A WRNA E C ENGINE SHUTDOWN ABORTED TAKEOFF R E J PARTIAL RPM/PWR LOSS VIBRATION/BUFFET WARNING INDICATION TO TAKEOFF 1 SO 05 311EA 193A1012 ON TAKEOFF ROLL AT 125 KNOTS, NR 1 ENGINE HAD COMPRESSOR STALL. VIBRATION INDICATOR AT 2 UNITS WITH CAUTION LIGHT ON. AIRCRAFT RETURNED TO GATE. PREPARATION FOR TWO ENGINE FERRY BEING ACCOMPLISHED IAW LOCKHEED MM AND TRADEWINDS GMM FOR E NGINE CHANGE AT MX BASE. (M) 2 L 7 3 4F 4 F A23WE E12EU 2001051000238 20010510 00238 NM 2001 5 10 USAASB01102 1 20010417 A 3350 900835A POWER SUPPLY BOEING 737 737201 1384454 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 261AU 22867 MCO - THE CENTER OVERHEAD EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE CENTER OVERHEAD EMERGENCY EX IT LIGHT POWER SUPPLY. (M) 2 L 7 2 4F A16WE 2001051000239 20010510 00239 NM 2001 5 10 USAASB01098 1 20010407 A 3350 6013211 POWER SUPPLY BOEING 737 737201 1384454 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 246US 22753 CLE - THE AFT SERVICE DOOR AND AFT ENTRY DOOR EMERGENCY EXIT SIGNS AND ENTRY DOOR LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK. (M) 2 L 7 2 4F A16WE 2001051000240 20010510 00240 WP 2001 5 10 USAA010406 1 20010316 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 926VJ 46875 48146 PIT - FOUND SKIN CRACKED 1 INCH, STATION 1095 LONGERON 4 RIGHT. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER PER SRM 53 -04 FIG 27. (M) 2 L 7 2 4F A6WE 2001051000241 20010510 00241 WP 2001 5 10 USAA010412 1 20010322 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 820US 51417 49119 BOS - FOUND SKIN CRACKED .375 INCH, ACCESS DOOR 6102A STATION 1474 AT LONGERON 23R. INSTALLED DOUBLER PER EA 57939A. ( M) 2 L 7 2 4F A6WE 2001051000242 20010510 00242 WP 2001 5 10 USAA010413 1 20010323 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 820US 51417 49119 PIT - FOUND SKIN CRACKED .75 INCH AND PREVIOUS CRACK .25 INCH, STOP DRILLED AND PATCHED AT STATION 1437 L3L. CUT OUT DA MAGE, INSTALLED FILLER AND DOUBLER PER SRM 53-04, FIG 27. (M) 2 L 7 2 4F A6WE 2001051000243 20010510 00243 WP 2001 5 10 USAA010419 1 20010403 A 5311 9911850 FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 813US 52482 48093 PIT - FOUND FRAME CRACKED, 3R 1.5 INCH; 4R 2 INCHES; 5R 1.5 INCHES; 4L 2.75 INCHES, FS 1446 STRINGER 11-3 LT, 3-11 RT. MODIFIED PART 7139 KITTED PER DOUGLAS PRINT SRO 9530086-7139 PER SRM 53-03 FIG 30. (M) 2 L 7 2 4F A6WE 2001051000244 20010510 00244 WP 2001 5 10 USAA010420 1 20010418 A 5330 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 810US 53196 48042 PIT - FOUND SKIN CRACKED 1 INCH, STATION 1474 CANTED AT 9 OCLOCK POSITION ON FUSELAGE. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01 FIG 2. (M) 2 L 7 2 4F A6WE 2001051000245 20010510 00245 WP 2001 5 10 USAAD01082 1 20010422 A 5730 NAS335CPA10 SCREW DOUG DC9 DC982 3022082 WP FUEL PANEL LOOSE A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 816US 48096 CLT-BUF - FLT 1507 - DURING CRUISE, THERE WAS A STRONG SMELL OF KEROSENE/EXHAUST IN THE COCKPIT AND FORWARD GALLEY AREA, BUT NO SMOKE OR HAZE. THE SMELL DIMINISHED AFTER ABOUT 45 MINUTES OF FLIGHT. THE AIRCRAFT DIVERTED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE TIGHTENED LOOSE SCREWS ON THE LEFT WING INBOARD FUEL PANEL. THE FUEL LEAK WAS IN THE PAT H OF THE LEFT ENGINE INTAKE. THE AIR CONDITIONING WATER SEPARATOR BAGS WERE REPLACED AS PRECAUTIONARY MEASURE. (M) 2 L 7 2 4F A6WE 2001051000246 20010510 00246 NM 2001 5 10 USAASB01104 1 20010419 A 3350 110049 CHARGER BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 514AU 23700 PIT - MAINTENANCE FOUND THE EMERGENCY LIGHTS INOPERATIVE FROM SEAT ROW 17 AND AFT. ALSO, FOUND TWO AFT EMERGENCY EXIT D OOR LOWER LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK (P/N 2013-1A) AND CHARGER ASSEMBLY, LOC ATED ABOVE AISLE BETWEEN LAST ROW OF SEATS, IN ASSOCIATION WITH MM 33-51-51. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001051000247 20010510 00247 EU 2001 5 10 USAA010410 1 20010321 A 5313 STRINGER FOKKER F28 F28MK0100 4990807 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 899US 20979 11399 PIT - FOUND STRINGER CRACKED .75 INCH, STRINGER 69, STATION 3850. REPAIRED PER SRM 51-70-06 DOUBLER. (M) 2 L 7 2 4F RT 2001051000250 20010510 00250 NM 2001 5 10 AWXA0001680 1 20010501 A 5312 65163007 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 169AW 23630 FS 178 BLKHD CRACK AT WL 202.4 LBL 4.5. CUT OUT DAMAGED AREA; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW B737-30 0 SRM 51-10-08 TR 53-15 PG 1-11. 2 L 7 2 4F RT A16WE 2001051000251 20010510 00251 NM 2001 5 10 AWXA0001687 1 20010501 A 5320 65163007 STIFFENER BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 169AW 23630 FS 1153 TORQUE BOX LEFT LWR O/B EDGE OF STIFFENER. CUT OUT DAMAGED AREA, LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW B737-300 SRM 51-70-13 FIG 1 PG 1. 2 L 7 2 4F RT A16WE 2001051000252 20010510 00252 NM 2001 5 10 AWXA0001691 1 20010501 A 5315 65C33940 FLOORBEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 169AW 23630 THREE SPOTS OF CORROSION ON UPPER FLANGE OF FLOORBEAM BS 294 RBL 28-31. REMOVED CORRODED SECTION; FORMED AND INSTALLED SECTION OF UPPER T-CHORD IAW B737 SRM 51-20-01 PG 1 AND 51-40-05 PG 3 AND 53-10-08 PG 12 AND 53-00-51 PG 207 AND 51-10-0 2 PG 2. 2 L 7 2 4F RT A16WE 2001051800031 20010518 00031 NM 2001 5 18 UPS01235828 1 20010508 A 3230 ACTUATOR BOEING 727 72727C 138400J NM LT MLG MALFUNCTIONED A IPXA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 915UP 19533 INSPECTION TYPE:N/A LT MLG WOULD NOT RETRACT AFTER LANDING GEAR RETRACTION THE RED DOORS WARNING LIGHT AND LEFT GEAR UNL OCKED RED LIGHT REMAINED ILLUMINATED WHEN GEAR HANDLE WAS PUT IN OFF POSITION THE LEFT GEAR GREEN LIGHT WAS ILLUMINATED. REMOVED AND REPLACED LT MLG DOOR, OPERATED VALVE PER M/M 32-32-21. REMOVED AND REPLACED LT MLG MAIN UPLOCK ACTUATOR A SSY PER M/M 32-32-61 C/W LANDING GEAR EXT AND RET TEST PER M/M 32-32-00. 2 L 7 3 4F A3WE 2001051800032 20010518 00032 NM 2001 5 18 UPS01235829 1 20010508 A 3350 1000677 BATTERY BOEING 727 72727C 138400J NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 909UP 19115 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT AT A/C ENTRANCE WILL NOT TEST. REPLACED BATTERIES. 2 L 7 3 4F A3WE 2001051800041 20010518 00041 NM 2001 5 18 UPS01235831 1 20010508 A 5320 ATTACH ANGLE BOEING 727 72725C 138400H NM WING TO BODY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:N/A WING TO BODY ATTACH ANGLE CRACKED REMOVED L BRACKET 6196. REMOVED SLIDING FAIRING STRICKER BRACKET T O FOM 61964 FABRICATED AND REINSTALLED BRACKET PER 51-1-0 OF SRM 2 L 7 3 4F A3WE 2001071300005 20010713 00005 NM 2001 7 13 UPS01435834 1 20010508 A 5312 PRESSURE PANEL BOEING 747 747* NM APU BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 524UP INSPECTION TYPE:N/A 2 INCH HOLE CORRODED IN APU PRESS PAN CUTOUT. *S/D* TRANSFERRED TO UPS NRC 352493. 2 L 7 4 4F RT A20WE 2001073000195 20010730 00195 NM 2001 7 30 UPS01635832 1 20010508 A 5610 SEAL BOEING 767 76734AF 1385212 NM COCKPIT DIRTY A IPXA K NONE O OTHER CL CLIMB 1 SO 01 307UP 27760 INSPECTION TYPE:N/A PILOT REPORTS LOUD NOISE COMING FROM UNDER CAPTS SLIDING WINDOW NOISE STARTED AT 2 PSID AND ENDED AT 8 PSID. PRESSURIZED AIRCRAFT, NO DEFECTS NOTED. FOUND CAPTS WINDOW SEAL STICKING TO WINDOW AND POPPING DURING PRESSUR IZATION. CLEANED BULB SEAL AND PRESSURIZED A/C SEVERAL TIMES. NO NOISE NOTED. 2 L 7 2 4F RT A1NM 2001051000254 20010510 00254 EU 2001 5 10 SIMA200109902 1 20010409 A 5347 7253725191 SEAT TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 SBP - FOUND BL 0.0 SEAT TRACK HAS CORROSION THROUGH ENTIRE LENGTH OF WING BOX AREA. REMOVED AND REPLACED SEAT TRACK ASS EMBLY ALSO FABRICATED EXTRA LENGTH TO SEAT TRACK AS IT WAS NOT OF SIGNIFICANT LENGTH, IAW SAAB SRM 53-70-60. (M) 2 L 7 2 4T RT A52EU 2001051000255 20010510 00255 NE 2001 5 10 GTIA010071 2 20010305 A 7321 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE NR 2 ENGINE OUT OF TOLERANCE A GTIA O OTHER O OTHER TO TAKEOFF 1 GL 23 801NK 48048 DTW - FLT 506 - THROTTLES SPLIT, ONE KNOW WIDTH AT TAKEOFF POWER. PERFORMED ENGINE RUN, FOUND NR 2 CUT OF TRIM. TRIM N R 2 ENGINE IAW MD-80 MM 71-00-00. FOUND NO THROTTLE SPLIT AFTER TRIM. (M) 2 L 7 2 4F 4 F A6WE E9NE 2001051000256 20010510 00256 2001 5 10 GTIA010063 4 20010312 A 2565 LANYARD DOUG DC9 DC981 3022081 WP SLIDE DETACHED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 TPA - SLIDE PACK RELEASE LANYARD NOT ATTACHED. RE-ATTACHED RELEASE LANYARD THROUGH GIRT BAR MM 25-62-00. (M) 2 L 7 2 4F A6WE 2001051000257 20010510 00257 WP 2001 5 10 GTIA010089 1 20010403 A 3350 08163001108 COVER DOUG DC9 DC931 3022065 WP CABIN DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 969ML 47268 REPLACED COVER FOR TRACK LIGHTING AT ROW 14. CUT AND INSTALL ADDITIONAL LIGHT LENS AND BULBS. REPLACED FLOOR TRACK LIG HTING COVER AT ROW 14. CUT AND INSTALLED LIGHT LENS AND BULB HOLES IN THE NEW FLOOR TRACK LIGHTING COVER TO MATCH THE O LD FLOOR TRACK LIGHTING COVER PER DC9 MM 33-53-00. (M) 2 L 7 2 4F A6WE 2001051000258 20010510 00258 NM 2001 5 10 UHLA013331 1 20010404 A 3350 6104789 BATTERY PACK DHAV DHC8 DHC8301 NM CABIN INOPERATIVE A UHLA K NONE L NO TEST IN INSP/MAINT 1 NE 03 806SA 345 295 279 FLT 200 - TTN-BED - ON PREFLIGHT, INSPECTION EXIT SIGNS AT FORWARD CABIN AND AT FORWARD EMERGENCY EXIT INOPERATIVE. MAI NTENANCE CLEANED CONTACTS ON BATTERY PACKS, OPS CHECK GOOD IAW DHMM 33-51-00. REMOVED AND REPLACED BATTERY PACK AS PREC AUTIONARY MEASURE IN BUF. (M) 2 H 7 2 4T RT A13NM 2001051000259 20010510 00259 EU 2001 5 10 USAAF01015 1 20010419 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 861US 11297 GSO - THE SECOND STRIP OF FLOOR ESCAPE LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. OPS CHEC KED OK. (M) 2 L 7 2 4F RT 2001051000260 20010510 00260 2001 5 10 SWAA011352 4 20010505 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001051000261 20010510 00261 2001 5 10 SWAA011354 4 20010506 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001051000264 20010510 00264 WP 2001 5 10 ZW0A0101006 1 20010426 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT FOUND MEMBRANE CORRODED AT STA 160 TO 200, RBL 44 INCHES. CUT OUT CORRODED SECTION OF MEMBRANE FRO M STA 160 TO 200, RBL 44 IN TO RBL 58 IN PER SRM 51-70-4 FIG 1. INSTALLED MEMBRANE FROM STA 160 TO 200 RBL 44 IN TO RBL 58 IN PER DRAWING 9930538 AND SRM 51-70-4 FIG 1. CORROSION TREATED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001051100001 20010511 00001 WP 2001 5 11 0101569870 1 20010427 A 2131 CONTROLLER DOUG DC9 DC951 3022051 WP CABIN PRESSURE MALFUNCTIONED A NWAA B A EMER. DESCENT UNSCHED LANDING O OTHER CR CRUISE 1 GL 01 779NC 48101 AIRCRAFT LOST PRESSURIZATION AT FL280. CABIN ALTITUDE WENT TO 16,000 FT AND MASKS DEPLOYED. REPORTS OF SMOKE IN CABIN WERE UNFOUNDED, POSSIBLE CONDENSATION DUE TO RAPID DECOMPRESSION. FLIGHT DIVERTED TO YYZ AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED A DIRTY CABIN TEMPERATURE ANTICIPATOR. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2001051100002 20010511 00002 SO 2001 5 11 C2XA01CL092 1 20010420 A 3350 LIGHT EMB 145 EMB145ER SO CABIN MALFUNCTIONED A C2XA K NONE L NO TEST NR NOT REPORTED 1 SW 27 13935 145022 CLE FLIGHT 4272 THE CREW REPORTED THE REAR PORTION OF EMERGENCY FLOOR LIGHTS WAS INOPERATIVE. MAINTENANCE INSPECTED AND PLACED ON MEL 33-50-00/2. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF EMERGENCY LIGHTS AND NO DEFECTS WERE FOUND . THE MEL WAS CLEARED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001051100003 20010511 00003 CE 2001 5 11 CA010425002 1 20010412 A 5230 15D12636 LEVER RAYTHN DH125 HAWKER800 7450004 CE CARGO DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) A CRACK WAS FOUND IN THE CREW/FREIGHT DOOR OPENING LEVER AND BEARING TUBE ASSEMBLY (TUBE P/N 20DD11576), WHERE THE LEVER ATTACHES TO THE TORQUE TUBE (FOR THE ASSIST SPRING ASSEMBLY). INVESTIGATION PROVED THAT THE LAST TIME THE BEARING TUBE WAS REPLACED, THE ATTACH HOLES WERE DRILLED INCORRECTLY. THIS RESULTED IN EXCESSIVE FORCES BEING APPLIED TO THE LE VER WHEN THE DOOR WAS IN THE FULLY CLOSED POSITION (ASSIST SPRING WAS FULLY COMPRESSED BEFORE THE DOOR WAS FULLY CLOSED) .THE LEVER, BEARING TUBE, AND ASSOCIATED HARDWARE WERE REPLACED, CARE BEING TAKEN TO ENSURE CORRECT POSITIONING. 2 L 7 2 4F RT A3EU 2001051100043 20010511 00043 WP 2001 5 11 CALA0100436 1 20010502 A 5320 993061269 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 LEFT CABIN CUSP WEB IS HEAVILY CORRODED FS 1155-1174. REMOVED AND REPLACED CUSP WEB PER SRM 51-30-2, 51-30-5, 51-30-3, AND 51-30-0. 2 L 7 2 4F A6WE 2001051100044 20010511 00044 WP 2001 5 11 CALA0100437 1 20010502 A 5712 RIB DOUG DC9 DC982 3022082 WP RT WING CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 RIGHT WING LEADING EDGE RIB INBOARD OF ANTI ICE DUCT IS CHAFED. REMOVED AND REPLACED RIB PER SRM 57-30-2, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 2001051100045 20010511 00045 WP 2001 5 11 MWEA010693 1 20010502 A 5330 29524711 DOUBLER DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 REMOVED EXTERNAL DOUBLER LOCATED AT STATIONS 1309-1322 BETWEEN LONGERON 4R AND 5R. FABRICATED, LOCATED, DRILLED AND INS TALLED NEW EXTERNAL DOUBLER. 2 L 7 2 4F A6WE 2001051100046 20010511 00046 WP 2001 5 11 MWEA010694 1 20010502 A 5320 59327311 SPLICE DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 SPLICE FITTING ON LONGERON 29 LEFT AT STATION 588 CORRODED. REMOVED FITTING, DRILLED AND LOCATED AND INSTALLED SPLICE F ITTING. 2 L 7 2 4F A6WE 2001051100047 20010511 00047 WP 2001 5 11 MWEA010695 1 20010502 A 5313 59365631 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 FOUR FASTENER HOLES CORRODED OR ELONGATED ON LONGERON 30 STATIONS 769-788. REAMED HOLES, INSTALLED FREEZE PLUGS, FABRIC ATED AND DRILLED WASHERS, INSTALLED FASTENERS. 2 L 7 2 4F A6WE 2001051100048 20010511 00048 WP 2001 5 11 MWEA10697 1 20010502 A 5320 991007815 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 SEVERAL AREAS OF CORROSION ON RIGHT LOWER CUSP FROM STATION 204-225. REMOVED FASTENERS, SPLICE PLATES, CORROSION, TRIMM ED, DRILLED AND INSTALLED LOWER CUSP. 2 L 7 2 4F A6WE 2001051100049 20010511 00049 WP 2001 5 11 MWEA010698 1 20010502 A 5310 59360715 SHEAR TIE DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 FORWARD SIDE OF SHEAR CLIP AT STATION 636 AND BETWEEN LONGERON 30 AND 29 LEFT IS CORRODED. REMOVED SECTION OF FORMER, C ORROSION, INTERCOSTAL, DRILLED, LOCATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001051100050 20010511 00050 WP 2001 5 11 MWEA010700 1 20010502 A 5320 993657827 INTERCOSTAL DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 INTERCOSTAL AT STATION 1136 IN AFT PIT DOOR JAMB IS CORRODED. REMOVED INTERCOSTAL, SHEAR TIE, CORROSION, FABRICATED SHE AR TIE, INSTALLED SHEAR TIE AND INTERCOSTAL. 2 L 7 2 4F A6WE 2001051100051 20010511 00051 WP 2001 5 11 MWEA010701 1 20010502 A 5320 991960387 INTERCOSTAL DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 INTERCOSTAL AT STATION 1231 IN AFT PIT IS CORRODED. REMOVED CORROSION, FABRICATED SHEAR TIE, LOCATED AND DRILLED SHEAR TIE. 2 L 7 2 4F A6WE 2001051100052 20010511 00052 WP 2001 5 11 MWEA010702 1 20010502 A 5730 99374558 DOUBLER DOUG DC9 DC981 3022081 WP RT WING DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 REWORK PREVIOUS REPAIR, EXTERNAL DOUBLER REPAIR RIGHT WING LOWER SURFACE ONE DOUBLER AT EITHER END OF REFUELING CONTROL PANEL DOOR. REMOVED, FABRICATED AND INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F A6WE 2001051100053 20010511 00053 WP 2001 5 11 MWEA010703 1 20010502 A 5330 59360033 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 REWORK PREVIOUS BLEND OUT FROM STATION 693 TO 694.5, 1 INCH TO 2.5 INCH ABOVE LONGERON 24 RIGHT RIVETS. DRILLED AND INS TALLED FASTENERS. 2 L 7 2 4F A6WE 2001051100054 20010511 00054 WP 2001 5 11 MWEA010704 1 20010502 A 5310 39360912 DOOR FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 AFT SERVICE DOOR JAMB, MODERATE CORROSION ON FORWARD FACE OF AFT LOWER JAMB SUPPORT LEG. REMOVED FITTING AND CORROSION, LOCATED, DRILLED AND INSTALLED NEW FITTING. 2 L 7 2 4F A6WE 2001051100055 20010511 00055 WP 2001 5 11 MWEA010705 1 20010502 A 5320 59360713 INTERCOSTAL DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 MID CARGO BAY INTERCOSTAL OVER LONGERON 29 LEFT AT STATION 693-712 HAS LIGHT CORROSION AT FORWARD END (STA 694) AND AT S TATION 700 ON INTERIOR SURFACE. REMOVED INTERCOSTAL, FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001051100056 20010511 00056 WP 2001 5 11 MWEA010706 1 20010502 A 5330 592032349 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 SMALL DENT ON EXTERIOR SKIN AT STATION 239 APPROXIMATELY 2 INCHES BELOW LONGERON 19 LEFT. REPAIRED DENT. 2 L 7 2 4F A6WE 2001051100057 20010511 00057 WP 2001 5 11 MWEA010707 1 20010502 A 5313 591140613 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 LONGERON CRACKED AT STATION 200 AND LONGERON 2 LEFT. REMOVED DAMAGED LONGERON AND SPLICE, FABRICATED NEW LONGERON SECTI ON AND SPLICE, INSTALLED LONGERON AND SPLICE. 2 L 7 2 4F A6WE 2001051100058 20010511 00058 WP 2001 5 11 MWEA010708 1 20010502 A 5313 5935875505 STRINGER DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 REWORK PREVIOUS REPAIR, CENTER FUEL TANK AT STRINGER 21 AND XCW 42L FORWARD SIDE OF STRINGER. BLENDED AREA, FABRICATED AND INSTALLED ANGLE DOUBLER. 2 L 7 2 4F A6WE 2001051100059 20010511 00059 WP 2001 5 11 MWEA010709 1 20010502 A 5711 59358182 SPAR DOUG DC9 DC981 3022081 WP RT WING DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 REWORK PREVIOUS REPAIR ON RIGHT WING FORWARD SPAR AFT FACE BETWEEN XCW 58 AND 79, APPROXIMATELY 1 INCH AROUND FASTENERS. BLENDED AREAS, INSTALLED TENSION NUTS AND WASHERS. 2 L 7 2 4F A6WE 2001051100060 20010511 00060 WP 2001 5 11 MWEA010710 1 20010502 A 5330 59360229 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 AFT CARGO DOOR LOWER JAMB AREA THIS IS SURFACE CORROSION BETWEEN THE FUSELAGE SKIN AND INTERNAL DOUBLER FROM STATION 117 0 TO 1200. REMOVED CORROSION. 2 L 7 2 4F A6WE 2001051100061 20010511 00061 WP 2001 5 11 MWEA010711 1 20010502 A 5711 59358181 SPAR DOUG DC9 DC981 3022081 WP LT WING DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 REWORK PREVIOUS REPAIR, CENTER FUEL TANK LEFT WING FORWARD SPAR AFT FACE BETWEEN XCW 58 AND 79 (3 BLEND OUTS, FROM IB .0 70, .020 APPROXIMATELY 1 INCH DIAMETER AROUND FASTENERS) UPPER SPAR. BLENDED AREAS, INSTALLED TENSION MINI-NUTS AND WAS HERS. 2 L 7 2 4F A6WE 2001051100062 20010511 00062 WP 2001 5 11 MWEA010712 1 20010502 A 5320 991007813 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 CUSP CORRODED FROM STATION 169 TO 195, RIGHT SIDE GALLEY SERVICE DOOR. REMOVED CUSP, DRILLED AND TRIMMED NEW UPPER CUSP , FABRICATED AND DRILLED SPLICE, INSTALLED NEW UPPER CUSP AND SPLICE. 2 L 7 2 4F A6WE 2001051100063 20010511 00063 WP 2001 5 11 MWEA010713 1 20010502 A 5320 3936595547 FITTING DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 FITTING ASSEMBLY AT STATION 1219.50 AND LONGERON 28 RIGHT IS DOUBLE DRILLED AND SEVERLY CORRODED. REMOVED, LOCATED, DRI LLED AND INSTALLED NEW FITTING. 2 L 7 2 4F A6WE 2001060100149 20010601 00149 CE 2001 6 1 GLBA2001088 1 20010501 A 2841 CONNECTOR BEECH 1900 1900D 1154162 CE FUEL SYS DIRTY A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 01 96UX UE96 ABORTED TAKEOFF, LT FUEL QTY ANNUNCIATOR ILLUMINATED. CLEANED CANNON PLUG, OPS CHECK SATISFACTORY. 2 L 7 2 4T RT A24CE 2001051100064 20010511 00064 WP 2001 5 11 MWEA010714 1 20010501 A 3260 801801 SENSOR DOUG DC9 DC932 3022066 WP MLG INOPERATIVE A MWEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 204ME 47680 AFTER TAKEOFF FROM MILWAUKEE WITH GEAR UP, GEAR DOWN OPEN LIGHT IS ON. RETURNED TO MILWAUKEE. NOTE: WITH GEARDOWN AND THREE GREEN, GEAR DOOR OPEN LIGHT WAS OFF, LANDED WITHOUT INCIDENT. 2 L 7 2 4F A6WE 2001051100065 20010511 00065 CE 2001 5 11 GLBA2001090 1 20010430 A 3244 50060285 TIRE BEECH 1900 1900D 1154162 CE MLG SEPARATED A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 260GL 117 UE260 NR 3 TIRE TREAD SEPARATED, AIR RETURN. REMOVED AND REPLACED NR 3 TIRE ASSY. 2 L 7 2 4T RT A24CE 2001051100066 20010511 00066 NM 2001 5 11 ABXA010215 1 20010501 A 2910 1850 RELIEF VALVE BOEING BOEING 767 767281 1385109 NM HYD SYSTEM LEAKING A ABXA H DEACTIVATE SYST/CIRCUITS K FLUID LOSS DE DESCENT 1 GL 23 775AX 38637 22790 THE RIGHT HYDRAULIC QUANTITY DECREASED TO .67. THE ENGINE DRIVEN PUMP DE-PRESSURIZED AND THE ALTERNATING CURRENT MOTOR PUMP WAS SELECTED OFF. MAINTENANCE INSPECTED AND REPLACED THE FILTER MODULE RELIEF VALVE IAW B767 29-11-17. OPS AND LE AK CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A1NM 2001051100067 20010511 00067 NM 2001 5 11 F3LA200100059 1 20010427 A 5313 STINGER BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3498 23177 DURING C-6 CHECK, INSPECTION REPORTED CORROSION ON STRINGER 26-L, BS 500 - 500A. FABRICATED AND INSTALLED REPLACEMENT S TRINGER PER SRM 53-00-03. 2 L 7 2 4F RT A16WE 2001051100068 20010511 00068 NM 2001 5 11 F3LA200100060 1 20010503 A 5320 INTERCOSTAL BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3498 23177 DURING C-6 CHECK, INSPECTION REPORTED AFT GALLEY INTERCOSTAL CORRODED BETWEEN BS 1016 AND 986, BL 8L. FABRICATED AND IN STALLED REPLACEMENT LT AND RT INTERCOSTALS PER EA 53-737-117. 2 L 7 2 4F RT A16WE 2001051100069 20010511 00069 NM 2001 5 11 PCAA0105036 1 20010503 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 851EX 343 BGM- DURING SCHEDULED MAINTENANCE 2 FLOOR PATH EMERGENCY LIGHTS AT FORWARD CABIN FOUND INOPERATIVE. MAINTENANCE REPLACE D POWER SUPPLY AND BATTERY AT POSITION 400. EMERGENCY LIGHTS OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001051100070 20010511 00070 NM 2001 5 11 F3LA200100061 1 20010503 A 5320 CHANNEL BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3498 23177 DURING C-6 CHECK, INSPECTION REPORTED HAT CHANNEL AT BS 993, LBL 15 CORRODED. FABRICATED AND INSTALLED REPLACEMENT HAT CHANNEL PER SRM 53-60-51. 2 L 7 2 4F RT A16WE 2001051100071 20010511 00071 WP 2001 5 11 ZW0A0101101 1 20010430 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 9616G 53563 SEVERAL OVERHEAD EMERGENCY LIGHTS, THE TAIL CONE SLIDE LIGHT, AND SEVERAL EGRESS LIGHTS WERE INOPERATIVE IN MID CABIN. OVERHEAD AND TAIL CONE SLIDE LIGHTS CHECKED NORMAL. SECURED SEVERAL LOOSE CONNECTORS AT ROWS 12 AND 25 FOR THE EGRESS L IGHTS. CHECK-C 8-18-00 JFK. 2 L 7 2 4F RT A6WE 2001051100072 20010511 00072 WP 2001 5 11 ZW0A0101102 1 20010426 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 906TW 49160 DURING CHECK-C MAINT FOUND CORROSION IN CUSP ANGLE FWD OF SERVICE DOOR STATION 149 TO 164 AT LONGERON 18R, ON CUSP ANGLE AND VERTICAL ANGLE FWD EDGE OF RT SERVICE DOOR INSIDE LIGHTENING HOLE, BEHIND FWD LOWER DOOR JAMB AT STA 170R, BL 59 IN CHES, AND BEHIND THE AFT LOWER DOOR JAMB AT STA 197R, BL 59 INCHES. REMOVED CORRODED SECTION OF UPPER RT CUSP ANGLE FRO M STA 164 AFT TO FACTORY PRODUCTION BREAK AT STA 230. INSTALLED DOUBLER AT STA 164 AND SPLICED IN NEW FACTORY CUSP ANGL E. THIS AND ASSOCIATED REPAIRS TO DOOR JAMB SPLICES ACCOMPLISHED PER DRAWING J060288 AND SRM 53-05 FIG 55. CORROSION T REATED PARTS PER SRM 51-10-3. REMOVED CORROSION PER SPM 6-80-01. TREATED PER SRM 51-10-3 PAGE 1 AND 2B. 2 L 7 2 4F A6WE 2001051100073 20010511 00073 2001 5 11 SWIA972544 4 20010430 A 3414 INDICATOR EMB 120 EMB120RT SO PWA 118 PW118 NE COCKPIT FAILED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 156CA 120156 HIGH SPEED AURAL WARNING SOUNDED DURING TAKEOFF, RIGHT AFTER POWER LEVERS WERE SET FOR TAKEOFF TORQUE. REPLACED NR 1 AI RSPEED INDICATOR WITH SERVICEABLE UNIT IAW MM 34-12-01. OPS CHECK GOOD. COMPLIED WITH PITOT/STATIC CHECK IAW MM 34-11- 00. NO LEAKS NOTED AT THIS TIME. P/N: 39948-E2903, S/N ON: 1150, P/N OFF: 320AS1, S/N OFF: AH789. 2 L 7 2 4T 4 T RT A31SO E20NE 2001051100074 20010511 00074 NE 2001 5 11 EISA20010075 2 20010415 A 7261 79522 GARLOCK SEAL BOEING 727 727223 1384074 NM PWA JT8 JT8D9 52048 NE NR 2 ENGINE DAMAGED A EISA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 07 6839 20192 NR 2 ENGINE OIL QUANTITY LOSS IN FLIGHT AT RATE OF 3 GALLONS PER HOUR. AIR TURNBACK TO (IND). FOUND GARLOCK SEAL DAMAG ED BEHIND HYDRAULIC A-PUMP. REMOVED AND REPLACED GARLOCK SEAL PER M/M 72-61, NO LEAKS NOTED. 2 L 7 3 4F 4 F A3WE E2EA 2001051100075 20010511 00075 EA 2001 5 11 JBXA000277 1 20010502 A 4970 SENSOR CNDAIR CL600 CL6002B19 EA APU FAILED A JBXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 05 584ML 7330 APU OIL TEMP CAUTION LIGHT ILLUMINATED IN FLIGHT. AIRCRAFT THEN AIR RETURNED TO RDU BECAUSE THE NR 2 ENGINE IDG HAD EAR ILER BEEN PLACED ON THE DEFERRED MAINTENANCE ITEM LIST PER THE CL-65 MEL. AFTER ARRIVAL AT RDU THE APU OIL TEMP SENSOR WAS REMOVED AND REPLACED IAW WITH THE CL-65 AMM 49-91-25. OPS CHECKED APU OIL TEMP SYSTEM CHECKED GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2001051100076 20010511 00076 NM 2001 5 11 VNAA0104017 1 20010425 A 3350 SIGN DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN LOOSE A VNAA K NONE O OTHER TX TAXI/GRND HDL 1 GL 07 328JS 3030 THE CREW REPORTED THAT THE EMERGENCY SIGN AT ROW 11A WAS MISSING A SCREW AND IS LOOSE. MAINTENANCE INSPECTED AND RESURE D THE SIGN IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT W AS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001051100077 20010511 00077 NM 2001 5 11 VNAA0104018 1 20010426 A 2911 ACCUMULATOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE HYD SYSTEM LACK OF LUBE A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 438JS 3056 THE FLIGHT LEVELED OFF AT 27,000 FEET AND THE CREW RECEIVED AN EMERGENCY PARKING BRAKE ACCUMULATOR LOW CAS MESSAGE. THE CREW REFERENCED THE QUICK REFERENCE HANDBOOK AND WERE DIRECTED TO RETURN TO CHS. AS FLIGHT 4069 DESCENDED THROUGH 8000 FEET THE CAS MESSAGE EXTINGUISHED AND FLIGHT 4069 LANDED WITH NO FURTHER INCIDENT. MAINTENANCE INSPECTED AND SERVICED THE EMERGENCY PARKING BRAKE ACCUMULATOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 12-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001051100078 20010511 00078 NM 2001 5 11 VNAA0104019 1 20010427 A 3244 TIRE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT MLG BLOWN A VNAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 07 457PS 3048 AS THE FLIGHT ACHIEVED V1, THE CREW FELT A VIBRATION. THE FLIGHT ATTENDANT REPORTED THAT A PASSENGER HEARD A LOUD BANG FROM UNDER THE AIRCRAFT. THE CREW CALLED FLIGHT CONTROL AND WAS INSTRUCTED TO RETURN TO THE FIELD. THE AIRCRAFT WAS FU LL OF FUEL AND PASSENGERS SO FLIGHT 4022 WAS IN A HOLDING PATTERN FOR 45 MINUTES. ALL AGENCIES WERE ADVISED AND THE FLI GHT LANDED WITHOUT ANY FURTHER INCIDENTS. THE AIRCRAFT STOPPED ON THE RUNWAY AND THE PASSENGERS WERE BUSSED BACK TO THE TERMINAL. MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND MAIN INBOARD TIRE IN ACCORDANCE WITH DORNIER MAINTENANCE MA NUAL 32-00-00. THEN THE AIRCRAFT WAS TOWED BACK TO THE GATE. MAINTENANCE ALSO FOUND A HYDRAULIC LINE LEAK BECAUSE OF TH 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001051100079 20010511 00079 SO 2001 5 11 SWIA972551 1 20010505 A 2751 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT DIRTY A SWIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 07 204SW 120243 WHEN FLAPS SELECTED 45 DEGREES, INBOARD PAIR STAYED AT 25 DEGREES AND OUTBOARD PAIR SHOWED APPROX 38 DEGREES. WHEN FLAP S SELECTED 25 DEGREES OUTBOARD PAIR SHOW TO BE AT APPROX 20 DEGREES. DISAGREEMENT WHEN FLAPS SELECTED 45 DEGREES. CLEA NED CANNON PLUGS AND ROLLERS AND CYCLED FLAPS SEVERAL TIME. OPS CHECK GOOD ON GROUND. TROUBLESHOOTING ON GOING. 2 L 7 2 4T 4 T RT A31SO E20NE 2001051100080 20010511 00080 EU 2001 5 11 20010510SG001 1 20010409 A 5320 7253720210 ANGLE SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 SBP - FOUND BL 18.3 LEFT SEAT TRACK HAS CORROSION AT SEAT 3A FLOOR FLANGE AND FORWARD REINFORCEMENT ANGLE. REMOVED AND REPLACED ANGLE CLIP AND FABRICATED SPLICE REPAIR IAW SAAB SRM 53-70 AND SAAB AMM 51-40. REF SIMA200109903. (M) 2 L 7 2 4T RT A52EU 2001051100081 20010511 00081 WP 2001 5 11 USAAD01085 1 20010403 A 3350 AD4002P BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 934VJ 48114 PIT - THE COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 2001051100082 20010511 00082 WP 2001 5 11 USAAD01086 1 20010411 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 811US 48043 BOS - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001051100083 20010511 00083 2001 5 11 USAAD01084 4 20010425 A 2565 D29985103 SLIDE DOUG DC9 DC981 3022081 WP SERVICE DOOR UNSERVICEABLE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 811US 48043 MCO - THE AFT SERVICE DOOR EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS LOW. MAINTENANCE REPLACED THE AFT SERVICE DOO R EVACUATION SLIDE. (M) 2 L 7 2 4F A6WE 2001051100084 20010511 00084 EU 2001 5 11 USAAF01016 1 20010425 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN DAMAGED A K NONE L NO TEST IN INSP/MAINT 1 EA 19 887US 11349 IND- A SECTION OF FLOOR ESCAPE LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED WIRING TO LIGHT STRIP. OPS CHECKED OK. (M) 2 L 7 2 4F RT 2001051100085 20010511 00085 NM 2001 5 11 USAA010394 1 20010416 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 246US 51146 22753 TPA - FOUND SKIN CRACKED 1.5 INCH, BS 727B PLUS 12 INCHES, STRINGER 17L. INSTALLED REPAIR DOUBLE, SRM 53-30-3, FIG 1. (M) 2 L 7 2 4F A16WE 2001051100086 20010511 00086 NM 2001 5 11 USAA010395 1 20010401 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 246US 51146 22753 TPA - FOUND SKIN CRACKED 4 INCHES, BS 747 PLUS 3 INCHES, STRINGER 18R. INSTALLED REPAIR DOUBLER, SRM 53-30-3 FIG 1. (M ) 2 L 7 2 4F A16WE 2001051100087 20010511 00087 NM 2001 5 11 USAA010396 1 20010416 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 246US 51146 22753 TPA - FOUND SKIN CRACKED BS 727A PLUS 1 INCH BELOW STRINGER 17L, BS 727A PLUS 18 INCHES ABOVE STRINGER 18L. REMOVED EXI STING REPAIR, INSTALLED REPAIR DOUBLER AND TRIPLER, SRM 53-30-03 FIG 1. (M) 2 L 7 2 4F A16WE 2001051100088 20010511 00088 WP 2001 5 11 USAAD01083 1 20010424 A 3350 873100272 LIGHT DOUG DC9 DC981 3022081 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 809US 48041 IND - THE LEFT AFT OVERWING EMERGENCY WINDOW EXIT IDENTIFIER LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EXIT IDENT IFIER LIGHT ASSEMBLY. (M) 2 L 7 2 4F A6WE 2001051100089 20010511 00089 NM 2001 5 11 USAASB01103 1 20010419 A 2910 HYDRAULIC LINE BOEING 737 7372B7 1384560 NM NR 1 ENGINE LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 283AU 23116 LGA-JAX - FLT 2650 - DURING CRUISE, THE ''A'' SYSTEM HYDRAULIC QUANTITY DECREASED TO ZERO. AN EMERGENCY WAS DECLARED AN D THE FLIGHT DIVERTED TO CLT. EN ROUTE TO CLT, BOTH ''A'' SYSTEM LOW PRESSURE LIGHTS ILLUMINATED. FLIGHT LANDED WITHOU T FURTHER INCIDENT AND WAS TOWED TO THE GATE. MAINTENANCE FOUND THE NR 1 ENGINE PRESSURE AND RETURN HYDRAULIC LINES CHA FED AND LEAKING. INSTALLED SERVICEABLE LINES AND REPLACED BOTH ENGINE DRIVEN HYDRAULIC PUMPS AND CASE DRAIN FILTERS. S ERVICED HYDRAULIC SYSTEM RESERVOIR. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F A16WE 2001051100090 20010511 00090 EU 2001 5 11 USAASA01012 1 20010418 A 3350 1012881 LIGHT AIRBUS A319 A319112 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 720US 1089 SNA - THE ROW THREE EMERGENCY EXIT SEAT LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPS CHECKED OK . (M) 2 L 7 2 4F RT A28NM 2001051100091 20010511 00091 EU 2001 5 11 USAASA01013 1 20010421 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319112 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 722US 5484 1097 PHL - THE LT AND RT OVERWING EXIT LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2001051100092 20010511 00092 EU 2001 5 11 USAASA01014 1 20010424 A 3350 321430 BATTERY AIRBUS A319 A319112 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 742UW 1275 DCA - THE FORWARD LEFT EMERGENCY EXIT POWER SUPPLY UNIT BATTERY TEST FAILED. MAINTENANCE REPLACED THE FORWARD LEFT EMER GENCY EXIT POWER SUPPLY BATTERY. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2001051100093 20010511 00093 EU 2001 5 11 USAASA01010 1 20010401 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320214 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 108UW 269 1061 TPA - THE AIRCRAFT FAILED THE EMERGENCY EXIT LIGHT TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT. SYSTEM TESTS NORMAL. (M) 2 L 7 2 4F RT A28NM 2001051100094 20010511 00094 NE 2001 5 11 SIMA20011075 2 20010417 A 7532 6068T56P01 BLEED VALVE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE INOPERATIVE A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 236AE 340B236 JFK - FLT 5016 - DURING CLIMB, THE LEFT IGNITION LIGHT WAS INTERMITTENT. AIRCRAFT RETURNED TO JFK. PUT ON MEL AT THIS TIME. MAINTENANCE REMOVED AND REPLACED THE ANTI-IC START BLEED VALVE FOR THE LEFT ENGINE IAW GE MM 75-00-00. OPS CHECK WAS GOOD IAW SAAB MM 71-00-00 AND 74-30-00. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 2001051100095 20010511 00095 EU 2001 5 11 SIMA200110201 1 20010412 A 7930 CHIP DETECTOR SAAB SF340 340B 7860101 EU LT ENGINE ACTIVATED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 397AE 340B397 DFW - FLT 3811 - LEFT ENGINE CHIP LIGHT CAME ON IN FLIGHT. AIR TURN BACK. (M) 2 L 7 2 4T RT A52EU 2001051100097 20010511 00097 EU 2001 5 11 SIMA0665 1 20010307 A 3350 3012701 LIGHT AEROSP ATR72 ATR72212 EU PAX DOOR INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 498AT 498 DFW - FLT 3726 - PASSENGER DOOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED MAIN DOOR EMERGENCY LIGHT ASSEMBLY I AW JIC 33-51-24. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 2001051100098 20010511 00098 NE 2001 5 11 SIMA200109803 2 20010408 A 7200 ENGINE AEROSP ATR72 ATR72212 EU PWA PW120 PW127 NE NR 1 ENGINE OVERTEMP A SIMA C ABORTED TAKEOFF M OVER TEMP TO TAKEOFF 1 SW 21 529AM 529 OKC - FLT 3574 - CREW ABORTED TAKEOFF DUE TO OVER TEMP ON NR 1 ENGINE. APPROX 1200 DEGREES FOR 3 SECONDS. REMOVED AND REPLACED NR 1 ENGINE IAW AMM. OPS CHECK GOOD IAW AMM. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 2001051100099 20010511 00099 EU 2001 5 11 SIMA0961 1 20010326 A 5320 S5367800021401 FLOOR SUPPORT AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AT 434 SAW - DURING CPCP-2 INSPECTION MAINTENANCE, REPORTED THE LAV FLOOR SUPPORT BETWEEN FRAMES 39 AND 40 CORRODED. MAINTENAN CE REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-25-03. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001051100100 20010511 00100 SW 2001 5 11 20010510SG002 1 20010203 A 2910 FITTING FRCHLD SA227 SA227DC 3377521 SW HYD SYSTEM LEAKING A BSAA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 NM 05 850LS DC850B ON SHORT FINAL, THE CREW NOTICED THE RT HYD PRESS LIGHT CAME ON. GEAR WAS ALREADY DOWN AND FLAPS WERE AT FULL. CREW NO TICED FLUCTUATIONS IN HYD PRESSURE. CREW TURNED OFF NOSE WHEEL STEERING. LANDING WAS UNEVENTFUL LT HYD PRESS LIGHT CAM E ON JUST BEFORE REACIHNG THE GATE. CREW SHUT DOWN AIRCRAFT WITH NO FURTHER PROBLEMS. HYDRAULIC LEAK IN LEFT FLAP ACTU ATOR AREA. REPLACED BULKHEAD FITTING THAT GOES FROM FLAP HARD LINE TO FLEX LINE IN AFT END OF NACELLE. SERVICED AND BLED HYDRAULIC SYSTEM. HYD SYSTEMS OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A18SW 2001051100104 20010511 00104 NM 2001 5 11 AALA20010195 1 20010203 A 3350 CONNECTOR BOEING 727 727227 1384078 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 726AA 20733 DFW - DURING OVERNIGHT MAINTENANCE, FLOOR PROXIMITY EMERGENCY EXIT PATH LIGHT DIM. REPAIRED FLOOR PROXIMITY EMERGENCY E XIT PATH LIGHT CONNECTION AT SEAT 5D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001051100105 20010511 00105 WP 2001 5 11 AALA20010724 1 20010403 A 5530 HINGE FITTING DOUG DC9 DC982 3022082 WP VERTICAL STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7514A 49891 TUL - FOUND TWO RIGHT OUTBOARD, TWO RIGHT INBOARD, TWO LEFT OUTBOARD, TWO LEFT INBOARD VERTICAL STABILIZER HINGE PLATES CORRODED. REMOVED AND REPLACED 2 RIGHT OUTBOARD, 2 RIGHT INBOARD, 2 LEFT OUTBOARD, 2 LEFT INBOARD VERTICAL STABILIZER H INGE PLATES PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2001051100106 20010511 00106 WP 2001 5 11 AALA20010725 1 20010324 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7514A 49891 TUL - FOUND CORROSION IN SEAT TRACK NR 1 AT 1208. INSTALLED NEW NR 1 SEAT TRACK FROM STATION 1174 TO STATION 1309 PER S RM 53-05. (M) 2 L 7 2 4F A6WE 2001051100107 20010511 00107 WP 2001 5 11 AALA20010726 1 20010324 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7514A 49891 TUL - FOUND CORROSION ON SEAT TRACK NR 1 AT STATION 1199-1202. INSTALLED NEW NR 1 SEAT TRACK FROM STATION 1174 TO STATI ON 1309 PER SRM 53-05. (M) 2 L 7 2 4F A6WE 2001051100108 20010511 00108 WP 2001 5 11 AALA20010727 1 20010322 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7514A 49891 TUL - FOUND SEAT TRACK NR 1 CORRODED STATION 522 PLUS 6. INSTALLED 1 NEW SEAT TRACK PLUG PER AARD 53-20-00-10. (M) 2 L 7 2 4F A6WE 2001051100109 20010511 00109 WP 2001 5 11 AALA20010728 1 20010324 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7514A 49891 TUL - FOUND CORROSION ON SEAT TRACK NR 1 AT STATION 1236-1237. INSTALLED NEW NR 1 SEAT TRACK FROM STATION 1174 TO 1309 PER SRM 53-05. (M) 2 L 7 2 4F A6WE 2001051100110 20010511 00110 WP 2001 5 11 AALA20010729 1 20010322 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7514A 49891 TUL - FOUND CORROSION ON LEFT CUSP STATION 598 TO 712. INSTALLED NEW CUSP SHEET FROM STATION 598 TO 712 LEFT SRM 51-01. (M) 2 L 7 2 4F A6WE 2001051100111 20010511 00111 WP 2001 5 11 AALA20010730 1 20010326 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7514A 49891 TUL - FOUND SMALL SPOT OF CORROSION ON RIGHT CUSP AT STATION 267. CUT OUT CORROSION PER SRM 51-10-3. INSTALLED DOUBLER PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2001051100112 20010511 00112 WP 2001 5 11 AALA20010731 1 20010322 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7514A 49891 TUL - FOUND CORROSION ON SEAT TRACK NR 5 STATION 230-237. REPLACED SEAT TRACK STATION 199-246 IAW SRM 53-05 FIG 4F SHEE T 2. (M) 2 L 7 2 4F A6WE 2001051100113 20010511 00113 WP 2001 5 11 AALA20010732 1 20010323 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7514A 49891 TUL - FOUND CORROSION ON AFT CARGO DOOR BEAM OUTBOARD FACE FROM STATION 1160 TO 1208. INSTALLED DOUBLER PER AARD 53-10- 00-3. (M) 2 L 7 2 4F A6WE 2001051100114 20010511 00114 WP 2001 5 11 AALA20010733 1 20010327 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7514A 49891 TUL - FOUND NR 6 SEAT TRACK FORWARD END CORRODED, FS 218. SPLICED IN NEW SECTION OF NR 6 SEAT TRACK FROM STATION 212-30 2 PER SRM 53-05 FIG 4F. (M) 2 L 7 2 4F A6WE 2001051100115 20010511 00115 WP 2001 5 11 AALA20010734 1 20010327 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7514A 49891 TUL - FOUND FUSELAGE SKIN DENTED BETWEEN LONGERONS 24R AND 25R STATION 472 TO 503, DENTED UP TO .050 INCH DEEP. REWORKE D SKIN TO CONTOUR AND INSTALLED INTERNAL DOUBLER PER SRM 53-04 FIG 38 SHEET 22 AND ESO 80559 DATED 6/2/2000. (M) 2 L 7 2 4F A6WE 2001051100116 20010511 00116 WP 2001 5 11 AALA20010735 1 20010327 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7514A 49891 TUL - FOUND DENT IN FUSELAGE SKIN STATION 1125 LEFT SIDE BETWEEN LONGERON 22 AND 23L. COLD WORKED DENTED AREA. DYE CHE CKED, NO CRACKS FOUND. INSTALLED REPAIR DOUBLER PER SRM 53-04. (M) 2 L 7 2 4F A6WE 2001051100117 20010511 00117 WP 2001 5 11 AALA20010736 1 20010321 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7514A 49891 TUL - FOUND LONGERON L4 CRACKED AT STATION 160 AT FASTENER HOLE. CUTOUT DAMAGE SECTION AND INSTLALED SPLICE PER SRM 53- 02 FIGURE 18. (M) 2 L 7 2 4F A6WE 2001051100118 20010511 00118 WP 2001 5 11 AALA20010737 1 20010321 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7514A 49891 TUL - FOUND LEFT CUSP CORRODED ALONG OUTBOARD EDGE STATION 527-540. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53- 04. (M) 2 L 7 2 4F A6WE 2001051100119 20010511 00119 WP 2001 5 11 AALA20010738 1 20010321 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7514A 49891 TUL - FOUND LEFT CUSP CORRODED AROUND LIGHTENING HOLE STATION 507. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-0 4. (M) 2 L 7 2 4F A6WE 2001051100120 20010511 00120 WP 2001 5 11 AALA20010739 1 20010320 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7514A 49891 TUL - FOUND CORROSION ON LEFT CUSP STATION 997. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-01 FIG 4. (M) 2 L 7 2 4F A6WE 2001051100121 20010511 00121 WP 2001 5 11 AALA20010740 1 20010324 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7514A 49891 TUL - FOUND DEEP GOUGES IN FUSELAGE SKIN AT STATION 534 AT LONGERON 27L. REMOVED DAMAGED AREA, DYE CHECKED, NO CRACKS F OUND. FABRICATED DOUBLER FROM GAL4V T1 .032 INCH FILLER FROM 2024T3 .050 INCH. INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M) 2 L 7 2 4F A6WE 2001051100122 20010511 00122 WP 2001 5 11 AALA20010741 1 20010328 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7514A 49891 TUL - FOUND FRAME 1485 IS CRACKED AT STAIR ACTUATOR CASTING, RIGHT SIDE. INSTALLED SPLICE PER ESO 80559 DATED 2-23-01, MRR WRITTEN. (M) 2 L 7 2 4F A6WE 2001051100123 20010511 00123 WP 2001 5 11 AALA20010742 1 20010328 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7514A 49891 TUL - FOUND ANTENNA INSTALLATION POINT AT FS 380 AND 402, BETWEEN LONERON 29 AND 30 LEFT HAVE CRACKS 1.5 INCHES LONG. C UT OUT DAMAGED AREAS 4 BY 6 INCHES AND INSTALLED INNER AND OUTER DOUBLER PER SRM 53-04, FIG 12B. (M) 2 L 7 2 4F A6WE 2001051100124 20010511 00124 WP 2001 5 11 AALA20010743 1 20010328 A 5230 SKIN DOUG DC9 DC982 3022082 WP CARGO DOOR DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7514A 49891 TUL - FOUND SEVERAL DENTS IN SKIN OF ''DOOR''. REMOVED OLD SKIN AND INSTALLED NEW SKIN PER ESO 80174 3-26-01 OF ENTIRE AFT CARGO DOOR. (M) 2 L 7 2 4F A6WE 2001051100125 20010511 00125 SW 2001 5 11 20010510SG003 1 20010218 A 3260 DOWNLOCK SWITCH SWRNGN SA227 SA227* SW LT MLG FAULTY A BSAA O OTHER N FALSE WARNING DE DESCENT 1 NM 05 1119K 830B LEFT MLG DOWN LIGHT DIDN''T COME ON. THE PRESS TO TEST SHOWED BULB WORKED. CREW CHECKED FOR GEAR DOWN BY PULLING POWER BACK TO IDLE, THERE WAS NO GEAR HORN SOUNDING. THIS MEANT THE GEAR WAS DOWN BECAUSE THE HORN IS RUN FROM THE OTHER HAL F OF THE GEAR DOWN SWITCH. GEAR SWITCH FAILURE. SWITCHES WERE CLEANED, GEAR WAS CYCLED 12 TIMES ON THE JACKS. NO PROB LEMS WERE NOTED. AIRCRAFT WAS TEST FLOWN WITH NO PROBLEMS. AIRCRAFT WAS RETURNED TO SERVICE. PROBLEM SEEMS TO BE A ON E TIME OR EXTREMELY INTERMITTENT SWITCH PROBLEM. (M) 2 L 7 2 4T RT A5SW 2001051100126 20010511 00126 EA 2001 5 11 SWIA972553 1 20010507 A 2750 FLAP CNDAIR CL600 CL6002B19 EA WING MALFUNCTIONED A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 412SW 7101 FLAPS FAILED AT 3 DEGREES ON RETRACTION. RETURNED TO AIRPORT. CYCLED POWER. C/W AD98-20-01, PARA B. FOUND FLAPS TO O PERATE NORMAL. 2 L 7 2 4F RT A21EA 2001051100127 20010511 00127 SO 2001 5 11 SWIA972554 1 20010507 A 2750 CONTROL HANDLE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT FAULTY A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 NM 07 190SW 120050 CONTROL FAULT AT FLAPS 15 DEGREES. REMOVE AND REPLACE FLAP CONTROL HANDLE IAW 27-50-01. OPS CHECK GOOD. P/N ON: 120- 42642-001, S/N ON: 120128, P/N OFF: 120-42642-507, S/N OFF: 120-283. 2 L 7 2 4T 4 T RT A31SO E20NE 2001051100128 20010511 00128 EA 2001 5 11 SWIA972556 1 20010508 A 2751 FCU CNDAIR CL600 CL6002B19 EA FLAPS FAILED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 412SW 7101 FLAP FAIL MESSAGE AFTER DEPARTURE. RETURNED TO SMF. REMOVED AND REPLACED FECU IAW RJ MM 27-51-05. REMOVED AND REPLACE D BOTH BPSU''S IAW RJ MM 27-51-10. FLAP SYSTEM OPS CHECK GOOD. BPSU LT P/N ON: 855D100-9, S/N ON: 1150, P/N OFF: 60 1R93105-7, S/N OFF: 303. BPSU RT P/N ON: 855D100-9, S/N ON: 418, P/N OFF: 601R93105-7, S/N OFF: 393, P/N: 860D100 -18, S/N ON: 222, S/N OFF: 233. 2 L 7 2 4F RT A21EA 2001051100129 20010511 00129 2001 5 11 SWAA011355 4 20010507 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 091SW 22963 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001051100130 20010511 00130 NM 2001 5 11 SWAA011371 1 20010506 A 5523 BACB28AK04 BUSHING BOEING 737 7377H4 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 705SW 27839 DURING SCHEDULED C4 CHECK, SWA SI 11038-55, FOUND LT ELEVATOR TAB INBD HINGE BUSHING WORN. REMOVED AND REPLACED BUSHING AND BOLT PER MM. 2 L 7 2 4F RT A16WE 2001051100131 20010511 00131 2001 5 11 SWAA011378 4 20010508 A 2565 D31354 SLIDE BOEING 737 7373Y0 1384671 NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 308SA 23498 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001051100132 20010511 00132 NM 2001 5 11 SWAA011379 1 20010507 A 2731 251A243010 CONTROL ARM BOEING 737 7377H4 NM ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 717SA 27851 DURING SCHEDULED SERVICE CHECK, SWA SI 11052-55, FOUND LT ELEVATOR TAB CONTROL MECHANISM HAS EXCESSIVE PLAY AT ROD CONNE CTIONS. REMOVED AND REPLACED ELEVATOR TAB CONTROL MECH PER MM. 2 L 7 2 4F RT A16WE 2001051100133 20010511 00133 2001 5 11 SWAA011380 4 20010507 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CASE. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001051100134 20010511 00134 2001 5 11 SWAA011381 4 20010508 A 2565 D31354 SLIDE BOEING 737 7377H4 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 710SW 27844 FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CASE. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001051500060 20010515 00060 CE 2001 5 15 20010515AP003 1 20010502 A 7603 5038901229 CONTROL CABLE BEECH 58 58 1152740 CE CONT O520 IO520* 17032 SO RT THROTTLE BROKEN D E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 SW 99 78DM TH281 816967 RH THROTTLE CABLE BROKE IN FLIGHT. PILOT PERFORMED IN FLIGHT SHUTDOWN. INSPECTION REVEALED CABLE BROKE INSIDE FERRULE JU ST BEFORE CRIMP ON ENGINE SIDE. THIS CONDITION WOULD BE IMPOSSIBLE TO DETECT BY NORMAL INSPECTION PROCEDURES. 1 L 7 2 3O 3 O 3A16 E5CE 2001051500062 20010515 00062 WP 2001 5 15 ZW0A0101103 1 20010501 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 924TW 49100 DURING CHECK-C MAINT IN MID CARGO COMPT AT STA 598, LONGERON 24R AND 27R, THE FLOOR SUPPORT WAS CRACKED IN 2 PLACES. WE LDING SHOP WELDED CRACKS AND STRESS RELIEVED ANGLE PER SSRM 53-00-106. PRIMED PER SRM 51-10-3. INSTALLED PER SRM 51-30 -2. 2 L 7 2 4F A6WE 2001051500063 20010515 00063 WP 2001 5 15 ZW0A0101104 1 20010501 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 924TW 49100 DURING CHECK-C MAINT IN FWD CARGO COMPT, STA 275 AND LONGERON 24L, THE FORMER HAD A CRACK. STOP DRILLED CRACK. SENT FL OOR SUPPORT TO WELDING FOR REPAIR IN REF TO SSRM 53-00-106. PAINTED SUPPORT PER SRM 51-10-3 AND SRM 51-30. 2 L 7 2 4F A6WE 2001051500064 20010515 00064 WP 2001 5 15 ZW0A0101105 1 20010501 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 924TW 49100 DURING CHECK-C MAINT IN THE FWD CARGO COMPT, FLOOR SUPPORT ANGLE WAS CRACKED ON FORMER STA 503, JUST INBOARD OF LONGERON 24L. REMOVED AND REPLACED RIVETS PER SRM 51-30-7 AND HI-LOKS PER SRM 51-30-5, TO REPAIR ANGLE PER SSRM 53-00-106. 2 L 7 2 4F A6WE 2001051500065 20010515 00065 WP 2001 5 15 ZW0A0101106 1 20010314 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 908TW 49169 DURING CHECK-C MAINT IN THE AFT CABIN THE FLOOR SUPPORT STRUCTURE WAS CORRODED AT STA 1250, LBL 23 TO RBL 43. REMOVED C ORRODED SUPPORT AND REPLACED WITH NEW AND INSTALLED WITH HI-LOK FASTENERS PER SRM 51-30-5. 2 L 7 2 4F A6WE 2001051500066 20010515 00066 WP 2001 5 15 ZW0A0101107 1 20010501 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT IN THE FWD CABIN FOUND CORROSION AT FLOOR TRACK NUMBER 4, BETWEEN STA 200 AND 237. REMOVED AND REP LACED PORTION OF CHAIR TRACK, AS REQUIRED, PER SRM 53-21-037. TREATED AND PRIMED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001051500067 20010515 00067 WP 2001 5 15 ZW0A0101108 1 20010501 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT IN THE AFT CABIN AND CARGO COMPT, CABIN FLOOR MEMBRANE WAS CORRODED AT STA 1250, LBL 51. REMOVED C ORRODED AREA AND REPAIRED PER SRM 53-01, FIG 4. 2 L 7 2 4F A6WE 2001051500068 20010515 00068 WP 2001 5 15 ZW0A0101109 1 20010502 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT CORRODED AT STA 160 TO 200, RBL 5, RBL 43 AND RBL 53. INSTALLED NEW SUPP ORTS PER SPM 6-70-01 AND SRM 51-30. 2 L 7 2 4F A6WE 2001051500069 20010515 00069 WP 2001 5 15 ZW0A0101110 1 20010502 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT CORRODED AT STA 148 TO 160 RBL 7, STA 160 LBL 5 TO RBL 5, STA 200 LBL 9 T O RBL 49, AND STA 180 RBL 9 TO 43. INSTALLED NEW SUPPORTS PER SPM 6-70-01 AND SRM 51-30. 2 L 7 2 4F A6WE 2001051500070 20010515 00070 WP 2001 5 15 ZW0A0101111 1 20010502 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT CABIN FLOOR TRACK NUMBER 5 WAS CORRODED BETWEEN STA 200 AND 246. REPLACED TRACK PER SRM 53-05, FIG 4F. 2 L 7 2 4F A6WE 2001051500071 20010515 00071 WP 2001 5 15 ZW0A0101112 1 20010502 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT FOUND CABIN FLOOR MEMBRANE CORRODED AT STA 151, RBL 5. REPAIRED PER SRM 53-01, FIG 4. 2 L 7 2 4F A6WE 2001051500072 20010515 00072 WP 2001 5 15 ZW0A0101113 1 20010503 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT IN RT FWD CABIN BETWEEN STA 218 AND 237, RBL 58 INCHES, MEMBRANE HAD CORRODED AND CRACKED AT NUMBER 6 FLOOR TRACK. SHOP FABRICATED NEW MEMBRANE AND INSTALLED PER SPM 6-70-01, PAGE 3 PARAGRAPH 4-B-2. 2 L 7 2 4F A6WE 2001051500073 20010515 00073 NM 2001 5 15 AWXA0001693 1 20010503 A 2910 NAS16128 O-RING MESSIER AIRBUS A319 A319132 NM HYD SYSTEM DAMAGED A AWXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 658AW H0919 1110 SJC - EMERGENCY LANDING - 4/27/01 - FLT 285 - EN ROUTE FROM PHX TO SJC THE CREW REC''D AN ECAM MSG HYD Y RSVR LO LVL FOL LOWED BY HYD Y ENG 2 PUMP LO PR. PERFORMED ECAM ACTIONS AND CONTINUED TO LANDING IN SJC. IN SJC MAINTENANCE FOUND THE CENTER FITTING ON AUTOMATIC BRAKE SELECTOR VALVE LEAKING. REMOVED THE FITTING AND REPLACED THE O-RING; THE HYD RESERVOI R WAS SERVICED AND OPERATIONAL AND LEAK CHECKS WERE GOOD. 2 L 7 2 4F RT A28NM 2001051500074 20010515 00074 NM 2001 5 15 AWXA0001450 1 20010301 A 5320 PLATE BOEING 737 7373S3 1384711 NM CARGO BAY DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 PERFORMED WELD REPAIRS TO AFT CARGO CENTER AND FWD SCUFF PLATES IAW ENG RESPONSES, 2/24/01 AND 2/27/01. REMOVED AND REI NSTALLED SCUFF PLATES, SIDEWALLS, FLOOR PANELS, FLOOR SUPPORT, (AFT CARGO) IAW SRM 51-40-02; PRESSURE CHECKED REPAIR ARE A. 2 L 7 2 4F RT A16WE 2001051500075 20010515 00075 WP 2001 5 15 CALA0100438 1 20010503 A 5320 59360381 CHANNEL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 MID BAG BIN DOOR JAMB Z CHANNEL HAS CORROSION AROUND HI-SHEARS. INSTALLED DOUBLER AND SPACER PER SRM 53-05 FIG 63. 2 L 7 2 4F A6WE 2001051500076 20010515 00076 WP 2001 5 15 CALA0100439 1 20010504 A 3350 MISC060 BATTERY DOUG DC9 DC982 3022082 WP L1 DOOR DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 477AC 48062 FORWARD ENTRANCE DOOR PORTABLE EMERGENCY LIGHT INOP AND WILL NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PAC K PER MM 33-53-00. 2 L 7 2 4F A6WE 2001051500077 20010515 00077 NM 2001 5 15 CALA0100440 1 20010503 A 5347 1A0870130 SEAT TRACK BOEING 737 737524 1384721 NM COCKPIT WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59630 27534 SEAT TRACK AFT INBOARD FIRST OFFICER SEAT WORN. REMOVED AND REPLACED SEAT TRACK PER MM 25-11-11. 2 L 7 2 4F RT A16WE 2001051500078 20010515 00078 NM 2001 5 15 CALA0100441 1 20010503 A 5320 52932222T12000 FLOOR SUPPORT BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59630 27534 Z-FLOOR SUPPORT STATION 992.5 RBL 37 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-10-02 AND 53-60-51. 2 L 7 2 4F RT A16WE 2001051500085 20010515 00085 EA 2001 5 15 COMA0160365 1 20010426 A 5320 6013600130 ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 929CA 17304 7035 THE FRAME AT FS 640 HAS A CRACKED ANGLE ON THE RIGHT SIDE AT THE ENGINE SUPPORT AREA. REMOVED CRACKED ANGLE (P/N 601-36 001-30) AND INSTALLED A NEW ANGLE (P/N 601-36001-30) IAW WVAC EO 601R-53-2390. 2 L 7 2 4F RT A21EA 2001051500086 20010515 00086 EA 2001 5 15 COMA0160366 1 20010430 A 5530 600210617 BUSHING CNDAIR CL600 CL6002B19 EA VERTICAL STAB SCORED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 929CA 17304 7035 LEFT AND RIGHT VERTICAL STABILIZER BUSHINGS ARE MIGRATED. REMOVED AND REPLACED LT AND RT VERTICAL STABILIZER BUSHINGS I AW WVAC EO 601R-55-2429. 2 L 7 2 4F RT A21EA 2001051500087 20010515 00087 EA 2001 5 15 COMA0160367 1 20010501 A 5753 601R1430354 VANE CNDAIR CL600 CL6002B19 EA LT & RT FLAPS CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 798CA 7348 FOUND CHAFING ON RT AND LT INBOARD FLAP VANE INBOARD END TO EXCEED ALLOWABLE LIMITS. REPAIRED RT AND LT INBOARD FLAP VA NE INBOARD END IAW WVAC EO 601R-57-2433. 2 L 7 2 4F RT A21EA 2001051500089 20010515 00089 WP 2001 5 15 IXXA0100023 1 20010503 A 3260 WARNING SYSTEM DOUG DC8 DC871F 302199D WP COCKPIT MALFUNCTIONED A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 826BX 45998 EN ROUTE FROM SJC TO TOL, THE LANDING GEAR DOOR WARNING LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE FLIGHT CR EW CYCLED THE LANDING GEAR AND THE GEAR DOOR WARNING LIGHT EXTINGUISHED. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE LANDING GEAR INDICATION SYSTEM WITH NO DISCREPANCIES NOTED. MAINTENANCE PLACED THE INDICATION SYSTEM ON DEFERRAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2001051500090 20010515 00090 CE 2001 5 15 20010515AP006 1 20010504 A 2752 DRIVE SHAFT CESSNA 421 421C 2076016 CE TE FLAP ACTUATOR SHEARED E BXSA O OTHER F FLT CONT AFFECTED AP APPROACH 1 EA 09 60RR 1193 QR43461 421C0885 FLAPS STARTED TO EXTEND, THEN FAILED TO EXTEND ANY FURTHER. FOUND THE FLAP ACTUATOR SPROCKET DRIVE SHAFT SHEARED WHERE IT COMES OUT OF THE GEARBOX. IT APPEARS THAT IT SHEARED BECAUSE THE INNER SPROCKET PIN HOLE IN THE DRIVE SHAFT HAD BEEN CROSS DRILLED. THE FIRST HOLE APPEARS TO HAVE BEEN DRILLED OFF CENTER, SO ANOTHER HOLE HAD BEEN DRILLED AT 90° TO THE FIRST HOLE THUS WEAKENING THE SHAFT. 1 L 7 2 3O A7CE 2001051500094 20010515 00094 NM 2001 5 15 SABA010012 1 20010502 A 3350 82425110001 LIGHT DHAV DHC8 DHC8103 1386005 NM CABIN INOPERATIVE A SABA K NONE L NO TEST CR CRUISE 1 SO 33 801WP 086 AIRCRAFT 801 ON FLIGHT FROM PGV TO CLT. DURING CRUISE BEFORE ARRIVING IN CLT FOUR RED FLOOR EMERGENCY ESCAPE PATH LIGHT S WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHTING STRIP. OPS CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001051500095 20010515 00095 NE 2001 5 15 NACA20010019 2 20010502 A 7411 10553991C COIL PWA CB3 DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE NR 5 CYLINDER SHORTED A NACA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 43872 36434 533294 36434 NR 1 ENGINE SHUTDOWN AT 2224Z DUE TO 1 BACKFIRE AND LOW COMPRESSION PATTERN ON CYLINDER NR 5. REPLACED NR 5 CYLINDER CO IL, CHECKED PLUGS, LEADS, AND Y-LEAD (ALL GOOD). NORMAL ANALYZER ON RUNNUP, COMPRESSION CHECK 70/80. 2 L 7 4 4R 4 R 6A3 5E8 2001051500096 20010515 00096 EU 2001 5 15 A6WA200100032 1 20010502 A 2751 FCU BAG BAE146 BAE146300A 1500267 EU FLAPS MALFUNCTIONED A A6WA K NONE F F FLT CONT AFFECTED FLT CONT AFFECTED CL CLIMB 1 GL 31 615AW E3141 ON CLIMBOUT FLAPS STUCK AT 24 DEGREES ON RETRACTION AND FLAP INOP LIGHT ILLUMINATED. MAINTENANCE RESET FLAP COMPUTER. 2 H 7 4 4F RT A49EU 2001051500097 20010515 00097 2001 5 15 PNSA010401 4 20010424 A 6122 GOVERNOR SWRNGN SA227 SA227AC 8780603 SW RT PROP OUT OF ADJ A PNSA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 AL 03 2708D AC713B RIGHT ENGINE POWER WAS LOW. ABORTED TAKEOFF. RETURNED TO BLOCK. ADJUSTED PROP GOVERNOR. OPS CHECK OK. 2 L 7 2 4T RT A8SW 2001051500098 20010515 00098 EA 2001 5 15 SWIA972545 1 20010503 A 3030 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT FALSE ACTIVATION A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 409SW 7056 AT APPROXIMATELY 500 FT AGL L STATIC HEAT CAUTION MESSAGE APPEARED. POWERED DOWN A/C. ALL PROBE HEAT FUNCTIONAL CHECK OK FOLLOWING POWER UP IAW GMPM VOL 1. 2 L 7 2 4F RT A21EA 2001051500099 20010515 00099 SO 2001 5 15 SWIA972546 1 20010429 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT FLAP FAILED A SWIA O OTHER F FLT CONT AFFECTED LD LANDING 1 NM 07 190SW 120050 INBOARD FLAPS FAILED TO RETRACT UPON LANDING. REMOVE AND REPLACE LEFT INBOARD FLAP ACTUATOR IAW MM 27-50-00. REPLACED BOTH INBOARD ROLLERS AND MOVEABLE OUTBOARD ROLLER ON LEFT INBOARD FLAP IAW 27-50-12. OPS AND LEAK CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001051500100 20010515 00100 EU 2001 5 15 MALA010429 1 20010427 A 3250 CONNECTOR SAAB SF340 340B 7860101 EU NLG STEERING DIRTY A MALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 GL 15 447XJ 447 NOSE WHEEL STEERING LOCKS UP INTERMITTENTLY. WORKS FINE AND THEN TILLER LOCKS IN THE LAST POSITION. UNABLE TO TURN LEF T OR RIGHT. FREE CASTERING WORKS OK. AIR RETURN TO DTW. MAINTENANCE INSPECTED AND CLEANED ELECTRICAL CONNECTOR. OPS CHECK GOOD OF STEERING SYSTEM IAW SF340AMM. 2 L 7 2 4T RT A52EU 2001051500101 20010515 00101 EU 2001 5 15 MALA010430 1 20010428 A 3250 SWITCH SAAB SF340 340B 7860101 EU NLG STEERING INOPERATIVE A MALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 15 447XJ 447 NOSE WHEEL STEERING INOP. RETURN TO GATE. MAINTENANCE REPLACED GROUND HANDLING SWITCH, 12GD RELAY, SERVO MOTOR, SWITCH 5GH AND SWITCH 3GH. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2001051500102 20010515 00102 EU 2001 5 15 MALA010431 1 20010429 A 2613 SENSOR SAAB SF340 340B 7860101 EU ENGINE FAULTY A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 412XJ 340B412 AFTER TAKEOFF FROM DTW, FLIGHT 2755, SELECTED THE LP BLEED ON AND HAD A LT DUCT OVERTEMP LIGHT WITH A LT BLD CIGED. OR H COMPLETED. RESET AND DUCT OVERTEMP LT RE-ILLUMINATED. L HP WAS OFF AS WELL AS TEMP SELECT IN AUTO POSITION. AIR RET URN TO DTW. MAINTENANCE REPLACED TEMP SENSOR. 2 L 7 2 4T RT A52EU 2001051500104 20010515 00104 EU 2001 5 15 MALA010434 1 20010501 A 2424 51539007B GCU SAAB SF340 SF340A 7850100 EU LT ENGINE DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 991XJ 091 LEFT DC GEN FAILED INFLIGHT, AIR RETURN TO DTW FOR LEFT DC GENERATOR OFFLINE. MAINTENANCE REPLACED LEFT DC GCU P/N 5153 9-007B, S/N ON 98658 IAW SAAB 340 AMM CHAP 24-31. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2001051500105 20010515 00105 EU 2001 5 15 MALA010435 1 20010502 A 3010 2500761 ANTI-ICE VALVE BAC 146 AVRO146RJ85A 1500097 EU RT WING FAILED A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 506XJ E2314 DURING FLIGHT NR 3518 OUT OF MSP, RIGHT OUTER WING ANTI-ICE VALVE IS FAILED SHUT. AIR RETURN TO MSP. MAINTENANCE REPLA CED RIGHT OUTER ANTI-ICE VALVE P/N HTE 250076-1, S/N ON FR158BA, S/N OFF FRTR074AV. OPS AND LEAK CHECK GOOD IAW AMM 30- 11-17-201. 2 H 7 4 4F RT A49EU 2001051500106 20010515 00106 SW 2001 5 15 PNSA010403 1 20010417 A 2435 230790001 STARTER GEN SWRNGN SA227 SA227AC 8780603 SW ENGINE FAILED A PNSA K NONE O OTHER TX TAXI/GRND HDL 1 AL 03 2708D 151 AC713B ENGINE WOULD NOT START. RIGHT STARTER FAILED. REPLACED STARTER. 2 L 7 2 4T RT A8SW 2001051500107 20010515 00107 EA 2001 5 15 JBXA000278 1 20010503 A 4990 160366 OIL COOLER CNDAIR CL600 CL6002B19 EA APU DEFECTIVE A JBXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 05 584ML 7330 IDG 2 MESSAGE APPEARED IN FLIGHT. APU OIL TEMP MESSAGE APPEARED IN FLIGHT. A/C RETURNED TO RDU. REPAIRED WIRE AT IDG OIL TEMP BULB CANNON PLUG PIN B IAW CL-65 WIRING MANUAL 20-00-00. OPS CHECK GOOD AT THIS TIME. REMOVED AND REPLACED AP U OIL COOLER ASSY LEAK CHECK AND OPERATIONAL CHECK GOOD IAW 49-91-07. A/C RETURNED TO SERVICE. NO FURTHER PROBLEMS. 2 L 7 2 4F RT A21EA 2001051500111 20010515 00111 2001 5 15 RAIA00105004 4 20010502 A 3417 7000700967 ADC JETAIR JETSTM JETSTM4101 1500501 EU E/E BAY FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 558HK 13104 1981 41071 5364-RIC-LEFT ALTIMETER FAILED DURING CLIMB, AIRCRAFT RETURNED FROM FLIGHT. MAINTENANCE INSPECTED AND REPLACED LEFT AIR DATA COMPUTER. 2 L 7 2 4T RT A41NM 2001051500112 20010515 00112 GL 2001 5 15 RAIA00105005 2 20010503 A 7200 AE3007A ENGINE EMB 145 EMB145 SO ALLSN AE300 AE3007A GL LT ENGINE OVERTEMP A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 805HK 4655 145096 310146 5267-MEM- ON TAKEOFF, LEFT ENGINE ITT REACHED 924, AND FLASHED RED, THROTTLE VERIFIED IN DETENT. MAINTENANCE INSPECTED AND REPLACED LEFT ENGINE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001051500113 20010515 00113 NM 2001 5 15 C1HA200192003 1 20010423 A 3232 CONNECTOR BOEING 727 727121C 1384044 NM DOOR ACTUATOR DIRTY A C1HA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 292AS 21458 AFTER GEAR RETRACT LEFT MLG DOOR ANNUNCIATOR ILLUMINATED. CYCLED GEAR LIGHT WENT OUT. CLEANED CANNON PLUG ON DOOR ACTU ATOR. 2 L 7 3 4F A3WE 2001051500114 20010515 00114 NM 2001 5 15 C1HA200181003 1 20010423 A 2197 WIRE BOEING 727 7272S7 138407Z NM CONTROL VALVE CHAFED A C1HA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 681CA 22020 AIRCRAFT PRESSURIZATION FAILED IN ALL MODES AIR RETURN. FOUND CHAFED WIRE ON RT PACK FLOW CONTROL VALVE. REPAIRED WIRE , OPS CHECKED NORMAL. 2 L 7 3 4F A3WE 2001051500115 20010515 00115 NE 2001 5 15 C1HA200184004 2 20010419 A 7230 JT8D17 ENGINE BOEING 727 7272S7 138407Z NM PWA JT8 JT8D17 52049 NE NR 2 ENGINE STALLED A C1HA K NONE R PARTIAL RPM/PWR LOSS DE DESCENT 1 GL 15 684CA 22491 688298 ENG NR 2 COMPRESSOR STALL DURING POWER REDUCTION ON DESCENT FROM FL350 AT APPROX 1.8-1.7 EPR. REMOVED AND REPLACED NR 2 ENGINE. 2 L 7 3 4F 4 F A3WE E2EA 2001051500116 20010515 00116 NM 2001 5 15 C1HA200184005 1 20010430 A 2611 WIRE BOEING 727 7272S7 138407Z NM SMOKE DETECTOR LOOSE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 684CA 22491 SMOKE DETECTOR INOP IN AFT LEFT LAV. SECURED LOOSE WIRE CHECKS GOOD. 2 L 7 3 4F A3WE 2001051500117 20010515 00117 NM 2001 5 15 C1HA200185004 1 20010423 A 2120 SMOKE BOEING 727 7272S7 138407Z NM CABIN DETECTED A C1HA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 685CA 22492 ON PUSHBACK, BURNING SMELL NOTED IN MID CABIN. INSPECTED ALL ELECTRICAL WIRING IN MID CABIN, INSPECTED GASPER FAN. NO DEFECTS NOTED, ALL SYSTEMS OPERABLE. OK FOR SERVICE. 2 L 7 3 4F A3WE 2001051500121 20010515 00121 NM 2001 5 15 C1HA200196002 1 20010426 A 3350 1000677 BATTERY PACK BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 696CA 22574 L-1 DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT BATTERY PACK. 2 L 7 3 4F RT A3WE 2001051500122 20010515 00122 NM 2001 5 15 C1HA200197002 1 20010424 A 2421 976J5981 GENERATOR BOEING 727 727270 138408P NM NR 3 ENGINE FAILED A C1HA D RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 697CA 23052 UPON TAKING RUNWAY FOR DEPARTURE NR 2 GENERATOR GB LIGHT TRIP. UNABLE TO RESET. DISCONNECTED CSD, RETURNED TO GATE. R EMOVED AND REPLACED NR 2 GENERATO, OPS CHECKED NORMAL. 2 L 7 3 4F RT A3WE 2001051500123 20010515 00123 NM 2001 5 15 C1HA200193004 1 20010502 A 7711 106073710 TRANSMITTER BOEING 727 727212 138407G NM NR 1 ENGINE FAILED A C1HA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 15 293AS 21348 NR 1 EPR GAUGE INOP AT TAKEOFF. ABORTED TAKEOFF 70KIAS. REMOVED AND REPLACED EPR TRANSMITTER, OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2001051500124 20010515 00124 SO 2001 5 15 LR7A01031 1 20010504 A 5310 ATTACH ANGLE LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 592 4698 DURING SCHEDULED B3 INSPECTION PER JOB HB0505 FOUND FS 846 RT VERTICAL WEB SKIN ATTACH FLANGE CRACKED AT ELEPHANT EAR AT TACH, WL 195, RBL 61. REPAIRED IAW LAC MEA 382-53-01-023 AND SRM SMP 583-50-10 . 2 H 7 4 4T A1SO 2001051500125 20010515 00125 SO 2001 5 15 LR7A01032 1 20010504 A 5230 SKIN LKHEED 382 382G 526414U SO CARGO DOOR DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 592 4698 DURING SCHEDULED B3 INSPECTION PER JOB HB0505 FOUND FS 867 CARGO DOOR SKIN PREVIOUS REPAIR WITH INSUFFICIENT NUMBER OF F ASTENERS AT RBL 40, WL 170. REMOVED PREVIOUS REPAIR AND INSTALLED NEW REPAIR IAW SRM SMP 583-51-140-12. 2 H 7 4 4T A1SO 2001051500126 20010515 00126 NM 2001 5 15 C1HA200196003 1 20010504 A 5350 PLATE BOEING 727 7272J4 1384006 NM FAIRING LOOSE A C1HA O OTHER E VIBRATION/BUFFET CR CRUISE 1 GL 15 696CA 22574 AT FL 290 AIRSPEED ABOVE 290KTS AIRFRAME HAS INTERMITTANT STRONG VIBRATION DOES NOT CHANGE WITH POWER SETTINGS. INSPECT ED AIRCRAFT AND FOUND LOOSE BODY TO WING FAIRING SEAL GUIDE PLATE. TIGHTENED AS REQUIRED. TEST FLEW A/C, NO DEFECTS NO TED. 2 L 7 3 4F RT A3WE 2001051500129 20010515 00129 NM 2001 5 15 SABA010013 1 20010507 A 3350 824251001 HARNESS DHAV DHC8 DHC8102 2809003 NM CABIN FAULTY A SABA K NONE O OTHER CR CRUISE 1 SO 33 841PH 82 AIRCRAFT 841 ON FLIGHT 5190 FROM AGS TO CLT. DURING CRUISE FLIGHT FOUR RED FLOOR EVACUATION LIGHT BULBS BECAME DIM AND UNUSABLE. NO INFLIGHT EMERGENCY WAS DECLARED. AIRCRAFT LANDED IN CLT WITH NO OTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED THE EVACUATION LIGHT WIRING HARNESS. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001051500130 20010515 00130 GL 2001 5 15 PNSA010501 3 20010505 A 6110 R321 O-RING SWRNGN SA227 SA227AC 8780603 SW ROTOL R321 R321482F8 GL RT PROP CUT A PNSA E A ENGINE SHUTDOWN UNSCHED LANDING B K J SMOKE/FUMES/ODORS/SPARKS FLUID LOSS WARNING INDICATION CL CLIMB 1 AL 03 640PA 11267 4856 AC759B DRG233481 ON CLIMBOUT A SLIGHT ODOR OF SMOKE WAS NOTICED IN THE CABIN. STARTED TO RETURN TO BASE WHEN RT OIL PRESSURE LOW LIGHT I LLUMINATED. THIS WAS CONFIRMED BY THE OIL PRESSURE INDICATOR. RT ENGINE WAS SECURED, AN UNEVENTFUL LANDING. FOUND PRO PELLER PISTON SEAL O-RING CUT AND ROLLED A LARGE QUANTITY OF OIL WAS FOUND ON COWLING AND INLET TO ENGINE. REPLACED O-R ING LEAK AND OPERATIONAL CHECK OK. 2 L 7 2 4T RT A8SW 6 C P61GL 2001060700035 20010607 00035 CE 2001 6 7 GLBA2001091 1 20010504 A 2131 13037432 CONTROLLER BEECH 1900 1900D 1154162 CE CABIN PRESSURE FAILED A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 240GL 6512 UE240 AIRCRAFT WILL NOT HOLD CABIN ALTITUDE (PRESSURIZATION). REPLACED PRESSURE CONTROLLER. 2 L 7 2 4T RT A24CE 2001051500131 20010515 00131 CE 2001 5 15 GLBA2001092 1 20010505 A 2841 CONNECTOR BEECH 1900 1900D 1154162 CE INDICATOR LOOSE A GLBA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 01 226GL UE226 LEFT FUEL FLOW/QUANTITY FLUX, INSPECTED FOUND LOOSE CANNON PLUG ON FUEL QUANTITY INDICATOR, OPS CHECKED SYSTEM SATISFACT ORY. 2 L 7 2 4T RT A24CE 2001051500133 20010515 00133 NM 2001 5 15 ZW0A0101201 1 20010505 A 3350 6100928 LIGHT BOEING 767 767330 NM CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 691LF 25137 THE EGRESS LIGHTS WERE INOPERATIVE AT SEAT ROW 1D, 5B, AND 16B. REPLACED THE LAMP AT EACH LOCATION. CHECK-C 9-23-00 LA X. 2 L 7 2 4F RT A1NM 2001051500134 20010515 00134 WP 2001 5 15 ZW0A0101202 1 20010501 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 9616G 53563 SEVERAL OVERHEAD EMERGENCY LIGHTS, THE TAIL CONE SLIDE LIGHT, AND MID CABIN EGRESS LIGHTS WERE INOPERATIVE. REPLACED LA MPS P/N 1315 FOR OVERHEAD EMERGENCY LIGHTS, REPLACED BATTERY PACK P/N 60-0304-512B FOR TAIL CONE SLIDE LIGHT, AND SECURE D CONNECTORS AT ROWS 12 AND 25 FOR EGRESS LIGHTS. CHECK-C 8-18-00 JFK. 2 L 7 2 4F RT A6WE 2001051500135 20010515 00135 WP 2001 5 15 ZW0A0101203 1 20010504 A 3350 2232 LIGHT DOUG DC9 DC982 3022082 WP TAIL INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 952U 49266 THE TAIL CONE SLIDE LIGHT AND TAIL CONE EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE LAMPS. CHECK-C 3-12-01 STL. 2 L 7 2 4F A6WE 2001051500136 20010515 00136 WP 2001 5 15 ZW0A0101204 1 20010506 A 3350 CANAC12A COVER DOUG DC9 DC983 3022083 WP CABIN MISSING A ZW0A K NONE O OTHER NR NOT REPORTED 1 CE 13 9405T 53141 THE COVER FOR THE EMERGENCY EXIT SIGN AT ROW 21 SEAT F WAS MISSING. INSTALLED THE COVER FOR THE RT SIDE FWD OVERWING EX IT SIGN. CHECK-C 10-23-00 STL. 2 L 7 2 4F RT A6WE 2001051500137 20010515 00137 WP 2001 5 15 ZW0A0101205 1 20010504 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT IN THE FWD CABIN, THE FLOOR MEMBRANE WAS CORRODED AT STA 160 TO 200, RBL 53 TO RBL 9. REPLACED MEM BRANE PER SPM 6-20-1 AND SRM 53-30-2. 2 L 7 2 4F A6WE 2001051500138 20010515 00138 WP 2001 5 15 ARWA0010501 1 20010504 A 2720 CONNECTOR DOUG DC8 DC863F 302198F WP RUDDER FAULTY A ARWA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 19 661AV 45969 RUDDER HARD OVER TO THE RIGHT ON TAKEOFF AND STAYED. RUDDER BACK FULL DEFLECTION TO LEFT. CAPTAIN REPORT YAW DISENGAGE , OVERWEIGHT LANDING ACCOMPLISHED WITHOUT INCIDENT. CORRECTIVE ACTION: REMOVED AND REPLACED RUDDER HYDRAULIC ACTUATOR PL UG P10-975, ALSO REPLACED WIRES TO SAME CONNECTOR IAW MM 20-50-1. PERFORMED RUDDER ADJUSTMENT AND TEST IAW MM 27-20-0 AN D YAW CHANNEL COMPUTER IAW MM 22-11-1, BOTH TEST NORMAL.PERFORMED OVERWEIGHT LANDING INSPECTION IAW ARROW AIR FORM 6372 NO DISCREPANCIES NOTED. 2 L 7 4 4F 4A25 2001051500139 20010515 00139 WP 2001 5 15 IXXA0100019 1 20010215 A 5330 SKIN DOUG DC8 DC862 3021970 WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 799AL 68532 1249 45922 DURING ROUTINE B-CHECK INSPECTION, A CRACK WAS DETECTED ON THE FUSELAGE EXTERNAL PLATING AT FUSELAGE STATION 242, BETWEE N LONGERONS 28L AND 29L. REPAIR ACCOMPLISHED STOP DRILLING CRACK. FABRICATION AND INSTALLATION A REPAIR DOUBLER IN ACC ORDANCE WITH DACO STRUCTURAL REPAIR MANUAL 51-1-20 AND 53-2-0. 2 L 7 4 4F 4A25 2001051500140 20010515 00140 WP 2001 5 15 IXXA0100020 1 20010215 A 5210 SKIN DOUG DC8 DC862 3021970 WP PAX DOOR CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 799AL 68532 1249 45922 DURING ROUTINE B-CHECK INSPECTION, A CRACK WAS DETECTED ON THE CREW ENTRY DOOR SKIN LOWER CORNER AT FUSELAGE STATION 241 . REPAIR ACCOMPLISHED STOP DRILLING CRACK, FABRICATION AND INSTALLATION A REPAIR DOUBLER IN ACCORDANCE WITH DACO STRUCT URAL REPAIR MANUAL 52-2-0, 51-1-8 AND 51-1-21. 2 L 7 4 4F 4A25 2001051500141 20010515 00141 WP 2001 5 15 IXXA0100021 1 20010315 A 5230 PAN DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 79927 2852 46065 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE LOWER C-PIT DOOR CORNER PAN. REPAIRED ACCOMPLISHED REMOV AL OF DAMAGED AREA, FABRICATION AND INSTALLATION A NEW PAN AND SPLICE PLATES IN ACCORDANCE WITH DAC DRAWINGS 5707387-501 , 5074349-7 AND DACO STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2001051500142 20010515 00142 WP 2001 5 15 ANCF200100007 1 20010505 A 5270 TARGET DOUG DC9 DC983 3022083 WP CARGO DOOR OUT OF POSITION W ANCF A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 99 593AN 53093 DURING CLIMB FWD CARGO DOOR ANNUNCIATION CAME ON AT FL 29000 FT AND CABIN ALTITUDE CLIMBED 8600 FT, NORMAL SHOULD BE 500 0 FT ACCORDING TO TABLE. AIR TURNBACK PROCEDURE WAS ACCOMPLISHED. TARGET WAS REPOSITIONED ON FWD CARGO DOOR, BITE WAS PERFORMED ON BOTH CONTROLLERS AND NFF. MANUAL PRESSURIZATION WAS ACCOMPLISHED WITH 3 PSI ACCORDING AMM 21-32-00. 2 L 7 2 4F RT A6WE 2001051500143 20010515 00143 WP 2001 5 15 ANCF200100008 1 20010505 A 5230 PRESSURE PANEL DOUG DC9 DC983 3022083 WP CARGO DOOR FAILED W ANCF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 99 593AN 17733 53093 DURING CRUISE FWD CARGO DOOR ANNUNCIATION CAME ON AT FL 270 (CABIN PRESS DIF 7.0). CABIN ALTITUDE KEPT ON INCREASING AN D COULD NOT BE MAINTAINED. RETURNED TO BAQ. THE SYSTEM AND DOOR WERE CHECKED FOR LEAKS, NO LEAKS. SELECTOR CABIN PRES SURE PANEL WAS CHANGED, TEST OK IN ACCORDANCE WITH AMM 21-32-00 PAGE 202-203, 21-00-00 PAGE 516 AND 52-31-00 PAGE 601. 2 L 7 2 4F RT A6WE 2001051500145 20010515 00145 EA 2001 5 15 SWIA972547 1 20010504 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT CRACKED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 417SW 7400 AT FL 330, THE CAPT''S WINDSHIELD SHATTERED. REMOVE AND REPLACE CAPTAIN''S WINDSHIELD IAW MM 56-11-01. PRESSURIZED AC IAW 21-31-00 FOR WINDSHIELD REPLACEMENT. OPS CHECK AND LEAK CHECK GOOD. P/N ON 601R33033-9, S/N ON 980048H7587, S/N OF F 00020H8018. 2 L 7 2 4F 4 F RT A21EA E15NE 2001051500146 20010515 00146 SO 2001 5 15 SWIA972549 1 20010504 A 3233 ACTUATOR EMB 120 EMB120RT SO PWA 118 PW118 NE MLG FAILED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 162CA 120150 LANDING GEAR WOULD NOT EXTEND NORMALLY. PERFORMED GEAR EXTENSION BY ELECTRIC OVERRIDE CHECK LIST IN QRH. ALL EXTENDED NORMALLY. REPLACED MAIN ACTUATING CYLINDER WITH A SERVICEABLE UNIT AND ADJUSTED INBOARD SEQUENCE VALVE ON RIGHT GEAR. ALL WORK DONE PER MM 32-32-00. GEAR RETRACT CHECKS GOOD ON GROUND AT THIS TIME. P/N ON 19595-000-07, S/N ON 617, S/N OFF 528. 2 L 7 2 4T 4 T RT A31SO E20NE 2001051500147 20010515 00147 SO 2001 5 15 SWIA972550 1 20010504 A 3231 SEQUENCE VALVE EMB 120 EMB120RT SO PWA 118 PW118 NE RT MLG DEFECTIVE A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 162CA 120150 EN ROUTE A SYSTEM GREEN LIGHT ON FOR RIGHT MAIN GEAR AFTER LOWERING GEAR HANDLE. ALL SIX DISAGREEMENT LIGHTS ON AND NO ADDITIONAL GREEN LIGHTS. AFTER APPROXIMATELY A 1 MINUTE DELAY, ALL SIX GREEN INDICATIONS. INSPECTED LANDING GEAR FOR D EFECTS FOUND RIGHT INBOARD GEAR DOOR SEQUENCE VALVE TO BE DEFECTIVE. REPLACED RIGHT INBOARD GEAR DOOR SEQUENCE VALVE WI TH SERVICEABLE UNIT. S/N OFF 506, S/N ON 1905. PERFORMED EXTENSIVE FUNCTIONAL CHECK OF LANDING GEAR SYSTEM. ALL FOUND GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001051500148 20010515 00148 NE 2001 5 15 C2XA01IA235 2 20010503 A 7200 ENGINE AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE NR 2 ENGINE DETERIORATED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 42836 200 PCE120869 CRP - DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE NUMBER TWO ENGINE PROPELLER SHAFT APPEARED TO BE LOOSE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NUMBER TWO PROP SHAFT TO BE LOOSE AND THE REDUCTION GEAR BOX CHIP DETE CTOR TO BE CONTAMINATED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ENGINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2001051500149 20010515 00149 2001 5 15 XNA01008 4 20010505 A 3414 INDICATOR AIRBUS 300 A300B4203 3930306 EU COCKPIT INOPERATIVE A TC8A C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 23 473AS 203 TAKEOFF ABORTED. NO AIRSPEED INDICATION ON CAPTAIN A/S INDICATOR. REMOVED AND REPLACED MACH/AIRSPEED INDICATOR. PERFO RMED PITOT OPS AND LEAK CHECK. OPS AND LEAK CHECK NORMAL IAW A300 MM 34-11-40. 2 L 7 2 4F RT A35EU 2001051500150 20010515 00150 EU 2001 5 15 SABA010014 1 20010506 A 6120 8659567 SWITCH BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A SABA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 33 966AE 966 AIRCRAFT 966 ON FLIGHT 5150 FROM SOP TO CLT. DURING TAKEOFF ROLL THE LEFT ENGINE BETA LIGHT CAME ON AT 70 KTS. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WITH NO OTHER PROBLEMS. NO EMERGENCY PROCEDURES WERE USED. MAINTENA NCE REMOVED AND REPLACED THE LEFT ENGINE BETA SWITCH. OPS CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A56EU 2001051500151 20010515 00151 SO 2001 5 15 C2XA01TY092 1 20010505 A 5313 13500400017 STRINGER EMB 135 EMB135ER 3260203 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 19503 145176 TYS DURING A SCHEDULED INSPECTION EXTERNAL STRINGER 19L WAS FOUND GOUGED AT STATION 15721.0. MAINTENANCE ACCOMPLISHED A BLEND REPAIR IAW EMB-GST-1459/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPE CTION. 2 L 7 2 4F RT T00011AT 2001051500152 20010515 00152 WP 2001 5 15 MWEA010683 1 20010507 A 5320 99236663 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 LEFT SIDE CUSP TEE AND CUSP WEB HAVE MODERATE CORROSION, FROM STATION 220 TO 240. BLENDED CORROSION AND CUSP ANGLE, FAB RICATED AND INSTALLED REPAIR CUSP WEB MEMBRANE, LOCATED, DRILLED AND INSTALLED NEW CUSP ANGLE SPLICE, INSTALLED NEW WEB MEMBRANE. 2 L 7 2 4F RT A6WE 2001051500153 20010515 00153 WP 2001 5 15 MWEA010715 1 20010507 A 5330 593600417 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 REWORK PREVIOUS REPAIR AT LOWER FUSELAGE EXTERIOR STATION 775, LONGERON 29 RIGHT TO 29 LEFT. REMOVED PREVIOUS REPAIR DO UBLER, PLUGGED HOLES, REPLACED CRACKED RIVET. 2 L 7 2 4F RT A6WE 2001051500154 20010515 00154 WP 2001 5 15 MWEA010716 1 20010507 A 5330 29524711 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 AFT FUSELAGE SKIN AT STATION 1290 HAS TWO PROTRUDING CREASES AT LONGERON 5 LEFT ONE IS 6 INCHES LONG AND ONE IS 4 INCHES LONG. CUT OUT DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F RT A6WE 2001051500155 20010515 00155 WP 2001 5 15 MWEA010717 1 20010507 A 5347 593054768 SEAT TRACK DOUG DC9 DC981 3022081 WP CABIN DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 HOLE IN NR SEAT TRACK AT STATION 236. REMOVED DAMAGED AREA, INSTALLED SEAT TRACK 3-LIP PLUG REPAIR. 2 L 7 2 4F A6WE 2001051500156 20010515 00156 WP 2001 5 15 MWEA010718 1 20010507 A 5330 5936434127 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 STATION 370-427 RIGHT FUSELAGE SKIN BLEND OUTS AT FORWARD LOWER CARGO DOOR JAMB. FABRICATED AND INSTALLED REPAIR DOUBLE RS. 2 L 7 2 4F A6WE 2001051500157 20010515 00157 WP 2001 5 15 MWEA010719 1 20010507 A 5347 593056677 SEAT TRACK DOUG DC9 DC981 3022081 WP CABIN DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 NR 2 SEAT TRACK AT STATION 1130 HAS A BLEND OUT FOR THE G3 INBOARD LOWER MOUNT FROM THE PREVIOUS AIRCRAFT OWNER AT THE I NBOARD FLANGE. REMOVED DAMAGED SECTION, FABRICATED, FITTED, TRIMMED AND INSTALLED NEW SEAT TRACK SECTION. 2 L 7 2 4F A6WE 2001051500158 20010515 00158 WP 2001 5 15 MWEA010720 1 20010507 A 5330 5936434127 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 STATION 531.5 BETWEEN LONGERON 29 LEFT AND 30 HAS A HOLE LEFT FROM A PREVIOUS ANTENNA INSTALLATION MODIFICATION. CUT OU T DAMAGED AREA ON SKIN, FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001051500159 20010515 00159 WP 2001 5 15 MWEA010722 1 20010507 A 5310 99364543 SHEAR TIE DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 SHEAR TIE AT STATION 731 FROM LONGERON 26 LEFT TO 28 RIGHT HAS CORROSION AND TOOL MARKS. REMOVED AREA OF SHEAR CLIP, DR ILLED, LOCATED AND INSTALLED NEW SHEAR CLIP. 2 L 7 2 4F A6WE 2001051500160 20010515 00160 WP 2001 5 15 MWEA010726 1 20010507 A 5320 991963635 INTERCOSTAL DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 FABRICATE AND INSTALL INTERCOSTAL 9919636-35 AT STATION 1231-1250 LONGERON 9 LEFT. FABRICATED INTERCOSTAL, CLIP, FORWAR D GUSSET, AFT GUSSET, LOCATED AND DRILLED ANGLE, INSTALLED INTERCOSTAL, GUSSETS AND CLIPS. 2 L 7 2 4F A6WE 2001051500161 20010515 00161 WP 2001 5 15 MWEA010728 1 20010507 A 5330 29524711 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 AFT FUSELAGE SKIN AT STATION 1320 HAS TWO PROTRUDING DENTS IN LONGERON 5 LEFT AREA. FABRICATED AND INSTALLED REPAIR DOU BLER. 2 L 7 2 4F A6WE 2001051500162 20010515 00162 WP 2001 5 15 MWEA010731 1 20010507 A 5754 99558382 FITTING DOUG DC9 DC981 3022081 WP L/E SLAT CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 RIGHT NR 2 SLAT OUTBOARD END RIB FITTING CORRODED AT FASTENER HOLE FOR ECCENTRIC BUSHING RETAINERS. BLENDED AREA, FABRI CATED AND INSTALLED REPAIR PLUG. 2 L 7 2 4F A6WE 2001051500163 20010515 00163 WP 2001 5 15 MWEA010732 1 20010507 A 5754 99558381 FITTING DOUG DC9 DC981 3022081 WP L/E SLAT CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 NR 2 SLAT OUTBOARD END RIB FITTING CORRODED, AT FASTENER HOLES FOR ECCENTRIC BUSHING RETAINERS, LEFT SLAT. BLENDED AREA S, FABRICATED AND INSTALLED REPAIR PLUGS. 2 L 7 2 4F A6WE 2001051500164 20010515 00164 WP 2001 5 15 MWEA010734 1 20010507 A 5320 59327311 SPLICE DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 LONGERON 30 SPLICE AT STATION 590 IS CORRODED BEYOND LIMITS. REMOVED SPLICE DRILLED AND INSTALLED NEW LONGERON SPLICE. 2 L 7 2 4F A6WE 2001051500165 20010515 00165 WP 2001 5 15 MWEA010735 1 20010507 A 5313 5936059503 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 LONGERON 26 RIGHT HAS CORROSION AND TOOL MARKS AT FASTENER HOLES STATION 700 - 712. BLENDED CORROSION, REMOVED TOOL MAR KS, REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED LONGERON AND REPAIR SPLICE. 2 L 7 2 4F A6WE 2001051500166 20010515 00166 WP 2001 5 15 MWEA010737 1 20010507 A 5310 99365755 SHEAR TIE DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 SHEAR TIE AT STATION 712 HAS ELONGATED HOLES. REMOVED , DRILLED AND INSTALLED NEW SHEAR TIE. 2 L 7 2 4F A6WE 2001051500167 20010515 00167 WP 2001 5 15 MWEA010738 1 20010507 A 5311 99360733 FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 AFT SIDE OF FRAME 693 LONGERON 30 - 28 RIGHT HAS TOOL MARKS, LIGHT CORROSION AND ELONGATED HOLES. REMOVED TOOL MARKS, R EMOVED DAMAGE, DRILLED AND INSTALLED NEW FRAME. 2 L 7 2 4F A6WE 2001051500168 20010515 00168 WP 2001 5 15 MWEA010739 1 20010507 A 5313 5936051501 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 LONGERON 28 LEFT HAS CORROSION AND TOOL MARKS STATION 655 - 674. REMOVED CORROSION AND TOOL MARKS, REMOVED DAMAGED SECT ION OF LONGERON, TRIMMED DRILLED AND INSTALLED NEW LONGERON. 2 L 7 2 4F A6WE 2001051500169 20010515 00169 EU 2001 5 15 AWXA0001695 1 20010507 A 5270 WARNING LIGHT AIRBUS 320 A320231 3930325 EU COCKPIT ILLUMINATED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 629AW 076 MSP - ABORTED TAKEOFF, THE AFT CARGO LIGHT APPEARED AFTER APPLYING T/O POWER ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED A ND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE DOOR AND OPERATED IT NUMEROUS CYCLES; THE OPERATION AND INDICATIONS WERE NORMAL; NO FURTHER DISCREPANCIES HAVE BEEN REPORTED. AS A FOLLOW UP, THE NEXT DAY TSM PROCEDURE 52-31 -00-810-802 WAS ACCOMPLISHED W/ NO FURTHER FAULTS. ALSO, CHECKED THE ROLLERS, LUBED AND ADJUSTED VENT AFT DOOR. 2 L 7 2 4F RT A28NM 2001051500170 20010515 00170 EU 2001 5 15 AWXA0001697 1 20010507 A 3251 C2473600001 CONTROL UNIT AIRBUS 320 A320232 3930326 EU NLG STEERING INTERMITTENT A AWXA O OTHER J WARNING INDICATION DE DESCENT 1 WP 28 652AW 35336 8553 953 LAS - EMERGENCY LANDING, INBOUND TO LAS THE CREW GOT AN ECAM MSG FOR NOSE WHEEL STEERING FAULT. THE AIRCRAFT MADE AN UN EVENTFUL LANDING IN LAS. IN LAS MAINTENANCE TROUBLESHOT IAW TSM 32-51-810-826 AND FOUND WATER IN CONNECTOR 6GC AT THE N OSE WHEEL STEERING SERVO CONTROL; NO CORROSION WAS PRESENT IN THE CONNECTOR; THE CONNECTOR WAS CLEANED AND FUNCTIONALLY TESTED GOOD. LATER IN PHX THE SAME FAULT WAS REPORTED AND THE NOSE WHEEL STEERING SERVO CONTROL WAS REPLACED IAW AMM 3 2-51-51-401; FUNCTIONAL CHECKS WERE GOOD AND NO FURTHER DISCREPANCIES HAVE BEEN REPORTED. 2 L 7 2 4F RT A28NM 2001051500172 20010515 00172 NM 2001 5 15 0101596305 1 20010418 A 5414 SKIN BOEING 747 747451 1384940 NM PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 665US 23820 DURING H-CHECK FOUND CRACK ON NUMBER ONE PYLON SKIN AT NACELLE STATION 293. REPAIRED PER EA 63-183398. 2 L 7 4 4F RT A20WE 2001051500173 20010515 00173 NM 2001 5 15 HNAA00029 1 20010503 A 3232 CONTROL CABLE DHAV DHC8 DHC8102 2809003 NM MLG DOOR OUT OF RIG A HNAA K NONE J WARNING INDICATION CL CLIMB 1 EA 07 934HA 139 LEFT MLG FWD DOOR OPENED IN FLIGHT AFTER GEAR RETRACTION SEQUENCE WAS COMPLETE. RERIGGED ALTERNATE EXTENSION CABLES FOR LT FWD DOOR ACTUATOR. 2 H 7 2 4T RT A13NM 2001051500174 20010515 00174 WP 2001 5 15 MWEA010740 1 20010505 A 5310 5911412 DOOR FRAME DOUG DC9 DC914 3022034 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 PREVIOUS REPAIR AT FORWARD CARGO JAMB STATION 370 IS CLASSIFIED AS TEMPORARY REPAIR, NEED TO INSTALL PERMANENT REPAIR IA W SRM 53-05 FIGURE 105 AND TELEX MWX-ORD-00-00543H. INSTALLED DOUBLER AND TRIPLER IN PLACE OF OLD TEMPORARY REPAIR, MAK ING IT A PERMANENT REPAIR. 2 L 7 2 4F A6WE 2001051500175 20010515 00175 SO 2001 5 15 C2XA01CL093 1 20010506 A 3350 20131A BATTERY EMB 145 EMB145LR SO CABIN DISCHARGED A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 16976 4178 1339 145171 CLE FLIGHT 3855 THE CREW REPORTED THE FIRST 3 EMERGENCY AISLE PATH LIGHT STRIPS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2001051500176 20010515 00176 WP 2001 5 15 MWEA010741 1 20010508 A 5311 9915558173 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 CRACK ON AFT PRESSURE BULKHEAD FORMER 2R, OUTBOARD CORNER OF FORMER. FABRICATED AND INSTALLED ANGLE REPAIR. 2 L 7 2 4F A6WE 2001051500177 20010515 00177 WP 2001 5 15 MWEA010742 1 20010508 A 5310 99577397 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 CRACK ON SHEAR TIE AT STATION 951 BETWEEN LONGERON 16 AND 15 LEFT. REMOVED, FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F A6WE 2001051500178 20010515 00178 WP 2001 5 15 MWEA010743 1 20010508 A 5310 9918553501 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 CRACK ON SHEAR TIE AROUND FASTENER AT STATION 980 JUST ABOVE LONGERON 16 LEFT. REMOVED CRACKED SHEAR TIE, FABRICATED AN D INSTALLED NEW SHEAR TIE. 2 L 7 2 4F A6WE 2001051500179 20010515 00179 SO 2001 5 15 C2XA01CL094 1 20010504 A 3350 7287580509 LIGHT EMB 145 EMB145ER SO CABIN INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 15941 145035 CLE FLIGHT 3897 THE CREW REPORTED THE EMERGENCY LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT S TRIP AT THE WING EMERGENCY EXIT. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001051500180 20010515 00180 EU 2001 5 15 C2XA01CL095 1 20010504 A 3340 NSA931320050 CIRCUIT BREAKER AEROSP ATR42 ATR42320 8680930 EU COCKPIT BURNED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 15816 105 CLE FLIGHT 3031 THE CREW REPORTED A BURNING SMELL IN THE COCKPIT. MAINTENANCE INSPECTED AND FOUND THE STROBE LIGHT CIRC UIT BREAKER TO BE BURNT. THE BREAKER WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERV ICE. 2 H 7 2 4T RT A53EU 2001051500181 20010515 00181 EU 2001 5 15 MALA010433 1 20010503 A 3297 85106RC84 WIRE SAAB SF340 340B 7860101 EU MLG BROKEN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 590MA 340B181 WHILE COMPLETING EMERGENCY EXTENSION CHECKS FOR THE LANDING GEAR AND SEPARATION BOLT DUAL BRIDGE WIRE CONTINUITY CHECKS FOUND THREE WIRES BROKE GOING TO THE SEPARATION BOLT. SUSPECT THAT IT IS A COMBINATION OF WIRE ROUTING AND THE SHIELDIN G THAT IS SOLDERED ON THE WIRE RUN. THE SOLDER POINT AND ROUTING BEND AREA APPROXIMATELY ONE INCH FROM THE CANNON PLUG. MAINTENANCE REPLACED THE RT SEPARATION BOLT CANNON PLUG P/N 85106RC8-4. CHECKS GOOD AS REQUIRED. 2 L 7 2 4T RT A52EU 2001051500182 20010515 00182 EU 2001 5 15 MALA010436 1 20010503 A 2621 365000071 EXTINGUISHER SAAB SF340 340B 7860101 EU CARGO BAY DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 415XJ 340B415 DURING FLIGHT 3208, CARGO 2 EXTINGUISH LIGHT ILLUMINATED. AIR TURNBACK TO MSP. MAINTENANCE REPLACED NR 2 FIRE EXTINGUI SHER PER TASK CARD 262203, P/N 36500007-1, S/N OFF 2921301, S/N ON 2801421, CARTRIDGE P/N 30903890, S/N OFF 018FM, S/N O N AEN1-7. 2 L 7 2 4T RT A52EU 2001051500183 20010515 00183 EU 2001 5 15 MALA010437 1 20010425 A 2730 7227105712 ATTACH FITTING SAAB SF340 SF340A 7850100 EU ELEVATOR BENT A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 46XJ 046 DURING 4K-INSPECTION IN CWA, MAINTENANCE NOTICED RT I/B FWD ELEVATOR CONTROL CABLE HAS BENT TURNBUCKLE ATTACH FITTING. MX REPLACED RT I/B FWD ELEVATOR CABLE AND TURNBUCKLE ATTACK FITTING (P/N 7227105-712) IAW SF340 AMM 27-31-15, RIGGED ELE VATOR CONTROL. 2 L 7 2 4T RT A52EU 2001051500184 20010515 00184 EU 2001 5 15 MALA010438 1 20010418 A 2710 7227151522 CONTROL CABLE SAAB SF340 SF340A 7850100 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 46XJ 046 DURING 4K-INSPECTION IN CWA, MAINTENANCE FOUND RT O/B AILERON CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED RT O/B AIL ERON CABLE P/N 7227151-522. SECURED AT AILERON O/B BELLCRANK, REQUIRES INSTALLATION ON IDLER END. 2 L 7 2 4T RT A52EU 2001051500185 20010515 00185 EU 2001 5 15 MALA010439 1 20010422 A 2730 7227705644 CONTROL CABLE SAAB SF340 SF340A 7850100 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 46XJ 046 DURING 4K INSPECTION IN CWA, MAINTENANCE FOUND LHOB FWD FUSELAGE ELEVATOR CABLE CHAFED. MAINTENANCE REMOVED AND REPLACE D LT FWD O/B FUSELAGE ELEVATOR CABLE P/N 7227705-644, IAW SAAB AMM 27-31-15. 2 L 7 2 4T RT A52EU 2001051500186 20010515 00186 SW 2001 5 15 20010511SG001 1 20010203 A 2910 AN8324D FITTING FRCHLD SA227 SA227DC 3377521 SW HYD SYSTEM LEAKING A BSAA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 NM 05 850LS DC850B ON SHORT FINAL, THE CREW NOTICED THE RIGHT HYD PRESS LIGHT CAME ON. GEAR WAS ALREADY DOWN AND FLAPS WERE AT FULL. CREW NOTICED FLUCTUATIONS IN HYD PRESSURE. CREW TURNED OFF NOSE WHEEL STEERING. LANDING WAS UNEVENTFUL LT HYD PRESS LIGHT CAME ON JUST BEFORE REACHING THE GATE. CREW SHUT DOWN AIRCRAFT WITH NO FURTHER PROBLEMS. HYDRAULIC LEAK IN LEFT FLAP A CTUATOR AREA. REPLACED BULKHEAD FITTING THAT GOES FROM FLAP HARD LINE TO FLEX LINE IN AFT END OF NACELLE. SERVICED AND BLED HYDRAULIC SYSTEM. HYDRAULIC SYSTEMS OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A18SW 2001051500187 20010515 00187 SW 2001 5 15 20010511SG002 1 20010420 A 2720 2672003014 RUDDER PEDAL SWRNGN SA227 SA227AC 8780603 SW COCKPIT CRACKED A BSAA K NONE O OTHER IN INSP/MAINT 1 NM 05 27465 AC755B MAINTENANCE FOUND PILOTS RIGHT RUDDER PEDAL CRACKED DURING COCKPIT INSPECTION. FATIGUE OR EXCESSIVE FORCE. REPLACED RU DDER PEDAL. (M) 2 L 7 2 4T RT A8SW 2001051500188 20010515 00188 SW 2001 5 15 20010511SG003 1 20010225 A 5270 WARNING LIGHT SWRNGN SA227 SA227AC 8780603 SW COCKPIT FALSE ACTIVATION A BSAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 05 159MC AC728B FOUND CARGO DOOR WARNING LIGHT CAME ON IN FLIGHT DURING CLIMB-OUT AT ABOUT 10,000 FEET MSL. CREW RETURNED TO STATION WI THOUT INCIDENT. INSPECTED CARGO DOOR CLICK-CLACKS, CLEANED AND LUBED SWITCHES, GROUND OPS CHECK GOOD. NO FURTHER PROBL EMS NOTED. (M) 2 L 7 2 4T RT A8SW 2001051500189 20010515 00189 SW 2001 5 15 20010511SG004 1 20010308 A 5270 WARNING SYSTEM FRCHLD SA227 SA227DC 3377521 SW COCKPIT MALFUNCTIONED A BSAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 05 850LS DC850B CARGO DOOR LIGHT CAME ON DURING CLIMB-OUT, CREW RETURNED TO STATION, LIGHT WENT OUT ON LANDING. DOOR WAS OPENED AND CLO SED MULTIPLE TIMES, LATCHES AND SWITCHES WERE INSPECTED, SYSTEM OPS CHECKED GOOD. NO FURTHER DEFECTS REPORTED. (M) 2 L 7 2 4T RT A18SW 2001051500190 20010515 00190 SW 2001 5 15 20010511SG005 1 20010402 A 5610 2621126008 WINDOW FRCHLD SA227 SA227DC 3377521 SW COCKPIT CRACKED A BSAA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 05 853LS DC853B WHILE EN ROUTE TO CO-PILOTS WINDSHIELD INNER PANE FRACTURED. TEH CREW REQUESTED A LOWER ALTITUDE AND DIVERTED TO LAND A T THE NEAREST STATION. THIS WAS MULTIPLE FRACTURES, MOST PIECES ENDING UP NO BIGGER THAN 1 INCH BY 5 INCHES. NO DAMAGE WAS NOTED TO OUTER PANE. THE CABIN DIFFERENTIAL PRESSURE WAS ABOUT 6.8 PSI AT THE TIME OF THE INCIDENT. NO APPARENT C AUSE NOTED. THE OUTER PANE WASN''T DAMAGED IN ANYWAY. THE WINDSHIELD FRAME (FOR THE BROKEN WINDOW) WAS NOT BEN OR SPRU NG. THERE WAS NO EVIDENCE OF OVERHEATING IN THE WINDSHIELD ELEMENT. REMOVED AND REPLACED WINDOW. (M) 2 L 7 2 4T RT A18SW 2001051500191 20010515 00191 SW 2001 5 15 20010511SG006 1 20010324 A 2497 WIRE FRCHLD SA227 SA227DC 3377521 SW COCKPIT OUT OF POSITION A O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 05 854LS DC854B DURING DESCENT, CREW NOTICED RT ESS BUSS PANEL WAS GLOWING, WAS HOT TO THE TOUCH AND HAD A HOT SMELL. CREW LANDED WITHO UT INCIDENT. RT ESS POWER WIRE CONTACTED THE CB PANEL. MAINTENANCE FOUND THE RT ESS POWER WIRE WAS CONTACTING THE CB P ANEL. REPOSITIONED WIRE TO CORRECT POSITION. INSPECTED WIRING, AND SURROUNDING STRUCTURE, NO DAMAGE WAS FOUND. (M) 2 L 7 2 4T RT A18SW 2001051500192 20010515 00192 EA 2001 5 15 UHLA003375 1 20010416 A 3350 OL3071BPEGPL LIGHT DHAV DHC8 DHC8311 1386006 EA CABIN INOPERATIVE A UHLA K NONE L NO TEST IN INSP/MAINT 1 NE 03 804SA 375 DURING OVERNIGHT MAINTENANCE, SEVERAL BULBS NOTED OUT IN THE FORWARD RIGHT EMERGENCY EXIT. REPLACED 4 LAMPS EMERGENCY L IGHTS. OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A13NM 2001051500193 20010515 00193 EA 2001 5 15 UHLA3374 1 20010416 A 3350 OL307BPEGPL LIGHT DHAV DHC8 DHC8311 1386006 EA CABIN INOPERATIVE A UHLA K NONE L NO TEST IN INSP/MAINT 1 NE 03 803SA 221 DURING RON MAINTENANCE, SEVERAL BULBS FOUND INOPERATIVE IN FORWARD RIGHT EMERGENCY EXIT SIGN. REMOVED AND REPLACED LAMP S EMERGENCY LIGHTS. OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A13NM 2001051500194 20010515 00194 NM 2001 5 15 UHLA013408 1 20010423 A 5210 CABLE DHAV DHC8 DHC8301 NM PAX DOOR BROKEN A K NONE O OTHER TX TAXI/GRND HDL 1 NE 03 806SA 279 FLT 256 - LGA-BED - WHEN THE MAIN PASSENGER DOOR WAS OPEN TO DEPLANE THE PASENGERS IN BED. THE PASSENGER DOOR SUPPORT C ABLE SNAPPED. NOBODY WAS HURT, ALL PASSENGERS WERE DEPLANED NORMALLY. MAINTENANCE REMOVED AND REPLACED THE PASSENGER D OOR SUPPORT CABLE. NO OTHER DEFECTS WERE NOTED. OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A13NM 2001051500195 20010515 00195 EU 2001 5 15 20010511SG007 1 20010405 A 2611 PPA110100 SMOKE DETECTOR AIRBUS 320 A320214 EU LAVATORY FAULTY A RYNA K NONE N FALSE WARNING IN INSP/MAINT 1 CE 07 GBVYA 354 SMOKE LAVATORY AND CARGO DETECTOR FAULT ECAM MESSAGE. REMOVED AND REPLACED AFT SMOKE DETECTOR. (M) 2 L 7 2 4F RT A28NM 2001051500196 20010515 00196 NM 2001 5 15 TSAA0133040 1 20010327 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED NR 3 FLOOR PROXIMITY LIGHT ASSEMBLY BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4F A16WE 2001051500197 20010515 00197 NM 2001 5 15 TSAA0133039 1 20010327 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 AFT ENTRY EMERGENCY EXIT IDENTIFIER INOPERATIVE. REPLACED POWER PACK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2001051500198 20010515 00198 NM 2001 5 15 TSAA0133041 1 20010421 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED NR 2 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001051500199 20010515 00199 NM 2001 5 15 AALA20010575 1 20010322 A 3350 P4010051126 MODULE BOEING 727 727227 1384078 NM CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 720AA 20613 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT AT R1 DOOR DIM. REPLACED EMERGENCY EXIT LIGHT MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001051500200 20010515 00200 EU 2001 5 15 AALA20010532 1 20010318 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN FAULTY A K NONE O OTHER IN INSP/MAINT 1 SW 21 1463A 11483 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT FORWARD ROW 11 DIM. REPLACED EMERGENCY EXIT LIGHT WIRE SPLICE AT ROW 11. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001051500201 20010515 00201 NM 2001 5 15 AALA20010626 1 20010326 A 3397 WIRE BOEING 727 727227 1384078 NM LAVATORY DAMAGED A K NONE O OTHER IN INSP/MAINT 1 SW 21 730AA 20737 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT RIGHT SIDE AFT LAVATORY WIRE DAMAGED. REPAIRED EMERGENCY EX IT LIGHT WIRE AT RIGHT SIDE AFT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001051500207 20010515 00207 NM 2001 5 15 AALA20010649 1 20010329 A 2530 4670017 COFFEEMAKER BOEING 767 767223 1385123 NM GALLEY SPARKS A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 21 332AA 22331 LHR - DURING OVERNIGHT MAINTENANCE, AFT GALLEY COFFEEMAKER WHEN FIRST TURNED ON SPARKS APPEARED. REPLACED AFT GALLEY CO FFEEMAKER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001051500208 20010515 00208 EU 2001 5 15 AALA20010756 1 20010409 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7083A 645 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 9C AND 9G INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIG HT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2001051500209 20010515 00209 NM 2001 5 15 AALA20010367 1 20010302 A 3350 TERMINAL BOEING 727 727223 1384074 NM AIRSTAIRS DISCONNECTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 843AA 20984 DFW - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIRS EMERGENCY EXIT LIGHT DIM. RE-SECURED AFT AIRSTAIRS EMERGENCY EXIT END TERMINAL LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001051500210 20010515 00210 NM 2001 5 15 AALA20010385 1 20010307 A 3350 SPLICE BOEING 727 727223 1384074 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 887AA 21526 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT FIRST CLASS INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT SPLI CE AT FIRST CLASS AFT SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001051500211 20010515 00211 NM 2001 5 15 AALA20010468 1 20010312 A 3350 CONNECTOR BOEING 727 727223 1384074 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 869AA 21374 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 17 DIM. REPAIRED EMERGENCY EXIT LIGHT CONNECTOR AT ROW 17. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001051500212 20010515 00212 NM 2001 5 15 AALA20010470 1 20010313 A 3350 SPLICE BOEING 727 727223 1384074 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 849AA 20990 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT IN COACH CLASS INOPERATIVE. REPAIRED EMEREGNCY EXIT LIGHT SPLIC E AT ROW 15 AND 25. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001051500213 20010515 00213 NM 2001 5 15 AALA20010484 1 20010314 A 3350 CONNECTOR BOEING 727 727223 1384074 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 849AA 20990 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 15-22 DIM. REPAIRED EMERGENCY EXIT LIGHT CONNECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001051500214 20010515 00214 EU 2001 5 15 AALA20010469 1 20010313 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN DAMAGED A K NONE L NO TEST IN INSP/MAINT 1 SW 21 1462C 11482 IAH - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 11 INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT R OW 11. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001051500215 20010515 00215 EU 2001 5 15 AALA20010276 1 20010215 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN OUT OF POSITION A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 1403M 11354 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT STRIP NOT SEATED. RE-SEATED EMERGENCY LIGHT STRIP. SYSTEM GRO UND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001051500216 20010515 00216 EU 2001 5 15 AALA20010238 1 20010209 A 3350 CONNECTOR FOKKER F28 F28MK0100 4990807 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1413A 11376 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT FIRST CLASS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONN ECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001051500217 20010515 00217 NM 2001 5 15 AALA20010587 1 20010326 A 3350 P4010051126 MODULE BOEING 727 727227 1384078 NM CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 727AA 20734 IAD - DURING OVERNIGHT MAINTENANCE, OVERWING EMERGENCY EXIT LIGHT DIM. REPLACED EMERGENCY EXIT LIGHT MODULE. SYSTEM GR OUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001051500218 20010515 00218 NM 2001 5 15 AALA20010498 1 20010315 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 731AA 20738 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT RIGHT OVERWING EXIT SIGN DIM. REPLACED EMERGENCY EXIT LIGHT AT RIGHT OVERWING EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001051500219 20010515 00219 NM 2001 5 15 AALA20010524 1 20010316 A 3350 LIGHT BOEING 727 727227 1384078 NM R1 DOOR DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 728AA 20735 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT R1 DOOR DIM. REPLACED EMERGENCY EXIT LIGHT AT R1 DOOR. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001051500220 20010515 00220 EU 2001 5 15 MALA010440 1 20010422 A 2730 7227105712 CONTROL CABLE SAAB SF340 SF340A 7850100 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 46XJ 046 FOUND DURING 4K-CHECK IN CWA, 4FWD LHIB FUSELAGE ELEVATOR CABLE CHAFED. MAINTENANCE REPLACED LHIB FWD FUSELAGE ELEVATOR CABLE P/N 7227105-712 IAW SAAB AMM 27-31-15. SAFTIED TURNBUCKLES AND INSTALL STEER PLUGS AS REQUIRED. 2 L 7 2 4T RT A52EU 2001051500221 20010515 00221 EU 2001 5 15 MALA010441 1 20010419 A 2720 7227105582 CONTROL CABLE SAAB SF340 SF340A 7850100 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 46XJ 046 FOUND DURING 4K-CHECK IN CWA, RT AFT FUSELAGE SINGLE RUDDER CABLE OF CIRCUIT I CHAFED. MAINTENANCE REMOVED AND REPLACED RT AFT FUSELAGE SINGLE RUDDER CABLE OF CIRCUIT I P/N 72277105-582 IAW SAAB AMM 27-21-25. 2 L 7 2 4T RT A52EU 2001051500222 20010515 00222 EU 2001 5 15 MALA010442 1 20010419 A 2720 7227105562 CONTROL CABLE SAAB SF340 SF340A 7850100 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 46XJ 046 FOUND DURING 4K-CHECK, RHOB FUSELAGE DUAL RUDDER CABLE OF CIRCUIT I CHAFED. MAINTENANCE REMOVED AND REPLACED RHOB FUSEL AGE CABLE CIRCUIT I IAW SAAB AMM 27-21-25, P/N 7227105-562. SEE 409 NR 122902 FOR RIGGING. 2 L 7 2 4T RT A52EU 2001051500223 20010515 00223 EU 2001 5 15 MALA010443 1 20010419 A 2720 7227105562 CONTROL CABLE SAAB SF340 SF340A 7850100 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 46XJ 046 FOUND DURING 4K-CHECK IN CWA, LT O/B FUSELAGE DUAL RUDDER CABLE OF CIRCUIT I CHAFED. MAINTENANCE REPLACED LT O/B FUSELA GE DUAL RUDDER CABLE OF CIRCUIT I P/N 7227105-562 IAW SAAB AMM 27-21-25. SEE 409 NR 122902 FOR RIGGING. 2 L 7 2 4T RT A52EU 2001051500224 20010515 00224 NM 2001 5 15 AWXA0001698 1 20010508 A 3230 26501844 CHECK VALVE BOEING 737 7373G7 1384595 NM MLG WW FAILED A AWXA O OTHER J WARNING INDICATION AP APPROACH 1 WP 28 157AW 23779 LAX - 4/30/01 - RT MAIN GEAR GREEN LIGHT DIDN''T ILLUMINATE WITH THE LANDING GEAR HANDLE IN THE DOWN POSITION; WARNING H ORN SOUNDED WITH FLAPS AT 5; THE GEAR WAS CYCLED 3 TIMES WITH NO CHANGE; A MANUAL GEAR EXTENSION WAS PERFORMED AND RESUL TED IN 3 GREEN LIGHTS AND MADE UNEVENTFUL LANDING. THE AIRCRAFT WAS INSPECTED IN LAX AND FOUND OK TO MAINTENANCE FERRY TO PHX. IN PHX DURING TROUBLESHOOTING THE RT MLG UPLOCK ACTUATOR AND MODULAR PKG WERE REPLACED AND DIDN''T FIX PROBLEM. IT WAS DETERMINED THE CHECK VALVE IN LINE WITH MODULAR PKG COULD CAUSE THE PROBLEM IF IT FAILED OPEN. THE CHECK VALVE WAS REPLACED AND THE LANDING OPERATION AND INDICATION RETURNED TO NORMAL. 2 L 7 2 4F RT A16WE 2001051500225 20010515 00225 2001 5 15 AWXA0001699 4 20010508 A 3442 MI585161 RADAR BOEING 737 737277 1384570 NM E/E BAY UNRELIABLE A AWXA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 28 187AW 36492 1862 22654 PHX - AIR TURNBACK, EN ROUTE FROM PHX TO AUS THE WEATHER RADAR BECAME UNRELIABLE; EXCESSIVE TILT UP, 6 DEG TO ELIMINATE GROUND CLUTTER (CLIMB THRU 16000 FT) WINGS LEVEL RADAR POINTS IMAGES TO RIGHT, OCCASIONALLY LEFT EVEN WITH TILT 6 DEG; S TABILIZATION OFF IMPROVES, BUT STILL UNRELIABLE; DUE TO WEATHER IN AUS THE AIRCRAFT RETURNED TO PHX. IN PHX THE PAX WER E PUT ON ANOTHER AIRCRAFT AND THE FLIGHT DEPARTED. THE RADAR WAS PLACED ON MEL 34-15 CONDITION 1 AND ROUTED ON A FLIGHT THAT DIDN''T REQUIRE ITS USE. ON 5/8/01 MAINTENANCE REPLACED THE RADAR RECIEVER/TRANSMITTER UNIT AND FUNCTIONALLY TEST ED GOOD AND THE MEL WAS CLEARED. 2 L 7 2 4F RT A16WE 2001051500226 20010515 00226 NM 2001 5 15 AWXA0001700 1 20010508 A 2934 SLFV1792A SWITCH BOEING 737 7373G7 1384595 NM STBY RESERVOIR DEFECTIVE A AWXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 28 154AW 23776 D: PHX - AIR TURNBACK, APPROX 30 MIN AFTER TAKEOFF THE STANDBY HYDRAULIC LOW QUANTITY LIGHT ILLUMINATED, A AND B SYSTEM QUANTITY WAS NORMAL. THE AIRCRAFT RETURNED TO PHX. MAINTENANCE INSPECTED THE AIRCRAFT FOR LEAKS AND FOUND NONE. THE S TANDBY HYDRAULIC RESEVOIR QUANTITY LOW LEVEL SWITCH WAS REPLACED AND TESTED NORMAL. 2 L 7 2 4F RT A16WE 2001051500227 20010515 00227 NM 2001 5 15 AWXA0001701 1 20010508 A 5312 65163007 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 UPON REMOVAL OF STRAP FOUND .2 INCH CRACK BS 178 WL 210 LBL 4.7. CUTOUT DAMAGED WEB; LOCATED, DRILLED, TRIMMED AND INST ALLED REPAIR DOUBLER AND FILLER IAW SRM 53-10-08 PG 287-298. 2 L 7 2 4F RT A16WE 2001051500228 20010515 00228 NM 2001 5 15 AWXA0001702 1 20010508 A 5312 65163007 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 BS 178 WEB CRACKED .5 INCH WL 206 RBL 1-1.5. CUT OUT DAMAGED WEB; LOCATED, DRILLED, TRIMMED AND INSTALLED REPAIR DOUBLE R AND FILLER IAW SRM 53-10-08 PG 287-298. 2 L 7 2 4F RT A16WE 2001051500229 20010515 00229 NM 2001 5 15 AWXA0001703 1 20010508 A 5312 65163007 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 BS 178 WEB CRACKED .4 INCH WL 198.2-198.6 RBL 6.7 BENEATH STRAP. CUT OUT DAMAGED WEB; LOCATED, DRILLED, TRIMMED AND INS TALLED REPAIR DOUBLER IAW SRM 53-10-08 PG 287-298. 2 L 7 2 4F RT A16WE 2001051500230 20010515 00230 NM 2001 5 15 AWXA0001704 1 20010508 A 5312 65163007 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 HFEC INDICATES .2 INCH CRACK EMANATING FROM BENEATH STRAP BS 178 BLKHD FORWARD SIDE WL 198.6-198.8 RBL 4.7. CUT OUT DAM AGED WEB; LOCATED, DRILLED, TRIMMED AND INSTALLED REPAIR DOUBLER IAW SRM 53-10-08 PG 287-298. 2 L 7 2 4F RT A16WE 2001051500231 20010515 00231 NM 2001 5 15 AWXA0001705 1 20010508 A 5312 65163007 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 HFEC INDICATES .25 INCH CRACK RUNNING HORIZ IN WEB BS 178 WL 207 RBL 11.6-11.75. CUT OUT DAMAGED WEB; LOCATED, DRILLED, TRIMMED AND INSTALLED REPAIR DOUBLER IAW SRM 53-10-08 PG 287-298. 2 L 7 2 4F RT A16WE 2001051500232 20010515 00232 NM 2001 5 15 AWXA0001706 1 20010508 A 5312 65163007 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 HFEC INDICATES .7 INCH CRACK EMANATING FROM BENEATH STRAP BS 178 FWD SIDE WL 201.8-202.1 LBL 4.7. CUT OUT DAMAGED WEB; LOCATED, DRILLED, TRIMMED AND INSTALLED REPAIR DOUBLER IAW SRM 53-10-08 PG 287-298. 2 L 7 2 4F RT A16WE 2001051500233 20010515 00233 NM 2001 5 15 AWXA0001707 1 20010508 A 5312 65163007 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 VISUAL INSPECTION OF BS 178 BLKHD WEB FWD SIDE REVEALED CRACK EMANATING FROM BENEATH STRAP AT WL 198.5-198.8 LBL 4.7. C UT OUT DAMAGED WEB; LOCATED, DRILLED, TRIMMED AND INSTALLED REPAIR DOUBLER IAW SRM 53-10-08 PG 287-298. 2 L 7 2 4F RT A16WE 2001051500234 20010515 00234 WP 2001 5 15 AALA20010744 1 20010328 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7514A 49891 TUL - FOUND CORROSION ON CUSP MEMBRANE FROM STATION 160-200, INBOARD OF FORWARD SERVICE DOOR. INSTALLED ONE DOUBLER PER SRM 53-01-00. (M) 2 L 7 2 4F A6WE 2001051500235 20010515 00235 WP 2001 5 15 AALA20010745 1 20010402 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7514A 49891 TUL - FOUND DENTS IN FUSELAGE SKIN AT STATIONS 238, 234, AND 218 LONGERON 18L AND 20L THERE WERE 2 EXISTING DOUBLER REPA IRS AFT OF STATION 239, THEY WERE CUT OUT WITH OTHER DAMAGE IN AREA. REPAIRED PER ESO 80559 DATED 3-29-2001. INSTALLED DOUBLER AND SKIN PLUG. (M) 2 L 7 2 4F A6WE 2001051500236 20010515 00236 WP 2001 5 15 AALA20010746 1 20010331 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7514A 49891 TUL - FOUND FUSELAGE SKIN CRACKED JUST AFT OF RIVET AT 1474 CANTED FRAME RIGHT SIDE APPROX 14 INCHES ABOVE AIRSTAIRS CUT OUT. INSTALLED DOUBLER PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2001051500237 20010515 00237 WP 2001 5 15 AALA20010747 1 20010402 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7514A 49891 TUL - FOUND CORROSION ON LEFT CUSP FROM 1263-1305. INSTALLED NEW CUSP SHEET FROM 1250-1309 LEFT PER SRM 51-01 AND ESO 8 0559 DATED 3/27/01. (M) 2 L 7 2 4F A6WE 2001051500238 20010515 00238 WP 2001 5 15 AALA20010748 1 20010329 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7514A 49891 TUL - FOUND FUSELAGE SKIN BLENDED DEEP AROUND FASTENER JUST BELOW WINDOW BELT LEFT SIDE OF FUSELAGE APPROX STATION 442. INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M) 2 L 7 2 4F A6WE 2001051500239 20010515 00239 WP 2001 5 15 AALA20010719 1 20010406 A 2613 WARNING SYSTEM DOUG DC9 DC983 3022083 WP COCKPIT ACTIVATED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 595AA 53285 ORD - FLT 1091 - EN ROUTE ORD-DEN, SHORTLY AFTER TAKEOFF DETECTED TAIL COMPARTMENT HIGHT TEMPERATURE LIGHT ILLUMINATE IN COCKPIT. INSPECTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT COMPONENTS. NO DEFECTS FOUND. TIGHTENED TAIL ANTI-ICE VAL VE B-NUT. TIGHTENED LEFT SIDE PRESSURE REGULATOR CLAMPS PER THE MM. ACCOMPLISHED LEFT SIDE AUGMENTATION VALVE CLAMP TO RQUE. ACCOMPLISHED REQUIRED LEAK CHECKS PER THE MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001051500240 20010515 00240 NM 2001 5 15 AALA20010764 1 20010409 A 2910 4091425 HYDRAULIC LINE BOEING 757 757223 1384957 NM HYD SYSTEM LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 669AA 25334 DFW - FLT 1843 - EN ROUTED DFW-SNA - DURING CLIMB, LEFT SIDE HYDRAULIC QUANTITY DECREASED TO ZERO. DECLARED EMERGENCY, RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED LEFT SIDE HYDRAULIC RETRACT ACTUATOR FLEXIBLE LINE. LEAK CH ECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001051500241 20010515 00241 WP 2001 5 15 AALA20010761 1 20010409 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 246AA 49258 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ASSEMBLY DIM. RE-CHARGED EMERGENCY EXIT LIGHT BATTERY PACK. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001051500242 20010515 00242 WP 2001 5 15 AALA20010763 1 20010409 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A K NONE L NO TEST IN INSP/MAINT 1 SW 21 7539A 49993 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 20DEF INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001051500243 20010515 00243 NM 2001 5 15 AWXA0001708 1 20010508 A 5312 65163007 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 ULTRASONIC INSPECTION OF BS 178 BLKHD WEB FOUND CRACK .4 INCH LENGTH LBL 6.7 WL 212-212.4 BENEATH STRAP. REMOVED BRACKE TS AND STIFFENER; CUT OUT DAMAGED WEB; LOCATED, DRILLED, TRIMMED AND INSTALLED REPAIR DOUBLER AND FILLER; REINSTALLED BR ACKETS AND STIFFENER IAW SRM 53-10-08 PG 287-298. 2 L 7 2 4F RT A16WE 2001051500244 20010515 00244 NM 2001 5 15 AWXA0001709 1 20010508 A 5312 65163007 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 A .5 INCH CRACK EMANATING FROM BENEATH STRAP BS 178 BLKHD FWD SIDE RBL 4.7 FROM WL 200.2-200.7. REMOVED BRACKETS, STIFF ENER AND L-ANGLE; CUT OUT DAMAGED WEB; LOCATED, DRILLED, TRIMMED AND INSTALLED REPAIR DOUBLER AND FILLER; REINSTALLED BR ACKETS AND STIFFENER AND L-ANGLE IAW SRM 53-10-08 PG 287-298. 2 L 7 2 4F RT A16WE 2001051500245 20010515 00245 NM 2001 5 15 AWXA0001710 1 20010508 A 5312 65163007 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 TWO CRACKS AT HI-LOKS BS 178 WEB FWD SIDE WL 234.1 LBL 11-12. REMOVED FASTENERS; CUT OUT DAMAGED WEB; LOCATED, DRILLED, TRIMMED AND INSTALLED REPAIR DOUBLER AND FILLER; REINSTALLED BRACKETS AND STIFFENER AND L-ANGLE IAW SRM 53-10-08 PG 287 -298. 2 L 7 2 4F RT A16WE 2001051500246 20010515 00246 NM 2001 5 15 AWXA0001711 1 20010508 A 5312 65163007 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 TWO CRACKS AT HI-LOKS BS 178 WEB FWD SIDE WL 234.1 RBL 11-12. REMOVED FASTENERS; CUT OUT DAMAGED WEB; LOCATED, DRILLED, TRIMMED AND INSTALLED REPAIR DOUBLER AND FILLER; REINSTALLED BRACKETS AND STIFFENER AND L-ANGLE IAW SRM 53-10-08 PG 287 -298. 2 L 7 2 4F RT A16WE 2001051500247 20010515 00247 NM 2001 5 15 AWXA0001712 1 20010508 A 5311 6516301301 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 LT MAIN FRAME CRACKED 1 INCH BS 178 WL 207. REMOVED STRAP, SEAL RETAINERS, ATTACH ANGLES, WEB AND SIDE CHORD; LOCATED A ND DRILLED NEW SIDE CHORD IAW SRM 51-10-02 PG 15 ITEM 8. INSTALLED SEAL RETAINERS, ATTACH ANGLES, BRACKETS, WEB AND SID E CHORD IAW SRM 51-40-02 PG 2, 10, 16. 2 L 7 2 4F RT A16WE 2001051500248 20010515 00248 NM 2001 5 15 AWXA0001713 1 20010508 A 5312 65163007 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 BLKHD 178 WEB HAS 2 CRACKS .5 INCH AT LBL .5 AND RBL .5 WL 189. REMOVED LOCALIZER ANTENNA MOUNT BOX; CUT OUT DAMAGED WE B; LOCATED, DRILLED, TRIMMED AND INSTALLED REPAIR DOUBLER AND FILLER; REINSTALLED LOCALIZER ANTENNA MOUNT BOX IAW SRM 53 -10-08 PG 287-298. 2 L 7 2 4F RT A16WE 2001051500249 20010515 00249 WP 2001 5 15 ZW0A0101306 1 20010430 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT IN THE AFT CARGO COMPT THE LT TIE DOWN TRACK HAD CORROSION FROM STA 1212 TO 1322. INSTALLED NEW TR ACK FROM STA 1212 TO STA 1322. 2 L 7 2 4F A6WE 2001051500250 20010515 00250 WP 2001 5 15 ZW0A0101302 1 20010504 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT FOUND CORROSION ON CABIN NUMBER 2 SEAT TRACK, STA 1117 TO 1250. REPLACED SECTION OF TRACK FROM STA 1117 TO 1250 PER SRM 51-30-2, 51-30-1, 51-10-3, AND SPM 6-70-1. 2 L 7 2 4F A6WE 2001051500251 20010515 00251 WP 2001 5 15 ZW0A0101303 1 20010416 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 908TW 49169 DURING CHECK-C MAINT IN THE MID CARGO COMPT THE LT TIE DOWN TRACK WAS CORRODED AT STA 598 TO 680. INSTALLED NEW TRACK P ER 53-05, FIG 4. 2 L 7 2 4F A6WE 2001051500252 20010515 00252 WP 2001 5 15 ZW0A0101304 1 20010506 A 2752 CASTING DOUG DC9 DC982 3022082 WP T/E FLAP ACT CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 924TW 49100 DURING CHECK-C MAINT IN THE RT MAIN GEAR WHEEL WELL, FOUND A CRACK IN THE CASTING SUPPORTING THE RIGHT T/E FLAP ACTUATOR , FORWARD END. ACCOMP HIGH FREQ EDDY CURRENT OF AREA PER NDT PART 6, 51-00-03. CASTING WAS CRACKED FROM CUTOUT INTO RA DIUS APPROX .125 IN LONG. REPLACED CASTING WITH NEW PER PRINT 9910155 AND SRM 51-30-3 AND 51-30-5, AND SPM 6-70-01. 2 L 7 2 4F A6WE 2001051500253 20010515 00253 NM 2001 5 15 AWXA0001714 1 20010508 A 5311 6516300302 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 RT MAIN FRAME BS 178 WL 195 FWD FACE CORRODED; HFEC INDICATES CRACK CONFIRMED FLUORESCENT PENETRANT. REMOVED SEAL RETAI NERS, ATTACH ANGLES, BRACKETS, WEB AND SIDE CHORD; LOCATED, DRILLED NEW SIDE CHORD IAW SRM 53-10-02 PG 15 ITEM 8; INSTAL LED SEAL RETAINERS, ATTACH ANGLES, BRACKETS, WEB AND SIDE CHORD IAW SRM 51-40-02 PG 2, 10, 16. 2 L 7 2 4F RT A16WE 2001051500254 20010515 00254 NM 2001 5 15 AWXA0001715 1 20010508 A 5312 65163007 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 ULTRASONIC CRACK INDICATION BS 178 BLKHD WEB, 1.1 INCH LENGTH, RBL 9.3-10.4 BENEATH ANGLE. REMOVED STRAPS, BRACKETS, AN GLES AND CHANNEL; CUT OUT DAMAGED WEB; LOCATED, DRILLED, TRIMMED AND INSTALLED REPAIR DOUBLER AND FILLER; REINSTALLED ST RAPS, BRACKETS, ANGLES AND CHANNEL IAW SRM 53-10-08 PG 287-298. 2 L 7 2 4F RT A16WE 2001051500255 20010515 00255 NM 2001 5 15 AWXA0001716 1 20010508 A 5320 651758351 ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 CRACK AT LBL 5.7 TEE, BS 178 BLKHD WEB WL 184-185 AFT SIDE OF BLKHD. REMOVED, FORMED, LOCATED, DRILLED AND INSTALLED RE PAIR ANGLES AND STRAPS IAW SRM 53-10-08 PG 221-240. 2 L 7 2 4F RT A16WE 2001051500256 20010515 00256 NM 2001 5 15 AWXA0001717 1 20010508 A 5320 65621258 TEE CHORD BOEING 737 737301 1384611 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 23258 REMOVE FASTENERS AND STRIP AREA AT BS 500D-510 STR 28R TO FACILITATE INSPECTION. REMOVED LOWER T-CHORD AND SKIN. REPAI RED LOWER T-CHORD AND SKIN IAW ER 03-5315-01120-DL1. 2 L 7 2 4F RT A16WE 2001051500257 20010515 00257 EA 2001 5 15 SWIA972552 1 20010505 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 EA COCKPIT CRACKED A SWIA K NONE O OTHER DE DESCENT 1 NM 07 410SW 7066 LEFT WINDSHIELD CRACKED. REMOVED AND REPLACED LT SIDE WINDOW (WINDSHIELD) IAW CRJ MM 56-12-01. PRESSURIZED AIRCRAFT TO 3.0 PSI. OPS LEAK CHECK OF WINDOW CHECKS GOOD. P/N ON 601R33033-11, S/N ON 0145H9919, S/N OFF 601R33033-3, S/N OFF 9 5039H2892 NP-139322-5-6. 2 L 7 2 4F RT A21EA 2001051500258 20010515 00258 SO 2001 5 15 SWIA972555 1 20010507 A 7722 INDICATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT INOPERATIVE A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 205SW 120260 T6 AURAL WARNING AND WARNING LIGHT FOR T6 BOTH CAME ON DURING CLIMBOUT. T6 WARNING LIGHT REMAINED ILLUMINATED FOR 5 MIN UTES EVEN WITH POWER REDUCED 30 PERCENT TQ. RETURNED TO FIELD. REPLACED NR 1 ENGINE T6 INDICATOR. P/N: SEL-0C19EG, S /N: 6066. 2 L 7 2 4T 4 T RT A31SO E20NE 2001051500259 20010515 00259 EA 2001 5 15 SWIA972557 1 20010508 A 2760 SPOILER CNDAIR CL600 CL6002B19 EA WING MALFUNCTIONED A SWIA K NONE F FLT CONT AFFECTED LD LANDING 1 NM 07 413SW 7102 FLT SPOILERS AND O/B GROUND LIFT DUMP RETRACTED AND RE-DEPLOYED AFTER LANDING. SYSTEM TESTED SECU NR 1 AND NR 2 IAW 27- 61-05. RUN FLT AND GROUND SPOILERS, NO FAULTS LOGGED. SYSTEM OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2001051500260 20010515 00260 WP 2001 5 15 AAQLA20010754 1 20010409 A 3350 SOCKET DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 292AA 49304 DFW - FLT DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 4 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001051500261 20010515 00261 WP 2001 5 15 AALA20010707 1 20010405 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 275AA 49272 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 8 THROUGH 11 DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001051500262 20010515 00262 WP 2001 5 15 AALA20010708 1 20010408 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP TAIL CONE DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 409AA 49320 DFW - DURING OVERNIGHT MAINTENANCE, TAIL CONE EMERGENCY EXIT LIGHT DIM. REPLACED TAIL CONE EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001051500263 20010515 00263 WP 2001 5 15 AALA20010709 1 20010407 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 481AA 49656 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT DIM. REPLACED OVERHEAD EMERGENCY EXIT LIGHT BATTERY P ACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001051500264 20010515 00264 WP 2001 5 15 AALA20010714 1 20010406 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP AIRSTAIRS DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 557AN 53087 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AFT AIRSTAIRS DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001051500265 20010515 00265 WP 2001 5 15 AALA20010715 1 20010406 A 3350 LIGHT DOUG DC9 DC982 3022082 WP TAIL CONE DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 490AA 49683 DFW - DURING OVERNIGHT MAINTENANCE, TAIL CONE EMERGENCY HANDLE RELEASE EXIT LIGHT DIM. REPLACED TAIL CONE EMERGENCY EXI T LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001051500266 20010515 00266 WP 2001 5 15 AALA20010716 1 20010404 A 3350 SOCKET DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 420AA 49332 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 15 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001051500267 20010515 00267 NM 2001 5 15 AALA20010671 1 20010401 A 2824 S343T00340 VALVE BOEING 737 737823 13844BZ NM FUEL TRANSFER LEAKING A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 907AN 29509 ATL - FLT 1066 - EN ROUTE MIA-ORD - SHORTLY AFTER TAKEOFF, DETECTED AN UNWANTED FUEL TRANSFER CAUSING A FUEL IMBALANCE. DIVERTED ATL AND LANDED WITHOUT FURTHER INCIDENT. REPLACED FUEL CROSSFIELD VALVE. SYSTEM GROUND CHECKED NORMAL OPERAT ION. (M) 2 L 7 2 4F RT A16WE 2001051500277 20010515 00277 NM 2001 5 15 AALA20010030 1 20010107 A 3350 LIGHT BOEING 727 727223 1384074 NM AIRSTAIR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 882AA 21521 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASS EMBLY AT AFT AIRSTAIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001051500278 20010515 00278 NM 2001 5 15 AALA20010040 1 20010110 A 3350 1001141 LIGHT BOEING 727 727223 1384074 NM AIRSTAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 889AA 21527 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT STAIRWAY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASS EMBLY AT AFT STAIRWAY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001051500279 20010515 00279 NM 2001 5 15 AALA20010098 1 20010118 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 863AA 21090 TUL - FOUND LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY ON E58 3668331, OPS CHECKED OK. (M) 2 L 7 3 4F A3WE 2001051500280 20010515 00280 NM 2001 5 15 AALA20010101 1 20010122 A 3350 CONTACTOR BOEING 727 727223 1384074 NM AIRSTAIR DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 709AA 22466 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIR INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT CONT ACT AT AFT AIRSTAIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001051500281 20010515 00281 NM 2001 5 15 AALA20010140 1 20010125 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 880AA 21519 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 6 THROUGH 21 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001051500282 20010515 00282 NM 2001 5 15 AALA20010147 1 20010127 A 3350 LIGHT BOEING 727 727223 1384074 NM GALLEY INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 861AA 21088 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT A SSEMBLY AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001051500283 20010515 00283 NM 2001 5 15 AALA20010148 1 20010128 A 3350 LIGHT BOEING 727 727223 1384074 NM AIRSTAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 886AA 21525 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AS SEMBLY AT AFT AIRSTAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001051500284 20010515 00284 NM 2001 5 15 AALA20010167 1 20010131 A 3350 LIGHT BOEING 727 727223 1384074 NM AIRSTAIR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 843AA 20984 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIR INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT A SSEMBLY AT AFT AIRSTAIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001051500285 20010515 00285 NM 2001 5 15 AALA20010235 1 20010209 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 712AA 22468 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SIDEWALL BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT FORWARD GALLEY SIDE WALL DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001051500286 20010515 00286 NM 2001 5 15 AALA20010282 1 20010216 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 849AA 20990 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT DIM. REPAIRED EMERGENCY EXIT PATHWAY LIGHT. SYSTEM GROUND CHE CKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001051500287 20010515 00287 NM 2001 5 15 AALA20010292 1 20010222 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN DAMAGED A K NONE L NO TEST IN INSP/MAINT 1 SW 21 873AA 21385 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR LIGHT FROM 16D THROUGH 26D INOPERATIVE. REPAIRED EMERGENCY EXI T LIGHT WIRE AT SEAT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001051500288 20010515 00288 EU 2001 5 15 AALA20010096 1 20010117 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1473K 11515 DFW - DURING OVERNIGHT MAINTENANCE, OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED OVERWING EMERGENCY EXIT LIGHT A SSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001051500292 20010515 00292 EU 2001 5 15 AALA20010139 1 20010125 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN DAMAGED A K NONE L NO TEST IN INSP/MAINT 1 SW 21 1400H 11340 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 12D INOPERATIVE. REPLACED EMERGENCY EXIT PATH LIGHT WIRE AT SEAT 12D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001051500293 20010515 00293 NM 2001 5 15 AALA20010133 1 20010124 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 719AA 20612 DFW - DURING OVERNIGHT MAINTENANCE, FLOOR PATH EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FLOOR PATH EMERGENCY EXIT LIG HT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001051500294 20010515 00294 NM 2001 5 15 AALA20010232 1 20010208 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 722AA 20730 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PROXIMITY LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SEG MENTS AT ROW 6, 8 AND 26. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001051500295 20010515 00295 NM 2001 5 15 AALA20010573 1 20010322 A 3350 P4010051126 MODULE BOEING 727 727227 1384078 NM AFT STAIRS DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 720AA 20613 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT ENTRY STAIRS DIM. REPLACED EMERGENCY EXIT LIGHT MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001051500296 20010515 00296 2001 5 15 GTIA010114 4 20010417 A 2210 AUTOPILOT SYS DOUG DC9 DC982 3022082 WP COCKPIT MALFUNCTIONED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 957AS 49126 FLT 623 - MLB - AUTOPILOT WILL NOT ENGAGE ON COMPUTER 1 WORKS FINE ON COMPUTER 2. ENT TO DIM NR 0013692-1 IAW MEL 22-14 -0 CAT C AMEND 1800Z HK. (M) 2 L 7 2 4F A6WE 2001051500297 20010515 00297 2001 5 15 GTIA010093 4 20010408 A 2210 AUTOPILOT SYS DOUG DC9 DC982 3022082 WP COCKPIT MALFUNCTIONED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 957AS 49126 FLL - FLT 679 - AUTOPILOT WILL NOT STAY ON THE NR 1 DFGS. WORKS ON NR 2 DFGS. TRANSFERRED TO DIM NR 0003269-2 IAW MEL 22-14-0. CAT ''C'' PLACARDED. (M) 2 L 7 2 4F A6WE 2001051500298 20010515 00298 2001 5 15 GTIA010092 4 20010413 A 2565 SLIDE DOUG DC9 DC982 3022082 WP L2 DOOR OUT OF POSITION A GTIA K NONE O OTHER NR NOT REPORTED 1 GL 23 817NK 49141 FLL - FLT 783 - L2 SLIDE FELL OFF OF DOOR. RE-INSTALLED SLIDE. OPS CHECK OK, IAW MM 25-62-00. (M) 2 L 7 2 4F A6WE 2001051500299 20010515 00299 2001 5 15 GTIA010091 4 20010408 A 2565 SLIDE DOUG DC9 DC982 3022082 WP L2 DOOR INOPERATIVE A GTIA K NONE L NO TEST NR NOT REPORTED 1 GL 23 817NK 49141 FLT 781 - ORD - FOUND SLIDE PACK L2 INOPERATIVE. REPACKED L2 SLIDE IAW MM 25-65-00. (M) 2 L 7 2 4F A6WE 2001051500300 20010515 00300 2001 5 15 GTIA010113 4 20010412 A 2210 AUTOPILOT SYS DOUG DC9 DC941 302207N WP COCKPIT FLUTTER A GTIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 GL 23 130NK 47604 MLB - FLT 72 - WHEN AUTOPILOT IS ENGAGED THERE IS A RAPID OSCILLATION (FLUTTER) IN PITCH, SERVO OFF NO OSCILLATION. TRA NFERRED TO MEL 22-16-0 DMI NR 0001663-1 CAT C DUE 4-22-01 AMEND NR 1 1115Z HK. (M) 2 L 7 2 4F A6WE 2001051500301 20010515 00301 2001 5 15 GTIA010112 4 20010414 A 2215 SERVO DOUG DC9 DC941 302207N WP AUTOPILOT SYS MALFUNCTIONED A GTIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 GL 23 130NK 47604 FLL - FLT 139 - WITH A/P ENGAGED AL PORPOISES ABRUPTLY WITH A/P ELEV SERVO OFF PROBLEM CEASES. DMI NR 1669-1 ASSIGNED P ER MEL 22-3-0 CAT C DUE DATE D4-24-01 AMEND NR 1 1730Z HR PLACARDED ELEV SERVO SWITCH. (M) 2 L 7 2 4F A6WE 2001051500302 20010515 00302 2001 5 15 GTIA010111 4 20010413 A 2230 AUTOTHRUST SYS DOUG DC9 DC983 3022083 WP AUTOPILOT SYS MALFUNCTIONED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 822NK 49392 ACY - FLT 1210 - AUTOTHROTTLES FREQUENTLY DISCONNECT AND WON''T RE-ENGAGE. AS SPIRIT MEL 22-15-2 CAT C TRANSFERRED TO D MI NR 0001928-1 PLACARDED. (M) 2 L 7 2 4F RT A6WE 2001053100132 20010531 00132 CE 2001 5 31 GLBA2001095 1 20010508 A 2130 1143800595 SHUTOFF VALVE BEECH 1900 1900D 1154162 CE CABIN PRESSURE FAILED A GLBA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 01 240GL 62 UE240 RETURN TO BLOCK - AIRCRAFT WOULD NOT PRESSURIZE. REPLACED PRSOV, OPS CHECKED SATISFACTORY. 2 L 7 2 4T RT A24CE 2001051500303 20010515 00303 CE 2001 5 15 GLBA2001096 1 20010508 A 2841 WARNING SYSTEM BEECH 1900 1900D 1154162 CE COCKPIT MALFUNCTIONED A GLBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 01 226GL UE226 ABORTED T/O - BOTH LOW FUEL QUANTITY ANNUNCIATORS ILLUMINATED. INSPECTED, NO FAULT FOUND. 2 L 7 2 4T RT A24CE 2001051500304 20010515 00304 EU 2001 5 15 RAIA00105006 1 20010509 A 3350 16701 LIGHT AEROSP ATR72 ATR72202 8680940 EU CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 722TE 220 7117-STL- EMERGENCY ESCAPE PATH LIGHTING HAS SEVERAL BULBS OUT. MAINTENANCE INSPECTED AND REPLACED EMERGENCY ESCAPE PAT H LIGHTING BULBS. 2 H 7 2 4T RT A53EU 2001051500305 20010515 00305 NM 2001 5 15 SWAA011356 1 20010506 A 3397 BR2013 WIRE BOEING 737 7377H4 1384404 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 701GS 27836 EEPLS TRACK WIRES EXPOSED AT ROW 6. SECURED EEPLS WIRES PER MM. 2 L 7 2 4F RT A16WE 2001051500306 20010515 00306 NM 2001 5 15 SWAA011357 1 20010506 A 3350 6104789 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED D-CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS INOP, LT AND RT. REMOVED AND REPLACED BATTERY PACK PER M M. 2 L 7 2 4F A16WE 2001051500307 20010515 00307 NM 2001 5 15 SWAA011358 1 20010507 A 3350 6104791 POWER SUPPLY BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY & FWD SVC DOORS EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY BOX PER MM. 2 L 7 2 4F A16WE 2001051500308 20010515 00308 NM 2001 5 15 SWAA011359 1 20010507 A 3350 BR2013 TRACK BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 655WN 28400 EEPLS FLOOR TRACK LOOSE AT MID CABIN. SECURED EEPLS TRACK PER MM. 2 L 7 2 4F RT A16WE 2001051500309 20010515 00309 NM 2001 5 15 SWAA011360 1 20010506 A 3350 079123 COVER BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 EEPLS FLOOR TRACK COVER LOOSE AT MID CABIN. REMOVED AND REPLACED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001051500310 20010515 00310 NM 2001 5 15 SWAA011361 1 20010506 A 3350 57771 CAP BOEING 737 7375H4 138449D NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 524SW 26566 EEPLS END CAP MISSING ON FWD END. INSTALLED END CAP PER MM. 2 L 7 2 4F RT A16WE 2001051500311 20010515 00311 NM 2001 5 15 SWAA011362 1 20010507 A 3350 6128251 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 635SW 27708 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT FWD CABIN. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2001051500312 20010515 00312 NM 2001 5 15 SWAA011363 1 20010507 A 3350 207377 LENS BOEING 737 7373A4 1384585 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 EEPLS LENS MISSING AT MID CABIN. DEFERRED PER MEL. LATER AT LAX INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2001051500313 20010515 00313 NM 2001 5 15 SWAA011364 1 20010507 A 3350 6104789 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 073SW 22673 DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC AND AFT ENTRY EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PA CK PER MM. 2 L 7 2 4F A16WE 2001051500314 20010515 00314 NM 2001 5 15 SWAA011365 1 20010506 A 3350 6104789 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2001051500315 20010515 00315 NM 2001 5 15 SWAA011366 1 20010506 A 3350 6104789 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED SERVICE CHECK, FOUND FWD EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2001051500316 20010515 00316 NM 2001 5 15 SWAA011367 1 20010507 A 5320 65C27314 TIE CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D-CHECK, FOUND STR TIE CLIPS CRACKED AT BS 706, STR 11R & BS 784, STR 13L. REMOVED AND REPLACED STR T IE CLIPS PER SRM. 2 L 7 2 4F A16WE 2001051500317 20010515 00317 NM 2001 5 15 SWAA011368 1 20010507 A 5310 6546569 DOOR FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D-CHECK, FOUND AFT ENTRY DOOR CUT OUT FWD FRAME CRACKED. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2001051500318 20010515 00318 NM 2001 5 15 SWAA011369 1 20010507 A 5320 BAC1503 STIFFENER BOEING 737 7373H4 1384600 NM MLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 331SW 23695 DURING SCHEDULED SERVICE CHECK, FOUND VERTICAL STIFFENERS CRACKED, AT MLG WHEEL WELL, BS 663, RBL 6.4, LBL 6.4. REPAIRE D PER SWA RA. 2 L 7 2 4F RT A16WE 2001051500319 20010515 00319 NM 2001 5 15 SWAA011370 1 20010506 A 5320 6547977 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 331SW 23695 DURING SCHEDULED SERVICE CHECK, FOUND BEADED WEB CRACKED AT BS 663, LBL 30. REPAIRED PER SWA TI. 2 L 7 2 4F RT A16WE 2001051500320 20010515 00320 NM 2001 5 15 SWAA011372 1 20010506 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING WALK-AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 25R. REPAIRED CRACK PER SRM. 2 L 7 2 4F RT A16WE 2001051500321 20010515 00321 NM 2001 5 15 SWAA011373 1 20010507 A 5312 6516300 BULKHEAD BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234, LBL 7.0. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001051500322 20010515 00322 NM 2001 5 15 SWAA011374 1 20010508 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 342SW 24133 DURING SCHEDULED SPECIAL VISIT FOUND WEB CRACKED AT BS 178, LBL 27, WL 207. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001051500323 20010515 00323 NM 2001 5 15 SWAA011375 1 20010507 A 3350 207377 LENS BOEING 737 7373A4 1384585 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 DURING RON, FOUND EEPLS LENS MISSING AT ROW 9. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2001051500324 20010515 00324 NM 2001 5 15 SWAA011376 1 20010507 A 3350 BR2013 LIGHT BOEING 737 7373A4 1384585 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 675AA 23253 DURING RON, FOUND EEPLS INOP AT ROW 17. RELAMPED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001051500325 20010515 00325 NM 2001 5 15 SWAA011377 1 20010507 A 5320 BAC1503 STIFFENER BOEING 737 7373H4 1384600 NM MLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 330SW 23694 DURING SCHEDULED SERVICE CHECK, FOUND VERTICAL STIFFENER CRACKED AT MLG WHEEL WELL, BS 663, RBL 6.5. REPAIRED PER SWA R A. 2 L 7 2 4F RT A16WE 2001051500326 20010515 00326 NM 2001 5 15 SWAA011382 1 20010505 A 3350 65C34691 LENS BOEING 737 7373K2 13844BA NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 345SA 23786 EMERGENCY LIGHT LENS MISSING AT ROW 22 LT SIDE. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2001051500327 20010515 00327 NM 2001 5 15 C1HA200192004 1 20010506 A 3350 110049 POWER SUPPLY BOEING 727 727212 138407G NM CABIN DISCHARGED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 293AS 21348 R2, L2, AND AFT ENTRY EMERGENCY EXIT SIGNS INOP. REMOVED AND REPLACED BATTERY POWER SUPPLY, OPS CHECKS GOOD. 2 L 7 3 4F A3WE 2001051500328 20010515 00328 NM 2001 5 15 C1HA200193005 1 20010506 A 3350 110049 POWER SUPPLY BOEING 727 727212 138407G NM CABIN DISCHARGED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 293AS 21348 R2, L2, AND AFT ENTRY EMERGENCY EXIT SIGNS INOP. REMOVED AND REPLACED BATTERY POWER SUPPLY, OPS CHECKS GOOD. 2 L 7 3 4F A3WE 2001051500329 20010515 00329 NM 2001 5 15 C1HA200193006 1 20010507 A 5270 SWITCH BOEING 727 727212 138407G NM AFT AIRSTAIRS OUT OF ADJ A C1HA K NONE N FALSE WARNING CR CRUISE 1 GL 15 293AS 21348 AFT AIRSTAIR AMBER LIGHT ILLUMINATED IN FLIGHT EN ROUTE TO DFW CONTINUED FLIGHT PER COM 2.52.2. ADJUSTED WARNING LIGHT SWITCH AT UPPER HANDLE, CHECKS GOOD. 2 L 7 3 4F A3WE 2001051500330 20010515 00330 NM 2001 5 15 C1HA200193007 1 20010508 A 5270 SWITCH BOEING 727 727212 138407G NM AIRSTAIR DOOR OUT OF ADJ A C1HA K NONE N FALSE WARNING CR CRUISE 1 GL 15 293AS 21348 AFT AIRSTAIR DOOR LIGHT ILLUMINATED IN FLIGHT VISUALLY INSPECTED DOOR CONFIRMED CLOSED. ADJUSTED AIRSTAIR SWITCH, OPS C HECK GOOD. 2 L 7 3 4F A3WE 2001051500331 20010515 00331 EU 2001 5 15 20010511CW001 1 20010322 A 6220 22125BC080026L BOLT UROCOP SNIAS 350 AS350B2 8680813 EU VIBRATION ASORB UNDERTORQUED B K NONE O OTHER IN INSP/MAINT 1 WP 23 223LA 999 M1645 3278 DURING ROUTINE INSPECTION OF THE VIBRATION ASORBER ASSEMBLY, THE ADDITIONAL WEIGHT WAS FOUND TO HAVE COME LOOSE. THIS C AUSED SEVERE DAMAGE TO THE WEIGHT ASSEMBLY, ADDITIONAL WEIGHT, BOLT AND PIN. THE PROBABLE CAUSE OF THE LOSS OF TORQUE ON THE ATTACHING HARDWARE IS THOUGHT TO BE EITHER LOW INITIAL TORQUE OR IMPROPER BENDING OF THE LOCKING TABS. POSSIBLY THE SOFT NATURE OF THE LEAD WEIGHT MATERIAL CONTRIBUTED TO THE LOSS OF TORQUE. 1 G 7 1 3U H9EU 2001051500333 20010515 00333 NM 2001 5 15 CA010502002 1 20010407 A 7500 323435 VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 1 ENGINE STUCK W E ENGINE SHUTDOWN E VIBRATION/BUFFET DE DESCENT 1 CA 085 (CAN) WHEN ENG POWER REDUCED FOR DESCENT, NR 1 ENGINE EXPERIENCED SIGNIFICANT VIBRATION/COMPRESSOR STALLING. CABIN AIR S UPPLY VALVE (WHICH IS AT P2.5 ENG STATION) FAILED IN OPEN POS WHICH ALLOWED P3 COMPRESSOR AIR TO ENTER COMPRESSOR AT LOW ER STAGE & CREATE STALL CONDITION (WHEN ENGINE POWR REDUCED). COMPRESSOR STALLING EXPERIENCED ON 3 SEPARATE EVENTS BEFOR E BEING CORRECTLY DIAGNOSED. DURING 1ST EVENT, ENG EXHIBITED SIGNIFICANT VIBRATION & TORQUE FLUXS, WHICH REQD ENGINE TO UNDERGO INFLT SHUTDOWN. OTHER 2 EVENTS WERE CONTROLLED IN FLT WITH REDUCTION OF POWER & DID NOT REQUIRE ENG TO BE SHUTDO WN. REPLACED OF CABIN AIR SUPPLY PNEUMATIC VALVE RECTIFIED PROBLEM. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001051500335 20010515 00335 CE 2001 5 15 CA010502006 1 20010331 A 5511 053200198 SPAR CESSNA 172 172M 2072418 CE LYC O320 O320E2D 41508 EA MCAULY 1C160 1C160DTM GL HORIZONTAL STAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 3173 (CAN) HORIZONTAL STAB SPAR FOUND CRACKED FROM CENTRE RELIEF HOLE (LIGHTNING HOLE) OUTWARD APPROXIMATELY 1/2 INCH. PART R EPLACED WITH NEW UNIT. THIS PROBLEM IS PROBABLY DUE TO INAPPROPRIATE GROUND LANDING OF THE AIRCRAFT, I.E. USING STAB AS SURFACE TO PUSH ON TO MANOEUVRE AIRCRAFT NOSE. 1 H 7 1 3O 3 O NT 3A12 E274 5 N P910 2001051500336 20010515 00336 NM 2001 5 15 CA010503002 1 20010411 A 2910 NAS16126 O-RING DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM LEAKING W O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 CA (CAN) THE FLIGHT CREW REPORTED LOSS OF NR 1 HYDRAULIC SYSTEM PRESSURE AND QUANTITY ON SHORT FINAL. AN UNEVENTFUL LANDIN G WAS COMPLETED. MAINTENANCE INVESTIGTION REVEALED A BLOWN/LEAKING O-RING AT THE SPU OUTLET ADAPTER. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001051500338 20010515 00338 EA 2001 5 15 CA010503004 1 20010410 A 2920 849557 POWER UNIT DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE HYD SYSTEM FAILED W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA 152 (CAN) THE FLIGHT CREW RETURNED TO THE GATE AFTER EXPERIENCING A NR 1 HYD HOT CAUTION LIGHT DURING TAXI FOR TAKEOFF. MAIN TENANCE REPLACED THE NR 1 SYSTEM STANDBY POWEER UNIT AND THE AIRCRAFT RETURNED TO SERVICE. THIS UNIT HAD RECENTLY BEEN R EPAIRED BY THE VENDOR. TTSN, TCSN WERE NOT READILY AVAILABLE DUE TO THIS UNIT BEING A LOANER. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001051500339 20010515 00339 NM 2001 5 15 CA010503005 1 20010425 A 3010 8SC0029028 BOOT DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE DEICE SYSTEM DELAMINATED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 1404 (CAN) DURING MAINTENANCE INSPECTION, A LARGE AREA OF DELAMINATION WAS FOUND ON THE OUTBOARD LOWER SURFACE OF THE RT INBO ARD LEADING EDGE ASSEMBLY. THIS ESTANE DEICE BOOT HAD BEEN IN SERVICE FOR LESS THAN ONE YEAR. THIS LATEST INCIDENT CONTI NUES A TREND OF DECREASED RELIABILITY OF THE BF GOODRICH ESTANE BOOTS. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001051500340 20010515 00340 NM 2001 5 15 CA010503006 1 20010411 A 3010 P29S7D5152 BOOT DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE DEICE SYSTEM FAILED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) THE RT NR 3 LEADING EDGE (FIRST SECTION OUTBOARD OF THE LANDING LIGHTS) DEICE BOOT FAILED AFTER 1 DAY IN SERVICE. THIS IS A NEW STYLE DEICE BOOT FROM BFG, WITH A PEEL & STICK TYPE OF APPLICATION. THE FAILURE OCCURRED DUE TO THE STITCH ING FAILING BETWEEN RIBS, CAUSING A LARGE CIRCULAR AREA OF SEPARATION WITHIN THE BOOT. DEICE SYSTEM PRESSURE WAS CHECKED WITHIN LIMITS. THE LEADING EDGE/BOOT ASSY WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001051500341 20010515 00341 EU 2001 5 15 CA010503007 1 20010319 A 2913 70AA6521 PUMP BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE HYD SYSTEM FAILED W H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION IN INSP/MAINT 1 CA 6045 (CAN) THE FLIGHT CREW REPORTED THAT THE C.B. FOR THE AC HYDRAULIC PUMP COOLING FAN POPPED WHEN THE AC PUMP WAS SELECTED ON. THE FAN WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. THE FAN HAD BEEN IN SERVICE FOR 62 DAYS, 512 HOURS, A ND 311 CYCLES SINCE REPAIR. 2 H 7 4 4F 4 F RT A49EU E6NE 2001051500342 20010515 00342 2001 5 15 CA010503008 4 20010420 A 3444 9650476088 COMPUTER DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE GROUND PROX FAILED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA 34768 5028 (CAN) WHILE POWERING UP THE AIRCRAFT AT THE GATE FOR THE FIRST FLIGHT OF THE DAY, AN ACRID SMELL WAS DETECTED. THE AIRCR AFT WAS DEPOWERED. THE GPWS CIRCUIT BREAKER ON THE 115 VAC BUS WAS FOUND TRIPPED. THE CAUSE OF THE SMELL WS DETERMINED T O BE COMING FROM THE INTERNALS OF THE GPWS COMPUTER. THE COMPUTER WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. TIME SINCE REPAIR 4376 HOURS. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001051500343 20010515 00343 NE 2001 5 15 CA010503009 2 20010418 A 7250 TURBINE BOEING 737 737275C NM PWA JT8 JT8D9A 52048 NE 4TH STAGE DAMAGED W E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 CA (CAN) A/C 752, APRIL 19/2001, FLT 3697, YQR, LOG SEQUENCE 0496405, 20 MINUTES FROM YQR, NR 1 ENGINE DEVELOPED HIGH VIBRA TIONS, ENGINE OIL TEMP WAS 10 DEGREES ABOVE NORMAL. CREW SHUTDOWN ENGINE AND DECLARED AN EMERGENCY, PROCEEDED TO YQR. LA NDED WITHOUT FURTHER INCIDENT. INSPECTION REVEALED 4TH STAGE TURBINE DAMAGE, NO INLET DAMAGE. ENGINE REPLACED AS PER WOR K CARD 1125-1. 2 L 7 2 4F 4 F A16WE E2EA 2001051500352 20010515 00352 SO 2001 5 15 CA010504005 1 20010411 A 3246 300608 WHEEL EMB 110 EMB110P1 3260122 SO PWA PT6 PT6A34 52043 EA LT MLG SEPARATED W O OTHER O OTHER TX TAXI/GRND HDL 1 CA (CAN) WHILE TAXIING OFF RUNWAY AFTER LANDING LT MAIN WHEEL FAILED. APPROXIMATELY 12 INCHES OF BEAD SEAT SEPARATED FROM I NBOARD WHEEL HALF INSTANTLY DEPRESSURIZING TIRE. AIRCRAFT TAXIED TO SAFE ZONE. MAINTENANCE REPLACED WHEEL ON TAXI WAY AN D AIRCRAFT WAS RETURNED TO SERVICE. 1 L 7 2 4T 4 T A21SO E4EA 2001051500353 20010515 00353 CE 2001 5 15 CA010504006 1 20010419 A 3243 6632401002011 VALVE LEAR 45 45LEAR 5170805 CE PARK BRAKE FAILED W K NONE N FALSE WARNING IN INSP/MAINT 1 CA 11 (CAN) EICAS PARK BRAKE ON MESSAGE WILL NOT EXTINGUISH. 2 L 7 2 4F RT T00008WI 2001051500354 20010515 00354 EU 2001 5 15 CA010504008 1 20010407 A 3020 SM600BA100N1 CIRCUIT BREAKER STBROS SD3 SD360 8100606 EU PWA PT6 PT6A65AR 52043 NE LT ENGINE SHORTED W O OTHER B M J SMOKE/FUMES/ODORS/SPARKS OVER TEMP WARNING INDICATION CR CRUISE 1 CA (CAN) LT ENGINE INLET HEAT OVER HEATED AND RESULTED IN DAMAGING THE INLET HEAT ASSY. THE CAUSE WAS THE REMOTE CIRCUIT BR EAKER FAILURE.PILOT REPORTED LEFT INTAKE WILL NOT SHUT OFF. ON GROUND, THE INLET HEATER WAS SMOKING AND CAUSED SMOKE SME LL IN CABIN WITH LEFT BLEED ON. CIRCUIT BREAKERS; 11A + 23 PULLED BUT STILL UNABLE TO SHUT OFF. THE REMOTE BREAKER & INT AKE HEAT GETS ITS POWER DIRECTLY FROM THE LT MAIN BUSBAR. DE-ENERGIZING THE MAIN BUSBAR, IS THE ONLY WAY TO STOP POWER G OING TO THE INTAKE HEAT IF THE REMOTE BREAKER FAILS. IT IS DIFFICULT TO TELL IF THE INTAKE HEAT HAS BEEN TURNED OFF WHIL E FLYING. 2 H 7 2 4T 4 T A41EU E4EA 2001051500358 20010515 00358 EA 2001 5 15 CA010504013 2 20010419 A 7414 106006463 DISTRIBUTOR GEAR ROBSIN R44 R44 7640120 WP LYC O540 O540F1B5 41532 EA MAGNETO SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA 1826 330 (CAN) AIRCRAFT WAS RUNNING AT 100 PERCENT JUST BEFORE LIFT OFF WHEN THE PILOT AND PASSENGER HEARD 2 SPUTTERS FOLLOWED BY THE ENGINE SHUTTING DOWN. AFTER FURTHER INVESTIGATION, BOTH MAGNETOS WERE FOUND TO HAVE SEVERAL SHEARED PLASTIC TEETH O N THE DISTRIBUTOR GEAR. BOTH MAGNETOS WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.MAGNETOS P/N 10-600646-3 AND 10 -600646-201. 1 G 7 1 3O 3 O H11NM E295 2001051500359 20010515 00359 SO 2001 5 15 CA010504015 1 20010413 A 5280 159L100071 FAIRING GRUMAN G159 GULSTM G159 G159 3952202 SO RROYCE DART DART5298X 54507 EU NLG DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 21681 104 (CAN) WHEN DOING THE POST FLIGHT INSPECTION A CRACK WAS FOUND IN THE NOSE GEAR DRAG BRACE FAIRING ASSEMBLY. THE CRACK WA S ON THE L/H SIDE FORMER WHICH WAS CRACKED COMPLETELY THROUGH. IF LEFT UNREPAIRED A FAILURE OF THE FAIRING ASSEMBLY WAS POSSIBLE. THE CRACK WAS QUITE NOTICEABLE DURING THE VISUAL INSPECTION.PART REMOVED, REPAIRED AND REINSTALLED. 2 L 7 2 4T 4 T 1A17 E297 2001051500360 20010515 00360 CE 2001 5 15 CA010504017 1 20010416 A 2720 151350022 SUPPORT BRACKET CESSNA 337C CESSNA 337 337C 2075712 CE CONT O360 IO360G 17025 SO MCAULY 2AF34C D2AF34C61 GL RUDDER PEDAL CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 7253 3370895 (CAN) DURING A 100 HOUR INSPECTION IT WAS OBSERVED THERE WA A CRACK IN THE ABOVE MENTIONED BRACKET. A NEW BRACKET WAS IN STALLED AND AIRCRAFT RELEASED FOR RETURN TO SERVICE. 1 H 7 2 3O 3 O A6CE E1CE 5 C P5EA 2001051500364 20010515 00364 NM 2001 5 15 CA010504023 1 20010414 A 2730 69416413 BRACKET BOEING 737 7372E3 NM PWA JT8 JT8D15 52051 NE HINGE WORN W O OTHER D INFLIGHT SEPARATION CL CLIMB 1 CA (CAN) CAREW REPORTED A VIBRATION IN CLIMB THRU 10,000 FEET THEN RECURRED ON DESCENT. AS THE AIRCRAFT DESCENDS BELOW 10,0 00 FEET. THE PROBLEM DID NOT OCCUR AFTER THE ELEVATOR TAIL HINE BRACKET WAS REPLACED. 2 L 7 2 4F 4 F RT A16WE E2EA 2001051500365 20010515 00365 NM 2001 5 15 CA010504024 1 20010413 A 7711 655813513 TUBE BOEING 737 737297 1384480 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE WORN W O OTHER J WARNING INDICATION CL CLIMB 1 CA 51868 (CAN) CREW REPORTED NR 1 ENGINE EPR INDICATION FLUCTUATING TO .20 EPR LOWER THAN NR 1 ENGINE. N1, N2 AND FUEL FLOWS WERE STEADY. INSPECTION FOUND A CHAFED WIRE AT THE R/H ANTI-ICE VALVE HAD ARCHED AND WORN A HOLE THRU THE SIDE OF THE LINE F ROM THE PT 7 PROBE. THE LINE WAS REPLACED AND THE CHAFED WIRE WAS REPAIRED. 2 L 7 2 4F 4 F A16WE E2EA 2001051500373 20010515 00373 CE 2001 5 15 CA010507010 1 20010416 A 3234 08135254 TERMINAL CESSNA 401 401B 207590E CE CONT O520 TSIO520EB 17040 SO GEAR SWITCH LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WHEN GEAR WAS SELECTED UP AFTER TAKEOFF IF DID NOT RETRACT. UNTIL THE PILOT HAD TURNED FOR RETURN TO RUNWAY. SUBSE QUENT INVESTIGATION REVEALED LOOSE WIRING TERMINALS ON GEAR SELECTOR HANDLE. 1 L 7 2 3O 3 O A7CE E8CE 2001051500374 20010515 00374 EU 2001 5 15 CA010507011 1 20010427 A 3240 2Q2395 HOSE BRAERO 748 HS7482B 1500248 EU NLG RUPTURED W D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 CA (CAN) DURING ENGINE START, A/C LOST OUTBOARD BRAKE PRESSURE: MARSHALER NOTICED HYDRAULIC FLUID COMING FROM RIGHT NACELLE , & APPROPRIATELY SIGNALLED A/C CREW. ENG SHUTDOWN, & HYDRAULIC LEAK INVESTIGATED. RUPTURED HOSE FOUND AT TOP OF RT MAIN GEAR SHOCK STRUT. 2 L 7 2 3T A24EU 2001051500375 20010515 00375 SO 2001 5 15 CA010507012 1 20010411 A 7714 SL76155 DRIVE SHAFT PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA TACHOMETER WORN W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 45 (CAN) AN OIL LEK LOCATED ON DAILY INSPECTION REVEALED A LEAK AT THE TACHOMETER DRIVE SEAL AREA. UPON CLOSER INSPECTION I T WAS NOTED THAT THE SHAFT HAD A WEAR GROOVE AROUND THE RADIUS OF THE TACHOMETER DRIVE SHAFT. IT WAS REPLACED AND NO OIL LEAKS FOUND AFTER. THIS ENGINE WAS JUST OVERHAULED 44.7 HRS PREVIOUS AND SUGGEST A QUALITY CONTROL PROBLEM AT THE OVERH AUL FACILITY. 1 L 7 2 3O 3 O A20SO E14EA 2001051500376 20010515 00376 EU 2001 5 15 CA010507014 1 20010410 A 3246 L305649 BEARING AMD FALC50 FALCON50MYST 2730106 EU GE CF700 CF7002D2 30010 NE RT OTBD WHEEL SEIZED W O OTHER O OTHER TX TAXI/GRND HDL 1 CA 213 (CAN) UPON LANDING IN MONCTON, PILOT IN COMMAND NOTICED ABNORMAL BRAKING FROM RT SIDE . AFTER A/C SHUTDOWN FLIGHT CREW R EPORTED TO MAINTENANCE NR 4 WHEEL ASSEMBLY DISLOCKED. IT WAS DETERMINED BY MAINTENANCE INSPECTION THAT A BEARING FAILURE HAD OCCURRED. THE BEARING P/N L305649 HAD OVERHEATED AND SEIZED. INSPECITON OF INNER BEARING INDICATED LACK OF LUBRICAT ION & DIRTINESS. THE LEAD FAILURE CANNOT BE DETERMINED DUE TO THE DESTRUCTION OF THE BEARING. 2 L 7 3 4F 4 F A46EU E7EA 2001051500378 20010515 00378 NM 2001 5 15 CA010507016 1 20010417 A 7711 FILTER PWA BOEING 727 727233 138408A NM PWA JT8 JT8D15A 52051 NE ENGINE PRESSURE BLOCKED W C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 CA 700329 (CAN) ON DEPARTURE THE AIRCRAFT EXPERIENCED A COMPRESSOR STALL ON NR 2 ENGINE. THE CREW DECISION WAS MADE TO RETURN TO P OINT OF DEPARTURE. MAINTENANCE INVESTIGATION FOUND THE PS3 SENSE LINE FILTER BLOCKED WITH WHAT APPEARED TO BE SHREDDED P APER FIBRE, ORIGIN UNKNOWN. THE FILTER WAS CLEANED AND THE AIRCRAFT GROUND RUN SUCCESSFULLY BEOFRE RETURN TO SERVICE. 2 L 7 3 4F 4 F RT A3WE E2EA 2001051500379 20010515 00379 NM 2001 5 15 CA010507017 1 20010409 A 2782 296900295 ACTUATOR BOEING 727 727233 138408A NM PWA JT8 JT8D15A 52051 NE NR 4 SLAT FRACTURED W O OTHER K FLUID LOSS AP APPROACH 1 CA 5028 (CAN) ON APPROACH TO WHEN FLAP 2 SELECTED THE CREW OBSERVED RAPID DECREASE IN A HYDRAULIC SYSTEM. HYDRAULIC LEAK/LOSS OK . LIST CARRIED OUT. MANUAL GEAR EXTENSION PERFORMED, AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS TOWED FROM THE R UNWAY TO THE HANGAR WHERE INVESTIGATION FOUND NR 4 SLAT ACTUATOR FAILED. THE CYLINDER WAS FRACTURED AT THE END CAP THREA D. THE ACTUATOR WAS REPLACED, BOTH A PUMPS REPLACED, AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F RT A3WE E2EA 2001051500380 20010515 00380 NM 2001 5 15 CA010507018 1 20010328 A 2425 915F2126 GCU BOEING 737 737210C 1384459 NM PWA JT8 JT8D9A 52048 NE NR 2 GENERATOR FAILED W O OTHER H ELECT. POWER LOSS-50 PC DE DESCENT 1 CA (CAN) SHORTLY AFTER DEPARTING NR 2 GEN WENT OFF LINE. CREW STARTED APU & THAT GEN BROUGHT ON LINE&FLT CONTINUED. COMMENC ING DESCENT NR 1 GEN WENT OFF LINE & CREW DECLARED. FLT CONCLUDED W/O FURTHER INCIDENT. ON ARRIVAL WERE NO GEN FAIL INDI CATION. LIGHTS ILLUMINATED. INVESTIGATION REVEALED NR 2 GENERATOR RESIDUAL VOLTAGE BELOW LIMITS & NR 1 CSD UNSTABLE AT L OWER RPM, BOTH UNITS WERE REPLACED. PREV NR 1 & 2 GCUS HAD BEEN SWAPPED FOR TROUBLE SHOOTING. NR 1 GCU RETURNED TO NR 2 POSITION & REPLACED UNIT INSTALLED IN NR 1 POS. NO GENS WERE OBSERVED TO HAVE GONE OFF LINE AT ANY TIME DURING COURSE TR OUBLESHOOTING. A/C TEST FLOWN & RETURNED TO SERVICE. 2 L 7 2 4F 4 F A16WE E2EA 2001051500381 20010515 00381 EU 2001 5 15 CA010507021 1 20010418 A 2150 5613C000002 A/C PACK PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL A/C BAY LEAKING W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 1959 1959 (CAN) DURING CRUISE FLIGHT A BURNED OIL SMELL WAS NOTICED IN THE COCKPIT AND CABIN. AFTER RETURNING TO BASE THE SAME SME LL COULD BE DUPLICATED ON THE GROUND. THE SMELL WOULD DISSIPATE WHEN THE E.C.S. WAS TURNED OFF. INVESTIGATION REVEALED A VERY BLACK AND DIRTY WATER SEPARATOR BAG AND DUCTS DOWNSTREAM OF THE REFRIGERATION PACK. THESE COMPONENTS HAD BEEN CLEA NED AND INSPECTED ON THE PREVIOUS 100 HOUR INSPECTION. THERE WAS NO TRACE OF OIL IN THE BLEED AIR DUCTS BEFORE THE REFRI GERATION PACK. IT WAS SUSPECTED THAT THE COOLING TURBINE HAD A INTERNAL OIL LEAK CAUSING THE BURNED OIL SMELL. THE REFRI GERATION PACK WAS REPLACED AND NO FURTHER PROBLEMS WERE NOTICED. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001051500382 20010515 00382 EU 2001 5 15 CA010507022 1 20010428 A 2434 9789601090 BRUSH HOLDER PILATS 5243212158 PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL GENERATOR WORN W K NONE O OTHER IN INSP/MAINT 1 CA 105 100318 (CAN) DURING A 100 HOUR INSPECTION, THE BRUSH ASSEMBLY WASREMOVED TO VERIFY THE CONDITION. THE BRUSH ASSEMBLY WAS WORN E XCESSIVELY, AND HAS BEEN REPLACED. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001051500383 20010515 00383 EU 2001 5 15 CA010508002 1 20010420 A 2911 9603001291 ACCUMULATOR PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL HYD POWER PACK LEAKING W H DEACTIVATE SYST/CIRCUITS R PARTIAL RPM/PWR LOSS CL CLIMB 1 CA 1497 (CAN) PILOT REPORTED LANDING GEAR FAILED TO LOCK UP IN RETRACTED POSITION. GEAR WAS SELECTED DOWN AND EMERGENCY HAND PUM P WAS USED TO LOCK GEAR IN PLACE. THE AIRCRAFT WAS THEN FLOWN TO MAINTENANCE BASE WITH GEAR DOWN. THIS SYSTEM HAS THE HY DRAULIC PUMP PRESSURE SWITCH ON THE NITROGEN SIDE OF THE ACCUMULATOR. WHEN THE SWITCH WAS REMOVED THERE WAS HYDRAULIC FL UID IN THE NITROGEN SIDE OF THE ACCUMULATOR. THE ACCUMULATOR WAS REPLACED AND GEAR RETRACTION AND EXTENSION FUNCTIONAL T EST CARRIED OUT. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001051500384 20010515 00384 EU 2001 5 15 CA010508003 1 20010418 A 5270 9733024202 SWITCH PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL CARGO DOOR BENT W D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CA 1516 (CAN) AFTER START UP PILOT NOTICED THE CARGO DOOR LIGHT WAS ON. HE SHUT DOWN AND CONFIRMED THE DOOR WAS CLOSED, THEN ADV ISED MAINTENANCE OF THE PROBLEM. THE DOOR HANDLE SWITCH LEVER ROLLER SPRING WAS FOUND BENT. THE SPRING WAS STRAIGHTENED AND ADJUSTED. AFTER PERFORMING FUNCTIONAL TESTS THE AIRCRAFT WAS RETURNED TO SERVICE. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001051500386 20010515 00386 EU 2001 5 15 CA010508005 1 20010418 A 2434 5005012235 BRUSHES PILATS 5243212158 PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL GENERATOR WORN W K NONE O OTHER IN INSP/MAINT 1 CA 265 (CAN) 1) NR 2 GENERATOR, S/N 100222, INSTALLED, 00-07-02 AT 3200.6 A/F HRS. 2) NR 2 GENERATOR, S/N 100222, FAILED, 00-12 -20 AT 3468.1 A/F HRS. TTSO: 267.5 HRS., FAILURE DUE TO WORN BRUSHES. 3) NR 2 GENERATOR, S/N 100262, INSTALLED 00-12-20 AT 3468.1 A/F HRS. POST SB 24-016 (REPLACEABLE BRUSH BLOCK).4) NR 2 GENERATOR FAILED, S/N 100262, 01-03-28 AT 3723.8 A/F HRS. TTSO: 264.7 HRS., FAILURE DUE TO WORN BRUSHES. 5) NEW BRUSH PACK INSTALLED, 01-03-28 AT 3723.8 A/F HRS. GENERATOR STILL IN SERVICE. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001051500387 20010515 00387 CE 2001 5 15 CA010508006 1 20010420 A 2434 C611503104RX ALTERNATOR FORD CESSNA 210 210R 2073458 CE CONT O520 IO520L 17032 SO MCAULY D3A34 D3A34C404 GL ELECTRICAL FAILED W O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 CA 7 97043226 (CAN) PILOT REPORTED 1 ALTERNATOR OFF LINE LIGHT CAME ON IN FLIGHT. FURTHER INVESTIGATION WHEN AIRCRAFT RETURNED TO BASE , REVEALED THAT THE PULLY/FAN AND RETAINING NUT HAD SEPARATED FROM THE ALTERNATOR. 1 H 7 1 3O 3 O RT 3A21 E5CE 5 C P47GL 2001051500391 20010515 00391 2001 5 15 CA010508010 4 20010424 A 2562 BRACKET CESSNA 172 172P 2072436 CE LYC O360 O360A4M 41514 EA ELT LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 829 (CAN) MOUNTING BRACKET FOR PORTABLE ELT ANTENNA HAS LOOSE FIT AND ALLOWS ANTENNA TO FALL OUT. MS 28775-009 O-RING USED T O RETAIN ANTENNA. 1 H 7 1 3O 3 O NT 3A12 E286 2001051500395 20010515 00395 SO 2001 5 15 CA010508015 1 20010330 A 2910 121720210703 LINE EMB 110 EMB110P1 3260122 SO PWA PT6 PT6A34 52043 EA HYD SYSTEM CRACKED W O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA (CAN) DURING CLIMB, HYDRAULIC FLUID LOW LEVEL WARNING LIGHT ILLUMINATED. MANUAL GEAR EXTENSION PERFORMED, AIRCRAFT LANDE D SAFELY. MAINTENANCE FOUND A CRACKED HYDRAULIC LINE IN THE L/H MAIN WHEEL BAY HYDRAULIC LINE REPLACED, HYDRAULIC SYSTEM SERVICED. HYDRAULIC SYSTEM PRESSURE CHECKED. NO FURTHER LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 4T 4 T A21SO E4EA 2001051500400 20010515 00400 CE 2001 5 15 CA010509007 1 20010411 A 5320 05530072 STIFFENER CESSNA 172 172M 2072418 CE LYC O320 O320E2D 41508 EA FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 5507 (CAN) THE REINFORCEMENT RIVETED TO THE FIREWALL AT THE MIDDLE RT LOWER COWL ATTACH BRACKET WAS FOUND CRACKED. THE ATTACH BRACKET SITS ON TOP OF THE REINFORCEMENT (SANDWICHED BETWEEN THE FIREWALL AND BRACKET). THE CRACK WAS FOUND AT A 200 HR INSPECTION AND WAS VISIBLE BEYOND THE ATTACH BRACKET. 1 H 7 1 3O 3 O NT 3A12 E274 2001051500401 20010515 00401 NM 2001 5 15 CA010509009 1 20010417 A 2910 82970010391 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 29111 (CAN) THE FLIGHT CREW REPORTED THE NR 2 HYDRAULIC QUANTITY WAS LOW. MAINTENANCE FOUND THE RIGID HYDRAULIC PRESSURE TUBE LEAKING AT THE R/H MLG DOOR SOLENOID SEQUENCE VALVE. THE PRESSURE TUBE WAS REPLACED, GEAR SWINGS CARRIED OUT AND THE SYS TEM LEAK CHECKED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001051500402 20010515 00402 NM 2001 5 15 CA010509010 1 20010410 A 7921 28E997 OIL COOLER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE ENGINE CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 15177 (CAN) MAINTENANCE NOTICED OIL LEAKING FROM THE RT OIL COOLER AREA. THE RIGHT OIL COOLER WAS REPLACED AND ALL CHECKS COMP LETED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001051500403 20010515 00403 NM 2001 5 15 CA010509011 1 20010417 A 3231 54C546349 SEQUENCE VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE MLG DOOR LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 29111 (CAN) THE FLIGHT CREW REPORTED NR 2 HYDRAULIC SYSTEM WAS LOW. UPON INVESTIGATION, MAINTENANCE DISCOVERED THE RT MLG DOOR S SOLENOID SEQUENCE VALVE WAS LEAKING FLUID WHILE UNDER PRESSURE.THE RT SOLENOID SEQUENCE VALVE WAS REPLACED, GEAR SWING S WERE CARRIED OUT AND THE SYSTEM LEAK CHECKED, SERVICEABLE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001051500404 20010515 00404 NM 2001 5 15 CA010509012 1 20010509 A 2910 82950010207 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 31737 (CAN) RT LIFT DUMP PRESSURE HYDRAULIC LINE FOUND LEAKING FROM A BEND IN THE LINE LOCATED APPROXIMATELY 6 INCHES FROM THE FITTING IN THE RIGHT NACELLE. THE HYDRAULIC LINE WAS REPLACED AND ALL CHECKS COMPLETED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001051500406 20010515 00406 CE 2001 5 15 CA010509016 1 20010409 A 2821 FUEL FILTER MTSBSI MU2 MU2B60 5780460 CE GARRTT TPE331 TPE33110 01514 WP RT WING DAMAGED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) CREW INFORMED MAINT THAT THEY HAD SLIGHT FUEL LEAK AT RT WING NEAR AIRFRAME FUEL FILTER BOWL. MAINT REMVD ACCESS P ANEL & DRIED EXCESS FUEL OFF FILTER HOUSING. FUEL AGAIN VISIBLE AT FILTER HEAD, ALL LINES IN AREA WERE INSP FOR LEAKS BU T NONE WERE FOUND. MAINT ACTIVATED BOOST PUMP TO PRESSURIZE BOWL, IT FOUND THAT HEAD LEAKING AT ATTACHING FLANGE AREA. C LOSER INSP FOUND FILTER HEAD IS ACTUALLY COMPRISED OF 2 PIECES HELD TOGETHER BY 3 COUNTERSUNK ALLEN HEAD SCREWS. ATTACH ED FLANGE ACTUALLY HOUSES DIAPHRAGM & SWITCH ASSY FOR FUEL FILTER BYPASS INDICATING SYS. SINCE IS NO GASKET SEALING THES E 2 PARTS, IT IS ASSUMED THAT DIAPHRAGMACTUALLY SEALS SWITCH CAVITY. IT IS ALSO ASSUM 1 H 7 2 3T 4 T RT A10SW E4WE 2001051500410 20010515 00410 EU 2001 5 15 CA010510006 1 20010428 A 2782 153B000601 SLEEVE LUCAS CHA1061004 AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE SLAT ACTUATOR WORN W O OTHER F FLT CONT AFFECTED DE DESCENT 1 CA 217 (CAN) SLATS WOULD NOT EXTEND DUE TO HIGH TORQUE REQUIRED TO ACTIVATE THE BALL SCREW.PROBABLY CAUSED BY POOR LUBRICATION LEADING TO WORN SLEEVE. 2 L 7 2 4F 4 F RT A35EU E23EA 2001051500415 20010515 00415 2001 5 15 CA010510013 4 20010324 A 2312 KTR9100A PANEL AIRBUS A319 A319114 NM RADIO MANAGEMENT FAILED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) STRONG BURNT ELECTRICAL SMELL IN THE FLIGHT DECK AS THE FIRST OFFICER RADIO MANAGEMENT PANEL WENT DEAD.NO SMOKE RE PORTED.REPLACED THE FIRST OFFICER RMP. 2 L 7 2 4F RT A28NM 2001051500416 20010515 00416 EU 2001 5 15 CA010510014 1 20010402 A 2120 FILTER AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE RECIRC SYS CONTAMINATED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CA (CAN) AFTER TAKEOFF, THE COCKPIT AND CABIN FILLED WITH STRONG FUMES. CREW REQUIRED OXYGEN TO OPERATE AIRCRAFT, LANDED WI THOUT ANY FURTHER INCIDENT. AIRCRAFT WAS DE-ICED 3 TIMES PRIOR FLIGHT, AIR CONDITION PACKS WERE ON WITH APU BLEED. MAINT ENANCE ACTION: WITH AIRCRAFT ENGINES ON LOW POWER, AIRCRAFT PRESSURIZED, PACKS OPERATED WITH APU PNEUMATIC SUPPLY, NIL F AULT FOUND. SUSPECT GLYCOL INGESTION FROM DE-ICING. CHANGED RECIRCULATION FILTERS DUE CONTAMINATED WITH GLYCOL. 2 L 7 2 4F 4 F RT A28NM E29NE 2001051500417 20010515 00417 EU 2001 5 15 CA010510015 1 20010402 A 2530 OVEN AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE GALLEY SMOKE W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CA (CAN) ONE GALLEY UNIT STARTED SMOKING AFTER TAKEOFF. J CLASS OVEN 5877 TURNED OFF.FOUND FOOD SPILLED ON ELEMENT. OVEN CL EANED, FUNCTIONAL CHECK CARRIED OUT NIL FAULT. 2 L 7 2 4F 4 F RT A28NM E29NE 2001051500418 20010515 00418 NM 2001 5 15 CA010510018 1 20010422 A 2410 740119D GENERATOR AIRBUS A319 A319114 NM NR 2 FAILED W O OTHER H ELECT. POWER LOSS-50 PC CR CRUISE 1 CA (CAN) FLIGHT INTO WINNIPEG, NR 2 INTEGRATED GENERATOR DISCONNECTED DUE LOW OIL PRESSURE LIGHT. APPROXIMATELY 40 MINUTES LATER, NR 1 INTEGRATED DRIVE GENERATOR WAS DISCONNECTED DUE FAILURE.AIRCRAFT OPERATED WITH AUXILIARY POWER UNIT GENERATO R.INTEGRATED DRIVE GENERATOR CHANGED ON NR 1 AND 2 ENGINE, SYSTEM CHECKED SERVICEABLE. 2 L 7 2 4F RT A28NM 2001051500419 20010515 00419 EA 2001 5 15 CA010510019 1 20010510 A 2740 70608 CONTROL UNIT CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE STABILIZER FAILED W A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 CA (CAN) AFTER TAKEOFF, UNABLE TO TRIM AIRCRAFT HORIZONTAL STABILIZER, AIRCRAFT RETURN TO OTTAWA, UNDER QRH PROCEDURE. RESE T ATTEMPTED WITH NO SUCCESS. FOUND TO BE THE HORIZONTAL STAB TRIM CONTROL UNIT AT FAULT. REPLACED THE HORIZONTAL STAB TR IM CONTROL UNIT. OPERATIONAL AND FUNCTIONAL TEST CARRIED OUT AS PE TASK 27-40-00-710-801 AND 27-40-00-720-801 TESTED OK. 2 L 7 2 4F 4 F RT A21EA E15NE 2001051500420 20010515 00420 EA 2001 5 15 CA010510020 1 20010328 A 3230 46193 ISOLATION VALVE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE MLG FAILED W O OTHER J WARNING INDICATION NR NOT REPORTED 1 CA 356 (CAN) EICAS CAUTION MESSAGE FOR GEAR DISAGREE WHEN GEAR SELECTED, ALL INDICATION TO NORMAL AFTER SEVERAL SECONDS. AFTER TROUBLESHOOTING AND AFTER THE REPLACEMENT OF 3A AND 3B HYDRAULIC PUMPS WITH A NIL FIX, THEY ISOLATED THE PROBLEM TO BE T HE MAIN LANDING GEAR ISOLATION VALVE.REPLACED THE MAIN LANDING GAR ISOLATION VALVE. GEAR SWING CARRIED OUT AND CONSIDERE D SERVICEABLE. 2 L 7 2 4F 4 F RT A21EA E15NE 2001051500421 20010515 00421 EA 2001 5 15 CA010510021 1 20010419 A 5610 NP1393211 WINDSHIELD CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE COCKPIT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ON TAXI IN YYZ THE CAPTAINS WINDSCREEN CRACKED. WINDSHIELD AND HEAT CONTROLLER REPLACED AS PER MAINTENANCE MANUAL TASKS 56-11-01-000-801 AND 56-11-01-400-801.HEAT CONTROLLER P/N 1659-1 2 L 7 2 4F 4 F RT A21EA E15NE 2001053100130 20010531 00130 NM 2001 5 31 AWXA0001694 1 20010507 A 5312 65163007 BULKHEAD BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 ULTRASONIC INSP REVEALS CRACK VERT POSITION AT I/B EDGE LBL 5.7 AT WL 234 BS 178 LOCATION .75 INCH LENGTH. REPAIRED IAW SRM 53-10-11 FIG 1 DETAIL III AND SRM 51-30-2 PG 5 AND REF DWG 65-16300. 2 L 7 2 4F RT A16WE 2001051500464 20010515 00464 WP 2001 5 15 GTIA010109 1 20010413 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN EXPOSED A K NONE O OTHER NR NOT REPORTED 1 GL 23 DALLR 53015 E.M. LIGHTS HAS SOME WIRES PROTRUDING, ROW 9. REINSTALLED LAMP AND REPOSITIONED WIRES IAW STANDARD WIRING PRACTICES MAN UALLY. OPS CHECK GOOD IAW MM 33-50-00. (M) 2 L 7 2 4F RT A6WE 2001051500465 20010515 00465 WP 2001 5 15 GTIA010105 1 20010410 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 DALLR 53015 DTW - CABIN EMERGENCY FLOOR TRACK LIGHT INOPERATIVE AT ROW 9. REPLACED BULB, OPS CHECKED GOOD IAW MD80 MM 33-53-00. (M ) 2 L 7 2 4F RT A6WE 2001051500466 20010515 00466 2001 5 15 GTIA010108 4 20010415 A 2565 CABLE DOUG DC9 DC981 3022081 WP EVAC SLIDE DISCONNECTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48016 R1 DOOR GIRT BAR CABLE DISCONNECTED. CONNECTED R1 GIRT BAR IAW MD80 MM 25-62-04. OPS CHECK GOOD, NO OTHER DEFECTS NOTE D AT THIS TIME. (M) 2 L 7 2 4F A6WE 2001051500467 20010515 00467 WP 2001 5 15 GTIA010107 1 20010413 A 2560 ESCAPE ROPE DOUG DC9 DC982 3022082 WP COCKPIT LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48087 DTW - FLT 1696 - CAPT ESCAPE ROPE LOOSE. REINSTALED ESCAPE ROPE IAW MD80 MM 25-60-00. (M) 2 L 7 2 4F A6WE 2001051500468 20010515 00468 WP 2001 5 15 GTIA010106 1 20010410 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 DALLR 53015 DTW - CABIN EMERGENCY FLOOR TRACK LIGHT INOPERATIVE AT ROW 11. REPLACED BULB, OPS CHECKED GOOD IAW MD80 MM 33-53-01. ( M) 2 L 7 2 4F RT A6WE 2001051500469 20010515 00469 WP 2001 5 15 GTIA010104 1 20010410 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 DALLR 53015 DTW - CABIN EMERGENCY FLOOR TRACK LIGHT INOPERATIVE AT ROW 5. REPLACED BULB, OPS CHECKED GOOD IAW MD80 MM 33-53-00. (M ) 2 L 7 2 4F RT A6WE 2001051500470 20010515 00470 WP 2001 5 15 GTIA010103 1 20010403 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A K NONE L NO TEST IN INSP/MAINT 1 GL 23 814NK 49619 EMERGENCY PATH LIGHTING PORTION NO LIGHTS. FOUND DISCONNECTED WIRES AT SEVERAL AREA, RECONNECTED WIRES. OPS CHECK NORM AL. (M) 2 L 7 2 4F RT A6WE 2001051500471 20010515 00471 WP 2001 5 15 GTIA010102 1 20010413 A 3350 58222 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 131NK 47605 FLL - ELS BATTERY INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OPS CHECK OK IAW MM 33-50-00. (M) 2 L 7 2 4F A6WE 2001051500472 20010515 00472 WP 2001 5 15 GTIA010101 1 20010409 A 3240 95607887 FITTING DOUG DC9 DC931 3022065 WP NR 1 BRAKE LEAKING A GTIA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 23 969ML 47268 FLT 284 - ACY - FOUND NR 1 BRAKE IS LEAKING AT AFT UPPER FITTING. REMOVED AND REPLACED NR 1 BRAKE ASSEMBLY IAW DC-9 MM 32-40-01. OPS AND LEAK CHECK GOOD AT THIS TIME. (M) 2 L 7 2 4F A6WE 2001051500473 20010515 00473 WP 2001 5 15 GTIA010100 1 20010412 A 2841 372001001 INDICATOR DOUG DC9 DC981 3022081 WP COCKPIT FAILED A GTIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 806NK 48051 DTW - FLT 629 - AFTER PUSHBACK, ALL FUEL QUANTITY VARIED BY SEVERAL THOUSAND LBS, WENT BLANK, FLASHED ETC. REPLACED FUE L QUANTITY INDICATOR. OPS CHECK NORMAL IAW MD-80 MM 28-40-00. (M) 2 L 7 2 4F A6WE 2001051500474 20010515 00474 WP 2001 5 15 GTIA010099 1 20010413 A 5250 PANEL DOUG DC9 DC981 3022081 WP COCKPIT DOOR UNSECURE A GTIA K NONE O OTHER CR CRUISE 1 GL 23 811NK 48017 FLT 1594 - COCKPIT DOOR KEEPS FALLING OUT. RESECURED COCKPIT DOOR LEFT BLOW OUT PANEL IAW MD-80 MM 52-10-00. NO FURTHE R DEFECTS NOTED. (M) 2 L 7 2 4F A6WE 2001051500475 20010515 00475 WP 2001 5 15 GTIA010098 1 20010412 A 3260 PROXIMITY SWITCH DOUG DC9 DC982 3022082 WP NLG DIRTY A GTIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 23 800NK 49144 DTW - FLT 521 - AFTER PUSHBACK, NOSE GEAR INDICATOR FLUCTUATED FROM RED TO GREEN. CLEANED PROX SWITCH AND PLUG FOR NOSE GEAR. OPS CHECK GOOD IAW MD-80 MM 32-60-00. NO DEFECTS NOTED AT THIS TIME. (M) 2 L 7 2 4F A6WE 2001051500476 20010515 00476 2001 5 15 GTIA010097 4 20010407 A 2210 AUTOPILOT SYS DOUG DC9 DC941 302207N WP COCKPIT MALFUNCTIONED A GTIA K NONE O OTHER CR CRUISE 1 GL 23 130NK 47604 FLT 72 - FLL - AUTO PILOT WILL NOT ENGAGE AT ALL. CHECKED THE AUTO PILOT OPERATIONS. FUNCTIONS NORMAL. TALKED TO THE CAPTAIN, HE STATED AUTO PILOT IS NORMAL BOTH ON GROUND AND IN FLIGHT. NO FAULT FOUND. THIS CLEARS DMI NR 0001619-1. P LACARDS REMOVED IAW DC-9 MM 22-10-00. (M) 2 L 7 2 4F A6WE 2001051500477 20010515 00477 2001 5 15 GTIA010095 4 20010401 A 2210 AUTOPILOT SYS DOUG DC9 DC982 3022082 WP COCKPIT MALFUNCTIONED A GTIA K NONE O OTHER CR CRUISE 1 GL 23 957AS 49126 LGA - FLT 600 - AUTO PILOT WILL NOT STAY CONNECTED IN DFGC NR 1 POSITION. TRANSFERRED TO DMI NR 0013680-1, PER MEL REF 22-15-00. PLACARDS INSTALLED CAT C. (M) 2 L 7 2 4F A6WE 2001051500478 20010515 00478 2001 5 15 GTIA010094 4 20010411 A 3425 6224507001 ADI DOUG DC9 DC982 3022082 WP COCKPIT MALFUNCTIONED A GTIA K NONE O OTHER CR CRUISE 1 GL 23 957AS 49126 FLT 679 - FLL - AUTOPILOT WILL NOT STAY ENGAGED WHEN SELECTED TO NR 1 POSITION. REMOVED AND REPLACED CAPTAINS ADI. OPS CHECK OK IAW MM 34-24-00. ALSO PERFORMED RTS CHECK. NO FAULTS, NO FAILURES. AUTO PILOT ENGAGES NORMAL. (M) 2 L 7 2 4F A6WE 2001051500479 20010515 00479 NE 2001 5 15 20010514SG001 2 20010225 A 7250 TURBINE BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE SEPARATED A MYWA E C ENGINE SHUTDOWN ABORTED TAKEOFF T K ENGINE CASE PENETRATION FLUID LOSS TO TAKEOFF 1 SO 19 804MA 22435 685520 AT TAKEOFF THRUST SETTING (ANV) LOUD EXPLOSION HEARD IN COCKPIT AND NR 1 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED AND O IL QTY DECREASED TO 2 GAL THEN INCREASED TO 3 GAL AFTER SHUTDOWN. ABORTED TAKEOFF AND PERFORMED EMERGENCY ENGINE SHUTDO WN PROCEDURES PER AOM 2-1-2. RETURNED TO RAMP. OIL PRESSURE ALSO DECREASED TO 20 PSI AND CONTINUED TO DECREASE. DISCO VERED T3 AND T4 HAD SEPARATED FROM ENGINE CAUSING DAMAGE TO TAIL PIPE ASSEMBLY. REMOVED AND REPLACED NR 1 ENGINE. OPS CHECK OK. LEAK CHECKED OK IAW B727 MM 71-00. (M) 2 L 7 3 4F 4 F A3WE E2EA 2001051500480 20010515 00480 NM 2001 5 15 20010514SG002 1 20010406 A 2897 WIRE BOEING 727 727225 1384077 NM SHUT OFF VALVE BURNED A I CABIN DEPRESSURIZATION J WARNING INDICATION CR CRUISE 1 SO 19 804MA 22435 DURING FLIGHT PLS/JFK, LEFT DUMP NOZZLE VALVE CAME ON INTERMITTENTLY. DEACTIVATED LEFT FUEL NOZZLE DUMP VALVE CLOSED AN D SAFETIED IAW MEL 28-9, TRANSFERRED TO DMI SLIP 1226. NO POWER TO PIN B AT CANNON PLUG. OPENED WING PANELS FOR INSPEC TION. FOUND BURNED WIRES AT WING STATION 546. REPAIRED WIRES AS REQUIRED FOR LEFT FUEL SHUTOFF VALVE IAW B727 SWPM REF 20-10-13. OPS CHECK NORMAL. CLEARED DMO. (M) 2 L 7 3 4F A3WE 2001051500481 20010515 00481 NM 2001 5 15 20010514SG003 1 20010403 A 3350 90053A CHARGER BOEING 727 727225 1384077 NM CABIN INOPERATIVE A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 803MA 22434 ON PREFLIGHT TRANSIT, FOUND R2 ''EMERGENCY EXIT'' SIGN LIGHT ABOVE DOOR INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AND CHARGER IAW MM 33-50-71. OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 2001051500482 20010515 00482 NM 2001 5 15 20010514SG004 1 20010309 A 3350 900835A BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 802MA 245 DURING P/T, FOUND CENTER AISLE EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AIW MM 33-50-72. OPS CH ECK GOOD. (M) 2 H 7 2 4T RT A13NM 2001051500483 20010515 00483 NM 2001 5 15 UIEA01038 1 20010410 A 5311 FRAME BOEING 747 7472D7B 1384803 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 77417 22337 DURING INSPECTION, FOUND FRAME CRACKED STATION 800 STRINGER 17L ADJACENT TO 2L MED. STOP DRILL NOT REQUIRED DUE CRACK R AN OFF END OF FRAME. FABRICATED REPAIR STACK UP DOUBLERS. INSTALLED PER STANDARD SRM PRACTICES. REF SB 53-10-04 FIG 1 14. (M) 2 L 7 4 4F RT A20WE 2001051500484 20010515 00484 NM 2001 5 15 UIEA01037 1 20010410 A 5330 65B0443513 SKIN BOEING 747 7472D7B 1384803 NM FUSELAGE CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 77417 15704 22337 DURING INSPECTION, FOUND SKIN CORROSION AT 4L MED LOWER AFT CORNER CUT OUT. TRIMMED AWAY CORRODED AREA. FABRICATED FIL LER AND REPAIR STACK UP DOUBLERS. INSTALLED FASTENERS PER STANDARD SRM 51-30-02 PRACTICES. (M) 2 L 7 4 4F RT A20WE 2001051500485 20010515 00485 NM 2001 5 15 UIEA01036 1 20010410 A 5330 SKIN BOEING 747 7472D7B 1384803 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 77417 15704 22337 DURING HFEC INSPECTION, FOUND UPPER FORWARD CORNER OF AFT LOWER LOBE CARGO COMPT CRACKED .87 INCHES AT BS 1815, STRINGER 27R. TRIMMED OUT CRACKED AREA. FABRICATED FILLER AND REPAIR STACK UP DOUBLERS PER SRM 53-30-03 FIG 60, TYPE II. INST ALLED PER SRM REPAIR SCHEME AS NOTED ABOVE. (M) 2 L 7 4 4F RT A20WE 2001051500486 20010515 00486 NM 2001 5 15 UIEA01035 1 20010410 A 5320 65B13346607 ANGLE BOEING 747 7472D7B 1384803 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 77417 15704 22337 DURING ROUTINE INSPECTION, FOUND CEILING ZEE CHORD ANGLE CRACKED IN LEFT BODY GEAR WHEEL WELL AT BS 1438 AND LBL 107. T RIMMED AWAY DAMAGED AREA. FABRICATED FILLER AND REPAIR ANGLES. INSTALLED PER STANDARD SRM PRACTICES. (M) 2 L 7 4 4F RT A20WE 2001051500487 20010515 00487 NM 2001 5 15 UIEA01034 1 20010410 A 5311 65B154611 FRAME BOEING 747 7472D7B 1384803 NM FUSELAGE DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 77417 15704 22337 DURING ROUTINE INSPECTION, FOUND UPPER CHORD WITH CRITICAL HOLE ELONGATED AT BS 1265L AT WL 197. STACK UP DOUBLERS REMO VED. AREA CHECKED, PREVIOUS CRACKS CONTAINED. ALL HOLES IN STACK UP DOUBLERS OVERSIZED. OVERSIZED FASTENERS INSTALLED PER STANDARD PRACTICES. REPAIR SUBJECT TO REPETETIVE INSPECTIONS. (M) 2 L 7 4 4F RT A20WE 2001051500488 20010515 00488 NM 2001 5 15 UIEA01031 1 20010410 A 5311 65B018499 FRAME BOEING 747 7472D7B 1384803 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 77417 22337 DURING HFEC INSPECTIN PER D6-7170 PART 6, 51-00-00, INSPECTION FOUND BS 2231 FRAME CRACK INDICATION AT STRINGER 25L. CR ACK CONFIRMED. CRACK AREA TRIMMED OUT. FILLERS AND STRAP DOUBLERS FABRICATED. INSTALLED PER SRM 51-30-02 AND STANDARD PRACTICES. REF SB 747-53A2450. (M) 2 L 7 4 4F RT A20WE 2001051500489 20010515 00489 WP 2001 5 15 USAAD01081 1 20010413 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 819US 48099 IND - THE LOW LEVEL EMERGENCY LIGHTS AND SEVERAL CABIN CEILING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL AND CABIN CEILING EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001051500490 20010515 00490 WP 2001 5 15 20010514SG005 1 20010413 A 3350 AD4002P BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 819US 48099 IND - THE LOW LEVEL EMERGENCY LIGHTS AND SEVERAL CABIN CEILING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL AND CABIN CEILING EMERGENCY LIGHT BATTERIES. REF USAAD01081. (M) 2 L 7 2 4F A6WE 2001051500491 20010515 00491 WP 2001 5 15 USAAD01044 1 20010308 A 3260 833703 PROXIMITY SENSOR DOUG DC9 DC981 3022081 WP NLG FAILED A USAA K NONE N FALSE WARNING CL CLIMB 1 EA 19 808US 48040 MSY-CLT - FLT 1278 - AFTER LANDING GEAR RETRACTION, THE RED NOSE GEAR INDICATION LIGHT REMAINED LIT. THE LANDING GEAR W AS CYCLED AND THE LIGHT WENT OUT BUT CAME BACK ON 5 MINUTES LATER. THE AIRCRAFT CONTINUED TO THE NEXT STATION AND LANDE D WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE GEAR UP/DOWN AND LOCKED POSITION PROXIMITY SENSOR ASSEMBLY. THE AIRC RAFT WAS JACKED AND THE LANDING GEAR WAS CYCLED. ALL CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 2001051500492 20010515 00492 WP 2001 5 15 USAAD01054 1 20010317 A 3222 STRUT DOUG DC9 DC981 3022081 WP NLG LOW A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 808US 48040 EWR-PIT - FLT 557 - AFTER TAKEOFF, THE NOSE LANDING GEAR RED INDICATION LIGHT REMAINED ON AND THE NOSE LANDING GEAR RETR ACTED INDICATION PIN WAS NOT VISIBLE. THE LANDING GEAR WAS EXTENDED AND THE AIRCRAFT DIVERTED TO LGA AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICED THE NOSE LANDING GEAR STRUT AND REPLACED THE SCHRADER VALVE AS PRECAUTION. (M) 2 L 7 2 4F A6WE 2001051500493 20010515 00493 NE 2001 5 15 ASOA01040 2 20010415 A 7200 ENGINE AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE RT ENGINE MALFUNCTIONED A ASOA A UNSCHED LANDING A B FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 11 535AS 464 124490 FLT 4137 - DURING FLIGHT FROM ATL TO VPS, PASSENGER AND FLIGHT ATTENDANT REPORTED SPARKS AND FLAMES COMING FROM THE RIGH T ENGINE. AN EMERGENCY WAS DECLARED, BUT THE FIRE BOTTLE WAS NOT BLOWN. THE AIRCRAFT RETURNED TO ATL SAFELY. ENGINE W AS SHUT DOWN ON GROUND. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE. OPS AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURN ED TO SERVICE. AWAITING TEAR DOWN REPORT ON ENGINE. (M) 2 H 7 2 4T 4 T RT E20NE 2001051500494 20010515 00494 EA 2001 5 15 ASOA01039 1 20010414 A 2131 CONTROLLER CNDAIR CL600 CL6002B19 EA CABIN PRESSURE FAILED A ASOA G O2 MASK DEPLOYED O OTHER CR CRUISE 1 SO 11 827AS 7212 DSM-ATL - FLT 4756 - DURING FLIGHT, CAPTAIN REPORTED PRESSURE UNCONTROLLABLE IN AUTO AND MANUAL. CREW RESET PRESSURE AN D MASKS DROPPED. AT FL100 CABIN ALTITUDE 15000 DP -2.1 TO -4.1. CABIN ALTITUDE AND DP WAS FLUCTUATING UP AND DOWN DURN IG DESCENT. AIRCRAFT LANDED SAFELY IN ATL. 2 L 7 2 4F RT A21EA 2001051500495 20010515 00495 WP 2001 5 15 ASAA0180123 1 20010331 A 3350 0105606005 LIGHT DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 SEA - DURING PRE-FLIGHT CHECK, FOUND AN EMERGENCY FLOOR TRACK LIGHT WIRING EXPOSED, DISCONNECTED IN 1ST CLASS CABIN. RE CONNECTED FLOOR TRACK LIGHT WIRING. TRACK LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001051500496 20010515 00496 WP 2001 5 15 ASAA0180122 1 20010331 A 3350 41B004AD07G3 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 977AS 53453 PDX - DURING LINE CHECK, OVERHEAD EMERGENCY LIGHTS AT ROW 8-12 WERE DETERMINED TO BE INOPERATIVE. REMOVED AND REPLACED BATTERIES WITHIN ASSOCIATED BATTERY PACK ASSEMBLY. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001051500497 20010515 00497 NM 2001 5 15 ASAA0110169 1 20010331 A 3397 8731002 WIRE BOEING 737 737290C 138448V NM CABIN DISCONNECTED A K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING MAINTENANCE CHECK, FOUND WIRES DISCONNECTED TO LIGHTED EMERGENCY EXIT SIGN. RECONNECTED WIRES AND LIGHT OP ERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2002010800161 20020108 00161 2002 1 8 ASAA0180120 4 20010329 A 2565 D29984103 WIRE HARNESS DOUG DC9 DC983 3022083 WP EVAC SLIDE FAILED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OAK - DURING C-CHECK, AFT PAX (TAILCONE) DOOR EMERGENCY SLIDE HARNESS FAILED THE AMPERAGE CHECK. REMOVED AND REPLACED T HE AFT DOOR EMERGENCY SLIDE HARNESS. (M) 2 L 7 2 4F RT A6WE 2001051500498 20010515 00498 WP 2001 5 15 ASAA0180125 1 20010402 A 3350 0105606005 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 950AS 53023 LAX - DURING PREFLIGHT, FOUND THE EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE FROM ROW 13 THROUGH 15. RECONNECTED LIGHT CO NNECTOR AT ROW 15. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001051500499 20010515 00499 NE 2001 5 15 20010514SG006 1 20010327 A 2913 167N1001 PUMP SKRSKY S61 S61N 8142104 NE ENGINE FAILED A ERAA O OTHER O OTHER LD LANDING 1 AL 03 563EH 914 61808 LANDING GEAR DID NOT DEPLOY NORMALLY. EMEREGNCY BLOW DOWN PROCEDURES EMPLOYED PER ROTORCRAFT FLIGHT MANUAL. HYDRAULIC PUMP MOTOR FAILURE CAUSED LACK OF PRESSURE TO OPERATE GEAR. DATE OF LAST INSPECTION WAS FEB 25, 2000. TYPE OF LAST INS PECTION WAS OVERHAUL. THE TBO FOR THE PUMP/MOTOR IS 2000 HOURS. (M) 2 G 7 2 4U 1H15 2001051500500 20010515 00500 NM 2001 5 15 20010514SG007 1 20010331 A 2910 6517840118 HYDRAULIC LINE BOEING 727 72722C 138400F NM HYD SYSTEM BROKEN A RYNA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 07 421EX 19099 LOST ''A'' SYSTEM HYDRAULICS IN FLIGHT. RAN APPROPRIATE CHECK LIST. EMERGENCY DECLARED. REMOVED AND REPLACED BROKE HY DRAULIC LINE ON NR 2 SPOILER ACTUATOR. (M) 2 L 7 3 4F A3WE 2001051500501 20010515 00501 NM 2001 5 15 P2EA001030 1 20010329 A 5730 SKIN BOEING 737 737244 138448U NM RT WING CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 OKC - DURING C-CHECK, FOUND THE RIGHT WING CENTER SECTION LOWER SKIN SURFACE ABOVE THE RIGHT RAM AIR DUCT WITH CORROSION OUT OF LIMITS AT RBL 40.5 THROUGH 43.5, STRINGER 4C AND 5C. REMOVED CORROSION AND TREATED. (M) 2 L 7 2 4F A16WE 2001051500502 20010515 00502 NM 2001 5 15 P2EA001031 1 20010329 A 5730 SKIN BOEING 737 737244 138448U NM LT WING CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 OKC - DURING C-CHECK, FOUND THE LEFT WING CENTER SECTION LOWER SKIN SURFACE ABOVE THE LEFT RAM AIR DUCT WITH CORROSION O UT OF LIMITS AT LBL 41, STRINGER 5C. REMOVED CORROSION AND TREATED. (M) 2 L 7 2 4F A16WE 2001051500503 20010515 00503 NM 2001 5 15 P2EA001032 1 20010404 A 5330 SKIN BOEING 737 737244 138448U NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 OKC - DURING C-CHECK, FOUND THE FORWARD FUSELAGE SKIN T STATION 196.5 AT LBL 3 WITH CRACK, .75 INCH IN LENGTH. REPAIRED THE FORWARD FUSELAGE SKIN AT STATION 196.5 TAT LBL 3.0 IAW BOEING SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 2001051500504 20010515 00504 NM 2001 5 15 P2EA01029 1 20010413 A 5753 FLAP BOEING 737 7372B7 1384560 NM LT WING DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 125NJ 22882 SJO - DURING C-CHECK, LEFT IMB AFT FLAP DELAMINATED AT OUTBOARD CORNER. REPAIRED LEFT WING INBOARD AFT FLAP P/N 6546434 -139, S/N 666 IAW COPESA EO NR COO-CMP-3-57-136-01. (M) 2 L 7 2 4F A16WE 2001051500505 20010515 00505 CE 2001 5 15 20010515AP001 1 20010514 A 5712 57222061 RIB CESSNA 441 441 2076020 CE LEFT CENTER WING CRACKED B K NONE O OTHER IN INSP/MAINT 1 SW 99 12DT 8620 4410040 DURING A SCHEDULED INSPECTION, THE LEFT WING CENTER SECTION CANTED RIB CAP (CWS 26.85 INCHES) WAS FOUND CRACKED. THE CAN TED RIB UPPER CAP (P/N: 5722206-1) WAS CRACKED AFT OF THE AFT MAIN SPAR AT FS 177.45, IN THE BEND RADIUS, AND RAN AFT AP PROXIMATELY 1.375 INCHES. THE CRACK WAS FIRST NOTED USING VISUAL INSPECTION THEN VERIFIED WITH DYE PENETRANT. AFTER REMO VING THE RIB CAP, CLOSE EXAMINATION OF THE PART REVEALED THAT THE CAP WAS MANUFACTURED SO THAT THE BEND WAS PARALLEL WIT H GRAIN OF THE METAL INSTEAD OF PERPENDICULAR WHICH COULD RESULT IN THIS TYPE OF FAILURE. CESSNA CURRENTLY DOES NOT HAVE ANY SPECIFIC INSPECTIONS RELATING TO THIS MATTER, THEREFORE,THIS AREA SHOULD BE CLOSELY CHECKED DURING INSPECTIONS. 1 L 7 2 3T RT A28CE 2001051600410 20010516 00410 EA 2001 5 16 MASA01034 1 20010403 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 87353 7353 WHILE PERFORMING AN 18 MONTH INSPECTION, FOUND ONE CABIN CEILING BULB INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB. OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001051600411 20010516 00411 EA 2001 5 16 MASA01033 1 20010403 A 3350 489142 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17337 7337 FLT 6623 - CMH-LGA - PILOT REPORTED AFT CABIN CEILING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE MEL''D THE DISCREP ANCY. THE AIRCRAFT WAS RETURNED TO SERVICE. DURING OVERNIGHT MAINTENANCE, THE BULB WAS REMOVED AND REPLACED THE BULB. OPS CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2001051600412 20010516 00412 SO 2001 5 16 MASA01032 1 20010403 A 3350 1317 LIGHT EMB 145 EMB145LR SO EXTERIOR INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 825MJ 145179 FLT 5875 - DCA-SDF - DURING PREFLIGHT, THE CAPTAIN REPORTED EXIT LIGHT AFT FUSELAGE EMERGENCY LIGHT INOPERATIVE. MAINTE NANCE REPLACED THE BULB. OPS CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001051600413 20010516 00413 NM 2001 5 16 GAIA01152OP 1 20010413 A 3350 1000679 LIGHT BOEING 727 727214 138407R NM L1 DOOR INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 751US 21513 DURING MAINTENANCE, IT WAS DISCOVERED THAT THE EMERGENCY LIGHT ASSEMBLY AT THE L1 DOORS APPEARS TO BE DISCHARGED. REMOV ED AND REPLACED THE L1 DOOR EMERGENCY LIGHT ASSEMBLY. OPERATIONALLY CHECKED NORMAL. THE AIRCRAFT WAS RETURNED TO SERVI CE. (M) 2 L 7 3 4F A3WE 2001051600414 20010516 00414 NM 2001 5 16 GAIA01153OP 1 20010417 A 3350 GUARD BOEING 727 727243 138408D NM COCKPIT BROKEN A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 1269Y 21269 DURING ROUTINE INSPECTION AT BOI, FOUND EMERGENCY EXIT LIGHT SWITCH GUARD BROKEN. REMOVED AND REPLACED SWITCH GUARD ON EMERGENCY EXIT LIGHT SWITCH. OPS CHECK NORMAL AT THIS TIME. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2001051600415 20010516 00415 NM 2001 5 16 USAASB01100 1 20010411 A 3040 2312 CONTROLLER BOEING 737 7374B7 1384702 NM E/E COMPT FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 433US 23139 24555 IAH - FLT 1934 - ON CLIMB-OUT FROM IAH, PASSING THROUGH FL180 EN ROUTE TO PHL, FLIGHT ATTENDANT ADVISED CREW OF A BURNIN G ODOR IN THE CABIN. FLIGHT RETURNED TO FIELD AT IAH AND LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE FORWARD RIGHT WINDOW HEAT CONTROLLER NOT FUNCTIONING. A TRANSFORMER SMELL WAS BEING EMITTED FROM THE NR 4 CONTROL BOX. REMOVED AND REPLACED THE NR 4 FORWARD RIGHT WINDOW HEAT CONTROLLER. OPS CHECK GOOD. CLEARED ODO R/SMOKE FROM CABIN. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2001051600416 20010516 00416 NE 2001 5 16 USAASB01101 2 20010415 A 7200 ENGINE BOEING 737 737301 1384611 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE MALFUNCTIONED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 576US 23741 720773 TPA - FLT 1580 - EN ROUTE FROM PHL TO TPA, A BURNING OIL SMELL WAS REPORTED COMING FROM THE LEFT PACK DURING FLIGHT. FL IGHT CONTINUED AND LANDED AT TPA WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE AS THE SOURCE OF THE ODOR. REMOVED AND REPLACED THE NR 1 ENGINE ASSEMBLY PER JOB CARD J371-00-01. OPERATIONAL CHECK AND LEAK CHECK GOOD. ALSO, REMOVED AND REPLACED BOTH WATER SEPARATOR BAGS (P/N V121-1) DUE TO STALE AIR SMELL. (M) 2 L 7 2 4F 4 F RT A16WE E2GL 2001051600417 20010516 00417 WP 2001 5 16 AALA20010749 1 20010402 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7514A 49891 TUL - FOUND CORROSION ON NR 2 SEAT TRACK AT 1200-1203, 1293, 1305. REPLACED NR 2 SEAT TRACK FROM 1136-1309 PER SRM 53-0 5 AND ESO 80559 DATED 3/27/2001. (M) 2 L 7 2 4F A6WE 2001051600418 20010516 00418 WP 2001 5 16 AALA20010753 1 20010324 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7514A 49891 TUL - FOUND CORROSION AROUND NUTPLATE HOLES AT STATION 1148 ABOVE LONGERON 26R COMMON TO WEB. FABRICATED DOUBLER, TREAT ED AND PRIMED AND INSTALLED PER SRM 51-70-4. (M) 2 L 7 2 4F A6WE 2001051600419 20010516 00419 NM 2001 5 16 AALA20010664 1 20010330 A 3350 4065623 PLATE BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 913AN 29514 TPA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT LEFT SIDE OVERWING BROKEN. REPLACED EMERGENCY EXIT LIGHT PL ATE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2001051600420 20010516 00420 2001 5 16 GTIA010096 4 20010406 A 2210 AUTOPILOT SYS DOUG DC9 DC941 302207N WP COOCKPIT VIBRATION A GTIA O OTHER E VIBRATION/BUFFET CR CRUISE 1 GL 23 130NK 47604 WITH AUTO PILOT ON, THERE IS A LOW FREQUENCY VIBRATION IN PATCH AXIS, PITCH SERVO OFF, NO VIBRATION. NORMAL OPERATION. OPS CHECK GOOD ON GROUND IAW DC-9 MM 22-10-00. THIS CLEARS DMI NR 000165-1. PLACARDS REMOVED. (M) 2 L 7 2 4F A6WE 2001051600423 20010516 00423 CE 2001 5 16 20010508CW011 1 20010409 A 2612 47327S FIRE DETECTOR BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A60A 52043 NE FIRE WARN SYS MISINSTALLED B R2JR K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 21 7VA BB670 WHILE TROUBLESHOOTING FAULTY FIRE WARNING LIGHT, FOUND 3 DETECTORS INSTALLED WITH BUTT SPLICES, CONTRARY TO KA200 MAIN TENANCE MANUAL, CAUTION NOT TO SPLICE SOME WIRES AND USE ONLY SEALED CONNECTORS ON OTHERS. REPLACED DETECTORS AND REMO VED SPLICES AND PINNED TO FORWARD PLUG. WORK DONE AT APPROVED FACILITY, YET, ACCEPTABLE DATA WAS NOT FOLLOWED. 1 L 7 2 4T 4 T A24CE E4EA 2001051600424 20010516 00424 WP 2001 5 16 USAAD01053 1 20010317 A 5240 DOOR DOUG DC9 DC982 3022082 WP SERVICE DOOR NOT CLOSED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 823US 49142 CLT-MSY - FLT 1035 - AFTER TAKEOFF, THE PRESSURIZATION FLOW LIGHT ILLUMINATED. THE FLIGHT ATTENDANT REPORTED AN EXTREME LY LOUD AIR NOISE AT THE AFT SERVICE DOOR. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AFT SERVICE DOOR NOT CLOSED PROPERLY. THE DOOR WAS PROPERLY CLOSED AND THE DOOR OPERATION AND THE DOOR WARNI NG LIGHT WAS VERIFIED AS OPERATING PROPERLY. (M) 2 L 7 2 4F A6WE 2001051600425 20010516 00425 WP 2001 5 16 ASAA0180099 1 20010310 A 3350 6011779 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 954AS 49387 SEA - DURING LINE CHECK, EXTERIOR EMERGENCY LIGHTS WERE DETERMINED TO BE INOPERATIVE. REMOVED AND REPLACED EXTERNAL EME RGENCY LIGHT BATTERY. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001051600426 20010516 00426 WP 2001 5 16 GTIA010049 1 20010314 A 3150 WARNING SYSTEM DOUG DC9 DC982 3022082 WP COCKPIT ACTIVATED A GTIA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 23 805NK 48087 DTW - FLT 629 - DURING TAKEOFF, ON 21L RECEIVED WINDSHEAR WARNING, PUSHED THROTTLES TO STOP FOR APPROX 20 SECONDS, AT RO TATION. PERFORMED BORESCOPE INSPECTION ON NR 1 AND NR 2 ENGINES. REMOVED AND REPLACED OIL FILTERS AND INSPECTED ENGINE MAG PLUGS, ALSO PERFORMED A VISUAL INSPECTION OF NR 4 GEARING RETURN LINE TEMP TAPE. NO DISCREPANCIES FOUND REF LG PG 111366 ITEM 1, 2, AND 3. (M) 2 L 7 2 4F A6WE 2001051600427 20010516 00427 NM 2001 5 16 USAA010351 1 20010403 A 5522 SKIN BOEING 757 757225 1384959 NM ELEVATOR DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND RIGHT ELEVATOR SKIN DELAMINATED 3.1 INCH BY .5 INCHES, OUTBOARD EDGE OF LOWER SKIN PANEL, 5 INCHES FORWARD T /E. COMPOSITE WET LAYUP REPAIR PER SRM 51-70-17. (M) 2 L 7 2 4F RT A2NM 2001051600428 20010516 00428 NM 2001 5 16 USAABB01020 1 20010407 A 2932 1821413 TRANSMITTER BOEING 767 7672B7 1385107 NM RT MLG WW INOPERATIVE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 656US 26847 PIT - FLT 741 - CREW HEARD A LOUD THUMP AFTER TAKEOFF FROM PIT. ON GEAR RETRACTION, THE CENTER HYDRAULIC SYSTEM WAS LOS T. CREW RECEIVED LOW PRESSURE INDICATIONS FROM ALL THE SYSTEMS. FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCI DENT. MAINTENANCE FOUND THE CENTER SYSTEM HYDRAULIC PRESSURE TRANSMITTER INOPERATIVE AND REPLACED IT. (M) 2 L 7 2 4F RT A1NM 2001051600429 20010516 00429 NM 2001 5 16 USAA010355 1 20010404 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND FRAME CHAFED 2.5 INCH, STATIN 1040 FRAME CUTOUT OF APU DUCT STRINGER 22L-26L. INSTALLED DOUBLER, TRIPLER AN D SHEAR TIES. INSTALLED DOUBLER, TRIPLER AND SHEAR TIES. (M) 2 L 7 2 4F A16WE 2001051600430 20010516 00430 NM 2001 5 16 USAA010352 1 20010404 A 5320 WEB BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND WEB CRACKED 2 INCHES, STATION 670-672 RBL 25 MWW CEILING. INSTALLED SPLICE PLATE, STIFFENERS, ANGLES WEB RE PAIR PER EA 69183. (M) 2 L 7 2 4F A16WE 2001051600431 20010516 00431 NM 2001 5 16 USAA010353 1 20010404 A 5510 SUPPORT BOEING 737 737201 1384454 NM HORIZ SSTAB DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND WEB SUPPORT WITH .5 INCH BULGE, HORIZ STAB JACKSCREW LOWER WEB SUPPORT, STATION 1088, LBL 4. INSTALLED WEB DOUBLER AND FILLER PER EA 69281. (M) 2 L 7 2 4F A16WE 2001051600432 20010516 00432 NM 2001 5 16 USAA010354 1 20010404 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND SKIN CRACKS, TWO CRACKS .4 INCHES, TWO CRACKS AT .7 INCH, STATION 380 AND 397 BETWEEN STRINGER 19R AND 20R. INSTALLED DOUBLER PER EA 69250. (M) 2 L 7 2 4F A16WE 2001051600433 20010516 00433 NM 2001 5 16 GAIA01112ST 1 20010312 A 5532 SKIN BOEING 727 727251 138408H NM VARTICAL STAB CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING A ROUTINE INSPECTION BEING PERFORMED AT FLIGHTSTAR AIRCRAFT SERVICES AT JAX, IT WAS DISCOVERED THAT THE RIGHT VER TICAL STABILIZER ROOT AT BS 1342, STRINGER S-10R IS CRACKED. REPAIRED PER BOEING SERVICE BULLETIN 727-55-82. THE AIRCR AFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001051600437 20010516 00437 NM 2001 5 16 ASAA0110121 1 20010311 A 3350 86210144 BATTERY BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT IDENTIFIER SIGN CYCLING ON AND OFF. REMOVED AND REPLACED REMOTE AS SEMBLY BATTERY AND LIGHT OPERATED NORMAL. (M) 2 L 7 2 4F RT A16WE 2001051600438 20010516 00438 NM 2001 5 16 ASAA0110118 1 20010308 A 3350 86210144 BATTERY BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT SIGN ON SMOKE BARRIER INOPERATIVE. REMOVED AND REPLACED REMOTE ASS EMBLY BATTERY AND LIGHT OPERATED NORMAL. (M) 2 L 7 2 4F RT A16WE 2001051600439 20010516 00439 WP 2001 5 16 ASAA0180102 1 20010313 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 29468 4296 53063 SEA - DURING SERVICE CHECK, FORWARD CABIN PORTABLE EMERGENCY LIGHT WAS DETERMINED TO BE INOPERATIVE. REPLACED LIGHT ASS EMBLY. LIGHT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001051600442 20010516 00442 NM 2001 5 16 ASAA0140002 1 20010109 A 3350 1370 LIGHT BOEING 737 7374Q8 NM L2 DOOR INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 783AS 25114 PDX - DURING LINE CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY SPOT LGIHT INOPERATIVE, BURNED OUT. REPLACED BULB, OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2001051600444 20010516 00444 WP 2001 5 16 ASAA0180103 1 20010314 A 3350 60030451 BATTERY DOUG DC9 DC983 3022083 WP COCKPIT DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 LAX - DURING PREFLIGHT, COCKPIT EMERGENCY EXIT LIGHTS FOUND INOPERATIVE. REPLACED BATTERIES. EXIT LIGHTS OPERATED PROP ERLY. (M) 2 L 7 2 4F RT A6WE 2001051600445 20010516 00445 NE 2001 5 16 MASA01028 2 20010320 A 7321 324485318 FUEL CONTROL DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE NR 2 ENGINE FAILED A MASA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER UK UNKNOWN 1 SW 07 449YV 449 FLT 6323 - GJT-PHX - RETURNED TO FIELD AFTER SHUTTING DOWN ENGINE NR 2 DUE TO NO RESPONSE TO POWER LEVER MOVEMENT. AFTE R AN UNEVENTFUL LANDING MAINTENANCE WAS CALLED. MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED THE MFC AND FUEL PUMP. AIRCRAFT WAS LEAK CHECKED. OPS CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T 4 T RT A13NM E20NE 2001051600446 20010516 00446 NM 2001 5 16 MASA01035 1 20010406 A 3350 6104789 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 449YV 449 DURING ROUTINE MAINTENANCE DISCOVERED F/A''S GALLEY EMERGENCY EXIT, RIGHT FORWARD EMERGENCY EXIT AND CEILING FORWARD AFT LIGHTS INOPERATIVE. REMOVED AND REPLACED NR 2 EMERGENCY POWER SUPPLY. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 2001051600447 20010516 00447 EA 2001 5 16 REXA01006 1 20010416 A 7110 BLC3BC11SL5C4 PIN CNDAIR CL600 CL6002B19 EA COWLING OUT OF POSITION A REXA A E UNSCHED LANDING ENGINE SHUTDOWN S AFFECT SYSTEMS CR CRUISE 1 SO 25 8390A 7390 EN ROUTE TO MONTEREY, MEXICO THE FLIGHT CREW DISCOVERED THAT THE THRUST LEVER OF THE LEFT ENGIEN COULD NOT BE REDUCED BE LOW 97 PERCENT N1. THE FLIGHT CREW CONTACTED MAINTENANCE CONTROL FOR POSSIBLE RESOLUTION. AFTER CONFERRING WITH MAINTE NANCE ENGINEERING, IT WAS DECIDED TO HAVE THE AIRCRAFT RETURN TO MEMPHIS, USING THE APPROPRIATE CHECKLISTS AND AN OTHERW ISE NORMAL LANDING WAS MADE. MAINTENANCE FOUND THAT THE PIN LOCKING THE COWLING STAY ROD IN THE STOWED POSITION HAD BAC KED OUT ALLOWING THE STAY ROD TO FALL DOWN AND JAM THE ENGINE CONTROL LINKAGE. FURTHER INSPECTION OF THE PIP TYPE PIN F OUND TAHT ONE OF THE LOCKING BALLS WAS MISSING. (M) 2 L 7 2 4F RT A21EA 2001051600448 20010516 00448 2001 5 16 GAIA01125OP 4 20010411 A 3418 2566A21 SENSOR BOEING 727 727222 1384073 NM STALL WARNING MALFUNCTIONED A GAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 90AX 20040 FLT 1765 - DFW-SAT - AFTER TAKEOFF, THE AIRCRAFT HAD A CONTINUOUS STICK SHAKER ON UNTIL LANDING. THE AIRCRAFT RETURNED TO DFW AND LANDED SAFELY, WITHOUT ANY FURTHER DIFFICULTY. THE AIRCRAFT DID PERFORM AN OVERWEIGHT LANDING. REMOVED AND REPLACED NR 1 ANGLE OF ATTACK AIRFLOW SENSOR PER BOEING MM. OPS CHECKS GOOD. MAINTENANCE PERFORMED AN OVERWEIGHT LANDI NG INSPECTION AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001051600449 20010516 00449 SO 2001 5 16 ASOA01029 1 20010317 A 3260 PROXIMITY SWITCH EMB 120 EMB120RT SO MLG MALFUNCTIONED A ASOA E ENGINE SHUTDOWN N FALSE WARNING AP APPROACH 1 SO 11 239AS 120057 FLT 4162 - DURING APPROACH INTO DFW FROM AEX, GEAR WOULD NOT COME DOWN WHEN COMMANDED. CREW EXECUTED AN ELECTRIC OVERRI DE. THE LEFT ENGINE INADVERTENTLY WENT FROM 50 PERCENT TORQUE AND 100 PERCENT PROPELLERS TO 94 PERCENT TORQUE AND 42 PE RCENT NP. CAPTAIN IMMEDIATELY SHUT DOWN THE LEFT ENGINE. AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLAC ED THE RIGHT MLG DOWNLOCK ''A'' INDICATION PROXIMITY SWITCH. OPS CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001051600450 20010516 00450 EA 2001 5 16 ASOA01030 1 20010320 A 5610 NP1393222 WINDOW CNDAIR CL600 CL6002B19 EA COCKPIT CRACKED A ASOA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 11 828AS 7656 7213 FLT 4473 - DURING FLIGHT FROM ATL TO HPN, RIGHT SIDE WINDOW CRACKED. CAPTAIN DIVERTED TO TRI AND LANDED SAFELY. MAINTE NANCE REMOVED AND REPLACED THE RIGHT SIDE WINDOW. OPS AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001051600451 20010516 00451 EA 2001 5 16 ASOA01031 1 20010322 A 5610 NP1393216 WINDSHIELD CNDAIR CL600 CL6002B19 EA COCKPIT CRACKED A ASOA K NONE O OTHER AP APPROACH 1 SO 11 854AS 7382 FLT 4464 - DURING APPROACH INTO CAE FROM DFW, FIRST OFFICERS WINDSHIELD SHATTERED. MAINTENANCE REMOVED AND REPLACED FIR ST OFFICER''S FRONT WINDSHIELD. HEATING AND PRESSURIZATION TESTS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001051600452 20010516 00452 SO 2001 5 16 ASOA01032 1 20010325 A 5230 12023117001 SEAL EMB 120 EMB120RT SO CARGO DOOR FAILED A ASOA G O2 MASK DEPLOYED O OTHER CR CRUISE 1 SO 11 275AS 120234 DURING FLIGHT FROM LFT TO MEI, AIRCRAFT EXPERIENCED AN FLIGHT LEVEL 17,000 FEET. PASSENGER OXYGEN MASKS DEPLOYED IN THE CABIN. CAPTAIN DECLARED AN EMERGENCY AND LANDED SAFELY IN MEI. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR SEAL. OPS AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001051600453 20010516 00453 NM 2001 5 16 P2EA01027 1 20010404 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 125NJ 22882 SJO - DURING C-CHECK, SKIN CRACK AT STRINGER 19R AT BS 765. REPAIRED FUSELAGE SKIN FROM BS 760 TO BS 769 BETWEEN STRING ER 18R TO STRINGER 20R IAW SRM 53-30-3 FIGURE 07 AND SRM 53-10-3 FIGURE 1. THIS IS A CLOSING ACTION FOR MRR NR 01021. (M) 2 L 7 2 4F A16WE 2001051600454 20010516 00454 NM 2001 5 16 P2EA01026 1 20010405 A 5320 CHANNEL BOEING 737 7372B7 1384560 NM FUSELAGE CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 125NJ 22882 SJO - DURING C-CHECK, FOUND CORROSION ON CHANNEL SUPPORT BETWEEN BS 986 AND BS 1006 AND BETWEEN STRINGER 25L AND 26L. C HANNEL REPLACED BETWEEN BS 986 AND BS 1006 AND BETWEEN STRINGERS 25L AND 26L, IAW SRM 51-10-1 PAGE 8. (M) 2 L 7 2 4F A16WE 2001051600455 20010516 00455 NM 2001 5 16 P2EA01025 1 20010408 A 5330 SKIN BOEING 737 737297 1384480 NM FUSELAGE PUNCTURED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 5WM 22629 FLT 350 - MDW - PUNCTURE THROUGH SKIN AT BS 933 WL 203 BETWEEN STRINGER 20L AND 21L. (M) 2 L 7 2 4F A16WE 2001051600456 20010516 00456 NM 2001 5 16 P2EA001018 1 20010405 A 5330 SKIN BOEING 737 737244 138448U NM FUSELAGE CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 OKC - DURING C-CHECK, FOUND THE INTERNAL FUSELAGE SKIN WITH CORROSION OUT OF LIMITS AT STATION 322 BETWEEN STRINGERS 28R AND 29R. (M) 2 L 7 2 4F A16WE 2001051600457 20010516 00457 NM 2001 5 16 P2EA001017 1 20010405 A 3211 BEAM BOEING 737 737244 138448U NM RT MLG GOUGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 OKC - DURING C-CHECK, FOUND THE RIGHT MAIN LANDING GEAR SUPPORT BEAM GOUGED 10 INCHES INBAORD FROM THE LOWER OUTBOARD EN D. AFTER BLENDING IT WAS FOUND TO BOUT OF LIMITS. (M) 2 L 7 2 4F A16WE 2001051600458 20010516 00458 NM 2001 5 16 USAA010348 1 20010403 A 5320 CHANNEL BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND HAT CHANNEL CORRODED 2 INCHES BY 4 INCHES, STATION 310 TO 324, RBL 42. INSTALLED NEW PART PER SRM 51-30-02. (M) 2 L 7 2 4F RT A2NM 2001051600459 20010516 00459 NM 2001 5 16 USAA010349 1 20010403 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND FLOORBEAM CORRODED 1 INCH BY 2 INCHES, STATION 365 LBL 10 TO RBL 65. T-CAP REPLACED/REPAIRED ANGLES PER EA 89244/69275. (M) 2 L 7 2 4F RT A2NM 2001051600460 20010516 00460 NM 2001 5 16 USAA010350 1 20010403 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND FLOORBEAM CORRODED 1 INCH BY 4 INCHES. T-CAP REPLACED, REPAIR ANGLES AND DOUBLERS INSTALLED PER TR 53-15-01 . (M) 2 L 7 2 4F RT A2NM 2001051600461 20010516 00461 NM 2001 5 16 DL72S010609 1 20010413 A 2612 SWITCH BOEING 727 727232 1384082 NM COCKPIT FAILED A DALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 27 529DA 21703 ABORTED T/O AT 100 KTS DUE TO APU FIRE WARN BELL/LIGHT. FOUND APU FIRE PUSH/PULL SWITCH BAD. REMOVED AND REPLACED SWITCH . OPS CHECKS GOOD. 2 L 7 3 4F A3WE 2001051600462 20010516 00462 NM 2001 5 16 DL78K010630 1 20010417 A 2120 UNKNOWN BOEING 737 737832 13844CF NM CABIN ODOR A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 399DA 30379 DURING T/O, AS PWR WAS ADVANCED-A VERY STRONG ODOR LIKE PLASTIC WITH NO SMOKE. ODOR SLOWLY DISSAPATED DURING FLT. AND THEN RETURNED DURING DESCENT BUT NOT AS STRONG AS T/O. C/A OPERATED BOTH AC PACKS PER AMM21-00-01-2. PLASTIC ODOR DISSA PATED AFTER SEVERAL MINUTES. NO ODOR REMAINED. 2 L 7 2 4F RT A16WE 2001051600463 20010516 00463 NM 2001 5 16 DL73K010632 1 20010417 A 7120 SUPPORT FITTING BOEING 737 737232 1384475 NM ENGINE MOUNT DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 301DL 23073 THE FWD ENGINE MOUNT SUPPORT FITTING WAS FOUND DAMAGED DUE TO MIGRATING BEARINGS FOR THE MOUNT HOLES. REPAIR PER ER/A 4 01670-14AD 2 L 7 2 4F RT A16WE 2001051600464 20010516 00464 NM 2001 5 16 DL72L010634 1 20010417 A 5210 SEAL BOEING 727 727232 1384082 NM ENTRY DOOR WORN A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 510DA 21312 LT FWD ENTRY DOOR SEAL MADE ALOUD SQUEAL UPON A/C PRESSURIZING AFTER TAKEOFF SQUEALED UNTIL 4.0 PSI DIFF.AND CEASED AT . 5 PSI DIFF. REPAIRED SEAL AREA PRESSURIZED ACFT CKS GOOD 2 L 7 3 4F A3WE 2001051600465 20010516 00465 2001 5 16 DL76G010635 4 20010417 A 3442 RADAR BOEING 767 7673P6 1385105 NM WEATHER RADAR FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 156DL 25354 AIR TURN BACK WEATHER RADAR INOP WEATHER RADAR FAULT ON. REPLACED R/T AND ANTENNA PER M/M POS CHECKS GOOD 2 L 7 2 4F RT A1NM 2001051600466 20010516 00466 NM 2001 5 16 DL72S010636 1 20010417 A 3350 POWER SUPPLY BOEING 727 727232 1384082 NM CABIN SHORTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 540DA 22386 DURING LAYOVER CHECK INSPECTION FOUND EMERG SEAT TRACK LIGHTS INOP BETWEEN SEAT ROWS 27 AND 36. REPLACED PWR SUPPLY. 2 L 7 3 4F A3WE 2001051600467 20010516 00467 NM 2001 5 16 DL72W010637 1 20010417 A 5330 65545703 SKIN BOEING 727 727247 138408F NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2815W 20871 FUSELAGE SKIN, FS 360-480 AT STR 4R SKIN LAP SPLICE CRACK REPAIR LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETW EEN FS 360 & 480 INDICATED CRACKS. INTERNAL MFEC INSPECTION CONFIRMED 5 CRACKS ALONG THE LOWER FASTENER ROW OF THE L OWER SKIN PANEL. AN EXISTING REPAIR WAS LOCATED BETWEEN FS 360 &380. THE REPAIR WAS REMOVED AND THE ENTIRE LAP JOINT CUT OUT. THE JOINT WAS REPAIRED WITH AN EXTERNAL DOUBLER AND STRUCTURAL FILLER PER ER/A 380573-14AD. 2 L 7 3 4F A3WE 2001051600468 20010516 00468 NM 2001 5 16 DL73K010638 1 20010418 A 5315 FLOORBEAM BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 307DL 23079 THE BL 0 LONGITUDINAL FLOORBEAM OVER THE CENTER WING WAS FOUND WITH A CRACK IN THE UPPER CHORD AND WEB AT FS 660 AND WIT H 4 CRACKS IN THE WEB AT UPPER CHORD ATTACH POINTS AT FS 700. THE CRACKING IS TYPICAL OF BAC S/B 737-57-1210. THE FLO ORBEAM WAS REPAIRED AND MODIFIED PER THE REQUIREMENTS OF THE S/B AND DOCUMENTED PER ER/A 380586-14. 2 L 7 2 4F RT A16WE 2001051600469 20010516 00469 WP 2001 5 16 DLL10010639 1 20010418 A 2120 DUCT LKHEED 1011 10113851 5265010 WP AC BAY CRACKED A DALA D RETURN TO BLOCK B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 730DA 25543 193C1199 000 OVERHEAT ON NR 2 PACK FLOW CONTROL COMPRESSOR DISCHARGE 320 DEG. CENT. THERE WAS A POPPING NOISE AND SOME SMOKE IN CABIN JUST BEFORE THE OVERHEAT. FOUND NR 2 PACK COMPRESSOR DISCHARGE DUCT CRACKED AND WATER SEPARATOR CAP BLOWN ALSO DISCHARG E SENSOR WIRES BROKE. REMOVED WATER SEP. CAP AND CAPPED AND STOWED WIRES AND LOCKED NR 2 PACK VALVE CLOSED. FWD TO MCO P LAC PER MEL 21-21-01B 2 L 7 3 4F A23WE 2001051600470 20010516 00470 NM 2001 5 16 DL757010640 1 20010418 A 2120 UNKNOWN BOEING 757 757232 1384965 NM COCKPIT ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 622DL 22912 IR- PUNGENT ODOR IN COCKPIT ON SHORT FINAL. ELECTRICAL OVERHEAT ODOR. THIS ODOR WAS NOT OBSERVED IN CABIN. UNABLE TO DUP LICATE. RAN PACKS TO FULL HOT NO ODORS. EQUIP COOLING CKS OK. REPLACED MAIN BATTERY AND CHARGER OPS CK OK. 2 L 7 2 4F RT A2NM 2001051600471 20010516 00471 NM 2001 5 16 DL72W010643 1 20010418 A 5610 5717623134 WINDOW 5717623134 BOEING 727 727247 138408F NM COCKPIT WORN A DALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 27 2816W 20872 R-2 WINDOW CAME OPEN ON T/O ROLL. CREW CLOSED WNDOW AND RETURNED TO ABQ. REMOVED AND REPLACED THE R-2 WINDOW 2 L 7 3 4F A3WE 2001051600472 20010516 00472 NM 2001 5 16 DLM88010644 1 20010418 A 2720 RUDDER PEDAL DOUG MD88 MD88 3023688 NM COCKPIT OBSTRUCTED A DALA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 941DL 49814 AFTER PUSHBACK FLIGHT CREW INITIALLY COULD NOT DEPRESS THE LEFT RUDDER PEDAL DURING FLIGHT CONTROL CHECK. RETRACTED FLAP S/SLATS, DISAGREEMENT LIGHT ILLUMINATED AND LEFT RUDDER PEDAL WAS OPERATIONAL, RTB. VISUALLY INSPECTED RUDDER SYSTEM CO NTROLS ON AIRCRAFT FORFREEDOM OF MOVEMENT OR BINDING RUDDER TRAVEL NORMAL. FOUND CAPPED WIRE BUNDLE AT F/O LT RUDDER PEDAL TUNNEL HANGING DOWN WITH BROKEN TY-WRAP.RESECURED BUNDLE. RUDDER CHECK NORMAL. 2 L 7 2 4F RT A6WE 2001051600473 20010516 00473 NM 2001 5 16 DLM90010645 1 20010419 A 2916 59654405501 RESERVOIR DOUG MD90 MD9030 3023690 NM RT MLG WW LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 904DA 53384 LOSS OF RT HYD PRESSURE, WENT TO ZERO AND OVERTEMP. FOUND RT HYD RES. LEAKING INTERNALLY. REPLACED SAME. 2 L 7 2 4F RT A6WE 2001051600474 20010516 00474 NM 2001 5 16 DL757010646 1 20010419 A 2421 GENERATOR BOEING 757 757232 1384965 NM NR 1 ENGINE INOPERATIVE A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 695DA 29727 LT GENERATOR DRIVE MESSAGE ON EICAS DURNING T/O ROLL. FOUND LEFT GENERATOR TO MCO AND PLC PER MEL 24-00-01 2 L 7 2 4F RT A2NM 2001051600475 20010516 00475 NE 2001 5 16 DL757010647 2 20010419 A 7200 ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 ENGINE LEAKING A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 655DL 5436 24395 A/C PACKS SMELL MUSTY AND STINK BAD. REPLACED NR 1 ENGINE 2 L 7 2 4F 4 F RT A2NM E17NE 2001051600476 20010516 00476 NM 2001 5 16 DL72S010648 1 20010419 A 3350 1000677 LIGHT BOEING 727 727232 1384082 NM R1 DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 532DA 22045 1R DOOR EMERGENCY LIGHT WOULD NOT COME ON WITH TEST. REPLACED EMER LIGHT ASSY. 2 L 7 3 4F A3WE 2001051600477 20010516 00477 NM 2001 5 16 DL72S010650 1 20010419 A 7120 MOUNT BOEING 727 727232 1384082 NM NR 1 ENGINE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 539DA 22385 WHILE ACCOMPLISHING INSPECTIONS OF THE FASTENER HOLES ON THENR 1 ENGINE PYLON FWD ENGINE MOUNT FITTING PER AD 97-05-08, A CRACK INDICATION WAS NOTED AT HOLE B. THE FASTENER HOLE WAS OVERSIZED TO REMOVE THE CRACK INDICATION WITH AN ADDITIO NAL 1/32 INCH INSURANCE CUT. AN OVERSIZE BOLT WAS THEN INSTALLED. THE REPAIR WAS ACCOMPLISHED PER FED-EX S/B 2000-541 0A01 AND ER/A 380610-14AD. 2 L 7 3 4F A3WE 2001051600478 20010516 00478 NM 2001 5 16 DL757010651 1 20010420 A 2612 FIRE WARNING BOEING 757 757232 1384965 NM COCKPIT MALFUNCTIONED A DALA K NONE N FALSE WARNING LD LANDING 1 SO 27 687DL 27586 FIRE BELL RANG CONTINUOUSLY DURING LANDING. ONLY WAY TO SILENCE WAS TO CYCLE GEN''S. INSP AND RAN TEST AND RESET M618 CA RD. FIRE BELL AND LIGHTS CH OK. 2 L 7 2 4F RT A2NM 2001051600479 20010516 00479 NM 2001 5 16 DLM88010652 1 20010420 A 2170 COALESCER BAG DOUG MD88 MD88 3023688 NM A/C BAY DIRTY A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 922DL 49646 FLIGHT ATTENDANT REPORTED BURNING SMELL IN ENTIRE CABIN DURING T/O. THE SMELL DISSIPATED DURING CLIMBOUT AND WAS GONE AR OUND 10000 FEET. CHANGED WATER SEPERATOR BAGS PERFORMED DUCT BURN OUT PER M/M . RAN ENGINES AT ALL POWER SETTINGS NO SME LL NOTED CKS GOOD A/C OK FOR SVC 2 L 7 2 4F RT A6WE 2001051600480 20010516 00480 NM 2001 5 16 DLM11010653 1 20010420 A 2530 FAN DOUG MD11 MD11 3023602 NM GALLEY MALFUNCTIONED A DALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 804DE 48475 IR- AFTER LANDING LAV SMOKE ANNUNCIATES FOR 10 SECONDS WITH HIGH PITCED TONE IN 4R LAV. INSPECTED 4R LAV. NO EVIDENC E OF SMOKE. HIGH PITCHED WHINE FOUND TO BE AFT GALLEY CHILLER VENT FAN. PULLED AND COLLARD C/B FWD TO MCO AND PLACARD ED. 2 L 7 3 4F RT A22WE 2001051600481 20010516 00481 NM 2001 5 16 DL72S010654 1 20010420 A 3350 10617839 SIGN BOEING 727 727232 1384082 NM CABIN BROKEN A DALA K NONE O OTHER CR CRUISE 1 SO 27 541DA 22387 EMERGENCY EXIT SIGN OVER AISLE AT OVERWING EXITS BROKE LOOSE FROM MOUNTING. CREW WAS UNABLE TO SECURE SO THEY CUT WIRES TO REMOVE LIGHT. REPLACED LIGHT ASSY, CANNON PLUG, AND BATTERY RACK. 2 L 7 3 4F A3WE 2001051600482 20010516 00482 NM 2001 5 16 DL72S010655 1 20010421 A 2910 000AE908D03 HYDRAULIC LINE BOEING 727 727232 1384082 NM HYDRAULIC SYS DAMAGED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 540DA 22386 TOTAL LOSS OF A SYSTEM HYDRAULICS ON DEPTATURE. LOST BOTH PRESSURE AND QUANTITY WHEN FLAPS WERE RETRACTED FROM 15 TO 5 F OUND LINE TO RIGHT MLG DOOR WITH HOLE IN LINE REPLACED LINE. 2 L 7 3 4F A3WE 2001051600483 20010516 00483 NM 2001 5 16 DL76S010656 1 20010421 A 3350 LIGHT BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 135DL 25145 FOUND RED EMERGENCY LIGHT INOP AT AFT R/H LAV. RELAMPED SAME OPS CK. GOOD. 2 L 7 2 4F RT A1NM 2001051600484 20010516 00484 NM 2001 5 16 DL72S010657 1 20010421 A 2612 894120 FIRE LOOP BOEING 727 727232 1384082 NM NR 1 ENGINE SHORTED A DALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 541DA 22387 695248 ON TAXI OUT NR 1 ENG FIRE WARNING SOUNDED. FOUND B LOOP SHORTED. ALSO FOUND THE LOOPS MISWIRED AT THE FIRE WALL DISCONNE CT. CORRECTED WIRING AND REPLACED THE LOOP. 2 L 7 3 4F A3WE 2001051600485 20010516 00485 NM 2001 5 16 DLM11010658 1 20010422 A 3830 380001285 TANK DOUG MD11 MD11 3023602 NM LAVATORY COLLAPSED A DALA O OTHER K FLUID LOSS DE DESCENT 1 SO 27 809DE 48480 ALL LAVS INOP. CREW HEARD LOUD BANG IN AFT CARGO COMP. 1 1/2 HOURS FROM ARRIVAL IN LAX. FOUND TANK COLLAPSED, AND CRACKE D WILL REQUIRE REQUIRE REPLACEMENT P/N 380001285 NASI LAX. WILL ALSO NEED APPROXIMATELY 25 FT OF BELLY BLANKTS REPLACED FWD OF AFT LAV TANK. REPLACED AFT LAV TANK AND INSULATION BLANKETS. 2 L 7 3 4F RT A22WE 2001051600486 20010516 00486 NM 2001 5 16 DL76L010659 1 20010422 A 2530 SMOKE BOEING 767 767332 1382001 NM FWD GALLEY DETECTED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 178DN 25143 ODOR OF BURNING PLASTIC/ELEC. SMOKE SEEMED TO COME FROM FWD GALLEY CEILING. PULL ALL FWD GALLEY C/B. ODOR DISAPPEARED IN ABOUT TEN MINUTES. PUSH C/B BACK IN. NO SMELL NOTED. A/C OK FOR SVC. 2 L 7 2 4F RT A1NM 2001051600487 20010516 00487 NM 2001 5 16 DL72S010660 1 20010423 A 3350 MS25237328 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 520DA 21471 LT OVERWING EMERG. LIGHTS INOP. RELAMPED LIGHTS. 2 L 7 3 4F A3WE 2001051600488 20010516 00488 NM 2001 5 16 DLM88010661 1 20010423 A 3350 0201984006 COVER DOUG MD88 MD88 3023688 NM L2 DOOR DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 L2 SERVICE DOOR EXIT SIGN WILL NOT STAY ON. FOUND EXIT SIGN COVER DAMAGED REPLACED COVER OK FOR SERVICE 2 L 7 2 4F RT A6WE 2001051600489 20010516 00489 NM 2001 5 16 DL72S010662 1 20010421 A 5330 SKIN BOEING 727 727225A 1384077 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 FUSELAGE SKIN, R1 DOOR CUTOUT LOWER AFT CORNER. A CRACK WAS FOUND IN THE SKIN AND UNDERLYING BEARSTRAP OF THE LOWER AF T CORNER OF THE FWD GALLEY (R1) DOOR CUTOUT. THE CRACK WAS REMOVED WITH A 3 IN X 3 IN CUTOUT. THE CRACK WAS REPAIRED WI TH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER INSTALLED PER ER/A 380623-14, REV A. 2 L 7 3 4F RT A3WE 2001051600490 20010516 00490 NM 2001 5 16 DL76A010663 1 20010421 A 5754 SLAT BOEING 767 767281 1385109 NM WING DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 774AX 22789 NR 1 SLAT T/E WEDGE IS DELAMINATED ON THE INBD EDGE. REPAIR PER ER/A 380633-14AD 2 L 7 2 4F RT A1NM 2001051600491 20010516 00491 NM 2001 5 16 DL76L010664 1 20010423 A 2530 811150417 COFFEEMAKER BOEING 767 767332 1382001 NM GALLEY DEFECTIVE A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 180DN 25985 FIRST CLASS COFFEE MAKER HAS BURING PLASTIC ODOR.REPLACED FWD GALLEY NR 1 COFFEEMAKER. OPS CKS GOOD NO ODOR NOTICED. 2 L 7 2 4F RT A1NM 2001051600492 20010516 00492 NM 2001 5 16 DL72S010665 1 20010423 A 3350 BATTERY PACK BOEING 727 727225A 1384077 NM CABIN NOT SEATED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8873Z 21291 BATTERY PACK OVER ROWS 20-25 WAS FOUND UNSEATED CAUSING SECTION OF EMERGENCY LIGHTS TO NOT WORK. SECURED BATTERY PACK. 2 L 7 3 4F RT A3WE 2001051600493 20010516 00493 NM 2001 5 16 DL757010666 1 20010423 A 2530 811150417 BRACKET BOEING 757 757232 1384965 NM COFFEEMAKER FAILED A DALA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 670DN 83 25331 DURING CRUISE SMOKE/ELECTRICAL ODORS FILLED MID CABIN. FLT DIVERTED INTO LNK ENROUTE TO DEN. FOUND MID GALLEY COFFEE MAK ER TO BE SOURCE OF SMOKE. THE BRACKET THAT HOLDS THE HEATER COIL TO THE HOT PLATE FAILED ALLOWING THE COIL TO DROP INTO THE DRIP PAN. THE PLASTIC PEICE FROM THE BROKEN BRACKET CLOGGED THE DRIP PAN DRAIN WHICH FILLED WITH COFFEE RESIDUE AND STARTED TO BURN OFF WHEN THE COFFEE MAKER WAS USED. REMOVED COFFEE MAKER AND COLLARED C/B IN GALLEY. A/C WAS RTS 2045C/2 3. 2 L 7 2 4F RT A2NM 2001051600494 20010516 00494 NM 2001 5 16 DL73K010667 1 20010423 A 3350 LIGHT BOEING 737 737232 1384475 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 311DL 23083 3 BULLNOSE EMERGENCY EXIT LIGHTS INOP C/A RELAMPED 2 L 7 2 4F RT A16WE 2001051600495 20010516 00495 WP 2001 5 16 DLL14010669 1 20010423 A 3260 DOWNLOCK SENSOR LKHEED 1011 1011385115 5265015 WP NLG OUT OF ADJ A DALA O OTHER N FALSE WARNING AP APPROACH 1 SO 27 740DA 193C1244 ORD/ 601121 WHEN THE GEAR WAS EXTENDED NLG LIGHT DID NOT ILL. TRANS LIGHT REMAINED ON. WENT THRU POM PROCEDURES CK, VISU AL INDICATION DOWN AND LOCKED. AFTER 15 MIN NLG LIGHT GREEN ILLUMINATED . NORM LDG MADE JACKED A/C ADJ NLG DOWN LOCK SE NSOR PER M/M TO PROPER CLEARANCES. RETRACTED AND CYCLED SAME SEVERAL TIMES. ALL IND. AND RATIONAL CKS NORM 2 L 7 3 4F A23WE 2001051600496 20010516 00496 NM 2001 5 16 DLM88010670 1 20010424 A 2910 AS15308K0254 HYDRAULIC LINE DOUG MD88 MD88 3023688 NM HYDRAULIC SYS LEAKING A DALA K NONE K FLUID LOSS AP APPROACH 1 SO 27 968DL 53161 LOSS OF HYD FLUID ON RT SIDE. STOPPED AT 1 QT. MTC FOUND LINE TO RT HYD FILTER MODULE LEAKING. LINE WAS REPLACED. 2 L 7 2 4F RT A6WE 2001051600497 20010516 00497 NM 2001 5 16 DL76G010671 1 20010423 A 2121 FAN BOEING 767 767332 1382001 NM E/E BAY DEFECTIVE A DALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 27 1603 29695 IN FLT NOTICED ELEC BURNING SMELL IN COCKPIT, NO ODOR IN THE CABIN. SHUT DOWN RECIR FAN, SMELL WENT AWAY. FOUND FWD EXHA UST FAN MSG ON EICAS REPLACED FWD EQUIPT EXHAUST FAN. SYS OPS CKS GOOD NO ODOR IN COCKPIT. 2 L 7 2 4F RT A1NM 2001051600498 20010516 00498 NM 2001 5 16 DL72S010672 1 20010424 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 542DA 22391 FOUND ON F 1 LETTER CK. L3 WINDOW FRAME CRACKED AFT LOWER SIDE. REPAIRED PER SRM 53-30-3. 2 L 7 3 4F A3WE 2001051600499 20010516 00499 NE 2001 5 16 DL73K010673 2 20010424 A 7200 JT8D15AHK ENGINE BOEING 737 737247 138448D NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE FAILED A DALA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SO 27 381DL 41656 0 23608 709120 CLIMBING THRU FL300 HEARD LOUD BANG AND LOST ENGINE POWER. OIL QTY DROPPED TO ZERO. REPORT FROM CABIN THAT FIREBALL SEEN FROM INLET FOLLOWED BY SPARKS AND DEBRIS FROM EXHAUST. MTC FOUND OIL STREAM OUT EXHAUST AND MULTIPLE TURBINE BLADES DAM AGED AND MISSING. REPLACED ENGINE 2 L 7 2 4F 4 F A16WE E2EA 2001051600500 20010516 00500 NM 2001 5 16 DL733010674 1 20010417 A 3520 LINE BOEING 737 7373B7 1384580 NM PAX OXYGEN MISINSTALLED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 952WP 23378 DURING THE ACCOMPLISHMENT OF 05-085011-12 IT WAS DISCOVERED THAT SEVERAL CABIN O2 MASK SUPPLY LINES WERE INSTALLED INCOR RECTLY AT THE O2 GENERATOR SUPPLY MANIFOLD OUTLETS. CA CORRECTED TUBE INSTALLATION. 2 L 7 2 4F RT A16WE 2001051600501 20010516 00501 NM 2001 5 16 DL76L010675 1 20010424 A 3350 BPS73 CHARGER BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1200K 28457 SEAT 25 FG EMERGENCY LIGHT INOP. REPLCED SEAT HARNESS AND BATTERY CHARGER M733 2 L 7 2 4F RT A1NM 2001051600502 20010516 00502 2001 5 16 DLM11010676 4 20010424 A 2565 AWD9831503 SLIDE DOUG MD11 MD11 3023602 NM R4 DOOR UNSERVICEABLE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 804DE 48475 PER SERVICE CK NR 3 INSPECTION INDICATED SLIDE AT R4 DOOR ABOVE GIRT BAR, THE CORDS WERE LOOSE AND THE SAFETY BROKEN ON THE PIN. REMOVED AND REPLACED R4 DOOR SLIDE. SN ON 0303 SN OFF 0430 DELTA PN 250007930. 2 L 7 3 4F RT A22WE 2001051600503 20010516 00503 NM 2001 5 16 DL76L010677 1 20010425 A 2121 732591F FAN BOEING 767 767332 1382001 NM E/E BAY FAULTY A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 197DN 28454 ACFT DIVERTED INTO KEF DUE TO SMOKE IN COCKPIT. REPLACED FWD EXH FAN PER M/M 21-58-06-4. LEAK CK AND OPS CKS O.K. NO FA ULT INDICATIONS 2 L 7 2 4F RT A1NM 2001051600504 20010516 00504 NM 2001 5 16 DL73K010678 1 20010426 A 3810 11152054 HEATER BOEING 737 737232 1384475 NM AFT LAVATORY FAULTY A DALA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 316DL 23088 A/C DIVERTED TO CHS.SMOKE /ELECTRICAL SMELL IN AFT LAV/GALLEY FOLLOWED POM. PULLED C/B SMELL DISIPATED. FOUND SOURCE TO BE AFT LAV WATER HEATER 2 L 7 2 4F RT A16WE 2001051600505 20010516 00505 WP 2001 5 16 DLL10010679 1 20010427 A 3350 337001090 CHARGER LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 730DA 193C1199 R2 SLIDE LIGHT INOP. REPLACED CHARGER UNIT. 2 L 7 3 4F A23WE 2001051600506 20010516 00506 NM 2001 5 16 DL73E010681 1 20010425 A 5312 65163007 BULKHEAD BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 379DL 23606 DURING AD 2000-05-29 INSPECTIONS, CRACKS WERE FOUND IN THE CENTER WEB AND LT AND RT SIDE CHORDS OF THE FS 178 BULKHEAD. A COMPLETE MODIFICATION PER SECTION XI OF S/B 737-53A1173 WAS ACCOMPLISHED. 2 L 7 2 4F A16WE 2001051600507 20010516 00507 NM 2001 5 16 DL73K010682 1 20010426 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 310DA 23082 FUSELAGE SKIN AFT GALLEY DOOR CUTOUT AT UPPER HINGE CUTOUT. THE UPPER HINGE CUTOUT OF THE AFT GALLEY DOOR CUTOUT (R2) WAS FOUND WITH A .25 CRACK IN THE SKIN. THE CRACK WAS ROUTED OUT AND REPAIRED WITH AN EXTERNAL STEEL DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 380674-14, REV A. 2 L 7 2 4F RT A16WE 2001051600508 20010516 00508 NM 2001 5 16 DL73K010683 1 20010426 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 310DA 23082 FUSELAGE SKIN AFT GALLEY DOOR CUTOUT AT LOWER HINGE CUTOUT: THE LOWER HINGE CUTOUT OF THE AFT GALLEY DOOR (R2) CUTOUT WA S FOUND WITH A 1 IN CRACK IN THE SKIN AND UNDERLYING BEAR STRAP. THE CRACK WAS ROUTED OUT OF ALL LAYERS OF THE SKIN AS SY AND REPAIRED WITH THREE EXTERNAL ALUMINUM DOUBLERS. THE REPAIR WAS ACCOMPLISHED PER ER/A 380675-14, REV B. 2 L 7 2 4F RT A16WE 2001051600509 20010516 00509 NM 2001 5 16 DL757010684 1 20010427 A 2910 000AE906D0522 HYDRAULIC LINE BOEING 757 757232 1384965 NM RT MLG RUPTURED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 648DL 24372 LEFT HYD QTY LOSS IN FLIGHT. UNABLE TO STOP LOSS WITH POM PROCEDURES. FOUND RIGHT GEAR TRUCK TILT PRESSURE LINE RUPTUR ED. REPLACED LINE. 2 L 7 2 4F RT A2NM 2001051600510 20010516 00510 NM 2001 5 16 DL73K010685 1 20010428 A 2121 215201 GASPER FAN BOEING 737 737247 138448D NM CARGO BAY DEFECTIVE A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 381DL 23608 ON TAKEOFF HAD AN ELECTRICAL BURNING SMELL IN REAR OF CABIN.TURNED OFF GASPER FAN. SMELL DIMINISHED. REPLACED GASPER FAN . NO ODORS PRESENT. 2 L 7 2 4F A16WE 2001051600511 20010516 00511 NM 2001 5 16 DLM11010686 1 20010429 A 3350 LIGHT DOUG MD11 MD11 3023602 NM CABIN INOPERATIVE A DALA H DEACTIVATE SYST/CIRCUITS L J NO TEST WARNING INDICATION IN INSP/MAINT 1 SO 27 809DE 48480 EMER LIGHTT BATTERY 6 LO MSG DISPLAYED AFTER EMER LIGHT TEST. CLEARED SHORT AT SEAT 46AB. MSG CLEARED. WHI TE LIGHT AT SEAT 46AB INOP FWD TO MCO AND PLAC PER MEL 33-50-03B RR 33-50-03B SEAT/SIDEWALL MOUNTED EMERGENCY ESCAPE PATH LIGHTING SYSTEM. 2 L 7 3 4F RT A22WE 2001051600512 20010516 00512 2001 5 16 DL738010688 4 20010430 A 2330 RDAV1113 VIDEO UNIT RDAV1113 BOEING 737 737832 13844CF NM CABIN DEFECTIVE A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 372DA 105028 29620 TAXI. FWD CABIN SMELLED STRONG BURNING ODOR IN VICINITY OF L-1 DOOR PAX IN 1B ALSO SMELLED ODOR F/A VERIFIED IT WAS NOT COMING FROM FWD GALLEY AREA NO SMOKE WAS SEEN. FOUND NR 1 VIDEO CASSETTE PLAYER HAD STRONG SMELL. REPLACED SAME OPS CK G OOD 2 L 7 2 4F RT A16WE 2001051600513 20010516 00513 NM 2001 5 16 DL73K010689 1 20010428 A 5310 65479592 DOOR FRAME BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 301DL 23073 C2 CARGO DOOR OPENING FS 794.3, FWD FRAME FOUND WITH A 1.75 IN CRACK. THE CRACK IS TYPICALOF BAC S/B 737-53-1096 AND AD 93-14-10. THE CRACK WAS REMOVED WITH A 2.1 IN TRIMOUT AND REPAIRED WITH AN ALUMINUM DOUBLER PER THE B737 SRM AND ER/A 380692-14AD. 2 L 7 2 4F RT A16WE 2001051600514 20010516 00514 NM 2001 5 16 DL73K010691 1 20010428 A 5315 6554410138 FLOORBEAM BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 302DL 23047 THE LONGITUDINAL FLOOR BEAM AT RBL 24 WAS FOUND WITH A TYPICAL CRACK IN THE BEAM WEB AND WEB DOUBLER AT FS 678. THE BE AM UPPER CHORD WAS FOUND CRACKED AT FS 674. THE UPPER CHORD WAS REMOVED AND REPLACED. THE WEB DOUBLER WAS REPLACED PER BAC S/B 737-57-1139 AND AN ALUMINUM DOUBLER INSTALLED TO REPAIR THE WEB. THE BEAM WAS THEN MODIFIED PER THE S/B. THE REPAIR WAS ACCOMPLISHED PER ER/A 380644-14. 2 L 7 2 4F RT A16WE 2001051600515 20010516 00515 NM 2001 5 16 DL767010692 1 20010430 A 2560 65B550504 BRACKET BOEING 767 767232 1385132 NM OVERHEAD BIN DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 108DL 22220 ON L/O FOUND 1ST CLASS MEGAPHONE AND MEGAPHONE BRACKET DAMAGED. REPLACED 1ST CLASS MEGAPHONE AND MEGAPHONE BRACKET PER M /M. FOUND BRACKET TO HAVE FAULTY LATCH RESULTING IN AN UNSECURE MEGAPHONE WHICH FELL FROM THE OVERHEAD BIN AND WAS DAMAG ED. 2 L 7 2 4F RT A1NM 2001051600516 20010516 00516 NM 2001 5 16 DL777010694 1 20010430 A 3510 OXYGEN MASK 174660N3 BOEING 777 777232 1385232 NM COCKPIT DAMAGED A DALA K NONE O OTHER CR CRUISE 1 SO 27 863DA 29735 CAPTS O2 MASK CAME APART WHEN TAKING FROM STOWAGE. CAPTS O2 MASK REPLACED LEAK CK CARRIED OUT 2 L 7 2 4F RT T00001SE 2001051600517 20010516 00517 NM 2001 5 16 DL757010695 1 20010430 A 2120 UNKNOWN BOEING 757 757232 1384965 NM CABIN ODOR A DALA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 6716C 30838 DURING TAKEOFF A STRONG HOT ODOR WAS NOTICEABLE THOUGHOUT. ODOR DISSIPATED AFTER POWER WAS REDUCED TO CLIMBOUT. INSP BOT H ENG INTAKES AND EXHAUST, AIR CONDITION BAYS AND OPERATED BOTH ENGS AND BOTH PACKS IN ALL CONFIGURATIONS, NO ABNORMAL O DORS NOTED NO FLUID LEAK NOTED ON EITHER ENG . DID A BIT CK ON A/C CONTROL BOXES. CHECKED OK 2 L 7 2 4F RT A2NM 2001051600518 20010516 00518 NM 2001 5 16 DL72S010696 1 20010417 A 5313 STRINGER BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 STRINGER 18A RT STA 940 CRACKED 1 INCH. REPAIRED PER MM 53-12-000-8 TIME LIMITED I REPAIR 2 L 7 3 4F A3WE 2001051600519 20010516 00519 NM 2001 5 16 DL777010697 1 20010501 A 2530 72077500 OVEN BOEING 777 777232 1385232 NM GALLEY OVERHEATED A DALA K NONE M OVER TEMP CR CRUISE 1 SO 27 862DA 29734 OVEN OVERHEATED. REPLACED OVEN, SYSTEM CHECKS NORMAL. 2 L 7 2 4F RT T00001SE 2001051600520 20010516 00520 NM 2001 5 16 DL733010698 1 20010502 A 5311 6516300301 FRAME BOEING 737 73735B NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 225DL 25069 A CRACK WAS FOUND IN THE LT SIDE CHORD OF THE FS 178 BLKHD. THE DAMAGE WAS REPAIRED PER S/B 737-53-1173 SECTION IX. THE CRACK WAS FOUND DURING THE AD INSPECTION AT HMV. 2 L 7 2 4F RT A16WE 2001051600521 20010516 00521 NM 2001 5 16 DL757010699 1 20010502 A 3350 0201720002 LIGHT BOEING 757 757232 1384965 NM CABIN MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 641DL 23995 SEAT MOUNTED ESCPAPE PATH LIGHTING COMPLETELY MISSING AT SEAT 2CD REPLACED ILLUMINATOR ASSY. OPS CKS OK. 2 L 7 2 4F RT A2NM 2001051600522 20010516 00522 NM 2001 5 16 DL757010700 1 20010502 A 2560 S416N2022001 SEAL BOEING 757 757232 1384965 NM SURVIVAL KIT MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 641DL 23995 SURVIVAL KIT FOR 2L DOOR MISSING LEAD SEAL. REMOVED AND REPLACED SURVIVAL KIT FOR 2L DOOR. 2 L 7 2 4F RT A2NM 2001051600523 20010516 00523 NM 2001 5 16 DL757010701 1 20010502 A 3350 0201720002 LIGHT BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 641DL 23995 SEAT MOUNTED ESCAPE PATH LIGHTING INOP AT SEAT 1CD. RELAMPED SAME, NO HELP. REMOVED/REPLACED ILLUMINATOR ASSY OPS CKS OK . 2 L 7 2 4F RT A2NM 2001051600524 20010516 00524 NM 2001 5 16 DL757010702 1 20010502 A 3350 0201820001 SIGN BOEING 757 757232 1384965 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 641DL 23995 FOUND DURING LAYOVER EMERGENCY EXIT IDENTIFIER AT R2 DOOR F/A SEAT BROKEN REPLACED SIGN BASE AND LENS COVER. OPERATIONA L CK OK. 2 L 7 2 4F RT A2NM 2001051600525 20010516 00525 NM 2001 5 16 DL733010703 1 20010501 A 5330 6545775594 SKIN BOEING 737 737347 1384647 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2310 23596 THE FUSELAGE SKIN AT THE AFT EDGE OF THE C2 DOOR CUTOUT WAS FOUND WITH A SMALL CRACK AT STRINGER 22R. THE CRACK WAS REM OVED WITH A 1.1 IN X .85 IN EDGE TRIM AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 380703-14, REV A. 2 L 7 2 4F RT A16WE 2001051600526 20010516 00526 NM 2001 5 16 DL73K010704 1 20010503 A 5330 SKIN BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 378DL 23605 A 2 INCH LONG CRACK WAS FOUND IN THE FUSELAGE SKIN 3 INCH FWD OF FS 756 AND JUST ABOVE STRINGER 20R. THE CRACK WAS REMO VED WITH A CUTOUT IN THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 380723-14. 2 L 7 2 4F A16WE 2001051600527 20010516 00527 NM 2001 5 16 DL733010705 1 20010502 A 5343 657376118 ATTACH FITTING BOEING 737 737347 1384647 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3301 23181 THE RT MLG SIDE STRUT SUPPORT FITTING AT FS 685 WAS FOUND WITH CORROSION IN THE BORE AND FACES OF THE WL 188.5 LUG. THE CORROSION WAS REMOVED BY OVERSIZING THE LUG BORE AND MACHINING THE LUG FACES. AN ALUMINUM REPAIR BUSHING AND NEW BEAR INGS WERE INSTALLED TO CORRECT THE CONDITION PER ER/A 380714-14, REV A. 2 L 7 2 4F RT A16WE 2001051600528 20010516 00528 NM 2001 5 16 DL72S010706 1 20010417 A 5313 655848827 STRINGER BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 STRINGER 18A LT AT STA 940 HAS A 3/4 INCH VISIBLE CRACK FROM RADIUS BLOCK LOWER BOLTS AND A 1 INCH CRACK FROM RADIUS BLO CK UPPER BOLTS. REPAIRED PER M/M 53-12-000-8 AND ERA 380727-14 ORIGINAL ISSUE. TIME LIMITED LEVEL 2 REPAIR RESTRICTIONS APPLY. REINSPECT REPAIR AT EVERY LETTERCHECK AND COMPLY WITH PERMANENT REPAIR AT NEXT HMV NOT TO EXCEED 15,220 CYCLES FR OM 4-17-01 2 L 7 3 4F A3WE 2001051600529 20010516 00529 NM 2001 5 16 PCAA0105037 1 20010504 A 3230 11300105 ACTUATOR DHAV DHC8 DHC8102 2809003 NM RT MLG BROKEN A PCAA K NONE O OTHER CL CLIMB 1 EA 13 842EX 17309 6593 335 MDT- FLIGHT 3716. CREW REPORTED RIGHT GEAR INTRANSIT LIGHT DOES NOT ILLUMINATE DURING GEAR RETRACTION, OK DURING EXTENS ION. MAINTENANCE FOUND SPRING ON UPLOCK ACTUATOR BROKEN. THE RIGHT GEAR UPLOCK ACTUATOR WAS REMOVED AND REPLACED IN AC CORDANCE WITH DASH 8 MAINTENANCE MANUAL 32-30-26. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001051600530 20010516 00530 NM 2001 5 16 PCAA0105038 1 20010507 A 3350 2078 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM CABIN DEFECTIVE A PCAA K NONE O OTHER NR NOT REPORTED 1 EA 13 819EX 12476 1535 016 LGA FLIGHT 3671. CREW REPORTED EMERGENCY LIGHTS STAY ON WITH THE SWITCH IN THE OFF POSITION. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY/BATTERY PACK IN COAT CLOSET. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001051600531 20010516 00531 GL 2001 5 16 C2XA01IA236 2 20010508 A 7321 23068697 FCU EMB 145 EMB145ER SO ALLSN AE300 AE3007A GL NR 1 ENGINE FAILED A C2XA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 27 15926 145005 IAH - FLIGHT 3838, THE CREW REPORTED THAT ON TAKEOFF ROLL, A NUMBER ONE ENGINE CONTROL B FAIL, AND CONTROL A DEGRADE MES SAGE APPEARED. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED TH E NUMBER 1A FADEC, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001051600532 20010516 00532 EU 2001 5 16 C2XA01IA238 1 20010509 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14830 184 IAH - DURING MAINTENANCE INSPECTION, THE AFT EMERGENCY LIGHT BATTERY PACK WAS FOUND TO HAVE LOW VOLTAGE. MAINTENANCE RE MOVED AND REPLACED THE AFFECTED BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001051600533 20010516 00533 EU 2001 5 16 C2XA01IA239 1 20010509 A 3397 6000 WIRE AEROSP ATR42 ATR42320 8680930 EU PAX DOOR BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14830 184 IAH - DURING MAINTENANCE INSPECTION, THE PASSENGER DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R EPAIRED A BROKEN WIRE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001051600534 20010516 00534 NM 2001 5 16 DL757010680 1 20010426 A 2422 100201021 INVERTER BOEING 757 757232 1384965 NM E/E BAY FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 683DA 27103 A/C 683 FLT 988. ENROUTE SLC-MSY DIVERTED TO OKC DUE TO SULFUR SMELL FUMES IN COCKPIT. IDENTIFIED THE STATIC INVERTER M2 17 DPN 241702694, MFG P/N 1-002-0102-1000, SERIAL NBR CJ001250 AS SOURCE. REPLACED INVERTER. 2 L 7 2 4F RT A2NM 2001051600535 20010516 00535 SW 2001 5 16 20010515SG001 1 20010406 A 5230 HANDLE SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR OUT OF POSITION A BSAA O OTHER O OTHER CL CLIMB 1 NM 05 160MC AC733B DURING CLIMB-OUT, CREW FOUND AIRCRAFT WOULDN''T PRESSURIZE IN EITHER MAN OR AUTO MODE. SUCTION GAUGE SHOWED IN NORMAL R ANGE. RECYCLED CARGO DOOR HANDLE, PRESSURIZATION OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A8SW 2001051600536 20010516 00536 NM 2001 5 16 CALA0100442 1 20010504 A 5320 ANGLE BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59630 27534 INSPECTION FOUND R-2 DOOR Z-ANGLE CORRODED AT STA 991. THE Z-ANGLE WAS REPLACED AND THE DRAIN PAN WAS REINSTALLED IAW S RM 51-10-02 AND 51-40-00. 2 L 7 2 4F RT A16WE 2001051600537 20010516 00537 NM 2001 5 16 CALA0100443 1 20010504 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70330 23460 INSPECTION FOUND FLOORBEAM CORRODED AROUND FASTENER HOLES AT STA 312, LBL 12-RBL 12. THE MAJORITY OF CORROSION WAS BURN ISHED OUT. A REPAIR STRAP WAS INSTALLED IAW SRM 53-00-1 AT ONE LOCATION FOUND OUT OF LIMITS. 2 L 7 2 4F RT A16WE 2001051600538 20010516 00538 WP 2001 5 16 CALA0100444 1 20010505 A 5342 ATTACH ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND A .5 INCH CRACK AT RIVET IN LOWER FLANGE OF RT VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE AT STA 1463 JUST FORWARD OF VERTICAL STABILIZER REAR SPAR PLANE. A REPAIR DOUBLER AND SPLICE WERE INSTALLED IAW SRM 53-05, FIGURE 23 AND 23A. 2 L 7 2 4F A6WE 2001051600539 20010516 00539 NM 2001 5 16 CALA0100445 1 20010507 A 5320 WEB BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 39340 23578 INSPECTION FOUND AFT CARGO PIT FORWARD CORNER INNER WEB CORRODED AT DOOR SILL AREA. THE WEB STRAP WAS REMOVED AND REPLA CED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001051600540 20010516 00540 NM 2001 5 16 CALA0100446 1 20010507 A 5753 SKIN BOEING 737 737524 1384721 NM T/E FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59630 27534 INSPECTION FOUND L/E SKIN WORN WITH A .25 INCH CRACK AT LT WING O/B MIDFLAP O/B HALF. A FILLER AND DOUBLER WERE INSTALL ED IAW SRM 57-53-01, FIGURE 208. 2 L 7 2 4F RT A16WE 2001051600541 20010516 00541 WP 2001 5 16 CALA0100447 1 20010507 A 5210 BEAM DOUG DC9 DC982 3022082 WP L1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND A .5 INCH CRACK IN RADIUS OF L-1 DOOR UPPER INTERNAL BEAM. A T-ANGLE AND DOOR PAN WERE REMOVED FOR ACC ESS IAW SRM 51-10-4 AND A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 31, 51-10-4, AND 51-30-5. 2 L 7 2 4F A6WE 2001051600542 20010516 00542 NM 2001 5 16 CALA0100448 1 20010507 A 5320 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70330 23460 INSPECTION FOUND R-1 DOOR ENTRYWAY Z-ANGLE CORRODED. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-2. 2 L 7 2 4F RT A16WE 2001051600543 20010516 00543 NM 2001 5 16 CALA0100449 1 20010507 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70330 23460 INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT STA 887-947.5. A SEAT TRACK REPAIR WAS INSTALLED IAW SRM 53-00-52, FIG URE 204. 2 L 7 2 4F RT A16WE 2001051600544 20010516 00544 WP 2001 5 16 CALA0100450 1 20010508 A 5320 BEAM DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12061 47851 INSPECTION FOUND REAR PRESSURE BULKHEAD T-SECTION LATERAL BEAM CORRODED AT ATTACHMENT POINTS AT STA Y = 2007 AND X = 58R , 58L, 27R, AND 27L. A NEW BEAM WAS INSTALLED IAW ECRA 5100-01844 AND SRM 53-16-01. 2 L 7 3 4F A22WE 2001051600545 20010516 00545 NM 2001 5 16 CALA0100451 1 20010508 A 5210 SKIN BOEING 737 737524 1384721 NM L1 DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59630 27534 INSPECTION FOUND THE L-1 DOOR SKIN DENTED BELOW UPPER HINGE. A DOUBLER WAS INSTALLED IAW SRM 52-00-01. 2 L 7 2 4F RT A16WE 2001051600546 20010516 00546 CE 2001 5 16 C2XA01CL096 1 20010507 A 7333 12281301 TRANSMITTER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ENGINE ERRATIC A C2XA K NONE O OTHER NR NOT REPORTED 1 SW 27 69549 7492 1294 UE194 CLE FLIGHT 3102, THE CREW REPORTED THE NR 1 ENGINE FUEL FLOW INDICATOR WAS ERRATIC DURING FLIGHT. THE FLUX WAS REPORTED BETWEEN 700PPH AND 1000PPH. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE FUEL FLOW TRANSMITTER. OPERATIONAL CHE CKS WERE GOOD. 2 L 7 2 4T 4 T RT A24CE E26NE 2001051600549 20010516 00549 WP 2001 5 16 ABXA010218 1 20010505 A 3260 H146 SWITCH DOUG DC9 DC932 3022066 WP NLG INTERMITTENT A ABXA O OTHER J WARNING INDICATION AP APPROACH 1 GL 23 986AX 50320 47543 WHEN THE MAIN LANDING GEAR WAS EXTENDED A NOSE GEAR UNSAFE LIGHT DID NOT ILLUMINATE. THE CREW COMPLETED A GEAR RECYCLE AND ALL INDICATIONS CHECKED NORMAL. MAINTENANCE INSPECTED AND REPLACED THE NOSE LANDING GEAR UP LIMIT SWITCH AND COMPLE TED OPERATIONAL CHECKS. 2 L 7 2 4F A6WE 2001051600550 20010516 00550 WP 2001 5 16 ABXA010216 1 20010503 A 7910 OIL CAP DOUG DC8 DC863F 302198F WP NR 4 ENGINE UNSECURE A ABXA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 23 816AX 46093 THE NR 4 ENGINE OIL PRESSURE AND QUANTITY BEGAN TO FLUCTUATE AT THE TOP OF THE DESCENT 10 TO 15 PSI. THE CREW COMPLETED THE ABNORMAL CHECKLIST AND SECURED THE NR 4 ENGINE. MAINTENANCE INSPECTED AND FOUND THE NR 4 ENGINE OIL CAP TO BE UNSE CURED. THE OIL WAS INSPECTED FOR FUEL. NONE WAS NOTED. THE OIL FILTER WAS INSPECTED FOR DEFECTS. NONE WERE NOTED. M AINTENANCE SERVICED THE ENGINE OIL AND COMPLETED AN ENGINE RUN. ALL PARAMETERS CHECKED NORMAL. ALL OTHER ENGINE OILS C APS WERE INSPECTED FOR SECURITY, NO DEFECTS WERE NOTED. 2 L 7 4 4F 4A25 2001051600551 20010516 00551 WP 2001 5 16 ABXA010217 1 20010502 A 3230 35972995501 CONTROL VALVE DOUG DC8 DC861 3021952 WP NLG FAILED A ABXA O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 23 853AX 80000 46037 THE NOSE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF FROM ILN. THE CREW COMPLETED THE ABNORMAL CHECKLIST AND RE-CYCLED THE LANDING GEAR. THE AIRCRAFT WAS INSPECTED FOR AND COMPLETED A MAINTENANCE FERRY FLIGHT FROM EWR TO ILN. ILN MAINTE NANCE INSPECTED AND REPLACED THE NOSE LANDING GEAR CONTROL VALVE IAW DC-8 MM. OPS CHECKS WERE COMPLETED AND THE AIRCRAF T WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2001051600554 20010516 00554 WP 2001 5 16 ABXA010219 1 20010507 A 3350 SWITCH DOUG DC9 DC933F 302207A WP COCKPIT INTERMITTENT A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 THE EMERGENCY EVACUATION LIGHT SWITCH WAS REPORTED AS INTERMITTENT. MAINTENANCE INSPECTED AND REPLACED THE COCKPIT EMER GENCY LIGHT CONTROL SWITCH, AND RELAMPED THE EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT W AS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001051700001 20010517 00001 2001 5 17 DHL2001362012 4 20010428 A 2230 AUTOTHRUST SYS AIRBUS 300 A300B4103 3930104 EU AUTOPILOT SYS MALFUNCTIONED A DHLA K NONE O OTHER CR CRUISE 1 SO 01 362DH 84 AUTO THROTTLE DOES NOT WORK IN THE N1 MODE. DEFERRED N1 PER MEL 22-31-01. PLACARD INSTALLED. UNABLE TO DUPLICATE PROBLEM . AUTO THROTTLE N1 MODE CHECKS NORMAL IAW M/M 22-31-00. 2 L 7 2 4F RT A35EU 2001051700002 20010517 00002 2001 5 17 DHL2001362013 4 20010428 A 2213 K4EM0 CONTROLLER AIRBUS 300 A300B4103 3930104 EU AUTOPILOT SYS FAILED A DHLA K NONE O OTHER CR CRUISE 1 SO 01 362DH 84 AUTO PILOT WILL NOT ENGAGE. DEFERRED NR 1 AP PER MEL 22-11-01. PLACARD INSTALLED. R&R AUTOPILOT CONT MODULE IAW M/M CH 22-11-12. OPS CHECK GOOD. 2 L 7 2 4F RT A35EU 2001051700003 20010517 00003 2001 5 17 DHL2001701006 4 20010428 A 2211 COMPUTER BOEING 727 72730C 1384009 NM AUTOPILOT SYS DEFECTIVE A DHLA K NONE O OTHER CR CRUISE 1 SO 01 701DH 19011 AT FL330 AT M-805 YOKE OSCILLATES BACK AND FORTH WITH AUTO-PILOT SELECT ON SERVO A. DEFERRED A MODE ON A/P PER DHL MEL 2 2-1-11A. PLACARD INSTALLED. REPLACED ROLL CHANNEL COMPUTER PER MM 22-11-111. OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2001051700004 20010517 00004 2001 5 17 DHL2001727012 4 20010428 A 2215 SERVO BOEING 727 727228 NM AUTOPILOT SYS WEAK A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 727DH 20204 IN ALL MODES (TURN KNOB & HEADING SELECT) AIRCRAFT ROLL JERKY. AUTOPILOT WILL NOT TRACK COURSE ON GPS. DISENGAGED NAV/LO C ON AUTOPILOT, AIRCRAFT ROLLED LEFT WITH JERKY MOTION INTO 30DEG. LEFT BANK. THEN TURN KNOB WOULD NOT BANK RIGHT UNTIL AUTOPILOT WAS DISENGAGED/REENGAGED (THIS WAS IN BOTH A&B MODES). DEFERRED AUTOPILOT SYSTEM PER MEL 22-1 PLACARD INSTALL ED. T/S SYS, FOUND A/P AILERON SERVO TO BE WEAK AND JERKY. REMOVED AND REPLACED AILERON SERVO AND OPS CHECKED IAW B727 MM 22-11-11. 2 L 7 3 4F A3WE 2001051700005 20010517 00005 2001 5 17 DHL2001806001 4 20010428 A 2211 2588788905 COMPUTER DOUG DC8 DC873F 302199F WP AUTOPILOT SYS MALFUNCTIONED A DHLA K NONE O OTHER CR CRUISE 1 SO 01 806DH 46002 AUTOPILOT WILL NOT BANK GREATER THAN 10 DEGREE WITH GPS 1 OR 2 IN AUX NAV. ALL LATERAL MODES FUNCTION NORMALLY. R&R ROL L CHANNEL COMPUTER PER DC8 M/M REF 22-12-1. OPS CKS SERVICABLE. P/N OFF 2588788-905, S/N OFF 1180385. P/N ON 2588788-9 05, S/N ON 1070200. 2 L 7 4 4F RT 4A25 2001051700006 20010517 00006 2001 5 17 DHL2001364016 4 20010501 A 2210 AUTOPILOT SYS AIRBUS 300 A300B4203 3930306 EU COCKPIT MALFUNCTIONED A DHLA K NONE J WARNING INDICATION CR CRUISE 1 SO 01 364DH 0141 PITCH TRIM 2 FAILED. OPS CHECK PERFORMED COULD NOT DUPLICATE ON GROUND. SWAPPED PITCH TRIM COMPUTERS FOR TROUBLESHOOTIN G IAW M/M 22-23-00. NO DEFECTS NOTED. 2 L 7 2 4F RT A35EU 2001051700007 20010517 00007 NM 2001 5 17 DHL2001741007 1 20010501 A 2611 302842 SMOKE DETECTOR BOEING 727 7272Q9 138448M NM CARGO BAY MALFUNCTIONED A DHLA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 741DH 21931 AT FL280, MAIN CARGO SMOKE LIGHT ILLUMINATED EMERGENCY PROCEDURES PERFORMED. EMERGENCY LANDING IN TUS.CHANGED NR 4 SMOK E DETECTOR. CK WIRING ON NR 5 SMOKE DET. ALL OK. CK SYSTEM PER AEI M/M CHAP 26. ALL OPERATIONS AND TEST NORMAL. 2 L 7 3 4F RT A3WE 2001051700008 20010517 00008 2001 5 17 DHL2001727013 4 20010501 A 2210 AUTOPILOT SYS BOEING 727 727228 NM COCKPIT MALFUNCTIONED A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 727DH 20204 A/P WILL NOT TRACK GPS WHEN SWITCHING FROM NAV/LOC TO MANUAL. A/P TURNS A/C INTO 30 DEGREE LEFT BANK TURN. OPS CHECK A/ P NO DEFECTS NOTED IAW B-M/M 22-11-11. 2 L 7 3 4F A3WE 2001051700009 20010517 00009 EU 2001 5 17 QXEA0100636 1 20010426 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN FAULTY A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 494US 11167 SEA- BOTH EMERGENCY EXIT SIGNS AT CENTER FUSELAGE OVERHEAD HAVE BULBS OUT. REPLACED CIRCUIT BOARDS. OPERATIONAL CHECKS G OOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001051700010 20010517 00010 EU 2001 5 17 QXEA0100634 1 20010429 A 2611 473597404 SMOKE DETECTOR FOKKER F28 F28MK4000 4990810 EU CARGO BAY MALFUNCTIONED A QXEA K NONE N FALSE WARNING UK UNKNOWN 1 NM 09 482US 3573 3573 11231 PDX- AFT SMOKE DETECTOR IN AFT BAG COMPARTMENT HAS RED LIGHT SHOWING. REMOVED AND REPLACED AFT SMOKE DETECTORS IN AFT CA RGO PIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001051700011 20010517 00011 NM 2001 5 17 QXEA0100633 1 20010424 A 2612 360188100039035 FIRE DETECTOR DHAV DHC8 DHC8202 2809007 NM NR 2 ENGINE MALFUNCTIONED A QXEA K NONE N FALSE WARNING UK UNKNOWN 1 NM 09 356PH 502 RDM- NR 2 ENGINE FAULT B LIGHT ILLUMINATED. REMOVED AND REPLACED NR 2 ENGINE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001051700012 20010517 00012 2001 5 17 DHL2001727014 4 20010501 A 2211 25858052 COMPUTER BOEING 727 727228 NM AUTOPILOT SYS FAILED A DHLA K NONE O OTHER CR CRUISE 1 SO 01 727DH 20204 AUTOPILOT WILL NOT TRACK VOR AND GPS IN BOTH A AND B MODES. T/S AUTOPILOT SYST. FOUND ROLL CHANNEL FAILED. R&R ROLL CH ANNEL. PERFORMED A/P SYSTEM ADJ TEST IAW MM 22-11-01. TESTED NORMAL IN A&B MODES VOR, NAV, LOC, AND HDG SELECT MODES. 2 L 7 3 4F A3WE 2001051700013 20010517 00013 2001 5 17 DHL2001727015 4 20010501 A 2211 25858052 COMPUTER BOEING 727 727228 NM AUTOPILOT SYS FAILED A DHLA K NONE O OTHER CR CRUISE 1 SO 01 727DH 20204 WHEN AUTOPILOT IS SWITCHED FROM NAV/LOC TO HDG SELECT, THE A/C BANKS 20 DEGREES HARD IN THE OPPOSITE DIRECTION. FOUND RO LL CHANNEL FAILED. R&R ROLL CHANNEL. PERFORMED A/P ADJ TEST IAW MM 22-11-01. TESTED NORMAL IN A&B MODES VOR, NAV LOC & HDG SELECT MODES. 2 L 7 3 4F A3WE 2001051700014 20010517 00014 2001 5 17 DHL2001365008 4 20010501 A 2230 AUTOTHRUST SYS AIRBUS 300 A300B4203 3930306 EU COCKPIT MALFUNCTIONED A DHLA K NONE O OTHER CR CRUISE 1 SO 01 365DH 149 AUTOTHROTTLES DROPPED OFF 5 TIMES IN CRUISE AT FL350, EACH TIME IN LIGHT TURBULENCE IN CLOUDS. OK IN LIGHT TURBULANCE I N CLEAR SKIES. RERACKED AUTO THROTTLE COMPUTER. PERFORMED GRND OPS CK, OK IAW MM 22-31-00. 2 L 7 2 4F RT A35EU 2001051700015 20010517 00015 NM 2001 5 17 DHL2001741008 1 20010501 A 2611 WARNING SYSTEM BOEING 727 7272Q9 138448M NM COCKPIT FALSE INDICATION A DHLA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 741DH 21931 WHILE TAXIING IN, THE CARGO SMOKE LIGHT CAME ON MOMENTARILY AND THEN OFF.TESTED MAIN CARGO SMOKE DETECTOR SYSTEM IAW B72 7-200 FREIGHTER MANUAL CHAPTER 26. SYSTEM OPS CHECK GOOD AT THIS TIME. 2 L 7 3 4F RT A3WE 2001051700016 20010517 00016 WP 2001 5 17 DHL2001806616 1 20010402 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - MAIN CARGO COMPT. BATHTUB FITTING CRACKED 2 INCH AT STA 680 L-7L.REMOVED CRACKED BATHTUB FITTING STA 680 L-7L IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW BATHTUB FITTING IAW SRM 51-1-20D PAGE 9. 2 L 7 4 4F RT 4A25 2001051700017 20010517 00017 WP 2001 5 17 DHL2001806617 1 20010406 A 5320 38917681 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - FWD CARGO COMPT. FITTING CRACKED 1/2 INCH AT STA 200 L26R. REMOVED CRACKED FITTING, CLEANED, TREATED AND PRIM ED AREA AND INSTALLED NEW FITTING AT STA 200 L-26RH IAW SRM 51-3-0 PAGE 1, 2, SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2001051700018 20010517 00018 NM 2001 5 17 DHL2001717006 1 20010502 A 2760 SPOILER BOEING 727 72723 1384004 NM LT WING OUT OF POSITION A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 717DH 19389 A/C, WITH BALL CENTERED AND LT WING SLIGHTLY LOW, AILERON TRIM INDICATES 3-1/8 UNITS TO RT, AND RUDDER TRIM 1/4 UNIT TO LT. ALSO THERE WAS 4 DEGREE RT WHEEL DEFLECTION AT FL310 AND MACH 0.80 WITH AUTOPILOT OFF. FOUND NR 2 FLIGHT SPOILER EX TERNAL MANUAL RELEASE NOT PROPERLY STOWED. STOWED MANUAL RELEASE PER B727 MM27-61-81. FLIGHT SPOILER SYSTEM OPERATES N ORMALLY. 2 L 7 3 4F A3WE 2001051700019 20010517 00019 2001 5 17 DHL2001802006 4 20010503 A 2211 2588789904 COMPUTER DOUG DC8 DC873F 302199F WP AUTOPILOT SYS MALFUNCTIONED A DHLA K NONE O OTHER CR CRUISE 1 SO 01 802DH 46076 AUTOPILOT SLOW TO LEVEL OFF FROM CLIMB AND DESCENTS. WHEN SELECTED DESCENT ON AUTOPILOT, AUTOPILOT INITIAL CLIMBS IN LE VEL FLIGHT AUTOPILOT SLOWLY CLIMBS AND THEN IS SLOW TO LEVEL OFF. REPLACED PITCH CHANNEL COMPUTER. OPS CHECK GOOD IAW D C-8 MM 22-13-1. 2 L 7 4 4F RT 4A25 2001051700020 20010517 00020 WP 2001 5 17 DHL2001804008 1 20010503 A 2510 SEAT BELT DOUG DC8 DC873F 302199F WP COCKPIT BROKEN A DHLA K NONE O OTHER CR CRUISE 1 SO 01 804DH 46124 2ND OFFICER SEAT BELT BROKEN. REINSTALLED RT LAP BELT IAW DC-8 MM 25-11-6. OPS CK OK. 2 L 7 4 4F RT 4A25 2001051700021 20010517 00021 EU 2001 5 17 QXEA0100638 1 20010501 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 481US 11230 BOI - THE MAIN CABIN DOOR AND FLIGHT COMPARTMENT ENTRY WAY EXIT SIGNS HAD INOPERATIVE LAMPS. REMOVED AND REPLACED EXIT S IGNS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001051700022 20010517 00022 2001 5 17 DHL2001802007 4 20010504 A 3417 9B8101015 ADC DOUG DC8 DC873F 302199F WP E/E BAY FAULTY A DHLA K NONE O OTHER CR CRUISE 1 SO 01 802DH 46076 AUTOPILOT WILL NOT RESPOND AND LEVEL OFF DURING FLIGHT. ALT HOLD PORTION OF AUTOPILOT DEFERRED IAW MEL 22-8-2E. PLACARD INSTALLED. WAS UNABLE TO DUPLICATE ON GROUND. REPLACED DADC IAW DHL DC-8 SM 34-11-0 AND 22-10-0. PN OFF AND ON 9B-81010 -15, SN OFF 15037, S/N ON 2691. 2 L 7 4 4F RT 4A25 2001051700023 20010517 00023 2001 5 17 DHL2001365009 4 20010503 A 2210 AUTOPILOT SYS AIRBUS 300 A300B4203 3930306 EU COCKPIT MALFUNCTIONED A DHLA K NONE O OTHER CR CRUISE 1 SO 01 365DH 149 AUTOPILOT NR 1 WILL NOT ENGAGE. MEL 22-11-01. REMOVED AND REPLACED A/P MODULE ENGAGE OPS CK AS PER MM 22-10 GOOD. AC OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2001051700024 20010517 00024 2001 5 17 DHL2001743004 4 20010504 A 2210 COUPLER BOEING 727 727225 1384077 NM AUTOPILOT SYS FAULTY A DHLA K NONE F FLT CONT AFFECTED AP APPROACH 1 SO 01 743DH 22438 ON APPROACH WITH AUTOPILOT ENGAGED, FELT UNCOMMANDED RUDDER INPUTS. DISENGAGED AUTOPILOT AND 30 SECONDS LATER INPUTS ST OPPED. CORRECTIVE ACTION - DEFERRED YAW DAMPERS PER DHL MEL 22-6. PLACARD INSTALLED. R&R LOWER YAW COUPLER. PERFORMED BITE TEST IAW MM 22-31-3. OPS CKS GOOD. 2 L 7 3 4F A3WE 2001051700025 20010517 00025 2001 5 17 DHL2001365010 4 20010504 A 2211 COMPUTER AIRBUS 300 A300B4203 3930306 EU AUTOPILOT SYS MALFUNCTIONED A DHLA K NONE N FALSE WARNING CL CLIMB 1 SO 01 365DH 149 DURING ALTITUDE CAPTION WITH ALT ACQ GREEN ON THE FPI, A SUBSQUENT CHANGE TO THE ALTITUDE ALERT WINDOW DOES NOT RESULT IN REVERSION TO ALT ACQ AMBER AND PITCH MODE. BUT REMAINS ALT ACQ GREEN WITH LARGE PITCH CHANGES. RERACKED PITCH COMPUT ERS AND AP/FD LONG COMPUTER. GRND OP''S CK''D OK IAW M/M 22-12-34. 2 L 7 2 4F RT A35EU 2001051700026 20010517 00026 2001 5 17 DHL2001364017 4 20010505 A 2210 AUTOPILOT SYS AIRBUS 300 A300B4203 3930306 EU COCKPIT MALFUNCTIONED A DHLA K NONE O OTHER CR CRUISE 1 SO 01 365DH 149 NR 2 PITCH TRIM DISCONNECTED IN FLIGHT. WOULD NOT RESET. COULD NOT DUPLICATE DISCREPANCY. OPS CK NORMAL. SWAPPED NR 1 AN D NR 2 PITCH TRIM COMPUTERS FOR TROUBLE SHOOTING. OPS CK IS GOOD IAW MM 22-23-34. 2 L 7 2 4F RT A35EU 2001051700027 20010517 00027 2001 5 17 DHL2001743005 4 20010505 A 2210 DAMPER BOEING 727 727225 1384077 NM AUTOPILOT SYS FAILED A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 743DH 22438 AIRCRAFT REQUIRED 4.0 UNITS OF LEFT RUDDER TRIM IN FLIGHT. LOWER RUDDER INDICATES SPLIT WITH UPPER. YAW DAMPER ON LOWE R WOULD NOT CHECK ON TAXI IN. LOWER YAW DAMPER COMP. FAILED. R&R LWR YAW DAMP COMP IAW M/M 22-11-131 AND 22-11-01. OPS CK''D NORMAL. OK FOR SERVICE. 2 L 7 3 4F A3WE 2001051700028 20010517 00028 NM 2001 5 17 DL72E010641 1 20010418 A 8012 97907821 START VALVE BOEING 727 727247 138408F NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE MALFUNCTIONED A DALA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 27 282WA 21484 695285 AT CRUISE THE NR 1 ENG START VALVE ILLUMINATED. FOLLOWED THE POM AND SHUT DOWN ENGINE. OIL PRESSURE AT 37 PSI FOR 1 HOUR AND 10 MINUTES. REPLACED NR 1 ENG. START VALVE AND PRESSURE SWITCH RAN ENG. CK NORMAL. PERFORMED WINDMILLING INSPECTION PER M/M. 2 L 7 3 4F 4 F A3WE E2EA 2001051700029 20010517 00029 WP 2001 5 17 DLL14010642 1 20010419 A 4990 CARBON SEAL LKHEED 1011 1011385115 5265015 WP APU LEAKING A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 737D 193C1228 ON PUSHBACK FROM GATE WHEN STARTING ENGINES, NOTICED HOT PLASTIC SMELL. NOTIFIED BY CABIN ATTENDANTS OF CABIN FILLING WI TH SMOKE AND ALL SMOKE ALARMS GOING OFF. FOUND GARLOCK SEAL FOR APU GENERATOR LEAKING OIL. REPLACED CARBON SEAL. 2 L 7 3 4F A23WE 2001051700030 20010517 00030 NM 2001 5 17 DL72S010687 1 20010430 A 7933 BULB BOEING 727 727232 1384082 NM NR 2 ENGINE FAULTY A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 539DA 700695 22385 700695 IN FLIGHT NR 2 ENGINE OIL TEMP CLIMBED INTO YELLOW ARC. POM PROC ACCOMPLISHED. REPLACED OIL TEMP BULB AND FUEL OIL COOLE R. RAN ENGINE. OP AND LK CK OK 2 L 7 3 4F A3WE 2001051700031 20010517 00031 NM 2001 5 17 DL72S010690 1 20010430 A 7921 749965 OIL COOLER BOEING 727 727232 1384082 NM NR 2 ENGINE FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 539DA 22385 700695 IN FLIGHT NR 2 ENG OIL TEMP CLIMBED INTO THE YELLOW ARC. POM PROCEDURES ACCOMPLISHED. FUEL HEAT WAS CYCLED AND INDICTED A DROP IN EPR. REPLACED NBR 2 ENG FUEL OIL COOLER AND OIL TEMP BULB. RAN ENG PER PFHB. ALL CKS NORMAL. 2 L 7 3 4F A3WE 2001051700032 20010517 00032 NM 2001 5 17 QXEA0100657 1 20010504 A 2611 CONNECTOR DHAV DHC8 DHC8202 2809007 NM SMOKE DETECTOR DIRTY A QXEA K NONE N FALSE WARNING NR NOT REPORTED 1 NM 09 357PH 504 SEA - THE MASTER SMOKE WARNING LIGHT ILLUMINATED MOMENTARALLY. CLEANED CANNON PLUG AT NR 1 & NR 2 SMOKE DETECTORS. NO PA RTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001051700033 20010517 00033 NM 2001 5 17 QXEA0100658 1 20010506 A 3230 LANDING GEAR DHAV DHC8 DHC8202 2809007 NM NLG & MLG MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 347PH 480 PDX - AT TAKE OFF, GEAR FAILED TO RETRACT. INTRANSIT LIGHTS REMAINED ILLUMINATED. LIGHTS WERE ACCOMPANIED BY UNUSUAL NOI SE IN NOSE GEAR WELL. 2 H 7 2 4T RT A13NM 2001051700035 20010517 00035 EU 2001 5 17 QXEA0100661 1 20010506 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 494US 11167 BOI - THE EXIT SIGN OVER THE MAIN CABIN DOOR WAS REPORTED INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECK S GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001051700036 20010517 00036 2001 5 17 DHL2001807010 4 20010508 A 2211 COMPUTER DOUG DC8 DC873 302199C WP AUTOPILOT SYS MALFUNCTIONED A DHLA K NONE O OTHER AP APPROACH 1 SO 01 807DH 45990 AT 12 DEGREE FLAPS AUTOPILOT CLICKED OFF ON APPROACH. RESET CLICKED OFF AT FLAPS 22. R&R PITCH COMPUTER PER M/M 22-13-0 1. PERFORMED TEST OF PITCH TRIM PORTION OF A/P IAW 22-13-01. TEST OK USING TIC 30 BOX. 2 L 7 4 4F RT 4A25 2001051700037 20010517 00037 NM 2001 5 17 QXEA0100640 1 20010429 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- SEAT TRACK NR 2 AT STATION 581 HAS GOUGE IN LOWER TRACK SURFACE. REPAIRED IAW HORIZON AIR EA 2-53-274 AND DHC-8 SRM 51-00-06. 2 H 7 2 4T RT A13NM 2001051700038 20010517 00038 NM 2001 5 17 QXEA0100641 1 20010429 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- SEAT TRACK NR 2 AT STATION 494 HAS MILD PITTING CORROSION. REPAIRED IAW DHC-8 SRM 51-00-06 AND HORIZON AIR EA 2-53- 274. 2 H 7 2 4T RT A13NM 2001051700039 20010517 00039 NM 2001 5 17 QXEA0100642 1 20010429 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- SEAT TRACK NO.2 AT STATION 570 HAS MILD PITTING CORROSION. REPAIRED IAW DHC-8 SRM 51-00-06 AND HORIZON AIR EA 2-53- 274. 2 H 7 2 4T RT A13NM 2001051700040 20010517 00040 NM 2001 5 17 QXEA0100643 1 20010429 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- SEAT TRACK NR 2 AT STATION 458 HAS MILD PITTING CORROSION. REPAIRED IAW DHC-8 SRM 51-00-06 AND HORIZON AIR EA 2-53- 274. 2 H 7 2 4T RT A13NM 2001051700041 20010517 00041 NM 2001 5 17 QXEA0100644 1 20010429 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- SEAT TRACK NR 2 AT STATION 436 HAS MILD PITTING CORROSION. REPAIRED IAW DHC-8 SRM 51-00-06 AND HORIZON AIR EA 2-53- 274. 2 H 7 2 4T RT A13NM 2001051700042 20010517 00042 NM 2001 5 17 QXEA0100645 1 20010501 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- SEAT TRACK NR 3 AT STATION 540 HAS MILD PITTING CORROSION. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-53-3644. 2 H 7 2 4T RT A13NM 2001051700043 20010517 00043 NM 2001 5 17 QXEA0100646 1 20010501 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- SEAT TRACK NR 3 AT STATION 531 HAS MILD PITTING CORROSION ON UPPER FLANGE SURFACE. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD8-53-3644. 2 H 7 2 4T RT A13NM 2001051700044 20010517 00044 NM 2001 5 17 QXEA0100647 1 20010501 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- SEAT TRACK NR 3 AT STATION 521 HAS MILD PITTING CORROSION. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-53-3644. 2 H 7 2 4T RT A13NM 2001051700045 20010517 00045 NM 2001 5 17 QXEA0100648 1 20010429 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- SEAT TRACK NR 4 AT STATION 331 HAS MILD PITTING AND SURFACE CORROSION. REPAIRED IAW DHC-8 SRM 51-00-06 AND HORIZON AIR EA 2-53-273. 2 H 7 2 4T RT A13NM 2001051700046 20010517 00046 NM 2001 5 17 QXEA0100649 1 20010429 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- SEAT TRACK NR 4 AT STATION 312 HAS MILD SURFACE CORROSION UNDER FLANGE LUG. REPAIRED IAW DHC-8 SRM 51-00-06 AND HOR IZON AIR EA 2-53-273. 2 H 7 2 4T RT A13NM 2001051700047 20010517 00047 NM 2001 5 17 QXEA0100650 1 20010429 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- SEAT TRACK NR 4 AT STATION 270 HAS MILD CORROSION UNDER LUG FLANGE. REPAIRED IAW DHC-8 SRM 51-00-06 AND HORIZON AIR EA 2-53-273. 2 H 7 2 4T RT A13NM 2001051700048 20010517 00048 NM 2001 5 17 QXEA0100651 1 20010429 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- SEAT TRACK NR 4 AT STATION 282 HAS MILD CORRROSION UNDER LUG FLANGE. REPAIRED IAW DHC-8 SRM 51-00-06 AND HORIZON AI R EA 2-53-273. 2 H 7 2 4T RT A13NM 2001051700049 20010517 00049 NM 2001 5 17 QXEA0100652 1 20010429 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- SEAT TRACK NR 4 AT STATION 296 HAS MILD PITTING CORROSION UNDER LUG FLANGE. REPAIRED IAW DHC-8 SRM 51-00-06 AND HOR IZON AIR EA 2-53-273. 2 H 7 2 4T RT A13NM 2001051700050 20010517 00050 NM 2001 5 17 QXEA0100653 1 20010429 A 7603 CONTROL CABLE DHAV DHC8 DHC8202 2809007 NM POWER LEVER KINKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- NR 1 ENGINE POWER LEVER CABLE HAS DEFORMED/KINKED BUNDLE STRANDS INBOARD OF FIRST FAIRLEAD FROM NACELLE UNDER LEAD EDGE AREA. REPAIRED IAW DHC-8 SRM 76-10-00 AND 76-10-14. 2 H 7 2 4T RT A13NM 2001051700051 20010517 00051 NM 2001 5 17 QXEA0100654 1 20010426 A 5730 PANEL DHAV DHC8 DHC8202 2809007 NM WING CORRODED A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 345PH 476 PDX- FUEL PANEL 524BT HAS LIGHT FRETTING CORROSION ON ALL FOUR CORNERS OF MATING SURFACE. REPAIRED IAW DHC-8 RD 8-57-320 . 2 H 7 2 4T RT A13NM 2001051700052 20010517 00052 NM 2001 5 17 QXEA0100655 1 20010427 A 5730 PANEL DHAV DHC8 DHC8202 2809007 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- FUEL PANEL 524AT HAS FRETTING CORROSION ON BOTH FORE AND AFT MATING SURFACES ALONG INBOARD HALF OF PANEL. REPAIRED IAW DHC-8 SRM 51-00-06 AND HORIZON AIR EA 2-57-102. 2 H 7 2 4T RT A13NM 2001051700053 20010517 00053 NM 2001 5 17 QXEA0100656 1 20010426 A 5730 PANEL DHAV DHC8 DHC8202 2809007 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- FUEL PANEL 524AT HAS FRETTING CORROSION ON BOTH ENDS OF PANEL. REPAIRED IAW DHC-8 RD 8-57-320. 2 H 7 2 4T RT A13NM 2001051700054 20010517 00054 2001 5 17 SWAA011353 4 20010506 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 634SW 27937 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001051700055 20010517 00055 2001 5 17 DHL2001727016 4 20010508 A 3450 RECEIVER BOEING 727 727228 NM E/E BAY FAULTY A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 727DH 20204 IN CRUISE, AUTOPILOT NAV/LOC WANDERS LT & RT OF COURSE MORE THAN A MILE, MANUAL CORRECTION NEEDED TO HOLD COURSE. TRANSF ERRED ITEM TO DEFERRAL AUTOPILOT VOR.LOC MODE PER MEL 22-1-7. PLACARD INSTALLED. REPLACED NR 1 NAV RECEIVER. A/P SYS O PS NORMAL ON GROUND IAW MM 20-00. 2 L 7 3 4F A3WE 2001051700056 20010517 00056 2001 5 17 DHL2001717007 4 20010508 A 2210 AUTOPILOT SYS BOEING 727 72723 1384004 NM COCKPIT MALFUNCTIONED A DHLA K NONE O OTHER CR CRUISE 1 SO 01 717DH 19389 AUTOPILOT WILL NOT TRACK A VOR OR LOCALIZER. DEFERRED PER DHL MEL 22-1-7. PLACARD INSTALLED. REPLACED NR 1 NAV AND TESTE D PER MM 2200 OP NORMAL TRACK AND CAPTURE. 2 L 7 3 4F A3WE 2001051700057 20010517 00057 2001 5 17 DHL2001803005 4 20010509 A 3421 INDICATOR DOUG DC8 DC873F 302199F WP COCKPIT FAULTY A DHLA K NONE O OTHER CR CRUISE 1 SO 01 803DH 46123 AUTOPILOT WHEN IN HEADING SELECT MODE DIVERGES IN ROLL. FOUND ON STEP 7A & 7B AT ROLL COMPUTER BITE CHECK, MM 22-12-0 PG 101-107, FAILED FULL SCALE RIGHT STOP WHEN SELECTING CAPT''S NAVIGATION INFO VIA NAV SELECT BUTTON. AUTOPILOT CONTROL P ANEL ROLL COMPUTER BITE TEST OK WHEN USING F/O NAVIGATION INFO. PROBLEM FOLLOWED WHEN SWAPPED CAPT & F/O PDI. REINSTAL LED CAPT & F/O PDI TO ORIGINAL POSITIONS. NEED NEW CAPT PDI IND. PLACARD INSTALLED. R&R CAPT PDI. PDI TESTS GOOD PER MM 34-21-0 & AUTOPILOT CKS GOOD PER MM22-10-0. 2 L 7 4 4F RT 4A25 2001051700058 20010517 00058 2001 5 17 DHL2001720010 4 20010509 A 3450 5224280105 RECEIVER BOEING 727 727228 NM E/E BAY FAULTY A DHLA K NONE F FLT CONT AFFECTED AP APPROACH 1 SO 01 720DH 19544 A/C PITCHES UP & DOWN ON ILS IN A & B MODE. R&R NAV UNIT IAW MM REF 34-31-21. GRND OP CK OK. 2 L 7 3 4F A3WE 2001051700059 20010517 00059 EU 2001 5 17 DHL2001362014 1 20010509 A 2433 F11QB3121 TRANSFORMER AIRBUS 300 A300B4103 3930104 EU E/E BAY FAILED A DHLA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 362DH 84 ESS TR OFF LIGHT ILLUMINATED DURING FLIGHT. CREW PERFORMED ABNORMAL PROCEDURE BY AOM. REMOVED AND REPLACED ESS T/R AS P ER MM 24-32-11. OPS CHECKED GOOD 2 L 7 2 4F RT A35EU 2001051700060 20010517 00060 EU 2001 5 17 QXEA0100635 1 20010428 A 3350 LIGHT FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 482US 11231 BIL- EMERGENCY EXIT ROW 9 SEAT A LIGHT INOPERATIVE. 2 L 7 2 4F RT A20EU 2001051700061 20010517 00061 NM 2001 5 17 QXEA0100662 1 20010501 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- AFT FUSELAGE SKIN IS SCRATCHED 3/4 INCH LONG, 3 INCH BELOW BAG DOOR THRESHOLD. REPAIRED IAW DHC-8 SRM 53-00-16, 51- 20-16 AND 51-20-26. 2 H 7 2 4T RT A13NM 2001051700062 20010517 00062 NM 2001 5 17 QXEA0100663 1 20010501 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- AFT FUSELAGE SKIN IS SCRATCHED BELOW BAG DOOR THRESHOLD 9.5 INCH AFT OF LOWER FORWARD CORNER 1 INCH BELOW DOOR. REP AIRED IAW DHC-8 SRM 53-00-16, 51-20-16 AND 51-20-26. 2 H 7 2 4T RT A13NM 2001051700063 20010517 00063 NM 2001 5 17 QXEA0100664 1 20010502 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- SEVERAL SCRATCHES/GOUGES ON FUSELAGE SKIN ABOVE PANEL 122BR AROUND UPPER SCREW HOLE SECOND FROM AFT CORNER. REPAIRE D IAW DHC-8 SRM 53-00-16 AND RD 8-53-2432. 2 H 7 2 4T RT A13NM 2001051700064 20010517 00064 NM 2001 5 17 QXEA0100665 1 20010426 A 3222 ARM DHAV DHC8 DHC8202 2809007 NM NLG CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- NOSE GEAR LOWER STRUT ARM HAS CHAFE DAMAGE. REPAIRED IAW DHC-8 RD 8-32-289. 2 H 7 2 4T RT A13NM 2001051700065 20010517 00065 NM 2001 5 17 QXEA0100666 1 20010429 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- CORROSION PITS ON RIGHT HAND OUTBOARD SEAT TRACK NR 10 AT STATION 299. REPAIRED IAW DHC-8 SRM 51-00-06 AND HORIZON AIR EA 2-53-274. 2 H 7 2 4T RT A13NM 2001051700066 20010517 00066 NM 2001 5 17 QXEA0100667 1 20010429 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- CORROSION PITS ON RIGHT HAND OUTBOARD SEAT TRACK NR 10 AT STATION 312. REPAIRED IAW DHC-8 SRM 51-00-06 AND HORIZON AIR EA 2-53-274. 2 H 7 2 4T RT A13NM 2001051700067 20010517 00067 NM 2001 5 17 QXEA0100668 1 20010429 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- CORROSION PITS ON RIGHT HAND OUTBOARD SEAT TRACK NR 10 AT STATION 330. REPAIRED IAW DHC-8 SRM 51-00-06 AND HORIZON AIR EA 2-53-274. 2 H 7 2 4T RT A13NM 2001051700068 20010517 00068 NM 2001 5 17 QXEA0100669 1 20010429 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- CORROSION PITS ON RIGHT HAND OUTBOARD SEAT TRACK NR 10 AT STATION 343. REPAIRED IAW DHC-8 SRM 51-00-06 AND HORIZON AIR EA 2-53-274. 2 H 7 2 4T RT A13NM 2001051700069 20010517 00069 NM 2001 5 17 QXEA0100670 1 20010502 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- CORROSION PITS ON RIGHT HAND OUTBOARD SEAT TRACK NR 10 AT STATION 375. REPAIRED IAW DHC-8 SRM 51-00-06 AND HORIZON AIR EA 2-53-276. 2 H 7 2 4T RT A13NM 2001051700070 20010517 00070 NM 2001 5 17 QXEA0100671 1 20010502 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- CORROSION PITS ON RIGHT HAND OUTBOARD SEAT TRACK NR 10 AT STATION 405. REPAIRED IAW DHC-8 SRM 51-00-06 AND HORIZON AIR EA 2-53-276. 2 H 7 2 4T RT A13NM 2001051700071 20010517 00071 NM 2001 5 17 QXEA0100672 1 20010429 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- CORROSION PITS ON RIGHT HAND OUTBOARD SEAT TRACK NR 11 UPPER FLANGE AT STATION 468. REPAIRED IAW DHC-8 SRM 51-00-06 AND HORIZON AIR EA 2-53-274. 2 H 7 2 4T RT A13NM 2001051700072 20010517 00072 NM 2001 5 17 QXEA0100673 1 20010429 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- CORROSION PITS ON RIGHT HAND OUTBOARD SEAT TRACK NR 11 AT STATION 468. REPAIRED IAW DHC-8 SRM 51-00-06 AND HORIZON AIR EA 2-53-274. 2 H 7 2 4T RT A13NM 2001051700073 20010517 00073 NM 2001 5 17 QXEA0100674 1 20010429 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- CORROSION PITS ON RIGHT HAND OUTBAORD SEAT TRACK NR 11 AT STATION 487. REPAIRED IAW DHC-8 SRM 51-00-06 AND HORIZON AIR EA 2-53-274. 2 H 7 2 4T RT A13NM 2001051700074 20010517 00074 NM 2001 5 17 QXEA0100675 1 20010501 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- MINOR GOUGES FROM SEAT FOOT ON RIGHT HAND OUTBOARD SEAT TRACK NR 12 AT STATION 541. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-53-8644. 2 H 7 2 4T RT A13NM 2001051700075 20010517 00075 NM 2001 5 17 QXEA0100676 1 20010429 A 5320 RIVET DHAV DHC8 DHC8202 2809007 NM SEAT TRACK CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- SEAT TRACK NR 4 AT STATION 182 THROUGH 201 OUTBOARD FLANGE HAS SEVERAL RIVETS CORRODED. REPAIRED IAW DHC-8 SRM 51- 00-06 AND HORIZON AIR EA 2-53-273. 2 H 7 2 4T RT A13NM 2001051700076 20010517 00076 NM 2001 5 17 QXEA0100677 1 20010429 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- SEAT TRACK NR 5 AT STATION 438 HAS A SEVERE GOUGE IN TRACK. REPAIRED IAW DHC-8 SRM 51-00-06 AND HORIZON AIR EA 2-53 -272. 2 H 7 2 4T RT A13NM 2001051700077 20010517 00077 NM 2001 5 17 QXEA0100678 1 20010429 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- SEAT TRACK NR 4 AT STATION 240.5 INBOARD FLANGE CORRODED ON UNDER SIDE. REPAIRED IAW DHC-8 SRM 51-00-06 AND HORIZON AIR EA 2-53-273. 2 H 7 2 4T RT A13NM 2001051700078 20010517 00078 NM 2001 5 17 QXEA0100679 1 20010429 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- REPLACE RIGHT HAND INBOARD FORWARD NR 7 SEAT TRACK DUE TO NUMEROUS DISCREPANCIES. REPAIRED IAW DHC-8 SRM 51-40-00, 51-40-11 AND RD 8-53-4472. 2 H 7 2 4T RT A13NM 2001051700079 20010517 00079 NM 2001 5 17 QXEA0100681 1 20010428 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- REPLACED LEFT HAND OUTBOARD FORWARD SEAT TRACK NR 1 DUE TO NUMEROUS DISCREPANCIES. REPAIRED IAW DHC-8 51-40-11. 2 H 7 2 4T RT A13NM 2001051700080 20010517 00080 NM 2001 5 17 QXEA0100683 1 20010423 A 5330 SHIELD DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- RIGHT HAND FUSELAGE ICE SHIELD AREA HAS LIGHT SURFACE CORROSION AROUND NUTPLATE HOLES. REPAIRED IAW DHC-8 SRM 53-00 -16, 51-20-16 AND HORIZON AIR EA 2-53-179. 2 H 7 2 4T RT A13NM 2001051700081 20010517 00081 NM 2001 5 17 QXEA0100684 1 20010423 A 5330 SHIELD DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- LEFT HAND FUSELAGE ICESHIELD AREA HAS LIGHT SURFACE CORROSION AROUND NUTPLATE HOLES. REPAIRED IAW DHC-8 SRM 53-00-1 6, 51-20-16 AND HORIZON AIR EA 2-53-179. 2 H 7 2 4T RT A13NM 2001051700082 20010517 00082 NM 2001 5 17 QXEA0100659 1 20010504 A 3350 82520977001 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 374PH 528 PSC - UPON INSPECTION, FOUND FIRST TWO LIGHTS ON FLOOR PATH LIGHTING INOP. REMOVED AND REPLACED LIGHT ASSEMBLY. OPERATIO NAL CHECKS GOOD AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001051700083 20010517 00083 NM 2001 5 17 QXEA0100685 1 20010504 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- FUSELAGE SKIN ABOVE F/O''S WINSHIELD IS SCRATCHED 9.5 INCH FROM UPPER OUTBOARD WINSHIELD CORNER. REPAIRED IAW DHC-8 SRM 51-00-16. 2 H 7 2 4T RT A13NM 2001051700084 20010517 00084 NM 2001 5 17 QXEA0100686 1 20010504 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- FUSELAGE FORWARD LEFT HAND SIDE SKIN IS SCRATCHED AT STATION 136.800 AND Z129.00. REPAIRED IAW DHC-8 SRM 51-00-16. 2 H 7 2 4T RT A13NM 2001051700085 20010517 00085 NM 2001 5 17 QXEA0100687 1 20010501 A 7110 SEAL DHAV DHC8 DHC8202 2809007 NM COWL DOOR MISSING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- RT ENGINE OUTBOARD FORWARD COWL DOOR 424AR IS MISSING 2 SECTIONS OF RED RUBBER SEAL ON THE INSIDE OF THE DOOR. REPL ACED MISSING RED RUBBER SEAL. 2 H 7 2 4T RT A13NM 2001051700086 20010517 00086 NM 2001 5 17 QXEA0100688 1 20010505 A 7110 DOOR DHAV DHC8 DHC8202 2809007 NM RT COWLING DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- RT ENGINE OUTBOARD AFT COWL DOOR 426AR IS DENTED AND BUCKLED AT LOWER EDGE OF DOOR. REPAIRED IAW DHC-8 SRM 51-00-06 AND HORIZON AIR EA 2-71-136. 2 H 7 2 4T RT A13NM 2001051700087 20010517 00087 NM 2001 5 17 QXEA0100689 1 20010428 A 5730 SKIN DHAV DHC8 DHC8202 2809007 NM LT WING SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- LT WING AT STATION YW 279.00 UPPER SKIN FORWARD EDGE IS SCRATCHED. REPAIRED IAW DHC-8 SRM 51-20-16, 51-20-56 AND HO RIZON AIR EA 2-57-100. 2 H 7 2 4T RT A13NM 2001051700088 20010517 00088 NM 2001 5 17 QXEA0100690 1 20010427 A 5730 PANEL DHAV DHC8 DHC8202 2809007 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- FUEL PANEL 524BT HAS LIGHT CORROSION ON ALL FOUR CORNERS OF MATING SURFACE. REPAIRED IAW DHC-8 SRM 51-00-06 AND HOR IZON AIR EA 2-57-103. 2 H 7 2 4T RT A13NM 2001051700089 20010517 00089 NM 2001 5 17 QXEA0100691 1 20010427 A 5730 PANEL DHAV DHC8 DHC8202 2809007 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- FUEL PANEL 524AT HAS FRETTING CORROSION ON BOTH ENDS OF PANEL. REPAIRED IAW DHC-8 SRM 51-00-06 AND HORIZON AIR EA 2 -57-103. 2 H 7 2 4T RT A13NM 2001051700090 20010517 00090 NM 2001 5 17 QXEA0100692 1 20010428 A 5753 SKIN DHAV DHC8 DHC8202 2809007 NM RT FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- RT WING INBOARD FLAP HAS CHAFE DAMAGE WITH BARE METAL ON UPPER SKIN SURFACE AT STATION 74.000. REPAIRED IAW DHC-8 R D 8-57-1022. 2 H 7 2 4T RT A13NM 2001051700091 20010517 00091 NM 2001 5 17 QXEA0100693 1 20010428 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- 1/2 INCH SCRATCH ON THE CARGO DOOR EXTERNAL SKIN AFT OF STATION X580.00 AND 5 7/8 INCH FROM THE TOP OF DOOR. REPAIR ED IAW DHC-8 SRM 52-00-16, 51-40-00, 51-40-11 AND RD 8-52-029. 2 H 7 2 4T RT A13NM 2001051700092 20010517 00092 NM 2001 5 17 QXEA0100694 1 20010426 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- TOP OF CARGO DOOR SKIN HAS 5 EACH SCRATCHES FROM DOOR HITTING AIRFRAME. REPAIRED IAW DHC-8 SRM 52-00-16 AND 51-20-1 6. 2 H 7 2 4T RT A13NM 2001051700093 20010517 00093 NM 2001 5 17 QXEA0100695 1 20010501 A 5220 RETAINER DHAV DHC8 DHC8202 2809007 NM ESCAPE HATCH BENT A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- ESCAPE HATCH SEAL RETAINER BENT NEXT TO FORWARD RIGHT HAND LATCH. REPAIRED IAW DHC-8 SRM 52-20-11 AND 51-40-11. 2 H 7 2 4T RT A13NM 2001051700094 20010517 00094 NM 2001 5 17 QXEA0100696 1 20010502 A 5210 SKIN DHAV DHC8 DHC8202 2809007 NM PAX DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- MAIN CABIN SHELL ALUMINUM SKIN HAS SMOOTH DENT AT FORWARD EDGE EVEN WITH UPPER STOPS. REPAIRED IAW DHC-8 SRM 51-00- 06, 51-00-05 AND HORIZON AIR EA 2-52-92. 2 H 7 2 4T RT A13NM 2001051700095 20010517 00095 NM 2001 5 17 QXEA0100697 1 20010428 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- 1/4 INCH SCRATCH ON THE CARGO DOOR EXTERNAL SKIN AFT OF STATION X564.00 3/4 FROM THE TOP OF DOOR. REPAIRED IAW DHC- 8 SRM 52-00-16. 2 H 7 2 4T RT A13NM 2001051700096 20010517 00096 NM 2001 5 17 QXEA0100698 1 20010501 A 5220 RETAINER DHAV DHC8 DHC8202 2809007 NM ESCAPE HATCH BENT A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX- ESCAPE HATCH SEAL RETAINER IS BENT NEXT TO FORWARD LEFT HAND LATCH. REPAIRED IAW DHC-8 SRM 51-40-11 AND 52-20-11. 2 H 7 2 4T RT A13NM 2001051700097 20010517 00097 NM 2001 5 17 QXEA0100699 1 20010510 A 3350 H8251002601 LIGHT DHAV DHC8 DHC8202 2809007 NM COCKPIT DEFECTIVE A QXEA K NONE O OTHER NR NOT REPORTED 1 NM 09 359PH 514 BOI - FLIGHT COMPARTMENT OVERHEAD EMERGENCY LIGHT WILL NOT STAY LATCHED. REMOVED AND REPLACED FLIGHT COMPARTMENT EMERGEN CY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001051700098 20010517 00098 EU 2001 5 17 QXEA0100700 1 20010507 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478US 11227 BOI - MID CABIN EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETU RNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001051700099 20010517 00099 EU 2001 5 17 QXEA0100701 1 20010508 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478US 11227 BOI - EXIT SIGN AT CABIN ENTERENCE, AND AT OVER FLIGHT COMPARTMENT DOOR INOPERATIVE. REMOVED AND REPLACED EXIT SIGNS. OP ERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001051700100 20010517 00100 EU 2001 5 17 QXEA0100702 1 20010506 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 481US 11230 GEG - AISLE EXIT SIGN FOUND TO HAVE BURNT BULBS. REMOVED AND REPLACED EXIT SIGN. OPERTAIONAL CHECKS GOOD. AIRCRAFT RETUR NED TO SERVICE. 2 L 7 2 4F RT A20EU 2001051700101 20010517 00101 CE 2001 5 17 20010515SG002 1 20010403 A 2730 1016100197 TORQUE TUBE BEECH 1900 1900D 1154162 CE ELEVATOR LOOSE A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 44812 237 UE410 DURING UNSCHEDULED MAINTENANCE OF FLIGHT CONTROL SYSTEM, FOUND LEFT ELEVATOR TORQUE TUBE LOOSE CREATING EXCESSIVE FREE O F PLAY OF CONTROL SURFACE. SIX OF THE 8 RIVETS WERE SMOKING. ELEVATOR STOPS WERE NOT ADJUSTED CORRECTLY WHICH CAN CAUS E OR CONTRIBUTE TO THIS PROBLEM. (M) 2 L 7 2 4T RT A24CE 2001051700102 20010517 00102 CE 2001 5 17 20010515SG003 1 20010316 A 2730 1016100198 TORQUE TUBE BEECH 1900 1900D 1154162 CE ELEVATOR LOOSE A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 833CA 1834 UE24 DURING SCHEDULED INSPECTION, RT ELEVATOR FREE PLAY FAILED ALLOWABLE LIMITS. PROBLEM WAS DISCOVERED AS THE ELEVATOR TORQ UE TUBE RIVETS BEING LOOSE AND WORN. UNIT REPLACED WITH NEW. OLD UNIT RETURNED TO MANUFACTURE. (M) 2 L 7 2 4T RT A24CE 2001051700103 20010517 00103 CE 2001 5 17 20010515SG004 1 20010309 A 2730 1016100197 TORQUE TUBE BEECH 1900 1900D 1154162 CE ELEVATORS LOOSE A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 848CA UE53 DURING SCHEDULED MAINTENANCE, FOUND LEFT AND RIGHT ELEVATORS FREE PLAY EXCESSIVE AND BEYOND THE EXCEPTABLE LIMITS. INVE STIGATION RESULTED THAT BOTH ELEVATOR TORQUE TUBE RIVETS WERE LOOSE AND SMOKING. UNITS REPLACED WITH NEW. (M) 2 L 7 2 4T RT A24CE 2001051700104 20010517 00104 CE 2001 5 17 20010515SG005 1 20010106 A 2730 1016100198 TORQUE TUBE BEECH 1900 1900D 1154162 CE ELEVATOR LOOSE A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 838CA UE396 DURING SCHEDULED INSPECTION, DISCOVERED LOOSE RIVETS ON RT ELEVATOR TORQUE TUBE, RESULTING IN EXCESSIVE FREE PLAY OF ELE VATOR. INSPECTED CONTROL SYTEM FOR OTHER DEFECTS, NONE NOTED. REPLACED TORQUE TUBE WITH NEW UNIT. (M) 2 L 7 2 4T RT A24CE 2001051700105 20010517 00105 2001 5 17 DHL2001807012 4 20010515 A 2210 1776001154 CONTROL PANEL DOUG DC8 DC873 302199C WP AUTOPILOT SYS MALFUNCTIONED A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 807DH 45990 AUTOPILOT PITCH CONTROL IS ERRATIC IN CLIMB AND TURNS. R&R A/P CONTROL PANEL IAW 22-10-2. A/P CHECKS GOOD. 2 L 7 4 4F RT 4A25 2001051700106 20010517 00106 2001 5 17 DHL2001364018 4 20010512 A 2211 COMPUTER AIRBUS 300 A300B4203 3930306 EU AUTOPILOT SYS MALFUNCTIONED A DHLA K NONE O OTHER CR CRUISE 1 SO 01 364DH 0141 NR 2 PITCH TRIM DISCONNECTED TWICE IN FLIGHT. RESET OPS NORMAL. DEFERRED NR 2 PITCH TRIM IAW MEL 22-11-03. C/W S.P. 22 -11-03-A.2. REMOVED AND REPLACED NR 2 PITCH COMPENSATION COMPUTER AND OPS CHECK OK PER 22-23-00. 2 L 7 2 4F RT A35EU 2001051700107 20010517 00107 2001 5 17 DHL2001365012 4 20010512 A 2210 DAMPENER AIRBUS 300 A300B4203 3930306 EU AUTOPILOT SYS MALFUNCTIONED A DHLA K NONE O OTHER CR CRUISE 1 SO 01 365DH 149 NR 1 YAW DAMPNER DIFFICULT TO ENGAGE. DROPS BACK OFF BEFORE CATCHING. COULD NOT DUPLICATE PROBLEM. SWAPPED NR 1 & NR 2 Y AW COMPUTERS. OPS CKS GOOD ON GND IAW A300 MM 22-21-00. 2 L 7 2 4F RT A35EU 2001051700108 20010517 00108 2001 5 17 DHL2001365014 4 20010512 A 2230 COMPUTER AIRBUS 300 A300B4203 3930306 EU AUTOPILOT SYS NOT SEATED A DHLA K NONE N FALSE WARNING CR CRUISE 1 SO 01 365DH 149 N1 LIMIT COMPUTER INTERMITTENT DISPLAY ERROR W/AUTO THROTTLE DISENGAGED. NOTE: S/O AUTOTHROTTLE TRE-FOIL INDICATED TRIP . RESEATED N1 LIMIT COMPUTER IAW MM 31-42-11 SYSTEM OPS CFS GOOD. 2 L 7 2 4F RT A35EU 2001051700109 20010517 00109 2001 5 17 DHL2001807013 4 20010515 A 2211 2588789904 COMPUTER DOUG DC8 DC873 302199C WP AUTOPILOT SYS MALFUNCTIONED A DHLA K NONE O OTHER CL CLIMB 1 SO 01 807DH 45990 AUTOPILOT PITCH CONTROL IS ERRATIC IN CLIMB AND TURNS (JERKS CENTER YOKE BACK & FORTH). REMOVED AND REPLACED PITCH CHANN EL 2 COMPUTER IAW DC-8 MM CH 22-13-1. AUTOPILOT PITCH CONTROL OPS CK NORMAL. 2 L 7 4 4F RT 4A25 2001051800001 20010518 00001 2001 5 18 DHL2001365007 4 20010501 A 3425 4004255901 ADI AIRBUS 300 A300B4203 3930306 EU COCKPIT FAILED A DHLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 365DH 149 ON TAXI OUT F/O FD WENT OUT, F/O ADI, FD, GSL & RW FLAGS IN VIEW. BOTH CAPTAINS & F/O RMI RDG VOR 1 & VOR 2 FLAGS IN VI EW, COMPASS 26V VAC BREAKER TRIPPED. R&R F/O ADI. OPS CK ON GRND OK PER AMM 34-25-23. 2 L 7 2 4F RT A35EU 2001051800002 20010518 00002 NM 2001 5 18 DHL2001721002 1 20010430 A 5754 65162276 CASTING BOEING 727 727228 NM L/E FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 NR 6 FLAP CENTER HINGE MOUNT CASTING CRACKED. R/R NR 6 FLAP WITH NEW, IAW B727 MM 27-81-1. OPS CK GOOD. 2 L 7 3 4F A3WE 2001051800004 20010518 00004 NM 2001 5 18 DHL2001712006 1 20010504 A 3240 TRANSMITTER BOEING 727 72729 1384007 NM BRAKE SYS LEAKING A DHLA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 712DH 19401 WITH PACKS OPERATING AFTER ABOUT 15 MINUTES ON THE GROUND DURING PREFLIGHT, SMOKE FILLED THE COCKPIT. TURNED OFF LEFT P ACK TO STOP SMOKE.FOUND BRAKE PRESSURE XMITR IN RT MLG WHEEL WELL LEAKING. REPLACED DAMAGED O-RING SEAL. LEAKAGE FROM XM TR LEAKING ON APU DUCT CAUSED SMOKE. OPS CK GOOD PER MM 29-33-1. 2 L 7 3 4F A3WE 2001053100255 20010531 00255 NM 2001 5 31 DHL2001705511 1 20010420 A 5714 651620252 STIFFENER BOEING 727 72722C 138400F NM WING CNTR BOX CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C-CHECK- WING CENTER SECTION STA 870 WEB VERTICAL STIFFENER AT BL 0 HAS CORROSION. REMOVED WEB VERTICAL STIFFENER AT WING CENTER SECTION FOR REPLACEMENT AS PER B727 SRM 51-30-2. INSTALLED NEW VERTICAL STIFFENER AT CENTER SECTION BS 870 BL 0 AS PER B727 SRM 57-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 2001053100254 20010531 00254 NM 2001 5 31 DHL2001705510 1 20010415 A 5310 PRESSURE PANEL BOEING 727 72722C 138400F NM NLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 C-CHECK- NLG WW RT SIDEWALL PANEL IS CRACKED BS 285.6 WL 158. CRACK RUNNING ALONG FASTENER ROWS-2 PLACES. INSTALLED DOUB LER REPAIR AT NLG WW RT SIDE FABRICATED EXTERNAL DOUBLER REPAIR AT NOSE WW RT SIDEWALL FROM BS 250 TO 294.5 AS PER B727 S/B 53-0065- MAT USED 2024 T3 .050 38 X 34 INCH LOT 35831 PO 83112359. ALODINED AND PRIMED AS PER B727 SRM 51-10-2. IN STALLED DOUBLER AS PER B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2001053100257 20010531 00257 2001 5 31 DHL2001705514 4 20010417 A 3452 103327 ANTENNA BOEING 727 72722C 138400F NM FUSELAGE DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C-CHECK- NR 2 ATC ANTENNA DELAMINATED AND GASKET DETERIORATED. REMOVED NR 2 ATC ANTENNA AND ROUTED TO STOCK IAW B727 MM 34-43-41. INSTALLED NR 2 ATC ANTENNA AS PER B727 MM 34-43-41. OPS CHECK NR 2 ATC SYSTEM PER B727 MM 34-43-0. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2001053100268 20010531 00268 NM 2001 5 31 DHL2001705516 1 20010416 A 5720 652165828 ANGLE BOEING 727 72722C 138400F NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C-CHECK-T/E LWR PANEL SUPPORT ANGLE IS CRACKED AT STA 545. REPLACED T/E LWR PANEL SUPPORT ANGLE AT R/W STA 545 PER B 727 SRM 51-30-2. 2 L 7 3 4F A3WE 2001053100266 20010531 00266 NM 2001 5 31 DHL2001705515 1 20010430 A 5320 WEB BOEING 727 72722C 138400F NM NLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 C-CHECK WEB CRACKED AT NLG WW RT SIDE AT STA 257 W/L 180 IN BETWEEN PANELS 3123 AND3125 AT 3 EA LOCATION. INSTALLED FILL ER & DOUBLER REPAIR AT NLG WW RT SIDE AT STA 257 W/L 180 AS PER B727 S/B 53-00-65. 2 L 7 3 4F A3WE 2001053100267 20010531 00267 NM 2001 5 31 DHL2001705518 1 20010419 A 5730 PANEL BOEING 727 72722C 138400F NM LT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 C-CHECK- LT WING FIXED LEADING EDGE. CORNER OF L/E PANEL IS BROKEN OFF. LOCATED DIRECTLY BELOW GHE I/B WING ROOT LANDING LIGHT ASSY. INSTALLED DOUBLER & FILLER. 2 L 7 3 4F A3WE 2001051800005 20010518 00005 NM 2001 5 18 DHL2001705519 1 20010417 A 5320 ATTACH ANGLE BOEING 727 72722C 138400F NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 C-CHECK- MAIN CARGO DOOR CUT-OUT AT BS 510 GILLLINER ATTACHING ANGLE DAMAGED. REMOVED & REPLACED GILL LINER ATTACH ANGLE . 2 L 7 3 4F A3WE 2001051800006 20010518 00006 NM 2001 5 18 DHL2001705520 1 20010419 A 5320 FLOOR SUPPORT BOEING 727 72722C 138400F NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 C-CHECK- CORROSION, FLOOR SUPPORT AFT BAGGAGE COMPART STA 1160 STR 26 WL 156 LBL 24 UNDER SIDE. REMOVED AND INSTALLED NE W FLOOR SUPPORT AT AFT CARGO COMPT BS 1160 FROM STR 26L TO 26R AS PER B727SRM 51-40-2 AND 51-30-2. 2 L 7 3 4F A3WE 2001051800007 20010518 00007 NM 2001 5 18 DHL2001705521 1 20010416 A 5320 101331401 ANGLE BOEING 727 72722C 138400F NM RAM AIR DUCT CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 C-CHECK LT RAM AIR DUCT SUPPORT STRUCTURE HAS CORROSION BULGE BS 660 AT LT RAM AIR DOOR INBD HINGE. REMOVED AND REPLACED RAM AIR DUCT SUPPORT ANGLE AS PER B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2001051800008 20010518 00008 NM 2001 5 18 DHL2001705522 1 20010419 A 5320 FLOOR SUPPORT BOEING 727 72722C 138400F NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 C-CHECK- CORROSION & CRACKED FLOOR SUPPORT AFT BAGGAGE COMPART LBL22 STA 1012-1027. REMOVED AND REPLACED FLOOR SUPPORT RUNNER FROM STA 960 TO STA 1027 LBL22 IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2001051800009 20010518 00009 NM 2001 5 18 DHL2001705523 1 20010415 A 5320 COVER BOEING 727 72722C 138400F NM NLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 C-CHECK NLG WW LT SIDEWALL LWR CHORD COVER SHOW CRACK AROUND FAST HEAD 2 EA. REMOVED AND REPLACED SIDEWALL LWR CHORD CO VER AT NLG WW LT SIDE AS PER B727SRM 51-30-2. 2 L 7 3 4F A3WE 2001051800010 20010518 00010 NM 2001 5 18 DHL2001705524 1 20010415 A 5310 PRESSURE PANEL BOEING 727 72722C 138400F NM NLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 C-CHECK- NLG WW TOP CEILLING PANEL IS CRACKED AROUND FASTENER ROW AT BS285.5 RBL 3. REMOVED DAMAGED AREA AND INSTALLED D OUBLER REPAIR & FILLER 2 L 7 3 4F A3WE 2001051800011 20010518 00011 NM 2001 5 18 DHL2001705525 1 20010419 A 5320 BAC150545585 ANGLE BOEING 727 72722C 138400F NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 C-CHECK, FWD LAVATORY HAS CORROSION UNDER CENTER ANGLE AT FS 340 RBL 40.REMOVED DAMAGED SECTION AND INSTALLED REPAIR. 2 L 7 3 4F A3WE 2001051800012 20010518 00012 NM 2001 5 18 DHL2001705526 1 20010417 A 5230 SKIN BOEING 727 72722C 138400F NM CARGO DOOR DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 C-CHECK- LOWER FWD CARGO DOOR EXT SKIN HAS MANY DENTS. REPAIRED CARGO DOOR SKIN. 2 L 7 3 4F A3WE 2001053100256 20010531 00256 NM 2001 5 31 DHL2001705512 1 20010415 A 5310 PRESSURE PANEL BOEING 727 72722C 138400F NM NLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C-CHECK- NOSE GEAR WHEEL WELL RT SIDEWALL PANEL IS CRACKED BS 285.6 WL 158. CRACK RUNNING ALONG FAST ROWS-2 PLACES. FABRICATED EXTERNAL DOUBLER REPAIR AT NOSE WW RT SIDEWALL FROM BS 250 TO 294.5 AS PER B727 S/B 53-0065- MAT USED 2024 T3 .050 38 X 34 INCH LOT 35831 PO 83112359. ALODINED AND PRIMED AS PER B727 SRM 51-10-2. INSTALLED DOUBLER AS PER B727 S RM 51-30-2. 2 L 7 3 4F A3WE 2001051800013 20010518 00013 NM 2001 5 18 DHL2001705527 1 20010417 A 5712 RIB BOEING 727 72722C 138400F NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C CHECK C/W DHL J/C MPRGAA1A57005 INSP, REPLACE WING OUTBOARD RIB WS 546.5 RT. HFEC INDICATED RIB IS CRACKED. 2 L 7 3 4F A3WE 2001051800014 20010518 00014 NM 2001 5 18 DHL2001705528 1 20010417 A 5712 RIB BOEING 727 72722C 138400F NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 C-CHECK C/W DHL J/C MPRGAA1A57005INSP, REPLACE WING OUTBOARD RIB WS 656.5. PERFORMED HFEC INSP OF RT WING RIB STA 656.5, RIB TO STRINGER ATTACH POINTS CRACK FOUND AT UPPER STRINGER FLANGE AT STRINGERS 13,12. INSTALLED REPAIRS. 2 L 7 3 4F A3WE 2001051800015 20010518 00015 NM 2001 5 18 DHL2001705529 1 20010417 A 5712 RIB BOEING 727 72722C 138400F NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 C-CHECK- C/W DHL J/C MPRGAA1A57005 INSP. REPLACE WING OUTBOARD RIB WS 686.5. PERFORMED HFEC INSP OF RT WING RIB STA 686. 5 RIB TO STRINGER ATTACH POINTS. CRACK FOUND AT UPPER STRINGER FLANGE AT STR 12. INSTALLED REPAIR. 2 L 7 3 4F A3WE 2001051800017 20010518 00017 WP 2001 5 18 DHL2001805006 1 20010508 A 2711 TRIM TAB DOUG DC8 DC873F 302199F WP AILERON LACK OF LUBE A DHLA K NONE F FLT CONT AFFECTED DE DESCENT 1 SO 01 805DH 46125 AILERON TRIM KNOB FROZEN IN POSITION WILL NOT MOVE. FIRST NOTED IN DESCENT AT FL240. REMAINED FROZEN TO APPROX 11000. INSPECTED AND LUBED CONTROL TRIM TAB. NO DEFECTS FOUND. PERFORMED OPS CK OK IAW M/M 27-10-0. READY FOR SERVICE. 2 L 7 4 4F RT 4A25 2001051800018 20010518 00018 WP 2001 5 18 DHL2001805007 1 20010509 A 2711 JACKSCREW DOUG DC8 DC873F 302199F WP AILERON TAB LACK OF LUBE A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 805DH 46125 AT CRUISE ALT FL330 AILERON TRIM KNOB FROZEN IN POSITION. UNABLE TO TRIM AILERONS. REMAINED FROZEN UNTIL BELOW 10,000 FEET MSL. LUBED AILERON TRIM JACK SCREWS IAW DC8 M/M 12-81-1. OPS CKS GOOD. 2 L 7 4 4F RT 4A25 2001051800019 20010518 00019 NM 2001 5 18 DHL2001701009 1 20010508 A 3233 65178197 ACTUATOR BOEING 727 72730C 1384009 NM RT MLG FAILED A DHLA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 701DH 19011 RT MLG DID NOT GO DOWN. RT MLG EXTENDED WITH GOOD INDICATIONS AFTER COMPLETION OF ABNORMAL MANUAL GEAR EXTENSION. REPLAC ED RT MLG LOCK ACTUATOR PER B727 M/M 32-32-61. PERFORMED GEAR SWING AND OPS CK NORMAL PER 32-32-0 AND 32-61-00. 2 L 7 3 4F A3WE 2001051800020 20010518 00020 2001 5 18 DHL2001727017 4 20010509 A 2210 AUTOPILOT SYS BOEING 727 727228 NM COCKPIT OUT OF ADJ A DHLA K NONE O OTHER CR CRUISE 1 SO 01 727DH 20204 AUTOPILOT TRACKS 1/2 TO 1 MILE LT OR RT OF COURSE IN NAV/LOC MODE AT CRUISE ON GPS INFO. GPS PARALLEL TRACK SET TO 1 MIL E LEFT OF COURSE SELECTED TO STANDBY. OPS CHECK GOOD IAW DHL B727 S/M 34-59-0. 2 L 7 3 4F A3WE 2001051800021 20010518 00021 WP 2001 5 18 DHL2001807011 1 20010504 A 5270 WARNING SYSTEM DOUG DC8 DC873 302199C WP COCKPIT MALFUNCTIONED A DHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 807DH 45990 FLIGHT INITIATED THE TAKE-OFF ROLL ON RUNWAY 27, WHEN THEY NOTICED A MAIN CABIN DOOR OPEN LIGHT ILLUMINATE. CREW REJECT ED THE TAKE-OFF, AND EXITED THE ACTIVE RUNWAY. DOOR WAS OPENED AND RECLOSED BY FLIGHT CREW. A/C TAXIED TO RUNWAY AND DE PARTED WITHOUT FURTHER INCIDENT. 2 L 7 4 4F RT 4A25 2001051800022 20010518 00022 2001 5 18 DHL2001365011 4 20010509 A 2210 WARNING SYSTEM AIRBUS 300 A300B4203 3930306 EU COCKPIT MALFUNCTIONED A DHLA K NONE N FALSE WARNING DE DESCENT 1 SO 01 365DH 149 WITH A/P ENGAGED DURING DESCENT ERROR MESSAGE SINGLE FMS OPERATION. DISENGAGED AUTOPILOT NR 2. TEMP RESTORED NAV MODE T HEN A/P NR 1 DISENGAGED, SAME ERROR MSG. SET FMS MASTER SWITCH YP FMC1. THIS ENGAGED BOTH A/P. RE-ENGAGED A/P NR 2. O PERATED NORMAL. BOTH NR 1 & NR 2 FMS OPS CHECKED GOOD PER MM 34-58-00. CHECKED NR 1 & NR 2 A/P PER MM 22-10-00. NO DEF ECTS NOTED. 2 L 7 2 4F RT A35EU 2001051800023 20010518 00023 NM 2001 5 18 DHL2001717008 1 20010510 A 2750 FLAP BOEING 727 72723 1384004 NM WING OUT OF ADJ A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 717DH 19389 STRAIGHT AND LEVEL FLIGHT AT 300KTS AND FL270 A/C REQUIRES 1-3/4 UNITS RT OF AILERON TRIM TO MAINTAIN STRAIGHT AND LEVEL FLIGHT. RDR TRIM VALVE AT LEFT 1/2 UNIT. ADJUSTED I/B T/E FLAPS PER LATERAL TRIM ADJUSTMENT CHART FIG 501, MM 27-00-21 . 2 L 7 3 4F A3WE 2001051800024 20010518 00024 EU 2001 5 18 DHL2001366502 1 20010508 A 5755 A577620312000 PLATE AIRBUS 300 A300B4203 3930306 EU AIRBRAKE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 366DH 249 C-CHECK - DOUBLER AT LWR SKIN OF OUTER AIRBRAKE AT HINGE ARM FOUND WITH (LEVEL 2) CORROSION BEYOND LIMITS REMOVED AND R EPLACED COVER PLATE. 2 L 7 2 4F RT A35EU 2001051800025 20010518 00025 EU 2001 5 18 DHL2001366500 1 20010504 A 5313 STRINGER AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 366DH 249 C-CHECK - STRINGER 55 LT AT FRAME 64 CORRODED BEYOND LIMITS IN AFT CARGO BAY PER SRM 53-00-20. 1 INCH LENGTH OF CORROSIO N ON STRINGER DIRECTLY BELOW FRAME CLEAT ON FR 61. STRINGER REPAIR CARRIED OUT IAW SRM 53-10-10 PG BLOCK 867. 2 L 7 2 4F RT A35EU 2001051800026 20010518 00026 EU 2001 5 18 DHL2001366501 1 20010508 A 5730 A537100720700 DOUBLER AIRBUS 300 A300B4203 3930306 EU RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 366DH 249 C-CHECK - LEVEL 2 CORROSION FOUND AT RT WING KRUEGER SLOT FLAP CUT-OUT DOUBLER. RT KRUEGER FLAP REMOVED FOR ACCESS IAW 2 7-81-48, PG 401. NOTCH FLAP ASSY AND ACTUATOR REMOVED IAW MM 27-81-52 PG 401. 2 L 7 2 4F RT A35EU 2001051800027 20010518 00027 EU 2001 5 18 DHL2001366503 1 20010510 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU CABIN DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 366DH 249 C-CHECK - NR 2 RT SEAT TRACK DAMAGED AT FR 29. DAMAGED AREA REMOVED AND FOUND TO BE OUT OF SRM 53-10-00 LIMITS. REPLACE D SEAT TRACK WITH NEW. 2 L 7 2 4F RT A35EU 2001051800028 20010518 00028 WP 2001 5 18 DHL2001805008 1 20010510 A 2711 PIN DOUG DC8 DC873F 302199F WP RT AILERON DRAGGING A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 805DH 46125 AILERON TRIM FROZEN AT CRUISE ALT FL310. INSPECTED & FOUND GUIDE PIN RT AILERON TRIM DRUM DRAGGING. R&R GUIDE PIN & GRO MMETS IAW DC-8 MM 27-10-0. OPS CK OK ON GROUND. READY FOR SERVICE. 2 L 7 4 4F RT 4A25 2001051800029 20010518 00029 WP 2001 5 18 DHL2001806618 1 20010406 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - MAIN CARGO FLOOR PANELS CUSP EXTRUSION TO FRAME FITTING CRACKED 1 INCH STA 25.000 RT. REMOVED CRACKED FITTING. CLEANED, TREATED & PRIMED AREA AND INSTALLED NEW FITTING IAW SRM 51-1-20D PAGE 21, 9, SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2001051800030 20010518 00030 NM 2001 5 18 UPS01235791 1 20010420 A 5751 SUPPORT BOEING 727 72722C 138400F NM AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C, O/B AILERON LT WING, ALL HINGE SUPPORTS ON REAR SPAR OF AILERON SHOW EVIDENCE OF CORROSION. LT O/B A ILERON REMOVED IAW MM 27-10-31, NEW AILERON INSTALLED IAW MM 27-10-31. 2 L 7 3 4F A3WE 2001051800033 20010518 00033 NM 2001 5 18 UPS01235837 1 20010429 A 5310 PRESSURE PANEL BOEING 727 72725C 138400H NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:C NLG WHEEL WELL LT SIDEWALL SHOW CRACK RUNNING BETWEEN FASTENERS AT BS 277.5 TO LOWER CHORD. REMOVED N OSE WHEEL WELL ACCESS PANEL LT AFT TO GAIN ACCESS AND REMOVED FASTENERS LT SIDE AT 277.5 S PER B727 SRM 51-30-2. CUT OU T CRACK SECTION AS PER B727 SRM 51-40-2. INSTALLED DOUBLER REPAIR AS PER B727 SRM 51-4-2 FIG 1. 2 L 7 3 4F A3WE 2001051800034 20010518 00034 NM 2001 5 18 UPS01235838 1 20010429 A 5310 PRESSURE PANEL BOEING 727 72725C 138400H NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:C NLG WHEEL WELL LT SIDEWALL SHOW CRACK RUNNING BETWEEN FASTENERS AT 243.7 TO LOWER CHORD. REMOVED LT S IDE WALL AND FASTENERS AT BS 243.7 IAW SRM 51-30-2. CUT OUT CRACK SECTION PER SRM 51-40-2 FIG 1. APPROX SIZE 7 X 1 INC H, INSTALLED DOUBLER REPAIR PER B727 SRM 51-40-2. 2 L 7 3 4F A3WE 2001051800036 20010518 00036 NE 2001 5 18 UPS01835836 2 20010510 A 7200 ENGINE DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE NR 4 ENGINE FLAMED OUT A IPXA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 SO 01 705UP 45949 INSPECTION TYPE:N/A NR 4 ENGINE FLAME-OUT IN FLT. REMOVED AND REPLACED NR 4 ENG FUEL FILTER. INSPECTED INTAKE AND EXHA UST FOR FOD. NONE FOUND. MANUALLY ROTATED FAN. ROTATES FREELY. INSPECTED CHIP DETECTORS. NO DEFECTS FOUND SUMPED NR 3 AND NR 4 AND NR 4 AUX FUEL TANKS (PER MM 71-00-00). 2 L 7 4 4F 4 F RT 4A25 E2GL 2001051800037 20010518 00037 WP 2001 5 18 DHL2001806619 1 20010325 A 5320 47723971 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - AFT FUSELAGE INTERIOR RT UPPER PART FITTING CRACKED 1-1/2 INCH AT STA 1766 L-9R. REMOVED CRACKED FITTING FROM AFT FUSELAGE INTERIOR RT UPPER PART IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED & PRIMED AREA IAW SRM 51-1-88. INSTAL LED NEW FITTING (P/N 4772397-1) IAW SRM 51-1-20D PAGE 9. 2 L 7 4 4F RT 4A25 2001051800038 20010518 00038 WP 2001 5 18 DHL2001806620 1 20010403 A 5321 ANGLE DOUG DC8 DC873F 302199F WP FLOOR PANEL CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - MAIN CARGO COMPARTMENT FLOOR PANEL B SHOWS CRACKED ANGLE 1 INCH AT STA 759. REMOVED CRACKED ANGLE FROM FLOOR P ANEL B STA 759 IAW SRM 51-1-21 PAGE 1. FABRICATED NEW ANGLE IAW SRM 53-2-D FIG 1B. CLEANED, TREATED & PRIMED IAW SRM 5 1-1-8B. INSTALLED NEW ANGLE IAW SRM 51-1-21 PAGE 1. 2 L 7 4 4F RT 4A25 2001051800039 20010518 00039 NM 2001 5 18 DHL2001705531 1 20010423 A 5712 RIB BOEING 727 72722C 138400F NM WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 FOUND WING O/B RIB CRACKED USING HFEC INSP. 2 L 7 3 4F A3WE 2001051800040 20010518 00040 NM 2001 5 18 DHL2001705538 1 20010507 A 5754 SKIN BOEING 727 72722C 138400F NM L/E SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 C-CHECK- LT WING IB L/E EDGE O/B SIDE UPPER SURFACE HAS 2 INCH CRACK. REMOVED DAMAGE AREA AND INSTALLED REPAIR PER B-727 SRM 57-30-4 FIG.6 2 L 7 3 4F A3WE 2001051800043 20010518 00043 NM 2001 5 18 UPS01635841 1 20010510 A 7931 TRANSMITTER BOEING 767 767300 1385204 NM COCKPIT INTERMITTENT A IPXA K NONE N FALSE WARNING NR NOT REPORTED 1 SO 01 310UP 27762 INSPECTION TYPE:ETOP PIREP RT OIL PRESS FLUX RUNS HIGHER THAN NORMAL. UP TO 155PSI. R&R OIL PRESS XMTR OPS AND LEAKS CHE CK GOOD. 2 L 7 2 4F RT A1NM 2001051800044 20010518 00044 WP 2001 5 18 UPS01835842 1 20010503 A 5320 4758514507 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA 1240 L33R FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4758514,AND SRM. 51-1-20D 2 L 7 4 4F RT 4A25 2001051800045 20010518 00045 WP 2001 5 18 UPS01835843 1 20010502 A 5320 47516251 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA 680 L11L ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG.4751625,AND SRM. 51 -1-20D 2 L 7 4 4F RT 4A25 2001051800046 20010518 00046 WP 2001 5 18 UPS01835844 1 20010502 A 5320 47516252N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA 680 L11R ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4751625,AND SRM 51-1-2 0D 2 L 7 4 4F RT 4A25 2001051800047 20010518 00047 WP 2001 5 18 UPS01835845 1 20010502 A 5320 3779659U501 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA 902-920 L3R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659,AND SRM 51-1-2 0D, 51-1-23 2 L 7 4 4F RT 4A25 2001051800048 20010518 00048 WP 2001 5 18 UPS01835846 1 20010503 A 5320 4753360U1 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA 830 L22L FITTING IS CRACKED. REMOVED AND REPALCED FITTING IAW DWG 4753360 AND SRM 51-1-20D, 51- 1-21 2 L 7 4 4F RT 4A25 2001051800049 20010518 00049 WP 2001 5 18 UPS01835847 1 20010501 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 LT WING L/E. UPPER RIB IS CRACKED AT XFS 660. REPAIRED RIB. 2 L 7 4 4F RT 4A25 2001051800050 20010518 00050 WP 2001 5 18 UPS01835848 1 20010501 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 LT WING L/E. UPPER RIB IS CRACKED AT XFS 828.75. REPAIRED RIB 2 L 7 4 4F RT 4A25 2001051800051 20010518 00051 WP 2001 5 18 UPS01835849 1 20010501 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 LT WING L/E. UPPER RIB IS CRACKED AT XFS 722.5. REPAIRED RIB 2 L 7 4 4F RT 4A25 2001051800052 20010518 00052 WP 2001 5 18 UPS01835850 1 20010501 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 LT WING L/E. UPPER RIB IS CRACKED AT XFS 728.75. REPAIRED RIB. 2 L 7 4 4F RT 4A25 2001051800053 20010518 00053 WP 2001 5 18 UPS01835851 1 20010501 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 LT WING L/E. UPPER RIB IS CRACKED AT XFS 741.25. REPAIRED RIB. 2 L 7 4 4F RT 4A25 2001051800054 20010518 00054 WP 2001 5 18 UPS01835852 1 20010501 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 LT WING L/E. UPPER RIB IS CRACKED AT XFS 816.25. REPAIRED RIB. 2 L 7 4 4F RT 4A25 2001051800055 20010518 00055 WP 2001 5 18 UPS01835853 1 20010502 A 5720 97532978 ANGLE DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 RT WING L/E. VERTICAL ATTACH ANGLE IS CRACKED AT XS 520. REMOVED, FABRICATED, AND REPLACED ANGLE. 2 L 7 4 4F RT 4A25 2001051800056 20010518 00056 WP 2001 5 18 UPS01835854 1 20010502 A 5712 576947027 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 RT WING L/E. UPPER AND LOWER RIBS ARE CRACKED AT XFS 885. REMOVED, FABRICATED, AND REPLACED RIBS. 2 L 7 4 4F RT 4A25 2001051800057 20010518 00057 WP 2001 5 18 UPS01835855 1 20010502 A 5320 4751625U1 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA 680 L11R ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4751625 AND SRM 51-1-2 0D 2 L 7 4 4F RT 4A25 2001051800058 20010518 00058 WP 2001 5 18 UPS01835856 1 20010502 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 RT WING L/E. UPPER RIB IS CRACKED AT XILD .7095. REPAIRED RIB 2 L 7 4 4F RT 4A25 2001051800059 20010518 00059 WP 2001 5 18 UPS01835857 1 20010502 A 5730 576960036 DOUBLER DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 RT WING OB L/E. LOWER INTERNAL DOUBLER IS CRACKED AT XFS 597.5. REMOVED, FABRICATED, AND REPLACED D OUBLER 2 L 7 4 4F RT 4A25 2001051800060 20010518 00060 WP 2001 5 18 UPS01835858 1 20010501 A 5310 SHEAR TIE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA 702 RBL 6 FRAME SHEAR TIE IS CRACKED. REPAIRED SHEARTIE IAW SRM 53-2-0 FIG 1B AND DWG 5753158 2 L 7 4 4F RT 4A25 2001051800061 20010518 00061 WP 2001 5 18 UPS01835859 1 20010509 A 5720 97532977 ANGLE DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 LT WING L/E. VERTICAL ATTACH ANGLE IS CRACKED AT XS 520. REMOVED,FABRICATED, AND REPLACED ANGLE 2 L 7 4 4F RT 4A25 2001051800062 20010518 00062 WP 2001 5 18 UPS01835860 1 20010502 A 5320 3779659501N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA 857 L5R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659 AND SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001051800063 20010518 00063 WP 2001 5 18 UPS01835861 1 20010502 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 RT WING L/E. UPPER RIBS ARE CRACKED AT XFS 603.75, XFS 616.25, XFS 622.5. REPAIRED RIBS. 2 L 7 4 4F RT 4A25 2001051800064 20010518 00064 WP 2001 5 18 UPS01835862 1 20010501 A 5320 47504181N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA 1240 L20R INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750418 A ND SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001051800065 20010518 00065 WP 2001 5 18 UPS01835863 1 20010502 A 5320 47504232 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA 857 L18L INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4 750423 AND SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001051800066 20010518 00066 WP 2001 5 18 UPS01835864 1 20010501 A 5730 576960040 DOUBLER DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 RT WING L/E. INTERNAL DOUBLER IS CRACKED AT XFS 572.5. REMOVED, FABRICATED, AND REPLACED DOUBLER. 2 L 7 4 4F RT 4A25 2001051800067 20010518 00067 WP 2001 5 18 UPS01835865 1 20010502 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 RT WING L/E. UPPER RIBS ARE CRACKED AT XFS 678.75, XFS 666.25, XFS 603.75. REPAIRED RIBS. 2 L 7 4 4F RT 4A25 2001051800068 20010518 00068 WP 2001 5 18 UPS01835866 1 20010501 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 LT WING L/E. UPPER RIB IS CRACKED AT XOLD 067. REPAIRED RIB 2 L 7 4 4F RT 4A25 2001051800069 20010518 00069 WP 2001 5 18 UPS01835867 1 20010501 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 LT WING L/E. UPPER RIB IS CRACKED AT XFS 810. REPAIRED RIB. 2 L 7 4 4F RT 4A25 2001051800070 20010518 00070 WP 2001 5 18 UPS01835868 1 20010501 A 5720 58027331 SPLICE DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 LT WING L/E. LOWER INNER SPLICE IS CRACKED AT XS 520.168. REMOVED, FABRICATED, AND REPLACED DOUBLER AND PLATE. 2 L 7 4 4F RT 4A25 2001051800071 20010518 00071 WP 2001 5 18 UPS01835870 1 20010430 A 5320 3610130501N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA 70 L21R CUSP JOINT ATTACH FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW D WG 3610130 AND SRM 51-1-20D, 51-1-21 2 L 7 4 4F RT 4A25 2001051800072 20010518 00072 WP 2001 5 18 UPS01835871 1 20010502 A 5330 5645332107 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA 857-879 LBL 63 FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED,FABRICATED,AND REPLACED DOUBLE R. 2 L 7 4 4F RT 4A25 2001051800073 20010518 00073 NM 2001 5 18 UPS01M35839 1 20010415 A 5347 S4929147075T6511 SEAT TRACK DOUG MD11 MD11F 3023600 NM CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 250UP INSPECTION TYPE:C MAIN DECK SEAT TRACK X=-27.50 STA 840 TO 890 FOUND CORROSION. CORROSION CLEANED, FOUND OUT OF LIMIT AT STA 832 TO 909 RBL 27. NEW SEAT TRACK AND 2EA SPLICE INSTALLED. 2 L 7 3 4F RT A22WE 2001051800074 20010518 00074 NM 2001 5 18 UPS01M35840 1 20010411 A 5347 S49291477075T651 SEAT TRACK DOUG MD11 MD11F 3023600 NM CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 250UP INSPECTION TYPE:C MAIN DECK SEAT TRACK RBL 9 CORRODED AT BS 840 TO 899. CORROSION CLEANED. FOUND OUT OF LIMIT AT STA 832 AND STA 909. NEW SEAT TRACK AND 2EA SPLICE INSTALLED. 2 L 7 3 4F RT A22WE 2001051800075 20010518 00075 NM 2001 5 18 DHL2001705543 1 20010415 A 5310 PRESSURE PANEL BOEING 727 72722C 138400F NM NLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 C-CHECK- NLG WW RT SIDEWALL PANEL CRACKED BS 263.5 FASTNENER ROW UPPER OF AFT ACCESS DOOR. CUT OUT DAMAGED SECTION AND INSTALLED REPAIR. 2 L 7 3 4F A3WE 2001051800076 20010518 00076 2001 5 18 DHL2001801005 4 20010515 A 3421 258733511 GYRO DOUG DC8 DC873F 302199F WP COCKPIT ERRATIC A DHLA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 801DH 46033 CAPT ADI ERRATIC INTERMITTENT +/- 5 DEG PITCH WITH GYRO FLAG AND BOW TIE ANNUNCIATOR ILLUMINATED. REMOVED AND REPLACED N R 1 VERTICAL GYRO. OPS CHECKS GOOD IAW DC-8 MM 34-25-1. 2 L 7 4 4F RT 4A25 2001051800077 20010518 00077 NM 2001 5 18 DHL2001702011 1 20010512 A 3150 WARNING SYSTEM BOEING 727 72730C 1384009 NM COCKPIT MALFUNCTIONED A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 702DH 19793 REJECTED T/O IN ROC DUE TO T/O WARNING HORN. WE DEPART RUNWAY. RESET CONTROLS. ON NEXT ATTEMPT, NO FURTHER PROBLEMS. T ESTED TAKEOFF WARNING SYSTEM PER MM 31-26-1. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2001051800078 20010518 00078 2001 5 18 DHL2001365013 4 20010512 A 2211 B77CMO COMPUTER AIRBUS 300 A300B4203 3930306 EU AUTOPILOT SYS MALFUNCTIONED A DHLA K NONE O OTHER CR CRUISE 1 SO 01 365DH 149 AUTO THROTTLE SYSTEM TRIPPED OFF WHEN ENTERING CLOUDS. RESET AND TRIPPED OFF 2 MORE TIMES WHILE IN CLOUDS. OPERATES NO RMALLY IN THE CLEAR. REPLACED SRS COMP. OPS CKS GOOD IAW MM 34-24-11. (WHEN CREW WAS DEBRIEFED THEY INDICATED THAT THE SPD MODE WAS FAULTY NOT THE N1 MODE). 2 L 7 2 4F RT A35EU 2001051800079 20010518 00079 GL 2001 5 18 S01J72014 2 20010421 A 7230 COMPRESSOR BOEING 747 747* NM GE CF6 CF680C2* GL NR 2 ENGINE DAMAGED W SAJF E ENGINE SHUTDOWN E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CR CRUISE 1 WP 03 CTEXT 2993 30761 706184 REGISTRATION NUMBER - B18703NR 2 ENGINE, NR 2 VIB IND 4.1 UNITS, ENGINE LOST POWER. IAW SOP SHUTDOWN ENGINE AND ENGINE E XPERIENCED 3 HOURS WINDMILL. BORESCOPE INSP FOUND NR 2 ENGINE ALL HPC 3RD STAGE BLADES DAMAGED SERIOUSLY. REPLACED NR 2 ENGINE AND RUN UP TEST NML. INITIAL INVESTIGATION: HPC BORESCOPE INSPECTION FOUND, STG 1 BLADE: 2 EA BALDES TIP CURL, STG 2 BLADE: SOME BLADES NICKS ON L/E. STG 3 THRU STG 5 BLADE: ALL BLADES FOUND SERIOUS DAMAGED (TEAR, LIBERATION, SE PARATION) ON AIRFOIL. NR 2 ENGINE WAS REMOVED AND REPLACED, ENGINE RUN UP NORMAL. 2 L 7 4 4F 4 F RT A20WE E23EA 2001051800080 20010518 00080 NE 2001 5 18 S01271013 2 20010403 A 7321 7788004 FUEL CONTROL BOEING 747 747* NM PWA JT9 JT9D7R4G2 52054 NE NR 2 ENGINE MALFUNCTIONED W SAJF O OTHER X ENGINE FLAMEOUT CL CLIMB 1 WP 03 CTEXT 24308 725343 REGISTRATION NUMBER - B18771NR 2 ENGINE FLAME OUT AT FL330, TAT -4 DEGREES C, EGT 352 DEGREES C, EPR 1.02 AND DROPPING, ENGINE SHUTDOWN, WINDMILLED APPROX 1 MIN AT OIL PRESS 22 PSI, ENG WAS RESTARTED AND OPERATED NORMALLY. IAW AMM 71-00-43, MAIN FUEL FILTER AND EVBC FUEL FILTER INSPECTED NML AND REPLACED. CHECKED EVBC PT3 AND PS3 WATER TRAP, NO WATER EVIDENC E FOUND. PFMED FUEL TANKS WATER DRAINING. REPLACED FCU AND FUEL PUMP. REPLACED FUEL HEATER DUE TO MUNT BOLTS INSERT DAMA GED. PFMED WINDMILLING INSP MAIN OIL FILTER AND ALL MAGNETIC CHIP DETECTORS INSPED NML. ENG RUN UP TEST WITH TAKEOFF PO WER SATISFACTORY. 2 L 7 4 4F 4 F RT A20WE E3NE 2001051800081 20010518 00081 NE 2001 5 18 S01271013A 2 20010403 A 7314 706801 PUMP BOEING 747 747* NM PWA JT9 JT9D7R4G2 52054 NE NR 2 ENGINE MALFUNCTIONED W SAJF O OTHER X ENGINE FLAMEOUT CL CLIMB 1 WP 03 CTEXT 24308 725343 REGISTRATION NUMBER - B18771 NR 2 ENGINE FLAME OUT AT FL330, TAT -4 DEGREES C, EGT 352 DEGREES C, EPR W.02 DROPPING, ENG INE SHUTDOWN, WINDMILLED APPROX 1 MIN AT OIL PRESS 22 PSI, ENG WAS RESTARTED AND OPERATED NORMALLY. IAW AMM 71-00-43, MA IN FUEL FILTER AND EVBC FUEL FILTER INSPECTED NML AND REPLACED. CHECK EVBC PT3 AND PS3 WATER TRAP, NO WATER EVIDENCE FOU ND. PFMED FUEL TANKS WATER DRAINING. REPLACED FUEL CONTROL UNIT AND FUEL PUMP ASSY. REPLACED FUEL HEATER DUE TO MOUNT BO LTS INSERT DAMAGEE. PFMED WINDMILLING INSP MAIN OIL FILTER AND ALL MAGNETIC CHIP DETECTORS INSPED NML. ENG RUN UP TEST W ITH TAKEOFF POWER SATISFACTORY. 2 L 7 4 4F 4 F RT A20WE E3NE 2001051800082 20010518 00082 NM 2001 5 18 S01271013B 1 20010403 A 7312 737062 FUEL HEATER BOEING 747 747* NM PWA JT9 JT9D7R4G2 52054 NE NR 2 ENGINE MALFUNCTIONED W SAJF O OTHER X ENGINE FLAMEOUT CL CLIMB 1 WP 03 CTEXT 24308 REGISTRATION NUMBER - B18771NR 2 ENGINE FLAME OUT AT FL330, TAT -4 DEGREES C, EGT 352 DEGREES C, EPR 1.02 AND DROPPING, ENGINE SHUTDOWN, WINDMILLED APROX 1 MIN AT OIL PRESS 22 PSI, ENG WAS RESTARTED AND OPERATED NORMALLY. IAW AMM 71-00-43, MAIN FUEL FILTER AND EVBC FUEL FILTER INSPECTED NML AND REPLACED. CHECKED EVBC PT3 AND PS3 WATER TRAP, NO WATER EVIDENCE FOUND. PFMED FUEL TANKS WATER DRAINING. REPLACED FULE CONTROL UNIT AND FUEL PUMP ASSY. REPLACED FUEL HEATER DUE MOUNT BOLTS INSERT DAMAGED. PFMED WINDMILLING INSP MAIN OIL FILTER AND ALL MAGNETIC CHIP DETECTORS INSPED NML. ENG RUN UP TES T WITH TAKEOFF POWER, SATISFACTORY. 2 L 7 4 4F 4 F RT A20WE E3NE 2001051800083 20010518 00083 NM 2001 5 18 DHL2001705540 1 20010505 A 2761 659892440 BRACKET BOEING BOEING 727 72722C 138400F NM NR 12 SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 C-CHECK, NR 12 SPOILER ACTUATOR MOUNT BRACKET IS CRACKED, OUTBOARD LWR LUG.REMOVED AND REPLACED NR 12 SPOILER ACTUATOR B RACKET. 2 L 7 3 4F A3WE 2001051800084 20010518 00084 NM 2001 5 18 DHL2001705537 1 20010417 A 5712 RIB BOEING 727 72722C 138400F NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 C-CHECK C/W DHL J/C MPRGAA1AS7005 INSP, REPLACE WING OUTBOARD RIB WS 738.5 RTPERFORMED HFEC INSP. OF RT. WING RIB STA 73 8.5 RIB, CRACK FOUND AT LOWER RIB STR 8. INSTALLED RIB REPAIR. 2 L 7 3 4F A3WE 2001051800085 20010518 00085 NM 2001 5 18 DHL2001709006 1 20010516 A 3260 327 LIGHT BOEING 727 72782C 1384026 NM COCKPIT INOPERATIVE A DHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 709DH 19968 LT LANDING GEAR INTRANSIT UNSAFE LIGHT DOES NOT ILLUMINATE DURING GEAR RETRACTION OR EXTENSION. ALL RED LIGHTS GROUND T EST NORMAL. FOUND LT MAIN GEAR RED LIGHT INOPERATIVE. (NO TEST) RELAMPED LIGHT. PERFORMED GEAR INDICATION WARNING TEST IAW B727 M/M 32-61-0. 2 L 7 3 4F A3WE 2001051800086 20010518 00086 NM 2001 5 18 UPS01235877 1 20010507 A 5320 BRACKET BOEING 727 72730C 1384009 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:C, WING TO BODY FAIRING ATTACH BRACKET BS 945 S18A LT CRACKED. NEW BRACKET FABRICATED 2 L 7 3 4F A3WE 2001051800087 20010518 00087 NM 2001 5 18 UPS01235893 1 20010515 A 5210 DOOR SEAL BOEING 727 72725C 138400H NM PAX DOOR TORN A IPXA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 SO 01 931UP 19858 INSPECTION TYPE:N/A PILOT REPORT-AT 5000 FT LOST CABIN PRESSURIZATION REPAIRED MAIN ENTRY DOOR SEAL 2 L 7 3 4F A3WE 2001051800088 20010518 00088 WP 2001 5 18 UPS01835872 1 20010503 A 5320 5751516229 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA 1340-1360 L31L INTERCOSTAL IS CORRODED BEYOND LIMITS. REMOVED,FABRICATED,AND REPLACED INTERCOST AL IAW DWG 5751516 AND SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001051800089 20010518 00089 WP 2001 5 18 UPS01835873 1 20010502 A 5330 5645332109 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA 879-902 RBL 65 FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED,FABRICATED,AND REPLACED DOUBLE R. 2 L 7 4 4F RT 4A25 2001051800090 20010518 00090 WP 2001 5 18 UPS01835876 1 20010505 A 5751 SKIN DOUG DC8 DC873F 302199F WP AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 LT I/B AILERON FWD UPPER SKIN CUTOUT AT XA 458 IS CORRODED BEYOND LIMITS. REPAIRED SKIN 2 L 7 4 4F RT 4A25 2001051800091 20010518 00091 WP 2001 5 18 UPS01835878 1 20010503 A 5320 9753254 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA 1677 INTERCOSTAL IS CRACKED AT LT CUSP. REMOVED,FABRICATED,AND REPLACED INTERCOSTAL IAW DWG 975 3254 AND SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001051800092 20010518 00092 WP 2001 5 18 UPS01835879 1 20010503 A 5320 37584981N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA 1240 L35L INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758498 AND SRM 51-1-21 2 L 7 4 4F RT 4A25 2001051800093 20010518 00093 WP 2001 5 18 UPS01835880 1 20010430 A 5320 5750540501N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA 660-680 L11R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 5750540 AND SRM 51-1- 20D, 51-1-23 2 L 7 4 4F RT 4A25 2001051800094 20010518 00094 WP 2001 5 18 UPS01835881 1 20010503 A 5320 3755847502N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA 1230 BANANA FITTING IS CRACKED AT L33R. REMOVED AND REPLACED FITTING IAW DWG 3755847 AND SRM 51 -1-20D 2 L 7 4 4F RT 4A25 2001051800095 20010518 00095 WP 2001 5 18 UPS01835882 1 20010502 A 5320 47505211 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA 834-857 L1 SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750521 AND SRM 51-1 -20D 2 L 7 4 4F RT 4A25 2001051800096 20010518 00096 WP 2001 5 18 UPS01835883 1 20010501 A 5320 47504192N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA 1240 L18R INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750419 A ND SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001051800097 20010518 00097 WP 2001 5 18 UPS01835884 1 20010502 A 5320 37045101 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA 280-300 L11R INTERCOSTAL IS CRACKED. REMOVED, FABRICATED, AND REPLACED INTERCOSTAL IAW DWG 3704 510 AND SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001051800098 20010518 00098 WP 2001 5 18 UPS01835885 1 20010502 A 5320 575072670 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA 80-100 L33R INTERCOSTAL IS CRACKED. REMOVED, FABRICATED, AND REPLACED INTERCOSTAL IAW DWG 57507 26 AND SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001051800099 20010518 00099 WP 2001 5 18 UPS01835886 1 20010506 A 5320 4750426501N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA 683 AT L36R SIDE FRAME ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING. 2 L 7 4 4F RT 4A25 2001051800100 20010518 00100 WP 2001 5 18 UPS01835887 1 20010504 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA 60 FRAME CRACKED UNDER DOUBLER AT RBL 24 REPAIRED FRAME. 2 L 7 4 4F RT 4A25 2001051800101 20010518 00101 WP 2001 5 18 UPS01835888 1 20010504 A 5320 WEB DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA 80 SUBFLOOR IS CRACKED AT LBL 10. REPAIRED SUBFLOOR. 2 L 7 4 4F RT 4A25 2001051800102 20010518 00102 WP 2001 5 18 UPS01835889 1 20010501 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 LT WING CENTER L/E. UPPER SKIN IS CORRODED BEYOND LIMITS AT XFS 391.5. REPAIRED SKIN. 2 L 7 4 4F RT 4A25 2001051800103 20010518 00103 WP 2001 5 18 UPS01835890 1 20010501 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 LT WING CENTER L/E. UPPER SKIN IS CORRODED BEYOND LIMITS AT XFS 304 AND XFS 335.25. REPAIRED SKIN 2 L 7 4 4F RT 4A25 2001051800104 20010518 00104 WP 2001 5 18 UPS01835891 1 20010501 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 LT WING L/E. UPPER RIB IS CRACKED AT XFS 791.25. REPAIRED RIB 2 L 7 4 4F RT 4A25 2001071300009 20010713 00009 WP 2001 7 13 UPS01835894 1 20010516 A 5312 PRESSURE PANEL DOUG DC8 DC873F 302199F WP LT MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:N/A LEFT MLG W/W WEB PANEL CRACKED. *S/D* REPAIRED PER SRM 51-1-5. 2 L 7 4 4F RT 4A25 2001052100003 20010521 00003 NM 2001 5 21 01FDEA00321 1 20010424 A 3230 656021123 ACCESSORY UNIT BOEING 727 7272S2F 1384O81 NM E/E BAY MALFUNCTIONED A FDEA O OTHER O OTHER CL CLIMB 1 SO 25 216FE 22937 AFT T/O NORM CLIMBOUT WENT TO RAISE GEAR HANDLE. GEAR WOULD NOT GO BEYOND OFF POS. PERFORMED OPS TEST ON SOLENOID. CK GOOD. REMOVED AND REPLACED LG ELECTRONIC MODULE PER 32-09-122. OK FOR SERVICE. 2 L 7 3 4F A3WE 2001052100004 20010521 00004 NM 2001 5 21 01FDEA00320 1 20010428 A 3230 656021123 ACCESSORY UNIT BOEING 727 727233 138408A NM E/E BAY FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 222FE 20933 ATTEMPT TO RAISE GEAR LEVER, WOULD NOT GO BEYOND OFF POS. COMPLIED WITH CKLIST WITH NEGATIVE RESULTS. REPLACED LG ELEC TRONIC MODULE PER MM 32-09-21-4. PERFORMED CONTROL HANDLE LOCK SYS TEST PER MM 32-31-011-5. SYS CK OK. 2 L 7 3 4F RT A3WE 2001052100005 20010521 00005 NM 2001 5 21 01FDEA00319 1 20010427 A 3020 VALVE DOUG MD11 MD11F 3023600 NM ANTI-ICE SYS INOPERATIVE A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 615FE 48767 ON CLIMBOUT WITH NR 2 NOSE COWL A/I VLV INOP, AND WIRED OPEN PER MEL 30-6D GOT NR 2 ENG A/I OFF ALERT CONSULTED RED TABS . REMOVED AND REPLACED ALL 3 SENSING ELEMENT D1-89, D1-90 & D1-91 PER MM 30-22-11-4. REMOVED AND REPLACED ENG A/I VALV E PER MM 30-22-00. 2 L 7 3 4F RT A22WE 2001052100006 20010521 00006 NE 2001 5 21 01FDEA00324 2 20010503 A 7230 COMPRESSOR AIRBUS 310 A310222 3930315 EU PWA JT9 JT9D7R4E1 52054 NE NR 1 ENGINE STALLED A FDEA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 25 420FE 339 NR 1 ENG BEGAN COMPRESSOR STALLING. ACCOMPANIED BY LARGE FLUCTUATION IN ALL NR 1 ENG INSTRUMENTS. 2 L 7 2 4F 4 F RT A35EU E3NE 2001052100007 20010521 00007 NM 2001 5 21 01FDEA00325 1 20010502 A 5320 SPLICE BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 270FE 22035 DURING ROUTINE INSP, BS 950 BULKHEAD FOUND CORRODED ON LWR CHORD AT RBL 20. *S/D* REMOVED, REPLACED AND FAB SPLICE ANG LE PER IAW BAC 727 SRM 51-40. 2 L 7 3 4F RT A3WE 2001052100008 20010521 00008 NE 2001 5 21 01FDEA00323 2 20010502 A 7314 7436025 PUMP BOEING 727 72722 1384002 NM PWA JT8 JT8D7B 52053 NE NR 1 ENGINE FAILED A FDEA A UNSCHED LANDING X ENGINE FLAMEOUT TO TAKEOFF 1 SO 25 189FE 19082 654114 ON T/O NR 1 ENG SHUTDOWN. ENG MET ALL RESTART PREM. REMOVED AND REPLACED NR 1 ENG FUEL CONTROL UNIT AND FUEL PUMP PER JRH, LEAK CK GOOD. OK FOR SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2001052100009 20010521 00009 NM 2001 5 21 01FDEA00326 1 20010505 A 2613 65249203 DETECTOR BOEING 727 727227 1384078 NM FIRE PROTECTION FAILED A FDEA K NONE N FALSE WARNING CR CRUISE 1 SO 25 482FE 21464 LWR AFT BODY OVERHEAT ILLUM. REMOVED AND REPLACED OVERHEAT DETECTOR PER MM 20-10-017-2. RAN ENG 1, 2 & 3 PER IAW 727 J RH. LWR AFT BODY OVERHEAT LIGHT DID NOT ILLUM. 2 L 7 3 4F A3WE 2001052100010 20010521 00010 WP 2001 5 21 01FDEA00327 1 20010505 A 7931 WARNING LIGHT DOUG DC10 DC1010F 3022111 WP COCKPIT ILLUMINATED A FDEA E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 SO 25 054FE 47808 SHUTDOWN NR 1 ENG AT 1209Z BECAUSE OF LOW OIL PRESS WARN LIGHT. RESET C/B NO CHANGE. 2 L 7 3 4F A22WE 2001052100011 20010521 00011 WP 2001 5 21 01FDEA00328 1 20010507 A 5270 RELAY DOUG DC10 DC1010F 3022111 WP A/C DOOR FAULTY A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 052FE 47806 AIR CONDITIONING DOOR CAUTION LIGHT INOP. REMOVED AND REPLACED RELAY R2-5431 AS PRECAUTIONARY PER CHPT 20, SYS OPS CK N ORMAL. PLACARD REMOVED. 2 L 7 3 4F A22WE 2001052100012 20010521 00012 WP 2001 5 21 01FDEA00329 1 20010507 A 3260 CONNECTOR DOUG DC10 DC1010F 3022111 WP MICROSWITCH CONTAMINATED A FDEA K NONE N FALSE WARNING CL CLIMB 1 SO 25 054FE 47808 UPON GEAR RETRACT LMG RED LIGHT ON S/O PNL REMAIN RED. FOUND WATER IN CANNON PLUG IN MICROSWITCH. CLEAN AND INSP WIRE NO DAMAGE FOUND. PERFORMED PROXIMITY ELECTRONIC UNIT NO FAULT FOUND. CND CK TARGETS PER MA 00-823, NO FAULT FOUND. 2 L 7 3 4F A22WE 2001060100159 20010601 00159 NM 2001 6 1 01FDEA00330 1 20010507 A 5320 INTERCOSTAL BOEING 727 72722 1384002 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 DURING ROUTINE INSP INTERCOSTAL EXTENTION FROM BS 440-460, STR 2L FOUND CRACKED AT 3RD FASTENER FROM AFT END UPPER ROW 1 2 O''CLOCK. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-30-2. 2 L 7 3 4F A3WE 2001060100158 20010601 00158 NM 2001 6 1 01FDEA00332 1 20010507 A 5754 RIB BOEING 727 72722 1384002 NM SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 DURING ROUTINE INSP NR 2 SLAT RIB AT SLAT BS 342 FOUND CRACKED. *S/D* REMOVED AND REPLACED NR 2 L/E SLAT PER IAW BAC 7 27 MM 27-81-011. 2 L 7 3 4F A3WE 2001070200027 20010702 00027 NM 2001 7 2 01FDEA00334 1 20010507 A 5330 SKIN BOEING 727 72722 1384002 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 DURING ROUTINE INSP FUSELAGE SKIN Found CRACKED AT BS 250.5 BELOW LT NR 3 COCKPIT. *S/D* Removed and replaced DAMAGE P ER IAW FEDEX EA 7-5330-57544. 2 L 7 3 4F A3WE 2001052100013 20010521 00013 NM 2001 5 21 01FDEA00336 1 20010507 A 5347 SEAT TRACK BOEING 727 72722 1384002 NM CABIN CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 DURING ROUTINE INSP NR 2 MAIN CABIN SEAT TRACK FOUND CRACKED AT BS 870. 2 L 7 3 4F A3WE 2001052100027 20010521 00027 NM 2001 5 21 2001UALA00597 1 20010426 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 DENT IN LT FUSELAGE TWO FEET FWD OF WING ILLUMINATION LIGHT. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2001061800009 20010618 00009 NM 2001 6 18 2001UALA00598 1 20010428 A 2150 8102093L4 ACM BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE AC BAY SEIZED A UALA J A DUMP FUEL UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 790UA 26943 SFO-FRA, APPROXIMATELY 1.5 HOURS AFTER DEPARTURE, EXPERIENCED AIR FLOW PROBLEMS WITH RIGHT PACK. DUMPED FUEL AND RETURN ED TO SFO. *S/D* RT PACK ACM WAS FOUND SEIZED AND WAS REPLACED. AIRCRAFT RETURNED TO REVENUE SERVICE WITH NO FURTHER INCIDENT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001052100028 20010521 00028 NM 2001 5 21 2001UALA00599 1 20010428 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 AFT CABIN FLOORBEAM STATION 947 UPPER SURFACE CORRODED FROM RBL 10 TO LBL 15. REMOVED DAMAGED AREA. SPLICED IN T-CHORD NESTED ANGLE REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100029 20010521 00029 NM 2001 5 21 2001UALA00600 1 20010429 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 314UA 23675 STA 178, LBL 5.7 VERTICAL CHORD CRACKED IN RADIUS AT WL 184. REPAIRED DAMAGED AREA. INSTALLED DOUBLER. MAJOR REPAIR AC COMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100030 20010521 00030 NM 2001 5 21 2001UALA00602 1 20010430 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 STA 178 BULKHEAD WEB, 2 CRACKS ON INBOARD SIDE OF LOWER RIGHT ANTENNA MOUNT. REMOVED DAMAGE. INSTALLED DOUBLER. MAJOR R EPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100031 20010521 00031 NM 2001 5 21 2001UALA00603 1 20010426 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 DENT IN FUSELAGE SKIN. STA 615.REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2001052100033 20010521 00033 NM 2001 5 21 2001UALA00605 1 20010429 A 5320 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 CABIN FLOOR INTERCOSTAL AT STA 365, RBL 42.45 CORRODED. REPLACED INTERCOSTAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2001052100034 20010521 00034 NM 2001 5 21 2001UALA00606 1 20010426 A 2131 CONTROLLER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN PRESSURE MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 7261U 21408 AIRCRAFT RETURNED TO DEN DUE TO PRESSURIZATION PROBLEM. CABIN PRESSURE CONTROLLER FAILED. REPLACED CONTROLLER. 2 L 7 3 4F 4 F A3WE E2EA 2001052100035 20010521 00035 NM 2001 5 21 2001UALA00607 1 20010430 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 314UA 23675 STA 500 FRAME HAS GOUGE AT STR 19L TO 20L. ACCOMPLISHED REINFORCEMENT TO FRAME STA 500 STR 19L TO 20L. MAJOR REPAIR ACC OMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100036 20010521 00036 NM 2001 5 21 2001UALA00609 1 20010430 A 5310 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 314UA 23675 FRAME TO STRINGER TIE IS CRACKED, LOCATED AT STA 500D AND STR 19R. INSTALLED DOUBLER AND ATTACHING PARTS. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100037 20010521 00037 NM 2001 5 21 2001UALA00610 1 20010430 A 5312 DOUBLER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BULKHEAD CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 314UA 23675 AFT PRESSURE BULKHEAD REPAIR AREA AT 2:00 POSITION SKIN HAS GOUGES OR CRACKS. REMOVED OLD DOUBLER. INSTALLED NEW DOUBL ER AND HAT CHANNEL. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100038 20010521 00038 NM 2001 5 21 2001UALA00611 1 20010501 A 5310 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 LT FWD NOSE COMPARTMENT AT STR 17L, WL 206 APPROX STA 195, INTERCOSTAL SHEAR TIE IS CRACKED. REPLACED SHEAR TIE. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100039 20010521 00039 NM 2001 5 21 2001UALA00612 1 20010501 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 LT EXTERNAL FUSELAGE. SKIN GOUGED AT STA 927 ABOVE STR 19L. REMOVED DAMAGE. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100040 20010521 00040 NM 2001 5 21 2001UALA00613 1 20010501 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 BS 178 BULKHEAD SKIN INBOARD UPPER CORNER CRACKED. ACCOMPLISHED DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100041 20010521 00041 NM 2001 5 21 2001UALA00614 1 20010501 A 5312 BULKHEAD BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 974UA 21597 BS 178 BULKHEAD 2 EA CRACKS ON INBD SIDE OF LWR WX RADAR ANTENNA MOUNT. ACCOMPLISHED DOUBLER REPAIRS. 2 L 7 2 4F 4 F A16WE E2EA 2001052100042 20010521 00042 NM 2001 5 21 2001UALA00615 1 20010501 A 5342 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HORIZ STAB DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 RT HORIZONTAL STAB DENTED 6 FT FROM INBD AND 6 INCHES FWD REAR SPAR. ACCOMPLISHED FLUSH REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100044 20010521 00044 NM 2001 5 21 2001UALA00618 1 20010429 A 5310 SHEAR TIE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7299U 21894 FORWARD PIT STATION 580 BETWEEN STR 28L AND 28R FRAME SHEAR TIE CORRODED BEYOND LIMIIT. REPLACED SHEAR TIE. 2 L 7 3 4F 4 F A3WE E2EA 2001052100045 20010521 00045 NM 2001 5 21 2001UALA00619 1 20010428 A 3411 B-NUT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE AIRSPEED IND LOOSE A UALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 29 7283U 21561 DURING TAKEOFF ROLL THERE WAS NO FIRST OFFICER''S AIRSPEED INDICATION. RETURNED TO BLOCKS FOUND LOOSE B-NUT ON PITOT AND STATIC LINE ON F/O AIRSPEED INDICATOR. TIGHTENED B-NUT AND PERFORMED A LOW LEVEL LEAK CHECK. 2 L 7 3 4F 4 F A3WE E2EA 2001052100047 20010521 00047 NM 2001 5 21 2001UALA00622 1 20010430 A 5754 RIB BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE SLAT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7299U 21894 NR 6 SLAT INBOARD END DAMAGED REMOVED AND REPLACED RIB PER SRM 51-30-3 2 L 7 3 4F 4 F A3WE E2EA 2001061800010 20010618 00010 NM 2001 6 18 2001UALA00623 1 20010502 A 2133 90231570381 OUTFLOW VALVE AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE CABIN PRESSURE FAILED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 807UA MR2130168 798 AIRCRAFT DIVERTED TO CLE DUE TO LOSS OF CABIN PRESSURE. *S/D* CFDS FAULTED OUTFLOW VALVE, REPLACED SAME AND BOTH CABIN PRESSURE CONTROLLERS PRECAUTIONARY, NO FURTHER DEFECTS REPORTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2001052100048 20010521 00048 NM 2001 5 21 2001UALA00625 1 20010502 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 BS 188 FRAME AFT SIDE AT RBL 27, WL207, CHORD ANGLE IS CRACKED IN RADIUS. ACCOMPLISHED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100049 20010521 00049 NM 2001 5 21 2001UALA00626 1 20010502 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 STA 178 BULKHEAD LBL 5.7, WL 214, UPPER LT ANT MOUNT O/B SIDE IS CRACKED. ACCOMPLISHED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100050 20010521 00050 NM 2001 5 21 2001UALA00627 1 20010502 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 314UA 23675 DAMAGE AT AFT CARGO DOOR CUTOUT STA 845, BETWEEN STR 21R AND 22R. TRIMMED OUT AFFECTED MATERIAL. ACCOMPLISHED REINFORC EMENT REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100051 20010521 00051 2001 5 21 2001UALA00628 4 20010428 A 3414 INDICATOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE COCKPIT FAILED A UALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 29 7283U 21561 ABORTED TAKEOFF AT 80 KNOTS DUE TO FAILURE OF THE FIRST OFFICERS AIRSPEED INDICATOR. 2 L 7 3 4F 4 F A3WE E2EA 2001052100052 20010521 00052 NM 2001 5 21 2001UALA00629 1 20010427 A 2822 PUMP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUEL BOOST FAILED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 7465U 21919 AIRCRAFT RETURNED TO DEN DUE TO LOSS OF THE SECOND FUEL BOOST PUMP IN THE CENTER TANK. BOOST PUMP FAILED. REPLACED THE BOOST PUMP. 2 L 7 3 4F 4 F A3WE E2EA 2001052100054 20010521 00054 NM 2001 5 21 2001UALA00631 1 20010504 A 5320 CHANNEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 CABIN FLOOR CHANNEL UPPER SURFACE CORRODED. STATION 365.25 RBL 26.INSTALLED FILLER AND DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2001052100055 20010521 00055 NM 2001 5 21 2001UALA00632 1 20010504 A 5320 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 INTERCOSTAL CRACKED IN AFT PIT. STA 1319 RBL 5 MAJOR REPAIR ACCOMPLISHED.REPAIRED INTERCOSTAL PER SRM 51-70-13. 2 L 7 2 4F 4 F RT A2NM E17NE 2001061800011 20010618 00011 NM 2001 6 18 2001UALA00633 1 20010202 A 2720 69372906 CONTROL ROD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RUDDER CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 304UA 23665 RUDDER POWER CONTROL UNIT CONTROL ROD AFT END OUTBOARD SIDE CHAFED, WORN AND KINKED. *S/D* CONTROL ROD REPLACED WITH S ERVICEABLE CONTROL ROD. OFF UNIT SCRAPPED PER BOEING SERVICE LETTER 737-SL-27-098 WHICH WAS WRITTEN TO ADDRESS THIS IS SUE IN APRIL 1995. HEAVY MAINTENANCE JOB INSTRUCTION CARDS ARE IN PLACE TO INSPECT RODS FOR SIDE CHAFING, AND DISPOSITI ON BASED ON FINDINGS. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100056 20010521 00056 NM 2001 5 21 2001UALA00634 1 20010504 A 5320 THRESHOLD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 314UA 23675 AFT PIT DOOR THRESHOLD WEB CORRODED AT STA 789. MAJOR REPAIR ACCOMPLISHED.REPLACED THRESHOLD WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100057 20010521 00057 NM 2001 5 21 2001UALA00635 1 20010504 A 5553 ATTACH FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE VERTICAL STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 314UA 23675 VERTICAL STABILIZER LUGS FRETTING ON BUSHING FLANGES. REWORKED VERTICAL STABILIZER ATTACH FITTINGS. 2 L 7 2 4F 4 F RT A16WE E2GL 2001061800012 20010618 00012 NM 2001 6 18 2001UALA00636 1 20010419 A 2720 69372906 CONTROL ROD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RUDDER CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 314UA 23675 RUDDER POWER CONTROL UNIT CONTROL ROD AFT END OUTBOARD SIDE CHAFED, WORN AND KINKED. *S/D* CONTROL ROD REPLACED WITH S ERVICEABLE CONTROL ROD. OFF UNIT SCRAPPED PER BOEING SERVICE LETTER 737-SL-27-098 WHICH WAS WRITTEN TO ADDRESS THIS ISS UE IN APRIL 1995. HEAVY MAINTENANCE JOB INSTRUCTION CARDS ARE IN PLACE TO INSPECT RODS FOR SIDE CHAFING, AND DISPOSITIO N BASED ON FINDINGS. 2 L 7 2 4F 4 F RT A16WE E2GL 2001061800013 20010618 00013 NM 2001 6 18 2001UALA00637 1 20010202 A 2720 69372906 CONTROL ROD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RUDDER CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 303UA 23644 RUDDER POWER CONTROL UNIT CONTROL ROD AFT END OUTBOARD SIDE CHAFED, WORN AND KINKED. *S/D* CONTROL ROD REPLACED WITH S ERVICEABLE CONTROL ROD. OFF UNIT FOUND TO BE WITHIN LIMITS PER BOEING SERVICE LETTER 737-SL-27-098 WHICH WAS WRITTEN TO ADDRESS THIS ISSUE BACK IN APRIL 1995. HEAVY MAINTENANCE JOB INSTRUCTION CARDS ARE IN PLACE TO INSPECT RODS FOR SIDE C HAFING, AND DISPOSITION BASED ON FINDINGS. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100058 20010521 00058 NM 2001 5 21 2001UALA00639 1 20010504 A 5330 SKIN BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 996UA 22456 FUSELAGE SKIN CRACKED BETWEEN WL 207 AND 218 AT RBL 5.7. REMOVED DAMAGE AND INSTALLED REPAIR PER SRM 53-10-11. 2 L 7 2 4F 4 F A16WE E2EA 2001071100028 20010711 00028 NE 2001 7 11 2001UALA00640 2 20010503 A 7314 378201 PUMP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE FAILED A UALA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 WP 29 7253U 63488 3860 21400 696611 AIRCRAFT DIVERTED TO MSP DUE TO NUMBER THREE ENGINE SHUTDOWN. *S/D* THE ENGINE DRIVEN FUEL PUMP LOST FUEL FLOW CAUSING THE ENGINE TO FLAME OUT. REPLACED THE FUEL CONTROL UNIT AND THE FUEL PUMP. 2 L 7 3 4F 4 F A3WE E2EA 2001052100059 20010521 00059 NM 2001 5 21 2001UALA00641 1 20010504 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 LH CHORD ANGLE CRACKED IN RADIUS WL 207 BS 188 LBL 27. MAJOR REPAIR ACCOMPLISHED. REPAIRED CHORD ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100060 20010521 00060 NM 2001 5 21 2001UALA00642 1 20010504 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 CREASE BEAM WEB CRACKED. STA 638 STR 17R. MAJOR REPAIR ACCOMPLISHED.REPLACED CREASE BEAM WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2001071200092 20010712 00092 NM 2001 7 12 2001UALA00645 1 20010502 A 3350 78941 HARNESS BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN FAULTY A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 779UA 26941 EEL LIGHTS (2) AT 3E INOP. *S/D* MOVEABLE SIDEREST/ARMREST DAMAGED THE FIRST CLASS PROXIMITY LUMINESCENT LIGHT STRIPS WIRE HARNESSES. REPLACED THE FIRST CLASS PROXIMITY LUMINESCENT LIGHT STRIPS WIRE HARNESSES, 2 EA. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001071200093 20010712 00093 NM 2001 7 12 2001UALA00646 1 20010502 A 2421 UALMR24121 IDG BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT ENGINE CONTAMINATED A UALA J A DUMP FUEL UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION NR NOT REPORTED 1 WP 29 214UA 30220 RIGHT GENERATOR DRIVE LIGHT AND RIGHT GENERATOR CONTROL OFF LIGHTS AND EICAS DISCONNECTED RIGHT DRIVE AS PER CHECKLIST. (FUEL JETTISONED APPROX 15,000 LBS) *S/D* ELEC GEN OFF R AND ELEC GEN SYS R STATUS MESSAGES WERE DISPLAYED WITH ASSOC IATED MAINTENANCE MESSAGE 24-31662. THE RIGHT IDG DPI WAS FOUND TRIPPED WITH HEAVY CONTAMINATION IN THE FILTER. THE ID G WAS REPLACED ALONG WITH IDG AIR/OIL HEAT EXCHANGER, FUEL OIL COOLER AND FLUSHED ALL LINES. IT WAS ALSO REPORTED THAT THE QUAD RING MOUNTING BOLTS WERE FOUND LOOSE IN THE GEAR BOX. THE QUAD RING MOUNTING BOLTS WERE ALSO REPLACED. A PREL IMINARY FINDING REPORT INDICATES THAT THE IDG ANTIDRIVE BEARING FAILED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001052100061 20010521 00061 NM 2001 5 21 2001UALA00647 1 20010430 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 FUSELAGE SKIN DENTED STA 1593-1596 BETWEEN STR 14R AND 15R. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2001052100062 20010521 00062 NM 2001 5 21 2001UALA00648 1 20010503 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 CABIN FLOORBEAM CAP CORRODED. STA 365 RBL 51 - 60. REMOVED DAMAGE AND INSTALLED NEW T CHORD. 2 L 7 2 4F 4 F RT A2NM E17NE 2001052100066 20010521 00066 NM 2001 5 21 2001UALA00649 1 20010504 A 2751 INDICATOR BOEING 737 737291 138448W NM PWA JT8 JT8D9A 52048 NE COCKPIT INOPERATIVE A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 981UA 21546 AFTER TAKEOFF FLAPS WOULD NOT RETRACT. REPLACED FLAP POSITION INDICATOR. 2 L 7 2 4F 4 F A16WE E2EA 2001052100067 20010521 00067 NM 2001 5 21 2001UALA00650 1 20010505 A 2844 SWITCH BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUEL SYSTEM INOPERATIVE A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 915UA 25382 ON TAKEOFF CLIMBOUT FWD BOOST PUMP LIGHTS ILLUMINATED ON NR 1 AND NR 2 MAIN TANKS. REPLACED BOTH PRESURE SWITCHES. 2 L 7 2 4F 4 F RT A16WE E2GL 2001060100163 20010601 00163 NM 2001 6 1 2001UALA00651 1 20010505 A 7711 58T52401 SENSE LINE PWA PW40903 BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 1 ENGINE FRACTURED A UALA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 29 791UA 16080 16080 222046 26933 222046 RIGHT ENGINE DID NOT SPOOL UP TO FULL TAKEOFF POWER, LAG 1.5 KNOTS BEHIND LEFT THROTTLE. ABORTED TAKEOFF AT LOW SPEEDS. *S/D* FOUND PROBLEM WITH LEFT ENGINE PT 4.95 LINE RIGHT ENGINE OPS NORMAL. FOUND LINE BROKEN ON LEFT ENGINE. PER 1- 0-13-3 INTRIM REPAIRED FOR ONE FLIGHT ONLY TO TERMINATION OF FLT 8894-06. ACFT TO OPERATE IN N1 MODE ONLY. LEFT ENGINE PT 4.95 EPR SENSE LINE REPLACED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001071200094 20010712 00094 NM 2001 7 12 2001UALA00653 1 20010506 A 2751 2061131 INDICATOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE COCKPIT FAILED A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 7287U 21565 LANDED UNDER AMBER ALERT DUE TO SPLIT TRAILING EDGE FLAP INDICATION. *S/D* THE FLAP POSITION INDICATOR FAILED. REMOVE D AND REPLACED BOTH INBOARD AND OUTBOARD FLAP POSITION INDICATOR. CYCLED FLAPS SEVERAL TIMES, OPERATION CHECKS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001052100068 20010521 00068 NM 2001 5 21 2001UALA00654 1 20010504 A 2131 CONTROLLER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN PRESSURE FAILED A UALA K NONE O OTHER DE DESCENT 1 WP 29 7280U 21558 AUTO PRESSURIZATION FAILED DURING DESCENT. 2 L 7 3 4F 4 F A3WE E2EA 2001071800012 20010718 00012 NM 2001 7 18 2001UALA00655 1 20010504 A 2782 269002910 ACTUATOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE L/E SLAT LEAKING A UALA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 7298U 21893 DURING TAXI LOST HYDRAULIC SYSTEM-A. *S/D* LT NR 3 SLAT ACTUATOR WAS LEAKING. REMOVED AND REPLACED LT NR 3 SLAT ACTUA TOR IN ACCORDANCE WITH MAINTENANCE MANUAL. OPERATIONAL CHECKS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001052100069 20010521 00069 NM 2001 5 21 2001UALA00656 1 20010506 A 5712 RIB BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7292U 21570 NR 6 SLAT ACTUATOR ATTACHMENT INBOARD AND OUTBOARD RIBS ARE CRACKED. REPAIRED ATTACHMENT RIBS PER SM-0R 70-57-56-01-AR5 . 2 L 7 3 4F 4 F A3WE E2EA 2001052100070 20010521 00070 EU 2001 5 21 2001UALA00657 1 20010503 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 463UA 1282 FWD LT EMERGENCY POWER SUPPLY UNIT, EMERGENCY LIGHT TEST FAILS. REPLACED EMERGENCY POWER SUPPLY UNIT AND BATTERY, TESTS OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2001061800016 20010618 00016 NM 2001 6 18 2001UALA00658 1 20010507 A 2782 755299B ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L/E SLAT FAILED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 503UA 24624 LEADING EDGE LIGHT ON AND EICAS L/E SLAT DISAGREE MESSAGE. *S/D* LEADING EDGE SLAT ROTARY ACTUATOR NR 2 FAILED, WHICH CAUSED THE SLAT SYSTEM TO LOCKOUT AND ILLUMINATE THE DISAGREE LIGHT AND MESSAGE. REPLACED ACTUATOR NR 2, 3 AND 10 DUE T O OVERLOAD INDICATORS POPPED. 2 L 7 2 4F 4 F RT A2NM E17NE 2001052100071 20010521 00071 NM 2001 5 21 2001UALA00659 1 20010505 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 FLOOR SUPPORT STRUCTURE CORRODED. STA 1673 WL 208 TOP AND BOTTOM SURFACE. REPLACED FLOOR SUPPORT STRUCTURE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001052100072 20010521 00072 NM 2001 5 21 2001UALA00660 1 20010505 A 5320 SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 DOOR FRAME SILL SUPOORT CORRODED. STA 1645 RBL 52 WL 208. MAJOR REPAIR ACCOMPLISHED. REPLACED SUPPORT CHANNEL. 2 L 7 2 4F 4 F RT A2NM E17NE 2001052100073 20010521 00073 NM 2001 5 21 2001UALA00661 1 20010506 A 5320 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 FWD PIT FLOOR SUPPORT INTERCOSTAL CRACKED. STA 663 RBL 19.8. MAJOR REPAIR ACCOMPLISHED. REPLACED INTERCOSTAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2001052100074 20010521 00074 NM 2001 5 21 2001UALA00662 1 20010506 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 CABIN FLOORBEAM CORRODED. STA 365 RBL 51 TO 70. SPLICED IN UPPER CHORD. 2 L 7 2 4F 4 F RT A2NM E17NE 2001052100075 20010521 00075 NM 2001 5 21 2001UALA00663 1 20010506 A 5310 DOOR FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 FWD CARGO DOOR LWR AFT EDGE FRAME IS CRACKED AT CORNER. REPLACED CORNER FRAME. 2 L 7 2 4F 4 F RT A2NM E17NE 2001052100076 20010521 00076 NM 2001 5 21 2001UALA00665 1 20010505 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 FRAME CRACKED. STA 188 STR 17L WL 207 INSTALLED SKIN ACCESS DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001071800013 20010718 00013 NM 2001 7 18 2001UALA00666 1 20010508 A 2751 1817381 TRANSMITTER BOEING 737 737291 138448W NM PWA JT8 JT8D9A 52048 NE T/E FLAP FAULTY A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 980UA * 21545 STICK SHAKER FROM LIFTOFF TO 1500 FOOT AGL AND FLAP RETRACTED. *S/D* REPLACED RIGHT FLAP POSITION TRANSMITTER. 2 L 7 2 4F 4 F A16WE E2EA 2001052100077 20010521 00077 NM 2001 5 21 2001UALA00667 1 20010430 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 588 STRINGER 39L-39R SHEARTIE CORRODED. MAJOR REPAIR ACCOMPLISHEDFABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH B AC DRAWING 140T2102 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001052100078 20010521 00078 NM 2001 5 21 2001UALA00668 1 20010430 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 347 STRINGER 39L-STRINGER 39R SHEARTIE CORRODED. MAJOR REPAIR ACCOMPLISHED FABRICATED AND INSTALLED REPAIR IN ACCORDA NCE WITH BAC DRAWING140T2102 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001052100079 20010521 00079 NM 2001 5 21 2001UALA00669 1 20010430 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 390 STRINGER 38R-39R SHEARTIE CORRODED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T1223 AND S RM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001052100080 20010521 00080 NM 2001 5 21 2001UALA00670 1 20010509 A 5330 SKIN AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 819UA 893 LT FUSELAGE SKIN DENT BETWEEN FRAME 23 AND FRAME 24 AND BETWEEN STRINGER 22LT AND STRINGER 23LT. REPAIRED FUSELAGE SKIN DENT. 2 L 7 2 4F 4 F RT A28NM E40NE 2001052100081 20010521 00081 NM 2001 5 21 2001UALA00671 1 20010430 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 1404-1439 STRINGER 34R CORRODED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 53-00-03 AND 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001052100082 20010521 00082 NM 2001 5 21 2001UALA00673 1 20010430 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 412 STRINGER 38L-39L SHEAR TIE CORRODED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 141T1224. 2 L 7 2 4F 4 F RT A1NM E3NE 2001052100083 20010521 00083 NM 2001 5 21 2001UALA00674 1 20010430 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 566 STRINGER 39L-39R SHEARTIE CORRODED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T2102 AND S RM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001052100084 20010521 00084 NM 2001 5 21 2001UALA00675 1 20010430 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 1153 BL-0 TO RBL 46 T-CAP CORRODED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 146T1060-2 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001052100085 20010521 00085 NM 2001 5 21 2001UALA00676 1 20010430 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS1210-1252 STRINGER 39L CORRODED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 53-00-03 AND 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001052100086 20010521 00086 NM 2001 5 21 2001UALA00677 1 20010430 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 1241-1263 STRINGER 39L CORRODED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 53-00-03 FIGURE 202. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071800015 20010718 00015 NM 2001 7 18 2001UALA00679 1 20010509 A 2120 123CH1A SENSOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EQUIP COOLING FAULTY A UALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 29 312UA 23673 EQUIPMENT COOLING EXHAUST FAN NORMAL AND ALT WARNING LIGHTS ILLUMINATED. *S/D* REPLACED THE M100 LOW FLOW SENSOR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100087 20010521 00087 NM 2001 5 21 2001UALA00680 1 20010430 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 390 STRINGER 39L TO 39R SHEAR TIE CORRODED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 141T1223. 2 L 7 2 4F 4 F RT A1NM E3NE 2001052100088 20010521 00088 NM 2001 5 21 2001UALA00681 1 20010503 A 5311 FRAME BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 1395 FRAME T-CAP CORRODED AT RBL 44. MAJOR REPAIR ACCOMPLISHED FABRICATED AND INSTALLED REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001052100089 20010521 00089 NM 2001 5 21 2001UALA00682 1 20010507 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 314UA 23675 R1 DOOR CUTOUT FRAME CRACKED AT INBD RADIUS. BS 296.5 STR 7R MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100090 20010521 00090 NM 2001 5 21 2001UALA00683 1 20010507 A 5320 STRAP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 314UA 23675 WEB SUPPORT STRAP CORRODED. AFT PIT STA 787-820 RBL 19. MAJOR REPAIR ACCOMPLISHED. REPLACED STRAP. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100091 20010521 00091 NM 2001 5 21 2001UALA00684 1 20010507 A 5320 ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 FRAME ANGLE CRACKED. STA 188 WL 207 STR 17L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100093 20010521 00093 NM 2001 5 21 2001UALA00686 1 20010506 A 5320 CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 FLOOR CLIP CRACKED. STA 178 LBL 28 WL 207 REPLACED CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100094 20010521 00094 NM 2001 5 21 2001UALA00687 1 20010506 A 5320 MOUNT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 314UA 23675 CRACK AT LOWER INBD FASTENER OF UPPER LH ANTENNA MOUNT ALONG STRAP EDGE. STA 178. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100095 20010521 00095 NM 2001 5 21 2001UALA00688 1 20010506 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 STRINGER CORRODED. AFT PIT STA 727 STR 25L. INSTALLED STRINGER SPLICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100096 20010521 00096 NM 2001 5 21 2001UALA00689 1 20010507 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 314UA 23675 WEB CRACKED AT UPPER RT RADAR MOUNT OUTBOARD LWR SIDE STA 178. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100097 20010521 00097 NM 2001 5 21 2001UALA00690 1 20010507 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 FWD PRESSURE BULKHEAD SKIN CRACKED. STA 178, WL 214.5, LBL 5.7 TO RBL 5.7. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100098 20010521 00098 NM 2001 5 21 2001UALA00691 1 20010506 A 5312 BULKHEAD BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 974UA 21597 BULKHEAD WEB CRACKED AT LOWER RT RADAR MOUNT. STA 178, WL200, RBL 5. REPAIR DOUBLER INSTALLED. 2 L 7 2 4F 4 F A16WE E2EA 2001052100099 20010521 00099 NM 2001 5 21 2001UALA00692 1 20010508 A 5315 FLOORBEAM BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 996UA 22456 FLOOR BEAM WEB CRACKED IN TWO PLACES. STA 706-716 BL 0. INSTALLED DOUBLER. 2 L 7 2 4F 4 F A16WE E2EA 2001052100101 20010521 00101 NM 2001 5 21 2001UALA00695 1 20010508 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 CIRCUMFORENTIAL CHORD CRACKED. FORWARD NOSE COMPARTMENT STA 188, STR 17R, WL 206. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100102 20010521 00102 NM 2001 5 21 2001UALA00696 1 20010509 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 OVERWING BODY FRAME TO STUB BEAM CRACKED. STA 616 LT SIDE. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100103 20010521 00103 NM 2001 5 21 2001UALA00697 1 20010508 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 FLOORBEAM UPPER SURFACE CORRODED. STA 1640 LBL 31 TO RBL 51 WL 208. INSTALLED T-CAP REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2001052100104 20010521 00104 NM 2001 5 21 2001UALA00698 1 20010509 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 FLOOR BEAM UPPER SURFACE CORRODED. STA 1681, RBL 12 AND RBL 24 TO RBL 30, WL 208. INSTALLED FILLERS AND DOUBLERS. 2 L 7 2 4F 4 F RT A2NM E17NE 2001052100105 20010521 00105 NM 2001 5 21 2001UALA00699 1 20010510 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 FLOORBEAM CORRODED. STA 1681 RBL 24 TO RBL 30. INSTALLED T-CAP REPAIR WITH STIFFINERS. 2 L 7 2 4F 4 F RT A2NM E17NE 2001052100106 20010521 00106 NM 2001 5 21 2001UALA00700 1 20010510 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 FLOORBEAM CORRODED STA 1681 RBL 12. INSTALLED T-CAP REPAIR AND STIFFENERS. 2 L 7 2 4F 4 F RT A2NM E17NE 2001052100107 20010521 00107 NM 2001 5 21 2001UALA00701 1 20010510 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 FLOORBEAM CORRODED STA 1681 RBL 32. INSTALLED T-CAP REPAIR AND STIFFENERS. 2 L 7 2 4F 4 F RT A2NM E17NE 2001052100108 20010521 00108 NM 2001 5 21 2001UALA00702 1 20010510 A 5320 WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 SHEAR WEB CORRODED. STA 1681 LBL 12. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER AND FILLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2001052100109 20010521 00109 NM 2001 5 21 2001UALA00703 1 20010510 A 5753 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE T/E FLAP DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 RT WING TRAILING EDGE AFT FLAP DAMAGED. LOWER COMPOSITE INBOARD OF NR 7 FLAP TRACK TO LAST 2 INCHES OF TRAILING EDGE. BO NDED IN FILLER AND BOTTOM LAYERS LAIDUP REPAIR PLYS. 2 L 7 2 4F 4 F RT A2NM E17NE 2001052100110 20010521 00110 NM 2001 5 21 2001UALA00704 1 20010510 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 FRAME DENTED. AFT PIT STA 787 RBL 26. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE, STRAP AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100111 20010521 00111 NM 2001 5 21 2001UALA00705 1 20010510 A 5553 ATTACH FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE VERTICAL STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 314UA 23675 AFT LEFT AND RIGHT FAILSAFE ATTACH LUGS ON VERTICAL STABILIZER FRETTED. REMOVED BUSHINGS, REWORKED LUG AREA AND INSTALLE D NEW BUSHINGS. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100112 20010521 00112 NM 2001 5 21 2001UALA00706 1 20010511 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 FLOORBEAM WEB CRACKED STA 195 WL 207 LBL 30 INBD OF STR 17L. INSTALLED NEW WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052100113 20010521 00113 NM 2001 5 21 2001UALA00707 1 20010511 A 5320 ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 FLOOR BEAM Z ANGLE CHORD CORRODED. STA 947-990 AT DOOR THRESHOLD. REPLACED Z ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052200001 20010522 00001 2001 5 22 SWAA011409 4 20010511 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULE C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. RE-ADJUSTED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001052200002 20010522 00002 2001 5 22 SWAA011430 4 20010511 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001052200003 20010522 00003 WP 2001 5 22 ZW0A0101305 1 20010507 A 5310 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9630A 53561 DURING CHECK-C MAINT IN THE LT MAIN GEAR WELL, THE FWD INBOARD CORNER OF THE LT GEAR WELL DOOR FRAME WAS CRACKED. STOP DRILLED CRACK AND INSTALLED 2 DOUBLERS PER SRM 53-01, FIG 2 SHEET 4. 2 L 7 2 4F RT A6WE 2001052200004 20010522 00004 NM 2001 5 22 ZW0A0101301 1 20010509 A 3350 LIGHT BOEING 767 7673Y0 NM CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 632TW 24953 THE AFT GALLEY EGRESS LIGHT WAS INOPERATIVE. REPAIRED BROKEN WIRES, REPLACED BROKEN LIGHT ASSEMBLY P/N 0202175-007, AND REPLACED BURNED OUT LAMP P/N 17023. CHECK-C 3-22-01 LAX. 2 L 7 2 4F RT A1NM 2001052200005 20010522 00005 NM 2001 5 22 ERKR200100105 1 20010509 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 SURFACE CORROSION ON R-5 WINDOW FRAME INTERIOR, AFT LOWER CORNER AT STA 250. REMOVED WINDOW FRAME PER 747 SRM 51-10-01. REMOVED CORROSION PER 747 SRM 56-20-01. FOUND WINDOW FRAME WITHIN LIMITS PER ECRA 3203-53-047-2. ALODINED WINDOW FRA ME PER 747 SRM 51-10-02 AND PRIMED PER SOPM 20-41-02. INSTALLED WINDOW FRAME PER 747 SRM 51-30-02. 2 L 7 4 4F A20WE 2001052200006 20010522 00006 WP 2001 5 22 IXXA0100024 1 20010509 A 2612 WARNING LIGHT DOUG DC8 DC871F 302199D WP COCKPIT FALSE ACTIVATION A IXXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 11 821BX 45811 EN ROUTE FROM BDL TO IND, THE LOWER FORWARD CARGO COMPARTMENT FIRE WARNING LIGHT ILLUMINATED. THE FORWARD LOWER CARGO C OMPARTMENT FIRE DETECTION SYSTEM WAS PREVIOUSLY ON DEFERRAL IN ACCORDANCE WITH THE COMPANY APPROVED MEL 26-10. THE FLIG HT CREW FOLLOWED COMPANY PROCEDURES AND RETURNED TO BDL FOR AN UNEVENTFUL LANDING. AIRPORT EMERGENCY CREWS MEET THE AIR CRAFT AND VERIFIED NO FIRE WAS PRESENT. THE AIRCRAFT RETURNED TO THE RAMP. MAINTENANCE DEACTIVATED THE LOWER CARGO FIR E DETECTION SYSTEM IN ACCORDANCE WITH THE COMPANY ENGINEERING ORDER 26-DC8-1249. THE AIRCRAFT WAS RETURNED TO SERVICE. UPON ACCOMPLISHMENT OF REPAIRS A FOLLOW UP WILL BE SUBMITTED. 2 L 7 4 4F RT 4A25 2001052200007 20010522 00007 NM 2001 5 22 ERKR200100106 1 20010509 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 RIGHT WINDOW AT STA 1210 HAS CORROSION ON AND AROUND WINDOW CASTING. REMOVED WINDOW FORGING PER 747 SRM 51-30-02. REMO VED CORROSION PER 747 SRM 51-10-01 AND FOUND WINDOW FORGING TO BE WITHIN ALLOWABLE LIMITS PER ECRA 3203-53-047-2. ALODI NED WINDOW FORGING PER 747 SRM 51-10-02 AND PRIMED PER SOPM 20-41-02. INSTALLED WINDOW FORGING PER 747 SRM 51-30-02. 2 L 7 4 4F A20WE 2001052200008 20010522 00008 NM 2001 5 22 ERKR200100107 1 20010509 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 L-12 WINDOW STA 370 HAS CORROSION ON AND AROUND WINDOW CASTING. REMOVED WINDOW CASTING PER 747 SRM 51-30-02. REMOVED C ORROSION ON CASTING PER 747 SRM 51-10-01 AND FOUND WINDOW CASTING WITHIN LIMITS PER ECRA 3203-53-047-2. ALODINED WINDOW CASTING PER 747 SRM 51-10-02 AND PRIMED PER SOPM 20-41-02. INSTALLED WINDOW CASTING PER 747 SRM 51-30-02. 2 L 7 4 4F A20WE 2001052200009 20010522 00009 NM 2001 5 22 ERKR200100108 1 20010509 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 WINDOW AT STA 1210 LEFT HAS CORROSION ON AND AROUND WINDOW CASTING. REMOVED WINDOW CASTING PER 747 SRM 51-30-02. REMOV ED CORROSION PER 747 SRM 51-10-01, AND FOUND WINDOW CASTING WITHIN LIMITS PER ECRA 3203-53-047-2. ALODINED WINDOW CASTI NG PER 747 SRM 51-10-02 AND PRIMED PER SOPM 20-41-02. INSTALLED WINDOW CASTING PER 747 SRM 51-30-02. 2 L 7 4 4F A20WE 2001052200010 20010522 00010 NM 2001 5 22 ERKR200100109 1 20010509 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 WINDOW AT STA 1130 LEFT HAS CORROSION ON AND AROUND WINDOW CASTING. REMOVED WINDOW CASTING PER 747 SRM 51-30-02. REMOV ED CORROSION FROM WINDOW CASTING PER 747 SRM 51-10-01 AND FOUND IT WITHIN LIMITS PER ECRA 3203-53-047-2. ALODINED WINDO W CASTING PER SRM 51-10-02 AND PRIMED PER SOPM 20-41-02. INSTALLED WINDOW CASTING PER 747 SRM 52-30-02. 2 L 7 4 4F A20WE 2001052200011 20010522 00011 NM 2001 5 22 ERKR200100110 1 20010409 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 WINDOW AT STA 1427 RIGHT HAS CORROSION ON AND AROUND WINDOW CASTING. REMOVED WINDOW CASTING PER 747 SRM 51-30-02. REMO VED CORROSION FROM WINDOW CASTING PER 747 SRM 51-10-01 AND FOUND WINDOW CASTING WITHIN LIMITS PER ECRA 3203-53-047-2. A LODINED WINDOW CASTING PER 747 SRM 51-10-02 AND PRIMED WINDOW CASTING PER SOPM 20-41-02. INSTALLED WINDOW CASTING PER 7 47 SRM 51-30-02. 2 L 7 4 4F A20WE 2001052200012 20010522 00012 NM 2001 5 22 ERKR200100111 1 20010509 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 MAIN CABIN STA 1040-1060 RIGHT HAND WINDOW FORGING HAS CORROSION COMING OUT FROM UNDER SEALANT. REMOVED WINDOW FORGING PER 747 SRM 51-30-02. REMOVED CORROSION FROM WINDOW FORGING PER 747 SRM 51-10-01, WINDOW CASTING FOUND TO BE WITHIN LIM ITS PER ECRA 3203-53-047-2. ALODINED WINDOW CASTING PER 747 SRM 51-10-02 AND PRIMED WINDOW CASTING PER SOPM 20-41-02. INSTALLED WINDOW CASTING PER 747 SRM 51-30-02. 2 L 7 4 4F A20WE 2001052200013 20010522 00013 NM 2001 5 22 ERKR200100112 1 20010509 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 MAIN CABIN LT SIDE BETWEEN STA 1416 AND STA 1438 S-20L AND S-22L HAS CORROSION AT WINDOW FORGING. REMOVED WINDOW FORGIN G PER 747 SRM 51-30-02. REMOVED CORROSION ON WINDOW FORGING PER 747 SRM 51-10-01, FOUND WINDOW FORGING WITHIN LIMITS PE R ECRA 3203-53-047-2. ALODINED WINDOW FORGING PER 747 SRM 51-10-02 AND PRIMED WINDOW FORGING PER SOPM 20-41-02. INSTAL LED WINDOW FORGING PER 747 SRM 51-30-02. 2 L 7 4 4F A20WE 2001052200014 20010522 00014 EU 2001 5 22 C2XA01CL097 1 20010508 A 3350 1155691 COVER AEROSP ATR42 ATR42320 8680930 EU CABIN BROKEN A C2XA K NONE O OTHER UK UNKNOWN 1 SW 27 25811 094 CLE FLIGHT 3747 THE CREW REPORTED EMERGENCY AISLE PATH LIGHTING COVER WILL NOT STAY ATTACHED. MAINTENANCE REPLACED EMER GENCY AISLE PATH LIGHTING COVER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A53EU 2001052200015 20010522 00015 EA 2001 5 22 COMA0160368 1 20010507 A 5753 601R14303 SKIN CNDAIR CL600 CL6002B19 EA RT FLAP VANE CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 914CA 18716 7012 INBOARD FLAP VANE LANDING EDGE SRM RIGHT HAND INBOARD FLAP CHAFED. REMOVED AND REPLACED INBOARD FLAP VANE LEADING EDGE SKIN ON RT INBOARD FLAP IAW WVAC EO 601R-57-2442. 2 L 7 2 4F RT A21EA 2001052200016 20010522 00016 EU 2001 5 22 MALA010444 1 20010506 A 2930 WARNING LIGHT BAC 146 AVRO146RJ85A 1500097 EU COCKPIT ILLUMINATED A MALA K NONE J WARNING INDICATION CR CRUISE 1 GL 15 532XJ E2366 DURING CRUISE ON FLIGHT 3528, IN DTW, YELLOW SYSTEM HI TEMP LIGHT CAME ON DURING CRUISE. QRH MAINTENANCE REMOVED AND RE PLACED ENG DRIVEN PUMP, L/P FILTER, AC PUMP, AND YELLOW SYSTEM TEMP SENSOR. SEE MM 409 CARD NR 133380 FOR DETAILS. ALL CHECKS GOOD AT THIS TIME. 2 H 7 4 4F RT A49EU 2001052200017 20010522 00017 EU 2001 5 22 MALA010445 1 20010508 A 3260 327 LIGHT SAAB SF340 SF340A 7850100 EU COCKPIT INOPERATIVE A MALA L ABORTED APPROACH O OTHER DE DESCENT 1 GL 15 41XJ 041 ON DESCENT FOR LANDING ON FLIGHT 3173, ONLY HAD 2 GEAR DOWN LIGHTS, AFTER GEAR EXTENSION. EXECUTED MISSED APPROACH OF R AN QRH, CHANGED BULBS, RECEIVED 3 GEAR DOWN LOCKED LIGHTS. 2 BULBS USED FROM BULB HOLDER. MAINTENANCE RESTOCKED BULBS. P/N 327. 2 L 7 2 4T RT A52EU 2001052200018 20010522 00018 EU 2001 5 22 RAIA00105007 1 20010510 A 3240 810007A COMPUTER AEROSP ATR42 ATR42300 8680920 EU E/E BAY FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 423TE 3052 119 7490-STL-BRAKE TEMPERATURE HOT LIGHT ILLUMINATED DURING TAXI. MAINTENANCE INSPECTED AND FOUND TO BE AN INDICATION PROBL EM. MAINTENANCE REPLACED THE BRAKE TEMPERATURE MONITORING UNIT, AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A53EU 2001052200019 20010522 00019 WP 2001 5 22 ZW0A0101501 1 20010510 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ZW0A K NONE L NO TEST NR NOT REPORTED 1 CE 13 959U 49704 THE EGRESS LIGHTING IN THE FIRST CLASS SECTION WAS INOPERATIVE. REMOVED THE LIGHT STRIP. CLEANED THE TRACK AND ELECTRI CAL CONTACTS. PRESERVED CONTACTS WITH MOISTURE LOCKOUT BEFORE RE-INSTALLING. CHECK-C 12-3-00 MCI. 2 L 7 2 4F A6WE 2001052200020 20010522 00020 CE 2001 5 22 GLBA2001097 1 20010509 A 5240 DOOR BEECH 1900 1900D 1154162 CE SERVICE DOOR OPEN A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 195GL UE195 RIGHT OIL SERVICE DOOR OPENED DURING CLIMBOUT. RESECURED DOOR, OPS CHECKED GOOD. 2 L 7 2 4T RT A24CE 2001061300029 20010613 00029 CE 2001 6 13 GLBA2001098 1 20010510 A 5220 DOOR BEECH 1900 1900D 1154162 CE EMERGENCY EXIT DIRTY A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 151UX UE151 CABIN ALTITUDE HI ILLUMINATED ON CLIMBOUT. CLEANED AND RESEALED EMERGENCY EXIT DOOR, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001052200021 20010522 00021 2001 5 22 SWIA972559 4 20010509 A 3422 FLUX DETECTOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT WING DEFECTIVE A SWIA A UNSCHED LANDING I FLT. ATTITUDE INST. CL CLIMB 1 NM 07 562SW 120336 UPON TAKEOFF OUT OF IYK, GOT THE HDG FLAG. SHORTLY THEREAFTER, GOT THE PIT AND ROL FLAGS. ATTEMPTED QRH RESET, NO RESU LTS. THE FIRST OFFICERS ATTITUDE INDICATOR SHOWED PITCH DOWN 10 PERCENT THE WHOLE FLIGHT. THE CAPTAINS ADI AND HEADING INDICATOR SHOWED FLAGS, BUT SEEMED TO OPERATE FINE. DIVERTED DUE TO WEATHER. REPLACED FDU-70 FLUX DETECTOR ON RIGHT W ING TIP FIRST OFFICERS SIDE IAW MM 34-21-03. OPS CHECK GOOD. P/N ON 622-5812-004, S/N ON 20021, S/N OFF 16722. 2 L 7 2 4T 4 T RT A31SO E20NE 2001052200022 20010522 00022 2001 5 22 SWIA972560 4 20010509 A 3425 COMPUTER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE E/E BAY OUT OF TOLERANCE A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 585SW 120353 AFTER BOTH AUTOPILOTS KICKED OFF LINE, BOTH RED HDG FLAGS ILLUMINATED. FIRST OFFICER''S HDG OFF 30 DEGREES; THEN BOTH H DG FLAGS TURNED YELLOW. DIVERTED TO SMF DUE TO WEATHER. ACCOMPLISHED RE-ORIENTATION OF AHRS IAW SKYWEST MM INFORMATION . SYSTEM CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001052200023 20010522 00023 SO 2001 5 22 SWIA972561 1 20010509 A 2150 VALVE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE A/C BAY FAILED A SWIA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 NM 07 187SW 120037 RIGHT PACK FAILED DURING CLIMB. APPROXIMATELY 1 MINUTE LATER, THE LAV SMOKE DETECTOR STARTED BEEPING AND THE FLIGHT ATT ENDANT REPORTED SMOKE IN THE CABIN. WITH RECIRCS AND GASPERS OFF, THE CABIN SLOWLY CLEARED. REMOVED LEFT AND RIGHT RAM AIR VENTILATION VALVES AND LEFT HEAT EXCHANGER SPRAYER (H2O) DUCT WITH SERVICEABLE UNITS IAW MM 21-26-01 & 21-51-02. O PS CHECK GOOD. VALVE P/N ON LT 120-42193-001, LT P/N OFF 120-21588-001, DUCT P/N ON RT 120-42193-002, RT P/N OFF 120- 21588-002. 2 L 7 2 4T 4 T RT A31SO E20NE 2001052200024 20010522 00024 SO 2001 5 22 SWIA972562 1 20010507 A 4960 RELAY EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT ODOR A SWIA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 07 236SW 120312 STRONG ELECTRICAL SMELL COMING FROM UNDERNEATH FIRST OFFICERS SHELF. THE SHELF IS ALSO VERY HOT. FOUND AP FEEDER PROTE CTION RELAY WARM. REPLACED APU FEEDER PROTECTION RELAY. OPS CHECK OF APU AND GENERATOR GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001052200025 20010522 00025 SO 2001 5 22 C2XA01IA240 1 20010511 A 4930 161544100 TANK EMB 120 EMB120ER 3260203 SO APU ODOR A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 58733 120197 IAH - AFTER ENGINE SHUTDOWN ON TAXI TO GATE THE CREW REPORTED A FUEL SMELL IN THE CABIN AFTER APU START. MAINTENANCE DR AINED THE APU EPA TANK, OPERATIONALLY CHECKED THE APU WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001052200026 20010522 00026 SO 2001 5 22 C2XA01IA241 1 20010508 A 3397 W220035524 WIRE EMB 120 EMB120ER 3260203 SO CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 57734 120199 SHV - DURING MAINTENMANCE INSPECTION, THE EMERGENCY EXIT SIGN AT SEAT 10-C WAS FOUND TO BE INOPERATIVE. MAINTENANCE REP AIRED A BROKEN WIRE ON THE EMERGENCY LIGHT SYSTEM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001052200027 20010522 00027 EU 2001 5 22 C2XA01IA242 1 20010510 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 19812 99 IAH - DURING MAINTENANCE INSPECTION, SEVERAL AISLE PATH EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001052200028 20010522 00028 NM 2001 5 22 01FDEA00342 1 20010510 A 2900 2249409501 DRAIN LINE DOUG MD11 MD11F 3023600 NM NR 2 ENGINE LEAKING A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 592FE 48550 DURING CRUISE GOT HYD SYS 2 FAIL LEVEL 2 ALERT. REPLACED ENGINE HYD CASE DRAIN FILTERS, LT AND RT EDPS AND SERVICED HYD RAULICS. NO LEAKS NOTED. 2 L 7 3 4F RT A22WE 2001052200029 20010522 00029 NM 2001 5 22 CALA0100455 1 20010512 A 5313 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70330 23460 INSPECTION FOUND STRINGER 14R GOUGED AT STA 600. A NEW STRINGER SECTION WAS INSTALLED IAW SRM 53-00-03, PAGE 201. 2 L 7 2 4F RT A16WE 2001052200030 20010522 00030 WP 2001 5 22 CALA0100456 1 20010513 A 5320 FLOOR SUPPORT DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12061 47851 INSPECTION FOUND LAV J O/B FLOOR SUPPORT BEAM CORRODED IN AREAS OF TIE DOWN BOLTS AT STAY = 1887-2007 AT X = 58R. THE F LOOR SUPPORT BEAM WAS REMOVED AND A NEW FLOOR SUPPORT BEAM WAS INSTALLED IAW SRM 53-16-01. 2 L 7 3 4F A22WE 2001052200031 20010522 00031 WP 2001 5 22 CALA0100457 1 20010513 A 5240 BOTTLE DOUG DC10 DC1030 3023501 WP R4 DOOR DISCHARGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 39081 47861 DOOR R-4 WAS HARD TO OPERATE. THE R-4 DOOR N2 BOTTLE WAS RESERVICED IAW MM 52-12-16. 2 L 7 3 4F A22WE 2001052200032 20010522 00032 EA 2001 5 22 COMA0160372 1 20010513 A 5320 60034017595 ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 973CA 11350 7146 THE AFT J-ANGLE AT FS 280.00 IS CORRODED BETWEEN LBL 9 AND RBL 9. TRIMMED OUT DAMAGED AREA, FABBED J, FABBED TWO SPLICE SECTIONS AND INSTALLED IAW WVAC EO 601R-53-2454A. 2 L 7 2 4F RT A21EA 2001052200033 20010522 00033 EU 2001 5 22 MALA010446 1 20010509 A 2460 A2043C POWER UNIT SAAB SF340 340B 7860101 EU DC POWER SYS DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 404XJ 340B404 DURING CLIMBOUT ON FLIGHT 2804, THE RT GENERATOR WENT OFF LINE. PERFORMED ORH AND RESET GEN. GEN CAME BACK ON LINE AND STAYED ON LINE FOR APPROXIMATELY 2 MINUTES BEFORE GOING BACK OFF LINE. AIR TURNBACK TO DTW. MAINTENANCE REPLACED RT P DU P/N A2043C, S/N ON CG45018, S/N OFF CH78958. 2 L 7 2 4T RT A52EU 2001052200034 20010522 00034 2001 5 22 SWAA011459 4 20010516 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 601WN 27695 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC S LIDE PER MM. 2 L 7 2 4F RT A16WE 2001052200035 20010522 00035 GL 2001 5 22 ERYA1039 1 20010506 A 2150 5861108 A/C PACK BOMBDR BD700 BD7001A10 1390006 GL A/C BAY SEIZED E ERYA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 07 722HP 1039 ON GROUND WITH APU SUPPLYING BLEED AIR, RIGHT ACU SELECTED ON, SMOKE ENTERED THE CABIN. FOUND RIGHT ACU TURBINE SEIZED. REPLACED ACU TURBINE. 2 L 7 2 4F RT T00003NY 2001052200036 20010522 00036 CE 2001 5 22 C2XA01CL098 1 20010508 A 6120 CONTROLLER BEECH 1900 1900D 1154162 CE NR 2 PROP MALFUNCTIONED A C2XA K NONE O OTHER CL CLIMB 1 SW 27 87555 UE234 CLE FLIGHT 3192 THE CREW REPORTED THE NR 2 PROPELLER CYCLED IN AND OUT OF AUTOFEATHER SEQUENCE AT 1200 AGL. THE AIRCRAF T LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND PERFORMED GROUND PERFORMANCE RUNS AND PERFORM ED AUTO FEATHER TEST. ALL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR TEST FLIGHT AND THE AIRCRAFT TEST FLEW SATIS FACTORY. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT A24CE 2001052200037 20010522 00037 NM 2001 5 22 DHL2001705502 1 20010419 A 5321 FLOOR PANEL BOEING 727 72722C 138400F NM FWD LAVATORY CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C-CHECK, FWD LAVATORY FWD FLOOR PANEL AT FS 303 HAS SEVERAL SPOTS OF CORROSION. REMOVED FWD LAV FLOOR PANEL AT STA 3 03 FOR REPLACEMENT AS PER B727 SRM 51-30-2. MADE NEW FLOOR PANEL MATERIAL USED 2024 T3 (.040) PO 83110438 LOT 220081 MA TERIAL SIZE 30 X 12. TREATED AND PRIMED AREA AS PER B727 SRM 51-10-2 AND 51-40-1. OK TO INSTALL FLOOR PANEL. INSTALLE D FOWARD LAV FLOOR PNL AT FS 303 PER B727 SRM 5130-2 AND SEALED WITH PRC 1422 B1/2 PER B727 SRM 51-20-4. 2 L 7 3 4F A3WE 2001052200038 20010522 00038 NM 2001 5 22 DHL2001705504 1 20010418 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM CABIN DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C-CHECK, SEAT TRACK NR 6 SHOWS PREVIOUS HEAVY BLEND-OUT REWORK AT BS 680 - BS 695 RBL 45. REMOVED AND REPLACED SECTIO N OF SEAT TRACK FROM STA 680 TO STA 695 RBL 45 AS PER B727 SRM 51-10-2. 2 L 7 3 4F A3WE 2001052200039 20010522 00039 NM 2001 5 22 AWXA0001718 1 20010509 A 2782 69734859 ROD END BOEING BOEING 737 737375 13844BN NM SLAT ACTUATOR DAMAGED A AWXA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 WP 28 336AW 0655 23707 PHX - AIR TURNBACK, AT ROTATION THE LEADING EDGE INTRANSIT LIGHT ILLUMINATED AND THEN EXTINGUISHED AS THE CLIMB WAS INIT IATED AND ALL SLATS WERE IN EXTENDED POSITION. WHEN FLAPS WERE RETRACTED A LOUD SOUND WAS HEARD AND THE NR 1 SLAT WAS A T FULL EXTEND WITH OTHER SLATS/FLAPS RETRACTED; THE QRH ASYMMETRICAL L/E SLATS CHECKLIST WAS ACCOMPLISHED & AN UNEVENTFU L LANDING IN PHX WAS ACCOMPLISHED. MAINTENANCE FOUND NR 1 L/E SLAT ACTUATOR ROD END FAILED; IT WAS SPLIT ALLOWING ACTUA TOR TO RETRACT BUT LEAVING SLAT EXTENDED. THE BEARING REMAINED ATTACHED TO SLAT; ACTUATOR WAS REMOVED AND SLAT AND WING LEADING EDGE INSPECTION WAS PERFORMED. SLAT ACTUATOR AND ROD END ASSY WERE REPLACED AND FUNCTIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2001052200040 20010522 00040 NM 2001 5 22 AWXA0001719 1 20010509 A 3230 PIN BOEING 737 737277 1384570 NM NLG INSTALLED A AWXA A UNSCHED LANDING J W WARNING INDICATION INADEQUATE Q C CL CLIMB 1 WP 28 188AW 22655 PHX - AIR TURNBACK, AFTER TAKEOFF WHEN THE LANDING GEAR HANDLE WAS SELECTED UP, THE NOSE GEAR DIDN''T RETRACT AND THE AI RCRAFT RETURNED TO PHX MAKING AN UNEVENTFUL LANDING. UPON ARRIVAL AT THE GATE IT WAS FOUND THAT THE NOSE GEAR DOWNLOCK PIN WAS INSTALLED. THE AIRCRAFT HAD REMAINED OVERNIGHT IN PHX AND THIS WAS THE FIRST FLIGHT OF THE DAY; DURING OVERNIGH T MAINTENANCE THE NOSE GEAR TIRES WERE REPLACED DUE TO WEAR; THE NOSE GEAR PIN WAS DOCUMENTED AS INSTALLED AND REMOVED I N THE AIRCRAFT LOGBOOK. AN INTERNAL INVESTIGATION INTO THE INCIDENT HAS BEEN INITIATED. 2 L 7 2 4F RT A16WE 2001052200041 20010522 00041 NM 2001 5 22 ERKR200100113 1 20010510 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 MAIN CABIN LT SIDE BETWEEN STA 1372 AND STA 1394 S-20L AND S-22L HAS CORROSION AT WINDOW FORGING LOWER AFT CORNER. REMO VED WINDOW FORGING PER 747 SRM 51-30-02. REMOVED CORROSION PER 747 SRM 51-10-01 AND FOUND WINDOW FORGING WITHIN LIMITS PER ECRA 3203-53-047-2. ALODINED WINDOW FORGING PER 747 SRM 51-10-02 AND PRIMED WINDOW FORGING PER SOPM 20-41-02. INST ALLED WINDOW FORGING PER 747 SRM 51-30-02. 2 L 7 4 4F A20WE 2001052200042 20010522 00042 NM 2001 5 22 AWXA0001720 1 20010509 A 5312 65163007 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 BS 178 BLKHD WEB AT LBL 10.3-10.6 WL 218 CRACKED BENEATH ANGLE. CUT OUT DAMAGE TO WEB AND INSTALLED A REPAIR DOUBLER AN D FILLER IAW SRM 53-10-08 PG 287-298. 2 L 7 2 4F RT A16WE 2001052200043 20010522 00043 EU 2001 5 22 C2XA01BT084 1 20010426 A 5330 SKIN AEROSP ATR42 ATR42320 8680930 EU FUSELAGE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14825 170 YUL---CO4370, DURING 4C INSPECTION MAINTENANCE FOUND SKIN DAMAGED ON RT SIDE JUST AFT OF FRAME 23 BETWEEN STRINGER 12 AN D 13 DUE TO DAMAGE FROM REFUELING PANEL. DAMAGE REPAIRED IAW ATR42 SRM 53-00-00 FIGURE 403 WITH 2024-T3--0.063, AND INS TALLED IAW ATR42 SRM 51-25-01. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T RT A53EU 2001052200044 20010522 00044 EU 2001 5 22 C2XA01BT085 1 20010502 A 5311 S5357140120900 FRAME AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14825 170 YUL---DURING 4C INSPECTION MAINTENANCE FOUND IN WINGBOX AREA, LT FAIRING FRAME AT FRAME 29A TO BE CRACKED. REPAIRED FRA ME IAW COX EC 5350-01031. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T RT A53EU 2001052200045 20010522 00045 EU 2001 5 22 C2XA01BT087 1 20010425 A 5410 S5411061920200 CHANNEL AEROSP ATR42 ATR42320 8680930 EU RT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14825 170 YUL---DURING 4C INSPECTION MAINTENANCE FOUND RT LOWER NACELLE IS CRACKED IN LT FORWARD CHANNEL. MAINTENANCE FABRICATED NEW EDGING AND INSTALLED IAW ATR42 SRM 54-12-61 AND ATR42 SRM 51-25-03. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T RT A53EU 2001052200046 20010522 00046 EU 2001 5 22 C2XA01BT088 1 20010502 A 7110 S541105862000 SKIN AEROSP ATR42 ATR42320 8680930 EU LT COWLING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14825 170 YUL---DURING 4C INSPECTION MAINTENANCE FOUND LT TOP COWLING CRACKED IN LT CORNER. MAINTENANCE REPAIRED COWLING BY FABRI CATING EDGING IAW ATR42 SRM 54-12-61 FIGURE 101 AND INSTALLED IAW ATR42 SRM 51-25-01. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T RT A53EU 2001052200047 20010522 00047 EU 2001 5 22 C2XA01BT089 1 20010502 A 7110 S541105862000 CHANNEL AEROSP ATR42 ATR42320 8680930 EU RT COWLING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14825 170 YUL---DURING 4C INSPECTION MAINTENANCE FOUND RT ENGINE TOP COWL TO BE CRACKED IN LT FORWARD CHANNEL. MAINTENANCE REPAIR ED COWLING IAW ATR42 SRM 54-12-61 FIGURE 101. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T RT A53EU 2001052200048 20010522 00048 EU 2001 5 22 C2XA01BT090 1 20010502 A 5210 SKIN AEROSP ATR42 ATR42320 8680930 EU APX DOOR DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14825 170 YUL---DURING 4C INSPECTION MAINTENANCE FOUND PASSENGER DOOR STAIRCASE FORWARD UPPER CORNER TO BE CRACKED. MAINTENANCE R EPAIRED PASSENGER DOOR BY REMOVING DOOR, INNER SKIN REPAIRED IAW ATR42 SRM 52-11-00 FIGURE 412, AFT ATTACH ANGLE FABRICA TED IAW ATR42 SRM 52-11-10, AND STAIRCASE FORWARD UPPER CORNER REPAIRED IAW ATR42 SRM 52-11-00 FIGURE 404, PASSENGER DO OR REINSTALLED IAW ATR42 JIC 52-11-00-RAI 100000-003. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T RT A53EU 2001052200049 20010522 00049 WP 2001 5 22 ABXA010222 1 20010509 A 3260 SOCKET DOUG DC9 DC931 3022065 WP COCKPIT CONTAMINATED A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 924AX 47403 THE NOSE LANDING GEAR DOWN AND LOCKED (GREEN) LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE CREW PERFORMED ABNO RMAL CHECKLIST AND COMPLETED A GEAR RE-CYCLE. MAINTENANCE INSPECTED AND CLEANED DEBRIS FROM THE NOSE LANDING GEAR GREEN LIGHT SOCKET. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001052200050 20010522 00050 WP 2001 5 22 ABXA010221 1 20010508 A 2742 30042502 ACTUATOR DOUG DC8 DC863 302198A WP STABILIZER SEIZED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 84250 45927 THE CREW REPORTED THE STABILIZER HYDRAULIC SYSTEM TO BE INOPERATIVE. THE LEFT SUITCASE HANDLE WAS JAMMED FULL FORWARD. MAINTENANCE INSPECTED AND REPLACED THE LEFT LONGITUDINAL TRIM ACTUATOR IAW DC8 MM. 2 L 7 4 4F 4A25 2001052200051 20010522 00051 WP 2001 5 22 ABXA010220 1 20010508 A 5310 STRUCTURE DOUG DC9 DC941 302207N WP FUSELAGE VIBRATION A ABXA K NONE E VIBRATION/BUFFET AP APPROACH 1 GL 23 967AX 47509 ON FINAL APPROACH WITH FLAPS EXTENDED TO 25 DEGREES, THE AIRCRAFT EXPERIENCED VIBRATIONS AND UNUSUAL NOISE. THE AIRCRAF T CONTINUED THE APPROACH AND LANDED WITH FLAPS AT 25 DEGREES. MAINTENANCE INSPECTED THE FLAPS, FAIRINGS BUTT DOORS, FIX ED AND MOVABLE VANES, SLATS AND LANDING GEAR DOORS. MAINTENANCE CHECKED THE FLAP SYSTEM OPERATION. NO DEFECTS WERE NOT ED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001052200052 20010522 00052 WP 2001 5 22 ABXA010223 1 20010512 A 5320 FITTING DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 CORROSION FOUND ON LONGERON 24 BACK UP FITTING AT STA 879, LEFT MAIN LANDING GEAR WHEEL WELL. FOUND TO BE CRACKED AFTER CORROSION REMOVAL. 2 L 7 4 4F 4A25 2001052200053 20010522 00053 NM 2001 5 22 PCAA0105040 1 20010511 A 3350 2078 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A PCAA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 13 819EX 12697 1562 016 PHL- FLIGHT 3882. CREW REPORTED EMERGENCY LIGHTS WON''T TEST. MAINTENANCE REPLACED FORWARD AND AFT EMERGENCY LIGHT POWE R SUPPLIES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001052200054 20010522 00054 NM 2001 5 22 PCAA0105039 1 20010511 A 3350 RESISTOR DHAV DHC8 DHC8102 2809003 NM POWER SUPPLY BROKEN A PCAA K NONE L NO TEST NR NOT REPORTED 1 EA 13 836EX 297 MDT - DURING ROUTINE MAINTENANCE AFT RIGHT FUSELAGE EMERGENCY LIGHTS FOUND TO BE INOPERATIVE. RESISTOR FOUND BROKEN OFF IN POWER SUPPLY POSITION 600. RESISTOR RESOLDERED, POWER SUPPLY REINSTALLED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURN ED TO SERVICE. 2 H 7 2 4T RT A13NM 2001052200055 20010522 00055 WP 2001 5 22 AT0100127 1 20010326 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE NICKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 837AT 45774 FOUND NICK AT BOTTOM AFT CORNER OF WINDOW FRAME NR 19. BLENDED NICK AT BOTTOM AFT CORNER OF WINDOWN FRAME, FABRICATED R EPAIR DOUBLER AND INSTALLED IAW DC9 SRM 53-05 AND RO 9530053-2003. 2 L 7 2 4F A6WE 2001052200056 20010522 00056 WP 2001 5 22 AT0100128 1 20010327 A 5311 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 837AT 45774 FOUND CRACK IN RIGHT MAIN FRAME AT BS 737. REMOVED AND REPLACED FRAME 737 IAW EO 12-5311-29-B1044. 2 L 7 2 4F A6WE 2001052200057 20010522 00057 WP 2001 5 22 AT0100130 1 20010328 A 5320 STRAP DOUG DC9 DC932 3022066 WP CARGO BAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 837AT 45774 FOUND CORROSION ON AFT PIT LEFT SIDE WALL PANEL DOUBLER STRAP. REMOVED AND REPLACED LEFT SIDE WALL PANEL DOUBLER STRAP. 2 L 7 2 4F A6WE 2001052200058 20010522 00058 WP 2001 5 22 AT0100131 1 20010411 A 7830 CONTROL VALVE DOUG DC9 DC932 3022066 WP THRUST REVERSER GROOVED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 837AT 45774 FOUND GROOVES IN SHAFT OF THRUST REVERSER CONTROL VALVE SECTOR. REPAIRED GROOVED SHAFT OF THRUST REVERSER CONTROL VALVE SECTOR BY MACHINING, FABRICATING AND INSTALLING REPAIR SLEEVE/BUSHING IAW TIMCO REO-L00340. 2 L 7 2 4F A6WE 2001052200059 20010522 00059 EA 2001 5 22 JBXA000280 1 20010510 A 5610 601R330334 WINDOW CNDAIR CL600 CL6002B19 EA COCKPIT CRACKED A JBXA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 05 581ML 7303 RIGHT SIDE WINDSHIELD CRACKED AT 20,000 FT, NO PRESSURIZATION PROBLEMS. REMOVED AND REPLACED COCKPIT RIGHT SIDE WINDOW IAW CL-65 AMM 56-12-01. OPS CHECK GOOD IAW 30-41-01. 2 L 7 2 4F RT A21EA 2001052200060 20010522 00060 EU 2001 5 22 RAIA00105008 1 20010503 A 3610 S2L226 SEAL JETAIR JETSTM JETSTM4101 1500501 EU BLEED AIR SYS FAILED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 569HK 10933 41088 7496-STL-RIGHT DUCT FAIL INDICATION ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE INSPECTED AND DEFERRED PER MEL. MAINTENAN CE REPLACED RIGHT BLEED AIR DUCT SEALS. 2 L 7 2 4T RT A41NM 2001052200061 20010522 00061 EU 2001 5 22 QXEA0100637 1 20010429 A 3260 WARNING LIGHT FOKKER F28 F28MK4000 4990810 EU COCKPIT ILLUMINATED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 482US 11231 FCA - AFTER GEAR RETRACTION, NOSE GEAR UNSAFE LIGHT ILLUMINATED. GEAR WAS CYCLED AS PER CHECK LIST, AT SUCH TIME THE NR 1 HYDRAULIC QUANTITY INDICATED ZERO. AFTER COMPLETING HYDRAULIC FAILURE CHECK LISTS, EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITH EXTENDED ROLL OUT, BUT WITH OUT FURTHER COMPLICATIONS. AIRCRAFT GROUNDED. 2 L 7 2 4F RT A20EU 2001052200062 20010522 00062 EA 2001 5 22 COMA0160369 1 20010514 A 5311 FRAME CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 995CA 7229 LEFT AND RIGHT FS 718 STR 10 AND 11 ARE CRACKED. REPAIRED LEFT AND RIGHT FUSELAGE FRAME STR 10 - 12 AT FS 718.00 IAW CA NADAIR REO 601R-53-61-193. 2 L 7 2 4F RT A21EA 2001052200063 20010522 00063 EA 2001 5 22 COMA0160370 1 20010510 A 5320 6003106819 FLOOR SUPPORT CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 936CA 16506 7043 FLOOR SUPPORT FITTING OUTBOARD OF RBL 9 FS 460 IS CRACKED. REMOVED CRACKED FLOOR SUPPORT FITTING OUTBOARD OF RBL 9 FS 4 60 P/N 600-31068-19 AND REPLACED WITH NEW FITTING P/N 600-31068-19 IAW WVAC EO 601R-53-2431. 2 L 7 2 4F RT A21EA 2001052200064 20010522 00064 EA 2001 5 22 COMA0160371 1 20010513 A 5320 601R3103077 SPLICE PLATE CNDAIR CL600 CL6002B19 EA FUSELAGE MISMANUFACTURED A COMA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 973CA 7146 TWO SPLICE PLATES WERE FABRICATED INCORRECTLY BY THE MANUFACTURER. FABBED TWO DOUBLER PLATES, REWORKED THE SPLICE PLATE AND INSTALLED DOUBLER PLATES AND SPLICE PLATES IAW WVAC EO 601R-53-2448. 2 L 7 2 4F RT A21EA 2001052200065 20010522 00065 SO 2001 5 22 C2XA01CL103 1 20010512 A 3350 LIGHT EMB 145 EMB145ER SO CABIN INOPERATIVE A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 15941 145035 CLE FLIGHT 3690 THE CREW REPORTED THE 4TH AND 5TH SECTION OF EMERGENCY LIGHTS WERE NOT OPERATING. MAINTENANCE INSPECTE D THE EMERGENCY LIGHTS AND RESET THE BATTERY PACK AT SEAT 12A. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2001052200066 20010522 00066 NM 2001 5 22 AWXA0001721 1 20010509 A 5310 6545409245 PRESSURE PANEL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 BS 663.75 LBL 31 PRESSURE WEB CRACKED. CUT OUT DAMAGED AREA; FABBED AND INSTALLED A REPAIR DOUBLER, FILLER AND STIFFENE R IAW ER 03-5702-01116-TB1. 2 L 7 2 4F RT A16WE 2001052200067 20010522 00067 NM 2001 5 22 AWXA0001722 1 20010509 A 5311 654653949 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MAIN CABIN BS 616 AT LBL 63 WL 201 FRAME CRACKED AT FASTENER. REMOVED, FORMED, LOCATED, DRILLED AND INSTALLED REPAIR AN GLES AND STRAPS IAW ER 03-5311-01120-BA1. 2 L 7 2 4F RT A16WE 2001052200068 20010522 00068 WP 2001 5 22 ZW0A0101401 1 20010504 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 924TW 49100 DURING CHECK-C MAINT IN THE MID CARGO COMPT, AT STA 579 AND LONGERON 25L, FOUND FLOOR SUPPORT CRACKED. INSTALLED FASTEN ERS PER SRM 51-30-2. SHOP WELDED PER DPS 10.255 USING TIG WELDING PROCESS WITH AM 4951 WELD ROD. STRESS RELIEVED PER D PS 6.33 PAGE 5. 2 L 7 2 4F A6WE 2001052200069 20010522 00069 WP 2001 5 22 ZW0A0101402 1 20010504 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 924TW 49100 DURING CHECK-C MAINT IN MID CARGO COMPT AT STA 617 AND LONGERON 27L, FOUND FLOOR SUPPORT WITH A CRACK. WELDED PER SSRM 53-00-106 PAGE 201. STRESS RELIEVED PER DACO DPS 6-33. STRESS RELIEVED PER DPS 6.33 PAGE 5. INSTALLED FLOOR SUPPORT P ER SRM 51-30-02. 2 L 7 2 4F A6WE 2001052200070 20010522 00070 WP 2001 5 22 ZW0A0101403 1 20010504 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 924TW 49100 DURING CHECK-C MAINT IN THE MID CARGO COMPT AT STA 579 AND LONGERON 27R, FOUND FLOOR SUPPORT CRACKED. REPAIRED ANGLE PE R SSRM 53-00-106, PAGE 201. STRESS RELIEVED PER DPS 6.33 PAGE 5. INSTALLED FASTENERS PER SRM 51-30-02. 2 L 7 2 4F A6WE 2001052200071 20010522 00071 2001 5 22 KBMA88726 4 20010421 A 3422 200DCL GYRO SNIAS 350 AS350B2 8680813 EU DIRECTIONAL GYRO ERRATIC E KBMA K NONE O OTHER NR NOT REPORTED 1 WP 19 53SH 5106 2009 REPLACED DIRECTIONAL GYRO, NEEDLE WAS ERRATIC. 1 G 7 1 3U H9EU 2001052200072 20010522 00072 WP 2001 5 22 RRXA011038 1 20010419 A 2150 WARNING LIGHT DOUG DC8 DC871F 302199D WP COCKPIT FALSE INDICATION A RRXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 15 996GE 45996 ON T/O BOTH PACK TRIP LIGHTS ON. RESET ALL PACK CB'S ALSO GND RELAY CB'S. ON RETURN TO MSY FLAPS STAYED DOWN, THEN SU DDENLY CAME UP AT THAT TIME, PUSHED RESET BUTTON, PACKS RESET. INSPECTED BOTH PACKS GROUND OPERATED, OPS CHECKS GOOD. INSPECTED FLAPS. GROUND RAN FLAPS UP AND DOWN SEVERAL TIMES. INSPECTED FLAPS LOCKOUTS AND FLUID QTY SYSTEM GROUND CHEC KS GOOD IAW CHAPTER 27-50-2. COULD NOT DUPLICATE PACK TRIPS ON GROUND. GROUND OP CHECKS GOOD IAW CHAPTER 21-55-00. 2 L 7 4 4F RT 4A25 2001052200073 20010522 00073 WP 2001 5 22 RRXA011041 1 20010430 A 2612 899096 FIRE LOOP DOUG DC8 DC871F 302199D WP NR 1 ENGINE FAILED A RRXA E F A ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 15 801GP 46039 ENGINE NR 1 ON TAKEOFF INTERMITTENT FIRE WARNING. AS PER QRH, ENG WAS SHUT DOWN AND FIRE LOOP TESTED. IT DID NOT RESET . DISCHARGED BOTTLE NR 1, WAITED 30 SEC, FIRE LOOP TESTED. IT DID NOT RESET, DISCHARGED BOTTLE NR 2, WAITED 30 SEC, LO OP DID NOT TEST. ALL OTHER INDICATIONS NORMAL. REMOVED AND REPLACED NR 1 ENGINE RT FWD FIRE DET LOOP. PERFORMED ENGIN E RUN-UP IAW EMERY RUN-UP HANDBOOK, NO DEFECTS DURING RUN. PRESET CSD PRIOR TO RUN-UP. 2 L 7 4 4F RT 4A25 2001052200074 20010522 00074 SO 2001 5 22 C2XA01BT092 1 20010512 A 2621 336000575 FIRE BOTTLE EMB 145 EMB145 SO TAIL FAULTY A C2XA K NONE J WARNING INDICATION CR CRUISE 1 SW 27 12957 145080 EWR---CO4148, DURING CRUISE FLIGHT SEGMENT CREW REPORTED FIRE EXT BTL E1-E2 BTL A INOPERATIVE DURING MOST OF CRUISE FLIG HT. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND A FAULTY FIRE BOTTLE A-POSITION. MAINTENANCE REMOVED AND REPLACED THE FIR E BOTTLE IN A-POSITION AND OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2001052200075 20010522 00075 SO 2001 5 22 C2XA01CL104 1 20010512 A 3350 20131A BATTERY EMB 145 EMB145ER SO CABIN DISCHARGED A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 16944 3553 703 145045 CLE FLIGHT 3862 THE CREW REPORTED THE EMERGENCY LIGHTS WOULD NOT STAY ON WHEN ACTIVATED. MAINTENANCE REPLACED THE NR 1, 2, 3, 4 EMERGENCY LIGHT BATTERIES. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.NR 2 S/N 63071 TSN4496/CSN3372/, NR 3 S/N 49851 TSN1719/CSN1557, NR 4 S/N 63662 TSN4246/CSN325, TSO 703. 2 L 7 2 4F RT T00011AT 2001052200076 20010522 00076 NM 2001 5 22 ERKR200100114 1 20010510 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 MAIN DECK RT SIDE FROM STA 1460 TO 1480 BETWEEN S-20R AND S-22R WINDOW FORGING HAS CORROSION UNDER FORGING. REMOVED WIN DOW FORGING PER 747 SRM 51-30-02. REMOVED CORROSION FROM WINDOW FORGING PER 747 SRM 51-10-01 AND FOUND WINDOW FORGING W ITHIN LIMITS PER ECRA 3203-53-047-2. ALODINED WINDOW FORGING PER 747 SRM 51-10-02 AND PRIMED WINDOW FORGING PER SOPM 20 -41-02. INSTALLED WINDOW FORGING PER 747 SRM 51-30-02. 2 L 7 4 4F A20WE 2001052200077 20010522 00077 CE 2001 5 22 C2XA01CL099 1 20010509 A 2913 11438800013 POWERPACK BEECH 1900 1900D 1154162 CE LT WING FAILED A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 27 69549 11126 UE194 CLE FLIGHT 3130 THE CREW REPORTED THE GEAR WOULD NOT EXTEND IN FLIGHT. THE GEAR HAD TO BE EXTENED MANUALLY. THE CREW A LSO REPORTED THE HYDRAULIC POWERPACK CIRCUIT BREAKER DID POP. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT . MAINTENANCE REPLACED THE HYDRAULIC POWER PACK. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT A24CE 2001052200078 20010522 00078 NM 2001 5 22 ERKR200100115 1 20010510 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 MAIN DECK RT FROM STA 1160 TO 1180 AND BETWEEN S-20R AND S-22R WINDOW FORGING HAS CORROSION UNDER FORGING. REMOVED WIND OW FORGING PER 747 SRM 51-30-02. REMOVED CORROSION FROM WINDOW FORGING PER 747 SRM 51-10-01 AND FOUND WINDOW FORGING WI THIN LIMITS PER ECRA 3203-53-047-2. ALODINED WINDOW FORGING PER 747 SRM 51-10-02 AND PRIMED WINDOW FORGING PER SOPM 20- 41-02. INSTALLED WINDOW FORGING PER 747 SRM 51-30-02. 2 L 7 4 4F A20WE 2001052200079 20010522 00079 NM 2001 5 22 ERKR200100116 1 20010510 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 MAIN DECK LT FROM STA 1040 TO 1060 AND BETWEEN S-20L AND S-22L WINDOW FORGING HAS CORROSION UNDER FORGING. REMOVED WIND OW FORGING PER 747 SRM 51-30-02. REMOVED CORROSION FROM WINDOW FORGING PER 747 SRM 51-10-01, AND FOUND WINDOW FORGING T O BE WITHIN LIMITS PER ECRA 3203-53-047-2. ALODINED WINDOW FORGING PER 747 SRM 51-10-02 AND PRIMED WINDOW FORGING PER S OPM 20-41-02. INSTALLED WINDOW FORGING PER 747 SRM 51-30-02. 2 L 7 4 4F A20WE 2001052200080 20010522 00080 NM 2001 5 22 AWXA0001723 1 20010509 A 5311 654653950 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MAIN CABIN BS 616 FRAME AT RBL 63 WL 201 FRAME CRACKED AT FASTENER. REMOVED, FORMED, LOCATED, DRILLED AND INSTALLED REP AIR ANGLES AND STRAPS IAW ER 03-5311-01120-BA1. 2 L 7 2 4F RT A16WE 2001052200081 20010522 00081 NM 2001 5 22 AWXA0001725 1 20010509 A 5240 69698541 FITTING BOEING 737 7373G7 1384595 NM R1 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 R1 DOOR LWR AFT CORNER FITTING CRACKED. REMOVED FITTING, FABED AND INSTALLED REPLACEMENT IAW SRM 51-40-02 PG 2-4 AND BA C DWG 69-69854-1. 2 L 7 2 4F RT A16WE 2001052200082 20010522 00082 NM 2001 5 22 AWXA0001726 1 20010509 A 5315 65468032 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MAIN CABIN BS 520 RBL 45.5 FLOORBEAM CRACKED IN RADIUS OF UPPER CHORD. REPAIRED MAIN CABIN FLOORBEAM IAW EO 53-14-12. 2 L 7 2 4F RT A16WE 2001052200083 20010522 00083 NM 2001 5 22 ERKR200100117 1 20010510 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 MAIN CABIN LT FROM STA 1080 TO 1100 AND BETWEEN S-20L AND S-22L WINDOW FORGING HAS CORROSION UNDER FORGING. REMOVED WIN DOW FORGING PER 747 SRM 51-30-02. REMOVED CORROSION FROM WINDOW FORGING PER 747 SRM 51-10-01, AND FOUND WINDOW FORGING TO BE WITHIN LIMITS PER ECRA 3203-53-047-2. ALODINED WINDOW FORGING PER 747 SRM 51-10-02 AND PRIMED WINDOW FORGING PER SOPM 20-41-02. INSTALLED WINDOW FORGING PER 747 SRM 51-30-02. 2 L 7 4 4F A20WE 2001052200084 20010522 00084 NM 2001 5 22 ERKR200100118 1 20010510 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 WINDOW AT STA 990 LEFT HAS CORROSION ON AND AROUND WINDOW CASTING. REMOVED WINDOW CASTING PER 747 SRM 51-30-02. REMOVE D CORROSION FROM WINDOW CASTING PER 747 SRM 51-10-01, FOUND WINDOW CASTING WITHIN LIMITS PER ECRA 3203-53-047-2. ALODIN ED WINDOW CASTING PER 747 SRM 51-10-02 AND PRIMED WINDOW CASTING PER SOPM 20-41-02. INSTALLED WINDOW CASTING PER 747 SR M 51-30-02. 2 L 7 4 4F A20WE 2001052200085 20010522 00085 SO 2001 5 22 C2XA01CL100 1 20010508 A 3350 LIGHT EMB 145 EMB145ER SO CABIN INOPERATIVE A C2XA K NONE L NO TEST NR NOT REPORTED 1 SW 27 15941 145035 CLE FLIGHT 3722, THE CREW REPORTED THE MIDDLE TWO EMERGENCY LIGHT STRIPS WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED AN D RESET THE EMERGENCY LIGHT SYSTEM. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2001052200086 20010522 00086 SO 2001 5 22 C2XA01CL101 1 20010509 A 3350 SIGN EMB 145 EMB145ER SO CABIN INOPERATIVE A C2XA K NONE L NO TEST NR NOT REPORTED 1 SW 27 14939 145030 CLE FLIGHT 3882, THE CREW REPORTED THE EMERGENCY EXIT SIGN AT THE MAIN CABIN DOOR WAS INOPERATIVE. MAINTENANCE INSPECTE D AND RESEATED THE CANNON PLUG ON THE INVERTER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001052200087 20010522 00087 NM 2001 5 22 011605505 1 20010504 A 2721 233T620121 CONTROL UNIT BOEING 757 757251 1384970 NM COCKPIT INOPERATIVE A NWAA K NONE F FLT CONT AFFECTED CL CLIMB 1 GL 01 505US 23194 DURING CLIMB, THE FIRST OFFICER APPLIED CONTROL INPUTS TO THE RUDDER TRIM. AFTER REMOVING HAND FROM THE TRIM CONTROL KN OB, RUDDER TRIM CONTINUED UNCOMMANDED MOVEMENT TO THE RIGHT. TRIM MOVEMENT STOPPED AFTER COMMANDING LEFT RUDDER TRIM. NO FURTHER PROBLEM NOTED BY FLIGHT CREW. MAINTENANCE REPLACED THE RUDDER TRIM CONTROL MODULE. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A2NM 2001052200088 20010522 00088 NM 2001 5 22 0101615518 1 20010504 A 3260 43467410331214 LIGHT BOEING 757 757251 1384970 NM COCKPIT INOPERATIVE A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 518US 23206 DURING APPROACH, THE RIGHT LANDING GEAR LIGHT DID NOT DISPLAY GREEN. FLIGHT CREW FOLLOWED COM PROCEDURE BUT THE LIGHT S TAYED OUT. EICAS MESSAGE GEAR DISAGREE WAS NOT DISPLAYED. LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR INDICATOR LIGHT ASSEMBLY. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A2NM 2001052200089 20010522 00089 WP 2001 5 22 0101631220 1 20010503 A 2120 SMOKE DOUG DC10 DC1030 3023501 WP CABIN DETECTED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 220NW 46577 AFTER TAKEOFF, FLIGHT ATTENDANTS REPORTED SMELL OF SMOKE IN CABIN AND FLIGHT DECK. TURNED OFF RECIRC FAN BUT SMELL REMA INED WITH SMOKE EVIDENT. FLIGHT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEARED AIRCRAFT OF ALL SMELL S WITH EXTERNAL POWER. ALL SYSTEMS OPERATED NORMALLY. 2 L 7 3 4F A22WE 2001052200090 20010522 00090 NM 2001 5 22 0101642204 1 20010504 A 2923 323636 PUMP BOEING 727 727251 138408H NM HYDRAULIC SYS LEAKING A NWAA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 204US 51203 3056 22544 DURING CRUISE, BOTH HYDRAULIC B-SYSTEM PUMPS LOW PRESSURE LIGHT ILLUMINATED. ALSO VERIFIED ALL B-SYSTEM FLUID DEPLETED. CONTINUED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED 2 B-SYSTEM HYDRAULIC PUMP. LEAK AND OPERATIONAL C HECK OK. 2 L 7 3 4F A3WE 2001052200091 20010522 00091 NM 2001 5 22 0101652287 1 20010505 A 3230 LANDING GEAR BOEING 727 727251 138408H NM NLG MALFUNCTIONED A NWAA K NONE J WARNING INDICATION AP APPROACH 1 GL 01 287US 21375 THE NOSE LANDING GEAR DID NOT EXTEND. THE RED NOSE GEAR LIGHT WAS ILLUMINATED AND NO OTHER WARNING LIGHT ON. CREW MANUA LLY EXTENDED NOSE LANDING GEAR AND MADE AN UNEVENTFUL LANDING. MAINTENANCE LUBED AND ACTUATED NOSE GEAR MULTIPLE TIMES WITH NO DISCREPANCY NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2001052200092 20010522 00092 NM 2001 5 22 0101666612 1 20010504 A 3610 112260A1 CHECK VALVE BOEING 747 747251B 1384892 NM PWA JT9 JT9D7J 52054 NE NR 4 ENGINE FAILED A NWAA O OTHER X ENGINE FLAMEOUT DE DESCENT 1 GL 01 612US 20357 662730 AFTER BEGINNING DESCENT FROM FL300, THE NR 4 ENGINE FLAMED OUT. THE CREW TRIED TO RESTART THE ENGINE PER COM PROCEDURES WITHOUT SUCCESS. THE REMAINDER OF THE DESCENT AND LANDING WERE MADE WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ENGI NE AND FOUND THE 8TH STAGE CHECK VALVE HAD FAILED. THE VALVE WAS REPLACED. RAN ENGINE TO HIGH POWER WITH NORMAL INDICA TIONS. 2 L 7 4 4F 4 F A20WE E20EA 2001052200093 20010522 00093 NM 2001 5 22 ZW0A0101602 1 20010513 A 3350 363674 LIGHT BOEING 757 7572Q8 1384972 NM CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 703TW 27620 THE EGRESS LIGHT WAS INOPERATIVE AT SEAT 1A. REPLACED THE FLEX LAMP ASSY. CHECK-C 4-12-01 LAX. 2 L 7 2 4F RT A2NM 2001052200094 20010522 00094 WP 2001 5 22 ZW0A0101603 1 20010510 A 3350 7732 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 9413T 53188 THE EGRESS LIGHT AT SEAT 8D WAS INOPERATIVE DURING TEST. REPLACED THE LAMP. CHECK-C 12-3-00 JFK. 2 L 7 2 4F RT A6WE 2001052200095 20010522 00095 2001 5 22 SWIA972571 4 20010422 A 2215 SERVO EMB 120 EMB120RT SO PWA 118 PW118 NE AUTOPILOT SYS FAILED A SWIA O OTHER J E F WARNING INDICATION VIBRATION/BUFFET FLT CONT AFFECTED UK UNKNOWN 1 NM 07 130G 120130 CO-PILOT''''S AUTOPILOT SERVO FAILURE, AMBER A ANNUNCIATED, VIBRATION ASSOCIATED WITH FAILURE PRIOR TO SERVO FAILURE. E XECUTED QRW PROCEDURES, VIBRATION REMAINED. REMOVED AND REPLACED AILERON SERVO, IAW MM 22-10-09, OPS CHECK GOOD. P/N 6 22-5734-002, S/N ON 10041, S/N OFF 5234. 2 L 7 2 4T 4 T RT A31SO E20NE 2001052200096 20010522 00096 NM 2001 5 22 0101686635 1 20010504 A 3350 POWER SUPPLY BOEING 747 747227B 1384888 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 635US 21682 DURING LINE CHECK, FOUND ZONE-E EMERGENCY FLOOR PATH LIGHTS INOPERATIVE. REPLACED THE POWER SUPPLY. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2001052200097 20010522 00097 NM 2001 5 22 0101696625 1 20010505 A 2120 UNKNOWN BOEING 747 747251B 1384892 NM CABIN ODOR A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 625US 21707 DURING CRUISE, A SMOKE ODOR WAS NOTICED AROUND DOOR 5L. THE ODOR DISSIPATED AFTER A FEW MINUTES AND THE AIRCRAFT CONTIN UED TO DESTINATION AND LANDED WITHOUT INCIDENT. CHECKED LIGHTS, CABIN ENTERTAINMENT SYSTEM, LAVATORIES, AND ELECTRONIC EQUIPMENT COMPARTMENT WITH NO FAULTS NOTED. 2 L 7 4 4F A20WE 2001052200098 20010522 00098 WP 2001 5 22 0101709923 1 20010502 A 2780 DUCT DOUG DC9 DC932 3022066 WP RT WING BINDING A NWAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 01 927RC 47469 ON APPROACH WHEN SLATS WERE EXTENDED, THE AIRCRAFT ROLLED RIGHT AND SLAT DISAGREEMENT ANNUNCIATOR LIGHT ILLUMINATED. FO LLOWED COM PROCEDURES AND AIRCRAFT MADE A SAFE NO-SLAT LANDING AT RAP. MAINTENANCE REPLACED THE RIGHT WING T-DUCT AND P ERFORMED A FUNCTIONAL CHECK. NO PROBLEMS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001052200099 20010522 00099 WP 2001 5 22 0101719959 1 20010429 A 3350 LIGHT DOUG DC9 DC931 3022065 WP CATWALK INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 919RW 47612 DURING LINE CHECK, FOUND CATWALK EMERGENCY LIGHT INOPERATIVE AT MOST AFT POSITION. MAINTENANCE REPLACED AFT CATWALK EME RGENCY LIGHT ASSEMBLY. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 2001052200100 20010522 00100 NM 2001 5 22 0101736635 1 20010427 A 3350 BATTERY PACK BOEING 747 747227B 1384888 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 635US 21682 DURING LINE CHECK, FOUND E-ZONE EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK N ORMAL. 2 L 7 4 4F A20WE 2001052200101 20010522 00101 NM 2001 5 22 0101746641 1 20010427 A 3350 BATTERY PACK BOEING 747 747212B 1384886 NM CABIN DISCHARGED A NWAA K NONE O OTHER CR CRUISE 1 GL 01 641NW 21941 DURING CRUISE, THE EMERGENCY ESCAPE PATH LIGHTING WENT INTERMITTENTLY ON AND OFF. MAINTENANCE REPLACED D-ZONE BATTERY P ACK AND POWER SUPPLY. OPERATIONAL CHECK NORMAL. P/N 60840017-7 AND 60840053-3. 2 L 7 4 4F A20WE 2001052200102 20010522 00102 NM 2001 5 22 AWXA0001724 1 20010509 A 5240 6551674501 BRACKET BOEING 737 7373G7 1384595 NM R1 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 UPON REMOVAL OF OUTER BRACKET R1 DOOR LWR AFT CORNER FOR ACCESS TO INNER FITTING, FOUND OUTER BRACKET ALSO CRACKED. REM OVED AND REPLACED OUTER BRACKET IAW SRM 51-40-02 PG 10-12. 2 L 7 2 4F RT A16WE 2001052200103 20010522 00103 NM 2001 5 22 0101625502 1 20010506 A 3350 6012113RF POWER SUPPLY BOEING 757 757251 1384970 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 502US 23191 DURING EMERGENCY LIGHT TEST, THE FIRST CLASS LIGHTING BATTERY PACK FAILED. MAINTENANCE REPLACED THE POWER SUPPLY. OPER ATIONAL CHECK NORMAL. 2 L 7 2 4F RT A2NM 2001052200104 20010522 00104 NM 2001 5 22 0101676625 1 20010505 A 2530 WIRE BOEING 747 747251B 1384892 NM GALLEY SHORTED A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 01 625US 21707 DURING FLIGHT, THE NR 2 HOT PLATE SPARKED AND EMITTED SMOKE RESULTING IN TRIPPING OF THE CIRCUIT BREAKER. AIRCRAFT CONT INUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPAIRED CHAFED WIRE. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2001052200105 20010522 00105 WP 2001 5 22 0101729973 1 20010427 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9337 47346 DURING LNE CHECK, FOUND CATWALK EMERGENCY TRACK LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 2001052200106 20010522 00106 EU 2001 5 22 C2XA01IA237 1 20010507 A 5730 S5391007500800 PANEL AEROSP ATR42 ATR42320 8680930 EU WING LOOSE A C2XA O OTHER F E FLT CONT AFFECTED VIBRATION/BUFFET AP APPROACH 1 SW 27 19812 99 CRP - FLIGHT 3352, THE CREW REPORTED THAT ON APPROACH TO CRP EXPERIENCED HEAVY ELEVATOR FLUTTER. THE ACFT LANDED AT IAH WITHOUT INCIDENT. MX INSPECTED THE ACFT AND FOUND THE CENTER FORWARD OVERWING PANEL TO BE LOOSE. MX SECURED THE PANEL , FERRIED THE AIRCRAFT TO IAH WHERE THE PANEL ATTACHMENT HARDWARE WAS REPLACED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. *S/D* ON 5/8/2001, FLIGHT 2917, THE CREW REPORTED THAT UPON DESCENT INTO CRP AT 240KT, THE ACFT EXPERIENC ED STRONG AIRFRAME BUFFETING/VIBRATION. MX INSPECTED THE ACFT AND FOUND THE SAME PANEL TO BE LOOSE. THE PANEL WAS RESE CURED AND THE AIRCRAFT FERRIED TO IAH WHERE THE PANEL WAS REMOVED AND REPLACED. 2 H 7 2 4T RT A53EU 2001052200107 20010522 00107 NM 2001 5 22 01FDEA00337 1 20010508 A 3610 CLAMP BOEING 727 7272S2F 1384O81 NM HEAT EXCHANGER LOOSE A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 216FE 22937 NR 1 ENG FIRE IND ON CLIMBOUT. SHUTDOWN ENG DID NOT FIRE BOTTLE. *S/D* REINSTALLED AIR HEAT EXCHANGER EXHAUST DUCT CL AMP PER MM 36-11-051-4. ALL IND NORMAL, OK FOR SERVICE. 2 L 7 3 4F A3WE 2001052200108 20010522 00108 NM 2001 5 22 01FDEA00340 1 20010508 A 5330 65C25335 SKIN BOEING 727 727225 1384077 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 468FE 21452 BULGING SKIN AROUND FASTENERS BS 352, RBL 13, WL 148. *S/D* REMOVED, REPLACED AND FAB CHORD PER IAW FEDEX SRM 51-30-2 1, 51-10-2, 51-30-5 & 51-10-6. 2 L 7 3 4F A3WE 2001052200110 20010522 00110 WP 2001 5 22 CALA0100452 1 20010509 A 5320 3913359545 WIRE ROPE DOUG DC9 DC982 3022082 WP TAILCONE FRAYED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16894 49393 THE TAIL CONE DID NOT RELEASE WHEN PULLED FROM AFT ENTRANCE DOOR. THE TAIL CONE CABLE WAS FOUND FRAYED. THE CABLE WAS REPLACED AND A TAIL CONE ADJUSTMENT/TEST WAS PERFORMED IAW MM 53-53-00. 2 L 7 2 4F A6WE 2001052200112 20010522 00112 EU 2001 5 22 C2XA01BT083 1 20010502 A 5311 FRAME AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14825 170 YUL---CO4370, DURING 4C INSPECTION, MAINTENANCE FOUND FRAME 25 CRACKED AT HYDRAULIC LINE CUTOUT ON BOTH LT AND RT SIDES. MAINTENANCE REPAIRED DAMAGE IAW COX EC 5310-01185. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T RT A53EU 2001052200113 20010522 00113 EU 2001 5 22 C2XA01BT086 1 20010430 A 5411 S5411061920200 FRAME AEROSP ATR42 ATR42320 8680930 EU LT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14825 170 YUL---DURING 4C INSPECTION MAINTENANCE FOUND LT LOWER NACELLE FORWARD LEFTHAND ATTACHMENT BOLT MISSING. LT NACELLE FRAM E CRACKED AND GUSSET BENT. LT LOWER NACELLE REMOVED, NEW EDGING FABRICATED AND INSTALLED IAW ATR42 SRM 51-12-61 FIGURE 106. LT GUSSET REPAIRED IAW ATR42 SRM 51-24-05. LT LOWER NACELLE REINSTALLED. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T RT A53EU 2001052200114 20010522 00114 WP 2001 5 22 MWEA010748 1 20010513 A 3320 0398030 BALLAST DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A MWEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 31 808ME 48070 AFT FLIGHT ATTENDANT DETECTED A HOT SMELL IN AFT CABIN AREA DURING CLIMBOUT. ODOR DISSIPATED WITHIN TWO MINTUES. INSPE CTED AND CHECKED OPERATION OF AVIONICS COOLING FAN, RECIRCULATING FAN, RADIO RACK FAN AND CARGO HEATERS. RAN APU AND EN GINES WITH BOTH PACKS ON, NO SMELL NOTED. FOUND OVERHEAD LAMP AT ROW 30 NOT FULLY ENGAGED AND BURNT THE END OF THE LAMP . REMOVED AND REPLACED LAMP AND BALLAST. 2 L 7 2 4F A6WE 2001052200115 20010522 00115 2001 5 22 SWIA972558 4 20010508 A 3425 COMPUTER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE E/E BAY OUT OF TOLERANCE A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 288SW 120316 FIRST OFFICERS HDG FLAG AND NR 1 RMI FLAG ON IN CRUISE. RETURNED TO THE FIELD. RE-ORIENTATED BOTH NR 1 AND 2 AHRS SYST EMS IAW 34-00-00. GROUND OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 2001052200116 20010522 00116 2001 5 22 SWAA011412 4 20010511 A 2565 D31354 SLIDE BOEING 737 737317 138447P NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EMER GENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001052200117 20010522 00117 2001 5 22 SWAA011413 4 20010511 A 2565 D31354 SLIDE BOEING 737 737301 1384611 NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED E MERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001052200118 20010522 00118 NM 2001 5 22 01FDEA00304 1 20010427 A 5330 650253371 SKIN BOEING 727 727225 1384077 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 468FE 21452 DENT IN SKIN BETWEEN BS 720A AND 720B BS 17 RT. *S/D* REMOVED, REPLACED AND FAB DOUBLER AND FILLER PER IAW FEDEX SRM 5 3-30-3 FIG 3. 2 L 7 3 4F A3WE 2001052200119 20010522 00119 2001 5 22 SWAA011431 4 20010512 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001052200120 20010522 00120 2001 5 22 SWAA011433 4 20010514 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 620SW 28036 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001052200121 20010522 00121 2001 5 22 SWAA011435 4 20010514 A 2565 65C16820 RETAINER BOEING 737 7373A4 1384585 NM ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER M M. 2 L 7 2 4F RT A16WE 2001052200122 20010522 00122 WP 2001 5 22 AT0100154 1 20010406 A 2170 COALESCER BAG DOUG DC9 DC932 3022066 WP A/C BAY DIRTY A ZZDA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 15 831AT 47674 HOT OILY SMELL NOTED AT 9000 FT. BOTH A/C TEMPS BELOW 25 DEGREES. REPLACED COALESCER BAGS AND SEALS. 2 L 7 2 4F A6WE 2001052200123 20010522 00123 WP 2001 5 22 AT0100155 1 20010513 A 2530 3510005801 COFFEEMAKER DOUG DC9 DC932 3022066 WP GALLEY SHORTED A ZZDA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 15 819AT 47260 SMELLED SMOKE IN FLIGHT DECK. REPLACED SHORTED COFFEEMAKER. 2 L 7 2 4F A6WE 2001052200124 20010522 00124 2001 5 22 SWAA011384 4 20010508 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EMER GENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001052200125 20010522 00125 NM 2001 5 22 SWAA011393 1 20010510 A 3350 10107451 LENS BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 514SW 25153 DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2001052200126 20010522 00126 NM 2001 5 22 SWAA011394 1 20010509 A 2560 P2070004 FLASHLIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 514SW 25153 DURING SCHEDULED D-CHECK, FOUND LOWER EMERGENCY FLASHLIGHT INOP AT AFT CABIN. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2001052200127 20010522 00127 2001 5 22 SWAA011397 4 20010510 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001052200128 20010522 00128 2001 5 22 SWAA011405 4 20010512 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001052200129 20010522 00129 NM 2001 5 22 CALA0100453 1 20010508 A 3234 CONTROL HANDLE BOEING 737 7373T0 1384582 NM COCKPIT LACK OF LUBE A CALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SW 09 17306 23357 WHEN THE LANDING GEAR WAS EXTENDED ON APPROACH TO SAT THE THREE GEAR GREEN LIGHTS AND THREE RED LIGHTS ILLUMINATED. A M ANUAL GEAR EXTENSION WAS PERFORMED DURING A GO-AROUND AND THE GEAR WAS VISUALLY CONFIRMED DOWN AND LOCKED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE GEAR HANDLE BINDING IN THE PULLED OUT POSITION. THE HANDLE WAS LUBRICA TED. THE GEAR HANDLE WAS OPERATED SEVERAL TIMES AND OPERATION CHECKED GOOD. IN ADDITION, THE S78 LANDING GEAR LEVER DO WN SWITCH WAS REPLACED AS A PRECAUTIONARY MEASURE IAW MM 32-61-11, PAGE 401. 2 L 7 2 4F RT A16WE 2001052200130 20010522 00130 NM 2001 5 22 CALA0100454 1 20010510 A 5310 CREASE BEAM BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59630 27534 INSPECTION FOUND A 1 INCH CRACK IN LT CREASE BEAM AT STA 360 - 390. THE CREASE BEAM WAS REMOVED AND REPLACED IAW SRM 51 -40-00. 2 L 7 2 4F RT A16WE 2001052200131 20010522 00131 NE 2001 5 22 NACA20010020 2 20010510 A 8530 356993 EXHAUST VALVE PWA CB3 DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE NR 16 CYLINDER STUCK A NACA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 2907F 667 667 P33688 44636 P33688 FEATHERED THE NR 1 ENGINE AT 0345Z DUE TO NR 16 CYLINDER LT & RT LOW COMPRESSION PATTERN. REPLACED THE NR 16 CYLINDER. (EXHAUST VALVE STUCK OPEN). 2 L 7 4 4R 4 R 6A3 5E8 2001052200132 20010522 00132 NM 2001 5 22 SABA010015 1 20010510 A 3230 LANDING GEAR DHAV DHC8 DHC8102 2809003 NM NLG & MLG MALFUNCTIONED A SABA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 880CC 277 AIRCRAFT 880 ON FLIGHT 5008 FROM CLT TO OAJ. AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED T O CLT AND LANDED WITH NO OTHER PROBLEMS. NO INFLIGHT EMERGENCY WAS DECLARED. WHEN THE AIRCRAFT ARRIVED AT THE GATE THE ALTERNATE GEAR EXTENSION PANEL WAS FOUND OPEN. PANEL WAS CLOSED, SYSTEM OPS CHECKED NORMAL. AIRCRAFT RETURNED TO SERV ICE. 2 H 7 2 4T RT A13NM 2001052200133 20010522 00133 EU 2001 5 22 JBXA000279 1 20010510 A 2133 OUTFLOW VALVE FOKKER F28 F28MK0100 4990807 EU CABIN PRESSURE FAILED A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 110ML 11486 CABIN PRESSURE CONTROL FAULT CAME ON AFTER TAKEOFF, CABIN WOULD NOT PRESSURIZE. PLACED CONTROL SWITCH TO MANUAL CABIN S TILL WOULD NOT PRESSURIZE. RETURNED TO RDU. REMOVED AND REPLACED SECONDARY OUTFLOW VALVE IAW F-100 AMM 21-31-04. PERF ORMED OPERATIONAL TEST OF SYSTEM IAW F-100 AMM 21-31-00, OPERATIONAL TEST GOOD. 2 L 7 2 4F RT 2001052200134 20010522 00134 NM 2001 5 22 ERKR200100102 1 20010509 A 5620 65B041657 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 MAIN CABIN LT SIDE AT STA 1350 TO STA 1372 S-20L AND S-22L HAS CORROSION AT WINDOW FORGING LOWER AFT CORNER. REMOVED MA IN CABIN WINDOW FORGING PER 747 SRM 51-30-02 AND FOUND WINDOW FORGING OUT OF LIMITS PER 747 SRM 56-20-01. REPLACED WIND OW FORGING PER 747 SRM 51-30-02 AND ALODINED PER 747 SRM 51-10-02 AND PRIMED PER 747 SOPM 20-41-02. 2 L 7 4 4F A20WE 2001052200135 20010522 00135 NM 2001 5 22 ERKR200100103 1 20010509 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 WINDOW FORGING BETWEEN STA 1020-1040 HAS CORROSION COMING OUT FROM UNDER THE SEALANT IN MAIN CABIN ON THE RIGHT SIDE. R EMOVED WINDOW FORGING PER 747 SRM 51-30-02, WINDOW FORGING FOUND IT WITHIN LIMITS PER ECRA 3203-53-047-2. INSTALLED WIN DOW FORGING PER 747 SRM 51-30-02 AND SEALED PER 747 SRM 51-10-06. 2 L 7 4 4F A20WE 2001052200136 20010522 00136 CE 2001 5 22 2001560AP006 1 20010507 A 5730 652200473 SKIN CESSNA CESSNA 500 560CESSNA 2076750 CE LT WING CORRODED E I5EA K NONE O OTHER IN INSP/MAINT 1 WP 07 302EJ 1337 0302 LT WING CORROSION UNDER INBD DE-ICE BOOT FOUND DURING SCHEDULED PHASE INSPECTION. CONTACTED CESSNA CITATION ENGINEERING FOR REPAIR SCHEME. DEEPEST CORROSION PIT IS THROUGH .050 SKIN PANEL AFTER ALL CORROSION WAS REMOVED. CESSNA HAS INDIC ATED A SERVICE BULLETIN IS PENDING. THE PROBLEM APPEARS TO STEM FROM MOISTURE ENCROACHMENT UNDER A LOOSE EDGE OF THE DE -ICE BOOT AND BEING TRAPPED UNDER THE BOND-TITE AERODYNAMIC FILLER. RECOMMEND REMOVAL OF BOTH WING LEADING EDGE DE-ICE BOOTS, REMOVAL AND REPAIR OF ANY CORROSION DAMAGE, TREATMENT OF BARE ALUMINUM, AND APPLICATION OF EPOXY PRIMER PRIOR TO INSTALLATION OF BOOTS. 2 L 7 2 4F RT A22CE 2001052200137 20010522 00137 WP 2001 5 22 MWEA010745 1 20010508 A 5310 59114023 RECEPTACLE DOUG DC9 DC932 3022066 WP CABIN DOOR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 EXTERIOR DOOR LATCH RECEPTACLE SHOWS DAMAGE FROM LATCH ON DOOR AND JETWAY MOVEMENT. REPAIRED BY INSTALLING EXTERNAL DOU BLER. 2 L 7 2 4F A6WE 2001052200138 20010522 00138 WP 2001 5 22 MWEA010744 1 20010510 A 7910 OIL CAP DOUG DC9 DC915 3022036 WP PWA JT8 JT8D7B 52053 NE RT ENGINE UNSECURE A MWEA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 GL 31 900ME 45841 6493027B RIGHT ENGINE OIL QUANTITY DROPPED TO 4.5 QUARTS ALL OTHER INDICATIONS NORMAL. MAINTENANCE SERVICED ENGINE OIL AND RESEC URED OIL CAP. 2 L 7 2 4F 4 F A6WE E2EA 2001052200139 20010522 00139 NM 2001 5 22 ERKR200100104 1 20010509 A 5620 WINDOW FRAME BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 SURFACE CORROSION INTERIOR SIDE OF R-4 WINDOW FRAME UPPER AFT CORNER AT STA 230. REMOVED WINDOW FRAME PER 747 SRM 51-20 -02. REMOVED CORROSION FROM WINDOW FRAME, FOUND WINDOW FRAME WITHIN LIMITS PER ECRA 3203-53-047-2. ALODINED PER 747 SR M 51-10-01, PRIMED PER SOPM 20-41-02. INSTALLED WINDOW FRAME PER 747 SRM 51-30-02. 2 L 7 4 4F A20WE 2001052200140 20010522 00140 SO 2001 5 22 C2XA01BT081 1 20010503 A 3350 20131A BATTERY PACK EMB 145 EMB145 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13965 145125 EWR---CREW REPORTED ON FLIGHT 3606 SEVERAL EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EME RGENCY LIGHT BATTERY PACK AND OPS. CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2001052200141 20010522 00141 EU 2001 5 22 C2XA01BT082 1 20010503 A 3260 WARNING LIGHT AEROSP ATR42 ATR42320 8680930 EU COCKPIT ILLUMINATED A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 27 14821 160 EWR---CO3228, CREW REPORTED RT MLG UNLOCK LIGHT CAME ON INFLIGHT. AIRCRAFT LANDED UNEVENTFULLY, MAINTENANCE TROUBLESHOO TING. AIRCRAFT RETURNED TO SERVICE WITH SYSTEM PLACARD IAW MEL. 2 H 7 2 4T RT A53EU 2001052300001 20010523 00001 2001 5 23 20010504CW004 4 20010504 A 3416 WL1605AM2 ALTIMETER BRAERO DH125 BAE125800A 1500285 EU GARRTT TFE731 TFE731* 01518 WP COCKPIT OUT OF TOLERANCE B PJYR K NONE O OTHER IN INSP/MAINT 1 GL 15 800PA NA0438 WHEN CHECKING OUT STANDBY ALTIMETER, FOUND THAT IT WAS 50-60 FEET OUT OF LIMITS. RETURNED TO VENDOR. 2 L 7 2 4F 4 F RT A3EU E6WE 2001052300002 20010523 00002 NE 2001 5 23 20010504CW007 2 20010209 A 7250 500074701 SHAFT DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE LT ENGINE SHEARED W MK1Y A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 EA 33 803NK 16640 48087 709901 AFTER NORMAL TAKEOFF AT WEIGHT OF 124K LBS. WHILE PASSING THROUGH ABOUT 4000 FEET. FELT AND HEARD A THUMP, SLIGHT YAW A ND LOOKED DOWN TO SEE LEFT ENGINE HAD SPOOLED DOWN. NO EVIDENCE OF VIBRATION OR COMPRESSOR STALLING. WE PERFORMED EMER GENCY CHECKLIST FOR ENGINE FAILURE/DAMAGE DECLARED EMERGENCY AND LANDED WITH NORMAL RESULT. LANDED AT APPROX 122K LBS. DURING DISASSEMBLY, FOUND HPT SHAFT SHEARED. 2 L 7 2 4F 4 F A6WE E9NE 2001052300004 20010523 00004 CE 2001 5 23 20010507CW005 1 20010307 A 5753 1011200567 BRACKET BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE FLAPS WORN B TIMR K NONE O OTHER IN INSP/MAINT 1 NM 07 153GA UB34 INSPECTION FOUND ALL FLAP TRACK BRACKETS WORN BEYOND ACCEPTABLE LIMITS. 2 L 7 2 4T 4 T RT A24CE E4EA 2001052300005 20010523 00005 CE 2001 5 23 20010507CW006 1 20010307 A 5753 1011200577 BRACKET BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE FLAPS WORN B TIMR K NONE O OTHER IN INSP/MAINT 1 NM 07 153GA UB34 INSPECTION FOUND ALL FLAP TRACK BRACKETS WORN BEYOND ACCEPTABLE LIMITS. 2 L 7 2 4T 4 T RT A24CE E4EA 2001052300006 20010523 00006 CE 2001 5 23 20010507CW007 1 20010307 A 5320 11443012531 FLOOR SUPPORT BEECH 1900 1900C 1154161 CE FUSELAGE CORRODED B TIMR K NONE O OTHER IN INSP/MAINT 1 NM 07 153GA 30471 UB34 4 FLOOR SUPPORT BRACKETS WERE FOUND WITH SIGNIFICANT CORROSION ON THE TOP SURFACE WHERE THEY ARE IN CONTACT WITH THE HON EYCOMB FLOOR PANEL. 2 L 7 2 4T RT A24CE 2001052300007 20010523 00007 CE 2001 5 23 20010507CW008 1 20010307 A 5320 FLOOR SUPPORT BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE FUSELAGE CORRODED B TIMR K NONE O OTHER IN INSP/MAINT 1 NM 07 153GA 30471 UB34 4 FLOOR SUPPORT BRACKETS WERE FOUND WITH SIGNIFICANT CORROSION ON THE TOP SURFACE WHERE THEY ARE IN CONTACT WITH THE HON EYCOMB FLOOR PANEL. 2 L 7 2 4T 4 T RT A24CE E4EA 2001052300008 20010523 00008 CE 2001 5 23 20010507CW011 1 20010404 A 2711 1011300181 TRIM TAB BEECH 1900 1900C 1154161 CE LT AILERON CORRODED B TIMR K NONE O OTHER IN INSP/MAINT 1 NM 03 172GA UB11 LEFT AILERON TRIM TAB HORN CORRODED. 2 L 7 2 4T RT A24CE 2001052300009 20010523 00009 CE 2001 5 23 20010507CW012 1 20010404 A 2731 101610000197 TRIM TAB BEECH 1900 1900C 1154161 CE LT ELEVATOR CORRODED B TIMR K NONE O OTHER IN INSP/MAINT 1 NM 07 195GA UB65 ELEVATOR TRIM TAB HORN CORRODED 2 L 7 2 4T RT A24CE 2001052300010 20010523 00010 CE 2001 5 23 20010507CW013 1 20010404 A 5510 10162001446 CAP BEECH 1900 1900C 1154161 CE LT STABILIZER CORRODED B TIMR K NONE O OTHER IN INSP/MAINT 1 NM 07 172GA UB11 LOWER CAP LEFT STABILIZER OUTER 6 IS CORRODED. 2 L 7 2 4T RT A24CE 2001052300011 20010523 00011 CE 2001 5 23 20010507CW014 1 20010307 A 5520 1016200113 BRACKET BEECH 1900 1900C 1154161 CE ELEVATOR CORRODED B TIMR K NONE O OTHER IN INSP/MAINT 1 NM 07 153GA UB34 INSPECTION DISCOVERED SIGNIFICANT CORROSION ON 2 RT ELEVATOR HINGE BRACKETS. 2 L 7 2 4T RT A24CE 2001052300012 20010523 00012 CE 2001 5 23 20010507CW015 1 20010307 A 5520 1016200133 BRACKET BEECH 1900 1900C 1154161 CE ELEVATOR CORRODED B TIMR K NONE O OTHER IN INSP/MAINT 1 NM 07 153GA UB34 INSPECTION DISCOVERED SIGNIFICANT CORROSION ON 2 RT ELEVATOR HINGE BRACKETS. 2 L 7 2 4T RT A24CE 2001052300013 20010523 00013 CE 2001 5 23 20010507CW016 1 20010307 A 5210 1144200341 DOOR FRAME BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE ENTRY DOOR CRACKED B TIMR K NONE O OTHER IN INSP/MAINT 1 NM 07 154GA 29861 UB25 DURING INSPECTION A CRACK WAS FOUND IN THE AIR-STAIR DOOR FRAME LOWER AFT AREA. CRACK ORIGINATED AT THE HING PIN RETAIN ER SCREWHOLE AND EXTENDED FORWARD APPROX. 10 INCHES THRU THE HINGE UPPER RIVET ROW. AFTER REMOVING THE HINGE, THE SKIN WAS FOUND CRACKED ALSO. 2 L 7 2 4T 4 T RT A24CE E4EA 2001052300014 20010523 00014 CE 2001 5 23 20010507CW017 1 20010404 A 2721 11463000047 TRIM TAB BEECH 1900 1900C 1154161 CE RUDDER CORRODED B TIMR K NONE O OTHER IN INSP/MAINT 1 NM 07 195GA UB65 RUDDER TAB HORN, CORRODED 2 L 7 2 4T RT A24CE 2001052300015 20010523 00015 EU 2001 5 23 20010507CW018 1 20010403 A 2130 645471038422 VALVE ISRAEL GALAXY GALAXY 4500307 EU CABIN PRESSURE CRACKED D VO2R A UNSCHED LANDING O OTHER CR CRUISE 1 GL 19 622SV 39 015 AT 41,000 FT. AIRCRAFT CABIN PRESSURE TARTED TO DROP. CREW RETURNED FOR MAINTENANCE WITHOUT INCIDENT. FOUND 1 INCH VER TICAL CRACK ON VALVE SEAT OF SAFETY VALVE. 2 L 7 2 4F RT A53NM 2001052300016 20010523 00016 CE 2001 5 23 20010507CW019 1 20010307 A 5313 STRINGER BEECH 1900 1900C 1154161 CE FUSELAGE CORRODED B TIMR K NONE O OTHER IN INSP/MAINT 1 NM 07 153GA 30471 UB34 INSPECTION REVEALED A .6 INCH SECTION OF FUSELAGE STRINGER 14L CORRODED AT APPROX F.S. 250 FUSELAGE SKIN WAS NOT DAMAGED . 2 L 7 2 4T RT A24CE 2001052300018 20010523 00018 CE 2001 5 23 20010508CW012 1 20010508 A 3411 LINE CESSNA 208 208B 2073701 CE PWA PT6 PT6A114 52043 NE PITOT-STATIC SYS MISMARKED D K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 05 4105C 208B0632 WITHIN THE LEFT WING BEHIND PANEL 603BB THE PITOT AND THE STATIC LINES WERE MISLABELED. THE STATIC LINE WAS MARKED PITO T AND THE PITOT LINE WAS MARKED STATIC FROM THE FACTORY. 1 H 7 1 3T 3 T A37CE E4EA 2001052300020 20010523 00020 CE 2001 5 23 20010508CW017 1 20010322 A 3221 5842000211 TRUNNION CESSNA 441 441 2076020 CE NLG WW CRACKED D K NONE O OTHER IN INSP/MAINT 1 NM 03 800AB 7121 4410162 NOSE GEAR TRUNNION INSPECTION/ REPLACEMENT. COMPLIED WITH CQB 00-3 AND FOUND BOTH PIVOT LUGS TO HAVE CRACKS AT THE FILL ETS, REPLACED TRUNNION ASSEMBLY. 1 L 7 2 3T RT A28CE 2001052300021 20010523 00021 GL 2001 5 23 20010508CW018 3 20010418 A 6111 A1590 COUNTERWEIGHT HARTZL PIPER PA23 PA23150 7102303 CE LYC O320 O320A3B 41508 EA HARTZL HCC2Y HCC2YL2 GL LT PROPELLER BROKEN D O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 NM 13 1140P 1059 AY42B 231555 L897827 AY42B DURING TRAINING FLIGHT, LEFT PROPELLER WOULD NOT COME COMPLETELY OUT OF FEATHER. THE ENGINE COULD ONLY DEVELOP 1500 RP M. WHEN THE ENGINE WAS SHUTDOWN ON THE GROUND, THE PROPELLER WENT BACK INTO FEATHER REGARDLESS OF THE PROP CONTROL POSI TION. UPON PROP DISASSEMBLY, ONE OF THE FEATHER LATCH WEIGHTS WAS FOUND BROKEN IN HALF. UNDER EXAMINATION THE METAL IN THE BREAK APPEARS VERY GRANULAR IN NATURE AND UNDER MAGNIFICATION THERE IS RUST IN SOME OF THE VOIDS BETWEEN METAL GRAI NS. 1 L 7 2 3O 3 O RT 1A10 E274 5 C P920 2001052300022 20010523 00022 NE 2001 5 23 SW15200110653 2 20010402 A 7230 30756451 CARBON SEAL AMD FALC10 FALCON10 2730101 EU GARRTT TFE731 TFE73121C NE ENGINE FAILED B O OTHER O OTHER NR NOT REPORTED 1 SW 15 10HE 842 111 73627 THE NR 5 CARBON SEAL COKED AND FAILED CAUSING OIL STARVATION ON THE NR 5 BEARING WHICH SUBSEQUENTLY FAILED. THE CARBON SEAL WAS INSTALLED. 2 L 7 2 4F 4 F A33EU E6WE 2001052300024 20010523 00024 SO 2001 5 23 20010508CW020 1 20010430 A 3232 BRACKET PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA MLG DOOR CRACKED E WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 300ED 317852008 DURING LANDING GEAR INSPECTION DISCOVERED THE FORWARD BRACKET FOR THE RIGHT INNER GEAR DOOR ACTUATOR WAS CRACKED THROUGH THE BOLT HOLE ON THE BEARING SIDE. NOTE: THIS BRACKET HAS A DOUBLER PIECE BEHIND THE STAMPED PIECE WHICH WAS NOT CRAC KED. 1 L 7 2 3O 3 O A20SO E14EA 2001052300025 20010523 00025 CE 2001 5 23 20010509CW001 1 20010412 A 2435 300SGL129Q STARTER GEN CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LEFT FAILED B AC1R O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 351WC 19981 809 5600330 AC WAS CLIMBING TO ALTITUDE, SEVERE CLEAR AIR TURBULENCE WAS ENCOUNTERED. THE LEFT GEN. TRIPPED OFF LINE. THE GEN. WAS RESET AND STAYED ON LINE FOR ABOUT 10 MIN. THEN TRIPPED AGAIN. DECISION WAS MADE TO COMPELTE TRIP WITH ONE GEN. WHEN LOWER COWLING WAS REMOVED, SMALL PIECES OF STARTER BRUSH LAYING IN THE BOTTOM. THE BRUSH COVER WAS REMOVED AND SEVERA L PIGTAIL RETAINING RIVETS AND PIECES OF BRUSH ALSO CAME OUT. ONE BRUSH WAS MOSTLY GONE. SEVERAL PIGTAILS HAD SIGNS OF MELTING AND SEPARATING FROM THE BRUSH. REMAINING BRUSHES INDICATED THERE WAS STILL WEAR LEFT TO GO TO OVERHAUL. ARMA TURE WOULD TURN BY HAND, EVEN WITH SPRING TENSION ON BRUSHES. INSTALLED OH STARTER, OPS CK OK. 2 L 7 2 4F 4 F RT A22CE E25EA 2001080600123 20010806 00123 WP 2001 8 6 RRXA011034 1 20010414 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DISCOVERED CORROSION UNDER THE LAVATORY WHEN PERFORMING FCD A53-4, INSP OF LOWER FUSELAGE. *S/D* REMOVED CORRODED L36 E ND FITTING I/A/W DC-8 SRM 51-1-21. TREATED, PRIMED & INSTALLED NEW L36 END FITTING I/A/W DC-8 SRM 51-1-8 & 51-1-20D. 2 L 7 4 4F RT 4A25 2001052300026 20010523 00026 WP 2001 5 23 RRXA011036 1 20010418 A 5330 SKIN DOUG DC10 DC1010F 3022111 WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 68042 46901 ON WALKAROUND FOUND CORROSION ON UNDER SIDE OF FUSELAGE, LOCATED APPROX 18 INCHES LEFT OF CENTER ACCESSORY COMPARTMENT ACCESS DOOR. REPAIRED DAMAGED AREA PER EWA EO M0419011 & MO420011, NOTE: THIS REPAIR IS A CLASS III TEMPORARY TYPE WITH VISUAL INSP EVERY 1,000 CYCLES & A LIFE LIMIT OF 5,000 CYCLES. 2 L 7 3 4F A22WE 2001052300027 20010523 00027 2001 5 23 RRXA011037 4 20010418 A 3416 D4034110246 ALTIMETER DOUG DC8 DC871F 302199D WP COCKPIT DEFECTIVE A RRXA A UNSCHED LANDING I FLT. ATTITUDE INST. CL CLIMB 1 WP 15 500MH 45812 F/O''S ALTIMETER STICKS AT 700 TO THOUSANDS OF FEET PER CLIMBOUT AND LEVEL FLIGHT. ON LANDING ALTIMETER STUCK AT 43,000 FT. VSI STUCK AT 1000 FPM DESCENT. RII ISOLATED STATIC LEAK TO F/O''S STATIC MANIFOLD. TIGHTENED ALL STATIC LINES A ND FITTINGS AT F/O''S STATIC MANIFOLD. REMOVED AND REPLACED CAPT''S ALTIMETER, ERROR CORRECTOR AND VSI. F/O''S PITOT STATIC SYSTEM, OPS CKD NORMAL IAW DC-8 MM 41-12-12-41. 2 L 7 4 4F RT 4A25 2001052300028 20010523 00028 WP 2001 5 23 RRXA011039 1 20010424 A 3260 806125 PROXIMITY SENSOR DOUG DC10 DC1010F 3022111 WP LT MLG MALFUNCTIONED A RRXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 15 68042 46901 LEFT LANDING GEAR RED LIGHT ON WITH GEAR HANDLE UP. REMOVED AND REPLACED PROXIMITY BOX IAW M/M 32-61-01. OPS CKS NORMA L. 2 L 7 3 4F A22WE 2001052300029 20010523 00029 WP 2001 5 23 RRXA011040 1 20010426 A 3230 47767085503 RESTRICTOR VALVE DOUG DC8 DC871F 302199D WP LT MLG FAILED A RRXA O OTHER J WARNING INDICATION LD LANDING 1 WP 15 8076U 45941 ON/BEFORE LANDING, WITH LANDING GEAR HANDLE PLACED DOWN, DOORS WARNING LIGHT ON, LANDING GEAR UNSAFE LT MLG GREEN LIGHT NOT ILLUM. ALT DOOR LT LIGHT ON LT GEAR WOULD NOT EXTEND. RAN EMERGENCY CHECKLIST AND PERFORMED EMERGENCY LEFT GEAR UP LANDING. REMOVED AND REPLACED LEFT MLG RETRACT ACTUATOR RESTRICTOR VALVE IAW DC-8 MM 32-31-19 REF W/O 1746 TASK 14637 AND LG PG 9865-18 FOR DETAILS AND PARTS CERTIFICATION, OPS CKS GOOD DURING GEAR SWING IAW DC-8 MM 32-30-00 REF 109 PAGE 9865-21 FOR GEAR SWING. 2 L 7 4 4F RT 4A25 2001052300030 20010523 00030 WP 2001 5 23 RRXA011044 1 20010508 A 3246 9550328 WHEEL DOUG DC8 DC871F 302199D WP NLG VIBRATION A RRXA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 15 8085U 45975 AT ROTATION NOSE GEAR VIBRATION FELT AND METALLIC SOUND HEARD. REMOVED AND REPLACED LEFT AND RIGHT NOSE WHEEL ASSY IAW DC8 MM 32-41-10. OPS CHECKS GOOD. 2 L 7 4 4F RT 4A25 2001052300032 20010523 00032 2001 5 23 SWIA972568 4 20010511 A 3422 FLUX DETECTOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE WING MALFUNCTIONED A SWIA A UNSCHED LANDING I FLT. ATTITUDE INST. CR CRUISE 1 NM 07 562SW 120336 YELLOW HEADING FLAG BOTH SIDES, RED HEADING FLAG FIRST OFFICER''S SIDE. BOTH DG''S OFF OF MAG COMPASS 35 DEGREES. RED FLAGS BOTH RMIS. GYRO SLAVING ON CAPTAINS SIDE PEGGED NEG (-), GYRO SLAVING ON F/O SIDE PEGGED POS (+). DIVERTED TO FA T. FOUND AIRCRAFT HAD NUMEROUS LIGHTNING STRIKES. COMPLIED WITH LIGHTNING STRIKE INSPECTION. REPLACED NR 2 FLUX DETEC TOR, P/N 622-5812-004, S/N ON 25412, OFF 20021. REPLACED NR 1 AHRS P/N 622-6190-204, S/N ON 2926, OFF 1894. PERFORMED COMPASS SWING. BOTH AHRS SYSTEMS OP CHECKED GOOD IAW AMM 34-21-00 PG 501. 2 L 7 2 4T 4 T RT A31SO E20NE 2001052300033 20010523 00033 SO 2001 5 23 C2XA01IA243 1 20010511 A 2120 UNKNOWN EMB 145 EMB145ER 3260211 SO CABIN ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 27 14943 145040 IAH - FLIGHT 3936, THE CREW REPORTED A STRONG EXHAUST ODOR IN THE CABIN AND COCKPIT AFTER STARTING THE APU IN FLIGHT. T HE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MX PLACED THE APU ON MEL. AIRCRAFT RETURNED TO IAH ON FLIGHT 4129 WHER E MAINTENANCE PERFORMED OPERATIONAL CHECKS ON THE APU AND PAX SYSTEMS WITH NO DEFECTS NOTED. AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. DISCREPANCY REPEATED ON 04/12/01. MAINTENANCE AGAIN PERFORMED OPERATIONAL CHECKS ON THE AFFECT ED SYSTEMS WITH NO DEFECTS NOTED. AIRCRAFT WAS AGAIN APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001052300034 20010523 00034 NM 2001 5 23 01FDEA00341 1 20010512 A 3260 656021132 ACCESSORY UNIT BOEING 727 727227 1384078 NM E&E BAY FALSE ACTIVATION A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 488FE 21491 RIGHT GEAR UNSAFE LIGHT CAME ON WITH GEAR HANDLE IN OFF POS. REMOVED AND REPLACED LAND GEAR ASSY UNIT PER MM 32-09-121. SYS TEST GOOD. 2 L 7 3 4F A3WE 2001052300035 20010523 00035 CE 2001 5 23 GLBA2001100 1 20010513 A 7331 1303800101 INDICATOR BEECH 1900 1900D 1154162 CE COCKPIT DEFECTIVE A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 118UX 9708 UE118 LEFT FUEL FLOW INDICATOR WENT FULL SCALE, REPLACED FUEL FLOW GAUGE OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001052300036 20010523 00036 CE 2001 5 23 20010523SG001 1 20010314 A 2730 TORQUE TUBE BEECH 1900 1900D 1154162 CE ELEVATOR LOOSE A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 44666 UE405 DURING SCHEDULED INSPECTION, FOUND LEFT ELEVATOR TORQUE TUBE ALL 8 RIVETS LOOSE AND SMOKING. THE RESULTS OF THESE LOOSE RIVETS CAUSES EXCESSIVE FREE PLAY OF THE ELEVATOR ASSEMBLE AND CAN CREATE ELEVATOR FLUDDER IN FLIGHT. (M) 2 L 7 2 4T RT A24CE 2001052300037 20010523 00037 CE 2001 5 23 20010523SG002 1 20010324 A 2730 1016100197 TORQUE TUBE BEECH 1900 1900D 1154162 CE ELEVATOR LOOSE A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 841CA UE40 DURING SCHEDULED INSPECTINO, DISCOVERED ELEVATORS WITH EXCESSIVE FREE PLAY. THIS CONDITION WAS THE RESULT OF LOOSE RIVE TS ON ELEVATOR TORQUE TUBES ON BOTH LEFT AND RIGHT ELEVATORS. INSPECTION OF CONTROL SYSTEM DID NOT UNCOVER ANY OTHER DE FECTS. UNITS REPLACED WITH NEW. (M) 2 L 7 2 4T RT A24CE 2001052300038 20010523 00038 SO 2001 5 23 C2XA01BT093 1 20010514 A 2611 FAU751A4 SMOKE DETECTOR EMB 145 EMB145LR SO LAVATORY FAULTY A C2XA O OTHER N FALSE WARNING DE DESCENT 1 SW 27 13995 145295 EWR---CO4009, CREW REPORTED ON DESCENT INTO EWR, LAV SMOKE INDICATION (CAME ON), NO VISUAL INDICATION OF FIRE OR SMOKE. MAINTENANCE REMOVED AND REPLACED SMOKE DETECTOR PANEL IAW EMB145 MM 26-14-02. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2001052300039 20010523 00039 WP 2001 5 23 01FDEA00351 1 20010511 A 3260 PROXIMITY SENSOR DOUG DC10 DC1010F 3022111 WP LT MLG FAULTY A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 054FE 47808 AFT T/O WITH GEAR HANDLE UP RED LIGHT ILLUM ON S/O GEAR IND PNL FOR THE LEFT GEAR. RAN RED TABS. REMOVED AND REPLACED PROX BOX, LT DOWNLOCK SENSORS, LT MLG DOOR LATCHED SENSOR. SPLICED WIRING PER IAW SMP. GEAR SWING PER IAW DC10 MM 32-1 0-00-5 AND GEAR IND OPS CK PER 32-60-00-5. OPS CHECK GOOD. 2 L 7 3 4F A22WE 2001052300040 20010523 00040 EU 2001 5 23 C2XA01CL105 1 20010513 A 2910 NTA152506 O-RING AEROSP ATR42 ATR42320 8680930 EU HYDRAULIC SYS DAMAGED A C2XA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 27 17831 185 CLE FLIGHT 3812 THE CREW REPORTED THE GREEN AND BLUE HYDRAULIC LOW LEVEL WARNING CAME ON INFLIGHT. THE CREW DECLARED A EMERGENCY AND LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND A O-RING LEAKING ON A UNIO N ON THE BLUE SYSTEM HYDRAULIC FILTER. THE O-RING WAS REPLACED AND THE SYSTEM WAS SERVICED AND PRESSURE CHECKED. THE A IRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A53EU 2001052300041 20010523 00041 NM 2001 5 23 ZW0A0101701 1 20010514 A 3350 8039251 POWER SUPPLY BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 2417F 55084 THE CEILING EMERGENCY LIGHTS FROM CABIN ROW 11 TO 17 WERE INOPERATIVE. REPLACED THE POWER SUPPLY. NO CHECK-C. 2 L 7 2 4F TR A6WE 2001052300042 20010523 00042 NM 2001 5 23 AWXA0001727 1 20010514 A 2782 65C3805810 ACTUATOR BOEING 737 73733A 1384673 NM NR 1 SLAT FAILED A AWXA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 28 169AW 44960 111 23630 PHX - AIR TURNBACK, AFTER TAKEOFF THE FLAPS WERE RETRACTED BUT L/E FLAPS TRANSIT LIGHT ON FORWARD PANEL AND NR 1 SLAT IN DICATOR ON THE OVERHEAD PANEL REMAINED ILLUMINATED. FLAPS WERE CYCLED BACK TO 1 & THEN UP SEVERAL TIMES. PILOT VISUALL Y CONFIRMED THAT NR 1 SLAT WAS STILL EXTENDED APPROX 1.5 INCH; THIS WAS THE CASE ON EACH TRY. THE AIRCRAFT RETURNED TO PHX MAKING AN UNEVENTFUL LANDING. IN PHX MAINTENANCE TROUBLESHOT AND CONFIRMED THE SLAT ACTUATOR WOULDN''''T FULLY RETR ACT. THE NR 1 ACTUATOR WAS REPLACED AND ALL FUNCTIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2001052300043 20010523 00043 2001 5 23 MWEA010747 4 20010514 A 3420 1428300000 GYRO DOUG DC9 DC981 3022081 WP COCKPIT FAILED A MWEA A UNSCHED LANDING I FLT. ATTITUDE INST. CL CLIMB 1 GL 31 804ME 48030 AFTER TAKEOFF, FIRST OFFICERS PFD LOST SKY/GROUND. NUMBER TWO COMPASS FROZE AND NUMEROUS FMA ANNUNCIATORS APPEARED. RE MOVED AND REPLACED NUMBER TWO LITTON GYRO. SYSTEM OPERATIONS CHECKS GOOD. 2 L 7 2 4F A6WE 2001052300044 20010523 00044 NM 2001 5 23 AWXA0001738 1 20010514 A 5320 THRESHOLD BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 R2 DOOR THRESHOLD HAS CORROSION FROM STA 992-967 UNDERNEATH THRESHOLD. REMOVED AND REPLACED R2 DOOR THRESHOLD INNER CHO RD THAT WAS FOUND OUT OF LIMITS IAW SRM 51-40-2. 2 L 7 2 4F RT A16WE 2001052300045 20010523 00045 EA 2001 5 23 COMA0160377 1 20010511 A 2751 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT ACTIVATED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 805CA 7354 DURING APPROACH INTO CKB FLAP FAIL MESSAGE APPEARED AFTER SELECTING 20 DEGREES. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3, (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER F LAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2001052300046 20010523 00046 SO 2001 5 23 SWIA972569 1 20010514 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE T/E FLAP FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 190SW 120050 FLAP CONTROL FAULT INTERMITTENT IN FLIGHT. TROUBLESHOT SYSTEM IAW EMB FAULT ISOLATION MANUAL 27-50-00. FOUND RIGHT OUT BOARD FLAP ACTUATOR BAD. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR IAW EMB MM 27-50-09 AND RII 27-307. SYSTEM OPS CHECK GOOD. P/N: 320300-1007, S/N ON: 1212, S/N OFF: 0026A. 2 L 7 2 4T 4 T RT A31SO E20NE 2001052300047 20010523 00047 EU 2001 5 23 KBMA88725 1 20010407 A 6710 350A76100920 PIVOT SUPPORT SNIAS 350 AS350B2 8680813 EU CYCLIC BROKEN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 53SH 5069 2009 BROKEN AT THE BASE OF SUPPORT (PLASTIC). 1 G 7 1 3U H9EU 2001052300048 20010523 00048 EU 2001 5 23 C2XA01CL106 1 20010514 A 3233 D228970003 ACTUATOR AEROSP ATR42 ATR42320 8680930 EU LT MLG UNSERVICEABLE A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 14828 24125 179 CLE FLIGHT 3191 THE CREW REPORTED THE LEFT GEAR UNLOCK LIGHT ILLUMINATED WITH GEAR HANDLE UP. THE WARNING EXTINGUISHED AFTER A FEW MINUTES. MAINTENANCE INSPECTED AND FOUND THE LEFT GEAR WAS RETRACTING SLOWER THAN MAINTENANCE MANUAL LIMITS . THE LEFT GEAR ACTUATOR WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. THE PSEU WAS ALSO REPLACED FOR PRECAUTIONARY R EASONS. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A53EU 2001052300049 20010523 00049 EU 2001 5 23 MALA010447 1 20010509 A 2730 CONTROL CABLE SAAB SF340 SF340A 7850100 EU ELEVATOR WORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 102XJ 340A102 DURING 4K INSPECTION LT I/B FWD ELEVATOR CABLE WAS WORN. MAINTENANCE REPLACED CABLE. 2 L 7 2 4T RT A52EU 2001052300050 20010523 00050 EU 2001 5 23 MALA010448 1 20010509 A 2720 CONTROL CABLE SAAB SF340 SF340A 7850100 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 102XJ 340A102 DURING 4K INSPECTION LT O/B RUDDER CABLE IN CIRCUIT I IS CHAFED. MAINTENANCE REPLACED LT O/B RUDDER CABLE IAW SF340AMM 27-21-25. SEE 409 NR 125261 FOR RIGGING. 2 L 7 2 4T RT A52EU 2001052300051 20010523 00051 EU 2001 5 23 SIMA200109913 1 20010409 A 2520 D2121F104 SEAT SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 SBP - FOUND SEAT 6BC IS CORRODED. REMOVED AND REPLACED SEAT ASSEMBLY IAW EO G1-2500-093-R5 PART 1. (M) 2 L 7 2 4T RT A52EU 2001052300052 20010523 00052 EU 2001 5 23 SIMA200109914 1 20010409 A 2520 D1121F10537A SEAT SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 SBP - FOUND SEAT 7A IS CORRODED. REMOVED AND REPLACED SEAT ASSEMBLY IAW EO G1-2500-093-R5. (M) 2 L 7 2 4T RT A52EU 2001052300053 20010523 00053 EU 2001 5 23 SIMA200109915 1 20010409 A 2520 D2121F10637A SEAT SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 SBP - FOUND SEAT 7BC CORRODED. REMOVED AND REPLACED SEAT ASSEMBLY IAW EO G1-2500-0093-R5 PART 1. (M) 2 L 7 2 4T RT A52EU 2001052300054 20010523 00054 EU 2001 5 23 SIMA200109916 1 20010409 A 2520 D1121F10337A SEAT SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 SBP - FOUND SEAT 11A IS CORRODED. REMOVED AND REPLACED SEAT ASSEMBLY IAW EO G1-2500-093-R5 PART 1. (M) 2 L 7 2 4T RT A52EU 2001052300055 20010523 00055 EU 2001 5 23 SIMA200109917 1 20010409 A 2520 D2121F10437A SEAT SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 SBP - FOUND SEAT 10BC IS CORRODED. REMOVED AND REPLACED SEAT ASSEMBLY IAW EO G1-2500-093-R5 PART 1. (M) 2 L 7 2 4T RT A52EU 2001052300056 20010523 00056 EU 2001 5 23 SIMA200109918 1 20010409 A 2520 D1121F10737 SEAT SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 SBP - FOUND SEAT 8A IS CORRODED. REMOVED AND REPLACED SEAT ASSEMBLY IAW EO G1-2500-093-R5 PART 1. (M) 2 L 7 2 4T RT A52EU 2001052300057 20010523 00057 EU 2001 5 23 SIMA200109919 1 20010409 A 2520 D2121F108R SEAT SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 FOUND SEAT 8BC IS CORRODED. REMOVED AND REPLACED SEAT ASSEMBLY IAW EO G1-2500-093-R5 PART 1. (M) 2 L 7 2 4T RT A52EU 2001052300058 20010523 00058 EU 2001 5 23 SIMA200109920 1 20010409 A 2520 D1121F10337A SEAT SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 SBP - FOUND SEAT 9A IS CORRODED. REMOVED AND REPLACED SEAT ASSEMBLY IAW EO G1-2500-093-R5 PART 1. (M) 2 L 7 2 4T RT A52EU 2001052300059 20010523 00059 EU 2001 5 23 SIMA200109921 1 20010409 A 2520 D2121F10437 SEAT SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 SBP - FOUND SEAT 9BC IS CORRODED. REMOVED AND REPLACED SEAT ASSEMBLY IAW EO G1-2500-093-R5 PART 1. (M) 2 L 7 2 4T RT A52EU 2001052300060 20010523 00060 EU 2001 5 23 SIMA200109922 1 20010409 A 2520 D1121F10337A SEAT SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 SBP - FOUND SEAT 10A IS CORRODED. REMOVED AND REPLACED SEAT ASSEMBLY IAW EO G1-2500-093-R5 PART 1. (M) 2 L 7 2 4T RT A52EU 2001052300061 20010523 00061 EU 2001 5 23 SIMA200109923 1 20010409 A 2520 D2121F10437A SEAT SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 SBP - FOUND SEAT 11BC IS CORRODED. REMOVED AND REPLACED SEAT ASSEMBLY IAW EO G1-2500-093-R5 PART 1. (M) 2 L 7 2 4T RT A52EU 2001052300062 20010523 00062 EU 2001 5 23 SIMA200109924 1 20010409 A 2520 D1121F10337 SEAT SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 SBP - FOUND SEAT 12A IS CORRODED. REMOVED AND REPLACED SEAT ASSEMBLY IAW EO G1-2500-093-R5 PART 1. (M) 2 L 7 2 4T RT A52EU 2001052300063 20010523 00063 EU 2001 5 23 SIMA200109925 1 20010409 A 2520 D2121F10437A SEAT SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 SBP - FOUND SEAT 12BC IS CORRODED. REMOVED AND REPLACED SEAT ASSEMBLY IAW EO G1-2500-093-R5 PART 1. (M) 2 L 7 2 4T RT A52EU 2001052300064 20010523 00064 EU 2001 5 23 SIMA200109926 1 20010409 A 2520 D4121F10137 SEAT SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 SBP - FOUND SEAT 14AD AND BC ARE CORRODED. REMOVED AND REPLACED SEAT ASSEMBLY IAW EO G1-2500-093-R5 PART 1. (M) 2 L 7 2 4T RT A52EU 2001052300065 20010523 00065 WP 2001 5 23 AALA016043 1 20010410 A 4950 3812761 APU DOUG DC9 DC983 3022083 WP APU BAY CONTAMINATED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 882RA 49949 LAX - AFTER LANDING STARTING APU CABIN FILLED WITH SMOKE, LIGHT IN COLOER AND NOT HEAVY. REPLACED SOCKS. OLD SOCKS WER E DAMP, NOT WET. INSTALLED TES9220 AND TES9338. REQS BURN OUT OF LT PACKS AND REPLACEMENT OF SOCKS AFTER BURN OUT SEE MM 21-20-02. PERFORMED PACK BUR PER MM WITH ENGINES ONLY. NO SMOKE PRESENT. WITH APU AIR, HEAVY SMOKE. BELIEVE FLUID IN APU LINES, REQUIRES FURTHER TROUBLE SHOOTING. NEED TO PLACARD APU INOPERATIVE. APU IS CONTAMINATED, OTHERWISE OPS CHECK OK. OK FOR SERVICE. (M) 2 L 7 2 4F RT A6WE 2001052300066 20010523 00066 NM 2001 5 23 BJNA010401 1 20010413 A 3350 3114981 LIGHT BOEING 737 737214 138446R NM EXTERIOR INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 457TM 20156 FOUND RIGHT LOWER EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY PER BMM 33-51-21. OPS CHEC K NORMAL. (M) 2 L 7 2 4F A16WE 2001052300067 20010523 00067 EU 2001 5 23 REXA01007 1 20010424 A 7997 WIRE SAAB SF340 SF340A 7850100 EU OIL PRESSURE BROKEN A E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 404BH 340A061 DURING CLIMB-OUT FROM FT SMITH, ARKANSAS, THE MASTER WARNING AND LEFT ENGINE OIL PRESSURE WARNINGS ILLUMINATED. THE LEF T PROPELLER GEARBOX OIL PRESSURE INDICATOR SHOWED LARGE FLUCTUATIONS (0-75 PSI). THE FLIGHT CREW FOLLOWED THE EMERGENCY CHECKLIST AND SHUT DOWN THE ENGINE. DECLARED AN EMERGENCY THROUGH RAZORBACK APPROACH AND RETURNED TO FT SMITH SINGLE E NGINE. THE LANDING WAS UNEVENTFUL AND THERE WERE NO INJURIES. MX FOUND AND REPAIED A BROKEN WIRE MID-SPAN BETWEEN THE PROPELLER GEARBOX OIL PRESSURE TRANSDUCER AND THE LEFT ENGINE FIREWALL CANNON PLUG. (M) 2 L 7 2 4T RT A52EU 2001052300068 20010523 00068 EU 2001 5 23 FJT01046431 1 20010427 A 5610 1379377C406 WINDSHIELD BAG JETSTM JETSTM3101 1500215 EU COCKPIT CRACKED A FJTA K NONE O OTHER CR CRUISE 1 SO 03 643JX 643 RDU - CREW REPORTED IN CRUISE FLIGHT AT 17,000 FEET WITH WINDSHIELD HEAT ON, A BRIGHT FLASH WAS OBSERVED FROM THE RIGHT WINDSHIELD FOLLOWED BY A LOUD POPPING SOUND. IT WAS OBSERVED THAT THE RIGHT OUTER PANE OF THE WINDSHIELD CRACKED IN THE SPIDER WEB PATTERN. THE AIRCRAFT MADE UNEVENTFUL LANDING IN RDU. UPON INVESTIGATION THE BROKEN WINDSHIELD, IT WS DETE RMINED THERE WERE BURN MARKS BETWEEN THE PANE OF IN THE AREA OF TEMP SENSORS. THE WINDSHIELD WAS REPLACED WITH A NEW UN IT; A FULL FUNCTIONAL TEST OF THE WINDSHIELD HEAT SYSTEM WAS ACCOMPLISHED WITH NO OTHER DEFECTS NOTED. (M) 2 L 7 2 4T RT A21EU 2001052300069 20010523 00069 EA 2001 5 23 ASOA1034 1 20010405 A 2611 473052 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA CARGO BAY MALFUNCTIONED A ASOA K NONE N FALSE WARNING AP APPROACH 1 SO 11 824AS 7203 FLT 4693 - DURING APPROACH INTO MYR FROM ATL, CREW HAD A CARGO SMOKE INDICATION LIGHT. CAPTAIN DECLARED AN EMERGENCY, B UT FIRE BOTTLES WERE NOT BLOWN. MAINTENANCE FOUND NO INDICATION OF CARGO FIRE. MAINTENANCE REMOVED AND REPLACED THE CA RGO SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001052300070 20010523 00070 EA 2001 5 23 ASOA01036 1 20010412 A 2611 473052 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA CARGO BAY MALFUNCTIONED A ASOA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 11 840AS 54 7290 FLT 4473 - DURING FLIGHT FROM HPN TO ATL, CREW RECEIVED A CARGO COMPARTMENT SMOKE WARNING THAT WOULD NOT EXTINGUISH. CA PTAIN DISCHARGED THE FIRE BOTTLES. CREW DIVERTED TO JFK AND LANDED SAFELY. MAINTENANCE AND THE FIRE DEPARTMENT FOUND N O EVIDENCE OF FIRE. MAINTENANCE REMOVED AND REPLACED THE CARGO COMPARTMENT SMOKE DETECTORS. MAINTENANCE ALSO REMOVED A ND REPLACED THE CARGO COMPARTMENT SMOKE DETECTOR. MAINTENANCE REMOVED AND REPLACED THE CARGO COMPARTMENT SMOKE DETECTOR S. MAINTENANCE ALSO REMOVED AND REPLACED NR 1 AND NR 2 SQUIBS AND FIRE BOTTLES. OPERATIONAL CHECKS WERE GOOD. AIRCRAF T RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001052300071 20010523 00071 EA 2001 5 23 ASOA01037 1 20010413 A 2910 AE4096G0060000 HYDRAULIC LINE CNDAIR CL600 CL6002B19 EA HYD SYSTEM CHAFED A ASOA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 11 834AS 7254 FLT 4572 - CLIMBING THROUGH FL250 INFLIGHT FROM ATL TO CRP, CREW RECEIVED A HYDRAULIC NR 1 LOW PRESSURE MESSAGE. HYDRAU LIC QUANTITY IN SYSTEM NR 1 INDICATED ZERO PERCENT. CREW DECLARED AN EMERGENCY AND DIVERTED TO BHM. AIRCRAFT LANDED SA FELY. MAINTENANCE FOUND CHAFFED STEEL BRAIDED HYDRAULIC LINE IN APU BAY. MAINTENANCE REMOVED AND REPLACED LINE AND NR 1 ENGINE HYDRAULIC PUMP. OPS AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001052300072 20010523 00072 EA 2001 5 23 ASOA01038 1 20010414 A 5610 NP1393211 WINDOW CNDAIR CL600 CL6002B19 EA COCKPIT CRACKED A ASOA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 821AS 8556 7194 FLT 4503 - DURING FLIGHT FROM ATL TO XNA, CAPTAINS SIDE WINDOW SHATTERED. AIRCRAFT RETURNED TO ATL AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED CAPTAINS SIDE WINDOW. OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SER VICE. (M) 2 L 7 2 4F RT A21EA 2001052300073 20010523 00073 NE 2001 5 23 ASOA01041 2 20010418 A 7532 97962641 BLEED VALVE EMB 120 EMB120RT SO PWA 118 PW118 NE ENGINE LEAKING A ASOA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 11 236AS 17633 120049 115146 FLT 4878 - SPS-DFW - DURING CLIMB-OUT, AT ABOUT 3600 FEET, THE RIGHT ENGINE DUCT LEAK LIGHT ILLUMINATED. THE ENGINE WAS SECURED AND ABOUT 45 SECONDS LATER THE LIGHT EXTINGUISHED. THE ENGINE WAS RESTARTED AND THE LIGHT DID NOT ILLUMINATE. AIRCRAFT RETURNED TO SPS AND LANDED SAFELY. NO DUCT LEAK INDICATIONS WERE NOTED ON GROUND. MAINTENANCE REMOVED AND RE PLACED RIGHT ENGINE BLEED DUCT O-RINGS AND DUCT OVERTEMP SENSORS AT INBOARD LEADING EDGE AND WING ROOT FAIRING. MAINTEN ANCE ALSO REMOVED AND REPLACED RIGHT ENGINE BLEED VALVE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 2001052300074 20010523 00074 2001 5 23 ASOA01042 4 20010418 A 3417 8220372140 ADC CNDAIR CL600 CL6002B19 EA E/E BAY DEFECTIVE A ASOA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SO 11 820AS 329 7188 FLT 4710 - DURING FLIGHT FROM DFW-SAV, MACH TRIM, F/O''S AIRSPEED, VSI, AND ALTIMETER ALL INOPERATIVE. AN EMERGENCY WAS DECLARED INBOUND TO DFW. AIRCRAFT RETURNED TO AND LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED AIR DATA COM PUTER. OPERATIONAL CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001052300075 20010523 00075 WP 2001 5 23 GTIA010205 1 20010418 A 2120 UNKNOWN DOUG DC9 DC982 3022082 WP CABIN ODOR A GTIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 805NK 48087 ORD - FLT 223 - EXHAUST FUMES FILL THE CABIN WHEN USING APU BLEED AIR USING LT OR RT PACK. SELECTED RT PACK AND RAM AIR , WITH APU OFF, FUMES CEASED. THIS CLEARS OUT THE EXHAUST FUMES FROM THE CABIN. TRANSFERRED TO DMI NR 0021799-1 CAT '' C''. PER MEL 49-1-2. (M) 2 L 7 2 4F A6WE 2001052300076 20010523 00076 2001 5 23 GTIA010204 4 20010422 A 2565 SLIDE DOUG DC9 DC982 3022082 WP L1 DOOR OUT OF POSITION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 L-1 DOOR SLIDE PACK FELL OFF OPENING DOOR AT GATE. RE-INSTALLED L1 DOOR SLIDE PACK IAW MM 25-60-00. NO OTHER DEFECTS N OTED AT THIS TIME. (M) 2 L 7 2 4F A6WE 2001052300077 20010523 00077 WP 2001 5 23 GTIA010203 1 20010422 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 809NK 49503 DTW - EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE ROWS 1 THROUGH 3. FOUND CONNECTION DISCONNECTED AT ROW 4, E-PATH LIGH T RECONNECTED CONNECTOR. OPS CHECKED GOOD PER MD-80 MM 33-60-01. NO OTHER DISCREPANCIES NOTED. (M) 2 L 7 2 4F RT A6WE 2001052300078 20010523 00078 WP 2001 5 23 GTIA010202 1 20010417 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 DALLQ 53014 DTW - FOUND FLOOR TRACK LIGHT BULBS AT ROW 13 AND 29 DO NOT LIGHT. REPLACED LIGHT PIGTAIL AT ROW 13 AND 29 IAW MD-80 MM 33-53-01. SYSTEM OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. (M) 2 L 7 2 4F RT A6WE 2001052300079 20010523 00079 WP 2001 5 23 GTIA010201 1 20010417 A 3350 LIGHT DOUG DC9 DC982 3022082 WP COCKPIT INOPERATIVE A GTIA K NONE L NO TEST CR CRUISE 1 GL 23 803NK 48087 EWR - FLT 1135 - FOUND PEANUT LIGHTS (EMERGENCY COCKPIT) INOPERATIVE. RELAMPED COCKPIT EMEREGNCY LIGHTS OPS CHECK OK PE R MM 33-53-00. (M) 2 L 7 2 4F A6WE 2001052300080 20010523 00080 2001 5 23 GTIA010200 4 20010417 A 2565 SLIDE DOUG DC9 DC982 3022082 WP R1 DOOR OUT OF POSITION A GTIA K NONE O OTHER CR CRUISE 1 GL 23 816NK 49190 DTW - FLT 572 - R1 DOOR SLIDE PACK FELL OFF. INSTALLED DOOR SLIDE PACK. REINSTALLED COVER AND LANYARD PIN IAW MD-80 MM 25-65-00. (M) 2 L 7 2 4F A6WE 2001052300081 20010523 00081 WP 2001 5 23 GTIA010119 1 20010418 A 3397 WIRE DOUG DC9 DC981 3022081 WP CABIN EXPOSED A K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FLT 506 - DTW - AT ROW 9 EMERGENCY FLOOR TRACK LIGHTS HAS EXPOSED WIRES FAA WRITE-UP. RE-INSTALLED FLOOR TRACK LIGHTS I AW MM 33-50-00. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2001052300082 20010523 00082 WP 2001 5 23 GTIA010118 1 20010410 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 GL 23 803NK 48087 DTW - FOUND TAIL EMERGENCY EXIT PATHWAY, 2 AFT WALL EMERGENCY LIGHTS NOT ILLUMINATING. REPAIRED BROKEN WIRES IAW MD-80 MM 33-50. SYSTEM OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. (M) 2 L 7 2 4F A6WE 2001052300083 20010523 00083 WP 2001 5 23 GTIA010117 1 20010416 A 2612 FIRE LOOP DOUG DC9 DC982 3022082 WP LT ENGINE GROUNDED A GTIA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 GL 23 816NK 49190 FLT 337 - MYR - AT GATE WITH ENGINES SHUTOFF HAD A LOOP LEFT SIDE ILLUMINATE WITH AN INTERMITTENT FIRE WARNING AND FIRE DET LOOP LIGHT. ONLY AN INTERMITTENT WARNING. OPENED LOWER COWL, INSPECTED LOOP, FOUND FIRE LOOP GROUNDED IN 2 PLACES. REPOSITIONED LOOP AND OPS CHECK GOOD IAW MD-80 MM 26-10-00. RESECURED LOWER COWL. AC OK FOR CONTINUED SERVICE. (M) 2 L 7 2 4F A6WE 2001052300084 20010523 00084 2001 5 23 GTIA010116 4 20010417 A 2230 AUTOTHRUST SYS DOUG DC9 DC983 3022083 WP COCKPIT MALFUNCTIONED A GTIA O OTHER O OTHER CL CLIMB 1 GL 23 814NK 49619 FLT 706 - DTW - ON INITIAL CLIMB-OUT AT KLGA, WHEN CL WAS SELECTED ON THE TRC, WITH A/T SYSTEM ENGAGED. LEFT ENGINE CAM E BACK TO NORMAL CLIMB POWER SETTING. RIGHT ENGINE VER RAPIDLY CAME BACK TO ALMOST FLIGHT IDLE. THIS HAPPENED SO FAST, UNABLE TO STOP IT IN TIME BEFORE HEAT SYSTEM ACTIVATED. AUTO THROTTLE SYSTEM WAS DISENGAGED AND NORMAL CLIMB POWER WAS OBTAINED BY MANUAL THROTTLES MOVEMENT. AUTOTHROTTLE SYSTEM WAS LATER RE-ENGAGED AND PERFORMED NORMALLY. PERFORMED FUN CTINAL CHECK ON AUTO-THROTTLE SYSTEM, RTS AND FLIGHT FAULT REVIEW. NO FAULTS FOUND. OPS CHECK GOOD PER MD-80 MM 22-01- 05. COULD NOT DUPLICATE. (M) 2 L 7 2 4F RT A6WE 2001052300085 20010523 00085 2001 5 23 GTIA010115 4 20010416 A 2565 SLIDE DOUG DC9 DC981 3022081 WP L2 DOOR OUT OF POSITION A GTIA K NONE O OTHER CR CRUISE 1 GL 23 810NK 48015 MCO - FLT 1599 - FOUND SLIDE PACK FELL OFF L2 DOOR. RE-INSTALLED L2 SLIDE PACK PER MM 25-62-00. (M) 2 L 7 2 4F A6WE 2001052300086 20010523 00086 WP 2001 5 23 GTIA010088 1 20010417 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN OUT OF POSITION A GTIA K NONE O OTHER CR CRUISE 1 GL 23 805NK 48087 ORD - FLT 784 - FOUND AISLE PATH LIGHTING OFF TRACK IN FORWARD AREA. REINSTALLED FLOOR TRACK LIGHT PANEL IAW MD-80 MM 3 3-50-00. OPS CHECK GOOD AT THIS TIME. (M) 2 L 7 2 4F A6WE 2001052300087 20010523 00087 NM 2001 5 23 USAASB01113 1 20010425 A 3350 900835A BATTERY BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 253AU 22795 BOS - THE EXIT LIGHTS ABOVE THE OVERWING EXITS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A16WE 2001052300088 20010523 00088 NM 2001 5 23 USAASB01112 1 20010425 A 3350 20131A BATTERY BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 288AU 23135 BWI - THE FORWARD ENTRY AND SERVICE DOOR EMERGENCY EXIT LIGHTS WERE INOPERATIVE, AND THE EXTERIOR ENTRY AND SERVICE DOOR ESCAPE SLIDE LIGHTS WERE WEAK. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A16WE 2001052300089 20010523 00089 NM 2001 5 23 20010523SG003 1 20010425 A 3350 6104789 BATTERY PACK BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 288AU 23135 BWI - THE FORWARD ENTRY AND SERVICE DOOR EMERGENCY EXIT LIGHTS WERE INOPERATIVE, AND THE EXTERIOR ENTRY AND SERVICE DOOR ESCAPE SLIDE LIGHTS WERE WEAK. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A16WE 2001052300090 20010523 00090 NM 2001 5 23 USAASB01122 1 20010321 A 3350 900835A BATTERY PACK BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 273AU 22885 IAD - THE CEILING EMERGENCY EXIT LIGHT AT SEAT ROW 10 WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK. (M) 2 L 7 2 4F A16WE 2001052300091 20010523 00091 NM 2001 5 23 USAASB01123 1 20010330 A 3350 900835A BATTERY PACK BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 273AU 22885 CLE - THE AISLE OVERWING EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK. (M) 2 L 7 2 4F A16WE 2001052300092 20010523 00092 WP 2001 5 23 USAAD01090 1 20010430 A 3350 60030451LB BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 811US 48043 TPA - THE FLOOR TRACK EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001052300093 20010523 00093 WP 2001 5 23 USAAD01087 1 20010430 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 802US 48036 IND - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001052300094 20010523 00094 EU 2001 5 23 ASOA01043 1 20010422 A 3242 AHA1653 BRAKE ASSY AEROSP ATR72 ATR72212 EU RT MLG OVERHEATED A ASOA K NONE M J OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 SO 11 636AS 375 FLT 4100 - AFTER LANDING ROLL OUT AT ATL AND CLEAR OF RUNWAY ON TAXI WAY, A HOT BRAKE LIGHT CAME ON. GROUND CREW DECLAR ED AN EMERGENCY. MFC SHOWS RIGHT INBOARD BRAKE HOT. RIGHT BRAKE COOLED AND NO DEFECTS WERE NOTED BY MAINTENANCE. AIRC RAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001052300095 20010523 00095 EA 2001 5 23 ASOA01044 1 20010422 A 5610 NP1393216 WINDSHIELD CNDAIR CL600 CL6002B19 EA COCKPIT CRACKED A ASOA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 11 851AS 3422 7360 FLT 4459 - DURING FLIGHT FROM CAE TO DFW, F/O''S FORWARD WINDSHIELD CRACKED AT 35,000 FEET. AN EMERGENCY WAS DECLARED. AIRCRAFT DIVERTED TO JAN AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED FORWARD RIGHT WINDSHIELD. LEAK AND OPERA TIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001052300096 20010523 00096 SO 2001 5 23 ASOA01045 1 20010423 A 2120 12046207002 RAM AIR DOOR EMB 120 EMB120RT SO FUSELAGE STUCK A ASOA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 11 274AS 120229 FLT 4159 - AFTER TAKEOFF FROM ATL, BOTH PILOTS SMELLED A BURNING ODOR FOLLOWED BY THE LAVATORY SMOKE DETECTOR SOUNDING. RIGHT PACK FAIL MESSAGE ILLUMINATED. AIRCRAFT RETURNED AND LANDED SAFELY IN ATL. MAINTENANCE FOUND RIGHT RAM AIR DOOR STUCK. MAINTENANCE LUBRICATED RAM AIR DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001052300097 20010523 00097 NM 2001 5 23 SWAA011383 1 20010508 A 3350 57771 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED C4 CHECK, FOUND EEPLS END CAP MISSING AT FWD END. INSTALLED END CAP PER MM. 2 L 7 2 4F A16WE 2001052300098 20010523 00098 NM 2001 5 23 SWAA011385 1 20010508 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED BC4 CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT INOP. REPAIRED EGRESS LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001052300099 20010523 00099 NM 2001 5 23 SWAA011386 1 20010508 A 3350 90083 CHARGER BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 514SW 25153 DURING SCHEDULED D-CHECK AT DALFORT, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHTS INOP, AT ROWS 10, 12, 14, 16, 18 AND 20 DEF, AND ROWS 16, 17, 19 AND 20 ABC. REMOVED AND REPLACED BATT CHARGER PER MM. 2 L 7 2 4F RT A16WE 2001052300100 20010523 00100 NM 2001 5 23 SWAA011387 1 20010509 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 361SW 26572 EEPLS TRACK COVER BROKEN AT ROWS 11 & 12. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2001052300101 20010523 00101 NM 2001 5 23 SWAA011388 1 20010508 A 5523 183A4210 HINGE BOEING 737 7377H4 NM RT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 754SW 29849 DURING SCHEDULED SERVICE CHECK, SWA SI 11052-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 RT E LEVATOR TAB HINGE FITTING ASSY PER MM. 2 L 7 2 4F RT A16WE 2001052300102 20010523 00102 NM 2001 5 23 SWAA011390 1 20010509 A 2612 D1098 CONNECTOR BOEING 737 7372H4 138448C NM NR 1 ENGINE CRACKED A SWAA E F A ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 102SW 23108 DECLARED EMERGENCY, DIVERSON AND IN-FLIGHT ENGINE SHUT DOWN. NR 1 ENG FIRE WARNING LIGHT ILLUMINATED IN FLIGHT, ENGINE SHUT DOWN LIGHT RE-ILLUMINATED, FIRE EXTINGUISHER DISCHARGED. MX FERRIED TO DAL. REMOVED AND REPLACED CONNECTOR AT NR 1 ENG LOWER LOOP AFT END. REMOVED AND REPLACED FIRE DETECTION UNIT PER MM. 2 L 7 2 4F A16WE 2001052300103 20010523 00103 NM 2001 5 23 SWAA011392 1 20010510 A 5523 BACB28AK04 BUSHING BOEING 737 7377H4 NM RT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 728SW 27860 DURING SCHEDULED A2 CHECK, SWA SI 11052-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 3 & 4 TAB H INGE BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2001052300104 20010523 00104 NM 2001 5 23 SWAA011395 1 20010509 A 3397 BR2013 WIRE BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 EEPLS TRACK WIRES LOOSE. SECURED EEPLS WIRES PER MM. 2 L 7 2 4F A16WE 2001052300105 20010523 00105 NM 2001 5 23 SWAA011396 1 20010509 A 3350 57771 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED C3 CHECK, FOUND EEPLS END CAP MISSING AT AFT END. INSTALLED END CAP PER MM. 2 L 7 2 4F A16WE 2001052300106 20010523 00106 NM 2001 5 23 SWAA011400 1 20010509 A 5523 65C26384 TAB BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED C4 CHECK, FOUND PLAY AT LT ELEVATOR TAB. REMOVED AND REPLACED TAB ASSY PER MM. 2 L 7 2 4F RT A16WE 2001052300107 20010523 00107 NM 2001 5 23 SWAA011403 1 20010509 A 2750 6550324 TRANSMISSION BOEING 737 7373H4 1384600 NM T/E FLAP FAILED A SWAA D RETURN TO BLOCK F FLT CONT AFFECTED CL CLIMB 1 SW 07 358SW 26595 AIR TURNBACK, T/E FLAPS WOULD NOT RETRACT PAST 5 DEGREES DURING CLIMBOUT. REMOVED AND REPLACED NR 4 FLAP TRANSMISSION P ER MM. 2 L 7 2 4F RT A16WE 2001052300108 20010523 00108 NM 2001 5 23 SWAA011404 1 20010509 A 3350 LIGHT BOEING 737 7377H4 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 715SW 27849 EEPLS INOP AND LENS MISSING AT FWD CABIN. RELAMPED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2001052300109 20010523 00109 NM 2001 5 23 SWAA011406 1 20010511 A 3350 LIGHT BOEING 737 7373A4 1384585 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 675AA 23253 EEPLS INOP AND LENS MISSING AT MID CABIN. RELAMPED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2001052300110 20010523 00110 NM 2001 5 23 SWAA011407 1 20010512 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 720WN 27854 DURING SCHEDULED C2 CHECK, FOUND SEVERAL EEPLS TRACK COVERS CRACKED. REPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2001052300111 20010523 00111 NM 2001 5 23 SWAA011408 1 20010511 A 3350 207377 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED C2 CHECK, FOUND EEPLS LENS MISSING AT ROW 11. REPLACED EEPLS LENS PER MM. 2 L 7 2 4F RT A16WE 2001052300112 20010523 00112 NM 2001 5 23 SWAA011410 1 20010512 A 3350 6128251 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT MID CABIN. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2001052300113 20010523 00113 NM 2001 5 23 SWAA011411 1 20010511 A 3350 6104789 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT MID CABIN. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2001052300114 20010523 00114 NM 2001 5 23 SWAA011414 1 20010511 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 637SW 27710 EEPLS COVER MISSING AND WIRES EXPOSED AT ROW 16. REPLACED EEPLS COVER AND SECURED WIRES PER MM. 2 L 7 2 4F RT A16WE 2001052300115 20010523 00115 NM 2001 5 23 SWAA011415 1 20010511 A 3350 65C34691 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 355SW 25250 OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 20 DEF. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2001052300116 20010523 00116 NM 2001 5 23 SWAA011416 1 20010512 A 3350 65C34691 LIGHT BOEING 737 7377H4 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 401WN 29813 DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 18 DEF. RELAMPED BULLNOSE LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001052300117 20010523 00117 NM 2001 5 23 SWAA011418 1 20010511 A 5523 DAS414A1508 BEARING BOEING 737 7373H4 1384600 NM LT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BEARING PER MM. 2 L 7 2 4F RT A16WE 2001052300118 20010523 00118 NM 2001 5 23 SWAA011419 1 20010512 A 2731 6545166 CONTROL ROD BOEING 737 7377H4 NM RT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 760SW 27874 DURING SCHEDULED SERVICE CHECK, SWA SI 11052-55, RT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED OUTBOARD ELEV ATOR TAB CONTROL ROD PER MM. 2 L 7 2 4F RT A16WE 2001052300119 20010523 00119 NM 2001 5 23 SWAA011427 1 20010512 A 3350 6556633 SIGN BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 087SW 22903 OVERWING DOOR EMERGENCY EXIT SIGN MISSING AT LT SIDE. REPLACED EMERGENCY EXIT SIGN PER MM. 2 L 7 2 4F A16WE 2001052300120 20010523 00120 NM 2001 5 23 SWAA011429 1 20010513 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 639SW 27712 EEPLS COVER LOOSE AT ROW 11. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2001052300121 20010523 00121 2001 5 23 SWAA011432 4 20010514 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001052300122 20010523 00122 NM 2001 5 23 SWAA011434 1 20010514 A 3397 BR2013 WIRE BOEING 737 7377H4 1384404 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 768SW 30587 DURING SCHEDULED RON, FOUND EEPLS TRACK WIRES EXPOSED AT ROWS 1 & 3. SECURED EEPLS WIRES PER MM. 2 L 7 2 4F RT A16WE 2001052300123 20010523 00123 NM 2001 5 23 SWAA011436 1 20010513 A 5523 BACB28AK04 BUSHING BOEING 737 7377H4 NM RT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 740SW 29276 DURING SCHEDULED SERVICE CHECK, SWA SI 11052-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVAT OR, TAB NR 1 HINGE BUSHING PER MM. 2 L 7 2 4F RT A16WE 2001052300124 20010523 00124 NM 2001 5 23 SWAA011440 1 20010513 A 3350 65C27095 BATTERY PACK BOEING 737 7372H4 138448C NM ENTRY DOOR DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 067SW 22356 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2001052300125 20010523 00125 NM 2001 5 23 SWAA011449 1 20010514 A 2613 6552808 ACCESSORY UNIT BOEING 737 7372T4 1384492 NM E&E BAY MALFUNCTIONED A SWAA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 722WN 22698 AIR TURNBACK, IN FLIGHT ENGINE SHUTDOWN AND DECLARED EMERGENCY. NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED DURING FLIGHT. INSPECTED ENGINE FOR SIGNS OF OVERHEAT, NONE NOTED. BULBS REMOVED FROM NR 2 ENGINE OVERHEAT LIGHT. OK TO CONTINUE PER MEL. LATER AT MDW REMOVED AND REPLACED ENGINE AND APU FIRE ACCESSORY UNIT. 2 L 7 2 4F A16WE 2001052300126 20010523 00126 SO 2001 5 23 C2XA01CL107 1 20010514 A 3350 20131A BATTERY PACK EMB 145 EMB145LR SO CABIN DISCHARGED A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 13964 83 83 145123 CLE FLIGHT 4075 THE CREW REPORTED THE EMERGENCY FLOOR LIGHTING WAS INOPERATIVE AT ROW 12. MAINTENANCE INSPECTED AND REP LACED THE EMERGENCY LIGHT BATTERY PACK NR 3. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001052300127 20010523 00127 SO 2001 5 23 C2XA01CL108 1 20010510 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN BROKEN A C2XA K NONE L NO TEST NR NOT REPORTED 1 SW 27 14920 145380 BNA-CLE FLIGHT 4034 THE CREW REPORTED THE AISLE PATH EMERGENCY LIGHTS WERE NOT WORKING AT ROWS 1 AND 2. MAINTENANCE INS PECTED AND REPAIRED A BROKEN WIRE ON THE AISLE PATH LIGHTING. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001080600122 20010806 00122 WP 2001 8 6 RRXA010046 1 20010510 A 5330 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8076U 45941 DURING FCD A53-4R2 INSPECTION OF LWR FUSELAGE CORROSION. MX DISCOVERED CORROSION BEYOND LIMITS. REMOVED CORROSION , FA BRICATED NEW FINGER DOUBLER AND INSTALLED PER EO 01-143 WITH APPROVED 8110-3 DATED 5/12/01. 2 L 7 4 4F RT 4A25 2001052300128 20010523 00128 WP 2001 5 23 RRXA010047 1 20010512 A 2120 UNKNOWN DOUG DC10 DC1010F 3022111 WP CABIN ODOR A RRXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 15 68044 46903 AIR COMING INTO THE AIRCRAFT FROM ANY OF THE 3 PACKS IS LADDEN WITH A STRONG SMOKEY ODOR WHICH BURNS THE EYES AND IS UN COMFORTABLE TO BREATHE. IT IS MORE PRONOUNCED THE WARMER YOU SELECT THE TEMP. SUSPECT A PETROLEUM PRODUCT IS BEING HE ATED/BURNED SOME WHERE IN SYSTEM. OPERATED ALL 3 PACKS WITH DOORS CLOSED COULD NOT DUPLICATE ODOR WITH SEVERAL DIFFEREN T PACKS SETTINGS WITH NO DEFECTS NOTED. AIRCRAFT SAFE FOR CONTINUED FLIGHT. 2 L 7 3 4F A22WE 2001052300130 20010523 00130 EU 2001 5 23 QXEA0100703 1 20010513 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 475AU 11222 SEA - THE FWD EMERGENCY EXIT SIGN WAS REPORTED INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001052300131 20010523 00131 WP 2001 5 23 01FDEA00353 1 20010516 A 2760 PUSHROD DOUG DC10 DC1030F 3023504 WP SPOILER BENT A FDEA O OTHER F FLT CONT AFFECTED LD LANDING 1 SO 25 302FE 46801 SPOILERS WOULD NOT DEPLOY INFLT. HANDLE WOULD NOT MOVE MORE THAN 1/3 DOWN. REMOVED AND REPLACED THROTTLE INTERLOCK PUS HROD ASSY PER MM 27-62-01-2-1. SYS CK NORM. OK FOR SERVICE. 2 L 7 3 4F RT A22WE 2001052300132 20010523 00132 WP 2001 5 23 AT0100156 1 20010419 A 2701 5614272503N CONTROL COLUMN DOUG DC9 DC932 3022066 WP COCKPIT CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 803AT 47261 FOUND CAPTAINS CONTROL COLUMN CRACKED BEYOND LIMITS. REPLACED CONTROL COLUMN IAW EO 12-2730-29-B1063. 2 L 7 2 4F A6WE 2001052300133 20010523 00133 WP 2001 5 23 AT0100170 1 20010513 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN BROKEN A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 832AT 47451 FOUND AFT EXIT EMERGENCY LIGHT INOPERATIVE. REPAIRED BROKEN WIRE. 2 L 7 2 4F A6WE 2001052300134 20010523 00134 NM 2001 5 23 AT0100171 1 20010515 A 3350 081691 SOCKET BOEING 737 737284 138448R NM CABIN BROKEN A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 470AT 21501 FOUND EMERGENCY PATH LIGHT SOCKET BROKEN. REPLACED SOCKET IAW STANDARD WIRING PRACTICES. 2 L 7 2 4F A16WE 2001052300135 20010523 00135 NM 2001 5 23 AWXA0001759 1 20010516 A 5320 65C807351 THRESHOLD BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 R2 DOOR THRESHOLD HAS CORROSION FROM STA 992 - 967 UNDERNEATH THRESHOLD. REMOVED AND REPLACED DOOR THRESHOLD INNER CHOR D THAT WAS FOUND TO BE OUT OF LIMITS IAW SRM 51-40-2. 2 L 7 2 4F RT A16WE 2001052300136 20010523 00136 NM 2001 5 23 SWAA011461 1 20010515 A 3350 6556633 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 314SW 23336 DURING SCHEDULED C4 CHECK, FOUND RT EMERGENCY EXIT SIDEWALL EXIT SIGN MISSING LENS. INSTALLED EMERGENCY EXIT SIGN LENS. 2 L 7 2 4F RT A16WE 2001052300137 20010523 00137 NM 2001 5 23 SWAA011462 1 20010516 A 3350 BR2013 TRACK BOEING 737 7377H4 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 714CB 27848 EEPLS TRACK LIGHTING LOOSE. SECURED EEPLS PER MM 2 L 7 2 4F RT A16WE 2001052300138 20010523 00138 NM 2001 5 23 SWAA011463 1 20010515 A 3350 6556681 LIGHT BOEING 737 7373H4 1384600 NM ENTRY DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 627SW 27935 FWD ENTRY DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001052300139 20010523 00139 NM 2001 5 23 SWAA011464 1 20010515 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 389SW 26592 EEPLS TRACK WIRES EXPOSED. SECURED EEPLS WIRES PER MM. 2 L 7 2 4F RT A16WE 2001052300140 20010523 00140 NM 2001 5 23 01FDEA00350 1 20010515 A 2133 OUTFLOW VALVE BOEING 727 72727C 138400J NM CABIN PRESSURE FAILED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 146FE 19110 A/C WILL NOT PRESSURIZE, EITHER PACK ANY BLEED SOURCE, MANUAL OR AUTO MODE. NO DOOR LIGHTS ILLUM ON 2ND OFF PNL. R&R LT & RT OUTFLOW VALVE & CABIN PRESSURE CONTROLLER PER 727 MM 21-30-051-4, 21-31-010-4 & 21-30-000-5. 2 L 7 3 4F A3WE 2001052400002 20010524 00002 SW 2001 5 24 WP012001B1974 1 20010319 A 2910 214076560103 SCREW TEXTRON BELL 214 214ST 1182106 SW SERVO BROKEN B K NONE O OTHER IN INSP/MAINT 1 SW 99 4488 0346 SERVO MOUNT ADJUSTER SCREW BROKEN WITH SCREW HEAD AND NUT MISSING. ADJUSTER SCREW PN 214-076-560-103 PIECE REMOVED FROM MOUNT APPEARS AT THE BREAK TO HAVE HYDROGEN EMBRITTLEMENT AND SOME RUST IN THE WRENCH SLOT. 2 G 7 2 4U H10SW 2001052400005 20010524 00005 NM 2001 5 24 HN6R0000150 1 20010516 A 5320 SILL BOEING 737 737400 NM FUSELAGE CORRODED B HN6R K NONE O OTHER IN INSP/MAINT 1 SW 99 931NU 25247 BS 940 TO 991, WL 208, LBL 46 TO 51, MOP SILL CORRODED. REMOVED AND REPLACED MOP SILL. 2 L 7 2 4F RT A16WE 2001071300021 20010713 00021 NM 2001 7 13 HN6R0000149 1 20010625 A 5311 FRAME BOEING 737 737400 NM FUSELAGE CRACKED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 932NU 25248 HFEC INSPECTION EXHIBITS CRACK INDICATION IN FRAME. BS 663.75, STR3, LT FORWARD HOLE. CAUSE UNKNOWN. REPAIRED FRAME PER SB. 2 L 7 2 4F RT A16WE 2001052400006 20010524 00006 NM 2001 5 24 HN6R0000251 1 20010516 A 5754 6546431280 SKIN BOEING 737 737400 NM L/E FLAP DELAMINATED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 931NU 25240 R/W O/B FORE FLAP UPPER SURFACE DELAMINATED. 9 INCHES FROM THE I/B END.REPAIRED SURFACE OF FLAP. 2 L 7 2 4F RT A16WE 2001052400008 20010524 00008 NM 2001 5 24 HN6R0000328 1 20010516 A 5311 FRAME BOEING 737 737400 NM FUSELAGE CRACKED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 931NU 25247 HFEC INSP EXHIBITS CRACK IN FRAME INNER CHORD BS616 10 WEST HOLE APPROX WL 203 RBL 55. F/S 9 BS 616 WC 203 RBL 55. IN STALLED FASTENERS. 2 L 7 2 4F RT A16WE 2001052400009 20010524 00009 NM 2001 5 24 HB6R0000329 1 20010516 A 5311 FRAME BOEING 737 737400 NM FUSELAGE CRACKED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 931NU 25247 HFEC INSP EXHIBITS CRACK IN FRAME INNER CHORD RS 616 LOWEST HOLE APPROX WL 203, LBL 55. F/S 9, BS 616 WL 203, INSTALLED FASTENERS. 2 L 7 2 4F RT A16WE 2001052400010 20010524 00010 NM 2001 5 24 HN6R0000456 1 20010516 A 5311 FRAME BOEING 737 737400 NM FUSELAGE CRACKED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 931NU 25247 HFEC FOUND CRACK INDICATION AT BS 663.75 STA 2R. FORWARD HOLE UNDER FRAME. CRACK RUNNING FORWARD. 2 L 7 2 4F RT A16WE 2001052400011 20010524 00011 NM 2001 5 24 HN6R0000499 1 20010516 A 5315 FLOORBEAM BOEING 737 737400 NM FUSELAGE CORRODED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 931NU 25247 FLOOR SPAR IS CORRODED AT BS 986, WL 208, RBL 43. REMOVED CORROSION, FABRICATED REPAIR PARTS AND INSTALLED. 2 L 7 2 4F RT A16WE 2001052400012 20010524 00012 NM 2001 5 24 HN6R0000450 1 20010516 A 5311 FRAME BOEING 737 737400 NM FUSELAGE CRACKED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 931NU 25247 HFEC FOUND CRACK INDICATION AT BS 663.75 STR 2L FORWARD HOLE, UNDER FRAME. 2 L 7 2 4F RT A16WE 2001052400014 20010524 00014 NM 2001 5 24 HN6R0000252 1 20010516 A 5754 6546431280 SKIN BOEING 737 737400 NM L/E FLAP DELAMINATED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 931NU 25247 RIGHT WING OUTBOARD FORE FLAP UPPER SURFACE DELAMINATED 92 INCHES FROM INBOARD END. REPAIRED UPPER SURFACE OF FLAP. 2 L 7 2 4F RT A16WE 2001052400015 20010524 00015 NM 2001 5 24 HN6R0000369 1 20010516 A 5753 6546435277 SKIN BOEING 737 737400 NM T/E FLAP DEBONDED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 931NU 25247 DEBOND INDICATION NOTED AT LEFT WING OUTBOARD AFT FLAP UPPER SURFACE 46 FROM INBOARD END AND 4 INCHES FROM TRAILING EDGE APPROX 1.75 INCHES IN DIA. REPAIRED UPPER SURFACE OF FLAP. 2 L 7 2 4F RT A16WE 2001052400016 20010524 00016 EU 2001 5 24 KBMA88714 1 20010515 A 6410 355A12004008 SPAR SNIAS 350 AS350B2 8680813 EU TAIL ROTOR DELAMINATED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 53SH 3805 2009 DELAMINATED SPAR. 1 G 7 1 3U H9EU 2001052400017 20010524 00017 CE 2001 5 24 20010510CW002 1 20010409 A 5210 1294000341 DOOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA PAX DOOR OPEN A JJBA O OTHER P NO WARNING INDICATION DE DESCENT 1 EA 01 842CA 1015 UE41 DURING DECENT AT APPROX 3000 FT, THE FORWARD CABIN ENTRANCE DOOR OPENED. EMERGENCY WAS DECLARED AND THE AIRCRAFT MADE A N UNEVENTFUL LANDING. UPON INSPECTION OF DOOR AND ANNUNICATOR SYSTEM THE FOLLOWING DEFECTS WERE FOUND: 1/ BOTH DOOR HA NDLE ANNUNICATOR SWITCHES WERE STUCK CLOSED AND HAD EVIDENCE OF CORROSION AT WIRE ATTACHMENT POINTS. 2 L 7 2 4T 3 T RT A24CE E2NE 2001052400018 20010524 00018 CE 2001 5 24 20010510CW003 1 20010409 A 5270 SWITCH BEECH 1900 1900D 1154162 CE PAX DOOR CORRODED A JJBA O OTHER P NO WARNING INDICATION DE DESCENT 1 EA 01 842CA UE41 BOTH DOOR HANDLE ANNUNCATOR SWITCHES WERE STUCK CLOSED AND HAD EVIDENCE OF CORROSION AT WIRE ATTACHMENT POINT. 2 L 7 2 4T RT A24CE 2001052400019 20010524 00019 CE 2001 5 24 20010510CW004 1 20010409 A 5210 SWITCH BEECH 1900 1900D 1154162 CE PAX DOOR OUT OF RIG A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 842CA UE41 BOTH CAM LATCH SWITCHES WERE NOT RIGGED CORRECTLY IN RELATION TO ANNUNICATOR OPERATION. 2 L 7 2 4T RT A24CE 2001052400020 20010524 00020 CE 2001 5 24 20010510CW006 1 20010409 A 5320 NUT BEECH 1900 1900D 1154162 CE ACTUATING ROD LOOSE A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 842CA UE41 TWO (2) LOCKING NUTS ON ACTUATING RODS WERE LOOSE AND WERE BACKED OFF. 2 L 7 2 4T RT A24CE 2001052400021 20010524 00021 CE 2001 5 24 20010510CW007 1 20010409 A 5210 WIRE ROPE BEECH 1900 1900D 1154162 CE DOOR LATCH OUT OF ADJ A K NONE O OTHER IN INSP/MAINT 1 EA 01 842CA UE41 DOOR LATCHING CABLES WERE BELOW RECOMMENDED TENSION. 2 L 7 2 4T RT A24CE 2001052400022 20010524 00022 CE 2001 5 24 20010510CW008 1 20010409 A 5210 WIRE ROPE BEECH 1900 1900D 1154162 CE DOOR LATCH FRAYED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 842CA UE41 DOOR LATCHING CABLE WAS FOUND FRAYED DUE TO CONTACT WITH CABLE GUIDE. CABLE PULLEY HAD A FOREIGN MATERIAL IN GROOVE CAU SING CABLE TO BE FORCED INTO CABLE GUIDE. 2 L 7 2 4T RT A24CE 2001052400023 20010524 00023 CE 2001 5 24 20010511CW010 1 20010511 A 5711 51220413 SPAR CAP CESSNA 421 421B 2076014 CE CONT O520 GTSIO520C 17032 SO LT WING CRACKED G K NONE O OTHER IN INSP/MAINT 1 GL 13 100YR 6580 0437 DURING AN ANNUAL INSPECTION, A CRACK APPROX 3 INCHES LONG WAS FOUND ON LEFT WING AFT SPAR, UPPER AFT CAP. BELOW BAGGA GE RACELLE. 1 L 7 2 3O 3 O A7CE E7CE 2001052400024 20010524 00024 CE 2001 5 24 20010511CW011 1 20010419 A 2121 99103992 BLOWER CESSNA 650 650 2076802 CE CABIN DEFECTIVE B T0DA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 50EJ 3922 650148 ON TAXI OUT CREW NOTICED SMOKE IN CABIN AND SMELLED SMOKE. AIRCRAFT WAS TAKEN TO REPAIR STATION AND THEY FOUND THE BLOW ER TO BE INOPERATIVE AND SMELLING STRONGLY OF BURNED WIRING. THEY INSTALLED AN OVERHAULED SYSTEM, OPS CHECKED OK. DUE T O NORMAL WEAR. 2 L 7 2 4F A9NM 2001052400025 20010524 00025 CE 2001 5 24 20010511CW012 1 20010411 A 5610 551128548 WINDOW CESSNA 500 550 2076604 CE COCKPIT CRACKED B K NONE O OTHER IN INSP/MAINT 1 NM 09 21SL 766 5500877 WHILE COMPLETING S/B FOUND CO PILOTS SIDE WINDOW CRACKED AT HOLES 3 AND 5. REQUIRING WINDOW REPLACEMENT. 1 L 7 2 4F A22CE 2001052400026 20010524 00026 CE 2001 5 24 20010511CW013 1 20010424 A 2421 90032 ALTERNATOR CESSNA 750 750 2076810 CE ENGINE FAILED G K NONE O OTHER NR NOT REPORTED 1 GL 23 5116 7500019 CREW STATED RIGHT HAND WINDSHIELD HEAT INOPERATIVE. TROUBLESHOT TO FAULTY LEFT HAND ALTERNATOR. UPON ALTERNATOR REMOVA L, NOTICED THAT THE COOLING FAN BLADES ON THE ALTERNATOR WERE ALL BROKEN OFF. 2 L 7 2 4J RT T00007WI 2001052400027 20010524 00027 CE 2001 5 24 20010514CW001 1 20010423 A 2711 258CW4939A JACKSCREW RAYTHN DH125 HAWKER800 7450004 CE GARRTT TFE731 TFE7312B WP AILERON TRIM STIFF B UO2R A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 19 826GA 258263 AIRCRAFT FLEW TO ALTITUDE AND AILERON TRIM CONTROL BECAME STIFF. UPON RETURN THE TRIM JACK WAS LUBED AS PER MM. SUSPEC T MOISTURE OR WATER FREEZING AT ALTITUDE. 2 L 7 2 4F 4 F RT A3EU E6WE 2001052400028 20010524 00028 GL 2001 5 24 20010514CW002 1 20010221 A 5320 GS2170237003 SUPPORT BRACKET BOMBDR BD700 BD7001A10 1390006 GL RROYCE BR700 BR700710A110 NE FUSELAGE CRACKED E K NONE O OTHER IN INSP/MAINT 1 EA 27 777GX 9036 CRAWLWAY SUPPORT BRACKET IS CRACKING AT BEND RADIUS ON 3 EA FLANGES THAT SUPPORT THE A FLOORBOARD. PART CANNOT BE REPAI RD, MUST BE REPLACED. 2 L 7 2 4F 4 F RT T00003NY E00057EN 2001052400031 20010524 00031 CE 2001 5 24 20010514CW005 1 20010417 A 2435 30B3749BT STARTER GEN LEAR 25 25D 5170514 CE LT ENGINE VIBRATES E CJPA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 NM 03 727CS 477 25D313 FLIGHT CREW EXPERIENCED AN AIRFRAME RUMBLE DURING TAKEOFF AND OPTED TO RETURN TO LANDING. MAINTENANCE CONFIRMED THE RUM BLE DURING GROUND RUN AND DETRMINED THE LEFT HAND STARTER GENERATOR CAUSING THE RUMBLE. A SERVICEABLE STARTER GENERATOR WAS INSTALLED, RUNUP GOOD AND AIRCRAFT APPROVE FOR RETURN TO SERVICE. 2 L 7 2 4J A10CE 2001052400032 20010524 00032 EU 2001 5 24 KBMA88727 1 20010418 A 8012 0174078010 START VALVE SNIAS 350 AS350BA 8680817 EU ENGINE LEAKING E KBMA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 19 270SH 7704 1864 REMOVED AND REPLACED START DRAIN VALVE. UNIT WAS LEAKING. 1 G 7 1 3U NC H9EU 2001052400033 20010524 00033 EU 2001 5 24 20010514CW006 1 20010427 A 5330 SKIN AMD FALCON FALCON20 2730103 EU GE CF700 CF700* 30010 NE FUSELAGE CORRODED B VO2R K NONE O OTHER IN INSP/MAINT 1 GL 19 731G 6272 6272 267 LEFT HAND NR 2 AND RIGHT HAND NR 1 CABIN WINDOW MOUNTING AREA AND INNER SKIN SHOWED CORROSION BEYOND SRM LIMITS. THE RE MAINING WINDOW MOUNTING AREAS SHOWED CORROSION BUT WERE WITHIN LIMITS. 2 L 7 2 4F 4 F RT A7EU E7EA 2001052400034 20010524 00034 SO 2001 5 24 20010514CW007 1 20010411 A 2720 96212000 TORQUE TUBE PIPER PA34 PA34200T 7103406 SO RUDDER CORRODED D K NONE O OTHER IN INSP/MAINT 1 SO 11 2900B 9000 347970338 REMOVED RUDDER TORQUE TUBE DUE TO ELONGATED HOLE AT BOTTOM FOR RUDDER HORN. UPON DISASSEMBLY FOUND PART SEVERLY RUSTED AND CORROSION ON ADJACENT RIBS AND SKINS. CAUSE FROM WATER ACCUMULATION AND POOR CORROSION PREVENTION ON PART. NOTE: SKINS AND RIBS HAD NO PRIMER AND THE TORQUE TUBE IS STEEL. 1 L 7 2 3O A7SO 2001052400035 20010524 00035 SO 2001 5 24 ASOA01046 1 20010425 A 2611 BATTERY EMB 120 EMB120RT SO SMOKE DETECT DISCHARGED A ASOA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 11 274AS 120229 FLT 4222 - AFTER TAKEOFF FROM GPT, CAPTAIN REPORTED LAVATORY SMOKE DETECTOR SOUNDING. AIRCRAFT RETURNED TO GPT AND LAND ED SAFELY. MAINTENANCE REMOVED AND REPLACED BATTERY IN LAVATORY SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RET URNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001052400036 20010524 00036 EA 2001 5 24 ASOA01047 1 20010426 A 3350 601R461011 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 859AS 7421 FLT 4653 - ON GROUND, FORWARD ORANGE SECTION OF FLOOR EMERGENCY LIGHTING DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REP LACED EMERGENCY LIGHTING STRIP. OPERATIONAL CHECKS OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001052400037 20010524 00037 SO 2001 5 24 ASOA01048 1 20010424 A 5311 FRAME EMB 120 EMB120RT SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 240AS 120060 DURING INSPECTION, MAINTENANCE FOUND CORROSION ON STRINGER 17 LEFT, FRAME 21. MAINTENANCE REPAIRED CORROSION FOLLOWING EO 120-53-0156, WHICH OUTLINES PROCEDURES FOR FRAME 21 CORROSION REPAIR. (M) 2 L 7 2 4T RT A31SO 2001052400038 20010524 00038 NE 2001 5 24 ASOA01049 2 20010428 A 7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LEFT FAILED A ASOA E A ENGINE SHUTDOWN UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SO 11 236AS 120049 115146 FLT 4063 - DURING CLIMB-OUT FROM ATL, AT APPROXIMATELY 15,000 MSL, AIRCRAFT EXPERIENCED LEFT ENGINE FAILURE. AIRCRAFT R ETURNED TO AND LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND RPLACED THE LEFT ENGINE HYDROMECHANICAL UNIT. ENGINE IS C URRENTLY UNDERGOING MAINTENANCE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 2001052400039 20010524 00039 WP 2001 5 24 GTIA010253 1 20010501 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 800NK 49144 FLT 572 - DTW - FOUND EMERGENCY LIGHTS NOT ILLUMINATING SEAT ROWS 16 TO 23. RESECURED EMERGENCY PATH LIGHTING ILLUMINAT ING STRIP TO FLOOR. SYSTEM NOW OPS CHECK GOOD REF 33-53-00 MD-80 MM. (M) 2 L 7 2 4F A6WE 2001052400040 20010524 00040 WP 2001 5 24 GTIA010252 1 20010430 A 3260 WARNING LIGHT DOUG DC9 DC983 3022083 WP COCKPIT ILLUMINATED A GTIA O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 DALLR 53015 FTW - FLT 952 - FOUND GEAR DOOR OPEN LIGHT ON EN ROUTE. ALL GEAR RED LIGHTS ILLUMINATED LATER ON. GEAR LIGHTS WENT OUT AFTER HYD PUMPS ON HIGH. GEAR DOOR LIGHT WENT OUT. CAME ON AGAIN, THEN WENT OUT. (M) 2 L 7 2 4F RT A6WE 2001052400041 20010524 00041 2001 5 24 GTIA010250 4 20010501 A 3460 4034242923 CONTROL PANEL DOUG DC9 DC982 3022082 WP COCKPIT FAULTY A GTIA K NONE O OTHER CR CRUISE 1 GL 23 816NK 49140 DTW - FLT 476 - FOUND MACH SET ON AUTO, PILOT INOPERATIVE.IAC IS FOR BOTH MACH AND IAS. REMOVED AND REPLACED DFGC CONTR OL PANEL. PERFORMED RTS AND SWITCH AND BUTTON TEST. SYSTEM OPS CHECK GOOD IAW MD-80 MM CHAPTER 22-01-05. (M) 2 L 7 2 4F A6WE 2001052400042 20010524 00042 WP 2001 5 24 GTIA010249 1 20010501 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 800NK 49144 DTW - FLT 656 - FOUND FLOOR TRACK LIGHTING OUT FROM ROW 16-23. UPON INSPECTION, FOUND LOOSE CONNECTION AT ROW 24. SECUR ED CONNECTION IAW MD-80 MM 33-53-01. OPS CHECK GOOD AT THIS TIME. NO DEFECTS NOTED. (M) 2 L 7 2 4F A6WE 2001052400043 20010524 00043 WP 2001 5 24 GTIA010247 1 20010429 A 2612 FIRE LOOP DOUG DC9 DC982 3022082 WP NR 1 ENGINE CHAFED A GTIA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 817NK 49141 FLL - FLT 781 - FOUND ENGINE NR 1 FIRE LOOP B ON. OPEN NR 1 ENGINE AND FOUND LOOP CHAFED TO GROUND POSITION. FIXED LOO P, CLOSED ENGINE COWL AND OPS CHECKED GOOD PER MM 26-10-00. (M) 2 L 7 2 4F A6WE 2001052400044 20010524 00044 WP 2001 5 24 GTIA010246 1 20010429 A 3260 WARNING SYSTEM DOUG DC9 DC981 3022081 WP COCKPIT MALFUNCTIONED A GTIA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 811NK 48017 EWR - FLT 456 - AT CRUISE, GEAR DOOR OPEN LIGHT COMES ON PUMPS ON HIGH LIGHT GOES OUT. PRESS BLEEDS DOWN LIGHT COMES BA CK ON. AFTER 20-30 MINUTES LIGHT GOES OUT. BITE TEST, NO MALFUNCTION ON THE GROUND CHECK AND CLEANED CANNON PLUG AND S ENSOR FOR GEAR BOX. OK TO CONTINUE MM 32-60-04. (M) 2 L 7 2 4F A6WE 2001052400045 20010524 00045 WP 2001 5 24 GTIA010244 1 20010429 A 3260 TARGET DOUG DC9 DC981 3022081 WP LT MLG DOOR OUT OF ADJ A GTIA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 811NK 48017 FLT 657 - RSW - FOUND GEAR DOOR OPEN ANNUNCIATOR ILLUMINATED AT 33,000, GEAR UP LIGHTS OUT. TURN PUMPS ON HIGH AND ON. ON LEFT MLG DOOR FOUND LEFT TARGET SENSOR GAP OUT OF LIMITS. ADJUSTED TARGET SENSOR TO LIMITS IAW MD-80 MM 32-50-05. (M) 2 L 7 2 4F A6WE 2001052400046 20010524 00046 2001 5 24 GTIA010243 4 20010429 A 2210 AUTOPILOT SYS DOUG DC9 DC983 3022083 WP COCKPIT MALFUNCTIONED A GTIA O OTHER O OTHER DE DESCENT 1 GL 23 822NK 49392 DTW - FLT 476 - DESCENDING INTO DTW, ALTITUDE ARMED, ALTITUDE DISARMED ITSELF WITHOUT PILOT INTO SHOWING TO 210 KTS AT 1 2,000 FT. AUTOPILOT WOULD NOT MAINTAIN ALTITUDE DFGC NR 1. CHECKED STP, NO FLIGHT FAULTS LOGGED, PERFORMED A RETURN TO SERVICE BIT CHECK OF BOTH DFGC''S SYSTEM. OPS CHECK GOOD IAW MD-80 MM 27-01-05. (M) 2 L 7 2 4F RT A6WE 2001052400047 20010524 00047 2001 5 24 GTIA010242 4 20010426 A 2210 AUTOPILOT SYS DOUG DC9 DC981 3022081 WP COCKPIT MALFUNCTIONED A GTIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 GL 23 811NK 48017 EWR - FLT 294 - GOING THROUGH 15,000 FT LOST AUTO PILOT, AUTO THROTTLE, YAW DAMPNER AND MACH TRIM. ALSO, ABILITY TO ADJ UST SPD/MACH AND LIGHTING ON FMA FOR ALTITUDE. TESTED DIGITAL FLIGHT GUIDANCE SYSTEM. RTS CHECK. ALL CHECK NORMAL PER MM 22-01-05. (M) 2 L 7 2 4F A6WE 2001052400048 20010524 00048 WP 2001 5 24 GTIA010241 1 20010426 A 2916 RESERVOIR DOUG DC9 DC981 3022081 WP HYD SYSTEM LACK OF LUBE A GTIA O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 811NK 48017 FLL - FLT 439 - FOUND GEAR DOOR OPEN LGIHT AT FL350. PLACED HYDRAULICS TO HIGH AND ON LIGHT EXTINGUISHED. SERVICED RT RESEVOIR TO FULL BLED AIR FROM SYSTEM OPS CHECK OK IAW 29-00-00 AND 32-00-00. (M) 2 L 7 2 4F A6WE 2001052400049 20010524 00049 WP 2001 5 24 GTIA010240 1 20010427 A 2741 SWITCH DOUG DC9 DC941 302207N WP HORIZ STAB OUT OF ADJ A GTIA O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 23 131NK 47605 ACY - FLT 807 - ON TAKEOFF ROLL, WARNING HORN SOUNDED. CONFIGURATION OK TRIM AT 1.6, HORN OFF WITH TRIM AT 2.0 OR GREAT ER. FLAPS 15, BRAKE OFF, SPOILER OFF. ADJUSTED HORIZONTAL STABILIZER. TAKEOFF WARNING SWITCH IAW MM 27-40-6. (M) 2 L 7 2 4F A6WE 2001052400050 20010524 00050 WP 2001 5 24 GTIA010238 1 20010425 A 3350 LIGHT DOUG DC9 DC987 3022087 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 807NK 49777 FLL - TWO ADJACENT GROUND PROX EMERGENCY LIGHTS INOPERATIVE AT ROW 12. REMOVED AND REPLACED EMERGENCY LIGHT BULBS AS RE QUIRED PER SPIRIT MM MD-80. (M) 2 L 7 2 4F RT A6WE 2001052400051 20010524 00051 WP 2001 5 24 GTIA010237 1 20010426 A 2750 CONTROL VALVE DOUG DC9 DC982 3022082 WP FLAPS DISCONNECTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FLL - FLAP CONTROL VALVE INPUT ROD DISCONNECTED IN LT MAIN W/W. RECONNECTED FLAP CONTROL VALVE IAW MM 27-52-02. OPS CH ECK GOOD. (M) 2 L 7 2 4F A6WE 2001052400052 20010524 00052 WP 2001 5 24 GTIA010236 1 20010426 A 2560 D21343101 LIFE VEST DOUG DC9 DC982 3022082 WP CABIN MISSING A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FLL - LIFEVEST MISSING FROM SEAT 20F. REPLACED MISSING LIFEVEST IAW MM 25-63-00. (M) 2 L 7 2 4F A6WE 2001052400053 20010524 00053 WP 2001 5 24 GTIA010235 1 20010425 A 2750 CONTROL CABLE DOUG DC9 DC982 3022082 WP LT FLAP BROKEN A GTIA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 GL 23 800NK 49144 FOUND LEFT W/W FLAP CONTROL EXTEND CABLE BROKEN. REMOVED AND REPLACED LEFT W/W FLAP CONTROL EXTEND CABLE IAW MD-80 MM 2 7-50-00. ALSO, RIGGED AND PERFORMED OPS CHECK IAW MM 27-50-00. (M) 2 L 7 2 4F A6WE 2001052400054 20010524 00054 WP 2001 5 24 GTIA010234 1 20010429 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 603CA 49508 DTW - FLT 656 - EMERGENCY FLOOR TRACK LIGHTING FROM ROW 33 AFT INOPERATIVE. FOUND EMERGENCY FLOOR TRACK LIGHTING DISCON NECTED AT ROW 33. RESECURED EMERGENCY FLOOR TRACK AT ROW 33. SYSTEM OPS CHECK GOOD IAW MD-80 MM 33-53-00. (M) 2 L 7 2 4F A6WE 2001052400055 20010524 00055 WP 2001 5 24 GTIA010233 1 20010426 A 2560 LIFE VEST DOUG DC9 DC983 3022083 WP CABIN MISSING A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 802NK 53168 DTW - FLT 476 - LIFEVEST MISSING AT SEAT 9F. REPLACED MISSING LIFE VEST AT SEAT 9F IAW MD-80 MM CHAPTER 25-61-00. (M) 2 L 7 2 4F RT A6WE 2001052400056 20010524 00056 WP 2001 5 24 GTIA010232 1 20010427 A 2560 P21343101 LIFE VEST DOUG DC9 DC983 3022083 WP CABIN MISSING A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 802NK 53168 DTW - LIFEVEST MISSING AT SEAT 11A. REPLACED MISSING LIFEVEST AT SEAT 11A IAW MD-80 MM CHAPTER 25-61-00. (M) 2 L 7 2 4F RT A6WE 2001052400057 20010524 00057 WP 2001 5 24 GTIA010231 1 20010426 A 2781 WARNING LIGHT DOUG DC9 DC982 3022082 WP COCKPIT ILLUMINATED A GTIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 23 800NK 49144 DTW - FLT 474 - AFTER FLAP RETRACTION SLAT DISAGREE LIGHT CAME ON. LEFT WING HEAVY CONTROLS REQUIRED. PERFORMED OPS CH ECK ON STALL AND FLAP SYSTEM IAW MM 34-19-00 AND 27-50-00. PERFORMED RTS AND FLIGHT FAULT REVIEW. NO DEFECTS NOTED. A LSO, PERFORMED SLAT TEST WITH SLAT DISAGREE BOX NO DEFECTS NOTED. OPS TEST GOOD. (M) 2 L 7 2 4F A6WE 2001052400058 20010524 00058 WP 2001 5 24 GTIA010228 1 20010424 A 3260 WARNING SYSTEM DOUG DC9 DC982 3022082 WP NLG MALFUNCTIONED A GTIA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 805NK 48087 ORD - FLT 220 - AFTER LANDING GEAR RETRACTED. THE NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. FOLLOWED QRH PROCEDURES A ND RECYCLED LANDING AND LIGHT WENT OUT AFTER GEAR WAS RETRACTED. INSPECTED NLG WHEEL WELL AREA AND SWITCHES. NO PROBLEM FOUND. PERFORMED PROXIMITY SWITCH ELECTRONIC UNIT TEST 32-60-04. TEST OPS CHECK OK. NO FAULTS FOUND, A/C GOOD FOR SERVI CE. (M) 2 L 7 2 4F A6WE 2001052400059 20010524 00059 WP 2001 5 24 GTIA010227 1 20010425 A 2611 WARNING SYSTEM DOUG DC9 DC981 3022081 WP CARGO BAY MALFUNCTIONED A GTIA K NONE N FALSE WARNING CR CRUISE 1 GL 23 806NK 48051 DTW - FLT 632 - CARGO SMOKE DETECTOR LIGHT CAME ON IN FLIGHT. AFT CARGO LOOP B DETECTOR LIGHT ALSO CAME ON. NO HORN, N O MASTER CAUTION, NO MASTER WARNING LIGHTS WENT OUT AFTER 2-3 MINUTES. PERFORMED CARGO SMOKE DETECTION SYSTEM CHECK, OP S CHECK GOOD IAW BARFIELD MM 26-16-00. NO FAULT FOUND. (M) 2 L 7 2 4F A6WE 2001052400060 20010524 00060 WP 2001 5 24 GTIA010225 1 20010423 A 3300 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 803NK 48087 ACY - PASSENGER O/H EMERGENCY AISLE LIGHTS INOPERATIVE FROM ROWS 4 TO 10 AND 29 TO 34. REMOVED AND REPLACED BATTERIES, OPS CHECK GOOD IAW MD-80 MM 33-51-00. (M) 2 L 7 2 4F A6WE 2001052400061 20010524 00061 WP 2001 5 24 GTIA010224 1 20010412 A 5320 ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - AFT STAIR LEFT SIDE SUPPORT ANGLE IS CRACKED. REMOVED DAMAGED ANGLE. FABRICATED NEW PART. (M) 2 L 7 2 4F RT A6WE 2001052400062 20010524 00062 WP 2001 5 24 GTIA010223 1 20010402 A 5753 FLAP DOUG DC9 DC931 3022065 WP LT WING CHAFED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 934ML 47526 FTW - LEFT FLAP INBOARD TRAILING EDGE CHAFING. REMOVED LEFT FLAP INBOARD TRAILING EDGE. (M) 2 L 7 2 4F A6WE 2001052400063 20010524 00063 WP 2001 5 24 GTIA010222 1 20010319 A 7110 COWLING DOUG DC9 DC931 3022065 WP NR 2 ENGINE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 934ML 47526 FTW - NR 2 ENGINE PYLON FIXED COWL CRACKED 3 PLACES. REMOVED EDGE MEMBER FROM ANGLE IAW DC-9 SRM 34-02. (M) 2 L 7 2 4F A6WE 2001052400064 20010524 00064 WP 2001 5 24 GTIA010221 1 20010410 A 2760 39246491 DRIVE LINK DOUG DC9 DC931 3022065 WP RT SPOILER CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 934ML 47526 FOUND RIGHT INBOARD SPOILER DRIVE LINK CRACKED. REMOVED DRIVE LINK IAW DC-9 MM 27-61-2 OK TO INSTALL DRIVE LINK. INSTA LLED DRIVE LINK IAW MM DC-9 27-61-2. (M) 2 L 7 2 4F A6WE 2001052400065 20010524 00065 NE 2001 5 24 R7MR32827 2 20010502 A 7250 410106701 SEAL RING BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE TURBINE SHROUD WORN E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 527RM 573 573 7111 WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2001052400067 20010524 00067 CE 2001 5 24 20010514CW008 1 20010418 A 7810 991029536 EXHAUST PIPE CESSNA 402 402B 207590P CE CONT O520 TSIO520* 17040 SO RT ENGINE DAMAGED E HBCA O OTHER R PARTIAL RPM/PWR LOSS AP APPROACH 1 SW 11 402BF 402B1076 WHILE ON FINAL APPROACH, THE PILOT REPORTED A LOSS OF MANIFOLD PRESSURE WITH THE RIGHT ENGINE. IT WAS FOUND THAT THERE WAS A HOLE APPROX 1.5 X 3.0 INCHES IN THE RIGHT ENGINE EXHAUST, MOST SPECIFICALLY FOCUSED AROUND THE NR 3 CYLINDER EXHA UST PIPE. THE EXHAUST STACK ASSEMBLY WAS REPLACED. 1 L 7 2 3O 3 O A7CE E8CE 2001052400068 20010524 00068 NM 2001 5 24 HN6R0000370 1 20010516 A 5753 654643489 SKIN BOEING 737 737400 NM T/E FLAP DEBONDED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 931NU 25247 DEBOND INDICATION NOTED: C LEFT WING INBOARD AFT FLAP LOWER SURFACE 11 INCHES FROM INBOARD END 1-6 INCHES FROM TRAILING EDGE APPROX 1.75 INCHES IN DIAMETER. REPAIRED DEBONDED SKIN. 2 L 7 2 4F RT A16WE 2001052400069 20010524 00069 NM 2001 5 24 HN6R0000371 1 20010516 A 5753 654643490 SKIN BOEING 737 737400 NM T/E FLAP DEBONDED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 931NU 25247 DEBOND INDICATION NOTED AT RIGHT WING INBOARD AFT FLAP UPPER SURFACE. 22 INCHES FROM TRAILING EDGE APPROX 2 INCHES IN D IA. REPAIRED SURFACE OF FLAP. 2 L 7 2 4F RT A16WE 2001052400070 20010524 00070 NM 2001 5 24 HN6R0000372 1 20010516 A 5753 6546435278 SKIN BOEING 737 737400 NM T/E FLAP DEBONDED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 931NU 25247 DEBOND INDICATION NOTED AT RIGHT WING OUTBOARD AFT FLAP UPPER SURFACE. 46 INCHES FROM INBOARD END. -4 DEGREES FROM TRA INING EDGE APPROX 1.5 INCHES IN DIA. REPAIRED UPPER SURFACE AT FLAP. CAUSE: UNKNOWN 2 L 7 2 4F RT A16WE 2001052400071 20010524 00071 NM 2001 5 24 HN6R0000546 1 20010516 A 5311 FRAME BOEING 737 737400 NM FUSELAGE CRACKED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 931NU 25247 CRACK INDICATION NOTED AT RS 178 LEFT HAND SIDE CHORD WL 207. REMOVED AND REPLACED LEFT HAND 178 BULKHEAD SIDE CHORD. 2 L 7 2 4F RT A16WE 2001052400072 20010524 00072 SO 2001 5 24 WVBA2001026 1 20010502 A 2752 475212 MOTOR PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA T/E FLAP FAILED E WVBA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 AL 01 3527U 2178 2178 317952141 PILOT REPORTED FLAPS STUCK IN DOWN POSITION, IT WAS DISCOVERED THAT THE FLAPS HAD STOPPED PRIOR TO HITTING THE DOWN LIMI T SWITCH AND WAS DETERMINED THAT THE MOTOR HAD BURNED OUT. THE UNIT WAS REMOVED AND REPLACED AND FLAP OPERATION APPEAR ED NORMAL. 1 L 7 2 3O 3 O A20SO E14EA 2001052400073 20010524 00073 SO 2001 5 24 WVBA2001030 1 20010510 A 2140 A23D04 REGULATOR PIPER PA31 PA31350 7103110 SO CABIN HEAT LEAKING E WVBA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 01 27755 290 290 317852148 UPON INSPECTING THE FUEL PRESSURE REGULATOR TO C/W AD 2001-8-1 IT WAS FOUND THAT THE REGULATOR WAS LEAKING PROFUSELY FRO M THE LOWER BODY PARTING SURFACES. REMOVED AND REPLACED UNIT, LEAK CHECK GOOD. 1 L 7 2 3O A20SO 2001052400074 20010524 00074 CE 2001 5 24 20010517CW001 1 20010412 A 5751 MS276455 BEARING LEAR 60 60LEAR 5170707 CE RT & LT AILERON DEFECTIVE B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 223FX 124 DURING A RESENT MAINTENANCE CHECK, AIRCRAFT PAINT AND REFURBISH, BOTH AILERONS WERE REMOVED FOR PAINT/BALANCE CHECK. TH E BEARINGS WERE FOUND DEFECTIVE. PROBABLE CAUSE: BEARINGS WERE DRY AND WERE VERY DIFFICULT TO MOVE, DUE TO LACK OF LU BRICATION. 2 L 7 2 4F RT A10CE 2001052400075 20010524 00075 SW 2001 5 24 20010517CW002 1 20010416 A 2611 327 LIGHT BELL 214 214ST 1182106 SW CARGO BAY INOPERATIVE E ALGA K NONE L NO TEST IN INSP/MAINT 1 SW 03 393AL 5801 28117 ON PRE-START CHECK, LEFT HAND BAGGAGE FIRE DETECTION SYSTEM WOULD NOT TEST, TEST LAMP BURNED OUT AND WIRE BROKEN ADJACEN T TO SMOKE DETECTOR. 2 G 7 2 4U H10SW 2001052400076 20010524 00076 GL 2001 5 24 20010517CW003 2 20010404 A 7200 ENGINE SKRSKY S76 S76 8143010 NE ALLSN 250C 250C30S 03013 GL NR 1 POWER LOSS E ALGR O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 SW 03 705AL 760267 CAE8900S ENROUTE, (55 MILES OUTBOUND) NR 1 ENGINE DROPPED OFFLINE, N1 DROPPED TO 36.8 PERCENT, T 5 DROPPED TO 580 DEGREES C AND T ORQUE TO 30 PERCENT, PC TUBE FOUND BROKEN AT THE PC FILTER END TUBE. 1 G 7 2 3U 3 U H1NE E1GL 2001052400079 20010524 00079 EU 2001 5 24 20010517CW004 1 20010419 A 2612 WIRE BOLKMS 105 BO105CBS 5626008 EU FIRE DETECTION BROKEN E K NONE O OTHER HO HOVERING 1 SW 03 5416F 794 WHILE HOVERING TO REFUELING POINT, WIRE BROKEN OFF AT A TERMINAL END FOR THE NR 1 LOWER SENSOR. 1 G 7 2 3U NC H3EU 2001052400080 20010524 00080 NM 2001 5 24 UIEA01044 1 20010421 A 5312 65B02534 BULKHEAD BOEING 747 747230B 1384889 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 509MC * 21221 DURING INSPECTION OF AFT PRESSURE BULKHEAD BS 2360 PER SB 747-53A2275 FOUND CRACK .75 INCH LONG ORIGINATING FROM FASTENE R HOLE FROM WEB TO Y-RING LAP JOINT BETWEEN STRINGER 24 AND 25R. CUT OUT CRACKED AREA. FABRICATED FILLER AND DOUBLER. OVERSIZED FASTENER HOLES AS NEEDED. INSTALLED FILLER AND DOUBLER PER STANDARD PRACTICES. (M) 2 L 7 4 4F A20WE 2001052400081 20010524 00081 NM 2001 5 24 UIEA01045 1 20010421 A 5310 PRESSURE PANEL BOEING 747 747230B 1384889 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 509MC 21221 DURING INSPECTION OF PRESSURE DECK NUMEROUS AREAS WERE FOUND WITH SPOT CORROSION BETWEEN BS 1460/1480 AT RBL 6, RBL 26.5 ; LBL 6, LBL 20, LBL 39, LBL 47.5. MOST AREAS BLENDED TO SRM LIMITS, TREATED AND FINISHED PER STANDARD PRACTICES. THE FOLLOWING AREAS WERE REPAIRED BY TRIMMING OUT THE CORRODED AREAS AT LBL 39, LBL 48. AT RBL 6; LBL 6 AND 20 CORROSION CR ACK WAS REMOVED BY STEP DRILLING AND SUBSEQUENTLY FREEZE PLUGS INSTALLED. FILLER SECTIONS AND REPAIR DOUBLERS WERE FABR ICATED FOR ALL ABOVE AREA. INSTALLED REPAIR FILLERS AND DOUBLERS PER STANDARD PRACTICES. (M) 2 L 7 4 4F A20WE 2001052400082 20010524 00082 NM 2001 5 24 UIEA01046 1 20010421 A 5330 SKIN BOEING 747 747230B 1384889 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 509MC * 21221 DURING HFEC INSPECTIN PER SB 747-53A2488 FOUND LOWER LOBE CARGO COMPT UPPER FORWARD DOOR CUT-OUT CRACKED 2MM. TRIMMED O UT CRACK. FABRICATED FILLER AND REPAIR DOUBLER. INSTALLED IAW SRM 53-30-03 TYPE 1 (SKIN CRACK ONLY). (M) 2 L 7 4 4F A20WE 2001052400083 20010524 00083 NM 2001 5 24 UIEA01047 1 20010426 A 5310 65B00006 DOOR FRAME BOEING 747 747230B 1384889 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 509MC * 21221 DURING HFEC INSPECTION PER SB 747-53A2488 FOUND UPPER AFT CARGO COMPARTMENT DOOR CUT OUT WITH CRACK INDICATION OF .5MM A T FASTENER HOLE UNDER AFT HINGE, AFT HOLE, LOWER ROW (SECOND LAYER). FASTENER IS OUT OF THE SB INSPECT AREA AND NOT SUB JECT TO REWORK PER ABOVE SB. INSTEAD, PER BOEING TELEX, FASTENER HOLE OVERSIZED UNTIL INDICATION DISAPPEARED. INSURANC E CUT BY REAMING HOLE TO .375 INCH DIAMETER. INSTALLED BACB30NN6K BOLT, NAS1805-6L NUT, BACW30BP6DP WASHER. (M) 2 L 7 4 4F A20WE 2001052400084 20010524 00084 NM 2001 5 24 UIEA01048 1 20010426 A 5230 65B042501 BEAM BOEING 747 747230B 1384889 NM CARGO DOOR CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 509MC * 21221 DURING INSPECTION OF LOWER AFT CARGO COMPARTMENT DOOR, FOUND CRACK 1.5 INCHES LONG ON LOWER FORWARD END OF LOWER EDGE BE AM. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLER. INSTALLED PER STANDARD PRACTICES IAW SRM 51-30. (M) 2 L 7 4 4F A20WE 2001052400085 20010524 00085 NM 2001 5 24 UIEA01049 1 20010426 A 5330 65B042501 SKIN BOEING 747 747230B 1384889 NM FUSELAGE CHAFED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 509MC * 21221 DURING INSPECTION OF LOWER FORWARD CARGO COMPARTMENT DOOR CUT OUT, FOUND FUSELAGE SKIN CHAFFED IN TWO AREAS AT THE AFT L OWER CORNER BETWEEN STRINGER 38/39R. POLISHED SKIN, HFEC INSPECTED, NO CRACKS. FABRICATED REPAIR DOUBLERS. INSTALLED PER STANDARD PRACTICES IAW SRM 51-30. (M) 2 L 7 4 4F A20WE 2001052400086 20010524 00086 NM 2001 5 24 UIEA01050 1 20010426 A 5414 65B9412824 SKIN BOEING 747 747230B 1384889 NM NR PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 509MC * 21221 DURING INSPECTION FOUND PYLON SKIN NR 4 POSITION CRACKED AT ACCESS DOOR R/S BETWEEN NAC 211.42 AND 222.50. TRIMMED OUT CRACKED AREA. HFEC AREA FOR ADDITIONAL CRACKING, NO CRACKS FOUND. FABRICATED FILLER AND REPAIR DOUBLER, INSTALLED SAME PER STANDARD PRACTICES SRM 51-30. (M) 2 L 7 4 4F A20WE 2001052400087 20010524 00087 NM 2001 5 24 UIEA01051 1 20010426 A 5753 65B170651 FLAP TRACK BOEING 747 747230B 1384889 NM T/E FLAP CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 509MC * 21221 DURING INSPECTION FOUND, NR 1 FLAP TRACK AFT INBOARD REAR SPAR ATTACH MOUNT HOLE CORRODED. REAMED HOLE OVERSIZE TO 1.13 9 FEET, FABRICATED BUSHING. INSTALLED BUSHING PER STANDARD PRACTICES. REINSTALLED WITH STANDARD SIZE HARDWARE. NR 3 F LAP TRACK BOTH REAR SPAR ATTACH HOLES CORRODED. REAMED HOLES OVERSIZED TO 1.285 INCH. FABRICATED BUSHINGS. INSTALLED PER STANDARD PRACTICES. REINSTALLED WITH STANDARD SIZE HARDWARE. (M) 2 L 7 4 4F A20WE 2001052400088 20010524 00088 NM 2001 5 24 USAASB01117 1 20010428 A 3350 LIGHT BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 438US 24560 TPA - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE FORWARD LEFT OVERWING LIGHT STATION 607L AND THE LEFT EXIT INDICATOR STATION 612L INOPERATIVE. (M) 2 L 7 2 4F RT A16WE 2001052400089 20010524 00089 NM 2001 5 24 USAABB01021 1 20010430 A 3350 9221009 BATTERY BOEING 757 7572B7 1384964 NM R3 DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 613AU 27144 MCO - FOUND R3 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2001052400090 20010524 00090 NM 2001 5 24 USAABB01022 1 20010501 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 626AU 27303 MCO - FOUND AISLE EMERGENCY LIGHTS AT ROWS 4, 6 AND 9 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2001052400091 20010524 00091 NM 2001 5 24 GAIA01156OP 1 20010501 A 2910 HYDRAULIC LINE BOEING 727 727224 1384076 NM HYD SYSTEM LEAKING A GAIA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 07 79748 22450 FLT 1850 - PDX-SEA - UPON LANDING GEAR EXTENSION, LOST A SYSTEM HYDRAULICS QUANTITY WENT TO ZERO. AIRCRAFT MADE AN UNEVE NTFUL LANDING IN SEA. INSPECTION OF AIRCRAFT FOUND LEAKING LEFT GEAR DOOR ACTUATOR RETURN HOSE. REMOVED AND LEFT ACTUA TOR RETURN HOSE. REMOVED AND REPLACED NR 1 AND NR 2 ENGINE DRIVEN HYDRAULIC PUMPS IAW B727 MM 29-11-31. SERVICED A SYSTE M. SYSTEM CHECKS GOOD IAW B727 MM 29-11-0. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001052400092 20010524 00092 NM 2001 5 24 USAASB01107 1 20010404 A 3350 900835A POWER SUPPLY BOEING 737 737201 1384454 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 261AU 22867 LGA - THE CENTER EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT POWER SUPPLY. (M) 2 L 7 2 4F A16WE 2001052400093 20010524 00093 NM 2001 5 24 USAASB01110 1 20010406 A 3350 900835A POWER SUPPLY BOEING 737 7372B7 1384560 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 273AU 22885 BWI - THE EXIT ROW OVERHEAD EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY . (M) 2 L 7 2 4F A16WE 2001052400094 20010524 00094 NM 2001 5 24 USAASB01111 1 20010409 A 3350 900835A POWER SUPPLY BOEING 737 7372B7 1384560 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 281AU 23114 BOS - THE OVERWING EMERGENCY EXIT CEILING LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY. (M) 2 L 7 2 4F A16WE 2001052400095 20010524 00095 WP 2001 5 24 GTIA010220 1 20010227 A 5520 BRACKET DOUG DC9 DC941 302207N WP ELEVATOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 131NK 47605 FTW - FOUND OUTBOARD MOUNTING BRACKET AT ELEVATOR POWER CONTROL FOLLOW UP MECHANISM CRACKED. REMOVED RIGHT OUTBOARD MOU NTING BRACKET, IAW DC-9 MM 27-30-3. (M) 2 L 7 2 4F A6WE 2001052400096 20010524 00096 WP 2001 5 24 GTIA010219 1 20010317 A 5313 LONGERON DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 131NK 47605 FTW - FOUND LONGERON 30 CORRODED AT FS 610. REMOVED OUT OF LIMITS SECTION IAW DC-9 SRM 51-30-2. DRILLED NEW SECTION OF LONGERON 30 IAW DC-9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2001052400097 20010524 00097 WP 2001 5 24 GTIA010218 1 20010317 A 5320 ATTACH ANGLE DOUG DC9 DC941 302207N WP G2 GALLEY CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 131NK 47605 FTW - FOUND FORWARD GALLEY G2 BASE COVER PANEL ATTACH ANGLES HAS CORROSION. REMOVED CORROSION, FOUND OUT OF LIMITS PER DC-9 SRM. FABRICATED ANGLES IAW DC-9 SRM. (M) 2 L 7 2 4F A6WE 2001052400098 20010524 00098 WP 2001 5 24 GTIA010217 1 20010317 A 5313 LONGERON DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 131NK 47605 FTW - FOUND CORROSION ON AND AROUND LONGERON NR 30 IN AREA BETWEEN FORWARD AUX FUEL TANK AND CENTER TANK. REMOVED OUTER AND INNER DOUBLER. REMOVED FRAME. INSTALLED LONGERON 30 END FITING. INSTALLED FRAMES. (M) 2 L 7 2 4F A6WE 2001052400099 20010524 00099 WP 2001 5 24 GTIA010216 1 20010317 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - MLG WHEEL WELL LEFT STATION 785-Z25 BETWEEN AFT BULKHEAD AND WIRING ROOT FRAME HAS A CRACK. REMOVED FRAME IAW BOE ING DC-9 SRM 51-10-2. FABRICATED FRAME IAW BOEING DC-9 SRM 51-10-02. (M) 2 L 7 2 4F RT A6WE 2001052400100 20010524 00100 WP 2001 5 24 GTIA010215 1 20010317 A 5320 ATTACH ANGLE DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 131NK 47605 FTW - FOUND RIGHT WING TO FUSELAGE ATTACH ANGLE CRACKED, LOCATED AT AREA2/ZONE 2 ACCESS 2214A. REMOVED ATTACH ANGLE IAW MM SRM DC-9 51-30-7. ATTACH ANGLE FOUND TO BE OUT OF LIMITS. INSTALLED NEW ANGLE IAW SRM DC-9 51-30-5. (M) 2 L 7 2 4F A6WE 2001052400101 20010524 00101 2001 5 24 GTIA010213 4 20010420 A 2565 D29985103 SLIDE DOUG DC9 DC981 3022081 WP L2 DOOR OUT OF POSITION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 UPON ARRIVAL, RAMP AGENT OPENED L2 DOOR IN WHICH SLIDE FELL TO THE GROUND AND BUSTED SLIDE PACK SHELL. REMOVED AND REPL ACE L2 SLIDE PACK IAW MD-80 MM 25-60-00. (M) 2 L 7 2 4F A6WE 2001052400102 20010524 00102 WP 2001 5 24 GTIA010212 1 20010414 A 3350 TRACK DOUG DC9 DC932 3022066 WP CABIN LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 133NK 48111 ACY - FLT 616 - FOUND EMERGENCY FLOOR LIGHTING STRIP LOOSE AT ROW 14. REINSTALLED LIGHTING TRACK, OPS CHECK GOOD IAW MM 33-53-00. (M) 2 L 7 2 4F A6WE 2001052400103 20010524 00103 2001 5 24 GTIA010211 4 20010420 A 3460 COMPUTER DOUG DC9 DC982 3022082 WP E/E BAY MALFUNCTIONED A GTIA O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 957AS 49126 FLL - FLT 679 - EN ROUTE NR 1 DFGC FAILED CREW SWITCHED TO NR 2 DFGC TO RESTORE NORMAL. FUNCTION PER FCOM PROCEDURES, Q RH PROCEDURES. AUTOPILOT AND AUTO THROTTLE SIMULTANEOUSLY DISENGAGED. TRANSFER TO DMI NR 0019634-3 NR 1 DFGC AS PER ME L 22-14-00. CAT ''C'' PLACARDS INSTALLED. (M) 2 L 7 2 4F A6WE 2001052400104 20010524 00104 2001 5 24 GTIA010210 4 20010422 A 2230 AUTOTHRUST SYS DOUG DC9 DC983 3022083 WP COCKPIT MALFUNCTIONED A GTIA K NONE O OTHER TO TAKEOFF 1 GL 23 822NK 49392 ORD - FLT 784 - AUTOTHROTTLE SYSTEM WILL NOT STAY ENGAGED WHEN USING AUTOPILOT NR 1 SYSTEM. WORKS NORMALLY IN AUTOPILOT NR 2 POSITION. ALSO ATS WILL NOT ENGAGE AT ALL ON TAKEOFF ROLL WITH A/P IN NR 1 POSITION. GROUND OPS CHECK GOOD IAW 7 8-03-00 MD-80 MM. (M) 2 L 7 2 4F RT A6WE 2001052400105 20010524 00105 WP 2001 5 24 GTIA010209 1 20010418 A 5240 ANGLE DOUG DC9 DC931 3022065 WP R1 DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 934ML 47526 FTW - FOUND R-1 DOOR BETWEEN BEAM NR 2 AND NR 3 SKIN ANGLE HAS CRACK. (M) 2 L 7 2 4F A6WE 2001052400106 20010524 00106 2001 5 24 GTIA010207 4 20010417 A 2230 AUTOTHRUST SYS DOUG DC9 DC983 3022083 WP COCKPIT MALFUNCTIONED A GTIA K NONE O OTHER DE DESCENT 1 GL 23 822NK 49392 AUTOTHROTTLE DISCONNECTED IN DESCENT AND WOULD NOT RECONNECT. REVIEW STP FOR APPLICABLE FAULTS. PERFORMED A/T MAINTENA NCE CHECK IAW MD-80 MM CH 22-31-00. NO DEFECTS NOTED. THIS CLEARS DMI NR 0001940. PLACARDS REMOVED. (M) 2 L 7 2 4F RT A6WE 2001052400107 20010524 00107 2001 5 24 GTIA010206 4 20010418 A 3460 COMPUTER DOUG DC9 DC982 3022082 WP E/E BAY MALFUNCTIONED A GTIA K NONE O OTHER DE DESCENT 1 GL 23 957AS 49126 FLL - FLT 679 - NR 1 DFGC WENT INTO RESET/TEST AT CRUISE KICKING OFF AUTO PILOT AND AUTO THROTTLES. THEN AGAIN ON DESCE NT. CARRY OUT DFGS STATUS/TEST. RETURN TO SERVICE IAW MM 22-01-05. CHECKED NORMAL. UNABLE TO DUPLICATE. (M) 2 L 7 2 4F A6WE 2001052400108 20010524 00108 NM 2001 5 24 GAIA01155OP 1 20010424 A 3230 659021132 ACCESSORY UNIT BOEING 727 727214 138407R NM E/E BAY FAILED A GTIA A UNSCHED LANDING O OTHER TO TAKEOFF 1 GL 23 750US 21512 FLT 710 - TOL-MKE - AFTER TAKEOFF FROM TOL, THE FLIGHT CREW FOUND THAT THE LANDING GEAR HANDLE WUOLD NOT MOVE PASSED THE OFF POSITION TO THE UP POSITION WITHOUT BYPASSING THE AIR GROUND SAFETY SWITCH. THE FLIGHT CREW DECIDED TO RETURN TO T OL. AN UNEVENTFUL LANDING WAS MADE. THE LANDING GEAR ACCY BOX WAS REMOVED AND REPLACED AND THE AIRCRAFT WAS TESTED IAW THE B727 MM CH 32-09. OPS CHECK WAS NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001052400109 20010524 00109 WP 2001 5 24 HALA0100100 1 20010424 A 2740 95906 TRIM MOTOR DOUG DC9 DC951 3022051 WP STABILIZER FAILED A HALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 WP 13 603DC 25472 2385 47784 HNL - FLT 139 - PRIMARY TRIM FAILED ON CLIMB, SECONDARY TRIM WORKED NORMALLY. PRIMARY TRIM DID WORK INTERMITTENTLY AFTE R INITIAL FAILURE. REPLACED PRIMARY TRIM MOTOR PER MM 27-40-1-401. OP CHECK OK. (M) 2 L 7 2 4F RT A6WE 2001052400110 20010524 00110 WP 2001 5 24 HALA0100103 1 20010424 A 2740 920710296 RELAY DOUG DC9 DC951 3022051 WP STABILIZER FAILED A HALA O OTHER F FLT CONT AFFECTED CL CLIMB 1 WP 13 603DC 47784 FLT 197 - HNL - ON CLIMB-OUT OF OGG, BOTH YOKE TRIM SWITCHES INTERMITTENT. SUITCASE HANDLES AND ALTERNATE TRIM LOOKED N ORMAL. REMOVED AND REPLACED NOSE DOWN RELAY R20-15 FOR PRIMARY LONG TRIM. ACCOMPLISHED ADJUSTMENT TEST PER MM 27-40-4- 501. OPS CHECK, ADJUSTED, TEST OK. (M) 2 L 7 2 4F RT A6WE 2001052400111 20010524 00111 WP 2001 5 24 HALA0100074 1 20010329 A 2611 473597404 SMOKE DETECTOR DOUG DC9 DC951 3022051 WP CARGO BAY MALFUNCTIONED A HALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 13 662HA 47742 LIH - FLT 232 - CARGO SMOKE ALARM ACTIVATED ABOUT 200 FEET AFTER TAKEOFF, BOTH FORWARD BAY FIRE PROTECTION SYSTEM SMOKE DETECTION CHANNELS INOPERATIVE. REMOVED AND REPLACED FORWARD CARGO SMOKE DETECTOR NR 4. OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 2001052400112 20010524 00112 CE 2001 5 24 20010524SG003 1 20010409 A 5520 1016200131 HINGE BRACKET BEECH 1900 1900C 1154161 CE LT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 187GA UC31 DURING SCHEDULED MAINTENANCE, LEFT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANUL AR CORROSION. REMOVED AND REPLACED LEFT OUTBOARD ELEVATOR HINGE BRACKET. (M) 2 L 7 2 4T RT A24CE 2001052400113 20010524 00113 CE 2001 5 24 20010524SG004 1 20010410 A 5520 1016200111 BRACKET BEECH 1900 1900C 1154161 CE RT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 187GA UC31 DURING ROUTINE MAINTENANCE, FOUND RIGHT CENTER ELEVATOR HINGE ATTACH BRACKET CORRODED. REMOVED AND REPLACED CENTER ELEV ATOR HINGE ATTACH BRACKET. (M) 2 L 7 2 4T RT A24CE 2001052400114 20010524 00114 CE 2001 5 24 20010524SG005 1 20010410 A 5511 10162001447 SPAR CAP BEECH 1900 1900C 1154161 CE HORIZ STAB CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 187GA UC31 AT SCHEDULED EMPENNAGE INSPECTION, DISCOVERED SOME EXFOLIATION CORROSION .5 INCH BY .125 INCH BY .020 INCH, ON LEFT HORI ZONTAL STABILIZER LOWER SPAR CAP ANGLE SIXTEEN INCHES FROM AIRCRAFT CENTERLINE. REMOVED CORRODED MATERIAL AND RE-PROTEC TED EXPOSED MATERIAL PER RAYTHEON ENGINEERING. (M) 2 L 7 2 4T RT A24CE 2001052400115 20010524 00115 CE 2001 5 24 20010524SG006 1 20010416 A 5520 1016200111 HINGE BRACKET BEECH 1900 1900C 1154161 CE RT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 1568W UC64 DURING SCHEDULED MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANU LAR CORROSION. REMOVED AND REPLACED RIGHT ELEVATOR OUTBOARD HINGE BRACKET. (M) 2 L 7 2 4T RT A24CE 2001052400116 20010524 00116 CE 2001 5 24 20010524SG007 1 20010416 A 5520 1016200111 HINGE BRACKET BEECH 1900 1900C 1154161 CE LT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 1568W UC64 DURING SCHEDULED MAINTENANCE, LEFT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANUL AR CORROSION. REMOVED AND REPLACED LEFT ELEVATOR OUTBOARD HINGE BRACKET. (M) 2 L 7 2 4T RT A24CE 2001052400117 20010524 00117 EA 2001 5 24 20010524SG008 2 20010418 A 7200 ENGINE DHAV DHC7 DHC7102 2802708 EA PWA PT6 PT6A50 52043 EA NR 1 FAILED A GUUA O OTHER Y ENGINE STOPPAGE NR NOT REPORTED 1 SO 19 706GA 53 PCE86401 FLT 1253 - HAV-MIA - EN ROUTE FROM HAVANA TO MIAMI, NR 1 ENGINE FAILED IN FLIGHT. REMOVED AND REPLACED NR 1 ENGINE. (M ) 2 H 7 4 4T 4 T A20EA E4EA 2001052400118 20010524 00118 SW 2001 5 24 20010517CW005 1 20010409 A 6320 407040034101 PINION GEAR BELL BELL 407 407 SW TRANSMISSION BROKEN E ALGA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 917AL 1998 A409 53381 CHIP LIGHT, EXCESSIVE METAL ON LOWER CHIP DETECTOR. FOUND INPUT PINION TO HAVE BROKEN TOOTH, CAUSING EXCESSIVE DAMAGE TO MAIN CASE. 1 G 7 1 3U O H2SW 2001052400119 20010524 00119 EA 2001 5 24 20010517CW006 1 20010503 A 2710 2772553101 TOGGLE CNDAIR CL600 CL6002B16 1900305 EA AILERON WORN B SH5R K NONE O OTHER IN INSP/MAINT 1 GL 03 914X 3281 5185 BEARING SPINNING IN AILERON TOGGLE LINK. 2 L 7 2 4F RT A21EA 2001052400120 20010524 00120 EU 2001 5 24 20010517CW007 1 20010313 A 7110 FGFB581200D2 COWLING AMD FALC90 FALCON900EX 2730009 EU NR 1 ENGINE SEPARATED B UO2R O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 GL 19 312P 228 067 NR 1 LOWER COWLING, PN FGFB581200D2 FELL OFF IN FLIGHT 3-12-2001. LOST COWLING NOT YET RECOVERED AS OF 3-13-2001 2 L 7 3 4F RT A46EU 2001052400121 20010524 00121 EU 2001 5 24 20010517CW008 1 20010221 A 4940 APU HWKSLY DH125 BH125400A 4230138 EU APU BAY MALFUNCTIONED E AJ6A F ACTIVATE FIRE EXT. A FLAME/FIRE NR NOT REPORTED 1 GL 23 800TG NA780 INTERRUPTION TO A FLIGHT, UPON ARRIVAL , START ATTEMPT OF APU AFTER FIRST ATTEMPT FAILED TO LIGHT, CAUSED A FIRE IN EXH AUST PIPE. APU FIRE BOTTLE WAS EXPENDED, FIRE EXTINGUISHED, FIRE DEPARTMENT SPRAYED PKP WHICH REQUIRED INSPECTION AND A PU AND APU FIRE BOTTLE DEFERRAL PRIOR TO AIRCRAFT RETURNING. 2 L 7 2 4J A3EU 2001052400122 20010524 00122 NM 2001 5 24 HN6R0000172 1 20010516 A 5315 FLOORBEAM BOEING 737 737400 NM FUSELAGE CORRODED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 931NU 25247 CORROSION ON TOP AND BOTTOM SIDE OF TOP FLANGE OF FLOOR BEAM. BS 312, WL 208, RBL 45 TO LBL 25. REMOVED , FABRICATED, AND REPLACED 25 T CHORD ON FLOOR BEAM ER 01-0287. 2 L 7 2 4F RT A16WE 2001052400123 20010524 00123 NM 2001 5 24 HN6R0000177 1 20010516 A 5315 FLOORBEAM BOEING 737 737400 NM FUSELAGE CORRODED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 931NU 25247 CORROSION ON TOP FLANGE OF FLOOR BEAM. BS 328, WL208, RBL 10 FOR RBL 50. REMOVED AND REPLACED SECTION OF TOP FLANGE ER 01-0286. 2 L 7 2 4F RT A16WE 2001052400124 20010524 00124 NM 2001 5 24 HN6R0000180 1 20010515 A 5315 FLOORBEAM BOEING 737 737400 NM FUSELAGE CORRODED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 931NU 25247 CORROSION ON TOP OF FLOORBEAM. BS 344, WL 208, LBL 65 TO RBL 15. FABRICATED AND REPLACED SECTION OF FLOORBEAM ER 01-02 86 2 L 7 2 4F RT A16WE 2001052400125 20010524 00125 NM 2001 5 24 20010524SG001 1 20010428 A 2611 308 LIGHT BOEING 727 72751C 1384015 NM SMOKE DETECTOR INOPERATIVE A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 417EX 19290 FOUND UPPER LEFT LIGHT BULB IN MAIN CABIN SMOKE DETECTOR IS BURNED OUT. REMOVED AND REPLACED LEFT AND RIGHT BULBS IN MA IN CABIN SMOKE DETECTOR. (M) 2 L 7 3 4F A3WE 2001052400126 20010524 00126 WP 2001 5 24 GTIA010214 1 20010422 A 4990 APU DOUG DC9 DC981 3022081 WP APU BAY LACK OF LUBE A GTIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 23 810NK 48015 ACY - FLT 1143 - APPROX 3 MINUTES AFTER STARTING APU INFLIGHT, APU OIL TEMP HIGH LIGHT CAME ON. PERFORMED QRH PROCEDURE S VRF. DIVERTED TO ACY, NO OVERWEIGHT LANDING. SERVICED APU OIL IAW 12-12-01. SYSTEM OPS CHECK GOOD PER MM. (M) 2 L 7 2 4F A6WE 2001052400127 20010524 00127 NE 2001 5 24 GAIA01154OP 2 20010420 A 7200 ENGINE BOEING 727 727223 1384074 NM PWA JT8 JT8D9A 52048 NE NR 2 VIBRATION A GTIA E A ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 GL 23 858AA 21085 687792 FLT 1804 - PHX-FWA - WHILE AT CRUISE AT 35,000 FEET, NR 2 ENGINE BEGAN VIBRATING AND MAKING NOISE AS NR 2 THROTTLE WAS R ETURNED TO IDLE, AND THE EGT INCREASED. THE CREW ACCOMPLISHED A PRECAUTIONARY ENGINE SHUT DOWN, DECLARED AN EMERGENCY, AND PROCEEDED TO LAND AT MCI. THE AIRCRAFT LANDED AT MCI WITHOUT ANY FURTHER DIFFICULTIES. THE AIRCRAFT WAS MAINTENANC E FERRIED TO DFW. THE NR 2 ENGINE WAS REMOVED AND REPLACED IAW KHA MCM AND OPS CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F 4 F A3WE E2EA 2001052400128 20010524 00128 CE 2001 5 24 20010524SG002 1 20010420 A 3150 WARNING SYSTEM BEECH 1900 1900C 1154161 CE COCKPIT MALFUNCTIONED A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 19 151GA UC171 FLT 9401 - JAX-TPA - DURING FLIGHT, FIRE DISCHARGE LIGHT ILLUMINATED. SECURED CANNON PLUG AT LEFT DISCHARGE LIGHT ASSEM BLY. (M) 2 L 7 2 4T RT A24CE 2001052400129 20010524 00129 NM 2001 5 24 HN6R0000151 1 20010516 A 5320 SILL BOEING 737 737400 NM FUSELAGE CORRODED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 931NU 25247 BS 270 TO 344, WL 208, RBL51 TO 63 MOP SILL CORRODED. REMOVED AND REPLACED MOP SILL. 2 L 7 2 4F RT A16WE 2001052400130 20010524 00130 CE 2001 5 24 20010510CW005 1 20010409 A 5210 HANDLE BEECH 1900 1900D 1154162 CE PAX DOOR OBSTRUCTED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 842CA UE41 DOOR HANDLE HAD TO BE FORCED TO THE LOCK POSITION AS A RESULT OF RESTRICTION BETWEEN DOOR WELD AND BUSHING AT CENTER DOO R HANDLE. 2 L 7 2 4T RT A24CE 2001052400132 20010524 00132 EA 2001 5 24 20010511CW004 2 20010427 A 7314 RG9080J7A GASKET PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA FUEL PUMP LEAKING G DRUA O OTHER A FLAME/FIRE LD LANDING 1 GL 25 4078L 1009 1009 318152060 DURING LANDING ROLLOUT, AN EXPLOSION AND FIRE OCCURRED IN LEFT ENGINE. EXAMINATION FOUND THE FUEL PUMP RELIEF VALVE COV ER GASKET LEAKING FUEL. AD AND SB HAD BEEN ACCOMPLISHED SEVERAL HUNDRED HOURS AGO. THE DAMAGE WILL REQUIRE REPLACEMENT OF ALL ENGINE ASSEMBLY, ENGINE, TURBOMOUNT, TOP COWL. PUMP WAS RECEIVED NEW WITH ENGINE. 1 L 7 2 3O 3 O A20SO E14EA 2001052400134 20010524 00134 CE 2001 5 24 20010511CW006 1 20010423 A 2140 654316C RING CONT BEECH 36 B36TC 1151609 CE CONT O520 TSIO520UB 17040 SO CABIN HEATER CRACKED B AKGR K NONE O OTHER IN INSP/MAINT 1 CE 05 74MT 115 EA659 527505 IN COMPLETING ANNUAL INSPECTION, CABIN HEATER ASSEMBLY WAS REMOVED FOR LEAK INSPECTION. FOUND ONE OF MUFF SUPPORT RINGS CRACKED HALF WAY AROUND. IF THIS WOULD HAVE CRACKED ALL THE WAY OFF THE EDGE WOULD HAVE CUT THROUGH EXHAUST PIPE PART OF MUFF, THIS WOULD LET CO INTO THE CABIN. 1 L 7 1 3O 3 O 3A15 E8CE 2001052400135 20010524 00135 CE 2001 5 24 20010509CW003 1 20010412 A 2913 99144603 PUMP CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL ENGINE FAILED C NOZA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 WP 23 22NG 2866 2866 7500039 AC ON DECENT WHEN AMBER EICAS INDICATION OF HYD VOLUME LOW(A) ILLUMINATED. FLIGHT CREW CONFIRMED THE EICAS INDICATION WA S AN ACTUAL PROBLEM BY VIEWING EICAS WHICH SHOWED, HYD LEVEL AT 16 PERCENT AND DECREASING. PRESSURE DROPING AND FLUID TE MP INCREASING. FLIGHT CREW FOLLOWED THE ABNORMAL CHECK LIST AND ELECTED TO DIVERT. WEATHER WAS VMC, VISUAL APPROACH TO R UNWAY 30 WAS REQUESTED AND APPROVED. FLIGHT CREW HAD REQUESTED EMERGENCY EQUIPEMNT TO BE STANDING BY BUT DID NOT FEEL IT NECESSARY TO DECLARE AN EMERGENCY. THE LANDING GEAR WAS EXTENDED BY THE ALTERNATE PROCEDURE BLOW DOWN AND AN UNEVENTFU L LANDING WAS MADE WITH THE USE OF PNEUMATIC EMERGENCY BRAKING AND STEERING ACCUMULATOR. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2001052400136 20010524 00136 CE 2001 5 24 20010509CW004 1 20010402 A 5520 1016200113 HINGE BRACKET BEECH 1900 1900C 1154161 CE ELEVATOR CORRODED B TIMR K NONE O OTHER IN INSP/MAINT 1 NM 07 172GA 31542 UB11 DURING INSPECTION, THE RIGHT OUTBOARD AND THE RIGHT MIDDLE ELEVATOR HINGE BRACKET WERE FOUND TO BE CORRODED. 2 L 7 2 4T RT A24CE 2001052400137 20010524 00137 CE 2001 5 24 20010509CW005 1 20010402 A 5320 1144301169 INTERCOSTAL BEECH 1900 1900C 1154161 CE FUSELAGE CRACKED B TIMR K NONE O OTHER IN INSP/MAINT 1 NM 07 172GA 31542 UB11 P43 INSPECTION FOUND A .8 INCH CRACK IN THE OUTDBOARD FLANGE RADIUS OF THE INTERCOSTAL AT THE UPPER CARGO DOOR FRAME A T FS 494. 2 L 7 2 4T RT A24CE 2001052400138 20010524 00138 CE 2001 5 24 20010509CW006 1 20010402 A 5511 10162001448 SPAR CAP BEECH 1900 1900C 1154161 CE HORZ STAB CORRODED B TIMR K NONE O OTHER IN INSP/MAINT 1 NM 07 172GA 31542 UB11 FOUND THE OUTBOARD 6 INCHES LOWER RIGHT REAR SPAR CAP EXTRUSION CORRODED. CORROSION WAS FOUND WHILE REPLACING A CORRODE D OUTBOARD ELEVATOR HINGE BRACKET. 2 L 7 2 4T RT A24CE 2001052400139 20010524 00139 NE 2001 5 24 GTIA010245 2 20010428 A 7230 COMPRESSOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE NR 2 ENGINE STALLED A GTIA O OTHER R E PARTIAL RPM/PWR LOSS VIBRATION/BUFFET CR CRUISE 1 GL 23 803NK 48087 MYR - FLT 7200 - SHUTDOWN NR 2 ENGINE DUE TO COMPRESSOR STALL AND VIBRATION. (M) 2 L 7 2 4F 4 F A6WE E9NE 2001052400140 20010524 00140 WP 2001 5 24 GTIA010239 1 20010426 A 3350 COVER DOUG DC9 DC987 3022087 WP CABIN LOOSE A GTIA K NONE O OTHER CR CRUISE 1 GL 23 807NK 49777 FLL - FLT 525 - FOUND AISLE PATH LIGHTING LOOSE ROW 12. RESECURED COVER ON FLOOR PATH LIGHTING ROW 12 CHECK OK. (M) 2 L 7 2 4F RT A6WE 2001052400141 20010524 00141 2001 5 24 GTIA010226 4 20010423 A 2210 CONTROL UNIT DOUG DC9 DC941 302207N WP AUTOPILOT SYS INOPERATIVE A GTIA K NONE O OTHER CR CRUISE 1 GL 23 130NK 47604 FLL - FLT 41 - AUTOPILOT PITCH CONTROL IS INOPERATIVE. TRANSFERRED TO CMI NR 0019690-3. CAT C MEL 22-10. PLACARD INST ALLED. (M) 2 L 7 2 4F A6WE 2001052400142 20010524 00142 CE 2001 5 24 20010509CW007 1 20010130 A 5510 1016200113 HINGE BRACKET BEECH 1900 1900C 1154161 CE ELEVATOR CORRODED B TIMR K NONE O OTHER IN INSP/MAINT 1 NM 07 154GA UB25 UPON INSPECTION OF RIGHT HAND OUTBOARD HORIZONTAL STABILATOR ELEVATOR HINGE BRACKET, A BADLY EXFOLIATED BRACKET WAS FOUN D. 2 L 7 2 4T RT A24CE 2001052400144 20010524 00144 CE 2001 5 24 20010511CW009 1 20010426 A 7910 HOSE CESSNA 425 425 2076018 CE PWA PT6 PT6A112 52043 NE OIL SYSTEM RUPTURED G O OTHER K FLUID LOSS CR CRUISE 1 SO 01 5CE 300 4250135 HOSE PN 156F001-12D0196 MANUFACTURED IQ99 INSTALLED 3, 00 RUPTURED IN FLIGHT DUMPING OIL ON LEFT ENGINE. 1 L 7 2 3T 3 T RT A7CE E4EA 2001052900002 20010529 00002 EA 2001 5 29 COMA0160373 1 20010513 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 973CA 11350 7146 FLOORBEAM WEB AT FS 280.00 IS CORRODED ON THE UPPER EDGE BETWEEN RBL 9 AND LBL 9. REMOVED FWD J-ANGLE, TRIMMED OUT CORR ODED AREA OF WEB, FABBED FILLER, REPAIR DOUBLER AND INSTALLED IAW WVAC EO WVAC 601R-53-2455A. 2 L 7 2 4F RT A21EA 2001052900003 20010529 00003 EA 2001 5 29 COMA0160374 1 20010513 A 5320 60034017357 ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 973CA 11350 7146 FWD J-ANGLE AT FS 280.00 BETWEEN LBL 9 AND RBL 9 IS CORRODED. REMOVED DAMAGED J-ANGLE AND INSTALLED NEW FORWARD J-ANGLE IAW WVAC EO 601R-53-2451. 2 L 7 2 4F RT A21EA 2001052900004 20010529 00004 EA 2001 5 29 COMA0160375 1 20010513 A 5315 6003401717 FLOORBEAM CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 973CA 11350 7146 FLOOR MEMBER AT FS 280.00 IS CRACKED JUST RIGHT OF FLOOR SUPPORT AT RBL 9. TRIMMED OUT CRACKED AREA IN FLOOR MEMBER, LP I CHECKED, FABBED REPAIR ANGLE AND INSTALLED IAW WVAC EO 601R-53-2450. 2 L 7 2 4F RT A21EA 2001052900005 20010529 00005 EA 2001 5 29 COMA0160376 1 20010513 A 5320 60034017373 ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 973CA 11350 7146 VERTICAL J-ANGLE CLIP INSIDE CBPI AT LBL 9 IS CRACKED. REMOVED AND REPLACED ANGLE IAW WVAC EO 601R-53-2449. 2 L 7 2 4F RT A21EA 2001052900006 20010529 00006 NE 2001 5 29 C2XA01CL102 2 20010510 A 7200 310450001 ENGINE AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE NR 1 FAILED A C2XA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 27 97841 24236 5913 280 121117 CLE FLIGHT 3031 THE CREW REPORTED SMOKE SMELL ON APPROACH TO CLEVELAND. MAINTENANCE INSPECTED AND FOUND THE NR 1 ENGINE TO BE LEAKING OIL INTERNALLY. THE NR 1 ENGINE WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASE D FOR SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2001052900007 20010529 00007 WP 2001 5 29 RRXA011042 1 20010501 A 5730 ARC0163504 PANEL DOUG DC10 DC1030F 3023504 WP RT WING DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 831LA 46936 PANEL ON RIGHT WING AFT OF NR 3 ENG IS REMOVED DUE TO SHEETMETAL DAMAGE OF PANEL. REMOVED AND REPLACED PNL PER DC-10 M/ M 53-30-00 SEALED PNL PER DC-10 M/M 20-00-00. 2 L 7 3 4F RT A22WE 2001052900008 20010529 00008 WP 2001 5 29 RRXA011043 1 20010503 A 5350 FAIRING DOUG DC10 DC1030F 3023504 WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 47816 47816 AFTER OFF LOAD, DISCOVERED DAMAGE TO ACFT WING/FUSELAGE FAIRING APPROX 30 INCHES FWD OF CENTER CARGO DOOR FWD EDGE. REP AIRED DAMAGED FORMED ANGLE COMMON TO THE WING/FUSELAGE FAIRING AT AREA NOTED AS PER GUIDELINES IN THE DC-10 SRM CHAPTER 51 STANDARD PRACTICES AND 53-00-01 FIG 8. 2 L 7 3 4F RT A22WE 2001052900009 20010529 00009 NM 2001 5 29 ERKR200100121 1 20010514 A 5320 INTERCOSTAL BOEING 747 747128 1384894 NM FUSELAGE DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 REPAIR OF INTERCOSTAL CHORD FWD AND AFT ENDS STA 1265, RBL 101 AND WL 199. THIS DOCUMENT PROVIDES REPAIR INSTRUCTIONS F OR THE DISPOSITION OF THE USE OF TWO LARGER FASTENERS IN LIEU OF TWO DRAWING FASTENERS COMMON TO THE FOWARD AND AFT INTE RCOSTAL CHORD ENDS. THE CHORDS WILL BE TRIMMED TO ALLOW THE LOWER ADJACENT FASTENER TO BE INSTALLED PER ECRA 3203-53-36 -2. 2 L 7 4 4F A20WE 2001052900010 20010529 00010 NM 2001 5 29 ERKR200100122 1 20010514 A 5311 65B05002185 FRAME BOEING 747 747128 1384894 NM FUSELAGE CRACKED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 REPAIR OF CRACKED OUTBOARD FLANGE OF UPPER PARTIAL FRAME, STA 806 S-18L. REPAIR OF CRACKED OUTBOARD FLANGE OF 65B05002- 185 UPPER PARTIAL FRAME AT STA 806 (FWD EDGE OF L2 DOOR FRAME), STRINGER 18L. CONSISTS OF REMOVING AND DISCARDING 65B05 002-4 RADIUS FILLER, TRIMMING OUT THE CRACK, INSTALLING A NET FIT FILLER AND AN INTERNAL DOUBLER PER ECRA 3203-53-038-2. 2 L 7 4 4F A20WE 2001052900011 20010529 00011 WP 2001 5 29 ZW0A0101604 1 20010510 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 924TW 49100 DURING CHECK-C MAINT IN THE FWD CARGO COMPT FOUND CRACK IN FLOOR SUPPORT ANGLE ON THE FORMER AT STA 446, BETWEEN LONGERO N 26L AND 27L. REPAIRED PARTS IN SHOP PER SSRM 53-00-106. INSTALLED PER SRM 51-30-2. 2 L 7 2 4F A6WE 2001052900012 20010529 00012 NM 2001 5 29 ERKR200100123 1 20010514 A 5330 SKIN BOEING 747 747128 1384894 NM FUSELAGE DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 REPAIR- FUSELAGE SKIN - FWD AND ABOVE NR 1 MAIN ENTRY DOOR. THIS REPAIR CONSISTS OF TRIMMING OUT THE DAMAGE AND INSTALL ING A MODIFIED SRM REPAIR, EXTERNAL SKIN DOUBLER, TRIPLER AND A SPLICE ARE FABRICATED AND FIT TO CORRECT THE DISCREPANT CONDITION PER ECRA 3203-53-39-2. 2 L 7 4 4F A20WE 2001052900013 20010529 00013 NM 2001 5 29 ERKR200100124 1 20010514 A 5311 65B01715170 FRAME BOEING 747 747128 1384894 NM FUSELAGE DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 REPAIR OF DAMAGED FRAME OUTER CHORD, STA 440, S-9R TO S-14R. THIS CONSISTS OF CUTTING AND SPLICING THE EXISTING 65B0171 5-170 FRAME BETWEEN STRINGERS 9 AND 10 AND REMOVING AND REPLACING THE FRAME SEGMENT LOCATED BELOW THE CUT TO THE EXISTIN G SPLICE LOCATED AT STRINGER 13A. REPAIR OF SHORT EDGE CONDITION EXISTING ON SKIN DOUBLER SPLICE PLATE LOCATED BETWEEN S-12R AND S-13R CONSISTS OF FABRICATING AND INSTALLING A NEW ONE IN PLACE OF THE ORIGINAL PER ECRA 3203-53-041-2. 2 L 7 4 4F A20WE 2001052900014 20010529 00014 NM 2001 5 29 ERKR200100125 1 20010514 A 5414 SKIN BOEING 747 747128 1384894 NM NACELLE DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 REPAIR- ENGINE STRUT NR 4, RIGHT SKIN DAMAGE-NAC STA 236.5. THIS DAMAGE IS IN A PREVIOUSLY REPAIRED AREA AT NAC STA 236 .5 AND COMMON AND TO THE LOWER EDGE OF THE SKIN. THE PREVIOUSLY INSTALLED REPAIR DOUBLER WAS DAMAGED. THIS REPAIR REPL ACES THE DAMAGED REPAIR DOUBLER WITH A NEW LARGER DOUBLER TO ADDRESS THE INCREASED DAMAGE SIZE PER ECRA 3203-54-024-2. 2 L 7 4 4F A20WE 2001052900015 20010529 00015 NE 2001 5 29 SWIA972563 2 20010513 A 7321 EEC EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RN 2 ENGINE FAILED A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 204SW 120243 NR 2 EEC FAILED ON TAKEOFF. ABORTED THE TAKEOFF. PERFORMED RIGHT ENGINE RUNS, EEC FAILED ON GROUND. OHMED EEC SYSTEM. FOUND HMU WIPER BAD. REPLACED RIGHT ENGINE HMU IAW EMB120 MM 73-21-00. PERFORMED RIGHT ENGINE RUNS. NO FURTHER DISC REPANCIES ON GROUND. OPS CHECKS GOOD AND NO LEAKS NOTED. P/N ON 786390-4, S/N ON F7586, S/N OFF F19962, S/N OFF 786390 -10. 2 L 7 2 4T 4 T RT A31SO E20NE 2001052900016 20010529 00016 EA 2001 5 29 SWIA972564 1 20010511 A 7830 ACTUATOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE THRUST REVERSER DEFECTIVE A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 403SW 7028 LEFT THRUST REVERSER UNLOCK CAUTION MESSAGE AT 1000 FEET AGL AFTER TAKEOFF. NO AUTO LEVER RETARD AND NO BUFFET. RETURN ED TO FIELD. LEFT REV UNLOCK LIGHT CAME ON AT TOP OF DESCENT AND STAYED ON UNTIL ENGINE SHUT DOWN. INSPECTED THE LEFT THRUST REVERSER FOUND THAT IT WAS CLOSED AND DID NOT APPEAR TO HAVE MOVED TOWARDS THE OPEN POSITION. FOUND THE LEFT REV EMERGENCY SWITCH LIGHT TO BE DIRTY. CLEANED THE SWITCH AND OPERATED THE REVERSER ON THE GROUND. REMOVED AND REPLACED LT LOWER INBOARD THRUST REVERSER BALLSCREW ACTUATOR. RIGGED AND ADJUSTED IAW MM 78-32-01. OPS CHECK GOOD REPEATEDLY. P/N ON 3272570-6, S/N ON 3085, S/N OFF 1774C. 2 L 7 2 4F 4 F RT A21EA E15NE 2001052900017 20010529 00017 EA 2001 5 29 SWIA972565 1 20010510 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT CRACKED A SWIA K NONE O OTHER DE DESCENT 1 NM 07 903SW 7425 ON DESCENT INTO DEN CAPTAINS WINDSHIELD SHATTERED, APPEARED TO BE MIDDLE LAYER. REPLACED CAPTAINS WINDSHIELD IAW CRJ MM 56-11-01 AND SKYWEST CARD RII 56-401. OPS CHECK GOOD ON GROUND. P/N ON: NP-139321-9 S/N ON: 01043H9715 P/N OFF: 601R33033-9 S/N OFF: 00111H5787. 2 L 7 2 4F 4 F RT A21EA E15NE 2001052900018 20010529 00018 EA 2001 5 29 SWIA972567 1 20010513 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT CRACKED A SWIA K NONE O OTHER AP APPROACH 1 NM 07 426SW 7468 RIGHT FIRST OFFICERS WINDSHIELD CRACKED ON FINAL APPROACH. REMOVED AND REPLACED THE RIGHT WINDSHEILD ASSEMBLY IAW RII 5 6-401 AND MM 56-11-01. LEAK AND OPS CHECKS GOOD. P/N ON PPGNP-13921-10, S/N ON 01095H5012, S/N OFF 00083H3537. 2 L 7 2 4F 4 F RT A21EA E15NE 2001052900019 20010529 00019 SO 2001 5 29 C2XA01IA244 1 20010509 A 5713 12016079002 STRINGER EMB 120 EMB120ER 3260203 SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 57734 120199 SJK - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, STRINGER 8 ON THE RIGHT WING WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE CRACKED STRINGER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001052900020 20010529 00020 SO 2001 5 29 C2XA01IA245 1 20010403 A 5411 12003852001 FRAME EMB 120 EMB120ER 3260203 SO LT & RT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 57734 120199 SJK - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FRAME 1 ON THE LEFT HAND AND RIGHT HAND NACELLES WERE FOUND TO BE C RACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FRAMES, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001061500088 20010615 00088 NM 2001 6 15 01FDEA00344 1 20010514 A 5714 WEB BOEING 727 72722 1384002 NM WINGBOX CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 DURING ROUTINE INSP CTR WING BOX FOUND CORRODED AT BS 870 NEXT TO LWR SPAR CHORD. *S/D* REMOVED AND REPLACED PER IAW F EDEX EA 7-5710-57245. 2 L 7 3 4F A3WE 2001070200028 20010702 00028 NM 2001 7 2 01FDEA00345 1 20010514 A 5330 SKIN BOEING 727 72722 1384002 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 DURING ROUTINE INSP FUSELAGE SKIN FOUND BULGING and CORRODED FROM BS 1154 - 1180 AT STR 19L. *S/D* Removed and replace d PER IAW FEDEX EA 7-5710-57242. 2 L 7 3 4F A3WE 2001061500089 20010615 00089 NM 2001 6 15 01FDEA00346 1 20010514 A 5330 SKIN BOEING 727 72722 1384002 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 DURING ROUTINE INSP FUSELAGE SKIN FROM BS 1166 - 1173 BETWEEN STR 20L & STR 21L FOUND BULGING AND CORRODED. *S/D* REMO VED AND REPLACED PER IAW FEDEX EA 7-5710-57242. 2 L 7 3 4F A3WE 2001052900021 20010529 00021 EU 2001 5 29 01FDEA00348 1 20010515 A 7830 WARNING SYSTEM AIRBUS 300 A300F4605R 3930327 EU COCKPIT ACTIVATED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 675FE 789 NR 2 REVERSER PRESSURED ECAM WARNING CAME ON AT 75 KIAS T/O ROLL. 2 L 7 2 4F RT A35EU 2001052900022 20010529 00022 CE 2001 5 29 GLBA2001099 1 20010511 A 6120 1013645801 CIRCUIT BOARD BEECH 1900 1900D 1154162 CE PROP CONTROL DEFECTIVE A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 255GL 9328 UE255 AFX DISABLE ANNUNCIATOR ILLUMINATED. INSPECTED FOUND BROKE WIRE W184A22 BY CAPTAINS LEFT LEG. ALSO REPLACED PCB, OPS C HECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001052900023 20010529 00023 NE 2001 5 29 XNA01009 2 20010515 A 7200 ENGINE AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE RIGHT MALFUNCTIONED A TC8A E ENGINE SHUTDOWN O OTHER CR CRUISE 1 GL 23 472AS 47876 2498 125 517510 LOUD BANG RIGHT ENGINE AT 16000 FT. EGT WENT TO RED LINE. SHUT ENGINE DOWN AT 06:12 Z. 2 L 7 2 4F 4 F RT A35EU E23EA 2001052900024 20010529 00024 WP 2001 5 29 U2RB050101 1 20010514 A 7830 57515631 FITTING DOUG DC8 DC863F 302198F WP THRUST REVERSER CRACKED I U2RB K NONE O OTHER IN INSP/MAINT 1 GL 23 865F 9 46088 669690 ON POST FLIGHT INSPECTION WITH NR 4 ENGINE THRUST REVERSER (T/R) TRANSLATING RING EXTENDED FOUND LOWER AFT T/R TRACK SUP PORT FITTING MOUNTED ON BOTTOM CENTER LINE OF ENGINE EXHAUST NOZZLE OUTBOARD FLANGE CRACKED THROUGHOUT BOLT HOLE. 2 L 7 4 4F 4A25 2001052900025 20010529 00025 NM 2001 5 29 DHL2001705534 1 20010417 A 5310 BEAM BOEING 727 72722C 138400F NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 ON C-CHECK, FWD SIDE BS 1183 VERTICAL BEAM LBL 26.83 WL 268 HAS A VISUAL CRACK TOP SIDE OF THE LIGHTENING HOLE (MARKED) REP MPRGAA1A53001 S/B 727-53AO173. AD 85-20-03. REMOVED FASTENERS ON VERTICAL BEAM STA 1183 BULKHEAD BL 2683, REMOVED ST IFFENER TEES AT WL 253 X 263, IAW BOEING S/B 727-53-0182 FIG 2. 2 L 7 3 4F A3WE 2001052900026 20010529 00026 NM 2001 5 29 ERKR200100126 1 20010515 A 5400 65B90316 FITTING BOEING 747 747128 1384894 NM NR 1 PYLON DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 ALTERNATE FASTENERS FOR NR 1 PYLON FWD INBOARD HANGER FITTING REWORK. A DEVIATION TO THE SERVICE BULLETIN 747-54A2203 W HICH CONSISTS OF USING LARGER FASTENER SIZES OF THE SAME TYPE AS LISTED IN THE SERVICE BULLETIN PER ECRA 3203-54-034-2. 2 L 7 4 4F A20WE 2001052900027 20010529 00027 NM 2001 5 29 ERKR200100127 1 20010515 A 5400 FITTING BOEING 747 747128 1384894 NM NR 2 PYLON DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 NR 2 ENGINE PYLON, FORWARD MOUNT, OVERSIZE HOLES. DURING SCHEDULED MAINTENANCE INSPECTION OF THE AIRPLANE CRACKS WERE F OUND IN THE INBOARD AND OUTBOARD HANGER FITTING UPPER ATTACHMENT HOLES. THE CRACKS WERE REMOVED BY OVERSIZING, AND NDT INSPECTED TO ASSURE A CRACK AND CORROSION FREE CONDITION. OVERSIZE DIA BOLTS WERE INSTALLED PER BOEING RECOMMENDATIONS PER ECRA 3203-54-049-2. 2 L 7 4 4F A20WE 2001052900028 20010529 00028 NM 2001 5 29 AWXA0001729 1 20010514 A 5310 65C25229 SHEAR TIE BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 FS 727D BETWEEN STR 27L AND 27R CORROSION ON FRAME SHEAR TIE. REPAIRED IAW AWA ER 03-5300-01131-JS1. 2 L 7 2 4F RT A16WE 2001052900029 20010529 00029 CE 2001 5 29 20010524SG009 1 20010422 A 6120 LINKAGE BEECH 1900 1900C 1154161 CE PITCH CONTROL LOOSE A GUUA O OTHER O OTHER CL CLIMB 1 SO 19 1568W UC64 FLT 9437 - MCO - AFTER TAKEOFF, RIGHT PROPELLER RPM FLUCTUATED BETWEEN 200 AND 1200 AND TORQUE WENT TO 5000 LBS. DETERM INED RIGHT PROPELLER LOW PITCH CONTROL LINKAGE TO BE SAFETIED BUT LOOSE. RIGGED PROPELLER LOW PITCH CONTROL LINKAGE TO BE SAFETIED BUT LOOSE. RIGGED PROPELLER LOW PITCH CONTROL FRONT WIRE ROPE AND BALL END LINKAGE. (M) 2 L 7 2 4T RT A24CE 2001052900030 20010529 00030 CE 2001 5 29 20010524SG010 1 20010419 A 6120 LINKAGE BEECH 1900 1900C 1154161 CE LOW PITCH CNTRL OUT OF RIG A GUUA O OTHER R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 19 1568W UC64 FLT 9411 - MCO/MIA - ON TAKEOFF AT V1 SPEED ROTATION, NR 2 ENGINE LOST POWER. RERIGGED RIGHT ENGINE LOW PITCH CONTROL S YSTEM. (M) 2 L 7 2 4T RT A24CE 2001052900031 20010529 00031 NM 2001 5 29 UIEA01041 1 20010421 A 5311 FRAME BOEING 747 747230B 1384889 NM FUSELAGE GOUGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 509MC 21221 DURING INSPECTION FOUND BS 360 FRAME DEEPLY GOUGED BETWEEN STRINGER 2L AND 2AL. CUT AWAY DAMAGED AREA. FABRICATED REPA IR FILLER, DOUBLERS AND SPLICE PLATES. INSTALLED PER STANDARD PRACTICES IAW BOEING TELEX. MODIFICATION SB 747-53-2272 PREVIOUSLY ACCOMPLISHED. (M) 2 L 7 4 4F A20WE 2001052900032 20010529 00032 NM 2001 5 29 UIEA01042 1 20010421 A 5312 65B07992126 DOUBLER BOEING 747 747230B 1384889 NM BULKHEAD CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 509MC * 21221 DURING INSPECTION, FOUND BONDED DOUBLER CORRODED ON CANTED BULKHEAD BS 1241 AT LBL 11.33. USED GUN BARREL REAMER, REMOV ED LAYER OF CORRODED SKIN OF BONDED DOUBLER. FABRICATED FILLER AND REPAIR DOUBLERS. INSTALLED PER STANDARD PRACTICES P ER BOEING TELEX. (M) 2 L 7 4 4F A20WE 2001052900033 20010529 00033 NM 2001 5 29 UIEA01043 1 20010421 A 5313 65B15085 STRINGER BOEING 747 747230B 1384889 NM FUSELAGE CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 509MC * 21221 DURING INSPECTION,FOUND STRINGER 51L AT BS 1480 CORRODED. TRIMMED OUT CORRODED AREA. FABRICATED NESTED CHANNEL REPAIR AND FILLER. INSTALLED NEW STRINGER END FITTING ALONG WITH FILLER AND NESTED CHANEL PER STANDARD PRACTICES. (M) 2 L 7 4 4F A20WE 2001052900034 20010529 00034 SW 2001 5 29 20010517CW010 1 20010425 A 6420 206011819109 YOKE BELL BELL 206 206L3 1182108 SW ALLSN 250C 250C30 03013 GL TAIL ROTOR MISMANUFACTURED B TU3R K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 07 32AZ A6426 51008 AN ATTEMPT WAS MADE TO INSTALL THE NEW TAIL ROTOR HUB AND BLADE ASSEMBLY ON THE AIRCRAFT AND THE FLAPING ANGLE COULD NOT BE ADJUSTED. ON INSPECTION IT WAS FOUND THAT THE YOKE ASSEMBLY WAS MACHINED 90 DEGREES TO WHERE THE CUTOUTS THAT ALLOW THE FLAPPING. THE RESULT WAS THE STATIC STOP PART NUMBER 206010742003 CONTACTED ON THE SIDE AND NOT STOP FACE DECREASI NG THE AMOUNT THE HUB ASSEMBLY IS ALLOWED TO TRAVEL. THE TAIL ROTOR HUB ASSEMBLY WAS REPLACED WITH A NEW PART. 1 G 7 1 3U 3 U H2SW E1GL 2001052900035 20010529 00035 SO 2001 5 29 20010517CW011 1 20010411 A 2433 9B4024A TRANSFORMER GULSTM G1159 G1159A 3970109 SO RROYCE SPEY SPEY5118 54523 EU E/E BAY DEFECTIVE D K NONE O OTHER IN INSP/MAINT 1 SW 05 35GZ 1205 465 DURING MAINTENANCE OPERATION, POSITIVE TERMINAL ON TRANSFORMER RECTIFIER WAS GLOWING RED WHEN INSTALLED WITH POWER APPLI ED. THIS WAS FOUND DURING A ROUTINE INSPECTION. THERE WAS NO INDICATION THAT THE AIRCRAFT WIRING HAD AN EFFECT ON THIS MALFUNCTION. THE AC CIRCUIT BREAKER DID NOT TRIP. POSITIVE TERMINAL LUG ON RECTIFIER WAS VERY DISCOLORED. THE PLAST IC INSULATOR WAS ALSO DISCOLORED AND MELTED DUE TO EXTREME HEAT. POSSIBLE DIRECT SHORT TO GROUND CAUSING MALFUNCTION. ATTACHMENT LUG LEADING INSIDE BOX NOTICED TO BE REPOSITIONED. RECOMMEND THAT A FAIL SAFE CIRCUIT PROTECTOR BE INSTALLED ON BOX. 2 L 7 2 4F 4 F A12EA E2EU 2001052900036 20010529 00036 SW 2001 5 29 MB5R055N 1 20010416 A 3210 73005836 ANGLE GULSTM 690TP 695A 7630519 SW GARRTT TFE731 TFE731* 01518 WP RT MLG CRACKED B MV5R K NONE O OTHER IN INSP/MAINT 1 GL 11 900EC 5211 96050 RIGHT MAIN LANDING GEAR OUTBOARD GEAR MOUNT SIDE BRACE TO WING ATTACHMENT ANGLE CRACKED. CRACK LOCATED AT THE AFT PORTI ON OF THE ANGLE EXTENDING ONE INCH FORWARD. 1 H 7 2 4T 4 F 2A4 E6WE 2001052900039 20010529 00039 SO 2001 5 29 WVBA2001027 1 20010502 A 2140 17E243R IGNITER PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA HEAT SYS INOPERATIVE E WVBA K NONE O OTHER NR NOT REPORTED 1 AL 01 300ED 38 38 317852008 PILOT REPORTED HEATER WOULD NOT FIRE OFF. IT WAS DETERMINED THAT THE IGNITION UNIT HAD NO OUTPUT. THE UNIT WAS REMOVED AND REPLACED. 1 L 7 2 3O 3 O A20SO E14EA 2001052900041 20010529 00041 NE 2001 5 29 KBMA88730 2 20010423 A 7200 989806D524 RESTRICTOR VALVE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE MISSING E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 2273A 3130 2273 PART MISSING FROM ENGINE. NUT INSTALLED DURING OVERHAUL. INSTALLED RESTRICTOR AS REQUIRED. 1 G 7 1 3U 3 U NC H9EU E19EU 2001052900042 20010529 00042 SW 2001 5 29 KBMA88731 1 20010419 A 2840 7G547 SWITCH BELL 206 206B 1181511 SW FUEL SYSTEM INOPERATIVE E KBMA K NONE O OTHER NR NOT REPORTED 1 WP 19 73DP 11296 2513 FUEL PRESSURE SWITCH FOUND INOPERATIVE. REMOVED AND REPLACED AS REQUIRED. 1 G 7 1 3U H2SW 2001052900043 20010529 00043 GL 2001 5 29 KBMA88732 2 20010419 A 7323 23065121 GOVERNOR BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL ENGINE FAILED E KBMA O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 WP 19 73DP 11296 2513 WILL NOT DEVELOP FULL RPM. REMOVED AND REPLACED GOVERNOR WITH OVERHAULED, AS REQUIRED. 1 G 7 1 3U 3 U H2SW E4CE 2001052900044 20010529 00044 NE 2001 5 29 KBMA88734 2 20010427 A 7250 0292253250 TURBINE WHEEL SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE OUT OF TOLERANCE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 37SH 9452 2300 MODULE 2 & 3 WERE REMOVED FOR REAR BEARING CLEANING. DURING A GENERAL INSPECTION OF THE 2ND STAGE TURBINE AND FREE TURB INE BLADES AND LOCKS, ALLOWED. DUE TO THIS ACCESS, THE 2ND STAGE TURBINE SHOWED VISUAL SIGNS OF BLADE MOVEMENT WITH LOO SE LOCKS. UNDER ADVISE OF MFG TECH, INSP WAS COMPLETED WHICH DEMONSTRATED THAT THE BLADE PLATFORM HEIGHT WAS OUT OF LI MITS AT .65MM.( .40 MM MAX ALLOWED) MODULE 2 AND 3 RETURNED FOR REPAIR. 1 G 7 1 3U 3 U H9EU E19EU 2001052900045 20010529 00045 EU 2001 5 29 KBMA88735 1 20010424 A 7714 56337078012 INDICATOR SNIAS 350 AS350B2 8680813 EU COCKPIT ERRATIC E KBMA K NONE O OTHER NR NOT REPORTED 1 WP 19 53SH 5111 2009 NC GAGE ERRATIC AND INTERMITTENT. REMOVED AND REPLACED WITH LOANER UNIT WHILE GAUGE IS BEING REPAIRED. 1 G 7 1 3U H9EU 2001052900046 20010529 00046 2001 5 29 KBMA88736 4 20010425 A 2312 064010560030 RADIO SNIAS 350 AS350B2 8680813 EU VHF COMM INOPERATIVE E KBMA K NONE O OTHER NR NOT REPORTED 1 WP 19 115SH 2410 3141 RADIO INOPERATIVE/ REPLACED WITH SERVICEABLE PART AS REQUIRED. 1 G 7 1 3U H9EU 2001052900047 20010529 00047 2001 5 29 KBMA88737 4 20010425 A 3452 066106200 TRANSPONDER SNIAS 350 AS350BA 8680817 EU COCKPIT INOPERATIVE E KBMA K NONE O OTHER NR NOT REPORTED 1 WP 19 2273A 3136 2273 TRANSPONDER IS INOPERATIVE. REMOVED AND REPLACED WITH SERVICABLE PART. 1 G 7 1 3U NC H9EU 2001052900048 20010529 00048 NM 2001 5 29 USAASB01108 1 20010425 A 3350 500000043 CHARGER BOEING 737 737201 1384454 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 252AU 22758 MCO - THE FORWARD SECTION OF LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWE R SUPPLY/CHARGER. (M) 2 L 7 2 4F A16WE 2001052900049 20010529 00049 NM 2001 5 29 USAASB01109 1 20010403 A 3350 900835A POWER SUPPLY BOEING 737 737201 1384454 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 265AU 22962 BWI - THE OUTSIDE AND AFT EXIT IDENTIFIER LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPL Y. (M) 2 L 7 2 4F A16WE 2001052900050 20010529 00050 NM 2001 5 29 USAASB01114 1 20010427 A 3350 LIGHT BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 394US 23316 TPA - MAINTENANCE FOUND SEAT 5C EMERGENCY SEAT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED SPLICE. OPS CHECK G OOD. (M) 2 L 7 2 4F RT A16WE 2001052900051 20010529 00051 NM 2001 5 29 USAASB01115 1 20010427 A 3350 21031005 FUSE BOEING 737 7373B7 1384580 NM EGRESS LIGHTING BLOWN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 394US 23316 TPA - MAINTENANCE FOUND THE FORWARD EMERGENCY EGRESS LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TWO 5 AMPS FUS ES. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001052900052 20010529 00052 NM 2001 5 29 USAASB01116 1 20010427 A 3350 110049 CHARGER BOEING 737 7373B7 1384580 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 373US 22952 PHL - MAINTENANCE FOUND THE LOW LEVEL EMERGENCY LIGHTS AT ROWS 1 THROUGH 4 INOPERATIVE AND THE EMERGENCY LIGHTS AT THE F ORWARD ENTRY AND SERVICE DOORS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK (P/N 2013-1A) AND CHAGER ASSEMBLY AT STATION 338L IN ASSOCIATION WITH MM. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001052900053 20010529 00053 NM 2001 5 29 USAASB01119 1 20010429 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 528AU 24410 PIT - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT ROWS 20 AND 22 AND ABOVE THE L2 DOOR INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE BATTERY PACK AT AFT RIGHT SIDE CEILING PANEL. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001052900054 20010529 00054 EU 2001 5 29 USAASA01011 1 20010414 A 2130 87292325V04 COMPUTER AIRBUS A319 A319112 EU E/E BAY FAULTY A USAA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 712US 3808 1038 CLT-RIC - FLT 1988 - AN ECAM AVIONICS SMOKE WARNING MESSAGE WAS RECEIVED AT FL250. QRH PROCEDURES WERE FOLLOWED AND THE FLIGHT DIVERTED TO RDU. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE AVIONICS SMOKE DETECTOR AND THE AEVC COMPUTER. OPS CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2001052900055 20010529 00055 NM 2001 5 29 USAASB01150 1 20010420 A 3350 1000679 LIGHT BOEING 737 7372B7 1384560 NM CABIN FAULTY A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 266AU 22878 SYR - PILOT REPORTED THE EMERGENCY LIGHT OVER THE FORWARD ENTRY DOOR IS ILLUMINATED WHEN GROUND SERVICES POWER IS SELECT ED WITH COCKPIT EMERGENCY LIGHT SWITCH OFF. ALL OTHER EMERGENCY LIGHTS ARE OFF. MAINTENANCE REMOVED AND REPLACED LIGHT ASSEMBLY OVER THE FORWARD ENTRY DOOR. OPS CEHCK GOOD. (M) 2 L 7 2 4F A16WE 2001052900056 20010529 00056 NM 2001 5 29 USAA010379 1 20010405 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 33516 22953 CLT - FOUND FLOORBEAM CORRODED 32 INCHES IN SEVERAL AREAS, STATION 344, LBL 16 THROUGH RBL 16. INSTALLED NEW T-CAP FROM LBL 23 - RBL 21 PE SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2001052900057 20010529 00057 NM 2001 5 29 USAA010380 1 20010405 A 5315 1121206 FLOORBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 33516 22953 CLT - FOUND TOP OF FLOORBEAM CORRODED IN SEVERAL AREAS, STATION 328 RBL 12 - RBL 54. REPLACED T-CAP PER SRM 53-10-51. CORROSION LEVEL 2. REPLACED T-CAP PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2001052900058 20010529 00058 NM 2001 5 29 USAA010383 1 20010405 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 33516 22953 CLT - FOUND FLOORBEAM CORRODED 63 INCHES SEVERAL AREAS, STATION 986.5, LBL 18-45. INSTALLED T-CAP PER TR 53-10-05 REV A . (M) 2 L 7 2 4F RT A16WE 2001052900059 20010529 00059 NM 2001 5 29 USAA010405 1 20010226 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 587US 43319 23932 PIT - FOUND FLOORBEAM CORRODED, .5 INCH BY 1 INCH IS LARGEST, 1 INCH, .75 INCH, AND .25 INCH STATION 996.5 LBL 50 RBL 50 . PER TYPICAL REPAIR 53-15-01B. (M) 2 L 7 2 4F RT A16WE 2001052900060 20010529 00060 NM 2001 5 29 USAA010409 1 20010320 A 5320 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 32132 24560 PIT - FOUND FLOOR SUPPORT ANGLE CORRODED 1.5 INCH DIAMETER - .020 INCH DEEP, STATION 947 ABOVE STRINGER 24L-25L FLOOR SU PPORT ANGLE. CORROSION LEVEL 1, TASK NR C53-202-01. REMOVED CORROSION, FABRICATED DOUBLER, INSTALLED REPAIR PER 53-60- 53 FIG 101, SRM 51-70-11, 51-40-02. (M) 2 L 7 2 4F RT A16WE 2001052900061 20010529 00061 NM 2001 5 29 USAA010411 1 20010322 A 5320 FLOOR SUPPORT BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 587US 43319 23932 PIT - FOUND FLOOR SUPPORT BEAM CORRODED 160 INCHES, STATION 500D TO STATION 380 FLOOR SUPPORT BEAM 26L. CORROSION LEVEL 1, TASK C53-208-01. REMOVED CORROSION, REPAIRED SUPPORT BEAM, REPLACED SECTION PER TYPICAL REPAIR 53-20-04. (M) 2 L 7 2 4F RT A16WE 2001052900062 20010529 00062 NM 2001 5 29 USAA010414 1 20010327 A 5320 DOUBLER BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 32132 24560 PIT - FOUND CORROSION .035 INCH DEEP, INTERCOSTAL CAP STRAP DOUBLER STATION 787-847 STRINGER 25-26R. CORROSION LEVEL 1, TASK NR C53-202-01. REPLACED STRAP PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2001052900063 20010529 00063 NM 2001 5 29 USAA010415 1 20010327 A 5320 1510434 CHANNEL BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 32132 24560 PIT - FOUND CHANNEL CORRODED 1 INCH BY 12 INCHES, AFT CARGO DOOR OPENING C-CHANNEL LOWER THRESHOLD. REPLACED CHANNEL WI TH NEW PART. CORROSION LEVEL 1, TASK NR C53-202-1. (M) 2 L 7 2 4F RT A16WE 2001052900064 20010529 00064 NM 2001 5 29 USAA010416 1 20010327 A 5330 BEAR STRAP BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 32132 24560 PIT - FOUND CORROSION 1 INCH BY 12 INCHES, AFT CARGO DOOR OPENING BEAR STRAP LOWER THRESHOLD. CORROSION LEVEL 1, TASK N R C53-202-1. DAMAGED AREA CUT OUT, REPAIR DOUBLER INSTALLED PER EA 70387. (M) 2 L 7 2 4F RT A16WE 2001052900065 20010529 00065 NM 2001 5 29 USAA010417 1 20010327 A 5320 FLOOR SUPPORT BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 587US 43319 23932 PIT - FOUND BEAM SUPPORT CORRODED .5 INCH TO 6 INCHES AT NUTPLATES, BS 727D-827 ON ALL LEFT SIDE FLOOR SUPPORT. CORROSI ON LEVEL 1, TASK NR C53-208-01. REPLACED DEFECTIVE PARTS WITH IDENTICAL BEAM SUPPORT PER TYPICAL REPAIR 53-10-06B. (M) 2 L 7 2 4F RT A16WE 2001052900066 20010529 00066 NM 2001 5 29 USAA010418 1 20010331 A 5230 46921528M DOOR FRAME BOEING 737 737301 1384611 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 339US 23236 PIT - FOUND FORWARD CORNER FRAME CRACKED 1 INCH AND .25 INCH, FORWARD CARGO DOOR LOWER FWD CORNER TOP FLANGE. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER EO 5290X045. (M) 2 L 7 2 4F RT A16WE 2001052900067 20010529 00067 NM 2001 5 29 USAASB01106 1 20010420 A 2750 65C275012 TRANSMISSION BOEING 737 7373B7 1384580 NM T/E FLAPS FAILED A USAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 EA 19 394US 29390 23316 IAD - FLT 1083 - ON APPROACH TO DCA, CAPTAIN REPORTED THAT THE FLAPS WERE STUCK AT 10 DEGREES. CREW CHECKED ALL CIRCUIT BREAKERS AND TRIED ALTERNATE METHOD WITH NO HELP. FLIGHT DIVERTED TO IAD AND LANDED WITHOUT FURTHER INCIDENT. NO EMER GENCY WAS DECLARED. MX PERFORMED VISUAL INSPECTION OF FLAPS INCLUDING TRACKS, TOGGLES AND FLAP DRIVES. NO DEFECTS NOTE D. PERFORMED OPS CHECK AS PER BOEING MM 27-51-00. REMOVED AND REPLACED FLAP POSITION INDICATOR (P/N 2061-14-1) AS PREC AUTIONARY. OPS CHECK GOOD. LATER THAT DAY, THE FLAPS LOCKED OUT AGAIN AT 10 DEGREES. MAINTENANCE REMOVED AND REPLACED THE LEFT OUTBOARD TRAILING EDGE FLAP TRANSMISSION. OPERATIONAL CHECK GOOD PER MM 27-51-73. (M) 2 L 7 2 4F RT A16WE 2001052900068 20010529 00068 NM 2001 5 29 USAA010374 1 20010405 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 33516 22953 CLT - FOUND FRAME CRACKED .25 INCH, STATION 787, BETWEEN STRINGER 8R-9R. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001052900069 20010529 00069 NM 2001 5 29 USAA010375 1 20010405 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 33516 22953 CLT - FOUND FRAME CRACKED .25 INCH, STATION 787, BETWEEN STRINGER 8R-9R. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001052900070 20010529 00070 NM 2001 5 29 USAA010376 1 20010405 A 5311 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 33516 23739 CLT - FOUND FRAME CRACKED .0500 INCH, STATION 7270, BETWEEN STRINGER 8R-9R. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001052900071 20010529 00071 NM 2001 5 29 USAA010377 1 20010405 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 33516 22953 CLT - FOUND FRAME CRACKED .75 INCH, STATION 727E, STRINGER 8R-9R. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001052900072 20010529 00072 NM 2001 5 29 USAA010378 1 20010405 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 33516 22953 CLT - FOUND FRAME CRACKED .500 INCH, STATION 380 BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2001052900073 20010529 00073 NM 2001 5 29 USAA010381 1 20010405 A 5313 6546877143 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 33516 22953 CLT - FOUND .250 INCH CRACK, STATION 726, STRINGER 18A LEFT SIDE. REMOVED AND REPLACED PART PER EA69397. (M) 2 L 7 2 4F RT A16WE 2001052900074 20010529 00074 NM 2001 5 29 USAA010382 1 20010405 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 33516 22953 CLT - FOUND FRAME CRACKED .250 INCH, STATION 887 BETWEEN STRINGER 8R-9R. INSTALLED DOUBLER AND SHIM PER TR 53-10-14. ( M) 2 L 7 2 4F RT A16WE 2001052900075 20010529 00075 NM 2001 5 29 USAA010384 1 20010405 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 33516 22953 CLT - FOUND FRAME CRACKED 1 INCH, STAITON 807, BETWEEN STRINGER 8L-9L. INSTALLED DOUBLERS PER SRM 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001052900076 20010529 00076 NM 2001 5 29 USAA010386 1 20010416 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 346US 40138 23515 CLT - FOUND SKIN CRACKED 2 INCHES, STATION 947 AT STRINGER 34L, FORWARD OF POTABLE WATER SERVICE PANEL. INSTALLED DOUBL ER PER SRM 53-00-01, FIG 201. (M) 2 L 7 2 4F RT A16WE 2001052900077 20010529 00077 NM 2001 5 29 USAA010387 1 20010416 A 5320 WEB BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 41775 23237 CLT - FOUND WEB CRACKED .5 INCH, BS 179, RBL 28, WL 207. REMOVED AND REPLACED WEB EO 5300V157. (M) 2 L 7 2 4F RT A16WE 2001052900078 20010529 00078 NM 2001 5 29 USAA010388 1 20010416 A 5320 WEB BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 41775 23237 CLT - FOUND WEB CRACKED .5 INCH, FLOORWEBS STATION 179, LBL 28, WL 207. REMOVED AND REPLACED WEB, EO 5300V157. (M) 2 L 7 2 4F RT A16WE 2001052900079 20010529 00079 NM 2001 5 29 USAA010389 1 20010416 A 5312 BULKHEAD BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 346US 41775 23515 CLT - FOUND WEB CRACKED 2 INCHES, BS 178, RBL 6, BETWEEN WL 197 AND 205. INSTALLED DOUBLER SRM 53-10-08, EO 5300V153. (M) 2 L 7 2 4F RT A16WE 2001052900080 20010529 00080 NM 2001 5 29 USAA010390 1 20010416 A 5320 INTERCOSTAL BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 41775 23237 CLT - FOUND INTERCOSTAL CRACKED 3 INCHES, WL 195, STATION 178, RBL 24. REMOVED AND REPLACED SRM 51-10-02, EO 5300V153. (M) 2 L 7 2 4F RT A16WE 2001052900081 20010529 00081 NM 2001 5 29 USAA010391 1 20010416 A 5311 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 41775 23237 CLT - FOUND SIDE CHORD CRACKED, .5 INCH, BS 178, LBL 24, WL 207. CUT OUT DAMAGE, SPLICED IN NEW SIDECHORD, SRM 51-10-02 , EO 5300V157. (M) 2 L 7 2 4F RT A16WE 2001052900082 20010529 00082 NM 2001 5 29 USAA010397 1 20010416 A 5312 BULKHEAD BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 34792 23988 CLT - FOUND BULKHEAD WEB CRACKED 1 INCH, BS 178, LBL 5.7, WL 199. INSTALLED DOUBLER EO 5300V153 AND EA 69407. (M) 2 L 7 2 4F RT A16WE 2001052900083 20010529 00083 NM 2001 5 29 USAA010398 1 20010416 A 5312 BULKHEAD BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 34792 23988 CLT - FOUND BULKHEAD WEB CRACKED .25 INCH AND .5 INCH, BS 178, WL 189, LBL .5 AND RBL .5. INSTALLED 1 REPAIR DOUBLER FO R BOTH CRACKS, EO 5300V153 AND EA 69407. 2 L 7 2 4F RT A16WE 2001052900084 20010529 00084 NM 2001 5 29 USAA010399 1 20010416 A 5312 BULKHEAD BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 34792 23988 CLT - FOUND BULKHEAD WEB CRACKED 1 INCH, BS 178, LBL 5.7, WL 201.5. INSTALLED DOUBLER, EO 5300V153 AND EA 69407. (M) 2 L 7 2 4F RT A16WE 2001052900085 20010529 00085 NM 2001 5 29 USAA010400 1 20010416 A 5312 BULKHEAD BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 34792 23988 CLT - FOUND BULKHEAD WEB CRACKED 1 INCH, BS 178, RBL 5.7, WL 201.5. INSTALLED DOUBLER, EO5300V153 AND EA 69407. (M) 2 L 7 2 4F RT A16WE 2001052900086 20010529 00086 NM 2001 5 29 USAA010401 1 20010416 A 5312 BULKHEAD BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 34792 23988 CLT - FOUND BULKHEAD WEB CRACKED 1 INCH, BS 178, RBL 5.7, WL 199. INSTALLED DOUBLER, EO5300V153 AND EA 69407. (M) 2 L 7 2 4F RT A16WE 2001052900087 20010529 00087 NM 2001 5 29 USAA010402 1 20010416 A 5312 BULKHEAD BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 34792 23988 CLT - FOUND BULKHEAD WEB CRACKED 1 INCH, BS 178, LBL 5.7, WL 210. INSTALLED DOUBLER, EO5300V153 AND EA 69407. (M) 2 L 7 2 4F RT A16WE 2001052900088 20010529 00088 NM 2001 5 29 USAA010403 1 20010416 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 34792 23988 CLT - FOUND SIDE CHORD CRACKED .5 INCH, BS 178, WL 207 RBL 26. CUT OUT DAMAGE, SPLICED IN NEW SIDE CHORD SECTION EO 530 0V157. (M) 2 L 7 2 4F RT A16WE 2001052900089 20010529 00089 NM 2001 5 29 USAA010404 1 20010416 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 34792 23988 CLT - FOUND SIDE CHORD CRACKED .25 INCH, BS 178, WL 207, LBL 26. CUTOUT DAMAGE, SPLICED IN NEW SIDECHORD SECTION. (M) 2 L 7 2 4F RT A16WE 2001052900090 20010529 00090 NM 2001 5 29 USAA010407 1 20010320 A 5720 BRACKET BOEING 737 737301 1384611 NM LT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 587US 43319 23932 PIT - FOUND BRACKET CRACKED .375 INCH, 14 INCHES INBOARD OF ENGINE PYLON LEFT WING REAR SPAR. REPAIRED PER 2024-T3 DWG NR 69-43586-7 SH 26 ZONE B6 PER SRM 57-20-10 PAGE 10. (M) 2 L 7 2 4F RT A16WE 2001052900091 20010529 00091 EU 2001 5 29 KBMA88739 1 20010428 A 2121 420800006 MOTOR SNIAS 350 AS350B2 8680813 EU BLOWER INOPERATIVE E KBMA K NONE O OTHER NR NOT REPORTED 1 WP 19 53SH 5127 2009 MOTOR FOUND TO BE INOPERATIVE. REMOVED AND REPLACED WITH SERVICEABLE UNIT AS REQUIRED. 1 G 7 1 3U H9EU 2001052900092 20010529 00092 2001 5 29 KBMA88740 4 20010429 A 3422 103007701 GYRO SNIAS 350 AS350B2 8680813 EU COCKPIT FAULTY E KBMA K NONE O OTHER NR NOT REPORTED 1 WP 19 53SH 5132 2009 D.G. IS INOPERATIVE, SPINS RAPIDLY. REMOVED AND REPLACED WITH SERVICEAABLE UNIT, AS REQUIRED. 1 G 7 1 3U H9EU 2001052900093 20010529 00093 2001 5 29 KBMA88742 4 20010430 A 3422 RCA15BK1 GYRO SNIAS 350 AS350BA 8680817 EU COCKPIT INOPERATIVE E KBMA K NONE O OTHER NR NOT REPORTED 1 WP 19 350SH 4688 2957 DIRECTIONAL GYRO INOPERATIVE, PRESESSES. REMOVED AND REPLACED WITH SERVICEABLE UNIT, AS REQUIRED. 1 G 7 1 3U NC H9EU 2001052900094 20010529 00094 EU 2001 5 29 KBMA88743 1 20010501 A 6410 355A09103601 BEARING SNIAS 350 AS350BA 8680817 EU T/R WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 230SH 3689 2337 BEARINGS WORN. REPLACED WITH NEW BEARINGS, AS REQUIRED. 1 G 7 1 3U NC H9EU 2001052900095 20010529 00095 2001 5 29 KBMA88744 4 20010503 A 3421 5040032902 INDICATOR SNIAS 350 AS350BA 8680817 EU COCKPIT PRECESSES E KBMA K NONE O OTHER NR NOT REPORTED 1 WP 19 1188P 10042 2347 UNIT PRECESSING BEYOND LIMIT. REMOVED AND INSTALLED SERVICEABLE UNIT AS REQUIRED. 1 G 7 1 3U NC H9EU 2001052900096 20010529 00096 EU 2001 5 29 KBMA88762 1 20010406 A 7160 350A54108004 INTAKE DUCT SNIAS 350 AS350B 8680801 EU ENGINE CRACKED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 37SH 9388 2300 CRACKED ENGINE INTAKE FORWARD. RIGHT HAND CORNER NORMAL WEAR AND TEAR. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H9EU 2001052900097 20010529 00097 EU 2001 5 29 R7MR32577 1 20010112 A 2422 SS120 INVERTER SNIAS 350 AS350B3 8680954 EU AC SYSTEM INOPERATIVE E R7MR K NONE O OTHER NR NOT REPORTED 1 NM 07 392LG 374 3252 UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 2001052900098 20010529 00098 NE 2001 5 29 R7MR32828 2 20010502 A 7250 410106802 SPRING BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE SEAR RING WORN E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 527RM 573 573 7111 WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2001052900099 20010529 00099 NE 2001 5 29 R7MR32839 2 20010502 A 7250 430144801 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE NR 3 BEARING LEAKING E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 527RM 573 573 7111 LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2001052900100 20010529 00100 NE 2001 5 29 R7MR32842 2 20010502 A 7230 430150601 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE NR 2 BEARING LEAKING E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 527RM 573 573 7111 LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2001052900101 20010529 00101 NM 2001 5 29 USAA010408 1 20010320 A 5710 LINK BOEING 737 737301 1384611 NM RT WING CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 587US 43319 23932 PIT - FOUND LINK WITH 3 INCH DIAMETER FRETTING, RIGHT WING INBOARD DOG BONE LINK LUG ON AFT SIDE OF SPAR. BLENDED AREA, DAMAGE TREATED AND PRIMED. (M) 2 L 7 2 4F RT A16WE 2001052900102 20010529 00102 NE 2001 5 29 SIMA200107001 2 20010311 A 7320 685038061458 HMU SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE MALFUNCTIONED A SIMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 21 261AE 340B261 BTV - FLT 4625 - CREW REPORTED ERRATCI ENGINE INDICATIONS ON NR 2 ENGINE. PROPELLER RPM FLUCTUATES PLUS/MINUS 1000. AF TER TORQUE MOTOR LOCKOUT THERE WERE NO MORE FLUCTUATIONS NOTED. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE HYDROMECH ANICAL FUEL CONTROL UNIT. OPS AND LEAK CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 2001052900103 20010529 00103 EU 2001 5 29 SIMA200106501 1 20010306 A 3350 44 LIGHT AEROSP ATR72 ATR72212A 8680902 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 538AT 538 DFW - FLT 3528 - PASSENGER DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB. OPS CHECK GOOD IAW AMM. (M) 2 H 7 2 4T RT A53EU 2001052900104 20010529 00104 EU 2001 5 29 SIMA200107102 1 20010312 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 498AT 498 DFW - DURING PHASE 2 INSPECTION MAINTENANCE REPORTED THE FORWARD EXIT DOOR LIGHT, AND SEVERAL FLOOR LIGHTS TO BE INOPERA TIVE. MAINTENANCE REMOVED AND REPLACED BATERY PACK FOR POWER SUPPLY UNIT 43WL. OPS CHECK WAS GOOD AND AIRCRAFT WAS RET URNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001052900105 20010529 00105 EU 2001 5 29 SIMA200107301 1 20010226 A 5315 S53672406208 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAMS 36, 38 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE F LOORBEAMS IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001052900106 20010529 00106 EU 2001 5 29 20010524SG011 1 20010226 A 5315 S5367240725201 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAMS 36, 38 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE F LOORBEAMS IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200107301. (M) 2 H 7 2 4T RT A53EU 2001052900107 20010529 00107 EU 2001 5 29 20010524SG012 1 20010226 A 5315 S5367240825400 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAMS 36, 38 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE F LOORBEAMS IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200107301. (M) 2 H 7 2 4T RT A53EU 2001052900108 20010529 00108 EU 2001 5 29 SIMA200107302 1 20010226 A 5311 S5367240725601 FRAME AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FRAMES 29 AND 38 CORRODED AT STRINGERS 20 AND 21. MAINTENANCE REMOV ED AND REPLACED THE LOWER FRAME SEGMENTS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001052900109 20010529 00109 EU 2001 5 29 20010524SG013 1 20010226 A 5311 S5367240725601 FRAME AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FRAMES 29 AND 38 CORRODED AT STRINGERS 20 AND 21. MAINTENANCE REMOV ED AND REPLACED THE LOWER FRAME SEGMENTS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200107302. (M) 2 H 7 2 4T RT A53EU 2001052900110 20010529 00110 EU 2001 5 29 SIMA200107303 1 20010226 A 5347 S53375001210 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD,LEF T MIDDLE OUTBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, LAV, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT IN BOARD, RIGHT AFT OUTBOARD, RIGHT MIDDLE OUTBOARD, RIGHT MIDDLE INBOARD AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORROD ED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001052900111 20010529 00111 EU 2001 5 29 20010524SG014 1 20010226 A 5347 S53375001202 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD,LEF T MIDDLE OUTBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, LAV, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT IN BOARD, RIGHT AFT OUTBOARD, RIGHT MIDDLE OUTBAORD, RIGHT MIDDLE INBOARD AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORROD ED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20 0107303. (M) 2 H 7 2 4T RT A53EU 2001052900112 20010529 00112 EU 2001 5 29 20010524SG015 1 20010226 A 5347 S53570203200 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD,LEF T MIDDLE OUTBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, LAV, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT IN BOARD, RIGHT AFT OUTBOARD, RIGHT MIDDLE OUTBAORD, RIGHT MIDDLE INBOARD AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORROD ED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20 0107303. (M) 2 H 7 2 4T RT A53EU 2001052900113 20010529 00113 EU 2001 5 29 20010524SG016 1 20010226 A 5347 S53570203202 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD,LEF T MIDDLE OUTBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, LAV, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT IN BOARD, RIGHT AFT OUTBOARD, RIGHT MIDDLE OUTBAORD, RIGHT MIDDLE INBOARD AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORROD ED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20 0107303. (M) 2 H 7 2 4T RT A53EU 2001052900114 20010529 00114 EU 2001 5 29 20010524SG017 1 20010226 A 5347 S53678001226 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD,LEF T MIDDLE OUTBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, LAV, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT IN BOARD, RIGHT AFT OUTBOARD, RIGHT MIDDLE OUTBAORD, RIGHT MIDDLE INBOARD AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORROD ED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20 0107303. (M) 2 H 7 2 4T RT A53EU 2001052900115 20010529 00115 EU 2001 5 29 20010524SG018 1 20010226 A 5347 S53678001224 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD,LEF T MIDDLE OUTBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, LAV, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT IN BOARD, RIGHT AFT OUTBOARD, RIGHT MIDDLE OUTBAORD, RIGHT MIDDLE INBOARD AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORROD ED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20 0107303. (M) 2 H 7 2 4T RT A53EU 2001052900116 20010529 00116 EU 2001 5 29 20010524SG019 1 20010226 A 5347 S53678001214 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD,LEF T MIDDLE OUTBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, LAV, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT IN BOARD, RIGHT AFT OUTBOARD, RIGHT MIDDLE OUTBAORD, RIGHT MIDDLE INBOARD AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORROD ED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20 0107303. (M) 2 H 7 2 4T RT A53EU 2001052900117 20010529 00117 EU 2001 5 29 20010524SG020 1 20010226 A 5347 S53678001210 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD,LEF T MIDDLE OUTBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, LAV, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT IN BOARD, RIGHT AFT OUTBOARD, RIGHT MIDDLE OUTBAORD, RIGHT MIDDLE INBOARD AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORROD ED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20 0107303. (M) 2 H 7 2 4T RT A53EU 2001052900118 20010529 00118 EU 2001 5 29 20010524SG021 1 20010226 A 5347 S53678001228 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD,LEF T MIDDLE OUTBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, LAV, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT IN BOARD, RIGHT AFT OUTBOARD, RIGHT MIDDLE OUTBAORD, RIGHT MIDDLE INBOARD AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORROD ED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20 0107303. (M) 2 H 7 2 4T RT A53EU 2001052900119 20010529 00119 EU 2001 5 29 20010524SG022 1 20010226 A 5347 S53678001226 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD,LEF T MIDDLE OUTBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, LAV, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT IN BOARD, RIGHT AFT OUTBOARD, RIGHT MIDDLE OUTBAORD, RIGHT MIDDLE INBOARD AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORROD ED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20 0107303. (M) 2 H 7 2 4T RT A53EU 2001052900120 20010529 00120 EU 2001 5 29 20010524SG023 1 20010226 A 5347 S53678001225 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD,LEF T MIDDLE OUTBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, LAV, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT IN BOARD, RIGHT AFT OUTBOARD, RIGHT MIDDLE OUTBAORD, RIGHT MIDDLE INBOARD AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORROD ED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20 0107303. (M) 2 H 7 2 4T RT A53EU 2001052900121 20010529 00121 EU 2001 5 29 20010524SG024 1 20010226 A 5347 S535702003202 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD,LEF T MIDDLE OUTBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, LAV, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT IN BOARD, RIGHT AFT OUTBOARD, RIGHT MIDDLE OUTBAORD, RIGHT MIDDLE INBOARD AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORROD ED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20 0107303. (M) 2 H 7 2 4T RT A53EU 2001052900122 20010529 00122 EU 2001 5 29 20010524SG025 1 20010226 A 5347 S53570203200 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD,LEF T MIDDLE OUTBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, LAV, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT IN BOARD, RIGHT AFT OUTBOARD, RIGHT MIDDLE OUTBAORD, RIGHT MIDDLE INBOARD AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORROD ED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20 0107303. (M) 2 H 7 2 4T RT A53EU 2001052900123 20010529 00123 EU 2001 5 29 20010524SG026 1 20010226 A 5347 S53575001210 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD,LEF T MIDDLE OUTBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, LAV, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT IN BOARD, RIGHT AFT OUTBOARD, RIGHT MIDDLE OUTBAORD, RIGHT MIDDLE INBOARD AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORROD ED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20 0107303. (M) 2 H 7 2 4T RT A53EU 2001052900124 20010529 00124 NE 2001 5 29 SIMA200104503 1 20010214 A 5610 SEAL SKRSKY S76 S76A 8143006 NE COCKPIT TORN A SIMA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 21 707AE 760276 BOS - FLT 4994 - AFTER TAKEOFF, LOUD NOISE AND VIBRATION CAME FROM NOSE OF AIRCRAFT. FOUND CAPTAINS WINDOW HUMP SEAL TO RN. REPAIRED HUMP SEAL IAW AMM. OPS CHECK GOOD. (M) 1 G 7 2 3U H1NE 2001052900125 20010529 00125 SO 2001 5 29 SIMA200104103 1 20010210 A 3610 14521182403 LINE EMB 145 EMB145LR SO BLEED AIR LEAKING A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 637AE 145170 CMH - FLT 5346 - CREW RETURNED TO FIELD DUE TO BAGGAGE SMOKE INDICATION FOLLOWED BY ENGINE TWO BLEED LEAK. MAINTENANCE REMOVED AND REPLACED THE NR 2 FUSELAGE THROUGH PYLON BLEED LINE AND THE CARGO DUCT ASSEMBLY. OPS CHECK WAS GOOD, FIRE BO TTLES WERE REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001052900126 20010529 00126 SO 2001 5 29 20010525SG001 1 20010210 A 3610 14521163406C DUCT EMB 145 EMB145LR SO BLEED AIR LEAKING A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 637AE 145170 CMH - FLT 5346 - CREW RETURNED TO FIELD DUE TO BAGGAGE SMOKE INDICATION FOLLOWED BY ENGINE TWO BLEED LEAK. MAINTENANCE REMOVED AND REPLACED THE NR 2 FUSELAGE THROUGH PYLON BLEED LINE AND THE CARGO DUCT ASSEMBLY. OPS CHECK WAS GOOD, FIRE BO TTLES WERE REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200104103. (M) 2 L 7 2 4T RT T00011AT 2001052900127 20010529 00127 EU 2001 5 29 SIMA200104501 1 20010214 A 3230 7232360151 SPRING SAAB SF340 340B 7860101 EU MLG WEAK A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 358RZ 340B358 JFK - FLT 5075 - CREW REPORTED LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. ATTEMPTED ONE RECYCLE WITH NO CHANGE. ALL OTHER INDICATIONS WERE NORMAL, HYDRAULIC AND ELECTRICAL. MAINTENANCE REMOVED AND REPLACED UPLOCK SPRINGS ON BOTH MAIN LANDING GEARS. OPS CHECK WAS GOOD AND AIRCRAFT FLEW A FUNCTIONAL CHECK FLIGHT. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001052900128 20010529 00128 EU 2001 5 29 SIMA200108802 1 20010329 A 3350 LP1670 LIGHT AEROSP ATR72 ATR72212 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST NR NOT REPORTED 1 SW 21 322AC 320 MIA - FLT 5409 - EMERGENCY FLOOR LAMP AFT OF GALLEY INOPERATIVE, MEL PER 33-30. REMOVED AND REPLACED BULB IAW AMM. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 2001052900129 20010529 00129 SO 2001 5 29 SIMA200108302 1 20010324 A 3610 V8545A7257226 O-RING EMB 145 EMB145LR SO BLEED AIR WORN A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 626AE 145117 CLE - FLT 4348 - CREW REPORTED THE NR 2 ENGINE BLEED LEAK CAME ON IN FLIGHT. AIRCRAFT WAS RETURNED TO CLE AND LANDED SA FELY. MAINTENANCE FOUND A BLEED LEAK IN A COUPLING AT FRAME 48 ABOVE RIGHT WING. O-RINGS WERE REPLACED ON COUPLING IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001052900130 20010529 00130 SO 2001 5 29 SIMA200106601 1 20010307 A 2611 4800401 LIGHT EMB 145 EMB145LR SO COCKPIT INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 639AE 145182 GRB - FLT 4200 - BAGGAGE COMPARTMENT SMOKE DETECTOR OVERHEAD WARNING LIGHT INOPERATIVE ISSUED CP MEL 26-09 AUTH 030152D CAT C. REMOVED AND REPLACED PUSH BUTTON OVERHEAD SWITCH IAW 20-13-04. OPS CHECK GOOD IAW EMB 145 AMM 26-10-00. (M) 2 L 7 2 4T RT T00011AT 2001052900131 20010529 00131 SO 2001 5 29 SIMA200106101 1 20010302 A 2740 3621001007 CONTROL UNIT EMB 145 EMB145LR SO HORIZ STAB FAILED A SIMA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 SW 21 649PP 145234 ORD - FLT 4406 - DURING CLIMB-OUT, CREW NOTED ON EICAS PITCH TRIM 1 FAIL. NOTE YOKE SWITCHES DID NOT WORK BUT THE BACK UP TRIM DID. AIRCRAFT RETURNED TO ORD SAFELY. NO FURTHER INCIDENTS WERE REPORTED. MAINTENANCE REMOVED AND REPLACED HS CU IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001052900132 20010529 00132 SO 2001 5 29 SIMA200106102 1 20010302 A 5610 163500110 WINDSHIELD EMB 145 EMB145LR SO COCKPIT CRACKED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 644AE 145204 HRL - FLT 3724 - ON CLIMB-OUT, CREW NOTED SPARKS CAME FROM FIRST OFFICERS WINDSHIELD SIDE AREA THEY THEN TURNED WINDSHIE LD HEAT OFF. AT THAT TIME THE WINDSHIELD CRACKED ALL OVER, SO THE CREW COMPLETED A EMERGENCY LANDING SAFELY. MAINTENAN CE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVI CE. (M) 2 L 7 2 4T RT T00011AT 2001052900133 20010529 00133 SO 2001 5 29 SIMA200108303 1 20010324 A 7830 83990137 SWITCH EMB 145 EMB145LR SO NR 2 T/R FAILED A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 621AE 145105 ORD - FLT 4211 - CREW REPORTED THE NR 2 THRUST REVERSER DISAGREE MESSAGE ON TAKEOFF ROLL. REMOVED AND REPLACED NR 2 ENG INE UPPER AND LOWER THRUST REVERSER STOW SWITCHES (S/N 1361 AND 1402) IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT T00011AT 2001052900134 20010529 00134 SO 2001 5 29 SIMA200108103 1 20010322 A 7830 WARNING SYSTEM EMB 135 EMB135LR SO NR 1 T/R MALFUNCTIONED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 709AE 145211 BOS - FLT 4994 - CREW ABORTED TAKEOFF DUE TO ENGINE 1 THRUST REVERSER DISAGREE MESSAGE ON EICAS. MESSAGE EXTINGUISHED D URING ABORT PROCEDURES. MAINTENANCE PERFORMED OPS CHECK AND COULD NOT FIND ANDY DISCREPANCY IAW EMB MM. NEXT TAKEOFF W AS ABORTED ALSO DUE TO SAME PROBLEM AS PREVIOUS DISCREPANCY. AT THIS TIME THRUST REVERSER WAS PUT ON MEL. (M) 2 L 7 2 4F RT TOOO11AT 2001052900135 20010529 00135 EU 2001 5 29 SIMA200108702 1 20010328 A 7930 CHIP DETECTOR SAAB SF340 340B 7860101 EU LT ENGINE ACTIVATED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 330AE 340B330 DURNG CLIMB-OUT, CREW REPORTED THE LEFT ENGINE CHIP DETECTOR LIGHT CAME ON INTERMITTENTLY. EMERGENCY WAS DECLARED AND A IRCRAFT RETUREND TO LAX. (M) 2 L 7 2 4T RT A52EU 2001052900136 20010529 00136 GL 2001 5 29 SIMA200108002 2 20010321 A 7200 ENGINE EMB 145 EMB145LR SO ALLSN AE300 AE3007A GL WING SHUTDOWN A SIMA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SW 21 624AE 145111 ORD - FLT 4309 - ON CLIMB-OUT, CREW HEARD LOUD NOISE AND ENGINE SHUTDOWN ON ITS OWN. CREW DECLARED EMERGENCY AND LANDED SAFELY IN ORD. CREW TRIED TO RESTART ENGINE, COULD NOT RESTART. (M) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2001052900137 20010529 00137 WP 2001 5 29 SIMA200108301 2 20010324 A 7200 ENGINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP NR 2 MALFUNCTIONED A SIMA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 21 359AE AC674 PIT - FLT 5106 - AFTER TAKEOFF CREW REPORTED WHAT APPEARED TO BE A COMPRESSOR STALL ON NR 2 ENGINE. A LOUD BANG FOLLOWE D BY LOSS IN TORQUE AND ITT RISE. MEMORY ITEMS WERE FOLLOWED AND POWER WAS RESTORED. OTHER INDICATIONS NOTED WERE OIL PRESSURE ON CWP ILLUMINATED, IGNITION LIGHT ON STATUS PANEL ILLUMINATED, TORQUE INDICATED ZERO, ITT WAS OBSERVED AT 902 DEGREES CELCIUS BUT WAS NOT OBSERVED THROUGHOUT THE INCIDENT. MAINTENANCE INSPECTED ENGINE IAW GE MM 72-00-00. BOROSCO PE INSPECTION REVEALED NO DEFECTS, INLET AND VARIABLE GOEMETRY SYSTEM WAS NORMAL. FDR DOWNLOAD SHOWED NO ITT EXCEEDANCE . GROUND ENGINE RUNS WERE NORMAL AND AIRCRAFT WAS RETURNED TO SERVICE. (M)(M) 2 L 7 2 4T 4 T RT A8SW E4WE 2001052900138 20010529 00138 NE 2001 5 29 R7MR32844 2 20010502 A 7230 430404701 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE NR 1 BEARING LEAKING E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 527RM 573 7111 LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2001052900155 20010529 00155 NE 2001 5 29 SIMA200109103 3 20010401 A 6140 8147994 BETA TUBE SAAB SF340 340B 7860101 EU ROTOL R354 R3544123F13 NE LT ENGINE FAILED A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 305AE 340B305 BOS - FLT 4862 - AFTER TAKEOFF, LEFT PROP SPEED INDICATION FAILED. ALL OTHER PARAMETERS WERE NORMAL. AIR TURN BACK TO BOS. REMOVED AND REPLACED BETA TUBE. (M) 2 L 7 2 4T RT A52EU 6 C P61GL 2001052900156 20010529 00156 SO 2001 5 29 SIMA200109104 1 20010401 A 2120 UNKNOWN EMB 135 EMB135LR 3260305 SO COCKPIT ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 707EB 145195 BOS - FLT 4745 - CREW REPORTED THAT DURING FLIGHT WHEN ANTI-ICE SYSTEM TURN ON THEY NOTICED A BURN ODOR IN THE COCKPIT. WHEN THE ANTI-ICE SYSTEM WENT OFF THE ODOR WENT AWAY. BOS MAINTENANCE RAN ENGINES IAW AMM AND COULD NOT DUPLICATE THE ODOR. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001052900157 20010529 00157 GL 2001 5 29 SIMA200108001 2 20010321 A 7310 2350672 FUEL LINE EMB 145 EMB145LR SO ALLSN AE300 AE3007A GL NR 2 ENGINE CHAFED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 21 628AE 145124 ORD - FLT 4100 - OIL SMELL IN CABIN. FOUND CHAFED FUEL LINE FROM FUEL PUMP METERING UNIT TO FUEL COOLED OIL COOLER ON N R 2 ENGINE. REMOVED AND REPLACED LINE IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2001052900158 20010529 00158 GL 2001 5 29 SIMA200107901 2 20010320 A 7313 1323065950A NOZZLE EMB 145 EMB145LR SO ALLSN AE300 AE3007A GL ENGINE DEFECTIVE A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 628AE 145124 IND - FLT 4007 - DURING ICING CONDITION WITH ANTI-ICING SELECTED F/A AND PASSENGERS SMELLED OIL/SMOKE SMELL IN CABIN. N O INJURIES. REMOVED AND REPLACED FUEL NOZZLES IAW AMM. OPS CHECK GOOD AT THIS TIME. (M) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2001052900159 20010529 00159 EU 2001 5 29 SIMA200108202 1 20010323 A 7930 4052T92P01 CHIP DETECTOR SAAB SF340 340B 7860101 EU RT ENGINE FALSE INDICATION A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 326AE 340B326 JFK - FLT 5136 - DURING CLIMB-OUT FROM JFK CREW GOT A RIGHT ENGINE CHIP DETECTOR LIGHT AND RETURNED TO JFK. ALL OTHER E NGINE PARAMETERS WERE NORMAL. MAINTENANCE REMOVED AND REPLACED THE ENGINE CHIP DETECTOR IAW GE CT7 CMM 79-00-00. LEAK CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001052900160 20010529 00160 SO 2001 5 29 SIMA200108602 1 20010327 A 2742 3622001011 ACTUATOR EMB 135 EMB135ER 3260203 SO STABILIZER FAILED A SIMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 21 718AE 145275 ORD - FLT 4433 - CREW REPORTED AFTER TAKEOFF PRIMARY TRIM CONTROL TO BE INOPERATIVE, FOLLOWED LATER BY AUTO TRIM FAIL. BACKUP TRIM FUNCTIONED NORMALLY. REMOVED AND REPLACED PITCH TRIM ACTUATOR IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4F RT T00011AT 2001052900161 20010529 00161 SO 2001 5 29 SIMA200107402 1 20010315 A 5610 SEAL EMB 135 EMB135LR SO COCKPIT OUT OF POSITION A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 729AE 145343 ORD - FLT 4419 - DURING CLIMB-OUT, CREW NOTED CAPTAIN WINDSHIELD HUMP SEAL COMING OUT AND CAUSING A SQUEAL. CREW ELECTE D TO RETURN TO ORD. MAINTENANCE TEMP REPAIRED SEAL AND PUT IT INTO TIME DEFERRED MAINTENANCE ITEM TO BE REPAIRED AT A L ATE DATE IAW CMM. REPAIRED HUMP SEAL IAW CMM 53-10-03. (M) 2 L 7 2 4F RT TOOO11AT 2001052900162 20010529 00162 2001 5 29 SIMA200108101 4 20010322 A 2300 COMPUTER EMB 145 EMB145 SO COCKPIT MALFUNCTIONED A SIMA A UNSCHED LANDING O OTHER AP APPROACH 1 SW 21 613AE 145081 MKE - FLT 4030 - ON APPROACH INTO ORD TUNING NR 2 RMU WENT TO DASHES. CHANGED TO NR 1 SYSTEM AND IT WENT TO DASHES. BA CK UP CONTROL HEAD ALSO WENT TO DASHES. DIVERTED INTO MKE BECAUSE THEY LOST THEIR ILS SYSTEM AND THEY NEEDED IT TO LAND IN ORD. RESET CIRCUIT BREAKERS FOR RMU, DAU AND 1-C600 WITH OUT RESETTING POWER. MAINTENANCE WENT OUT AND PERFORMED O PS CHECK AND FOUND TO BE GOOD IAW AMM. (M) 2 L 7 2 4F RT T00011AT 2001052900164 20010529 00164 2001 5 29 SIMA200108801 4 20010329 A 3140 7013345935 DAU EMB 145 EMB145LR SO E/E BAY INOPERATIVE A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 723AE 145288 ORD - FLT 4377 - DURING CLIMB-OUT, CREW NOTED LAVATORY SMOKE DETECTOR WARNING IND. VERIFIED NO SMOKE IN LAVATORY. CREW RETURNED TO ORD. NO EMERGENCY DECLARED AND NO OVERWEIGHT LANDING REPORTED. AIRCRAFT LANDED SAFELY, NO FURTHER INCIDEN TS REPORTED. REMOVED AND REPLACED NR 2 DAU AND LAVATORY SMOKE DETECTOR IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT T00011AT 2001052900165 20010529 00165 SO 2001 5 29 20010525SG002 1 20010329 A 2611 FOS765A2 SMOKE DETECTOR EMB 145 EMB145LR SO LAVATORY MALFUNCTIONED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 723AE 145288 ORD - FLT 4377 - DURING CLIMB-OUT, CREW NOTED LAVATORY SMOKE DETECTOR WARNING IND. VERIFIED NO SMOKE IN LAVATORY. CREW RETURNED TO ORD. NO EMERGENCY DECLARED AND NO OVERWEIGHT LANDING REPORTED. AIRCRAFT LANDED SAFELY, NO FURTHER INCIDEN TS REPORTED. REMOVED AND REPLACED NR 2 DAU AND LAVATORY SMOKE DETECTOR IAW AMM. OPS CHECK GOOD. REF SIMA200108801. ( M) 2 L 7 2 4T RT T00011AT 2001052900167 20010529 00167 SO 2001 5 29 SIMA200003901 1 20010208 A 2611 FDS765A2 SMOKE DETECTOR EMB 145 EMB145LR SO LAVATORY MALFUNCTIONED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 706RG 145194 ORD - FLT 4401 - DURING CLIMB, CREW REPORTED THE LAV SMOKE CAUTION LIGHT ILLUMINATED. AIRCRAFT RETURNED TO ORD, LIGHT E XTINGUISHED DURING APPROACH. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPS CHECK WAS GOOD AND AIRCRAFT WAS RELEASED FOR FLIGHT. NEXT FLIGHT SAME DISCREPANCY. MAINTENANCE THEN REPLACED LAV COMPARTMENT SMOKE DETECTOR. OPS CHECK WAS GO OD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001052900168 20010529 00168 EU 2001 5 29 SIMA200108701 1 20010327 A 5347 7253799379 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 273AE 340B273 ABI - DURING MBV INSPECTION MAINTENANCE FOUND SEAT TRACK AT BL 18 3L FROM STATION 288.0 TO 299.5 DAMAGED. SEAT TRACK WA S REPAIRED IAW SAAB SRM 72LKS3079 REV 37 AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001052900170 20010529 00170 EU 2001 5 29 SIMA200107101 1 20010312 A 2130 1305381 CONTROL PANEL SAAB SF340 340B 7860101 EU COCKPIT MALFUNCTIONED A SIMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 370AM 340B370 DFW - FLT 3895 - CREW REPORTED CABIN PRESSURIZATION LIGHT ON CWP ILLUMINATED AT 10,000 FEET. MAINTENANCE REMOVED AND RE PLACED PRESSURE CONTROL PANEL IAW SAAB MM 21-31-00. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. ( M) 2 L 7 2 4T RT A52EU 2001052900171 20010529 00171 EU 2001 5 29 SIMA200107008 1 20010311 A 2611 72111211000A SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 312AE 340B312 SBP - MAINTENANCE REPORTED BEFORE ENGINE GROUND RUNS CARGO SMOKE WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED CARGO FORWARD SMOKE DETECTOR IAW SAAB AMM 26-13-15. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001052900177 20010529 00177 EU 2001 5 29 SIMA200000803 1 20010108 A 3350 1313 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 174AE 340B174 DFW - FLT 3669 - EMERGENCY EXIT IN OVERHEAD PANEL AT SEATS 3BC INOPERATIVE. ISSUED MEL 33-13. REMOVED AND REPLACED LIG HT BULB IN 3BC IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001052900179 20010529 00179 EU 2001 5 29 SIMA200101001 1 20010110 A 3620 WARNING SYSTEM AEROSP ATR72 ATR72212 EU COCKPIT ACTIVATED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 536AT 536 DFW - FLT 3515 - DURING TAKEOFF, OUT OF DFW CREW NOTED ENGINE NR 1 BLEED OVERHEAT INDICATION. (M) 2 H 7 2 4T RT A53EU 2001052900180 20010529 00180 EU 2001 5 29 SIMA200100804 1 20010108 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN BROKEN A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 309AE 340B309 MIA - FLT 5236 - EMERGENCY LIGHT FIXTURE BY GALLEY CART IS BROKEN. MAINTENANCE REPLACED THE LIGHT ASSEMBLY IN GALLEY. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001052900182 20010529 00182 WP 2001 5 29 USAAD01088 1 20010430 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 803US 48035 MCO - THE LOW LEVEL EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001052900183 20010529 00183 WP 2001 5 29 USAAD01089 1 20010430 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 813US 48093 MCO - THE LOW LEVEL EMERGENCY LIGHTS IN THE FIRST CLASS SECTION WERE BLINKING RED AND GREEN. MAINTENANCE REPLACED THE E MERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001052900184 20010529 00184 WP 2001 5 29 USAAD01091 1 20010501 A 4910 DUCT DOUG DC9 DC981 3022081 WP APU CONTAMINATED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 803US 48035 PIT-BUF - FLT 1120 - AFTER TAKEOFF, THE LAVATORY SMOKE DETECTORS ACTIVATED AND THERE WAS THE SMELL OF SMOKE IN THE CABIN . THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE ISOLATED THE PROBLEM TO THE APU, AND PLA CED THE APU ON MEL. THE AIRCONDITIONING WATER SEPARATOR COALESCER BAGS WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVI CE. TWO FLIGHTS LATER, CLT-ATL - FLT 2378 - THERE AGAIN WAS SMOKE IN THE CABIN AFTER TAKEOFF. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE STEAM CLEANED OIL AND DIRT FROM THE APU INLET, CLEANED RESIDUE FROM THE AIRCONDITIONING DUCTS AND REPLACED THE AIRCONDITIONING WATER SEPARATOR COALESCER BAGS. (M) 2 L 7 2 4F A6WE 2001052900185 20010529 00185 NM 2001 5 29 AALA20010847 1 20010419 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 890AA 22006 TUL - FOUND FORWARD ENTRY DOOR LOWER HINGE CUTOUT SKIN CRACKED, FS 303. TRIMMED OUT CRACK, INSTALLED DOUBLER IAW SB 727 -53-0198 FIG 4. (M) 2 L 7 3 4F A3WE 2001052900186 20010529 00186 NM 2001 5 29 AALA20010848 1 20010417 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 890AA 22006 TUL - FOUND 1.5 INCH BY .125 INCH GOUGE LOCATION NEAR RIGHT NLG DOOR. DAMAGE IS APPROX 12 INCHES AFT AND 18 INCHES ABOV E AFT AND OF RIGHT NLG DOOR. REMOVED AREA DAMAGED AND INSTALLED DOUBLER JUST AFT AND ABOVE AFT RIGHT NLG DOOR PER SRM 5 3-30-3 PAGE 13 PART 1. (M) 2 L 7 3 4F A3WE 2001052900187 20010529 00187 WP 2001 5 29 AALA20010906 1 20010502 A 3350 4080478 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 510AM 49804 DFW - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY PATH MARKING SEAT MOUNTED LIGHT INOPERATIVE ON SEAT ROW 3. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900188 20010529 00188 WP 2001 5 29 AALA20010885 1 20010429 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A K NONE L NO TEST IN INSP/MAINT 1 SW 21 253AA 49286 AUS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED EMEREGNCY EXIT LIGHT WIRE. SYSTEM GROUN D CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900189 20010529 00189 WP 2001 5 29 AALA20010883 1 20010430 A 3350 8034001 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 251AA 49270 DFW - DURING OVERNIGHT MAINTENANCE, TAIL CONE EMERGENCY EXIT LIGHT DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900190 20010529 00190 WP 2001 5 29 AALA20010876 1 20010427 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 474 49649 DFW - DURING OVERNIGHT MAINTENANCE, PORTABLE EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED PORTABLE EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900191 20010529 00191 WP 2001 5 29 AALA20010877 1 20010429 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7543A 53025 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 3, 4, 7 12, 13, 17 AND 21 DIM. REPLACED EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900192 20010529 00192 WP 2001 5 29 AALA20010879 1 20010430 A 3350 SOCKET DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 283AA 49296 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT AT SEAT 7D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900193 20010529 00193 WP 2001 5 29 AALA20010874 1 20010429 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 584AA 53247 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 11, 12, 17, 18, 22, 24, 28 THROUGH 31 DIM. REPLACED EMERGEN CY EXIT LIGHT. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900194 20010529 00194 WP 2001 5 29 AALA20010865 1 20010424 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7541A 49995 DEN - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM G ROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900195 20010529 00195 WP 2001 5 29 AALA20010866 1 20010424 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP TAIL CONE INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 574AA 53151 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT TAIL CONE INOPERATIVE. REPLACED TAIL CONE EMERGENCY EXIT LI GHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900209 20010529 00209 WP 2001 5 29 AALA20010868 1 20010428 A 3350 WIRE DOUG DC9 DC982 3022082 WP TAIL CONE DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 484AA 49677 BOS - DURING OVERNIGHT MAINTENANCE, AFT EMERGENCY EXIT PATH LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT AF T TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900210 20010529 00210 WP 2001 5 29 AALA20010869 1 20010428 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 437AA 49455 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD SEAT MOUNTED EMERGENCY EXIT LIGHT DIM. REPLACED SEAT MOUNTED EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900211 20010529 00211 WP 2001 5 29 AALA20010870 1 20010428 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 505AA 49799 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 3, 7, 9, 10, 13, 16, 18, 19, 21, 22, 23, 25, 26 THROUGH 31 DIM. REPLACED EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900212 20010529 00212 WP 2001 5 29 AALA20010871 1 20010428 A 3350 8034001 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7535A 49989 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM G ROUND CHEKCED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900213 20010529 00213 WP 2001 5 29 AALA20010857 1 20010426 A 3350 8034001 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 417AA 49328 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD OVERWING EMERGENCY EXIT SIGN DIM. REPLACED FORWARD OVERWING EMERGENCY EXIT SIGN BATTERY PACK AT 20F. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900214 20010529 00214 WP 2001 5 29 AALA20010858 1 20010426 A 3350 8034001 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7506 49800 DFW - DURING OVERNIGHT MAINTENANCE, CEILING MOUNTED EMERGENCY EXIT LIGHT AT ROW 13 THROUGH 17 DIM. REPLACED CEILING MOU NTED EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900215 20010529 00215 WP 2001 5 29 AALA20010859 1 20010426 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 598AA 53288 DFW - DURING OVERNIGHT MAINTENANCE, HELD EMERGENCY LIGHT INOPERATIVE. REPLACED HAND HELD EMERGENCY LIGHT. SYSTEM GROUN D CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001052900216 20010529 00216 WP 2001 5 29 AALA20010860 1 20010426 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 598AA 53288 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 7D, 11D, 13D, 14D, 17D, 19D, 20D, 21D, 22D, 25D, 26D, 2 7D, 29D, 30D, 31D DIM. REPLACED EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001052900217 20010529 00217 WP 2001 5 29 AALA20010861 1 20010426 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 582AA 53159 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT SEAT 9D, 12D, 17D, 19D, 20D, 21D, 25D, 26D, 29D, 30D, 31D DIM. REPLACED EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900218 20010529 00218 NM 2001 5 29 AALA20010904 1 20010430 A 5711 SPAR CAP BOEING 757 757 UTILUSE NM WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 621AA 283 TUL - FOUND CORROSION ON UPPER REAR SPAR CAP AT STATION WS 160-204 ALSO HAS BULGING FASTENERS. FABRICATED 2 REPAIR STRA PS AND ATTACH ON LOWER SIDE OF WING SKIN LAND. THE LOWER STRAP THAT IS AGAINST WING SKIN SHOULD EXTENDED ONE ROW OF FAS TENERS BEYOND THE UPPER STRAP ON BOTH ENDS. REPAIRED IAW ESO 90309, DATED 4-30-01. (M) 2 L 7 2 4F RT A2NM 2001052900219 20010529 00219 NM 2001 5 29 AALA20010896 1 20010416 A 3221 TRUNNION BOEING 727 727227 1384078 NM NLG CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 721AA 20729 TUL - FOUND CORROSION IN BORE RIGHT NOSE GEAR TRUNNION, FS 303. REMOVED AND REPLACED RIGHT NOSE GEAR TRUNNION PER S/B 7 27-53-0119. (M) 2 L 7 3 4F A3WE 2001052900220 20010529 00220 NM 2001 5 29 AALA20010894 1 20010416 A 3221 TRUNNION BOEING 727 727227 1384078 NM NLG CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 721AA 20729 TUL - FOUND LEFT NOSE GEAR TRUNNION CORRODED. REMOVED AND REPLACED LEFT TRUNNION SUPPORT FITTING PER SB-727-53-119, GEA R INSTALLATION ON CARD 2613. (M) 2 L 7 3 4F A3WE 2001052900221 20010529 00221 EU 2001 5 29 AALA20010905 1 20010502 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN FAULTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70079 619 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY FLOODLIGHT ON FIRST CLASS BULKHEAD ON RIGHT SIDE OF CABIN FOUND INOPERATIV E. REPLACED CONNECTOR ON WIRE HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2001052900222 20010529 00222 WP 2001 5 29 AALA20010789 1 20010414 A 4920 5940405503 APU DOUG DC9 DC982 3022082 WP APU BAY LEAKING A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 59523 49915 ORD - FLT 829 - EN ROUTE ORD-YYC, SHORTLY AFTER TAKEOFF DETECTED STRONG SMELL AND SMOKE AT CABIN. RETURNED ORD AND LAND ED WITHOUT FURTHER INCIDENT. REPLACED APU. (M) 2 L 7 2 4F A6WE 2001052900223 20010529 00223 WP 2001 5 29 AALA20010771 1 20010410 A 2120 CLAMP DOUG DC9 DC982 3022082 WP ACM LOOSE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 7519A 49896 DFW - FLT 68 - EN ROUTE DFW-MIA - DETECTED TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATE. AIR INTERRUPTED, RETURNE D DFW AND LANDED WITHOUT INCIDENT. RE-SECURED CLAMP AT FORWARD SIDE OF PACK COOLING SYSTEM. SYSTEM GROUND CHECKED NORM AL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900224 20010529 00224 EU 2001 5 29 AALA20010808 1 20010417 A 3232 125007 ACTUATOR FOKKER F28 F28MK0100 4990807 EU NLG DOOR FAILED A AALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SW 21 1425A 11408 ORD - FLT 1831 - EN ROUTE SWF-ORD, ON APPROACH NOSE LANDING GEAR FAILED TO EXTEND. UNSAFE NOSE LANDING GEAR LIGHT ILLUM INATED. EXECUTED MISSED APPROACH. NOSE LANDING GEAR LGIHT TURNED GREEN. NOSE LANDING GEAR EXTENDED SUCCESSFULLY. LAN DED ORD WITHOUT FURTHER INCIDENT. REPLACED NOSE LANDING DOOR ACTUATOR AND SELECTOR VALVE FILTER. SERVICED NOSE STRUT. PERFORMED SEVERAL GEAR EXTENSIONS AND RETRACTIONS. SYTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001052900225 20010529 00225 EU 2001 5 29 AALA20010783 1 20010414 A 2121 6459951 FAN FOKKER F28 F28MK0100 4990807 EU A/C BAY FAULTY A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 1456D 11468 DFW - FLT 2393 - EN ROUTE MDW-DFW - CREW REPORTS FUMES AND SMOKE IN CABIN. ACCOMPLISHED SMOKE/FIRE CHECKLISTS. DECLARE D EMERGENCY PROCEEDED TO DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED RIGHT SIDE RECIRCULATION FAN. PERFORMED PAC K BURNOUT PER THE MM. NO SMOKE OR ODOR NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001052900226 20010529 00226 EU 2001 5 29 AALA20010593 1 20010322 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN DAMAGED A K NONE O OTHER IN INSP/MAINT 1 SW 21 1400H 11340 IAH - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 11 PULSES ON AND OFF. REPAIRED EMERGENCY EXIT LIGHT WIR E AT ROW 11. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001052900227 20010529 00227 EU 2001 5 29 AALA20010600 1 20010323 A 3350 CONNECTOR FOKKER F28 F28MK0100 4990807 EU CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1410E 11368 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT MODULE INOPERATIVE. RE-CONNECTED EMERGENCY EXI LIGHT MODULE CO NNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001052900228 20010529 00228 EU 2001 5 29 AALA20010641 1 20010328 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1412A 11370 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM G ROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001052900229 20010529 00229 EU 2001 5 29 AALA20010710 1 20010408 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU COCKPIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1474D 11520 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT DOME LIGHT AT FLIGHT DECK INOPERATIVE. REPLACED EMERGENCY EXIT DOME LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001052900230 20010529 00230 EU 2001 5 29 AALA20010662 1 20010330 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 21 1423A 11406 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT WIRE AT AISLE FOUR BROKEN. REPAIRED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001052900231 20010529 00231 EU 2001 5 29 AALA20010605 1 20010321 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN DAMAGED A K NONE L NO TEST IN INSP/MAINT 1 SW 21 1474D 11520 ORD - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT AT ROW 11 INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001052900232 20010529 00232 EU 2001 5 29 AALA20010606 1 20010321 A 3350 CONNECTOR FOKKER F28 F28MK0100 4990807 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1449D 11458 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 13 INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT CONNECT OR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001052900233 20010529 00233 EU 2001 5 29 AALA20010604 1 20010321 A 3350 CONNECTOR FOKKER F28 F28MK0100 4990807 EU CABIN LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 1418A 11397 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 1 THROUGH 11 OPERATES INTERMITTENTLY. RE-SECURED EMERGE NCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001052900234 20010529 00234 EU 2001 5 29 AALA20010520 1 20010317 A 3350 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 1432A 11417 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 20H THROUGH 29H DIM. REPLACED EMERGENCY EXIT LIGHT BAT TERY PACK AT SEATS 24H AND 25H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001052900235 20010529 00235 EU 2001 5 29 AALA20010591 1 20010322 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1440A 11435 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT FORWARD CLOSET INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT S PLICE AT FORWARD CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001052900236 20010529 00236 NM 2001 5 29 AALA20010792 1 20010411 A 5330 SKIN BOEING 727 727227 1384078 NM FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 723AA 20731 TUL - FOUND GOUGE IN FUSELAGE SKIN, FS 965. BLENDED AND INSTALLED DOUBLER .080 2024T3 PER AARD 53-30-3. (M) 2 L 7 3 4F A3WE 2001052900237 20010529 00237 NM 2001 5 29 AALA20010816 1 20010417 A 5720 ANGLE BOEING 727 727227 1384078 NM WING CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 721AA 20729 TUL - FOUND CHORD ANGLE CRACKED BELOW NR 7 SPOILER ACTUATOR MOUNT BRACKET. STOP DRILLED CRACK. INSTALLED REPAIR DOUBLE R PER SRM 51-20-1. MAT 7075-T6 ORIG REPAIR .063 301.5 HARD INSTALLED 3 ROWS PAST DAMAGE .25 INCH STEEL PER 51-40-4 PAGE 1. (M) 2 L 7 3 4F A3WE 2001052900238 20010529 00238 NM 2001 5 29 AALA20010817 1 20010408 A 5330 SKIN BOEING 727 727227 1384078 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 721AA 20729 TUL - FOUND SKIN BULGING AT SKIN LAP FROM STATION 590 TO STATION 620 STRINGER 26L. CUT OUT CORRODED SKIN. INSTALLED RE PAIR DOUBLER PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 2001052900239 20010529 00239 NM 2001 5 29 AALA20010818 1 20010410 A 5330 SKIN BOEING 727 727227 1384078 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 721AA 20729 TUL - FOUND SKIN BULGING AT SKIN LAP FROM STATION 480 TO 490. INSTALLED DOUBLER AND TRIPLER PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 2001052900240 20010529 00240 NM 2001 5 29 AALA20010819 1 20010416 A 5730 SKIN BOEING 727 727227 1384078 NM CENTER WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 721AA 20729 TUL - CENTER WING LOWER SKIN BULGING INBOARD OF RIGHT SECONDARY HEAT EXCHANGER FS 787-790. INSTALLED DOUBLER AND TRIPLE R PER RM 57-30-3 PAGE 1. (M) 2 L 7 3 4F A3WE 2001052900241 20010529 00241 WP 2001 5 29 AALA20010780 1 20010415 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7538A 49992 DFW - DURING OVERNIGHT MAINTENANCE, PORTABLE EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED PORTABLE EMERGENCY EXIT LIGHT A SSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900242 20010529 00242 WP 2001 5 29 AALA20010770 1 20010410 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7549A 53031 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT AT SEAT 13D, 19D, 28D, 29D, AND 31D, DIM. REPLACED EMERGENCY EX IT LIGHT AT SEAT 13D, 19D, 28D, 29D, AND 31D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900243 20010529 00243 WP 2001 5 29 AALA20010773 1 20010412 A 3350 8039001 BATTERY DOUG DC9 DC982 3022082 WP AIRSTAIRS DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 560AA 53090 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900244 20010529 00244 WP 2001 5 29 AALA20010802 1 20010417 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 566AA 49348 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PORTABLE LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT PORTABLE LIGHT A SSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001052900245 20010529 00245 WP 2001 5 29 AALA20010807 1 20010418 A 3397 WIRE DOUG DC9 DC982 3022082 WP TAILCONE BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 21 432AA 49350 DFW - DURING OVERNIGHT MAINTENANCE, TAIL CONE EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED TAIL CONE EMERGENCY EXIT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900246 20010529 00246 WP 2001 5 29 AALA20010824 1 20010422 A 3350 8039001 BATTERY DOUG DC9 DC982 3022082 WP L1/R1 DOOR DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 225AA 49175 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT AT R1 AND L1 DOOR DIM. REPLACED EMEREGNCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900247 20010529 00247 WP 2001 5 29 AALA20010826 1 20010422 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7509 49803 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 7 DIM. REPLACED EMERGENCY EXIT LIGHT AT ROW 7. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900248 20010529 00248 WP 2001 5 29 AALA20010827 1 20010421 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70504 49798 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 7D DIM. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT ROW 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900249 20010529 00249 WP 2001 5 29 AALA20010830 1 20010421 A 3350 SOCKET DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 481AA 49656 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 12D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET AT SEAT 12D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900250 20010529 00250 WP 2001 5 29 AALA20010834 1 20010420 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 18D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 18D. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900251 20010529 00251 WP 2001 5 29 AALA20010835 1 20010420 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 9D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 9D. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900252 20010529 00252 WP 2001 5 29 AALA20010836 1 20010420 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 8D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 8D. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900253 20010529 00253 WP 2001 5 29 AALA20010839 1 20010421 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AA 49300 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT OVERWING EXIT TOO BRIGHT. REPLACED EMERGENCY EXIT LIGHT AT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900254 20010529 00254 WP 2001 5 29 AALA20010843 1 20010423 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 9D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 9D. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900255 20010529 00255 NM 2001 5 29 AALA20010850 1 20010420 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 862AA 21089 TUL - FOUND CORROSION ON SKIN AT STATION 950F PLUS 3 - 950F PLUS 7, LEFT SIDE OF STRINGER 30. REMOVED CORROSION AND DAM AGED SKIN PER SRM 51-10-6. REPAIRED SKIN AT STATINO 950F PLUS 3 - 950F PLUS 7 PER 53-30-3 FIG 3. (M) 2 L 7 3 4F A3WE 2001052900256 20010529 00256 NM 2001 5 29 AALA20010851 1 20010419 A 5320 6518915265 ANGLE BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 862AA 21089 TUL - FOUND CORROSION ON ANGLE FOR FLOOR SUPPORT IN RIGHT NWW TUNNEL. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PE R ESO 11697 DATED 4-18-01. (M) 2 L 7 3 4F A3WE 2001052900257 20010529 00257 NM 2001 5 29 AALA20010852 1 20010418 A 5313 STRINGER BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 862AA 21089 TUL - FOUND CORROSION ON STRINGER 29R, AFT OF STATION 950E. REMOVED CORROSION AND INSTALLED REPAIR PER ESO 11697, DATED 4-18-2001. (M) 2 L 7 3 4F A3WE 2001052900258 20010529 00258 EU 2001 5 29 R7MR33080 1 20010329 A 6500 4619002005 GEARBOX BOLKMS 105 BO105S 5626006 EU TAIL ROTOR CONTAMINATED E R7MA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 485EC S754 AFTER SERVICING THE GEARBOX AND ON FIRST RUN THE PILOT NOTICED A CHIP LIGHT. THE AIRCRAFT WAS SHUTDOWN AND THE GEARBOX INSPECTED. UPON REMOVING THE OIL SITE GLASS THE MECHANIC NOTICED BLACK MATERIAL AND VER SMALL SPECKS OF SHINY METALLIC PARTICLES IN THE OIL. THE GEARBOX WAS FLUSHED TWICE AND EACH TIME THE PILOT RECEIVED A CHIP LIGHT. GEARBOX REMOVED FRO M SERVICE DUE TO METAL CONTAMINATION AND REPLACED WITH OVERHAULED, CORRECTED PROBLEM. 1 G 7 2 3U H3EU 2001052900259 20010529 00259 NE 2001 5 29 R7MR33142 2 20010118 A 7250 414104802 SLEEVE BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101650B1 41560 NE NR 3 BEARING WORN E R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 61LF 447 7230 WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2001052900261 20010529 00261 NE 2001 5 29 KBMA33147 2 20010118 A 7250 430144801 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101650B1 41560 NE NR 3 BEARING LEAKING E R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 61LF 447 7230 LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2001052900262 20010529 00262 2001 5 29 R7MR33197 4 20010322 A 3425 5040121910 INDICATOR SNIAS 350 AS350B3 8680954 EU COCKPIT INOPERATIVE E R7MR K NONE L NO TEST IN INSP/MAINT 1 NM 07 397LG 222 3268 UNIT INOPERATIVE. GYRO WILL NOT CAGE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 2001052900263 20010529 00263 NE 2001 5 29 R7MR33253 2 20010321 A 7320 0292928540 FMU SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE FUEL CONTROL LEAKING E R7MR K NONE K FLUID LOSS IN INSP/MAINT 1 NM 07 397LG 220 3268 LEAKING FUEL FROM DRIVE DRAIN. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2001052900264 20010529 00264 EU 2001 5 29 R7MR33256 1 20010420 A 5610 350120234 WINDSHIELD SNIAS 350 AS350B2 8680813 EU COCKPIT DISTORTED E R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 213LP 2828 EXCESSIVE DISTORTIONS CAUSING VISUAL PROBLEMS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 2001052900265 20010529 00265 EU 2001 5 29 R7MR33257 1 20010501 A 5610 350120233 WINDSHIELD SNIAS 350 AS350B2 8680813 EU COCKPIT DISTORTED E R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 213LP 2828 EXCESSIVE DISTORTIONS CAUSING VISUAL PROBLEMS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 2001052900266 20010529 00266 EU 2001 5 29 R7MR33258 1 20010420 A 5610 350120233 WINDSHIELD SNIAS 350 AS350B2 8680813 EU COCKPIT DISTORTED E R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 213LP 2828 EXCESSIVE DISTORTIONS CAUSING VISUAL PROBLEMS. REPLACED WITH UNCOATED WINDSHIELD, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 2001052900267 20010529 00267 EU 2001 5 29 R7MR33259 1 20010420 A 5610 350120234 WINDSHIELD SNIAS 350 AS350B2 8680813 EU COCKPIT DISTORTED E R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 213LP 2828 EXCESSIVE DISTORTIONS CAUSING VISUAL PROBLEMS. REPLACED WITH UNCOATED WINDSHIELD CORRECTED PROBLEM. 1 G 7 1 3U H9EU 2001052900268 20010529 00268 EA 2001 5 29 R7MR33267 1 20010127 A 7110 900F3318201101 DAMPER CNDAIR CL600 CL6002B19 EA COWLING WORN E R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 01 4396 7141 WORN BEYOND SERVICEABLE LIMITS. FAILD SPRING CHECK. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 2 L 7 2 4F RT A21EA 2001052900270 20010529 00270 EA 2001 5 29 FWRA2001003 2 20010511 A 8520 76220 THRU BOLT PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA NR 3 CYLINDER FRACTURED G FWRA A UNSCHED LANDING A R FLAME/FIRE PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 01 45008 1097 318052167 L697661A AT CRUISE FLIGHT, THE NR 3 CYLINDER SEPARATED FROM THE ENGINE CASE, WHICH RESULTED IN AN INFLIGHT FIRE. THE ENGINE CASE , CYLINDER HOLD DOWN STUDS, THROUGH BOLT STUDS AND NR 3 CONNECTING ROD WERE SENT FOR LABORATORY INVESTIGATION. THE IN VESTIGATION RESULTED IN THE FOLLOWING CONCLUSION: THE PRIMARY CAUSE WHICH LED TO THE SEPARATION OF THE NR 3 CYLINDER WA S THAT THE THROUGH BOLT STUDS WERE MOST LIKELY NOT PROPERLY TORQUED. 1 L 7 2 3O 3 O A20SO E14EA 2001052900274 20010529 00274 NM 2001 5 29 N8TA01042303 1 20010411 A 3350 20131A BATTERY BOEING 757 757231 1384950 NM CABIN DISCHARGED A N8TA K NONE L NO TEST IN INSP/MAINT 1 WP 19 522NA 25133 AIRCRAFT HAD BEEN ON GROUND FOR 5 DAYS WITHOUT POWER APPLIED. UPON TEST OF EMERGENCY LIGHTS FWD ENTRY DOOR BATTERY PACK LIGHTS WOULD NOT ILLUMINATE. CHARGED BATTERY PACK; OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A2NM 2001052900275 20010529 00275 NM 2001 5 29 N8TA01042302 1 20010402 A 3350 20131 BATTERY BOEING 757 757231 1384950 NM CABIN DISCHARGED A N8TA K NONE L NO TEST IN INSP/MAINT 1 WP 19 522NA 25133 R2 DOOR EMERGENCY EXIT LIGHT AFT OF DOOR R2 DOES NOT ILLUMINATE WITH CREW OR ATTENDANT SWITCH. AIRCRAFT HAD BEEN SETTIN G WITHOUT ANY POWER APPLIED. RECHARGED BATTERY; OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A2NM 2001052900276 20010529 00276 NM 2001 5 29 N8TA01042301 1 20010402 A 3350 20131 BATTERY BOEING 757 757231 1384950 NM R2 DOOR DISCHARGED A N8TA K NONE L NO TEST IN INSP/MAINT 1 WP 19 522NA 25133 R2 DOOR EMERGENCY EXIT LIGHTS FAILED TO ILLUMINATE USING CREW OR ATTENDANT SWITCHES. AIRCRAFT HAD BEEN SETTING 5 DAYS WI THOUT ANY POWER APPLIED. 2 L 7 2 4F RT A2NM 2001052900277 20010529 00277 EA 2001 5 29 COEA0101222 1 20010212 A 3246 9541587 WHEEL FRCHLD F27 F27F 3373008 EA RT MLG DEPARTED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 222DG 275 31 AFTER LANDING, MAINTENANCE DISCOVERED THAT THE RT MLG WHEEL ASSEMBLY WAS MISSING. AXLE NUT AND SECURING BOLT WERE NOT R ECOVERED. NO DAMAGE TO LANDING GEAR AXLE WAS FOUND SO MAINTENANCE INSTALLED ANOTHER WHEEL ASSEMBLY AND RETURNED THE AIR CRAFT TO SERVICE. INVESTIGATION DID NOT REVEAL THE CAUSE OF THE WHEEL SEPARATION. 2 H 7 2 4T 7A1 2001052900278 20010529 00278 NM 2001 5 29 N8TA01042305 1 20010417 A 5520 BEARING BOEING 757 757* NM ELEVATOR WORN A N8TA O OTHER E VIBRATION/BUFFET CR CRUISE 1 WP 19 542NA 26245 LEVEL AT FL 350 AT MACH .80, EXPERIENCED WHAT APPEARED TO BE ELEVATOR FLUTTER FOR APPROX 1 MINUTE. DESCENDED TO FL 310, REDUCED TO MACH .78. SITUATION DID NOT RECUR. PERFORMED ELEVATOR FREE PLAY CHECK; NO DEFECTS FOUND. AS A PRECAUTION REPLACED IDLER LINK BEARINGS AND REACTION LINK BEARINGS ON ALL 3 LEFT AND RIGHT ELEVATOR PCA. OPERATIONALLY TESTED AND ACCOMPLISHED FLIGHT TEST WITH NO DISCREPANCIES. 2 L 7 2 4F RT A2NM 2001052900279 20010529 00279 2001 5 29 N8TA01042304 4 20010416 A 2565 BACR12BU9B RING BOEING 757 757231 1384950 NM SLIDE FAILED A N8TA K NONE L NO TEST IN INSP/MAINT 1 WP 19 522NA 25133 DURING OPERATIONAL TESTING OF THE SLIDE THE LATCH SPLIT RING FAILED. SLIDE DID NOT DEPLOY. INCORPORATED SB, LATCH ASSE MBLY MODIFICATION. 2 L 7 2 4F RT A2NM 2001052900284 20010529 00284 GL 2001 5 29 20010524CW003 1 20010506 A 2150 5861108 A/C PACK BOMBDR BD700 BD7001A10 1390006 GL A/C BAY SEIZED E ERYA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 07 722HP 1039 ON THE GROUND WITH APU SUPPLYING BLEED AIR, RIGHT ACU SELECTED ON, SMOKE ENTERED THE CABIN. 2 L 7 2 4F RT T00003NY 2001052900285 20010529 00285 NM 2001 5 29 COOSDR010032 1 20010524 A 5744 65217767 SUPPORT BOEING 727 72731 1384010 NM LT WING CRACKED E K NONE O OTHER IN INSP/MAINT 1 EA 25 220NE 18905 LEFT WING AILERON, SUPPORT ASSY PN 65-21776-7 LUG CRACKED. 2 L 7 3 4F A3WE 2001052900286 20010529 00286 NM 2001 5 29 COOSDR010033 1 20010524 A 2710 652440013 FITTING BOEING 727 72731 1384010 NM GEARBOX CRACKED E K NONE O OTHER IN INSP/MAINT 1 EA 25 220NE 18905 LEFT WING AILERON, GEAR BOX ASSY P/N 65-24400-13 LUG CRACKED. 2 L 7 3 4F A3WE 2001052900287 20010529 00287 CE 2001 5 29 WVBA2001031 1 20010516 A 2701 15703081 CONTROL CABLE CESSNA 206 U206A 2073316 CE YOKE OUT OF POSITION E A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 AL 01 756DJ U20604005 PILOT REPORTED UNCONTROLLABLE PITCH CONTROL AND LIMITED AILERON CONTROL. IN FLIGHT, AFTER TAKEOFF, WHICH RESULTED IN A CRASH LANDING. ON EXAMINATION OF THE AIRCRAFT IT WAS DISCOVERED THAT THE RIBBON CABLE ASSY FOR ELECTRICAL CONTROLS ON T HE YOKE, HAD FOULED THE CONTROL WHEEL BEARING ASSEMBLY. (UNIVERSAL) BY JAMMING THE CABLE BETWEEN THE ROLLERS AND THE CON TROL TUBE. THIS KEPT THE PILOT FROM HAVING ELEVATOR RESPONSE UNLESS MAXIMUM FORCE WAS APPLIED. 1 H 7 1 3O A4CE 2001052900288 20010529 00288 EA 2001 5 29 WVBA2001033 2 20010517 A 7314 RG9080J7SM PUMP PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA FUEL SYSTEM LEAKING E WVBA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 01 3527U 276 276 317952141 DURING INSPECTION IT WAS NOTICED THAT FUEL STAIN WAS ON THE BODY OF THE FUEL PUMP NEAR THE DRAIN COMING FROM THE PARTING SURFACE (LOWER) NOTE THIS IS A NEW STYLE PUMP DESIGNED TO RELIEVE THE LEAKING PROBLEM THE OLDER PUMPS HAD IN THIS AREA . THE PUMP WAS REPLACED WITH A SERVICABLE UNIT. 1 L 7 2 3O 3 O A20SO E14EA 2001052900289 20010529 00289 NM 2001 5 29 COOSDR010019 1 20010524 A 5730 SKIN BOEING 727 727233 138408A NM WING CORRODED E EE4Y K NONE O OTHER IN INSP/MAINT 1 EA 25 395AJ 21100 WING CENTER SECTION UPPER SKIN CORRODED. LOCATION BS 783.95, RBL 63.0, BTWN S-14 AND S-16. 2 L 7 3 4F RT A3WE 2001052900291 20010529 00291 NM 2001 5 29 USAASB01121 1 20010430 A 2133 7110033 OUTFLOW VALVE BOEING 737 7373B7 1384580 NM CABIN PRESSURE MALFUNCTIONED A USAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 397US 36807 23319 PIT - FLT 1107 - EN ROUTE FROM YYZ TO CLT, AT FL350, THE CABIN ALTITUDE ALERT SOUNDED AS CABIN WAS AT 10,000 FEET AND CL IMBING AT APPROXIMATELY 600 FEET PER MINUTES. CREW INITIATED DESCENT TO FL115 AND COMPLIED WITH QUICK REFERENCE HANDBOO K PROCEDURES BUT OUTFLOW VALVE WAS NOT CONTROLLABLE. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. NO OX YGEN MASKS WERE DEPLOYED AN NO EMERGENCY WAS DECLARED. MAINTENANCE ACCOMPLISHED OPERATIONAL CHECK PER MM 21-31-00 AND F OUND THE AFT OUTFLOW VALVE INTERMITTENT. REMOVED AND REPLACED AFT OUTFLOW VALVE. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001052900292 20010529 00292 EU 2001 5 29 USAAF01018 1 20010430 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 880US 11331 IND - THE AFT CABIN EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK IN THE POWER SUPPLY. OPS CHECKED OK. (M) 2 L 7 2 4F RT 2001052900293 20010529 00293 EU 2001 5 29 USAAF01019 1 20010505 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK1000 4990808 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 868US 11313 IND - THE EMERGENCY LIGHTS AND EMERGENCY EXIT LIGHT IN THE FORWARD ENTRANCE AREA WERE FOUND INOPERATIVE. MAINTENANCE RE PLACED THE BATTERY PACK IN THE POWER SUPPLY. OPS CHECKED OK. (M) 2 L 7 2 4F RT A20EU 2001052900294 20010529 00294 EU 2001 5 29 USAAF01020 1 20010507 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 884US 11338 IND - THE AFT CENTER CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATERY PACK IN THE POWER S UPPLY. OPS CHECKED OK. (M) 2 L 7 2 4F RT 2001052900295 20010529 00295 EU 2001 5 29 USAA010458 1 20010425 A 5330 SKIN AIRBUS 320 A320214 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 110UW 2559 1112 CLT - FOUND FUSELAGE SKIN CRACKED 4 INCHES, FRAME 79 JUST AFT OF BETWEEN S1R AND S2R. INSTALLED DOUBLER PER SRM 53-00-1 1, PAGE 209/210. (M) 2 L 7 2 4F RT A28NM 2001052900296 20010529 00296 CE 2001 5 29 20010525SG007 1 20010501 A 7722 13038004113 INDICATOR BEECH 1900 1900D 1154162 CE COCKPIT FAULTY A JJBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 01 847CA UE52 ABORTED TAKEOFF DUE TO LEFT ENGINE ITT INDICATION HIGH. REPLACED ITT INDICATOR. OPS CHECKED SATISFACTORY. (M) 2 L 7 2 4T RT A24CE 2001052900297 20010529 00297 NM 2001 5 29 20010525SG008 1 20010501 A 3350 3071BPEGPL LIGHT BOEING 757 757236 NM CABIN INOPERATIVE A N8TA K NONE L NO TEST IN INSP/MAINT 1 WP 19 544NA 29942 FOUND EMERGENCY LIGHTS ROW 11 INOPERATIVE. REPLACED LAMPS. (M) 2 L 7 2 4F RT A2NM 2001052900298 20010529 00298 NM 2001 5 29 20010529SG001 1 20010430 A 3397 WIRE BOEING 757 757236 1384971 NM CABIN EXPOSED A K NONE O OTHER IN INSP/MAINT 1 WP 19 544NA 29942 WIRES STICKING OUT FROM UNDER COVER. RESTOWED WIRES AND SECURED COVER. (M) 2 L 7 2 4F RT A2NM 2001052900299 20010529 00299 NM 2001 5 29 20010529SG002 1 20010429 A 3350 3071BPEGPL LIGHT BOEING 757 757236 NM CABIN INOPERATIVE A N8TA K NONE L NO TEST IN INSP/MAINT 1 WP 19 547NA 29946 EMERGENCY LIGHTS AT ROW 4 INOPERATIVE. REPLACE LAMPS. (M) 2 L 7 2 4F RT A2NM 2001052900300 20010529 00300 NM 2001 5 29 BJNA010501 1 20010503 A 3350 1315 LIGHT BOEING 737 737214 138446R NM CABIN INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 457TM 20156 L1 EMERGENCY EXIT OVER DOOR LIGHT INOPERATIVE. RELAMPED PER BMM 33-51-101, OPS CHECK NORMAL. (M) 2 L 7 2 4F A16WE 2001052900301 20010529 00301 NM 2001 5 29 BJNA010502 1 20010503 A 3350 LIGHT BOEING 737 737214 138446R NM CABIN INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 457TM 20156 ROW 5 SEAT EMERGENCY LIGHT INOPERATIVE. RESEATED LAMP IN SOCKET, OPS CHECK NORMAL. (M) 2 L 7 2 4F A16WE 2001052900302 20010529 00302 NM 2001 5 29 BJNA010503 1 20010507 A 3350 900835A BATTERY PACK BOEING 737 737282 13844AT NM CABIN DISCHARGED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 233TM 23043 CENTER CABIN EMERGENCY EXIT SIGN LIGHTS INOPERATIVE. REMOVED AND REPLACED LIGHTS BATTERY PACKS 2. OPS CHECK OF EMERGEN CY EXIT LIGHTS GOOD IAW BMM 33-51-51. (M) 2 L 7 2 4F RT A16WE 2001052900303 20010529 00303 WP 2001 5 29 AALA016045 1 20010421 A 3350 BR9194501 LIGHT DOUG DC9 DC987 3022087 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 755RA 49727 CCI - RIGHT AFT EMERGENCY EXIT LIGHT AND 3 RED PATH LIGHTS INOPERATIVE. REMOVED AND REPLACED RIGHT AFT EMERGENCY EXIT L IGHT PACK. OPS CHECK GOOD ON PATH LIGHT PACK. OPS CHECK GOOD ON PATH LIGHTS AND EXIT LIGHTS. (M) 2 L 7 2 4F RT A6WE 2001052900304 20010529 00304 WP 2001 5 29 AALA016046 1 20010426 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 822RA 49932 CABIN EMERGENCY LIGHTS ON RIGHT SIDEWALL CAME ON IN FLIGHT. REPLACED EMERGENCY LIGHT POWER PACK AT AFT RIGHT EXIT DOOR. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2001052900305 20010529 00305 WP 2001 5 29 AALA016047 1 20010428 A 3350 BR964411 LIGHT DOUG DC9 DC983 3022083 WP CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 832RA 53044 MAIN ENTRY, FOUND EMERGENCY ESCAPE PATH LIGHT AT SEAT 3EF DAMAGED. REPLACED EMERGENCY ESCAPE PATH LIGHT SEAT 3EF. OPS CHECK GOOD. REMOVED PLACARD MEL 04-110-C CLEARED MIC SHEET. (M) 2 L 7 2 4F RT A6WE 2001052900306 20010529 00306 NE 2001 5 29 20010529SG003 2 20010423 A 7200 ENGINE LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE NR 1 VIBRATION A WRNA E A ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 05 311EA 193A1012 ENGINE SHUTDOWN FOR HIGH VIBRATION INDICATION AT FL350. IN CRUISE INDICATION 3 AND AMBER LIGHT. BOTH A AND B PICKUPS. LOW SELECTION INDICATES THIS PROBLEM. TEST CARRIED OUT IAW 71-00-00 TEST 16. ALL TRIM WEIGHTS REMOVED. EPR 1.53=1.3 UNITS 90 PERCENT N1=1.0, 85 PERCENT = .8, 80 PERCENT = .4. (M) 2 L 7 3 4F 4 F A23WE E12EU 2001052900307 20010529 00307 NM 2001 5 29 TSAA0151047 1 20010423 A 5330 6545866688 SKIN BOEING 737 737282C 13844AU NM FUSELAGE CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 826AL 23051 FOUND BS 500B, CORROSION FOUND AT STATION 500B STRINGER 28R KEEL BEAM. REMOVED CORROSION AND CUT OUT A 5 INCH HOLE. FA BRICATED FILLER AND SKIN PATCH. INSTALLED FILLER, PATCH PER SRM 51-10-6 PAGE 4, REPAIR COMPLETED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001052900308 20010529 00308 NM 2001 5 29 TSAA0151042 1 20010426 A 5315 101362401 FLOORBEAM BOEING 737 7372T4 1384492 NM FUSELAGE CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 808AL 23445 EXFOLIATION CORROSION DISCOVERED ON FLOORBEAM AT BS 277. REMOVED CORROSION BY CLEANING AND TREATING AFFECTED AREA PER S RM 51-10-6. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2001052900309 20010529 00309 NM 2001 5 29 TSAA0151044 1 20010426 A 5315 101362401 FLOORBEAM BOEING 737 7372T4 1384492 NM FUSELAGE CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 808AL 23445 EXFOLIATED CORROSION DISCOVERED ON FLOORBEAM AT BS 294.5 PLUS 8 AND PLUS 13 RBL 12. REMOVED CORROSION BY REPLACING THE FLOORBEAM SECTION AT BS 294.5 PLUS 8 AND PLUS 13 IAW BOEING DRAWING 65-45808. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2001052900310 20010529 00310 NM 2001 5 29 TSAA0151045 1 20010426 A 5315 101362401 FLOORBEAM BOEING 737 7372T4 1384492 NM FUSELAGE CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 808AL 23445 SURFACE CORROSION DISCOVERED ON FLOORBEAM AT BS 312, LBL 12 TO RBL 12. REMOVED CORROSION BY REPLACING THE INTERCOSTAL IA W SRM 51-10-01. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2001052900311 20010529 00311 WP 2001 5 29 AALA20010864 1 20010425 A 4990 O-RING DOUG DC9 DC982 3022082 WP APU LEAKING A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 218AA 49168 DFW - FLT 2090 - EN ROUTE SAN-DFW - SHORTLY AFTER TAKEOFF, DETECTED HAZE IN CABIN. LANDED DFW WITHOUT FURTHER INCIDENT. REPLACED MAGNETIC DRAIN PLUG O-RING AT APU. PERFORMED LEAK CHECK. NO LEAKS NOTED. PERFORMED PACK BURNOUT PER THE MM . SYSTEM GRUOND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900312 20010529 00312 WP 2001 5 29 AALA20010886 1 20010430 A 2910 PLUG DOUG DC9 DC982 3022082 WP RUDDER LOOSE A AALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 427AA 49339 DFW - FLT 1104 - EN ROUTE LAS-DFW - DETECTED DECREASE RIGHT SIDE HYDRAULIC QUANTITY. RIGHT SIDE HYDRAUILC SYSTEM SHUT O FF WITH A QUANTITY OF FOUR QUARTS. LANDED WITHOUT FURTHER INCIDENT. RE-SECURED PLUG AT RIGHT SIDE RUDDER SHUTOFF VALVE . NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001052900313 20010529 00313 WP 2001 5 29 AALA20010889 1 20010414 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 TUL - FOUND RIGHT AFT LAVATORY STATION 1338 FLOORBEAM DAMAGED, CORROSION AROUND FASTENER HOLE. REPAIRED FLOORBEAM PER S RM 53-05 PART 1. (M) 2 L 7 2 4F A6WE 2001052900314 20010529 00314 WP 2001 5 29 AALA20010891 1 20010412 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 TUL - FOUND CORROSION ON SEAT TRACK 6 AT STATION 215. REMOVED CORRODED SECTION AND SPLICED IN NEW SEAT TRACK FROM STATI ON 215 TO 303 PER 53-05 PT 1 FIG 4F. (M) 2 L 7 2 4F A6WE 2001052900315 20010529 00315 WP 2001 5 29 AALA20010892 1 20010410 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 426AA 49338 TUL - FOUND LONGERON 4L CRACKED AT STATION 160. REPAIRED PER SRM 53-02, FIG 18. (M) 2 L 7 2 4F A6WE 2001052900316 20010529 00316 WP 2001 5 29 AALA20010893 1 20010409 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 TUL - FOUND CORROSION AND WEAR ON SEAT TRACK NR 1 FROM 1118-1121. INSTALLED SEAT TRACK PLUG STATION 1110-1123 PER SRM 5 3-05 PART 1, FIG 4A. APPLIED COAT OF WHITE POLYURETHANE PAINT. (M) 2 L 7 2 4F A6WE 2001052900317 20010529 00317 NM 2001 5 29 AALA20010853 1 20010418 A 5730 SKIN BOEING 727 727223 1384074 NM RT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 862AA 21089 TUL - FOUND CORROSION FOUND AT STATION 725 ON LOWER TRAILING EDGE OF WING, RT WING. REMOVED CORROSION AND INSTALLED DOU BLER PER ESO DATED 4/18/2001 ESO 11697. (M) 2 L 7 3 4F A3WE 2001052900318 20010529 00318 NM 2001 5 29 AALA20010854 1 20010419 A 5310 SHEAR TIE BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 862AA 21089 TUL - FOUND CORROSION AT SHEAR TIE BETWEEN STRINGER 28R AND 29R AT STATION 950E PLUS 5 INCHES. REMOVED CORROSION AND IN STALLED SHEAR TIE REPAIR AS PER 53-10-4 OF SRM. (M) 2 L 7 3 4F A3WE 2001052900319 20010529 00319 NM 2001 5 29 AALA20010844 1 20010418 A 5320 STIFFENER BOEING 727 727223 1384074 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 890AA 22006 TUL - FOUND AFT BULKHEAD 1183 RIGHT BL 9 VERTICAL STIFFENER HAS CRACK UNDER OUTBOARD TOWER RADIUS BLOCK. STOP DRILLED C RACK AND INSTALLED REPAIR AS PER SB 727-53-0175. (M) 2 L 7 3 4F A3WE 2001052900320 20010529 00320 NM 2001 5 29 AALA20010845 1 20010418 A 5510 BEAM BOEING 727 727223 1384074 NM HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 890AA 22006 TUL - FOUND LEFT HORIZONTAL T/E BEAM CORRODED AT OUTBOARD END. REMOVED CORROSION AND INSTALLED DOUBLER PER ESO 11697 DA TED 4/17/01. (M) 2 L 7 3 4F A3WE 2001052900321 20010529 00321 NM 2001 5 29 AALA20010846 1 20010418 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 890AA 22006 TUL - FOUND FORWARD ENTRY DOOR UPPER HINGE CUTOUT CRACKED. INSTALLED DOUBLER IAW SB 727-53-0198 FIG 4, TRIMMED OUT CRAC K. (M) 2 L 7 3 4F A3WE 2001052900322 20010529 00322 EA 2001 5 29 UHLA003405 1 20010428 A 3350 1004021 CONNECTOR DHAV DHC8 DHC8311 1386006 EA CABIN LOOSE A UHLA K NONE L NO TEST IN INSP/MAINT 1 NE 03 802SA 250 FLT 498 - BUF-BED - DURING PILOT PREFLIGHT CREW NOTED MAIN DOOR EXIT SIGN NOT ILLUMINATING. FOUND LOOSE CONNECTION. RE SECURED CONNECTION IAW DMM 25-60-00, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 2001052900323 20010529 00323 NM 2001 5 29 UIEA01054 1 20010427 A 5300 SKIN BOEING 747 7472D3B 1384805 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 78537 21251 DURING HFEC INSPECTION PER SB 747-53A2488 FOUND LOWER LOBE CARGO COMPARTMENT AFT DOOR UPPER CUT OUT, FORWARD CORNER CRAC KED UNDER 2 INCH. SHIMS OVER .055 THICK. TRIMMED OUT CRACK. FABRICATED FILLER AND REPAIR DOUBLER. INSTALLED IAW SRM 53-30-03 TYPE II. (M) 2 L 7 4 4F RT A20WE 2001052900324 20010529 00324 WP 2001 5 29 USAA010453 1 20010425 A 5330 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 809US 52897 48041 CLT - FOUND 2 CRACKS IN FUSELAGE SKIN, BS 58.75, RIGHT SIDE APPROX 10 INCHES BELOW FLOORLINE. INSTALLED DOUBLER PER SRM 53-01, FIG 2. (M) 2 L 7 2 4F A6WE 2001052900325 20010529 00325 NM 2001 5 29 USAASB01128 1 20010507 A 3350 900835A BATTERY BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 275AU 22887 BDL - THE OVERHEAD EMERGENCY LIGHT FOR THE OVERWING EXITS WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BAT TERY. (M) 2 L 7 2 4F A16WE 2001052900326 20010529 00326 NM 2001 5 29 USAASB01126 1 20010502 A 3350 6104789 BATTERY BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 253AU 22795 BWI - THE LEFT AND RIGHT FORWARD DOOR EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY EXIT LI GHT BATTERY PACK. (M) 2 L 7 2 4F A16WE 2001052900327 20010529 00327 NM 2001 5 29 USAASB01118 1 20010428 A 3350 900542 POWER SUPPLY BOEING 737 737201 1384454 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 241US 22443 BWI - DURING WEEKLY CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT ROWS 7 ABC THROUGH15 ABC INOPERATIVE. MAINTEN ANCE REMOVED AND REPLACED THE POWER SUPPLY. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 2001052900328 20010529 00328 WP 2001 5 29 USAAD01092 1 20010503 A 3260 833703 PROXIMITY SENSOR DOUG DC9 DC981 3022081 WP RT MLG FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 800US 48034 PHL - BOS - FLT 343 - AFTER TAKEOFF, AND THE LANDING GEAR WAS RETRACTED, THE RIGHT MAIN GEAR RED LIGHT STAYED ILLUMINATE D. THE LANDING GEAR WAS CYCLED BUT THE RED LIGHT REMAINED ILLUMINATED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED W ITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT MAIN GEAR UP LOCK PROX SENSOR. (M) 2 L 7 2 4F A6WE 2001052900329 20010529 00329 WP 2001 5 29 USAAD01093 1 20010503 A 2150 1718567 COUPLING DOUG DC9 DC981 3022081 WP LT ACM DISCONNECTED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 803US 48035 CLT-MIA - FLT 895 - AFTER TAKEOFF THERE WAS A SLIGHT ODOR AND THE LEFT AIR CONDITIONING PACK TRIPPED OFF. WITH THE AIR CONDITIONING PACK OFF THE ODOR WENT AWAY. THE LEFT PACK WAS TURNED OFF FOR THE DURATION OF THE FLIGHT AND THE AIRCRAFT ARRIVED AT ITS DESTINATION WITHOUT INCIDENT. MAINTENANCE RECONNECTED FLEX COUPLING AT THE LEFT AIR CONDITIONING PACK AI R CYCLE MACHINE AND PROGRAMMED ITS REPLACEMENT AS A PRECAUTION. THE COUPLING AND CLAMPS WERE REPLACED AT THE MAINTENANC E OVERNIGHT. (M) 2 L 7 2 4F A6WE 2001052900330 20010529 00330 WP 2001 5 29 USAAD01094 1 20010503 A 2150 39271411 REGULATOR VALVE DOUG DC9 DC981 3022081 WP AC BAY FAILED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 803US 65430 33546 48035 MIA-CLT - FLT 1850 - AFTER TAKEOFF, THERE WAS A BURNING SMELL EMANATING FROM THE LEFT AIR CONDITIONING PACK. THE LEFT P ACK WAS SHUTOFF AND THE ODOR WENT AWAY. THE AIRCRAFT CONTINUED TO ITS DESTINATION AND LANDED WITHOUT INCIDENT. MAINTEN ANCE PLACED THE LEFT AIR CONDITIONING PACK ON MEL AND RELEASED THE AIRCRAFT FOR SERVICE. AT THE MAINTENANCE OVERNIGHT, THE LEFT AIR CONDITIONING PACK PRESSURE REGULATOR VALVE AND PILOT PRESSURE REGULATOR WERE REPLACED. (M) 2 L 7 2 4F A6WE 2001052900331 20010529 00331 WP 2001 5 29 20010529SG004 1 20010503 A 2150 39245431 REGULATOR DOUG DC9 DC981 3022081 WP AC BAY FAILED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 803US 45539 48035 MIA-CLT - FLT 1850 - AFTER TAKEOFF, THERE WAS A BURNING SMELL EMANATING FROM THE LEFT AIR CONDITIONING PACK. THE LEFT P ACK WAS SHUTOFF AND THE ODOR WENT AWAY. THE AIRCRAFT CONTINUED TO ITS DESTINATION AND LANDED WITHOUT INCIDENT. MAINTEN ANCE PLACED THE LEFT AIR CONDITIONING PACK ON MEL AND RELEASED THE AIRCRAFT FOR SERVICE. AT THE MAINTENANCE OVERNIGHT, THE LEFT AIR CONDITIONING PACK PRESSURE REGULATOR VALVE AND PILOT PRESSURE REGULATOR WERE REPLACED. (M) 2 L 7 2 4F A6WE 2001052900332 20010529 00332 WP 2001 5 29 USAAD01097 1 20010507 A 2150 39613011 CONTROL VALVE DOUG DC9 DC931 3022065 WP AC BAY FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 925VJ 42941 48145 DTW-PHL FLT 298 - AFTER TAKEOFF, THERE WAS A STRONG CHEMICAL SMELL. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHO UT INCIDENT. MAINTENANCE REPLACED THE LEFT AIR CONDITIONING FLOW CONTROL VALVE AND WATER SEPARATOR. (M) 2 L 7 2 4F A6WE 2001052900333 20010529 00333 EU 2001 5 29 COEA102740 1 20010430 A 3230 9804050100 VALVE FOKKER F27 F27MK600 4990706 EU LT MLG LEAKING A COEA O OTHER O OTHER AP APPROACH 1 NM 13 740FE 623 10329 DURING LANDING APPROACH TO PSC, LEFT MAIN LANDING GEAR WOULD NOT EXTEND. AFTER SEVERAL ATTEMPTS, FLIGHT CREW LOWERED GE AR USING EMERGENCY GEAR EXTENSION SYSTEM. LANDING GEAR PRESSURE REDUCER VALVE WAS FOUND TO BE THE CAUSE AND WAS SUBSEQU ENTLY REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T A817 2001052900334 20010529 00334 NE 2001 5 29 20010525CW003 2 20010507 A 7200 ENGINE LEAR 25 25 5170506 CE GE CJ610 CJ6101 30006 NE RIGHT FLAMED OUT E KKFA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 GL 23 222B 047 RIGHT HAND ENGINE FLAMED OUT DURING MAX ACCELERATION CHECK. ENGINE WAS RESTARTED AND UNEVENTFUL LANDING ACCOMPLISHED. COMPLIED WITH LEARJET SSK959 REPLACEMENT OF CJ610-6 ENGINE EXHAUST NOZZLE KIT. SATISFACTORYILY COMPLIED WITH ALTITUDE A CCELERATION CHECK AFTER NOZZLE REPLACEMENT. 2 L 7 2 4J 4 J A10CE 1E16 2001052900335 20010529 00335 EA 2001 5 29 20010525CW004 1 20010503 A 5610 60033030R WINDSHIELD CNDAIR CL600 CL6002B16 1900305 EA COCKPIT DELAMINATED D K NONE O OTHER IN INSP/MAINT 1 NM 03 140CH 1227 5047 WINDSHIELD MFG, SIERRACIN, DELAMINATED. 2 L 7 2 4F RT A21EA 2001052900339 20010529 00339 CE 2001 5 29 SDRS2001001 1 20010430 A 5751 991300003 SKIN BEECH 90 E90 1152914 CE AILERON CRACKED E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 28MS LW100 DURING SCHEDULED INSPECTION, TOP OF THE AILERON JUST OUTBOARD OF THE INNERMOST HINGE POINT ALONG THE LAP JOINT WAS FOUND TO BE CRACKED. CRACK WAS APPROX 4.5 INCHES LONG AND HAD BEEN CONCEALED UNDER THE PAINT. REPLACED THE AILERON WITH A S ERVICEABLE PART. 1 L 7 2 3T 3A20 2001052900342 20010529 00342 NE 2001 5 29 20010529CW004 1 20010501 A 3230 7665001801103 BOTTLE SKRSKY S76 S76A 8143006 NE GEAR BLOWDOWN LEAKING A MV1R K NONE O OTHER IN INSP/MAINT 1 EA 17 38 760087 RECEIVED NEW BOTTLE FROM HSI ON 4/27/2001. INSTALLED AND SERVICED IAW MM TO 3000 PSIG. ON MONDAY 4/30/01 FOUND BOTTLE PSIG AT 200. REMOVED BOTTLE AND SUMERGED UNDER WATER, FOUND LEAKING AT VALVE ACTUATING AREA. 1 G 7 2 3U H1NE 2001052900343 20010529 00343 SW 2001 5 29 20010529CW005 1 20010509 A 5312 206032308003A BULKHEAD BELL 206 206L4 1182110 SW FUSELAGE CRACKED A BLBR K NONE O OTHER IN INSP/MAINT 1 GL 23 193TW 1753 SL026 CRACKED AT 2:00 POSITION IN RADIUS OF BEND. CRACK LENGTH 2 INCHES. 1 G 7 1 3U NC H2SW 2001052900344 20010529 00344 SO 2001 5 29 20010529CW006 1 20010425 A 3710 2H2211 VALVE PIPER PA31 PA31350 7103110 SO VACUUM SYS BROKEN A K NONE O OTHER IN INSP/MAINT 1 SO 13 111VC 317952190 DURING ANNUAL INSPECTION WE FOUND BOTH DEICE/INSTRUMENT AIR VALVES TO BE BROKEN IN THE SAME PLACE ON BOTH SIDES. THE R ELIEF VALVE HOUSING WAS BROKEN AWAY FROM THE REGULATOR AT THE GLUE LINE. 1 L 7 2 3O A20SO 2001053100001 20010531 00001 NM 2001 5 31 SWAA011420 1 20010512 A 5314 6545866 KEELBEAM BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED 1/4 D-CHECK, FOUND KEEL BEAM STRUCTURE CORRODED FROM BS 500D TO BS 523, STR 28R. REPAIRED KEEL BEAM PE R BFG ER. 2 L 7 2 4F RT A16WE 2001053100002 20010531 00002 WP 2001 5 31 AT0100150R1 1 20010421 A 5311 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 811AT 47285 FOUND NOSE WHEEL WELL AT BS 110 HAS CORROSION. REMOVED CORROSION, FABRICATED REPAIR DOUBLERS, DRILLED, AND INSTALLED IA W DC9 SRM 51-10-3, 53-10, 51-10-4, 51-30-0, RES 01-0508. 2 L 7 2 4F A6WE 2001053100003 20010531 00003 WP 2001 5 31 CALA0100468 1 20010517 A 2560 S168MA MEGAPHONE BARFIELD DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14890 49114 THE AFT CABIN MEGAPHONE WAS FOUND INOPERATIVE DURING TEST. THE AFT CABIN MEGAPHONE WAS REMOVED AND REPLACED IAW MM 25-6 0-00. 2 L 7 2 4F A6WE 2001053100004 20010531 00004 NM 2001 5 31 AWXA0001760 1 20010516 A 5347 SEAT TRACK BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 FWD GALLEY SEAT TRACK BS 312 LBL 30 IS CORRODED. REMOVED DAMAGED SEAT TRACK AND REPLACED WITH NEW TRACK IAW SRM 51-40-0 2 AND REF 53-00-52. 2 L 7 2 4F RT A16WE 2001053100005 20010531 00005 NM 2001 5 31 AWXA0001762 1 20010516 A 5311 651630086 FRAME BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 BS 178 BLKHD LT CHORD O/B HAS CRACK INDICATION AT WL 207. NDT INSP IAW BOEING NDTM PT 6 51-00-00 FIG 23; LT SIDE CHORD REPLACED IAW SRM 51-10-1 PG 8 AND SRM 51-10-2 PG 2-3 AND DWG 65-16300; METAL REPROTECTED IAW SRM 51-30-2 PG 7; EDGE SEAL ED IAW SRM 51-24-0; RESTORED FINISH IAW MM 51-21-0. 2 L 7 2 4F RT A16WE 2001053100006 20010531 00006 WP 2001 5 31 AT0100151R1 1 20010423 A 5511 SPAR CAP DOUG DC9 DC932 3022066 WP HORIZ STAB CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 811AT 47285 FOUND RIGHT HORIZONTAL STAB SPAR CAP CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER IAW TIMCO SERVICE ORDER 151108-2 1080. 2 L 7 2 4F A6WE 2001053100007 20010531 00007 NM 2001 5 31 SWAA011425 1 20010512 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B+2, BOTTOM OF STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001053100008 20010531 00008 NM 2001 5 31 SWAA011442 1 20010514 A 5320 6551698 SPLICE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 664.5, STR 8R. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F A16WE 2001053100009 20010531 00009 2001 5 31 MWEA010772 4 20010517 A 3425 5223908001 ADI DOUG DC9 DC915 3022036 WP COCKPIT INOPERATIVE A MWEA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 300ME 45718 CAPTAIN FLIGHT DIRECTOR DOES NOT OPERATE IN HEADING MODE AND WILL NOT TRACK IN NAV MODE. REMOVED AND REPLACED NR 1 STEE RING COMPUTER AND CAPT ADI. 2 L 7 2 4F A6WE 2001053100010 20010531 00010 WP 2001 5 31 ABXA010227 1 20010408 A 5320 ATTACH ANGLE DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 78059 45999 KEEL BEAM TO WEB ATTACHMENT ANGLE IN THE RIGHT MAIN LANDING GEAR WHEEL WELL WAS CORRODED. MAINTENANCE INSPECTED AND REP AIRED THE AREA IAW DC-8 SRM 51-1-8 AND 51-2-0. 2 L 7 4 4F 4A25 2001053100011 20010531 00011 WP 2001 5 31 ABXA010228 1 20010414 A 5320 3706753 STANCHION DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 78059 45999 RIGHT TUNNEL STANCHION CORRODED AT FUSELAGE STATION 360, FORWARD CARGO BAY RIGHT SIDE. MAINTENANCE INSPECTED AND REPAIR ED THE AREA IAW DC-8 SRM 51-1-8, 53-2-0. 2 L 7 4 4F 4A25 2001053100012 20010531 00012 NM 2001 5 31 UPS01235892 1 20010515 A 2133 OUTFLOW VALVE BOEING 727 727173C 1384059 NM CABIN PRESSURE OBSTRUCTED A IPXA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 SO 01 938UP 19506 INSPECTION TYPE:N/A DIVERSION-UNABLE TO PRESSURIZE AIRCRAFT. CLEARED DEBRIS FROM OUTFLOW VALVE. 2 L 7 3 4F A3WE 2001053100013 20010531 00013 NM 2001 5 31 UPS01235907 1 20010508 A 5330 SKIN BOEING 727 72730C 1384009 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:C, FUSELAGE SKIN FOUND TO HAVE WEAR HOLE AT BS 1187 BETWEEN S24 LT & S26 LT SECT 48. REPAIR CARRIED OUT IAW SRM 53-30-3, 51-30-1, 51-20-00, 51-10-2. 2 L 7 3 4F A3WE 2001053100014 20010531 00014 NM 2001 5 31 UPS01235908 1 20010511 A 5530 WEB BOEING 727 72730C 1384009 NM VERTICAL STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:C STRUCTURE ABOVE NR 2 ENGINE, WEB CRACKED AT BS 1388 APPROX RT SIDE. NEW WEB INSTALLED IAW SRM 51-30-0 2 & BOEING DRAWING 65-17555. 2 L 7 3 4F A3WE 2001053100015 20010531 00015 NE 2001 5 31 NACA20010021 2 20010515 A 8530 356993 CYLINDER PWA CB3 DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE NR 3 ENGINE DEFECTIVE A NACA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 99330 1559 1559 P36225 43576 P36225 FEATHERED THE NR 3 ENGINE AT 2311Z DUE TO LOW COMPRESSION INDICATION NR 2 CYLINDER. REPLACED THE NR 2 CYLINDER. 2 L 7 4 4R 4 R 6A3 5E8 2001053100016 20010531 00016 NM 2001 5 31 SWAA011460 1 20010515 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 314SW 23336 DURING SCHEDULED BC4 CHECK, FOUND FUSELAGE SKIN CRACKED AT STR 10R, BS 727B AND BS 510. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001053100017 20010531 00017 NM 2001 5 31 SWAA011465 1 20010516 A 5743 6549488 FITTING BOEING 737 7373H4 1384600 NM LT & RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED D-CHECK, FOUND LT AND RT MLG BEAM AFT OUTBOARD SUPPORT FITTINGS CRACKED. REMOVED AND REPLACED SUPPORT FITTINGS PER SWA RA. 2 L 7 2 4F RT A16WE 2001053100018 20010531 00018 NM 2001 5 31 UPS01235909 1 20010515 A 5754 SKIN BOEING 727 72730C 1384009 NM L/E FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:C, CRACK ON ANTI-ICE SKIN NR 3 L/E FLAP I/B OF ACTUATOR ATTACH POINT. REPAIR CARRIED OUT IAW UPS EO B72 7-5750-3082. 2 L 7 3 4F A3WE 2001053100019 20010531 00019 NM 2001 5 31 UPS01235924 1 20010501 A 5330 SKIN BOEING 727 727247 138408F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 210UP 21697 INSPECTION TYPE:C, FUSE SKIN BS 1010, S-28R HAS BULGE AT RIVET. CORROSION FOUND BEYOND LIMITS. REMOVED CORROSION IAW S RM 53-30-3, CUT OUT AREA AND INSTALLED DOUBLER IAW SRM 53-30-3. 2 L 7 3 4F A3WE 2001053100020 20010531 00020 NM 2001 5 31 UPS01235925 1 20010501 A 5313 STRINGER BOEING 727 727247 138408F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 210UP 21697 INSPECTION TYPE:C, FUSELAGE SKIN AT BS 1010 S29 HAS BULGE AT RIVET HEAD. REMOVED FASTENERS FOR ACCESS INSPECTED AREA. FOUND CORROSION BEYOND LIMITS PER SRM PER 51-30-2. CLEANED AREA AND REPLACED STRINGER AS PER SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 2001053100021 20010531 00021 NM 2001 5 31 UPS01435898 1 20010508 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:C2 EMP - RT UPPER FUSELAGE SKIN FOUND CRACKED AT STA 2654 TO STA 2658 WL 314 STR 9R (AS MARK). EMP - RT UPPER FUSELAGE SKIN REPAIRED AS PER SRM 53-30-03 FIG 1A. 2 L 7 4 4F A20WE 2001053100022 20010531 00022 NM 2001 5 31 UPS01435900 1 20010504 A 5310 65B1117615 DOOR FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:C-2 M/D -L3 DOOR FWD CUTOUT REVEAL FOUND CRACKED AT NR 3 TO 4 STOP FITTING AREA AS MARK. REVEAL PANEL R EPLACED IAW SRM 51-10-01 WITH HX S/TAG FF069197. 2 L 7 4 4F A20WE 2001053100023 20010531 00023 NM 2001 5 31 UPS01435901 1 20010508 A 5310 65B11751601 DOOR FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:C-2 M/D L3 DR FWD CUTOUT LWR CORNER REVEAL FOUND CRACKED. LWR CORNER REVEAL FTG REPLACED IAW SRM 51-10- 01 WITH HX S/TAG FF069254. 2 L 7 4 4F A20WE 2001053100024 20010531 00024 NM 2001 5 31 ERKR200100129 1 20010516 A 5720 65B172235 FITTING BOEING 747 747128 1384894 NM WING CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 ADDITIONAL WING REAR SPAR TO WING CENTER SECTION UPPER SPLICE FITTING REWORK. A DEVIATION TO AND ADDITIONAL REWORK FOR S/B 747-57-2110 TERMINATING ACTION PER FIG 4. THE DEVIATION CONSISTS OF USING A FILLER BETWEEN THE REPLACEMENT (NEW) 65 B17223-5 SPLICE FITTING AND THE UPPER WING SKIN. THE ADDITIONAL REWORK CONSISTS OF MATCHING THE O/B LOWER EDGE OF THE E XISTING EXTERNAL LONGERON SPLICE & USE OF OVERSIZE FASTENERS IN ADJACENT STRUCTURE. THE FILLER IS REQUIRED TO ACCOUNT F OR A CONFIGURATION MISMATCH BETWEEN THE REPLACEMENT (NEW) 65B17223-5 SPLICE FITTING AND THE REPLACED 65B12071-1 SPLICE F ITTING. 2 L 7 4 4F A20WE 2001053100025 20010531 00025 WP 2001 5 31 ABXA010224 1 20010420 A 5320 57519451 DOUBLER DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 LOWER T-CAP DOUBLER STA 980 AFT CARGO PIT WAS CRACKED FROM LONGERON 35L TO 35R. MAINTENANCE INSPECTED AND REPLACED THE T-CAP DOUBLER IAW DC-8 SRM 51-1-24. 2 L 7 4 4F 4A25 2001053100026 20010531 00026 NM 2001 5 31 SWAA011450 1 20010515 A 5330 6545871 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR CUTOUT FUSELAGE SKIN CRACKED AT LWR AFT CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001053100027 20010531 00027 NM 2001 5 31 SWAA011452 1 20010515 A 5523 183A81001 HINGE BOEING 737 7377H4 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 710SW 27844 DURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, LT ELEVATOR TAB INBOARD HINGE FAILED FREE PLAY CHECK. REMOVED AND REPL ACED LT ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2001053100028 20010531 00028 NM 2001 5 31 SWAA011453 1 20010515 A 5523 BACB28AK04 BUSHING BOEING 737 7377H4 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 708SW 27842 DURING SCHEDULED PM CHECK, SWA SI 11038-55, FOUND RT ELEVATOR TAB INBOARD HINGE BUSHING WORN. REMOVED AND REPLACED BUSH ING PER MM. 2 L 7 2 4F RT A16WE 2001053100029 20010531 00029 NM 2001 5 31 SWAA011454 1 20010514 A 3350 6104789 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED A1 CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2001053100030 20010531 00030 NM 2001 5 31 SWAA011455 1 20010514 A 3350 207377 LENS BOEING 737 7372T4 1384492 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 EEPLS LENSES MISSING AT ROW 18 AND ROW 20. REPLACED EEPLS LENSES PER MM. 2 L 7 2 4F A16WE 2001053100031 20010531 00031 NM 2001 5 31 SWAA011456 1 20010511 A 2612 896768 FIRE LOOP BOEING 737 7372H4 138448C NM APU FAULTY A SWAA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 073SW 22673 AIR TURNBACK / DECLARED EMERGENCY. APU FIRE WARNING BELL AND FIRE WARNING LIGHT ILLUMINATED DURING FLIGHT. DISCHARGED APU FIRE BOTTLE, LIGHT DID NOT EXTINGUISH. INSPECTED APU COMPARTMENT, NO EVIDENCE OF FIRE. DEFERRED PER MEL. LATER AT HOU REMOVED AND REPLACED APU FIRE DETECTION LOOP M515 PER MM. 2 L 7 2 4F A16WE 2001053100032 20010531 00032 NM 2001 5 31 UPS01435902 1 20010509 A 5310 65B0831914 STOP FITTING BOEING 747 747123 1384873 NM DOOR FRAME CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:C-2 M/D- R3 DOOR FWD CUTOUT STOP FITTING FOUND CRACKED NR 3. STOP FTG REPLACED AS PER SRM 51-10-01 WITH HX S/TAG FF069228. 2 L 7 4 4F A20WE 2001053100033 20010531 00033 NM 2001 5 31 UPS01435903 1 20010509 A 5310 65B0831916 STOP FITTING BOEING 747 747123 1384873 NM DOOR FRAME CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:C-2 M/D - R3 DOOR FWD CUTOUT STOP FITTING FOUND CRACK AT NR 5. STOP FTG REPLACED AS PER SRM 51-10-01 WI TH HX S/TAG FF 069341. 2 L 7 4 4F A20WE 2001053100034 20010531 00034 NM 2001 5 31 UPS01435904 1 20010509 A 5310 65B0831973 STOP BOEING 747 747123 1384873 NM DOOR FRAME CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:C-2 M/D - L3 DOOR STOP SUPPORT FTG FOUND CRACKED AT BS 1265 S-23L. STOP FTG REPLACED AS PER SRM 51-10-0 1 WITH HX S/TAG FF069231. 2 L 7 4 4F A20WE 2001053100035 20010531 00035 NM 2001 5 31 UPS01435905 1 20010509 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:C-2 CABIN - RT NR 3 MED CUTOUT FWD FRAME BELOW LOWER STILL FOUND 1 FASTENER HOLE CRACK AT FRAME WEB. WEB REPLACED IAW UPS EO B747-5310-12070-F APPENDIX E. 2 L 7 4 4F A20WE 2001053100036 20010531 00036 NM 2001 5 31 UPS01435906 1 20010511 A 5310 DOOR FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 VINSPECTION TYPE:C-2 M/D - LT BS 1265 FRAME NR 2 DOOR STOP FTG AREA FOUND TWO FASTENER HOLES CRACKED. ONE CRACK AT FRAM E INNER CHORD. ANOTHER CRACK AT FRAME WEB. CHORD AND WEB REPLACED IAW UPS EO B747-5310-12070-F APPENDIX E. 2 L 7 4 4F A20WE 2001053100037 20010531 00037 NM 2001 5 31 SWAA011457 1 20010515 A 5320 6516300 WEB BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 180.5, RBL 5.70 AND WL187.5. REPAIRED PER SWA RA. 2 L 7 2 4F RT A16WE 2001053100038 20010531 00038 NM 2001 5 31 SWAA011458 1 20010515 A 5312 6516300 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 090SW 22905 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL CHORD WEBS CRACKED AT BS 178, LT AND RT. REPAIRED PER SWA ACO. 2 L 7 2 4F A16WE 2001053100039 20010531 00039 NE 2001 5 31 RAIA00105009 2 20010515 A 7200 TPE33114GR ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE LEFT OVERTEMP A RAIA D RETURN TO BLOCK M OVER TEMP TX TAXI/GRND HDL 1 CE 03 566HK 11164 2791 41084 76086 7607-STL-LEFT ENGINE EGT EXCEEDED RED LINE LIMITATION (OVER TEMP). MAINTENANCE INSPECTED AND REPLACED LEFT ENGINE. 2 L 7 2 4T 4 T RT A41NM E18NE 2001053100040 20010531 00040 EU 2001 5 31 RAIA00105010 1 20010515 A 2912 QA03043 FILTER JETAIR JETSTM JETSTM4101 1500501 EU HYDRAULIC BAY DIRTY A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 562HK 41078 5392-EWR-AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT, AIRCRAFT RETURNED FROM FLIGHT AND LANDED WITHOUT INCIDENT. MAINT ENANCE INSPECTED AND FOUND HYDRAULIC BY PASS PIN POPPED, MAINTENANCE REPLACED HYDRAULIC RETURN FILTER, RESET BY PASS PIN AND PERFORMED GEAR SWING, SYSTEM OPERATIONALLY CHECKED GOOD. 2 L 7 2 4T RT A41NM 2001053100041 20010531 00041 NM 2001 5 31 F3LA200100066 1 20010510 A 5311 FRAME BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3498 23177 DURING C-6 CHECK, INSPECTION REPORTED CORROSION ON VERTICAL FLANGE OF BS 794.3 FRAME, BETWEEN STR 24-R AND 26-R. INSTAL LED REPLACEMENT FRAME PER SRM 51-40-2. 2 L 7 2 4F RT A16WE 2001053100042 20010531 00042 2001 5 31 ANCF200100009 4 20010516 A 2300 AUDIO PANEL DOUG DC9 DC983 3022083 WP COMM SYSTEM INOPERATIVE W ANCF A UNSCHED LANDING O OTHER CR CRUISE 1 SO 23 190AN 12443 1600 53190 LT COMMUNICATIONS WAS COMPLETELY INOPERATIVE. AIR TURNBACK PROCEDURE WAS ACCOMPLISHED. LT AUDIO BOX WAS CHANGED IAW AM M 23-50-02 P 201 AND FLIGHT INTERPHONE CB A-10 WAS RESEATED. SYSTEM OPERATION WAS CHECKED IAW AMM 23-00-00 PG 1. CHECK ED OK. 2 L 7 2 4F RT A6WE 2001053100043 20010531 00043 NM 2001 5 31 F3LA200100065 1 20010516 A 2910 MS219214J B-NUT AIRBUS A319 A319111 NM HYD SYSTEM LOOSE A F3LA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 NM 03 901FR 20 20 MSN1488 DURING TRAINING FLIGHT, FLIGHT CREW REPORTED LOSS OF GREEN HYDRAULIC SYSTEM. AN EMERGENCY WAS DECLARED AND AIRCRAFT LAN DED IN PHX WITHOUT INCIDENT. AIRCRAFT WAS TOWED OFF THE RUNWAY DUE TO THE LOSS OF THE NOSE WHEEL STEERING. THE B-NUT O N THE HYDRAULIC PRESSURE LINE FOR THE RT MLG DOOR UPLOCK WAS FOUND TO BE LOOSE. THE HYDRAULIC LINE WAS RETORQUED AND TH E SYSTEM WAS SERVICED. 2 L 7 2 4F RT A28NM 2001053100044 20010531 00044 WP 2001 5 31 NACA20010022 1 20010515 A 5330 PLUG DOUG DC6 DC6A 3021706 WP FUSELAGE CRACKED A NACA K NONE O OTHER IN INSP/MAINT 1 AL 03 1377K 44596 RT FUSELAGE STA 300 WINDOW PLUGS WORKING. FOUND FORWARD CORNER CRACKED. REMOVED DAMAGED MATERIAL, DIMPLED HOLES, FABBE D FILLER AND DOUBLER. PRIMED, TREATED, AND INSTALLED REPAIR PARTS, USING 507-8 STAINLESS STEEL SCREWS PER ROD SKETCH 90 -05-05-010. 2 L 7 4 4R 6A3 2001053100045 20010531 00045 NM 2001 5 31 UPS01435911 1 20010506 A 5320 SUPPORT BOEING 747 747123 1384873 NM FAIRING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:C-2 BODY FAIRING SUPPORT STA 920 RBL 60 - LBL 60 FOUND CORRODED. BODY FAIRING SUPPORT REPAIR AT BS 920 LBL 60 TO RBL 60 PER SRM 53-50-04 FIG 2. 2 L 7 4 4F A20WE 2001053100046 20010531 00046 NM 2001 5 31 UPS01435913 1 20010509 A 5320 SPLICE PLATE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:C-2 NLG W/W STA 400 S-44R SPLICE PLATE FOUND CRACK AT CORNER RADIUS. HFEC INSP C/OUT AS PER NTM PT6 51- 00-00 FIG 1. CRACK FOUND AT AFT HOLE AT SPLICE FITTING, BUT NIL CRACK AFTER AFT HOLE REF SCATCH ON CWS 330869. EXISTIN G REPAIR DOUBLER REINSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2001053100047 20010531 00047 NM 2001 5 31 UPS01435914 1 20010509 A 5320 SPLICE PLATE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:C-2 NLG W/W STA 400 S-44L SPLICE PLATE FOUND CRACK AT CORNER RADIUS. HFEC INSP C/OUT AS PER NTM PT6, 51 -00-00 FIG 1. NIL CRACK FOUND AT AFT HOLES OF PREVIOUS CRACKED HOLE. EXISTING REPAIR DOUBLER REINSTALLED AS PER SRM 51 -30-02. 2 L 7 4 4F A20WE 2001053100048 20010531 00048 NM 2001 5 31 UPS01435916 1 20010507 A 2520 65B1117613 PANEL BOEING 747 747123 1384873 NM CAIBN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:C-2 M/D - L3 DR FWD CUTOUT UPPER REVEAL CRACKED AT LWR EDGE AREA. REVEAL PANEL REPLACED AS PER SRM 51-1 0-01. 2 L 7 4 4F A20WE 2001053100049 20010531 00049 NM 2001 5 31 UPS01435918 1 20010509 A 5310 PRESSURE PANEL BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:C-2 M/D - BS 1241 RBL 17-25 BELOW FLOOR CANTED PRESS DECK FOUND CORR. BS 1241 RBL 16 TO 28 CANTED PRESS DECK REPAIRED AS PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 2001053100050 20010531 00050 WP 2001 5 31 ABXA010229 1 20010516 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 952AX 47615 THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE DURING THE PREFLIGHT INSPECTION. MAINTENANCE INSPECTED AND REPLACED T HE EMERGENCY LIGHT BATTERIES IAW DC-9 MM. 2 L 7 2 4F A6WE 2001053100051 20010531 00051 WP 2001 5 31 MWEA010775 1 20010521 A 5330 5911406 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 PAX DOOR JAMB SKIN INNER DOUBLER CRACKED AT TOP FORWARD CORNER. REMOVED DAMAGED, FABRICATED, LOCATED AND DRILLED DOUBLE RS AND FILLER, INSTALLED FILLER, DOUBLER AND TRIPLER. 2 L 7 2 4F A6WE 2001053100052 20010531 00052 CE 2001 5 31 GLBA2001101 1 20010515 A 2150 A/C PACK BEECH 1900 1900D 1154162 CE AC BAY FAILED A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 01 184UX UE184 RIGHT ENVIROMENTAL FAIL ON T/O ROLL. INSPECTED, COULD NOT DUPLICATE. 2 L 7 2 4T RT A24CE 2001053100053 20010531 00053 EU 2001 5 31 C2XA01CL109 1 20010516 A 3230 C24589000 UPLOCK AEROSP ATR42 ATR42320 8680930 EU LT MLG FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14828 42131 42131 179 CLE FLIGHT 3750 THE CREW REPORTED THE LEFT MAIN GEAR WOULD NOT RETRACT. THE INDICATION WAS UNLOCK LIGHT ON THE LEFT GEA R. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT GEAR UPLOCK B OX ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A53EU 2001053100054 20010531 00054 SO 2001 5 31 SWIA972574 1 20010515 A 3231 LATCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT MLG DOOR FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 576SW 120345 RIGHT SIDE FORWARD, OUTBOARD, GEAR DOOR WON''T RETRACT. RETURNED TO PDX. REPLACED LATCH ASSEMBLY ON RIGHT FORWARD OUTB OARD GEAR DOOR PER MM 32-32-00 AND MM 52-81-01. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001053100055 20010531 00055 SO 2001 5 31 SWIA972575 1 20010514 A 2932 PRESSURE SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE HYD SYSTEM FAULTY A SWIA O OTHER J WARNING INDICATION DE DESCENT 1 NM 07 568SW 120343 RUDDER OVERBOOST LIGHT ILLUMINATED ON DESCENT. FOLLOWED QRH. REPLACED RELAYS K0331, K0319, K0323, K0317, DID NOT SOLVE PROBLEM. REPLACED NR 1 AND 2 AIRSPEED INDICATORS WITH SERVICEABLE UNIT. DID NOT FIX PROBLEM. REINSTALLED NR 1 AND 2 AIRSPEED INDICATORS TO ORIGINAL POSITIONS. BOTH AIRSPEED INDICATORS OPS CHECK GOOD MM 34-12-00. PERFORMED OVERBOOST FA ULT ISOLATION MM CHECKS, STEPS 1 THRU 2, 3, AND 4. REMOVED AND REPLACED GREEN SYSTEM PRESSURE SWITCH. PROBLEM STILL EX ISTS. REMOVED AND REPLACED RUDDER CONTROL SWITCH S0449 (GREEN SYSTEM SWITCH). OPS CHECKED SYSTEM AND FOUND NORMAL. OV ERBOOST LIGHT DID NOT ILLUMINATE. NO LEAKS NOTED AT THIS TIME.GREEN PRESSURE SWITCH P/N 1206P0114-01. 2 L 7 2 4T 4 T RT A31SO E20NE 2001053100056 20010531 00056 SO 2001 5 31 SWIA972576 1 20010509 A 5246 FASTENER EMB 120 EMB120RT SO PWA 118 PW118 NE FUEL SERVICE DR LOOSE A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 137H 120137 ABORTED TAKEOFF FOR RED DOOR LIGHT ON MAP AND SERVICE DOOR ON AT 80 KIAS. INBOARD FUEL SERVICE DOOR AFT FASTENER CAME L OOSE. SECURED FASTENER. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001053100057 20010531 00057 NM 2001 5 31 PCAA0105041 1 20010514 A 5310 PRESSURE PANEL DHAV DHC8 DHC8102 2809003 NM NLG WW CRACKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 851EX 343 BGM- DURING ROUTINE MAINTENANCE VISIT, 4 CRACKS WERE FOUND IN LEFT AND RIGHT NOSE LANDING GEAR WELL AREA AT STATIONS X96 .19 AND X97.0. MAINTENANCE REPAIRED CRACKS IN ACCORDANCE WITH DEHAVILLAND REPAIR DRAWINGS RD 8-53-675, RD 8-53-5873, AN D RD 8-53-5869. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001053100058 20010531 00058 CE 2001 5 31 C2XA01CL110 1 20010517 A 3297 602EN16 WIRE BEECH 1900 1900D 1154162 CE DOWNLOCK SWITCH BROKEN A C2XA O OTHER N FALSE WARNING AP APPROACH 1 SW 27 81538 UE199 CLE FLIGHT 3135, THE CREW REPORTED ON APPROACH TO CLEVELAND AFTER GEAR EXTENSION, HAD NO GREEN DOWN AND LOCKED LIGHT FOR THE NOSE GEAR. A EMERGENCY WAS DECLEARED AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND A BROKEN WIRE FOR THE NOSE GEAR ACTUATOR DOWN POSITION SWITCH. THE SWITCH WAS REPLACED AND OPERATIONAL CHECKS WER E GOOD. 2 L 7 2 4T RT A24CE 2001053100059 20010531 00059 NM 2001 5 31 UPS01435919 1 20010509 A 5310 PRESSURE PANEL BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:C-2 M/D - BS 1241 RBL 17-25 BELOW FLOOR CANTED PRESS DECK FOUND CORR. BS 1241 RBL 16-28 CANTED PRESS DE CK REPAIRED AS PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 2001053100060 20010531 00060 WP 2001 5 31 UPS01835896 1 20010429 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C1 FWD PIT - STN 90 - S33R - INTERCOSTAL UNDER CARGO TRACK IS BENT AND CRACKED. REMOVED AND FABBED NEW INTERCOSTAL P/N 5750726-70. ALODINED, PRIMED AND INSTALLED INTERCOSTAL CARGO TRACK IAW DC8 SRM 51-3-0 AND 51-1-21. 2 L 7 4 4F RT 4A25 2001053100061 20010531 00061 WP 2001 5 31 UPS01835897 1 20010501 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C1 AFT PIT STA 1060 L36 FRAME HAS CORROSION ON UNDERSIDE OF J-CHANNEL A T-NUT PLATE. REMOVED CORROSION OF FRAME OUT OF LIMITS. LOCATED AND DRILLED NEW FRAME CAP, FABBED REPAIR ANGLES, ALODINED PRIMED INSTALLED FRAME CAP RE PAIR ANGLES GUSSETTE IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001053100062 20010531 00062 WP 2001 5 31 UPS01835921 1 20010502 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 316.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001053100063 20010531 00063 NM 2001 5 31 0101546310 1 20010513 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 670US 24225 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE BETWEEN PASSENGER DOOR 1L AND 2L. RECONNECTED WIRIN G. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001053100064 20010531 00064 NM 2001 5 31 0101586635 1 20010509 A 3350 BATTERY BOEING 747 747227B 1384888 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 635US 21682 DURING LINE CHECK, FOUND ZONE-E EMERGENCY FLOOR ESCAPE PATH LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY. OPER ATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2001053100065 20010531 00065 WP 2001 5 31 0101759981 1 20010512 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP ACCESSORY BAY INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 994Z 47097 DURING LINE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE AT CATWALK AND TAIL CONE RELEASE HANDLE. REPLACED SEALED POWER SU PPLY IAW DC-9 WM 33-51-04. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001053100066 20010531 00066 SO 2001 5 31 C2XA01IA246 1 20010514 A 3350 M8372375R1624N CONNECTOR EMB 145 EMB145ER SO CABIN LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15941 145035 CLE - FLIGHT 4058, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE AISLE PATH LIGHTS IN THE CENTER CABIN WERE IN OPERATIVE. MAINTENANCE RESECURED THE CANNON PLUG ON THE AFFECTED POWER SUPPLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001053100067 20010531 00067 NM 2001 5 31 VNAA0105007 1 20010511 A 3244 26107012 TIRE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT MLG FLAT A VNAA O OTHER E VIBRATION/BUFFET TX TAXI/GRND HDL 1 GL 07 424JS 3033 WHILE TAXIING FROM THE RUNWAY AFTER LANDING, THE CREW NOTICED A VIBRATION WHICH WAS GETTING STRONGER. THE CREW STOPPED THE AIRCRAFT AND THE CAPTAIN GOT OUT AND INSPECTED THE AIRCRAFT AND FOUND THAT BOTH THE LEFT SIDE MAIN LANDING GEAR TIRE S WERE FLAT. THE PASSENGERS WERE BUSSED TO THE TERMINAL AND MAINTENANCE REPLACED THE LEFT HAND MAIN LANDING GEAR WHEEL ASSEMBLIES IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT W AS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001053100068 20010531 00068 2001 5 31 VNAA0105005 4 20010508 A 3460 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT ACTIVATED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 442JS 3060 DURING THE TAKEOFF ROLL, THE CREW RECEIVED A FGC LATERAL MODE FAIL CAS MESSAGE. THE CREW REFERENCED THE QUICK REFERENCE HANDBOOK AND ABORTED TAKEOFF. THE MESSAGE CLEARED AND FLIGHT 4124 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 412 4 DEPARTED ELM WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001053100069 20010531 00069 NM 2001 5 31 DHL2001705530 1 20010419 A 5343 SUPPORT FITTING BOEING 727 72722C 138400F NM LT MLG CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C-CHECK - LEFT MAIN BEAM WHEEL WELL SUPPORT FITTING BS 930 SHOW'S CRACK AT L-18L, AS MKD LOWER FWD SIDE. CRACK VERIF Y BY NDT AS PER 51-000 FIG 1 RUNNING BETWEEN FASTENERS 1 & 2 FROM BOTTOM. LEFT MAIN GEAR WHEEL WELL SUPPORT FITTING BS 930 CRACK HAS BEEN PREVIOUSLY REPAIR IAW BOEING SERVICE BULLETIN 727-53-130. REMOVED CABLES AND QUADRANT MECHANISM OF L T MANUAL DOOR OPEN SYSTEM IAW B727 MM 32-34-01. FOUND CRACK ON FWD VERT O/B FLANGE RUNNING FROM W/W INTO CABIN. REMOVE D WEB SECTIONS AT FLOOR LEVEL BETWEEN STA 920 AND 940 LT SIDE FOR ACCESS PER B727 SRM 51-30-2. FOUND AFT HORIZ FLANGE O F 930 FITTING CRACKED AT PRESS WEB AREA. REMOVED FASTENER IN FWD VERT O/B FLANGE FOR ACCESS. 2 L 7 3 4F A3WE 2001053100070 20010531 00070 NM 2001 5 31 AWXA0001735 1 20010514 A 5315 65468101 FLOORBEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 FLOORBEAM STA 967 HAS SURFACE CORROSION LBL 30-31. REMOVED CORROSION; FABBED AND INSTALLED REPAIR STRAP AND TAPERED FIL TER IAW SRM 53-00-51. 2 L 7 2 4F RT A16WE 2001053100071 20010531 00071 SO 2001 5 31 SWIA972570 1 20010513 A 7334 PRESSURE SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT FUEL PUMP FAULTY A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 308SW 120326 DURING EN ROUTE CLIMB THE RIGHT REAR ELECTRIC FUEL PUMP COULD NOT SUPPLY ENOUGH PRESSURE. THE RIGHT FORWARD PUMP WOULD CYCLE ON AND OFF. WITH THE FORWARD PUMP IN THE ON POSITION THE LOW PRESSURE LIGHT WENT OUT. REMOVED AND REPLACED RIGHT ENGINE LOW PRESSURE SWITCH IAW EMB MM 73-32-01. RAN ENGINE. OPS CHECK OK. 2 L 7 2 4T 4 T RT A31SO E20NE 2001053100072 20010531 00072 WP 2001 5 31 RRXA010045 1 20010502 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 COMPLY WITH FCD A53-4R1 INSPECTION FOR LOWER FUSELAGE CORROSION. INSPECTED LOWER FUSELAGE FOR CORROSION. FOUND CORROSI ON AT STA 100 L36 LEVEL 2 CORROSION. BLENDED CORROSION, BEYOND LIMITS. AIRCRAFT FERRIED TO TENNESSEE TECHNICAL SERVICE S, LLC. INSPECTED THIS AIRCRAFT AND FOUND IT SAFE FOR THE FLIGHT INTENDED. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FAB RICATED DOUBLER, TREATED, PRIMED AND INSTALLED REPAIR PER EO 01-131 WITH APPROVED 8110-3 DATED 05/03/01. 2 L 7 4 4F RT 4A25 2001053100073 20010531 00073 WP 2001 5 31 MWEA010773 1 20010517 A 2121 7005888 FAN DOUG DC9 DC932 3022066 WP E/E BAY FAILED A MWEA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 31 206ME 47791 IN ROUTE TO DSM WEATHER RADAR FAILED. AIRCRAFT DIVERTED TO OMA. REMOVED AND REPLACED WEATHER RADAR RT AND RT FAN. 2 L 7 2 4F A6WE 2001053100074 20010531 00074 NM 2001 5 31 SCNA01319 1 20010428 A 5315 FLOORBEAM BOEING 727 7272J4 1384006 NM FUSELAGE CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 211DB 20766 DURING C-CHECK, CORROSION WAS DISCOVERED OUT OF LIMITS ON THE FORWARD LOWER FLANGE OF THE FLOORBEAM AT BS 1130, LBL 40 T O RBL 44. ACCOMPLISHED GENERAL REPAIR IAW B727 SRM CHAPTERS 51 AND 531008 FIG 8. TRIMMED LOWER CHORD FLANGE. 2 L 7 3 4F RT A3WE 2001053100075 20010531 00075 NM 2001 5 31 AWXA0001737 1 20010514 A 5347 6940352 SEAT TRACK BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 FWD GALLEY SEAT TRACK BS 312 RBL 30 IS CORRODED. REMOVED DAMAGED SEAT TRACK SECTION AND REPLACED WITH NEW TRACK SECTION IAW SRM 51-40-02 AND 53-00-52. 2 L 7 2 4F RT A16WE 2001053100076 20010531 00076 NM 2001 5 31 F3LA200100067 1 20010510 A 5320 STRAP BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3498 23177 DURING C-6 CHECK, INSPECTION REPORTED AFT CARGO BAY FLOOR STRAP CORRODED AT BS 800-840, ABOVE STR. 25-R, INBD OF THRESHO LD WEB. REPLACED FLOOR STRAP PER SRM 53-60-15 AND 51-10-02. 2 L 7 2 4F RT A16WE 2001090400123 20010904 00123 NM 2001 9 4 QXEA0100706 1 20010515 A 2610 6504 MODULE DHAV DHC8 DHC8202 2809007 NM FIRE WARNING FAILED A QXEA K NONE J WARNING INDICATION DE DESCENT 1 NM 09 374PH 4796 528 PDX- ON SHORT FINAL, NR 2 ENGINE "FAULT B" LIGHT ILLUMINATED. PLACED ON RSI 322870. (REPLACED #2 ENGINE FIRE DETECTION C ONTROL UNIT. NO HELP.) ON 5/16/01 REPLACED NR 2 SWITCHING VALVE CASE SEALING TUBE. OPERATIONAL CHECK GOOD. AIRCRAFT RETU RNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001053100077 20010531 00077 NM 2001 5 31 QXEA0100707 1 20010517 A 3350 82520977001 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 353PH 496 SEA- SEVERAL EMERGENCY LIGHTS ALONG CABIN AISLEWAY OUT AT ROW 1. REPLACED EMERGENCY LIGHT STRIP AT ROW 1. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001053100078 20010531 00078 NM 2001 5 31 QXEA0100708 1 20010513 A 5210 LATCH DHAV DHC8 DHC8* NM PAX DOOR LACK OF LUBE A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 400QX 4030 PDX- FORWARD CABIN DOOR HARD TO OPEN FROM INSIDE CABIN. CLEANED AND LUBED UPPER MAIN CABIN DOOR LATCHES. NO PARTS REPL ACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURN TO SERVICE. 2 H 7 2 4T RT A13NM 2001053100079 20010531 00079 NM 2001 5 31 QXEA0100709 1 20010515 A 5210 STOP DHAV DHC8 DHC8* NM PAX DOOR LACK OF LUBE A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 400QX 4030 PDX- MAIN CABIN AIRSTAIR DOOR HARD TO OPEN AND CLOSE FROM INSIDE. LUBRICATED MAIN CABIN DOOR STOPS, OPENED AND CLOSED D OOR SEVERAL TIMES USING INSIDE HANDLE. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001053100080 20010531 00080 EU 2001 5 31 QXEA0100710 1 20010517 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 476US 11224 SEA- FORWARD EXIT SIGN HAS LAMPS INOP. REMOVED AND REPLACED LAMP CARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001053100081 20010531 00081 NM 2001 5 31 DHL2001705500 1 20010420 A 5320 BAC1510335 CHANNEL BOEING 727 72722C 138400F NM FUSLEAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C-CHECK, FUSELAGE CORROSION AT HAT CHANNEL ATTACHED TO FLOORBEAM, STA 344 RBL 39. REMOVED HAT CHANNEL FOR REPLACEMEN T AS PER SRM 51-30-22. FABRICATED AND INSTALLED NEW HAT CHANNEL AT FWD LAV STA 344 FROM RBL 15 TO RBL 60 AS PER SRM 53- 10-2 FIG 3 AND 51-30-2. ALODINED AND PRIMED AS PER B727 SRM 51-10-2. HAT CHANNEL INFO 5 FT P/N BAC 1510-335 PO 2113519 1 LOT DD0T9GMI AS PER SRM 53-30-2. 2 L 7 3 4F A3WE 2001053100082 20010531 00082 NM 2001 5 31 DHL2001705501 1 20010417 A 5320 ATTACH ANGLE BOEING 727 72722C 138400F NM CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C-CHECK, MAIN CARGO DOOR CUTOUT, UPPER AFT CORNER AREA, GILL LINER ATTACH ANGLE SHOWS CRACK DAMAGE. REMOVED CRACKED GIL LINER ATTACH ANGLE AT MAIN CARGO DOOR CUTOUT AFT CORNER AREA AS PER B727 SRM 51-30-2. REMOVED AND REPLACED GILL LIN ER ATTACH ANGLE ON CARGO DOOR CUTOUT, UPPER AFT CORNER AREA AS PER B727 SRM 51-30-2 MAT USED ALUMINUM 2024-0 .040 LOT 47 4051 PO 83110595 SIZE = 2'' X 6. TREATED AND PRIMED AREA AS PER B727 SRM 51-10-2. HEAT TREATED MATERIAL TO 2924 T3 AS PER B727 SRM 51-10-3. 2 L 7 3 4F A3WE 2001053100083 20010531 00083 NM 2001 5 31 DHL2001705509 1 20010421 A 5311 652662170 FRAME BOEING 727 72722C 138400F NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C-CHECK-NOSE W/W RT SIDE WALL, SIDE FRAME CORRODED AT INNER AREA OF FUSE TUNNEL STA 257 WL 180 AND IN BETWEEN ACCESS PANEL 3123. REMOVED FASTENER AND CUTOUT DAMAGE SECTION WITH CORROSION BEYOND LIMITS AT T-ANGLE WEB SUPPORT AT NOSE W/W RT SIDE WALL BETWEEN STA 245 TO BS 265 WL 180 18 .5 INCH LONG AS PER B727 SRM 51-40-4 FIG 1, NO MORE CORROSION NOTED. N DT CUT OUT DAMAGE, NO CRACK INDICATION PER B727 NDT MANUAL PART 6 51-00-00 FIG 4. REMOVED NLD FWD RT DOOR IAW B727 MM 3 2-22-1. FOUND RT HAND WEB CRACK AT 3 LOCATION WHEN OPENING WEB FOR ACCESS TO REPAIR INNER FRAME AT STA 257 WL 180 IN BE TWEEN ACCESS PANEL 3123 AND 3125. WEB REPAIR ON N/R 3397 AS PER B727 SRM 51-40-2. INSTALLED NLG FWD RT. 2 L 7 3 4F A3WE 2001053100084 20010531 00084 NM 2001 5 31 DHL2001705503 1 20010417 A 7110 ANGLE BOEING 727 72722C 138400F NM COWLING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C-CHECK, NR 2 ENG LT AFT COWL HAS LOWER FWD COENER WITH CRACK ANGLE. REMOVED AND REPLACED NR 2 LT AFT CORNER ANGLE. MATERIAL USED 2024T3 .050 MATERIAL SIZE 12 X 2.5 PO 83112359 LOT 35803 AS PER B727 SRM 51-30-202. TREATED AND PRIMED AREA AS PER B727 SRM 51-10-2. 2 L 7 3 4F A3WE 2001053100085 20010531 00085 NM 2001 5 31 DHL2001705505 1 20010416 A 7110 ANGLE BOEING 727 72722C 138400F NM COWLING BENT A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C-CHECK, NR 1 ENG, LWR COWL O/B FWD AREA , INT ANGLE WORN AND BENT. REFERENCE: FWD OF 2ND U-BOLT, UPPER OF OIL SERVI CE DOOR. REMOVED AND REPLACED INTERNAL ANGLE ON 1 ENG, LWR COWL O/B FWD OF 2ND U-BOLT ABOVE OIL SERVICE DOOR PER B727 S RM 51-30-2. MAT USED 2024-0-.050 28 X 31 PIECE PO 83110438LOT 7Y153Y05 HEAT TREATED TO 2024T3 PER GENERAL PROCESS SPECI FICATION 98PMSI247PS-01. 2 L 7 3 4F A3WE 2001053100086 20010531 00086 NM 2001 5 31 DHL2001705506 1 20010418 A 7110 DOUBLER BOEING 727 72722C 138400F NM COWLING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C-CHECK, NR 3 ENG, LWR COWL INTERNAL SURFACE, RIGHT AFTER 2ND U-BOLT, STRINGER PREVIOUS DOUBLER REPAIR SHOWS BIG HOLE (8 O''CLOCK POS APPROX). REMOVED DAMAGED EXISTING DOUBLER IAW B727 SRM 51-30-2. FABRICATED DOUBLER 8 X 12 2024-0 .050 LOT 471153 PO 8319629. HEAT TREATED IAW SRM-1003 FIG NR 6. CLEANED, TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALL ED NEW DOUBLER IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2001053100087 20010531 00087 NM 2001 5 31 DHL2001705507 1 20010417 A 5755 651734862 SPOILER BOEING 727 72722C 138400F NM WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 C-CHECK, NR 9 SPOILER IS DELAMINATED AT FWD UPPER RT CORNER. REMOVED AND REPLACED NR 9 SPOILER PANEL PER B727 MM 27-62- 1 P 401. ADJUST AND TEST. ACCOMPLISH OPERATIONAL CHECK OF NR 9 SPOILER IAW B727 CH 27-62-0 MM, OPS CHECK OK. 2 L 7 3 4F A3WE 2001053100088 20010531 00088 NM 2001 5 31 DHL2001705508 1 20010418 A 2810 65296052 RETAINER BOEING 727 72722C 138400F NM CENTER TANK CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C-CHECK, FUSELAGE BS 870 REAR UPPER CHORD CENTER TANK RBL 46 TO OUT. HEAVY CORROSION AND PRESSURE SEAL RETAINER IS A LSO CRACKED. FOUND SEAL RETAINER ATTACH ANGLE TO BE CORRODED BS 870 RBL46 AND CRACKED. REMOVED ATTACH ANGLE FROM RBL 4 0 TO RBL 63 APPROX, PER B727 SRM 51-10-2 NO CORRSION FOUND ON UPPER CHORD. INSTALLED NEW 2 PRESSURE SEAL RETAINER PER S RM 51-10-1. ALODINED AND PRIMED PER SRM 51-10-2. 2 L 7 3 4F A3WE 2001053100089 20010531 00089 NM 2001 5 31 01FDEA00343 1 20010514 A 5714 ANGLE BOEING 727 72722 1384002 NM CNTR WING BOX CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 DURING ROUTINE INSP CTR WING BOX AFT SPAR LWR CHORD ANGLE FOUND CORRODED. R&R PER 727 SRM 57-10-1 FIG 3, 51-10-2. 2 L 7 3 4F A3WE 2001053100090 20010531 00090 WP 2001 5 31 ABXA010225 1 20010513 A 5230 3485173503 SEAL DOUG DC8 DC861 3021952 WP MIAN CARGO DOOR DAMAGED A ABXA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 23 849AX 45891 AN EXTREMELY LOUD NOISE WAS NOTED IN THE MAIN CARGO COMPARTMENT AROUND THE MAIN CARGO DOOR. THE CREW REPORTED HEARING A THUMP AND PRESSURIZATION INCREASED TO 1000 FPM RATE OF CLIMB. PRESSURIZATION COULD NOT BE CONTROLLED MANUALY AT FL21. THE CREW DONNED O2 MASKS AND DIVERTED TO ILN FOR REPAIRS. MAINTENANCE INSPECTED AND DEFERRED THE MAIN CARGO DOOR SEAL AND MANUAL PRESSURIZATION PER ABX REA 852-41121 AND DC-8 MEL. MAINTENANCE COMPLETED DOOR SEAL REPAIR IAW ABX REA D852-4 1134 AND REMOVED THE DEFERRALS FROM THE AIRCRAFT. 2 L 7 4 4F 4A25 2001053100091 20010531 00091 NM 2001 5 31 DL73E010723 1 20010504 A 5330 6552988 SKIN BOEING 737 7372J8 1384489 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 235WA 22859 A TYPICAL CRACK WAS FOUND IN THE LOWER FORWARD CORNER OF THE AFT ENTRY DOOR CUTOUT. THE CRACK WAS IN THE BONDED SKIN AS SY AND THE UNDERLYING BEAR STRAP. THE CRACK WAS REMOVED WITH A 2.5 X 1 INCH CUTOUT. THE AREA WAS REPAIRED WITH THREE EXTERNAL ALUMINUM DOUBLERS INSTALLED PER ER/A 380730-14, REV A. 2 L 7 2 4F RT A16WE 2001053100092 20010531 00092 NM 2001 5 31 DL757010724 1 20010507 A 2400 TERMINAL BLOCK BOEING 757 757232 1384965 NM GEN PANEL BURNED A DALA D RETURN TO BLOCK M S OVER TEMP AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 27 6713Y 30777 TERMINAL BLOCK TB5046 FOUND TO HAVE BURNED WIRES WHICH CAUSED FAILURES IN LT FWD BOOST PUMP, RT FWD BOOST PUMP, MID LAV FLUSH MOTOR, FWD LAV FLUSH MOTOR, CAPTS SEAT MOTOR. INSTALLED NEW TERMINAL STRIP. 2 L 7 2 4F RT A2NM 2001053100093 20010531 00093 NM 2001 5 31 DL73K010725 1 20010504 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 332DL 23104 A TYPICAL CRACK WAS FOUND IN THE BONDED SKIN AND UNDERLYING BEAR STRAP IN THE LOWER FWD CORNER OF THE AFT GALLEY DOOR CUTOUT. THE CRACK WAS REMOVED WITH A 1.2 X 1.3 INCH CUTOUT IN ALL LAYERS. THE AREA WAS REPAIRED WITH THREE EXTERNAL A LUMINUM DOUBLERS PER ER/A 380739-14, REV A. 2 L 7 2 4F RT A16WE 2001053100094 20010531 00094 NM 2001 5 31 DL73K010726 1 20010504 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 332DL 23104 A .5 INCH CRACK WAS FOUND IN THE BONDED SKIN OF THE UPPER HINGE CUTOUT OF THE AFT ENTRY DOOR CUTOUT. THE CRACK WAS REMO VED WITH A SMALL CUTOUT. THE AREA WAS REPAIRED WITH AN EXTERNAL CRES STEEL DOUBLER PER ER/A 380735-14, REV A. 2 L 7 2 4F RT A16WE 2001053100095 20010531 00095 NM 2001 5 31 DL757010727 1 20010507 A 3350 BR9279108 SIGN BOEING 757 757232 1384965 NM CABIN BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 643DL 23997 JUMPSEAT LFT AFT ENTRY DOOR 4L FOR MAINT ON EMERGENCY EXIT SIGN (SOCKET BROKEN). REPLACED EMERGENCY EXIT LIGHT ASSY, OP S CK GOOD. 2 L 7 2 4F RT A2NM 2001053100096 20010531 00096 NM 2001 5 31 DL72L010730 1 20010507 A 3233 ACTUATOR BOEING 727 727232 1384082 NM RT MLG WW FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 501DA 21303 AFTER T/O AND GEAR HANDLE WAS SELECTED TO OFF AFTER 30 SEC. CREW GOT DOOR LIGHT ON FWD PANEL AND RED RT GEAR LT ON FOLL OWED BY TAIL SKID LIGHT AND RED NOSE GEAR LT. CREW CHECK OF GEAR VISUALLY LT MAIN AND NOSE UP AND LOCKED BUT RT MAIN WA S DOWN AND LOCKED. REMOVED AND REPLACED RIGHT MAIN GEAR ACTUATOR PER M/M. 2 L 7 3 4F A3WE 2001053100097 20010531 00097 NM 2001 5 31 DL72L010731 1 20010506 A 3350 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 512DA 21314 EMERGENCY EXIT LIGHT SEAT 22D INOP. REPLACED LIGHT ASSY AT SEAT 22D. MCO AND PLAC REMOVED. 2 L 7 3 4F A3WE 2001053100098 20010531 00098 NM 2001 5 31 DL73E010732 1 20010509 A 3350 LIGHT BOEING 737 737247 138448D NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 379DL 23606 1L EXTERIOR EMERGENCY LIGHT INOP. RELAMPED SAME. 2 L 7 2 4F A16WE 2001053100099 20010531 00099 NM 2001 5 31 DL73K010733 1 20010507 A 5315 6545410138 FLOORBEAM BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 321DL 23093 THE LONGITUDINAL FLOORBEAM OVER THE CENTER WING AT RBL 24 WAS FOUND WITH A CRACK IN THE BEAM WEB DOUBLER AT FS 678 AND I N THE FLOOR BEAM UPPER CHORD AT FS 674. THE CRACKED WEB DOUBLER AND UPPER CHORD WERE REMOVED. A NEW WEB DOUBLER AND CH ORD WERE INSTALLED ALONG WITH THE BEAM MODIFICATION PER BAC S/B 737-57-1139. THE REPAIR WAS ACCOMPLISHED PER ER/A 38072 2-14, REV A. 2 L 7 2 4F RT A16WE 2001053100100 20010531 00100 NM 2001 5 31 DL73K010734 1 20010507 A 5315 6545410137 FLOORBEAM BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 321DL 23093 THE LBL 24 LONGITUDINAL FLOORBEAM OVER THE CENTER WING WAS FOUND WITH A CRACK IN THE BEAM WEB DOUBLER AT FS 678. THE C RACKED WEB DOUBLER WAS REMOVED. A NEW WEB DOUBLER WAS INSTALLED AND THE BEAM MODIFIED PER BAC S/B 737-57-1139. THE REP AIR WAS ACCOMPLISHED PER ER/A 380725-14, REV A. 2 L 7 2 4F RT A16WE 2001053100101 20010531 00101 NM 2001 5 31 DL72S010738 1 20010509 A 5754 ATTACH ANGLE BOEING 727 727232 1384082 NM L/E SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 519DA 21470 A 1 INCH CRACK COVE SKIN ATTACH ANGLE AT O/B STOP PAD. REPAIR PER M/M 57-54-000-8. 2 L 7 3 4F A3WE 2001053100102 20010531 00102 NM 2001 5 31 DL767010740 1 20010509 A 3350 BPS73 POWER SUPPLY BOEING 767 767232 1385132 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 103DA 22215 LEFT OVERWING EXTERIOR EMERGENCY LIGHTING INOP. REMOVED AND REPLACED POWER SUPPLY AND BATTERY ASSEMBLY PER M/M. 2 L 7 2 4F RT A1NM 2001053100103 20010531 00103 NE 2001 5 31 DL757010741 2 20010509 A 7261 TUBE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE CLOGGED A DALA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 SO 27 661DN 27639 24972 726701 ON ARRIVAL INTO GATE A31, NR 2 ENG TAILPIPE FIRE. MTC MOTORED ENG AND EXTINGUISHED FIRE. FOUND NR 5 BEARING SCAV TUBE CLOGGED. C/W OPN 2002, NR 5 SCAV TUBE CLEANING. 2 L 7 2 4F 4 F RT A2NM E17NE 2001053100104 20010531 00104 NM 2001 5 31 DL767010742 1 20010509 A 3350 20131A BATTERY BOEING 767 767232 1385132 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 103DA 22215 LEFT OVERWING EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY AND BATTERY ASSEMBLY PER M/M. 2 L 7 2 4F RT A1NM 2001053100105 20010531 00105 NM 2001 5 31 DLM88010743 1 20010430 A 2430 6RW176YN3 TRANSFORMER DOUG MD88 MD88 3023688 NM E/E BAY DAMAGED A DALA K NONE M OVER TEMP IN INSP/MAINT 1 SO 27 942DL 49815 FWD E/E ABOVE TR L-2 HAS EVIDENCE OF HIGH HEAT TEMPERATURE DUE TO INSULATION BLANKET DAMAGE AND WORN FRAME AT STA 48 LB L 20. REPAIRED DAMAGE. 2 L 7 2 4F RT A6WE 2001053100106 20010531 00106 NE 2001 5 31 DL757010745 2 20010510 A 7230 PW2037RTC COMPRESSOR BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE FAILED A DALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 27 686DA 36020 0 27589 716544 ON TAKEOFF AT 1500 FT ASPD 190 NR 2 ENG COMP STALL FOLLOWED BY EGT IN YELLOW. EPR DROPPED TO 1.0. REDUCED POWER TO IDL E AND STAYED THERE THE REMAINDER OF THE FLIGHT WITH EGT 475. ENGINE FAILED 2ND AND 3RD STAGE BOROSCOPE. REPLACED NR 2 ENGINE PER 6T103 RII COMPLETED ON 6T103. 2 L 7 2 4F 4 F RT A2NM E17NE 2001053100107 20010531 00107 NM 2001 5 31 DLM88010746 1 20010510 A 2120 UNKNOWN DOUG MD88 MD88 3023688 NM COCKPIT ODOR A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 918DE 11102 49959 P80253 SMELLED FUMES / ODOR IN COCKPIT FROM 120 KNOTS ON TAKEOFF ROLL UNTIL 10,000 FT. ODOR VERY ACIDIC. NO SMOKE VISABLE BUT STUNG OUR EYES. CROSSFEEDS WERE CLOSED, ALL ANTI-ICE AND APU WERE OFF. TEMP CONTROLS WERE BOTH AT 12 O'CLOCK AND FLEX 50 EPR SETTING WAS 1.86. REPLACED RECIRC FAN FILTER. PERFORMED OPN 5088 DUCT BURNOUT. COULD NOT IDENTIFY CAUSE. REF LOG D286229004 FOR APU MCO. REPLACED WATER SEPARATOR BAGS. LEAK CHECKED NORMAL. ALSO CHECKED ALL WIRING IN COCKPIT O VERHEAD AND C/B PANELS. ALL NORMAL. OK FOR SERVICE. 2 L 7 2 4F RT A6WE 2001053100108 20010531 00108 NM 2001 5 31 DL72S010747 1 20010511 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 546DA 22677 THE FUSELAGE SKIN WAS FOUND WITH A 1 INCH LONG CRACK AT FS 570 BETWEEN STRINGERS 6R & 7R. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 380795-14. 2 L 7 3 4F A3WE 2001053100109 20010531 00109 NM 2001 5 31 DL73K010748 1 20010508 A 5315 FLOORBEAM BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 321DL 23093 THE LONGITUDINAL FLOORBEAM OVER THE CENTER WING BOX AT BL 0 WAS FOUND WITH A CRACK IN THE FLOORBEAM WEB AND UPPER CHO RD AT FS 660 AND 2 CRACKS IN THE FLOORBEAM WEB AT FS 705. THE CRACKED BEAM WAS REPAIRED PER BAC S/B 737-57-1210 AND ER/ A 380765-14. 2 L 7 2 4F RT A16WE 2001053100110 20010531 00110 NM 2001 5 31 DLM88010750 1 20010511 A 2120 SMOKE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE COCKPIT DETECTED A DALA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 918DE 49959 718214 ON TAKEOFF NOTICED THE SMELL IN THE COCKPIT AND THE AFT LAV SMOKE ALARM WENT OFF. PREPARED FOR FERRY FLIGHT TO ATL. 2 L 7 2 4F 4 F RT A6WE E9NE 2001053100111 20010531 00111 NM 2001 5 31 DL72S010751 1 20010512 A 3350 10617844 POWER SUPPLY BOEING 727 727232 1384082 NM CABIN MALFUNCTIONED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 521DA 21472 LT OVERWING EMERGENCY LIGHT STAYS ON WITH EMERGENCY LIGHT SW OFF. REPLACED POWER SUPPLY RACK. 2 L 7 3 4F A3WE 2001053100112 20010531 00112 NM 2001 5 31 DL72S010752 1 20010512 A 3350 100835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DEFECTIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 521DA 21472 LT AFT EMERGENCY LIGHT FLICKERS ON AND OFF. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 2001053100113 20010531 00113 NM 2001 5 31 DL72S010753 1 20010512 A 3350 900835A BATTERY BOEING 727 727225A 1384077 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8890Z 21859 RT OVERWING LIGHT INOP. REPLACED BATTERY. 2 L 7 3 4F RT A3WE 2001053100114 20010531 00114 WP 2001 5 31 DLL14010754 1 20010511 A 3350 5165741 POWER SUPPLY LKHEED 1011 1011385115 5265015 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 737D 193C1228 PWR SUPPLY WILL NOT ILLUMINATE OVERHEAD SIGNS AT R2 DOOR. REPLACED POWER SUPPLY. 2 L 7 3 4F A23WE 2001053100115 20010531 00115 NM 2001 5 31 DL76L010756 1 20010512 A 3230 273T610010 FUSE BOEING 767 767332 1382001 NM LT MLG FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 179DN 25144 AFTER T/O LEFT MAIN REMAINED DOWN AND LOCKED. GEAR HANDLE UP W/ LEFT MAIN GREEN LIGHT, DOOR AND GEAR CAUTION LIGHT. EI CAS GEAR DISAGREE GEAR DOORS. REPLACED LT EXT/RET FUSE. 2 L 7 2 4F RT A1NM 2001053100116 20010531 00116 NE 2001 5 31 DLM88010757 2 20010513 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 FAILED A DALA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 27 905DL 32305 0 49536 718151 DURING FLIGHT WHILE LEVELING AT FL310 NR 1 ENGINE CAUSED LOUD BOOM AND BEGAN ROLLING BACK. ENGINE WAS SHUT DOWN AND AIR CRAFT RETURNED TO ATL. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A6WE E9NE 2001053100117 20010531 00117 NM 2001 5 31 DL72S010758 1 20010513 A 3040 2312 CONTROL UNIT BOEING 727 727232 1384082 NM COCKPIT OVERHEATED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 523DA 21583 ON DESCENT, LIGHT SMOKE NOTICED BELOW PILOT''S L-2 WINDOW. WINDOW HEAT TURNED OFF AND SMOKE STOPPED. 2 L 7 3 4F A3WE 2001053100118 20010531 00118 NM 2001 5 31 DL76L010760 1 20010512 A 3350 RECEPTACLE 3015645 BOEING 767 767332 1382001 NM SLIDE LIGHT CORRODED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 194DN 28451 LT EXTERIOR EMERGENCY SLIDE ILLUMINATION LIGHT INOP. CHANGED ASSY RECEPTACLE. MOUNTING ASSY CKS OK. LIGHT CKS GOOD. 2 L 7 2 4F RT A1NM 2001053100119 20010531 00119 NM 2001 5 31 DL76S010761 1 20010513 A 2560 FLASHLIGHT BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 126DL 24076 EMERGENCY FLASHLIGHT AT 1L NOT FLASHING. FOUND DURING LAYOVER CHECK. REPLACED SAME. 2 L 7 2 4F RT A1NM 2001053100120 20010531 00120 NM 2001 5 31 DLM90010762 1 20010513 A 3350 LP726501 LIGHT DOUG MD90 MD9030 3023690 NM CABIN INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 901DA 53381 EMERGENCY TRACK LIGHT INOP NEAR SEAT 1A. RELAMPED LIGHT. 2 L 7 2 4F RT A6WE 2001053100121 20010531 00121 NM 2001 5 31 DLM90010763 1 20010513 A 3350 LP726501 LIGHT DOUG MD90 MD9030 3023690 NM CABIN INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 901DA 53381 EMERGENCY TRACK LIGHTING AT SEAT 15C INOP / BROKEN. REPLACED TRACK AND LIGHT ASSY. 2 L 7 2 4F RT A6WE 2001053100122 20010531 00122 NM 2001 5 31 DL73S010764 1 20010514 A 5320 6546877143 WEB BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 323DL 23095 CRACKS WERE FOUND IN LT AND RT STR 18A AT FS 727. THE CRACKS ARE SIMILIAR TO THAT IN S/B 737-53-1170. THE WEBS WERE RE PLACED AND THE PREVENTATIVE MODIFICATION WAS ACCOMPLISHED AT HMV. 2 L 7 2 4F RT A16WE 2001053100123 20010531 00123 NM 2001 5 31 DL757010765 1 20010511 A 5310 143N02121 DOOR FRAME BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 602DL 22809 THE C1 DOOR OPENING LOWER SILL WAS FOUND BADLY CORRODED AND REQUIRES REPLACEMENT BETWEEN STRINGERS 25R & 26R. THE LOWER SECTIONS WERE TEMPORARILY REMOVED TO ALLOW INSTALLATION OF A NEW SILL CHORD. THE CHORD WAS SPLICED BACK WITH TWO ALUMINUM ANGLES AND THE WEB WITH AN ALUM DOUBLER PER ER/A 380663-14. 2 L 7 2 4F RT A2NM 2001053100124 20010531 00124 NM 2001 5 31 DL757010766 1 20010511 A 5330 146N34007 SKIN BOEING 757 757232 1384965 NM FUSLEAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 602DL 22809 WHILE ACCOMPLISHING A SKIN REINFORCEMENT MODIFICATION TO THE LOWER AFT VHF ANTENNA CUTOUT, AN EXISTING REPAIR DOUBLER WA S FOUND. THE EXISTING REPAIR WAS REMOVED AND THE CUTOUT AREA INCREASED TO 18 X 5.25 INCHES. THE CUTOUT WAS REPAIRED WI TH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER PER ER/A 380619-14, REV A. 2 L 7 2 4F RT A2NM 2001053100125 20010531 00125 NM 2001 5 31 DL76L010768 1 20010514 A 2121 732591F FAN BOEING 767 767332 1382001 NM E/E BAY FAILED A DALA H DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 27 189DN 25990 FWD EQPT EXHAUST FAN STATUS MESSAGE ILLUMINATED. FWD EXH EQUIP COOL FAN C/B POPPED. CAPT REPORTED SMOKE IN COCKPIT. R EPLACED LING ON LAND LINE. REPLACED FWD EQUIPMENT COOLING FAN. 2 L 7 2 4F RT A1NM 2001053100126 20010531 00126 NM 2001 5 31 DL76L010769 1 20010514 A 3150 M1000 CIRCUIT BOARD BOEING 767 767332 1382001 NM E/E BAY FAULTY A DALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 27 181DN 25986 REJECTED T/O DUE TO AUDIBLE WARNING WITH NO OTHER INDICATION. GW 361.3, NO TR''S USED, USED RTO AUTO BRAKES, WIND 350/1 4KTS. GND SPEED 110KTS. DUE TO HISTORY OF AURAL WARNINGS GOING OFF W/ NO OTHER INDICATIONS CHANGED THE M1000 CARD FOR AURAL WARNING AND CHIME. ALSO CHANGED THE WARNING ELEC POWER SUPPLY M621 MODULE B AND AS A PRECAUTION CHANGED DUCT LEAK AND WHEEL WELL FIRE CONT M691. OPS CHECK NORMAL PER MM. 2 L 7 2 4F RT A1NM 2001053100127 20010531 00127 NM 2001 5 31 DLM90010772 1 20010514 A 3350 8039251 POWER SUPPLY DOUG MD90 MD9030 3023690 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 914DN 53394 AFT OVERRHEAD AISLE EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY. 2 L 7 2 4F RT A6WE 2001053100128 20010531 00128 NM 2001 5 31 DL757010773 1 20010514 A 5330 143N33002 SKIN BOEING 757 757232 1384965 NM FUSELAGE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 602DL 22809 THE FUSELAGE SKIN BETWEEN FS 590-660 AND BETWEEN STRINGES 16L & 18L WAS FOUND WITH SEVERAL DENTS AND GOUGES. THE DAMAGE S WERE REMOVED WITH THREE SEPARATE CUTOUTS. EACH CUTOUT WAS REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER. THE REPAIR WA S ACCOMPLISHED PER ER/A 380592-14, REV A. 2 L 7 2 4F RT A2NM 2001053100129 20010531 00129 NM 2001 5 31 DL757010774 1 20010514 A 5315 146N509116 FLOORBEAM BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 602DL 22809 THE UPPER CAP OF THE FS 1681 PASSENGER FLOORBEAM WAS FOUND WITH SEVERAL AREAS OF CORROSION ALONG ITS LENGTH. THE UPPER C AP WAS TRIMMED OFF ALONG THE ENTIRE BEAM LENGTH TO REMOVE ALL CORROSION. A NEW UPPER CAP WAS FABRICATED FROM AN ALUMINU M EXTRUSION AND INSTALLED PER ER/A 380597-14, REV A. 2 L 7 2 4F RT A2NM 2001053100133 20010531 00133 WP 2001 5 31 ZW0A0101809 1 20010511 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 924TW 49100 DURING CHECK-C MAINT FOUND WEB CRACKED AFT OF LONGERON 18R, APPROX 34 INCHES RBL, CANT 1463. STOP DRILLED CRACK PER SRM 53-01 FIG 2. 2 L 7 2 4F A6WE 2001053100134 20010531 00134 2001 5 31 01FDEA00352 4 20010515 A 3442 RADAR BOEING 727 727233 138408A NM WEATHER RADAR FAULTY A FDEA A UNSCHED LANDING I FLT. ATTITUDE INST. CL CLIMB 1 SO 25 219FE 21102 AT 14000 MSL WITH A/C STRAIGHT AND LEVEL RADAR TILT AT +2.5 DEG.R&R RADAR ANTENNA DRIVE UNIT PER AMM 34-41-021-4. R&R RA DAR T/R PER AMM 34-41-041-4. TEST NORM. 2 L 7 3 4F RT A3WE 2001053100135 20010531 00135 NM 2001 5 31 SWAA011451 1 20010514 A 3350 BR2013 LIGHT BOEING 737 7377H4 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 788SA 30603 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT ROW 7. RELAMPED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001053100136 20010531 00136 NM 2001 5 31 01FDEA00355 1 20010515 A 5311 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 276FE 22041 DENTED BS 580, LBL 33, WL 159 PER FEDEX EA 7-5310-29267. R&R PER FEDEX SRM 51-40-3 2 L 7 3 4F RT A3WE 2001053100137 20010531 00137 NM 2001 5 31 01FDEA00356 1 20010515 A 5311 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 276FE 22041 DENTED FRAME AT BS 600, LBL 33, WL 159. R&R PER FEDEX SRM 51-40-3 2 L 7 3 4F RT A3WE 2001053100138 20010531 00138 NM 2001 5 31 01FDEA00360 1 20010515 A 5311 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 276FE 22041 FWD CARGO BAY LT FRAME AT BS 500, LBL 40 HAS A DENT IN TOP FLANGE. REMOVED AND REPLACED PER FEDEX SRM 51-40-3. ALODINED AND PRIMED PER FEDEX 51-20-151. 2 L 7 3 4F RT A3WE 2001053100139 20010531 00139 NM 2001 5 31 VNAA0105008 1 20010513 A 2120 SMOKE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DETECTED A VNAA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 460PS 3061 DURING TAXI TO THE RUNWAY, THE FLIGHT ATTENDANT NOTIFIED THE CAPTAIN THERE WAS SMOKE IN THE CABIN. APPROXIMATELY 10 TO 15 SECONDS LATER THE CREW RECEIVED A LAV SMOKE CAS MESSAGE. THE CREW IMMEDIATELY FOLLOWED THE QUICK REFERENCE HANDBOOK AND EVACUATED THE PLANE. THERE WERE NO INJURIES OR DAMAGE TO THE PLANE. MAINTENANCE SENT MECHANICS FROM PIT TO INSPECT THE AIRCRAFT. THE MECHANICS GROUND RAN THE AIRCRAFT AND INSPECT THE ENVIRONMENTAL CONTROL SYSTEM. NO DEFECTS WERE FOU ND AND THE PROBLEM COULD NOT BE DUPLICATED. THE AIRCRAFT WAS REPOSITIONED TO PIT WITH NO FURTHER INCIDENTS, AGAIN THE A IRCRAFT WAS INSPECTED WITH NO DEFECTS FOUND. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001053100140 20010531 00140 WP 2001 5 31 CALA0100466 1 20010516 A 5730 SKIN DOUG DC10 DC1030 3023501 WP RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12061 47851 INSPECTION FOUND A CRACK IN RT WING LEADING EDGE SKIN AT SLAT NR 7 I/B TRACK, XORS 79.9. REPAIRED IAW SRM 57-10-00. 2 L 7 3 4F A22WE 2001053100141 20010531 00141 NM 2001 5 31 AWXA0001761 1 20010516 A 5311 651630087 FRAME BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 BS 178 BLKHD RT CHORD O/B HAS CRACK INDICATION AT WL 207 ON FUSE SKIN. NDT INSP IAW BOEING NDTM PT 6 51-00-00 FIG 23; RT SIDE CHORD REPLACED IAW SRM 51-10-1 PG 8 AND SRM 51-30-2 PG 2-3 AND DWG 65-16300; METAL REPROTECTED IAW SRM 51-10-2 P G 7; EDGE SEALED IAW SRM 51-24-0; RESTORED FINISH IAW MM 51-21-0. 2 L 7 2 4F RT A16WE 2001053100142 20010531 00142 NM 2001 5 31 01FDEA00361 1 20010515 A 5311 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 276FE 22041 DENTED FRAME AT BS 540, LBL 40, WL 164 PER EA 7-5310-29267. REMOVED AND REPLACED PER FEDEX SRM 51-40-3. ALODINED AND PR IMED PER FEDEX 51-20-151. 2 L 7 3 4F RT A3WE 2001053100143 20010531 00143 NM 2001 5 31 01FDEA00362 1 20010515 A 5311 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 276FE 22041 DENTED FRAME AT BS 560, LBL 47, WL 168 PER EA 7-5310-29267. R&R PER IAW FEDEX EA 7-5310-29267, SRM 51-40-3. 2 L 7 3 4F RT A3WE 2001053100144 20010531 00144 NM 2001 5 31 01FDEA00363 1 20010515 A 5311 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 276FE 22041 DENTED FRAME AT BS 560, LBL 35, WL 160 PER FEDEX EA 7-5310-29267. R&R PER IAW FEDEX EA 7-5310-29267, SRM 51-40-3. 2 L 7 3 4F RT A3WE 2001053100145 20010531 00145 NM 2001 5 31 01FDEA00364 1 20010515 A 5315 BAC1503100060 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 276FE 22041 CORROSION ON FLOORBEAM AT FASTENER HOLES BS 560 BETWEEN RBL 25 & LBL 25, WL 208. REMOVED, REPLACED AND FAB PER IAW FEDEX SRM 53-10-1, 53-10-8, 51-10-2, 51-20-4 & 51-30-2. 2 L 7 3 4F RT A3WE 2001053100146 20010531 00146 NM 2001 5 31 01FDEA00365 1 20010515 A 5313 65562166 STRINGER BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 276FE 22041 STR 27L CRACKED AT BS 480 (FWD SIDE OF 480 FRAME). R&R STRINGER PER FEDEX SRM 53-10-3. 2 L 7 3 4F RT A3WE 2001053100147 20010531 00147 NM 2001 5 31 01FDEA00367 1 20010515 A 5315 651758866 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 276FE 22041 (C53-221-01) AT UPPER SURFACE OF 25-G BEAM BS 270, WL 208, LBL 1-6. 2 L 7 3 4F RT A3WE 2001053100148 20010531 00148 2001 5 31 DL76L010714 4 20010504 A 3442 20412170416 TRANSCEIVER BOEING 767 767332 1382001 NM E/E BAY FAILED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 188DN 27583 RADAR SYSTEM BLANK EN ROUTE. DIVERTED DUE TO IMPENDING WEATHER INTO BOS. REPLACED WEATHER RADAR TRANSCEIVER. ALL SYTE MS CHECK GOOD. 2 L 7 2 4F RT A1NM 2001053100149 20010531 00149 2001 5 31 01FDEA00369 4 20010513 A 3418 STALL WARNING DOUG MD11 MD11F 3023600 NM COCKPIT FAULTY A FDEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 25 617FE 48748 ON SHORT FINAL GOT STICK SHAKER. AMBER SLATS WERE ILLUM ON PFD. PREF RTS ON FCC NR 1 AND 2 AOA TESTS AND AUTOLAND TEST S ALL PASSED OK TO CONTINUE. 2 L 7 3 4F RT A22WE 2001053100150 20010531 00150 NE 2001 5 31 DL76G010716 2 20010505 A 7261 1335M94G01 LINE BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 1 ENGINE CRACKED A DALA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 1605 30198 704883 ENG OIL QTY IND ZERO, TEMP/PRESSURE IND NORMAL. QTY IND ZERO FROM EICAS COMPUTER AUTO AND RIGHT. ON LANDING OIL PRESS WENT INTO YELLOW WHEN REVERSE WAS APPLIED. SERVICED ENG OIL TO TOP (21 QTS) SPUN ENG. FOUND LINE CRACKED. LINE SCAVEN GE LINE FROM ANGLE GEARBOX TO SCAVENGE PUMP. REPLACED AND RUN UP LEAK CHECK GOOD. CHECKED MASTER CHIP DETECTOR AND SC AVENGE CHIP DETECTORS. CHECKED MAIN OIL SCREEN, ALL GOOD. 2 L 7 2 4F 4 F RT A1NM E13NE 2001053100151 20010531 00151 NM 2001 5 31 DL73E010722 1 20010505 A 5343 6546543509 SUPPORT FITTING BOEING 737 7372J8 1384489 NM LT MLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 235WA 22859 THE WL 188.5 LUG ON THE LT MLG SIDE STRUT SUPPORT FITTING AT FS 685 WAS FOUND WITH CORROSION IN THE LUG BORE. THE CORRO SION WAS REMOVED BY OVERSIZING THE LUG BORE. AN ALUMINUM REPAIR BUSHING WAS INSTALLED TO RESTORE THE LUG DIAMETER PER E R/A 380741-14. 2 L 7 2 4F RT A16WE 2001053100152 20010531 00152 WP 2001 5 31 ARWA0010502 1 20010514 A 3233 57740355508 ACTUATOR DOUG DC8 DC861 3021952 WP RT MLG FAILED A ARWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 30UA 45888 AFTER TAKEOFF RIGHT GEAR UNSAFE LIGHT ILLUMINATED AND DOOR NOT LATCHED LIGHT ILLUMINATED. RECYCLED GEAR, NO HELP. RETU RNED TO SAL. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR ACTUATING CYLINDER PER J/C 6209 SYSTEM OPERATIONAL CHECK NORMAL. NO LEAKS NOTED. 2 L 7 4 4F 4A25 2001053100153 20010531 00153 WP 2001 5 31 MWEA010749 1 20010515 A 5311 991184133 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 CORROSION ON FORWARD SIDE OF FORMER AT STATION 1087 BETWEEN LONGERONS 17 RIGHT AND 19 RIGHT. REMOVED SHEAR TIE, CANTED FRAME BRACKET, CORROSION, FABRICATED AND INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001053100154 20010531 00154 WP 2001 5 31 MWEA010750 1 20010515 A 5310 5917579141 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 LEFT LAV AREA AFT PRESSURE BULKHEAD DOOR JAMB HAS A CRACK ON WEB ATTACHED TO TEE 4L INBOARD SIDE. STOP DRILLED CRACK, F ABRICATED, LOCATED, DRILLED AND INSTALLED ANGLES. 2 L 7 2 4F A6WE 2001053100155 20010531 00155 WP 2001 5 31 MWEA010751 1 20010515 A 5311 9915588253 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 LEFT LAV AREA AFT PRESSURE BULKHEAD UPPER FORMER (1L) IS CRACKED ON OUTBOARD CORNER. STOP DRILLED CRACK, FABRICATED AND INSTALLED ANGLE REPAIR. 2 L 7 2 4F A6WE 2001053100156 20010531 00156 WP 2001 5 31 MWEA010752 1 20010515 A 5310 99577397 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 CRACK ON SHEAR TIE AT STATION 945 BETWEEN LONGERON 16 AND 15 RIGHT. REMOVED CRACKED SHEAR TIE, FABRICATED AND INSTALLED NEW SHEAR TIE. 2 L 7 2 4F A6WE 2001053100157 20010531 00157 WP 2001 5 31 MWEA010753 1 20010515 A 5310 995773927 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 CRACK IN RADIUS OF SHEAR TIE AT STATION 951 BETWEEN LONGERON 16 AND 15 RIGHT. REMOVED SHEAR TIE, FABRICATED AND INSTALL ED NEW SHEAR TIE. 2 L 7 2 4F A6WE 2001053100158 20010531 00158 WP 2001 5 31 MWEA010754 1 20010515 A 5311 995823869 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 CRACK IN RADIUS OF FRAME AT STATION 980 JUST BELOW LONGERON 14 RIGHT. REMOVED CRACKED SHEAR TIE, FABRICATED AND INSTALL ED NEW SHEAR TIE. 2 L 7 2 4F A6WE 2001053100159 20010531 00159 WP 2001 5 31 MWEA010755 1 20010515 A 5320 99155851 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 INTERCOSTAL BETWEEN LAV BS 965-980 (CENTER LINE) DISTORTED. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001053100160 20010531 00160 WP 2001 5 31 MWEA010757 1 20010515 A 5753 5910134143 SKIN DOUG DC9 DC932 3022066 WP T/E FLAP DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 LEFT FLAP, LOWER SKIN HAS TWO SHARP DENTS, LOCATED JUST AFT OF LEFT MLG. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001053100161 20010531 00161 WP 2001 5 31 MWEA010758 1 20010515 A 5230 59101413 SKIN DOUG DC9 DC932 3022066 WP CARGO DOOR BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 FORWARD CARGO DOOR SKIN IS BENT IN THE LOWER AFT CORNER. REFORMED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND SHIMS. 2 L 7 2 4F A6WE 2001053100162 20010531 00162 NM 2001 5 31 VNAA0105019 1 20010527 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 438JS 348 3056 THE CREW REPORTED THAT THE EMERGENCY BATTERIES WERE DRAINED. THE AIRCRAFT WAS FERRIED TO PIT WHERE MAINTENANCE REPLACED THE EMERGENCY BATTERIES IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001053100163 20010531 00163 WP 2001 5 31 MWEA010759 1 20010515 A 5310 39148701 DOUBLER DOUG DC9 DC932 3022066 WP DOOR FRAME CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 FORWARD PAX DOOR JAMB INTERNAL TITANIUM DOUBLER IS CRACKED AT UPPER FORWARD CORNER. REMOVED DOUBLER, LOCATED, DRILLED A ND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001053100164 20010531 00164 WP 2001 5 31 MWEA010761 1 20010515 A 5347 9957871 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 FIRST OFFICERS INBOARD AFT SEAT TRACK IS WORN AT STOP PIN HOLES. REMOVED SEAT TRACK, LOCATED AND DRILLED REPAIR STRAP, REMOVED DAMAGE FROM SEAT TRACK, INSTALLED REPAIR STRAP AND SEAT TRACK. 2 L 7 2 4F A6WE 2001053100165 20010531 00165 WP 2001 5 31 MWEA010762 1 20010515 A 5347 9957871 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 FIRST OFFICERS OUTBOARD SEAT TRACK IS WORN AT STOP PIN HOLES. REMOVED SEAT TRACK, LOCATED AND DRILLED REPAIR STRAP, REM OVED DAMAGE FROM SEAT TRACK, INSTALLED REPAIR STRAP AND SEAT TRACK. 2 L 7 2 4F A6WE 2001053100166 20010531 00166 WP 2001 5 31 MWEA010764 1 20010516 A 5311 591359577 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 AFT ACCESSORY FRAME STATION 1076 IS CRACKED AT LONGERON 2 LEFT. FABRICATED REPAIR SPLICE, REMOVED DAMAGED, LOCATED AND DRILLED REPAIR SPLICE, INSTALLED FRAME SPLICE. 2 L 7 2 4F A6WE 2001053100167 20010531 00167 WP 2001 5 31 MWEA010765 1 20010516 A 5311 591359577 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 AFT ACCESSORY FRAME STATION 1076 SHEAR TIE HAS A CRACK BETWEEN LONGERON 1 AND 2 RIGHT. REMOVED DAMAGE, FABRICATED, LOCA TED AND DRILLED NEW SHEAR TIE, INSTALLED NEW SHEAR TIE AND SPLICE. 2 L 7 2 4F A6WE 2001053100168 20010531 00168 NM 2001 5 31 VNAA0105012 1 20010521 A 2432 DTSP400L BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE E/E BAY OVERHEATED A VNAA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 GL 07 440JS 265 3058 DURING CLIMB, THE CREW RECEIVED A RED WARNING PANEL INDICATION OF A NR 2 BATTERY OVERHEAT. FLIGHT 9406 RETURNED TO THE FIELD WHERE MAINTENANCE INSPECTED AND REPLACED THE NR 2 MAIN BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00 -00. OPERATIONAL CHECKS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001053100169 20010531 00169 WP 2001 5 31 AT0100133 1 20010421 A 5347 CARGO TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 811AT 47285 FOUND FORWARD PIT LOWER SIDEWALL PANEL AND TRACK CORRODED AT BS 427-598. REMOVED CORROSION AND FOUND TO BE OUT OF LIMIT S. CUT, DRILLED, TREATED, PRIMED AND INSTALLED NEW CARGO SECTIONS IAW DC9 SRM 53-01 FIGURE 1, 53-21-0 FIGURE 78, 51-10- 03, 53-05 FIGURE 4C AND 51-10-3. 2 L 7 2 4F A6WE 2001053100170 20010531 00170 WP 2001 5 31 AT0100134 1 20010424 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 811AT 47285 FOUND FLOOR SUPPORT ANGLE AT BS 170-195 CORRODED. REMOVED OLD SUPPORT, CUT, DRILLED, TREATED, PRIMMED AND INSTALLED NEW SUPPORT IAW DC9 SRM 51-10-2, 51-30-2, 51-10-3. 2 L 7 2 4F A6WE 2001053100171 20010531 00171 WP 2001 5 31 AT0100135 1 20010424 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 811AT 47285 FOUND CABIN FLOOR SUPPORT ANGLE CORRODED AT BS 195-LBL 20. REMOVED FLOOR SUPPORT, CUT AND TRIMMED TO FIT IAW DC9 SRM 53 -11-1 FIGURE 13, 51-10-3. 2 L 7 2 4F A6WE 2001053100172 20010531 00172 WP 2001 5 31 AT0100136 1 20010424 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 811AT 47285 FOUND CORROSION ON FLOOR SUPPORT ANGLE AT BS 160-197. REMOVED AND REPLACED, CUT, DRILLED, TREATED, AND PRIMED FLOOR SUP PORT IAW DCI SRM 53-10 FIGURE 1, 51-10-2, 53-11-1 FIGURE 13, 51-10-3, 51-30-2. 2 L 7 2 4F A6WE 2001053100173 20010531 00173 WP 2001 5 31 AT0100137 1 20010424 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 811AT 47285 FOUND CORROSION ON FLOOR SUPPORT ANGLE AT BS 160-208. REMOVED AND REPLACED, CUT, TRIMMED, DRILLED, TREATED, PRIMED AND INSTALLED NEW ANGLE IAW DC9 SRM 51-30-2, 51-30-5, 51-10-4, 53-11-1 FIGURE 13. 2 L 7 2 4F A6WE 2001053100174 20010531 00174 WP 2001 5 31 ZW0A0101901 1 20010514 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 907TW 49165 DURING CHECK-C MAINT THE CHAIR TRACK AT LBL 34 HAD CORROSION AT STA 1130 TO 1138. REPLACED TRACK PER DRAWING C03580 AND INSTALLED PER SRM 51-30-1. 2 L 7 2 4F A6WE 2001053100175 20010531 00175 NM 2001 5 31 SWAA011476 1 20010518 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 389SW 26592 EEPLS TRACK WIRING LOOSE. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001053100176 20010531 00176 2001 5 31 SWAA011477 4 20010518 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001053100177 20010531 00177 2001 5 31 SWAA011478 4 20010518 A 2565 63551101 SLIDE BOEING 737 7377H4 NM SERVICE DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 726SW 27858 AFT SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001053100178 20010531 00178 WP 2001 5 31 AT0100138 1 20010422 A 5347 CARGO TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 811AT 47285 FOUND CORROSION ON FORWARD CARGO TRACK AT BS 427-518. REMOVED AND REPLACED SECTION OF TRACK IAW DC9 SRM 51-10-3, 51-10- 4, 53-27-0 FIGURE 7A. 2 L 7 2 4F A6WE 2001053100179 20010531 00179 WP 2001 5 31 AT0100139 1 20010417 A 5311 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 811AT 47285 FOUND CRACK AT BS 1074. PERFORMED PERMINATE REPAIR AT BS 1074 IAW DCI SRM 51-10-3 AND DC9 MM 53-10 FIGURE 811. 2 L 7 2 4F A6WE 2001053100180 20010531 00180 WP 2001 5 31 AT0100140 1 20010424 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 811AT 47285 FOUND FORWARD CABIN FLOOR SUPPORT ANGLE CORRODED AT BS 200 - RBL20. REMOVED AND REPLACED, CUT, DRILLED, TRIMMED, AND PR IMED NEW ANGLE IAW DC9 SRM 53-11-1 FIGURE 13, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 2001053100181 20010531 00181 WP 2001 5 31 AT0100142 1 20010423 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 811AT 47285 FOUND AFT CARGO COMPARTMENT AT BS 870 FLOOR SUPPORT ANGLE CRACKED. REMOVED SUPPORT ANGLE, WELDED CRACK AND REINSTALLED SUPPORT IAW EA 12-5521-29-C1362. 2 L 7 2 4F A6WE 2001053100182 20010531 00182 WP 2001 5 31 ZW0A0101902 1 20010514 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 907TW 49165 DURING CHECK-C MAINT FOUND CORROSION ON TRACK NUMBER 4 AT STA 200 TO 266, IN TRACK AND FLOOR SUPPORT. REPLACED TRACK SE CTION STA 200 TO 266 PER DRAWING C03580. INSTALLED PER SRM 51-30-5. SEALED PER SRM 51-20-0. TREATED SURFACES PER 51-1 0-3. 2 L 7 2 4F A6WE 2001053100183 20010531 00183 WP 2001 5 31 ZW0A0101903 1 20010516 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 924TW 49100 DURING CHECK-C MAINT IN MID CARGO COMPT FOUND CRACK STARTING IN ANGLE ATTACHED TO FORMER STA 593, 6 INCHES OTBD OF LEFT TRACK. USED PURE TITANIUM WELD ROD, INSERT GAS SHIELD, WELDED LENGTH OF CRACK. STRESS RELIEVED ANGLE PER DACO OPS 6-33 AFTER WELDING PAGE 13. RE-INSTALLED ANGLE PER SRM 51-30-02. 2 L 7 2 4F A6WE 2001053100184 20010531 00184 WP 2001 5 31 ZW0A0101904 1 20010515 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT IN AFT CARGO COMPT FOUND CORROSION ON LONGERON 29L, JUST FWD OF STA 1338. REMOVED CORROSION PER SP M 6-80-01. REPLACED FITTING PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-5 AND 51-30-1. 2 L 7 2 4F RT A6WE 2001053100185 20010531 00185 WP 2001 5 31 ZW0A0101905 1 20010515 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT IN THE AFT CABIN THE NUMBER 3 SEAT TRACK HAD HEAVY CORROSION FROM STA 1288 TO 1309, LBL 24 INCHES. REPLACED SEAT TRACK PER SRM 53-05, FIG 4, AND DRAWING 5930566. 2 L 7 2 4F RT A6WE 2001053100186 20010531 00186 WP 2001 5 31 ZW0A0101906 1 20010515 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT IN THE AFT CABIN THE NUMBER 3 SEAT TRACK HAD HEAVY CORROSION FROM STA 1031 TO 1288, LBL 24 INCHES. REPLACED SEAT TRACK PER SRM 53-05, FIG 4, AND DRAWING 5930566. 2 L 7 2 4F RT A6WE 2001053100187 20010531 00187 WP 2001 5 31 ZW0A0101908 1 20010516 A 5320 ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT AT CABIN OVERWING BELOW CABIN FLOOR AN ANGLE WAS CRACKED AT STA 826, LBL 60 INCHES, 5 INCHES BELOW FLOOR. INSTALLED NEW FACTORY PART PER SPM 6-70-01, PART 4B, AND DRAWING 3920342. 2 L 7 2 4F RT A6WE 2001053100188 20010531 00188 WP 2001 5 31 ZW0A0101909 1 20010518 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 907TW 49165 DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT LBL 8, STA 185 TO 200. REPLACED WITH NEW SUPPORT. 2 L 7 2 4F A6WE 2001053100189 20010531 00189 2001 5 31 SWAA011479 4 20010518 A 2565 D31354 MOUNT BOEING 737 7373H4 1384600 NM EVAC SLIDE LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 371SW 26598 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE MOUNT LOOSE. SECURED MOUNT PER MM. 2 L 7 2 4F RT A16WE 2001053100190 20010531 00190 NM 2001 5 31 SWAA011480 1 20010518 A 5320 BAC1503 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED SERVICE CHECK, FOUND MLG WHEEL WELL BULKHEAD VERTICAL STIFFENER CRACKED, BS 663, RBL 6.5. REPAIRED PER SWA RA. 2 L 7 2 4F RT A16WE 2001053100191 20010531 00191 NM 2001 5 31 SWAA011482 1 20010518 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, JUST ABOVE STR 12L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001053100192 20010531 00192 NM 2001 5 31 SWAA011483 1 20010519 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D-CHECK, FOUND STR 11L CRACKED AT BS 867. REPAIRED STR PER BFG ER. 2 L 7 2 4F A16WE 2001053100193 20010531 00193 NM 2001 5 31 SWAA011484 1 20010518 A 5311 6546529 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 188, STR 17R, WL 208. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2001053100194 20010531 00194 NM 2001 5 31 SWAA011485 1 20010518 A 5310 6546529 SHEAR TIE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 360, RBL 70, WL 225.5. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F A16WE 2001053100195 20010531 00195 EU 2001 5 31 RAIA00105012 1 20010518 A 2424 10200311 GCU AEROSP ATR42 ATR42300 8680920 EU E/E BAY FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 426TE 24618 1902 5101177 228 7006-SGF-LEFT DC GENERATOR FAULT ILLUMINATED AFTER TAKEOFF. MAINTENANCE INSPECTED AND REPLACED LEFT GENERATOR CONTROL U NIT (GCU) AND LEFT DC GENERATION SYSTEM HALL EFFECT SENSOR. 2 H 7 2 4T RT A53EU 2001053100196 20010531 00196 NM 2001 5 31 SWAA011486 1 20010518 A 5312 6516300 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 178, WL 208. REPAIRED WEB PER SRM. 2 L 7 2 4F A16WE 2001053100197 20010531 00197 NM 2001 5 31 SWAA011487 1 20010518 A 5312 6516300 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED D-CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17.1, WL 230. REPAIRED WEB PER BFG ER. 2 L 7 2 4F A16WE 2001053100198 20010531 00198 NM 2001 5 31 SWAA011488 1 20010518 A 5315 6546804 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CRACKED AT BS 647.5, LBL 54, WL 208. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F A16WE 2001053100199 20010531 00199 NM 2001 5 31 SWAA011489 1 20010518 A 5330 6545773 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT LT WINDOW NR 28, 29, 25, 24, 26 AND 27, UPPER AFT CORNER CUTOUT S. REPAIRED PER BFG ER. 2 L 7 2 4F A16WE 2001053100200 20010531 00200 2001 5 31 SWAA011468 4 20010516 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED BC1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED EMERGENCY EVAC SL IDE PER MM. 2 L 7 2 4F RT A16WE 2001053100201 20010531 00201 WP 2001 5 31 MWEA010794 1 20010521 A 5311 995773921 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 FRAME AT BS 945 LEFT HAS SEVERAL ELONGATED HOLES AND SOME EXTRA HOLES. REMOVED DAMAGED FRAME, LOCATED, DRILLED AND INST ALLED FRAME AND SHEAR TIE. 2 L 7 2 4F A6WE 2001053100202 20010531 00202 WP 2001 5 31 MWEA010795 1 20010521 A 5311 995733931 SPLICE DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 FRAME SPLICE AT STATION 945 LEFT SIDE BETWEEN LONGERON 9 LEFT AND 10 LEFT IS DAMAGED. FABRICATED, LOCATED, DRILLED AND INSTALLED SPLICE. 2 L 7 2 4F A6WE 2001053100203 20010531 00203 WP 2001 5 31 MWEA010796 1 20010521 A 5310 995773927 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 SHEAR TIE AT STATION 945 LEFT SIDE FROM LONGERON 10-14 HAS MISDRILLED AND ELONGATED HOLES. REMOVED, FABRICATED AND INST ALLED SHEAR TIE. 2 L 7 2 4F A6WE 2001053100204 20010531 00204 WP 2001 5 31 MWEA010797 1 20010521 A 5320 591013037 CHANNEL DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 CRACK INDICATION DISCOVERED ON RADIOGRAPH RLB CRACK LOCATED ON RIGHT SIDE OF STRUCTURE UNDER LOWER VENTRAL DOOR JAMB PAN EL. REMOVED CRACKED CHANNEL, LOCATED, DRILLED AND INSTALLED NEW CHANNEL. 2 L 7 2 4F A6WE 2001070200029 20010702 00029 NM 2001 7 2 01FDEA00366 1 20010515 A 5330 655458045 SKIN BOEING 727 727233 138408A NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 276FE 22041 UPON REMOVAL OF FAIRING BRACKET FOR FAIRING 3619 BS 950D, STR 18R FOUND HOLE IN FUSELAGE SKIN ELONGATED. *S/D* removed and replaced per fedex ea 7-5310-57265, srm 51-10-2, 53-10-3, 51-10-2, 51-30-5, 51-30-2. 2 L 7 3 4F RT A3WE 2001053100205 20010531 00205 WP 2001 5 31 AT0100157 1 20010420 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 803AT 47261 FOUND AFT CARGO COMPARTMENT BS 965 RBL 12 FLOORBEAM ATTACH ANGLE TO HAVE EXFOLIATED CORROSION. REPLACED FLOORBEAM IAW R EO L00433 REV A, DC9 SRM 53-04 FIG 12C, 53-05 FIG 79, 51-10-04, 51-10-03, 51-30-02, 51-30-05, 51-30-01, AND MM 20-18. 2 L 7 2 4F A6WE 2001053100206 20010531 00206 NM 2001 5 31 2001UALA00403 1 20010402 A 2400 ELECTRICAL SYS BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE E/E BAY POWER LOSS A UALA O OTHER H ELECT. POWER LOSS-50 PC CL CLIMB 1 WP 29 926UA 26648 ELECTRICAL POWER LOSS IN FLIGHT. *S/D* POWER WAS RESTORED IN FLIGHT AND THE AIRCRAFT LANDED AT ITS DESTINATION AIRPORT WITHOUT INCIDENT. MAINTENANCE COULD NOT DUPLICATE PROBLEM ON THE GROUND. NO FAULTS WERE FOUND DURING TROUBLESHOOTING. 2 L 7 2 4F 4 F RT A16WE E2GL 2001053100207 20010531 00207 NM 2001 5 31 01FDEA00338 1 20010508 A 3232 65239337 FITTING BOEING 727 727227 1384078 NM LT MLG SHEARED A FDEA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 25 495FE 21669 LT MLG DOOR ACTUATOR RIB FITTING SHEARED IN FLIGHT. LOG PAGE 00199388 IND TEST FLT UNSAT DUE TO MLG DOOR BROKEN IN FLT. *S/D* REMOVED AND REPLACED LT MLG INBOARD DOOR ASSY, (P/N 65-24764-129) ACTUATOR (P/N 7-3141-4), PUSHROD ASSY (P/N 69 -21445). 2 L 7 3 4F A3WE 2001053100208 20010531 00208 NM 2001 5 31 PCAA0105043 1 20010520 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A PCAA K NONE L NO TEST NR NOT REPORTED 1 EA 13 819EX 016 ALB- FLIGHT 3550. CREW REPORTED FLOOR EMERGENCY LIGHTS ON RIGHT SIDE OF AIRCRAFT INOPERATIVE FROM ROW 2 TO ROW 6. MAIN TENANCE INSPECTED AND FOUND CONNECTOR LOOSE AT ROW 2. CONNECTOR WAS RESECURED. EMERGENCY LIGHTS OPERATE NORMALLY. AIR CRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001053100209 20010531 00209 NM 2001 5 31 VNAA0105002 1 20010505 A 3260 LIGHT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA A UNSCHED LANDING N FALSE WARNING LD LANDING 1 GL 07 430JS 3044 WHEN LANDING THE CREW RECEIVED THREE RED THEN TWO GREEN GEAR INDICATIONS. THE CREW DECLARED AN EMERGENCY AND DIVERTED T O DAY. FLIGHT 5002 LANDED IN DAY WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED AND REPLACED THE GEAR INDICATION BUL BS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEA SED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001053100210 20010531 00210 NM 2001 5 31 VNAA0105003 1 20010506 A 3250 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT ACTIVATED A VNAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 07 328JS 3030 AT THE OUTER MARKER THE CREW ATTEMPTED TO LOWER THE LANDING GEAR AND RECEIVED A NOSE WHEEL STEERING POWER-UP FAIL CAS ME SSAGE. THE CREW NOTIFIED THE TOWER AND PERFORMED A GO AROUND. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK PROCEDURE S AND RECYCLED THE LANDING GEAR. AFTER FOLLOWING THESE PROCEDURES THE CAS MESSAGES CLEARED AND FLIGHT 4024 LANDED WITHO UT ANY FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001053100211 20010531 00211 NM 2001 5 31 SABA010016 1 20010404 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 813SN 052 AIRCRAFT 813 IN CVG. DURING PREFLIGHT THE FRONT FOUR FLOOR LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. AIRCRAFT WAS FERRI ED TO CLT FOR REPAIR. NO EMERGENCY WAS DECLARED AND NO EMERGENCY PROCEDURES WERE USED. MAINTENANCE REPAIRED A BROKEN W IRE TO THE LIGHTS. SYSTEM CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001053100212 20010531 00212 NM 2001 5 31 DLM88010708 1 20010503 A 2760 5951789503 ROLLER DOUG MD88 MD88 3023688 NM CONTROL LEVER MISSING A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 907DE 53416 WHEN PERFORMING T/O WARNING CHECK PRIOR TO T/O THE AUTOBRAKES AURAL WARNING SOUNDED AND COULD NOT BE SILENCED. T/S AND FOUND ROLLER MISSING FROM SPEEDBRAKE CTRL LEVER ARMING SWITCH PACK ON PEDESTAL. REMOVED AND REPLACED SAME PER M/M. PER F ADJ TEST PER M/M FUNCT CK OK. PERF DFGC RTS 1-2 BOTH PASS OK. AUTOSPOILER SYST CKS OK. 2 L 7 2 4F RT A6WE 2001053100213 20010531 00213 NM 2001 5 31 DLM88010709 1 20010426 A 4920 38005041 TURBINE DOUG MD88 MD88 3023688 NM APU FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 907DE 12200 0 53416 P80131 APU FAILED IN FLIGHT, WOULD NOT RESTART ON GROUND. REPLACED SPEED SENSOR AND CONTROLLER, NO HELP. APU HANGS AT 20 PERC ENT WITH SPARKS OUT OF TAILPIPE SUSPECT TURBINE FAILURE. REMOVED AND REPLACED APU ASSY PER M/M. OPS / LK CK OK. MCO/P LAC REMOVED. 2 L 7 2 4F RT A6WE 2001053100214 20010531 00214 WP 2001 5 31 01FDEA00347 1 20010512 A 5313 ADA7020537 LONGERON DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 304FE 46992 INNER GRANULAR CORROSION DEVELOPING INSIDE LONGERON 44L APPROX 7 STA 1126 AS VIEWED INSIDE CTR ASSY COMPT BELOW WORK STE PS ON LT SIDE OF CAC ACCESS DOOR. *S/D* CLEAN AND TREATED 44L PER SRM 51-21-01. INSTALL NEW LONGERON SPLICE PER EA 8- 5311-53297. 2 L 7 3 4F RT A22WE 2001053100215 20010531 00215 WP 2001 5 31 NACA20010023 1 20010515 A 5330 SKIN DOUG DC6 DC6A 3021706 WP FUSELAGE CORRODED A NACA K NONE O OTHER IN INSP/MAINT 1 AL 03 1377K 44596 LT FUSELAGE STA 260 STRINGER 14, SKIN SURFACE CORROSION (SKIN APPEARS TO BE LIFING). OPENED UP DAMAGED AREA, CLEANED OU T CORROSION, REMOVED DAMAGED SKIN SECTION. ACID ETCHED AND ALODINED IAW DC-6 MM SRM. FABBED FILLER AND DOUBLER USING 2 024-T3 .040 ALUMINUM, PRIMED, PAINTED AND INSTALLED WITH AN470AD-4 RIVETS, RESTORED FINISH. 2 L 7 4 4R 6A3 2001053100216 20010531 00216 NM 2001 5 31 SWAA011475 1 20010518 A 3350 BR2013 TRACK BOEING 737 7377H4 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 701GS 27836 EEPLS TRACK LOOSE AT ROW 1. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001053100217 20010531 00217 NM 2001 5 31 DL78K010711 1 20010503 A 3320 335140035 BALLAST BOEING 737 737832 13844CF NM CABIN FAULTY A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 3733Z 30539 IMMEDIATELY AFTER T/O, RECEIVED REPORT OF SMOKE IN THE CABIN FROM F/A CREW. ALSO NOTICED A DISTINCTIVE SMELL LIKE BURNE D TOAST IN COCKPIT. RETURNED TO BOS TO LAND. FOUND CEILING LIGHT AT 10 DEF WITH BLOWN FUSE. REPLACED LIGHT ASSY. RAN ENGINES AT IDLE AND POWER PACKS ON, NO SMELL OR SMOKE. 2 L 7 2 4F RT A16WE 2001053100218 20010531 00218 NM 2001 5 31 DL757010712 1 20010503 A 5330 143N36503 SKIN BOEING 757 757232 1384965 NM FUSELAGE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 637DL 23760 THE FUSELAGE SKIN WAS FOUND WITH A DEEP GOUGE AT THE SKIN BUTT JOINT AT FS 780 NEAR STRINGER 18L. THE GOUGE WAS REMOVED WITH A 3.5 X 1 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 380515-14, REV A. 2 L 7 2 4F RT A2NM 2001053100219 20010531 00219 NM 2001 5 31 DL757010713 1 20010503 A 5330 146N35318 SKIN BOEING 757 757232 1384965 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 637DL 23760 WHILE ACCOMPLISHING A DOUBLER MODIFICATION TO THE SKIN CUTOUT FOR THE LOWER AFT VHF ANTENNA AT FS 1473 & RBL 3.2, AN EX ISTING REPAIR DOUBLER WAS FOUND. THE EXISTING REPAIR WAS REMOVED AN THE ANTENNA CUTOUT INCREASED TO REMOVE THE PREVI OUS REPAIR FASTENER LOCATIONS. AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER WERE INSTALLED PER ER/A 380557-14, REV BTO REPA IR THE AREA. 2 L 7 2 4F RT A2NM 2001053100220 20010531 00220 NM 2001 5 31 SWAA011481 1 20010519 A 5330 65C35794 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001053100221 20010531 00221 WP 2001 5 31 ZW0A0101801 1 20010508 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 904TW 49156 DURING CHECK-C MAINT FOUND CORROSION ON NUMBER 1 CHAIR TRACK, STA 1174 TO 1250. INSTALLED NEW TRACK AT STA 1174 TO 1250 PER SRM 53-05, FIG 4. 2 L 7 2 4F A6WE 2001053100222 20010531 00222 WP 2001 5 31 ZW0A0101802 1 20010514 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND CABIN ENTRY BRACKET CORRODED AT STA 160 TO 194, IN LINE WITH NUMBER 1 CHAIR TRACK. FABRICATE D NEW FLOOR SUPPORT BRACKET PER SAMPLE AND SPM 6-70-01. PRIMED AND PAINTED PER SRM 51-10-3. INSTALLED RIVETS PER SRM 5 1-30-2. 2 L 7 2 4F RT A6WE 2001053100223 20010531 00223 WP 2001 5 31 ZW0A0101803 1 20010514 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 924TW 49100 DURING CHECK-C MAINT INNER GRANNULAR CORROSION WAS FOUND ON FLOOR SUPPORT 4 INCHES FROM RT SIDE OF FUSELAGE, STA 1338. CUT OUT CORRODED WEB, SANDED, CLEANED AND PRIMED PER SRM 51-10-2A AND 51-10-03. WEB REPAIR PER SRM 51-70-4, FIG 2 AND S RM 51-30-4 AND 51-30-3. 2 L 7 2 4F A6WE 2001053100224 20010531 00224 WP 2001 5 31 ZW0A0101804 1 20010510 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 924TW 49100 DURING CHECK-C MAINT FOUND FLOOR SUPPORT CRACKED IN MID CARGO COMPT, STA 598 AND LONGERON 27L. REPAIRED PART PER SSRM 5 3-00-106. INSTALLED PER SRM 51-30-02. 2 L 7 2 4F A6WE 2001053100225 20010531 00225 WP 2001 5 31 ZW0A0101805 1 20010509 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 924TW 49100 DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT BL 45, STA 160 TO 200. MADE NEW FLOOR SUPPORT FROM EXTRUSION. INSTALLED WITH RIVETS PER SRM 51-30-02. PAINTED PER SRM 51-10-03. 2 L 7 2 4F A6WE 2001053100226 20010531 00226 WP 2001 5 31 ZW0A0101806 1 20010509 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 924TW 49100 DURING CHECK-C MAINT IN FWD CARGO COMPT, FOUND CORROSION IN BOTTOM ANGLE OF FORMER, STA 446, JUST ABOVE LONGERON 28R. 2 L 7 2 4F A6WE 2001053100227 20010531 00227 WP 2001 5 31 ZW0A0101807 1 20010510 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 924TW 49100 DURING CHECK-C MAINT IN THE FWD CARGO COMPT AT LONGERON 28R AND BETWEEN STA 427 AND 465, FOUND CORROSION ON CARGO FLOOR SUPPORT. 2 L 7 2 4F A6WE 2001053100228 20010531 00228 WP 2001 5 31 ZW0A0101808 1 20010511 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 924TW 49100 DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 200 FROM BL 9R TO BL 46R. FOUND FLOOR SUPPORT CORRODED BEY OND LIMITS. FABRICATED NEW SUPPORT. 2 L 7 2 4F A6WE 2001053100229 20010531 00229 WP 2001 5 31 ZW0A0101811 1 20010511 A 5320 BRACKET DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 924TW 49100 DURING CHECK-C MAINT IN THE AFT FUSELAGE, FOUND CRACKED BRACKET BELOW END OF LONGERON 18R, CANT 1463. FABRICATED NEW BR ACKET PER SRM 53-14-4 FIG 3, AND SAMPLE CRACKED BRACKET. 2 L 7 2 4F A6WE 2001053100230 20010531 00230 WP 2001 5 31 ZW0A0101812 1 20010513 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 924TW 49100 DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR SUPPORT AT STA 160 TO 200, LBL 44 IN AND 56 INCHES. REPLACED FLOOR SUPPORT PER SPM 6-70-01. FASTENERS INSTALLED PER SRM 51-30-02 AND 51-30-5. 2 L 7 2 4F A6WE 2001053100231 20010531 00231 WP 2001 5 31 ZW0A0101813 1 20010513 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 924TW 49100 DURING CHECK-C MAINT BETWEEN STA 636 AND 693, AND LONGERON 29R THE FLOOR SUPPORT HAD CORROSION AND ELONGATED HOLES. REP LACED FLOOR SUPPORT PER SPM 6-70-01. INSTALLED BOLTS PER SRM 51-30-02, AND RIVETS PER SRM 51-30-02. 2 L 7 2 4F A6WE 2001053100232 20010531 00232 WP 2001 5 31 ZW0A0101814 1 20010514 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 924TW 49100 DURING CHECK-C MAINT IN THE AFT CABIN FOUND CORROSION ON NUMBER 2 CHAIR TRACK BETWEEN STA 1155 THRU 1182. REPLACED SEAT TRACK PER SRM 53-05, FIG 4C SHEET 1, STA 1030 TO 1203. 2 L 7 2 4F A6WE 2001053100233 20010531 00233 WP 2001 5 31 ZW0A0101815 1 20010514 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 924TW 49100 DURING CHECK-C MAINT IN THE AFT CABIN, FOUND CORROSION ON NUMBER 2 CHAIR TRACK AT STA 1155 THRU 1230, OUTBOARD SIDE FLOO R PANEL MOUNT HOLE. REPLACED SEAT TRACK PER SRM 53-05,FIG 4F SHEET 1 FROM STA 1030 TO 1203. 2 L 7 2 4F A6WE 2001053100234 20010531 00234 WP 2001 5 31 ZW0A0101816 1 20010514 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 907TW 49165 DURING CHECK-C MAINT FOUND CRACK IN LONGERON 4L, INBOARD SIDE AT FASTENER, STA 160. REPLACED DAMAGED PORTION OF LONGERO N WITH NEW. INSTALLED LONGERON SPLICE PER SRM 53-02, FIG 18. SHIMMED LONGERON AT STA 160 AS NECESSARY. 2 L 7 2 4F A6WE 2001053100235 20010531 00235 WP 2001 5 31 AT0100149 1 20010422 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 811AT 47285 FOUND FLOOR SUPPORT CRACKED AT BS 813. WELDED FLOOR SUPPORT AT BS 813 IAW EA 12-5321-29-C1362. 2 L 7 2 4F A6WE 2001053100236 20010531 00236 WP 2001 5 31 AT010147 1 20010422 A 5311 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 811AT 47285 FOUND AFT CARGO COMPARTMENT FRAME AT BS 917 CORRODED. REMOVED CORRODED SECTION, FABRICATED AND INSTALLED REPAIR SECTION S IAW DC9 SRM 53-03. 2 L 7 2 4F A6WE 2001053100237 20010531 00237 NM 2001 5 31 CALA0100461 1 20010516 A 5330 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70330 23460 INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN AND INTERIOR SUPPORT FOR NR 3 VHF ANTENNA BETWEEN STA 727D AND 727E, BL 0. REPAIRED IAW SRM 53-00-01. 2 L 7 2 4F RT A16WE 2001053100238 20010531 00238 NM 2001 5 31 DLM11010775 1 20010514 A 2497 PS5750305 WIRE DOUG MD11 MD11 3023602 NM SEAT CHAFED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 801DE 48472 SEATS 1CG 2 CG AND 3CG INOP ELECTRICALLY FOUND POWER CABLE AND EMPOWERMENT CABLE CHAFED AND SIGNS OF ACRING. REPLACED CABLE. 2 L 7 3 4F RT A22WE 2001053100239 20010531 00239 NM 2001 5 31 DL757010776 1 20010515 A 3350 CONNECTOR BOEING 757 757232 1384965 NM EXTERIOR LIGHT DISCONNECTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 634DL 23615 EXTERIOR EMERGENCY LIGHT AFT OF R-1 DOOR WILL NOT TEST OR ILLUMINATE. REMOVED PART OF GALLEY AND GAINED ACCESS TO BACK OF THE EMERGENCY LIGHT. FOUND PLUGS D4474 AND D4476 DISCONNECTED. RECONNECTED BOTH PLUGS AND LIGHT OPER IS NORMAL. PL ACED GALLEY BACK IN PLACE. 2 L 7 2 4F RT A2NM 2001053100240 20010531 00240 NM 2001 5 31 DL72S010778 1 20010515 A 5310 651751738 BEAM BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 THE RT TORQUE BOX FOR THE AFT VENTRAL STAIRWAY OPENING WAS FOUND WITH A TYPICAL CRACK IN THE UPPER HORIZONTAL BEAM AT F S 1263. THE CRACK IS TYPICAL OF BAC S/B 727-53-0129. THE CRACKED PART WAS REMOVED AND REPLACED WITH A NEW PART PER THE REQUIREMENTS OF THE S/B AND PER ER/A 380826-14AD. 2 L 7 3 4F A3WE 2001053100241 20010531 00241 NE 2001 5 31 DL72S010780 2 20010516 A 7261 JT8D15AHK LINE BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE LOOSE A DALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 531DA 66843 21814 695307 DURING CRUISE AND DESCENT NR 2 ENG OIL QTY SLOWLY DECREASED FROM 3.2 TO 0 GAL. OIL TEMP AND PRESS IN GREEN ARC. ON FIN ALOIL PRESS BEGAN TO FLUC AND DROPPED OUT OF GREEN W/LOW OIL PRESS LIGHT ILLUM. IN FLT SHUTDOWN CK COMPLETED. REPLACED MAIN OIL FILTER. INSPECTED FILTER AND CHIP DETECTOR PER WINDMILL INSP, BOTH OK. FOUND OIL FILTER DIFF PRESS SW LINES LOOSE/ LEAKING. SECURED LINES. RAN ENG, LEAK CHECK GOOD. 2 L 7 3 4F 4 F A3WE E2EA 2001053100242 20010531 00242 NE 2001 5 31 DL757010781 2 20010516 A 7261 PW2037RTC ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 LEAKING A DALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 27 684DA 35706 27104 716316 FLT 1041 ATL-ONT AT 250 KTS AT APPROX FL 250 HAD LEFT ENG OIL PRESS EICAS MSG AND DISCRETE LIGHT. OIL QTY IND ZERO. PR ESS CONTINUED TO DROP AND OIL TEMP IN RED WARNING AREA. S/D END PER POM PROCEDURE. WINDMILL TIME APPROX 10 MINUTES. CREW BELIEVES OIL PRESS IND 0 DURING WINDMILL BUT IS UNSURE. REMOVED FLT DATA RECORDER FOR READOUT CONFIRMATION OF PARA METERS. CONTRACT MTC REPORTS ENG WET UNDER REVERSER HALVES. PENDING FLT DATA REPORTS LAX MTC WILL T/S. 2 L 7 2 4F 4 F RT A2NM E17NE 2001053100243 20010531 00243 NM 2001 5 31 DLM88010782 1 20010516 A 3610 99193 BLEED VALVE DOUG MD88 MD88 3023688 NM BLEED AIR LEAKING A DALA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 SO 27 913DL 49544 ON T/O AFTER PASSING 1000 FT AGL TAIL COMPARTMENT TEMP HIGH MESSAGE ILLUMINATED ON AOP. FOLLOWED ABNORMAL PROCEDURE IN POM AND ISLOATED RT PACK OFF AND MSG WENT OUT. MESSAGE RE-ILLUMINATED WITH PWR UP AND CLIMBING THUR 240. REPLACED RIGH T CROSS-BLEED VALVE AND CLAMPS. RAN ENGINE TO TAKEOFF POWER AND CHECKS OK PER PFHB. PRESSURIZED AIRCRAFT, LEAK CK''D D UCTING, OPERATED PACKS AND ALL CKS OK. 2 L 7 2 4F RT A6WE 2001053100244 20010531 00244 NM 2001 5 31 DL72L010783 1 20010516 A 5313 STRINGER BOEING 727 727232 1384082 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 506DA 21308 FOUND ON B2 LETTER CK CORROSION STR 26L STA 464. REPAIRED PER SRM 53-10-3. 2 L 7 3 4F A3WE 2001053100245 20010531 00245 NM 2001 5 31 DL72S010784 1 20010516 A 3350 1102837 LIGHT BOEING 727 727232 1384082 NM AIRSTAIR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 529DA 21703 AIRSTAIR LIGHT INOP. REPLACED LIGHT ASSY. 2 L 7 3 4F A3WE 2001053100246 20010531 00246 NM 2001 5 31 DL73S010785 1 20010517 A 5551 ATTACH FITTING BOEING 737 737232 1384475 NM HORIZ STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 323DL 23095 CORROSION WAS FOUND ON THE LT AND RT HORIZONTAL STABILIZER ATTACH FITTINGS. DAMAGE WAS REMOVED FROM THE FACES AND BORE S, OVERSIZED BUSHINGS INSTALLED PER ERA 397579-14 AT HMV. 2 L 7 2 4F RT A16WE 2001053100247 20010531 00247 NM 2001 5 31 DL72L010787 1 20010517 A 5311 65175061 FRAME BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 506DA 21308 THE INNER CHORD OF THE FS 1303 FRAME WAS FOUND WITH A 2 INCH LONG CRACK IN THE AFT FLANGE OF THE CHORD. THE CRACK WAS A T A HYDRAULIC LINE CLAMP LOCATION JUST ABOVE THE RT AFT VENTRAL STAIRWAY TORQUE BOX ASSY. THE FLANGE WAS TRIMMED TO REM OVE THE CRACK AND AN ALUMINUM REPAIR ANGLE INSTALLED PER ER/A 380851-14, REV A. 2 L 7 3 4F A3WE 2001053100248 20010531 00248 NM 2001 5 31 DLM88010788 1 20010517 A 2910 LINE DOUG MD88 MD88 3023688 NM HYD SYSTEM LOOSE A DALA K NONE K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 918DL 49583 LEFT HYD QTY DECREASED TO 3 QTS CLIMBING THRU 17K. TURNED OFF LEFT ENG HYD PUMP AND QTY INCREASED TO 15 QTS. ON FINAL W/ LEFT ENG PUMP AND XFER PUMP ON LEFT HYD QTY AND PRESS WENT TO 0. MTC NOTED EMPTY RESERVOIR. FOUND T/R CNTRL VLV L INE LEAKING. SECURED SAME. LEAK CHECK OK. 2 L 7 2 4F RT A6WE 2001053100249 20010531 00249 EU 2001 5 31 01FDEA00371 1 20010518 A 2130 CONTROLLER AIRBUS 310 A310222 3930315 EU CABIN PRESSURE INOPERATIVE A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 419FE 345 CABIN PRESS INOP. 2 L 7 2 4F RT A35EU 2001053100250 20010531 00250 WP 2001 5 31 01FDEA00370 1 20010517 A 3260 TARGET DOUG DC10 DC1010 3022110 WP LT MLG BROKEN A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 368FE 46606 LMG WOULD NOT RETRACT, BOTH IND WERE RED. REMOVED AND REPLACED TARGET. OK FOR SERVICE. 2 L 7 3 4F A22WE 2001070200030 20010702 00030 NM 2001 7 2 01FDEA00373 1 20010516 A 5531 65168164 SPAR BOEING 727 727233 138408A NM VERTICAL STAB CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 276FE 22041 VERTICAL STAB, RT STR 7 MID SPAR CHORD IS CHAFED 3 inches IN FRONT OF SLIDING SEAL. *S/D* Removed and replaced PER FEDE X SRM 55-30-3 FIG 3, FEDEX EA 7-5530-54061. 2 L 7 3 4F RT A3WE 2001070200031 20010702 00031 NM 2001 7 2 01FDEA00374 1 20010516 A 5531 65165163 SPAR BOEING 727 727233 138408A NM VERTICAL STAB CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 276FE 22041 VERTICAL STAB LT STR 7, MID SPAR CHORD IS CHAFED 3 inches IN FRONT OF SLIDING SEAL. *S/D* Removed and replaced PER FEDE X SRM 55-30-6 FIG 3, FEDEX EA 7-5530-54061. 2 L 7 3 4F RT A3WE 2001053100251 20010531 00251 WP 2001 5 31 MWEA010769 1 20010517 A 5751 9957571504 SKIN DOUG DC9 DC932 3022066 WP AILERON DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 RIGHT AILERON UPPER SURFACE HAS DENT. EVALUATE AND REPAIR. 2 L 7 2 4F A6WE 2001053100252 20010531 00252 WP 2001 5 31 MWEA010770 1 20010517 A 5751 9957571503 SKIN DOUG DC9 DC932 3022066 WP AILERON DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 LEFT AILERON UPPER SURFACE HAS DENT. EVALUATE AND REPAIR. 2 L 7 2 4F A6WE 2001053100253 20010531 00253 EU 2001 5 31 QXEA0100711 1 20010515 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 492US 11159 GEG- BOTH EMERGENCY EXIT SIGNS AT ROW 8 INOPERATIVE. REPLACED BOTH EXIT SIGNS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETU RNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001053100258 20010531 00258 WP 2001 5 31 MWEA010771 1 20010517 A 5751 9957571503 SKIN DOUG DC9 DC932 3022066 WP AILERON DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 LEFT AILERON UPPER SURFACE HAS DENT. EVALUATE AND REPAIR. 2 L 7 2 4F A6WE 2001053100259 20010531 00259 WP 2001 5 31 CALA0100469 1 20010517 A 5347 SEAT TRACK DOUG DC10 DC1030 3023501 WP FUSLEAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12061 47851 INSPECTION FOUND SEAT TRACK CORRODED AT STA Y = 2000-2007, X = 90L. THE SEAT TRACK WAS REPAIRED IAW SRM 53-70-00, FIGUR E 5 AND ECRA 5100-01844. 2 L 7 3 4F A22WE 2001053100260 20010531 00260 WP 2001 5 31 CALA0100470 1 20010517 A 5320 FLOOR SUPPORT DOUG DC10 DC1030 3023501 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12061 47851 INSPECTION FOUND A 6 INCH CRACK IN CENTER CARGO FLOOR SUPPORT FLANGE AT STA 1601, X = 18R. THE FLOOR SUPPORT WAS REMOVE D AND A NEW SUPPORT WAS INSTALLED IAW SRM 53-30-1 AND GMM 10-900-01. 2 L 7 3 4F A22WE 2001053100261 20010531 00261 WP 2001 5 31 CALA0100472 1 20010518 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND CABIN LT O/B FLOOR PANEL DELAMINATED AT FS 1155. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INSTA LLED IAW ECRA 5320-01265 AND ECRA 5100-01844. 2 L 7 2 4F A6WE 2001053100262 20010531 00262 WP 2001 5 31 CALA0100473 1 20010518 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND CABIN RIGHT I/B FLOOR PANEL GOUGED AT FS 946. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLE D IAW ECRA 5320-01265 AND ECRA 5100-01844. 2 L 7 2 4F A6WE 2001053100263 20010531 00263 WP 2001 5 31 CALA0100474 1 20010518 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND CABIN LEFT I/B FLOOR PANEL CRACKED IN TWO PLACES AT FS 313. THE FLOOR PANEL WAS REMOVED AND A NEW PANE L WAS INSTALLED IAW ECRA 5320-01265, ECRA 5100-01844, AND SRM 51-30-1. 2 L 7 2 4F A6WE 2001053100264 20010531 00264 WP 2001 5 31 CALA0100475 1 20010518 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND CABIN RIGHT I/B FLOOR PANEL DELAMINATED AT FS 466. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INS TALLED IAW ECRA 5320-01265, ECRA 5100-01844, AND SRM 51-30-1. 2 L 7 2 4F A6WE 2001053100265 20010531 00265 NE 2001 5 31 RAIA00105011 2 20010517 A 7412 4300212 EXCITER JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 552HK 14859 41057 76093 7104-STL-RIGHT ENGINE WOULD NOT START. MAINTENANCE INSPECTED AND REPLACED RIGHT ENGINE EXCITER BOX. 2 L 7 2 4T 4 T RT A41NM E18NE 2001053100269 20010531 00269 NM 2001 5 31 C8GA20010010 1 20010515 A 2612 FIRE WARNING BOEING 727 727223 1384074 NM COCKPIT FALSE ACTIVATION A C8GA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SO 15 898AA 22014 FLT 740 FROM TOL TO MCI. IN CRUISE, AT APPROXIMATELY 126 MILES FROM MCI, THE APU FIRE LIGHT CAME ON. ACCOMPLISHED APU FIRE CHECKLIST IAW AOM. AIRCRAFT CONTINUED TO MCI AND LANDED WITHOUT INCIDENT. INVESTIGATION FOUND THAT HEAVY RAIN IN TOL DURING CARGO LOADING INDUCED A FALSE APU FIRE WARNING INDICATION. THE APU FIRE BOTTLE WAS REPLACED IAW 26-23-1 AND APU SYSTEMS OPS CKECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2001053100270 20010531 00270 NM 2001 5 31 PCAA0105042 1 20010517 A 3244 H31X97513 TIRE DHAV DHC8 DHC8102 2809003 NM LT MLG FLAT A PCAA K NONE O OTHER CL CLIMB 1 EA 13 827EX 18966 225 390 FLIGHT 3535 PIT-BGM. LEFT INBOARD MAIN TIRE WENT FLAT AFTER TAKEOFF. EMERGENCY DECLARED. AIRCRAFT LANDED IN BGM WITHO UT FURTHER INCIDENT. MAINTENANCE REPLACED INBOARD LEFT AND OUTBOARD LEFT MAIN WHEEL/TIRE ASSEMBLIES, AND PERFORMED SPEC IAL INSPECTION FOR TIRE BURST AND EXCESSIVE BREAKING IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL. NO DEFEC TS FOUND. 2 H 7 2 4T RT A13NM 2001053100271 20010531 00271 NM 2001 5 31 SWAA011398 1 20010509 A 5330 6545765 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 353, BETWEEN STR 7R & 8R, BS 429, BETWEEN STR 5R & 6R AND BS 440, BETWEEN STR 5R & 6R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001053100272 20010531 00272 SO 2001 5 31 SWIA972572 1 20010509 A 5246 DOOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE SERVICE DOOR UNLATCHED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 301YV 120301 SERVICE DOOR AND MAP DOORS LIGHT ILLUMINATED SHORTLY AFTER DEPARTURE. RETURNED TO THE FIELD. INBOARD FUEL SERVICE DOOR FORWARD FASTENER CAME UNLATCHED. LATCHED DOORS. OPS CHECK GOOD FOR SECURITY. 2 L 7 2 4T 4 T RT A31SO E20NE 2001053100273 20010531 00273 EU 2001 5 31 QXEA0100704 1 20010512 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - UPON INSPECTION, FOUND STRINGER INBOARD OF THE AIR CYCLE MACHINE INLET CRACKED. REPAIRED IN ACCORDANCE WITH FOKKE R STRUCTERAL REPAIR MANUAL. COMPLIED WITH REQUIRED INSPECTION BUY BACK. CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001053100274 20010531 00274 EU 2001 5 31 QXEA0100705 1 20010513 A 5753 SKIN FOKKER F28 F28MK4000 4990810 EU T/E FLAP DAMAGED A QXEA K NONE O OTHER NR NOT REPORTED 1 NM 09 498US 11181 PDX - FLIGHT CREW REPORTED SMALL HOLE AT INBOARD SECTION OF RIGHT WING FLAP. REPAIRED HOLE AS PER FOKKER STRUCTURAL REP AIR MANUAL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001053100275 20010531 00275 WP 2001 5 31 MWEA010756 1 20010515 A 5230 59101573 SKIN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 AFT CARGO DOOR SKIN HAS A CRACK LOCATED AT LOWER FORWARD CORNER. STOP DRILLED CRACK, FABRICATED, LOCATED, DRILLED AND I NSTALLED DOUBLER AND SHIMS. 2 L 7 2 4F A6WE 2001053100276 20010531 00276 WP 2001 5 31 MWEA010763 1 20010515 A 5347 9957871 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 CAPTAINS INBOARD AFT SEAT TRACK IS WORN AT STOP PIN HOLES AND INBOARD UPPER EDGE. REMOVED SEAT TRACK, LOCATED AND DRILL ED REPAIR STRAP, REMOVED DAMAGE FROM UPPER CAP, INSTALLED REPAIR STRAP AND SEAT TRACK. 2 L 7 2 4F A6WE 2001053100277 20010531 00277 WP 2001 5 31 ZW0A0102001 1 20010518 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 969TW 53619 THE FORWARD ENTRY DOOR PORTABLE EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE LIGHT ASSEMBLY. CHECK-C 7-28-00 JFK. 2 L 7 2 4F RT A6WE 2001053100278 20010531 00278 WP 2001 5 31 ZW0A0102002 1 20010520 A 3350 58222 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 923TW 49379 THE EGRESS LIGHTS WERE INOPERATIVE FROM ROW 1 TO 10, AND ROW 18 TO 22. REPLACED THE BATTERY PACK FOR ROW 1 TO 10, AND R EPAIRED A BROKEN WIRE FOR ROW 18 TO 22. CHECK-C 6-9-00 JFK. 2 L 7 2 4F RT A6WE 2001053100279 20010531 00279 WP 2001 5 31 ZW0A0102003 1 20010519 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 965TW 53615 THE OVERWING EMERGENCY EXIT SIGN WAS MISSING AT SEAT 21A, THE FWD ENTRANCE DOOR PORTABLE EMERGENCY LIGHT WAS INOPERATIVE , AND THE THE RED EGRESS LIGHT WAS INOPERATIVE AT THE FWD GALLEY AND AFT LAVATORY. INSTALLED EXIT MARKER P/N 0105612-00 1, REPLACED 2 DISCHARGED BATTERIES P/N 408822-101 FOR THE PORTABLE LIGHT, AND REPLACED THE BURNED OUT LAMP P/N 7732 FOR EACH EGRESS LIGHT POSITIONS. CHECK-C 5-3-01 STL. 2 L 7 2 4F RT A6WE 2001053100280 20010531 00280 WP 2001 5 31 ZW0A0102004 1 20010517 A 3350 0105606005 SOCKET DOUG DC9 DC983 3022083 WP AIRSTAIRS BROKEN A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9401W 53137 THE EGRESS LAMP BASE WAS BROKEN IN THE AFT AIRSTAIRS MIDDLE POSITION. REPLACED THE EGRESS BASE. CHECK-C 3-3-01 MCI. 2 L 7 2 4F RT A6WE 2001053100281 20010531 00281 NM 2001 5 31 ZW0A0102005 1 20010521 A 3350 CONNECTOR BOEING 757 7572Q8 1384972 NM CABIN DIRTY A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 703TW 27620 THE EGRESS LIGHT AT SEAT ROW 1 WAS INOPERATIVE. CLEANED AND RE-INSTALLED THE LAMP CONNECTOR. CHECK-C 4-12-01 LAX. 2 L 7 2 4F RT A2NM 2001053100282 20010531 00282 WP 2001 5 31 ZW0A0102006 1 20010517 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 907TW 49165 DURING CHECK-C MAINT THE FLOOR SUPPORT HAD CORROSION AT STA 1165, LBL 52 TO 55, AND AT STA 1143, LBL 52 TO 55. AT BOTH LOCATIONS, NEW PART PRIMED AND PAINTED PER SRM 51-10-3 AND INSTALLED ON MEMBRANE PER SRM 51-30-05. 2 L 7 2 4F A6WE 2001053100283 20010531 00283 WP 2001 5 31 ZW0A0102007 1 20010517 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 924TW 49100 DURING CHECK-C MAINT FOUND FLOOR SUPPORT CORRODED FROM BLR 9 TO BLR 45, STA 180. FABRICATED FLOOR SUPPORT AND INSTALLED SUPPORT USING RIVETS PER SRM 51-30-2. 2 L 7 2 4F A6WE 2001053100284 20010531 00284 NM 2001 5 31 AWXA0001742 1 20010514 A 5320 BAC1496377 FLOOR SUPPORT BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 AFT CARGO FLOOR SUPPORT Z-ANGLE RBL 20 STA 727-767 FOUND CRACKED DURING CORROSION REMOVAL. FABBED AND INSTALLED NEW FLO OR SUPPORT Z-ANGLE IAW SRM 53-60-53. 2 L 7 2 4F RT A16WE 2001053100285 20010531 00285 NM 2001 5 31 AWXA0001744 1 20010514 A 5315 BAC1506210 FLOORBEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 CORROSION ON STA 1016 FLOORBEAM FROM LBL 12 - RBL 35. REPAIRED FLOORBEAM IAW AWA ER 03-5310-01118-JS1. 2 L 7 2 4F RT A16WE 2001053100286 20010531 00286 NM 2001 5 31 AWXA0001750 1 20010514 A 5320 INTERCOSTAL BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 INTERCOSTAL AT BS 178 BLKHD RHS AT WL 207 IS CRACKED. REPAIRED IAW AWA ER 03-5313-01119-BA1. 2 L 7 2 4F RT A16WE 2001053100287 20010531 00287 NM 2001 5 31 AWXA0001751 1 20010514 A 5313 STRINGER BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 STR 27L STA 967 CRACKED WHERE ATTACHED TO TIE CLIPC: REMOVED DMGD AREA OF STR; FABBED REPAIR PARTS; TREATED, PRIMED, TOP COATED AND INSTALLED REPAIR PARTS IAW SRM 53-00-03. 2 L 7 2 4F RT A16WE 2001053100288 20010531 00288 WP 2001 5 31 MWEA010766 1 20010517 A 5730 59127351 SKIN DOUG DC9 DC932 3022066 WP LT WING DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 LEFT WING UPPER SURFACE AT STATION XRS 477 REQUIRES REPAIR OR REPLACEMENT. HOT BOND CORE AND SKIN. 2 L 7 2 4F A6WE 2001053100289 20010531 00289 WP 2001 5 31 MWEA010767 1 20010517 A 5522 5910410503 SKIN DOUG DC9 DC932 3022066 WP ELEVATOR DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 LEFT ELEVATOR HAS TWO DENTS THAT REQUIRED SPACING IS NOT MET. FABRICATED TWO ROW ROUND PATCH AND INSTALLED. 2 L 7 2 4F A6WE 2001053100290 20010531 00290 WP 2001 5 31 AT0100132 1 20010422 A 5313 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 811AT 47285 FOUND CORROSION ON LONGERON 28R AND SPLICE AT BS 218-237. REMOVED AND REPLACED SECTION OF LONGERON 28R AND SPLICE. 2 L 7 2 4F A6WE 2001053100291 20010531 00291 WP 2001 5 31 01FDEA00339 1 20010507 A 5743 ARB06421 FITTING DOUG DC10 DC1030F 3023504 WP RT MLG CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 304FE 46992 REF EO 8-5740-7-4312 RT MLG RETRACT CYLINDER SUPPORT FRAME HAS A CRACK IND AT FWD FLANGE FROM TOP TO RADIUS. *S/D* REM OVED AND REPLACED RT MLG RETRACT CYLINDER SUPPORT PER EO 8-5740-7-4312 PART 3. 2 L 7 3 4F RT A22WE 2001053100292 20010531 00292 NE 2001 5 31 F3LA200100064 2 20010513 A 7261 OIL FILTER BOEING 737 7372Y5 1384554 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE DIRTY A F3LA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 NM 03 921WA 36497 35 23039 702762 FLIGHT CREW REPORTED NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED AT CRUISE. NR 1 ENGINE WAS SHUT DOWN IN FLIGHT AND AN EMERGENCY WAS DECLARED. AIRCRAFT DIVERTED TO MCI FROM ITS PLANNED DESTINATION OF MDW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NR 1 ENGINE OIL FILTER PER MM 79-35-0, PERFORMED BREATHER PRESSURE TEST PER MM 79-21-0 AND OPS CHEC KED OK. 2 L 7 2 4U 4 F RT A16WE E2EA 2001053100293 20010531 00293 WP 2001 5 31 AT0100141 1 20010424 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP COCKPIT CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 811AT 47285 FOUND FORWARD COCKPIT FLOORBOARD CORRODED AT BS 148-160. REMOVED AND REPLACED FLOORBOARD IAW DC9 SRM 51-10-3, 51-10 FIG URE 1, 53-05 FIGURE 1 AND 53-21 FIGURE 2. 2 L 7 2 4F A6WE 2001053100294 20010531 00294 WP 2001 5 31 ZW0A0101907 1 20010515 A 5320 SPLICE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT IN THE AFT CARGO COMPT, FACTORY SPLICE HAD A 6 INCH LONG CRACK AT LONGERON 27L, BETWEEN STA 1193 AN D 1212. REPLACED SPLICE PER SRM 53-02, FIG 14 PAGE 35. INSTALLED FASTENERS PER SRM 51-30-01. 2 L 7 2 4F RT A6WE 2001053100297 20010531 00297 EU 2001 5 31 MALA010493 1 20010516 A 3097 WIRE SAAB SF340 340B 7860101 EU ANTI-ICE SYS CHAFED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 451XJ 451 RT INTAKE CAUTION LIGHT CAME ON AFTER TURNING ON. LIGHT CYCLED ON/OFF EVERY FIVE SECONDS. TEST OK ON THE GROUND BEFORE TAKEOFF. AIR RETURN TO DTW. MAINTENANCE FOUND CHAFED WIRE ON THE RT INTAKE EXHAUST NOZZLE. REPAIRED WIRE, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2001053100298 20010531 00298 NM 2001 5 31 SCNA01034 1 20010415 A 3397 WIRE BOEING 737 7378Q8 13844BX NM CABIN BROKEN A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 802SY 30628 DURING A MAINTENANCE LINE CHECK THE EMERGENCY PATH LIGHTING INOPERATIVE ON THE FORWARD COAT CLOSET AFT LIGHTING. REPAIR ED BROKEN WIRE BEHIND THE EMERGENCY LIGHT ASSEMBLY. 2 L 7 2 4F RT A16WE 2001053100299 20010531 00299 NM 2001 5 31 SCNA01035 1 20010502 A 3350 LENS BOEING 727 7272J4 1384006 NM CABIN LOOSE A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 290SC 20764 DURING A MAINTENANCE LINE CHECK THE AFT RIGHT OVERWING EMERGENCY EXIT SIGN LENS WAS FOUND TO BE LOOSE. REMOVED AND REPL ACED AFT RIGHT OVERWING EMERGENCY EXIT SIGN (20DEF). 2 L 7 3 4F RT A3WE 2001053100300 20010531 00300 NM 2001 5 31 SCNA01036 1 20010515 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 282SC 22558 DURING A MAINTENANCE LINE CHECK THE LEFT FORWARD OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED T HE BATTERY PACK. 2 L 7 3 4F A3WE 2001053100301 20010531 00301 SO 2001 5 31 C2XA01CL111 1 20010516 A 2120 UNKNOWN EMB 135 EMB135ER 3260203 SO CABIN ODOR A C2XA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 14505 145192 CLE FLIGHT 3966 THE CREW REPORTED STRONG SMOKE ODOR INFLIGHT. ODOR WENT AWAY AFTER CREW TURNED OFF PACK NR 1. THE AIR CRAFT LANDED IN CLEVELAND WITHOUT FURTHER PROBLEM. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF NR1 BLEED SYSTEM NO DEFE CTS WERE NOTED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2001053100302 20010531 00302 NM 2001 5 31 AWXA0001757 1 20010516 A 5320 143N536672 FLOOR SUPPORT BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 23566 FWD CARGO PIT FLOOR SUB STRUCTURE FLOOR SUPPORT FOR FLOOR BOARD RT SIDE RBL 25 FS 590-650 HAS CORROSION. REMOVED AND RE PLACED DAMAGED FLOOR SUPPORT IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2001053100303 20010531 00303 NM 2001 5 31 ERKR200100128 1 20010515 A 5522 65B0577117 SKIN BOEING 747 747128 1384894 NM ELEVATOR CRACKED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 REPAIR- RIGHT INBD ELEVATOR LEADING EDGE, UPPER SURFACE ELEV STA 77-86. AN EXISTING REPAIR WAS FOUND OUTBOARD OF THE CR ACK LOCATION. THE EXISTING REPAIR WAS REMOVED TO INCORPORATE THE NEW CRACK INTO THE REPAIR. UPON DISASSEMBLY IT WAS FO UND THAT THE PRIOR REPAIR AREA WAS A RESULT OF DEFORMATION AND CRACK DAMAGE (CRACK WAS STOPPED DRILLED). REPAIR OF THIS AREA AND THE NEW CRACK IS ACCOMPLISHED BY TRIMMING OUT THE DAMAGED AREA AND INSTALLING A NEW INTERNAL DOUBLER. THIS DO UBLER REPLACES THE OLD REPAIR DOUBLER AND THE ORIGINAL PRODUCTION DOUBLER (65B05771-17) PER ECRA 3203-55-035-2. 2 L 7 4 4F A20WE 2001053100304 20010531 00304 NM 2001 5 31 AWXA0001728 1 20010514 A 5510 65C2514411 HINGE FITTING BOEING 737 7373G7 1384595 NM HORIZ STAB DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 LEFT HORIZONTAL STABILIZER OUTBOARD RIB NR 6 HINGE MOUNT HAS 2 ELONGATED HOLES. REPAIRED HINGE FITTING IAW AWA ER 03-55 10-01124-TB1. 2 L 7 2 4F RT A16WE 2001053100305 20010531 00305 NM 2001 5 31 AWXA0001730 1 20010514 A 5310 65C25230 SHEAR TIE BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 FS 727E BETWEEN STR 28L & 238R CORROSION ON FRAME SHEAR TIE. REPAIRED IAW AWA ER 03-5300-01130-JS1. 2 L 7 2 4F RT A16WE 2001053100306 20010531 00306 NM 2001 5 31 AWXA0001731 1 20010514 A 5311 651630087 FRAME BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 FWD BLKHD STA 178 RT SIDE CHORD CRACKED WL 207. REMOVED AND REPLACED SIDE CHORD IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001053100307 20010531 00307 NM 2001 5 31 AWXA0001732 1 20010514 A 5311 65630086 FRAME BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 FWD BLKHD STA 178 LT SIDE CHORD CRACKED AT WL 207. REMOVED AND REPLACED CHORD IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001053100308 20010531 00308 NM 2001 5 31 AWXA0001733 1 20010514 A 5315 FLOORBEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 FLOORBEAM AT STA 294.5 HAS CORROSION. REMOVED AND REPLACED FLOORBEAM IAW SRM 53-10-08 AND 53-10-51. 2 L 7 2 4F RT A16WE 2001053100309 20010531 00309 NM 2001 5 31 AWXA0001734 1 20010514 A 5312 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 FWD BLKHD AT STA 178 HAS A CRACK INDICATION AT APPROX RBL 10 WL 234 FWD EXTERIOR SURFACE. REPAIRED IAW SRM 53-10-08 FIG 209 DETAIL 2. 2 L 7 2 4F RT A16WE 2001053100310 20010531 00310 NM 2001 5 31 AWXA0001736 1 20010514 A 5315 FLOORBEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 STA 1006 FLOORBEAM HAS CORROSION RBL 14-28. REPAIRED FLOORBEAM IAW SRM 53-00-51 FIG 203. 2 L 7 2 4F RT A16WE 2001053100311 20010531 00311 NM 2001 5 31 AWXA0001739 1 20010514 A 5311 FRAME BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 BS 178 BLKHD VERT CHORD AT LBL 5.7 HAS CRACK APPROX 2.5 INCHES ON INBOARD FLANGE AT WL 181. CUT OUT DAMAGE; FABBED REPA IR PARTS; TREATED AND PRIMED; TOPCOATED AND INSTALLED IAW SRM 51-30-01, 51-20-01 AND 53-10-08. 2 L 7 2 4F RT A16WE 2001053100312 20010531 00312 NM 2001 5 31 AWXA0001740 1 20010514 A 5310 CREASE BEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 LT CREASE BEAM CORRODED STA 967-1006. REMOVED AND REPLACED IAW SRM 53-40-02. 2 L 7 2 4F RT A16WE 2001053100313 20010531 00313 NM 2001 5 31 AWXA0001741 1 20010514 A 5347 SEAT TRACK BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 CRACK APPROX 1 INCH ON SEAT TRACK T-EXTRUSION FLANGE EDGE TO FASTENER HOLE AT STA 727B LBL 45. REMOVED, FABBED AND INST ALLED NEW REPAIR STRAP IAW AWA ER 03-5310-01110-551. 2 L 7 2 4F RT A16WE 2001053100314 20010531 00314 NM 2001 5 31 DL76L010717 1 20010506 A 2761 GASKET BOEING 767 767332 1382001 NM SPOILER ACTUATOR BLOWN A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 187DN 27582 CTR HYD SYS QTY LOSS. FOUND BLOWN SEAL ON NR 4 SPOILER ACTUATOR. REPLACED GASKET. LEAK CHECKS OK. SERVICED HYD SYS T O FULL. 2 L 7 2 4F RT A1NM 2001053100315 20010531 00315 NM 2001 5 31 DL76K010718 1 20010506 A 3350 767 LIGHT BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 171DZ 29690 ON S/C FOUND BOTH MOST AFT EMERGENCY LIGHTS EXTERIOR LT HAND SIDE INOP. RELAMPED BOTH AFT LT EMERGENCY LIGHTS PER MM. 2 L 7 2 4F RT A1NM 2001053100316 20010531 00316 2001 5 31 DL72S010719 4 20010505 A 2397 WIRE 174660N2 BOEING 727 727232 1384082 NM MICROPHONE BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 524DA 09764 21584 CAPT O2 MASK MICROPHONE WIRE BROKEN. REPLACED MASK. 2 L 7 3 4F A3WE 2001053100317 20010531 00317 NM 2001 5 31 DL76L010720 1 20010505 A 2121 FAN BOEING 767 767332 1382001 NM CABIN DEFECTIVE A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 182DN 25987 BURNING SMELL IN CABIN. AT DEPARTURE BURNING SMELL IN CABIN. 02 FAULT TRACED TO RT RECIRC FAN, CB PULLED, FWD TO MCO A ND PLACARD PER MEL 21-25-01A. 2 L 7 2 4F RT A1NM 2001053100318 20010531 00318 NM 2001 5 31 DL73E010721 1 20010505 A 5330 65458576 SKIN BOEING 737 7372J8 1384489 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 235WA 22859 A 1.2 INCH LONG CRACK WAS FOUND IN THE BONDED SKIN ASSY AT THE LOWER FWD CORNER OF THE AFT GALLEY DOOR CUTOUT. THE CRA CK WAS REMOVED WITH A CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER PER E R/A 380732-14, REV B. 2 L 7 2 4F RT A16WE 2001053100319 20010531 00319 NM 2001 5 31 AWXA0001743 1 20010514 A 5312 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 CORROSION ON APB INTERIOR SKIN AND LAP SEAM STIFFENERS AFT STA 1016 BL 0 AND BELLY. REPAIRED APB SKIN IAW S/B 737-53A10 75 AND DWG 65C28106 IAW AWA ER 03-5312-01120-ES1. 2 L 7 2 4F RT A16WE 2001053100320 20010531 00320 NM 2001 5 31 AWXA0001745 1 20010514 A 5313 BAC1498162 STRINGER BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 CORROSION ON STR SIDES 27L AT STA 1006. BLENDED OUT CORROSION - FOUND OUT OF LIMITS; FABBED REPAIR PARTS; HEAT TREATED; TREATED AND PRIMED PARTS AND INSTALLED REPAIR PARTS IAW SRM 53-00-03. 2 L 7 2 4F RT A16WE 2001053100321 20010531 00321 NM 2001 5 31 AWXA0001746 1 20010514 A 5330 SKIN BOEING 737 73733A 1384673 NM FUSELAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 FUSELAGE SKIN STA 187 WL 195 LBL 32 ELONGATED HOLE FOUND ON INTERCOSTAL REMOVAL. REPAIRED SKIN IAW SRM 53-00-01 FIG 201 . 2 L 7 2 4F RT A16WE 2001053100322 20010531 00322 NM 2001 5 31 AWXA0001747 1 20010514 A 5315 BAC1506210 FLOORBEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 FLOORBEAM AT STA 986.5 HAS SURFACE CORROSION. REPAIRED IAW AWA ER 03-5305-01117-DD3. 2 L 7 2 4F RT A16WE 2001053100323 20010531 00323 NM 2001 5 31 AWXA0001748 1 20010514 A 5311 FRAME BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 CORROSION AND BULGED BETWEEN FRAME STRUCTURES AT INTERIOR BELLY OF FWD SIDE APB FRAME AND CIRCUM FRAME STA 1016 LBL 3 - RBL 3. REMOVED AND REPLACED STRINGER END FITTINGS AND FRAME T-CHORD SPLICE PNL IAW SRM 53-80-08 AND 51-40-2. 2 L 7 2 4F RT A16WE 2001053100324 20010531 00324 NM 2001 5 31 AWXA0001749 1 20010514 A 5312 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 WEB AT WL 207 HAS CRACK IN WEB AT BS 179.5 APPROX .300 INCH LONG. REMOVED, FABBED AND REPLACED DAMAGED WEB IAW S/B 737- 53A1173 AND DWG 45833. 2 L 7 2 4F RT A16WE 2001053100325 20010531 00325 NM 2001 5 31 AWXA0001752 1 20010514 A 5312 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 RHS INTERCOSTAL ATWL 207 HAS CRACK IN WEB AT BS 179.5 APPROX 1.25 INCH LONG. REMOVED DAMAGED WEB; FABBED AND INSTALLED NEW WEB IAW DWG 65-45833 AND SRM 51-40-2. 2 L 7 2 4F RT A16WE 2001053100326 20010531 00326 NM 2001 5 31 AWXA0001753 1 20010514 A 5320 FLOOR SUPPORT BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 CORROSION ON FLOOR SUPPORT STA 1006-1016 RBL 38. FABBED NEW FLOOR SUPPORT IAW SRM 53-60-51. 2 L 7 2 4F RT A16WE 2001053100327 20010531 00327 NM 2001 5 31 AWXA0001754 1 20010514 A 5310 PRESSURE PANEL BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 A .75 INCH LONG CRACK COMING OUT OF FASTENER HEAD AT NLG BEAM WEB ADJACENT TO NLG WARNING HORN BRACKET MOUNT BS 225. RE PAIRED IAW AWA ER 03-5310-01119-SS2. 2 L 7 2 4F RT A16WE 2001053100328 20010531 00328 NM 2001 5 31 AWXA0001755 1 20010514 A 5320 65524577 PAN BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 SURFACE CORROSION ON THE PLATE UNDER THE AFT LAV TANKS FWD FROM FWD FACE OF APB TO STA 1006. REMOVED AND INSTALLED NEW AFT FLOOR PANS IAW DWG 65-46812. 2 L 7 2 4F RT A16WE 2001053100329 20010531 00329 NM 2001 5 31 AWXA0001756 1 20010514 A 5320 146N5318 WEB BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 23566 MAIN CABIN FLOORD STRUCTURE AFT DECK SHEAR WEB HAS CORROSION AT STA 1710-1720 RBL 65-60 AND RBL 6.5-17. CUT OUT DAMAGED AREA; FABBED AND INSTALLED FILLER, DOUBLER AND SHIMS IAW SRM 53-60-51 FIG 203, AFT CABIN DECK PLATE IAW SRM 51-40-02 AN D SRM 53-60-51 FIG 203. 2 L 7 2 4F RT A2NM 2001053100330 20010531 00330 WP 2001 5 31 ZW0A0101810 1 20010511 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 924TW 49100 DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR SUPPORT FROM STA 160 TO 200, 8 INCHES LBL. REPLACED PART PER SPM 6- 70-01, USING SRM 51-30-1 TO INSTALL HARDWARE. 2 L 7 2 4F A6WE 2001053100331 20010531 00331 NM 2001 5 31 SWAA011417 1 20010512 A 5320 6516300 WEB BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED D-CHECK, FOUND WEBS CRACKED AT BS 294.5, STR 12L & 15L. REPAIRED WEBS PER SRM. 2 L 7 2 4F A16WE 2001053100332 20010531 00332 NM 2001 5 31 SWAA011421 1 20010511 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 637, STR 8L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001053100333 20010531 00333 NM 2001 5 31 SWAA011422 1 20010512 A 5312 6516300 BULKHEAD BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 522SW 26564 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 6, WL 213. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001053100334 20010531 00334 NM 2001 5 31 SWAA011423 1 20010512 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 745, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001053100335 20010531 00335 NM 2001 5 31 SWAA011424 1 20010511 A 5315 65C33722 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD IS CRACKED AT BS 947.5, LBL 55. REPAIRED CHORD PER BFG ER. 2 L 7 2 4F A16WE 2001053100336 20010531 00336 NM 2001 5 31 SWAA011426 1 20010512 A 5330 65C36183 SKIN BOEING 737 737317 138447P NM FUSRLAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING WALKAROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT UPPER RIGHT CORNER OF AFT CARGO BIN OPENING. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001053100337 20010531 00337 NM 2001 5 31 SWAA011428 1 20010511 A 5330 65C36183 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 507SW 24184 DURING WALKAROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 847, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001053100338 20010531 00338 NM 2001 5 31 SWAA011437 1 20010512 A 5330 6545772 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR UPPER HINGE CUT. REPAIRED SKIN PER MM. 2 L 7 2 4F RT A16WE 2001053100339 20010531 00339 NM 2001 5 31 SWAA011438 1 20010512 A 5330 6552988 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 900, STR 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001053100340 20010531 00340 NM 2001 5 31 SWAA011439 1 20010513 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 900, STR 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001053100341 20010531 00341 NM 2001 5 31 SWAA011441 1 20010514 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER 7L CRACKED AT BS 1010. REPAIRED STR PER SRM. 2 L 7 2 4F A16WE 2001053100342 20010531 00342 NM 2001 5 31 SWAA011443 1 20010513 A 5312 6516300 BULKHEAD BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 522SW 26564 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 5, WL 213. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001053100343 20010531 00343 NM 2001 5 31 SWAA011444 1 20010511 A 5311 6545877 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 3L. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2001053100344 20010531 00344 NM 2001 5 31 SWAA011445 1 20010514 A 5310 6546569 SHEAR TIE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED, BS 1121, BETWEEN STR 2R AND 3R. REMOVED AND REPLACED SHEAR TIE PER S RM. 2 L 7 2 4F A16WE 2001053100345 20010531 00345 NM 2001 5 31 SWAA011446 1 20010512 A 5330 65C35775 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING WALKAROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT STR 19R, BS 767, BS 759 AND BS 727D+3. REPAIRED SKIN PER S RM. 2 L 7 2 4F RT A16WE 2001053100346 20010531 00346 NM 2001 5 31 SWAA011447 1 20010512 A 5330 65C35794 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING WALKAROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 722, STR 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001053100347 20010531 00347 NM 2001 5 31 SWAA011448 1 20010512 A 5330 6552988 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING WALKAROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 963, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001053100348 20010531 00348 WP 2001 5 31 AT0100158 1 20010421 A 5320 THRESHOLD DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 803AT 47261 FOUND AFT ENTRANCE THRESHOLD CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 51-10-02, 51-10-03, 51 -10-04, 51-30, 51-30-02, 51-30-05, AND 51-30-08. 2 L 7 2 4F A6WE 2001053100349 20010531 00349 WP 2001 5 31 AT0100159 1 20010415 A 5342 ATTACH ANGLE DOUG DC9 DC932 3022066 WP VERTICAL STAB CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 803AT 47261 FOUND DORSAL FIN ATTACH ANGLES CRACKED BEYOND LIMITS. REPLACED ATTACH ANGLES IAW EO 09-5350-29-E1645. 2 L 7 2 4F A6WE 2001053100350 20010531 00350 WP 2001 5 31 AT0100160 1 20010416 A 5313 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 803AT 47261 FOUND LONGERON 11 FRAME AT BS 598 CRACKED. INSTALLED REPAIR IAW REO L00432. 2 L 7 2 4F A6WE 2001053100351 20010531 00351 WP 2001 5 31 AT0100161 1 20010507 A 5310 STOP FITTING DOUG DC9 DC932 3022066 WP DOOR FRAME CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 848AT 47559 FOUND MAIN CABIN DOOR STOP CRACKED. REPAIRED CRACK IAW EO 09-5310-E1703. 2 L 7 2 4F A6WE 2001053100352 20010531 00352 WP 2001 5 31 AT0100162 1 20010408 A 5310 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 803AT 47261 FOUND AFT STAIRWAY DOOR FRAME CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED ATTACH ANGLE REPAIR IAW DC9 SRM 53-01 FI G 1, 51-30, 51-10-03, 51-10-02, 51-10-04 AND 51-30-01. 2 L 7 2 4F A6WE 2001053100353 20010531 00353 WP 2001 5 31 AT0100163 1 20010501 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 848AT 47559 FOUND SEAT TRACK AT BS 200 - 965 CORRODED BEYOND LIMITS. REPLACED SEAT TRACKS IAW DC9 MM 55-20-01. 2 L 7 2 4F A6WE 2001053100354 20010531 00354 WP 2001 5 31 AT0100165 1 20010503 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 848AT 47559 FOUND FUSELAGE CORRODED AT BS 714-759. BLENDED CORROSION IAW REO L00437. 2 L 7 2 4F A6WE 2001053100355 20010531 00355 WP 2001 5 31 AT0100166 1 20010424 A 5347 CARGO TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 848AT 47559 FOUND FORWARD CARGO PIT TRACK EXFOLIATED BEYOND LIMITS. REPLACED TRACK IAW DC9 SRM 51-10-04, 51-30-01, AND 53-21-01. 2 L 7 2 4F A6WE 2001053100356 20010531 00356 WP 2001 5 31 AT0100167 1 20010503 A 5320 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 848AT 47559 FOUND CABIN FLOOR SUPPORT WEB CORRODED BEYOND LIMITS AT BS 160-218 LBL 55-RBL 55. FABRICATED AND INSTALLED REPAIR DOUBL ER IAW DC9 SRM 53-01 FIG 1, 53-01 FIG 4, AND 51-10-03. 2 L 7 2 4F A6WE 2001053100357 20010531 00357 WP 2001 5 31 AT0100168 1 20010507 A 5240 DOOR DOUG DC9 DC932 3022066 WP LAV SERVICE DR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 848AT 47559 FOUND LEFT AFT LAV SERVICE DOOR CORRODED BEYOND LIMITS. REPLACED DOOR PANEL IAW DC9 SRM 51-30-01. 2 L 7 2 4F A6WE 2001053100358 20010531 00358 WP 2001 5 31 AT0100169 1 20010503 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 848AT 47559 FOUND CABIN FLOOR SUPPORT ANGLES CORRODED BEYOND LIMITS AT BS 200 LBL 0-55. FABRICATED AND INSTALLED NEW FLOOR SUPPORTS IAW DC9 SRM 51-10-02, 51-10-03, 51-10-04, 51-30-01, AND 51-30-05. 2 L 7 2 4F A6WE 2001053100359 20010531 00359 WP 2001 5 31 AT0100143 1 20010421 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 811AT 47285 FOUND 2 CRACKS AT LEFT FUSELAGE NOSE UPPERS SKIN AT BS 69.5. CUT OUT CRACKS, HFEC INSPECTED, FABRICATED, TREATED, PRIME D AND INSTALLED DOUBLERS IAW DC9 SRM 51-10-2, DWG SRO9530239. 2 L 7 2 4F A6WE 2001053100360 20010531 00360 WP 2001 5 31 AT0100144 1 20010422 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 811AT 47285 FOUND AFT CARGO COMPARTMENT FLOOR SUPPORT CRACKED AT BS 889. REMOVED SUPPORTS, WELDED REPAIRS AND REINSTALLED IAW EA 12 -15321-29-C1362 AND DC9 SRM 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 2001053100361 20010531 00361 WP 2001 5 31 AT0100145 1 20010423 A 5320 BRACKET DOUG DC9 DC932 3022066 WP FWD LAVATORY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 811AT 47285 FOUND FORWARD LAVATORY BRACKETS CORRODED. REMOVED CORROSION, FORMED REPAIR BRACKETS, HEAT TREATED, DRILLED, TRIMMED, TR EATED, PRIMED AND INSTALLED IAW DCI SRM 53-01 FIGURE 1, 51-10-2, 51-10-4, 51-10-3, 51-30-2. 2 L 7 2 4F A6WE 2001053100362 20010531 00362 WP 2001 5 31 AT0100146 1 20010424 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 811AT 47285 FOUND FORWARD CABIN FLOOR SUPPORT CORRODED AT BS 140 - 168. REMOVED CORROSION, FABRICATED NEW SECTION AND INSTALLED IAW DC9 SRM 51-10-2, 53-11-1 FIGURE 13, 51-30-8, 51-10-3. 2 L 7 2 4F A6WE 2001053100363 20010531 00363 WP 2001 5 31 AT0100148 1 20010427 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSLEAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 811AT 47285 FOUND AFT CARGO COMPARTMENT FLOOR SUPPORT CRACKED AT BS 851. REMOVED FLOOR SUPPORT, WELDED REPAIR AND REINSTALLED IAW E A 12-5321-29-C1362, DC9 SRM 51-30-0, 51-30-2, 51-10-3. 2 L 7 2 4F A6WE 2001053100366 20010531 00366 WP 2001 5 31 AT0100152 1 20010424 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 811AT 47285 FOUND FORWARD CABIN FLOOR SUPPORT ANGLE CORRODED AT BS 160. REMOVED CORROSION AND ANGLE, FABRICATED AND INSTALLED REPAI R ANGLE IAW DC9 SRM 51-01 FIGURE 1, 51-30-2, 51-30-5, 51-10-4, 53-11 FIGURE 13, 51-10-3. 2 L 7 2 4F A6WE 2001053100367 20010531 00367 WP 2001 5 31 AT0100153 1 20010423 A 5752 005126 TRIM TAB DOUG DC9 DC932 3022066 WP AILERON CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 811AT 47285 FOUND RIGHT WING AILERON TRIM TAB UPPER AND LOWER SURFACE CORRODED AND DELAMINATED. REMOVED AND REPLACED RIGHT AILERON TRIM TAB IAW DC9 MM 27-10-5. 2 L 7 2 4F A6WE 2001053100368 20010531 00368 NM 2001 5 31 AWXA0001758 1 20010516 A 5311 FRAME BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 BS 178 BLKHD VERT CHORD AT LBL 5.7 HAS AN APPROX 2.5 INCH CRACK ON INBD FLANGE AT WL 181. REMOVED PARTS FOR ACCESS; CUT OUT DAMAGE; FABBED REPAIR PARTS, FILLERS, ANGLE AND STRAPS; INSTALLED, TREATED, PRIMED AND TOP COATED IAW SRM 51-30-01 AND 51-20-01 AND 53-10-08. 2 L 7 2 4F RT A16WE 2001053100369 20010531 00369 NM 2001 5 31 CALA0100458 1 20010515 A 5711 SPAR BOEING 737 7373T0 1384582 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70330 23460 INSPECTION FOUND A 0.1 INCH CRACK IN RT REAR SPAR UPPER CHORD AT RT MLG BEAM O/B END AFT SPAR FITTING ATTACH AREA. THE CRACK WAS REPAIRED IAW ECRA 5743-01033. A DIP WAS ISSUED TO REINSPECT THE AREA AT 3,000 FLIGHT CYCLE INTERVALS. 2 L 7 2 4F RT A16WE 2001053100370 20010531 00370 NM 2001 5 31 CALA0100459 1 20010516 A 5330 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70330 23460 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 1008, S16L. THE DENTED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SR M 53-00-01, FIGURE 202. 2 L 7 2 4F RT A16WE 2001053100371 20010531 00371 NM 2001 5 31 CALA0100460 1 20010516 A 5330 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70330 23460 INSPECTION FOUND A SMALL CREASE IN FUSELAGE SKIN AT STA 1042, S13L. A DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 20 2 AND 51-70. 2 L 7 2 4F RT A16WE 2001053100372 20010531 00372 WP 2001 5 31 CALA0100462 1 20010516 A 5320 FLOOR SUPPORT DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12061 47851 INSPECTION FOUND J-SECTION FLOOR SUPPORT CORRODED AT STA Y = 824, X = 50 TO 74. THE FLOOR SUPPORT WAS REPLACED IAW SRM 53-14-01 AND GMM 10-900-01. 2 L 7 3 4F A22WE 2001053100373 20010531 00373 WP 2001 5 31 CALA0100463 1 20010516 A 5310 SHEAR TIE DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12061 47851 INSPECTION FOUND SHEAR CLEAT CORRODED AT STA 1902 BETWEEN LONGERONS 51R AND 50R AND BETWEEN LONGERONS 48L AND 47L. THE SHEAR CLEATS WERE REMOVED AND NEW SHEAR CLEATS WERE INSTALLED IAW SRM 51-30-01 AND GMM 10-900-01. 2 L 7 3 4F A22WE 2001053100374 20010531 00374 WP 2001 5 31 CALA0100464 1 20010516 A 5310 SHEAR TIE DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12061 47851 INSPECTION FOUND SHEAR CLEAT CORRODED AT STA 1841 BETWEEN LONGERON 48R AND 47R. THE SHEAR CLEAT WAS REMOVED AND A NEW S HEAR CLEAT WAS INSTALLED IAW SRM 51-30-01 AND GMM 10-900-01. 2 L 7 3 4F A22WE 2001053100375 20010531 00375 WP 2001 5 31 CALA0100465 1 20010516 A 5310 SHEAR TIE DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12061 47851 INSPECTION FOUND SHEAR CLEAT IN CENTER CARGO BILGE CORRODED AT STA 1801 BETWEEN LONGERON 49L AND 49R. THE SHEAR CLEAT W AS REMOVED AND A NEW SHEAR CLEAT WAS INSTALLED IAW SRM 51-30-01 AND GMM 10-900-01. 2 L 7 3 4F A22WE 2001053100376 20010531 00376 WP 2001 5 31 CALA0100467 1 20010516 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND A 2 INCH CRACK AND LOOSE SCREWS IN CABIN LT O/B FLOOR PANEL AT FS 313. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-05, FIGURE 1, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 2001053100377 20010531 00377 NM 2001 5 31 UPS01435910 1 20010506 A 5320 SUPPORT BOEING 747 747123 1384873 NM FAIRING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:C-2 BODY FAIRING SUPPORT STA 880 RBL 0 - 60 FOUND CORRODED. BODY FAIRING SUPPORT REPAIR AT BS 880 BL 0 TO RBL 40 PER SRM 53-50-04 FIG 2. 2 L 7 4 4F A20WE 2001053100378 20010531 00378 NM 2001 5 31 SWAA011389 1 20010509 A 5311 65C33722 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D-CHECK, FOUND COMPRESSION CHORDS CRACKED AT BS 727A, STR 18L &18R. REPLACED CHORDS PER SWA ACO. 2 L 7 2 4F A16WE 2001053100379 20010531 00379 NM 2001 5 31 SWAA011391 1 20010509 A 5310 6545409 PRESSURE PANEL BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 663, LBL 39. REPAIRED WEB PER SWA RA. 2 L 7 2 4F RT A16WE 2001053100380 20010531 00380 NM 2001 5 31 SWAA011399 1 20010510 A 5330 6545871 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SVC DOOR SKIN CUTOUT, LOWER AFT CORNER. REPAIRED SKIN P ER MM. 2 L 7 2 4F RT A16WE 2001053100381 20010531 00381 NM 2001 5 31 SWAA011401 1 20010510 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D-CHECK, FOUND STRINGERS CRACKED BETWEEN BS 1006 & BS 1016, STR 5R, AND AT BS 867, STR 11L. REPAIRED S TRINGS PER SRM. 2 L 7 2 4F A16WE 2001053100382 20010531 00382 NM 2001 5 31 SWAA011402 1 20010510 A 5315 6546804 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, RBL 50 TO LBL 50. REPAIRED PER SWA TI. 2 L 7 2 4F A16WE 2001053100383 20010531 00383 WP 2001 5 31 CALA0100471 1 20010518 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND A CREASE IN EXTERNAL RT FUSELAGE SKIN AT FS 522, LONGERONS 16L AND 18L. DOUBLERS WERE INSTALLED IAW SR M 53-04, FIGURE 38, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 2001053100384 20010531 00384 NM 2001 5 31 DL72S010737 1 20010509 A 5720 STIFFENER BOEING 727 727232 1384082 NM WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 519DA 21470 A 2 INCH CRACK WING L/E SPAR STIFFENER I/B TRACK NR 2 SLAT I/B STIFFENER. REPLACED ANGLE PER M/M 57-200021-8. 2 L 7 3 4F A3WE 2001053100385 20010531 00385 NM 2001 5 31 DL72S010749 1 20010511 A 5532 SKIN BOEING 727 727232 1384082 NM VERTICAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 546DA 22677 THE LT SKIN OF THE VERTICAL STABILIZER WAS FOUND WITH A .75 INCH CRACK EMANATING FROM AN ATTACHMENT TO THE REAR SPAR. T HE CRACK WAS LOCATED JUST ABOVE THE FUSELAGE SKIN INTERFACE. THE CRACK WAS STOP DRILLED AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 380797-14, REV B. 2 L 7 3 4F A3WE 2001053100386 20010531 00386 NE 2001 5 31 DLM88010759 2 20010513 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 FAILED A DALA A UNSCHED LANDING R X PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT CL CLIMB 1 SO 27 905DL 32305 0 49536 718151 DURING CLIMB THROUGH FL300, ENGINE STALLED AND FLAMED-OUT UPON INITIAL POWER REDUCTION. THE ENGINE WAS BOROSCOPED ON 05 /12/01 FOR ANOTHER STALL AT ALTITUDE. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A6WE E9NE 2001053100387 20010531 00387 NE 2001 5 31 DLM88010767 2 20010513 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 DAMAGED A DALA C ABORTED TAKEOFF M OVER TEMP TO TAKEOFF 1 SO 27 991DL 31416 0 53343 718224 ABORTED TAKEOFF 100 KIAS LEFT ENG EGT PEAK 610 DEGREES. MTC FOUND NR 1 ENG HAS LINER DAMAGED IN COLD STREAM AT APPROX 1 1:00 POS. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A6WE E9NE 2001053100388 20010531 00388 NM 2001 5 31 DLM88010770 1 20010514 A 2450 947F9463 BPCU DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE E/E BAY FAULTY A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 984DL 53311 718232 LT BUS POWER INTERUPTIONS AT 33000 FT. RAN AC POWER INTER- CHECKLIST. APU WAS STARTED AND EMERGENCY DECLARED AND A DES CENT INTO PHL. PHL MTC FOUND LEFT ENGINE FREQS AT 383 ON ENGINE RUN. WOULD NOT HOLD BUS WHEN LOADED DOWN. REPLACED BUSS POWER CONTROL UNIT. 2 L 7 2 4F 4 F RT A6WE E9NE 2001053100389 20010531 00389 NM 2001 5 31 DL72S010777 1 20010516 A 5330 655457023 SKIN BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 515DA 21431 THE FWD UPPER CORNER OF THE R1 DOOR CUTOUT WAS FOUND WITH A .5 INCH CRACK EMANATING FROM A FASTENER HOLE TO THE CUTOUT E DGE. THE CRACK WAS REMOVED WITH A 1 INCH TRIMOUT THROUGH THE SKIN AND BONDED DOUBLERS. THE CUTOUT WAS REPAIRED WITH A N EXTERNAL ALUMINUM DOUBLER PER ER/A 380839-14, REV A. 2 L 7 3 4F A3WE 2001053100390 20010531 00390 NM 2001 5 31 DL76P010786 1 20010516 A 2611 SA308C SMOKE DETECTOR BOEING 767 767332 1382001 NM CABIN ACTIVATED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 140LL 25988 3R, 2R, 2L SMOKE DETECTORS WENT OFF IN FLIGHT, NO SIGN OF SMOKE, LIGHT SMELL (FLIGHT ATTENDANTS DESCRIBED AS SLIGHT ELECTRICAL SMELL). RAN ALL GALLEY EQPT, TURNED ON ALL CABIN LIGHTS, RAN PACKS WITH ENG AIR DOORS CLOSED AND NO SMOK E OR ELECTRICAL SMELL IN ANY AREA. CLEANED CABIN TEMP SENSOR FILTERS, LAV VENT FILTER AND RAN ENGS TO HIGH POWER PER PF HB WITH PACKS ON. UNABLE TO DUPLICATE. REPLACED SMOKE DETECTOR. 2 L 7 2 4F RT A1NM 2001053100391 20010531 00391 NM 2001 5 31 DL76S010789 1 20010516 A 3397 WIRE BOEING 767 767332 1382001 NM CABIN SHORTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 129DL 24079 ON L/O FOUND EMERGENCY LIGHTS INOP. LEFT AND RIGHT SIDES SEAT ROW 35 AFT FLOOR TRACK LIGHTING. T/S PER WDM TRIED PWR S UPPLY, NO HELP. ISOLATED SHORT IN WIRING TO SEAT 35AB. REPAIRED SAME. 2 L 7 2 4F RT A1NM 2001053100392 20010531 00392 SO 2001 5 31 C2XA01CL112 1 20010518 A 3350 CONNECTOR EMB 145 EMB145ER SO CABIN LOOSE A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 15941 145035 CLE FLIGHT 4149 THE CREW REPORTED THE EMERGENCY AISLE PATH LIGHTING WAS INOPERATIVE AT SEATS 9-11. MAINTENANCE RESECURE D CONNECTOR ON BATTERY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001060100001 20010601 00001 2001 6 1 DHL2001745005 4 20010522 A 2210 AUTOPILOT SYS BOEING 727 727224 1384076 NM COCKPIT MALFUNCTIONED A DHLA K NONE O OTHER AP APPROACH 1 SO 01 745DH 20665 AUTOPILOT WILL NOT MAINTAIN LOCALIZER ON APPROACH BELOW 2000 FT ABOVE AIRPORT. PERFORMED OPS CHECK OF A/P NAV/LOC. CHE CKS GOOD WITH COMPANY EQUIPMENT. 2 L 7 3 4F A3WE 2001060100002 20010601 00002 2001 6 1 DHL2001707006 4 20010519 A 2211 25858043 COMPUTER BOEING 727 72722 1384002 NM AUTOPILOT SYS MALFUNCTIONED A DHLA K NONE F FLT CONT AFFECTED DE DESCENT 1 SO 01 707DH 18321 WITH AUTOPILOT IN AUTO G/S MODE, AND GLIDE SLOPE CAPTURED, THE AIRCRAFT PITCHES UP AND DOWN AND MAY OR MAY NOT RECOVER T O GLIDE PATH. REPLACED PITCH CHANNEL COMPUTER WITH A SERVICABLE UNIT IAW B727 M/M 22-11-121. CHECKS GOOD AT THIS TIME IAW B727 M/M 22-11-01. 2 L 7 3 4F A3WE 2001060100003 20010601 00003 2001 6 1 DHL2001743006 4 20010519 A 2210 AUTOPILOT SYS BOEING 727 727225 1384077 NM COCKPIT MALFUNCTIONED A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 743DH 22438 FL 330 FT MACH .80, AUTOPILOT ENGAGED. AIRCRAFT STARTED TO DUTCH ROLL, DISENGAGED AUTOPILOT. DUTCH ROLL STOPPED. NOTE D, NO RUDDER MOVEMENT. TRANSFERRED PER MEL 22-1. DMI 5665, PLACARD INSTALLED. TESTED AUTOPILOT. SYSTEM OPS CKS GOOD IAW B727 MM 22-11. THIS CLEARS DMI 5665. PLACARDS REMOVED. 2 L 7 3 4F A3WE 2001060100004 20010601 00004 2001 6 1 DHL2001701011 4 20010518 A 2211 25858051 COMPUTER BOEING 727 72730C 1384009 NM AUTOPILOT SYS FAULTY A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 701DH 19011 HDG MODE AIRCRAFT BANKS GREATER THAN 30 DEG ANGLE OF BANK, TRACKS 5 DEG LEFT OF SELECTED HDG, AND OVERSHOOTS IN TURNS TO THE SELECTED HDG BY 25 DEG. REPLACED ROLL CHANNEL (REF ITEM 1P) AND OPS CK PER B-727 MM 72-11-01. OPS CK GOOD. 2 L 7 3 4F A3WE 2001060100005 20010601 00005 2001 6 1 DHL2001807014 4 20010516 A 2210 LINKAGE DOUG DC8 DC873 302199C WP AUTOPILOT SYS JAMMED A DHLA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SO 01 807DH 45990 AUTOPILOT PITCH CONTROL IS ERRATIC IN CLIMB AND TURNS JERKS CONTROL YOKE BACK AND FORTH. FOUND JAMMED LINKAGE ABOVE SER VO MICRO-SWITCH. REMOVED AND PROPERLY REPOSITIONED LINKAGE. CLEANED CONNECTOR TO MICROSWITCH AND SERVO. OPS CK''D OK IAW MM 22-20-0. 2 L 7 4 4F RT 4A25 2001060100006 20010601 00006 2001 6 1 DHL2001807015 4 20010518 A 2215 61574317 SERVO DOUG DC8 DC873 302199C WP AUTOPILOT SYS DEFECTIVE A DHLA K NONE F FLT CONT AFFECTED CL CLIMB 1 SO 01 807DH 45990 AUTOPILOT ELEVATOR CONTROL JERKS ON CLIMBOUT AND LEVEL FLIGHT. AUTOPILOT ELEVATOR SERVO INDICATOR SHOWS CORRESPONDING M OVEMENT. REMOVED AND REPLACED ELEVATOR SERVO DRIVE IAW DHL DC-8 MM 22-10-4. OPS CK GOOD IAW MM 22-10-4. RII SERVO DRI VE INSTALLATION. 2 L 7 4 4F RT 4A25 2001060100007 20010601 00007 WP 2001 6 1 ZW0A0102101 1 20010521 A 3350 58222 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 921L 47107 THE EGRESS LIGHTS WERE INOPERATIVE IN FIRST CLASS AND PART OF COACH CABIN. REPLACED THE POWER SUPPLY. CHECK-C 8-2-00 M CI. 2 L 7 2 4F A6WE 2001060100008 20010601 00008 EU 2001 6 1 MALA010470 1 20010419 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 427 DURING C-CHECK, FOUND CORROSION AT BL 18.3 FS 294 TO STA 401. PARTIAL REPLACED SEAT TRACK AS RECOMMENDED IN SAAB STATEME NT 72SDS1560. FOR CORRECTIVE ACTION SEE CELSIUS WO 19645, TASK 1503. 2 L 7 2 4T RT A52EU 2001060100009 20010601 00009 SO 2001 6 1 SWIA972580 1 20010516 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE T/E FLAP FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 195SW 120127 CONTROL FAULT NAC 1 BAR IN FLIGHT, WOULD NOT RESET. BELOW 180 KTS WE WERE ABLE TO RESET AND USE FLAPS NORMALLY. PERFOR MED A WIPER TEST AND FOUND THE LEFT NACELLE FLAP ACTUATOR BAD. REMOVED AND REPLACED IAW AMM 27-50-09. OPS CHECK GOOD A ND PERFORMED IAW RII 27-307. P/N ON 308200-1007, S/N ON 0587, S/N OFF 0464. 2 L 7 2 4T 4 T RT A31SO E20NE 2001060100011 20010601 00011 WP 2001 6 1 ABXA010226 1 20010516 A 5330 SKIN DOUG DC8 DC861 3021952 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 847AX 54825 46031 THE FUSELAGE SKIN WAS CORRODED AND FASTENERS WERE BULGING AND MISSING AT FUSELAGE STA 50, LONGERON 34R. MAINTENANCE INS PECTED AND REPAIRED AND DEFERRED IAW ABX REA D853-41127-MR. 2 L 7 4 4F 4A25 2001060100012 20010601 00012 WP 2001 6 1 UPS01835920 1 20010517 A 2510 SEAT DOUG DC8 DC871F 302199D WP COCKPIT LOOSE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:N/A PILOT REPORT-CAPT SEAT LOOSE. *S/D* REMOVED AND REPLACED CAPTS SEAT, OPS CHECK GOOD IAW MM 25-11-0 1. 2 L 7 4 4F RT 4A25 2001060100013 20010601 00013 EU 2001 6 1 MALA010454 1 20010416 A 5260 TRACK SAAB SF340 340B 7860101 EU AIRSTAIRS CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 427 DURING C-CHECK ,AIRSTAIR TRACK CORRODED. MAINTENANCE REMOVED CORROSION FROM AIRSTAIR TRACK. NEGLIGABLE MATERIAL LOSS WI THIN LIMITS. ALODINED, PRIMED, AND PAINTED AIRSTAIR TRACK IAW SRM 51-20-05/10. 2 L 7 2 4T RT A52EU 2001060100014 20010601 00014 EU 2001 6 1 MALA010455 1 20010416 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 427 DURING C-CHECK ,CORROSION ON FLOORBOARD SUPPORT CHANNELS UNDER FLOOR PANEL 122EZ. MX BLENDED OUT CORROSION ON SUPPORT CH ANNELS ON PNLS 122EZAND 122DE. MIDDLE AND AFT CHANNELS OUT OF LIMITS. FWD CHANNEL WITHIN LIMITS. CHANNELS WERE REPLAC ED ON WO 19645 TASK 1559. 2 L 7 2 4T RT A52EU 2001060100015 20010601 00015 EU 2001 6 1 MALA010456 1 20010416 A 5347 7253721459 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 427 DURING C-CHECK ,GALLEY SEAT TRACK CORROSION. MX REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED GALLEY SEAT TRACK IAW SRM 51-40-27/21. INSTALLED NEW GALLEY SEAT TRACK P/N 7253721-459. 2 L 7 2 4T RT A52EU 2001060100016 20010601 00016 EU 2001 6 1 MALA010457 1 20010416 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 427 DURING C-CHECK ,CORROSION ON FLOOR SUPPORT CHANNEL BETWEEN FS 236 AND 258 AT LBL 18.3. MX REMOVED CORROSION ON SUPPORT C HANNEL BETWEEN STA 236-258 AT LBL 18.3. MATERIAL REMAINING WITHIN ALLOWABLE LIMITS REF SRM 51-10-10. ALODINED, PRIMED AND PAINTED AFFECTED AREA. 2 L 7 2 4T RT A52EU 2001060100017 20010601 00017 EU 2001 6 1 MALA010459 1 20010416 A 5320 ANGLE SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 427 DURING C-CHECK ,CORROSION ON UPPER ANGLE, UNDER FLOORBOARDS AT STA 258. MX REMOVED CORROSION ON UPPER ANGLE AT STA 258 B ETWEEN LBL 10 AND RBL 18 IAW SRM 51-70-40. MATERIAL REMAINING OUT OF LIMITS, REF SRM 51-10-10. 2 L 7 2 4T RT A52EU 2001060100018 20010601 00018 EU 2001 6 1 MALA010460 1 20010416 A 5320 INTERCOSTAL SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 427 DURING C-CHECK ,FOUND CORROSION ON UPPER ANGLE OF INTERCOASTAL BETWEEN STA 272-288 AT RBL 10. MX REMOVED CORROSION ON UP PER ANGLE BETWEEN STA 272-288 AT RBL 10. MATERIAL OUT OF LIMITS, REF IPM-12 FOR WORK ACCOMPLISHED. 2 L 7 2 4T RT A52EU 2001060100019 20010601 00019 EU 2001 6 1 MALA010461 1 20010416 A 5347 7253799379 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 427 DURING C-CHECK ,FOUND CARGO AREA SEAT TRACKS HAVE NICKS, SCRATCHES, GOUGES AND LIGHT CORROSION. MX REMOVED CORRODED RT, CTR AND LT CARGO SEAT TRACKS. MATERIAL REMAINING OUT OF LIMITS ON SEAT TRACKS AT LBL 18.3 AND BL 0. MATERIAL REMAINING ON SEAT TRACK AT RBL 18.3 WITHIN LIMITS. REF SRM 53-70-60, 51-10-10. 2 L 7 2 4T RT A52EU 2001060100020 20010601 00020 WP 2001 6 1 CALA0100479 1 20010519 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND CABIN RT I/B FLOOR PANEL GOUGED AT FS 1040. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-1, ECRA 5320-01265, AND 5100-01844. 2 L 7 2 4F A6WE 2001060100021 20010601 00021 WP 2001 6 1 CALA0100482 1 20010520 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND CABIN RT I/B FLOOR SUPPORT CORRODED WITH A 1.5 INCH EDGE CRACK AT FS 210. THE FLOOR SUPPORT WAS REMOVE D AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-10-3. 2 L 7 2 4F A6WE 2001060100022 20010601 00022 EU 2001 6 1 MALA010462 1 20010416 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 427 DURING C-CHECK ,FOUND CENTER SEAT TRACK AT BL 0 IS CORRODED AT THE CENTER AISLE FLOORBOARD FLANGE FROM STA 294-363. MX R EMOVED CORROSION. MATERIAL REMAINING OUT OF LIMITS REF SRM 53-70-60, 51-10-10. REPAIRED CORRODED SEAT TRACK SECTION, S EE IPM 12 FORM. 2 L 7 2 4T RT A52EU 2001060100023 20010601 00023 EU 2001 6 1 MALA010463 1 20010416 A 5347 7253799379 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 427 DURING C-CHECK, FOUND LT I/B SEAT TRACK AT LBL 18.3 IS CORRODED AT THE CENTER AISLE FLOORBOARD FLANGE FROM STA 294-376. MX REMOVED CORROSION IAW 51-21-42 MATERIAL REMAINING OUT OF LIMITS. REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK REPLACED TRACK FROM STA 294-376 AREA TO SPLICE IS 401.9 IS WITHIN ALLOWABLE LIMIT. 2 L 7 2 4T RT A52EU 2001060100024 20010601 00024 EU 2001 6 1 MALA010464 1 20010417 A 5230 DOOR SAAB SF340 340B 7860101 EU CARGO BAY DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 427 DURING C-CHECK, FOUND CARGO DOOR DENTED IN SEAL AREA AT LOWER FORWARD CORNER. MX MEASURED DENT AND FOUND TO BE OUT OF LI MITS. NDT PERFFVNDT006EC & 004UT BOND NO DELAM NO CRACKS NOTED REPAIRED DENT PER SAAB SDS001496. COMPLIED WITH CABIN PR ESSURE LEAK CHECK. 2 L 7 2 4T RT A52EU 2001060100025 20010601 00025 EU 2001 6 1 MALA010465 1 20010417 A 5320 INTERCOSTAL SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 427 DURING C-CHECK, FOUND INTERCOSTAL CORRODED AND CRACKED AT AFT END AT LBL 18 AND STA 272.0. MX FABRICATED REPAIR ANGLE AN D FILLER PER PRINCIPLES OF SRM 51-70-20, ALODINED, PRIMED AND TOPCOATED PER SRM 51-20-42/43. NO CRACKS NOTED IAW FFVNDT 006. INSTALLED REPAIR ANGLE AND FILLER IAW SRM 51-40-21 AND 23. 2 L 7 2 4T RT A52EU 2001060100026 20010601 00026 EU 2001 6 1 MALA010466 1 20010518 A 5320 SPLICE PLATE SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 427 DURING C-CHECK, FOUND FLOOR PANEL SPLICE PLATE UNDER FLOOR PANEL 122DZ HAVE CORROSION. MX REMOVED CORROSION ON SPLICE PL ATES AND FOUND THEM TO BE OUT OF LIMITS. FABRICATED NEW PLATES IAW SRM 51-40-40. ALODINED, PRIMED AND TOPCOATED IAW SR M 51-20-41/42. 2 L 7 2 4T RT A52EU 2001060100027 20010601 00027 EU 2001 6 1 MALA010467 1 20010419 A 5320 CHANNEL SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 427 DURING C-CHECK, FOUND CORROSION ON C-CHANNEL UNDER FLOOR BOARDS AT STA 258 BETWEEN LBL 10.0 AND LL 18.3. MX REMOVED C-CH ANNEL AT STA 258 BEWEEN LBL 10 AND 18.3. FABRICATED, ALODINED AND PRIMED NEW C-CHANNEL, INSTALLED NEW C-CHANNEL AT STA 258 BETWEEN LBL 10-LBL 18.3, ALODINED, PRIMED AND PAINTED. REF SAAB SRM 51-20-42/43. 2 L 7 2 4T RT A52EU 2001060100028 20010601 00028 EU 2001 6 1 MALA010469 1 20010419 A 5320 WEB SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 427 DURING C-CHECK, FOUND CORROSION ON WEB AT STA 290.0 UNDER FLOOR. MX REMOVED WEB AT STA 290, REPLACED WEB WITH NEW WEB A T STA 290, TOPCOATED WEB IAW SRM 51-20-42/43. 2 L 7 2 4T RT A52EU 2001060100029 20010601 00029 EU 2001 6 1 MALA010482 1 20010404 A 5330 DOUBLER SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 429XJ 429 FOUND DURING C-CHECK IN BNA, RT FUSELAGE HAS A GROUP OF DENTS IN THE ICE SHIELD STA 319.0 AND SL1634. MX REMOVED ICE GUA RD, DENTS ARE OUT OF LIMITS. NDT/BOND TEST PER FFVNDT006/SRM 51-10-10, SHOWS NO CRACKS OR DISBOND. FABRICATED ICE SHIE LD 3RD FROM TOP AND INSTALLED. REF SRM 53-70-10. DENTS ARE ACCEPTED AS IS REF SAAB EO 340SDS001422. 2 L 7 2 4T RT A52EU 2001070200032 20010702 00032 NM 2001 7 2 01FDEA00376 1 20010521 A 5311 6515932 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 276FE 22041 FRAME DENTED BS 580 BETWEEN STR 16 - 17R, WL 213. *S/D* Removed and replaced PER FEDEX SRM 51-40-3 FIG 1. 2 L 7 3 4F RT A3WE 2001060100030 20010601 00030 NM 2001 6 1 01FDEA00375 1 20010516 A 5330 SKIN BOEING 727 727233 138408A NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 276FE 22041 EXTERNAL FUSELAGE SKIN CREASED BS 1327, STR 17 LT 18 LT. *S/D* REMOVED, REPLACED AND FAB PER IAW FEDEX SRM 53-30-3, 51 -30-2, 51-30-5, 51-30-8 & FEDEX MM 51-21-151. 2 L 7 3 4F RT A3WE 2001060100031 20010601 00031 SO 2001 6 1 SWIA972578 1 20010516 A 3234 12038594501 CONTROL BOX EMB 120 EMB120RT SO PWA 118 PW118 NE COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 130G 120130 AFTER SELECTING GEAR UP, ALL RED AND GREEN INDICATING LIGHTS REMAINED ILLUMINATED. FOLLOWED QRH AND RECYCLED LANDING GE AR WITH SAME RESULTS. RETURNED FOR LANDING. REMOVED AND REPLACED LANDING GEAR SOLENOID VALVE. REMOVED AND REPLACED LAN DING GEAR CONTROL BOX. CYCLED GEAR 5 TIMES. OPS CHECK GOOD, BOTH CONTROLLER AND SOLENOID VALVE. OPS CHECK GOOD IAW MM 32-32-03. LEAK CHECK GOOD. BOX P/N: 120-38594-501, S/N ON: 120349, S/N OFF: 240191-310. VALVE: 18190-003, S/N O N: 343, S/N OFF: 486. 2 L 7 2 4T 4 T RT A31SO E20NE 2001060100032 20010601 00032 SO 2001 6 1 SWIA972579 1 20010514 A 2750 FLAP EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT WING MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 195SW 120127 ASYMMETRY ON FINAL WHEN FLAPS SELECTED 45. RIGHT INBOARD FLAPS DID NOT GO DOWN ALL THE WAY. AVERAGE INDICATION OF 40 D EGREES. FLAPS WOULD NOT RETRACT AFTER LANDING (THE INBOARD). RAN QRH TO RAISE FLAPS, INBOARD FLAPS NOW INOP. RERACKED FLAP COMPUTER AND CHECKED ACTUATOR CANNON PLUGS. COULD NOT DUPLICATE PROBLEM. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001060100033 20010601 00033 NM 2001 6 1 ERKR200100131 1 20010520 A 5315 65B10670 FLOORBEAM BOEING 747 747128 1384894 NM FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 3203Y 19751 REPAIR OF CANTED PRESSURE DECK AND ANGLE, STA1238 - 1265, LBL 41 - RBL 53. REPAIR OF THE CORROSION DAMAGE TO 65B07992-1 (CANTED) PRESSURE DECK BETWEEN STA 1238 AND 1265 LBL 41 TO BL 0 AND SHORT E/D COMMON TO THE 65B10670 FLOORBEAM LOWER CH ORD. CONSIST OF TRIMMING OUT THE CORROSION DAMAGE AND INSTALLING NET FIT FILLERS, EXTERNAL AND INTERNAL DOUBLERS. TRIM MING OUT THE DISCREPANT SHORT E/D HOLES, AND INSTALLATION OF A REPAIR STRAP, TEE AND FILLERS, COMMON TO THE 65B10670 FLO ORBEAM LOWER CHORD PER ECRA 3203-53-046-2 REV A. 2 L 7 4 4F A20WE 2001060100034 20010601 00034 EU 2001 6 1 MALA010472 1 20010423 A 3610 DUCT SAAB SF340 340B 7860101 EU BLEED AIR CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 427 DURING C-CHECK, COWLING 453BR NACA DUCT CRACKED ON TRAILING EDGE. ROUTED OUT DAMAGE AND ON LOWER NACA DUCT. NDTPERFFVND T006EC NO CRACKS PAST STOP. REPAIRED CRACKED NACA DUCT ON 453BR. 2 L 7 2 4T RT A52EU 2001060100035 20010601 00035 EU 2001 6 1 MALA010473 1 20010424 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 427 DURING C-CHECK, FOUND CORROSION ON LOWER FLANGES AND SIDE OF WEB AT BL 0 AT FS STA 294 TO STA 40L. MAINTENANCE REPLACED SEAT TRACK PARTIAL AS RECOMMENDED IN SAAB STATEMENT 72SDS1560. FOR CORRECTIVE ACTION SEE CELSIUS WO 19645 TASK 1504. 2 L 7 2 4T RT A52EU 2001060100036 20010601 00036 EU 2001 6 1 MALA010474 1 20010425 A 5510 STRUCTURE SAAB SF340 340B 7860101 EU HORIZ STAB DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 427 DURING C-CHECK, TOOL MARK AND/OR ELONGATED HOLE AT RT HORIZONTAL STABILIZER AT THE FORWARD SPAR. AINTENANCE COMPLIED WIT H MESABA EO AD991921-03 HORIZONTAL STAB FWD SPAR COLDWORKING. 2 L 7 2 4T RT A52EU 2001060100037 20010601 00037 EU 2001 6 1 MALA010449 1 20010413 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 427 DURING C-CHECK, GROUP OF DENTS ON RT FUSELAGE AT STA 339.0. MX FOUND DENTS OUT OF ALLOWABLE LIMITS. NDT PERFFVNDT006 EC NO CRACKS NOTED. DENTS ARE ACCEPTED AS IS REF SAAB STATEMENT 340SDS001496. 2 L 7 2 4T RT A52EU 2001060100038 20010601 00038 EU 2001 6 1 MALA010450 1 20010413 A 5330 DOUBLER SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 427 DURING C-CHECK ,FOUND TWO GROUPS OF DENTS AFT OF LT ICESHIELD AT STA 363.0. MX FOUND GROUP OF DENTS AT STA 363 BELOW WI NDOW REINFORCEMENT OUT OF ALLOWABLE LIMIT, 2ND GROUP STA 347 ARE WINTHIN ALLOWABLE LIMITS. NDT PERFFVNDT006EC NO CRACKS NOTED. DENTS ARE ACCEPTED AS IS IAW SAAB STATEMENT 340SDS001496. 2 L 7 2 4T RT A52EU 2001060100039 20010601 00039 EU 2001 6 1 MALA010451 1 20010416 A 5320 INTERCOSTAL SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 427 DURING C-CHECK ,CORROSION ON UPPER ANGLE OF INTERCOASTAL BETWEEN FS 272 AND FS 288 AT LBL10. MX REMOVED CORROSION ON UPP ER ANGLE LBL 10 BETWEEN STA 272-288. MATERIAL REMAINING WITHIN ALLOWABLE LIMITS. ALODINED, PRIMED AND PAINTED AFFECTED AREA. 2 L 7 2 4T RT A52EU 2001060100040 20010601 00040 EU 2001 6 1 MALA010452 1 20010416 A 5320 ANGLE SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 427 DURING C-CHECK ,CORROSION ON UPPER ANGLE UNDER FLOOR AT STA 272. MX REMOVED CORROSION ON UPPER ANGLE AT STA 272, MATERIA L OUT OF LIMITS. MX REMOVED UPPER ANGLE, FABRICATED NEW ANGLE, ALODINED PRIMED AND INSTALLED NEW ANGLE (FLOOR FLANGE) A T STA 272, TOPCOATED. 2 L 7 2 4T RT A52EU 2001060100041 20010601 00041 EU 2001 6 1 MALA010471 1 20010423 A 3610 DUCT SAAB SF340 340B 7860101 EU BLEED AIR CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 427 DURING C-CHECK, COWLING 453AL NACA DUCT CRACKED ON TRAILING EDGE. MAINTENANCE STOP DRILLED CRACK, NDTPERFFVNDT006 EC NO CRACKS PAST STOP. REPAIRED NACA DUCT ON 453AL REF: SB 340-54-007. 2 L 7 2 4T RT A52EU 2001060100042 20010601 00042 NE 2001 6 1 2001UALA00718 2 20010507 A 7310 ENGINE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 LEAKING A UALA A UNSCHED LANDING K J Y FLUID LOSS WARNING INDICATION ENGINE STOPPAGE CR CRUISE 1 WP 29 652UA 25390 NR 1 ENGINE SHUTDOWN DUE CONFIRMED FUEL LEAK. DIVERTED SDF. 2 L 7 2 4F 4 F RT A1NM E24NE 2001081300011 20010813 00011 NM 2001 8 13 2001UALA00719 1 20010510 A 2612 FIRE WARNING BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE COCKPIT MALFUNCTIONED A UALA K NONE N FALSE WARNING CL CLIMB 1 WP 29 7448U 21902 DURING CLIMB, THE FLIGHT CREW HEARD A FIRE WARNING BELL WITH NO INDICATION OF THE SOURCE. THE AIRCRAFT CONTINUED TO ORD. CREW REPORTED THAT ON CLIMBOUT THRU FL200, FIRE BELL SOUNDED WITH NO OTHER INDICATIONS. RESET SYS, TESTED ENG'S AND CAR GO SYS'S, ALL TESTED NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001081300012 20010813 00012 NM 2001 8 13 2001UALA00720 1 20010510 A 3350 900542U1 BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7454U 21908 RH OVER WING EMERGENCY EXIT SIGNS ARE INOPERABLE. BATTERY PACK AND CHARGER FAILED. REPLACED BATTERY PACK AND CHARGER. 2 L 7 3 4F 4 F A3WE E2EA 2001060100043 20010601 00043 NM 2001 6 1 QXEA0100773 1 20010520 A 3350 LIGHT DHAV DHC8 DHC8202 2809007 NM COCKPIT MISSING A QXEA K NONE O OTHER NR NOT REPORTED 1 NM 09 357PH 504 SEA - FLIGHT CREW REPORTED THAT THE FLIGHT COMPARTMENT EMERGENCY OVERHEAD FLOOD LIGHT WAS MISSING. REPLACED FLOOD LIGHT . 2 H 7 2 4T RT A13NM 2001060100044 20010601 00044 EU 2001 6 1 QXEA0100774 1 20010518 A 3350 XB864041 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN LOOSE A QXEA K NONE O OTHER NR NOT REPORTED 1 NM 09 479AU 11228 SEA - EXIT SIGN ON SEAT 9A WAS FOUND LOOSE. REMOVED AND REPLACED EXIT SIGN. OPERTAIONAL CHECKS GOOD. AIRCRAFT RETURNE D TO SERVICE. 2 L 7 2 4F RT A20EU 2001060100045 20010601 00045 SO 2001 6 1 C2XA01IA247 1 20010516 A 3320 LIGHT EMB 145 EMB145ER 3260211 SO LAVATORY SMOKE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 14937 145026 IAH - FLIGHT 4128, THE CREW REPORTED THAT THE LAV LIGHT EMITTED A BURNING ODOR. THE AIRCRAFT LANDED AT IAH WITHOUT INCI DENT. MAINTENANCE PLACED THE LAV ON MEL 25-60-02/6 CONTROL NUMBER 010247, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO S ERVICE. 2 L 7 2 4F RT T00011AT 2001060100046 20010601 00046 SO 2001 6 1 C2XA01IA249 1 20010518 A 3350 D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15725 120173 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOP ERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001081300013 20010813 00013 NM 2001 8 13 2001UALA00721 1 20010511 A 2530 SMOKE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE GALLEY DETECTED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7464U 21918 FORWARD GALLEY HAS ELECTRICAL SMOKE AND SMELL. NOT ENOUGH INFORMATION TO DETERMINE CAUSE. FORWARD GALLEY HOT FOOD UNIT WAS DISCONNECTED AND REPLACED BY GATES GOURMET. NEW UNIT INSTALLED AND OPERATION CHECKS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001060100048 20010601 00048 NM 2001 6 1 CALA0100476 1 20010516 A 8011 8109701 STARTER BOEING 757 757224 1384958 NM RROYCE RB211 RB211535E4B3 NE NR 1 ENGINE FAILED A CALA E ENGINE SHUTDOWN A J FLAME/FIRE WARNING INDICATION CR CRUISE 1 SW 09 21108 23865 27298 31407 THE NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED WHILE EN ROUTE FROM ANC TO SEA. ENGINE POWER WAS REDUCED AND THE LIGHT EX TINGUISHED. ILLUMINATION OF THE FIRE WARNING LIGHT WAS INTERMITTENT. THE NR 1 ENGINE WAS SHUTDOWN AND THE AIRCRAFT LAN DED IN SEA WITHOUT INCIDENT. EXAMINATION OF THE ENGINE BY MAINTENANCE FOUND THAT THE ENGINE HAD AN INFLIGHT FIRE DUE TO AN UNCONTAINED FAILURE OF THE STARTER. THE NR 1 ENGINE WAS REMOVED AND REPLACED. 2 L 7 2 4F 4 F RT A2NM E12EU 2001060100049 20010601 00049 WP 2001 6 1 CALA0100477 1 20010518 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND CABIN RT I/B FLOOR PANEL DELAMINATED AT FS 916. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INSTAL LED IAW SRM 51-30-1, ECRA 5320-01265, AND ECRA 5100-01844. 2 L 7 2 4F A6WE 2001060100050 20010601 00050 WP 2001 6 1 CALA0100478 1 20010518 A 5320 PAN DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 INSPECTION FOUND FORWARD BAGGAGE BIN DOOR PAN CORRODED BETWEEN LOWER DOOR STOPS AT STA 389-408. SPLICES WERE INSTALLED ON FORWARD CARGO DOOR PAN IAW SRM 53-05, FIGURE 44. 2 L 7 2 4F A6WE 2001060100051 20010601 00051 WP 2001 6 1 CALA0100480 1 20010519 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND FORWARD ENTRY FLOOR PANEL DAMAGED (BROKEN CORNERS AND SOFT SPOTS) AT FS 160-200, LBL 44 TO LBL 54. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001060100052 20010601 00052 WP 2001 6 1 CALA0100481 1 20010519 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND CABIN LT I/B FLOOR PANEL GOUGED AT FS 916. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED I AW ECRA 5320-01265 AND ECRA 5100-01844. 2 L 7 2 4F A6WE 2001060100053 20010601 00053 WP 2001 6 1 CALA0100483 1 20010520 A 5320 WEB DOUG DC9 DC982 3022082 WP CARGO BAY CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 INSPECTION FOUND TWO .5 INCH CRACKS IN FORWARD LOWER SILL PLATE WEB AT AFT BAGGAGE BIN DOOR JAMB AREA. THE SILL PLATE W EB WAS REMOVED AND REPLACED IAW SRM 51-30-0. 2 L 7 2 4F A6WE 2001060100054 20010601 00054 WP 2001 6 1 CALA0100484 1 20010520 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND A 2 INCH CRACK IN CUSP WEB AT FS 237, RBL 56. THE CUSP WEB WAS REMOVED AND THE CRACK WAS STOP DRILLED IAW SRM 51-30-2 AND 53-01, FIGURE 2. A REPAIR DOUBLER AND THE CUSP WEB WERE INSTALLED IAW SRM 53-01, FIGURE 4, 51-30-2, AND 51-30-1. 2 L 7 2 4F A6WE 2001060100055 20010601 00055 NM 2001 6 1 CALA0100485 1 20010520 A 5230 WEB BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70330 23460 INSPECTION FOUND A 0.3 INCH CRACK IN C-2 DOOR AT LIGHTENING HOLE LOCATED AT ACCESS TO SPRING SUPPORT FITTING. THE CRACK ED AREA WAS TRIMMED AND DRESSED UP AND A DOUBLER WEB REPAIR WAS INSTALLED IAW SRM 51-70-13. 2 L 7 2 4F RT A16WE 2001060100056 20010601 00056 WP 2001 6 1 CALA0100486 1 20010521 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND CABIN CENTER FLOOR PANEL CRACKED AT FS 905-946. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IA W SRM 51-30-2 AND 51-30-8. 2 L 7 2 4F A6WE 2001060100057 20010601 00057 NM 2001 6 1 VNAA0105010 1 20010517 A 2612 SD947022 FIRE DETECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CARGO BAY MALFUNCTIONED A VNAA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 436JS 805 3052 FLIGHT 4044 WAS CLIMBING AND THE CREW RECEIVED A CARGO FIRE LIGHT INDICATION ACCOMPANIED BY THE TRIPLE CHIME. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK, MEMORY ITEMS, AND COMPANY PROCEDURES AND DECLARED AN EMERGENCY. THE AIRCRAFT LAN DED OVERWEIGHT DUE TO THE EMERGENCY, CLEARED THE RUNWAY, AND STOPPED ON THE TAXIWAY. THE PASSENGERS WERE INSTRUCTED TO EXIT AND WERE ESCORTED TO THE TERMINAL. MAINTENANCE PERFORMED THE OVERWEIGHT INSPECTION AND REPLACED THE CARGO SMOKE DE TECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL TESTS WERE PERFORMED AND THE AIRCRAFT WAS RE LEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001060100058 20010601 00058 EU 2001 6 1 RAIA00105013 1 20010520 A 2750 877701 CONTROL HANDLE JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 551HK 10242 544 41040 7309-DEC-ON TAXI OUT FLAP ASYMMETRY CAPTION ILLUMINATED. MAINTENANCE INSPECTED AND REPLACED COCKPIT FLAP HANDLE. 2 L 7 2 4T RT A41NM 2001060100059 20010601 00059 NM 2001 6 1 SWAA011466 1 20010516 A 3350 BR2013 TRACK BOEING 737 737317 138447P NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK LIGHTING LOOSE AT ROW 24. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001060100060 20010601 00060 NM 2001 6 1 F3LA200100068 1 20010510 A 5320 STRAP BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3498 23177 DURING C-6 CHECK, INSPECTION REPORTED CORROSION AT NUT PLATE HOLES, FLOOR SUPPORT STRAP, BS 859, RBL 18 TO LBL 18. FABR ICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT STRAP PER SRM 53-60-53 AND 51-10-2. 2 L 7 2 4F RT A16WE 2001060100061 20010601 00061 2001 6 1 SWAA011522 4 20010523 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 383SW 26589 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001060100062 20010601 00062 NM 2001 6 1 SWAA011524 1 20010522 A 3350 57771 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 060SW 21812 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS FLOOR TRACK MISSING END CAP. INSTALLED END CAP PER MM. 2 L 7 2 4F A16WE 2001060100063 20010601 00063 NM 2001 6 1 SWAA011526 1 20010522 A 3350 6104789 BATTERY PACK BOEING 737 7375H4 138449D NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED SERVICE CHECK, FOUND SEVERAL EMERGENCY LIGHTS INOP AT AFT CABIN. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2001060100064 20010601 00064 NE 2001 6 1 SWAA011535 2 20010523 A 7230 340035211 FAN BLADE BOEING 737 7377H4 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE OUT OF TOLERANCE A SWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 07 765SW 29805 876313 DURING CLIMB, NR 2 ENG VIB BEGAN INCREASING WITH NOTICEABLE AIRFRAME VIBRATION. AT FULL PWR, VIB INCREASED PAST 4. RED UCED PWR PER QRH TO MAINTAIN 4. PRIOR TO TURNBACK COULD MAINTAIN ONLY 92 PERCENT N1 WITH 4.0 VIB. REMOVED NR 2 ENG FAN BLADES, CHECKED BLADE WEIGHT. TRIM WEIGHT ARE IN CORRECT POSITION, ALL FOUND OK. REINSTALLED FAN BLADE SET PER MM. P ERFORMED FAN TRIM BALANCE PER MM AND ADJUSTED WEIGHTS PER AVM. 2 L 7 2 4F 4 F RT A16WE E2GL 2001060100065 20010601 00065 2001 6 1 SWAA011536 4 20010524 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 063SW 22061 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001071800020 20010718 00020 NE 2001 7 18 2001UALA00752 2 20010516 A 7230 52G386 CARBON SEAL BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 1 ENGINE LEAKING A UALA K NONE J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 793UA 14397 26946 222008 ACRID-ONLY SMOKE SMELL IN COCKPIT AND CABIN NO SMOKE VISIBLE. OUT OF FL204 IN DESCENT BETTER BY 104. *S/D* REPLACED N R 1 ENGINE. SHOP INVESTIGATION REVEALED NO VISIBLE OIL IN THE ENGINE GAS PATH OR PNEUMATIC DUCTS AND NO EXTERNAL OIL LE AKS. NO OIL IN FAN HUB OR SPINNER. VACUUM TEST OF NR 1, 1.5 & 2 BEARING COMPARTMENTS INDICATED LEAKAGE ONE PPH OVER LIM IT. DISASSEMBLY REVEALED LIGHT OIL COATING ON INNER WALL OF LPC DRUM. COMPONENT TEST OF NR 1.5 & 2 BEARING CARBON SEAL ASSEMBLY REVEALED HIGH AIR LEAKAGE AT THE 1.5 CARBON SEAL OF 7.3 CU. FT. / MINUTE (LIMIT = 3.0 CU FT / MIN). POSSIBLE CAUSE OF COCKPIT AND CABIN ODOR IS OIL LEAKAGE PAST THE NR 1.5 CARBON SEAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001060100066 20010601 00066 EU 2001 6 1 MALA010453 1 20010416 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 427 DURING C-CHECK ,CORROSION ON FLOOR SUPPORT ANGLE AT COCKPIT DOORWAY. REMOVED CORROSION FROM SUPPORT ANGLE AT COCKPIT DOO RWAY. MATERIAL REMAINING OUT OF ALLOWABLE LIMITS. FABRICATED REPAIR ANGLE PER PRINCIPLES OF SRM 51-70-20, ALODINED, PR IMED AND TOP COATED. 2 L 7 2 4T RT A52EU 2001060100067 20010601 00067 2001 6 1 SWAA011537 4 20010523 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 652SW 27722 AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001060100068 20010601 00068 2001 6 1 SWAA011538 4 20010523 A 2565 D31354 SLIDE BOEING 737 7372T4 1384492 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001060100069 20010601 00069 NM 2001 6 1 SWAA011540 1 20010524 A 3350 6104781 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED C3 CHECK, FOUND EEPLS INOP. REMOVED AND REPLACED FWD AND AFT EEPLS BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2001060100070 20010601 00070 NM 2001 6 1 SWAA011541 1 20010523 A 3350 6556633 LENS BOEING 737 7373H4 1384600 NM ENTRY DOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 391SW 27378 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXIT LIGHT MISSING LENS. INSTALLED EMERGENCY EXIT LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2001060100071 20010601 00071 2001 6 1 SWAA011542 4 20010523 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 391SW 27378 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED EMERGENCY EVAC SLIDE P ER MM. 2 L 7 2 4F RT A16WE 2001060100072 20010601 00072 2001 6 1 SWAA011543 4 20010523 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 391SW 27378 DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUSTMENT. ADJUSTED EMERGENCY EVAC SLIDE GIRT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001060100073 20010601 00073 NM 2001 6 1 SWAA011544 1 20010523 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 526SW 26568 DURING SCHEDULED BC4 CHECK, FOUND EEPLS INOP AT FWD CABIN. REPOSITIONED EEPLS WIRING PER MM. 2 L 7 2 4F RT A16WE 2001060100074 20010601 00074 NM 2001 6 1 SWAA011545 1 20010523 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 631SW 27706 DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY EXIT LIGHT BROKEN AND COVER MISSING AT FWD LAV OUTER WALL. REMOVED AND REP LACED EMERGENCY LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001060100075 20010601 00075 NM 2001 6 1 SWAA011495 1 20010521 A 3350 BR2013 TRACK BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 383SW 26589 EEPLS TRACK LOOSE AT ROW 22. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001060100076 20010601 00076 NM 2001 6 1 SWAA011496 1 20010520 A 3350 BR2013 TRACK BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 642WN 27715 EEPLS TRACK LOOSE AT ROW 14. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001060100077 20010601 00077 NM 2001 6 1 SWAA011497 1 20010521 A 3350 BR9442 LIGHT BOEING 737 7377H4 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 762SW 27876 EEPLS TRACK LIGHT BROKEN, AT FWD END OF CABIN. REMOVED AND REPLACED EEPLS LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001060100078 20010601 00078 NM 2001 6 1 SWAA011499 1 20010521 A 3350 6104789 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 073SW 22673 DURING SCHEDULED A1 CHECK, FOUND BOTH AFT DOORS EMERGENCY EVAC SLIDE LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2001060100079 20010601 00079 NM 2001 6 1 SWAA011500 1 20010520 A 3350 57771 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED C1 CHECK, FOUND EEPLS END CAP MISSING. INSTALLED EEPLS END CAP PER MM. 2 L 7 2 4F A16WE 2001060100080 20010601 00080 2001 6 1 SWAA011501 4 20010520 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001060100081 20010601 00081 2001 6 1 SWAA011502 4 20010518 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUSTMENT. ADJUSTED EMERGENCY EV AC SLIDE GIRT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001060100082 20010601 00082 2001 6 1 SWAA011503 4 20010521 A 2565 D31354 SLIDE BOEING 737 7377H4 NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 711HK 27845 DURING SCHEDULED C4 CHECK, FOUND FWD SVC & FWD ENTRY DOORS EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUSTMENT. ADJUSTED E MERGENCY EVAC SLIDE GIRT ASSY''S PER MM. 2 L 7 2 4F RT A16WE 2001060100083 20010601 00083 2001 6 1 SWAA011505 4 20010520 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 396SW 27690 FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001060100084 20010601 00084 2001 6 1 SWAA011512 4 20010522 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 FWD ENTRY & FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BARS CONTACT DOOR FRAME WHEN DOORS ARE OPENED. REMOVED AND REPLACED EMERGENCY EVAC SLIDES AND CONTAINERS PER MM. 2 L 7 2 4F RT A16WE 2001060100085 20010601 00085 2001 6 1 SWAA011513 4 20010522 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001060100086 20010601 00086 NM 2001 6 1 SWAA011514 1 20010522 A 3350 079123 COVER BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 091SW 22963 DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVER LOOSE AT AFT END. SECURED EEPLS COVER PER MM. 2 L 7 2 4F A16WE 2001060100087 20010601 00087 NM 2001 6 1 SWAA011515 1 20010522 A 3350 610478 BATTERY PACK BOEING 737 7373A4 1384585 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHTS INOP, AT ROW 9 DEF AND ROWS 7 AND 11 A BC. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2001060100088 20010601 00088 2001 6 1 SWAA011551 4 20010525 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 609SW 27929 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001060100089 20010601 00089 2001 6 1 SWAA011553 4 20010525 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 636WN 27709 DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001060100090 20010601 00090 2001 6 1 SWAA011557 4 20010525 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. INSTALLED EMERGENCY EVAC IN CONTAINER PER MM. 2 L 7 2 4F RT A16WE 2001060100091 20010601 00091 NM 2001 6 1 SWAA011559 1 20010525 A 2560 6557463 BRACKET BOEING 737 7373H4 1384600 NM ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 397SW 27691 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET LOOSE. SECURED GIRT BAR ASSY BRAC KET PER MM. 2 L 7 2 4F RT A16WE 2001060100092 20010601 00092 2001 6 1 SWAA011560 4 20010525 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM ENTRY DOOR FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 397SW 27691 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR CABLE FRAYED. REMOVED AND REPLACED GIRT B AR CABLE PER MM. 2 L 7 2 4F RT A16WE 2001060100093 20010601 00093 NE 2001 6 1 SWAA011571 2 20010525 A 7261 CFM56 ENGINE BOEING 737 7373H4 1384600 NM GE CFM56 CFM56* 13802 NE NR 1 LEAKING A SWAA C ABORTED TAKEOFF K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 07 615SW 27698 721125 ON TAKEOFF SMOKE APPEARED IN COCKPIT DUE TO OIL SEAL LEAK INTO BLEED SYS. REMOVED AND REPLACED NR 1 ENG PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2001060100094 20010601 00094 NM 2001 6 1 SWAA011573 1 20010528 A 2560 65C34691 GIRT BAR BOEING 737 7375H4 138449D NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 523SW 26565 FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUSTMENT. ADJUSTED EMERGENCY EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001060100095 20010601 00095 2001 6 1 SWAA011574 4 20010528 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SEVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 636WN 27709 DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED E MERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001060100096 20010601 00096 2001 6 1 SWAA011575 4 20010529 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 063SW 22061 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001060100097 20010601 00097 2001 6 1 SWAA011577 4 20010528 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR` OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 074SW 22674 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR & AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF VIEW. REPOS ITIONED BOTH EMERGENCY EVAC SLIDES PER MM. 2 L 7 2 4F A16WE 2001060100098 20010601 00098 NM 2001 6 1 DLM11010715 1 20010505 A 2760 CONTROL CABLE DOUG MD11 MD11 3023602 NM RT SPOILER ICED A DALA K NONE F FLT CONT AFFECTED AP APPROACH 1 SO 27 807DE 48478 ON DESCENT WHILE ATTEMPING TO DEPLOY SPOILERS NO SPOILERS DEPLOYED ON RIGHT SIDE. ALSO DID NOT GET RIGHT SPOILERS ON GR OUND AND WHEN PLACING FLAPS TO 15 DEGREES GOT ROLLING MOMENT AND FLAP ASYMMTRY LIGHT D305007004. FOUND LARGE AMOUNT OF ICE BUILDUP IN RIGHT FORWARD SECTION OF THE RIGHT WHEEL WELL CAUSING SPOILER CABLE OPERATION RESTRICTION. REMOVED ALL I CE VISUALLY CHECKED AND PERFORMED SATISFACTORY OPERATIONAL CHECK OF ALL FLIGHT CONTROLS PER M/M. CLOSED OFF WATER SHUTO FF VALVE LAV M - C/W SERVICE BULLETIN MD11-53-064. 2 L 7 3 4F RT A22WE 2001060100099 20010601 00099 NM 2001 6 1 SWAA011467 1 20010517 A 3350 57771 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 635SW 27708 DURING SCHEDULED PMC CHECK, FOUND TWO EEPLS END CAPS MISSING, AND TWO EEPLS LIGHTS INOP. INSTALLED END CAPS AND RELAMPE D EEPLS LIGHTS PER MM. 2 L 7 2 4F RT A16WE 2001060100100 20010601 00100 2001 6 1 SWAA011523 4 20010522 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001060100101 20010601 00101 NM 2001 6 1 SWAA011525 1 20010523 A 3350 101114 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 629SW 27704 DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY LIGHT COVER MISSING AT FWD LAV OUTER WALL. INSTALLED LIGHT COVER PER MM. 2 L 7 2 4F RT A16WE 2001060100102 20010601 00102 NM 2001 6 1 SWAA011539 1 20010524 A 3397 079123 WIRE BOEING 737 7377H4 1384404 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 751SW 29803 EEPLS LIGHT COVER BROKEN AND WIRES EXPOSED AT FWD CABIN. REMOVED AND REPLACED EEPLS COVER AND SECURED EEPLS WIRES PER MM. 2 L 7 2 4F RT A16WE 2001060100103 20010601 00103 NM 2001 6 1 UPS01435937 1 20010508 A 5312 PRESSURE PANEL BOEING 747 747123 1384873 NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:C-2 NOSE W/W TUNNEL - LT BS 320 VERTICAL BEAM WEB BTN 4TH & 5TH CLIP (COUNT FROM TOP) FOUND CRACK AT STA ND OFF HOLE APPROX .125 INCH LONG. BS 320 LT WEB REPLACED PER SRM 51-10-01 & 51-30-02. 2 L 7 4 4F A20WE 2001060100104 20010601 00104 NM 2001 6 1 UPS01635927 1 20010519 A 7930 J221P904 O-RING BOEING 767 76734AF 1385212 NM OIL PRESSURE CUT A IPXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 303UP 27241 INSPECTION TYPE:ETOP LEFT ENGINE LOW OIL PRESS, OIL QTY. REPLACED CUT O-RING ON AFT FITTING OF OIL PRESSURE TRANSMITTER . 2 L 7 2 4F RT A1NM 2001071300007 20010713 00007 NM 2001 7 13 UPS01635939 1 20010519 A 2781 TARGET BOEING 767 76734AF 1385212 NM L/E SLAT MISSING A IPXA K NONE F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 SO 01 313UP 27764 INSPECTION TYPE:N/A PILOT REPORT, ON ROLLOUT L/E SLAT ASSY MESSAGE AND FLAP LOCKOUT. *S/D* CYCLED L/E ALTN ARM SWITCH PER FIM 27-81-00 RAN SLATS SEVERAL TIMES. SYSTEM STILL LOCKS OUT AFTER 1 DEG AND SAME MESSAGES APPEAR. FOUND NR 9 SLAT I/B INTERMEDIATE TARGET FOR PROX SWITCH 303 MISSING. 2 L 7 2 4F RT A1NM 2001060100105 20010601 00105 WP 2001 6 1 UPS01835926 1 20010501 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C1 AFT PIT STA 1020 L36 2 EA NUT PLATES WITH CORROSION ON FRAME UNDER NUT PLATES. REMOVED CORROSION MAT OUT OF LIMITS IAW 53-2-0. REMOVED FRAME CAP LT & RT GUSSET AND R & L SUPPORT ANGLES IAW DC8 SRM 51-1-21 MAT ID IS 7075 -0 .090 PO 344427 FOR ANGLE REPAIR AND 7075-T6 .125 FOR FILLER. FAB REPAIR ANGLE AND FILLER IAW UPS EO DWG DC8-53A-011. HEAT TREAT REPAIR ANGLE, ALODINED AND PRIMED ANGLE AND FILLER IAW 51-1-8 INSTALLED IAW 51-1-20. 2 L 7 4 4F RT 4A25 2001060100106 20010601 00106 NM 2001 6 1 SWAA011498 1 20010521 A 3350 BR2013 TRACK BOEING 737 7377H4 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 711HK 27845 DURING SCHEDULED C4 CHECK, FOUND EEPLS TRACK LOOSE AT FWD CABIN AND EEPLS COVER BROKEN AT ROW 11. SECURED EEPLS AND INS TALLED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2001060100107 20010601 00107 2001 6 1 SWAA011504 4 20010521 A 2565 D31354 SLIDE BOEING 737 7377H4 NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 711HK 27845 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY & AFT SVC DOORS EMERGENCY EVAC SLIDE GIRT ASSY OUT OF AJUSTMENT. ADJUSTED EM ERGENCY EVAC SLIDE GIRT ASSY''''S PER MM. 2 L 7 2 4F RT A16WE 2001060100108 20010601 00108 NM 2001 6 1 SWAA011550 1 20010526 A 3350 207377 LENS BOEING 737 7375H4 138449D NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 521SW 25320 EEPLS LENS MISSING. INSTALLED EEPLS LENS PER MM. 2 L 7 2 4F RT A16WE 2001060100109 20010601 00109 NM 2001 6 1 0101765502 1 20010427 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 502US 23191 DURING H-CHECK FOUND CORROSION ON FLOORBEAM AT BS 1681. REPAIRED PER EA 55-183364. 2 L 7 2 4F RT A2NM 2001060100110 20010601 00110 NM 2001 6 1 0101775502 1 20010406 A 5320 SUPPORT FITTING BOEING 757 757251 1384970 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 502US 23191 DURING H-CHECK FOUND CORROSION ON SEAT TRACK SUPPORT FITTING AT BS 418 RBL 45. REPAIRED PER EA 55-183418. 2 L 7 2 4F RT A2NM 2001060100111 20010601 00111 NM 2001 6 1 0101785502 1 20010425 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 502US 23191 DURING H-CHECK FOUND CRACK IN FLOORBEAM UPPER CAP AT BS 680 LBL 25. REPAIRED PER EA 55-183446. 2 L 7 2 4F RT A2NM 2001060100112 20010601 00112 NM 2001 6 1 0101795502 1 20010424 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 502US 23191 DURING H-CHECK FOUND CRACK IN FLOORBEAM UPPER CAP AT BS 700 LBL 25. REPAIRED PER EA 55-183447. 2 L 7 2 4F RT A2NM 2001060100113 20010601 00113 NM 2001 6 1 0101805502 1 20010406 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 502US 23191 DURING H-CHECK FOUND CORROSION ON FLOORBEAM UPPER CAP AT BS 377 RBL 10. REPAIRED PER EA 55-183448. 2 L 7 2 4F RT A2NM 2001060100114 20010601 00114 2001 6 1 SWAA011552 4 20010525 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 510SW 24187 DURING SCHEDULED SERVICE CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED E MERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001060100115 20010601 00115 2001 6 1 SWAA011558 4 20010525 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED EMERGENCY EVAC GIRT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001060100116 20010601 00116 2001 6 1 SWAA011576 4 20010529 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUSTMENT. ADJUSTED AFT SVC DOOR EMERGENCY EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001060100117 20010601 00117 NM 2001 6 1 UPS01435928 1 20010511 A 5347 BAC152015667178 SEAT TRACK BOEING 747 747123 1384873 NM COCKPIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:C-2 U/D - BS 480-520 RBL 65 SEAT TRACK FOUND HEAVY CORROSION DURING FLOOR COVERING REMOVED. TIE DOWN TR ACK REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001060100118 20010601 00118 NM 2001 6 1 UPS01435929 1 20010509 A 5310 65B0831973 STOP FITTING BOEING 747 747123 1384873 NM DOOR FRAME CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 20323 INSPECTION TYPE:C-2 M/D - L3 DOOR STOP SUPPORT FTG FOUND CRACKED AT BS 1265 S3L. STOP FTG REPLACED AS PER SRM 51-10-01 WITH HX S/TAG FF 069231. 2 L 7 4 4F A20WE 2001060100119 20010601 00119 NM 2001 6 1 UPS01435930 1 20010511 A 5411 RIB BOEING 747 747123 1384873 NM NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:C-2, NR 1 PYLON - RESERVOIR LT STRUCTURE RIB CRACK FOUND AS MARKED. NR 1 PYLON HYD RESERVOIR LT RIB REP LACED PER SRM 51-10-01. LEAK CHECKED SATISFACTORY PER MM 29-11-00. 2 L 7 4 4F A20WE 2001060100120 20010601 00120 NM 2001 6 1 UPS01435935 1 20010508 A 5312 PRESSURE PANEL BOEING 747 747123 1384873 NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:C-2 NOSE W/W TUNNEL - LT BS 300 VERTICAL BEAM WEB BETWEEN 1ST & 2ND CLIP (COUNT FROM TOP) FOUND CRACK AT LOWER STAND OFF HLE APPROX .375 & .25 INCH LONG. LT BS 300 VERTICAL BEAM WEB REPLACED AS PER SRM 51-10-01 & 51-30-02. 2 L 7 4 4F A20WE 2001060100121 20010601 00121 NM 2001 6 1 UPS01435936 1 20010508 A 5312 PRESSURE PANEL BOEING 747 747123 1384873 NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:C-2 NOSE W/W TUNNEL - RT BS 320 VERTICAL BEAM WEB BTN 4TH & 5TH CLIP FOUND CRACK AT STANDOFF HOLW APPROX .125 & .0625 INCH LONG. CRACKED WEB REPLACED PER SRM 51-10-01 & 51-30-02. 2 L 7 4 4F A20WE 2001060100122 20010601 00122 NM 2001 6 1 01FDEA00372 1 20010518 A 2910 LINE BOEING 727 727233 138408A NM HYD SYSTEM LEAKING A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 278FE 22345 AFT T/O FLT CONTROL LIGHTS CAME ON AND B-SYS QUANTITY WENT TO ZERO. *S/D* REMOVED AND REPLACED FLEX LINE IN 727-200 MM 20-10-012. OK FOR SERVICE. 2 L 7 3 4F RT A3WE 2001060100123 20010601 00123 NM 2001 6 1 01FDEA00368 1 20010517 A 2612 FIRE DETECTOR BOEING 727 7272S2F 1384O81 NM ENGINE FAULTY A FDEA E F A ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 216FE 22937 AFT T/O ENG FIRE LIGHT ILLUM. BOTTLES 1 AND 2 DISCHARGED LIGHT REMAIN ILLUM. *S/D* REMOVED AND REPLACED FIRE DETECTIO N UNIT AND FIRE BOTTLES AND DISCHARGE IND DISK PER STANDARD PRACTICE AND MM 26-21-001-4, MM 26-11-001-5. GOOD FOR SERVI CE. 2 L 7 3 4F A3WE 2001060100124 20010601 00124 NM 2001 6 1 F3LA200100069 1 20010510 A 5320 STRAP BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3498 23177 DURING C-6 CHECK, INSPECTION REPORTED CORROSION ON STRAP UNDER FRAME AT BS 794. FABRICATED AND INSTALLED REPLACEMENT ST RAP PER BOLD DRAWING 65-47959, SHEET 15 OF 49, SRM 51-10-02 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001060100125 20010601 00125 NM 2001 6 1 F3LA200100070 1 20010510 A 5320 STRAP BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3498 23177 DURING C-6 CHECK, INSPECTION REPORTED CORROSION ON HORIZONTAL FLOOR STRAP AT BS 772, RBL 21 TO LBL 21. FABRICATED AND I NSTALLED REPLACEMENT FLOOR STRAP PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001060100126 20010601 00126 EU 2001 6 1 MALA010475 1 20010403 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 429XJ 429 DURING C-CHECK IN BNA, RT FUSELAGE HAS A GROUP OF DENTS AFT OF THE ICE SHIELD STA 363.0 AND SL1634. MAINTENANCE FOUND DE NTS OUT OF ALLOWABLE LIMIT. REF SAAB SRM 51-10-10 NDT/BOND TEST SHOWS NO CRACKS OR DISBOND, REF FFVNT006 AND SRM 51-10- 00. DENTS ARE ACCEPTED AS IS REF SAAB EO 340SDS001422. 2 L 7 2 4T RT A52EU 2001060100127 20010601 00127 EU 2001 6 1 MALA010476 1 20010403 A 5347 7253721459 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 429XJ 429 FOUND DURING C-CHECK IN BNA, GALLEY/LAV SEAT TRACK IS CORRODED BETWEEN STA 231 AND STA 272 AT RBL 16. REFER TO CELSIUS WO 19582, TASK 1515. MAINTENANCE REMOVED CORROSION, MATERIAL REMOVAL IS OUT OF LIMIT REF SRM 51-10-10. TRACK P/N 72537 21-459 AND PROFILE P/N 7253721-495. REMOVED AND REPLACED GALLEY LAV SEAT TRACK AND PROFILE IAW SRM 51-40-21, 22, 27. 2 L 7 2 4T RT A52EU 2001060100128 20010601 00128 EU 2001 6 1 MALA010477 1 20010404 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 429XJ 429 FOUND DURING C-CHECK IN BNA, FLOOR SUPPORT FLANGE IS CORRODED ON THE FRAME AT STA 272 BETWEEN RBL 19 AND RBL 30. REFER TO CELSIUS WO 19582, TASK 1517. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40. MATERIAL REMOVED IS OUT OF LIMITS. FA BRICATED AND INSTALLED NEW SUPPORT ANGLE AND SHIM IAW SRM 51-20-20, 51-20-50, 51-40-40, AND 51-40-21. 2 L 7 2 4T RT A52EU 2001060100129 20010601 00129 EU 2001 6 1 MALA010478 1 20010404 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 429XJ 429 FOUND DURING C-CHECK IN BNA, RT FUSELAGE HAS A GROUP OF DENTS AFT OF THE ICE SHIELD STA 339 AND SL1634. MAINTENANCE FOUN D DENTS OUT OF ALLOWABLE LIMIT. NDT/BOND TEST PER FFVNDT006/SRM 51-10-10 SHOWS NO CRACKS OR DISBOND AREA. DENTS ARE AC CEPTED AS IS REF SAAB EO 340SDS001422. 2 L 7 2 4T RT A52EU 2001060100130 20010601 00130 EU 2001 6 1 MALA010479 1 20010404 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 429XJ 429 DURING C-CHECK IN BNA, INTERCOSTAL FLOOR SUPPORT FLANGES ARE CORRODED AT LBL 10 BETWEEN FS 236 AND FS 258. MAINTENANCE R EMOVED CORROSION IAW SRM 51-70-40, MATERIAL REMOVED IS OUT OF LIMITS. NEW FLOOR SUPPORT FABRICATED I/B SIDE LBL 10 STA 236 & 258 REPAIR ANGLE FABRICATED FOR O/B SIDE. ALODINED AND PRIMED, INSTALLED REPAIR AND NEW SUPPORT IAW SRM 51-40-21. 2 L 7 2 4T RT A52EU 2001060100131 20010601 00131 EU 2001 6 1 MALA010480 1 20010404 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 429XJ 429 DURING C-CHECK IN BNA, FLOOR SUPPORT FLANGES ARE CORRODED ON THE FRAME AT STA 258 BETWEEN LBL 16 AND RBL 12. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40. MATERIAL REMOVED IS OUT OF LIMITS. REPAIRED ANGLES, FABRICATED FROM 2024-T-3 .050 IN REFERENCE TO 53-70-20. ALODINED AND PRIMED TOPCOAT APPLIED, INSTALLED IAW SRM 51-40-21/ 51-20-50 AND 53-70-30. 2 L 7 2 4T RT A52EU 2001060100132 20010601 00132 EU 2001 6 1 MALA010481 1 20010404 A 5753 SKIN SAAB SF340 340B 7860101 EU T/E FLAP CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 429XJ 429 DURING C-CHECK IN BNA, RT I/B FLAP UPPER SURFACE CHAFED. MX BLENDED RT FLAP IN UPPER SURFACE. REMAINING MATERIAL IS OUT OF LIMITS. NDT OF BLEND AREA PER FFVNDT006, SHOWS NO CRACKS. DAMAGE IS ACCEPTED AS IS REF SAAB EO 340SDS001422. 2 L 7 2 4T RT A52EU 2001060100133 20010601 00133 EU 2001 6 1 MALA010484 1 20010404 A 5320 605872 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 429XJ 429 DURING C-CHECK IN BNA, FLOOR SUPPORT T-EXTRUSION IS CORRODED AT LBL 10 BETWEEN STA 231-236 DIRECTLY IN FRONT OF THE AVIO NICS RACK. MAINTENANCE REMOVED CORROSION, MATERIAL REMOVED IS OUT OF LIMITS. REMOVED T-SUPPORT, FABRICATED NEW PART FRO M T-EXTENSION P/N 60-5872, 2024T3 .063 PO 55192. ALODINED AND PRIMED, APPLY TOPCOAT, INSTALLED NEW SUPPORT.. 2 L 7 2 4T RT A52EU 2001060100134 20010601 00134 EU 2001 6 1 MALA010485 1 20010404 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 429XJ 429 DURING C-CHECK IN BNA, CORRODED RIVETS IN THE TOP OF THE FLOOR SUPPORT FRAME AT FS 236. MAINTENANCE REMOVED CORROSION AN D SEVERAL RIVETS. MATERIAL REMOVED IS OUT OF LIMITS. FABRICATED FILLER AND DOUBLER IAW SRM 51-20-20/51-40-60. LOCATED AND DRILLED FILLER AND DOUBLER PER PRINCIPLES OF SRM 51-70-20. ALODINED, PRIMED AND TOPCOATED. INSTALLED PER SRM 51-40 -21. 2 L 7 2 4T RT A52EU 2001060100135 20010601 00135 EU 2001 6 1 MALA010486 1 20010405 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 429XJ 429 DURING C-CHECK IN BNA, RT FLOORBOARD SUPPORT FLANGE IS GALLED AT RBL 30 BETWEEN STA 363 AND STA 389. MAINTENANCE REMOVED GALLED/CORROSION DAMAGE, MATERIAL REMAINING IS WITHIN LIMITS. ALODINED, PRIMED AND PAINTED. 2 L 7 2 4T RT A52EU 2001060100136 20010601 00136 EU 2001 6 1 MALA010487 1 20010405 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 429XJ 429 DURING C-CHECK IN BNA, LT FLOORBOARD SUPPORT FLANGE IS GALLED BETWEEN FS 339 AND FS 389. MAINTENANCE REMOVED GALLED/CORR OSION DAMAGE, MATERIAL REMAINING IS WITHIN LIMITS. OK TO TREAT PRIME AND PAINT. ALODINED, PRIMED AND PAINTED IAW SRM 5 1-242/43. 2 L 7 2 4T RT A52EU 2001060100137 20010601 00137 EU 2001 6 1 MALA010488 1 20010406 A 5347 7253799383 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 429XJ 429 DURING C-CHECK IN BNA, CENTER AISLE SEAT TRACK LB 0 IS CORRODED ON HORIZONTAL AND VERTICAL I/B FLANGES FROM FS 294-FS 40 1. MAINTENANCE CUT OUT CORRODED SECTION OF SEAT TRACK. LOCATED AND DRILLED NEW SECTION AND SPLICE, INSTALLED NEW SEAT T RACK P/N 7253-799-383 AND U-BEAM P/N 7253799-379. AREAS NOT COVERED WITH SEAT TRACK REPLACEMENT ARE ACCEPTED AS IA REF SAAB EO 340SDS001422. PERFORMED SURFACE TREATMENT AND PROTECTION PER SAAB EO 340SDS001422. 2 L 7 2 4T RT A52EU 2001060100138 20010601 00138 EU 2001 6 1 MALA010489 1 20010407 A 5347 7252799383 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 429XJ 429 DURING C-CHECK IN BNA, CENTER AISLE SEAT TRACK LBL 18.3 IS CORRODED ON HORIZONTAL AND VERTICAL I/B FLANGES FROM FS 294.0 TO FS 401. MAINTENANCE CUT OUT CORRODED SECTION OF SEAT TRACK P/N 7253799-383, LOCATED, DRILLED NEW SECTION OF TRACK/SP LICE, INSTALLED NEW SEAT TRACK SECTION IAW SRM 51040-21/25. 2 L 7 2 4T RT A52EU 2001060100139 20010601 00139 EU 2001 6 1 MALA010490 1 20010409 A 5347 CARGO TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 429XJ 429 DURING C-CHECK IN BNA, CARGO BAY SEAT TRACK LT CENTER RT CENTER IS CORRODED ON UPPER FLANGES FROM FS 640.0 TO FS 868. MA INTENANCE REMOVED CORROSION ON LT, ENTER AND RT CARGO SEAT TRACKS. REMOVED AND REPLACED LT, CENTER AND RT SEAT TRACKS D UE MATERIAL REMOVAL OUT OF ALLOWABLE LIMIT REF SRM 53-7060. 2 L 7 2 4T RT A52EU 2001060100140 20010601 00140 EU 2001 6 1 MALA010492 1 20010404 A 5320 7253721439 WEB SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 429XJ 429 DURING C-CHECK IN BNA, FLOOR SUPPORT WEB IS CORRODED BETWEEN FS 288 AND FS 294. MAINTENANCE REMOVED CORROSION AND SEVERA L RIVETS. MATERIAL REMOVED IS OUT OF LIMITS IAW SRM 51-10-10. REMOVED AND REPLACED CORRODED WEB WITH NEW WEB IAW SRM 5 1-40-23. 2 L 7 2 4T RT A52EU 2001060100141 20010601 00141 2001 6 1 MALA010494 4 20010515 A 3418 861CAR TRANSMITTER SAAB SF340 340B 7860101 EU STALL WARNING DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 450XJ 450 RT STALL FAIL LIGHT ILLUMNATES MULTIPLE TIME INFLIGHT. LIGHT ILLUMINATES MASTER CAUTION AND SINGLE CHIME. LIGHT GOES O UT ON OWN AFTER ABOUT ONE SECOND. CAME ON APPROXIMATELY THIRTY TIMES. AIR RETURN TO DTW. MAINTENANCE REPLACED RT ANGL E OF ATTACK TRANSMITTER P/N 861CAR, S/N ON 00082, S/N OFF 01163. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2001060100142 20010601 00142 EU 2001 6 1 MALA010495 1 20010517 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU E/E BAY MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 456XJ 456 IN FLIGHT AVIONICS SMOKE MASTER WARNING LIGHT CAME ON. RAN MEMORY ITEMS AND QRH CHECKLIST. LIGHT REMAINED ON DURING FL IGHT AND EXTINGUISHED AFTER LANDING NO ACTUAL SMOKE OR FIRE DETECTED. DIVERTED FLIGHT TO ATW. MAINTENANCE DEFERRED AVI ONICS RACK SMOKE DETECTION SYSTEM PER MEL 26-13-3-B. ENTERED INTO DMR MXC NOTIFIED. MAINTENANCE PROCEDURES C/W. MAINT ENANCE REPLACED AVIONICS SMOKE DETECTOR. 2 L 7 2 4T RT A52EU 2001060100143 20010601 00143 EU 2001 6 1 MALA010496 1 20010519 A 2731 TRIM TAB SAAB SF340 340B 7860101 EU ELEVATOR INOPERATIVE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 439XJ 439 PITCH TRIM INOP. AIR RETURN TO MSP. MAINTENANCE DEFERRED ELEVATOR TRIM SYNC IAW MEL 27-32-10. ENTERED INTO DMR MXC NO TIFIED. 2 L 7 2 4T RT A52EU 2001060100144 20010601 00144 CE 2001 6 1 CIEA0004 1 20010518 A 5610 5042006924 WINDSHIELD BEECH 90 E90 1152914 CE COCKPIT CRACKED E CIEA K NONE O OTHER IN INSP/MAINT 1 NM 03 92DV 8751 107 LW292 DURING WASHING OF THE AIRCRAFT THE MECHANIC NOTICED AN UNUSUAL MARK ON THE CO-PILOTS WINDSHIELD. FURTHER INSPECTION REV EALED A CRACK IN THE OUTER WINDOW GLASS PANE APPROXIMATELY .5 INCH INBOARD OF THE CENTER POST AREA, RUNNING VERTICALLY A PPROXIMATELY 12 INCHES. THE MANUFACTURE DATE ON THE WINDSHIELD WAS 1978. 1 L 7 2 3T 3A20 2001060100145 20010601 00145 NE 2001 6 1 01FDEA00378 2 20010521 A 7200 ENGINE AIRBUS 310 A310222 3930315 EU PWA JT9 JT9D7R4E1 52054 NE NR 1 MALFUNCTIONED A FDEA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 SO 25 454FE 278 716109 A/C ENCOUNTERED MODERATE TURBULENCE, CIRRUS CLOUDS AND STATIC ELECTRICITY. NR 1 ENG ROLLED BACK TO IDLE/OFF. EGT CLIMB TO GREATER THAN 600 DEG. 2 L 7 2 4F 4 F RT A35EU E3NE 2001060100146 20010601 00146 EU 2001 6 1 MALA010458 1 20010416 A 5320 INTERCOSTAL SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 427 DURING C-CHECK ,CORROSION ON INTERCOASTAL BETWEEN STA 236 AND STA 258 AT LBL 10. REMOVED CORROSION ON INTERCOSTAL BETWEE N STA 236-258 AT LBL 10 IAW SRM 51-70-40. INSTALLED NEW ANGLE, SHIM AND SUPPORT DOUBLER ON INTERCOSTAL BETWEEN STA 236- 258 AT LBL 10 IAW 51-40-21. 2 L 7 2 4T RT A52EU 2001060100147 20010601 00147 EU 2001 6 1 QXEA0100775 1 20010518 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN FAULTY A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 499US 11182 PDX - UPON INSPECTION, FOUND EXIT SIGN ABOVE FLIGHT COMPARTMENT DOOR AND CENTER AISLE TO HAVE INOPERATIVE LAMPS. REMOVE D AND REPLACED CIRCUIT CARDS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001060100148 20010601 00148 EU 2001 6 1 MALA010468 1 20010419 A 5347 7253721495 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 427 DURING C-CHECK, FOUND GALLEY SEAT TRACK PROFILE IS CORRODED. MX REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED GA LLEY SEAT TRACK PROFILE, LOCATED AND DRILLED HOLES ON NEW PROFILE, ALODINED, PRIMED HOLES AND INSTALLED NEW SEAT TRACK P ROFILE IAW SRM 51-40-21/27. 2 L 7 2 4T RT A52EU 2001060100151 20010601 00151 NM 2001 6 1 DHL2001741009 1 20010515 A 7711 TRANSMITTER BOEING 727 7272Q9 138448M NM NR 1 ENGINE MALFUNCTIONED A DHLA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 741DH 21931 WHEN SETTING T/O THRUST NR 3 EPR GAUGE OVERSHOT EXPECTED SETTING WHEN ALL OTHER ENGINE INDICATIONS (NR 1, 2, 3) WERE EVE N. NR 3 N1 96.0, EGT 570, N2 96.8, FF 8400PPH MATCHED NR 1 ENG N1. DEFERRED PER MEL 77-1-1 CTRL NR 5594 CAT A. SEE RE STRICTIONS PLA INSTALLED. ENG TRIM SHEET GENERATED. R&R NR 3 EPR XMTR IAW B727 MM CHPT 77-11-11. PERFORMED P/P & T/O E PR CHECK IAW DHL JRH 7.7. OPS CHECK GOOD. 2 L 7 3 4F RT A3WE 2001060100152 20010601 00152 NM 2001 6 1 01FDEA00354 1 20010515 A 5311 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 276FE 22041 DENTED FRAME AT BS 580, LBL 47, WL 165 PER FEDEX EA 7-5310-29267. R&R PER FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 2001060100153 20010601 00153 NM 2001 6 1 01FDEA00357 1 20010515 A 5311 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 276FE 22041 DENTED FRAME BS 680, LBL 38, WL 162 PER FEDEX EA 7-5310-29267. R&R PER FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 2001060100154 20010601 00154 NM 2001 6 1 01FDEA00358 1 20010515 A 5311 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 276FE 22041 FRAME DENTED BS 700, LBL 42, WL 160 FOUND TO BE OUT OF LIMITS PER FEDEX EA 7-5310-29267. REMOVED AND REPLACED PER FEDEX SRM 51-40-3. ALODINED AND PRIMED PER FEDEX 51-20-151. 2 L 7 3 4F RT A3WE 2001060100155 20010601 00155 NM 2001 6 1 01FDEA00359 1 20010515 A 5311 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 276FE 22041 FWD CARGO BAY LT FRAME AT BS 520 HAS TWO DENTS SIDE BY SIDE LBL 38. R&R FRAME PER IAW FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 2001060100156 20010601 00156 EU 2001 6 1 MALA010483 1 20010404 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 429XJ 429 DURING C-CHECK IN BNA, FLOOR SUPPORT ANGLE IS CORRODED AFT OF THE COCKPIT ENTRANCE AT FS 231 BETWEEN LBL 10 AND LBL 14. MAINTENANCE REMOVED CORROSION/MATERIAL, REMOVED IS OUT OF LIMITS IAW SRM 51-10-10. FABRICATED REPAIR ANGLE FROM 2024T3 .050. ALODINED, PRIMED AND TOPCOAT. INSTALLED REPAIR ANGLE IAW SRM 51-40-21. 2 L 7 2 4T RT A52EU 2001060100164 20010601 00164 EU 2001 6 1 RAIA00105014 1 20010520 A 2751 TY175902B FCU JETAIR JETSTM JETSTM4101 1500501 EU E/E BAY FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 551HK 15577 41040 7496-STL-ON TAXI OUT, FLAP ASYMMETRY CAPTION ILLUMINATED, THEN FLAP FAULT CAPTION ILLUMINATED. MAINTENANCE INSPECTED AN D REPLACED ELECTRONIC FLAP CONTROL UNIT. 2 L 7 2 4T RT A41NM 2001060100165 20010601 00165 WP 2001 6 1 ABXA010231 1 20010518 A 3250 47743701 LINK DOUG DC8 DC861 3021952 WP NLG BROKEN A ABXA K NONE J WARNING INDICATION LD LANDING 1 GL 23 850AX 45894 THE AIRCRAFT DID NOT TRANSITION INTO GROUND SHIFT MODE UPON LANDING. MAINTENANCE INSPECTED AND REPLACED THE RESERVE PRE SSURE SHUTOFF VALVE BUNGEE LINK IAW DC-8 MM. OPS CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2001060100166 20010601 00166 WP 2001 6 1 ABXA010230 1 20010518 A 2740 3715377 SHAFT DOUG DC8 DC863 302198A WP HORIZ STAB DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 THE LEFT HORIZONTAL STABILIZER SHAFT HARDNESS CHECKED LOW DURING TEST. MAINTENANCE COMPLETED ABX REA D855-41165 AND INI TIATED A CARRY OVER ITEM DEFERRAL FOR TRACKING. 2 L 7 4 4F 4A25 2001060100167 20010601 00167 WP 2001 6 1 CALA0100488 1 20010521 A 3350 60030431 BATTERY PACK GRIMES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16895 49394 INSPECTION FOUND FIRST CLASS OVERHEAD EMERGENCY LIGHTS INOPERATIVE. THE EMERGENCY LIGHT BATTERY PACK WAS REMOVED AND REP LACED IAW MM 33-53-00. 2 L 7 2 4F A6WE 2001060100168 20010601 00168 NM 2001 6 1 UPS01235942 1 20010521 A 3350 LIGHT BOEING 727 72751C 1384015 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:IN EMERGENCY LIGHTS UNARMED LIGHT INOP WHEN UNARMED AND PRESS TO TEST. RELAMPED AND FUNCTIONALLY CK GOO D AS PER 33-50. 2 L 7 3 4F A3WE 2001060100169 20010601 00169 NM 2001 6 1 QXEA0100776 1 20010520 A 3320 1010951 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN MALFUNCTIONED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 350PH 488 PDT- STRONG SMELL OF BURNED WIRES IN AFT OF CABIN AND IN CARGO AREA. NO VISIBLE SMOKE PRESENT. WHEN GROUND FAN TURNED OFF, SMELL SEEMED TO SUBSIDE. FOUND OVERHEAD LIGHT ASSEMBLY AT ROW 9AB SMOKING. REMOVED AND REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001060100170 20010601 00170 EU 2001 6 1 QXEA0100779 1 20010517 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN DEFECTIVE A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 475AU 11222 SEA- EMERGENCY LIGHT EXIT SIGNS AT CABIN ENTRANCE AND AFT CABIN POSITIONS DIM. REMOVED AND REPLACED EXIT SIGN CIRCUIT B OARDS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001060100171 20010601 00171 GL 2001 6 1 01FDEA00380 2 20010522 A 7200 ENGINE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2* GL NR 1 VIBRATION A FDEA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 25 592FE 48550 702292 CLIMBING 11,000 FT FELT VIB NOTICED NR 1 ENG N1 DECREASING, NR 1 ENG VIB MONITORS AMBER. NO FIRE WARNING. SECURED ENG IAW CHECK LIST. 2 L 7 3 4F 4 F RT A22WE E23EA 2001060600003 20010606 00003 NM 2001 6 6 P2EA01007 1 20010323 A 5330 DOUBLER BOEING 737 737247 138448D NM FUSELAGE LEAKING A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 SJO - REPAIR LEAKING ON FUSELAGE AT BS 727 TO BS 907 BETWEEN STRINGER 3R AND 5R. SENT TO BOEING ENGINEERING ON 3/26/01. IT WAS DETERMINED THAT NO MINOR REPAIR EXISTED. (M) 2 L 7 2 4F A16WE 2001060600004 20010606 00004 NM 2001 6 6 GAIA01126ST 1 20010413 A 5730 DOUBLER BOEING 727 7272J0 138407E NM LT WING LEAKING A GAIA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 07 284KH 21108 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT WING AT STATION 224.5 HAD A PREVIOUS DOUBLER REPAIR THAT WA S LEAKING FUEL FROM SEVERAL HI-LOCKS FASTENERS. REMOVED AND REPLACED DOUBLER IAW KHA EA B7-57-025. FLIGHT VEHICLES CON SULTING DRAWING 57-01141-1, AND 8110-3 DATED 4/8/01. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2001060600005 20010606 00005 CE 2001 6 6 RU3A0102 1 20010418 A 2710 2322550 AILERON LEAR 60 60LEAR 5170707 CE WING ICED A RU3A O OTHER F FLT CONT AFFECTED DE DESCENT 1 SW 21 56 60033 AFTER FLIGHT IN RAIN, SUBSEQUENT CLIMB ABOVE FREEZING LEVEL, AND DESCENT FOR LANDING: DURING VECTOR FOR ILS FINAL, AUTOP ILOT WAS MANUALLY DISCONNECTED BY (PIC). AIRCRAFT IMMEDIATELY BANKED LEFT, NOTED FULL LEFT AILERON TRIM DEPICTED ON TRI M INDICATOR. AILERONS DIFFICULT TO MOVE TO FORCE WINGS LEVEL. AFTER WORKING AILERONS, THEY RETURNED TO NORMAL CONTROL. LANDED NORMALLY. ICE FORMED IN GAP BETWEEN WING AND AILERON. INSPECTED GAP AND GAP SEAL AFTER LANDING NO ICE NOTED. (M) 2 L 7 2 4F RT A10CE 2001060600006 20010606 00006 SO 2001 6 6 SIMA200102901 1 20010129 A 5101 STRUCTURE EMB 135 EMB135LR SO FUSELAGE LEAKING A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 732DH 145358 LGA - FLT 4559 - DURING CLIMB, CREW REPORTED A PRESSURIZATION LEAK IN THE FORWARD NOSE GEAR AREA. CABIN PRESSURE STARTE D TO CLIMB TO 6 PSI AT 5000 FEET. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL CHECK IAW EMB MM 21-31-00 W AS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001060600007 20010606 00007 WP 2001 6 6 ABXA010232 1 20010519 A 3230 4702971503 CONTROL CABLE DOUG DC8 DC861 3021952 WP LT MLG BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 848AX 46032 THE LEFT MAIN LANDING GEAR UPLOCK HOOK WAS NOTED TO BE IN THE FLIGHT POSITION. THE MANUAL RELEASE CABLE WAS FOUND TO BE BROKEN. MAINTENANCE INSPECTED AND REPLACED THE MANUAL RELEASE CABLE RUN ASSEMBLY IAW DC-8 MM 32-31-00. ADJUSTMENT AND TEST PROCEDURES WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2001060600008 20010606 00008 NM 2001 6 6 HNAA0100030 1 20010518 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8201 2809001 NM CARGO BAY DEFECTIVE A HNAA K NONE N FALSE WARNING CR CRUISE 1 EA 07 983HA 4925 478 NR 1 BAG BAY SMOKE DETECTOR LIGHT ILLUMINATED IN FLIGHT. REPLACED NR 1 BAG BAY SMOKE DETECTOR. 2 H 7 2 4T RT A13NM 2001060600009 20010606 00009 NM 2001 6 6 F3LA200100071 1 20010510 A 5320 FLOOR SUPPORT BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3498 23177 DURING C-6 CHECK, INSPECTION REPORTED AFT CARGO FLOOR SUPPORT BETWEEN BS 767 AND BS 787, RBL 3, CORRODED AND BENT. FABR ICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT AND ANGLES PER SRM 53-00-53, 53-10-53 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2001060600010 20010606 00010 EA 2001 6 6 COMA0160378 1 20010521 A 5320 60034017373 ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 976CA 11314 7151 THE VERTICAL J-ANGLE CLIP LOCATED INSIDE OF CBPI AT LBL 9 WAS FOUND CRACKED. PERFORMED A MAJOR REPAIR BY REPLACING VERT ICAL J-ANGLE P/N 600-34017-373 IAW WVAC EO 601R-53-2475. 2 L 7 2 4F RT A21EA 2001060600016 20010606 00016 NM 2001 6 6 2001UALA00672 1 20010430 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 434 TO 325 STRINGER 39L TO BE REPLACED WITH BELLY SKIN. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER 39L PE R SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001060600017 20010606 00017 NM 2001 6 6 2001UALA00709 1 20010512 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 FLOORBEAM WEB CRACKED STA 520 RBL 45.5. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001060600018 20010606 00018 NM 2001 6 6 2001UALA00710 1 20010514 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 FLOORBEAM UPPER CAP CORRODED STA 324, RBL 43-48. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2001060600019 20010606 00019 NM 2001 6 6 2001UALA00711 1 20010503 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 DOOR 1R FRAME LOWER CORNER CRACKED AT LOWER HINGE CUTOUT. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001060600020 20010606 00020 NM 2001 6 6 2001UALA00712 1 20010512 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 FRAME CRACKED STA 188, WL 207, COCKPIT FLOORLINE LEFT SIDE. MAJOR REPAIR ACCOMPLISHED. INSTALLED WEB REPAIR ANGLE UND ER WEB STIFFENER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001060600021 20010606 00021 NM 2001 6 6 2001UALA00713 1 20010511 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 314UA 23675 FRAME CRACKED STA 189, WL 206, RIGHT SIDE. MAJOR REPAIR ACCOMPLISHED. INSTALLED WEB REPAIR ANGLE UNDER WEB STIFFENER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001060600022 20010606 00022 NM 2001 6 6 2001UALA00714 1 20010510 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 CIRCUMFERENTIAL FRAME CRACKED STA 188, STR 17L WL 207. MAJOR REPAIR ACCOMPLISHED. INSTALLED WEB REPAIR ANGLE UNDER WEB STIFFENER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001060600024 20010606 00024 NM 2001 6 6 2001UALA00716 1 20010511 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 FLOORBEAM UPPER SURFACE CORRODED STA 294, RBL 36-51. MAJOR REPAIR ACCOMPLISHED. INSTALLED FLOORBEAM SPLICE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001060600025 20010606 00025 NM 2001 6 6 2001UALA00717 1 20010511 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 STRINGER DAMAGED STA 601-603, STR 15L. MAJOR REPAIR ACCOMPLISHED. INSTALLED J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001060600026 20010606 00026 NM 2001 6 6 2001UALA00722 1 20010505 A 5522 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE ELEVATOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7298U 21893 RT ELEVATOR UPPER SURFACE HAS SEVERAL LOOSE WORKING FASTENERS AT THE TRAILING EDGE JUST OUTBOARD OF THE ELEVATOR TAB. R EPAIRED ELEVATOR PER SRM 55-20-03. WEIGHT OF REPAIR MATERIALS CALCULATED PER SRM 51-80-07, AND IS WITHIN LIMITS. MAJOR REPAIR ACCOMPLISHED. 2 L 7 3 4F 4 F A3WE E2EA 2001060600027 20010606 00027 NM 2001 6 6 2001UALA00725 1 20010514 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 434 - 325 STRINGER 39R REQUIRES REPLACEMENT WITH BELLY SKIN. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER 3 9R IN ACCORDANCE WITH SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001060600029 20010606 00029 NM 2001 6 6 2001UALA00727 1 20010514 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 AFT PIT BODY FRAME INNER CAP IS GOUGED AT BS 727E, STR 19L. SPLICED IN NEW CAP SECTION. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001060600030 20010606 00030 NM 2001 6 6 2001UALA00728 1 20010515 A 5310 CASTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 FWD GALLEY DOOR FUSE FRAME CUTOUT, UPPER FWD CORNER CASTING IS CRACKED. REPLACED UPPER FWD SURROUND CASTING. MAJOR REP AIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001060600032 20010606 00032 NM 2001 6 6 2001UALA00731 1 20010514 A 5320 STRINGER CLIP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 434 STRINGER 34R CLIP BROKEN. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DR AWING 143T1225 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001060600033 20010606 00033 NM 2001 6 6 2001UALA00732 1 20010514 A 5330 SKIN BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BELLY SKIN BS 287 - 434 STRINGER 37L TO 37R HAS HEAVY CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW IN ACCORDANC E WITH SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001060600034 20010606 00034 NM 2001 6 6 2001UALA00733 1 20010515 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 434 STRINGER 35R CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T1228 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001060600035 20010606 00035 NM 2001 6 6 2001UALA00734 1 20010515 A 5320 SPLICE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 434 - 456 STRINGER 38R - 37 STRINGER SPLICE CRACKED AND CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALL ED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T0115 AND SRM 53-00-03 FIGURE 202. 2 L 7 2 4F 4 F RT A1NM E3NE 2001060600036 20010606 00036 NM 2001 6 6 2001UALA00735 1 20010515 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 434 STRINGER 38R DAMAGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW STRINGER IN ACCORDANCE WITH SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001060600037 20010606 00037 NM 2001 6 6 2001UALA00736 1 20010508 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 FUSELAGE SKIN DENTED AT STA 600 STR 17 LT AND STR 18 LT. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2001060600038 20010606 00038 NM 2001 6 6 2001UALA00737 1 20010504 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 564UA 26666 FUSELAGE SKIN AND STRINGER DAMAGED STA 780, STR 16 LT. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER SPLICE AND DOUBLE R. 2 L 7 2 4F 4 F RT A2NM E17NE 2001060600039 20010606 00039 NM 2001 6 6 2001UALA00738 1 20010506 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 570UA 26678 FUSELAGE SKIN DENTED FWD OF STA 1720 STR 14 LT. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2001060600040 20010606 00040 NM 2001 6 6 2001UALA00739 1 20010506 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 570UA 26678 FUSELAGE SKIN DAMAGED AT STA 1280 STR 20 RT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2001060600041 20010606 00041 NM 2001 6 6 2001UALA00740 1 20010508 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 582UA 26702 FUSELAGE SKIN DENTED AT STA 600 TO 620 STR 16 LT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2001060600042 20010606 00042 NM 2001 6 6 2001UALA00742 1 20010517 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 CABIN FLOORBEAM UPER SURFACE CORRODED STA 1681, STR RBL 12, RBL 24 TO RBL 30, WL 208. MAJOR REPAIR ACCOMPLISHED. INSTA LLED FILLERS AND DOUBLERS. 2 L 7 2 4F 4 F RT A2NM E17NE 2001060600043 20010606 00043 NM 2001 6 6 2001UALA00743 1 20010516 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 511UA 24799 CABIN FLOORBEAM WEB CORRODED STA 1425, STR RBL 70. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2001060600044 20010606 00044 NM 2001 6 6 2001UALA00744 1 20010516 A 5315 FLOORBEAM BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 996UA 22456 FLOORBEAM CRACKED AT FLOOR LEVEL AT BS 663, BL 0. REMOVED DAMAGED AREA. ACCOMPLISHED SPLICE REPAIR. MAJOR REPAIR ACCO MPLISHED. 2 L 7 2 4F 4 F A16WE E2EA 2001060600045 20010606 00045 NM 2001 6 6 2001UALA00745 1 20010516 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 944UA 26683 DENT IN FUSELAGE 30 INCHES AFT OF LT REAR ENTRY DOOR. TRIMMED OUT DAMAGE. INSTALLED DOUBLER REPAIR. MAJOR REPAIR ACCO MPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001060600046 20010606 00046 NM 2001 6 6 2001UALA00746 1 20010516 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 FWD GALLEY DOOR CUTOUT FWD FRAME CRACKED AT UPPER STOP FITTING. REMOVED DAMAGED AREA. ACCOMPLISHED REINFORCEMENT REPAI R. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001060600047 20010606 00047 NM 2001 6 6 2001UALA00747 1 20010516 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 FLOORBEAM STA 947, LBL 22 THRU RBL 18 HAS EXCESS MATERIAL REMOVED. ACCOMPLISHED SPLICE REPAIR. MAJOR REPAIR ACCOMPLISH ED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001060600048 20010606 00048 NM 2001 6 6 2001UALA00748 1 20010511 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 AFT PIT BODY FRAME INNER CAP IS DAMAGED STA 727C STR 19L. MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW CAP SECTION. 2 L 7 2 4F 4 F RT A16WE E2GL 2001071800018 20010718 00018 NE 2001 7 18 2001UALA00749 2 20010516 A 7320 7157M68P03 COMPUTER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE FAILED A UALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 29 366UA 24535 722437 NR 2 ENGINE HIGH EGT AND FUEL FLOW. *S/D* REPLACED NR 2 ENGINE. POWER MANAGEMENT COMPUTER FAILED SHOP TEST. REPLACED UNIT ON ENGINE. 2 L 7 2 4F 4 F RT A16WE E2GL 2001060600050 20010606 00050 NM 2001 6 6 2001UALA00751 1 20010511 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 FUSELAGE SKIN DENTED STA 385 TO STA 390 STR 17L. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001071800021 20010718 00021 NM 2001 7 18 2001UALA00753 1 20010502 A 2613 285N0028 CARD BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE OVERHEAT SYS FAULTY A UALA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 WP 29 663UA 27160 727330 RT ENG OVHT EICAS MESSAGE. FOLLOWED FLIGHT MANUAL PROCEDURE, REDUCED THROTTLE, MESSAGE REMAINED. SHUTDOWN ENGINE. *S/ D* THE EICAS RT ENG OVHT MSG WITHOUT DISCRETE LIGHT ON WAS CAUSED BY AFOLTS CARD M10274. THE CARD WAS REPLACED AND SYS TEM CHECKED OK. SHOP CHECK OF THE CARD CONFIRMED THE FAULT WAS A SHORTED COMPONENT ON THE CARD. 2 L 7 2 4F 4 F RT A1NM E24NE 2001060600051 20010606 00051 NM 2001 6 6 2001UALA00755 1 20010517 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 AFT PIT BODY FRAME INNER CAP IS GOUGED AT BS 727E, STR 19L. ACCOMPLISHED SPLICE REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001060600052 20010606 00052 NM 2001 6 6 2001UALA00756 1 20010517 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 CABIN FLOORBEAM UPPER CHORD IS CORRODED AT BS 1016, LBL 42 TO RBL 42, AT WL 208. REPLACED ENTIRE UPPER CHORD. MAJOR RE PAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001060600053 20010606 00053 NM 2001 6 6 2001UALA00757 1 20010518 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 FLOORBEAM WEB HAS ELONGATED FASTENER HOLES STA 324 RBL 43 WL 204. MAJOR REPAIR ACCOMPLISHED. INSTALLED FREEZE PLUGS, A NGLE REPAIR AND DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2001060600054 20010606 00054 NM 2001 6 6 2001UALA00758 1 20010513 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 FUSELAGE FRAME INNER FLANGE CORRODED STA 1640, BETWEEN STR 7L AND 8L. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAI R TO FRAME. 2 L 7 2 4F 4 F RT A2NM E17NE 2001060600055 20010606 00055 NM 2001 6 6 2001UALA00759 1 20010507 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 569UA 26677 FUSELAGE SKIN PUNCTURED STA 1816 STR 21R. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2001060600056 20010606 00056 NM 2001 6 6 2001UALA00760 1 20010510 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 568UA 26674 FUSELAGE SKIN DAMAGED STA 580 STR 9L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2001060600057 20010606 00057 NM 2001 6 6 2001UALA00761 1 20010508 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 FLOORBEAM CORRODED STA 1681 LBL 12. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND T-CAP REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2001060600058 20010606 00058 NM 2001 6 6 01FDEA00379 1 20010522 A 5315 BAC15052922 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 276FE 22041 CORROSION AT FASTENER HOLES ON FLOORBEAM AT BS 344, LBL 60 - RBL 60, WL 208. R&R PER FEDEX DWG 27-53-007 & SRM 51-30-2 2 L 7 3 4F RT A3WE 2001060600059 20010606 00059 WP 2001 6 6 MWEA010776 1 20010521 A 5347 59108205 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 NR 4 SEAT TRACK HAS CORROSION BETWEEN STATION 218 - 237. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED NEW SECTION OF SEAT TRACK, INSTALLED NEW SECTION. 2 L 7 2 4F A6WE 2001060600060 20010606 00060 WP 2001 6 6 MWEA010777 1 20010521 A 5320 9910501 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 SUBFLOOR WEB OUTBOARD OF NR 4 SEAT TRACK AT ABOUT STATION 242 HAS A CRACK FROM RIVET HOLE. STOP DRILLED 2 CRACKS, LOCAT ED AND DRILL REPAIR DOUBLER, INSTALLED PART. 2 L 7 2 4F A6WE 2001060600061 20010606 00061 WP 2001 6 6 MWEA010778 1 20010521 A 5412 9912243107 BULKHEAD DOUG DC9 DC932 3022066 WP RT PYLON965 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 RIGHT PYLON BULKHEAD WEB WALL AT STATION 965 IS CRACKED APPROXIMATELY 8 INCHES LONG OUTBOARD FROM FLOOR LINE UP. CUT OU T DAMAGED WEB, FABRICATED, LOCATED, DRILLED AND INSTALLED NEW WEB. 2 L 7 2 4F A6WE 2001060600062 20010606 00062 WP 2001 6 6 MWEA010779 1 20010521 A 5320 39132911 SPLICE DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 CORROSION ON LONGERON DOUBLER BETWEEN STATION 945 TO 965 LONGERON 30. REMOVED LONGERON SPLICE, CORROSION DRILLED UP AND INSTALLED NEW SPLICE FITTING. 2 L 7 2 4F A6WE 2001060600063 20010606 00063 WP 2001 6 6 MWEA010781 1 20010521 A 5330 59128703 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FUSELAGE SKIN IS CRACKED OUT OF ONE FASTENER HOLE AT STATION 1068 BELOW LONGERON 15 LEFT. STOP DRILLED CRACK, FABRICATE D AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001060600064 20010606 00064 WP 2001 6 6 MWEA010782 1 20010521 A 5330 591140027 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FUSELAGE SKIN CRACKED AT STATION 37 JUST BELOW LONGERON 18 ON LEFT SIDE. STOP DRILLED CRACK, FABRICATED AND INSTALLED R EPAIR DOUBLER. 2 L 7 2 4F A6WE 2001060600065 20010606 00065 WP 2001 6 6 MWEA010783 1 20010521 A 5714 59148657 FITTING DOUG DC9 DC932 3022066 WP CENTER WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 CENTER WING FORWARD SPAR LOWER ATTACH FITTINGS TO PRESSURE BULKHEAD WEB AND FUSELAGE SKIN IS CRACKED IN RADIUS. FUSELAG E STATION 606 ABOVE LONGERON 24 LEFT. REMOVED CRACKED FITTING, LOCATED, DRILLED AND INSTALLED NEW FITTING. 2 L 7 2 4F A6WE 2001060600066 20010606 00066 WP 2001 6 6 MWEA010784 1 20010521 A 5320 4912458507 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 CORROSION ON INTERCOSTAL TOP SIDE AND BOTTOM SIDE AROUND FASTENERS ALSO ON BOTH SIDES AT STATION 945 TO 965 ABOVE LONGER ON 29 RIGHT. REMOVED INTERCOSTAL, REMOVED CORROSION FROM INTERCOSTAL, FABRICATED AND INSTALLED NEW TEE ANGLE. 2 L 7 2 4F A6WE 2001060600067 20010606 00067 WP 2001 6 6 MWEA010785 1 20010521 A 5313 49122611 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FORWARD CARGO COMPARTMENT VERY DEEP GOUGES ON LONGERON 24 RIGHT LOWER VERTICAL LEG, LOCATED BETWEEN STATION 218 - 237. REMOVED SPLICE SECTION, BLENDED, LOCATED, DRILLED AND INSTALLED NEW SPLICE. 2 L 7 2 4F A6WE 2001060600068 20010606 00068 WP 2001 6 6 MWEA010786 1 20010521 A 5320 99234843 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FORWARD ENTRY SUB FLOOR WEB HAS A .5 INCH CRACK STATION 201 RBL 7. CUT OUT DAMAGE, FABRICATED, LOCATED, DRILLED AND INS TALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001060600069 20010606 00069 WP 2001 6 6 MWEA010787 1 20010521 A 5320 99234843 WEB DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FORWARD ENTRY SUB FOOR WEB HAS A HOLE STATION 178 LBL 36. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER . 2 L 7 2 4F A6WE 2001060600070 20010606 00070 WP 2001 6 6 MWEA010788 1 20010521 A 5320 99234843 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FORWARD ENTRY SUB FLOOR WEB HAS (3) 1 INCH CRACKS STATION 195 LBL 27, 30 & 40. FABRICATED AND INSTALLED NEW WEB. 2 L 7 2 4F A6WE 2001060600071 20010606 00071 WP 2001 6 6 MWEA010789 1 20010521 A 5320 99234843 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FORWARD ENTRY SUB FLOOR HAS (4) 1 INCH CRACKS STATION 195 LBL 4, 8, 11 & 14. FABRICATED, LOCATED, DRILLED AND INSTALLED WEB. 2 L 7 2 4F A6WE 2001060600072 20010606 00072 WP 2001 6 6 MWEA010790 1 20010521 A 5320 591013037 CHANNEL DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 CRACK INDICATION FOUND ON RADIOGRAPH RLB (RT LOWER VENTRAL DOOR CORNER BELOW FLOOR). VERIFIED VISUALLY THAT CRACK HAS P ROGRESSED AFT, BEYOND AN EXISTING ANGLE REPAIR. LOCATION IS ON AFT SIDE OF AFT PRESSURE BULKHEAD BELOW VENTRAL DOOR SCU FF PLATE AT RIGHT SIDE OF ANGLE EXTRUSION. REMOVED UPPER STEP PLATE, FABRICATED, LOCATED, DRILLED AND INSTALLED REPAIR ANGLE. 2 L 7 2 4F A6WE 2001060600073 20010606 00073 WP 2001 6 6 MWEA010791 1 20010521 A 5320 3916209501 BRACKET DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 NR 1 SEAT TRACK SUPPORT BRACKET AT STATION 680 IS CRACKED. REMOVED DAMAGED SUPPORT, LOCATED, DRILLED AND INSTALLED SUPP ORT BRACKET. 2 L 7 2 4F A6WE 2001060600074 20010606 00074 NM 2001 6 6 TSAA0153043 1 20010426 A 5711 6545470 SPAR BOEING 737 7372T4 1384492 NM RT WING CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 808AL 23445 EXFOLIATED CORROSION DISCOVERED ON RIGHT UNDER WING T/E AFT SPAR LOWER APPROXIMATELY 21 INCHES OUTBOARD OF WBL 355 SKIN PANEL. CLEANED AND TREATED AS EP SRM 51-10-6 PAGE 12. EVALUATED AND REPAIRED IAW ECO 3213. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4F A16WE 2001060600075 20010606 00075 WP 2001 6 6 AALA20010895 1 20010412 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 TUL - FOUND DENT WITH SHARP CREASES DOWN INSIDE, LEFT FUSELAGE STATION 290 L22L, MARKED. INSTALLED DOUBLER PER SRM 53-0 4 FIG 38 SHEET 24. (M) 2 L 7 2 4F A6WE 2001060600076 20010606 00076 WP 2001 6 6 AALA20010897 1 20010417 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 TUL - FOUND CRACK AT BASE OF CANT FRAME 1485 RIGHT JUST OUTBOARD OF STAIR ACT. REMOVED DAMAGE (CRACK), AND INSTALLED WE B SPLICE PER ESO 80559 DATED 2-23-01. (M) 2 L 7 2 4F A6WE 2001060600077 20010606 00077 WP 2001 6 6 AALA20010898 1 20010418 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CHAFED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 TUL - FOUND STATION 1401 L21R FRAME WORN FROM INCORRECT LINE STAND OFF. BLENDED OUT WEAR AREA. TREATED, PRIMED AND INS TALLED DOUBLERS PER 53-03 P5 FLT 32 SHEET 4. (M) 2 L 7 2 4F A6WE 2001060600078 20010606 00078 WP 2001 6 6 AALA20010899 1 20010413 A 5532 SKIN PANEL DOUG DC9 DC982 3022082 WP VERTICAL STAB DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 TUL - FOUND VERTICAL STAB SKIN WORN 50 PERCENT THROUGH BY DAMAGED SEAL BRACKET JUST AFT OF RIGHT ROLLER TRACK. PART REP LACEMENT. REMOVED AND REPLACED STAB SKIN PANEL WITH NEW TREATED PRIMED AND PAINTED PER SRM 51-10-3. (M) 2 L 7 2 4F A6WE 2001060600079 20010606 00079 WP 2001 6 6 AALA20010900 1 20010418 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 TUL - FOUND TEMPORARY REPAIR INSTALLED AT LONGERON 21R STATION 500. INSTALLED DOUBLER PER SRM 53-04 FIG 38, SHEET 24 AN D ESO 80559 DATED 4/10/2001. (M) 2 L 7 2 4F A6WE 2001060600080 20010606 00080 WP 2001 6 6 AALA20010901 1 20010427 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CHAFED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70425 49337 TUL - FOUND STATION 1388 CANT HAS HEAVY CHAFING AT 12:00 POSITION. BLENDED CHAFING AND INSTALLED DOUBLER/TRIPLER. REPA IR PER ESO 80559 DATED 4/25/01. (M) 2 L 7 2 4F A6WE 2001060600081 20010606 00081 WP 2001 6 6 AALA20010812 1 20010418 A 2120 CLAMP DOUG DC9 DC983 3022083 WP AC BAY LOOSE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 567AM 53293 SJD - FLT 286 - EN ROUTE SJD-ORD, DETECTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. AIR INTERRUPTED, RETURN ED SJD AND LANDED WITHOUT FURTHER INCIDENT. RE-SECURED CLAMP ON LEFT AND RIGHT SIDE PACK. LEAK CHECKED GOOD. SYSTEM G ROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001060600082 20010606 00082 WP 2001 6 6 AALA20010811 1 20010416 A 7910 CAP DOUG DC9 DC982 3022082 WP NR 1 ENGINE LOOSE A AALA K NONE K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 90511 49805 LAX - FLT 1816 - EN ROUTE LGB-LAX - SHORTLY AFTER TAKEOFF, LEFT ENGINE OIL BEGAN TO DECREASE. RAN OIL QUANTITY DECREASI NG CHECK LIST. LANDED LAX WITHOUT FURTHER INCIDENT. RE-SECURED LEFT SIDE ENGINE OIL TANK CAP. SERVICED LEFT SIDE ENGI NE OIL TANK. REPLACED MAIN OIL FILTER. LEAK CHECKED OK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001060600083 20010606 00083 WP 2001 6 6 AALA20010810 1 20010416 A 2150 20495061 ACM DOUG DC9 DC982 3022082 WP AC BAY LEAKING A AALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 21 59523 49915 ORD - FLT 2339 - EN ROUTE ORD-DFW, AFTER TAKEOFF CABIN FILLED WITH SMOKE. LEFT SIDE TEMPERATURE HIGH LIGHT ILLUMINATED. RETURNED ORD AND LANDED WITHOUT FURTHER INCIDENT. REPLACED LEFT SIDE COOLING TURBINE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001060600084 20010606 00084 WP 2001 6 6 AALA20010809 1 20010416 A 2170 1808492 COALESCER BAG DOUG DC9 DC982 3022082 WP AC BAY DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 468AA 49598 ORD - FLT 1326 - EN ROUTE ORD-TPA - SHORTLY AFTER TAKEOFF, CABIN FILLED WITH SMOKE. RETURNED ORD AND LANDED WITHOUT INC IDENT. REPLACED COALESCER BAGS. ACCOMPLISHED PACK BURNOUT PER MAINTENANCE MANUAL. NO SMOKE OR ODOR NOTED. SYSTEM GRO UND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001060600085 20010606 00085 WP 2001 6 6 AALA20010921 1 20010411 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 517AA 49894 TUL - FOUND CORROSION ON SEAT TRACK NR 6, STATION 1058. ROUTED OUT DAMAGED AREA AND INSTALLED PLUG PER SRM 53-05 PART 1 FIG 4A. (M) 2 L 7 2 4F A6WE 2001060600086 20010606 00086 WP 2001 6 6 AALA20010922 1 20010411 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 517AA 49894 TUL - FOUND CORROSION ON SEAT TRACK NR 6 STATION 1073. ROUTED OUT DAMAGED AREA AND INSTALLED PLUG PER SRM 53-05 PART 1 FIG 4A. (M) 2 L 7 2 4F A6WE 2001060600087 20010606 00087 WP 2001 6 6 AALA20010923 1 20010417 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 517AA 49894 TUL - FOUND CUSP IS CORRODED AT FORWARD SERVICE DOOR. INSTALLED DOUBLER FROM STATION 169-200 PER SRM 53-01, FIG 4. (M) 2 L 7 2 4F A6WE 2001060600088 20010606 00088 WP 2001 6 6 AALA20010924 1 20010426 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 517AA 49894 TUL - FOUND DENT IN FUSELAGE SKIN STATION 236 BETWEEN L-19L, AND LONGERON 20L. DAMAGED FUSE SKIN CUT OUT AND REPAIRED P ER SRM 53-04 FIG 38 WITH MINOR DEVIATIONS PER ESO 80559 DATED 4/24/2001. (M) 2 L 7 2 4F A6WE 2001060600089 20010606 00089 WP 2001 6 6 AALA20010925 1 20010426 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 517AA 49494 TUL - FOUND CORROSION AROUND GALLEY TIE DOWN ON SEAT TRACK NR 1 AND CORROSION ON UPPER FLANGE OF TRACK AT STATION 1279. INSTALLED NEW SEAT TRACK NR 1, STATION 1174-1309 IAW SRM 53-05. (M) 2 L 7 2 4F A6WE 2001060600090 20010606 00090 WP 2001 6 6 AALA20010926 1 20010418 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 517AA 49894 TUL - FOUND NUMEROUS AREAS OF CORROSION BEGINNING AT STATION 858 AND ENDING AT STATION 1028. REPLACED ENTIRE SEAT TRACK NR 6 FROM STATION 797 TO STATION 1036. (M) 2 L 7 2 4F A6WE 2001060600091 20010606 00091 WP 2001 6 6 AALA20010927 1 20010420 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 517AA 49894 TUL - FOUND CORROSION ON SEAT TRACK STATION 1279 UPPER FLANGE. INSTALLED NEW SEAT TRACK NR 1 FROM STATION 1174 TO STATI ON 1308 IAW SRM 53-05. (M) 2 L 7 2 4F A6WE 2001060600092 20010606 00092 WP 2001 6 6 AALA20010928 1 20010423 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 517AA 49874 TUL - FOUND CORROSION ON TOP OF SEAT TRACK NR 2 FROM STATION 1300-1309. REPLACED SEAT TRACK FROM STATION 1260-1309 PER SRM 53-05. (M) 2 L 7 2 4F A6WE 2001060600093 20010606 00093 WP 2001 6 6 AALA20010929 1 20010416 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 517AA 49894 TUL - FOUND CORROSION ON NR 6 SEAT TRACK AT STATION 579. ROUTED OUT DAMAGE AND INSTALLED PLUG REPAIR PER SRM 53-05 PART 1 FIG 4A. (M) 2 L 7 2 4F A6WE 2001060600094 20010606 00094 WP 2001 6 6 AALA20010930 1 20010412 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 517AA 49894 TUL - FOUND DOOR JAMB WEB CRACKED AT STATION 208, LONGERON 15L. FABRICATED AND INSTALLED REPAIR STRAP PER AARD 53-10-00 -11. (M) 2 L 7 2 4F A6WE 2001060600095 20010606 00095 WP 2001 6 6 AALA20010932 1 20010419 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 517AA 49494 TUL - FOUND LEFT CUSP CORRODED AT STATION 1094. CUT OUT CORRODED SECTION OF CUSP AND INSTALLED DOUBLER REPAI PER SRM 53 -01 FIG 4. (M) 2 L 7 2 4F A6WE 2001060600096 20010606 00096 WP 2001 6 6 AALA20010933 1 20010419 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 517AA 49894 TUL - FOUND CORROSION ON LEFT CUSP. INSTALLED NEW SECTION OF CUSP FROM STATION 1250-1309 PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2001060600097 20010606 00097 WP 2001 6 6 AALA20010934 1 20010426 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 517AA 49894 TUL - FOUND STATION 1338, 15 INCHES FROM OUTBOARD END, FLOORBEAM DAMAGED AROUND HOLE. INSTALLED REPAIR STRAP ON FLOORBE AM STATION 1338 RIGHT SIDE PER ESO 80559 4-24-2001. (M) 2 L 7 2 4F A6WE 2001060600098 20010606 00098 WP 2001 6 6 AALA20010935 1 20010419 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 517AA 49894 TUL - FOUND CORROSION ON CUSP. INSTALLED NEW CUSP SHEET FROM STATION 1174-1250. (M) 2 L 7 2 4F A6WE 2001060600099 20010606 00099 WP 2001 6 6 AALA20010936 1 20010419 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 517AA 49894 TUL - FOUND GOUGE IN WEB. BLENDED OUT DAMAGED AREA AND INSTALLED DOUBLER PER AARD 53-10-00-24. (M) 2 L 7 2 4F A6WE 2001060600100 20010606 00100 WP 2001 6 6 AALA20010937 1 20010419 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 517AA 49894 TUL - FOUND CUSP WEB CRACKED. INSTALLED NEW CUSP WEB PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2001060600101 20010606 00101 WP 2001 6 6 AALA20010941 1 20010423 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 517AA 49894 TUL - FOUND CRACKED FRAME. INSTALLED FRAME REPAIR PER AARD 53-10-00-33. (M) 2 L 7 2 4F A6WE 2001060600102 20010606 00102 WP 2001 6 6 AALA20010942 1 20010419 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 517AA 49894 TUL - FOUND FUSELAGE SKIN CRACKED FROM FASTENER HOLE STATION 1380, 9 INCHES ABOVE LEFT ENGINE STRUT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2001060600103 20010606 00103 WP 2001 6 6 AALA20010943 1 20010418 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7517A 49894 TUL - FOUND CORROSION BEYOND LIMITS. INSTALLED WEB REPAIR PER AARD 53-00-00-2. (M) 2 L 7 2 4F A6WE 2001060600104 20010606 00104 WP 2001 6 6 AALA20010944 1 20010417 A 5310 WINDOW FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 517AA 49894 TUL - FOUND WINDOW FRAME CRACKED AT TOP AFT CORNER. INSTALLED DOUBLER PER AARD 53-10-00-25. (M) 2 L 7 2 4F A6WE 2001060600105 20010606 00105 WP 2001 6 6 AALA20010945 1 20010418 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7517A 49894 TUL - FOUND CORROSION ON RT CUSP, STATION 617 TO STATION 674, HEAVY AT FRAME CUTOUTS AND STATION 660. REMOVED CORROSION , CUT OUT SMALL SECTION, TREATED AND PAINTED. INSTALLED DOUBLER PER SRM 53-01 FIG 4-3. (M) 2 L 7 2 4F A6WE 2001060600106 20010606 00106 NM 2001 6 6 P2EA01048 1 20010507 A 5754 6546423270A SLAT BOEING 737 7372B7 1384560 NM RT WING DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 126NJ 22884 SJO - DURING C-CHECK, RIGHT WING NR 4 SLAT, P/N 65-46423-270A, S/N BN-320 WITH DELAMINATION. (M) 2 L 7 2 4F A16WE 2001060600107 20010606 00107 NM 2001 6 6 P2EA01049 1 20010327 A 5315 FLOORBEAM BOEING 737 737244 138448U NM FUSELAGE CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 OKC - DURING C-CHECK, FOUND CORROSION ON FLOORBEAM AT BS 312, BOTTOM AFT SIDE OF UPPER CHORD AT BL 0, LBL 8 AND RBL 8. REPAIRED PER DRAWING 53-01181-1 AND 8110-3. (M) 2 L 7 2 4F A16WE 2001060600108 20010606 00108 NM 2001 6 6 P2EA01038 1 20010428 A 5320 STRAP BOEING 737 737244 138448U NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 DURING C-CHECK, INNER TEAR STRAP AT BS 1136 TO BS 1156, WL 240 ON RIGHT SIDE IS CRACKED. (M) 2 L 7 2 4F A16WE 2001060600109 20010606 00109 NM 2001 6 6 AALA01037 1 20010328 A 5753 FLAP BOEING 737 737244 138448U NM LT WING DELAMINATED A AALA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 OKC - DURING C-CHECK, LEFT WING OUTBOARD MID-FLAP INBOARD EDGE DELAMINATED, LENGTH 2 INCHES, WIDTH 1 INCH. REPAIRED IAW SRM 57-50-2 AND SRM 51-40-2. (M) 2 L 7 2 4F A16WE 2001060600110 20010606 00110 NM 2001 6 6 P2EA01043 1 20010501 A 5320 ANGLE BOEING 737 737244 138448U NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 OKC - DURING C-CHECK, L-ANGLE CRACKED AT BS 1150 WL 238, RIGHT SIDE. REPAIRED L-ANGLE IAW SRM 51-40-3. (M) 2 L 7 2 4F A16WE 2001060600111 20010606 00111 NM 2001 6 6 P2EA01045 1 20010504 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 126NJ 22884 SJO - DURING C-CHECK, FOUND LOWER FUSELAGE, FORWARD CARGO COMPARTMENT CUTOUT BS 492 BETWEEN STRINGER 22/23 RT SKIN WITH WEAR. (M) 2 L 7 2 4F A16WE 2001060600112 20010606 00112 NM 2001 6 6 P2EA01040 1 20010502 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 126NJ 22884 SJO - DURING C-CHECK, FUSELAGE STATION 307 BETWEEN STRINGER 10 AND 11 LEFT SKIN WITH CRACK. (M) 2 L 7 2 4F A16WE 2001060600113 20010606 00113 NM 2001 6 6 P2EA01044 1 20010502 A 5330 DOUBLER BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 126NJ 22884 DURING C-CHECK, LOWER FUSELAGE STRINGER 24 AND 25 LEFT, POTABLE WATER SERVICED ACCESS DOOR CUT OUT, INTERNAL DOUBLER WIT H CRACK. (M) 2 L 7 2 4F A16WE 2001060600114 20010606 00114 NM 2001 6 6 P2EA01041 1 20010426 A 5320 ANGLE BOEING 737 737244 138448U NM FUSELAGE CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 OKC - DURING C-CHECK, FOUND CORROSION ON EXTRUDED ANGLES IN RIGHT SIDE OF TORQUE BOX AT BS 1088 TO BS 1156. FOUND TO BE OUT OF LIMITS 5/1/2001. (M) 2 L 7 2 4F A16WE 2001060600115 20010606 00115 NM 2001 6 6 P2EA01046 1 20010507 A 5753 FLAP BOEING 737 7372B7 1384560 NM LT WING DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 126NJ 22884 SJO - DURING C-CHECK, FOUND LEFT WING, OUTBOARD AFT FLAP, P/N 65-46435-235, S/N BN365, WITH SEVERAL DELAMINATIONS AT THE TRAILING EDGE. (M) 2 L 7 2 4F A16WE 2001060600116 20010606 00116 NM 2001 6 6 P2EA01047 1 20010507 A 5754 SKIN BOEING 737 7372B7 1384560 NM L/E SLAT DEBONDED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 126NJ 22884 SJO - DURING C-CHECK, FOUND LEFT WING NR 2 SLAT, P/N 65-46422-281, S/N BN-60 WITH SKIN DISBONDED AT THE TRAILING EDGE SE CTION. (M) 2 L 7 2 4F A16WE 2001060600117 20010606 00117 EA 2001 6 6 MASA01027 1 20010319 A 4920 38004883 APU CNDAIR CL600 CL6002B19 EA EQUIP BAY FAILED A MASA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 07 7291Z 7291 FLT 6706 - BOS-CMH - REPORTED AN APU OIL PRESSURE CAUTION IN FLIGHT WITH THE APU SHUTTING ITSELF DOWN, ALSO REPORTED SMO KE IN THE CABIN. AFTER AN UNEVENTFUL LANDING MAINTENANCE CALLED. MAINTENANCE INSPECTED AND FOUND OIL IN THE PACK (AIR COND) SYSTEM. MAINTENANCE CLEANED UP THE OIL AND THE DISCREPANCY WAS DEFERRED. THE AIRCRAFT WAS RETURNED TO SERVICE. MAINTENANCE REMOVED AND REPLACED THE APU. OPS CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2001060600118 20010606 00118 EA 2001 6 6 MASA01038 1 20010428 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77331 7331 FLT 7331 - DURING A ROUTINE MAINTENANCE, THE CREW DISCOVERED A RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. THE EMERGENC Y LIGHT WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001060600119 20010606 00119 EA 2001 6 6 MASA01039 1 20010429 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7264V 7264 DURING AN OVERNIGHT INSPECTION, THE CREW FOUND A RIGHT AFT UPPER EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPL ACED THE LIGHT AND OPS CHECKED GOOD. WORK ORDER NR 1010428015. (M) 2 L 7 2 4F RT A21EA 2001060600120 20010606 00120 EA 2001 6 6 MASA01040 1 20010430 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77195 7195 FLT 7195 - DURING OVERNIGHT MAINTENANCE, THE CREW FOUND A RIGHT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE B ULB AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2001060600121 20010606 00121 NM 2001 6 6 GAIA01127ST 1 20010505 A 5312 BULKHEAD BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING MAINTENANCE, TWO CRACKS WERE DISCOVERED PROTRUDING OUT OF FASTENERS HOLES AT BULKHEAD BS 178 WL 238 LBL 12-14. A CCOMPLISHED BS 178 BULKHEAD REPAIR BS 178 WL 238 LBL 12-14 IAW B727 SRM 53-10-9 FIG 4. (M) 2 L 7 3 4F A3WE 2001060600122 20010606 00122 NM 2001 6 6 GAIA010128ST 1 20010505 A 5312 BULKHEAD BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING MAINTENANCE, 3 CRACKS WERE DISCOVERED PROTRUDING OUT OF FASTENER HOLES AT BULKHEAD BS 178 WL 238 RBL 08-16. ACCO MPLISHED BS 178 BULKHEAD REPAIR BS 178 WL 238 RBL 08-1 6 IAW B727 SRM 53-10-9 FIG 4. (M) 2 L 7 3 4F A3WE 2001060600123 20010606 00123 NM 2001 6 6 GAIA01129ST 1 20010505 A 5312 BULKHEAD BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING MAINTENANCE A .375 INCH CRACK PROTRUDING OUT OF VERTICAL STIFFENER IN BULKHEAD WEB WAS DISCOVERED AT BS 178 WL 19 8 RBL 01. ACCOMPLISHED BS 178 BULKHEAD REPAIR, BS 178 WL 198 RBL 01 IAW B727 SRM 53-10-9 FIG 4. (M) 2 L 7 3 4F A3WE 2001060600124 20010606 00124 NM 2001 6 6 GAIA01130ST 1 20010505 A 5312 BULKHEAD BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING MAINTENANCE, A CRACK WAS DISCOVERED AT BS 178 WL 218 RBL 6-20 AT STIFFENER 1R. ACCOMPLISHED BS 178 BULKHEAD WEB REPAIR BS 178 WL 218 RBL 6-20 IAW KITTY HAWK WORK CARD 2210 FIG 2 REV DATED JUNE 15, 1994. (M) 2 L 7 3 4F A3WE 2001060600125 20010606 00125 NM 2001 6 6 GAIA01131ST 1 20010505 A 5320 WEB BOEING 727 727223 1384074 NM AIRSTAIRS CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING MAINTENANCE, TWO CRACKS WERE DISCOVERED IN AFT AIRSTAIR BY UPPER LIGHTENING HOLE BELOW AIRSTAIR ACTUATOR BEHIND T HE DOUBLER AT BS 1263. ACCOMPLISHED WEB REPAIR BS 1263 RT IAW B727 SRM 51-40-2 FIG 1. (M) 2 L 7 3 4F A3WE 2001060600126 20010606 00126 NM 2001 6 6 GAIA01132ST 1 20010505 A 5312 PRESSURE PANEL BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING MAINTENANCE IT WAS DISCOVERED THAT THE INNER WEB IS CRACKED IN THE NOSE WHEEL WELL LEFT SIDE AT BS 277, WL 160 IN SIDE THE LIGHTENING HOLE. ACCOMPLISHED INNER WEB REPAIR BS 277 LEFT WL 160 IAW B727 SRM 53-10-2 FIG 1 SRM 51-30-2. (M) 2 L 7 3 4F A3WE 2001060600127 20010606 00127 NM 2001 6 6 GAIA01133ST 1 20010505 A 5312 PRESSURE PANEL BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING MAINTENANCE, A CRACK WAS DISCOVERED IN THE NOSE WHEEL WELL UPPER PRESSURE WEB AT BS 243. ACCOMPLISHED NOSE WHEEL WELL UPPER PRESSURE WEB REPAIR BS 243 RBL 15 IAW B727 SRM 51-40-2 FIG 1. (M) 2 L 7 3 4F A3WE 2001060600128 20010606 00128 NM 2001 6 6 GAIA01134ST 1 20010505 A 5312 PRESSURE PANEL BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, A CRACK WAS DISCOVERED AT FASTENER ON THE NOSE WHEEL WELL LEFT SIDEWALL BS 240, BELOW PANEL CUT OUT. ACCOMPLISHED NOSE WHEEL WELL LEFT SIDE PRESSURE WEB REPAIR BS 240 IAW B727 SRM 51-40-2 FIG 1. (M) 2 L 7 3 4F A3WE 2001060600129 20010606 00129 NM 2001 6 6 GAIA01135ST 1 20010505 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, A CRACK WAS DISCOVERED AT RBL 45.5 LONGITUDINAL FLOORBEAM UPPER CHORD AT BS 760, WL 207. ACCOM PLISHED LONGITUDINAL FLOORBEAM UPPER CHORD REPLACEMENT BS 760-848 RBL 45.5 IAW B727 SRM 51-30-5 AND SRM 51-30-2. (M) 2 L 7 3 4F A3WE 2001060600130 20010606 00130 NM 2001 6 6 GAIA01136ST 1 20010505 A 5311 FRAME BOEING 727 727223 1384074 NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, A FRAME WAS DISCOVERED DENTED AT BS 700 STRINGER 24 LEFT. ACCOMPLISHED FUSELAGE FRAME REPAIR B S 700 LEFT AT STRINGER 24L IAW B727 SRM 53-10-4 FIG 2. (M) 2 L 7 3 4F A3WE 2001060600131 20010606 00131 NM 2001 6 6 GAIA01137ST 1 20010505 A 5311 FRAME BOEING 727 727223 1384074 NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, A FRAME WAS DISCOVERED DENTED AT BS 500, BETWEEN STRINGER 24-25 RT. ACCOMPLISHED FUSELAGE FRAM E REPAIR BS 500 RT AT STRINGER 24R AND 25R IAW B727 SRM 53-10-4 FIG 2. (M) 2 L 7 3 4F A3WE 2001060600132 20010606 00132 NM 2001 6 6 GAIA01138ST 1 20010505 A 5311 FRAME BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC, INSPECTION A FRAME WAS DISCOVERED CRACKED AT BS 910 STRINGER 14 RT. ACCOMPLISHED FUSELAGE FRAME REPAIR BS 910 AT STRINGER 14 RT IAW B727 SRM 53-10-2 AND SRM 51-30-2. (M) 2 L 7 3 4F A3WE 2001060600133 20010606 00133 NM 2001 6 6 GAIA01139ST 1 20010505 A 5320 GUSSET BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION IT WAS DISCOVERED AT BS 825.95 THE LEFT LOWER FRAME GUSSET CRACKED AT WL 200, LBL 50. ACCOMPLIS HED BS 825.95 FUSELAGE FRAME GUSSET REMOVAL AND REPLACEMENT BS 825-95 WL 200 LBL 50 IAW B727 SRM 51-30-2. (M) 2 L 7 3 4F A3WE 2001060600134 20010606 00134 SO 2001 6 6 SIMA20011265 1 20010506 A 3240 211118 SHUTTLE VALVE EMB 145 EMB145 SO BRAKE SYS DEFECTIVE A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 606AE 145062 ORD - FLT 3331 - DURING CRUISE, CREW NOTED HYDRAULIC SYSTEM ONE QUANTITY IN THE YELLOW. PRESSURE WAS WITHIN LIMITS. CR EW DIVERTED TO ORD, EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE BRAKE S HUTTLE VALVE IAW EMB MM AND SERVICED THE NR 1 HYDRAULIC SYSTEM. OPS AND LEAK CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001060600135 20010606 00135 SO 2001 6 6 SIMA20011271 1 20010507 A 2740 3621001007 CONTROL UNIT EMB 145 EMB145LR SO HORIZ STAB INOPERATIVE A SIMA K NONE F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 21 647AE 145222 ORD - FLT 4366 - CREW REPORTED A PITCH TRIM 1 INOPERATIVE MESSAGE ON EICAS AND BOTH MAIN SWITCHES INOPERATIVE. MAINTENA NCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001060600136 20010606 00136 SO 2001 6 6 SIMA200111205 1 20010422 A 5315 FLOORBEAM EMB 145 EMB145LR SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 635AE 145158 ABI - FOUND LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS AT FRAME 20. REPAIRED FRAME IAW EMBRAER SRM 145/ 1142 REV 12 CHAPTER 53-21-10 PAGE 208. (M) 2 L 7 2 4T RT T00011AT 2001060600137 20010606 00137 SO 2001 6 6 SIMA20011261 1 20010506 A 2611 WARNING LIGHT EMB 135 EMB135LR SO COCKPIT INTERMITTENT A SIMA K NONE N FALSE WARNING UK UNKNOWN 1 SW 21 722AE 145287 BOS - FLT 4936 - CREW REPORTED THE LAVATORY SMOKE LIGHT TO BE INTERMITTENT. PUT ON MEL AT THIS TIME. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001060600138 20010606 00138 SO 2001 6 6 SIMA200112277 1 20010502 A 2760 145330022409 CONTROL VALVE EMB 135 EMB135LR SO SPOILER FAILED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 730AE 145346 CMH - FLT 4857 - DURING TAKEOFF ROLL, CREW REPORTED A SPOILER DISAGREE MESSAGE ON EICAS. TAKEOFF WAS ABORTED AND AIRCRA FT WAS RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE SPOILER CONTROL VALVE IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001060600139 20010606 00139 SO 2001 6 6 SIMA20011303 1 20010510 A 2916 RESERVOIR EMB 135 EMB135LR SO HYD SYSTEM LACK OF LUBE A SIMA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 704PG 145174 LGA - FLT 4512 - DURING APPROACH, CREW REPORTED HYDRAULIC QUANTITY LOW ADVISORY ON EICAS, DECLARED EMERGENCY INTO LGA, N O FURTHER INCIDENTS REPORTED. MAINTENANCE SERVICED THE HYDRAULIC RESERVOIR IAW EMB MM. AIRCRAFT WAS RETURNED TO SERVIC E. (M) 2 L 7 2 4F RT TOOO11AT 2001060600140 20010606 00140 SO 2001 6 6 SIMA20011305 1 20010510 A 2720 RUDDER PEDAL EMB 135 EMB135ER 3260203 SO COCKPIT STIFF A SIMA C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 SW 21 713AE 145249 BOS - FLT 4942 - DURING TAKEOFF ROLL, THE CREW NOTED THE RUDDER PEDALS WERE STIFF TO OPERATE. TAKEOFF WAS ABORTED AND A IRCRAFT WAS RETURNED TO THE GATE. NO FAILURES FOR THE RUDDER SYSTEM WERE REPORTED. JUST BEFORE AIRCRAFT RETURNED TO GA TE THE YAW DAMPNER FAILED. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED T O SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001060600141 20010606 00141 EU 2001 6 6 SIMA200111711 1 20010412 A 5320 S5367800821602 ANGLE AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AM 440 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE RIGHT ZEE MEMBER BETWEEN FRAMES 39 AND 44 CORRODED. MAINTENANC E REMOVED AND REPLACED THE ZEE MEMBER IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001060600142 20010606 00142 EU 2001 6 6 SIMA200111710 1 20010412 A 5320 S5367131830401 SILL AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AM 440 DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE SERVICE DOOR SILL PLATE WEB CORRODED BETWEEN FRAMES 36 AND 39. MAINT ENANCE REMOVED AND REPLACED THE WEB IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001060600143 20010606 00143 EU 2001 6 6 SIMA20011179 1 20010412 A 5320 S5367121729402 SILL AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AM 440 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE PAX DOOR WEB BETWEEN FRAMES 36 AND 39 CORRODED. MAINTENANCE RE MOVED AND REPLACED THE WEB IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001060600144 20010606 00144 EU 2001 6 6 SIMA20011178 1 20010412 A 5347 E95300013019 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AM 440 SAW - DURNIG CPCP-2 INSPECTION MAINTENANCE REPORTED THE RIGHT FLIGHT ATTENDANT AND LEFT FLIGHT ATTENDANT SEAT TRACKS COR RODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001060600145 20010606 00145 EU 2001 6 6 20010606SG001 1 20010412 A 5347 E95300013023 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AM 440 SAW - DURNIG CPCP-2 INSPECTION MAINTENANCE REPORTED THE RIGHT FLIGHT ATTENDANT AND LEFT FLIGHT ATTENDANT SEAT TRACKS COR RODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001060600146 20010606 00146 EU 2001 6 6 SIMA20011177 1 20010412 A 5320 S5367800826802 INTERCOSTAL AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AM 440 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE THE LEFT INTERCOSTALS BETWEEN FRAMES 38 AND 40 CORRODED, AND THE RIGHT INTER COSTALS BETWEEN FRAMES 36 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTALS IAW SRM 51-25-02. AIRCRAF T WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001060600147 20010606 00147 EU 2001 6 6 20010606SG002 1 20010412 A 5320 S5367800021401 INTERCOSTAL AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AM 440 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE THE LEFT INTERCOSTALS BETWEEN FRAMES 38 AND 40 CORRODED, AND THE RIGHT INTER COSTALS BETWEEN FRAMES 36 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTALS IAW SRM 51-25-02. AIRCRAF T WAS RETURNED TO SERVICE. REF SIMA20011177. (M) 2 H 7 2 4T RT A53EU 2001060600148 20010606 00148 EU 2001 6 6 20010606SG003 1 20010412 A 5320 S5367800920102 INTERCOSTAL AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AM 440 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE THE LEFT INTERCOSTALS BETWEEN FRAMES 38 AND 40 CORRODED, AND THE RIGHT INTER COSTALS BETWEEN FRAMES 36 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTALS IAW SRM 51-25-02. AIRCRAF T WAS RETURNED TO SERVICE. REF SIMA20011177. (M) 2 H 7 2 4T RT A53EU 2001060600149 20010606 00149 EU 2001 6 6 20010606SG004 1 20010412 A 5320 S5367800826902 INTERCOSTAL AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AM 440 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE THE LEFT INTERCOSTALS BETWEEN FRAMES 38 AND 40 CORRODED, AND THE RIGHT INTER COSTALS BETWEEN FRAMES 36 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTALS IAW SRM 51-25-02. AIRCRAF T WAS RETURNED TO SERVICE. REF SIMA20011177. (M) 2 H 7 2 4T RT A53EU 2001060600150 20010606 00150 EU 2001 6 6 SIMA20011176 1 20010412 A 5320 S5367800826401 GUSSET AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AM 440 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT GUSSET BETWEEN FRAMES 40 AND 41 CORRODED. MAINTENANCE REM OVED AND REPLACED THE GUSSET IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001060600151 20010606 00151 EU 2001 6 6 SIMA20011175 1 20010412 A 5315 S5367240620802 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AM 440 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAMS 36, 38, 39 AND 40 CORRODED. MAINTENANCE REMOVED AND REPL ACED FLOORBEAMS 36, 38, AND 39 IAW SRM 51-25-02. MAINTENANCE REPAIRED FLOORBEAM 40 IAW SRM 53-00-00 FIGURE 436. AIRCRA FT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001060600152 20010606 00152 EU 2001 6 6 20010606SG005 1 20010412 A 5315 S5367240725201 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AM 440 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAMS 36, 38, 39 AND 40 CORRODED. MAINTENANCE REMOVED AND REPL ACED FLOORBEAMS 36, 38, AND 39 IAW SRM 51-25-02. MAINTENANCE REPAIRED FLOORBEAM 40 IAW SRM 53-00-00 FIGURE 436. AIRCRA FT WAS RETURNED TO SERVICE. REF SIMA20011175. (M) 2 H 7 2 4T RT A53EU 2001060600153 20010606 00153 EU 2001 6 6 20010606SG006 1 20010412 A 5315 S5367240825402 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AM 440 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAMS 36, 38, 39 AND 40 CORRODED. MAINTENANCE REMOVED AND REPL ACED FLOORBEAMS 36, 38, AND 39 IAW SRM 51-25-02. MAINTENANCE REPAIRED FLOORBEAM 40 IAW SRM 53-00-00 FIGURE 436. AIRCRA FT WAS RETURNED TO SERVICE. REF SIMA20011175. (M) 2 H 7 2 4T RT A53EU 2001060600154 20010606 00154 EU 2001 6 6 20010606SG007 1 20010412 A 5315 S5367240921802 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AM 440 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAMS 36, 38, 39 AND 40 CORRODED. MAINTENANCE REMOVED AND REPL ACED FLOORBEAMS 36, 38, AND 39 IAW SRM 51-25-02. MAINTENANCE REPAIRED FLOORBEAM 40 IAW SRM 53-00-00 FIGURE 436. AIRCRA FT WAS RETURNED TO SERVICE. REF SIMA20011175. (M) 2 H 7 2 4T RT A53EU 2001060600155 20010606 00155 EU 2001 6 6 SIMA20011174 1 20010412 A 5320 S5367121729801 TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AM 440 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE SERVICE DOOR AND PAX DOOR DRAIN TRACKS CORRODED. MAINTENANCE R EMOVED AND REPLACED THE DRAIN TRACKS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001060600156 20010606 00156 EU 2001 6 6 20010606SG008 1 20010412 A 5320 S5367121733601 TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AM 440 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE SERVICE DOOR AND PAX DOOR DRAIN TRACKS CORRODED. MAINTENANCE R EMOVED AND REPLACED THE DRAIN TRACKS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20011174. (M) 2 H 7 2 4T RT A53EU 2001060600157 20010606 00157 EU 2001 6 6 SIMA200112203 1 20010502 A 7600 LIGHT SAAB SF340 340B 7860101 EU COCKPIT INOPERATIVE A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 266AE 340B266 PSP - FLT 3098 - LEFT APR LIGHT FAILED TO ILLUMINATE ON TAKEOFF WHEN APR SELECTED ON. ABORTED TAKEOFF, MEL 76-2. REF L OG PAGE 1019987. (M) 2 L 7 2 4T RT A52EU 2001060600158 20010606 00158 EU 2001 6 6 SIMA200111802 1 20010428 A 3350 85 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SW 21 301AE 340B301 LAX - FLT 3067 - EMERGENCY ARMED LIGHT INOPERATIVE ON FLIGHT ATTENDANTS PANEL. REMOVED AND REPLACED BULB IAW AMM 23-30- 00. (M) 2 L 7 2 4T RT A52EU 2001060600159 20010606 00159 EU 2001 6 6 SIMA20011173 1 20010427 A 2450 BUSS SAAB SF340 340B 7860101 EU COCKPIT FAILED A SIMA C ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 SW 21 392AE 340B392 ABI - FLT 3328 - CREW REPORTED DURING TAKEOFF ROLL, THE RIGHT MAIN BUSS FAILED. TAKEOFF WAS ABORTED. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. GROUND RUN OF AIRCRAFT SHOWED NO PROBLEMS. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001060600160 20010606 00160 EU 2001 6 6 SIMA20011161 1 20010426 A 3350 L235A01711 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST UK UNKNOWN 1 SW 21 902AE 340B269 DFW - FLT 3790 - CREW REPORTED THE EMERGENCY EXIT LIGHT LOCATED DIRECTLY BELOW CABIN FLIGHT ATTENDANT HANDSET TO BE INOP ERATIVE. MAINTENANCE REPLACED BULBS AT FLIGHT ATTENDANT STATION. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVI CE. (M) 2 L 7 2 4T RT A52EU 2001060600161 20010606 00161 EU 2001 6 6 SIMA200111503 1 20010425 A 2450 POWER UNIT SAAB SF340 340B 7860101 EU ELEC SYS FAILED A SIMA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 SW 21 236AE 340B236 ALB - FLT 4873 - DURING FLIGHT, THE LEFT MAIN AND ESSENTIAL BUSSES FELL OFF LINE. HYDRAULIC PUMP FAILED AND GEAR DID NO T COME DOWN. PERFORMED EMERGENCY EXTENSION OF GEAR. LANDED IN ALB WITHOUT FLAP AND LOST NOSE WHEEL STEERING AND BRAKES , PDU P/N A2042C LEFT, P/N A2043C RIGHT. REMOVED AND REPLACED LEFT AND RIGHT POWER DISTRIBUTION UNTIS IAW AMM. OPS CHE CK GOOD. (M) 2 L 7 2 4T RT A52EU 2001060600162 20010606 00162 EU 2001 6 6 SIMA20011144 1 20010424 A 2121 M4401D8A FAN SAAB SF340 340B 7860101 EU E/E BAY FAILED A SIMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 343SB 340B343 PVD - FLT 4528 - FOUND CREW REPORTED THE AVIONICS SMOKE LIGHT ILLUMINATED DURING TAXI. AIRCRAFT WAS RETURNED TO THE GAT E. PUT ON MEL AT THIS TIME. MAINTENANCE REMOVED AND REPLACED THE AVIONICS FAN MOTOR IAW AMERICAN EAGLE WORK CARD 1716. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001060600163 20010606 00163 EU 2001 6 6 SIMA20011147 1 20010424 A 3350 1317 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 326AE 340B326 BOS - FLT 4598 - EMERGENCY LIGHTS OVER SEATS 4A AND 7A ARE INOPERATIVE. MAINTENANCE REPLACED LIGHT BULBS OVER SEAT 4A A ND 7A IAW AMM 33-60-00. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001060600164 20010606 00164 EU 2001 6 6 SIMA20011121 1 20010422 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 240DS 340B240 RDU - MAINTENANCE REPORTED SEVERAL EMERGENCY LIGHT IN THE CABIN TO BE INOPERATIVE. POWER SUPPLY UNIT 21LN WAS REMOVED A ND REPLACED IAW SAAB MM 33-50-10. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001060600165 20010606 00165 EU 2001 6 6 SIMA200111204 1 20010422 A 3350 GE85 LIGHT SAAB SF340 340B 7860101 EU COCKPIT INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 174AE 340B174 DFW - FLT 3344 - EMERGENCY SWITCH PUSHBUTTON BACK LIGHTING ON FA PANEL INOPERATIVE. RELAMPED, OPS CHECK GOOD IAW AMM. (M) 2 L 7 2 4T RT A52EU 2001060600166 20010606 00166 EU 2001 6 6 SIMA20011102 1 20010420 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN MALFUNCTIONED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 243AE 340B243 BOS - FLT 4902 - CREW REPORTED THE OVERHEAD EMERGENCY LIGHT AT ROW 8A IS INOPERATIVE. MAINTENANCE COULD NOT DUPLICATE D ISCREPANCY. OPS CHECK OF EMERGENCY LIGHTS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001060600167 20010606 00167 EU 2001 6 6 SIMA20011098 1 20010419 A 3350 66362 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 375AE 340B375 DFW - FLT 3913 - FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING AT ROW 4/5 ARE INOPERATIVE. LIGHT PUT ON MEL AT THIS TIM E. MAINTENANCE REPLACED THE FLOOR PROXIMITY LIGHT STRIP. OPS CHECK WAS GOOD IAW SAAB MM 33-50-20 AND AIRCRAFT WAS RETU RNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001060600168 20010606 00168 EU 2001 6 6 SIMA20011082 1 20010418 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 901AE 340B401 DFW - FLT 3301 - CREW REPORTED SEVERAL FLOOR PROXIMITY EMERGENCY LIGHTS TO BE INOPERATIVE AT SEATS 4A, 7A, 10A AND 12A. PUT ON MEL AT THIS TIME. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPS CHECK WAS GOOD IAW SAAB MM 33-15-30. AIRCR AFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001060600169 20010606 00169 EU 2001 6 6 SIMA20011083 1 20010418 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 371AE 340B371 DFW - FLT 3337 - CREW REPORTED THE EMERGENCY EXIT FLOOR STRIP LIGHTING TO BE INOPERATIVE AT SEATS 4A, 7A, 10A AND 14A. PUT ON MEL AT THIS TIME. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPS CHECK WAS GOOD IAW SAAB MM 33-50-00 AND 33-1 5-30. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001060600170 20010606 00170 EU 2001 6 6 SIMA20011084 1 20010418 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 298AE 340B298 BGR - FLT 4922 - FLIGHT ATTENDANT REPORTED THE EMERGENCY LIGHT ARM SWITCH WILL NOT ILLUMINATE. MAINTENANCE REPLACED COC KPIT LIGHT SWITCH 5LN IAW SAAB MM. OPS CHECK WAS GOOD IAW SAAB MM 33-50-00. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001060600171 20010606 00171 2001 6 6 SIMA20011063 4 20010416 A 3417 6227713004 COMPUTER SAAB SF340 340B 7860101 EU COCKPIT FAILED A SIMA A UNSCHED LANDING O OTHER UK UNKNOWN 1 SW 21 390AE 340B390 DFW - FLT 3253 - CAPTAINS EFIS TUBE WENT BLANK, THEN BACK ON SEVERAL TIMES IN FLIGHT. AIRCRAFT WAS RETURNED TO DFW. MA INTENANCE REMOVED AND REPLACED THE DATA PROCESSING UNIT IAW SAAB MM. OPERATIONAL CHECK WAS GOOD IAW SAAB MM 34-24-00 AN D AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001060600172 20010606 00172 EU 2001 6 6 SIMA200110404 1 20010411 A 3411 PITOT LINE SAAB SF340 340B 7860101 EU PITOT SYS CONTAMINATED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 903AE 340B282 DFW - FLT 3299 - FIRST OFFICER AIRSPEED INDICATOR FAILED TAKEOFF. CLEANED WATER FROM F/O PITOT STATIC SYSTEM IAW AMM. OPS CHECK GOOD IAW AMM. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001060600173 20010606 00173 EU 2001 6 6 SIMA20011024 1 20010412 A 3350 6839BPF LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 354SB 340B354 BTV - FLT 4636 - CREW REPORTED AN EMERGENCY FLOOR LIGHT AT ROW 5 TO BE INOPERATIVE. PUT ON MEL AT THIS TIME. MAINTENAN CE REPLACED THE BULB AT ROW 5 EMERGENCY FLOOR LIGHT. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001060600174 20010606 00174 EU 2001 6 6 SIMA200110103 1 20010411 A 3350 66362 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 400BR 340B400 DFW - FLT 3913 - FLOOR PROX LIGHT AT 4A ISSUED MEL 33-15-3 AUTH 040303 CAT C. RAI FLOOR PROX LIGHT STRIP IAW AMM 33-50- 20. OPS CHECKS GOOD. MEL ITEM RESTORED. REF LOG PAGE 1290613 ITEM NR 4. (M) 2 L 7 2 4T RT A52EU 2001060600175 20010606 00175 EU 2001 6 6 SIMA20011152 1 20010425 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 550LL 550 JAN - FLT 3578 - CREW REPORTED SEVERAL EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY PACK AT POWER SUPPLY UNIT 62WL. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001060600176 20010606 00176 EU 2001 6 6 SIMA200112202 1 20010502 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 431AT 431 MIA - FLT 5209 - SOME OF THE EMERGENCY LIGHTS COME ON WHEN THE SYSTEM IS ARMED. REPLACED BATTERY PACK AT POWER SUPPLY 7 3WL IAW AMM. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 2001060600177 20010606 00177 EU 2001 6 6 SIMA20011092 1 20010419 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 541AM 541 JAN - FLT 3578 - CREW REPORTED THE AFT EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT 62WL. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001060600178 20010606 00178 EU 2001 6 6 SIMA20011058 1 20010415 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 540AE 540 DFW - DURING PHASE 3 INSPECTION, MAINTENANCE REPORTED THE AFT FLOOR PROXIMITY LIGHTS AND AN EXIT SIGN WERE INOPERATIVE. BATTERY PACK WAS REMOVED AND REPLACED IN POWER SUPPLY UNIT 73WL. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVI CE. (M) 2 H 7 2 4T RT A53EU 2001060600179 20010606 00179 EU 2001 6 6 SIMA20011045 1 20010414 A 3350 1031309111 LIGHT AEROSP ATR72 ATR72212 EU CABIN BROKEN A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 260AE 263 MIA - FLT 9221 - CREW REPORTED ONE FLOOR PROXIMITY LIGHT AT ROW 15 IS BROKEN. MAINTENANCE REPLACED EMERGENCY LIGHT AT R OW 15. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001060700001 20010607 00001 CE 2001 6 7 GLBA2001102 1 20010517 A 3610 TUBE BEECH 1900 1900D 1154162 CE BLEED AIR DAMAGED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 240GL UE240 CABIN ALTITUDE HI AND DUAL BLEED AIR FAILURE ANNUNCIATORS ILLUMINATED DURING CLIMB. INSPECTED AND FOUND DUCT ASSEMBLY L OOSE AND EVA TUBING DAMAGED. TIGHTENED DUCT AND REPAIRED EVA TUBING. 2 L 7 2 4T RT A24CE 2001060700002 20010607 00002 NE 2001 6 7 SIMA200106701 2 20010308 A 7210 OIL SYSTEM SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE NR 1 GEARBOX FLUCTUATES A SIMA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SW 21 313AE 340B313 BTV - FLT 4750 - NOTED LOW NR 1 PGB OIL TEMP FOLLOWED BY FLUCTUATING NR 1 PGB OIL PRESS AND NR 1 ENGINE OIL PRESS, APPLI ED ENGINE SHUTDOWN PROCEDURE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 2001060700003 20010607 00003 WP 2001 6 7 MWEA010792 1 20010521 A 5320 3916209502 BRACKET DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 NR 4 SEAT TRACK SUPPORT BRACKET AT STATION 680 IS CRACKED. REMOVED DAMAGED SUPPORT, LOCATED, DRILLED AND INSTALLED SUPP ORT. 2 L 7 2 4F A6WE 2001060700004 20010607 00004 WP 2001 6 7 MWEA010793 1 20010521 A 5320 49125151 CLIP DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 UPPER FUSELAGE SHOVEL CLIP HAS BARE METAL AND LIGHT CORROSION STATION 996 LONGERON 6 LEFT. REMOVED OLD SHOVEL CLIP, LOC ATED, DRILLED AND INSTALLED NEW SHOVEL CLIP. 2 L 7 2 4F A6WE 2001060700005 20010607 00005 NM 2001 6 7 F3LA200100073 1 20010510 A 5320 FLOOR SUPPORT BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3498 23177 DURING C-6 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR SUPPORT, LT OF CENTER LINE BETWEEN BS 727 AND 727A, CO RRODED. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPPORT CHANNEL, SPLICE ANGLE AND STRAP PER SRM 53-60-53, SRM 57-40 -02 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2001060700006 20010607 00006 2001 6 7 DHL2001801006 4 20010522 A 3425 2587909903 ADI DOUG DC8 DC873F 302199F WP COCKPIT DEFECTIVE A DHLA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 801DH 46033 F/O ADI JUMPING UP & DOWN FROM 2 DEG TO 7 DEG AT A TIME. ALL PHASES OF FLIGHT. REMOVED AND REPLACED F/O ADI INDICATOR. OPS CHECK GOOD PER 34-29-0. 2 L 7 4 4F RT 4A25 2001060700007 20010607 00007 WP 2001 6 7 DHL2001805009 1 20010518 A 2742 30042502 ACTUATOR DOUG DC8 DC873F 302199F WP STABILIZER FAILED A DHLA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 805DH 46125 CONTROL WHEELS TRIM SWITCHES INOPERATIVE. REMOVED AND REPLACED LEFT LONG TRIM ACTUATOR. OP CHECKS GOOD PER M/M. 2 L 7 4 4F RT 4A25 2001060700008 20010607 00008 2001 6 7 DHL2001804009 4 20010519 A 2210 AUTOPILOT SYS DOUG DC8 DC873F 302199F WP COCKPIT MALFUNCTIONED A DHLA K NONE F FLT CONT AFFECTED DE DESCENT 1 SO 01 804DH 46124 AUTOPILOT MADE AN UNCOMMANDED DESCENT FROM 4000 FT LEVEL FLIGHT. COULD NOT DUPLICATE ON GROUND. AUTOPILOT CHECKS GOOD IAW DC-8 MM 22-10-0. BITE CHECK ALSO GOOD. 2 L 7 4 4F RT 4A25 2001060700009 20010607 00009 2001 6 7 DHL2001807017 4 20010516 A 2210 LINKAGE DOUG DC8 DC873 302199C WP AUTOPILOT SYS OUT OF POSITION A DHLA K NONE O OTHER CL CLIMB 1 SO 01 807DH 45990 AUTOPILOT EXCEEDED 35 DEG BANK DURING TURNS. REPOSITIONED LINKAGE ABOVE SERVO MICROSWITCH. OPS CK''D OK IAW MM 22-20-0 . 2 L 7 4 4F RT 4A25 2001060700010 20010607 00010 WP 2001 6 7 MWEA010810 1 20010521 A 5730 99117801 SKIN DOUG DC9 DC914 3022034 WP RT WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 RIGHT WING LEADING EDGE HAS ONE DENT AT APPROXIMATELY XRS 353 WITH CRACK INDICATIONS. REMOVED DAMAGE AND INSTALLED DOUB LER. 2 L 7 2 4F A6WE 2001060700011 20010607 00011 WP 2001 6 7 MWEA010811 1 20010521 A 5730 59121614 SKIN DOUG DC9 DC914 3022034 WP RT WING DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 RIGHT WING WALK AREA HAS A DENT .075 DEEP AND FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA, REMOVED DAMAGED CORNER A ND MADE NEW REPAIR PARTS. 2 L 7 2 4F A6WE 2001060700012 20010607 00012 WP 2001 6 7 ZW0A0102102 1 20010518 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 907TW 49165 DURING CHECK-C MAINT THE CABIN FLOOR SUPPORT HAD CORROSION AT LBL 56 TO 59, STA 1140 AND 1168. INSTALLED NEW FLOOR SUPP ORT AT BOTH LOCATION PER SRM 51-30-5. 2 L 7 2 4F A6WE 2001060700013 20010607 00013 WP 2001 6 7 ZW0A0102103 1 20010518 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 907TW 49165 DURING CHECK-C MAINT FOUND MEMBRANE/FLOOR PAN CORRODED, STA 1136 TO 1174, LBL 50-59. REMOVED AND REPLACED WEB SECTION P ER SRM 51-70-4, FIG 2 SHEET 1 PAGE 5. 2 L 7 2 4F A6WE 2001060700014 20010607 00014 WP 2001 6 7 ZW0A0102104 1 20010519 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 907TW 49165 DURING CHECK-C MAINT FOUND CORROSION ON NUMBER 3 CABIN CHAIR TRACK, STA 1261 TO 1308, 1155 TO 1193, 1221 TO 1261, AND 11 93 TO 1221. INSTALLED SEAT TRACK REPAIR AT EACH LOCATION PER SRM 53-05, FIG 4 SHEET 1, VIEW 7001 PAGE 106. 2 L 7 2 4F A6WE 2001060700015 20010607 00015 WP 2001 6 7 ZW0A0102105 1 20010518 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 907TW 49165 DURING CHECK-C MAINT IN THE AFT CABIN, CHAIR TRACK NUMBER 3 HAD CORROSION AT STA 1130 TO 1155. CHANGED TRACK. DRILLED TRACK AND INSTALLED 2 SPLICES. INSTALLED SEAT TRACK REPAIR PER SRM 53-05, FIG 4 SHEET 1 VIEW 7001, PAGE 106. 2 L 7 2 4F A6WE 2001060700016 20010607 00016 WP 2001 6 7 ZW0A0102106 1 20010518 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 924TW 49100 DURING CHECK-C MAINT IN THE FWD CABIN FOUND CORROSION ON FLOOR SUPPORT AT STA 200 AND BETWEEN BL 5L THRU BL 5R. PRIMED, PAINTED AND INSTALLED PER SPM 6-70-01, ITEM 4. INSTALLED NEW FASTENERS PER SRM 51-20. MADE UP NEW ANGLE PER SRM 53-14 -1, PAGE 29 ITEM 49. 2 L 7 2 4F A6WE 2001060700017 20010607 00017 WP 2001 6 7 ZW0A0102107 1 20010518 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND CABIN MEMBRANE CORRODED, RT SIDE AT STA 522 TO 541. CUT OUT CORRODED MEMBRANE FROM APPROX ST A 522 TO 546, AND FROM CUSP RT TO RBL 54 INCHES. INSTALLED DOUBLER PER SRM 53-01, FIG 4 SHEET 3. 2 L 7 2 4F RT A6WE 2001060700018 20010607 00018 WP 2001 6 7 ZW0A0102108 1 20010517 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND CORROSION ON FWD SIDE OF FORMER AT STA 1174, JUST TO RT OF LONGERON 30, AND BETWEEN 30 TO 29R . FORMER FOOT ANGLE REPAIRED PER SPM 6-70-01 AND DRAWING 9936073-27. PAINTED AND PRIMED PARTS PER SRM 51-10-03, AND SR M 53-03 PAGE 7. 2 L 7 2 4F RT A6WE 2001060700019 20010607 00019 WP 2001 6 7 ZW0A0102109 1 20010518 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND FLOOR SUPPORT WITH CORROSION AT STA 182 AND LBL 18 TO LBL 43, AND AT STA 200 TO 202 AND LBL 4 6 INCHES. FABRICATED NEW FLOOR SUPPORTS FOR BOTH LOCATIONS PER DRAWING 993653-43 SAMPLE AND SPM 6-70-01. PRIMED AND PA INTED PER SRM 51-10-03. INSTALLED WITH RIVETS PER SRM 51-30-02. 2 L 7 2 4F RT A6WE 2001060700020 20010607 00020 EU 2001 6 7 MALA010497 1 20010521 A 3411 9453 PITOT TUBE BAC 146 AVRO146RJ85A 1500097 EU PITOT SYS DEFECTIVE A MALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 15 527XJ E2352 DURING FLIGHT 3460, OUT OF GFK, SMOKE IN FLIGHT DECK. AIR RETURN TO GFK. RIGHT PITOT HEATER FAIL LIGHT CAME ON AFTER T AKEOFF. SMOKE ON F/O SIDE CAME OUT OF FLOOR VENT FOR 30 SECONDS THEN DISSIPATED. MAINTENANCE REPLACED RT MAIN PITOT TU BE P/N 9453, S/N OFF 8652. PITOT TUBE LEAK CHECK AND HEAT CHECKS GOOD IAW ARJ85MM CHAP 34. 2 H 7 4 4F RT A49EU 2001060700021 20010607 00021 WP 2001 6 7 ABXA010233 1 20010518 A 2121 60529042 COOLING FAN DOUG DC9 DC932 3022066 WP CABIN FAULTY A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 23 987AX 7080 47364 THE RIGHT HEAT EXCHANGER COOLING FAN CIRCUIT BREAKER OPENED ON TAKEOFF. FOLLOWED BY AN UNUSUAL ODOR FOR SEVERAL MINUTES . MAINTENANCE INSPECTED AND REPLACED THE GROUND COOLING FAN IAW DC-9 MM. NO UNUSUAL ODORS WERE NOTED. 2 L 7 2 4F A6WE 2001060700022 20010607 00022 WP 2001 6 7 ABXA010234 1 20010523 A 5320 561504011 FITTING DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 58055 46113 FITTING AT STA 980 IN LEFT MAIN LANDING GEAR WHEEL WELL ABOVE LONGERON 24 IS CRACKED. MAINTENANCE INSPECTED AND REPAIRE D THE AREA IAW DC-8 SRM. 2 L 7 4 4F 4A25 2001060700023 20010607 00023 WP 2001 6 7 IXXA0100025 1 20010523 A 2150 BELT DOUG DC8 DC862 3021970 WP A/C UNIT LOOSE A IXXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 11 21CX 68713 2167 45955 EN ROUTE FROM KWA TO HIK, AN ODOR WAS SENSED IN THE COCKPIT EMITTING FROM THE COCKPIT AIR CONDITIONING UNIT. THE FLIGHT CREW SECURED THE AIR CONDITIONER AND THE ODOR SUBSIDED. THE FLIGHT CONTINUED TO HIK FOR AN UNEVENTFUL LANDING. MAINTE NANCE INSPECTED THE AIR CONDITIONER WHICH REVEALED A LOOSE COMPRESSOR DRIVE BELT AND A CLOGGED DRAIN LINE. MAINTENANCE ADJUSTED THE DRIVE BELT, CLEAR THE DRAIN LINE AND PERFORMED AS SUCCESSFUL OPERATIONAL CHECK IN ACCORDANCE WITH THE COMPA NY MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2001060700024 20010607 00024 NM 2001 6 7 C1HA200183002 1 20010513 A 3350 CONNECTOR BOEING 727 7272S7 138407Z NM CABIN LOOSE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 683CA 22490 STRIP OF EMERGENCY LIGHTING INOP BETWEEN ROWS 19-27. RESECURED BATTERY CONNECTION, OPS CHECK GOOD. 2 L 7 3 4F A3WE 2001060700025 20010607 00025 NM 2001 6 7 0101856612 1 20010518 A 3350 POWER SUPPLY BOEING 747 747251B 1384892 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 612US 20357 DURING LINE CHECK, FOUND E-ZONE EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY. OPERATI ONAL CHECK NORMAL. 2 L 7 4 4F A20WE 2001060700026 20010607 00026 NM 2001 6 7 0101866626 1 20010519 A 3350 LIGHT BOEING 747 747251B 1384892 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 626US 21708 DURING LINE CHECK, FOUND CABIN CEILING EMERGENCY LIGHTS INOPERATIVE AT SEAT 55GH, 16FJ, AND 65CD. REPLACED LIGHT ASSEMB LIES. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F A20WE 2001060700027 20010607 00027 WP 2001 6 7 0101909608 1 20010514 A 2131 2075301AA CONTROLLER DOUG DC9 DC932 3022066 WP E/E BAY FAILED A NWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 608NW 2178 2178 47233 DURING CRUISE FLIGHT, THE AIRCRAFT EXPERIENCED LOSS OF CABIN PRESSURIZATION. THE FLIGHT CREW FOLLOWED COM PROCEDURES. AIRCRAFT LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE REPLACED NR 1 DIGITAL CABIN PRESSURE CONTROLLER AND PERFOR MED SYSTEM BITE TEST. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 2001060700028 20010607 00028 NM 2001 6 7 0101913102 1 20010519 A 2150 1303A000002 FLOW VALVE AIRBUS A319 A319113 NM AC BAY DEFECTIVE A NWAA A UNSCHED LANDING B M SMOKE/FUMES/ODORS/SPARKS OVER TEMP CL CLIMB 1 GL 01 302NB 4806 1062 DURING CLIMB FOLLOWING AN AIR CONDITIONING PACK 2 RESET DUE TO AN OVERHEAT, FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN . NR 2 PACK WAS SELECTED OFF. RETURNED TO DEPARTURE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE DEACTIVATED THE NR 2 PACK AND PLACED ON MEL. LATER, MAINTENANCE REPLACED NR 2 PACK FLOW CONTROL VALVE. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 2001060700029 20010607 00029 EU 2001 6 7 C2XA01BT096 1 20010523 A 2121 COOLING FAN AEROSP ATR42 ATR42320 8680930 EU AC BAY FAULTY A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 15816 105 EWR---CO3579, CREW REPORTED SMOKE IN COCKPIT, CAME FROM PACK. EWR MAINTENANCE TROUBLESHOOTING FOUND FAULTY GROUND COOLI NG FAN. 2 H 7 2 4T RT A53EU 2001060700030 20010607 00030 EU 2001 6 7 C2XA01BT097 1 20010523 A 3350 7012210 LIGHT AEROSP ATR42 ATR42320 8680930 EU EXTERIOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 26826 172 BTV---CO2938, DURING 4A INSPECTION, MAINTENANCE FOUND RIGHTHAND AFT EXTERIOR EMERGENCY LIGHT TO BE FAULTY. REMOVED AND REPLACED RIGHTHAND AFT EXTERIOR EMERGENCY LIGHT IAW ATR42 JIC 33-51-24. OPS CHECKED GOOD. 2 H 7 2 4T RT A53EU 2001060700031 20010607 00031 SO 2001 6 7 C2XA01BT098 1 20010522 A 3350 1317 LIGHT EMB 145 EMB145ER SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15941 145035 BTV---CO3944, DURING 4A INSPECTION MAINTENANCE FOUND ROW 12A EMERGENCY LIGHT IN PSU INOPERATIVE. REMOVED AND REPLACED 1 2A EMERGENCY LIGHT BULB IAW EMB145 MM 33-50-08. OPS, CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2001060700032 20010607 00032 SO 2001 6 7 C2XA01BT099 1 20010522 A 3350 B6245305276005 LIGHT EMB 145 EMB145ER SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15941 145035 BTV---CO3944, DURING 4A INSPECTION MAINTENANCE FOUND EMERGENCY LIGHT IN THE SERVICE DOOR TO BE INOPERATIVE. REMOVED AND REPLACED SERVICE DOOR LIGHT ASSY AND FUSE F2 IN NR 2 POWER SUPPLY IAW EMB145 MM 33-50-10 AND EMB145 CMM 25-60-03. EMER GENCY LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2001060700033 20010607 00033 SO 2001 6 7 C2XA01BT100 1 20010522 A 3350 6E209 LIGHT EMB 145 EMB145ER SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15941 145035 BTV---CO3944, DURING 4A INSPECTION MAINTENANCE FOUND EMERGENCY LIGHT ABOVE PASSENGER/CREW DOOR TO BE INOPERATIVE. REMOV ED AND REPLACED EMERGENCY LIGHT ABOVE PASSENGER/CREW DOOR IAW EMB145 MM 33-50-06. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2001060700034 20010607 00034 SO 2001 6 7 C2XA01CL115 1 20010521 A 3350 CONNECTOR EMB 145 EMB145ER SO CABIN LOOSE A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 15941 145035 CLE FLIGHT 3943 THE CREW REPORTED THE EMERGENCY AISLE PATH LIGHTS WERE INOPERATIVE AT ROWS 9-11. MAINTENANCE INSPECTED AND SECURED THE LOOSE CONNECTION AT ROW 11A BATTERY CHARGER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED F OR SERVICE. 2 L 7 2 4F RT T00011AT 2001060700036 20010607 00036 NM 2001 6 7 QXEA0100783 1 20010523 A 2120 UNKNOWN DHAV DHC8 DHC8102 2809003 NM CABIN ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 829PH 304 SEA- FUEL ODOR FROM BLEEDS AFTER ENGINE START. NO FUEL LEAKS NOTED. CYCLED BLEEDS. NO PARTS REPLACED. OPERATIONAL CH ECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001060700037 20010607 00037 EU 2001 6 7 C2XA01BT102 1 20010524 A 3350 AD3127 BATTERY AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14825 170 BTV---CO3014, DURING WEEKLY INSPECTION MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS FAILED TEST. REMOVED AND REPLACED EM ERGENCY LIGHT BATTERY AT 3WL IAW ATR42 JIC 33-51-21. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001060700038 20010607 00038 NM 2001 6 7 UPS01235993 1 20010524 A 3350 LIGHT BOEING 727 727180C 138406G NM CABIN MALFUNCTIONED A IPXA K NONE O OTHER UK UNKNOWN 1 SO 01 920UP 19873 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT CAME ON IN FLIGHT, NOW WILL NOT TEST ON THE GROUND. PERFORMED OPS CHECK OF EME RGENCY EXIT LIGHTS, OPS CHECK OK. NO DEFECTS NOTED. 2 L 7 3 4F A3WE 2001060700039 20010607 00039 NM 2001 6 7 UPS01235994 1 20010524 A 3350 LIGHT BOEING 727 727180C 138406G NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE:N/A REF ITEM 1 THIS PAGE. SUSPECT EMER LIGHT FWD SOCKET TO BE BAD. REMOVED AND REPLACED EMERGENCY EXIT LIGHT, OPS CK GOOD. 2 L 7 3 4F A3WE 2001060700040 20010607 00040 WP 2001 6 7 UPS01835992 1 20010524 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. 2 L 7 4 4F RT 4A25 2001060700041 20010607 00041 EU 2001 6 7 QXEA0100784 1 20010522 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 496US 11169 SEA - THE FORWARD EXIT SIGN HAS BURNT BULBS. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURN ED TO SERVICE. 2 L 7 2 4F RT A20EU 2001060700042 20010607 00042 EU 2001 6 7 C2XA01BT104 1 20010503 A 5320 BRACKET AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 99838 259 YUL---DURING 2C INSPECTION, MAINTENANCE REPORTED TWO CRACKS FOUND ON JOINING BRACKET AT FRAME 29 STRINGER 2R AND 2L. BR ACKETS FABRICATED IAW ATR42 SRM 53-91-80 FIGURE 102 AND INSTALLED IAW ATR42 SRM 51-25-01. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001060700043 20010607 00043 NM 2001 6 7 ZW0A0102201 1 20010521 A 3350 LIGHT BOEING 757 757231 1384950 NM CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 724TW 28488 THE EGRESS LIGHTS WERE INOPERATIVE BETWEEN THE RT SIDE NUMBER 3 AND 4 CABIN DOORS. REMOVED WATER CONTAMINATION FROM THE AFT STRIP LAMPS. CHECK-C 2-28-01 LAX. 2 L 7 2 4F RT A2NM 2001060700045 20010607 00045 SW 2001 6 7 20010529CW008 1 20010430 A 6320 222040022 QUILL BELL BELL 230 230 1182149 SW TRANSMISSION MISOVERHAULED A LOVA K NONE K FLUID LOSS NR NOT REPORTED 1 NM 09 230LF 1555 146 A164 23017 EXCESSIVE OIL LEAKAGE, PAST CORK PN 120-179-13A. IN INNER QUILL ASSEMBLY OF OUTBOARD QUILL. CORK INSTALLED INCORRECTLY BY OVERHAUL FACILITY. RIGHT HAD OUTBOARD QUILL PN 222-040-022-108 OF SAME TRANSMISSION, HAD SAME PROBLEM AT THE SAME T IME. 1 G 7 2 3U NC H9SW 2001060700046 20010607 00046 EA 2001 6 7 COMA0160381 1 20010526 A 5320 601R31171 ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 927CA 17669 7031 THE ANGLES AT FS 484.0, BL 27 (LT & RT) ARE CRACKED (UNDER FLOOR). REPLACED CRACKED ANGLES IAW WVAC EO 601R-53-2438. 2 L 7 2 4F RT A21EA 2001060700047 20010607 00047 CE 2001 6 7 20010529CW009 1 20010510 A 2612 37702810 CONTROL BOX LEAR 25 25D 5170514 CE TAILCONE MALFUNCTIONED E MXIA O OTHER N FALSE WARNING CR CRUISE 1 EA 21 800RF 7271 7271 281 RIGHT ENGINE FIRE LIGHT ON IN FLIGHT. TROUBLESHOOTING PER MM. ALL CIRCUITS TESTED GOOD. REPLACED FIRE DETECT CONTROL BOX. 2 L 7 2 4J A10CE 2001060700050 20010607 00050 NM 2001 6 7 ZW0A0102301 1 20010528 A 3350 8100022002 LIGHT BOEING 767 7673Y0 NM CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 639TW 26208 THE EGRESS LIGHT FACING THE R1 FLT ATTENDANT JUMP SEAT WAS INOPERATIVE. FOUND WIRES PULLED OUT OF LIGHT STRIP. REPLACE D THE LIGHT STRIP. CHECK-C 5-1-01 LAX. 2 L 7 2 4F RT A1NM 2001060700051 20010607 00051 WP 2001 6 7 ZW0A0102302 1 20010524 A 3350 408821101 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ZW0A K NONE L NO TEST NR NOT REPORTED 1 CE 13 9305N 49395 THE EGRESS LIGHTING IN THE FIRST CLASS CABIN WAS INOPERATIVE. REPLACED THE BATTERIES IN THE BATTERY PACK. CHECK-C 5-7- 01 STL. 2 L 7 2 4F RT A6WE 2001060700052 20010607 00052 WP 2001 6 7 ZW0A0102303 1 20010527 A 2560 61020 BATTERY DOUG DC9 DC983 3022083 WP FLASHLIGHT DISCHARGED A ZW0A K NONE L NO TEST NR NOT REPORTED 1 CE 13 9620D 53591 THE THREE AFT CABIN EMERGENCY FLASHLIGHTS WERE INOPERATIVE. REPLACED THE BATTERIES IN EACH. CHECK-C 11-5-00 STL. 2 L 7 2 4F RT A6WE 2001060700053 20010607 00053 WP 2001 6 7 ZW0A0102304 1 20010524 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN CONTAMINATED A ZW0A K NONE O OTHER NR NOT REPORTED 1 CE 13 955U 49427 THE EMERGENCY EGRESS LIGHTS BETWEEN ROWS 15 AND 22 ILLUMINATED WITH THE SWITCH ARMED. REMOVED WATER FROM THE ELECTRICAL CONNECTORS. CHECK-C 2-13-01 STL. 2 L 7 2 4F A6WE 2001060700054 20010607 00054 SO 2001 6 7 20010529CW012 1 20010427 A 2822 2B663FR PUMP PIPER PA31 PA31350 7103110 SO FUEL SYSTEM FAILED A FFSA O OTHER O OTHER NR NOT REPORTED 1 AL 01 4501B 290 318052168 PILOT REPORTED RT ENG SURGING AT HIGH POWER SETTINGS, WITH FULL FUEL FLOW FLUXUATIONS, 23-30 PSI FUEL PRESSURE FLUX, AND INTERMITTENT LOW PRESS FUEL WARNING LITE. INVESTIGATION REVEALED THAT THE RETAINING CLIP THAT SECURES RELIEF VALVE AND SPRING ASSY IN THE INLINE LOW PRESSURE FUEL BOOST PUMP WAS MISSING. THIS ALLOWED THE SPRING & PLUNGER ASSY TO MOVE INS IDE ITS HSG. TO A POSITION THAT BLOCKED THE EXIT OF THE PUMP. THIS PREVENTED SUFFICIENT FUEL TO THE ENG AT HIGH RPM. REPLACE FUEL PUMP AND ENG OPERATED NORMALLY. COULD HAVE PROVEN HAZARDOUS DURING CRITICAL STAGES OF FLT, RECOMMEND CLOSE R INSP PRIOR TO INSTALL. 1 L 7 2 3O A20SO 2001060700055 20010607 00055 WP 2001 6 7 20010529CW013 2 20010416 A 7321 307080022 FUEL CONTROL CESSNA 650 650 2076802 CE GARRTT TFE731 TFE7314R 01518 WP NR 2 ENGINE MALFUNCTIONED E T0DA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 CE 03 50EJ 1605 650148 ENGINE LOST POWER IN FLIGHT. PILOT REPORTED THAT FUEL FLOW WAS ERRATIC AND THAT NR 1 BECAME LIMITED TO 40 PERCENT. WHE N TROUBLESHOT, THE FAULT WAS TRACED TO THE FUNCTION OF THE FUEL CONTROL UNIT. A REPLACEMENT FUEL CONTROL UNIT WAS INSTA LLED AND THE DEFECTIVE UNIT WAS SENT FOR TEARDOWN EVALUATION AND OVERHAUL. 2 L 7 2 4F 4 F A9NM E6WE 2001060700056 20010607 00056 WP 2001 6 7 ABXA010240 1 20010530 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC932F 3022067 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 909AX 47148 EMERGENCY LIGHTS INOP, WOULD NOT TEST. REPLACED EMERGENCY BATTERIES AND BATTERY PACK IAW DC-9 MM 33-53-00. 2 L 7 2 4F A6WE 2001060700057 20010607 00057 CE 2001 6 7 GLBA2001114 1 20010529 A 2133 OUTFLOW VALVE BEECH 1900 1900D 1154162 CE CABIN PRESSURE DIRTY A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 254GL UE254 AIRCRAFT WILL NOT PRESSURIZE. CLEANED OUTFLOW VALVES AND DOOR SEALS. 2 L 7 2 4T RT A24CE 2001060700058 20010607 00058 NM 2001 6 7 ZW0A0102401 1 20010529 A 3350 6100928 LIGHT BOEING 767 7673Q8 NM CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 634TW 28132 THE CABIN EGRESS LIGHTS WERE INOPERATIVE FROM 16AC TO 18AC, 16HJ TO 22HJ, AND LAVATORY J. SECURED LOOSE WIRING AND REPL ACED LAMPS AT 17AC AND 16HJ. CHECK-C 10-25-00 LAX. 2 L 7 2 4F RT A1NM 2001060700059 20010607 00059 WP 2001 6 7 ZW0A0102402 1 20010529 A 3350 8039001 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ZW0A K NONE L NO TEST NR NOT REPORTED 1 CE 13 902TW 49153 THE EMERGENCY LIGHTS DID NOT COME ON IN HALF OF THE FIRST CLASS SECTION. REPLACED THE POWER SUPPLY. CHECK-C 2-5-01 STL . 2 L 7 2 4F A6WE 2001060700060 20010607 00060 CE 2001 6 7 C2XA01CL120 1 20010524 A 2121 1143800287 BLOWER BEECH 1900 1900D 1154162 CE CABIN FAULTY A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 69549 3119 1686 UE194 CLE FLIGHT 3236 THE CREW REPORTED A STRONG ODOR THROUGHOUT THE CABIN. MAINTENANCE INSPECTED AND REPLACED THE FORWARD VE NT BLOWER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT A24CE 2001060700061 20010607 00061 EU 2001 6 7 QXEA0100717 1 20010425 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - CRACKED CABIN CLIP AT FRAME 16660 AND STATION 25. REPAIRED IAW FOKKER SRM 53-02-01, PAGE 14. 2 L 7 2 4F RT A20EU 2001060700062 20010607 00062 EU 2001 6 7 QXEA0100718 1 20010427 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - CRACKED CASTELLATION ON FRAME 13815B AT STRINGER 2. REPAIRED IAW HORIZON AIR EA 4-53-1482. 2 L 7 2 4F RT A20EU 2001060700063 20010607 00063 EU 2001 6 7 QXEA0100719 1 20010427 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - CRACKED CASTELLATION ON FRAME 13815B AT STRINGER 73. REPAIRED IAW HORIZON AIR EA 4-53-1481. 2 L 7 2 4F RT A20EU 2001060700064 20010607 00064 EU 2001 6 7 QXEA0100720 1 20010427 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - CRACKED CASTELLATION ON FRAME 13815A AT STRINGER 2. REPAIRED IAW HORIZON AIR EA 4-53-1480. 2 L 7 2 4F RT A20EU 2001060700065 20010607 00065 EU 2001 6 7 QXEA0100721 1 20010426 A 5320 WEB FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - CORROSION FOUND IN LOWER WEB IN MAIN CABIN DOOR TORSION BOX BETWEEN STATION 4900 - 4610. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4A, PAGE 9. 2 L 7 2 4F RT A20EU 2001060700066 20010607 00066 NM 2001 6 7 QXEA0100785 1 20010523 A 2120 UNKNOWN DHAV DHC8 DHC8202 2809007 NM CABIN ODOR A QXEA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 349PH 486 SEA - AFTER ENGINE START, A OIL LIKE ODOR WAS NOTED COMING FROM THE BLEED AIR SYSTEM. ODOR DISSIPATED AFTER TAKEOFF. E NGINE WAS INSPECTED FOR LEAKS, NONE NOTED. RAN ENGINE THROUGH NUMEROUS POWER SETTINGS, NO ODOR NOTED. COULD NOT DUPLIC ATE DISCREPENCY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001060700067 20010607 00067 NM 2001 6 7 QXEA0100786 1 20010527 A 2121 FAN DHAV DHC8 DHC8202 2809007 NM CABIN FAULTY A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 364PH 524 PDX - PRIOR TO TAKEOFF, FLIGHT ATTENDENT NOTED SMOKE IN THE CABIN. UPON INSPECTION, SMELL WAS ISOLATED TO THE RECIRCULA TION FAN. FAN WAS DEFERRED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001060700068 20010607 00068 NM 2001 6 7 QXEA0100787 1 20010528 A 3350 82520977001 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 351PH 490 PDX - A SECTION OF THE EMERGENCY FLOOR PATH LIGHTING WAS FOUND INOPERATIVE. REMOVED AND REPLACED DEFECTIVE SECTION OF T HE PATH LIGHTING. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001060700069 20010607 00069 NM 2001 6 7 QXEA0100788 1 20010528 A 3350 8250977001 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 356PH 502 PSC - UPON INSPECTION, FOUND FORWARD EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REMOVED AND REPLACED FLOOR PATH LI GHTING STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001060700070 20010607 00070 NM 2001 6 7 QXEA0100789 1 20010524 A 3350 CONNECTOR DHAV DHC8 DHC8202 2809007 NM CABIN LOOSE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 826PH 526 SEA- EMERGENCY EXIT ROW FLOOR PATH LIGHTING FOUND INOPERATIVE. FOUND LOOSE ELECTRICAL CONNECTION. RESEATED CANNON PLUG . OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001060700071 20010607 00071 NM 2001 6 7 QXEA0100790 1 20010528 A 3350 1010951 SIGN DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 826PH 526 SEA - EMERGENCY EXIT SIGN AT ROW 4 A/B REPORTED INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001060700072 20010607 00072 EU 2001 6 7 QXEA0100791 1 20010526 A 3350 RELAY FOKKER F28 F28MK4000 4990810 EU EMERG LIGHTS FAILED A QXEA K NONE O OTHER NR NOT REPORTED 1 NM 09 478US 11227 SEA - EMERGENCY AND EVACUATION LIGHTS ILLUMINATED IN THE ARM POSITION. REMOVED AND REPLACED EMERGENCY LIGHTING CONTROL PANEL RELAY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001060700073 20010607 00073 EU 2001 6 7 QXEA0100792 1 20010525 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN DEFECTIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 GEG - CENTER AISLE EXIT SIGN LIGHTS FOUND INOPERATIVE. REMOVED AND REPLACED CIRCUIT BOARD. OPERATIONAL CHECKS GOOD. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001060700074 20010607 00074 EU 2001 6 7 QXEA0100793 1 20010526 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 493US 11161 PDX - EMERGENCY EXIT SIGN ABOVE FLIGHT COMPARTMENT DOOR REPORTED INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIO NAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001060700075 20010607 00075 EU 2001 6 7 QXEA0100722 1 20010430 A 5310 BRACKET FOKKER F28 F28MK4000 4990810 EU DOOR FRAME CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YCC - UPPER TORSION BOX OF REAR CARGO DOOR APERTURE HAS CORROSION AFT OF AFT HOOK LATCH BRACKET. REPAIRED IAW FOKKER SR M 53-01-01, PARAGRAPH B, PAGE 6, AND FOKKER SRM 51-10-04, PARAGRAPH 4, PAGE 7. 2 L 7 2 4F RT A20EU 2001060700076 20010607 00076 EU 2001 6 7 QXEA0100723 1 20010426 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YCC - CORROSION ON FRAME 16660 BETWEEN STRINGER 74 AND STRINGER 1. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 0, PARAGRAPH 4A. 2 L 7 2 4F RT A20EU 2001060700077 20010607 00077 EU 2001 6 7 QXEA0100724 1 20010501 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - CORROSION ON CASTELLATION ATTACHED TO FRAME 13815 BETWEEN STRINGER 3 AND 72. REPAIRED IAW FOKKER SRM 53-22-04, FI GURE 14 AND SRM FOKKER SRM 51-31-07, PAGE 13 AND 14. 2 L 7 2 4F RT A20EU 2001060700078 20010607 00078 EU 2001 6 7 QXEA0100725 1 20010426 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - CORROSION ON SKIN UNDER AFT RAD ALT ANTENNA. REPAIRED IAW FOKKER SRM 51-10-09, PAGE 9, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 2001060700079 20010607 00079 EU 2001 6 7 QXEA0100726 1 20010426 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YCC - CORROSION ON FUSELAGE SKIN UNDER MARKER BEACON ANTENNA. REPAIRED IAW FOKKER SRM 51-10-09, PAGE 9, PARAGRAPH 4 AND SRM 51-10-04. 2 L 7 2 4F RT A20EU 2001060700080 20010607 00080 EU 2001 6 7 QXEA0100727 1 20010426 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - CORROSION ON FUSELAGE SKIN UNDER AFT DME ANTENNA. REPAIRED IAW FOKKER SRM 51-10-09, PAGE 9, PARAGRAPH 4 AND SRM 5 1-10-04. 2 L 7 2 4F RT A20EU 2001060700081 20010607 00081 EU 2001 6 7 QXEA0100728 1 20010425 A 5330 DOUBLER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - CORROSION ON REPAIR PLATE UNDER FORWARD LOWER VHF/NAV ANTENNA. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAP H 4A. 2 L 7 2 4F RT A20EU 2001060700082 20010607 00082 EU 2001 6 7 QXEA0100729 1 20010426 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - CORROSION ON FUSELAGE SKIN UNDER AFT RAD ALT BLANKING PLATE. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4A. 2 L 7 2 4F RT A20EU 2001060700083 20010607 00083 EU 2001 6 7 QXEA0100730 1 20010426 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - CORROSION ON SKIN UNDER FORWARD RAD ALT ANTENNA. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4A. 2 L 7 2 4F RT A20EU 2001060700084 20010607 00084 EU 2001 6 7 SIMA200110202 1 20010412 A 3350 1011309111 LIGHT AEROSP ATR72 ATR72212 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 308AE 309 MIA - FLT 5236 - LIGHT ON FLOOR EMERGENCY LIGHTS WILL NOT ILLUMINATE. ISSUED MEL 33-30 UNTIL ITEM CAN BE REPAIRED. MAI NTENANCE REPLACED LIGHT ASSEMBLY AT SEAT 6A IAW ATR MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001060700085 20010607 00085 EU 2001 6 7 SIMA200110003 1 20010410 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 545AT 545 DFW - AFT EMERGENCY LIGHTS EVERY OTHER ONE INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT 62WL AND 73WL (S /N 1237 AND 1595) IAW ATR JIC 33-51-21. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 2001060700086 20010607 00086 EU 2001 6 7 SIMA200112201 1 20010502 A 3350 3011180 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 223AT 223 MIA - FLT 5248 - EMERGENCY LIGHTS ON THE FORWARD EMERGENCY EXIT AND THE OUTSIDE GROUND ILLUMINATION ON THE FORWARD LEFT SIDE OF THE AIRCRAFT AND THE OVERHEAD AISLE LIGHT IN FORWARD PART OF CABIN AND TRACK LIGHTS ARE INOPERATIVE. REPLACED T HE EMERGENCY LIGHT POWER SUPPLY AT 3WL IAW AMM. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 2001060700087 20010607 00087 EU 2001 6 7 SIMA200111301 1 20010323 A 3350 LP167006 LIGHT AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 282AT 282 TPA - FLT 5244 - EMERGENCY FLOOR LIGHTING AT SEAT 1A INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM. OPS CHECK GOO D. (M) 2 H 7 2 4T RT A53EU 2001060700088 20010607 00088 EU 2001 6 7 SIMA20011096 1 20010419 A 2424 243211 GCU AEROSP ATR42 ATR42300 8680920 EU NR 1 ENGINE FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 135MQ 135 MIA - FLT 5201 - CREW REPORTED THE NR 1 ACW ALTERNATOR FAULTED IN FLIGHT. CREW RETURNED TO MIA WITH NO FURTHER INCIDENT S. MAINTENANCE REMOVED AND REPLACED THE NR 1 ACW GENERATOR CONTROL UNIT. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS R ETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001060700089 20010607 00089 EU 2001 6 7 SIMA20011097 1 20010419 A 3350 3011180 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 223AT 223 MIA - FLT 5211 - CREW REPORTED FLOOR PROXIMITY EMERGENCY LIGHT AT SEAT 7A TO BE INOPERATIVE. LIGHT WAS PUT ON MEL AT TH IS TIME. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY UNIT FOR AFFECTED LIGHTS. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001060700090 20010607 00090 EU 2001 6 7 SIMA20011065 1 20010416 A 2420 EO24428AO RELAY AEROSP ATR42 ATR42300 8680920 EU ELEC POWER FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 21 125MQ 135 MIA - FLT 5251 - DURING TAKEOFF, THE NR 1 ACW ALTERNATOR FAULTED. AIRCRAFT WAS RETURNED TO MIA WITH NO FURTHER INCIDENT S. MAINTENANCE REPLACED RELAY 35GB AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001060700091 20010607 00091 SO 2001 6 7 SIMA200111803 1 20010428 A 5230 14532594001 TAB EMB 145 EMB145LR SO CARGO DOOR WEAK A SIMA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SW 21 601GH 145046 DAY - FLT 4150 - DURING TAKEOFF, CREW REPORTED THAT THE BAGGAGE DOOR OPEN INDICATION CAME ON THE EICAS. CREW RETURNED T O DAY AND COMPLIED WITH MEL PROCEDURES. REMOVED AND REPLACED SPRING TAB FOR BAGGAGE DOOR HANDLE IAW EMB 145 AMM 52-30-0 1-000-801 AND 52-30-01-400-801 AND OPS CHECK GOOD IAW EMB AMM 52-30-00-700-801 MEL RESTORED. (M) 2 L 7 2 4T RT T00011AT 2001060700092 20010607 00092 SO 2001 6 7 SIMA200112205 1 20010502 A 2621 32600731 FIRE BOTTLE EMB 135 EMB135LR SO CARGO BAY FAILED A SIMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 705AE 145185 ORF - FLT 4968 - EICAS MESSAGE INOPERATIVE. REMOVED AND REPLACED CARGO FIRE BOTTLE IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4F RT TOOO11AT 2001060700093 20010607 00093 NM 2001 6 7 GAIA01140ST 1 20010505 A 5313 STRINGER BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION STRINGER 15 LEFT WAS DISCOVERED CRACKED AT LEFT WING SCANNING LIGHT BS 720B PLUS 15. ACCOMPLISH ED STRINGER REPAIR BS 720B PLUS 15 STRINGER 15 LEFT IAW B727 SRM 53-10-3 FIG 5. (M) 2 L 7 3 4F A3WE 2001060700094 20010607 00094 NM 2001 6 7 GAIA01141ST 1 20010505 A 5313 STRINGER BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION STRINGER 15 LEFT WAS DISCOVERED CRACKED AT LEFT WING SCANNING LIGHT BS 720B PLUS 5. ACCOMPLISHE D STRINGER REPAIR BS 720B PLUS 5 STRINGER 15 LEFT IAW B727 SRM 53-10-3 FIG 5. (M) 2 L 7 3 4F A3WE 2001060700095 20010607 00095 NM 2001 6 7 GAIA01142ST 1 20010505 A 5311 FRAME BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION AT IT WAS DISCOVERED AT THE FORWARD ELECTRONIS COMPARTMENT, ZONE 11.2, STATION 196.5, RIGHT FRAM E CRACKED WITH A PIECE OF MATERIAL MISSING. ACCOMPLISHED FUSELAGE FRAME REPAIR BS 196.5 RBL 12.0 IAW B727 SRM 51-40-2 F IG 1. (M) 2 L 7 3 4F A3WE 2001060700096 20010607 00096 NM 2001 6 7 GAIA01143ST 1 20010505 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, BULGING SKIN WAS DISCOVERED AT BS 350-360, STRINGER 22L, UNDER STRINGER TIE FITTING. ACCOMPLIS HED FUSELAGE SKIN REPAIR BS 350-360 STRINGER 22 LEFT IAW B727 SRM 53-30-3 FIG 3A. (M) 2 L 7 3 4F A3WE 2001060700097 20010607 00097 NM 2001 6 7 GAIA01144ST 1 20010505 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, CORROSION ON FLOORBEAM WAS DISCOVERED AT BS 1130R WHERE SHEAR TIE AND FLOORBEAM INTERSECT, AS V IEWED FROM AFT CARGO. ACCOMPLISHED FLOORBEAM STABILIZATION STRAP REPAIR BS 1130 RBL 45.5 IAW B727 SRM 53-10-8 FIG 6. ( M) 2 L 7 3 4F A3WE 2001060700098 20010607 00098 NM 2001 6 7 GAIA01145ST 1 20010505 A 5754 FLAP BOEING 727 727223 1384074 NM WING CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, PITTING CORROSION AROUND DATA PLATE WAS DISCOVERED ON THE NR 6 KRUGER FLAP, INNER FLAP SURFACE. ACCOMPLISHED NR 6 KRUGER FLAP REPAIR IAW B727 SRM 57-50-3 FIG 2. (M) 2 L 7 3 4F A3WE 2001060700099 20010607 00099 NM 2001 6 7 GAIA01146ST 1 20010505 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, FOUND CORROSION ON FLOORBEAM LOWER SIDE WAS DISCOVERED AT BS 1110, AS VIEWED FROM AFT CARGO. A CCOMPLISHED FLOORBEAM LOWER CHORD REPAIR BS 1110 IAW B727 SRM 53-10-8 FIG 8. (M) 2 L 7 3 4F A3WE 2001060700100 20010607 00100 NM 2001 6 7 GAIA01147ST 1 20010505 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, FOUND CORROSION ON FLOORBEAM WAS DISCOVERED AT BS 1110 BL 30L AS VIEWED FROM LOWER CARGO COMPAR TMENT, LOWER SIDE OF UPPER T-CHORD. ACCOMPLISHED FLOORBEAM UPPER CHORD REPAIR BS 1110 LBL 30 IAW B727 SRM 53-10-8 FIG 8 . (M) 2 L 7 3 4F A3WE 2001060700101 20010607 00101 NM 2001 6 7 GAIA01148ST 1 20010505 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, CORROSION AND GOUGES WERE DISCOVERED ON THE FUSELAGE SKIN AT BS 366-370, STRINGER 17-18 LEFT. ACCOMPLISHED FUSELAGE SKIN REPAIR BS 366-370, BETWEEN STRINGER 17-18 LEFT IAW B727 SRM 53-30-3 FIG 3. (M) 2 L 7 3 4F A3WE 2001060700102 20010607 00102 NM 2001 6 7 GAIA01149ST 1 20010505 A 5320 WEB BOEING 727 727223 1384074 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION IT WAS DISCOVERED THAT THE LEFT AFT SHEAR WEB IN CABIN IS CORRODED. ACCOMPLISHED SHEAR WEB REMO VAL AND REPLACEMENT BS 1130-1176 LEFT IAW B727 SRM 53-10-2 AND SRM 51-30-2. (M) 2 L 7 3 4F A3WE 2001060700103 20010607 00103 NM 2001 6 7 GAIA010150ST 1 20010505 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE BS 740 FLOORBEAM UPPER CHORD IS CRACKED IN THE RADIUS UNDER THE RBL 45.5 SEAT TRACK. ACCOMPLISHED FLOORBEAM UPPER CHORD REPAIR BS 740 RBL 45.5 IAW B727 SRM 53-10-4 FIG 4. (M) 2 L 7 3 4F A3WE 2001060700104 20010607 00104 NM 2001 6 7 GAIA01151ST 1 20010505 A 5242 DOOR FRAME BOEING 727 727223 1384074 NM E/E DOOR CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION IT WAS DISCOVERED THAT THE E/E COMPARTMENT DOOR INTERIOR HAS A CRACK IN THE RADIUS OF DOOR FRAME . ACCOMPLISHED E/E DOOR FRAME REPAIR IAW B727 SRM 51-40-3 FIG 1. (M) 2 L 7 3 4F A3WE 2001060700105 20010607 00105 NM 2001 6 7 GAIA01157ST 1 20010505 A 5310 DOOR FRAME BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, A CRACK WAS DISCOVERED ON THE C-1 CARGO DOOR CUTOUT AFT FRAME WEB AT NR 6 STOP. ACCOMPLISHED C -1 DOOR CUTOUT AFT FRAME REPAIR BS 620 BETWEEN STRINGER 26/25R IAW B727 SRM 51-40-2 FIG 1. (M) 2 L 7 3 4F A3WE 2001060700106 20010607 00106 NM 2001 6 7 GAIA01158ST 1 20010505 A 5311 FRAME BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION IT WAS DISCOVERED AT BS 520 FRAME DENTED BETWEEN STRINGER 23-24R. ACCOMPLISHED FUSELAGE FRAME R EPAIR BS 520 BETWEEN STRINGER 23/24R IAW B727 SRM 53-10-4 FIG 3. (M) 2 L 7 3 4F A3WE 2001060700107 20010607 00107 NM 2001 6 7 GAIA01159ST 1 20010505 A 5310 CREASE BEAM BOEING 727 727223 1384074 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, FOUND CORROSOIN WAS DISCOVERD ON LOWER SURFACE OF CREASE BEAM BS 317, RBL 55, WL 208, AND UPPER SURFACE FROM BS 344-380. ACCOMPLISHED CREASE BEAM REPLACEMENT BS 301-360, RBL 55, WL 208 IAW B727 SRM 53-10-2, SRM 51- 20-1, AND SRM 51-30-2. (M) 2 L 7 3 4F A3WE 2001060700108 20010607 00108 NM 2001 6 7 GAIA01160ST 1 20010505 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION FOUND CORROSION ON A FLOORBEAM WAS DISCOVERED AT BS 1130, BBL 0 AS VIEWED FROM THE AFT PIT. ACC OMPLISHED BS 1130, BBL 0 FLOORBEAM C ANGLE REPAIR IAW B727 SRM 53-10-2 FIG 7 AND SRM 51-30-2. (M) 2 L 7 3 4F A3WE 2001060700109 20010607 00109 NM 2001 6 7 GAIA01161ST 1 20010505 A 2782 ATTACH FITTING BOEING 727 727223 1384074 NM NR 4 SLAT CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE NR 4 SLAT ACTUATOR ATTACH FITTING PREVIOUS REPAIR IS CRACKED, INSIDE SLAT. ACCOMPLISHED NR 4 SLAT ACTUATOR RIB REPAIR IAW B727 SRM 57-50-3 FIG 9. (M) 2 L 7 3 4F A3WE 2001060700110 20010607 00110 NM 2001 6 7 GAIA01162ST 1 20010505 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, IT WAS DISCOVERED AT BS 940-950, LBL 24.75 SEAT TRACK OUTBOARD FLANGE IS CORRODED. ACCOMPLISHE D SEAT TRACK REPLACEMENT BS 870-950 PLUS 10 INCHES LBL 24.75 IAW B727 SRM 57-50-3 FIG 9. (M) 2 L 7 3 4F A3WE 2001060700111 20010607 00111 NM 2001 6 7 GAIA01163ST 1 20010505 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, IT WAS DISCOVERED AT RBL 24.75 A LONGITUDINAL FLOORBEAM UPPER CHORD IS CRACKED AT BS 760, WL 20 7. ACCOMPLISHED LONGITUDINAL FLOORBEAM UPPER CHORD REPLACEMENT BS 740-848 RBL 24.75 IAW B727 SRM 51-30-2 AND SRM 51-10- 1. (M) 2 L 7 3 4F A3WE 2001060700112 20010607 00112 NM 2001 6 7 GAIA01164ST 1 20010505 A 5347 CARGO TRACK BOEING 727 727223 1384074 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT IN THE AFT MAIN CARGO COMPARTMENT A SEAT TRACK IS CORRODED FROM BS 1110- 1136, AT LBL 45. ACCOMPLISHED SEAT TRACK REPAIR BS 1050-1140 LBL 45.5 IAW B727 SRM 53-10-5 FIG 1. (M) 2 L 7 3 4F A3WE 2001060700113 20010607 00113 NM 2001 6 7 GAIA01165ST 1 20010505 A 5320 TIE BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT AT BS 1183 A VERTICAL BEAM AT LBL 47.03 TENSION TIE IS CRACKED AND CORRO DED. ACCOMPLISHED BS 1183 AT LBL 47.03 TENSION TIE REMOVAL AND REPLACEMENT IAW B727 SRM 51-30-2 AND SRM 51-20-1. (M) 2 L 7 3 4F A3WE 2001060700114 20010607 00114 NM 2001 6 7 GAIA01166ST 1 20010505 A 5530 STRINGER BOEING 727 727223 1384074 NM VERTICAL STAB CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE LEFT VERTICAL STABILIZER INTERIOR STRINGER 3RD BAY DOWN FROM PANEL 9 504 IS CRACKED. ACCOMPLISHED VERTICAL STAB STRINGER REPAIR STRINGER 8L FIN STATION 60 IAW B727 SRM 55-30-4 FIG 1. (M) 2 L 7 3 4F A3WE 2001060700115 20010607 00115 NM 2001 6 7 GAIA01167ST 1 20010505 A 5320 STIFFENER BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION A HORIZONTAL STIFFENER WAS DISCOVERED CRACKED AT BS 178 BULKHEAD, WL 198, RBL 6, OUTBOARD END. ACCOMPLISHED BS 178 BULKHEAD REPAIR BS 178, WL 198, RBL 6 IAW B727 SRM 53-10-2 AND SRM 51-30-2. (M) 2 L 7 3 4F A3WE 2001060700116 20010607 00116 NM 2001 6 7 GAIA01168ST 1 20010505 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE GOUGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION A GOUGE IN THE SKIN WAS DISCOVERED AT LEFT STATION 277 STRIGNER 26. ACCOMPLISHED FUSELAGE SKIN REPAIR BS 277 AT STRINGER 26L IAW B727 SRM 53-30-3 FIG 3. (M) 2 L 7 3 4F A3WE 2001060700117 20010607 00117 NM 2001 6 7 GAIA01169ST 1 20010505 A 5320 SPLICE BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE LEFT AFT OVERWING EXIT, AFT LOWER SIDE, BS 850 STRINGER 16L STRINGER SPLICE IS CRACKED IN TWO PLACES, UPPER AND LOWER SIDE OF STRINGER. ACCOMPLISHED STRINGER SPLICE REPAIR BS 850 STRINGER 16L IAW B727 SRM 53-10-2 FIG 9 AND SRM 51-30-2. (M) 2 L 7 3 4F A3WE 2001060700118 20010607 00118 NM 2001 6 7 GAIA01170ST 1 20010505 A 5312 PRESSURE PANEL BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, A CRACK WAS DISCOVERED IN THE NOSE WHEEL WELL LEFT WEB JUST BELOW FORWARD PRESS PANEL STATION 2 77. ACCOMPLISHED NOSE WHEEL WELL PRESSURE WEB REPAIR BS 277 LEFT IAW B727 SRM 53-10-2 FIG 2 AND SRM 51-30-2. (M) 2 L 7 3 4F A3WE 2001060700119 20010607 00119 NM 2001 6 7 GAIA01171ST 1 20010505 A 5320 STRAP BOEING 727 727223 1384074 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, CORROSION WAS DISCOVERED ON THE BS 950 DOUBLER/MODIFICATION, STRINGER 14R AND 17R. ACCOMPLISHE D BLENDOUT REPAIR BS 950 AT STRIGNER 14R AND 17R ON THE WEIGHT UPGRADE REINFORCEMENT STRAP IAW B727 SRM 51-10-6. OK FOR CONTINUED SERVICE PER STRESS ANALYSIS BY FLIGHT SCIENCES INT INC REPORT NR 3089-0 DATED 4/23/2001. (M) 2 L 7 3 4F A3WE 2001060700120 20010607 00120 NM 2001 6 7 GAIA01172ST 1 20010505 A 5310 DOOR FRAME BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE C-1 CARGO DOOR FORWARD FRAME WEB IN THE CUT OUT IS CRACKED IN 4 AREA S. ACCOMPLISHED C-1 CARGO DOOR CUTOUT FORWARD FRAME WEB REPAIR BS 560 IAW SRM 51-40-2 FIG 1. (M) 2 L 7 3 4F A3WE 2001060700121 20010607 00121 NM 2001 6 7 GAIA01173ST 1 20010505 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, A DENT WAS DISCOVERED ON FUSELAGE SKIN AT BS 244, 1 INCH UNDER STRINGER 17L. ACCOMPLISHED FUSE LAGE SKIN REPAIR BS 244, 1 INCH BELOW STRINGER 17L IAW SRM 51-40-2 FIG 1. (M) 2 L 7 3 4F A3WE 2001060700122 20010607 00122 NM 2001 6 7 VNAA0105020 1 20010528 A 3610 4069B000 BLEED VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CROSS BLEED FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 434JS 4204 3051 DURING CLIMBOUT THE RIGHT HAND PACK FAILED. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK THEN HAD A DUAL PACK OVERPRE SSURE FAIL CAS MESSAGE. THE CREW DECIDED TO RETURN TO TYS. THE AIRCRAFT WAS FERRIED TO PIT WHERE MAINTENANCE REPLACED THE CROSS BLEED VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 21-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001060700123 20010607 00123 NM 2001 6 7 GAIA01185ST 1 20010505 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, BULGING SKIN AND DISHED/POPPED FASTENERS WERE DISCOVERED ALONG STRINGER 27 LEFT, BS 305-312, LE FT LOWER NOSE CHORD. ACCOMPLISHED LOWER NOSE LANDING GEAR WHEEL WELL LOWER NOSE CHORD REMOVAL AND REPLACEMENT AND FUSEL AGE SKIN REPAIR AND SHEAR TIE REPAIR LEFT BS 305-360 IAW B727 SRM 53-10-4 FIG 7 AND 13, SRM 51-30-2, SRM 51-30-8, AND SR M 51-20-1. (M) 2 L 7 3 4F A3WE 2001060700124 20010607 00124 NM 2001 6 7 GAIA01186ST 1 20010505 A 5310 DOOR FRAME BOEING 727 727223 1384074 NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, DISCOVERED C1 DOOR CUTOUT AREA UPPER SKIN HAS TWO DENTS IN WEB. ACCOMPLISHED FORWARD CARGO DOO R C-1 UPPER WEB REPAIR BS 580-600 WL 198 IAW B727 SRM 51-40-2 FIG 1. (M) 2 L 7 3 4F A3WE 2001060700125 20010607 00125 SO 2001 6 7 SIMA20011151 1 20010425 A 2131 22250NO30201 CONTROLLER EMB 145 EMB145LR SO COCKPIT INOPERATIVE A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 706RG 145194 XNA - FLT 3546 - CREW REPORTED PRESSURIZATION WAS INOPERATIVE IN AUTO/MANUAL. AIRCRAFT WAS RETURNED TO FIELD. MAINTENA NCE REMOVED AND REPLACED THE DIGITAL PRESSURE CONTROLLER. OPS CHECK WAS GOOD IAW EMB MM. AIRCRAFT WAS RETURNED TO SERV ICE. (M) 2 L 7 2 4T RT T00011AT 2001060700126 20010607 00126 SO 2001 6 7 SIMA20011172 1 20010421 A 5315 FLOORBEAM EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 700LE 145156 ABI - MAINTENANCE FOUND THE LEFT OMEGA BEAM TO BE CORRODED BEYOND SRM LIMITS AT FRAME 20. MAINTENANCE REPAIRED FRAME IA W EMB SRM 53-21-10. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001060700127 20010607 00127 SO 2001 6 7 SIMA20011171 1 20010421 A 5315 FLOORBEAM EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 700LE 145156 ABI - MAINTENANCE REPORTED THE LEFT OMEGA BEAM TO BE CORRODED BEYOND SRM LIMITS BETWEEN FRAMES 23 AND 25. MAINTENANCE R EPAIRED DAMAGE IAW EMB SRM AND REPAIR STATEMENT GST 1298/01. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001060700128 20010607 00128 SO 2001 6 7 SIMA200109501 1 20010405 A 3610 14523699413 DUCT EMB 135 EMB135LR SO BLEED AIR FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 738NR 145401 LGA - FLT 4510 - DURING CLIMB-OUT, CREW NOTED ENGINE BLEED 1 LEAK IND. DURING THIS A LOUD NOISE WAS HEARD FROM AFT AREA . CREW RETURNED TO LGA SAFELY. NO FURTHER INCIDENTS WERE REPORTED. REMOVED AND REPLACED DUCT IAW AMM. OPS CHECK GOOD . (M) 2 L 7 2 4F RT TOOO11AT 2001060700129 20010607 00129 NM 2001 6 7 USAA010385 1 20010416 A 5320 WEB BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 618AU 47860 22210 CLT - FOUND TRANSITION ANGLE WEB CORRODED 4 INCHES, STATION 1340/1360 AT STRINGER 27 RIGHT. REMOVED AND REPLACED TA WEB , SRM 51-40-02. (M) 2 L 7 2 4F RT A2NM 2001060700130 20010607 00130 NM 2001 6 7 USAA010447 1 20010425 A 5312 PRESSURE PANEL BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND PRESSURE DECK WEB 2 INCH, BS 663-676, RBL 20 TO RBL 50. INSTALLED DOUBLED, STIFFENERS, CHORD SEGMENT, FILLE RS, WEB PER EA''S 69129, 69125, 69183. (M) 2 L 7 2 4F A16WE 2001060700131 20010607 00131 NM 2001 6 7 USAA010448 1 20010425 A 5320 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 50347 22756 CLT - FOUND TIE CLIP CRACKED .25 INCH, BS 707, AFT SIDE OF STRINGER 11R. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-01 , INSTALLED FREEZE PLUG REPAIR PER EA 69175. (M) 2 L 7 2 4F A16WE 2001060700132 20010607 00132 NM 2001 6 7 USAA010450 1 20010425 A 5311 FRAME BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 51677 22879 CLT - FOUND SIDE CHORD CRACKED, BS 178 WL 207 RIGHT SIDE CHORD. DAMAGED SECTION CUTOUT, SPLICED IN NEW CHORD SECTION PE R EO 5300V157. (M) 2 L 7 2 4F A16WE 2001060700133 20010607 00133 NM 2001 6 7 USAA010451 1 20010425 A 5311 FRAME BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 51677 22879 CLT - FOUND SIDE CHORD CRACKED .5 INCH, BS 178 WL 207 LEFT SIDE. REMOVED DAMAGED SECTION, SPLICED IN NEW CHORD SECTION PER EO 5300V157. (M) 2 L 7 2 4F A16WE 2001060700134 20010607 00134 NM 2001 6 7 USAA010452 1 20010425 A 5330 DOUBLER BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 51677 22879 CLT - FOUND SKIN DOUBLER CRACKED .09375, BS 178, 12 OCLOCK POSITION, STRINGER 1L. ROUTED OUT DAMAGE (TIME LIMITED REPAI R) PER EA 69533. (M) 2 L 7 2 4F A16WE 2001060700135 20010607 00135 NM 2001 6 7 USAA010476 1 20010429 A 5320 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND TIE CLIP CRACKED .25 INCH, BS 747, S4L. REMOVED AND REPLACED TIE CLIP PER EO 5393G227. (M) 2 L 7 2 4F A16WE 2001060700136 20010607 00136 NM 2001 6 7 USAA010477 1 20010429 A 5320 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND TIE CLIP CRACKED .25 INCH, BS 787, S9L AND S10L. REMOVED AND REPLACED BOTH TIE CLIPS PER EO 5393G227. (M) 2 L 7 2 4F A16WE 2001060700137 20010607 00137 NM 2001 6 7 USAA010478 1 20010429 A 5320 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51503 22754 CLT - FOUND TIE CLIP CRACKED .25 INCH, BS 807, S7L. REMOVED AND REPLACED TIE CLIP PER EO5393G227. (M) 2 L 7 2 4F A16WE 2001060700138 20010607 00138 NM 2001 6 7 USAA010479 1 20010429 A 5320 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51503 22754 CLT - FOUND 4 CRACKS .25 INCH, BS 767, S3L, S4L, S5L, AND S6L. REMOVED AND REPLACED 4 TIE CLIPS PER PER EO 5393G227. R EMOVED AND REPLACED 4 TIE CLIPS PER EO 5393G227. (M) 2 L 7 2 4F A16WE 2001060700139 20010607 00139 NM 2001 6 7 USAA010480 1 20010429 A 5310 CREASE BEAM BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND CREASE BEAM WEB CRACKED .25 INCH, BS 616-639, S17R. REMOVED AND REPLACED WEB PER SRM 51-30-10. (M) 2 L 7 2 4F A16WE 2001060700140 20010607 00140 NM 2001 6 7 USAA010481 1 20010429 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND FRAME CRACKED .25 INCH, BS 639, S17R. INSTALLED REPAIR DOUBLER PER SRM 51-40-2 FIG 1 AND SRM 51-30-00. (M) 2 L 7 2 4F A16WE 2001060700141 20010607 00141 NM 2001 6 7 USAA010482 1 20010429 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND FRAME CHORD ANGLE .25 INCH, BS 639, 2.75 INCH INBOARD OF STRINGER 16L. REMOVED AND REPLACED INNER CHORD ANG LE PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2001060700142 20010607 00142 NM 2001 6 7 USAA010483 1 20010429 A 5320 WEB BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND WEB CRACKED .5 INCH, BS 639, 2.75 INCH INBOARD OF S16L. REMOVED DAMAGED WEB SECTION, INSTALLED NEW WEB DOUB LER AND FILLER PER SRM 51-40-02, FIG 1. (M) 2 L 7 2 4F A16WE 2001060700143 20010607 00143 NM 2001 6 7 USAA010484 1 20010429 A 5313 STRINGER BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND SHELF CRACKED .5 INCH, BS 727, S18A RIGHT, INBOARD FASTENER. REMOVED AND REPLACED SHELF PEER EA 69507 AND B AC DRAWING NR 65-46877-76. (M) 2 L 7 2 4F A16WE 2001060700144 20010607 00144 NM 2001 6 7 USAA010485 1 20010429 A 5310 CREASE BEAM BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND CREASE BEAM WEB CRACKED .25 INCH, BS 637, RBL 70. REMOVED AND REPLACED WEB PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2001060700145 20010607 00145 NM 2001 6 7 USAA010486 1 20010429 A 5313 STRINGER BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND STRINGER CRACKED .5 INCH, BS 358, S7L. FABRICATED WEB CLIP, REPLACED STRINGER AND TIE CLIP PER SRM 51-10-1 AND 51-30-0. (M) 2 L 7 2 4F A16WE 2001060700146 20010607 00146 NM 2001 6 7 USAA010487 1 20010429 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND FUSELAGE SKIN CRACKED 1.7 INCH, RIGHT AFT GALLEY SERVICE DOOR CUTOUT, FORWARD LOW CORNER. DAMAGE CUTOUT, IN STALLED FILLER AND REPAIR DOUBLER, TEXAS PATCH, PER SRM 53-30-3 FIG 24. (M) 2 L 7 2 4F A16WE 2001060700147 20010607 00147 NM 2001 6 7 USAA010488 1 20010429 A 5313 STRINGER BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND STRINGER CRACKED .5 INCH, BS 360, S15L. REMOVED AND REPLACED STRINGER SECTION PER RM 51-10-1. (M) 2 L 7 2 4F A16WE 2001060700148 20010607 00148 NM 2001 6 7 USAA010489 1 20010429 A 5320 INTERCOSTAL BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND INTERCOSTAL CRACKED 1 INCH, BS 178, WL 195, RBL 24. REMOVED AND REPLACED INTERCOSTAL PER EO 5300V155. (M) 2 L 7 2 4F A16WE 2001060700149 20010607 00149 NM 2001 6 7 USAA010490 1 20010429 A 5313 STRINGER BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND STRINGER CRACKED 1 INCH, BS 787, S16R. INSTALLED STRINGER SPLICE REPAIR PER SRM 53-30-3, 53-10-2. (M) 2 L 7 2 4F A16WE 2001060700150 20010607 00150 NM 2001 6 7 USAA010492 1 20010429 A 5320 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND TIE CLIP CRACKED .25 INCH, BS 360, S4L. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM 51-30-2. (M) 2 L 7 2 4F A16WE 2001060700151 20010607 00151 NM 2001 6 7 USAA010494 1 20010429 A 5320 ANGLE BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND VERTICAL TIE ANGLE CRACKED .75 INCH AND 1 INCH, BS 360, BETWEEN S14L AND S15L. REMOVED DAMAGED ANGLE, FABRI CATED AND INSTALLED NEW ANGLE PER SRM 51-10-01, 51-40-3 AND 53-10-2. (M) 2 L 7 2 4F A16WE 2001060700152 20010607 00152 NM 2001 6 7 USAA010495 1 20010429 A 5751 HINGE FITTING BOEING 737 737201 1384454 NM AILERON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND HINGE CASTING CRACKED .5 INCH, RT AILERON, NR 2 HINGE SUPPORT CASTING, LOWER OUTBOARD PANEL. REMOVED AND RE PLACED CASTING PER BOEING DRAWING NR 65-63445-1. (M) 2 L 7 2 4F A16WE 2001060700153 20010607 00153 NM 2001 6 7 USAA010498 1 20010429 A 5312 BULKHEAD BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND BULKHEAD CRACKED 1 INCH, BS 178, WL 234, RBL 11. INSTALLED DOUBLER AND FILLER PER SRM 53-10-11 FIG 1. (M) 2 L 7 2 4F A16WE 2001060700154 20010607 00154 NM 2001 6 7 USAA010499 1 20010429 A 5320 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND TIE CLIP CRACKED .125 INCH, BS 663, S10R. REMOVED AND REPLACED TIE CLIP PER EO 5393G227. (M) 2 L 7 2 4F A16WE 2001060700155 20010607 00155 NM 2001 6 7 USAA010500 1 20010429 A 5320 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND TIE CLIP CRACKED .25 INCH, BS 706, S11R. FABRICATED NEW CLIP AND INSTALLED PER BLUEPRINT NR 69-45156 AND SR M 51-30-2. (M) 2 L 7 2 4F A16WE 2001060700156 20010607 00156 NM 2001 6 7 USAA010501 1 20010429 A 5320 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND TIE CLIP CRACKED .5 INCH, BS 344 S11R. FABRICATED AND INSTALLED NEW TIE CLIP PER BOEING DRAWING NR 69-38939 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 2001060700157 20010607 00157 NM 2001 6 7 USAA010502 1 20010429 A 5320 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND TIE CLIP CRACKED .125 INCH, BS 597, S5R. INSTALLED NEW TIE CLIP PER SRM 51-30-2. (M) 2 L 7 2 4F A16WE 2001060700158 20010607 00158 NM 2001 6 7 USAA010503 1 20010429 A 5320 TIE CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND TIE CLIP CRACKED .125 INCH, BS 597, STRINGER 4R. INSTALLED NEW TIE CLIP PER EO 5393G227. (M) 2 L 7 2 4F A16WE 2001060700159 20010607 00159 NM 2001 6 7 USAA010473 1 20010429 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 3 INCHES, BS 1006, LBL 10. DAMAGE REMOVED, INSTALLED FILLER AND REPAIR ANGLE S PER SRM 53-10-9 FIG 2. (M) 2 L 7 2 4F A16WE 2001060700160 20010607 00160 NM 2001 6 7 USAA010474 1 20010429 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND FLOORBEAM T-CAP CORRODED 1 INCH BY .5 INCH AREA, BS 312, BL 0. DAMAGE REMOVED, SPLICED IN REPAIR ANGLES AND T-CAP SECTION PER TYPICAL REPAIR 53-10-13. (M) 2 L 7 2 4F A16WE 2001060700161 20010607 00161 NM 2001 6 7 GAIA01174ST 1 20010505 A 5312 PRESSURE PANEL BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, A CRACK WAS DISCOVERED IN THE NOSE WHEEL WELL UPPER PRESSURE WEB AT BL 0 AT BS 277. ACCOMPLISH ED NOSE WHEEL WELL UPPER PRESSURE WEB REPAIR BS 277 BL 0 IAW SRM 51-40-2 FIG 1. (M) 2 L 7 3 4F A3WE 2001060700162 20010607 00162 NM 2001 6 7 GAIA01175ST 1 20010505 A 5320 STIFFENER BOEING 727 727223 1384074 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, A HORIZONTAL STIFFENER WAS DISCOVERED CORRODED AT BS 178 BULKHEAD, WL 188 LBL 25 TO RBL 25. AC COMPLISHED BS 178 BULKHEAD HORIZONTAL STIFFENER REMOVAL AND REPLACEMENT BS 178 WL 188 LBL 25 TO RBL 25 IAW SRM 53-10-2 P AGE 3 AND SRM 51-30-5 AND SRM 51-10-2. (M) 2 L 7 3 4F A3WE 2001060700163 20010607 00163 NM 2001 6 7 GAIA01176ST 1 20010505 A 5522 SKIN BOEING 727 727223 1384074 NM ELEVATOR CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION IT WAS DISCOVERED THAT THE LEFT ELEVATOR INBOARD TRAILING EDGE STATIC WICK MOUNT BASE HAS CORROS ION UNDER BASE AND EDGES. ACCOMPLISHED LEFT ELEVATOR UPPER SKIN REPAIR ELEV STATION 209.96 IAW SRM 55-20-3 FIG 2. (M) 2 L 7 3 4F A3WE 2001060700164 20010607 00164 NM 2001 6 7 GAIA01177ST 1 20010505 A 5312 TEE CHORD BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION IT WAS DISCOVERED THAT THE STATION 950 BULKHEAD UPPER ATTACH ANGLE IN LEFT WHEEL WELL (LBL 50) I S CRACKED. ACCOMPLISHED 950 BULKHEAD T-CHORD REPAIR LBL 50 IAW SRM 51-40-4 FIG 1. (M) 2 L 7 3 4F A3WE 2001060700165 20010607 00165 NM 2001 6 7 GAIA01178ST 1 20010505 A 5320 WEB BOEING 727 727223 1384074 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, THE FLOORBEAM IN AFT CARGO FLOOR WAS DISCOVERED TO HAVE A CORRODED FASTENER THAT IS WORKING INT O THE FACE OF THE FLOORBEAM AT BS 1166 AT BL 25L. ACCOMPLISHED SHEAR WEB REPAIR BS 1166 TO 1176 IAW SRM 53-10-2 AND SRM 51-30-2 AND SRM 51-10-2. (M) 2 L 7 3 4F A3WE 2001060700166 20010607 00166 NM 2001 6 7 GAIA01179ST 1 20010505 A 5313 STRINGER BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, DISCOVERED STRINGERS ABOVE AND BELOW NR 3 ENGINE PRECOOLER EXHAUST DUCT WERE CRACKED AT BS 1273 STRINGER 10R AND 11R. ACCOMPLISHED STRINGER REPAIRS BS 1273 STRINGER 10R AND 11R IAW SRM 53-10-3 FIG 2. (M) 2 L 7 3 4F A3WE 2001060700167 20010607 00167 NM 2001 6 7 GAIA01180ST 1 20010505 A 5320 FITTING BOEING 727 727223 1384074 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, BS 1183 STRINGER 19L STRINGER TIE FITTING WAS DISCOVERED CORRODED. ACCOMPLISHED BS 1183 STRING ER 19L STRINGER END TIE FITTING REMOVAL AND REPLACEMENT IAW SRM 53-10-3 AND SRM 51-30-2. (M) 2 L 7 3 4F A3WE 2001060700168 20010607 00168 NM 2001 6 7 GAIA01181ST 1 20010505 A 5755 HINGE FITTING BOEING 727 727223 1384074 NM NR 9 SPOILER CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, THE NR 9 SPOILER HINGE SUPPORT FITTING WAS DISCOVERED CRACKED ON THE INBOARD SIDE, ABOVE HINGE BOLT. ACCOMPLISHED NR 9 SPOILER SUPPORT FITTING REPAIR PER REPAIR ORDER FASI-011RO-1 REV I/R DATED 4/26/2001. (M) 2 L 7 3 4F A3WE 2001060700169 20010607 00169 NM 2001 6 7 GAIA01182ST 1 20010505 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, THE BS 950 FLOORBEAM UPPER CHORD WAS DISCOVERED CORRODED LBL 24.75 TO 45.50. ACCOMPLISHED BS 9 50 FLOORBEAM UPPER CHORD REPAIR LBL 32.75 IAW REPAIR ORDER FASI-101RO-1 REV IR DATED 04/26/01. (M) 2 L 7 3 4F A3WE 2001060700170 20010607 00170 NM 2001 6 7 GAIA01183ST 1 20010505 A 5711 SPAR BOEING 727 727223 1384074 NM LT WING CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, THE LEFT LOWER SPAR CHORD WAS DISCOVERED CORRODED AT WING LEADING EDGE STATION 305 THROUGH STAT ION 325. ACCOMPLISHED LEFT WING LOWER SPAR CHORD REPAIR FSS 327 IAW REPAIR ORDER FASI-0099O-1 REV IR DATED 4/26/01. (M ) 2 L 7 3 4F A3WE 2001060700171 20010607 00171 NM 2001 6 7 GAIA01184ST 1 20010505 A 5711 SPAR BOEING 727 727223 1384074 NM LT WING CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING A LTC INSPECTION, THE LEFT FRONT SPAR LOWER CHORD WAS DISCOVERED CORRODED BELOW NR 3 SLAT OUTBOARD TRACK. ACCOMP LISHED LEFT WING LOWER SPAR CHORD REPAIR FSS 450 IAW REPAIR ORDER FASI-009RO-1 REV IR DATED 4/26/02. (M) 2 L 7 3 4F A3WE 2001060700172 20010607 00172 WP 2001 6 7 0101969998 1 20010522 A 3320 TRANSFORMER DOUG DC9 DC931 3022065 WP CABIN OVERHEATED A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 01 8934E 47143 ON DESCENT, THE LEAD FLIGHT ATTENDANT REPORTED A SMOKE ODOR IN THE AREA OF THE FORWARD FLIGHT ATTENDANT JUMPSEAT WHICH D ISSIPATED IN 1-2 MINUTES. FOUND THE LEFT FORWARD READING LIGHT TRANSFORMER WIRING COVER MELTED AND BURNT. REPLACED TRA NSFORMER T1-52, WIRING TERMINAL ENDS, AND TERMINAL COVER. 2 L 7 2 4F A6WE 2001060700173 20010607 00173 EU 2001 6 7 QXEA0100731 1 20010426 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - CORROSION ON FUSELAGE SKIN UNDER FORWARD RAD ALT BLANKING PLATE. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGR APH 4. 2 L 7 2 4F RT A20EU 2001060700174 20010607 00174 EU 2001 6 7 QXEA0100732 1 20010425 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - FORWARD PIT AT STATION 9305B, STRINGER 74 LIGHT CORROSION UNDER ANCHOR NUT ON FRAME FLANGE. BLENDED OUT CORROSION IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4A. INSTALLED ANCHOR NUT IAW FOKKER SRM 51-31-01, PARAGRAPH 7, PAGE 13 AND 14. FOUND CORROSION TO BE WITHIN LIMITS AS PER FOKKER SRM 53-01-01, PAGE 6. 2 L 7 2 4F RT A20EU 2001060700175 20010607 00175 EU 2001 6 7 QXEA0100733 1 20010425 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - FORWARD PIT AT STATION 9305A AND STRINGER 1-2 UPPER FLANGE OF FRAME EXFOLIATED UNDER ANCHOR NUT AND TWO RIVETS. B LENDED OUT CORROSION AS PER FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4A. INSTALLED RIVETS AND ANCHOR NUT IAW FOKKER SRM 5 1-31-01, PARAGRAPH 6, PAGES 13 AND 14. FOUND CORROSION TO BE WITHIN LIMITS AS PER FOKKER SRM 53-01-01, PAGE 6. 2 L 7 2 4F RT A20EU 2001060700176 20010607 00176 EU 2001 6 7 QXEA0100734 1 20010426 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - FORWARD PIT AT STATION 9305 AND STRINGER 2 HAS CORROSION UNDER ANCHOR NUT OF FRAME FLANGE. BLENDED OUT CORROSION AS PER FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4A. FOUND TO BE WITHIN LIMITS IAW FOKKER SRM 53-01-01, PAGE 8, PARAGRAPH B. INSTALLED ANCHOR NUT IAW FOKKER SRM 51-31-01, PARAGRAPH 7, PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001060700177 20010607 00177 EU 2001 6 7 QXEA0100735 1 20010425 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - FORWARD PIT STATION 6805 ABOVE STRINGER 74, FRAME UPPER FLANGE IS EXFOLIATED UNDER ANCHOR NUT. BLENDED OUT MINOR CORROSION AS PER FOKKER SRM 51-10-04, PARAGRAPH 4A, PAGE 9. FOUND TO BE WITHIN LIMITS AS PER FOKER SRM 53-01-01, PAGE 6 . INSTALLED ANCHOR NUT IAW FOKKER SRM 51-31-01, PARAGRAPH 7, PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001060700178 20010607 00178 EU 2001 6 7 QXEA0100737 1 20010427 A 5315 FLOORBEAM FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - CORROSION ON FLOORBEAM AT FRAME 1385 AND BL280L. BLENDED AS PER FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4A. ALODI NED AS PER FOKKER SRM 51-10-04, PAGE 7, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 2001060700179 20010607 00179 EU 2001 6 7 QXEA0100738 1 20010426 A 5315 FLOORBEAM FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - CORROSION ON FLOORBEAM AT FRAME 1890 AND BL280L. BLENDED AS PER FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4A. ALODIN ED AS PER FOKKER SRM 51-10-04, PARAGRAPH 4, PAGE 7. 2 L 7 2 4F RT A20EU 2001060700180 20010607 00180 EU 2001 6 7 QXEA0100739 1 20010506 A 5280 BRACKET FOKKER F28 F28MK4000 4990810 EU LT MLG BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - TUNNEL BETWEEN WHEELBAYS, LEFT-HAND AFT MAIN LANDING GEAR DOOR BACKUP BRACKETS, FORWARD BRACKET CRACKED, AFT BRACK ET HAS LOOSE HI-LOK. REPAIRED IAW FOKKER SRM 51-30-02, PAGES 9 AND 10 AND SRM 51-31-01, PARAGRAPH 7, PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001060700181 20010607 00181 EU 2001 6 7 QXEA0100742 1 20010505 A 5310 STRUCTURE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - FRAME BOX FOR MAIN CABIN DOOR ACTUATOR FOUND TO BE CRACKED. INSTALLED NEW PART IAW FOKKER SRM. 2 L 7 2 4F RT A20EU 2001060700182 20010607 00182 EU 2001 6 7 QXEA0100743 1 20010511 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - CORROSION FOUND ON UPPER FRAME FLANGE OF FRAME 14755, IN VICINITY OF STRINGER 2. CORROSION BLENDED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4A. CORROSION BLENDED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4A. FOUND TO BE BEYOND AC CEPTABLE LIMITS. REPAIRED IAW HORIZON AIR EA 4-53-1487. 2 L 7 2 4F RT A20EU 2001060700183 20010607 00183 EU 2001 6 7 QXEA0100748 1 20010502 A 5210 CASTING FOKKER F28 F28MK4000 4990810 EU PAX DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - MAIN CABIN DOOR AFT LATCH FITTING BACK UP CASTING HAS MINOR CORROSION. BLENDED CORROSION IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4A. FOUND TO BE WITHIN LIMITS IAW FOKKER SRM 51-00-00, PAGE 2, PARAGRAPH 2. 2 L 7 2 4F RT A20EU 2001060700184 20010607 00184 EU 2001 6 7 QXEA0100750 1 20010424 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DISTORTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - FUSELAGE SKIN LOWER BELLY AFT OF REAR PRESSURE BULKHEAD AND FORWARD OF APU ACCESS DOOR 41-A, DISTORTED BEYOND LIMI TS IAW SRM 53-01-01. REPAIRED IAW FOKKER SRM 53-25-01, PAGE 3, ITEM 45 AND SRM 51-31-01, PARAGRAPH 7, PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001060700185 20010607 00185 NM 2001 6 7 USAA010519 1 20010508 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51503 22754 CLT - FOUND SIDE CHORD CRACKED .25 INCH, BS 178, WL 195 LEFT SIDE CHORD. DAMAGE REMOVED, SPLICED IN NEW CHORD SECTION P ER EO 5300V157. (M) 2 L 7 2 4F A16WE 2001060700186 20010607 00186 NM 2001 6 7 USAA010520 1 20010508 A 5312 PRESSURE PANEL BOEING 737 737201 1384454 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND UNBEADED PRESSURE WEB APPROX 3 SQUARE FEET, BS 666 WL 55. REINFORCING ANGLES INSTALLED PER SB 737-57-1234 A ND EA 69561. (M) 2 L 7 2 4F A16WE 2001060700187 20010607 00187 NM 2001 6 7 USAA010521 1 20010510 A 5313 STRINGER BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND STRINGER CRACKED .070 INCH, BS 380, STRINGER 2L. REMOVED DAMAGE SECTION, SPLICED IN NEW STRINGER SECTION PE R SRM 53-10-3. (M) 2 L 7 2 4F A16WE 2001060700188 20010607 00188 NM 2001 6 7 USAA010522 1 20010510 A 5320 ANGLE BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND SUPPORT ANGLE CRACKED 1.5 INCH, BS 727, LBL 27, WHEEL WELL COMPRESSION CHORD. INSTALLED REPAIR STRAPS AND D OUBLER ANGLE PER BOEING DRAWING NR 691A0068 AND EA 69571. (M) 2 L 7 2 4F A16WE 2001060700189 20010607 00189 NM 2001 6 7 USAA010523 1 20010510 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND FRAME CRACKED .25 INCH, BS 480 STRINGER 21L. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 51-40-3, FIG 1 . (M) 2 L 7 2 4F A16WE 2001060700190 20010607 00190 NM 2001 6 7 USAA010524 1 20010510 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND FRAME CRACKED 1.125 INCH, BS 277, STRINGER 16L. REMOVED DAMAGE, INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51-40-2, FIG 1. (M) 2 L 7 2 4F A16WE 2001060700191 20010607 00191 NM 2001 6 7 USAA010525 1 20010510 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND FUSELAGE SKIN WITH TWO CRACKS 1 INCH EACH, BS 727 PLUS 1 INCH AT STRINGER 17R AND BS 727A PLUS 6 INCHES AT S TRINGER 19R. INSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F A16WE 2001060700192 20010607 00192 NM 2001 6 7 USAA010533 1 20010511 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 284AU 47733 23131 CLT - FOUND SEVERAL 1 INCH AREAS OF CORROSION ON FLOORBEAM, BS 967, RBL 28 TO LBL 28. REMOVED DAMAGE, INSTALLED T-CAP S PLICE REPAIR PER SRM 53-10-09. (M) 2 L 7 2 4F A16WE 2001060700194 20010607 00194 EU 2001 6 7 USAASA01015 1 20010430 A 3397 WIRE AIRBUS A319 A319112 3930323 EU CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 EA 19 702UW 0896 MCO - EMERGENCY EXIT LIGHT AT ROW 6 WILL NOT ILLUMINATE. FOUND BROKEN WIRE AT CONNECTOR 5751VC AND REPAIRED SAME. (M) 2 L 7 2 4F RT A28NM 2001060700195 20010607 00195 EU 2001 6 7 USAASA01016 1 20010501 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320214 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 108UW 282 1061 CLT - FOUND AN INOPERATIVE POWER SUPPLY UNIT DURING TEST. MAINTENANCE REPLACED THE INOPERATIVE EMERGENCY POWER SUPPLY U NIT. OPERATIONALLY CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2001060700196 20010607 00196 EU 2001 6 7 USAA010507 1 20010507 A 5330 SKIN AIRBUS 320 A320214 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 110UW 2559 1112 DCA - FOUND FUSELAGE SKIN CRACKED 4 INCHES, JUST AFT OF FRAME NR 79, BETWEEN STRINGER 1R AND 2R. INSTALLED REPAIR DOUBL ER PER SRM 53-00-11 PAGE 209/210. (M) 2 L 7 2 4F RT A28NM 2001060800001 20010608 00001 2001 6 8 DHL2001807016 4 20010519 A 3421 GYRO DOUG DC8 DC873 302199C WP COCKPIT FAULTY A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 807DH 45990 AUTOPILOT ELEVATOR CONTROL JERKS ON CLIMBOUT AND IN LEVEL FLIGHT. AUTOPILOT ELEVATOR SERVO INDICATOR SHOWS CORRESPONDIN G MOVEMENT. THIS IS A REPEAT ITEM. COULD NOT DUPLICATE AUTOPILOT JERKS. SWAPPED TO AUX VERTICAL GYRO FOR TROUBLESHOOT ING. CAPTAINS NORMAL GYRO TO BE DEFERRED. SEE ITEM 3M. AUTOPILOT CHECKS GOOD IAW DC-8 22-0. 2 L 7 4 4F RT 4A25 2001060800002 20010608 00002 SO 2001 6 8 C2XA01IA248 1 20010517 A 4930 12018198017 B-NUT EMB 120 EMB120ER 3260203 SO APU LOOSE A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 16731 120190 IAH - FLIGHT 3443, THE CREW REPORTED A FUEL SMELL FROM THE APU BLEED. MAINTENANCE INSPECTED THE APU AND TIGHTENED THE B -NUT ATTACHING THE APU FUEL LINE TO THE APU, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001060800004 20010608 00004 SO 2001 6 8 C2XA01IA251 1 20010521 A 3231 12024188001 DOOR EMB 120 EMB120ER 3260203 SO LT MLG UNLATCHED A C2XA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SW 27 15725 120173 IAH - FLIGHT 2913, THE CREW REPORTED A NOSE GEAR UNSAFE LIGHT DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WITHOUT INCIDE NT. MAINTENANCE INSPECTED THE AIRCRAFT AND RELATCHED THE LEFT HAND FORWARD MAIN LANDING GEAR DOOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001060800005 20010608 00005 NM 2001 6 8 VNAA0105006 1 20010510 A 5270 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 427JS 3039 A PASSENGER DOOR OPEN INDICATION ON THE RWP. DISP WAS RELAYING INFO TO MX CONT WHO WAS GUIDING THE CREW THROUGH A PRESS PROBLEM. CREW REPORTED THAT PRESS WAS CLIMBING AROUND 1200 FT P/MIN, CAB PRESS NOT ALT. MX CONT INSTR CREW TO SWITCH FROM AUTO TO MAN, BEFORE THE CREW COULD SWITCH THE A/C PRESS WAS DESCENDNG AND THE LIGHT EXTINGUISHED. CREW DISCUSSED D IVERT BUT MX CON SAID IF DOOR IS SHUT AND LOCKED WITH NO LOSS OF PRESS IT IS A INDICATION PROB. CREW CONT, PRESS STABI LIZED AND NO FURTHER INCIDENT THE REST OF FLT. IN PHL CREW TBLSHOT PRESS PROB W/MX CON BY OPENING AND CLOSING DOOR. CO ULD NOT DUPLICATE FAILURE. NO OTHER PROBLEM REST OF FLIGHT. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001060800006 20010608 00006 NM 2001 6 8 0101815502 1 20010427 A 5320 CHANNEL BOEING 757 757251 1384970 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 502US 23191 DURING H-CHECK FOUND CORROSION ON INBOARD CHANNEL OF NUMBER 2 PASSENGER DOORWAY LOWER SILL BETWEEN BS 720 TO BS 740. RE PAIRED PER EA 55-183809. 2 L 7 2 4F RT A2NM 2001060800007 20010608 00007 NM 2001 6 8 CALA0100499 1 20010523 A 5753 SKIN BOEING 737 737524 1384721 NM FLAP GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19623 27527 INSPECTION FOUND NR 4 MID FLAP LOWER SKIN WORN/GOUGED AT NR 7 FLAP TRACK FAIRING, WBL 254. A REPAIR DOUBLER WAS INSTALL ED IAW ECRA 5753-01155, REV A. 2 L 7 2 4F RT A16WE 2001060800008 20010608 00008 WP 2001 6 8 CALA0100500 1 20010524 A 5531 SPAR DOUG DC9 DC982 3022082 WP VERTICAL STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 INSPECTION FOUND A .5 INCH CRACK IN VERTICAL STABILIZER LT FRONT SPAR AT CANTED FRAME STA 1388. THE CRACK WAS LOCATED N INE INCHES UP FROM BOTTOM END. THE SPAR WAS REPAIRED IAW ECRA 5510-01581. 2 L 7 2 4F A6WE 2001060800009 20010608 00009 WP 2001 6 8 CALA0100501 1 20010524 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND LT EXTERNAL FUSELAGE SKIN DENTED AT FS 233, LONGERON 23L. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-10 -4 AND 51-30-2. 2 L 7 2 4F A6WE 2001060800010 20010608 00010 EU 2001 6 8 SABA010017 1 20010518 A 7722 COMPUTER BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE331* 01514 WP RT ENGINE FAILED A SABA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 33 964AE 964 66313C AIRCRFT 964 ON FLIGHT 5071. DURING THE RIGHT ENGINE SRL BECAME INOPERATIVE. TAKEOFF WAS ABORTED. NO EMERGENCY WAS DEC LARED AND NO EMERGENCY PROCEDURES WERE USED. MAINTENANCE DEFERRED THE RIGHT SRL PER MEL. THIS REPORT TO BE SUPPLEMENTE D WHEN DEFERRAL IS CLEARED. 2 L 7 2 4T 3 T RT A56EU E2WE 2001060800011 20010608 00011 NM 2001 6 8 F3LA200100074 1 20010510 A 5320 FLOOR SUPPORT BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3498 23177 DURING C-6 CHECK INSPECTION REPORTED FLOOR STRINGER AT RBL 18.1 - BS 807-847 CORRODED. REMOVED DAMAGED FLOOR SUPPORT, F ABRICATED AND INSTALLED NEW SUPPORT AND ANGLES PER SRM 57-40-02, 53-60-53 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2001060800012 20010608 00012 WP 2001 6 8 AALA20010911 1 20010502 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 423AA 49335 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY PATH LIGHTING SYSTEM ON SEAT 5E IN OPERATIVE. REPLACED FORWARD LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY PATH LIGHTING ON SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001060800013 20010608 00013 EU 2001 6 8 AALA20010956 1 20010506 A 3350 AB51 BATTERY AIRBUS 300 A300B4605R 3930308 EU CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7082A 643 BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT FROM SEAT 18 THROUGH 27 DIM. REPLACED EMERGENCY EXIT LIGHT BAT TERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2001060800014 20010608 00014 WP 2001 6 8 AALA20010038 1 20010105 A 3150 WARNING SYSTEM DOUG DC9 DC982 3022082 WP COCKPIT MALFUNCTIONED A AALA K NONE N FALSE WARNING CR CRUISE 1 SW 21 292AA 49304 ORD - FLT 1800 - EN ROUTE DEN-ORD - HEARD A LOUD BANG AFT OF AIRCRAFT. PRESSURE FLOW LIGHT ILLUMINATED AND LATER LIGHT TURNED OFF. DETECTED LOSS OF CABIN PRESSURIZATION. LANDED ORD WITHOUT FURTHER INCIDENT. ACCOMPLISHED SINGLE PACK OPER ATIONS CHECK. NO DEFICIENCIES NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001060800015 20010608 00015 WP 2001 6 8 AALA20010931 1 20010411 A 5510 CASTING DOUG DC9 DC982 3022082 WP HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7517A 49894 TUL - FOUND HORIZONTAL STABILIZER SPREADER CASTING IS CORRODED BEYOND LIMITS, YV 222.4321. REMOVED AND REPLACED HORIZON TAL STABILIZER SPREADER CASTING PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2001060800016 20010608 00016 NM 2001 6 8 USAA010475 1 20010429 A 5320 ANGLE BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND AFT SERVICE DOOR Z-ANGLE CORRODED 40 INCHES BY .5 INCH, BS 947 TO 987, LBL 50. REMOVED AND REPLACED Z-ANGLE PER SRM 51-10-01. (M) 2 L 7 2 4F A16WE 2001060800017 20010608 00017 NM 2001 6 8 USAA010491 1 20010429 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND FLOORBEAM T-CAP CORRODED APPROX 13 SQUARE INCHES, BS 986.5, LBL 45 TO RBL 45. REMOVED AND REPLACED T-CAP PE R TYPICAL REPAIR 53-60-01 REV ''A''. (M) 2 L 7 2 4F A16WE 2001060800018 20010608 00018 NM 2001 6 8 USAA010493 1 20010429 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND FLOORBEAM T-CAP CORRODED .125 INCH, BS 967, RBL 42. DAMAGE REMOVED, SPLICED IN T-CAP REPLACEMENT PER SRM 53 -10-9. (M) 2 L 7 2 4F A16WE 2001060800019 20010608 00019 NM 2001 6 8 USAA010496 1 20010429 A 5313 STRINGER BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND STRINGER CORRODED 1 INCH BY 10 INCH AREA, BS 1006 TO 1016, S24R. REMOVED DAMAGE, FABRICATED NEW SECTION AND INSTALLED PER SRM 53-10-2. (M) 2 L 7 2 4F A16WE 2001060800020 20010608 00020 NM 2001 6 8 USAA010497 1 20010429 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND FUSELAGE SKIN CORRODED 2 INCH BY 3 INCH AREA, BS 468 BL 0. DAMAGED AREA CUTOUT, REPAIR DOUBLER INSTALLED PE R SRM 53-30-3. (M) 2 L 7 2 4F A16WE 2001060800021 20010608 00021 NM 2001 6 8 USAASB01127 1 20010503 A 2751 FLAP BOEING 737 7373B7 1384580 NM WINGS MALFUNCTIONED A USAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 EA 19 527AU 23862 ROC - FLT 582 - ON DESCENT INTO ROC FROM LGA, AT APPROXIMATELY 3,000 FEET, THE FLAP POSITION INDICATOR SHOWED A FLAP DIS AGREEMENT AND THE TRAILING EDGE FLAP INDICATOR CIRCUIT BREAKER WAS POPPED. CREW ACCOMPLISHED A ZERO FLAPS LANDING AT RO C WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RESET THE TRAILING CIRCUIT BREAKER AND PERFORMED OPERAT IONAL CHECK OF THE FLAPS SEVERAL TIMES. NO DEFECTS NOTED. (M) 2 L 7 2 4F RT A16WE 2001060800022 20010608 00022 NM 2001 6 8 USAASB01129 1 20010507 A 3260 189929 PROXIMITY SENSOR BOEING 737 737301 1384611 NM LANDING GEAR FAILED A USAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 19 563AU 23551 CLT - FLT 1670 - AFTER TAKEOFF FROM SAV, EN ROUTE TO CLT, CREW ATTEMPTED TO RAISE THE LANDING GEAR HANDLE BUT THE HANDLE WOULD NOT MOVE MORE THAN HALFWAY UP. AFTER FLAPS WERE UP, GEAR WARNING HORN STOPPED SOUNDING. CREW DID NOT ATTEMPT OV ER-RIDE BUT ELECTED TO CONTINUE TO CLT WITH THE LANDING GEAR DOWN AND LOCKED. FLIGHT LANDED AT CLT WITHOUT FURHTER INCI DENT. NO EMERGENCY WAS DECLARED. MAINTENANCE T/S SYSTEM PER MM AND FOUND THE S106 AIR/GROUND PROXIMITY SENSOR OPEN. R EMOVED AND REPLACED SENSOR PER MM 32-09-01. GEAR EXTENSION AND RETRACTION CHECKS GOOD. (M) 2 L 7 2 4F RT A16WE 2001060800023 20010608 00023 2001 6 8 USAASB01125 4 20010502 A 2216 AR6460M2 SERVO BOEING 737 7373B7 1384580 NM AUTOPILOT SYS FAILED A USAA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 EA 19 383US 31476 22956 CLT - FLT 1549 - ON CLIMB-OUT FROM CLT, EN ROUTE TO DFW, CREW RECEIVED A STABILIZER OUT OF TRIM LIGHT THAT WOULD FLICKER OFF AND ON. AT APPROXIMATELY FL270, THE AUTOPILOT BEGAN TO GIVE THE AIRCRAFT INCORRECT TRIM INPUTS AND THE AIRCRAFT WO ULD START TO NOSE OVER. ALSO, THE AUTO TRIM CIRCUIT BREAKER WOULD TRIP AND WHEN THE CREW TRIED TO RESET IT, IT WOULD TR IP AGAIN. AIRCRAFT COULD BE HAND FLOWN WITH NO PROBLEM AND WHEN MAINTENANCE SUGGESTED RESETTING CIRCUIT BREAKER (WHICH CREW HAD ALREADY TRIED), CAPTAIN DECIDED TO RETURN TO FIELD AT CLT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGEN CY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE AUTO PILOT STABILIZER TRIM SERVO PER MM 22-11-81. FUNCTIONAL CHE 2 L 7 2 4F RT A16WE 2001060800024 20010608 00024 NM 2001 6 8 USAA010504 1 20010507 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 270AU 49760 22882 SJO - FOUND FUSELAGE SKIN CRACKED 2.5 INCHES, BS 767, STRINGER 19R. DAMAGED AREA CUTOUT, INSTALLED FILLER AND REPAIR DO UBLER PER SRM 53-30-3, FIG 7. (M) 2 L 7 2 4F A16WE 2001060800025 20010608 00025 NM 2001 6 8 2001UALA00811 1 20010519 A 3350 COVER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN OUT OF ADJ A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 659UA 27114 EMERGENCY LIGHTS REMAIN DISARMED WITH COCKPIT CONTROL SWITCH IN ARMED POSITION. SUPPLEMENTAL DATA UPDATE ADJUSTED SWITCH COVER, OPS CHECK OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 2001060800027 20010608 00027 NM 2001 6 8 2001UALA00777 1 20010521 A 2131 CONTROLLER BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN PRESSURE MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 902UA 25002 UNSCHEDULED LANDING DUE TO PRESSURIZATION PROBLEM. SUPPLEMENTAL DATA UPDATE ACCOMPLISHED CHECK OF BOTH PACK SYSTEMS, AND ACCOMPLISHED PRESSURIZATION SYSTEM CHECK. NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001060800028 20010608 00028 NM 2001 6 8 F3LA200100075 1 20010521 A 2612 FIRE DETECTOR BOEING 737 7373M8 1384615 NM APU MALFUNCTIONED A F3LA F D ACTIVATE FIRE EXT. RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 03 303FL 25039 DURING TAXI FLIGHT CREW REPORTED APU FIRE WARNING SYSTEM WARNING LIGHT ILLUMINATED. DISCHARGED SQUIB. MAINTENANCE COND UCTED INSPECTION OF APU COMPARTMENT AND FOUND NO EVIDENCE OF FIRE. PLACARD SYSTEM PER MEL 26-07. AN ADDENDUM WILL BE I SSUED WHEN REPAIR IS ACCOMPLISHED. RAN APU SEVERAL HOURS AND PERFORMED OPERATIONAL CHECK OF APU FIRE DETECTION SYSTEM P ER MM 26-15-00, WITH NO DISCREPANCIES NOTED. 2 L 7 2 4F RT A16WE 2001060800029 20010608 00029 EU 2001 6 8 DHL2001364001 1 20010519 A 5410 ANGLE AIRBUS 300 A300B4203 3930306 EU NR 2 PYLON CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 0141 ON A-5 CHECK- NR 2 ENGINE PYLON HEAT EXCHANGER ACCESS, I/B AFT CORNER SUPPORT ANGLE CRACKED. REPLACED FORMED ANGLE AT N R 2 ENGINE PYLON HEAT EXCHANGER ACCESS CORNER IAW A-300 SRM 78-32-11 MATERIAL USED 2 INCH X 3 INCH OF 321-.032 LOT 68859 082, PO 8314616. 2 L 7 2 4F RT A35EU 2001060800030 20010608 00030 WP 2001 6 8 MWEA010822 1 20010524 A 5313 59114267 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 LONGERON 13 RIGHT AT 965 BULKHEAD ATTACH POINT, UPPER AND LOWER. REMOVED DAMAGED SECTION OF LONGERON, DRILLED NEW SECTI ON OF LONGERON, FABRICATED AND INSTALLED REPAIR SPLICE. 2 L 7 2 4F A6WE 2001060800031 20010608 00031 NM 2001 6 8 USAA010513 1 20010507 A 5312 BULKHEAD BOEING 737 737401 1384701 NM FUSELAGE BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 34933 23990 CLT - FOUND PRESSURE BULKHEAD WEB WITH BROKEN AREA .5 INCH BY .5 INCH, BS 178 WL 183 AT RBL 17. REMOVED DAMAGE AND INST ALLED REPAIR DOUBLER. (M) 2 L 7 2 4F RT A16WE 2001060800032 20010608 00032 WP 2001 6 8 AALA20010966 1 20010508 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP SERVICE DOOR SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 578AA 53155 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ASSEMBLY AT AFT SERVICE DOOR SHORTED. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT AFT SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001060800033 20010608 00033 NM 2001 6 8 AALA20010908 1 20010502 A 3350 0201875003 HARNESS BOEING 757 757223 1384957 NM CABIN FAULTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 625AA 24583 DFW - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT 19D INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT HARNESS AND LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001060800034 20010608 00034 EU 2001 6 8 USAAF01023 1 20010513 A 3110 6227957411 CONTROL PANEL FOKKER F28 F28MK0100 4990807 EU COCKPIT OVERHEATED A USAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 855US 20652 11283 MKE-PIT - FLT 1455 - DURING THE FLIGHT, A 'HOT PLASTIC' SMELL WAS NOTD IN THE COCKPIT. THE LEFT WINDSHIELD HEAT BUTTON WAS SELECTED OFF AND THE SMELL DIMINISHED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE THRUST RAT ING CONTROL PANEL. FUNCTIONALLY CHECKED OK. (M) 2 L 7 2 4F RT 2001060800035 20010608 00035 NM 2001 6 8 USAASB01132 1 20010509 A 3350 15AT17 SWITCH BOEING 737 737301 1384611 NM COCKPIT FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 576US 23741 CLT - MAINTENANCE FOUND THE EMERGENCY LIGHTS (NOT ARMED)INOPERATIVE/WON''T TEST. MAINTENANCE REMOVED AND REPLACED THE S OCKET/SWITCH ASSEMBLY ON THE P5 OVERHEAD PANEL. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001060800036 20010608 00036 NM 2001 6 8 USAASB01134 1 20010510 A 3350 1012621 LIGHT BOEING 737 737301 1384611 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 350US 23553 PIT - PILOT REPORTED THAT THE FORWARD FLOOR LEVEL EMERGENCY EXIT LIGHT, IN THE AISLE, IS DEFECTIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AND THE BATTERY PACK (P/N 2013-1A). OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001060800037 20010608 00037 NM 2001 6 8 USAA010508 1 20010507 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 33533 24548 CLT - FOUND BS 178 PRESSURE BULKHEAD WEB WITH CRACKS .125 INCH, .5 INCH, .8 INCH, 1 INCH AND 1.1 INCH, BS 178, FROM WL 1 88 TO WL 212.5, RBL 6.6 TO LBL 5. DAMAGE REMOVED, FILLERS AND REPAIR DOUBLER INSTALLED PER SRM 53-10-01, 53-10-08 AND E O 5300V153. (M) 2 L 7 2 4F RT A16WE 2001060800038 20010608 00038 NM 2001 6 8 USAA010509 1 20010507 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 33533 24548 CLT - FOUND SIDE CHORD CRACKED .5 INCH, BS 178, WL 207 LEFT SIDE OF AC. DAMAGED AREA CUTOUT, SPLICED IN NEW CHORD SECTI ON PER E5300157. (M) 2 L 7 2 4F RT A16WE 2001060800039 20010608 00039 NM 2001 6 8 USAA010510 1 20010507 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 34934 23990 CLT - FOUND LEFT SIDE CHORD CRACKED 1.2 INCH, BS 178 WL 207. DAMAGE REMOVED, SPLICED IN NEW CHORD SECTION PER EO 5300V1 57. (M) 2 L 7 2 4F RT A16WE 2001060800040 20010608 00040 NM 2001 6 8 USAA010511 1 20010507 A 5312 BULKHEAD BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 34934 23990 CLT - FOUND PRESSURE BULKHEAD WEB WITH THREE CRACKS, .125 INCH, .250 INCH AND .85 INCH, BS 178 WL 188 AND WL 234 RBL .5 TO LBL 12. DAMAGE CUTOUT, INSTALLED FILLERS AND REPAIR DOUBLER PER SRM 53-10-08 FIG 209, EO 5300V153 AND EA 69580. (M) 2 L 7 2 4F RT A16WE 2001060800041 20010608 00041 NM 2001 6 8 USAA010526 1 20010510 A 5320 TIE CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND STRINGER TIE CLIP CRACKED .25 INCH, BS 663, STRINGER 10R. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-2. ( M) 2 L 7 2 4F RT A16WE 2001060800042 20010608 00042 NM 2001 6 8 USAA010527 1 20010510 A 5320 TIE CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND STRINGER TIE CLIP CRACKED, BS 727A, STRINGER 6R. REMOVED AND REPLACED TIE CLIP P ER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 2001060800043 20010608 00043 NM 2001 6 8 USAA010528 1 20010510 A 5320 TIE CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43908 23743 CLT - FOUND STRINGER TIE CLIP CRACKED, .1875 INCH, BS 827, STRINGER 16R. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 2001060800044 20010608 00044 NM 2001 6 8 USAA010529 1 20010510 A 5320 TIE CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND TIE CLIPS CRACKED .25 INCH, BS 908, STRINGER 4L AND 5L. REMOVED AND REPLACED TIE CLIPS PER SRM 51-10-2. (M ) 2 L 7 2 4F RT A16WE 2001060800045 20010608 00045 NM 2001 6 8 USAA010530 1 20010510 A 5311 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND FRAME CRACKED .25 INCH, BS 727B, STRINGER 9R. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001060800046 20010608 00046 NM 2001 6 8 USAA010531 1 20010510 A 5311 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND FRAME CRACKED .5 INCH, BS 827 AT STRINGER 8R AND 9R. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001060800047 20010608 00047 EU 2001 6 8 USAASA01017 1 20010508 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319112 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 717UW 1069 SFO - THE EMERGENCY POWER SUPPLY UNIT POWER L FAILED THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE INOPERATIVE EM ERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2001060800048 20010608 00048 WP 2001 6 8 AALA20010965 1 20010507 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN LOOSE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 283AA 49296 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT GALLEY INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT WIR E AT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001060800049 20010608 00049 WP 2001 6 8 AALA20010969 1 20010510 A 3620 1173T0640 THERMOSWITCH DOUG DC9 DC982 3022082 WP TAIL DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 477AA 49652 DFW - FLT 1009 - EN ROUTE DFW-PHX, SHORTLY AFTER TAKEOFF AND CLIMB TAIL COMPARTMENT HIGH LIGHT ''ON'' ILLUMINATED. CHEC KLIST ACCOMPLISHED AND LIGHT EXTINGUISHED. AFTER SEVERAL MINUTES COMMENCED CLIMB AND LIGHT ILLUMINATED. LANDED DFW WIT HOUT INCIDENT. REPLACCED LEFT TAIL COMPARTMENT THERMOSWITCH AND CLEANED BOTH FLAPPER DOORS. SYSTEM GROUND CHECKED NORM AL OPERATION. (M) 2 L 7 2 4F A6WE 2001060800050 20010608 00050 NM 2001 6 8 AALA20010970 1 20010510 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 602AN 27053 DFW - DURING OVERNIGHT MAINTENANCE, RIGHT OVERWING EXIT SIGN DIM. REPLACED LAMPS IN RIGHT VOERWING EXIT SIGN. SYSTEM G ROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001060800051 20010608 00051 WP 2001 6 8 AALA20010971 1 20010510 A 3350 AML8095100GPL LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 221AA 49172 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR LIGHT INOPERATIVE AT SEAT 22. RELAMPED EMERGENCY EXIT LIGHT AT SEAT 22. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001060800052 20010608 00052 NM 2001 6 8 AALA20010972 1 20010510 A 3350 8039001 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 678AN 29428 DFW - DURING OVERNIGHT MAINTENANCE, AFT GALLEY EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED AFT GALLEY EMERGENCY EXIT BA TTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001060800053 20010608 00053 NM 2001 6 8 AALA20010973 1 20010510 A 3350 4008751 LIGHT BOEING 727 727227 1384078 NM AFT AIRSTAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 728AA 20735 DFW - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR EMERGENCY EXIT LIGHT ASSEMBLY INOPERATIVE. REPLACED AFT AIRSTAIR EMERG ENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001060800054 20010608 00054 WP 2001 6 8 AALA20010974 1 20010510 A 3350 AML8095100GPL LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 221AA 49172 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT ROW 7 INOPERATIVE. RELAMPED EMERGENCY EXIT FLOOR PATH LIGHT AT ROW 7. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001060800055 20010608 00055 NM 2001 6 8 AALA20010975 1 20010510 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 398AN 29605 ORD - DURING OVERNIGHT MAINTENANCE, AFT EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 3H DIM. RELAMPED AFT EMERGENCY EXIT FLO OR PATH LIGHT AT SEAT 3H. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001060800056 20010608 00056 NM 2001 6 8 AALA20010415 1 20010311 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 773AN 29583 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 35 THROUGH 40 DIM. REPLACED EMERGENCY EXIT LIGHT BATTER Y PACK AND CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001060800057 20010608 00057 NM 2001 6 8 AALA20010775 1 20010413 A 3350 8039001 BATTERY BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 645AA 24603 DFW - DURING OVERNIGHT MAINTENANCE, COCKPIT EMERGENCY EXIT LIGHT DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GR OUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001060800058 20010608 00058 NM 2001 6 8 AALA20010907 1 20010503 A 3350 SOCKET BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 658AA 24616 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT ROW 4 INOPERATIVE. REPLACED AFT LIGHT SOCKET ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001060800059 20010608 00059 NM 2001 6 8 AALA20010909 1 20010503 A 3350 AB51 BATTERY PACK BOEING 767 767223 1385123 NM CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 313AA 22316 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS FLICKER AT ROWS 30 THROUGH 37 LEFT. REPLACED BATTERY PACK FOR ROWS 30 THROUGH 37. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001060800060 20010608 00060 NM 2001 6 8 AALA20010912 1 20010502 A 3350 PIN BOEING 767 767323 1385205 NM CONNECTOR DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 379AA 25448 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT AT SEAT 34H INOPERATIVE. REPLACED CONNECTOR PIN ON SEAT 34H EMERGEN CY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001060800061 20010608 00061 NM 2001 6 8 AALA20010913 1 20010502 A 3350 PIN BOEING 767 767323 1385205 NM CONNECTOR DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 361AA 24042 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 33H INOPERATIVE. REPLACED CONNECTOR PIN ON SEAT 33H EM ERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001060800062 20010608 00062 NM 2001 6 8 AALA20010952 1 20010506 A 3350 LIGHT BOEING 767 767223 1385123 NM L1 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 315AA 22317 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L1 DOOR INOPERATIVE. RE-SEATED EMERGENCY EXIT LIGHT AT L1 D OOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001060800063 20010608 00063 NM 2001 6 8 AALA20010958 1 20010505 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 393AN 29430 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 22B INOPERATIVE. RE-SEATED EMERGENCY EXIT LIGHT CONNEC TOR AT SEAT 22B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001060800064 20010608 00064 NM 2001 6 8 AALA20010959 1 20010505 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 632AA 24590 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 14D AND 15D BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSE MBLY AT SEAT 14D AND 15D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001060800065 20010608 00065 NM 2001 6 8 AALA20010981 1 20010513 A 3350 TERMINAL BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 383AN 26995 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHT AT SEAT 31H INOPERATIVE. REPLACED BROKEN TERMINAL AT CO NNECTOR EMERGENCY ESCAPE PATH LIGHT AT SEAT 31H. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001060800066 20010608 00066 WP 2001 6 8 MWEA010813 1 20010521 A 5730 5912737502 PANEL DOUG DC9 DC914 3022034 WP RT WING DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 RIGHT WING TRAILING EDGE PANEL HAS A 1.25 INCH BY 1.5 INCH DENT, .063 DEEP LOCATED AT XRS 397. REMOVED DAMAGE AND INSTA LLED REPAIR IN ACCORDANCE WITH 57-04. 2 L 7 2 4F A6WE 2001060800067 20010608 00067 WP 2001 6 8 MWEA010812 1 20010521 A 5753 591216844 VANE DOUG DC9 DC914 3022034 WP RT WING FLAP DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 RIGHT WING FLAP MOVEABLE VANE HAS A 1.5 INCH BY .875 INCH, .063 INCH DENT 15 INCHES FROM INBOARD EDGE. REMOVED DAMAGE A ND INSTALLED REPAIR IN ACCORDANCE WITH 51-70-2. 2 L 7 2 4F A6WE 2001060800068 20010608 00068 WP 2001 6 8 MWEA010819 1 20010521 A 5753 99580764 RIB DOUG DC9 DC932 3022066 WP T/E FLAP CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 RIGHT WING NR 3 FLAP TRAILING EDGE OF RIB NR 3 END HOLE FOUND TO BE CRACKED. REMOVED NR 3 RIB, FABRICATED NEW ANGLE, NR 3 RIB AND INSTALLED NR 3 RIB AND RIB CAP. 2 L 7 2 4F A6WE 2001060800069 20010608 00069 NM 2001 6 8 UPS01235953 1 20010508 A 5313 STRINGER BOEING 727 72730C 1384009 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:C, AREA OF SUSPECT CORROSION AT S4L BS 1185. REPAIR CARRIED OUT IAW SRM 51-30-2, 53-10-00, 51-30-4. 2 L 7 3 4F A3WE 2001060800070 20010608 00070 EU 2001 6 8 QXEA0100740 1 20010506 A 3232 BRACKET FOKKER F28 F28MK4000 4990810 EU RT MLG CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - TUNNEL BETWEEN WHEELBAYS, RIGHT-HAND AFT MAIN LANDING GEAR DOOR ACTUATOR BACKUP BRACKETS, FORWARD BRACKET CRACKED. REPAIRED IAW FOKKER SRM 51-30-02, PAGE 9 AND 10 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001060800071 20010608 00071 NM 2001 6 8 AALA20010982 1 20010513 A 3350 TERMINAL BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 383AN 26995 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHT AT SEAT 29B INOPERATIVE. REPLACED BROKEN TERMINAL AT CO NNECTOR EMERGENCY ESCAPE PATH LIGHT AT SEAT 29B. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001060800072 20010608 00072 NM 2001 6 8 AALA20010984 1 20010514 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN DEFECTIVE A K NONE O OTHER IN INSP/MAINT 1 SW 21 613AA 24489 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD FIRST CLASS EMERGENCY PATH LIGHTING SYSTEM DIM. REPLACED BAD JUMPER WIRE FO R FORWARD FIRST CLASS EMERGENCY PATH LIGHTING SYSTEM. SYSTEM GROUND CHECK NORMAL OPERATIONS. (M) 2 L 7 2 4F RT A2NM 2001060800073 20010608 00073 NM 2001 6 8 CALA0100487 1 20010521 A 5330 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59302 23353 INSPECTION FOUND A .5 INCH CRACK IN SKIN OF AFT CUTOUT FOR THE E&E COMPARTMENT COOLING EXHAUST AT STA 373. AN INTERNAL DOUBLER WAS INSTALLED IAW ECRA 5330-02894. 2 L 7 2 4F RT A16WE 2001060800074 20010608 00074 WP 2001 6 8 CALA0100489 1 20010521 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND CABIN CENTER FLOOR PANEL DELAMINATED AT FS 905 - 946. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW ECRA 5100-01844. 2 L 7 2 4F A6WE 2001060800075 20010608 00075 WP 2001 6 8 CALA0100490 1 20010522 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 INSPECTION FOUND A .5 INCH CRACK IN TAIL COMPARTMENT BELTFRAME AT STA 1418, LONGERON 2L TO 2R. REPAIRED IAW DRAWING SR0 9530003. 2 L 7 2 4F A6WE 2001060800076 20010608 00076 WP 2001 6 8 CALA0100491 1 20010522 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND EXTERNAL FUSELAGE SKIN CREASED AT FS 312, LONGERON 24L. THE SKIN WAS COLD WORKED AND A DOUBLER WAS INS TALLED IAW SRM 51-10-2, 53-04, FIGURE 38, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 2001060800077 20010608 00077 WP 2001 6 8 CALA0100492 1 20010522 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND THE EXTERNAL FUSELAGE SKIN DENTED AT FS 340, LONGERON 24L. THE DENTED AREA WAS REFORMED AND A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38. 2 L 7 2 4F A6WE 2001060800078 20010608 00078 WP 2001 6 8 CALA0100493 1 20010522 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AND CREASED AT FS 322, LONGERON 25R. A REPAIR DOUBLER WAS INSTALLED IAW S RM 53-04, FIGURE 38, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 2001060800079 20010608 00079 WP 2001 6 8 MWEA010800 1 20010521 A 5730 5910013502 PANEL DOUG DC9 DC914 3022034 WP RT WING DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 RIGHT WING TRAILING EDGE PANEL HAS A 1.625 BY 1.0625 INCH DENT, 060 DEEP LOCATED AT XRS 474. REMOVED DAMAGE AND INSTALL ED REPAIR IN ACCORDANCE WITH 57-04. 2 L 7 2 4F A6WE 2001060800080 20010608 00080 WP 2001 6 8 MWEA010801 1 20010521 A 5730 5910013502 PANEL DOUG DC9 DC914 3022034 WP RT WING DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 RIGHT WING TRAILING EDGE PANEL HAS A 2.25 INCH BY 2.125 INCH DENT, .099 INCH DEEP LOCATED AT XRS 467. REMOVED DAMAGE AN D INSTALLED REPAIR IN ACCORDANCE WITH 57-04. 2 L 7 2 4F A6WE 2001060800081 20010608 00081 WP 2001 6 8 MWEA010802 1 20010521 A 5730 5912737502 PANEL DOUG DC9 DC914 3022034 WP RT WING DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 RIGHT WING TRAILING EDGE PANEL HAS 1 INCH BY 1 INCH DENT, .064 INCH DEEP LOCATED AT XRS 354. REMOVED DAMAGE AND INSTALL ED REPAIR IN ACCORDANCE WITH 57-04. 2 L 7 2 4F A6WE 2001060800082 20010608 00082 WP 2001 6 8 MWEA010814 1 20010521 A 5730 591237502 PANEL DOUG DC9 DC914 3022034 WP RT WING DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 RIGHT WING TRAILING EDGE PANEL HAS A 1.5 INCH BY 1.625 INCH DENT, .075 INCH DEEP LOCATED AT XRS 443. REMOVED DAMAGE AND INSTALLED REPAIR IN ACCORDANCE WITH 57-04. 2 L 7 2 4F A6WE 2001060800083 20010608 00083 WP 2001 6 8 MWEA010815 1 20010521 A 5730 5910013502 PANEL DOUG DC9 DC914 3022034 WP RT WING DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 RIGHT WING TRAILING EDGE PANEL HAS A 3 INCH BY 1.375 INCH DENT, .060 INCH DEEP LOCATED AT XRS 487. REMOVED DAMAGE AND I NSTALLED REPAIR IN ACCORDANCE WITH 57-04. 2 L 7 2 4F A6WE 2001060800084 20010608 00084 WP 2001 6 8 MWEA010809 1 20010521 A 5521 99184659 RIB DOUG DC9 DC914 3022034 WP ELEVATOR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 RIGHT ELEVATOR XHS 116 RIB HAS DAMAGE AT THE FORWARD OUTBOARD EDGE. REPAIRED DAMAGE IN ACCORDANCE WITH 51-30. 2 L 7 2 4F A6WE 2001060800085 20010608 00085 WP 2001 6 8 MWEA010808 1 20010521 A 5522 591041215 SKIN DOUG DC9 DC914 3022034 WP ELEVATOR DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 UPPER RIGHT ELEVATOR SKIN HAS FIVE DENTS BETWEEN STATION XHS 100 AND XHS 119. INSTALLED DOUBLER IN ACCORDANCE WITH 55-0 3. 2 L 7 2 4F A6WE 2001060800086 20010608 00086 WP 2001 6 8 MWEA010805 1 20010521 A 5730 5920872143 PANEL DOUG DC9 DC914 3022034 WP LT WING DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 DENT FOUND IN LEFT WING TRAILING EDGE PANEL LOCATED 10 INCHES OUTBOARD OF AILERON AND 10 INCHES FORWARD OF TRAILING EDGE . REPAIRED DAMAGE IN ACCORDANCE WITH 57-01. 2 L 7 2 4F A6WE 2001060800087 20010608 00087 WP 2001 6 8 MWEA010799 1 20010521 A 5730 591000317 SKIN DOUG DC9 DC914 3022034 WP RT WING DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 DENT LOCATED ON RIGHT WING LEADING EDGE AT STATION 477. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001060800088 20010608 00088 WP 2001 6 8 MWEA010816 1 20010521 A 5310 99577397 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 CRACK ON SHEAR TIE AT STATION 945 BETWEEN LONGERON 16 AND 15 LEFT. REMOVED SHEAR TIE, FABRICATED AND INSTALLED SHEAR TI E. 2 L 7 2 4F A6WE 2001060800089 20010608 00089 WP 2001 6 8 MWEA010820 1 20010521 A 5310 995773923 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 SHEAR TIE AT BS 945 LONGERON 10 TO 12 LEFT HAS ELONGATED HOLE. CUT OUT DAMAGED SECTION, FABRICATED NEW SECTION, DRILLED AND TRIMMED NEW SECTION, INSTALLED SHEAR TIE. 2 L 7 2 4F A6WE 2001060800090 20010608 00090 WP 2001 6 8 MWEA010803 1 20010521 A 5730 5912737501 PANEL DOUG DC9 DC914 3022034 WP LT WING DELAMINATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 REPAIR XRS 437 IS DELAMINATED ON LEFT WING TRAILING EDGE PANEL. REMOVED DAMAGE AND INSTALLED REPAIR IN ACCORDANCE WITH 51-70. 2 L 7 2 4F A6WE 2001060800091 20010608 00091 WP 2001 6 8 MWEA010804 1 20010521 A 5730 59127351 PANEL DOUG DC9 DC914 3022034 WP LT WING DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 DENT ON TOP SIDE OF LEFT WING TRAILING EDGE PANEL LOCATED ABOVE OUTBOARD AILERON. REMOVED DAMAGE AND INSTALLED REPAIR I N ACCORDANCE WITH 51-70. 2 L 7 2 4F A6WE 2001060800092 20010608 00092 WP 2001 6 8 MWEA010806 1 20010521 A 5730 5912737501 PANEL DOUG DC9 DC914 3022034 WP LT WING DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 FOUR DENTS FOUND ON TOP LEFT WING INBOARD TRAILING EDGE PANEL FORWARD OF AILERON. REMOVED DAMAGE AND INSTALLED REPAIR I N ACCORDANCE WITH 51-70. 2 L 7 2 4F A6WE 2001060800093 20010608 00093 WP 2001 6 8 MWEA010807 1 20010521 A 5730 99117844 PANEL DOUG DC9 DC914 3022034 WP RT WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 RIGHT WING D-DUCT LOCATED AT XRS 320 HAS A CRACK. INSTALLED DOUBLER IN ACCORDANCE WITH 57-06 FIG. 01. 2 L 7 2 4F A6WE 2001060800094 20010608 00094 WP 2001 6 8 MWEA010821 1 20010522 A 2613 7274551 CIRCUIT BREAKER DOUG DC9 DC982 3022082 WP COCKPIT FAILED A MWEA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 804ME 48030 WHEEL WELL OVERHEAT SENSOR CIRCUIT BREAKER TRIPPED. CHECK ALL SENSORS FOR OPERATION, REPLACED EFFECTED CIRCUIT BREAKER. 2 L 7 2 4F A6WE 2001060800095 20010608 00095 WP 2001 6 8 ABXA010236 1 20010516 A 3230 2763608 PIN DOUG DC8 DC863 302198A WP NLG SHEARED A ABXA K NONE O OTHER CL CLIMB 1 GL 23 820AX 46155 AFTER TAKEOFF, THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE RETRACT POSITION. THE JET PUMP WOULD NOT TURN OFF AND AUTO PRESSURIZATION CONTROL WOULD NOT WORK. MAINTENANCE INSPECTED AND REPLACED THE ANTI-RETRACTION SWIVEL PIN ON THE GROUND SHIFT MECHANISM. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2001060800096 20010608 00096 WP 2001 6 8 ABXA010235 1 20010515 A 5610 LOCK DOUG DC9 DC941 302207N WP COCKPIT DISCONNECTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 951AX 47616 THE PILOTS CLEARVIEW WINDOW AFT LOCK WAS DISCONNECTED. MAINTENANCE INSPECTED AND RECONNECTED THE AFT LOCK AS REQUIRED. 2 L 7 2 4F A6WE 2001060800097 20010608 00097 NM 2001 6 8 UPS01235946 1 20010510 A 5230 DOOR FRAME BOEING 727 72730C 1384009 NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:C, SUSPECT CRACK IN LWR AFT CORNER OF FWD CARGO DOOR FRAME. REPLACED LWR AFT CORNER OF FWD CARGO DOOR F RAME IAW DRAWING 65-18620. 2 L 7 3 4F A3WE 2001060800098 20010608 00098 NM 2001 6 8 UPS01435940 1 20010508 A 5312 PRESSURE PANEL BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:C-2 NOSE W/W TUNNEL RT BS 300 VERTICAL BEAM WEB BETWEEN 1ST & 2ND CLIP (COUNT FROM TOP) FOUND LOWER STAN DOFF HOLE CRACKED APPROX .25 INCH & .375 INCH LONG. CRACKED WEB REPLACED PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001060800099 20010608 00099 NM 2001 6 8 UPS01435941 1 20010510 A 3221 65B1008123 TRUNNION BOEING 747 747123 1384873 NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:C-2 NLG W/W - LT BS 380 TRUNNION FITTING MOST FWD LOWER HOLE FOUND CRACKED AT 5 O''CLOCK AND 11 O''CLOCK POSITION (LOOKING O/B). THE DISCREPANT CRACK STOP DRILLED, OPEN HOLE HFEC INSP C/O & NLG W/W LT BS 380 TRUNNION FITTIN G AND FOUND CRACK FREE. DETAIL VISUALLY INSP C/O & NO DEFECTS FOUND. TRUNNION FITTING REPAIRED AS PER RS-53-24-34657. THIS REPAIR IS TIME LIMITED FOR 24 MONTHS OR 500 CYCLES. TRUNNION FITTING TO BE REPLACED AT THE NEXT C-CHECK. 2 L 7 4 4F A20WE 2001060800100 20010608 00100 NM 2001 6 8 UPS01435960 1 20010509 A 5210 65B0831913 FITTING BOEING 747 747123 1384873 NM L3 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:C-2 M/D - L3 DOOR STOP SUPPORT FITTING FOUND CRACKED AT BS 1265 S-23L. STOP FITTING REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001060800101 20010608 00101 NM 2001 6 8 UPS01435962 1 20010507 A 5310 69B023288 SHEAR TIE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:C-2 FWD CARGO COMPT AFT BHD BS 1000 RBL 34 UPPER EDGE SHEAR TIE CRACKED. SHEAR TIE REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001060800102 20010608 00102 NM 2001 6 8 UPS01435963 1 20010507 A 5330 DOUBLER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:C-2 M/D - L5 DOOR FWD CUTOUT UPPER REVEAL DOUBLER FOUND CRACKED AT BS 2230 STR 15-16. DOUBLER REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001060800103 20010608 00103 WP 2001 6 8 UPS01835954 1 20010501 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C1 AFT PIT STA 1020 L36 2 NUT PLATES WITH CORROSION ON FRAME UNDER NUT PLATES. REMOVED CORROSION MAT ID 7075-T6 0.625 PO 334056. FAB IAW DWG DC8-53 A-011. HEAT TREATED, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. NEW FRAME CA P P/N 57643434507. LOCATED AND DRILLED HOLES IAW DC8 SRM 51-1-24. INSTALLED IAW DC8 SRM 51-2-20D. 2 L 7 4 4F RT 4A25 2001060800104 20010608 00104 WP 2001 6 8 UPS01835955 1 20010429 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C1 SKIN BELOW CUTOUT FOR AFT LT ENTRANCE DOOR CRACKED LWR FWD CORNER. REPAIRED AREA IAW REO G08018. 2 L 7 4 4F RT 4A25 2001060800105 20010608 00105 NM 2001 6 8 UPS01M35965 1 20010516 A 5210 LINE DOUG MD11 MD11F 3023600 NM L1 DOOR LOOSE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 251UP INSPECTION TYPE:C L1 DOOR CANNOT BE OPENED DURING DOOR ESCAPE SLIDE / RAFT DEPLOYMENT. L1 DOOR PNEUMATIC LINE FOUND LEA KING. LINE TIGHTENED, OPERATION CHECK IAW MM 52-11-04. 2 L 7 3 4F RT A22WE 2001060800106 20010608 00106 NM 2001 6 8 QXEA0100778 1 20010522 A 5210 CABLE DHAV DHC8 DHC8202 2809007 NM PAX DOOR OUT OF POSITION A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 345PH 476 SEA- MAIN CABIN DOOR WILL NOT OPEN. FOUND DOOR LIFT CABLE LOOPED AROUND LOWER FORWARD DOOR ROLLER. UNLOOPED CABLE. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001060800107 20010608 00107 EU 2001 6 8 01FDEA00382 1 20010523 A 2611 SMOKE DETECTOR AIRBUS 300 A300F4605R 3930327 EU E/E BAY ACTIVATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 665FE 769 AFTER GEAR RETRACT AVIONICS SMOKE ON ECAM. OPERATED SNIFFER FAN, NO SMOKE DETECTED. 2 L 7 2 4F RT A35EU 2001060800108 20010608 00108 WP 2001 6 8 CALA0100494 1 20010523 A 5342 ATTACH ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72825 49485 INSPECTION FOUND A 2 INCH CRACK IN LT VERTICAL STABILIZER LOWER ATTACH ANGLE, 7 INCHES FROM TRAILING EDGE. REPAIRED IAW SRM 53-05. 2 L 7 2 4F A6WE 2001060800109 20010608 00109 WP 2001 6 8 CALA0100495 1 20010523 A 5342 ATTACH ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72825 49485 INSPECTION FOUND A 1.5 INCH CRACK IN RT VERTICAL STABILIZER LOWER ATTACH ANGLE, 6 INCHES FROM TRAILING EDGE. REPAIRED I AW SRM 53-05. 2 L 7 2 4F A6WE 2001060800110 20010608 00110 WP 2001 6 8 CALA0100496 1 20010523 A 5350 CLIP DOUG DC9 DC982 3022082 WP TAILCONE OUT OF ADJ A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 THE INTERIOR TAIL CONE RELEASE HANDLE PULL FORCE WAS EXCESSIVE. THE TAIL CONE HANDLE CLIPS WERE ADJUSTED IAW MM 53-53-0 0. 2 L 7 2 4F A6WE 2001060800111 20010608 00111 WP 2001 6 8 CALA0100497 1 20010523 A 5350 CLIP DOUG DC9 DC982 3022082 WP TAILCONE OUT OF ADJ A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 THE EXTERIOR TAIL CONE RELEASE HANDLE PULL FORCE WAS LOW. THE TAIL CONE HANDLE CLIPS WERE ADJUSTED IAW MM 53-53-00. 2 L 7 2 4F A6WE 2001060800112 20010608 00112 WP 2001 6 8 CALA0100498 1 20010523 A 5350 CLIP DOUG DC9 DC982 3022082 WP TAILCONE OUT OF ADJ A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 THE CABIN AFT ENTRY DOOR TAIL CONE RELEASE HANDLE PULL FORCE WAS LOW. THE TAIL CONE HANDLE CLIPS WERE ADJUSTED IAW MM 5 3-53-00. 2 L 7 2 4F A6WE 2001060800113 20010608 00113 NM 2001 6 8 F3LA200100072 1 20010510 A 5347 CARGO TRACK BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3498 23177 DURING C-6 CHECK, INSPECTION REPORTED CARGO FLOOR TRACK CORRODED AT BS 800 TO 840 ABOVE STR 26R IN AFT CARGO BAY. FABRI CATED FLOOR TRACK AND SPLICE PLATES AND INSTALLED PER SRM 53-00-53, 51-10-02, SEC 53, AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2001061300001 20010613 00001 2001 6 13 DHL2001807018 4 20010516 A 2210 AUTOPILOT SYS DOUG DC8 DC873 302199C WP COCKPIT MALFUNCTIONED A DHLA K NONE F FLT CONT AFFECTED AP APPROACH 1 SO 01 807DH 45990 AUTOPILOT WHILE ON FINAL APPROACH BELOW 1000 FT ALT CONTINUED TO DIVERGE BELOW GLIDESLOPE WITHOUT CORRECTION. REPOSITIO NED LINKAGE ABOVE SERVO MICROSWITCH, OPS CKD OK IAW MM 22-20-0. 2 L 7 4 4F RT 4A25 2001061300002 20010613 00002 NM 2001 6 13 01FDEA00377 1 20010522 A 2612 FIRE LOOP BOEING 727 7272S2F 1384O81 NM NR 1 ENGINE FAULTY A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 216FE 22937 ON CLIMB FIRE WARNING SYS (WITH BELL) ACTUATED FOR 2 SEC. FIRE SYS TEST OK. *S/D* REMOVED AND REPLACED NR 1 ENG AND F IRE WALL LOOPS PER MM 26-11-012-4. OPS CK OK FOR SERVICE. 2 L 7 3 4F A3WE 2001061300003 20010613 00003 WP 2001 6 13 MWEA010823 1 20010524 A 5320 991960315 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 CORROSION ON FORWARD AND AFT SIDE OF SHEAR TIE BETWEEN LONGERON 29 LEFT TO 29 RIGHT STATION 890. REMOVED SHEAR TIE AND CORROSION, FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F A6WE 2001061300004 20010613 00004 EU 2001 6 13 A6WA200100033 1 20010426 A 5311 FRAME BAG BAE146 BAE146200A 1500266 EU FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 181US E2042 FUSELAGE FRAME 18 CRACKED. MAINTENANCE REPARED FRAME 18 LT SIDE IAW BAE SYSTEMS FAX REF BARA/AVR/5362/01, BARA/AVR/5360 /01, AND RIL HC537H9453. 2 H 7 4 4F RT A49EU 2001061300005 20010613 00005 EA 2001 6 13 A6WA200100035 2 20010520 A 7530 216035041 ACTUATOR BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502* 41580 EA NR 4 ENGINE FAILED A A6WA E ENGINE SHUTDOWN A FLAME/FIRE TX TAXI/GRND HDL 1 GL 31 156TR 7365 966 E2156 LF05224 NR 4 ENGINE AUTO SHUTDOWN GROUND PERSONNEL NOTICED FLAMES COMING OUT OF TAIL PIPE PILOT FIRED BOTH FIRE BOTTLES. MAINTE NANCE REMOVED AND REPLACED BLEED BAND ACTUATOR. 2 H 7 4 4F 4 F RT A49EU E6NE 2001061300006 20010613 00006 NM 2001 6 13 A6WA200100036 1 20010515 A 3260 870004 PSEU DORNER DO32 DO328100 2996000 NM LANDING GEAR FAILED A A6WA O OTHER J WARNING INDICATION DE DESCENT 1 GL 31 332PH 420 420 3010 HYD AUX QTY FAIL AND PROX SYS CAS DURING DESCENT GEAR WILL NOT COME DOWN AND HAD TO BE MANUALLY LOWERED. MAINTENANCE RE MOVED AND REPLACED PSEU. 2 H 7 2 4T RT A45NM 2001061300007 20010613 00007 NM 2001 6 13 01FDEA00381 1 20010523 A 2120 UNKNOWN BOEING 727 7272S2F 1384O81 NM COCKPIT ODOR A FDEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 25 217FE 22938 CREW SMELLED FUMES IN COCKPIT. DEBRIEF FUMES W/N SKYDROL, NOR FUEL, NOR ELECTRICAL. AS PRECAUTION RAN ENG AND PRESSURI ZED A/C PER 727 JRH. NO IRREGULAR ODORS, OPS CK NORMAL. 2 L 7 3 4F A3WE 2001061300008 20010613 00008 NM 2001 6 13 01FDEA00383 1 20010524 A 2824 40574 VALVE BOEING 727 72727C 138400J NM FUEL SYS STUCK A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 146FE 19110 NR 3 FUEL CROSSFEED VALVE W/N OPEN. *S/D* REMOVED AND REPLACED CROSSFEED VALVE ACTUATOR PER MM 28-22-011-4 PAR 4 A-D & PAR 9 A-P. VALVE OPS CK GOOD. 2 L 7 3 4F A3WE 2001061300009 20010613 00009 NM 2001 6 13 01FDEA00384 1 20010524 A 3510 OXYGEN BOTTLE BOEING 727 727227 1384078 NM FWD & AFT DEFECTIVE A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 485FE 21488 AFT APPROX 90 MIN OF FLIGHT OXYGEN PRESSURE WENT TO 100 PSI. ALL MASK IND WENT TO ORANGE. *S/D* REMOVED AND REPLACED BOTH FWD AND AFT NR 2 BOTTLES PER 727-200 MM 12-15-011-2 PAR 2. LEAK CK GOOD PER MM 35-00-000-2. 2 L 7 3 4F A3WE 2001061300010 20010613 00010 NM 2001 6 13 C1HA200184006 1 20010520 A 7930 CONNECTOR BOEING 727 7272S7 138407Z NM NR 1 ENGINE CONTAMINATED A C1HA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 684CA 22491 NR 1 LOW PRESSURE LIGHT INTERMITTANT BECAME CONTINUOUS. CONTACT MX CONTROL VIA ARINC PERFORMED COM CHECKLIST, DIVERTED TO DENVER. LIGHT CONTINUED TO FLICKER AFTER SHUTDOWN OF ENGINE. CLEANED CANNON PLUG ON OIL BYPASS SWITCH, OPS CHECK GO OD. 2 L 7 3 4F A3WE 2001061300011 20010613 00011 NM 2001 6 13 C1HA200194011 1 20010517 A 2923 57186 PUMP BOEING 727 727290 138408W NM NR 1 FAILED A C1HA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 294AS 22146 RETURN TO GATE. NR 1 B-PUMP OVERHEAT LIGHT ON CIRCUIT BREAKER POPPED. REMOVED AND REPLACED NR 1 B-PUMP LEAK AND OPS CH ECKED GOOD. 2 L 7 3 4F A3WE 2001061300012 20010613 00012 NM 2001 6 13 C1HA200194012 1 20010517 A 2923 PUMP BOEING 727 727290 138408W NM NR 1 MALFUNCTIONED A C1HA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 294AS 22146 NR 1 B-PUMP INOP BREAKER POPS REPEATEDLY. RE-SET BREAKER, REPLACED CASE DRAIN FILTERS FOUND CLEAN. OPERATED PUMP FOR 2 0 MIN WHILE OPERATING A & B SYSTEM COMPONENTS, OPS CK GOOD. 2 L 7 3 4F A3WE 2001061300013 20010613 00013 NM 2001 6 13 C1HA200193008 1 20010518 A 3520 OXYGEN MASK BOEING 727 727212 138407G NM CABIN DEPLOYED A C1HA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 15 293AS 21348 WHILE ON GROUND IN CANCUN. PASSENGER OXYGEN SYSTEM FELL (PRESSURIZED). RESET PAX O2 LEVER. REINSTALLED ALL O2 MASKS. O2 PRESSURE NORMAL. 2 L 7 3 4F A3WE 2001061300014 20010613 00014 EA 2001 6 13 COMA0160379 1 20010509 A 5346 60135006 BEAM CNDAIR CL600 CL6002B19 EA ENGINE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 914CA 18716 7012 LT SIDE OF ENGINE SUPPORT BEAM IS CRACKED AT PANEL CUTOUT AT FS 625.0. REMOVED DAMAGED AREA AND REPAIRED WITH PO 28317/ 2 .071 AND PO 29987/2 .063 7075 T6, IAW WVAC EO 601R-53-2437. 2 L 7 2 4F RT A21EA 2001061300015 20010613 00015 WP 2001 6 13 MWEA010828 1 20010524 A 5753 5912146504 PANEL DOUG DC9 DC932 3022066 WP T/E FLAP DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 REMOVED NR 3 FLAP TRAILING EDGE PANEL, TIP, C-CHANNEL, UPPER SKIN AND LEADING EDGE ANGLE. FABRICATED AND INSTALLED SKIN , C-CHANNEL AND ANGLES. LOCATED, DRILLED AND INSTALLED TIP. INSTALLED TRAILING EDGE PANEL. 2 L 7 2 4F A6WE 2001061300016 20010613 00016 NM 2001 6 13 0101825646 1 20010516 A 3246 162N000196 WHEEL BOEING 757 757251 1384970 NM NLG FAILED A NWAA K NONE O OTHER TX TAXI/GRND HDL 1 GL 01 546US 26493 DURING TAXI, APPROACHING RUNWAY FOR TAKEOFF, FLIGHT CREW HEARD NOSE GEAR POP. IMMEDIATELY INFORMED BY ANOTHER AIRCRAFT THAT THE TIRE APPEARED TO BE SEPARATING FROM THE WHEEL. MAINTENANCE FOUND THE BEAD FLANGE ON THE WHEEL SEPARATED. REPL ACED BOTH NOSE GEAR WHEEL ASSEMBLIES. 2 L 7 2 4F RT A2NM 2001061300017 20010613 00017 NM 2001 6 13 0101835501 1 20010516 A 2910 HYDRAULIC LINE BOEING 757 757251 1384970 NM NLG STEERING RUPTURED A NWAA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 01 501US 23190 DURING APPROACH AFTER GEAR EXTENSION, THE LEFT HYDRAULIC SYSTEM LOST ALL FLUID. AN EMERGENCY WAS DECLARED WITH DFR EQUI PMENT CALLED OUT. LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED THE RUPTURED NOSE GEAR STEERING HYDRAULIC LINE AND SERV ICED THE LEFT HYDRAULIC SYSTEM. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A2NM 2001061300018 20010613 00018 2001 6 13 0101845511 4 20010516 A 2565 D31041146 SLIDE BOEING 757 757251 1384970 NM L3 DOOR FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 511US 50616 5937 23199 EMERGENCY DOOR 3L ESCAPE SLIDE DID NOT DEPLOY WHEN DOOR WAS OPENED DURING DEPLOYMENT SAMPLING. THE SLIDE DID DEPLOY WHE N RESERVE HANDLE WAS PULLED. MAINTENANCE REPLACED DOOR 3L ESCAPE SLIDE ASSEMBLY. 2 L 7 2 4F RT A2NM 2001061300019 20010613 00019 WP 2001 6 13 0101871155 1 20010516 A 2530 HARNESS DOUG DC10 DC1040 3023508 WP OVEN BURNED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 155US 46764 DURING CLIMBOUT OF MSP, CABIN CREW REPORTED SMOKE AND ODOR IN MID CABIN. FOLLOWED COM PROCEDURE WITH NO NOTICEABLE CHAN GE IN CONDITION. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE DRAINED GEARBOX AND RESERVICED. CHAN GED SOCKS AND BURNED OUT PACKS. FOUND OVEN HARNESS BURNED. REPLACED HARNESS AND OVEN. RAN ENGINE WITH PACKS ON. OPER ATIONAL CHECK GOOD. 2 L 7 3 4F A22WE 2001061300020 20010613 00020 WP 2001 6 13 0101881155 1 20010517 A 2150 A/C PACK DOUG DC10 DC1040 3023508 WP A/C BAY CONTAMINATED A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 155US 46764 DURING CLIMB, FLIGHT ATTENDANTS REPORTED FUMES AND FINE MIST IN CABIN. FOLLOWED COM PROCEDURE. SMOKE DISSIPATED AFTER NR 1 PACK TURNED OFF. FLIGHT CONTINUED TO MCO FOR AN UNEVENTFUL LANDING. MAINTENANCE FOUND NR 1 PACK CONTAMINATED WITH OIL. REPLACED ALL THREE COALESCER BAGS. MEL NR 1 PACK. SYSTEM OPERATIONAL CHECK GOOD. 2 L 7 3 4F A22WE 2001061300021 20010613 00021 EA 2001 6 13 COMA0160380 1 20010320 A 5346 60135006 BEAM CNDAIR CL600 CL6002B19 EA ENGINE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 971CA 11497 7145 ENGINE SUPPORT BEAM ON THE LEFT AND RIGHT SIDE LOWER WEB HAS A CRACK AT THE FORWARD INBOARD CORNER OF THE LOWER ACCESS P ANEL. REPAIRED IAW WVAC EO 601R-53-2304C. 2 L 7 2 4F RT A21EA 2001061300022 20010613 00022 CE 2001 6 13 WVBA2001032 1 20010516 A 2701 12708441 CONTROL CABLE CESSNA 207 207A 2073604 CE YOKEE OUT OF POSITION E K NONE O OTHER IN INSP/MAINT 1 AL 05 738OU 20700428 AFTER A CRASH LANDING OF A SIMILAR AIRCRAFT, IT WAS DECIDED THAT AN INSPECTION OF THE RIBBON CABLE ASSEMBLY ON THE PILOT S CONTROL COLUMN BE CONDUCTED TO INSURE IT WAS NOT FOULING THE CONTROL COLUMN BEARING ASSEMBLY (UNIVERSAL) ON THE PILOTS CONTROL. IT WAS DISCOVERED THAT THE CABLE CONTACTED THE ROLLERS WHEN THE ELEVATOR WAS MOVED TO NOSE UP THIS COULD LEAD TO THE CABLE JAMMING THE ROLLERS RESULTING IN LOSS OF ELEVATOR CONTROL. PLASTIC TUBE WAS PLACED OVER THE CABLE TO PREV ENT THIS. 1 H 7 1 3O A16CE 2001061300023 20010613 00023 SO 2001 6 13 C2XA01BT094 1 20010520 A 2120 SMOKE EMB 145 EMB145 SO ALLSN AE300 AE3007A GL COCKPIT DETECTED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 12957 145080 EWR---CO4187 CREW REPORTED SMOKE IN COCKPIT AND AIRPLANE. DECLARED EMERGENCY AND RETURNED TO EWR. AIRCRAFT LANDED UNEV ENTFULLY. MAINTENANCE TROUBLESHOOTING FOUND NR ENGINE LEAKING OIL AT BOTTEM OF FAN, SUSPECT ZERO BEARING. RAN BOTH ENG INES AT POWER, NO SMOKE NOTED. AIRCRAFT BEING MAINTENANCE FERRIED TO TYS FOR ENGINE CHANGE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001061300024 20010613 00024 SO 2001 6 13 C2XA01BT095 1 20010522 A 2120 SMOKE EMB 145 EMB145 SO ALLSN AE300 AE3007A GL COCKPIT DETECTED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 14947 145054 ALB---CO3297, CREW REPORTED AT 7000 FEET AND 9 DEGREES CENTIGRADE THE ICE TEST WAS PERFORMED, NOTED A BURNING SMELL AND SMOKE FILLED COCKPIT. DECLARED EMERGENCY AND AIR RETURNED TO ALB. AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE TROUBLESH OOTING RAN BOTH ENGINES TO TAKEOFF POWER, PERFORMED ICE TEST. NO DEFECTS NOTED, OPS CHECKED GOOD IAW EMB145 MM 72-00-00 . AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001061300027 20010613 00027 CE 2001 6 13 GLBA2001106 1 20010522 A 7722 INDICATOR BEECH 1900 1900D 1154162 CE COCKPIT MALFUNCTIONED A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 01 247GL UE247 LEFT ENGINE ITT INDICATION HIGH AFTER T/O, PERFORMED ENGINE RUN ALL PARAMITERS WITHIN LIMITS. RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 2001082300003 20010823 00003 2001 8 23 GLBA2001107 4 20010523 A 2210 LMD7111P RELAY BEECH 1900 1900D 1154162 CE COCKPIT INTERMITTENT A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 01 154GL UE154 YAW DAMP ENGAGED ON T/O, REPLACE RELAY DMO8 PN LMD-7111-P AND MODULE K010 PN# LMD-5000-P OPS CHECK SYSTEM SATISFACTORY 2 L 7 2 4T RT A24CE 2001061300028 20010613 00028 CE 2001 6 13 GLBA2001108 1 20010523 A 7931 1013890233 TRANSDUCER BEECH 1900 1900D 1154162 CE LT ENGINE FLUCTUATES A GLBA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 01 169GL 5157 UE169 RIGHT ENGINE OIL PRESSURE FLUX. INSPECTED AND REPLACED PRESSURE TRANSDUCER. 2 L 7 2 4T RT A24CE 2001061300030 20010613 00030 EU 2001 6 13 C2XA01BT101 1 20010524 A 3234 F96GA0102 CONTROL HANDLE AEROSP ATR42 ATR42320 8680930 EU COCKPIT FAULTY A C2XA O OTHER N FALSE WARNING CR CRUISE 1 SW 27 14828 179 BTV---CO2938, CREW REPORTED LANDING GEAR UNLOCK LIGHT ON DURING FLIGHT BOTH SYSTEMS (LEFT MAIN). MAINTENANCE REMOVED AN D REPLACED LANDING GEAR CONTROL LEVER IAW ATR42 JIC 32-31-81. OPS CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001061300031 20010613 00031 GL 2001 6 13 C2XA01TY093 2 20010520 A 7200 23070401 BEARING EMB 145 EMB145 SO ALLSN AE300 AE3007A GL RT ENGINE LEAKING A C2XA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 12957 5395 5395 145080 CAE311150 EWR FLIGHT 4187. CREW REPORTED SMOKE IN THE COCKPIT AND CABIN DURING CLIMB. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE RIGHT HAND ENGINE ZERO BEARING TO BE LEAKING. THE AIRCRAFT WAS FERRIED TO TYS AND THE RIGHT HAND ENGINE WAS REMOVED AND REPLACED IAW CONTINENTAL EXPRESS TASK CARD 6271001 , ALL OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001061300032 20010613 00032 WP 2001 6 13 AT0100172 1 20010416 A 5311 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 803AT 47261 FOUND FRAME AT BS 598 LONGERON 11 CRACKED. FABRICATED AND INSTALLED REPAIR IAW REO-L00432. 2 L 7 2 4F A6WE 2001061300033 20010613 00033 WP 2001 6 13 AT0100173 1 20010323 A 5320 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 FOUND CRACK IN CABIN SUBFLOOR AT BS 598 LBL 52. FABRICATED AND INSTALLED REPAIR AND DOUBLER IAW DC9 SRM 53-01 PG 18. 2 L 7 2 4F A6WE 2001061300034 20010613 00034 WP 2001 6 13 AT0100174 1 20010323 A 5280 SKIN DOUG DC9 DC932 3022066 WP RT NLG DOOR CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 FOUND RIGHT SIDE OF NOSE GEAR DOOR SKIN CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-10-04, 53-05 FI G 62, AND 51-10-03. 2 L 7 2 4F A6WE 2001061300035 20010613 00035 WP 2001 6 13 AT0100175 1 20010323 A 5280 SKIN DOUG DC9 DC932 3022066 WP LT NLG DOOR CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 FOUND LEFT NOSE GEAR DOOR SKIN CRACKED. STOP DRILLED CRACKS AND INSTALLED DOUBLER IAW DC9 SRM 53-05 FIG 62, 51-10-05, A ND 51-10-03. 2 L 7 2 4F A6WE 2001061300036 20010613 00036 EU 2001 6 13 MALA010498 1 20010523 A 6120 231300701 CONTROLLER BAC 146 AVRO146RJ85A 1500097 EU NR 1 ENGINE FAILED A MALA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 GL 15 520XJ E2345 ON FLIGHT 3685 DEPARTING OUT OF XNA, 1,000 FT NR 1 ENGINE FLAMED OUT. FLIGHT CONTINUED TO MEM. NO EMERGENCY DECLARED. MAINTENANCE REPLACED OVERSPEED CONTROLLER P/N ON/OFF 2-313-007-01, S/N OFF 476 IAW 76-20-01 201. OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 2001061300037 20010613 00037 EU 2001 6 13 MALA010499 1 20010524 A 7730 TIMER SAAB SF340 340B 7860101 EU LT ENGINE DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 436XJ 436 FLIGHT 3112, EXPERIENCED LT ENGINE DDT SHIFT AND/OR RUNNING HOT. ON DEPARTURE ITT SHOWED A DIFFERENCE OF OVER 80 DEGREE S BETWEEN LT AND RT ENGINES AND AN EXCESS OF 40 DEGREES. FROM THE LAST CHARTED DELTA DELTA T. AIR RETURN TO DTW. MAIN TENANCE REMOVED AND REPLACED LT TIMER WITH SERVICEABLE UNIT. FOUND CRACK IN LT HP BLEED TUBE. REPLACED WITH SERVICEABL E UNIT IAW 340MM, ATA 72-00 AND CT7-9MM 72-00. 2 L 7 2 4T RT A52EU 2001061300038 20010613 00038 NM 2001 6 13 UPS01235967 1 20010509 A 5240 DOOR FRAME BOEING 727 72730C 1384009 NM GALLEY DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:C, CRACK ON AFT UPPER SECTION OF GALLEY DOOR FRAME. REPAIR CARRIED OUT IAW UPS EO B727-5240-4626. 2 L 7 3 4F A3WE 2001061300039 20010613 00039 NM 2001 6 13 UPS01235968 1 20010509 A 5320 STRAP BOEING 727 72730C 1384009 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:C CRACK INDICATIONS IN REINFORCING STRAP AT MID GALLEY DOOR FWD UPPER CORNER. REPAIR CARRIED OUT IAW UP S EO B727-5330-2685. 2 L 7 3 4F A3WE 2001061300040 20010613 00040 NM 2001 6 13 UPS01235975 1 20010509 A 5230 BEAM BOEING 727 72730C 1384009 NM CARGO DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:C MCD UPPER BEAM AND UPPER BEAM DOUBLER CORRODED. DOOR REMOVED AND UPPER BEAM AND UPPER BEAM DOUBLER RE PLACED. 2 L 7 3 4F A3WE 2001061300041 20010613 00041 NM 2001 6 13 UPS01235978 1 20010511 A 5754 WEB BOEING 727 72730C 1384009 NM L/E SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:C NR 3 SLAT ANTI ICE WEB IS CRACKED AT CUTOUT FOR ANTI ICE DUCT. REPAIRED IAW UPS AUTORIZATION B727-57- 20028 AND SMRO EO 2001-016-006. 2 L 7 3 4F A3WE 2001061300042 20010613 00042 NM 2001 6 13 UPS01235979 1 20010509 A 5320 FITTING BOEING 727 72730C 1384009 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:C NDI ON BS 950 RT FITTING CONFIRMED CRACK ON OUTBOARD FLANGE BETWEEN S9R AND 10R. RT 950 FRAME FITTING REPLACED IAW UPS EO B727-5310-3011. 2 L 7 3 4F A3WE 2001061300043 20010613 00043 NM 2001 6 13 UPS01235980 1 20010428 A 5312 BULKHEAD BOEING 727 72725C 138400H NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:C PRESSURE BULKHEAD CRACKED RBL 18 AT HAND PUMP LOWER OUTBOARD MOUNT BRACKET. CUT OUT CRACKED AREA AT B S 1183 RBL 18 AS PER SRM 51-10-1. NDI NO CRACK FOUND, INSTALLED DOUBLER PER B727 SRM 53-10-9. 2 L 7 3 4F A3WE 2001061300044 20010613 00044 NM 2001 6 13 UPS01235981 1 20010429 A 5310 BEAM BOEING 727 72725C 138400H NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:N/A VERTICAL BEAM AT BS 1183 CRACKED LBL 26.83 WL 260 APPROX 2 INCH LONG FROM LIGHTENING HOLE. REPAIRED CRACK BY STOP DRILLING. HFEC AREA INSTALLED REPAIR PER B727. 2 L 7 3 4F A3WE 2001061300045 20010613 00045 NM 2001 6 13 UPS01235982 1 20010428 A 3230 DRAG BRACE BOEING 727 72725C 138400H NM NLG CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:N/A DRAG BRACE SUPPORT BEAM IS CRACKED AT LT AFT CORNER CONFIRMED BY HFEC. STOP DRILLED CRACK PER SRM H FEC INSPECTED AREA FOUND NO CRACKS BEYOND AREA. FOUND CRACK TO BE BEYOND REPAIRABLE LIMITS PER UPS EO B727 -5310-0943. REMOVED AND REPLACED NOSE GEAR DRAG BRACE SUPPORT BEAM AND GEAR ANGLES PER EO AND BOEING DRAWING 65C15725. PERFORMED L EAK CHECK PER B727 MM 21-31-00, NO LEAKS FOUND. 2 L 7 3 4F A3WE 2001061300046 20010613 00046 NM 2001 6 13 UPS01435974 1 20010508 A 5411 FRAME BOEING 747 747123 1384873 NM NR 4 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:C-2, NR 4 PYLON AFT TORQUE BULKHEAD LT CHORD ABOVE LOWER SPAR FITTING FOUND 1 HOLE CRACK AT 2 O''CLOCK P OSITION (LOOKING FWD) APPROX 0.100 INCH LONG. NR 4 PYLON AFT TORQUE BULKHEAD LT CHORD ABOVE LWR SPAR FITTING REPAIRED A S PER HX RS R54-53-34658. 2 L 7 4 4F A20WE 2001061300047 20010613 00047 WP 2001 6 13 UPS01835986 1 20010508 A 5720 5769857304 INTERCOSTAL DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2,3 RIGHT WING L/E INTERCOSTAL IS CRACKED AT XS 454.976. REMOVED, FABRICATED, AND REPLACED INTERCOSTAL IAW DWG 5769857 AND SRM 57-1-0, 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001061300048 20010613 00048 WP 2001 6 13 UPS01835987 1 20010503 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2,3 STA 1400 FRAME IS CRACKED AT LONG 34R. REPAIRED FRAME IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001061300049 20010613 00049 WP 2001 6 13 UPS01835988 1 20010503 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2,3 STA 1394 FRAME IS CRACKED AT LONG 34R. REPAIRED FRAME IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001061300050 20010613 00050 WP 2001 6 13 UPS01835989 1 20010501 A 5210 SKIN DOUG DC8 DC873F 302199F WP PAX DOOR CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2,3 STA 45 FWD ENTRY DOOR SKIN IS CHAFED BEYOND LIMITS ABOVE HANDLE OPENING. REPAIRED SKIN IAW SRM 52- 2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001061300051 20010613 00051 WP 2001 6 13 UPS01835990 1 20010502 A 5312 PRESSURE PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2,3 STA 4 RBL 58 PRESSURE WEB IS CORRODED BEYOND LIMITS. REPAIRED WEB IAW SRO 8530026. 2 L 7 4 4F RT 4A25 2001061300052 20010613 00052 2001 6 13 SWIA972584 4 20010517 A 3425 COMPUTER EMB 120 EMB120RT SO PWA 118 PW118 NE E/E BAY MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 130G 120130 WHEN AUTOPILOT IS ENGAGED ON CAPTAINS SIDE, THE YOKE AND AIRCRAFT OSCILLATE ON ROLL AXIS CONTINUOUSLY. YOKE ROLLS ABOUT 2 INCHES TRAVEL. REMOVED AND REPLACED NR 1 AHC85 PER MM 34-21-01. OPS CHECK GOOD PER MM 34-21-00. AUTOPILOT OPS CHEC K GOOD PER MM 22-10-00. P/N: 622-6190-204, S/N ON: 2268, S/N OFF: 2125. (REFERENCE TRANS 659949 FOR TROUBLESHOOTING ). 2 L 7 2 4T 4 T RT A31SO E20NE 2001061300053 20010613 00053 SO 2001 6 13 SWIA972589 1 20010524 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE T/E FLAP DEFECTIVE A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 212SW 120276 FLAP ASYMMETRY ON OUTBOARD PAIR OF FLAPS ON FLAP RETRACTION DEPARTING CODY. FOLLOWED QRH, CYCLED FLAPS AND PROBLEM CORR ECTED. CONTINUED ON TO SLC. REMOVE AND REPLACE LEFT OUTBOARD FLAP ACTUATOR. OPS CHECKS GOOD. P/N ON 343000-1003, S/N ON 0520, S/N OFF 0244. 2 L 7 2 4T 4 T RT A31SO E20NE 2001061300054 20010613 00054 SO 2001 6 13 SWIA972590 1 20010524 A 3260 PROXIMITY SENSOR EMB 120 EMB120RT SO PWA 118 PW118 NE RT MLG OUT OF ADJ A SWIA O OTHER N FALSE WARNING AP APPROACH 1 NM 07 593SW 120191 ON APPROACH TO YUM, LEFT MAIN LANDING GEAR A-SYSTEM RED LIGHT WOULD NOT EXTINGUISH. A-SYSTEM GREEN LIGHT WOULD NOT ILLU MINATE. INSTALLED GEAR PINS AND SECURED. INSPECTED ALL PROXIMITY SENSORS, FOUND RIGHT MLG DOWNLOCK PROXIMITY SENSORS O UT OF ADJUSTMENT. ADJUSTED IAW MM 32-61-01. CYCLED GEAR SEVERAL TIMES. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001061300055 20010613 00055 2001 6 13 SWIA972591 4 20010522 A 3418 STALL WARNING EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 209SW 120269 SYSTEM 1 STALL WARNING CAME ON DURING TAKEOFF. REPLACED LAMP IN STALL WARNING PANEL. RERACKED NR 1 STALL COMPUTER. ST ALL WARNING OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001061300056 20010613 00056 EU 2001 6 13 JBXA000282 1 20010526 A 7931 APTE173TR1756 TRANSMITTER FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAY650 NE NR 1 ENGINE FAILED A JBXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 05 107ML 11450 17354 EN ROUTE FROM PHL TO DCA, PLANE RECEIVED A LIGHTNING SRIKE TO LEFT HAND SIDE OF PLANE. CREW RECEIVED A LOW OIL PRESSURE WARNING AND NR 1 ENGINE SHUT DOWN. CAPTAIN TRIED TO RESTART NR 1 ENGINE, RESTART WAS SUCCESSFUL, BUT RECIVED A LOW OIL PRESSURE WARNING AND CREW SHUT THE ENGINE DOWN. FLIGHT WAS NORTH OF BWI. CREW DECLARED AN EMERGENCY AND DIVERTED INTO BWI WITH ONE ENGINERUNNING. MX INSPECTED A/C FOR DAMAGE AND INSPECTED ENGINES. FOUND FAULTY OIL PRESSURETRANSMITTER O N THE NR 1 ENGINE. REMOVED AND REPLACED NR 1 ENGINE OIL TRANSMTITER IAW F-100 AMM 71-00-00. PERFORMED OPERATIONAL TEST OF NR 1 ENGINE. OPERATIONAL TEST PERFORMED GOOD IAW 71-00-00. 2 L 7 2 4F 4 F RT E25NE 2001061300057 20010613 00057 NM 2001 6 13 JBXA000283 1 20010521 A 3040 MOTOR BOEING 737 73776N NM WINDSHIELD WIPER MALFUNCTIONED A JBXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 05 311ML 30051 CAPTAINS WINDSHIELD WIPER STUCK IN THE VERTICAL POSITION WILL NOT OPERATE. DUE TO WEATHER PROBLEMS AT DESTINATION AIRPO RT AIRCRAFT RETURNED TO RDU. INSPECTED CAPTAINS SIDE WIPER MOTOR, CYCLED CIRCUIT BREAKER FOR WIPER MOTOR. PERFORMED OP ERATIONAL CHECK OF WIPER MOTOR IAW B-737 AMM 30-42-31. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2001061300058 20010613 00058 NM 2001 6 13 HNAA0100031 1 20010523 A 3234 574205 SELECTOR VALVE DHAV DHC8 DHC8102 2809003 NM LANDING GEAR LEAKING A HNAA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 EA 07 930HA 34622 8974 126 ON GEAR DOWN SELECTION, 3 UNSAFE RED LIGHTS ILLUMINATED AND GEAR DID NOT COME DOWN. GEAR ALTERNATE RELEASE WAS PERFORME D. 2 H 7 2 4T RT A13NM 2001061300059 20010613 00059 2001 6 13 JBXA000284 4 20010524 A 3418 TRANSDUCER CNDAIR CL600 CL6002B19 EA AOA FAILED A JBXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 05 588ML 7368 STALL FAIL CAUTION MESSAGE ON CLIMBOUT. COULD NOT GET TO RESET IN AIR. AIRCRAFT RETURNED TO RDU. REMOVED AND REPLACED NR 1 ANGLE OF ATTACK TRANSDUCER IAW CRJ AMM 27-35-05. RESET STALL PROTECTION COMPUTER MEMORY IAW CRJ AMM 27-35-01. PE RFORMED OPERATIONAL CHECK OF STALL PROTECTION SYSTEM IAW CRJ AMM 27-35-01. ALL OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2001061300060 20010613 00060 EU 2001 6 13 C2XA01BT103 1 20010503 A 5280 BUSHING AEROSP ATR42 ATR42320 8680930 EU LT MLG DOOR WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 99838 259 YUL---DURING 2C INSPECTION MAINTENANCE FOUND LEFTHAND MAIN LANDING GEAR DOOR HAS SOME PLAY ON LANDING GEAR LEG ATTACHMEN T. LEFTHAND MAIN LANDING GEAR BARREL REBUSHED AT BARREL LUG IAW EXELTECH EO 42/32/27. PLAY REMOVED FROM DOOR ATTACHMEN T. OPS CHECKED GOOD. 2 H 7 2 4T RT A53EU 2001061300061 20010613 00061 EU 2001 6 13 C2XA01BT105 1 20010504 A 7120 9507203 MOUNT AEROSP ATR42 ATR42320 8680930 EU LT ENGINE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 99838 259 YUL---DURING 2C INSPECTION IN MONTREAL, MAINTENANCE FOUND LEFTHAND ENGINE AFT INBOARD ENGINE MOUNT/CANISTER TORN ABOUT 1 .5 INCH. REMOVED AND REPLACED MOUNT WITH SERVICEABLE UNIT. OPS CHECKED GOOD IAW ATR42 JIC 71-22-01. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001061300062 20010613 00062 EU 2001 6 13 C2XA01BT106 1 20010509 A 7120 9509707BR MOUNT AEROSP ATR42 ATR42320 8680930 EU RT ENGINE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 99838 259 YUL---DURING 2C INSPECTION MAINTENANCE FOUND RT ENGINE INBOARD AFT MOUNT CRACKED (CANISTER). REMOVED AND REPLACED RT EN GINE INBOARD AFT MOUNT. OPS CHECKED GOOD. 2 H 7 2 4T RT A53EU 2001061300063 20010613 00063 EU 2001 6 13 C2XA01BT107 1 20010504 A 5415 415541020401F MOUNT AEROSP ATR42 ATR42320 8680930 EU RT ENGINE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 99838 259 YUL---DURING 2C INSPECTION MAINTENANCE FOUND RT ENGINE LT LOWER NACELLE ATTACHMENT HAS HOLE ELONGATED. RT FORWARD Z-MOU NT REMOVED AND REPLACED IAW ATR42 JIC 54-11-61. 2 H 7 2 4T RT A53EU 2001061300064 20010613 00064 EU 2001 6 13 C2XA01BT108 1 20010511 A 5744 ATTACH FITTING AEROSP ATR42 ATR42320 8680930 EU WINGS FAULTY A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 99838 259 YUL---DURING 2C INSPECTION MAINTENANCE FOUND FAULTY TRAILING EDGE ATTACH BRACKETS. REPAIRED THE UPPER SURFACE TRAILING EDGE ATTACHMENT FITTINGS IAW ATR42 SRM 57-50-00 FIGURE 402. 2 H 7 2 4T RT A53EU 2001061300065 20010613 00065 EU 2001 6 13 C2XA01BT109 1 20010510 A 5230 FRAME AEROSP ATR42 ATR42320 8680930 EU CARGO DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 99838 259 YUL---DURING 2C INSPECTION MAINTENANCE FOUND FIRST TWO CARGO DOOR UPPER FRAMES ARE CRACKED. CRACKED FRAMES REPAIRED IAW ATR42 SRM 52-31-00 FIGURE 402. AIRCRAFT RETURNED TO SERVICEABLE CONDITION. 2 H 7 2 4T RT A53EU 2001071100194 20010711 00194 NM 2001 7 11 01FDEA00385 1 20010525 A 5260 AIRSTAIR BOEING 727 727233 138408A NM FUSELAGE FIRE A FDEA O OTHER A FLAME/FIRE IN INSP/MAINT 1 SO 25 277FE 22042 DURING POST FLT SERVICE CHECK FIRE OCCURRED IN LEFT SIDE OF AFT AIRSTAIR AREA. *S/D* COMPLIED WITH KNOWN DISCREPANCY O F LEFT AFT AIRSTAIR FIRE UNDER HANGAR WORK ORDER NUMBER 17187. 2 L 7 3 4F RT A3WE 2001061300066 20010613 00066 EU 2001 6 13 01FDEA00387 1 20010527 A 2611 SMOKE DETECTOR AIRBUS 300 A300F4605R 3930327 EU MAIN CARGO BAY LOOSE A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 665FE 769 AFT T/O MAIN DECK CARGO SMOKE WARNING ON ECAM ILLUM. NR 2 UPPER DECK SMOKE DETECTOR UNIT LOOSE, TIGHTENED HOLDING NUT A ND PERF SMOKE DETECTOR SYS TEST PER IAW AMM 26-19-00-5, ALL TEST OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2001061300067 20010613 00067 NM 2001 6 13 01FDEA00389 1 20010525 A 5310 655613141 DOOR FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 276FE 22041 NR 3 CARGO DOORWAY FWD FRAME AT BS 1090 IS DENTED WITH A GOUGE IN THE CTR LOCATED BETWEEN NR 1 STOP PAD AND LATCH PLATE. R&R PER FEDEX EA 7-5310-56599, SRM 51-10-2, 51-20-4, 51-30-2. 2 L 7 3 4F RT A3WE 2001061300068 20010613 00068 WP 2001 6 13 ABXA010237 1 20010414 A 5320 3706753 STANCHION DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 78059 45999 THE FWD CARGO RT TUNNEL STANCHION WAS CORRODED ON THE LOWER RIGHT SIDE AT STA 360. MAINTENANCE INSPECTED AND REPLACED T HE STANCHION IAW DAC DRAWING 3706753 AND DC-8 SRM. 2 L 7 4 4F 4A25 2001061300069 20010613 00069 WP 2001 6 13 IXXA0100026 1 20010525 A 3231 DOOR DOUG DC8 DC871F 302199D WP MLG OUT OF RIG A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 826BX 45998 EN ROUTE FROM TOL TO BDL, THE LANDING GEAR DOOR UNSAFE WARNING LIGHT ILLUMINATED AFTER A SUCCESFUL GEAR UP LATCH CHECK W AS PERFORMED. THE FLIGHT RETURNED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED THE MAIN LANDING GEAR DOOR FOLLOW UP SYSTEM MISRIGGED. MAINTENANCE RIGGED THE FOLLOW UP SYSTEM IN ACCORDANCE WITH THE M AINTENANCE MANUAL AND PERFORMED A SUCCESSFUL OPERATIONAL CHECK. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2001061300070 20010613 00070 WP 2001 6 13 MWEA010829 1 20010529 A 5753 5910010505 VANE DOUG DC9 DC914 3022034 WP T/E FLAP DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 DENT FOUND IN LEFT FLAP MOVEABLE VANE, DENT MEASURES .080 DEEP. REPAIRED IN ACCORDANCE WITH 51-70-2. 2 L 7 2 4F A6WE 2001061300071 20010613 00071 EA 2001 6 13 COMA0160382 1 20010523 A 5311 FRAME CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 973CA 7146 LT AND RT FRAME AND AFT DOUBLER AT FS 718.0 ARE CRACKED BETWEEN STR 10-12. REPAIRED LT AND RT FS 718 IAW CANADAIR REO 6 01R-53-61-193. 2 L 7 2 4F RT A21EA 2001061300072 20010613 00072 EA 2001 6 13 COMA0160383 1 20010523 A 5320 601R313077 SPLICE PLATE CNDAIR CL600 CL6002B19 EA FUSELAGE MISMANUFACTURED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 976CA 11314 7151 ONE SPLICE PLATE 601R31030-77 WAS FABRICATED INCORRECTLY BY THE MANUFACTURER. FABRICATION OF SPLICE PLATE DOUBLER, IAW REO 601R-53-1477. 2 L 7 2 4F RT A21EA 2001061300073 20010613 00073 2001 6 13 C2XA01CL116 4 20010521 A 2350 7511001939 CONTROL PANEL EMB 135 EMB135LR SO COCKPIT BURNED OUT A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 16525 424 145403 LGA FLIGHT 3461 THE CREW REPORTED SMOKE IN THE COCKPIT AFTER ELECTRICAL POWER WAS TURNED ON. MAINTENANCE INSPECTED AND FOUND OBSERVER''S AUDIO CONTROL PANEL WAS BURNED OUT. THE PANEL WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. THE AIR CRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT TOOO11AT 2001061300074 20010613 00074 EU 2001 6 13 C2XA01BT110 1 20010526 A 3260 WARNING LIGHT AEROSP ATR42 ATR42320 8680930 EU COCKPIT ILLUMINATED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14828 179 EWR---CO3571, CREW REPORTED AIR RETURN TO EWR DUE TO GEAR UNLOCK LIGHT ILLUMINATING IN FLIGHT (LEFTHAND SIDE). MAINTENA NCE IN EWR AND BTV TROUBLESHOOTING AIRCRAFT. 2 H 7 2 4T RT A53EU 2001061300075 20010613 00075 2001 6 13 C2XA01CL117 4 20010522 A 3425 WIRE AEROSP ATR42 ATR42320 8680930 EU COCKPIT CHAFED A C2XA O OTHER I B FLT. ATTITUDE INST. SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 14832 187 CLE FLIGHT 3792 THE CREW REPORTED THE STANDBY ATTITUDE INDICATOR WENT BLANK FOLLOWED BY A ELECTRICAL SMELL IN FLIGHT. T HE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND THE POWER WIRE FOR THE INDICATOR WAS CHAFI NG ON A FRAME. THE WIRE WAS REPAIRED AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A53EU 2001061300076 20010613 00076 2001 6 13 DHL2001364019 4 20010523 A 2210 COMPUTER AIRBUS 300 A300B4203 3930306 EU AUTOPILOT SYS MALFUNCTIONED A DHLA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 364DH 0141 DURING TAXI THE PITCH FEEL NR 1 LIGHT ILLUMINATED. RAN ABNORMAL PROCEDURE AND SYS WAS RECOVERED. LIGHT EXTINGUISHED. RE-RACKED NR 1 ART FEEL COMPUTER AND CHECKED PER M/M 27-33-00. OK FOR CONTINUED SERVICE. 2 L 7 2 4F RT A35EU 2001061300077 20010613 00077 NE 2001 6 13 DHL2001708003 2 20010523 A 7260 STUD BOEING 727 72725 1384006 NM PWA JT8 JT8D7B 52053 NE GEARBOX MISSING A DHLA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 01 708DH 18275 649136 PRECAUTIONARY ENGINE SHUTDOWN DUE TO LOSS OF OIL. SHUTDOWN WHEN OIL PRESSURE STARTED TO DECREASE. ENGINE OIL PRESS/TEM P GOOD UNTIL TOUCHDOWN. PERFORMED ABNORMAL PROCEDURES. N1 & N2 ROTATION GOOD UNTIL TOUCHDOWN. ENGINE NR 1. FOUND GEA RBOX THRU STUD FELL OUT AND OIL LEAKING FROM GEARBOX SUMP. INSTALLED INSERT AND REINSTALLED STUD PER MM 72-61. RAN ENG INE, LEAK CHECK NORMAL. NO LEAKS NOTED. 2 L 7 3 4F 4 F A3WE E2EA 2001061300078 20010613 00078 2001 6 13 DHL2001365015 4 20010517 A 2230 B7CM1 COMPUTER AIRBUS 300 A300B4203 3930306 EU AUTOTHRUST SYS FAULTY A DHLA K NONE O OTHER CR CRUISE 1 SO 01 365DH 149 AUTO THROTTLES KEEP DISENGAGING. TEST COMPUTER GAVE CODE NR 61. REMOVED AND REPLACED AUTOTHROTTLE COMPUTER IAW MM 22-3 1-34, OPS CHECKS GOOD. 2 L 7 2 4F RT A35EU 2001061300079 20010613 00079 2001 6 13 DHL2001365016 4 20010525 A 2210 B5FM1 COMPUTER AIRBUS 300 A300B4203 3930306 EU AUTOPILOT SYS MALFUNCTIONED A DHLA K NONE O OTHER CR CRUISE 1 SO 01 365DH 149 A/P NR 1 WILL NOT STAY ENGAGED IN ARCH MODE. COULD NOT DUPLICATE ON GROUND. SWAPPED LOCK MONITOR COMPUTERS FOR TROUBLE SHOOTING PURPOSES. OPS NORMAL AT THIS TIME. 2 L 7 2 4F RT A35EU 2001061300080 20010613 00080 2001 6 13 DHL2001367005 4 20010517 A 2210 B5FM1 COMPUTER AIRBUS 300 A300B4203 3930306 EU AUTOPILOT SYS MALFUNCTIONED A DHLA K NONE O OTHER DE DESCENT 1 SO 01 367DH MSN265 AUTOPILOT NR 2 WOULD NOT TRACK LOCALIZER IN APPR MODE. DEVIATED UP TO 10 DEG LEFT AND RIGHT OF LOC HDG WITH CALM WIND. DURING TROUBLESHOOTING, FOUND MA TRIPPED FOR NR 2 AP/FD LOGIC/MONITOR COMPUTER ON AFCS TEST PANEL. PERF COMP TEST WITH FAULT CODE OF 52. SWAPPED NR 1 & NR 2 LOGIC/MONITOR COMPUTERS FOR FURTHER TROUBLESHOOTING. PERFORMED OPS OK W/CO, OP S NORMAL. 2 L 7 2 4F RT A35EU 2001061300081 20010613 00081 NM 2001 6 13 DHL2001709007 1 20010518 A 3260 LIGHT BOEING 727 72782C 1384026 NM COCKPIT MALFUNCTIONED A DHLA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 709DH 19968 LEFT GEAR WARNING LIGHT IN TRANSIT (RED) DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED. ALL GEAR LIGHTS TEST ARE NORMAL. M AIN LANDING GEAR LOCK SWITCHES TESTED PER MM 32-61-21 (4) CHKS OPS CHECK. 2 L 7 3 4F A3WE 2001061300082 20010613 00082 NM 2001 6 13 UPS01436013 1 20010526 A 5312 BULKHEAD BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:SP STA 2360 AFT PRESSURE BULKHEAD WEB IS CRACKED AT APPROX RADIAL STIFFENER 23. REPAIRED WEB IAW 8110-3 APPROVED DH SK 681-617. 2 L 7 4 4F A20WE 2001061300083 20010613 00083 WP 2001 6 13 UPS01835999 1 20010515 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 RIGHT WING L/E LOWER SKIN IS CORRODED BEYOND LIMITS AT XFS 372.75 TO XFS 379. REPAIRED SKIN IAW 81 10-3 APPROVED DH SK 880-554. 2 L 7 4 4F RT 4A25 2001061300084 20010613 00084 WP 2001 6 13 UPS01836000 1 20010502 A 5320 36169452 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA 830 FRAME FITTING BELOW LONG 21L AFT FACE IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITT ING IAW DWG 3616945,8110-3 APPROVED DH SK 880-861, SRM 53-1-0, 51-1-20D. 2 L 7 4 4F RT 4A25 2001061300085 20010613 00085 WP 2001 6 13 UPS01836001 1 20010501 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 FUSELAGE SKIN STA 1150 - 1230 LONG 28R - 33R IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SKIN SECTION IAW 8110-3 APPROVED DH SK 880-559. 2 L 7 4 4F RT 4A25 2001061300086 20010613 00086 WP 2001 6 13 UPS01836002 1 20010430 A 5330 9754028501 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA 270 - 370 LONG 28R - 33R FUSELAGE SKIN IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SKIN SE CTION IAW 8110-3 APPROVED DH SK 880-334. 2 L 7 4 4F RT 4A25 2001061300087 20010613 00087 WP 2001 6 13 UPS01836003 1 20010504 A 5312 PRESSURE PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 RIGHT NOSE TUNNEL UPPER PRESSURE WEB IS CORRODED BEYOND LIMITS AT STA -80 TO -99 AT RBL 36. REPAIR ED WEB IAW SRM 53-2-0 FIG 1D. 2 L 7 4 4F RT 4A25 2001061300088 20010613 00088 WP 2001 6 13 UPS01836004 1 20010506 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA -99 LT SIDE BULKHEAD CAP ANGLE IS CRACKED. REPAIRED ANGLE IAW 8110-3 APPROVED DH SK 880-270. 2 L 7 4 4F RT 4A25 2001061300089 20010613 00089 WP 2001 6 13 UPS01836006 1 20010503 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA 1140 FRAME IS CORRODED AND HAS MISDRILED HOLES BETWEEN LONG 32L TO 32R. REPAIRED FRAME IAW 811 0-3 APPROVED DH SK 880-085. 2 L 7 4 4F RT 4A25 2001061300090 20010613 00090 WP 2001 6 13 UPS01836007 1 20010430 A 5312 97537514N BULKHEAD DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA 683 PRESSURE BULKHEAD IS CRACKED RBL 6-24. REMOVED AND REPLACED BULKHEAD IAW DWG 9753751, AND SRM 53-1-0, 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001061300091 20010613 00091 WP 2001 6 13 UPS01836008 1 20010511 A 5312 PRESSURE PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 RT NOSE TUNNEL UPPER PRESSURE WEB IS CORRODED BEYOND LIMITS STA-16 AT RBL 20. REPAIRED WEB IAW 811 0-3 APPROVED DH SK 880-304. 2 L 7 4 4F RT 4A25 2001061300092 20010613 00092 WP 2001 6 13 UPS01836009 1 20010501 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1,3 STA 1766 LONG 10R BULKHEAD ANGLE/CHORD IS CRACKED. REPAIRED ANGLE IAW SRM 53-2-5 FIG 9. 2 L 7 4 4F RT 4A25 2001061300093 20010613 00093 WP 2001 6 13 ZW0A0102305 1 20010522 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 960TW 49231 DURING CHECK-C MAINT FUSELAGE STA 1380, LONGERON 14L, HAD .25 INCH INCH CRACK AFT OF RIVET. REPAIRED PER SRM 53-04, FIG 18, AND 51-30-2. 2 L 7 2 4F A6WE 2001061300094 20010613 00094 WP 2001 6 13 ZW0A0102306 1 20010521 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 924TW 49100 DURING CHECK-C MAINT AT THE AFT FUSELAGE FRAME, INNERGRANULAR CORROSION WAS FOUND ON THE FLOOR SUPPORT 4 INCHES FROM THE RT SIDE OF THE FUSELAGE, STA 138. CUT OUT CORRODED WEB, SANDED, CLEANED, PRIMED PER SRM 5-10-2A AND 51-10-3. MADE WEB REPAIR PER SRM 51-70-4 FIG 2, AND SRM 51-30-1 AND 51-30-3. 2 L 7 2 4F A6WE 2001061300095 20010613 00095 WP 2001 6 13 ZW0A0102307 1 20010524 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 907TW 49165 DURING CHECK-C MAINT THE FORMER FOOT WAS CRACKED AT STA 1437, BETWEEN LONGERON 1 AND 2R. INSTALLED NEW CLIP (FORMER FOO T) PER SRM 51-30-2, SRM 51-30-5 AND SRM 51-60-0. 2 L 7 2 4F A6WE 2001061300096 20010613 00096 WP 2001 6 13 ZW0A0102308 1 20010524 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 924TW 49100 DURING CHECK-C MAINT FOUND CORROSION AND CRACKS ON FLOOR MEMBRANE AT STA 1136 TO 1287, APPROX LEFT BODY LINE 58. REMOVE D AND REPLACED WITH NEW MEMBRANE PER SRM 51-30-1 AND 55-30-2, AND 51-30-5, AND SPM 6-70-01 FROM STATION 1098 TO 1309 LEF T. 2 L 7 2 4F A6WE 2001061300097 20010613 00097 WP 2001 6 13 ZW0A0102309 1 20010524 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 924TW 49100 DURING CHECK-C MAINT THE NUMBER 1 CHAIR TRACK FLOOR MOUNT BOLT HOLES HAD CORROSION ON OUTBOARD SIDE OF TRACK BETWEEN STA 1174 AND 1193. NEW TRACK INSTALLED PER SRM 51-30-02, SRM 51-30-01, AND SPM 6-70-01. 2 L 7 2 4F A6WE 2001061300098 20010613 00098 WP 2001 6 13 ZW0A0102310 1 20010522 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND CORROSION IN FORMER STA 1231 AFT SIDE AT LONGERON 29R, 30, 29L, 28L, 2 7L, AND 26L. ALSO CORROSION ON UNDER SIDE. 2 L 7 2 4F RT A6WE 2001061300099 20010613 00099 WP 2001 6 13 ZW0A0102311 1 20010522 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT AT THE AFT SVC AREA, STA 1166 FLOOR SUPPORT WAS CORRODED, LBL 23 INCHES. MADE NEW SUPPORT FROM NEW EXTRUSION PER SRM 53-14-3 AND INSTALLED WITH HI-LOK PER SRM 51-30-5. 2 L 7 2 4F RT A6WE 2001061300100 20010613 00100 WP 2001 6 13 ZW0A0102312 1 20010522 A 5320 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT IN THE AFT CARGO COMPT, STA 1152 BETWEEN LONGERON 30 AND 29R THE INTERCOSTAL WAS CORRODED. REMOVED CORROSION PER SRM 6-80-01. INSTALLED INTERCOSTAL AT STA 1152, BETWEEN LONGERON 30 AND 29R PER SRM 51-30. 2 L 7 2 4F RT A6WE 2001061300101 20010613 00101 WP 2001 6 13 ZW0A0102313 1 20010523 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT IN THE CABIN THE FLOOR SUPPORT WAS CORRODED AT STA 204, LBL 6 INCHES. FABRICATED FLOOR SUPPORT FRO M 7075-T6 PER SAMPLE AND PER SPM 6-70-01. 2 L 7 2 4F RT A6WE 2001061300102 20010613 00102 WP 2001 6 13 ZW0A0102314 1 20010523 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT IN THE AFT CARGO COMPT THE FLOOR SUPPORT ANGLE WAS CORRODED AT STA 1155, BETWEEN LONGERON 29R AND 2 8R, TOP AND BOTTOM. . 2 L 7 2 4F RT A6WE 2001061300103 20010613 00103 WP 2001 6 13 ZW0A0102315 1 20010523 A 2560 FITTING DOUG DC9 DC983 3022083 WP CABIN CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT IN THE AFT CABIN THE AFT SERVICE DOOR AFT GIRT BAR FITTING HAD CORROSION. REPLACED GIRT BAR FITTIN G PER DRAWING 9930612. INSTALLED SAME PER SRM 51-30-5. 2 L 7 2 4F RT A6WE 2001061300104 20010613 00104 WP 2001 6 13 ZW0A0102316 1 20010523 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT MEMBRANE WAS CRACKED AT STA 1168 AT AFT GIRT BAR FITTING. REPAIRED MEMBRANE PER SRM 51-70-4, FIG 2 . 2 L 7 2 4F RT A6WE 2001061300105 20010613 00105 WP 2001 6 13 ZW0A0102317 1 20010524 A 5280 CHANNEL DOUG DC9 DC983 3022083 WP RT MLG DOOR CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT THE RT MLG WHEEL WELL GEAR DOOR FWD ANGLE WAS CRACKED JUST AFT OF THE HYD RESERVOIR SERVICE DOOR. INSTALLED NEW CHANNEL. MADE NEW CLIPS AS NEEDED PER DRAWING 5930584 FOR MATERIAL AND SHAPE. INSTALLATION PER SRM 51-30 -2 AND 51-30-4. SEALED PER SRM 51-20-0. 2 L 7 2 4F RT A6WE 2001061300106 20010613 00106 WP 2001 6 13 ZW0A0102318 1 20010524 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND CABIN MEMBRANE CORRODED ON LT SIDE AT STA 833 TO 837. CUT OUT CORRODED AREA AND MADE REPAIR DOUBLER. INSTALLED REPAIR PER SRM 51-70-4. 2 L 7 2 4F RT A6WE 2001061300107 20010613 00107 WP 2001 6 13 ZW0A0102319 1 20010524 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT IN THE AFT CARGO COMPT AT STA 1155, LONGERON 30 TO 29R, THE FORMER FOOT WAS CORRODED. REPLACED PAR T PER SPM 6-70-01 USING PRINT 9936073. INSTALLED HI-LOKS PER 51-30-5 AND RIVETS PER SRM 51-30-02. 2 L 7 2 4F RT A6WE 2001061300108 20010613 00108 WP 2001 6 13 ZW0A0102321 1 20010524 A 5320 ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND ANGLE CRACKED AT STA 110, FWD SIDE OF WEB, JUST OTBD OF RAIN REPELLANT BOTTLE AT INTERCOSTAL. INSTALLED NEW ANGLE PER SRM 51-30-3 AND SRM 51-30-0. 2 L 7 2 4F RT A6WE 2001061300109 20010613 00109 WP 2001 6 13 ZW0A0102322 1 20010524 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT ON LT SIDE OF CABIN, STA 1212 TO 1231, FOUND CORROSION ON MEMBRANE. CUT OUT CORROSION FROM MEMBRAN E. FABRICATED AND INSTALLED REPAIR PER SRM 51-70-4. TREATED AND PRIMED AND INSTALLED WET PER SRM 51-10-3. 2 L 7 2 4F RT A6WE 2001061300110 20010613 00110 WP 2001 6 13 ZW010102323 1 20010523 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 907TW 49165 DURING CHECK-C MAINT FOUND CORROSION ON TOP SIDE OF FLOORBEAM AT STA 1338, BL 47R THRU BL 57R. REMOVED DAMAGED SECTION OF FLOORBEAM CAP. MANUFACTURED NEW SECTION OF FLOORBEAM CAP PER SRM 51-10-1. TREATED PER SRM 51-10-3. INSTALLED NEW S ECTION OF FLOORBEAM CAP PER SRM 51-30-5. 2 L 7 2 4F A6WE 2001061300111 20010613 00111 WP 2001 6 13 ZW0A0102324 1 20010523 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 907TW 49165 DURING CHECK-C MAINT FOUND NUMBER 1 CHAIR TRACK CORRODED FROM STA 1079 TO 1309. REPLACED CORRODED SECTION OF TRACK FROM STA 1079 TO 1136 WITH NEW SECTION. INSTALLED PER SRM 51-30-01. 2 L 7 2 4F A6WE 2001061300112 20010613 00112 WP 2001 6 13 ZW0A0102325 1 20010523 A 5320 BRACKET DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 907TW 49165 DURING CHECK-C MAINT FOUND CORROSION IN BRACKET, LOWER AFT CORNER OF THE AFT CARGO DOOR THRESHOLD. REPLACED LOWER AFT T HRESHOLD BRACKET. USED SUBSTITUTE HI-LOKS PER SRM 51-60-0, FIG 4 PAGE 36. 2 L 7 2 4F A6WE 2001061300113 20010613 00113 WP 2001 6 13 ZW0A0102326 1 20010524 A 5320 BRACKET DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 907TW 49165 DURING CHECK-C MAINT FOUND CORROSION IN BRACKET, LOWER FWD CORNER OF AFT CARGO DOOR THRESHOLD. INSTALLED NEW BRACKET PE R SRM 51-10-5 AND SRM 51-60-0, FIG 4 PAGE 36. 2 L 7 2 4F A6WE 2001061300114 20010613 00114 WP 2001 6 13 ZW0A0102327 1 20010523 A 5320 STRAP DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 924TW 49100 DURING CHECK-C MAINT AT STA 225, LBL 58 INCHES, STRAP ON TOP OF MEMBRANE HAD HEAVY CORROSION AND RIVET HEADS CORRODED OF F. FABRICATED SPLICE PER DRAWING 9923666-9 PER SPM 6-70-01 PAR 4. 2 L 7 2 4F A6WE 2001061300115 20010613 00115 WP 2001 6 13 ZW0A0102328 1 20010523 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 924TW 49100 DURING CHECK-C MAINT FOUND HEAVY CORROSION ON MEMBRANE AND CUSP ANGLE AT STA 225, LBL 58 INCHES. REMOVED CORROSION PER SPM 6-80-01 FROM CUSP. REMOVED DAMAGED AREA OF MEMBRANE. METAL SHOP FABRICATED SECTION OF MEMBRANE. INSTALLED MEMBRAN E SECTION PER 53-09, PAGE 9, AND SPM 6-70-01 PARAGRAPH 4. 2 L 7 2 4F A6WE 2001061300116 20010613 00116 WP 2001 6 13 ZW0A0102329 1 20010521 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT IN FWD CARGO COMPT, FOUND CORROSION GROUND TOO THIN AT STA 522, RT TRACK. CORROSION WAS REMOVED. REMOVED AND REPLACED WITH NEW TRACK WITH SPLICE REPAIR PER SRM 53-05, PAGE 10R. 2 L 7 2 4F RT A6WE 2001061300117 20010613 00117 WP 2001 6 13 CALA0100502 1 20010524 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND RT EXTERNAL FUSELAGE SKIN DENTED BETWEEN FS 313 - 332, LONGERON 20-21R. THE EXISTING DOUBLER WAS REMOV ED IAW SRM 51-30-05 AND 51-30-02. THE DENTED SKIN WAS REMOVED IAW SRM 53-04, FIGURE 12 & 13. REPAIR DOUBLERS AND FINGE R DOUBLERS WERE INSTALLED IAW SRM 53-04, FIGURE 12B, 51-10-3, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 2001061300118 20010613 00118 WP 2001 6 13 CALA0100503 1 20010524 A 5280 SKIN DOUG DC9 DC982 3022082 WP RT MLG DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND RT MLG DOOR EXTERNAL SKIN DENTED IN TWO PLACES 7 INCHES APART I/B OF DOOR SKID. A REPAIR PATCH WAS INS TALLED IAW SRM 52-01, FIGURE 2 AND 51-30-3. 2 L 7 2 4F A6WE 2001061300119 20010613 00119 WP 2001 6 13 CALA0100504 1 20010525 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND RT INTERNAL FUSELAGE SKIN GOUGED AT FS 1429. THE AREA WAS BLENDED AND A REPAIR DOUBLER WAS INSTALLED I AW SRM 53-01, 51-10-3, 51-10-4, AND 51-30-2. 2 L 7 2 4F A6WE 2001061300120 20010613 00120 WP 2001 6 13 CALA0100505 1 20010525 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND MAIN CABIN FLOOR SUPPORT CORRODED AT FS 160-200, RBL 56. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPO RT WAS INSTALLED IAW SRM 51-10-4, 51-30-3, 51-30-4, AND 51-30-2. 2 L 7 2 4F A6WE 2001061300121 20010613 00121 WP 2001 6 13 CALA0100506 1 20010525 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND LT EXTERNAL FUSELAGE SKIN DENTED AT FS 195, LONGERON 23L. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGUR E 38. 2 L 7 2 4F A6WE 2001061300122 20010613 00122 NM 2001 6 13 CALA0100507 1 20010525 A 2560 ACREM1A MEGAPHONE BOEING 737 737524 1384721 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 33608 27321 THE FORWARD MEGAPHONE WAS FOUND INOPERATIVE. THE MEGAPHONE WAS REPLACED IAW MM 25-00-00. 2 L 7 2 4F RT A16WE 2001061300123 20010613 00123 WP 2001 6 13 CALA0100508 1 20010526 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND SUPPORT CORRODED AT AFT LT SIDE OF WEB AT CUSP AREA, STA 1309. THE SUPPORT WAS REMOVED AND A NEW SUPPO RT WAS INSTALLED IAW SRM 51-30-2 AND 51-10-4. 2 L 7 2 4F A6WE 2001061300124 20010613 00124 WP 2001 6 13 CALA0100509 1 20010526 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND FLOOR SUPPORT CORRODED ON UPPER AND LOWER SURFACE IN MID CARGO AREA AT FS 636, LONGERON 28R-29R. THE F LOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-1. 2 L 7 2 4F A6WE 2001061300125 20010613 00125 WP 2001 6 13 CALA0100510 1 20010526 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND MAIN CABIN CUSP WEB CORRODED AT FS 160 - 200, RBL 56. THE CORRODED AREA WAS CUT OUT IAW SRM 53-01, FIG URE 3. A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-14-1, FIGURE 11, 51-30-02, 51-10-3, AND 53-01, FIGURE 3. 2 L 7 2 4F A6WE 2001061300126 20010613 00126 WP 2001 6 13 CALA0100511 1 20010526 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND MAIN CABIN CUSP WEB CRACKED IN SEVERAL PLACES AT FS 1280, RBL 54. THE CRACKS WERE APPROXIMATELY 1 INCH LONG. FLOOR PANELS WERE REMOVED TO GAIN ACCESS. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-05, FIGURE 96, 51-10-3, AND 51-30-2. THE FLOOR PANELS WERE REINSTALLED IAW ECRA 5100-01844. 2 L 7 2 4F A6WE 2001061300127 20010613 00127 WP 2001 6 13 CALA0100512 1 20010526 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND CUSP WEB CORRODED AT FS 200 - 207, RBL 56. THE CUSP WEB WAS REMOVED AND A REPAIR DOUBLER AND FILLER WE RE INSTALLED IAW SRM 53-01, FIGURE 1, 51-30-02, 51-30-08, AND 51-10-3. 2 L 7 2 4F A6WE 2001061300128 20010613 00128 NE 2001 6 13 20010529CW015 2 20010413 A 7420 165376 HARNESS BEECH 18 E18S 1151006 CE PWA R985 R985AN14B 52008 NE RT ENGINE CONTAMINATED E GGPA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 NM 01 48K 1242 1242 BA202 RT ENGINE STARTED RUNNING ROUGH. PILOT COULD NOT GET AIRCRAFT TO CLIMB. TURNED BACK TO LAND. RT ENGINE STARTED TO LOO SE POWER SO THE RT PROPELLER WAS FEATHERED. FOUND ON INSPECTION OF RIGHT ENGINE, WATER IN IGN HARNESS. 1 L 7 2 3R 3 R A765 5E1 2001061300129 20010613 00129 SW 2001 6 13 20010530CW002 1 20010322 A 2497 WIRE SWRNGN SA227 SA227BC 3377519 SW COCKPIT BROKEN E K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 05 768ML BC768B PILOT SMELLED SOMETHING THAT MIGHT HAVE BEEN SMOKE OR A CARBON SMELL. FOUND THE LEFT ESSENTIAL BUSS PANEL BROKEN AND A BROKEN WIRE. 2 L 7 2 4T RT A8SW 2001061300131 20010613 00131 SW 2001 6 13 20010530CW004 1 20010208 A 3213 NUT SWRNGN SA227 SA227AC 8780603 SW LT MLG MISSING E MEJR K NONE O OTHER IN INSP/MAINT 1 NM 05 378PH 2230 AC575 AFTER NORMAL LANDING PILOT NOTICED LEFT INBOARD MAIN WHEEL WAS MISSING. THE AXLE NUT WITH COTTER KEY AND BOTH INNER BEA RING RACES WERE STILL IN TACT. MAINTENANCE IS INSPECTING THE AIRCRAFT FOR HIDDEN DAMAGE. 2 L 7 2 4T RT A8SW 2001061300132 20010613 00132 EU 2001 6 13 KBMA88745 1 20010505 A 2121 95092 MOTOR SNIAS 350 AS350BA 8680817 EU CABIN INOPERATIVE E KBMA K NONE L NO TEST NR NOT REPORTED 1 WP 19 1188P 2347 FAN MOTOR FOUND INOPERATIVE. REMOVED AND REPLACED WITH NEW UNIT AS REQUIRED. 1 G 7 1 3U NC H9EU 2001061300133 20010613 00133 EU 2001 6 13 KBMA88746 1 20010508 A 2150 451400003 BELT SNIAS 350 AS350BA 8680817 EU A/C SYSTEM DELAMINATED E KBMA K NONE O OTHER NR NOT REPORTED 1 WP 19 270SH 7490 1864 AIR CONDITIONER BLOWING WARM AIR. INOPERATIVE. FOUND DELAMINATED BELT. REPLACED BELT WITH NEW AS REQUIRED. 1 G 7 1 3U NC H9EU 2001061300134 20010613 00134 EU 2001 6 13 KBMA88747 1 20010509 A 2150 0660018 BELT SNIAS 350 AS350BA 8680817 EU A/CM SYSTEM DELAMINATED E KBMA K NONE O OTHER NR NOT REPORTED 1 WP 19 1188P 9660 2347 AIR CONDITIONER NOT BLOWING COLD. FOUND DELAMINATED BELT. REMOVED AND REPLACED A/C BELT WITH NEW AS REQUIRED. 1 G 7 1 3U NC H9EU 2001061300135 20010613 00135 2001 6 13 KBMA88748 4 20010510 A 3422 5050031904 GYRO SNIAS 350 AS350BA 8680817 EU COCKPIT PRECESSES E KBMA K NONE O OTHER NR NOT REPORTED 1 WP 19 230SH 55 2337 DIRECTIONAL GYRO INOPERATIVE, PRECESSES. BENCH CHECK REQUIRED. REMOVED AND REPLACED WITH SERVICEABLE UNIT AS REQUIRED. 1 G 7 1 3U NC H9EU 2001061300136 20010613 00136 EU 2001 6 13 KBMA88749 1 20010510 A 2420 524031 LEAD SNIAS 350 AS350B2 8680813 EU STARTER GEN BROKEN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 115SH 3141 FOUND BROKEN LEAD. REPLACED TERMINAL AS REQUIRED. 1 G 7 1 3U H9EU 2001061300137 20010613 00137 NM 2001 6 13 2001UALA00786 1 20010519 A 2530 OVEN BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE GALLEY MALFUNCTIONED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 606UA 21867 OVEN SMOKING. 2 L 7 2 4F 4 F RT A1NM E3NE 2001061300138 20010613 00138 NM 2001 6 13 2001UALA00812 1 20010522 A 2530 SMOKE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE OVEN MALFUNCTIONED A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 614UA 21875 OVEN SMOKING. 2 L 7 2 4F 4 F RT A1NM E3NE 2001061400001 20010614 00001 EU 2001 6 14 CA010511024 1 20010424 A 2721 PIN BRAERO 748 HS7482B 1500248 EU RROYCE DART DART5342 EU RUDDER WHEEL DISLODGED W A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CA (CAN) WHEN CLIMBING THROUGH 12,000 FEET, PILOT REALIZED THERE WAS NO RUDDER TRIM INPUT WHEN WHEEL WAS TURNED. AIRCRAFT R ETURNED TO BASE AND LANDED OVERWEIGHT. TAPER PIN THAT HOLD RUDDER WHEEL WAS FOUND DISLODGED. PIN WAS RE INSTALLED AN SEC URED. OVERWEIGHT LANDING INSPECTION WAS CARRIED OUT AND AIRCRAFT RETURNED TO SERVICE. NOTE: NO PREVIOUS WORK WAS CARRIED OUT ON THIS SYSTEM. 2 L 7 2 3T 4 T A24EU A196 2001070200065 20010702 00065 NM 2001 7 2 01FDEA00399 1 20010607 A 3610 SHUTOFF VALVE BOEING 727 72722 1384002 NM BLEED AIR SYS FAILED A FDEA K NONE J WARNING INDICATION CL CLIMB 1 SO 25 191FE 19084 DURING CLIMB LWR AFT BODY OVERHEAT LIGHT ILLUM. NR 3 BLEED ON, RT PACK ON TURN RT PACK OFF, LIGHT EXTINGUISHED. Remove d and replaced RT PURGE LINE SHUTOFF VALVE PER MM 36-13-011-4. LEAK CK OK. 2 L 7 3 4F A3WE 2001061400005 20010614 00005 EU 2001 6 14 CA010511028 1 20010409 A 2530 HEATER AIRBUS 310 A310304 EU GE CF6 CF680C2B2 30025 NE GALLEY WATER FAILED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) DURING FLIGHT, SMOKE WAS OBSERVED COMING FROM FORWARD GALLEY NR 2 BOILER. ALL CB PULLED & GALLEY POWER SHEDDED. N O MORE SMOKE OBSERVED & FLIGHT CONTINUED WITHOUT INCIDENT. NR 2 WATER BOILER CHANGED IAW MM 25-30 & CHECKED SERVICEABLE. NO FURTHER INCIDENT DURING SUBSEQUENT FLIGHT. 2 L 7 2 4F 4 F RT A35EU E13NE 2001061400006 20010614 00006 NM 2001 6 14 CA010511029 1 20010330 A 7931 REGULATOR VALVE BOEING 737 737201 1384454 NM PWA JT8 JT8D9A 52048 NE OIL PRESSURE FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA (CAN) ON CLIMB, NR 1 ENGINE OIL PRESSURE INDICATED 66 PSI. NR 1 ENGINE SHUT DOWN AS A PRECAUTION. AIRCRAFT RETURNED WITH OUT INCIDENT. O-RING FOUND DAMAGED IN VALVE HOUSING. O-RING REPLACED, VALVE RE INSTALLED AND ADJUSTED IAW MM. 72-00. NO FURTHER INCIDENT DURING SUBSEQUENT FLIGHT. 2 L 7 2 4F 4 F A16WE E2EA 2001061400008 20010614 00008 NM 2001 6 14 CA010515002 1 20010331 A 5210 FORK DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE AIRSTAIR DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 37577 (CAN) CHASSIS FORKED ENDS (WHERE AIRSTAIR DOOR GAS SPRING STRUTS ATTACH) WERE FOUND CRACKED AT BASE OF THE FORKS. THE CH ASSIS WAS REPLACED WITH A NEW UNIT. THIS WAS FOUND DURING AN INSPECTION (FCD - FLEET CAMPAIGN DIRECTIVE) OF OUR DASH-8 F LEET. THE FCD WAS RAISED WHEN THE FIRST CHASSIS WAS FOUND CRACKED ON MARCH 16 (ON ANOTHER AIRCRAFT C-FABT), WHILE COMPLE TING INSTALLATION OF NEW BANSBACH GAS SPRING STRUTS (AS PART OF AD CF-2000-19). 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001061400009 20010614 00009 NM 2001 6 14 CA010515003 1 20010329 A 5210 FORK DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE AIRSTAIR DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 32413 (CAN) CHASSIS FORKED ENDS (WHERE AIRSTAIR DOOR GAS SPRING STRUTS ATTACH) WERE FOUND CRACKED AT BASE OF THE FORKS. THE CH ASSIS WAS REPLACED WITH A NEW UNIT. THIS WAS FOUND DURING AN INSPECTION (FCD - FLEET CAMPAIGN DIRECTIVE) OF OUR DASH-8 F LEET. THE FCD WAS RAISED WHEN THE FIRST CHASSIS WAS FOUND CRACKED ON MARCH 16 (ON ANOTHER AIRCRAFT C-FABT), WHILE COMPLE TING INSTALLATION OF NEW BANSBACH GAS SPRING STRUTS (AS PART OF AD CF-2000-19). 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001061400026 20010614 00026 EA 2001 6 14 HNAA0100036 1 20010612 A 3230 574205 SELECTOR VALVE DHAV DHC8 DHC8311 1386006 EA INOPERATIVE A HNAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 07 343EN 16001 340 AFTER TAKE-OFF THE LANDING GEAR WOULD NOT RETRACT. 2 H 7 2 4T RT A13NM 2001061400028 20010614 00028 NM 2001 6 14 CA010522003 1 20010522 A 2421 GENERATOR BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE APU FAILED W A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 CA (CAN) 20 MINUTES AFTER DEPARTURE, APU GENERATOR DROPPED OFF LINE. RETURNED DUE #2 CSD WAS ON MEL. REPLACED #2 GENERATOR AND CSD AS PER WORK CARDS 1177-2 AND 1182-2. GROUND RUNUP COMPLETED, APU AND NR 2 GENERATOR CHECKED SERVICEABLE. 2 L 7 2 4F 4 F A16WE E2EA 2001061400029 20010614 00029 NM 2001 6 14 CA010522005 1 20010506 A 3010 DUCT BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE ANTI-ICE VALVE SEPARATED W A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 CA (CAN) ON CLIMB NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. THRUST REDUCED AND LIGHT EXTINGUISHED. RETURNED. MAINTENANCE INSP ECTION FOUND RIGHT ANTI-ICE DUCT SEPARATED FROM ANTI-ICE VALVE. DUCT REPLACED GROUND RUN, SYSTEM CHECKED SERVICEABLE. 2 L 7 2 4F 4 F A16WE E2EA 2001061400031 20010614 00031 NM 2001 6 14 CA010522007 1 20010501 A 2420 CSD BOEING 737 7372T5 NM PWA JT8 JT8D17 52049 NE NR 1 UNRELIABLE W A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 CA 46504 37061 2197 (CAN) AT FL 230, NR 1 CONSTANT SPEED DRIVE LOW OIL PRESSURE LIGHT ILLUMINATED. FLIGHT ELECTED TO RETURN DUE APU ELECTRIC S WERE UNRELIABLE. REPLACED NR 1 CSD AS PER WORK CARD 1182-1. APU AND NR 1 CSD CHECKED SERVICEABLE DURING GROUND RUN. 2 L 7 2 4F 4 F RT A16WE E2EA 2001061400032 20010614 00032 NM 2001 6 14 CA010522009 1 20010413 A 5411 FITTING BOEING 767375 BOEING 767 767375 NM GE CF6 CF680C2B6 30025 NE LT PYLON CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 57886 24084 (CAN) DURING INSPECTION NR 2 PYLON INBOARD MIDSPAR FITTING WAS FOUND CRACKED AT UPPER AFT INBOARD FASTENER HOLE. NR 2 P YLON MIDSPAR FITTING REPLACED AS PER EVA 01-767-54-4058. 2 L 7 2 4F 4 F RT A1NM E13NE 2001061400037 20010614 00037 SW 2001 6 14 CA010522018 1 20010507 A 3243 CLEVIS BOLT CLEVELAND 105 BBAVIA 7 7ECA 21101NN SW LYC O235 O235C1 41505 EA MASTER CYLINDER BENT W K NONE O OTHER IN INSP/MAINT 1 CA 13 13 (CAN) BRAKES WERE NOT AS RESPONSIVE AS USUAL. UPON INSPECTION RT MASTER BRAKE CYLINDER CLEVIS BOLT FOUND TO BE BENT. 1 H 7 1 3O 3 O A759 E223 2001061400039 20010614 00039 CE 2001 6 14 CA010522022 1 20010412 A 2160 VALVE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA PRE COOLER LEAKING W O OTHER J WARNING INDICATION DE DESCENT 1 CA (CAN) P3 AIR LEAKING THROUGH PRE COOLER VALVE (BYPASS) CAUSED INABILITY TO PRESSURE CABIN ON LT SIDE. 2 L 7 2 4T 4 T RT A24CE E4EA 2001061400041 20010614 00041 CE 2001 6 14 CA010523003 1 20010508 A 3320 LIGHT BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA COCKPIT SHORTED W O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 CA (CAN) SHORTLY AFTER GEAR DOWN SELECTED ON FINAL, PUFF OF SMOKE NOTICED BY PASSENGER IN AREA OF LT NR 1 & 2 WINDOWS. LDG CARRIED OUT NORMLLY AS NO FURTHER SMOKE. AS PRECAUTION A/C STOPPED & SHUTDOWN AT THE 1ST AVAILABLE RWY TURNOFF & PASSENG ER UNLOADED. FAULT COULD NOT BE DUPLICATED DURING SUBSEQUENT GROUND TESTING SO AREPL A/C SENT FOR PASSENGERS FOR RETURN FLT, ALONG WITH AME TO INVESTIGAGE PROBLEM. THE AME FOUND THAT THEREADING LIGHT MOUNTED IN LT NR 1 WINDOW SERVICE PANEL INCORRECTLY WIRED, HAVING GROUND WIRE (#3A18) ATTACHED TO INSULATED POSITIVE POST OF LIGHT & 24 VDC WIRE (#L31A18) ATTAC HED TO NEGATIVE POST, WHICH IS NOT ISOLATED FROM LIGHT ASSY CASE. THERE 1 L 7 2 4T 4 T A24CE E4EA 2001061400044 20010614 00044 WP 2001 6 14 MWEA010946 1 20010613 A 2430 2634006106 CHARGER DOUG DC9 DC914 3022034 WP E&E COMPARTMENT DEFECTIVE A MWEA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 GL 31 500ME 45711 ON CLIMB OUT THROUGH FL 200 BATTERY CHARGER C.B. POPPED. -- REMOVED AND REPLACED BATTERY CHARGER. REMOVED AND REPLACED LEFT AND RIGHT SHIP BATTERIES. 2 L 7 2 4F A6WE 2001061400045 20010614 00045 WP 2001 6 14 AALA20011114 1 20010518 A 5300 SEAT TRACK DOUG DC9 DC982 3022082 WP FS 200-245 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3515 49892 TUL - FOUND SEAT TRACK NR 5 CORRODED STATION 200-245. INSTALLED SEAT TRACK FROM STATION 200-245 NR 5. (M) 2 L 7 2 4F A6WE 2001061400046 20010614 00046 WP 2001 6 14 AALA20011115 1 20010518 A 5300 WEB DOUG DC9 DC982 3022082 WP FS 200-210 A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3515 49892 TUL - FOUND ACCESS HOLE REQUIRED TO FOM AT STATION 200-210 BETWEEN SEAT TRACK 5/6 RT. INSTALLED DOUBLER OVER ACCESS HOL E AT STATION 200-210 PER SRM 53-01 FIG 4. (M) 2 L 7 2 4F A6WE 2001061400047 20010614 00047 NM 2001 6 14 AALA20011086 1 20010521 A 2400 766088 GENERATOR BOEING 767 767323 1385205 NM APU INOPERATIVE A AALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 SW 21 7375A 25202 SFO - FLT 1402 - EN ROUTE SFO-DFW, APU AUTO SHUTDOWN RESULTING IN APU GENERATOR GOING OFFLINE. AIR INTERRUPTED AND DECL ARED EMERGENCY. LANDED WITHOUT INCIDENT. REPLACED RIGHT IDG, WHICH HAD BEEN PREVIOUSLY MEL'D. ALSO REPLACED APU ELECT RONIC CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001061400048 20010614 00048 NM 2001 6 14 AALA20011020 1 20010510 A 2400 GEN5103 GENERATOR BOEING 767 767323 1385205 NM RT ENG GEARBOX FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 351AA 24032 JFK - FLT 24 - EN ROUTE FL330 LIGHT TO MODERATE TURBULENCE, RIGHT ENGINE DRIVEN GENERATOR FAILED. GENERATOR WOULD NOT R ESET, FIELD OFF LIGHT ILLUMINATED CHECK STATUS MESSAGES. APU REQUIRED 2 ATTEMPTS TO START. REPLACED PER B767MM RIGHT E NGINE GENERATOR. OPS CHECK LEAK CHECK OK FOR SERVICE. BITE CHECK EB, NO FAULTS NOTED. APU STARTED FIRST ATTEMPTS.(M) 2 L 7 2 4F RT A1NM 2001061400049 20010614 00049 NM 2001 6 14 AALA20010522 1 20010517 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM CABIN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 648AA 24606 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS ROWS 15 THROUGH 23 DIM. REPLACED BATTERY PACK FOR EMERGENCY EXIT ESCAPE PATH LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001061400050 20010614 00050 NM 2001 6 14 AALA20011088 1 20010519 A 3397 WIRE BOEING 767 767223 1385123 NM CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 21 307AA 22313 LAX - DURING OVERNIGHT MAINTENANCE, LEFT MID GALLEY EMERGENCY LIGHT INOPERATIVE. REPAIRED BROKEN WIRE TO EMERGENCY LIGH T. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001061400051 20010614 00051 NM 2001 6 14 AALA20011093 1 20010518 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 621AM 24579 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS ROW 27DEF INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001061400052 20010614 00052 WP 2001 6 14 AAL20011035 1 20010515 A 3600 5953625511 DUCT DOUG DC9 DC983 3022083 WP AFT ACCESSORY A AALA A UNSCHED LANDING J O WARNING INDICATION OTHER CL CLIMB 1 SW 21 572AA 49458 ORD - FLT 1666 - EN ROUTE ORD-ALB, TAIL COMPARTMENT HIGH TEMP LIGHT ILLUMINATED DURING CLIMB-OUT AT 24,000 FEET. RETURN ED AND LANDED ORD WITHOUT INCIDENT. REPLACED UPPER RETURN SYSTEM AIR CONDITIONING DUCT. SYSTEM GROUND CHECKED NORMAL O PERATION. (M) 2 L 7 2 4F RT A6WE 2001061400053 20010614 00053 WP 2001 6 14 AALA20011039 1 20010507 A 5300 SEAT TRACK DOUG DC9 DC982 3022082 WP FS 1289 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3515 49892 TUL - FOUND CORROSION ON NR 3 SEAT TRACK AT STATION 1289 AROUND SCREW HOLE. CUT OUT DAMAGED AREA AND INSTALLED REPAIR P ER SRM 53-05 FIG 4A. (M) 2 L 7 2 4F A6WE 2001061400054 20010614 00054 WP 2001 6 14 AALA20011040 1 20010504 A 5300 SEAT TRACK DOUG DC9 DC982 3022082 WP FS 880 CUT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3515 49892 TUL - FOUND DEEP CUT IN NR 3 SEAT TRACK TIE DOWN LUG INBOARD SIDE STATION 880. CUT OUT DAMAGE, INSTALLED SEAT TRACK PLU G PER SRM 53-05-4A. (M) 2 L 7 2 4F A6WE 2001061400055 20010614 00055 WP 2001 6 14 AALA20011041 1 20010504 A 5300 SEAT TRACK DOUG DC9 DC982 3022082 WP FS 898 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3515 49892 TUL - FOUND DEEP GOUGES IN NR 3 SEAT TRACK STATION 898. CUT OUT DAMAGE, INSTALLED SEAT TRACK PLUG PER SRM 53-04-4A. (M ) 2 L 7 2 4F A6WE 2001061400056 20010614 00056 WP 2001 6 14 AALA20011042 1 20010503 A 5300 SEAT TRACK DOUG DC9 DC982 3022082 WP FS 1284 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3515 49892 TUL - FOUND CORROSION ON NR 3 SEAT TRACK STATION 1284. CUT OUT CORROSION AND INSTALLED PLUG REPAIR PER SRM 53-05 FIG 4A . (M) 2 L 7 2 4F A6WE 2001061400057 20010614 00057 EU 2001 6 14 C2XA01CL140 1 20010614 A 3350 3011180A POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU CABIN DEFECTIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 34820 159 DURING ROUTINE MAINTENACE THE EMERGENCY AISLE LIGHT WAS FOUND TO BE INOPERATIVE AT 2A AND 5A.MAINTENANCE REPLACED THE FO RWARD EMERGENCY LIGHT POWER SUPPLY.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A53EU 2001061400058 20010614 00058 WP 2001 6 14 MWEA010948 1 20010614 A 5313 591142275 LONGERON DOUG DC9 DC981 3022081 WP STA 1297-1332 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 LONGERON 5 LEFT AT STATION 1287-1332 HAS PREVIOUS MOUNT HOLES IN THE UPPER HAT. -- REMOVED LONGERON, DRILLED NEW LONGE RON SECTION, FABRICATED SECTION SPLICE AND DRILLED, INSTALLED LONGERON. 2 L 7 2 4F A6WE 2001061400059 20010614 00059 WP 2001 6 14 MWEA010949 1 20010614 A 5330 59364341 SKIN DOUG DC9 DC981 3022081 WP STATION 270 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 (E.O. 2-34-041) REMOVED DME ANTENNA DOUBLER ON FUSELAGE SKIN AT STATION 270. -- FABRICATED DOUBLERS AND FINGER DOUBLER S, INSTALLED REPAIR PARTS. 2 L 7 2 4F A6WE 2001061400060 20010614 00060 WP 2001 6 14 MWEA010950 1 20010614 A 5313 995823859 LONGERON DOUG DC9 DC981 3022081 WP STATION 1322 PUNCTURED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 FRAME AT STATION 1322 BETWEEN LONGERONS 24 LEFT AND 25 LEFT HAS SEVERAL DEEP PUNCTURES. -- REMOVED DAMAGE, FABRICATED, LOCATED, DRILLED AND INSTALLED SPLICES AND FILLER. 2 L 7 2 4F A6WE 2001061500001 20010615 00001 2001 6 15 DHL2001701010 4 20010519 A 2210 HEAD BOEING 727 72730C 1384009 NM AUTOPILOT SYS MALFUNCTIONED A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 701DH 19011 AUTOPILOT MAKES GRADUAL UNCOMMAND RIGHT TURNS IN MANUAL MODE. DEFERRED IAW DHL MEL 22-1 CAT B MAINTENANCE PROCEDURES CO MPLIED WITH. PLACARD INSTALLED, DMI 5661. REMOVED AND REPLACED AUTOPILOT CONTROL HEAD CKS GOOD PER 22-00. THIS CLEARS DMI 5661. PLACARD REMOVED. 2 L 7 3 4F A3WE 2001061500002 20010615 00002 NM 2001 6 15 01FDEA00386 1 20010526 A 2613 MODULE BOEING 727 727227 1384078 NM OVERHEAT DETECT MALFUNCTIONED A FDEA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CL CLIMB 1 SO 25 482FE 21464 LWR AFT BODY O/H LIGHT ON AT TOP OF CLIMB WITH ENG ANTI-ICE ON. LIGHT EXTING AFT CLOSING ANTI-ICE AND PWR REDUCTION AT LEVEL OFF. *S/D* REMOVED AND REPLACED SERVICEABLE MODULE ASSY, CONTROLLER PER MM 26-14-000-1. 2 L 7 3 4F A3WE 2001061500003 20010615 00003 NM 2001 6 15 01FDEA00388 1 20010525 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 276FE 22041 (C53-111-01) CORROSION ON FASTENER HOLES IN THE FLOORBEAM LWR CHORD BS 1130, RBL 44.5 TO LBL 44.5, WL 200. *S/D* REMOV ED AND REPLACED DAMAGED FLOORBEAM PER IAW FEDEX EA 7-5310-57249. 2 L 7 3 4F RT A3WE 2001061500004 20010615 00004 WP 2001 6 15 DHL2001805010 1 20010518 A 2742 ACTUATOR DOUG DC8 DC873F 302199F WP HORIZ STAB FAILED A DHLA K NONE O OTHER CR CRUISE 1 SO 01 805DH 46125 CONTROL WHEELS TRIM SWITCHES INOP. REMOVED AND REPLACED LT ROTARY ACT PER DC-8 MM 27-41-10. 2 L 7 4 4F RT 4A25 2001061500005 20010615 00005 2001 6 15 DHL2001365017 4 20010526 A 2230 AUTOTHRUST SYS AIRBUS 300 A300B4203 3930306 EU COCKPIT MALFUNCTIONED A DHLA K NONE O OTHER CR CRUISE 1 SO 01 365DH 149 AUTO THROTTLE WOULD NOT REMAIN ENGAGED IN SLIGHT TO MODERATE TURBULENCE. COULD NOT DUPLICATE ON GROUND; OPS CHECK GOOD IAW MM 22-71-00. 2 L 7 2 4F RT A35EU 2001061500006 20010615 00006 2001 6 15 DHL2001727019 4 20010526 A 2210 AUTOPILOT SYS BOEING 727 727228 NM COCKPIT MALFUNCTIONED A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 727DH 20204 AUTOPILOT OVERBANKS. COULD NOT DUPLICATE ON GROUND. AUTOPILOT OPS CKS GOOD IAW B727 MM 22-11-01. 2 L 7 3 4F A3WE 2001061500007 20010615 00007 NM 2001 6 15 DHL2001741010 1 20010526 A 2742 ACTUATOR BOEING 727 7272Q9 138448M NM HORIZ STAB INTERMITTENT A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 741DH 21931 MAIN ELECTRIC TRIM WILL NOT TRIM NOSE UP FOR CAPT OF P/N CRUISE TRIM WORKS NORMAL. PROBLEM IS INTERMITTENT. REMOVED AN D REPLACED MAIN ELECTRIC TRIM STAB ACTUATOR. OPS CHK'D GOOD ALL WORK DONE IAW MM 27-40-31. 2 L 7 3 4F RT A3WE 2001061500008 20010615 00008 NM 2001 6 15 DHL2001703003 1 20010526 A 3260 SWITCH BOEING 727 72730C 1384009 NM NLG FAULTY A DHLA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 703DH 19010 UPON FIRST GEAR EXTENSION INTO CVG NOSE GEAR GREEN LIGHT WAS INTERMITTENT. RECYCLED LANDING GEAR AND ALL INDICATIONS NO RMAL. REMOVED AND REPLACED NOSE POSITION SWITCH IAW B727 MM 32-61-21, OPS CHECK OK. 2 L 7 3 4F A3WE 2001061500009 20010615 00009 2001 6 15 DHL2001715005 4 20010526 A 3431 RECEIVER BOEING 727 727155C 138404Z NM COCKPIT UNSERVICEABLE A DHLA K NONE O OTHER CR CRUISE 1 SO 01 715DH 19618 AUTOPILOT WILL NOT TRACK VOR IN NAV/LOC MODE. REPLACED NR 1 NAV RCVR PER MM 34-31-21, OPS CKS GOOD. THIS CLEARS DMI 57 72. 2 L 7 3 4F A3WE 2001061500010 20010615 00010 2001 6 15 DHL2001715006 4 20010526 A 2211 COMPUTER BOEING 727 727155C 138404Z NM AUTOPILOT SYS MALFUNCTIONED A DHLA K NONE F FLT CONT AFFECTED CL CLIMB 1 SO 01 715DH 19618 ON CLIMBOUT IN A-MODE AUTOPILOT PORPOISED. REPLACED PITCH CHANNEL PER MM 22-11-101. OPS CKS GOOD. THIS CLEARS DMI 577 1. 2 L 7 3 4F A3WE 2001061500011 20010615 00011 2001 6 15 DHL2001742007 4 20010526 A 2210 AUTOPILOT SYS BOEING 727 727225 1384077 NM COCKPIT MALFUNCTIONED A DHLA K NONE O OTHER CR CRUISE 1 SO 01 742DH 21290 AUTOPILOT INTERMITTENTLY WOULD NOT ENGAGE IN A AND B MODE. RAN SYSTEM NUMEROUS TIMES. SYSTEM OPS CHECKED NORMAL. 2 L 7 3 4F A3WE 2001061500012 20010615 00012 NE 2001 6 15 DHL2001708004 2 20010518 A 7200 ENGINE BOEING 727 72725 1384006 NM PWA JT8 JT8D7B 52053 NE NR 1 UNSERVICEABLE A DHLA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 708DH 18275 655459 REMOVED AND REPLACED ENG FOR EXCESSIVE OIL CONSUMPTION. REF W/O 600003170. REMOVED NR 1 ENG AND REPLACED PER DHL 727 T ASK MANUAL MANUAL 71-01-03 THRU 71-01-18. 2 L 7 3 4F 4 F A3WE E2EA 2001061500013 20010615 00013 NM 2001 6 15 UPS01236010 1 20010526 A 5312 PRESSURE PANEL BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:N/A, RT WHEEL WELL CRACKS. *S/D* REPAIRED PER SRM 51-1-9A. 2 L 7 3 4F A3WE 2001061500014 20010615 00014 WP 2001 6 15 ARWA0010503 1 20010525 A 2910 O-RING DOUG DC8 DC862 3021970 WP HYD SYSTEM FAILED A ARWA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 19 8969U 46070 ON APPROACH TO TNCC (CURAZAO) LOSS OF HYDRAULIC FLUID. PERFORMED EMERGENCY CHECKLIST AS PER ARROW AIR PROCEDURE. AIRCR AFT LANDED WITHOUT INCIDENT. REPLACED O-RING FROM NR 3 ENGINE DRIVEN HYDRAULIC PUMP PRESSURE LINE ELBOW IAW MM 29-10-12 , LEAK CKD OK, OPERATIONAL CKD DURING RUN UP IAW MM 71-00. 2 L 7 4 4F 4A25 2001061500015 20010615 00015 2001 6 15 AWXA0001773 4 20010529 A 2230 AUTOTHRUST SYS AIRBUS 320 A320232 3930326 EU COCKPIT MALFUNCTIONED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 655AW 1075 PHX - ABORTED TAKEOFF - FLT 253 - 5/27/01 - REJECTED TAKEOFF AT APPROX 20-25 KTS; EPRS MATCHED AT 1.05 AND THROTTLES SMO OTHLY MOVED UP TO FLEX STAYING SLIGHTLY AHEAD OF ACTUAL EPR; PASSING CLIMB DETENT A/C YAWED TO LEFT AND GOT A MASTER CAU TION. NO POSTFLIGHT INDICATION OF FAULT; BITE CHECKED EFCS 1&1 - SFCC 1&2 - BMC 1&2 - LGCIU 1&2 - BSCU 1&2 - NO FAULT F OUND ON ANY SYSTEM; TEST TAXI A/C AT SPEEDS UP TO 32 KTS. MAINTAINED TAXI LINE WITH MINOR CORRECTIONS AS KLPER AMM 32-5 1-00-810-823; OK FOR SERVICE AT THIS TIME. 2 L 7 2 4F RT A28NM 2001061500016 20010615 00016 NM 2001 6 15 AWXA0001776 1 20010529 A 2424 GCU BOEING 737 7372U9 1384498 NM APU FAILED A AWXA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 WP 28 149AW 22575 DURING BOARDING SEVERAL CIRCUIT BREAKERS POPPED AND MULTIPLE AMBER LIGHTS ON OVERHEAD ILLUMINATED; SMOKE FILLED THE COCK PIT; ORDERED A/C EVACUATED; POWERED A/C DOWN. REPLACED APU GENERAL CONTROL UNIT DUE TO FAILURE IAW MM 24-21-81; CHANGED APU GENERAL BREAKER PRECAUTIONARY, FOR SIGN IF HIGH TEMP IAW AWA CARD A8M24001. 2 L 7 2 4F RT A16WE 2001061500017 20010615 00017 2001 6 15 SWIA972593 4 20010522 A 2360 STRAP EMB 120 EMB120RT SO PWA 118 PW118 NE NLG BROKEN A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 161CA 120143 AFTER TAKEOFF AND GEAR SELECTED UP, HAD A HIGH FREQUENCY THUMPING NOISE. RETURNED TO SFO. WHEN SELECTED GEAR DOWN NOIS E WENT AWAY. FOUND NOSE LANDING GEAR STRUT BONDING STRAP BROKEN. INSTALLED NEW TERMINAL END ON NLG BONDING STRAP AND R E-SECURED. 2 L 7 2 4T 4 T RT A31SO E20NE 2001061500018 20010615 00018 SO 2001 6 15 SWIA972594 1 20010524 A 3260 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT MLG FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 215SW 120281 RIGHT MAIN GEAR POSITION INDICATOR DISAGREED WITH GEAR HANDLE POSITION (A&B RED LIGHTS ON) UP. TRIED RECYCLE 2 TIMES PE R QRH WITH NO SUCCESS. ADJUSTED RIGHT INBOARD SEQUENCE VALVE IAW 32-32-04. REMOVE AND REPLACE RIGHT B-UPLOCK PROXIMITY SENSOR IAW 32-61-01. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001061500019 20010615 00019 EA 2001 6 15 SWIA972595 1 20010528 A 2710 PCU CNDAIR CL600 CL6002B19 EA LT AILERON OUT OF ADJ A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 412SW 7101 AIRCRAFT DOES NOT FLY LEVEL. THE RIGHT WING IS LOWER THAN LEFT. REQUIRES LEFT AILERON ALL THE TIME. DOES NOT SET LEVE L ON THE GROUND. ALMOST 1/2 BALL OUT ON THE GROUND. ADJUSTED LEFT AILERON PCUS UP PER RIGGING PROCEDURE IN MM 27-11-00 AND SERVICED RIGHT STRUT PER 12-12-32. 2 L 7 2 4F RT A21EA 2001061500020 20010615 00020 WP 2001 6 15 AALA20011043 1 20010507 A 5300 SEAT TRACK DOUG DC9 DC982 3022082 WP FS 1176-1279 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3515 49892 TUL - FOUND CORROSION ON NR 1 SEAT TRACK, 1 INCH BY 103 INCHES. REMOVED AND REPLACED SEAT TRACK NR 1. (M) 2 L 7 2 4F A6WE 2001061500021 20010615 00021 WP 2001 6 15 AALA20011044 1 20010510 A 5300 SEAT TRACK DOUG DC9 DC982 3022082 WP FS 1164-1309 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3515 49892 TUL - FOUND CORROSION AND GOUGES ON SEAT TRACK NR 3 STATION 1164-1309. REPLACED SEAT TRACK STATION 1164-1309, SRM 51-01 . (M) 2 L 7 2 4F A6WE 2001061500022 20010615 00022 WP 2001 6 15 AALA20011053 1 20010503 A 5330 SKIN DOUG DC9 DC982 3022082 WP FS 247 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3515 49892 TUL - FOUND DENT 48 INCHES AFT OF FORWARD ENTRY DOOR 3 INCH BELOW RED STRIPE. INSTALLED INTERNAL DOUBLER PER SRM 53-04 FIG 38, DAMAGED AND REMOVED. (M) 2 L 7 2 4F A6WE 2001061500023 20010615 00023 WP 2001 6 15 AALA20011054 1 20010514 A 5330 SKIN DOUG DC9 DC982 3022082 WP FS 229-264 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3515 49892 TUL - FOUND SEVERAL DENTS AND GOUGES IN FUSELAGE SKIN STATION 229 TO 264 LONGERONS 18 TO 20 LEFT. INSTALLED DOUBLER PER ESO 80559 DATED 5-11-2001. (M) 2 L 7 2 4F A6WE 2001061500024 20010615 00024 WP 2001 6 15 AALA20011078 1 20010514 A 5100 ANGLE DOUG DC9 DC982 3022082 WP FS 951 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3515 49892 TUL - FOUND ANGLE AT TOP OF TRAPEZOIDAL PANEL CORRODED AROUND FASTENERS STATION 951-955. REMOVED AND REPLACED ANGLE SRM 51-01. (M) 2 L 7 2 4F A6WE 2001061500025 20010615 00025 WP 2001 6 15 AALA20011080 1 20010507 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3515 49892 TUL - FOUND CORROSION ON TOP OF 1322 FLOORBEAM RIGHT LAV AFT .25 INCH HOLE. BLENDED OUT CORROSION INSTALLED WEAR STRIPS PER SRM 53-05 PART 1 PAG 30A. (M) 2 L 7 2 4F A6WE 2001061500026 20010615 00026 WP 2001 6 15 AALA20011081 1 20010507 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3515 49892 TUL - FOUND CORROSION ON FLOORBEAM TOP STATION 1338 AT SCREW HOLES UNDER RIGHT AFT LAV. BLENDED OUT CORROSION INSTALLED WEAT STRIPS PER SRM 53-05 PART 1 PAGE 30A. (M) 2 L 7 2 4F A6WE 2001061500027 20010615 00027 WP 2001 6 15 AALA20011056 1 20010510 A 5330 SKIN DOUG DC9 DC983 3022083 WP FS 1380 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 TUL - FOUND CRACK IN FUSELAGE SKIN AT FASTENERS HOLE STATION 1380 LEFT SIDE APPROX 12 INCHES ABOVE PYLON. INSTALLED DOU BLER OVER CRACK IAW SRM 53-01 FIG 2. (M) 2 L 7 2 4F RT A6WE 2001061500028 20010615 00028 WP 2001 6 15 AALA20011057 1 20010506 A 5330 SKIN DOUG DC9 DC983 3022083 WP FS 644-648 A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 TUL - FOUND TWO DEEP BLENDOUT ON FUSELAGE SKIN. INSTALLED INTERNAL DOUBLER SRM 53-05 FIG 38 PAGE 218. (M) 2 L 7 2 4F RT A6WE 2001061500029 20010615 00029 WP 2001 6 15 AALA20011058 1 20010504 A 5300 SKIN DOUG DC9 DC983 3022083 WP FS 615 A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 TUL - FOUND THREE DEEP BLEND OUTS ON FUSELAGE SKIN STATION 610 TO STATION 619 BELOW LONGERON 26 LEFT. BLENDOUTS OUT OF LIMIT, INSTALLED INTERNAL DOUBLER PER SRM 53-04 FIG 38. (M) 2 L 7 2 4F RT A6WE 2001061500030 20010615 00030 WP 2001 6 15 AALA20011059 1 20010508 A 5330 SKIN DOUG DC9 DC983 3022083 WP FS 933 A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 TUL - FOUND DEEP BLENDOUT IN SKIN STATION 933 LONGERON 10R. INSTALLED INTERNAL DOUBLER PER SRM 53-04 FIG 38 AND ESO 805 59 DATED 5-8-2001. (M) 2 L 7 2 4F RT A6WE 2001061500031 20010615 00031 WP 2001 6 15 AALA20011064 1 20010508 A 5100 BRACKET DOUG DC9 DC983 3022083 WP FS 1155 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 TUL - FOUND CORROSION ON DOOR CUTOUT FORWARD LOWER CORNER CURVED BRACKET. INSTALLED NEW BRACKET SRM 51-01. (M) 2 L 7 2 4F RT A6WE 2001061500032 20010615 00032 WP 2001 6 15 AALA20011068 1 20010508 A 5100 FITTING DOUG DC9 DC983 3022083 WP FS 1155 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 TUL - FOUND CORROSION ON DOOR CUTOUT FORWARD LOWER CORNER FITTING. INSTALLED NEW CORNER FITTING SRM 51-01. (M) 2 L 7 2 4F RT A6WE 2001061500034 20010615 00034 SO 2001 6 15 SWIA972597 1 20010526 A 5753 FLAP TRACK EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE T/E FLAPS DIRTY A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 209SW 120269 FLAP DISAGREEMENT OUTBOARD PAIR WHEN SELECTING FLAPS UP AFTER TAKEOFF, 2 BARS STILL LIGHTED ON PANEL. WOULD NOT RECYCLE PER QRH. WOULD NOT EXCEED 15 DEGREES UPON LANDING. CLEANED AND LUBRICATED TRACKS AND ROLLERS. OPS CHECK NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 2001061500035 20010615 00035 SO 2001 6 15 SWIA972598 1 20010526 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE T/E FLAP FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 NM 07 195SW 120127 LANDING AT SLC RECEIVED FLAP CONTROL FAULT THAT WOULD NOT RESET AFTER LANDING. RETRACTED FLAPS, INBOARD FLAPS REMAINED AT 25 DEGREES SETTING. REMOVE AND REPLACE RIGHT INBOARD FLAP ACTUATOR. OPS CHECK AND LEAK CHECK GOOD. P/N ON 320300-1 005, S/N ON 0427, S/N OFF 0109. 2 L 7 2 4T 4 T RT A31SO E20NE 2001061500036 20010615 00036 EA 2001 6 15 JBXA000286 1 20010527 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 EA COCKPIT CRACKED A JBXA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 05 571ML 7209 EN ROUTE TO BOS AT FL290 260KIAS DIFF/PRES 8.1 LEFT WINDSHIELD SHATTERED PRESSURIZATION MAINTAINED CABIN ALTITUDE. DIVER TED TO PHL FOR LANDING. REMOVED AND REPLACED WINDSHIELD IAW AMM 56-11-01. 2 L 7 2 4F RT A21EA 2001061500037 20010615 00037 CE 2001 6 15 C2XA01CL143 1 20010614 A 3260 11438004115 ACTUATOR BEECH 1900 1900D 1154162 CE RIGHT GEAR INTERMITTENT A C2XA O OTHER P NO WARNING INDICATION AP APPROACH 1 SW 27 87557 1561 1561 UE246 CLE FLIGHT#3196 THE CREW REPORTED THE RIGHT GEAR LIGHT DID NOT ILLUMINTE ON THE 1ST GEAR EXTENSION.THE 2ND EXTENSION THE LIGHT ILLUMINATED.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE REPLACED THE RIGHT GEAR ACTUATOR.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT A24CE 2001061500038 20010615 00038 NM 2001 6 15 CALA0100542 1 20010613 A 5311 FRAME BOEING 737 7373T0 1384582 NM STA 727E CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16301 23352 INSPECTION FOUND A 1" CRACK IN FRAME AT STA 727E, RBL 1. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001061500039 20010615 00039 NM 2001 6 15 CALA0100544 1 20010615 A 5320 ANGLE BOEING 737 7373T0 1384582 NM STA 967-985 CUT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16301 23352 INSPECTION FOUND TOOLING MARKS CUT INTO L-2 DOOR Z-ANGLE AT STA 967-985. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-1 0-02. 2 L 7 2 4F RT A16WE 2001061500040 20010615 00040 EU 2001 6 15 RAIA00106007 1 20010613 A 2460 A2105F POWER UNIT JETAIR JETSTM JETSTM4101 1500501 EU ELEC BAY FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 562HK 8370 6285 41078 5379-ALB-RIGHT BATTERY WOULD NOT COME ON LINE. MAINTENANCE INSPECTED AND REPLACED RIGHT POWER DISTRIBUTION UNIT (PDU). 2 L 7 2 4T RT A41NM 2001061500041 20010615 00041 NM 2001 6 15 UPS01236100 1 20010527 A 5310 BULKHEAD BOEING 727 72725C 138400H NM NWW BS 294.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:C CRACKS AT BULKHEAD STA 294.5 RBL 12, NOSE LANDING GEAR WHEEL WELL, INSPECTED. INSPECTED NLG WHEEL WELL BULKHEAD AND VERIFY CRACK AS PER B727 NAT MANUAL PART 6 51-00-00 FIG 4. REMOVED VERTICAL ANGLE TO ACCESS REPAIR AN D CUT OUT CRACK AREA AS PER B727 SRM 51-30-2 REPAIR IN ACCORDING PER UPS EFILE# B72753-200-18 AND AUITAS EREPAIR ORDER# AUH M223RO-1 REV IR 2 L 7 3 4F A3WE 2001061500042 20010615 00042 NM 2001 6 15 UPS01236102 1 20010529 A 5300 SKIN BOEING 727 72725C 138400H NM NLGWW BS 294 R/H CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:C NOSE WHEEL WELL R/H SIDE WALL SHOW CRACK AT BS 294 WL165 CRACK ABOUT 10" LONG LOOKING GROM INSIDE REMOVED VERTICAL ANGLE FOR ACCESS REPAIR PER B727 SRM 51-30-2 CUT OUT DAMAGE AREA PER B727 SRM 51-40-2 APP.4 SIDE CUT OUT 6"X1" PERFORMED HFEC INSP AT CUT OUT DAMAGE. INSTALL DOUBLER REPAIR AS PER B727 SRM 51-30-2 REPAIR SIZE APPROX 10"X 4". 2 L 7 3 4F A3WE 2001061500043 20010615 00043 NM 2001 6 15 UPS01236105 1 20010531 A 5310 STRINGER BOEING 727 72725C 138400H NM BS1183 STR 18L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:C STRINGER TERMINAL FITTING CORRODED AT BS 1183 STR 18L REMOVED CORRODED STRINGER BS 1183, STR18L. P ER SRM 51-30-2, FABRICATED STRINGER TERMINAL FITTING PER BOEING DRAWING 65-242276 AND B727 SRM 51-10-2 TREATED AND PRIME D. INSTALLED STRINGER TERMINAL FITTING ON AIRCRAFT. 2 L 7 3 4F A3WE 2001061500044 20010615 00044 NE 2001 6 15 NACA20010024 2 20010614 A 7230 356993 CYLINDER PWA CB3 DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE ENGINE CRACKED A NACA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 779TA 519 P31070 45529 P31070 DISCREPANCY: #4 Engine will not take a lean & #17 cylinder shows no compression on analyzer.CORRECTIVE ACTION: Replaced the #4 cylinder assy. 2 L 7 4 4R 4 R A781 5E8 2001061500045 20010615 00045 WP 2001 6 15 MWEA010951 1 20010615 A 5310 9912243225 CLIP DOUG DC9 DC932 3022066 WP STATION 965 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 STATION 965 AT LONGERON 17 LEFT HAS A CRACKED CLIP ON THE AFT SIDE OF THE ENGINE FORWARD PYLON BULKHEAD. -- REMOVED AN GLE, FABRICATED AND INSTALLED NEW ANGLE. 2 L 7 2 4F A6WE 2001061500046 20010615 00046 WP 2001 6 15 MWEA010952 1 20010615 A 5310 99578899 INTERCOSTAL DOUG DC9 DC932 3022066 WP STATION 228 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FORWARD ENTRY INTERCOSTAL HAS 3 OPEN FASTENER HOLES INNER LEG HAS MATERIAL TRIMMED OUT SATION 228 ABOVE LONGERON 15 LEFT . -- FABRICATED AND INSTALLED REPAIRS. 2 L 7 2 4F A6WE 2001061500047 20010615 00047 WP 2001 6 15 MWEA010953 1 20010615 A 5310 59203493 FRAME DOUG DC9 DC932 3022066 WP STATION 579 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 STATION 579 BETWEEN LONGERON 5 AND 6 LEFT SIDE HAS SEVERAL OPEN DRILL HOLES. -- FABRICATED REPAIR DOUBLER, PLUGGED HOL ES, INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001061500048 20010615 00048 WP 2001 6 15 MWEA010954 1 20010615 A 5310 59114471 FRAME DOUG DC9 DC932 3022066 WP STATION 256 ELONGATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FUSELAGE FRAME STATION 256 AT LONGERON 6 RIGHT HAS ONE ELONGATED HOLE. -- REMOVED INTERCOSTAL CLIP AND FORMER SPLICE, FARICATED REPAIR DOUBLER, INSTALLED REPAIR, CLIP AND FORMER. 2 L 7 2 4F A6WE 2001061500049 20010615 00049 WP 2001 6 15 MWEA010955 1 20010615 A 5310 3912221503 FRAME DOUG DC9 DC932 3022066 WP STATION 294 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FUSELAGE FRAME STATION 294 AT LONGERON 6 RIGHT HAS NUMEROUS OPEN HOLES. -- PLUGGED HOLES IN FRAME, FABRICATED REPAIR P ARTS, INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001061500050 20010615 00050 WP 2001 6 15 MWEA010956 1 20010615 A 5310 3912238501 FRAME DOUG DC9 DC932 3022066 WP STATION 332 MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FUSELAGE FRAME STATION 332 AT LONGERON 6 RIGHT HAS A MISDRILLED HOLE. -- PLUGGED HOLES AND FABRICATED REPAIR DOUBLER, FABRICATED REPAIR, INTALLED REPAIR. 2 L 7 2 4F A6WE 2001061500051 20010615 00051 WP 2001 6 15 MWEA010957 1 20010615 A 5310 59114471 FRAME DOUG DC9 DC932 3022066 WP STATION 408 MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FUSELAGE FRAME STATIO N408 HAS MISDRILLED/OPEN HOLES (2 EA) A LONGERON 4 LEFT. -- FABRICATED, LOCATED AND DRILLED REPA IR ANGLE, INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001061500052 20010615 00052 WP 2001 6 15 MWEA010958 1 20010615 A 5310 59114471 FRAME DOUG DC9 DC932 3022066 WP STATION 408 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FUSELAGE FRAME STATION 408 HAS OPEN FASTENER HOLES AT LONGERON 4 RIGHT. -- FABRICATED, LOCATED AND DRILLED ANGLE REPAI R, INSTALLED NOMINAL FASTENERS. 2 L 7 2 4F A6WE 2001061500053 20010615 00053 WP 2001 6 15 MWEA010959 1 20010615 A 5310 59123651 FRAME DOUG DC9 DC932 3022066 WP STATION 427 MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FUSELAGE FRAME STATION 427 HAS MISDRILLED/OPEN FASTENER HOLES AT LONGERON 6 LEFT. -- FABRICATED REPAIR DOUBLER, INSTAL LED REPAIR. 2 L 7 2 4F A6WE 2001061500054 20010615 00054 WP 2001 6 15 MWEA010960 1 20010615 A 5310 59114471 FRAME DOUG DC9 DC932 3022066 WP STATION 446 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FUSELAGE FRAME STATION 446 HAS MISDRILLED/OPEN FASTENER HOLES AT LONGERON 6 LEFT. -- FABRICATED REPAIR DOUBLER, PLUGGE D HOLES, INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001061500055 20010615 00055 WP 2001 6 15 MWEA010961 1 20010615 A 5310 592034013 FRAME DOUG DC9 DC932 3022066 WP STATION 658 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 UPPER FUSELAGE FRAME STATION 658 HAS THREE HOLES THAT DO NOT HAVE (2 D) SPACING BETWEEN LONGERON 5 TO 6 LEFT. -- PLUGG ED HOLES, FABRICATED, LOCATED AND DRILLED ANGLE DOUBLER, INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001061500056 20010615 00056 WP 2001 6 15 MWEA010962 1 20010615 A 5310 592034013 FRAME DOUG DC9 DC932 3022066 WP STATION 658 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 UPPER FUSELAGE FRAME STATION 658 HAS HOLES THAT DO NOT HAVE (2 D) SPACING LONGERON 5 TO 6 RIGHT. -- PLUGGED HOLES, FAB RICATED REPAIR ANGLE, INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001061500057 20010615 00057 WP 2001 6 15 MWEA010965 1 20010615 A 5310 59203381 FRAME DOUG DC9 DC932 3022066 WP STATION 718 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 UPPER FUSELAGE FRAME STATION 718 HAS TWO FASTENER HOLES THAT DO NOT HAVE (2 D) SPACING INBOARD OF LONGERON 5 AND 6 LEFT. -- PLUGGED HOLES, FABRICATED REPAIR ANGLE, INSTALLED REPAIR ANGLE. 2 L 7 2 4F A6WE 2001061500058 20010615 00058 WP 2001 6 15 MWEA010966 1 20010615 A 5310 59203381 FRAME DOUG DC9 DC932 3022066 WP STATION 718 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 UPPER FUSELAGE FRAME STATION 718 HAS TWO FASTENER HOLES THAT DO NOT HAVE (2 D) SPACING INBOARD OF LONGERON 6 RIGHT. -- PLUGGED HOLES, FABRICATED AND INSTALLED REPAIR ANGLE. 2 L 7 2 4F A6WE 2001061500059 20010615 00059 WP 2001 6 15 MWEA010967 1 20010615 A 5310 59203493 FRAME DOUG DC9 DC932 3022066 WP STATION 579 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FRAME STATION 579 IN BETWEEN LONGERON 4 AND 5 RIGHT SIDE TWO OPEN DRILL HOLES CHECK EDGE DISTANCE. -- FABRICATED REPAI R DOUBLER, INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001061500060 20010615 00060 WP 2001 6 15 MWEA010968 1 20010615 A 5310 59203493 FRAME DOUG DC9 DC932 3022066 WP STATION 579 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FRAME STATION 579 IN BETWEEN LONGERON 5 AND 6 RIGHT SIDE HAS SEVERAL OPEN DRILL HOLES. -- FABRICATED REPAIR DOUBLER, I NSTALLED REPAIR. 2 L 7 2 4F A6WE 2001061500061 20010615 00061 WP 2001 6 15 MWEA010969 1 20010615 A 5310 59203371 FRAME DOUG DC9 DC932 3022066 WP STATION 598 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FRAME STATION 598 IN BETWEEN LONGERON 5 AND 6 RIGHT SIDE HAS SEVERAL OPEN DRILL HOLES ONE IS FIGURE EIGHT. -- PLUGGED HOLES, FABRICATED REPAIR DOUBLER, INSTALLED ANGLE REPAIR. 2 L 7 2 4F A6WE 2001061500062 20010615 00062 WP 2001 6 15 MWEA010970 1 20010615 A 5310 59203371 FRAME DOUG DC9 DC932 3022066 WP STATION 598 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FRAME STATION 598 IN BETWEEN LONGERON 5 AND 6 LEFT SIDE HAS SEVERAL OPEN DRILL HOLES ONE IS IN THE RADIUS. -- PLUGGED HOLES AND FABRICATED REPAIR DOUBLER, INSTALLED ANGLE REPAIR. 2 L 7 2 4F A6WE 2001061500063 20010615 00063 WP 2001 6 15 MWEA010971 1 20010615 A 5310 5920338503 FRAME DOUG DC9 DC932 3022066 WP STATION 756 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 UPPER FUSELAGE FRAME STATION 756 HAS TWO HOLES THAT DO NOT HAVE (2 D) SPACING BETWEEN LONGERON 5 AND 6 RIGHT. -- FABRI CATED, LOCATED AND DRILLED REPAIR, INSTALLED REPAIR ANGLE. 2 L 7 2 4F A6WE 2001061500064 20010615 00064 WP 2001 6 15 MWEA010972 1 20010615 A 5310 59114471 FRAME DOUG DC9 DC932 3022066 WP STATION 794 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 UPPER FUSELAGE FRAME STATION 794 HAS TWO HOLES THAT DO NOT HAVE (2 D) SPACING BETWEEN LONGERON 5 AND 6 LEFT. -- FABRIC ATED REPAIR DOUBLER AND SHIMS, INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001061500065 20010615 00065 WP 2001 6 15 MWEA010973 1 20010615 A 5310 59114471 FRAME DOUG DC9 DC932 3022066 WP STATION 832 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 UPPER FUSELAGE FRAME STATION 832 HAS TWO HOLES THAT DO NOT HAVE 2D SPACING BETWEEN LONGERON 5 AND 6 RIGHT. -- PLUGGED HOLES, FABRICATED A REPAIR ANGLE, INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001061500066 20010615 00066 WP 2001 6 15 MWEA010974 1 20010615 A 5310 59114471 FRAME DOUG DC9 DC932 3022066 WP STATION 503 MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FRAME STATION 503 IN BETWEEN LONGERON 5 AND 6 RIGHT SIDE HAS ONE MISDRILLED HOLE AND THREE OPEN DRILLED HOLES, CHECK EDG E DISTANCE. -- FABRICATED, LOCATED AND DRILLED NEW ANGLE, INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001061500067 20010615 00067 WP 2001 6 15 MWEA010975 1 20010615 A 5310 59114471 FRAME DOUG DC9 DC932 3022066 WP STATION 813 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 UPPER FUSELAGE FRAME 813 HAS THREE HOLES THAT DO NOT HAVE (2D) SPACING BETWEEN LONGERON 5 AND 6 LEFT. -- PLUGGED HOLES IN FRAME, FABRICATED REPAIR PARTS, INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001061500068 20010615 00068 WP 2001 6 15 MWEA010976 1 20010615 A 5310 59114471 FRAME DOUG DC9 DC932 3022066 WP STATION 870 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 UPPER FUSELAGE STATION 870 HAS TWO HOLES THAT DO NOT HAVE (2D) SPACING BETWEEN LONGERON 5 AND 6 LEFT. -- PLUGGED HOLES , FABRICATED A REPAIR ANGLE, INSTALLED REPAIR ANGLE. 2 L 7 2 4F A6WE 2001061500069 20010615 00069 WP 2001 6 15 MWEA010977 1 20010615 A 5310 59114471 FRAME DOUG DC9 DC932 3022066 WP STATION 870 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 UPPER FUSELAGE FRAME 870 HAS TWO HOLES THAT DO NOT HAVE (2D) SPACING BETWEEN LONGERON 5 AND 6 RIGHT. -- PLUGGED HOLES, FABRICATED A REPAIR ANGLE, INSTALLED REPAIR ANGLE. 2 L 7 2 4F A6WE 2001061500070 20010615 00070 WP 2001 6 15 MWEA010978 1 20010615 A 5310 991960343 FRAME DOUG DC9 DC932 3022066 WP STATION 889 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 UPPER FUSELAGE FRAME STATION 889 HAS THREE HOLES THAT DO NOT HAVE (2D) SPACING BETWEEN LONGERON 5 AND 6 LEFT. -- FABRI CATED, LOCATED AND DRILLED REPAIR ANGLE AND FILLER, INSTALLED REPAIR ANGLE DOUBLER. 2 L 7 2 4F A6WE 2001061500071 20010615 00071 WP 2001 6 15 MWEA010979 1 20010615 A 5310 99578893 INTERCOSTAL DOUG DC9 DC932 3022066 WP STATION 228 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FORWARD ENTRY INTERCOSTAL HAS FIVE OPEN FASTENER HOLES AND INNER LEG HAS MATERIAL TRIMMED OUT STATION 228 ABOVE LONGERON 11 LEFT. -- FABRICATED AND INSTALLED REPAIR ANGLES. 2 L 7 2 4F A6WE 2001061500072 20010615 00072 NM 2001 6 15 0101896631 1 20010613 A 3350 POWER SUPPLY BOEING 747 747251B 1384892 NM EMERG LTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 631US 23111 DURING LINE CHECK, FOUND "C" ZONE EMERGENCY ESCAPE PATH LIGHTING FAILED OPERATIONAL CHECK. REPLACED POWER SUPPLY. OPE RATIONAL CHECK NORMAL. 2 L 7 4 4F A20WE 2001061500073 20010615 00073 NM 2001 6 15 0102076303 1 20010609 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM EMER LTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 663US 23818 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTS INOPERATVE IN "B" ZONE AND BETWEEN SEATS 1JK-4JK "A" ZONE. REPL ACED "B" ZONE POWER SUPPLY AND SECURED CONNECTOR PIN ON LIGHT ASSEMBLY AT SEAT 4JK. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001061500074 20010615 00074 2001 6 15 MWEA010981 4 20010612 A 2210 2587788902 SERVO DOUG DC9 DC932 3022066 WP LOWER PEDESTAL INOPERATIVE A MWEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 31 209ME 47730 WHEN AUTOPILOT WAS ENGAGED THE AIRCRAFT ROLLED VIOLENTLY TO THE LEFT. AP WAS IMMEDIATELY DISENGAGED AND WE NOTICED A WHI NING/HUMMING SOUND WHICH CONTINUED FOR REMAINDER OF THE FLIGHT. -- DEFERRED AUTOPILOT CONTROLLER PER MEL 22-05 PULLED AND COLLERED C/B'S D-2, E-2 DUE TO AILERON SERVO RUNNING CONTINUOUSLY. AILERON SERVO ALSO VIBRATES WHEN RUNNING. PLACARD S INSTALLED. REMOVED AND REPLACED STICK SHAKER DRIVE SERVO. 2 L 7 2 4F A6WE 2001061500075 20010615 00075 WP 2001 6 15 2001F00000 1 20010514 A 3350 AD4002P BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 827US 48049 IND - THE LOW LEVEL EMERGENCY LIGHTS, NACELLE SCAN, AND CEILING LIGHTS AT SEAT ROWS 7 TO 17 WERE INOPERATIVE. MAINTENAN CE REPLACED THE LOW LEVEL, NACELLE SCAN, AND CEILING EMERGENCY LIGHT BATTERIES. REF USAAD01103. (M) 2 L 7 2 4F A6WE 2001061500076 20010615 00076 NM 2001 6 15 2001F00002 1 20010416 A 3350 8821004 BATTERY BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY TRACK LIGHTS WOULD NOT TEST USING COCKPIT SWITCH. REMOVED AND REPLACED THREE REMOTE ASSEMBLY BATTERIES AND ONE REMOTE ASSEMBLY RECEIVER AT ROW 16, THEN LIGHTS OPERATED NORMAL. REF ASAA011021 8. 2 L 7 2 4F A16WE 2001061500077 20010615 00077 NM 2001 6 15 2001F00003 1 20010416 A 3350 86210144 BATTERY BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE ON SEAT PALLETS 1-4 AND 2-11. REMOVED AND REPL ACED REMOTE ASSEMBLY BATTERIES AND RECEIVER IN PALLET 1-4, AND REMOTE ASSEMBLY RECEIVER IN PALLET 2-11, THEN LIGHTS TEST ED NORMAL. REF ASAA0110211. (M) 2 L 7 2 4F RT A16WE 2001061500078 20010615 00078 NE 2001 6 15 2001F00004 2 20010414 A 7261 KB21353 O-RING LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE OIL SYSTEM PINCHED A WRNA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 05 311EA 193A1012 10063 NR 3 ENGINE OIL QUANTITY DROPPED TO 1 QUART, OIL PRESSURE FLUCTUATED BUT DID NOT DROP BELOW 35 PSI. AIRCRAFT LANDED WIT HOUT INCIDENT. FOUND DAMAGED (PINCHED) O-RING AT NR 3 ENGINE OIL PRESSURE FILTER BOWL CAP. REMOVED AND REPLACED O-RING IAW MM 72-01-00. RESERVICED ENGINE TO PROPER OIL LEVEL. ENGINE RUN UP CHECK AND LEAK CHECK COMPLIED WITH. NO LEAK NO TED, A/C RETURNED TO SERVICE. (M) 2 L 7 3 4F 4 F A23WE E12EU 2001061500079 20010615 00079 WP 2001 6 15 AALA016048 1 20010501 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A K NONE L NO TEST NR NOT REPORTED 1 SW 21 823RA 49889 CCI-RNO - EMERGENCY LIGHT AT SEAT 3E INOPERATIVE. REPAIRED BROKEN WIRE AT SEAT 3E EMERGENCY LIGHT. OPS CHECKS OK. (M) 2 L 7 2 4F A6WE 2001061500080 20010615 00080 WP 2001 6 15 0101929852 1 20010524 A 3240 ACCUMULATOR DOUG DC9 DC951 3022051 WP BRAKE SYSTEM DISCHARGED A NWAA K NONE J WARNING INDICATION DE DESCENT 1 GL 01 761NC 47709 DURING DESCENT INTO DTW, THE LEFT BRAKE SYSTEM PRESSURE WENT TO ZERO PSI WITH LEFT HYDRAULIC SYSTEM PRESSURE 3000 PSI, Q UANTITY WAS GOOD. COMPLIED WITH COM PROCEDURES WITH NO RESULTS. DECLARED AN EMERGENCY AND REQUESTED LONGEST RUNWAY AVA ILABLE. LANDED UNEVENTFULLY WITH BRAKE SELECT IN BOTH. DURING BRAKE ACTION THE LEFT BRAKE PRESSURE RECOVERED TO 3000 P SI. MAINTENANCE FOUND LEFT BRAKE ACCUMULATOR FLAT. RESERVICED BRAKE ACCUMULATOR AND BLED BRAKES. OPERATIONAL CHECK OK . 2 L 7 2 4F RT A6WE 2001061500081 20010615 00081 NM 2001 6 15 0101936301 1 20010524 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 661US 23719 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE BETWEEN SEATS 31C-29C, 51C-64C, AT LEFT SIDE OF FIRS T CLASS SECTION, AND BETWEEN LAV DOORS 1L-2L. RECONNECTED LOOSE WIRING AT 39C, 60C, 64, AND 4J. OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 2001061500082 20010615 00082 NM 2001 6 15 0101946642 1 20010512 A 2530 RECEPTACLE BOEING 747 747251B 1384892 NM GALLEY FAULTY A NWAA H DEACTIVATE SYST/CIRCUITS B A SMOKE/FUMES/ODORS/SPARKS FLAME/FIRE LD LANDING 1 GL 01 642NW 21942 ON LANDING, FLIGHT ATTENDANT NOTICED SPARKS AND FLAME AT NR 2 GALLEY NR 2 COFFEEMAKER. REPLACED COFFEEMAKER ELECTRICAL RECEPTACLE. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F A20WE 2001061500083 20010615 00083 WP 2001 6 15 0101951153 1 20010523 A 7714 8TJ141AAG1 TRANSMITTER DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 3 ENGINE MALFUNCTIONED A NWAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 01 153US 42268 46762 686135 AT APPROXIMATELY 80 KTS ON TAKEOFF ROLL, THE NR 3 ENGINE FAIL LIGHT ILLUMINATED. THE CREW OBSERVED THE NR 3 N1 AND N2 I NDICATIONS DECREASING AND ABORTED TAKEOFF AT 100 KTS. THE EPR INDICATION WAS REPORTED AS NORMAL. MAINTENANCE REPLACED THE N1 TRANSMITTER AND OPERATED THE ENGINE WITH ALL INDICATIONS NORMAL. THE N2 DISCREPANCY COULD NOT BE DUPLICATED. 2 L 7 3 4F 4 F A22WE E20EA 2001061500084 20010615 00084 WP 2001 6 15 MWEA010982 1 20010613 A 2920 182205 SOLENOID VALVE DOUG DC9 DC932 3022066 WP RIGHT WHEEL WELL INOPERATIVE A MWEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 31 209ME 47730 RIGHT HYDRAULIC TEMP HI ANNUNCIATOR CAME ON DURING TAXI OUT. -- REFERENCE DMI #6-50 "ALTERNATE PUMP WILL NOT OPERATE W HEN SWITCH IS TURNED ON," REMOVED AND REPLACED ALTERNATE PUMP SOLENOID VALVE, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 2001061500085 20010615 00085 WP 2001 6 15 MWEA010983 1 20010615 A 5310 5920338501 FRAME DOUG DC9 DC932 3022066 WP STATION 737 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 UPPER FUSELAGE FRAME STATION 737 HAS THREE HOLES THAT DO NOT HAVE (2D) SPACING BETWEEN LONGERONS 5 AND 6 LEFT. -- PLUG GED HOLES, FABRICATED, LOCATED AND DRILLED REPAIR ANGLES, INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001061500086 20010615 00086 WP 2001 6 15 MWEA010984 1 20010615 A 5310 991960111 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 REMOVED CABIN FLOORBOARD B10 TO FACILITATE OTHER MAINTENANCE. -- FABRICATED NEW SKIN AND HAT SECTIONS, INSTALLED INSUL ATION AND SHIM MATERIAL. 2 L 7 2 4F A6WE 2001061500087 20010615 00087 WP 2001 6 15 MWEA010985 1 20010615 A 5310 591142485 SKIN DOUG DC9 DC932 3022066 WP STATION 813 GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 GOUGE AT STATION 813 BETWEEN LONGERONS 25 AND 26 RIGHT. -- BLENDED GOUGE, CUT OUT SKIN, REMOVED LOWER FLANGE OF SHEAR TIES, FABRICATED REPAIR, INSTALLED REPAIR DOUBLER AND SKIN REPAIR, FABRICATED SHEAR TIE REPAIR ANGLES, INSTALLED SHEAR T IES. 2 L 7 2 4F A6WE 2001081300201 20010813 00201 NM 2001 8 13 F3LA200100090 1 20010612 A 3350 1000679 LIGHT BOEING 737 7372Y5 1384554 NM COCKPIT INOPERATIVE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 118RW 20 23040 DURING SERVICE CHECK, MAINTENANCE REPORTED FLIGHT DECK EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LIGHT ASSY. AND CHECK ED OKAY. 2 L 7 2 4U RT A16WE 2001061500090 20010615 00090 EU 2001 6 15 QXEA0100941 1 20010609 A 2740 FOKKER FOKKER F28 F28MK4000 4990810 EU A QXEA O OTHER Z SIGNIFICANT FAILURE REPORT DE DESCENT 1 NM 09 475AU MC132 11222 SEA - CREW REPORTED BOTH HORIZONTAL STABILIZER CHANNEL LIGHTS ILLUMINATED DURING DECENT. ALTERNATE STABILIZER TRIM ALSO FOUND INOPERATIVE. FLIGHT CREW COMPLIED WITH JAMMED STABILIZER CHECKLIST. LANDING AND ROLL OUT PERFORMED WITHOUT INCIDEN T. REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001061500091 20010615 00091 EU 2001 6 15 QXEA0101033 1 20010613 A 3350 POWER SUPPLY GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 499US 1980 11182 PDX - AFT EXTERIOR EMERGENCY EXIT LIGHTS. REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURN ED TO SERVICE. 2 L 7 2 4F RT A20EU 2001061700001 20010617 00001 NM 2001 6 17 C1HA200196004 1 20010601 A 2611 473597404 SMOKE DETECTOR BOEING 727 7272J4 1384006 NM FWD PIT FAULTY A C1HA K NONE J WARNING INDICATION IN INSP/MAINT 1 GL 15 696CA 22574 Smoke detection alarm in aft pit:ACTION TAKEN:R&R'd fwd smoke detector. 2 L 7 3 4F RT A3WE 2001061700002 20010617 00002 NM 2001 6 17 C1HA200193009 1 20010607 A 3350 1000679 LIGHT BOEING 727 727212 138407G NM COCKPIT INOPERATIVE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 293AS 21348 Cockpit portable emergency lighjt inop.ACTION TAKEN:R&R'd emergency light ops ck good. 2 L 7 3 4F A3WE 2001061700003 20010617 00003 NM 2001 6 17 C1HA200194013 1 20010609 A 3610 356644400 SENSOR BOEING 727 727290 138408W NM #1 PYLON FAILED A C1HA O A OTHER UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 15 294AS 22146 On rotation #1 strut overheat light illuminated at 1000ft. AGL. reduced power #1 engine light went out. Air return overw eight landing made wt.177,000sink rate at touchdown 300' per min very little braking used.ACTION TAKEN:Inspected and fou nd air leak at 13th stage mod valve removed and replaced valve perormed ground run overheat condition still exists. Repl aced #1 eng strut sensor performed ground run ops ck good. Performed overweight landing inspection no defects noted. 2 L 7 3 4F A3WE 2001061700004 20010617 00004 NM 2001 6 17 C1HA200196005 1 20010614 A 3610 32146451 SHUTOFF VALVE BOEING 727 7272J4 1384006 NM #2 STUCK A C1HA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 15 696CA 22574 Prior to 60kts during TO roll auto pack trip occured and eng fail light flickered.ACTION TAKEN:Ts bleed system found #2 engine shutoff valve stuck in open position replaced valve ops ck good. 2 L 7 3 4F RT A3WE 2001061700005 20010617 00005 NM 2001 6 17 C1HA200197004 1 20010609 A 3350 100865 CHARGER BOEING 727 727270 138408P NM FWD FAILED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 697CA 23052 Forward emergency floor track lighting inop.ACTION TAKEN:Replaced fwd. track lighting charger ops checked good. 2 L 7 3 4F RT A3WE 2001061800001 20010618 00001 NM 2001 6 18 01FDEA00390 1 20010530 A 2730 CONNECTOR BOEING 727 727227 1384078 NM FEE L COMPUTER CONTAMINATED A FDEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 25 496FE 1659D 21670 ON DEPARTURE, ELEV FEEL LIGHT CAME ON. *S/D* REMOVED AND REPLACED ELEV FEEL COMPUTER PITOT LINES CONNECTIONS. RIGGED STAB TRIM POTENTIMETER PER MM 22-11-061-4. BIRD NEST AND BIRD EGGS FOUND IN PNLS 9710, 9118, 9218. 2 L 7 3 4F A3WE 2001061800002 20010618 00002 NM 2001 6 18 01FDEA00391 1 20010529 A 5313 STRINGER BOEING 727 72725C 138400H NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 118FE 19300 AT BS 400 STR 1, 2R & 3L ARE CRACKED AT FASTENER COMMON TO STR AND FRAME. REMOVED AND REPLACED STRINGERS PER IAW FEDEX EA 7-5310-57956. 2 L 7 3 4F A3WE 2001061800003 20010618 00003 EU 2001 6 18 01FDEA00392 1 20010601 A 2150 A21510424 LEVER AIRBUS 310 A310222 3930315 EU A/C SYSTEM BROKEN A FDEA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 25 452FE 313 ON LD MIN EQUIP BAY SMOKE LIGHT ON ECAM. FAULT TRACED TO BROKEN CRANK AT DEFLECT. MAN SELECT HELD OPEN FAULT CLEARED. PACK OPS NORM. 2 L 7 2 4F RT A35EU 2001061800004 20010618 00004 NM 2001 6 18 01FDEA00393 1 20010602 A 2613 SENSOR BOEING 727 727227 1384078 NM AFT AIRSTAIR FAULTY A FDEA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SO 25 482FE 21464 LWF AFT BODY WARN LIGHT ILLUM. REMOVED AND REPLACED 6 O/H SENSORS IN AFT AIRSTAIR. REPLACED D1306 CONNECTOR. 2 L 7 3 4F A3WE 2001061800005 20010618 00005 NM 2001 6 18 01FDEA00394 1 20010605 A 2120 UNKNOWN BOEING 727 72722 1384002 NM CABIN ODOR A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 25 191FE 19084 UNIDENTIFIED ODOR NOTICED IN FLT. FOLLOWED APPROPRIATE QUICK REF HANDBOOK CK LIST. INSP AIRCRAFT NO CONTAMINATION FOUN D. 2 L 7 3 4F A3WE 2001061800017 20010618 00017 NM 2001 6 18 2001UALA00762 1 20010521 A 5310 BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 511UA 24799 CREASE BEAM WEB CORRODED STA 1160-1180 LEFT SIDE. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2001061800018 20010618 00018 NM 2001 6 18 2001UALA00763 1 20010519 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 511UA 24799 CREASE BEAM CORRODED STA 965 LEFT SIDE. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2001061800019 20010618 00019 NM 2001 6 18 2001UALA00764 1 20010519 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 511UA 24799 CREASE BEAM WEB CORRODED STA 1160-1180 RIGHT SIDE. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2001061800020 20010618 00020 NM 2001 6 18 2001UALA00765 1 20010520 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 511UA 24799 CABIN FLOORBEAM CORRODED STA 1640 RBL 11-58. MAJOR REPAIR ACCOMPLISHED. INSTALLED CAP SPLICE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001061800021 20010618 00021 NM 2001 6 18 2001UALA00766 1 20010520 A 5311 DOUBLER BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 996UA 22456 PREVIOUS FRAME REPAIR CRACKED AT BS 420, STR 23L. REPLACED REPAIR DOUBLER. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F A16WE E2EA 2001061800022 20010618 00022 NM 2001 6 18 2001UALA00767 1 20010520 A 5320 WEB BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 996UA 22456 FLOOR PRESSURE WEB CRACKED AT BS 1004, LBL 40, WL 208. REMOVED AND REPLACED WEB. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F A16WE E2EA 2001061800023 20010618 00023 NM 2001 6 18 2001UALA00768 1 20010521 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 WEB CRACKED AT BS 178, LBL 7, WL 213. REMOVED DAMAGE. INSTALLED DOUBLER. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001061800024 20010618 00024 NM 2001 6 18 2001UALA00769 1 20010520 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 317UA 23949 WEB CRACKED AT BS 178, BL 0, WL 188. INSTALLED WEB DOUBLER. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001061800025 20010618 00025 NM 2001 6 18 2001UALA00770 1 20010518 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 CABIN FLOORBEAM UPPER FLANGE HAS EXCESSIVE MATERIAL LOSS AT STA 294, RBL 16 TO RBL 45, WL 208. REPLACED FLOORBEAM UPPER FLANGE. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001061800026 20010618 00026 2001 6 18 2001UALA00771 4 20010520 A 3418 COMPUTER BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE STALL WARNING MALFUNCTIONED A UALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 29 903UA 25003 STICK SHAKER ACTIVATION ON TAKE-OFF. SUPPLEMENTAL DATA UPDATE REPLACED NR 1 AND NR 2 STALL MANAGEMENT COMPUTER 2 L 7 2 4F 4 F RT A16WE E2GL 2001071800023 20010718 00023 NM 2001 7 18 2001UALA00772 1 20010518 A 3230 LANDING GEAR BOEING 737 737322 1384676 NM NLG & MLG MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 389UA 24664 GEAR WOULD NOT RETRACT AFTER TAKEOFF. *S/D* MAINTENANCE ACCOMPLISHED MAIN LANDING GEAR OPERATIONAL CHECK PER THE MAINT ENANCE MANUAL. ACCOMPLISHED INSPECTION OF MAIN LANDING GEAR SAFETY SENSORS WITH NO DISCREPANCIES NOTED. MAINTENANCE FO UND ALL LANDING GEAR OPERATIONS TO BE NORMAL AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2001061800027 20010618 00027 NM 2001 6 18 2001UALA00773 1 20010520 A 5755 FITTING BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SPOILER DEFECTIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 772UA 26930 NR 8 SPOILER WILL NOT TAKE LUBRICATION AT CNT OUTBOARD HINGE. MAJOR REPAIR. FITTING REWORKED PER EVA G95-7722. SPOILE R REMOVED AND REINSTALLED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001061800028 20010618 00028 NM 2001 6 18 2001UALA00776 1 20010522 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 511UA 24799 FLOORBEAM CORRODED STA 324, RBL 57. MAJOR REPAIR ACCOMPLISHED. INSTALLED SPLICE ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2001061800029 20010618 00029 NM 2001 6 18 2001UALA00778 1 20010521 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 FUSE FRAME CRACKED IN RADIUS AT BS 188, WL 207, RT SIDE. ACCOMPLISHED REINFORCEMENT REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001061800030 20010618 00030 NM 2001 6 18 2001UALA00779 1 20010521 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 STRINGER 38R CRACKED AT THE END UNDER FRAME STATION 456 RT. MAJOR REPAIR ACCOMPLISHED. REPAIRED STRINGER PER SRM 53-00 -03 AND 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001061800031 20010618 00031 NM 2001 6 18 2001UALA00780 1 20010521 A 5320 CLIP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE MISALIGNED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 STRINGER 39L FORWARD END CLIP DOES NOT ALIGN WITH PREDRILLED STRINGER STATION 325. MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP PER BAC DRAWING 141T3001 AND T-ANGLE PER BAC DRAWING 141T1220 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001061800032 20010618 00032 NM 2001 6 18 2001UALA00781 1 20010517 A 5270 WARNING LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 661UA 27158 EICAS FWD CARGO DOOR WITH ASSOCIATED LIGHT DISPLAYED IN CLIMB. LIMITED TO 10,000 FT ALT. ACFT TO RETURN TO JFK. 2 L 7 2 4F 4 F RT A1NM E24NE 2001061800033 20010618 00033 2001 6 18 2001UALA00782 4 20010518 A 2565 D30674101 TUBE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SLIDE UNSERVICEABLE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 404UA * 1 450 SLIDE/RAFT D30665-105 TOP INFLATION TUBE RT SIDE SEAM FAILED DURING PROOF PRESSURE TEST. TOP TUBE HAS A 4 FOOT SEAM RIP ON RT SIDE ABOVE THE REDUCER BULKHEAD FROM THE FAILURE. UNIT IS BEING SENT TO THE VENDOR FOR REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2001061800034 20010618 00034 NM 2001 6 18 2001UALA00784 1 20010519 A 5242 ATTACH ANGLE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE E/E BAY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 FORWARD EQUIPMENT BAY DOOR HAS A CRACK ON ATTACH ANGLE IN HANDLE BAY, CENTER OF DOOR.SUPPLEMENTAL DATA UPDATE MAJOR REPA IR ACCOMPLISHED REMOVED INNER DOOR SKIN, FABRICATED NEW ATTACH ANGLE PER BAC DRAWING 141T6422 AND INSTALLED PER SRM 51-4 0-02, REINSTALLED SKIN DOOR PER SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001061800035 20010618 00035 NM 2001 6 18 SWAA011667 1 20010608 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN FLOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 651SW 27721 EEPLS COVER LOOSE AT ROW 14. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2001061800036 20010618 00036 2001 6 18 SWAA011671 4 20010608 A 2565 6557463 BRACKET BOEING 737 7377H4 NM AFT SVC DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 793SA 27888 AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR LATCH BROKEN. R&R AFT SVC DOOR GIRT BAR LATCH P ER MM. 2 L 7 2 4F RT A16WE 2001061800037 20010618 00037 NM 2001 6 18 SWAA011673 1 20010608 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM AFT CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 331SW 23695 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER LOOSE AT AFT CABIN. SECURED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2001061800038 20010618 00038 NM 2001 6 18 SWAA011674 1 20010608 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 331SW 23695 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001061800039 20010618 00039 NM 2001 6 18 SWAA011675 1 20010608 A 5300 6545773 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, ABOVE LAP SEAM BETWEEN WINDOWS # 5 & # 6. 2 L 7 2 4F RT A16WE 2001061800040 20010618 00040 NM 2001 6 18 SWAA011676 1 20010609 A 5330 6552988 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR LOWER HINGE CUTOUT. REPAI RED SKIN PER SRM. 2 L 7 2 4F A16WE 2001061800041 20010618 00041 NM 2001 6 18 SWAA011677 1 20010609 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED D CHECK, FOUND STRINGER 15R CRACKED AT BS 530. REPAIRED STR PER SRM. 2 L 7 2 4F A16WE 2001061800042 20010618 00042 NM 2001 6 18 SWAA011681 1 20010608 A 5330 6552988 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001061800043 20010618 00043 NM 2001 6 18 SWAA011684 1 20010608 A 5311 6546529 FRAME BOEING 737 7372H4 138448C NM FWD CARGO CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED FWD CARGO AT BS 440, RBL 39 & WL 160. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2001061800044 20010618 00044 NM 2001 6 18 SWAA011685 1 20010608 A 5330 6545773 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT RH WINDOW #'S 3, 4, 8, 10, 12, 5 & 6, UPPER FWD CORNER CUTOUTS. REPAIRED SKIN PER BFG ER 2 L 7 2 4F A16WE 2001061800045 20010618 00045 NM 2001 6 18 SWAA011686 1 20010608 A 5330 6545773 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT RH WINDOW #'S 25, 26, 27 & 8, LWR FWD CORNER CUTOUTS. REPAIRED SKIN PER BFG ER. 2 L 7 2 4F A16WE 2001061800046 20010618 00046 NM 2001 6 18 SWAA011687 1 20010608 A 5330 6545773 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT RH WINDOW #'S 2, 3, 5, 6, 7, 8, 9 & 10, LWR AFT CORNER CUTOUTS. REPAIRED PER BFG ER. 2 L 7 2 4F A16WE 2001061800047 20010618 00047 NM 2001 6 18 SWAA011688 1 20010608 A 5330 6545773 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT RH WINDOW #'S 28 & 27, UPPER AFT CORNER. REPAIRED PER BFG ER. 2 L 7 2 4F A16WE 2001061800048 20010618 00048 NM 2001 6 18 SWAA011657 1 20010607 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED D CHECK, FOUND STRINGERS CRACKED AT BS 537,STR 14L & BS 1010, STR 5L. RE PAIRED STRINGERS PER SRM. 2 L 7 2 4F A16WE 2001061800049 20010618 00049 NM 2001 6 18 SWAA011658 1 20010606 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN FLOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 709SW 27843 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER CRACKED AT FWD CABIN. R&R EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2001061800050 20010618 00050 NM 2001 6 18 SWAA011659 1 20010606 A 2731 BACB28AK04 BUSHING BOEING 737 7377H4 NM LH ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 709SW 27843 DURING SCHEDULED C2 CHECK, FOUND VERTICAL PLAY AT LH ELEVATOR TAB # 3 HINGE. R&R # 3 HIN GE BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2001061800051 20010618 00051 NM 2001 6 18 SWAA011662 1 20010606 A 5330 65C35794 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 967, STR 21L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001061800052 20010618 00052 NM 2001 6 18 SWAA011652 1 20010606 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED D CHECK, FOUND STR 16L CRACKED AT BS 767, BS 807 & BS 827. REPAIRED STR PER SRM. 2 L 7 2 4F A16WE 2001061800053 20010618 00053 NM 2001 6 18 2001UALA00785 1 20010521 A 5320 ATTACH ANGLE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 AFT CARGO PIT BS 1087 AT STR 39L, STRINGER TO FRAME ATTACH ANGLE CORRODED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001061800054 20010618 00054 NM 2001 6 18 SWAA011729 1 20010614 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED D CHECK, FOUND STRINGER 8L HAS SEVERAL CRACKS AT BS 500D TO BS 524. R EPAIRED STR PER SRM. 2 L 7 2 4F RT A16WE 2001061800055 20010618 00055 NM 2001 6 18 SWAA011703 1 20010611 A 5313 BAC1498 STRINGER BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CORRODED, AT BS 500D, STR 26R. REPAIRED STR PER SRM. 2 L 7 2 4F RT A16WE 2001061800056 20010618 00056 NM 2001 6 18 SWAA011711 1 20010613 A 5330 6552988 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001061800057 20010618 00057 NM 2001 6 18 SWAA011714 1 20010613 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN FLOOR DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 357SW 26594 EEPLS COVERS DAMAGED. R&R EEPLS COVERS PER MM. 2 L 7 2 4F RT A16WE 2001061800058 20010618 00058 NM 2001 6 18 SWAA011715 1 20010613 A 3350 65C34691 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 OVER HEAD BIN BULL NOSE EMERGENCY EXIT LENS MISSING AT ROW 20 DEF. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2001061800059 20010618 00059 NM 2001 6 18 SWAA011719 1 20010611 A 5310 6546569 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8-9 LH. 2 L 7 2 4F RT A16WE 2001061800060 20010618 00060 NM 2001 6 18 SWAA011720 1 20010612 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKINS CRACKED AT BS 500B, STR 10R & BS 360, STR 10L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001061800061 20010618 00061 NM 2001 6 18 SWAA011721 1 20010612 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, STR 23R. REPAIRED STR PER SRM. 2 L 7 2 4F RT A16WE 2001061800062 20010618 00062 NM 2001 6 18 SWAA011722 1 20010612 A 5330 65C35794 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 22R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001061800063 20010618 00063 NM 2001 6 18 SWAA011723 1 20010612 A 5330 65C27755 SKIN BOEING 737 7373T5 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 667SW 23063 DURING SCHEDULED C4 CHECK, FOUND FUSELGE SKIN CRACKED AT AFT SVC DOOR UPPER HINGE CUTOUT. REPAIR ED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001061800064 20010618 00064 NM 2001 6 18 SWAA011724 1 20010613 A 5330 6545769 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, WL 148 & RBL6. REPAIRED SKI N PER SRM. 2 L 7 2 4F RT A16WE 2001061800066 20010618 00066 2001 6 18 SWAA011689 4 20010610 A 2565 65C16820 RETAINER BOEING 737 7373Y0 1384671 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 682SW 23496 FED ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM. 2 L 7 2 4F RT A16WE 2001061800067 20010618 00067 NM 2001 6 18 SWAA011691 1 20010610 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN FLOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 718SW 27852 DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVERS CRACKED AT ROW'S 1, 2, 4, 6, 13, 15, 16, 17 & 23. R&R EEPLS TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 2001061800068 20010618 00068 NM 2001 6 18 SWAA011697 1 20010611 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 090SW 22905 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER CRACKED AT BS 530, STR 15L & 14R. REPAIRED STR PER SRM. 2 L 7 2 4F A16WE 2001061800069 20010618 00069 NM 2001 6 18 SWAA011699 1 20010609 A 5710 6549488 SUPPORT FITTING BOEING 737 7373H4 1384600 NM RH WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 380SW 26587 DURING SCHEDULED A2 CHECK, FOUND RH MLG WALKING BEAM SUPPORT FITTING CORRODED. R&R MLG SUPPORT FITTING PER ALM WORK CARD 3371. 2 L 7 2 4F RT A16WE 2001061800070 20010618 00070 NM 2001 6 18 SWAA011700 1 20010608 A 5330 6545773 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKS AT LH WINDOW CUTOUTS # 1 THRU # 10 & # 24 THRU # 30. REPAIRED SKIN PER BFG ER. 2 L 7 2 4F A16WE 2001061800071 20010618 00071 NM 2001 6 18 2001UALA00790 1 20010521 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 CORROSION INSIDE STRINGER 33R BETWEEN FRAME STA 478-500 RT. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REPAIRED STRINGER AS PER SRM 53-00-03 AND 51-40-2. 2 L 7 2 4F 4 F RT A1NM E3NE 2001061800072 20010618 00072 NM 2001 6 18 VNAA0106002 1 20010603 A 3300 BULB DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA O OTHER O OTHER DE DESCENT 1 GL 07 442JS 3060 DURING DESCENT, THE CREW RECEIVED NO GEAR DOWN INDICATION FOR THE NOSE GEAR. THE CREW REFERENCED THE QUICK REFERENCE HA NDBOOK. THE CREW DECLARED A EMERGENCY AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NOS E GEAR INDICATION BULB IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND TH E AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001061800073 20010618 00073 NM 2001 6 18 2001UALA00794 1 20010521 A 5414 SKIN BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE NR 1 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 NR 1 ENG PYLON LT OUTBOARD SIDE, PANEL 436BL CUTOUT IS CRACKED AT FWD UPPER FASTENER HOLE. SUPPLEMENTAL DATA UPDATE MAJO R REPAIR ACCOMPLISHED. REPAIRED SKIN PER SRM 54-53-97. 2 L 7 2 4F 4 F RT A1NM E3NE 2001061800074 20010618 00074 NM 2001 6 18 VNAA0106006 1 20010526 A 2700 001A554A0000018 RUDDER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA O OTHER O OTHER DE DESCENT 1 GL 07 461PS 12915 3075 THIS IS A CONTINUATION ODR FOR ODR VNAA0105018. MAINTENANCE INSPECTED AND REPLACED THE RUDDER IN ACCORDANCE WITH DORNI ER MAINTENANCE MANUAL 27-00-00. OPERATIONAL TESTS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001061800075 20010618 00075 EU 2001 6 18 2001UALA00798 1 20010402 A 2822 PUMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CENTER TANK BURNED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 418UA 485 FOUND CONNECTOR FOR NR 1 CENTER TANK BOOST PUMP BURNED AND DAMAGED. 2 L 7 2 4F 4 F RT A28NM E40NE 2001061800076 20010618 00076 NM 2001 6 18 VNAA0106010 1 20010611 A 2600 SD947022 DETECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE AFT FAILED A VNAA O OTHER N FALSE WARNING CL CLIMB 1 GL 07 457PS 857 3048 DURING CLIMB OUT OF PIT, THE CREW RECEIVED A RED WARNING PANEL INDICATION OF A CARGO FIRE. THE CREW WENT THROUGH THE QU ICK REFERENCE PROCEDURES AND RETURNED TO PIT. THE CREW HAD DECLARED AN EMERGENCY AND THE AIRCRAFT WAS EVACUATED ON THE RUNWAY, THERE WAS A ORDERLY AND NON INJURY EVACUATION. MAINTENANCE INSPECTED AND REPLACED THE CARGO FIRE DETECTOR IN AC CORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS FERRIED TO DA Y WHERE MAINTENANCE INSPECTED AND REPLACED THE CARGO FIRE BOTTLES IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00 . OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001061800077 20010618 00077 NE 2001 6 18 CA010529002 2 20010504 A 7240 COMBUSTION LINER PWA PT6A67B PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL CERAMIC COATING FAILED W K NONE O OTHER DE DESCENT 1 CA 3561 3561 PCEPR0089 (CAN) SPARKS OBSERVED COMING FROM ENGINE EXHAUST STACKS DURING APPROACH. ENGINE BORESCOPE INSPECTION CARRIED OUT WITH AS SISTANCE OF PRATT & WHITNEY FIELD REP. EVIDENCE OF CERAMIC COATING IMPACT ON TURBINE BLADES. SUSPECT SPARKS WERE CAUSED BY CERAMIC COATING BREAKING AWAY FROM COMBUSTION LINER. NO OTHER DEFECTS FOUND. . . 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001061800078 20010618 00078 NM 2001 6 18 2001UALA00800 1 20010523 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 BS 188 FUSELAGE FRAME CRACKED AT WL 207, STR 17L. ACCOMPLISHED DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001061800079 20010618 00079 NM 2001 6 18 2001UALA00801 1 20010523 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 393UA 24668 BS 188 RT FUSE FRAME CRACKED AT STR 17R, WL 207 IN RADIUS. ACCOMPLISHED DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001061800080 20010618 00080 NM 2001 6 18 2001UALA00802 1 20010523 A 5320 WEB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 FUSELAGE WEB IS CRACKED AT BS180, STR 17R, WL 207. ACCOMPLISHED WEB REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001061800081 20010618 00081 NM 2001 6 18 2001UALA00803 1 20010523 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 LT FWD EXTERIOR SKIN PITTED AT BS 223, STR 22L. ACCOMPLISHED DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001061800082 20010618 00082 NM 2001 6 18 2001UALA00804 1 20010523 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 LT EXT SKIN DENTED BEYOND LIMITS AT BS 470, STR 19L. ACCOMPLISHED DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001061800083 20010618 00083 NM 2001 6 18 2001UALA00805 1 20010523 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 CARGO DOOR LOWER CUTOUT VERTICAL WEB HAS EXCESSIVE MATERIAL LOSS AT BS 794 TO BS 847. REPLACED VERTICAL WEB. MAJOR REP AIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001061800084 20010618 00084 NM 2001 6 18 2001UALA00806 1 20010523 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 FUSELAGE STRINGER 14L IS CRACKED AT BS 990. REPAIRED STRINGER. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001061800085 20010618 00085 NM 2001 6 18 AWXA0001859 1 20010615 A 5312 65163007 WEB BOEING 737 7373G7 1384595 NM A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 305AW 24012 d: upom removal of strap HFEC Indicates crack .7" WL 212 RBL 6.8 on BS178 Blkhd web fwd facec: repaired IAW B737-300 SrM 53-10-08 Pg 287-298 2 L 7 2 4F RT A16WE 2001061800086 20010618 00086 NM 2001 6 18 AWXA0001861 1 20010615 A 5312 65163007 WEB BOEING 737 7373G7 1384595 NM A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 305AW 24012 d: upom removal of strap HFEC Indicates crack .7" WL 212 RBL 6.8 on BS178 Blkhd web fwd facec: repaired IAW B737-300 SrM 53-10-08 Pg 287-298 2 L 7 2 4F RT A16WE 2001061800087 20010618 00087 NM 2001 6 18 AWXA0001866 1 20010615 A 5312 65163007 WEB BOEING 737 7373G7 1384595 NM CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 305AW 24012 d: upom removal of strap HFEC Indicates crack .7" WL 212 RBL 6.8 on BS178 Blkhd web fwd facec: repaired IAW B737-300 SrM 53-10-08 Pg 287-298 2 L 7 2 4F RT A16WE 2001061800088 20010618 00088 NM 2001 6 18 AWXA0001872 1 20010615 A 5330 6552988 SKIN BOEING 737 7373G7 1384595 NM CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 305AW 24012 d: upom removal of strap HFEC Indicates crack .7" WL 212 RBL 6.8 on BS178 Blkhd web fwd facec: repaired IAW B737-300 SrM 53-10-08 Pg 287-298 2 L 7 2 4F RT A16WE 2001061800089 20010618 00089 NM 2001 6 18 AWXA0001873 1 20010615 A 5311 6546539 FRAME BOEING 737 7373G7 1384595 NM CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 305AW 24012 d: upom removal of strap HFEC Indicates crack .7" WL 212 RBL 6.8 on BS178 Blkhd web fwd facec: repaired IAW B737-300 SrM 53-10-08 Pg 287-298 2 L 7 2 4F RT A16WE 2001061800090 20010618 00090 NM 2001 6 18 AWXA0001862 1 20010615 A 5312 65163007 WEB BOEING 737 7373G7 1384595 NM CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 305AW 24012 d: upom removal of strap HFEC Indicates crack .7" WL 212 RBL 6.8 on BS178 Blkhd web fwd facec: repaired IAW B737-300 SrM 53-10-08 Pg 287-298 2 L 7 2 4F RT A16WE 2001061800091 20010618 00091 NM 2001 6 18 AWXA0001860 1 20010615 A 5312 65163007 WEB BOEING 737 7373G7 1384595 NM CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 305AW 24012 d: upom removal of strap HFEC Indicates crack .7" WL 212 RBL 6.8 on BS178 Blkhd web fwd facec: repaired IAW B737-300 SrM 53-10-08 Pg 287-298 2 L 7 2 4F RT A16WE 2001061800092 20010618 00092 NM 2001 6 18 AWXA0001863 1 20010615 A 5312 6545409245 WEB BOEING 737 7373G7 1384595 NM CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 305AW 24012 d: upom removal of strap HFEC Indicates crack .7" WL 212 RBL 6.8 on BS178 Blkhd web fwd facec: repaired IAW B737-300 SrM 53-10-08 Pg 287-298 2 L 7 2 4F RT A16WE 2001061800093 20010618 00093 NM 2001 6 18 AWXA0001864 1 20010615 A 5315 BEAM BOEING 737 7373G7 1384595 NM CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 305AW 24012 d: upom removal of strap HFEC Indicates crack .7" WL 212 RBL 6.8 on BS178 Blkhd web fwd facec: repaired IAW B737-300 SrM 53-10-08 Pg 287-298 2 L 7 2 4F RT A16WE 2001061800094 20010618 00094 NM 2001 6 18 2001UALA00807 1 20010523 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 317UA 23949 CABIN FLOORBEAM CORRODED AROUND NUT PLATE HOLE AT BS 294, RBL 21. INSTALLED STRAP DOUBLER. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001061800095 20010618 00095 NM 2001 6 18 2001UALA00808 1 20010523 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 317UA 23949 FLOOR SUPPORT INTERCOSTAL CRACKED THRU UPPER CHORD FASTENER HOLE AT BS 360, BL 0. REPLACED INTERCOSTAL. MAJOR REPAIR A CCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001061800097 20010618 00097 NM 2001 6 18 2001UALA00810 1 20010508 A 2120 UNKNOWN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN ODOR A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 658UA 27113 OIL ODOR IN CABIN AFTER RT ENGINE START. 2 L 7 2 4F 4 F RT A1NM E24NE 2001061800098 20010618 00098 NM 2001 6 18 2001UALA00813 1 20010524 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 CABIN FLOORBEAM UPPER T-CAP DAMAGED AT BS 1016, RBL 11. REPLACED UPPER T-CAP. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001061800099 20010618 00099 NM 2001 6 18 2001UALA00814 1 20010524 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 317UA 23949 AFT PIT FRAME DENTED AT BS 767, ABOVE STR 24L. REPAIRED WITH FRAME DOUBLER. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001061800100 20010618 00100 NM 2001 6 18 2001UALA00815 1 20010524 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 317UA 23949 FRAME WEB HAS EXCESSIVE MATERIAL LOSS AT BS 500, BL 0, WL 151. ACCOMPLISHED DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001061800101 20010618 00101 NM 2001 6 18 2001UALA00816 1 20010524 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 318UA 23950 AFT PRESSURE BULKHEAD WEB IS GOUGED AT BS 1016, WL 259, RBL 13. ACCOMPLISHED DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED . 2 L 7 2 4F 4 F RT A16WE E2GL 2001061800102 20010618 00102 NM 2001 6 18 2001UALA00818 1 20010524 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 615UA 21876 BS 434 STRINGER 37L - 38L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANC E WITH BAC DRAWINGS 140T2102 AND 143T1001. 2 L 7 2 4F 4 F RT A1NM E3NE 2001061800103 20010618 00103 NM 2001 6 18 2001UALA00824 1 20010521 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 AFT PIT STRINGER 34L BS 1329 - 1362 CORRODED.SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPAIRED STRINGER PER S RM 53-00-03 AND 51-20-2. 2 L 7 2 4F 4 F RT A1NM E3NE 2001061800104 20010618 00104 NM 2001 6 18 2001UALA00831 1 20010525 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 511UA 24799 RT CREASE BEAM CORRODED, STA 1125. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW CREASE BEAM WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2001061800105 20010618 00105 NM 2001 6 18 2001UALA00832 1 20010525 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 511UA 24799 FRAME DENTED STA 640 STR 18L. 2 L 7 2 4F 4 F RT A2NM E17NE 2001061800106 20010618 00106 NM 2001 6 18 2001UALA00834 1 20010525 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 511UA 24799 FRAME DAMAGED STA 1480, BETWEEN STR 26L AND 27L. 2 L 7 2 4F 4 F RT A2NM E17NE 2001061800107 20010618 00107 NM 2001 6 18 2001UALA00838 1 20010521 A 5330 SKIN BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 LOWER FUSELAGE SKIN HAS HOLE AT STA 380, BL 0. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED SKIN REPAIR PER SRM 53-00-01, FIG 214, AND SRM 51-40-2. 2 L 7 2 4F 4 F RT A1NM E3NE 2001061800108 20010618 00108 NM 2001 6 18 2001UALA00839 1 20010511 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 368 STR 38R TO 37R SHEAR TIE CORRODED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001061800109 20010618 00109 NM 2001 6 18 2001UALA00840 1 20010511 A 5320 STRINGER CLIP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 347 LBL 5 STR CLIP CRACKED.SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED CLIP IN ACCOR DANCE WITH BAC DRAWING 141T1221 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001061800110 20010618 00110 SO 2001 6 18 ASOA01056 1 20010516 A 7900 3022375 GARLOCK SEAL EMB 120 EMB120 3260201 SO ACCY GEAR BOX LEAKING A ASOA K NONE K FLUID LOSS CR CRUISE 1 SO 11 245AS 120075 FLT 4857 - DURING FLIGHT FROM DFW TO ICT, PASSENGER REPORTED SEEING FLUID LEAKING OUT OF THE LEFT ENGINE. THE CREW VERI FIED THE LEAK AND DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY IN ICT. MAINTENANCE INSPECTED AIRCRAFT AND FOUND OIL L EAKING FROM THE DRAIN TUBE FOR THE STARTER GENERATOR. MAINTENANCE REMOVED AND REPLACED THE STARTER GENERATOR GARLOCK SE AL. OPS AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001061800111 20010618 00111 NM 2001 6 18 UIEA01055 1 20010530 A 5400 65B9405310 DOUBLER BOEING 747 7472D7B 1384803 NM WORN A UIEA O OTHER O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 DURING INSPECTION OF NR 3 PYLON ACCESS PLATE CUTOUT (473AR) NAC STATION 290 WL 145, THE CONTACT AREA OF THE INNER SKIN T O LATCHES WAS FOUND WORN (THREE PLACES). AREAS TRIMMED OUT. HFEC INSPECTED AREAS FOR CRACKS, NONE FOUND. FABRICATED A ND INSTALLED CRES-STEEL WEAR PLATES IN THE AREAS OF THE LATCH TO SKIN CONTACT SURFACES PER BOEING TELEX. AREA TO BE VIS UALLY REINSPECTED AT SUBSEQUENCE C-CHECKS NOT TO EXCEED 18 MONTHS. (M) 2 L 7 4 4F RT A20WE 2001061800112 20010618 00112 NM 2001 6 18 UIEA01056 1 20010530 A 5300 65B1059545 FITTING BOEING 747 7472D7B 1384803 NM CORRODED A UIEA O OTHER O OTHER IN INSP/MAINT 1 EA 15 528MC 65332 12777 22472 DURING INSPECTION OF REMOVED LANDING GEAR FOUND CORROSION PITTING ON THE INBOARD TRUNNION SUPPORT BUSHING CAP OF THE LEF T BODY LANDING GEAR EXCEEDING SRM LIMITS. CORROSION CLEANED UP BY BLENDING AFFECTED AREAS. AREAS PLOTTED, MEASURED AND TREATED PER STANDARD SRM PRACTICES. GEAR REINSTALLED. DATA SENT TO BOEING FOR APPROVAL. REWORK CONSIDERED A PERMANEN T REPAIR PER BOEING WITH NO REPETITIVE INSPECTIONS REQUIRED. (M) 2 L 7 4 4F RT A20WE 2001061800113 20010618 00113 SO 2001 6 18 ASOA01058 1 20010522 A 3350 MS277892K SWITCH EMB 120 EMB120 3260201 SO CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 237AS 120051 ON GROUND IN ATL, CREW REPORTED EMERGENCY LIGHTS WOULD NOT COME ON OR TEST. MAINTENANCE INSPECTED AND FOUND SWITCH AT F LIGHT ATTENDANT STATION INOPERATIVE. MAINTENANCE REMOVED AND REPLACED SWITCH. OPERATIONAL CHECK OF LIGHTS OK. AIRCRAF T RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001061800114 20010618 00114 EU 2001 6 18 ASOA01062 1 20010527 A 3350 3012000 BATTERY PACK AEROSP ATR72 ATR72 EU CABIN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 635AS 372 ON GROUND IN ATL, CAPTAIN REPORTS RIGHT FRONT EMERGENCY EXIT LIGHT IS OUT. MAINTNANCE REMOVED AND REPLACED EMERGENCY EX IT LIGHT ON THE RIGHT SIDE AND THE BATTERY PACK AT 43VU. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT 2001061800115 20010618 00115 NM 2001 6 18 USAA010555 1 20010518 A 5300 DOUBLER BOEING 737 737201 1384454 NM BS 676 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND DOUBLER CRACKED 2 INCHES, BS 676, BETWEEN LBL 24 AND RBL 24, WL 206. INSTALLED RE-INFORCEMENT CHANNELS PER EO 5791G632. (M) 2 L 7 2 4F A16WE 2001061800116 20010618 00116 NM 2001 6 18 USAA010553 1 20010518 A 5300 FRAME BOEING 737 737201 1384454 NM BS 440 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND FRAME CRACKED .375 INCH, LATERALLY THROUGH EDGE OF FRAME BS 440, LBL 21. INSTALLED FORMED FRAME REPAIR DOUB LER PER SRM 51-40-3, FIG 1. (M) 2 L 7 2 4F A16WE 2001061800117 20010618 00117 NM 2001 6 18 USAA010552 1 20010518 A 5300 FRAME BOEING 737 737201 1384454 NM BS 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND FRAME CRACKED .25 INCH, BS 639, STRINGER 17R. INSTALLED REPAIR DOUBLER PER SRM 51-40-2, FIG 1. (M) 2 L 7 2 4F A16WE 2001061800118 20010618 00118 WP 2001 6 18 USAA010587 1 20010530 A 5300 FRAME DOUG DC9 DC981 3022081 WP BS 1437 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 812US 53328 48092 PIT - FOUND FRAME CRACKED .5 INCH, STATION 1437 AT L16R. STOP DRILLED CRACK, INSTALLED DOUBLER PER TYP REPAIR 53-01. ( M) 2 L 7 2 4F A6WE 2001061800119 20010618 00119 EA 2001 6 18 ASOA01055 1 20010514 A 7900 MS938708 O-RING CNDAIR CL600 CL6002B19 EA BROKEN A ASOA A E UNSCHED LANDING ENGINE SHUTDOWN J K Y WARNING INDICATION FLUID LOSS ENGINE STOPPAGE CL CLIMB 1 SO 11 821AS 7194 UPON CLIMB-OUT FROM ATL, PASSING THROUGH 17,000 FT, CAPTAIN RECEIVED RIGHT ENGINE OIL PRESSURE WARNING. OIL PRESSURE WA S READING 23 PSI AND THE TEMPERATURE WAS 98 DEGREES. CAPTAIN SECURED THE ENGINE IN FLIGHT BY FOLLOWING EMERGENCY AND AB NORMAL CHECKLISTS. AIRCRAFT RETURNED AND LANDED SAFELY IN ATL. MX INSPECTED RIGHT ENGINE AND FOUND UPPER UNION ON B SU MP SCAVENGE PUMP UPPER RIGHT INSTALLED WITH A BROKEN SEAL. MAINTENANCE REMOVED AND REPLACED UNION O-RING AND REINSTALLE D UNION. THE RIGHT ENGINE WAS GROUND RAN AT HIGH POWER SETTINGS FOR 30 MINUTES. NO LEAKS OR DEFECTS WERE NOTED. AIRCR AFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001061800120 20010618 00120 NM 2001 6 18 UIEA01057 1 20010530 A 5310 SKIN BOEING 747 7472D7B 1384803 NM BS 1814 CRACKED A UIEA O OTHER O OTHER IN INSP/MAINT 1 EA 15 528MC 65332 12777 22472 DURING HFEC INSPECTION PER SB 747-53A2488 FOUND LOWER LOBE AFT CARGO COMPT DOOR UPPER FORWARD CUTOUT WITH TWO CRACK INDI CATIONS, ONE FROM FASTENER HOLE TO RADIUS CUTOUT, THE OTHER 7MM LONG FROM FASTENER HOLE. AREA TRIMMED OUT. FILLER AND STACK DOUBLER FABRICATED AND INSTALLED PER STANDARD SRM PRACTICES WITH 300 CYCLE REPETITIVE THEREAFTER. (M) 2 L 7 4 4F RT A20WE 2001061800121 20010618 00121 WP 2001 6 18 AALA20010360 1 20010227 A 5310 ANGLE DOUG DC10 DC1010 3022110 WP FS 879-824 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 126AA 46947 TUL - FOUND CORROSION ON J-ANGLE AT STATION 879 AND STRINGER 52 AND CORROSION AT STATION 52 AND STRINGER 868-824. REPLA CES SECTION OF J-ANGLE AND SECTION OF STRINGER PER SRM 53-00-01 VOL I AND SRM 53-10-00. (M) 2 L 7 3 4F A22WE 2001061800122 20010618 00122 EU 2001 6 18 USAAF01027 1 20010522 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 898US 11398 IND - THE AFT CABIN LOW LEVEL AND THE LOWER WING TO BODY EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERY IN A POWER SUPPLY AT ROW 16. OPS CHECKED OK. (M) 2 L 7 2 4F RT 2001061800123 20010618 00123 NM 2001 6 18 2001UALA00841 1 20010511 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 325 RBL 4 SHEAR TIE CORRODED.SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPLACED SHEARTIE IN ACCORDANCE WITH SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001061800124 20010618 00124 NM 2001 6 18 2001UALA00843 1 20010511 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 610 STR 39L-39R SHEAR TIE CORRODED.SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAI R IN ACCORDANCE WITH BAC DRAWING 140T2102 AND SRM 51-40-02 2 L 7 2 4F 4 F RT A1NM E3NE 2001061800125 20010618 00125 NM 2001 6 18 2001UALA00848 1 20010511 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 347 STR 38R-39R SHEAR TIE CORRODED.SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAI R IN ACCORDANCE WITH BAC DRAWING 141T1221 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001061800126 20010618 00126 NM 2001 6 18 2001UALA00850 1 20010511 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 434 STR 35R-34R SHEAR TIE CORRODED.SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAI R IN ACCORDANCE WITH BAC DWG 140T2102 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001061800128 20010618 00128 NM 2001 6 18 2001UALA00852 1 20010511 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 456 STR 39L-38L SHEAR TIE CORRODED.SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAI R IN ACCORDANCE WITH BAC DRAWING 140T2102-307. 2 L 7 2 4F 4 F RT A1NM E3NE 2001061800129 20010618 00129 WP 2001 6 18 ABXA010238 1 20010525 A 3260 H141003 DOWNLOCK SWITCH DOUG DC8 DC863 302198A WP RT MLG FAILED A ABXA K NONE N FALSE WARNING AP APPROACH 1 GL 23 822AX 46079 RIGHT MAIN GEAR DOWN GREEN LIGHT DID NOT COME ON, ON GEAR EXTENSION. REPLACED RIGHT MAIN GEAR LOCK SWITCH PER DC-8 MM 3 2-60-00. 2 L 7 4 4F 4A25 2001061800130 20010618 00130 WP 2001 6 18 ABXA010241 1 20010523 A 5730 SKIN DOUG DC8 DC863 302198A WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 LEFT WING UPPER WING PLATING CRACKED AT XCW 69.5 AT TRAILING EDGE. 2 L 7 4 4F 4A25 2001061800131 20010618 00131 WP 2001 6 18 ABXA010242 1 20010525 A 5320 9754949 ATTACH ANGLE DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 AFT CARGO PIT AT FS 1260 ABOVE LONGERON 35 RIGHT, FLOOR ATTACH ANGLE CRACKED. REPAIRED AREA IAW DAC DWG 9754949 AND DC8 SRM 51. 2 L 7 4 4F 4A25 2001061800132 20010618 00132 WP 2001 6 18 ABXA010243 1 20010525 A 5240 5755980 SEAL BRACKET DOUG DC8 DC863 302198A WP SERVICE DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 RIGHT (TYPE I) FORWARD DOOR, FORWARD LOWER CORNER SEAL DEPRESSION CRACKED. REPAIRED IAW DC8 SRM 52-2-2. 2 L 7 4 4F 4A25 2001061800133 20010618 00133 WP 2001 6 18 MWEA010987 1 20010617 A 2133 20219741 ACTUATOR DOUG DC9 DC982 3022082 WP TAILCONE INOPERATIVE A MWEA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 GL 31 810ME 48072 ON CLIMB 16,000 MSL, UNABLE TO MAINTAIN CABIN PRESSURE BOTH PACKS SHOWED NORMAL, CONTRO VALVE CLOSED, PRIMARY AND STANDB Y CONTROLLERS SHOW FAILED. -- PERFORMED BITE AND LOGIC CHECK ON CONTROLLERS, FOUND GOOD. REPLACED OUTFLOW VALVE ACTUAT OR. 2 L 7 2 4F A6WE 2001061800134 20010618 00134 WP 2001 6 18 ABXA010244 1 20010525 A 5320 5616520243 WEB DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 FORWARD LOWER CARGO COMPARTMENT (C2) DOOR TORQUE BOX WEB CRACKED/CORRODED AT FASTENER HOLE, STA 560 LONGERON 34 RIGHT. REPAIRED IAW DC8 SRM 51. 2 L 7 4 4F 4A25 2001061800135 20010618 00135 WP 2001 6 18 ABXA010245 1 20010525 A 5751 5705334 ANGLE DOUG DC8 DC863 302198A WP AILERON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 RIGHT INBOARD AILERON ON OUTBOARD TRAILING EDGE CRACKED. REPAIRED AREA IAW DAC DWG 5705334, DC8 SRM 51-1-8, 51-1-24, AN D 51-1-21. 2 L 7 4 4F 4A25 2001061800136 20010618 00136 WP 2001 6 18 ABXA010246 1 20010525 A 5320 5779929 INTERCOSTAL DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 AFT LOWER CARGO STA 980 LONGERON 35 LEFT INTERCOSTAL LOWER FLANGE CORRODED AT FASTENERS. REMOVED CORROSION IAW DC8 SRM 51-1-8. FABBED NEW INTERCOSTAL AND INSTALLED IAW DAC DWG 5779929, DC8 SRM 51-1-8, AND 51-1-20. 2 L 7 4 4F 4A25 2001061800137 20010618 00137 WP 2001 6 18 MWEA010988 1 20010618 A 2730 5910414504 TAB DOUG DC9 DC932 3022066 WP RIGHT ELEVATOR DELAMINATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 RIGHT ELEVATOR GEARED TAB HAS TWO AREAS OF DELAMINATION ON PREVIOUS REPAIR. 1.5" BY 6.0" AREA ON TOP AND 4.0" BY 2.5" AR EA ON BOTTOM. -- REMOVED DELAMINATED REPAIR, BONDED ON NEW REPAIR. 2 L 7 2 4F A6WE 2001061800138 20010618 00138 WP 2001 6 18 MWEA010989 1 20010618 A 5310 49559471 SKIN DOUG DC9 DC932 3022066 WP FWD PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 EXTERIOR SKIN ABOVE FORWARD PAX DOOR HOLD OPEN HOOK CUT OUT HAS TWO SMALL CRACKS. -- TRIMMED, LOCATED AND DRILLED PLAT E AND DOUBLERS, INTSTALLED DOUBLERS, PAN, PIN. 2 L 7 2 4F A6WE 2001061800139 20010618 00139 WP 2001 6 18 MWEA010990 1 20010618 A 5310 99579457 BRACKET DOUG DC9 DC932 3022066 WP FWD CARGO DOOR ELONGATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 ATTACH BRACKET HOLES ELONGATED FORWARD AND AFT, FORWARD CARGO DOOR HINGES ATTACH TO FUSELAGE. -- FABRICATED AND INSTAL LED DOUBLERS. 2 L 7 2 4F A6WE 2001061800140 20010618 00140 WP 2001 6 18 MWEA010991 1 20010618 A 5310 5912285 FRAME DOUG DC9 DC932 3022066 WP WINDOW 9L GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 WINDOW 9L INNER WINDOW FRAME HAS SEVERAL MODERATE GOUGES/TOOL MARKS IN RADIUS OF FRAME BOTH FORWARD AND AFT SIDES. -- BLENDED TOOL MARKS, LOCATED AND DRILLED NEW INNER WINDOW FRAME, INSTALLED WINDOW RETAINER. 2 L 7 2 4F A6WE 2001061800141 20010618 00141 WP 2001 6 18 MWEA010992 1 20010618 A 5310 59108203 SEAT TRACK DOUG DC9 DC932 3022066 WP STATION 200 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 #3 SEAT TRACK CORRODED AT FORWARD END APPROXIMATELY STATION 200. -- REMOVED CORROSION, REMOVED DAMAGED SECTION OF SEAT TRACK, LOCATED AND DRILLED AND INSTALLED NEW SEAT TRACK. 2 L 7 2 4F A6WE 2001061800142 20010618 00142 WP 2001 6 18 MWEA010993 1 20010618 A 5310 99581561 FRAME DOUG DC9 DC932 3022066 WP WINDOW 9L DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 EXTERIOR FUSELAGE HAS LIGHTENING STRIKES AT WINDOW 9L. -- BLENDED OUT DAMAGED AREAS, LOCATED AND DRILLED DOUBLER, INST ALLED REPAIR AT WINDOW. 2 L 7 2 4F A6WE 2001061800143 20010618 00143 WP 2001 6 18 MWEA010994 1 20010618 A 5210 59100817 SKIN DOUG DC9 DC932 3022066 WP FWD PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 FORWARD PAX DOOR SKIN HAS A SMALL CRACK AT THE LOWER SIDE OF THE HOLD OPEN HOOK CUT OUT. -- REMOVED DAMAGE, FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001061800144 20010618 00144 WP 2001 6 18 MWEA010995 1 20010618 A 2730 5918036519 SKIN DOUG DC9 DC932 3022066 WP STATION XHS 70 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 LEFT ELEVATOR UPGRADE REPAIR INSTALLED AT STATION XHS 70 TO SRM 55-03 FIGURE 14. -- REMOVED SKIN, FABRICATED NEW SKIN AND FINGER DOUBLER, INSTALLED SKIN. 2 L 7 2 4F A6WE 2001061800145 20010618 00145 WP 2001 6 18 ABXA010247 1 20010525 A 5320 3755843501 ANGLE DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 AFT LOWER CARGO Z-FITTING, STA 1180 LONGERON 34 - 33 RIGHT CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8. FABBED AND INSTALLED ANGLE IAW DC8 SRM 53-2-0. 2 L 7 4 4F 4A25 2001061800146 20010618 00146 WP 2001 6 18 ABXA010248 1 20010525 A 5320 3755843501 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 AFT LOWER CARGO STA 1160 LONGERON 36 - 35 RIGHT, Z-FITTING CORRODED. REPLACED CRACKED FITTING IAW DC8 SRM 53-2-0. 2 L 7 4 4F 4A25 2001061800147 20010618 00147 WP 2001 6 18 ABXA010249 1 20010525 A 5320 3755843501 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 AFT LOWER CARGO Z-FITTING, STA 1160 LONGERON 34 - 33 RIGHT, FLANGE CRACKED AT FASTENER HOLE. REPAIRED IAW DC8 SRM 51, A ND DC8 SRM 53. 2 L 7 4 4F 4A25 2001061800148 20010618 00148 WP 2001 6 18 ABXA010250 1 20010525 A 5320 37558412 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 AFT CARGO PIT AT FS 1230 BETWEEN LONGERON 33 - 34 RIGHT, Z-FITTING CORRODED. REPLACED Z-FITTING IAW DC8 SRM 53-2-0, AND DC8 SRM 51. 2 L 7 4 4F 4A25 2001061800149 20010618 00149 WP 2001 6 18 ABXA010251 1 20010525 A 5320 37536452 SUPPORT FITTING DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 TAILSKID RIGHT UPPER SUPPORT FITTING CORRODED AROUND (3) OUTBOARD FASTENERS ON UPPER SIDE OF FITTING AT FS 1766 RBL 8. REPLACED RIGHT TAILSKID UPPER SUPPORT FITTING IAW DC8 SRM 51-1-2, AND DWG 5753522. 2 L 7 4 4F 4A25 2001061800150 20010618 00150 NM 2001 6 18 PCAA0106052 1 20010614 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM CARGO BAY FALSE ACTIVATION A PCAA O OTHER N FALSE WARNING AP APPROACH 1 EA 13 834EX 11003 859 285 BOS- FLIGHT#3898. CREW REPORTED SMOKE IN BAGBAY LIGHT ILLUMINATED THEN WENT OUT. MAINTENANCE ISOLATED PROBLEM TO #2 SMOK E DETECTOR.#2 SMOKE DETECTOR REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001061800151 20010618 00151 WP 2001 6 18 ABXA010252 1 20010525 A 5320 3755844IN FITTING DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 AFT CARGO AT FS 1150 BETWEEN LONGERON 31 LEFT TO 32 LEFT Z-FITTING WAS CRACKED. REMOVED AND REPLACED Z-FITTING IAW DC-8 SRM 53-2-0, 51-1-8, AND 51-1-20D. 2 L 7 4 4F 4A25 2001061800152 20010618 00152 WP 2001 6 18 ABXA010253 1 20010525 A 5320 3755841501 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 AFT CARGO AT FS 1180 BETWEEN LONGERON 33 RIGHT - 34 RIGHT Z-FITTING WAS CORRODED. REMOVED AND REPLACED Z-FITTING IAW DC -8 SRM 51-1-20D, 53-2-0, AND 51-1-8. 2 L 7 4 4F 4A25 2001070200083 20010702 00083 WP 2001 7 2 ABXA010293 1 20010423 A 7120 BOLT DOUG DC8 DC863 302198A WP NR 2 ENGINE SHEARED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 NR 2 ENGINE AFT OUTBOARD ARM BOLT SUPPORT ASSEMBLY OUTBOARD END SHEARED OFF. 2 L 7 4 4F 4A25 2001061800155 20010618 00155 EU 2001 6 18 AALA20010324 1 20010501 A 5320 SILL AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3075A 606 TUL - FOUND DOOR SILL BEAM CORRODED ON UPPER LIP AT FRAME 60. REMOVED CORRODED AREA AND REPAIRED PER SRM 53-17-18-2. ( M) 2 L 7 2 4F RT A35EU 2001061800156 20010618 00156 WP 2001 6 18 AALA20010425 1 20010212 A 5320 SPLICE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 126AA 46947 TUL - FOUND CORROSION ON STRINGER SPLICE LN 50L STATION 755 TO 775 E-58 0193619, 0193621, 0193622, 0193632. REPAIRED PE R ESO 7349 DATED 3-7-01. (M) 2 L 7 3 4F A22WE 2001061800157 20010618 00157 NM 2001 6 18 AALA20010704 1 20010403 A 2421 GEN5103 IDG BOEING 767 767223 1385123 NM LT ENGINE FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 321AA 22322 LHR - FLT 121 - LEFT GENERATOR FAILED ONE HOUR INTO FLIGHT ATTEMPTED ONE RESET UNABLE TO RESET STARTED APU. REPLACED LE FT GCU AND LEFT IDG. ACCOMPLISHED ENGINE RUN AND LEAK CHECK ALL OPS NORMAL. (M) 2 L 7 2 4F RT A1NM 2001061800158 20010618 00158 NM 2001 6 18 AALA20010705 1 20010403 A 2421 HARNESS BOEING 767 767223 1385123 NM IDG CONTAMINATED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 321AA 22322 LHR - FLT 121 - LEFT GENERATOR FAILED 10 MINUTES AFTER TAKEOFF, UNABLE TO RESET. STARTED APU RETURNED TO LHR TAXI TIME PRIOR TO TAKEOFF WAS 18 MIN. LEFT IDG/GCU WIRING TROUBLESHOOT IAW B767 FIM 24-20-00-1. ALL FOUND TO BE OK. LEFT IDG E NGINE HARNESS INSPECTED FOR CHAFING. ALL OK. IDG HARNESS FOUND TO HAVE OIL INGRESS FROM PREVIOUS OIL LEAK. IDG HARNES S AND C/P CLEANED ALL OIL REMOVED. C/P RECONNECTED. LEFT ENGINE GROUND RUN FOR 40 MINUTES WITH NUMEROUS ELECTRICAL LO AD CHANGES. ALL OPS AND IND NORMAL. NO REPEAT OF FAULT ON THE GROUND. (M) 2 L 7 2 4F RT A1NM 2001061800159 20010618 00159 NM 2001 6 18 AALA20010720 1 20010404 A 2612 901908 FIRE LOOP BOEING 767 767323 1385205 NM NR 1 ENGINE DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 355AA 24036 STL - FLT 19 - EN ROUTE JFK-LAX, DURING CRUISE DETECTED LEFT ENGINE FIRE LOOP 1 AND 2 ILLUMINATE. DIVERTED STL AND LAND ED WITHOUT FURTHER INCIDENT. REPLACED LEFT SIDE UPPER FIRE LOOP ASSEMBLY. ACCOMPLISHED FIRE LOOP OPERATIONAL CHECKS PE R THE MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001061800160 20010618 00160 EU 2001 6 18 AALA20010722 1 20010404 A 5320 4051445 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 33069 512 TUL - FOUND CORROSION ON LAVATORY SUPPORT TIE DOWN BETWEEN D/LT AND E/LT BETWEEN FRAME 72 AND 73. REMOVED LAV SUPPORT A ND INSTALLED NEW LAVATORY SUPPORT AND BETWEEN D/LT AND E/LT FROM FRAME 72-74, REF SRM 51-72-10-00. (M) 2 L 7 2 4F RT A35EU 2001061800161 20010618 00161 WP 2001 6 18 AALA20010765 1 20010409 A 5330 SKIN DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 127AA 46948 TUL - FOUND DEEP CORROSION ON INSIDE. MADE REPAIR PER RM 53-20-00 FIG 12. (M) 2 L 7 3 4F A22WE 2001061800162 20010618 00162 NM 2001 6 18 AALA20010772 1 20010410 A 2752 40863 MOTOR BOEING 727 727223 1384074 NM T/E FLAP LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 844AA 20985 BNA - FLT 844 - EN ROUTE RDU-DFW - LOST ALL HYDRAULIC FLUID FROM THE A-SYSTEM. DIVERTED BNA AND LANDED WITHOUT FURTHER INCIDENT. REPLACED HYDRAULIC PUMP AND FILTER ELEMENTS. REPLACED INBOARD TRAILING EDGE FLAP HYDRAULIC MOTOR. SYSTEM GR OUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001061800163 20010618 00163 WP 2001 6 18 AALA20010787 1 20010411 A 5310 DOOR FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 127AA 46948 TUL - FOUND CORROSION ON LOWER FORWARD CORNER OF DOOR JAMB FRAME AROUND NUT PLATE. REMOVED CORROSION PER SRM 51-21-01, VOL 2. INSTALLED REPAIR PER SRM 53-50-00 FIG 23. (M) 2 L 7 3 4F A22WE 2001061800164 20010618 00164 WP 2001 6 18 AALA20010793 1 20010416 A 5330 DOUBLER DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 127AA 46948 TUL - FOUND FINGER DOUBLER CORRODED. REPLACED FINGER DOUBLER PER SRM 53-00-01. (M) 2 L 7 3 4F A22WE 2001061800165 20010618 00165 WP 2001 6 18 AALA20010794 1 20010416 A 5320 FITTING DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 127AA 46948 TUL - FOUND ANTENNA SUPPORT FITTING CORRODED. REPLACED ANTENNA SUPPORT FITTING PER SRM 53-00-01 VOL 2. (M) 2 L 7 3 4F A22WE 2001061800166 20010618 00166 NM 2001 6 18 AALA20010795 1 20010411 A 2421 GEN5103 IDG BOEING 767 767323 1385205 NM LT ENGINE FAILED A AALA K NONE J WARNING INDICATION CR CRUISE 1 SW 21 383AN 26995 GRU - FLT 999 - LEFT GEN LIGHT FLICKERED ON/OFF FOR 1 HOUR BEFORE STAYING ON. DISCONNECTED GEN DRIVE. REMOVED AND REPL ACED LEFT IDG DUE NOTED OIL LEAKAGE AS PER MM. ACCOMPLISHED LEAKAGE AN DOPS TEST AS REQUIRED. OK FOR SERVICE. (M) 2 L 7 2 4F RT A1NM 2001061800167 20010618 00167 2001 6 18 AALA20010797 4 20010411 A 3460 COM7165 FMC BOEING 767 767323 1385205 NM E/E BAY FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 387AM 27184 DFW - FLT 48 - LT FMC FAIL MESSAGE APPEARED ON CLIMB-OUT. PULLED AND RESET FMC CB-E9 AS PER ABNORMAL PROCEDURE. NO EFF ECT SELECTED ALT AND FMC AND GOT DISPLAY BACK. REPLACED LT FMC COMPUTER. OPS CHECK OK AS PER MM 34-61-01-4. (M) 2 L 7 2 4F RT A1NM 2001061800168 20010618 00168 WP 2001 6 18 AALA20010799 1 20010410 A 5330 SKIN DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 127AA 46948 TUL - FOUND DRAIN HOLES CORRODED. FABRICATED DOUBLER AND INSTALLED PER SRM 51-21-01 VOL 2 AND ESO 7349 DATED 4-6-2001. (M) 2 L 7 3 4F A22WE 2001061800169 20010618 00169 WP 2001 6 18 AALA20010800 1 20010411 A 5312 AYB7105 CAP DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 127AA 46948 TUL 0 FOUND T-CAP CRACKED AT 39R STATION 1156 TOP FORWARD FASTENER HOLE IN PRESSURE BULKHEAD AFT LEG. INSTALLED NEW T-CA P PER ENGINEERING DRAWING SR10530073. (M) 2 L 7 3 4F A22WE 2001061800170 20010618 00170 WP 2001 6 18 AALA20010820 1 20010419 A 5347 CARGO TRACK DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 127AA 46948 TUL - FOUND CORROSION. REPLACED SECTION OF TRACK PER SRM 51-01-00-05. (M) 2 L 7 3 4F A22WE 2001061800171 20010618 00171 WP 2001 6 18 AALA20010821 1 20010419 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 127AA 46948 TUL - FOUND CORROSION ON BACKSIDE OF Z-ANGLE AT STATION 859 LEFT JUST FORWARD OF THE SLIDING GALLEY DOOR. BLENDED AREA SMOOTH, CLEANED, ALODINED, PRIMED AND PAINTED AREA PER ESO 7349 DATED 4-12-01. (M) 2 L 7 3 4F A22WE 2001061800172 20010618 00172 WP 2001 6 18 AALA20010822 1 20010418 A 5330 SKIN DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 127AA 46948 TUL - FOUND SURFACE CORROSION ON BOTTOM SURFACE OF CENTER WING BOX EXTERIOR IN LOWER BARREL STATION 1270 AFT SIDE OF BOX SPLICE BL LEFT 1 TO BL RIGHT 7. REMOVED CORROSION TREATED AND PRIMED AREA PER SRM 51-21-01 VOL 2. INSTALLED SHIM AND DOUBLER PER ESO 7349 DATED 04-02-01. (M) 2 L 7 3 4F A22WE 2001061800173 20010618 00173 WP 2001 6 18 AALA20010823 1 20010419 A 2131 21172803 CONTROLLER DOUG DC9 DC982 3022082 WP CABIN PRESSURE DEFECTIVE A AALA G O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 SW 21 468AA 49598 TUL - FLT 1704 - EN ROUTE ORD-EWR, AT 33,000 FEET, CREW REPORTED DROP IN ALTITUDE TO 10,000 FEET. DEPLOYED OXYGEN MASKS , AND LANDED EWR WITHOUT FURTHER INCIDENT. FERRIED AIRCRAFT TUL. REPLACED NR 1 CABIN PRESSURE CONTROLLER. SYSTEM GROU ND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001061800174 20010618 00174 NM 2001 6 18 AALA20010833 1 20010420 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 923AN 29524 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 13D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2001061800175 20010618 00175 WP 2001 6 18 AALA20010849 1 20010423 A 5730 SKIN DOUG DC10 DC1010 3022110 WP LT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 127AA 46948 TUL - FOUND CORROSION ON LOWER WING SKIN APPROX 18 INCHES AFT OF REAR SPAR AND 24 INCHES OUTBOARD OF LEFT MAIN GEAR TRUN NION. CORROSION REMOVAL REF SRM 51-21-01. ALODINED AND PAINTED PER SRM 51-21-01. REPAIRED COMPLETED PER ESO 7349/REPA IR NR 281571000. (M) 2 L 7 3 4F A22WE 2001061800176 20010618 00176 NM 2001 6 18 AALA20010863 1 20010426 A 3242 260881211 BRAKE ASSY BOEING 767 767323 1385205 NM MLG SEIZED A AALA K NONE A FLAME/FIRE LD LANDING 1 SW 21 395AN 29432 DFW - FLT 102 - EN ROUTE HNL-DFW, UPON LANDING DETECTED NR 1 WHEEL ASSEMBLY DRAG. LANDED DFW WITHOUT FURTHER INCIDENT. AT GATE ARRIVAL DETECTED FIRE AT NR 1 WHEEL ASSEMBLY CHOCKS. EXTINGUISHED FLAMES. REPLACED NR 1 TIRE ASSY DUE TO BRAK E SEIZURE. REPLACED NR 1 WHEEL BRAKE ASSY. PERFORMED INSPECTION OF THE MLG PER THE MM. NO DEFECTS NOTED. SYSTEM GROU ND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001061800177 20010618 00177 WP 2001 6 18 ABXA010254 1 20010525 A 5320 3755841501N FITTING DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 AFT CARGO AT FS 1200 BETWEEN LONGERON 33 RIGHT - 34 RIGHT Z-FITTING WAS CORRODED. REMOVED AND REPLACED Z-FITTING IAW DC -8 SRM 53-2-0, 51-1-8, AND 51-1-20D. 2 L 7 4 4F 4A25 2001061800178 20010618 00178 WP 2001 6 18 ABXA010255 1 20010525 A 5320 37558452N FITTING DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 AFT CARGO AT FS 1200, AT LONGERON 35 RIGHT Z-FITTING WAS CRACKED. REMOVED AND REPLACED Z-FITTING IAW DC-8 SRM 53-3-0, 5 3-2-0, 51-1-8, AND 51-1-20D. 2 L 7 4 4F 4A25 2001061800179 20010618 00179 NM 2001 6 18 CALA0100548 1 20010616 A 5320 CHANNEL BOEING 737 7373T0 1384582 NM STA 990 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16301 23352 INSPECTION FOUND HAT CHANNEL AND MOUNT FLANGE CORRODED AT STA 990, RBL 40. THE HAT CHANNEL AND MOUNT FLANGE WERE REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001061800180 20010618 00180 NM 2001 6 18 CALA0100551 1 20010617 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM STA 986.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16301 23352 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, LBL 48. THE TOP CAP OF FLOORBEAM WAS REPLACED IAW ECRA 5310-03851. 2 L 7 2 4F RT A16WE 2001061800181 20010618 00181 WP 2001 6 18 ABXA010256 1 20010525 A 5320 37558422 FITTING DOUG DC8 DC863 302198A WP FUSELAGE BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 AFT CARGO AT FS 1160, BETWEEN LONGERON 27 LEFT - 28 LEFT Z-FITTING ATTACHING FLANGES WERE MISSING. REPLACED Z-FITTING I AW DC-8 SRM 53-2-0, 51-1-8, 51-1-20D, 51-3-0, AND 51-1-21. 2 L 7 4 4F 4A25 2001061800182 20010618 00182 WP 2001 6 18 ZW0A0103701 1 20010618 A 3350 58222 BATTERY PACK DOUG DC9 DC983 3022083 WP SEE TEXT A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9303K 49529 THE EGRESS LIGHTS WERE OUT FROM STA 982 TO 1200, AND AFT OF THE OVERWING EMERGENCY EXIT. REPLACED THE BATTERY PACK AT S TATIONS 982, 991, AND 1057. CHECK-C 12-24-00 STL. --CLOSED- 2 L 7 2 4F RT A6WE 2001061800183 20010618 00183 WP 2001 6 18 ABXA010258 1 20010525 A 5320 575311337 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 UPPER SIDE OF LONGERON NR 24 FITTING CORRODED AT RIGHT MAIN LANDING GEAR WHEEL WELL, AT FORWARD AND AFT SIDE OF FS 920 B ATHTUB FITTING, AND FS 920 BATHTUB FITTING CORRODED ON AFT SIDE AT UPPER PRESSURE WEB. REPLACED BATHTUB FITTING IAW DC- 8 SRM 51-1-8, 51-1-21, 53-2-0, 51-2-0, 51-1-17, 51-1-20D, 51-3-0, AND DAC DWG 5802677. 2 L 7 4 4F 4A25 2001070200097 20010702 00097 WP 2001 7 2 ABXA010310 1 20010608 A 5313 LONGERON DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 AFT LOWER CARGO LONGERON 35 LEFT CORRODED AT STATION FS 1020. 2 L 7 4 4F 4A25 2001070200107 20010702 00107 WP 2001 7 2 ABXA010320 1 20010608 A 5320 57558422 FITTING DOUG DC8 DC863 302198A WP AFT CARGO CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 AFT CARGO AT FUSELAGE 1160 BETWEEN LONGERON 27 LEFT - 28 LEFT Z-FITTING WAS CORRODED. 2 L 7 4 4F 4A25 2001070300079 20010703 00079 WP 2001 7 3 ABXA010323 1 20010607 A 5511 SPAR DOUG DC8 DC863 302198A WP HORIZ STAB CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 LEFT HORIZONTAL STABILIZER LEADING EDGE LOWER SPAR XE 114 WAS CORRODED INSIDE AROUND A RIVET BUCKTAIL. 2 L 7 4 4F 4A25 2001070200086 20010702 00086 WP 2001 7 2 ABXA010296 1 20010606 A 5313 LONGERON DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 AFT FUSELAGE BETWEEN STATION 1680 TO 1667 LONGERON 22 LEFT WAS CORRODED. 2 L 7 4 4F 4A25 2001061800184 20010618 00184 WP 2001 6 18 ABXA010259 1 20010525 A 5720 SR070004 FITTING DOUG DC8 DC863 302198A WP LT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 LEFT WING REAR SPAR XRS 0 AFT FACE OF VERTICAL WEB HAD CORROSION OMITTING AROUND FASTENERS. REPAIRED AREA IAW DC-8 SRM 51, DAC DWG'S 4753127, 4652943, 4652944, 5751690, AND REA'S D857-40389, AND D857-40382MR. 2 L 7 4 4F 4A25 2001061800185 20010618 00185 WP 2001 6 18 ABXA010260 1 20010525 A 5720 36411171 FITTING DOUG DC8 DC863 302198A WP LT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 LEFT WING REAR SPAR SKI FITTING TO BOTTLE BOLT VERTICAL ATTACH FITTING HAD CORROSION AT LOWER SKI FITTING ATTACH AREA (P /N 3641117-1). REPAIRED AREA IAW DC-8 SRM 51. 2 L 7 4 4F 4A25 2001061800186 20010618 00186 WP 2001 6 18 ABXA010261 1 20010525 A 5313 3750545502 LONGERON DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 AFT LOWER CARGO STA 1050-1070 LONGERON 35 RIGHT, LONGERON AND SPLICE ASSEMBLY HAD CORROSION BETWEEN LONGERON SPLICE ASSE MBLY AND SKIN, CAUSING BULGE BETWEEN SKIN AND LONGERON. REPAIRED AREA IAW DC-8 SRM 53-2-0, 51-1-8, 51-20D, 51-1-21, 51- 3-0, AND DAC DWG 9758507, AND REA 853-40346. 2 L 7 4 4F 4A25 2001061800187 20010618 00187 WP 2001 6 18 ABXA010262 1 20010525 A 5320 3755845IN FITTING DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 AFT CARGO AT FS 1150 BETWEEN LONGERON 35 RIGHT - 36 RIGHT Z-FITTING WAS CORRODED. REPAIRED AREA IAW DC-8 SRM 51-1-8, 51 -1-20D, AND 53-2-0. 2 L 7 4 4F 4A25 2001061800188 20010618 00188 NM 2001 6 18 C8GA20010014 1 20010617 A 2610 BACC10AU450 CLAMP BOEING 727 727223 1384074 NM DETERIORATED A C8GA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 15 898AA 22014 Flt 898 from JAX to MCO. After takeoff #3 engine strut overheat light illuminated. Accomplished appropiate check list, a nd air turnback to JAX. Aircraft landed without incident. During inspection, found and replaced clamps on #3 engine blee d valve (pylon) IAW MM 36-10-01 and 20-80-01. System ops checked good and aircraft returned to service. 2 L 7 3 4F A3WE 2001061800189 20010618 00189 SO 2001 6 18 C2XA01BT113 1 20010606 A 2530 MS3470L1412P RECEPTACLE EMB 145 EMB145LR SO GALLEY FAULTY A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 14972 145151 EWR--CO4228, CREW REPORTED BURNING SMELL COMING FROM COFFEE POT.....MAINTENANCE REMOVED AND REPLACED COFFEE POT RECEPTAC LE IAW EMB145 MM #25-31-00....OPS. CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2001061900001 20010619 00001 SO 2001 6 19 C2XA01IA269 1 20010618 A 2730 12027655017 CONTROL CABLE EMB 120 EMB120ER 3260203 SO CARGO COMPT FRAYED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16729 120185 IAH - DURING "A" CHECK INSPECTION, THE LEFT HAND INBOARD ELEVATOR CABLE WAS FOUND TO HAVE SEVERAL BROKEN STRANDS IN THE CARGO COMPARTMENT. MAINTENANCE REMOVED AND REPLACED THE EFFECTED CABLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. 2 L 7 2 4T RT A31SO 2001061900002 20010619 00002 WP 2001 6 19 ABXA010263 1 20010525 A 5320 37536451 SUPPORT FITTING DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 TAILSKID LEFT UPPER SUPPORT FITTING HAD CORROSION AROUND 3 OUTBOARD FASTENERS ON UPPER SIDE OF FITTING AT FS 1766 LEFT B UTT LINE 8. REPAIRED AREA IAW DC-8 SRM 51-1-20D, 51-3-0, AND DAC DWG 5753522. 2 L 7 4 4F 4A25 2001061900003 20010619 00003 WP 2001 6 19 ABXA010264 1 20010525 A 5320 3755842503 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 AFT CARGO AT FS 1180 BETWEEN LONGERON 32 - 33 LEFT Z-FITTING WAS CORRODED. REPAIRED AREA IAW DC-8 SRM 51-1-20D, 51-3, 5 1-1-0, 52-2-0, AND 53-2-0. 2 L 7 4 4F 4A25 2001061900004 20010619 00004 WP 2001 6 19 ABXA010265 1 20010525 A 5720 5640281532534 FITTING DOUG DC8 DC863 302198A WP RT WING DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 RIGHT WING SKI FITTING AREA HAS 2 DAMAGED FASTENER HOLES AT STA 51 AND AFT SPAR. REPAIRED AREA IAW DC-8 SRM 51-1-12, 51 -1-8, 51-1-20D, AND REA D857-40385. 2 L 7 4 4F 4A25 2001061900005 20010619 00005 WP 2001 6 19 ABXA010266 1 20010525 A 5313 LONGERON DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 LONGERON 24 LEFT CRACKED BETWEEN FASTENERS, TOPSIDE STA 980. REPAIRED AREA IAW DC-8 SRM 53-2-2, 51-1-8, AND 51-1-20. 2 L 7 4 4F 4A25 2001061900006 20010619 00006 WP 2001 6 19 ABXA010267 1 20010525 A 5312 5640923501 BULKHEAD DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 AFT LOWER CARGO STA 980 BETWEEN LONGERON 35 RIGHT TO LONGERON 35 LEFT LOWER BULKHEAD HAD CORROSION AT PREVIOUS REPAIR. REPAIRED IAW DC-8 SRM 53-2-0, 51-1-24, 51-1-8, AND REA D853-40335 MR. 2 L 7 4 4F 4A25 2001070900007 20010709 00007 NM 2001 7 9 01FDEA00453 1 20010618 A 5320 SUPPORT BOEING 727 72722C 138400F NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 DURING ROUTINE INSP THE NR 1 SEAT TRACK SUPPORT AT BS 860 FOUND CRACKED. *S/D* REMOVED AND REPLACED SUPPORT PER IAW BA C 727 SRM 51-30-2. 2 L 7 3 4F A3WE 2001061900007 20010619 00007 NM 2001 6 19 01FDEA00454 1 20010618 A 5310 BAC1498138 STRINGER BOEING 727 7272D4 138407U NM BS 460 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 NR 838 WHILE WORKING N0301 FND CRACK EMANATING FROM OPEN HOLE AT BS 460, STR 3 L/H. ** S/D ** R&R STRING PER FEDEX SRM 53-10-3, 51-20-151, 53-10-3. 2 L 7 3 4F A3WE 2001070900008 20010709 00008 NM 2001 7 9 01FDEA00455 1 20010618 A 5311 FRAME BOEING 727 7272D4 138407U NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 FRAME IS DENTED AT BS 680 AT STRINGER 24 RT. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 51-30-2, 51-40-3. 2 L 7 3 4F A3WE 2001070900009 20010709 00009 NM 2001 7 9 01FDEA00456 1 20010618 A 5311 FRAME BOEING 727 7272D4 138407U NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 FRAME IS DENTED AT BS 660 AT STRINGER 25 RT. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 51-30-2, 51-40-3. 2 L 7 3 4F A3WE 2001070900010 20010709 00010 NM 2001 7 9 01FDEA00457 1 20010618 A 5310 69436834 SHEAR TIE BOEING 727 7272D4 138407U NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 EXTERIOR SKIN BULGED BS 500 BETWEEN STR 25 & 26 RT. *S/D* REMOVED AND REPLACED CORRODED SHEAR TIE PER IAW FEDEX SRM 51 -10-6, 51-30-2, FEDEX MM 51-20-191, 51-20-21. 2 L 7 3 4F A3WE 2001070900011 20010709 00011 NM 2001 7 9 01FDEA00458 1 20010618 A 5330 6554581 SKIN BOEING 727 7272D4 138407U NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 BULGE IN EXT BELLY SKIN BS 950+5 INCH BL 0. REMOVED AND REPLACED PER FEDEX SRM 53-10-3 FIG 1, EA 7-5330-57281. 2 L 7 3 4F A3WE 2001061900008 20010619 00008 NM 2001 6 19 01FDEA00460 1 20010616 A 2910 HYDRAULIC SYSTEM BOEING 727 727233 138408A NM BROKEN A FDEA H DEACTIVATE SYST/CIRCUITS K FLUID LOSS DE DESCENT 1 SO 25 271FE 22036 01-195 DUR DESCENT HYD SYS A FLUID LEVEL 1.2 GAL. FOLLOWED PROC & CKLIST. TURN OFF SPOILERS. LEAK STOPPED. UPON LOWERING FLAPS & GEAR, FLUID LEVEL DROPPED TO 0. SAFETY WIRE FOR ALT FLAPS SWITCH & GPWS OVERRIDE SWITCH BROKEN DUR PROCEDURE. ** S/D ** R&R LMG DOOR ACTUATOR OPEN HOSE ASSY PER MM 20-10-012-4. OPS CK NORM. 2 L 7 3 4F RT A3WE 2001061900009 20010619 00009 NM 2001 6 19 01FDEA00449 1 20010614 A 2120 UNKNOWN BOEING 727 727227 1384078 NM COCKPIT ODOR A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 481FE 21463 01-190 AT FLT LEVEL 330 FLT CREW SMELLED ODOR IN COCKPIT. AIRCRAFT WAS DOWNLOADED & CANS CHECKED FOR ODOR. CHECK A/C PAC KS, CND. 2 L 7 3 4F A3WE 2001061900010 20010619 00010 EU 2001 6 19 01FDEA00452 1 20010615 A 5610 NP1752331 WINDOW AIRBUS 300 A300F4605R 3930327 EU L3 CRACKED A FDEA B A EMER. DESCENT UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 657FE 748 01-193 IN CRUISE WINDOW L3 CRACKED. R&R LH FIXED SIDE WINDOW PER MM 56-11-12-4. R&R WINDOW HEAT CONTROLLER & WINDOW HEAT PROTECTION PER MM 30-42-11-4 & 30-42-51-4, MM 30-42-00-5. 2 L 7 2 4F RT A35EU 2001061900011 20010619 00011 WP 2001 6 19 ABXA010268 1 20010525 A 5730 56429401 PANEL DOUG DC8 DC863 302198A WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 SIX BOLT HOLES REAMED UP AFTER NDT CHECK BEYOND LIMITS OF SRM PANEL 505 F. REPAIRED AREA IAW DC-8 SRM 51-1-8, 51-1-20D, 51-1-20B, 51-1-21, DAC DWG 5613609, AND REA D857-40362MR. 2 L 7 4 4F 4A25 2001061900012 20010619 00012 WP 2001 6 19 ABXA010269 1 20010525 A 5720 36491172 FITTING DOUG DC8 DC863 302198A WP LT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 LEFT WING REAR SPAR SKI FITTING TO BOTTLE BOLT VERTICAL ATTACH FITTING HAD CORROSION AT LOWER SKI FITTING ATTACH AREA. P/N 3641117-2. REPAIRED AREA IAW DC-8 SRM 51. 2 L 7 4 4F 4A25 2001061900013 20010619 00013 WP 2001 6 19 ABXA010270 1 20010525 A 5720 56163441 FITTING DOUG DC8 DC863 302198A WP LT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 LEFT WING TRAPEZOID FITTING VERTICAL ATTACH FITTING P/N 5616344-1 WAS CORRODED. REPLACED FITTING IAW DC-8 SRM 51. 2 L 7 4 4F 4A25 2001070600008 20010706 00008 NM 2001 7 6 01FDEA00415 1 20010607 A 2700 ACH712715 FAIRLEAD DOUG MD11 MD11 3023602 NM FLIGHT CONTROL BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 583FE 48421 MAIN DECK CONTROL CABLE FAIRLEAD FOUND BROKEN AT BS 575, RBL 30 BELOW FLOOR PANEL. 2 L 7 3 4F RT A22WE 2001061900014 20010619 00014 WP 2001 6 19 ABXA010271 1 20010525 A 5311 2645791 FRAME DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 AFT CARGO AT FS 1340 ABOVE LONGERON 36 FRAME WAS CORRODED. REPAIRED AREA IAW DC-8 SRM 51. 2 L 7 4 4F 4A25 2001070900004 20010709 00004 NM 2001 7 9 01FDEA00434 1 20010611 A 5330 69436833 SKIN BOEING 727 7272D4 138407U NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 BULGE IN EXTERIOR SKIN BS 700 JUST ABOVE STR 26 RT. 2 L 7 3 4F A3WE 2001061900015 20010619 00015 WP 2001 6 19 ABXA010272 1 20010531 A 5210 RETAINER DOUG DC8 DC861 3021952 WP ENTRY DOOR BENT A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 847AX 46031 UNABLE TO OPEN CREW ENTRY DOOR FROM INSIDE AIRCRAFT AFTER LANDING. FOUND BENT SEAL RETAINER AND DOOR JAMB. STRAIGHTENE D RETAINER AS REQUIRED. DOOR OPS CHECKED GOOD WITH AIRCRAFT PRESSURIZED IAW DC8 MM 52-11-01. 2 L 7 4 4F 4A25 2001061900016 20010619 00016 WP 2001 6 19 ABXA010273 1 20010530 A 3350 60030451 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 966AX 47510 ON SERVICE CHECK FOUND EMERGENCY LIGHTS VERY WEAK. REPLACED EMERGENCY LIGHTS BATTERIES IAW DC9 MM 33-53-00. 2 L 7 2 4F A6WE 2001061900017 20010619 00017 WP 2001 6 19 ABXA010274 1 20010521 A 5730 59127372 PANEL DOUG DC9 DC931 3022065 WP RT WING DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 UPPER INBOARD TRAILING EDGE BONDED PANEL WAS DELAMINATED. REPLACED PANEL IAW DC-9 SRM 51-30-2 AND 51-30-1. 2 L 7 2 4F A6WE 2001061900018 20010619 00018 WP 2001 6 19 ABXA010275 1 20010517 A 5320 3915135501 ANGLE DOUG DC9 DC931 3022065 WP LT MLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 KEEL SUPPORT L-ANGLE CRACKED INSIDE LEFT KEEL, AFT SIDE UNDER RESERVOIR. INSTALLED NEW FITTING IAW DC-9 SRM 51-30-1, AN D 51-30-5. 2 L 7 2 4F A6WE 2001061900019 20010619 00019 WP 2001 6 19 ABXA010276 1 20010521 A 5313 59203192 LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 LONGERON 29 LEFT VERTICAL LEG CRACKED AT SPLICE BETWEEN STATION 408 - 427. REPLACED SECTION OF LONGERON 29 LEFT STATION 408 - 427 IAW DC-9 SRM 53-02, FIG 14 AND DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2001061900020 20010619 00020 WP 2001 6 19 ABXA010277 1 20010531 A 5610 5613217 WINDOW DOUG DC8 DC863 302198A WP COCKPIT OUT OF ADJ A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 RIGHT CLEAR VIEW WINDOW WOULD NOT OPEN. ADJUSTED RIGHT CLEAR VIEW WINDOW IAW DC-8 MM 56-10-3. REPAIRED EPOCAST. PRESS URIZED AIRCRAFT TO 4 PSID. NO LEAKS NOTED. WINDOW OPENS FREELY. 2 L 7 4 4F 4A25 2001070900003 20010709 00003 NM 2001 7 9 01FDEA00432 1 20010611 A 5311 FRAME BOEING 727 7272D4 138407U NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 FRAME IS DENTED AT BS 700 BETWEEN STR 23 RT AND 24 RT. 2 L 7 3 4F A3WE 2001061900021 20010619 00021 2001 6 19 ANCF200100012 4 20010603 A 3436 WARNING SYSTEM DOUG DC9 DC983 3022083 WP COCKPIT ACTIVATED W ANCF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 23 593AN 53093 DURING TAKEOFF ROLL, WIND-SHEAR AURAL WARNING AND ANNUNCIATION RED LIGHT CAME ON. TAKEOFF WAS REJECTED. 2 L 7 2 4F RT A6WE 2001070900001 20010709 00001 NM 2001 7 9 01FDEA00430 1 20010611 A 5311 FRAME BOEING 727 7272D4 138407U NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 FRAME IS DENTED AT BS 600 BETWEEN STRINGER 23 LT & 24 LT. 2 L 7 3 4F A3WE 2001061900022 20010619 00022 WP 2001 6 19 ARWA0010504 1 20010530 A 2611 SMOKE DETECTOR DOUG DC8 DC863F 302198F WP CARGO BAY MALFUNCTIONED A ARWA O OTHER N FALSE WARNING AP APPROACH 1 SO 19 661AV 45969 ON SHORT FINAL LOWER CARGO FIRE LIGHT CAME ON. DECLARE EMERGENCY AND CALLED FOR FIRE TRUCKS. AIRCRAFT LANDED WITHOUT I NCIDENT. Performed troubleshooting, found MTX display codes FB15785(a), AC15722, AD11039, and AD12614 ratio too low. Re moved and Replaced CCU IAW MM 26-15-01-2. Reprogrammed configuration module, ops ckd cargo compartment smoke detection system IAW MM 26-15-00-7 and STC ST00746LA-D found normal. 2 L 7 4 4F 4A25 2001061900023 20010619 00023 WP 2001 6 19 GTIA010498 1 20010602 A 3300 100491 FLASHLIGHT DOUG DC9 DC932 3022066 WP INOPERATIVE A GTIA O OTHER O OTHER IN INSP/MAINT 1 GL 23 133NK 48111 ACY - FOUND FORWARD EMERGENCY PORTABLE FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY PORTABLE FLASHLIGHT. OPS CHECK OK IAW MM 33-53-0. (M) 2 L 7 2 4F A6WE 2001061900024 20010619 00024 WP 2001 6 19 GTIA010488 1 20010602 A 3300 1001191 FLASHLIGHT DOUG DC9 DC932 3022066 WP INOPERATIVE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 133NK 48111 FLT 616 - ACY - FOUND FORWARD EMERGENCY PORTABLE FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY PORTABLE FLASHL IGHT. OPS CHECK GOOD IAW MM 33-53-00. (M) 2 L 7 2 4F A6WE 2001061900025 20010619 00025 WP 2001 6 19 GTIA010448 1 20010601 A 3350 LIGHT DOUG DC9 DC982 3022082 WP COCKPIT INOPERATIVE A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 804NK 49104 FLL - FLT 439 - FOUND COCKPIT OVERHEAD EMERGENCY LIGHT OUT. RELAMPED OVERHEAD EMERGENCY LIGHTS, OPS CHECK GOOD OK IAW M M 33-50-00. (M) 2 L 7 2 4F A6WE 2001061900026 20010619 00026 NM 2001 6 19 P2EA001083 1 20010330 A 3200 LANDING GEAR BOEING 737 737244 138448U NM WORN A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 OKC - DURING C-CHECK, FOUND THE RIGHT MAIN LANDING GEAR TRUNNION RACE WITH WEAR OUT OF LIMITS. REPAIRED THE RIGHT MLG T RUNNION RACE IAW BOEING OVERHAUL MANUAL, SEE FAA FORM 8130-3 TRACKING NR W/O 323910 FROM REPAIR STATION VQ4R605M. (M) 2 L 7 2 4F A16WE 2001061900027 20010619 00027 WP 2001 6 19 AALA016050 1 20010522 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP INOPERATIVE A AALA O OTHER O OTHER IN INSP/MAINT 1 SW 21 753RA 49587 SJC - FOUND COCKPIT OVERHEAD EMERGENCY LIGHTS INOPERATIVE, RELAMPED. NO LAMP. REMOVED AND REPLACED EMERGENCY BATTERY P ACK, OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 2001061900028 20010619 00028 WP 2001 6 19 AALA016051 1 20010515 A 3350 5100303 BATTERY DOUG DC9 DC987 3022087 WP INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 754RA 49641 CCI-SNA - FOUND SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE ON SEATS 17D, 18D, 19D AND 20D. REPLACED SEGMENT BATTERY AND C HARGER, OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 2001061900029 20010619 00029 NM 2001 6 19 BJNA010507 1 20010527 A 2700 65445101803 HYDRAULIC LINE BOEING 737 737214 138446R NM A BJNA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS F G J FLT CONT AFFECTED MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 WP 11 457TM 20156 LOST BOTH A/B HYDRAULIC SYSTEM PRESSURE. INSPECTED A/C FOUND NR 1 ENGINE 'A' SYSTEM HYDRAULIC LINE FAILURE AT PRESSURE MODULE. A/C IS SAFE FOR ITS INTENDED FERRY FLIGHT WITH THE NR 1 ENGINE 'A' PUMP IN THE OFF POSITION. INSTALLED APPROVE D RATED TEMPORARY FLEX HOSE OPS CHECK, LEAK CHECK, NORMAL IAW BMM 20-10-52. A/C RELEASED PER DMI TLD 0503, TLD NR 45702 82-1, ITEM TRANSFERRED TO MASTER DMI LOG. REMOVED TEMP FLEX LINE AND INSTALLED HARD LINE PER BMM 20-10-51, LEAK AND OPS CHECK OK. 'A' SYSTEM AND 'B' SYSTEM RETURN LINES ON RUDDER PCU FOUND REVERSED. RETURNED 'A' AND 'B' RETURN LINES TO T HE CORRECT POSITION, IAW DIAGRAM ON 27-21-91, PAGE 404, OPS AND LEAK CHECK NORMAL. NO LEAKS FOUND. AN INVESTIGATION IN 2 L 7 2 4F A16WE 2001062700143 20010627 00143 WP 2001 6 27 USAAD01114 1 20010521 A 3260 DOWNLOCK SENSOR DOUG DC9 DC931 3022065 WP RT MLG CORRODED A USAA L ABORTED APPROACH N FALSE WARNING DE DESCENT 1 EA 19 922VJ 48142 PIT-CRW - FLT 1282 - DURING DESCENT, WHEN THE LANDING GEAR WAS EXTENDED THE RIGHT MAIN LANDING GEAR GREEN DOWN AND LOCKE D LIGHT DID NOT ILLUMINATE. THE LANDING GEAR WAS VERIFIED DOWN BY THE CONTROL TOWER. THE LANDING GEAR WAS CYCLED AND T HE GREEN LIGHT ILLUMINATED. THE AIRCRAFT THEN LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED CORROSION FROM THE DOWN LOC K SENSOR ELECTRICAL CONNECTOR. (M) 2 L 7 2 4F A6WE 2001061900030 20010619 00030 WP 2001 6 19 AT0100176 1 20010212 A 3260 PROXIMITY SENSOR DOUG DC9 DC932 3022066 WP NLG OUT OF ADJ A ZZDA K NONE J WARNING INDICATION CL CLIMB 1 SO 15 866AT 47168 AIRCRAFT WOULD NOT TRANSFER TO FLIGHT MODE. AIRCRAFT WAS FERRIED FOR TROUBLESHOOTING. RIGGED AND ADJUSTED GROUND SENSE MECHANISM AND SERVICED NOSE STRUT IAW DC9 MM 32-23-1, 32-21-2. 2 L 7 2 4F A6WE 2001061900031 20010619 00031 NE 2001 6 19 AT0100177 2 20010416 A 7200 BR715A130 ENGINE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE NR 1 MALFUNCTIONED A ZZDA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 SO 15 940AT 55004 ON TAKE OFF CLIMB NR 1 ENGINE SURGE FOLLOWED BY ENGINE FLAME OUT. CORRECTIVE ACTION: REMOVED AND REPLACED NR 1 ENGINE. IAW 717 MM 72-00 2 L 7 2 4F 4 F TR A6WE E00061EN 2001061900032 20010619 00032 NM 2001 6 19 AT0100178 1 20010529 A 3350 8039251 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 945AT 55008 FOUND AFT ACCESSORY COMPARTMENT LOWER WALKWAY EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK IAW 717 AMM 33-51-03. 2 L 7 2 4F TR A6WE 2001061900033 20010619 00033 WP 2001 6 19 AT0100179 1 20010523 A 3350 6011779 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE C F.O.D. IN INSP/MAINT 1 SO 15 846AT 47226 FOUND EMERGENCY LIGHTS CHARGING CIRCUIT BREAKER POPPED. REPLACED EMERGENCY NACELLE FLOOD LIGHT BATTERY PACK IAW DC9 MM 33-53. 2 L 7 2 4F A6WE 2001061900034 20010619 00034 NE 2001 6 19 SCNA01045 2 20010618 A 7261 780650 GEARBOX BOEING 727 727227 1384078 NM PWA JT8 JT8D17R 52049 NE A SCNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 275AF 22092 707177 On climbout from MSP the number one engine low oil pressure light illuminated, oil quantity dropped and oil pressure gau ge started to drop verifying the warning light. Removed and replaced the gearbox, found oil pressure line leaking. 2 L 7 3 4F 4 F A3WE E2EA 2001061900035 20010619 00035 WP 2001 6 19 AT0100180 1 20010529 A 5310 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 836AT 47397 FOUND AFT PRESSURE BULKHEAD DOOR JAMB CRACKED. REMOVED UPPER DOOR JAMB AND FRAME IAW DC9 SRM 53-05, 53-01, AND SB 53-13 7 REV A DRAWING JD600-88. 2 L 7 2 4F A6WE 2001061900036 20010619 00036 WP 2001 6 19 AT0100181 1 20010525 A 5312 BULKHEAD DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 836AT 47397 FOUND AFT PIT BULKHEAD LEFT AND RIGHT PANELS CORRODED BEYOND LIMITS. INSTALLED DOUBLER IAW DC9 SRM 53-01 FIG 2, 53-01 F IG 1, AND 51-10-03. 2 L 7 2 4F A6WE 2001061900037 20010619 00037 NM 2001 6 19 AWXA0001763 1 20010529 A 5312 65163007 BULKHEAD BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 ULTRASONIC INSP REVEALS CRACK - HORIZ POSITION AT UPPER EDGE OF WL 218 ANGLE RBL 5.7-17; APPROX LENGTH 1 INCH. REPAIRED IAW SRM 53-10-11 FIG 1 DET 3 AND SRM 51-30-2 PG 5 AND REF DWG 65-16300. 2 L 7 2 4F RT A16WE 2001061900038 20010619 00038 NM 2001 6 19 AWXA0001764 1 20010529 A 5520 65C2514411 BRACKET BOEING 737 7373G7 1384595 NM RT ELEVATOR WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 RIGHT ELEVATOR OUTBOARD STAB MOUNT BRACKET HAS PLAY AT STAB MOUNT BOLTS (FITTING BOLT HOLES ARE ELONGATED). REPAIRED IA W AWA ER 03-5500-01143-JS1. 2 L 7 2 4F RT A16WE 2001061900039 20010619 00039 NM 2001 6 19 AWXA0001765 1 20010529 A 5754 65C26603100 SLAT BOEING 737 73733A 1384673 NM RT WING CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 RIGHT WING NR 4 SLAT CRACKED AT 3 FASTENER HOLES AT WBL 253-257. REMOVED CRACKED AREA AND INSTALLED REPAIR DOUBLER IAW SRM 57-43-01. 2 L 7 2 4F RT A16WE 2001061900040 20010619 00040 NM 2001 6 19 AWXA0001766 1 20010529 A 5754 65C26602218 SLAT BOEING 737 73733A 1384673 NM RT WING CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 NR 5 SLAT LOWER SURFACE CRACKED AT TWO FASTENER HOLES WBL 392. REMOVED CRACKED AREA AND INSTALLED REPAIR DOUBLER IAW SR M 57-43-01 PG 216-219. 2 L 7 2 4F RT A16WE 2001061900041 20010619 00041 NM 2001 6 19 AWXA0001767 1 20010529 A 5754 65C26601174 SLAT BOEING 737 73733A 1384673 NM RT WING CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 RIGHT WING NR 6 SLAT CRACKED AT FASTENER HOLE WBL 550 LOWER SURFACE. REMOVED CRACKED AREA AND INSTALLED REPAIR DOUBLER IAW SRM 57-43-01. 2 L 7 2 4F RT A16WE 2001061900042 20010619 00042 NM 2001 6 19 AWXA0001768 1 20010529 A 5311 963006501 FRAME BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 VERTICAL CHORD CRACKED BS 178 LBL 5.7 WL 184. REPAIRED AFT SIDE VERT CHORD IAW SRM 53-10-08 PG 221-235, 238-240. 2 L 7 2 4F RT A16WE 2001061900043 20010619 00043 NM 2001 6 19 AWXA0001769 1 20010529 A 5312 65C375903 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 CRACKED BS 178 BULKHEAD WEB WL 201.5 RBL 4.7. REPAIRED IAW SRM 53-10-08 PG 287-298. 2 L 7 2 4F RT A16WE 2001061900044 20010619 00044 NM 2001 6 19 AWXA0001770 1 20010529 A 5312 65C375903 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 AFT SIDE BS 178 BLKHD WEB CRACKS RBL .7-1.3 WL 205.7 AND LBL 1-1.5 WL 206. REPAIRED IAW SRM 53-10-08 PG 287-298. 2 L 7 2 4F RT A16WE 2001061900045 20010619 00045 NM 2001 6 19 AWXA0001771 1 20010529 A 5311 654653950 FRAME BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 FUSELAGE FRAME FITTING CRACKED AT FLOORBEAM ATTACH POINT RT SIDE BS 616. REMOVED FASTENER AND CUT OUT AREAS IAW AWA ER 03-5311-01157-KB1; FORMED ANGLE, FILLER IAW ER 03-5311-01127-KB1; DRILLED, TREATED AND PRIMED FILLER AND CAD PLATED ANGL E IAW ER 03-5311-01127-KB1; INSTALLED ANGLE REPAIR IAW ER 03-5311-01127-KB1. 2 L 7 2 4F RT A16WE 2001061900046 20010619 00046 NM 2001 6 19 AWXA0001772 1 20010529 A 5312 65C375903 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 AFT SIDE BLKHD WEB BS 178 CRACKED 2 PLACES LBL .6 WL 187.2-188.6 AND RBL .6 WL 187.1-188.6. REPAIRED IAW SRM 53-10-08 P G 287-298. 2 L 7 2 4F RT A16WE 2001061900047 20010619 00047 NM 2001 6 19 AWXA0001774 1 20010529 A 5754 6546431256SP DOUBLER BOEING 737 73733A 1384673 NM L/E SLAT CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 RT WING OUTBOARD FOREFLAP OUTBOARD L/E REPAIR DOUBLER CHAFED 2 SPOTS. REMOVED DOUBLER IAW SRM 51-40-02 PG 9; TRIMMED OU T CRACKED AREA IAW SRM 57-53-01 PG 201-201; FORMED, DRILLED AND LOCATED IAW SRM 57-53-01 PG 202; TREATED AND PRIMED IAW SRM 51-20-01; INSTALLED IAW SRM 51-40-02 PG 9. 2 L 7 2 4F RT A16WE 2001061900048 20010619 00048 NM 2001 6 19 AWXA0001775 1 20010529 A 5312 65C375903 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 TEMPORARY CHERRY MAX INSTALLED REPAIR BS 178 BLKHD WEB WL 189 LBL 21. REPAIRED IAW SRM 53-10-08 PG 216-220 AND 51-40-02 PG 2-3, 10-11 AND 51-20-01 PG 1-6, 10. 2 L 7 2 4F RT A16WE 2001070900015 20010709 00015 NM 2001 7 9 01FDEA00463 1 20010618 A 5313 BAC1498145 STRINGER BOEING 727 7272D4 138407U NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 CORROSION ON STR 28L, BS 700+15, WL 153. *S/D* REMOVED AND REPLACED STR PER IAW FEDEX SRM 53-10-1, 53-10-3. 2 L 7 3 4F A3WE 2001061900049 20010619 00049 NM 2001 6 19 01FDEA00464 1 20010618 A 5330 6554581 SKIN BOEING 727 7272D4 138407U NM BS 950E+3 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 NR 703 BULGE EXTERIOR SKIN BS 950E+3, STR 28 LH. ** S/D ** R&R SKIN PER IAW FEDEX EA 7-5330-57274. 2 L 7 3 4F A3WE 2001061900050 20010619 00050 NM 2001 6 19 AWXA0001777 1 20010530 A 5320 6545833440 WEB BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 COCKPIT RT FLOOR WEB CRACKED AT LIGHTENING HOLE BS 180 RBL 24 WL 207. REMOVED AND REPLACED WEB IAW SRM 51-40-02 PG 2-3, 10-11 AND 51-20-01 PG 1-6 & 10. 2 L 7 2 4F RT A16WE 2001061900051 20010619 00051 NM 2001 6 19 AWXA0001778 1 20010530 A 5320 651630091 STRAP BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 FOUND BS 178 BLKHD FWD SIDE 0 BL STRAP CRACKED THROUGH WL 187. REPLACED STRAP IAW SRM 51-40-02 AND 51-20-01. 2 L 7 2 4F RT A16WE 2001061900052 20010619 00052 NM 2001 6 19 AWXA0001779 1 20010530 A 5312 65C375903 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 ULTRASONIC CRACK INDICATION BS 178 BLKHD WEB BENEATH STRAP FWD SIDE WL 218 RBL 14.1-13.3. REPAIRED IAW SRM 53-10-08 PG 265-268. 2 L 7 2 4F RT A16WE 2001061900053 20010619 00053 NM 2001 6 19 AWXA0001780 1 20010530 A 5312 65C375903 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 ULTRASONIC CRACK INDICATION BS 178 BLKHD WEB BENEATH STRAP RBL 4.7 WL 198.5-198.7. REPAIRED IAW SRM 53-10-08 PG 287-298 . 2 L 7 2 4F RT A16WE 2001061900054 20010619 00054 NM 2001 6 19 AWXA0001781 1 20010530 A 5312 65C375903 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 ULTRASONIC CRACK INDICATION BS 178 BLKHD WEB BENEATH STRAP RBL 4.7 WL 212-212.6. REPAIRED IAW SRM 53-10-08 PG 287-298. 2 L 7 2 4F RT A16WE 2001061900055 20010619 00055 NM 2001 6 19 AWXA0001782 1 20010530 A 5312 65C375903 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 ULTRASONIC CRACK INDICATION BS 178 BLKHD WEB BENEATH STRAP LBL 4.7 WL 209.7-210. REPAIRED IAW SRM 53-10-08 PG 287-298. 2 L 7 2 4F RT A16WE 2001061900056 20010619 00056 NM 2001 6 19 AWXA0001783 1 20010530 A 5312 65C375903 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 HFEC INDICATES CRACK BS 178 BLKHD WEB WL 199 LBL 4.7 FWD SIDE. REPAIRED IAW SRM 53-10-08 PG 287-298. 2 L 7 2 4F RT A16WE 2001061900057 20010619 00057 NM 2001 6 19 AWXA0001784 1 20010530 A 5320 6545833440 WEB BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 COCKPIT LT FLOOR WEB CRACKED AT LIGHTENING HOLE BS 180 LBL 24 WL 207. REMOVED AND REPLACED FLOOR WEB IAW SRM 51-40-02 P G 2-3 AND 51-20-01 PG 1-6 & 10. 2 L 7 2 4F RT A16WE 2001061900058 20010619 00058 NM 2001 6 19 AWXA0001785 1 20010530 A 5230 65C3836422 FRAME BOEING 737 73733A 1384673 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 LWR CHORD OF FWD CARGO DOOR CRACKED AT 3 FASTENER HOLES CONFIRMED BY HFEC. REPAIRED IAW AWA ER 03-5231-01130-DL1. 2 L 7 2 4F RT A16WE 2001061900059 20010619 00059 NM 2001 6 19 AWXA0001786 1 20010530 A 5330 6545778 SKIN BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 R2 DOOR FUSELAGE LWR HINGE CUTOUT HFEC INDICATES CRACK BS 947.5 EMANATING FROM BENEATH WINDOW BELT DOUBLER .625 INCH AT WL 227. REPAIRED IAW SRM 53-60-01. 2 L 7 2 4F RT A16WE 2001061900060 20010619 00060 NM 2001 6 19 AWXA0001787 1 20010530 A 5312 6516300512 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 CRACK IN WEB BS 178 BLKHD WL 200 RBL 16.5. REPAIRED IAW SRM 53-10-08 PG 265-268, 216-220. 2 L 7 2 4F RT A16WE 2001061900061 20010619 00061 NM 2001 6 19 AWXA0001788 1 20010530 A 5230 6548921528 CROSSBEAM BOEING 737 73733A 1384673 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 CRACK IN FWD CARGO DOOR CROSSBEAM 1.25 INCH THROUGH FASTENER HOLE COMMON TO LWR TEE AND BEAM. INSTALLED FILLER AND REPA IR DOUBLER ON CROSSBEAM IAW AWA ER 03-5231-01130-DL1. 2 L 7 2 4F RT A16WE 2001061900062 20010619 00062 NM 2001 6 19 AWXA0001789 1 20010530 A 5230 6548921528 BEAM BOEING 737 73733A 1384673 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 CRACK IN FWD CARGO DOOR LWR BEAM 1 INCH THROUGH FASTENER HOLE COMMON TO LWR TEE AND BEAM AT 4TH FASTENER HOLE BS 444. R EPAIRED IAW AWA ER 03-5231-01130-DL1. 2 L 7 2 4F RT A16WE 2001061900063 20010619 00063 NM 2001 6 19 AWXA0001790 1 20010530 A 5230 65C3836438 FRAME BOEING 737 73733A 1384673 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 FWD CARGO DOOR PAN FRAME CRACKED 3 INCHES NEAR HOLD OPEN HOOK. REMOVED AND REPLACED FWD CARGO DOOR, FWD LWR CORNER PAN IAW SRM 51-40-05 PG 1-2 AND 51-40-02 PG 2-4. 2 L 7 2 4F RT A16WE 2001061900064 20010619 00064 NM 2001 6 19 AWXA0001791 1 20010530 A 5414 311A11022 PLATE BOEING 737 73733A 1384673 NM LT PYLON CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 TOP LEFT PYLON LAND FOR ACCESS PANEL CRACKED NAC STA 214. REPAIRED IAW AWA ER 03-5433-00340-DL1. 2 L 7 2 4F RT A16WE 2001061900065 20010619 00065 NM 2001 6 19 AWXA0001792 1 20010530 A 5753 6546486 WEDGE BOEING 737 73733A 1384673 NM T/E FLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 LEFT WING INBOARD MID FLAP WEDGE LWR SIDE HAS 2 AREAS OF DELAMINATION. REPAIRED IAW SRM 51-70-17 PG 68 & 70 AND AWA ER 03-5750-01145-JS1. 2 L 7 2 4F RT A16WE 2001061900066 20010619 00066 NM 2001 6 19 AWXA0001793 1 20010530 A 5753 6546486 WEDGE BOEING 737 73733A 1384673 NM T/E FLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 LEFT WING INBOARD MID FLAP WEDGE PANEL DELAMINATED AT INBOARD BOTTOM SIDE. CUT OUT DISBONDED SKIN ON LWR SURFACE OF LT WING INBD MID FLAP WEDGE PANEL; MADE FILLER AND DOUBLER, ETCHED, TREATED AND PRIMED ADHESIVE PRIMER TO REPAIR AREA, BOND ED REPAIR, TREATED SEALED REPAIR AREA IAW SRM 51-20-10 PGS.88C, 88D AND 51-20-01 PG 9-10 AND 51-20-05 PG 2-8. 2 L 7 2 4F RT A16WE 2001061900067 20010619 00067 NM 2001 6 19 AWXA0001794 1 20010531 A 5312 65C375903 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 VISUAL AFT SIDE BS 178 WEB WL 189-187.8 RBL .6; 1.2 INCH CRACK VERIFIED BY HFEC. REPAIRED IAW SRM 53-10-8 PG 287-298 FI G 211. 2 L 7 2 4F RT A16WE 2001061900068 20010619 00068 NM 2001 6 19 AWXA0001795 1 20010531 A 5312 65C375903 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 HFEC INDICATES 4 CRACKS BS 178 BLKHD WEB FWD SURFACE WL 234.1 RBL 8, 9, 11, 12 HI-LOK FASTENER HOLES. REPAIRED IAW SRM 53-10-8 FIG 209 PG 265-274. 2 L 7 2 4F RT A16WE 2001061900069 20010619 00069 NM 2001 6 19 AWXA0001796 1 20010531 A 5312 65C375903 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 HFEC INSP FWD SIDE OF BS 178 BLKHD 2 CRACKS LBL 4.7 WL 199-199.4 AND 201-201.5. REPAIRED IAW SRM 53-10-8 FIG 211 PG 287 -298. 2 L 7 2 4F RT A16WE 2001070900016 20010709 00016 NM 2001 7 9 01FDEA00465 1 20010618 A 5310 6556124 SHEAR TIE BOEING 727 727277 138408S NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 CORROSION ON SHEAR TIE AT BS 950F LBL 9 WL 138.5. *S/D* REMOVED, REPLACED AND FAB PER IAW FEDEX SRM 53-10-1, 51-10-2, 53-10-4. 2 L 7 3 4F RT A3WE 2001071300029 20010713 00029 NM 2001 7 13 01FDEA00466 1 20010618 A 5310 65561321 DOOR FRAME BOEING 727 727277 138408S NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 CORROSION (C53-111-02, 2) ON NR 3 CARGO DOORWAY AFT FRAME BS 1136 RBL 30 WL 157. *S/D* REMOVED AND REPLACED NR 3 CARGO DOORWAY AFT FRAME PER EA 7-5310-57293. 2 L 7 3 4F RT A3WE 2001061900070 20010619 00070 NM 2001 6 19 AWXA0001797 1 20010531 A 5330 6545778 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 HFEC INDICATES CRACK IN FUSELAGE SKIN AT AFT SERVICE DOOR LWR HINGE CUTOUT BS 947.5 WL 226.5. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW SRM 53-60-01 FIG 207 PG 217-224. 2 L 7 2 4F RT A16WE 2001061900071 20010619 00071 NM 2001 6 19 AWXA0001798 1 20010531 A 5230 6548921528 CROSSBEAM BOEING 737 7373G7 1384595 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 CRACK FOUND IN FWD CARGO DOOR CROSSBEAM AFT LWR END. CUT OUT CRACKED SECTION AND INSTALLED FILLER AND REPAIR DOUBLER IA W AWA ER 03-5200-01129-JS1. 2 L 7 2 4F RT A16WE 2001061900072 20010619 00072 NM 2001 6 19 AWXA0001799 1 20010531 A 5312 65C375903 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 HFEC INSP FWD SIDE OF BS 178 BLKHD WEB FOUND 3 CRACKS WL 234.1 LBL 9, 11, 12 AT HI-LOK FASTENER HOLES. REPAIRED IAW SRM 53-10-8 PG 265-274 FIG 209. 2 L 7 2 4F RT A16WE 2001061900073 20010619 00073 WP 2001 6 19 2001F00013 1 20010515 A 3350 260BC1011 CHARGER DOUG DC9 DC987 3022087 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 754RA 49641 CCI-SNA - FOUND SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE ON SEATS 17D, 18D, 19D AND 20D. REPLACED SEGMENT BATTERY AND C HARGER, OPS CHECK OK. REF AALA016051. (M) 2 L 7 2 4F RT A6WE 2001061900074 20010619 00074 NM 2001 6 19 2001F00007 1 20010605 A 2910 651782114 MODULE BOEING 737 7372K5 138448X NM HYD SYSTEM MALFUNCTIONED A RJEF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 231TA 22596 MIA - FLT 321 - AFTER TAKEOFF OF FLIGHT, THE LANDING GEAR DID NOT GO UP WHEN RAISED. THE AIRCRAFT RETURNED TO DEPARTURE AIRPORT FOR MAINTENANCE, LANDING WAS NORMAL. T/S WAS PERFORMED AS PER AMM 32-09-200 PAGE 501, ADJUSTED GROUND SAFETY S WITCH, AIRCRAFT JACKED AND PERFORMED SEVERAL LANDING GEAR EXTENSIONS/RETRACTIONS AS PER AMM 32-32-0, OPERATION WAS NORMA L. THE PROPER SYSTEM OPERATION WAS VERIFIED DURING 'NONREVENUE' FLIGHT. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001061900075 20010619 00075 2001 6 19 2001F00008 4 20010606 A 3414 2594621918 INDICATOR AIRBUS 300 A300B4203 3930306 EU COCKPIT FAILED A RJEF A UNSCHED LANDING O OTHER CL CLIMB 1 SO 23 59140 3426 140 MIA - FLT 821 - DURING TAKEOFF, THE CAPTAIN REPORTED THE FIRST OFFICER AIR SPEED INDICATOR FROZEN AT 120 KNOTS, THE AIRC RAFT RETURNED TO MIA STATION FOR MAINTENANCE. AFTER LANDING, MAINTENANCE PERSONNEL REMOVED AND REPLACED THE FIRST OFFIC ER AIRSPEED INDICATOR ACCORDING TO AMM 34-11-40, PERFORMED OPERATIONAL TEST ACCORDING TO AMM 34-11-40 PAGE 501. THE AIR CRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A35EU 2001061900076 20010619 00076 SO 2001 6 19 2001F00009 1 20010507 A 5610 1159SCB31024 WINDSHIELD GULSTM G1159 G1159 3953505 SO COCKPIT CRACKED A DVYA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 23 221CM 343 WHILE EN ROUTE FROM KVNY TO KTEB, EXPERIENCED A CRACK IN THE NR 2 WINDSHIELD, 30 MINUTES INTO FLIGHT. THE PILOT IN COMM AND RETURNED THE AIRCRAFT TO THE MAINTENANCE FACILITY IN KVNY. AFTER RETURNING, THE WINDOW WAS ASSESSED BY TRANS-EXEC A IR SERVICE, INC MX DEPT. THE AIRCRAFT NR 2 WINDSHIELD WAS REPLACED WITH A NEW UNIT, AND THE AIRCRAFT WAS RETURNED TO SE RVICE. (M) 2 L 7 2 4F RT A12EA 2001061900077 20010619 00077 CE 2001 6 19 2001F00010 1 20010522 A 3340 7270510 SWITCH BEECH 1900 1900C 1154161 CE COCKPIT SHORTED A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 19 130GA UC96 FLT 9396 - MIA/EYW - AFTER DEPARTURE FROM MIAMI, STRONG ELECTRICAL SMELL OBSERVED. FOUND LEFT LANDING LIGHT SWITCH SHOR TED. REMOVED AND REPLACED SWITCH AND SECURED WIRE AT LEFT LANDING LIGHT. OPS CHECK NORMAL. (M) 2 L 7 2 4T RT A24CE 2001061900078 20010619 00078 NM 2001 6 19 2001F00011 1 20010509 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 887MA 21857 ON PREFLIGHT TRANSIT, FOUND RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXI T LIGHT BATTERY PACK IAW MM 33-50-01. OPS CHECK OK. (M) 2 L 7 3 4F A3WE 2001061900079 20010619 00079 NM 2001 6 19 2001F00012 1 20010426 A 3222 651637115 TORQUE LINK BOEING 727 727276 138408R NM NLG DAMAGED A FX7A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 19 908PG 20951 DURING PUSH BACK UPPER NOSE LANDING GEAR SCISSOR TORQUE TUBE LINK DROPPED TO THE DOWN POSITION AND WEDGED BETWEEN THE NO SE WHEELS SCUFFING IT AND KNOCKING OUT THE GREASE FITTING. REMOVED AND REPLACED NOSE LANDING GEAR UPPER SCISSOR TORQUE LINK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2001061900080 20010619 00080 NE 2001 6 19 AALA016049 2 20010510 A 7321 AS3578020 O-RING DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE FCU CUT A AALA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 SW 21 753RA 33262 49587 725706 AIRCRAFT GROUND INTERRUPTED AND SHUTDOWN NR 1 ENGINE WITH A LEAK REPORTED BY ANOTHER AIRCRAFT. FOUND FUEL LEAK BETWEEN FUEL CONTROL AND ENGINE FUEL PUMP. PLAN TO REPLACE FUEL CONTROL AND ENGINE FUEL PUMP OR SEALS AS REQUIRED. FOUND CUT O -RINGS ON FUEL CONTROL. REPLACED CUT O-RINGS. LEAK CHECK OK DURING ENGINE RUN. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2001061900081 20010619 00081 WP 2001 6 19 AALA016052 1 20010504 A 3350 MB10P2 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 823RA 49889 CCI-LAX - FOUND SEAT 3E EMERGENCY LIGHT DOES NOT ILLUMINATE. FOUND LOOSE CONNECTOR. RESECURED PLUG CONNECTOR. OPS CHE CK GOOD. (M) 2 L 7 2 4F A6WE 2001061900082 20010619 00082 EU 2001 6 19 AALA20010887 1 20010429 A 2821 FILTER AIRBUS 300 A300B4605R 3930308 EU NR 1 ENGINE CLOGGED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 7062A 474 SJU - FLT 1385 - EN ROUTE JFK-BGI, DURING CRUISE NR 1 FUEL CLOG LIGHT ILLUMINATED. DIVERTED SJU AND LANDED WITHOUT FURT HER INCIDENT. REPLACED NR 1 ENGINE FUEL FILTER. NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2001061900083 20010619 00083 EU 2001 6 19 AALA20010888 1 20010430 A 2910 HOSE AIRBUS 300 A300B4605R 3930308 EU HYD SYSTEM LEAKING A AALA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 21 14061 471 JFK - FLT 1152 - EN ROUTE MIA-JFK, ON SHORT FINAL GREEN HYDRAULIC SYSTEM DECREASED TO ZERO. HYDRAULIC PUMPS WERE IMMEDI ATELY SHUT OFF. LANDED JFK WITHOUT FURTHER INCIDENT. REPLACED LEFT SIDE MAIN LANDING GEAR PRESSURE FLEXIBLE HOSE. SER VICED GREEN SYSTEM. NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2001061900084 20010619 00084 WP 2001 6 19 AALA20010910 1 20010502 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 489AA 49682 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS FROM SEAT 12 TO 16 FOUND INOPERATIVE. REPLACED EMERG ENCY EXIT LIGHT BATTERY PACK. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001061900085 20010619 00085 WP 2001 6 19 AALA20010914 1 20010430 A 3610 5953625 DUCT DOUG DC9 DC983 3022083 WP A/C BAY LEAKING A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 566AA 49348 DFW - FLT 1507 - EN ROUTE DFW-YVR - ON TAKEOFF, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. ACCOMPLISHED EMERG ENCY PROCEDURE, DECLARED EMERGENCY AND LANDED DFW WITHOUT FURTHER INCIDENT. INSTALLED NEW DUCT ASSEMBLY IN AFT ACCESSOR Y COMPARTMENT, PERFORMED HIGH PRESSURE DUCT LEAK CHECK. NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001061900086 20010619 00086 NM 2001 6 19 AALA20010915 1 20010426 A 5330 SKIN BOEING 727 727227 1384078 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 719AA 20612 TUL - FOUND CRACK IN SKIN AT FASTENER HOLE AT STATION 328 JUST BELOW STRINGER 20L. INSTALLED REPAIR PER SRM 53-30-3 FIG 13. (M) 2 L 7 3 4F A3WE 2001061900087 20010619 00087 WP 2001 6 19 AALA20010917 1 20010419 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 517AA 49894 TUL - FOUND BELLFRAME TOP LIP DENTED STATION 1258 ABOVE LONGERON 30. INSTALLED REPAIR PER ESO 80559 DATED 04/25/2001. (M) 2 L 7 2 4F A6WE 2001061900088 20010619 00088 WP 2001 6 19 AALA20010918 1 20010416 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 517AA 49894 TUL - FOUND CORROSION ON SEAT TRACK NR 2 STATION 1200-1201 .050 BY 1.0 BY .080. ROUTED OUT DAMAGED AREA AND INSTALLED S EAT TRACK PLUG REPAIR PER AARD 53-20-00-10. (M) 2 L 7 2 4F A6WE 2001061900089 20010619 00089 WP 2001 6 19 AALA20010919 1 20010419 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 517AA 49894 TUL - FOUND CORROSION BEYOND LIMITS. INSTALLED CUSP DOUBLER PER AARD 53-04. (M) 2 L 7 2 4F A6WE 2001061900090 20010619 00090 WP 2001 6 19 AALA20010920 1 20010411 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 517AA 49894 TUL - FOUND CORROSION ON SEAT TRACK NR 6 STATION 1041. ROUTED OUT DAMAGED AREA AND INSTALLED PLUG PER SRM 53-05 PART 1 FIG 4A. (M) 2 L 7 2 4F A6WE 2001061900091 20010619 00091 NM 2001 6 19 AALA20010938 1 20010411 A 5210 STOP FITTING BOEING 727 727227 1384078 NM PAX DOOR CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 723AA 20731 TUL - FOUND AFT LOWER DOOR STOP PIN FITTING CRACKED ON FORWARD ENTRY DOOR. REMOVED AND REPLACED LOWER AFT STOP FITTING PER ESO 2436. (M) 2 L 7 3 4F A3WE 2001061900092 20010619 00092 NM 2001 6 19 AALA20010939 1 20010411 A 5210 STOP FITTING BOEING 727 727227 1384078 NM PAX DOOR CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 723AA 20731 TUL - FOUND UPPER AFT STOP PIN FITTING CRACKED ON FORWARD ENTRY DOOR. INSTALLED NEW STOP FITTING PER ESO2436. (M) 2 L 7 3 4F A3WE 2001061900093 20010619 00093 NM 2001 6 19 AALA20010940 1 20010411 A 5210 SKIN BOEING 727 727227 1384078 NM PAX DOOR CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 723AA 20731 TUL - FOUND 2.5 INCH CRACK ON EXTERIOR SKIN OF FORWARD ENTRY DOOR, LOWER. DAMAGED CUT OUT. DOUBLER AND FILLER INSTALLE D PER SRM 52-00-3 AND ESO2436. (M) 2 L 7 3 4F A3WE 2001061900094 20010619 00094 WP 2001 6 19 AALA20010946 1 20010506 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 592AA 53255 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT DIM. REPLACED EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NOR MAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001061900095 20010619 00095 WP 2001 6 19 AALA20010947 1 20010506 A 3397 WIRE DOUG DC9 DC982 3022082 WP AIRSTAIRS LOOSE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 456AA 49561 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT WIRE AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001061900096 20010619 00096 WP 2001 6 19 AALA20010948 1 20010506 A 3397 WIRE DOUG DC9 DC982 3022082 WP R1 DOOR DAMAGED A K NONE L NO TEST IN INSP/MAINT 1 SW 21 581AA 53158 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT R1 DOOR INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001061900097 20010619 00097 WP 2001 6 19 AALA20010949 1 20010506 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 251AA 49270 DFW - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT DIM. REPLACED SEAT MOUNTED EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001061900098 20010619 00098 WP 2001 6 19 AALA20010950 1 20010506 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 246AA 49258 DFW - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT DIM. REPLACED SEAT MOUNTED EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001061900099 20010619 00099 WP 2001 6 19 AALA20010951 1 20010502 A 3350 AB51 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 259AA 49289 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT FROM ROW 13D THROUGH 16D DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001061900100 20010619 00100 WP 2001 6 19 AALA20010953 1 20010505 A 3350 SPLICE DOUG DC9 DC982 3022082 WP TAILCONE CHAFED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 73444 49470 DFW - DURING OVERNIGHT MAINTENANCE, TAILCONE EMERGENCY EXIT LIGHT WIRE CHAFED. REPLACED EMERGENCY EXIT LIGHT WIRE SPLIC E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001061900101 20010619 00101 WP 2001 6 19 AALA20010957 1 20010505 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 244AA 49256 DFW - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT DIM. REPLACED EMERGENCY EXIT LIGHT. SYSTEM GROUN D CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001061900102 20010619 00102 2001 6 19 AALA20010961 4 20010502 A 2320 4971262 TELEPRINTER BOEING 767 767323 1385205 NM COCKPIT OVERHEATED A AALA O OTHER M OVER TEMP CR CRUISE 1 SW 21 398AN 29605 CDG - FLT 62 - EN ROUTE MIA-CDG, DETECTED MALFUNCTION AND OVERHEAT AT ACARS PRINTER. PULLED AND COLLARED ACARS PRINTER CIRCUIT BREAKER. LANDED CDG WITHOUT FURTHER INCIDENT. REPLACED ACARS PRINTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001061900103 20010619 00103 NM 2001 6 19 AALA20010962 1 20010503 A 5330 SKIN BOEING 727 727227 1384078 NM FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 719AA 20612 TUL - FOUND AREA OF FUSELAGE SKIN HAS DEEP BLEND OUT AREAS OF PREVIOUS GOUGES BETWEEN STRINGER 17 AND 18L AT STATION 109 0. INSTALLED DOUBLER OVER DAMAGED AREA PER SRM 53-30-3 FIG 1. (M) 2 L 7 3 4F A3WE 2001061900104 20010619 00104 NM 2001 6 19 AALA20010963 1 20010501 A 5313 STRINGER BOEING 727 727227 1384078 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 719AA 20612 TUL - FOUND CORROSION ON STRINGER 23R STATION 1165. INSTALLED STRINGER REPAIR PER SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 2001061900105 20010619 00105 EU 2001 6 19 AALA20010964 1 20010504 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70072 515 TUL - FOUND CORROSION FS 75-80, BEYOND LIMITS. REPLACED GALLEY SUPPORT FROM FS 75-80 PER SRM 51-72-10-01. (M) 2 L 7 2 4F RT A35EU 2001061900106 20010619 00106 WP 2001 6 19 AALA20010968 1 20010508 A 2540 WIRE DOUG DC9 DC982 3022082 WP LAVATORY ARCED A K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 418AA 49329 ORD - FLT 2370 - EN ROUTE DFW-ORD, FLIGHT ATTENDANT REPORTED SMOKE AND ARCING AT FORWARD LAVATORY. LANDED ORD WITHOUT F URTHER INCIDENT. REPAIRED DOOR LOCK SWITCH WIRING AT FORWARD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001061900107 20010619 00107 WP 2001 6 19 AALA20010976 1 20010513 A 3397 WIRE DOUG DC9 DC982 3022082 WP TAILCONE DAMAGED A K NONE L NO TEST IN INSP/MAINT 1 SW 21 486AA 49679 DFW - DURING OVERNIGHT MAINTENANCE, TAIL CONE HANDLE EMERGENCY LIGHT INOPERATIVE. REPLACED WIRING TO TAIL CONE HANDLE E MERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001061900108 20010619 00108 NM 2001 6 19 AWXA0001876 1 20010618 A 5310 6545777150 STRINGER BOEING 737 7373G7 1384595 NM CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 307AW 24634 D: Stringer #1 LT. at BS 727A cracked C: Removed damaged section of Stringer #1 LT. BS 727A- Formed and Installed String er repair cables. Installed Stringer filler at Stringer 1 LT. BS 727A All IAW B737-300 SRM 53-00-03 Fig 203 PG214-216 2 L 7 2 4F RT A16WE 2001061900109 20010619 00109 WP 2001 6 19 AALA20010977 1 20010513 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 486AA 49679 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY LIGHTS AT FLIGHT DECK AND R1 DOOR FAILED TO STAY ILLUMINATED. RE PLACED BATTERY ASSEMBLY TO OVERHEAD EMERGENCY LIGHTS AT FLIGHT DECK AND R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION . (M) 2 L 7 2 4F A6WE 2001061900110 20010619 00110 WP 2001 6 19 AALA20010978 1 20010513 A 3350 SPLICE DOUG DC9 DC982 3022082 WP TAILCONE DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 486AA 49679 DFW - DURING OVERNIGHT MAINTENANCE, TAILCONE SIDEWALL EMERGENCY LIGHTS INOPERATIVE. REPLACED BAD SPLICE AT FEEDER WIRE FOR TAIL CONE SIDEWALL EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001061900111 20010619 00111 WP 2001 6 19 AALA20010979 1 20010511 A 3350 AB51 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 294AA 49306 LAX - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY LIGHTS ABOVE ROWS 8, 9, AND 10 REPORTED DIM. REPAIRED BATTERY PAC K FOR CEILING EMERGENCY LIGHTS ABOVE ROWS 8, 9, AND 10. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001061900112 20010619 00112 WP 2001 6 19 AALA20010980 1 20010511 A 3350 AB51 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 294AA 49306 LAX - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY LIGHTS ABOVE ROWS 29, 30, AND 31 REPORTED INOPERATIVE. REPLACED B ATTERY PACK FOR CEILING EMERGENCY LIGHTS ABOVE ROWS 29, 30 AND 31. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001061900113 20010619 00113 EU 2001 6 19 AALA20010983 1 20010509 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14053 420 TUL - FOUND FRAME 18, STRINGER 54R TO 54L HAS CORROSION ON SHEAR TIE. INSTALLED NEW FRAME SECTION PER SRM 51-72-10. (M ) 2 L 7 2 4F RT A35EU 2001061900114 20010619 00114 WP 2001 6 19 AALA20010985 1 20010513 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 452AA 49553 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD GALLEY AND COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD GALLEY AND COCKPIT EMERGENCY LIGHTS. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001061900115 20010619 00115 EU 2001 6 19 AALA20010986 1 20010514 A 3350 60030451 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE O OTHER CR CRUISE 1 SW 21 33069 512 JFK - FLT 655 - DURING FLIGHT TO STT, CABIN EMERGENCY ESCAPE PATH EXIT LIGHTS CAME ON THREE OR FOUR TIMES FOR A FEW SECO NDS EACH TIME. REPLACED BATTERY PACK AND BATTERY AT M10801. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2001061900116 20010619 00116 WP 2001 6 19 AALA20010987 1 20010513 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 566AA 49348 ORD - DURING OVERNIGHT MAINTENANCE, LOWER RIGHT OVER WING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED LOWER RIGHT OVER W ING EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001061900117 20010619 00117 NM 2001 6 19 AALA20010988 1 20010513 A 5712 RIB BOEING 727 727223 1384074 NM LT WING CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 890AA 22006 TUL - FOUND DURING SCHEDULED C-CHECK INSPECTION, A CRACK WAS FOUND IN THE LBL 70.5 UPPER RIB CHORD AT BS 760. INSTALLED THE PREVENTATIVE MODIFICATION 65C33202-99 PER BOEING 727 SB 727-57-0112 WITH DEVIATION PER ESO 11697 DATED 5-9-2001. (M ) 2 L 7 3 4F A3WE 2001061900118 20010619 00118 WP 2001 6 19 AALA20010989 1 20010512 A 3397 WIRE DOUG DC9 DC982 3022082 WP AFT AIRSTAIRS BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 21 478AA 49653 DFW - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR FORWARD EMERGENCY LIGHT MARKER INOPERATIVE. REPAIRED BROKEN WIRE ON AF T STAIRS FORWARD EMERGENCY LIGHT MARKER. SYSTEM GROUND CHECK OPERATION NORMAL. (M) 2 L 7 2 4F A6WE 2001061900119 20010619 00119 NM 2001 6 19 AALA20010990 1 20010507 A 5330 SKIN BOEING 727 727227 1384078 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AA 20611 TUL - FOUND CORROSION ON SKIN BL 3L AT STATION 720 PLUS 7. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER IAW S RM 53-30-3. TREATED AND PRIMED ALL PARTS IAW MM 51-20-0. (M) 2 L 7 3 4F A3WE 2001061900120 20010619 00120 NM 2001 6 19 AALA20010991 1 20010430 A 5330 SKIN BOEING 727 727227 1384078 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AA 20611 TUL - FOUND CORROSION ON SKIN OUTBOARD OF STRINGER 27R. CUTOUT LIMIT AREA FABRICATED AND INSTALLED DOUBLER IAW SRM 53-3 0-3. TREATED AND PRIMED AREA DOUBLER IAW MM 51-20-0. 2 L 7 3 4F A3WE 2001061900121 20010619 00121 NM 2001 6 19 AALA20010992 1 20010509 A 5711 SPAR BOEING 727 727227 1384078 NM WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AA 20611 TUL - FOUND CORROSION ON FRONT SPAR UPPER CHORD ABOVE NR 5 SLAT ACTUATOR. INSTALLED REPAIR ANGLE PER ESO 11697, DATED 5 -1-01. (M) 2 L 7 3 4F A3WE 2001061900122 20010619 00122 NM 2001 6 19 AALA20010993 1 20010428 A 5730 SKIN BOEING 727 727227 1384078 NM CENTER WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AA 20611 TUL - FOUND CORROSION ON LOWER SURFACE OF CENTER SECTION WING SKIN RBL 30 BETWEEN STRINGER 4 AND STRINGER 5. INSTALLED DOUBLER AND TRIPLER PER SRM 57-30-3 FIG 10. (M) 2 L 7 3 4F A3WE 2001061900123 20010619 00123 NM 2001 6 19 AALA20010994 1 20010508 A 5330 SKIN BOEING 727 727227 1384078 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AA 20611 TUL - FOUND SKIN LAP 20L AND FASTENER ABOVE BULGED AND BROKEN STATION 1148. REMOVED CORROSION, INSTALLED DOUBLER PER SR M 53-30-3. (M) 2 L 7 3 4F A3WE 2001061900124 20010619 00124 NM 2001 6 19 AALA20010995 1 20010509 A 5313 STRINGER BOEING 727 727227 1384078 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AA 20611 TUL - FOUND SKIN BULGE STATION 720 PLUS 6 STRINGER 23L, FOUND CORROSION ON STRINGER 23L, STATION 720 PLUS 6. INSTALLED SHIM AND STRINGER SPLICE AT STATION 720 PLUS 6 STRINGER 23L PER SRM 53-10-3. REMOVED CORROSION BY CUTTING OUT. (M) 2 L 7 3 4F A3WE 2001061900125 20010619 00125 EU 2001 6 19 AALA20011002 1 20010509 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14053 420 TUL - FOUND FRAME 18 TO FRAME 19 STRINGER 53R IS CORRODED, 2 INCHES BY 1 INCH. INSTALLED NEW STRINGER AT FRAME 18 TO FR AME 19 PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 2001061900126 20010619 00126 EU 2001 6 19 AALA20010997 1 20010509 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14053 420 TUL - FOUND FRAME 18 STRINGER 54R TO 53R SHEAR TIE CORRODED. INSTALLED NEW FRAME SECTION PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 2001061900127 20010619 00127 EU 2001 6 19 AALA20010998 1 20010509 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14053 420 TUL - FOUND FRAME 18 STRINGER 53R TO STRINGER 52R SHEAR TIE CORRODED, 3 INCHES BY 2 INCHES. INSTALLED NEW FRAME SECTION PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 2001061900128 20010619 00128 EU 2001 6 19 AALA20010999 1 20010509 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14053 420 TUL - FOUND FRAME 18 STRINGER 52R TO 51R HAS CORROSION ON SHEAR TIE, 1 INCH BY 2 INCHES, BS 1336. INSTALLED NEW FRAME S ECTION PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 2001061900129 20010619 00129 EU 2001 6 19 AALA20011000 1 20010509 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14053 420 TUL - FOUND FRAME 18 STRINGER 50R TO 49R CORROSION ON SHEAR TIE, FS 1336. INSTALLED NEW FRAME SECTION FRAME 18 STRINGER 50R TO 49R PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 2001061900130 20010619 00130 EU 2001 6 19 AALA20011001 1 20010509 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14053 420 TUL - FOUND FRAME 18 STRINGER 51R TO 50R, CORRODED ON SHEAR TIE, BS 1336. INSTALLED NEW FRAME SECTION PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 2001061900131 20010619 00131 WP 2001 6 19 CALA0100559 1 20010619 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP FS 148-160 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND MAIN CABIN PAN SUPPORT CORRODED AT FS 148-160, RBL 54. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS IN STALLED IAW SRM 51-30-2, 53-11, FIGURE 22, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 2001061900132 20010619 00132 EU 2001 6 19 AALA20011003 1 20010509 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14053 420 TUL - FOUND CORROSION ON STRINGER 53 RIGHT OUTBOARD OF ELECTRICAL POWER BOX, FS 1336, 3 INCHES BY 1 INCH. INSTALLED NEW STRINGER PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 2001061900133 20010619 00133 NM 2001 6 19 PCAA0106056 1 20010616 A 3350 61047811 BATTERY DHAV DHC8 DHC8102 2809003 NM POSITION 100 DISCHARGED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 830EX 155 MDT- DURING ROUTINE MAINTENANCE VISIT FORWARD LEFT HAND EGRESS AND PASSENGER DOOR OVERHEAD EMERGENCY EXIT SIGN LIGHTS FO UND INOPERATIVE. BATTERY PACK AT POSITION 100 REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001061900134 20010619 00134 EU 2001 6 19 AALA20011004 1 20010509 A 5320 STRINGER CLIP AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14053 420 TUL - FOUND FRAME 18 STRINGER 51R STRINGER CLIP IS CORRODED, FS 1336. INSTALLED NEW STRINGER CLIP AT FRAME 18 STRINGER 51R PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 2001061900135 20010619 00135 EU 2001 6 19 AALA20011005 1 20010509 A 5320 STRINGER CLIP AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14053 420 TUL - FOUND FRAME 18 STRINGER 52R STRINGER CLIP IS CORRODED. INSTALLED NEW STRINGER CLIP AT FRAME 18 STRINGER 52R PER S RM 51-72-10. (M) 2 L 7 2 4F RT A35EU 2001061900136 20010619 00136 EU 2001 6 19 AALA20011006 1 20010508 A 5330 SKIN AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14053 420 TUL - FOUND AREA OF LOWER FUSELAGE SKIN BULGED APPROX 1.5 SQUARE INCHES LOCATED BETWEEN FS 18-19 OF THE NOSE GEAR CUTOUT AFT DOUBLER, LEFT FINGER CORROSION IS AT PREVIOUS REPAIR EDGE. AREA REPAIRED PER ESO 30595 DATED 5/8/2001. (M) 2 L 7 2 4F RT A35EU 2001061900137 20010619 00137 NM 2001 6 19 PCAA0106055 1 20010617 A 3350 82410162005 CONTROL BOX DHAV DHC8 DHC8102 2809003 NM INOPERATIVE A PCAA K NONE O OTHER NR NOT REPORTED 1 EA 13 817EX 191 MDT- FLIGHT#3754. CREW REPORTED EMERGENCY LIGHTS WILL NOT TURN OFF. MAINTENANCE REPLACED EMERGENCY LIGHT CONTROL BOX. OP ERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001061900138 20010619 00138 NM 2001 6 19 AALA20011007 1 20010514 A 2824 AAP3043A VALVE BOEING 727 727223 1384074 NM NR 3 ENGINE FAILED A AALA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 SW 21 890AA 22006 BNA - FLT 1216 - EN ROUTE DFW-PHL, AIR INTERRUPTED BNA, AFTER NR 3 ENGINE FLAME OUT AND NO FUEL TRANSFER FROM NR 2 TANK. REPLACED NR 2 CROSSOVER FEED VALVE. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001061900140 20010619 00140 NM 2001 6 19 AALA20011010 1 20010509 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 877AA 21389 TUL - FOUND FLOORBEAM HAS CORROSION ON TOP FLANGE. FIXED IT PER ESO 11697 DATED 5/9/01. (M) 2 L 7 3 4F A3WE 2001061900141 20010619 00141 NM 2001 6 19 AALA20011011 1 20010510 A 5311 BELTFRAME BOEING 727 727223 1384074 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 877AA 21389 TUL - FOUND BELTFRAME DENTED AND CRACKED AT STATION 500 JUST ABOVE STRINGER 24. FABRICATED AND INSTALLED REPAIR DOUBLER ON BELT FRAME AT STATION 500 ABOVE STRINGER 24R PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 2001061900142 20010619 00142 WP 2001 6 19 AALA20011017 1 20010510 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 410AA 49321 AUS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS DIM. REPLACED EMERGENCY EXIT ESCAPE PATH LIGHT BA TTERY PACK. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001061900143 20010619 00143 2001 6 19 AALA20011022 4 20010511 A 3425 UNI1108 COMPUTER BOEING 777 777223 1385213 NM COCKPIT FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 792AN 30253 DFW - FLT 48 - SAARU STATUS MESSAGE APPEARED IN FLIGHT ACCOMPANIED BY STANDBY ATTITUDE INDICATIONS FAILED. TROUBLESHOT FOUND MM 34-30700 HAS AN INTERNAL FAULT IN SAARU. PER F/M REMOVED AND REPLACED SAARU. ACCOMPLISHED OPERATIONAL CHECK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT T00001SE 2001061900144 20010619 00144 NM 2001 6 19 AALA20011024 1 20010509 A 5730 SKIN BOEING 727 727227 1384078 NM WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AA 20611 TUL - FOUND CORROSION UNDER PLENUM ATTACH ANGLE, BETWEEN STRINGER 5 AND 7, RIGHT SIDE, INBOARD FLANGE RBL 15. ACCOMPLIS HED REPAIR PER SRM 57-30-1, 51-10-6 AND ESO 11697 DATED 5-4-01. (M) 2 L 7 3 4F A3WE 2001061900145 20010619 00145 NM 2001 6 19 AALA20011025 1 20010514 A 5330 148N3211 SKIN BOEING 757 757223 1384957 NM FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 622AA 24580 TUL - FOUND FUSELAGE SKIN DAMAGE EITHER SIDE OF STRINGER 17 AND STATION 1720 TO 1730. REMOVED DAMAGED AREA AND INSTALLE D DOUBLER PER SRM 53-00-01-2. (M) 2 L 7 2 4F RT A2NM 2001061900146 20010619 00146 NM 2001 6 19 AALA20011026 1 20010501 A 5312 PRESSURE PANEL BOEING 727 727227 1384078 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AA 20611 TUL - FOUND TWO CRACKS ON UPPER PRESS DECK AT STATION 290 IN NLG W/W. STOP DRILLED CRACKS AND INSTALLED DOUBLER PER SRM 53-10-9. (M) 2 L 7 3 4F A3WE 2001061900147 20010619 00147 NM 2001 6 19 AALA20011027 1 20010510 A 5510 BEAM BOEING 727 727227 1384078 NM HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AA 20611 TUL - FOUND CORROSION ON HORIZONTAL STABILIZER UPPER T/E BEAM 2 PLACES, 4 INCHES BY 1 INCH AND 5 INCHES BY 1 INCH. BLEN DED OUT CORROSION AND INSTALLED 2024T3.063 DOUBLER PER ESO 11697 DATED 5-10-01. (M) 2 L 7 3 4F A3WE 2001061900148 20010619 00148 NM 2001 6 19 AALA20011028 1 20010510 A 5313 STRINGER BOEING 727 727227 1384078 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AA 20611 TUL - FOUND STRINGER 21L CORRODED STATION 720B. COMPLETED STRINGER REPAIR AS PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 2001061900149 20010619 00149 NM 2001 6 19 AALA20011029 1 20010510 A 5712 RIB BOEING 727 727227 1384078 NM WING CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AA 20611 TUL - FOUND CRACK IN RADIUS AT LEFT STATION 760 RIB CHORD. ROUTED OUT DAMAGE. INSTALLED REPAIR PER S/B 727-57-0112 AND ESO 11697 DATED 5/9/01. (M) 2 L 7 3 4F A3WE 2001061900150 20010619 00150 WP 2001 6 19 AALA20011030 1 20010515 A 3350 SOCKET DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 588AA 53251 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHT AT SEAT 15D INOPERATIVE. REPLACED EMERGENCY EXIT E SCAPE PATH LIGHT SOCKET AT SEAT 15D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001061900151 20010619 00151 WP 2001 6 19 AALA20011031 1 20010516 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 77421 49333 ORD - DURING OVERNIGHT MAINTENANCE, AFT LEFT SIDE EMERGENCY EXIT ESCAPE PATH LIGHTS DIM. REPLACED BATTERY PACK FOR AFT LEFT SIDE EMERGENCY EXIT ESCAPE PATH LIGHTS. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001061900152 20010619 00152 WP 2001 6 19 AALA20011034 1 20010515 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7512A 49806 DFW - DURING OVERNIGHT MAINTENANCE, AFT LOWER EMERGENCY EXIT SLIDE LIGHT DID NOT ILLUMINATE. REPLACED AFT LOWER EMERGEN CY EXIT SLIDE LIGHT BATTERY PACK. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001061900153 20010619 00153 WP 2001 6 19 AALA20011036 1 20010515 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 286AA 49298 BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS ROWS 17 THROUGH 21 AND 22 THROUGH 27 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT ESCAPE PATH LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001061900154 20010619 00154 NM 2001 6 19 AALA20011037 1 20010516 A 3350 LIGHT BOEING 767 767223 1385123 NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 312AA 22315 SFO - DURING OVERNIGHT MAINTENANCE, R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT ASSEMBLY INOPERATIVE. UNABLE TO ACCESS LIGHT ASSEMBLY WITHOUT REMOVING GALLEY. AWAITING MAINTENANCE SCHEDULING. (M) 2 L 7 2 4F RT A1NM 2001061900155 20010619 00155 WP 2001 6 19 AALA20011038 1 20010510 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3515 49892 TUL - FOUND CORROSION NR 2 SEAT TRACK STATION 1300, 1251, AND 1287. INSTALLED NEW SECTION OF NR 2 SEAT TRACK FROM STATI ON 1240 TO 1309 PER SRM 53-05 FIG NR 4F. (M) 2 L 7 2 4F A6WE 2001061900156 20010619 00156 WP 2001 6 19 AALA20011045 1 20010503 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 TUL - FOUND PITTING CORROSION, NR 6 SEAT TRACK, STATION 392. ACCOMPLISHED SEAT TRACK PLUG REPAIR PER SRM 53-05 PART NR 1, FIG 4. TREATED AND PRIMED PER SRM 53-10-3. (M) 2 L 7 2 4F RT A6WE 2001061900157 20010619 00157 WP 2001 6 19 AALA20011046 1 20010507 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3515 49892 TUL - FOUND CORROSION ON CUSP 1.5 INCH BY 1 INCH THROUGH CUSP. CUT OUT DAMAGED CORROSION INSTALLED DOUBLER PER SRM 53-0 1 FIG 4. (M) 2 L 7 2 4F A6WE 2001061900158 20010619 00158 2001 6 19 RAIA00106008 4 20010615 A 3420 HG2010AC02 COMPUTER EMB 145 EMB145ER SO AVIONICS BAY FAILED A RAIA C ABORTED TAKEOFF I FLT. ATTITUDE INST. TO TAKEOFF 1 CE 03 808HK 5772 971 145157 5252-RIC-RIGHT AHRS COMPUTER FAILED DURING POWER UP FOR TAKEOFF. MAINTENANCE INSPECTED AND REPLACED RIGHT AHRS COMPUTER. 2 L 7 2 4F RT T00011AT 2001061900159 20010619 00159 EU 2001 6 19 RAIA00106009 1 20010618 A 2430 8260121 GENERATOR AEROSP ATR72 ATR72202 8680940 EU LEFT ENGINE INTERMITTENT A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 722TE 220 7324-STL-DC BUS WENT OFFLINE TWICE WHILE TAXIING. MAINTENANCE INSPECTED AND REPLACED LEFT STARTER GENERATOR. 2 H 7 2 4T RT A53EU 2001061900160 20010619 00160 NM 2001 6 19 F3LA200100091 1 20010615 A 2782 654476224 ACTUATOR BOEING 737 73736Q 1384409 NM NO. 5 L.E. SLAT LEAKING A F3LA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 03 307FL 56 28760 AIR TURN BACK. FLIGHT CREW REPORTED "B" SYSTEM ENGINE DRIVEN HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED AND LOSS OF "B" SYSTEM HYDRAULIC FLUID. MAINTENANCE REPLACED NO. 2 ENGINE DRIVEN HYDRAULIC PUMP AND NO. 5 LEADING EDGE SLAT ACTUATO R. 2 L 7 2 4F RT A16WE 2001061900161 20010619 00161 NM 2001 6 19 F3LA200100092 1 20010616 A 3260 SENSOR BOEING 737 7373Q8 1384670 NM INOPERATIVE A F3LA O OTHER J WARNING INDICATION CR CRUISE 1 NM 03 318FL 64 26293 ENROUTE, FLIGHT CREW REPORTED NOSE GEAR RED LIGHT ILLUMINATED AND REMAINED ILLUMINATED THROUGHOUT NORMAL AND MANUAL GEAR ACTUATION. MAINTENANCE REPLACED SENSORS S-485 AND S-486 PER MM 32-61-41 AND WDM 32-64-01. PERFORMED SYSTEM CHECKS PER MM 32-33-00 AND CHECKED NORMAL. 2 L 7 2 4F RT A16WE 2001062000001 20010620 00001 NM 2001 6 20 OZIA013125001 1 20010224 A 2750 001A270A0002130 TORQUE TUBE DORNER DO32 DO328300 NM OUT OF TOLERANCE A OZIA K NONE G MULTIPLE FAILURE CR CRUISE 1 CE 05 410Z 2192 3125 Severe turbulence caused autopilot disconnect, FDR fail; subsequent smell of smoke in cockpit, frost on inside of side c ockpit windows, howling sound all of which disappeared after approximately 5-10 minutes. Aircraft ferried to SAT for sev ere turbulence inspection.Severe turbulence inspection performed by Fairchild Aircraft Services. Found a defect in the f lap torque tube. Removed and replaced torque tube. Torque tube sent for NDT. X-rays revealed the paint was cracked and t he tube assembly was not cracked. 2 H 7 2 4T RT A55NM 2001062000002 20010620 00002 SO 2001 6 20 C2XA01IA270 1 20010619 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16729 120185 IAH - DURING A-CHECK INSPECTION, THE AISLE PATH EMERGENCY EXIT LIGHTS WERE FOUND TO BE MALFUNCTIONING. MAINTENANCE REMOV ED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001062000003 20010620 00003 WP 2001 6 20 AALA20011047 1 20010510 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3515 49892 TUL - FOUND CORROSION ON CUSP STATION 1250 THROUGH 1308. INSTALLED NEW CUSP SHEET STATION 1250 THROUGH 1308 SRM 51-01. (M) 2 L 7 2 4F A6WE 2001062000004 20010620 00004 WP 2001 6 20 AALA20011048 1 20010508 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3515 49892 TUL - FOUND STATION 1170 LEFT CUSP CORRODED UNDER FLOOR. INSTALLED DOUBLER PER AARD 53-00-00-2 AND SRM 53-0 FIG 43. (M ) 2 L 7 2 4F A6WE 2001062000005 20010620 00005 WP 2001 6 20 AALA20011049 1 20010509 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3515 49892 TUL - FOUND LEFT CUSP CORRODED STATION 1174 TO 1250. REPLACED LEFT CUSP STATION 1174-1250 PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2001062000006 20010620 00006 WP 2001 6 20 AALA20011050 1 20010515 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3515 49892 TUL - FOUND VARIOUS SPOTS OF CORROSION ON CUSP T FROM STATION 185 TO STATION 232 RIGHT AT FORWARD SERVICE DOOR. SPLICED IN NEW CUSP T ANGLE PER SRM 53-05 PART 1 FIGURE 55 SHEET 2. (M) 2 L 7 2 4F A6WE 2001062000007 20010620 00007 WP 2001 6 20 AALA20011051 1 20010502 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 TUL - FOUND UPPER SURFACE OF CUSP CORROSION RIGHT STATION 500. REPAIR DOUBLER INSTALLED AS PER SRM 53-01 FIG 4 SH 3. ( M) 2 L 7 2 4F RT A6WE 2001062000008 20010620 00008 WP 2001 6 20 AALA20011052 1 20010507 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 TUL - FOUND DEEP GOUGE IN RIGHT CUSP WEB APPROX STATION 313. CUT OUT DAMAGE, DRILLED DOUBLER, .032, 7025T6, INSTALLED F ASTENERS, PER SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2001062000009 20010620 00009 WP 2001 6 20 AALA20011055 1 20010507 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 TUL - FOUND DEEP BLENDOUT AREA OF FUSELAGE SKIN AT LONGERON 22R APPROX STATION 304. INSTALLED DOUBLER. REMOVED REPAIR FORWARD OF DAMAGE AND INCORPORATED INTO NEW REPAIR PER 53-04 FIG 38. (M) 2 L 7 2 4F RT A6WE 2001062000010 20010620 00010 WP 2001 6 20 AALA20011062 1 20010508 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 TUL - FOUND LEFT TIE DOWN TRACK CORRODED FS 1117, 1174-1206. REMOVED AND REPLACED SECTION OF LEFT TIE DOWN TRACK FROM S TATION 1007-1221. (M) 2 L 7 2 4F RT A6WE 2001062000011 20010620 00011 WP 2001 6 20 AALA20011063 1 20010515 A 5240 HANDLE DOUG DC9 DC983 3022083 WP SERVICE DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 TUL - FOUND DOOR HANDLE MECH, FORWARD GALLEY SERVICE DOOR, SLEEVES HAS CORROSION BETWEEN SLEEVES. REMOVED AND REPLACED DOOR HANDLE MECHANISM WITH SERVICEABLE PER ESO 80177. (M) 2 L 7 2 4F RT A6WE 2001062000012 20010620 00012 WP 2001 6 20 AALA20011065 1 20010508 A 5320 BRACKET DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 TUL - FOUND CORROSION ON DOOR CUTOUT LOWER ATTACH CORNER CURVED BRACKET. INSTALLED SERVICEABLE BRACKET SRM 51-01. (M) 2 L 7 2 4F RT A6WE 2001062000013 20010620 00013 NM 2001 6 20 AALA20011066 1 20010515 A 5711 SPAR BOEING 757 757223 1384957 NM RT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 622AA 24580 TUL - FOUND CORROSION AT RIGHT WING AFT SPAR BOOST PUMP LOWER BOND JUMPER AREA. REPAIR PER ESO 90309 DATED 05-15-2001. (M) 2 L 7 2 4F RT A2NM 2001062000014 20010620 00014 WP 2001 6 20 AALA20011069 1 20010508 A 5320 FITTING DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 TUL - FOUND CORROSION ON DOOR CUTOUT LOWER AFT CORNER FITTING. INSTALLED NEW CORNER FITTING SRM 51-01. (M) 2 L 7 2 4F RT A6WE 2001062000015 20010620 00015 WP 2001 6 20 AALA20011070 1 20010511 A 5310 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 TUL - FOUND DOOR JAMB WEB CRACKED STATION 208 LONGERON 15L. INSTALLED DOUBLER PER AARD 53-10-00-11. (M) 2 L 7 2 4F RT A6WE 2001062000016 20010620 00016 WP 2001 6 20 AALA20011072 1 20010504 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 TUL - FOUND AREA OF CORROSION AT GALLEY TIE DOWN AND FLOOR DIAPHRAGM. REMOVED SECTION OF CORRODED DIAPHRAGM AND INSTALL ED DOUBLER PER AARD 53-00-00-2. (M) 2 L 7 2 4F RT A6WE 2001062000017 20010620 00017 WP 2001 6 20 AALA20011074 1 20010507 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 TUL - FOUND GOUGE IN SUBFLOOR STATION 200 RBL 21. REMOVED DAMAGE, INSTALLED DOUBLER PER AARD 53-00-00-00-02 PAGE 1. (M ) 2 L 7 2 4F A6WE 2001062000018 20010620 00018 WP 2001 6 20 AALA20011075 1 20010510 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 TUL - FOUND FORWARD SERVICE DOOR JAMB FRAME GOUGED LOWER AFT CORNER. REMOVED AND REPLACED FORWARD SERVICE DOOR JAMB ASS EMBLY 4002982 PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2001062000019 20010620 00019 WP 2001 6 20 AALA20011076 1 20010514 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 TUL - FOUND SMALL GOUGE IN MEMBRANE STATION 198 RBL 16. ACCOMPLISHED DOUBLER REPAIR 7075 T-6.026 AFTER DAMAGED AREA CUT OUT AS PER AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 2001062000020 20010620 00020 WP 2001 6 20 AALA20011077 1 20010511 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3515 49892 TUL - FOUND CANT FRAME 1485 IS CRACKED AT STAIR ACTUATOR CASTING. INSTALLED REPAIR SPLICE AS PER AARD 53-10-00-33. (M) 2 L 7 2 4F A6WE 2001062000021 20010620 00021 WP 2001 6 20 AALA20011079 1 20010508 A 5310 BEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3515 49892 TUL - FOUND CORROSION ON AFT CARGO DOOR JAMB BEAM FROM STATION 1160-1208. REPLACED DOOR BEAM PER SRM 51-30-5. (M) 2 L 7 2 4F A6WE 2001062000022 20010620 00022 WP 2001 6 20 AALA20011082 1 20010515 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 228AA 49178 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY CEILING LIGHTS FROM ROWS 26 THROUGH 29 DIM. REPLACED BATTERY PACK FOR EME RGENCY CEILING LIGHTS AT ROW 26 THROUGH 29. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001062000023 20010620 00023 NM 2001 6 20 AALA20011084 1 20010515 A 5320 ANGLE BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 622AA 24580 TUL - FOUND CORROSION ON HORIZONTAL CHORD ANGLE AT STATION 1180 LEFT W/W. REPAIR PER SRM 51-70-11-0 AND ESO90309 DATED 5-15-2001. (M) 2 L 7 2 4F RT A2NM 2001062000024 20010620 00024 EU 2001 6 20 AALA20011085 1 20010516 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70072 515 TUL - FOUND CORROSION. INSTALLED STRAP REPAIR PER ESO 30595 DATED 5/15/01 TRACK TO BE REPLACED AT MBU 8. (M) 2 L 7 2 4F RT A35EU 2001062000025 20010620 00025 WP 2001 6 20 AALA20011087 1 20010519 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 561AA 53091 ORD - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY LIGHTS BETWEEN SEATS 26 THROUGH 29 DIM. REPLACED AFT CEILING EMER GENCY LIGHT PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001062000026 20010620 00026 WP 2001 6 20 AALA20011089 1 20010518 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 597AA 53287 DFW - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY LIGHTS ABOVE SEAT 18 THROUGH 22 INOPERATIVE. REPLACED BATTERY PAC K FOR CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001062000027 20010620 00027 WP 2001 6 20 AALA20011090 1 20010521 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 451AA 49477 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS ROWS 3 THROUGH 19 INOPERATIVE. REPLACED FORWARD A ND AFT EMERGENCY EXIT ESCAPE PATH BATTERY PACKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001062000028 20010620 00028 WP 2001 6 20 AALA20011091 1 20010520 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 286AA 49298 DFW - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY LIGHTS ABOVE SEATS ROWS 13 THROUGH 15 DIM. REPLACED CEILING EMERG ENCY LIGHTS BATTERY PACK ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001062000029 20010620 00029 WP 2001 6 20 AALA20011092 1 20010521 A 3350 4008751 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 471AA 49601 LAX - DURING OVERNIGHT MAINTANANCE, EMERGENCY EXIT ESCAPE PATH LIGHT SEAT 24 INOPERATIVE. REPLACED EMERGENCY EXIT ESCAP E PATH LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001062000030 20010620 00030 NM 2001 6 20 AALA20011095 1 20010517 A 5730 SKIN BOEING 757 757223 1384957 NM LT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 622AA 24580 TUL - FOUND 3 INCH BY 15 FT OF CORROSION ON LEFT WING SKIN SURFACE (UPPER) 1 INCH OUTBOARD OF WING TO BODY FAIRING ALONG BLACK STRIPE. SEE ESO 90309 DATED 5/16/2001. (M) 2 L 7 2 4F RT A2NM 2001062000031 20010620 00031 NM 2001 6 20 AALA20011096 1 20010517 A 5330 143N3340 SKIN BOEING 757 757223 1384957 NM FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 645AA 24603 TUL - FOUND TWO SMALL DENTS IN FUSELAGE SKIN 6 INCHES FORWARD AND 8 INCHES TO THE RIGHT OF E/E COMPT DOOR. REMOVED DAMA GE AND INSTALLED DOUBLE PER SRM 53-00-01-2. (M) 2 L 7 2 4F RT A2NM 2001062000032 20010620 00032 NM 2001 6 20 AALA20011097 1 20010517 A 5330 SKIN BOEING 757 757223 1384957 NM FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 645AA 24603 TUL - FOUND TWO DENTS IN FUSELAGE SKIN 6 INCHES FORWARD AND 8 INCHES TO THE RIGHT OF E/E COMP DOOR. DOUBLER INSTALLED P ER SRM 53-00-01-2. (M) 2 L 7 2 4F RT A2NM 2001062000033 20010620 00033 NM 2001 6 20 AALA20011099 1 20010519 A 3350 LIGHT BOEING 767 767223 1385123 NM CABIN INTERMITTENT A AALA K NONE O OTHER CR CRUISE 1 SW 21 301AA 22307 JFK - FLT 282 - EN ROUTE SAN-JFK - FLIGHT ATTENDANT REPORTED EMERGENCY EXIT ESCAPE PATH LIGHTS ON RIGHT SIDE OF CABIN RO W 30 AND AFT FUNCTIONED INTERMITTENTLY. PERFORMED EMERGENCY EXIT ESCAPE PATH LIGHT TEST. NO DEFECTS NOTED. SYSTEM GRO UND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001062000034 20010620 00034 WP 2001 6 20 AALA20011100 1 20010521 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 203AA 49145 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY DOOR PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED PORTABLE EMERGENC Y LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001062000036 20010620 00036 WP 2001 6 20 AALA20011103 1 20010518 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP TAILCONE DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 578AA 53155 ATL - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS FOR TAILCONE DROP HANDLE INOPERATIVE. REPLACED BATTERY PACK FOR TA ILCONE DROP HANDLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001062000037 20010620 00037 WP 2001 6 20 AALA20011104 1 20010520 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 294AA 49306 DFW - DURING OVERNIGHT MAINTENANCE, AFT RIGHT OVERHEAD EMERGENCY LIGHTS DIM. REPLACED BATTERY PACK FOR AFT RIGHT OVERHE AD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001062000038 20010620 00038 WP 2001 6 20 AALA20011107 1 20010521 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 426AA 49338 ORD - DURING OVERNIGHT MAINTENANCE, RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK RIGH T FORWARD OVERWING EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001062000039 20010620 00039 NM 2001 6 20 AALA20011108 1 20010518 A 5730 SKIN BOEING 757 757223 1384957 NM RT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 645AA 24603 TUL - FOUND CORROSION ON UPPER RIGHT WING SKIN AT TRAILING EDGE SPLICE WS 100.50 TO WS 369.50. REPAIRED PER ESO 90309 D ATED 5/18/2001. (M) 2 L 7 2 4F RT A2NM 2001062000040 20010620 00040 NM 2001 6 20 AALA20011109 1 20010518 A 5730 SKIN BOEING 757 757223 1384957 NM RT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 645AA 24603 TUL - FOUND CORROSION ON UPPER RIGHT WING SKIN SPLICE AT L/E STATION WS 95 TO WS 565.50. REPAIRED PER ESO 90309 DATED 5 -18-01. (M) 2 L 7 2 4F RT A2NM 2001062000041 20010620 00041 NM 2001 6 20 AALA20011110 1 20010518 A 5730 SKIN BOEING 757 757223 1384957 NM WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 645AA 24603 TUL - FOUND CORROSION UNDER BLACK STRIP AROUND WING WALK AREA FOR EMERGENCY ESCAPE PATH, RBL 70.50 WBL 250. REPAIRED PE R ESO90309 DATED 5-18-01. (M) 2 L 7 2 4F RT A2NM 2001062000042 20010620 00042 WP 2001 6 20 AALA20011111 1 20010518 A 5210 SKIN DOUG DC9 DC982 3022082 WP ENTRY DOOR DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3515 49892 TUL - FOUND 6 INCH DENT ON EXTERIOR SKIN. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 52-05 FIG 37. (M) 2 L 7 2 4F A6WE 2001062000043 20010620 00043 NM 2001 6 20 AALA20011112 1 20010518 A 5730 SKIN BOEING 757 757223 1384957 NM WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 645AA 24603 TUL - FOUND CORROSION ON UPPER SKIN SURFACE AT ROOT NUMEROUS AREAS UNDER WALKWAY PAINT, WS 70 TO WS 177. REPAIRED PER E SO 90309 DATED 5-18-01. (M) 2 L 7 2 4F RT A2NM 2001062000044 20010620 00044 WP 2001 6 20 AALA20011113 1 20010516 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3515 49892 TUL - FOUND CORROSION ON TOP LAYER OF SUBFLOOR RIGHT SIDE STATION 180 TO 179 RBL 48 TO OUTBOARD OF A/C. INSTALLED DOUBL ER AND FILLER PER SRM 53-01 FIG 4. (M) 2 L 7 2 4F A6WE 2001062000045 20010620 00045 NM 2001 6 20 ASA2001F00000 1 20010413 A 3350 8821004 BATTERY BOEING 737 7372Q8C 138448S NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE ON SEAT PALLET 9-4, ROW 16. REMOVED AND REPLAC ED REMOTE ASSEMBLY BATTERY AND RECEIVER, THEN LIGHTS TESTED NORMAL. REF ASAA0110208. (M) 2 L 7 2 4F A16WE 2001062000046 20010620 00046 NM 2001 6 20 ASAA0110205 1 20010409 A 3350 8821004 BATTERY BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROW 16. REMOVED AND REPLACED REMOTE ASSEMBL Y AND LIGHTS OPERATED NORMAL. (M) 2 L 7 2 4F A16WE 2001062000047 20010620 00047 NM 2001 6 20 ASAA0110208 1 20010413 A 3350 88310144 RECEIVER BOEING 737 7372Q8C 138448S NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE ON SEAT PALLET 9-4, ROW 16. REMOVED AND REPLAC ED REMOTE ASSEMBLY BATTERY AND RECEIVER, THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F A16WE 2001062000048 20010620 00048 NM 2001 6 20 ASAA0110209 1 20010413 A 3350 883200312 RECEIVER BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE ON SEAT PALLET 6-4, ROW 11. REMOVED AND REPLAC ED REMOTE ASSEMBLY RECEIVER, THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2001062000049 20010620 00049 NM 2001 6 20 ASAA0110210 1 20010414 A 3350 86210144 BATTERY BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE ON SEAT PALLETS 10-11 AND 7-9. REMOVED AND REP LACED REMOTE ASSEMBLY BATTERIES, THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2001062000050 20010620 00050 NM 2001 6 20 ASAA0110211 1 20010416 A 3350 883200312 RECEIVER BOEING 737 737298C 1384490 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE ON SEAT PALLETS 1-4 AND 2-11. REMOVED AND REPL ACED REMOTE ASSEMBLY BATTERIES AND RECEIVER IN PALLET 1-4, AND REMOTE ASSEMBLY RECEIVER IN PALLET 2-11, THEN LIGHTS TEST ED NORMAL. (M) 2 L 7 2 4F RT A16WE 2001062000051 20010620 00051 NM 2001 6 20 ASAA0110218 1 20010416 A 3350 883200312 RECEIVER BOEING 737 737210C 1384459 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY TRACK LIGHTS WOULD NOT TEST USING COCKPIT SWITCH. REMOVED AND REPLACED THREE REMOTE ASSEMBLY BATTERIES AND ONE REMOTE ASSEMBLY RECEIVER AT ROW 16, THEN LIGHTS OPERATED NORMAL. (M) 2 L 7 2 4F A16WE 2001062000052 20010620 00052 NM 2001 6 20 ASAA0110219 1 20010417 A 3350 88210044 BATTERY BOEING 737 7372Q8C 138448S NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY TRACK LIGHTS AND EXIT LIGHTS ON THE SMOKE BARRIER WOULD NOT TEST AFTER A IRCRAFT RECONFIGURATION. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERIES ON THE SMOKE BARRIER AND THE AFT MOST SEAT PALL ET, THEN LIGHTS OPERATED NORMAL. (M) 2 L 7 2 4F A16WE 2001062000056 20010620 00056 NE 2001 6 20 20010531CW004 2 20010507 A 7320 32908001 CONTROL VALVE GARRTT MTSBSI MU300 MU30010 5781300 CE PWA JT15 JT15D4 52112 NE ECU CRACKED B FGQR K NONE O OTHER IN INSP/MAINT 1 SO 01 703JH 13 40125 A010SA CRACKED WHERE DIAPHRAGM AND VALVE MEET. BAD CASTING OR DESIGN FLAW. 2 H 7 2 4F 4 F RT A14SW E1NE 2001062000057 20010620 00057 EU 2001 6 20 20010531CW005 1 20010509 A 2120 66434303053 DUCT ISRAEL GALAXY GALAXY 4500307 EU CABIN LEAKING B UO2R K NONE O OTHER NR NOT REPORTED 1 GL 19 414KD 022 RIGHT HAND UPPER AIR DUCT WAS FOUND TO BE LEAKING AT FACTORY SEALED SEAMS CAUSING LOW AIRFLOW TO RIGHT SIDE OF CABIN CON DITIONED AIR OUTLETS. 2 L 7 2 4F RT A53NM 2001062000058 20010620 00058 CE 2001 6 20 20010601CW001 1 20010509 A 3233 4379826 ROD END WESTERNHYD CESSNA 402 402C 207590R CE NLG WORN D K NONE O OTHER IN INSP/MAINT 1 SW 01 2711X 402C0116 DURING NOSE GEAR DRAG BRACE REPLACEMENT, WHEN RIGGING NLG ACTUATOR, FOUND ROD END LOOSE IN FEMALE THREADS OF PISTON, REP LACED PISTON ROD WITH SERVICEABLE UNIT. PROBABLE CAUSE: INCORRECT RIGGING OF NLG ROD END. 1 L 7 2 3O A7CE 2001062000060 20010620 00060 CE 2001 6 20 20010601CW003 1 20010320 A 7603 STOP PIN BEECH BEECH 1900 1900C 1154161 CE POWER LEVER LOOSE A YADA K NONE O OTHER NR NOT REPORTED 1 AL 03 41UE ACE786008 UC41 PIN TO ARM WELD JOINT FAILED AND ALLOWED PIN TO MOVE/FALL OUT OF ARM (STOP PIN REPLACED BY FLEET SUPPORT SERVICES AT PRE VIOUS REPAIR). WITH PIN OUT OF LOCATION, POWER LEVER REVERSE WHILE IN FLIGHT. THIS HAS BEEN A CONTINUING PROBLEM WITH FLEET REPAIRED UNITS AND WE HAVE STOPPED USING REPAIRED POWER LEVERS DUE TO CONTINUAL FAILURE OF THIS PIN ATTACHMENT. 2 L 7 2 4T RT A24CE 2001062000067 20010620 00067 CE 2001 6 20 20010601CW010 1 20010511 A 2823 169920000 SELECTOR VALVE BEECH 23 C23 1151242 CE FUEL SYS DAMAGED B K NONE O OTHER IN INSP/MAINT 1 GL 13 9743L M1371 THIS FUEL VALVE DID NOT MEET THE CRITERIA OF MFG S.B.. THE RUNNING TORQUE OF THE VALVE WAS VERY HARD TO MOVE. WHEN TE STED WITH A TORQUE WRENCH IT EXCEEDED 25 INCH POUNDS. THE FUEL VALVE WAS DISASSEMBLED FOR LUBRICATION AND VALVE CONE WA S FOUND TO BE SEVERELY SCORED. THE VALVE WAS REPLACED WITH A NEW FUEL VALVE KIT NR 2390151S. 1 L 7 1 3O A1CE 2001062000068 20010620 00068 NM 2001 6 20 20010601CW011 1 20010501 A 3260 656021132 ACCESSORY UNIT BOEING 727 727225 1384077 NM E/E BAY DEFECTIVE A RYNA O OTHER N FALSE WARNING AP APPROACH 1 CE 07 801EA 22432 ON APPROACH, LANDING GEAR INDICATOR SHOWED 3 GREEN LIGHTS AND RIGHT MAIN UNSAFE LIGHT. DECLARED AN EMERGENCY. FOLLOWED REQUIRED PROCEDURE AND AIRCRAFT LANDED WITHOUT INCIDENT. CORRECTION: REPLACED LANDING GEAR ACCESSORY UNIT. TESTED RI GHT MAIN LANDING GEAR DOWNLOCK SENSOR. OPERATIONAL CHECK GOOD. 2 L 7 3 4F A3WE 2001062000069 20010620 00069 NM 2001 6 20 20010601CW012 1 20010505 A 3260 MS24266R16B74S CONNECTOR BOEING 727 72777C 1380420 NM COCKPIT LOOSE A RYNA O OTHER N FALSE WARNING AP APPROACH 1 CE 07 526PC 20370 NO GEAR LIGHT WITH LANDING GEAR DOWN. EMERGENCY DECLARED. CORRECTION: RESECURED CANNON PLUG ON BACK OF LANDING GEAR LIGHT ASSEMBLY. LIGHTS OPERATE NORMAL. 2 L 7 3 4F A3WE 2001062000070 20010620 00070 SO 2001 6 20 20010601CW013 1 20010509 A 3242 ARM10195 CLIP DUNLOP GULSTM GV GV SO BRAKE ROTOR SHEARED E UG8A K NONE O OTHER NR NOT REPORTED 1 GL 23 920DC 1545 VS100 534 NR 1 BRAKE, OUTBOARD ROTOR, DRIVE CLIPS FAILED AND SHEARED OFF THE ROTOR. EIGHT(8) SHEARED OFF OUT OF SIXTEEN (16) TOTA L PER ROTOR. CAUSE: THE CARBON FIBER ROTOR MATERIAL, FAILED. BRAKE WAS REPLACED WITH OVERHAULED UNIT. NO OTHER DAMA GE WAS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A12EA 2001062000071 20010620 00071 CE 2001 6 20 20010601CW014 1 20010515 A 4960 CIRCUIT BOARD RAYTHN DH125 HAWKER800XP CE APU CONTROL DEFECTIVE B UO2R K NONE O OTHER IN INSP/MAINT 1 GL 19 801WB 2867 258287 DEEC/COMPUTER CIRCUITS (NR 1 AND NR 2) DESIGN DOES NOT UTILIZE THE OVERSPEED PROTECTION THAT THE DEEC IS CAPABLE OF PERF ORMING. WHEN PILOT SELECTS THE OVERSPEED PROTECTION POSITION WITH THE COMPUTER SWITCH (NR 1 AND NR 2) THE PROTECTION WI LL NOT BE ACTIVATED WITHIN THE DEEC. WIRE MISSING TO PROVIDE OVERSPEED CONDITION WHEN SELECTED TO OVERSPEED PROTECTION SWITCH POSITION. APU DOES NOT MATCH THE OPERATION OF THE COMPUTER. 2 L 7 2 4F RT A3EU 2001072600256 20010726 00256 WP 2001 7 26 AT0100182 1 20010615 A 3350 CM3071 LIGHT DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 845AT 47238 FOUND 2 RED EMERGENCY FLOOR TRACK LIGHTS AT FORWARD GALLEY INOPERATIVE. RELAMPED BULBS IAW DC9 MM 33-50. 2 L 7 2 4F A6WE 2001062000075 20010620 00075 NM 2001 6 20 AWXA0001800 1 20010604 A 5311 6546539 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 FWD SIDE OF FUSELAGE FRAME CRACKED ABOVE CENTER WING BS 616 RBL 64 WL 201. TRIMMED OUT DAMAGED SECTION; INSTALLED REPAI R ANGLE AND FILLER IAW AWA ER 03-5311-01130-DL2. 2 L 7 2 4F RT A16WE 2001062000076 20010620 00076 NM 2001 6 20 AWXA0001801 1 20010604 A 5312 6545409245 PRESSURE PANEL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 CRACK IN PRESSURE WEB BS 663 APPROX LBL 34 ON TOP OF WEB. REPAIRED IAW ER 03-5702-01135-JS2. 2 L 7 2 4F RT A16WE 2001062000077 20010620 00077 NM 2001 6 20 AWXA0001802 1 20010604 A 5330 6545775594 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE SCRATCHED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 RT EXTERNAL FUSELAGE HAS SCRATCH AFT OF RT WING TO BODY FAIRING JUST FWD AND BELOW EGRESS LIGHT. REPAIRED IAW SRM 53-00 -01 FIG 201 PG 201-203. 2 L 7 2 4F RT A16WE 2001062000078 20010620 00078 NM 2001 6 20 AWXA0001803 1 20010604 A 5312 65C375903 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 ULTRASONIC CRACK INDICATION BS 178 FWD FACE BLKHD WEB RBL 6.6 WL 212-212.7 .7 INCH LENGTH. REPAIRED IAW SRM 53-10-8 PG 287-298. 2 L 7 2 4F RT A16WE 2001062000079 20010620 00079 NM 2001 6 20 AWXA0001804 1 20010604 A 5312 65C375903 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 ULTRASONIC CRACK INDICATIONS BS 178 BLKHD WEB FWD FACE 2 LBL 6.6 WL 209.5-210, 212.1-212.4 .5 INCH AND .3 INCH RESPECTIV ELY. REPAIRED CRACKS IAW SRM 53-10-08 PG 287-298. 2 L 7 2 4F RT A16WE 2001062000080 20010620 00080 NM 2001 6 20 AWXA0001805 1 20010604 A 5312 65C375903 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 HFEC INSP FWD SIDE OF BS BLKHD WEB FOUND 2 CRACKS RBL 4.7 WL 196.2-197.1 AND 199.9-201.5. REPAIRED IAW SRM 53-10-8 FIG 211 PG 287-298. 2 L 7 2 4F RT A16WE 2001062000081 20010620 00081 NM 2001 6 20 AWXA0001806 1 20010604 A 5311 6546539 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 FWD SIDE OF FUSELAGE FRAME CRACKED ABOVE CENTER WING BS 616 LBL 65. TRIMMED OUT DAMAGE; INSTALLED REPAIR ANGLE AND FILL ER IAW AWA ER 03-5311-01130-DL2 AND SB 737-53-1182. 2 L 7 2 4F RT A16WE 2001062000082 20010620 00082 EU 2001 6 20 AWXA0001807 1 20010604 A 5315 D53472193200190 FLOORBEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 642AW 584 AFT GALLEY AREA AT FR 68 FLOORBEAM Y765 CORRODED AT HOLE (RT INBD FLOOR TRACK BEAM). REPLACED FLOORBEAM IAW A320 DWG D5 34721932000. 2 L 7 2 4F RT A28NM 2001062000083 20010620 00083 EU 2001 6 20 AWXA0001808 1 20010604 A 5753 D57570296203 FITTING AIRBUS 320 A320231 3930325 EU T/E FLAP CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 642AW 584 RT WING NR 2 FLAP CANOE AFT ATTACH LINK LEVER ASSY WORN AT FLAP FITTING AND ATTACH BRACKET. REPAIRED IAW AWA ER 26-5751 -01149-KB1 -- ADDITIONAL P/N: D5757055500300. 2 L 7 2 4F RT A28NM 2001062000084 20010620 00084 EU 2001 6 20 AWXA0001809 1 20010604 A 5320 D5311282600101 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 642AW 584 LIGHT SURFACE CORROSION ON TOP OF FLOOR SUPPORT AT FR 14 BL -503.2. REPLACED IAW SRM 51-42-11 PG 1. 2 L 7 2 4F RT A28NM 2001062000085 20010620 00085 EU 2001 6 20 AWXA0001810 1 20010604 A 5347 D53112782200 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 642AW 584 LIGHT SURFACE CORROSION ON TOP OF FLOOR TRACK AT FR 20 BL -Y1292. CORROSION CLEANED UP, MAT LOSS BEYOND LIMITS. TRACK FABBED IAW DWG D53112782200; INSTALLED IAW SRM 51-42-11 PG 1. 2 L 7 2 4F RT A28NM 2001062000086 20010620 00086 EU 2001 6 20 AWXA0001811 1 20010604 A 5315 ASNS2495 FLOORBEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 642AW 584 LIGHT SURFACE CORROSION ON TOP OF FLOORBEAM C20 BL -Y254. CORROSION CLEANED UP, MAT LOSS BEYOND LIMITS. FRAME REPAIRED IAW SRM 53-11-14 FIG 201 PG 203-208; REPAIRED IAW AMM 51-75-00-001. 2 L 7 2 4F RT A28NM 2001062000087 20010620 00087 EU 2001 6 20 AWXA0001812 1 20010604 A 5330 D53230349200 SKIN AIRBUS 320 A320231 3930325 EU FUSELAGE DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 642AW 584 FUSELAGE SKIN DENTED AT LAP JOINT (APPROX FR 28) BELOW AFT EDGE OF C1 DOOR CUTOUT. EVIDENCE OF PRESSURE LEAK. REPAIRED IAW SRM 53-00-11 PARA 4E FIG 211. 2 L 7 2 4F RT A28NM 2001062000088 20010620 00088 EU 2001 6 20 AWXA0001813 1 20010604 A 5240 D53480040200 WEB AIRBUS 320 A320231 3930325 EU L2 DOOR GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 642AW 584 FRAME 66 AT UPPER FWD CORNER OF L2 DOOR, WEB AND RIVETS DAMAGED. REPAIRED IAW AWA ER 26-5345-01150-DD1; FINISH RESTORED IAW AMM 55-70-00 PG 1. 2 L 7 2 4F RT A28NM 2001062000089 20010620 00089 NM 2001 6 20 C1HA200182004 1 20010524 A 2130 54193211 CONTROL VALVE BOEING 727 7272S7 138407Z NM A/C BAY FAILED A C1HA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 682CA 22019 ON INITIAL CLIMB LOST CONTROL OF A/C PRESSURIZATION IN AUTO CLIMB TO 2000 FPM. CLOSED CARGO HEAT VALVE AND WENT TO STAN DBY MODE OUTFLOW VALVE FULL CLOSED CLIMB 500 FPM. AIR RETURN TO DFW OVERWEIGHT LANDING 173,000 SMOOTH. UNABLE TO DUPLI CATE ON GROUND. TEST FLIGHT ACCOMPLISHED REVERIFIED. FOUND WATER SEPARATOR CLAMP OUT OF POSITION. REPOSITIONED AND SE CURED CLAMP ON LEFT PACK. 2ND TEST FLIGHT ACCOMPLISHED AT 10K FT CABIN HELD WITH OUTFLOW VALVE FULL CLOSED. ON LEFT PA CK CPRESS HELD. ON RIGHT PACK CABIN CLIMBED 2000 FPM. REMOVED AND REPLACED RIGHT PACK 35 DEGREE VALVE. 3RD TEST FLIGHT SYSTEM CHECKS NORMAL. 2 L 7 3 4F A3WE 2001062000090 20010620 00090 2001 6 20 C1HA200182005 4 20010525 A 2565 SLIDE BOEING 727 7272S7 138407Z NM L1 DOOR OUT OF POSITION A C1HA K NONE O OTHER CR CRUISE 1 GL 15 682CA 22019 DURING FLIGHT L-1 DOOR SLIDE FELL ON FLOOR. REPACKED AND HUNG L-1 DOOR SLIDE. 2 L 7 3 4F A3WE 2001062000091 20010620 00091 NM 2001 6 20 C1HA200182006 1 20010525 A 3510 80130724 OXYGEN BOTTLE BOEING 727 7272S7 138407Z NM CREW OXYGEN DAMAGED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 682CA 22019 THREADS ON NECK OF CREW O2 BOTTLE CROSSED. REMOVED AND REPLACED CREW O2 AT BOTTLE. 2 L 7 3 4F A3WE 2001062000092 20010620 00092 2001 6 20 C1HA200182007 4 20010527 A 2565 SLIDE BOEING 727 7272S7 138407Z NM L1 DOOR OUT OF POSITION A C1HA K NONE O OTHER CR CRUISE 1 GL 15 682CA 22019 L-1 DOOR SLIDE COMES OUT OF CASING. SECURED SLIDE IN COVER PER 52-12-00. 2 L 7 3 4F A3WE 2001062000093 20010620 00093 NM 2001 6 20 C1HA200195004 1 20010530 A 5330 SKIN BOEING 727 727290 138408W NM FUSELAGE DENTED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 DENT AT BS 479 STR 9 & 10R OUT OF LIMITS. CUT OUT DAMAGE REPAIRED PER SRM 53-30-2 & 3, 3A AND 4. 2 L 7 3 4F A3WE 2001062000094 20010620 00094 NM 2001 6 20 C1HA200195007 1 20010530 A 5330 SKIN BOEING 727 727290 138408W NM FUSELAGE DAMAGED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 CREASE IN SKIN BEYOND LIMITS. REPAIRED PER SRM 53-30-3. 2 L 7 3 4F A3WE 2001062000095 20010620 00095 NM 2001 6 20 C1HA200195008 1 20010530 A 5330 SKIN BOEING 727 727290 138408W NM FUSELAGE DAMAGED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 CREASE IN SKIN BEYOND LIMITS. REPAIRED PER SRM 53-30-3. 2 L 7 3 4F A3WE 2001062000096 20010620 00096 NM 2001 6 20 C1HA200195009 1 20010530 A 5330 SKIN BOEING 727 727290 138408W NM FUSELAGE DAMAGED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 TWO CREASES IN AFT RT FUSELAGE SKIN. REPAIRED PER SRM 53-30-3. 2 L 7 3 4F A3WE 2001062000097 20010620 00097 NM 2001 6 20 C1HA200195010 1 20010530 A 5310 SHEAR TIE BOEING 727 727290 138408W NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 SHEAR TIE CORRODED. REPAIRED PER SRM 53-30-1, 53-10-4 AND 53-30-4. 2 L 7 3 4F A3WE 2001062000098 20010620 00098 CE 2001 6 20 C2XA01CL114 1 20010524 A 3260 C2006 SWITCH BEECH 1900 1900D 1154162 CE COCKPIT OUT OF ADJ A C2XA O OTHER P NO WARNING INDICATION AP APPROACH 1 SW 27 87555 UE234 CLE FLIGHT 3007 THE CREW REPORTED THE GEAR WARNING HORN DOESN'T COME ON WHEN THE POWER LEVERS ARE PULLED BACK TO 80 PERC ENT. THE HORN AND LIGHT COME ON WHEN FLAPS 35 DEGREES ARE SELECTED WITH GEAR UP, BUT HORN AND LIGHT DO NOT COME ON WITH POWER LEVERS PULLED BACK. MAINTENANCE INSPECTED AND ADJUSTED THE GEAR WARNING HORN SWITCHES TO CLOSE AT 85 PERCENT N1 ON BOTH ENGINES. THE AIRCRAFT WAS TEST FLOWN AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICES. 2 L 7 2 4T RT A24CE 2001062000099 20010620 00099 SO 2001 6 20 C2XA01CL118 1 20010524 A 3234 7455501 CONTROL HANDLE EMB 135 EMB135LR SO COCKPIT DEFECTIVE A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 15527 301 145413 CLE FLIGHT 3678 THE CREW REPORTED THE NOSE GEAR WAS SLOW TO RETRACT. RECEIVED A L/G GEAR LEVER DISAGREEMENT. THE MESS AGE CLEARED ON ITS OWN. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR CONTROL HA NDLE. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT TOOO11AT 2001062000100 20010620 00100 CE 2001 6 20 C2XA01CL119 1 20010526 A 5210 MS27039116 SCREW BEECH 1900 1900D 1154162 CE ENTRY DOOR SHEARED A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 81556 UE239 CLE FLIGHT 2998 THE CREW REPORTED THE MAIN CABIN DOOR WILL NOT LATCH SHUT FROM THE OUTSIDE. REPORTED THE DOOR LATCHED O K FROM THE INSIDE. MAINTENANCE INSPECTED AND FOUND ONE OF THE SCREWS ON THE ARM ASSEMBLY OF THE AIRSTAIR DOOR LATCH MEC HANISM HAD SHEARED. A NEW ARM ASSEMBLY AND LOWER AND UPPER SUPPORT ASSEMBLY WERE REPLACED. OPERATIONAL CHECKS WERE GOO D. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT A24CE 2001062000101 20010620 00101 SO 2001 6 20 C2XA01CL121 1 20010526 A 2530 MS3476L2221S CONNECTOR EMB 135 EMB135LR SO GALLEY BURNED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 12519 145366 CLE FLT 3618 THE CREW REPORTED ELECTRICAL BURNING SMELL COMING FROM COFFEE WARMER AREA. MAINTENANCE INSPECTED AND FOUN D COFFEE WARMER CONNECTOR BURNT. MAINTENANCE REPLACED BURNT COFFEE WARMER CONNECTOR. PERFORMED OPERATIONAL CHECKS AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT TOOO11AT 2001062000102 20010620 00102 SO 2001 6 20 C2XA01CL122 1 20010530 A 2150 8152403 ACM EMB 145 EMB145ER SO A/C BAY FAILED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 14933 1260 923 145018 CLE FLIGHT 3992 THE CREW REPORTED A HEAVY BURNING ODOR IN THE COCKPIT AND CABIN FOLLOWED BY SMOKE DURING TAKEOFF AND AFT ER LANDING. RECEIVED A PACK NR 1 OVERHEAT MESSAGE. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 AIR CYCLE MACHINE. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001062000103 20010620 00103 EU 2001 6 20 C2XA01CL123 1 20010529 A 3260 D228830001 PROXIMITY SENSOR AEROSP ATR42 ATR42320 8680930 EU NLG INTERMITTENT A C2XA K NONE N FALSE WARNING CL CLIMB 1 SW 27 14822 18538 18538 163 CLE FLIGHT 3158 THE CREW REPORTED A INTERMITTENT NOSE GEAR UNLOCK LIGHT IN FLIGHT. MAINTENANCE REPLACED THE NR 1 NOSE G EAR PROXIMITY SENSOR. OPERATIONAL CHECKS WERE GOOD. 2 H 7 2 4T RT A53EU 2001062000104 20010620 00104 EU 2001 6 20 C2XA01CL124 1 20010529 A 3350 LP1670 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 27 26826 172 CLE FLIGHT 3004 THE CREW REPORTED EMERGENCY AISLE PATH LIGHTING HAD TWO LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BU LBS AND OPERATIONAL CHECKS WERE GOOD. 2 H 7 2 4T RT A53EU 2001062000105 20010620 00105 SO 2001 6 20 C2XA01CL125 1 20010602 A 3234 7455501 CONTROL HANDLE EMB 145 EMB145LR SO COCKPIT FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 18982 145223 CLE FLT 3985 THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLEVELAND A ND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LANDING GEAR SELECTOR LEVER. OPERATIONAL CHECKS WERE GOOD . AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001062000106 20010620 00106 SO 2001 6 20 C2XA01CL126 1 20010603 A 7931 23062185 VALVE EMB 135 EMB135ER 3260203 SO ENGINE FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14505 145192 CLE FLT 3962 THE CREW REPORTED NR 1 ENGINE OIL PRESSURE WARNING CONTINUOUSLY IN FLIGHT, PRESSURE NORMAL. AIRCRAFT RETU RNED TO CLEVELAND AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE OIL TANK PRESSURE VALVE. O PERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2001062000107 20010620 00107 SO 2001 6 20 C2XA01CL127 1 20010601 A 3397 W192868022 WIRE EMB 135 EMB135LR 3260305 SO CABIN BROKEN A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 16520 145372 CLE FLT 3863 THE CREW REPORTED SECOND ROW AISLE PATH EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT TOOO11AT 2001062000108 20010620 00108 SO 2001 6 20 C2XA01CL128 1 20010603 A 3234 7455501 CONTROL HANDLE EMB 145 EMB145LR SO COCKPIT FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 12996 2268 2268 145296 CLE FLIGHT 4059 THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM CLEVELAND. RECEIVED A LG/LEVER DISAGREE MESSAGE ON THE EICAS. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REP LACED THE LANDING GEAR CONTROL LEVER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001062000109 20010620 00109 EU 2001 6 20 C2XA01CL129 1 20010604 A 2612 51216086 CONNECTOR AEROSP ATR42 ATR42320 8680930 EU FIRE LOOP LOOSE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 15816 105 CLE FLT 3114 THE CREW REPORTED NR 2 ENGINE FIRE TEST WOULD NOT TEST. MAINTENANCE INSPECTED AND TIGHTENED LOOSE FIRE LO OP CONNECTOR. OPERATIONAL TEST WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001062000110 20010620 00110 CE 2001 6 20 C2XA01CL130 1 20010604 A 3234 1013841377 CONTROL HANDLE BEECH 1900 1900D 1154162 CE COCKPIT INTERMITTENT A C2XA K NONE J WARNING INDICATION CL CLIMB 1 SW 27 87552 8014 1331 UE216 CLE FLIGHT 4360 THE CREW REPORTED THE GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDE NT. MAINTENANCE REPLACED THE LANDING GEAR SELECTOR HANDLE. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FO R SERVICE. 2 L 7 2 4T RT A24CE 2001062000111 20010620 00111 CE 2001 6 20 C2XA01CL131 1 20010605 A 3230 1143640681 PRINTED CKT BOAR BEECH 1900 1900D 1154162 CE LANDING GEAR FAULTY A C2XA K NONE J WARNING INDICATION CL CLIMB 1 SW 27 87552 UE216 CLE FLIGHT 4355 THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED PCB A316. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS TEST FLOWN AND NO DISCREPANC Y WAS NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT A24CE 2001062000112 20010620 00112 SO 2001 6 20 C2XA01IA252 1 20010526 A 3350 3071BPE LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15713 120114 IAH - FLIGHT 3034, DURING PREFLIGHT INSPECTION, THE CREW REPORTED SEVERAL EMERGENCY EXIT LIGHTS TO BE INOPERATIVE. MAIN TENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULBS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001062000113 20010620 00113 SO 2001 6 20 C2XA01IA253 1 20010529 A 2730 14532475401 BELLCRANK EMB 145 EMB145ER SO LT ELEVATOR BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15926 145005 MYR - DURING ROUTINE INSPECTION, THE LEFT HAND ELEVATOR BELLCRANK ASSEMBLY WAS FOUND TO BE BROKEN AT THE TORQUE TUBE MAT ING AREA. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BELLCRANK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001062000114 20010620 00114 SO 2001 6 20 C2XA01IA254 1 20010531 A 4920 168401201 APU EMB 120 EMB120ER 3260203 SO APU BAY LEAKING A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 16723 120169 IAH- DURING FLIGHT THE CREW NOTED SMOKE IN THE CABIN AND RETURNED TO IAH WITHOUT INCIDENT. IAH- MAINTENANCE INSPECTED T HE AIRCRAFT AND DETERMINED THE APU TO BE THE CAUSE OF SMOKE IN THE CABIN AND PLACED THE APU ON MEL. IAH ON 06/02/2001 M AINTENANCE REMOVED AND REPLACED THE APU, PERFORMED A OPERATIONAL CHECK AND A LEAK CHECK WITH NO DISCREPANCIES NOTED, CLE ARED THE MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001062000115 20010620 00115 SO 2001 6 20 C2XA01IA255 1 20010601 A 3260 LIGHT EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A C2XA K NONE O OTHER CR CRUISE 1 SW 27 16723 120169 IAH- THE CREW REPORTED THE RIGHT MAIN LANDING GEAR B-INDICATES RED IN TRANSITION LIGHT AFTER GEAR RETRACTION. IAH-ON 06 /02/2001 MAINTENANCE PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM. COULD NOT DUPLICATE THE PROBLEM AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001062000116 20010620 00116 SO 2001 6 20 C2XA01IA256 1 20010531 A 3350 20131A BATTERY EMB 145 EMB145LR SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13964 145123 IAH- DURING 1A INSPECTION IT WAS NOTED THAT THE EMERGENCY FLOOR LIGHTING MIDDLE SECTION DID NOT ILLUMINATE WHEN SELECTED . IAH- MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY, OPERATIONAL CHECKED. NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001062000117 20010620 00117 EU 2001 6 20 C2XA01IA257 1 20010531 A 3234 1005383400 SELECTOR VALVE AEROSP ATR42 ATR42320 8680930 EU HYD BAY FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 93840 271 IAH- ON DEPARTURE THE CREW NOTICED THAT THE GEAR WOULD NOT RETRACT AND RETURNED TO IAH. IAH- MAINTENANCE REMOVED AND RE PLACED THE LANDING GEAR SELECTOR VALVE, PERFORMED AN OPERATIONAL CHECK, NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001062000118 20010620 00118 SO 2001 6 20 C2ZA01IA258 1 20010329 A 3260 852701 PROXIMITY SENSOR EMB 145 EMB145ER SO LT MLG FAILED A C2XA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 27 14938 145029 EWR- DURING FLIGHT 3959 THE CREW NOTED THAT THE LANDING GEAR AIR/GROUND FAIL MESSAGE APPEARED APPROXIMATELY SEVEN MINUT ES AFTER TAKEOFF. THE AIRCRAFT RETURNED TO EWR AND LANDED WITHOUT INCIDENT. EWR- MAINTENANCE REMOVED AND REPLACED LEF T HAND MAIN LANDING GEAR PROXIMITY SENSORS (2 EA) AND OPERATIONAL CHECK CHECKED GOOD. THE AIRCRAFT WAS APPROVED FOR RET URN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001062000119 20010620 00119 NM 2001 6 20 C8GA20010011 1 20010601 A 3260 SWITCH BOEING 727 727223 1384074 NM LT MLG LOOSE A C8GA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 15 713AA 50950 22469 FLT 722 FROM TOL TO CLT. LEFT MAIN GEAR DOOR LIGHT REMAINED ON AFTER GEAR RETRACTION ON TAKEOFF. RECYCLED GEAR CYCLE P ER AOM PROCEDURES WITH NO HELP, LIGHT REMAIN ON. AIR TURNBACK TO TOL AND LANDED WITHOUT ANY INCIDENT. INVESTIGATION FO UND THE MLG DOOR SWITCH LOOSE. CLEANED, TIGHTENED MLG DOOR SWITCH AND PERFORMED OPERATIONAL SYSTEM CHECK OF LIGHT INDIC ATION IAW MM 32-62-0. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2001062000120 20010620 00120 NM 2001 6 20 C8GA20010012 1 20010602 A 3260 656021136 ACCESSORY UNIT BOEING 727 727223 1384074 NM MLG FAULTY A C8GA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 15 708AA 278 22465 FLT 719 FROM MCO TO MEM. AFTER GEAR RETRACTION, THE LEFT MAIN GEAR DOOR UNSAFE LIGHT REMAIN ON. RECYCLED THE GEAR CYCL E PER AOM PROCEDURES WITH NO HELP. AIR TURNBACK TO MCO AND LANDED WITHOUT INCIDENT. FOUND GEAR ACCESSORY UNIT FAILED. REPLACED LANDING GEAR ACCESSORY UNIT AND OPS CHECKED SYSTEM IAW MM 32-61-0. AIRCRAFT RETURN TO SERVICE. 2 L 7 3 4F A3WE 2001062000121 20010620 00121 WP 2001 6 20 CALA0100516 1 20010529 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND MID CARGO DOOR LOWER JAMB BEAM CORRODED AROUND RIVNUTS. THE DOOR JAMB WAS REPAIRED IAW ECRA 5310-03027 . 2 L 7 2 4F A6WE 2001062000122 20010620 00122 WP 2001 6 20 CALA0100517 1 20010529 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND MID CARGO RT TIE DOWN TRACK CORRODED BETWEEN FS 693 AND 788. THE CARGO TRACK WAS REMOVED AND A NEW TRA CK WAS INSTALLED IAW SRM 51-30-01, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 2001062000123 20010620 00123 WP 2001 6 20 CALA0100518 1 20010529 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND AFT CARGO FRAME CORRODED AT FS 1117, LONGERON 30. THE CORRODED SECTION OF FRAME WAS REMOVED AND A NEW FRAME SECTION WAS INSTALLED IAW SRM 51-30-5, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 2001062000124 20010620 00124 WP 2001 6 20 CALA0100519 1 20010529 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND MID CARGO SUPPORT CORRODED AT FS 750 BETWEEN LONGERONS 29L AND 29R. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW 51-30-5, 51-10-4, AND 51-30-2. 2 L 7 2 4F A6WE 2001062000125 20010620 00125 WP 2001 6 20 CALA0100520 1 20010529 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND AFT CARGO OVERHEAD FLOORBEAM CORRODED ON NUT PLATES AND EXFOLIATION CORROSION ON RT SIDE AT FS 1309. T HE FLOORBEAM WAS REMOVED AND A NEW FLOORBEAM WAS INSTALLED IAW SRM 51-30-2 AND 51-10-4. 2 L 7 2 4F A6WE 2001062000126 20010620 00126 WP 2001 6 20 CALA0100522 1 20010530 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND AFT CARGO FALSE BULKHEAD LOWER SUPPORTS CORRODED AND CRACKED AT FS 1007, LONGERON 28L AND 28R. BOTH SU PPORTS WERE REMOVED AND NEW SUPPORTS WERE INSTALLED IAW SRM 51-10-5, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 2001062000127 20010620 00127 WP 2001 6 20 CALA0100523 1 20010530 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND MID CARGO FRAME CORRODED AT FS 560 BETWEEN LONGERONS 26R AND 26L. THE CORRODED SECTION OF FRAME WAS RE MOVED AND A Z-FRAME REPAIR SPLICE WAS INSTALLED IAW SRM 53-03, FIGURE 2A AND 51-10-3. 2 L 7 2 4F A6WE 2001062000128 20010620 00128 WP 2001 6 20 CALA0100524 1 20010531 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND MID CARGO FRAME CORRODED AT FS 541 BETWEEN LONGERONS 26R AND 26L. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 2A, 51-10-4, 51-10-3, 53-05, FIGURE 2A, AND 51-30-5. 2 L 7 2 4F A6WE 2001062000129 20010620 00129 NM 2001 6 20 CALA0100525 1 20010601 A 2560 ACREM1A MEGAPHONE BOEING 737 7373Q8 1384670 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 73385 26314 INSPECTION FOUND THE FORWARD MEGAPHONE INOPERATIVE. THE MEGAPHONE WAS REMOVED AND REPLACED IAW MM 25-60-00. 2 L 7 2 4F RT A16WE 2001062000130 20010620 00130 NM 2001 6 20 CALA0100526 1 20010601 A 5315 FLOORBEAM BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 62631 27535 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT SEVERAL FASTENER HOLES, STA 986, LONGERON 29R AND 27L. STRAP REPAIRS WERE INSTALLED IAW SRM 53-00-51. 2 L 7 2 4F RT A16WE 2001062000131 20010620 00131 WP 2001 6 20 CALA0100527 1 20010602 A 5310 BEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND AFT CARGO DOOR JAMB BEAM CORRODED. THE LOWER DOOR JAMB BEAM WAS REMOVED AND A NEW LOWER DOOR JAMB BEAM WAS INSTALLED USING A DOUBLER AND SPACER IAW SRM 51-30-5 AND 51-30-2. 2 L 7 2 4F A6WE 2001062000132 20010620 00132 WP 2001 6 20 CALA0100528 1 20010602 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND AFT CARGO CABIN FLOORBEAM AND NUT PLATES CORRODED AT FS 1322. THE FLOORBEAM WAS REPAIRED IAW SRM 53-05 AND 53-05, FIGURE 20A. 2 L 7 2 4F A6WE 2001062000133 20010620 00133 WP 2001 6 20 CALA0100529 1 20010602 A 5320 STRAP DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND AFT CARGO DOOR JAMB TORQUE BOX FWD STRAP CORRODED. THE FORWARD STRAP WAS REMOVED AND A NEW STRAP WAS I NSTALLED IAW SRM 53-01, FIGURE 1, 51-10-4, 51-10-3, AND 51-30-5. 2 L 7 2 4F A6WE 2001062000134 20010620 00134 WP 2001 6 20 CALA0100530 1 20010603 A 5754 SKIN DOUG DC9 DC982 3022082 WP L/E SLAT DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND RT WING EXTERNAL SURFACE OF ZERO SLAT SKIN DENTED I/B OF THE DRIVE TRACK. THE SLAT WAS REMOVED, REPAIR ED, AND REINSTALLED IAW MM 27-80-01, EA 9-5740-2-A0890, AND ECRA 5740-01040. 2 L 7 2 4F A6WE 2001062000135 20010620 00135 WP 2001 6 20 CALA0100531 1 20010603 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND AFT CARGO FLOORBEAM AND NUT PLATES CORRODED AT FS 1338. THE UPPER L-ANGLE ON FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-05, 51-30-01, 51-30-02, 51-30-05, AND 51-10-4. 2 L 7 2 4F A6WE 2001062000136 20010620 00136 2001 6 20 USAASB01142 4 20010520 A 3400 STATIC LINE BOEING 737 737301 1384611 NM E/E NOSE COMPT LEAKING A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 577US 23742 DCA - FLT 556 - EN ROUTE FROM DCA TO MHT, AT FL200, THE F/O'S ALTIMETER WAS READING 500 FT LOW AT 19,500 FEET. DUE TO P REVIOUS PROBLEMS AND LACK OF MX IN MHT, FLIGHT RETURNED TO FIELD AT DCA. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EM ERGENCY WAS DECLARED. MX REMOVED AND REPLACED THE F/O'S PITOT TUBE (P/N 0856AE18) WITH NO HELP. FOUND STATIC LINE LEAD ING TO FIRST OFFICERS PITOT STATIC TUBE LEAKING. REPLACED LINE. SYSTEM OPS CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001062000137 20010620 00137 NM 2001 6 20 USAASB01136 1 20010513 A 3260 189929 UPLOCK SENSOR BOEING 737 737301 1384611 NM NLG FAULTY A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 577US 23742 PHL - FLT 1922 - AFTER GEAR RETRACTION, WITH GEAR HANDLE IN 'UP' POSITION, THE NOSE GEAR RED LIGHT REMAINED ILLUMINATED. CREW EXTENDED THE GEAR AND RECEIVED THREE GREEN LIGHTS. CREW RETRACTED GEAR AND AGAIN RECEIVED THE NOSE GEAR RED LIGH T. CREW DECIDED TO RETURN TO PHL. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REM OVED AND REPLACED THE NOSE LANDING GEAR UPLOCK SENSOR AND THE E-11 M983 PROXIMITY CARD (P/N 65-58250-29). ACCOMPLISHED GEAR SWING. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001062000138 20010620 00138 NM 2001 6 20 USAA010589 1 20010531 A 5510 HINGE FITTING BOEING 737 7372B7 1384560 NM CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 284AU 23131 CLT - FOUND STABILIZER HINGE FITTING CORRODED 1 SQUARE INCH, LEFT HORIZ STAB REAR SPAR, LOWER ATTACH POINT LUG. REWORKE D PER EA 69633. (M) 2 L 7 2 4F A16WE 2001062000139 20010620 00139 NM 2001 6 20 USAA010590 1 20010516 A 5320 BEAM BOEING 737 737301 1384611 NM CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND BEAM CORRODED 4 AREAS 2 INCHES, SUPPORT FOR FLOORBOARD NR 6. CORROSION LEVEL 1, TASK NR 53-107-02. SPLICED IN BEAM SECTION THAT WAS BLENDED BEYOND LIMITS PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2001062000140 20010620 00140 NM 2001 6 20 USAA010591 1 20010516 A 5315 FLOORBEAM BOEING 737 737301 138447R NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND FLOORBEAM CORRODED .5 INCH BY 1 FOOT, STATION 344 UNDER FLOORBOARD NR 8. SPLICED IN BEAM REPAIR. (M) 2 L 7 2 4F RT A16WE 2001062000141 20010620 00141 NM 2001 6 20 USAA010585 1 20010522 A 5300 SKIN BOEING 737 7373B7 1384580 NM BS 969 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 522AU 23857 PIT - FOUND SKIN CORRODED 1 INCH BY 2 INCHES, STATION 969 BETWEEN RIGHT STRINGER 27 AND 28. CORROSION LEVEL 1, TASK NR C53-208-01. INSTALLED DOUBLER PER EA NR 70922. (M) 2 L 7 2 4F RT A16WE 2001062000142 20010620 00142 NM 2001 6 20 USAA010586 1 20010510 A 5300 SKIN BOEING 737 737401 1384701 NM FS 727D CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 36538 23882 PIT - FOUND SKIN CRACKED 2.5 INCHES, STRINGER 23R STATION 727D. CUT OUT DAMAGE, INSTALLED EXTERNAL DOUBLER PER EA 71032 AND SRM 53-00-01 FIG 202. (M) 2 L 7 2 4F RT A16WE 2001062000143 20010620 00143 NM 2001 6 20 USAA010571 1 20010525 A 5300 INTERCOSTAL BOEING 737 737201 1384454 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 242US 52490 22444 CLT - FOUND INTERCOSTAL CRACKED 1.5 INCHES, BS 178, WL 195, LBL 25 AND RBL 25. REMOVED AND REPLACED INTERCOSTAL. (M) 2 L 7 2 4F A16WE 2001062000144 20010620 00144 WP 2001 6 20 USAAD01121 1 20010605 A 3350 S103 BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801US 48037 IND - THE WALK AROUND FLASHLIGHT BY THE MAIN ENTRY DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F A6WE 2001062000145 20010620 00145 WP 2001 6 20 USAAD01120 1 20010603 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 828US 48028 MCO - FOUND ROW 25 SEAT MOUNTED FLOOR PATH LIGHT WOULD NOT ILLUMINATE DURING TEST. MAINTENANCE REPLACED THE BATTERY AND LIGHT ASSEMBLY. (M) 2 L 7 2 4F A6WE 2001062000146 20010620 00146 EU 2001 6 20 DKAA01014 1 20010525 A 7900 R289P04 FITTING AMD FALC20 FALCON 2720302 EU CRACKED A DKAA E ENGINE SHUTDOWN K FLUID LOSS CL CLIMB 1 GL 23 230RA 230 NR 2 ENGINE OIL PRESSURE DROPPED TO ZERO ON CLIMB-OUT (ABQ). NR 2 ENGINE GEARBOX FITTING CRACKED. REPLACED FITTING, SE RVICED ENGINE OIL CHECKED OIL FILTER IAW GE MM SEI-187. OPERATION CHECK AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4F A7EU 2001062000147 20010620 00147 WP 2001 6 20 DKAA01010 1 20010320 A 5300 FRAME DOUG DC9 DC915F 3022037 WP FS 148.55 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 561PC 50257 47014 FOUND FRAME AT FS 148.55 BETWEEN L17R AND L18R CORRODED. REPAIRED PER DER DRAWING NR 53-01100-1 DATED 3/20/2001. AIRCR AFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 2001062000148 20010620 00148 EU 2001 6 20 DKAA01011 1 20010330 A 7100 B19D84 FUEL HEATER AMD FALC20 FALCON 2720302 EU LEAKING A DKAA K NONE R PARTIAL RPM/PWR LOSS AP APPROACH 1 GL 23 810RA 81 LEFT ENGINE SURGED IN FLIGHT, EPR FLUCTUATED APPROXIMATELY .2 TO .3 AND HEAVY FUEL LEAK ON GROUND AFTER SHUTDOWN (MSY). REPLACED LEFT FUEL HEATER IAW AMD MM CHAPTER 71-11. OPS AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A7EU 2001062000149 20010620 00149 WP 2001 6 20 DKAA01001 1 20010308 A 5700 SKIN DOUG DC9 DC915F 3022037 WP WING DAMAGED A DKAA K NONE O OTHER IN INSP/MAINT 1 GL 23 916R 47229 47010 RIGHT WING TIP ASSEMBLY BOTTOM SKIN DAMAGED. REPLACED AFFECTED SKIN PANELS PER DER DOCUMENT 01-02 REV A, DATED 1/18/200 1. AIRCRAFT RETURNED TO SEVICE. (M) 2 L 7 2 4F A6WE 2001062000150 20010620 00150 WP 2001 6 20 DKAA01006 1 20010308 A 5300 WEBBING DOUG DC9 DC915F 3022037 WP FS 446-465 CRACKED A DKAA K NONE O OTHER IN INSP/MAINT 1 GL 23 916R 47229 47010 FOUND LEFT CARGO FLOOR WEBBING CRACKED AT STATION 446-465. REPAIRED PER DER DRAWING NR 53-01010-2, DATED 01/16/2001. A IRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 2001062000151 20010620 00151 WP 2001 6 20 CALA0100532 1 20010603 A 5210 WEB DOUG DC9 DC982 3022082 WP L1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND A 1 INCH CRACK IN L1 DOOR TORQUE BOX WEB AFT OF TANG AT LONGERON 15L. THE FASTENERS WERE REMOVED, TANG S TRIMMED, AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 51-30-2, 51-10-4, AND EA 9-5314-2-A0884. 2 L 7 2 4F A6WE 2001062000152 20010620 00152 WP 2001 6 20 CALA0100533 1 20010603 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND TAIL COMPARTMENT LT SIDE CANTED FRAME GOUGED AT FS 1463. THE CORROSION WAS REMOVED AND REPAIR ANGLES W ERE INSTALLED IAW SRM 51-30-5, 53-01, FIGURE 1, 51-10-3, AND EA 9-5311-2-A0888, FIGURE 2. 2 L 7 2 4F A6WE 2001062000153 20010620 00153 EA 2001 6 20 COMA0160384 1 20010601 A 5311 6003603023 FRAME CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 976CA 11314 7151 THE LEFT HAND FRAME AT FS 718.0 BETWEEN STR 10-12 IS CRACKED. REPAIRED CRACKED FRAME IAW REO 601R-53-61-193 REV A. 2 L 7 2 4F RT A21EA 2001062000154 20010620 00154 EA 2001 6 20 COMA0160385 1 20010605 A 5320 601R3103077 SPLICE PLATE CNDAIR CL600 CL6002B19 EA FUSELAGE MISMANUFACTURED A COMA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 SO 01 940CA 7048 TWO SPLICE PLATES P/N 601R31030-77 WERE FABRICATED INCORRECTLY BY MANUFACTURER. FABBED TWO DOUBLER PLATES, REWORKED SPL ICE PLATES, INSTALLED DOUBLER PLATES AND INSTALLED THE REWORKED SPLICE PLATES IAW WVAC EO 601R-53-2493. 2 L 7 2 4F RT A21EA 2001062000155 20010620 00155 CE 2001 6 20 CSXA01CL110 1 20010517 A 3297 602EN16 WIRE BEECH 1900 1900D 1154162 CE NLG SWITCH BROKEN A C2XA O OTHER N FALSE WARNING AP APPROACH 1 SW 27 81538 UE199 CLE FLIGHT 3135 THE CREW REPORTED ON APPROACH TO CLEVELAND AFTER GEAR EXTENSION, HAD NO GREEN DOWN AND LOCKED LIGHT FOR THE NOSE GEAR. EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUN D A BROKEN WIRE FOR THE NOSE GEAR ACTUATOR DOWN POSITION SWITCH. THE SWITCH WAS REPLACED AND OPERATIONAL CHECKS WERE GO OD. 2 L 7 2 4T RT A24CE 2001062000156 20010620 00156 WP 2001 6 20 2001F00023 1 20010603 A 3350 9731045 LIGHT DOUG DC9 DC981 3022081 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 828US 48028 MCO - FOUND ROW 25 SEAT MOUNTED FLOOR PATH LIGHT WOULD NOT ILLUMINATE DURING TEST. MAINTENANCE REPLACED THE BATTERY AND LIGHT ASSEMBLY. REF USAAD01120 (M) 2 L 7 2 4F A6WE 2001062000157 20010620 00157 NM 2001 6 20 C1HA200195011 1 20010601 A 7100 7436D25 FUEL CONTROL BOEING 727 727290 138408W NM #2 ENGINE FAULTY A C1HA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 GL 15 295AS 22147 #2 eng failed @ flight level 350. All indications EPR, N1, N2, EGT and F/F very erratic prior to engine flame out,ACTION TAKEN:Performed T/S per JT8 MM 72-00 pg. 161 tru 165. Accomplished adjustment test per MM 72-00. Removed and replaced F CU Ops ck good ok for service. 2 L 7 3 4F A3WE 2001062000158 20010620 00158 NM 2001 6 20 C1HA200181005 1 20010610 A 4960 10508003756 SENSOR BOEING 727 7272S7 138407Z NM APU FAULTY A C1HA F D ACTIVATE FIRE EXT. RETURN TO BLOCK J WARNING INDICATION NR NOT REPORTED 1 GL 15 681CA 22020 APU Fire Bell and light illuminated after APU shutdown. APU fire bottle discharged.ACTION TAKEN:Inspected and placed on MEL 49-1.Cleared MEL:Removed and replaced Apu overheat sensor ops cks good. Removed and replaced depleted fire bottle. 2 L 7 3 4F A3WE 2001062000159 20010620 00159 NM 2001 6 20 S01224017 1 20010510 A 2420 21B732A GENERATOR BOEING 747 747209B NM PWA JT9 JT9D7Q 52054 NE # 4 DAMAGED W SAJF O OTHER O OTHER TO TAKEOFF 1 WP 03 44410 22447 B-18755 AIRCRAFT AIR TURN BACK BECAUSE NO.4 BTB COULD NOT CLOSE WITH GEN OPEN LT ILLUM.GEN ABNORMAL CSD DISCONNECTED.C/A :1.GCU SWAPPED WITH #1,FOUND #4 FAILED. 2.SHOP AND QA INSPECTED THE GCU,AND REPORTED THAT THERE WERE MOISTURE IN THE GCU . 3.THE REST OF GCU S WERE ALSO REMOVED FOR BENCH CHECK. 4.E.O.N WAS PERFORMED TO RE-SEAL THE FLOOR PANELS AND CLEAN THE DRAINS,NO MORE LEAK WAS FOUND. 2 L 7 4 4F 4 F RT A20WE E3NE 2001062100001 20010621 00001 2001 6 21 OZIA013127003 4 20010424 A 3197 VARIOUS WIRE HONEYWELL DORNER DO32 DO328300 NM AVIONICS RACK REVERSED A OZIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 05 430Z 1921 VARIOUS 3127 UPON COMPLYING WITH SB 328J-31-097, FOUND PITCH AND ROLL INPUTS TO THE DAUS TO BE INCORRECT (REVERSED WIRING). CORRECTED WIRING. 2 H 7 2 4T RT A55NM 2001062100002 20010621 00002 2001 6 21 DHL2001362016 4 20010530 A 2210 AUTOPILOT SYS AIRBUS 300 A300B4103 3930104 EU COCKPIT MALFUNCTIONED A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 362DH 84 AUTOPILOT HAS DIFFICULTY MAINTAINING ALTITUDE PLUS OR MINUS 200 FT WITH CONFIGURATION CHANGES IE, FLAPS 0 DEGREE TO FLAP S 8 DEGREE. RESEATED NR 1 AND 2 ADC ALTITUDE ACO AND HOLD OPS CHECKED GOOD AS PER MM 22-13-00. 2 L 7 2 4F RT A35EU 2001062100003 20010621 00003 EU 2001 6 21 DHL2001362017 1 20010530 A 2760 SWITCH AIRBUS 300 A300B4103 3930104 EU RT SPEEDBRAKE LOOSE A DHLA K NONE N FALSE WARNING CR CRUISE 1 SO 01 362DH 84 INFLIGHT SPEED BRAKE ANNUNCIATOR LIGHT REMAINED ILLUMINATED WITH HANDLE STOWED. RECYCLED SPEED BRAKES FOUR TIMES TO GET ANNUNCIATOR TO EXTINGUISH. FOUND MICROSWITCH FOR RIGHT SIDE OUTER AIRBRAKE NR 1 LOOSE. SECURED AS NEEDED. SPEED BRAK ES OPS NORMAL AS PER MM 27-61-00. 2 L 7 2 4F RT A35EU 2001062100004 20010621 00004 2001 6 21 DHL2001362018 4 20010530 A 2212 B3BM2 COMPUTER AIRBUS 300 A300B4103 3930104 EU AUTOPILOT SYS FAULTY A DHLA K NONE O OTHER CL CLIMB 1 SO 01 362DH 84 PRIOR TO LEVEL OFF, A/P NR 1 DISENGAGED, UPON RE-ENGAGEMENT, CAPT FPI INDICATES NORMAL. HOWEVER, A/C DIDN'T CAPTURE ALT . DISENGAGED A/P AND FLEW BACK TO LEVEL. RE-ENGAGED A/P WOULDN'T CAPTURE ALT. RE-DISCONNECTED AND TURNED ON A/P A THI RD TIME AND A/P FUNCTIONED NORMALLY. DEFERRED PER MEL 22-11-1. ASSIGNED DMI 5813. PLACARD AUTOPILOT PANEL. REMOVED A ND REPLACED NR 1 LONGITUDINAL COMPUTER. TEST OK IAW MM 22-10-00. THIS CLEARS DMI 8813. PLACARD REMOVED. MCX NOTIFIED . 2 L 7 2 4F RT A35EU 2001062100005 20010621 00005 NE 2001 6 21 DHL2001705003 2 20010602 A 7250 TURBINE WHEEL BOEING 727 72722C 138400F NM PWA JT8 JT8D NE NR 3 ENGINE DAMAGED A DHLA A UNSCHED LANDING E Y VIBRATION/BUFFET ENGINE STOPPAGE CL CLIMB 1 SO 01 705DH 19191 653870 EXCESSIVE VIBRATION AFTER TAKEOFF - DURING CLIMB NR 3 ENG VIBRATED AND LOST POWER. DECLARED EMERGENCY. RETURNED TO ROC . FOUND TURBINE WHEEL DAMAGED. REMOVED AND REPLACED ENGINE. CORRECTIVE ACTION - REMOVED AND REPLACED #3 ENGINE PN JT8 D-7B OFF S/N 653870, TO JT8D-7B ON S/N 653316 IAW B727 MM 71-00. 2 L 7 3 4F 4 F A3WE E2EA 2001062100006 20010621 00006 2001 6 21 DHL2001708005 4 20010621 A 3400 MI585162 RECEIVER BOEING 727 72725 1384006 NM UNSERVICEABLE A DHLA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 708DH 18275 RADAR PAINTS GROUND CLUTTER AT 6 DEG TILT UP, WHEN TURNING PAINTS GROUND.CORRECTIVE ACTION - R&R RADAR RT PER M/M 34-41- 01 OPS CK NORMAL. STATUS-CLOSED. 2 L 7 3 4F A3WE 2001071100008 20010711 00008 NM 2001 7 11 01FDEA00473 1 20010619 A 5320 WEB BOEING 727 727277 138408S NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 CRACKED VERTICAL TORQUE BOX WEB BS 1236, LBL 20.5, WL 195. *S/D* REMOVED, REPLACED AND FAB PER IAW FEDEX SRM 51-10-1, 51-40-2 FIG 1. 2 L 7 3 4F RT A3WE 2001062100007 20010621 00007 NM 2001 6 21 01FDEA00474 1 20010619 A 5310 WEB BOEING 727 727277 138408S NM BS 1225 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 NR 272 CRACKED VERTICAL TORQUE BOX WEB BS 1225, LBL 20.5, WL 193. ** S/D ** R&R & FAB PER IAW FEDEX SRM 51-10-11, 51- 40-2 FIG 1. 2 L 7 3 4F RT A3WE 2001070600023 20010706 00023 NM 2001 7 6 01FDEA00429 1 20010611 A 5311 651766445 FRAME BOEING 727 7272D4 138407U NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 FRAME IS DENTED AT BS 560 AT STRINGER 24 LT. 2 L 7 3 4F A3WE 2001070900002 20010709 00002 NM 2001 7 9 01FDEA00431 1 20010611 A 5311 651766445 FRAME BOEING 727 7272D4 138407U NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 FRAME DENTED TWO PLACES AT BS 500 BETWEEN STR 23 LT AND 25 LT. 2 L 7 3 4F A3WE 2001062100008 20010621 00008 WP 2001 6 21 DKAA01007 1 20010308 A 5315 1414813 FLOORBEAM DOUG DC9 DC915F 3022037 WP FUSELAGE DAMAGED A DKAA K NONE O OTHER IN INSP/MAINT 1 GL 23 916R 47229 47010 FOUND RIGHT UPPER SIDE FLOORBEAM DAMAGED AT FS 160. REPAIRED PER DER DRAWING NR 53-01010-4, DATED 01/16/2001. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 2001062100009 20010621 00009 NE 2001 6 21 DKAA01012A 2 20010421 A 7200 ENGINE DOUG DC9 DC915F 3022037 WP PWA JT8 JT8D7B 52053 NE A DKAA K NONE E VIBRATION/BUFFET TX TAXI/GRND HDL 1 GL 23 916R 47010 656878 NR 2 ENGINE HAS VIBRATION. REMOVED NR 2 ENGINE. SHIPPED TO ENGINE REPAIR CENTER, AWAITING RESULTS INVESTIGATION WORKSC OPE. (M) 2 L 7 2 4F 4 F A6WE E2EA 2001062100010 20010621 00010 WP 2001 6 21 USAAD01118 1 20010530 A 3350 9721055 BATTERY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 829US 49429 MCO - THE LOW LEVEL LIGHT AT SEAT 25D DID NOT TEST. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F A6WE 2001062100011 20010621 00011 NM 2001 6 21 USAA010566 1 20010518 A 5300 SKIN BOEING 737 737201 1384454 NM BS 468 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND FUSELAGE SKIN CORRODED, BS 468, BL 0. REMOVED DAMAGE, INSTALLED REPAIR DOUBLER PER SRM 51-20-4 AND 53-30-3. (M) 2 L 7 2 4F A16WE 2001062100012 20010621 00012 NM 2001 6 21 USAA010565 1 20010518 A 5300 SKIN BOEING 737 737201 1384454 NM CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND FUSELAGE SKIN CRACKED .25 INCH AFT ENTRY DOOR, UPPER HINGE CUTOUT. INSTALLED DOUBLER PER SRM 543-30-3, FIG 21A. (M) 2 L 7 2 4F A16WE 2001062100013 20010621 00013 NM 2001 6 21 USAA010564 1 20010518 A 5300 SKIN BOEING 737 737201 1384454 NM BS 345 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND SKIN CRACKED .25 INCH, BS 345, AFT LOWER CORNER OF AIRSTAIR CUTOUT. REMOVED AND REPLACED REPAIR TRIPLER PER EA 69582. (M) 2 L 7 2 4F A16WE 2001062100014 20010621 00014 NM 2001 6 21 USAA010563 1 20010518 A 5300 BEAM BOEING 737 737201 1384454 NM BS 663 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND BEAM CRACKED 3 INCHES, BS 663, BL 0. INSTALLED REPAIR ANGLES PER EA 69611. (M) 2 L 7 2 4F A16WE 2001062100015 20010621 00015 NM 2001 6 21 USAA010560 1 20010518 A 5300 WEB BOEING 737 737201 1384454 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND PRESSURE BULKHEAD WEB WITH CRACKS .125 INCH TO 1 INCH, BS 178, LBL 12 TO RBL 17, WL 188 TO WL 214. DAMAGED REMOVED, INSTALLED REPAIR DOUBLER PER EO 5300V153 AND EA 69493. (M) 2 L 7 2 4F A16WE 2001062100016 20010621 00016 NM 2001 6 21 USAA010557 1 20010518 A 5310 WEB BOEING 737 737201 1384454 NM BS 712 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND WEB CRACKED 1 INCH, BS 712, LBL 24. INSTALLED REPAIR DOUBLER, REPLACEMENT WEB AND 4 VERTICAL STIFFENERS PER EA 69504. (M) 2 L 7 2 4F A16WE 2001062100017 20010621 00017 NM 2001 6 21 USAA010556 1 20010518 A 5300 SHEAR TIE BOEING 737 737201 1384454 NM BS 986 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND FRAME SHEAR TIE CORRODED 5 INCHES BY 1 INCH, BS 986 STRINGER 24R/25R. FABRICATED AND REPLACED SHEAR TIE PER BAC DRAWING 65-46564, SRM 51-10-0 AND 51-30-0. (M) 2 L 7 2 4F A16WE 2001062100018 20010621 00018 EU 2001 6 21 SIMA20010163 1 20010116 A 5315 S5337241123402 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AT 431 SAW - DURING MBV-1 INSPECTION MAINTENANCE REPORTED FLOORBEAM 29 HAD AN OVERSIZED HI-LOCK HOLE AT THE LEFT AFT SEAT TRACK ATTACH POINT. MAINTENANCE REPAIRED THE FLOORBEAM IAW SRM 53-00-00 FIGURE 429. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001062100019 20010621 00019 EU 2001 6 21 SIMA20010592 1 20010228 A 3350 AD3127 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA O OTHER L NO TEST NR NOT REPORTED 1 SW 21 293AT 293 MIA - FLT 5370 - CREW REPORTED FLOOR PROXIMITY LIGHTS OUT AT ROW 10, 11, 12. MAINTENANCE REMOVED AND REPLACED POWER SUP PLY UNIT 15WL. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001062100021 20010621 00021 EU 2001 6 21 SIMA20010671 1 20010308 A 7100 12456008 VALVE SAAB SF340 340B 7860101 EU LT ENGINE INOPERATIVE A SIMA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SW 21 313AE 340B313 BTV - FLT 4750 - NOTED LOW NR 1 PGB OIL TEMP FOLLOWED BY FLUCTUATING NR 1 PGB OIL PRESS AND NR 1 ENGINE OIL PRESS, APPLI ED ENGINE SHUTDOWN PROCEDURE. MAINTENANCE REMOVED AND REPLACED THE PROPELLER OIL TEMPERATURE REGULATOR IAW SAAB MM. OP ERATIONAL AND LEAK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001062100022 20010621 00022 EU 2001 6 21 SIMA20010682 1 20010309 A 7720 7278013507 SENSOR SAAB SF340 340B 7860101 EU LT/RT ENGINES A SIMA D RETURN TO BLOCK G MULTIPLE FAILURE TO TAKEOFF 1 SW 21 238AE 340B238 ALB - FLT 5142 - AFTER TAKEOFF CREW REPORTED RIGHT TAIL PIPE HOT LIGHT CAME ON. CREW RETARDED POWER LEVER AND LIGHT WEN T OUT, 30 SECONDS LATER LEFT TAIL PIPE HOT LIGHT CAME ON, POWER LEVER WAS RETARDED BUT LIGHT STAYED ON. MAINTENANCE FOU ND HIGH RESISTANCE ON LEFT SENSORS. ALL SENSORS FOR BOTH ENGIENS WERE REMOVED AND REPLACED. OPS CHECK WAS GOOD AND AIR CRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001062100023 20010621 00023 EU 2001 6 21 SIMA20010792 1 20010320 A 2600 72111211000 DETECTOR SAAB SF340 340B 7860101 EU LAVATORY INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 320AE 340B320 SBP - FOUND LAVATORY SMOKE INDICATOR ILLUMINATED ON CENTRAL WARNING PANEL. REMOVED AND REPLACED IAW SAAB AMM 26-13. OP S CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001062100024 20010621 00024 EU 2001 6 21 SIMA20010812 1 20010322 A 2400 23080031 GENERATOR SAAB SF340 340B 7860101 EU RT ENGINE INOPERATIVE A SIMA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 393AE 340B393 DFW - FLT 3351 - CREW REPORTED THE RIGHT DC GENERATOR FAILED SHORTLY AFTER TAKEOFF. MAINTENANCE REMOVED AND REPLACED TH E RIGHT DC GENERATOR IAW SAAB MM. OPERATIONAL AND LEAK CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001062100025 20010621 00025 EU 2001 6 21 SIMA20010861 1 20010327 A 3200 D49412001 CONTROL PANEL SAAB SF340 340B 7860101 EU COCKPIT INOPERATIVE A SIMA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SW 21 340RC 340B340 BOS - FLT 4601 - AFTER TAKEOFF, CREW REPORTED THE LANDING GEAR INTRANSIT LIGHT STAYED ON. MAINTENANCE REMOVED AND REPLA CED LANDING GEAR CONTROL PANEL IAW SAAB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001062100026 20010621 00026 EU 2001 6 21 SIMA20010901 1 20010331 A 3350 V72914 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 236AE 340B236 PWM - FLT 4864 - SEVERAL EMERGENCY LIGHTS INOPERATIVE, FERRY TO ALB FOR REPAIRS. REMOVED AND REPLACED ALL POWER SUPPLIE S (20LN, S/N 19174, 21LN, S/N 18287, 22LN S/N 18991, 23LN S/N 18189, 24LN S/N 18315, IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001062100027 20010621 00027 WP 2001 6 21 01FDEA00476 1 20010621 A 3230 ARG7531502 TARGET DOUG DC10 DC1010F 3022111 WP RH MG DOOR BROKEN A FDEA O OTHER J P WARNING INDICATION NO WARNING INDICATION TO TAKEOFF 1 SO 25 383FE 46616 01-203 ON T/O AT GEAR RETRACTION RMLG IND (BOTH PILOT & S/O POS) REMAIN RED WITH L/MAIN & NOSE GEAR IND UP, RECYCLED GEA R PER RED TABS PROC & RMG IND REMAIN RED. R&R RH GEAR DOOR UPLOCK TARGET PER DC10 MM 32-34-2-1. 2 L 7 3 4F A22WE 2001062100028 20010621 00028 NM 2001 6 21 01FDEA00477 1 20010621 A 2830 FUEL CAP BOEING 727 727227 1384078 NM #3 ENGINE FAULTY A FDEA A UNSCHED LANDING K FLUID LOSS TO TAKEOFF 1 SO 25 496FE 21670 01-204 AFT T/O #3 FUEL TANK GAUGE IND LOSS OF FUEL FROM THAT TANK. #3 BOOST PUMPS SHUTOFF & CROSSFEED #3 ENG FROM #1 FUE L TANK. INSTALL NEW FUEL CAP IN ACCORD WITH B727 MM 28-11-031-4. OK TO CONTINUE. 2 L 7 3 4F A3WE 2001071800043 20010718 00043 NM 2001 7 18 2001UALA00986 1 20010611 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 317UA 23949 FLOORBEAM CORRODED STA 947.5, RBL 30. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001071800044 20010718 00044 NM 2001 7 18 2001UALA00987 1 20010611 A 5320 CHANNEL BOEING 737 737322 1384676 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 318UA 23950 AFT PIT BILGE ANTENNA CUTOUT CORRODED STA 727 LBL 11. MAJOR REPAIR ACCOMPLISHED. REPLACED CHANNEL. 2 L 7 2 4F RT A16WE 2001071800056 20010718 00056 NM 2001 7 18 2001UALA00988 1 20010611 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 CREASE BEAM WEB CORRODED STA 635, LBL 69, WL 208. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM WEB. 2 L 7 2 4F RT A16WE 2001071800057 20010718 00057 NM 2001 7 18 2001UALA00989 1 20010611 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 FLOORBEAM CORRODED STA 1016. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOORBEAM UPPER CAP. 2 L 7 2 4F RT A16WE 2001071800058 20010718 00058 NM 2001 7 18 2001UALA00990 1 20010611 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 INTERCOSTAL CRACKED STA 178, WL 207, RBL 24. MAJOR REPAIR ACCOMPLISHED. REPLACED INTERCOSTAL WEB. 2 L 7 2 4F RT A16WE 2001071800074 20010718 00074 NM 2001 7 18 2001UALA01008 1 20010612 A 5330 SKIN BOEING 757 757222 1384956 NM FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 503UA 24624 FUSELAGE SKIN GOUGED STA 760-780, STR 16L. MAJOR REPAIR ACCOMPLISHED. REMOVED PREVIOUS REPAIR AND INSTALLED NEW DOUBLE R. 2 L 7 2 4F RT A2NM 2001071800075 20010718 00075 NM 2001 7 18 2001UALA01009 1 20010612 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 AFT CABIN FLOORBEAM LOWER SURFACE CORRODED STA 1681, RBL 4, RBL 30, LBL 12. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE AND STRAP REPAIR. 2 L 7 2 4F RT A2NM 2001071800095 20010718 00095 NM 2001 7 18 2001UALA01023 1 20010613 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 CABIN FLOOR SUPPORT STRUCTURE CORRODED STA 324 - 344, RBL 60. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR STRAPS. 2 L 7 2 4F RT A2NM 2001062100029 20010621 00029 NM 2001 6 21 AWXA0001885 1 20010620 A 5330 6562212 SKIN BOEING 737 7373G7 1384595 NM CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 D: Skin damage on D/B side of L/H emergecy exit center AFT sideC Repaired IAW b737-300 SRM 52-00-01 PG 203-204 2 L 7 2 4F RT A16WE 2001062100030 20010621 00030 NM 2001 6 21 AWXA0001886 1 20010620 A 5310 140N5318 WEB BOEING 757 7572S7 1384962 NM CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 D: Aft galley shear web corroded F$ 1715 at RBL 14 to LBL 51C Removed corrosion, fabricated and installed repair doubler s at F5 1715 LBL 17-34 and RBL 14-23 Per SRM 53-60-51 fig 203 and SRM 51-40-02 2 L 7 2 4F RT A2NM 2001062100031 20010621 00031 EU 2001 6 21 RAIA00106012 1 20010620 A 2750 TY175902 CONTROL BOX JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT FAILED A RAIA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 CE 03 551HK 5901 41040 7034-STL-FLAP ASSYMETRY CAPTION ILLUMINATED DURING TAXI. MAINTENANCE INSPECTED AND REPLACED FLAP CONTROL UNIT. 2 L 7 2 4T RT A41NM 2001062100032 20010621 00032 NE 2001 6 21 RAIA00106010 2 20010618 A 7300 31059008 FUEL CONTROL JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE LEFT ENGINE FAILED A RAIA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CE 03 573HK 3983 1258 41092 75103 7137-MEM-LEFT ENGINE WOULD NOT ACHEIVE TARGET TORQUE. MAINTENANCE INSPECTED AND REPLACED LEFT ENGINE FUEL CONTROL UNIT. 2 L 7 2 4T 4 T RT A41NM E18NE 2001062100033 20010621 00033 EU 2001 6 21 RAIA00106011 1 20010619 A 2613 51228801 OVERHEAT JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 559HK 13021 41075 5398-EWR-RIGHT NACELLE OVERHEAT LIGHT ILLUMINATED DURING TAXI. MAINTENANCE INSPECTED AND REPLACED RIGHT ENGINE OVERHEAT LOOP. 2 L 7 2 4T RT A41NM 2001062100034 20010621 00034 NM 2001 6 21 DHL2001709008 1 20010531 A 3234 69529501 CONTROL HANDLE BOEING 727 72782C 1384026 NM COCKPIT BROKEN A DHLA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 709DH 19968 GREEN GEAR NOSE LIGHT EXTINGUISHED AND RED GEAR LIGHT ILLUMINATED WITH GEAR LEVER DOWN. ABNORMAL PROCEDURES ACCOMPLISHE D. FOUND ARM AND LINKAGE BROKEN AT APEX ATTACH POINT. REPLACED LEVERS WITH NEW AND INSTALLED IAW BMM 32-61-21. ALL TE STING CHECKED GOOD. 2 L 7 3 4F A3WE 2001062100035 20010621 00035 2001 6 21 DHL2001743008 4 20010531 A 2210 CONTROL PANEL BOEING 727 727225 1384077 NM COCKPIT DIRTY A DHLA K NONE O OTHER CL CLIMB 1 SO 01 743DH 22438 AUTOPILOT VERTICAL SPEED KNOB DOES NOT FOLLOW VERTICAL SPEED. UNABLE TO ENGAGE AUTOPILOT. CLEANED AND RESEATED MODE CO NTROL PANEL OPS CHECK NORMAL IAW MM 22-11-101. TESTED SYSTEM IAW 22-11-01. SYS CKS NORMAL. NO DEFECTS NOTED. 2 L 7 3 4F A3WE 2001062100036 20010621 00036 NE 2001 6 21 2001UALA00788 2 20010518 A 7530 CONTROL UNIT BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE ENGINE OUT OF RIG A UALA O OTHER M OVER TEMP CR CRUISE 1 WP 29 610UA 21871 FUEL QTY FOR WINGS PLUS-MINUS 1700 LBS BETWEEN GAUGES. VARIED THROUGHOUT FLIGHT. FMC QTY APPEARS ACCURATE. SUPPLEMENTA L DATA UPDATE ENGINE WAS REPLACED DUE TO OVERTEMP. DURING ENGINE PRE-REPAIR RUN, FOUND ENGINE VANE BLEED CONTROL(EVBC) WAS OUT OF TRIM. EVBC WILL BE OVERHAULED 2 L 7 2 4F 4 F RT A1NM E3NE 2001062100037 20010621 00037 NM 2001 6 21 DL72L010805 1 20010519 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 506DA 21308 LEFT FORWARD OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, CKS GOOD. 2 L 7 3 4F A3WE 2001062100038 20010621 00038 NM 2001 6 21 DL72L010822 1 20010522 A 5720 STIFFENER BOEING 727 727232 1384082 NM WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 504DA 21306 A 2 INCH CRACK AT WING L/E FRONT SPAR STIFFENER AT NR 6 SLAT O/B TRACK-O/B STIFFENER. REPAIR PER M/M 57-20-021-8. 2 L 7 3 4F A3WE 2001062100039 20010621 00039 NM 2001 6 21 DL72L010836 1 20010523 A 5320 651751738 BEAM BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 504DA 21306 INSPECTION OF THE RT TORQUE BOX STRUCTURE OF VENTRAL STAIRWAY OPENING REVEALED A 3 INCH CRACK IN THE UPPER HORIZONTAL BE AM AT FS 1263. THE CRACKED PART WAS REMOVED AND A NEW PART INSTALLED PER ER/A 380894-14AD. THE CRACK IS TYPICAL OF BAC S/B 727-53-0129. 2 L 7 3 4F A3WE 2001062100040 20010621 00040 NM 2001 6 21 DL72L010862 1 20010529 A 5313 STRINGER BOEING 727 727232 1384082 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 514DA 21430 FOUND CORROSION STR 27L AT STA 1050 REF NRC 68. REPAIR PER SRM 53-10-3. 2 L 7 3 4F A3WE 2001062100041 20010621 00041 NM 2001 6 21 DL72L010863 1 20010529 A 5720 STIFFENER BOEING 727 727232 1384082 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 514DA 21430 BOTH L/E SPAR STIFFENERS CRACKED AT NR 2 SLAT I/B TRACK. REPAIR PER M/M 57-20-021-8. 2 L 7 3 4F A3WE 2001062100043 20010621 00043 NM 2001 6 21 DL72L010910 1 20010604 A 5755 ANGLE BOEING 727 727232 1384082 NM SPOILER CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 O/B ATTACH ANGLE CRACKED NR 12 SPOILER ACT SUPPORT CASTING. REPLACED ANGLE PER M/M 57-42-000-8. 2 L 7 3 4F A3WE 2001062100044 20010621 00044 NM 2001 6 21 DL72L010911 1 20010604 A 5754 ANGLE BOEING 727 727232 1384082 NM SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 FOUND ON C1 LETTER CK NR 2 SLAT LOWER COVE SKIN ANGLE IS CRACKED AT THE TAI DUCT. REPAIRED PER MM 57-54-000-8. 2 L 7 3 4F A3WE 2001062100045 20010621 00045 NM 2001 6 21 DL72L010912 1 20010604 A 5754 RIB BOEING 727 727232 1384082 NM SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 FOUND ON C1 LETTER CK NR 1 SLAT NOSE RIB IS CRACKED I/B SIDE OF ACTUATOR ROD END. REPAIRED PER MM 57-54-000-8. 2 L 7 3 4F A3WE 2001062100046 20010621 00046 NM 2001 6 21 DL72S010790 1 20010518 A 3350 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 537DA 22073 DURING STBY ELEC CK NOTICED SEVERAL EMERGENCY LIGHTS WERE INOP. REPLACED AFT CRT AISLE EXIT LIGHT BATTERY PACK. REPLAC ED MID CABIN CTR AISLE EXIT LIGHT ASSY. 2 L 7 3 4F A3WE 2001062100047 20010621 00047 NM 2001 6 21 DL72S010798 1 20010518 A 3350 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 539DA 22385 LEFT INTERIOR EMERGENCY EXIT SIGN INOP. RELAMPED SAME, CHECKS OK. 2 L 7 3 4F A3WE 2001062100048 20010621 00048 NM 2001 6 21 DL72S010799 1 20010519 A 3350 900542 RACK BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 528DA 21702 MID CABIN CTR AISLE EXIT LIGHT INOP. REPAIRED CONNECTOR. REPLACED BATTERY AND RACK. 2 L 7 3 4F A3WE 2001062100049 20010621 00049 NM 2001 6 21 DL72S010800 1 20010519 A 3350 900542 RACK BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 528DA 21702 AFT CTR AISLE EMERGENCY LIGHT INOP. REPLACED RACK AND BATTERY, OPER NOW OK. 2 L 7 3 4F A3WE 2001062100050 20010621 00050 NM 2001 6 21 DL72S010808 1 20010520 A 3350 900542 BATTERY PACK BOEING 727 727225A 1384077 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8873Z 21291 AFT OVERWING EMERGENCY LIGHT INOP. BATTERY PACK WAS FOUND TO BE BAD. REMOVED AND REPLACED SAME. 2 L 7 3 4F RT A3WE 2001062100051 20010621 00051 NM 2001 6 21 DL72S010821 1 20010522 A 7110 DOOR BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 3 ENGINE MISSING A DALA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 SO 27 519DA 44203 21470 700591 PANEL NR 3 ENGINE OIL SERVICE DOOR MISSING. REPLACED NR 3 OIL SERVICE DOOR. 2 L 7 3 4F 4 F A3WE E2EA 2001062100052 20010621 00052 NM 2001 6 21 MWEA010997 1 20010619 A 2750 V3601 SWITCH DOUG MD88 MD88 3023688 NM COCKPIT DIRTY A MWEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 31 601ME 49762 ON TAKE OFF WHEN POWER LEVERS ADVANCED A TAKE OFF FLAP WARNING WITH SLAT EXTEND AND FLAPS AT 11 POSTION. -- FLAP TAKE O FF WARNING SWITCH WAS CLEANED AND TESTED. TAKE OFF WARNING SYSTEM FUNCTIONALLY CHECKED OK. 2 L 7 2 4F RT A6WE 2001062100053 20010621 00053 WP 2001 6 21 MWEA010999 1 20010618 A 5310 59114013 SKIN DOUG DC9 DC914 3022034 WP FWD DOOR JAMB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 FUSELAGE SKIN CRACKED IN LOWER AFT CORNER OF FORWARD AIRSTAIR DOOR JAMB. -- REMOVED DAMAGE AND INSTALLED DOUBLER AND F ILLER. 2 L 7 2 4F A6WE 2001062100054 20010621 00054 NM 2001 6 21 DL72S010831 1 20010524 A 7120 MOUNT BOEING 727 727232 1384082 NM NR 3 ENGINE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 540DA 22386 REPETITIVE INSPECTION OF THE FWD ENGINE MOUNT SUPPORT FITTING ON THE NR 3 PYLON REVEALED SMALL TYPICAL CRACKS IN HOLES B , C, D, F, & H OF THE FITTING. THE CRACKS ARE TYPICAL OF AD 97-05-08. THE HOLES WERE OVERSIZED TO REMOVE THE CRACKS AN D THEN OVERSIZED FURTHER FOR INSURANCE. LARGER DIAMETER FASTENERS WERE INSTALLED PER THE PROCEDURES OF FED EX S/B 2000 -5410A01 AND ER/A 380887-14AD. 2 L 7 3 4F A3WE 2001062100055 20010621 00055 NM 2001 6 21 DL72S010832 1 20010523 A 5330 6518420761 SKIN BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 525DA 21585 THE L1 DOOR OPENING SKIN ASSY WAS FOUND WITH A CRACK IN THE SKIN AND BONDED DOUBLER AS WELL AS THE UNDERLYING BEARSTRAP AT THE UPPER HINGE CUTOUT. THE CRACK WAS REMOVED WITH A 3.4 INCH CUTOUT IN THE SKIN AND A 3.1 X 1 INCH CUTOUT IN THE BEARSTRAP. THE CUTOUTS WERE REPAIRED WITH 2 EXTERNAL ALUMINUM DOUBLERS PER ER/A 380835-14, REV A. 2 L 7 3 4F A3WE 2001062100056 20010621 00056 NM 2001 6 21 DL72S010833 1 20010523 A 5320 BEAM BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 525DA 21585 THE RBL 36.83 VERTICAL BEAM ON THE FS 1183 BULKHEAD WAS FOUND WITH A 1 INCH TYPICAL CRACK AT WL 238. THE CRACK IS TYPIC AL OF BAC S/B 727-53-0192. THE CRACK WAS STOP DRILLED AND REPAIRED WITH 2 REPAIR ANGLES PER THE REQUIREMENTS OF THE S/B AND ER/A 380836-14, REV A. 2 L 7 3 4F A3WE 2001062100057 20010621 00057 NM 2001 6 21 DL72S010834 1 20010523 A 5330 655457023 SKIN BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 525DA 21585 THE UPPER FWD CORNER OF THE R1 DOOR CUTOUT WAS FOUND WITH A .5 INCH CRACK IN THE SKIN AND BONDED DOUBLERS. THE CRACK W AS REMOVED WITH A TRIMOUT TO ALL SKIN LAYERS. THE TRIMOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 380802-14, REV A. 2 L 7 3 4F A3WE 2001062100058 20010621 00058 NM 2001 6 21 DL72S010835 1 20010523 A 5311 651592231 FRAME BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 525DA 21585 THE FS 380 FRAME ABOVE THE R1 DOOR WAS FOUND WITH A .5 INCH CRACK IN THE INNER FLANGE AT THE LOWER END OF THE FRAME AT WL 280. THE CRACK WAS EMANATING FROM A FASTENER HOLE. THE CRACKED AREA OF FLANGE WAS TRIMMED AWAY TO REMOVE THE CRACK AN REPAIRED WITH A REPAIR ANGLE PER ER/A 380837-14, REV A. 2 L 7 3 4F A3WE 2001062100059 20010621 00059 NM 2001 6 21 DL72S010839 1 20010524 A 3350 FUSE BOEING 727 727232 1384082 NM POWER SUPPLY BLOWN A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 539DA 22385 SEAT EMERGENCY EXIT LIGHTS AT ROWS 12-19 INOP. REPLACED FUSE ON PWR SUPPLY M9026. 2 L 7 3 4F A3WE 2001062100060 20010621 00060 NM 2001 6 21 DL72S010865 1 20010529 A 3350 SIGN BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST CR CRUISE 1 SO 27 536DA 22049 EMERGENCY EXIT SIGN INOP ACROSS FROM ROW 32. RELAMPED EMERGENCY EXIT SIGN. 2 L 7 3 4F A3WE 2001062100061 20010621 00061 NM 2001 6 21 DL72S010872 1 20010530 A 3350 900542 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8873Z 21291 EMERGENCY EXIT LIGHT AT ROW 32 INOP. REPLACED LIGHT RACK. 2 L 7 3 4F A3WE 2001062100062 20010621 00062 WP 2001 6 21 CALA0100564 1 20010620 A 5330 SKIN DOUG DC9 DC982 3022082 WP FS 275 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND R/H FUSELAGE SKIN DENTED AT FS 275, LONGERON 24R. THE DENTED AREA WAS REFORMED IAW SRM 51-10-2. A REPAI R DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, SHEET 22, 51-10-3, AND 51-10-2. 2 L 7 2 4F A6WE 2001062100063 20010621 00063 WP 2001 6 21 CALA0100565 1 20010621 A 5330 SKIN DOUG DC9 DC982 3022082 WP AFT OF R1 DR GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND EXTERNAL FUSELAGE SKIN GOUGED AFT OF R-1 DOOR GUST LOCK. THE GOUGED AREA WAS REMOVED. SKIN FILLER AND R EPAIR DOUBLERS WERE INSTALLED IAW SRM 53-34-0, 51-10-4, 51-10-3, AND 53-04, FIGURE 24. 2 L 7 2 4F A6WE 2001062100064 20010621 00064 WP 2001 6 21 CALA0100567 1 20010621 A 5330 SKIN DOUG DC9 DC982 3022082 WP FS 264 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND L/H FUSELAGE EXTERNAL SKIN DENTED AT FS 264 JUST BELOW LONGERON 23L. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 2001062100065 20010621 00065 EU 2001 6 21 2001F00026 1 20010328 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 548AT 548 DFW - DURING SCHEDULED PS-2 CHECK MAINTENANCE REPORTED SEVERAL EMERGENCY LIGHTS IN CABIN TO BE INOPERATIVE. MAINTENANCE FOUND TWO EMERGENCY LIGHT POWER SUPPLY UNIT BATTERIES TO HAVE LOW VOLTAGE. MAINTENANCE CHANGED ALL FOUR BATTERIES. OP ERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. RED SIMA20010873. (M) 2 H 7 2 4T RT A53EU 2001062100066 20010621 00066 EU 2001 6 21 2001F00027 1 20010328 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 548AT 548 DFW - DURING SCHEDULED PS-2 CHECK MAINTENANCE REPORTED SEVERAL EMERGENCY LIGHTS IN CABIN TO BE INOPERATIVE. MAINTENANCE FOUND TWO EMERGENCY LIGHT POWER SUPPLY UNIT BATTERIES TO HAVE LOW VOLTAGE. MAINTENANCE CHANGED ALL FOUR BATTERIES. OP ERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20010873. (M) 2 H 7 2 4T RT A53EU 2001062100067 20010621 00067 EU 2001 6 21 2001F00028 1 20010328 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 548AT 548 DFW - DURING SCHEDULED PS-2 CHECK, MAINTENANCE REPORTED SEVERAL EMERGENCY LIGHTS IN CABIN TO BE INOPERATIVE. MAINTENANC E FOUND TWO EMERGENCY LIGHT POWER SUPPLY UNIT BATTERIES TO HAVE LOW VOLTAGE. MAINTENANCE CHANGED ALL FOUR BATTERIES. O PERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001062100068 20010621 00068 EU 2001 6 21 2001F00029 1 20010331 A 3350 V72914 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 236AE 340B236 PWM - FLT 4864 - SEVERAL EMERGENCY LIGHTS INOPERATIVE, FERRY TO ALB FOR REPAIRS. REMOVED AND REPLACED ALL POWER SUPPLIE S (20LN, S/N 19174, 21LN, S/N 18287, 22LN S/N 18991, 23LN S/N 18189, 24LN S/N 18315, IAW AMM. OPS CHECK GOOD. REF SIMA2 0010901. (M) 2 L 7 2 4T RT A52EU 2001062100069 20010621 00069 NM 2001 6 21 0102106307 1 20010608 A 5414 SKIN BOEING 747 747451 1384940 NM CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 667US 24222 During line check found crack in skin on the lower aft corner of cutout for number one pylon access panel 452ER . Repair ed per EA 63-184047. 2 L 7 4 4F RT A20WE 2001062100070 20010621 00070 WP 2001 6 21 USA2001F00000 1 20010504 A 3350 873100191 RECEIVER DOUG DC9 DC981 3022081 WP TAILCONE FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 803US 48035 WOULD NOT TEST. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES AND THE TAILCONE EMERGEIND - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE AND THE TAILCONE EMERGENCY REMOTE RECEIVER NCY REMOTE RECEIVER. REF USAAD01095. (M) 2 L 7 2 4F A6WE 2001062100071 20010621 00071 WP 2001 6 21 USA2001F00001 1 20010512 A 3350 86210151 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 808US 48040 IND - THE LOW LEVEL EMERGENCY LIGHTS DID NOT TEST. MAINTENANCE REPLACED THE CONTROL MODULE BATTERIES, THE LOW LEVEL LIG HT BATTERIES, AND THE OVERWING EXIT IDENTIFIER LIGHT ASSEMBLY. REF USAAD01102. (M) 2 L 7 2 4F A6WE 2001062100072 20010621 00072 WP 2001 6 21 USA2001F00002 1 20010512 A 3350 873100272 LIGHT DOUG DC9 DC981 3022081 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 808US 48040 IND - THE LOW LEVEL EMERGENCY LIGHTS DID NOT TEST. MAINTENANCE REPLACED THE CONTROL MODULE BATTERIES, THE LOW LEVEL LIG HT BATTERIES, AND THE OVERWING EXIT IDENTIFIER LIGHT ASSEMBLY. REF USAAD01102. (M) 2 L 7 2 4F A6WE 2001062100073 20010621 00073 WP 2001 6 21 USA2001F00003 1 20010514 A 3350 MISC0639 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 827US 48049 IND - THE LOW LEVEL EMERGENCY LIGHTS, NACELLE SCAN, AND CEILING LIGHTS AT SEAT ROWS 7 TO 17 WERE INOPERATIVE. MAINTENAN CE REPLACED THE LOW LEVEL, NACELLE SCAN, AND CEILING EMERGENCY LIGHT BATTERIES. REF USAAD01103. (M) 2 L 7 2 4F A6WE 2001062100074 20010621 00074 WP 2001 6 21 USA2001F00004 1 20010509 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 813US 48093 CLT - THE EMERGENCY LIGHTS FLICKERED ON AND OFF. MAINTENANCE REPLACED THE EMERGENCY LIGHT CONTROL MODULE BATTERY PACKS AND THE LOW LEVEL EMERGENCY LIGHT BATTERY AT SEAT 3D. REF USAAD01099. (M) 2 L 7 2 4F A6WE 2001062100075 20010621 00075 NM 2001 6 21 USAA0100440 1 20010420 A 5320 GUSSET BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 47122 22953 CLT - FOUND ATTACH BEAM GUSSET CRACKED .5 INCH, NOSE GEAR ACTUATOR STATION 259.5 BL 0. REMOVED AND REPLACED GUSSET, SRM 51-10-02, 51-40-00, BAC DRAWING NR 65-45819. (M) 2 L 7 2 4F RT A16WE 2001062100076 20010621 00076 NM 2001 6 21 USAA010422 1 20010420 A 5320 TIE CLIP BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 32200 24559 CLT - FOUND TIE CLIP APPROX .25 INCH, STATION 663, STRINGER 10L. REMOVED AND REPLACED SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001062200001 20010622 00001 NM 2001 6 22 0102126641 1 20010615 A 3350 6104781 BATTERY PACK BOEING 747 747212B 1384886 NM UPPER DECK INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 641W 21941 DURING LINE CHECK, FOUND UPPER DECK EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CH ECK NORMAL. 2 L 7 4 4F A20WE 2001062200002 20010622 00002 NM 2001 6 22 0102165517 1 20010612 A 3350 8P573 POWER SUPPLY BOEING 757 757251 1384970 NM FIRST CLASS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 517US 23205 DURING ROUTINE TEST, FORWARD EMERGENCY POWER SUPPLY FAILED 15 MINUTE TEST. MAINTENANCE REPLACED THE POWER SUPPLY AND BA TTERY. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A2NM 2001071100014 20010711 00014 NM 2001 7 11 01FDEA00483 1 20010621 A 5310 SHEAR TIE BOEING 727 727277 138408S NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 FRAME SHEAR TIE CRACKED BS 1263 BETWEEN STR 11L - 12L. *S/D* REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-4, 53-10-1. 2 L 7 3 4F RT A3WE 2001071100015 20010711 00015 NM 2001 7 11 01FDEA00484 1 20010621 A 5310 SHEAR TIE BOEING 727 727277 138408S NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 SHEAR TIE CRACKED AT FRAME BS 1263 BETWEEN STRINGER 11L - 12L. *S/D* REMOVED AND REPLACED PER SRM 51-10-1, 51-30-2, 51 -20-1, 51-10-2 & EA 7-5310-57285. 2 L 7 3 4F RT A3WE 2001071100016 20010711 00016 NM 2001 7 11 01FDEA00485 1 20010621 A 5310 SHEAR TIE BOEING 727 727277 138408S NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 CRACKED SHEAR TIE BS 1263 BETWEEN STR 11R-12R. *S/D* REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-1, 51-30-2, 51-20-1, 51-10-2. 2 L 7 3 4F RT A3WE 2001071100017 20010711 00017 NM 2001 7 11 01FDEA00486 1 20010621 A 5310 SHEAR TIE BOEING 727 727277 138408S NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 CRACKED FRAME SHEAR TIE BS 1263 BETWEEN STR 11R-12R. *S/D* REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-1, 51-30-2, 51 -20-1, 51-10-2. 2 L 7 3 4F RT A3WE 2001062200003 20010622 00003 NM 2001 6 22 01FDEA00487 1 20010617 A 5310 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 635 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 620FE 48791 SNRM N 202 MAIN DECK CARGO COMPT SEAT TRACK AT BS 635, RH X=8.5 FND CRACKED APPROX 4" LONG. R&R SEAT TRACK PER SRM 53-7 0-00, VOL I. 2 L 7 3 4F RT A22WE 2001062200004 20010622 00004 NM 2001 6 22 01FDEA00489 1 20010617 A 5310 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 635 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 620FE 48791 SNRM N 201 MAIN DECK CARGO COMPT SEAT TRACK AT BS 635 RH X=8.5 FND CRACKED APPROX 4" LONG. ** S/D ** R&R SEAT TRACK PER SRM 53-70-00 VOL I. 2 L 7 3 4F RT A22WE 2001070300099 20010703 00099 WP 2001 7 3 ABXA010343 1 20010606 A 5311 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 988AX 47084 CRACK ON FRAME AT FS 980 AND LONGERON 16 LEFT. REPAIRED FRAME IAW DC-9 SRM 53-03, FIGURE 32. 2 L 7 2 4F A6WE 2001062200005 20010622 00005 NM 2001 6 22 PCAA0106057 1 20010614 A 2121 M4641P2A FAN DHAV DHC8 DHC8102 2809003 NM BURNED OUT A PCAA K NONE O OTHER NR NOT REPORTED 1 EA 13 822EX 26577 187 ORH- FLIGHT#3712. CREW REPORTED STRONG ELECTRICAL SMELL IN COCKPIT. NO VISIBLE SMOKE. MAINTENANCE INSPECTED AIRCRAFT. F ORWARD FLIGHT COMPARTMENT FAN FOUND TO BE CAUSING ELECTRICAL SMELL. MEL 21-09 ISSUED FOR FLIGHT COMPARTMENT FAN. AIRCRAF T RETURNED TO SERVICE. FLIGHT COMPARTMENT FAN REPLACED 20 JUNE 2001. OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2001062200006 20010622 00006 NM 2001 6 22 PCAA0106058 1 20010620 A 2752 734374D JACKSCREW DHAV DHC8 DHC8102 2809003 NM RIGHT #3 CRACKED A PCAA K NONE O OTHER TX TAXI/GRND HDL 1 EA 13 841EX 19879 249 BGM- DURING ROUTINE MAINTENANCE VISIT WHILE PERFORMING TASK 2750/02, RIGHT OUTBOARD FLAP, INBOARD JACKSCREW STOP ASSEMBL Y WAS FOUND CRACKED. CRACK VERIFIED USING EDDY CURRENT TESTING. ACTUATOR REPLACED IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL 27-52-24. CYCLED FLAPS SEVERAL TIMES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001062200007 20010622 00007 WP 2001 6 22 CALA0100571 1 20010621 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP COCKPIT DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND COCKPIT FLOOR PANELS B,C,D,&E DELAMINATED. THE FLOOR PANELS WERE REPLACED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001062200008 20010622 00008 WP 2001 6 22 CALA0100579 1 20010622 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 1041-1117 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND CABIN FLOOR PANEL DELAMINATED AT STA 1041-1117. THE FLOOR PANEL WAS REPLACED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001062200009 20010622 00009 WP 2001 6 22 ABXA010344 1 20010603 A 5300 59356508N DOUBLER DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 924AX 47403 RIGHT F.S. 699 MAIN FRAME INBOARD POCKET UPPER FORWARD FLANGE CRACKED IN AREA OF "Z" ANGLE. INSTALLED REPAIR ANGLE DOUBL ER IAW DC-9 E.A. 53400120-001-1. 2 L 7 2 4F A6WE 2001062200010 20010622 00010 WP 2001 6 22 ABXA010345 1 20010604 A 5313 591147279 LONGERON DOUG DC9 DC931 3022065 WP PYLON BLKHD. CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 924AX 47403 CRACKED LONGERON 17 LEFT AT PYLON BULKHEAD. REPLACED LONGERON 17 LEFT IAW DC-9 SRM. 2 L 7 2 4F A6WE 2001062200011 20010622 00011 WP 2001 6 22 ABXA010346 1 20010604 A 5300 3916212501AX ANGLE DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 924AX 47403 FLOOR BEAM SUPPORT ANGLE AT 617 LEFT BUTT LINE 20 CRACKED. REPLACED ANGLE BRACKET IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2001062200012 20010622 00012 EU 2001 6 22 C2XA01BT116 1 20010622 A 3350 3011180A POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU CABIN FAULTY A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 34820 159 BTV---CO3014, DURING LINE CHECK ON RON MAINTENANCE FOUND LOWER AFT EMERGENCY LIGHT INOPERATIVE.....REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY IAW ATR42 MM 33-51-21. OPS. CHECKED GOOD. 2 H 7 2 4T RT A53EU 2001062200013 20010622 00013 EU 2001 6 22 C2XA01BT115 1 20010622 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN MISSING A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 34820 159 BTV---CO3014, DURING LINE CHECK ON RON MAINTENANFOUND FRONT EMERGENCY LIGHT POWER SUPPLY MISSING BATTERY PACK.....INSTAL LED EMERGENCY LIGHT BATTERY PACK IAW ATR42 MM 33-51-21. OPS. CHECKED GOOD. 2 H 7 2 4T RT A53EU 2001062200014 20010622 00014 EU 2001 6 22 RAIA00106013 1 20010620 A 2750 TY176004A TRANSMITTER JETAIR JETSTM JETSTM4101 1500501 EU RIGHT FLAP FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 555HK 15756 41072 7444-STL-FLAP ASSYMETRY CAPTION ILLUMINATED DURING TAXI. MAINTENANCE INSPECTED AND REPLACED RIGHT FLAP POSITION TRANSMIT TER. 2 L 7 2 4T RT A41NM 2001062200015 20010622 00015 EU 2001 6 22 RAIA00106014 1 20010621 A 2435 23095002 GENERATOR JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILED A RAIA D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 CE 03 568HK 19 41086 7202-STL-RIGHT GENERATOR FELL OFF LINE DURING TAXI. MAINTENANCE INSPECTED AND REPLACED RIGHT ENGINE STARTER GENERATOR. 2 L 7 2 4T RT A41NM 2001062200016 20010622 00016 EU 2001 6 22 QXEA0101057 1 20010617 A 3350 GRIMES FOKKER F28 F28MK4000 4990810 EU A QXEA K NONE O OTHER NR NOT REPORTED 1 NM 09 475AU 1422 11222 FAT - CREW FOUND ALL EVACUATION LIGHTS INOPERATIVE. REMOVED AND REPLACED ALL NINE POWER SUPPLIES. OPERATIONAL CHECKS GOO D. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001062500001 20010625 00001 SO 2001 6 25 C2XA01IA273 1 20010621 A 3397 W18800624 WIRE EMB 120 EMB120ER 3260203 SO CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 51726 120174 IAH- DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHT AT SEAT 10A FAILED TO ILLUMINATE DURING TEST OF THE EMERGE NCY LIGHT SYSTEM. IAH- MAINTENANCE PLACED THE SYSTEM ON MEL, IAH- ON 06/22/2001 MAINTENANCE TROUBLESHOT THE SYSTEM,AND , FOUND A BROKEN WIRE, REPAIRED THE BROKEN WIRE,PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM,NO DEFECT S NOTED,CLEARED THE "MEL",AND,THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001062500002 20010625 00002 EU 2001 6 25 C2XA01IA274 1 20010621 A 3350 AD3127 POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 19812 099 IAH- MAINTENANCE,WHILE PERFORMING A LINE CHECK MAINTENANCE NOTED THAT THE CABIN EMERGENCY FLOOR LIGHTS FAILED TO ILLUMI NATE DURING TEST, IAH- MAINTENANCE REMOVED AND REPLACED THE LEFT HAND FORWARD POWER SUPPLY NUMBER 1, PERFORMED A OPERAT IONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001062500003 20010625 00003 2001 6 25 SWAA011734 4 20010616 A 2565 65C16820 RETAINER BOEING 737 7377H4 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 748SW 29800 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER LOOSE. R&R RIVET PER MM. 2 L 7 2 4F RT A16WE 2001062500004 20010625 00004 NM 2001 6 25 SWAA011742 1 20010616 A 5710 6567172 ATTACH FITTING BOEING 737 7373H4 1384600 NM LH WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 331SW 23695 DURING SCHEDULED SERVICE CHECK, FOUND LH MLG WALKING BEAM ATTACH FITTING CORRODED. R&R BEAM ATT ACH FITTING PER MM. 2 L 7 2 4F RT A16WE 2001062500005 20010625 00005 NM 2001 6 25 SWAA011743 1 20010617 A 5314 BAC1503 STIFFENER BOEING 737 7373A4 1384585 NM MAIN WHEEL WELL CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL STIFFENER CRACKED IN MAIN WHEEL WELL BULKHEAD BS 663, RBL 615. REPAIRED STIFFENER PER SWA RA. 2 L 7 2 4F RT A16WE 2001062500006 20010625 00006 NM 2001 6 25 SWAA011746 1 20010617 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 294, RBL 55 & WL 208, BS 440 BETWEEN STRINGERS 8R & 9R, BS 480 BETEWWN STRINGERS 8L & 9L. REPAIRED FRAMES PER BFG ER. 2 L 7 2 4F RT A16WE 2001062500007 20010625 00007 NM 2001 6 25 SWAA011747 1 20010617 A 5311 6546546 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMED CRACKED BETWEEN STR 8L & 9L, BS 787, BS 827 & BS 867, BETWEEN STR 8R & 9 R, BS 747. REPAIRED FRAMES PER BFG ER. 2 L 7 2 4F RT A16WE 2001062500008 20010625 00008 NM 2001 6 25 SWAA011749 1 20010616 A 5330 6545769 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 311SW 23333 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 428, STRINGER 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001062500009 20010625 00009 NM 2001 6 25 SWAA011751 1 20010617 A 5311 6546543 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RBL 64 & WL 201. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001062500010 20010625 00010 NM 2001 6 25 SWAA011759 1 20010618 A 5311 6547951 FRAME BOEING 737 7373H4 1384600 NM FWD CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED D CHECK, FOUND FWD CARGO DOOR FRAME CUT OUT CRACKED AT BS 492, RBL 37, WL 160. REPAIRED FRAME PER BOEING SERVICE BULLETIN. 2 L 7 2 4F RT A16WE 2001062500011 20010625 00011 NM 2001 6 25 SWAA011760 1 20010617 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING WALKAROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED ABOVE WINDOW 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001062500012 20010625 00012 NM 2001 6 25 SWAA011761 1 20010618 A 5313 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001062500013 20010625 00013 NM 2001 6 25 SWAA011771 1 20010618 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 11R. REPAIRED SKIN PER SR M. 2 L 7 2 4F RT A16WE 2001062500014 20010625 00014 2001 6 25 SWAA011772 4 20010619 A 2565 6556685 BRACKET BOEING 737 7373H4 1384600 NM AFT SVC DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE FWD ATTACH BRACKET CRACKED. R&R EMERGENCY EVAC SLIDE ATTACH BRACKET PER MM. 2 L 7 2 4F RT A16WE 2001062500015 20010625 00015 NM 2001 6 25 SWAA011774 1 20010619 A 5310 141A880 WINDOW POST BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 501SW 24178 DURING SCHEDULED RON CHECK, FOUND WINDOW POST CRACKED AT CAPT'S #1 WINDOW, UPPER LH CORNER. REPA IRED WINDOW POST PER SRM. 2 L 7 2 4F RT A16WE 2001062500016 20010625 00016 NM 2001 6 25 SWAA011777 1 20010619 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHT LENS MISSING AT FWD CABIN CEILING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2001062500017 20010625 00017 NM 2001 6 25 SWAA011778 1 20010619 A 3350 6556633 LENS BOEING 737 7373H4 1384600 NM FUSELAGE BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY OVER WING EXIT LIGHT LENS BROKEN. R&R EXIT LIGHT LE NS PER MM. 2 L 7 2 4F RT A16WE 2001062500018 20010625 00018 NM 2001 6 25 SWAA011780 1 20010620 A 5313 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 634SW 27937 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. R&R STR CLIP PER S RM. 2 L 7 2 4F RT A16WE 2001062500019 20010625 00019 NM 2001 6 25 SWAA011781 1 20010620 A 2731 BACB28AK04 BUSHING BOEING 737 7377H4 NM RH ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 797MX 27890 DURING SCHEDULED SERVICE CHECK, SI 11052, FOUND PLAY AT RH ELEVATOR TAB # 3 HINGE. R&R # 3 HINGE BUSHING PER MM. 2 L 7 2 4F RT A16WE 2001062500020 20010625 00020 NM 2001 6 25 SWAA011782 1 20010619 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT STRINGER 10R, BS 500C & BS 727B. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001062500021 20010625 00021 NM 2001 6 25 SWAA011783 1 20010619 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 19L. REPAIRED SKIN PER S RM. 2 L 7 2 4F RT A16WE 2001062500022 20010625 00022 NM 2001 6 25 SWAA011784 1 20010619 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT STRINGER 10L, BS 500A & BS 400. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001062500023 20010625 00023 NM 2001 6 25 SWAA011788 1 20010621 A 5314 BAC1498 STIFFENER BOEING 737 7373A4 1384585 NM MAIN WHEEL WELL CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED 1/4D CHECK, FOUND MLG WHEEL WELL BULKHEAD VERTICAL STIFFENER CRACKED BS 663, LBL6.15. R&R STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 2001062500025 20010625 00025 NM 2001 6 25 SWAA011790 1 20010621 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN FLOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 390SW 26593 DURING SCHEDULED C3 CHECK, FOUND EEPLS COVERS CRACKED BETWEEN ROWS 5 TO 24. R&R EEPLS COVE RS PER MM. 2 L 7 2 4F RT A16WE 2001062500026 20010625 00026 NM 2001 6 25 SWAA011791 1 20010621 A 5753 6546435 FLAP BOEING 737 7373H4 1384600 NM AFT FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED C3 CHECK, FOUND LH OTBD AFT FLAP DELAMINATED ON UPPER & LWR INBD SURFACES. R&R LH OTBD AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2001062500027 20010625 00027 NM 2001 6 25 SWAA011792 1 20010619 A 5310 6545776 BEAR STRAP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED D CHECK, FOUND BEAR STRAP CORRODED AT BS 844, RBL 15 TO RBL 18, WL157. REPAIRED BEAR STRAP PER BFG ER. 2 L 7 2 4F RT A16WE 2001062500028 20010625 00028 NM 2001 6 25 SWAA011793 1 20010621 A 5320 6546568 WEB BOEING 737 7373H4 1384600 NM AFT BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED 1/2D CHECK, FOUND WEB CRACKED AT PRESS BULKHEAD BS 1016, RBL 39. R&R WEB SECT ION PER SRM. 2 L 7 2 4F RT A16WE 2001062500029 20010625 00029 NM 2001 6 25 SWAA011799 1 20010620 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 091SW 22963 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND FUSELAGE STRINGERS CRACKED AT BS 360, STR 15R & BS 540, STR 15L. REPAIRED STRINGERS PER SRM. 2 L 7 2 4F A16WE 2001062500030 20010625 00030 2001 6 25 DHL2001805011 4 20010526 A 2213 1776001194 CONTROLLER DOUG DC8 DC873F 302199F WP AUTOPILOT SYS MALFUNCTIONED A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 805DH 46125 AUTOPILOT IN HDG MODE, RIGHT TURN 35 DEG BANK, LEFT TURN 25 DEG BANK. REMOVED AND REPLACED AUTOPILOT CONTROLLER. PERFO RMED OPERATIONAL CHECK IAW MM 22-20-0. OK FOR SERVICE. 2 L 7 4 4F RT 4A25 2001062500031 20010625 00031 2001 6 25 DHL2001805012 4 20010526 A 3425 2587909903 ADI DOUG DC8 DC873F 302199F WP COCKPIT DEFECTIVE A DHLA K NONE O OTHER AP APPROACH 1 SO 01 805DH 46125 AUTOPILOT WILL NOT TRACK GLIDESLOPE. 1 DOT OUTSIDE 5 MI, 1.5 DOT INSIDE 5 MI. REMOVED AND REPLACED HORIZON FLT INDICAT OR. OPERATIONAL CHECK FOUND GOOD. OK FOR SERVICE (F/O SIDE). 2 L 7 4 4F RT 4A25 2001062500032 20010625 00032 WP 2001 6 25 DHL2001806621 1 20010409 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - RT MLG W/W ANGLE LWR PART CRACKED 2 INCHES WITH STOP HOLE BETWEEN STA 920.000 TO STA 940.000 AND L-30R4. FABR ICATED REINFORCEMENT ANGLE WITH ALCLAD (7075 T6 0.050) IAW SRM 53-2-0 FIG 1B. TREATED AND PRIMED IAW SRM 51-1-8B. INST ALLED REINFORCEMENT ANGLE IAW SRM 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 2001062500033 20010625 00033 WP 2001 6 25 DHL2001806622 1 20010402 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - MAIN CARGO C-FLOOR INNER ANGLE FROM STA 640.00 TO STA 680 SHOWS 02 CRACKS OF 5 INCHES. REMOVED CRACKED ANGLE FROM FLOOR PANEL-C (STA 640 - 680) IAW SRM 51-1-21 PAGE 1. FABRICATED ANGLE (EXTRUSION BAC 1503.100122) IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE IAW SRM 51-1-21 PAGE 1. 2 L 7 4 4F RT 4A25 2001062500035 20010625 00035 WP 2001 6 25 DHL2001806624 1 20010408 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - FUSELAGE NOSE SECTION EXTERNAL SKIN CRACKED 1 INCH AT FS -40 L-32R. REMOVED FASTENERS IAW SRM 51-3-0 PAGE 1, 2 SRM 51-1-20D PAGE 21. CUT DAMAGED SKIN IAW DHL EO 010330, EO 2406, EO 2001076. CLEANED, TREATED, AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FILLER AND DOUBLER (7075 T6 0.050/0.063) IAW DHL EO 010330, EO 2406, EO 2001076. CLEANED, TRE ATED, AND PRIMED IAW SRM 51-1-8B APPLIED (PRC) SEALANT TO REWORK AREA IAW SRM 51-1-15 PAGE 1. INSTALLED FILLER AND DOUB LER WITH NEW FASTENERS IAW DHL EO 010330, EO 2406, EO 2001076, SRM 51-3-0 PAGE 1, 2, SRM 51-1-20D PAGE 21. 2 L 7 4 4F RT 4A25 2001062500036 20010625 00036 WP 2001 6 25 DHL2001806625 1 20010304 A 5751 SKIN DOUG DC8 DC873F 302199F WP AILERON DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - RT OUTBD AILERON UPPER SKIN SURFACE DENTED BETWEEN STA XRS 640-660. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1. REMOVED DAMAGED SKIN IAW DHL EO O10313, EO 2411, EO 2001078. CLEANED, TREATED, AND PRIMED AREA IAW SRM 51-1-8B. FABR ICATED NEW SKIN (ALCLAD 2024 T3 0.032) IAW DHL EO 010313, EO 2411, EO 2001078. CLEANED, TREATED AND PRIMED IAW SRM 51-1 -8B. INSTALLED NEW SKIN AND NEW FASTENERS IAW DHL EO 010313, EO 2411, EO 2001073, SRM 51-1-21 PAGE 21. REFER TO N/R 33 95 FOR WEIGHT AND BALANCE. 2 L 7 4 4F RT 4A25 2001062500037 20010625 00037 WP 2001 6 25 DHL2001806626 1 20010409 A 5522 SKIN DOUG DC8 DC873F 302199F WP LT ELEVATOR DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LT ELEVATOR UPPER EXTERNAL SKIN SHOWS DENT AND DEFORMATION STA XE 0.00 - XE 132.00. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1, REMOVED DAMAGED SKIN IAW EO DHL 010405, EO 2410, EO 2001099. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED SKIN (ALCLAD 2024 T3 0.032) IAW EO DHL 010405, EO 2410, EO 2001099. CLEANED, TREATED AND PRIMED IA W SRM 51-1-8B. INSTALLED NEW SKIN & NEW FASTENERS IAW EO DHL 010405, EO 2410, EO 2001099, SRM 51-1-21 PAGE 1. REFER TO N/R 3023 FOR WEIGHT AND BALANCE. 2 L 7 4 4F RT 4A25 2001062500038 20010625 00038 WP 2001 6 25 DHL2001806627 1 20010408 A 5522 SKIN DOUG DC8 DC873F 302199F WP LT ELEVATOR DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LT ELEVATOR UPPER EXTERNAL SKIN DEFORMED AND DENTED FROM STA XE 210 TO XE 246. REMOVED FASTENERS IAW SRM 51-1 -21 PAGE 1, REMOVED DAMAGED SKIN IAW EO DHL 010403, EO 2408, EO 2001123. CLEANED, TREATED, AND REPAIRED AREA IAW SRM 51 -1-8B. FABRICATED NEW SKIN (ALCLAD 2024 T3 0.032) IAW EO DHL 010403, EO 2408, EO 2001123. CLEANED, TREATED, AND REPAIR ED AREA IAW SRM 51-1-8B. INSTALLED NEW SKIN AND NEW FASTENERS IAW EO DHL 010403, EO 2408, EO 2001123. CLEANED, TREATED , SRM 51-1-21, PAGE 1. REFER TO N/R 3023 FOR WEIGHT AND BALANCE. 2 L 7 4 4F RT 4A25 2001062500039 20010625 00039 WP 2001 6 25 DHL2001806628 1 20010401 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - AFT CARGO COMPARTMENT AFT DOOR FWD UPPER CORNER (CUTOUT) DENTED AND CORRODED. REMOVED FASTENERS IAW SRM 51-1- 21 PAGE 1. BLENDED OUT DAMAGED AREA, FOUND OUT OF LIMITS IAW SRM 53-7-0 PAGE 2P. CLEANED, TREATED, AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED DOUBLER AND TRIPLER (7075 T6 0.080 / 0.090) IAW EO DHL 0103-6, EO 2332, EO 2001094. CLEANED, TREATED, AND PRIMED IAW SRM 51-1-8B. APPLIED (PRC) SEALANT TO FRAYING SURFACES IAW SRM 51-1-15 PAGE 1. INSTALLED DOUBL ER AND TRIPLER WITH NEW FASTENERS IAW EO DHL O10306, EO 2532, EO 2001094, SRM 51-1-21 PAGE 1. 2 L 7 4 4F RT 4A25 2001062500040 20010625 00040 WP 2001 6 25 DHL2001806629 1 20010409 A 5220 SKIN DOUG DC8 DC873F 302199F WP EXIT DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - RT AFT OVERWING EMERGENCY EXIT DOOR SKIN HAS 1 INCH CRACK AT RT FWD LWR CORNER. CUT OUT DAMAGED SKIN IAW DHL EO 010402, EO 2405, EO 2001124. CLEANED, TREATED, AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED DOUBLER (ALCLAD 7075 T6 0.071) IAW DHL EO 010402, EO 2405, AND EO 2001124. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. APPLIED (PRC) SEALANT ON REWORK AREA IAW 51-1-15 PAGE 1. INSTALLED DOUBLER IAW EO DHL 010402, EO 2405, AND EO 2001124, SRM 51-1-20 PAGE 9. 2 L 7 4 4F RT 4A25 2001062500041 20010625 00041 WP 2001 6 25 DHL2001806630 1 20010405 A 5320 3750257503D FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - AFT CARGO COMPARTMENT - SPLICE FITTING CRACKED 3 INCHES FROM STA 1040.000 TO STA 1060.000 L-31L. REMOVED CRAC KED FITTING FROM AFT CARGO COMPARTMENT (STA 1040 - 1060 L-31L) IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED AR EA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PAGE 9. 2 L 7 4 4F RT 4A25 2001062500042 20010625 00042 WP 2001 6 25 DHL2001806631 1 20010410 A 5320 975405837 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - AFT CARGO COMPARTMENT SHROUD ASSY ANGLE CRACKED 8 INCHES. REMOVE CRACKED ANGLE IAW SRM 51-1-21 PAGE 1. CLEAN ED, TREATED, AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-1-21 PAGE 1. 2 L 7 4 4F RT 4A25 2001062500043 20010625 00043 WP 2001 6 25 DHL2001806633 1 20010330 A 5543 47014521 HINGE BRACKET DOUG DC8 DC873F 302199F WP RUDDR TAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - UPPER RUDDER TAB HINGE LUG CRACKED AT ZRT 134.618. REMOVED CRACKED HINGE (BRACKET) IAW SRM 51-1-21 PAGE 1. F ABRICATED NEW HINGE (BRACKET) IAW ATM NR 044010A, EA 2001058, DWG 34701452. CLEANED, TREATED, AND PRIMED IAW SRM 51-1-8 B AND INSTALLED HINGE (BRACKET) IAW SRM 51-1-21 PAGE 1. 2 L 7 4 4F RT 4A25 2001062500044 20010625 00044 WP 2001 6 25 DHL2001806634 1 20010322 A 5320 5773275177 CHANNEL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - MAIN CARGO JOINT ANGLE FROM CROSSBEAM - INTERCOSTAL AT STA 680.000 LBL 46.5 CRACKED 2 INCHES. REMOVED CRACKED ANGLE (CHANNEL) IAW SRM 51-3-0 PAGE 1, 2. FABRICATED NEW ANGLE (CHANNEL) IAW ATM 044340A, EA 2001131, DWG 573275. CLE ANED, TREATED, AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE (CHANNEL) WITH NEW FASTENERS IAW SRM 51-3-0 PAGE 1, 2. 2 L 7 4 4F RT 4A25 2001062500045 20010625 00045 WP 2001 6 25 DHL2001806635 1 20010329 A 5320 5773275178 CHANNEL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - MAIN CARGO JOINT ANGLE FROM CROSSBEAM - INTERCOSTAL AT STA 630.000 LBL 24.000 CRACKED 1 INCH. REMOVED CRACKED ANGLE (CHANNEL) IAW SRM 51-1-20D PAGE 21. FABRICATED NEW ANGLE (CHANNEL) IAW ATM 044720A, EA 2001077, DWG 5773275. CL EANED, TREATED, AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE (CHANNEL) WITH NEW FASTENERS IAW SRM 51-1-20D PAGE 9. 2 L 7 4 4F RT 4A25 2001062500046 20010625 00046 WP 2001 6 25 DHL2001806636 1 20010410 A 5320 975044887 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - FUSELAGE - CUSP EXTRUSION - AFT DOOR FRAME JOINT ANGLE AT STA 1614.000 L-21 (LT) SHOWS CRACK OF 2 INCHES. REM OVED CRACKED ANGLE IAW SRM 51-1-20D PAGE 21. FABRICATED ANGLE IAW ATM 044210 A, EA 2001134, DWG 9750448. CLEANED, TREA TED, AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE IAW SRM 51-1-20D PAGE 9. 2 L 7 4 4F RT 4A25 2001062500047 20010625 00047 NM 2001 6 25 DL72S010866 1 20010529 A 8012 97907821 START VALVE BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE MALFUNCTIONED A DALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 515DA 21431 700089 START VALVE OPEN LIGHT FOR NR 1 ENGINE ILLUMINATED AFTER TAKEOFF. COMPLIED WITH POM PROCEDURES. START VALVE EXTINGUISH ED AFTER APPROXIMATELY 3 MINUTES AT IDLE POWER AND BLEED VALVE CLOSED. NO SECONDARY INDICATIONS. ACCOMPLISHED PRECAUTI ONARY SHUTDOWN FOR NR 1 ENGINE. REPLACED VALVE. ALSO REPLACED THE START VALVE PRESSURE SWITCH P/N 1G309, S/N 150. 2 L 7 3 4F 4 F A3WE E2EA 2001062500048 20010625 00048 NM 2001 6 25 DL72S010867 1 20010529 A 2130 39854021 VALVE BOEING 727 727232 1384082 NM LT PACK INOPERATIVE A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 540DA 22386 LOSS OF PRESSURIZATION IN FLT AT FL 330 CABIN ALT ROSE TO 13000. MTC FOUND THE LT PACK FWD PACK VALVE INOP. REPLACED S AME. 2 L 7 3 4F A3WE 2001062500049 20010625 00049 NM 2001 6 25 DL72S010874 1 20010531 A 5753 651626920 FLAP TRACK BOEING 727 727232 1384082 NM T/E FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 532DA 22045 DURING OVERHAUL THE INBD FLAP, INBD TRACK ASSY WAS FOUND WITH CORROSION AND WEAR. DAMAGE EXCEEDED ALLOWABLE LIMITS AT THE MLG BEAM ATTACH BOLT HOLES AND SPOTFACES, SPOILER BEAM ATTACH HOLES, MLG DOOR FWD AND AFT HINGE FITTING ATTACH HOLES, HINGE SUPPORT FITTING HOLES, FWD ATTACH LUG BORES AND GAPS, AND THE TOGGLE DETENT HOLE. REPAIR PER ER/A 401901- 14AD AND BF GOODRICH DOCUMENT 23-0859. 2 L 7 3 4F A3WE 2001062500050 20010625 00050 NM 2001 6 25 DL72S010875 1 20010531 A 5753 651927012 FLAP TRACK BOEING 727 727232 1384082 NM T/E FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 532DA 22045 DURING OVERHAUL THE INBD FLAP, INBD TRACK WAS FOUND WITH CORROSION AND WEAR EXCEEDING THE ALLOWABLE LIMITS. REPAIRED PE R ER/A 401900-14AD AND BF GOODRICH DOCUMENT 23-0682. 2 L 7 3 4F A3WE 2001062500051 20010625 00051 NM 2001 6 25 DL72S010876 1 20010531 A 2751 2061111 INDICATOR BOEING 727 727232 1384082 NM COCKPIT FAULTY A DALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 27 543DA 22392 AFTER TAKEOFF RETRACTING FLAPS TO 5 DEGS INBD FLAPS REMAINED AT 15 DEGS. INBOARD FLAPS REMAINED AT 15 DEGS AFTER POM PRO CEDURES. PILOT DECLARED EMERGENCY. REPLACED INBD FLAP POSITION IND AND INBD FLAP ASSY LOCK OUTRELAY R-187. 2 L 7 3 4F A3WE 2001062500052 20010625 00052 NM 2001 6 25 DL72S010877 1 20010531 A 5240 DOOR FRAME BOEING 727 727232 1384082 NM R1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 521DA 21472 R1 DOOR AFT FRAME IS CRACKED AT LWR STOP FITTING. REPAIRED PER M/M 52-12-000-8. 2 L 7 3 4F A3WE 2001062500053 20010625 00053 NM 2001 6 25 DL72S010881 1 20010530 A 7120 MOUNT BOEING 727 727225A 1384077 NM NR 1 ENGINE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8889Z 21858 INSPECTION OF THE FWD ENGINE MOUNT SUPPORT FITTING HOLES PER AD 97-05-08 REVEALED A CRACK IN THE BORE OF HOLES A & B. T HE HOLES WERE OVERSIZED TO REMOVE THE CRACK INDICATIONS AND AN INSURANCE CUT ADDED. LARGER DIAMETER BOLTS WERE THEN INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 380942-14AD AND FED EX S/B 2000-5410A01. 2 L 7 3 4F RT A3WE 2001062500054 20010625 00054 NM 2001 6 25 DL72S010892 1 20010531 A 3350 900835A BATTERY PACK BOEING 727 727225A 1384077 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8890Z 21859 DURING SVC CHECK FOUND LT AFT OVERWING EMERGENCY LIGHT OUT. RELAMPED, NO HELP. NO POWER AT SOCKETS. REPLACED BATTERY PACK, OPS CHECK GOOD. 2 L 7 3 4F RT A3WE 2001062500055 20010625 00055 NM 2001 6 25 DL72S010897 1 20010603 A 2130 39854021 VALVE BOEING 727 727232 1384082 NM RT PACK OVERHEATED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 529DA 21703 RT PACK OVERHEAT. CREW OBSERVED LIGHT HAZE IN CABIN. REPLACED RT PACK VALVE AND COALESCER BAGS. 2 L 7 3 4F A3WE 2001062500056 20010625 00056 NM 2001 6 25 2001F00022 1 20010602 A 2910 65C268091173 HYDRAULIC LINE BOEING 737 7373B7 1384580 NM HYD SYSTEM CHAFED A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 389US 23311 DCA - FLT 2299 - AFTER TAKEOFF FROM \, AS CREW RETRACTED THE LANDING GEAR, THEY RECEIVED A RED LIGHT FOR THE RT MLG. SH ORTLY AFTER, THEY RECEIVED A RED LIGHT FOR THE 'A' SYSTEM HYDRAULIC. CREW CONTINUED THEIR CLIMB TO FL190 AND THEN PERFO RMED PROCEDURES FOR 'A' SYSTEM HYDRAULIC FAILURE. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT DCA WHERE THE FLI GHT LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT WAS THEN TOWED TO GATE. MAINTENANCE FOUND THE RT MLG ACTUATOR PRESSURE L INE AND SPOILER 'B' SYSTEM RETURN LINE LEAKING AND CHAFING AGAINST ONE ANOTHER. REMOVED AND REPLACED BOTH HYDRAULIC LIN ES. ALSO, REMOVED AND REPLACED THE 'A' SYSTEM ELECTRIC HYDRAULIC PUMP (P/N MPEV3-056-9A) AND NR 1 ENGINE DRIVEN HYDRAUL 2 L 7 2 4F RT A16WE 2001062500057 20010625 00057 EU 2001 6 25 2001F00030 1 20010331 A 3350 V72914 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 236AE 340B236 PWM - FLT 4864 - SEVERAL EMERGENCY LIGHTS INOPERATIVE, FERRY TO ALB FOR REPAIRS. REMOVED AND REPLACED ALL POWER SUPPLIE S (20LN, S/N 19174, 21LN, S/N 18287, 22LN S/N 18991, 23LN S/N 18189, 24LN S/N 18315, IAW AMM. OPS CHECK GOOD. REF SIMA 20010901. (M) 2 L 7 2 4T RT A52EU 2001062500058 20010625 00058 EU 2001 6 25 2001F00032 1 20010331 A 3350 V72914 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 236AE 340B236 PWM - FLT 4864 - SEVERAL EMERGENCY LIGHTS INOPERATIVE, FERRY TO ALB FOR REPAIRS. REMOVED AND REPLACED ALL POWER SUPPLIE S (20LN S/N 19174, 21LN S/N 18287, 22LN S/N 18991, 23LN S/N 18189, 24LN S/N 18315) IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001062500059 20010625 00059 EU 2001 6 25 2001F00033 1 20010331 A 3350 V72914 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 236AE 340B236 PWM - FLT 4864 - FOUND SEVERAL EMERGENCY LIGHTS INOPERATIVE, FERRY TO ALB FOR REPAIRS. REMOVED AND REPLACED ALL POWER S UPPLIES (20LN S/N 19174, 21LN S/N 18287, 22LN S/N 18991, 23LN S/N 18189, 24LN S/N 18315) IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001062500060 20010625 00060 NM 2001 6 25 AALA20011032 1 20010517 A 2823 AV311 ACTUATOR BOEING 767 767323 1385205 NM FUEL SYSTEM DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 366AA 25193 DFW - FLT 911 - EN ROUTE LAX-MIA - THIRTY MINUTES INTO FLIGHT RIGHT FUEL TANK INDICATED 2000 LBS FUEL IMBALANCE. DETERM INED CROSSFEED VALVE PROBLEM AND DIVERTED TO DFW. LANDED WITHOUT INCIDENT. TROUBLESHOT SYSTEM AND REPLACED LEFT DEFUEL ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001062500061 20010625 00061 NM 2001 6 25 ASAA0110221 1 20010419 A 3350 88210044 BATTERY BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY TRACK LIGHTS AT ROWS 5, 8 AND 11 WERE INOPERATIVE. REMOVED AND REPLACED THREE REMOTE ASSEMBLY BATTERIES AT ROWS 5, 8 AND 11, THEN LIGHTS OPERATED NORMAL. (M) 2 L 7 2 4F RT A16WE 2001062500062 20010625 00062 NM 2001 6 25 ASAA0140048 1 20010409 A 3397 8100022608 WIRE BOEING 737 7374Q8 NM CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 NM 01 771AS 25104 SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING AT ROWS 16ABC TO 19ABC INOPERATIVE, WIRE BROKEN. REPAIRED BROKEN WIRE. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2001062500063 20010625 00063 NM 2001 6 25 ASAA0140049 1 20010409 A 3397 8100022608 WIRE BOEING 737 7374Q8 NM CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 NM 01 782AS 25113 SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING AT MID CABIN INOPERATIVE, WIRE BROKEN. REPAIRED BROKEN WI RE. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2001062500064 20010625 00064 NM 2001 6 25 ASAA0140054 1 20010410 A 3397 8100022608 WIRE BOEING 737 737490 1384715 NM CABIN DISCONNECTED A K NONE L NO TEST IN INSP/MAINT 1 NM 01 713AS 30161 ANC - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING AT ROW 14 INOPERATIVE, WIRE DISCONNECTED. RECONNECTED WIR E, OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2001062500065 20010625 00065 NM 2001 6 25 ASAA0140059 1 20010420 A 3350 8100022607 WIRE BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 773AS 25106 SEA - BEFORE FLIGHT, FOUND EMERGENCY TRACK LIGHTS AT ROW 17-19 INOPERATIVE, WIRE DISCONNECTED. RECONNECTED WIRES. OPS CHECKED NORMAL. (M) 2 L 7 2 4F RT A16WE 2001062500066 20010625 00066 WP 2001 6 25 ASAA0180112 1 20010321 A 5610 5613217520 GUIDE DOUG DC9 DC982 3022082 WP COCKPIT OUT OF POSITION A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 954AS 49387 PDX - DURING PREFLIGHT CHECK, FIRST OFFICERS SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. RESET WINDOW GUIDE PIN. WINDOW T HEN OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 2002010400132 20020104 00132 2002 1 4 ASAA0180118 4 20010329 A 2565 D29982107 HARNESS DOUG DC9 DC983 3022083 WP L1 DOOR FAILED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 33646 6334 53019 OAK - DURING C-CHECK, L1 DOOR EMERGENCY SLIDE HARNESS FAILED THE AMPERAGE CHECK. REMOVED AND REPLACED COMPLETE L1 SLIDE ASSEMBLY WITH SERVICEABLE ASSEMBLY. (M) 2 L 7 2 4F RT A6WE 2002010400133 20020104 00133 2002 1 4 ASAA0180119 4 20010407 A 2565 D29985107 HARNESS DOUG DC9 DC983 3022083 WP L2 DOOR FAILED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 38648 3715 53019 OAK - DURING C-CHECK, L-2 DOOR EMERGENCY SLIDE HARNESS FAILED THE AMPERAGE CHECK. REMOVED AND REPLACED L-2 DOOR SLIDE A SSEMBLY WITH SERVICEABLE ASSY. (M) 2 L 7 2 4F RT A6WE 2001062500067 20010625 00067 2001 6 25 ASAA0180121 4 20010329 A 2565 3961899501 LANYARD DOUG DC9 DC983 3022083 WP R1 DOOR DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 SEA - DURING PREFLIGHT CHECK, R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. RESECURED LANYARD. (M) 2 L 7 2 4F RT A6WE 2001062500068 20010625 00068 WP 2001 6 25 ASAA0180124 1 20010331 A 5350 2919845 WIRE ROPE DOUG DC9 DC983 3022083 WP TAILCONE OUT OF POSITION A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 PDX - DURING SERVICE CHECK, FOUND TAILCONE RELEASE CABLE OFF ONE OF THE CAMS. PROPERLY LOOPED RELEASE CABLE OVER CAM. (M) 2 L 7 2 4F RT A6WE 2001062500069 20010625 00069 WP 2001 6 25 ASAA0180126 1 20010403 A 5210 5910081167 DOOR DOUG DC9 DC983 3022083 WP L1 DOOR OUT OF RIG A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 33613 398 53075 SEA - DURING PREFLIGHT CHECK, L1 DOOR (FORWARD LEFT CREW/PAX DOOR) WAS FOUND TO BE DIFFICULT TO OPEN AND CLOSE. RIGGED L1 DOOR. DOOR THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001062500070 20010625 00070 2001 6 25 ASAA0180133 4 20010408 A 2565 3961899501 LANYARD DOUG DC9 DC983 3022083 WP R1 DOOR DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 RNO - DURING PREFLIGHT CHECK, R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. RESECURED LANYARD. (M) 2 L 7 2 4F RT A6WE 2001062500071 20010625 00071 WP 2001 6 25 ASAA0180136 1 20010412 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN 1ST CLASS CABIN. REMOVED AND REPLACED F LOOR TRACK LIGHT MODULES. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001062500072 20010625 00072 WP 2001 6 25 ASAA0180137 1 20010414 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 SEA - DURING LINE MAINTENANCE CHECK, OVERWING EMERGENCY EXIT LIGHTS WERE DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIA TED BATTERY PACK (POWER SUPPLY). LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001062500073 20010625 00073 WP 2001 6 25 ASAA0180138 1 20010415 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 973AS 53449 SEA - DURING LINE MAINTENANCE CHECK, AFT EXTERIOR EMERGENCY EXIT LIGHTS WERE DETERMINED TO BE INOPERATIVE. REPLACED ASS OCIATED BATTERY PACK (POWER SUPPLY). LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001062500074 20010625 00074 WP 2001 6 25 ASAA0180139 1 20010415 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 974AS 53450 ANC - DURING LINE MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 3. SECURED CONNECTION TO LIG HT ASSEMBLY. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001062500075 20010625 00075 WP 2001 6 25 ASAA0180142 1 20010413 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP CABIN MISSING A ASAA K NONE O OTHER CR CRUISE 1 NM 01 979AS 53471 LAX - DURING PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LAMP MODULES MISSING AT ROW 10. REPLACED MISSING LAMP MODULES . LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001062500076 20010625 00076 WP 2001 6 25 ASAA0180145 1 20010419 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 953AS 49386 PDX - DURING LINE CHECK, FORWARD CABIN PORTABLE EMERGENCY LIGHT WAS DETERMINED TO BE INOPERATIVE. REPLACED LIGHT ASSEMB LY. LIGHT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001062500077 20010625 00077 WP 2001 6 25 ASAA0180147 1 20010420 A 3350 0105606005 LIGHT DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 PDX - DURING LINE CHECK, EMERGENCY FLOOR TRACK LIGHTING AT ROWS 6 THROUGH 8 WERE DETERMINED TO BE INOPERATIVE. RECONNEC TED TRACK LIGHT ASSEMBLIES. TRACK LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001062500078 20010625 00078 WP 2001 6 25 ASAA0180148 1 20010421 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE AT ROW 6-7. REPLACED LAMP MODULE. LIGHTS THE N OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001062500079 20010625 00079 WP 2001 6 25 ASAA0180149 1 20010423 A 3350 0105606003 WIRE DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 PDX - DURING SERVICE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE AT ROW 6-7. RESECURED ELECTRICAL WIRING TO LAMP MODULE. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001062500080 20010625 00080 NE 2001 6 25 ASOA01040S 2 20010415 A 7200 MS945226 BOLT AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE RT ENGINE FRACTURED A ASOA A UNSCHED LANDING A B FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 11 535AS 464 124490 FLT 4137 - DURING FLIGHT FROM ATL-VPS, PASSENGER AND FLIGHT ATTENDANT REPORTED SPARKS AND FLAMES COMING FROM THE RIGHT E NGINE. AN EMERGENCY WAS DECLARED, BUT THE FIRE BOTTLE WAS NOT BLOWN. THE AIRCRAFT RETURNED TO ATL SAFELY. ENGINE WAS SHUT DOWN ON GROUND. ENGINE TEARDOWN REPORT, FROM STANDARD AERO, STATES THE PRIMARY FAILURE WAS CAUSED BY A FRACTURED N R 5 BEARING HOUSING BOLT. (M) 2 H 7 2 4T 4 T RT E20NE 2001062500081 20010625 00081 NE 2001 6 25 ASOA01050 2 20010507 A 7261 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF34* NE RT LACK OF LUBE A ASOA E A ENGINE SHUTDOWN UNSCHED LANDING J R WARNING INDICATION PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 11 836AS 7263 872334 FLT 4757 - EN ROUTE FROM ATL TO DSM, THERE WAS A LOSS OF OIL PRESSURE ON THE RIGHT ENGINE. THE ENGINE ROLLED BACK AND T HE PILOT SECURED IT. AIRCRAFT DIVERTED AND LANDED SAFELY IN EVV. ON GROUND, THE CREW REPORTED THE CHIP DETECTOR LIGHT ILLUMINATED. MAINTENANCE DETERMINED THE ENGINE HAD NO OIL AND THE CHIP DETECTOR WAS COVERED. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2001062500082 20010625 00082 SO 2001 6 25 ASOA01051 1 20010510 A 2910 12035694009 HYDRAULIC LINE EMB 120 EMB120RT SO HYD SYSTEM CHAFED A ASOA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 11 232AS 120036 FLT 4456 - INBOUND TO DFW FROM LBB, AIRCRAFT LOST GREEN SIDE HYDRAULICS AND HAD TO MANUALLY EXTEND THE GEAR. CREW DECLA RED AN EMERGENCY. AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REPLACED LEFT ENGINE HYDRAULIC PUMP, HYDRAULIC RESERVOIR FILTERS ON LEFT SIDE, AND ENGINE PRESSURE LINE AT LEFT NACELLE AFT FIRE WALL. OPERATIONAL AND LEAK CHECKS GOOD. NO CON TAMINATION WAS FOUND IN THE FILTERS. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001062500083 20010625 00083 EU 2001 6 25 ASOA01052 1 20010512 A 3350 1011191 LIGHT AEROSP ATR72 ATR72 EU AIR STAIR DOOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 643AS 413 ON GROUND INSPECTION, CAPTAIN REPORTED AIR STAIR DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACE BULB . OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT 2001062500084 20010625 00084 SO 2001 6 25 ASOA01053 1 20010513 A 3350 D36604001 BATTERY PACK EMB 120 EMB120 3260201 SO CABIN DISCHARGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 275AS 120234 DURING C-CHECK INSPECTION, MAINTENANCE DISCOVERED EMERGENCY EXIT TRACK LIGHTING DIM. MAINTENANCE REPLACED EMERGENCY LIG HT BATTERY PACK. SYSTEM OPS CHECKS GOOD. (M) 2 L 7 2 4T RT A31SO 2001062500085 20010625 00085 SO 2001 6 25 ASOA01054 1 20010513 A 2120 UNKNOWN EMB 120 EMB120 3260201 SO COCKPIT ODOR A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 280AS 120231 FLT 4327 - IN CRUISE FROM ATL TO EVV, CAPTAIN REPORTED SMELL OF BURNING MATCHES, TWICE AT 18,000 FT AND ONCE AFTER LEFT ENGINE WAS SECURED ON TAXI INTO EVV. EACH TIME THE SMELL LASTED BETWEEN 5-10 SECONDS AND LOCATION COULD NOT BE ISOLATED . MX PERFORMED VISUAL INSPECTION OF ENGINE, APU AREAS, AND BUS BARS ON F/O'S SIDE. NO DEFECTS WERE FOUND. MAINTENANCE THEN RAN APU FOR 30 MINUTES AND ENGINE FOR ONE HOUR AT VARIOUS POWER SETTINGS AND BLEED AIR SOURCES. NO ABNORMAL FUMES WERE NOTED AT THAT TIME. VISUAL INSPECTION AFTER RUNS WAS OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001062500086 20010625 00086 EA 2001 6 25 ASOA01057 1 20010521 A 3350 362624 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 820AS DURING GROUND INSPECTION AT XNA, CREW REPORTED EMERGENCY FLOOR TRACK LIGHTING AT ROW 5 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED ROWS 4 AND 5 EMERGENCY FLEX LIGHTING STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001062500087 20010625 00087 EU 2001 6 25 ASOA01059 1 20010522 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN MALFUNCTIONED A ASOA K NONE O OTHER TX TAXI/GRND HDL 1 SO 11 536AS 465 DURING TAXI IN ATL, THE TWO MINUTE EMERGENCY LIGHTS CAME ON FOR NO REASON AND WOULD NOT EXTINGUISH. MAINTENANCE COULD N OT DUPLICATE THE EVENT. TWO MINUTE EMERGENCY LIGHTS OPERATE NORMALLY. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT 2001062500088 20010625 00088 EA 2001 6 25 ASOA01060 1 20010524 A 4950 1098047 CONTROL VALVE CNDAIR CL600 CL6002B19 EA APU MALFUNCTIONED A ASOA O OTHER M J OVER TEMP WARNING INDICATION AP APPROACH 1 SO 11 862AS 7476 ON SHORT FINAL APPROACH FROM TLH TO ATL, CAPTAIN RECEIVED APU OVERHEAT MESSAGE. CAPTAIN BLEW THE FIRE BOTTLE AND DECLAR ED AN EMERGENCY. AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE FIRE BOTTLE, SQUIB AND APU LOAD C ONTROL VALVE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001062500089 20010625 00089 EA 2001 6 25 ASOA01061 1 20010527 A 4960 21188002 ECU CNDAIR CL600 CL6002B19 EA APU INOPERATIVE A ASOA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 11 854AS 4390 7382 AT LEVEL CRUISE FROM ATL TO VPS, FL240, THE APU MADE A LOUD POPPING NOISE. THE APU SHUTDOWN AND WOULD NOT RESTART. WHE N THE APU DID RESTART IT MADE THE SAME SOUND. THE IDG WAS DEFERRED SO CREW DECLARED AN EMERGENCY. AIRCRAFT DIVERTED AN D LANDED SAFELY IN CSG. MAINTENANCE REMOVED AND REPLACED THE APU ECU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO S ERVICE. (M) 2 L 7 2 4F RT A21EA 2001062500090 20010625 00090 EA 2001 6 25 ASOA01065 1 20010601 A 3234 7455021 CONTROL HANDLE CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 860AS 7433 FLT 4528 - AFTER DEPARTURE FROM ATL, WHEN GEAR WAS SELECTED UP, GEAR DID NOT COME UP, AND IT STAYED LOCKED THE ENTIRE FL IGHT. CAPTAIN ALSO RECEIVED A PARKING BRAKE SHUTOFF VALVE AND AN INBOARD ANTI-SKID CAUTION MESSAGE ON EICAS. CREW DECL ARED AN EMERGENCY. AFTER PUTTING THE GEAR HANDLE IN THE DOWN POSITION ALL EICAS CAUTION MESSAGES WENT OUT. AIRCRAFT RE TURNED AND LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED GEAR HANDLE ASSEMBLY. OPERATIONAL CHECK GOOD. NO OT HER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001062500091 20010625 00091 EA 2001 6 25 ASOA01066 1 20010602 A 3350 487191 CONNECTOR CNDAIR CL600 CL6002B19 EA CABIN CONTAMINATED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 853AS 7374 DURING GROUND INSPECTION IN ATL, CREW REPORTED RIGHT SIDE EMERGENCY STRIP LIGHTING INOPERATIVE. MAINTENANCE INSPECTED A ND CLEANED WATER FROM CONNECTION. OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001062500092 20010625 00092 NM 2001 6 25 BJNA010504 1 20010514 A 3350 900835A BATTERY BOEING 737 737282 13844AT NM CABIN DISCHARGED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 233TM 23043 ON WALK AROUND, FOUND OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY CARTRIDGE AND POWER UNIT IAW 33-53-00. (M) 2 L 7 2 4F RT A16WE 2001062500093 20010625 00093 NM 2001 6 25 BJNA010505 1 20010520 A 3350 LIGHT BOEING 737 737282 13844AT NM CABIN DISCONNECTED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 233TM 23043 FOUND FORWARD FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. SWAPPED BATTERY PACK WITH CENTER TRACK LIGHTING BATTERY FOUND SERVICEABLE, BUT TRACK NR 1 SECTION FOUND UNHOOKED FROM CIRCUIT. RECONNECTED LIGHTS, OPS CHECK GOOD IAW BMM 33-52 -11. (M) 2 L 7 2 4F RT A16WE 2001062500094 20010625 00094 NM 2001 6 25 BJNA010506 1 20010523 A 3350 362624 LIGHT BOEING 737 737282 13844AT NM CABIN DAMAGED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 233TM 23043 AFT CABIN EMERGENCY EXIT TRACK LIGHT DAMAGED BEYOND REPAIR. REMOVED AND REPLACED AFT CABIN EMERGENCY EXIT TRACK LIGHTIN G, OPS CHECK GOOD IAW 33-51-01. (M) 2 L 7 2 4F RT A16WE 2001062500095 20010625 00095 WP 2001 6 25 ABXA010353 1 20010608 A 5300 5910082 SKIN DOUG DC9 DC941 302207N WP FUSELAGE CHIPPED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 957AX 47759 FUSELAGE SKIN CRACKED OUT AT UPPER AFT CORNER OF MAIN ENTRY DOOR CUT-OUT. REPAIRED AREA IAW DC-9 REA D953-41305. 2 L 7 2 4F A6WE 2001062500096 20010625 00096 WP 2001 6 25 ABXA010354 1 20010612 A 5700 9919308 FITTING DOUG DC9 DC941 302207N WP LEFT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 957AX 47759 STRUCTURAL FITTING ON LEFT WING LEADING EDGE ON OUTBOARD SIDE OF #7 SLAT TRACK CRACKED BETWEEN TWO LOWER FASTENER HOLES. REPAIRED AREA IAW DC-9 REA D957-41317. 2 L 7 2 4F A6WE 2001062500097 20010625 00097 NM 2001 6 25 CIC2001F00000 1 20010513 A 2120 SMOKE DHAV DHC8 DHC8201 2809001 NM COCKPIT DETECTED A CICA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 07 993HA 456 A BRIEF OCCURRENCE OF SMOKE COMING FROM FIRST OFFICER LARGE GASPER. INSPECTED AIRCRAFT ACM FOR OIL CONTAMINATION AND AP U COMPARTMENT FOR ABNORMALITIES. NONE WERE NOTED, PERFORMED ENGINE RUN UP AND CYCLED BLEEDS NO DEFECT NOTED. REQUESTED AN ACCEPTANCE FLIGHT, ACCEPTANCE FLIGHT COMPLETED. NO DEFECTS WERE NOTED. PRECAUTIONARY REPLACED RECIRCULATION FAN P/ N 778728-6, S/N 860375. (M) 2 H 7 2 4T RT A13NM 2001062500098 20010625 00098 EU 2001 6 25 COEA0101740 1 20010501 A 3251 AC66150 MOTOR FOKKER F27 F27MK600 4990706 EU NLG STEERING LEAKING A COEA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 13 740FE 10329 ON DEPARTURE FROM GEG, NOSE GEAR IN TRANSIT LIGHT REMAINED ON AFTER GEAR SELECTED UP. MAINTENANCE REMOVED AND REPLACED LEAKING STEERING MOTOR TO CORRECT PROBLEM. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T A817 2001062500099 20010625 00099 WP 2001 6 25 DKAA01002 1 20010308 A 5753 5912992501 FLAP DOUG DC9 DC915F 3022037 WP RT WING DAMAGED A DKAA K NONE O OTHER IN INSP/MAINT 1 GL 23 916R 47010 RIGHT INBOARD FLAP NR 2 AFT PANEL DAMAGED AT XFS209.5. REPAIRED PER DER DRAWING NR 57-01010-3, DATED 01/16/2001. AIRCR AFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 2001062500100 20010625 00100 WP 2001 6 25 DKAA01003 1 20010308 A 5230 59101571 SKIN PANEL DOUG DC9 DC915F 3022037 WP CARGO DOOR CRACKED A DKAA K NONE O OTHER IN INSP/MAINT 1 GL 23 916R 47229 47010 AFT LOWER CARGO DOOR FORWARD OUTER PANEL CRACKED AT BEAM 1. REPAIRED PER DER DRAWING NR 52-01013-6, DATED 1/16/2001. A IRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 2001062500101 20010625 00101 WP 2001 6 25 DKAA01004 1 20010308 A 5230 59101411 SKIN PANEL DOUG DC9 DC915F 3022037 WP CARGO DOOR CRACKED A DKAA K NONE O OTHER IN INSP/MAINT 1 GL 23 916R 47229 47010 FORWARD LOWER CARGO DOOR UPPER FORWARD PANEL CRACKED AT BEAM 5. REPAIRED PER DER DRAWING NR 52-01013-6, DATED 1/16/2001 . AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 2001062500102 20010625 00102 WP 2001 6 25 DKAA01005 1 20010308 A 5522 5910412502 SKIN DOUG DC9 DC915F 3022037 WP ELEVATOR CORRODED A DKAA K NONE O OTHER IN INSP/MAINT 1 GL 23 916R 47010 FOUND CORROSION ON BOTTOM OF RIGHT ELEVATOR. REPAIRED PER DER DRAWING NR 55-01010-5, DATED 01/16/2001. AIRCRAFT RETURN ED TO SERVICE. (M) 2 L 7 2 4F A6WE 2001062500103 20010625 00103 WP 2001 6 25 DKAA01008 1 20010308 A 5321 FLOOR PANEL DOUG DC9 DC915F 3022037 WP COCKPIT CORRODED A DKAA K NONE O OTHER IN INSP/MAINT 1 GL 23 916R 47010 FOUND COCKPIT FLOOR CORRODED, RIGHT SIDE FS 148-218. REPAIRED PER DER DRAWING NR 53-01010-1, DATED 01/16/2001. AIRCRAF T RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 2001062500104 20010625 00104 WP 2001 6 25 DKAA01009 1 20010308 A 5700 STRUCTURE DOUG DC9 DC915F 3022037 WP WING DAMAGED A DKAA K NONE O OTHER IN INSP/MAINT 1 GL 23 916R 47229 47010 FOUND THREE ELONGATED HOLES AT LEFT XFS206, RIGHT XFS184, XFS184. REPAIRED PER DER DRAWING NR 57-01590-1, DATED 02/07/2 001. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 2001062500105 20010625 00105 NE 2001 6 25 DKAA01012B 2 20010601 A 7230 489674E BEARING DOUG DC9 DC915F 3022037 WP PWA JT8 JT8D7B 52053 NE ENGINE FAILED A DKAA K NONE O OTHER IN INSP/MAINT 1 GL 23 916R 47010 656878 ENGINE WAS INDUCTED FOR MAINTENANCE MAY, 2001 FOR VIBRATION AND METAL CONTAMINATION OF THE OIL SYSTEM. TEARDOWN AND INS PECTION REVEALED A NR 6 BEARING FAILURE. A MORE DETAILED PIECE PART INSPECTION SHOWED NO OTHER DAMAGE ASSOCIATED WITH T HIS DEFECT OF WHICH COULD HAVE CONTRIBUTED TO THE FAILURE THE ENGINE WAS DISASSEMBLED, CLEANED, REPAIRED FLUSHED AND RE ASSEMBLED IAW JT8 ENGINE MANUAL. THE ROOT CAUSE FOR THE NR 6 BEARING FAILURE IS UNDETERMINED. ENGINE RETURNED TO SERVI CE. (M) 2 L 7 2 4F 4 F A6WE E2EA 2001062500106 20010625 00106 EU 2001 6 25 QXEA0100712 1 20010422 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC-CREASE IN FUSELAGE SKIN AT LAP JOINT AND SKIN BELOW LAP JOINT STATION 6805 - 7305 STRINGER 17. REPAIRED IAW FOKKER SRM 53-02-07, SRM 51-31-01, AND SRM 53-01-01. 2 L 7 2 4F RT A20EU 2001062500107 20010625 00107 EU 2001 6 25 QXEA0100713 1 20010424 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC-CREASE IN FUSELAGE SKIN FORWARD OF MID CARGO DOOR STATION 7805 STRINGER 61. REPAIRED IAW FOKKER SRM 53-01-01, SRM 5 3-02-07, PAGE 2, SRM 53-15-01, PAGE 3 AND 5, AND SRM 51-31-01, PAGE 13. 2 L 7 2 4F RT A20EU 2001062500108 20010625 00108 EU 2001 6 25 QXEA0100714 1 20010422 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC-FORWARD CARGO DOOR OUTER SKIN DENTED UPPER FORWARD CORNER. REPAIRED IAW FOKKER SRM 52-01-01, AND SRM 52-02-04, PAGE 2, 3. 2 L 7 2 4F RT A20EU 2001062500109 20010625 00109 EU 2001 6 25 QXEA0100715 1 20010423 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC-FORWARD CARGO DOOR OUTER SKIN IS DENTED BETWEEN HOOK LATCH WINDOWS. REPAIRED IAW FOKKER SRM 52-01-01, AND SRM 52-02 -04, PAGE 2, 3. 2 L 7 2 4F RT A20EU 2001062500110 20010625 00110 EU 2001 6 25 QXEA0100716 1 20010428 A 5310 DOOR FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC-CRACKS UNDER DOOR SUPPORT ROD BRACKET ON AFT CARGO DOOR APERTURE. REPAIRED IAW FOKKER SRM 53-02-16, PAGE 4. 2 L 7 2 4F RT A20EU 2001062500111 20010625 00111 EU 2001 6 25 QXEA0100736 1 20010503 A 5313 LONGERON FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - CRACKED LONGERON IN FORWARD LOWER FRONT FUSELAGE JUST AHEAD OF FRAME 3450, RIGHT-HAND SIDE, THIRD LONGERON INBOARD . REPAIRED IAW FOKKER SRM 53-11-05, PAGE 10M ITEM 340 AND SRM 53-32-01, PAGE 15, PARAGRAPH 5. 2 L 7 2 4F RT A20EU 2001062500112 20010625 00112 EU 2001 6 25 QXEA0100741 1 20010427 A 5320 MOUNT FOKKER F28 F28MK4000 4990810 EU AC BAY CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - LEFT-HAND ACM BAY HAS CRACKED MOUNTING BOX FOR MIXING DUCT ELBOW ATTACH. REPAIRED IAW FOKKER SRM 53-11-05, PAGE 2 , FIGURE 01, ITEM 730. 2 L 7 2 4F RT A20EU 2001062500113 20010625 00113 EU 2001 6 25 QXEA0100744 1 20010420 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - SHARP DENT IN FUSELAGE SKIN AT STATION 7805, STRINGER 17A. REPAIRED IAW FOKKER SRM 53-02-02, FIGURE 1. 2 L 7 2 4F RT A20EU 2001062500114 20010625 00114 EU 2001 6 25 QXEA0100745 1 20010425 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - CRACKED CABIN CLIP AT FRAME 16660 AND STRINGER 59. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 14. 2 L 7 2 4F RT A20EU 2001062500115 20010625 00115 EU 2001 6 25 QXEA0100746 1 20010425 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - CRACKED CABIN CLIP AT FRAME 16660 AND STRINGER 58. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 14. 2 L 7 2 4F RT A20EU 2001062500116 20010625 00116 EU 2001 6 25 QXEA0100747 1 20010425 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - CRACKED CABIN CLIP AT FRAME 16060 AND STRINGER 58. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 2001062500117 20010625 00117 EU 2001 6 25 QXEA0100749 1 20010504 A 5210 DOOR FRAME FOKKER F28 F28MK4000 4990810 EU PAX DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - MAIN CABIN DOOR AFT LOWER CORNER, BENEATH SEAL AND RETAINER CORRODED. FOUND TO WITHIN LIMITS AS PER FOKKER FAX TS 01-54526 AND HORIZON AIR EA 4-52-453. 2 L 7 2 4F RT A20EU 2001062500118 20010625 00118 EU 2001 6 25 QXEA0100751 1 20010430 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - FRAME 18575, STRINGER 57, CASTELLATION CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 3 AND SRM 53-30-02, PAGE S 9 AND 10. 2 L 7 2 4F RT A20EU 2001062500119 20010625 00119 EU 2001 6 25 QXEA0100752 1 20010427 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - FRAME 32-2, STRINGER 50, CASTELLATION CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3. 2 L 7 2 4F RT A20EU 2001062500120 20010625 00120 EU 2001 6 25 QXEA0100753 1 20010429 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - FRAME 50-2, STRINGER 4B, CASTELLATION CRACKED. REPAIRED IAW FOKKER FAX TS97.59355 AND HORIZON AIR EA 4-53-1484. 2 L 7 2 4F RT A20EU 2001062500121 20010625 00121 EU 2001 6 25 QXEA0100754 1 20010429 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - FRAME 50-2, STRINGER 48, CASTELLATION CRACKED. REPAIRED IAW FOKKER FAX TS97.59355 AND HORIZON AIR EA 4-53-1484. 2 L 7 2 4F RT A20EU 2001062500122 20010625 00122 EU 2001 6 25 QXEA0100755 1 20010429 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - RIGHT-HAND SIDE FRAME 50-2, STRINGER 50, CASTELLATION CRACKED. REPAIRED IAW FOKKER FAX TS97.59355 AND HORIZON AIR EA 4-53-1484. 2 L 7 2 4F RT A20EU 2001062500123 20010625 00123 EU 2001 6 25 QXEA0100756 1 20010429 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - LEFT-HAND SIDE FRAME 50-2, STRINGER 27, CASTELLATION CRACKED. REPAIRED IAW FOKKER FAX TS97.59355 AND HORIZON AIR EA 4-53-1484. 2 L 7 2 4F RT A20EU 2001062500124 20010625 00124 EU 2001 6 25 QXEA0100757 1 20010427 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - LEFT-HAND SIDE FRAME 32-2, STRINGER 21A, CASTELLATION CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3 . 2 L 7 2 4F RT A20EU 2001062500125 20010625 00125 EU 2001 6 25 QXEA0100758 1 20010427 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - LEFT-HAND SIDE FRAME 32-2, STRINGER 28, CASTELLATION CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3. 2 L 7 2 4F RT A20EU 2001062500126 20010625 00126 EU 2001 6 25 QXEA0100759 1 20010426 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CANNING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - REAR PRESSURE BULKHEAD AT FRAME 17065 SKIN IS OIL CANNING BETWEEN HORIZONTAL BEAMS 4 AND 5 AND BL1050L AND 4256. REPAIRED IAW HORIZON AIR EA 4-53-1483. 2 L 7 2 4F RT A20EU 2001062500127 20010625 00127 EU 2001 6 25 QXEA0100760 1 20010426 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - TAIL SECTION HAS DENTS LEFT-HAND FUSELAGE, STATION 23003, STRINGER 19. REPAIRED IAW HORIZON AIR EA 4-53-1485 AND FOKKER FAX TS01-54512. 2 L 7 2 4F RT A20EU 2001062500128 20010625 00128 EU 2001 6 25 QXEA0100761 1 20010427 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - FRAME 32-2, STRINGER 22, CASTELLATION FOUND TO BE CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3. 2 L 7 2 4F RT A20EU 2001062500129 20010625 00129 EU 2001 6 25 QXEA0100762 1 20010427 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - FRAME 32-2 AND STRINGER 44, CASTELLATION FOUND TO BE CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3. 2 L 7 2 4F RT A20EU 2001062500130 20010625 00130 EU 2001 6 25 QXEA0100763 1 20010427 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - FRAME 32-2 AND STRINGER 30, CASTELLATION FOUND TO BE CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3. 2 L 7 2 4F RT A20EU 2001062500131 20010625 00131 EU 2001 6 25 QXEA0100764 1 20010427 A 2742 FITTING FOKKER F28 F28MK4000 4990810 EU HORIZ STAB CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - HORIZONTAL STAB DRIVE FITTING HAS SOME FRETTING OF THE RIGHT-HAND AFT LUGS, INBOARD SIDE. REPAIRED IAW HORIZON AI R EA 4-55-290 AND FOKKER FAX TS06.54293. 2 L 7 2 4F RT A20EU 2001062500132 20010625 00132 EU 2001 6 25 QXEA0100765 1 20010503 A 5755 BUSHING FOKKER F28 F28MK4000 4990810 EU RT SPOILER WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - RIGHT-HAND NR 3 LIFT DUMPER SPIGOT BUSHINGS WORN. RIGHT-HAND LIFT DUMPER BELLCRANK REMOVED, INTERNAL BUSHINGS AND SPIGOT MEASURED AS PER FOKKER FAX AND HORIZON AIR EA 4-57-555, ALL WITHIN LIMITS. 2 L 7 2 4F RT A20EU 2001062500133 20010625 00133 EU 2001 6 25 QXEA0100766 1 20010503 A 5755 BUSHING FOKKER F28 F28MK4000 4990810 EU RT SPOILER WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - RIGHT-HAND NR 2 LIFT DUMPER SPIGOT BUSHINGS WORN. RIGHT-HAND NR 2 LIFT DUMPER BELLCRANK REMOVED, INTERNAL BUSHING S AND SPIGOT MEASURED AS PER FOKKER FAX AND HORIZON AIR EA 8-57-555, ALL WITHIN LIMITS. 2 L 7 2 4F RT A20EU 2001062500134 20010625 00134 EU 2001 6 25 QXEA0100768 1 20010506 A 5530 RIVET FOKKER F28 F28MK4000 4990810 EU VERTICAL STAB LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - VERTICAL STABILIZER LEFT-HAND SIDE ABOVE TAIL CONE HAS LOOSE RIVETS. INSTALLED FASTENERS IAW FOKKER SRM 51-32-04 AND HORIZON AIR EA 4-55-289. 2 L 7 2 4F RT A20EU 2001062500135 20010625 00135 EU 2001 6 25 QXEA0100769 1 20010504 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU RT WING DELAMINATED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - RIGHT-HAND OUTBOARD WING TRAILING EDGE TAP TEST CARRIED OUT. THREE MINOR DELAMS INNER MOST INBOARD END ON TOP SKI N. REPAIRED IAW FOKKER SRM 51-70-00, PAGE 10B, FIGURE 6B AND PAGE 12. 2 L 7 2 4F RT A20EU 2001062500136 20010625 00136 EU 2001 6 25 QXEA0100770 1 20010509 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU RT WING DELAMINATED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - RIGHT-HAND OUTBOARD WING TRAILING EDGE TAP TEST CARRIED OUT. MULTIPLE DELAMS OUT MOST OUTBOARD END ON TOP SKIN. REPAIRED IAW HORIZON AIR EA 4-57-557. 2 L 7 2 4F RT A20EU 2001062500137 20010625 00137 EU 2001 6 25 QXEA0100771 1 20010509 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU RT WING DELAMINATED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - RIGHT-HAND OUTBOARD WING TRAILING EDGE TAP TEST CARRIED OUT. REPAIRED IAW HORIZON AIR EA 4-57-557. 2 L 7 2 4F RT A20EU 2001062500138 20010625 00138 EU 2001 6 25 QXEA0100772 1 20010504 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU LT WING DELAMINATED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - LEFT-HAND INBOARD WING TRAILING EDGE TAP TEST CARRIED OUT. REPAIRED IAW HORIZON AIR EA 4-57-536. 2 L 7 2 4F RT A20EU 2001062500139 20010625 00139 EU 2001 6 25 QXEA0100780 1 20010504 A 5210 SKIN FOKKER F28 F28MK4000 4990810 EU PAX DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - MAIN CABIN DOOR OUTER SKIN BY GRIP HANDLE SHARP DENT AND CREASE MEASURED AND BEYOND LIMITS. REPAIRED IAW HORIZON AIR EA 4-52-449. 2 L 7 2 4F RT A20EU 2001062500140 20010625 00140 EU 2001 6 25 QXEA0100781 1 20010427 A 5755 BUSHING FOKKER F28 F28MK4000 4990810 EU LT SPOILER WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - LEFT-HAND LIFT DUMPER SPIGOT BUSHINGS WORN. LEFT-HAND NR 2 LIFT DUMPER BELLCRANK REMOVED SPIGOT AND BELLCRANK BUS HING MEASURED AS PER HORIZON AIR EA 4-57-554, FOUND WITHIN LIMITS. 2 L 7 2 4F RT A20EU 2001062500141 20010625 00141 EU 2001 6 25 QXEA0100782 1 20010427 A 5755 BUSHING FOKKER F28 F28MK4000 4990810 EU SPOILER WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - LEFT-HAND NR 1 LIFT DUMPER SPIGOT BUSHINGS WORN. LEFT-HAND NR 1 LIFT DUMPER BELLCRANK REMOVED, SPIGOT AND BELLCRA NK BUSHING MEASURED AS PER HORIZON AIR EA 4-57-554. FOUND TO BE WITHIN LIMITS. 2 L 7 2 4F RT A20EU 2001062500142 20010625 00142 EU 2001 6 25 QXEA0100794 1 20010527 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US 11161 PDX - LIGHT BULB FOUND BURNT OUT ON NR 3 EXIT SIGN. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001062500143 20010625 00143 NM 2001 6 25 QXEA0100795 1 20010529 A 5210 STOP DHAV DHC8 DHC8202 2809007 NM PAX DOOR LACK OF LUBE A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 826PH 526 SEA - CREW REPORTED MAIN CABIN DOOR HARD TO OPERATE. CLEANED AND LUBED DOOR STOPS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001062500144 20010625 00144 NM 2001 6 25 QXEA0100796 1 20010512 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT-HAND INBOARD SEAT TRACK HAS A NICK IN SIDE WHERE IT MOUNTS TO AFT MAIN FRAME STATION 424, OUTBOARD SIDE OF T RACK. REPAIRED IAW DHC-8 SRM 51-20-16, 51-20-36 AND 51-20-11, PAGE 11, FIGURE 6. 2 H 7 2 4T RT A13NM 2001062500145 20010625 00145 NM 2001 6 25 QXEA0100797 1 20010511 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - CORROSION ON STATION 202 FRAME CASTELLATION AND KEEL BEAM AT STRINGER 315. REPAIRED IAW PSM1-GEN-5, CHAPTER 4, PA GES 4-16, STEP 8 AND DHC-8 SRM 51-20-16, PAGE 2, STEP 4. 2 H 7 2 4T RT A13NM 2001062500146 20010625 00146 NM 2001 6 25 QXEA0100802 1 20010510 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT OUTBOARD SEAT TRACK HAS CORROSION ON INBOARD AND OUTBOARD TOP AND INSIDE CENTER OF FORWARD SIX INCHES OF TRA CK FROM STATION 262-268. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001062500147 20010625 00147 NM 2001 6 25 QXEA0100803 1 20010510 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT OUTBOARD SEAT TRACK HAS CORROSION ON OUTBOARD TOP FROM STATION 270 TO 274. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001062500148 20010625 00148 NM 2001 6 25 QXEA0100804 1 20010510 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT OUTBOARD SEAT TRACK HAS CORROSION ON INSIDE OF TRACK ON INSIDE EDGE AT STATION 291. REPAIRED IAW RD 8-53-13 42. 2 H 7 2 4T RT A13NM 2001062500149 20010625 00149 NM 2001 6 25 QXEA0100805 1 20010510 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT OUTBOARD SEAT TRACK HAS CORROSION ON BOTH SIDES OF INSIDE AND ON INBOARD TOP OF TRACK AT STATION 310. REPAI RED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001062500150 20010625 00150 NM 2001 6 25 QXEA0100806 1 20010510 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT OUTBOARD SEAT TRACK HAS CORROSION ON INSIDE CENTER AT STATION 390. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001062500151 20010625 00151 NM 2001 6 25 QXEA0100807 1 20010510 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT OUTBOARD SEAT TRACK HAS CORROSION ON INSIDE CENTER AND TOP INBOARD ALSO GOUGED APPROXIMATELY .005 INCH AT TO P OUTBOARD AT STATION 421 TO 423. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001062500152 20010625 00152 NM 2001 6 25 QXEA0100808 1 20010510 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT OUTBOARD SEAT TRACK IS CORRODED AT INSIDE AND TOP INBOARD AND OUTBOARD AT STATION 436 TO 439. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001062500153 20010625 00153 NM 2001 6 25 QXEA0100809 1 20010510 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT OUTBOARD SEAT TRACK IS GOUGED APPROXIMATELY .005 AT TOP INBOARD AND OUTBOARD AT STATION 454. REPAIRED IAW R D 8-53-1342. 2 H 7 2 4T RT A13NM 2001062500154 20010625 00154 NM 2001 6 25 QXEA0100810 1 20010510 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT OUTBOARD SEAT TRACK CORRODED INSIDE CENTER AND UNDER INSIDE TOP AT STATION 467-471. REPAIRED IAW RD 8-53-13 42. 2 H 7 2 4T RT A13NM 2001062500155 20010625 00155 NM 2001 6 25 QXEA0100811 1 20010510 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT OUTBOARD SEAT TRACK CORRODED ON INBOARD TOP AT STATION 470. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001062500156 20010625 00156 NM 2001 6 25 QXEA0100812 1 20010510 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT OUTBOARD SEAT TRACK CORRODED ON TOP INBOARD AND OUTBOARD AT STATION 485 TO 487. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001062500157 20010625 00157 NM 2001 6 25 QXEA0100813 1 20010510 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT OUTBOARD SEAT TRACK CORRODED IN INSIDE CENTER AT STATION 516 TO 517. REPAIRED IAW RD 8-53-3644. 2 H 7 2 4T RT A13NM 2001062500158 20010625 00158 NM 2001 6 25 QXEA0100814 1 20010510 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT OUTBOARD SEAT TRACK CORRODED AT INSIDE CENTER AT STATION 538. REPAIRED IAW RD 8-53-3644. 2 H 7 2 4T RT A13NM 2001062500159 20010625 00159 NM 2001 6 25 QXEA0100815 1 20010510 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - LEFT OUTBOARD SEAT TRACK GOUGED .003 INCH ON INBOARD RAIL AT STATION 270. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001062500160 20010625 00160 NM 2001 6 25 QXEA0100816 1 20010510 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - LEFT OUTBOARD SEAT TRACK CORRODED ON INBOARD SIDE OF CHANNEL AT STATION 298-312. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001062500161 20010625 00161 NM 2001 6 25 QXEA0100817 1 20010510 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - LEFT OUTBOARD SEAT TRACK CORRODED ON OUTBOARD RAIL IN LUG AREA AT STATION 363. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001062500162 20010625 00162 NM 2001 6 25 QXEA0100818 1 20010510 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - LEFT OUTBOARD SEAT TRACK CORRODED ON INBOARD SIDE OF CHANNEL UNDER LUGS AT STATION 375. REPAIRED IAW RD 8-53-1342 . 2 H 7 2 4T RT A13NM 2001062500163 20010625 00163 NM 2001 6 25 QXEA0100819 1 20010510 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - LEFT OUTBOARD SEAT TRACK CORRODED IN CHANNEL AT STATION 395-395. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001062500164 20010625 00164 NM 2001 6 25 QXEA0100820 1 20010510 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - LEFT OUTBOARD SEAT TRACK CORRODED ON INBOARD SIDE OF CHANNEL AT STATION 436. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001062500165 20010625 00165 EU 2001 6 25 QXEA0100899 1 20010529 A 4920 38075412 APU FOKKER F28 F28MK4000 4990810 EU APU BAY MALFUNCTIONED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 487US 1643 1020 11238 PDX - AFTER ENGINE SHUTDOWN AT GATE, AIRCRAFT BEGAN SHAKING, AND APU ENGINE PARAMETERS BEGAN CLIMBING. CABIN FILLED WIT H SMOKE. SHUT DOWN APU MANUALLY. REMOVED AND REPLACED APU. COMPLIED WITH BLEED AIR DUCTING BLOW OUT. OPERATIONAL CHE CKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001062500166 20010625 00166 NM 2001 6 25 AWXA0001890 1 20010625 A 5312 65375903 WEB BOEING 737 7373G7 1384595 NM CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 D: Crack in BS 178 center web WL 188 RBL .6C: Removed and replaced BS 178 center web IAW AWA ER # 03-5311-01167-DD2 2 L 7 2 4F RT A16WE 2001062500169 20010625 00169 NM 2001 6 25 20010604CW007 1 20010510 A 2932 V25W712025505 SEAL ISRAEL 1125 1125 NM HYD PRESS SWTCH DETERIORATED A O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NE 02 75GZ 075 THIRTY (30) MINUTES AFTER TAKEOFF, WARNING LIGHT ILLUMINATED, INDICATING A LOW LEVEL OF HYDRAULIC FLUID IN THE TANK; OI L PRESSURE READING FELL TO 0. THE EDP PUMPS (RIGHT AND LEFT) WARNING LIGHTS FOR LOW OIL PRESSURE ILLUMINATED AFTER LAN DING (AC PERFORMED EMERGENCY LANDING) DEFECT WAS DUE TO PRESSURE SWITCH SEAL DETERIORATION. 2 L 7 2 4F RT A16NM 2001062500170 20010625 00170 EU 2001 6 25 20010604CW008 1 20010509 A 3243 LA5714004005 VALVE ISRAEL GALAXY GALAXY 4500307 EU BRAKE SYS LEAKING A VO2R K NONE O OTHER NR NOT REPORTED 1 GL 19 622SV 24 24 015 ORIGINAL INSTALLATION POWER BRAKE VALVE WAS FOUND TO BE LEAKING INTERNALLY CAUSING SKYDROL FLUID TO BE SPILLED ON THE PR ESSURE SIDE OF THE FORWARD PRESSURE BULKHEAD. 2 L 7 2 4F RT A53NM 2001062500171 20010625 00171 EU 2001 6 25 20010604CW009 1 20010509 A 2721 D25W582050005 ACTUATOR ISRAEL GALAXY GALAXY 4500307 EU RUDDER TRIM MALFUNCTIONED D UO2R K NONE F FLT CONT AFFECTED CR CRUISE 1 GL 19 414KD 30 30 022 ORIGINAL EQUIPMENT RUDDER TRIM ACTUATOR FROZE UP AT ALTITUDE. WHEN DESCENDING TO WARMER AIR, THE ACTUATOR STARTED WORKI NG BUT NOT ALLOWING FOR FULL RUDDER TRIM TRAVEL. ACTUATOR WAS REPLACED WITH SERVICEABLE ACTUATOR. 2 L 7 2 4F RT A53NM 2001062500173 20010625 00173 GL 2001 6 25 20010604CW013 2 20010520 A 7321 320580 BEARING BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL FUEL CONTROL FAILED A O OTHER O OTHER CR CRUISE 1 GL 19 6BU 1329 4034 CAE270422 AIRCRAFT IN CRUISE FLIGHT. PILOT NOTICED THAT THE MAIN ROTOR NR 2 STARTED TO OVER SPEED. PILOT LANDED AIRCRAFT SAFELY UNDER ITS OWN POWER. AFTER INVESTIGATION CAUSE, IT WAS FOUND THAT THE ENGINE FUEL CONTROL SHAFT BEARING HAD FAILED CAUS ING FUEL CONTROL TO GO ERRATIC. 1 G 7 1 3U 3 U H2SW E4CE 2001062500175 20010625 00175 WP 2001 6 25 ZW0A0104003 1 20010622 A 3350 58222 BATTERY PACK DOUG DC9 DC982 3022082 WP ROW 18 A ZW0A K NONE O OTHER CR CRUISE 1 CE 13 904TW 49156 THE EGRESS LIGHTS FROM ROW 15 THRU THE AFT CABIN ILLUMINATED WITH THE SWITCH ARMED. REPLACED THE BATTERY PACK. CHECK-C 5-18-01 MCI. --CLOSED--- 2 L 7 2 4F A6WE 2001062500177 20010625 00177 NE 2001 6 25 ARWA0010406 2 20010426 A 7530 BLEED VALVE DOUG DC8 DC863 302198A WP PWA JT3D JT3D7 52039 NE A ARWA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 19 345JW 46042 671393 Log Page 54673. Discrepancy: Take Off roll was aborted at 65 Knots due to compressor stall on #3 engine. Corrective Acti on: Performed test of compressor bleed valve IAW MM 75-30-3 found normal. Checked on engine run up IAW MM 71-00 found no rmal operation no compressor stall noted. 2 L 7 4 4F 4 F 4A25 1E8 2001062500178 20010625 00178 WP 2001 6 25 CALA0100582 1 20010623 A 3222 STRUT DOUG DC9 DC981 3022081 WP NOSE GEAR DEFLATED A CALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 09 37882 48027 THE NOSE GEAR UNSAFE LIGHT ILLUMINATED WHILE ENROUTE TO EWR. THE CREW FOLLOWED QRH PROCEDURES. WHEN THE GEAR WAS LOWERED ALL THREE GEAR INDICATED DOWN AND LOCKED. QRH PROCEDURES WERE CONTINUED AND WHEN CREW ATTEMPTED TO RAISE GEAR THE HANDL E WOULD NOT COME UP. THE GEAR WAS LEFT DOWN AND THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR STRUT BOTTOMED OUT. THE NOSE GEAR STRUT WAS FULLY SERVICED IAW MM 32-21-02. THE NOSE GEAR WAS SWUNG SEVERAL TIMES W ITH OPERATION AND INDICATIONS CHECKING NORMAL. 2 L 7 2 4F A6WE 2001062500179 20010625 00179 WP 2001 6 25 CALA0100583 1 20010622 A 5330 SKIN DOUG DC9 DC982 3022082 WP FS 474 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND L/H FUSELAGE EXTERNAL SKIN DENTED AT FS 474 JUST ABOVE LONGERON 21L. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 3B. 2 L 7 2 4F A6WE 2001062500180 20010625 00180 WP 2001 6 25 CALA0100584 1 20010622 A 5320 FITTING DOUG DC9 DC982 3022082 WP FS 160 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND CABIN FRAME TO WEB FITTING CORRODED AT FS 160, RBL 56. THE FRAME FITTING WAS REMOVED AND REPLACED IAW S RM 51-30-01, 51-30-05, AND 51-10-4. 2 L 7 2 4F A6WE 2001062500181 20010625 00181 WP 2001 6 25 CALA0100585 1 20010622 A 5730 SKIN DOUG DC9 DC982 3022082 WP R/H WING I/B DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND R/H WING SKIN I/B LOWER SURFACE NICKED AND DENTED. NEW SKIN WAS FABRICATED AND INSTALLED IAW SRM 51-60- 4 AND 51-30-2. 2 L 7 2 4F A6WE 2001062500182 20010625 00182 WP 2001 6 25 CALA0100586 1 20010623 A 5320 CHANNEL DOUG DC9 DC982 3022082 WP AFT ENTRY DR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND AFT ENTRY DOOR SEAL AREA AFT HAT CHANNEL FOR THRESHOLD CORRODED. THE HAT CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-30-2 AND 51-10-4. 2 L 7 2 4F A6WE 2001062500183 20010625 00183 WP 2001 6 25 CALA0100587 1 20010623 A 5320 ANGLE DOUG DC9 DC982 3022082 WP AFT ENTRY DR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND AFT ENTRY DOOR Z-ANGLE COMMON TO CUSP MEMBRANE CORRODED AT FS 1136-1174, LBL 48.5. THE Z-ANGLE WAS REMO VED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2 AND 51-10-4. 2 L 7 2 4F A6WE 2001062500184 20010625 00184 WP 2001 6 25 CALA0100588 1 20010623 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FS 1140 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND L/H MAIN CABIN T-ANGLE CORRODED AT FS 1140. THE T-ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW S RM 51-10-3, 51-10-4, 51-10-5, AND 51-30-2. 2 L 7 2 4F A6WE 2001062500185 20010625 00185 WP 2001 6 25 CALA0100589 1 20010623 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FS 1097-1215 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND SEAT TRACK CORRODED AT FS 1097-1215, LBL 45. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED I AW SRM 51-30-2, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 2001062500186 20010625 00186 NM 2001 6 25 CALA0100590 1 20010623 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM STA 328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14358 23943 INSPECTION FOUND FLOORBEAM CORRODED AT STA 328, LBL 49. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 2001062500187 20010625 00187 WP 2001 6 25 CALA0100593 1 20010624 A 5340 FITTING DOUG DC9 DC982 3022082 WP FS 1136 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND ATTACH FITTING(FORWARD OF L-2 DOOR) CORRODED AT FS 1136, LBL 56. THE FITTING WAS REMOVED AND A NEW FITT ING WAS INSTALLED IAW SRM 51-30-1, 51-30-4, AND 51-10-3. 2 L 7 2 4F A6WE 2001062500188 20010625 00188 WP 2001 6 25 CALA0100595 1 20010624 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FS 1070-1203 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND MAIN CABIN SEAT TRACK CORRODED AT FS 1070-1203, LBL 25. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-05, FIGURE 4, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 2001062500189 20010625 00189 WP 2001 6 25 CALA0100596 1 20010624 A 5330 SKIN DOUG DC9 DC982 3022082 WP FS 370 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND R/H EXTERNAL FUSELAGE SKIN DENTED AT FS 370 JUST BELOW LONGERON 20R. THE DENTED AREA WAS COLD WORKED AN D A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38. 2 L 7 2 4F A6WE 2001062500190 20010625 00190 WP 2001 6 25 CALA0100597 1 20010624 A 5330 SKIN DOUG DC9 DC982 3022082 WP FS 541 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND R/H FUSELAGE EXTERNAL SKIN DENTED AT FS 541 BETWEEN LONGERONS 20R AND 21R. A REPAIR DOUBLER WAS INSTALL ED IAW SRM 53-04, FIGURE 38. 2 L 7 2 4F A6WE 2001062500191 20010625 00191 NM 2001 6 25 QXEA0101060 1 20010620 A 3350 GRIMES DHAV DHC8 DHC8202 2809007 NM A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PSC - UPON INSPECTION, FOUND THE FLOOR PATH LIGHTING STRIPS IN NEED OF REPAIR. REMOVED AND REPLACED #1 AND #2 FORWARD FL OOR PATH LIGHTING STRIPS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001062500192 20010625 00192 EU 2001 6 25 RAIA00106015 1 20010623 A 7700 331EDP12 DISPLAY JETAIR JETSTM JETSTM4101 1500501 EU INST PANEL FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 556HK 9603 41073 5387-BWI- CREW REPORTS RIGHT RPM GAUGE IS INOPERATIVE, BOTH ANALOG AND DIGITAL. MAINTENANCE INSPECTED AND REPLACED THE E NGINE DISPLAY PANEL. 2 L 7 2 4T RT A41NM 2001072700042 20010727 00042 CE 2001 7 27 C2XA01CL148 1 20010622 A 3260 DT2RA7 SWITCH BEECH 1900 1900D 1154162 CE COCKPIT DIRTY A C2XA K NONE J WARNING INDICATION CL CLIMB 1 SW 27 87554 UE227 CLE FLT 4377 THE CREW REPORTED LANDING GEAR WARNING HORN AND RED GEAR HANDLE LIGHT ON WITH LANDING GEAR IN UP POSITION . MAINTENANCE CLEANED FLAP POSITION SWITCHES. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT A24CE 2001062600001 20010626 00001 NM 2001 6 26 20010604CW018 1 20010430 A 2761 654494713 HOUSING BOEING 737 737 UTILSYS NM SPOILER ACTUATOR CRACKED E IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 HOUSING IS CRACKED ON THE OPPOSITE SIDE OF PORTS. PROVIDE REPAIR TO INCLUDE USE OF PN 65-449-15 HOUSING ON ALL ACTUATO RS, A MODIFICATION KIT TO THE LATEST CONFIGURATION PN 65-44851-14 OR REPLACEMENT HOUSINGS MADE OF 15-5 PH STEEL OR 7075 -T73 FORGINGS FOR ALL THE DASH NUMBER ACTUATORS. 2 L 7 2 4F RT A16WE 2001062600002 20010626 00002 NM 2001 6 26 20010604CW019 1 20010430 A 3230 65446924 HOUSING BOEING BOEING 737 737 UTILSYS NM MLG MODULE CRACKED B IU6R O OTHER O OTHER NR NOT REPORTED 1 NM 01 1374 HOUSING IS CRACKED IN THE D PRIORITY PORT FLOW PASSAGE. PROBABLE CAUSE: FATIGUE 2 L 7 2 4F RT A16WE 2001062600003 20010626 00003 NM 2001 6 26 20010604CW020 1 20010430 A 3240 511531 HOUSING BOEING 737 737 UTILSYS NM SHUTTLE VALVE CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 HOUSING IS CRACKED INSIDE THE MOUNTING HOLE. FATIGUE, DEFECT IN THE CASTING OF THE HOUSING AND/OR OVER TORQUED BOLTS ON INSTALLATION. IMPROVE DESIGN OR CHANGE THE MATERIAL OF THE HOUSING FOR INCREASED STRENGTH AND RELIABILITY. 2 L 7 2 4F RT A16WE 2001062600004 20010626 00004 NM 2001 6 26 20010605CW001 1 20010430 A 3240 511531 HOUSING BOEING 737 737 UTILSYS NM SHUTTLE VALVE CRACKED B K NONE O OTHER IN INSP/MAINT 1 NM 01 HOUSING IS CRACKED INSIDE THE MOUNTING HOLE. PROBABLE CAUSE: FATIGUE, DEFECT IN THE CASTING OF THE HOUSING AND/OR OVER TORQUED BOLTS ON INSTALLATION. 2 L 7 2 4F RT A16WE 2001062600005 20010626 00005 NM 2001 6 26 20010605CW002 1 20010430 A 3240 511531 HOUSING BOEING 737 737 UTILSYS NM SHUTTLE VALVE CRACKED B K NONE O OTHER IN INSP/MAINT 1 NM 01 HOUSING IS CRACKED INSIDE THE MOUNTING HOLE ALONG THE CASTING SEAM. PROBABLE CAUSE: FATIGUE, DEFECT IN THE CASTING OF THE HOUSING AND/OR OVER TORQUED BOLTS ON INSTALLATION. 2 L 7 2 4F RT A16WE 2001062600006 20010626 00006 NM 2001 6 26 20010605CW003 1 20010430 A 2782 69358521 SLEEVE BOEING 737 737 UTILSYS NM BLOCKING VALVE CRACKED B K NONE O OTHER IN INSP/MAINT 1 NM 01 SLEEVE (31) IS CRACKED. PROBABLE CAUSE: FATIGUE. 2 L 7 2 4F RT A16WE 2001062600007 20010626 00007 NM 2001 6 26 20010605CW004 1 20010430 A 2782 69358521 SLEEVE BOEING 737 737 UTILSYS NM BLOCKING VALVE CRACKED B K NONE O OTHER IN INSP/MAINT 1 NM 01 SLEEVE (145) IS CRACKED. PROBABLE CAUSE: FATIGUE. 2 L 7 2 4F RT A16WE 2001062600008 20010626 00008 NM 2001 6 26 20010605CW005 1 20010430 A 2782 69358521 SLEEVE BOEING 737 737 UTILSYS NM BLOCKING VALVE CRACKED B K NONE O OTHER IN INSP/MAINT 1 NM 01 SLEEVE (145) IS CRACKED. PROBABLE CAUSE: FATIGUE. 2 L 7 2 4F RT A16WE 2001070600013 20010706 00013 WP 2001 7 6 01FDEA00420 1 20010601 A 5330 SKIN DOUG DC10 DC1030F 3023504 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 RIGHT SIDE AFT OF MID CARGO DOOR DAMAGE NEXT TO PRE-EXISTING DOUBLER, FRAME 20, L-39 RT. REMOVED AND REPLACED DOUBLER P ER EA 8-5310-52550A. 2 L 7 3 4F RT A22WE 2001062600009 20010626 00009 NM 2001 6 26 20010605CW006 1 20010430 A 2910 65447821 HOUSING BOEING 737 737 UTILSYS NM HYD VALVE DAMAGED B K NONE O OTHER IN INSP/MAINT 1 NM 01 HOUSING HAS A PINHOLE LEAK OUTSIDE OF PORT NR 1. 2 L 7 2 4F RT A16WE 2001062600010 20010626 00010 NM 2001 6 26 20010605CW007 1 20010424 A 3230 65446925 HOUSING BOEING 737 737 UTILSYS NM MLG MODULE CRACKED B K NONE O OTHER IN INSP/MAINT 1 NM 01 HOUSING IS CRACKED IN THE THREADS OF PORT NR 5. 2 L 7 2 4F RT A16WE 2001062600011 20010626 00011 NM 2001 6 26 20010605CW008 1 20010424 A 3230 65446924 HOUSING BOEING 737 737 UTILSYS NM MLG MODULE CRACKED B K NONE O OTHER IN INSP/MAINT 1 NM 01 HOUSING IS CRACKED IN THE D PRIORITY PORT FLOW PASSAGE. PROBABLE CAUSE: FATIGUE 2 L 7 2 4F RT A16WE 2001062600012 20010626 00012 NM 2001 6 26 20010605CW009 1 20010511 A 2910 123412 COVER BOEING 737 737 UTILSYS NM SHUTOFF VALVE CRACKED B K NONE O OTHER IN INSP/MAINT 1 NM 01 COVER FOUND TO BE CRACKED IN TWO PLACED DURING NDI. PROBABLE CAUSE: FATIGUE. 2 L 7 2 4F RT A16WE 2001062600013 20010626 00013 NM 2001 6 26 20010605CW010 1 20010511 A 2761 65C268636 HOUSING BOEING 737 737 UTILSYS NM ACTUATOR BROKEN B K NONE O OTHER IN INSP/MAINT 1 NM 01 HOUSING IS BROKEN AT THE THREADED BORE FOR RETAINING NUT. PROBABLE CAUSE: FATIGUE 2 L 7 2 4F RT A16WE 2001062600014 20010626 00014 NM 2001 6 26 20010605CW011 1 20010511 A 2761 654494718 HOUSING BOEING 737 737 UTILSYS NM SPOILER ACTUATOR CRACKED B K NONE O OTHER IN INSP/MAINT 1 NM 01 HOUSING ASSEMBLY IS CRACKED UNDER RETRACT PORT. 2 L 7 2 4F RT A16WE 2001062600015 20010626 00015 NM 2001 6 26 20010605CW012 1 20010511 A 2922 654468311 HOUSING BOEING 737 737 UTILSYS NM FILTER PORT CRACKED B K NONE O OTHER IN INSP/MAINT 1 NM 01 HOUSING ASSEMBLY IS CRACKED APPROX 5 INCHES LONG AROUND PACKING AND RETAINER AREA. PROBABLE CAUSE: OVER PRESSURE. 2 L 7 2 4F RT A16WE 2001062600016 20010626 00016 NM 2001 6 26 20010605CW013 1 20010522 A 2140 NYLC50427 ACTUATOR BOEING 727 727212 138407G NM HEAT BYPASS VLV FAILED B MZZA O OTHER O OTHER NR NOT REPORTED 1 EA 07 296AS 21459 HEAT VALVE FAILED IN OPEN CAUSING RAW BLEED AIR TO ENTER CABIN. CABIN FILLED WITH SMOKE (IFE). 2 L 7 3 4F A3WE 2001062600021 20010626 00021 2001 6 26 DHL2001805013 4 20010531 A 2210 AUTOPILOT SYS DOUG DC8 DC873F 302199F WP COCKPIT MALFUNCTIONED A DHLA K NONE O OTHER CR CRUISE 1 SO 01 805DH 46125 AUTOPILOT BANKS 40 DEGREES TO LEFT IN HDG MODE. OVERSHOOTS HEADING SELECTED BY 10 - 12 DEGREES. SWAPPED NR 1 & 2 FOGS. BOTH CK OK IAW LITTON EO 41007 DOC 464544. A/P CKS OK ON BOTH SIDES IAW 22-10-00. ROLL CHANNEL BITE CKS OK IAW 22-12 -00. 2 L 7 4 4F RT 4A25 2001062600022 20010626 00022 NM 2001 6 26 DL72W010810 1 20010519 A 5270 DOOR BOEING 727 727247 138408F NM CARGO DOOR OBSTRUCTED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 2816W 20872 AFT CARGO DOOR LIGHT ILLUM DURING CLIMBOUT. THERE WAS NO REPORTED PRESSURIZATION PROBLEMS. MTC CLEANED DEBRIS FROM TH E DOOR JAMB. NO FURTHER PROBLEMS. 2 L 7 3 4F A3WE 2001062600023 20010626 00023 NM 2001 6 26 DL72W010811 1 20010519 A 5753 6519270 SHIM BOEING 727 727247 138408F NM T/E FLAP OUT OF POSITION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 290WA 22108 DURING INSPECTION OF THE LT INBD FLAP INBD TRACK PER AD 90-07-05 AND BAC S/B 727-57-0178, THE UPPER ANTI FRET STRIP WAS FOUND MIGRATED. THE STRIP WAS REMOVED AND A NEW STRIP INSTALLED PER ER/A 380869-14AD. 2 L 7 3 4F A3WE 2001062600024 20010626 00024 NM 2001 6 26 DL72W010827 1 20010523 A 3233 65404676 ACTUATOR BOEING 727 727247 138408F NM NOSE GEAR WELL FAILED A DALA K NONE K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 27 2816W 20872 NOSE GEAR FAILED TO EXTEND, ASSOCIATED HYDRAULIC SYSTEM QTY WENT TO ZERO. FOUND NLG LOCK ACTUATOR BLOWN APART. REPLACE D SAME. 2 L 7 3 4F A3WE 2001062600025 20010626 00025 NM 2001 6 26 DL72W010853 1 20010527 A 2131 CONTROLLER BOEING 727 727247 138408F NM CABIN PRESSURE FAULTY A DALA I CABIN DEPRESSURIZATION O OTHER CL CLIMB 1 SO 27 2815W 20871 A/C WILL NOT HOLD PRESSURIZATION AT FL240 WITH 1 PACK. DESCENDED TO FL150 TO MAINTAIN CABIN. REPLACED PRESSURE CONTROL LER AND E/E OVERBOARD VALVE. 2 L 7 3 4F A3WE 2001062600026 20010626 00026 NM 2001 6 26 DL72W010879 1 20010531 A 3350 RPS1 POWER SUPPLY BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 296WA 22533 AFT 6 ROWS OF SEATS EMERGENCY LIGHTS INOP AND R2 DOOR EMERGENCY LIGHT INOP. REPLACED POWER SUPPLY. 2 L 7 3 4F A3WE 2001062600027 20010626 00027 NM 2001 6 26 DL72W010880 1 20010531 A 2912 651782119 FILTER HOUSING BOEING 727 727247 138408F NM HYD SYSTEM CRACKED A DALA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 294WA 22112 LOST A-SYS HYDRAULICS ON LANDING GEAR RETRACTION PRESSURE AND QTY DECREASED TO ZERO. FOUND A-SYS FILTER MODULE CRACKED AT CHECK VALVE REPLACED SAME. 2 L 7 3 4F A3WE 2001062600028 20010626 00028 NM 2001 6 26 DL733010815 1 20010521 A 3350 0201991008 LIGHT BOEING 737 737347 1384647 NM CABIN MISSING A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 303WA 23183 FOUND SEAT EMERGENCY LIGHT MISSING AT 16D. REPLACED MISSING LIGHT AND CABLE ASSY. 2 L 7 2 4F RT A16WE 2001062600029 20010626 00029 NM 2001 6 26 DL733010852 1 20010527 A 3260 PROXIMITY SENSOR BOEING 737 737330 NM NLG LOOSE A DALA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 242DL 23834 ON APPROACH WHEN LDG GEAR SELECTED DOWN. NOSE GEAR RED UNSAFE INDICATION ON FWD PNL. EXTENDED NOSE GEAR MANUALLY PER P OM WITH NO CHANGE ON FWD PNL. THEN NOTICED GEAR GREEN INDICATION ON OVERHEAD PNL. NOSE GEAR VISUALLY INSPECTED DOWN AF TER TOUCH DOWN NOSE GEAR INDICATED GREEN. FOUND PROX SW S 846 PRIMARY NOSE DOWNLOCK SENSOR LOOSE AND GAP OUT OF LIMITS. ADJ AND SECURED NOSE DOWNLOCK SENSOR PER M/M. 2 L 7 2 4F RT A16WE 2001062600030 20010626 00030 NM 2001 6 26 DL733010886 1 20010531 A 5330 654576987 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947WP 23376 THE FUSELAGE SKIN WAS FOUND CORRODED AT FS 525 AND STRINGER 28R ADJACENT TO THE GROUND AC ACCESS DOOR. THE CORROSION WAS REMOVED WITH A 5 X 2.2 CUTOUT. THE DAMAGE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PERER/A 3 80935-14, REV A. 2 L 7 2 4F RT A16WE 2001062600031 20010626 00031 NM 2001 6 26 DL733010905 1 20010601 A 5312 65163007 BULKHEAD BOEING 737 737301 1384611 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 948WP 23259 INSPECTION OF THE FS 178 BULKHEAD WEB REVEALED A CRACK IN A TOOLING HOLE AT WL 234 AND LBL 12. A SECOND CRACK WAS FOUND AT A FASTENER HOLE AT WL 233 AND LBL 12. THE HOLES WERE OVERSIZED TO REMOVE THE CRACKS. THE AREA WAS THEN REPAIRED WI TH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 380947-14AD. 2 L 7 2 4F RT A16WE 2001062600032 20010626 00032 2001 6 26 DL73E010864 4 20010529 A 3454 1784460655 INDICATOR BOEING 737 7372S3 NM COCKPIT FAILED A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 367DL 21774 NR 1 INST XMFR C/B POPPED ON PRE-DEPARTURE. REPLACED CAPTS RMI DUE TO OFF FLAG IN VIEW. 2 L 7 2 4F RT A16WE 2001062600033 20010626 00033 2001 6 26 DL73K010795 4 20010518 A 3442 284T02204 ANTENNA BOEING 737 737232 1384475 NM WX RADAR FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 331DL 23103 WX RADAR ANTENNA FAULT. REPLACED WX RADAR ANTENNA, TEST GOOD. THIS WAS AN AIR TURNBACK. 2 L 7 2 4F RT A16WE 2001062600034 20010626 00034 NM 2001 6 26 DL73K010812 1 20010521 A 2120 UNKNOWN BOEING 737 737247 138448D NM CABIN ODOR A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 382DL 23609 AFTER NR 2 ENG GEN PUT ON LINE XFER BUSS NR 1 DID NOT TAKE POWER. RECYCLED BUSS XFER SWITCH, OPS NORMAL. NR 2 FUEL HEA T LIGHT WOULD BLINK PERIODICALLY. AT V1 SMELLED ELECTRICAL BURNING ODOR. THE FLIGHT ATTENDANTS CONFIRMED THE ODOR. RA N BOTH ENGS, ALL POWER TRANSFER NORMAL AND SMOOTH. BETWEEN APU AND ENGS WITH ENGS RUNNING AND PACKS OPERATING CKD GALLE YS, CABIN AND LAVS NO BURNING ODOR NOTED. REPLACED COALESCER BAGS AS PRECAUTION. CHECKED FUEL HTR WIRING FROM COCKPIT TO ENG, ALL OK. RAN ENGS OPS OF FUEL HEAT VLV NORMAL. 2 L 7 2 4F A16WE 2001062600035 20010626 00035 NM 2001 6 26 DL73K010814 1 20010521 A 2150 20405011 ACM BOEING 737 737247 138448D NM A/C BAY SEIZED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 239WA 23187 A/C DIVERTED INTO JAX WITH SMOKE/FUMES IN THE CABIN AND COCKPIT. PASSENGERS IN SEAT 10ABC FELT AND HEARD RUMBLING UNDER FLOOR INDICATING A PACK PROBLEM. UPON FURTHER INVESTIGATION FOUND THE LEFT PACK ACM HAD SEIZED UP CAUSING THE FUMES AN D SMOKE. LEFT PACK WAS PUT ON MCO AND POSITION FERRIED BACK TO ORLANDO. 2 L 7 2 4F A16WE 2001062600036 20010626 00036 NM 2001 6 26 DL73K010816 1 20010521 A 3350 20131A BATTERY PACK BOEING 737 737232 1384475 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 321DL 23093 ON SERVICE CK, FOUND CABIN OVERWING EXIT SIGN INOP FOR CENTER AISLE. REPLACED BATTERY PACK PER M/M, CKS OK. 2 L 7 2 4F RT A16WE 2001062600037 20010626 00037 NM 2001 6 26 DL73K010840 1 20010525 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 329DL 23101 A 1 INCH LONG CRACK WAS FOUND IN THE FUSELAGE SKIN AT FS 750 JUST ABOVE STRINGER 18R. THE CRACK WAS REMOVED WITH A CUTO UT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B737-200 SRM 53-30-3, FIG 17 AND ER/A 380 916-14. 2 L 7 2 4F RT A16WE 2001062600038 20010626 00038 NM 2001 6 26 DL73K010851 1 20010527 A 2913 623337 PUMP 6937317110 BOEING 737 737247 138448D NM ENGINE DEFECTIVE A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 245WA MX281270MX50 23519 IN CRUISE FLT 28,000 FEET, SYS-A HYD LOW PRESS LIGHT ON NR 1 ENGINE CAME ON. A-SYS HYD PRESS DROPPED. TURNED OFF THAT SWITCH. 3-5 MINUTES LATER THE OTHER LOW PRESS LIGHT CAME ON. THIS DROPPED SYS-A PRESS FROM 2500 PSI TO ZERO. FOLLOWED LOSS OF SYSTEM-A PROCEDURE AND LANDED UNEVENTFULLY. MAINT TOWED A/C TO GATE. HYD QTY CKD FULL. NO LEAKS FOUND. CASE DRAIN FILTERS CLEAN. ON ENGINE RUN OPN NORMAL. REPLACED BOTH ENGINE HYD PUMPS. RAN ENGINES AND CYCLED FLT CONTROLS. 2 L 7 2 4F A16WE 2001062600039 20010626 00039 NM 2001 6 26 DL73K010869 1 20010530 A 5311 FRAME BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 320DL 23092 A CRACK WAS FOUND IN THE LOWER FASTENER HOLE OF BOTH THE LT AND RT FS 616 FRAME TO STUB BEAM. THE CRACK WAS REMOVED AND REPAIRED PER S/B 737-53-1182 AT HMV. 2 L 7 2 4F RT A16WE 2001062600040 20010626 00040 NM 2001 6 26 DL73S010828 1 20010518 A 5330 655298881 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 323DL 23095 THE L2 DOOR HAS A 0.50 INCH CRACK IN THE LOWER HINGE CUTOUT SKIN. ER/A 363983-14 REV A. 2 L 7 2 4F RT A16WE 2001062600041 20010626 00041 NM 2001 6 26 DL73S010858 1 20010529 A 5313 65476937 STRINGER BOEING 737 737232 1384475 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 323DL 23095 CORROSION WAS FOUND ON THE S27L KEEL CHORD AT APPROXIMATELY FS 757. THE DAMAGED SECTION WAS REMOVED AND REPAIRED BY INS TALLING TWO REPAIR ANGLES PER ERA 397569-14 AT HMV. 2 L 7 2 4F RT A16WE 2001062600042 20010626 00042 NM 2001 6 26 DL757010797 1 20010518 A 5350 141N782013 RADOME BOEING 757 757232 1384965 NM FUSELAGE DAMAGED A DALA K NONE J WARNING INDICATION DE DESCENT 1 SO 27 631DL 23612 CREW REPORTED RADAR FAILED AT FL240. ON ARR PBI GROUND CREW NOTICED RADOME UPPER LEFT CRUSHED IN. AN AREA ABOUT THE SI ZE OF THREE BASKET BALLS. THE RADOME WAS REPLACED, AND THE RADAR ANTENNA ALSO AS A PRECAUTION. INSPECTED NOSE BULKHEAD AND A/C, NO OTHER DAMAGE FOUND. 2 L 7 2 4F RT A2NM 2001062600043 20010626 00043 2001 6 26 DL757010807 4 20010520 A 2565 D30654131 SLIDE BOEING 757 757232 1384965 NM R1 DOOR OUT OF POSITION A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 652DL 24392 EMERGENCY SLIDE COVER AT R1 DOOR FELL OFF. MAINTENANCE FOUND SLIDE COVER AND SLIDE SEPARATED FROM DOOR. MAINTENANCE RE INSTALLED SLIDE AND COVER ONTO THE R1 DOOR. NO ONE PRESENT HAD AN EXPLANATION AS TO WHY THE SLIDE FELL OFF. 2 L 7 2 4F RT A2NM 2001062600044 20010626 00044 NM 2001 6 26 DL757010826 1 20010523 A 3350 02019241007 LIGHT BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 629DL 22919 LARGE RED RECTANGULAR EMERGENCY LIGHT(L9011), IN F/C FAILED TO ILLUMINATE WHEN TESTED. REPLACED LIGHT ASSY. 2 L 7 2 4F RT A2NM 2001062600045 20010626 00045 WP 2001 6 26 AT0100184 1 20010514 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 1117-L17R CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 840AT 47523 FOUND CORROSION ON LONGERON AND SKIN AREA AT BS 1117-L17R IN AFT ACCESSORY COMPARTMENT. CORRECTIVE ACTION: REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REPLACED LONGERON SECTION WITH REPAIR LONGERON, TRIMMED, FABRICATED A ND INSTALLED REPAIR DOUBLER. IAW DC9 SRM 51-10-2, 51-10-3, 51-10-4, 51-30-2, 51-30-5 2 L 7 2 4F A6WE 2001062600046 20010626 00046 WP 2001 6 26 AT0100185 1 20010514 A 5311 PAN DOUG DC9 DC932 3022066 WP FWD CARGO CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 840AT 47523 FOUND FORWARD CARGO DOOR FRAME LOWER PAN CORRODED. CORRECTIVE ACTION: REMOVED CORROSION AND FOUND TO B E OUT OF LIMIITS. REMOVED FORWARD AND AFT LOWER PAN SPLICES. CUT, TRIMMED, DRILLED AND INSTALLED SPLICES. IAW DC9 SRM 53-04 FIGURE 44, 51-10-3, 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 2001062600047 20010626 00047 WP 2001 6 26 AT0100186 1 20010516 A 5311 FRAME DOUG DC9 DC932 3022066 WP FRAME 965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 840AT 47523 FOUND CORROSION ON AFT SIDE OF FRAME 965. CORRECTIVE ACTION: REMOVED CORROSION AND INSTALLED NEW FRAME , LOWER AND UPPER SPLICES. FABRICATED DOUBLER AND INSTALLED. IAW DC9 SRM 53-03 FIGURE 24, 57-10-2,51-10-3,51-10-4,51 -30-2,51-30-5 2 L 7 2 4F A6WE 2001062600048 20010626 00048 WP 2001 6 26 AT0100187 1 20010523 A 5347 TRACK DOUG DC9 DC932 3022066 WP BS 200-240 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 840AT 47523 FOUND CABIN SEAT TRACK AT BS 200-240 WAS FOUND TO BE CORRODED BEYOND LIMITS. CORRECTIVE ACTION: INSTAL LED NEW SEAT TRACK SPLICE. IAW DC9 SRM 51-30-5,51-30-1,53-05 FIGURE 4. 2 L 7 2 4F A6WE 2001062600049 20010626 00049 WP 2001 6 26 AT0100189 1 20010516 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 200-247 BL22L CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 840AT 47523 FOUND CABIN SEAT TRACK CORRODED AT BS 200-965 BL22L. CORRECTIVE ACTION: REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR. IAW DC9 SRM 51-30-5, 51-30-2, 53-05 FIGURE 4, 51-10-3, 51-10-2. 2 L 7 2 4F A6WE 2001062600050 20010626 00050 WP 2001 6 26 AT0100190 1 20010517 A 5315 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP BS 160-218 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 840AT 47523 FOUND CABIN FLOOR SUPPORT AT BS 160-218 CORRODED. CORRECTIVE ACTION: REMOVED CORROSION, FABRICATED AND INSTALLED FLOOR SUPPORT REPAIR. IAW DC9 SRM 53-11-1 FIGURE 11, 51-10-3,51-30-2 2 L 7 2 4F A6WE 2001062600051 20010626 00051 WP 2001 6 26 AT0100191 1 20010517 A 5315 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 840AT 47523 FOUND CABIN FLOOR SUPPORT AT BS 200 CORRODED. CORRECTIVE ACTION: REMOVED CORROSION, FABRICATED AND INS TALLED FLOOR SUPPORT REPAIR. IAW DC9 SRM 53-01,51-10-4,53-11-1,51-30-5 2 L 7 2 4F A6WE 2001062600052 20010626 00052 WP 2001 6 26 AT0100192 1 20010518 A 5315 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP BS 992 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 840AT 47523 FOUND CABIN FLOOR SUPPORT AT BS 992 CORRODED. CORRECTIVE ACTION: REMOVED CORROSION, FABRICATED AND INS TALLED FLOOR SUPPORT REPAIR. IAW DC9 SRM 53-11-1 FIGURE 11, 51-10-3,51-30-2, 53-01 FIGURE 2 2 L 7 2 4F A6WE 2001062600053 20010626 00053 WP 2001 6 26 AT0100196 1 20010516 A 5320 SKIN DOUG DC9 DC932 3022066 WP L-1 DOOR CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 840AT 47523 FOUND CRACK IN FORWARD CORNER OF L-1 DOOR CUT OUT. CORRECTIVE ACTION TRIMMED OUT CRACK, FABRICATED AND INSTALLEK FILLER, DOUBLER AND TRIPLER. IAW DC9 SRM 53-05 FIGURE 114 AND RES01-0565 2 L 7 2 4F A6WE 2001062600054 20010626 00054 NM 2001 6 26 DL757010837 1 20010524 A 5754 114N4004145 WEDGE BOEING 757 757232 1384965 NM L/E SLAT DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 629DL 22919 DURING CURRENT PSV, DENT WAS FOUND ON THE NR 3 LEADING EDGE SLAT TRAILING EDGE WEDGE. REPAIR PER ER/A 380892-14AD. 2 L 7 2 4F RT A2NM 2001062600055 20010626 00055 NE 2001 6 26 DL757010841 2 20010525 A 7321 756001778 EEC BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 639DL 23993 716584 ALL RT ENG INSTRUMENTS FLUCTUATED DURING INITIAL CLIMB OUT. AT 10K LEVEL OFF (250K) IND STABILIZED BUT RESUMED FLUX ON SUBSEQUENT CLIMB TO 14K. RETURNED TO SLC. NOTICED BIRD PASS BY RT SIDE ON INITIAL CLIMB. RAN ENGS PER PFHB, NOTICED F LUX ON EPR, N1 AND EGT-AT 80 PERCENT N1 TO 83SA PERCENT N1-T/S PER FIM CKED C/P'S AT PMC-CK OK-CK C/P J-10 AND J-4 ON EE C CK OK. REPLACED RT EEC PER MM RAN ENGS PER PFHB. ALL IND CK NORMAL. NO INDICATION OF BIRD STRIKE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001062600056 20010626 00056 NM 2001 6 26 DL757010845 1 20010526 A 5610 141T480119 WINDOW BOEING 757 757232 1384965 NM COCKPIT DAMAGED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 619DL 22909 AT FLT LVL 330 - 40 MILES OUT OF BNA, TOOK 1 BREATH OF FRESH AIR, THE NEXT BREATH WAS FOUL AND TOXIC, SMELL WAS THROUGHO UT CABIN AND COCKPIT. ON GROUND 30 SECONDS SMELL GOT WORSE. EVACUATED A/C. REPLACED PWR WIRE AND L-1 WINDOW ASSY DUE TO HEAT DAMAGE. 2 L 7 2 4F RT A2NM 2001062600057 20010626 00057 NM 2001 6 26 DL757010850 1 20010526 A 2760 251N509914 TORQUE TUBE BOEING 757 757232 1384965 NM A/C BAY BENT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 611DL 22818 WHILE WORKING MCO ON TRIM AIR SYSTEM DISCOVERED INSULATION BLANKET ALONG WITH WIRING WRAPPED AROUND SLAT TORQUE TUBE. 2 L 7 2 4F RT A2NM 2001062600058 20010626 00058 NM 2001 6 26 SWAA011469 1 20010517 A 5523 BACB28AK04 BUSHING BOEING 737 7377H4 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 787SA 29812 DURING SCHEDULED SERVICE CHECK, SWA SI 11052-55, FOUND LT ELEVATOR, NR 2 & 3 TAB HINGE BUSHINGS WORN. REMOVED AND REPLA CED BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2001062600059 20010626 00059 NM 2001 6 26 SWAA011470 1 20010517 A 5311 963820 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL CHORD CRACKED AT BS 178, WL 183 AND LBL 5.5. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2001062600060 20010626 00060 NM 2001 6 26 SWAA011471 1 20010516 A 5320 65C27314 TIE CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STR TIE CLIP PER SRM . 2 L 7 2 4F RT A16WE 2001062600061 20010626 00061 NM 2001 6 26 SWAA011472 1 20010516 A 5311 6545877 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 14R. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2001062600062 20010626 00062 NM 2001 6 26 SWAA011473 1 20010516 A 5511 6550582 SPAR BOEING 737 7373H4 1384600 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED C1 CHECK, FOUND RT HORIZ STABILIZER AFT SPAR LWR SURFACE CRACKED, APPROX 60 INCHES OTBD OF ROOT. REPA IRED SPAR PER SRM. 2 L 7 2 4F RT A16WE 2001062600063 20010626 00063 NM 2001 6 26 SWAA011474 1 20010518 A 5310 141A880 WINDOW POST BOEING 737 7372H4 138448C NM COCKPIT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 090SW 22905 DURING SPECIAL VISIT CHECK, FOUND F/O'S C-D UPPER WINDOW POST CRACKED. REPAIRED POST PER SRM. 2 L 7 2 4F A16WE 2001062600064 20010626 00064 NM 2001 6 26 SWAA011490 1 20010518 A 5330 6545773 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT LT WINDOW NR 10, 5, 7 AND 2, LOWER AFT CORNER CUTOUTS. 2 L 7 2 4F A16WE 2001062600065 20010626 00065 NM 2001 6 26 SWAA011491 1 20010518 A 5330 6545773 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT LT WINDOW NR 26, 27 AND 28, LOWER FWD CORNER CUTOUTS. 2 L 7 2 4F A16WE 2001062600066 20010626 00066 NM 2001 6 26 SWAA011492 1 20010518 A 5330 6545773 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT LT WINDOW NR 4, 5, 9, 1, 2 AND 3, UPPER FWD CORNER CUTOUTS. 2 L 7 2 4F A16WE 2001062600067 20010626 00067 NM 2001 6 26 SWAA011493 1 20010518 A 5330 6545773 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT RT WINDOW NR 11, 3, 6, AND 2, UPPER FWD CORNER CUTOUTS. 2 L 7 2 4F A16WE 2001062600068 20010626 00068 NM 2001 6 26 SWAA011494 1 20010518 A 5330 6545773 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT RT WINDOW NR 5, 9, 11 AND 2, LOWER AFT CORNER CUTOUTS. 2 L 7 2 4F A16WE 2001062600069 20010626 00069 NM 2001 6 26 SWAA011506 1 20010518 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001062600070 20010626 00070 SO 2001 6 26 C2XA01CL149 1 20010622 A 4900 4501968D APU EMB 145 EMB145LR SO AFT FUSELAGE FAILED A C2XA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 27 13956 2986 145078 BTV FLIGHT#4059 THE CREW REPORTED THE APU HAD A AUTO SHUT DOWN ON THE GROUND.MAINTENANCE REPLACED THE APU.OPERATIONAL C HECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001062600071 20010626 00071 NM 2001 6 26 SWAA011507 1 20010519 A 5330 65C35775 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 743, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001062600072 20010626 00072 NM 2001 6 26 SWAA011508 1 20010519 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 380, STR 15L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001062600073 20010626 00073 NM 2001 6 26 SWAA011509 1 20010518 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 480 & BS 500A, STR 10L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001062600074 20010626 00074 NM 2001 6 26 SWAA011510 1 20010519 A 5330 6545773 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT RT WINDOW NR 31, 28, 30, 29, 25 AND 26, UPPER AFT CORNER CUTOUT S. 2 L 7 2 4F A16WE 2001062600075 20010626 00075 NM 2001 6 26 SWAA011511 1 20010519 A 5330 6545773 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT RT WINDOW NR 31, 27, 28, 25, 30, 29 AND 26, LOWER FWD CORNER CU TOUTS. 2 L 7 2 4F A16WE 2001062600076 20010626 00076 NM 2001 6 26 SWAA011516 1 20010522 A 3211 65C31332 BEARING BOEING 737 7373G7 1384595 NM RT MLG GROOVED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED SERVICE CHECK, FOUND GROOVED RT MLG TRUNNION BEARING. REMOVED AND REPLACED RT MLG TRUNNION BEARING PER MM. 2 L 7 2 4F RT A16WE 2001062600077 20010626 00077 NM 2001 6 26 SWAA011517 1 20010522 A 5312 6546568 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED C1 CHECK, FOUND THROUGH HFEC INSPECTION CRACKS AT TWO LOCATIONS, BS 1016 BULKHEAD, STR 6L. REPAIRED BU LKHEAD PER SRM. 2 L 7 2 4F A16WE 2001062600078 20010626 00078 NM 2001 6 26 SWAA011518 1 20010522 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOORBEAMS AFT CARGO COMP, AT BS 727+4 AND BS 727B+4, LBL 2.5 TO RBL 2.5. REPAIRED FLOORBEAMS PER SRM. 2 L 7 2 4F RT A16WE 2001062600079 20010626 00079 NM 2001 6 26 SWAA011519 1 20010522 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOORBEAM AFT CARGO COMP, BS 727D+5, LBL 8 TO RBL 8. REPAIRED FLOORBEAM PE R SRM. 2 L 7 2 4F RT A16WE 2001062600080 20010626 00080 NM 2001 6 26 SWAA011520 1 20010522 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOORBEAM AFT CARGO COMP AT BS 767, LBL 12 TO RBL 20. REPAIRED FLOORBEAM P ER SRM. 2 L 7 2 4F RT A16WE 2001062600081 20010626 00081 WP 2001 6 26 ZW0A0104102 1 20010625 A 3350 0105606003 MODULE DOUG DC9 DC983 3022083 WP ROW 12 TO 15 A ZW0A K NONE O OTHER NR NOT REPORTED 1 CE 13 9627R 53597 THE EGRESS LIGHTS AT ROW 12 TO 15 WERE INOPERATIVE. REPLACED THE LAMP MODULE. CHECK-C 12-17-00 JFK. --CLOSED-- 2 L 7 2 4F RT A6WE 2001062600082 20010626 00082 NM 2001 6 26 SWAA011521 1 20010520 A 3210 654610914 BEAM BOEING 737 7373G7 1384595 NM RT MLG WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED SERVICE CHECK, FOUND RT MLG ACTUATOR CLEVIS BEAM ARM BUSHING WORN AND CORRODED. REMOVED AND REPLACED C LEVIS BEAM ARM PER MM. 2 L 7 2 4F RT A16WE 2001062600083 20010626 00083 NM 2001 6 26 SWAA011527 1 20010522 A 5511 6550582 SPAR BOEING 737 7375H4 138449D NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 DURING SCHEDULED C4 CHECK, FOUND LT HORIZ STABILIZER AFT SPAR LWR SURFACE CRACKED, 72 INCHES OUTBOARD OF ROOT. REPAIRED SPAR PER SRM. 2 L 7 2 4F RT A16WE 2001071200100 20010712 00100 WP 2001 7 12 ARWA0010606 1 20010622 A 3310 TRANSFORMER DOUG DC8 DC863 302198A WP COCKPIT MALFUNCTIONED A ARWA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 19 345JW 46042 TAXI OUT SMOKE CAME OUT OF ELECTRICAL PANEL. AIRCRAFT RETURN TO BLOCKS WITHOUT INCIDENT. LOCATED THE SOURCE, GLARE INS TRUMENT WHITE LIGHTS BALLAST TRANSFORMER. DEACTIVATED GLARESHIELD AND INSTRUMENT WHITE LIGHTS AND ENTERED ON DMI 15265 AS PER MEL 33-1 CAT C. 2 L 7 4 4F 4A25 2001062600084 20010626 00084 EU 2001 6 26 C2XA01BT118 1 20010524 A 5315 S5317220625800 BEAM AEROSP ATR42 ATR42320 8680930 EU CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 97841 280 YUL-Durring a scheduled 3C inspection, Corrosion was found in the cockpit, left side at frame 9, WL2640. Maintence remov ed and replaced the floor beam I.A.W.-ATR-42-SRM-51-25-01. 2 H 7 2 4T RT A53EU 2001062600085 20010626 00085 NM 2001 6 26 SWAA011528 1 20010523 A 5330 65C35794 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 313SW 23335 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 805, STR 19. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001062600086 20010626 00086 NM 2001 6 26 SWAA011529 1 20010523 A 5312 6517582 BULKHEAD BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED D-CHECK, FOUND VERTICAL BEAMS CRACKED AT BS 178, LBL 17.1, LBL 5.7. REPAIRED PER SWA RA. 2 L 7 2 4F RT A16WE 2001062600087 20010626 00087 NM 2001 6 26 SWAA011530 1 20010523 A 5312 6517583 BULKHEAD BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED D-CHECK, FOUND VERTICAL BEAM CRACKED AT BS 178, RBL 17.1. REPAIRED PER SWA RA. 2 L 7 2 4F RT A16WE 2001062600088 20010626 00088 NM 2001 6 26 SWAA011531 1 20010523 A 5754 65C26601 SKIN BOEING 737 7375H4 138449D NM L/E SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 504SW 24181 DURING SCHEDULED C1 CHECK, FOUND NR 1 L/E SLAT LWR SKIN CRACKED AT AFT ROW OF RIVETS, IN 4 PLACES. REMOVED AND REPLACED NR 1 L/E SLAT PER MM. 2 L 7 2 4F RT A16WE 2001062600089 20010626 00089 NM 2001 6 26 SWAA011532 1 20010523 A 5312 6546568 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 090SW 22905 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND AFT PRESS BULKHEAD CRACKED AT BS 1016, CENTER AREA. REPAIRED PER SRM AND BO EING TELEX. 2 L 7 2 4F A16WE 2001062600090 20010626 00090 NM 2001 6 26 SWAA011533 1 20010522 A 2730 65617516 SHAFT BOEING 737 7377H4 NM ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 711HK 27845 DURING SCHEDULED C4 CHECK, RT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR OUTPUT SHAFT PER MM. 2 L 7 2 4F RT A16WE 2001062600091 20010626 00091 NM 2001 6 26 SWAA011534 1 20010523 A 5240 6523464 SKIN BOEING 737 7373H4 1384600 NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 611SW 27697 FWD SVC DOOR SKIN CRACKED AT UPPER LEFT CORNER. REMOVED AND REPLACED FWD SVC DOOR PER MM. 2 L 7 2 4F RT A16WE 2001062600092 20010626 00092 NM 2001 6 26 SWAA011546 1 20010524 A 5330 6545773 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED RON CHECK, ON WALK AROUND INSPECTION FOUND FUSELAGE SKIN CRACKED AT BS 500+5, STR 10R. REPAIRED SKIN P ER SRM. 2 L 7 2 4F RT A16WE 2001062600093 20010626 00093 NM 2001 6 26 SWAA011547 1 20010523 A 3210 6567172 BEAM BOEING 737 7373H4 1384600 NM LT & RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED D-CHECK, FOUND CORROSION ON LT AND RT MLG STABILIZER BEAMS. REMOVED AND REPLACED LT & RT MLG STABILIZE R BEAMS PER MM. 2 L 7 2 4F RT A16WE 2001062600094 20010626 00094 NM 2001 6 26 SWAA011548 1 20010524 A 5310 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2001062600095 20010626 00095 NM 2001 6 26 SWAA011549 1 20010524 A 5330 6545773 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 455, STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001062600096 20010626 00096 NM 2001 6 26 SWAA011554 1 20010525 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 384SW 26590 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT CENTER CABIN. REPAIRED AND SECURED LOOSE WIRING PER MM. 2 L 7 2 4F RT A16WE 2001062600097 20010626 00097 NM 2001 6 26 SWAA011555 1 20010525 A 3350 BR2013 LIGHT BOEING 737 7377H4 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 768SW 30587 EEPLS LOOSE AT ROW 2. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001062600098 20010626 00098 NM 2001 6 26 SWAA011556 1 20010525 A 3397 BR2013 WIRE BOEING 737 7377H4 1384404 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 733SA 27865 DURING SCHEDULED RON CHECK, FOUND EEPLS WIRES EXPOSED AT ROW 1. SECURED WIRES PER MM. 2 L 7 2 4F RT A16WE 2001062600099 20010626 00099 NM 2001 6 26 SWAA011561 1 20010525 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 636WN 27709 DURING SCHEDULED C3 CHECK, FOUND NUMEROUS EEPLS COVERS CRACKED BETWEEN ROWS 3 & 24. REMOVED AND REPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2001062600100 20010626 00100 NM 2001 6 26 SWAA011562 1 20010526 A 5312 6516300 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 218.5, RBL 10-11. REPAIRED BULKHEAD WEB PER SRM. 2 L 7 2 4F A16WE 2001062600101 20010626 00101 NM 2001 6 26 SWAA011563 1 20010526 A 5312 6517582 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED D-CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178 BULKHEAD, WL 184, LBL 17.1. REPAIRED VERT BEAM WEB PER BFG ERO AND BAC DWG. 2 L 7 2 4F A16WE 2001062600102 20010626 00102 NM 2001 6 26 SWAA011564 1 20010527 A 5320 BAC1503 STIFFENER BOEING 737 7373T5 NM MLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 667SW 23063 DURING SCHEDULED SERVICE CHECK, FOUND VERTICAL STIFFENER CRACKED, AT MLG WHEEL WELL, BS 663, RBL 6.4. REPAIRED PER SWA RA. 2 L 7 2 4F RT A16WE 2001062600103 20010626 00103 NM 2001 6 26 SWAA011565 1 20010525 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 500C & 500D AT STR 15L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001062600104 20010626 00104 NM 2001 6 26 SWAA011566 1 20010527 A 5310 6546569 SHEAR TIE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED D-CHECK, FOUND CRACKED SHEAR TIE AT BS 1040, BETWEEN STR 2R & 3R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F A16WE 2001062600105 20010626 00105 NM 2001 6 26 SWAA011567 1 20010525 A 5320 6551698 SPLICE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED D-CHECK, FOUND STR SPLICE CRACKED AT BS 908, STR 4L. REPAIRED STR SPLICE PER SRM. 2 L 7 2 4F A16WE 2001062600106 20010626 00106 NM 2001 6 26 SWAA011568 1 20010525 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504.5C, ABOVE STR15L. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 2001062600107 20010626 00107 NM 2001 6 26 SWAA011569 1 20010527 A 3397 BR2013 WIRE BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 524SW 26566 EEPLS WIRES BROKEN AT ROW 13. REPAIRED EEPLS WIRES PER MM. 2 L 7 2 4F RT A16WE 2001062600108 20010626 00108 NM 2001 6 26 SWAA011570 1 20010527 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 389SW 26592 EEPLS LIGHTS INOP AT MID CABIN. REPAIRED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001062600109 20010626 00109 NM 2001 6 26 SWAA011572 1 20010527 A 3350 65C27093 PLATE BOEING 737 7375H4 138449D NM ENTRY DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 512SW 24189 DURING SCHEDULED RON CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT BASE PLATE BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BASE PLATE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001062600110 20010626 00110 NM 2001 6 26 SWAA011578 1 20010527 A 5523 BACB28AM07 BUSHING BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED C4 CHECK, FOUND RT ELEVATOR TAB INBD HINGE BUSHING WORN. REMOVED AND REPLACED TAB INBD HINGE BUSHING P ER MM. 2 L 7 2 4F RT A16WE 2001062600111 20010626 00111 NM 2001 6 26 SWAA011579 1 20010526 A 5743 6567172 FITTING BOEING 737 7373A4 1384585 NM LT & RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED SERVICE CHECK, FOUND LT & RT WALKING BEAM HANGER FITTINGS CORRODED AT FWD OTBD, LT & RT MLG. REMOVED A ND REPLACED BOTH WALKING BEAM HANGER FITTINGS PER MM. 2 L 7 2 4F RT A16WE 2001062600112 20010626 00112 NM 2001 6 26 SWAA011580 1 20010529 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOORBEAM AFT CARGO COMP AT BS 727D+5, LBL 17 & WL 155.5. REPAIRED FLOORBE AM PER SRM. 2 L 7 2 4F RT A16WE 2001062600113 20010626 00113 NM 2001 6 26 SWAA011581 1 20010530 A 3350 65C34691 LENS BOEING 737 7373Q8 1384670 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LENS MISSING AT RT OVERWING EXIT. REPLACED BULL NOSE LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001062600114 20010626 00114 NM 2001 6 26 SWAA011582 1 20010529 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 734SA 27866 DURING SCHEDULED C3 CHECK, FOUND EEPLS COVER CRACKED AT FWD CABIN. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2001062600115 20010626 00115 NM 2001 6 26 SWAA011583 1 20010529 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 396SW 27690 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER CRACKED AT MID CABIN. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2001062600116 20010626 00116 2001 6 26 SWAA011584 4 20010529 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001062600117 20010626 00117 NM 2001 6 26 SWAA011585 1 20010529 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 751SW 29803 EEPLS COVER BROKEN AT FWD CABIN. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2001062600118 20010626 00118 NM 2001 6 26 SWAA011586 1 20010529 A 3397 BR2013 WIRE BOEING 737 7377H4 1384404 NM CABIN EXPOSED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 733SA 27865 EEPLS TRACK WIRES EXPOSED AT ROW 1. SECURED EEPLS WIRES PER MM. 2 L 7 2 4F RT A16WE 2001062600119 20010626 00119 NM 2001 6 26 SWAA011587 1 20010530 A 3350 BR2013 TRACK BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 389SW 26592 EEPLS TRACK LOOSE AT ROW 11 TO ROW 21. SECURED EEPLS TRACK PER MM. 2 L 7 2 4F RT A16WE 2001062600120 20010626 00120 2001 6 26 SWAA011588 4 20010530 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 068SW 22357 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001062600121 20010626 00121 NM 2001 6 26 PCAA0106059 1 20010620 A 3310 RV4NBYSD502A RHEOSTAT DHAV DHC8 DHC8102 2809003 NM CAPTAINS SIDE BURNED A PCAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 13 812EX 312 IAP- FLIGHT#3622. CREW REPORTED SMOKE COMING OUT FROM PANEL BETWEEN HANDLE AND WINDSHIELD.(OVERHEAD) MAINTENANCE DETERMI NED TO BE CAPTAINS OVERHEAD MAP LIGHT RHEOSTAT. WIRING ISOLATED. MEL 33-01 ISSUED. AIRCRAFT RETURNED TO SERVICE. 22 JUN 01 RHEOSTAT FOR CAPTAINS OVERHEAD MAP LIGHT REPLACED. OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2001062600122 20010626 00122 NM 2001 6 26 SWAA011589 1 20010529 A 5330 6552988 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 942, STR 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001062600123 20010626 00123 NM 2001 6 26 SWAA011590 1 20010530 A 2731 6545166 ROD END BOEING 737 7377H4 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 710SW 27844 DURING SCHEDULED SERVICE CHECK, FOUND LT ELEVATOR TAB CONTROL ROD ENDS WORN. REMOVED AND REPLACED TAB CONTROL ROD ENDS PER MM. 2 L 7 2 4F RT A16WE 2001062600124 20010626 00124 NM 2001 6 26 SWAA011591 1 20010530 A 5523 BACB28AK04B BUSHING BOEING 737 7377H4 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 710SW 27844 DURING SCHEDULED SERVICE CHECK SWA AD 11052-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATO R INBOARD HINGE BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2001062600125 20010626 00125 NM 2001 6 26 SWAA011592 1 20010529 A 5311 6546546 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, BETWEEN STR 8L AND STR 9L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001062600126 20010626 00126 NM 2001 6 26 SWAA011593 1 20010530 A 5754 65C26601 SKIN BOEING 737 7372H4 138448C NM L/E SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED D-CHECK, FOUND NR 1 L/E SLAT LOWER SKIN CRACKED AT AFT ROW OF RIVETS, 31 FROM OUTBOARD END. 2 L 7 2 4F A16WE 2001062600127 20010626 00127 2001 6 26 SWAA011594 4 20010530 A 2565 NAS604 SCREW BOEING 737 7377H4 NM EVAC SLIDE MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 713SW 27847 FWD ENTRY DOOR EMERGENCY EVAC SLIDE, SCREW MISSING FROM RETAINING HOLDER. INSTALLED SCREW PER MM. 2 L 7 2 4F RT A16WE 2001062600128 20010626 00128 NM 2001 6 26 SWAA011595 1 20010530 A 7711 PIN BOEING 737 7372H4 138448C NM CONNECTOR BENT A SWAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 07 067SW 22356 (ABORTED TAKEOFF) NR 2 EPR DID NOT RESPOND INITIALLY, CAME UP BUT VARIED FROM IDLE TO APPROX 1.6. REMOVED AND REPLACED NR 2 ENG EPR TRANSMITTER AND REMOVED AND REPLACED BENT PIN AT TRANSMITTER CONNECTOR PER MM. 2 L 7 2 4F A16WE 2001062600129 20010626 00129 NM 2001 6 26 SWAA011596 1 20010530 A 2560 RIVET BOEING 737 7377H4 NM SERVICE DOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 760SW 27874 DURING SCHEDULED BC1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK RETAINER MISSING RIVET. INSTALLED RET AINER RIVET PER SRM. 2 L 7 2 4F RT A16WE 2001062600130 20010626 00130 2001 6 26 SWAA011597 4 20010530 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED RON CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EME RGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001062600131 20010626 00131 NM 2001 6 26 SWAA011598 1 20010531 A 3350 BR2013 TRACK BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 639SW 27712 EEPLS TRACK LOOSE AT MID CABIN. SECURED EEPLS TRACK PER MM. 2 L 7 2 4F RT A16WE 2001062600132 20010626 00132 NM 2001 6 26 SWAA011599 1 20010531 A 3350 079123 COVER BOEING 737 7373A4 1384585 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 EEPLS COVER MISSING AT ROW 10. INSTALLED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2001062600133 20010626 00133 2001 6 26 SWAA011600 4 20010531 A 2565 D31354 SLIDE BOEING 737 7377H4 NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 798SW 28436 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001062600134 20010626 00134 NM 2001 6 26 SWAA011601 1 20010531 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM AFT DOORS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 379SW 26586 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY AND AFT SVC DOORS MISSING OVERHEAD EMERGENCY EXIT LIGHT LENSES. INSTALL ED EXIT LIGHT LENSES PER MM. 2 L 7 2 4F RT A16WE 2001062600135 20010626 00135 NM 2001 6 26 SWAA011602 1 20010530 A 2612 6130766501 CONNECTOR BOEING 737 7372H4 138448C NM APU CORRODED A SWAA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 102SW 23108 (AIR TURNBACK) DURING FLIGHT, 5 MINUTES AFTER APU SHUT DOWN FIRE WARNING LIGHT ILLUMINATED. PERFORMED APU FIRE PROCEDUR E AND FIRED BOTTLE. WARNING LIGHT REMAINED ILLUMINATED AND HAD INTERMITTENT FIRE BELL. RETURNED TO MSY. FOUND CONNECT OR D4834 CORRODED/SHORTED. REMOVED AND REPLACED CONNECTOR & HARNESS. 2 L 7 2 4F A16WE 2001062600136 20010626 00136 NM 2001 6 26 SWAA011603 1 20010531 A 5330 6546546 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001062600137 20010626 00137 NM 2001 6 26 SWAA011604 1 20010531 A 2121 645405 FAN BOEING 737 7377H4 NM A/C BAY OVERHEATED A SWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 701GS 27836 DURING CRUISE FUMES ODOR IN COCKPIT AND FWD CABIN. TURNED OFF RECIRC FAN, AIR CLEARED. REMOVED AND REPLACED RECIRC FAN PER MM. 2 L 7 2 4F RT A16WE 2001062600138 20010626 00138 NM 2001 6 26 SWAA011605 1 20010531 A 7711 LG14C14 TRANSMITTER BOEING 737 7372H4 138448C NM NR 2 EPR ERRATIC A SWAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 07 067SW 22356 (ABORTED TAKEOFF) NR 2 EPR INDICATION ERRATIC DURING POWER INCREASE. REMOVED AND REPLACED NR 2 EPR TRANSMITTER PER MM. 2 L 7 2 4F A16WE 2001062600139 20010626 00139 NE 2001 6 26 DKAA01013 2 20010503 A 7200 ENGINE AMD FALC20 FALCOND 2720304 EU GE CF700 CF7002D2 30010 NE RIGHT FLAMED OUT A DKAA B EMER. DESCENT X ENGINE FLAMEOUT CL CLIMB 1 GL 23 226R 226 RIGHT ENGINE FLAME OUT DURING CLIMB IN TURBULENCE THROUGH FL390, 210 KTS IAS TEMP DROPPED TO 200 DEGREES C, ANTI-ICE, IG NITION OFF, 10 MINUTES UNTIL RELIGHT, OIL PRESSURE 20 PSI. RESTARTED ON FIRST TRY AT FL290. CHECKED RIGHT ENGINE FOR F OD AND CHECKED TURBINE AREA. OPENED COWLING INSPECTED EXTERNAL ENGINE. PERFORMED ENGINE START AND RUN-UP, ENGINE OPERA TED NORMALLY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F A7EU E7EA 2001062600140 20010626 00140 WP 2001 6 26 DKAA01015 1 20010526 A 3230 59151695512 LATCH DOUG DC9 DC915F 3022037 WP RT MLG DEFECTIVE A DKAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 23 915R 47015 RIGHT RED LIGHT ON MAIN GEAR WOULD NOT GO OUT WHEN RETRACTING THE GEAR IN FLIGHT (DEN). JACKED AIRCRAFT, FOUND MAIN GEA R DOOR LATCH CYLINDER DEFECTIVE, REPLACED RIGHT MAIN GEAR DOOR LATCH MECHANISM IAW DC9 MM 32-31-4, PERFORMED GEAR RETRAC TION AND LATCH TEST IAW DC9 MM 32-00, SYSTEM OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 2001062600141 20010626 00141 NM 2001 6 26 USAA010423 1 20010420 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 32200 24559 CLT - FOUND PRESSURE WEB WEB WITH TWO CRACKS .75 INCH LONG, BS 178 BULKHEAD, WL 201 RBL 5 AND LBL 5, WL 198 RBL 5. INST ALLED DOUBLER, EO 5300V153, SRM 53-10-08 FIG 211, EA 69273. (M) 2 L 7 2 4F RT A16WE 2001062600142 20010626 00142 WP 2001 6 26 CALA0100598 1 20010625 A 5330 SKIN DOUG DC9 DC982 3022082 WP FS 569 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND R/H FUSELAGE EXTERNAL SKIN DENTED AT FS 579 BETWEEN LONGERONS 20R AND 21R. A REPAIR DOUBLER WAS INSTALL ED IAW SRM 53-04, FIGURE 38. 2 L 7 2 4F A6WE 2001062600143 20010626 00143 WP 2001 6 26 CALA0100599 1 20010625 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 826-927 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND L/H O/B FLOOR PANEL CRACKED AROUND SCREW HOLES AT BOTH ENDS, STA 826-927. A DOUBLER WAS INSTALLED AT EA CH END IAW SRM 53-01, FIGURE 4 AND 51-10-3. 2 L 7 2 4F A6WE 2001062600144 20010626 00144 WP 2001 6 26 CALA0100600 1 20010625 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP PANEL "F" CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND CABIN FLOOR PANEL "F" CORRODED AROUND FASTENER HOLES. THE PANEL WAS REPLACED IAW SRM 53-21-0 AND 51-10- 3. 2 L 7 2 4F A6WE 2001062600145 20010626 00145 NM 2001 6 26 CALA0100601 1 20010625 A 5230 6546921528 DOOR BOEING 737 7373T0 1384582 NM FWD CARGO CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 63305 23356 INSPECTION FOUND TWO 4.5" CRACKS IN FORWARD CARGO DOOR AT LOWER AFT CORNER. THE FORWARD CARGO DOOR WAS REMOVED AND REPLA CED IAW MM 52-31-00. 2 L 7 2 4F RT A16WE 2001062600146 20010626 00146 NM 2001 6 26 CALA0100602 1 20010625 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM STA 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14358 23943 INSPECTION FOUND FLOORBEAM CORRODED AT STA 344, BL 0 TO LBL 59. THE FLOORBEAM WAS REMOVED AND A NEW FLOORBEAM WAS INSTAL LED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 2001062600147 20010626 00147 WP 2001 6 26 CALA0100603 1 20010625 A 5320 SHEAR TIE DOUG DC9 DC982 3022082 WP FS 370 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND A 1" CRACK IN FORWARD CARGO SHEAR TIE AT FS 370, LONGERON 22-23L. THE CRACKED AREA WAS REMOVED AND A RE PAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 7, 53-03, FIGURE 7, AND 51-10-3. 2 L 7 2 4F A6WE 2001062600148 20010626 00148 WP 2001 6 26 CALA0100604 1 20010625 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FS 200-214 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND MAIN CABIN WEB ATTACH ANGLE CORRODED AT FS 200-214, LBL 54. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS I NSTALLED IAW SRM 51-10-3 AND 51-30-5. 2 L 7 2 4F A6WE 2001062600149 20010626 00149 WP 2001 6 26 CALA0100605 1 20010625 A 5330 SKIN DOUG DC9 DC982 3022082 WP FS 389 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND L/H FUSELAGE EXTERNAL SKIN CREASED AND DENTED AT FS 389, LONGERON 22L. THE DAMAGED AREA WAS REFORMED AN D A DOUBLER WAS INSTALLED IAW SRM 51-10-2, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 2001062600150 20010626 00150 NM 2001 6 26 USAA010424 1 20010420 A 5313 STRINGER BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 3220 24559 CLT - FOUND STRINGER CRACKED 1 INCH, BS 1140 ABOVE STAB HINGE CUTOUT, S5L. INSTALLED REPAIR ANGLES, SRM 53-00-01, FIG 2 21. (M) 2 L 7 2 4F RT A16WE 2001062600151 20010626 00151 NM 2001 6 26 USAA010425 1 20010420 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 32200 24559 CLT - FOUND FRAME CRACKED .25 INCH, STATION 747 BETWEEN S8R AND S9R, AT A/C DIST SUPPORT BRACKET. INSTALLED DOUBLER, TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001062600152 20010626 00152 NM 2001 6 26 USAA010426 1 20010420 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 32200 24559 CLT - FOUND FRAME CRACKED .25 INCH, STATION 500A, BETWEEN S8L AND S9L. INSTALLED DOUBLER, TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001062600153 20010626 00153 NM 2001 6 26 USAA010427 1 20010420 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 32200 24559 CLT - FOUND PRESSURE WEB WITH TWO CRACKS 1 INCH AND .350 INCH, BS 178, WL 188, RBL .5 AND LBL .5. INSTALLED DOUBLER, EO 5300V153, SRM 53-10-08, EA 69273, EA 69321. (M) 2 L 7 2 4F RT A16WE 2001062600154 20010626 00154 NM 2001 6 26 01FDEA00496 1 20010626 A 5310 65163391 FRAME BOEING 727 727277 138408S NM BS 970 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 NR 613 CORROSION (C53-113-01(2)) ON SHEAR TIE BS 970, LBL 10, WL 138.5. ** S/D ** COMING 2 L 7 3 4F RT A3WE 2001062600155 20010626 00155 NM 2001 6 26 01FDEA00498 1 20010626 A 5751 SKIN BOEING 727 72722 1384002 NM RH OB AILERON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 N 501 DUR ROUTINE INSP RH OB AILERON IB LE SKIN FOUND CRACKED. ** S/D ** R&R BRACKET PER IAW BAC 727 SRM 51-30-2. 2 L 7 3 4F A3WE 2001062600156 20010626 00156 NM 2001 6 26 01FDEA00499 1 20010626 A 5720 BRACKET BOEING 727 72722 1384002 NM #8 FLAP TRACK CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 N 500 DUR ROUTINE INSP IB BRACKET ON THE #8 FLAP TRACK FOUND CRACKED. R&R & FAB BRACKET PER IAW BAC 727 SRM 51-20-1, 51 -30-2. 2 L 7 3 4F A3WE 2001062600157 20010626 00157 NM 2001 6 26 01FDEA00500 1 20010626 A 5313 SKIN BOEING 727 72722 1384002 NM BS 303.9 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 N 318 DUR ROUTINE INSP FUSELAGE SKIN FOUND CRACKED AT BS 303.9 AT STR 4L LWR FASTENER HOLE. R&R FASTENER PER IAW BAC 727 SRM 51-30-2. 2 L 7 3 4F A3WE 2001071200037 20010712 00037 NM 2001 7 12 01FDEA00501 1 20010626 A 3350 BATTERY BOEING 727 72722 1384002 NM PAX DOOR DISCHARGED A FDEA K NONE L NO TEST IN INSP/MAINT 1 SO 25 187FE 19079 DURING ROUTINE INSP FWD ENTRY DOOR EMERGENCY ESCAPE SLIDE LIGHT FOUND INOPERATIVE. *S/D* REMOVED AND REPLACED BATTERY PER IAW BAC 727 MM 33-50-121-2. 2 L 7 3 4F A3WE 2001062600158 20010626 00158 NM 2001 6 26 USAA010428 1 20010420 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 32000 24559 CLT - FOUND PRESSURE WEB CRACKED .300 INCH, BS 178, WL 206 RBL 1. DAMAGE CUT OUT, INSTALLED DOUBLER, EO 5300V153, SRM 5 3-10-08 FIG 211, EA 69321 AND EA 69273. (M) 2 L 7 2 4F RT A16WE 2001062600159 20010626 00159 NM 2001 6 26 USAA010429 1 20010420 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 32200 24559 CLT - FOUND PRESSURE WEB CRACKED .25 INCH, BS 178, WL 198, LBL 4.8. INSTALLED DOUBLER, EO 5300V153, SRM 53-10-08 FIG 21 1, EA 69321 AND EA 69273. (M) 2 L 7 2 4F RT A16WE 2001062600160 20010626 00160 NM 2001 6 26 USAA010430 1 20010420 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 32200 24559 CLT - FOUND PRESSURE WEB CRACKED .25 INCH, BS 178, WL 198 LBL 4.8. INSTALLED DOUBLER, EO 5300V153, SRM 53-10-08 FIG 211 , EA 69321 AND EA 69273. (M) 2 L 7 2 4F RT A16WE 2001062600161 20010626 00161 NM 2001 6 26 USAA010431 1 20010420 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 32200 24559 CLT - FOUND FLOORBEAM CORRODED 64 SQUARE INCHES, BS 947 LBL 16 TO RBL 16. UPPER T-CAP REPLACEMENT, SRM 53-60-02. (M) 2 L 7 2 4F RT A16WE 2001062600162 20010626 00162 NM 2001 6 26 USAA010432 1 20010420 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 32000 24559 CLT - FOUND SIDE CHORD CRACKED .5 INCH, BS 178, WL 207 LBL 26. CUTOUT DAMAGE, SPLICED IN REPAIR, EO 5300V157. (M) 2 L 7 2 4F RT A16WE 2001062600163 20010626 00163 NM 2001 6 26 USAA010433 1 20010420 A 5320 STIFFENER BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 24559 CLT - FOUND STIFFENER CRACKED .5 INCH BS 178,WL 184, LBL 5.7. INSTALLED REPAIR KIT, EO 5300V155. (M) 2 L 7 2 4F RT A16WE 2001062600164 20010626 00164 NM 2001 6 26 USAA010434 1 20010420 A 5320 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 32200 24559 CLT - FOUND ANGLE CRACKED 1 INCH, BS 294.5 FUSELAGE CUTOUT FOR FORWARD GALLEY SERVICE DOOR. INSTALLED REPAIR DOUBLER PE R SRM 51-70-11. (M) 2 L 7 2 4F RT A16WE 2001062600165 20010626 00165 NM 2001 6 26 USAA010436 1 20010420 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 47122 22953 CLT - FOUND INTERNAL SKIN CRACKED .5 INCH, BS 947, STRINGER 11L AT AFT ENTRY DOOR. INSTALLED FILLER AND DOUBLER, EA 693 62 ALLOWS 737-200 TR 53-30-07A. (M) 2 L 7 2 4F RT A16WE 2001062600166 20010626 00166 NM 2001 6 26 USAA010437 1 20010420 A 5320 STRAP BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 47122 22953 CLT - FOUND STRAP CRACKED, AFT SERVICE DOOR, UPPER HINGE FUSELAGE CUTOUT, STRINGER 11R. INSTALLED FILLER AND DOUBLER, E A 69362 AND 737-200 TR 53-30-07A. (M) 2 L 7 2 4F RT A16WE 2001062600167 20010626 00167 NM 2001 6 26 USAA010438 1 20010420 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 47122 22953 CLT - FOUND FLOORBEAM T-CAP CORRODED, 3 INCHES BY 25 INCHES, BS 967, LBL 17 TO LBL 50. REMOVED AND REPLACED T-CAP, SRM 53-00-51 AND EA 96458. (M) 2 L 7 2 4F RT A16WE 2001062600168 20010626 00168 NM 2001 6 26 USAA010439 1 20010420 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 47122 22953 CLT - FOUND FUSELAGE SKIN .25 INCH CRACK, AFT ENTRY DOOR FUSELAGE CUTOUT, UPPER HINGE. INSTALLED REPAIR DOUBLER SRM 53- 60-01. (M) 2 L 7 2 4F RT A16WE 2001062600169 20010626 00169 NM 2001 6 26 USAA010441 1 20010420 A 5320 TIE CLIP BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 47122 22953 CLT - FOUND TIE CLIP CORRODED 1 INCH BY .75 INCH AREA, STATION 1016, STRINGER 27R. REMOVED AND REPLACED TIE CLIP, SRM 5 1-10-02. (M) 2 L 7 2 4F RT A16WE 2001062600170 20010626 00170 NM 2001 6 26 USAA010442 1 20010420 A 5320 ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 47122 22953 CLT - FOUND Z-ANGLE CORRODED APPROXIMATELY 61 INCHES, STATION 947.5 TO 1006, LBL 53. REMOVED AD REPLACED Z-ANGLE, SRM 5 1-10-02. (M) 2 L 7 2 4F RT A16WE 2001062600171 20010626 00171 NM 2001 6 26 AWXA0001903 1 20010626 A 5311 65C8073525 TEE CHORD BOEING 737 7373G7 1384595 NM CROSS BEAM CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 307AW 24634 D: Fwd Cargo Door Lower: Cross Beam Cracked, Top Side, Thru 5th Fastner Hole Common to Tee Chord Fwd End.C: Repaired IAW E.O 52-31-04 pg 17-36 2 L 7 2 4F RT A16WE 2001062600172 20010626 00172 NM 2001 6 26 AWXA0001904 1 20010626 A 5315 65C8073525 TEE CHORD BOEING 737 7373G7 1384595 NM TEE CHORD CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 307AW 24634 D: Fwd Cargo Door Lower Cross Beam Cracked Aft End.C: Repaired IAW E.O 52-31-04 Pg 17-36 2 L 7 2 4F RT A16WE 2001062600173 20010626 00173 NM 2001 6 26 AWXA0001906 1 20010626 A 5311 65C8073525 TEE CHORD BOEING 737 7373G7 1384595 NM TEE CHORD CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 307AW 24634 D: Fwd Cargo Door Lower Cross Beam Tee Chord Cracked At Fwd End in 3rd Fastener.C: Repaired IAW E.O 52-31-04 Pg 17-36 2 L 7 2 4F RT A16WE 2001062600174 20010626 00174 NM 2001 6 26 AWXA0001899 1 20010626 A 5713 6545767 STRINGER BOEING 737 7373G7 1384595 NM STR16L/BS500C CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 307AW 24634 D: STR 16L (Left side) Cracked Just Fwd of L/E Wing Light ReceplacleC: Repaired IAW S/B 737-53-1145 2 L 7 2 4F RT A16WE 2001062600175 20010626 00175 NM 2001 6 26 AWXA0001905 1 20010626 A 5320 6546551 SHEAR TIE BOEING 737 7373G7 1384595 NM TIES/BS 807 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 307AW 24634 D: Aft Cargo - 2 EA. Shear Ties Cracked @ BS 807 Between STR 27L and 27RC: Repaired IAW B737-300 SRM 53-00-02 Fig 203 Pg 207 2 L 7 2 4F RT A16WE 2001062600176 20010626 00176 NM 2001 6 26 USAA010443 1 20010424 A 5310 CREASE BEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 22953 CLT - FOUND CREASE BEAM WEB CORRODED .5 INCH AREA, STATION 639, STRINGER 17R. REMOVED AND REPLACED WEB, SRM 51-10-2. ( M) 2 L 7 2 4F RT A16WE 2001062600177 20010626 00177 NM 2001 6 26 USAA010444 1 20010424 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 47122 22953 CLT - FOUND SIDE CHORD CRACKED .5 INCH, BS 178, WL 207, FAR LEFT SIDE. DAMAGE CUTOUT, SPLICED IN REPAIR PER EO 5300V157 . (M) 2 L 7 2 4F RT A16WE 2001062600178 20010626 00178 NM 2001 6 26 DL76L010913 1 20010604 A 2120 732591F FAN 732591F BOEING 767 767332 1382001 NM FWD EQUIP EXH FAULTY A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 199DN 4548A 28456 SMOKE IN COCKPIT. ALSO GOT FWD EQ EXH FAN STATUS MSG WITH POPPED CB. WENT TO OVRD ON EQUIP COOLING AND SMOKE DISSIPATED. ON LANDING GOT NO COOLING LIGHT AND WENT TO STBYSUSPECT FWD EQ EXH FAN BURNED OUT. FWD TO MCO. OPERATE PER MEL 21-58-04B. REPLACED FWD EQ EXHAUST FAN. OPS CHK NORMAL. MCO REMOVED ON OFF A 211002542 3826 4548A ETOPS CATEGORY 'B': DIVERSION OR TURNBACK 2 L 7 2 4F RT A1NM 2001062600179 20010626 00179 NM 2001 6 26 DL757010918 1 20010605 A 2560 BPS73 POWER SUPPLY BOEING 757 757232 1384965 NM CABIN CEILING FAILED A DALA O OTHER O OTHER IN INSP/MAINT 1 SO 27 639DL 23993 ON A-CHECK FOUND FWD ENTRY DOOR EMERGENCY LITE INOP REPLACED POWER SUPPLY-OPS OK 2 L 7 2 4F RT A2NM 2001062600180 20010626 00180 NM 2001 6 26 DLM88010920 1 20010606 A 5730 3075100 PANEL DOUG MD88 MD88 3023688 NM LEFT UPPER DELAMINATED A DALA K NONE D INFLIGHT SEPARATION CR CRUISE 1 SO 27 978DL 53259 LT. OVER WING ACCESS PANEL DELAMINATED AND TORN - REPLACED SAME 2 L 7 2 4F RT A6WE 2001062600181 20010626 00181 WP 2001 6 26 DLL10010943 1 20010610 A 3350 5165741 POWER SUPPLY LKHEED 1011 10113851 5265010 WP CABIN LOW A DALA O OTHER O OTHER IN INSP/MAINT 1 SO 27 730DA 193C1199 TRACK LIGHTING INOP IN E ZONE-REPLACED POWER SUPPLY 2 L 7 3 4F A23WE 2001062600182 20010626 00182 NM 2001 6 26 DL72S010948 1 20010612 A 5330 655457116 SKIN BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 532DA 22045 A CRACK WAS FOUND IN THE STR 26L LAP JOINT BETWEEN FS 620 AND 640. THE CRACK WAS REMOVED AND REPIARED PER SRM 53-30-3, FIGURE 5. THE DAMAGE WAS FOUND AT HMV. 2 L 7 3 4F A3WE 2001062600183 20010626 00183 NM 2001 6 26 DL73K010950 1 20010612 A 5311 6546594502 FRAME BOEING 737 737232 1384475 NM FRAME CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 320DL 23092 CORROSION WAS FOUND ON THE LOWER LOBE FRAME AT FS 500B ON THE INBOARD FLANGE JUST OUTBOARD OF STR 27R. THE DAMAGE WAS TRIMMED AWAY AND A FACTORY SPLICE WAS EXTENDED TO REPAIR THEDAMAGE. THE REPAIR WAS ACCOMPLISHED AT HMV. 2 L 7 2 4F RT A16WE 2001062600184 20010626 00184 NM 2001 6 26 DL738010957 1 20010612 A 3600 1074925 CONTROLLER BOEING 737 737832 13844CF NM LT ENG FAILED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 394DA 7537 30562 IRR/ NBR 1 ENG BLEED TRIP OFF LIGHT ILLUMINATED AS A/C LEVELED OF FL350. REPLACED BLEED AIR CONTROLLER 2 L 7 2 4F RT A16WE 2001062600185 20010626 00185 NE 2001 6 26 DL76G010960 2 20010613 A 7200 CF680C2B6 ENGINE BOEING 767 7673P6 1385105 NM GE CF6 CF680C2B6 30025 NE #2 ENGINE FAILED A DALA E ENGINE SHUTDOWN Y ENGINE STOPPAGE AP APPROACH 1 SO 27 155DL 34749 25269 695476 SHIP 1505 FLT 107/13 FRA/JFK AT FL4K CAPT ATTEMPTED A LVL CHANGE AT FL4K RT ENG DID NOT RESPOND. THROTTLE BACK TO IDLE THE EGT CONTINUED TO CLIMB TO 895 THE ENG WAS SHUT DOWN./C MTC FOUND METAL IN TAIL PIPE. /C REPLACED THE ENG. ETOPS CATEGORY 'A': ANY IN-FLIGHT SHUTDOWN 2 L 7 2 4F 4 F RT A1NM E13NE 2001062600186 20010626 00186 NM 2001 6 26 DL73K010965 1 20010614 A 5321 6545808172 BEAM BOEING 737 737232 1384475 NM CABIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 320DL 23092 A CRACK WAS FOUND IN THE FS 294.5 FLOOR BEAM IN THE UPPER CAP SIMILIAR TO THAT FOUND IN S/B 737-53-1090. A SECTION OF THE UPPER CAP WAS REPLACED PER ERA 397624-14AD AT HMV. 2 L 7 2 4F RT A16WE 2001062600187 20010626 00187 NM 2001 6 26 DL72S010967 1 20010614 A 2750 FLAP BOEING 727 727232 1384082 NM INBD STUCK A DALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 27 524DA 21584 INBD FLAPS WONT RETRACT STUCK AT 15 DEGREES - LUBED AND RAN FLAPS - UNABLE TO DUPLICATE 2 L 7 3 4F A3WE 2001062600188 20010626 00188 NM 2001 6 26 DLM88010969 1 20010612 A 5330 593666751 SKIN DOUG MD88 MD88 3023688 NM FS 1287, L-30 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DE 49967 FUSELAGE / SKIN / FS 1287 / L-30 : DENT CUTOUT REPAIR THE FUSELAGE SKIN WAS DENTED BY GROUND EQUIPMENT AT FS 1287 AND LONGERON 30. THE DAMAGED AREA OF SKIN WAS REMOVED WITH A 14" X 22.25" SKIN CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 381018-14, REV B. 2 L 7 2 4F RT A6WE 2001062600189 20010626 00189 NM 2001 6 26 DLM88010970 1 20010612 A 5330 593666751 SKIN DOUG MD88 MD88 3023688 NM FS 1250, L-29L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DE 49967 FUSELAGE / SKIN / FS 1250 / L-29L : DENT CUTOUT REPAIR THE FUSELAGE SKIN WAS DENTED BY GROUND EQUIPMENT AT FS 1250 AND LONGERON 29L. THE DENTED AREA WAS REMOVED WITH A 16.1" X 20.1" CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 381017 -14, REV B. 2 L 7 2 4F RT A6WE 2001062600190 20010626 00190 NM 2001 6 26 DL73K010976 1 20010615 A 5311 6546541504 FRAME BOEING 737 737232 1384475 NM CABIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 320DL 23092 CRACKS WERE FOUND IN THE FS 663.75 FRAME AT STR 3R, 1, 2L AND 3L. THE CRACKS WERE CUT OUT AND THE FRAME WAS REPAIRED PER SRM 53-10-4, FIGURE 14. THE FUSELAGE SKIN WAS CUT LOCALLY FOR ACCESS. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001062600191 20010626 00191 NM 2001 6 26 DL76G010978 1 20010613 A 5330 146T35308002 SKIN BOEING 767 767332 1382001 NM FS 1373, S-27R DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 16065 30199 FUSELAGE / SKIN ASSY / FS 1373 / STRG. 27R : GROUND DAMAGE REPAIR THE FUSELAGE SKIN WAS BADLY DENTED BY GROUND EQUIPMENT AT FS 1373 NEAR STRINGER 27R. AN UNDERLYING FRAME SHEAR CLIP AND INTERCOSTAL WERE ALSO DAMAGED. THE SKIN DAMAGE WAS REMOVED WITH A 3.5" X 5" CUTOUT AND THE DAMAGED PARTS WERE REMOVED AND REPLACED. THE SKIN CUTOUT WAS REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS PER ER/A 381060-14. 2 L 7 2 4F RT A1NM 2001062600192 20010626 00192 NM 2001 6 26 DL76S010981 1 20010614 A 2750 285T004953 FSEU BOEING 767 767332 1382001 NM MAIN E/E COMPART SHORTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 128DL 24078 AT LEVEL OFF GOT FLAP/SLAT ELEC MESSAGE C/B P11G16 POPPED SMOKE IN COCKPIT. FOUND FLAP/SLAT ELECTRONICS UNIT HAD A TRANS FORMER THAT HAD OVERHEATED. REPLACED THE FLAP / SLAT ELECTRONICS UNIT AND TESTED PER MAINT MANUAL. OPERATED FLAPS IN ALT ERNATE AND NORMAL MODES ALL CHKS OK. 2 L 7 2 4F RT A1NM 2001062600193 20010626 00193 NM 2001 6 26 DLM88010990 1 20010614 A 3240 MD88M TRANSDUCER DOUG MD88 MD88 3023688 NM #2 MAIN FAILED A DALA K NONE G MULTIPLE FAILURE LD LANDING 1 SO 27 909DL 49540 LANDED WITH AUTOBRAKES SELECTED MAX- VREF WAS 131 AND A/C LANDED ON SPEED IN THE TOUCHDOWN ZONE- AUTOBRAKES SEEMED TO ENGAGE NORMAL BUT AS THE BRAKES WERE SELECTED TO MED BOTH LEFT MAIN TIRES BLEW. REPLACED #2 ANTI-SKID TRANSDUCER 2 L 7 2 4F RT A6WE 2001062600194 20010626 00194 NM 2001 6 26 DL75A011001 1 20010615 A 5310 148N23011 BULKHEAD BOEING 757 757212 NM FS 1720, BL 0 GOUGED A DALA K NONE O OTHER LD LANDING 1 SO 27 750AT 23126 FUSELAGE / SKIN & BULKHEAD / FS 1700-1780 / STRG. 26L-26R : GROUND DAMAGE REPAIR THE FUSELAGE SKIN FWD AND AFT OF THE FS 1720 BULKHEAD WAS GOUGED AND PUNCTURED FROM A TAIL STRIKE DURING LANDING. THE BULKHEAD WEB WAS SLIGHTLY BUCKLED AND THE LOWER CHORDS GOUGED. THE DAMAGE TO THE SKIN AND WEB WAS CUTOUT AND REPAIRED WITH ALUMINUM DOUBLERS. THE DAMAGE TO THE CHORD WAS REPAIRED WITH A STEEL STRAP. THE REPAIRS ARE INTERIM UNTIL PART REPLACEMENT AT HMV PER ER/A 381027-14, REV A. 2 L 7 2 4F RT A2NM 2001062600195 20010626 00195 NM 2001 6 26 DL757011002 1 20010615 A 5330 146N3700 SKIN BOEING 757 757232 1384965 NM FS 1681, S-20R PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 687DL 27586 FUSELAGE / SKIN / FS 1681 / STRG. 19R-22R : GROUND DAMAGE CUTOUT REPAIR THE FUSELAGE SKIN WAS STRUCK BY GROUND EQUIPMENT AT FS 1681 BETWEEN STRINGERS 19R & 22R. THE DAMAGE WAS REMOVED WITH A 6" X 15" CUTOUT. THE CUTOUT WAS REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS INSTALLED PER ER/A 381061-14, REV A. 2 L 7 2 4F RT A2NM 2001062600196 20010626 00196 NM 2001 6 26 DL757011005 1 20010615 A 7100 PW2037 ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE #2 ENGINE UNSERVICEABLE A DALA E ENGINE SHUTDOWN X ENGINE FLAMEOUT CL CLIMB 1 SO 27 614DL 30037 22821 716590 17,000 FT LOUD BANG AND BUFFET NBR 2 ENGINE ROLL BACK AND EGT WENT WELL INTO RED. SMOKE RECORDED IN CABIN._C/A REPLACE ENGING 2 L 7 2 4F 4 F RT A2NM E17NE 2001062600197 20010626 00197 NM 2001 6 26 DL72S011017 1 20010530 A 5311 FRAME BOEING 727 727232 1384082 NM #2 ENG COWL WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 532DA 22045 AT HMV FOUND FRAME WORN STA.1342 6,O-CLOCK POSITION FRAME FOR FWD END OF #2 ENG COWL'S. CORR: REMVD DAMAGE PER MM 53-11-000-8,FABD REPAIR ANGLE PER MM 53-11-000-8,2054-0-.071,DRILLED DOUBLER PER MM 53-11-000- 8,FABD FILLER,OK INSTL REPAIR,T/P PER PS 2-4-1 #2,INSTLD DBLER PER MM 53-11-000-8. 2 L 7 3 4F A3WE 2001062600198 20010626 00198 NM 2001 6 26 DL72W011020 1 20010620 A 5530 SKIN BOEING 727 727247 138408F NM R/H VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 293WA 22111 LWR END OF VERT STAB SKIN CRACKED R/H SIDE STA 1342 REPAIR PER M/M 55-30-000-8 FIG 801 2 L 7 3 4F A3WE 2001062600199 20010626 00199 NM 2001 6 26 DL777011029 1 20010621 A 2430 263BA1012 BATTERY BOEING 777 777232 1385232 NM BULK BIN UNSERVICEABLE A DALA O OTHER O OTHER CR CRUISE 1 SO 27 861DA 29952 APU STATUS MSG APU BATTERY.APU CHARGER.ADDITIONAL APU BATTERY OVERHEAT.OVERHEAT WENT AWAY VOLTS APU BATTERY DOWN TO 19V STEADY 1 AMP DISCHARGE__T/S PER FIM R AND R APU BATTERY AND APU BATTERY CHARGER PER FIM STATUS MESSAGE CLEARED CHECKS OK ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS 2 L 7 2 4F RT T00001SE 2001062600200 20010626 00200 NM 2001 6 26 DL72S011035 1 20010622 A 5314 65C139131 SKIN BOEING 727 727232 1384082 NM SKIN CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 532DA 22045 THE FUSELAGE SKIN AND STRINGER WERE FOUND CORRODED AT FS 950E AND STR 29R. THE STRINGER WAS CUT AT FS 950D +10 AND REMOVED TO THE AFT END OF THE PART. A NEW SECTION WAS SPLICED IN. AN EXTERNAL DOUBLER AND TRIPLE WERE USED TO REPAIR THE SKIN. THE DAMAGE WAS FOUND AT HMV. 2 L 7 3 4F A3WE 2001062600201 20010626 00201 NM 2001 6 26 DL72S011036 1 20010622 A 5330 65C139132 SKIN BOEING 727 727232 1384082 NM SKIN CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 532DA 22045 THE FUSELAGE SKIN WAS FOUND TO BE CORRODED AT FS1009 BETWEENSTR 29L AND 28R. THE SKIN WAS REPAIRED SIMILIAR TO THAT OF SRM 53-30-3, FIGURE 3A. THE DAMAGE WAS FOUND AT HMV. 2 L 7 3 4F A3WE 2001062600202 20010626 00202 NM 2001 6 26 DL733011038 1 20010621 A 5330 65458001128 SKIN BOEING 737 737301 1384611 NM FS 280, S-20R PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 948WP 23259 FUSELAGE / SKIN / FS 277-295 / STRG. 19R-20R : GROUND DAMAGE CUTOUT REPAIR THE FUSELAGE SKIN BETWEEN FS 277 & 295 AT STRINGERS 19R & 20R WAS STRUCK BY GROUND EQUIPMENT RESULTING IN A PUNCTURE AND SEVERAL DENTS AND GOUGES. THE DAMAGE AREA WAS REMOVED WITH A 19" X 10" CUTOUT. THE CUTOUT WAS REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS PER ER/A 381091-14, REV A. 2 L 7 2 4F RT A16WE 2001062600203 20010626 00203 NM 2001 6 26 DL73K011051 1 20010624 A 2400 BACC18R15B CIRCUIT BREAKER BOEING 737 737232 1384475 NM P6-12 BURNED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 311DL 23083 SMOKE IN COCKPIT FOUND LEFT SIDE WINDOW ANTI-ICE C/B C392 AND C848 STANBY HYD PUMP ALTERNATE C/B BURNED 2 L 7 2 4F RT A16WE 2001062600204 20010626 00204 NM 2001 6 26 C1HA200181006 1 20010622 A 3150 10507724 WARNING SYSTEM BOEING 727 7272S7 138407Z NM ONLY FAILED A C1HA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 GL 15 681CA 22020 During taxi out from DFW while performing taxi checks flight control warning test would not work returned to gate.ACTION TAKEN:R&R'd audio control box ops check OK per MM 2 L 7 3 4F A3WE 2001062600205 20010626 00205 NM 2001 6 26 C1HA200185006 1 20010618 A 3350 900542 POWER SUPPLY BOEING 727 7272S7 138407Z NM RIGHT AFT FAILED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 685CA 22492 Emergency light above R-2 door inop.ACTION TAKEN:R&R'd emergency light power supply. 2 L 7 3 4F A3WE 2001062600206 20010626 00206 NM 2001 6 26 C1HA200185007 1 20010622 A 2611 824PY SMOKE DETECTOR BOEING 727 7272S7 138407Z NM FWD LAV FAILED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 685CA 22492 Fwd lav smoke detector inop.ACTION TAKEN:R&R'd fwd lav smoke detector. 2 L 7 3 4F A3WE 2001062600207 20010626 00207 NM 2001 6 26 C1HA200186006 1 20010622 A 2612 CONNECTOR BOEING 727 7272S7 138407Z NM FAULTY A C1HA O OTHER L NO TEST NR NOT REPORTED 1 GL 15 686CA 22021 APU fire system will not test.ACTION TAKEN:Replaced connector at sensor responder checks good. 2 L 7 3 4F A3WE 2001062600208 20010626 00208 NM 2001 6 26 EVA001 1 20010626 A 2730 65B5730006 BALANCE WEIGHT BOEING 747 74745E 1384947 NM DETACHED W QOCF K NONE O Z OTHER SIGNIFICANT FAILURE REPORT UK UNKNOWN 1 WP 03 405EV 38061 27142 1. DURING C10 CHECK FOUND R/H HORIZONTAL STABLIZER PANEL BROKEN.2. AFTER INSPECTION FOUND R/H OUTBOARD ELEVATOR SUPPORT RIBS OF BALANCE WEIGHT FALLING DOWN AND DAMAGED TO THE ELVATOR PANEL.3. REPLACE THE R/H OUTBOARD ELEVATOR PER BOEING AMM 27-31-01.CONDITION BACK TO NML. 2 L 7 4 4F RT A20WE 2001062700001 20010627 00001 EU 2001 6 27 SIMA20010922 1 20010402 A 7100 7239060503 CTOT PANEL SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 21 243AE 340B243 ALB - FLT 4893 - ABORTED TAKEOFF DUE TO NO APR ON LEFT ENGINE. REMOVED AND REPLACED CTOT PANEL WITH SERVICEABLE PANEL R EF S340AMM 71-00-00 CHECKED GOOD REF AMM 76-10-00 APR SYSTEM CHECKS NORMAL. (M) 2 L 7 2 4T RT A52EU 2001062700002 20010627 00002 EU 2001 6 27 USAAF01031 1 20010531 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU PAX CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 886US 11346 RDU - THE AFT CABIN AND LAVATORY EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY IN THE AFT EMERGENCY LIGHTS BATTERY PACK. OPS CHECKED OK. (M) 2 L 7 2 4F RT 2001062700003 20010627 00003 EU 2001 6 27 USAAF01032 1 20010606 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU PAX CABIN FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 899US 11399 RIC - FOUND NR 6 CEILING AND LAVATORY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE NR 8 BATTERY PACK. OPERAT IONALLY CHECKED OK. (M) 2 L 7 2 4F RT 2001062700004 20010627 00004 EU 2001 6 27 SIMA200114801 1 20010528 A 5300 72111211000 DETECTOR SAAB SF340 340B 7860101 EU INOPERATIVE A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 307AE 340B307 JFK - FLT 5113 - CREW REPORTED SMOKE INDICATION IN COCKPIT. FIRE BOTTLE WAS USED AND AIRCRAFT WAS RETURNED TO JFK. MAI NTENANCE REMOVED AND REPLACED FORWARD CARGO SMOKE DETECTOR IAW SAAB MM 26-13-10 OPERATIONAL CHECK WAS GOOD. FIRE BOTTLE WAS REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001062700005 20010627 00005 EU 2001 6 27 SIMA200114314 1 20010523 A 2600 2313M4082 CONVERTER SAAB SF340 340B 7860101 EU RT ENGINE FAILED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 345SB 340B345 ALB - FLT 5092 - RIGHT TAIL PIPE HOT LIGHT. REMOVED AND REPLACED CONVERTER AND TAIL PIPE SENSORS IAW AMM. OPS CHECK GO OD. (M) 2 L 7 2 4T RT A52EU 2001062700006 20010627 00006 SO 2001 6 27 SIMA200114809 1 20010528 A 3600 A7257226 O-RING EMB 145 EMB145LR SO WORN A SIMA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SW 21 609AE 145069 ORD - FLT 4112 - CREW REPORTED ENGINE TWO BLEED LEAK LIGHT CAME ON AFTER TAKEOFF. CREW RETURNED AIRCRAFT TO ORD. MAINT ENANCE REPLACED O-RINGS AT COUPLING UNDER AFT PASSENGER SEAT NEAR THE LAVATORY. OPS CHECK WAS GOOD AND AIRCRAFT WAS RET URNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001062700007 20010627 00007 SO 2001 6 27 SIMA200114310 1 20010521 A 5300 AL2024T3 SKIN EMB 135 EMB135LR SO CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 701MH 145162 ABI - DURING MBV MAINTENANCE, FOUND CORROSION IN THE OMEGA BEAM. MAINTENANCE REPAIRED OMEGA BEAM IAW EMB SRM 53-21-10. (M) 2 L 7 2 4F RT TOOO11AT 2001062700008 20010627 00008 SO 2001 6 27 SIMA200114311 1 20010521 A 5300 AL2024T3 SKIN EMB 135 EMB135LR SO CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 701MH 145162 ABI - DURING MBV INSPECTION, MAINTENANCE FOUND THE FORWARD GALLEY DIGITAL CORRODED. MAINTENANCE REPAIRED THE GALLEY DIG ITAL IAW EMB REPAIR STATEMENT GST-1630/01. (M) 2 L 7 2 4F RT TOOO11AT 2001062700009 20010627 00009 SO 2001 6 27 SIMA200114312 1 20010521 A 5300 AL2024T3 SKIN EMB 135 EMB135LR SO CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 701MH 145162 ABI - DURING MBV INSPECTION, MAINTENANCE FOUND THE AFT GALLEY DIGITAL TO BE CORRODED. MAINTENANCE REPAIRED AFT GALLEY D IGITAL IAW EMB GST 1630/01. (M) 2 L 7 2 4F RT TOOO11AT 2001062700010 20010627 00010 2001 6 27 SIMA20011426 4 20010522 A 3441 4980100V1 RADOME EMB 135 EMB135LR SO A SIMA D RETURN TO BLOCK S AFFECT SYSTEMS CL CLIMB 1 SW 21 708AE 145205 ORD - FLT 4237 - CREW REPORTED THAT AFTER FLYING THROUGH PRECIPITATION, WEATHER RADAR DISPLAYED ARC OF PRECIPITATION THA T WS NOT THERE. CREW RETURNED AIRCRAFT TO ORD FOR MAINTENANCE. MAINTENANCE REMOVED AND REPLACED THE RADOME IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001062700011 20010627 00011 EU 2001 6 27 SIMA20011291 1 20010403 A 5300 7253814437 FRAME SAAB SF340 340B 7860101 EU FS 640 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 339SB 340B339 DURING MBV MAINTENANCE, FOUND FRAME 640 TO HAVE DAMAGE ON THE RIGHT SIDE ABOVE WL 73.5. MAINTENANCE REMOVED AND REPLACE D FRAME IAW SAAB MM. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001062700012 20010627 00012 EU 2001 6 27 SIMA20011312 1 20010510 A 3200 AIR843502 DRAG BRACE SAAB SF340 340B 7860101 EU NOSE GEAR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 280AE 340B280 SBP - DURING MBV INSPECTION, MAINTENANCE FOUND THE NOSE LANDING GEAR RIGHT TRUNNION BUSHING CORRODED. REMOVED AND REPLA CED DRAG BRACE IAW SAAB AMM 32-21. (M) 2 L 7 2 4T RT A52EU 2001062700013 20010627 00013 NM 2001 6 27 USAA010445 1 20010424 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 47122 22953 CLT - FOUND SIDE CHORD CRACKED .5 INCH, BS 178, WL 207 FAR RIGHT SIDE. DAMAGE CUTOUT, SPLICED IN REPAIR PER EO 5300V157 AND SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001062700014 20010627 00014 EU 2001 6 27 SIMA20011313 1 20010510 A 3200 AIR127292 TRUNNION SAAB SF340 340B 7860101 EU NOSE GEAR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 280AE 340B280 SBP - DURING MBV MAINTENANCE, FOUND THE NOSE LANDING GEAR DRAG BRACE RIGHT TRUNNION PIN CORRODED. REMOVED AND REPLACED NOSE LANDING GEAR DRAG BRACE IAW SAAB AMM 32-21. (M) 2 L 7 2 4T RT A52EU 2001062700015 20010627 00015 EU 2001 6 27 SIMA20011314 1 20010510 A 5300 7253721439 WEB SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 280AE 340B280 SBP - DURING MBV INSPECTION, MAINTENANCE FOUND THE WEB REINFORCEMENT BETWEEN FS 288 AND FS 294 HAS LARGE AREA OF CORROSI ON ON LEFT SIDE. REMOVED AND REPLACED WEB IAW SAAB SRM 51-40-21. (M) 2 L 7 2 4T RT A52EU 2001062700016 20010627 00016 EU 2001 6 27 SIMA20011315 1 20010510 A 5300 7253710871 TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 280AE 340B280 SBP - DURING MBV INSPECTION, MAINTENANCE FOUND AIRSTAIR TRACK HAS AREAS OF CORROSION. REMOVED AND REPLACED AIRSTAIR TRA CK IAW SAAB SRM 51-40-21 AND 51-24-50. (M) 2 L 7 2 4T RT A52EU 2001062700017 20010627 00017 NM 2001 6 27 USAA010446 1 20010424 A 5510 ANGLE BOEING 737 7373B7 1384580 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 47122 22953 CLT - FOUND GUSSET/ANGLE CRACKED, HORIZ STAB CENTER SECTION, LEFT, THRUST BEAM INBOARD LOWER CHORD. INSTALLED DOUBLER P ER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 2001062700018 20010627 00018 NM 2001 6 27 USAA010454 1 20010425 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 515AU 44427 23701 FOUND FUSELAGE SKIN CRACKED .25 INCH, BS 360, LOWER BELLY, BL 0. INSTALLED DOUBLER PER TYPICAL REPAIR 53-30-07. (M) 2 L 7 2 4F RT A16WE 2001062700019 20010627 00019 NM 2001 6 27 USAA010456 1 20010425 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 428US 33281 24550 CLT - FOUND BULKHEAD WEB WITH CRACKS RANGING IN SIZE FROM .250 INCH TO .800 INCH, BS 178, WL 188 TO 212, RBL 7 TO LBL 6. 5. INSTALLED REPAIR DOUBLER PER EO 5300V153. (M) 2 L 7 2 4F RT A16WE 2001062700020 20010627 00020 NM 2001 6 27 USAA010457 1 20010425 A 5320 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 428US 33194 24550 CLT - FOUND SIDE CHORD ANGLE WITH TWO CRACKS .625 ON LEFT, .5 ON RIGHT, BS 178, WL 207, LEFT AND RIGHT SIDE CHORD. REMO VED DAMAGED SECTIONS ON LEFT AND RIGHT SIDE, SPLICED IN NEW CHORD SECTIONS PER EO 5300V157. (M) 2 L 7 2 4F RT A16WE 2001062700021 20010627 00021 NM 2001 6 27 USAA010459 1 20010425 A 5320 ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 47122 22953 CLT - FOUND ANGLE DENTED .75 INCH BY .75 INCH, BS 639, LBL 68 AT CREASE BEAM WEB. FABRICATED AND INSTALLED NEW ANGLE PE R BOEING DRAWING 69-37422, SRM 51-30-01, 51-40-00 AND 51-40-03. (M) 2 L 7 2 4F RT A16WE 2001062700022 20010627 00022 NM 2001 6 27 USAA010460 1 20010425 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 47122 22953 CLT - FOUND FRAME/DOUBLER CRACKED .5 INCH, BS 1104 FRAME AFT SIDE, FORWARD LOWER LEFT HORIZONTAL STABILIZER FIT. INSTAL LED REPAIR DOUBLER, FILLERS, SHIMS PER EA 69484 AND SRM 51-70-11. (M) 2 L 7 2 4F RT A16WE 2001062700023 20010627 00023 NM 2001 6 27 USAA010461 1 20010425 A 5320 TIE CLIP BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 47122 22953 CLT - FOUND TIE CLIP CRACKED .5 INCH, BS 1104, S5R. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001062700024 20010627 00024 NM 2001 6 27 USAA010462 1 20010425 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 47122 22953 CLT - FOUND FORMER CORRODED 1.5 INCH BY 1 INCH AREA, BS 1016, FRAME BL 0, UNDER FLOOR. INSTALLED REPAIR PLATE, FILLER P ER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2001062700025 20010627 00025 NM 2001 6 27 USAA010463 1 20010425 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 47122 22953 CLT - FOUND FORMER CORRODED 1.5 INCH BY 1 INCH, BS 1016, L SIDE OF PRESSURE BULKHEAD BL-0. INSTALLED REPAIR PLATE AND F ILLER PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2001062700026 20010627 00026 NM 2001 6 27 USAA010464 1 20010425 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 47122 22953 CLT - FOUND PRESSURE WEB CORRODED 5.5 INCHES BY 1.5 INCHES, BS 1016, BL 0. INSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F RT A16WE 2001062700027 20010627 00027 NM 2001 6 27 USAA010465 1 20010425 A 5320 ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 47122 22953 CLT - FOUND FAIL/SAFE ANGLE CORRODED .5 INCH BY .5 INCH, BS 767, BETWEEN S27L AND S26L. INSTALLED REPAIR DOUBLER PER SR M 51-20-01, 51-70-11, AND 53-00-07. (M) 2 L 7 2 4F RT A16WE 2001062700028 20010627 00028 NM 2001 6 27 USAA010466 1 20010425 A 5510 GUSSET BOEING 737 7373B7 1384580 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 47122 22953 CLT - FOUND GUSSET/FITTING CRACKED .5 INCH, HORIZONTAL STABILIZER CENTER SECTION, AFT LEFT INT SECTION OF BEAMS. FABRIC ATED NEW ANGLE PER BOEING DRAWING 65-47598, INSTALLED PER SRM 51-40-02 AND 03. (M) 2 L 7 2 4F RT A16WE 2001062700029 20010627 00029 NM 2001 6 27 USAA010467 1 20010425 A 5510 GUSSET BOEING 737 7373B7 1384580 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 47122 22953 CLT - FOUND GUSSET/ANGLE CRACKED 6 INCHES, HORIZONTAL STABILIZER CENTER SECTION, INT SEC OF BEAMS INBOARD SIDE UP CHORD. INSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F RT A16WE 2001062700030 20010627 00030 NM 2001 6 27 USAA010468 1 20010425 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 47122 22953 CLT - FOUND BULKHEAD WEB CRACKED .5 INCH, BS 178, WL 234, RBL 8. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER EO 5300V1 53 AND SRM 53-10-08. (M) 2 L 7 2 4F RT A16WE 2001062700031 20010627 00031 NM 2001 6 27 USAA010469 1 20010425 A 5320 STRAP BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 47122 22953 CLT - FOUND INNERCHORD STRAP CORRODED 3 SQUARE INCH AREA, BS 794, S20R TO S25R. REMOVED AND REPLACED STRAP, SRM 51-10-2 , SRM 51-40-00. (M) 2 L 7 2 4F RT A16WE 2001062700032 20010627 00032 NM 2001 6 27 USAA010470 1 20010427 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 47122 22953 CLT - FOUND FLOORBEAM CORRODED .5 INCH B.25 INCH, BS 1006, LBL 10. REPLACED T-CAP SECTION PER EA 69149A. (M) 2 L 7 2 4F RT A16WE 2001062700033 20010627 00033 NM 2001 6 27 USAA010471 1 20010427 A 5312 BULKHEAD BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 34934 23990 CLT - FOUND PRESSURE WEB CRACKED TWO PLACES .125 INCH BOTH LOCATIONS, BS 178, WL 213 RBL 5.5 AND WL 234 RBL 10. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER EO 5300V153 AND SRM 53-10-08 FIG 209. (M) 2 L 7 2 4F RT A16WE 2001062700034 20010627 00034 NM 2001 6 27 USAA010472 1 20010427 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 429US 33707 24551 CLT - FOUND PRESSURE WEB WITH 5 CRACKS, TWO .250 INCH, TWO .150 INCH AND ONE .100 INCH, BS 178, WL 195, 198, 201.5, 206. 6; LBL 5 TO RBL 7. DAMAGE CUTOUT, REPAIR DOUBLER INSTALLED PER EO 5300V153 AND EA 69566. (M) 2 L 7 2 4F RT A16WE 2001062700035 20010627 00035 NM 2001 6 27 USAA010534 1 20010515 A 5320 WEB BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 284AU 47733 23131 CLT - FOUND WEB CRACKED TWO PLACES .5 INCH AND 1 INCH, BS 707-712, BBL 0, WL 203. FABRICATED AND INSTALLED REPAIR DOUBL ER PER TYPICAL REPAIR 57-10-05. (M) 2 L 7 2 4F A16WE 2001062700036 20010627 00036 NM 2001 6 27 USAA010535 1 20010515 A 5320 WEB BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 284AU 47733 23131 CLT - FOUND TORQUE BOX WEB CRACKED .1875 INCH, BS 947.5 STRINGER 11L, TORQUE BOX, FORWARD/ABV HINGE CUTOUT. REMOVED DAM AGE, INSTALLED REPAIR FILLER AND DOUBLER PER TR 53-30-07A. (M) 2 L 7 2 4F A16WE 2001062700037 20010627 00037 NM 2001 6 27 01FDEA00502 1 20010626 A 3231 FITTING BOEING 727 72722C 138400F NM BS 227.8 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 N 773 DUR ROUTINE INSP, NLG DOOR UPR LINK FITTING BS 227.8 FND CORRODED. R&R FITTING IAW BAC 727 SRM 51-30-2. 2 L 7 3 4F A3WE 2001062700038 20010627 00038 NM 2001 6 27 01FDEA00503 1 20010626 A 5330 SKIN BOEING 727 72722C 138400F NM BS 425-440 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 N 371 DUR ROUTINE INSP FUSELAGE SKIN FND CORRODED FROM BS 425-440 BETWEEN STR 3L AND 4L. R&R & FAB SKIN PER IAW BAC 727 SRM 53-30-3. 2 L 7 3 4F A3WE 2001062700039 20010627 00039 EU 2001 6 27 C2XA01BT119 1 20010524 A 5315 S5367240921800 BEAM AEROSP ATR42 ATR42320 8680930 EU CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 97841 280 YUL--Durring a schedule 3C inspection, corrosion was found on floor beam at frame 40, Maintence repaired corroded area I .A.W.-EC5310-01037. 2 H 7 2 4T RT A53EU 2001062700040 20010627 00040 EU 2001 6 27 C2XAA01BT121 1 20010531 A 2770 YCRS16CP CAM FOLLOWER AEROSP ATR42 ATR42320 8680930 EU SEIZED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 21837 202 YUL---Durring a scheduled 4C inspection. The pitch uncoupling mechanism was found seized.Maintenance removed and replace d the cam follower and bearing I.A.W.-ATR-42-JIC-27-31-42,20-21-00 AND 20-26-14. 2 H 7 2 4T RT A53EU 2001062700041 20010627 00041 EU 2001 6 27 C2XA01CL151 1 20010627 A 3260 141FL01D3 SWITCH AEROSP ATR42 ATR42320 8680930 EU RIGHT GEAR DEFECTIVE A C2XA K NONE J WARNING INDICATION CR CRUISE 1 SW 27 14821 160 CLE FLIGHT#3040 THE CREW REPORTED THE #2 GEAR SYSTEM GEAR UNLOCK LIGHT STAYS ILLUMINATED WHEN THE GEAR IS UP.THE AIRCRAF T LANDED WITHOUT INCIDENT.MAINTENANCE REPLACED THE # 2 GEAR UNLOCK SWITCH.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A53EU 2001062700042 20010627 00042 NM 2001 6 27 USAA010536 1 20010515 A 5313 STRINGER BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 284AU 47733 23131 CLT - FOUND SHELF CRACKED APPROX .75 INCH, STRINGER 18A, LEFT SIDE. REMOVED AND REPLACED 18A SHELF. (M) 2 L 7 2 4F A16WE 2001062700043 20010627 00043 NM 2001 6 27 USAA010537 1 20010515 A 5311 FRAME BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 284AU 47733 23131 CLT - FOUND VERTICAL CHORD .6 INCH AND .5 INCH, BS 178, LBL 5.7, WL 184. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER E O 5300V155. (M) 2 L 7 2 4F A16WE 2001062700044 20010627 00044 NM 2001 6 27 USAA010538 1 20010515 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 284AU 47733 23131 CLT - FOUND FLOORBEAM CORRODED SEVERAL AREAS 1 INCH, BS 328, RBL 12 TO RBL 60 TO FLOOR LEVEL. REMOVED AND REPLACED UPPE R T-CAP OF FLOORBEAM PER TYPICAL REPAIR 53-10-13. (M) 2 L 7 2 4F A16WE 2001062700045 20010627 00045 NM 2001 6 27 USAA010539 1 20010515 A 5320 WEB BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 284AU 47733 23131 CLT - FOUND CLOSEOUT WEB CRACKED APPROX .1875 INCH, BS 948 JUST BELOW STRINGER 11R. INSTALLED REPAIR DOUBLER PER TYPICA L REPAIR 53-30-7A. (M) 2 L 7 2 4F A16WE 2001062700046 20010627 00046 NM 2001 6 27 USAA010540 1 20010515 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 284AU 47733 23131 CLT - FOUND FLOORBEAM CORRODED, SEVERAL 1 INCH AREAS, BS 1006, BETWEEN LBL 10 AND LBL 30. REMOVED AND REPLACED UPPER T- CAP PER SRM 51-30-0. (M) 2 L 7 2 4F A16WE 2001062700047 20010627 00047 EU 2001 6 27 C2XA01CL152 1 20010626 A 3350 7007552 FUSE AEROSP ATR42 ATR42320 8680930 EU CABIN BLOWN A C2XA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 27 16824 166 CLE FLIGHT# 3119 THE CREW REPORTED 3 LIGHTS IN THE EMERGENCY AISLE PATH LIGHTING WERE INOPERATIVE.MAINTENANCE REPLACED THE FUSE IN POWER SUPPLY 30 WL.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A53EU 2001062700048 20010627 00048 NM 2001 6 27 USAA010541 1 20010515 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 284AU 47733 23131 CLT - FOUND FLOORBEAM T-CAP CORRODED SEVERAL 1 INCH DIAMETER AREAS, BS 947 BETWEEN RBL 14 AND LBL 14. REMOVED AND REPLA CED PREVIOUS T-CAP REPAIR PER SRM 53-10-9, FIG 2. (M) 2 L 7 2 4F A16WE 2001062700049 20010627 00049 NM 2001 6 27 USAA010542 1 20010515 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 284AU 47733 23131 CLT - FOUND STRINGER TIE CLIP CRACKED .375 INCH, BS 616, STRINGER 4L. REMOVED AND REPLACED TIE CLIP PER SRM 53-30-00. (M) 2 L 7 2 4F A16WE 2001062700050 20010627 00050 NM 2001 6 27 USAA010543 1 20010515 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 284AU 47733 23131 CLT - FOUND FLOORBEAM CORRODED 1 INCH BY 24 INCHES, BS 259.5 RBL 12 TO LBL 12 ALONG COCKPIT FLOOR. DAMAGED REMOVED, INS TALLED REPAIR PER SRM 51-10-02 AND TR 53-10-16. (M) 2 L 7 2 4F A16WE 2001062700051 20010627 00051 NM 2001 6 27 USAA010544 1 20010515 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 284AU 47733 23131 CLT - FOUND FLOORBEAM CORRODED SEVERAL 1 INCH AREAS, BS 312, BETWEEN LBL 12 AND RBL 12, AT FLOOR LEVEL. REMOVED AND REP LACED PREVIOUS T-CAP REPAIR PER TYPICAL REPAIR 53-10-13. (M) 2 L 7 2 4F A16WE 2001062700052 20010627 00052 NM 2001 6 27 USAA010545 1 20010515 A 5320 ANGLE BOEING 737 7372B7 1384560 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 284AU 47733 23131 CLT - FOUND Z-ANGLE CORRODED 1 INCH BY 40 INCH AREA, BS 947 TO 987, RIGHT SIDE. REMOVED AND REPLACED Z-ANGLE PER SRM 51 -10-02. (M) 2 L 7 2 4F A16WE 2001062700053 20010627 00053 NM 2001 6 27 USAA010546 1 20010515 A 5320 SPLICE BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 284AU 47733 23131 CLT - FOUND STRINGER SPLICE CRACKED .5 INCH, BS 909, STRINGER 4L. FABRICATED AND INSTALLED NEW STRINGER SPLICE PER SRM 51-10-01. (M) 2 L 7 2 4F A16WE 2001062700054 20010627 00054 NM 2001 6 27 USAA010547 1 20010430 A 5542 RCN35501 SKIN BOEING 737 737301 1384611 NM RUDDER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 40168 23739 PIT - FOUND RUDDER DELAMINATED AND GOUGED IN SEVERAL AREAS, LT AND RT RUDDER SKIN AND ONE LEADING EDGE GOUGE. COMPOSITE WET LAYUP REPAIR 230. (M) 2 L 7 2 4F RT A16WE 2001062700055 20010627 00055 EU 2001 6 27 USAA010548 1 20010508 A 5720 STRAP AIRBUS A319 A319112 EU WING BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 712US 6646 1038 PIT - FOUND TIE STRAP CRACKED AND BROKEN, BETWEEN WING RIBS 22 AND 24 LEFT WING UPPER SURFACE. REMOVED AND REPLACED BRO KEN PARTS, REPAIRED PER EA 71017. (M) 2 L 7 2 4F RT A28NM 2001062700056 20010627 00056 NM 2001 6 27 USAA010549 1 20010417 A 5751 05761 AILERON BOEING 737 737301 1384611 NM RT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 40168 23739 PIT - FOUND RIGHT AILERON CRACKED .5 INCH BY .5 INCH, AILERON FRONT SPAR UPPER FLANGE AT NR 1 HINGE ACCESS. INSTALLED W ET LAYUP WITH A 230 CURE WITH ONE EXTRA PLY PER SRM 51-70-17, EA 70844. (M) 2 L 7 2 4F RT A16WE 2001062700057 20010627 00057 WP 2001 6 27 USAA010550 1 20010420 A 5330 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 810US 53196 48042 PIT - FOUND SKIN CRACKED .25 INCH, STATION 1418 LONGERON 2 RT. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER PER SRM 53- 04 FIG 40. (M) 2 L 7 2 4F A6WE 2001062700058 20010627 00058 NM 2001 6 27 USAA010558 1 20010518 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND FLOORBEAM T-CAP CRACKED, BS 520, RBL 25, WL 208. INSTALLED DOUBLER AND PIVOT LINK ASSY PER SB 737-53-1120 A ND EA 69537. (M) 2 L 7 2 4F A16WE 2001062700059 20010627 00059 NM 2001 6 27 USAA010559 1 20010518 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND CHORD CRACKED 1 INCH, BS 663, LBL 24, WL 203. INSTALLED REPAIR CHORD PER EA 69538 AND SB 737-53-1184. (M) 2 L 7 2 4F A16WE 2001062700060 20010627 00060 EU 2001 6 27 SIMA20011316 1 20010510 A 5300 7253721459 TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 280AE 340B280 SBP - DURING MBV INSPECTION, FOUND LAVATORY TRACK HAS SEVERAL CORRODED AREAS. REMOVED AND REPLACED TRACK IAW SAAB AMM 2 0-10-00. (M) 2 L 7 2 4T RT A52EU 2001062700061 20010627 00061 EU 2001 6 27 SIMA20011317 1 20010510 A 5300 7253721413 WEB SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 280AE 340B280 SBP - DURING MBV INSPECTION, FOUND FLOOR WEB AT FS 258 BETWEEN BL 18.3 AND BL 11.0 HAS SEVERE CORROSION. REMOVED AND RE PLACED FLOOR WEB IAW SAAB SRM 51-40-21. (M) 2 L 7 2 4T RT A52EU 2001062700062 20010627 00062 EU 2001 6 27 SIMA20011318 1 20010510 A 5300 7253721427 INTERCOSTAL SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 280AE 340B280 SBP - DURING MBV INSPECTION, FUOND THE INTERCOSTAL AND REINFORCEMENT ANGLE UNDER FORWARD EDGE OF LEFT GALLEY HAS CORRODE D AREAS. REMOVED AND REPLACED INTERCOSTAL AND ANGLE IAW SAAB SRM 51-40-21. (M) 2 L 7 2 4T RT A52EU 2001062700063 20010627 00063 EU 2001 6 27 SIMA20011319 1 20010510 A 5300 7253711165 ANGLE SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 280AE 340B280 SBP - DURING MBV INSPECTION, MAINTENANCE FOUND THE LEFT AFT FLOOR PANEL SUPPORT ANGLE IS CORRODED. REMOVED AND REPLACED SUPPORT ANGLE IAW SAAB SRM 51-40-21. (M) 2 L 7 2 4T RT A52EU 2001062700064 20010627 00064 EU 2001 6 27 SIMA200113115 1 20010508 A 5300 7253813499 FRAME SAAB SF340 340B 7860101 EU FS 649 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 339SB 340B339 ABI - DURING MBV INSPECTION, A DENT WAS FOUND ON RIGHT FUSELAGE AT FRAME 649. FRAME WAS REMOVED AND REPLACED IAW SAAB S RM. (M) 2 L 7 2 4T RT A52EU 2001062700065 20010627 00065 EU 2001 6 27 SIMA200113119 1 20010511 A 2100 7769106 ACM SAAB SF340 340B 7860101 EU INOPERATIVE A SIMA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 381AE 340B381 DFW - FLT 3365 - CREW WAS UNABLE TO CONTROL CABIN TEMPERATURE IN EITHER AUTO OR MANUAL MODE, CREW RETURNED TO FIELD. MA INTENANCE REMOVED AND REPLACED THE LEFT AIR CYCLE MACHINE IAW SAAB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001062700066 20010627 00066 EU 2001 6 27 SIMA200113112 1 20010510 A 5700 NAS739E111 BUSHING SAAB SF340 340B 7860101 EU GEAR ASSY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 280AE 340B280 SBP - DURING MBV MAINTENANCE, FOUND THE LEFT MAIN LANDING GEAR OUTBOARD CONNECTING LINK AFT BUSHING IS CORRODED. REMOVE D AND REPLACED BUSHING IAW SAAB AMM 57-40-05. (M) 2 L 7 2 4T RT A52EU 2001062700067 20010627 00067 EU 2001 6 27 SIMA200113111 1 20010510 A 5700 NAS739E111 BUSHING SAAB SF340 340B 7860101 EU GEAR ASSY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 280AE 340B280 SBP - DURING MBV MAINTENANCE, FOUND THE RIGHT MAIN LANDING GEAR INBOARD CONNECTING LINK AFT BUSHING IS CORRODED. REMOVE D AND REPLACED BUSHING IAW SAAB AMM 57-40-05. (M) 2 L 7 2 4T RT A52EU 2001062700068 20010627 00068 SO 2001 6 27 SIMA20011404 1 20010518 A 5300 AL2024T3 SKIN EMB 135 EMB135LR SO CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 701MH 145165 DURING MBV INSPECTION, MAINTENANCE FOUND THE OMEGA BEAM AT FRAME 20 CORRODED. MAINTENANCE REMOVED CORROSION AND INSTALL ED DOUBLER REPAIR IAW EMB GST 1630/01. (M) 2 L 7 2 4F RT TOOO11AT 2001062700069 20010627 00069 SO 2001 6 27 SIMA20011403 1 20010518 A 5300 AL2024T3 SKIN EMB 145 EMB145LR SO FWD DIGITAL CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 638AE 145172 ABI - DURING MBV INSPECTION, MAINTENANCE FOUND THE FORWARD DIGITAL CORRODED. CORROSION WAS REMOVED AND A DOUBLER WAS IN STALLED IAW EMB GST-1595/01. (M) 2 L 7 2 4T RT T00011AT 2001062700070 20010627 00070 NM 2001 6 27 GAIA01216ST 1 20010611 A 5300 SEAT TRACK BOEING 727 727251 138408H NM BS 690-740 A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A LTC INSPECTION AT FLIGHSTAR, IT WAS DISCOVERED THAT SEAT TRACK BS 700 LBL 24.75 HAS ELONGATED LOCK HOLES. ACCO MPLISHED SEAT TRACK REPAIR BS 690-740 LBL 24.75 IAW B727 SRM 53-10-5 FIG 1. (M) 2 L 7 3 4F A3WE 2001062700071 20010627 00071 NM 2001 6 27 GAIA01213ST 1 20010611 A 5300 STRINGER BOEING 727 727251 138408H NM BS 720B CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT STRINGER 15R IS CRACKED AT BS 720B PLUS 15. ACCOMPLISHED STRINGER REPAIR BS 720B PLUS 15 STRINGER 15R IAW B727 SRM 53-10-3 FIG 5. (M) 2 L 7 3 4F A3WE 2001062700072 20010627 00072 NM 2001 6 27 GAIA01212ST 1 20010611 A 5300 STRINGER BOEING 727 727251 138408H NM BS 720B CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT STRINGER 15L IS CRACKED AT BS 720B PLUS 15. ACCOMPLISHED STRINGER REPAIR BS 720B PLUS 15 STRINGER 15L IAW B727 SRM 53-10-3 FIG 5. (M) 2 L 7 3 4F A3WE 2001062700073 20010627 00073 NM 2001 6 27 GAIA01211ST 1 20010611 A 5300 STIFFENER BOEING 727 727251 138408H NM BS 309 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT HORIZONTAL STIFFENER AT BS 309 LBL 12 - RBL 12 WL 181 ON T OP OF NOSE WHEEL WELL IS EXFOLIATED. ACCOMPLISHED HORIZONTAL STIFFENER REPLACEMENT BS 309 LBL 12 TO RBL 12 WL 181 IAW B 727 SRM 53-10-2 FIG 2 AND 51-30-2. (M) 2 L 7 3 4F A3WE 2001062700074 20010627 00074 NM 2001 6 27 GAIA01210ST 1 20010611 A 5300 SKIN BOEING 727 727251 138408H NM BS 630 GOUGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT A GOUGE ON FUSELAGE SKIN BS 630 STRINGER 15-16R. ACCOMPLI SHED FUSELAGE SKIN REPAIR BS 630 STRINGER 15-16R IAW B727 SRM 53-30-3 FIG 3. (M) 2 L 7 3 4F A3WE 2001062700075 20010627 00075 NM 2001 6 27 GAIA01205ST 1 20010611 A 5312 BULKHEAD BOEING 727 727251 138408H NM BS 178 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT TWO CRACKS IN BS 178 B/H WEB AT FASTENER LOCATIONS WL 235 RBL 10-12. ACCOMPLISHED BS 178 BULKHEAD WEB REPAIR BS 178 WL 235 RBL 10-12 IAW B727 SRM 53-10-9 FIG 4. (M) 2 L 7 3 4F A3WE 2001062700076 20010627 00076 NM 2001 6 27 GAIA01204ST 1 20010611 A 5300 BULKHEAD BOEING 727 727251 138408H NM BS 178 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT TWO CRACKS IN BS 178 B/H WEB AT FASTENER LOCATIONS WL 235 LBL 10-12. ACCOMPLISHED BS 178 BULKHEAD WEB REPAIR BS 178 WL 235 LBL 10-12 IAW B727 SRM 53-10-9 FIG 4. (M) 2 L 7 3 4F A3WE 2001062700077 20010627 00077 NM 2001 6 27 GAIA01202ST 1 20010611 A 5300 STRINGER BOEING 727 727251 138408H NM BS 440 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT CORROSION ON SKIN LAP BS 440 STRINGER 26L. ACCOMPLISHED S TRINGER REPAIR BS 440 STRINGER 26L IAW B727 SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 2001062700078 20010627 00078 NM 2001 6 27 GAIA01201ST 1 20010611 A 5300 STIFFENER BOEING 727 727251 138408H NM BS 1183 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT BS 1183 AFT BULKHEAD UPPER RIGHT SIDE STIFFENER IS CORRODE D. ACCOMPLISHED 1183 BULKHEAD STIFFENER REPAIR IAW B727 SRM 51-40-4. (M) 2 L 7 3 4F A3WE 2001062700079 20010627 00079 NM 2001 6 27 GAIA01198ST 1 20010611 A 5300 FRAME BOEING 727 727251 138408H NM BS 1166 DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT LEFT BS 1166 FRAME DENTED AT WL 212. ACCOMPLISHED FUSELAG E FRAME REPAIR BS 1166 LEFT WL 212 IAW B727 SRM 53-10-4 FIG 2. (M) 2 L 7 3 4F A3WE 2001062700080 20010627 00080 NM 2001 6 27 USAA010561 1 20010518 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND VERTICAL CHORD CRACKED 1.3 INCHES, BS 178, LBL 6, WL 198. INSTALLED REPAIR KIT PER EO 5300V155. (M) 2 L 7 2 4F A16WE 2001072400006 20010724 00006 NM 2001 7 24 2001UALA00916 1 20010624 A 5320 DOUBLER BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 DRAIN DOUBLER CORRODED BS 1400 - 1410 STRINGER 35R - 36R. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED C HANNEL AND DOUBLER IN ACCORDANCE WITH BAC DRAWING 146T3534 AND SRM 51-40-02. 2 L 7 2 4F RT A1NM 2001072600012 20010726 00012 NM 2001 7 26 2001UALA00953 1 20010606 A 5754 WEDGE BOEING 757 757222 1384956 NM L/E SLAT DEPARTED A UALA K NONE D INFLIGHT SEPARATION AP APPROACH 1 WP 29 519UA 24872 NR 5 LEADING EDGE SLAT WEDGE, 49 INCH SECTION DEPARTED AIRCRAFT. SUPPLEMENTAL DATA UPDATE REPLACED THE NR 5 LEADING EDGE SLAT. THE LOSS OF THE 49 INCH SECTION OF THE TRAILING EDGE WEDGE WAS DUE TO DELAMINATION BETWEEN THE SKIN-TO-CORE BOND LINE. DELAMINATION IS BELIEVED TO BE CAUSED BY WATER INGRESSION. 2 L 7 2 4F RT A2NM 2001072400009 20010724 00009 NM 2001 7 24 2001UALA00992 1 20010623 A 3350 M9035 CHARGER BOEING 767 767222 1385122 NM CABIN FAILED A UALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 29 615UA 21876 ALL EEL AND EMERGENCY LIGHTS ILLUMINATED AFT OF ROW 27 WITH EMERGENCY LIGHT SWITCH IN AUTO. UNABLE TO EXTINGUISH LIGHTS EXCEPT BY PLACING EMERGENCY LIGHT SWITCH TO OFF. *S/D* REPLACED BATTERY PACK AND BATTERY CHARGER M9035. OP CHECKS OK PER MM 33-51-00 PAGE 501. 2 L 7 2 4F RT A1NM 2001062700081 20010627 00081 NM 2001 6 27 2001UALA01044 1 20010616 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 CABIN FLOORBEAM UPPER SURFACE CORRODED. STA 324, RBL 58 MAJOR REPAIR ACCOMPLISHED. INSTALLED FREEZE PLUB AND INSTALLE D T-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2001062700082 20010627 00082 NM 2001 6 27 2001UALA01045 1 20010617 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 CABIN FLOOR SUPPORT CORRODED. STA 297, RBL 40-42. MAJOR REPAIR ACCOMPLISHED. REPLACED L-ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001062700083 20010627 00083 NM 2001 6 27 2001UALA01049 1 20010618 A 5315 SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 FLOOR SUPPORT CORRODED. MAJOR REPAIR ACCOMPLISHED.INSTALLED NEW J-ANGLE AND STRAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2001062700084 20010627 00084 NM 2001 6 27 2001UALA01051 1 20010616 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 318UA 23950 FUSELAGE SKIN THICKNESS BELOW MINIMUM LIMITS. STA 796, STR 22R-23R. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001062700085 20010627 00085 NM 2001 6 27 2001UALA01053 1 20010616 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 318UA 23950 FRAME CRACKED. STA 188, WL 207, LEFT SIDE. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001062700086 20010627 00086 NM 2001 6 27 2001UALA01055 1 20010617 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 FRAME CRACKED. STA 188, STR 17L, WL 207. MAJOR REPAIR ACCOMPLISHED.INSTALLED NESTED ANGLE REPAIR AND SKIN DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001062700087 20010627 00087 NM 2001 6 27 2001UALA01057 1 20010617 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 FRAME WEB DAMAGED. STA 616, RBL 64. MAJOR REPAIR ACCOMPLISHED.INSTALLED NEW WEB AND DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001062700088 20010627 00088 NM 2001 6 27 2001UALA01058 1 20010618 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 FRAME CRACKED. STA 188, WL 206. MAJOR REPAIR ACCOMPLISHED.INSTALLED ANGLE REPAIR AND SKIN DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001062700089 20010627 00089 NM 2001 6 27 2001UALA01059 1 20010618 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 318UA 23950 FRAME CRACKED. STA 181, WL 183 AT INSULATION SPIKE HOLE. MAJOR REPAIR ACCOMPLISHED.INSTALLED NEW WEB AND SPLICED PLATE. 2 L 7 2 4F 4 F RT A16WE E2GL 2001062700090 20010627 00090 NM 2001 6 27 2001UALA01061 1 20010616 A 3350 BATTERY BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE WEAK A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 951UA 26696 EEL LIGHTING VERY DIM. ROW 3-10 AND 15-AFT. REPLACED BATTERY PACKS AND AFT CABIN POWER INVERTER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001062700091 20010627 00091 NM 2001 6 27 2001UALA01062 1 20010619 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 FWD PIT FRAME DAMAGED. STA 500, STR 25R TO STR 26R. MAJOR REPAIR ACCOMPLISHED.INSTALLED J-ANGLE REINFORCEMENT REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001062700093 20010627 00093 NM 2001 6 27 2001UALA01097 1 20010618 A 5230 65C8073527 FRAME 6546921225 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NICKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 1843 24657 FWD CARGO DOOR LOWER AFT CORNER FRAME HAS A NICK BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED.REPLACED CORNER FRAME. 2 L 7 2 4F 4 F RT A16WE E2GL 2001062700094 20010627 00094 NM 2001 6 27 2001UALA01103 1 20010621 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 513UA 24810 FLOORBEAM CAP CORRODED. STA 1640, LBL 6 AND RBL 62. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE SPLICE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001062700095 20010627 00095 NM 2001 6 27 2001UALA01125 1 20010622 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE MISDRILLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 FRAME SHEAR TIE HAS MISDRILLED HOLE. STA 967, OB OF STR 4R. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER AND NEW SHEAR T IE. 2 L 7 2 4F 4 F RT A16WE E2GL 2001062700096 20010627 00096 NM 2001 6 27 USAA010562 1 20010518 A 5553 ATTACH FITTING BOEING 737 737201 1384454 NM VERTICAL STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND FUSELAGE ATTACH LUGS CORRODED 3 SQUARE INCHES, VERT FIN, AFT OUTBOARD LEFT AND AFT OUTBOARD RIGHT ATTACH POI NTS. CORROSION REMOVED AND LUGS REWORKED PER EA 69591 AND EO 5593G087. (M) 2 L 7 2 4F A16WE 2001062700097 20010627 00097 NM 2001 6 27 USAA010567 1 20010525 A 5312 BULKHEAD BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 36765 23877 CLT - FOUND PRESSURE WEB .5 INCH, .75 INCH AND 1.5 INCH, BS 178 WL 199 AND 201, LBL 6.5 TO RBL 6.5. REMOVED DAMAGED, IN STALLED REPAIR FILLERS AND DOUBLER PER EO 5300V153. (M) 2 L 7 2 4F RT A16WE 2001062700098 20010627 00098 NM 2001 6 27 USAA010568 1 20010525 A 5754 DOUBLER BOEING 737 737401 1384701 NM L/E SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 36765 23877 CLT - FOUND REPAIR DOUBLER CRACKED .5 INCH, NR 2 SLAT, OUTBOARD OF ACTUATOR ATTACH. REMOVED CRACKED DOUBLER, INSTALLED NEW DOUBLER PER SRM 57-43-01. (M) 2 L 7 2 4F RT A16WE 2001062700099 20010627 00099 NM 2001 6 27 USAA010569 1 20010525 A 5312 BULKHEAD BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 242US 52490 22444 CLT - FOUND PRESSURE WEB WITH CRACKS RANGING IN SIZE FROM .375 INCH TO 1.5 INCH, BS 178, WL 199 TO WL 234 LBL 10.5 TO RB L 10.5. DAMAGE REMOVED, REPAIR FILLERS AND DOUBLER INSTALLED PER EO 5300V153, EA 69712, SRM 53-10-11 FIG 1. (M) 2 L 7 2 4F A16WE 2001062700100 20010627 00100 NM 2001 6 27 USAA010570 1 20010525 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 242US 52490 22444 CLT - FOUND SIDE CHORD CRACKED .5 INCHES AND 1.25 INCHES, BS 178, LEFT AND RIGHT SIDE CHORD, WL 195. DAMAGED SECTIONS C UTOUT, INSTALLED CHORD SPLICE REPAIR PER EO 5300V157 AND SRM 51-10-02. (M) 2 L 7 2 4F A16WE 2001062700101 20010627 00101 NM 2001 6 27 USAA010572 1 20010525 A 5312 BULKHEAD BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 242US 52490 22444 CLT - FOUND WEB CRACKED .250 INCH, BS 178 WL 195.7, LBL 23. REMOVED DAMAGED AREA, INSTALLED FILLER AND DOUBLER PER EA 6 9714 AND SRM 53-10-11 FIG 2. (M) 2 L 7 2 4F A16WE 2001062700102 20010627 00102 NM 2001 6 27 USAA010573 1 20010520 A 5314 KEEL BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51502 22754 CLT - FOUND KEEL CHORD OUTBOARD FLANGE WITH 3 INCH AREA OF CORROSION, BS 727A, RBL 7, BELLY AREA. REMOVED DAMAGE, INSTA LLED SPLICE REPAIR PER TR 53-10-24, EA 69672, SRM 51-20-1 FIG 10, 53-10-6 FIG 3. (M) 2 L 7 2 4F A16WE 2001062700103 20010627 00103 NM 2001 6 27 USAA010582 1 20010522 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 522AU 40769 23857 PIT - FOUND SKIN CORRODED 1 INCH BY 2 INCHES, STATION 969 BETWEEN RIGHT STRINGER 27 AND 28. INSTALLED DOUBLER PER EA NR 70922. CORROSION LEVEL 1, TASK NR C53-208-01. (M) 2 L 7 2 4F RT A16WE 2001062700104 20010627 00104 NM 2001 6 27 QXEA0101064 1 20010625 A 3350 GRIMES DHAV DHC8 DHC8202 2809007 NM A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 9711051 477 PDX - UPON INSPECTION, FOUND THE FORWARD, CENTER, AND AFT OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLAC ED #1 AND #2 POWER SUPPLIES. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001062700105 20010627 00105 NM 2001 6 27 USAA010583 1 20010522 A 5313 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 522AU 40769 23857 PIT - FOUND STRINGER CORRODED 1 INCH BY .500 INCH, STRINGER 28 AT STATION 948. CORROSION LEVEL 1, TASK NR C53-208-01. INSTALLED REPAIR SPLICES PER SRM 53-00-01 FIG 201. (M) 2 L 7 2 4F RT A16WE 2001062700106 20010627 00106 NM 2001 6 27 USAA010584 1 20010522 A 5313 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 522AU 40769 23857 PIT - FOUND STRINGER CORRODED 1 INCH BY .500 INCH, STRINGER 28 AT STATION 948. CORROSION LEVEL 1 TASK NR C53-208-01. I NSTALLED REPAIR SPLICES PER SRM 53-00-01 FIG 201. (M) 2 L 7 2 4F RT A16WE 2001062700107 20010627 00107 NM 2001 6 27 USAA010592 1 20010516 A 5311 FRAME BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND UPPER CHORD CORRODED 1 INCH BY 4 INCHES, BS 986.5. CORROSION LEVEL NR 1, TASK NR C53-107-02. CLEAN/TREAT/P RIME, ALSO CUT OUT DAMAGE SPLICE IN NEW STRUCTURE PER TYP REPAIR 53-60-01. (M) 2 L 7 2 4F RT A16WE 2001062700108 20010627 00108 NM 2001 6 27 USAA010593 1 20010516 A 5311 FRAME BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND UPPER CHORD CORRODED 1 INCH BY 3 INCHES CORROSION, BS 967. CORROSION LEVEL 1, TASK NR C53-107-02. CLEAN/TR EAT/PRIME AND INSTALL STRAP PER EA 70646 IAW SRM 53-00-51. (M) 2 L 7 2 4F RT A16WE 2001062700109 20010627 00109 EU 2001 6 27 USAA20010723 1 20010404 A 5320 4061641 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 33069 512 TUL - FOUND CORROSION ON CROSS SUPPORT BETWEEN E/RT AND D/RT, BETWEEN FRAME 71 AND 72, LAVATORY TIE DOWN. REPLACED CROS S SUPPORT (CPN 4061641) BETWEEN E/RT AND D/RT, BETWEEN FRAME 71 AND 72 PER SRM 51-72-00. (M) 2 L 7 2 4F RT A35EU 2001062700110 20010627 00110 EU 2001 6 27 USAABA01004 1 20010520 A 3350 32146220 POWER SUPPLY AIRBUS 330 A330323 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 673UW 337 PHL - FOUND NR 2R EPSU FAILED ON MFDU. MAINTENANCE REPLACED THE EPSU. (M) 2 L 7 2 4F RT A46NM 2001062700111 20010627 00111 NM 2001 6 27 USAABB01023 1 20010515 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 611AU 27123 MCO - FOUND FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE AT ROWS 13, 18 AND 33. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2001062700112 20010627 00112 NM 2001 6 27 USAABB01024 1 20010507 A 3350 873100151REV12 LIGHT BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 608AU 22204 BDL - FOUND AFT AISLE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001062700113 20010627 00113 NM 2001 6 27 USAABB01025 1 20010517 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 612AU 27124 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE AT ROW 4. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001062700114 20010627 00114 NM 2001 6 27 USAABB01027 1 20010519 A 3350 873100151REV12 LIGHT BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 607AU 22203 CLT - FOUND FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE AT ROW 18. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001062700115 20010627 00115 NM 2001 6 27 USAABB01028 1 20010519 A 3350 8731002511REV14 SIGN BOEING 757 757225 1384959 NM L4 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 607AU 22203 CLT - FOUND L4 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE IDENTIFIER ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001062700116 20010627 00116 NM 2001 6 27 USAABB01029 1 20010519 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 611AU 27123 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 3 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001062700117 20010627 00117 NM 2001 6 27 USAABB01030 1 20010521 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 623AU 27244 CLT - ALL FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES (10 TOTAL). (M) 2 L 7 2 4F RT A2NM 2001062700118 20010627 00118 WP 2001 6 27 USAAD01095 1 20010504 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 803US 48035 WOULD NOT TEST. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES AND THE TAILCONE EMERGEIND - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE AND THE TAILCONE EMERGENCY REMOTE RECEIVER NCY REMOTE RECEIVER. (M) 2 L 7 2 4F A6WE 2001062700119 20010627 00119 WP 2001 6 27 USAAD01096 1 20010505 A 3350 AD4002P BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 813US 48093 BOS - THE AFT GALLEY EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE AFT GALLEY EMERGENCY LIGHT BATTERY. ( M) 2 L 7 2 4F A6WE 2001062700120 20010627 00120 WP 2001 6 27 USAAD01098 1 20010509 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 813US 48093 PHL - THE EMERGENCY LIGHTS WERE FLICKERING ON AND OFF. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES. ( M) 2 L 7 2 4F A6WE 2001062700121 20010627 00121 WP 2001 6 27 USAAD01099 1 20010509 A 3350 86210151 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 813US 48093 CLT - THE EMERGENCY LIGHTS FLICKERED ON AND OFF. MAINTENANCE REPLACED THE EMERGENCY LIGHT CONTROL MODULE BATTERY PACKS AND THE LOW LEVEL EMERGENCY LIGHT BATTERY AT SEAT 3D. (M) 2 L 7 2 4F A6WE 2001062700122 20010627 00122 WP 2001 6 27 USAAD01100 1 20010510 A 3350 8732030153 MODULE DOUG DC9 DC981 3022081 WP CABIN FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 810US 48042 CLT - THE EMERGENCY LIGHTS IN THE AFT PASSENGER CABIN WOULD NOT OPERATE CORRECTLY. MAINTENANCE REPLACED THE AFT EMERGEN CY LIGHT CONTROL MODULE. (M) 2 L 7 2 4F A6WE 2001062700123 20010627 00123 WP 2001 6 27 USAAD01101 1 20010510 A 3350 8732030153 MODULE DOUG DC9 DC981 3022081 WP CABIN FAILED A USAA K NONE O OTHER AP APPROACH 1 EA 19 813US 48093 RSW-PIT - FLT 1032 - DURING APPROACH, THE EMERGENCY EXIT LIGHTS STARTED TO FLICKER. MAINTENANCE REPLACED THE FORWARD CO NTROL MODULE, THE MAIN ENTRY DOOR EXIT LIGHT ASSEMBLY, AND LOW LEVEL EMERGENCY LIGHT BATTERY FOR THE AFT SEAT MOUNTED LI GHT ASSEMBLY. (M) 2 L 7 2 4F A6WE 2001062700124 20010627 00124 WP 2001 6 27 USAAD01102 1 20010512 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 808US 48040 IND - THE LOW LEVEL EMERGENCY LIGHTS DID NOT TEST. MAINTENANCE REPLACED THE CONTROL MODULE BATTERIES, THE LOW LEVEL LIG HT BATTERIES, AND THE OVERWING EXIT IDENTIFIER LIGHT ASSEMBLY. (M) 2 L 7 2 4F A6WE 2001062700125 20010627 00125 WP 2001 6 27 USAAD01103 1 20010514 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 827US 48049 IND - THE LOW LEVEL EMERGENCY LIGHTS, NACELLE SCAN, AND CEILING LIGHTS AT SEAT ROWS 7 TO 17 WERE INOPERATIVE. MAINTENAN CE REPLACED THE LOW LEVEL, NACELLE SCAN, AND CEILING EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001062700126 20010627 00126 WP 2001 6 27 USAAD01104 1 20010515 A 3350 873100272 SIGN DOUG DC9 DC982 3022082 WP CABIN BURNED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 815US 48095 PIT - THE FORWARD RIGHT EMERGENCY WINDOW EXIT IDENTIFIER WAS BURNED AND MELTED. MAINTENANCE REPLACED THE EXIT IDENTIFIE R. (M) 2 L 7 2 4F A6WE 2001062700127 20010627 00127 WP 2001 6 27 USAAD01105 1 20010514 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 812US 48092 TPA - THE LOW LEVEL EMERGENCY LIGHTING AT SEAT ROW 3 WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 2001062700128 20010627 00128 WP 2001 6 27 USAAD01106 1 20010515 A 3350 TRANSMITTER DOUG DC9 DC981 3022081 WP CABIN INTERMITTENT A USAA K NONE O OTHER AP APPROACH 1 EA 19 813US 48093 MCO - DUE TO PREVIOUS PROBLEMS WITH THE EMERGENCY LIGHTS FLASHING DURING FLIGHT, THE COCKPIT EMERGENCY LIGHT SWITCH AND THE EMERGENCY LIGHT ARM AND CHARGE CIRCUIT BREAKER WERE REPLACED. MCO-PIT - FLT 1120 - DURING APPROACH, THE EMERGENCY L IGHTS WERE FLASHING AND ON STEADY OCCASIONALLY. MAINTENANCE REPLACED THE THREE LOW LEVEL EMERGENCY LIGHT TRANSMITTERS. NO FURTHER EMERGENCY LIGHT PROBLEMS. (M) 2 L 7 2 4F A6WE 2001062700129 20010627 00129 WP 2001 6 27 USAAD01107 1 20010516 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 801US 48037 IND - THE LOW LEVEL EMERGENCY LIGHT AT SEAT ROW 30 WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 2001062700130 20010627 00130 WP 2001 6 27 USAAD01108 1 20010516 A 3350 9731044 LIGHT DOUG DC9 DC981 3022081 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 810US 48042 PHL - THE LOW LEVEL EMERGENCY LIGHT AT SEAT ROW 25 WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT AND TRANSMITTER ASSE MBLY. (M) 2 L 7 2 4F A6WE 2001062700131 20010627 00131 2001 6 27 USAAD01109 4 20010516 A 2565 3961899501 LANYARD DOUG DC9 DC982 3022082 WP SERVICE DOOR DETERIORATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 825US 49237 PHL - THE FORWARD SERVICE DOOR EVACUATION SLIDE LANYARD WAS DETERIORATED. MAINTENANCE REPLACED THE LANYARD ASSEMBLY. ( M) 2 L 7 2 4F A6WE 2001062700132 20010627 00132 WP 2001 6 27 USAAD01110 1 20010519 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 803US 48035 TPA - THE LOW LEVEL EMERGENCY LIGHT AT SEAT ROW 11 AND THE EMERGENCY LIGHT AT THE AFT RIGHT SERVICE DOOR WERE INOPERATIV E. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001062700133 20010627 00133 WP 2001 6 27 USAAD01111 1 20010520 A 3820 WATER HEATER DOUG DC9 DC982 3022082 WP LAVATORY MALFUNCTIONED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 19 829US 49429 PHL-IND - FLT 1787 - DURING DESCENT, AN ELECTRICAL BURNING SMELL WAS DETECTED IN THE LAVATORY AREA. THE AFT LAVATORY WA TER HEATER CIRCUIT BREAKER WAS PULL BUT THE SMELL CONTINUED. THE AIRCRAFT CONTINUED TO ITS DESTINATION AND LANDED WITHO UT INCIDENT. MAINTENANCE CHECKED THE AFT LAVATORY AND ADJACENT AREA LIGHTING, AND BALLASTS, FLUSH MOTOR, WATER HEATER, AND WIRING. THE APU AND BOTH AIR CONDITIONING PACKS WERE OPERATED. THE TAIL COMPARTMENT AND AFT BAGGAGE COMPARTMENT WE RE CHECKED. THEY WERE UNABLE TO DUPLICATE ANY SMELL. THE AFT LAVATORY WATER HEATER WAS PLACED ON MEL AS A PRECAUTIONAR Y MEASURE AND THE AIRCRAFT WAS RELEASED FOR SERVICE. THE WATER HEATER WAS REPLACED ON THE MX OVERNIGHT. (M) 2 L 7 2 4F A6WE 2001062700134 20010627 00134 WP 2001 6 27 USAAD01112 1 20010521 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 807US 48039 BOS - THE LOW LEVEL LIGHTS FAILED TO TEST AT SEAT ROWS 1, 11, 25 AND 30. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTE RIES. (M) 2 L 7 2 4F A6WE 2001062700135 20010627 00135 WP 2001 6 27 USAAD01113 1 20010520 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 826US 48026 IND - THE LOW LEVEL EMERGENCY LIGHT AT SEAT ROW 6 WOULD NOT TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M ) 2 L 7 2 4F A6WE 2001062700136 20010627 00136 NM 2001 6 27 UPS01236171 1 20010613 A 5330 SKIN PANEL BOEING 727 72722C 138400F NM BS1343 WL246.5R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE:C CRACK IN SKIN BS 1342.4 AT WL246.5R CRACKED REMOVED BY BLENDING MATERIAL. DAMAGED AREA REPAIRED IA W SRM5 3-30-3FIG3A USING 2024T3.050 AND .040. 2 L 7 3 4F A3WE 2001062700137 20010627 00137 NM 2001 6 27 UPS01236174 1 20010613 A 5230 WEB BOEING 727 72722C 138400F NM BS612.9 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE:C ON INSPECTION OF MCD LATCH FITTINGS BY NDT, CRACK FOUND IN FRAME WEB CLEAT AT BS 612.9 DAMAGED AR EA TRIMMED OUT AND REPAIRED IAW SRM 51-40-2 2 L 7 3 4F A3WE 2001062700138 20010627 00138 NM 2001 6 27 UPS01236178 1 20010615 A 5310 65852082 FITTING BOEING 727 72722C 138400F NM TAILSKID CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE:C TIAL SKID BAY L/H UPPER TIE LINK AFT FITTING, EVIDENCE OF CRACK ON V ERTICAL FLANGE BETWEEN FASTENERS. FITTING REPLACED. 2 L 7 3 4F A3WE 2001062700139 20010627 00139 NM 2001 6 27 UPS01236180 1 20010613 A 5310 NPN WINDOW POST BOEING 727 72722C 138400F NM F+N WINDOW POST CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE:C CRACK FOUND IN F+N WINDOW POST ON SKIN DOUBLER ATL/H WINDOW POST AT WINDOW CUTOUT RADIUS POINT E R EPAIRED IAW UPS EO B727-5310-0012 2 L 7 3 4F A3WE 2001062700140 20010627 00140 NM 2001 6 27 UPS01236184 1 20010627 A 2780 SUPPORT BRACKET BOEING 727 72722C 138400F NM #6 KREUGER FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE:C #6 KREUGER FLAP ACTUATOR, BASE MOUNT SUPPORT BRACKET IS CRACKED ON O UTBOARD SIDE. #6 KREUGER FLAP ACTUATOR REMOVED IAW MM BASE MOUNT SUPORT BRACKET FABRICATED AND INSTALLED. 2 L 7 3 4F A3WE 2001062700141 20010627 00141 NM 2001 6 27 UPS01236185 1 20010616 A 5755 BRACKET BOEING 727 72722C 138400F NM #8GRND SPOILER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE:C #8 GRND SPOILER INBD END HINGE , CASTING ATTACHED TO MLG BEAM WHICH SUPPORTS THE END HINGE THROUGH A S UPPORT ROD IS CRACKED. REPLACED BRACKET IAW SRM 51-30-02. BRACKET REPLACED WITH ORIGINAL BO LTS. 2 L 7 3 4F A3WE 2001062700142 20010627 00142 NM 2001 6 27 UPS01236186 1 20010627 A 5310 FRAME BOEING 727 72722C 138400F NM BS 910LH CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE:C CRACK IN BS 910 FRAME L/H BELOW FLOOR LEVEL REPAIRED IAW DWG 65C27194 2 L 7 3 4F A3WE 2001062700144 20010627 00144 WP 2001 6 27 USAAD01115 1 20010522 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 811US 48043 IND - THE LOW LEVEL EMERGENCY LIGHT FAILED TO TEST AT SEAT ROWS 1, 3, 6 AND 19. THE CEILING EMERGENCY LIGHTS AT SEAT RO WS 1 TO 3 AND THE RIGHT AFT EMERGENCY EXIT LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES, (P/N 9721055, AD4002P, 9721050). (M) 2 L 7 2 4F A6WE 2001062700145 20010627 00145 WP 2001 6 27 USAAD01119 1 20010601 A 3350 MISC0639 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 825US 49237 PIT - THE OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) 2 L 7 2 4F A6WE 2001062700146 20010627 00146 EU 2001 6 27 USAAF01021 1 20010508 A 2560 D31873101 GIRT BAR FOKKER F28 F28MK0100 4990807 EU EVAC SLIDE DISCONNECTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 866US 18536 11310 PIT - DURING A SCHEDULED SLIDE CHANGE, FOUND THE SLIDE TO BE REMOVED DID NOT HAVE THE SLIDE GIRT ATTACHED TO THE GIRT BA R, ALTHOUGH THE FIRING CABLE WAS STILL ATTACHED. MAINTENANCE COMPLETED THE SLIDE CHANGE. (M) 2 L 7 2 4F RT 2001062700147 20010627 00147 EU 2001 6 27 USAAF01024 1 20010515 A 3350 59174 LIGHT FOKKER F28 F28MK0100 4990807 EU ENTRY DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 882US 11334 IND - THE EMERGENCY EXIT LIGHT ON THE MAIN ENTRY DOOR HINGE WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. FUNCTIONALLY CHECKED OK. (M) 2 L 7 2 4F RT 2001062700148 20010627 00148 WP 2001 6 27 ZW0A0102403 1 20010525 A 5311 FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 907TW 49165 DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND CORROSION AT FWD AND AFT SIDES OF FORMER FOOT, STA 1212 BETWEEN LONGER ON 30 AND 29R. REMOVED FORMER FOOT. REMOVED AND TREATED LIGHT CORROSION ON SKIN PER SPM 6-80-1 AND INSTALLED NEW FORME R FOOT PER SRM 51-30-2 AND SRM 51-30-5. 2 L 7 2 4F A6WE 2001062700149 20010627 00149 WP 2001 6 27 ZW0A0102404 1 20010525 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 907TW 49165 DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND CORRODED INTERCOSTAL AT STA 1212 TO 1219, BETWEEN LONGERON 30 AND 29R. REMOVED CORRODED INTERCOSTAL. INSTALLED NEW INTERCOSTAL PER SRM 51-30-2 AND SRM 51-30-5. 2 L 7 2 4F A6WE 2001062700150 20010627 00150 WP 2001 6 27 ZW0A0102405 1 20010525 A 5320 FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 907TW 49165 DURING CHECK-C MAINT FOUND T-FITTINGS CRACKED AT STA 1309, BETWEEN LONGERON 15 AND 16, AND ANOTHER BELOW LONGERON 14R AN D FWD SIDE OF PYLON SUPPORT WALL. INSTALLED NEW ANGLES PER DRAWING 9912243 WITH FASTENERS PER SRM 51-30-0. 2 L 7 2 4F A6WE 2001062700151 20010627 00151 WP 2001 6 27 ZW0A0102406 1 20010525 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE BULGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 907TW 49165 DURING CHECK-C MAINT FOUND BULGE 12 INCHES TO 15 INCHES ABOVE CUSP AT STA 246, LT SIDE SKIN. REMOVED DAMAGED SKIN. REP AIRED PER SRM 53-04-12C. 2 L 7 2 4F A6WE 2001062700152 20010627 00152 WP 2001 6 27 ZW0A0102407 1 20010526 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND CORROSION ON MEMBRANE TOP AND BOTTOM AROUND HOLES AT STA 1250 TO 1308, OUTBOARD OF NUMBER 1 T RACK. INSTALLED REPAIR PER SRM 51-70-04. 2 L 7 2 4F RT A6WE 2001062700153 20010627 00153 WP 2001 6 27 ZW0A0102408 1 20010526 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND CORROSION ON MEMBRANE AT STA 860 TO 905, LT SIDE OTBD OF NUMBER 1 TRACK. CUT OUT CORRODED AR EA AND INSTALLED DOUBLER PER SRM 51-70-4. 2 L 7 2 4F RT A6WE 2001062700154 20010627 00154 WP 2001 6 27 ZW0A0102409 1 20010529 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND CORROSION ON FORMER AT STA 1271 AT LONGERON 30, 25R, 26R, AND 27R. REMOVED CORROSION AND REP AIRED PER SRM 53-03, FIG Q, P, 4E AND 4J. 2 L 7 2 4F RT A6WE 2001062700155 20010627 00155 WP 2001 6 27 ZW0A0102410 1 20010527 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND MEMBRANE BADLY CORRODED AT STA 541, APPROX 3 INCHES OUTBOARD OF LT OUTBOARD FLOOR TRACK. FAB RICATED AND INSTALLED NEW MEMBRANE, STA 541 TO 560. 2 L 7 2 4F RT A6WE 2001062700156 20010627 00156 WP 2001 6 27 ZW0A0102411 1 20010527 A 5320 ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND CORROSION IN FLOOR STRUCTURE AT STA 219, 13 INCHES LBL, 9 IN RBL. FABRICATED NEW ANGLE PER D RAWING 9936535. INSTALLED AND SEALED PER SRM 51-30-02 AND 51-20-0. 2 L 7 2 4F RT A6WE 2001062700157 20010627 00157 WP 2001 6 27 ZW0A0102501 1 20010530 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 926TW 49356 THE EGRESS LIGHTS DID NOT COME ON FROM ROW 1 TO 7. REPLACED THE DISCHARGED BATTERY PACK P/N 5822-1, REPLACED ONE BURNED OUT LAMP P/N 36262-4, AND CLEANED MOISTURE FROM THE TRACK. CHECK-C 8-29-00 STL. 2 L 7 2 4F A6WE 2001062700158 20010627 00158 WP 2001 6 27 ZW0A0102502 1 20010529 A 5320 CLIP DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT IN E AND E COMPT FOUND LIGHT CORROSION INSIDE INSPECTION HOLE IN AFT LT CORNER OF DOOR FRAME, STA 1 59. REMOVED CORRODED CLIP. FABRICATED NEW CLIP PER SPM 6-70-01 AND DRAWING 9911550 USING EXTRUSION S1642726. INSTALLE D NEW ANGLE PER DRAWING 9911550. INSTALLED WITH HI-LOKS PER SRM 51-30-5. TREATED PER SRM 51-010-7 PAGE 46 ITEM 3. 2 L 7 2 4F RT A6WE 2001062700159 20010627 00159 WP 2001 6 27 ZW0A0102503 1 20010529 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND CORROSION ON MEMBRANE AT STA 200 TO 204, RBL 44 INCHES TO RBL 52 INCHES, RBL 24 IN TO RBL 44 INCHES, AND LBL 24 IN TO RBL 24 INCHES. REMOVED CORROSION PER SPM 6-80-01 AND TREATED PER SRM 51-10-3. 2 L 7 2 4F RT A6WE 2001062700160 20010627 00160 WP 2001 6 27 ZW0A0102504 1 20010529 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT CORRODED AT STA 200, RBL 10 INCHES TO RBL 48 IN. INSTALLED NEW ANGLE PER SRM 51-30-3. SEALED PER SRM 51-20-0. 2 L 7 2 4F RT A6WE 2001062700161 20010627 00161 NM 2001 6 27 GAIA01197ST 1 20010611 A 5300 FRAME BOEING 727 727251 138408H NM BS 1166 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT RIGHT BS 1166 FRAME FAIL/SAFE CHORD CRACKED AT STRINGER 9R . ACCOMPLISHED FUSELAGE FRAME REPAIR BS 1166 RIGHT STRINGER 9R IAW B727 SRM 51-40-3 FIG 1. (M) 2 L 7 3 4F A3WE 2001062700162 20010627 00162 NM 2001 6 27 GAIA01196ST 1 20010611 A 5300 FRAME BOEING 727 727251 138408H NM BS 1166 DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT LEFT BS 1166 FRAME DENTED AT WL 212. ACCOMPLISHED FUSELAG E FRAME REPAIR BS 1166 LEFT WL 212 IAW B727 SRM 53-10-4 FIG 2. (M) 2 L 7 3 4F A3WE 2001062700163 20010627 00163 NM 2001 6 27 GAIA01195ST 1 20010611 A 5300 SKIN BOEING 727 727251 138408H NM BS 215-227 DEFORMED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT DEFORMED FUSELAGE SKIN BS 215-227 STRINGER 25-26R. ACCOMP LISHED FUSELAGE SKIN REPAIR BS 215-227 STRINGER 25-26R IAW B727 SRM 53-30-3 FIG 3A. (M) 2 L 7 3 4F A3WE 2001062700164 20010627 00164 NM 2001 6 27 GAIA01194ST 1 20010611 A 5500 WEB BOEING 727 727251 138408H NM LOWER RUDDER CHAFED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT TOP TRAILING EDGE OF LOWER RUDDER HAS METAL CHAFED THROUGH TOP. ACCOMPLISHED LOWER RUDDER CLOSE OUT WEB REPAIR IAW B727 SRM 55-30-1 AND 51-30-2. (M) 2 L 7 3 4F A3WE 2001062700165 20010627 00165 NM 2001 6 27 GAIA01193ST 1 20010611 A 5300 WEB BOEING 727 727251 138408H NM BS 1323 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT LEFT VENTRAL STAIRS TORQUE BOX AT BS 1323 AFT LIGHTING HOL E HAS A CRACK ON LOWER HOLE EDGE. ACCOMPLISHED AFT AIRSTAIR LEFT LOWER TORQUE BOX WEB REPAIR BS 1323 IAW B727 SRM 51-40 -2 FIG 1. (M) 2 L 7 3 4F A3WE 2001062700166 20010627 00166 NM 2001 6 27 GAIA01190ST 1 20010611 A 5300 SEAT TRACK BOEING 727 727251 138408H NM BS 690-740 A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT BS 700 RBL 45.50 SEAT TRACK HAS ELONGATED LOCK HOLES. ACC OMPLISHED BS 690-740 RBL 45.50 SEAT TRACK REPAIR IAW B727 SRM 53-10-5 FIG 1. (M) 2 L 7 3 4F A3WE 2001062700167 20010627 00167 NM 2001 6 27 GAIA01189ST 1 20010611 A 5300 WEB BOEING 727 727251 138408H NM BS 178 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT BS 178 B/H WEB IS CRACKED AT FASTENER LOCATION WL 198 RBL 3 AND WL 201 STIFFENERS ARE CRACKED AT RBL 8. ACCOMPLISHED BS 178 BULKHEAD WEB REPAIR BS 178 WL 198 RBL 3 IAW B727 SRM 53-10-9 FIG 4 AND REPLACED STIFFENERS IAW B727 SRM 51-40-4 AND 51-30-2. (M) 2 L 7 3 4F A3WE 2001062700168 20010627 00168 NM 2001 6 27 GAIA01188ST 1 20010611 A 5300 FRAME BOEING 727 727251 138408H NM BS 360 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT BS 360 FRAME INBOARD FLANGE CHORD CRACKED IN THE RADIUS AT STRINGER 9L. ACCOMPLISHED FUSELAGE FRAME REPAIR BS 360 STRINGER 9L IAW B727 SRM 53-10-4 FIG 2. (M) 2 L 7 3 4F A3WE 2001062700169 20010627 00169 NM 2001 6 27 GAIA01187ST 1 20010611 A 5300 SEAT TRACK BOEING 727 727251 138408H NM BS 690 A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT SEAT TRACK BS 720C LBL 45.50 HAS ELONGATED LOCK HOLES. AC COMPLISHED SEAT TRACK REPAIR BS 690-740 LBL 45.50 IAW B727 SRM 53-10-5 FIG 1. (M) 2 L 7 3 4F A3WE 2001062700170 20010627 00170 NM 2001 6 27 USAASB01157 1 20010603 A 3350 20121 POWER SUPPLY BOEING 737 7374B7 1384702 NM MID CABIN FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 BDL - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT ROWS 11 TO 12 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PO WER SUPPLY. OPS CHECK GOOD PER MM. (M) 2 L 7 2 4F RT A16WE 2001062700171 20010627 00171 NM 2001 6 27 USAASB01158 1 20010604 A 3350 20131A BATTERY PACK BOEING 737 7374B7 1384702 NM FWD CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 780AU 24997 BDL - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT ROWS 1 AND 2 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BAT TERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001062700172 20010627 00172 NM 2001 6 27 USAASB01159 1 20010604 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM FWD CABIN OVERHEATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 23704 CLT - FLT 461 - PILOT REPORTED THAT THE AIRCRAFT ARRIVED AT THE GATE WITH AN ELECTRICAL/BURNING ODOR IN THE CABIN. MAIN TENANCE FOUND TWO FORWARD EMERGENCY LIGHT BATTERY PACKS EXCESSIVELY HOT/OVERHEATED. REMOVED AND REPLACED BOTH UNITS. R AN ENGINES AND PACKS. NO SMOKE OR ODOR NOTED. (M) 2 L 7 2 4F RT A16WE 2001062700173 20010627 00173 EU 2001 6 27 USAA010588 1 20010519 A 5300 FRAME FOKKER F28 F28MK0100 4990807 EU CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 887US 23422 11349 PIT - FOUND FRAME CRACKED 1.25 INCH, LEFT SIDE TOP OF OBLIQUE FRAME 67.2. TEMPORARY REPAIR WITH STOP DRILL PER EA 71082 AND SRM 51-22-01. (M) 2 L 7 2 4F RT 2001062700174 20010627 00174 NM 2001 6 27 USAA010551 1 20010403 A 5300 STRINGER BOEING 737 7373B7 1384580 NM BS 380-400 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 22953 CLT - FOUND STRINGER DENTED 3 INCH AREA, BS 380-400, STRINGER 25R. INSTALLED DOUBLER REPAIR PER SRM 53-00-03, DETAIL V. (M) 2 L 7 2 4F RT A16WE 2001062700175 20010627 00175 EU 2001 6 27 USAAF01030 1 20010529 A 3350 M210D4N003 RELAY FOKKER F28 F28MK0100 4990807 EU COCKPIT FAULTY A USAA K NONE P NO WARNING INDICATION AP APPROACH 1 EA 19 888US 11357 CLT - THE EMERGENCY EXIT LIGHTS IN CABIN DID NOT COME ON WHEN GEAR WAS EXTENDED. MAINTENANCE REPLACED RELAY K3982A. OP S CHECKED OK. (M) 2 L 7 2 4F RT 2001062700176 20010627 00176 SO 2001 6 27 SIMA20011402 1 20010517 A 5300 AL2024T3 SKIN EMB 145 EMB145LR SO CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 638AE 145172 ABI - MAINTENANCE FOUND CORROSION IN FLOOR CENTER BEAM AT FRAME 20 AND 22. CORROSION WAS REMOVED AND A DOUBLER WAS INST ALLED IAW EMB GST-159/01. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001062700177 20010627 00177 SO 2001 6 27 SIMA20011401 1 20010516 A 5300 SKIN EMB 145 EMB145LR SO CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 638AE 145172 ABI - OMEGA BEAM AT FRAME 20 WAS FOUND TO BE OUT OF LIMITS AFTER REMOVAL OF CORROSION. DAMAGE WAS REPAIRED IAW EMB SRM 53-21-01. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001062700178 20010627 00178 SO 2001 6 27 SIMA20011371 1 20010517 A 3200 0132AFU1 SENSOR EMB 145 EMB145LR SO INOPERATIVE A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 620AE 145102 DFW - FLT 3759 - CREW REPORTED A NR 2 HOT BRAKE INDICATION ON TAKEOFF ROLL. TAKEOFF WAS ABORTED AND AIRCRAFT WAS RETURN ED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE LEFT INBOARD BRAKE TEMP SENSOR IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001062700179 20010627 00179 EU 2001 6 27 SIMA200114901 1 20010529 A 3200 D228830001 SWITCH AEROSP ATR42 ATR42300 8680920 EU RT MAIN GEAR INOPERATIVE A SIMA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SW 21 314AM 314 MCO - FLT 5410 - AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. CREW FOUND LDG BREAKER OUT. LANDING GEAR PUT ON ME L AT THIS TIME. MAINTENANCE REMOVED AND REPLACED THE RIGHT MLG PROXIMITY SWITCH IAW ATR MM. OPS CHECK WAS GOOD AND AIRC RAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001062700180 20010627 00180 NM 2001 6 27 USAASB01162 1 20010605 A 3350 20131A BATTERY PACK BOEING 737 7372B7 1384560 NM MID CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 287AU 23134 BDL - MAINTENANCE FOUND THE MID-LEVEL EMERGENCY SEAT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PA CK. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 2001062700181 20010627 00181 NM 2001 6 27 USAASB01154 1 20010602 A 3350 210310005 FUSE BOEING 737 7372B7 1384560 NM FWD CABIN BLOWN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 272AU 22884 TPA - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE FORWARD ENTRY DOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND THE FUSE IN THE POWER SUPPLY BLOWN. REMOVED AND REPLACED FUSE. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 2001062700182 20010627 00182 NM 2001 6 27 USAASB01139 1 20010517 A 3350 S106 BATTERY BOEING 737 7372B7 1384560 NM PAX CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 279AU 22891 IAD - THE EMERGENCY LIGHT ABOVE THE AFT RIGHT SERVICE DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BA TTERY PACK. (M) 2 L 7 2 4F A16WE 2001062700183 20010627 00183 NM 2001 6 27 USAASB01131 1 20010510 A 3350 6104789 BATTERY BOEING 737 7372B7 1384560 NM AFT CARGO BAY DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 277AU 22889 SYR - THE AFT RIGHT SERVICE DOOR EMERGENCY EVACUATION LIGHT WAS DIM. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A16WE 2001062700184 20010627 00184 CE 2001 6 27 RU3A0103 1 20010515 A 2800 600600144 TUBE LEAR 60 60LEAR 5170707 CE ELBOW CHAFED A RU3A K NONE O OTHER IN INSP/MAINT 1 SW 15 58 057 DURING C-CHECK INSPECTION, THE RIGHT MOTIVE FLOW LINE WAS FOUND CHAFFING THE FORWARD ENGINE BLEED AIR LINE IN THE PYLON AREA. THE TWO LINES WERE RUBBING METAL TO METAL. THIS FUEL LINE RUNS ABOUT 300 PSI AND THE BLEED LINE IS ABOUT 500 DEG REES. IPC REFERENCE 28-24-26 ITEMS NR 8 AND 34 OR 45. NOTED NO PROBLEM IN LEFT PYLON. APPARENT CAUSE, LINES AT INSTAL LATION CAN BE INSTALLED BACKWARDS THUS CAUSING INTERFERENCE. BOTH LINES ARE PROPERLY INSTLALED WITH ELBOW AT ENGINE FIR EWALL. (M) 2 L 7 2 4F RT A10CE 2001062700185 20010627 00185 EA 2001 6 27 ASOA010359 1 20010411 A 7900 4054T13P01 BEARING CNDAIR CL600 CL6002B19 EA RT ENGINE FAILED A ASOA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 11 843AS 7310 DURING FLIGHT FROM AUS TO ATL, CREW RECEIVED A NR 2 ENGINE 'LOW OIL PRESS' LIGHT. CREW SHUT DOWN RIGHT ENGNIE FOLLOWING QRH AND DECLARED AN EMERGENCY. AIRCRAFT DIVERTED TO JAN AND LANDED SAFELY. MAINTENANCE PERFORMED MAGNETIC CHIP DETECT OR INSPECTION AS PER CRJ AMM 72-00-00 AND DETERMINED THE NR 2 ENGINE TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND REPLA CED THE RIGHT ENGINE. TEARDOWN REPORT FROM LUFTHANSA STATE THE ENGINE FAILURE WAS DUE TO A PTO DUPLEX BEARING FAILURE. THE BEARING CAGE WAS DAMAGED AND SOME BEARING BALLS WERE MISSING. (M) 2 L 7 2 4F RT A21EA 2001062800001 20010628 00001 EU 2001 6 28 S01629020 1 20010613 A 2900 HYDRAULIC SYSTEM AIRBUS A300 A300F4622R 3930360 EU PWA 4158 PW4158 NE # 1 ENG, # 2 ENG W SAJF O OTHER O OTHER TO TAKEOFF 1 WP 03 536 B-18573 DURING T/O,GEAR RETRACT ECAM WARNING MSG S 2 L 7 2 4F 4 F RT A35EU E24NE 2001062800002 20010628 00002 SO 2001 6 28 C2XA01IA276 1 20010502 A 5700 12017063009 SUPPORT EMB 120 EMB120ER 3260203 SO CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 40717 120133 SJK - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, TWO (2) WING SKIN SUPPORTS WERE FOUND TO BE CRACKED AT RIB 20 OF TH E LEFT HAND WING. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001062800003 20010628 00003 SO 2001 6 28 C2XA01IA277 1 20010502 A 5700 12017054607 SUPPORT EMB 120 EMB120ER 3260203 SO CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 40717 120133 SJK - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUR (4) SKIN SUPPORTS WERE FOUND TO BE CRACKED IN THE LEFT WING AT RIB 8. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE . 2 L 7 2 4T RT A31SO 2001062800004 20010628 00004 SO 2001 6 28 C2XA01IA279 1 20010504 A 5300 12019594001 STRAP EMB 120 EMB120ER 3260203 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 40717 120133 SJK - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE REINFORCING STRAP AT FRAME 38 WAS FOUND TO BE CORRODED. MAINTEN ANCE REMOVED AND REPLACED THE AFFECTED STRAP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001062800005 20010628 00005 SO 2001 6 28 C2XA01IA281 1 20010426 A 5280 12013959001 SKIN EMB 120 EMB120ER 3260203 SO CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 40717 120133 SJK - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE INTERNAL SKIN OF THE RIGHT HAND AFT NOSE LANDING GEAR DOOR WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A DOUBLER REPAIR ON THE AFFECTED DOOR, AND THE AIRCRAFT WAS APPROVED FOR RETU RN TO SERVICE. 2 L 7 2 4T RT A31SO 2001062800006 20010628 00006 SO 2001 6 28 C2XA01IA282 1 20010425 A 3350 1317 BULB EMB 120 EMB120ER 3260203 SO FUSELAGE BURNED OUT A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 40717 120133 SJK - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE RIGHT HAND OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE . MAINTENANCE REMOVED AND REPLACED THE AFFECTED BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001062800007 20010628 00007 WP 2001 6 28 MWEA011003 1 20010627 A 5230 3914025501N FITTING DOUG DC9 DC914 3022034 WP AFT CARGO DOOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 AFT CARGO DOOR #1 BEAM FORWARD END FITTING HAS LIGHT TO MODERATE CORROSION PRESENT. -- INSTALLED NEW FITTING. 2 L 7 2 4F A6WE 2001062800008 20010628 00008 WP 2001 6 28 MWEA011004 1 20010627 A 5310 991224661 SHEAR TIE DOUG DC9 DC914 3022034 WP STATION 859 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 SHEAR TIE CRACKED AT STATION 859 AT LONGERON 18 LEFT. -- CUT AND REMOVED CRACKED SECTION OF FORMER, FABRICATED AND INS TALLED NEW SECTION OF FORMER, REPAIR SPLICE AND ANGLE. 2 L 7 2 4F A6WE 2001062800009 20010628 00009 WP 2001 6 28 MWEA011002 1 20010627 A 5230 4920233503N FITTING DOUG DC9 DC914 3022034 WP FWD CARGO DOOR WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FORWARD CARGO DOOR AFT/MIDDLE STOP FITTING IS WORN. -- LOCATED, DRILLED AND INSTALLED NEW STOP FITTING. 2 L 7 2 4F A6WE 2001062800010 20010628 00010 EU 2001 6 28 20010604CW011 1 20010510 A 4980 4AS6900620501 DUCT ISRAEL GALAXY GALAXY 4500307 EU APU MISALIGNED D K NONE O OTHER IN INSP/MAINT 1 GL 19 62GX 20 20 031 THE FLEX COUPLER COULD NOT BE INSTALLED DUE TO MISALIGNMENT OF APU GENERATOR EXHAUST DUCT AND ADJOINING DUCT ON RIGHT HA ND SIDE OF FUSELAGE. 2 L 7 2 4F RT A53NM 2001062800011 20010628 00011 EU 2001 6 28 20010604CW010 1 20010510 A 4980 4AS6900620501 DUCT ISRAEL GALAXY GALAXY 4500307 EU APU MISALIGNED D UO2R K NONE O OTHER IN INSP/MAINT 1 GL 19 60GX 24 24 028 THE FLEX COUPLER COULD NOT BE INSTALLED DUE TO MISALIGNMENT OF GENERATOR DUCT (APU) AND ASSOCIATED DUCT ON RIGHT HAND SI DE OF FUSELAGE. 2 L 7 2 4F RT A53NM 2001062800017 20010628 00017 NE 2001 6 28 20010606CW005 1 20010510 A 6220 6510311020102 HINGE PIN SKRSKY S64 S64F NE M/R HEAD CRACKED A JYDR K NONE O OTHER IN INSP/MAINT 1 NM 09 223AC 999 64086 S-64F MAIN ROTOR HEAD HINGE PINS DO OCCASIONALLY CRACK FROM DAMPER NUT SAFETY HOLES (APPROX. 15 PERCENT OF THE TIME), BU T TYPICALLY THE CRACKS TRAVEL OUTBOARD TO THE EDGE OF THE HINGE PIN. HINGE PIN SN A041-00236 CRACKED INBOARD THROUGH TH E THREADS INTO THE THREAD RELIEF AND STARTED AROUND THE HINGE PIN. APPROXIMATE LENGTH OF CRACK AROUND THE THREAD RELIEF IS .60 INCHES. 2 G 7 2 4U H6EA 2001062800018 20010628 00018 NE 2001 6 28 20010606CW008 2 20010505 A 7261 SEAL DOUG MD900 MD900 3027375 NM PWA PW206 PW206A NE NR 1 ENGINE FAILED E EGRA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 17 900LF 90000022 EXCESSIVE OIL CONSUMPTION NR 1 ENGINE. SMOKE NOTED EMANATING FROM FUEL PIPE, BEFORE AND AFTER SHUTDOWN. INTERNAL OIL S EAL FAILURE. ENGINE REMOVED AND RETURNED TO MFG FOR REPAIR. 1 G 7 2 3U 3 U NC H19NM E42NE 2001062800019 20010628 00019 SO 2001 6 28 ASOA01067 1 20010603 A 2150 22045402 ACM EMB 120 EMB120 3260201 SO AC BAY MALFUNCTIONED A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 257AS 120126 FLT 4916 - DURING FLIGHT FROM HOU TO DFW, CAPTAIN REPORTED BOTH PACKS ONLY PRODUCING WARM TO HOT AIR AND A STORNG BURNIN G SMELL OF PLASTIC. AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED LEFT PACK ACM. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001062800020 20010628 00020 SO 2001 6 28 ASOA01070 1 20010604 A 3350 D36604001 BATTERY PACK EMB 120 EMB120 3260201 SO CABIN FAILED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 238AS 22156 120053 DURNIG HANGAR CHECK, MAINTENANCE FOUND NR 2 EMERGENCY LIGHT BATTERY PACK FAILED AFTER 5 SECONDS. MAINTENANCE REMOVED AN D REPLACED NR 2 EMERGENCY LIGHTING BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001062800021 20010628 00021 NM 2001 6 28 UIEA01061 1 20010611 A 2100 60B0002656 DOOR ACTUATOR BOEING 747 7472D7B 1384803 NM NR 2 PACK FAILED A UIEA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 527MC 22471 NR 2 AIR CONDITIONING PACK OVERHEATED WITH A DOOR OUT OF SEQUENCE INDICATION. CAUSED FUMES IN AIR CONDITIONING SYSTEM. MANUALLY POSITIONED NR 2 PACK INLET DOOR CLOSED. REPLACED INLET DOOR ACTUATOR. (M) 2 L 7 4 4F RT A20WE 2001062800022 20010628 00022 SO 2001 6 28 SIMA200115803 1 20010607 A 7820 83990137 SWITCH EMB 135 EMB135LR SO NR 1 FAILED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 700LE 145156 DFW - FLT 3423 - NR 1 THRUST REVERSER DISAGREE DURING TAKEOFF. ABORTED TAKEOFF. REMOVED AND REPLACED LOWER INBOARD UPP ER OUTBOARD STOW SWITCH IAW EMB AMM 78-34-01-000. OPS CHECK GOOD. (M) 2 L 7 2 4F RT TOOO11AT 2001062800023 20010628 00023 EU 2001 6 28 SIMA200115506 1 20010604 A 2500 B0200124 FLASHLIGHT AEROSP ATR72 ATR72212A 8680902 EU CABIN FAILED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 550LL 550 DFW - FLT 3551 - AFT CABIN EMERGENCY FLASHLIGHT INOPERATIVE. ISSUED MEL. REMOVED AND REPLACED FLASHLIGHT IAW AMM. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 2001062800024 20010628 00024 EU 2001 6 28 SIMA200114403 1 20010524 A 5300 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 340B270 SAW - DURING MBV-1 INSPECTION MAINTENANCE REPORTED RIGHT AFT INBOARD AND LEFT AFT INBOARD SEAT TRACKS CORRODED. MAINTEN ANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001062800025 20010628 00025 EU 2001 6 28 SIMA20011425 1 20010522 A 2500 P4010021 FLASHLIGHT AEROSP ATR72 ATR72212A 8680902 EU CABIN INOPERATIVE A SIMA O OTHER O OTHER IN INSP/MAINT 1 SW 21 499AT 499 DFW - FLT 3760 - FLIGHT ATTENDANT REPORTED THE FORWARD CABIN EMERGENCY FLASHLIGHT IS INOPERATIVE. FLASHLIGHT PUT ON MEL AT THIS TIMES. MAINTENANCE REPLACED THE FLIGHT ATTENDANTS FLASHLIGHT AND RESTORED MEL. AIRCRAFT WAS RETURNED TO SERVI CE. (M) 2 H 7 2 4T RT A53EU 2001062800026 20010628 00026 EU 2001 6 28 SIMA20011391 1 20010508 A 5300 S5367120500605 SKIN AEROSP ATR72 ATR72212 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 SAW - DURING MBV-1 INSPECTION MAINTENANCE REPORTED A DENT IN THE LEFT SIDE OF THE FUSELAGE BETWEEN FRAMES 31 AND 32 AND STRINGERS 12 AND 13. MAINTENANCE REPAIRED THE DENT IAW SRM 53-00-00 FIGURE 405. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001062800027 20010628 00027 EU 2001 6 28 SIMA20011433 1 20010510 A 5315 S5367240720201 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAM 38 AND 40 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAMS IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001062800028 20010628 00028 EU 2001 6 28 SIMA20011434 1 20010510 A 5320 S5367800920102 FLOOR SUPPORT AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE RIGHT FLOOR SUPPORT BETWEEN FRAMES 36 AND 38 CORRODED, AND RIGHT FLOOR SUPPORT BETWEEN FRAMES 38 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORTS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001062800029 20010628 00029 EU 2001 6 28 SIMA20011435 1 20010510 A 5320 S5367800826801 FLOOR SUPPORT AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE LEFT FLOOR SUPPORT BETWEEN FRAMES 38 AND 39 CORRODED, AND LEFT F LOOR SUPPORT BETWEEN FRAMES 39 AND 40 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORTS IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001062800030 20010628 00030 EU 2001 6 28 SIMA20011193 1 20010429 A 6100 SFA13U1P0A BLADE AEROSP ATR42 ATR42300 8680920 EU NR 1 PROP A SIMA D RETURN TO BLOCK E VIBRATION/BUFFET CL CLIMB 1 SW 21 971NA 017 MIA - FLT 5257 - DURING CLIMB-OUT, CREW NOTICED UNUSUAL PROPELLER VIBRATION. REDUCING POWER ON NR 1 ENGINE REDUCED THE VIBRATION. MAINTENANCE REMOVED AND REPLACED THE NR 1 BLADE ON THE NR 1 PROPELLER IAW ATR MM. OPS WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001062800031 20010628 00031 NM 2001 6 28 DL72S010908 1 20010529 A 5711 SPAR BOEING 727 727232 1384082 NM WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 532DA 22045 AT HMV FOUND FAST SPAR LWR CHORD - CRACK, REPAIR LOOSE LOC AT LWR END OF NR 7 SPOILER ACT FITTING. REMOVED NR 6/7 SPOIL ER MOUNT ARM, REMOVED DAMAGED SECTION OF BEAM PER MM 57-55-00-08 FIG 805, FABD AND DRILLED UP PARTS PER MM 57-55-00-08 F IG 805, OK TO INSTALL, INSTALLED REPAIR PER MM 57-55-00-08 AND REINSTALLED SUPPORT ARM. 2 L 7 3 4F A3WE 2001062800032 20010628 00032 NM 2001 6 28 DL757010856 1 20010528 A 2910 000AE906D052 HYDRAULIC LINE BOEING 757 757232 1384965 NM HYD SYSTEM LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 647DL 24218 AFTER TAKEOFF GEAR DOORS LIGHT AND ADVISORY MESSAGE ON WHEN GEAR RAISED. GEAR RECYCLED, LIGHT STILL ON. FLT ATTN REPOR TS VIBRATION IN FLOOR NEAR GEAR DOOR AREA. FOUND FLEX HYD LINE LEAKING ABOVE RT MLG. MADE APPROVED HYD REPAIR. INSTAL LED TEMP HYD LINE PER MM 20-10-09, TIME LIMITED 350 HRS. LEAK CKS GOOD. P/N 326201061 HOSE P/N 00AE90-6D052 FWD TO MCO /PLAC. 2 L 7 2 4F RT A2NM 2001062800033 20010628 00033 2001 6 28 DL757010870 4 20010530 A 2565 D30656132 SLIDE BOEING 757 757232 1384965 NM R 3 DOOR DEPLOYED A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 6710E 30482 3R DOOR SLIDE DEPLOYED. REPLACED 3R DOOR SLIDE. 2 L 7 2 4F RT A2NM 2001062800034 20010628 00034 NM 2001 6 28 DL757010871 1 20010530 A 2121 6067723 FAN BOEING 757 757232 1384965 NM CABIN DEFECTIVE A DALA H DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 614DL 22821 AFTER T/O FLT ATTENDANTS REPORT ELECTRICAL FUMES IN MID CABIN. FUMES SUBSIDED THEN RT RECIRC FAN MSG APPEARED ON EICAS. TURNED OFF RT RECIRC FAN ON OVERHEAD PANEL. NOTIFIED MCC. PULLED C/B P23. CONTRACT MTC REPLACED RT RECIRC FAN. FAI NT ODOR FROM FAN. 2 L 7 2 4F RT A2NM 2001062800035 20010628 00035 NM 2001 6 28 DL757010891 1 20010602 A 2530 831620403MODA OVEN BOEING 757 757232 1384965 NM GALLEY SMOKE A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 684DA 27104 STRONG ELEC SMOKE ODOR AND LIGHT SMOKE DETECTED FROM FIRST GALLEY OVEN AREA. REPLACED F/C OVEN. 2 L 7 2 4F RT A2NM 2001062800036 20010628 00036 NM 2001 6 28 DL757010893 1 20010602 A 2722 3800022107 ACTUATOR BOEING 757 757232 1384965 NM RUDDER LEAKING A DALA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 6705Y 30397 LT HYD QTY EICAS MSSG ASSOCAITED WITH L HYD QTY AT .45. USED POM PROCEDURE AND QTY STILL DECREASED SO BOTH LT ENG PUMP AND LT ELEC PUMP WERE TURNED OFF. QTY LEAKED TO .20. FOUND RUDDER RATIO CHANGER ACTUATOR LEAKING. REPLACED RUDDER RAT IO ACTUATOR PER M/M. LEAK CHECK OKAY. INSPECTION COMPLETED. RCCA INSTALLATION GOOD AND M/M REQUIRED TEST GOOD. 2 L 7 2 4F RT A2NM 2001062800037 20010628 00037 NM 2001 6 28 DL757010895 1 20010602 A 3350 LIGHT BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 6705Y 30397 EMERGENCY LIGHTS AT 45 DEF INOP. REPLACED LIGHT ASSY, OPS CKS GOOD. 2 L 7 2 4F RT A2NM 2001062800038 20010628 00038 NM 2001 6 28 DL757010896 1 20010602 A 3350 BPS73 BATTERY PACK BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 658DL 24420 IN-SEAT ESCAPE PATH LIGHTS INOP FROM 19FED THRU 26FED. REPLACED BATTERY PACK AND RACK M9002. 2 L 7 2 4F RT A2NM 2001062800039 20010628 00039 NM 2001 6 28 DL757010903 1 20010601 A 5330 143N340058 SKIN BOEING 757 757* NM FUSELAGE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 900PC 28446 THE FUSELAGE SKIN WAS FOUND GOUGED IN THE UPPER SKIN OF THE STRINGER 26R SKIN LAP SPLICE AT FS 470. THE GOUGE WAS REMOV ED WITH A CUTOUT IN THE UPPER SKIN. THE GOUGE WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 380877- 14, REV A. 2 L 7 2 4F RT A2NM 2001062800040 20010628 00040 NM 2001 6 28 DL757010904 1 20010601 A 5330 146N35317 SKIN BOEING 757 757* NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 900PC 28446 THE SKIN AROUND THE TWO AIRFONE ANTENNA CUTOUTS AT FS 1510 BETWEEN STRINGERS 28R & 28L WAS FOUND CORRODED AND WITH SEVE RAL KNIFE EDGE FASTENERS INSTALLED. THE DAMAGED AREAS WERE TRIMMED OUT TO REMOVE ALL CORROSION AND BAD COUNTERSINKS. BO TH CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 380910-14, REV A. 2 L 7 2 4F RT A2NM 2001062800041 20010628 00041 NM 2001 6 28 DL757010906 1 20010601 A 5330 141N32163 SKIN BOEING 757 757232 1384965 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 602DL 22809 THE FUSELAGE SKIN WAS FOUND CREASED JUST FWD OF THE E&E COMPARTMENT DOOR CUTOUT AT RBL 2.3 BETWEEN FS 223 & 239. THE DA MAGE WAS CUTOUT OF THE SKIN AND REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS PER ER/A 380763-14, REV A. 2 L 7 2 4F RT A2NM 2001062800042 20010628 00042 NM 2001 6 28 DL757010907 1 20010601 A 5310 146N851210 DOOR FRAME BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 602DL 22809 THE LOWER DOOR SILL CHORD OF THE C2 DOOR CUTOUT WAS CORRODED AND REQUIRED REPLACEMENT. TO ALLOW REMOVAL AND INSTALLATIO N OF A NEW CHORD, THE OUTER CHORD OF THE FS 1440 DOOR OPENING FRAME WAS CUT NEAR STRINGER 27R AND THE LOWER SECTION REMO VED. A NEW SECTION WAS LATER INSTALLED AND SPLICED IN WITH TWO ALUMINUM REPAIR ANGLES INSTALLED PER ER/A 380664-14, REV A. 2 L 7 2 4F RT A2NM 2001062800043 20010628 00043 NM 2001 6 28 DL764010819 1 20010519 A 7930 WIRE BOEING 767 767432ER 1385134 NM OIL INDICATING CHAFED A DALA O OTHER N FALSE WARNING CR CRUISE 1 SO 27 827MH 29698 INTERMITTENT OIL PRESSURE INDICATIONS. FOUND FAN AIR DUCT CRACKED AND CHAFING ON WIRES FOR OIL PRESSURE SWITCH. REPAIR ED DUCT AND WIRING. 2 L 7 2 4F RT A1NM 2001062800044 20010628 00044 NM 2001 6 28 DL767010818 1 20010518 A 5315 146T51411 FLOORBEAM BOEING 767 767232 1385132 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 106DA 22218 CORROSION FOUND ON THE STA 1480 FLOORBEAM AT THE RT O/B FRAME ATTACHMENT LOCATION AND AT RBL 72 AFT UPPER FLANGE. ER/A 397554-14. 2 L 7 2 4F RT A1NM 2001062800045 20010628 00045 NM 2001 6 28 DL767010883 1 20010531 A 5311 148T27405004 FRAME BOEING 767 767232 1385132 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 102DA 22214 INSPECTION OF THE FS 1809.5 BULKHEAD CHORDS PER BAC S/B 767-53-0078 AND AD 2001-09-13 REVEALED A CRACK IN THE AFT CHORD, 2 FASTENER HOLE CRACKS IN THE FWD CHORD, AND A FASTENER HOLE CRACK IN THE MID CHORD. THE AFT CHORD WAS REPLACED, THE F WD CHORD CUT AND SPLICED PER THE S/B, AND THE MID CHORD HOLE OVERSIZED AND BUSHED. THE WORK WAS ACCOMPLISHED PER ER/A 3 80849-14AD, REV B. 2 L 7 2 4F RT A1NM 2001062800046 20010628 00046 NM 2001 6 28 DL76K010890 1 20010601 A 3350 HARNESS BOEING 767 767332 1382001 NM CABIN DAMAGED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 178DZ 30596 SEAT 2 EF EMERGENCY LIGHTS INOP. REPAIRED DAMAGED SEAT HARNESS. 2 L 7 2 4F RT A1NM 2001062800047 20010628 00047 NM 2001 6 28 DL76L010794 1 20010518 A 2821 FILTER BOEING 767 767332 1382001 NM NR 2 ENGINE CLOGGED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 186DN 27962 ACFT HAD AIR TURNBACK, RT ENGINE FUEL FILTER BYPASS. REPLACED FUEL FILTER. 2 L 7 2 4F RT A1NM 2001062800048 20010628 00048 NM 2001 6 28 DL76L010838 1 20010523 A 5330 141T33111 SKIN BOEING 767 767332 1382001 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 184DN 27111 EXISTING UNIDENTIFIED REPAIR AT DOOR STA 89 AND S8L WAS REMOVED AND NEW REPAIR PER SRM INSTALLED. ER/A 364286-14 REV B. 2 L 7 2 4F RT A1NM 2001062800049 20010628 00049 NE 2001 6 28 DL76L010848 2 20010526 A 7320 8010003 FMU BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE FAILED A DALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 27 188DN 27583 F24922 FLUCTUATING PARAMETERS ON NR 2 ENGINE AT CRUISE. REPLACED FMU. 2 L 7 2 4F 4 F RT A1NM E24NE 2001062800050 20010628 00050 NM 2001 6 28 DL76L010859 1 20010528 A 3830 LAVATORY BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 176DN 25061 DIVERTED TO CCS DUE TO LAV SYSTEMS INOP. SERVICED LAVS. 2 L 7 2 4F RT A1NM 2001062800051 20010628 00051 NM 2001 6 28 DL76L010889 1 20010601 A 2432 425404 CHARGER BOEING 767 767332 1382001 NM E/E BAY FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 173DN 24800 CREW REPORTED BATTERY CHARGER MSG WITH VOLTAGE AT 24 VOLTS. REPLACED BATTERY CHARGER. 2 L 7 2 4F RT A1NM 2001062800052 20010628 00052 NM 2001 6 28 DL76S010823 1 20010522 A 3350 20131A BATTERY PACK BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 138DL 25409 LEFT EXTERNAL EMERGENCY LIGHTS INOP AFT OF WING. REPLACED BATTERY PACK. 2 L 7 2 4F RT A1NM 2001062800053 20010628 00053 NM 2001 6 28 DL76S010854 1 20010524 A 5720 111T20005 STIFFENER BOEING 767 767332 1382001 NM CTR WNG CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 CRACKS DISCOVERED IN THE RBL AND LBL 10 VERTICAL STIFFENERS OF THE WING CENTER SECTION FRONT SPAR. THE DAMAGE IS IN THE WEB OF EACH OF THE STIFFENERS AT THE OVERWING LONGITUDINAL FLOORBEAM TO STIFFENER JOINT. ER/A 397596-14. 2 L 7 2 4F RT A1NM 2001062800054 20010628 00054 NM 2001 6 28 DL76S010873 1 20010531 A 7920 400606100194S LINE BOEING 767 767332 1382001 NM NR 1 ENGINE LEAKING A DALA C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 116DL 23275 LT ENG GEN DRIVE LIGHT CAME ON DURING T/O ROLL. DISCONTINUED T/O AT APPROX 90 KNOTS GROSS WGT 295000. FOUND OIL LINE F ROM IDG FILTER TO OIL COOLER LEAKING. REPLACED SAME. MOTORED ENG LEAK CKS OK. RAN ENG IDG. OPERATION AND INDICATION NORMAL. 2 L 7 2 4F RT A1NM 2001062800055 20010628 00055 NM 2001 6 28 DL777010806 1 20010520 A 2530 1105011 COFFEEMAKER BOEING 777 777232 1385232 NM GALLEY MALFUNCTIONED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 862DA 29734 AFT COFFEEMAKER SPARKING. REPLACED COFFEEMAKER, CHECKS OK. 2 L 7 2 4F RT T00001SE 2001062800056 20010628 00056 NM 2001 6 28 DL777010909 1 20010604 A 3350 HARNESS BOEING 777 777232 1385232 NM CABIN FAULTY A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 860DA 29951 EMERGENCY LIGHTS 1-6 LEFT AND RIGHT IN WILL NOT TEST. FOUND FUSE IN EMERGENCY LIGHT PACK BAD. TROUBLESHOT TO 4G AFT LI GHT ASSY. TRIED NEW ONE, NO HELP. REPLACED SEAT HARNESS. 2 L 7 2 4F RT T00001SE 2001062800057 20010628 00057 NM 2001 6 28 DL78K010796 1 20010518 A 3350 767 LIGHT BOEING 737 737832 13844CF NM LT WING INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 397DA 30537 LEFT WING AFT LOWER FILLET EMERGENCY LIGHT INOP. RELAMPED SAME, OPS CKS GOOD. 2 L 7 2 4F RT A16WE 2001062800058 20010628 00058 NM 2001 6 28 DL78K010824 1 20010523 A 3150 WARNING SYSTEM BOEING 737 737832 13844CF NM COCKPIT FALSE ACTIVATION A DALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 27 396DA 30378 TAKEOFF WARNING HORN SOUNDED DURING TAKEOFF. PERFORMED TAKEOFF WARNING SYSTEM TEST PER MM 31-51-00-5. NO MALFUNCTIONS NOTED. TAKEOFF WARNING SYSTEM CKS GOOD. 2 L 7 2 4F RT A16WE 2001062800059 20010628 00059 WP 2001 6 28 DLL10010847 1 20010527 A 3350 5165744 POWER SUPPLY LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 728DA 193C1173 MID AISLE EMERGENCY LIGHTS NOT WORKING. REPLACED POWER SUPPLY. 2 L 7 3 4F A23WE 2001062800060 20010628 00060 WP 2001 6 28 DHL2001801008 1 20010627 A 2150 3964202 FLOW VALVE DOUG DC8 DC873F 302199F WP A/C BAY FAILED A DHLA O OTHER O OTHER CR CRUISE 1 SO 01 801DH 46033 AT CRUISE ALTITUDE IN BOTH AUTO AND MANUAL PRESSURIZATION AT ALL FLOW SETTINGS, CABIN CLIMBS AND DESCENDS UP TO 700 FPM AND WILL NOT STABILIZE AT CONSTANT PRESSURE LT MANIFOLD PRESSURE FLUCTUATES 3 PSI IN CRU.FOUND LT FLOW CONTROL VALVE TO INTERMITTENT/INOP IN ANY POSITION ABOVE MIN FLOW DEFER VARIABLE RATE FUNCTION PER MEL 21-40-1. R&R FLOW CONTROL VALVE IA W SMM21-55-5. CHECKED OPERATION OK. 2 L 7 4 4F RT 4A25 2001062800061 20010628 00061 WP 2001 6 28 DLL14010825 1 20010523 A 2780 7200105 TORQUE TUBE LKHEED 1011 1011385115 5265015 WP L/E SLAT BROKEN A DALA K NONE F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 1738D 193C1234 GOT A FLAP/SLAT LOCK LIGHT. FOUND O/B SLATS RT WING INOP DUE TO A BROKEN TORQUE TUBE. 2 L 7 3 4F A23WE 2001062800062 20010628 00062 NM 2001 6 28 DLM11010802 1 20010519 A 2913 PUMP DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 3 ENGINE FAILED A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 805DE 48476 733746 NR 3 HYDRAULIC, RIGHT EDP FAILED FOR TEMP. REPLACED BOTH NR 3 HYDRAULIC PUMPS. REPLACED SYSTEM FILTERS. SERVICED, BLE D AND LEAK CHECKED SYSTEM. 2 L 7 3 4F 4 F RT A22WE E24NE 2001062800063 20010628 00063 NM 2001 6 28 DLM11010803 1 20010519 A 2530 2676 CHILLER DOUG MD11 MD11 3023602 NM G4 GALLEY FAULTY A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 815DE 48624 FRC-250-XX000 SEE LOGBOOK FOR DETAILS - G4 CHILLER SHUT DOWN DUE ELEC SMELL. REMOVED AND REPLACED CHILLER. 2 L 7 3 4F RT A22WE 2001062800064 20010628 00064 NM 2001 6 28 DLM11010809 1 20010520 A 3350 LIGHT DOUG MD11 MD11 3023602 NM CABIN INOPERATIVE A DALA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 27 808DE 48479 ON PRE FLT FOUND TEST SWITCH EMERGENCY LIGHT NR 6 BATTERY LOW MESSAGE ON. REMOVED AND REPLACED SEAT 54B LIGHT ASSY AND HARNESS SYSTEM CHK'S NORMAL PER MM, OK FOR SVC. 2 L 7 3 4F RT A22WE 2001062800065 20010628 00065 NM 2001 6 28 DLM11010888 1 20010601 A 3320 COVER DOUG MD11 MD11 3023602 NM CABIN MISSING A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 815DE 48624 PAX AND F/A RECEIVED SHOCK WHEN ADJUSTING READING LIGHT AT SEAT 4G. ADJUSTED READING LIGHT WITH COVER ON. NO SHOCK, PR ESENT LIGHT OPS NORMAL. 2 L 7 3 4F RT A22WE 2001062800066 20010628 00066 NM 2001 6 28 DLM11010900 1 20010603 A 3350 6044113 BATTERY PACK DOUG MD11 MD11 3023602 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 807DE 48478 EMERGENCY LIGHT BATTERY 2 LOW MESSAGE IN COCKPIT DURING TEST. REPLACED BATTERY PACK. 2 L 7 3 4F RT A22WE 2001062800067 20010628 00067 NM 2001 6 28 DLM88010791 1 20010518 A 2910 290051518 HYDRAULIC LINE DOUG MD88 MD88 3023688 NM HYD SYSTEM LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 989DL 53341 LEFT HYD QTY 4 COMPLIED W/POM, WHEN SYS REPRESSURIZED ON APPROACH GOT ZERO PRESSURE INDICATION. FOUND T/R LINE LEAKING IN 48 SECTION. REMOVED AND REPLACED SAME, SERV HYD. OK FOR SERVICE. 2 L 7 2 4F RT A6WE 2001062800068 20010628 00068 NE 2001 6 28 DLM88010793 2 20010518 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 FAILED A DALA E ENGINE SHUTDOWN J WARNING INDICATION LD LANDING 1 SO 27 968DL 23795 53161 726824 NR 1 ENG FAILED ON LANDING. SPEED WAS 135 KIAS THROTTLES WERE AT REV IDLE. NO OVERTEMP NOTED. REMOVED AND REPLACED NR 1 ENG. 2 L 7 2 4F 4 F RT A6WE E9NE 2001062800069 20010628 00069 NE 2001 6 28 DLM88010804 2 20010519 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 FAILED A DALA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SO 27 935DL 30347 49722 725423 AFTER CLIMBOUT PASSING THRU 1000 FEET LOST THE RIGHT ENGINE. ENGINE SEIZED, NO RELIGHT WAS ATTEMPTED. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A6WE E9NE 2001062800070 20010628 00070 NM 2001 6 28 DLM88010843 1 20010525 A 2560 BATTERY P4010021SM DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 905DL 0 49536 UPPER EMERGENCY FLASHLIGHT AT L1 DOOR HAS DEAD BATTERY. REPLACED BATTERY, OPS NORMAL. 2 L 7 2 4F RT A6WE 2001062800071 20010628 00071 NM 2001 6 28 DLM88010849 1 20010526 A 3350 LIGHT DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 907DL 49538 ON L/O FOUND EMERGENCY LIGHTS INOP SEAT 18ED-29ED-36ED. RELAMPED, OPS CKS GOOD. 2 L 7 2 4F RT A6WE 2001062800072 20010628 00072 NM 2001 6 28 DLM88010899 1 20010603 A 3350 41B030CF00101 BATTERY PACK DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 998DL 53370 LT AND RT WING EXT EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK, CKS OK. 2 L 7 2 4F RT A6WE 2001062800073 20010628 00073 NM 2001 6 28 DLM90010801 1 20010519 A 2530 50459 OVEN DOUG MD90 MD9030 3023690 NM GALLEY FAULTY A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 913DN 53393 FLT ATT SMELLED SMOKE IN FIRST CLASS AREA RIGHT AFTER T/O TURNED OVENS OFF AND GALLEY POWER OFF. SMOKE AND SMELL P ERSISTED. FOUND F/C OVEN WITH STRONG BURNING SMELL. REPLACED SAME. NO ODOR PRESENT. 2 L 7 2 4F RT A6WE 2001062800074 20010628 00074 NM 2001 6 28 DLM90010868 1 20010529 A 2540 0EQ1111A02G0 SEAL DOUG MD90 MD9030 3023690 NM LAVATORY DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 905DA 53385 TOILET SHROUD SEAL WAS FOUND DAMAGED. A REPLACEMENT SEAL WAS MANUFACTURED PER ER/A 401873-14AD. 2 L 7 2 4F RT A6WE 2001062800075 20010628 00075 CE 2001 6 28 ERYARK71 1 20010528 A 3242 BRAKE BEECH MU300 400A 1155402 CE MLG FAILED E ERYA K NONE O OTHER LD LANDING 1 CE 07 402GS RK71 BRAKE FAILURE AFTER RETURN FROM RAYTHEON MAINTENANCE CENTER, FTY, FOR 3 PREVIOUS BRAKE FADING OCCURRENCES WITH 3 DIFFERE NT PILOTS. 2 H 7 2 4F RT A16SW 2001062800076 20010628 00076 CE 2001 6 28 GLBA2001109 1 20010527 A 7603 1145240971 POWER LEVER BEECH 1900 1900D 1154162 CE COCKPIT FAULTY A GLBA K NONE O OTHER UK UNKNOWN 1 CE 01 100UX UE100 LT POWER LEVER WILL NOT GO INTO GROUND FINE, RT POWER LEVER WILL NOT COME OUT OF GROUND FINE. REMOVED AND REPLACED BOTH POWER LEVERS. 2 L 7 2 4T RT A24CE 2001062800077 20010628 00077 CE 2001 6 28 GLBA2001110 1 20010527 A 7797 WIRE BEECH 1900 1900D 1154162 CE LT ENGINE LOOSE A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 01 195GL UE195 LT ITT ABOVE 780 DEG IN CLIMB WITH TQ SET AT 2200 LBS (ANTI-ICE ON). RETURNED TO BLOCK. FOUND WIRE LOOSE ON ITT PROBE. PERFORMED MAINTENANCE, OPS CHECKED GOOD. 2 L 7 2 4T RT A24CE 2001062800078 20010628 00078 CE 2001 6 28 GLBA2001112 1 20010527 A 3260 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE RT MLG OUT OF ADJ A GLBA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 01 97UX UE97 INTRANSIT LIGHT ILLUMINATED WITH GEAR UP. ADJUSTED RT UPLOCK SWITCH; OPS CHECKED GOOD. 2 L 7 2 4T RT A24CE 2001062800079 20010628 00079 CE 2001 6 28 00115 1 20010523 A 2844 FLOAT BEECH MU300 400A 1155402 CE FUEL SYS DEFECTIVE E DJFA O OTHER J WARNING INDICATION AP APPROACH 1 EA 23 457CW RK57 AIRCRAFT HAD A LOW FUEL PRESSURE INDICATION DURING LANDING. AIRCRAFT LANDED WITH NO PROBLEMS. FOUND FUEL LOW PRESSURE FLOAT DEFECTIVE. REPLACED FLOAT, OPS CHECKED OK. 2 H 7 2 4F RT A16SW 2001062800080 20010628 00080 NM 2001 6 28 0101975526 1 20010605 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 526US 23620 DURING L-CHECK FOUND CRACK IN FLOORBEAM UPPER CAP AT BS 700 LBL 45. REPAIRED PER EA 55-184135. 2 L 7 2 4F RT A2NM 2001062800081 20010628 00081 NM 2001 6 28 0101985526 1 20010602 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 526US 23620 During l-check found crack in floorbeam upper cap at BS 700 LBL 25. Repaired per EA 55-184136. 2 L 7 2 4F RT A2NM 2001062800082 20010628 00082 NM 2001 6 28 0101995506 1 20010601 A 3350 6012113RF POWER SUPPLY BOEING 757 757251 1384970 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 506US 23195 DURING LINE CHECK, FOUND MID CABIN FLOOR MOUNTED EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE REPLACED THE M9002 AND M9 003 POWER SUPPLIES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A2NM 2001062800083 20010628 00083 WP 2001 6 28 0102019620 1 20010602 A 7603 THROTTLE CABLE DOUG DC9 DC932 3022066 WP LT ENGINE CONTAMINATED A NWAA K NONE F FLT CONT AFFECTED CR CRUISE 1 GL 01 620NW 47533 AT FL330 AND RAT -20C, THE LEFT THROTTLE WOULD NOT MOVE WITH POWER AT 1.80 EPR. AFTER TWO TRIES, THE THROTTLE WOULD INC H FORWARD TO 1.90 EPR BUT WOULD NOT GO LOWER THAN 1.80 EPR. ON DESCENT, RAT 0C, THROTTLE FREED UP AND OPERATED NORMALLY . AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND STANDING WATER IN COWL. DRAINED WATER FROM COWL. OPERATIONAL C HECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001062800084 20010628 00084 WP 2001 6 28 0102029984 1 20010606 A 2780 SWITCH DOUG DC9 DC932 3022066 WP COCKPIT INTERMITTENT A NWAA A UNSCHED LANDING F FLT CONT AFFECTED TO TAKEOFF 1 GL 01 8934E 47383 ON TAKEOFF FROM MEM AND ON RETRACTION, SLAT DISAGREEMENT LIGHT ILLUMINATED WITH A SLIGHT ROLL FELT. CREW FOLLOWED COM P ROCEDURES AND ROLL CEASED WHEN FLAPS EXTENDED. AIRCRAFT RETURNED TO MEM. MAINTENANCE FOUND SLAT HANDLE SWITCH INTERMIT TENT. REPLACED SWITCH S1-298 AND CYCLED SLATS NUMEROUS TIMES. OPERATIONAL CHECK NORMAL. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F A6WE 2001062800085 20010628 00085 NE 2001 6 28 0102036642 2 20010604 A 7200 ENGINE BOEING 747 747212B 1384886 NM PWA JT9 JT9D7Q 52054 NE NR 4 FLAMED OUT A NWAA K NONE X ENGINE FLAMEOUT CR CRUISE 1 GL 01 642NW 21942 702038 WHILE IN CRUISE AT FL370, THE NR 4 ENGINE FLAMED OUT. THE CREW FOLLOWED COM PROCEDURES AND RESTARTED THE ENGINE SUCCESS FULLY AT FL280. ENGINE OPERATION WAS NORMAL FOR THE REMAINDER OF THE FLIGHT. MAINTENANCE INSPECTED THE ENGINE AND PERF ORMED AN ENGINE RUN TO HIGH POWER WITH NO DEFECTS OR ABNORMAL INDICATIONS. THE ENGINE CONDITION MOTOR WAS REPLACED AS A PRECAUTION. 2 L 7 4 4F 4 F A20WE E3NE 2001062800086 20010628 00086 NM 2001 6 28 0102046305 1 20010402 A 5347 SEAT TRACK BOEING 747 747451 1384940 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 665US 23820 During H-check found corrosion on crown of seat track at BS 1080 LBL 12. Repaired per EA 63-182922. 2 L 7 4 4F RT A20WE 2001062800087 20010628 00087 NM 2001 6 28 0102056626 1 20010522 A 5711 SPAR BOEING 747 747251B 1384892 NM RT WING CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 626US 21708 During L-check found corrosion on Rt wing front spar web at OLES 1381 outboard and behind stiffener. Repaired per EA 66 -183239. 2 L 7 4 4F A20WE 2001062800088 20010628 00088 NM 2001 6 28 0102066642 1 20010426 A 5320 STIFFENER BOEING 747 747251B 1384892 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 642NW 21942 During L-check found corrosion on stiffener in Rt wheel well pressure deck at BS 1340 RBL 77. Repaired per EA 66-183372 . 2 L 7 4 4F A20WE 2001062800089 20010628 00089 NM 2001 6 28 0102086303 1 20010605 A 2913 3508806 PUMP BOEING 747 747451 1384940 NM NR 4 ENGINE FAILED A NWAA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 01 663US 48850 148 23818 DURING FLIGHT, RECEIVED HYD PRESS SYS 4 AND HYD QTY LOW 4 MESSAGE AND THE HYDRAULIC FLUID QUANTiTY IN THE NR 4 SYSTEM IN DICATED ZERO. FOLLOWED COM PROCEDURE AND THE AIRCRAFT CONTINUED TO NRT. DURING APPROACH WHILE ALTERNATE EXTENDING THE LANDING GEAR, THE RIGHT WING LANDING GEAR FAILED TO FULLY EXTEND. AIRCRAFT LANDED WITH THE RIGHT WING LANDING GEAR STIL L IN THE WHEEL WELL. THE AIRCRAFT WAS DEPLANED ON THE RUNWAY AND TOWED TO THE RAMP. REPLACED THE NR 4 ENGINE DRIVEN HY DRAULIC PUMP AND RIGHT WING LANDING GEAR DOOR STRIKER BOARD. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2001062800090 20010628 00090 NM 2001 6 28 0102116311 1 20010616 A 3350 PIN BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE O OTHER UK UNKNOWN 1 GL 01 671US 26477 EMERGENCY LIGHTS ILLUMINATED WITH EMERGENCY LIGHT SWITCH IN THE OFF POSITION. SECURED GROUNDING PIN NR 24 AT FLIGHT AT TENDANT HANDSET HOLDER. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001062800091 20010628 00091 WP 2001 6 28 0102179759 1 20010614 A 2611 473597407 SMOKE DETECTOR DOUG DC9 DC941 302207N WP CARGO BAY MALFUNCTIONED A NWAA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 GL 01 759NW 47287 DURING APPROACH INTO GRB, FORWARD CARGO COMPARTMENT FIRE DETECTOR SOUNDED. FOLLOWED COM PROCEDURES AND EXTINGUISHING BO TTLE WAS DISCHARGED. LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED CARGO SMOKE DETECTOR, ECU, AND BOTTLE. AIRCRAFT RET URNED TO SERVICE. 2 L 7 2 4F A6WE 2001062800092 20010628 00092 NM 2001 6 28 QXEA0100821 1 20010510 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - LEFT OUTBOARD SEAT TRACK CORRODED IN CHANNEL AT STATION 471. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001062800093 20010628 00093 NM 2001 6 28 QXEA0100822 1 20010510 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - LEFT OUTBOARD SEAT TRACK CORRODED ON INBOARD RAIL AT STATION 468 TO 471. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001062800094 20010628 00094 NM 2001 6 28 QXEA0100823 1 20010510 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - LEFT OUTBOARD SEAT TRACK CORRODED ON INBOARD AND OUTBOARD LUGS AT STATION 466. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001062800095 20010628 00095 NM 2001 6 28 QXEA0100824 1 20010510 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - LEFT OUTBOARD SEAT TRACK CORRODED IN OUTBOARD SIDE OF CHANNEL AT STATION 531. REPAIRED IAW RD 8-53-3644. 2 H 7 2 4T RT A13NM 2001062800096 20010628 00096 NM 2001 6 28 QXEA0100825 1 20010510 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - LEFT OUTBOARD SEAT TRACK CORRODED ON INBOARD AND OUTBOARD RAILS AT STATION 545. REPAIRED IAW RD 8-53-3611. 2 H 7 2 4T RT A13NM 2001062800097 20010628 00097 NM 2001 6 28 QXEA0100826 1 20010510 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - LEFT OUTBOARD SEAT TRACK GOUGED IN CHANNEL IN AFT 4 INCHES OF TRACK AT STATION 545. REPAIRED IAW RD8-53-1342. 2 H 7 2 4T RT A13NM 2001062800098 20010628 00098 NM 2001 6 28 QXEA0100827 1 20010510 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT INBOARD SEAT TRACK CORRODED AROUND BOLT HOLE AT STATION 202. REPAIRED IAW RD8-53-1139. 2 H 7 2 4T RT A13NM 2001062800099 20010628 00099 NM 2001 6 28 QXEA0100828 1 20010516 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - LEFT INBOARD SEAT TRACK HAS GOUGES AND CORROSION IN CHANNEL ON LEFT AND RIGHT RAILS AT STATION 539. REPAIRED IAW DHC-8 SRM 51-20-16 AND HORIZON AIR EA 9-53-617. 2 H 7 2 4T RT A13NM 2001062800100 20010628 00100 NM 2001 6 28 QXEA0100829 1 20010510 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - LEFT INBOARD SEAT TRACK GOUGED AT STATION 520. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2001062800101 20010628 00101 NM 2001 6 28 QXEA0100830 1 20010517 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - REPLACE LEFT-HAND INBOARD SEAT TRACK NR 4 DUE TO NUMEROUS CORROSION DISCREPANCIES. REPLACED SEAT TRACK IAW DHC-8 SRM \ AND SRM 51-40-00. 2 H 7 2 4T RT A13NM 2001062800102 20010628 00102 NM 2001 6 28 QXEA0100831 1 20010511 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT INBOARD SEAT TRACK CHAFED IN CHANNEL 8 INCHES TO 11 INCHES LONG AT STATION 291. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2001062800103 20010628 00103 NM 2001 6 28 QXEA0100832 1 20010511 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT INBOARD SEAT TRACK GOUGED ON LUGS AT STATION 295. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2001062800104 20010628 00104 NM 2001 6 28 QXEA0100833 1 20010511 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT INBOARD SEAT TRACK CORRODED IN CHANNEL AT STATION 322. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2001062800105 20010628 00105 NM 2001 6 28 QXEA0100834 1 20010511 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT INBOARD SEAT TRACK CORRODED ON OUTBOARD LUG AT STATION 324. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2001062800106 20010628 00106 NM 2001 6 28 QXEA0100835 1 20010514 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT INBOARD SEAT TRACK DRIP FLANGE ON INBOARD SIDE OF TRACK HAS PAINT WORN AND LIGHTLY CHAFED FROM STATION 262 - 277. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2001062800107 20010628 00107 NM 2001 6 28 QXEA0100836 1 20010511 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT INBOARD SEAT TRACK CORRODED IN CHANNEL AT STATION 360. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2001062800108 20010628 00108 NM 2001 6 28 QXEA0100837 1 20010511 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT INBOARD SEAT TRACK CORRODED IN CHANNEL AT STATION 387. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2001062800109 20010628 00109 NM 2001 6 28 QXEA0100838 1 20010511 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT INBOARD SEAT TRACK CORRODED ON LEFT AND RIGHT LUGS AT STATION 390. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2001062800110 20010628 00110 NM 2001 6 28 QXEA0100839 1 20010511 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT INBOARD SEAT TRACK CHAFED ON INBOARD LUG AT STATION 405. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2001062800111 20010628 00111 NM 2001 6 28 QXEA0100840 1 20010511 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT INBOARD SEAT TRACK GOUGED .002 INCH ON OUTBOARD LUG AT STATION 418. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2001062800112 20010628 00112 NM 2001 6 28 QXEA0100841 1 20010511 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT INBOARD SEAT TRACK CORRODED IN CHANNEL AT STATION 430. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2001062800113 20010628 00113 NM 2001 6 28 QXEA0100842 1 20010511 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT INBOARD SEAT TRACK CORRODED ON LEFT AND RIGHT RAIL AT STATION 436. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2001062800114 20010628 00114 NM 2001 6 28 QXEA0100843 1 20010511 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT INBOARD SEAT TRACK CHAFED IN CHANNEL AT STATION 456. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2001062800115 20010628 00115 NM 2001 6 28 QXEA0100844 1 20010511 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT INBOARD SEAT TRACK CORRODED IN CHANNEL AT STATION 486. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2001062800116 20010628 00116 NM 2001 6 28 QXEA0100845 1 20010511 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT INBOARD SEAT TRACK CORRODED ON INBOARD SIDE OF CHANNEL, IN CHANNEL AND ON LEFT AND RIGHT LUGS AT NR 8. REPA IRED IAW RD 8-53-1339. 2 H 7 2 4T RT A13NM 2001062800117 20010628 00117 NM 2001 6 28 QXEA0100846 1 20010511 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT INBOARD SEAT TRACK CORRODED AFT OF SEAT RAILS AND ON OUTBOARD RAIL AT STATION 547. REPAIRED IAW RD 8-53-133 9. 2 H 7 2 4T RT A13NM 2001062800118 20010628 00118 NM 2001 6 28 QXEA0100847 1 20010511 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT INBOARD SEAT TRACK CORRODED IN CHANNEL AND ON LUGS AT STATION 597. REPAIRED IAW RD8-53-784. 2 H 7 2 4T RT A13NM 2001062800119 20010628 00119 NM 2001 6 28 QXEA0100848 1 20010515 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - AT FLOOR LEVEL ON RIGHT-HAND SIDE OF FRAME AT 618.0 IT HAS A CHAFE FROM FLOOR BOARD APPROXIMATELY .010 INCH DEEP. REPAIRED IAW DHC-8 SRM 51-20-00. 2 H 7 2 4T RT A13NM 2001062800120 20010628 00120 NM 2001 6 28 QXEA0100849 1 20010511 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - INBOARD END RIVET AND CORNER RADIUS CORRODED ON FRAME CASTELLATION OF FRAME 580.0 AND STRINGER 315. REPAIRED IAW DHC-8 SRM 51-20-16, PAGE 2, PARAGRAPH 4 AND SRM 51-20-26, PAGE 7, PARAGRAPH 5A (1), (2), (3). 2 H 7 2 4T RT A13NM 2001062800121 20010628 00121 NM 2001 6 28 QXEA0100850 1 20010512 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - LEFT-HAND INBOARD SEAT TRACK FITTING AT FRAME 597.5 HAS GOUGE ON INBOARD SIDE OF FITTING BY HI-LOK COLLAR. REPAIR ED IAW DHC-8 SRM 51-20-11, PAGE 9. 2 H 7 2 4T RT A13NM 2001062800122 20010628 00122 NM 2001 6 28 QXEA0100851 1 20010512 A 5313 RIVET DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - SEVEN RIVET TAILS ON STRINGER 33 JUST FORWARD OF FRAME 580.5 HAVE SIGNS OF CORROSION. REPAIRED IAW DHC-8 SRM 51-4 0-00. 2 H 7 2 4T RT A13NM 2001062800123 20010628 00123 NM 2001 6 28 QXEA0100852 1 20010512 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - CORROSION ON BOTTOM OF SKIN AT NUT PLATE JUST OUTBOARD OF LEFT-HAND SIDE PULLEY QUADRANT, JUST FORWARD OF FRAME 59 7.5. REPAIRED IAW DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2001062800124 20010628 00124 NM 2001 6 28 QXEA0100854 1 20010513 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - CORROSION ON FRAME CASTELLATION AT FRAME 222 AND STRINGER 31S. REPAIRED IAW DHC-8 PSM 1-GEN-S-CHAPTER 4, STEP 8 A ND SRM 51-00-04. 2 H 7 2 4T RT A13NM 2001062800125 20010628 00125 NM 2001 6 28 QXEA0100855 1 20010516 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - CORROSION ON CASTELLATION OF FRAME 202 AND STRINGER 325. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 7 AND DHC-8 MM 20- 34-08, PAGES 1-9. 2 H 7 2 4T RT A13NM 2001062800126 20010628 00126 NM 2001 6 28 QXEA0100856 1 20010515 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - CORROSION AT STRINGER 31S AND FRAME 312 SKIN CASTELLATION. REPAIRED IAW DHC-8 PSM 1-GEN-5-CHAPTER 4, STEP 8 AND D HC-8 SRM 53-00-16, PAGE 3, TABLE 1, SHEET 2. 2 H 7 2 4T RT A13NM 2001062800127 20010628 00127 NM 2001 6 28 QXEA0100857 1 20010524 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT-HAND FUSELAGE SKIN HAS AREA WITH GOUGE MARKS EXTENDING 6 INCHES FORWARD OF LAVATORY SERVICE DOOR AND .200 IN CH WIDE. REPAIRED IAW HORIZON AIR EA 9-53-621. 2 H 7 2 4T RT A13NM 2001062800128 20010628 00128 NM 2001 6 28 QXEA0100858 1 20010520 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - LEFT-HAND FUSELAGE SKIN AFT OF BAGGAGE DOOR HAS AREA WITH GOUGE MARKS .750 X .200 X APPROXIMATELY .003 DEEP AT FRA ME X607.00 AND STRINGER 105.00. REPAIRED IAW DHC-8 SRM 51-20-00. 2 H 7 2 4T RT A13NM 2001062800129 20010628 00129 NM 2001 6 28 QXEA0100859 1 20010524 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - LOWER VHF COMM ANTENNA ON FUSELAGE IS HEAVILY CORRODED. REPAIRED IAW HORIZON AIR EA 9-53-619. 2 H 7 2 4T RT A13NM 2001062800130 20010628 00130 NM 2001 6 28 QXEA0100860 1 20010520 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - FUSELAGE SKIN UNDERNEATH DME ANTENNA IS CORRODED. REPAIRED IAW CORROSION PREVENTION MANUAL CHAPTER 4, PAGE 4-25 A ND 4-26 AND DHC-8 MM 20-32-02, PAGE 2, 4A, B AND C. 2 H 7 2 4T RT A13NM 2001062800131 20010628 00131 NM 2001 6 28 QXEA0100861 1 20010524 A 5330 DOUBLER DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - INNER DOUBLER SKIN HAS CRACK INDICATION APPROXIMATELY .625 INCH LONG, FORWARD OF LAVATORY SERVICE DOOR. REPAIRED IAW HORIZON AIR EA 9-53-622. 2 H 7 2 4T RT A13NM 2001062800132 20010628 00132 NM 2001 6 28 QXEA0100862 1 20010516 A 5320 THRESHOLD DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - CORROSION ON MAIN CABIN DOOR LOWER THRESHOLD. REPAIRED IAW DHC-8 MM 51-40-11, PAGE 11, 1 THRU 4. 2 H 7 2 4T RT A13NM 2001062800133 20010628 00133 2001 6 28 SWAA011606 4 20010601 A 2565 SLIDE BOEING 737 7373G7 1384595 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC S LIDE PER MM. 2 L 7 2 4F RT A16WE 2001062800134 20010628 00134 NM 2001 6 28 SWAA011607 1 20010602 A 5320 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 180, RBL 17.1. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001062800135 20010628 00135 NM 2001 6 28 SWAA011608 1 20010601 A 3350 COVER BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 502SW 24179 EEPLS TRACK COVER LOOSE AT MID CABIN. INSTALLED EEPLS TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001062800136 20010628 00136 2001 6 28 SWAA011609 4 20010531 A 2565 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001062800137 20010628 00137 2001 6 28 SWAA011610 4 20010531 A 2565 SLIDE BOEING 737 7373T5 NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUSTMENT. ADJUSTED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001062800138 20010628 00138 NM 2001 6 28 SWAA011611 1 20010601 A 3350 COVER BOEING 737 7377H4 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 725SW 27857 EEPLS TRACK COVER LOOSE AT FWD CABIN. SECURED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2001062800139 20010628 00139 2001 6 28 SWAA011612 4 20010601 A 2565 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 091SW 22963 DURING SCHEDULED RON CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVA C SLIDE PER MM. 2 L 7 2 4F A16WE 2001062800140 20010628 00140 NM 2001 6 28 SWAA011613 1 20010601 A 5320 STIFFENER BOEING 737 7373H4 1384600 NM MLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND VERTICAL STIFFENER CRACKED AT MLG WW BS 663, LBL 6. REPAIRED PER SWA RA. 2 L 7 2 4F RT A16WE 2001062800141 20010628 00141 NM 2001 6 28 SWAA011614 1 20010601 A 5312 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 180 & RBL 20. REPAIRED WEB PER SRM. 2 L 7 2 4F A16WE 2001062800142 20010628 00142 WP 2001 6 28 AT0100188 1 20010622 A 3350 BULB DOUG DC9 DC932 3022066 WP AFT TAIL INOPERATIVE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 828AT 47274 FOUND AFT TAIL CONE OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. CORRECTIVE ACTION: RELAMPED LIGHTS. IA W DC9 MM 33-00 2 L 7 2 4F A6WE 2001062800143 20010628 00143 WP 2001 6 28 AT0100194 1 20010516 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP COCKPIT CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 840AT 47523 FOUND CAPTAINS SEAT TRACK AFT INBOARD AREA CORRODED. CORRECTIVE ACTION: REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR. IAW DC9 53-01 FIGURE 1, 51-30-2, 51-10-4, 51-10-3. 2 L 7 2 4F A6WE 2001062800144 20010628 00144 WP 2001 6 28 AT0100197 1 20010516 A 5315 ANGLE DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 840AT 47523 FOUND CORROSION IN THE AFT PIT ON THE CABIN FLOOR BEAM AT BS 996. CORRECTIVE ACTION: REMOVED, FABRICATED , DRILLED, AND INSTALLED REPLACEMENT UPPER CAP. IAW DC9 SRM 51-10-3, 53-01 FIGURE 1 51-30-2, 51-30-5, 51-10-4, 55-11-3 2 L 7 2 4F A6WE 2001062800145 20010628 00145 WP 2001 6 28 AT0100198 1 20010517 A 5315 LONGERON DOUG DC9 DC932 3022066 WP BS 680-699 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 840AT 47523 FOUND LONGERON 16L CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED LONGERON SECTION AT BS 680-699. IAW DC9 SRM 51-10-1 FIGURE 36 2 L 7 2 4F A6WE 2001062800147 20010628 00147 NM 2001 6 28 EISA20010085 1 20010413 A 5310 FABRICATED STRINGER BOEING 727223 BOEING 727 727223 1384074 NM STA 1100 AND 114 DAMAGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 702NE 22460 22460 STRINGER 25 RIGHT DAMAGED BETWEEN STATION 1100 AND 1140. CORRECTIVE ACTION: REMOVED DAMAGED SECTION OF STRINGER, FABRICA TED REPAIR SECTIONS AND SPLICES, IAW SRM 53-10-3, 51-10-2, 53-10-3 FIG 1. 2 L 7 3 4F A3WE 2001062800148 20010628 00148 NM 2001 6 28 EISA20010078 1 20010427 A 5712 65217222 RIB BOEING 727223 BOEING 727 727223 1384074 NM RIGHT WING DAMAGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6819 19494 19494 WHILE AICRAFT WAS PARKED, AIRBOURNE EXPRESS VAN STRUCK WING FROM BEHIND.DAMAGED #2 RIB FROM OUTBOARD RIGHT WING TIP. COR RECTIVE ACTION: REMOVED AND REPLACED RIGHT WING DAMAGED RIB. PER SRM 51-30-2. 2 L 7 3 4F A3WE 2001062800149 20010628 00149 NM 2001 6 28 EISA20010079 1 20010427 A 5712 6521722 RIB BOEING 727223 BOEING 727 727223 1384074 NM RIGHT WING DAMAGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6819 19494 19494 WHILE AIRCRAFT WAS PARKED, AIRBOURNE EXPRESS VAN STRUCK AIRCRAFT FROM BEHIND ON RIGHT WING. RIGHT WING TIP OUTBOARD RIB DAMAGED. CORRECTIVE ACTION: REMOVED DAMAGED RIB AND FABRICATED, TREATED AND PRIMED PART, IAW 51-40-3, 51-10-2, 51-40-03. 2 L 7 3 4F A3WE 2001062800150 20010628 00150 NM 2001 6 28 EISA20010080 1 20010427 A 5712 65249618 CHANNEL BOEING 727223 BOEING 727 727223 1384074 NM RIGHT WING DAMAGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6819 19494 19494 WHILE AIRCRAFT WAS PARKED, AIRBOURNE EXPRESS VAN STRUCK, AIRCRAFT FROM BEHIND ON RIGHT WING, RIGHT WING TIP CHANNEL IS D AMAGED. CORRECTIVE ACTION: REMOVED AND REPLACED RIGHT WING TIP CHANNEL IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2001062800151 20010628 00151 NM 2001 6 28 EISA20010081 1 20010427 A 5712 FABRICATED SKIN BOEING 727223 BOEING 727 727223 1384074 NM RIGHT WING DAMAGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6819 19494 19494 WHILE AIRCRAFT WAS PARKED, AIRBOURNE EXPRESS VAN STRUCK AIRCRAFT RIGHT WING TIP FROM BEHIND. RIGHT WING TIP TOP AND BOTT OM SKIN DAMAGED.CORRECTIVE ACTION: CUT OUT DAMAGED AREA FABRICATED SKIN, TREATED, PRIMED, AND INSTALLED PER E.O.#01-123 WITH APPROVED 8110-3, DATED 04-25-2001. 2 L 7 3 4F A3WE 2001062800152 20010628 00152 WP 2001 6 28 ZW0A0104301 1 20010626 A 3350 0105610001 COVER DOUG DC9 DC983 3022083 WP SEAT 21A A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 978TW 53628 AT SEAT 21A THE EMERGENCY EXIT SIDEWALL LIGHT COVER WAS MISSING. REPLACED THE COVER. CHECK-C 10-27-00 STL. --CLOSED-- 2 L 7 2 4F RT A6WE 2001062800153 20010628 00153 NM 2001 6 28 SWAA011615 1 20010601 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, LBL 6 & WL 200. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001062800154 20010628 00154 NM 2001 6 28 SWAA011616 1 20010601 A 5311 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT STR 8L & 9L, BS 727D, BS 867 & BS 907. REPAIRED FRAMES PER S RM. 2 L 7 2 4F RT A16WE 2001062800155 20010628 00155 NM 2001 6 28 SWAA011617 1 20010601 A 5520 BUSHING BOEING 737 7373Y0 1384671 NM RT ELEVATOR WORN A SWAA K NONE E VIBRATION/BUFFET NR NOT REPORTED 1 SW 07 682SW 23496 VIBRATION FELT ABOVE 250 KTS IN REAR OF AIRCRAFT, NOT ENG RELATED. Removed and replaced Rt ELEVATOR TAB BUSHING. REPAI RED ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2001062800156 20010628 00156 NM 2001 6 28 SWAA011618 1 20010601 A 5330 SKIN BOEING 737 7373T5 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED BEHIND AFT LOWER WING TO BODY FAIRING Rt SIDE. REPAIRED SKIN PE R SRM. 2 L 7 2 4F RT A16WE 2001062800157 20010628 00157 NM 2001 6 28 SWAA011619 1 20010526 A 5314 KEELBEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 080SW 22675 DURING SCHEDULED SERVICE CHECK, FOUND Rt KEEL BEAM CORRODED AT BS 500A+6, STR 28R. REPAIRED KEEL BEAM PER SWA RA. 2 L 7 2 4F A16WE 2001062800158 20010628 00158 NM 2001 6 28 SWAA011620 1 20010601 A 2730 BEARING BOEING 737 7372H4 138448C NM ELEVATOR WORN A SWAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SW 07 103SW 23109 AT LOWER SPEED, LESS THAN 250 KNOTS, A PRONOUNCED DEAD SPOT IN PITCH CONTROL FELT. Removed and replaced ELEV CONTROL LO WER TORQUE TUBE BEARINGS PER MM. 2 L 7 2 4F A16WE 2001062800159 20010628 00159 NM 2001 6 28 SWAA011621 1 20010601 A 3350 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 524SW 26566 DURING SCHEDULED C1 CHECK, FOUND EEPLS LIGHTS INOP IN VARIOUS LOCATIONS. Removed and replaced CONNECTOR BLOCK AND RECON NECTED WIRES PER MM. 2 L 7 2 4F RT A16WE 2001062800160 20010628 00160 NM 2001 6 28 SWAA011622 1 20010601 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 089SW 22904 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKINS CRACKED AT BS 800, STR 24L & BS 934, STR 25R & BS 800, STR 24L. REP AIRED SKIN CRACKS PER SRM. 2 L 7 2 4F A16WE 2001062800161 20010628 00161 NM 2001 6 28 SWAA011623 1 20010601 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 089SW 22904 ON WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 310, STR 8R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001062800162 20010628 00162 2001 6 28 SWAA011624 4 20010601 A 2565 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 355SW 25250 DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. Removed and replaced EMER GENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001062800163 20010628 00163 NM 2001 6 28 SWAA011625 1 20010529 A 5320 TIE CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED D-CHECK, FOUND STR TIE CLIPS CRACKED AT BS 663, STR 10R & 10L, BS 520, STR 8L. Removed and replaced TI E CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001062800164 20010628 00164 NM 2001 6 28 SWAA011626 1 20010601 A 5311 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 440, STR 9R AND BS 400, BETWEEN STR 8L & 9L. REPAIRED FRA MES PER SRM. 2 L 7 2 4F RT A16WE 2001062800165 20010628 00165 NM 2001 6 28 SWAA011627 1 20010601 A 5311 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R & 9R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001062800166 20010628 00166 NM 2001 6 28 SWAA011628 1 20010601 A 2612 FIRE LOOP BOEING 737 7372H4 138448C NM NR 2 ENGINE FAULTY A SWAA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 063SW 22061 AIR TURNBACK, ENGINE SHUTDOWN and DECLARED EMERGENCY. DURING FLIGHT, NR 2 ENGINE FIRE WARNING LIGHT ILLUMINATED and FIR E BELL SOUNDED, DID NOT FIRE BOTTLE. Removed and replaced NR 2 ENGINE UPPER FIRE LOOP PER MM. 2 L 7 2 4F A16WE 2001062800167 20010628 00167 NM 2001 6 28 SWAA011629 1 20010530 A 3244 TIRE BOEING 737 7373Y0 1384671 NM LT MLG SEPARATED A SWAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 664WN 23495 AIR TURNBACK, ENGINE SHUTDOWN and DECLARED EMERGENCY. DURING TAKEOFF, NR 2 MLG TIRE SEPARATED DAMAGING NR 1 ENGINE FAN BLADES AND NOSE COWL ASSY. ALSO DAMAGING LT T/E AFT FLAP LOWER SURFACE, LT INBD GROUND SPOILER, LT MLG DOWNLOCK BUNGEE SPRINGS AND LINK ASSY, LT MLG OUTBOARD PRIORITY VALVE HYD LINE AND LT INBOARD T/E LOWER SHELF PANEL. REMOVED AND REPLAC ED NR 2 MLG TIRE, WHEEL, BRAKE ASSY. REMOVED AND REPLACED NR 1 ENG AND NOSE COWL ASSY. TEMP REPAIRED OTHER COMPONENTS AND MX FERRY TO DAL FOR DAMAGED COMPONENTS REPLACEMENT. ALL WORK DONE PER MM. 2 L 7 2 4F RT A16WE 2001062800168 20010628 00168 NM 2001 6 28 SWAA011630 1 20010603 A 3350 079123 COVER BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 524SW 26566 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER LOOSE AT AFT CABIN. Removed and replaced EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2001062800169 20010628 00169 NM 2001 6 28 SWAA011631 1 20010603 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 524SW 26566 DURING SCHEDULED C1 CHECK, FOUND EEPLS INOP AT ROW 1 & ROW 2. RELAMPED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001062800170 20010628 00170 NM 2001 6 28 SWAA011632 1 20010603 A 3397 BR2013 WIRE BOEING 737 7375H4 138449D NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 524SW 26566 EEPLS SEGMENT INOP. RECONNECTED EEPLS WIRES PER MM. 2 L 7 2 4F RT A16WE 2001062800171 20010628 00171 NM 2001 6 28 SWAA011633 1 20010604 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM ENTRY DOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 618WN 28034 FWD ENTRY DOOR EMERGENCY EXIT LIGHT MISSING LENS. INSTALLED EMERGENCY EXIT LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2001062800172 20010628 00172 NM 2001 6 28 SWAA011634 1 20010604 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 388SW 26591 EEPLS INOP BETWEEN ROW 14 & ROW 12. RECONNECTED EEPLS WIRES PER MM. 2 L 7 2 4F RT A16WE 2001062800173 20010628 00173 EU 2001 6 28 MALA010541 1 20010623 A 7710 BLEED BAND BAC 146 AVRO146RJ85A 1500097 EU DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 15 512XJ E2326 Aircraft experienced a sudden ITT spike along with an N2 drop after Takeoff. Flight returned to DTW. Air turnback. Ma intenance replaced #1 Engine Bleed Band. All Checks good. See 409 Card #134852 for details 2 H 7 4 4F RT A49EU 2001062800174 20010628 00174 EU 2001 6 28 MALA010542 1 20010627 A 2150 ACM SAAB SF340 340B 7860101 EU DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 439XJ 340B439 During Flight #3323, out of MSP, unable to cool cabin to 35 degrees C. Left duct Temp reads 29 degress C. in both Auto a nd Manual modes. Shut off Left Bleed and Duct Temp rises to above 50 degrees C. shut off right Bleed, no help QRH'd no help. Air Return to MSP. Maintenance completed 409 Card #053572, replaced Right ACM and Right Auto Controller, ran AC ops check good. Ref 409 Card for work details. 2 L 7 2 4T RT A52EU 2001062800175 20010628 00175 WP 2001 6 28 MWEA011005 1 20010628 A 5310 591000644 ANGLE DOUG DC9 DC932 3022066 WP STATION 604 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 RIGHT WING TO FUSELAGE FITTING AT STATION 604 LONGERON 22 RIGHT IS CRACKED. -- REMOVED FITTING, LOCATED AND INSTALLED NEW FITTING. 2 L 7 2 4F A6WE 2001062800176 20010628 00176 NM 2001 6 28 SWAA011635 1 20010604 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 379SW 26586 EEPLS COVER LOOSE AT ROW 8. SECURED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2001062800177 20010628 00177 NM 2001 6 28 EISA20010092 1 20010530 A 3411 0851CM2 PITOT TUBE BOEING BOEING 727 727223 1384074 NM RIGHT FUSELAGE CLOGGED A EISA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 07 6819 19494 ABORTED TAKEOFF DUE TO FIRST OFFICERS AIRSPEED IND INOP. USED NORMAL BRAKING DUE TO LOW SPEED ABORT. CORRECTIVE ACTION: FOUND F/O'S PITOT TUBE BLOCKED. CLEANED PITOT TUBE OPS CHECK F/O'S AIRSPEED IND PER M/M 34-11-00, TESTED NORMAL ON GROUN D. 2 L 7 3 4F A3WE 2001062800178 20010628 00178 NM 2001 6 28 EISA20010094 1 20010608 A 5312 HLT4286 RIVET BOEING BOEING 727 727223 1384074 NM SHEARED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6813 19488 RIVET MIGRATED AT 1183 BULKHEAD AFT LT. SIDE 12" O/B OF DOOR CUT-OUT & 10" BELOW DOOR TOP (EO)FOUND DURING B-2 CHECKCORR ECTIVE ACTION:CUT-OFF HEAD OF TRAPPED (MIGRATING) RIVET PER E.O. #01-163. INSTALLED TWO EACH HLT 428-6 HILOCS IAW E.O. # 01-163 & SEALED WITH PR 1422 B1/2 IAW E.O. #01-163 WITH APPROVED 8110-3 DATED 6/7/01 2 L 7 3 4F A3WE 2001062800179 20010628 00179 NM 2001 6 28 EISA20010087 1 20010412 A 5310 FABRICATED SKIN BOEING 727223 BOEING 727 727223 1384074 NM STATION 1100 DAMAGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 702NE 22460 22460 DAMAGED TO RIGHT SIDE OF AIRCRAFT AT STATION 1100-1135 BETWEEN STRINGER 24 & 25R DUE TO BAGGAGE CART BLOWN INTO AIRCRAFT . CORRECTIVE ACTION: CUT OUT DAMAGED AREA PER E.O. #01-112, REV A FABRICATED FILLER, DOUBLER, SHIMS. TREATED PRIMED AND INSTALLED REPAIR PERE.O. #01-112, REV A WITH APPROVED 8110-3 DATED 04-013-2001. 2 L 7 3 4F A3WE 2001062800180 20010628 00180 NM 2001 6 28 EISA20010098 1 20010619 A 3350 1000679 LIGHT BOEING BOEING 727 727223 1384074 NM INOPERATIVE A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6815 19490 ON POSTFLIGHT INSPECTION FOUND COCKPIT EMERGENCY LIGHT INOP.CORRECTIVE ACTION: REPLACED COCKPIT EMERGENCY EXIT LIGHT PE R MM REF 33-50 2 L 7 3 4F A3WE 2001062800181 20010628 00181 NM 2001 6 28 EISA20010095 1 20010610 A 3246 48282 BEARING BENDIX BOEING 727 727223 1384074 NM FAILED A EISA O OTHER E VIBRATION/BUFFET LD LANDING 1 SW 07 313NE B3707 19702 ON LANDING IN PITTSBURGH RIGHT BRAKE CHATTERED. USED MINIMUM BRAKES TO PARKING. VIEWED DAMAGED WHEEL ASSY ON POSTFLIGHT. TAXI AND TAKEOFF (PHIL.) WAS UNEVENTFUL.CORRECTIVE ACTION:FOUND #3 WHEEL BEARING FAILED. REPLACED AXEL SLEEVE, BRAKE, AXLE NUT AND WHEEL ASSY. 2 L 7 3 4F A3WE 2001062800182 20010628 00182 NM 2001 6 28 EISA20010096 1 20010619 A 5730 NPN SKIN BOEING BOEING 727 727223 1384074 NM CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 80623 80623 19475 RIGHT WING TIP AFT SECTION UPPER SURFACE HAS 1" CRACK DIRECTLY BEHIND NAV. LIGHT ACCESS PANELFOUND DURING 'B' CHECKCORRE CTIVE ACTION:REMOVED R/H WING TIP IAW B727 SRM 51-30-2. STOP DRILLED CRACK IAW B727 SRM 51-40-20. NDT VERIFIED CRACK HAD BEEN STOPPED. FABRICATED DOUBLER REPAIR IAW B727 SRM 51-20-1. TREATED, PRIMED AND INSTALLED REPAIR DOUBLER IAW B727 51- 10-2 & 51-30-2. RE-INSTALLED WING TIP IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2001062800183 20010628 00183 NM 2001 6 28 EISA20010097 1 20010619 A 5713 NPN STRINGER BOEING BOEING 727 727223 1384074 NM CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 80623 80623 19475 B.S. STA. 1183 & STRINGER 22 LEFT HAS CORROSION BLISTER 8" FWD OF BULKHEAD.CORRECTIVE ACTION: REMOVED DAMAGED SECTION O F STR. 22L PER B727 SRM 53-10-3, FIG. 1. FABRICATED REPLACEMENT STRINGER USING BAC 1498-144 & STRINGER SPLICE USING BAC 1498-132. TREATED & PRIMED PER B727 SRM 51-10-6. INSTALLED STRINGER AND SPLICE PER B727 SRM 51-10-3. 2 L 7 3 4F A3WE 2001062800184 20010628 00184 NM 2001 6 28 EISA20010093 1 20010613 A 3297 WIRE BOEING BOEING 727 727200 138407E NM BROKEN A EISA K NONE J WARNING INDICATION DE DESCENT 1 SW 07 702NE 22460 NOSE GEAR UNSAFE LIGHT ON WITH LANDIN GEAR DOWN RECYCLED GEAR TO EXTINGUISH LIGHT.CORRECTIVE ACTION:REPAIRED NOSE LANDIN G GEAR DOWN LOCK SWITCH WIRES BY SPLICING IAW B727 STANDARD WIRING MANUAL 20-30-22. OPS CHECKS GOOD IAW B727 32-61-71. 2 L 7 3 4F RT A3WE 2001062800185 20010628 00185 NM 2001 6 28 EISA20010089 1 20010523 A 3200 1U1085 SEQUENCE VALVE BOEING BOEING 727 727223 1384074 NM LEFT GEAR INTERMITTENT A EISA O OTHER O OTHER TO TAKEOFF 1 SW 07 316NE 19475 AFTER TAKEOFF AND GEAR RETRACTION HAD COMPLETE "A" SYSTEM LOSS.CORRECTIVE ACTION: REMOVED AND REPLACED MAIN GEAR LOCK SE QUENCE VALVE. IAW M/M 32-32, OPS CHECK NORMAL. 2 L 7 3 4F A3WE 2001062800186 20010628 00186 NM 2001 6 28 SWAA011636 1 20010604 A 2560 P2070001 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 368SW 26579 AFT CABIN UPPER EMERGENCY FLASHLIGHT INOP. Removed and replaced EMERGENCY FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001062800187 20010628 00187 WP 2001 6 28 MWEA011006 1 20010628 A 5310 59124111 FITTING DOUG DC9 DC932 3022066 WP STATION XCW 40 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FRAME ATTACH FITTING FORWARD SPAR CENTER TANK STATION XCW 40 LEFT IS CRACKED. -- LOCATED AND INSTALLED NEW FITTING. 2 L 7 2 4F A6WE 2001062800188 20010628 00188 EA 2001 6 28 JBXA000298 1 20010622 A 7100 CF343B ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE A JBXA O OTHER O OTHER IN INSP/MAINT 1 SO 05 573 7227 872294 Discrepancy: #2 engine borescope inspection task card #021-440-107, HPT stage 1 and 2.Failed inspection.Corrective actio n: Removed and replaced #2 engine IAW CL-65 AMM 71-00-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2001062800189 20010628 00189 NM 2001 6 28 AWXA0001908 1 20010628 A 5730 114N407523 SKIN BOEING 757 7572S7 1384962 NM LT.WS.797 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 D: L/H Wing Leading Edge Slat #1 cracked In the Cove Skin At W.S. 797C: Repaired #1 Slat Per SRM 51-70-13 Fig 1 Pg 1 2 L 7 2 4F RT A2NM 2001062800190 20010628 00190 SO 2001 6 28 SIMA200115801 1 20010607 A 7100 ENGINE EMB 145 EMB145LR SO A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 647AE 145222 ON TAKEOFF, E1 ATTS NO MARGIN. ABORTED TAKEOFF. REMOVED AND REPLACED LEFT ENGNIE IAW WC 05-50-00-400-801-A RUN AND OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001062800191 20010628 00191 EA 2001 6 28 UHLA003506 1 20010523 A 3350 6104789 BATTERY PACK DHAV DHC8 DHC8311 1386006 EA WEAK A UHLA K NONE L NO TEST IN INSP/MAINT 1 NE 03 806SA 279 BUF/RON - DURING OVERNIGHT MAINTENANCE, AFT AND RIGHT OUTSIDE EMERGENCY LIGHT WERE INOPERATIVE. REMOVED AND REPLACED RO W 11 NR 2 EMERGENCY BATTERY PACK IAW DMM 33-51-00. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 2001062800192 20010628 00192 NM 2001 6 28 USAASB01172 1 20010613 A 3350 20131A BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 23559 PHL - MAINTENANCE FOUND VARIOUS EMERGENCY LIGHTS IN THE FORWARD, MIDDLE AND AFT CABIN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACKS AT THE FORWARD LEFT, MIDDLE LEFT, AND AFT LEFT SIDE OF CABIN. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001062800193 20010628 00193 NM 2001 6 28 USAASB01169 1 20010608 A 3350 6104789 BATTERY PACK BOEING 737 737201 1384454 NM FWD CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 245US 22751 BDL - MAINTENANCE FOUND THE L1 AND R1 DOOR EMERGENCY EXIT IDENTIFIER LIGHTS DIM DURING TEST. MAINTENANCE REMOVED AND RE PLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 2001062800194 20010628 00194 CE 2001 6 28 FJT01031261 1 20010301 A 5200 45A5310141 DOOR SEAL MTSBSI MU300 MU300 5780602 CE CABIN DOOR WORN A FJTA O OTHER O OTHER CL CLIMB 1 SO 03 126GA A059SA BNA - CREW REPORTED DURING CLIMB TO 27,000 FT GOING THROUGH APPROXIMATELY 26,000 FT JUST PRIOR TO CABIN ATTAINING MAXIMU M DIFFERENTIAL A LOUD HOWL WAS HEARD FROM THE CABIN DOOR WHICH TURNED INTO A LOUD WHINING SOUND WHEN AIRCRAFT LEVELED AT 27,000 FT. CREW NOTICED THAT CABIN WAS CLIMBING AT A RATE OF 2,000 FT PER MINUTED. CREW ELECTED TO DAWN OXYGEN MASKS AND DROP PASSENGER MASK AND DESCENDED TO 10,000 FEET. AT APPROXIMATELY 10,000 FT THE CABIN HAD STABILIZED TO ZERO RATE OF CLIMB AND CABIN ALTITUDE OF APPROXIMATELY 2,500 FT. AN UNEVENTFUL LANDING WAS MADE IN BNA. INSPECTION OF THE DOOR S EAL REVEALED A PUNCTURE OF THE DOOR SEAL, CAUSE UNKNOWN. DEFECTIVE CABIN DOOR SEAL WAS REPLACED GROUND CHECKS PERFORMED 2 H 7 2 4F RT A14SW 2001062800195 20010628 00195 2001 6 28 GLBA2001133 4 20010624 A 3400 066030620008 ALTIMETER BEECH 1900 1900D 1154162 CE CAPTAINS INOPERATIVE A GLBA D RETURN TO BLOCK O OTHER CL CLIMB 1 CE 01 202UX 130 UE202 CAPTAINS ALTIMETER FLAGGED, REPLACED ALTIMETER OPS CHECKED SATISFACTORY 2 L 7 2 4T RT A24CE 2001062900001 20010629 00001 EU 2001 6 29 MALA010500 1 20010524 A 3320 BALLAST SAAB SF340 SF340A 7850100 EU CABIN FAULTY A MALA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 89XJ 089 FA NOTED A BURNING ELECTRICAL SMELL ON FLIGHT 2836 TO ABR. NO EMERGENCY DECLARED. CREW FOUND FLUORESCENT LIGHT INOP AT 9A. SUSPECT BALLAST BURNT. MAINTENANCE INSPECTED CABIN AREA, SMELL WAS LIMITED TO 9A OVERHEAD LIGHT AREA. LIGHT IS N OW INOP. SUSPECT BULB BALLAST BURNT OUT: DEFERRED OVERHEAD LIGHT 9A IAW MEL 33-20-1C. ENTERED ITEM INTO DMR DISPATCH A ND MXC NOTIFIED. 2 L 7 2 4T RT A52EU 2001062900002 20010629 00002 EU 2001 6 29 MALA010501 1 20010526 A 3230 HP848430721 CONTROL VALVE SAAB SF340 SF340A 7850100 EU LANDING GEAR DEFECTIVE A MALA K NONE J WARNING INDICATION AP APPROACH 1 GL 15 103XJ 340A103 DURING FLIGHT 3178 FROM RFD TO DTW, LANDING GEAR SELECTED DOWN, INTRANSIT REMAINED ILLUMINATED WITH NO GREEN LIGHTS. CHE CKED CIRCUIT BREAKER, FOLLOWED QRH, IT CALLED FOR EMERGENCY EXTENSION AND THE GEAR (ALL THREE) CAME DOWN AND LOCKED. MA INTENANCE REPLACED THE LANDING GEAR CONTROL VALVE P/N HP848430-721, S/N OFF 1167 S/N ON 2059. FOR DETAILS ALL WORKED PE RFORMED REFER 409 CARD 133427. ALL WORK PERFORMED IAW SAAB MM CHAP 32. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2001062900003 20010629 00003 EU 2001 6 29 MALA010502 1 20010526 A 3241 ACM28076 TRANSDUCER BAC 146 AVRO146RJ85A 1500097 EU NR 4 WHEEL FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 501XJ E2208 ANTI-SKID FAULT ILLUMINATED CLIMBING OUT ABOUT 10 MINUTES AFTER DEPARTURE FROM MSP ON FLIGHT 3533. NOTE: SPOILERS DEPLO YED NORMALLY ON LANDING. MAINTENANCE INSPECTED ANTI-SKID COMPUTER FAULT CODES, AND FOUND NR 4 WHEEL SPEED X-DUCER AT FA ULT. REPLACED NR 4 TRANSDUCER P/N ON/OFF ACM28076, S/N ON SV200, S/N OFF UW042 IAW AVRO MM 31-41-44. OPS CHECK GOOD DU RING GROUND TEST. NO FAULTS DURING TEST. 2 H 7 4 4F RT A49EU 2001062900004 20010629 00004 EU 2001 6 29 MALA010503 1 20010527 A 3020 44730501 MODULE SAAB SF340 SF340A 7850100 EU LT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 119XJ 119 DURING FLIGHT 3079 LT INTAKE ENGINE ANTI-ICE LT INTAKE WARNING LIGHT ILLUMINATED. MAINTENANCE REPLACED THE DE-ICE MODUL E P/N 44730-501, S/N ON A00202. RAN LT ENGINE FOR 1 HOUR WITH ENGINE DE-ICE/ANTI-ICE SELECTED. ALL CHECKS GOOD AT THIS TIME. ALL IAW SF340 & GE MM. 2 L 7 2 4T RT A52EU 2001062900005 20010629 00005 NE 2001 6 29 MALA010504 2 20010330 A 7530 216118216 BLEED BAND BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 3 ENGINE MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 512XJ E2328 DURING FLIGHT 3599 IN MEM, DURING T/O NR 3 ENGINE N2=98.1, EGT=647, N1=89, NR 3 N1 DID NOT SYNC WITH OTHER ENGINES. SHU T OFF AUTO THROTTLE TO BRING NR 3 ENG THROTTLE BACK TO KEEP EGT BELOW LIMIT. N2 ON PED BLINKING. AC DID AIR RETURN. M AINTENANCE REPLACED BLEED BAND P/N 2-161-182-16 IAW AMM 75-30-03 401 AND PERFORMED COMPRESSOR BLEED BAND TEST IAW 75-30- 04. OPS CHECK GOOD. 2 H 7 4 4F 4 F RT A49EU E6NE 2001062900006 20010629 00006 NE 2001 6 29 MALA010505 2 20010527 A 7532 7858023 BLEED VALVE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 414XJ 340B414 FLIGHT 3199 OUT OF MSP, LT BLEED FAULT AND LT BLEED CLOSED LIGHTS ILLUMINATED SHORTLY AFTER T/O. ATTEMPTED TO RESET WIT H NO EFFECT. CLOSED LT BLEED VALVE AND FAULT LIGHT EXTINGUISHED AFTER ABOUT 5 MINUTES. AIR RETURN TO MSP. MAINTENANCE REPLACED LT LP REG. VALVE P/N 785802-3, S/N ON 9611050, S/N OFF 9610013 IAW AMM 36-11-05-2. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2001062900007 20010629 00007 EU 2001 6 29 MALA010506 1 20010525 A 2611 WIRE SAAB SF340 SF340A 7850100 EU SMOKE DETECTOR BROKEN A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 106XJ 106 CARGO SMOKE DETECT WILL NOT TEST PROPERLY. LAV AND AVIONICS SMOKE DETECT TEST PROPERLY. ON LAMPS TEST ALL LIGHTS DO IL LUMINATE. MAINTENANCE INSPECTED AC FOUND SAFE FOR FERRY FLIGHT FROM SCE TO DTW WITH CARGO SMOKE DETECTOR INOP. MAINTEN ANCE IN DTW REPAIRED BROKEN WIRE WK112-24. SECURITY CHECK GOOD. PERFORMED FUNCTIONAL CHECK OF CARGO SMOKE SYSTEM. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2001062900008 20010629 00008 EU 2001 6 29 MALA010507 1 20010525 A 3020 WARNING LIGHT SAAB SF340 340B 7860101 EU COCKPIT ILLUMINATED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 444XJ 444 ON FLIGHT 3333, LT INTAKE LIGHT ON. AIR RETURN TO MSP. MAINTENANCE SWAPPED THERMISTOR CANNON PLUG FROM NR 4 TO 5. OPS CHECK GOOD ON LT SHOEBOX. 2 L 7 2 4T RT A52EU 2001062900009 20010629 00009 EU 2001 6 29 MALA010509 1 20010531 A 3020 44730501 MODULE SAAB SF340 340B 7860101 EU RT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 437XJ 340B437 DURING FLIGHT 2934, IN ICING CONDITIONS, RT INTAKE LIGHT ILLUMINATED. QRH PROCEDURE FOLLOWED, BUT NO FIX, UNDER DIRECTI ON OF MX CONTROL, RT INTAKE CIRCUIT BREAKER CYCLED, BUT NO FIX. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED DE -ICE CONTROL MODULE P/N 44730-501, S/N OFF A00072, S/N ON A000281 IAW ACTMM 30-21-03. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2001062900010 20010629 00010 SO 2001 6 29 SWIA972592 1 20010525 A 3697 WIRE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE BLEED AIR SYS LOOSE A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 294SW 120321 JUST AFTER DEPARTURE FROM PDX, RECEIVED A DUCT LEAK WARNING ON MAP AND UPPER PANEL (RIGHT PACK). FOLLOWED QRH PROCEDURE . LIGHT DID NOT EXTINGUISH. RETURNED FOR LANDING AT PDX. LIGHT EXTINGUISHED ON DESCENT AT ABOUT 1500 FT. OPENED PANE LS, INBOARD LEADING EDGE, CHECKED BLEED AIR DUCTING, CLAMPS, AND SENSORS. FOUND SENSOR JUST INBOARD OF RIB NACELLE WITH LOOSE WIRE. RECONNECTED WIRE PER WIRING MANUAL 20-40-00. 2 L 7 2 4T 4 T RT A31SO E20NE 2001062900011 20010629 00011 SO 2001 6 29 SWIA972599 1 20010528 A 3150 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT ACTIVATED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 204SW 120243 ABORTED TAKEOFF DUE TO T/O AURAL WARNING; TRIM WHEEL WELL WITHIN THE GREEN ARC. RESET CB FOR AURAL WARNING UNIT. CYCLE D AURAL WARNING AND PERFORMED TAKEOFF CHECKS. GROUND CHECK NORMAL. WARNING TRIM WARNINGS CHECK NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 2001062900012 20010629 00012 SO 2001 6 29 SWIA972600 1 20010526 A 3260 DOOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE NLG UNLATCHED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 268UE 120207 RED NOSE GEAR LIGHT REMAINED ON AFTER GEAR RETRACTION AND RECYCLE. RETURNED TO PSP. LATCHED NOSE GEAR DOORS. SYSTEM O PS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001062900013 20010629 00013 WP 2001 6 29 MWEA010825 1 20010524 A 5311 99196053 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 UPPER FUSELAGE FRAME STATION 929 HAS MECHANICAL DAMAGE IN RADIUS INBOARD LONGERON 8 LEFT. REMOVED, LOCATED AND DRILLED FRAME SECTION, FABRICATED SPLICE, INSTALLED SPLICE AND FRAME SECTION. 2 L 7 2 4F A6WE 2001062900014 20010629 00014 WP 2001 6 29 MWEA010826 1 20010524 A 5320 3917624515 FITTING DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 ELONGATED HOLES ON VENTRAL DOOR JAMB FITTING RIGHT SIDE BACK SIDE OF JAMB. REMOVED FITTING, CUT OUT DAMAGE HOLE AREA, F ABRICATED DOUBLER AND FILLER, LOCATED, DRILLED AND INSTALLED DOUBLER AND FITTING. 2 L 7 2 4F A6WE 2001062900015 20010629 00015 WP 2001 6 29 MWEA010830 1 20010601 A 5320 59667602 FITTING DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 FITTING AT STATION 1104 RIGHT VENT STAIRWAY JAM FOUND TO BE OUT OF LIMITS. REMOVED FITTING, FABRICATED FITTING, LOCATED , DRILLED AND INSTALLED FITTING. 2 L 7 2 4F A6WE 2001062900016 20010629 00016 WP 2001 6 29 MWEA010831 1 20010601 A 5321 99579261 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN PUNCTURED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 CABIN FLOORBOARD E-14 HAS A PUNCTURE HOLE. REMOVED DAMAGED AREA, LOCATED, DRILLED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001062900017 20010629 00017 WP 2001 6 29 MWEA010832 1 20010601 A 5321 991559714 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 CABIN FLOORBOARD A4 HAS A CRACK ON AFT END. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001062900018 20010629 00018 WP 2001 6 29 MWEA010833 1 20010601 A 5321 9957717501 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 CABIN FLOORBOARD B9, FORWARD END HAS WORN HOLES. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED SKIN SPLICE AND STRAP. 2 L 7 2 4F A6WE 2001062900019 20010629 00019 WP 2001 6 29 MWEA010834 1 20010601 A 5321 99579181 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 CABIN FLOORBOARD B8 HAD DAMAGE AND CRACKS. REMOVED DAMAGE, FABRICATED AND INSTALLED DOUBLER AND FILLER. 2 L 7 2 4F A6WE 2001062900020 20010629 00020 WP 2001 6 29 MWEA010835 1 20010601 A 5321 995791820 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 CABIN FLOORBOARD F3 HAS TWO HOLES WITH CRACKS AROUND FASTENERS. FABRICATED FLOOR PANEL SKIN, REASSEMBLED FLOOR PANEL WI TH NEW SECTION OF SKIN. 2 L 7 2 4F A6WE 2001062900021 20010629 00021 WP 2001 6 29 MWEA010837 1 20010601 A 5320 9910078873 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 GALLEY FLOOR AREA, SUBFLOOR AT STATION 200 BETWEEN NR 3 AND 4 SEAT TRACKS HAS A SMALL CRACK. CUT OUT DAMAGED AREA, FABR ICATED AND INSTALLED REPAIR DOUBLER AND FILLER. 2 L 7 2 4F A6WE 2001062900022 20010629 00022 WP 2001 6 29 MWEA010838 1 20010603 A 3230 29200331 BRACKET DOUG DC9 DC932 3022066 WP LT MLG WORN A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 502ME 48132 LEFT GEAR UNSAFE LIGHT CAME ON. REPLACED LATCH ROLLER BRACKET. 2 L 7 2 4F A6WE 2001062900023 20010629 00023 EU 2001 6 29 QXEA0100767 1 20010508 A 5744 SUPPORT FOKKER F28 F28MK4000 4990810 EU RT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 YYC - RIGHT-HAND INBOARD FLAP A-FRAME SUPPORT ASSEMBLY HAS OVER SIZED BORES IN AFT 3 ATTACH HOLES. OVERSIZE HOLES REAME D TO .3125 MIN FOR 5/16 BOLT AS PER FOKKER SRM 51-32-01, PAGE 11, TABLE 6. BOLTS INSTALLED PER FOKKER FAX TS01.54655 AN D HORIZON AIR EA 4-57-558. 2 L 7 2 4F RT A20EU 2001062900024 20010629 00024 NM 2001 6 29 DLM88010813 1 20010521 A 3260 WARNING LIGHT DOUG MD88 MD88 3023688 NM COCKPIT FALSE INDICATION A DALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 27 914DE 49957 ALL 3 GEAR LIGHTS INDICATED RED ON EXTENSION. F/O WIGGLED HANDLE AND ALL WENT GREEN. TOWER CONFIRMED GEAR DOWN ON FLYB Y. JACKED AIRCRAFT AND SWUNG GEAR. UNABLE TO DUPLICATE OR FIND FAULT. 2 L 7 2 4F RT A6WE 2001062900025 20010629 00025 NM 2001 6 29 DLM88010842 1 20010525 A 2170 COALESCER BAG DOUG MD88 MD88 3023688 NM A/C BAY CONTAMINATED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 985DL 53312 FLT ATT REPORTED SMELL FROM AFT OF A/C ON TAKEOFF OUT OF CHS SMELL SMOKE, BUT NO SMOKE. TRANSFER FEEDS CLOSED. AIRFOIL A/I OFF ENG A/I OFF. APU OFF, SMOKE DISSIPATED AFTER 5 MINS. REPLACED COALESCER BAGS. 2 L 7 2 4F RT A6WE 2001062900026 20010629 00026 2001 6 29 DLM88010857 4 20010527 A 2340 TA4715 RECEPTACLE DOUG MD88 MD88 3023688 NM CABIN BURNED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 923DL 49705 FLT ATTN CALL LIGHT WILL NOT RESET AT AFT POSITION. FOUND CANNON PLUG AT SEAT ROW 16DE BURNT. REPLACED CANNON PLUG FLT ATTN CALL LIGHT, SYS OPS CKS GOOD. 2 L 7 2 4F RT A6WE 2001062900027 20010629 00027 NE 2001 6 29 DLM88010898 2 20010603 A 7250 TURBINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE DAMAGED A DALA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SO 27 938DL 35370 49811 716789 CLIMBING THROUGH 22,000 FT, RIGHT ENGINE BANGED AND NOTED EGT DECREASING THROUGH 650 DEG C WITH INDICATIONS THAT ENGINE WAS ROLLING BACK. ENGINE SHUT DOWN AND RETURNED TO ATL. FOUND TURBINE SECTION DAMAGED. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A6WE E9NE 2001062900028 20010629 00028 CE 2001 6 29 GLBA2001115 1 20010531 A 3297 WIRE BEECH 1900 1900D 1154162 CE LANDING GEAR SYS CHAFED A GLBA O OTHER J WARNING INDICATION DE DESCENT 1 CE 01 208GL UE208 LANDING GEAR WOULD NOT EXTEND ON COMMAND C/B POPPED. INSPECTED FOUND CHAFED WIRE AND REPAIRED, OPS CHECKED SYSTEM SATIS FACTORY. 2 L 7 2 4T RT A24CE 2001062900029 20010629 00029 2001 6 29 HNAA0100033 4 20010603 A 3460 7003975901 CONTROLLER DHAV DHC8 DHC8102 2809003 NM COCKPIT FAULTY A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 910HA 26141 6 022 ON DEPARTURE FROM LGA, AUTO PILOT ENGAGED WITHOUT COMMAND. AFTER CANCELLING AUTO PILOT REMAINS ILLUMINATED BOTH YAW DAM PER CARROTT AND HSI CARROTT REMAIN ON. REMOVED AND REPLACED FGC CONTROLLER. 2 H 7 2 4T RT A13NM 2001062900030 20010629 00030 EA 2001 6 29 HNAA0100034 1 20010604 A 2920 HYDRAULIC SYSTEM DHAV DHC8 DHC8311 1386006 EA NR 2 SYS OVERSERVICED A HNAA O OTHER J WARNING INDICATION CR CRUISE 1 EA 07 327EN 261 LOSS OF NR 1 HYDRAULIC SYSTEM FLUID IN FLIGHT. NR 1 HYDRAULIC ISO VALVE LIGHT AND ROLL SPOILER INBOARD LIGHT ILLUMINATE D. NR 1 HYDRAULIC SYSTEM DID NOT GO TO ZERO. FOUND NR 2 HYDRAULIC SYSTEM OVERSERVICED AND OVERSPILL CONTAINER FULL. I NSPECTED FILTERS AND BYPASS INDICATORS, NO DEFECTS NOTED. OPERATED HYDRAULIC SYSTEMS, NO LEAKS OR FLUID LOSS NOTED. 2 H 7 2 4T RT A13NM 2001062900031 20010629 00031 NM 2001 6 29 HNAA010032 1 20010529 A 3234 574205A SELECTOR VALVE DHAV DHC8 DHC8102 2809003 NM LANDING GEAR FAILED A HNAA K NONE J WARNING INDICATION AP APPROACH 1 EA 07 910HA 21764 10 022 THE GEAR WOULD NOT EXTEND WHEN SELECTED DOWN. CREW PERFORMED ALTERNATE EXTENSION. REPLACED LANDING GEAR SELECTOR VALVE . 2 H 7 2 4T RT A13NM 2001062900032 20010629 00032 EA 2001 6 29 JBXA000287 1 20010604 A 5270 HANDLE CNDAIR CL600 CL6002B19 EA PAX DOOR DIRTY A JBXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 05 586 7341 A/C DEPARTED RDU ENROUTE FOR ATL, ON CLIMBOUT CREW RECEIVED A PAX DOOR OUTER HANDLE CAUTION MESSAGE. A/C RETURNED TO RD U. MAINTENANCE INSPECTED DOOR FOR ANY DEFECTS. MAINTENANCE THEN CLEANED AND LUBRICATED PAX DOOR INNER HANDLE AND PERFO RMED OPERATIONAL TEST OF PAX DOOR IAW CL-65 AMM 52-70-04. NO FAULT NOTED AT THIS TIME. A/C THEN DEPARTED RDU FOR ATL W ITH NO FURTHER PROBLEMS. 2 L 7 2 4F RT A21EA 2001062900033 20010629 00033 EU 2001 6 29 MALA010508 1 20010531 A 6120 CONTROL UNIT SAAB SF340 340B 7860101 EU LT PROP FLUCTUATES A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 438XJ 438 DURING FLIGHT 3200 OUT OF DTW, LT PROP RPM FLUCTUATES AFTER T/O. LT PROP CYCLED 20-30 RPM WITH SYNC ON, TURNED PROP SYN C OFF, NO HELP. MOVE CONDITION LEVER, NO HELP. LT PROP OIL PSI=100 PSI AND OIL TEMP WAS IN GREEN ARC. AIR RETURN TO D TW. MAINTENANCE RAN LT ENGINE AT VARIOUS POWER SETTINGS NO FLUCTUATION LT PROP Z NOTED. PROP SYNC OPERATED NORMAL. NO DISCREPANCIES NOTED. 2 L 7 2 4T RT A52EU 2001062900034 20010629 00034 NM 2001 6 29 PCAA0105044 1 20010525 A 3350 2078 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 820EX 9203 6044 019 BGM- DURING ROUTINE MAINTENANCE VISIT AFT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED AFT POWER SUPPLY OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001062900035 20010629 00035 NM 2001 6 29 PCAA0105045 1 20010526 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 829EX 146 MDT- DURING ROUTINE MAINTENANCE VISIT RIGHT FORWARD EMERGENCY LIGHTS ALONG FUSELAGE FOUND INOPERATIVE. MAINTENANCE REPL ACED THE POWER SUPPLY BOX IN POSITION 200. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001062900036 20010629 00036 SO 2001 6 29 RAIA00105015 1 20010513 A 3020 C1460092 ANTI-ICE VALVE EMB 145 EMB145LR SO LT ENGINE FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 811HK 1118 145256 5288-BOS-LEFT ENGINE ANTI-ICE VALVE WILL NOT OPEN. MAINTENANCE INSPECTED AND REPLACED LEFT ENGINE ANTI-ICE VALVE. 2 L 7 2 4T RT T00011AT 2001062900037 20010629 00037 EU 2001 6 29 RAIA00105016 1 20010515 A 3610 NSA8206145 SEAL AEROSP ATR42 ATR42300 8680920 EU BLEED AIR SYS FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 426TE 228 7153-MEM-LEFT BLEED LEAK, PACK AND BLEED FAULTED DURING TAXI. MAINTENANCE INSPECTED AND REPLACED LEFT AND RIGHT WING LE ADING EDGE BLEED AIR SEALS. 2 H 7 2 4T RT A53EU 2001062900038 20010629 00038 EU 2001 6 29 RAIA00105017 1 20010521 A 3320 OL3112 LIGHT AEROSP ATR42 ATR42300 8680920 EU CABIN DEFECTIVE A RAIA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 CE 03 422TE 106 7145-STL-NO SMOKING/FASTEN SEAT BELT SIGN CIRCUIT BREAKER POPS WHEN NO SMOKING/FASTEN SEAT BELT SIGNS ARE TURNED ON. MAI NTENANCE INSPECTED AND DEFERRED SYSTEM IAW ATR42 MEL. MAINTENANCE REPLACED BULBS AT SEAT 2CD NO SMOKING/FASTEN SEAT BELT SIGN. 2 H 7 2 4T RT A53EU 2001062900039 20010629 00039 EA 2001 6 29 SWIA972601 1 20010516 A 2761 PCU CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE SPOILERONS MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 426SW 7468 LEFT SPOILERONS FAULT STATUS MESSAGE ON PDI2 IN FLIGHT. REMOVE AND REPLACE LEFT SPOILERON OUTBOARD PCU IAW 27-62-00 AND RESET CB4CN THEN CLEARED SECU FAIL LOGS. OPS CHECKS GOOD ON FLIGHT CONTROL. NO DEFECTS NOTED AT THIS TIME. P/N ON 27 000-7, S/N ON MAL-347, S/N OFF 3979. 2 L 7 2 4F 4 F RT A21EA E15NE 2001062900040 20010629 00040 SO 2001 6 29 SWIA972602 1 20010529 A 2422 RELAY EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE ELECTRICAL PWR FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 567SW 120342 LOST NR 1 INVERTER ON CLIMBOUT, 115 VAC. REMOVED AND REPLACED 115 VAC SENSE RELAY K0005. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001062900041 20010629 00041 SO 2001 6 29 SWIA972605 1 20010518 A 5270 SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FWD DOOR OUT OF ADJ A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 295UX 120295 FORWARD DOOR LIGHT ILLUMINATED DURING TAKEOFF ROLL. ABORTED AND RETURNED TO GATE. ADJUSTED BOTH FORWARD DOOR SWITCHES. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001062900042 20010629 00042 2001 6 29 SWIA972606 4 20010519 A 2216 SERVO EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RUDDER DEFECTIVE A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 212SW 120276 IN CRUISE FLIGHT, WITH AUTOPILOT ON, EXPERIENCED A SUDDEN YAW MOVEMENT AND BALL WENT OUT OF CENTER. RETRIMMED WITH NO PR OBLEMS. THEN IN DESCENT, WITH AUTOPILOT OFF, NOTICED TRIM WOULD NOT CENTER BALL. THEN 2 OR 3 MINUTES LATER THERE WAS A NOTHER SUDDEN YAW. AP WAS OFF ON DESCENT, BUT YAW DAMPER WAS ON THROUGHOUT FLIGHT. FERRIED TO SLC FOR MAINTENANCE. RE PLACED RUDDER TRIM SERVO IAW MM 32-10-05. OPS CHECKS GOOD. P/N, S/N ON 8092, OFF 5875. 2 L 7 2 4T 4 T RT A31SO E20NE 2001062900043 20010629 00043 SO 2001 6 29 SWIA972607 1 20010531 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE T/E FLAP LEAKING A SWIA A UNSCHED LANDING K F J FLUID LOSS FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 232SW 120306 LOST ALL HYDRAULIC BLUE SYSTEM FLUID. LOW PSI, LOW RESERVOIR WARNING LIGHTS. MAIN PUMP LOW PRESSURE INDICATION FOR BLU E SYSTEM. RETURNED TO SFO. REPLACED LEFT NACELLE FLAP ACTUATOR PER MM 27-50-00 AND CHECKED BLUE SYSTEM HYDRAULIC FILTE RS. ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001062900044 20010629 00044 SO 2001 6 29 SWIA972608 1 20010531 A 3150 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT FALSE ACTIVATION A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 195SW 120127 FLAP AURAL WARNING ON TAKEOFF ROLL. PERFORMED TAKEOFF WARNING TEST IAW MM 27-50-00, PAGES 516-518. OPS CHECK GOOD, NO DEFECTS NOTED. 2 L 7 2 4T 4 T RT A31SO E20NE 2001062900045 20010629 00045 SO 2001 6 29 SWIA972609 1 20010524 A 5270 LATCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FUEL DOOR UNLATCHED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 584SW 120352 ABORTED TAKEOFF AND RETURNED TO GATE BECAUSE SERVICE DOOR LIGHT CAME ON. RESECURED FUEL DOOR LATCH. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001062900046 20010629 00046 SO 2001 6 29 SWIA972612 1 20010602 A 5753 ROLLER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE T/E FLAP WORN A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 212SW 120276 AFTER T/O WHEN SELECTING FLAPS UP, OUTBOARD PAIR DISAGREEMENT WOULD NOT CLEAR AFTER QRH PROCEDURE. RETURNED TO SLC. TR OUBLESHOOT SYSTEM, FOUND LEFT OUTBOARD FLAP TRACKS AND ROLLERS WORN. REMOVED AND REPLACED (4) FLAP ROLLERS, (3) FLAP TR ACKS. ROLLER P/N PE61026-1 IAW EMB 120 MM 27-50-12. P/N ON 120-33507-0035, P/N OFF 120-33045-501. P/N ON 120-33045-50 1, P/N OFF 120-333501-003. P/N ON 120-33018-001, P/N OFF 120-3304-001. 2 L 7 2 4T 4 T RT A31SO E20NE 2001062900047 20010629 00047 SO 2001 6 29 SWIA972613 1 20010603 A 2751 ANNUNCIATOR EMB 120 EMB120RT SO PWA 118 PW118 NE COCKPIT MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 137H 120137 FLAP DISAGREEMENT ON TAKEOFF, DURING RETRACTION. REPLACED FLAP ANNUNCIATOR UNIT PER MM 27-50-00. OPS CHECK GOOD ON GRO UND. P/N: 306900-1017, S/N ON: 0010, S/N OFF: 0217. CHANGED ALL WORN FLAP ROLLERS (8) AND FLAP TRACKS (3). REPLACE D RIGHT INBOARD FLAP ACTUATOR IAW MM 27-50-00. OPS AND LEAK CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001062900048 20010629 00048 SO 2001 6 29 SWIA972614 1 20010526 A 4930 FUEL CONTROL EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE APU FAULTY A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 233SW 120307 UPON LIFT OFF FROM PDX, STRONG FUEL SMELL NOTED IN CABIN AND FLIGHT DECK. APU BLEED WAS POWERING BOTH PACKS. INSPECTED APU AND BLEED SYSTEM. NO FAULTS NOTED. REMOVED AND REPLACED APU FUEL CONTROL UNIT. OPS CHECK GOOD IAW ALLIED SIGNAL MM 49-00-00. P/N: 3882730-9, S/N ON: A1124, S/N OFF: 15683. 2 L 7 2 4T 4 T RT A31SO E20NE 2001062900049 20010629 00049 WP 2001 6 29 ZW0A0102505 1 20010529 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND CORROSION ON CABIN MEMBRANE AT STA 148 TO 160, RBL 10 TO RBL 18. CUT OUT CORROSION PER SRM 5 1-70-4 AND SPM 6-80-01. TREATED PER SRM 51-10-3. REPAIRED MEMBRANE PER SRM 51-70-4 AND SRM 53-14-1. INSTALLED FASTENE RS PER SRM 51-30-2 AND SRM 51-30-5. SEALED PER SRM 51-20-0. 2 L 7 2 4F RT A6WE 2001062900050 20010629 00050 WP 2001 6 29 ZW0A0102506 1 20010529 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 907TW 49165 DURING CHECK-C MAINT FOUND CRACK IN LOWER AFT INBD CORNER OF RT WHEEL WELL IN SUPPORT AND REPAIR DOUBLER, APPROX STA 988 . REPLACED SUPPORT AND FASTENERS PER SPM 6-70-01 AND SRM 51-30-5 AND SRM 51-30-2. 2 L 7 2 4F A6WE 2001062900051 20010629 00051 WP 2001 6 29 ZW0A0102507 1 20010529 A 5320 SUPPORT BRACKET DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 907TW 49165 DURING CHECK-C MAINT THE SUPPORT BRACKET WAS CRACKED IN THREE AREAS AT FWD OTBD CORNER OF KEEL BEAM, INTERNAL STA 938 AP PROX 3 INCHES ABOVE SKIN. REPLACED SUPPORT BRACKET PER DRAWING 9936368. 2 L 7 2 4F A6WE 2001062900052 20010629 00052 WP 2001 6 29 ZW0A0102508 1 20010529 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 907TW 49165 DURING CHECK-C MAINT THE FWD LT CORNER OF KEEL BEAM INTERNAL STRUCTURE WAS CRACKED APPROX 3.5 IN AT STA 938 ABOVE AND FW D OF LT GEAR DOOR. REPLACED INTERCOSTAL PER DRAWING 9936368. 2 L 7 2 4F A6WE 2001062900053 20010629 00053 WP 2001 6 29 ZW0A0102509 1 20010529 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 907TW 49165 DURING CHECK-C MAINT FOUND LONGERON 22L CORRODED AT STA 1297. REMOVED CORRODED AREA AND INSTALLED FILLER AND SPLICES PE R SRM 53-02, FIG 18. 2 L 7 2 4F A6WE 2001062900054 20010629 00054 WP 2001 6 29 ZW0A0102510 1 20010530 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 907TW 49165 DURING CHECK-C MAINT FOUND STA 1309 FORMER RING CORRODED BETWEEN LONGERON 27L AND 27R. REMOVED CORROSION PER SPM 6-80-0 1 AND SPLICED IN NEW SECTION PER SRM 53-03, FIG 2A. 2 L 7 2 4F A6WE 2001062900055 20010629 00055 WP 2001 6 29 ZW0A0102511 1 20010530 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 907TW 49165 DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 160 TO 200, RBL 53. REMOVED AND INSTALLED NEW FLOOR SUPPOR T MADE FROM SAMPLE EXTRUDED AND INSTALLED PER SRM 51-30-2. 2 L 7 2 4F A6WE 2001062900056 20010629 00056 WP 2001 6 29 ZW0A0102512 1 20010530 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 907TW 49165 DURING CHECK-C MAINT FOUND CRACK IN MEMBRANE ON RT SIDE AT STA 217, UNDER NUMBER 5 FLOOR PANEL, AND FOUND CORROSION AT S TA 200. INSTALLED 7075-T6 0.025 MEMBRANE PER SRM 51-30-02. 2 L 7 2 4F A6WE 2001062900057 20010629 00057 WP 2001 6 29 ZW0A0102513 1 20010530 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 907TW 49165 DURING CHECK-C MAINT FOUND CORROSION ON TRACK NUMBER 5, STA 200 TO 246, SEVERAL PLACES ON FLOOR SUPPORT. REPLACED CORRO DED SECTION OF TRACK FROM STA 200-246 WITH NEW. REPLACED EXISTING SPLICE PER 53-05, FIG 4F. ALSO REMOVED CORROSION FRO M FLOOR SUPPORT AREA AND TREATED AREA. 2 L 7 2 4F A6WE 2001062900058 20010629 00058 WP 2001 6 29 ZW0A0102514 1 20010530 A 5520 RIVET DOUG DC9 DC982 3022082 WP ELEVATOR CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 929TW 48014 DURING CHECK-C MAINT ON THE INBD LT ELEVATOR, FWD OF INBD MOUNT, HAD A METAL PLATE WITH RIVET CRACKED OUT. REPLACED MET AL PLATE PER SRM 55-20-0 AND 51-30-02. 2 L 7 2 4F A6WE 2001062900059 20010629 00059 WP 2001 6 29 ZW0A0102515 1 20010531 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 929TW 48014 DURING CHECK-C MAINT FOUND CORROSION ON AFT GALLEY GIRT BAR SUPPORTS. REMOVED CORROSION ON FWD GIRT BAR SUPPORT PER SPM 6-80-01, PAGE 2. REPLACED AFT GIRT BAR SUPPORT PER SRM 51-00 PAGE 27, ITEM B. TREATED PER SRM 51-10-3 PAGE 14. 2 L 7 2 4F A6WE 2001062900060 20010629 00060 WP 2001 6 29 ZW0A0102516 1 20010530 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT IN THE FWD CABIN FOUND CORROSION ON UPPER AND LOWER SIDE OF CUSP AND LOWER FWD DOOR FRAME (FORMER) STRUCTURE FROM STA 165 TO 168, RBL 56 IN TO RBL 60 INCHES. REMOVED CORROSION PER SPM 6-80-01 PAGE 1 ITEM 3A AND PAGE 2B . CORROSION TREATED AREA PER SRM 51-10-3. INSTALLED FASTENERS IN CUSP AND LOWER DOOR FRAME STRUCTURE PER SRM 51-30-2 A ND SRM 51-30-5. SEALED AREA PER SRM 51-20-0. 2 L 7 2 4F RT A6WE 2001062900061 20010629 00061 WP 2001 6 29 ZW0A0102517 1 20010530 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT CORRODED AT STA 200 LBL 6 IN TO RBL 6 IN, STA 200 LBL 6 IN TO RBL 6 IN, A ND STA 160 LBL 3 INCHES. INSTALLED NEW FLOOR SUPPORT AT EACH LOCATION PER SPM 6-70-01, PAGE 3, B, (1), (2) AND PER DRAW ING 9936534, SRM 51-30-2, AND SRM 51-30-5. SEALED PER SRM 51-20-0. 2 L 7 2 4F RT A6WE 2001062900062 20010629 00062 WP 2001 6 29 ZW0A0102518 1 20010530 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT CORRODED AT STA 148 TO 200, LBL 7 INCHES, AND STA 180 TO STA 200, LBL 6 I NCHES. INSTALLED NEW SUPPORTS PER SRM 51-30-1. FINISH PER SRM 51-10-3. 2 L 7 2 4F RT A6WE 2001062900063 20010629 00063 NM 2001 6 29 ZW0A0102601 1 20010531 A 2761 NAS1611021 SEAL BOEING 717 717200 1383700 NM SPOILER WORN A ZW0A H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 13 2404A 55071 THE RT HYDRAULIC QUANTITY DROPPED TO ZERO. PUMPS WERE SHUT OFF AND FLIGHT RETURNED TO STL. NECESSARY TO REPLACE SEALS FOR THE NUMBER 4 FLIGHT SPOILER ACTUATOR RETAINER, P/N NAS1611, NAS1611021, MS28774021, AND NAS 1611-018. NO CHECK-C. 2 L 7 2 4F TR A6WE 2001062900064 20010629 00064 WP 2001 6 29 ZW0A0102602 1 20010530 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT CORRODED AT STA 160 TO 200, RBL 44. REPLACED FLOOR SUPPORT PER SPM 6-70- 01. PAINTED PER SRM 51-10-3. INSTALLED FASTENERS PER SRM 51-30-3. 2 L 7 2 4F RT A6WE 2001062900065 20010629 00065 EU 2001 6 29 QXEA0101071 1 20010625 A 3350 GRIMES FOKKER F28 F28MK4000 4990810 EU A QXEA K NONE O OTHER NR NOT REPORTED 1 NM 09 493US 11161 SEA - EXIT SIGN ATTACHED TO SEAT 8B REPORTED DAMAGED. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001062900066 20010629 00066 WP 2001 6 29 ZW0A0102603 1 20010530 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND CORROSION ON CABIN MEMBRANE BEYOND REPAIRABLE LIMITS. CUT OUT AREA FROM STA 160 TO 200, LBL 8 IN, TO RBL 58 IN. INSTALLED MEMBRANE PER SPM 6-70-01. PAINTED PER SRM 51-30-01. INSTALLED PER SRM 51-30-3. 2 L 7 2 4F RT A6WE 2001062900067 20010629 00067 WP 2001 6 29 ZW0A0102604 1 20010530 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT CORRODED AT STA 148 TO 200, RBL 7 INCHES. REMOVED AND REPLACED FLOOR SUP PORT WITH NEW PER SPM 6-70-01 AND DRAWING 9936534-73. INSTALLED HARDWARE PER SRM 51-30-1, PAGE 11, 12, AND 13. 2 L 7 2 4F RT A6WE 2001062900068 20010629 00068 WP 2001 6 29 ZW0A0102605 1 20010530 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND G1 GALLEY TRACK AREA FLOOR SUPPORT BEAM WAS BADLY CORRODED THE FULL LENGTH FROM STA 160 TO 20 0, RBL 44 INCHES. REPLACED FLOOR SUPPORT PER SPM 6-70-01. PAINTED PER SRM 51-10-3 AND INSTALLED FASTENERS PER SRM 51-3 0-3. 2 L 7 2 4F RT A6WE 2001062900069 20010629 00069 WP 2001 6 29 ZW0A0102606 1 20010530 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT IN AFT CABIN FOUND CORROSION ON MEMBRANE AT STA 1155, LBL 38 INCHES. REPAIRED PER SRM 51-70-4. SE ALED REPAIR PER SRM 51-20-0. TREATED PER SRM 51-10-03. 2 L 7 2 4F RT A6WE 2001062900070 20010629 00070 WP 2001 6 29 ZW0A0102607 1 20010530 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT CORRODED AT STA 180 TO 200, RBL 6 INCHES. REMOVED AND REPLACED PART PER SPM 6-70-01. MADE NEW FLOOR SUPPORT PER DRAWING 9936534-73. INSTALLED USING HARDWARE PER SRM 51-30-1, PAGES 11, 12, AN D 13. 2 L 7 2 4F RT A6WE 2001062900071 20010629 00071 WP 2001 6 29 ZW0A0102608 1 20010530 A 5320 SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND G1 GALLEY TRACK AREA FLOOR CROSS SECTION SUPPORT BEAM AT STA 180, RBL 8 IN TO RBL 43 IN, WAS BADLY CORRODED. FABRICATED NEW FLOOR SUPPORT PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-01. PRIMED AND PAINTE D PER SRM 51-10-3. 2 L 7 2 4F RT A6WE 2001062900072 20010629 00072 WP 2001 6 29 ZW0A0102609 1 20010530 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR SUPPORT AT STA 160 TO 200, RBL 56 INCHES. INSTALLED FLOOR SUPPORT P ER SPM 6-70-01. PAINTED PER SRM 51-30-01. INSTALLED FASTENERS PER SRM 51-10-3 AND SRM 51-10-1, PAGE 21 AND 33. 2 L 7 2 4F RT A6WE 2001062900073 20010629 00073 NM 2001 6 29 ZW0A0102701 1 20010531 A 3350 767 LIGHT BOEING 767 7673Q8 NM CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 636TW 30301 THE EGRESS LIGHTS AT ROWS 37 TO 43 ON RT SIDE OF CABIN, AND THE SECOND EMERGENCY LIGHT AFT OF THE LEFT WING, WERE INOPER ATIVE. SECURED LOOSE WIRES AT ROW 43HJ, AND REPLACED THE LAMP FOR THE EMERGENCY LIGHT. CHECK-C 1-7-01 LAX. 2 L 7 2 4F RT A1NM 2001062900074 20010629 00074 NM 2001 6 29 ZW0A0102702 1 20010601 A 3350 80741 LIGHT BOEING 767 76733AER 1385230 NM CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 637TW 25403 THE EGRESS LIGHT AT CABIN SEAT 38 RT SIDE WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 1-27-01 LAX. 2 L 7 2 4F RT A1NM 2001062900075 20010629 00075 NM 2001 6 29 ZW0A0102703 1 20010531 A 3350 CONNECTOR BOEING 757 7572Q8 1384972 NM CABIN DISCONNECTED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 713TW 28173 WITH POWER REMOVED FROM THE AIRCRAFT THE EMERGENCY EXIT LIGHTS AT ROWS 24 AND 26 ILLUMINATED. FOUND LOOSE ELECTRICAL CO NNECTOR AT M10919 AND SECURED SAME. CHECK-C 7-22-00 LAX. 2 L 7 2 4F RT A2NM 2001120500130 20011205 00130 NE 2001 12 5 ZW0A0102704 2 20010531 A 7230 1B8110 STATOR VANE BOEING 757 757231 1384950 NM PWA 2037 PW2037 NE NR 1 ENGINE FRACTURED A ZW0A E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 CE 13 714P 28482 4905 JUST AFTER TAKEOFF CREW HEARD LOUD NOISE FROM NUMBER 1 ENGINE, FOLLOWED BY EGT GOING TO 653. CREW SHUT DOWN THE ENGINE AND RETURNED TO STL. METAL WAS FOUND IN THE TAIL PIPE AND THE ENGINE WAS REPLACED. FOUND VANES FROM THE 10TH AND 11TH S TAGE COMPRESSOR, QUADRANT NUMBER 4, HAD FRACTURED AT THE 10 O'CLOCK POSITION AND MOVED INTO THE GAS PATH STRIKING THE C- 10 BLADES. THE DAMAGE THEN MULTIPLIED. 2 L 7 2 4F 4 F RT A2NM E17NE 2001062900076 20010629 00076 WP 2001 6 29 ZW0A0102705 1 20010602 A 3350 60030431 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ZW0A K NONE O OTHER CR CRUISE 1 CE 13 9305N 49395 AN OVERWING EMERGENCY EXIT LIGHT REMAINED ON IN FLIGHT. REPLACED THE POWER SUPPLY. CHECK-C 5-7-01 STL. 2 L 7 2 4F RT A6WE 2001062900077 20010629 00077 WP 2001 6 29 ZW0A0102706 1 20010503 A 7830 41000740104 CONTROL VALVE DOUG DC9 DC983 3022083 WP LT T/R LEAKING A ZW0A O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 CE 13 9307R 49663 THE LT HYDRAULIC SYSTEM QUANTITY WAS LOST ON APPROACH. REPLACED THE LT THRUST REVERSER CONTROL VALVE. CHECK-C 1-26-01 MCI. 2 L 7 2 4F RT A6WE 2001062900078 20010629 00078 WP 2001 6 29 ZW0A0102707 1 20010601 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT CORRODED AT STA 200, RBL 52 INCHES. FABRICATED NEW FLOOR SUPPORT PER SPM 6-70-01 PAGE 2, 4, A(1) AND DRAWING 9936531. CORROSION TREATED PART PER SRM 51-10-3. INSTALLED FLOOR SUPPORT PER SPM 6-70-01 PAGE 3 AND DRAWING 9936534 AND SRM 51-30-02. SEALED SUPPORT PER SRM 51-20-0. 2 L 7 2 4F RT A6WE 2001062900079 20010629 00079 WP 2001 6 29 ZW0A0102708 1 20010601 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND CABIN SEAT TRACK AND FLOOR CORROSION ON DIAPHRAGM TOP AND BOTTOM, STA 1174 TO 1309, LONGERON 18L BETWEEN NUMBER 1 TRACK AND SIDEWALL. CUT OUT WEB AND REPAIRED PER SRM 51-70-4, PAGE 1, FIG 1, SHEET 2. 2 L 7 2 4F RT A6WE 2001062900080 20010629 00080 WP 2001 6 29 ZW0A0102709 1 20010601 A 5320 FITTING DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND CORROSION IN FITTING, AFT LOWER CORNER OF DOOR OPENING. INSTALLED NEW FITTING PER SPM 6-70-01. SEALED PER SRM 51-10-03. 2 L 7 2 4F RT A6WE 2001062900081 20010629 00081 WP 2001 6 29 ZW0A0102801 1 20010601 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT IN E/E COMPT FOUND CORROSION ON BOTTOM OF MEMBRANE AT STA 200, RBL 22 TO RBL 44. REMOVED CORRODED AREA OF MEMBRANE, FABRICATED NEW MEMBRANE FROM SAME TYPE MATERIAL AND TREATED PER SRM 51-10-3. INSTALLED PER SRM 51-70- 4 FIGURE 2 SHEET 1. 2 L 7 2 4F RT A6WE 2001062900082 20010629 00082 WP 2001 6 29 ZW0A0102802 1 20010601 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT THE CABIN FLOOR SUPPORT WAS CORRODED AT STA 200, RBL 46 TO RBL 56. REMOVED FLOOR SUPPORT AND FABRI CATED NEW FLOOR SUPPORT AT STA 200, RBL 46 TO 56, PER SPM 6-70-01 AND DRAWING 9936534. INSTALLED NEW FLOOR SUPPORT PER SPM 6-70-01 PAGE 3 AND DRAWING 9936534 AND SRM 51-30-02. TREATED PER 51-10-3. SEALED PER SRM 51-20-0. 2 L 7 2 4F RT A6WE 2001062900083 20010629 00083 WP 2001 6 29 ZW0A0102803 1 20010603 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND CORROSION AT STA 250, LBL 18, ON FLOOR STIFFENER. REPLACED FLOOR SUPPORT PER SRM 51-30-2 AND 51-30-1. 2 L 7 2 4F RT A6WE 2001062900084 20010629 00084 WP 2001 6 29 ZW0A0102804 1 20010603 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND CORROSION ON FORMER AT STA 1309, BETWEEN STRINGER 28R AND 29R. REMOVED CORROSION PER SPM 6-8 0-01. TREATED CORROSION AREAS PER SRM 51-10-3. REPAIRED FORMER PER SRM 53-03, FIG 2A REPAIR 7005. 2 L 7 2 4F RT A6WE 2001062900085 20010629 00085 WP 2001 6 29 ZW0A0102805 1 20010603 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND CORROSION ON RT TIE DOWN TRACK AT STA 1212 TO 1322. INSTALLED NEW TIE DOWN TRACK PER SRM 51- 60-0, SRM 51-10-4, AND SRM 51-30-1. 2 L 7 2 4F RT A6WE 2001062900086 20010629 00086 WP 2001 6 29 2001F00064 2 20010605 A 7200 ENGINE LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP RIGHT FLAMED OUT A EXOA O OTHER X ENGINE FLAMEOUT DE DESCENT 1 SO 17 37HJ 230 P89286 RIGHT ENGINE FLAMED OUT DURING DESCENT, RESTART UNSUCCESSFUL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED FU EL FILTERS, SUMPS, ENGINE FUEL PRESSURES. PERFORMED ENGINE GROUND PERFORMANCE RUN ALL WITH NO DEFECTS NOTED. AIRCRAFT RELEASED FOR TEST FLIGHT. NO DEFECTS. COULD NOT DUPLICATE. A/C RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F A10CE E6WE 2001062900087 20010629 00087 WP 2001 6 29 GTIA010358 1 20010511 A 3260 CONNECTOR DOUG DC9 DC982 3022082 WP NLG DIRTY A GTIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 23 800NK 49144 MYR - FLT 1572 - NOSE GEAR WARNING LIGHT ILLUMINATED AT END OF RUNWAY. REMOVED AND CLEANED PROX SWITCH CANNON PLUG. RE INSTALLED CANNON PLUG GEAR WARNING. OPS CHECK GOOD PER MM 32-20-00. (M) 2 L 7 2 4F A6WE 2001062900088 20010629 00088 2001 6 29 GTIA010360 4 20010515 A 2211 CONNECTOR DOUG DC9 DC982 3022082 WP AUTOPILOT SYS DIRTY A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 602CA 49415 FLL - FLT 1457 - AUTO THROTTLE DISENGAGES IN FLIGHT. CLEANED 'RACK' CONNECTORS OF BOTH NR 1 AND NR 2 DFGC'S. PERFORMED OPERATIONAL TEST OF AT/SC AS PE PARA Z M/M 22-31-00, OPS CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 2001062900089 20010629 00089 NM 2001 6 29 P2EA001082 1 20010405 A 3211 BEAM BOEING 737 737244 138448U NM RT MLG GOUGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 OKC - DURING C-CHECK, FOUND THE RIGHT MLG SUPPORT BEAM GOUGED 10 INCHES INBOARD FROM THE LOWER OUTBOARD END, AFTER BLEND ING IT WAS FOUND TO BE OUT OF LIMITS. REPAIRED THE RT MLG SUPPORT BEAM GOUGED 10 INCHES INBOARD FROM THE LOWER OUTBOARD END PER BOEING TELEX NR AOC-OKC-01-00082H DATED 4-16-01. 2 L 7 2 4F A16WE 2001062900090 20010629 00090 NM 2001 6 29 P2EA001084 1 20010330 A 5730 SKIN BOEING 737 737244 138448U NM RT WING CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 OKC - DURING C-CHECK, FOUND THE RIGHT WING LEADING EDGE AT NR 6 LEADING EDGE SLAT ANTI-ICE TUB CUTOUT WITH CRACK, .25 IN CH. REPAIRED THE RIGHT WING LEADING EDGE AT NR 6 LEADING EDGE SLAT ANTI-ICE TUBE CUTOUT IAW BOEING SRM 57-30-4 FIG 1. (M) 2 L 7 2 4F A16WE 2001062900091 20010629 00091 NM 2001 6 29 P2EA001085 1 20010405 A 5330 SKIN BOEING 737 737244 138448U NM FUSELAGE CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 OKC - DURING C-CHECK, FOUND THE INTERNAL FUSELAGE SKIN WITH CORROSION OUT OF LIMITS AT STATION 322 BETWEEN STRINGERS 28R AND 29R, LEVEL 2. REPAIRED THE INTERNAL FUSELAGE SKIN WITH CORROSION OUT OF LIMITS AT STATION 322 BETWEEN STRINGERS 28 R AND 29R IAW BOEING SRM 53-30-3 FIG 46. (M) 2 L 7 2 4F A16WE 2001062900092 20010629 00092 NM 2001 6 29 P2EA001088 1 20010426 A 5320 ANGLE BOEING 737 737244 138448U NM FUSELAGE CORRODED A P2EA O OTHER K FLUID LOSS IN INSP/MAINT 1 CE 05 620PC 19708 OKC - DURING C-CHECK, FOUND CORROSION ON EXTRUDED ANGLES IN RIGHT SIDE OF TORQUE BOX AT BS 1088 TO BS 1156. FOUND TO BE OUT OF LIMITS, LEVEL 2. REPAIRED EXTRUDED ANGLES IN RIGHT SIDE OF TORQUE BOX AT BS 1088 TO BS 1156 IAW BOEING SRM 51-3 0-5, 51-20-1. (M) 2 L 7 2 4F A16WE 2001062900093 20010629 00093 NM 2001 6 29 P2EA01050 1 20010507 A 2781 PROXIMITY SWITCH BOEING 737 737230 NM L/E SLAT OUT OF ADJ A P2EA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 05 124NJ 124NJ FLT 350 - MCI-MDW EN ROUTE CALL, 'INTRANSIT' LEADING EDGE SLAT. WOULD HAVE TO MAKE FLAPS 15 LANDING AND WOULD BE UNABLE TO LAND IN MDW. DECISION MADE TO RETURN TO MCI. DID NOT DECLARE EMERGENCY IN MCI. OVERNIGHT MAINTENANCE AT MCI ADJUS TED NR 1 SLAT PROXIMITY SWITCH, OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A16WE 2001062900094 20010629 00094 NM 2001 6 29 P2EA01051 1 20010502 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE CANNING A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 126NJ 22884 SJO - DURING C-CHECK, FOUND LOWER FUSELAGE STATION 873 BETWEEN STRINGER 24 AND 25 RIGHT SKIN WITH OIL CAN. REPAIRED FUS ELAGE SKIN SECTION FROM BS 866.5 TO BS 886.5 BETWEEN STRINGER 23 AND 26 RIGHT. 2 L 7 2 4F A16WE 2001062900095 20010629 00095 NM 2001 6 29 P2EA01052 1 20010504 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE WORN A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 126NJ 22884 SJO - DURING C-CHECK, LOWER FUSELAGE, FORWARD CARGO COMPARTMENT CUTOUT BS 492 BETWEEN STRINGER 22 AND 23 RIGHT, SKIN WIT H WEAR. REPAIRED FUSELAGE SKIN SECTION FROM BS 491 TO BS 500 BETWEEN STRINGER 21 AND 24RT DUE TO WEAR IAW SRM 53-30-3 F IG 46. (M) 2 L 7 2 4F A16WE 2001062900096 20010629 00096 NM 2001 6 29 P2EA01053 1 20010328 A 5753 657190224 FLAP BOEING 737 737244 138448U NM RT WING DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 OKC - DURING C-CHECK, RIGHT WING INBOARD MID-FLAP OUTBOARD EDGE DELAMINATED 6.5 INCHES, WIDTH 1 INCH. REPAIRED IAW SRM 51-40-20. (M) 2 L 7 2 4F A16WE 2001062900097 20010629 00097 NM 2001 6 29 P2EA01055 1 20010512 A 2750 FLAP BOEING 737 737230 NM WINGS MALFUNCTIONED A P2EA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 CE 05 122NJ 22120 MCI - FLT 356, 354, 2259 - WHILE ON APPROACH INTO MCI FROM BUF, FLAPS WOULD NOT EXTEND BEYOND 25 DEGREES. MAINTENANCE P ERFORMED OPERATIONAL CHECK PER BOEING MM 27-51-01. SYSTEM CHECKED NORMAL ON GROUND. SUBSEQUENTLY, ON APPROACH TO MDW FR OM MCI, FLAPS WOULD NOT EXTEND BEYOND 15 DEGREES. MAINTENANCE PERFORMED A VISUAL INSPECTION OF TRAILING EDGE FLAPS AND LEADING EDGE FLAPS SYSTEM WITH NO DEFECTS NOTED. PERFORMED A LUBE 1 ON TRAILING EDGE FLAPS AND PERFORMED OPERATIONAL CH ECK PER BOEING MM 27-51-01. OPS CHECK OK ON GROUND. WHILE ON APPROACH TO MCI FROM DFW FLAPS WOULD NOT EXTEND BEYOND 12 TO 13 DEGREES. (M) 2 L 7 2 4F RT A16WE 2001062900098 20010629 00098 NM 2001 6 29 P2EA01056 1 20010502 A 5330 DOUBLER BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 126NJ 22884 SJO - DURING C-CHECK, FOUND LOWER FUSELAGE STRINGER 24 AND 25 LEFT, PORTABLE WATER SERVICE ACCESS DOOR CUTOUT, INTERNAL DOUBLER WITH CRACK. DOUBLER REPLACED FROM STRINGER 24 TO 25 LT IAW SRM 51-10-1, PAGE 8. (M) 2 L 7 2 4F A16WE 2001062900099 20010629 00099 NM 2001 6 29 P2EA01057 1 20010514 A 5755 SKIN BOEING 737 7372Q8 138448K NM SPOILER DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 121NJ 21735 SJO - DURING C-CHECK RIGHT WING NR 8 GROUND SPOILER, P/N 65-79950-7, S/N BN-013 WITH LOWER SKIN DISBONDED. (M) 2 L 7 2 4F RT A16WE 2001062900100 20010629 00100 NM 2001 6 29 P2EA01058 1 20010514 A 5753 SKIN BOEING 737 7372Q8 138448K NM FLAP DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 121NJ 21735 SJO - DURNG C-CHECK, LEFT WING INBOARD AFT FLAP, P/N 65-46434-139, S/N BN-299, UPPER SURFACE WITH DENT AT WBL 92.5. (M) 2 L 7 2 4F RT A16WE 2001062900101 20010629 00101 NM 2001 6 29 P2EA01059 1 20010514 A 5754 SKIN BOEING 737 7372Q8 138448K NM L/E SLAT DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 121NJ 21735 SJO - DURING C-CHECK, FOUND LEFT WING INBOARD FORE FLAP, P/N 65-46430-86, S/N BN-295, LOWER SURFACE WITH DENTS AND WORN AT WBL 71.24. (M) 2 L 7 2 4F RT A16WE 2001062900102 20010629 00102 NM 2001 6 29 P2EA01060 1 20010514 A 5753 SKIN BOEING 737 7372Q8 138448K NM T/E FLAP DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 121NJ 21735 SJO - DURING C-CHECK, FOUND RIGHT WING INBOARD AFT FLAP, P/N 65-46434-140, S/N BN-299, UPPER SKIN WITH DENT WBL 87.75. (M) 2 L 7 2 4F RT A16WE 2001062900103 20010629 00103 NM 2001 6 29 P2EA01061 1 20010514 A 5754 SLAT BOEING 737 7372Q8 138448K NM RT WING DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 121NJ 21735 SJO - DURING C-CHECK, FOUND RIGHT WING, SLAT NR 5, P/N 65-46422-282, S/N BN-64, OUTBOARD CORNER WITH DELAMINATION. (M) 2 L 7 2 4F RT A16WE 2001062900104 20010629 00104 NM 2001 6 29 P2EA01063 1 20010514 A 5280 BUSHING BOEING 737 737247 138448D NM RT MLG DOOR LOOSE A P2EA O OTHER E VIBRATION/BUFFET CR CRUISE 1 CE 05 912MP 19607 MCI - FLT 350 - DURING FLIGHT AT 300 KNOTS, AIRCRAFT HAD LOW FREQUENCY AIRFRAME VIBRATION. PERFORMED DETAILED INSPECTIO N OF FLIGHT CONTROLS IAW BOEING MM 27-11-00, 27-51-0 AND 27-61-0, NO DEFECTS FOUND. INSPECTED AIRCRAFT A/C BAY DOORS IA W BOEING MM 52-49-0, NO DEFECTS FOUND. INSPECTED THE MAIN LANDING GEAR DOORS AND FOUND THE RIGHT OUTER DOOR WITH LOOSE BUSHINGS AND HARDWARE. REMOVED DOOR AND PLACED ON CDL ITEM NR C912410. (M) 2 L 7 2 4F A16WE 2001062900105 20010629 00105 NM 2001 6 29 P2EA01064 1 20010413 A 5311 FRAME BOEING 737 737244 138448U NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 OKC - DURING C-CHECK, FLOOR UPPER CHORD AFT FLANGE AT BS 328 BL 0 CRACKED .400 INCHES. REPAIRED FLOORBEAM PER SRM 53-10 -9. (M) 2 L 7 2 4F A16WE 2001062900106 20010629 00106 NM 2001 6 29 P2EA01065 1 20010417 A 5311 FRAME BOEING 737 737244 138448U NM FUSELAGE DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 OKC - DURING C-CHECK, FRAME AT BS 827 DENTED BETWEEN 24L AND 25L, LENGTH 2 INCHES, WIDTH 1 INCH, DEPTH .080 INCH. REPAI RED IAW SRM 53-10-4. (M) 2 L 7 2 4F A16WE 2001062900107 20010629 00107 NM 2001 6 29 P2EA01066 1 20010507 A 5754 SLAT BOEING 737 7372B7 1384560 NM RT WING DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 126NJ 22884 SJO - DURING C-CHECK, RIGHT WING NR 4 SLAT, P/N 65-46423-270A, S/N BN-320 WITH DELAMINATION. REPAIRED NR 4 SLAT, P/N 65 -46423-270A, S/N BN-320 FROM STR 35 TO 42 AT LOWER SURFAE IAW SRM 51-40-20, REPAIR NR 21, FIG 30. (M) 2 L 7 2 4F A16WE 2001062900108 20010629 00108 NM 2001 6 29 P2EA01067 1 20010428 A 5320 STRAP BOEING 737 737244 138448U NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 OKC - DURING C-CHECK, INNER TEAR STRAP AT BS 1136 TO BS 1156 WL 240 ON RIGHT SIDE OF APU TORQUE BOX CRACKED 5 INCHES. F ABRICATED TEAR STRAP AND REPLACED IAW SRM 51-20-1. (M) 2 L 7 2 4F A16WE 2001062900109 20010629 00109 NM 2001 6 29 P2EA01069 1 20010507 A 5753 SKIN BOEING 737 7372B7 1384560 NM T/E FLAP DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 126NJ 22884 DURING C-CHECK, FOUND LEFT WING OUTBOARD AFT FLAP, P/N 65-46435-235, S/N BN-365 WITH SEVERAL DELAMINATIONS AT THE T/E. REPAIRED UPPER SKIN BETWEEN STATION WBL 373.025 AND WBL 340.525 STATION WBL 232.025 AND WBL 266.025 OF LEFT WING OUTBOAR D AFT FLAP P/N 65-46435-235, S/N BN-365 DUE TO DELAMINATION. (M) 2 L 7 2 4F A16WE 2001062900110 20010629 00110 NM 2001 6 29 P2EA01070 1 20010521 A 5754 SKIN BOEING 737 7372B7 1384560 NM L/E SLAT DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 126NJ 22884 DURING C-CHECK, FOUND LEFT WING NR 2 SLAT, P/N 65-46422-281, S/N BN-60 WITH SKIN DISBONDED AT THE T/E SECTION. REPAIRED NR 2 SLAT, P/N 65-46422-281, S/N BN-60 AT INNER SKIN BETWEEN SLAT STATION 254.27 AND 237.27 DUE TO DELAMINATION. SLAT INBOARD SECTION BETWEEN SLAT STATION 124/128 REPAIRED IAW SRM 51-40-20, REPAIR NR 21 FIG 30. (M) 2 L 7 2 4F A16WE 2001062900111 20010629 00111 NM 2001 6 29 P2EA01071 1 20010502 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 126NJ 22884 SJO - DURING C-CHECK, FUSELAGE STATION 307 BETWEEN STRINGER 10 AND 11 LEFT SKIN WITH CRACKS. MODIFIED FUSELAGE FORWARD ENTRY DOOR WAY SKIN CUT OUT FROM BS 303 TO BS 311 BETWEEN STRINGER 10 AND 13 LEFT IAW S/B 737-53-1074 REV 3 DATED 09-15- 94, SECT 3 FIG 2 DUE TO CRACK. REPAIRED FUSELAGE FORWARD ENTRY DOOR WAY SKIN CUT OUT LOWER HINGE FROM BS 299 TO BS 305 BETWEEN STRINGER 12 AND 14 LEFT DUE TO CRACK AND ELONGATED HOLES. (M) 2 L 7 2 4F A16WE 2001062900112 20010629 00112 NM 2001 6 29 P2EA01072 1 20010514 A 5754 SKIN BOEING 737 7372Q8 138448K NM L/E SLAT DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 121NJ 21735 SJO - DURING C-CHECK, LEFT WING INBOARD FORE FLAP P/N 65-46430-89, S/N BN-295, LOWER SURFACE WITH DENTS AND WORN AT WBL 71.24. REPAIRED UPPER SKIN OF FORE FLAP P/N 65-46430-89, S/N BN-295 IAW SRM 51-40-20, REPAIR NR 22 FIG 31. DENTS AT WB L 101.24 AND 115.00 LOWER SURFACE FOUND WITHIN LIMITS IAW SRM 57-50-1 FIG 16, DETAIL XIV, DENTS FILLED IAW SRM 51-40-1. (M) 2 L 7 2 4F RT A16WE 2001062900113 20010629 00113 NM 2001 6 29 P2EA01073 1 20010514 A 5754 SKIN BOEING 737 7372Q8 138448K NM L/E SLAT DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 121NJ 21735 SJO - DURING C-CHECK, RIGHT WING SLAT NR 5, P/N 65-46422-282, S/N BN-64, OUTBOARD CORNER WITH DELAMINATION. REPAIRED SL AT NR 5 PN 65-46422-282, S/N BN-64 AT LOWER SKIN BETWEEN SLAT STATION 244.53 AND 254 IAW SRM 51-40-20, REPAIR 15, FIG 24 . (M) 2 L 7 2 4F RT A16WE 2001062900114 20010629 00114 NM 2001 6 29 P2EA01074 1 20010514 A 5753 SKIN BOEING 737 7372Q8 138448K NM T/E FLAP DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 121NJ 21735 SJO - DURING C-CHECK, FOUND LEFT WING INBOARD AFT FLAP P/N 65-46434-139, S/N BN-299, UPPER SURFACE WITH DENT AT WBL 92.5 . REPAIRED INBOARD AFT FLAP P/N 65-46434-139, S/N BN-299 AT UPPER SKIN BETWEEN WBL 80 AND 87 IAW SRM 51-40-20 REPAIR 9 FIG 18. (M) 2 L 7 2 4F RT A16WE 2001062900115 20010629 00115 NM 2001 6 29 P2EA01075 1 20010514 A 5753 SKIN BOEING 737 7372Q8 138448K NM T/E FLAP DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 121NJ 21735 SJO - DURING C-CHECK, FOUND RIGHT WING INBOARD AFT FLAP, P/N 65-46434-140, S/N BN-299, UPPER SKIN WITH DENT WBL 87.75. REPAIRED RT INBOARD AFT FLAP, P/N 65-46434-140, S/N BN-299 AT UPPER SKIN BETWEEN WBL 86 AND 95 IAW SRM 51-40-20 REPAIR 9 , FIG 18. (M) 2 L 7 2 4F RT A16WE 2001062900116 20010629 00116 EA 2001 6 29 COMA0160407 1 20010620 A 5320 601R3171 INTERCOSTAL CNDAIR CL600 CL6002B19 EA CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 915CA 18536 7013 THE INTERCOSTAL FLANGE AT RBL 36 AND ANGLES AT BL27 LH AND RH ARE CRACKED FS 484.INSTALLED NEW SERVICEABLE LH AND RH 484 ANGLES I/A/W WVAC E.O. 601R-53-2516 2 L 7 2 4F RT A21EA 2001062900117 20010629 00117 NM 2001 6 29 P2EA01076 1 20010516 A 5312 BULKHEAD BOEING 737 7372Q8 138448K NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 121NJ 21735 SJO - DURING C-CHECK, FOUND FUSELAGE FORWARD PRESSURE BULKHEAD BS 178, WEB WITH CRACK INDICATIONS AT WL 195 LBL 12 INCHE S, RBL 15 INCHES, AND WL 218 LBL 12 INCHES. REPAIRED FUSELAGE AT BS 178, FORWARD PRESSURE BULKHEAD WEB FROM RBL 1.3 TO RBL 18 BETWEEN WL 210 AND 233 DUE TO CRACK, IAW COOPESA EO NR COO-3-53-222-01. PERFORMED HFEC INSPECTION ON FORWARD PRE SSURE BULKHEAD WEB AT WL 195, LBL 12 AND RBL 15 IAW B737 NDT MANUAL D6-37239, PART 6, SUB 51-00-00 FIG 23 AND NO CRACKS WERE FOUND. (M) 2 L 7 2 4F RT A16WE 2001062900118 20010629 00118 NM 2001 6 29 P2EA01077 1 20010528 A 5347 CARGO TRACK BOEING 737 7372Q8 138448K NM FUSELAGE BROKEN A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 121NJ 21735 SJO - DURING C-CHECK, FOUND LOWER FUSELAGE, AFT CARGO COMPT BETWEEN BS 790 AND 794 AND BL 19, TRACK BROKEN. TRACK REPAI RED FROM BS 780 TO 808, LBL 19 IAW SRM 53-10-5 FIG 11. (M) 2 L 7 2 4F RT A16WE 2001062900119 20010629 00119 NM 2001 6 29 P2EA01079 1 20010514 A 5755 SKIN BOEING 737 7372Q8 138448K NM SPOILER DEBONDED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 121NJ 21735 SJO - DURING C-CHECK, FOUND RIGHT WING NR 8 GROUND SPOILER, P/N 65-79950-7, S/N BN-03 WITH LOWER SKIN DISBONDED. BONDED LOWER SKIN AROUND ACTUATOR FITTING IAW SRM 51-40-20 FIG 10 REPAIR 1. BONDED LOWER SKIN AROUND ACTUATOR FITTING IAW SRM 51-40-20 FIG 10 REPAIR 1. (M) 2 L 7 2 4F RT A16WE 2001062900120 20010629 00120 NM 2001 6 29 P2EA01080 1 20010329 A 5511 RIB BOEING 737 737244 138448U NM HORIZ STAB CHAFED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 OKC - DURING C-CHECK, FOUND RIGHT HORIZONTAL STABILIZER BALANCE BAY RIB WEBS CHAFED AT ES 66.54, ES 94.07 ES 121.59 AND ES 149.12. REPAIRED IAW DRAWING 55-01204-1 AND DETERMINED TO BE MAJOR ON 8110-3 DATED MAY 9, 2001. (M) 2 L 7 2 4F A16WE 2001062900121 20010629 00121 NM 2001 6 29 P2EA01081 1 20010529 A 5511 RIB BOEING 737 737244 138448U NM HORIZ STAB CHAFED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 OKC - DURING C-CHECK, FOUND LEFT HORIZONTAL STABILIZER BALANCE BAY RIB WEB CHAFED AT ES 66.54 ES 94.07, ES 121.59 AND 14 9.12. REPAIRED IAW DRAWING 55-01204-1 AND DETERMINED TO BE MAJOR ON 8110-3 DATED MAY 9, 2001. (M) 2 L 7 2 4F A16WE 2001062900122 20010629 00122 NM 2001 6 29 P2EA01087 1 20010601 A 2612 67185 CONTROL PANEL BOEING 737 7372Q8 138448K NM COCKPIT DEFECTIVE A P2EA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 05 121NJ 21735 SJO - DURING FERRY FLIGHT OUT OF C-CHECK, MASTER FIRE WARNING LIGHT CAME ON AND FIRE WARNING BELL SOUNDED AFTER APPROX 2 5 MINUTES OF FLIGHT. WARNING LIGHT WOULD NOT EXTINGUISH AND BELL WOULD NOT SILENCE. NO OTHER SYSTEM FIRE WARNING LIGHT S WERE ON. AIRCRAFT RETURNED TO BASE, NO EMERGENCY DECLARED. DETERMINED THE CARGO SMOKE DETECTOR CONTROL PANEL TO BE A T FAULT AND REPLACED SAME. PERFORMED SMOKE DETECTOR SYSTEM TEST IAW MM 26-20-00/26-20-13 AND NO FAULT INDICATED. (M) 2 L 7 2 4F RT A16WE 2001071200101 20010712 00101 WP 2001 7 12 ARWA0010607 1 20010625 A 5320 37532351 SPLICE DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 DURING MX CHECK NON-ROUTINE 93, AFT LOWER CARGO COMPARTMENT STA 980 LONGERON 22R, SPLICE WITH 4 INCH CRACKED. REMOVED S PLICE, FABRICATED NEW SPLICE IAW DOUGLAS DRAWING 3753235, PRIMED AND INSTALLED SPLICE IAW SRM 51-3-0 & SRM 51-1-20D. 2 L 7 4 4F 4A25 2001070100001 20010701 00001 NM 2001 7 1 C1HA200192005 1 20010625 A 7100 652245031 MANIFOLD BOEING 727 727212 138407G NM RUPTURED A C1HA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 15 292AS 21458 Take off aborted, #2 eng.EGT reached red line EPR would not come up to pwr. #2 power lever 3-4 knobs ahead of 1 & 3.ACTI ON TAKEN:Inspected #2 eng and found 6th stage bleed manifold had failed and duct ruptured. R&R'd 6th stage bleed manifol d assy. Accomplished adj. test. check good . 2 L 7 3 4F A3WE 2001070100002 20010701 00002 NM 2001 7 1 C1HA200181CA 1 20010625 A 3350 LAMP BOEING 727 7272S7 138407Z NM BURNED OUT A C1HA O OTHER L NO TEST IN INSP/MAINT 1 GL 15 681CA 22020 Overwing exit lights are burned out.ACTION TAKEN 2 L 7 3 4F A3WE 2001070100003 20010701 00003 NM 2001 7 1 C1HA200182009 1 20010621 A 7100 JT8D17 ENGINE BOEING 727 7272S7 138407Z NM PWA JT8 JT8D17 52049 NE FAILED A C1HA C E D ABORTED TAKEOFF ENGINE SHUTDOWN RETURN TO BLOCK J R WARNING INDICATION PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 15 682CA 22019 688130 #3 Engine Failed on takeoff.ACTION TAKEN:Inspected and found #3 engine turbine failure. R&R'd #3 engine. 2 L 7 3 4F 4 F A3WE E2EA 2001070100004 20010701 00004 NM 2001 7 1 C1HA200185008 1 20010627 A 2611 430MI HORN BOEING 727 7272S7 138407Z NM ONLY FAILED A C1HA O OTHER L NO TEST IN INSP/MAINT 1 GL 15 685CA 22492 APU fire protection external warning horn inop.ACTION TAKEN:R&R'd ground crew call horn Checks good. 2 L 7 3 4F A3WE 2001070100005 20010701 00005 NM 2001 7 1 C1HA200196007 1 20010627 A 2611 105080037510 FIRE LOOP BOEING 727 7272J4 1384006 NM APU FAILED A C1HA O OTHER L NO TEST IN INSP/MAINT 1 GL 15 696CA APU fire warning inop.ACTION TAKEN:R&R'd APU fire loop chs good. 2 L 7 3 4F RT A3WE 2001070200001 20010702 00001 NM 2001 7 2 SWAA011859 1 20010627 A 5330 6545773 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 480, STR 4L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001070200002 20010702 00002 NM 2001 7 2 SWAA011860 1 20010628 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 329SW 23693 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001070200003 20010702 00003 NM 2001 7 2 SWAA011863 1 20010525 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED D CHECK AT DALFORT, FOUND STRINGER CRACKED AT BS 907, STR 4L. REPAIRED STR PER SRM. 2 L 7 2 4F RT A16WE 2001070200004 20010702 00004 NM 2001 7 2 SWAA011864 1 20010517 A 5311 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED D CHECK AT DALFORT, FOUND SHEAR TIE CRACKED AT BS 360, STR 14R. R&R SHEAR TIE PER SRM . 2 L 7 2 4F RT A16WE 2001070200005 20010702 00005 NM 2001 7 2 SWAA011865 1 20010518 A 5310 6547978 WEB BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED D CHECK AT DALFORT, FOUND CREASE BEAM WEB CRACKED 4 EA PLACES, BETWEEN BS 428 & BS 520. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001070200006 20010702 00006 NM 2001 7 2 SWAA011825 1 20010624 A 3350 07912 COVER BOEING 737 7375H4 138449D NM CABIN FLOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 507SW 24184 EEPLS COVER LOOSE AT ROW 21. SECURED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2001070200007 20010702 00007 NM 2001 7 2 SWAA011830 1 20010625 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED D CHECK, FOUND CRACKED FUSELAGE FRAME AT BS 380, BETWEEN STR 8R & STR 9R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001070200008 20010702 00008 NM 2001 7 2 SWAA011832 1 20010625 A 2731 BACB28AK04 BUSHING BOEING 737 7377H4 NM RH ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 709SW 27843 DURING SCHEDULED A2 CHECK, SWA SI 11052-55,FOUND RH ELEVATOR TRIM TAB ATTACH BUSHINGS WORN AT # 2 & #3 HINGES. R&R TRIM TAB BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2001070200009 20010702 00009 NM 2001 7 2 SWAA011834 1 20010624 A 3210 65C313326 BEARING BOEING 737 7372H4 138448C NM LH MLG WORN A SWAA B EMER. DESCENT J WARNING INDICATION DE DESCENT 1 SW 07 105SW 23249 DECLARED EMERGENCY……………….DURING GEAR EXTENSION FOR LANDING, THE LEFT MAIN RED LIGHT REMAINED ON & NO GREEN LIGHT. NOSE & RIGHT MAIN WERE GREEN. AFTER MANUAL GEAR EXTENSION RED LIGHT REMAINED ON.. INSTALLED LEFT MAIN GEAR DOWNLOCK PIN FOR ONE TIME FERRY FLIGHT TO HOU. R&R LH MLG FWD TRUNION BEARING PER MM. 2 L 7 2 4F A16WE 2001070200010 20010702 00010 NM 2001 7 2 SWAA011846 1 20010626 A 3350 100885 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN ERRATIC A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 378SW 26585 DURING SCHEDULED RON CHECK, FOUND EEPLS ILLUMINATING ERRATICALLY AT AFT CABIN. R&R EEPLS BAT TERY PACK PER MM. 2 L 7 2 4F RT A16WE 2001070200011 20010702 00011 NM 2001 7 2 SWAA011849 1 20010627 A 5754 65C26601 SLAT BOEING 737 7373L9 1384470 NM LH WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING SCHEDULED C3 CHECK, FOUND # 1 & # 3 L/E SLATS TRAILING EDGE SKINS CRACKED ON AFT ROW OF RIVETS. REPAIRED SLATS PER SWA RA. 2 L 7 2 4F RT A16WE 2001070200012 20010702 00012 NM 2001 7 2 SWAA011850 1 20010627 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001070200013 20010702 00013 NM 2001 7 2 SWAA011851 1 20010626 A 5330 6523693 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 420, STR 4L. REPAIRED S KIN PER SRM. 2 L 7 2 4F RT A16WE 2001070200014 20010702 00014 NM 2001 7 2 SWAA011852 1 20010626 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 20R. REPAIRED SKIN PER S RM. 2 L 7 2 4F RT A16WE 2001070200015 20010702 00015 NM 2001 7 2 SWAA011853 1 20010626 A 5330 6545773 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, STR 10R. REPAIRED SKIN PER S RM. 2 L 7 2 4F RT A16WE 2001070200016 20010702 00016 NM 2001 7 2 COOSDR010036 1 20010621 A 5313 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 29SW 21340 PAX CABIN, STA 618, STRINGER 17R, HORIZONTAL FLANGE CRACKED. 2 L 7 2 4F A16WE 2001070200017 20010702 00017 NM 2001 7 2 SWAA011835 1 20010625 A 5313 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 500D, STR'S 19R & 19L R&R S TR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001070200018 20010702 00018 NM 2001 7 2 SWAA011840 1 20010626 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 602SW 27953 EMERGENCY EXIT LIGHT NEAR FWD ENTRY DOOR MISSING LENS. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2001070200019 20010702 00019 NM 2001 7 2 SWAA011842 1 20010624 A 5310 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD CRACKED AT BS 178, RBL 0.5 & WL 207. REPAIRED B ULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 2001070200020 20010702 00020 NM 2001 7 2 VNAA0106017 1 20010623 A 2100 4068B000002 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 424JS 15151 2532 3033 ON CLIMB OUT OF PIT THE RIGHT LOW PRESSURE BLEED VALVE FAILED. AIRCRAFT RETURNED TO PIT AND MAINTENANCE REPLACED THE VAL VE AND OPERATIONAL CHECK GOOD 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001070200021 20010702 00021 NM 2001 7 2 VNAA0106016 1 20010622 A 2420 20040 ALTERNATOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 429JS 10711 9 3043 ON CLIMB OUT THRU FL100 THE CREW GOT AN ALTERNATOR FAIL. THE CREW WAS INSTRUCTED TO RETURN TO PIT. MAINTENANCE REPLACED THE RIGHT ALTERNATOR AND OPERATIONAL CHECKED GOOD. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001071300031 20010713 00031 NM 2001 7 13 01FDEA00509 1 20010614 A 5310 SHEAR TIE BOEING 727 727277 138408S NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 CORROSION (C53-113-01, 2) ON SHEAR TIE AT BS 1010, RBL 2, WL 138.5. *S/D* REMOVED AND REPLACED SHEAR TIE PER FEDEX SRM 53-10-4. 2 L 7 3 4F RT A3WE 2001070200022 20010702 00022 EA 2001 7 2 SWIA972603 1 20010530 A 3150 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT ACTIVATED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 410SW 7066 ON TAKEOFF ROLL ABOVE APPROXIMATELY 90 PERCENT N1, HAD A RED WARNING MESSAGE CONFIG AILERON AND CONFIG TRIM WITH AURAL WARNING. TRIM WAS IN THE GREEN. ABORTED TAKEOFF. PERFORMED OPS CHECK IAW AMM 31-41-00. RAN ENGINES ABOVE 70 PERCENT N1 AND HAD (T/O CONFIGURATION OK). COULD NOT DUPLICATE. OPS CHECK OF SYSTEM OK. 2 L 7 2 4F RT A21EA 2001070200023 20010702 00023 WP 2001 7 2 0100037O 1 20010620 A 7722 WARNING SYSTEM DOUG DC8 DC871F 302199D WP COCKPIT ACTIVATED A IXXA C ABORTED TAKEOFF M OVER TEMP TO TAKEOFF 1 SW 11 824BX 45946 PRIOR TO ROTATION AIRCRAFT EXPERIENCED ABNORMAL EXHAUST GAS TEMPERATURE INDICATION. AIRCRAFT ABORTED TAKEOFF AND RETURN ED TO PARKING. NO FURTHER ABNORMALITIES OCCURRED. 2 L 7 4 4F RT 4A25 2001070200024 20010702 00024 WP 2001 7 2 0102099913 1 20010613 A 3610 CLAMP DOUG DC9 DC931 3022065 WP CABIN PRESSURE LOOSE A NWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 963N 47415 INBOUND TO RAP, LOST PRESSURIZATION AT 26,000 FEET. CABIN PRESSURE LIGHT AND AFT CABIN DOOR LIGHT ILLUMINATED, MASKS DE PLOYED, AND STARTED TO CLIMB 1000 FEET PER MINUTE. FOLLOWED COM PROCEDURES AND DESCENDED TO 10,000 FEET WITH NO FURTHER PROBLEMS. SECURED LOOSE CLAMPS ON RIGHT PACK SUPPLY DUCT. CHECKED AFT CABIN DOOR, NO PROBLEMS FOUND. FERRIED TO MSP TO REPLACED USED OXYGEN GENERATORS, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 2001070200033 20010702 00033 NM 2001 7 2 01FDEA00395 1 20010606 A 2611 774001 SMOKE DETECTOR BOEING 727 727233 138408A NM CARGO BAY MALFUNCTIONED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 218FE 21101 ON CLIMB WITH WING ANTI-ICE ON MAIN CARGO SMOKE DETECTION SYS DETECT SMOKE IN THE NR 6 POS. Removed and replaced NR 6 C ARGO SMOKE DETECTOR PER MM 26-16-001-4. OPS CHECK GOOD. 2 L 7 3 4F RT A3WE 2001070200034 20010702 00034 NM 2001 7 2 01FDEA00396 1 20010606 A 3230 LINK BOEING 727 72725C 138400H NM NLG VIBRATION A FDEA O OTHER E VIBRATION/BUFFET TX TAXI/GRND HDL 1 SO 25 116FE 19298 UPON LANDING WITH SPOILER and REVERSERS ABOUT 90 KTS. NOSE GEAR START VIBRATING. *S/d* Removed and replaced NLG TORSI ON LINKS PER IAW MM 32-21-051-4, LT & RT NLG WHEELS PER IAW MM 32-45-011-4. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2001070200035 20010702 00035 WP 2001 7 2 01FDEA00397 1 20010606 A 2612 FIRE WARNING DOUG DC10 DC1030F 3023504 WP COCKPIT ACTIVATED A FDEA F ACTIVATE FIRE EXT. J WARNING INDICATION TX TAXI/GRND HDL 1 SO 25 311FE 46871 ON START APU FIRE LIGHT ILLUM RED TAB, AND FIRED CYLINDER NR 1 BOTTLE. Removed and replaced ENG 2/APU NR 1 FIRE EXT CON TAINER PER DC-10 AMM 26-21-02-2. Removed and replaced APU CARTRIDGE, STARTER PER MM 49-44-01. LEAK CHECK GOOD. 2 L 7 3 4F RT A22WE 2001070200037 20010702 00037 NM 2001 7 2 AALA20011154 1 20010518 A 5100 STRINGER BOEING 727 727223 1384074 NM FS 1150 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 866AA 21371 TUL - FOUND STRINGER CORRODED AND SPLIT AT THE DRAIN MAST. INSTALLED STRINGER REPAIR AS PER SRM 53-10-3. INSTALLED NEW DRAIN MAST PAN PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 2001070200038 20010702 00038 NM 2001 7 2 AALA20011157 1 20010517 A 5300 WEB BOEING 727 727223 1384074 NM FS 1168-1174 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 866AA 21371 TUL - FOUND CORROSION 6 INCHES BY 1 INCH ON WEB AND PLATE RBL 16. INSTALLED FILLER AND DOUBLER AT STATION 1168-1174 RBL 16 PER 51-40-2. (M) 2 L 7 3 4F A3WE 2001070200039 20010702 00039 NM 2001 7 2 AALA20011150 1 20010522 A 5410 BRACKET BOEING 727 727227 1384078 NM A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 728AA 20735 TUL - FOUND THROTTLE CONTROL DRUM MOUNT BRACKET CRACKED UPPER END, NR 3 ENGINE. REPAIRED CRACK IN CONTROL DRUM MOUNT BR ACKET PER ESO 11697 DATED 5-21-01 AND SRM 54-10-3 PAGE 42A. (M) 2 L 7 3 4F A3WE 2001070200040 20010702 00040 NM 2001 7 2 AALA20011152 1 20010522 A 5330 SKIN BOEING 727 727227 1384078 NM FS 680 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 728AA 20735 TUL - FOUND FASTENER HEAD DISHED FUSE SKIN STATION 680 STRINGER 28R AND SKIN CORRODED. CUT OUT CORRODED AREA INSTALLED FILLER AND DOUBLER PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 2001070200041 20010702 00041 NM 2001 7 2 AALA20011153 1 20010518 A 5330 SKIN BOEING 727 727227 1384078 NM FS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 728AA 20735 TUL - FOUND CRACK IN FUSELAGE SKIN AT STATION 720A AND 19 BL 0. INSTALLED DOUBLER PER 53-30-03 PART 1 PAGE 5-8. (M) 2 L 7 3 4F A3WE 2001070200042 20010702 00042 NM 2001 7 2 AALA20011149 1 20010522 A 5100 STRAP BOEING 727 727227 1384078 NM FS 680 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 728AA 20735 TUL - FOUND CORROSION 4 INCHES BY 12 INCHES, ON BUTT SPLICE STRAP AT STATION 680, BETWEEN 28L AND 28R. REMOVED CORRODED STRAP AND INSTALLED NEW STRAP. (M) 2 L 7 3 4F A3WE 2001070200043 20010702 00043 NM 2001 7 2 AALA2001148 1 20010522 A 5100 WEB BOEING 727 727227 1384078 NM FS 303-312 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 728AA 20735 TUL - FOUND LEFT HORIZONTAL WALKWAY CORRODED 9 INCHES BY 3 INCHES UNDERSIDE BETWEEN STATION 303 TO 312. REMOVED CORRODE D AREA OF WALKWAY. INSTALLED DOUBLER PER SRM. (M) 2 L 7 3 4F A3WE 2001070200044 20010702 00044 NM 2001 7 2 AALA20011147 1 20010522 A 5100 SPLICE BOEING 727 727227 1384078 NM FS 680 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 728AA 20735 TUL - FOUND STRINGER SPLICE CRACKED. REMOVED AND REPLACED STRINGER SPLICE. (M) 2 L 7 3 4F A3WE 2001070200045 20010702 00045 WP 2001 7 2 AALA20011172 1 20010531 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 21 7543A 53025 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT DIM. REPLACED EMERGENCY EXIT LIGHT WIRE AT SPLICE. SYSTEM GRO UND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001070200046 20010702 00046 WP 2001 7 2 AALA20011175 1 20010601 A 3397 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70401 49312 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT CONNECTOR AT MODULE INOPERATIVE. RE-CONNECTED FORWARD EMERGENC Y EXIT LIGHT MODULE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001070200047 20010702 00047 WP 2001 7 2 AALA20011129 1 20010524 A 3350 SOCKET DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 287AA 49299 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHT AT ROW 13 INOPERATIVE. REPLACED LIGHT SOCKET ASSEM BLY AT ROW 13. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001070200048 20010702 00048 WP 2001 7 2 AALA20011126 1 20010522 A 3350 SPLICE DOUG DC9 DC982 3022082 WP CABIN DISCONNECTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 487AA 49680 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT FORWARD GALLEY AISLE WALL INOPERATIVE. REPAIRED QUICK DISCO NNECT SPLICES AT GALLEY AISLE WALL EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001070200049 20010702 00049 WP 2001 7 2 AALA20011123 1 20010519 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 591AA 53254 ORD - DURING OVERNIGHT MAINTENANCE, EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK TO EXTERIOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001070200050 20010702 00050 WP 2001 7 2 AALA20011124 1 20010519 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 591AA 53254 ORD - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK TO OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001070200051 20010702 00051 WP 2001 7 2 AALA20011120 1 20010522 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7509 49803 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY CEILING LIGHTS INOPERATIVE ROWS 28 THROUGH 29. REPLACED BATTERY PACKS FOR EMERGENCY CEILING LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001070200052 20010702 00052 EA 2001 7 2 REXA01008 1 20010611 A 2700 601R931059 BPSU CNDAIR CL600 CL6002B19 EA LT WING FLAPS FAILED A REXA A UNSCHED LANDING F FLT CONT AFFECTED TO TAKEOFF 1 SO 25 8492C 7492 FLAP FAILURE MESSAGE AND FLAPS STUCK AT 20 DEGREES. INTERROGATED FECU (FLAP ELECTRONIC CONTROL UNIT) FOUND LEFT BPSU (B RAKE POSITION SENSING UNIT) FAILURE MESSAGE. REMOVED AND REPLACED LEFT FLAP BPSU. (M) 2 L 7 2 4F RT A21EA 2001070200053 20010702 00053 EU 2001 7 2 AALA20011179 1 20010528 A 4900 QACF100 APU FOKKER F28 F28MK0100 4990807 EU APU LEAKING A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 1411G 11369 DFW - FLT 1794 - EN ROUTE MTY-DFW - SHORTLY AFTER NR 1 ENGINE START DETECTED OIL SMELL AND SMOKE IN COCKPIT AND CABIN. SHUTDOWN APU. SMOKE DISSIPATED. LANDED DFW WITHOUT FURTHER INCIDENT. REPLACED APU. SYSTEM GROUND CHECKED NORMAL OPER ATION. (M) 2 L 7 2 4F RT 2001070200054 20010702 00054 NM 2001 7 2 AALA20011188 1 20010608 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 665AA 25299 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 21D INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT CON NECTOR AT SEAT 21D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001070200055 20010702 00055 NM 2001 7 2 AALA20011189 1 20010610 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN INOPERATIVE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 352AA 24033 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 29H INOPERATIVE. RE-PINNED EMERGENCY EXIT LIGHT WIRE AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001070200056 20010702 00056 NM 2001 7 2 AALA20011190 1 20010610 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 352AA 24033 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 39H INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT CON NECTOR AT SEAT 39H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001070200057 20010702 00057 WP 2001 7 2 AALA20011140 1 20010526 A 3350 AB51 BATTERY DOUG DC9 DC982 3022082 WP R1 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 585AA 53248 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT R1 DOOR DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY AT R1 DO OR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001070200058 20010702 00058 NM 2001 7 2 AALA20011141 1 20010528 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 21 374AA 25201 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 23H INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT 23H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001070200059 20010702 00059 NM 2001 7 2 AALA20011138 1 20010527 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39367 25194 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 35B INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT CON NECTOR AT SEAT 35B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001070200060 20010702 00060 NM 2001 7 2 AALA20011132 1 20010524 A 3350 P4010049 BATTERY PACK BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 371AA 25198 MIA - DURING OVERNIGHT MAINTENANCE, RIGHT AFT OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERIES FOR RIGHT AFT OVERHEAD EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL. (M) 2 L 7 2 4F RT A1NM 2001070200061 20010702 00061 NM 2001 7 2 AALA20011131 1 20010524 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 670AA 25335 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH IGHT 18D INOPERATIVE. RESEATED CONNECTOR SEAT 18D. SYST EM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001070200062 20010702 00062 NM 2001 7 2 AALA20011130 1 20010524 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 357AA 24038 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS BEHIND SEAT 3AB INOPERATIVE. RESECURED CONNECTOR AT SEAT 3AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001070200063 20010702 00063 NM 2001 7 2 AALA20011144 1 20010530 A 3350 SOCKET BOEING 767 767323 1385205 NM CABIN DIRTY A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 397AN 29604 ORD - DURING OVERNIGHT, MAINTENANCE FORWARD OVERWING EMERGENCY EXIT LIGHT DIM. CLEANED EMERGENCY EXIT LIGHT SOCKET. SY STEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001070200064 20010702 00064 NM 2001 7 2 AALA20011186 1 20010605 A 3350 TERMINAL BOEING 767 767323 1385205 NM LT WING INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 384AA 26996 LAX - DURING OVERNIGHT MAINTENANCE, LEFT SIDE WING EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED AND SECURED EMERGENCY EXIT LIGHT WIRE TERMINAL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001070200066 20010702 00066 WP 2001 7 2 MWEA011007 1 20010629 A 2751 C27207 TRANSDUCER DOUG DC9 DC914 3022034 WP LEFT INOPERATIVE A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 600ME 45725 STALL WARNING AND STICK SHAKER ACTUATED AND WOULD NOT CEASE UNTIL CAPTAINS STALL WARNING/STICK SHAKER C.B. WAS PULLED. -- REMOVED AND REPLACED LEFT STALL WARNING TRANSDUCER. 2 L 7 2 4F A6WE 2001070200067 20010702 00067 WP 2001 7 2 01FDEA00400 1 20010606 A 5320 29298591200 STANCHION DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 313FE 48311 AFT FUS WASTE COMP, FS 1967, AT X=23, X=0, X=23 3 EA STANCHIONS THAT RUN VERTICALLY FROM FLOORBOARD LEVEL TO COMP FLOOR HAVE LEVEL 2 EXFOLIATION CORROSION AROUND NUT PLATES. 2 L 7 3 4F A22WE 2001070200068 20010702 00068 WP 2001 7 2 ABXA010239 1 20010525 A 5610 WINDOW DOUG DC8 DC863 302198A WP COCKPIT STUCK A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 FIRST OFFICER'S SLIDING WINDOW WOULD NOT OPEN. REMOVED EXCESSIVE SEALANT FROM EPICAST AREA. WINDOW OPERATED NORMALLY I AW DC-8 MM 56-10-3. 2 L 7 4 4F 4A25 2001070200069 20010702 00069 WP 2001 7 2 ABXA010278 1 20010525 A 5313 9758507 LONGERON DOUG DC8 DC863 302198A WP CARGO BAY CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 AFT CARGO AT FS 1060 - 1080 LONGERON 36 WAS CORRODED. REPAIRED AREA IAW DC-8 SRM 51, DAC DWG 9758507, AND REA 853-40346 MR. 2 L 7 4 4F 4A25 2001070200070 20010702 00070 WP 2001 7 2 ABXA010279 1 20010525 A 5313 3755822513 STRINGER DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 STATION 320 STRINGER 34 RIGHT HAD CORROSION INBOARD SIDE. REPAIRED AREA IAW DC-8 SRM 53-2-0, AND DC-8 SRM 51. 2 L 7 4 4F 4A25 2001070200071 20010702 00071 WP 2001 7 2 ABXA010280 1 20010525 A 5320 37558451 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 AFT LOWER CARGO Z-FITTING, STATION 1220, LONGERON 33 - 34 LEFT CORRODED. REPAIRED AREA IAW DC-8 SRM 53-2-0, 51-1-8, AND 51-1-20D. 2 L 7 4 4F 4A25 2001070200072 20010702 00072 WP 2001 7 2 ABXA010281 1 20010602 A 3350 60030451 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 976AX 47596 THE EMERGENCY EXIT LIGHTS WERE DIM. REPLACED EMERGENCY LIGHTS BATTERIES AND BATTERY POWER SUPPLY. OPS CHECKED GOOD IAW DC-9 MM 33-53-00. 2 L 7 2 4F A6WE 2001070200073 20010702 00073 WP 2001 7 2 ABXA010282 1 20010418 A 2750 58956951 BRACKET DOUG DC8 DC863F 302198F WP LT MLG WW CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 BRACKET FOR FLAP CABLE GUIDE WHEEL HAD CORROSION AFT OF STATION 902 FITTING LEFT MAIN LANDING GEAR WHEEL WELL. REPLACED FLAP BUS CABLE BRACKET IAW DC-8 MM 27-50-00 AND 20-17-00. 2 L 7 4 4F 4A25 2001070200074 20010702 00074 WP 2001 7 2 ABXA010283 1 20010420 A 5313 STRINGER DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 AFT LOWER CARGO STRINGER 35 RIGHT CORRODED CAUSING CRACK TO APPEAR. REPAIRED AREA IAW DC-8 SRM 53-2-0, 53-2-1, 51-1-8, 51-1-20D, 51-1-21, 51-3-0, DAC DWG 5759639, AND REA D853-40796MR. 2 L 7 4 4F 4A25 2001070200075 20010702 00075 WP 2001 7 2 ABXA010284 1 20010529 A 5320 564340217 STIFFENER DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 LEFT MAIN LANDING GEAR STATION 940 STIFFENER CRACKED ADJACENT TO CABLE PULLEY ON OUTBOARD WEB. REPAIRED AREA IAW DC-8 D AC DWG 5643402, DC-8 SRM 53-2-0, 51-1-8, 51-1-11, 51-1-21A, AND 51-1-20D. 2 L 7 4 4F 4A25 2001070200076 20010702 00076 WP 2001 7 2 ABXA010285 1 20010530 A 5313 975491349 LONGERON DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 FORWARD CARGO COMPARTMENT CORROSION ON LONGERON 34 RIGHT AT FS 280 INSIDE TORQUE BOX. REPAIRED AREA IAW DC-8 SRM 51-3-0 , 51-1-20D, 53-2-2, AND REA D853-40226MR. 2 L 7 4 4F 4A25 2001070200077 20010702 00077 WP 2001 7 2 ABXA010286 1 20010604 A 5313 975491313 LONGERON DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 FORWARD CARGO COMPARTMENT LONGERON 28 LEFT CORRODED AT FS 280 INSIDE TORQUE BOX. REPAIRED AREA IAW DC-8 SRM 51-3-0, 51- 1-21, 51-1-20D, AND REA D853-40780MR. 2 L 7 4 4F 4A25 2001070200078 20010702 00078 WP 2001 7 2 ABXA010288 1 20010408 A 5320 ATTACH ANGLE DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 RIGHT MAIN LANDING GEAR WHEEL WELL AT FS 880 KEEL BEAM TO WEB ATTACH ANGLE WAS CORRODED. REMOVED SURFACE CORROSION IAW DC-8 SRM 51-1-8. ALODINED AND PRIMED IAW DC-8 SRM 51-1-8. FOUND BLEND OUT TO BE WITHIN LIMITS IAW DC-8 SRM 53-2-0. 2 L 7 4 4F 4A25 2001070200079 20010702 00079 WP 2001 7 2 ABXA010289 1 20010409 A 5320 564644414 INTERCOSTAL DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 RIGHT MAIN LANDING GEAR WHEEL WELL AT FS 975, LONGERON 28 RIGHT INTERCOSTAL WAS CRACKED AT FORWARD END. FABRICATED INTE RCOSTAL IAW DC-8 DWG 5646444. ALODINED IAW DC-8 SRM 51-1-8. PRIMED IAW DC-8 SRM 51-1-8. INSTALLED IAW DC-8 SRM 51-1-2 0D. 2 L 7 4 4F 4A25 2001070200080 20010702 00080 WP 2001 7 2 ABXA010290 1 20010426 A 5343 5750092504 FITTING DOUG DC8 DC863F 302198F WP RT MLG WW CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 RIGHT MAIN LANDING GEAR WHEEL WELL HAD CORROSION ON INBOARD UPPER CHAMBER ON TRAP FITTING. BLENDED AND REMOVED CORROSIO N FOUND WITHIN LIMITS IAW DC-8 SRM 53-2-0, FIGURE 1, SHEET 3. ALODINED AND PRIMED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 2001070200081 20010702 00081 WP 2001 7 2 ABXA010291 1 20010430 A 5330 SKIN DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 FS 660 - 680 LONGERON 36 - 35 RIGHT AIRCRAFT SKIN WAS CORRODED UNDER ACCELEROMETER BRACKET INSIDE AND OUTSIDE AIRCRAFT. REPAIRED AREA IAW DC-8 SRM 51-1-21, 51-1-8, 53-2-0, 51-1-20D, AND 53-2-1. 2 L 7 4 4F 4A25 2001070200082 20010702 00082 WP 2001 7 2 ABXA010292 1 20010601 A 5313 5750198501 LONGERON DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 LEFT MAIN LANDING GEAR WHEEL WELL LONGERON 24 HAD CORROSION ON UPPER SURFACE BETWEEN STATION 879 - 902. CORROSION ALSO RUNS UNDER FITTING AT STATION 902. REPLACED LEFT LONGERON 24 IAW DAC DWG 5750198. 2 L 7 4 4F 4A25 2001070200084 20010702 00084 WP 2001 7 2 ABXA010294 1 20010605 A 5521 5644420504 SPAR CAP DOUG DC8 DC863 302198A WP RT ELEVATOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 RIGHT ELEVATOR UPPER SPAR CAP XE 95 WAS CORRODED BOTH SIDES OF RIB, INSIDE AREA. 2 L 7 4 4F 4A25 2001070200085 20010702 00085 WP 2001 7 2 ABXA010295 1 20010605 A 5521 5644420504 SPAR CAP DOUG DC8 DC863 302198A WP RT ELEVATOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 RIGHT ELEVATOR UPPER SPAR CAP XE 65 WAS CORRODED BOTH SIDES OF THE RIB AND OUTER WEB. 2 L 7 4 4F 4A25 2001070200087 20010702 00087 WP 2001 7 2 ABXA010297 1 20010606 A 5313 LONGERON DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 AFT FUSELAGE BETWEEN STATION 1717 TO 1700 LONGERON 20 LEFT WAS CORRODED. 2 L 7 4 4F 4A25 2001070200088 20010702 00088 WP 2001 7 2 ABXA010298 1 20010606 A 5311 FRAME DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 AFT FUSELAGE AT STATION 1734 BETWEEN LONGERON 6 LEFT TO 7 LEFT FRAME WAS CORRODED. 2 L 7 4 4F 4A25 2001070200089 20010702 00089 WP 2001 7 2 ABXA010299 1 20010606 A 5310 SHEAR TIE DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 AFT CARGO AT STATION 1120 BETWEEN LONGERON 35 LEFT AND 36 LEFT, SHEAR TIE CRACKED. 2 L 7 4 4F 4A25 2001070200090 20010702 00090 WP 2001 7 2 ABXA010300 1 20010606 A 5310 SHEAR TIE DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 AFT CARGO AT STATION 1140 BETWEEN LONGERON 34 RIGHT AND 35 RIGHT, SHEAR TIE AND FRAME CORRODED. 2 L 7 4 4F 4A25 2001070200091 20010702 00091 NM 2001 7 2 ABXA010301 1 20010606 A 5250 HANDLE BOEING 767 767281 1385109 NM COCKPIT DOOR LACK OF LUBE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 773AX 22788 THE COCKPIT DOOR WAS DIFFICULT TO OPEN FROM INSIDE THE COCKPIT. DOOR STUCK, HAD TO BE PRIED OPEN. LUBRICATED DOOR HAND LE MECHANISM. MAINTENANCE OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2001070200092 20010702 00092 WP 2001 7 2 ABXA010302 1 20010606 A 2170 SEPARATOR DOUG DC9 DC941 302207N WP A/C BAY CONTAMINATED A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 23 953AX 47608 ON TAKEOFF ROLL, AT ILN AND FLL, CREW IDENTIFIED AN UNKNOWN ODOR IN THE COCKPIT. ODOR SEEMED TO BE PNEUMATIC IN NATURE, NOT ELECTRICAL. IT STARTED HALFWAY THROUGH EACH TAKEOFF ROLL AND DISSIPATED WITHIN 15 MINUTES IN THE CLIMB. ODOR WAS OBVIOUS AND CLEARLY ABNORMAL. INSPECTED PNEUMATIC SYSTEM AT TAIL COMPARTMENT AREA. CLAMPS, CONNECTOR HOSES AND DUCT WE RE ALL FOUND NORMAL. THE LEFT WATER SEPARATOR WAS SOAKED WITH WATER. REMOVED AND CLEANED DRAIN FILTER AND REPLACED COA LESCER BAG IAW ABX DC-9 MM 21-20-02. ENGINES RUN AND CHECKED AIR CONDITIONING SYSTEM. NO DEFECTS OR ODORS WERE NOTED. SYSTEM CHECKED GOOD IAW DC-9 MM. 2 L 7 2 4F A6WE 2001070200093 20010702 00093 WP 2001 7 2 ABXA010303 1 20010608 A 5250 DOOR DOUG DC8 DC863F 302198F WP COCKPIT FAULTY A ABXA K NONE O OTHER CR CRUISE 1 GL 23 811AX 46113 COCKPIT DOOR WAS DIFFICULT TO KEEP CLOSED. UNSAFE AS IS REF, UNABLE TO KEEP CLOSED DURING EMERGENCY PROCEDURE. COCKPIT SMOKE REMOVAL, STEP 6. NOTE: DOOR CAME OPEN SEVERAL TIMES DURING FLIGHT. OPEN AND CLOSED COCKPIT DOOR SEVERAL TIMES BY USING THE COCKPIT DOOR HANDLE AND FOUND NO DEFECTS. AFTER CLOSING DOOR, MAINTENANCE ATTEMPTED SEVERAL TIMES TO MAKE DO OR COME OPEN AND COULD NOT. 2 L 7 4 4F 4A25 2001070200094 20010702 00094 NM 2001 7 2 ABXA010306 1 20010610 A 3260 PSEU BOEING 767 767281 1385109 NM COCKPIT MALFUNCTIONED A ABXA K NONE N FALSE WARNING CR CRUISE 1 GL 23 787AX 22785 EICAS MESSAGE LANDING GEAR MONITOR DISPLAYED WITH LANDING GEAR UP AND LOCKED. REPLACED PSEU PER B767 MM 32-09-03. OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2001070200095 20010702 00095 WP 2001 7 2 ABXA010308 1 20010608 A 5313 LONGERON DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 FS 1000 LONGERON 35 LEFT CORRODED ON INBOARD SIDE. 2 L 7 4 4F 4A25 2001070200096 20010702 00096 WP 2001 7 2 ABXA010309 1 20010608 A 5310 SHEAR TIE DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 AFT LOWER CARGO, FUSELAGE 1040, LONGERON 35 RIGHT - 36, SHEAR TIE CORRODED. 2 L 7 4 4F 4A25 2001070200098 20010702 00098 WP 2001 7 2 ABXA010311 1 20010608 A 5310 SHEAR TIE DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 AFT LOWER CARGO SHEAR TIE CORRODED AT STATION FS 1020 BETWEEN LONGERON 35 RIGHT - LONGERON 36. 2 L 7 4 4F 4A25 2001070200099 20010702 00099 WP 2001 7 2 ABXA010312 1 20010608 A 5311 FRAME DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 AFT LOWER CARGO FRAME CORRODED AT STATION FS 1050 LONGERON 35 LEFT. 2 L 7 4 4F 4A25 2001070200100 20010702 00100 WP 2001 7 2 ABXA010313 1 20010608 A 5311 FRAME DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 AFT LOWER CARGO FRAME CORRODED AT FUSELAGE 1500 LONGERON 36. 2 L 7 4 4F 4A25 2001070200101 20010702 00101 WP 2001 7 2 ABXA010314 1 20010608 A 5320 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 AFT LOWER CARGO BATHTUB FITTING CORRODED AT FUSELAGE 1050 LONGERON 28 LEFT. 2 L 7 4 4F 4A25 2001070200102 20010702 00102 WP 2001 7 2 ABXA010315 1 20010608 A 5320 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 FORWARD LOWER CARGO FITTING CORRODED AT FUSELAGE 70 LONGERON 36. 2 L 7 4 4F 4A25 2001070200103 20010702 00103 WP 2001 7 2 ABXA010316 1 20010608 A 5313 LONGERON DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 AFT LOWER CARGO LONGERON 36 CORRODED AT STATION FUSELAGE 1021. 2 L 7 4 4F 4A25 2001070200104 20010702 00104 WP 2001 7 2 ABXA010317 1 20010608 A 5330 SKIN DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 AFT LOWER CARGO SKIN CORRODED AROUND SEVERAL FASTENERS FROM STATION FS 980 TO STATION FS 1040 BETWEEN LONGERON 35 LEFT A ND LONGERON 35 RIGHT. 2 L 7 4 4F 4A25 2001070200105 20010702 00105 WP 2001 7 2 ABXA010318 1 20010608 A 5320 ANGLE DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 FS 980 LONGERON 35 LEFT BULKHEAD ATTACH ANGLE WAS CORRODED. 2 L 7 4 4F 4A25 2001070200106 20010702 00106 WP 2001 7 2 ABXA010319 1 20010608 A 5410 ANGLE DOUG DC8 DC863 302198A WP NR 4 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 NR 4 PYLON INTERIOR INBOARD VERTICAL ANGLE STATION YN 298 UNDER UPPER SPAR WEB CRACKED. 2 L 7 4 4F 4A25 2001071200102 20010712 00102 WP 2001 7 12 ARWA0010701 1 20010629 A 5512 PANEL LKHEED 1011 1011385115 5265015 WP HORIZ STAB CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 307GB 193U1131 DURING SCHEDULE MAINTENANCE RT HORIZONTAL STABILIZER L/E PANEL AT T/E OF PANEL 331A HAS CRACK AT I/B CORNER. INSTALLED DOUBLER REPAIR AT RT HORIZONTAL STABILIZER L/E IAW DRAWING AS 11269. 2 L 7 3 4F A23WE 2001070200108 20010702 00108 WP 2001 7 2 ARWA0010703 1 20010629 A 5311 FRAME LKHEED 1011 1011385115 5265015 WP A ARWA O OTHER O OTHER IN INSP/MAINT 1 SO 19 307GB 193U1131 DURING SCHEDULE MAINTENANCE. N/R 470. DISCREPANCY: R/H ECS COMPARTMENT STATION 449 BULKHEAD FRAME IS CRACKED ON FWD SIDE BETWEEN STRINGER 26 AND STRINGER 27. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT BULKHEAD FRAME STA 449. INSTALLED REPAIR ANGLES + DOUBLERS AS REQUIRED ALL WORK ACCOMPLISHED IAW SRM 53-11-00 FIG. 833. 2 L 7 3 4F A23WE 2001070200109 20010702 00109 WP 2001 7 2 ARWA0010704 1 20010629 A 5320 FLOOR SUPPORT LKHEED 1011 1011385115 5265015 WP FUSELAGE CRACKED A ARWA O OTHER O OTHER IN INSP/MAINT 1 SO 19 307GB 193U1131 DURING SCHEDULE MAINTENANCE. FLOOR PANEL SUPPORT BETWEEN SEAT TRACK 10&11 CRACKED AT FS 980. REPLACED CRACKED FLOOR PA NEL SUPPORT AT FS 980 BETWEEN SEAT TRACK 10 & 11 IAW SRM 51-40-4. 2 L 7 3 4F A23WE 2001070200110 20010702 00110 WP 2001 7 2 ARWA0010705 1 20010629 A 5101 SPLICE LKHEED 1011 1011385115 5265015 WP A ARWA O OTHER O OTHER IN INSP/MAINT 1 SO 19 307GB 193U1131 DURING SCHEDULE MAINTENANCE. N/R 234. DISCREPANCY: FS 1183 BELOW WL 200 CRACK ON SPLICE. CORRECTIVE ACTION: INSTALLED SP LICE AT FS 1183 RH IAW SRM 51-40-01. 2 L 7 3 4F A23WE 2001070200111 20010702 00111 WP 2001 7 2 ARWA0010706 1 20010629 A 5101 SPLICE LKHEED 1011 1011385115 5265015 WP A ARWA O OTHER O OTHER IN INSP/MAINT 1 SO 19 307GB 193U1131 DURING SCHEDULE MAINTENANCE. N/R 235. DISCREPANCY: SPLICE CRACKED AT FS 1203 BELOW WL200. CORRECTIVE ACTION: REMOVED CRA CKED SPLICE & REPLACED WITH NEW ONE IAW SRM 51-40-01. 2 L 7 3 4F A23WE 2001070200112 20010702 00112 WP 2001 7 2 ARWA0010707 1 20010629 A 5101 FITTING LKHEED 1011 1011385115 5265015 WP A ARWA O OTHER O OTHER IN INSP/MAINT 1 SO 19 307GB 193U1131 DURING SCHEDULE MAINTENANCE. N/R 493. DISCREPANCY: C2 CARGO DOOR CUT-OUT, CENTER UPPER DOOR SILL PIVOT CLEVIS ATTACH FIT TING IS CRACKED. CORRECTIVE ACTION: REMOVED FASTENERS C2 CARGO DOOR CENTER UPPER DOOR SILL PIVOT FITTING, CLEAN SURFACE CORROSION IAW SRM 51-21-07 PAGE 1, ALODINE AND PRIMED IAW SRM 51-21-01 PAGE 2. INSTALLED NEW FITTING IAW SRM 51-40-01 PA GE 1. 2 L 7 3 4F A23WE 2001070200113 20010702 00113 NM 2001 7 2 AWXA0001814 1 20010604 A 5320 143N5370 FLOOR SUPPORT BOEING 757 7572S7 1384962 NM FUSELAGE CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 23566 FWD cargo pit floorboard support at FS 610 RBL 6 has chafed area. cut out damaged section; FABBED and installed floor s upport IAW SRM 53-30-53 fig 1; treated and primed IAW SRM 51-20-01. 2 L 7 2 4F RT A2NM 2001070200114 20010702 00114 NM 2001 7 2 AWXA0001815 1 20010604 A 5230 143N66211 DOOR FRAME BOEING 757 7572S7 1384962 NM CARGO DOOR CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 23566 FWD cargo door LWR frame edge beam has chafe marks along entire length - 43 inches. removed damaged edge beam; FABBED r eplacement beam IAW BAC DWG 143N6621; installed IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2001070200115 20010702 00115 NM 2001 7 2 AWXA0001816 1 20010604 A 5312 65163007 BULKHEAD BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 FWD pressure BLKHD BS 178 cracked web at WL 189 BL 0. repaired IAW SRM 51-40-2 fig 1 and SRM 51-30-2 pgs 2&3. 2 L 7 2 4F RT A16WE 2001070200116 20010702 00116 NM 2001 7 2 AWXA0001817 1 20010604 A 5310 65C352433 DOOR FRAME BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 aft cargo FWD doorway frame cracked from just above stop fitting NR 5 to area covered by fitting (refer to AWA EO 53-10- 01) marked APPROX STA 807. replaced FWD frame segment IAW REF DWG 65C35243(-3) and DWG 65-47959(-2) and REF SRM 51-10-1 pg 8 and SRM 51-30-2 pg 2-5 and SRM 51-20-4 pg 4 and SRM 51-10-2 pg 7 (note: p/n 65-47959-2 is now 65C35243-3). 2 L 7 2 4F RT A16WE 2001070200117 20010702 00117 NM 2001 7 2 AWXA0001819 1 20010604 A 5315 6545410511 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 cracks on FLOORBEAM web RBL 24 BS 707-715. NDT confirmed cracks in FLOORBEAM web; area repaired IAW SRM 51-40-2 fig 2 p g 1-3. 2 L 7 2 4F RT A16WE 2001070200118 20010702 00118 NM 2001 7 2 AWXA0001820 1 20010604 A 5315 6545410515 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 cracks on FLOORBEAM web LBL 0 BS 708-713. repair parts made and installed IAW ER 15-5710-01137-SS2. 2 L 7 2 4F RT A16WE 2001070200119 20010702 00119 NM 2001 7 2 AWXA0001821 1 20010604 A 5315 6545410515 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 cracks on FLOORBEAM LBL 0 STA 660 across top cap and vert web. repaired IAW ER 15-5710-01137-SS2. 2 L 7 2 4F RT A16WE 2001070200120 20010702 00120 NM 2001 7 2 AWXA0001822 1 20010604 A 5230 6546994504 STIFFENER BOEING 737 737277 1384570 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 aft cargo pit door cracked on web radius at FWD LWR upper corner - FWD LWR door stop fitting LWR inside upper corner. a ft cargo door removed; repaired stiffener radius by replacing IAW SRM 51-10-1 and DWG 65-46994; door reinstalled. 2 L 7 2 4F RT A16WE 2001070200122 20010702 00122 NM 2001 7 2 01FDEA00511 1 20010629 A 5310 STIFFENER BOEING 727 727233 138408A NM BS 1330 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 269FE 21675 01-215 STIFFENER BS 1330, THAT HYDRAULIC LINE CLAMPS TO IS WORN COMPLETELY THROUGH HALF OF ITS SPAN BY HYD LINE. R&R PE R B727 STRUCTURAL REPAIR MANUAL 51-40-4. 2 L 7 3 4F RT A3WE 2001070200123 20010702 00123 NM 2001 7 2 AWXA0001823 1 20010604 A 2520 908356BZ SEAT BOEING 737 737277 1384570 NM CABIN WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 the sides of FWD F/A seat where the pivot arms attach have elongated holes. seat removed; repaired IAW ER 15-2525-01120 -TB1; seat installed IAW MM 25-25-12 pg 201. 2 L 7 2 4F RT A16WE 2001070200124 20010702 00124 NM 2001 7 2 AWXA0001824 1 20010604 A 5330 SKIN BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 fuselage skin cracked at FWD entry door upper hinge cutout, crack is APPROX .625 inch long. crack repaired IAW SRM 53-3 0-3 fig 21. 2 L 7 2 4F RT A16WE 2001070200125 20010702 00125 NM 2001 7 2 AWXA0001825 1 20010604 A 5240 DOOR BOEING 757 7572S7 1384962 NM L4 DOOR OUT OF RIG A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 904AW 23566 PHX - air turnback - 5/31/01 - FLT 49 - on climbout at 10000 ft the left aft entry door light illuminated. the door han dle was observed not fully closed and had a small air leak (L4 door); the aircraft returned to PHX making an uneventful landing. in PHX the L4 door was rigged IAW AMM 52-11-13 and operational and pressurization checks were good; no further discrepancies. 2 L 7 2 4F RT A2NM 2001070200126 20010702 00126 NM 2001 7 2 AWXA0001827 1 20010605 A 5320 651758245 WEB BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 aft side BLKHD vert web has 2 inch crack BS 183 WL 182.5. removed and replaced vert web IAW BAC DWG 65-17582 and SRM 51 -40-02 pg 2, 3, 6, 7 and 38. 2 L 7 2 4F RT A16WE 2001070200127 20010702 00127 NM 2001 7 2 AWXA0001828 1 20010605 A 5311 6516300302 FRAME BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 RT BS 178 chord cracked in center of radius WL 207. removed and replaced cracked side chord IAW SRM 51-10-02 pg 15 item NR 8 and 51-40-02 pg 2 & 10. 2 L 7 2 4F RT A16WE 2001070200128 20010702 00128 NM 2001 7 2 AWXA0001829 1 20010605 A 5311 6516300301 FRAME BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 visual inspection of aft side of BS 178 BLKHD found LT side chord cracked WL 194-195 in center of radius. removed and r eplaced cracked side chord IAW SRM 51-10-02 pg 15 item NR 8 and 51-40-02 pg 2 & 10. 2 L 7 2 4F RT A16WE 2001070200129 20010702 00129 NM 2001 7 2 AWXA0001830 1 20010605 A 5311 654653949 FRAME BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 fuselage frame inner chord cracked at FLOORBEAM attach point left side BS 616. cut out damaged area; FABBED repair angl e and filler; drilled, treated, primed and installed repair IAW BOEING S/B 737-53-1182 and AWA ER 03-5311-01127-KB1. 2 L 7 2 4F RT A16WE 2001070200130 20010702 00130 NM 2001 7 2 AWXA0001831 1 20010605 A 5754 SKIN BOEING 737 73733A 1384673 NM L/E SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 left wing NR 2 leading edge slat lower surface has 4 cracks from rivet holes. cut out damaged area and installed filler and repair doubler IAW SRM 57-43-01 fig 206. 2 L 7 2 4F RT A16WE 2001070200132 20010702 00132 NM 2001 7 2 AWXA0001833 1 20010605 A 5312 65163007 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 HFEC indicates cracks at 4 HI-LOK fasteners in BS 178 BLKHD web WL 234.1 RBL 8-14. cut out damaged area of web and inst alled repair doubler and filler IAW SRM 53-10-08 pg 265-269. 2 L 7 2 4F RT A16WE 2001070200133 20010702 00133 NM 2001 7 2 AWXA0001834 1 20010605 A 5312 65163007 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 HFEC indicates cracks at 4 HI-LOK fasteners in BS 178 BLKHD web WL 234.1 LBL 8-14. cut out damaged area and installed r epair doubler and filler IAW SRM 53-10-08 pg 265-269 and 53-10-08 pg 265 item 13. 2 L 7 2 4F RT A16WE 2001070200134 20010702 00134 NM 2001 7 2 AWXA0001835 1 20010605 A 5320 672038U1 INTERCOSTAL BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 visual inspection of aft side of BS 178 BLKHD found LT intercostal cracked WL 195 LBL 24. removed and replaced cracked intercostal IAW SRM 51-10-02 pg 15 and 51-40-02 pg 2&10. 2 L 7 2 4F RT A16WE 2001070200135 20010702 00135 NM 2001 7 2 AWXA0001836 1 20010605 A 5320 6720382 INTERCOSTAL BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 aft side of BS 178 BLKHD RT intercostal is cracked WL 195 RBL 24. removed cracked intercostal; drilled, treated, primed and installed new intercostal IAW SRM 51-10-02 pg 15 and 51-40-02 pg 2&10. 2 L 7 2 4F RT A16WE 2001070200136 20010702 00136 NM 2001 7 2 AWXA0001837 1 20010605 A 5312 6545409245 PRESSURE PANEL BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 left main wheel well upper pressure web cracked at BS 664 LBL 33. repaired damaged area in web IAW ER 03-5702-01123-KB1 . 2 L 7 2 4F RT A16WE 2001070200137 20010702 00137 NM 2001 7 2 AWXA0001838 1 20010606 A 2161 32193211 CONTROL VALVE BOEING 737 7373Y0 1384671 NM LT A/C PACK FAILED A AWXA A UNSCHED LANDING O OTHER UK UNKNOWN 1 WP 28 331AW 43480 10777 23747 PHX - air turnback - 6/2/01 - FLT 521 - after takeoff from PHX en route to RNO the flight crew reported the LT air condi tioning pack was blowing warm air, not cooling the aircraft and returned to PHX. PHX maintenance troubleshot and found t he 35 degree control valve staying open; the 35 degree control valve and sensor were replaced IAW AMM 21-51-30 & 21-51-5 1; functional checks were good; no further discrepancies noted. 2 L 7 2 4F RT A16WE 2001070200138 20010702 00138 NM 2001 7 2 AWXA0001839 1 20010606 A 5230 143N66186 DOOR FRAME BOEING 757 7572S7 1384962 NM CARGO DOOR DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 FWD cargo door FWD LWR corner frame dented. removed damaged FWD cargo door FWD LWR frame corner IAW SRM 51-40-2; instal led customer supplied p/n 143N6618-6 R844567 IAW SRM 51-40-2. 2 L 7 2 4F RT A2NM 2001070200139 20010702 00139 EU 2001 7 2 AWXA0001840 1 20010608 A 5610 NP1653116 WINDSHIELD AIRBUS 320 A320231 3930325 EU COCKPIT CRACKED A AWXA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 28 628AW 67 DTW - unscheduled landing - 6/7/01 - FLT 55 - en route from JFK to LAS the First Officer's NR 1 window outer pane cracke d and the aircraft diverted to DTW making an uneventful landing. window changed and aircraft returned to service. 2 L 7 2 4F RT A28NM 2001070200140 20010702 00140 EU 2001 7 2 AWXA0001841 2 20010608 A 7250 CFM563 TURBINE BOEING 737 737301 1384611 NM CFMINT CFM56 CFM563B2 13802 EU LT ENGINE FAILED A AWXA C ABORTED TAKEOFF Y ENGINE STOPPAGE TO TAKEOFF 1 WP 28 324AW 32669 8610 23261 724432 DTW - aborted takeoff - 6/7/01 - FLT 528 - on takeoff, loud noise heard from left side of aircraft, lost several fan bla des, E-1 LPT-1 turbine failed. takeoff aborted. no airframe damage; engine changed and aircraft returned to service. 2 L 7 2 4F 4 F RT A16WE E21EU 2001071200156 20010712 00156 NM 2001 7 12 AWXA0001842 1 20010608 A 2730 GUARD BOEING 737 73733A 1384673 NM ELEVATOR OUT OF POSITION A AWXA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 WP 28 168AW 49007 23629 PHX - AIR TURNBACK - 6/7/01 - FLT 519 - HEAVY ELEVATOR AFTER ROTATION; AIRCRAFT RETURNED TO AIRPORT W/ NO FURTHER PROBLE MS. MX FOUND CABLE PULLEY BRACKET AT STA 420 ON CABLE EBS WORN; REPLACED PULLEY BRACKET; AIRCRAFT RETURNED TO SERVICE. THE ELEV CABLE EB-5 WAS FOUND TO HAVE COME OFF THE PULLEY AND SLIPPED BETWEEN THE PULLEY AND BRACKET. FURTHER INVESTIG ATION FOUND THE PULLEY GUARD WAS LOCATED 4.383 INCH FROM THE PULLEY CENTER BOLT HOLE. BOEING DWG 69-73450 INDICATES IT SHOULD BE 4.268 TO 4.278 INCH. THE AIRCRAFT CAME OUT OF C-CHECK ON 5-26-2001 WHERE WORK HAD BEEN PERFORMED THAT REQUIRE D THE FWD END OF THE CABLE RUN TO BE LOOSENED. THE CABLE PROBABLY CAME OFF AT THAT TIME. 2 L 7 2 4F RT A16WE 2001070200141 20010702 00141 NM 2001 7 2 AWXA0001843 1 20010611 A 5315 6546812 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 aft cabin FLOORBEAM BS 947 has APPROX 1 sq inch corrosion at LBL 11. removed corrosion IAW SRM 53-60-51 fig 101 pg 110 det VII; corrosion exceeded limits IAW SRM 53-60-51 fig 101 pg 110 (max allowed .013 inch, removed .023 inch). repaired damaged area IAW SRM 53-00-51 fig 202 pg 209-211; repair angles heat treated IAW TPS-1003 revision A. 2 L 7 2 4F RT A16WE 2001070200142 20010702 00142 NM 2001 7 2 AWXA0001844 1 20010611 A 5315 6546811 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 aft lav FLOORBEAM BS 986.5 has moderate to severe exfoliated corrosion upper T-cap APPROX 30 sq inch. repaired IAW SRM 53-00-51 fig 202 sht 1-4. 2 L 7 2 4F RT A16WE 2001070200143 20010702 00143 NM 2001 7 2 AWXA0001845 1 20010611 A 5311 651630030 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 cockpit LT side chord cracked at center of radius WL 207 BS 178 confirmed HFEC. removed and replaced chord IAW SRM 51-4 0-02 pg 38, 2&3. 2 L 7 2 4F RT A16WE 2001070200144 20010702 00144 NM 2001 7 2 AWXA0001846 1 20010611 A 5310 6545855 CREASE BEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 RT crease beam (wet area) BS 947-990 has APPROX 10 sq inch surface corrosion and 1 drilled off fastener. removed surfac e corrosion on RT crease beam - corrosion within limits IAW SRM 53-60-15 fig 101. 2 L 7 2 4F RT A16WE 2001070200145 20010702 00145 NM 2001 7 2 AWXA0001847 1 20010611 A 5330 654824050 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 fuselage skin is chafed 2 places below RT HORIZ stab rear spar mount lug. replaced two skin plates IAW DWG 65-48240 and SRM 51-40-02 pg 6-7. 2 L 7 2 4F RT A16WE 2001070200146 20010702 00146 NM 2001 7 2 AWXA0001848 1 20010611 A 5320 65C320747 FLOOR SUPPORT BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 corrosion on transverse floor support BS 993 RBL 33 WL 208. repaired IAW SRM 51-40-02 pg 6. 2 L 7 2 4F RT A16WE 2001070200147 20010702 00147 NM 2001 7 2 AWXA0001849 1 20010611 A 5512 65C27494 SKIN BOEING 737 7373G7 1384595 NM HORIZ STAB GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 RT HORIZ stab LWR skin gouged APPROX 14 inches aft of FWD spar, stab STA 175-184. repaired skin IAW SRM 55-10-01 pg 216 -220, 225-228. 2 L 7 2 4F RT A16WE 2001070200148 20010702 00148 NM 2001 7 2 AWXA0001850 1 20010611 A 5753 654782124 SPINDLE BOEING 737 737277 1384570 NM FLAP CARRIAGE BROKEN A AWXA K NONE F FLT CONT AFFECTED NR NOT REPORTED 1 WP 28 187AW 22654 ELP - 5/30/01 - FLT 459 - pilot reported the aircraft used excessive lateral trim when the flaps were down. MX ferry to PHX. MX found NR 7 flap carriage spindle broken. flap carriage changed, aircraft returned to service. 2 L 7 2 4F RT A16WE 2001070200149 20010702 00149 NM 2001 7 2 SWAA011637 1 20010601 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 787SA 29812 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER BROKEN AT OVERWING EXIT. Removed and replaced EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2001070200150 20010702 00150 NM 2001 7 2 SWAA011638 1 20010602 A 3350 6104789 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR and FWD SVC DOOR EMERGENCY EXIT LIGHTS INOP. Removed and replaced EMERGENCY LIGHT BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2001070200151 20010702 00151 NM 2001 7 2 SWAA011639 1 20010601 A 3350 1000689 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 090SW 22905 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. Removed and replaced EMERGENCY EXIT LIG HT BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2001070200152 20010702 00152 2001 7 2 SWAA011640 4 20010603 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001070200153 20010702 00153 NM 2001 7 2 SWAA011641 1 20010604 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED RON CHECK, FOUND FUSE SKIN CRACKED BETWEEN BS 360 & BS 380, JUST ABOVE STR 15L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001070200154 20010702 00154 NM 2001 7 2 SWAA011642 1 20010604 A 5523 BACB28AK04 BUSHING BOEING 737 7377H4 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 740SW 29276 DURING SCHEDULED SERVICE CHECK, SWA SI 11052-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. Removed and replaced RT ELEVAT OR NR 1 HINGE BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2001070200155 20010702 00155 NM 2001 7 2 SWAA011643 1 20010605 A 5330 6552988 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001070200156 20010702 00156 2001 7 2 SWAA011644 4 20010604 A 2565 D31354 SLIDE BOEING 737 7373K2 13844BA NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 340LV 23738 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC S LIDE PER MM. 2 L 7 2 4F RT A16WE 2001070200157 20010702 00157 2001 7 2 SWAA011645 4 20010604 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 089SW 22904 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC S LIDE PER MM. 2 L 7 2 4F A16WE 2001070200159 20010702 00159 NM 2001 7 2 SWAA011647 1 20010604 A 3350 57771 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 089SW 22904 DURING SCHEDULED C4 CHECK, FOUND EEPLS END CAP MISSING ON AFT END. INSTALLED END CAP PER MM. 2 L 7 2 4F A16WE 2001070200160 20010702 00160 NM 2001 7 2 SWAA011648 1 20010605 A 5311 963820 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 630WN 27705 DURING SCHEDULED 1/2D CHECK AT DALFORT, FOUND BULKHEAD SIDE CHORD CRACKED AT BS 178, WL 207, LT SIDE. Removed and repla ced CHORD PER SWA ACO. 2 L 7 2 4F RT A16WE 2001070200161 20010702 00161 NM 2001 7 2 SWAA011649 1 20010604 A 5320 BAC1503 STIFFENER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED SERVICE CHECK, FOUND VERTICAL STIFFENER CRACKED AT MLG W/W, BS 663, LBL 6.15. REPAIRED STIFFENER PER S WA RA. 2 L 7 2 4F A16WE 2001070200162 20010702 00162 NM 2001 7 2 SWAA011650 1 20010606 A 5320 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED 1/4D CHECK, FOUND STR CLIP CRACKED AT BS 500C, STR 27L. Removed and replaced STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001070200163 20010702 00163 2001 7 2 SWAA011651 4 20010606 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. Removed and replaced EMERG ENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001070200164 20010702 00164 NM 2001 7 2 SWAA011653 1 20010605 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 521SW 25320 EEPLS INOP AT FWD END OF STRIP. REPAIRED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001070200165 20010702 00165 NM 2001 7 2 SWAA011654 1 20010605 A 3397 BR2013 WIRE BOEING 737 7373A4 1384585 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 EEPLS WIRES EXPOSED AT ROW 9. SECURED EEPLS WIRES PER MM. 2 L 7 2 4F RT A16WE 2001070200166 20010702 00166 NM 2001 7 2 SWAA011655 1 20010606 A 3411 BACB30FL3 SCREW BOEING 737 737317 138447P NM PITOT TUBE LOOSE A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 693SW 23174 AIR TURNBACK. DURING CLIMB F/A HEARD LOUD POP and HIGH SQUEAL STARTED IN COCKPIT. FOUND CAPT AUX PITOT TUBE SCREWS LOO SE, TIGHTEN SCREWS PER MM. 2 L 7 2 4F RT A16WE 2001070200167 20010702 00167 NM 2001 7 2 SWAA011656 1 20010605 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 525SW 26567 EEPLS INOP AT MID CABIN. REPAIRED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001070200168 20010702 00168 NM 2001 7 2 SWAA011660 1 20010606 A 3350 57771 CAP BOEING 737 7375H4 138449D NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 521SW 25320 DURING SCHEDULED C3 CHECK, FOUND EEPLS END CAP MISSING AT FWD END. INSTALLED EEPLS END CAP PER MM. 2 L 7 2 4F RT A16WE 2001070200169 20010702 00169 CE 2001 7 2 C2XA01CL153 1 20010624 A 3230 1013841377 SWITCH BEECH 1900 1900D 1154162 CE COCKPIT FAILED A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 47542 11233 UE198 CLE FLIGHT# 3375 THE CREW REPORTED AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT WITHOUT USING THE DOWN LOCK RELEASE SWITCH.MAINTENANCE REPLACED THE LANDING GEAR CONTROL SWITCH.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR S ERVICE. 2 L 7 2 4T RT A24CE 2001070200170 20010702 00170 NM 2001 7 2 SWAA011661 1 20010607 A 5220 4439 LATCH BOEING 737 7377H4 NM COCKPIT UNSECURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 401WN 29813 COCKPIT DOOR EMERGENCY EXIT HATCH NOT SECURED. RESEATED EMERGENCY EXIT LATCHES PER MM. 2 L 7 2 4F RT A16WE 2001070200171 20010702 00171 NM 2001 7 2 SWAA011663 1 20010607 A 5315 6546804 FLOORBEAM BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED IN AFT CARGO AT BS 807 & BS 860, LBL 17. REPAIRED FLOORBEAMS PER SRM. 2 L 7 2 4F RT A16WE 2001070200172 20010702 00172 NM 2001 7 2 SWAA011664 1 20010607 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 986, WL 208, RBL 30 TO LBL 20. REPAIRED FLOORBEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2001070200173 20010702 00173 NM 2001 7 2 SWAA011665 1 20010608 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 380SW 26587 EEPLS WIRES EXPOSED. SECURED EEPLS WIRES PER MM. 2 L 7 2 4F RT A16WE 2001070200174 20010702 00174 NM 2001 7 2 SWAA011666 1 20010608 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 394SW 27380 EEPLS WIRES EXPOSED AT ROW 17. SECURED EEPLS WIRES PER MM. 2 L 7 2 4F RT A16WE 2001070200175 20010702 00175 2001 7 2 SWAA011668 4 20010608 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 378SW 26585 DURING SCHEDULED BC1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PE R MM. 2 L 7 2 4F RT A16WE 2001070200176 20010702 00176 2001 7 2 SWAA011669 4 20010608 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 074SW 22674 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001070200177 20010702 00177 NM 2001 7 2 SWAA011670 1 20010609 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 344SW 24152 FWD CABIN OUTBOARD EMERGENCY FLASHLIGHT INOP. Removed and replaced EMERGENCY FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2001070200178 20010702 00178 EA 2001 7 2 COMA0160410 1 20010628 A 2750 852010011 ACTUATOR CNDAIR CL600 CL6002B19 EA BINDING A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 958CA 12871 6480 7111 FLAPS FAILED AT 30 DEGREES.REPLACED THE LEFT HAND #1 FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2001070200179 20010702 00179 CE 2001 7 2 C2XA01CL155 1 20010624 A 3260 LIGHT BEECH 1900 1900D 1154162 CE COCKPIT DIRTY A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 81538 UE199 CLE FLIGHT# 3108 THE CREW REPORTED THE NOSE GEAR LIGHT DID NOT ILLUMINATE WHEN THE GEAR WAS EXTENDED.THE AIRCRAFT LANDE D WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND CLEANED THE NOSE GEAR LIGHT SOCKET.OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT A24CE 2001070200180 20010702 00180 2001 7 2 SWAA011672 4 20010609 A 2565 D31354 SLIDE BOEING 737 7377H4 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 792SW 27887 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. INSTALLED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001070200181 20010702 00181 NM 2001 7 2 SWAA011678 1 20010609 A 5320 65C27314 STRINGER CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT STR 12L, BS 747, BS767, BS 787 & BS 807. REPAIRED CLIPS PER S RM. 2 L 7 2 4F A16WE 2001070200182 20010702 00182 CE 2001 7 2 C2XA01CL156 1 20010625 A 3260 MS25237327 LAMP BEECH 1900 1900D 1154162 CE COCKPIT BURNED OUT A C2XA O OTHER L NO TEST NR NOT REPORTED 1 SW 27 69549 UE194 CLE FLIGHT# 3196 THE CREW REPORTED THE UPPER RED LIGHT ON GEAR HANDLE WAS INOPERATIVE.MAINTENANCE REPLACED THE UPPER LAM P ON THE GEAR HANDLE.OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT A24CE 2001070200183 20010702 00183 NM 2001 7 2 SWAA011679 1 20010608 A 2730 6545166 CONTROL ROD BOEING 737 7373H4 1384600 NM ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED C4 CHECK, FOUND RT ELEVATOR FAILED FREE PLAY CHECK. Removed and replaced ELEVATOR INPUT ROD PER MM. 2 L 7 2 4F RT A16WE 2001070200184 20010702 00184 NM 2001 7 2 SWAA011680 1 20010608 A 2731 6545190 TRIM TAB BOEING 737 7373H4 1384600 NM ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED C4 CHECK, FOUND RT ELEVATOR TAB FAILED FREE PLAY CHECK. Removed and replaced RT ELEVATOR CONTROL TAB M ECHANISM PER MM. 2 L 7 2 4F RT A16WE 2001070200185 20010702 00185 NM 2001 7 2 SWAA011682 1 20010610 A 5315 BAC1509 FLOORBEAM BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CRACKED AFT CARGO BS 787, STR 27R. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2001070200186 20010702 00186 NM 2001 7 2 SWAA011683 1 20010608 A 5315 BAC1509 FLOORBEAM BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON FLOORBEAMS AFT CARGO AT BS 860, LBL 8, RBL 3 & RBL 8. REPAIRED FLOORBEA MS PER SWA RA. 2 L 7 2 4F RT A16WE 2001070200187 20010702 00187 NM 2001 7 2 SWAA011690 1 20010608 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 394SW 27380 EEPLS WIRES LOOSE AT ROW 17. SECURED EEPLS WIRES PER MM. 2 L 7 2 4F RT A16WE 2001070200188 20010702 00188 NM 2001 7 2 SWAA011692 1 20010610 A 3350 6574550 LIGHT BOEING 737 7373H4 1384600 NM SERVICE DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED D-CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE LIGHT INOP. REPAIRED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001070200189 20010702 00189 NM 2001 7 2 SWAA011693 1 20010610 A 3350 57771 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED C1 CHECK, FOUND EEPLS END CAPS MISSING AT FWD & AFT END. INSTALLED EEPLS END CAP PER MM. 2 L 7 2 4F A16WE 2001070200190 20010702 00190 NM 2001 7 2 SWAA011694 1 20010611 A 5312 6517582 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 090SW 22905 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND VERTICAL BEAM CRACKED AT BS 178, LBL 17.1. REPAIRED VERTICAL BEAM PER SRM. 2 L 7 2 4F A16WE 2001070200191 20010702 00191 NM 2001 7 2 SWAA011695 1 20010611 A 5312 6517582 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 090SW 22905 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND VERTICAL BEAM CRACKED AT BS 178, RBL 17.1. REPAIRED VERTICAL BEAM PER SRM. 2 L 7 2 4F A16WE 2001070200192 20010702 00192 NM 2001 7 2 SWAA011696 1 20010611 A 5320 6551698 SPLICE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 090SW 22905 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER SPLICE and TIE CLIP CRACKED AT BS 360, STR 4L. REPAIRED STR SPLICE and TIE CLIP PER SRM. 2 L 7 2 4F A16WE 2001070200194 20010702 00194 NM 2001 7 2 ZW0A0104401 1 20010630 A 3350 6100928 LAMP BOEING 767 767300 1385204 NM SEAT 34H BURNED OUT A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 691LF 25137 THE EGRESS LIGHT AT SEAT 34H WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 9-23-00 LAX. ---CLOSED-- 2 L 7 2 4F RT A1NM 2001070200195 20010702 00195 NM 2001 7 2 ZW0A0104402 1 20010629 A 3350 767 LIGHT BOEING 767 7673Q8 1385142 NM EXTERIOR INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 635TW 28207 THE EMERGENCY LIGHT ON THE FUSELAGE AFT OF THE RT WING WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 2-22-01 LAX. --CLOS ED-- 2 L 7 2 4F RT A1NM 2001070200196 20010702 00196 NM 2001 7 2 SWAA011701 1 20010612 A 3350 65C34691 LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 514SW 25153 DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LOOSE, AT LT OVERWING EXIT. SECURED B ULL NOSE EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001070200197 20010702 00197 NM 2001 7 2 SWAA011702 1 20010612 A 3350 6556633 LIGHT BOEING 737 7373G7 1384595 NM FUSELAGE INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 683SW 24008 DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT AFT RIGHT FUSELAGE. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001070200198 20010702 00198 NM 2001 7 2 SWAA011704 1 20010611 A 3350 90083 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED D-CHECK, FOUND EMERGENCY EXIT SIGN INOP AT OVERWING EXIT. Removed and replaced BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2001070200199 20010702 00199 2001 7 2 SWAA011705 4 20010611 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC S LIDE PER MM. 2 L 7 2 4F A16WE 2001070200200 20010702 00200 NM 2001 7 2 SWAA011706 1 20010611 A 3350 65C27093 COVER BOEING 737 737* NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 798SW 28436 FWD ENTRY DOOR EMERGENCY EXIT LIGHT COVER LOOSE. Removed and replaced EXIT LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001070200201 20010702 00201 NM 2001 7 2 SWAA011707 1 20010612 A 3350 BR2013 LENS BOEING 737 7377H4 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 714CB 27848 EEPLS FLOOR TRACK LENSES LOOSE, AT FWD CABIN. SECURED EEPLS LENSES PER MM. 2 L 7 2 4F RT A16WE 2001070200202 20010702 00202 NM 2001 7 2 SWAA011708 1 20010612 A 3350 BR2013 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 702ML 22054 EEPLS INOP AT ROW 3. RELAMPED EEPLS PER MM. 2 L 7 2 4F A16WE 2001070200203 20010702 00203 NM 2001 7 2 SWAA011710 1 20010610 A 5523 BACB28AK04 BUSHING BOEING 737 7377H4 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 710SW 27844 DURING SCHEDULED SERVICE CHECK, SWA SI 11052-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. Removed and replaced RT ELEVAT OR INBOARD HINGE BUSHING PER MM. 2 L 7 2 4F RT A16WE 2001070200204 20010702 00204 NM 2001 7 2 SWAA011712 1 20010613 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 652SW 27722 EEPLS LOOSE AT ROW 12. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001070200205 20010702 00205 NM 2001 7 2 SWAA011713 1 20010613 A 3350 6104789 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 090SW 22905 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. Removed and replaced BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2001070200206 20010702 00206 NM 2001 7 2 SWAA011716 1 20010613 A 3350 6104781 BALLAST BOEING 737 7377H4 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 754SW 29849 DURING SCHEDULED C2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. Removed and replaced LIGHT BALLAST PER MM. 2 L 7 2 4F RT A16WE 2001070200207 20010702 00207 NM 2001 7 2 DHL2001715008 1 20010630 A 3260 DOWNLOCK SWITCH BOEING 727 727155C 138404Z NM A DHLA O L OTHER ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 715DH 19618 DURING GEAR EXTENSION @ CVG LT. MAIN GEAR LIGHT DID NOT ILLUMINATE. RED LEFT GEAR DOOR LIGHT REMAINED ILLUMINATED. PERFO RMED ABNORMAL PROCEDURE, PROBLEM WAS NOT CORRECTED.R&R'D LEFT MAIN GEAR DOWNLOCK SWITCH IAW B-727 M/M 32-09-211. OP CHEC KS SERVICEABLE. 2 L 7 3 4F A3WE 2001070200209 20010702 00209 NM 2001 7 2 SWAA011718 1 20010611 A 5311 6546546 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT STR 8-9R, BS 827, BS 867 & BS 727D. REPAIRED FRAMES PER BFG ER. 2 L 7 2 4F RT A16WE 2001070200210 20010702 00210 2001 7 2 SWAA011725 4 20010613 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUSTMENT. ADJUSTED EMERGENCY EV AC SLIDE GIRT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001070200211 20010702 00211 NM 2001 7 2 SWAA011726 1 20010614 A 3397 BR2013 WIRE BOEING 737 7375H4 138449D NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 EEPLS WIRES EXPOSED AT ROW 10. SECURED EEPLS WIRES PER MM. 2 L 7 2 4F RT A16WE 2001070200212 20010702 00212 NM 2001 7 2 SWAA011727 1 20010612 A 3350 BR2013 TRACK BOEING 737 7377H4 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 714CB 27848 EEPLS TRACK LOOSE FWD CABIN. SECURED EEPLS TRACK PER MM. 2 L 7 2 4F RT A16WE 2001070200213 20010702 00213 WP 2001 7 2 CALA0100618 1 20010629 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP STA 256-313 PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND R/H CABIN FLOOR PANEL PUNCTURED AT STA 256-313 SIDEWALL SUPPORT STRUCTURE. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND ECRA 5320-01265. 2 L 7 2 4F A6WE 2001070200214 20010702 00214 WP 2001 7 2 CALA0100621 1 20010630 A 5730 SKIN DOUG DC9 DC982 3022082 WP PANEL #1613 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND LOWER SURFACE OF SKIN PANEL #1613 GOUGED AT R/H I/B FLAP T/E AREA. THE PANEL SKIN WAS REMOVED AND NEW S KIN WAS INSTALLED IAW SRM 51-30-2, 57-50-9, AND 51-10-3. 2 L 7 2 4F A6WE 2001070200215 20010702 00215 WP 2001 7 2 CALA0100622 1 20010630 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FS 1338 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND JACK SUPPORT ANGLE CORRODED IN CHANNEL AREA AT BOTTOM OF APB, FS 1338, LONGERON 30. THE JACK SUPPORT AN GLE AND VERTICAL CHANNEL STRINGER TIE FITTINGS WERE REMOVED IAW SRM 51-30-2 AND 51-30-5. A NEW ANGLE WAS INSTALLED WITH TIE FITTINGS IAW SRM 51-10-4, 51-10-3, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 2001070200216 20010702 00216 WP 2001 7 2 CALA0100623 1 20010630 A 5320 PAN DOUG DC9 DC982 3022082 WP FWD CARGO DR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND FORWARD PIT DOOR PAN BETWEEN TWO LOWER STOPS AT DRAIN HOLE CORRODED. THE CORRODED AREA WAS CUT OUT IAW SRM 53-05, FIGURE 44. A NEW LOWER PAN AND REPAIR ANGLES WERE INSTALLED IAW SRM 51-10-4, 53-05, FIGURE 44, 51-30-1, 51-30 -2, 51-30-5, AND 51-10-3. 2 L 7 2 4F A6WE 2001070200217 20010702 00217 NM 2001 7 2 CALA0100626 1 20010701 A 5330 SKIN BOEING 737 7373T0 1384582 NM BS 219-227 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND FUSELAGE SKIN BETWEEN FORWARD EQUIPMENT ACCESSORY DOOR AND NOSE GEAR WHEEL WELL GOUGED AT BS 219-227, B L 0. THE SKIN WAS REPAIRED IAW ECRA 5310-04157. 2 L 7 2 4F RT A16WE 2001070200218 20010702 00218 NM 2001 7 2 AWXA0001911 1 20010701 A 5313 143N3110 STRINGER BOEING 757 757225 1384959 NM STA623 DENTED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 907AW 22691 D: Found Stringer 16L at Sta 623 to have dent C: Removed damaged stringer section and installed repair IAW SRM 530-00-03 Fig 201 2 L 7 2 4F RT A2NM 2001070200219 20010702 00219 NM 2001 7 2 AWXA0001912 1 20010701 A 5330 143N3300923 SKIN BOEING 757 757225 1384959 NM STE640,15L-17L DENTED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 907AW 22691 D: Fuselage skin STA 640 between STR 17L and 15L is dented and has 3 existing doublers which do not meet SRM seperation requirements.C: Repaired damaged skin per E.R. 19-5331-01179- DOI 2 L 7 2 4F RT A2NM 2001070200220 20010702 00220 NM 2001 7 2 AWXA0001913 1 20010701 A 5300 146N3750 SKIN BOEING 757 757225 1384959 NM STR1556 STR21L PUNCTURED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 907AW 22691 D: 1.5" x 1.5" hole in fuselage below & fwd of L-4 door below STR 21LC: repaired per E.R. 19-5331-01171-DL3 2 L 7 2 4F RT A2NM 2001070200221 20010702 00221 WP 2001 7 2 DHL2001804012 1 20010630 A 3150 PROXIMITY SWITCH DOUG DC8 DC873F 302199F WP A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 804DH 46124 DURING TAKEOFF TAKEOFF WARNING HORN WENT OFFREMOVED AND REPLACED LANDING GEAR PROX BOX IAW MM 27-52-1, 27-52*-2 OPS CK GOOD 2 L 7 4 4F RT 4A25 2001070200222 20010702 00222 NE 2001 7 2 NACA20010025 2 20010629 A 7230 356995 CYLINDER PWA CB3 DOUG DC6 C118A 3021710 WP PWA R2800 R2800CB3 52026 NE ENGINE FAILED A NACA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 1377K 1905 1327 36710 44596 36710 DISCREPANCY; #1 engine #10 cylinder left side shorted secondary, and running rough. #1 engine backfiring, and BMEP errat ic at all power settings.CORRECTIVE ACTION; Replaced #10 coil and #10 cylinder. 2 L 7 4 4R 4 R 6A3 5E8 2001070300001 20010703 00001 NE 2001 7 3 EVA002 2 20010624 A 7220 CF680C2D1F ENGINE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE FOD W QOCF J D E DUMP FUEL RETURN TO BLOCK ENGINE SHUTDOWN C E F.O.D. VIBRATION/BUFFET TO TAKEOFF 1 WP 03 48546 704721 1. AIRCRAFT B-16107 DURING T/O RUN IN BRU, A/C NO.3 ENGINE BIRD STRIKE. VIBRATION JUMP UP TO 4.2 & FELT BY THE CREW. CAP TAIN S/D THE ENGINE, DUMP FUEL AND AIR RETURN TO BRU.2. ON GND, VISUAL CHK FND 3 FAN BLADES DAMAGED.3. PFM BSI ON #3 ENG INE, ALL COND NML.4. PER MM DETAIL INSPECT THE DAMAGED FAN BLADES, RPL 2 BLADES AND ENGINE RUNUP TEST NML. 2 L 7 3 4F 4 F RT A22WE E31N3 2001070300002 20010703 00002 SO 2001 7 3 C2XA01IA284 1 20010627 A 3350 3071BPE BULB EMB 120 EMB120ER 3260203 SO CABIN BURNED OUT A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15726 120174 IAH - DURING POST FLIGHT INSPECTION, SEVERAL EMERGENCY AISLE PATH LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THA FFECTED LIGHT BULBS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001070300003 20010703 00003 SO 2001 7 3 C2XA01IA286 1 20010701 A 2100 32144143 VALVE EMB 120 EMB120ER 3260203 SO INOPERATIVE A C2XA K NONE O OTHER UK UNKNOWN 1 SW 27 12715 120125 IAH - FLIGHT 2963, THE CREW REPORTED SMOKE IN THE COCKPIT AFTER THE NUMBER ONE PACK WAS TURNED ON. MAINTENANCE REMOVED A ND REPLACED THE NUMBER ONE PRESSURIZATION AND SHUT OFF VALVE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001070300004 20010703 00004 WP 2001 7 3 0102139918 1 20010613 A 3610 CLAMP DOUG DC9 DC932 3022066 WP A/C BAY BROKEN A NWAA G O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 GL 01 940N 47572 AT 35,000 FEET, MASTER WARNING AND CABIN ALT LIGHTS ILLUMINATED WITH CABIN CLIMBING AT 1000 FT PER MINUTE AND ALL PASSEN GER OXYGEN MASKS DEPLOYED. FOLLOWED COM PROCEDURES AND WERE UNABLE TO CONTROL CABIN IN AUTO OR MANUAL WITH AIRFOIL AND ENGINE ANTI-ICE OFF. DESCENDED TO 10,000 FT AND RETURNED TO MSP. MAINTENANCE FOUND A BLOWN DUCT BOOT AND BROKEN CLAMP AFT OF RIGHT WATER SEPARATOR. REPLACED BOOT AND CLAMPS. OPERATIONAL AND PRESSURIZATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001070300005 20010703 00005 WP 2001 7 3 0102149942 1 20010613 A 2130 39613011 CONTROL VALVE DOUG DC9 DC932 3022066 WP A/C BAY FAILED A NWAA G B O2 MASK DEPLOYED EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 3991C 54582 47175 AIRCRAFT LOST PRESSURIZATION AT 35,000 FT. MASKS DEPLOYED AND AIRCRAFT INITIATED AN EMERGENCY DESCENT, DIVERTED TO GFK, AND LANDED WITHOUT INCIDENT. REPLACED THE FLOW CONTROL VALVE, PRESSURE REGULATOR VALVE, AND PILOT PRESSURE REGULATOR. OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 2001070300006 20010703 00006 WP 2001 7 3 0102159603 1 20010611 A 2150 ACM DOUG DC9 DC932 3022066 WP A/C BAY FAILED A NWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 603NW 47101 CABIN PRESSURIZATION LIGHT ILLUMINATED AT 35,000 FEET. AN EMERGENCY DESCENT WAS MADE. MAINTENANCE REPLACED THE AIR CYC LE MACHINE, WATER SEPARATOR CONTROL VALVE, COMPRESSOR DISCHARGE SWITCH, PRIMARY AND SECONDARY HEAT EXCHANGERS, AND DIVER TER VALVE. OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 2001070300007 20010703 00007 NM 2001 7 3 0102186626 1 20010616 A 2170 SEPARATOR BOEING 747 747251B 1384892 NM A/C BAY ODOR A NWAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 01 626US 21708 DURING TAXI OUT, FLIGHT ATTENDANT AND PASSENGER SMELLED BURNING IN VICINITY OF DOOR 3 AISLE. RETURNED TO GATE WITHOUT I NCIDENT. INSPECTED FORWARD CARGO COMPARTMENT, GALLEYS, LAVS, CABIN, SEATBOXES, WIRE BUNDLES, CALL LIGHTS, READING LIGHT S, SIDEWALL, CEILING LIGHTS, ALL ZONE VIDEO PROJECTORS, AND LEFT WHEEL WELL. REPLACED COALESCER WATER SEPARATORS FOR AL L 3 PACKS. ALL SYSTEMS OPERATIONAL CHECK NORMAL. 2 L 7 4 4F A20WE 2001070300008 20010703 00008 EU 2001 7 3 0102193264 1 20010615 A 2910 O-RING AIRBUS 320 A320212 EU HYD SYSTEM LEAKING A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 364NW 911 DURING CRUISE, CREW RECEIVED HYDRAULIC GREEN RESERVOIR LEVEL LOW ECAM WARNING. CREW FOLLOWED COM PROCEDURE AND DIVERTED TO LAX. MAINTENANCE REPLACED O-RING FILTER ON NR 5 SPOILER FILTER HOUSING AND SERVICED HYDRAULIC SYSTEM. LEAK AND OPER ATIONAL CHECK NORMAL. 2 L 7 2 4F RT A28NM 2001070300009 20010703 00009 WP 2001 7 3 IXXA0100036O 1 20010606 A 3260 HINGE PIN DOUG DC8 DC871F 302199D WP MAIN GEAR DOORS WORN A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 826BX 83219 1107 45998 IN ROUTE FROM RDU TO TOL AFTER GEAR RETRACTION LANDING GEAR DOOR UNSAFE LIGHT ILLUMINATED. FLIGHT CREW CYCLED THE LANDIN G GEAR, WARNING INDICATION REMAINED THE SAME. FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENACE INSPECTED TH E LANDING GEAR WHICH REVEALED MAIN LANDING GEAR DOOR HINGE PINS WORN. MAINTENACE REPLACED THE HINGE PINS AND PERFORM A S UCCESSFUL OPERATIONAL CHECK. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2001070300010 20010703 00010 2001 7 3 0102209988 4 20010626 A 2565 13621228 SLIDE DOUG DC9 DC931 3022065 WP TAIL UNSERVICEABLE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8944E 54434 73 47167 DURING LINE CHECK, DISCOVERED TAIL EVACUATION SLIDE PRESSURE AT ZERO PSI. REPLACED SLIDE AND RETURNED REMOVED SLIDE TO SHOP FOR REPAIR. 2 L 7 2 4F A6WE 2001070300011 20010703 00011 NM 2001 7 3 0102212714 1 20010623 A 2910 HYDRAULIC LINE BOEING 727 7272S7 138407Z NM HYD SYSTEM FAILED A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 718RC 22344 AFTER TAKEOFF AND DURING GEAR RETRACTION, THE A-SYSTEM HYDRAULICS FAILED. FLIGHT RETURNED TO DEN AND COMPLETED AN UNEVE NTFUL LANDING. MAINTENANCE REPLACED LEFT GEAR RETRACT ACTUATOR FLEX LINE AND NR 1 ENGINE DRIVEN PUMP. LEAK AND OPERATI ONAL CHECK OK. 2 L 7 3 4F A3WE 2001070300012 20010703 00012 NM 2001 7 3 0102222762 1 20010620 A 3260 63200036 SWITCH BOEING 727 7272M7 138407S NM RT MLG DOOR FAULTY A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 722RW 21201 AFTER TAKEOFF, CREW RETRACTED GEAR AND RECEIVED A RIGHT GEAR DOOR WARNING INDICATION. CREW PERFORMED COM PROCEDURE AND RECYCLED GEAR WITH NO HELP, WARNING LIGHT STILL ILLUMINATED. CREW FOLLOWED COM PROCEDURE AND RETURNED TO MSP AND MADE A N UNEVENTFUL LANDING. MAINTENANCE PLACED GEAR DOOR ON MEL AND FLIGHT CONTINUED TO IND. MAINTENANCE REPLACED THE DOOR S WITCH. OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 2001070300013 20010703 00013 NM 2001 7 3 0102236302 1 20010621 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN BROKEN A NWAA O OTHER O OTHER CR CRUISE 1 GL 01 662US 23720 DURING CRUISE, EMERGENCY ESCAPE PATH LIGHTS ILLUMINATED BETWEEN ROWS 39R-60R. REPAIRED OPEN WIRE. OPERATIONAL CHECK NO RMAL. 2 L 7 4 4F RT A20WE 2001070300014 20010703 00014 NM 2001 7 3 0102246302 1 20010622 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 662US 23720 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE AT PASSENGER DOORS 1R AND 4L. RECONNECTED WIRING. OP ERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001070300015 20010703 00015 WP 2001 7 3 0102259882 1 20010621 A 2131 2075301AA CONTROLLER DOUG DC9 DC951 3022051 WP CABIN PRESSURE FAULTY A NWAA O OTHER O OTHER CR CRUISE 1 GL 01 670MC 47659 AT CRUISE ALTITUDE, CABIN PRESSURE BECAME UNCONTROLLABLE IN AUTO MODE. FOLLOWED COM PROCEDURE. AIRCRAFT DESCENDED TO A LOWER ALTITUDE AND CABIN PRESSURE WAS MAINTAINED WITH AUTO CONTROLLER. MADE AN UNEVENTFUL LANDING IN MKE. MAINTENANCE REPLACED NR 2 CABIN PRESSURE CONTROLLER. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2001070300016 20010703 00016 WP 2001 7 3 0102269859 1 20010624 A 2780 DUCT DOUG DC9 DC951 3022051 WP L/E SLAT GROOVED A NWAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 01 768NC 47729 DURING APPROACH INTO DTW WHEN SLATS EXTENDED, SLAT DISAGREEMENT LIGHT ILLUMINATED ACCOMPANIED WITH AIRCRAFT ROLL. WHEN SLATS RETRACTED THE LIGHT EXTINGUISHED. FOLLOWED COM PROCEDURES AND MADE AN UNEVENTFUL LANDING. MAINTENANCE FOUND THE RIGHT T-DUCT GROOVED AND LEFT WING T-DUCT WITH .1562 INCH OF PLAY. REPLACED BOTH T-DUCTS. AIRCRAFT RETURNED TO SERVICE . 2 L 7 2 4F RT A6WE 2001070300017 20010703 00017 CE 2001 7 3 0117 1 20010619 A 3242 5010614 BRAKE ASSY BEECH MU300 400A 1155402 CE LT MLG OBSTRUCTED E DJFA O OTHER E VIBRATION/BUFFET TX TAXI/GRND HDL 1 EA 23 491CW RK91 DURING TAXI AT FCI THIS AIRCRAFT EXPERIENCED A VIBRATION AND THEN THE LT BRAKE LOCKED UP. THE BRAKE WAS REMOVED AND DET ERMINED THAT A SMALL SCREW HAD WEDGED ITSELF BETWEEN THE BRAKE PADS AND THE DISC AND BROKE SEVERAL OF THE BRAKE PADS LOO SE WHICH CAUSED THE BRAKE TO LOCK UP. THIS COULD ONLY HAVE LOCKED UP DURING TAXI BECAUSE THE AIRCRAFT WAS MOVING SLOW. NEW BRAKE WAS INSTALLED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4F RT A16SW 2001070300018 20010703 00018 NM 2001 7 3 01FDEA00401 1 20010611 A 5312 BEAM BOEING 727 72722C 138400F NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 DURING ROUTINE INSP BS 1183 BULKHEAD VERTICAL BEAM AT LBL 27 FOUND CRACKED AT WL 263. *S/D* REMOVED AND REPLACED PER V ERTICAL BEAM PER IAW FEDEX EO 7-5310-7-2346 PART 2. 2 L 7 3 4F A3WE 2001070300019 20010703 00019 WP 2001 7 3 AALA20011241 1 20010605 A 5310 LONGERON DOUG DC9 DC983 3022083 WP FS 160 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 566AA 49348 TUL - FOUND LONGERON NR 3 LEFT CRACKED AT STATION 160. ERPAIRED PER SRM 53-02 WITH LONGERON SPLICE. (M) 2 L 7 2 4F RT A6WE 2001070300020 20010703 00020 WP 2001 7 3 AALA20011242 1 20010605 A 5300 LONGERON DOUG DC9 DC983 3022083 WP FS 160 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 566AA 49348 TUL - FOUND LONGERON NR 4 LEFT CRACKED AT STATION 160. REPAIRED PER SRM 53-02 WITH LONGERON SPLICE. (M) 2 L 7 2 4F RT A6WE 2001070300021 20010703 00021 NM 2001 7 3 AALA20011194 1 20010607 A 2100 6067723 FAN BOEING 757 757223 1384957 NM ACM BAY LEAKING A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 682AA 25339 DEN - FLT 119 - EN ROUTE EWR-LAX, DETECTED STRONG ELECTRICAL SMELL IN COCKPIT AND CABIN. DIVERTED DEN AND LANDED WITHOU T FURTHER INCIDENT. REPLACED RIGHT SIDE RECIRCULATION FAN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001070300022 20010703 00022 NM 2001 7 3 AALA20011197 1 20010611 A 2900 4091425 HOSE BOEING 757 757223 1384957 NM MLG RUPTURED A AALA K NONE K FLUID LOSS LD LANDING 1 SW 21 640A 24598 PHL - FLT 1463 - EN ROUTE DFW-PHX - UPON LANDING, LOST LEFT SIDE HYDRAULIC SYSTEM. LANDED PHX WITHOUT FURTHER INCIDENT. REPLACED LEFT SIDE MLG PRESSURE HOSE. SERVICED HYDRAULIC SYSTEM. LEAK CHECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPE RATION. (M) 2 L 7 2 4F RT A2NM 2001070300023 20010703 00023 WP 2001 7 3 AALA20011196 1 20010606 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP TAIL INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 496AA 49734 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT AT TAIL COMPARTMENT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONN ECTOR AT TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001070300024 20010703 00024 NM 2001 7 3 AALA20011201 1 20010604 A 5300 STRINGER BOEING 727 727223 1384074 NM AFT CARGO CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 867AA 21372 TUL - FOUND CORROSION ON STRINGER 22L AT STATION 1175. STRINGER REPAIRED SRM 53-10-03. (M) 2 L 7 3 4F A3WE 2001070300025 20010703 00025 NM 2001 7 3 AALA20011202 1 20010604 A 5300 STRINGER BOEING 727 727223 1384074 NM FS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 867AA 21372 TUL - FOUND OUTBOARD SIDE OF STRINGER 26R, CORRODED AT STATION 720D PLUS 3. INSTALLED STRINGER REPAIR SPLICE PER SRM 53 -10-3 AT STRINGER 26R STATION 720C PLUS 10 TO 720D PLUS 10. (M) 2 L 7 3 4F A3WE 2001070300026 20010703 00026 NM 2001 7 3 AALA20011203 1 20010604 A 5200 DOOR BOEING 727 727223 1384074 NM FS 380 A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 867AA 21372 TUL - FOUND EXTERIOR SKIN EDGE ON FORWARD GALLEY DOOR BLENDED BEYOND LIMITS BETWEEN UPPER AND LOWER HINGE. INSTALLED DO UBLER PER SRM 52-00-03. (M) 2 L 7 3 4F A3WE 2001070300027 20010703 00027 NM 2001 7 3 AALA20011204 1 20010601 A 5300 STRINGER BOEING 727 727223 1384074 NM FS 1010-1017 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 867AA 21372 TUL - FOUND CORROSION 2 INCHES BY 7 INCHES INSIDE STRINGER 28R STATION 1010-1017. REMOVED CORROSION AND INSTALLED STRIN GER REPAIR PER SRM 53-10-3 PAGE 3. (M) 2 L 7 3 4F A3WE 2001070300028 20010703 00028 NM 2001 7 3 AALA20011205 1 20010530 A 5300 SHEAR TIE BOEING 727 727223 1384074 NM FS 680 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 867AA 21372 TUL - FOUND SHEAR TIE CORRODED 1 INCH BY 3 INCHES AT STATION 680 STRINGER 26L. REMOVED AND REPLACED SHEAR TIE IAW MM 51 -10-1 REPLACEMENT OF PART. (M) 2 L 7 3 4F A3WE 2001070300029 20010703 00029 NM 2001 7 3 AALA20011207 1 20010530 A 5300 SHEAR TIE BOEING 727 727223 1384074 NM FS 699-701 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 867AA 21372 TUL - FOUND SHEAR TIE CORRODED STATION 699-700 BOTH SIDES 700 FRAME BETWEEN STRINGER 28R-27R. INSTALLED SHEAR TIE REPAI R AT STATION 700 STRINGER 27B-28R AS PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 2001070300030 20010703 00030 NM 2001 7 3 AALA20011208 1 20010530 A 5300 WEB BOEING 727 727223 1384074 NM FS 700 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 867AA 21372 TUL - FOUND FORWARD SIDE FRAME WEB CORRODED. INSTALLED SHEAR TIE REPAIR AT STATION 700 STRINGER 27R-28R AS PER SRM 53-1 0-4. (M) 2 L 7 3 4F A3WE 2001070300031 20010703 00031 NM 2001 7 3 AALA20011209 1 20010606 A 5300 SKIN BOEING 727 727223 1384074 NM FS 711 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 867AA 21372 TUL - FOUND BILGE SKIN CORRODED STATION 705-717, LBL 2 - RBL 2. CUT OUT CORRODED SKIN. INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 2001070300032 20010703 00032 EU 2001 7 3 AALA20011180 1 20010527 A 3350 BATTERY AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE O OTHER CR CRUISE 1 SW 21 19059 469 SJU - FLT 661 - EN ROUTE EWR-SJU - EMERGENCY EXIT FLOOR PATH LIGHT FLICKERED ON AND OFF. LANDED SJU WITHOUT FURTHER INC IDENT. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2001070300033 20010703 00033 EU 2001 7 3 AALA20011168 1 20010524 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 40064 507 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS INOPERATIVE AT SEATS 13C, 13G. RESEATED CONNECTOR FOR EMERGENCY EXIT ESCAPE LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2001070300034 20010703 00034 NM 2001 7 3 AALA20011158 1 20010518 A 5330 SKIN BOEING 727 727223 1384074 NM FS 1050-1130 A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 866AA 21371 TUL - FOUND SKIN BULGED BROKEN, PITTED, CORRODED, PUCKERED AT LONGERON 28R STATION 1050-1130. CORROSION REMOVED, DOUBLE R REPAIR INSTALLED PER SRM 53-30-3 STRINGER REPAIR INSTALLED PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 2001070300035 20010703 00035 NM 2001 7 3 AALA20011159 1 20010518 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 866AA 21371 TUL - FOUND TOP FLANGE OF FLOORBEAM CORRODED AT STATION 1070 APPROX LBL 15. INSTALLED DOUBLER PER SRM 53-10-07-02 TREAT ED AND PRIMED. (M) 2 L 7 3 4F A3WE 2001070300036 20010703 00036 NM 2001 7 3 AALA20011160 1 20010521 A 5500 SKIN BOEING 727 727223 1384074 NM LT ELEVATOR CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 866AA 21371 TUL - FOUND ELEVATOR LOWER SKIN CRACKED FORWARD SIDE OF SKIN 28 INCHES FROM INBOARD END. STOP DRILLED CRACK AND INSTALL ED DOUBLER PER SRM 55-20-3 PAGE 1 FIG 1. (M) 2 L 7 3 4F A3WE 2001070300037 20010703 00037 NM 2001 7 3 AALA20011161 1 20010524 A 5300 SKIN BOEING 727 727223 1384074 NM FS 1183 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 866AA 21371 TUL - FOUND CORROSION AT STRINGER END FITTING STATION 1183 STRINGER 27R. INSTALLED REPAIR DOUBLER PER ESO 11697 DATED 5 /24/01. (M) 2 L 7 3 4F A3WE 2001070300038 20010703 00038 NM 2001 7 3 AALA20011162 1 20010523 A 5300 WEB BOEING 727 727223 1384074 NM FS 950E CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 866AA 21371 TUL - FOUND NR 2 CARGO DOOR FUSELAGE CUT OUT, FORWARD DOOR JAMB WEB CRACKED AT BOTTOM DOOR STOP FITTING. INSTALLED DOUB LER PER S/B 727-53A0199. (M) 2 L 7 3 4F A3WE 2001070300039 20010703 00039 NM 2001 7 3 AALA20011163 1 20010517 A 5300 SHEAR TIE BOEING 727 727223 1384074 NM FS 1148 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 866AA 21371 TUL - FOUND SHEAR TIE CORRODED FORWARD OF DRAIN MAST STATION 1148 STRINGER 29L. INSTALLED NEW SHEAR TIE PER SRM 51-10-1 . (M) 2 L 7 3 4F A3WE 2001070300040 20010703 00040 NM 2001 7 3 AALA20011164 1 20010524 A 5300 STRINGER BOEING 727 727223 1384074 NM FS 1125-1130 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 866AA 21371 TUL - FOUND CORROSION ON OUTBOARD SIDE STRINGER 29R, DOUBLER BULGED BELOW STRINGER 29R. REMOVED CORROSION, INSTALLED SK IN DOUBLER AND STRINGER REPAIR PER SRM 53-30-3 AND 53-10-3. (M) 2 L 7 3 4F A3WE 2001070300041 20010703 00041 NM 2001 7 3 AALA20011146 1 20010524 A 5200 DOOR BOEING 727 727223 1384074 NM FS 380 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 866AA 21371 TUL - FOUND DOOR SKIN CRACKED, FORWARD EDGE ABOVE LOWER HINGE. ROUTED OUT CRACK, INSTALLED DOUBLER ESO 11697 DATED 5/24 /2001. (M) 2 L 7 3 4F A3WE 2001070300042 20010703 00042 WP 2001 7 3 AALA20011195 1 20010605 A 2800 6937317 PUMP DOUG DC9 DC982 3022082 WP CENTER FUEL TANK INOPERATIVE A AALA A UNSCHED LANDING J O WARNING INDICATION OTHER TO TAKEOFF 1 SW 21 7509 49803 MCI - FLT 2237 - EN ROUTE ORD-DFW - SHORTLY AFTER DEPARTURE ONE CENTER FUEL BOOST PUMP INOPERATIVE. THE SECOND CENTER F UEL BOOST PUMP ON PLACARD. DIVERTED MCI AND LANDED WITHOUT FURTHER INCIDENT. REPLACED CENTER FUEL BOOST PUMP. LEAK CH ECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001070300043 20010703 00043 WP 2001 7 3 AALA20011244 1 20010612 A 2900 FITTING DOUG DC9 DC982 3022082 WP AFT LT HYD SYS LOOSE A AALA K O NONE OTHER J O WARNING INDICATION OTHER TX TAXI/GRND HDL 1 SW 21 452AA 49553 DFW - FLT 1594 - EN ROUTE ELP-DFW - NEAR DFW GATE DETECTED SMOKE/HAZE IN CABIN. TURNED OFF PACKS. USED RAM AIR. SMOKE DISSIPATED. ARRIVED AT DFW GATE WITHOUT FURTHER INCIDENT. TIGHTENED T-FITTING AT LEFT SIDE HYDRAULIC PUMP FILTER HOUS ING NEAR APU AREA. ACCOMPLISHED PACK BURNOUT PER THE MM. LEAK CHECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. ( M) 2 L 7 2 4F A6WE 2001070300044 20010703 00044 NM 2001 7 3 P2EA01092 1 20010610 A 5700 69508091 TUBE BOEING 737 737230 NM REFUEL PANEL DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 122NJ 22120 MCI - FLT 906 - DURING WALK AROUND, FOUND THAT THE AIRCRAFT REFUELING DOOR HAD BEEN LEFT OPEN ON ITS FLIGHT FROM MSY. D AMAGE WAS CAUSED TO AN ANTI-ICE DUCT, TWO HOLD OPEN RODS AND ATTACH BRACKETS IAW BOEING MM 30-22-0, 57-30-00. (M) 2 L 7 2 4F RT A16WE 2001070300045 20010703 00045 NM 2001 7 3 AALA20011176 1 20010602 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 325AA 22326 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 36H INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT CON NECTOR AT SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001070300046 20010703 00046 NM 2001 7 3 AALA20011171 1 20010531 A 3397 WIRE BOEING 777 777223 1385213 NM CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 21 786AN 30250 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT CLOSET BROKEN. REPLACED EMERGENCY EXIT LIGHT WIRE CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001070300047 20010703 00047 NM 2001 7 3 AALA20011118 1 20010523 A 3350 S283T0143 BATTERY PACK BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 370AA 25197 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTS SEAT 2B INOPERATIVE. REPLACED BATTERY PACK AFT OF SEAT 2B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001070300048 20010703 00048 NM 2001 7 3 AALA20011169 1 20010530 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 646AA 24604 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHT INOPERATIVE SEAT 19D. RESEATED CONNECTOR FOR EMERG ENCY EXIT ESCAPE PATH LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001070300049 20010703 00049 NM 2001 7 3 AALA20011165 1 20010529 A 3350 CONNECTOR BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 770AN 29578 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTS SEAT 26 INOPERATIVE. RESEATED CONNECTOR AT SEA 26C. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001070300050 20010703 00050 WP 2001 7 3 AALA20011239 1 20010603 A 5300 SKIN DOUG DC9 DC983 3022083 WP FS 579 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 566AA 49348 TUL - FOUND DENT IN SKIN NEXT TO DOUBLER STATION 579 BETWEEN LONGERON 29L-30R. REMOVED REPAIRED DOUBLER NEXT OT DENT. INSTALLED LARGER DOUBLER OVER DENT PER ESO-80559, DATED 6/1/2001. (M) 2 L 7 2 4F RT A6WE 2001070300051 20010703 00051 WP 2001 7 3 AALA20011240 1 20010605 A 5100 BEAM DOUG DC9 DC983 3022083 WP FS 1174/1192 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 566AA 49348 TUL - FOUND CORROSION UNDER DOOR STOPS AT AFT CARGO DOOR LOWER CUTOUT. COMPLETED DOOR JAMB REPAIR PER AARD 53-10-00-3 A ND SRM 51-10-3. (M) 2 L 7 2 4F RT A6WE 2001070300052 20010703 00052 NM 2001 7 3 01FDEA00402 1 20010611 A 5320 SUPPORT BOEING 727 72722C 138400F NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 DURING ROUTINE INSP THE NR 1 SEAT TRACK SUPT AT BS 840 FOUND CRACKED. 2 L 7 3 4F A3WE 2001070300053 20010703 00053 WP 2001 7 3 ARWA0010714 1 20010629 A 5101 BRACKET LKHEED 1011 1011385115 5265015 WP A ARWA O OTHER O OTHER IN INSP/MAINT 1 SO 19 307GB 193U1131 DURING SCHEDULE MAINTENANCE. N/R 633. DISCREPANCY: EVIDENCE OF CORROSION, RIGHT WING TO FUSELAGE BRACKET AT WHEEL WELL. CORRECTIVE ACTION: REMOVED CORROSION, FILLED AREA WITH DEVCON, FABRICATED -11 DOUBLER AND INSTALLED WITH HILOCKS. PRIMED + PAINTED AS REQUIRED REFERENCE AS 11282. 2 L 7 3 4F A23WE 2001070300054 20010703 00054 WP 2001 7 3 ARWA0010709 1 20010629 A 5101 FLOOR PANEL LKHEED 1011 1011385115 5265015 WP A ARWA O OTHER O OTHER IN INSP/MAINT 1 SO 19 307GB 193U1131 DURING SCHEDULE MAINTENANCE. N/R 488. DISCREPANCY: FWD ENTRY AREA, FLOOR PANEL SUPPORT STRUCTURE IS CORRODED FROM STA 26 0 TO STA 280 AT LBL30. CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR PANEL STA260 TO 280 AT LBL 30 IAW SRM 51-40-01. 2 L 7 3 4F A23WE 2001070300055 20010703 00055 NM 2001 7 3 01FDEA00403 1 20010611 A 5541 RIB BOEING 727 72722C 138400F NM RUDDER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 DURING ROUTINE INSP LWR RUDDER, LWR THRUST HINGE RIB FOUND CRACKED AT FASTENER COMMON TO FIN REAR SPAR. *S/D* HFEC IND CRACK TERMINATED. REMOVED, REPLACED AND FAB PER IAW FEDEX DRAWING SRM 27-55-005, SRM 51-30-2. 2 L 7 3 4F A3WE 2001070300056 20010703 00056 NM 2001 7 3 01FDEA00404 1 20010611 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 DURING ROUTINE INSP FLT DECK FLOORBEAM WEB AT BS 299, LBL 6 FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB WEB PER IAW BAC 727 SRM 51-20-1, SRM 51-30-2. 2 L 7 3 4F A3WE 2001070300057 20010703 00057 WP 2001 7 3 CALA0100627 1 20010701 A 5320 WEB DOUG DC9 DC982 3022082 WP FS 336 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND FORWARD PIT(TORQUE BOX) FWD CLOSEOUT AT LIGHTENING HOLE(SLANT PANEL) CORRODED AT AND AROUND FASTENER HO LES AT FS 336. REMOVED FITTING, WEB, AND ANGLE IAW SRM 51-30-1 AND 51-30-2. A NEW WEB AND ANGLE WERE INSTALLED IAW SRM 5 1-10-4, 51-10-3, AND 51-30-2. INSTALLED FITTING IAW SRM 51-30-1. 2 L 7 2 4F A6WE 2001070300058 20010703 00058 WP 2001 7 3 CALA0100628 1 20010701 A 5230 DOUBLER DOUG DC9 DC982 3022082 WP FWD CARGO DR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND A 3" CRACK IN EXISTING DOUBLER REPAIR AT LOWER FORWARD CARGO DOOR. THE EXISTING DOUBLER WAS REMOVED AND THE CRACK WAS STOP DRILLED IAW SRM 51-10-4. A NEW DOUBLER WAS INSTALLED IAW SRM 52-33, FIGURE 1, 51-10-3, 51-10-4, AND 51-30-4. 2 L 7 2 4F A6WE 2001070300059 20010703 00059 WP 2001 7 3 CALA0100629 1 20010702 A 5230 SKIN DOUG DC9 DC982 3022082 WP AFT CARGO DR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND AFT CARGO DOOR EXTERIOR SKIN DENTED. THE SKIN WAS REPAIRED IAW SRM 52-05, PAGE 2. 2 L 7 2 4F A6WE 2001070300060 20010703 00060 EU 2001 7 3 RAIA00106016 1 20010629 A 2120 S2L226 SEAL JETAIR JETSTM JETSTM4101 1500501 EU LEFT WING DETERIORATED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 560HK 41076 7154-STL-LEFT DUCT FAIL LITE DURING TAXI.MAINTENANCE REMOVED AND REPLACED LEFT BBLEED AIR DUCT SEALS 2 L 7 2 4T RT A41NM 2001070300061 20010703 00061 NM 2001 7 3 01FDEA00405 1 20010611 A 5320 FITTING BOEING 727 72722C 138400F NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 DURING ROUTINE INSP, HFEC IND CRACK IN FASTENER HOLES IN ROW 3, LT BS 870 FITTING AT STR 9L. *S/D* HFEC IND NO CRACKS PER IAW BAC 727 NDT MANUAL PART 6. 2 L 7 3 4F A3WE 2001070300062 20010703 00062 NM 2001 7 3 01FDEA00406 1 20010611 A 5312 BULKHEAD BOEING 727 72722C 138400F NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 DURING ROUTINE INSP, HFEC IND CRACK IN BS 1183 BULKHEAD WEB AT WL 283, RBL 17.8. *S/D* REMOVED AND REPLACED PER IAW FE DEX EO 7-5310-7-5000 PARTS 3 & 5. 2 L 7 3 4F A3WE 2001070300063 20010703 00063 NM 2001 7 3 01FDEA00407 1 20010611 A 5312 BULKHEAD BOEING 727 72722C 138400F NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 DURING ROUTINE INSP, HFEC IND TWO CRACKS IN BS 1183 BULKHEAD WEB AT WL 283. *S/D* REMOVED AND REPLACED WEB PER IAW FED EX EO 7-5310-7-5000 PARTS 2 & 4. 2 L 7 3 4F A3WE 2001070300067 20010703 00067 WP 2001 7 3 IXXA0100031 1 20010315 A 5510 DOUBLER DOUG DC8 DC871F 302199D WP STABILIZSER CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 820BX 79927 2852 46065 DURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON THE RIGHT HORIZONTAL STABILIZER AFT SPAR WEB INTERNAL DOUBLER AT STATION XE 105. REPAIR ACCOMPLISHED REMOVAL OF DAMAGE AREA, FABRICATION AND INSTALLATION A NEW INTERNAL DOUBLER IN A CCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING ORDER 53-DC8-1786. 2 L 7 4 4F RT 4A25 2001070300068 20010703 00068 WP 2001 7 3 IXXA0100032 1 20010517 A 5300 WEB DOUG DC8 DC871F 302199D WP WHEEL WELL CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 820BX 79927 2852 46065 DURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON THE VERTICAL WEB IN THE RIGHT WHEEL WELL AT FUSELAGE STATION 860, RIB LINE 14. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED WEB, FABRICATION AND INSTALLATION OA NEW WEB IN ACCORDANCE WITH DOUGLAS DRAWING 5654672 AND ENGINEERING ORDER 53-DC8-1786. 2 L 7 4 4F RT 4A25 2001070300069 20010703 00069 WP 2001 7 3 IXXA0100034 1 20010328 A 5313 FITTING DOUG DC8 DC871F 302199D WP STA 8 CORRODED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 820BX 79927 2852 46065 DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON LONGERON 36 END FITTING BETWEEN FUSELAGE STATION 8 AND 10. REPAIR ACCOMPLISHED REMOVAL OF END FITTING, FABRICATION AND INSTALLATION NEW END FITTING IN ACCORDANCE WITH DOUGLAS DRAW ING 9755865 AND ENGINEERING ORDER 53-DC8-1792. 2 L 7 4 4F RT 4A25 2001070300070 20010703 00070 WP 2001 7 3 IXXA0100028 1 20010315 A 5311 FLANGE DOUG DC8 DC871F 302199D WP F.S 1380 CORRODED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 820BX 79927 2852 46065 DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON FRAME FLANGE AT FUSELAGE STATION 1380, LONGERON 35 LEFT. RE PAIR ACCOMPLISH CORROSION REMOVAL, FABRICATION AND INSTALLATION A REPAIR ANGLE IN ACCORDANCE WITH DACO STRUCTURAL REPAIR MANUAL AND ENGINEERING ORDER 51-DC8-1782. 2 L 7 4 4F RT 4A25 2001070300071 20010703 00071 WP 2001 7 3 IXXA0100035 1 20010306 A 5300 INTERCOSTAL DOUG DC8 DC871F 302199D WP STA 520 CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 820BX 79927 2852 46065 DURING ROUTINE C CHECK INSPECTION, CORROSION AND CRACKS WERE DETECTED ON INTERCOSTALS BETWEEN FUSELAGE STATION 520 AND 5 60, LONGERON 33 RIGHT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGE AREA, FABRICATION AND INSTALLATION INTERCOSTALS IN ACCORDAN CE WITH DOUGLAS DRAWING 5616520 AND ENGINEERING ORDER 53-DC8-1762. 2 L 7 4 4F RT 4A25 2001070300072 20010703 00072 WP 2001 7 3 IXXA0100029 1 20010315 A 5311 CAP DOUG DC8 DC871F 302199D WP STA 1703 GOUGED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 820BX 79927 2852 46065 DURING ROUTINE C CHECK INSPECTION, A GOUGED WAS DETECTED AT FUSELAGE STATION 1703, LONGERON 22 LEFT FUSELAGE FRAME CAP. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED CAP, FABRICATION AND INSTALLATION IN ACCORDANCE WITH DACO DRAWING 5612146 AND ENG INEERING ORDER 53-DC8-1783. 2 L 7 4 4F RT 4A25 2001070300073 20010703 00073 WP 2001 7 3 IXXA0100030 1 20010315 A 5313 FITTING DOUG DC8 DC871F 302199D WP STA 857 CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 820BX 79927 2852 46065 DURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED AT LONGERON END FITTING LOCATED AT FUSELAGE STATION 857, LONGERO N 1. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FITTING, FABRICATION AND ISTALLATION NEW END FITTING IN ACCORDANCE WITH DACO DRAWING 4750521 AND ENGINEERING ORDER 53-DC8-1784. 2 L 7 4 4F RT 4A25 2001070300077 20010703 00077 WP 2001 7 3 ABXA010321 1 20010608 A 5320 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 AFT CARGO AT FUSELAGE 1180 BETWEEN LONGERON 27 LEFT - 28 LEFT Z-FITTING WAS CRACKED. 2 L 7 4 4F 4A25 2001070300078 20010703 00078 WP 2001 7 3 ABXA010322 1 20010608 A 5330 SKIN DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 AFT CARGO AT FUSELAGE 1180 - 1220 AT LONGERON 29 LEFT SKIN WAS CORRODED UNDER AND BESIDE L-ANGLE. 2 L 7 4 4F 4A25 2001070300080 20010703 00080 WP 2001 7 3 ABXA010324 1 20010607 A 5311 FRAME DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 MAIN CABIN BETWEEN STATION 1360 TO 1347 FRAME AT STATION 1360 BETWEEN LONGERON 12 LEFT TO 5 A WAS CORRODED. 2 L 7 4 4F 4A25 2001070300081 20010703 00081 WP 2001 7 3 ABXA010325 1 20010607 A 5313 LONGERON DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 MAIN CABIN BETWEEN STATION 1120 TO 1100 LONGERON 16 LEFT WAS CORRODED. 2 L 7 4 4F 4A25 2001070300082 20010703 00082 WP 2001 7 3 ABXA010326 1 20010607 A 5311 FRAME DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 MAIN CABIN BETWEEN STATION 1180 TO 1160 FRAME 1180 AT LONGERON 4 LEFT WAS CORRODED. 2 L 7 4 4F 4A25 2001070300083 20010703 00083 WP 2001 7 3 ABXA010327 1 20010607 A 5311 FRAME DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 MAIN CABIN BETWEEN STATION 1260 TO 1240 FRAME 1260 WAS CORRODED AT CUSP. 2 L 7 4 4F 4A25 2001070300084 20010703 00084 WP 2001 7 3 ABXA010328 1 20010607 A 5311 FRAME DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 AIR COND/PRESSURIZATION COMPARTMENT AT FS 24, LONGERON 35 LEFT AND 35 RIGHT, FRAME WAS CORRODED AROUND ATTACH FASTENER T O LONGERON. 2 L 7 4 4F 4A25 2001070300085 20010703 00085 WP 2001 7 3 ABXA010329 1 20010607 A 5330 SKIN DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 AIR COND/PRESSURIZATION COMPARTMENT AT FS 36 - 54, BETWEEN LONGERON 30 LEFT - 31 LEFT, WAS CORRODED FROM UNDER FINGER DO UBLER. 2 L 7 4 4F 4A25 2001070300086 20010703 00086 WP 2001 7 3 ABXA010330 1 20010607 A 5320 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 AIR COND/PRESSURIZATION COMPARTMENT AT FS 70, LONGERON 29 LEFT, END FITTING WAS CORRODED. 2 L 7 4 4F 4A25 2001070300087 20010703 00087 WP 2001 7 3 ABXA010331 1 20010607 A 5320 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 AIR COND/PRESSURIZATION COMPARTMENT AT FS 70, BETWEEN LONGERON 30 LEFT - 31 LEFT, PRODUCTION SPLICE FITTING WAS CORRODED . 2 L 7 4 4F 4A25 2001070300088 20010703 00088 WP 2001 7 3 ABXA010332 1 20010607 A 5320 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 AIR COND/PRESSURIZATION COMPARTMENT AT FS 70, LONGERON 31 LEFT, END FITTING WAS CORRODED. 2 L 7 4 4F 4A25 2001070300089 20010703 00089 WP 2001 7 3 ABXA010333 1 20010607 A 5320 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 AIR COND/PRESSURIZATION COMPARTMENT AT FS 70, LONGERON 34 LEFT, END FITTING WAS CORRODED. 2 L 7 4 4F 4A25 2001070300090 20010703 00090 WP 2001 7 3 ABXA010334 1 20010607 A 5320 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 AIR COND/PRESSURIZATION COMPARTMENT AT FS 70, LONGERON 35 LEFT, END FITTING WAS CORRODED. 2 L 7 4 4F 4A25 2001070300091 20010703 00091 WP 2001 7 3 ABXA010335 1 20010417 A 5320 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 AFT LOWER CARGO Z-FITTING CRACKED AT STATION 1680 BETWEEN LONGERON 34 RIGHT - LONGERON 33 RIGHT. REPLACED Z-FITTING AND REPAIRED AREA IAW DC-8 SRM 51-1-20D, 53-20, 53-2-0, AND 51-1-8. 2 L 7 4 4F 4A25 2001070300092 20010703 00092 WP 2001 7 3 ABXA010336 1 20010419 A 5320 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 AFT LOWER CARGO Z-FITTING CRACKED AT STATION 1200 - LONGERON 34 RIGHT AND LONGERON 33 RIGHT. REPLACED Z-FITTING AND REP AIRED AREA IAW DC-8 SRM 51-1-20D, 53-2-0, AND 51-1-8. 2 L 7 4 4F 4A25 2001070300093 20010703 00093 WP 2001 7 3 ABXA010337 1 20010611 A 5320 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 AFT LOWER CARGO Z-FITTING CRACKED AT STATION 1180 FROM LONGERON 35 RIGHT TO LONGERON 34 RIGHT. REPLACED Z-FITTING AND R EPAIRED AREA IAW DC-8 SRM 51-1-20D, 53-2-0, 51-1-8, AND 51-1-24. 2 L 7 4 4F 4A25 2001070300094 20010703 00094 WP 2001 7 3 ABXA010338 1 20010605 A 5320 5750198 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 RIGHT WHEEL WELL LONGERON 24 BATHTUB FITTING HAD CRACK EXTENDING BEYOND ORIGINAL STOP DRILL. REPAIRED AREA IAW DC-8 SRM 53-2-2, AND 51-1-8. 2 L 7 4 4F 4A25 2001070300095 20010703 00095 WP 2001 7 3 ABXA010339 1 20010608 A 2510 LOCK DOUG DC8 DC863F 302198F WP CAPTAIN SEAT LACK OF LUBE A ABXA K NONE O OTHER UK UNKNOWN 1 GL 23 811AX 46113 CAPTAIN'S SEAT WOULD NOT REMAIN IN SELECTED POSITION. INTERMITTENTLY CAUSED SEAT TO SLIDE BACK ON TRACK. LUBRICATED CA PTAIN'S SEAT TRACKS AND LOCKING MECHANISM. SEAT NOW STAYS IN SELECTED POSITION. 2 L 7 4 4F 4A25 2001070300096 20010703 00096 WP 2001 7 3 ABXA010340 1 20010420 A 5311 564024027 FRAME DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 AFT ACCESSORY COMPARTMENT FRAME CORRODED AT FS 1620, AT LONGERON 24 LEFT. REMOVED AND REPLACED FRAME, AND REPAIRED AREA IAW DC-8 SRM 51-1-20D, 51-1-21, 51-1-8, AND ABX DWG 5640240. 2 L 7 4 4F 4A25 2001070300097 20010703 00097 WP 2001 7 3 ABXA010341 1 20010618 A 2612 FIRE WARNING DOUG DC9 DC932 3022066 WP COCKPIT FALSE ACTIVATION A ABXA B EMER. DESCENT N FALSE WARNING CR CRUISE 1 GL 23 983AX 47257 LOWER CARGO FIRE LIGHT ILLUMINATED IN FLIGHT. ESTABLISHED EMERGENCY DESCENT TO SIOUX FALLS, SD. LIGHT WENT OUT WHILE D ESCENDING. LANDED IN SIOUX FALLS WITH NO PROBLEMS. NO FIRE/SMOKE DETECTED BY SIOUX FALLS FIRE/RESCUE PERSONNEL. ABX E NGINEERING DOWNLOADED DATA FROM THE CCU. NO DISCREPANCIES NOTED. SYSTEM CHECKED GOOD IAW DC-9 MM CHAPTER 26. 2 L 7 2 4F A6WE 2001070300098 20010703 00098 WP 2001 7 3 ABXA010342 1 20010605 A 5315 99115441 FLOORBEAM DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 988AX 47084 FLOORBEAM AT STATION 275 LBL 50 HEAVILY CORRODED. REPAIRED FLOORBEAM IAW DC-9 SRM DWG K07411. 2 L 7 2 4F A6WE 2001070300100 20010703 00100 WP 2001 7 3 ABXA010347 1 20010530 A 5310 995773910 SHEAR TIE DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 RIGHT FUSELAGE FRAME SHEAR TIE AT STATION 1021 HAD CRACK AT RIVET BETWEEN LONGERON 14 AND 15 RIGHT. REPAIRED SHEAR TIE AT STATION 1021 BETWEEN LONGERON 14 RIGHT - 15 RIGHT IAW DC-9 SRM 53-03, FIGURE 3. 2 L 7 2 4F A6WE 2001070300101 20010703 00101 WP 2001 7 3 ABXA010348 1 20010530 A 5311 99118594 FRAME DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 CANTED FRAME AT STATION 1180 WAS CRACKED AT LONGERON 16 RIGHT - 19 RIGHT. REPLACED FRAME IAW DC-9 SRM. 2 L 7 2 4F A6WE 2001070300102 20010703 00102 WP 2001 7 3 ABXA010349 1 20010530 A 5310 99124494 SHEAR TIE DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 SHEAR TIE APPROXIMATELY FS 432 LONGERON 16 RIGHT CRACKED. REPLACED SHEAR TIE FS 432 LONGERON 16 RIGHT IAW DC-9 SRM. 2 L 7 2 4F A6WE 2001070300103 20010703 00103 WP 2001 7 3 ABXA010350 1 20010530 A 5330 59203233 SKIN DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 THREE EACH CRACK INDICATIONS ON FORWARD LOWER CARGO UPPER FORWARD CORNER. INSPECTION EVALUATED AND ONLY FOUND TWO CRACK S. REPAIRED FORWARD LOWER CARGO CORNER IAW DC-9 EA 53100110-001. 2 L 7 2 4F A6WE 2001070300104 20010703 00104 WP 2001 7 3 ABXA010351 1 20010530 A 5330 5911412221 SKIN DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 FOUR CRACKS AT FORWARD LOWER CARGO DOOR CUTOUT AFT LOWER CORNER. INSPECTION EVALUATED AND ONLY FOUND ONE CRACK. REPAIR ED AREA IAW DC-9 EA 53100113-001 AND REA D953-41279-MR. 2 L 7 2 4F A6WE 2001070300105 20010703 00105 WP 2001 7 3 ABXA010352 1 20010621 A 2612 FIRE WARNING DOUG DC9 DC941 302207N WP COCKPIT FALSE ACTIVATION A ABXA K NONE N FALSE WARNING IN INSP/MAINT 1 GL 23 975AX 47512 CREW REPORTED LOWER CARGO FIRE WARNING AT ILN ON GROUND. CFR WAS DISPATCHED TO AIRCRAFT. CFR REPORTED NO FIRES. NO DE FECTS NOTED. SYSTEM CHECKED GOOD IAW DC-9 MM 26. 2 L 7 2 4F A6WE 2001070300106 20010703 00106 WP 2001 7 3 ABXA010355 1 20010626 A 5610 WINDOW DOUG DC8 DC863 302198A WP COCKPIT OBSTRUCTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 FIRST OFFICER'S SLIDING WINDOW WOULD NOT OPEN. FOUND AFT LOWER LOCK ON FIRST OFFICER'S WINDOW OBSTRUCTED BY SEALANT. R EMOVED SEALANT. WINDOW OPERATED NORMAL. 2 L 7 4 4F 4A25 2001070300107 20010703 00107 WP 2001 7 3 ABXA010356 1 20010320 A 5330 DOUBLER DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 AFT LOWER CARGO AT STATION 1040 - 1060.0 BETWEEN LONGERON 31 LEFT TO LONGERON 31 RIGHT CIRCUMFERENTIAL SPLICE TEAR STRAP AND FINGER DOUBLER HAD CORROSION BETWEEN SKIN TEAR STRAP AND FINGER DOUBLER. REPAIRED AREA AND REPLACED TEAR STRAP, LO NGERON SPLICES, INTERCOSTALS, TIE DOWNS, AND PANEL SUPPORTS IAW DC-8 SRM 51-1-20D, 51-1-21, 51-1-8, 53-2-0, AND DAC DWG 5750322. 2 L 7 4 4F 4A25 2001070300108 20010703 00108 NE 2001 7 3 ABXA010357 2 20010418 A 7220 633683 CASE DOUG DC8 DC863 302198A WP PWA JT3D JT3D7 52039 NE NR 4 ENGINE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 669191 NR 4 ENGINE INLET GUIDE VANE CASE HAD NUMEROUS CRACKS AT WELDS. WELDED CRACKS ON INLET CASE IAW P&W OVERHAUL MANUAL 72- 21-1. 2 L 7 4 4F 4 F 4A25 1E8 2001070300109 20010703 00109 WP 2001 7 3 ABXA010358 1 20010626 A 2170 COALESCER BAG DOUG DC9 DC933F 302207A WP A/C BAY DIRTY A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 23 932AX 47465 THERE WAS AN OIL SMELL COMING FROM BOTH A/C PACKS. CLEANED RIGHT COALESCER FILTER AND REPLACED THE LEFT COALESCER FILTE R IAW DC-9 MM 21-20-02. 2 L 7 2 4F A6WE 2001070300110 20010703 00110 NM 2001 7 3 ABXA010359 1 20010626 A 3610 ISOLATION VALVE BOEING 767 767281 1385109 NM BLEED AIR MALFUNCTIONED A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 787AX 23020 DURING CLIMBOUT OF KDAL, THERE WAS A BAD OIL ODOR. DISSIPATED AT HIGH ALTITUDE AND WHEN RIGHT PACK WAS TURNED OFF. PAS SING 13,000 FEET, ODOR RETURNED. CREW DONNED OXYGEN MASKS DUE TO ODOR. CHECKED NR 1 AND NR 2 INLETS AND EXHAUST, NR 1 AND NR 2 ENGINE 8TH AND 14TH STAGE OUTLET DUCTS. REPLACED RIGHT ISOLATION VALVE. CHECKED LEFT AND RIGHT ACM TURBINE OU TLET DUCTS. NO DEFECTS NOTED ON NR 1 OR NR 2 ENGINES. COMPLIED WITH ENGINE RUN, NR 1 AND NR 2 AT VARIOUS POWERS AND PN EUMATIC SETTINGS WITH NO ABNORMAL ODORS NOTED IAW B767 MM 71-00. 2 L 7 2 4F RT A1NM 2001070300111 20010703 00111 WP 2001 7 3 ABXA010360 1 20010626 A 3350 5708458503 BATTERY PACK DOUG DC8 DC861 3021952 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 850AX 45894 DURING MAINTENANCE PRE-DEPARTURE CHECK, FOUND BATTERY EMERGENCY LIGHT PACK FAILED TO ILLUMINATE LIGHTS. REPLACED EMERGE NCY LIGHT RACK ASSEMBLY IAW DC-8 MM 33-50-01-2. OPS CHECKED GOOD. NO OTHER DEFECTS NOTED. 2 L 7 4 4F 4A25 2001070300112 20010703 00112 NM 2001 7 3 AWXA0001914 1 20010701 A 5320 6545833640 WEB BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 CRACK IN COCKPIT FLOOR WEB BS 178-180 WL 207 LBL 24. REMOVED AND REPLACED WEB IAW B737-300 SRM 51-40-02 PG 6 & 38 AND 5 1-40-05 PG 1 - 10 2 L 7 2 4F RT A16WE 2001070300113 20010703 00113 NM 2001 7 3 AWXA0001915 1 20010701 A 5312 651630010 ANGLE BOEING 737 7373G7 1384595 NM ANGLE/ 178 BLKHD CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 D: Approx 1" crack on horizon angle Aft side of Bulkhead B.S. 178 W/195 RBL 9.5-10.5C: Removed and replaced cracked angl e IAW B737 SRM 51-40-02 pg 3 & 38 2 L 7 2 4F RT A16WE 2001070300114 20010703 00114 WP 2001 7 3 ABXA010361 1 20010627 A 2910 HYDRAULIC LINE DOUG DC8 DC861 3021952 WP HYD SYSTEM LEAKING A ABXA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 852AX 46016 AFTER 1.5 HOURS OF FLIGHT, EXPERIENCED LOSS OF HYDRAULICS. PRESSURE DROPPED TO ZERO ACCOMPANIED BY AILERON AND RUDDER C ONTROL MANUAL LIGHTS. ISOLATED SYSTEM PRIOR TO QUANTITY REACHING STANDPIPE LEVEL. FOUND NR 3 ENGINE HYDRAULIC PRESSURE LINE LEAKING NEAR HYDRAULIC PUMP. REPLACED PRESSURE LINE, SERVICED MAIN HYDRAULIC RESERVOIR AND OPERATIONALLY CHECKED NR 2 AND NR 3 ENGINES AND AUX PUMPS. OPS CHECKED GOOD. NO LEAKS NOTED. 2 L 7 4 4F 4A25 2001070300115 20010703 00115 NM 2001 7 3 AWXA0001818 1 20010604 A 5720 69378948 ANGLE BOEING 737 737277 1384570 NM RT WING CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 RT WING - SUSPECTED CRACK ON ANGLE RADIUS AT I/B SIDE OF ENGINE TOWER SHAFT ACCESS PANEL CUTOUT JUST FWD OF WING FRONT S PAR. FORMER P/N 69-37894-8 AT STA 226.47 CRACK REPAIRED IAW ER 15-6740-01137-JS4 AND REF DWG 65-49535 AND SRM 51-30-2 P G 2-5; NDT CONFIRMED CRACK IAW NDTM PT 6 51-00-00 FIG 23. 2 L 7 2 4F RT A16WE 2001070300116 20010703 00116 CE 2001 7 3 GLBA2001132 1 20010624 A 2130 1274400501 SEAL BEECH 1900 1900D 1154162 CE A GLBA D RETURN TO BLOCK O OTHER CL CLIMB 1 CE 01 254GL UE254 WILL NOT HOLD PRESSURIZATION, INSPECT FOUND CARGO DOOR SEAL TORN, REPLACED OPS CHECK SATISFACTORY 2 L 7 2 4T RT A24CE 2001070300117 20010703 00117 SO 2001 7 3 GLBA2001131 1 20010617 A 2120 832481 O-RING EMB 120 EMB120ER 3260203 SO A GLBA D RETURN TO BLOCK O OTHER CL CLIMB 1 CE 01 297UX 120297 LEFT ENGINE DUCT LEAK, INSPECTED FOUND PEUMATIC LINE LEAKING, REPLACE O-RING OPS CHECKED SYSTEM SATISFACTORY 2 L 7 2 4T RT A31SO 2001070300118 20010703 00118 CE 2001 7 3 GLBA2001125 1 20010611 A 2120 1299700321 LINE BEECH 1900 1900D 1154162 CE A GLBA D RETURN TO BLOCK O OTHER CL CLIMB 1 CE 01 101UX UE101 RIGHT BLEED AIR FAILURE AFTER T/O, REPLACED PEUMATIC LINE ON R/H SHUTOFF VALVE 2 L 7 2 4T RT A24CE 2001080700435 20010807 00435 NE 2001 8 7 MALA010536 2 20010618 A 7200 ENGINE BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 2 MALFUNCTIONED A MALA A UNSCHED LANDING J Y WARNING INDICATION ENGINE STOPPAGE CR CRUISE 1 GL 15 529XJ E2363 NR 2 ENGINE N1 WENT TO 103 PERCENT FADEC LIGHT ILLUMINATED THEN AUTO-SHUTDOWN. AC WAS SCHEDULED TO FLY MSP-PIT, DIVERTE D TO RST MINNESOTA. LANDED WITHOUT INCIDENT. NR 2 ENGINE FAILED. (NO FIRE) N1 WENT TO 103 PERCENT, FADEC LIGHT ILLUMIN ATED, N1 DROPPED, OIL PRESSURE LT. ILLUMINATED CONDUCTED SHUTDOWN/FAIL CHECKLIST. MAINTENANCE INSPECTED AC FOUND OK FOR 1 TIME FERRY FLIGHT FROM RST TO MSP. INSTALLED NR 2 HYDRAULIC PUMP P/N 521449 S/N MX634958. 2 H 7 4 4F 4 F RT A49EU E6NE 2001070300119 20010703 00119 NM 2001 7 3 AWXA0001857 1 20010615 A 5311 6516300302 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 305AW 24012 BS 178 BLKHD RT SIDE CHORD CRACKED AT CENTER OF RADIUS, AFT SIDE WL 207 CONFIRMED HFEC. REPAIRED IAW SRM 51-40-02 PG 2& 10. 2 L 7 2 4F RT A16WE 2001070300120 20010703 00120 NM 2001 7 3 AWXA0001858 1 20010615 A 5311 6516300301 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 305AW 24012 BS 178 BLKHD LT SIDE CHORD CRACKED AT CENTER OF RADIUS, AFT SIDE WL 207 CONFIRMED HFEC. REMOVED AND REPLACED CHORD IAW B737-300 SRM 51-40-02 PG 2&10. 2 L 7 2 4F RT A16WE 2001070300121 20010703 00121 NM 2001 7 3 AWXA0001865 1 20010615 A 5330 654577567 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 305AW 24012 FUSELAGE DENT 2 INCH AFT OF CARGO DOOR 13 INCHES LONG, 3 INCHES WIDE , 250 DEEP, 20 INCHES AFT CARGO DOOR. TRIMMED DAM AGED AREA, FABBED -1, -2, -3, -4 FILLER INSTALLED -1, -2, -3, -4 FILLERS AND DOUBLER IAW ER 03-5331-01150-DL1. 2 L 7 2 4F RT A16WE 2001070300122 20010703 00122 NM 2001 7 3 AWXA0001867 1 20010615 A 5754 65464307 SKIN BOEING 737 7373G7 1384595 NM L/E FLAP DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 305AW 24012 LEFT I/B FORE FLAP SKIN 61.5 INCH FROM O/B END. REPAIR NOT ACCOMPLISHED PER SRM 51-70-10. REPAIRED I/B LEFT FORE FLAP SKIN WITH PERMANENT REPAIR IAW B737-300 SRM 51-70-10 PG 88C, 88D, 88E. 2 L 7 2 4F RT A16WE 2001070300123 20010703 00123 NM 2001 7 3 AWXA0001868 1 20010615 A 5753 BAC15201370 PANEL BOEING 737 7373G7 1384595 NM T/E FLAP DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 305AW 54012 LEFT I/B MIDFLAP T/E PANEL 7220 41.25 INCHES FROM O/B END NOT REPAIRED PER 737 SRM 51-70-10 PGS 68-69. INSTALLED PERMAN ENT REPAIR ON LEFT I/B MIDFLAP T/E PANEL IAW B737 SRM 51-70-10 PG 68-69. 2 L 7 2 4F RT A16WE 2001070300124 20010703 00124 NM 2001 7 3 AWXA0001869 1 20010615 A 5310 651758351 TEE CHORD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 305AW 24012 AFT SIDE OF BS 178 BULKHEAD BELOW FLOOR TEE CHORD CRACKED LBL 5.7, WL 185, I/B SIDE. REPAIRED TEE CHORD AFT SIDE OF BUL KHEAD BS 178 LBL 5.7 WL 185 IAW B737-300 SRM PAGES 221-240. 2 L 7 2 4F RT A16WE 2001070300125 20010703 00125 NM 2001 7 3 AWXA0001870 1 20010615 A 5753 BAC5201370 STRAP BOEING 737 7373G7 1384595 NM T/E FLAP DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 305AW 24012 LEFT I/B MIDFLAP T/E PANEL 7220 CHAFE STRIP NOT INSTALLED PER SRM 51-70-10. REMOVED OLD CHAFE STRIP, ALODINED MATING SU RFACE AND APPLIED PRIMER IAW B737-300 SRM 51-20-01 PAGES 9 & 10 AND 51-70-09 PG 26 & 27. INSTALLED NEW RUB STRIP IAW B7 37 MM 51-51-00 PG 805 & 806. 2 L 7 2 4F RT A16WE 2001070300126 20010703 00126 NM 2001 7 3 AWXA0001871 1 20010615 A 5753 BAC15201370 PANEL BOEING 737 7373G7 1384595 NM T/E FLAP DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 305AW 24012 LEFT I/B MID FLAP T/E PANEL 7220L HOT BOND REPAIR 13.75 FROM OUTBOUND EDGE NOT ACCOMPLISHED PER SRM. REMOVED REPAIR AND INSTALLED PERMANENT REPAIR IAW B737-300 SRM 51-70-10 PG 88C, 88D, 88E ON LT INBOUND MID FLAP T/E PANEL 7220L. 2 L 7 2 4F RT A16WE 2001070300127 20010703 00127 NM 2001 7 3 AWXA0001874 1 20010615 A 5754 65464307 SKIN BOEING 737 7373G7 1384595 NM L/E FLAP DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 305AW 24012 LEFT INBOUND FOREFLAP LOWER SKIN 15 INBOUND OF O/B END REPAIR NOT ACCOMPLISHED PER SRM 51-70-10. REMOVED REPAIR ON LT I NBOUND FOREFLAP LOWER SKIN 15 INCHES INBOUND OF O/B END AND INST PERMANENT REPAIR IAW B737-300 SRM 51-70-10 PAGE 88C, 88 D, 88E. 2 L 7 2 4F RT A16WE 2001070300128 20010703 00128 EU 2001 7 3 2001F00041 1 20010523 A 2613 1734362450 SENSOR SAAB SF340 340B 7860101 EU TAIL PIPE FAULTY A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 345SB 340B345 ALB - FLT 5092 - RIGHT TAIL PIPE HOT LIGHT. REMOVED AND REPLACED CONVERTER AND TAIL PIPE SENSORS IAW AMM. OPS CHECK GO OD. REF SIMA200114314. (M) 2 L 7 2 4T RT A52EU 2001070300129 20010703 00129 2001 7 3 2001F00042 4 20010519 A 3418 0020BM4 COMPUTER EMB 135 EMB135LR SO STALL WARNING INOPERATIVE A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 737MW 145396 GSO - FLT 4020 - DURING CLIMB, CREW REPORTED THE SPS 1 FAIL INTERMITTENTLY. CREW THEN RECEIVED AN SPS ADVANCE MESSAGE A N AT THAT POINT BOTH FAIL MESSAGES STAYED ON. CREW FOLLOWED AOM PROCEDURES AND RETURNED TO FIELD. EMERGENCY WAS DECLAR ED AND AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED THE AOA VANE AND THE STALL PROTE CTION COMPUTER IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001070300130 20010703 00130 EU 2001 7 3 2001F00043 1 20010521 A 5347 7253799379 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 347SB 340B347 ABI - DURING MBV INSPECTION MAINTENANCE, FOUND SEAT TRACK BL 0 AT STATION 297 TO 328.5 CORRODED BEYOND LIMITS. SEAT TRA CK WAS REPAIRED IAW SAAB SRM. REF SIMA20011439. (M) 2 L 7 2 4T RT A52EU 2001070300131 20010703 00131 EU 2001 7 3 2001F00044 1 20010521 A 5347 7253799379 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 347SB 340B347 ABI - DURING MBV INSPECTION MAINTENANCE, FOUND SEAT TRACK BL 0 CORRODED FROM STATIONS 619 TO 688.88. MAINTENANCE REPAIR ED SEAT TRACK IAW SAAB SRM. REF SIMA20011438. (M) 2 L 7 2 4T RT A52EU 2001070300132 20010703 00132 EU 2001 7 3 2001F00045 1 20010521 A 5347 7253799379 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 347SB 340B347 ABI - DURING MBV INSPECTION, MAINTENANCE FOUND CORROSION ON SEAT TRACK AT BL 18.3L AT FS 297 OUT OF SRM LIMITS. SEAT TR ACK WAS REPAIRED IAW SAAB SRM. REF SIMA20011437. (M) 2 L 7 2 4T RT A52EU 2001070300133 20010703 00133 EU 2001 7 3 2001F00049 1 20010601 A 2422 WEF271500 INVERTER FOKKER F27 F27MK600 4990706 EU NR 1 FAILED A COEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 13 701FE 10419 DEPARTED LAS VEGAS EN ROUTE TO OAK - FLT 7709 - SHORTLY, AFTER TAKEOFF, THE NR 1 INVERTER FAILED. THE FLIGHT CREW DECLA RED AN INFLIGHT EMERGENCY AND RETURNED TO LAS. MAINTENANCE WAS DISPATCHED AND REPLACED THE NR 1 INVERTER. THE AIRCRAFT WAS RETURNED TO SERVICE AND DEPARTED LAS AT APPROX 0525Z. (M) 2 H 7 2 4T A817 2001070300134 20010703 00134 NM 2001 7 3 2001F00050 1 20010603 A 3397 WIRE BOEING 757 75723A 1384967 NM CABIN CUT A K NONE L NO TEST IN INSP/MAINT 1 WP 19 757NA 24567 FOUND FLOOR PROXIMITY EMERGENCY ESCAPE PATH LIGHT AT ROW 18 INOPERATIVE, WIRES CUT AT LIGHT. SPLICED WIRES AND RESTOWED CORRECTLY. (M) 2 L 7 2 4F RT A2NM 2001070300135 20010703 00135 NM 2001 7 3 2001F00051 1 20010608 A 3350 20131A BATTERY PACK BOEING 757 757236 NM CABIN DISCHARGED A N8TA K NONE L NO TEST IN INSP/MAINT 1 WP 19 521NA 25592 FOUND EMERGENCY LIGHTS AT ROWS 27 AND 29 INOPERATIVE. DURING TROUBLESHOOTING FOUND BATTERY PACK AT DOOR R3 WITH LOW VOL TAGE. REPLACED BATTERY PACKS AT AFT GALLEY RIGHT AND DOOR R3, SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A2NM 2001070300136 20010703 00136 EU 2001 7 3 2001F00052 1 20010510 A 5320 7253721447 ANGLE SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 280AE 340B280 SBP - DURING MBV INSPECTION, FOUND THE INTERCOSTAL AND REINFORCEMENT ANGLE UNDER FORWARD EDGE OF LEFT GALLEY HAS CORRODE D AREAS. REMOVED AND REPLACED INTERCOSTAL AND ANGLE IAW SAAB SRM 51-40-21. REF SIMA20011318. (M) 2 L 7 2 4T RT A52EU 2001070300137 20010703 00137 EU 2001 7 3 2001F00053 1 20010524 A 5320 S5367121729801 TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 DURING MBV-1 INSPECTION, MAINTENANCE REPORTED THE SERVICE DOOR SILL PLATE AND DRAIN TRACK CORRODED BETWEEN FRAMES 36 AND 39. MAINTENANCE REMOVED AND REPLACED THE DRAIN TRACK IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200 114402. (M) 2 H 7 2 4T RT A53EU 2001070300138 20010703 00138 EU 2001 7 3 2001F00054 1 20010524 A 5347 S53678001226 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 340B270 SAW - DURING MBV-1 INSPECTION MAINTENANCE REPORTED RIGHT AFT INBOARD AND LEFT AFT INBOARD SEAT TRACKS CORRODED. MAINTEN ANCE REMOVED AND REPLACED SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200114403. (M) 2 H 7 2 4T RT A53EU 2001070300139 20010703 00139 EU 2001 7 3 2001F00055 1 20010522 A 2560 P2070003 FLASHLIGHT AEROSP ATR72 ATR72212A 8680902 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 499AT 499 DFW - FLT 3760 - FLIGHT ATTENDANT REPORTED THE FORWARD CABIN EMERGENCY FLASHLIGHT IS INOPERATIVE. FLASHLIGHT PUT ON MEL AT THIS TIMES. MAINTENANCE REPLACED THE FLIGHT ATTENDANTS FLASHLIGHT AND RESTORED MEL. AIRCRAFT WAS RETURNED TO SERVI CE. REF SIMA20011425. (M) 2 H 7 2 4T RT A53EU 2001070300140 20010703 00140 NE 2001 7 3 2001F00056 2 20010519 A 7321 8201541001 EEC AEROSP ATR72 ATR72212A 8680902 EU PWA PW120 PW127 NE RT ENGINE FAULTY A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 545AT 545 DFW - FLT 3503 - WHILE IN CILMB-OUT FROM DFW, THE NR 2 PROPELLER SINGLE CHANNEL PE FAULT LIGHT ILLUMINATED WITH AN ASSOC IATED TORQUE SURGE. THE AIRCRAFT WAS RETURNED TO DFW DUE TO CONTINUOUS SURGING FROM THE PROPELLER. THE AIRCRAFT WAS RE TURNED WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE PROPELLER ELECTRONIC CONTROL AND THE EN GINE ELECTRONIC CONTROL IAW ATR MM. OPS CHECK WAS GOOD AND AIRCRAFT WS RELEASED FOR A FUNCTIONAL CHECK FLIGHT. FCF WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20011393. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 2001070300141 20010703 00141 EU 2001 7 3 2001F00057 1 20010509 A 5753 S5751211120400 GUIDE AEROSP ATR72 ATR72212 EU T/E FLAP CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 SAW - DURING MBV-1 INSPECTION MAINTENANCE FOUND THE LEFT OUTBOARD FLAP NR 5 CAM GUIDE CORRODED, AND THE LEFT INBOARD FLA P NR 3 CAM GUIDE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CAM GUIDES IAW CMM 57-53-11. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20011432. (M) 2 H 7 2 4T RT A53EU 2001070300142 20010703 00142 EU 2001 7 3 2001F00058 1 20010510 A 5315 S5367240921801 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAM 38 AND 40 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAMS IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20011433. (M) 2 H 7 2 4T RT A53EU 2001070300143 20010703 00143 EU 2001 7 3 2001F00059 1 20010510 A 5320 S5367800826901 FLOOR SUPPORT AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE RIGHT FLOOR SUPPORT BETWEEN FRAMES 36 AND 38 CORRODED, AND RIGHT FLOOR SUPPORT BETWEEN FRAMES 38 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORTS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20011434. (M) 2 H 7 2 4T RT A53EU 2001070300144 20010703 00144 EU 2001 7 3 2001F00060 1 20010510 A 5320 S5367800822251 FLOOR SUPPORT AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE LEFT FLOOR SUPPORT BETWEEN FRAMES 38 AND 39 CORRODED, AND LEFT F LOOR SUPPORT BETWEEN FRAMES 39 AND 40 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORTS IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20011435. (M) 2 H 7 2 4T RT A53EU 2001070300145 20010703 00145 EU 2001 7 3 2001F00061 1 20010510 A 5320 S5367800821602 FITTING AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE FOUND THE LEFT AFT ZEE MEMBER BETWEEN FRAMES 39 AND 40 CORRODED, AND THE RIG HT AFT ZEE MEMBER BETWEEN FRAMES 39 AND 41 CORRODED. MAINTENANCE REMOVED AND REPLACED BOTH ZEE MEMBERS IAW SRM 53-25-04 . AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20011436. (M) 2 H 7 2 4T RT A53EU 2001070300146 20010703 00146 2001 7 3 2001F00065 4 20010524 A 3421 258733511 GYRO BOEING 737 7372X6C 1384552 NM E/E BAY MALFUNCTIONED A TSAA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 13 816AL 23122 FLT 96 - HNL-KOA - WHILE CLIMBING THROUGH 6000 FEET, FLIGHT CREW REPORTED A PROBLEM WITH THE FIRST OFFICER'S ADI TO MAIN TENANCE CONTROL. MAINTENANCE CONTROL ADVISED THE CREW TO RETURN TO HNL FOR REPAIRS. LANDING WAS ACCOMPLISHED WITH NO F URTHER PROBLEMS. MAINTENANCE REPLACED THE F/O'S ADI AND THE NR 2 VERTICAL GYRO. GROUND OPS CHECK OF THE ATTITUDE SYSTE M TESTED GOOD. AIRCRAFT RETURNED TO SERVICE. REF TSAA0134064. (M) 2 L 7 2 4F RT A16WE 2001070300147 20010703 00147 2001 7 3 2001F00066 4 20010609 A 3442 MI585161 TRANSMITTER BOEING 737 7372L9 1384497 NM WEATHER RADAR INOPERATIVE A SOKF A UNSCHED LANDING O OTHER CL CLIMB 1 SO 23 281LF 59 22071 SJO - FLT 610 - DURING TAKEOFF, THE CAPTAIN REPORTED RADAR INOPERATIVE. THE AIRCRAFT RETURNED TO SJO STATION FOR MAINTE NANCE. AFTER LANDING MAINTENANCE PERSONNEL REMOVED AND REPLACED THE WEATHER RADAR TRANSMITTER, ACCORDING TO AMM 34-41-0 0. PERFORMED OPERATIONAL TEST ACCORDING TO AMM 34-41-00 PAGE 501, RESULT WERE SATISFACTORY. THE AIRCRAFT RETURNED TO S ERVICE. (M) 2 L 7 2 4F RT A16WE 2001070300148 20010703 00148 2001 7 3 2001F00073 4 20010616 A 3421 H321BHM1 INDICATOR AIRBUS 320 A320233 EU COCKPIT FAILED A SOKF A UNSCHED LANDING O OTHER CR CRUISE 1 SO 23 951LR 460 LIM - FLT 641 - DURING FLIGHT, WHILE AIRCRAFT TURNED, STANDBY HORIZON TILTED 22 DEGREES RIGHT BANK. AFTER TURN, THE IND ICATOR DID NOT RECOVER, IT REMAINED IN THAT POSITION, AND NO FLAG APPEARED. AIRCRAFT RETURNED TO LIMA AIRPORT. AFTER L ANDING, MAINTENANCE TECHNICIANS PERFORMED INSPECTION OF THE INDICATOR AND FOUND THE INDICATOR STUCK IN POSITION (BANKED) . THE DEFECTIVE INDICATOR WAS REPLACED ACCORDING TO AMM TASK 34-22-24-000-00100. THE INDICATOR WAS TESTED ACCORDING TO AMM AIRCRAFT 34-22-24-400-00100/ 33-13-00-710-001 WITH SATISFACTORY RESULTS. AIRCRAFT RETURNED TO NORMAL OPERATION. ( M) 2 L 7 2 4F RT A28NM 2001070300149 20010703 00149 NM 2001 7 3 2001F00074 1 20010620 A 2750 FLAP BOEING 737 737230 NM WING MALFUNCTIONED A RJEF A UNSCHED LANDING O OTHER CL CLIMB 1 SO 23 261LR 22402 SAL - FLT 441 - AFTER TAKEOFF, WHEN PILOT SELECTED FLAP TO UP POSITION, IT DID NOT RESPOND. ALTERNATE FLAP EXTENSION WA S PERFORMED FOR LANDING. THE AIRCRAFT RETURNED TO THE EL SALVADOR AIRPORT. THE AIRCRAFT REMAINED ON GROUND FOR MAINTEN ANCE. (M) 2 L 7 2 4F RT A16WE 2001070300150 20010703 00150 NM 2001 7 3 GAIA01191ST 1 20010611 A 5320 STIFFENER BOEING 727 727251 138408H NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT HORIZONTAL STIFFENER EXFOLIATED ON TOP OF NOSE WHEEL WELL BS 302 RBL 12-LBL 12 WL 181. ACCOMPLISHED HORIZONTAL STIFFENER REPLACEMENT BS 302 WL 181 LBL 12 - RBL 12 IAW B727 SRM 5 3-10-2 FIG 2 AND 51-30-2, 51-30-9. FASI NON ROUTINE 06653. (M) 2 L 7 3 4F A3WE 2001070300151 20010703 00151 NM 2001 7 3 GAIA01192ST 1 20010611 A 5311 FRAME BOEING 727 727251 138408H NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT CORROSION ON LEFT 1070 FRAME INBOARD CHORD AT STRINGER 10L. ACCOMPLISHE D FUSELAGE FRAME REPAIR BS 1070 STRINGER 10L IAW B727 SRM 53-10-4 FIG 2. (M) 2 L 7 3 4F A3WE 2001070300152 20010703 00152 NM 2001 7 3 GAIA01199ST 1 20010611 A 5320 WEB BOEING 727 727251 138408H NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT SHEAR WEB DENTED AT BS 1153 LBL 25 WL 208. ACCOMPLISHED SHEAR WEB REPAI R BS 1153 LBL 25 WL 208 IAW B727 SRM 51-40-2 FIG 1. (M) 2 L 7 3 4F A3WE 2001070300153 20010703 00153 NM 2001 7 3 GAIA01200ST 1 20010611 A 5210 SKIN BOEING 727 727251 138408H NM L1 DOOR CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT L1 DOOR SKIN CRACKED AT LOWER HINGE CUT OUT. ACCOMPLISHED L1 DOOR EXTER NAL SKIN REPAIR IAW B727 SRM 52-03-00 FIG 3. (M) 2 L 7 3 4F A3WE 2001070300154 20010703 00154 NM 2001 7 3 GAIA01203ST 1 20010611 A 5242 SKIN BOEING 727 727251 138408H NM E/E DOOR CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT CORROSION ON THE MAIN ELECTRONIC COMPARTMENT DOOR SKIN BS 420-440 STRING ER 28L-28R. ACCOMPLISHED E/E DOOR EXTERNAL SKIN REPLACEMENT IAW B727 SRM 52-40-1 FIG 2 AND 51-30-2. (M) 2 L 7 3 4F A3WE 2001070300155 20010703 00155 NM 2001 7 3 GAIA01206ST 1 20010611 A 5330 SKIN BOEING 727 727251 138408H NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT A CRACK IN FUSELAGE SKIN BS 300 STRINGER 17R AT FASTENER VERIFIED BY HFE C. ACCOMPLISHED FUSELAGE SKIN REPAIR BS 300 STRINGER 17R IAW B727 SRM 53-30-3 FIG 3. (M) 2 L 7 3 4F A3WE 2001070300156 20010703 00156 NM 2001 7 3 GAIA01207ST 1 20010611 A 5312 PRESSURE PANEL BOEING 727 727251 138408H NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT A CRACK IN THE UPPER SKIN IN THE NOSE WHEEL WELL BS 287-292 BBL 0 WL 200 . ACCOMPLISHED NOSE WHEEL WELL UPPER SKIN REPAIR BS 287-292 BBL 0 WL 200 IAW B727 SRM 51-40-2 FIG 1. (M) 2 L 7 3 4F A3WE 2001070300157 20010703 00157 NM 2001 7 3 GAIA01208ST 1 20010611 A 5522 SKIN BOEING 727 727251 138408H NM ELEVATOR CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE LEFT ELEVATOR INBOARD TRAILING EDGE STATIC DISCHARGER CORROSION BETW EEN BASE AND ELEVATOR SKIN. ACCOMPLISHED LEFT ELEVATOR UPPER SKIN REPAIR ELEVATOR STATION 209.96 IAW B727 SRM 55-20-3 F IG 3. (M) 2 L 7 3 4F A3WE 2001070300158 20010703 00158 NM 2001 7 3 TSAA0133051 1 20010511 A 3350 900542 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED AFT CENTER CEILING EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVIC E. (M) 2 L 7 2 4F A16WE 2001070300159 20010703 00159 NM 2001 7 3 TSAA0133052 1 20010511 A 3350 86210066 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED NR 6 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001070300160 20010703 00160 2001 7 3 TSAA0134064 4 20010524 A 3425 7725005005 ADI BOEING 737 7372X6C 1384552 NM COCKPIT MALFUNCTIONED A TSAA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 13 816AL 23122 FLT 96 - HNL-KOA - WHILE CLIMBING THROUGH 6000 FEET, FLIGHT CREW REPORTED A PROBLEM WITH THE FIRST OFFICER'S ADI TO MAIN TENANCE CONTROL. MAINTENANCE CONTROL ADVISED THE CREW TO RETURN TO HNL FOR REPAIRS. LANDING WAS ACCOMPLISHED WITH NO F URTHER PROBLEMS. MAINTENANCE REPLACED THE F/O'S ADI AND THE NR 2 VERTICAL GYRO. GROUND OPS CHECK OF THE ATTITUDE SYSTE M TESTED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001070300161 20010703 00161 NM 2001 7 3 TSAA0153057 1 20010508 A 5330 86210066 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 817AL 23292 FUSELAGE SKIN WRINKLE BETWEEN BS 663.75 AND BS 706, S13 AND S16. (M) 2 L 7 2 4F RT A16WE 2001070300162 20010703 00162 NM 2001 7 3 TSAA0153058 1 20010508 A 5330 6546544 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 817AL 23292 FOUND FUSELAGE SKIN WRINKLE BETWEEN BS 663.75 AND BS 706, S13L AND S16L. (M) 2 L 7 2 4F RT A16WE 2001070300163 20010703 00163 NM 2001 7 3 TSAA0153059 1 20010507 A 5311 86210066 FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 817AL 23292 FUSELAGE BS 727, STRINGER 18A LEFT OUTBOARD CHORD DETECTED CRACK BY METHOD OF HFEC INSPECTION. (M) 2 L 7 2 4F RT A16WE 2001070300164 20010703 00164 NM 2001 7 3 TSAA0153060 1 20010507 A 5311 65C372772 FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 817AL 23292 FOUND FUSELAGE BS 727, STRINGER 18A RIGHT OUTBOARD CHORD DETECTED CRACK BY METHOD OF HFEC INSPECTION. (M) 2 L 7 2 4F RT A16WE 2001070300165 20010703 00165 NM 2001 7 3 TSAA0153061 1 20010501 A 5312 66545833510 PRESSURE PANEL BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 817AL 23292 FOUND CRACK NOTED AT LEFT UPPER CORNER NLG PRESSURE PANEL. CONFIRMED CRACK BY UTILIZING HFEC METHOD. (M) 2 L 7 2 4F RT A16WE 2001070300166 20010703 00166 NM 2001 7 3 TSAA0153062 1 20010501 A 5330 86210066 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 817AL 23292 DURING HARD LANDING INSPECTION, DISCOVERED 2 INCHES CRACK AT BS 540, STRINGER 1R AND 2R, VERIFIED BY USING HFEC. (M) 2 L 7 2 4F RT A16WE 2001070300167 20010703 00167 NM 2001 7 3 TSAA0153063 1 20010521 A 5330 6545767103 SKIN BOEING 737 7372Q9 138448M NM FUSELAGE DENTED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 DENT AT FUSELAGE SKIN AT BS 360-BS400, STRINGER 17L. REMOVED DAMAGED AREA, HFEC INSPECTION COMPLETED NO DEFECTS NOTED A ROUND CUTOUT AREA, INSTALLED 7075-T6 CREASE BEAM, INSTALLED .071 INCH FILLER 2024-T3 INSTALLED .032 INCH DOUBLER 2024-T3 , INSTALLED .050 INCH TRIPLER 2024-T6, AND CLEAN AND TREATED ALL BARE SURFACES IAW ECO 3186 OPTION 1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2001070300168 20010703 00168 NM 2001 7 3 TSAA0157066 1 20010601 A 5730 86210151 SKIN BOEING 737 737209 NM RT WING CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 827AL 23913 DISCOVERED CORROSION AT RIGHT WING LOWER SURFACE WS 581.5, BLENDOUT TO REMOVE ALL CORROSION, OBTAINED A SURFACE OF 125 M ICROINCHES RADIUS, CONFIRMED COMPLETE REMOVAL OF CORROSION BY 10 BY GLASS VISUAL INSPECTION, FLAP PEEN REWORKED AREAS PE R SOPM 20-10-03, APPLIED ALODINE, PRIMER AND ENAMEL TO ALL EXPOSED SURFACES, IAW ECO 3091R4. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4F RT A16WE 2001070300169 20010703 00169 NM 2001 7 3 USAABB01034 1 20010601 A 3397 WIRE BOEING 767 767201 1385125 NM CABIN SHORTED A O OTHER O OTHER CR CRUISE 1 EA 19 645US 23897 PHL - FLT 11 - EMERGENCY EXIT LIGHTS ILLUMINATED IN FLIGHT. MAINTENANCE REPAIRED A WIRE AT SEAT ROW 30 WHICH WAS SHORTI NG TO GROUND. (M) 2 L 7 2 4F RT A1NM 2001070300170 20010703 00170 EU 2001 7 3 USAAF01025 1 20010515 A 3350 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN CORRODED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 886US 11346 RDU - THE AFT LAVATORY AREA EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE CLEANED CORROSION FROM BATTERY PACK CO NTACTS IN NR 8 EMERGENCY POWER SUPPLY. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT 2001070300171 20010703 00171 EU 2001 7 3 USAAF01026 1 20010519 A 3350 6040681 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 893US 11373 RDU - THE EMERGENCY LIGHTS IN THE AREA AFT OF FIRST CLASS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED A POWER PACK. O PS CHECKED OK. (M) 2 L 7 2 4F RT 2001070300172 20010703 00172 EU 2001 7 3 USAASA01018 1 20010511 A 3397 WIRE AIRBUS A319 A319112 3930323 EU CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 EA 19 704US 922 SFO - ROWS SIX AND THIRTEEN SEAT MOUNTED EMERGENCY LIGHTS WERE INOPERATIVE WITH BROKEN WIRES AT THE SEAT CONNECTORS. MA INTENANCE REPLACED THE WIRES. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2001070300174 20010703 00174 2001 7 3 USAASA01021 4 20010601 A 2565 D30665105 SLIDE AIRBUS A319 A319112 EU SERVICE DOOR TORN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 703UW 8887 904 TPA - DURING AN OPERATIONAL TEST OF THE AFT RIGHT SERVICE DOOR EMERGENCY ESCAPE SLIDE, THE SLIDE DID NOT INFLATE DUE TO A LARGE TEAR IN THE SLIDE. MAINTENANCE REPLACED THE SLIDE. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2001070300175 20010703 00175 EU 2001 7 3 MALA010545 1 20010622 A 5320 7253720325 BEAM SAAB SF340 340B 7860101 EU CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 403XJ 340B403 Found during 4K-Check, Beam between Sta 272-287 LBL11 is corroded. Maintenance removed and replaced beam PN 7253720-325 IAW SRM Chap 51. Refer to 409 #024452. 2 L 7 2 4T RT A52EU 2001070300176 20010703 00176 EU 2001 7 3 MALA010546 1 20010622 A 5320 7273720337 ANGLE SAAB SF340 340B 7860101 EU CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 403XJ 340B403 During 4K-Check, Angle on beam between Sta 272-287 RBL 10 is corroded. Maintenance removed and replaced Angle PN 725372 0-337 IAW SRM Chap. 51. 2 L 7 2 4T RT A52EU 2001070300177 20010703 00177 EU 2001 7 3 MALA010547 1 20010622 A 5320 FRAME SAAB SF340 340B 7860101 EU CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 403XJ 340B403 Found during 4K-Check, corrosion on Frame Sta 225. Completed repair IAW Saab Statement #340SDS002013. Rev A EO S53097. Maintenance completed repairs IAW Saab Statement 340SDS0021 dated 2001-06-27 2 L 7 2 4T RT A52EU 2001070300178 20010703 00178 EU 2001 7 3 MALA010554 1 20010624 A 5320 7253721413 CHANNEL SAAB SF340 340B 7860101 EU CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 403XJ 340B403 Found during 4K-Check in CWA, beam between LBL12-19 and Sta 258-254 is corroded. Maintenance Replaced channel PN 725372 1-413 between Sta 258-254. 2 L 7 2 4T RT A52EU 2001070300179 20010703 00179 EU 2001 7 3 MALA010555 1 20010624 A 5320 7253722001 ANGLE SAAB SF340 340B 7860101 EU CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 403XJ 340B403 Found during 4K-Check in CWA, Angle on Frame 258 corroded. Maintenance replaced Angle on Frame 258 PN 7253722-001 IAW S aab SRM 51. 2 L 7 2 4T RT A52EU 2001070300180 20010703 00180 EU 2001 7 3 MALA010556 1 20010624 A 5320 7253721447 ANGLE SAAB SF340 340B 7860101 EU CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 403XJ 340B403 Found during 4K-Check in CWA, Angle between Frame 237 and 258 is corroded. Maintenance installed new Angle at Frame 237 and 258. IAW Saab SRM 51 PN 7253721-447 2 L 7 2 4T RT A52EU 2001070300181 20010703 00181 CE 2001 7 3 GLBA2001126 1 20010614 A 2910 1013880167 HYDRAULIC LINE BEECH 1900 1900D 1154162 CE HYDRAULIC SYS DEFECTIVE A GLBA O OTHER O OTHER CR CRUISE 1 CE 01 170GL UE170 LANDING GEAR RELAY CB POPS WHEN GEAR SELECTED DOWN REPLACED LT MLG ACTUATOR HYDRAULIC LINE, OPS CHECKED SYSTEM SATISFACT ORY 2 L 7 2 4T RT A24CE 2001070400001 20010704 00001 WP 2001 7 4 USAAD01124 1 20010612 A 2500 11331780 SLIDE DOUG DC9 DC982 3022082 WP FWD ENTRY DOOR A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 825US 49237 PHL - THE FORWARD ENTRY DOOR EVACUATION SLIDE GIRT BAR WAS HARD TO ENGAGE AND DISENGAGE. MAINTENANCE REPLACED THE EVACU ATION SLIDE AND GIRT BAR. (M) 2 L 7 2 4F A6WE 2001070400002 20010704 00002 NM 2001 7 4 USAABB01033 1 20010528 A 3350 9221009 BATTERY BOEING 757 7572B7 1384964 NM R4 DOOR DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 624AU 27245 CLT - FOUND R4 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2001070400003 20010704 00003 WP 2001 7 4 USAAD01116 1 20010527 A 3350 AD4002P BATTERY DOUG DC9 DC982 3022082 WP PAX CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 820US 49119 PIT - THE FORWARD SECTION OF OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTE RIES. (M) 2 L 7 2 4F A6WE 2001070400004 20010704 00004 WP 2001 7 4 USAAD01122 1 20010606 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 804US 48052 PIT - THE EMERGENCY LIGHT ON SEAT 20 DEF WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F A6WE 2001070400005 20010704 00005 WP 2001 7 4 USAAD01125 1 20010613 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 807US 48039 IND - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001070400006 20010704 00006 EU 2001 7 4 USAASA01025 1 20010611 A 3350 NSA93411201 DIODE AIRBUS 320 A320214 EU E/E BAY FAULTY A USAA K NONE O OTHER NR NOT REPORTED 1 EA 19 122UW 1298 PIT - THE EMERGENCY EXIT LIGHTS FAILED CAME ON INTERMITTENTLY WITH THE COCKPIT EMERGENCY LIGHT SWITCH ARMED. MAINTENANC E REPLACED DIODE 1158VD. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2001070400007 20010704 00007 EU 2001 7 4 USAASA01024 1 20010611 A 3350 EO242A28AO RELAY AIRBUS 320 A320214 EU E/E BAY FAULTY A USAA K NONE O OTHER NR NOT REPORTED 1 EA 19 122UW 1298 CLT - THE EMERGENCY EXIT LIGHTS FAILED CAME ON INTERMITTENTLY WITH THE COCKPIT EMERGENCY LIGHT SWITCH ARMED. MAINTENANC E REPLAED RELAY 8WL. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2001070400008 20010704 00008 WP 2001 7 4 AALA20011145 1 20010530 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 491AA 49684 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY FLOOR PATH LIGHT INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001070400009 20010704 00009 WP 2001 7 4 AALA20011133 1 20010524 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP AFT ASSY INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 258AA 49288 DFW - DURING OVERNIGHT MAINTENANCE, TAIL CONE LOWER EMERGENCY ESCAPE SLIDE LIGHT AND EMERGENCY ESCAPE LIGHTS ABOVE AFT F LIGHT ATTENDANT JUMP SEAT INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001070400010 20010704 00010 WP 2001 7 4 AALA20011184 1 20010604 A 2500 892146062 HEATER DOUG DC9 DC982 3022082 WP LAVATORY CORRODED A AALA K O NONE OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 466AA 49596 LGA - FLT 1194 - EN ROUTE MIA-LGA - FLIGHT ATTENDANT REPORTED A BURNING SMELL AT FIRST CLASS LAVATORY. LANDED LGA WITHO UT FURTHER INCIDENT. REPLAED WATER HEATER AND CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001070400011 20010704 00011 WP 2001 7 4 AALA20011183 1 20010530 A 3600 535610 CLAMP DOUG DC9 DC982 3022082 WP TAIL DEFECTIVE A AALA A UNSCHED LANDING J O WARNING INDICATION OTHER TO TAKEOFF 1 SW 21 228AA 49178 LAX - FLT 335 - EN ROUTE LAX-SJD - SHORTLY AFTER TAKEOFF TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. RETURNED LAX AND LANDED WITHOUT FURTHER INCIDENT. REPLACED LEFT SIDE AUGMENTATION VALVE CLAMP. LEAK CHECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001070400012 20010704 00012 WP 2001 7 4 AALA20011182 1 20010530 A 3600 S1309 SENSOR DOUG DC9 DC982 3022082 WP HEAT EXCHANGER DEFECTIVE A AALA A UNSCHED LANDING J O WARNING INDICATION OTHER CL CLIMB 1 SW 21 477AA 49652 DFW - FLT 1612 - EN ROUTE DFW-LIT, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED TAIL COMPARTMENT HIGH TEMPERATURE SENSORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001070400013 20010704 00013 WP 2001 7 4 AALA20011178 1 20010603 A 3697 WIRE DOUG DC9 DC982 3022082 WP TAIL SHORTED A A UNSCHED LANDING J O WARNING INDICATION OTHER TO TAKEOFF 1 SW 21 553AA 53083 DFW - FLT 369 - EN ROUTE DFW-BOS, SHORTLY AFTER TAKEOFF TAIL COMPARTMENT HIGH LIGHT ILLUMINATED. RETURNED DFW AND LANDE D WITHOUT FURTHER INCIDENT. REPAIRED TAIL TEMPERATURE SENSOR WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001070400014 20010704 00014 WP 2001 7 4 AALA20011125 1 20010523 A 3600 CLAMP DOUG DC9 DC982 3022082 WP A AALA A UNSCHED LANDING J O WARNING INDICATION OTHER CL CLIMB 1 SW 21 465A 49595 DFW - FLT 1580 - EN ROUTE DFW-DCA, TAIL HIGH TEMP LIGHT ILLUMINATED. RETURNED DFW LANDED WITHOUT INCIDENT. REPOSITIONE D CLAMP ON LEFT PACK ANTI-ICE VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001070400015 20010704 00015 WP 2001 7 4 AALA20011105 1 20010519 A 7800 FITTING DOUG DC9 DC982 3022082 WP RT ENGINE LOOSE A AALA A UNSCHED LANDING J O WARNING INDICATION OTHER CL CLIMB 1 SW 21 400AA 49311 DFW - FLT 1953 - EN ROUTE DFW-SHV, RIGHT ENGINE REVERSER ACCUMULATOR LIGHT ILLUMINATED DURING CLIMB-OUT AND RIGHT HYDRAU LIC QUANTITY DECREASED. AIR INTERRUPTED AND RETURNED TO DFW. LANDED WITHOUT INCIDENT. TIGHTENED LOOSE FITTING ON ACCU MULATOR LINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001070400016 20010704 00016 WP 2001 7 4 AALA20011102 1 20010518 A 3200 833703 SENSOR DOUG DC9 DC982 3022082 WP NOSE GEAR DEFECTIVE A AALA K O NONE OTHER J O WARNING INDICATION OTHER CL CLIMB 1 SW 21 481AA 49656 ORD - FLT 9563 - DURING LOCAL FUNCTIONAL CHECK, FLIGHT NOSE LANDING GEAR RED LIGHT ILLUMINATED INTERMITTENTLY. REPLACED NOSE GAR POSITION SENSORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M( 2 L 7 2 4F A6WE 2001070400017 20010704 00017 WP 2001 7 4 AALA20011177 1 20010531 A 4900 5940405503 APU DOUG DC9 DC982 3022082 WP APU LEAKING A AALA K O NONE OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 21 70404 49315 BOS - FLT 1540 - EN ROUTE DFW-BOS - SHORTLY AFTER TAKEOFF CABIN FILLED WITH SMOKE. DE-PRESSURIZED AIRCRAFT. SMOKE DISS IPATED. LANDED BOS WITHOUT FURTHER INCIDENT. REPLACED APU. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001070400018 20010704 00018 WP 2001 7 4 AALA20011018 1 20010517 A 2600 AYLF97141 ELEMENT DOUG DC9 DC983 3022083 WP TAIL DEFECTIVE A AALA A UNSCHED LANDING J O WARNING INDICATION OTHER TO TAKEOFF 1 SW 21 563AA 49345 DFW - FLT 2344 - DFW-MEX - AIR INTERRUPTED DUE TO TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATION. RETURNED DFW AND LANDE D WITHOUT INCIDENT. REPLACED TAIL COMPARTMENT OVERHEAT ELEMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001070500001 20010705 00001 SW 2001 7 5 20010606CW010 1 20010508 A 6520 407012101111 GEARBOX BELL 407 407 SW TAIL ROTOR LOOSE E H11A K NONE E VIBRATION/BUFFET TX TAXI/GRND HDL 1 SO 11 9137N 42 53466 UPON COMPLETION OF A 1.7 HR FLT, PILOT NOTICED SHUDDERING VIBRATION AFTER ROLLING THE TWIST GRIP TO IDLE. PILOT REPORTE D PROBLEM TO MAINT, INSPECTION REVEALED MOVEMENT BETWEEN T/R G/B AND TAILBOOM CASTING. THREE G/B STUD NUTS WERE FOUND LOOSE, ONE ALIGNMENT PIN LOOSE, ONE MOUNT STUD BROKEN, AND TAILBOOM TO G/B MOUNT HOLES WERE WORN BEYOND LIMITS. NO VISI BLE DAMAGE WAS NOTED ON T/R ASSY. THE TAILBOOM AND G/B WERE REPLACED USING ORIGINAL T/R ASSY. STRONG VIBRATION EMANATI NG FROM THE T/R WAS FELT DURING GROUND RUN AT IDLE. SERVICEABLE T/R ASSY WAS INSTALLED. GROUND RUN, NML AND T/R WAS BA LANCED. ALL PARTS WERE SENT TO MFG FOR EVALUATION. 1 G 7 1 3U O H2SW 2001070500002 20010705 00002 SO 2001 7 5 20010607CW002 2 20010517 A 7322 6299042 FUEL CONTROL BEECH 33 F33A 1151425 CE CONT O520 IO520* 17032 SO ENGINE DEFECTIVE A VJ3R A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SW 99 5609S 48 CE1454 THE PILOT REPORTED A ROUGH ENGINE IN FLIGHT AND RETURNED TO AIRPORT, A SAFE LANDING WAS MADE. MAINTENANCE GROUND RUN A IRCRAFT AND A FLUCTUATION IN FUEL FLOW WAS NOTED. THEY FOUND THAT THE MIXTURE CONTROL WAS STIFF WHEN MOVING. (POSSIBLE GALLING). FUEL CONTROL WAS REMOVED AND A NEW ONE INSTALLED, ENGINE WAS TRIMMED, TEST FLIGHT CHECKED NORMAL. FUEL CON TROL WAS SENT IN FOR WARRANTY. 1 L 7 1 3O 3 O 3A15 E5CE 2001070500004 20010705 00004 NM 2001 7 5 DHL2001717011 1 20010703 A 2613 DUCT BOEING 727 72723 1384004 NM A DHLA A UNSCHED LANDING M OVER TEMP CR CRUISE 1 SO 01 717DH 19389 IN FLIGHT LWR AFT BODY OVHT LT ILLUMINATED, LT EXTINGUISHED AFTER #3 THRUST LEVER WAS RETARDED C/W ABNORMAL PROCEDURET/ S LWR AFT BODY OVHT LT. FOUND TAI DUCT TO BE CRACKED, REMOVED DUCT. DUCT REPAIRED BY VENDOR JLWR146K IAW B727 OHM CHPT 3 6-10-01. REINSTALLED DUCT. LEAK CK GOOD IAW B727 MM CHPT 36-00-1STATUS: CLOSED 2 L 7 3 4F A3WE 2001070500008 20010705 00008 NM 2001 7 5 CA010621010 1 20010605 A 5210 85210109009 STRUT DHAV 85210109009 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE AT SWAGE BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) THE FORWARD HANDRAIL STRUT ASSEMBLY FOR THE PASSENGER DOOR WAS FOUND TO BE BROKEN IN THE AREA WHERE IT IS SWAGED O N THE PIVOT CASTING, JUST BELOW THE SWAGE REINFORCING BAND. THE STRUT WAS REPLACED. 17271 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001070500009 20010705 00009 NM 2001 7 5 CA010621014 1 20010605 A 5210 85210109009 STRUT DHAV 85210109009 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE AT SWAGE BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) THE FORWARD HANDRAIL STRUT ASSEMBLY FOR THE PASSENGER DOOR WAS FOUND TO BE BROKEN IN THE AREA WHERE IT IS SWAGED O N THEPIVOT CASTING. JUST BELOW THE SWAGE REINFORCING BAND. THE STRUT WAS REPLACED. 17271 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001070500010 20010705 00010 NM 2001 7 5 CA010621031 1 20010526 A 7921 28E997 OIL COOLER HONEYWELL 28E997 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE OIL COOLER LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 23081 1669 04900583 (CAN) MAINTENANCE INVESTIGATION OF AN OIL LEAK ON # 2 ENGINE RESULTED IN THE REPLACEMENT OF THE ENGINE OIL COOLER HAD AC CUMLATED 169 HOURS AND 2454 CYCLES SINCE RECORDING BY HONEYWELL LORI HEAT TRANSFER. 13320 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001070500011 20010705 00011 NM 2001 7 5 CA010622010 1 20010605 A 2434 GENERATOR BOEING 767 767375 NM GE CF6 CF680C2B6F 30025 NE GENERATOR FAILED W D RETURN TO BLOCK O OTHER TO TAKEOFF 1 CA 8526 8526 (CAN) F/O'S FMC FAILED, F/O'S ADI & HSI FLICKERED CONTINIOUSLY. AUTO THROTTLE DROPPED OFF. SINGLE FMC MESSAGE & RESYNCHI NG OTHER FMC MESSAGE ALL COME ON. WHEN THE RIGHT GENERATOR BREAKER WAS OPENED & THE APU GENERATOR WAS PUT ON LINE, ALL S YSTEMS OPERATE NORMAL. AIRCRAFT RETURNED TO BLOCKS FOR TROUBLE SHOOTING. 2 L 7 2 4F 4 F RT A1NM E13NE 2001070500012 20010705 00012 NM 2001 7 5 CA010622016 1 20010512 A 7921 28E997 OIL COOLER HONEYWELL 28E997 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE OIL COOLER LEAKING W K NONE K FLUID LOSS NR NOT REPORTED 1 CA 7548 364 118 (CAN) INVESTIGATION OF AN OIL LEAK ON THE # 2 ENGINE RESULTED IN THE REPLACEMENT OF THE ENGINE OIL COOLER. THE OIL COOLE R HAD BEEN IN SERVICE 115 DAYS SINCE REPAIR FOR LEAKING . 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001070500017 20010705 00017 NM 2001 7 5 CA010628001 1 20010619 A 3297 WIRE BOEING 727 727260 NM PWA JT8 JT8D17 52049 NE WIRE BROKEN W O OTHER J WARNING INDICATION DE DESCENT 1 CA (CAN) WHEN LANDING GEAR EXTENDED, R/H MAIN GEAR DOOR LIGHTS DO NO ILLUMINATE. INSPECTED RT MAIN GEAR DOOR CANNON PLUG, W IRE PIN 6 BROKEN, REPAIRED WIRE TO PIN 6. IAW WDM 32-60-04, CANNON PLUG RESECURED FUNCTION CHECKED SERVICABLE. 2 L 7 3 4F 4 F RT A3WE E2EA 2001070500018 20010705 00018 CE 2001 7 5 CA010628017 1 20010610 A 2100 CLAMP BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3A NE WING LEADING EDG LOOSE W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA (CAN) REJECTED TAKE OFF OUT OF DORVAL, QUEBEC ON JUNE 10, 2001 AROUND 11:00AM R/H BLEED AIR FAIL LIGHT CAME ON DURING TA KEOFF. TAKE OFF REJECTED. MAINTENAMCE INSPECTED THE AIRCRAFT AND FOUND A LOOSE CLAMP ON THE R/H BLEED AIR DUCT BEHIND TH E LEADING EDGE. E.V.A TUBING REPAIRED. AIRCRAFT GROUND TESTED SERVICED AND RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2001070500019 20010705 00019 NM 2001 7 5 CA010628053 1 20010531 A 8012 START VALVE PWA JT8D17 BOEING 727 727217 NM PWA JT8 JT8D17 52049 NE INDICATION FAILED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA 702698 (CAN) #2 ENGINES START VALVE OPEN LIGHT ILLUMINATED IN FLIGHT. DEFERRED #2 ENGINE START VALVE FOR PARTS & T/S IAW MEL 80 -1 CAT "C" ITEM EXPIRES 6/10/01. 2 L 7 3 4F 4 F RT A3WE E2EA 2001070500023 20010705 00023 GL 2001 7 5 20010607CW004 2 20010516 A 7260 GEARBOX EMB 145 EMB145LR SO ALLSN AE300 AE3007A GL ENGINE MAKING METAL A OZRR K NONE O OTHER NR NOT REPORTED 1 SW 11 618AE 145097 METAL DEBRIS FOUND ON CHIP COLLECTOR DRAIN VALVE (GEARBOX, OIL TANK). 2 L 7 2 4T 4 F RT T00011AT TE6CH 2001070500024 20010705 00024 EA 2001 7 5 20010607CW005 2 20010314 A 7230 311211702 BEARING BEECH 200 200BEECH 1152920 CE PWA PT6 PT6* 52043 EA COMPRESSOR FAILED B O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 19 711CR 29 BB16 ENGINE WAS SHUT DOWN IN FLIGHT DUE TO LOSS OF PROPELLER ROTATION. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. TEAR DOWN REVEALED CAUSE OF PROBLEM TO BE NR 1 BEARING FAILURE. FAILURE IS CONSIDERED TO BE AN ISOLATED INCIDENT. 1 L 7 2 4T 3 T A24CE E2NE 2001070500025 20010705 00025 SO 2001 7 5 20010607CW006 1 20010514 A 3260 487863 SAFETY SWITCH PIPER PA30 PA30 7103002 SO LYC O360 IO360B1A 41514 EA LT MLG FAILED D A UNSCHED LANDING O OTHER LD LANDING 1 CE 07 8353Y 7000 301500 THE SAFETY SWITCH MOUNTED ON THE LEFT LANDING GEAR WORKS AS A SQUAT SWITCH. FAILED BOTH WAYS. IT HAD ELECTRICITY GOING TO IT, BUT NONE COMING OUT EITHER UP OR DOWN TRAVEL. THE LANDING GEAR STARTED UP ENOUGH TOO. RELEASE THE DOWN LOCK, T HEN FAILED, GEAR WOULD NOT GO UP OR DOWN. THE PILOT FLEW BACK TO HOME BASE WITH GEAR DOWN. THE PILOT ASSUMED THAT THE GEAR WAS DOWN AS HE INSTALLED THE EMERGENCY HANDLE AND TRIED TO PUSH IT DOWN, BUT WAS SOLID, SO HE ASSUMED IT WAS DOWN. WHEN LANDING, IT COLLAPSED. 1 L 7 2 3O 3 O A1EA 1E10 2001070500026 20010705 00026 NM 2001 7 5 2001F00076 1 20010620 A 2751 106079113 INDICATOR BOEING 737 737230 NM COCKPIT INTERMITTENT A RJEF A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SO 23 261LR 22402 SAL - FLT 441 - AFTER TAKEOFF, WHEN PILOT SELECTED FLAP TO UP POSITION, IT DID NOT RESPONDED. ALTERNATE FLAP EXTENSION WAS PERFORMED FOR LANDING. THE AIRCRAFT RETURN TO THE EL SALVADOR AIRPORT. AT EL SALVADOR STATION, MAINTENANCE TECHS T ESTED THE FLAPS INDICATION ACCORDING TO AMM 27-58-01. THE POSITION TRANSMITTER LT/RT WERE REPLACED DUE TO INTERMITTENT WORKS ACCORDING TO AMM 27-58-12. ALSO, THE FLAPS POSITIONS INDICATOR WERE REPLACED ACCORDING TO AMM 27-58-41. AFTER SA TISFACTORY FUNCTIONAL CHECKS, THE AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001070500027 20010705 00027 NE 2001 7 5 C2XA01BT122 2 20010701 A 7200 PW121 ENGINE AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE SHUTDOWN A C2XA E O ENGINE SHUTDOWN OTHER B J Z SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION SIGNIFICANT FAILURE REPORT AP APPROACH 1 SW 27 15816 22992 10225 105 120800 BTV---CO2942, CREW REPORTED (ON APPROACH) "#2 PACK OVERHEAT CAUSED SMOKE IN CABIN." AND "#2 ENGINE-OIL PRESSURE DROPPED. ENGINE SHUTDOWN IN FLIGHT." LANDED UNEVENTFULLY....MAINTENANCE FOUND ENGINE OIL IN PACK WHICH CAUSED SMOKE IN CABIN, RE MOVED AND REPLACED #2 ENGINE IAW TASK CARD #2272001. OPS. AND LEAKED CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2001070500029 20010705 00029 EU 2001 7 5 2001F00079 1 20010413 A 2910 HYDRAULIC SYSTEM STBROS SD3 SD360 8100606 EU FUSELAGE CONTAMINATED A PIVA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 13 711MP SH3698 FLT 3825 - DECLARED EMERGENCY AND LANDED SAFE. AFTER BOTH HYD WARNING LIGHT ON CWP ILLUMINATED. CHECKED HYD SYSTEM FOUN D OUT LOTS OF AIR IN THE SYSTEM. COMPLIED WITH BLEEDING AND COMPLETED HYD SYSTEM REPLENISHMENT OBSERVED HYD SYSTEM. NO FAULT NOTED. (M) 2 H 7 2 4T A41EU 2001070500030 20010705 00030 NM 2001 7 5 C1HA200186007 1 20010630 A 7100 JT8D17 ENGINE BOEING 727 7272S7 138407Z NM PWA JT8 JT8D17 52049 NE #2 FOD A C1HA A D UNSCHED LANDING RETURN TO BLOCK R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 15 686CA 22021 688719 #2 eng EPR dropped from 2.19 to 2.12 after liftoff #2 power lever @ firewall 3 to 4 inches further than 1 or 3. Air retu rn/Return to block.Action Taken:Inspection found internal compressor damage. Removed and replaced #2 engine. 2 L 7 3 4F 4 F A3WE E2EA 2001070500031 20010705 00031 NM 2001 7 5 C1HA200196008 1 20010630 A 2130 39608831 FLOW VALVE BOEING 727 7272J4 1384006 NM LEFT FAILED A C1HA J A D DUMP FUEL UNSCHED LANDING RETURN TO BLOCK O OTHER CL CLIMB 1 GL 15 696CA 22574 Unable to pressureise A/C during climb out Ran checklist, no pressureisation. Dump fuel made air return.ACTION TAKEN:R&R 'd L/H flow control valve ops checked normal. 2 L 7 3 4F RT A3WE 2001070500032 20010705 00032 NM 2001 7 5 2001F00081 1 20010416 A 3411 BACH30BC060170 HOSE BOEING 737 737296 1384486 NM PITOT/STATIC SYS LEAKING A RJEF A UNSCHED LANDING O OTHER CL CLIMB 1 SO 23 232TA 22277 FLT 410 - SAL - DURING CLIMB, THE CAPTAIN REPORTED THAT DURING INITIAL CLIMB THERE WAS A DIFFERENCE OF 100 FEET BETWEEN CAPTAIN AND FIRST OFFICER ALTIMETER, AT 17,000 FEET, THE DIFFERENCE INCREASE TO 1000 FEET AND WHEN LEVEL AT FL270, THE D IFFERENCE INCREASE TO 1500 FEET. THE AIRCRAFT RETURNED TO EL SALVADOR AIRPORT. AFTER LANDING, MAINTENANCE TECHNICIANS PERFORMED THE PITOT STATIC SYSTEM ADJUSTMENT TEST, ACCORDING TO MM 34-11-00, AND FOUND PNEUMATIC LEAK AT THE HOSE THAT S UPPLY PRESSURE TO FIRST OFFICER ALTIMETER. THE HOSE WAS REPLACED, AND PERFORMED A LEAK CHECK ACCORDING TO MM 34-11-00. THE AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2001070500033 20010705 00033 EU 2001 7 5 C2XA01BT123 1 20010702 A 3350 167006 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA O OTHER L NO TEST IN INSP/MAINT 1 SW 27 25811 094 MAINTENANCE FOUND (DURING 3A INSPECTION) EMERGENCY LIGHT ON FLOOR TRACK FIFTH FROM THE AFT WAS INOPERATIVE. MAINTENANC E RELAMPED EMERGENCY LIGHT ON FLOOR TRACK IAW ATR42 MM 33-10-00. OPS. CHECKED GOOD. 2 H 7 2 4T RT A53EU 2001070500034 20010705 00034 CE 2001 7 5 2001F00082 1 20010214 A 2750 SWITCH BEECH 200 200BEECH 1152920 CE RT T/E FLAP DIRTY A HSYA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 05 279CA BB279 BIL - AT 1000 FEET AGL FLAPS WOULD NOT RETRACT FROM 40 PERCENT. FLAP HANDLE RECYCLED AND CIRCUIT BREAKER CHECKED. CONT AMINATION ON LIMIT SWITCHES AT RIGHT WING. NO DEFECTIVE PART IDENTIFIED. THE LIMIT SWITCHES WERE CLEANED WITH ELECTRIC AL CONTACT CLEANER. SYSTEM FUNCTION CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. (M) 1 L 7 2 4T A24CE 2001070500037 20010705 00037 SW 2001 7 5 2001F00085 1 20010131 A 3213 2751540003 PIN SWRNGN SA227 SA227AC 8780603 SW RT MLG BROKEN A BSAA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 05 27465 755B GEAR WAS COCKED TO THE SIDE BETWEEN 30 AND 45 DEGREES. CREW THOUGHT THEY HAD A FLAT TIRE BEFORE THEY GOT OUT OF THE AIR CRAFT. RIGHT MLG UPPER TORQUE LINK PIN BROKE IN TWO PLACES. PIN BROKE AT THE TWO ADDITIONAL HOLES THAT AREN'T USED FOR THIS INSTALLATION. THE OLDER 001 PIN ONLY HAD THE ONE HOLE FOR THE ROLL PIN. THE 001 PIN HAS BEEN REPLACED BY THE 003 PIN. HAVE NOT RECEIVED THE PIN FROM THE OUTSTATION YET TO TRY AND DETERMINE THE FAILURE MODE/CAUSE ON THE TORQUE LINK PIN. REPLACED BROKEN PIN, INSPECTED GEAR, ATTACH TRUNNIONS, KEELSON WEBS, DRAG LINK ATTACH EARS, AND PERFORMED GEAR SWI NG. NO DEFECTS NOTED. (M) 2 L 7 2 4T RT A8SW 2001070500040 20010705 00040 CE 2001 7 5 2001F00088 1 20010424 A 5510 1016200111 HINGE BRACKET BEECH 1900 1900 1154160 CE RT STABILIZER CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 199GA UB13 DURING SCHEDULED MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANN ULAR CORROSION. REMOVED AND REPLACED RIGHT ELEVATOR OUTBOARD HINGE BRACKET. (M) 2 L 7 2 4T RT A24CE 2001070500041 20010705 00041 CE 2001 7 5 2001F00089 1 20010424 A 5510 1016200131 HINGE BRACKET BEECH 1900 1900 1154160 CE LT STABILIZER CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 199GA 31549 UB13 DURING SCHEDULED MAINTENANCE, LEFT CENTER ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANNULA R CORROSION. REMOVED AND REPLACED LEFT ELEVATOR CENTER HINGE BRACKET. (M) 2 L 7 2 4T RT A24CE 2001070500042 20010705 00042 CE 2001 7 5 2001F00090 1 20010525 A 5510 1016200131 HINGE BRACKET BEECH 1900 1900C 1154161 CE RT STABILIZER CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 1568W 17970 UC64 DURING SCHEDULED MAINTENANCE, RIGHT CENTER ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANNUL AR CORROSION. REMOVED AND REPLACED RIGHT ELEVATOR CENTER HINGE BRACKET. (M) 2 L 7 2 4T RT A24CE 2001070500043 20010705 00043 NM 2001 7 5 C1HA200181007 1 20010625 A 3350 LAMP BOEING 727 7272S7 138407Z NM BURNED OUT A C1HA O OTHER L NO TEST IN INSP/MAINT 1 GL 15 681CA 22020 Overwing exit lights are burned out.ACTION TAKEN:Relamped ops check normal. 2 L 7 3 4F A3WE 2001070500044 20010705 00044 WP 2001 7 5 AALA20011016 1 20010516 A 2613 WARNING LIGHT DOUG DC9 DC983 3022083 WP COCKPIT FALSE INDICATION A AALA K NONE N FALSE WARNING CR CRUISE 1 SW 21 563AA 49345 DFW - EN ROUTE BNA-DFW - TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. TROUBLESHOT SYSTEM COULD NOT DUPLICATE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001070500045 20010705 00045 WP 2001 7 5 AALA20011060 1 20010508 A 5347 TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 TUL - FOUND LAV TIE DOWN AT STATION 255 LBL 32 CORRODED. REMOVED AND REPLACED TIE DOWN TRACK WITH NEW SRM 51-01. (M) 2 L 7 2 4F RT A6WE 2001070500046 20010705 00046 WP 2001 7 5 AALA20011061 1 20010508 A 5347 TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 TUL - FOUND LAVATORY TIE DOWN AT STATION 253 LBL 19 CORRODED. REMOVED AND REPLACED TIE DOWN SECTION WITH NEW SRM 51-01. (M) 2 L 7 2 4F RT A6WE 2001070500047 20010705 00047 NM 2001 7 5 AALA20011094 1 20010519 A 3242 260881211 BRAKE ASSY BOEING 767 767323 1385205 NM LT MLG DEFECTIVE A AALA D RETURN TO BLOCK O OTHER TO TAKEOFF 1 SW 21 39367 25194 DFW - FLT 367 - DURING TAKEOFF, AIRCRAFT BEGAN TRACKING TO LEFT. AIRCRAFT RETURNED DFW GATE WITHOUT INCIDENT. REPLACED NR 1 BRAKE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001070500048 20010705 00048 NM 2001 7 5 AALA20011106 1 20010520 A 2120 UNKNOWN BOEING 777 777223 1385213 NM CABIN ODOR A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 780AN 29956 DFW - FLT 61 - EN ROUTE DFW-NRT - IN CRUISE AN UNIDENTIFIABLE STRONG NOXIOUS ODOR DETECTED ONBOARD. AIR INTERRUPTED AND RETURNED TO DFW. LANDED WITHOUT INCIDENT. TROUBLESHOT AIR CONDITIONING DUCTING AND LIGHTING FIXTURES IN CABIN AND FORW ARD CARGO AREAS. NO DISCREPANCIES FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001070500049 20010705 00049 WP 2001 7 5 AALA20011128 1 20010524 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7530 49922 BOS - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY PORTABLE LIGHT DIM. REPLACED FORWARD EMERGENCY PORTABLE LIGHT ASS EMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001070500050 20010705 00050 NE 2001 7 5 AALA20011136 2 20010521 A 7200 ENGINE BOEING 767 767323 1385205 NM GE CF6 CF680C2B6 30025 NE RIGHT VIBRATION A AALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 21 358AA 24039 HNL - FLT 298 - RIGHT ENGINE VIBRATION IND 2.8 WITH MASTER CAUTION ON ROTATION. ACCOMPLISHED VIBRATION SURVEY PER MM 71 -00-00-5-H NR 7 VIBRATION WITHIN LIMITS 1.8 ON RUN-UP. NO PRV LIGHT OR MASTER CAUTION LIGHT BITE CHECK ON AIRSUPPLY MOD ULE ENGINE VIBRATION MONITOR OK. CONCURRED WITH TECH SERVICE. CHECKED ALL ENGINE PNEU DUCTS, CLAMPS, LINES. ALL OK. INLET AND EXHAUST OK 1.8 AT 104-1.4 AT 98.7 AT 95. (M) 2 L 7 2 4F 4 F RT A1NM E13NE 2001070500051 20010705 00051 WP 2001 7 5 AALA20011139 1 20010526 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 259AA 49289 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 7 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001070500052 20010705 00052 NM 2001 7 5 AALA20011142 1 20010527 A 3350 LIGHT BOEING 767 767323 1385205 NM EXIT DOOR DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 376AN 25445 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT EXIT DOOR INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGH T ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001070500053 20010705 00053 NM 2001 7 5 AALA20011151 1 20010521 A 5320 PAN BOEING 727 727227 1384078 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 728AA 20735 TUL - FOUND CORROSION 2 INCHES BY 8 INCHES ON LOWER SIDE OF LAVATORY FLOOR PAN AND DOUBLER STATION 1164-1178 AT LBL 24-2 8. CUT OUT DAMAGED AREA INSTALLED FILLER AND DOUBLER PER SRM 51-40-2. (M) 2 L 7 3 4F A3WE 2001070500054 20010705 00054 SO 2001 7 5 RAIA00107001 1 20010701 A 3030 0851HU SENSOR EMB 145 EMB145LR SO Zone 100 FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 812HK 1163 145373 5273-RIC ON TAXI OUT #1 PITOT HEAT FAILED-MAINTENANCE REMOVED AND REPLACED #1 PITOT TUBE/SENSOR 2 L 7 2 4T RT T00011AT 2001070500055 20010705 00055 WP 2001 7 5 AALA20011156 1 20010508 A 5530 PLATE DOUG DC9 DC982 3022082 WP VERTICAL STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3515 49892 TUL - FOUND 4 INCH BY 4 INCH CORROSION ON ALL 4 VERTICAL STABILIZER HINGE PLATES FOR HORIZONTAL STABILIZER. REMOVED PLA TES AND REPLACED SRM 51-01. (M) 2 L 7 2 4F A6WE 2001070500056 20010705 00056 NM 2001 7 5 AALA20011167 1 20010529 A 3350 A3060723 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 616AA 24524 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT R2 DOOR. REPLACED EMERGENCY EXIT LIGH T SEGMENT SUPPLY ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001070500057 20010705 00057 WP 2001 7 5 AALA20011173 1 20010601 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 442AA 49468 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 8 BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYST EM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001070500058 20010705 00058 WP 2001 7 5 AALA20011174 1 20010603 A 3350 LIGHT DOUG DC9 DC982 3022082 WP L2 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7541A 49995 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L2 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001070500059 20010705 00059 WP 2001 7 5 AALA20011187 1 20010605 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP AIRSTAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 442AA 49468 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AS SEMBLY AT AFT AIRSTAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001070500060 20010705 00060 NM 2001 7 5 AALA20011191 1 20010607 A 3350 TERMINAL BOEING 767 767323 1385205 NM R2 DOOR BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 366AA 25193 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT R2 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT TERMINAL END AT R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001070500061 20010705 00061 NM 2001 7 5 AALA20011206 1 20010603 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 867AA 21372 TUL - FOUND STATION 720D-720E OUTBOARD SIDE STRINGER 26R SKIN LAP HAS 3 INCH BY 10 INCHES OF CORROSION AROUND ATTACH FAS TENERS. REMOVED CORROSION PER SRM 51-10-6, CUTOUT CORROSION AT SKIN LAP. INSTALLED REPAIR DOUBLER PER SRM 53-30-3. (M ) 2 L 7 3 4F A3WE 2001070500062 20010705 00062 WP 2001 7 5 AALA20011238 1 20010602 A 5320 CAP DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 566AA 49348 TUL - FOUND CORROSION 2 INCHES BY 4 INCHES AROUND FASTENERS ON LONGERON 23R AT STATION 1220. REMOVED AND INSTALLED NEW END CAP ON LONGERON PER SRM 51-01. (M) 2 L 7 2 4F RT A6WE 2001070500063 20010705 00063 EU 2001 7 5 C2XA01BT124 1 20010627 A 2420 243211 GCU AEROSP ATR42 ATR42320 8680930 EU CPT. ELECT PNL. FAULTY A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 34820 159 EWR---CO3433, CREW REPORTED ACW GENERATOR #2 FAULT LIGHT ILLUMINATED IN FLIGHT, SMELL OF ELECTRICAL INSULATION BURNING W AS PRESENT FOR ABOUT TEN MINUTES AFTER WE DESELECTED THE ACW GEN 2 PUSHBUTTON.......MAINTENANCE FOUND A CHAFFED WIRE AT ACW GEN #2 REPAIRED WIRE, ALSO FOUND #2 ACW GENERATOR CONTROL UNIT FAILED (SUSPECTED CAUSED BY CHAFFED/SHORTED WIRE).... MAINTENANCE REMOVED AND REPLACED #2 ACW GENERATOR CONTROL UNIT (GCU) IAW ATR42 JIC 24-22-84. OPS. CHECKED SYSTEM GOOD. 2 H 7 2 4T RT A53EU 2001070500064 20010705 00064 NE 2001 7 5 AALA20011243 2 20010612 A 7261 ENGINE BOEING 727 727223 1384074 NM PWA JT8 JT8D1 52044 NE NR 1 LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 21 879AA 21391 21391 IAH - FLT 1963 - MIA-IAH, ON SHORT FINAL NR 1 ENGINE OIL QUANTITY DECREASED TO ZERO. LANDED IAH WITHOUT FURTHER INCIDEN T. REPLACED NR 1 ENGINE. SYSTEM GROUND CHCKED NORMAL OPERATION. (M) 2 L 7 3 4F 4 F A3WE E2EA 2001070500065 20010705 00065 CE 2001 7 5 AOQA201C 1 20010604 A 3260 LIGHT LEAR 35 35A 5170602 CE COCKPIT INOPERATIVE A AOQA O OTHER N FALSE WARNING AP APPROACH 1 EA 11 747GM 308 UPON LANDING GEAR EXTENSION, DURING FINAL APPROACH, RIGHT MAIN GEAR GREEN DOWN AND LOCK LIGHT DID NOT ILLUMINATE. PERFO RMED LIGHT TEST AND CONFIRMED LIGHT INOPERATIVE. REPLACED BULBS IN LANDING GEAR CONTROL PANEL. JACKED AIRCRAFT AND PER FORMED LANDING GEAR FUNCTIONAL CHECK. OPS CHECK GOOD IAW LEARJET MM. FLT CREWS SUSPECTED GEAR DOWN LIGHT INDICATION BU LB TO BE AT FAULT. RAN ALL APPROPRIATE CHECKS AND AS FURTHER PRECAUTION REQUESTED TOWER FLYBY FOR LANDING GEAR DOWN VER IFICATION. (M) 2 L 7 2 4F A10CE 2001070500066 20010705 00066 NE 2001 7 5 ASOA01035 2 20010411 A 7200 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE NR 2 FAILED A ASOA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 11 843AS 7310 FLT 4742 - DURING FLIGHT FROM AUS TO ATL, CREW RECEIVED A NR 2 ENGINE 'LOW OIL PRESSURE' LIGHT. CREW SHUT DOWN RIGHT EN GINE FOLLOWING QRH AND DECLARED AN EMERGENCY. AIRCRAFT DIVERTED TO JAN AND LANDED SAFELY. MAINTENANCE PERFORMED MAGNET IC CHIP DETECTOR INSPECTION AS PER CRJ AMM 72-00-00 AND DETERMINED THE NR 2 ENGINE TO BE OUT OF LIMITS. MAINTENANCE REM OVED AND REPLACED THE RIGHT ENGINE. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2001070500067 20010705 00067 EU 2001 7 5 ASOA01068 1 20010603 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN MALFUNCTIONED A ASOA K NONE O OTHER CR CRUISE 1 SO 11 641AS 387 FLT 4052 - DURING FLIGHT FROM CHA-ATL, TWO MINUTE LIGHT STAYS ON THE WHOLE FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT IN ATL. MAINTENANCE INSPECTED BUT COULD NOT DUPLICATE THE DISCREPANCY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERV ICE. (M) 2 H 7 2 4T RT 2001070500068 20010705 00068 EA 2001 7 5 ASOA01069 1 20010526 A 2750 FLAP CNDAIR CL600 CL6002B19 EA WING MALFUNCTIONED A ASOA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 11 854AS 7382 FLT 4720 - ON APPROACH INTO ATL, CAPTAIN SELECTED FLAPS TO 8 DEGREES AND GOT ALL ESS FAIL CAUTION MESSAGES FOR ONE SECON D THEN A FLAP FAIL MESSAGE. CAPTAIN COMPLIED WITH QRH PROCEDURES AND DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY IN ATL WITH ZERO FLAPS. MAINTENANCE FOUND NO FAULT IN FLAP ELECTRONIC CONTROL UNIT. MAINTENANCE THEN RESET CIRCUIT BREAKE R AND CYCLED FLAPS NUMEROUS TIMES WITH NO FAIL MESSAGES. OPERATIONAL CHECKS GOOD ON GROUND. AIRCRAFT OK FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001070500069 20010705 00069 EU 2001 7 5 ASOA01071 1 20010604 A 3350 101191 LIGHT AEROSP ATR72 ATR72 EU AIRSTAIR DOOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 634AS 370 ON GROUND IN ATL, CREW REPORTED THE AIRSTAIR DOOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EME RGENCY LIGHT BULB ON AIRSTAIR DOOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT 2001070500070 20010705 00070 EA 2001 7 5 ASOA01072 1 20010627 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 848AS 7339 FLT 4798 - ON GROUND IN ATL, CREW DISCOVERED GREEN EMERGENCY LIGHT FLOOR STRIP AT ROW 3 WAS INOPERATIVE. MAINTENANCE FO UND STRIP IN POSITION ABOVE THE ONE TO THE AFT. STRIP WAS REMOVED AND PLACED IN ITS CORRECT POSITION. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2001070500071 20010705 00071 EA 2001 7 5 COMA0160423 1 20010628 A 3600 32895902 VALVE CNDAIR CL600 CL6002B19 EA LEAKING A COMA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 SO 01 982CA 9808 7168 R/H 14TH STAGE DUCT WARNING MESSAGE AND ANTI-ICE DUCT WARNING.FOUND 14TH STAGE BLEED VALVE LEAKING, REMOVED AND REINISTA LLED VALVE. 2 L 7 2 4F RT A21EA 2001070500072 20010705 00072 SO 2001 7 5 ASOA01073 1 20010612 A 5311 FRAME EMB 120 EMB120 3260201 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 257AS 120126 DURING INSPECTION IN TXK, MAINTENANCE FOUND CORROSION ON FRAME 21 IN BETWEEN STRINGER 19 RIGHT AND 19 LEFT. MAINTENANCE REPAIRED CORROSION IAW ASA EO 120-53-0159, WHICH OUTLINE THE REPAIR SPECIFICATIONS FOR THIS OCCURRENCE. (M) 2 L 7 2 4T RT A31SO 2001070500073 20010705 00073 NM 2001 7 5 EIA2001224 1 20010504 A 5753 YOKE BOEING 747 747SR46 NM T/E FLAP FAILED A EIAA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 NM 09 478EV 21033 MZJ-EAC - DURING C-CHECK, CHAFING DAMAGE IN THE AREA OF MID FLAP CARRIAGE DUE TO FAILURE OF YOKE ON LEFT INBOARD MID FLA P. REPAIRED PER ECRA 478-57-103-1. (M) 2 L 7 4 4F A20WE 2001070500074 20010705 00074 NM 2001 7 5 EIA2001225 1 20010516 A 2810 SUMP BOEING 747 747128 1384894 NM RT FUEL TANK LEAKING A EIAA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 NM 09 3203Y 19751 KSEA - AFTER TAKEOFF, STRONG ODOR OF FUEL NOTICED IN COCKPIT FOR SEVERAL MINUTES AFTER FIRST AC PACK NR 1 TURNED ON. RE SEALED LEAKING RIGHT SUMP DRAIN. (M) 2 L 7 4 4F A20WE 2001070500075 20010705 00075 EA 2001 7 5 COMA0160427 1 20010630 A 2750 854D10012 ACTUATOR CNDAIR CL600 CL6002B19 EA BINDING A COMA A UNSCHED LANDING S AFFECT SYSTEMS TO TAKEOFF 1 SO 01 712CA 2287 7244 FLAPS FAILED AT 13 DEGREES.REPLACED THE R/H #4 FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2001070500076 20010705 00076 EA 2001 7 5 COMA0160428 1 20010702 A 2750 852D10011 ACTUATOR CNDAIR CL600 CL6002B19 EA BINDING A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 958CA 8561 1 7111 FLAPS FAILED AT 40 DEGREES.REPLACED THE R/H #1 FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2001070500077 20010705 00077 EA 2001 7 5 COMA0160429 1 20010702 A 2750 854D10012 ACTUATOR CNDAIR CL600 CL6002B19 EA BINDING A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 806CA 13111 7359 FLAPS FAILED AT 30 DEGREES.REPLACED THE R/H #4 FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2001070500078 20010705 00078 NM 2001 7 5 EIA2001226 1 20010517 A 3610 1896801 COOLER BOEING 747 747121 1384871 NM NR 3 ENGINE CRACKED A EIAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 480EV 20348 KLAX - ON CLIMB-OUT, NR 3 ENGINE A/B FIRE LOOP INDICATORS ROSE INTO UPPER BAND. FIRE WARNING LIGHTS, NR 3 FIRE SWITCH, AND FIRE WARNING BELL SOUNDED INTERMITTENTLY. ENGINE FIRE CHECKLIST ACCOMPLISHED. FIRE WARNING LIGHTS EXTINGUISHED, NO FIRE BOTTLE DISCHARGED. PERFORMED INSPECTION AND T/S. FOUND PRECOOLER CRACK. REPLACED NR 3 ENGINE BLEED AIR PRECOOLE R. SYSTEM CHECK NORMA ON ENGINE RUN-UP. NO FURTHER FIRE WARNING FAULTS NOTED. (M) 2 L 7 4 4F A20WE 2001070500079 20010705 00079 NM 2001 7 5 EIA2001227 1 20010517 A 2612 FIRE LOOP BOEING 747 747121 1384871 NM NR 3 ENGINE CHAFED A EIAA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 480EV 20348 KLAX - ON CLIMB-OUT, NR 3 ENGINE A/B FIRE DETECTION LOOP INDICATORS FLUCTUATED UP AND DOWN FULL SCALE. FIRE DETECTION L IGHT ON. REDUCED NR 3 THRUST LEVER, LIGHT EXTINGUISHED, LOOP INDICATIONS WENT TO NORMAL. FOUND NR 3 ENGINE FUEL COND M OTOR AND BOTH A/B LOOP WIRING CHAFING TOGETHER. REPAIRED WIRES. RAN ENGINE TO 1.31 EPR, SYSTEM CHECK NORMAL. (M) 2 L 7 4 4F A20WE 2001070500080 20010705 00080 WP 2001 7 5 EIA2001228 1 20010517 A 3260 WARNING LIGHT DOUG DC9 DC933F 302207A WP COCKPIT ILLUMINATED A EIAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 933F 47191 FLT 9161 - KMZJ - DURING CLIMB, GEAR DOOR OPEN LIGHT ILLUMINATED. CYCLED GEAR DOWN, LIGHT REMAINED ILLUMINATED. GEAR C YCLED UP, LIGHT EXTINGUISHED. (M) 2 L 7 2 4F A6WE 2001070500081 20010705 00081 WP 2001 7 5 EIA2001229 1 20010517 A 2613 WARNING LIGHT DOUG DC9 DC933F 302207A WP COCKPIT ILLUMINATED A EIAA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 NM 09 933F 47191 FLT 9172 - KMZJ - ON CLIMB, TAIL COMPARTMENT TEMP HIGHT LIGHT ILLUMINATED. EMERGENCY CHECK COMPLETED. RETURNED TO MZJ. (M) 2 L 7 2 4F A6WE 2001070500082 20010705 00082 NM 2001 7 5 EIA2001230 1 20010517 A 2611 69B464751 SMOKE DETECTOR BOEING 747 747273C 1384896 NM CABIN MALFUNCTIONED A EIAA O OTHER N FALSE WARNING AP APPROACH 1 NM 09 470EV 20653 KJFK - ALL MAIN DECK SMOKE DETECTOR LIGHT ILLUMINATED INTERMITTENTLY. NO SMOKE DETECTED IN AIRCRAFT. REPLACED MAIN DEC K SMOKE DETECTOR MODULE. (M) 2 L 7 4 4F A20WE 2001070500083 20010705 00083 GL 2001 7 5 ERA2001F00000 2 20010521 A 7321 3300588 FUEL CONTROL CVAC 340 34031 2422704 WP ALLSN 501D 501D13H 03004 GL LT ENGINE MALFUNCTIONED A ERAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 569JA 69 LEFT ENGINE SHUTDOWN IN CRUISE DUE TO POWER DROPPING OFF, POWER LEVER ADVANCE HAD NO EFFECT. MADE UNEVENTFUL LANDING AN C. REPLACED NR 1 ENGINE FUEL CONTROL UNIT. GROUND OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4R 4 T 6A6 E282 2001070500084 20010705 00084 NM 2001 7 5 GAIA01209ST 1 20010611 A 5330 SKIN BOEING 727 727251 138408H NM FUSELAGE BULGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT BULGING SKIN ALONG LAP SEAM BS 1130-1148 STRINGER 3-4L. ACCOMPLISHED FU SELAGE SKIN REPAIR BS 1130-1148 STRINGER 3-4L IAW B727 SRM 53-30-3 FIG 1. (M) 2 L 7 3 4F A3WE 2001070500085 20010705 00085 NM 2001 7 5 GAIA01214ST 1 20010611 A 5320 STRINGER CLIP BOEING 727 727251 138408H NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT STRINGER CLIPS AT BS 990 STRINGER 7, 8, 9L AND 660 STRINGER 8, 9R AND 68 0 STRINGER 7R AND 700 STRINGER 9R ARE CRACKED. ACCOMPLISHED STRINGER CLIP REPLACEMENT AT BS 990 STRINGER 7, 8, 9R AND 6 60 STRINGER 8, 9R AND 680 STRINGER 7R AND 700 STRINGER 9R IAW B727 SRM 51-30-2. (M) 2 L 7 3 4F A3WE 2001070500086 20010705 00086 NM 2001 7 5 GAIA01215ST 1 20010611 A 5210 SKIN BOEING 727 727251 138408H NM L1 DOOR CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE L1 DOOR FORWARD LOWER SKIN WAS CRACKED, FORWARD LOWER CORNER. ACCOM PLISHED L1 DOOR EXTERNAL SKIN REPAIR LOWER FORWARD CORNER IAW B727 SRM 52-00-30. (M) 2 L 7 3 4F A3WE 2001070500087 20010705 00087 NM 2001 7 5 GAIA01238ST 1 20010511 A 3350 LIGHT BOEING 727 727224 1384076 NM CABIN NOT SEATED A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 79748 22450 MAINTENANCE FOUND EMERGENCY EXIT LIGHTS INOPERATIVE. FOUND LIGHT ASSEMBLY NOT SEATED IN CONNECTOR. REINSTALLED AND OPER ATIONALLY CHECKED SYSTEM. SYSTEM CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001070500088 20010705 00088 NM 2001 7 5 GAIA01239ST 1 20010521 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A ROUTINE MAINTENANCE INSPECTION, IT WAS DISCOVERED THAT THE FLOORBEAM AT BS 1030, RBL 34.5 WAS CORRODED OUT OF L IMITS. REPAIRED FLOORBEAM AT BS 1030, RBL 34.5 IAW BOEING 727 SRM 53-10-8, FIGURE 3. THE AIRCRAFT WAS RETURNED TO SERV ICE. (M) 2 L 7 3 4F A3WE 2001070500089 20010705 00089 NM 2001 7 5 GAIA01240OP 1 20010523 A 3260 H1010153 SWITCH BOEING 727 727224 1384076 NM NLG DIRTY A GAIA K NONE N FALSE WARNING AP APPROACH 1 SW 07 69735 20664 FLT 2011 - PDX-MHR - DURING APPROACH, THE GEAR WAS SELECTED TO THE DOWN POSITION. ALL THREE GREEN LIGHTS ILLUMINATED AN D THE NOSE GEAR LIGHT WENT OUT AND DID NOT COME BACK ON. THE FLIGHT CREW DECLARED EMERGENCY, VERIFIED NOSE GEAR POSITIO N THROUGH THE VIEWING PORT AND LANDED. THE AIRCRAFT LANDED AT MHR WITHOUT ANY FURTHER DIFFICULTIES. CLEANED THE NOSE G EAR DOWN AND LOCKED SWITCH. PERFORMED A RETRACTION AND EXTENSION. OPS CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERV ICE. (M) 2 L 7 3 4F A3WE 2001070500090 20010705 00090 NM 2001 7 5 GAIA01241OPS 1 20010525 A 2781 CONNECTOR BOEING 727 727223 1384074 NM L/E FLAP DIRTY A GAIA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 6816 19491 FLT 718 - ELP - ON CLIMB-OUT, FLAPS RETRACTED NORMALLY. THEN AMBER 'L/E FLAPS' LIGHT ILLUMINATED AT 8,000 FT CONFIRMED DOWN L/E NR 6 ON FE PANEL. LOWERED FLAPS AT 230 KIAS TO 2 DEGREES WITH NORMAL GREEN LIGHT AN NO AMBER. RETRACTED AND ' L/E FLAPS' REMAINED AMBER. RECYCLED AGAIN WITH WING ANTI-ICE ON. 'L/E AMBER LIGHT EXTINGUISHED. AIRCRAFT MADE AN UNEV ENTFUL RETURN TO ELP. DISCONNECTED AND CLEANED LEADING EDGE NR 6 FLAP CANNON PLUG AND RE-SECURED. LOWERED AND RETRACTE D FLAPS. LEADING EDGE FLAPS TEST LIGHTS GOOD. OPERATIONAL TEST GOOD ON GROUND. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001070500091 20010705 00091 NM 2001 7 5 GAIA01242OP 1 20010615 A 2613 CLAMP BOEING 727 727214 138407R NM OVERHEAT SYS LOOSE A GAIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 750US 21512 FLT 707 - PHX-OKC - LOWER AFT BODY HEAT LIGHT ILLUMINATED IN FLIGHT. FOLLOWED PROCEDURE. AIRCRAFT MADE AN UNEVENTFUL R ETURN TO PHX. INSPECTED LEFT AND RIGHT PACK BAYS. INSPECTED AFT AIR STAIR AREA AND FOUND LOOSE CLAMP ON FIRE LOOP LEFT FORWARD LOWER SIDE OF AIR STAIR. RAN ENGINES AND RAN BOTH PACKS. NO AIR LEAKS FOUND. BODY OVERHEAT LIGHT DID NOT ILL UMINATE. SYSTEM OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001070500092 20010705 00092 WP 2001 7 5 GTIA010363 1 20010514 A 3350 111397605 COVER DOUG DC9 DC982 3022082 WP CABIN CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 DTW - LEFT AND RIGHT EMERGENCY DOOR LIGHT COVER CRACKED, EXIT. REMOVED AND REPLACED LEFT AND RIGHT EMERGENCY DOOR LIGHT COVER IAW MD80 MM 33-21-00. (M) 2 L 7 2 4F A6WE 2001070500093 20010705 00093 WP 2001 7 5 GTIA010391 1 20010518 A 5753 SKIN DOUG DC9 DC932 3022066 WP T/E FLAP DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 133NK 48111 DTW - REFERENCE CARRY OVER NR 0001551-2 TRAILING EDGE SHOW SIGN OF DELAMINATION. REPAIR TRAILING EDGE IAW DC-9 SRM 51-7 0 THIS CLEARS CARRY OVER 0001551-2. (M) 2 L 7 2 4F A6WE 2001070500094 20010705 00094 WP 2001 7 5 GTIA010392 1 20010519 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 809NK 49503 DTW - EMERGENCY FLOOR TRACK LIGHTING OUT AT FIRST OVERWING EXIT. RELAMPED EMERGENCY FLOOR TRACK LIGHTING IAW MD-80 MM 3 3-53-00. OPS CHECK GOOD, NO DEFECTS NOTED AT THIS TIME. (M) 2 L 7 2 4F RT A6WE 2001070500095 20010705 00095 WP 2001 7 5 GTIA010395 1 20010514 A 5751 59554162 AILERON DOUG DC9 DC987 3022087 WP RT WING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 807NK 49777 FLL - FLT 1181 - RIGHT AILERON T/E BETWEEN BOTH TRIM TABS HAS 3 INCH CRACK IN FAIRING. CLEANED AREA AND APPLIED SPEED T APE PER MD-80 SRM 51-02 PAGE 1 PARA A ITEM ON CARRY OVER REFERENCE CONTROL NR 002000-2. REMOVED AND REPLACED RT WING AI LERON TRAILING EDGE PANEL PER 51-02 THIS CLEARS C/O 0022000-2. (M) 2 L 7 2 4F RT A6WE 2001070500096 20010705 00096 WP 2001 7 5 GTIA010400 1 20010519 A 3231 DOOR DOUG DC9 DC931 3022065 WP NLG OUT OF RIG A GTIA O OTHER E VIBRATION/BUFFET CL CLIMB 1 GL 23 969ML 47268 ACY - FLT 8055 - AIR RETURN, AFTER TAKEOFF DURING GEAR RETRACTION HAD 'EXTREME' VIBRATION, RECYCLED GEAR WITH NO RESOLVE . RERIGGED NLG DOOR RT SIDE AND INSTALLED SHIMS IN INBOARD BRACKET. NLG SWING IAW DC9 MM 32-22-01. OPS CHECK NORMAL. NO DEFECTS FOUND AT THIS TIME. (M) 2 L 7 2 4F A6WE 2001070500097 20010705 00097 WP 2001 7 5 GTIA010401 1 20010519 A 3260 TARGET DOUG DC9 DC981 3022081 WP LANDING GEAR OUT OF ADJ A GTIA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 806NK 48051 FLT 460 - EWR - GEAR DOOR OPEN LIGHT CAME ON IN FLIGHT, WENT OUT WITH HYD IN HIGH. ADJUSTED PROX SENSORS TARGET IAW MM 32-60-05, GEAR WARNING SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2001070500098 20010705 00098 WP 2001 7 5 GTIA010402 1 20010520 A 3260 PROXIMITY SENSOR DOUG DC9 DC981 3022081 WP LT MLG DOOR OUT OF ADJ A GTIA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 806NK 48051 EWR - FLT 1456 - GEAR DOOR LIGHTS STAYS ON. AFTER GEAR RAISED LIGHT GOES OUT, WHEN HYD SWITCHED TO LOW LIGHT ON, STAYED ON AND FLICKERING IN FLIGHT. READJUSTED LEFT MLG DOOR PROX SENSOR IAW MM 32-60-05. OPS CHECK GEAR WARNING SYSTEM SEVE RAL TIMES. OPS NORMAL. (M) 2 L 7 2 4F A6WE 2001070500099 20010705 00099 WP 2001 7 5 GTIA010403 1 20010518 A 8011 38334211 STARTER DOUG DC9 DC981 3022081 WP LT ENGINE FAULTY A GTIA E ENGINE SHUTDOWN O OTHER TX TAXI/GRND HDL 1 GL 23 810NK 48015 ORD - ABORTED START ON LEFT ENGINE MAX, EGT 500 DEGREE TEMP RISE WAS VERY RAPID BEFORE ABORT, MAX N2 BEFORE FUEL WAS PLA CED ON 20 PERCENT PNEUMATIC PRESS -40 PSI NORMAL FUEL FLOW. REMOVED AND REPLACED LEFT ENGINE STARTER AND START VALVE, E NGINE RUN CHECKS GOOD WITH NORMAL PARAMETERS IAW MM 80-00-00. (M) 2 L 7 2 4F A6WE 2001072400241 20010724 00241 NM 2001 7 24 2001UALA01140 1 20010623 A 7920 FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE CRACKED A UALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION DE DESCENT 1 WP 29 374UA 24639 720925 NR 2 ENGINE SHUTDOWN IN-FLIGHT DUE TO LOW OIL PRESSURE INDICATION. *S/D* FOUND CRACKED 90 DEGREE ELBOW FITTING ON THE OIL PRESSURE LINE FROM THE OIL PRESSURE TRANSMITTER TO THE TRANSFER GEARBOX. THE FITTING WAS REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001070500100 20010705 00100 WP 2001 7 5 GTIA010404 1 20010518 A 3260 TARGET DOUG DC9 DC981 3022081 WP LANDING GEAR CONTAMINATED A GTIA K NONE O OTHER CR CRUISE 1 GL 23 806NK 48051 FLT 460 - EWR - GEAR DOOR OPEN LIGHT ON IN FLIGHT, WENT OUT WITH HYD IN HIGH POSITION. NO OTHER UNSAFE CONDITIONS PRESE NT IN GEAR HANDLE. CLEANED GEAR DOOR SWITCH FOUND GREASE ON TARGET, ACCOMPLISHED PROXIMITY TEST OF GEAR DOOR WIRING, NO DEFECTS NOTED. OPS CHECK OF GEAR WARNING SYSTEM OK IAW MM 32-60-05. (M) 2 L 7 2 4F A6WE 2001070500101 20010705 00101 NM 2001 7 5 2001UALA01166 1 20010624 A 5330 BOEING 6546921528 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE OUTER SKIN DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 1537 23951 FWD CARGO DOOR HAS NUMEROUS DENTS BEYOND LIMITS. CUT OUT DENTED AREAS AND INSTALLED EXTERNAL DOUBLER. MAJOR REPAIR ACCO MPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001072400343 20010724 00343 NM 2001 7 24 2001UALA01167 1 20010625 A 2163 123CH1A SENSOR BOEING 737 737322 1384676 NM E/E BAY FAULTY A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 307UA 23668 UNSCHEDULED LANDING DUE TO EQUIPMENT COOLING EXHAUST WARNING. *S/D* M100 AVIONICS COOLING SENSOR FAILED. REPLACED THE AVIONICS COOLING SENSOR. 2 L 7 2 4F RT A16WE 2001070500102 20010705 00102 EU 2001 7 5 2001UALA01196 1 20010620 A 5751 D5764000000300 AILERON AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE A UALA O OTHER C F.O.D. IN INSP/MAINT 1 WP 29 451UA 865 RH AILERON ASSEMBLY UPPER SKIN DAMAGE BY HAIL RESULTING IN A DENT 1 INCH IN DIAMETER ON THE UPPER SKIN, .5 INCHES FROM T HE INBOARD EDGE AND 5 INCHES FROM THE TRAILING EDGE. THERE IS ALSO A CRACK AT THE BOTTOM OF THE DENT MEASURING .5 INCHE S LONG. ACCOMPLISHED COMPOSITE REPAIR OF THE RH AILERON ASSEMBLY. THIS WAS A MAJOR REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2001070500103 20010705 00103 NE 2001 7 5 2001UALA01199 2 20010627 A 7321 SENSE LINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LOOSE A UALA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 29 560UA 26660 ABORTED TAKEOFF DUE TO LOSS OF POWER ON RIGHT ENGINE. BURNER SENSE LINE LOOSE.SECURED SENSE LINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001070500104 20010705 00104 WP 2001 7 5 GTIA010423 1 20010523 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP TAIL CONE DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 800NK 49144 FLL - WHILE PERFORMING WORK CARD 00409 OF A2 CHECK, FOUND TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED TAIL CONE EMERGENCY BATTERY PACK B5-28 AND SECURED LOGIC CIRCUIT GROUND WIRES TO TERM 3 OF BOTH B527 AND B5-28 BATTERY P ACKS, OPS CHECK OK IAW A2 CHK TASK CARD 00409. (M) 2 L 7 2 4F A6WE 2001070500105 20010705 00105 WP 2001 7 5 GTIA010460 1 20010526 A 3350 LIGHT DOUG DC9 DC981 3022081 WP A/C BAY INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 SW 21 819NK 48016 FLL - FLT 171 - TAIL COMP EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BULB IN TAIL FOR EMERGENCY LIGHTS IAW MM C HAPTER 33-53-00. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2001070500106 20010705 00106 WP 2001 7 5 GTIA010461 1 20010529 A 2720 7912647525 LIMITER DOUG DC9 DC982 3022082 WP RUDDER CRACKED A GTIA O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 800NK 49144 FLT 931 - MCO - AT 200 KTS AND 31,000 FT, THE RUDDER TRAVEL UNRESTRICTED LIGHT ILLUMINATED. FOLLOWED QRH PROCEDURES AND LANDED UNEVENTFULLY AT 320 KTS IN DESCENT LIGHT EXTINGUISHED. FOUND HARD LINE FROM SUMP CAN TO RUDDER THROW LIMITER BE LLOWS CRACKED. REPLACED WITH FLEX LINE AND OPS CHECKED PER MM 27-20-06. NO DEFECTS NOTED AT THIS TIME. (M) 2 L 7 2 4F A6WE 2001070500107 20010705 00107 2001 7 5 GTIA010466 4 20010531 A 2230 AUTOTHRUST SYS DOUG DC9 DC982 3022082 WP COCKPIT MALFUNCTIONED A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 812NK 48021 FLT 1268 - ACY - AUTO THROTTLES DISCONNECTED WITHOUT COMMAND. TRIED TO RE-ENGAGE AND WOULD NOT STAY ENGAGED. SWITCHED TO NR 2 DFGC AND CADC BOTH ON 2 AND AUTOTHROTTLES REMAINED ENGAGED FOR A WHILE. DURING CLIMB, THE FMA SWITCHED BETWEEN EPR CLIMB CLAMP. ALSO, A/C WOULD NOT CLIMB AT THE SAME SPEED THAT WAS SELECTED IN THE IAW/MACH ANNUNCIATOR. SWITCHED F O CMD TO BOTH ON NR 1 AND CADC BOTH ON NR 2, AND DFGC ON NR 2 AND ALL SYSTEMS WORKED NORMAL. PERFORMED DFGC 1 AND 2 RET URN TO SERVICE CHECK IAW MC-80 MM 22-01-05. NO FAULT FOUND AND SYSTEMS OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2001070500108 20010705 00108 WP 2001 7 5 GTIA010467 1 20010601 A 3350 60030451 POWER SUPPLY DOUG DC9 DC982 3022082 WP COCKPIT DEFECTIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 817NK 49141 RSW - FOUND COCKPIT LIGHTS EMERGENCY OVERHEAD LIGHTS INOPERATIVE. FOUND BAD CONTACT IN POWER SUPPLY. REMOVED AND REPLA CED POWER SUPPLY AS REQUIRED PER MD-80 MM 33-53-00. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2001070500109 20010705 00109 WP 2001 7 5 GTIA010489 1 20010603 A 2613 WARNING LIGHT DOUG DC9 DC983 3022083 WP COCKPIT FALSE INDICATION A GTIA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 602CA 49415 ORD - FLT 1781 - DURING CLIMB-OUT OF LAX, THE TAIL COMPARTMENT TEMP HI LIGHT CAME ON. QRH PROCEDURES OF CHECKING PNEU X FEEDS CLOSED, ANTI-ICING OFF AND SWITCHING A/C SUPPLY'S TO HP BLEED OFF WAS ACCOMPLISHED. THE LIGHT FLICKERED ON AND OF F FOR ABOUT 1.5 MINUTES AND THEN STAYED OFF. AFTER LOOKING AT MEL, TURNED RIGHT A/C SUPPLY TO AUTO. TAIL COMP TEMP HI LIGHT REMAINED OFF. INSPECTED TAIL COMPARTMENT FOR PNEUMATIC LEAKS, SECURITY OF COMPARTMENT SENSOR AND OPERATION OF CHE CK VALVE ON LEFT AND RIGHT SIDE WARNING LIGHT NO ILLUMINATED AT THIS TIME, 36-20-01. NO DEFECTS NOTED. (M) 2 L 7 2 4F RT A6WE 2001070500110 20010705 00110 WP 2001 7 5 GTIA010490 1 20010603 A 3350 LIGHT DOUG DC9 DC982 3022082 WP A/C BAY INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 801NK 48048 FLL - FOUND TWO OVERHEAD EMERGENCY LIGHTS INOPERATIVE IN TAIL COMPARTMENT. REPAIRED WIRE ON FORWARD LAMP AND RELAMPED A FT LIGHT, OPS CHECK NORMAL IAW MM 33-50-00. (M) 2 L 7 2 4F A6WE 2001070500111 20010705 00111 WP 2001 7 5 GTIA010492 1 20010602 A 3350 BATTERY DOUG DC9 DC981 3022081 WP A/C BAY DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 819NK 48016 FLL - FLT 779 - TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES FOR TAIL COMPARTMENT EMERGENCY LIGHTS . OPS CHECK NORMAL IAW MM 33-50-00 AND 33-53-01. (M) 2 L 7 2 4F A6WE 2001070500112 20010705 00112 WP 2001 7 5 GTIA010494 1 20010601 A 2740 SWITCH DOUG DC9 DC981 3022081 WP HORIZ STAB DEFECTIVE A GTIA O OTHER F FLT CONT AFFECTED IN INSP/MAINT 1 GL 23 805NK 48058 FLT 1337 - LGA - DURING PREFLIGHT, THE RIGHT LEVER ACTUATED THE ALTERNATE TRIM MOTOR WITH THE LEFT HALF IN THE NEUTRAL P OSITION. THIS ALLOWED EITHER NOSE UP OR NOSE DOWN TRIM USING ONLY THE RIGHT HALF. T/S TO ALTERNATE LONGITUDINAL TRIM B RAKE CONTROL SWITCH. REMOVED AND REPLACED SWITCH S10-8 AS PER MM 27-40-09. OPS CHECK NORMAL, OK FOR SERVICE. (M) 2 L 7 2 4F A6WE 2001070500113 20010705 00113 WP 2001 7 5 GTIA010497 1 20010604 A 3350 20131A BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 133NK 48111 ACY - EMERGENCY PATH LIGHTING NOT TURNING ON. REMOVED AND REPLACED BATTERY PACK, IAW DC-9 MM 33-53-01, OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2001070500114 20010705 00114 WP 2001 7 5 GTIA010510 1 20010411 A 5523 SKIN DOUG DC9 DC983 3022083 WP CONTROL TAB DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 RIGHT CONTROL TAB HAS DELAMINATION ON THE BOTTOM (MARKED IN RED) DOT NR 005. REMOVED AREAS OF DELAMINATION IAW DC-9 MM. FABRICATED REPAIR DOUBLER IAW DC-9 MM MD 80 SRM 55-04. INSTALLED DOUBLER IAW DC-9 MD-80 SRM 55-04. WEIGHED AND BALAN CED TAB PER BOEING. (M) 2 L 7 2 4F RT A6WE 2001070500115 20010705 00115 WP 2001 7 5 GTIA010513 1 20010611 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 GL 23 804NK 49104 DTW - FOUND EMERGENCY FLOOR TRACK LIGHTS LAST TWO IN THE BACK INOPERATIVE. FOUND BROKEN EMERGENCY FLOOR TRACK WIRE. RE PAIRED WIRE ON LAST TWO EMERGENCY FLOOR TRACK LIGHTS. OPS CHECK GOOD, IAW MD-80 MM CHAPTER 33-50-01. (M) 2 L 7 2 4F A6WE 2001070500116 20010705 00116 WP 2001 7 5 GTIA010533 1 20010608 A 5280 5914985202 DOOR DOUG DC9 DC931 3022065 WP NLG DAMAGED A GTIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 23 969ML 47268 ACY - FLT 8157 - ON GEAR RETRACTION LOUD THUMP IN NOSE GEAR FOLLOWED BY VIBRATION APPARENTLY CAUSED BY NOSE GEAR DOORS. RETURNED TO AIRPORT. REPLACED RIGHT NOSE GEAR DOOR ASSEMBLY ON PERFORMED OPS IAW DC9 MM 32-22-01 PAGE 201-205. OPS CH ECK GOOD, NO DEFECTS NOTED. (M) 2 L 7 2 4F A6WE 2001070500117 20010705 00117 CE 2001 7 5 GUU2001F00000 1 20010424 A 2621 WIRE BEECH 1900 1900D 1154162 CE FIRE BOTTLE LOOSE A O OTHER N FALSE WARNING CR CRUISE 1 SO 19 81536 UE152 FLT 9453 - NAS-MIA - DURING FLIGHT, LEFT ENGINE FIRE BOTTLE DISCHARGE LIGHT ILLUMINATED. SECURED WIRE AT LEFT ENGINE FI RE BOTTLE. (M) 2 L 7 2 4T RT A24CE 2001070500118 20010705 00118 2001 7 5 GUU2001F00002 4 20010324 A 2360 10138005311 STATIC WICK BEECH 1900 1900C 1154161 CE RT WING DEFECTIVE A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 19 139GA UC126 FLT 9253 - FLL/FPO - PASSENGER REPORTED SPARKS COMING FROM TOP OF RIGHT WING OUTBOARD OF ENGINE NEXT TO INSPECTION PLATE . REMOVED AND REPLACED BAD STATIC WICKS. ALSO, REMOVED AND REPLACED NR 2 INVERTER. (M) 2 L 7 2 4T RT A24CE 2001070500119 20010705 00119 CE 2001 7 5 GUU2001F00003 1 20010422 A 3260 SQUAT SWITCH BEECH 1900 1900C 1154161 CE LANDING GEAR OUT OF ADJ A GUUA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 19 147GA UC86 FLT 9230 - NAS/FLL - DURING FLIGHT, LEFT PROPELLER GOES INTO GROUND FINE PRIOR TO LANDING WITH POWER STILL ON LEFT ENGIN E. RIGGED AND ADJUSTED RIGHT SQUAT SWITCH. (M) 2 L 7 2 4T RT A24CE 2001070500120 20010705 00120 CE 2001 7 5 GUU2001F00004 1 20010423 A 6120 VALVE BEECH 1900 1900C 1154161 CE LT PROPELLER OUT OF ADJ A GUUA O OTHER O OTHER CR CRUISE 1 SO 19 138GA UC138 FLT 2050 - FLL - DURING FLIGHT, LEFT PROPELLER GOES TO GROUND FINE WITH POWER AT FLIGHT IDLE. ADJUSTED LEFT PROPELLER B ETA VALVE. (M) 2 L 7 2 4T RT A24CE 2001070500121 20010705 00121 CE 2001 7 5 GUU2001F00005 1 20010410 A 5520 1016200111 HINGE BRACKET BEECH 1900 1900C 1154161 CE LT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 141UE UC141 DURING SCHEDULED MAINTENANCE, LEFT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANUL AR CORROSION. REMOVED AND REPLACED LEFT ELEVATOR OUTBOARD HINGE BRACKET. (M) 2 L 7 2 4T RT A24CE 2001070500122 20010705 00122 CE 2001 7 5 GUU2001F00006 1 20010410 A 5520 1016200111 HINGE BRACKET BEECH 1900 1900C 1154161 CE RT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 141UE UC141 DURING SCHEDULED MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANU LAR CORROSION. REMOVED AND REPLACED RIGHT ELEVATOR OUTBOARD HINGE BRACKET. (M) 2 L 7 2 4T RT A24CE 2001070500123 20010705 00123 CE 2001 7 5 GUU2001F00007 1 20010425 A 5520 1016200131 HINGE BRACKET BEECH 1900 1900 1154160 CE ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 194GA UB8 DURING SCHEDULED MAINTENANCE, RIGHT CENTER ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS ON INTERGRANULA R CORROSION. REMOVED AND REPLACED RIGHT ELEVATOR CENTER HINGE BRACKET. (M) 2 L 7 2 4T RT A24CE 2001070500124 20010705 00124 CE 2001 7 5 GUU2001F00008 1 20010425 A 5520 1016200111 HINGE BRACKET BEECH 1900 1900 1154160 CE ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 194GA UB8 DURING SCHEDULED MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANU LAR CORROSION. REMOVED AND REPLACED RIGHT ELEVATOR OUTBOARD HINGE BRACKET. (M) 2 L 7 2 4T RT A24CE 2001070500125 20010705 00125 NM 2001 7 5 01FDEA00516 1 20010704 A 2613 322861001 VALVE BOEING 727 727225 1384077 NM AIR STAIR FAILED A FDEA O OTHER J WARNING INDICATION CR CRUISE 1 SO 25 461FE 22548 01-218 LWR AFT BODY OVERHEAT LIGHT ILLUM. ACCOMPLISH RED TAB PROC. LIGHT WENT OUT FOLLOWING CLOSING #3 BLD AIR VALVE. LEAK BETWEEN #3 BLD AIR VALVE & RH PACK VALVE. R&R LEFT PURGE VALVE PER MM 36-13-011. OPS CK GOOD. 2 L 7 3 4F A3WE 2001070500126 20010705 00126 CE 2001 7 5 GUU2001F00009 1 20010424 A 5520 1016200131 HINGE BRACKET BEECH 1900 1900C 1154161 CE ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 199GA UB13 DURING SCHEDULED MAINTENANCE, LEFT CENTER ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANULAR CORROSION. REMOVED AND REPLACED LEFT ELEVATOR CENTER HINGE BRACKET. (M) 2 L 7 2 4T RT A24CE 2001070500127 20010705 00127 CE 2001 7 5 GUU2001F00010 1 20010424 A 5520 1016200111 HINGE BRACKET BEECH 1900 1900C 1154161 CE ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 199GA UB13 DURING SCHEDULED MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANU LAR CORROSION. REMOVED AND REPLACED RIGHT ELEVATOR OUTBOARD HINGE BRACKET. (M) 2 L 7 2 4T RT A24CE 2001070500128 20010705 00128 CE 2001 7 5 GUU2001F00011 1 20010423 A 5520 1016200111 HINGE BRACKET BEECH 1900 1900C 1154161 CE ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 38011 UC9 DURING SCHEDULED MAINTENANCE, LEFT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANUL AR CORROSION. REMOVED AND REPLACED LEFT ELEVATOR OUTBOARD HINGE BRACKET. (M) 2 L 7 2 4T RT A24CE 2001070500129 20010705 00129 CE 2001 7 5 GUU2001F00012 1 20010425 A 3310 8545AT33L SWITCH BEECH 1900 1900D 1154162 CE COCKPIT SPARKS A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 19 17534 UE141 FLT 5401 - FPO-FLL - DURING FLIGHT WHEN THE MASTER PANEL LIGHT SWITCH WAS TURNED ON, A SPARK AND SMOKE WAS OBSERVED. RE MOVED AND REPLACED MASTER LIGHT SWITCH. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4T RT A24CE 2001070500130 20010705 00130 CE 2001 7 5 GUU2001F00013 1 20010428 A 7933 1303800455 INDICATOR BEECH 1900 1900D 1154162 CE COCKPIT FAULTY A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 19 53545 UE185 FLT 9507 - EYW-TPA - DURING FLIGHT, LEFT ENGINE OIL TEMPERATURE WENT TO 130 DEGREES AND BANGING NOISES WERE HEARD COMING FROM THE ENGINE. TROUBLESHOT OIL TEMPERATURE SYSTEM. DETERMINED OIL TEMPERATURE INDICTOR TO BE AT FAULT. REMOVED AND REPLACED INDICATOR. PERFORMED ENGINE RUNS, NO BANGING NOISES DETECTED. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4T RT A24CE 2001070500131 20010705 00131 CE 2001 7 5 GUU2001F00015 1 20010509 A 5520 1016200111 HINGE BRACKET BEECH 1900 1900C 1154161 CE ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 143GA 22814 UC145 DURING SCHEDULED MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANU LAR CORROSION. REMOVED AND REPLACED RIGHT ELEVATOR OUTBOARD HINGE BRACKET. (M) 2 L 7 2 4T RT A24CE 2001070500132 20010705 00132 CE 2001 7 5 GUU2001F00016 1 20010502 A 5520 1016200131 HINGE BRACKET BEECH 1900 1900C 1154161 CE ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 147GA 26069 UC86 DURING SCHEDULED MAINTENANCE, RIGHT CENTER ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANULA R CORROSION. REMOVED AND REPLACED RIGHT ELEVATOR CENTER HINGE BRACKET. (M) 2 L 7 2 4T RT A24CE 2001070500133 20010705 00133 CE 2001 7 5 GUU2001F00017 1 20010502 A 5520 1016200111 HINGE BRACKET BEECH 1900 1900C 1154161 CE ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 147GA 26068 UC86 DURING SCHEDULED MAINTENANCE, LEFT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANUL AR CORROSION. REMOVED AND REPLACED LEFT ELEVATOR OUTBOARD HINGE BRACKET. (M) 2 L 7 2 4T RT A24CE 2001070500134 20010705 00134 CE 2001 7 5 JJB2001F00000 1 20010427 A 2150 19357222 PACKING BEECH 1900 1900D 1154162 CE A/C PACK ODOR A JJBA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 01 848CA UE53 ODOR IN CABIN DURING CLIMB-OUT. REPLACED PACKING. REFRIGERATION PACK TIME CHANGED. (M) 2 L 7 2 4T RT A24CE 2001070500135 20010705 00135 EA 2001 7 5 MASA01042 1 20010513 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17275 7275 DURING OVERNIGHT MAINTENANCE, IT WAS DISCOVERED THAT THE NR 4 CEILING EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MAINTENANC E REMOVED AND REPLACED BULB IAW CRJ AMM 33-51-16. OPS CHECK GOOD, THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001070500136 20010705 00136 NM 2001 7 5 N8T2001F00000 1 20010507 A 3350 FUSE BOEING 757 757236 NM BATTERY PACK BLOWN A N8TA K NONE L NO TEST IN INSP/MAINT 1 WP 19 547NA 29946 EMERGENCY LIGHTS ON SEATS 7 THROUGH 15 INOPERATIVE. REPLACED FUSE IN BATTERY PACK. (M) 2 L 7 2 4F RT A2NM 2001070500137 20010705 00137 NM 2001 7 5 P2EA01093 1 20010611 A 5312 BULKHEAD BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 127NJ 22886 SJO - DURING C-CHECK, INSPECTION PER S/B 737-53A1173, PRESSURE BULKHEAD, BS 178 VERTICAL CHORD CRACKED AT LBL 57 WL 185, PRESSURE BULKHEAD BS 178 RIGHT LATERAL CHORD CRACKED AT WL 207, PRESSURE BULKHEAD, BS 178 LEFT LATERAL CHORD CRACKED AT WL 207. BS 178 FORWARD PRESSURE BULKHEAD VERTICAL CHORD REPAIRED AT LBL 5.7 BETWEEN WL 197 AND 76 DUE TO CRACK IAW SRM 53-10-11 FIG 8. BS 178 FWD PRESSURE BULKHEAD RT CHORD REPAIRED BETWEEN WL 216 AND 185 DUE TO CRACK IAW S/B 737-53A1173 REV 3 SECTION II FIG 60. BS 178 FORWARD PRESSURE BULKHEAD LEFT SIDE CHORD REPAIRED BETWEEN WL 216 AND 185 DUE TO CRACK IAW S/B 737-53A1173 REV 3 SECTION III FIG 60. (M) 2 L 7 2 4F A16WE 2001070500138 20010705 00138 2001 7 5 SWAA011728 4 20010614 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001070500139 20010705 00139 NM 2001 7 5 SWAA011730 1 20010614 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOORBEAM E&E COMP, AT BS 312, WL 208, LBL 11 TO RBL 11. REPAIRED FLOORBEA M PER SRM. 2 L 7 2 4F RT A16WE 2001070500140 20010705 00140 NM 2001 7 5 SWAA011731 1 20010614 A 5250 65C33828 PIN BOEING 737 7373Y0 1384671 NM COCKPIT DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 308SA 23498 COCKPIT DOOR UPPER ESCAPE PANEL FELL OUT. REMOVED AND REPLACED PANEL TOP SHEAR PINS PER MM. 2 L 7 2 4F RT A16WE 2001070500141 20010705 00141 NM 2001 7 5 SWAA011732 1 20010614 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOORBEAM AFT CARGO, BS 767, WL 157, RBL 7.5 TO LBL 17. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2001070500142 20010705 00142 NM 2001 7 5 SWAA011733 1 20010614 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOORBEAMS AFT CARGO AT BS 727D TO BS 847, WL 157, LBL 7.5 TO RBL 2.5. REP AIRED FLOORBEAMS PER SRM. 2 L 7 2 4F RT A16WE 2001070500143 20010705 00143 NM 2001 7 5 SWAA011735 1 20010616 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 386SW 26601 EEPLS INOP AT OVERWING EXIT. RELAMPED EEPLS LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001070500144 20010705 00144 NM 2001 7 5 SWAA011736 1 20010614 A 3397 BR2013 WIRE BOEING 737 7375H4 138449D NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 EEPLS WIRES EXPOSED AT ROW 10. SECURED EEPLS WIRES PER MM. 2 L 7 2 4F RT A16WE 2001070500145 20010705 00145 NM 2001 7 5 SWAA011737 1 20010615 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 353SW 24889 DURING SCHEDULED BC3 CHECK, FOUND EEPLS LOOSE AT AFT CABIN. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001070500146 20010705 00146 NM 2001 7 5 SWAA011738 1 20010616 A 3350 6556633 SIGN BOEING 737 7377H4 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 768SW 30587 EMERGENCY EXIT SIGN MISSING AT LT OVERWING EXIT. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2001070500147 20010705 00147 NM 2001 7 5 SWAA011739 1 20010616 A 3350 BR2013 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 636WN 27709 EEPLS COVERS LOOSE. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001070500148 20010705 00148 NM 2001 7 5 SWAA011740 1 20010614 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 647SW 27717 DURING SCHEDULED C4 CHECK, FOUND EEPLS LOOSE AT ROWS 8 & 9. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001070500149 20010705 00149 2001 7 5 SWAA011741 4 20010614 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 647SW 27717 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUSTMENT. ADJUSTED SLIDE ASSY P ER MM. 2 L 7 2 4F RT A16WE 2001070500150 20010705 00150 NM 2001 7 5 SWAA011744 1 20010617 A 5310 6547977 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 400 TO BS 420, RBL 68 & WL 208. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001070500151 20010705 00151 NM 2001 7 5 SWAA011745 1 20010616 A 2731 183A8100 TAB BOEING 737 7377H4 NM ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 701GS 27836 DURING SCHEDULED SERVICE CHECK, SWA SI 11052-55, FOUND RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2001070500152 20010705 00152 NM 2001 7 5 SWAA011748 1 20010617 A 5320 65C27314 TIE CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 706, STRINGER 11L. REPAIRED TIE CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001070500153 20010705 00153 NM 2001 7 5 SWAA011750 1 20010617 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 737.5, LBL 12 & WL 157. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2001070500154 20010705 00154 NM 2001 7 5 SWAA011752 1 20010617 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED D-CHECK, FOUND FLOORBEAMS CORRODED AT BS 294, RBL 16 WL 208. REPAIRED FLOORBEAMS PER SRM. 2 L 7 2 4F RT A16WE 2001070500155 20010705 00155 NM 2001 7 5 SWAA011753 1 20010618 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 651SW 27721 DURING SCHEDULED PM CHECK, FOUND EEPLS INOP AT MID CABIN. RECONNECTED WIRES PER MM. 2 L 7 2 4F RT A16WE 2001070500156 20010705 00156 NM 2001 7 5 SWAA011754 1 20010617 A 3350 65C27095 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT AFT CABIN. REMOVED AND REPLACED BATTERY PACK PER MM . 2 L 7 2 4F A16WE 2001070500157 20010705 00157 NM 2001 7 5 SWAA011755 1 20010618 A 3397 BR2013 WIRE BOEING 737 7375H4 138449D NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 EEPLS WIRES EXPOSED AT ROW 10. SECURED EEPLS WIRES PER MM. 2 L 7 2 4F RT A16WE 2001070500158 20010705 00158 NM 2001 7 5 SWAA011756 1 20010618 A 3350 101074 SIGN BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 504SW 24181 AFT SVC DOOR EMERGENCY EXIT SIGN LOOSE. SECURED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2001070500159 20010705 00159 NM 2001 7 5 SWAA011757 1 20010617 A 3350 101074 SIGN BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 AFT SVC DOOR EMERGENCY EXIT SIGN LOOSE. SECURED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2001070500160 20010705 00160 NM 2001 7 5 SWAA011758 1 20010616 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM SERVICE DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 344SW 24152 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001070500161 20010705 00161 NM 2001 7 5 SWAA011762 1 20010617 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 312, LBL 9 TO RBL 8. REPAIRED FLOORBEAM PER SWA TI. 2 L 7 2 4F RT A16WE 2001070500162 20010705 00162 NM 2001 7 5 SWAA011763 1 20010617 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 500C, LBL 18 TO RBL 13. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2001070500163 20010705 00163 NM 2001 7 5 SWAA011764 1 20010616 A 5320 6517583 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL WEBS CRACKED AT BS 180, WL 236, LBL 17.1 & WL 183 RBL 5.7. REPAIRED WEBS PE R SRM. 2 L 7 2 4F RT A16WE 2001070500164 20010705 00164 NM 2001 7 5 SWAA011765 1 20010617 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 773, RBL 7.5 TO LBL 2.5. REPAIRED FLOORBEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2001070500165 20010705 00165 NM 2001 7 5 SWAA011766 1 20010614 A 3040 6613907 BRACKET BOEING 737 7375H4 138449D NM WINDOW BROKEN A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 501SW 24178 DECLARED EMERGENCY, TOXIC FUMES IN COCKPIT. SOURCE OF ODOR AT, F/O'S NR 5 EYEBROW WINDOW. SENSOR SPRING BRACKET BROKEN , SPRING SHORTED OUT SENSOR WIRES. CONT PER MEL 30-11. ON 16 JUN AT DAL REMOVED AND REPLACED SPRING BRACKET PER MM. 2 L 7 2 4F RT A16WE 2001070500166 20010705 00166 NM 2001 7 5 SWAA011767 1 20010608 A 2731 6545190 TAB BOEING 737 7373H4 1384600 NM ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED C4 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND ELEVATOR TAB CONTROL MECHANISM PER MM. 2 L 7 2 4F RT A16WE 2001070500167 20010705 00167 EU 2001 7 5 RAIA00107002 1 20010702 A 7710 31056294 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU ZONE 400 INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 552HK 4083 13 41057 7034-STL-LEFT GREEN BETA LIGHT WOULD NOT ILLUMINATE.MAINTENANCE REMOVED AND REPLACED LEFT BETA SWITCH 2 L 7 2 4T RT A41NM 2001070500168 20010705 00168 WP 2001 7 5 ZW0A0104601 1 20010703 A 3350 58222 POWER SUPPLY DOUG DC9 DC982 3022082 WP ROW 29 A ZW0A K NONE O OTHER CR CRUISE 1 CE 13 917TW 49366 INTERMITTANT OPERATION OF PASSENGER EGRESS LIGHTING INFLIGHT ROWS 29-33. REPLACED POWER SUPPLY P/N 5822-2. LAST CHEC K C 06/23/01 STL ---CLOSED--- 2 L 7 2 4F A6WE 2001070500169 20010705 00169 EU 2001 7 5 QXEA0101131 1 20010629 A 2420 SUNDSTRANDEM FOKKER F28 F28MK4000 4990810 EU A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 493US XB837 11161 SEA - CREW REPORTED AND ELECTRICAL BURNING SMELL, FOLLOWED BY THE #2 GENERATOR CAUTION LIGHT ILLUMINATING. REMOVED AND R EPLACED GENERATOR CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001070500170 20010705 00170 2001 7 5 GTIA010528 4 20010617 A 2200 25866863 COMPUTER DOUG DC9 DC932 3022066 WP E/E BAY A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 133NK 48111 DTW - FLT 9951 - AUTO PILOT VERTICAL SPPED WHEN COMMANDED UP OR DOWN THERE IS NO CONTROL UP TO 1500 FT PER MIN GOES DIRE CTLY TO 1500 FT PER MINUTE. REMOVED AND REPLACED PITCH AXIS COMPUTER, OPS CHECKED GOOD PER DC9 MM 22-13-01. NO OTHER D ISCREPANCIES NOTED. (M) 2 L 7 2 4F A6WE 2001070500171 20010705 00171 WP 2001 7 5 GTIA010519 1 20010612 A 3350 60030451 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 DALLO 53012 FLL - EMERGENCY CEILING LIGHTS FROM SEATS 8 THROUGH 14 INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY REF MM 33 -53-01, OPS CHECKED OK REF MM 33-53-00. (M) 2 L 7 2 4F RT A6WE 2001070500172 20010705 00172 WP 2001 7 5 AALA20011237 1 20010601 A 5300 WEB DOUG DC9 DC983 3022083 WP FS 693 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 566AA 49348 TUL - FOUND WEB UNDER RIGHT FLOORBOARD SUPPORT DAMAGED AT STATION 693. REPAIRED WEB PER AARD 53-10-00-24. (M) 2 L 7 2 4F RT A6WE 2001070500173 20010705 00173 WP 2001 7 5 AALA20011213 1 20010529 A 5300 WEB DOUG DC9 DC982 3022082 WP FS 208 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 TUL - FOUND LONGERON 15L WEB TANG CRACKED AT 208. FABRICATED AND INSTALLED STRAP ON WEB AT L15L, STATION 208 PER AARD 5 3-10-00-11 PAGE 1/2. (M) 2 L 7 2 4F A6WE 2001070500174 20010705 00174 WP 2001 7 5 AALA20011219 1 20010530 A 5300 LONGERON DOUG DC9 DC982 3022082 WP FS 160 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 TUL - FOUND LONGERON 4L IS CRACKED AROUND FASTENER AT STATION 160. INSTALLED DOUBLER PER SRM 53-14-1 AND SRM 53-02. (M ) 2 L 7 2 4F A6WE 2001070500175 20010705 00175 WP 2001 7 5 AALA20011223 1 20010530 A 5300 SKIN DOUG DC9 DC982 3022082 WP FS 330 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 TUL - FOUND DENT ABOVE LEFT FORWARD CABIN WINDOW. INSTALLED DOUBLER PER SRM 53-04 FIG 38 SHEET 20. (M) 2 L 7 2 4F A6WE 2001070500176 20010705 00176 WP 2001 7 5 AALA20011226 1 20010601 A 5300 FRAME DOUG DC9 DC982 3022082 WP FS 484 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 TUL - FOUND UPPER LEG OF FRAME CRACKED AND BENT AT 484, ABOVE L26L. REPAIRED FRAME PER AARD 53-10-00-17. (M) 2 L 7 2 4F A6WE 2001070500177 20010705 00177 NM 2001 7 5 AALA20011192 1 20010606 A 3350 POWER SUPPLY BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 363AA 24044 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 20AB THROUGH 24 AB INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT POWER SUPPLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001070500178 20010705 00178 NM 2001 7 5 AALA20011185 1 20010604 A 3350 4033578 HARNESS BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 650AA 24608 JFK - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT 23D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT HARNESS AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001070500179 20010705 00179 NM 2001 7 5 P2EA01089 1 20010607 A 2900 AS11508K01080 HYDRAULIC LINE BOEING 737 737297 1384480 NM MLG W/W INOPERATIVE A P2EA O OTHER J K WARNING INDICATION FLUID LOSS AP APPROACH 1 CE 05 5WM 22629 FLT 408 - MCI - WHILE ON APPROACH INTO MCI, AIRCRAFT A SYSTEM HYDRAULIC FAILED. DECLARED AN EMERGENCY. INSPECTED HYDRA ULIC SYSTEM A AND FOUND LEAK IN FORWARD LEFT MAIN WHEEL WELL. REMOVED AND REPLACED HYDRAULIC LINE LEAK CHECKED GOOD PER BOEING MM 29-00 PARA 1 BUS PARA A. (M) 2 L 7 2 4F A16WE 2001070500180 20010705 00180 WP 2001 7 5 AALA20011230 1 20010601 A 5300 SKIN DOUG DC9 DC982 3022082 WP FS 1380 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 TUL - FOUND FUSELAGE SKIN CRACKED STATION 1380 AT LONGERON 14 LEFT. INSTALLED EXTERNAL REPAIR PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2001070500181 20010705 00181 WP 2001 7 5 AALA20011231 1 20010606 A 5200 SKIN DOUG DC9 DC982 3022082 WP FS 170 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 TUL - FOUND DENTS IN BOTH LOWER CORNERS OF OUTER SKIN. INSTALLED REPAIR DOUBLER PER AARD 52-10-00. (M) 2 L 7 2 4F A6WE 2001070500182 20010705 00182 WP 2001 7 5 AALA20011232 1 20010607 A 5300 FRAME DOUG DC9 DC982 3022082 WP FS 522 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 TUL - FOUND FRAME AT FS 522 DAMAGED AT L23-L26, LEFT HAS TOOLING MARKS. INSTALLED DOUBLER PER ESO 80559. (M) 2 L 7 2 4F A6WE 2001070500183 20010705 00183 WP 2001 7 5 AALA20011233 1 20010606 A 5300 FRAME DOUG DC9 DC982 3022082 WP FS 522 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 TUL - FOUND FRAME AT STATION 522 GOUGED ON UPPER LOG IN 6 PLACES FROM L23R TOL27R. INSTALLED DOUBLER PER ESO 80559. (M ) 2 L 7 2 4F A6WE 2001070500184 20010705 00184 WP 2001 7 5 AALA20011198 1 20010611 A 3600 CLAMP DOUG DC9 DC982 3022082 WP ACM BAY A AALA A UNSCHED LANDING J O WARNING INDICATION OTHER CL CLIMB 1 SW 21 70401 49312 DFW - FLT 552 - EN ROUTE DFW-PIT, DETECTED TAIL HIGH TEMPERATURE LIGHT ILLUMINATE IN COCKPIT. RETURNED DFW AND LANDED W ITHOUT FURTHER INCIDENT. RE-SECURED CLAMP AT LEFT SIDE ACY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001070600001 20010706 00001 NM 2001 7 6 01FDEA00408 1 20010611 A 5220 SKIN BOEING 727 72722C 138400F NM EXIT HATCH CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 DURING ROUTINE INSP, LT FWD EMERGENCY EXIT HATCH UPPER INNER SKIN FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB PER I AW BAC 727 SRM 52-00-3, 51-30-2. 2 L 7 3 4F A3WE 2001070600002 20010706 00002 NM 2001 7 6 01FDEA00409 1 20010611 A 5320 TIE CLIP BOEING 727 72722C 138400F NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 DURING ROUTINE INSP, STR TIE CLIP AT BS 328, STR 14R FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SR M 51-20-1, 51-30-2. 2 L 7 3 4F A3WE 2001070600003 20010706 00003 NM 2001 7 6 01FDEA00410 1 20010611 A 5320 TIE CLIP BOEING 727 72722C 138400F NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 DURING ROUTINE INSP, STR TIE CLIP AT BS 312, STR 4R FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-20-1, 51-30-2. 2 L 7 3 4F A3WE 2001070600004 20010706 00004 NM 2001 7 6 01FDEA00411 1 20010611 A 5320 WEB BOEING 727 72722C 138400F NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 DURING ROUTINE INSP, RT SIDE WEB IN AFT AIRSTAIR AREA FOUND CRACKED AT BS 1283. *S/D* REMOVED, REPLACED AND FAB PER IA W BAC 727 BAC 727 SRM 51-40-2, 51-30-2. 2 L 7 3 4F A3WE 2001070600005 20010706 00005 NM 2001 7 6 01FDEA00412 1 20010611 A 2731 FITTING BOEING 727 72722C 138400F NM ELEVATOR TAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 DURING ROUTINE INSP, RT ELEVATOR TAB ROD FITTING FOUND CRACKED. *S/D* REMOVED AND REPLACED RIGHT ELEVATOR TAB PER IAW BAC 727 MM 27-30-011-2. 2 L 7 3 4F A3WE 2001070600006 20010706 00006 NM 2001 7 6 01FDEA00413 1 20010611 A 5320 WEB BOEING 727 72722C 138400F NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 DURING ROUTINE INSP, LT SIDE WEB IN AIRSTAIR COMPT FOUND CRACKED AT LIGHTENING HOLE AT BS 1263. *S/D* REMOVED, REPLACE D AND FAB PER IAW BAC 727 SRM 51-40-2, 51-30-2. 2 L 7 3 4F A3WE 2001070600007 20010706 00007 NM 2001 7 6 01FDEA00414 1 20010611 A 5312 PRESSURE PANEL BOEING 727 72722C 138400F NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 DURING ROUTINE INSP LT SIDE WEB IN NOSE WHEEL WELL WAS FOUND CRACKED AT BS 1260. *S/D* REMOVED, REPLACED AND FAB PER I AW BAC 727 SRM 51-20-1, 51-30-2. 2 L 7 3 4F A3WE 2001070600009 20010706 00009 EU 2001 7 6 01FDEA00416 1 20010609 A 2612 FIRE WARNING AIRBUS 310 A310222 3930315 EU COCKPIT ILLUMINATED A FDEA E F A ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING A J FLAME/FIRE WARNING INDICATION CL CLIMB 1 SO 25 416FE 288 NR 1 ENG FIRE WARNING LIGHT ILLUM DURING CLIMBOUT. PERFORMED PROC BOTH FIRE BOTTLES FIRED. 2 L 7 2 4F RT A35EU 2001070600010 20010706 00010 WP 2001 7 6 01FDEA00417 1 20010609 A 5320 FLOOR SUPPORT DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 313FE 48311 BS 1984 X=2R, Z=-19 LWR SIDE OF FLOOR SUPPORT HAS LEVEL (2) CORROSION APPROX 3.0 LONG X 2.0 WIDE AROUND MISSING NUT PLAT E. 2 L 7 3 4F A22WE 2001070600011 20010706 00011 WP 2001 7 6 01FDEA00418 1 20010601 A 5220 ADA00061 BEAM DOUG DC10 DC1030F 3023504 WP EXIT DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 LEFT NR 3 OVERWING EXIT DOOR UPPER AFT DOOR FRAME IS CRACKED AND BROKEN OFF. REMOVED AND REPLACED BEAM PER IAW DWG ADA3 462 & SRM 52-12-01, 51-30-01. 2 L 7 3 4F RT A22WE 2001070600012 20010706 00012 WP 2001 7 6 01FDEA00419 1 20010601 A 5311 FRAME DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 PRIOR TO LWR SKIN REMOVAL BS 469, RBL 65, 3 INCH CRACK IN FRAME COMMON TO UPPER FLANGE. REMOVED AND REPLACED FRAME PER IAW DC10 SRM 53-30-00 FIG 11 & 51-21-01. 2 L 7 3 4F RT A22WE 2001070600014 20010706 00014 WP 2001 7 6 01FDEA00421 1 20010601 A 5347 AGA385515 SEAT TRACK DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 AFT CARGO COMP SEAT TRACK BY CARGO DOOR CORRODED. REMOVED AND REPLACED PER IAW DC10 SRM 51-33-01 & 51-21-01. 2 L 7 3 4F RT A22WE 2001070600015 20010706 00015 WP 2001 7 6 01FDEA00422 1 20010601 A 5320 NUT PLATE DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 AFT CARGO COMPT BS 1790=X=42 FWD VERTICAL SUPPORT BEAM CORRODED NUT PLATE. REMOVED AND REPLACED PER IAW DC10 SRM 53-00- 01 & 51-21-01. 2 L 7 3 4F RT A22WE 2001070600016 20010706 00016 WP 2001 7 6 01FDEA00423 1 20010601 A 5311 ADA01307A FRAME DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 FWD CARGO FRAME FORMER RT HAS PRE-EXISTING CRACK BS 916 LNG 34, RBL 59. REMOVED AND REPLACED PER IAW DC10 SRM 51-50-03, 51-31-01 & 51-21-01. 2 L 7 3 4F RT A22WE 2001070600017 20010706 00017 WP 2001 7 6 01FDEA00424 1 20010601 A 5310 DOOR FRAME DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 L2 DOOR FRAME HAS PUNCTURE FWD UPPER. REMOVED, REPLACED AND FAB PER IAW DC10 SRM 51-21-01 & 53-00-01. 2 L 7 3 4F RT A22WE 2001070600018 20010706 00018 WP 2001 7 6 01FDEA00425 1 20010601 A 5310 DOOR FRAME DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 R-3 DOOR BS 1294-1300 AFT DOOR FRAME LWR RELIEF HOLE IN BOTTOM OF FRAME CRACK. FAB, STOP DRILL CRACK INSTALL DOUBLER PE R IAW DC10 SRM 53-50-00 FIG 19. 2 L 7 3 4F RT A22WE 2001070600019 20010706 00019 WP 2001 7 6 01FDEA00426 1 20010601 A 5510 ALC750211 CAP DOUG DC10 DC1030F 3023504 WP HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 LEFT HORZ STAB SSI CARD INSP FOUND BS XFS & 166, CTR I/B LEADING EDGE ON O/B TEE CAP. REMOVED AND REPLACED TEE CAP PER IAW DC10 SRM 51-30-01. 2 L 7 3 4F RT A22WE 2001070600020 20010706 00020 WP 2001 7 6 01FDEA00427 1 20010601 A 5320 GUSSET DOUG DC10 DC1030F 3023504 WP FUSELAGE BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 PRIOR TO LWR SKIN REMOVAL AT BS 440, LBL 27 GUSSET COMMON TO FRAME AND INTERCOSTAL BROKEN. REMOVED, REPLACED AND FAB PE R IAW DC10 SRM 53-11-014, 51-21-01. 2 L 7 3 4F RT A22WE 2001070600021 20010706 00021 SO 2001 7 6 C2XA01CL161 1 20010704 A 2611 47359713 DETECTOR EMB 135 EMB135LR SO CARGO BAY INTERMITTENT A C2XA A F UNSCHED LANDING ACTIVATE FIRE EXT. J WARNING INDICATION CR CRUISE 1 SW 27 11526 145410 CLE-MEM FLIGHT#3887 THE CREW REPORTED A BAGGAGE SMOKE WARNING IN FLIGHT.THE AIRCRAFT DIVERTED TO SDF AND LANDED WITHOUT INCIDENT.MAINTENANCE INSPECTED AND FOUND NO EVIDENCE OF SMOKE OR FIRE.THEY REPLACED THE BAGGAGE SMOKE DETECTOR AND THE BAGGAGE FIRE BOTTLES THAT THE CREW DISCHARGED. OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT TOOO11AT 2001070600022 20010706 00022 WP 2001 7 6 01FDEA00428 1 20010601 A 5313 1418496S LONGERON DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 ANGLE HAS LEVEL 2 CORROSION IN NR 2 A/C BAY FWD LT SIDE PRIMARY STRUCTURE. REMOVED, REPLACED AND FAB LONGERON PER IAW D C10 SRM 51-30-01, 51-31-01, 53-12-01 FIG 24, SHT 1, & 51-41-01. 2 L 7 3 4F RT A22WE 2001070600024 20010706 00024 NM 2001 7 6 01FDEA00433 1 20010611 A 5330 6517529 SKIN BOEING 727 7272D4 138407U NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 CREASE IN EXTERNAL SKIN AT BS 1193 JUST BELOW STR 16R. *S/D* REMOVED AND REPLACED SKIN PER FEDEX SRM 53-30-3 FIG 1. 2 L 7 3 4F A3WE 2001070600025 20010706 00025 NM 2001 7 6 01FDEA00435 1 20010612 A 2910 O-RING DOUG MD11 MD11F 3023600 NM HYD SYSTEM LEAKING A FDEA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 605FE 48514 HYD SYS NR 1 FAIL 1 HR INTO FLT FOUND LEAKS FROM HOL STAB CONTROL VALVE NR 2 SYS NR 1 PRESS LINE ON VALVE FITTING. REMO VED AND REPLACED DELAMINATED O-RING OF FITTING. 2 L 7 3 4F RT A22WE 2001070600026 20010706 00026 WP 2001 7 6 01FDEA00437 1 20010612 A 5347 AGA38553 SEAT TRACK DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 AFT CARGO COMP LBL 20, BS 1790 TO 1964 HAS CORROSION TOP, BOTTOM AND AROUND SCREW HOLES OF TIE DOWN TRACK. REMOVED AND REPLACED SEAT TRACK PER IAW SRM 51-31-01. 2 L 7 3 4F RT A22WE 2001070600027 20010706 00027 WP 2001 7 6 01FDEA00438 1 20010612 A 5230 ADA7127502 BEAM DOUG DC10 DC1030F 3023504 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 LWR, FWD CARGO DOOR COUNTER BALANCE SNUBBER BEAM ASSY CRACKED. REMOVED AND REPLACED BEAM ASSY PER IAW AMM 52-31-07-2-1 & 52-31-07-2-1. 2 L 7 3 4F RT A22WE 2001070600028 20010706 00028 WP 2001 7 6 01FDEA00439 1 20010612 A 5730 PANEL DOUG DC10 DC1030F 3023504 WP RT WING DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 PANEL 635 LT, RT WING O/B TRAILING LEADING EDGE HAS DELAMINATED EDGES ON (2) EDGES. REPAIRED EDGES PER IAW SRM 51-71-00 . 2 L 7 3 4F RT A22WE 2001070600029 20010706 00029 WP 2001 7 6 01FDEA00440 1 20010612 A 5753 FAIRING DOUG DC10 DC1030F 3023504 WP T/R FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 LT TRAILING EDGE, FLAP, O/B, FLAP FAIRING HAS 2 CRACKS ON INSIDE 6 INCHES. REMOVED, REPLACED AND FAB PER IAW DC10 SRM 5 1-21-01 & 51-35-01. 2 L 7 3 4F RT A22WE 2001070600030 20010706 00030 WP 2001 7 6 01FDEA00441 1 20010612 A 5311 ABA722331 FRAME DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 BS 410, RBL 5 INCHES CRACK COMMON TO FWD, LWR FLANGE AND BS 410, LBL 13 2. CORROSION COMMON TO SKIN. REMOVED AND REPLA CED FRAME PER IAW SRM 51-35-01 & 51-33-01. 2 L 7 3 4F RT A22WE 2001070600031 20010706 00031 WP 2001 7 6 01FDEA00442 1 20010612 A 5311 FRAME DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 AFT CARGO COMP BS 1902, CRACKS FOUND ON LONGERON 42L, & BS 1942 BETWEEN LONGERON 40L AND 41L. REMOVED AND REPLACED FRAM ES PER IAW DC DPS 10.225, SRM 51-21-01 & 51-33-01. 2 L 7 3 4F RT A22WE 2001070600032 20010706 00032 WP 2001 7 6 01FDEA00443 1 20010612 A 5230 DOOR FRAME DOUG DC10 DC1030F 3023504 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 BS 112, LBL 112, Z=+34 FWD SIDE UPPER CARGO DOOR FRAME NET ATTACH RING 2.8 CRACK AT ATTACH POINT. REMOVED AND REPLACED PER IAW EA 8-5230-56137, DC10 SRM 53-50-00 & GMM 4-1-975 FIG 5. 2 L 7 3 4F RT A22WE 2001070600033 20010706 00033 WP 2001 7 6 01FDEA00444 1 20010612 A 5414 SKIN DOUG DC10 DC1030F 3023504 WP NR 2 NACELLE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 SKIN FWD OF NR 2 ENG MATES TO FAN COWL WORN THRU NACELLE SKIN BS YTN138.977. REPAIRED PER IAW EA 8-5410-53241. 2 L 7 3 4F RT A22WE 2001070600034 20010706 00034 NM 2001 7 6 01FDEA00445 1 20010612 A 2612 2240153503 FIRE DETECTOR DOUG MD11 MD11F 3023600 NM NR 1 ENGINE INTERMITTENT A FDEA O OTHER N FALSE WARNING DE DESCENT 1 SO 25 601FE 48401 ON ARRIVAL INTERMITTENT ENG 1 FIRE (AURAL ALSO) WARN. SHOW AS LEVEL 1 ALERT. REMOVED AND REPLACED UPPER RIGHT FIRE DET ECTOR ASSY PER MM 26-11-03-4. OPS CK OK. CLOSED COWLING. 2 L 7 3 4F RT A22WE 2001070600035 20010706 00035 EU 2001 7 6 01FDEA00446 1 20010613 A 2432 BATTERY AIRBUS 310 A310222 3930315 EU NR 1 DISCHARGED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 421FE 342 NR 1 BATTERY INOP. REMOVED AND REPLACED NR 1 BATTERY PER MM 24-31-11-4. OPS CK GOOD. 2 L 7 2 4F RT A35EU 2001070600036 20010706 00036 EU 2001 7 6 01FDEA00447 1 20010614 A 2611 SMOKE DETECTOR AIRBUS 310 A310222 3930315 EU MAIN CARGO DECK ACTIVATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 421FE 342 AFT T/O AFT AND MID MAIN DECK CARGO SMOKE IND FOLLOW BY MIN EQUIP BAY SMOKE IND. SUSPECT OIL IN BLD DUCT FROM APU SHUTD OWN FOR LOW OIL. 2 L 7 2 4F RT A35EU 2001070600037 20010706 00037 EU 2001 7 6 01FDEA00448 1 20010614 A 2611 SMOKE DETECTOR AIRBUS 300 A300F4605R 3930327 EU NR 2 MAIN DECK FALSE INDICATION A FDEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 25 665FE 769 DURING TAXI BOTH MID 2 MAIN DECK CARGO SMOKE LIGHT ILLUM TRIGGERING MC DECK CARGO VALVE, ISO VALVE, ETC. PERF SMOKE TES T NO FAULTS FOUND. RERACKED SMOKE MODULES AND ALL 3 PASSED SELF TEST PER TSM 28-19-00. 2 L 7 2 4F RT A35EU 2001070600038 20010706 00038 NE 2001 7 6 NACA20010026 2 20010704 A 7230 404482 CYLINDER PWA CB3 DOUG DC6 DC6B 3021712 WP PWA R2800 R2800CB3 52026 NE #9 CRACKED A NACA E ENGINE SHUTDOWN K R FLUID LOSS PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 867TA 1400 1400 NK510177 45202 NK510177 DISCREPANCEY: #2 engine will not take a lean, oil loss noted.CORRECTIVE ACTION: Replaced the #9 cylinder assy. 2 L 7 4 4R 4 R 6A4 5E8 2001070600039 20010706 00039 NM 2001 7 6 CALA0100633 1 20010705 A 5230 SKIN BOEING 737 7373T0 1384582 NM AFT CARGO DR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59302 23353 A PERMANENT REPAIR WAS INSTALLED WHERE AN INTERIM REPAIR HAD PREVIOUSLY BEEN DONE FOR 4 EACH CRACKS AT LIGHTENING HOLES IN AFT CARGO DOOR INNER SKIN. THE INTERIM REPAIR HAD BEEN PERFORMED IAW ECRA 5230-01488 AND A DIP WAS ISSUED. THE PERMAN ENT REPAIR WAS INSTALLED IAW ECRA 5230-01509. 2 L 7 2 4F RT A16WE 2001070600040 20010706 00040 NM 2001 7 6 CALA0100634 1 20010706 A 5310 FRAME BOEING 737 7373T0 1384582 NM L-1 WINDOW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59302 23353 INSPECTION FOUND A 1" CRACK IN L-1 WINDOW FRAME AT UPPER O/B CORNER. THE WINDOW FRAME WAS REPAIRED IAW SRM 53-10-01. 2 L 7 2 4F RT A16WE 2001070600043 20010706 00043 NM 2001 7 6 QXEA0100863 1 20010520 A 3211 FITTING DHAV DHC8 DHC8202 2809007 NM LT MLG CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - H MEMBER OF LEFT-HAND MAIN LANDING GEAR HAS FRETTING CORROSION AT TOP AND BOTTOM ATTACHMENT POINTS OF THE MAIN LAN DING GEAR RETRACTION ACTUATOR ATTACHMENT FITTING. REPAIRED IAW RD8-54-523. 2 H 7 2 4T RT A13NM 2001070600044 20010706 00044 NM 2001 7 6 QXEA0100864 1 20010520 A 3211 FITTING DHAV DHC8 DHC8202 2809007 NM LT MLG CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - H MEMBER OF LEFT-HAND MAIN LANDING GEAR HAS FRETTING CORROSION AT TOP AND BOTTOM ATTACHMENT POINTS OF THE MAIN LAN DING GEAR RETRACTION ACTUATOR ATTACHMENT FITTING. REPAIRED IAW RD 8-54-523 AND HORIZON AIR EA 9-54-299. 2 H 7 2 4T RT A13NM 2001070600045 20010706 00045 NM 2001 7 6 QXEA0100865 1 20010525 A 3211 FITTING DHAV DHC8 DHC8202 2809007 NM LT MLG CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - H MEMBER ON LEFT-HAND MAIN LANDING GEAR HAS FRETTING CORROSION AT TOP AND BOTTOM ATTACH POINTS ON THE MAIN LANDING GEAR RETRACTION ACTUATOR ATTACH FITTING. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001070600046 20010706 00046 NM 2001 7 6 QXEA0100866 1 20010323 A 5414 PANEL DHAV DHC8 DHC8202 2809007 NM NR 1 NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - INBOARD SIDE PANEL OF NR 1 NACELLE TO ACCESS RIGHT-HAND H MEMBER. REPAIRED IAW DHC-8 SRM 51-20-51. 2 H 7 2 4T RT A13NM 2001070600047 20010706 00047 NM 2001 7 6 QXEA0100867 1 20010516 A 3211 FITTING DHAV DHC8 DHC8202 2809007 NM RT MLG DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT-HAND MAIN LANDING GEAR RETRACT FITTING UPPER ATTACH POINT PITTED. REPAIRED IAW HORIZON AIR EA 9-54-295. 2 H 7 2 4T RT A13NM 2001070600048 20010706 00048 NM 2001 7 6 QXEA0100868 1 20010514 A 5280 SEAL DHAV DHC8 DHC8202 2809007 NM RT MLG DOOR WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT-HAND MAIN LANDING GEAR AFT RIGHT-HAND DOOR SEAL FOR FORWARD EDGE ON WHEEL WELL WORN. REMOVED TORN DOOR SEAL , INSTALLED AND SECURED NEW DOOR SEAL. 2 H 7 2 4T RT A13NM 2001070600049 20010706 00049 NM 2001 7 6 QXEA0100869 1 20010516 A 3211 FITTING DHAV DHC8 DHC8202 2809007 NM RT MLG CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - H MEMBER UNDER RIGHT-HAND MAIN LANDING GEAR RETRACTION ACTUATOR FITTING, HAS AREAS WITH PITTING CORROSION, ADJACEN T TO BOTH LOWER ATTACH POINT HOLES. REPAIRED IAW HORIZON AIR EA 9-54-295. 2 H 7 2 4T RT A13NM 2001070600050 20010706 00050 NM 2001 7 6 QXEA0100870 1 20010522 A 5730 SKIN DHAV DHC8 DHC8202 2809007 NM RT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT-HAND WING TOP SKIN HAS .125 INCH X .5 INCH CHAFED AREA BELOW AFT EDGE OF PANEL 422ET. REPAIRED IAW DHC-8 MM 57-10-16, TABLE 1. 2 H 7 2 4T RT A13NM 2001070600051 20010706 00051 NM 2001 7 6 QXEA0100871 1 20010517 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM LT WING SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - LEFT-HAND WING, OUTER WING, FORWARD SPAR, LOWER FLANGE HAS LIGHT SCRATCHING FROM LEADING EDGE REMOVAL ALONG ENTIRE LENGTH. REPAIRED IAW HORIZON AIR EA 9-57-577 AND RD 8-57-1675. 2 H 7 2 4T RT A13NM 2001070600052 20010706 00052 NM 2001 7 6 QXEA0100872 1 20010515 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM LT WING SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - LEFT-HAND WING, OUTER WING, FORWARD SPAR, UPPER FLANGE HAS LIGHT SCRATCHING FROM LEADING EDGE REMOVAL ALONG ENTIRE LENGTH. REPAIRED IAW RD 8-57-1119. 2 H 7 2 4T RT A13NM 2001070600053 20010706 00053 NM 2001 7 6 QXEA0100873 1 20010512 A 5753 FLAP DHAV DHC8 DHC8202 2809007 NM LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - LEFT-HAND WING; INBOARD FLAP CHAFED ON PREVIOUS REPAIR, 7 INCHES LONG X 1.8 INCH WIDE. REPAIRED IAW RD 8-57-1022. 2 H 7 2 4T RT A13NM 2001070600054 20010706 00054 NM 2001 7 6 QXEA0100874 1 20010520 A 5753 FLAP DHAV DHC8 DHC8202 2809007 NM LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - LEFT-HAND WING; OUTBOARD FLAP HAS CHAFE 1 INCH X .25 INCH ON TOP SURFACE. REPAIRED IAW RD 8-57-1022. 2 H 7 2 4T RT A13NM 2001070600055 20010706 00055 NM 2001 7 6 QXEA0100875 1 20010520 A 5753 FLAP DHAV DHC8 DHC8202 2809007 NM LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - LEFT-HAND WING - OUTER FLAP CHAFE, 4 INCHES LONG X 1.4 INCH WIDE ON PREVIOUS REPAIR. REPAIRED IAW RD 8-57-1022 AN D DHC-8 SRM 51-20-26. 2 H 7 2 4T RT A13NM 2001070600056 20010706 00056 NM 2001 7 6 QXEA0100876 1 20010516 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM LT WING WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - LEFT-HAND WING - NR 1 FLAP TRACK PLATING WORN THROUGH ON TRACK Y. REPAIRED IAW RD 8-57-985, PAGES 4 AND 5 AND COM PLIED WITH RD STEP 3 OF RD 8-57-985, PAGE 5. 2 H 7 2 4T RT A13NM 2001070600057 20010706 00057 NM 2001 7 6 QXEA0100877 1 20010516 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM LT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - LEFT-HAND WING - NR 2 FLAP TRACK, TRACK W AND X HAVE DIVETS OPPOSITE EACH OTHER LEAVING REMAINING TRACK THICKNESS OF .244. REPAIRED IAW RD 8-57-986, PAGES 5 AND 6. 2 H 7 2 4T RT A13NM 2001070600058 20010706 00058 NM 2001 7 6 QXEA0100878 1 20010516 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM LT WING WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - LEFT-HAND WING - NR 3 FLAP TRACK, TRACKS X AND Y HAVE PLATING WORN THROUGH IN SPOTS. REPAIRED IAW RD 8-57-987, PA GES 4 AND 5. 2 H 7 2 4T RT A13NM 2001070600059 20010706 00059 NM 2001 7 6 QXEA0100879 1 20010516 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM LT WING WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - LEFT-HAND WING - NR 4 FLAP TRACK, TRACKS B AND D HAVE PLATING WORN THROUGH. REPAIRED IAW RD 8-57-988, PAGES 5-7. 2 H 7 2 4T RT A13NM 2001070600060 20010706 00060 NM 2001 7 6 QXEA0100880 1 20010513 A 5730 SKIN DHAV DHC8 DHC8202 2809007 NM RT WING SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT-HAND WING TOP SKIN HAS FIVE SCRATCHES LOCATED 3 - 7 INCHES FORWARD OF PANEL 624BT AT STATION Y279. REPAIRED IAW DHC-8 SRM 51-20-05, 51-20-16 AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2001070600061 20010706 00061 NM 2001 7 6 QXEA0100881 1 20010516 A 5753 FLAP DHAV DHC8 DHC8202 2809007 NM RT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT-HAND WING, OUTBOARD FLAP NR 4 TRACK HAS PITTED PLATING AND AREAS OF MISSING PLATING ON ALL BEARING SURFACES. REPAIRED IAW RD 8-57-988, STEPS 1-2 AND PAGE 7 AND HORIZON AIR EA 9-57-573. 2 H 7 2 4T RT A13NM 2001070600062 20010706 00062 NM 2001 7 6 QXEA0100882 1 20010516 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM RT WING WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT-HAND WING OUTBOARD FLAP, NR 5 TRACK HAS PITTED PLATING AND AREAS OF MISSING PLATING ON ALL BEARING SURFACES. REPAIRED IAW RD 8-57-989, PAGE 7, STEP 1 AND PAGE 5 AND HORIZON AIR EA 9-57-575. 2 H 7 2 4T RT A13NM 2001070600063 20010706 00063 NM 2001 7 6 QXEA0100883 1 20010516 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM RT WING WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT-HAND WING OUTBOARD FLAP, NR 3 FLAP TRACK SURFACE Y HAS PLATING LOSS. REPAIRED IAW RD 8-57-987, PAGES 1-5. 2 H 7 2 4T RT A13NM 2001070600064 20010706 00064 NM 2001 7 6 QXEA0100884 1 20010516 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM RT WING WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT-HAND WING OUTBOARD FLAP NR 3 FLAP TRACK SURFACE X HAS PLATING LOSS. REPAIRED IAW RD 8-57-987, PAGES 1-5. 2 H 7 2 4T RT A13NM 2001070600065 20010706 00065 NM 2001 7 6 QXEA0100885 1 20010515 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM RT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT-HAND WING INBOARD FLAP NR 1 UPPER TRACK HAS TWO PAIRS OF PITS ON OPPOSITE SIDE OF TRACK. COMPLIED WITH RD 8 -57-985, PAGE 5, STEPS 3 AND 4. 2 H 7 2 4T RT A13NM 2001070600066 20010706 00066 NM 2001 7 6 QXEA0100886 1 20010515 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM RT WING WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT-HAND WING INBOARD FLAP NR 1 LOWER TRACK HAS WEAR THROUGH PLATING ON SURFACE Y. COMPLIED WITH RD 8-57-985, P AGE 5, STEPS 4 AND 5. 2 H 7 2 4T RT A13NM 2001070600067 20010706 00067 NM 2001 7 6 QXEA0100887 1 20010515 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM RT WING WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT-HAND WING INBOARD FLAP NR 1 UPPER TRACK HAS PLATING LOSS ON SURFACES W AND X. COMPLIED WITH RD 8-57-985, PA GE 5, STEPS 3 AND 4. 2 H 7 2 4T RT A13NM 2001070600068 20010706 00068 NM 2001 7 6 QXEA0100888 1 20010515 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM RT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT-HAND WING INBOARD FLAP NR 2 UPPER TRACK HAS PITTED PLATING ON SURFACE X. COMPLIED WITH RD 8-57-986, PAGE 1- 5, STEP 1 AND RD 8-57-986 PDGE 5, STEPS 3 AND 4. 2 H 7 2 4T RT A13NM 2001070600069 20010706 00069 NM 2001 7 6 QXEA0100889 1 20010515 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM RT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT-HAND WING INBOARD FLAP NR 2 LOWER TRACK SURFACE Y HAS PITTING PLATING ON FORWARD PORTION OF TRACK. COMPLIED WITH RD 8-57-986, PAGE 1-5, STEP 1 AND RD 8-57-986, PAGE 5, STEPS 3 AND 4. 2 H 7 2 4T RT A13NM 2001070600070 20010706 00070 NM 2001 7 6 QXEA0100890 1 20010515 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM RT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT-HAND WING INBOARD FLAP NR 2 UPPER TRACK HAS TWO PITS AT FORWARD END ON OPPOSITE SIDES OF TRACK. COMPLIED WI TH RD 8-57-986, PAGES 1-5, STEP 1 AND RD 8-57-986, PAGE 5, STEPS 3 AND 4. 2 H 7 2 4T RT A13NM 2001070600071 20010706 00071 NM 2001 7 6 QXEA0100891 1 20010513 A 5730 SKIN DHAV DHC8 DHC8202 2809007 NM RT WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT-HAND WING BOTTOM SKIN FORWARD EDGE GOUGED IN SEVERAL PLACES BETWEEN STATION YW243 AND YW297. REPAIRED IAW D HC-8 SRM 51-20-36 AND SRM 51-20-51. 2 H 7 2 4T RT A13NM 2001070600072 20010706 00072 NM 2001 7 6 QXEA0100892 1 20010513 A 5730 SKIN DHAV DHC8 DHC8202 2809007 NM RT WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT-HAND WING TOP SKIN FORWARD EDGE GOUGED IN SEVERAL PLACES BETWEEN STATION YW261 AND YW297. REPAIRED IAW DHC- 8 SRM 51-20-36 AND SRM 51-20-51. 2 H 7 2 4T RT A13NM 2001070600073 20010706 00073 NM 2001 7 6 QXEA0100893 1 20010514 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM RT WING SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT-HAND WING FRONT SPAR TOP CAP SCRATCHED ALONG SEALANT LINE BETWEEN STATION YW261 AND YW297. REPAIRED IAW DHC -8 RD 8-54-119. 2 H 7 2 4T RT A13NM 2001070600074 20010706 00074 NM 2001 7 6 QXEA0100894 1 20010514 A 5730 PLATE DHAV DHC8 DHC8202 2809007 NM WING SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - MATING SURFACE OF LADDER PLATE FOR FUEL PANEL 624AT FORWARD AND AFT SURFACES HAVE CIRCULAR SCRATCHES. REPAIRED IA W DHC-8 RD 8-57-611. 2 H 7 2 4T RT A13NM 2001070600075 20010706 00075 NM 2001 7 6 QXEA0100895 1 20010520 A 5730 SKIN DHAV DHC8 DHC8202 2809007 NM RT WING SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - SCRATCH IN RIGHT-HAND WING TOP SKIN COMING FROM FORWARD OUTBOARD CORNER OF FUEL ACCESS PANEL 624BT APERTURE. REPA IRED IAW DHC-8 SRM 53-00-16, PAGE 3, TABLE 1, SHEET 2. 2 H 7 2 4T RT A13NM 2001070600076 20010706 00076 NM 2001 7 6 QXEA0100896 1 20010513 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM RT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - RIGHT-HAND WING NR 5 TRACK OUTBOARD FORWARD SURFACE HAS AN AREA WITH PITTING. REPAIRED IAW DHC-8 RD 8-57-989, PAG E 7, STEP 5. 2 H 7 2 4T RT A13NM 2001070600077 20010706 00077 NM 2001 7 6 QXEA0100897 1 20010515 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - BAG DOOR SKIN HAS 4.5 INCH LONG SCRATCH THROUGH PAINT AND PRIMER FROM TOP EDGE GOING DOWN APPROXIMATELY CENTER. R EPAIRED IAW DHC-8 SRM 51-20-26, PAGE 7 AND SRM 51-20-51, PAGES 1-5, STEPS 1 THROUGH 5D. 2 H 7 2 4T RT A13NM 2001070600078 20010706 00078 NM 2001 7 6 QXEA0100898 1 20010515 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 526 PDX - BAG DOOR SKIN TOP EDGE HAS HALF MOON GOUGE APPROXIMATELY .5 X .2 X 13 INCH. REPAIRED IAW DHC-8 DRM 51-20-16, PARA GRAPH 4, SRM 51-20-26, PAGE 7, PARAGRAPH 5A AND SRM 51-20-51, PAGES 1-5, STEPS 1-5D. 2 H 7 2 4T RT A13NM 2001070600079 20010706 00079 EU 2001 7 6 QXEA0100900 1 20010601 A 5230 DOOR FRAME FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX- UPON INSPECTION, FOUND DAMAGE TO CARGO DOOR FRAME. REPAIRED IN ACCORDANCE WITH FOKKER STRUCTURAL REPAIR MANUAL. R EQUIRED INSPECTION COMPLIED WITH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001070600080 20010706 00080 EU 2001 7 6 QXEA0100901 1 20010603 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 478US 11227 GEG- EMERGENCY EXIT SIGN, FORWARD SIDE OF ROW 8 INOP. REMOVED AND REPLACED SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RE TURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001070600081 20010706 00081 EU 2001 7 6 QXEA0100902 1 20010602 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 483US 11233 SEA- EXIT LIGHT OVER GALLEY HAS LAMPS OUT. REMOVED AND REPLACED EXIT LIGHT ASSY. OPERATIONAL CHECKS GOOD. AIRCRAFT RE TURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001070600082 20010706 00082 EU 2001 7 6 QXEA0100903 1 20010530 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 499US 11182 SEA- EMERGENCY LIGHT EXIT SIGN INOP AT MID CABIN FORWARD POSITION. REMOVED AND REPLACED FORWARD FACING MID CABIN EXIT S IGN CIRCUIT BOARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001070600083 20010706 00083 NM 2001 7 6 QXEA0100904 1 20010605 A 3350 61047811 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 830PH 6384 41 526 SEA- EMERGENCY LIGHT SIGN OVER MAIN CABIN DOOR AND AIRSTAIR EGRESS LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY 1. O PERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001070600084 20010706 00084 NM 2001 7 6 SWAA011768 1 20010618 A 5523 BACB28AK04 BUSHING BOEING 737 7377H4 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 799SW 28209 DURING SCHEDULED C3 CHECK, ELEVATORS FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT AND RT ELEVATOR CONTROL BUSS ASSY BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2001070600085 20010706 00085 NM 2001 7 6 SWAA011769 1 20010619 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 587, STR 10R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001070600086 20010706 00086 NM 2001 7 6 SWAA011770 1 20010619 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 794, LBL 2.5. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2001070600087 20010706 00087 NM 2001 7 6 SWAA011773 1 20010618 A 3350 6556633 LENS BOEING 737 7373Q8 1384670 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 663SW 23256 DURING SCHEDULED BC4 CHECK, FOUND EMERGENCY EXIT SIGN LENS LOOSE AT RT OVERWING EXIT. REMOVED AND REPLACED EMERGENCY EX IT LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001070600088 20010706 00088 NM 2001 7 6 SWAA011775 1 20010617 A 5315 6545410 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED D-CHECK, FOUND CENTER LONGITUDINAL FLOORBEAM CRACKED AT BS 663. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2001070600089 20010706 00089 NM 2001 7 6 SWAA011776 1 20010619 A 3350 57771 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULED C3 CHECK, FOUND EEPLS END CAP MISSING AT AFT GALLEY. INSTALLED END CAP PER MM. 2 L 7 2 4F A16WE 2001070600090 20010706 00090 NM 2001 7 6 SWAA011779 1 20010618 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DEFECTIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY LIGHT BATTERY PACK AT LT OVERWING NOT CHARGING. REMOVED AND REPLACED BATTE RY PACK PER MM. 2 L 7 2 4F RT A16WE 2001070600091 20010706 00091 NM 2001 7 6 SWAA011785 1 20010618 A 5753 6546435 FLAP BOEING 737 7373Q8 1384670 NM LT WING DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 663SW 23256 DURING SCHEDULED C4 CHECK, FOUND LT OTBD AFT FLAP DISBONDED AT INBD LWR END. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2001070600092 20010706 00092 NM 2001 7 6 SWAA011786 1 20010618 A 5753 65495053 FLAP BOEING 737 7373Q8 1384670 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 663SW 23256 DURING SCHEDULED C4 CHECK, FOUND LT OTBD T/E MID FLAP LEADING EDGE CRACKED AT CONTROL ROD CUTOUT. REPAIRED FLAP PER SWA RA 1-357-1047 REV 1. 2 L 7 2 4F RT A16WE 2001070600093 20010706 00093 NM 2001 7 6 SWAA011787 1 20010619 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 727D+6, LBL 12 TO RBL 2.5. REPAIRED PER SWA RA. 2 L 7 2 4F RT A16WE 2001070600094 20010706 00094 NM 2001 7 6 SWAA011794 1 20010621 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED UNDER FLOOR SUPPORT AT BS 859, RBL 8.0. REPAIRED FLOORBEAM PER SW A RA. 2 L 7 2 4F RT A16WE 2001070600095 20010706 00095 NM 2001 7 6 SWAA011795 1 20010621 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 295, LBL 6. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2001070600096 20010706 00096 NM 2001 7 6 SWAA011796 1 20010621 A 3350 6104781 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHTS INOP AT RT OVERWING. REMOVED AND REPLACED RT OVERWING BATTERY PA CK PER MM. 2 L 7 2 4F A16WE 2001070600097 20010706 00097 NM 2001 7 6 SWAA011797 1 20010621 A 3350 65C27093 LIGHT BOEING 737 7372T4 1384492 NM ENTRY DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIG HT PER MM. 2 L 7 2 4F A16WE 2001070600098 20010706 00098 2001 7 6 SWAA011798 4 20010620 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001070600099 20010706 00099 NM 2001 7 6 SWAA011822 1 20010622 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 651SW 27721 EEPLS INOP AT ROW 14. RECONNECTED EEPLS WIRES PER MM. 2 L 7 2 4F RT A16WE 2001070600100 20010706 00100 NM 2001 7 6 SWAA011823 1 20010624 A 3350 57771 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED C1 CHECK, FOUND EEPLS END CAP MISSING AT AFT END. INSTALLED END CAP PER MM. 2 L 7 2 4F A16WE 2001070600101 20010706 00101 NM 2001 7 6 SWAA011824 1 20010625 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED 1/4D CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT BATTERY PACK INOP. REMOVED AND REPLACED OVERWING BA TTERY PACK. 2 L 7 2 4F RT A16WE 2001070600102 20010706 00102 2001 7 6 SWAA011826 4 20010624 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 AFT DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001070600103 20010706 00103 2001 7 6 SWAA011827 4 20010625 A 2565 61620468 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 614SW 28033 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001070600104 20010706 00104 2001 7 6 SWAA011828 4 20010625 A 2565 22D22900131 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 089SW 22904 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001070600105 20010706 00105 GL 2001 7 6 20010604CW017 3 20010604 A 6111 C19773D CLAMP CASA C212 C212200 2410304 EU HARTZL HCB4T HCB4TN5 GL PROP BLADE CRACKED E K NONE O OTHER IN INSP/MAINT 1 NM 04 117BH 481 171 CRACK DISCOVERED DURING ROUTINE 100 HOUR INSPECTION. DETECTED VISUALLY. REASON FOR CRACK NOT KNOWN. CLAMP ASSEMBLY RE PLACED WITH FACTORY NEW UNIT. 2 H 7 2 4T RT A43EU 6 C P40EA 2001070600106 20010706 00106 EA 2001 7 6 COMA0160430 1 20010704 A 5310 60034017723 ANGLE CNDAIR CL600 CL6002B19 EA CRACKED A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 991CA 7216 VERTICAL "J" ANGLE CLIP INSIDE CBPI @BL 9.0 L/H IS CRACKED.INSTALLED NEW "J" ANGLE CLIP P/N #600-34017-723 I/A/W WVAC E. O. #601R-53-2543A. 2 L 7 2 4F RT A21EA 2001070600107 20010706 00107 EA 2001 7 6 COMA0160436 1 20010703 A 2750 852D10011 ACTUATOR CNDAIR CL600 CL6002B19 EA BINDING A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 958CA 8561 1 7111 FLAPS FAILED AT 42 DEGREES.REPLACED THE RIGHT HAND #1 FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2001070600108 20010706 00108 EA 2001 7 6 COMA0160437 1 20010704 A 2750 852D10011 ACTUATOR CNDAIR CL600 CL6002B19 EA BINDING A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 958CA 10789 1 7111 FLAPS FAILED AT 40 DEGREES.REPLACED THE R/H #1 FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2001070600109 20010706 00109 2001 7 6 RAIA00107003 4 20010705 A 3425 7011672112 SYMBOL GENERATOR JETAIR JETSTM JETSTM4101 1500501 EU AVIONICS BAY FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 566HK 7034 5228 41084 7402-STL- COPILOT MULTI-FUNCTION DISPLAY FAILED. MAINTENANCE REMOVED AND REPLACED SYMBOL GENERATOR 2 L 7 2 4T RT A41NM 2001070900005 20010709 00005 WP 2001 7 9 01FDEA00450 1 20010614 A 2910 HYDRAULIC LINE DOUG DC10 DC1030 3023501 WP HYDRAULIC SYS DAMAGED A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SO 25 316FE 48314 NR 3 HYD QTY LEAK TO A QTY OF .2 GAL CAUSING LVL ALERT OF HYD 3 FAIL. ACCOMPLISH RED TABS INCLUDING ALT GEAR EXT. REMO VED AND REPLACED DAMAGED SECTION OF HYD LINE AND INSTALL NEW PIECE OF TUBING AND SWAGGED PER MM 20-10-01-2. LEAK CK GOO D. REINSTALLED PANELS AND SERVICED NR 3 HYD SYS. 2 L 7 3 4F A22WE 2001070900006 20010709 00006 NM 2001 7 9 01FDEA00451 1 20010615 A 3251 CONTROL CABLE DOUG MD11 MD11F 3023600 NM NLG LACK OF LUBE A FDEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 25 621FE 48792 ON T/O AIRCRAFT STARTED TO GO TO RIGHT. LEFT RUDDER COULD NOT CORRECT AND HAD TO USE TILLER. LUBED NLG PER SMP INSP ST EERING CABLES PER MM 32-51-00-0 & 32-50-00-5. RESERVICED NLG STRUT PER MM 32-11-01. AC OK FOR SERVICE. 2 L 7 3 4F RT A22WE 2001070900012 20010709 00012 NM 2001 7 9 01FDEA00459 1 20010615 A 2710 ACTUATOR DOUG MD11 MD11 3023602 NM AILERON OUT OF ADJ A FDEA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 SO 25 587FE 48489 A/C MADE AIR TURNBACK DUE DEFLECT AILERON DISAGREE ALERT. LT O/B ACTUATOR ADJUSTED AND SAFETIED PER MXP 27-2 METHOD "D" . 2 L 7 3 4F RT A22WE 2001070900013 20010709 00013 2001 7 9 01FDEA00461 4 20010616 A 3140 441790 WARNING SYSTEM AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2A5 NE COCKPIT ACTIVATED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 681FE 799 80C2 ON T/O ECAM WARN ENG FAIL NR 2 ABORTED TAKEOFF. RETURN FOR 2ND TRY AND RECEIVED ECAM WARN ENG SHUTDOWN. 2 L 7 2 4F 4 F RT A35EU E13NE 2001070900014 20010709 00014 EU 2001 7 9 01FDEA00462 1 20010616 A 3610 CONTACTOR AIRBUS 310 A310222 3930315 EU PNEUMATIC SYS DIRTY A FDEA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 25 416FE 288 BOTH BLD VLVS FAULTED RESULTING IN LOSS OF PRESSURE. CLEANED CONTACTS OF PSC'S AND INTERCHANGED THE SAME. SECURED PSC' S AND RAN ENG PER A310 JRH. NO FAULT NOTED. 2 L 7 2 4F RT A35EU 2001070900017 20010709 00017 EU 2001 7 9 01FDEA00467 1 20010619 A 3240 C20101303201 CONTROL UNIT AIRBUS 310 A310222 3930315 EU BRAKE SYSTEM FAILED A FDEA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 25 455FE 331 DURING BLOCK IN WITH PEDALS FULLY DEPRESSED, A/C WOULD NOT STOP. USED PARKING BRAKE TO STOP. BRAKE ANTI-SKID SEL IN NO RMAL/ON. REMOVED AND REPLACED BRAKE CONTROL UNIT (29GG) MM 32-42-72-4. 2 L 7 2 4F RT A35EU 2001070900018 20010709 00018 EU 2001 7 9 01FDEA00468 1 20010619 A 2611 SMOKE WARNING AIRBUS 310 A310222 3930315 EU COCKPIT ILLUMINATED A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 451FE 303 AFT T/O AT APPROX 300 FT, GOT SMOKE WARNING AFT MAIN DECK CARGO COMP DID ECAM PROC AND SMOKE LIGHT WENT OUT. 2 L 7 2 4F RT A35EU 2001070900019 20010709 00019 NM 2001 7 9 DHL2001708008 1 20010707 A 2761 2145014 ACTUATOR BOEING 727 72725 1384006 NM A DHLA K NONE O OTHER DE DESCENT 1 SO 01 708DH 18275 IN WINGS LEVEL DESCENT @ 280 KNOTS IAS SPEED BRAKE DEPLOYMENT CAUSES AIRCRAFT TO ROLL TO THE RIGHT. STOWING SPEED BRAKE CAUSES AIRCRAFT TO ROLL ABRUPTLY LEFT 15 DEGREES OPPOSITE DIRECTION YOKE DISPLACEMENT REQUIRED TO COUNTERACT ROLLING MOM ENT. PROBLEM STILL PRESENT AT 250KNT IAS"FOUND #ONE FLIGHT SPOILER ACTUATOR BY-PASSING R&R #ONE FLIGHT SPOILER ACTUATOR IAW B727 M/M 27-61-81, OPS CHECKS SERVICEABLEP/N OFF 21450-14 S/N OFF 417835 P/N ON 21450-14 S/N ON 458783STATUS: CL OSED 2 L 7 3 4F A3WE 2001070900020 20010709 00020 WP 2001 7 9 CALA0100636 1 20010706 A 5754 SLAT DOUG DC9 DC982 3022082 WP R/H WING, #2 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND R/H WING #2 SLAT DENTED AT LEADING EDGE. THE DENT WAS FILLED IAW SRM 57-03, FIGURE 20A & B. 2 L 7 2 4F A6WE 2001070900021 20010709 00021 NM 2001 7 9 CALA0100637 1 20010706 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 807 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14358 23943 INSPECTION FOUND FUSELAGE SKIN "DAMAGED" AT STA 807, S28L TO S26R. THE DAMAGE WAS REMOVED AND FILLER AND DOUBLER WERE IN STALLED IAW SRM 53-00-01. 2 L 7 2 4F RT A16WE 2001070900022 20010709 00022 WP 2001 7 9 CALA0100638 1 20010707 A 5330 SKIN DOUG DC9 DC982 3022082 WP FS 120 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND L/H FORWARD FUSELAGE EXTERNAL SKIN DENTED AT FS 120, LONGERON 18L. THE DENT WAS COLD WORKED AND A REPAI R DOUBLER WAS INSTALLED IAW EA 9-5331-2-A0902 AND ECRA 5331-01095. 2 L 7 2 4F A6WE 2001070900023 20010709 00023 NM 2001 7 9 CALA0100640 1 20010708 A 5230 SKIN BOEING 737 7373T0 1384582 NM C-1 DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14358 23943 INSPECTION FOUND THREE DENTS ON C-1 DOOR EXTERNAL SKIN. THE DENTS WERE LOCATED 12 INCHES FROM FORWARD EDGE OF DOOR. A RE PAIR DOUBLER WAS INSTALLED IAW SRM 52-00-01, FIGURE 203. 2 L 7 2 4F RT A16WE 2001070900024 20010709 00024 NM 2001 7 9 AWXA0001920 1 20010705 A 5730 654549517 SKIN PANEL BOEING 737 7372U9 1384498 NM WBL 172 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 149AW 60162 22575 D: PHX- While performing routine maintenance a 2" crack was found, (visually) on the L/H wing upper skin surface at WBL 172. The crack went from the Aft edge of skin panel Fwd though one rivit hole and to the next rivit hole Fwd where it te rminated.C: Maintenance repaired the crack per AWA engineering repair E.R. 15-5724-01182-DL1 and associated 8110-3. The repair is based off Boeing S/B 737-57-1144. 2 L 7 2 4F RT A16WE 2001070900025 20010709 00025 NM 2001 7 9 AWXA0001922 1 20010705 A 5330 656212550129 SKIN BOEING 737 7373G7 1384595 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 D: Phx- during routine maitenance the lower lobe skin was found to have corrosion at BS727-727A between STR 27L and Str 27R.C: Repaired per SRM 53-10-01, 51-10-6 and AWA E.R. 15-5331-01179-JL2 2 L 7 2 4F RT A16WE 2001070900026 20010709 00026 NM 2001 7 9 AWXA0001923 1 20010705 A 3260 841602 PSEU BOEING 757 7572S7 1384962 NM UNRELIABLE A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 904AW 38762 5229 23566 D: Phx- Air turnback - Flt 494 - Shortly after take off EICAS displayed Air/ Ground Disagree message, FRM code 32-09-03- 00, and the aircraft returned to Phx. C: In Phx maitenance trouble shot and performed a bite test of the PSEU which show ed no faults when faults should have existed. The PSEU was replaced. As a precaution both NLG not compressed sensors wer e replaced as well.Part name: Sensor(2ea) MFG: ELDEC Corp. P/N:8-345-01 Part Loc: NLG Part condition: Good (Precautiona ry) 2 L 7 2 4F RT A2NM 2001070900027 20010709 00027 NM 2001 7 9 AWXA0001933 1 20010705 A 5310 6546532 FRAME BOEING 737 7373G7 1384595 NM STA500 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 151AW 23219 D: Fuselage frame at fuselage station 500 cracked at upper flange and web. Forward of lower antenna. Between Stringer 2 8L and 28RC: Corrective action removed damaged area Fab'd repair parts, treated top coated and installed per SRM 51-70-1 1 2 L 7 2 4F RT A16WE 2001070900028 20010709 00028 NM 2001 7 9 AWXA0001934 1 20010705 A 5315 654583391 CREASE BEAM BOEING 737 7373G7 1384595 NM BS 178 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 151AW 23219 D: L/H crease beam cracked / broken at STA 178 W L 207C: Corrective action Fabricated repair clip Per E.R. # 03-5311-011 77-DD4 and installed. 2 L 7 2 4F RT A16WE 2001070900029 20010709 00029 NM 2001 7 9 AWXA0001935 1 20010705 A 5310 INTERCOSTAL BOEING 737 7373G7 1384595 NM STA 178 WL 207 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 151AW 23219 D: Intercostal at WL 207 B.S. 178.0 Shows evidence of crackC: Removed and replaced cracked intercostal WL 207 BS 178 Ref SRM 53-10-08 2 L 7 2 4F RT A16WE 2001070900030 20010709 00030 NM 2001 7 9 AWXA0001937 1 20010705 A 5311 65L35243 FRAME BOEING 737 7373G7 1384595 NM WL170 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 151AW 23219 D: STA 847 Frame Cracked Approx 3" at LWR stop fitting W.L170 RBL 40C: Removed & replaced frame per DWG 65C35243 2 L 7 2 4F RT A16WE 2001070900031 20010709 00031 WP 2001 7 9 AT0100201 1 20010611 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 106 LBL 15 CHAFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 819AT 47260 FOUND FRAME CHAFED AT BS 106 LBL 15. CORRECTIVE ACTION: INSTALLED REPAIR ANGLE IAW DC9 SRM 51-10-04, 51-10-03, AND 53-01 FIG 2. 2 L 7 2 4F A6WE 2001070900032 20010709 00032 WP 2001 7 9 AT0100202 1 20010606 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP BS 237-313 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 819AT 47260 FOUND CABIN FLOOR PANEL #48 CORRODED. CORRECTIVE ACTION: FABRICATED AND INSTALLED REPAIRS IAW DC9 SRM 53-20-01, 51-10-03 AND 51-10-02. 2 L 7 2 4F A6WE 2001070900033 20010709 00033 WP 2001 7 9 AT0100203 1 20010613 A 5330 SKIN DOUG DC9 DC932 3022066 WP FWD SERVICE DOOR CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 819AT 47260 FOUND CRACK IN FORWARD SERVICE DOOR JAMB CORNER. CORRECTIVE ACTION: FABRICATED AND INSTA LLED REPAIR IAW DC9 SRM 51-30-02, 51-30-03, 51-30-04, AND 51-30-05. 2 L 7 2 4F A6WE 2001070900034 20010709 00034 WP 2001 7 9 AT0100205 1 20010611 A 5315 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP BS 205-218 LBL15 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 819AT 47260 FOUND CABIN FLOOR SUPPORT AT LBL 15 IS CORRODED BEYOND LIMITS AT BS 205-218. CORRECTIVE ACTION: FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 51-30-05. 2 L 7 2 4F A6WE 2001070900035 20010709 00035 WP 2001 7 9 AT0100206 1 20010611 A 5315 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP BS 205 RBL 22-44 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 819AT 47260 FOUND FLOOR SUPPORT AT BS 205 RBL 22-44 CORRODEDBEYOND LIMITS. CORRECTIVE ACTION: FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 51-30-05. 2 L 7 2 4F A6WE 2001070900036 20010709 00036 WP 2001 7 9 AT0100207 1 20010611 A 5315 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP BS 160-218 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 819AT 47260 FOUND FLOOR SUPPORT AT BS 160-218 CORRODED BEYOND LIMITS. CORRECTIVE ACTION: FABRICATED AND INSTALLE D REPAIR IAW DC9 SRM 51-30-05. 2 L 7 2 4F A6WE 2001070900037 20010709 00037 WP 2001 7 9 AT0100208 1 20010610 A 5315 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 819AT 47260 FOUND FLOOR SUPPORT AT BS 160-200 CORRODED BEYOND LIMITS. CORRECTIVE ACTION: FABRICATED AND INSTALL ED REPAIR IAW DC9 SRM 51-10-04, 51-10-03, 51-20, AND 51-30-02. 2 L 7 2 4F A6WE 2001070900038 20010709 00038 WP 2001 7 9 AT0100210 1 20010611 A 5315 FLOOR PANEL DOUG DC9 DC932 3022066 WP BS 218-332 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 819AT 47260 FOUND FORWARD PIT FLOOR PANEL AT BS 218-332 CORRODED BEYOND LIMITS. CORRECTIVE ACTION: FABRICATED AND INSTALLED REPAIR PANEL IAW DC9 SRM 51-10-02, 51-10-03, AND 51-10-04. 2 L 7 2 4F A6WE 2001070900039 20010709 00039 WP 2001 7 9 AT0100211 1 20010612 A 5313 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 965-980 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 819AT 47260 FOUND AFT CARGO PIT INTERCOSTAL CORRODED BEYOND LIMITS AT BS 965-980. CORRECTIVE ACTION: FABRICATED AND INSTALLED NEW INTERCOSTAL IAW DC9 SRM 51-10-03, 51-30-02, 53-11-03, 51-10-04, AND 51-30-05. 2 L 7 2 4F A6WE 2001070900040 20010709 00040 WP 2001 7 9 AT0100212 1 20010613 A 5532 SPAR DOUG DC9 DC932 3022066 WP RT HORIZ STAB CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 819AT 47260 FOUND RIGHT HORIZONTAL STABILIZER SPAR CRACKED. CORRECTIVE ACTION: FABRICATED AND INSTALLED SPLICE ANGLES AND REPLACEMENT SECTION OF SPAR IAW 51-30-01, 51-30-05, AND 55-01 FIG 2. 2 L 7 2 4F A6WE 2001070900041 20010709 00041 EA 2001 7 9 COMA0160440 1 20010704 A 5310 60034017723 ANGLE CNDAIR CL600 CL6002B19 EA CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 991CA 7216 VERTICAL "J" ANGLE CLIP INSIDE CBPI @BL 9.0 LEFT HAND IS CRACKED.INSTALLED NEW "J" ANGLE CLIP P/N #600-34017-723 I/A/W W VAC E.O.#601R-53-2543A. 2 L 7 2 4F RT A21EA 2001070900042 20010709 00042 NM 2001 7 9 DHL2001717012 1 20010704 A 2613 DUCT BOEING 727 72723 1384004 NM A DHLA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 01 717DH 19389 WHILE CLIMBING THROUGH 18,500 THE LOWER AFT BODY OVHT LT ILLUMINATED ABNORMAL PROCEDURE COMPLIED WITHITEM TRANSFERRED T O DMI# 6261 PER DHL MEL 26-10-1 PLACARDS INSTALLED AND SPECIAL PROCEDURES 26-10-1 C/W RKENSIK 35047 07042001REF DMI 626 1 - CLIMB THROUGH 18,500 LWR AFT BODY OVHT ILLIMUNATEDINSPECTED DUCTING IN AFT AIRSTAIRS AND NO DEFECTS FOUND, RAN ENGIN E PER JRH 5.2 COULD NOT DUPLICATE OVER HEAT IND NO LEAKS FOUND OK FOR SERVICE PER 26-14-00 THIS CLEARS DMI# 6261DUE TO P REVIOUS HISTORY AND PER MXC REQUEST T/S AFT LOWER BODY OVERHEAT SYSTEM THOROUGHLYFOLLOWING THE R+R OF WING ANTI-ICE DUCT (SEE LP 260048 ITEM 7M) AND LOWER AFT BODY HEAT FIRE DETECTION SENSING ELEMENT(SEE LP 260049 ITEM 8 2 L 7 3 4F A3WE 2001070900043 20010709 00043 EU 2001 7 9 ASOA01076 1 20010605 A 5300 FRAME AEROSP ATR72 ATR72 EU CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 530AS 11668 453 DURING C-CHECK INSPECTION IN BNA, MAINTENANCE FOUND CRACK AT FRAME 26. MAINTENANCE REPAIRED CRACK AT FRAME 26 IAW ASA E 072-53-0111 AND ATR S/B 72-53-1078, WHICH OUTLINES THIS REPAIR. (M) 2 H 7 2 4T RT 2001070900044 20010709 00044 SO 2001 7 9 ASOA01082 1 20010617 A 3397 MS2275941249 WIRE EMB 120 EMB120 3260201 SO CABIN CHAFED A K NONE L NO TEST TX TAXI/GRND HDL 1 SO 11 229AS 120042 FLT 4001 - DURING TAXI FOR TAKEOFF OUT OF ABY, EMERGENCY LIGHT CIRCUIT BREAKER POPPED AND EMERGENCY LIGHT NOT ARMED LIGH T ILLUMINATED. CREW RESET CIRCUIT BREAKER. IT POPPED AGAIN AFTER ENGINE WAS SHUTDOWN AND THE FASTEN SEATBELT SWITCH WA S TURNED OFF. MAINTENANCE REMOVED AND REPLACED BOTH CONTROL SWITCHES (RELAY K00201) AND CONTACTOR (K0028), BUT IT WAS N O HELP. MAINTENANCE THEN FOUND A CHAFED WIRE AT ROW 7 AND RESECURED IT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001070900045 20010709 00045 CE 2001 7 9 S2YA01010 1 20010513 A 3230 MS24171D1 RELAY BEECH 1900 1900D 1154162 CE A S2YA O OTHER J WARNING INDICATION AP APPROACH 1 GL 13 841SK UE84 FLT 1056 - MKE-IND - DURING APPROACH, THE CREW SELECTED GEAR DOWN BUT DID NOT ACHIEVE DOWN AND LOCKED ALSO THE RED INTRA NSIT LGHT IN THE GEAR HANDLE REMAINED ILLUMINATED. THE CREW THEN EMERGENCY HAND PUMPED THE GEAR DOWN AND ACHIEVED THREE GREEN DOWN AND LOCKED. THE CREW MADE AN UNEVENTFUL LANDING AND LATER FERRIED THE A/C BACK TO MKE. MAINTENANCE INSPECT ED THE SYSTEM AND FOUND THE LANDING GEAR CIRCUIT BREAKER (CB) POPPED AND A LOOSE POSITIVE STUD ON THE LANDING GEAR POWER PACK MOTOR. MAINTENANCE RESET THE CB AND REPLACED THE POWER PACK MOTOR. MAINTENANCE OPERATED THE LANDING GEAR AND THE CB POPPED AFTER TWO CYCLES. MAINTENANCE REPLACED THE POWER PACK RELAY AND CB. MAINTENANCE OPERATED THE LANDING GEAR W 2 L 7 2 4T RT A24CE 2001070900046 20010709 00046 WP 2001 7 9 USAAD01127 1 20010615 A 3350 AD4002P BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 804US 48052 IND - THE AFT LEFT AND RIGHT OVERWING EMERGENCY EXIT SIGNS DID NOT ILLUMINATE DURING TEST. MAINTENANCE REPLACED THE EME RGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001070900047 20010709 00047 NM 2001 7 9 EIA2001201 1 20010326 A 5300 PAN BOEING 747 747128 1384894 NM FS 807 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - FOUND STATION 807 FORWARD UPPER EDGE L2 DOOR CUTOUT, DOOR FRAME PAN CRACKED. REPAIRED PER ECRA 3203-53-038-2. (M) 2 L 7 4 4F A20WE 2001070900048 20010709 00048 NM 2001 7 9 EIA2001207 1 20010328 A 5300 DOUBLER BOEING 747 747128 1384894 NM FS 440-460 BULGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - FOUND LEFT STATION 440-460 STRINGER 14L TO STRINGER 14EL, SKIN UNDER REPAIR DOUBLER BULGED. REPAIRED PER ECRA 3203-53-039-2. (M) 2 L 7 4 4F A20WE 2001070900049 20010709 00049 NM 2001 7 9 EIA2001208 1 20010328 A 5300 FORGING BOEING 747 747128 1384894 NM FS 1040-1060 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - FOUND RIGHT STATION 1040-1010 CORROSION EXTENDING OUT FROM UNDER WINDOW FORGING SEALANT. REPAIRED PER ECRA 32 03-53-047-2. (M) 2 L 7 4 4F A20WE 2001070900050 20010709 00050 NM 2001 7 9 EIA2001209 1 20010328 A 5300 FORGING BOEING 747 747128 1384894 NM FS 1427 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - FOUND RIGHT STATION 1427 CORROSION ON AND AROUND WINDOW FORGING. REPAIRED PER ECRA 3203-53-047-2. (M) 2 L 7 4 4F A20WE 2001070900051 20010709 00051 NM 2001 7 9 EIA2001210 1 20010328 A 5300 FORGING BOEING 747 747128 1384894 NM FS 1130 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - FOUND LEFT STATION 1130 CORROSION ON AND AROUND WINDOW FORGING. REPAIRED PER ECRA 3203-53-047-2. (M) 2 L 7 4 4F A20WE 2001070900052 20010709 00052 NM 2001 7 9 EIA2001211 1 20010328 A 5300 FORGING BOEING 747 747128 1384894 NM FS 370 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - FOUND STATION 370 CORROSION ON AND AROUND L-12 WINDOW FORGING. REPAIRED PER ECRA 3203-53-047-2. (M) 2 L 7 4 4F A20WE 2001070900053 20010709 00053 NM 2001 7 9 EIA2001212 1 20010328 A 5300 FORGING BOEING 747 747128 1384894 NM FS 1210 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - FOUND RIGHT STATION 1210 CORROSION ON AND AROUND WINDOW FORGING. REPAIRED PER ECRA 3203-53-047-2. (M) 2 L 7 4 4F A20WE 2001070900054 20010709 00054 NM 2001 7 9 EIA2001213 1 20010328 A 5300 FORGING BOEING 747 747128 1384894 NM FS 250 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - FOUND STATION 250 SURFACE CORROSION ON R-5 WINDOW FRAME INTERIOR AFT LOWER CORNER. REPAIRED PER ECRA 3203-53- 047-2. (M) 2 L 7 4 4F A20WE 2001070900055 20010709 00055 NM 2001 7 9 EIA2001214 1 20010328 A 5300 FORGING BOEING 747 747128 1384894 NM FS 230 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - FOUND STATION 230 SURFACE CORROSION ON R-4 WINDOW FRAME INTERIOR AFT UPPER CORNER. REPAIRED PER ECRA 3203-53- 047-2. (M) 2 L 7 4 4F A20WE 2001070900056 20010709 00056 NM 2001 7 9 EA2001215 1 20010328 A 5300 WEB BOEING 747 747128 1384894 NM BS 1265 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - FOUND MED NR 3 BS 1265 FRAME CRACKS. REPAIRED AND MODIFIED PER EO 53-747-1580-00 REV D. (M) 2 L 7 4 4F A20WE 2001070900057 20010709 00057 NM 2001 7 9 EIA2001216 1 20010329 A 5300 FORGING BOEING 747 747128 1384894 NM FS 1416-1438 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - FOUND MAIN CABIN LEFT STATION 1416-1438 STRINGER 20L TO STRINGER 22L CORROSION AT WINDOW FORGING. REPAIRED PE R ECRA 3203-53-047-2. (M) 2 L 7 4 4F A20WE 2001070900058 20010709 00058 NM 2001 7 9 EIA2001218 1 20010331 A 5300 FORGING BOEING 747 747128 1384894 NM FS 560-580 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - FOUND RIGHT STATION 560-580 STRINGER 8R TO STRINGER 10R CORROSION AROUND EDGES OF 1R WINDOW FORGING. REPAIRED PER ECRA 3203-53-047-2. (M) 2 L 7 4 4F A20WE 2001070900059 20010709 00059 NM 2001 7 9 EIA2001219 1 20010331 A 5300 FORGING BOEING 747 747128 1384894 NM FS 620 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - LEFT STATION 620-640 STRINGER 10L CORROSION ON 2L WINDOW FORGING. REPAIRED PER ECRA 3203-53-047-2. (M) 2 L 7 4 4F A20WE 2001070900060 20010709 00060 NM 2001 7 9 EIA2001220 1 20010331 A 5300 FORGING BOEING 747 747128 1384894 NM FS 1080-1100 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - LEFT STATION 1080-1100 STRINGER 20L TO STRINGER 22L CORROSION UNDER WINDOW FORGING. REPAIRED PER ECRA 3203-53 -047-2. (M) 2 L 7 4 4F A20WE 2001070900061 20010709 00061 NM 2001 7 9 USAASB01173 1 20010615 A 3350 20131A BATTERY PACK BOEING 737 7374B7 1384702 NM AFT CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 428US 24550 PHL - MAINTENANCE FOUND THE EMERGENCY LIGHTS IN THE AFT SECTION OF CABIN IN SEAT ROWS 20 TO 23, 20 TO 21 OVERHEAD AND AF T EXIT DOORS SIGNS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001070900062 20010709 00062 NM 2001 7 9 USAASB01176 1 20010616 A 3350 6104789 BATTERY PACK BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 22885 BWI - THE LEFT OVERWING AN LEFT LOWER FUSELAGE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LI GHT BATTERY PACK. (M) 2 L 7 2 4F A16WE 2001070900063 20010709 00063 WP 2001 7 9 USAAD01129 1 20010620 A 4900 36177502 FUEL CONTROL DOUG DC9 DC981 3022081 WP FAILED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 828US 48028 PIT-MIA - FLT 375 - DURING CRUISE, THE APU QUIT RUNNING. THE APU WAS RESTARTED AND RAN A FEW MINUTES BEFORE QUITTING AG AIN. AS THE LEFT ENGINE DRIVEN GENERATOR WAS ON MEL, THE AIRCRAFT NOW ONLY HAD ONE OPERATING GENERATOR. THE AIRCRAFT D IVERTED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE APU FUEL CONTROL, FUEL SOLENOID VALVE, AND COMBUST ION CAN. THE LEFT ENGINE GENERATOR POWER RELAY WAS ALSO REPLACED AND THE LEFT GENERATOR MEL REMOVED. (M) 2 L 7 2 4F A6WE 2001070900064 20010709 00064 WP 2001 7 9 ZW0A0104701 1 20010708 A 3350 58222 POWER SUPPLY DOUG DC9 DC983 3022083 WP B5-28 A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9622A 53593 THE EGRESS LIGHTS WERE INOPERATIVE FROM ROW 25 BACK. REPLACED THE POWER SUPPLY. CHECK-C 8-3-00 STL. --CLOSED-- 2 L 7 2 4F RT A6WE 2001070900065 20010709 00065 NM 2001 7 9 UPS01236256 1 20010620 A 5310 WEB BOEING 727 72721C 138400M NM NLGWW BS259 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 INSPECTION TYPE:C NOSE LANDING GEAR BAY LH SIDE AT BS 259 SIDE WALL HAS A CRACK INICATION. REMOVED ACCESS PANEL #312 4 AND LOWER WEB TO GAIN ACCESS TO DAMAGE AREA, CUT OUT DAMAGE AREA APPROX 5"X1" AT NOSE LANDING GEAR BS259 AS PER B727 S RM51-40-2 ACCOMPLISHED NDT INSPECTION AT CUT OUT AREA INSTALL DOUBLER REPARI APPROX 8"X6" 2 L 7 3 4F A3WE 2001070900066 20010709 00066 NM 2001 7 9 UPS01236257 1 20010628 A 5310 FRAME BOEING 727 72721C 138400M NM FUSELAGE BS913.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 INSPECTION TYPE:C CRACK INDICATION AT FRAME, FUSELAGE BS913.5 RIGHT SIDE. CRACK CONFIRMED BY NDT INSP. PART 6 51-00 -00 STOP DRILL CRACK AT FRAME AT BS 913.5 B727-51-10-01 INSTALLED KIT REPAIR AS PER EO B727- 5310-1896-B APPENDIX C AT FRAM FUSELAGE BS 913.5 RH SIDE KIT #65627 194-26. 2 L 7 3 4F A3WE 2001070900067 20010709 00067 NM 2001 7 9 UPS01236258 1 20010620 A 5310 WEB BOEING 727 72721C 138400M NM NLGWW BS266 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 INSPECTION TYPE:C NOSE LANDING GEAR BAY RH SIDE WALL AT BS 266 HAS A CRACK INDICATION. REMOVED ACCESS PANEL #3125 AS PER SRMB727-51-30-2 CUT OUT DAMAGE AREA AS PER B727-51-40-2 APPROX 3.5"X1" ACCOMLPISHED NDT INSPECTION AND INSTALLED DO UBLER REPAIR AS PER B727-SRM51-40-2 FIG 1 APPROX SIZE 3"X1". 2 L 7 3 4F A3WE 2001070900068 20010709 00068 NM 2001 7 9 UPS01236260 1 20010620 A 5310 BULKHEAD BOEING 727 72721C 138400M NM RH W/W STA 870 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 INSPECTION TYPE:C RIGHT WHEEL WELL STA 870 BULKHEAD CRACK AT APU VALVE CUT OUT RBL4.5 STOP DRILL CRACK ON RH W/W STA 870 AT APU VALVE CUT OUT RBL45 STOP DRILL 1/4" SIVE AND NDT INSPECTION ACCOMPISHED HFEC AS PER PART6-51- 00-00 FIG4 IN STALL 3 DOUBLER REPAIRS PART# 15-5PH. INSTALLED REPAIR AT RH W/W AT STA 870 RBL45 AS PER SRMB727-53-10-9 FIG #5. 2 L 7 3 4F A3WE 2001070900069 20010709 00069 NM 2001 7 9 DL72S011070 1 20010626 A 5311 UNK WEB BOEING 727 727232 1384082 NM AFT FUSELAGE CRACKED A DALA O OTHER O OTHER IN INSP/MAINT 1 SO 27 539DA 22385 FOUND ON F2 LETTER CHECK; L/H AND R/H WEB CRACKED 1 INCH AT TAIL CRAWLWAY BOTTOM END AT STA. 1303 REPAIRED PER DRD 53-10-4D FIG 802D 2 L 7 3 4F A3WE 2001070900070 20010709 00070 NM 2001 7 9 DL767011077 1 20010626 A 5312 148T31101 BULKHEAD BOEING 767 767232 1385132 NM STA 1809 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 104DA 22216 DURING ACCOMPLISHMENT INSPECTIONS PER BAC S/B 767-53-0078, CRACKS WERE FOUND IN THE TENSION FITTING, FWD OUTER CHORD, AND SKIN. THE S/B ONLY COVERS CRACKS IN THE OUTER CHORD. CORRECTIVE ACTION: REPAIRED PER DAL ERA 397710-14AD 2 L 7 2 4F RT A1NM 2001070900071 20010709 00071 NM 2001 7 9 DL72S011080 1 20010627 A 5330 SKIN BOEING 727 727232 1384082 NM FS 303, S-10L CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 539DA 22385 FUSELAGE / SKIN / L1 DOOR CUTOUT / UPPER HINGE CUTOUT : CRACK REPAIR A .75" CRACK WAS FOUND IN THE SKIN AT THE UPPER HINGE CUTOUTOF THE L1 DOOR OPENING. THE CRACK WAS ROUTED OUT OF THE SKIN AND REPAIRED WITH AN EXTERNAL STEEL DOUBLER PER THE PROCEDURES OF BAC S/B 727-53-0198 AND ER/A 381212-14, REV B. 2 L 7 3 4F A3WE 2001070900072 20010709 00072 NM 2001 7 9 DL73K011081 1 20010627 A 5330 65737433 SKIN BOEING 737 737247 138448D NM FS 492, S-25R CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 382DL 23609 FUSELAGE / SKIN ASSY / C1 DOOR CUTOUT / FS 492 / STRG. 25R :CRACK REPAIR THE FUSELAGE SKIN AND UNDERLYING BEARSTRAP WERE FOUND CRACKED AT AN EXISTING FASTENER LOCATION COMMON TO THE FS 492 FRAME BELOW STRINGER 25R. THE CRACK WAS REMOVED WITH A 1.8" CUTOUT THROUGH THE SKIN AND BEARSTRAP. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM DOUBLERS INSTALLED PER ER/A 381125-14, REV A. 2 L 7 2 4F A16WE 2001070900073 20010709 00073 NM 2001 7 9 DL73K011082 1 20010627 A 5330 654577646 SKIN BOEING 737 737247 138448D NM FS 837, S-27R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 382DL 23609 FUSELAGE / SKIN / FS 837 / STRG. 27R / ANTENNA CUTOUT : CORROSION REPAIR THE FUSELAGE SKIN WAS FOUND CORRODED AT AN EXISTING ANTENNA CUTOUT AT FS 837 BETWEEN STRINGERS 26R & 27R. THE CUTOUT REINFORCING DOUBLER WAS ALSO CORRODED. THE DOUBLER WAS REMOVED AND A NEW DOUBLER INSTALLED. THE CORROSION IN THE SKIN WAS REMOVED BY INCREASING THE CUTOUT TO 2" X 1.5". THE SKIN WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 381045-14, REV B. 2 L 7 2 4F A16WE 2001070900074 20010709 00074 NM 2001 7 9 DL72S011087 1 20010629 A 5330 65182175 SKIN BOEING 727 727232 1384082 NM SKIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 532DA 22045 DURING THE ACCOMPLISHMENT OF THE INSPECTIONS REQUIRED BY AD 99-04-22, TWO CRACKS WERE FOUND IN THE STR 4L LAP JOINT BETWEEN FS 380 AND 400. THE CRACKS WERE CUT OUT AND REPAIRED PER B727 SRM 53-30-3, FIGURE 5. THE CRACKS WERE FOUND AT HMV. 2 L 7 3 4F A3WE 2001070900075 20010709 00075 NM 2001 7 9 DL73K011088 1 20010629 A 5311 FRAME BOEING 737 737232 1384475 NM CABIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 317DL 23089 CRACKS WERE FOUND AT THE BOTTOM TWO FASTENERS ON THE INNER CCHORD OF THE LEFT FS 616 FRAME AT THE OVERWING FRAME TO STUB BEAM JOINT. THE CRACKS ARE TYPICAL OF THAT SHOWN IN S/B 737-53-1182. THE CRACKS WERE CUT OUT AND REPAIRED PER S/B 737-53-1182. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001070900076 20010709 00076 NM 2001 7 9 DL72S011089 1 20010629 A 5330 6554574158 SKIN BOEING 727 727232 1384082 NM SKIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 532DA 22045 DURING AN INSPECTION REQUIRED BY AD 99-04-22 CRACKS WERE FOUND IN THE STR 4R LAP JOINT BETWEEN FS 660 AND 680. THE CRACKS WERE CUT OUT AND AN EXTERNAL REPAIR INSTALLED. THE DAMAGE WAS FOUND AT HMV. 2 L 7 3 4F A3WE 2001070900077 20010709 00077 NM 2001 7 9 DL72S011090 1 20010629 A 5311 651631633 FRAME BOEING 727 727232 1384082 NM CABIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 532DA 22045 DURING HMV A CRACK WAS FOUND IN THE FS 344 FRAME DIRECTLY ABOVE THE L1 DOOR. THE CRACK WAS .5". THE CRACK WAS CUT OUT AND A DOUBLER WAS INSTALLED. THE DAMAGE WAS FOUND AT HMV. 2 L 7 3 4F A3WE 2001070900078 20010709 00078 NM 2001 7 9 DLM88011091 1 20010629 A 3397 WHITE22N WIRE DOUG MD88 MD88 3023688 NM FIRST CLASS BROKEN A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 916DE 53421 FIRST CLASS WALL MOUNTED RED EMER. LIGHT INOP. CORR:REPAIRED 2 EA BROKEN WIRES APPROX. 3.5 FEET FROM LITE ASSY. 2 L 7 2 4F RT A6WE 2001070900079 20010709 00079 NM 2001 7 9 DL72S011098 1 20010701 A 5410 65187227 FITTING BOEING 727 727232 1384082 NM PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 532DA 22045 DURING INSPECTIONS PER AD 97-05-08, CRACKS WERE FOUND IN THE#1 FORWARD ENGINE MOUNT AT HOLES C AND D. THE HOLES WERE OVERSIZED, INSPECTED AND NEW FASTENERS INSTALLED PER ERA 397735-14AD AT HMV. 2 L 7 3 4F A3WE 2001070900080 20010709 00080 NE 2001 7 9 DL76L011101 2 20010702 A 7200 PW4060 ENGINE 8010003 BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE #1 ENGINE FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 176DN F23430 25061 724687 ACFT ATB DUE TO NBR 1 ENGINE FLUX. REPLACED FMU. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS 2 L 7 2 4F 4 F RT A1NM E24NE 2001070900081 20010709 00081 NM 2001 7 9 DL76G011109 1 20010704 A 2150 111975 DETECTOR BOEING 767 767332 1382001 NM E/E COMPT DIRTY A DALA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SO 27 169DZ 29689 GOT FWD EQP OVERHEAT LT ON TAXI-OUT. WENT TO STANDBY PER MANUALS FOR 5 MINS NO LIGHT. TOOK OFF GOT LITE AGAIN AFTER T/O WENT TO OVRD PER POM AND RETURNED TO AIRPORT C/A - ECS PG SHOWS FLT DK SUP FLOW MAINT MSG. PER F.I.M. CLEANED TS163 SENSOR. 2 L 7 2 4F RT A1NM 2001070900082 20010709 00082 NM 2001 7 9 DL72S011117 1 20010706 A 5330 6518217190 SKIN BOEING 727 727232 1384082 NM LAP JOINT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 533DA 22046 WHILE ACCOMPLISHING LFEC INSPECTIONS PER AD 99-04-22, A CRACK WAS FOUND IN THE STR 4L LAP JOINT AT BETWEEN FS 440 AND 460. THE CRACK WAS CUT OUT AND REPAIRED PER B727 SRM 53-30-3, FIGURE 5. THE DAMAGE WAS FOUND AT HMV. 2 L 7 3 4F A3WE 2001070900083 20010709 00083 NM 2001 7 9 DL757011120 1 20010705 A 5330 143N33203 SKIN BOEING 757 757232 1384965 NM FS 620, S-17L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 640DL 23994 FUSELAGE / SKIN / FS 615-630 / STRG. 17L : SKIN CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND WITH AN EXISTING BLIND FASTENER REPAIR AND A DENT BETWEEN FS 615 & 630 AT STRINGER 17L. THE REPAIR WAS REMOVED AND ALL FASTENER HOLES COMMON TO THE REPAIR AND THE DENT REMOVED WITH A SINGLE 14" X 8 " CUTOUT. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM DOUBLERS INSTALLED PER ER/A 381112-14, REV A. 2 L 7 2 4F RT A2NM 2001070900084 20010709 00084 NM 2001 7 9 DL72W011133 1 20010708 A 3350 10617842 BATTERY BOEING 727 727247 138408F NM F/C CABIN DISCHARGED A DALA K NONE H ELECT. POWER LOSS-50 PC IN INSP/MAINT 1 SO 27 2820W 21058 1ST CLASS AISLE EMERGENCY LT INOP - REPLACED BATTERY PACK 2 L 7 3 4F A3WE 2001070900085 20010709 00085 NM 2001 7 9 DL72S011135 1 20010709 A 5311 6516326 FRAME BOEING 727 727232 1384082 NM CABIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 533DA 22046 A CRACK WAS FOUND IN THE LOWER HOLE OF THE FS 783.95 FRAME TYPICAL TO THAT NOTED IN SB 727-53-0197. THE CRACK WAS CUT OUT AND REPAIRED WITH A 65C36280-24 KIT PER THE S/B. THE DAMAGE WAS FOUND DURING THE AD MANDATED INSPECTION. 2 L 7 3 4F A3WE 2001070900086 20010709 00086 NM 2001 7 9 DLM88011136 1 20010709 A 5311 991859501 FRAME DOUG MD88 MD88 3023688 NM CABIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 943DL 49816 CRACKS WERE FOUND IN THE FS 1446 FRAME ON BOTH THE LEFT AND RIGHT SIDES SIMILIAR TO THOSE NOTED IN S/B 53-227. THE FRAME WAS REPLACED. THE DAMAGE WAS NOTED PER INSPECTION AT HMV. 2 L 7 2 4F RT A6WE 2001070900087 20010709 00087 2001 7 9 PNSA010606 4 20010620 A 2300 TELEPHONICS SAAB SF340 340B 7860101 EU A PNSA K NONE S AFFECT SYSTEMS TX TAXI/GRND HDL 1 AL 03 695PA 0126 340B310 DURING PREFLIGHT CHECKS RH AUDIO PANEL FAILED CAUSING STATIC IN THE COMM SYSTEMS. REPLACED AUDIO PANEL. OPERATIONAL CHEC K OK. 2 L 7 2 4T RT A52EU 2001070900088 20010709 00088 EU 2001 7 9 RAIA00107004 1 20010705 A 3610 S2L226 SEAL JETAIR JETSTM JETSTM4101 1500501 EU LEFT/RIGHT L/E FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 553HK 41066 5408-EWR-LEFT AND RIGHT DUCT FAIL CAPTION ILLUMINATED DURING TAXI. MAINTENANCE INSPECTED AND REPLACED LEFT AND RIGHT LEA DING EDGE BLEED AIR SEALS. 2 L 7 2 4T RT A41NM 2001070900089 20010709 00089 EU 2001 7 9 RAIA00107005 1 20010706 A 3230 AIR869461 ACTUATOR JETAIR JETSTM JETSTM4101 1500501 EU L/H MLG FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 566HK 14185 41084 7412-STL-LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. MAINTENANCE INSPECTED AND REPLACED LEFT MAIN LANDING GEAR RETRACT ACTUATOR. 2 L 7 2 4T RT A41NM 2001070900090 20010709 00090 2001 7 9 RAIA00107006 4 20010706 A 3417 7000700959 ADC AEROSP ATR42 ATR42300 8680920 EU AVIONICS BAY FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 422TE 23659 2290 106 7166-STL-ADU SCREEN SHOWING FLAT LINE INDICATION. MAINTENANCE INSPECTED AND REPLACED LEFT AIR DATA COMPUTER. 2 H 7 2 4T RT A53EU 2001070900091 20010709 00091 EU 2001 7 9 RAIA00107007 1 20010706 A 2844 D10036D06 FITTING JETAIR JETSTM JETSTM4101 1500501 EU LEAKING A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 555HK 41072 7098-STL-LEFT ENGINE LOW FUEL PRESSURE CAPTION ILLUMINATED ON TAKEOFF. MAINTENANCE INSPECTED AND FOUND LEFT ENGINE MOTIV E FLOW VALVE FUEL LINE FITTING LEAKING. MAINTENANCE REPLACED LEFT MOTIVE FLOW FUEL LINE FITTING. 2 L 7 2 4T RT A41NM 2001070900092 20010709 00092 2001 7 9 RAIA00107008 4 20010708 A 3420 7003360944 COMPUTER AEROSP ATR42 ATR42300 8680920 EU AVIONICS BAY FAILED A RAIA D RETURN TO BLOCK I FLT. ATTITUDE INST. TX TAXI/GRND HDL 1 CE 03 426TE 19313 4175 228 7011-STL-FIRST OFFICERS ATTITUDE PITCH FAILED DURING TAXI. MAINTENANCE INSPECTED AND REPLACED RIGHT AHRS COMPUTER. 2 H 7 2 4T RT A53EU 2001071000001 20010710 00001 CE 2001 7 10 C2XA01CL162 1 20010707 A 2120 1005240731 MOTOR BEECH 1900 1900D 1154162 CE BURNED A C2XA K NONE O OTHER AP APPROACH 1 SW 27 81556 UE239 CLE FLT.#3104 THE CREW REPORTED PUNGENT SMELL FROM VENT BLOWERSMAINTENANCE FOUND FLAP MOTER CAUSING SMELL AND REPLACED FLAP MOTOR. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 2001071000002 20010710 00002 SO 2001 7 10 C2XA01CL163 1 20010707 A 2610 3601133500230 LOOP EMB 145 EMB145LR SO ENGINE COWLING FAULTY A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 14972 151 CLE FLT.#3743 THE CREW REPORTED RIGHT ENGINE FIRE DETECTOR FAILED TESTMAINTENANCE REPLACED RIGHT ENGINE FIRE DETECTOR LOOP. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2001071000003 20010710 00003 SO 2001 7 10 C2XA01IA292 1 20010704 A 3350 3071BPE LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16718 120136 IAH - 3302, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT AN OVERHEAD EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTE NANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001080900263 20010809 00263 NM 2001 8 9 01FDEA00523 1 20010702 A 5315 AFA78037 FLOORBEAM DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 608FE 48548 SNRM N 552 MAIN DECK COMPT FLOORBEAM AT BS 1661 FND CRACKED. R&R PER EA 1-5310-57085. 2 L 7 3 4F RT A22WE 2001081500071 20010815 00071 NM 2001 8 15 01FDEA00524 1 20010706 A 5330 SKIN BOEING 727 72725C 138400H NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 DURING INSP HFEC IND CRACK FUSELAGE SKIN RT AT BS 252 BELOW CO-PILOTS NR 3 WINDOW. *S/D* REMOVED AND REPLACED PER IAW EA 7-5330-57300. 2 L 7 3 4F A3WE 2001081500072 20010815 00072 NM 2001 8 15 01FDEA00525 1 20010709 A 5330 SKIN BOEING 727 727277 138408S NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 LWR EXTERNAL SKIN HAS DENT FWD OF BS 196.5 AT RBL 11, WL 170. *S/D* REMOVED AND REPLACED SKIN PER IAW FEDEX SRM 53-30- 3 FIG 1. 2 L 7 3 4F RT A3WE 2001081500073 20010815 00073 NM 2001 8 15 01FDEA00526 1 20010709 A 5310 TORQUE BOX BOEING 727 727277 138408S NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 CRACKED RT LWR VERTICAL TORQUE BOX WEB BS 1225, RBL 20.5, WL 193. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 51-40-2 . 2 L 7 3 4F RT A3WE 2001071000004 20010710 00004 CE 2001 7 10 20010604CW004 1 20010410 A 2720 41112 CAM CESSNA CESSNA 402 402C 207590R CE RUDDER DAMAGED D HYIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NE 01 68391 402C0483 AFTER T/O CREW EXPERIENCED RUDDER LOCK. THROUGH MANIPULATION OF THE ELEVATOR. CONTROLLED RUDDER GUST LOCK RELEASE AND BY WORKING THE RUDDER PEDALS, THE SYSTEM WAS UNLOCKED. MECHANIC FOUND RUDDER GUST LOCK RELEASE CAM DISFIGURED, CAUSING THE RELEASE MECHANISM TO BE INEFFECTIVE WELL BEYOND NORMAL RELEASE RANGE. FOUND THAT IF AN APPLIED SIDE LOAD (IE TRYING TO RELEASE THE RUDDER LOCK W/PEDALS HARDOVER IN TAXI CAUSED EXCESS PRESSURE ON THE RELEASE CAM BENDING IT OUT OF RIG RE NDERING THE LOCK INEFFECTIVE. SUGGEST RELEASING PRIOR TO TAXI OR DURING PRE-FLIGHT. 1 L 7 2 3O A7CE 2001071000005 20010710 00005 NM 2001 7 10 2001F00095 1 20010607 A 2130 7248272 RELIEF VALVE BOEING 727 727224 1384076 NM CABIN PRESSURE FAILED A FX7A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 79749 22451 FLT 523 - MIA-CCS - DURING CLIMB-OUT, CREW UNABLE TO CONTROL CABIN PRESSURE. OUTFLOW VALVE CLOSED DURING ENTIRE TIME. AIRCRAFT RETURNED TO MIAMI WITH NO EMERGENCY LANDING DECLARED. SWAPPED AIRCRAFT, FLIGHT DEPARTED TO ORIGINAL DESTINATIO N 3:45 MIN DELAY. TROUBLE SHOT PRESSURIZATION PROBLEM TO CABIN SAFETY RELIEF VALVE FAILED IN THE OPEN POSITION. REMOVE D AND REPLACED SAFETY RELIEF VALVE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001071000006 20010710 00006 NM 2001 7 10 2001F00096 1 20010612 A 2130 39296421 SHUTOFF VALVE BOEING 727 727225 1384077 NM CABIN PRESSURE LEAKING A MYWA B A EMER. DESCENT UNSCHED LANDING O OTHER CR CRUISE 1 SO 19 889MA 21854 WHILE ON SINGLE PACK OPERATION AND AT FL250 CABIN PRESS KEPT CLIMBING. FOLLOWED AOM PROCEDURE AND DESCENDED. WHILE DES CENDING CABIN CONTINUED TO CLIMB TO FL160 WITH THRUST LEVERS UP, PASS MASKS DROPPED AT 13,000 FEET. FOUND CLAMPS TO HEA T EXCHANGER VERY LOOSE AND SHUTOFF VALVE LEAKING. REMOVED/REPLACED SHUTOFF VALVE AND TIGHTENED ALL CLAMPS ON LEFT AND R IGHT SIDE HEAT EXCHANGERS. REMOVED AND REPLACED NR 1 ENGINE 13TH STAGE MODULATING VALVE IAW 36-12-41. REMOVED AND REPL ACED E/E FAN BLOWER VALVE IAW 21-58-21. RUNUP WAS PERFORMED, ALL PRESS SYSTEMS OPS CHECK GOOD IAW AMM 21-30-00. LEAK C HECK OF NR 1 ENGINE VALVE AND E/E FAN EXHAUST VALVE OK IAW AMM 36-12-41 AND AMM 21-58-21. (M) 2 L 7 3 4F A3WE 2001071000007 20010710 00007 NM 2001 7 10 2001F00098 1 20010527 A 5753 DAT6278A14 BEARING BOEING 727 727225 1384077 NM T/E FLAP FROZEN A MYWA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 19 887MA 21857 DURING CLIMB-OUT FROM NGU, UPON RETRACTING FLAPS INBOARD FLAPS STUCK AT 15 DEGREES. ACCOMPLISHED ABNORMAL PROCEDURES, N O HELP. RETURNED TO NGU. FOUND RIGHT INBOARD FLAP INBOARD JACKSCREW FAIRING (ELEPHANT EAR) BEARING FROZEN. CLEANED BE ARING AND LUBED IAW MM 12-22-01. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001071000008 20010710 00008 NM 2001 7 10 2001F00099 1 20010614 A 2612 356644400 ELEMENT BOEING 727 72782C 1384026 NM RT MLG WW MALFUNCTIONED A RYNA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 07 528PC 19597 WHEEL WELL FIRE LIGHT ILLUMINATED 4 MINUTES AFTER TAKEOFF. EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. REMO VED AND REPLACED RIGHT WHEEL WELL FIRE SENSING ELEMENT. (M) 2 L 7 3 4F A3WE 2001071000009 20010710 00009 NM 2001 7 10 AALA20011193 1 20010611 A 3350 4082135 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 752AN 30260 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 62C INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBL Y. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001071000010 20010710 00010 WP 2001 7 10 AALA20011211 1 20010528 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 TUL - FOUND CORROSION RIGHT CUSP AROUND FASTENERS, LIGHTENING HOLE STATION 541-560. INSTALLED NEW RIGHT CUSP SHEET FROM STATION 503-598 PER SRM 5301. (M) 2 L 7 2 4F A6WE 2001071000011 20010710 00011 WP 2001 7 10 AALA20011212 1 20010529 A 5320 WEB DOUG DC9 DC982 3022082 WP CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 TUL - FOUND BOTTOM SIDE OF LEFT CUSP CORRODED. CUT OUT CORRODED AREA AND INSTALLED DOUBLER PER SRM 53-01 FIG 4, SHT 3. (M) 2 L 7 2 4F A6WE 2001071000012 20010710 00012 WP 2001 7 10 AALA20011214 1 20010529 A 5320 BEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 TUL - FOUND AFT CX DOOR BEAM CORRODED 4 INCHES BY 52 INCHES FROM STATION 1160-1212. BLENDED OUT CORROSION FROM 1160-121 2 PER AARD 53-10-003, TREATED PRIMED AND PAINTED. INSTALLED DOUBLER FROM 1167-1182 PER AARD 53-10-00-3. (M) 2 L 7 2 4F A6WE 2001071000013 20010710 00013 WP 2001 7 10 AALA20011215 1 20010528 A 5320 BRACKET DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 TUL - FOUND G1 GALLEY TIE DOWN CORRODED INSIDE HOLE. INSTALLED NEW SERVICEABLE TIE DOWN BRACKET PER SRM 51-10-3. (M) 2 L 7 2 4F A6WE 2001071000014 20010710 00014 WP 2001 7 10 AALA20011216 1 20010528 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 TUL - FOUND STATION 798-801 CUSP CRACKED FOR 3 INCHES RIGHT SIDE. INSTALLED DOUBLER PER AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 2001071000015 20010710 00015 WP 2001 7 10 AALA20011217 1 20010530 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 TUL - FOUND DENT IN FUSELAGE AFT OF FORWARD LEFT LAVATORY SERVICE PANEL. INSTALLED DOUBLER PER SRM 53-04 FIG 13B. (M) 2 L 7 2 4F A6WE 2001071000016 20010710 00016 WP 2001 7 10 AALA20011218 1 20010530 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 TUL - FOUND CUSP CRACKED AT 1300 BETWEEN SEAT TRACKS NR 1 AND NR 2. CUSP CRACKED AT 1250 BETWEEN SEAT TRACKS NR 1 AND N R 2. CUSP CORRODED AROUND LIGHTENING HOLE AT 1280. INSTALLED NEW CUSP SHEET FROM 1250-1308 LEFT PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2001071000017 20010710 00017 WP 2001 7 10 AALA20011220 1 20010531 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 TUL - FOUND LEFT CUSP CORRODED STATION 992-999. INSTALLED CUSP DOUBLER PER AARD 53-00-00-2. (M) 2 L 7 2 4F A6WE 2001071000018 20010710 00018 WP 2001 7 10 AALA20011221 1 20010530 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 TUL - FOUND CORROSION ON CUSP STATION 665-693 AND CORROSION AND CRACK ON CUSP STATION 712. INSTALLED NEW CUSP SHEET STA TION 598-712 SRM 51-01. (M) 2 L 7 2 4F A6WE 2001071000019 20010710 00019 WP 2001 7 10 AALA20011222 1 20010531 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE SCRATCHED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 TUL - FOUND SCRATCH AT STATION 1309 BETWEEN L18R-19R. INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M) 2 L 7 2 4F A6WE 2001071000020 20010710 00020 WP 2001 7 10 AALA20011224 1 20010602 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 TUL - FOUND FS 1485 CANT FRAME WEB CRACKED AT LEFT UPPER FASTENER JUST AFT OF LOWER VENT BOX. STOP DRILLED CRACK. INST ALLED DOUBLER PER AARD 53-10-00-32. (M) 2 L 7 2 4F A6WE 2001071000021 20010710 00021 WP 2001 7 10 AALA20011225 1 20010603 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 TUL - FOUND CANT FRAME 1485 IS CRACKED ON RIGHT SIDE OF STAIR CUTOUT WHERE ACTUATOR CASTING MOUNTS. CUTOUT DAMAGED SECT ION OF FRAME AND INSTALLED SPLICED REPAIR AS PER AARD/DH 53-10-00-33 PAGE 1. (M) 2 L 7 2 4F A6WE 2001071000022 20010710 00022 WP 2001 7 10 AALA20011227 1 20010601 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 TUL - FOUND SMELL DENT ABOUT 4 FEET FORWARD OF LEFT GROUND FLOOD LIGHT ON LEFT OF FUSELAGE. INSTALLED PERMANENT REPAIR PER SRM 53-04, FIG 12B, SHEET 5. (M) 2 L 7 2 4F A6WE 2001071000023 20010710 00023 WP 2001 7 10 AALA20011228 1 20010604 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 TUL - FOUND CORROSION ON CUSP STATION 200-281 RBL 56. CUT OUT CORROSION, INSTALLED DOUBLER PER AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 2001071000024 20010710 00024 WP 2001 7 10 AALA20011229 1 20010604 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 TUL - FOUND CLASS 2 DOUBLER INSTALLED AT 446, L24L. INSTALLED CLASS 1 PERMANENT REPAIR PER SRM 53-04 FIG 12B SHEETS. ( M) 2 L 7 2 4F A6WE 2001071000025 20010710 00025 WP 2001 7 10 AALA20011234 1 20010604 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 TUL - FOUND CORROSION 3 INCHES BY 3 INCHES, FS 200-218, FORWARD SERVICE DOOR. INSTALLED DOUBLER PER AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 2001071000026 20010710 00026 WP 2001 7 10 AALA20011235 1 20010601 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 566AA 49348 TUL - FOUND CORROSION ON AFT CARGO RIGHT TIE DOWN STRAP AROUND FASTENER HOLES FROM STATION 1211 TO STATION 1255 IN UPPER AND LOWER SURFACES. INSTALLED NEW RIGHT TIE DOWN STRAP PER SRM 53-20-00-3. (M) 2 L 7 2 4F RT A6WE 2001071000027 20010710 00027 WP 2001 7 10 AALA20011236 1 20010529 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 566AA 49348 TUL - FOUND LEFT CUSP CRACKED AT LIGHTENING HOLE BETWEEN STATION 218 AND STATION 229. INSTALLED DOUBLER PER SRM 53-01 P AGE 18 FIG 4. (M) 2 L 7 2 4F RT A6WE 2001071000028 20010710 00028 EA 2001 7 10 ASOA01077 1 20010616 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 835AS 7258 DURING GROUND INSPECTION IN ATL, MAINTENANCE DISCOVERED LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LEFT OVERWING EMERGENCY LIGHT BULB. OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001071000029 20010710 00029 EA 2001 7 10 ASOA01078 1 20010616 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 EA NLG MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 856AS 7404 FLT 4477 - ON TAKEOFF FROM HPN TO ATL, WHEN GEAR HANDLE WAS SELECTED UP THE NOSE GEAR DID NOT RETRACT. GEAR POSITION IN DICATOR SHOWED YELLOW GEAR INTRANSIT AND RED GEAR DISAGREED WITH CHIME. COMPLIED WITH QRH. CAPTAIN DECLARED AND EMERGE NCY FOR AN UNSAFE LANDING GEAR INDICATION. WHEN GEAR WAS SELECTED DOWN, ALL THREE POSITION INDICATORS SHOWED DOWN AND L OCKED. AIRCRAFT DIVERTED AND LANDED SAFELY AT JFK. GEAR PINS WERE INSTALLED AND SAFETIED. MAINTENANCE REMOVED AND REP LACED THE NOSE LANDING GEAR PRIORITY VALVE. BLEEDS LEAK AND OPERATIONAL CHECKS GOOD. GEAR PINS WERE REMOVED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001071000030 20010710 00030 EU 2001 7 10 ASOA01079 1 20010617 A 3350 3011210 LIGHT AEROSP ATR72 ATR72 EU CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 643AS 413 DURING HANGAR MAINTENANCE IN MCN, PASSENGER DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENC Y LIGHTING ASSY. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2001071000031 20010710 00031 SO 2001 7 10 ASOA01080 1 20010616 A 3350 CIRCUIT BREAKER EMB 120 EMB120 3260201 SO COCKPIT TRIPPED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 229AS 120042 FLT 4204 - DURING GROUND INSPECTION IN ATL, EMERGENCY LIGHT CIRCUIT BREAKER POPPED. CREW RESET CIRCUIT BREAKER PER MAIN TENANCE CONTROL. MAINTENANCE INSPECTED AND FOUND NO DEFECTS AT THAT TIME. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001071000032 20010710 00032 EU 2001 7 10 USAAF01035 1 20010625 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU PAX CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 895US 11380 IND - THE AFT CABIN CEILING EMERGENCY LIGHTS, LAVATORY EMERGENCY LIGHTS, AND THE LAVATORY AREA EMERGENCY LIGHTS WERE INO PERATIVE. MAINTENANCE REPLACED THE BATTERY PACK IN THE AFT CABIN CEILING UNIT. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT 2001071000033 20010710 00033 EU 2001 7 10 SIMA20011662 1 20010615 A 6100 10223NR00 GAUGE SAAB SF340 340B 7860101 EU COCKPIT INOPERATIVE A SIMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 21 356SB 340B356 ROC - FLT 4877 - CREW ABORTED TAKEOFF DUE TO THE RIGHT PROPELLER RPM INDICATOR GOING TO ZERO. MAINTENANCE REMOVED AND R EPLACED THE INDICATOR IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001071000034 20010710 00034 EU 2001 7 10 SIMA200115601 1 20010605 A 2700 7255163003 PIN SAAB SF340 340B 7860101 EU ELEVATOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 335AE 340B335 SBP - RIGHT ELEVATOR OUTBOARD ATTACH SPIGOT CORRODED. REMOVED AND REPLACED ATTACH SPIGOT IAW SAAB AMM 55-10-20. (M) 2 L 7 2 4T RT A52EU 2001071000035 20010710 00035 EU 2001 7 10 SIMA200115602 1 20010605 A 5300 7253799381 TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 335AE 340B335 SBP - FOUND BL 18.3 LEFT SEAT TRACK HAS SOME CORROSION AT THE FORWARD END SEAT 3A AISLE, FLOOR FLANGE. COMPLETED SPLICE INSTALLATION OF SEAT TRACK IAW SAAB SRM 53-70-60. (M) 2 L 7 2 4T RT A52EU 2001071000036 20010710 00036 EU 2001 7 10 SIMA200115604 1 20010605 A 5300 7253720319 INTERCOSTAL SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 335AE 340B335 SBP - FOUND INTERCOSTAL BETWEEN FS 272 AND 288 RIGHT IS CORRODED. REMOVED AND REPLACED INTERCOSTAL IAW SAAB SRM 51-40-4 0 AND 51-40-21. (M) 2 L 7 2 4T RT A52EU 2001071000037 20010710 00037 EU 2001 7 10 SIMA200115605 1 20010605 A 5300 7253722001 ANGLE SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 335AE 340B335 SBP - FOUND FUSELAGE FRAME AT FS 258 IS CORRODED ON THE PREVIOUS REPAIR FILLER. REMOVED AND REPLACED ANGLE IAW SAAB SRM 51-40-40 AND 51-40-21. (M) 2 L 7 2 4T RT A52EU 2001071000038 20010710 00038 EU 2001 7 10 SIMA200115606 1 20010605 A 5310 7253721447 ANGLE SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 335AE 340B335 REINFORCEMENT ANGLE AND INTERCOSTAL BETWEEN FS 236.5 AND 258 HAS SURFACE CORROSION. REMOVED AND REPLACED ANGLE IAW SAAB SRM 51-40-40 AND 51-40-21. (M) 2 L 7 2 4T RT A52EU 2001071000039 20010710 00039 EU 2001 7 10 SIMA200115610 1 20010605 A 3200 89106RC4SNB CONNECTOR SAAB SF340 340B 7860101 EU RT MLG BROKEN A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 335AE 340B335 SBP - RIGHT MAIN LANDING GEAR SEPARATION BOLT WIRE HARNESS HAS A BROKEN WIRE. REPAIRED WIRE HARNESS IAW SAAB WMM 20-00- 00. (M) 2 L 7 2 4T RT A52EU 2001071000040 20010710 00040 EU 2001 7 10 SIMA200116206 1 20010611 A 3200 3810010106 COLLAR SAAB SF340 340B 7860101 EU NOSE L/G WORN A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 243AE 340B243 JFK - FLT 5053 - NOSE WHEEL SHIMMY ABOVE 80 KTS, ABORTED TAKEOFF. REMOVED AND REPLACED NOSE LANDING GEAR COLLAR AND LIN KAGE IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001071000041 20010710 00041 NM 2001 7 10 BJNA0101603 1 20010618 A 2900 65445101803 HYDRAULIC LINE BOEING 737 737214 138446R NM A BJNA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS F G J FLT CONT AFFECTED MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 WP 11 457TM 20156 TOTAL HYDRAULIC FAILURE, FIRST NR 1 'A' SYSTEM PRESSURE LIGHT CAME ON, 'A' SYSTEM QUANTITY WENT TO ZERO. APPROXIMATELY 2 MINUTES LATER 'B' SYSTEM LOW QUANTITY LIGHT CAME ON. DIVERTED INTO SALT LAKE CITY, UT. INSPECTION FOUND BROKEN 'A' S YSTEM PRESSURE LINE AT PRESSURE MODULE. INSTALLED TEMPORARY FLEX LINE, OPS CHECK NORMAL, LEAK CHECK NORMAL IAW BMM 20-1 0-52, TO BE REINSPECTED AT PHASE CHECK. REVEALED 'B' SYSTEM BLEEDS TO 'A' SYSTEM. A/C RELEASED FOR FERRY FLIGHT, A/C I S SAFE FOR INTENDED FLT SLC TO EKO OPENED DMI TLD NR 0603, FOR TEMP FLEX LINE. UPON INVESTIGATION OF PROBLEM FOUND RUDD ER PCU RETURN LINES SWAPPED IN TAIL SECTION, CORRECTED PROBLEM IAW 27-21-91. FOUND ELEVATOR FEEL ACTUATOR A/B RETURN LI 2 L 7 2 4F A16WE 2001071000042 20010710 00042 NM 2001 7 10 BJNA010601 1 20010615 A 3350 P4010020 BATTERY PACK BOEING 737 737214 138446R NM CABIN DISCHARGED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 457TM 20156 RIGHT FORWARD ACCESS DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK PER BMM 33-51-71, OPS CHECK NO RMAL. (M) 2 L 7 2 4F A16WE 2001071000043 20010710 00043 NM 2001 7 10 BJNA010602 1 20010615 A 3350 P4010020 BATTERY PACK BOEING 737 737214 138446R NM A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 457TM 20156 FOUND LEFT FORWARD ACCESS DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK PER BMM 33-51-71, OPS CHE CK NORMAL. (M) 2 L 7 2 4F A16WE 2001071000044 20010710 00044 WP 2001 7 10 AALA016056 1 20010601 A 3350 6011779 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 822RA 49932 CCI-LAX - EMERGENCY LIGHT IN TAIL CONE SECTION ON LEFT SIDE IS INOPERATIVE. REPLACED POWER SUPPLY AND LIGHTS. SECURED POWER SUPPLY, OPS CHECK OK. (M) 2 L 7 2 4F A6WE 2001071000045 20010710 00045 WP 2001 7 10 AALA016057 1 20010606 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 754RA 49641 CCI-LAX - FOUND ROW 21, 22, 23, 24 EMERGENCY AISLE LIGHT INOPERATIVE. REPLACED LEFT BATERY PACK AT 19A, OPS NORMAL. (M ) 2 L 7 2 4F RT A6WE 2001071000046 20010710 00046 WP 2001 7 10 AALA016053 1 20010601 A 2600 5938323508 FIRE DETECTOR DOUG DC9 DC987 3022087 WP NR 1 ENGINE INOPERATIVE A AALA E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 SW 21 755RA 49727 LEFT ENGINE FIRE DETECTOR LOOP B ILLUMINATED DURING FLIGHT. SWITCHED TO LOOP A AND ACCOMPLISHED A GOOD TEST. LEFT SWIT CH IN LOOP A AS PER PROCEDURE. PULLING INTO GATE AT SJC LEFT ENGINE FIRE LIGHT AND BELL ILLUMINATED. SHUT DOWN ENGINE, PULLED FIRE HANDLE, FIRED BOTH BOTTLES. LIGHT REMAINED ILLUMINATED. GROUND CREW REPORTED A SMALL AMOUNT OF SMOKE COMI NG FROM TOP OF ENGINE AFTER FIRING BOTTLES. UPON INVESTIGATION, MAINTENANCE DETERMINED THERE WAS NO ACTUAL FIRE. MAINT ENANCE FOUND UPPER FIRE DETECTOR LOOP A AND B BAD. REPLACED UPPER FIRE DETECTOR LOOP A AND B. PERFORMED FIRE DETECTOR TEST AS REQUIRED. REMOVED AND REPLACED NR 1 AND NR 2 FIRE EXTINGUISHER, INSTALLED SQUIBB, FIRE SYSTEM TEST OK PER MM. 2 L 7 2 4F RT A6WE 2001071000047 20010710 00047 NM 2001 7 10 AALA20011290 1 20010624 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 378AN 25447 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 23H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECT OR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001071000048 20010710 00048 NM 2001 7 10 EIA2001199 1 20010320 A 5310 FORGING BOEING 747 747128 1384894 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - FOUND LEFT STATION 1210 CORROSION ON AND AROUND WINDOW FORGING. REPAIRED PER ECRA 3203-53-047-2. (M) 2 L 7 4 4F A20WE 2001071000049 20010710 00049 NM 2001 7 10 EIA2001200 1 20010324 A 5730 SKIN BOEING 747 747128 1384894 NM RT WING DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - FOUND RIGHT WING L/W BULLNOSE DAMAGED AND LOOSE FASTENERS AT AFT WEB ANGLE. REMOVED DAMAGED BULLNOSE AND AFT ANGLE WEB LOOSE FASTENERS. FABRICATED NEW SPLICE ANGLE AND REPAIR DOUBLERS. INSTALLED NEW BULLNOSE, SPLICE ANGLES, AND REPAIR DOUBLERS PER SRM 51-30-02, 57-20-02, 51-40-02, 51-10-02 AND SOPM 20-41-02. (M) 2 L 7 4 4F A20WE 2001071000050 20010710 00050 NM 2001 7 10 EIA2001202 1 20010327 A 5310 FORGING BOEING 747 747128 1384894 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - FOUND RIGHT STATION 1020-1040 CORROSION ON WINDOW FORGING AND UNDER SEALANT. REPAIRED PER ECRA 3203-53-047-2. (M) 2 L 7 4 4F A20WE 2001071000051 20010710 00051 NM 2001 7 10 EIA2001203 1 20010327 A 5310 FORGING BOEING 747 747128 1384894 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - FOUND RIGHT STATION 620-640 STRINGER 8R, CORROSION ON AND AROUND 2R WINDOW FORGING. REPAIRED PER ECRA 3203-53 -047-2. (M) 2 L 7 4 4F A20WE 2001071000052 20010710 00052 NM 2001 7 10 EIA2001204 1 20010327 A 5310 FORGING BOEING 747 747128 1384894 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - FOUND LEFT STATION 990 CORROSION ON AND AROUND WINDOW FORGING. REPAIRED PER ECRA 3203-53-047-2. (M) 2 L 7 4 4F A20WE 2001071000053 20010710 00053 NM 2001 7 10 EIA2001205 1 20010327 A 5310 FORGING BOEING 747 747128 1384894 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - FOUND LEFT STATION 1372-1394 STRINGER 10L TO STRINGER 22L, CORROSION AT WINDOW FORGING LOWER AFT CORNER. REPA IRED PER ECRA 3203-53-047-2. (M) 2 L 7 4 4F A20WE 2001071000054 20010710 00054 NM 2001 7 10 EIA2001206 1 20010327 A 5310 FORGING BOEING 747 747128 1384894 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - FOUND RIGHT STATION 1460-1480 STRINGER 20R TO STRINGER 22R CORROSION UNDER WINDOW FORGING. REPAIRED PER ECRA 3203-053-047-2. (M) 2 L 7 4 4F A20WE 2001071000055 20010710 00055 NM 2001 7 10 EIA2001221 1 20010331 A 5310 FORGING BOEING 747 747128 1384894 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 FOUND LEFT STATION 1040-1060 STRINGER 20L TO STRINGER 22L CORROSION UNDER WINDOW FORGING. REPAIRED PER ECRA 3203-53-047 -2. (M) 2 L 7 4 4F A20WE 2001071000056 20010710 00056 NM 2001 7 10 EIA2001222 1 20010331 A 5310 FORGING BOEING 747 747128 1384894 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - FOUND RIGHT STATION 1160-1180, STRINGER 20R TO STRINGER 22R CORROSION UNDER WINDOW FORGING. REPAIRED PER ECRA 3203-53-047-2. (M) 2 L 7 4 4F A20WE 2001071000057 20010710 00057 NM 2001 7 10 GAIA01243OP 1 20010106 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM L1 DOOR INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6808 19483 FLT 2016 - MHR-DEN - DURING ROUTINE PERIODIC SERVICE CHECK, MAINTENANCE REMOVED AND REPLACED THE LEFT FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT ASSEMBLY. OPS CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001071000058 20010710 00058 EU 2001 7 10 20010529CW002 1 20010427 A 4950 4AS6900620501 DUCT ISRAEL GALAXY GALAXY 4500307 EU APU MISALIGNED E VO2R K NONE O OTHER IN INSP/MAINT 1 GL 19 414KD 022 THE FLEX COUPLER COULD NOT BE INSTALLED DUE TO THE MISALIGNMENT OF THE DUCT FROM THE GENERATOR AND THE EXHAUST DUCT ON T HE RIGHT SIDE OF THE FUSELAGE. 2 L 7 2 4F RT A53NM 2001071000061 20010710 00061 EU 2001 7 10 20010530CW005 1 20010427 A 4950 AS6900620505 DUCT ISRAEL GALAXY GALAXY 4500307 EU APU MISALIGNED E VO2R K NONE O OTHER IN INSP/MAINT 1 GL 19 414DH 29 023 THE FLEX COUPLER COULD NOT BE INSTALLED DUE TO THE MISALIGNMENT OF THE DUCT FROM THE APU GENERATOR AND THE EXHAUST DUCT ON THE RIGHT SIDE OF THE FUSELAGE. 2 L 7 2 4F RT A53NM 2001071000062 20010710 00062 NM 2001 7 10 ASAA0110207 1 20010410 A 3350 88210044 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT AT LEFT OVERWING EXIT DOOR INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY AND SIGN OPERATED NORMAL. (M) 2 L 7 2 4F RT A16WE 2001071000063 20010710 00063 NM 2001 7 10 ASAA0140055 1 20010411 A 3397 8100022608 WIRE BOEING 737 737490 1384715 NM CABIN DISCONNECTED A K NONE L NO TEST IN INSP/MAINT 1 NM 01 767AS 27081 SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING AT ROW 15-21 INOPERATIVE, WIRE DISCONNECTED. RECONNECTED WIRE. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2001071000064 20010710 00064 WP 2001 7 10 ASAA0180127 1 20010404 A 3350 0105606003 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 974AS 53450 SEA - DURING PREFLIGHT, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN FIRST CLASS. REPAIRED CONNECTION. LIGHTS THE N OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001071000065 20010710 00065 WP 2001 7 10 ASAA0180132 1 20010409 A 3350 60030451 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 954AS 49387 SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN 1ST CLASS CABIN. REMOVED AND REPLACED ASSOCI ATED POWER SUPPLY. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001071000066 20010710 00066 WP 2001 7 10 ASAA0180134 1 20010409 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 954AS 49387 OAK - DURING LINE CHECK, OVERHEAD EMERGENCY LIGHTS FROM FORWARD ENTRY TO ROW 1 WERE INOPERATIVE. REMOVED AND REPLACED A SSOCIATED BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001071000067 20010710 00067 WP 2001 7 10 ASAA0180135 1 20010411 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 LAX - DURING PREFLIGHT CHECK, FOUND TWO EMERGENCY FLOOR TRACK LIGHTS MODULES INOPERATIVE IN 1ST CLASS CABIN. REMOVED AN D REPLACED TWO FLOOR TRACK LIGHT MODULES. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001071000068 20010710 00068 NM 2001 7 10 DHL2001702012 1 20010518 A 2751 SWITCH BOEING 727 72730C 1384009 NM T/E FLAPS DIRTY A DHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 702DH 19793 UPON CLEARANCE FOR TAKEOFF, ADVANCED THRUST LEVER T/O CONFIG WARNING HORN SOUNDED (REF - SPEEDBRAKE WAS STOWED, TRIM SET FLAPS WERE 15 - 15 GREEN). CLEANED FLAP WARNING SWITCH CYCLED FLAPS TO 15 DEG. OPS CK GOOD. NO HORN AND RESET FLAPS TO 0 DEG. 2 L 7 3 4F A3WE 2001071000069 20010710 00069 2001 7 10 DHL2001727018 4 20010523 A 2211 COMPUTER BOEING 727 727228 NM AUTOPILOT MALFUNCTIONED A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 727DH 20204 AUTOPILOT IN A-MODE HAD UNCONTROLLED ROLLS IN BOTH DIRECTION, B-MODE NORMAL. DEFERRED IAW MEL REF 22-1 CAT B CTL 5716 A SSIGNED. PLACARD INSTALLED. REMOVED AND REPLACED ROLL CHANNEL, OPS CK NORMAL IAW M/M 22-11-0, CLEARS DMI 5716. PLACAR D REMOVED. 2 L 7 3 4F A3WE 2001071000070 20010710 00070 2001 7 10 DHL2001743007 4 20010518 A 2210 25858001 COUPLER BOEING 727 727225 1384077 NM YAW DAMPER DEFECTIVE A DHLA K NONE F FLT CONT AFFECTED DE DESCENT 1 SO 01 743DH 22438 DURING DESCENT THRU 14000 FT AT 280KTS SPEEDBRAKE DEPLOYED AIRCRAFT BEGAN TO YAW AFTER TURNING LOWER YAW DAMPER OFF. DU TCH ROLL STOPPED. REPLACED LOWER RUDDER YAW DAMPNER COUPLER IAW B727 M/M 22-11-131. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2001071000071 20010710 00071 2001 7 10 DHL2001807019 4 20010524 A 2210 COMPUTER DOUG DC8 DC873 302199C WP AUTOPILOT SYS MALFUNCTIONED A DHLA K NONE O OTHER CL CLIMB 1 SO 01 807DH 45990 AUTOPILOT WILL NOT LEVEL OFF FROM CLIMB OR DESCENTS EVEN WITH MIN RATE ON INITIATION LEVEL OFF. CLEANED AND RE-SEATED A /P PITCH COMPUTER IN RACK. PERFORMED TEST OF A/P PITCH CHANNEL PER M/M 22-13-0. ALL TESTS GOOD. 2 L 7 4 4F RT 4A25 2001071000072 20010710 00072 EU 2001 7 10 KBMA88751 1 20010507 A 7920 J26109 HOSE SNIAS 350 AS350BA 8680817 EU OIL SYSTEM LEAKING E KBMA O OTHER K FLUID LOSS NR NOT REPORTED 1 WP 19 350SH 2957 MAIN OIL HOSE AT THERMAL BYPASS VALVE, LEAKING. ALT NR 704A34-410021. REPLACED WITH REMANUFACTURED HOSE, AS REQUIRED. 1 G 7 1 3U NC H9EU 2001071000073 20010710 00073 NM 2001 7 10 USAA010505 1 20010507 A 5530 FITTING BOEING 737 7372B7 1384560 NM VERTICAL STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 270AU 22882 SJO - FOUND HINGE RIB FITTING CRACKED .75 INCH, VERT FS 23.27. DAMAGE REMOVED. FABRICATED AND INSTALLED FILLER AND REP AIR ANGLE PER EA 70830. (M) 2 L 7 2 4F A16WE 2001071000074 20010710 00074 NM 2001 7 10 USAA010506 1 20010507 A 5320 CHANNEL BOEING 737 7372B7 1384560 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 270AU 49760 22882 SJO - FOUND 3 INCH SQUARE CORROSION, BS 986 TO 1006 BETWEEN STRINGER 26L AND 27L. FABIRCATED AND INSTALLED REPAIR CHANN EL PER SRM 51-10-3. (M) 2 L 7 2 4F A16WE 2001071000075 20010710 00075 NM 2001 7 10 USAA010518 1 20010508 A 5320 WEB BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 51503 22754 CLT - FOUND FLOOR STRUCTURE WEB CRACKED 1 INCH, BS 178, WL 207 AT LBL 24. REMOVED AND REPLACED WEB PER EO 5300V157. (M ) 2 L 7 2 4F A16WE 2001071000076 20010710 00076 NM 2001 7 10 USAASB01124 1 20010501 A 3260 189929 UPLOCK SENSOR BOEING 737 7373B7 1384580 NM LT MLG FAULTY A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 385US 22958 IAH - FLT 1620 - AFTER TAKEOFF FROM IAH, WHEN THE LANDING GEAR WAS RAISED, CREW RECEIVED TWO GREEN LIGHTS AND A LEFT MLG RED LIGHT. AN UNUSUAL RUMBLE WAS ALSO NOTICED WHILE GEAR WAS BEING RETRACTED. CREW RECYCLED GEAR AND GOT THREE GREEN L IGHTS WHEN GEAR WAS DOWN BUT AGAIN RECEIVED TWO GREEN LIGHTS AND A LEFT MAIN LANDING GEAR RED LIGHT WHEN THE GEAR WAS RA ISED. CREW LOWERED GEAR AGAIN AND GOT THREE GREEN LIGHTS AND DECIDED TO RETURN TO FIELD AT IAH. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND RETURNED TO THE GATE. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND A BAD GROUND ON THE LEFT MLG U PLOCK SENSOR. REMOVED AND REPLACED UPLOCK SENSOR AND ACCOMPLISHED GEAR SWING. SYSTEM CHECKS NORMAL PER MM 32-61-21. ( 2 L 7 2 4F RT A16WE 2001071000077 20010710 00077 EU 2001 7 10 2001F00101 1 20010605 A 5347 7253799379 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 335AE 340B335 SBP - FOUND BL 18.3 LEFT SEAT TRACK HAS SOME CORROSION AT THE FORWARD END SEAT 3A AISLE, FLOOR FLANGE. COMPLETED SPLICE INSTALLATION OF SEAT TRACK IAW SAAB SRM 53-70-60. REF SIMA200115602. (M) 2 L 7 2 4T RT A52EU 2001071000078 20010710 00078 EU 2001 7 10 2001F00102 1 20010605 A 3297 D43636 WIRE SAAB SF340 340B 7860101 EU RT MLG BROKEN A K NONE O OTHER IN INSP/MAINT 1 SW 21 335AE 340B335 SBP - RIGHT MAIN LANDING GEAR SEPARATION BOLT WIRE HARNESS HAS A BROKEN WIRE. REPAIRED WIRE HARNESS IAW SAAB WMM 20-00- 00. REF SIMA200115610. (M) 2 L 7 2 4T RT A52EU 2001071000079 20010710 00079 NM 2001 7 10 2001F00100 1 20010608 A 2781 1062221 SWITCH BOEING 737 737* NM L/E SLAT INOPERATIVE A MEDF B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 CE 07 EIBXK 25736 DURING FLIGHT, LOUD BANG NOISE HEARD, FOLLOWED BY A LEADING EDGE FLAP TRANSIT AND OVERHEAD LEADING EDGE DEVICE NR 3 TRAN SIT LIGHT ILLUMINATED. EMERGENCY DECLARED. LANDED WITH NO INCIDENT AND NORMAL GREEN LIGHT INDICATIONS. REMOVED AND RE PLACED NR 3 LEADING EDGE SLAT, UP SWITCH. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2001071000080 20010710 00080 WP 2001 7 10 AALA016054 1 20010605 A 3350 3102806 FUSE DOUG DC9 DC987 3022087 WP CABIN BLOWN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 754RA 49641 CCI-SNA - EMERGENCY LIGHTING INOPERATIVE, RIGHT OVERWING SEAT LIGHTING. REPLACED FUSE IN BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 2001071000081 20010710 00081 WP 2001 7 10 AALA016055 1 20010606 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN NOT SEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 822RA 49932 CCI-SNA - FOUND 15 DEF EMERGENCY LIGHTS INOPERATIVE. RESEATED CONNECTOR. OPS CHECK OK. (M) 2 L 7 2 4F A6WE 2001071000082 20010710 00082 WP 2001 7 10 AALA016058 1 20010614 A 3350 CLIP DOUG DC9 DC982 3022082 WP CABIN DETACHED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 823RA 49889 CCI-SJC - FOUND SEAT 26D EMERGENCY LIGHT WIRE HARNESS CANNON PLUG CLIP DETACHED. SECURED SEAT 26D EMERGENCY LIGHT HARNE SS CLIP. OPS CHECKS GOOD. (M) 2 L 7 2 4F A6WE 2001071000083 20010710 00083 WP 2001 7 10 AALA20011267 1 20010612 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 TUL - FOUND FLOOR WEB CORRODED 20 INCHES BY 6 INCHES STATION 150-170 RBL 43-49. INSTALLED DOUBLER PER SRM 53-01 FIG 4 A ND AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 2001071000084 20010710 00084 NM 2001 7 10 EIA20011217 1 20010330 A 7120 FASTENER BOEING 747 747128 1384894 NM NR 2 PYLON FAILED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 MZJ-EAC - NR 2 PYLON FORWARD ENGINE MOUNT HANGAR FITTING FASTENERS FAILED TORQUE CHECK, PRIMARY FAST INBOARD NR 1 AND NR 4, OUTBOARD NR 4, SECONDARY FAST INBOARD NR 2, AND OUTBOARD NR 3. COMPLIED WITH SB 54-747-1611-00 REV E AND ECRA 3203- 54-049-2. (M) 2 L 7 4 4F A20WE 2001071000085 20010710 00085 WP 2001 7 10 GTIA010517 1 20010613 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A K NONE L NO TEST NR NOT REPORTED 1 GL 23 804NK 49104 DTW - FOUND EMERGENCY FLOOR TRACK LIGHTING LAST TWO INOPERATIVE. REPAIRED WIRES ON FLOOR TRACK, AFT LIGHTS. OPS CHECKS NORMAL ON GROUND IAW MM 33-53-01. (M) 2 L 7 2 4F A6WE 2001071000086 20010710 00086 WP 2001 7 10 GTIA010518 1 20010612 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 DALLO 53012 FLL - FOUND LEFT SIDE AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED LIGHT ASSEMBLY. OPS CHECKED OK REF MM 33-53-0 0. (M) 2 L 7 2 4F RT A6WE 2001071000087 20010710 00087 WP 2001 7 10 GTIA010530 1 20010615 A 2432 Z634006106 CHARGER DOUG DC9 DC983 3022083 WP E/E BAY MALFUNCTIONED A GTIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 23 602CA 49415 LGA - FLT 628 - REACHING THE GATE-GND PRESSURE ADVISED OF SMOKE COMING FROM BATTERY VENT, NORMAL BATTERY INDICATIONS IN COCKPIT. REMOVED AND REPLACED BATTERY CHARGER IAW 24-30-02. (M) 2 L 7 2 4F RT A6WE 2001071000088 20010710 00088 WP 2001 7 10 ABXA010365 1 20010625 A 2700 49141731 PIN DOUG DC9 DC941 302207N WP HORZ. STAB. CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 958AX 47760 FORWARD HORIZONTAL STABILIZER PIN WAS CORRODED ON END AND TAB. REPLACED PIN IAW DC-9 MM 27-40-01. 2 L 7 2 4F A6WE 2001071000089 20010710 00089 WP 2001 7 10 ABXA010366 1 20010625 A 2700 49141731 PIN DOUG DC9 DC941 302207N WP HORZ. STAB. CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 958AX 47760 AFT HORIZONTAL STABILIZER PIN HAD CORROSION ON END AND TAB. REPLACED PINS IAW DC-9 MM 27-40-01. 2 L 7 2 4F A6WE 2001071000090 20010710 00090 WP 2001 7 10 ABXA010367 1 20010626 A 5400 995815410 DOUBLER DOUG DC9 DC941 302207N WP RIGHT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 958AX 47760 RIGHT PYLON INTERIOR UPPER ANGLE FORWARD OF AFT ENGINE MOUNT ABOVE ENGINE CANNON PLUGS CRACKED. INSTALLED DOUBLER IAW DC -9 REA D954-41543. 2 L 7 2 4F A6WE 2001071000091 20010710 00091 CE 2001 7 10 GUU2001F00014 1 20010428 A 7600 LINK BEECH 1900 1900C 1154161 CE LT ENGINE OUT OF RIG A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 19 139GA UC126 FLT 9122 - NAS/FLL - DURING FLIGHT AT 2000 FEET WITH LEFT ENGINE TORQUE SET TO 2000 FT/LBS AND PROPELLER SET TO 1500 RPM , PROPELLER SURGED TO 1750 RPM AND TOQUE FELL TO 1500 FT/LBS. RIGGED LOST MOTION LINK ON LEFT ENGINE. OPERATIONAL CHEC K NORMAL. (M) 2 L 7 2 4T RT A24CE 2001071000092 20010710 00092 NM 2001 7 10 P2EA01094 1 20010611 A 5312 BULKHEAD BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 127NJ 22886 DURING C-CHECK INSPECTION PER S/B 737-53A1173, PRESSURE BULKHEAD BS 178 WEB CRACKED AT WL 234, RBL 12 INCHES, PRESSURE B ULKHEAD BS 178 RT SIDE INTERCOSTAL CRACKED AT WL 195, PRESSURE BULKHEAD BS 178 LEFT SIDE INTERCOSTAL CRACKED AT WL 185. BS 178 FORWARD PRESSURE BULKHEAD WEB REPAIRED FROM WL 230 TO 238 BETWEEN RBL 7 INCHES AND RBL 16 INCHES DUE TO CRACK IA W SRM 53-10-11 FIG 1. BS 178 FORWARD PRESSURE BULKHEAD RIGHT SIDE INTERCOSTAL REPLACED AT WL 195 DUE TO CRACK IAW SB 737 -53A1173, REV 3 SECTION III FIG 47. BS 178 FORWARD PRESSURE BULKHEAD LEFT SIDE INTERCOSTAL REPLACED AT WL 195 DUE TO CR ACK IAW S/B 737-53A1173, REV 3 SECTION III FIG 47. (M) 2 L 7 2 4F A16WE 2001071000093 20010710 00093 NM 2001 7 10 P2EA01095 1 20010614 A 5754 SLAT BOEING 737 7372B7 1384560 NM RT WING DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 127NJ 22886 SJO - DURING C-CHECK, RIGHT WING NR 6 LEADING EDGE SLAT WITH DELAMINATION AT TRAILING EDGE AREA, FROM SS 352 TO SS 360 A ND FROM SS 417 TO SS 430. (M) 2 L 7 2 4F A16WE 2001071000094 20010710 00094 NM 2001 7 10 P2EA01096 1 20010614 A 5754 SLAT BOEING 737 7372B7 1384560 NM LT WING DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 127NJ 22886 SJO - DURING C-CHECK, FOUND LEFT WING NR 3 LEADING EDGE SLAT WITH DELAMINATION AT TRAILING EDGE AREA, FROM SS 0.00 TO SS 15.00. (M) 2 L 7 2 4F A16WE 2001071000095 20010710 00095 NM 2001 7 10 P2EA01097 1 20010614 A 5753 SKIN BOEING 737 7372B7 1384560 NM T/E FLAP DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 127NJ 22886 SJO - DURING C-CHECK, FOUND LEFT WING INBOARD AFT FLAP LOWER SKIN WITH DELAMINATION FROM WBL 71 TO WBL 95. (M) 2 L 7 2 4F A16WE 2001071000096 20010710 00096 NM 2001 7 10 P2EA01098 1 20010614 A 5751 SKIN BOEING 737 7372B7 1384560 NM AILERON DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 127NJ 22886 SJO - DURING C-CHECK, FOUND LEFT WING AILERON UPPER SKIN WITH DENTS AND LOWER SKIN WITH DELAMINATION AT WBL 480. (M) 2 L 7 2 4F A16WE 2001071000097 20010710 00097 NM 2001 7 10 P2EA01099 1 20010613 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 127NJ 22886 SJO - DURING C-CHECK, FOUND LOWER FUSELAGE PNEUMATIC GROUND CONNECTOR AREA, FROM BS 520 TO BS 540 BETWEEN STRINGER 28L T O 28R, CUT OUT SKIN WITH SHARP EDGES AND CRACK. (M) 2 L 7 2 4F A16WE 2001071000098 20010710 00098 NM 2001 7 10 P2EA01100 1 20010613 A 5313 STRINGER BOEING 737 7372B7 1384560 NM FUSELAGE CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 127NJ 22886 SJO - DURING C-CHECK, LOWER FUSELAGE AFT ACCESSORY COMPARTMENT BETWEEN BS 967 AND 984.5 STRINGER 25 LEFT CORRODED LEVEL 2. FUSELAGE STRINGER SECTION REPAIRED AT STRINGER 25 LEFT SIDE BETWEEN BS 967 AND 984.5 IAW SRM 53-10-3, FIG 1. (M) 2 L 7 2 4F A16WE 2001071000099 20010710 00099 NM 2001 7 10 P2EA01101 1 20010613 A 5313 STRINGER BOEING 737 7372B7 1384560 NM FUSELAGE CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 127NJ 22886 SJO - DURING C-CHECK, LOWER FUSELAGE, AFT ACCESSORY COMPT BETWEEN BS 967 AND 985.5 STRINGER 26RT CORRODED, LEVEL 2. FUS ELAGE STRINGER SECTION REPAIRED AT STRINGER 26 RT SIDE BETWEEN BS 967 AND 986.5 IAW SRM 53-10-3 FIG 1. (M) 2 L 7 2 4F A16WE 2001071000100 20010710 00100 NM 2001 7 10 P2EA01102 1 20010613 A 5313 STRINGER BOEING 737 7372B7 1384560 NM FUSELAGE CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 127NJ 22886 SJO - DURING C-CHECK, FOUND LOWER FUSELAGE, AFT ACCESSORY COMPARTMENT BETWEEN BS 986.5 AND 1016 STRINGER 27 LEFT CORRODE D, LEVEL 2. FUSELAGE STRINGER SECTION REPAIRED AT STRINGER 27 LEFT SIDE BETWEEN BS 986.5 AND 1016 IAW SRM 53-10-3, FIG 1. (M) 2 L 7 2 4F A16WE 2001071000101 20010710 00101 NM 2001 7 10 P2EA01103 1 20010613 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 127NJ 22886 DURING C-CHECK, FUSELAGE STATION 274, BETWEEN STRINGER 16 AND 17 RT SKIN WITH DENT. FUSELAGE SKIN REPAIRED FROM BS 269. 5 AND 271.5 BETWEEN STRINGER 16 AND 18 RIGHT DUE TO DENT IAW SRM 53-30-3, FIG 1. (M) 2 L 7 2 4F A16WE 2001071000102 20010710 00102 NM 2001 7 10 P2EA01104 1 20010617 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 127NJ 22886 SJO - DURING C-CHECK, FOUND FUSELAGE STATION 817, BETWEEN STRINGER 26 AND 27 RT SKIN WITH DENT OUT OF LIMITS. FUSELAGE SKIN REPAIR FROM BS 813 TO 824.5 BETWEEN STRINGER 26 AND 28RT DUE TO DENT IAW SRM 53-30-3, FIG 6. (M) 2 L 7 2 4F A16WE 2001011105840 20010111 05840 NM 2001 1 11 MWEA010025 1 20010103 A 3222 LANDING GEAR DOUG MD88 MD88 3023688 NM NOSE MALFUNCTIONED A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 805ME 48031 NOSE LANDING GEAR IN-TRANSIT LIGHT STAYED ON WITH GEAR HANDLE UP. -- MAINTENANCE VERIFIED INTEGRITY OF WIRING, PERFORM ED DETAIL INSPECTION OF NOSE GEAR, VERIFIED PROPER NOSE GEAR STRUT SERVICING, PERFORMED NUMEROUS GEAR SWINGS, CHECKED FO R PROPER ACTUATION OF GROUND SENSING SWITCHES. ALL CHECKS PERFORMED ARE ALL OK. NO FAULTS FOUND. LUBED NOSE LANDING GEAR ASSEMBLY. 2 L 7 2 4F RT A6WE 2001071000103 20010710 00103 NE 2001 7 10 REXA01009 2 20010612 A 7321 6071T20P10 ECU SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE FAULTY A REXA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 SO 25 370PX 340B300 ON SEVEN MILE FINAL INTO MEMPHIS, THE LEFT ENGINE WENT INTO AUTOCOURSEN. TORQUE INDICATION WENT TO ZERO, BUT ALL OTHER INDICATIONS WERE NORMAL. THE FLIGHT CREW FOLLOWED THE EMERGENCY CHECKLIST AND SHUTDOWN THE ENGINE. MAINTENANCE REPLACE D THE DIGITAL ELECTRONIC CONTROL UNIT. GROUND RUN OF ENGINE SHOWED NORMAL OPERATION AND THE AIRCRAFT WAS RELEASED FOR S ERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 2001071000104 20010710 00104 NM 2001 7 10 RJE2001F00000 1 20010522 A 3230 LANDING GEAR BOEING 737 7372K5 138448X NM LT & RT MALFUNCTIONED A RJEF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 231TA 22596 SAP - FLT 220 - AFTER TAKEOFF FROM SAP STATION, LEFT AND RIGHT MAIN LANDING GEARS DID NOT SECURE IN UPLOCK POSITION. TH E AIRCRAFT RETURNED TO SAP STATION FOR MAINTENANCE. A FERRY FLIGHT PERMIT HAS BEEN GRANTED BY THE FAA AND LOCAL CAA'S, AIRCRAFT WAS FLOWN FROM SAN PEDRO TO EL SALVADOR FOR PROPER REPAIR AND FURTHER CHECKS. (M) 2 L 7 2 4F RT A16WE 2001071000105 20010710 00105 NM 2001 7 10 AWXA0001944 1 20010709 A 5311 654583340 WEB BOEING 737 7373G7 1384595 NM STA 178 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 304AW 24011 D: Web Crack on Floor Level (WL 207) At STA .178 on R/H Side RBL 28C: Removed Cracked Web, Fabricated New Web P/N 65-458 33-40 Per REF DWG 65-45833, install Web Per 45-45833 2 L 7 2 4F RT A16WE 2001071000106 20010710 00106 NM 2001 7 10 AWXA0001946 1 20010709 A 5312 65163007 WEB BOEING 737 7373G7 1384595 NM STA 178 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 304AW 24011 D: Center Bulkhead Web Crack At Body STA .178 . WL 187. BLO.C: Remove Crack Per SRM 53-10-08 Fig 203. NDT Checked For Cr ack Containment. Frabricate Repair Parts and installed Per SRM 53-10-08 Fig 203 2 L 7 2 4F RT A16WE 2001071000107 20010710 00107 NM 2001 7 10 AWXA0001949 1 20010709 A 5313 654583392 STRINGER BOEING 737 7373G7 1384595 NM STA 178, WL 207, CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 304AW 24011 D: Stringer crack at STA 178. WL 207. RBL 28C: fabricated repair parts per SRM 51-70-12 Fig 1 detail 7. Installed repair parts per SRM 51-70-12 Fig 1 2 L 7 2 4F RT A16WE 2001071000108 20010710 00108 NM 2001 7 10 AWXA0001954 1 20010709 A 5315 141N51911 FLOOR SUPPORT BOEING 757 7572S7 1384962 NM STA 330-360 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 D: corrosion on top surface of floor structure, FS 350 BL 00C: Removed damaged section of floor support from STA 330 to STA 360 BL0 fabricated installed repair per SRM 51-70-11 fig 1 pg 1 2 L 7 2 4F RT A2NM 2001071000109 20010710 00109 NM 2001 7 10 AWXA0001957 1 20010709 A 5330 SKIN BOEING 737 737317 138447P NM BS 259.5 DENTED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 D: Upper fuselage skin at B/S 259.5 damaged by HailC: Removed damage, Fabricated repair parts and installed per AWA ER 0 3-5331-01187-JS2 2 L 7 2 4F RT A16WE 2001071000110 20010710 00110 NM 2001 7 10 AWXA0001958 1 20010709 A 5330 SKIN BOEING 737 737317 138447P NM A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 D: Upper fuselage skin at B/S 928.5 and STR 4R damaged by hail.C: Removed damge, fabricated and installed repair parts p er AWA ER 03-5331-01187-JS6 2 L 7 2 4F RT A16WE 2001071000111 20010710 00111 NM 2001 7 10 AWXA0001959 1 20010709 A 5330 SKIN BOEING 737 737317 138447P NM BS 996.0 DENTED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 D: Upper fuselage skin B/S 996.0 and STR 6R damaged by hailC: Removed damage and fabricated repair parts and installed p er AWA ER 03-5331-01187-JS7 2 L 7 2 4F RT A16WE 2001071000112 20010710 00112 NM 2001 7 10 AWXA0001960 1 20010709 A 5330 SKIN BOEING 737 737317 138447P NM BS 340-360 DENTED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 D: Hail damage on crown skin between STA 340 and 360 Between STR 2L and 3LD: Removed and replaced damage, fabricated rep air parts and installed per AWA ER 03-5331-01187-JS3 2 L 7 2 4F RT A16WE 2001071000113 20010710 00113 NM 2001 7 10 AWXA0001961 1 20010709 A 5330 SKIN BOEING 737 737317 138447P NM BS 695.5 STR 4L DENTED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 D: Upper fuselage skin at B/S 695.5 StR 4L damaged by hail.C: Removed damage, fabricated repair parts and installed per AWA Er 03-5331-01187-JS5 2 L 7 2 4F RT A16WE 2001071000114 20010710 00114 NM 2001 7 10 AWXA0001962 1 20010709 A 5330 SKIN BOEING 737 737317 138447P NM BS 500B DENTED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 D: Upper fuselage skin at B/S 500B and STR 3R damged by hail.C: removed damage, fabricated repair parts and installed pe r AWA ER 03-5331-01187-JS4 2 L 7 2 4F RT A16WE 2001071000115 20010710 00115 NM 2001 7 10 AWXA0001963 1 20010709 A 5311 WEB BOEING 737 737317 138447P NM FWD CARGO DOOR CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 D: Fwd Cargo door lwr fwd crossbeam web cracked at fasteners 2 placesC: removed cargo door and replaced cracked Webs per SRM 51-40-02 Reinstalled cargo door per task card R 8M 52001 2 L 7 2 4F RT A16WE 2001071000116 20010710 00116 NM 2001 7 10 2001UALA01272 1 20010629 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 STRINGER 39R AT FS 1794 IS DENTED BEYOND LIMITS. REPLACED STRINGER SPLICE PER SRM 53-00-03 AND INSTALLED PER SRM 53-00- 03 ON NON-ROUTINE D5766V. MAJOR REPAIR 2 L 7 2 4F 4 F RT A1NM E3NE 2001071000117 20010710 00117 NM 2001 7 10 2001UALA01275 1 20010629 A 5311 FRAME BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 AFT PIT STA 1304, RBL 40, TOP OF FRAME IS CORRODED. REPAIRED FRAME PER BAC DWG 146T8533 AND INSTALLED PER SRM 51-40-2 O N NON-ROUTINE J7789I. MAJOR REPAIR 2 L 7 2 4F 4 F RT A1NM E3NE 2001071000118 20010710 00118 NM 2001 7 10 2001UALA01276 1 20010629 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 STA 698, STR 39R ON THE AFT SIDE IS CORRODED. REPLACED SHEAR TIE PER BAC DWG 143T1212 AND INSTALLED PER SRM 51-40-2 ON NON-ROUTINE G7966H. MAJOR REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071000121 20010710 00121 NM 2001 7 10 S2YA01007 1 20010430 A 5210 DOOR DORNER DO32 DO328300 NM ENTRY DOOR OUT OF RIG A S2YA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 13 351SK 3108 FLT 2019 - DCA-GRR - DURING FLIGHT, AN CAS MESSAGE FOR THE CABIN DOOR ILLUMINATED. THE CREW DIVERTED TO PIT. MAINTENAN CE REPLACED A PROXI SENSOR AND RETURNED THE A/C TO SERVICE. LATER THE SAME DAY ON FLT 2162 - MKE-IAD, THE CAS MESSAGE F OR THE CABIN DOOR ILLUMINATED. THE CREW MADE AN AIR-TURN-BACK TO MKE. MAINTENANCE INSPECTED THE A/C ON THE GROUND AND DURING A MX FLIGHT. MAINTENANCE ADJUSTED THE SPRING TENSION, RE-RIGGED THE DOOR AND OPERATION CHECKED THE DOOR WITH NO FURTHER DEFECTS. MAINTENANCE RELEASED THE A/C TO SERVICE. (M) 2 H 7 2 4T RT A55NM 2001071000122 20010710 00122 NM 2001 7 10 S2YA01008 1 20010501 A 3230 LANDING GEAR DORNER DO32 DO328300 NM RT MLG MALFUNCTIONED A S2YA O OTHER J WARNING INDICATION CR CRUISE 1 GL 13 353SK 3164 FLT 2020 - GRR-DCA - DURING CRUISE, THE RIGHT MAIN GEAR UNLOCKED AND ANNUNCIATOR ILLUMINATED. THE GEAR WENT BACK UP AND LOCKED ON ITS OWN. THE CREW LANDED IN DCA WITHOUT INCIDENT. THE AIRCRAFT WAS INSPECTED AND FERRIED BACK TO MKE. MAIN TENANCE INSPECTED THE RIGHT MAIN GEAR AND PERFORMED SEVERAL GEAR SWINGS AND ALSO PERFORMED AND OVERSPEED INSPECTION OF T HE GEAR. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A55NM 2001071000123 20010710 00123 NM 2001 7 10 S2YA01009 1 20010507 A 3230 2240530000 UPLOCK DORNER DO32 DO328300 NM RT MLG FAULTY A S2YA O OTHER J WARNING INDICATION CR CRUISE 1 GL 13 353SK 320 3164 FLT 2297 - YYZ-MKE, DURING CRUISE, THE RIGHT MAIN GEAR UNLOCK LIGHT ILLUMINATED. THE FLIGHT CREW LANDED IN MKE WITHOUT INCIDENT. MAINTENANCE INSPECTED THE RIGHT MLG, NO DEFECTS WERE FOUND. MAINTENANCE REPLACED THE RIGHT MLG UPLOCK ASSEMB LY FOR TROUBLESHOOTING. PERFORMED OPS CHECK AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2 H 7 2 4T RT A55NM 2001071000124 20010710 00124 WP 2001 7 10 DHL2001803500 1 20010702 A 5347 S2955978 SEAT TRACK DOUG DC8 DC873 302199C WP BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 DURING C CHK FOUND FWD CARGO COMPARTMENT R/H TRACK LUGS BROKEN WORN AND POINTS OF CORROSION BETWEEN STA 70.000 AND STA 1 60.000.REMOVED DAMAGED TRACK(STA70-160)PER SRM 51-1-88.CLEANED TREATED AND PRIMED AREA PER SRM 51-1-88.INSTALLED NEW TRA CK P/N S 2955978 PER SRM 51-3-0 PAGE 1 51-3-1 PAGE 1.SDR CLOSED 2 L 7 4 4F RT 4A25 2001071000125 20010710 00125 WP 2001 7 10 DHL2001803501 1 20010702 A 5347 S2955978 SEAT TRACK DOUG DC8 DC873 302199C WP LOWER CARGO BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 FWD CARGO COMPARTMENT-R/H TRACK LUGS BROKEN AND WORN AND POINTS OF CORROSION BETWEEN STA 160.00 AND 260.00.REMOVED DAMAG ED TRACK(STA 160-260)PER SRM 51-3-0 PAGE 1. CLEANED TREATED AND PRIMED PER SRM 51-1-8 B.INSTALLED NEW TRACK (P/N S295597 8)PER SRM 51-3-0 PAGE 1,51-3-1 PAGE 1 2 L 7 4 4F RT 4A25 2001071000126 20010710 00126 EA 2001 7 10 COMA0160442 1 20010708 A 5300 50034017351 ANGLE CNDAIR CL600 CL6002B19 EA CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 18999 7014 THE FWD "J" ANGLE AT F.S. 280.00 BETWEEN LBL9 AND RBL 9 IS CORRODED.REMOVED AND REPLACED FWD "J" ANGLE AT FS 280.00 BETW EEN LBL9 AND RBL9 I/A/W WVAC E.O. 601R-53-1551. 2 L 7 2 4F RT A21EA 2001071000127 20010710 00127 EA 2001 7 10 COMA0160443 1 20010708 A 5300 601R3866949 DOUBLER CNDAIR CL600 CL6002B19 EA CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 18999 7014 DOUBLER P/N 601R38669-49 FWD OF SERVICE DOOR IS CORRODED.REMOVED AND REPLACED DOUBLER P/N 601R38669-49 FWD OF SERVICE DO OR I/A/W WVAC E.O. 601R-53-2550. 2 L 7 2 4F RT A21EA 2001071000128 20010710 00128 EA 2001 7 10 COMA0160444 1 20010708 A 5300 601R31148127 THRESHOLD CNDAIR CL600 CL6002B19 EA CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 18999 7014 THE THRESHOLD/SILL PANEL AFT OF THE SERVICE DOOR IS CORRODED.TRIMMED THRESHOLD AREA, FABED SPLICE ANGLE AND INSTALLED I/ A/W WVAC EO 601R-53-2554A. 2 L 7 2 4F RT A21EA 2001071000129 20010710 00129 EA 2001 7 10 COMA0160446 1 20010708 A 5300 BEAM CNDAIR CL600 CL6002B19 EA CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 18999 7014 THE FLOOR BEAM WEB AT F.S. 280.00 IS CORRODED ON UPPER EDGE BETWEEN RBL9 AND LBL9.TRIMMED OUT DAMAGED AREA, FABED FILLER , FABED REPAIR DOUBLER, AND INSTLALED I/A/W WVAC E.O. 601R-53-2553. 2 L 7 2 4F RT A21EA 2001071000130 20010710 00130 WP 2001 7 10 MWEA011014 1 20010710 A 5310 9911878 SKIN DOUG DC9 DC914 3022034 WP STATION 962 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FUSELAGE SKIN DENTED AT STATION 962. -- BLENDED CHAFFE IN SKIN, FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001071000131 20010710 00131 WP 2001 7 10 MWEA011015 1 20010710 A 5310 27779221 LONGERON DOUG DC9 DC914 3022034 WP STATION 256-275 BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FORWARD CARGO BAY HAS A BENT LONGERON AT 19 LEFT STATION 256-275. -- FABRICATED, LOCATED, DRILLED AND INSTALLED REPLAC EMENT SECTION OF LONGERON AND SPLICES. 2 L 7 2 4F A6WE 2001071000132 20010710 00132 WP 2001 7 10 MWEA011016 1 20010710 A 5310 5910228212 SKIN DOUG DC9 DC914 3022034 WP STATION 989-976 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FUSELAGE SKIN HAS DENTS BETWEEN CANTED FRAME STATION 989-976. -- FABRICTED REPAIR DOUBLER AND REMOVED DAMAGE AS REQUIR ED, INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001071000133 20010710 00133 WP 2001 7 10 MWEA011017 1 20010710 A 5310 5910228212 SKIN DOUG DC9 DC914 3022034 WP STATION 967 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FUSELAGE SKIN DENTED AT STATION 967. -- FABRICATED, LOCATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001071000134 20010710 00134 WP 2001 7 10 MWEA011018 1 20010710 A 5310 59114242 SKIN DOUG DC9 DC914 3022034 WP STATION 740 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FUSELAGE SKIN IS CRACKED AT STATIN 740 ALONG LONGERON 17 RIGHT. -- CUT OUT AREA CRACK, FABRICATED AND INSTALLED REPAIR PARTS. 2 L 7 2 4F A6WE 2001071000135 20010710 00135 WP 2001 7 10 MWEA011019 1 20010710 A 5310 99582283 INTERCOSTAL DOUG DC9 DC914 3022034 WP STATION 703 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 INTERCOSTAL HAS AN AREA OF LIGHT TO MODERATE CORROSION, LONGERON 29 RIGHT STATION 703. -- REMOVED CORROSION, FABRICATE D, LOCATED, DRILLED AND INSTALLED NEW INTERCOSTAL. 2 L 7 2 4F A6WE 2001071000136 20010710 00136 WP 2001 7 10 MWEA011020 1 20010710 A 5310 9958215 FRAME DOUG DC9 DC914 3022034 WP STATION 766 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 RIGHT SIDE BETWEEN LONGERON 15 AND 16 FRAME 766 SHEAR TIE HAS A FILLER ON IT THAT NEEDS TO BE REMOVED FOR FURTHER INSPEC TION. -- REMOVED FILLER, SHEAR TIE HAS A CRACK IN THE RADIUS, FABRICATED, LOCATED AND INSTALLED NEW SHEAR TIE. 2 L 7 2 4F A6WE 2001071000137 20010710 00137 WP 2001 7 10 MWEA011021 1 20010710 A 5310 9911840 FRAME DOUG DC9 DC914 3022034 WP STATION 989 CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 CANTED FRAME AT STATINO 989 HAS CHAFES ON AFT SIDE AND TOP RADIUS. -- DRILLED CHAFE ON AFT SIDE OF FRAME, PLUGGED HOLE , BLENDED ROUGH EDGES, FABRICATED AND INSTALLED ANGLES. 2 L 7 2 4F A6WE 2001071000138 20010710 00138 NM 2001 7 10 SWAA011869 1 20010629 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN FLOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 394SW 27380 EEPLS COVERS MISSING AT ROW 12 THRU ROW 14. INSTALLED COVERS PER MM. 2 L 7 2 4F RT A16WE 2001071000139 20010710 00139 NM 2001 7 10 SWAA011870 1 20010630 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN FLOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 388SW 26591 EEPLS COVER LOOSE AT AFT CABIN. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2001071000140 20010710 00140 NM 2001 7 10 SWAA011872 1 20010629 A 5311 65C35794 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 521SW 25320 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, LBL 65 , WL 202. REPAIRED FR AME PER T1-153-018. 2 L 7 2 4F RT A16WE 2001071000141 20010710 00141 NM 2001 7 10 SWAA011873 1 20010628 A 5330 65C35794 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 316SW 23338 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 10R. REPAIRED SKIN PER S WA RA. 2 L 7 2 4F RT A16WE 2001071000142 20010710 00142 NM 2001 7 10 SWAA011874 1 20010628 A 5330 6545769 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 316SW 23338 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKINS CRACKED AT BS 520, STR 12R & BS 482, STR 10R. REPAIRED SKINS PER SWA RA. 2 L 7 2 4F RT A16WE 2001071000143 20010710 00143 NM 2001 7 10 SWAA011876 1 20010630 A 5330 6545769 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING RON FOUND FUSE SKIN CRACKED AT BS 500, STR 10R. REPAIRED SKIN PER SWA RA. 2 L 7 2 4F A16WE 2001071000144 20010710 00144 NM 2001 7 10 SWAA011877 1 20010629 A 5310 65C27314 STRINGER CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 1138, STR 15L. R&R STR CLIP PER S RM. 2 L 7 2 4F A16WE 2001071000145 20010710 00145 NM 2001 7 10 SWAA011878 1 20010629 A 3350 07912 COVER BOEING 737 7375H4 138449D NM CABIN FLOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 519SW 25318 EEPLS COVERS LOOSE. SECURED EEPLS COVERS PER MM. 2 L 7 2 4F RT A16WE 2001071000146 20010710 00146 NM 2001 7 10 SWAA011880 1 20010630 A 2731 DAS414A1508 BEARING BOEING 737 7377H4 NM TAIL LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 706SW 27840 DURING SCHEDULED SERVICE CHECK, SWA SI 11055-55, FOUND LH & RH ELEVATORS # 4 ELEVATOR HINGE BEARINGS LOOSE. R&R BOTH ELEVATOR HINGE ASSY'S PER SWA RA. 2 L 7 2 4F RT A16WE 2001071000147 20010710 00147 NM 2001 7 10 SWAA011882 1 20010630 A 5330 6552988 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA RA. 2 L 7 2 4F A16WE 2001071000148 20010710 00148 NM 2001 7 10 SWAA011884 1 20010628 A 5310 6551698 SPLICE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 521SW 25320 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE'S CRACKED AT BS 908, STR 4L & 4R. R&R STRINGER SPLICE'S PER SRM 2 L 7 2 4F RT A16WE 2001071000149 20010710 00149 WP 2001 7 10 MWEA011022 1 20010710 A 5320 991245314 FRAME DOUG DC9 DC914 3022034 WP STATION 370 GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FORWARD CARGO BAY HAS A DEEP GOUGE ON FRAME CAP AT STATION 370, LONGERON 27 LEFT. -- BLENDED DEEP GOUGE, REMOVED CAP, FABRICATED NEW GUSSET, INSTALLED FRAME CAP AND MISSING FASTENERS. 2 L 7 2 4F A6WE 2001071000150 20010710 00150 WP 2001 7 10 MWEA011023 1 20010710 A 5310 76378133 LONGERON DOUG DC9 DC914 3022034 WP STATION 897 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 IMPACT DAMAGE IN THE AFT ACCESSORY TO LONGERON 23 RIGHT AT STATION 897 AND DAMAGE TO THE FRAME AT SAME LOCATION. -- RE MOVED DAMAGED SECTION OF FRAME, FABRICATED LONGERON SPLICE, INSTALLED LONGERON, FABRICATED NEW FRAME SECTION AND SHEAR C LIP, INSTALLED FRAME AND SHEAR CLIP. 2 L 7 2 4F A6WE 2001071000151 20010710 00151 WP 2001 7 10 MWEA011024 1 20010710 A 5310 3913291501 SPLICE DOUG DC9 DC914 3022034 WP STATION 360 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 LONGERON 29 LEFT SPLICE HAS SEVERAL DRILL STARTS AT STATION 360. -- REMOVED SPLICE, LOCATED, DRILLED AND INSTALLED NEW LONGERON SPLICE. 2 L 7 2 4F A6WE 2001071000152 20010710 00152 WP 2001 7 10 MWEA011025 1 20010710 A 5310 995821512 LONGERON DOUG DC9 DC914 3022034 WP STATION 740 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 DUE TO SKIN REPAIR AT STATION 740 RIGHT SIDE AT LONGERON 17 RIGHT, FORMER BETWEEN LONGERON 16 RIGHT AND 17 RIGHT HAS TO BE CUT BETWEEN LONGERON 15 AND 16 RIGHT AND RE-MADE, THEN SPLICED INTO FORMER BETWEEN LONGERON 15 AND 16 RIGHT. -- REM OVED LONGERON ON FORMER, FABRICTED AND INSTALLED FORMER. 2 L 7 2 4F A6WE 2001071000153 20010710 00153 WP 2001 7 10 MWEA011026 1 20010710 A 5310 2777948 LONGERON DOUG DC9 DC914 3022034 WP STATION 750-786 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 AFT CARGO LONGERON 26 LEFT HAS LIGHT CORROSION ALONG TOP VERTICAL LEG BETWEEN STATION 750-786. -- REMOVED LONGERON SEC TION, LOCATED AND INSTALLED NEW LONGERON. 2 L 7 2 4F A6WE 2001071000154 20010710 00154 WP 2001 7 10 MWEA011027 1 20010710 A 5310 991224339 CLIP DOUG DC9 DC914 3022034 WP STATION 786 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 LEFT SIDE SHEAR CLIP ON LONGERON 17 AT STATION 786 IS CRACKED AT THE FASTENER HOLE. -- REMOVED SHEAR CLIP, FABRICATED AND INSTALLED SHEAR CLIP. 2 L 7 2 4F A6WE 2001071000155 20010710 00155 WP 2001 7 10 MWEA011028 1 20010710 A 5310 27779244 LONGERON DOUG DC9 DC914 3022034 WP STATION 801 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 LEFT SIDE LONGERON 17 IS CRACKED AT STATION 801. -- REMOVED DAMAGED SECTION, DRILLED AND INSTALLED NEW SECTION OF LONG ERON AND SPLICE. 2 L 7 2 4F A6WE 2001071000156 20010710 00156 NM 2001 7 10 SWAA011885 1 20010630 A 5710 6567172 FITTING BOEING 737 7373H4 1384600 NM LH WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 324SW 23414 DURING SCHEDULED SERVICE CHECK, FOUND MLG WALKING BEAM SUPPORT FITTING CORRODED AT LH FWD. R &R FITTING PER MM. 2 L 7 2 4F RT A16WE 2001071000157 20010710 00157 NM 2001 7 10 SWAA011887 1 20010702 A 2731 BACB28AK04 BUSHING BOEING 737 7377H4 NM RH ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 782SA 29808 DURING SCHEDULED SERVICE CHECK, SWA SI 11052-55, FOUND RH ELEVATOR TAB # 2 HINGE BUSHING WORN. R&R ELEVATOR TAB BUSHING PER MM. 2 L 7 2 4F RT A16WE 2001071000158 20010710 00158 NM 2001 7 10 SWAA011888 1 20010701 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN FLOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 386SW 26601 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP & COVER BROKEN AT ROW 7. R&R EEPLS COVER AND REL AMPED PER MM. 2 L 7 2 4F RT A16WE 2001071000159 20010710 00159 NM 2001 7 10 SWAA011890 1 20010701 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN FLOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 362SW 26573 EEPLS INOP & COVER BROKEN AT ROW 12. R&R EEPLS COVER & RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2001071000160 20010710 00160 NM 2001 7 10 SWAA011892 1 20010702 A 5310 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 521SW 25320 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 3R. R&R STR CLIP PER SR M. 2 L 7 2 4F RT A16WE 2001071000161 20010710 00161 NM 2001 7 10 SWAA011893 1 20010702 A 5310 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 521SW 25320 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 3R & STR 4R. R&R STR CLIPS PE R SRM. 2 L 7 2 4F RT A16WE 2001071000162 20010710 00162 NM 2001 7 10 SWAA011894 1 20010702 A 5310 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 521SW 25320 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727C, STR 4R, STR 2R, STR 4L & STR 3L. R&R STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001071000163 20010710 00163 NM 2001 7 10 SWAA011895 1 20010702 A 5310 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 521SW 25320 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 767, STR 4L & STR 4R. R&R S TR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001071000164 20010710 00164 NM 2001 7 10 SWAA011896 1 20010702 A 5310 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 521SW 25320 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 4L. R&R STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001071000165 20010710 00165 NM 2001 7 10 SWAA011902 1 20010702 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 615SW 27698 DURING SCHEDULED C3 CHECK, FOUND RH OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED EXIT LEN S PER MM. 2 L 7 2 4F RT A16WE 2001071000166 20010710 00166 NM 2001 7 10 SWAA011904 1 20010703 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 FUSELAGE SKIN CRACKED AT BS 1050, STRINGER 22L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001071000167 20010710 00167 NM 2001 7 10 SWAA011905 1 20010702 A 5330 6545835 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT E&E EQUIPTMENT COOLING DUCT CUT-OUT AFT EDGE. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001071000168 20010710 00168 NM 2001 7 10 SWAA011906 1 20010704 A 5314 6545819 WEB BOEING 737 7375H4 138449D NM NOSE W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 514SW 25153 DURING SCHEDULED SPV CHECK, FOUND NLG W/W LH WEB CRACKED AT BS 259.5, WL 180.. REPAIRED WEB PER SWA RA. 2 L 7 2 4F RT A16WE 2001071000169 20010710 00169 NM 2001 7 10 SWAA011907 1 20010704 A 5330 6545774 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED, BS 727D, AFT OF RH WING BODY FAIRING EMERGENCY EXIT LIGHT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001071000170 20010710 00170 NM 2001 7 10 SWAA011908 1 20010704 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 312SW 23334 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STRINGER 10L. REPAIRED SK IN PER SWA RA. 2 L 7 2 4F RT A16WE 2001071000171 20010710 00171 NM 2001 7 10 SWAA011909 1 20010704 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 312SW 23334 DURING SCHEDULED C1 CHECK, FOUND 3 EACH FUSELAGE SKIN CRACKS, BS 482, STRINGERS 10R & 4R, AND BS 787, STR 10L.. REPAIRED SKIN PER SWA RA. 2 L 7 2 4F RT A16WE 2001071000172 20010710 00172 NM 2001 7 10 SWAA011913 1 20010705 A 2731 183A8410 BUSHING BOEING 737 7377H4 NM RH ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 736SA 27868 DURING SCHEDULED SERVICE CHECK,(SI 11038-55) FOUND RH ELEVATOR TAB OTBD CONTROL ROD BUSHING WORN. R &R BUSHING PER MM. 2 L 7 2 4F RT A16WE 2001071000173 20010710 00173 NM 2001 7 10 SWAA011914 1 20010705 A 5754 65C26601 SLAT BOEING 737 7373Q8 1384670 NM LH WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D CHECK AT DALFORT, FOUND #1 L/E SLAT LOWER SURFACE SKIN CRACKED AT OTBD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2001071000174 20010710 00174 NM 2001 7 10 SWAA011916 1 20010704 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STRINGER 10R. REPAIRED SKIN PER BOEING SB & SWA RA. 2 L 7 2 4F RT A16WE 2001071000175 20010710 00175 NM 2001 7 10 SWAA011917 1 20010705 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 980, STRINGER 22L. REPAIR ED SKIN PER SWA RA. 2 L 7 2 4F RT A16WE 2001071000176 20010710 00176 NM 2001 7 10 SWAA011923 1 20010707 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN FLOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 EEPLS COVER NOT SECURED AT ROW 8. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2001071000177 20010710 00177 NM 2001 7 10 SWAA011925 1 20010706 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 22L. REPAIRED SKI N PER SRM. 2 L 7 2 4F RT A16WE 2001071000178 20010710 00178 NM 2001 7 10 SWAA011926 1 20010705 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 638SW 27711 DURING SCHEDULED C3 CHECK, FOUND FWD OVERHEAD EXIT SIGN LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2001071000179 20010710 00179 NM 2001 7 10 SWAA011927 1 20010707 A 5311 6545409 WEB BOEING 737 7373A4 1384585 NM RH MLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 665, RBL 38. REPAIRED WEB PER SWA TI. 2 L 7 2 4F RT A16WE 2001071000180 20010710 00180 NM 2001 7 10 SWAA011929 1 20010708 A 5311 6545871 FRAME BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 635SW 27708 DURING SCHEDULED 1/2D CHECK, FOUND AFT ENTRY DOOR FWD FRAME CRACKED AT CUTOUT FOR #2 STOP. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001071000181 20010710 00181 NM 2001 7 10 SWAA011930 1 20010708 A 7920 3352348510 CHIP DETECTOR BOEING 737 7375H4 138449D NM CFM56 CFM56* 13802 NE # 1 ENGINE DISLODGED A SWAA B A EMER. DESCENT UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 508SW 24185 723134 (ENGINE SHUT DOWN, DIVERSON & DECLARED EMERGENCY)…………………………DURING CRUSE # 1 ENGINE OIL PRESS & OIL QUANITY INDICATED OUT OF LIMITS. FOUND # 1 ENG AFT OIL CHIP DETECTOR DISLODGED, SECURED CHIP DETECTOR PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2001071000182 20010710 00182 NM 2001 7 10 VNAA0107005 1 20010704 A 3000 7008470822 RADAR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FWD FAILED A VNAA O OTHER O OTHER CL CLIMB 1 GL 07 424JS 10695 3033 FLIGHT 4075 WAS CLIMBING THROUGH 15,000 FEET AND THE WEATHER RADAR BEGAN TO MALFUNCTION. THE CREW CONTACTED DISPATCH AN D WAS ADVISED TO RETURN TO PIT. MAINTENANCE INSPECTED AND REPLACED THE WEATHER RADAR IN ACCORDANCE WITH DORNIER MAINTEN ANCE MANUAL 30-00-00. OPERATIONAL TESTS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001071000183 20010710 00183 NM 2001 7 10 VNAA0107004 1 20010704 A 3000 7008470822 RADAR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FWD FAILED A VNAA O OTHER O OTHER CR CRUISE 1 GL 07 427JS 12857 3039 FLIGHT 4007 WAS IN CRUISE AT 22,000 AND WAS INFORMED OF SHOWERS IN THE FLIGHT PATH. THE WEATHER RADAR WAS NOT INDICATIN G ANY SHOWERS. THE CREW CALLED DISPATCH TO CONFIRM SHOWERS IN THE FLIGHT PATH, DISPATCH DID CONFIRM THE SHOWERS. FLIGH T 4007 THEN RETURNED TO PIT TO HAVE THE RADAR INSPECTED. MAINTENANCE INSPECTED AND REPLACED THE WEATHER RADAR IN ACCORD ANCE WITH DORNIER MAINTENANCE MANUAL 30-00-00. OPERATIONAL TESTS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVI CE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001071000184 20010710 00184 NM 2001 7 10 VNAA0107006 1 20010704 A 7100 HARNESS DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LH FAILED A VNAA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 07 436JS 3052 AFTER APPLYING POWER FOR TAKE OFF, THE AIRCRAFT LOST 50 PERCENT TORQUE AS THE AIRCRAFT ROTATED. THE POWER CAME BACK AND THE CREW DECIDED TO RETURN TO THE FIELD. THE CREW ALSO RECEIVED A LEFT HAND ELECTRONIC CONTROL UNIT FAILURE. MAINTENA NCE INSPECTED AND FOUND DEBRIS AND SLUDGE ON THE ELECTRONIC CONTROL UNIT AND INTERCOMP BLEED VALVE CANNON PLUGS. MAINTE NANCE CLEANED THE CANNON PLUGS THEN CLEANED ALL THE ENGINE HARNESS CANNON PLUGS IN ACCORDANCE WITH DORNIER MAINTENANCE M ANUAL 71-00-00. OPERATIONAL TESTS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001071000185 20010710 00185 NM 2001 7 10 VNAA0107009 1 20010707 A 2800 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 440JS 3058 FLIGHT 4082 WAS ENROUTE TO YOW AND THE CREW RECEIVED A CROSS BLEED FAIL CAS MESSAGE. FLIGHT 4082 THEN RETURNED TO PIT W HERE MAINTENANCE INSPECTED AND REPLACED THE FUEL CROSS BLEED SHUT OFF VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUA L 28-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001071000186 20010710 00186 EU 2001 7 10 SIMA20010571 1 20010226 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 971NA 017 MCO - DURING PS CHECK MAINTENANCE FOUND FLOOR PROXIMITY LIGHTS AT 1AB, 3AB, AND 4AB TO BE INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THREE EMERGENCY LIGHT POWER SUPPLY UNIT BATTERY PACKS (S/N'S 480, 26685, 17819). OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001071000187 20010710 00187 WP 2001 7 10 ZW0A0104805 1 20010708 A 3350 58222 POWER SUPPLY DOUG DC9 DC982 3022082 WP A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9002 49153 FIRST CLASS EGRESS LIGHTS INOP . REPLACED EGRESS LIGHTING POWER SUPPLY P/N 5822-2.LAST CHECK C 2/5/01 STL ---CLOSED--- 2 L 7 2 4F A6WE 2001071100001 20010711 00001 2001 7 11 01FDEA00530 4 20010709 A 3416 ADC AIRBUS 310 A310222 3930315 EU FAULTY A FDEA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 SO 25 419FE 345 01-228 AIRSPEEDS. R&R #2 ADC PER MM 34-11-34 & PURGED F/O PITOT LINE. OPS CK OK. 2 L 7 2 4F RT A35EU 2001081500079 20010815 00079 NM 2001 8 15 01FDEA00531 1 20010710 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11 3023602 NM MAIN DECK DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 592FE 48550 MAIN DECK FLOOR TRACK DAMAGED AT BS Y=800 X= 47. *S/D* REMOVED AND REPLACED SEAT TRACK PER SRM 51-70-00 FIG 1 VOL 1. 2 L 7 3 4F RT A22WE 2001071100002 20010711 00002 NM 2001 7 11 0102006313 1 20010601 A 2530 OVEN BOEING 747 747451 1384940 NM GALLEY FIRE A NWAA H DEACTIVATE SYST/CIRCUITS A FLAME/FIRE CR CRUISE 1 GL 01 673US 30268 DURING CRUISE, THE NR 4 GALLEY NR 1 OVEN CONTENTS CAUGHT FIRE. FLIGHT ATTENDANTS PULLED CIRCUIT BREAKERS, REMOVED FOOD, AND FOUND SUBSTANTIAL AMOUNT OF GREASE ON BOTTOM OF OVEN. MAINTENANCE INSPECTED OVEN AREA, ELECTRICAL WIRING AND CONNE CTIONS CHECKED OK. REPLACED OVEN, OPERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001071100003 20010711 00003 NM 2001 7 11 01FDEA00436 1 20010613 A 2820 ACTUATOR BOEING 727 727233 138408A NM FUEL SYSTEM FAULTY A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 276FE 22041 IN CRUISE NR 2 FUEL PUMPS ON, ALL CROSS FEEDS OPEN, TANK NR 1 & 3 FUEL PUMP OFF. FUEL STILL BURN TANK TO ENG. *S/D* R EMOVED AND REPLACED ACT ASSY PER MM 28-22-011-4, REMOVED AND REPLACED CANNON PLUG D40 REF 727-200 MM CH 20. 2 L 7 3 4F RT A3WE 2001071100004 20010711 00004 EU 2001 7 11 01FDEA00469 1 20010620 A 2130 INDICATOR AIRBUS 310 A310203 EU COCKPIT FAULTY A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 409FE 47806 ON CLIMB GOT ECAM ADVISORY CAB PRESS - VENT OVERBOARD FAULT WITH XX'S ON ECAM PG. CABIN WOULD NOT PRESSURIZE. 2 L 7 2 4F RT A35EU 2001071100005 20010711 00005 WP 2001 7 11 01FDEA00470 1 20010620 A 5270 WARNING LIGHT DOUG DC10 DC1010F 3022111 WP COCKPIT ILLUMINATED A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 052FE 47806 AFT T/O CR AIR CONDITIONER DOOR LIGHT STARTED FLICKERING THEN BECAME STEADY PER RED TAB. ACN RELEASE PER MEL. ALL A/C DOOR VERIFIED CLOSED AND LOCKED. 2 L 7 3 4F A22WE 2001071100006 20010711 00006 NM 2001 7 11 01FDEA00471 1 20010620 A 2612 892809040001F CONTROL UNIT BOEING 727 727233 138408A NM COCKPIT FAULTY A FDEA O OTHER N FALSE WARNING LD LANDING 1 SO 25 271FE 22036 NR 1 ENG FIRE LIGHT ILLUM ON LAND ALONG WITH BELL AND MASTER FIRE LIGHT ENG FIRE CKLIST ACCOMP. REMOVED AND REPLACED NR 1 FIRE DETECTION CONTROL UNIT. TEST GOOD PER 727 MM 26-11-001-5. INSP FIRE LOOPS NO DAMAGE NOTED. FOUND BLD AIR LINE LOOSE AT VALVE. TIGHTENED LINE PER SMP. 2 L 7 3 4F RT A3WE 2001071100007 20010711 00007 NM 2001 7 11 01FDEA00472 1 20010617 A 5730 SKIN BOEING 727 727233 138408A NM WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 223FE 20935 LOWER WING SKIN CORRODED AT BS 840, LBL 30 ABOVE PRIMARY HEAT EXCHANGE. REMOVED AND REPLACED PER IAW FEDEX 7-5710-57961 . 2 L 7 3 4F RT A3WE 2001071100009 20010711 00009 EU 2001 7 11 01FDEA00475 1 20010611 A 2700 A2717051120000 BUSHING AIRBUS 310 A310203 EU ACTUATOR MISSING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 427FE 362 DURING REMOVAL OF RT WING ASA ACTUATOR FOUND THEY WERE RUBBING INTO THE WING STRUCTURE AT 3 POS. REMOVED AND REPLACED A CTUATOR RODEND BEARINGS AND BUSHING. 2 L 7 2 4F RT A35EU 2001071100010 20010711 00010 WP 2001 7 11 01FDEA00478 1 20010619 A 5320 POMF00110 FLOOR SUPPORT DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 313FE 48311 BS 1139 X=+6 THERE IS A 2 INCH CRACK IN FLOOR SUPPORT. *S/D* REMOVED, REPLACED AND FAB PER IAW SRM 51-10-01, 51-21-01, 51-31-01. 2 L 7 3 4F RT A22WE 2001071100011 20010711 00011 WP 2001 7 11 01FDEA00479 1 20010608 A 5347 WAC7002 SEAT TRACK DOUG DC10 DC1030F 3023504 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 313FE 48311 BS 119 RT SIDE OF CENTERLINE OF UPPER CARGO TRACK NR 3 SEAT TRACK IS DAMAGED APPROX 4 INCHES. *S/D* REMOVED AND REPLAC ED SEAT TRACK PER IAW SRM 53-70-00 & 53-42-01. 2 L 7 3 4F RT A22WE 2001071100012 20010711 00012 WP 2001 7 11 01FDEA00480 1 20010608 A 5347 WAC7002 SEAT TRACK DOUG DC10 DC1030F 3023504 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 313FE 48311 BS 949 RT SIDE OF CENTERLINE TRACK NR 3 UPPER CARGO COMP SEAT TRACK IS DAMAGED APPROX 8 INCHES. *S/D* REMOVED AND REPL ACED SEAT TRACK PER IAW SRM 53-70-00, 53-42-01. 2 L 7 3 4F RT A22WE 2001071100013 20010711 00013 WP 2001 7 11 01FDEA00481 1 20010608 A 5347 WAC7002 SEAT TRACK DOUG DC10 DC1030F 3023504 WP FUSELAGE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 313FE 48311 BS 1050 LT SIDE OF CENTERLINE SEAT TRACK WORN APPROX 6 INCHES. *S/D* REMOVED AND REPLACED SEAT TRACK PER IAW SRM 53-70 -00. 2 L 7 3 4F RT A22WE 2001071100018 20010711 00018 NM 2001 7 11 01FDEA00490 1 20010620 A 2923 PUMP DOUG MD11 MD11F 3023600 NM HYDRAULIC SYS BURNED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 BOTH NR 1 & 2 HYD AUXILIARY PUMPS FOUND BURNT/DAMAGED DURING RT MLG WHEEL WELL CLEANING. REMOVED AND REPLACED BOTH PUMP S. 2 L 7 3 4F RT A22WE 2001071100019 20010711 00019 WP 2001 7 11 01FDEA00491 1 20010623 A 7722 INDICATOR DOUG DC10 DC1010F 3022111 WP COCKPIT FAULTY A FDEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 25 368FE 46606 451301 ON T/O ROLL PWR COMING UP AT 60 - 70 PERCENT NR 2 EGT WENT OFF SCALE HIGH ON BOTH POINTER AND DIGITAL READOUT. T/O ABOR TED AT 15 KTS GROUND SPEED. REMOVED AND REPLACED NR 2 EGT GAUGE AND CB PER MM 77-21-00. OPS GOOD. 2 L 7 3 4F A22WE 2001071100020 20010711 00020 NM 2001 7 11 01FDEA00492 1 20010623 A 2612 CONTROL UNIT BOEING 727 727233 138408A NM FIRE DETECTION FAULTY A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 271FE 22036 ON APPROACH NR 1 FIRE HANDLE ILLUM AND FIRE WARN BELL SOUNDED. THE THROTTLES WERE AT FLT IDLE. REPEAT WRITE UP. FIRE WARNING 1-2 SEC. *S/D* REMOVED AND REPLACED NR 1 CONTROL UNIT AND NR 1 STRUT FIREWALL LOOP AS PRECAUTIONARY SYS PER MM 26-11-012-4 & 26-11-002-5. 2 L 7 3 4F RT A3WE 2001071100023 20010711 00023 NM 2001 7 11 0102282707 1 20010702 A 3211 TRUNNION BOEING BOEING 727 727225 1384077 NM CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 816EA 3365 22553 During Overnight inspection found crack in Right Main Landing Gear aft trunnion boss. Replaced Right Main Landing per Ma intenance Manual procedure 3211-9803. Reference Logpage 1631910. 2 L 7 3 4F A3WE 2001071100025 20010711 00025 2001 7 11 2001UALA00467 4 20010407 A 3431 RECEIVER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE ILS SYSTEM FAULTY A UALA K NONE J WARNING INDICATION AP APPROACH 1 WP 29 673UA 29241 LOST BOTH LOC AND GS SIGNALS ON BOTH CAPT AND FO'S SIDE ON FINAL APPROACH. *S/D* DUE TO AIR DATA COMPUTER FAULT CODES, THE LEFT AIR DATA COMPUTER WAS REPLACED. ON THE NEXT FLIGHT LEG THE FIRST OFFICER'S GLIDESLOPE AND LOCALIZER FLAGS WER E ON AND OFF DURING FINAL. THE RIGHT MULTI MODE RECEIVER PART NUMBER WAS REPLACED AND OPS CHECK GOOD. ILS SYSTEM OPER ATION HAS BEEN NORMAL TO DATE. BOTH REMOVED UNITS WERE CHECKED IN THEIR RESPECTIVE COMPONENT SHOP AND THERE WERE NO FAU LTS FOUND IN BOTH CASES. 2 L 7 2 4F 4 F RT A1NM E24NE 2001071100029 20010711 00029 NM 2001 7 11 DHL2001712008 1 20010710 A 7603 FUEL CONTROL BOEING 727 72729 1384007 NM A DHLA E ENGINE SHUTDOWN S R AFFECT SYSTEMS PARTIAL RPM/PWR LOSS DE DESCENT 1 SO 01 712DH 19401 AT TOP IF DESENT #1 ENGINE WOULD NOT RESPOND TO THRUST LEVER MOVEMENTS, STAYED AT MIN OF 75% N1, PRECAUTIONARY ENG SHUT DOWN ACCOMPLISHED WITH UNEVENTFUL LANDING#1 ENG FUEL CONTROL R&R SEE ITEM 7M LOG PG. 224983.STATUS: CLOSED 2 L 7 3 4F A3WE 2001071100030 20010711 00030 NM 2001 7 11 2001UALA00783 1 20010520 A 2121 FAN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 652UA 25390 CREW EXPERIENCED BURNING ODOR IN COCKPIT AND FOUND EQUIP EXHAUST FAN 1 CB TRIPPED. 2 L 7 2 4F 4 F RT A1NM E24NE 2001071100031 20010711 00031 NM 2001 7 11 2001UALA00787 1 20010521 A 5320 ANGLE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 AFT CARGO PIT BS 1087 AT STR 36R FRAME TO STRINGER ATTACH ANGLE CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED F RAME ATTACH ANGLE PER BAC DRAWING 146T1070-5 AND SRM 51-40-2. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071100032 20010711 00032 NM 2001 7 11 2001UALA00791 1 20010521 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 CORROSION ON STRINGER 34R FROM STATION 412-434 FORWARD PIT. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED STRINGER PER SR M 53-00-03 AND 51-40-2. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071100033 20010711 00033 NM 2001 7 11 2001UALA00792 1 20010521 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 CORROSION ON STRINGER 34R FROM STATION 412 - 434, FORWARD PIT. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED STRINGER AS PER SRM 53-00-03 AND 51-40-2. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071100034 20010711 00034 NM 2001 7 11 2001UALA00793 1 20010521 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 MAIN CABIN UNDER FLOOR T-CAP CORRODED BS 873, RBL 12. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED T-CAP PER SRM 53-00-5 1. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071100035 20010711 00035 NM 2001 7 11 2001UALA00795 1 20010521 A 5330 SKIN BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE GROOVED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 LEFT SIDE OF EMPENNAGE SKIN HAS LONG WEAR GROOVE FS 1809, WL 226.10. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED SKIN A S PER SRM 53-80-01. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071100036 20010711 00036 NM 2001 7 11 2001UALA00796 1 20010521 A 5320 CLIP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 FORWARD PIT STATION 370 FRAME CLIP CRACKED BETWEEN STRINGERS 39R AND 39L. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED F RAME CLIP PER SRM 51-40-2 AND BAC DRAWING 141T3220. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071100037 20010711 00037 NM 2001 7 11 2001UALA00797 1 20010521 A 5320 SPLICE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 SPLICE 146T1033-60 CORRODED BEYOND LIMITS STATION 1439, BETWEEN STRINGERS 25R AND 26R. *S/D* MAJOR REPAIR ACCOMPLISHED . REPLACED SPLICE PER BAC DRAWING 146T1033 AND SRM 51-40-2. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071100038 20010711 00038 EU 2001 7 11 2001UALA00799 1 20010504 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 434UA 592 DENT IN FUSELAGE SKIN, 13 INCHES AFT OF FRAME 65 AND BETWEEN STRINGER 23R AND 24R WAS FOUND CRACKED. 2 L 7 2 4F 4 F RT A28NM E40NE 2001071100039 20010711 00039 NM 2001 7 11 2001UALA00817 1 20010524 A 5311 FRAME BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 615UA 21876 BS 1241 LBL 45 - RBL 45 FRAME T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 51-40-02 AND BAC DRAWINGS 141T1060 AND 146T1208. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071100040 20010711 00040 NM 2001 7 11 2001UALA00819 1 20010521 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 AFT PIT APPROX BS 1279 SHEAR TIE BETWEEN 33R AND 34R CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE PE R BAC DRAWING 146T8561 AND SRM 51-40-2. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071100041 20010711 00041 NM 2001 7 11 2001UALA00822 1 20010521 A 5320 CLIP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE MISALIGNED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 STRINGER 39R FORWARD END CLIP DOES NOT ALIGN WITH PRE-DRILLED STRINGER STATION 325. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP PER BAC DRAWING 141T1220-45 AND SRM 51-40-2. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071100043 20010711 00043 NM 2001 7 11 2001UALA00826 1 20010521 A 5320 CLIP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 FORWARD PIT, STRINGER CLIP CRACKED STATION 434 STRINGER 39L. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP PER BAC D RAWING 141T1225 AND SRM 51-40-2. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071100044 20010711 00044 NM 2001 7 11 2001UALA00828 1 20010521 A 5320 SPLICE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 FORWARD PIT STRINGER 34R BS 434 HAS A CRACK. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED SPLICE PER SRM 53-00-03 AND BA C DRAWING 140T0115-4. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071100045 20010711 00045 NM 2001 7 11 2001UALA00829 1 20010521 A 5320 CLIP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 AFT PIT STATION 1351, STRINGER 34L, STRINGER CLIP IS CRACKED. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP PER BAC DRAWING 140T2101 AND SRM 51-30-2. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071100046 20010711 00046 NM 2001 7 11 2001UALA00830 1 20010521 A 5320 STRINGER CLIP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 FORWARD PIT STATION 412 AND STRINGER 37L, CLIP IS CORRODED. *S/D* MAJOR REPAIR IS ACCOMPLISHED. REPLACED STRINGER CLI P PER SRM 51-40-2 AND BAC DRAWING 141T1225. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071100047 20010711 00047 NM 2001 7 11 2001UALA00833 1 20010521 A 5320 STRINGER CLIP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 FORWARD PIT, STRINGER CLIP AT STATION 434, STRINGER 37L BROKEN. *S/D* MAJOR REPAIR IS ACCOMPLISHED. REPLACED CLIP PER BAC DRAWING 140T2101-573 AND SRM 51-40-2. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071100048 20010711 00048 NM 2001 7 11 2001UALA00835 1 20010521 A 5320 STRINGER CLIP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 FORWARD PIT, STRINGER CLIP AT STATION 434 STRINGER 38R BROKEN. *S/D* MAJOR REPAIR IS ACCOMPLISHED. REPLACED CLIP PER BAC DRAWING 140T2101-573 AND SRM 51-40-2. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071100049 20010711 00049 NM 2001 7 11 2001UALA00837 1 20010521 A 5320 SPLICE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 STRINGER 38R SPLICE AT STATION 434 HAS AN ELONGATED HOLE FOR STRINGER CLIP. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED SPLICE PER SRM 53-30-03 AND 51-40-2. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071100050 20010711 00050 NM 2001 7 11 2001UALA00842 1 20010511 A 5320 SPLICE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 434 STRINGER 36R TO 36L BUTT SPLICE DAMAGED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED BUTT SPLICE IN ACCORDANCE WITH BAC DRAWING 140T0111 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071100051 20010711 00051 NM 2001 7 11 2001UALA00844 1 20010511 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 610-620 STRINGER 37R INTERCOSTAL CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACC ORDANCE WITH BAC DRAWING 143T5000 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071100052 20010711 00052 NM 2001 7 11 2001UALA00845 1 20010511 A 5320 SPLICE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 434 STRINGER SPLICE 39R CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE W ITH BAC DRAWING 140T0115 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071100053 20010711 00053 NM 2001 7 11 2001UALA00846 1 20010511 A 5320 SPLICE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 434 STRINGER 39L SPLICE CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE W ITH BAC DRAWING 140T01115 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071100054 20010711 00054 NM 2001 7 11 2001UALA00847 1 20010511 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 438 STRINGER 35R CRACKED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND REPAIRED IN ACCORDANCE WITH SRM 53-30-03 , FIG 202. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071100055 20010711 00055 NM 2001 7 11 2001UALA00849 1 20010511 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 434-456 STRINGER 37R STRINGER CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORD ANCE WITH SRM 53-30-03 AND 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071100056 20010711 00056 NM 2001 7 11 2001UALA00853 1 20010514 A 2421 736664 IDG BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LT ENGINE MALFUNCTIONED A UALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 WP 29 620UA 21880 LT GEN DRIVE LIGHT ON AFTER TAKEOFF. LT GEN DRIVE DISCONNECTED, RTF. *S/D* REPLACED LEFT HAND (NR 1) INTEGRATED DRIV E GENERATOR, OPS CHECKS NORMAL ON ENGINE RUN. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071100057 20010711 00057 NE 2001 7 11 MALA010570 2 20010704 A 7220 200304815 ENGINE BAC 146 AVRO146RJ85A 1500097 EU CT7TP CT75A 30030 NE A MALA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 15 509XJ E2321 During Flight # 3407, enroute to Fargo, #3 Engine Oil Pressure low light illuminated. Crew checked Oil Press gauge, ind icated no oil pressure in #3 Engine. N1 was about 19%, N2 was about 12%, Airspeed 230 Kts. Windmill time 15 min. Temp at Shutdown normal. Maintenance removed and replaced #3 Engine, PN 2-003-048-15, SN/off P07666, SN/on P07793. Refer to J/ C 7100-502 for details. Ops checks good and leaks good. IAW AMM 71-00-00-501. 2 H 7 4 4F 4 T RT A49EU E8NE 2001071100058 20010711 00058 EU 2001 7 11 MALA010572 1 20010707 A 3230 801801 PROXIMITY SWITCH BAC 146 AVRO146RJ85A 1500097 EU DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 502XJ E2307 On Flight # 3569,LH Gear Intransit light would not go out on retraction. Air return to MEM. Maintenance replaced Proxi mity Switch @ GJ 13 PN 8-018-01. Ref AMM 32-60-17 (401) for replacement and Ref AMM 32-60-17 (501) for test. 2 H 7 4 4F RT A49EU 2001071100059 20010711 00059 NM 2001 7 11 2001UALA00855 1 20010527 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 FLOORBEAM CORRODED STA 345, RBL 54. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED STRAP REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2001071100060 20010711 00060 NM 2001 7 11 2001UALA00856 1 20010527 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 511UA 24799 FRAME DAMAGED IN AFT PIT STA 1260 RBL 25. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLERS AT UPPER FLANGE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001071100061 20010711 00061 NM 2001 7 11 2001UALA00857 1 20010527 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 543UA 25698 FUSELAGE SKIN DENTED STA 600 - 620 WL 207. MAJOR REPAIR ACCOMPLISHED. INSTALLED SKIN DOUBLER AND SPLICED CREASE BEAM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001071100062 20010711 00062 NM 2001 7 11 2001UALA00858 1 20010528 A 5511 RIB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HORIZ STAB DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 359UA 24452 LT STABILIZER LEADING EDGE HAS DENT ON NR 12 RIB FROM INBOARD END. STRAIGHTENED SHEETMETAL AND RIB. MAJOR REPAIR ACCOM PLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001071100063 20010711 00063 NM 2001 7 11 2001UALA00859 1 20010526 A 5230 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 951UA 26696 FWD CARGO DOOR SKIN DAMAGED. INSTALLED DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001071100064 20010711 00064 NM 2001 7 11 2001UALA00861 1 20010526 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 317UA 23949 FWD CABIN FRAME AT BS 400, NEAR STR 16R IS DENTED. ACCOMPLISHED STRAP REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001071100065 20010711 00065 NM 2001 7 11 2001UALA00863 1 20010527 A 5311 FRAME BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 974UA 21597 FRAME CRACKED IN RADIUS AT BS 188, WL 207. REPAIRED FRAME. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F A16WE E2EA 2001071100066 20010711 00066 NM 2001 7 11 2001UALA00864 1 20010528 A 5311 FRAME BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 974UA 21597 FUSE FRAME CRACKED IN RADIUS AT BS 188, WL 207, STR 17L. ACCOMPLISHED FRAME REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F A16WE E2EA 2001071100067 20010711 00067 NM 2001 7 11 2001UALA00865 1 20010528 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 317UA 23949 EXCESSIVE MATERIAL LOSS ON CABIN FLOORBEAM AT BS 947.5, LBL 15. ACCOMPLISHED REINFORCING ANGLE REPAIR. MAJOR REPAIR AC COMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001071100068 20010711 00068 NM 2001 7 11 2001UALA00866 1 20010528 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 318UA 23950 INTERCOSTAL FWD END IS CRACKED AT BS 380, BL 0. REPLACED INTERCOSTAL. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001071100069 20010711 00069 NM 2001 7 11 2001UALA00867 1 20010527 A 5553 FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE VERTICAL STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 CORROSION FOUND ON VERTICAL STABILIZER LT & RT MAIN CHORD ATTACH FITTING AND LT & RT FAIL-SAFE CHORD ATTACH FITTING. *S /D* REMOVED CORROSION. INSTALLED OVERSIZE BUSHINGS. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001071100070 20010711 00070 NM 2001 7 11 2001UALA00868 1 20010529 A 7603 THROTTLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE STUCK A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 324UA 23956 725119 UNSCHEDULED LANDING DUE TO NR 2 ENGINE THROTTLE STUCK. *S/D* THE S650 THRUST REVERSER SWITCH WAS FOUND HANGING ON THE LEFT HAND SIDE OF THE PEDESTAL WITH NO ATTACHING HARDWARE. THE ENGINE THROTTLE BOX WAS ALSO REPLACED AS A PRECAUTION. 2 L 7 2 4F 4 F RT A16WE E2GL 2001071100071 20010711 00071 2001 7 11 2001UALA00869 4 20010529 A 3442 6225122103 TRANSMITTER BOEING 737 737522 138449F NM WEATHER RADAR INOPERATIVE A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 943UA 26680 UNSCHEDULED LANDING DUE TO WEATHER RADAR SYSTEM INOPERATIVE. *S/D* REPLACED WXR TR UNIT, SCANNER AND CONTROL PANEL. W XR TR - 622-5122-103, SCANNER - 622-5125-001, CONTROL PANEL - 622-5129-107. 2 L 7 2 4F RT A16WE 2001071100072 20010711 00072 NE 2001 7 11 2001UALA00870 2 20010526 A 7530 7765555 CONTROL VALVE BOEING 767 767322 1385200 NM PWA JT9 JT9D7R4D 52054 NE ENGINE OUT OF RIG A UALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION NR NOT REPORTED 1 WP 29 644UA 25094 707543 WEATHER RADAR INOP. DIVERTED TO MCO DUE TO T-STORMS IN MIA AREA. *S/D* ENGINE WAS REPLACED DUE TO OVERTEMP. DURING E NGINE PRE-REPAIR RUN, FOUND ENGINE VANE BLEED CONTROL (EVBC) WAS OUT OF TRIM. EVBC WILL BE OVERHAULED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071100073 20010711 00073 NM 2001 7 11 2001UALA00871 1 20010530 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 511UA 24799 FRAME CORRODED STA 1020 LBL 75, WL 208. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW T-CHORD REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2001071100074 20010711 00074 NM 2001 7 11 2001UALA00872 1 20010525 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 573UA 26685 FUSELAGE DAMAGED STA 580 - 600, STR 16L-17L. MAJOR REPAIR ACCOMPLISHED. SPLICED STRINGER, INSTALLED NEW SHEAR TIE AND INSTALLED SKIN DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2001081600102 20010816 00102 NM 2001 8 16 2001UALA00873 1 20010530 A 2920 1211233005 ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RAM AIR TURBINE MALFUNCTIONED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 549UA 25397 RAM AIR TURBINE FAILED TO DEPLOY DURING FUNCTIONAL CHECK OF THE MANUAL SYSTEM ACCOMPLISHED AT HEAVY MAINTENANCE VISIT. *S/D* REPLACED RAT ACTUATOR. ACTUATOR WAS TESTED BY THE MANUFACTURER, NO FAULT FOUND, RETURNED TO SERVICE. AFTER SUBS EQUENTLY TESTED ON A NEW ACFT, RAT DEPLOYED AS REQUIRED. 2 L 7 2 4F 4 F RT A2NM E17NE 2001071100075 20010711 00075 NM 2001 7 11 2001UALA00875 1 20010528 A 7830 WARNING LIGHT BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE COCKPIT ILLUMINATED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 601UA 21862 LT REV EICAS AMBER LIGHT CAME ON DURING GROUND ROLL AT APPROXIMATELY 80 KTS. RTO. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071100076 20010711 00076 NM 2001 7 11 2001UALA00877 1 20010530 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY LIGHT INOP AT DOOR 1 LEFT AFT SILL. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2001071100077 20010711 00077 NM 2001 7 11 2001UALA00878 1 20010530 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 318UA 23950 CRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. INSTALLED DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001071100078 20010711 00078 NM 2001 7 11 AALA20011117 1 20010519 A 3350 900542 BATTERY PACK BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 864AA 21369 DTW - DURING OVERNIGHT MAINTENANCE, LEFT FORWARD EXTERNAL OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK F OR LEFT FORWARD EXTERNAL OVERWING EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071100079 20010711 00079 NM 2001 7 11 AALA20011256 1 20010616 A 3397 WIRE BOEING 727 727223 1384074 NM AFT AIRSTAIR BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 21 861AA 21088 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIR INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIR E AT AFT AIRSTAIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071100080 20010711 00080 NM 2001 7 11 AALA20011014 1 20010501 A 3350 900542 BATTERY PACK BOEING 727 727227 1384078 NM BS 752 BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 718AA 20611 TUL - FOUND BATTERY PACK CASE BROKEN, RIGHT FORWARD AND RIGHT AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REF E-58 3878614. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 2001071100081 20010711 00081 NM 2001 7 11 AALA20011285 1 20010624 A 3350 SOCKET BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 646AA 24604 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 16D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001071100082 20010711 00082 NM 2001 7 11 AALA20011284 1 20010624 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 398AN 29605 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 32H INOPERATIVE. RE-SECURED EMERGENCY EXIT LGHT CONNEC TOR AT SEAT 32H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001071100083 20010711 00083 NM 2001 7 11 AALA20011283 1 20010623 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 386AA 27060 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 2B INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT CONN ECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001071100084 20010711 00084 NM 2001 7 11 AALA20011282 1 20010623 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 386AA 27060 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 28B INOPERATIVE. RE-SEATED EMERGENCY EXIT LIGHT CONNEC TOR AT SIDE WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001071100085 20010711 00085 NM 2001 7 11 AALA20011303 1 20010622 A 5300 STRINGER BOEING 727 727223 1384074 NM FS 720B CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 869AA 21374 TUL - FOUND CORROSION 1 INCH BY 2 INCHES ON INSIDE OF STRINGER 27R. REMOVED CORROSION AND REPAIRED STRINGER PER SRM 53- 10-3. (M) 2 L 7 3 4F A3WE 2001071100086 20010711 00086 NM 2001 7 11 AALA20011304 1 20010620 A 5100 WEB BOEING 727 727223 1384074 NM FS 1250 A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 869AA 21374 TUL - FOUND RIGHT LOWER TORQUE BOX VERTICAL WEB ROUTED OUT AT LIGHTENING HOLE WITHOUT REPAIR. INSTALLED DOUBLER REPAIR ON WEB PER SRM 51-40-2 FIG 1, PAGE 1. (M) 2 L 7 3 4F A3WE 2001071100087 20010711 00087 NM 2001 7 11 AALA20011305 1 20010623 A 5300 STRINGER BOEING 727 727223 1384074 NM FS 683-686 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 869AA 21374 TUL - FOUND STRINGER 26L HAS HEAVY CORROSION AT STATION 683 TO 686, OUTBOARD SIDE OF STRINGER. INSTALLED STRINGER REPAI R PER SRM 53-10-03. (M) 2 L 7 3 4F A3WE 2001071100088 20010711 00088 NM 2001 7 11 AALA20011306 1 20010626 A 5330 SKIN BOEING 727 727223 1384074 NM FS 680-720A CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 869AA 21374 TUL - FOUND CORROSION 60 INCHES BY 30 INCHES, ON SKIN OUTBOARD OF STRINGER 26R. REPAIRED AREA PER SRM 53-30-3 FIG 14. (M) 2 L 7 3 4F A3WE 2001071100089 20010711 00089 NM 2001 7 11 AALA20011307 1 20010626 A 5330 SKIN BOEING 727 727223 1384074 NM FS 680-720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 869AA 21374 TUL - FOUND CORROSION ON SKIN OUTBOARD STRINGER 26L. REPAIRED PER SRM 53-30-3 FIG 14. (M) 2 L 7 3 4F A3WE 2001071100090 20010711 00090 NM 2001 7 11 AALA20011276 1 20010620 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 377AN 25446 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 28B INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT CONNECT OR AT BULKHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001071100091 20010711 00091 EU 2001 7 11 AALA20011264 1 20010616 A 3350 5482461 SWITCH AIRBUS 300 A300B4605R 3930308 EU L1 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 90070 513 EWR - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT L1 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SWITCH AT L 1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2001071100092 20010711 00092 NM 2001 7 11 AALA20011262 1 20010619 A 3350 CONNECTOR BOEING 767 767223 1385123 NM R1 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 306AA 22312 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT R1 DOOR INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT CONNECTOR AT R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001071100093 20010711 00093 NM 2001 7 11 AALA20011260 1 20010619 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN INOPERATIVE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 385AM 27059 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 9D INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001071100094 20010711 00094 NM 2001 7 11 AALA20011254 1 20010615 A 3350 SPLICE BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 183AN 29593 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT DIM. REPAIRED EMERGENCY EXIT LIGHT SPLICE. SYSTEM GROUND CHEC KED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001071100095 20010711 00095 NM 2001 7 11 AALA20010759 1 20010409 A 3350 MODULE BOEING 727 727227 1384078 NM L2 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 727AA 20734 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L2 DOOR DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071100096 20010711 00096 NM 2001 7 11 AALA20010758 1 20010409 A 3350 BATTERY PACK BOEING 727 727227 1384078 NM INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 727AA 20734 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIR DIM. TIGHTENED EMERGENCY EXIT LIGHT BATTERY PA CK AT AFT AIRSTAIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071100097 20010711 00097 NM 2001 7 11 AALA20010663 1 20010329 A 3350 P400051126 MODULE BOEING 727 727227 1384078 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 722AA 20730 MIA - DURING OVERNIGHT MAINTENANCE FIRST CLASS EMERGENCY EXIT LIGHT DIM. REPLACED FIRST CLASS EMERGENCY EXIT LIGHT MODU LE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071100098 20010711 00098 NM 2001 7 11 AALA20011019 1 20010511 A 3397 WIRE BOEING 727 727227 1384078 NM CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 21 730AA 20737 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTING WIRE BROKEN AT CLASS DIVIDER. REPLACED WIRE TO EMERGENCY EXIT ESCAPE PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071100099 20010711 00099 NM 2001 7 11 AALA20010829 1 20010421 A 3350 SPLICE BOEING 727 727227 1384078 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 719AA 20612 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AFT OF FIRST CLASS DIM. REPLACED EMERGENCY EXIT LIGHT FLOOR SP LICE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071100100 20010711 00100 NM 2001 7 11 AALA20010779 1 20010415 A 3350 8039001 BATTERY BOEING 727 727227 1384078 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 719AA 20612 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PROXIMITY LIGHT DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071100101 20010711 00101 NM 2001 7 11 AALA20010967 1 20010508 A 3350 SPLICE BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 889AA 21527 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT DIM. REPAIRED EMERGENCY EXIT LIGHT SPLICE. SYSTEM GRUOND CHEC KED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071100102 20010711 00102 NM 2001 7 11 AALA20011122 1 20010521 A 3350 CONNECTOR BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 892AA 22008 DFW - DURING OVERNIGHT MAINTENANCE, COACH EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY ESC APE PATH LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071100103 20010711 00103 NM 2001 7 11 2001UALA00879 1 20010531 A 5313 STRINGER BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 994UA 22384 STRINGER CRACKED AT BS 1016, STR 6L. ACCOMPLISHED SPLICE REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F A16WE E2EA 2001071100104 20010711 00104 NM 2001 7 11 2001UALA00880 1 20010526 A 3230 LANDING GEAR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NLG MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7260U 21407 A/C RETURNED TO MIA AFTER NOSE GEAR FAILED TO RETRACT. 2 L 7 3 4F 4 F A3WE E2EA 2001081300014 20010813 00014 NM 2001 8 13 2001UALA00881 1 20010530 A 3350 S106 BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7266U 21413 CEILING EMERGENCY EXIT SIGN INOPERABLE. BATTERY FAILED. REPLACED BATTERY, OPERATIONS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001071100105 20010711 00105 NM 2001 7 11 2001UALA00882 1 20010531 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7257U 21404 CRACK LOCATED NEAR FASTENER AT STA 480. INSTALLED DOUBLER AND TRIPLER PER MAJOR SHEETMETAL REPAIR SPECIFICATIONS SRM 53 -30-03 FIG 3A AND FIG 24. MAJOR REPAIR ACCOMPLISHED. 2 L 7 3 4F 4 F A3WE E2EA 2001081300015 20010813 00015 NM 2001 8 13 2001UALA00883 1 20010530 A 2782 651785211 ACTUATOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE L/E FLAP LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 7457U 21911 RETURNED TO IAH DUE TO LOSS OF 'A' SYSTEM HYDRAULICS, FOUND NR 2 LEADING EDGE FLAP ACTUATOR LEAKING. REPLACED NR 2 FLAP ACTUATOR PER 727 MM, REPLACED NR 1, AND NR 3 ENGINE DRIVEN HYDRAULIC PUMPS PER 727 MM. 2 L 7 3 4F 4 F A3WE E2EA 2001071100106 20010711 00106 NM 2001 7 11 2001UALA00884 1 20010514 A 4920 APU BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE APU BAY MALFUNCTIONED A UALA O OTHER O OTHER CR CRUISE 1 WP 29 658UA 27113 APU NO START 3 ATTEMPTS. TWICE AT FL390 AND ONCE DESCENDING THRU FL290. MAX RPM 22 AND MAX EGT 10. 2 L 7 2 4F 4 F RT A1NM E24NE 2001071100107 20010711 00107 EU 2001 7 11 2001UALA00885 1 20010601 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 428UA 523 CABIN EMERGENCY LIGHT TEST FAILED. REPLACED DOOR 1 LEFT SLIDE AND EMERGENCY LIGHT SYSTEM POWER SUPPLY ASSEMBLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2001071100108 20010711 00108 NM 2001 7 11 2001UALA00888 1 20010531 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 STRINGER CLIP CRACKED AT BS 639, STR 8L. REPLACED CLIP. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001071100109 20010711 00109 NM 2001 7 11 2001UALA00889 1 20010531 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 WEB CRACKED AT BS 178, WL 234, RBL 12. INSTALLED DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001071100110 20010711 00110 NM 2001 7 11 2001UALA00890 1 20010531 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 CABIN FLOORBEAM UPPER T-CAP DAMAGED AT BS 1016, RBL 11. REPLACED UPPER T-CAP. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001071100111 20010711 00111 NM 2001 7 11 2001UALA00891 1 20010531 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 317UA 23949 AFT PIT FRAME DENTED AT BS 767, ABOVE STR 24L. ACCOMPLISHED FRAME DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001071100112 20010711 00112 NM 2001 7 11 2001UALA00893 1 20010531 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 318UA 23950 AFT PRESSURE BULKHEAD FWD WEB IS GOUGED AT BS 1016, WL 259, RBL 13. ACCOMPLISHED DOUBLER REPAIR. MAJOR REPAIR ACCOMPLI SHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001071100113 20010711 00113 NM 2001 7 11 2001UALA00898 1 20010602 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM CABIN INOPERATIVE A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 784UA 26951 AFT EMERGENCY PROX LIGHT AT SEAT 1F IS INOP. *S/D* POSSIBLE CAUSE OF AFT EMERGENCY PROX LIGHT AT SEAT 1F FAILURE IS DA MAGE TO THE PROX LIGHT FROM PASSENGER LUGGAGE. EXACT FAILURE CAUSE IS UNKNOWN. REPLACED LIGHT ASSEMBLY. OPS CHECKED G OOD. 2 L 7 2 4F RT T0001SE 2001071100114 20010711 00114 NM 2001 7 11 2001UALA00899 1 20010601 A 3397 801723424 WIRE BOEING 777 777222 1385219 NM CABIN DAMAGED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 793UA 26946 EMERGENCY LIGHTS AT SEAT 3F (FLOOR PROX) ARE INOP. *S/D* EMERGENCY PROX LIGHTS AT SEAT 3F WERE INOP DUE TO CHAFED OR D AMAGED WIRES NEAR THE THE SEAT DISCONNECT ALONG THE WIRE RUN WHICH CONTAINS THE INVERTERS. INSTALLED TEMPORARY REPAIR B Y SPLICING WIRE HARNESS. PERMANENT REPAIR IS SCHEDULED FOR THE NEXT MAINTENANCE OPPORTUNITY. 2 L 7 2 4F RT T0001SE 2001071100115 20010711 00115 NM 2001 7 11 2001UALA00904 1 20010602 A 3350 LIGHT BOEING 767 767322 1385200 NM CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 670UA 29240 EMERGENCY EEL LIGHT'S INOP FROM RT ROW 37 TO ROW 41 AND BOTH AFT LAV AND GALLEY FLOOR EEL LIGHTS. *S/D* LEFT TANK UNIT S 3, 5, 6, 7 AND 8 AND RIGHT TANK UNITS 5, 6, 7, 8 AND COMPENSATOR CAPACITANCE VALUES WERE OUT OF UPPER LIMIT. UNITS W ERE REMOVED AND REPLACED WITH SERVICEABLE UNITS. CAPACITANCE VALUES AND QUANTITY READINGS CORRECT AFTER TANK UNIT CHANG E. TANK UNITS CHECKED BY SHOP AND FAULT UNCONFIRMED. UNITS SERVICEABLE AFTER CLEANING AND CHECK. 2 L 7 2 4F RT A1NM 2001071100116 20010711 00116 2001 7 11 2001UALA00915 4 20010604 A 2330 285W00123 CONTROL PANEL BOEING 777 777222 1385219 NM CABIN OVERHEATED A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 769UA 26921 ELECTRICAL SMELL IN CABIN BY DOOR 2L. *S/D* THE TWO BACKLIGHTS FOR THE TOUCHSCREEN ON THE CACP AT DR 2L HAD FAILED. T HE FAILURE CREATED AN OVERHEAT CONDITION AT THE LIGHT INSULATION. THE OVERHEAT OF THE INSULATION WAS THE SOURCE OF THE ODOR. THE CACP WAS DEACTIVATED UNTIL PART WAS REPLACED. 2 L 7 2 4F RT T0001SE 2001071100117 20010711 00117 NM 2001 7 11 2001UALA00925 1 20010604 A 2120 UNKNOWN BOEING 737 737322 1384676 NM COCKPIT ODOR A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 390UA 24665 UNSCHEDULED LANDING DUE TO ELECTRICAL ODOR IN THE FLIGHT DECK. NO HARD FAULT WAS ISOLATED. ALL RESPECTIVE ATA SYSTEMS AND SUB-SYSTEMS WERE CHECKED, NO FAULT FOUND. 2 L 7 2 4F RT A16WE 2001071100118 20010711 00118 NM 2001 7 11 2001UALA00931 1 20010516 A 2530 CONTROLLER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GALLEY SMOKE A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 662UA 27159 P62 CART CONTROLLER IS SMOKING WHEN THE PIGTAIL IS UNPLUGGED. 2 L 7 2 4F 4 F RT A1NM E24NE 2001071100119 20010711 00119 NM 2001 7 11 2001UALA00932 1 20010530 A 3350 CHARGER BOEING 767 767222 1385122 NM CABIN DEFECTIVE A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 604UA 21865 EMERGENCY LIGHTS ILLUMINATED ON LEFT SIDE FROM DOOR 1 LEFT TO OVERWING EXIT BOTH UPPER LIGHTING AND EEL. *S/D* REPLACE D BATTERY CHARGER AND BATTERY M735 AND EEL POWER SUPPLY. TEST OK. 2 L 7 2 4F RT A1NM 2001071100120 20010711 00120 NM 2001 7 11 2001UALA00933 1 20010529 A 3350 POWER SUPPLY BOEING 767 767222 1385122 NM CABIN MALFUNCTIONED A UALA K NONE O OTHER CR CRUISE 1 WP 29 604UA 21865 EMERGENCY PATH LIGHTING SECTION LEFT FWD OF COACH SECTION INTERMITTENTLY ON-OFF THROUGHOUT FLIGHT. ALSO BUSINESS CLASS SECTION. *S/D* POWER SUPPLY AT STATION 425 LT. ALL LIGHTS OPS NORMAL. 2 L 7 2 4F RT A1NM 2001071100122 20010711 00122 2001 7 11 2001UALA00939 4 20010507 A 2565 SLIDE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN DEPLOYED A UALA K NONE O OTHER AP APPROACH 1 WP 29 664UA 29236 RT OVERWING SLIDE DEPLOYED. 2 L 7 2 4F 4 F RT A1NM E24NE 2001071100123 20010711 00123 NM 2001 7 11 2001UALA00942 1 20010602 A 5330 SKIN BOEING 747 747422 1384935 NM FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 193UA 26890 RIGHT SIDE OF AIRCRAFT 4 FEET ABOVE AFT OUT FLOW VALVE FOUND DENT 2.5 INCH WIDE X 2.125 INCH LONG. ALSO AREA INSIDE DEN T HAS A GOUGE .25 WIDE X 1 INCH LONG .1562 DEEP WITH SHARP METAL INSIDE GOUGED AREA. *S/D* REPAIR ACCOMPLISHED PER SRM 53-00-01 201 FIG 201. 2 L 7 4 4F RT A20WE 2001071100124 20010711 00124 NM 2001 7 11 2001UALA00951 1 20010621 A 2781 WARNING SYSTEM BOEING 767 767222 1385122 NM COCKPIT MALFUNCTIONED A UALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 WP 29 603UA 21864 ON APPROACH WHEN FLAPS SELECTED TO 25, RECEIVED LEADING EDGE AMBER CAUTION AND L/E SLAT DISAGREE EICAS MESSAGE. ON GO-AR OUND SELECTED FLAPS 20 AND CAUTION AND EICAS CLEARED. 2 L 7 2 4F RT A1NM 2001071100125 20010711 00125 NM 2001 7 11 2001UALA00958 1 20010607 A 2121 6454051 FAN BOEING 737 737322 1384676 NM CABIN FAILED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 390UA 24665 RETURNED TO FIELD, ELECTRICAL SMELL IN CABIN. *S/D* THE RECIRCULATION FAN FAILED. REPLACED THE RECIRCULATION FAN. 2 L 7 2 4F RT A16WE 2001071100126 20010711 00126 NM 2001 7 11 2001UALA00962 1 20010608 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 318UA 23950 STRINGER CLIP HAS CORROSION AT BS 767, STR 26R, RBL 15. REPLACED CLIP. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001071100127 20010711 00127 NM 2001 7 11 2001UALA00963 1 20010608 A 5312 BULKHEAD BOEING 737 737322 1384676 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 BULKHEAD WEB 2 CRACKS AT UPPER LT WX RADAR ANTENNA MOUNT AT INBD AND OUTBD EDGES OF STRAP AT BS 178, WL 213, LBL 5-6. A CCOMPLISHED DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001071100128 20010711 00128 WP 2001 7 11 ARWA0010601 1 20010601 A 7921 715447 OIL COOLER DOUG DC8 DC862 3021970 WP NR 4 ENGINE FAILED A ARWA E ENGINE SHUTDOWN M OVER TEMP CR CRUISE 1 SO 19 8968U 46069 NR 4 ENGINE OIL TEMP ROSE TO 145 DEGREES, COMPLETED IN FLIGHT SHUT DOWN CHECKLIST, ENGINE WAS SHUT DOWN AT 22:45ZULU, WI NDMILLING OIL PRESS 20 PSI. AIRCRAFT LANDED WITHOUT INCIDENTS. REMOVED AND REPLACED NR 4 OIL TEMP. INDICATOR FOR T/S. REMOVED AND REPLACED NR 4 FUEL/OIL TEMPERATURE REGULATOR IAW MM 73-11-0. REMOVED AND REPLACED OIL COOLER ASSY IAW MM 7 9-20-2, LEAK AND OPS CK PERFORMED ENGINE RUN UP. DRAINED OIL AND SERVICED IAW MM 12-10-1 AND MM 79-10-7. NO LEAKS NOTE D ON RUN UP IAW MM 71-00, OPS FOUND NORMAL. 2 L 7 4 4F 4A25 2001071100129 20010711 00129 NM 2001 7 11 UPS01236163 1 20010622 A 3230 ACTUATOR BOEING 727 72730C 1384009 NM LEAKING A IPXA K NONE E VIBRATION/BUFFET CR CRUISE 1 SO 01 919UP 19012 INSPECTION TYPE:N/A RIGHT MAIN GEAR DOOR OPENED ENROUTE GEAR HANDLE PLACED TO "UP" POSIT ION DOOR CLOSED GEAR HANDLE RET URNED TO "OFF" POSITION OPS NORMAL ****SUPPLEMENTAL MRR*** REMOVED AND REPLACED GEAR DOOR ACTUATOR R/H PER MM 32-32- 81 ADJ TEST GROUND DOOR MECHANISM PER 32-34-00 ADJ DOOR WARNING SWITCH REF 32-62 -11. JACKED AIRCRAFT PER MM 7-11-00. SW UNG GEAR. OPS CHECK NORMAL 2 L 7 3 4F A3WE 2001071100130 20010711 00130 NM 2001 7 11 UPS01236281 1 20010702 A 5310 STIFFENER BOEING 727 72727C 138400J NM AIRSTAIR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 910UP 19117 INSPECTION TYPE:C VERTICAL STIFFENER LOCATED IN AIRSTAIRS MANUAL PUMP CAVITY HAS A SUS PECT CRACK REPAIR CARRIED OUT IAW SRM 51-10-1, 51-20-1, 51-40-4 2 L 7 3 4F A3WE 2001071100131 20010711 00131 NM 2001 7 11 UPS01236282 1 20010701 A 5330 LAP JOINT BOEING 727 72727C 138400J NM BS 1115 TO 1175 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 910UP 19117 INSPECTION TYPE:C SUSPECT CORROSION AT LAP JOINT BS 1115 TO 1175 S4R REPAIR CARRIED OUT IAW SRM 51-30-2 & UPS EO B72 7-5330-0509 APPENDIX 8.3 2 L 7 3 4F A3WE 2001071100132 20010711 00132 NM 2001 7 11 UPS01236287 1 20010705 A 5280 FRAME BOEING 727 72727C 138400J NM LT MLG DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 909UP 19115 INSPECTION TYPE: C, LT MLG WING DOOR (OUTER HALF) O/B DOOR FRAME AFT CORNER CRACKED. REPAIR CARRIED OUT IAW SRM 51-10- 2 & SRM 51-40-3 2 L 7 3 4F A3WE 2001071100133 20010711 00133 EU 2001 7 11 QXEA0101138 1 20010706 A 3350 POWER SUPPLY GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE O OTHER NR NOT REPORTED 1 NM 09 482US 904 11231 PDX - THE NR 1 GALLEY EXIT LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKS GOOD. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001071100134 20010711 00134 EU 2001 7 11 C2XA01BT111 1 20010615 A 3230 LANDING GEAR AEROSP ATR42 ATR42320 8680930 EU NLG & MLG MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14832 187 IAD---CO3487, CREW REPORTED NO GEAR RETRACTION AFTER TAKEOFF. SUCCEEDED IN RETRACTING GEAR BY RET OVRD PB. AIRCRAFT WA S RELEASED IAW MEL 32-31-01 CONTROL NUMBER 008726. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001071100135 20010711 00135 EU 2001 7 11 C2XA01BT112 1 20010609 A 3350 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN DOOR INOPERATIVE A C2XA K NONE O OTHER NR NOT REPORTED 1 SW 27 14819 156 EWR---CO3333, CREW REPORTED CABIN DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT IA W ATR42 MM 33-51-24, OPS CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001071100136 20010711 00136 SO 2001 7 11 C2XA01BT114 1 20010613 A 2530 RECEPTACLE EMB 145 EMB145LR SO COFFEMAKER ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 16919 145393 GSP---CO4088, CREW REPORTED LEFT HAND COFFEE RECEPTACLE GIVES OFF BURN SMELL. MAINTENANCE PLACED BOTH COFFEEMAKERS ON M EL AND RETURNED THE AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2001071100137 20010711 00137 SO 2001 7 11 C2XA01BT117 1 20010622 A 4920 APU EMB 145 EMB145LR SO APU BAY FAILED A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 13956 145078 BTV---CO4069, CREW REPORTED WHILE TAXING OUT THAT THE APU FAILED AND FILLED THE CABIN WITH SMOKE. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND FOUND FAULTY APU, PLACED APU ON MEL AND RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2001071100138 20010711 00138 EU 2001 7 11 C2XA01BT120 1 20010620 A 5320 S5367121729801 THRESHOLD AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15823 165 YUL--DURING A SCHEDULED 1C INSPECTION, THE PASSENGER DOOR THRESHOLD WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACE D THRESHOLD IAW ATR-42-SRM-51-25-01. 2 H 7 2 4T RT A53EU 2001071100139 20010711 00139 EU 2001 7 11 C2XA01BT125 1 20010705 A 2540 WIRE AEROSP ATR42 ATR42320 8680930 EU LAVATORY CHAFED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 25811 094 EWR---CO2942, CREW REPORTED BURNING SMELL COMING FROM LAV AREA. MAINTENANCE FOUND AND REPAIRED CHAFED WIRE AT LAV OVERH EAD SPEAKER IAW ATR 42 WIRING MANUAL CHAPTER 20. OPS CHECKED GOOD. 2 H 7 2 4T RT A53EU 2001071100140 20010711 00140 EU 2001 7 11 C2XA01BT126 1 20010622 A 3350 3011180A POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU CABIN FAULTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 25811 094 YUL---DURING LINE CHECK ON MODIFICATION LINE IN YUL MAINTENANCE FOUND EMERGENCY EXIT LIGHT UNDER RT EMERGENCY DOOR INOPE RATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT IAW ATR42 MM 33-51-21 RAI 10000-004. OPS CHECK GOOD. 2 H 7 2 4T RT A53EU 2001071100141 20010711 00141 SO 2001 7 11 C2XA01BT127 1 20010702 A 3350 LIGHT EMB 135 EMB135LR SO CABIN INOPERATIVE A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 16525 145403 CLE---CO3946, CREW REPORTED EMERGENCY EXIT ROW LIGHTS 9-11 BURNED OUT. CLE MAINTENANCE REPLACED EMERGENCY LIGHT STRIP A T ROW 9-11 IAW EMB 135 MM 33-50-12. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT TOOO11AT 2001071100142 20010711 00142 SO 2001 7 11 C2XA01CL132 1 20010605 A 3350 7287580501 CONNECTOR EMB 145 EMB145ER SO CABIN LOOSE A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 14933 145018 CLE FLIGHT 3690 THE CREW REPORTED THE 2ND STRIP OF AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE RESECURED THE CONNECTOR OF THE 2ND STRIP OF EMERGENCY LIGHTS. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVIC E. 2 L 7 2 4F RT T00011AT 2001071100143 20010711 00143 EU 2001 7 11 C2XA01CL133 1 20010605 A 3260 D23110000 HARNESS AEROSP ATR42 ATR42320 8680930 EU LT MLG SHORTED A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 97841 280 CLE FLIGHT 3194 THE CREW REPORTED A LEFT MAIN GEAR UNSAFE LIGHT ALONG WITH A HOT BRAKE LIGHT ON THE LEFT GEAR AFTER TAKE OFF. THE AIRCRAFT DID A AIR RETURN AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN GEAR UPPER EXTERNAL PROXIMITY SENSOR HARNESS. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A53EU 2001071100144 20010711 00144 WP 2001 7 11 DHL2001803502 1 20010701 A 5320 ANGLE DOUG DC8 DC873 302199C WP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CK; FWD CARGO COMPT.- RH SHROUD ANGLE WITH 1/2" CRACK ON DOOR. REMOVED CRACKED ANGLE IAW SRM 51-1-21 PG 1, CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B, FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-1-21, PG 1. REF. N/R 1362. SDR CL OSED. 2 L 7 4 4F RT 4A25 2001071100145 20010711 00145 WP 2001 7 11 DHL2001803503 1 20010701 A 5712 RIB DOUG DC8 DC873 302199C WP BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CK; LH WING-CLOSING RIB BROKEN ON INBOARD AILERON RH LATERAL PART. REMOVED FASTNERS IAW SRM 51-1-21A, PG 1, CLEANED ,TREATED AND PRIMED AREA IAW SRM 51-1-8B, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-1, PAR. 1, SRM 51-1-21A, PG 1. R EF: N/R 0616. SDR CLOSED. 2 L 7 4 4F RT 4A25 2001071100146 20010711 00146 WP 2001 7 11 DHL2001803504 1 20010629 A 5320 DOUBLER DOUG DC8 DC873 302199C WP CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CK; COCKPIT- FINGER DOUBLER SHOWS CORROSION STA. 8.000 THRU STA. 20.000, LBL 60, L-22L. REMOVED FASTNERS IAW SRM 51 -1-21, PG 7, REMOVED CORROSION AT FINGER DOUBLER IAW SRM 51-1-8, PG 17-18, FOUND OUT OF LIMITS IAW SRM 53-2-0, PG 2, CLE ANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, FABRICATED AND INSTALLED NEW FILLER AND DOUBLER AND FASTNERS IAW SRM 53-2- 0. REF: N/R 1814. SDR CLOSED. 2 L 7 4 4F RT 4A25 2001071100147 20010711 00147 WP 2001 7 11 DHL2001803505 1 20010628 A 5230 DOOR DOUG DC8 DC873 302199C WP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CK; FWD CARGO COMPT.-AFT DOOR FWD UPPER CORNER CRACKED 1/4" AT STA. 520.000. CUTOUT DAMAGED AREA IAW SRM 53-2-0, FI G 20, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 53-2-0, FIG 2 0, PG 141 & SRM 51-1-21 PG 1. REF: N/R 1397. SDR CLOSED. 2 L 7 4 4F RT 4A25 2001071100148 20010711 00148 WP 2001 7 11 DHL2001803506 1 20010630 A 5511 COVER DOUG DC8 DC873 302199C WP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CK; RH HORIZONTAL STAB. CLOSING REAR SPAR COVER SHOWS 2", 1 1/2",2" AND 1" CRACKS FROM STA. XRS 179 TO XRS 221. REM OVED DAMAGED COVER IAW SRM 55-2-0 FIG 6, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, INSTALLED NEW COVER IAW SRM 55 -2-0 FIG 6. REF: N/R 1688. SDR CLOSED. 2 L 7 4 4F RT 4A25 2001071100149 20010711 00149 WP 2001 7 11 DHL2001803523 1 20010625 A 5347 52772660 SEAT TRACK DOUG DC8 DC873 302199C WP MAIN CARGO WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 MAIN CARGO COMPT - LUGS WORN ON L/H # 1 TRACK AT STA 1570-1710.CUR OUT DAMAGED TRACK AT MAIN CARGO COMPT, STA 1530.000 - 1710.000 PER SRM 53-2-3 PG 1&2.CLEANED , TREATED AND PRIMED AREA PER SRN 51-1-8B.INSTALLED NEW TRACK PER SRM 53-2-3 PG 1 & 2 2 L 7 4 4F RT 4A25 2001071100150 20010711 00150 CE 2001 7 11 C2XA01CL134 1 20010606 A 3230 1143810441 SAFETY SWITCH BEECH 1900 1900D 1154162 CE RT MLG FAULTY A C2XA K NONE J WARNING INDICATION CL CLIMB 1 SW 27 87552 UE216 CLE FLT 3032 THE CREW REPORTED LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED RIGHT MAIN LANDING GEAR SAFETY SWITCH, OPERATIONAL CHECKS WERE GOOD. AIRCRAFT W AS TEST FLOWN AND NO DISCREPANCY WAS NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT A24CE 2001071100151 20010711 00151 SO 2001 7 11 C2XA01CL135 1 20010606 A 3350 1317 LIGHT EMB 145 EMB145ER SO CABIN INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 14939 145030 CLE FLT 3680 THE CREW REPORTED EMERGENCY LIGHT ABOVE ROW 11 AND 12 NOT ILLUMINATING ON TEST. MAINTENANCE REPLACED LAMP . OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RELEASED TO SERVICE. 2 L 7 2 4F RT T00011AT 2001071100152 20010711 00152 EA 2001 7 11 COMA0160453 1 20010709 A 2750 853D10011 ACTUATOR CNDAIR CL600 CL6002B19 EA JAMMED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 805CA 3265 7354 FLAPS FAILED AT 16 DEGREES.REPLACED THE L/H #3 FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2001071100153 20010711 00153 SO 2001 7 11 C2XA01CL136 1 20010606 A 2611 M83726316002P RELAY EMB 135 EMB135ER 3260203 SO SMOKE DETECTION FAILED A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 12519 145366 CLE FLT 3369 THE CREW REPORTED WARNING ANNUNCIATOR DOES NOT ILLUMINATE FOR BAGGAGE SMOKE DURING FIRE TEST. MAINTENANCE REMOVED AND REPLACED BAGGAGE SMOKE DETECTOR TEST RELAY. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT WAS RELEASED TO SERV ICE. 2 L 7 2 4F RT T00011AT 2001071100154 20010711 00154 SO 2001 7 11 C2XA01CL137 1 20010611 A 3260 355022002 CONTROL UNIT EMB 145 EMB145LR SO COCKPIT FAILED A C2XA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 27 13968 7807 7807 145138 BTV DURING OPERATIONAL CHECK OF LANDING GEAR WARNING SYSTEM THE RIGHT DOWN INDICATOR DID NOT SHOW DOWN AND LOCKED. MAI NTENANCE REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVIC E. 2 L 7 2 4T RT T00011AT 2001071100155 20010711 00155 SO 2001 7 11 C2XA01CL138 1 20010611 A 2612 3601133500230 FIRE LOOP EMB 145 EMB145ER SO NR 2 ENGINE FAULTY A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 15941 145035 BDL FLT 4122 THE CREW REPORTED NR 2 ENGINE FIRE DETECTION FAILED TEST. MAINTENANCE REPLACED NR 2 ENGINE FIRE DETECTION LOOP. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001071100156 20010711 00156 WP 2001 7 11 CALA0100521 1 20010530 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND EXTERNAL FUSELAGE SKIN CREASED AT FS 230 BETWEEN LONGERON 17L AND 18L. THE SKIN WAS REPAIRED IAW ECRA 5330-02445. 2 L 7 2 4F A6WE 2001071100157 20010711 00157 WP 2001 7 11 CALA0100534 1 20010606 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND CUSP ANGLE CORRODED AT FS 200, RBL 54. THE R-1 DOOR, FRAME FITTING, AND CUSP ANGLE WERE REMOVED IAW MM 52-41-00, SRM 51-30-05, AND 53-05, FIGURE 55. A NEW ANGLE AND REPAIR SPLICE ANGLES WERE INSTALLED IAW SRM 51-30-01. T HE R-1 DOOR WAS REINSTALLED IAW MM 52-41-00. 2 L 7 2 4F A6WE 2001071100158 20010711 00158 NM 2001 7 11 CALA0100535 1 20010525 A 5314 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70330 23460 INSPECTION FOUND A 0.045 INCH CRACK AT HOLE OF KEEL BEAM RT LOWER CHORD, STA 682, RBL 8 (WHEEL WELL AREA). THE CRACKED AREA WAS REMOVED, A FREEZE PLUG AND REPAIR STRAP WAS INSTALLED IAW ECRA 5310-04144. 2 L 7 2 4F RT A16WE 2001071100159 20010711 00159 WP 2001 7 11 CALA0100536 1 20010607 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND FORWARD CARGO DOOR FORWARD JAMB UPPER WEB CORRODED. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IA W SRM 51-30-2, 51-10-4, AND 51-30-5. 2 L 7 2 4F A6WE 2001071100160 20010711 00160 NM 2001 7 11 CALA0100644 1 20010709 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 917 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14358 23943 INSPECTION FOUND EXTERIOR FUSELAGE SKIN DENTED AT STA 917, S19L. A DOUBLER WAS INSTALLED IAW SRM 53-00-01. 2 L 7 2 4F RT A16WE 2001071100161 20010711 00161 NM 2001 7 11 CALA0100645 1 20010710 A 5320 ANGLE BOEING 737 7373T0 1384582 NM BS 270 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14358 23943 INSPECTION FOUND COCKPIT FLOOR Z-ANGLE CORRODED AT BS 270, LBL 10 TO RBL 10. A REPAIR WAS INSTALLED IAW ECRA 5320-01683. 2 L 7 2 4F RT A16WE 2001071100162 20010711 00162 NM 2001 7 11 CALA0100646 1 20010710 A 5512 SKIN BOEING 737 7373T0 1384582 NM R/H HOR STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14358 23943 INSPECTION FOUND A 1" CRACK IN R/H HORIZONTAL STABILIZER LOWER SKIN FORWARD OF AFT SPAR AT I/B ELEVATOR BALANCE PANEL. T HE SKIN WAS REPAIRED IAW ECRA 5510-01585 AND SRM 55-10-01. 2 L 7 2 4F RT A16WE 2001071100163 20010711 00163 WP 2001 7 11 CALA0100537 1 20010610 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND AFT CARGO PIT TORQUE BOX WEB CORRODED. THE TORQUE BOX WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-5. 2 L 7 2 4F A6WE 2001071100164 20010711 00164 NM 2001 7 11 CALA0100647 1 20010710 A 5230 SKIN BOEING 737 7373T0 1384582 NM FWD CARGO DR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14358 23943 INSPECTION FOUND TWO DENTS IN FORWARD CARGO DOOR EXTERNAL SKIN AT CENTER OF DOOR AND 14" FROM AFT EDGE OF DOOR. A DOUBLE R WAS INSTALLED IAW SRM 52-00-01. 2 L 7 2 4F RT A16WE 2001071100165 20010711 00165 WP 2001 7 11 CALA0100538 1 20010612 A 2560 BATTERY DOUG DC9 DC982 3022082 WP MEGAPHONE DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16887 49116 INSPECTION FOUND AFT CABIN MEGAPHONE INOPERATIVE. THE MEGAPHONE BATTERIES WERE REPLACED AND OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 2001071100166 20010711 00166 WP 2001 7 11 CALA0100539 1 20010612 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND MID CARGO INTERCOSTAL CORRODED AT FS 769-788 BETWEEN LONGERONS 27R AND 28R. PANEL 2214C WAS REMOVED IA W SRM 51-30-01. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-05. PANEL 2214C WAS REINSTALLED IAW SRM 51-30-01. 2 L 7 2 4F A6WE 2001071100167 20010711 00167 WP 2001 7 11 CALA0100540 1 20010612 A 5753 SKIN DOUG DC9 DC982 3022082 WP T/E FLAP DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND LEFT I/B FLAP LOWER SKIN SURFACE DENTED. THE LEFT I/B FLAP PANEL WAS REMOVED AND NEW SKIN WAS INSTALLE D IAW SRM 51-50-14, 51-10-3, 51-50-20, AND 57-52-14. THE PANEL WAS INSTALLED IAW SRM 51-30-1. 2 L 7 2 4F A6WE 2001071100168 20010711 00168 WP 2001 7 11 CALA0100541 1 20010612 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69826 49486 INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT FS 1041-1322. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-05 AND 51-30-01. 2 L 7 2 4F A6WE 2001071100169 20010711 00169 NM 2001 7 11 CALA0100543 1 20010614 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16301 23352 INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 986.5-1006, RBL 17. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51 -10-02. 2 L 7 2 4F RT A16WE 2001071100170 20010711 00170 NM 2001 7 11 CALA0100545 1 20010615 A 5280 BOLT BOEING 737 7373T0 1384582 NM LT MLG DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10323 23374 INSPECTION FOUND BOTH LT LANDING GEAR DOOR TO STABILIZER BEAM BOLTS PITTED AND CRACKED. THE CRACKS WERE .25 INCH LONG. NEW BOLTS, WASHERS, AND NUTS WERE INSTALLED IAW MM 32-00-00. 2 L 7 2 4F RT A16WE 2001071100171 20010711 00171 NM 2001 7 11 CALA0100546 1 20010615 A 5280 BOLT BOEING 737 7373T0 1384582 NM RT MLG DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10323 23374 INSPECTION FOUND BOTH RT LANDING GEAR DOOR TO STABILIZER BEAM BOLTS PITTED AND ONE BOLT HAD A .25 INCH CRACK. NEW BOLTS , WASHERS, AND NUTS WERE INSTALLED IAW MM 32-00-00. 2 L 7 2 4F RT A16WE 2001071100172 20010711 00172 NM 2001 7 11 CALA0100547 1 20010616 A 3397 BR964411 WIRE BOEING 737 737524 1384721 NM CABIN BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69603 27316 INSPECTION FOUND EMERGENCY LIGHT AT ROW 21ABC HAD BROKEN WIRES. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED. 2 L 7 2 4F RT A16WE 2001071100173 20010711 00173 EA 2001 7 11 COMA0160387 1 20010613 A 5320 60034017374 STIFFENER CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 936CA 16506 7043 THE VERTICAL STIFFENER AT RBL 9 IS CRACKED. REMOVED OLD VERTICAL STIFFENER AT RBL 9 AND INSTALLED NEW STIFFENER ALT P/N 600-34017-724 IAW WVAC EO 601R-53-2501. 2 L 7 2 4F RT A21EA 2001071100174 20010711 00174 EA 2001 7 11 COMA0160389 1 20010615 A 5320 601R311719171 ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 945CA 14501 7069 LEFT AND RIGHT FS 484 ANGLES ARE CRACKED. REPAIRED LEFT AND RIGHT FS 484 ANGLES IAW WVAC EO 601R-53-2507. 2 L 7 2 4F RT A21EA 2001071100175 20010711 00175 EA 2001 7 11 COMA0160390 1 20010614 A 5753 601R1430342 VANE CNDAIR CL600 CL6002B19 EA T/E FLAP CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 945CA 14501 7069 RT INBOARD FLAP VANE CHAFED BEYOND LIMITS. REPAIRED RIGHT INBOARD FLAP VANE IAW AERODESIGN REPORT 1286. 2 L 7 2 4F RT A21EA 2001071100176 20010711 00176 NM 2001 7 11 VNAA0105004 1 20010508 A 3240 METERING VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT BRAKE FAILED A VNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 426JS 10584 3038 FLIGHT 4097 WAS TAXIING AND THE FIRST OFFICER'S LEFT HAND BRAKE WAS INEFFECTIVE AND THE CREW RETURNED TO THE GATE. THE AIRCRAFT WAS FERRIED TO PIT WHERE MAINTENANCE INSPECTED AND BLED THE BRAKE METERING UNIT IN ACCORDANCE WITH DORNIER MAIN TENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001071100177 20010711 00177 EA 2001 7 11 COMA0160457 1 20010707 A 2750 852D10011 ACTUATOR CNDAIR CL600 CL6002B19 EA BINDING A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 983CA 9326 7169 FLAP FAIL CAUTION MESSAGE AT 38 DEGREE FLAP POSITION DURING APPROACH INTO CVG.COMPLIED WITH AD 98-20-01 FLAP CAUTION MES SAGE "SECOND EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 3(D AND E)4. REPLACED INBOARD FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2001071100178 20010711 00178 NM 2001 7 11 C1HA200181004 1 20010601 A 3260 CONNECTOR BOEING 727 7272S7 138407Z NM RT MLG DOOR LOOSE A C1HA O OTHER N FALSE WARNING CL CLIMB 1 GL 15 681CA 22020 ON DEPARTURE PASSING 12K FT RIGHT MLG DOOR LIGHT CAME ON. POSITION GEAR HANDLE TO UP AND LIGHT WENT OUT POSITION GEAR H ANDLE TO OFF LIGHT CAME ON AGAIN CONTINUED FLIGHT WITH GEAR HANDLE IN UP POSITION. FOUND RIGHT GEAR DOOR INDICATION CAN NON PLUG HALF OFF. RESECURED SAME, PINNED ALL GEAR AND OPS CHECKED GEAR DOOR CHECKS NORMAL. REMOVED GEAR PINS, OK FOR SERVICE. 2 L 7 3 4F A3WE 2001071100179 20010711 00179 2001 7 11 C1HA200182008 4 20010601 A 2565 SLIDE BOEING 727 7272S7 138407Z NM L1 DOOR OUT OF POSITION A C1HA K NONE O OTHER NR NOT REPORTED 1 GL 15 682CA 22019 L-1 DOOR ESCAPE SLIDE FALLS OUT OF DOOR HOLDER. INSPECTED AND REINSTALLED, CKS GOOD. 2 L 7 3 4F A3WE 2001071100180 20010711 00180 NE 2001 7 11 C1HA200183003 2 20010615 A 7261 OIL FILTER BOEING 727 7272S7 138407Z NM PWA JT8 JT8D17 52049 NE NR 3 ENGINE DIRTY A C1HA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 683CA 22490 AFTER ENGINE START NR 3 ENGINE LOW OIL PRESS/FILTER BYPASS LIGHT ILLUMINATED. REMOVED AND REPLACED MAIN OIL FILTER, RAN ENG, LEAK AND OPS CHECK GOOD. 2 L 7 3 4F 4 F A3WE E2EA 2001071100181 20010711 00181 EA 2001 7 11 COMA0160459 1 20010705 A 2750 853D10013 ACTUATOR CNDAIR CL600 CL6002B19 EA BINDING A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 984CA 13128 1962 7171 FLAPS FAILED AT 8 DEGREES.REPLACED THE LEFT HAND #3 FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2001071100182 20010711 00182 EA 2001 7 11 COMA0160460 1 20010707 A 2750 853D10012 ACTUATOR CNDAIR CL600 CL6002B19 EA JAMMED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 710CA 6936 7241 FLAP FAIL CAUTION APPROACH INTO CVG.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "SECOND EVENT" MAINTENANCE ACTION, PA RAGRAPH (B) 3(D AND E) 4. REPLACED THE INBOARD FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2001071100183 20010711 00183 NM 2001 7 11 AALA20010620 1 20010323 A 3350 LIG5714 LIGHT BOEING 727 727223 1384074 NM AIRSTAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 888AA 21373 TUL - FOUND AFT AIRSTAIRS EMERGENCY EXIT LIGHT INOPERATIVE. INSTALLED SERVICEABLE EMERGENCY EXIT LIGHT ASSEMBLY PER MM 33-50-061-4 PAGE 401, OPS CHECK OK. (M) 2 L 7 3 4F A3WE 2001071100184 20010711 00184 EA 2001 7 11 COMA0160461 1 20010707 A 2750 853D10012 ACTUATOR CNDAIR CL600 CL6002B19 EA JAMMED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 710CA 6936 7241 FLAP FAIL CAUTION DURING APPROACH INTO CVG.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "SECOND EVENT" MAINTENANCE ACT ION, PARAGRAPH (B) 3 (D AND E)4. REPLACED THE OUTBOARD FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2001071100185 20010711 00185 NM 2001 7 11 AALA20011013 1 20010503 A 3350 LIG5714 LIGHT BOEING 727 727227 1384078 NM AIRSTAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 719AA 20612 TUL - FOUND LIGHT INOPERATIVE, EMERGENCY AFT STAIR OVERHEAD. INSTALLED SERVICEABLE LIGHT ASSEMBLY. OPS CHECK OK. (M) 2 L 7 3 4F A3WE 2001071100186 20010711 00186 NM 2001 7 11 AALA20011015 1 20010507 A 3350 1001141 LIGHT BOEING 727 727227 1384078 NM AIRSTAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 718AA 20611 TUL - FOUND EMERGENCY EXIT SPOT LIGHT OVER AFT STAIRS INOPERATIVE. REMOVED AND REPLACED ON E-58 3878760, OPS CHECKED GO OD. (M) 2 L 7 3 4F A3WE 2001071100187 20010711 00187 NM 2001 7 11 AALA20011121 1 20010522 A 3350 900542 CHARGER BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 707AA 22464 DFW - DURING OVERNIGHT MAINTENANCE, LEFT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY CHARGER SYSTEM FOR LEFT OVERWING EMERGENCY EXIT LIGHT. (M) 2 L 7 3 4F A3WE 2001071100188 20010711 00188 EA 2001 7 11 COMA0160462 1 20010710 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA WORN A COMA O OTHER S AFFECT SYSTEMS CL CLIMB 1 SO 01 941CA 9249 7050 FLAP CAUTION MESSAGE DURING APPROACH INTO CVG, AN EMERGENCY WAS DECLARED, AIRCRAFT LANDED SAFETLY.COMPLIED WITH AD 98-20 -01 FLAP CAUTION MESSAGE "SECOND EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 3 (D AND E)4. REPLACED THE RIGHT BRAKE POSITI ONING SENSING UNIT. 2 L 7 2 4F RT A21EA 2001071100189 20010711 00189 NM 2001 7 11 AALA20011143 1 20010528 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 879AA 21391 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT STRIP. SYSTEM GROU ND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071100190 20010711 00190 NM 2001 7 11 AALA20011248 1 20010613 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN MALFUNCTIONED A AALA K NONE O OTHER TO TAKEOFF 1 SW 21 676AN 29426 SJU - FLT 1888 - EN ROUTE SJU-BDL, ON TAKEOFF, ROLL EMERGENCY EXIT LIGHT ILLUMINATED IN CABIN. LIGHTS TURNED OFF AFTER TAKEOFF. LANDED BDL WITHOUT FURTHER INCIDENT. INSPECTED EMERGENCY EXIT LIGHT SYSTEM. NO DEFECTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001071100191 20010711 00191 NM 2001 7 11 AALA20011252 1 20010614 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN DEFECTIVE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 867AA 21372 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD CABIN EMERGENCY EXIT LIGHT DIM. REPLACED EMERGENCY EXIT LIGHT JUMPER WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071100192 20010711 00192 NM 2001 7 11 AALA20011253 1 20010615 A 3350 1001191 LIGHT BOEING 727 727223 1384074 NM R1 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 861AA 21088 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT R1 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071100193 20010711 00193 NM 2001 7 11 AALA20011255 1 20010615 A 3350 1001191 LIGHT BOEING 727 727227 1384078 NM VENTRAL STAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 721AA 20729 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT VENTRAL STAIRS INOPERATIVE. REPLACED EMERGENCY EXIT LIG HT ASSEMBLY AT AFT VENTRAL STAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071100195 20010711 00195 NM 2001 7 11 AALA20011258 1 20010616 A 3350 1001191 LIGHT BOEING 727 727223 1384074 NM VENTRAL STAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 877AA 21389 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT VENTRAL STAIRS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT A SSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071100196 20010711 00196 NM 2001 7 11 AALA20011263 1 20010618 A 3350 1001191 LIGHT BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 384AA 26996 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 2B BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT S EAT 2B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001071100197 20010711 00197 WP 2001 7 11 AALA20011268 1 20010612 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 TUL - FOUND FLOOR WEB CORRODED AT STATION 197 RBL 41. REPLACED FLOOR WEB PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2001071100198 20010711 00198 NM 2001 7 11 AALA20011272 1 20010619 A 3610 VALVE BOEING 757 757223 1384957 NM BLEED AIR SYS FAILED A AALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 687AA 25695 LAX - FLT 161 - LEFT HIGH STAGE VALVE CAME ON DURING TAKEOFF. PLACARDED HIGH STAGE VALVE, INOPERATIVE PER MEL. TROUBLE SHOT PER MM 36-00-99-1 FIG 101. REPAIRED/REPLACED PER FINDINGS. (M) 2 L 7 2 4F RT A2NM 2001071200001 20010712 00001 NM 2001 7 12 AALA20011278 1 20010616 A 2120 SMOKE BOEING 757 757223 1384957 NM CABIN DETECTED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 184AN 29594 FLT 632 - AUA-MIA - FLIGHT ATTENDANT REPORTED SMELL OF ELECTRICAL FUMES AND SMOKE IN CABIN. RETURNED AUA AND LANDED WIT HOUT FURTHER INCIDENT. INSPECTED RECIRCULATION FANS. INSPECTED A/C DISTRIBUTION. INSPECTED MID GALLEY COFFEE MAKERS A ND WIRING. NO DEFECTS NOTED. PRESSURIZED AIRCRAFT. NO SMELL NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001071200002 20010712 00002 NM 2001 7 12 AALA20011286 1 20010624 A 3350 1001141 LIGHT BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 320AA 22321 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 37B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBL Y AT SEAT 37B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001071200003 20010712 00003 NM 2001 7 12 AALA20011287 1 20010624 A 3350 1001141 LIGHT BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 320AA 22321 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 39B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBL Y. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001071200004 20010712 00004 CE 2001 7 12 GUU2001F00001 1 20010326 A 3297 WIRE BEECH 1900 1900C 1154161 CE LANDING GEAR LOOSE A O OTHER J WARNING INDICATION AP APPROACH 1 SO 19 150GA UC150 FLT 9432 - NAS/MIA - DURING APPROACH, LANDING GEAR CIRCUIT BREAKER POPPED. UNABLE TO POWER LANDING GEAR. AFTER RESETTI NG CIRCUIT BREAKER LANDING GEAR CAME DOWN, BUT NO GREEN INDICATOR UNTIL AFTER GEAR RECYCLED. SECURED LINE GOING TO BLEE D VALVE. ALSO SECURED LOOSE WIRE GOING TO LANDING GEAR WARNING CIRCUIT BREAKER. PERFORMED LANDING GEAR EXTENSION AND R ETRACTION. CIRCUIT BREAKER DID NOT TRIP. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4T RT A24CE 2001071200005 20010712 00005 EU 2001 7 12 SIMA20010591 1 20010228 A 3397 WIRE AEROSP ATR42 ATR42300 8680920 EU PAX DOOR BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 21 269AT 269 MCO - MAINTENANCE REPORTED PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT DOOR STEP. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001071200006 20010712 00006 EU 2001 7 12 SIMA20010741 1 20010315 A 2611 SMOKE WARNING SAAB SF340 340B 7860101 EU COCKPIT FALSE INDICATION A SIMA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 21 376AE 340B376 TYR - FLT 3712 - FOUND CREW REPORTED AVIONIC SMOKE LIGHT ON CWP. PUT ON MEL. MAINTENANCE COULD NOT DUPLICATE DISCREPAN CY. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001071200007 20010712 00007 EU 2001 7 12 SIMA20010803 1 20010321 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 259AE 340B259 BDL - FLT 5018 - FLIGHT ATTENDANT REPORTS CABIN EMS LIGHTS DO NOT REMAIN ON WHEN TESTED. REMOVED AND REPLACED CABIN EMS POWER SUPPLY 24LN IAW AMM. OPS CHECK NORMAL AT THIS TIME. (M) 2 L 7 2 4T RT A52EU 2001071200008 20010712 00008 EU 2001 7 12 SIMA20010873 1 20010328 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 548AT 548 DFW - DURING SCHEDULED PS-2 CHECK MAINTENANCE REPORTED SEVERAL EMERGENCY LIGHTS IN CABIN TO BE INOPERATIVE. MAINTENANCE FOUND TWO EMERGENCY LIGHT POWER SUPPLY UNIT BATTERIES TO HAVE LOW VOLTAGE. MAINTENANCE CHANGED ALL FOUR BATTERIES. OP ERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001071200009 20010712 00009 EU 2001 7 12 SIMA20010882 1 20010329 A 3350 LIGHT AEROSP ATR72 ATR72212 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 322AC 0320 MIA - FLT 5409 - FOUND EMERGENCY FLOOR LAMP AFT OF GALLEY INOPERATIVE, MEL PER 33-30. (M) 2 H 7 2 4T RT A53EU 2001071200010 20010712 00010 SO 2001 7 12 SIMA20010931 1 20010403 A 2611 SMOKE DETECTOR EMB 135 EMB135LR SO LAVATORY ACTIVATED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 723AE 145288 CMH - FLT 4975 - LAVATORY SMOKE INDICATION CAME ON DURING TRANSITION FROM APU BLEED TO ENGINE BLEED. POSSIBLE ENGINE OI L LEAK. (M) 2 L 7 2 4F RT TOOO11AT 2001071200011 20010712 00011 EU 2001 7 12 SIMA20010951 1 20010405 A 3150 WARNING LIGHT SAAB SF340 340B 7860101 EU COCKPIT ILLUMINATED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 338AE 340B338 CLE - FLT 5074 - CREW ABORTED TAKEOFF DUE TO CONFIGURATION LIGHT COMING ON. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY . OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001071200012 20010712 00012 SO 2001 7 12 SIMA20011079 1 20010417 A 2510 SMOKE EMB 135 EMB135LR SO COCKPIT DETECTED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 21 732DH 145358 LGA - FLT 4521 - DURING INITIAL POWER UP ON AIRCRAFT WITH BATTERY AND AVIONICS SWITCHES ON, SMOKE WAS OBSERVED POURING O UT OF THE CENTER CONSOLE. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. PERFORMED APU START AND RAN ELECTRICAL SYSTEM A ND FOUND NO EVIDENCE OF SMOKE. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001071200013 20010712 00013 SO 2001 7 12 SIMA200112005 1 20010430 A 3350 7287503507 LIGHT EMB 135 EMB135LR SO CABIN SMOKE A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 704PG 145174 DFW - FLT 3277 - CABIN SMOKE AND FUMES, SHUTDOWN APU. APPEARS TO BE COMING FROM ROW 4 AND 5 ON B AND C. SMOKE DISCOVER ED DURING BOARDING OF PAX. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4F RT TOOO11AT 2001071200014 20010712 00014 SO 2001 7 12 SIMA20011272 1 20010507 A 3350 1317 LIGHT EMB 145 EMB145LR SO CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 601GH 145046 DFW - DURING SCHEDULED PS-2 CHECK, MAINTENANCE REPORTED THE LEFT WING EMERGENCY EXIT LIGHT TO BE INOPERATIVE. MAINTENAN CE REPLACED THE BULB FOR THE LEFT WING EMERGENCY EXIT LIGHT. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SE RVICE. (M) 2 L 7 2 4T RT T00011AT 2001071200015 20010712 00015 SO 2001 7 12 SIMA20011284 1 20010508 A 3350 STUD EMB 135 EMB135LR SO CABIN LOOSE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 716AE 145264 YYZ - FLT 4754 - FLOOR EMERGENCY LIGHTS OUT ROW 1 THROUGH 6. MAINTENANCE FOUND LOOSE GROUND STUD GS508. MAINTENANCE TI GHTENED STUD PER EMB WIRING MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001071200016 20010712 00016 EU 2001 7 12 SIMA20011294 1 20010509 A 3350 LIGHT AEROSP ATR72 ATR72212A 8680902 EU CABIN MALFUNCTIONED A SIMA K NONE O OTHER NR NOT REPORTED 1 SW 21 550LL 550 DFW - FLT 3709 - CREW REPORTED MULTIPLE FLOOR PROXIMITY LIGHTS INOPERATIVE IN FORWARD CABIN. MAINTENANCE COULD NOT DUPL ICATE DISCREPANCY. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001071200017 20010712 00017 EU 2001 7 12 SIMA200113110 1 20010510 A 2520 D1121F10337 SEAT SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 280AE 340B280 SBP - DURING MBV INSPECTION, MAINTENANCE FOUND THE PASSENGER SEAT 5A REAR TUBE IS CORRODED. REMOVED AND REPLACED SEAT A SSEMBLY IAW SAAB AMM 25-20-00. (M) 2 L 7 2 4T RT A52EU 2001071200018 20010712 00018 EU 2001 7 12 SIMA200113113 1 20010510 A 5743 7257500067 LINK SAAB SF340 340B 7860101 EU LT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 280AE 340B280 SBP - DURING MBV MAINTENANCE, FOUND THE LEFT MAIN LANDING GEAR OUTBOARD CONNECTING LINK AFT HOLE FOR ATTACH FITTING IS C ORRODED. REMOVED AND REPLACED CONNECTING LINK ASSEMBLY IAW SAAB AMM 57-40-05. (M) 2 L 7 2 4T RT A52EU 2001071200019 20010712 00019 EU 2001 7 12 SIMA200113114 1 20010510 A 5743 7257500067 LINK SAAB SF340 340B 7860101 EU RT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 280AE 340B280 SBP - DURING MBV MAINTENANCE, FOUND THE RIGHT MLG INBOARD CONNECTING LINK AFT HOLE FOR ATTACH FITTING IS CORRODED. REMO VED AND REPLACED CONNECTING LINK ASSEMBLY IAW SAAB AMM 57-40-05. (M) 2 L 7 2 4T RT A52EU 2001071200020 20010712 00020 EU 2001 7 12 SIMA20011322 1 20010512 A 3234 F966A0102 CONTROL HANDLE AEROSP ATR72 ATR72212A 8680902 EU COCKPIT FAULTY A SIMA K NONE N FALSE WARNING CR CRUISE 1 SW 21 536AT 536 DFW - FLT 3660 - CREW REPORTED THE RIGHT MAIN LANDING GEAR HAS AN UNLOCK INDICATION ON OVERHEAD PANEL. ALSO, NOTED GREE N SYSTEM HYDRAULIC SYSTEM HAD FLUCTUATING PRESSURE. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER IAW ATR MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001071200021 20010712 00021 EU 2001 7 12 SIMA20011332 1 20010513 A 3230 SPLICE AEROSP ATR72 ATR72212A 8680902 EU RT MLG LOOSE A SIMA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 536AT 536 DFW - FLT 3405 - CREW REPORTED THE RIGHT MAIN GEAR CYCLES IN FLIGHT AFTER RETRACTION. AIRCRAFT WAS RETURNED TO DFW. MA INTENANCE INSPECTED AND FOUND A SPLICE CONNECTOR IN WIRE 5000VS LOOSE. WIRE WAS REPAIRED IAW ATR AWM 20-43-12. OPS CHE CK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001071200022 20010712 00022 SO 2001 7 12 SIMA20011392 1 20010519 A 3350 BATTERY EMB 135 EMB135LR SO CABIN DISCONNECTED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 718AE 145275 CLE - FLT 4462 - FIRST HALF OF FLOOR EMERGENCY LIGHTS DO NOT ILLUMINATE. MAINTENANCE INSPECTED EMERGENCY LIGHTING SYSTE M AND FOUND BATTERY NR 2 IN GALLEY NOT CONNECTED, BATTERY WAS RECONNECTED. OPERATIONAL CHECK WAS GOOD IAW AMM 33-50-00 AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001071200023 20010712 00023 EU 2001 7 12 SIMA20011393 1 20010519 A 6120 8163323201 CONTROL UNIT AEROSP ATR72 ATR72212A 8680902 EU RT PROP FAULTY A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 545AT 545 DFW - FLT 3503 - WHILE IN CILMB-OUT FROM DFW, THE NR 2 PROPELLER SINGLE CHANNEL PE FAULT LIGHT ILLUMINATED WITH AN ASSOC IATED TORQUE SURGE. THE AIRCRAFT WAS RETURNED TO DFW DUE TO CONTINUOUS SURGING FROM THE PROPELLER. THE AIRCRAFT WAS RE TURNED WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE PROPELLER ELECTRONIC CONTROL AND THE EN GINE ELECTRONIC CONTROL IAW ATR MM. OPS CHECK WAS GOOD AND AIRCRAFT WS RELEASED FOR A FUNCTIONAL CHECK FLIGHT. FCF WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001071200024 20010712 00024 2001 7 12 SIMA20011397 4 20010519 A 3418 0861DTS VANE EMB 135 EMB135LR SO STALL WARNING FAULTY A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 737MW 145396 GSO - FLT 4020 - DURING CLIMB, CREW REPORTED THE SPS 1 FAIL INTERMITTENTLY. CREW THEN RECEIVED AN SPS ADVANCE MESSAGE A ND AT THAT POINT BOTH FAIL MESSAGES STAYED ON. CREW FOLLOWED AOM PROCEDURES AND RETURNED TO FIELD. EMERGENCY WAS DECLA RED AND AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED THE AOA VANE AND THE STALL PROT ECTION COMPUTER IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001071200025 20010712 00025 SO 2001 7 12 SIMA20011406 1 20010520 A 3040 ANTI-ICE SYSTEM EMB 135 EMB135LR SO COCKPIT MALFUNCTIONED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 706AE 145194 PWM - FLT 4482 - DURING TAKEOFF, THE NR 1 WINDSHIELD FAULT LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AND AIRCRAFT WAS RETU RNED TO THE GATE. PUT ON MEL AT THIS TIME. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPS CHECK WS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001071200026 20010712 00026 EU 2001 7 12 SIMA20011411 1 20010521 A 5610 7256100502 WINDSHIELD SAAB SF340 340B 7860101 EU COCKPIT CRACKED A SIMA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 266AE 340B266 SMX - FLT 3146 - CREW REPORTED DURING CRUISE FLIGHT, THE FIRST OFFICERS WINDSHIELD SHATTERED. AIRCRAFT WAS DIVERTED TO SMX. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRA FT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001071200027 20010712 00027 SO 2001 7 12 SIMA20011415 1 20010521 A 3412 102AU1AF PROBE EMB 145 EMB145LR SO NR 2 INOPERATIVE A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 645AE 145212 ORD - FLT 4003 - DURING CRUISE FLIGHT, THE RIGHT TAT HEAT FAILED. THE FLT WAS RETURNED TO ORD. MAINTENANCE REMOVED AND REPLACED THE NR 2 TAT PROBE IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001071200028 20010712 00028 SO 2001 7 12 SIMA20011417 1 20010521 A 3350 20131A BATTERY EMB 135 EMB135LR SO CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 705AE 145185 CREW REPORTED SEVERAL EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY UNIT BATTERY. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001071200029 20010712 00029 EU 2001 7 12 SIMA20011422 1 20010522 A 3060 8174432 LEAD SAAB SF340 340B 7860101 EU RT PROPELLER BROKEN A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 356AE 340B356 ALB - FLT 4919 - RIGHT PROPELLER DE-ICE BLUE LIGHT EXTINGUISHED WITH SWITCH ON FOLLOWED BY MASTER CAUTION ICE PROTECTION LIGHT ON CWP. MAINTENANCE REPLACED BROKEN PROPELLER DE-ICE LEAD ON NR 4 BLADE IAW HS MM 61-00-00. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001071200030 20010712 00030 SO 2001 7 12 SIMA20011428 1 20010522 A 2910 HYDRAULIC SYSTEM EMB 135 EMB135LR SO NR 1 LACK OF LUBE A SIMA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 736DT 145388 RIC - FLT 4944 - CREW REPORTED THE NR 1 HYDRAULICS SYSTEM LOW LIGHT CAME ON FOLLOWED BY A NR 1 ENGINE HYDRAULIC SYSTEM F AILURE. SYSTEM PRESSURE DROPPED TO ZERO AND WAS REGAINED UPON LANDING GEAR EXTENSION. MAINTENANCE SERVICED THE NR 1 HY DRAULIC SYSTEM IAW EMB MM. HYDRAULIC SYSTEM WAS INSPECTED, HYDRAULIC FILTERS WERE INSPECTED. NO DEFECTS WERE FOUND AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001071200031 20010712 00031 NM 2001 7 12 0102275519 1 20010610 A 2760 SPOILER BOEING 757 757251 1384970 NM WING MALFUNCTIONED A NWAA K NONE F FLT CONT AFFECTED AP APPROACH 1 GL 01 519US 23207 DURING FLIGHT LAS TO LAX TO DTW, CREW REPORTED TWO FLIGHT CONTROL ABNORMALITIES. ON APPROACH TO LAX, CREW REPORTED WITH FLAPS 15, CONTROL WHEEL TURNED TWO DEGREES LEFT WITH DEPLOYMENT OF SPOILERS. MAINTENANCE PERFORMED FUNCTIONAL AND BITE CHECK OF SPOILER SYSTEM WITH NO FAULTS FOUND. FROM LAX TO DTW, CREW REPORTED GREATER THAN NORMAL PULL ON THE YOLK ON R OTATION AT TAKEOFF. DURING APPROACH TO DTW, THE CONTROL WHEEL TURNED TWO DEGREES LEFT WITH FLAPS 15 AND SPOILERS DEPLOY ED. MAINTENANCED PERFORMED FUNCTIONAL CHECK OF SPOILER SYSTEM, NO FAULTS FOUND. 2 L 7 2 4F RT A2NM 2001071200032 20010712 00032 NM 2001 7 12 01FDEA00488 1 20010617 A 3610 BLANKET DOUG MD11 MD11F 3023600 NM RT WING BURNED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 620FE 48791 RT WING LEAD/EDGE PNEU DUCT BLANKET FOUND WITH BURN (CHARRED) MARK, JUST AFT NR 3 ENGINE FIRE BOTTLES. REMOVED AND REPL ACED BLANKET. 2 L 7 3 4F RT A22WE 2001071200033 20010712 00033 NM 2001 7 12 01FDEA00493 1 20010623 A 3260 WARNING SYSTEM BOEING 727 727233 138408A NM COCKPIT MALFUNCTIONED A FDEA O OTHER N FALSE WARNING TO TAKEOFF 1 SO 25 271FE 22036 01-208 AFT T/O RT MLG DOOR ILLUM ON 2ND OFF PANEL ALONG WITH THE RED DOORS WHEN HANDLE PLACED IN OFF POS. AFTER CYCLED GEAR BOTH LIGHTS EXTINGUISHED. UNABLE TO DUPLICATE. REMOVED AND REPLACED MAIN LANDING GEAR DOOR WARNING SWITCH PRECAUT IONARY. OPS CK GOOD PER MM 32-62-011-4. 2 L 7 3 4F RT A3WE 2001071200034 20010712 00034 WP 2001 7 12 01FDEA00494 1 20010625 A 3242 BRAKE DOUG DC10 DC1010F 3022111 WP NR 7 FIRE A FDEA K NONE A FLAME/FIRE TX TAXI/GRND HDL 1 SO 25 383FE 46616 NR 7 BRAKE ON FIRE AT BLOCK-IN. REMOVED AND REPLACED NR 7 BRAKE ASSY AND NR 7 MAIN TIRE REF MM 32-43-01, 32-41-01. 2 L 7 3 4F A22WE 2001071200035 20010712 00035 NM 2001 7 12 01FDEA00495 1 20010626 A 3260 189915 SENSOR BOEING 727 7272S2F 1384O81 NM LT MLG INOPERATIVE A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 212FE 22934 LANDING GEAR FAILED TO RETRACT ON T/O. FOLLOW PREC IN QUICK REF HANDBOOK. LANDING GEAR ALIGNMENT MARKS ALIGNED, HORN W OULD SOUND, BUT THE WING ANTI-ICE GROUND TEST WOULD NOT TEST. GEAR HANDLE WOULD NOT GO PASS THE OFF POS. *S/D* REMOVE D AND REPLACED RELAY R-92 AND LEVER LATCH SOL AND LG ACC UNIT PER MM 32-30-01, 32-09-121 AND AIR SENSING SENSOR PER WDM 32-31-01. 2 L 7 3 4F A3WE 2001071200036 20010712 00036 NM 2001 7 12 01FDEA00497 1 20010626 A 5315 FLOORBEAM BOEING 727 727277 138408S NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 (C53-224-01) CORROSION ON FLOORBEAM AT BS 620, LBL 42, WL 208. *S/D* REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8 FI G 3. 2 L 7 3 4F RT A3WE 2001071200038 20010712 00038 NM 2001 7 12 01FDEA00505 1 20010626 A 2750 CONTROL CABLE DOUG MD11 MD11F 3023600 NM LT FLAP FAIRING DISCONNECTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 616FE 48747 DURING WALKAROUND, FOUND CABLE HANGING FROM LEFT INBD FLAP FAIRING. 2 L 7 3 4F RT A22WE 2001071200039 20010712 00039 WP 2001 7 12 01FDEA00506 1 20010613 A 3230 AYG7332501 TURNBUCKLE DOUG DC10 DC1030F 3023504 WP LANDING GEAR BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 313FE 48311 CENTER LAND GEAR LT DOWNLOCK SPRING TURNBUCKLE BROKEN. REMOVED AND REPLACED TURNBUCKLE PER IAW AMM 32-16-01. FUNCTION TEST PERF IN CONJUNCTION WITH 32C3301, TEST GOOD. 2 L 7 3 4F RT A22WE 2001071200040 20010712 00040 EU 2001 7 12 01FDEA00507 1 20010623 A 2750 548G000001 JACKSCREW AIRBUS 310 A310203 EU T/E FLAP MISINSTALLED A FDEA K NONE F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 SO 25 427FE 362 ON LANDING FLAPS FLAP SHOW JAM ON ECAM AND SFCC COMPUTER FAULTED. THE NR 3 LT SCREWJACK BALLSCREW WAS PUT ON BACKWARD B Y THE OVERHAUL MANUFACTURER. REMOVED AND REPLACED SCREWJACK AND RIGGED FLAPS, RESET LT TORQUE LIMITER. OPS CK NORM. 2 L 7 2 4F RT A35EU 2001071200041 20010712 00041 EU 2001 7 12 01FDEA00508 1 20010627 A 3610 CLAMP AIRBUS 300 A300F4605R 3930327 EU BLEED AIR LOOSE A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 675FE 789 CLIMBING THRU 3000 FT ON NR 2 BLEED LEAK ILLUM WITH ECAM WARN. TIGHTENED LOOSE CLAMP. REMOVED AND REPLACED HOT AIR SUP PLY VALVE PER IAW A300-600 MM 21-62-11. OPS AND LEAK CK GOOD. 2 L 7 2 4F RT A35EU 2001071200042 20010712 00042 NM 2001 7 12 01FDEA00512 1 20010630 A 2751 WARNING LIGHT DOUG MD11 MD11F 3023600 NM COCKPIT ILLUMINATED A FDEA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 SO 25 616FE 48747 TAXI OUT RT OUTBOARD FLAP SHOW AMBER X NO GREEN BOX DURING FLT CONTROL CK FOR RT SPOILER. AFTER FLAP RETRACTION, RT FLA P IND SHOW 0 AND AN AMBER X. 2 L 7 3 4F RT A22WE 2001071200043 20010712 00043 NM 2001 7 12 01FDEA00513 1 20010630 A 3241 WARNING SYSTEM DOUG MD11 MD11F 3023600 NM COCKPIT MALFUNCTIONED A FDEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 25 607FE 48547 ANTI-SKID FAIL ALERT AFT ENGINES START. CYCLE ANTI-SKID CONTROL SYS NR 1 & 2 C/B'S. PER ASCU R-T-S ON ALL IND TEST. A LL TEST PASSED. A/C OK FOR SERVICE. 2 L 7 3 4F RT A22WE 2001071200044 20010712 00044 WP 2001 7 12 01FDEA00514 1 20010625 A 5754 SKIN DOUG DC10 DC1030F 3023504 WP L/E SLAT GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 313FE 48311 SEVERAL GOUGES LT WING LWR MIDDLE SURFACE OF SLATS NR 6, 7, 8. ALSO SEVERAL GOUGES ON UPPER SURFACE OF LT WING AT SLATS NR 6, 7, 8. REPAIRED PER EA 8-5750-56805 AND NR N415 UNDER WO 16747. 2 L 7 3 4F RT A22WE 2001071200045 20010712 00045 WP 2001 7 12 01FDEA00515 1 20010609 A 5320 AGA7088 FLOOR SUPPORT DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 FE 48311 STA 1984, X=2R, Z=-19 LWR SIDE OF FLOOR SUPPORT HAS LEVEL 2 CORROSION AROUND MISSING NUT PLATE. REMOVED AND REPLACED FL OOR SUPPORT PER IAW SRM 51-31-01. 2 L 7 3 4F RT A22WE 2001071200046 20010712 00046 NM 2001 7 12 01FDEA00517 1 20010704 A 2430 ELECTRICAL SYS DOUG MD11 MD11F 3023600 NM COCKPIT MALFUNCTIONED A FDEA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 615FE 48767 DURING CLIMB GOT BUS R EMER OFF LEVEL 1 ALERT. DUMP 65,000 LBS FUEL. DOWN POWERED AND POWERED UP A/C, AC RETURN TO NOR MAL. AS PRECAUTION REPLACED B1-138 R EMER A/C FEED RCCB3 PER MM 24-50-01-4 & EPCU RTS TEST PASSED PER MM 24-08-01-5. 2 L 7 3 4F RT A22WE 2001071200047 20010712 00047 NE 2001 7 12 01FDEA00518 2 20010706 A 7230 COMPRESSOR AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2A5 NE NR 1 ENGINE STALLED A FDEA A UNSCHED LANDING R A PARTIAL RPM/PWR LOSS FLAME/FIRE CL CLIMB 1 SO 25 671FE 778 705252 DURING CLIMBOUT NR 1 ENG HAD 2 COMPRESSOR STALLS WITH FLAMES REPORTED BY TOWER DURING 2ND ONE. 2 L 7 2 4F 4 F RT A35EU E13NE 2001071200048 20010712 00048 NM 2001 7 12 01FDEA00519 1 20010706 A 2910 O-RING DOUG MD11 MD11F 3023600 NM HYD SYSTEM BROKEN A FDEA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 605FE 48514 IN CR HYD 1 OFF ILLUM. REMOVED AND REPLACED BROKEN O-RING PER SMP. LEAK CK OK. 2 L 7 3 4F RT A22WE 2001071200049 20010712 00049 WP 2001 7 12 01FDEA00520 1 20010706 A 3610 MANIFOLD DOUG DC10 DC1010 3022110 WP PNEUMATIC SYS FAILED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 058FE 46705 WHEN APPLYING MAX PWR FOR T/O, RECEIVED NR 2 MANIFOLD FAILURE WITH PNEU MANIFOLD FAILURE ON OVERHEAD PNL. 2 L 7 3 4F A22WE 2001071200050 20010712 00050 EU 2001 7 12 01FDEA00521 1 20010707 A 3411 PITOT LINE AIRBUS 300 A300F4605R 3930327 EU COCKPIT OBSTRUCTED A FDEA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 SO 25 683FE 801 NO AIRSPEED ON T/O ON NR 1 STBY, PFD AND NR 2 STBY PD. FLUSHED CAPT, F/O'S AND STBY PITOT LINES. OPS CK PER MM 34-10-0 0-5, TEST OK. 2 L 7 2 4F RT A35EU 2001071200051 20010712 00051 WP 2001 7 12 ABXA010384 1 20010712 A 3260 7000010101ABX1 SWITCH DOUG DC9 DC932 3022066 WP RT WHEEL WELL DEFECTIVE A ABXA K NONE O OTHER CL CLIMB 1 GL 23 900AX 47380 UPON GEAR RETRACTION, GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. GEAR WAS RECYCLED PER ABNORMALS A ND GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED WITH THE GEAR EXTENDED ALSO. REPLACED THE RIGHT MAIN LANDING GEAR DOOR SWIT CH IAW DC-9 MM 32-60-03-02. 2 L 7 2 4F A6WE 2001071200052 20010712 00052 EA 2001 7 12 2001B4106 1 20010402 A 2731 RIVET VIKING DHAV DHC3 DHC3 2800202 EA PWA PT6 PT6A135 52043 NE ELEVATOR TAB SHEARED E GJRR O OTHER D INFLIGHT SEPARATION CL CLIMB 1 NM 01 50KA 165 221 35097 ALL RIVETS SECURING MASS BALANCE ARM (INSTALLED PER VIKING AIR LTD. ANTIFLUTTER MOD KIT NO VALTOC1136 AND APPROVED PER STC ST01243NY) SHEARED RESULTING IN SEPARATION OF THE SERVO TAB ACTUATION WITH THE MOVEMENT OF THE ELEVATOR CONTROL. PI LOT FELT OSCILLATION IN ELEVATOR CONTROL DURING HIGH POWER SETTINGS DURING TAKEOFF AND CLIMB. CAUSE MAY BE DUE TO HEAVY ARM ASSEMBLY ATTACHED WITH ALUMINUM RIVETS TO SERVO TAB END BLOCK AND VIBRATION BETWEEN TAB AND MASS BALANCE ARM ASSEMB LY. TAB P/N: C3TE13-12 MASS BALANCE P/N: VALTOC1136-12 TAB FILLER BLOCK P/N: VALTOC1136-18. 1 H 7 1 3R 4 T A815 E4EA 2001071200053 20010712 00053 NM 2001 7 12 AALA20011302 1 20010625 A 5100 STIFFENER BOEING 727 727223 1384074 NM FS 244 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 869AA 21374 TUL - FOUND VERTICAL STIFFENER CORRODED OUTBOARD OF NR 2 LEADING EDGE FLAP ACTUATOR AT NR 2 TANK PRESSURE SWITCHES AT WF S 244. REPLACED STIFFENER PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 2001071200054 20010712 00054 NM 2001 7 12 AALA20011292 1 20010620 A 5300 SKIN BOEING 727 727227 1384078 NM E/E COMPT CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AA 20732 TUL - FOUND SKIN CRACKED AT RIVIT HOLE STATION 328 JUST BELOW STRINGER 206. ALSO, FOUND SKIN CRACKED AT TWO RIVITS STA TION 328 JUST BELOW STRINGER 21L. CUT OUT DAMAGED SECTION OF SKIN AND INSTALLED DOUBLER PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 2001071200055 20010712 00055 NM 2001 7 12 AALA20011293 1 20010619 A 5300 STRINGER BOEING 727 727227 1384078 NM FS 675 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AA 20732 TUL - FOUND STRINGER SPLICE AT STATION 675 STRINGER 28R HAS CRACK AND IS BULGED, EMITTING CORROSION. REMOVED CORRODED S PLICE AND 5 INCHES OF STRINGER. FABRICATED AND INSTALLED NEW SPLICE IAW SRM 53-10-3. TREATED AND PRIMED ALL PARTS IAW MM 51-20-0. (M) 2 L 7 3 4F A3WE 2001071200056 20010712 00056 NM 2001 7 12 AALA20011294 1 20010620 A 5310 BULKHEAD BOEING 727 727227 1384078 NM FS 870 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AA 20732 TUL - FOUND CRACK IN WEB BELOW APU LOAD CONTROL VALVE, STATION 870 BULKHEAD 4 INCHES LONG. CRACK IN FS 870 BULKHEAD FOR WARD SIDE AT APU CONTROL VALVE BOTTOM OUTBOARD SIDE OF CUTOUT. REPAIRED PER SRM 53-10-2 WITH DOUBLER. (M) 2 L 7 3 4F A3WE 2001071200057 20010712 00057 NM 2001 7 12 AALA20011296 1 20010620 A 5322 SHEAR TIE BOEING 727 727227 1384078 NM FS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AA 20732 TUL - FOUND SHEAR TIE STATION 720C STRINGER 28 RIGHT CORRODED. REMOVED AND REPLACED SHEAR TIE 51-01 SRM. (M) 2 L 7 3 4F A3WE 2001071200058 20010712 00058 NM 2001 7 12 AALA20011297 1 20010621 A 5322 SHEAR TIE BOEING 727 727227 1384078 NM FS 520 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AA 20732 FOUND FORWARD SIDE OF STATION 520 SHEAR TIE HAS LIGHT CORROSION BETWEEN STRINGER 28 RL. CUT AND REMOVED CORRODED AND CR ACKED FLANGE OF SHEAR TIE. FABRICATED AND INSTALLED REPAIR PART IAW SRM 53-10-4 FIG 5. (M) 2 L 7 3 4F A3WE 2001071200059 20010712 00059 NM 2001 7 12 AALA20011298 1 20010621 A 5300 STRINGER BOEING 727 727227 1384078 NM FS 1130 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AA 20732 TUL - FOUND STRINGER 27R CORRODED AT STATION 1130 INBOARD SIDE. REMOVED DAMAGED STRINGER AND INSTALLED NEW STRINGER SEC TION AND SPLICE PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 2001071200060 20010712 00060 NM 2001 7 12 AALA20011300 1 20010624 A 5100 STRINGER BOEING 727 727227 1384078 NM FS 950C CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AA 20732 TUL - FOUND STRINGER 28R IS CORRODED ON OUTBOARD SIDE. REMOVED CORRODED STRINGER AT STATION 950C PLUS 9,5 INCH AND 950 PLUS 8 INCHES. INSTALLED STRINGER FILLERS SPLICE ANGLES PER ESO 11697 DATED 6-22-2001. (M) 2 L 7 3 4F A3WE 2001071200061 20010712 00061 NM 2001 7 12 AALA20011251 1 20010614 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 306AA 22312 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 19H INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT CONNE CTOR AT SEAT 19H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001071200062 20010712 00062 NM 2001 7 12 AALA20011250 1 20010614 A 3397 WIRE BOEING 767 767223 1385123 NM CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 21 306AA 22312 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 27B INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001071200063 20010712 00063 NM 2001 7 12 AALA20010501 1 20010315 A 3350 LAMP BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 872AA 21384 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT AT ROW 15 AND 20 DIM. REPLACED OVERHEAD EMERGENCY EXI T LIGHT AT ROW 15 AND 20. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200064 20010712 00064 NM 2001 7 12 AALA20010502 1 20010315 A 3350 LAMP BOEING 727 727223 1384074 NM OVERWING INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 872AA 21384 DFW - DURING OVERNIGHT MAINTENANCE, RIGHT SIDE OVERWING EMERGENCY EXIT LIGHT DIM. REPLACED OVERWING EMERGENCY EXIT LIGH T. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200065 20010712 00065 NM 2001 7 12 AALA20010497 1 20010315 A 3350 LAMP BOEING 727 727223 1384074 NM R2 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 880AA 21519 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT AT R2 DOOR DIM. REPLACED EMERGENCY EXIT LIGHT AT R2 DOOR. SYSTE M GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200066 20010712 00066 NM 2001 7 12 AALA20010492 1 20010315 A 3350 BATTERY PACK BOEING 727 727223 1384074 NM L1 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 880AA 21519 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L1 DOOR DIM. REPLACED EMERGENCY EXIT LGIHT BATTERY PACK AND CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200067 20010712 00067 NM 2001 7 12 AALA20010523 1 20010316 A 3350 LAMP BOEING 727 727223 1384074 NM OVERWING INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 893AA 22009 DFW - DURING OVERNIGHT MAINTENANCE, RIGHT SIDE OVERWING EMERGENCY LIGHT DIM. RE-SECURED RIGHT SIDE OVERWING EMERGENCY E XIT LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200068 20010712 00068 NM 2001 7 12 AALA20010521 1 20010316 A 3350 SOCKET BOEING 727 727223 1384074 NM OVERWING INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 893AA 22009 DFW - DURING OVERNIGHT MAINTENANCE, LEFT SIDE OVERWING EMERGENCY LIGHT DIM. RE-SECURED LEFT SIDE OVERWING EMERGENCY EXI T LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200069 20010712 00069 NM 2001 7 12 AALA20010506 1 20010318 A 3350 BATTERY PACK BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 846AA 20987 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT DIM. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT BATTE RY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200070 20010712 00070 NM 2001 7 12 AALA20010567 1 20010320 A 3350 BATTERY PACK BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 879AA 21391 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY EXIT FLOOR PATH LIGHT DIM. CHARGED EMERGENCY EXIT LIGHT BATTERY P ACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200071 20010712 00071 NM 2001 7 12 AALA20010569 1 20010320 A 3350 BATTERY PACK BOEING 727 727223 1384074 NM MID CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 879AA 21391 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT MID CABIN DIM. CHARGED EMERGENCY EXIT LIGHT EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200072 20010712 00072 NM 2001 7 12 AALA20010568 1 20010320 A 3350 BATTERY PACK BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 879AA 21391 DFW - DURING OVERNIGHT MAINTENANCE, AFT EMERGENCY EXIT FLOOR PATH LIGHT DIM. CHARGED EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200073 20010712 00073 NM 2001 7 12 AALA20010599 1 20010323 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 21 881AA 21520 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 20 BROKEN. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT 20. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200074 20010712 00074 NM 2001 7 12 AALA20010577 1 20010322 A 3350 CONNECTOR BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 872AA 21384 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 15 DIM. REPLACED EMERGENCY EXIT LIGHT CONNECTOR. SYSTE M GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200075 20010712 00075 NM 2001 7 12 AALA20010644 1 20010328 A 3350 MODULE BOEING 727 727223 1384074 NM AFT AIRSTAIR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 868AA 21373 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIGN ABOVE AFT AIRSTAIR DIM. REPLACED EMERGENCY EXIT LIGHT MODULE AT AFT AIRSTAIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200076 20010712 00076 NM 2001 7 12 AALA20010643 1 20010328 A 3350 P400051126 MODULE BOEING 727 727223 1384074 NM AFT STAIR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 866AA 21371 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT ENTRY STAIR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200077 20010712 00077 NM 2001 7 12 AALA20010755 1 20010409 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN INOPERATIVE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 889AA 21527 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 6 DIM. REPLACED EMERGENCY EXIT FLOOR PROXIMITY JUMPER W IRE AT ROW 6. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200078 20010712 00078 NM 2001 7 12 AALA20010713 1 20010407 A 3350 CONNECTOR BOEING 727 727223 1384074 NM AFT AIRSTAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 848AA 20989 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT SIGN AT AFT AIRSTAIRS DIM. RE-SECURED EMERGENCY EXIT LIGHT CON NECTOR AT AFT AIRSTAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200079 20010712 00079 NM 2001 7 12 AALA20010785 1 20010228 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN LOOSE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 870AA 21382 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 13D INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT WIRE AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200080 20010712 00080 NM 2001 7 12 AALA20010781 1 20010415 A 3350 CONNECTOR BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 860AA 21087 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT SECTION OF COACH CLASS DIM. REPLACED EMERGENCY EXIT CON NECTOR AT MID SECTION OF COACH CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200081 20010712 00081 NM 2001 7 12 AALA20010806 1 20010418 A 3350 P401001126 MODULE BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 868AA 21373 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT DIM. REPLACED OVERHEAD EMERGENCY OVERHEAD EXIT LIGHT MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200082 20010712 00082 NM 2001 7 12 AALA20010805 1 20010418 A 3350 P4010051126 MODULE BOEING 727 727223 1384074 NM L1 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 868AA 21373 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L1 DOOR DIM. REPLACED EMERGENCY EXIT LIGHT MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200083 20010712 00083 NM 2001 7 12 AALA20010804 1 20010418 A 3350 P4010051126 MODULE BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 868AA 21373 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 8 DIM. REPLACED EMERGENCY EXIT LIGHT MODULE. SYSTEM GR OUND CHECK NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200084 20010712 00084 NM 2001 7 12 AALA20010803 1 20010418 A 3350 WIRE BOEING 727 727200 138407E NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 894AA 22010 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT BETWEN FIRST CLASS AND COACH CLASS BROKEN. REPLACED EMERGENCY EXIT LIGHT WIRE BETWEEN FIRST CLASS AND COACH CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A3WE 2001071200085 20010712 00085 NM 2001 7 12 AALA20010837 1 20010420 A 3350 8039001 BATTERY BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 878AA 21390 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHE CKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200086 20010712 00086 NM 2001 7 12 AALA20010875 1 20010429 A 3350 CONNECTOR BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 844AA 20985 DFW - DURING OVERNIGHT MAINTENANCE, FLOOR PATH EMERGENCY EXIT LIGHT AT COACH CLASS DIM. REPLACED FLOOR PATH EMERGENCY E XIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200087 20010712 00087 NM 2001 7 12 AALA20010878 1 20010429 A 3350 CONNECTOR BOEING 727 727223 1384074 NM AFT AIRSTAIR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 866AA 21371 ATL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIR INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT CONN ECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200088 20010712 00088 NM 2001 7 12 AALA20011246 1 20010613 A 2900 MX2220 PUMP BOEING 727 727223 1384074 NM NR 2 ENGINE LEAKING A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 871AA 21383 MIA-DTW - FLT 926 - SHORTLY AFTER TAKEOFF, DETECTED A HYDRAULIC LOW LEVEL LIGHT ILLUMINATE. RETURNED MIA AND LANDED WIT HOUT INCIDENT. REPLACED NR 2 HYDRAULIC PUMP. LEAK CHECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200089 20010712 00089 CE 2001 7 12 2001F00006 1 20010522 A 3230 24170161 UPLOCK LEAR 55 55LEAR 5170702 CE NLG CORRODED G BQVA K NONE O OTHER IN INSP/MAINT 1 EA 01 57MH 55113 AS PART OF A SCHEDULED INSPECTION BEING PERFORMED, AN EMERGENCY EXTENSION CHECK OF THE LANDING GEAR WAS PERFORMED. NITR OGEN WAS HEARD LEAKING FROM THE LEFT SIDE NOSE WHEEL WELL AREA. FURTHER TROUBLESHOOTING REVEALED THE NOSE LANDING GEAR UPLOCK ACTUATOR (PNEUMATIC) TO BE LEAKING BY THE PISTON SHAFT AREA. CONSIDERABLE CORROSION WAS FOUND INTERNALLY (PISTON SPRING & CYLINDER SHAFT AREA). 2 L 7 2 4F A10CE 2001083000992 20010830 00992 CE 2001 8 30 GLBA2001139 1 20010701 A 5610 10138402518 WINDSHIELD BEECH 1900 1900D 1154162 CE COCKPIT CRACKED A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 01 201YQ UE201 COPILOTS WINDSHIELD CRACKED IN FLIGHT, REPLACE WINDSHIELD 2 L 7 2 4T RT A24CE 2001071200095 20010712 00095 EU 2001 7 12 RAIA00106017 1 20010627 A 3320 EO33601 SOCKET AEROSP ATR72 ATR72202 8680940 EU FAILED A RAIA O OTHER O OTHER LD LANDING 1 CE 03 723TE 283 7400-STL-CREW REPORTED FORWARD AND AFT EMERGENCY LIGHTS FLICKERED ON AND OFF WITH AN ELECTRICAL BURNING SMELL IN THE CAB IN. MAINTENANCE INSPECTED, FOUND DEFECTIVE LIGHT SOCKET AT SEAT 18AB LATERAL LIGHT, CAUSING SMELL. MAINTENANCE DISABLED LIGHTING BALLAST. EMERGENCY LIGHTING WAS NOT EFFECTED. MAINTENANCE DEFERRED LATERAL LIGHT AT 18AB. MAINTENANCE CLEARED M EL AT SEAT 18AB BY REMOVING AND REPLACING THE LIGHT SOCKET. 2 H 7 2 4T RT A53EU 2001071200096 20010712 00096 WP 2001 7 12 ARWA0010602 1 20010603 A 2910 37602655501 SELECTOR VALVE DOUG DC8 DC862 3021970 WP HYD SYSTEM LEAKING A ARWA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 1804 45896 HYDRAULIC PRESS LOST OUT OF SLLP. AILERON AND RUDDER POWER LIGHTS CAME ON, CHECKLISTS WERE COMPLETED AND DIVERTED TO SP IM. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED HYDRAULIC SYSTEM SELECTOR VALVE IAW MM 29-10-18. OPERATION AL CHECKED OK, NO LEAKS NOTED. 2 L 7 4 4F 4A25 2001071200097 20010712 00097 WP 2001 7 12 ARWA0010603 1 20010608 A 3231 510361C LINK ROD DOUG DC8 DC862 3021970 WP NLG DOOR DEFECTIVE A ARWA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 19 1808E 46105 AFTER TAKEOFF OUT OF KMIA AND RAISED THE LANDING GEAR EXPERIENCED HEAVY NOSE VIBRATION. RECYCLED LANDING GEAR, BUT DID NOT HELP. DECLARED EMERGENCY AND LANDED OVERWEIGHT WITH FULL FLAPS. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REP LACED NLG DOOR LT FWD DOOR LINK IAW MM 32-22-1. PERFORMED LANDING GEAR SWING AND FOUND NORMAL IAW MM 32-22-1. PERFORME D SPECIAL STRUCTURAL VISUAL INSPECTION IAW ARROW AIR DC8 MM 5-4-8 PAGE 1-6, NO DEFECTS NOTED. 2 L 7 4 4F 4A25 2001071200098 20010712 00098 NE 2001 7 12 ARWA0010604 2 20010616 A 7200 ENGINE LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B402 54555 NE NR 1 VIBRATION A ARWA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 19 308GB 193U1133 ENGINE NR 1 SUDDEN INCREASE IN VIBRATION FROM 1.8 TO 3.0 UNITS WITH A OR B SELECTED ON NORMAL OR LOW. WARNING LIGHT WAS ON. AIRCRAFT LANDED WITHOUT INCIDENT. ACCOMPLISHED BORESCOPE INSPECTION, NO DEFECTS NOTED. INSPECTED CHIPS AND REMOV ED AND REPLACED OIL FILTERS, ALL CHECKED CLEAN, NO INDICATION OF FAILURE. INSPECTED INLET AND EXHAUST AREAS, NO DEFECTS NOTED. FAN BLADES REMOVED AND CLEANED, ALSO CLEANED DAMPNERS. ALL ABOVE ACCOMPLISHED IAW MM FAULT ISOLATION MANUAL 71 -91-00 PAGE 106 THRU 108. ACCOMPLISHED TEST NR 11 VIBRATION WITHIN MM LIMITS IAW MM 71-00-00 PAGE 217. MAX AVM AT 1.63 T/O EPR WAS .09. 2 L 7 3 4F 4 F A23WE E12EU 2001071200099 20010712 00099 NE 2001 7 12 ARWA0010605 2 20010619 A 7200 ENGINE DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE NR 1 MALFUNCTIONED A ARWA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 19 810BN 45905 DURING TAKEOFF ROLL LOSS POWER ON NR 1 ENGINE. ABORTED TAKEOFF AT 70 KNOTS. REFERRED TO PERFORMANCE MANUAL BRAKE ENERG Y CHART OK TO TAXI. CHECKED ALL TANK CROSSFEED VALVES AND SELECTOR VALVES FOR OPERATION FOUND NORMAL IAW MM 28-22-2,3. INSPECTED FUEL FILTERS AND ALL FUEL SUPPLY LINES FOR DEFECTS, NONE NOTED PER MM 73-10-4. CHECKED SENSE LINES TO FUEL C ONTROL AND FOUND NORMAL IAW MM 73-20-3 AND 73-20. PERFORMED ENGINE RUN UP PER MM 71-00 AND FOUND ALL PARAMETERS WITHIN LIMITS AT ALL POWER SETTINGS. UNABLE TO DUPLICATE POWER LOSS. 2 L 7 4 4F 4 F 4A25 1E8 2001071200103 20010712 00103 WP 2001 7 12 ARWA0010702 1 20010629 A 5311 FRAME LKHEED 1011 1011385115 5265015 WP FUSELAGE CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 307GB 193U1131 DURING SCHEDULE MAINTENANCE, LT ECS COMPARTMENT, STATION 449 BULKHEAD FRAME IS CRACKED ON FWD SIDE BETWEEN STRINGER 41 T O STRINGER 42. STOP DRILLED CRACK, CUT AND TRIMMED REPAIR ANGLES, DRILLED, PRIMED PAINTED AND PREPPED AREA. INSTALLED PARTS AND INSTALLED FASTENERS ALL WORK ACCOMPLISHED IN ACCORDANCE WITH SRM 53-11-00 FIG 833. 2 L 7 3 4F A23WE 2001071200104 20010712 00104 WP 2001 7 12 ARWA0010708 1 20010629 A 5315 FLOORBEAM LKHEED 1011 1011385115 5265015 WP FUSELAGE CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 307GB 193U1131 DURING SCHEDULE MAINTENANCE FWD ENTRY AREA, STA 281 FLOORBEAM, TOP CAP HAS CORROSION FROM APPROX LBL 48 TO RBL 48. REMO VED CORROSION AT FLOORBEAM STA 281 IAW SRM 51-21-01, FOUND OUT OF LIMITS IAW SRM 51-21-01, INSTALLED FLOORBEAM REPAIR IA W SRM 53-21-00 FIG 815. 2 L 7 3 4F A23WE 2001071200105 20010712 00105 WP 2001 7 12 ARWA0010710 1 20010629 A 5315 FLOORBEAM LKHEED 1011 1011385115 5265015 WP FUSELAGE CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 307GB 193U1131 DURING SCHEDULE MAINTENANCE FLOORBEAM FS 281 FROM BL 22L TO BL 22R HAS EVIDENCE OF CORROSION. REMOVED FLOOR TO EVALUATE . REMOVED CORROSION AT FLOORBEAM STA 281 BL 22L TO BL 22R IAW SRM 51-21-01. FOUND OUT OF LIMITS IAW SRM 51-21-01. INS TALLED FLOORBEAM REPAIR IAW SRM 53-21-00 FIG 815. 2 L 7 3 4F A23WE 2001071200106 20010712 00106 WP 2001 7 12 ARWA0010711 1 20010629 A 5320 SUPPORT LKHEED 1011 1011385115 5265015 WP FUSELAGE CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 307GB 193U1131 DURING SCHEDULE MAINTENANCE WALL SUPPORT FS 281 BL 22L HAS CORROSION BEYOND LIMITS. INSTALLED FLOORBEAM REPAIR AT FS 28 1 BL22L IAW SRM 53-21-00 FIG 815. 2 L 7 3 4F A23WE 2001071200107 20010712 00107 WP 2001 7 12 ARWA0010712 1 20010629 A 5315 FLOORBEAM LKHEED 1011 1011385115 5265015 WP FUSELAGE CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 307GB 193U1131 DURING SCHEDULE MAINTENANCE FLOORBEAM AT FS 251 HAS EVIDENCE OF CORROSION. REMOVE TO EVALUATE. REMOVED CORROSION ON FS 251 FLOORBEAM AS PER SRM 51-21-01, FOUND OUT OF LIMITS AS PER 51-21-01. INSTALLED FLOORBEAM REPAIR ON FS 251 IAW SRM 5 3-21-00 FIG 815. 2 L 7 3 4F A23WE 2001071200108 20010712 00108 WP 2001 7 12 ARWA0010713 1 20010629 A 5315 FLOORBEAM LKHEED 1011 1011385115 5265015 WP FUSELAGE CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 307GB 193U1131 DURING SCHEDULE MAINTENANCE FLOORBEAM AT FS 237 HAS EVIDENCE OF CORROSION UNDER MOON COVER. REMOVED TO EVALUATE. REMOV ED CORROSION AT FS 237 IAW SRM 51-21-01 FOUND OUT OF LIMITS IAW SRM 51-21-01. INSTALLED FLOORBEAM REPAIRED IAW SRM 53-2 1-00 FIG 815. 2 L 7 3 4F A23WE 2001081600163 20010816 00163 NE 2001 8 16 ARWA0010715 2 20010703 A 7200 RB211524B402 ENGINE LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B02 54555 NE NR 1 VIBRATION A ARWA E A ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 19 308GB 193U1133 14736 AT TOP OF CLIMB NR 1 ENGINE VIBRATION SPIKED AT 3.0 BOTH CHANNELS IN-FLIGHT SHUT DOWN AND RETURN TO KMIA. AIRCRAFT LAND ED WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ENGINE - PER MM L1011 FORM 7104A, OPS CHECK OK IAW MM L1011 - 7102B; RUN UP IAW MM 71-00-00. 2 L 7 3 4F 4 F A23WE E12EU 2001071200109 20010712 00109 WP 2001 7 12 MWEA011029 1 20010712 A 5310 991224343 FRAME DOUG DC9 DC914 3022034 WP STATION 786 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 AFT CARGO STATION 786 FRAME HAS LIGHT CORROSION ON AFT SIDE AND UNDER BOTTOM LIP BETWEEN LONGERONS 28 LEFT AND 29 RIGHT. -- REMOVED DAMAGED SECTION OF FRAME, LOCATED AND DRILLED NEW SECTION, FABRICATED NEW INTERCOSTAL SPLICE, INSTALLED FR AME SPLICE DOUBLER ANGLE AND FORMER SPLICE STRAPS. 2 L 7 2 4F A6WE 2001071200110 20010712 00110 WP 2001 7 12 MWEA011030 1 20010712 A 5310 991151029 FORMER DOUG DC9 DC914 3022034 WP STATION 120 TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 TOOLING MARKS ON FORMER AFT SIDE BETWEEN LONGERON 28 RIGHT AND 27 RIGHT STATION 120. -- BLENDED TOOLING MARKS, REMOVED DAMAGED FORMER, FORMED NEW FORMER, LOCATED FASTENER HOLES, FABRICATED 2 REPAIR SPLICES, INSTALLED FORMER SECTION. 2 L 7 2 4F A6WE 2001071200111 20010712 00111 WP 2001 7 12 MWEA011031 1 20010712 A 5340 9957871 SEAT TRACK DOUG DC9 DC914 3022034 WP COCKPIT WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FIRST OFFICERS AFT INBOARD SEAT TRACK IS WORN AROUND LOCK PIN HOLES. -- REMOVED DAMAGE, FABRICATED AND INSTALLED REPAI R DOUBLER. 2 L 7 2 4F A6WE 2001071200112 20010712 00112 WP 2001 7 12 MWEA011032 1 20010712 A 5340 9957871 SEAT TRACK DOUG DC9 DC914 3022034 WP COCKPIT WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 CAPTAINS AFT INBOARD SEAT TRACK IS WORN AROUND LOCK PIN HOLES. -- REMOVED DAMAGED FROM SEAT TRACK, FABRICATED AND INST ALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001071200113 20010712 00113 WP 2001 7 12 MWEA011033 1 20010712 A 5340 99578712 SEAT TRACK DOUG DC9 DC914 3022034 WP COCKPIT WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FIRST OFFICERS OUTBOARD SEAT TRACK IS WORN AROUND LOCK PIN HOLES. -- FABRICATED, LOCATED, DRILLED AND INSTALLED NEW SE AT TRACK. 2 L 7 2 4F A6WE 2001071200114 20010712 00114 WP 2001 7 12 MWEA011034 1 20010712 A 5230 591014211 WEB DOUG DC9 DC914 3022034 WP STATION 351 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FORWARD CARGO BAY DOOR JAMB WEB HAS A SHARP DENT AT STATION 351 LONGERON 29 RIGHT. -- REMOVED DOOR JAMB WEB, LOCATED, DRILLED AND INSTALLED NEW WEB. 2 L 7 2 4F A6WE 2001071200115 20010712 00115 WP 2001 7 12 MWEA011035 1 20010712 A 5340 9957871 SEAT TRACK DOUG DC9 DC914 3022034 WP COCKPIT WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 CAPTAINS AFT OUTBOARD SEAT TRACK IS WORN AROUND LOCK PIN HOLES. -- REMOVED DAMAGE FROM SEAT TRACK UPPER CAP SURFACE, F ABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001071200116 20010712 00116 NM 2001 7 12 AAL20011265 1 20010613 A 5330 FRAME BOEING 727 727223 1384074 NM FS 500 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 882AA 21521 TUL - FOUND BELLFRAME DENTED 3 INCHES BY 1 INCH, STATION 500 STRINGER 25R. INSTALLED BELLFRAME REPAIR DOUBLER PER SRM 5 3-10-4. (M) 2 L 7 3 4F A3WE 2001071200117 20010712 00117 NM 2001 7 12 AALA20011269 1 20010609 A 5100 SPAR BOEING 727 727223 1384074 NM FS 625.3 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 881AA 21520 TUL - FOUND CORROSION ON FRONT SPAR AT NR 2 SLAT ACTUATOR CUT OUT LOWER SIDE. FABRICATED STRAP .040-17-7 PH STAINLESS S TEEL. INSTALLED 6 EACH FASTENERS EITHER SIDE OF BLEND AREA WET. INSTALLED PER ESO 11697 DATED 6/07/2001. (M) 2 L 7 3 4F A3WE 2001071200118 20010712 00118 NM 2001 7 12 AALA20011270 1 20010608 A 5500 ELEVATOR BOEING 727 727223 1384074 NM FS 37-47 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 881AA 21520 TUL - FOUND CRACK IN LOWER SKIN OF LEFT ELEVATOR. CUT OUT DAMAGED AREA AND INSTALLED FILLER AND REPAIR DOUBLER PER SRM 55-20-3 PAGE 7. (M) 2 L 7 3 4F A3WE 2001071200119 20010712 00119 EU 2001 7 12 AALA20010517 1 20010317 A 3350 CONNECTOR FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1414D 11377 ORD - DURING OVERNIGHT MAINTENANCE, COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. RE-SECURED COCKPIT EMERGENCY EXIT LIGHT C ONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001071200120 20010712 00120 EU 2001 7 12 AALA20010519 1 20010317 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU L1 DOOR INOPERATIVE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 1432A 11417 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L1 DOOR INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT FLOOR CONNECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001071200121 20010712 00121 EU 2001 7 12 AALA20010855 1 20010425 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 21 1413A 11376 SAT - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED OVERHEAD EMERGENCY EXIT LIGHT W IRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001071200122 20010712 00122 EU 2001 7 12 AALA20010832 1 20010420 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU GALLEY DOOR BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 21 1404D 11355 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT GALLEY DOOR BROKEN. REPAIRED EMERGENCY EXIT LIGHT WIRE AT G ALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001071200123 20010712 00123 EU 2001 7 12 AALA20010801 1 20010417 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU L1 DOOR INOPERATIVE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 1425A 11408 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L1 DOOR INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRES AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001071200124 20010712 00124 NM 2001 7 12 UIEA01062 1 20010626 A 5300 SKIN BOEING 747 747243B 1384830 NM FS 1814 CRACKED A UIEA O OTHER O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 DURING HFEC INSPECTION, FOUND THE LOWER AFT CARGO COMPARTMENT DOOR CUT-OUT, UPPER FORWARD CORNER SKIN CRACKED. CRACK TR IMMED AWAY. FILLER AND REPAIR DOUBLERS FABRICATED AND INSTALLED PER STANDARD PRACTICES IAW SRM 53-30-03 FIG 60, TYPE II . REINSPECTION IS REQUIRED AFTER INSTALLATION OF REPAIR AT 15,000 CYCLES INITIAL AND REPETITIVLY AT 3000 CYCLES THEREAF ER. (M) 2 L 7 4 4F A20WE 2001071200125 20010712 00125 NM 2001 7 12 UIEA01063 1 20010626 A 5310 65B01717515 FRAME BOEING 747 747243B 1384830 NM BS 480 CRACKED A UIEA O OTHER O OTHER IN INSP/MAINT 1 EA 15 516MC 77446 22507 DURING INSPECTION FOUND FRAME STATION 480 CRACKED AT STRINGER 14R COMMON TO THE CUTOUT. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLER AND INSTALLED PER STANDARD PRACTICES IAW SRM 53-10-04. REINSPECTION TO BE ACCOMPLISHED AT 3000 CYCLES A ND REPETITIVE AT 3000 CYCLES UNTIL 747-53-2272 IS INCORPORATED AT THE 20000 CYCLE LIMIT. (M) 2 L 7 4 4F A20WE 2001071200126 20010712 00126 NM 2001 7 12 UIEA01064 1 20010626 A 5300 FRAME BOEING 747 747243B 1384830 NM BS 800 CRACKED A UIEA O OTHER O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 DURING HFEC INSPECTION, FOUND FRAME STATION 800 CRACKED AT STRINGER 17R COMMON TO THE AFT INNER CHORD AT A FASTENER HOLE . TRIMMED OUT CRACK. FABRICATED FILLER AND REPAIR STRAPS AND INSTALLED PER STANDARD PRACTICES IAW SRM 53-10-04 FIG 114 . HFEC (FLAT SURFACE) REINSPECTION TO BE ACCOMPLISHED OF THE ENTIRE STACK UP AND SURROUNDING AREA AT 3000 CYCLE INTERVA LS. (M) 2 L 7 4 4F A20WE 2001071200127 20010712 00127 NM 2001 7 12 UIEA01065 1 20010626 A 5300 65B01714565 DOUBLER BOEING 747 747243B 1384830 NM BS 420 CRACKED A UIEA O OTHER O OTHER IN INSP/MAINT 1 EA 15 516MC 77446 22507 DURING INSPECTION, FOUND FRAME STATION 420 CRACKED AT STRINGER 14 (E)L AND STRINGER 15L AT THE SHEAR DOUBLER COMMON TO T HE STRINGER CUTOUT. TRIMMED AWAY TWO FASTENER ROWS OF THE OUTBOARD REINFORCING ANGLE. STOP DRILLED CRACKS. FABRICATED FILLER, DOUBLERS AND REPAIR ANGLE, INSTALLED PER STANDARD PRACTICES. REINSPECT AREA PER SB 747-53A2265 AT 3000 CYCLE I NTERVALS. (M) 2 L 7 4 4F A20WE 2001071200128 20010712 00128 NM 2001 7 12 UIEA01066 1 20010626 A 5310 65B017145003 FRAME BOEING 747 747243B 1384830 NM BS 420 CRACKED A UIEA O OTHER O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 DURING INSPECTION, FOUND FRAME WEB DOUBLER STATION 420 CRACKED AT STRINGER 16L COMMON TO THE STRINGER CUT-OUT. CRACK NO T STOP DRILLED DUE TO CRACK PROXIMITY TO EDGE OF THE PART. FABRICATED DOUBLER AND INSTALLED PER STANDARD PRACTICES IAW SRM 53-10-04. REINSPECT AREA PER SB 747-53A2265 AT 3000 CYCLE INTERVALS. (M) 2 L 7 4 4F A20WE 2001071200129 20010712 00129 NM 2001 7 12 UIEA01067 1 20010626 A 5310 65B017185003 FRAME BOEING 747 747243B 1384830 NM BS 500 CRACKED A UIEA O OTHER O OTHER IN INSP/MAINT 1 EA 15 516MC 77446 22507 DURING INSPECTION, FOUND FRAME DOUBLER AND CLIP COMMON TO STATION 500 CRACKED AT STRINGER 10A (L) AND 11L. FABRICATED D OUBLERS AND INSTALLED PER STANDARD PRACTICES IAW SRM 53-10-04. CLIP REPLACED. REINSPECT AREA PER SB 747-53A2265 AT 300 0 CYCLE INTERVALS. (M) 2 L 7 4 4F A20WE 2001071200130 20010712 00130 NM 2001 7 12 UIEA01068 1 20010626 A 5310 65B017195003 FRAME BOEING 747 747243B 1384830 NM BS 520 CRACKED A UIEA O OTHER O OTHER IN INSP/MAINT 1 EA 15 516MC 77446 22507 DURING INSPECTION, FOUND FRAME AND DOUBLER STATION 520 CRACKED AT STRINGER 10A (L) AND 11L COMMON TO THE STRINGER CUT-OU T AT 10A(L) AND 11L. FABRICATED DOUBLERS AND INSTALLED PER STANDARD PRACTICES IAW SRM 53-10-04. CLIP REPLACED. REINSP ECT AREA PER SB 747-53A2265 AT 3000 CYCLES INTERVALS. (M) 2 L 7 4 4F A20WE 2001071200131 20010712 00131 NM 2001 7 12 UIEA01069 1 20010626 A 5300 65B0170446 FRAME BOEING 747 747243B 1384830 NM BS 220 CRACKED A UIEA O OTHER O OTHER IN INSP/MAINT 1 EA 15 516MC 77446 22507 DURING INSPECTION, FOUND FRAME WEB STATION 220 CRACKED AT STRINGER 14R, 1.2 INCH COMMON TO THE TRIANGULAR CUTOUT. STOP DRILLED CRACK. PERFORMED OPEN HOLE HFEC INSPECTION TO ENSURE CRACK CONTAINMENT IN STOP HOLE. FABRICATED DOUBLER AND IN STALLED PER STANDARD PRACTICES. REINSPECT AREA PER SB 747-53A2265 AT 3000 CYCLES INTERVALS. (M) 2 L 7 4 4F A20WE 2001071200132 20010712 00132 NM 2001 7 12 TSAA0153077 1 20010618 A 5300 6545455 SPAR BOEING 737 7372M6C 1384708 NM FS 476-481.7 CORRODED A TSAA O OTHER O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 FOUND CORROSION DURING HEAVY CHECK AT RIGHT WING FRONT SPAR LOWER CHORD FORWARD FLANGE LOWER SURFACE AT FSS 476.0 THROUG H FSS 481.7. (M) 2 L 7 2 4F RT A16WE 2001071200133 20010712 00133 NM 2001 7 12 TSAA01080 1 20010621 A 2100 503063 TURBINE BOEING 737 7372X6C 1384552 NM RT AC PACK SEIZED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 HNL - WHILE ON THE GROUND AT GATE 51 WITH APU AND ONE PACK OPERATING (RIGHT), THE CAPTAIN REPORTED SMOKE IN THE COCKPIT AND CABIN. THE AIRCRAFT WAS EVACUATED AND CRASH CREW CALLED. NOTE THAT THE LEFT PACK WAS ON DEACTIVATED FOR MEL 26-12 AND THE RIGHT PACK WAS OPERATING. REMOVED AND REPLACED THE ACM, RIGHT PACK TEMP SWITCH AND WATER SEPARATOR. OPS LEAK A ND OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001071200134 20010712 00134 NM 2001 7 12 USAA010603 1 20010601 A 5300 FRAME BOEING 737 7372B7 1384560 NM BS 767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 284AU 47733 23131 CLT - FOUND FRAME CRACKED .0625 INCH, BS 767, STRINGER 13L. ENLARGED FASTENER HOLE TO .25 INCH, INSTALLED HI-LOCK PER S RM 51-10-02. (M) 2 L 7 2 4F A16WE 2001071200135 20010712 00135 NM 2001 7 12 USAA010602 1 20010601 A 5400 TIE CLIP BOEING 737 7372B7 1384560 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 284AU 47733 23131 CLT - FOUND STRINGER TIE CLIP CRACKED .25 INCH, BS 747, STRINGER 7L. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-02. ( M) 2 L 7 2 4F A16WE 2001071200136 20010712 00136 NM 2001 7 12 USAA010596 1 20010531 A 5400 FRAME BOEING 737 7372B7 1384560 NM BS 847 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 284AU 23131 CLT - FOUND FRAME CORRODED APPROXIMATELY 4 SQUARE INCH AREA, BS 847, ABOVE STRINGER 25R. REMOVED DAMAGED SECTION, REPLA CED SECTION PER BOEING DRAWING NR 65C35243 AND EA69063. (M) 2 L 7 2 4F A16WE 2001071200137 20010712 00137 SO 2001 7 12 LR7A01036 1 20010711 A 5315 3598362 CAP LKHEED 382 382G 526414U SO FS 797E CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 DURING POST TAIL STRIKE DAMAGE EVALUATION (REF. OPER CTRL NO. LR7A01033) FOUND FS 797E - 817E BEAM LOWER CAP CRACKED FS 797E AT LBL 10, WL 127.75.FABRICATED AND REPLACED LOWER CAP IAW SRM SMP 583-53-10 PG 7 D., 51-70. NR 9, CONT. SHEET ITE M 17, 18, 19. 2 H 7 4 4T A1SO 2001071200138 20010712 00138 SO 2001 7 12 LR7A01037 1 20010711 A 5311 3626741 STIFFENER LKHEED 382 382G 526414U SO FS 807E CRUSHED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 DURING POST TAIL STRIKE DAMAGE EVALUATION (REF. OPER CTRL NO. LR7A01033) FOUND FS 807E CIRCUMFERENTIAL STIFFENER CRUSHED AT LBL 10 - RBL 10, WL 129.5.FABRICATED AND REPLACED CIRCUMFERENTIAL STIFFENER IAW SRM SMP 583-53-10 PG 7 D., 51-70. N R 9, CONT. SHEET ITEM 24, 25, 26. 2 H 7 4 4T A1SO 2001071200139 20010712 00139 SO 2001 7 12 LR7A01038 1 20010711 A 5315 35699719L19R STIFFENER LKHEED 382 382G 526414U SO FS 797E DISTORTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 DURING POST TAIL STRIKE DAMAGE EVALUATION (REF. OPER CTRL NO. LR7A01033) FOUND FS 797E VERTICAL STIFFENERS DISTORTED AT LBL 10 AND RBL 10, WL 127.75 - 145.FABRICATED AND REPLACED STIFFENERS IAW SRM SMP 583-53-10 PG 7 D., 51-70. NR 9, CONT. SHEET ITEM 8, 9, 10. 2 H 7 4 4T A1SO 2001071200140 20010712 00140 SO 2001 7 12 LR7A01039 1 20010711 A 5320 3569975L BRACE LKHEED 382 382G 526414U SO FS 797E DISTORTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 DURING POST TAIL STRIKE DAMAGE EVALUATION (REF. OPER CTRL NO. LR7A01033) FOUND FS 797E DIAGONAL BRACE DISTORTED AT LBL 8 , WL 127.5.FABRICATED AND REPLACED DIAGONAL BRACE IAW SRM SMP 583-53-10 PG 7 D., 51-70. NR 9, CONT. SHEET ITEM 14, 15, 16. 2 H 7 4 4T A1SO 2001071200141 20010712 00141 SO 2001 7 12 LR7A01040 1 20010711 A 5313 3596681L1R STIFFENER LKHEED 382 382G 526414U SO FS 797E-817E BROKEN A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 DURING POST TAIL STRIKE DAMAGE EVALUATION (REF. OPER CTRL NO. LR7A01033) FOUND FS 797E - 817E LONGITUDINAL STIFFENERS BR OKEN AT LBL 3.57 AND RBL 3.57, WL 127.75.FABRICATED AND REPLACED LONGITUDINAL STIFFENERS IAW SRM SMP 583-53-10 PG 7 D., 51-70. NR 9, CONT. SHEET ITEM 11, 12, 13. 2 H 7 4 4T A1SO 2001071200142 20010712 00142 SO 2001 7 12 LR7A01041 1 20010711 A 5320 3599427 PLATE LKHEED 382 382G 526414U SO FS 797E-817E DISTORTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 DURING POST TAIL STRIKE DAMAGE EVALUATION (REF. OPER CTRL NO. LR7A01033) FOUND FS 797E - 817E STRIKE PLATE DISTORTED AT LBL 10 - RBL 10, WL 127.75 - WL 129.5.FABRICATED AND REPLACED STRIKE PLATE IAW SRM SMP 583-53-10 PG 7 D., 51-70. NR 9, CONT. SHEET ITEM 27, 28, 29. 2 H 7 4 4T A1SO 2001071200143 20010712 00143 SO 2001 7 12 LR7A01042 1 20010711 A 5313 36201456 STIFFENER LKHEED 382 382G 526414U SO FS 787E-797E DEFORMED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 DURING POST TAIL STRIKE DAMAGE EVALUATION (REF. OPER CTRL NO. LR7A01033) FOUND FS 787E - 797E LONGITUDINAL STIFFENERS DE FORMED AT LBL 20.95 AND RBL 20.95, WL 127.5 - 128.5.REPLACED LONGINTUDINAL STIFFENERS IAW SRM SMP 583-51-70. NR 9, CONT .SHEET ITEM 42. 2 H 7 4 4T A1SO 2001071200144 20010712 00144 SO 2001 7 12 LR7A01043 1 20010711 A 5313 36201457 STIFFENER LKHEED 382 382G 526414U SO FS 777E-787E DEFORMED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 DURING POST TAIL STRIKE DAMAGE EVALUATION (REF. OPER CTRL NO. LR7A01033) FOUND FS 777E - 787E LONGITUDINAL STIFFENERS DE FORMED AT LBL 20.95 AND RBL 20.95, WL 127.5.REPLACED LONGINTUDINAL STIFFENERS IAW SRM SMP 583-51-70. NR 9, CONT. SHEET ITEM 31. 2 H 7 4 4T A1SO 2001071200145 20010712 00145 SO 2001 7 12 LR7A01044 1 20010711 A 5313 348191 STIFFENER LKHEED 382 382G 526414U SO FS 777E-797E BROKEN A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 DURING POST TAIL STRIKE DAMAGE EVALUATION (REF. OPER CTRL NO. LR7A01033) FOUND FS 777E - 797E LONGITUDINAL STIFFENERS BR OKEN AT LBL 10 AND RBL 10, WL 127.75.REPLACED LONGINTUDINAL STIFFENERS IAW SRM SMP 583-51-70. NR 9, CONT. SHEET ITEM 41 . 2 H 7 4 4T A1SO 2001071200147 20010712 00147 SO 2001 7 12 LR7A01046 1 20010711 A 5313 36201459 STIFFENER LKHEED 382 382G 526414U SO FS 777E-787E BENT A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 DURING POST TAIL STRIKE DAMAGE EVALUATION (REF. OPER CTRL NO. LR7A01033) FOUND FS 777E - 787E LONGITUDINAL STIFFENERS BE NT AT LBL 3.57 AND RBL 3.57, WL 126.REPLACED LONGINTUDINAL STIFFENERS IAW SRM SMP 583-51-70. NR 9, CONT. SHEET ITEM 33. 2 H 7 4 4T A1SO 2001071200148 20010712 00148 SO 2001 7 12 LR7A01047 1 20010711 A 5311 36201434 STIFFENER LKHEED 382 382G 526414U SO FS 787E BROKEN A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 DURING POST TAIL STRIKE DAMAGE EVALUATION (REF. OPER CTRL NO. LR7A01033) FOUND FS 787E CIRCUMFERENTIAL STIFFENER BROKEN AT LBL 20.95 - RBL 20.95, WL 127.5.REPLACED CIRCUMFERENTIAL STIFFENER IAW SRM SMP 583-51-70. NR 9, CONT. SHEET ITEM 34. 2 H 7 4 4T A1SO 2001071200149 20010712 00149 SO 2001 7 12 LR7A01048 1 20010711 A 5311 3759749 CAP LKHEED 382 382G 526414U SO FS 797E CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 DURING POST TAIL STRIKE DAMAGE EVALUATION (REF. OPER CTRL NO. LR7A01033) FOUND FS 797E BULKHEAD LOWER CAP CRACKED AND BR OKEN AT LBL 20.95 - RBL 20.95, WL 127.5 - 128.5.REPLACED LOWER CAP IAW SRM SMP 583-51-70. NR 9, CONT. SHEET ITEM 2. 2 H 7 4 4T A1SO 2001071200150 20010712 00150 SO 2001 7 12 LR7A01049 1 20010711 A 5311 3569843 CAP LKHEED 382 382G 526414U SO FS 777E CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 DURING POST TAIL STRIKE DAMAGE EVALUATION (REF. OPER CTRL NO. LR7A01033) FOUND FS 777E BULKHEAD LOWER CAP CRACKED AT LBL 4 - RBL 10, WL 126.REPLACED LOWER CAP IAW SRM SMP 583-51-70. NR 9, CONT. SHEET ITEM 3. 2 H 7 4 4T A1SO 2001071200151 20010712 00151 SO 2001 7 12 LR7A01050 1 20010711 A 5330 33050139 SKIN LKHEED 382 382G 526414U SO FS 777E-817E TORN A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 DURING POST TAIL STRIKE DAMAGE EVALUATION (REF. OPER CTRL NO. LR7A01033) FOUND FS FS 777E - 817E SKIN PANEL TORN AT FS 7 77E, LBL 4 - RBL 10, WL 126.REPLACED SKIN PANEL FS 777E - 817E, LBL 61.25 - RLB 61.25, WL 126 IAW SRM SMP 583-53-10 PG 2/3 D., 51-70 NR 9, CONT. SHEET ITEM 4. 2 H 7 4 4T A1SO 2001071200152 20010712 00152 SO 2001 7 12 LR7A01051 1 20010711 A 5330 330501311 SKIN LKHEED 382 382G 526414U SO FS 737E-777E DISTORTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 DURING POST TAIL STRIKE DAMAGE EVALUATION (REF. OPER CTRL NO. LR7A01033) FOUND FS FS 737E - 777E SKIN PANEL DISTORTED AN D SCRATCHED AT FS 757E - 777E, LBL 20.95 - RBL 20.95, WL 126.FABRICATED AND REPLACED SKIN PANEL FS 737E - 777E, LBL 61. 25 - RLB 61.25, WL 126 IAW SRM SMP 583-53-10 PG 2 D., 51-70. NR 9, CONT. SHEET ITEM 5, 6, 7. 2 H 7 4 4T A1SO 2001071200153 20010712 00153 SO 2001 7 12 LR7A01052 1 20010711 A 5311 35662519 STIFFENER LKHEED 382 382G 526414U SO FS 817E CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 DURING POST TAIL STRIKE DAMAGE EVALUATION (REF. OPER CTRL NO. LR7A01033) FOUND FS 817E BULKHEAD VERTICAL STIFFENER CRACK ED AT BL 0, WL 132.FABRICATED AND REPLACED VERTICAL STIFFENER IAW SRM SMP 583-53-10 PG 7 D., 51-70 NR 9, CONT. SHEET IT EM 35, 36, 37. 2 H 7 4 4T A1SO 2001071200154 20010712 00154 SO 2001 7 12 LR7A01053 1 20010710 A 5320 342603 CLIP LKHEED 382 382G 526414U SO FS 597 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 460 4590 DURING THRU FLIGHT WALK AROUND FOUND FS 597 RH PRESSURE FAIRING FORMER ATTACH CLIP CRACKED AT RBL 23, WL 285.REPLACED AT TACH CLIP IAW SRM SMP 583-51-10, PARA F. (1). D&C NO. M-5. 2 H 7 4 4T A1SO 2001071200155 20010712 00155 WP 2001 7 12 ARWA0010716 1 20010708 A 2612 D5030 FIRE LOOP DOUG DC8 DC863F 302198F WP NR 2 & 3 ENGINE MALFUNCTIONED A ARWA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 19 441J 45988 AT 10,000 FT MSL MASTER FIRE WARNING SOUNDED MOMENTARILY NR 2 FIRE HANDLE ILLUMINATED, APPROX 30 SECONDS LATER MASTER FI RE WARNING SOUNDED MOMENTARILY AGAIN AND NR 3 FIRE HANDLE ILLUMINATED. ENGINE SEVERE DAMAGE OR SEPARATION CHECKLIST INI TIATED, ENGINE NR 1, 2, 3 FIRE WARNING TESTED OK AND NR 4 DID NOT. ON THE SECOND IDENTIFY ENGINE NR 1, 2, 4 TESTED OK A ND NR 3 DID NOT. AIRCRAFT RETURNED TO MIAMI WITHOUT INCIDENT. OVERWEIGHT LANDING PERFORMED INTO MIAMI. PERFORMED NR 2 ENGINE ELECTRICAL WIRING CHECK, FOUND NORMAL, FOR T/S REMOVED AND REPLACED NR 2 AMPLIFIER FIRE WARNING IAW MM 26-10-4 ( WD 26-1-1). PERFORMED NR 3 ENGINE ELECTRICAL WIRING CHECK FOUND NORMAL IAW WD 26-1-1, FOR T/S REM. 2 L 7 4 4F 4A25 2001071200157 20010712 00157 NM 2001 7 12 AWXA0001851 1 20010611 A 2913 5718607 PUMP BOEING 737 7373S3 1384711 NM HYD SYSTEM LEAKING A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION UK UNKNOWN 1 WP 28 316AW 47431 442 23713 AIR TURNBACK,EN ROUTE FROM LAS TO SNA THE A/C LOST B-HYD SYSTEM QUANTITY AND THE NR 2 ENG DRIVEN HYD PUMP LOW PRESSURE L IGHT ILLUMINATED FOLLOWED BY THE B-SYSTEM ELEC PUMP LOW PRESSURE LIGHT. A/C RETURNED TO LAS MAKING AN UNEVENTFUL LANDIN G. MX FOUND HYD FLUID COMING OUT OF RT WHEEL WELL AREA; LEAK CHECK PERFORMED USING THE ELEC PUMP AND FOUND IT WAS LEAKI NG AND WAS REPLACED; THE ENG DRIVEN AND ELEC PUMP CASE DRAIN FILTERS WERE INSPECTED FOR CONTAMINATION AND NONE FOUND. F ILTERS REPLACED; THE NR 2 ENG WAS RUN TO CHECK THE NR 2 ENG DRIVEN PUMP. FOUND LEAKING AND WAS REPLACED. NO FURTHER DI SCREPANCIES HAVE BEEN REPORTED. ENG DR HYD PUMP P/N: 65075-06. 2 L 7 2 4F RT A16WE 2001071200158 20010712 00158 NM 2001 7 12 2001F00107 1 20010621 A 2163 1173T101 SWITCH BOEING 737 7372X6C 1384552 NM RT AC PACK FAILED A TSAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 13 816AL 23122 HNL - WHILE ON THE GROUND AT GATE 51 WITH APU AND ONE PACK OPERATING (RIGHT), THE CAPTAIN REPORTED SMOKE IN THE COCKPIT AND CABIN. THE AIRCRAFT WAS EVACUATED AND CRASH CREW CALLED. NOTE THAT THE LEFT PACK WAS ON DEACTIVATED FOR MEL 26-12 AND THE RIGHT PACK WAS OPERATING. REMOVED AND REPLACED THE ACM, RIGHT PACK TEMP SWITCH AND WATER SEPARATOR. OPS LEAK A ND OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. REF TSAA01080. (M) 2 L 7 2 4F RT A16WE 2001071200159 20010712 00159 NM 2001 7 12 AALA20010505 1 20010318 A 3350 LIGHT BOEING 727 727223 1384074 NM AIRSTAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 859AA 21086 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AS SEMBLY AT AFT AIRSTAIRS. (M) 2 L 7 3 4F A3WE 2001071200160 20010712 00160 NM 2001 7 12 AALA20010625 1 20010326 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 868AA 21373 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 25 DIM. REPLACED EMERGENCY EXIT LIGHT STRIP AT ROWS 25. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200161 20010712 00161 NM 2001 7 12 AALA20010757 1 20010409 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN EXPOSED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 891AA 22007 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT EXPOSED. RE-SECURED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GRO UND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200162 20010712 00162 NM 2001 7 12 AALA20010760 1 20010409 A 3350 BATTERY BOEING 727 727227 1384078 NM COCKPIT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 727AA 20734 DFW - DURING OVERNIGHT MAINTENANCE, FOUND COCKPIT EMERGENCY EXIT LIGHT DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY MODUL E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200163 20010712 00163 EU 2001 7 12 AALA20010768 1 20010410 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN LOOSE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 1425A 11408 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT WIRING LOOSE. RE-SECURED EMERGENCY EXIT LIGHT WIRING AT SEAT 4 EF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001071200164 20010712 00164 NM 2001 7 12 AALA20010769 1 20010410 A 3350 1001141 LIGHT BOEING 727 727200 138407E NM AIRSTAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 894AA 22010 BNA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASS EMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A3WE 2001071200165 20010712 00165 NM 2001 7 12 AALA20010786 1 20010325 A 3350 LIGHT BOEING 727 727223 1384074 NM GALLEY INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 889AA 21527 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT S TRIP AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200166 20010712 00166 NM 2001 7 12 AALA20010815 1 20010419 A 3350 LIGHT BOEING 727 727223 1384074 NM AIRSTAIR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 886AA 21525 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASS EMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200167 20010712 00167 NM 2001 7 12 AALA20010825 1 20010422 A 3350 LIGHT BOEING 727 727223 1384074 NM AIRSTAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 861AA 21088 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AS SEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200168 20010712 00168 NM 2001 7 12 AALA20010838 1 20010420 A 3350 SPLICE BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 860AA 21087 DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT SPLICE AT LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200169 20010712 00169 EU 2001 7 12 AALA20010856 1 20010425 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU ENTRY DOOR BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1437B 11427 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PASSENGER ENTRY DOOR BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT PASSENGER ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001071200170 20010712 00170 NM 2001 7 12 AALA20010880 1 20010430 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 844AA 20985 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001071200171 20010712 00171 EU 2001 7 12 AALA20011119 1 20010518 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1459A 11479 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTS AT 16D WALKWAY STRIP INOPERATIVE. REPAIRED EMERGENCY E SCAPE PATH WALKWAY STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001071200172 20010712 00172 NM 2001 7 12 AALA20011266 1 20010612 A 5311 FRAME BOEING 727 727223 1384074 NM FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 882AA 21521 TUL - FOUND BELT FRAME DENTED, FS 500 STRINGER 23R. INSTALLED BELTFRAME DOUBLER PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 2001071200173 20010712 00173 NM 2001 7 12 AALA20011299 1 20010621 A 5311 FRAME BOEING 727 727227 1384078 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AA 20732 TUL - FOUND BELT FRAME CRACKED STATION 1110, RBL 18 TOP OF FLANGE. REPAIRED BELT FRAME BY CUTTING OUT CRACKED AREA AND INSTALLING REPAIR TO BELT FRAME PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 2001071200174 20010712 00174 NM 2001 7 12 GAIA01244AOP 1 20010601 A 2612 FIRE WARNING BOEING 727 727223 1384074 NM CARGO BAY MALFUNCTIONED A GAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 07 854AA 20995 FLT 1800 - MCO-CLT - AT 75K, GOT AFT LOWER FIRE WARNING INDICATION. CREW DECLARED AN EMERGENCY. AIRCRAFT MADE AN UNEVE NTFUL REJECTED TAKEOFF (75K) IN MCO. DEFERRED LOWER CARGO COMPARTMENT FIRE DETECTION SYSTEM IAW B727 MEL 26-19. AIRCRA FT WAS INSPECTED AND NO FIRE EVIDENCE WAS FOUND. AIRCRAFT WAS ALSO INSPECTED FOR REJECTED TAKEOFF AND RETURNED TO SERVI CE. (M) 2 L 7 3 4F A3WE 2001071200175 20010712 00175 NM 2001 7 12 GAIA01244BOP 1 20010626 A 2611 BATTERY BOEING 727 727223 1384074 NM SMOKE DETECTOR DISCHARGED A GAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 07 854AA 20995 FLT 1800 - MCO-CLT - AT 75K, GOT AFT LOWER FIRE WARNING INDICATION. CREW DECLARED AN EMERGENCY. AIRCRAFT MADE AN UNEVE NTFUL REJECTED TAKEOFF (75K) IN MCO. REMOVED AND REPLACED LOWER AFT CARGO SMOKE DETECTORS BATTERIES. SMOKE DETECTOR SY STEM TEST GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001071200176 20010712 00176 NM 2001 7 12 GAIA01245OP 1 20010626 A 2781 WIRE BOEING 727 727223 1384074 NM L/E SLAT FAULTY A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 6806 19481 KHA - FLT 202 - TYS TO DFW, ON CLIMB-OUT FROM TYS, THE NR 2 SLAT DID NOT RETRACT WHEN THE FLAP HANDLE WAS MOVED TO THE U P POSITION. EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO TYS. AN UNEVENTFUL LANDING WAS MADE. INSPECTION REVEA LED THAT A WIRING HAD FAILED ON THE NR 2 SLAT POSITION SWITCH. THE SPLICE WAS REPLACE OPERATIONAL CHECK WAS NORMAL. TH E AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001071200177 20010712 00177 CE 2001 7 12 GLBA2001154 1 20010711 A 6100 1293640919 CIRCUIT BOARD BEECH 1900 1900D 1154162 CE INOPERATIVE A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 192GL UE192 LEFT AUTO FEATHER INOPERATIVE, REPLACED PCB OPS CHECKED SYSTEM STATISFACTORY 2 L 7 2 4T RT A24CE 2001071200178 20010712 00178 CE 2001 7 12 GLBA2001152 1 20010711 A 2600 24412886 FIRE LOOP BEECH 1900 1900D 1154162 CE INOPERATIVE A GLBA D RETURN TO BLOCK O OTHER CL CLIMB 1 CE 01 97UX UE97 LEFT FIRE LOOP AND PULL HANDLE WARNING LIGHT ILLUMINATED, REPLACED FIRE LOOP OPS CHECKED SYSTEM SATISFACTORY 2 L 7 2 4T RT A24CE 2001071200179 20010712 00179 CE 2001 7 12 GLBA2001150 1 20010710 A 6100 1143800663 INDICATOR BEECH 1900 1900D 1154162 CE #2 COCKPIT STUCK A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 01 211UX 3229 UE211 RIGHT PROP RPM INDICATOR FAILED ON T/O, REPLACE INDICATOR AND TACH GENERATOR 2 L 7 2 4T RT A24CE 2001071300001 20010713 00001 SO 2001 7 13 SWIA972604 1 20010526 A 3610 CLAMP EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE BLEED AIR LOOSE A SWIA A UNSCHED LANDING J G WARNING INDICATION MULTIPLE FAILURE CL CLIMB 1 NM 07 294SW 120321 JUST AFTER TAKEOFF FROM PDX, RECEIVED A DUCT LEAK WARNING ON MAP AND UPPER PANEL RIGHT PACK. CONSULTED QRH AND RETURNED FOR LANDING AT PDX. LIGHT WENT OUT ON DESCENT INTO PDX ABOUT 2,000 FT. DURING QRH PROCEDURE WHEN BLEED WAS CLOSED BLU E HYDRAULIC INDICATOR WENT TO EMPTY WITH NO ASSOCIATED WARNING. INVESTIGATED, FOUND BAD WIRE ON THERMAL SWITCH. REPAIR ED SAME. FOUND TWO LEAKING CLAMPS AT HEAT EXCHANGER. REPAIRED AND TIGHTENED CLAMPS AND FOUND A DEICE SYSTEM PRESSURE R EGULATOR LEAKING. REMOVED AND REPLACED PRESSURE REGULATOR. RAN ENGINES, NO LEAKS. OPS CHECK GOOD AS PER MM 30-10-20. P/N: 38E96-6A, S/N ON: B2407. 2 L 7 2 4T 4 T RT A31SO E20NE 2001071300002 20010713 00002 SO 2001 7 13 SWIA972610 1 20010527 A 3260 CONNECTOR EMB 120 EMB120RT SO PWA 118 PW118 NE LT MLG FAULTY A SWIA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 NM 07 1117H 120117 AFTER GEAR RETRACTION, LEFT MAIN GEAR SYSTEM-A RED LIGHT STILL ILLUMINATED. LOUD VIBRATION IN AIRCRAFT. TROUBLESHOOT S YSTEM. FOUND PUSHED BACK PIN ON A-UPLOCK CONNECTOR, RESET PIN. REMOVED AND REPLACED A-UPLOCK HARNESS AND BOTH PROXIMIT Y SENSORS. ADJUSTED UPLOCK PLUNGER. SWUNG GEARS SEVERAL TIMES AND ALL CHECKED GOOD IAW EMB MM 32-61-01. HARNESS - P/N ON 120-41126-1, S/N ON T01743, S/N OFF T01747. PROXIMITY SENSORS P/N ON 7S-00370-02, S/N ON (TOP) 592 (BOTTOM) 588. S/N OFF (TOP) 582, (BOTTOM) 585. 2 L 7 2 4T 4 T RT A31SO E20NE 2001071300003 20010713 00003 NE 2001 7 13 SWIA972611 3 20010602 A 6112 PROP HEAT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE HAMSTD 14RF 14RF9 NE LT PROP INTERMITTENT A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 295UX 120295 CREW REPORTS LEFT PROP HEAT FAILS INTERMITTENTLY INFLIGHT. RETURNED TO PDX. MAINTENANCE FOUND THE PROP HAD BEEN STRUCK BY LIGHTNING. REMOVED AND REPLACED LEFT BULKHEAD ASSEMBLY, DID NOT FIX PROBLEM. P/N ON 784784-1, S/N ON 960443, S/N O FF 9202318. REMOVED AND REPLACED ALL PROP BLADES IAW MM 61-13-04. 2 L 7 2 4T 4 T RT A31SO E20NE 6 C P11NE 2001071300004 20010713 00004 SO 2001 7 13 SWIA972616 1 20010604 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE T/E FLAP FAILED A SWIA O OTHER K F J FLUID LOSS FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 229SW 120305 WHEN FLAPS WERE SELECTED TO 15 DEGREES ON APPROACH, FLAP DISAGREEMENT WAS NOTED FOLLOWED BY LOSS OF BLUE HYDRAULIC SYSTE M. REPLACED RIGHT NACELLE FLAP ACTUATOR IAW EMB 120 MM 27-50-00. OPS AND LEAK CHECK GOOD. SERVICED BLUE HYDRAULIC RES ERVOIR AND CHECKED HYDRAULIC PUMPS. ALL CHECKS GOOD. P/N ON 343100-1001, S/N ON 0177, S/N OFF 0210. 2 L 7 2 4T 4 T RT A31SO E20NE 2001071300006 20010713 00006 NM 2001 7 13 UPS01536014 1 20010530 A 2910 HYDRAULIC LINE BOEING 757 75724APF 1384969 NM HYD SYSTEM LEAKING A IPXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SO 01 406UP 23728 INSPECTION TYPE:N/A ATB-LOSS OF HYD FLUID. *S/D* INSTALLED TEMP FLEX LINE HOSE ON LT MLG SIDE STRUT ACTUATOR LEAK CHEC KS OK. REMOVED AND REPLACED HYD PUMP AND FILTERS IAW MM 29-11-05, OPS AND LEAKS CHECK GOOD. 2 L 7 2 4F RT A2NM 2001071300008 20010713 00008 NM 2001 7 13 UPS01636017 1 20010604 A 4920 APU BOEING 767 76734AF 1385212 NM APU BAY MALFUNCTIONED A IPXA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 SO 01 308UP 27761 INSPECTION TYPE:ETOP ATB-DURING CLIMB AT 330FL EICAS MESSAGE. APU FAULT APU SHUTDOWN AIRCRAFT, ATB TO HNL. BITE APU EC U. LAST FLT FAULT DC PWR LOSS. PERFORM FIM 49-11-00, SYS TEST OK. RUN AND SHUT DOWN APU, OP CHECK NORMAL. 2 L 7 2 4F RT A1NM 2001071300010 20010713 00010 WP 2001 7 13 UPS01836016 1 20010530 A 3350 LIGHT DOUG DC8 DC873F 302199F WP COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:N/A DURING BISE CHECK THE EMERGENCY LIGHT ON THE GLARESHIELD AND OVER CREW ENTRY DOOR DO NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK AND RELAY UNIT, OPS CHECKS GOOD IAW MM 33-50-01. 2 L 7 4 4F RT 4A25 2001082400245 20010824 00245 2001 8 24 UPS01836018 4 20010605 A 2565 CONTAINER DOUG DC8 DC873F 302199F WP ENTRY DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:N/A DEPARTURE, ESCAPE SLIDE FELL OUT WHEN FWD ENTRY DOOR CLOSED. DEFERRED SLIDE CONTAINER DUE TO DAMAGE. 2 L 7 4 4F RT 4A25 2001071300011 20010713 00011 NM 2001 7 13 VNAA0105011 1 20010519 A 2844 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 427JS 3039 FLIGHT 4073 WAS ON TAKEOFF AND THE CREW RECEIVED A FUEL PRESSURE LOW CAS MESSAGE. THE CREW ABORTED TAKEOFF. ON THE WAY BACK TO THE GATE, THE MESSAGE CLEARED AND FLIGHT 4073 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4073 DEPARTED WI TH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001071300012 20010713 00012 NM 2001 7 13 VNAA0105014 1 20010524 A 3244 26107012 TIRE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT MLG BLOWN A VNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 423JS 118 3032 WHILE TAXIING, THE CREW HEARD WHAT SOUNDED LIKE A TIRE BLOWING. THE CAPTAIN CONTACTED GROUND AND RECEIVED PERMISSION TO SHUT DOWN THE ENGINES AND DO A VISUAL CHECK. THE CAPTAIN FOUND THE LEFT MAIN OUTBOARD TIRE TO BE BLOWN. THE PASSENGER S WERE BUSSED BACK TO THE TERMINAL. THE AIRCRAFT WAS TAXIED TO THE HANGAR WHERE OUTSTATION MAINTENANCE INSPECTED AND RE PLACED THE TIRE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001071300013 20010713 00013 NM 2001 7 13 VNAA0105016 1 20010526 A 2750 CONTROL BOX DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE E/E BAY MALFUNCTIONED A VNAA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CR CRUISE 1 GL 07 431JS 3028 FLIGHT 4157 WAS EN ROUTE TO DCA AND RECEIVED A AMBER CAS MESSAGE INDICATING A STANDBY HYDRAULIC FAILURE. THE CREW CHECK ED THE HYDRAULIC PAGE WHICH ONLY HAD DASHES ON IT. THE CREW REFERENCED THE QUICK REFERENCE HANDBOOK AND CALLED MAINTENA NCE CONTROL. FLIGHT 4157 DIVERTED TO IAD BECAUSE OF THE LONGER RUNWAY. THE CREW DECLARED AN EMERGENCY AND PERFORMED A NO FLAP LANDING AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE SENT A MECHANIC AND PARTS TO IAD TO INSPECT THE AIRCRAFT. MAINTENANCE RERACKED THE FLAP CONTROL BOX, PERFORMED SEVERAL GEAR EXTENSIONS, SEVERAL FLAP CYCLES, AND ALL APPLICABLE OPERATIONAL TESTS WITH NO FURTHER INCIDENTS. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001071300014 20010713 00014 EA 2001 7 13 COMA0160464 1 20010711 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA FAILED A COMA A UNSCHED LANDING S AFFECT SYSTEMS TO TAKEOFF 1 SO 01 710CA 7945 7241 AFTER T/O FROM CVG FLAP FAULT CAUTION MESSAGE, AIRCRAFT RETURNED TO THE FIELD.COMPLIED WITH AD 98-20-01 FLAP CAUTION MES SAGE "SECOND EVENT" MAINTENANCE ACTION, PARAGRAPH (B)3(D AND E)4. REPLACED THE RIGHT BRAKE AND POSITION SENSOR. 2 L 7 2 4F RT A21EA 2001071300016 20010713 00016 CE 2001 7 13 2001F00014 1 20010601 A 5753 122101015 FLAP TRACK CESSNA 206 TU206G 2073357 CE T/E FLAP LOOSE A K NONE O OTHER IN INSP/MAINT 1 GL 15 9851Z 2941 U20606701 RIGHT INBOARD FLAPTRACK IS WORKING LOOSE. THIS WAS INDICATED BY A CRACKED COVE SKIN AT THE ATTACH BRACKET LOCATION. 1 H 7 1 3O A4CE 2001071300017 20010713 00017 CE 2001 7 13 2001F00016 1 20010522 A 2910 6010003014 HYDRAULIC LINE CESSNA 337 P337H 2075731 CE NLG LEAKING B O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 15 4DU P3370311 AEROQUIP HOSE, STEEL BRAIDED G01, THAT GOES TO THE NOSE GEAR ACTUATOR DEVELOPED A LEAK IN THE MIDDLE OF THE HOSE ASSEMBL Y, RESULTING IN LOSS OF HYDRAULIC FLUID. AIRCRAFT WAS UNABLE TO LOWER THE RIGHT MAIN GEAR, DAMAGE TO THE AIRCRAFT WAS MINOR. 1 H 7 2 3O A6CE 2001071300018 20010713 00018 CE 2001 7 13 2001F00024 1 20010329 A 5312 5512020731 BULKHEAD CESSNA 500 550 2076604 CE FUSELAGE CRACKED B K NONE O OTHER IN INSP/MAINT 1 SW 01 26494 5500605 DURING SCHEDULED INSP, BULKHEAD (P/N 551202731) WAS FOUND CRACKED; IT IS AT STATION 456.50 LT SIDE. IT SHOULD BE NOTED THAT THE CRACK STARTS AT A HOLE THAT WAS MISDRILLED DURING PRODUCTION THEN FILLED AT THE FACTORY BY INSTALLING A DOUBLE FLUSH RIVET. THE HOLE WAS THEN RE-DRILLED ADJACENT TO FILLED EDGE. THIS AC WAS MODIFIED AT THE FACTORY FOR ADDED RADI O RACKS. THIS ADDED WEIGHT AND THAT A HOLE WAS DRILLED AND THEN FILLED AND RE-DRILLED MOST LIKELY HELPED IN THE FORMING OF THIS CRACK. INSPECTION OF ADDED EQUIPMENT STORAGE SHOULD BE INCLUDED IN AC THAT ARE MODIFIED AT THE FACTORY OR IN T HE FIELD, AS NORMAL INSP PROCEDURES MAY NOT SHOW THIS AREA TO LOOK AT. 1 L 7 2 4F A22CE 2001071300019 20010713 00019 NM 2001 7 13 COOSDR010037 1 20010621 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 29SW 21340 PAX CABIN, STA 947 FLOOR BEAM UPPER FLANGE CORRODED AT LBL 50. 2 L 7 2 4F A16WE 2001071300020 20010713 00020 NM 2001 7 13 COOSDR010038 1 20010621 A 5314 65564416 KEELBEAM BOEING 727 727231 1384079 NM FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 54352 21984 LOWER FUSELAGE - AFT CARGO COMPARTMENT BS 950E, STR 29 RT KEEL BEAM CHORD WITH SEVERE CORROSION. THE PROBABLE CAUSE OF THIS DAMAGE WAS CORROSION FATIGUE. 2 L 7 3 4F A3WE 2001071300022 20010713 00022 NM 2001 7 13 HN6R0000152 1 20010625 A 5311 FRAME BOEING 737 737400 NM FUSELAGE CRACKED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 932NU 25248 HFEC INSPECTION EXHIBITS CRACK INDICATION IN FRAME AT BS 663.75, STR 2, RT FORWARD AND AFT HOLES. CAUSE UNKNOWN. REPAI RED FRAME PER SB. 2 L 7 2 4F RT A16WE 2001071300023 20010713 00023 NM 2001 7 13 HN6R0000157 1 20010625 A 5312 WEB BOEING 737 737400 NM FUSELAGE CRACKED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 932NU 25248 EDDY CURRENT EXAMINATION REVEALS CRACK INDICATIONS AT TWO LINING RETAINING HOLES, BS 178, LBL 17.1, VERTICAL BEAM WEBS, WL 189 TO 191. CAUSE UNKNOWN ACCOMPLISHED ENGINEERING REPAIR NO. 01-0414. 2 L 7 2 4F RT A16WE 2001071300024 20010713 00024 NM 2001 7 13 HN62001F00000 1 20010625 A 5312 BULKHEAD BOEING 737 737400 NM FUSELAGE CRACKED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 932NU 25248 EDDY CURRENT EXAMINATION REVEALS CRACK INDICATIONS AT FIVE LINING RETAINING HOLES, BS 178, RBL 17.1 VERTICAL BEAM WEBS, WL 209 TO WL 230. COURSE UNKNOWN. ACCOMPLISHED ENGINEERING REPAIR 01-0414. 2 L 7 2 4F RT A16WE 2001071300025 20010713 00025 EA 2001 7 13 JBXA000307 1 20010712 A 2913 PU304448 HYDRAULIC SYSTEM CNDAIR CL600 CL6002B19 EA FAILED A JBXA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 05 575ML 7256 Discrepancy : Lost #2 engine driven hydraulic pump and all fluid. Corrective Action : Removed and replaced #2 ED hydraul ic pump I-A-W AMM 29-11-01 Ops check and leak check good. 2 L 7 2 4F RT A21EA 2001071300026 20010713 00026 NM 2001 7 13 CALA0100650 1 20010711 A 5330 SKIN BOEING 737 7373T0 1384582 NM BS 219 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14358 23943 INSPECTION FOUND FUSELAGE SKIN DENTED AT BS 219, S23L, TEN INCHES ABOVE L/H SIDE OF FORWARD ACCESSORY DOOR AT EDGE OF BO NDED DOUBLER. THE DENTED SKIN WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 53-00-01. 2 L 7 2 4F RT A16WE 2001071300027 20010713 00027 NM 2001 7 13 CALA0100651 1 20010711 A 5242 SKIN BOEING 737 7373T0 1384582 NM E&E DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59302 23353 INSPECTION FOUND EXTERNAL SKIN OF E&E DOOR DENTED. THE E&E DOOR OUTER SKIN WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 2001071300028 20010713 00028 NM 2001 7 13 CALA0100652 1 20010712 A 5751 AILERON BOEING 737 7373T0 1384582 NM L/H WING CRUSHED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59302 23353 INSPECTION FOUND LEADING EDGE I/B CORNER OF L/H AILERON CRUSHED. THE AILERON WAS REPAIRED IAW ECRA 5761-01026. 2 L 7 2 4F RT A16WE 2001071300030 20010713 00030 NM 2001 7 13 01FDEA00504 1 20010627 A 2613 WARNING LIGHT BOEING 727 727225 1384077 NM OVERHEAT SYS ILLUMINATED A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 SO 25 461FE 22548 LWR AFT BODY OVERHEAT LIGHT ILLUM DURING CLIMBOUT. LIGHT WENT OUT WHEN NR 3 BLD VALVE AND RIGHT PACK TURN OFF PER RED T ABS. RAN 2 AND 3 ENG PER JET RUN HANDBOOK CND. NO HISTORY NOTED. OK FOR SERVICE. 2 L 7 3 4F A3WE 2001071300032 20010713 00032 2001 7 13 01FDEA00522 4 20010710 A 3460 837101A COMPUTER AIRBUS 310 A310203 EU E/E BAY FAILED A FDEA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SO 25 411FE 359 AT T/O LOST ADC1, FD1, ATS2, REG1, PITOT HEAT AND TAT, PITCH TRIM. REMOVED AND REPLACED PROX DET PROC UNIT. TEST OK. 2 L 7 2 4F RT A35EU 2001071300033 20010713 00033 NM 2001 7 13 01FDEA00527 1 20010710 A 2782 651781823 ACTUATOR BOEING 727 727233 138408A NM L/E SLAT FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 276FE 22041 WHEN RETRACT FLAPS FROM 2 DEG TO 0 NR 7 LED FAILED TO RETRACT. REMOVED AND REPLACED RIGHT WING NR 7 SLAT ACTUATOR PER M M 27-81-032-4. OPS AND LEAK CK GOOD. 2 L 7 3 4F RT A3WE 2001071300034 20010713 00034 2001 7 13 01FDEA00528 4 20010710 A 2210 DAMPER BOEING 727 727233 138408A NM AUTOPILOT SYS FAULTY A FDEA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SO 25 258FE 20940 EXPERIENCED UNCOMMANDED YAW PULLED UPPER RUDDER YAW DAMPER AC & DC CB YAW DISCONTINUED. 2 L 7 3 4F RT A3WE 2001081500076 20010815 00076 NM 2001 8 15 01FDEA00529 1 20010710 A 2150 2040751 ACM BOEING 727 7272S2F 1384O81 NM A/C BAY FAILED A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 208FE 22930 BLUE/BLACK OILY SMOKE IN COCKPIT 3 MIN AFT T/O SEEM TO BE RIGHT AFT NR 3 BLD AND RT PACK TURN ON. *S/D* REMOVED AND RE PLACED RT AIR CYCLE MACHINE AND PERFORMED FUNCTIONAL CK PER MM 21-55-011-4. A/C OK TO CONTINUE. 2 L 7 3 4F A3WE 2001071300035 20010713 00035 NM 2001 7 13 01FDEA00532 1 20010710 A 2710 AILERON DOUG MD11 MD11F 3023600 NM WING MALFUNCTIONED A FDEA J A DUMP FUEL UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 607FE 48547 DURING FLAP/SLAT RET AFT T/O (AIL DEFLECT DISAG) ALERT LVL 2 CK LIST COMPLIED. REINSTALLED P1-880 FOR PRECAUTION A/C ST ILL DEFER, AC RELEASE PER MEL. 2 L 7 3 4F RT A22WE 2001083100150 20010831 00150 NM 2001 8 31 01FDEA00533 1 20010711 A 5243 DOOR BOEING 727 727247 138408F NM HYD SERVICE MISSING A FDEA O OTHER D INFLIGHT SEPARATION UK UNKNOWN 1 SO 25 236FE 21330 ON ARRIVAL FOUND HYDRAULIC SERVICING BAY DOOR TORN OFF & MISSING. INSTALLED BODY FAIRING 3519 PER SRM 51-30-02. 2 L 7 3 4F A3WE 2001081500081 20010815 00081 NM 2001 8 15 01FDEA00534 1 20010711 A 5270 PROXIMITY SWITCH BOEING 727 727227 1384078 NM CARGO DOOR FAULTY A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 486FE 21489 MAIN CARGO DOOR LIGHT ILLUM. PERFORMED QUICK REF HDBK PROC. DIVERT TO MSP. *S/D* REMOVED AND REPLACED MCD CTR PROX S W 29038 PER MM 52-34-009-5. AC OK FOR SERVICE. 2 L 7 3 4F A3WE 2001071300036 20010713 00036 WP 2001 7 13 01FDEA00536 1 20010711 A 5330 2932050S SKIN DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 SKIN FWD OF WHERE ENG NR 2 MATES HAS CRACKS AND CORROSION WHERE THE ENG DOOR ACTUATION FLEX SHAFT GOES THRU THE SKIN. R EMOVED AND REPLACED FRAME PER SRM 54-10-00, 51-31-01 & EA 8-5230-56137. 2 L 7 3 4F RT A22WE 2001071300037 20010713 00037 WP 2001 7 13 01FDEA00537 1 20010709 A 5320 ANGLE DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 L-ANGLE AFT CARGO, LWR DOOR SILL, INSIDE TORQUE BOX IS CORRODED. REMOVED AND REPLACED FRAME PER EA 8-5310-52551 & SRM 5 3-50-00. 2 L 7 3 4F RT A22WE 2001071300038 20010713 00038 WP 2001 7 13 01FDEA00538 1 20010709 A 5311 AFA39293 FRAME DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 BS 1831 LWR AFT FRAME IS CORRODED BEYOND LIMITS PER IAW DC-10 SRM 53-00-31 FIG 1B. REMOVED AND REPLACED FRAME PER IAW D AC AFA3929. 2 L 7 3 4F RT A22WE 2001071300039 20010713 00039 SO 2001 7 13 2001F00017 1 20010523 A 2140 A23D04 VALVE PIPER PA31 PA31350 7103110 SO HEATING SYS LEAKING A K NONE K FLUID LOSS IN INSP/MAINT 1 SO 05 4093W 160 318152176 WHILE PERFORMING AD AND SB ON JANITROL PN-A23D04 AIRCRAFT HEATER FUEL REGULATOR AND SHUTOFF VALVE FOUND UNIT TO BE LEAKI NG FUEL FROM ONE OF THE MOUNTING SCREW HOLES. NOTE: THIS UNIT MFG DATE 1/01 WHICH THE AD REQUIRES TO BE INSTALLED IF FO UND LEAKING. 1 L 7 2 3O A20SO 2001071300040 20010713 00040 SO 2001 7 13 2001F00018 1 20010531 A 5280 4752932 HINGE BRACKET PIPER PA31 PA31350 7103110 SO RT MLG BROKEN A L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NM 01 335WB 317952135 PILOT REPORTED RIGHT GEAR UNSAFE LIGHT ILLUMINATED, AFTER 2 LOWER FLY BY. THE GEAR APPEARED DOWN AND LOCKED WITH ONLY THE RIGHT GEAR DOOR STAYING OPEN. THE PILOT MADE AN UNEVENTFUL LANDING AND THE FORWARD INBOARD GEAR DOOR HINGE WAS CONF IRMED BROKEN. 1 L 7 2 3O A20SO 2001071300041 20010713 00041 NM 2001 7 13 COOSDR010039 1 20010621 A 5311 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 29SW 21340 PAX CABIN, BS 727, AT STR 14L LEVEL FRAME CRACKED. PROBABLE CAUSE IS FATIGUE. 2 L 7 2 4F A16WE 2001071300042 20010713 00042 NM 2001 7 13 COOSDR010043 1 20010621 A 5312 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 29SW 21340 AFT PRESSURE BULKHEAD - BS 1016 WEB CRACKED, Y CHORD INSPECTION. 2 L 7 2 4F A16WE 2001071300043 20010713 00043 NM 2001 7 13 COOSDR010044 1 20010621 A 5711 SPAR BOEING 737 7372H4 138448C NM CENTER WING CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 29SW 21340 WING - CENTER WING BOX - REAR SPAR CRACKED - STA 663.0/ RBL6.150/ WL 170.4 2 L 7 2 4F A16WE 2001071300044 20010713 00044 NM 2001 7 13 COOSDR010049 1 20010712 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE DENTED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 29SW 21340 EXTERNAL FUSELAGE, BETWEEN BS 423 AND BS 435 BETWEEN STR 20R, SKIN DENTED. 2 L 7 2 4F A16WE 2001071300045 20010713 00045 NM 2001 7 13 COOSDR010050 1 20010712 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 29SW 21340 EXTERNAL FUSELAGE, E & E COMPARTMENT, DOOR AROUND CUT OUT SKIN WITH SHARP EDGES AND CRACKED. 2 L 7 2 4F A16WE 2001071300046 20010713 00046 NM 2001 7 13 COOSDR010052 1 20010712 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 03 29SW 21340 FORWARD C/C, FLOOR BEAM, LOWER CHORD, RBL 25 INCHES, WL 201 WITH CRACK. 2 L 7 2 4F A16WE 2001071300047 20010713 00047 NM 2001 7 13 COOSDR010053 1 20010712 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CANNING B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 03 29SW 21340 EXT. FUSELAGE BS 864 BETWEEN STRINGER 16L AND 17L, SKIN WITH OIL CAN. 2 L 7 2 4F A16WE 2001071300048 20010713 00048 NM 2001 7 13 COOSDR010054 1 20010712 A 5313 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 03 29SW 21340 PAX CABIN, BS 727+9INCHES, STRINGER NR 1 CRACKED. 2 L 7 2 4F A16WE 2001071300049 20010713 00049 NM 2001 7 13 COOSDR010056 1 20010712 A 5313 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 29SW 21340 UPPER FUSELAGE MAIN CABIN STRINGER 11R AT BS 540, CRACKED. 2 L 7 2 4F A16WE 2001071300050 20010713 00050 NM 2001 7 13 COOSDR010060 1 20010712 A 5313 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 29SW 21340 FUSELAGE STRINGER SECTION FROM BS 429 TO BS 450 AT STR 4R, CRACKED. 2 L 7 2 4F A16WE 2001071300051 20010713 00051 NM 2001 7 13 COOSDR010061 1 20010712 A 5313 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 03 29SW 21340 FUSELAGE STRINGER SECTION FROM BS 306 TO BS 326 AT STR 4R, CRACKED. 2 L 7 2 4F A16WE 2001071300052 20010713 00052 NM 2001 7 13 COOSDR010062 1 20010712 A 5311 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 29SW 21340 FUSELAGE FRAME SECTION AT BS 328 BETWEEN STR 1R AND 4R, CRACKED. 2 L 7 2 4F A16WE 2001071300053 20010713 00053 NM 2001 7 13 COOSDR010063 1 20010712 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SW 23 29SW 21340 FUSELAGE FLOOR BEAM SECTION UPPER CHORD AT BS 328 BETWEEN RBL 24.5 AND RBL40, CRACKED. 2 L 7 2 4F A16WE 2001071300054 20010713 00054 NM 2001 7 13 COOSDR010064 1 20010712 A 5313 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 29SW 21340 FUSELAGE STRINGER SECTION 27L FROM BS 960 TO BS 1016, CRACKED. 2 L 7 2 4F A16WE 2001071300055 20010713 00055 NM 2001 7 13 COOSDR010066 1 20010712 A 5754 SKIN BOEING 737 7372H4 138448C NM L/E SLAT DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 29SW 21340 LEFT WING SLAT NR 3 UPPER SKIN DELAMINATED. 2 L 7 2 4F A16WE 2001071300056 20010713 00056 NM 2001 7 13 COOSDR010067 1 20010712 A 5755 SKIN BOEING 737 7372H4 138448C NM SPOILER DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 29SW 21340 LEFT WING, GROUND SPOILER NR4 UPPER SKIN DELAMINATED. 2 L 7 2 4F A16WE 2001071300057 20010713 00057 NM 2001 7 13 COOSDR010068 1 20010712 A 5754 SKIN BOEING 737 7372H4 138448C NM L/E FLAP DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 29SW 21340 LEFT WING, IB FORE FLAP UPPER SKIN DELAMINATED. 2 L 7 2 4F A16WE 2001071300058 20010713 00058 NM 2001 7 13 COOSDR010069 1 20010712 A 5755 SKIN BOEING 737 7372H4 138448C NM SPOILER DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 29SW 21340 RIGHT WING, FLIGHT SPOILER NR 8 UPPER SKIN, DELAMINATED. 2 L 7 2 4F A16WE 2001071300059 20010713 00059 NM 2001 7 13 COOSDR010070 1 20010712 A 5755 SKIN BOEING 737 7372H4 138448C NM SPOILER DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 29SW 21340 LEFT WING GROUND SPOILER NR 5 WITH UPPER SKIN DELAMINATED. 2 L 7 2 4F A16WE 2001071300060 20010713 00060 NM 2001 7 13 COOSDR010071 1 20010712 A 5320 ANGLE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 29SW 21340 LOWER FUSELAGE RIGHT WHEEL WELL, BULKHEAD BS 727, BL 0 AND WL 208 ANGLE, CRACKED. 2 L 7 2 4F A16WE 2001071300061 20010713 00061 NM 2001 7 13 COOSDR010072 1 20010712 A 5311 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 29SW 21340 LOWER FUSELAGE LEFT WHEEL WELL, BS 663.75 LBL 25 AND WL 208 CHORD, CRACKED. 2 L 7 2 4F A16WE 2001071300062 20010713 00062 NM 2001 7 13 COOSDR010073 1 20010712 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM FLOORBEAM CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 29SW 21340 PAX CABIN FROM BS 520 RBL 25 AND WL 208, FLOOR BEAM CRACKED. 2 L 7 2 4F A16WE 2001071300063 20010713 00063 NM 2001 7 13 COOSDR010048 1 20010712 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE DENTED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 29SW 21340 EXTERNAL FUSELAGE BS890 BETWEEN STR 20R AND STR 21R DENTED. 2 L 7 2 4F A16WE 2001071300064 20010713 00064 NM 2001 7 13 COOSDR010051 1 20010712 A 5313 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 29SW 21340 AFT C/C BAY, STA967, STR 27R CORRODED. 2 L 7 2 4F A16WE 2001071300065 20010713 00065 NM 2001 7 13 COOSDR010055 1 20010712 A 5313 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 29SW 21340 UPPER FUSELAGE MAIN CABIN STRINGER 11L AT BS 540 CRACKED. 2 L 7 2 4F A16WE 2001071300066 20010713 00066 NM 2001 7 13 COOSDR010057 1 20010712 A 5313 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 29SW 21340 FUSELAGE STRINGER SECTION 9R FROM BS 755 TO BS 780, CRACKED. 2 L 7 2 4F A16WE 2001071300067 20010713 00067 NM 2001 7 13 COOSDR010058 1 20010712 A 5313 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 29SW 21340 FUSELAGE STRINGER SECTION 9L FROM BS 727A+7 TO BS 727B+12, CRACKED. 2 L 7 2 4F A16WE 2001071300068 20010713 00068 NM 2001 7 13 COOSDR010059 1 20010712 A 5311 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 29SW 21340 FUSELAGE FRAME SECTION AT BS 344 FROM STR. 4L AND STR 6L, CRACKED. 2 L 7 2 4F A16WE 2001071300069 20010713 00069 NM 2001 7 13 HN6R0000197 1 20010618 A 5313 0705TG STRINGER BOEING 737 737400 NM FUSELAGE CORRODED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 932NU 25248 AT STA 847, LBL 72, WL208, STRINGER 17 IS CORRODED. CAUSE UNKNOWN. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INS TALLED. 2 L 7 2 4F RT A16WE 2001071300070 20010713 00070 NM 2001 7 13 HN6R0000198 1 20010618 A 5313 STRINGER BOEING 737 737400 NM FUSELAGE CORRODED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 932NU 25248 STA 867, LBL 72, WL 208, THE STRINGER 17 IS CORRODED. CAUSE UNKNOWN. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTA LLED. 2 L 7 2 4F RT A16WE 2001071300071 20010713 00071 NM 2001 7 13 HN6R0000203 1 20010618 A 5320 654587570 SILL BOEING 737 737400 NM FUSELAGE CORRODED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 932NU 25248 CORROSION ON LEFT HAND MOPSIL BS 360- BS 300, WL208. CAUSE UNKNOWN. REMOVED AND REPLACED MOP SILL. 2 L 7 2 4F RT A16WE 2001071300072 20010713 00072 NM 2001 7 13 HN6R0000205 1 20010618 A 5320 654587570 SILL BOEING 737 737400 NM FUSELAGE CORRODED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 932NU 25248 CORROSION ON RIGHT HAND MOP SILL AT BS 294 TO BS 335, WL208. CAUSE UNKNOWN. REMOVED AND REPLACED MOP SILL. 2 L 7 2 4F RT A16WE 2001071300073 20010713 00073 NM 2001 7 13 HN6R0000212 1 20010618 A 5311 FRAME BOEING 737 737400 NM FUSELAGE CRACKED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 932NU 25248 BS 400 FRAME IS CRACKED AT PSU RAIL ATTACHMENT BRACKET INBOARD FASTENER (LEFT HAND SIDE). CAUSE UNKNOWN. REMOVED DAMAG E, FABRICATED REPAIR PARTS AND INSTALLED. 2 L 7 2 4F RT A16WE 2001071300074 20010713 00074 NM 2001 7 13 HN6R0000213 1 20010618 A 5311 FRAME BOEING 737 737400 NM FUSELAGE CRACKED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 932NU 25248 BS 400 FRAME IS CRACKED AT PSU RAIL ATTACHMENT BRACKET INBOARD FASTENER (RIGHT SIDE). CAUSE UNKNOWN. REMOVED DAMAGE, F ABRICATED REPAIR PARTS AND INSTALLED. 2 L 7 2 4F RT A16WE 2001071300075 20010713 00075 NM 2001 7 13 HN6R0000214 1 20010618 A 5311 FRAME BOEING 737 737400 NM FUSELAGE CRACKED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 932NU 25248 BS 727B FRAME IS CRACKED AT PSU ATTACHMENT BRACKET INBOARD FASTENER (LEFT SIDE). CAUSE UNKNOWN. REMOVED DAMAGE, FABRIC ATED REPAIR PARTS AND INSTALLED. 2 L 7 2 4F RT A16WE 2001071300076 20010713 00076 NM 2001 7 13 HN6R0000215 1 20010618 A 5311 FRAME BOEING 737 737400 NM FUSELAGE CRACKED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 932NU 25248 BS 727B FRAME IS CRACKED AT PSU RAIL ATTACHMENT BRACKET INBOARD FASTENER (RIGHT SIDE). CAUSE UNKNOWN. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED. 2 L 7 2 4F RT A16WE 2001071300077 20010713 00077 NM 2001 7 13 HN6R0000216 1 20010618 A 5311 FRAME BOEING 737 737400 NM FUSELAGE CRACKED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 932NU 25248 BS 727D FRAME IS CRACKED AT PSU RAIL ATTACHMENT BRACKET INBOARD FASTENER (RIGHT SIDE). CAUSE UNKNOWN. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED. 2 L 7 2 4F RT A16WE 2001071300078 20010713 00078 NM 2001 7 13 HN6R0000217 1 20010618 A 5311 FRAME BOEING 737 737400 NM FUSELAGE CRACKED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 932NU 25248 BS 747 FRAME IS CRACKED AT PSU RAIL ATTACHMENT BRACKET INBOARD FASTENER (RIGHT SIDE). CAUSE UNKNOWN. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED. 2 L 7 2 4F RT A16WE 2001071300080 20010713 00080 NM 2001 7 13 HN6R0000219 1 20010618 A 5311 FRAME BOEING 737 737400 NM FUSELAGE CRACKED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 932NU 25248 BS 867 FRAME IS CRACKED AT PSU RAIL ATTACHMENT BRACKET INBOARD FASTENER (LEFT HAND SIDE). CAUSE UNKNOWN. REMOVED DAMAG E, FABRICATED REPAIR PARTS, AND INSTALLED. 2 L 7 2 4F RT A16WE 2001071300081 20010713 00081 NM 2001 7 13 HN6R0000220 1 20010618 A 5311 FRAME BOEING 737 737400 NM FUSELAGE CRACKED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 932NU 25248 BS 867 FRAME IS CRACKED AT PSU RAIL ATTACHMENT BRACKET INBOARD FASTENER (RIGHT SIDE). CAUSE UNKNOWN. REMOVED DAMAGE, FABRICATION REPAIR PARTS AND INSTALLED. 2 L 7 2 4F RT A16WE 2001071300082 20010713 00082 NM 2001 7 13 HN6R0000243 1 20010618 A 5310 CREASE BEAM BOEING 737 737400 NM FUSELAGE CORRODED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 932NU 25248 AT BS 380 TO 390 RBL 65, WL 207, THERE IS CORROSION ON THE CREASE BEAM. CAUSE UNKNOWN. REMOVED CORROSION, FABRICATED RE PAIR PARTS AND INSTALLED. 2 L 7 2 4F RT A16WE 2001071300083 20010713 00083 NM 2001 7 13 HN6R0000244 1 20010619 A 5315 FLOORBEAM BOEING 737 737400 NM FUSELAGE CORRODED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 932NU 25248 CORROSION ON FLOOR BEAM AT BS 294.5, RBL45, WL208. CAUSE UNKNOWN. REMOVED DAMAGE FABRICATED REPAIR PART AND INSTALLED. 2 L 7 2 4F RT A16WE 2001071300084 20010713 00084 2001 7 13 SWAA011829 4 20010623 A 2565 63551101 SLIDE BOEING 737 7377H4 NM SERVICE DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 798SW 28436 AFT SVC DOOR EMERGENCY EVAC SLIDE DEPLOYED ON GROUND. REMOVED AND REPLACED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001071300085 20010713 00085 NM 2001 7 13 SWAA011831 1 20010624 A 3350 100031 GROUND WIRE BOEING 737 7377H4 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 732SW 27864 DURING SCHEDULED PM CHECK, FOUND EXIT LIGHT INOP AT FWD CEILING. SECURED GROUND WIRE AT CEILING GROUNDING BLOCK PER MM. 2 L 7 2 4F RT A16WE 2001071300086 20010713 00086 NM 2001 7 13 SWAA011833 1 20010625 A 3350 6556633 LIGHT BOEING 737 7377H4 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 700GS 27835 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED GROUNDING BLOCK GD 38 02S PER MM. 2 L 7 2 4F RT A16WE 2001071300087 20010713 00087 NM 2001 7 13 UPS01236298 1 20010702 A 5310 WEB BOEING 727 72727C 138400J NM BS 1183 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 909UP 19115 INSPECTION TYPE:C CORROSION ON CABIN FLOOR WEB FWD OF BS 1183 BLK OF BBL 12R ***CPCP*** WEB REPLACED IAW SRM 51-10-0 1 2 L 7 3 4F A3WE 2001071300088 20010713 00088 NM 2001 7 13 UPS01236300 1 20010702 A 5510 SKIN BOEING 727 72727C 138400J NM STAB STA. 80 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 909UP 19115 INSPECTION TYPE:C CORROSION OF RH STAB SKIN UPPER SURFACE & RIVET PULLED @ STAB STA 80 APPROX FWD OF REAR SPAR ***CPCP* ** REPAIR CARRIED OUT IAW SRM 55-10-3 2 L 7 3 4F A3WE 2001071300089 20010713 00089 NM 2001 7 13 UPS01236301 1 20010703 A 5320 INTERCOSTAL BOEING 727 72727C 138400J NM BS 830 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 909UP 19115 INSPECTION TYPE:C CRACK ON INTERCOSTAL AT STR 17R AT BS 830 INTERCOSTAL REPLACED IAW SRM 51-30-1 2 L 7 3 4F A3WE 2001071300090 20010713 00090 NM 2001 7 13 UPS01236308 1 20010701 A 5330 LAP JOINT BOEING 727 72727C 138400J NM STA1110-1165 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 910UP 19117 INSPECTION TYPE:C SUSPECT CORROSION AT LAP JOINT STA 1110 TO 1165 STR4L DAMAGE REAPIRED IAW B727-5330-0509 APPENDIX 8.3 2 L 7 3 4F A3WE 2001071300091 20010713 00091 NM 2001 7 13 UPS01236309 1 20010702 A 2780 RIB BOEING 727 72727C 138400J NM #6 SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 909UP 19115 INSPECTION TYPE:C SUSPECT CRACK IN #6 SLAT RIB, O/B OF SLAT ACTUATOR DAMAGED RIB REPAIRED IAW SRM 57-30-3 2 L 7 3 4F A3WE 2001071300092 20010713 00092 NM 2001 7 13 UPS01236313 1 20010701 A 3200 SUPPORT BRACKET BOEING 727 72727C 138400J NM BS 910 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 909UP 19115 INSPECTION TYPE:C BS 910 FRAME FWD FLANGE LWR CORNER SUPPORT BRACKET CRACKED REPAIR CARRIED OUT IAW SRM 51-20-01, 51 -30-2 2 L 7 3 4F A3WE 2001071300093 20010713 00093 NM 2001 7 13 UPS01236314 1 20010709 A 5310 STRINGER BOEING 727 72727C 138400J NM BS 676 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 909UP 19115 INSPECTION TYPE:C END OF STRINGER 15 @ BS 676 LH IS CRACKED REPAIR CARRIED OUT IAW 51-30-2 & 53-10-3 2 L 7 3 4F A3WE 2001071300094 20010713 00094 NM 2001 7 13 SWAA011836 1 20010622 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 39 & WL 208. REPAIRED FLOORBEAM PER SRM & SWA RA. 2 L 7 2 4F RT A16WE 2001071300095 20010713 00095 NM 2001 7 13 SWAA011837 1 20010622 A 5312 6517582 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED D-CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17 & WL 230. REPAIRED WEB PER BFG ER. 2 L 7 2 4F RT A16WE 2001071300096 20010713 00096 2001 7 13 SWAA011838 4 20010625 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC S LIDE PER MM. 2 L 7 2 4F RT A16WE 2001072700180 20010727 00180 EA 2001 7 27 COMA0160391 1 20010618 A 5754 601R140022 FLAP CNDAIR CL600 CL6002B19 EA RT WING CHAFED A COMA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 SO 01 986CA 9475 7174 RT INBD FORE-FLAP CHAFFED AT IMPACT STRIPS.PERFORMED S.B. 601R-57-022 2 L 7 2 4F RT A21EA 2001071300097 20010713 00097 NM 2001 7 13 SWAA011839 1 20010625 A 5523 BACB28AMO7 BUSHING BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED C2 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB ATTACH BUSHINGS PE R MM. 2 L 7 2 4F RT A16WE 2001071300098 20010713 00098 NM 2001 7 13 SWAA011841 1 20010622 A 5315 6545410 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED D-CHECK, FOUND CENTER LONGITUDINAL FLOORBEAM CRACKED AT BS 660 & BS 663. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2001071300099 20010713 00099 NM 2001 7 13 SWAA011843 1 20010627 A 3397 BR2013 WIRE BOEING 737 7377H4 1384404 NM CABIN EXPOSED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 743SW 29279 EEPLS WIRES EXPOSED AT ROW 8. SECURED EEPLS WIRES PER MM. 2 L 7 2 4F RT A16WE 2001071300100 20010713 00100 NM 2001 7 13 SWAA011844 1 20010627 A 3350 6104789 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT FWD FUSELAGE EXTERIOR. REMOVED AND REPLACED BATTER Y PACK PER MM. 2 L 7 2 4F A16WE 2001071300101 20010713 00101 NM 2001 7 13 SWAA011845 1 20010626 A 3350 300432 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED C4 CHECK, FOUND LOWER AND FWD LEFT OVERWING EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001071300102 20010713 00102 NM 2001 7 13 SWAA011847 1 20010627 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 380SW 26587 DURING SCHEDULED A1 CHECK, FOUND EEPLS INOP. REPAIRED EEPLS WIRES PER MM. 2 L 7 2 4F RT A16WE 2001071300103 20010713 00103 NM 2001 7 13 SWAA011848 1 20010620 A 3350 7003665 BALLAST BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED D-CHECK, FOUND RT OVERWING EXIT LIGHT INOP AND LENS BROKEN. REMOVED AND REPLACED BALLAST AND LENS PER MM. 2 L 7 2 4F RT A16WE 2001071300104 20010713 00104 2001 7 13 SWAA011854 4 20010627 A 2565 22D22900131 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 063SW 22061 AFTER FERRY FLIGHT TO HOU, FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED EMERGENCY E VAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001071300105 20010713 00105 EA 2001 7 13 COMA0160392 1 20010618 A 2780 601R140021 FLAP CNDAIR CL600 CL6002B19 EA CHAFED A COMA O OTHER F FLT CONT AFFECTED IN INSP/MAINT 1 SO 01 986CA 9475 7174 LT INBD FORE-FLAP CHAFFED AT IMPACT STRIPS.PERFORMED S.B. 601R-57-022. 2 L 7 2 4F RT A21EA 2001071300106 20010713 00106 NE 2001 7 13 SWAA011855 2 20010627 A 7532 3017927010 ACTUATOR BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 1 ENGINE SHEARED A SWAA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 07 389SW 26592 AIR TURNBACK, DURING TAKEOFF AND CLIMB OVER TEMP LIGHT ON 1 ENGINE ILLUMINATED. REMOVED AND REPLACED VBV ACTUATOR SHAFT AND MASTER BALL SCREW ACTUATOR PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2001071300107 20010713 00107 EA 2001 7 13 COMA0160393 1 20010614 A 7830 22850200139 TORQUE BOX CNDAIR CL600 CL6002B19 EA FAILED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 986CA 10066 7174 LEFT THRUST REVERSER BLOCKER DOOR HAS BROKEN ATTACH BRACKET AT 10 O'CLOCK POSITION.REMOVED AND REPLACED LEFT THRUST REVE RSER TORQUE BOX ASSY. 2 L 7 2 4F RT A21EA 2001071300108 20010713 00108 2001 7 13 SWAA011856 4 20010628 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 063SW 22061 AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. RE-ADJUSTED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001071300109 20010713 00109 NM 2001 7 13 SWAA011857 1 20010628 A 2560 P207001 FLASHLIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 511SW 24188 EMERGENCY FLASHLIGHT INOP AT AFT UPPER POSITION. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2001071300110 20010713 00110 NM 2001 7 13 SWAA011858 1 20010628 A 3350 6107789 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED A1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 2001071300111 20010713 00111 2001 7 13 SWAA011861 4 20010627 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 331SW 23695 DURING SCHEDULED RON CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EMERG ENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001071300112 20010713 00112 EA 2001 7 13 COMA0160394 1 20010620 A 2780 601R40022 FLAP CNDAIR CL600 CL6002B19 EA CHAFED A COMA O OTHER F FLT CONT AFFECTED IN INSP/MAINT 1 SO 01 946CA 7072 RIGHT INBD FORE-FLAP CHAFFED AT IMPACT STRIPS.PERFORMED S/B 601R-57-022. 2 L 7 2 4F RT A21EA 2001071300113 20010713 00113 EA 2001 7 13 COMA0160397 1 20010621 A 5322 60135006 WEB CNDAIR CL600 CL6002B19 EA CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 917CA 18559 7017 DURING COMPLIANCE OF ALERT SERVICE BULLETIN A601R-53-059 THE UPPER WEB OF THE ENGINE SUPPORT BEAM WAS FOUND TO BE CRACKE D AT LBL 7.5 EXTENDING FROM FS 639.39 - 639.00REPAIRED IN ACCORDANCE WITH REO 601R-53-61-345. 2 L 7 2 4F RT A21EA 2001071300114 20010713 00114 EA 2001 7 13 COMA0160398 1 20010621 A 5322 60135006 WEB CNDAIR CL600 CL6002B19 EA CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 917CA 18559 7017 DURING COMPLIANCE OF ALERT SERVICE BULLETIN A601R-53-059 THE LOWER WEB OF THE ENGINE SUPPORT BEAM WAS FOUND TO BE CRACKE D AT LBL 7.5, F.S. 638.625.REPAIRED IN ACCORDANCE WITH REO 601R-53-61-345. 2 L 7 2 4F RT A21EA 2001071300115 20010713 00115 NM 2001 7 13 SWAA011862 1 20010628 A 5752 6546455 TAB BOEING 737 7373L9 1384470 NM AILERON DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SCHEDULED SERVICE CHECK, FOUND LT AILERON TAB DELAMINATED. REMOVED AND REPLACED AILERON TAB PER MM. 2 L 7 2 4F RT A16WE 2001071300116 20010713 00116 NM 2001 7 13 SWAA011867 1 20010630 A 5312 6517582 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17.1, WL 185. REPAIRED VERTICAL BEAM PER SW A RA. 2 L 7 2 4F A16WE 2001071300117 20010713 00117 EA 2001 7 13 COMA0160401 1 20010625 A 5346 60135006 BEAM CNDAIR CL600 CL6002B19 EA CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 936CA 16506 7043 DURING INCORORATION OF COMAIR EO 53-021 (VISUAL INSP. OF THE ENGINE SUPPORT BEAM) THE ENGINE SUPPORT BEAM WAS FOUND CRCK ED 1.5" ON RH SIDE LOWER WEB I/B CORNER AT FS 621.0 - FS 640.0PERFORMED A TEMPORARY MAJOR REPAIR TO ENGINE SUPPORT BEAM LOWER WEB I/B CORNER AT FS 621.0 - FS 640.0 I/A/W CRJ REO 601R-53-61-358. 2 L 7 2 4F RT A21EA 2001071300118 20010713 00118 2001 7 13 SWAA011868 4 20010630 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 645SW 28330 FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001071300119 20010713 00119 2001 7 13 SWAA011871 4 20010630 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 331SW 23695 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001071300120 20010713 00120 2001 7 13 SWAA011875 4 20010629 A 2565 22D22901 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EMER GENCY EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001071300121 20010713 00121 2001 7 13 SWAA011879 4 20010627 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 641SW 27714 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001071300122 20010713 00122 NM 2001 7 13 SWAA011881 1 20010630 A 3350 20131A BATTERY BOEING 737 7373A4 1384585 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED PMC CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT LT OVERWING. REMOVED AND REPLACED EMERGENCY EXIT LIGHT B ATTERY PER MM. 2 L 7 2 4F RT A16WE 2001071300123 20010713 00123 EA 2001 7 13 COMA0160404 1 20010627 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA FAILED A COMA K NONE O OTHER DE DESCENT 1 SO 01 958CA 11500 7111 FLAP FAIL CAUTION AT 42 DEGREES DURING DESCENT INTO SDF.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "SECOND EVENT" MA INTENANCE ACTION, PARAGRAPH (B)3 (D AND E) 4 AND REPLACED THE RIGHT BRAKE POSITION SENSING UNIT. 2 L 7 2 4F RT A21EA 2001071300124 20010713 00124 NM 2001 7 13 SWAA011883 1 20010630 A 5320 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 521SW 25320 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT STR 16R, BS 400 & BS 480. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001071300125 20010713 00125 NM 2001 7 13 SWAA011889 1 20010629 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN EXPOSED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 640SW 27713 EEPLS LOOSE AND WIRES EXPOSED AT ROW 7. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001071300126 20010713 00126 EA 2001 7 13 COMA0160406 1 20010626 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA FAILED A COMA K NONE O OTHER DE DESCENT 1 SO 01 958CA 11499 7111 FLAP FAIL CAUTION AT 18 DEGREES DURING DESCENT INTO CVG.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIRST EVENT" MAI NTENANCE ACTION, PARAGRAPH (B) 1,2,3, (A,B,C AND E) AND REPLACED THE LEFT BRAKE POSITON SENSING UNIT. 2 L 7 2 4F RT A21EA 2001071500001 20010715 00001 EA 2001 7 15 JBXA000308 1 20010714 A 5210 840534 PROXIMITY SWITCH CNDAIR CL600 CL6002B19 EA FAILED A JBXA A D UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 05 571ML 7209 After T.O. at RDU 1000' pax door out handle caution msg illuminated 2 L 7 2 4F RT A21EA 2001071600002 20010716 00002 EA 2001 7 16 20010606CW006 1 20010423 A 2450 HARNESS BOEING 234 234 1385049 EA NR 2 ENGINE CORRODED E CHIR A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 245CH MJ022 AT TAKEOFF AND INTO CRUISE FLIGHT, THE NR 2 ENGINE BEGAN OSCILLATING AND GOING TO HIGH SIDE. THE NR 2 ENGINE WAS BROUGH T BACK TO THE GROUND POSITION AND HELICOPTER WAS RETURNED TO THE SERVICE LANDING. TROUBLESHOOTING REVEALED CORROSION/ R ESISTANCE IN THE NR 2 ENGINE, NR 2 DECK CANNON PLUG 103P17. THE NR 2 ENGINE N2 HARNESS WAS REPLACED, OPERATIONALLY CHEC KED GOOD AND THE HELICOPTER RETURNED TO SERVICE. 2 G 7 2 4U H9EA 2001071600005 20010716 00005 SO 2001 7 16 20010607CW009 2 20010430 A 8520 536379 BOLT CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO CRANKSHAFT SHEARED D HYIA K NONE O OTHER TX TAXI/GRND HDL 1 NE 01 406GA 900 900 402C0329 RIGHT ENGINE WOULD NOT START. FORWARD DRIVE GEAR FOR STARTER ADAPTOR LOOSE IN ACCESSORY CASE. ALL 6 BOLTS SHEARED OFF CRANKSHAFT END. 1 L 7 2 3O 3 O A7CE E8CE 2001071600006 20010716 00006 SO 2001 7 16 20010608CW003 1 20010523 A 5541 4044000 RIB PIPER PA31 PA31350 7103110 SO RUDDER CRACKED B R2JR K NONE O OTHER IN INSP/MAINT 1 EA 21 13FS 3692 318352024 WHILE C/U CHECKLIST ITEM FOR RUDDER BALANCE WEIGHT ON ANNUAL INSPECTION: FOUND WEIGHT LOOSE, YET BOLTS WERE TIGHT. INV ESTIGATION SHOWED UPPER RIB ON RUDDER BROKEN OUT UNDER BALANCE WEIGHT. THIS ITEM INSPECTED 149 HOURS PREVIOUS AND FOUND TIGHT. PERIODIC REMOVAL OF BALANCE WEIGHT TO CHECK STRUCTURE FOR CRACKS NEEDED. COULD CAUSE LOSS OF CONTROL OF AIRCRA FT, CANNOT SEE STRUCTURE WITHOUT REMOVING CAP AND WEIGHT. 1 L 7 2 3O A20SO 2001071600012 20010716 00012 CE 2001 7 16 20010612CW003 1 20010515 A 5511 07321014 SPAR CESSNA CESSNA 182 182S 2072701 CE LYC O540 IO540AB1A5 EA HORIZ STAB CRACKED A VPFG K NONE O OTHER IN INSP/MAINT 1 SO 03 63CE 1600 169502 18280357 L2657048A REAR STABILIZER/ REAR SPAR LEFT SIDE/ CRACKED. 1 H 7 1 3O 3 O NT 3A13 1E4 2001071600015 20010716 00015 EA 2001 7 16 20010612CW006 1 20010604 A 5610 6003303021 WINDOW CNDAIR CL600 CL6001A11 1900302 EA COCKPIT DEBONDED B K NONE O OTHER IN INSP/MAINT 1 NM 03 103HB 1059 PILOTS LEFT SIDE WINDOW WAS DISBONDED AT FORWARD VERTICAL EDGE. 2 L 7 2 4F RT A21EA 2001071600016 20010716 00016 EA 2001 7 16 20010612CW007 1 20010604 A 5610 6003303025 WINDSHIELD CNDAIR CL600 CL6001A11 1900302 EA COCKPIT DELAMINATED E K NONE O OTHER IN INSP/MAINT 1 NM 03 103HB 1059 OUTER FACE PLY DELAMINATION OF LEFT HAND PILOTS WINDSHIELD. PLY SEPARATION WAS BEYOND LIMITS OF MANUFACTURES STRUCTURAL REPAIR MANUAL TO CONTINUE OPERATION. 2 L 7 2 4F RT A21EA 2001071600017 20010716 00017 CE 2001 7 16 20010612CW008 1 20010410 A 2121 45053 IMPELLER CESSNA 650 650 2076802 CE BLOWER DISINTEGRATED E DXTA K NONE J WARNING INDICATION NR NOT REPORTED 1 GL 07 782QS 2164 2164 7082 WRITE-UP, WEMAC BOOST INOPERATIVE, PART ON ORDER. FOUND FAN CASE IMPELLER HAD DISINTEGRATED. 2 L 7 2 4F A9NM 2001071600018 20010716 00018 EU 2001 7 16 20010612CW009 1 20010524 A 2120 66439353051 DUCT ISRAEL GALAXY GALAXY 4500307 EU CABIN LEAKING B UO2R K NONE O OTHER NR NOT REPORTED 1 GL 19 414KD 13 13 022 LEFT HAND CABIN INTERIOR UPPER CONDITIONED AIR DUCT WAS REMOVED FROM AIRCRAFT DUE TO AIR LEAKING FROM OUTBOARD OF DUCT. LEAKS WERE LOCATED DURING BENCH PRESSURE TESTING TO 5 PSI. REPAIRED LEAKS PER SPECIFICATIONS, PROBABLE CAUSE WOULD BE A MANUFACTURE DEFECT. 2 L 7 2 4F RT A53NM 2001071600019 20010716 00019 NE 2001 7 16 20010612CW010 2 20010420 A 8530 116733CP ROCKER DOUG DC3 DC3C 3021457 WP PWA R1830 R1830* 52020 NE NR 5 CYLINDER BROKEN E VLLA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 GL 05 36AP 2666 166 13439 IN CRUISE FROM TOL TO CYOO, RIGHT ENGINE STARTED RUNNING ROUGH. DIVERTED TO IAG. FOUND NR 5 CYLINDER EXHAUST ROCKER AS SEMBLY BROKEN. EXHAUST VALVE WOULD NOT OPEN. 2 L 7 2 4R 4 R A669 5E4 2001071600020 20010716 00020 SO 2001 7 16 20010612CW011 2 20010408 A 7310 FUEL LINE BEECH 58 58 1152740 CE CONT O520 IO520C 17032 SO FUEL SYS LEAKING E BSYA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 525GW TH557 RT ENGINE CLIMBING OUT, AROUND 3000 FEET , NOTICED F/F DOWN TO 12 GPM FOUND FUEL LEAK BETWEEN FUEL LINE AND FUEL MANIFOL D. REPAIRED FUEL LEAK, OPS CHECKED GOOD. 1 L 7 2 3O 3 O 3A16 E5CE 2001071600021 20010716 00021 GL 2001 7 16 20010612CW012 3 20010518 A 6111 S84B0 BLADE BEECH 33 E33C 1151432 CE CONT O520 IO520* 17032 SO MCAULY 2A36C 2A36C* GL PROPELLER CRACKED B W59R K NONE O OTHER IN INSP/MAINT 1 WP 07 7735R 2010 1310 CJ8 BLADE FOUND CRACKED IN THE SECOND RETENTION THREAD DURING PENETRANT INSPECTION PERFORMED AT OVERHAUL. NO RED DYE LEAKAG E REPORTED. NO ABNORMAL VIBRATION REPORTED. 1 L 7 1 3O 3 O 3A15 E5CE 5 C P880 2001071600025 20010716 00025 EU 2001 7 16 20010612CW016 1 20010529 A 2131 4AS7810052005 CONTROLLER ISRAEL GALAXY GALAXY 4500307 EU CABIN PRESSURE FAILED E UO2R O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 19 414DH 29 29 023 DEFECTIVE UNIT CAUSES AIRCRAFT TO AUTO PRESSURIZE, EICAS MISCOMPARE MESSAGE AND FAULT LIGHT TO ILLUMINATE. NO PROBABLE CAUSE FOR CABIN PRESSURE CONTROLLER FAILURE. 2 L 7 2 4F RT A53NM 2001071600028 20010716 00028 CE 2001 7 16 20010613CW001 1 20010522 A 2750 DIODE LEAR 25 25D 5170514 CE FLAP SYS FAILED E MXIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 EA 17 321GL 289 FLAP CIRCUIT BREAKER POPS WHEN FLAPS ARE SELECTED DOWN. CORRECTIVE ACTION: FOUND DIODE ON TB-28 IN RIGHT MAIN LANDING GEAR. WHEEL WELL SHORTED. INSTALLED NEW DIODE. PROBABLE FAILURE RELATED TO DIODE AND PC BOARD BEING EXPOSED TO ALL WEATHER ELEMENTS, CORROSION. 2 L 7 2 4J A10CE 2001071600030 20010716 00030 SO 2001 7 16 20010613CW003 1 20010521 A 3222 402312 BOLT PIPER PA34 PA34200 7103405 SO TORQUE LINK SEIZED D K NONE O OTHER LD LANDING 1 EA 25 24TB 1330 347250047 PILOT UNABLE TO EXTEND LANDING GEAR AND HAVE ALL THREE DOWN AND LOCKED. LANDING WAS MADE WITH NOSE AND LEFT MAIN GEAR D OWN AND RIGHT MAIN ONLY PARTIALLY EXTENDED. AC SUSTAINED ONLY MINOR DAMAGE. POST LANDING INSP REVEALED THAT THE TORQUE LINKS SEPARATED AT CENTER PIVOT AND WERE CAUGHT IN WHEEL WELL PREVENTING EXTENSION. CENTER TORQUE LINK BOLT PN 402-31 2 FAILED. BOLT, SHANK, AND NUT WITH COTTER PIN WERE STILL IN POSITION BUT SEIZED IN LOWER TORQUE LINK ASSY. LACK OF GR EASE FITTINGS AT CENTER PIVOT MAY HAVE BEEN CONTRIBUTING FACTOR AS ONLY MEANS OF LUBE IS SPRAY LUBE, WHICH CAN BE WASHED OUT DURING FLIGHTS IN WET CONDITIONS. AC TT 4544 AND ESTIMATED TIME ON BOLT PN 402312 IS AT LEAST 1330. 1 L 7 2 3O A7SO 2001071600031 20010716 00031 CE 2001 7 16 20010613CW007 1 20010507 A 5620 1014400421 WINDOW BEECH 200 B200 1152922 CE CABIN BROKEN B LN3R A UNSCHED LANDING O OTHER CL CLIMB 1 WP 07 132N BB1053 THE AIRCRAFT WAS CLIMBING TO ALTITUDE PRESSURIZED WHEN PILOT HEARD BANG IN BACK OF CABIN. THE SMALL WINDOW AFT OF CABIN DOOR HAD CATASTROPHIC FAILURE AND AIRCRAFT DEPRESSURIZED. LOG BOOKS WERE NOT AVAILABLE FOR REVIEW. PILOT STATED HE BE LIEVED THE WINDOW HAD NEVER BEEN REPLACED. THE OPPOSITE WINDOW WAS REPLACED AT THE SAME TIME AT THE PILOTS REQUEST.` 1 L 7 2 4T A24CE 2001071600036 20010716 00036 SO 2001 7 16 20010613CW013 2 20010517 A 7324 6314272A20 FLOW DIVIDER BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO ENGINE STUCK B VJ3R K NONE O OTHER NR NOT REPORTED 1 WP 07 5609S 48 CE1454 820444 ENGINE RUN ROUGH AND SOMETIME WOULD NOT SHUT DOWN, THE FUEL FLOW DIVIDER WOULD STICK OPEN, LETTING FUEL TOO CONTINUAL TO THE ENGINE. THE FLOW DIVIDER WAS REMOVED AND REPLACED WITH A NEW ONE, OPERATION OF ENGINE CHECKED OUT NORMAL. 1 L 7 1 3O 3 O 3A15 E5CE 2001071600037 20010716 00037 SO 2001 7 16 20010613CW014 2 20010518 A 7314 64621216A2 PUMP BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO ENGINE LEAKING B VJ3R K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 WP 07 38071 434 CE935 820386R ON LANDING, A SMELL OF FUEL WAS DETECTED IN THE CABIN OF THE AIRCRAFT. MAINTENANCE WAS CALLED TO CHECK THE AIRCRAFT FOR A FUEL LEAK, UPON INSPECTION IT WAS FOUND TO BE LEAKING FUEL FROM THE CASE DRAIN IN THE ENGINE DRIVEN PUMP. PUMP WAS R EMOVED AND TRIMMED IAW MM AND RETURNED TO SERVICE. PUMP SENT FOR WARRANTY. 1 L 7 1 3O 3 O 3A15 E5CE 2001071600038 20010716 00038 CE 2001 7 16 20010613CW015 1 20010522 A 7920 B-NUT BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA TORQUE MANIFOLD LOOSE B TIMR E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 NM 07 172GA UB11 32412 OIL LINE TO THE TORQUE MANIFOLD B-NUT CAME LOOSE. OIL PRESSURE FLUCTUATED AND ENGINE SHUT DOWN. AIRCRAFT LANDED. ENGI NE WAS INSPECTED AS PER PWA MM. LOW OIL PRESSURE PROCEDURE, NO DAMAGE FOUND. OIL SERVICED AND ENGINE TEST RUN, PER PWA CHECK. 2 L 7 2 4T 4 T RT A24CE E4EA 2001071600039 20010716 00039 SO 2001 7 16 20010613CW016 1 20010529 A 2913 1159SCH5057 PUMP GULSTM GV GV SO LT ENGINE DETERIORATED B LD2R K NONE O OTHER IN INSP/MAINT 1 GL 15 83M 253 557 FLUID SAMPLE TAKEN AT 100 HR INTERVAL SHOW THAT THE PUMP NEEDS TO BE REPLACED. REPLACE PUMP AND BLED SYSTEM WITH SIGHT GAUGE INSTALLED IN RETURN LINE OF HYDRAULIC RIG, TO HELP EVALUATE AIR REMOVAL FROM SYSTEM. 2 L 7 2 4F RT A12EA 2001071600040 20010716 00040 NE 2001 7 16 20010613CW017 1 20010521 A 6210 641520201048 BLADE SKRSKY S64 S64E 8142604 NE MAIN ROTOR CRACKED B JYDR K NONE O OTHER IN INSP/MAINT 1 NM 09 217AC 8329 64064 BLADE REMOVED FOR BIM INDICATION. THE SPAR IS CRACKED ON BOTTOM SIDE UNDER NR 9 POCKET, APPROXIMATELY 1 INCH STARTING A T BACK WALL RADIUS, RUNNING CHORDWISE TOWARDS LEADING EDGE. PROBABLE CAUSE: CORROSION. 2 G 7 2 4U H4EA 2001071600041 20010716 00041 NE 2001 7 16 20010613CW018 1 20010521 A 6210 641520601044 BLADE SKRSKY S64 S64F NE MAIN ROTOR CRACKED B JYDR K NONE L NO TEST NR NOT REPORTED 1 NM 09 159AC 3721 64084 REMOVED FROM AIRCRAFT FOR BIM INDICATION. PERFORMED LEAK CHECK. DETECTED LEAK AND FOUND CRACK. CRACK IS CHORDWISE, AN D .5000 INCH LONG WITH CORROSION PIT LOCATED IN CENTER. LOCATION OF CRACK IS 23.5 INCHES FROM TIP END ON BOTTOM SIDE OF BLADE AND 4 INCHES FROM LEADING EDGE. PROBABLE CAUSE: CORROSION. 2 G 7 2 4U H6EA 2001071600043 20010716 00043 CE 2001 7 16 20010613CW020 1 20010110 A 3411 CM29446600 HOSE CESSNA 500 560CESSNA 2076750 CE PITOT/STATIC SYS LEAKING B CWQR K NONE O OTHER IN INSP/MAINT 1 GL 05 373QS 5600373 DURING TEST OF BOTH STATIC SYSTEMS ON AIRCRAFT, FOUND EXCESSIVE STATIC LEAK IN BOTH NR1 AND NR2 SYSTEMS. FOUND STATIC H OSE IN BOTH SIDES LEAKING IN EXCESS OF FACTORY SPECS. REMOVED DEFECTIVE HOSES AND REPLACED WITH NEW, STATIC SYSTEM TEST ED SATISFACTORY. 2 L 7 2 4F RT A22CE 2001071600044 20010716 00044 GL 2001 7 16 20010613CW021 2 20010520 A 7321 320580 BEARING BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL FUEL CONTROL FAILED E DDZA O OTHER O OTHER CR CRUISE 1 CE 03 6BU 1329 4034 AIRCRAFT IN CRUISE FLIGHT. PILOT NOTICED THAT THE MAIN ROTOR NR 2 STARTED TO OVER-SPEED. PILOT LANDED AIRCRAFT SAFELY UNDER ITS OWN POWER. AFTER INVESTIGATING CAUSE, IT WAS FOUND THAT THE ENGINE FUEL CONTROL SHAFT BEARING HAD FAILED CAUS ING FUEL CONTROL TO GO ERRATIC. 1 G 7 1 3U 3 U H2SW E4CE 2001071600045 20010716 00045 EU 2001 7 16 20010613CW022 1 20010424 A 2612 FIRE WARNING BOLKMS 105 BO105S 5626006 EU NR 1 SYS WILL NOT TEST A ALGA K NONE L NO TEST IN INSP/MAINT 1 SW 03 107AL S772 DURING PRESTART CHECK. NR 1 FIRE WARNING SYSTEM WOULD NOT TEST. AFTER ENGINES WERE RUN AND ENGINE COMPARTMENTS WERE DR IED OUT, SYSTEM TESTED NORMALLY. 1 G 7 2 3U H3EU 2001071600047 20010716 00047 SW 2001 7 16 20010613CW024 1 20010402 A 5531 2050308465 SPAR BELL BELL 204 UH1L 118141G SW VERTICAL STAB CRACKED B TZ0R K NONE O OTHER IN INSP/MAINT 1 NM 05 137US BBBH0215 151874 FATIGUE CRACK OCCURRED ON RIGHT HAND VERTICAL FIN SPAR MEMBER APPROXIMATELY .5 INCH FORWARD OF THE 90 DEGREE GEARBOX ATT ACH FITTING. THIS CRACK WAS DETECTED DURING COMPLIANCE OF AD. PROBABLE CAUSE: FATIGUE. REMOVED AND REPLACED VERTICAL FIN SPAR ASSEMBLY IAW AD, SHOULD PRECLUDE THE PROBLEM. 1 G 7 1 4U EXPA1G71 2001071600048 20010716 00048 NM 2001 7 16 PCAA0107071 1 20010713 A 3230 574205A SELECTOR VALVE DHAV DHC8 DHC8102 2809003 NM WING ROOT INOPERATIVE A PCAA O OTHER J WARNING INDICATION LD LANDING 1 EA 13 837EX 23951 3769 217 RDG-PIT FLIGHT#3923. CREW SELECTED GEAR DOWN, SAW YELLOW IN-TRANSIT LIGHTS AND RED GEAR HANDLE LIGHTS ILLUMINATE. GEAR D ID NOT EXTEND. ALTERNATE GEAR EXTENSION PERFORMED, AND FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LANDING GEAR SELECTOR VALVE IN ACCORDANCE WITH DASH 8 MAINTENANCE MANUAL 32-30-41. OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT RETURNE D TO SERVICE. 2 H 7 2 4T RT A13NM 2001071600050 20010716 00050 CE 2001 7 16 2001F00031 1 20010417 A 3250 12606311 ROD END CESSNA 206 TU206G 2073357 CE NLG STEERING FAILED B K NONE O OTHER IN INSP/MAINT 1 SW 01 5424X U20604524 DURING A DAILY AND PREFLIGHT INSPECTION THE RUDDER TRIM AND NOSE STEERING WERE FOUND INOPERATIVE. AT CLOSER INSPECTION THE ROD END (PN 12606311) FOR THE NOSE STEERING BUNGEE HAD FAILED AT THE (PN 12606323) RUDDER TRIM GEAR. THIS EFFECTUAL LY DISCONNECTS NOT ONLY RUDDER TRIM BUT NOSE STEERING. IT IS NOT KNOWN IF THE STEERING STOPS WERE EXCEEDED AND THERE IS NO INDICATION OF THIS BEING DONE. 1 H 7 1 3O A4CE 2001071600051 20010716 00051 SO 2001 7 16 2001F00034 1 20010420 A 2823 6965212 COVER PIPER PA32 PA32R300 7103213 SO FUEL SELECTOR LOOSE A A UNSCHED LANDING Y ENGINE STOPPAGE UK UNKNOWN 1 SO 05 38261 32R7780408 THE PLASTIC COVER AROUND THE FUEL SELECTOR CONTAINS THE SAFETY STOP. TO PREVENT GOING TO THE OFF POSITION THIS COVER WA S NOT PROPERLY INSTALLED OR HAD COME LOOSE, ALLOWING THE PILOT TO GO TO THE OFF POSITION WITH THE FUEL SELECTION WHEN HE ATTEMPTED TO SWITCH TO THE LEFT TANK. SUBSEQUENTLY THE ENGINE QUIT AND THE AIRCRAFT WAS LANDED GEAR UP IN A FIELD AND IS A TOTAL LOSS, NO INJURIES. 1 L 7 1 3O A3SO 2001071600052 20010716 00052 SO 2001 7 16 2001F00036 1 20010612 A 2497 WIRE PIPER PA32 PA32R300 7103213 SO COCKPIT LOOSE A O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 AL 05 148RF 32R7680076 DURING FLIGHT, POWER WAS LOST TO AVIONICS CAUSING AMP GAUGE FLUCTUATIONS. UPON INSPECTION WIRES WERE FOUND TO BE LOOSE ON MASTER SWITCH FOR AVIONICS AND SOME ARCING WAS NOTICED. REPLACED TERMINAL ENDS AND SCREWS AND LOCKWASHERS. OPS CHEC KED SYSTEM. 1 L 7 1 3O A3SO 2001071600053 20010716 00053 CE 2001 7 16 2001F00038 1 20010412 A 3230 MC815AS1 CONTROLLER BEECH 100 B100 1152919 CE LANDING GEAR DEFECTIVE D O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 03 264PA 8605 BE86 INTERNAL RELAYS FAILED TO CONTACT WHEN GEAR SELECTED DOWN. REPLACED UNIT, SYSTEM WORKED NORMAL. NO RECOMMENDATION. 1 L 7 2 4T A14CE 2001071600054 20010716 00054 CE 2001 7 16 2001F00039 1 20010521 A 2430 MDX3 FUSE CESSNA 402 402C 207590R CE COCKPIT BLOWN D O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 NE 01 6879R 402C0611 CREW NOTICED SMELL OF SMOKE, LEFT ALTERNATOR OUT LIGHT ILLUMINATED, FOUND LEFT ALTERNATOR FIELD FUSE BLOWN. MECHANIC RE PLACED FUSE, INSPECTED ALTERNATOR WIRING, ALTERNATOR, VOLTAGE REGULATORS. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVI CE. 1 L 7 2 3O A7CE 2001071600055 20010716 00055 SO 2001 7 16 2001F00040 1 20010612 A 2432 CB35A BATTERY PIPER PA32 PA32R300 7103213 SO FUSELAGE SHORTED B O OTHER H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 AL 05 108NS 32R7680288 DURING TAKEOFF, PILOT STARTED TO HEAR WHINE IN OVERHEAD SET, FOLLOWED BY POWER LOSS. UPON INSPECTION BATTER WAS FOUND H AVE INTERNAL SHORT CAUSING BATTERY TO GO DEAD. REPLACED BATTERY WITH SERVICEABLE UNIT. OPS CHECKED ELECTRICAL SYSTEM. FOUND OK 1 L 7 1 3O A3SO 2001071600056 20010716 00056 CE 2001 7 16 2001F00047 1 20010615 A 2130 1313741 FILTER LEAR 25 25B 5170511 CE CABIN PRESURE INOPERATIVE E A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 23 50CK 20037 157 CABIN ALTITUDE WARNING HORN WENT OFF AND CABIN ALTITUDE CLIMBED TO 10,000 FEET. AIRCRAFT RETURNED TO AIRPORT. REMOVED AND CLEANED PRESSURIZATION MODULE FILTER AND ORIFICE. GROUND PRESSURIZATION CHECK PERFORMED SATISFACTORY PER THE MM. 2 L 7 2 4J A10CE 2001071600059 20010716 00059 EA 2001 7 16 COMA0160466 1 20010711 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA FAILED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 710CA 689 7241 FLAP FAIL CAUTION FLIGHT TEST OF FLAP SYSTEM, AIRCRAFT RETURNED TO CVG AND LANDED SAFETY.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "SECOND EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 3 AND (D AND E) 4. REPLACED THE RIGHT BRAKE POSITIONIN G SENSING UNIT. 2 L 7 2 4F RT A21EA 2001071600061 20010716 00061 EA 2001 7 16 COMA0160469 1 20010613 A 5300 601R3103077 SPLICE PLATE CNDAIR CL600 CL6002B19 EA DEFECTIVE A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 936CA 7043 TWO SPLICE PLATES WERE FABRICATED INCORRECTLY.FABED DOUBLER PLATES, REWORK SPLICE PLATES AND INSTALLED DOUBLERS I/A/W WV AC EO 601R-53-2500. 2 L 7 2 4F RT A21EA 2001071600062 20010716 00062 EA 2001 7 16 COMA0160396 1 20010620 A 5551 600230681 BUSHING CNDAIR CL600 CL6002B19 EA SCORED A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 945CA 7069 FOUND 3 EACH VERTICAL TO HORIZONTAL PIVOT POINT BUSHINGS TO BE SCORED.REMOVED HORIZONTAL STAB ASSY. REMOVED THE DAMAGED BUSHINGS. INSTALLED 3 EACH NEW BUSHINGS AND FINAL REAMED. REINSTALLED SAME HORIZONTAL STAB ASSEMBLY. ALL WORK WAS PE RFORMED I/A/W CRJ AMM AND WVAC E.O. #601R-55-2509A. 2 L 7 2 4F RT A21EA 2001071600063 20010716 00063 NM 2001 7 16 CALA0100654 1 20010713 A 5512 SKIN BOEING 737 7373T0 1384582 NM STA 138.7 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14358 23943 INSPECTION FOUND A 1.6" CRACK IN L/H HORIZONTAL STABILIZER LOWER SKIN ALONG REAR SPAR AREA AT STA 138.7. THE SKIN WAS RE PAIRED IAW ECRA 5510-01586. 2 L 7 2 4F RT A16WE 2001071600064 20010716 00064 NM 2001 7 16 CALA0100656 1 20010714 A 5230 SKIN BOEING 737 7373T0 1384582 NM C-2 DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14358 23943 INSPECTION FOUND C-2 DOOR EXTERNAL SKIN DENTED AT LOWER AFT CORNER. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-00-01, FIG URE 203. 2 L 7 2 4F RT A16WE 2001071600065 20010716 00065 EA 2001 7 16 COMA0160399 1 20010620 A 2780 601R140021 FLAP CNDAIR CL600 CL6002B19 EA CHAFED A COMA O OTHER F FLT CONT AFFECTED IN INSP/MAINT 1 SO 01 946CA 14039 7072 LEFT INBOARD FLAP, INTERIOR SKIN CHAFFED AT OUTBOARD ACTUATOR BONDING STRAP ATTACH POINT.REPLACED LEFT INBOARD FLAP WITH A SERVICEABLE PART S/N:SB/RJ/027. 2 L 7 2 4F RT A21EA 2001071600066 20010716 00066 EA 2001 7 16 COMA0160400 1 20010625 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA MALFUNCTIONED A COMA O OTHER O OTHER AP APPROACH 1 SO 01 937CA 7547 7037 FLAPS FAILED AT 16 DEGREES DURING APPROACH.REPLACED THE RIGHT HAND FLAP BPSU, C/W AD 98-20-01 PARAGRAPH (B) 1,2,3,A,B,C, E. 2 L 7 2 4F RT A21EA 2001071600067 20010716 00067 EA 2001 7 16 COMA0160402 1 20010628 A 2780 601R140021 FLAP CNDAIR CL600 CL6002B19 EA CHAFED A COMA O OTHER F FLT CONT AFFECTED IN INSP/MAINT 1 SO 01 947CA 13722 7077 LEFT INBOARD FORE-FLAP CHAFFED AT IMPACT STRIPS.PERFORMED S/B 601R-57-022B. 2 L 7 2 4F RT A21EA 2001071600068 20010716 00068 EA 2001 7 16 COMA0160403 1 20010628 A 2780 601R140022 FLAP CNDAIR CL600 CL6002B19 EA CHAFED A COMA O OTHER F FLT CONT AFFECTED IN INSP/MAINT 1 SO 01 947CA 13722 7077 RIGHT INBOARD FORE-FLAP CHAFFED AT IMPACT STRIPS.PERFORMED S/B 601R-57-022B. 2 L 7 2 4F RT A21EA 2001071600069 20010716 00069 EA 2001 7 16 COMA0160405 1 20010627 A 2750 860D10018 FCU CNDAIR CL600 CL6002B19 EA FAILED A COMA K NONE O OTHER DE DESCENT 1 SO 01 958CA 12870 7111 FLAP FAIL CAUTION AT 42 DEGREES DURING DESCENT INTO SDF.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "SECOND EVENT" MA ITNENANCE ACTION, PARAGRAPH (B)3(D AND E) 4 AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT. 2 L 7 2 4F RT A21EA 2001071600070 20010716 00070 EA 2001 7 16 COMA0160411 1 20010628 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 712CA 16061 2193 7244 FLAPS FAILED AT 13 DEGREES.REPLACED THE LEFT HAND BPSU. 2 L 7 2 4F RT A21EA 2001071600071 20010716 00071 EA 2001 7 16 COMA0160414 1 20010628 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 937CA 8629 8494 7044 FLAPS FAILED AT 39 DEGREES.REPLACED THE LEFT HAND BPSU. 2 L 7 2 4F RT A21EA 2001071600072 20010716 00072 NE 2001 7 16 2001F00105 2 20010602 A 7200 310479601 GEAR SHAFT AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE ENGINE SHEARED A TRBA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 262AT 262 1211099 AFTER DEPARTING FROM ANGUILLA ISLAND AND DURING THE CLIMBING STAGE THE ENGINE SURGED APPROXIMATELY 40-50 PERCENT TORQUE. ENGINE WAS SHUTDOWN AND AIRCRAFT DIVERTED AND LANDED IN ST MARTEEN ISLAND. FURTHER INVESTIGATION REVEALED THAT THE EN GINE TOWER SHAFT WAS SHEARED CAUSING THE ENGINE SURGE. ENGINE WAS REMOVED AND REPLACED. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 2001071600073 20010716 00073 NE 2001 7 16 2001F00106 2 20010602 A 7200 310479601 GEAR SHAFT AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE ENGINE SHEARED A TRBA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CL CLIMB 1 SO 21 262AT 17740 262 121099 AFTER DEPARTING FROM ANGUILLA ISLAND AND DURING THE CLIMBING STAGE THE ENGINE SURGED APPROXIMATELY 40-50 PERCENT TORQUE. ENGINE WAS SHUT DOWN AND AIRCRAFT DIVERTED AND LANDED IN ST MARTEEN ISLAND. FURTHER INVESTIGATION REVEALED THAT THE E NGINE TOWER SHAFT WAS SHEARED CAUSING THE ENGINE SURGE. ENGINE WAS REMOVED AND REPLACED. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 2001071600074 20010716 00074 EA 2001 7 16 COMA0160422 1 20010702 A 5346 60135006 BEAM CNDAIR CL600 CL6002B19 EA CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 967CA 12010 7134 DURING INCORPORATION OF COMAIR EO 53-021 (VISUAL INSPECTION OF THE ENGINE SUPPORT BEAM) FOUND THE RIGHT SIDE CRACKED ON LOWER WEB FWD.REPAIRED ENGINE SUPPORT BEAM I/A/W CRJ REO 601-53-61-366 REV B AND WVAC EO 601R-53-2542. 2 L 7 2 4F RT A21EA 2001071600075 20010716 00075 EA 2001 7 16 COMA0160421 1 20010702 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 EA CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 954CA 7100 L/H LOWER WING PLANK CRACKED AT 540 CB - W.S. 76.161 & 550BB - W.S. 188.040. AND R/H LOWER WING PLANK CRACKED AT 610BB - W.S. 32.263 & 640 CB, W.S. 16.161.BLENDED OUT DAMAGED AREAS AND ROTO-PEENED I/A/W REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 2001071600076 20010716 00076 EA 2001 7 16 COMA0160420 1 20010701 A 5346 60135006 BEAM CNDAIR CL600 CL6002B19 EA CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 967CA 12010 7134 DURING INCORPORATION OF COMAIR EO 53-021 (VISUAL INSPECTION OF THE ENGINE SUPPORT BEAM) FOUND THE L/H SIDE CRACKED ON LO WER WEB FWD.PERFORMED A TEMPORARY MAJOR REPAIR TO ENGINE SUPPORT BEAM LOWER WEB I/A/W CRJ REO 601R-53-61-358. 2 L 7 2 4F RT A21EA 2001071600078 20010716 00078 EA 2001 7 16 MASA01037 1 20010411 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 EA EMERG EXIT DOOR OUT OF ADJ A MASA K NONE N FALSE WARNING CL CLIMB 1 SW 07 17275 7275 FLT 6132 - PHX-MRY - PILOT REPORTED SHORTLY AFTER TAKEOFF, A LEFT OVERWING EMERGENCY EXIT CAUTION LIGHT ILLUMINATED. MA INTENANCE WAS CALLED IN MRY. MAINTENANCE ADJUSTED THE PROX TARGET. EN ROUTE FROM MRY-PHX, THE PILOT AGAIN NOTICED THE EMERGENCY EXIT LIGHT ILLUMINATE. IN PHX MX WAS CALLED. MAINTENANCE ADJUSTED THE PROX SENSOR AND TARGET. OP CHECKS GOO D. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001071600079 20010716 00079 EA 2001 7 16 COMA0160424 1 20010629 A 2750 852D10011 ACTUATOR CNDAIR CL600 CL6002B19 EA FROZEN A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 937CA 14412 7044 FLAPS FAILED AT 36 DEGREES.REPLACED THE LEFT HAND #1 FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2001071600080 20010716 00080 EA 2001 7 16 COMA0160425 1 20010630 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 958CA 6343 7111 FLAPS FAILED AT 40 DEGREES.REPLACED THE R/H BPSU. 2 L 7 2 4F RT A21EA 2001071600081 20010716 00081 EA 2001 7 16 COMA0160426 1 20010630 A 2750 860D10018ABC FCU CNDAIR CL600 CL6002B19 EA FAILED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 819CA 1789 7415 FLAPS FAILED AT 45 DEGREES.REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2001071600082 20010716 00082 EU 2001 7 16 SIMA20011432 1 20010509 A 5753 S5751204920400 GUIDE AEROSP ATR72 ATR72212 EU T/E FLAP CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 DURING MBV-1 INSPECTION, MAINTENANCE REPORTED THE LEFT OUTBOARD FLAP NR 5 CAM GUIDE CORRODED, AND THE LEFT INBOARD FLAP NR 3 CAM GUIDE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CAM GUIDES IAW CMM 57-53-11. AIRCRAFT WAS RETURNED TO SE RVICE. (M) 2 H 7 2 4T RT A53EU 2001071600083 20010716 00083 EU 2001 7 16 SIMA20011436 1 20010510 A 5320 S5367800820002 FITTING AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE FOUND THE LEFT AFT ZEE MEMBER BETWEEN FRAMES 39 AND 40 CORRODED, AND THE RIG HT AFT ZEE MEMBER BETWEEN FRAMES 39 AND 41 CORRODED. MAINTENANCE REMOVED AND REPLACED BOTH ZEE MEMBERS IAW SRM 53-25-04 . AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001071600084 20010716 00084 EU 2001 7 16 SIMA20011437 1 20010521 A 5347 7253799381 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 347SB 340B347 ABI - DURING MBV INSPECTION, MAINTENANCE FOUND CORROSION ON SEAT TRACK AT BL 18.3L AT FS 297 OUT OF SRM LIMITS. SEAT TR ACK WAS REPAIRED IAW SAAB SRM. (M) 2 L 7 2 4T RT A52EU 2001071600085 20010716 00085 EU 2001 7 16 SIMA20011438 1 20010521 A 5347 7253799457 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 347SB 340B347 ABI - DURING MBV INSPECTION MAINTENANCE, FOUND SEAT TRACK BL 0 CORRODED FROM STATIONS 619 TO 688.88. MAINTENANCE REPAIR ED SEAT TRACK IAW SAAB SRM. (M) 2 L 7 2 4T RT A52EU 2001071600086 20010716 00086 EU 2001 7 16 SIMA20011439 1 20010521 A 5347 7253799381 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 347SB 340B347 ABI - DURING MBV INSPECTION MAINTENANCE, FOUND SEAT TRACK BL 0 AT STATION 297 TO 328.5 CORRODED BEYOND LIMITS. SEAT TRA CK WAS REPAIRED IAW SAAB SRM. (M) 2 L 7 2 4T RT A52EU 2001071600087 20010716 00087 EA 2001 7 16 COMA0160431 1 20010704 A 2750 8651007 PDU CNDAIR CL600 CL6002B19 EA FROZEN A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 712CA 2412 7244 FLAPS FAILED AT 16 DEGREES.REPLACED THE FLAP PDU. 2 L 7 2 4F RT A21EA 2001071600088 20010716 00088 EU 2001 7 16 SIMA200114402 1 20010524 A 5320 S5367131828001 SILL AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 DURING MBV-1 INSPECTION, MAINTENANCE REPORTED THE SERVICE DOOR SILL PLATE AND DRAIN TRACK CORRODED BETWEEN FRAMES 36 AND 39. MAINTENANCE REMOVED AND REPLACED THE DRAIN TRACK IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001071600089 20010716 00089 EA 2001 7 16 COMA0160433 1 20010629 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 931CA 14621 7971 7037 FLAPS FAILED AT 38 DEGREES.REPLACED THE LEFT HAND BPSU. 2 L 7 2 4F RT A21EA 2001071600090 20010716 00090 EA 2001 7 16 COMA0160434 1 20010703 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 EA MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 931CA 13293 7037 FLAPS FAILED AT 37 DEGREES.REPLACED THE FLAP PDU. 2 L 7 2 4F RT A21EA 2001071600091 20010716 00091 SO 2001 7 16 SIMA200114501 1 20010525 A 2730 SWITCH EMB 145 EMB145LR SO COCKPIT MALFUNCTIONED A SIMA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SW 21 634AE 145200 CVG - FLT 4390 - CAPTAINS AND FIRST OFFICERS PITCH TRIM INOPERATIVE ON THE YOKE. STANDBY TRIM OPERATED NORMAL. EMERGEN CY WAS DECLARED AND AIRCRAFT WAS LANDED SAFELY. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPS CHECK OF CAPTAIN AND FIRST OFFICERS YOKE TRIM WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001071600092 20010716 00092 WP 2001 7 16 DHL2001803544 1 20010703 A 5300 4753360502N FITTING DOUG DC8 DC873 302199C WP A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 MAIN CARGO JOINT FITTING WITH INTERCOSTAL L-22.RH SHOWS 5 IN BREAK AT STA FS 834.000.REMOVED BROKEN FITTING PER SRM 51-1 -20D.PG 21.CLEANED TREATED AND PRIMED PER SRM 51-18B.INSTALLED NEW FITTING PER SRM51-1-20D PG 9 2 L 7 4 4F RT 4A25 2001071600093 20010716 00093 WP 2001 7 16 DHL2001803547 1 20010626 A 5347 S2772660T SEAT TRACK DOUG DC8 DC873 302199C WP WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 MAIN CARGO COMPT - LUGS WORN ON CENTRAL TRACK AT STA 163.00 TO STA 62.000.REMOVED DAMAGED CTR TRACK (STA 62-163)PER SRM 51-3-0 PG 1.CLEANED TREATED AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW TRACK PER SRM 57-3-0 PG 1 AND 51-3-1 PG 1 2 L 7 4 4F RT 4A25 2001071600094 20010716 00094 EA 2001 7 16 COMA0160438 1 20010703 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 712CA 6813 1 7244 FLAP FAILED AT 17 DEGREES.REPLACED THE LEFT HAND BPSU. 2 L 7 2 4F RT A21EA 2001071600095 20010716 00095 EA 2001 7 16 COMA0160441 1 20010702 A 5346 60135006 BEAM CNDAIR CL600 CL6002B19 EA CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 967CA 12010 7134 DURING INCORPORATION OF COMAIR EO 53-021 (VISUAL INSPECTION OF THE ENGINE SUPPORT BEAM) FOUND THE RIGHT SIDE CRACKED ON LOWER WEB FWD.REPAIRED ENGINE SUPPORT BEAM I/A/W CRJ REO 601-53-61-366 REV B AND WVAC EO 601R-53-2542. 2 L 7 2 4F RT A21EA 2001071600096 20010716 00096 EA 2001 7 16 COMA0160470 1 20010708 A 5300 50034017351 ANGLE CNDAIR CL600 CL6002B19 EA CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 18999 7014 THE FWD "J" ANGLE AT F.S. 280.00 BETWEEN LBL9 AND RBL 9 IS CORRODED.REMOVED AND REPLACED FWD "J" ANGLE AT FS 280.00 BETW EEN LBL9 AND RBL9 I/A/W WVAC E.O. 601R-53-1551. 2 L 7 2 4F RT A21EA 2001071600097 20010716 00097 EA 2001 7 16 COMA0160471 1 20010708 A 5300 601R3866949 DOUBLER CNDAIR CL600 CL6002B19 EA CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 18999 7014 DOUBLER P/N 601R38669-49 FWD OF SERVICE DOOR IS CORRODED.REMOVED AND REPLACED DOUBLER P/N 601R38669-49 FWD OF SERVICE DO OR I/A/W WVAC E.O. 601R-53-2550. 2 L 7 2 4F RT A21EA 2001071600098 20010716 00098 EA 2001 7 16 COMA0160472 1 20010708 A 5300 601R31148127 THRESHOLD CNDAIR CL600 CL6002B19 EA CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 18999 7014 THE THRESHOLD/SILL PANEL AFT OF THE SERVICE DOOR IS CORRODED.TRIMMED THRESHOLD AREA, FABED SPLICE ANGLE AND INSTALLED I/ A/W WVAC EO 601R-53-2554A. 2 L 7 2 4F RT A21EA 2001071600100 20010716 00100 EA 2001 7 16 COMA0160408 1 20010628 A 2750 FLAP CNDAIR CL600 CL6002B19 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 981CA 7163 FLAPS FAILED AT 42 DEGREES.COMPLIED WITH INSPECTION OF FLAP SYSTEM I/A/W AD 98-20-01. NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 2001071600101 20010716 00101 EU 2001 7 16 SIMA200114602 1 20010526 A 5610 7256100502 WINDSHIELD SAAB SF340 340B 7860101 EU COCKPIT CRACKED A SIMA B EMER. DESCENT O OTHER CR CRUISE 1 SW 21 243AE 340B243 BGR - FLT 4924 - FIRST OFFICERS WINDSHIELD SHATTERED IN FLIGHT. MAINTENANCE REMOVED AND REPLACED FIRST OFFICERS WINDSHI ELD IAW SAAB MM AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001071600102 20010716 00102 EA 2001 7 16 COMA0160409 1 20010628 A 2750 FLAP CNDAIR CL600 CL6002B19 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 959CA 7116 FLAPS FAILED MESSAGE AT 45 DEGREES.COMPLIED WITH INSPECTION OF FLAP SYSTEM I/A/W AD 98-20-01. NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 2001071600103 20010716 00103 EU 2001 7 16 SIMA200114603 1 20010526 A 3350 30112000 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 308AE 309 DFW - FLT 3857 - CREW REPORTED NUMEROUS EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPP LY BATTERY PACK AT POSITION 73WL. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001071600104 20010716 00104 EU 2001 7 16 SIMA200114604 1 20010526 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU E/E BAY MALFUNCTIONED A SIMA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 SW 21 234AE 340B234 PWM - FLT 4637 - CREW REPORTED THE AVIONICS SMOKE LIGHT WILL NOT GO OUT. PUT ON MEL AT THIS TIME. MAINTENANCE REMOVED, CLEANED AND REINSTALLED AVIONIC SMOKE DETECTOR. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001071600105 20010716 00105 EU 2001 7 16 SIMA200114701 1 20010527 A 3350 LIGHT AEROSP ATR72 ATR72212 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 426AT 426 CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS AT ROWS 3, 11 AND 16 ARE INOPERATIVE. LIGHT WERE PUT ON MEL AT THIS TIME. (M) 2 H 7 2 4T RT A53EU 2001071600106 20010716 00106 EA 2001 7 16 COMA0160445 1 20010708 A 5300 601R31527221 ANGLE CNDAIR CL600 CL6002B19 EA CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 18999 7014 THE THRESHOLD SUPPORT ANGLE AT THE PASSENGER DOOR IS SEVERELY CORRODED.REMOVED CORRODED THRESHOLD ANGLE P/N 601R31527-22 1, FABED NEW THRESHOLD ANGLE AND INSTALL I/A/W W.V.A.C. T.O. 601R-53-2557. 2 L 7 2 4F RT A21EA 2001071600107 20010716 00107 EU 2001 7 16 SIMA200114702 1 20010527 A 3350 3011210 LIGHT AEROSP ATR42 ATR42300 8680920 EU CABIN DOOR INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 293AT 293 MIA - FLT 5305 - CREW REPORTED THE CABIN DOOR EXIT LIGHT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASS EMBLY IAW ATR MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001071600108 20010716 00108 EA 2001 7 16 COMA0160473 1 20010708 A 5300 BEAM CNDAIR CL600 CL6002B19 EA CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 18999 7014 THE FLOOR BEAM WEB AT F.S. 280.00 IS CORRODED ON UPPER EDGE BETWEEN RBL9 AND LBL9.TRIMMED OUT DAMAGED AREA, FABED FILLER , FABED REPAIR DOUBLER, AND INSTLALED I/A/W WVAC E.O. 601R-53-2553. 2 L 7 2 4F RT A21EA 2001071600109 20010716 00109 SO 2001 7 16 SIMA200114703 1 20010527 A 2740 3621001007 CONTROL UNIT EMB 145 EMB145LR SO HORIZ STAB INOPERATIVE A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 612AE 145079 DFW - FLT 3331 - CREW REPORTED THE NR 1 PITCH TRIM INOPERATIVE MESSAGE ON EICAS. MAINTENANCE REMOVED AND REPLACED THE H ORIZONTAL STABILIZER CONTROL UNIT IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001071600110 20010716 00110 SO 2001 7 16 SIMA200114704 1 20010527 A 3350 LIGHT EMB 135 EMB135LR SO PAX DOOR LOOSE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 724AE 145301 ORD - FLT 4054 - CREW REPORTED THE PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE FOUND THE BULB LOOSE I N SOCKET AND A GROUND WIRE THAT WAS LOOSE. THE BULB WAS TIGHTENED IN SOCKET AND THE GROUND WIRE WAS ALSO TIGHTENED. OP S CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001071600111 20010716 00111 EU 2001 7 16 SIMA200114705 1 20010527 A 5220 HANDLE SAAB SF340 340B 7860101 EU EMERGENCY EXIT UNSECURE A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 334AE 340B334 JFK - FLT 5193 - CREW REPORTED THE HANDLE ON THE EMERGENCY EXIT ACROSS FROM MAIN DOOR CAME DOWN ON TAKEOFF AND AIRCRAFT WOULD NOT PRESSURIZE. FLIGHT ATTENDANTS SECURED HANDLE AND AIRCRAFT WAS RETURNED TO JFK WITH NO FURTHER INCIDENTS. MAI NTENANCE COULD NOT DUPLICATE DISCREPANCY. EMERGENCY EXIT WAS REMOVED AND A THROUGH INSPECTION OF THE LOCKING MECHANISM INTERNAL AND EXTERNAL WITH NO DEFECTS FOUND. DOOR WAS REINSTALLED AND A GROUND PRESSURIZATION CHECK WAS COMPLIED WITH A ND NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001071600112 20010716 00112 2001 7 16 COMA0160449 4 20010706 A 3460 6229815704 COMPUTER CNDAIR CL600 CL6002B19 EA MALFUNCTIONED A COMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 01 807CA 332 7364 UNCOMMANDED YAWING DURING CLIMB.REPLACED THE #1 AND #2 FCC-4000. 2 L 7 2 4F RT A21EA 2001071600113 20010716 00113 SO 2001 7 16 SIMA200114804 1 20010528 A 5240 DOOR EMB 145 EMB145LR SO GPU ACCESS OPEN A SIMA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 21 631AE 145139 ORD - FLT 4215 - CREW REPORTED AN AUDIBLE VIBRATION COMING FROM THE LEFT SIDE OF AIRCRAFT NOSE. MAINTENANCE FOUND THE G PU ACCESS DOOR TO BE OPEN. DOOR WAS DAMAGED AND WAS PUT ON CDL AT THIS TIME. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001071600114 20010716 00114 EA 2001 7 16 COMA0160450 1 20010705 A 2750 854D10011 ACTUATOR CNDAIR CL600 CL6002B19 EA MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 810CA 2940 7370 FLAPS FAILED AT 36 DEGREES.REPLACED THE LEFT HAND #3 FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2001071600115 20010716 00115 WP 2001 7 16 MWEA011036 1 20010716 A 5310 591143277 LONGERON DOUG DC9 DC914 3022034 WP STATION 897 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 STATION 897 AT LONGERON 2 RIGHT IS CRACKED. -- REMOVED DAMAGE, TRIMMED AND LOCATED SPLICES AND FRAME, INSTALLED REPAIR PARTS. 2 L 7 2 4F A6WE 2001071600116 20010716 00116 WP 2001 7 16 MWEA011037 1 20010716 A 5310 27779223 LONGERON DOUG DC9 DC914 3022034 WP STATION 897 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 TWO MISDRILLED HOLES IN LONGERON 17 RIGHT AT STATION 897. -- FABRICATED AND LOCATED NEW LONGERON SECTION AND SPLICE, IN STALLED NEW LONGERON AND SPLICE. 2 L 7 2 4F A6WE 2001071600117 20010716 00117 WP 2001 7 16 MWEA011038 1 20010716 A 5310 591143277 ANGLE DOUG DC9 DC914 3022034 WP STATION 897 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 STATION 897 CRACKED AT LONGERON 2 LEFT, ALSO SUPPORT ANGLE AT THAT STATION IS CRACKED. -- FABRICATED GUSSET, LOCATED S UPPORT ANGLE, INSTALLED SUPPORT ANGLE. 2 L 7 2 4F A6WE 2001071600118 20010716 00118 WP 2001 7 16 MWEA011039 1 20010716 A 5310 5911432 ANGLE DOUG DC9 DC914 3022034 WP STATION 897 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 STATION 897 AT LONGERON 2 RIGHT SUPPORT ANGLE IS CRACKED. -- REMOVED, FABRICATED AND INSTALLED SUPPORT ANGLE. 2 L 7 2 4F A6WE 2001071600119 20010716 00119 WP 2001 7 16 MWEA011040 1 20010716 A 5310 59114329 LONGERON DOUG DC9 DC914 3022034 WP STATION 897 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 LONGERON 2 RIGHT IS CRACKED WHERE IT ATTACHES TO FRAME AT STATION 897. -- REMOVED DAMAGED SECTION OF LONGERON, FABRICA TED, LOCATED AND DRILLED NEW SECTION OF LONGERON, INSTALLED REPAIR PARTS. 2 L 7 2 4F A6WE 2001071600120 20010716 00120 WP 2001 7 16 MWEA011041 1 20010716 A 5310 59114329 LONGERON DOUG DC9 DC914 3022034 WP STATION 897 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 LONGERON 2 LEFT IS CRACKED WHERE IT ATTACHES TO FRAME AT STATION 897. -- REMOVED DAMAGED SECTION OF LONGERON, FABRICAT ED, LOCATED, DRILLED NEW SECTION OF LONGERON, INSTALLED REPAIR PARTS. 2 L 7 2 4F A6WE 2001071600121 20010716 00121 WP 2001 7 16 MWEA011042 1 20010716 A 5230 59101417 PAN DOUG DC9 DC914 3022034 WP FWD CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FORWARD CARGO DOOR FORWARD UPPER CORNERS ON THE INNER PAN IS CRACKED AROUND A SEAL FASTENER HOLE. -- LOCATED, DRILLED AND INSTALLED NEW PAN. 2 L 7 2 4F A6WE 2001071600122 20010716 00122 WP 2001 7 16 MWEA011043 1 20010716 A 5310 5910142 FRAME DOUG DC9 DC914 3022034 WP STATION 378 BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FORWARD CARGO BAY DOOR JAMB FRAME IS BENT AT STATION 378 LONGERON 29 LEFT TO 29 RIGHT. -- RE-CONTOURED BEND, FABRICATE D AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001071600123 20010716 00123 WP 2001 7 16 MWEA011044 1 20010716 A 5310 2777930 FRAME DOUG DC9 DC914 3022034 WP STATION 389 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FORWARD CARGO BAY HAS CORROSION ON FRAME 389 AFT SIDE AT LONGERONS 28 LEFT TO 28 RIGHT. -- BLENDED CORROSION, FABRICAT ED AND LOCATED DOUBLERS, LOCATED NEW FRAME SECTION, INSTALLED FRAME REPAIR SPLICE. 2 L 7 2 4F A6WE 2001071600124 20010716 00124 WP 2001 7 16 MWEA011045 1 20010716 A 5310 2912727 LONGERON DOUG DC9 DC914 3022034 WP STATION 446-465 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FORWARD CARGO BAY HAS CORROSION ON LONGERON 29 RIGHT AT STATION 446 TO 465 AROUND RIVETS. -- REMOVED CORROSION, REMOVE D DAMAGED SECTION OF LONGERON, LOCATED NEW LONGERON SECTION, LOCATED AND DRILLED NEW SPLICE, INSTALLED NEW LONGERON SECT ION AND SPLICE. 2 L 7 2 4F A6WE 2001071600125 20010716 00125 WP 2001 7 16 MWEA011046 1 20010716 A 5230 99576623 INTERCOSTAL DOUG DC9 DC914 3022034 WP AFT CARGO DOOR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 LOWER AFT CARGO DOOR JAMB HINGE INTERCOSTAL HAS AN ELONGATED HOLE. -- FABRICATED 2 EACH BUSHING PLATES, INSTALLED PLAT ES. 2 L 7 2 4F A6WE 2001071600126 20010716 00126 WP 2001 7 16 MWEA011047 1 20010716 A 5310 27779305 FRAME DOUG DC9 DC914 3022034 WP STATION 427 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FORWARD CARGO BAY HAS CORROSION ON FRAME 427 AFT SIDE AND BOTTOM, FROM LONGERON 28 LEFT TO 28 RIGHT. -- REMOVED CORRO SION, FLOOR SUPPORTS, DAMAGED SECTION OF FRAME, LOCATED NEW FRAME, INSTALLED FRAME SECTION AND DOUBLERS. 2 L 7 2 4F A6WE 2001071600127 20010716 00127 WP 2001 7 16 MWEA011048 1 20010716 A 5710 5911306507 CAP DOUG DC9 DC914 3022034 WP XCW 58.5 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 3 1/2" CRACK FOUND ON LEFT UPPER FORWARD SPAR CAP 2 1/2" OUTBOARD OF XCW 58.5 AS VIEWED THROUGH ACCESS PANEL. -- TRIMM ED OUT CRACK, TRIMMED AND LOCATED FILLERS, NESTED ANGLE, STIFFNER, INSTALLED FILLER AND ANGLE. 2 L 7 2 4F A6WE 2001071600128 20010716 00128 WP 2001 7 16 MWEA011050 1 20010716 A 5310 995823973 DOUBLER DOUG DC9 DC932 3022066 WP STATION 1019 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 AFT ACCESSORY COMPARTMENT SHEAR TIE DOUBLER AT FRAME STATION 1019 AT LONGERON 14 LEFT IS CRACKED. -- REMOVED SHEAR TIE DOUBLER, FABRICATED AND INSTALLED NEW SHEAR TIE DOUBLER. 2 L 7 2 4F A6WE 2001071600129 20010716 00129 EA 2001 7 16 COMA0160451 1 20010705 A 2750 FLAP CNDAIR CL600 CL6002B19 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 810CA 7370 FLAPS FAILED AT 36 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2001071600130 20010716 00130 EA 2001 7 16 COMA0160452 1 20010705 A 2750 FLAP CNDAIR CL600 CL6002B19 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 983CA 7169 FLAPS FAILED AT 38 DEGREES.INSPECTED FLAP SYSTEM PER AD 98-20-01 - NO FAUTLS FOUND. LUBRICATED FLAP ACTUATORS. 2 L 7 2 4F RT A21EA 2001071600131 20010716 00131 2001 7 16 COMA0160448 4 20010706 A 3460 6229815704 COMPUTER CNDAIR CL600 CL6002B19 EA MALFUNCTIONED A COMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 01 807CA 4100 7364 UNCOMMANDED YAWING DURING CLIMB.REPLACED THE #1 AND #2 FCC-4000. 2 L 7 2 4F RT A21EA 2001071600132 20010716 00132 GL 2001 7 16 SIMA200114807 2 20010528 A 7200 23072902 CARBON SEAL EMB 145 EMB145LR SO ALLSN AE300 AE3007A GL NR 2 ENGINE LEAKING A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 610AE 145073 ORD - FLT 4051 - CREW REPORTED THE LAVATORY SMOKE WARNING MESSAGE ON EICAS AND THEN WENT OUT. TAKEOFF WAS ABORTED AND E MERGENCY WAS DECLARED. ORD FIRE DEPARTMENT FOUND NO EVIDENCE OF ANY SMOKE OR ANYTHING BURNED. MAINTENANCE FOUND THE ZE RO CARBON SEAL LEAKING IN THE NR 2 ENGINE. CARBON SEAL WAS REPLACED IAW RR MM. OPERATIONAL AND LEAK CHECKS WERE GOOD A ND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2001071600133 20010716 00133 EA 2001 7 16 COMA0160454 1 20010708 A 3350 NA LIGHT CNDAIR CL600 CL6002B19 EA LOOSE A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 796CA 7338 EMERGENCY FLOOR PATH LIGHTING IS PARTIALLY INOP.FASTENED LOOSE WIRE AT FLOOR LIGHTING. 2 L 7 2 4F RT A21EA 2001071600134 20010716 00134 EA 2001 7 16 COMA0160455 1 20010710 A 2750 NA FLAP CNDAIR CL600 CL6002B19 EA FAILED A COMA O OTHER S AFFECT SYSTEMS CL CLIMB 1 SO 01 941CA 7050 FLAP CAUTION MESSAGE AFTER TAKE-OFF FROM GSP, AIRCRAFT RETURNED TO THE FIELD.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESS AGE "FIREST EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 1,2,3 (A,B,C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CA UTION MESSAGE. 2 L 7 2 4F RT A21EA 2001071600135 20010716 00135 EA 2001 7 16 COMA0160456 1 20010707 A 2750 852D10011 ACTUATOR CNDAIR CL600 CL6002B19 EA LEAKING A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 983CA 9326 7169 FLAP FAIL CAUTION MESSAGE AT 38 DEGREE FLAP POSITION DURING APPROACH INTO CVG.COMPLIED WITH AD 98-20-01 FLAP CAUTION MES SAGE "SECOND EVENT" MAINTENANCE ACTION, PARAGRAPH (B)3 (D AND E) 4. REPLACED OUTBOARD FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2001071600136 20010716 00136 EA 2001 7 16 COMA0160458 1 20010709 A 2750 852D10011 ACTUATOR CNDAIR CL600 CL6002B19 EA FROZEN A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 819CA 1790 7415 FLAP FAIL CAUTION MESSAGE AT 40 DEGREE FLAP POSITION DURING APPROACH INTO CVG.COMPLIED WITH AD 98-20-01 FLAP CAUTION MES SAGE "SECOND EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 3 (D AND E) 4. REPLACED INBOARD FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2001071600137 20010716 00137 EA 2001 7 16 COMA0160463 1 20010711 A 2750 601R930507 FCU CNDAIR CL600 CL6002B19 EA FAILED A COMA A UNSCHED LANDING S AFFECT SYSTEMS TO TAKEOFF 1 SO 01 710CA 1497 7241 AFTER T/O FROM CVG FLAP FAULT CAUTION MESSAGE, AIRCRAFT RETURNED TO THE FIELD.COMPLIED WITH AD 98-20-01 FLAP CAUTION MES SAGE "SECOND EVENT" MAINTENANCE ACTION, PARAGRAPH (B)3(D AND E)4. REPLACED THE FLAP ELECTRONIC CONTROL UNIT. 2 L 7 2 4F RT A21EA 2001071600138 20010716 00138 EA 2001 7 16 COMA0160465 1 20010711 A 2760 NA SPOILER CNDAIR CL600 CL6002B19 EA A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 960CA 7117 CONFIG AILERON AND CONFIG SPOILER WARNINGS DURING T/O.COULD NOT DUPLICATE. FOUND CONFIG WARNING SYSTEM FUNCTIONED PROPE RLY. 2 L 7 2 4F RT A21EA 2001071600139 20010716 00139 EA 2001 7 16 COMA0160467 1 20010712 A 2750 860D10018ABC FCU CNDAIR CL600 CL6002B19 EA FAILED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 932CA 9981 985 7038 FLAPS FAILED.REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2001072700184 20010727 00184 EA 2001 7 27 COMA0160412 1 20010628 A 2750 FLAP CNDAIR CL600 CL6002B19 EA WING FAILED A COMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 01 712CA 7244 FLAPS FAILED AT 17 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2001071600140 20010716 00140 EA 2001 7 16 COMA0160413 1 20010628 A 3230 GEAR CNDAIR CL600 CL6002B19 EA A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 914CA 7012 LANDING GEAR SELECTOR LOCK DID NOT RELEASE. LANDING GEAR COULD NOT BE RETRACTED.COULD NOT DUPLICATE. INSPECTED RETRACT ED SYSTEM, AND FOUND NO DEFECTS. 2 L 7 2 4F RT A21EA 2001071600141 20010716 00141 EU 2001 7 16 SIMA200114903 1 20010529 A 7603 LEVER SAAB SF340 340B 7860101 EU COCKPIT MALFUNCTIONED A SIMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 21 283AE 340B283 RDU - FLT 5048 - ABORTED TAKEOFF IN RDU DUE TO CONDITION LEVER CREEP BACK. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. PERFORMED MEASUREMENT CHECK OF CONTROL QUADRANT WITH NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001071600142 20010716 00142 EA 2001 7 16 COMA0160415 1 20010629 A 2750 FLAP CNDAIR CL600 CL6002B19 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 981CA 7163 FLAPS FAILED AT 16 DEGREES.INSPECTED FLAP SYSTEM I/A/W AD98-20-01. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2001071600143 20010716 00143 EA 2001 7 16 COMA0160416 1 20010629 A 2750 FLAP CNDAIR CL600 CL6002B19 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 978CA 7158 FLAPS FAILED WHEN SELECTED TO 45 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2001071600144 20010716 00144 SO 2001 7 16 SIMA200114904 1 20010529 A 2740 3621001007 CONTROL UNIT EMB 135 EMB135LR SO HORIZ STAB INOPERATIVE A SIMA O OTHER J WARNING INDICATION CL CLIMB 1 SW 21 733KR 145368 ORD - FLT 4120 - DURING CLIMB AT 245 KNOTS AND 10200 MSL, THE PITCH TRIM ONE WAS INOPERATIVE ON EICAS. PITCH TRIM WOULD NOT RESPOND TO CAPTAIN, FIRST OFFICERS, OR BACK UP COMMANDS. AIRCRAFT WAS LANDED SAFELY. MAINTENANCE REMOVED AND REPL ACED HORIZONTAL STABILIZER CONTROL UNIT IAW MB MM. CMC AND DFDR WERE ALSO DOWNLOADED. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001071600145 20010716 00145 EA 2001 7 16 COMA0160418 1 20010630 A 5310 60034007351 ANGLE CNDAIR CL600 CL6002B19 EA CORRODED A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 991CA 7216 THE FWD "J" ANGLE @ F.S. 280 BETWEEN LBL 9.0 AND RBL 9.0 IS CORRODED.REMOVED AND REPLACED "J" ANGLE I/A/W WVAC E.O. #601 R-53-2540 REF MAN LOG PAGE 405333. WORK PERFORMED UNDER COMAIR W/O #169657. 2 L 7 2 4F RT A21EA 2001071600146 20010716 00146 2001 7 16 SIMA200115002 4 20010530 A 3418 0861DT55 SENSOR EMB 145 EMB145LR SO NR 2 DEFECTIVE A SIMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 634AE 145150 ORD - FLT 4431 - CREW REPORTED SPS TWO WARNING ON EICAS. AIRCRAFT WAS RETURNED TO ORD. MAINTENANCE REMOVED AND REPLACE D THE NR 2 AOA SENSOR. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001071600147 20010716 00147 EA 2001 7 16 COMA0160419 1 20010701 A 5320 NA FLANGE CNDAIR CL600 CL6002B19 EA CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 916CA 7014 iNTERCOSTAL OUTBOARD FLANGE AT FS 484 AND RBL 36 IS CRACKED.REPAIRED I/A/W WVAC EO 601R-53-2531A. 2 L 7 2 4F RT A21EA 2001071600148 20010716 00148 EU 2001 7 16 SIMA200115103 1 20010531 A 3241 WARNING LIGHT AEROSP ATR42 ATR42300 8680920 EU COCKPIT ILLUMINATED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 971NA 017 FLL - FLT 5427 - CREW REPORTED AFTER TAKEOFF, AN ANTI-SKID FAULT ON RIGHT SIDE. FLIGHT DIVERTED TO MIA DUE TO WET RUNWA YS IN NAS. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. PERFORMED OPS CHECK OF ANTI-SKID IAW AMM 32-42. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001071600149 20010716 00149 EA 2001 7 16 COMA0160435 1 20010703 A 2750 860D10018ABC FLAP CNDAIR CL600 CL6002B19 EA MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 984CA 8838 1762 7171 FLAPS FAILED AT 45 DEGREES.REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2001071600150 20010716 00150 SO 2001 7 16 SIMA200115507 1 20010604 A 7830 SWITCH EMB 145 EMB145LR SO THRUST REVERSER OUT OF ADJ A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 610AE 145073 ORF - FLT 4366 - ABORTED TAKEOFF, NR 1 ENGINE REVERSE DISAGREE ICAS. PERFORMED STOW SWITCH TEST IAW EMB AMM 78-34-01-70 0-801A. PERFORMED ADJUSTMENT IAW 78-34-01-820-801A OF AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT T00011AT 2001071600151 20010716 00151 EA 2001 7 16 COMA0160439 1 20010701 A 2710 AILERON CNDAIR CL600 CL6002B19 EA DIRTY A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 778CA 7297 LOUD SQUEAKING NOISE FROM LEFT AILERON.CLEANED LEFT AILERON ATTACHMENTS AND OPS CHECK NORMAL. 2 L 7 2 4F RT A21EA 2001071600152 20010716 00152 EU 2001 7 16 SIMA200115508 1 20010604 A 3350 3012701 LIGHT AEROSP ATR72 ATR72212A 8680902 EU CABIN CORRODED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 550LL 550 DFW - FLT 3737 - EMERGENCY EXIT FLOOR LIGHTS INOPERATIVE. FOUND PAX DOOR EMERGENCY LIGHT ASSEMBLY CORRODED. REMOVED AN D REPLACED PAX DOOR EMERGENCY LIGHT ASSY IAW AMM. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 2001071600153 20010716 00153 EA 2001 7 16 COMA0160447 1 20010708 A 5300 60034017373 ANGLE CNDAIR CL600 CL6002B19 EA CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 18999 7014 VERTICAL "J" ANGLES LOCATED INSIDE CBPI, CBP2 AT BL9 L/H AND R/H ARE CRACKED.REMOVED DAMAGED "J" ANGLES, FABED NEW ANGLE S AND INSTALLED I/A/W WVAC E.O. 601R-53-2544. 2 L 7 2 4F RT A21EA 2001071600154 20010716 00154 EU 2001 7 16 SIMA200115603 1 20010605 A 5260 7253710871 TRACK SAAB SF340 340B 7860101 EU AIRSTAIR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 335AE 340B335 SBP - FOUND AIRSTAIR TRACK HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED AIRSTAIR TRACK ASSEMBLY IAW SAAB SRM 51 -40-40 AND 51-40-21. (M) 2 L 7 2 4T RT A52EU 2001071600155 20010716 00155 EU 2001 7 16 SIMA200115607 1 20010605 A 5320 7253721439 STIFFENER SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 335AE 340B335 SBP - FOUND WEB REINFORCEMENT BETWEEN FS 288 AND 294 IS CORRODED. REMOVED AND REPLACED WEB REINFORCEMENT IW SAAB SRM 51 -40-40 AND 51-40-21. (M) 2 L 7 2 4T RT A52EU 2001071600156 20010716 00156 EU 2001 7 16 SIMA200115608 1 20010605 A 3211 7257162515 TRUNNION SAAB SF340 340B 7860101 EU LT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 335AE 340B335 SBP - LEFT MAIN LANDING GEAR AFT TRUNNION FITTING BEARING HOUSING IS CORRODED. REMOVED AND REPLACED TRUNNION ASSEMBLY I AW SAAB AMM 57-40-05. (M) 2 L 7 2 4T RT A52EU 2001071600157 20010716 00157 EU 2001 7 16 SIMA200115609 1 20010605 A 3211 7257500182 TRUNNION SAAB SF340 340B 7860101 EU RT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 335AE 340B335 SBP - RIGHT MAIN LANDING GEAR AFT TRUNNION FITTING BEARING HOUSING IS CORRODED. REMOVED AND REPLACED TRUNNION ASSEMBLY IAW SAAB AMM 57-40-05. (M) 2 L 7 2 4T RT A52EU 2001071600158 20010716 00158 EA 2001 7 16 COMA0160468 1 20010713 A 5346 6013350061 BEAM CNDAIR CL600 CL6002B19 EA CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 965CA 11987 7131 CRACKS FOUND IN ENGINE SUPPORT BEAM LOWER WEB BETWEEN F.S. 640.0 - 625.30 ON LEFT HAND AND RIGHT HAND SIDES.REPAIRED CRA CKS I/A/W REO 601R-53-61-366 REV B AND WVAC E.O.'S 601R-53-2560-1A AND 601R-53-2545B. 2 L 7 2 4F RT A21EA 2001071600159 20010716 00159 EA 2001 7 16 COMA0160474 1 20010715 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 959CA 15561 5027 7116 FLAPS FAILED AT 41 DEGREES.REPLACED THE L/H BPSU. 2 L 7 2 4F RT A21EA 2001071600160 20010716 00160 NE 2001 7 16 SIMA200115616 2 20010605 A 7321 CONNECTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE DECU DISCONNECTED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 264AE 340B264 HPN - FLT 4583 - AIRCRAFT ABORTED TAKEOFF FOR LOSS OF LEFT TORQUE INDICATION. RESECURED CANNON PLUG ON DECU. INSPECTED AND RESECURED CANNON PLUG ON TORQUE AND OVERSPEED SENSOR IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 2001071600161 20010716 00161 EU 2001 7 16 SIMA200115617 1 20010605 A 5297 WIRE AEROSP ATR72 ATR72212 8680945 EU PAX DOOR BROKEN A A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 426AT 426 TUL - FLT 3656 - MAIN CABIN DOOR WARNING CAME ON IN FLIGHT. RETURNED TO BASE. INSPECTED DOOR ASSEMBLY AND ISSUED MEL. S/D - FOUND BROKEN WIRE AT CANNON PLUG, REPAIRED SAME IAW AMM 52-11-00. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 2001071600162 20010716 00162 EU 2001 7 16 SIMA200115618 1 20010605 A 7712 PLUG AEROSP ATR42 ATR42300 8680920 EU TSCU CONTAMINATED A SIMA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 21 277AT 277 JAX - FLT 5258 - NR 2 ENGINE SURGED ON TAKEOFF. TAKEOFF WAS ABORTED AND RETURNED TO GATE. S/D - FOUND OIL ON PLUGS ON THE TSCU. CLEANED PLUGS AND PERFORMED RUNS IAW AMM 72-00-00. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 2001071600163 20010716 00163 EU 2001 7 16 SIMA200115620 1 20010605 A 7712 7239060503 CONTROL PANEL SAAB SF340 340B 7860101 EU COCKPIT FAILED A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 298AE 340B298 FLT 5113 - JFK - LEFT APR LIGHT DID NOT ILLUMINATE. ABORTED TAKEOFF. ISSUED MEL. REMOVED AND REPLACED CTOT/APR CONTRO L PANEL IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001071600164 20010716 00164 EA 2001 7 16 COMA0160475 1 20010713 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 EA BURNED OUT A COMA O OTHER L NO TEST TX TAXI/GRND HDL 1 SO 01 776CA 7293 EMERG CEILING LIGHT AT ROW 5 IS INOPERABLE.REPLACED THE LIGHT BULB. 2 L 7 2 4F RT A21EA 2001071600165 20010716 00165 SO 2001 7 16 SIMA200115621 1 20010605 A 7830 WARNING SYSTEM EMB 135 EMB135LR SO COCKPIT FALSE INDICATION A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 700LE 145156 MKE - FLT 3276 - THRUST REVERSER DISAGREE ON TAKEOFF ROLL ALONG WITH NO TAKEOFF CONFIG ON EICAS. COMPLETED HIGH SPEED T AXI AND THRUST REVERSER OPS CHECK IAW AMM 78-31-01. COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. (M ) 2 L 7 2 4F RT TOOO11AT 2001071600166 20010716 00166 SO 2001 7 16 SIMA200115622 1 20010605 A 7540 WARNING LIGHT EMB 145 EMB145LR SO COCKPIT FALSE INDICATION A SIMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 624AE 145111 CMH - FLT 4093 - NR 2 BLEED LEAK IN FLIGHT. COULD NOT DUPLICATE PROBLEM. PERFORMED CHECKS IAW AMM. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001071600167 20010716 00167 EU 2001 7 16 SIMA200115623 1 20010605 A 7603 LEVER SAAB SF340 340B 7860101 EU COCKPIT OUT OF RIG A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 266AE 340B266 ABI - FLT 9730 - ON TAKEOFF ROLL, LEFT ENGINE CTOT DID NOT ENGAGE. RIGGED LEFT CONDITION LEVERS IAW AMM 76-10-00. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001071600168 20010716 00168 SO 2001 7 16 SIMA200115701 1 20010606 A 3610 G30020C O-RING EMB 145 EMB145LR SO BLEED AIR SYS LEAKING A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 624AE 145111 CMH - FLT 4160 - AIRCRAFT RETURNED TO FIELD FOR NR 1 BLEED LEAK. REMOVED AND REPLACED CARGO COMPARTMENT BLEED LINE O-RI NG IAW AMM 36-11-801-A AND 36-11-00-400-801-A. OPS CHECK GOOD. (M) 2 L 7 2 4T RT T00011AT 2001071600169 20010716 00169 SO 2001 7 16 SIMA200115702 1 20010606 A 7830 T8204103A CONTROL VALVE EMB 145 EMB145LR SO THRUST REVERSER FAULTY A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 613AE 145081 SHV - FLT 3370 - ABORTED TAKEOFF, NR 2 THRUST REVERSE DISAGREE ICAS MESSAGE. MEL REMOVED AND REPLACED NR 2 ISOLATION CO NTROL VALVE UNIT IAW EMB 78-33-01. OPS CHECK GOOD. (M) 2 L 7 2 4T RT T00011AT 2001071600170 20010716 00170 EA 2001 7 16 COMA0160476 1 20010708 A 5300 601R31527141 CHANNEL CNDAIR CL600 CL6002B19 EA CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 18999 7014 "U" CHANNEL P/N 601R31527-141 AT F.S. 349.00 IS CORRODED.REMOVED AND REPLACED "U" CHANNEL P/N 601R31527-141 AT F.S. 349. 00 I/A/W WVAC EO 601R-53-2558. 2 L 7 2 4F RT A21EA 2001071600171 20010716 00171 EA 2001 7 16 COMA0160477 1 20010708 A 5300 60034017595 ANGLE CNDAIR CL600 CL6002B19 EA CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 18999 7014 AFT "J" ANGLE AT F.S. 280 IS CORRODED BETWEEN LBL9 AND RBL 9.REMOVED DAMAGED, FABRICATED AND INSTALLED SPLICE "J" ANGLE I/A/W WVAC EO 601R-53-2552A. 2 L 7 2 4F RT A21EA 2001071600172 20010716 00172 SO 2001 7 16 SIMA200115703 1 20010606 A 7830 WARNING SYSTEM EMB 135 EMB135LR SO COCKPIT MALFUNCTIONED A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 700LE 145156 SAV - FLT 3478 - ABORTED TAKEOFF. THRUST REVERSE DISAGREE ICAS MESSAGE. PERFORMED OPS CHECKS AND HIGH SPEED RUNS IAW A MM. OPS CHECK GOOD. COULD NOT DUPLICATE. (M) 2 L 7 2 4F RT TOOO11AT 2001071600173 20010716 00173 SO 2001 7 16 SIMA200115706 1 20010606 A 5270 SWITCH EMB 145 EMB145LR SO CARGO DOOR OUT OF ADJ A SIMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 610AE 145073 BMI - FLT 4427 - CARGO DOOR WARNING LIGHT CAME ON INFLIGHT. DROPPED TO 10,000. RETURNED TO BASE. ADJUSTED FORWARD AND AFT MICROSWITCHES ON CARGO DOOR IAW AMM 52-76-01-820-801-A. OPS CHECK GOOD. (M) 2 L 7 2 4T RT T00011AT 2001071600174 20010716 00174 SO 2001 7 16 SIMA200115802 1 20010607 A 7830 ACTUATOR EMB 135 EMB135LR SO THRUST REVERSER OUT OF ADJ A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 701MH 145162 DFW - FLT 3423 - NR 2 THRUST REVERSER DISAGREE DURING TAKEOFF. ABORTED TAKEOFF. ADJUSTED NR 2 THRUST REVERSER ACTUATOR ROD ENDS IAW AMM 78-32-01-420-001-A00. OPS CHECK GOOD. (M) 2 L 7 2 4F RT TOOO11AT 2001071600175 20010716 00175 EU 2001 7 16 SIMA200115901 1 20010607 A 3350 LIGHT AEROSP ATR72 ATR72212A 8680902 EU PAX DOOR INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 494AE 494 DFW - FLT 3515 - EMERGENCY FLOOR LIGHTS ON AIRSTAIR INOPERATIVE. REPAIRED WIRES ON PAX DOOR FOR EMERGENCY LIGHTS IAW AM M. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 2001071600176 20010716 00176 SO 2001 7 16 SIMA200116207 1 20010611 A 7830 WARNING SYSTEM EMB 135 EMB135LR SO COCKPIT MALFUNCTIONED A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 704PG 145174 ORD - FLT 4243 - ABORTED TAKEOFF. REVERSE DISAGREE ICAS MESSAGE ON. PERFORMED HIGH SPEED RUNS IAW AMM. COULD NOT DUPL ICATE DISCREPANCY. (M) 2 L 7 2 4F RT TOOO11AT 2001071600177 20010716 00177 SO 2001 7 16 SIMA200116301 1 20010612 A 3350 7287580501 LIGHT EMB 145 EMB145LR SO CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 616AE 145092 DFW - FOUND ROWS 4 AND 6 EMERGENCY FLOOR LIGHTING INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT STRIP IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT T00011AT 2001071600178 20010716 00178 EA 2001 7 16 COMA0160478 1 20010713 A 5346 601350061 BEAM CNDAIR CL600 CL6002B19 EA CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 926CA 18280 7027 CRACKS FOUND IN ENGINE SUPPORT BEAM LOWER WEB BETWEEN FS 625.30 - 640.00 ON THE LEFT/RIGHT SIDE OF THE SUPPORT BEAMREPAI RS WERE ACCOMPISHED IN ACCORDANCE WITH REO 601R-53-61-366 REV B. 2 L 7 2 4F RT A21EA 2001071600179 20010716 00179 NE 2001 7 16 SIMA200116302 3 20010612 A 6140 CONNECTOR SAAB SF340 340B 7860101 EU ROTOL R354 R3544123F13 NE RT PROPELLER DIRTY A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 374AE 340B374 SGF - FLT 3610 - ON TAKEOFF ROLL, RIGHT PROP OIL AND TEMP GAUGE WENT TO ZERO. ABORTED TAKEOFF. RESET BREAKER AND CLEAN ED CANNON PLUG ON GAUGE IAW AMM. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 6 C P61GL 2001071600180 20010716 00180 SO 2001 7 16 SIMA200116303 1 20010612 A 3320 7287501537 LIGHT EMB 135 EMB135LR SO CABIN SMOKE A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 714BZ 145260 LGA - FLT 4504 - FOUND OVERHEAD LIGHT AT SEAT 8A CREATED SMOKE AND SPARKS. REMOVED AND REPLACED LIGHT ASSEMBLY IAW WORK CARD 33-21-06-00-801-A. OPS CHECK GOOD. (M) 2 L 7 2 4F RT TOOO11AT 2001071600181 20010716 00181 EU 2001 7 16 SIMA200116401 1 20010613 A 7603 LEVER SAAB SF340 340B 7860101 EU COCKPIT OUT OF RIG A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 313AE 340B313 DFW - CONFIG WARNING ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE. RIGGED LEFT CONDITION LEVER IAW AMM 76-10-00. OPS CHECK GOOD. PARAMETERS RUN GOODS. (M) 2 L 7 2 4T RT A52EU 2001071600182 20010716 00182 EA 2001 7 16 COMA0160479 1 20010715 A 5346 601350061 BEAM CNDAIR CL600 CL6002B19 EA CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 918CA 18726 7018 R/H ENGINE SUPPORT BEAM CRACKED FWD L/H SIDE.R/H ENGINE SUPPORT BEAM REPAIRED I/A/W REO 601R-53-61-366 REV B. 2 L 7 2 4F RT A21EA 2001071600183 20010716 00183 NM 2001 7 16 ABXA010399 1 20010711 A 5610 1894T1001 GEARBOX BOEING 767 767281 1385109 NM COCKPIT DEFECTIVE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 775AX 22790 FIRST OFFICER'S OPENABLE WINDOW, HAND CRANK WOULD NOT OPEN OR CLOSE WINDOW. REPLACED FIRST OFFICER'S OPERATING GEARBOX I AW B767 56-11-04-4. OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2001071600184 20010716 00184 EU 2001 7 16 SIMA200116402 1 20010613 A 2120 DUCT SAAB SF340 340B 7860101 EU AIR CONDITIONING LOOSE A SIMA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 21 244AE 340B244 DFW - FLT 5115 - ON TAXI, HAD MULTIPLE LAVATORY SMOKE INDICATIONS ON CWP. RETURNED TO GATE. FOUND LOOSE AIR CONDITIONI NG DUCT BY LAVATORY SMOKE DETECTOR. TIGHTEN DUCT AND PERFORMED OPS CHECK IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001071600185 20010716 00185 SO 2001 7 16 SIMA200116501 1 20010614 A 7830 DOOR EMB 145 EMB145LR SO THRUST REVERSER OUT OF ADJ A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 639AE 145182 CID - FLT 3954 - ON TAKEOFF ROLL HAD NR 1 THRUST REVERSER DISAGREE AND THAN NR 2. ABORTED TAKEOFF AND RETURNED TO GATE. ADJUSTED LEFT AND RIGHT THRUST REVERSE ACTUATOR DOORS IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT T00011AT 2001071600186 20010716 00186 EA 2001 7 16 COMA0160395 1 20010619 A 5300 601R3103077 SPLICE PLATE CNDAIR CL600 CL6002B19 EA MISMANUFACTURED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 967CA 7134 TWO SPLICE PLATES P/N 601R31030-71 WERE FABED INCORRECTLY BY MANUFACTURER.FABED TWO DOUBLER PLATES, REWORKED SPLICE PLAT ES AND INSTALLED DOUBLER PLATES I/A/W WVAC EO 601R-53-2511. 2 L 7 2 4F RT A21EA 2001071600187 20010716 00187 WP 2001 7 16 CALA0100549 1 20010617 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND LT FUSELAGE EXTERNAL SKIN CREASED FORWARD OF AOA VANE AT FS 70. A NEW DOUBLER WAS INSTALLED IAW SRM 53 -01, FIGURE 2, 51-10-4, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 2001071600188 20010716 00188 NM 2001 7 16 CALA0100550 1 20010618 A 3234 10612131 SELECTOR VALVE BOEING 737 7373T0 1384582 NM LANDING GEAR INOPERATIVE A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 14320 51893 23371 THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM CLE. QRH WAS COMPLETED AND THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. TROUBLESHOOTING FOUND THE LANDING GEAR SELECTOR VALVE AT FAULT. THE LG SELECTOR VALVE WAS REMOVED AND REPLACED IAW MM 32-31-51. LEAK AND OPERATIONAL CHECKS WERE GOOD. THE GROUND SPOILER INTERLOCK VALVE CABLE WAS ALSO REMOVED AND REPLACED IAW MM 27-62-51 DUE TO BINDING. 2 L 7 2 4F RT A16WE 2001071600189 20010716 00189 WP 2001 7 16 CALA0100552 1 20010618 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND LT LAV WALL AND FLOOR SUPPORT CORRODED AT FS 1303 - 1338. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOO R SUPPORT WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 2001071600190 20010716 00190 EA 2001 7 16 COMA0160417 1 20010630 A 5270 DOOR CNDAIR CL600 CL6002B19 EA A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 409CA 7441 CARGO DOOR CAUTION MESSAGE.DEFERRED MAINTENANCE ON DOOR WARNING SYSTEM PER MEL 52-70-04. 2 L 7 2 4F RT A21EA 2001071600191 20010716 00191 NM 2001 7 16 CALA0100553 1 20010615 A 2424 766300F GCU BOEING 767 767424ER NM RT ENGINE FAILED A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 76055 1147 29450 THE RT GENERATOR AND RT AC BUS WERE LOST AND SMOKE ENTERED THE COCKPIT AND CABIN WHILE EN ROUTE FROM EWR TO GRU. THE AP U WAS STARTED, BUT IT WOULD NOT RECOVER THE RT AC BUS. THE AIRCRAFT WAS DIVERTED TO BSB WHERE IT LANDED WITHOUT INCIDEN T. MAINTENANCE FOUND THE RT GCU BURNED OUT. THE RT GCU WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A1NM 2001071600192 20010716 00192 WP 2001 7 16 CALA0100554 1 20010618 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND A 4 INCH CRACK IN MAIN CABIN CUSP WEB AT FS 1245, LBL 56. THE CRACK WAS STOP DRILLED IAW SRM 53-01, FI GURE 1. A DOUBLER WAS INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-2, AND 53-01, FIGURE 1. 2 L 7 2 4F A6WE 2001071600193 20010716 00193 WP 2001 7 16 CALA0100555 1 20010618 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND A 6 INCH CRACK IN MAIN CABIN CUSP WEB AT FS 1198, LBL 56. A DOUBLER WAS INSTALLED IAW SRM 51-30-2, 53- 01, FIGURE 2, AND 51-10-3. 2 L 7 2 4F A6WE 2001071600194 20010716 00194 WP 2001 7 16 CALA0100556 1 20010618 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND RT FUSELAGE EXTERNAL SKIN CREASED AT FS 370, JUST BELOW LONGERON 19R. THE AREA WAS COLD WORKED AND A D OUBLER WAS INSTALLED IAW SRM 51-10-3 AND 53-04, FIGURE 38, SHEET 22. 2 L 7 2 4F A6WE 2001071600195 20010716 00195 WP 2001 7 16 CALA0100557 1 20010619 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND MAIN CABIN CUSP WEB CORRODED AT FS 200 - 218, LBL 20. THE CORRODED AREA WAS CUT OUT IAW SRM 53-01, FIG URE 1, SHEET 1. A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 1, 51-10-4, 51-10-3, 51-30-2, AND 51-30-8. 2 L 7 2 4F A6WE 2001071600196 20010716 00196 NM 2001 7 16 F3LA200100095 1 20010713 A 5330 SKIN BOEING 737 737317 138447P NM CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 545 23177 DURING A-3 CHECK, MAINTENANCE REPORTED A 2" CRACK IN FUSELAGE SKIN AT STA. 727E, STR. 18R. REMOVED DAMAGED AREA, FABRIC ATED REPAIR DOUBLER AND INSTALLED PER SRM 53-00-01. 2 L 7 2 4F RT A16WE 2001071600197 20010716 00197 EU 2001 7 16 RAIA00107009 1 20010713 A 3246 31518 WHEEL AEROSP ATR42 ATR42300 8680920 EU FAILED A RAIA A UNSCHED LANDING D INFLIGHT SEPARATION TO TAKEOFF 1 CE 03 423TE B37 119 7003-STL-DURING TAKEOFF TO CLIMB, THE LEFT MAIN LANDING GEAR OUTBOARD WHEEL ASSEMBLY DEPARTED THE AIRCRAFT. THE AIRCRAFT LANDED WITHOUT INCEDENT. MAINTENANCE INSPECTED THE LEFT MAIN LANDING GEAR AND AXLE ASSEMBLY. MAINTENANCE REPLACED THE L EFT MAIN LANDING GEAR AXLE ASSEMBLY, LEFT MAIN OUTBOARD BRAKE ASSEMBLY AND LEFT MAIN OUTBOARD LANDING GEAR WHEEL. INVEST IGATION IS ONGOING TO DETERMINE CAUSES. 2 H 7 2 4T RT A53EU 2001071600198 20010716 00198 SO 2001 7 16 RAIA00107010 1 20010713 A 8011 35059104 STARTER EMB 145 EMB145ER SO ALLSN AE300 AE3007A GL FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 807HK 4533 145119 310131 5284-MEM-LEFT ENGINE WILL NOT START. MAINTENANCE INSPECTED AND REPLACED THE LEFT ENGINE AIR TURBINE STARTER. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001071600199 20010716 00199 EU 2001 7 16 RAIA00107011 1 20010714 A 3350 3011151 BATTERY AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 424TE 124 7003-STL-EMERGENCY LIGHTING REMAINS ON ALL THE TIME. MAINTENANCE INSPECTED AND REPLACED EMERGENCY LIGHT BATTERY PACK. 2 H 7 2 4T RT A53EU 2001071600200 20010716 00200 2001 7 16 RAIA00107012 4 20010715 A 3420 7003360904 COMPUTER AEROSP ATR72 ATR72202 8680940 EU AVIONICS BAY FAILED A RAIA A UNSCHED LANDING I FLT. ATTITUDE INST. CL CLIMB 1 CE 03 721TE 20347 217 7009-STL-FIRST OFFICERS EFIS PITCH COMPARATOR DISAGREE ILLUMINATED. MAINTENANCE INSPECTED AND REPLACED THE #2 AHRS COMPU TER. 2 H 7 2 4T RT A53EU 2001071600201 20010716 00201 NM 2001 7 16 USAA010632 1 20010608 A 5300 FRAME BOEING 737 737301 1384611 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND FRAME CRACKED .5 INCH, BS 747, BETWEEN STRINGER 8/9R. DAMAGED REMOVED, INSTALLED DOUBLER AND FILLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001071600202 20010716 00202 NM 2001 7 16 USAA010631 1 20010608 A 5300 FRAME BOEING 737 737301 1384611 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND FRAME CRACKED 1 INCH, BS 727D, BETWEEN STRINGER 8L AND 9L. DAMAGED REMOVED, INSTALLED REPAIR DOUBLER AND FI LLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001071600203 20010716 00203 NM 2001 7 16 USAA010630 1 20010608 A 5300 FRAME BOEING 737 737301 1384611 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND FRAME CRACKED 1 INCH, BS 747, BETWEEN STRINGER 8/9L. DAMAGED REMOVED, INSTALLED REPAIR PER TYPICAL REPAIR 5 3-10-14. (M) 2 L 7 2 4F RT A16WE 2001071600204 20010716 00204 NM 2001 7 16 USAA010629 1 20010608 A 5300 FRAME BOEING 737 737301 1384611 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND FRAME CRACKED .5 INCH, BS 787, STRINGER 8 AND 9 RIGHT. DAMAGED REMOVED, INSTALLED DOUBLER PER TYPICAL REPAI R 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001071600205 20010716 00205 NM 2001 7 16 USAA010628 1 20010608 A 5300 FRAME BOEING 737 737301 1384611 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND FRAME CRACKED 1 INCH, BS 727, STRINGER 16R. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER, FILLERS, ANGLES PER E A 69664. (M) 2 L 7 2 4F RT A16WE 2001071600206 20010716 00206 NM 2001 7 16 USAA010627 1 20010608 A 5300 69387901 TIE CLIP BOEING 737 737301 1384611 NM BS 597 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND STRINGER TIE CLIP CRACKED .25 INCH, BS 597, STRINGER 10R. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-2. ( M) 2 L 7 2 4F RT A16WE 2001071600207 20010716 00207 NM 2001 7 16 USAA010626 1 20010608 A 5310 69387902 TIE CLIP BOEING 737 737301 1384611 NM BS 578 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND TIE CLIP CRACKED .25 INCH, BS 578, STRINGER 10R. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 2001071600208 20010716 00208 NM 2001 7 16 USAA010639 1 20010608 A 5310 FRAME BOEING 737 737301 1384611 NM BS 500C CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND FRAME CRACKED.5 INCH, BS 500C, STRINGER 8R. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001071600209 20010716 00209 NM 2001 7 16 USAA010638 1 20010608 A 5310 FRAME BOEING 737 737301 1384611 NM BS 400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND FRAME CRACKED .5 INCH, BS 400, STRINGER 8L. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001071600210 20010716 00210 NM 2001 7 16 USAA010637 1 20010608 A 5300 FRAME BOEING 737 737301 1384611 NM BS 440 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND FRAME CRACKED .5 INCH, BS 440, STRINGER 8L. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001071600211 20010716 00211 NM 2001 7 16 USAA010636 1 20010608 A 5300 FRAME BOEING 737 737301 1384611 NM BS 400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND FRAME CRACKED .5 INCH, BS 400 STRINGER 8R. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001071600212 20010716 00212 NM 2001 7 16 USAA010635 1 20010608 A 5300 FRAME BOEING 737 737301 1384611 NM BS 500A CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND FRAME CRACKED .5 INCH, BS 500A, STRINGER 8L. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001071600213 20010716 00213 NM 2001 7 16 USAA010687 1 20010517 A 5300 SEAT TRACK BOEING 737 737301 1384611 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND SEAT TRACK CORRODED 1 INCH BY 4 INCHES, LT INBOARD AFT OF BS 344. CORROSION LEVEL 1, TASK NR C53-107-01. C UT OUT DAMAGE, INSTALLED NEW AND SPLICE PER SRM 53-00-52, FIG 203. (M) 2 L 7 2 4F RT A16WE 2001071600214 20010716 00214 NM 2001 7 16 USAA010703 1 20010517 A 5300 STRINGER BOEING 737 737301 1384611 NM BS 967 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND STRINGER CUT TO FASCILITATE CLIP REMOVAL, BS 967 AT S25L. SPLICED STRINGER PER SRM 53-00-3. (M) 2 L 7 2 4F RT A16WE 2001071600215 20010716 00215 WP 2001 7 16 USAA010685 1 20010605 A 5340 ATTACH ANGLE DOUG DC9 DC982 3022082 WP FS 1463 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 829US 41770 49429 PIT - FOUND ATTACH ANGLE CRACKED .75 INCH, RIGHT UPPER PYLON ATTACH ANGLE CANTED STATION 1464. STOP DRILLED CRACK PER T YPICAL REPAIR 54-10-06A. (M) 2 L 7 2 4F A6WE 2001071600216 20010716 00216 WP 2001 7 16 USAA010683 1 20010611 A 5300 FRAME DOUG DC9 DC981 3022081 WP BS 1437 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 812US 53328 48092 PIT - FOUND FRAME CRACKED .5 INCH, STATION 1437 AT L16R. STOP DRILLED CRACK, INSTALLED DOUBLER PER TYPICAL REPAIR 53-01 . (M) 2 L 7 2 4F A6WE 2001071600217 20010716 00217 WP 2001 7 16 USAA010682 1 20010611 A 5330 SKIN DOUG DC9 DC981 3022081 WP BS 1380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 803US 54621 48035 PIT - FOUND SKIN CRACKED .125 INCH, STATION 1380 AT L14L. CUT OUT CRACK, INSTALLED FILLER AND DOUBLER PER SRM 53-01 FIG 2 SHT 3. (M) 2 L 7 2 4F A6WE 2001071600218 20010716 00218 NM 2001 7 16 UIEA01070 1 20010626 A 5300 65B017155003 FRAME BOEING 747 747243B 1384830 NM BS 440 CRACKED A UIEA O OTHER O OTHER IN INSP/MAINT 1 EA 15 516MC 77446 22507 DURING INSPECTION, FOUND FRAME WEB AND DOUBLER STATION 440 CRACKED AT STRINGER 13R, CRACK ENDS IN EXISTING FASTENER LOCA TION. PERFORMED OPEN HOLE HFEC INSPECTION TO ENSURE CRACK CONTAINMENT. FABRICATED DOUBLERS AND FILLERS. INSTALLED PER STANDARD PRACTICES IAW SRM 53-10-04. REINSPECT AREA PER SB 747-53A2265 AT 3000 CYCLE INTERVALS. (M) 2 L 7 4 4F A20WE 2001071600219 20010716 00219 NM 2001 7 16 UIEA01071 1 20010626 A 5310 65B0187031 INTERCOSTAL BOEING 747 747243B 1384830 NM BS 340-380 CRACKED A UIEA O OTHER O OTHER IN INSP/MAINT 1 EA 15 516MC 77446 22507 DURING INSPECTION, FOUND MAIN DECK FLOOR LINE INTERCOSTALS FROM STATION 340-380 LEFT CRACKED AT NUMEROUS FASTENER HOLES. TRIMMED OFF SHEAR TIES CONTAINING CRACKED FASTENER HOLES. PERFORMED HFEC INSPECTION AT CUT LINE TO ENSURE NO CRACKS. NO CRACKS FOUND. FABRICATED REPAIR ANGLES, INSTALLED PER STANDARD SRM PRACTICES. (M) 2 L 7 4 4F A20WE 2001081500091 20010815 00091 NM 2001 8 15 01FDEA00542 1 20010703 A 5310 SHEAR TIE BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 221FE 20932 CORROSION ON SHEAR TIE BS 640, LBL 2, WL 146. *S/D* REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-4 FIG 15. 2 L 7 3 4F RT A3WE 2001081500094 20010815 00094 NM 2001 8 15 01FDEA00543 1 20010703 A 5330 SKIN BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 221FE 20932 CORROSION (C53-113-01,1) ON INNER SKIN BS 640, RBL 15, WL 148. *S/D* REMOVED AND REPLACED SKIN PER SRM 53-30-3 FIG 3. 2 L 7 3 4F RT A3WE 2001081500084 20010815 00084 NM 2001 8 15 01FDEA00540 1 20010705 A 5330 SKIN BOEING 727 727233 138408A NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 221FE 20932 DAMAGE ON EDGE OF EXTERNAL SKIN AT BS 1352, 3 AREAS FROM STR 20R-23R. *S/D* REMOVED AND REPLACED SKIN PER SRM 53-30-1. 2 L 7 3 4F RT A3WE 2001071700001 20010717 00001 NM 2001 7 17 SWAA011977 1 20010708 A 5330 6545765 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D CHECK AT DALFORT, FOUND FUSELAGE SKIN CRACKED AT BS 518, STR 12L. REPAIRE D SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001071700002 20010717 00002 NM 2001 7 17 SWAA011979 1 20010711 A 5311 65C33722 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED 1/2D CHECK, FOUND FRAME CRACKED AT BS 616, STR 17L. REPAIRED FRAME PER SWA TI. 2 L 7 2 4F RT A16WE 2001071700003 20010717 00003 NM 2001 7 17 SWAA011981 1 20010712 A 2731 6573782 TAB BOEING 737 7373H4 1384600 NM RH ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED 1/2D CHECK, FOUND RH ELEVATOR TAB INBD HINGE WORN. R&R TAB PER MM. 2 L 7 2 4F RT A16WE 2001071700004 20010717 00004 NM 2001 7 17 SWAA011982 1 20010629 A 5754 65C26601 SLAT BOEING 737 7373Q8 1384670 NM LH WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D CHECK AT DALFORT, FOUND # 1 L/E SLAT LOWER SKIN CRACKED AT OTBD END. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001071700005 20010717 00005 NM 2001 7 17 SWAA011966 1 20010709 A 2730 BACB28AK04 BUSHING BOEING 737 7377H4 NM RH ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 705SW 27839 DURING SCHEDULED SERVICE CHECK, SI 11052-55, FOUND RH ELEVATOR TAB # 3 HINGE BUSHING WORN. R&R HINGE B USHING PER MM. 2 L 7 2 4F RT A16WE 2001071700006 20010717 00006 NM 2001 7 17 SWAA011967 1 20010710 A 5314 47977 WEB BOEING 737 7377H4 NM RH MLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 725SW 27857 DURING SCHEDULED C1 CHECK, FOUND RH MLG W/W AFT WEB CRACKED. R&R WEB PER SRM. 2 L 7 2 4F RT A16WE 2001071700007 20010717 00007 NM 2001 7 17 SWAA011969 1 20010710 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 386SW 26601 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED AT ROWS # 3, # 4, # 11 & # 24. R&R EEPLS CO VERS PER MM. 2 L 7 2 4F RT A16WE 2001071700008 20010717 00008 NM 2001 7 17 SWAA011970 1 20010711 A 3350 65C34691 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 352SW 24888 DURING SCHEDULED A1 CHECK, FOUND BULLNOSE EMERGENCY LIGHT COVER MISSING. INSTALLED BULLNOSE COVE R PER MM. 2 L 7 2 4F RT A16WE 2001071700009 20010717 00009 NM 2001 7 17 SWAA011971 1 20010710 A 3350 65C27093 LENS BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 330SW 23694 DURING SCHEDULED C3 CHECK, FOUND SIDE WALL EMERGENCY LIGHT LENS BROKEN AT FWD ENTRY. R&R LENS PER MM. 2 L 7 2 4F RT A16WE 2001071700010 20010717 00010 NM 2001 7 17 SWAA011974 1 20010711 A 5310 6546546 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 316SW 23338 DURING SCHEDULED SERVICE CHECK, FOUND FRAME CRACKED AT BS 727E, STR 18R, WL 208. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001071700011 20010717 00011 NM 2001 7 17 SWAA011975 1 20010711 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM FWD SVC DOOR ERRATIC A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 FWD SVC DOOR EMERGENCY EXIT LIGHT WOULD NOT EXTINGUISH. R&R BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2001071700012 20010717 00012 NM 2001 7 17 SWAA011959 1 20010710 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 385SW 26600 EEPLS MISSING COVER. REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2001071700013 20010717 00013 NM 2001 7 17 SWAA011960 1 20010710 A 3350 6556633 LENS BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 367SW 26578 LH OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. R&R EXIT LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2001071700014 20010717 00014 NM 2001 7 17 SWAA011963 1 20010709 A 5330 6516300 WEB BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED 1/4D CHECK, FOUND WEB CRACKED AT BS 178, LBL 11.0, WL 218. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001071700015 20010717 00015 NM 2001 7 17 SWAA011964 1 20010709 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 950, STR 24L. REPAIRED SKIN PER S RM. 2 L 7 2 4F RT A16WE 2001071700016 20010717 00016 NM 2001 7 17 SWAA011965 1 20010710 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 314SW 23336 DURING SCHEDULED SERVICE CHECK, FOUND 2 EA CRACKS AT FUSELAGE SKIN, BS 500 & 500D, STR 12L REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001071700017 20010717 00017 NM 2001 7 17 SWAA011932 1 20010709 A 3350 07912 COVER BOEING 737 7377H4 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 708SW 27842 EEPLS MISSING COVER AT ROW 11. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2001071700018 20010717 00018 NM 2001 7 17 SWAA011936 1 20010708 A 3350 65C34691 LENS BOEING 737 7377H4 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 750SA 29802 DURING SCHEDULED A2 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 16 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2001071700019 20010717 00019 NM 2001 7 17 SWAA011938 1 20010707 A 3350 07912 COVER BOEING 737 7377H4 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 751SW 29803 EEPLS COVER CRACKED. R&R COVER PER MM. 2 L 7 2 4F RT A16WE 2001071700020 20010717 00020 NM 2001 7 17 SWAA011939 1 20010709 A 5311 6516303 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 521SW 25320 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 296, RBL 54, WL 209. REPAI RED FRAME PER BFG ER. 2 L 7 2 4F RT A16WE 2001071700021 20010717 00021 NM 2001 7 17 SWAA011940 1 20010706 A 2731 BACB28AMO7 BUSHING BOEING 737 7373H4 1384600 NM LH ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED C2 CHECK, LH ELEVATOR TAB FAILED FREE PLAY CHECK. R&R ELEVATOR TAB BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2001071700022 20010717 00022 NM 2001 7 17 SWAA011942 1 20010707 A 5330 65C35794 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 662SW 23255 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727 + 12 IN, STR 19R. REPAI RED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001071700023 20010717 00023 NM 2001 7 17 SWAA011944 1 20010625 A 5510 65C27494 SKIN BOEING 737 7375H4 138449D NM RH HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 521SW 25320 DURING SCHEDULED D CHECK, FOUND RH HORIZ STAB LOWER SKIN CRACKED AT STA 124. REPAIRED SKIN PER SWA ACO. 2 L 7 2 4F RT A16WE 2001071700024 20010717 00024 NM 2001 7 17 SWAA011945 1 20010708 A 2731 BACB28AK04 BUSHING BOEING 737 7377H4 NM LH ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 750SA 29802 DURING SCHEDULED A2 CHECK, SWA SI 11038-55, FOUND LH ELEVATOR TAB # 4 HINGE WORN. R&R # 4 TA B HINGE BUSHING PER MM. 2 L 7 2 4F RT A16WE 2001071700025 20010717 00025 NM 2001 7 17 SWAA011946 1 20010708 A 5330 65C35794 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 087SW 22903 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727A, STR 10R & BS 625, STR 4R. REPAIRED SKINS PER SWA RA. 2 L 7 2 4F A16WE 2001071700026 20010717 00026 NM 2001 7 17 SWAA011947 1 20010709 A 2731 BACB28AK04 BUSHING BOEING 737 7377H4 NM RH ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 726SW 27858 DURING SCHEDULED SERVICE CHECK, SWA SI 11075-55, FOUND RH ELEVATOR TAB HINGE BUSHINGS WORN AT HINGE'S #2, #3 & #4. R&R HINGE BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2001071700027 20010717 00027 NM 2001 7 17 SWAA011986 1 20010713 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED 1/2D CHECK, FOUND FLOOR BEAM UPPER T CHORD CRACKED AT BS 344, LBL 9. REPAIRED FLOOR BEAM TEE PER SRM. 2 L 7 2 4F RT A16WE 2001071700028 20010717 00028 NM 2001 7 17 SWAA011987 1 20010702 A 5330 6552988 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 521SW 25320 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER BFG ER & SRM. 2 L 7 2 4F RT A16WE 2001071700029 20010717 00029 NM 2001 7 17 SWAA011988 1 20010713 A 5314 BAC1503 STIFFENER BOEING 737 7373A4 1384585 NM MAIN WHEEL WELL CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED 1/4D CHECK, FOUND MLG WHEEL WELL BULKHEAD VERTICAL STIFFENER CRACKED AT BS 663, RBL 6.5. REPAIRED STIFFENER PER SWA RA. 2 L 7 2 4F RT A16WE 2001071700030 20010717 00030 NM 2001 7 17 SWAA011991 1 20010712 A 5754 6573714 SLAT BOEING 737 7373H4 1384600 NM LH WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED 1/2D CHECK, FOUND # 4 L/E SLAT LOWER SKIN CRACKED OTBD OF ACTUATOR ATTACH. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001071700031 20010717 00031 NM 2001 7 17 VNAA0107012 1 20010708 A 3200 S4340200001 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 434JS 15182 3051 DURING TAXI THE CREW RECEIVED A EMERGENCY PARKING BRAKE ACCUMULATOR FAIL CAS MESSAGE. THE CREW REFERENCED THE QUICK REF ERENCE HANDBOOK AND FOLLOWED THE PROCEDURES AND THE MESSAGE CLEARED. DURING FURTHER TAXI, THE CREW RECEIVED THE SAME ME SSAGE AND CONTACTED MAINTENANCE CONTROL WHO CONFIRMED THE QUICK REFERENCE HANDBOOK PROCEDURE WAS COORECT. THE MESSAGE H AD CLEARED AND ASKED MAINTENANCE CONTROL FOR VERIFICATION TO DEPART. DURING CLIMBOUT THE CREW RECEIVED THE EMERGENCY PA RKING BRAKE ACCUMULATOR FAIL MESSAGE AND WERE ADVISED TO RETURN TO PIT. MAINTENANCE INSPECTED AND REPLACED THE EMERGENC Y PARKING BRAKE CHECK VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED A 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001071700032 20010717 00032 WP 2001 7 17 MWEA011053 1 20010717 A 5510 59180001 CAP DOUG DC9 DC914 3022034 WP STATION XHS 146 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 CRACK INDICATION ON LEFT HORIZONTAL STABILIZER REAR SPAR LOWER CAP, EXTENDING BETWEEN TWO RIVETS, CONFIRMED BY HFEC STAT ION XHS 146 APPROXIMATELY. -- REMOVED CORROSION, FABRICATED FILLER, DRILLED AND INSTALLED REPAIR ANGLE AND FILLER. 2 L 7 2 4F A6WE 2001071700033 20010717 00033 SO 2001 7 17 20010613CW004 2 20010413 A 8540 632330 BEARING CESSNA 421 421C 2076016 CE CONT O520 GTSIO520L 17032 SO ENGINE SEIZED B OF1R K NONE K FLUID LOSS IN INSP/MAINT 1 EA 17 6794D 1590 239 421C1030 AT 25 HR OIL CHANGE, INTERVAL OIL WAS FOUND VENTING OUT THE RIGHT ENGINE OVERBOARD DRAIN AND THE OIL DRAINED FROM THE EN GINE HAD A METALLIC GLIMMER TO IT, ALTHOUGH CUTTING THE OIL FILTER DID NOT REVEAL ANY UNUSUAL AMOUNT OF METAL. OIL VE NTING WAS TRACED TO ENGINE DRIVEN HYDRAULIC PUMP ACCESSORY DRIVE. PUMP AND DRIVE ASSY WERE REMOVED AND INSPECTED. PLAI N BEARING IN ADAPTOR HAD SEIZED TO THE DRIVE SHAFT AND WAS SPINNING IN THE HOUSING, GALLING AND DEPOSITING SIGNIFICANT AMOUNT OF BRONZE AND ALUMINUM INTO OIL SUMP THROUGH ACCESSORY CASE. GALLING PRODUCED ENOUGH HEAT TO MELT REAR SHAFT SEAL WHICH WAS WHY OIL HAD STARTED VENTING OVERBOARD. PARTS WERE ALL REPLACED WITH NEW AND ENGINE, ACCESSORIES FLUSHED 1 L 7 2 3O 3 O A7CE E7CE 2001071700034 20010717 00034 SO 2001 7 17 20010613CW005 2 20010413 A 8540 632799 DRIVE SHAFT CESSNA 421 421C 2076016 CE CONT O520 GTSIO520L 17032 SO ENGINE SEIZED B OF1R K NONE K FLUID LOSS IN INSP/MAINT 1 EA 17 6794D 1590 239 421C1030 AT 25 HR OIL CHANGE, INTERVAL OIL WAS FOUND VENTING OUT RIGHT ENGINE OVERBOARD DRAIN AND OIL DRAINED FROM ENGINE HAD MET ALLIC GLIMMER TO IT, ALTHOUGH CUTTING THE OIL FILTER DID NOT REVEAL ANY UNUSUAL AMOUNT OF METAL. OIL VENTING WAS TRACED TO ENGINE DRIVEN HYDRAULIC PUMP ACCY DRIVE. PUMP AND DRIVE ASSY WERE REMOVED AND INSP. PLAIN BEARING IN THE ADAPTER H AD SEIZED TO DRIVE SHAFT AND WAS SPINNING IN HOUSING, GALLING AND DEPOSITING SIGNIFICANT AMOUNT OF BRONZE AND ALUMINUM I NTO OIL SUMP THROUGH THE ACCY CASE. THIS GALLING PRODUCED ENOUGH HEAT TO MELT REAR SHAFT SEAL WHICH WAS WHY OIL HAD STA RTED VENTING OVERBOARD. PARTS WERE ALL REPLACED WITH NEW, ENGINE AND ACCESSORIES FLUSHED. 1 L 7 2 3O 3 O A7CE E7CE 2001071700038 20010717 00038 CE 2001 7 17 2001F00069 1 20010615 A 2840 CONNECTOR BEECH 90 C90 1152913 CE FUEL SYSTEM CORRODED D KIMA K NONE N FALSE WARNING NR NOT REPORTED 1 EA 21 96DQ LJ814 NO FUEL TRANSFER LIGHT WOULD STAY ILLUMINATED EVEN IF FUEL WAS BEING TRANSFERRED. THIS WAS AN INTERMITTENT PROBLEM AND WAS NOT ABLE TO BE SOLVED UNTIL THE PROBLEM OCCURRED WHEN A MECHANIC COULD TROUBLESHOOT THE SYSTEM. AT TIMES THE NO FUE L TRANSFER LAMP WOULD COME ON WITH NO AIRCRAFT POWER APPLIED ALSO. VISUAL EXAMINATION OF CANON PLUG DID NOT REVEAL ANY DEFECTS (IE CORROSION OR BENT PINS) BUT DISASSEMBLY REVEALED EXTENSIVE CORROSION TO PIN BACKS AND SEVERAL SHORED PINS. INSTALLATION OF NEW PINS AND CANON PLUG FIXED PROBLEM. 1 L 7 2 3T 3A20 2001071700043 20010717 00043 WP 2001 7 17 MWEA011054 1 20010717 A 5740 99117731 SKIN DOUG DC9 DC914 3022034 WP STA. XFS 202-299 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 NUMEROUS CRACKS ON LEFT WING UPPER AND LOWER INNER SKIN OF #2 LEADING EDGE, BETWEEN STATIONS XFS 202.400 - 299.939. -- REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F A6WE 2001071700045 20010717 00045 EU 2001 7 17 2001F00112 1 20010620 A 2435 23032022 STARTER GEN SNIAS 350 AS350BA 8680817 EU LYC LTS101 LTS101600A3 41560 NE ENGINE FAULTY D IXXA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 WP 19 57717 593 1334 LE43402CE AIRCRAFT ENGINE BEGAN SURGING IN FLIGHT WITH EVIDENCE OF POWER LOSS BY ROTOR RPM DROOP. A PRECAUTIONARY LANDING WAS COM PLETED WITH ENGINE OPERATING. A NORMAL SHUTDOWN/COOLDOWN WAS COMPLETED. SUBSEQUENT GROUND RUN VERIFIED STRONG HIGH FRE QUENCY VIBRATION IN BOTH STARTER GENERATOR AND FUEL CONTROL AND ENGINE SURGING. REPLACEMENT OF STARTER GENERATOR CORREC TED DEFECT. BAD STARTER, OVERHAULED IN 1993. SUSPECT GREASE DRIED UP. RECOMMENDED CALENDER BASED BEARING REPLACEMENT S. 1 G 7 1 3U 3 U NC H9EU E5NE 2001071700047 20010717 00047 CE 2001 7 17 GLBA2001158 1 20010715 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE FAILED A GLBA D RETURN TO BLOCK O OTHER DE DESCENT 1 CE 01 96UX 64 UE96 BATTERY CHARGE ANNUNCIATOR ILLUMINATED INFLIGHT, REPLACED BATTERY 2 L 7 2 4T RT A24CE 2001071700048 20010717 00048 CE 2001 7 17 GLBA2001157 1 20010714 A 3210 50060285 TIRE BEECH 1900 1900D 1154162 CE #3 BLEW OUT A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 01 245GL 171 UE245 #3 TIRE BLEW OUT ON T/O, REPLACED TIRE 2 L 7 2 4T RT A24CE 2001071700049 20010717 00049 WP 2001 7 17 ABXA010362 1 20010703 A 3350 60030451 BATTERY PACK DOUG DC9 DC933F 302207A WP COCKPIT DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 934AX 7583 765 47462 COCKPIT EMERGENCY LIGHTING WAS FOUND TO BE INOPERATIVE AT RFD. MAINTENANCE INSPECTED AND RE-SEATED THE EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. IN ILN AS A PRECAUTION, MAIN TENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK IAW DC-9 MM 33-5-02. 2 L 7 2 4F A6WE 2001071700051 20010717 00051 NM 2001 7 17 ABXA010363 1 20010702 A 5311 148T11504 FRAME BOEING 767 767281 1385109 NM FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 784AX 23017 DURING EDDY CURRENT INSPECTION OF THE RIGHT OUTER CHORD FLANGE, STA 1809.5, FOUND A CRACK AT WL 25.3. CRACK STARTED AT THE FORWARD END OF FLANGE, RAN THROUGH THE FIRST AND SECOND FASTENER HOLES TO THE AFT RADIUS, REF 53-80-04, FIG 1, NOTES 1 & 2 AD 2001-09-13. FLANGE WAS REPLACED IAW SB 767-53-0078. 2 L 7 2 4F RT A1NM 2001071700052 20010717 00052 NM 2001 7 17 ABXA010364 1 20010702 A 5311 148T11503 FRAME BOEING 767 767281 1385109 NM FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 784AX 23017 DURING EDDY CURRENT INSPECTION OF THE LEFT OUTER CHORD FLANGE, STA 1809.5, FOUND A CRACK AT WL 25.3. CRACK STARTED AT T HE FORWARD EDGE OF FLANGE AND RAN TO THE FIRST FASTENER HOLE. REF BOEING NDT MANUAL 53-80-04, FIG 1, NOTE 2 AD 2000-09- 13. FLANGE WAS REPLACED IAW SB 767-53-0078. 2 L 7 2 4F RT A1NM 2001071700053 20010717 00053 WP 2001 7 17 ABXA010368 1 20010618 A 5620 39197891 RETAINER DOUG DC9 DC932 3022066 WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 CRACK AT RADIUS OF FORWARD LOWER CORNER OF WINDOW RETAINER, FS 598 AND LONGERON 15 RIGHT. REPAIRED WINDOW RETAINER ON L OWER CORNER AT FS 598 AND LONGERON 15 RIGHT IAW DC-9 SRM DWG K07226. 2 L 7 2 4F A6WE 2001071700054 20010717 00054 WP 2001 7 17 ABXA010369 1 20010618 A 5315 991224357 FLOORBEAM DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 FLOORBEAM LOWER FORWARD ANGLE CORRODED AT FS 965 LT, LBL 22-44. REPAIRED AREA IAW REA D953-41486MR. 2 L 7 2 4F A6WE 2001071700055 20010717 00055 WP 2001 7 17 ABXA010370 1 20010618 A 5330 5920323513 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DENTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 REPAIR ON FUSELAGE SKIN DENTED AT STA 346, LONGERON 21 RIGHT. REPAIRED DAMAGE ON FUSELAGE SKIN IAW REA D953-41469MR. 2 L 7 2 4F A6WE 2001071700056 20010717 00056 WP 2001 7 17 ABXA010371 1 20010618 A 5330 5920323513 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DENTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 FUSELAGE SKIN DENTED AT STA 353 BETWEEN LONGERON 21 AND 22 RIGHT. REPAIRED DAMAGE ON FUSELAGE SKIN IAW REA D953-41469MR . 2 L 7 2 4F A6WE 2001071700057 20010717 00057 WP 2001 7 17 ABXA010372 1 20010618 A 5330 5920323513 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 FUSELAGE SKIN CREASED AT STA 358 BETWEEN LONGERONS 21 RIGHT AND 22 RIGHT. REPAIRED DAMAGE ON FUSELAGE SKIN IAW REA D953 -41469MR. CUTOUT WAS 2.1 INCH IN DIAMETER. 2 L 7 2 4F A6WE 2001071700058 20010717 00058 WP 2001 7 17 ABXA010373 1 20010619 A 5311 9912243 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 UPPER CARGO FLOOR FRAME AT STA 965 WAS HEAVILY CORRODED FROM LONGERON 26 LEFT OUTBOARD TO LONGERON 22 LEFT. REPAIRED IA W REA D953-41486MR. 2 L 7 2 4F A6WE 2001071700059 20010717 00059 WP 2001 7 17 ABXA010374 1 20010619 A 5311 9912243 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 UPPER AND LOWER SPLICE CHANNELS IN FRAME AT STA 937 WAS HEAVILY CORRODED AND BULGING ABOVE LONGERON 28 LEFT AND LONGERON 27 LEFT. REPLACED FRAME AT STA 937, LONGERON 28 TO LONGERON 25 LEFT IAW DC-9 SRM. 2 L 7 2 4F A6WE 2001071700060 20010717 00060 WP 2001 7 17 ABXA010375 1 20010619 A 5311 99196171 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 FORWARD RIGHT MAINFRAME AT STA 699 WAS CRACKED IN THE FORWARD FLOORBEAM POCKET UPPER FLANGE. VERIFIED WITH EDDY CURRENT INSPECTION. INSTALLED REPAIR DOUBLER IAW DC-9 EA 53400120-1. 2 L 7 2 4F A6WE 2001071700061 20010717 00061 WP 2001 7 17 ABXA010376 1 20010619 A 5311 9919619503N FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 AFT LEFT MAINFRAME AT STA 737 WAS CRACKED IN THE AFT FLOORBEAM POCKET UPPER FLANGE. VERIFIED WITH EDDY CURRENT INSPECTI ON. REPAIRED MAINFRAME IAW DC-9 EA 53400310-001-1. 2 L 7 2 4F A6WE 2001071700062 20010717 00062 WP 2001 7 17 ABXA010377 1 20010620 A 5315 9712243 FLOORBEAM DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 FLOORBEAM AT STA 965, LEFT BUTT LINE 45 WAS CORRODED ON AFT SIDE THROUGH LIGHTENING HOLE. REPAIRED FLOORBEAM IAW REA D9 53-41486MR. 2 L 7 2 4F A6WE 2001071700063 20010717 00063 WP 2001 7 17 ABXA010378 1 20010620 A 5315 99115441 FLOORBEAM DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 FORWARD SIDE OF FLOORBEAM WEB EXFOLIATED AT FS 389, AT APPROXIMATELY LEFT BUTT LINE 48. REPAIRED FLOORBEAM AT FS 389, L EFT BUTT LINE 48 IAW REA D953-41479. MATERIAL REMOVED WAS APPROXIMATELY 1 - 2 INCHES. 2 L 7 2 4F A6WE 2001071700064 20010717 00064 WP 2001 7 17 ABXA010379 1 20010620 A 5620 39197871 RETAINER DOUG DC9 DC932 3022066 WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 CRACK AT LOWER AFT FASTENER OF WINDOW RETAINER, FS 658 AND LONGERON 15 RIGHT. REPAIRED AREA IAW DC-9 SSRM K07226. 2 L 7 2 4F A6WE 2001071700065 20010717 00065 WP 2001 7 17 ABXA010380 1 20010620 A 5320 J060234 SPLICE DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, THE AFT PRESSURE BULKHEAD SPLICES WERE FOUND TO HAVE ELONGATED HOLES. REPAIRED AFT PRESSURE BULKHEAD TE E CAP SPLICES IAW REA D953-41487MR. 2 L 7 2 4F A6WE 2001071700066 20010717 00066 WP 2001 7 17 ABXA010381 1 20010703 A 2612 100105201 CONTROL UNIT DOUG DC9 DC941 302207N WP E/E BAY DEFECTIVE A ABXA K NONE N FALSE WARNING CR CRUISE 1 GL 23 975AX 47512 CARGO FIRE WARNING INDICATED FORWARD BELLY FIRE. SHORTLY AFTER, FIRE LIGHT WENT OUT, FORWARD SMOKE INOPERATIVE LIGHT CA ME ON. THEN REPEATED FIRE WARNING AGAIN. COMPLETED EMERGENCY PROCEDURE. REPLACED THE CENTRAL CONTROL UNIT. OPS CHECK ED GOOD IAW DC-9 AMM 26-15-00-5. 2 L 7 2 4F A6WE 2001071700067 20010717 00067 WP 2001 7 17 ABXA010382 1 20010710 A 3260 0080004003 CONTROL BOX DOUG DC9 DC941 302207N WP E/E BAY FAULTY A ABXA K NONE N FALSE WARNING CR CRUISE 1 GL 23 957AX 47759 AFTER GEAR RETRACTION, LEFT GEAR UNSAFE LIGHT WAS INTERMITTENTLY ON. RECYCLED GEAR, LIGHT REMAINED ON INTERMITTENTLY. OPERATED WITH RIGHT HYDRAULIC PUMP IN HIGH AND RESTRICTED AIRSPEED TO 300 KNOTS. REPLACED THE PROXIMITY CONTROL BOX AND THE MAIN GEAR UPLOCK SWITCH IAW DC-9 AMM 32. OPS CHECKED PROXIMITY SWITCH CONTROL BOX IAW DC-9 AMM 32-60-01-2. PERFOR MED GEAR SWING CHECK. OPS CHECKED GOOD IAW DC-9 MM. 2 L 7 2 4F A6WE 2001071700068 20010717 00068 WP 2001 7 17 ABXA010383 1 20010624 A 5312 5910163181 DOUBLER DOUG DC9 DC932 3022066 WP BULKHEAD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 AFT PRESSURE BULKHEAD CENTERLINE FINGER DOUBLER WAS CRACKED AND HAD A PIECE MISSING ON THE FORWARD SIDE OF BULKHEAD. RE PAIRED AREA IAW REA D953-41525. 2 L 7 2 4F A6WE 2001071700069 20010717 00069 WP 2001 7 17 ABXA010385 1 20010619 A 5311 FRAME DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 AFT LOWER CARGO FRAME AT STA 1440, LONGERON 35 RIGHT WAS CRACKED ABOVE LONGERON 35 RIGHT. REPLACED REPAIR ANGLE IAW DC- 8 SRM 53-2-0, 51-1-21, 51-1-20D, AND 51-1-8. 2 L 7 4 4F 4A25 2001071700070 20010717 00070 WP 2001 7 17 ABXA010386 1 20010607 A 5313 37585931 LONGERON DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 LONGERON 36 WAS CRACKED UNDER SPLICE FITTING AT STA 1350. RECEIVED LONGERON, DRILLED AND REAMED LONGERON IAW DC-8 SRM 5 1-3-2. INSTALLED IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F 4A25 2001071700071 20010717 00071 WP 2001 7 17 ABXA010387 1 20010607 A 5311 FRAME DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 MAIN CABIN BETWEEN STA 1180 TO 1160, FRAME 1180 AT LONGERON 4 LEFT WAS CORRODED. REMOVED CORROSION, ALODINED AND PRIMED IAW DC-8 SRM 51-1-8. CORROSION WITHIN LIMITS IAW DC-8 SRM 53-2-0. 2 L 7 4 4F 4A25 2001071700072 20010717 00072 WP 2001 7 17 ABXA010388 1 20010628 A 5330 57583231 SKIN DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 FUSELAGE SKIN BULGING AT FASTENER, AT APPROXIMATELY FS 205, LONGERON 31 LEFT. REMOVED CORROSION. REPLACED FINGER DOUBL ER AND REPAIRED AREA IAW DC-8 SRM 51-1-20D, 51-1-21, 53-2-0, 51-1-8, 51-1-11, AND REA D853-40861MR. 2 L 7 4 4F 4A25 2001071700073 20010717 00073 WP 2001 7 17 ABXA010389 1 20010702 A 5311 FRAME DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 AFT LOWER CARGO FRAME AT STA 1420, LONGERON 35 RIGHT WAS CRACKED ABOVE LONGERON 35 RIGHT. REMOVED AND REPLACED DAMAGED FRAME SECTION IAW DC-8 SRM. 2 L 7 4 4F 4A25 2001071700074 20010717 00074 WP 2001 7 17 ABXA010390 1 20010702 A 5320 57799298 INTERCOSTAL DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 AFT LOWER CARGO INTERCOSTAL CRACKED AT STA 1004, LONGERON 35 RIGHT. REMOVED AND REPLACED CRACKED INTERCOSTAL IAW DAC DW G 5779929, DC-8 SRM 51-1-8, AND 51-1-20D. 2 L 7 4 4F 4A25 2001071700075 20010717 00075 WP 2001 7 17 ABXA010391 1 20010702 A 5320 3754473501N SPLICE DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 LONGERON 31 LEFT SPLICE FITTING CRACKED AT STA 1270. REMOVED AND REPLACED SPLICE FITTING IAW DC-8 SRM. 2 L 7 4 4F 4A25 2001071700076 20010717 00076 EU 2001 7 17 RAIA00107013 1 20010703 A 7600 E0242A28AO RELAY AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE RELAY RACK FAILED A RAIA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 CE 03 424TE 124 120561 7003-STL-LEFT ENGINE ATPCS UPTRIM TEST DOES NOT DROP NP WHEN PLACED IN ARM POSITION. MAINTENANCE DEFERRED ATPCS SYSTEM P ER MEL. MAINTENANCE INSPECTED AND REPLACED RELAY 34KF, SYSTEM TESTS NORMALLY. 2 H 7 2 4T 4 T RT A53EU E20NE 2001071700077 20010717 00077 EU 2001 7 17 SIMA20011301 1 20010510 A 3350 3071BPLGL BULB SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 332AE 340B332 LAX - FLT 3130 - ONE LIGHT ON EMS TRACK FLOOR LIGHTS INOPERATIVE NEAR ROWS 8/9. REMOVED AND REPLACED EMS LIGHT BULB AT ROW 8 IAW SAAB AMM 33-50-20. CREW REPORTED ONE FLOOR PROXIMITY EMERGENCY LIGHT INOPERATIVE AT ROW 8. LIGHT BULB WAS RE PLACED, OPS CHECK WAS GOOD AND AIRCAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001071700078 20010717 00078 EU 2001 7 17 SIMA20011304 1 20010510 A 2400 A20426 PDU SAAB SF340 340B 7860101 EU LEFT INOPERATIVE A SIMA O OTHER H ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 SW 21 272AE 340B272 DFW - FLT 3712 - CREW REPORTED LOSING THE LEFT DATA PROCESSING UNIT (DISPLAY UNIT) WHEN HYDRAULIC PUMP ON. EMERGENCY PO WER LGIHT CAME ON AND THEN WENT OUT. AFTER LANDING AIRCRAFT HAD NO HYDRAULICS DUE TO BATTERY FAILURE. LEFT DC MAIN BUS LIGHT ILLUMINATED AND LEFT BATTERY TEMPERATURE WAS 70 DEGREES. MAINTENANCE INSPECTED AND FOUND BATTERY LEAD INCORRECTL Y CONNECTED TO LEFT POWER DISTRIBUTION UNIT. THE LEFT PDU WAS REMOVED AND REPLACED IAW SAAB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001071700079 20010717 00079 EU 2001 7 17 SIMA20011331 1 20010513 A 2611 72711211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU E&E BAY MALFUNCTIONED A SIMA K NONE N FALSE WARNING CR CRUISE 1 SW 21 235AE 340B235 BUF - FLT 5135 - CREW REPORTED THE AVIONICS SMOKE LIGHT ILLUMINATED INFLIGHT. PUT ON MEL AT THIS TIME. MAINTENANCE REM OVED AND REPLACED THE SMOKE DETECTOR IAW SAAB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001071700080 20010717 00080 EU 2001 7 17 SIMA20011342 1 20010514 A 3350 1371 BULB SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 219AE 340B219 DFW - FLT 3814 - EMERGENCY FLOOR LIGHTING AT ROW 9 IS INOPERATIVE. MAINTENANCE REPLACED BULB AT ROW 9 EMERGENCY LIGHT. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001071700081 20010717 00081 EU 2001 7 17 SIMA20011351 1 20010515 A 3350 MC85 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SW 21 349AE 340B349 SAN - FLT 3212 - FLIGHT ATTENDENT REPORTED ON TAXI OUT, THE EMERGENCY LIGHT ARM LIGHT WOULD NOT COME ON. CREW RETURNED TO GATE. MAINTENANCE REPLACED BULBS IN ARM LIGHT SWITCH. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVI CE. (M) 2 L 7 2 4T RT A52EU 2001071700082 20010717 00082 EU 2001 7 17 SIMA20011352 1 20010515 A 3350 3071PBE LAMP SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 261AE 340B261 MHT - FLT 4516 - ONE FLOOR PROXIMITY EMERGENCY LIGHT AT ROW 9 WILL NOT ILLUMINATE. PUT ON MEL AT THIS TIME. MAINTENANC E REPLACED THE BULB AT ROW 9 EMERGENCY LIGHT IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVI CE. (M) 2 L 7 2 4T RT A52EU 2001071700083 20010717 00083 EU 2001 7 17 SIMA20011364 1 20010516 A 3350 CM85 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SW 21 312AE 340B312 LAX - FLT 3235 - FLIGHT ATTENDANT EMERGENCY LIGHT ARMED LIGHT WILL NOT ILLUMINATE. MAINTENANCE REPLACED THE BULB FOR TH E FLIGHT ATTENDANT EMERGENCY LIGHT ARM SWITCH. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001071700084 20010717 00084 EU 2001 7 17 SIMA20011381 1 20010518 A 3350 8G500545405 LAMP SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AE 340B282 DFW - FLT 3269 - CREW REPORTED THE EMERGENCY LIGHT AT ROW 10 IS INOPERATIVE. MAINTENANCE REPLACED THE BULB AT ROW 10. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001071700085 20010717 00085 EU 2001 7 17 SIMA20011409 1 20010520 A 7900 AC9718F25 FILTER SAAB SF340 340B 7860101 EU LEFT ENGINE CLOGGED A SIMA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 21 901AE 340B401 DFW - FLT 3387 - LEFT OIL BYPASS LIGHT ILLUMINATED ON OVERHEAD PANEL ACCOMPANIED WITH ENGINE LIGHT ON CWP. BOTH WERE IN TERMITTENT. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE OIL FILTER IAW GE CT7 EMM 79-00-00. LEAK CHECK WAS GOOD AND A IRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001071700086 20010717 00086 2001 7 17 SIMA20011412 4 20010521 A 3400 6223975001 ALTIMETER SAAB SF340 340B 7860101 EU COCKPIT INOPERATIVE A SIMA O OTHER O OTHER CR CRUISE 1 SW 21 396AE 340B396 DFW - FLT 3543 - CREW REPORTED THAT THE CAPTAINS ALTIMETER RED FLAGGED. CREW ELECTED TO RETURN TO DFW. NO OTHER PROBLE MS NOTED. MAINTENANCE REMOVED AND REPLACED CAPTAINS ALTIMETER IAW SAAB MM. OPS CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001071700087 20010717 00087 EU 2001 7 17 SIMA20011414 1 20010521 A 3350 6510368 BULB SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 286AE 340B286 BOS - FLT 4932 - FOUND EMERGENCY OVERHEAD LIGHT AT ROW 10C IS INOPERATIVE. MAINTENANCE REPLACED LIGHT BULB FOR EMERGENC Y OVERHEAD LIGHT IAW SAAB AMM CH 33-50-00. OPS CHECK GOOD AT THIS TIME AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001071700088 20010717 00088 2001 7 17 SIMA200115102 4 20010531 A 3400 6227337001 TRANSMITTER SAAB SF340 340B 7860101 EU A SIMA D RETURN TO BLOCK O OTHER CR CRUISE 1 SW 21 222AE 340B222 FLT 3258 - TXK - CREW REPORTED RADAR DID NOT DIFFERENCIATE WEATHER, IT JUST SHOWED A BAND OF GREEN/RED CLOSE TO AIRCRAFT . MAINTENANCE REMOVED AND REPLACED THE RADAR RECEIVER TRANSMITTER IAW SAAB 34-42-05. OPS CHECK WAS GOOD AND AIRCRAFT W AS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001071700089 20010717 00089 EU 2001 7 17 SIMA200115414 1 20010603 A 3320 2064332 SOCKET SAAB SF340 340B 7860101 EU LAVATORY DEFECTIVE A SIMA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 21 396AE 340B396 LFT - FLT 3279 - LAVATORY SMOKE LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE FOUND BURNED LIGHT SOCKET. LAVATORY WAS PUT O N MEL AT THIS TIME. REMOVED AND REPLACED LAVATORY LIGHT SOCKET IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001071700090 20010717 00090 2001 7 17 SIMA200116002 4 20010609 A 3100 005WS00 WEU SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 235AE 340B235 BOS - FLT 4934 - ON TAKEOFF, NUMEROUS WARNING SOUNDED. ABORTED AT 120KTS. REMOVED AND REPLACED WARNING ELECTRONIC UNIT IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001071700091 20010717 00091 EU 2001 7 17 SIMA200116103 1 20010610 A 6100 523535 INDICATOR SAAB SF340 340B 7860101 EU FLT DECK FAILED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 349SB 340B349 LAX - FLT 3080 - ON TAKEOFF ROLL, RIGHT PROP OIL TEMP AND PRESSURE GAUGE WENT TO ZERO. ABORTED TAKEOFF. NO OTHER PROBL EM NOTED. REMOVED AND REPLACED PROP OIL TEMP INDICATOR IAW AMM. PERFORMED GROUND RUNS. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001071700092 20010717 00092 NM 2001 7 17 ABXA010392 1 20010627 A 5311 148T2140 FRAME BOEING 767 767231 1385131 NM FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 709AX 22572 DURING ACCOMPLISHMENT OF AD, INSPECTION REPORTED CRACK INDICATIONS AT 2 FASTENER LOCATIONS ON THE HORIZONTAL STABILIZER PIVOT BOX, LEFT AND RIGHT CHORDS. THE FASTENERS WERE REMOVED AND THE HOLES WERE REWORKED, OVER SIZING THE HOLES BY .016 INCH. THE REWORKED HOLES WERE REINSPECTED AND THE CRACKS WERE VERIFIED AS REMOVED. WHILE ACCOMPLISHING THE REPAIR, MA INTENANCE DISCOVERED 1 ELONGATED FASTENER HOLE IN THE LEFT OUTER CHORD. A HFEC INSPECTION WAS ACCOMPLISHED ON THE HOLE AND NO CRACKS WERE REPORTED IAW REA B653-41539MR. 2 L 7 2 4F RT A1NM 2001071700093 20010717 00093 NM 2001 7 17 ABXA010393 1 20010627 A 5311 148T2240 FRAME BOEING 767 767231 1385131 NM FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 709AX 22572 DURING ACCOMPLISHMENT OF AD 2001-09-13, INSPECTION REPORTED CRACK INDICATIONS AT 2 FASTENER LOCATIONS, ON THE HORIZONTAL STABILIZER PIVOT BOX, LEFT AND RIGHT CHORDS. THE FASTENERS WERE REMOVED AND THE HOLES WERE REWORKED OVER SIZING THE 2 HOLES BY .016 INCH. THE REWORKED HOLES WERE REINSPECTED AND THE CRACKS WERE VERIFIED AS REMOVED IAW REA B653-41517MR. 2 L 7 2 4F RT A1NM 2001071700094 20010717 00094 WP 2001 7 17 ABXA010394 1 20010702 A 5320 4753360501 FITTING DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 FRAME TO LONGERON FITTING WAS CRACKED AFT SIDE, STA 820, ABOVE LONGERON 22 RIGHT. REPLACED FITTING IAW DC-8 DWG 4753360 , SRM 53-1-0 AND 51-1-20D. 2 L 7 4 4F 4A25 2001071700095 20010717 00095 WP 2001 7 17 ABXA010395 1 20010620 A 5711 5597829502 SPAR CAP DOUG DC8 DC863F 302198F WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 RIGHT WING AFT UPPER SPAR CAP WAS CRACKED BETWEEN XCW 69.5 AND XCW 46. REPLACED RIGHT WING UPPER SPAR CAP BETWEEN XCW 0 TO XRS 74.8 IAW REA D857-41242MR. 2 L 7 4 4F 4A25 2001071700096 20010717 00096 WP 2001 7 17 ABXA010397 1 20010708 A 5347 SEAT TRACK DOUG DC8 DC863F 302198F WP COCKPIT DIRTY A ABXA K NONE O OTHER NR NOT REPORTED 1 GL 23 811AX 46113 AFTER MOVING THE CAPTAIN'S SEAT FORWARD OR AFT, THE HANDLE DID NOT LOCK DOWN ALLOWING THE SEAT TO MOVE. CLEANED AND LUB RICATED THE SEAT TRACK. CHECKED GOOD IAW DC-8 MM 25-11-01. 2 L 7 4 4F 4A25 2001071700097 20010717 00097 WP 2001 7 17 ABXA010398 1 20010702 A 3242 BRAKE DOUG DC8 DC863F 302198F WP MLG MALFUNCTIONED A ABXA K NONE O OTHER LD LANDING 1 GL 23 811AX 46113 ON LANDING, 5 MAIN LANDING GEAR TIRES BLEW. MECHANICS FOUND THAT THE EMERGENCY AIR BRAKE BOTTLE WENT OFF. REPLACED AFT AIR BRAKE MECHANICAL CONTROL CABLE. REF CABLE RUN 81B, 82B, IAW DC-8 MM 32-45-00. SERVICED AIR BRAKE BOTTLE. OPS CHE CK OF AIR BRAKE SYSTEM GOOD IAW DC-8 MM 32-44-00. WHEEL ASSEMBLIES REPLACED: 1, 2, 3, 4, 5, 6, 7, 8. REPLACED DAMAGED BRAKE ASSEMBLIES 3 AND 4. COMPLIED WITH REA D832-41587. REPLACED DAMAGED WHEEL SPEED TRANSDUCERS 4 AND 7. BOTH OPS CH ECKED GOOD IAW DC-8 MM 32-43-02. 2 L 7 4 4F 4A25 2001071700098 20010717 00098 2001 7 17 ABXA010400 4 20010712 A 2565 101623201 SLIDE BOEING 767 767281 1385109 NM CABIN DEPLOYED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 789AX 23022 THE EMERGENCY SLIDE WAS DEPLOYED ACCIDENTLY WHEN THE DOOR WAS OPENED BY THE SUPERNUMERARY AFTER SHUTDOWN. REPLACED THE ENTRY DOOR ESCAPE SLIDE PACK IAW B767 AMM 25-66-01-4. PRESSURE INDICATOR WAS IN THE GREEN BAND AND THE PIN WAS REMOVED. 2 L 7 2 4F RT A1NM 2001071700099 20010717 00099 NM 2001 7 17 AWXA0001852 1 20010612 A 2120 WARNING LIGHT AIRBUS A319 A319132 NM COCKPIT ILLUMINATED A AWXA A D UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 WP 28 806AW 1056 PHX - AIR TURNBACK - 6/8/01 - FLT 83 - AFTER TAKEOFF THE EQUIPMENT COOLING EXTRACT VALVE LIGHT REMAINED AMBER AND THE AI RCRAFT RETURNED TO PHX. MX PERFORMED A BITE CHECK OF THE AVEC SYSTEM WHICH TESTED OK. CHECKED THE LAST LEG REPORT AND NO FAULTS NOTED. CHECKED CLASS 3 FAULTS AND NO FAULTS NOTED. PERFORMED A VISUAL INSPECTION OF THE EXTRACT DOOR AND NO DISCREPANCIES WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE AND NO FURTHER DISCREPANCIES HAVE BEEN REPORTED. 2 L 7 2 4F RT A28NM 2001071700100 20010717 00100 EU 2001 7 17 C2XA01CL139 1 20010612 A 3234 F96GA0102 CONTROL HANDLE AEROSP ATR42 ATR42320 8680930 EU COCKPIT SHORTED A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 27 17831 185 DAY FLT 3233 THE CREW REPORTED NO LANDING GEAR DOWN INDICATION ON MAIN PANEL AND LANDING GEAR CONTROL CIRCUIT BREAKER POPPED IN FLIGHT. CLE MAINTENANCE REPLACED LANDING GEAR CONTROL LEVER. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001071700101 20010717 00101 EU 2001 7 17 C2XA01CL141 1 20010614 A 2150 A/C PACK AEROSP ATR42 ATR42320 8680930 EU A/C BAY DEFECTIVE A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 21837 202 CLE FLIGHT 3705 THE CREW REPORTED A SMELL OF SMOKE IN THE CABIN DURING CLIMB. THE AIRCRAFT RETURNED TO CLEVELAND WITHOU T FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND NR 2 PACK SYSTEM CAUSING THE SMELL IN THE CABIN. THE SYSTEM WAS PL ACED ON MEL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001071700102 20010717 00102 EU 2001 7 17 C2XA01CL142 1 20010612 A 3260 WARNING LIGHT AEROSP ATR42 ATR42320 8680930 EU COCKPIT FALSE INDICATION A C2XA K NONE N FALSE WARNING AP APPROACH 1 SW 27 14828 179 CLE FLIGHT 3784 THE CREW REPORTED A UNSAFE GEAR INDICATION ON SYSTEM NR 1 NOSE GEAR. THE NR 2 SYSTEM CHECKED OK. THE A IRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND RELEASED AIRCRAFT IAW MEL 32-61-01. *S/D* MAINTENA NCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE LANDING GEAR. NO DEFECTS WERE FOUND. THE MEL WAS CLEARED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A53EU 2001071700103 20010717 00103 NE 2001 7 17 C2XA01CL144 2 20010517 A 7323 8210161C GOVERNOR AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE RT ENGINE LEAKING A C2XA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 27 99838 20173 114 259 CLE FLIGHT 3054 THE CREW REPORTED THE NR 2 ACW GENERATOR FAULTED ON THE GROUND RESULTING IN LOSS OF GREEN HYDRAULIC SYS TEM. NO BRAKES. MAINTENANCE REPLACED THE NR 2 ENGINE OVERSPEED GOVERNOR. THE OPERATIONAL CHECKS WERE GOOD. 2 H 7 2 4T 4 T RT A53EU E20NE 2001071700105 20010717 00105 NM 2001 7 17 PCAA0106046 1 20010609 A 5210 STOP FITTING DHAV DHC8 DHC8102 2809003 NM MAIN DOOR OUT OF ADJ A PCAA K NONE O OTHER TX TAXI/GRND HDL 1 EA 13 849EX 337 BWI-FLIGHT 3806. CREW REPORTED MAIN AIRSTAIR DOOR HANDLE EXTREMELY DIFFICULT TO MOVE UP FROM CLOSED POSITION. MAINTENA NCE ADJUSTED AIRSTAIR DOOR STOPS IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL 52-10-00, AND LUBRICATED THE D OOR STOPS. DOOR OPENS WITHIN MANUAL LIMITS. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001071700106 20010717 00106 NM 2001 7 17 PCAA0106047 1 20010610 A 3244 H31X97513 TIRE DHAV DHC8 DHC8102 2809003 NM LT MLG BLOWN A PCAA K NONE O OTHER LD LANDING 1 EA 13 822EX 15134 407 187 ITH- FLIGHT 3540. CREW REPORTED LEFT INBOARD TIRE BLEW ON LANDING. MAINTENANCE PERFORMED TIRE BURST INSPECTION, NO DEF ECTS FOUND. REMOVED AND REPLACED LEFT INBOARD MAIN WHEEL ASSEMBLY AND LEFT INBOARD BRAKE ASSEMBLY. AIRCRAFT RETURNED T O SERVICE. 2 H 7 2 4T RT A13NM 2001071700107 20010717 00107 NM 2001 7 17 PCAA0106048 1 20010611 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A PCAA K NONE O OTHER NR NOT REPORTED 1 EA 13 815EX 21693 321 SYR-FLIGHT 3997. CREW REPORTED FRONT TWO RED EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE TROUBLESHOT AND FOUND POWER SUP PLY BAD. POWER SUPPLY AND BATTERY REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001081500097 20010815 00097 NM 2001 8 15 01FDEA00545 1 20010714 A 5320 FLOOR SUPPORT BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277FE 22042 DURING ROUTINE INSP RIGHT MOST LONGITUDINAL FLOOR SUPPORT IN FWD BAG BIN FOUND CRACKED. *S/D* REMOVED AND REPLACED PER SRM 51-40-3 & 51-30-2. 2 L 7 3 4F RT A3WE 2001081500099 20010815 00099 NM 2001 8 15 01FDEA00546 1 20010714 A 5752 TAB BOEING 727 727233 138408A NM RT WING DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277FE 22042 DURING ROUTINE INSP RT OUTBOARD AILERON FOUND DELAMINATED AT THE INBOARD END. *S/D* REMOVED AND REPLACED AILERON PER M M 27-10-041-4. 2 L 7 3 4F RT A3WE 2001081500102 20010815 00102 NM 2001 8 15 01FDEA00547 1 20010714 A 5320 INTERCOSTAL BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277FE 22042 DURING ROUTINE INSP INTERCOSTAL BETWEEN NR 6 & 7 MAIN CABIN SEAT TRACK FOUND CRACKED AT RBL 60, BS 760. *S/D* REMOVED AND REPLACED INTERCOSTAL PER IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2001081500112 20010815 00112 NM 2001 8 15 01FDEA00550 1 20010714 A 5320 TIE CLIP BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277FE 22042 DURING ROUTINE INSP TIE CLIP AT STR 3R, BS 560 FOUND CRACKED. *S/D* REMOVED AND REPLACED TIE CLIP PER SRM 51-20-1, 51- 30-2. 2 L 7 3 4F RT A3WE 2001081500113 20010815 00113 NM 2001 8 15 01FDEA00551 1 20010714 A 5320 TIE CLIP BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277FE 22042 DURING ROUTINE INSP TIE CLIP AT STR 3L, BS 560 FOUND CRACKED. *S/D* REMOVED AND REPLACED CLIP PER SRM 51-20-1, 51-30-2 . 2 L 7 3 4F RT A3WE 2001071700108 20010717 00108 NM 2001 7 17 01FDEA00552 1 20010714 A 5320 TIE CLIP BOEING 727 727233 138408A NM FUSELAGE TOP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277FE 22042 N 508 DUR ROUTINE INSP TIE CLIP AT STR 4R, BS 540 FND CRACKED. ** S/D ** COMING 2 L 7 3 4F RT A3WE 2001071700109 20010717 00109 NM 2001 7 17 01FDEA00553 1 20010714 A 5320 TIE CLIP BOEING 727 727233 138408A NM FUSELAGE TOP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277FE 22042 N 507 DUR ROUTINE INSP TIE CLIP AT STR 1, BS 540 FND CRACKED. ** S/D ** COMING 2 L 7 3 4F RT A3WE 2001081600074 20010816 00074 NM 2001 8 16 01FDEA00554 1 20010714 A 5320 TIE CLIP BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277FE 22042 DURING ROUTINE INSP TIE CLIP AT STR 3R, BS 500 FOUND CRACKED. *S/D* REMOVED AND REPLACED TIE CLIP PER SRM 51-20-1, 51- 30-2. 2 L 7 3 4F RT A3WE 2001081600075 20010816 00075 NM 2001 8 16 01FDEA00555 1 20010714 A 5313 STRINGER BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277FE 22042 DURING ROUTINE INSP STR 17L FOUND CRACKED AT BS 456. *S/D* REMOVED AND REPLACED STRINGER PER SRM 53-10-3, 51-30-2. 2 L 7 3 4F RT A3WE 2001081600076 20010816 00076 NM 2001 8 16 01FDEA00556 1 20010714 A 5320 TIE CLIP BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277FE 22042 DURING ROUTINE INSP SHEAR TIE CLIP AT STR 23L, BS 600 FOUND CRACKED. *S/D* REMOVED AND REPLACED CLIP PER SRM 51-20-1, 51-30-2. 2 L 7 3 4F RT A3WE 2001081600078 20010816 00078 NM 2001 8 16 01FDEA00559 1 20010714 A 5320 INTERCOSTAL BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277FE 22042 DURING ROUTINE INSP INTERCOSTAL JUST AFT OF FWD ENTRY DOOR BETWEEN BS 344 & BS 360 FOUND CRACKED. *S/D* REMOVED AND RE PLACED PER SRM 51-20-1, 51-30-2. 2 L 7 3 4F RT A3WE 2001081600171 20010816 00171 NM 2001 8 16 01FDEA00560 1 20010714 A 5210 DOOR BOEING 727 727233 138408A NM ENTRY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277FE 22042 DURING ROUTINE INSP FWD ENTRY DOOR AFT TOP CORNER FOUND CRACKED. *S/D* REMOVED AND REPLACED DOOR PER SRM 51-20-1, 51-3 0-2. 2 L 7 3 4F RT A3WE 2001081600172 20010816 00172 NM 2001 8 16 01FDEA00561 1 20010714 A 5752 TAB BOEING 727 727233 138408A NM AILERON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277FE 22042 LEFT OUTBOARD AILERON LEADING EDGE SKIN CRACKED. *S/D* REMOVED AND REPLACED AILERON TAB PER MM 27-10-041-4. 2 L 7 3 4F RT A3WE 2001091700158 20010917 00158 NM 2001 9 17 PCAA0106049 1 20010607 A 5315 85310380 FLOORBEAM DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 822EX 187 BGM- DURING SCHEDULED A INSPECTION NOSE GEAR WHEEL WELL FLOORBEAM AT STATION X97 FOUND CRACKED. REPAIR STRAP INSTALLED PER DEHAVILLAND REPAIR DRAWING RD 8-53-5817 AS AN INTERIM REPAIR. RD 8-53-1336 IS REQUIRED TO BE INSTALLED WITHIN NEXT 2 50 HOURS. PERMANENT REPAIR TO FLOORBEAM INSTALLED IN ACCORDANCE WITH DEHAVILLAND REPAIR DRAWING RD8-53-1336. AIRCRAFT R ETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001071700110 20010717 00110 WP 2001 7 17 CALA0100558 1 20010619 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND RT FUSELAGE EXTERNAL SKIN CREASED AT FS 351, JUST BELOW LONGERON 23R. RIVETS WERE REMOVED AND THE SKIN WAS COLD FORMED IAW SRM 51-30-2 AND 53-04, FIGURE 38. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38 AND 51-10-3. 2 L 7 2 4F A6WE 2001071700111 20010717 00111 WP 2001 7 17 CALA0100560 1 20010619 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND MAIN CABIN CUSP WEB CORRODED UNDER PAN AT FS 140 - 160, RBL 45 - 55. THE DRAIN PAN WAS REMOVED AND THE CORRODED AREA WAS CUT OUT IAW SRM 51-30-1 AND 53-01, FIGURE 2. A DOUBLER WAS INSTALLED IAW SRM 53-14-01, 51-10-3, AND 51-30-2. THE DRAIN PAN WAS REINSTALLED IAW SRM 51-30-1. 2 L 7 2 4F A6WE 2001071700112 20010717 00112 WP 2001 7 17 CALA0100561 1 20010619 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND MAIN CABIN FLOOR SUPPORT CORRODED AT FS 1155, LBL 22-45. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPO RT WAS INSTALLED IAW SRM 51-30-2, 53-11-0, AND 51-10-3. 2 L 7 2 4F A6WE 2001071700113 20010717 00113 WP 2001 7 17 CALA0100562 1 20010619 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND FUSELAGE SKIN CREASED AT FS 503, LONGERON 22R. RIVETS WERE REMOVED AND THE SKIN WAS COLD FORMED IAW SR M 51-30-2 AND 53-04. A DOUBLER WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 53-04, FIGURE 38, SHEET 22. 2 L 7 2 4F A6WE 2001071700114 20010717 00114 WP 2001 7 17 CALA0100563 1 20010619 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND A 2 INCH CRACK IN MAIN CABIN CUSP WEB AT FS 1303, LBL 56. THE CRACK WAS STOP DRILLED IAW SRM 53-01, FI GURE 2. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 96, 51-10-4, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 2001071700115 20010717 00115 WP 2001 7 17 CALA0100566 1 20010621 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND FIVE INTERCOSTALS CORRODED INSIDE TORQUE BOX AT AFT CARGO PIT AREA, FS 1165 - 1203. THE INTERCOSTALS W ERE REMOVED AND NEW INTERCOSTALS WERE INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-1, AND 51-30-5. 2 L 7 2 4F A6WE 2001071700116 20010717 00116 WP 2001 7 17 CALA0100568 1 20010621 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND CABIN FLOOR PANELS DELAMINATED AT FS 828 - 864 (LEFT I/B), FS 864 - 886 (RIGHT I/B), AND FS 864 - 927 ( RIGHT I/B). THE PANELS WERE REPLACED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001071700117 20010717 00117 WP 2001 7 17 CALA0100569 1 20010621 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND CABIN FLOOR PANELS DELAMINATED AT FS 1003 - 1079, LEFT O/B, AND FS 1250 - 1309, RIGHT I/B. THE FLOOR P ANELS WERE REPLACED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001071700118 20010717 00118 WP 2001 7 17 CALA0100570 1 20010621 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND CABIN FLOOR PANELS DELAMINATED AT FS 160 - 196 (PANELS F&G) AND AT FS 196 - 256 (PANELS M,N, AND O). T HE FLOOR PANELS WERE REPLACED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001071700119 20010717 00119 WP 2001 7 17 CALA0100572 1 20010621 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND CABIN ENTRY FLOOR PANELS H&K DELAMINATED. THE FLOOR PANELS WERE REPLACED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001071700120 20010717 00120 WP 2001 7 17 CALA0100573 1 20010621 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND CABIN FLOOR PANELS DELAMINATED AT FS 927 - 1003, RIGHT I/B, FS 946 - 1003, CENTER, AND FS 1003 - 1079, RIGHT I/B. THE FLOOR PANELS WERE REPLACED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001071700121 20010717 00121 WP 2001 7 17 CALA0100574 1 20010621 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND CABIN FLOOR PANELS DELAMINATED AT FS 828 - 864, RIGHT I/B, AND FS 875 - 886, LEFT I/B. THE FLOOR PANEL S WERE REPLACED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001071700122 20010717 00122 WP 2001 7 17 CALA0100575 1 20010622 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND CABIN FLOOR PANELS DELAMINATED AT FS 1174 - 1193, RIGHT I/B, FS 1174 - 1287, LEFT O/B, FS 1212 - 1287, CENTER, AND FS 1287 - 1338, CENTER. THE FLOOR PANELS WERE REPLACED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001071700123 20010717 00123 WP 2001 7 17 CALA0100576 1 20010622 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND CABIN FLOOR PANELS DELAMINATED FS 1113 - 1155, LEFT I/B, FS 1117 - 1174, RIGHT I/B, FS 1155 - 1212, CEN TER, AND FS 1193 - 1250, RIGHT I/B. THE FLOOR PANELS WERE REPLACED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001071700124 20010717 00124 WP 2001 7 17 CALA0100577 1 20010622 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND CABIN FLOOR PANELS DELAMINATED AT FS 693 - 769, RIGHT I/B, LEFT I/B, AND CENTER AND FS 769 - 826, CENTE R. THE FLOOR PANELS WERE REPLACED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001071700125 20010717 00125 WP 2001 7 17 CALA0100578 1 20010622 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND CABIN FLOOR PANELS I & J AT LT FORWARD ENTRY DELAMINATED. THE FLOOR PANELS WERE REPLACED IAW ECRA 5320 -01265. 2 L 7 2 4F A6WE 2001071700126 20010717 00126 WP 2001 7 17 CALA0100580 1 20010622 A 3350 252005 FUSE DOUG DC9 DC982 3022082 WP BATTERY PACK BLOWN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14889 49118 INSPECTION FOUND L-2 DOOR AND AFT STAIRWAY DOOR EXIT IDENTIFIER LIGHTS INOPERATIVE. THE FUSE FOR BATTERY PACK IN AFT CA BIN DROP CEILING WAS REPLACED AND OPERATION CHECKED GOOD IAW MM 33-53-00. 2 L 7 2 4F A6WE 2001071700127 20010717 00127 WP 2001 7 17 CALA0100581 1 20010622 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 33817 49371 THE FORWARD SERVICE AND FORWARD GALLEY AND COCKPIT OVERHEAD EMERGENCY LIGHTS WOULD NOT ILLUMINATE DURING TEST. THE BATT ERIES IN FORWARD DROP PANEL BATTERY PACK (STA 213) WERE REPLACED AND OPERATION CHECKED GOOD IAW MM 33-53-00. 2 L 7 2 4F A6WE 2001071700128 20010717 00128 WP 2001 7 17 CALA0100591 1 20010624 A 3350 BATTERY PACK DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14871 48022 THE LT AND RT FORWARD OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE DURING TEST. THE B5-103 BATTERY PACK WAS RE MOVED AND REPLACED IAW MM 33-53-00. 2 L 7 2 4F A6WE 2001071700129 20010717 00129 WP 2001 7 17 CALA0100592 1 20010624 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND MAIN CABIN CUSP WEB CORRODED AT FS 1174 - 1193, LBL 54. THE CORRODED AREA WAS REMOVED AND A NEW WEB WA S INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 2001071700130 20010717 00130 WP 2001 7 17 CALA0100594 1 20010624 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND LT FLOOR CUSP WEB CORRODED ON LOWER SURFACE AT FS 1117. THE CORRODED AREA WAS REMOVED AND A NEW CUSP W EB WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-1. 2 L 7 2 4F A6WE 2001071700131 20010717 00131 WP 2001 7 17 CALA0100606 1 20010626 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND CUSP WEB CRACKED IN TWO PLACES AT FS 218 - 238, RBL 54. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLE D IAW SRM 51-30-2 AND 51-30-4. 2 L 7 2 4F A6WE 2001071700132 20010717 00132 WP 2001 7 17 CALA0100607 1 20010626 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND FORWARD ENTRY SUBFLOOR CORRODED AT FS 160 - 200, RBL 56. THE FLOOR SUPPORTS AND WEB SUPPORTS WERE REMO VED TO GAIN ACCESS TO SUBFLOOR. THE SUBFLOOR WAS REMOVED AND A NEW SUBFLOOR WAS INSTALLED WITH WEB AND FLOOR SUPPORTS I AW SRM 53-14-1, 51-30-02, 51-30-05, AND 51-30-08. 2 L 7 2 4F A6WE 2001071700133 20010717 00133 WP 2001 7 17 CALA0100608 1 20010626 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND FLOOR SUPPORT IN CENTER CARGO PIT CORRODED ON UPPER SURFACE AT FS 636 FROM LONGERON 29R-28L. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 2001071700134 20010717 00134 WP 2001 7 17 CALA0100609 1 20010626 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND LT FLOOR CUSP WEB BEHIND LAV AREA CORRODED AT FS 218 - 228, LBL 45 - 56. THE CUSP WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2, 51-30-5, 51-30-8, 51-10-3, AND 51-10-4. 2 L 7 2 4F A6WE 2001071700135 20010717 00135 WP 2001 7 17 CALA0100610 1 20010626 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND FORWARD PIT RT SIDE CARGO TIE DOWN TRACK CORRODED AT LOWER SIDE OF FASTENER HOLES FROM FS 218 TO FORWAR D DOOR FRAME. THE TIE DOWN TRACK AND ATTACHING ANGLE WERE REMOVED AND A NEW TRACK AND ATTACH ANGLE WERE INSTALLED IAW S RM 51-30-2 AND 51-30-1. 2 L 7 2 4F A6WE 2001071700136 20010717 00136 WP 2001 7 17 CALA0100611 1 20010626 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 157 - 198, RBL 45. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 2001071700137 20010717 00137 WP 2001 7 17 CALA0100612 1 20010626 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 157 - 200, RBL 6. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT W AS INSTALLED IAW SRM 51-30-4, 51-10-1, AND 51-10-3. 2 L 7 2 4F A6WE 2001071700138 20010717 00138 WP 2001 7 17 CALA0100613 1 20010626 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 160 - 195, LBL 56. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-4 AND 51-30-2. 2 L 7 2 4F A6WE 2001071700139 20010717 00139 WP 2001 7 17 CALA0100614 1 20010626 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND A 6 INCH CRACK IN COCKPIT CENTER FLOORBOARD CENTER FLOOR SUPPORT AT FS 140, BL 0. THE FLOOR SUPPORT WA S REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 2001071700140 20010717 00140 WP 2001 7 17 CALA0100615 1 20010626 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 160 - 196, LBL 44. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 2001071700141 20010717 00141 WP 2001 7 17 CALA0100616 1 20010628 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69826 49486 INSPECTION FOUND FUSELAGE SKIN CREASED JUST BELOW CUSP LINE AT STA 408-446. A REPAIR WAS INSTALLED IAW ECRA 5310-04154 AND SRM 53-04, FIGURE 12B. 2 L 7 2 4F A6WE 2001071700142 20010717 00142 WP 2001 7 17 CALA0100617 1 20010629 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND MAIN CABIN CUSP WEB CORRODED AT FS 202-218, RBL 54. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IA W SRM 51-30-02, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 2001071700143 20010717 00143 WP 2001 7 17 CALA0100619 1 20010629 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND CUSP WEB CORRODED AT LOWER CORNER FORWARD END OF R-1 DOOR JAMB, FS 160 - 238. THE LOWER DOOR PAN, TWO TORQUE BOX WEB PANELS, STRAPS, AND COMPOSITE CHANNEL WERE REMOVED TO GAIN ACCESS. THE CUSP WEB WAS REPLACED IAW SRM 53- 05, FIGURE 55. REINSTALLED ALL REMOVED PANELS AND PARTS IAW SRM 51-30-2. 2 L 7 2 4F A6WE 2001071700144 20010717 00144 NM 2001 7 17 CALA0100620 1 20010630 A 3350 D71701100 BATTERY PACK BOEING 737 737824 13844BZ NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16217 28777 INSPECTION FOUND EMERGENCY LIGHT BATTERY PACK AT M1695 (STA 565) INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-06 AND OPERATION CHECKED GOOD. 2 L 7 2 4F RT A16WE 2001071700145 20010717 00145 NM 2001 7 17 CALA0100624 1 20010630 A 3350 D71701100 BATTERY PACK BOEING 737 737724 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 13718 28937 THE EMERGENCY LIGHT BATTERY PACK FORWARD OF RT OVERWING EXIT FAILED CAPACITY TEST. THE BATTERY PACK WAS REMOVED AND REP LACED IAW MM 33-51-06 AND OPERATION CHECKED GOOD. 2 L 7 2 4F RT A16WE 2001071700146 20010717 00146 WP 2001 7 17 CALA0100625 1 20010701 A 3350 41B004AD0763 BATTERY PACK DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 13881 48045 INSPECTION FOUND FIRST CLASS OVERHEAD EMERGENCY LIGHTS INOPERATIVE. THE BATTERIES IN OVERHEAD BATTERY PACK WERE REPLACE D IAW MM 33-50-00 AND OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 2001071700147 20010717 00147 WP 2001 7 17 CALA0100630 1 20010702 A 3350 AD4002P BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17812 49250 THE EMERGENCY CEILING LIGHTS WERE FOUND INOPERATIVE AT ROW 15. THE BATTERIES WERE REMOVED AND REPLACED AND OPERATION CH ECKED GOOD. 2 L 7 2 4F A6WE 2001071700148 20010717 00148 WP 2001 7 17 CALA0100631 1 20010703 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND A 5 INCH CRACK IN DOOR JAMB SKIN TANG AT AFT END OF L-1 DOOR, FS 207, LONGERON 11L. A 1 INCH CRACK WAS FOUND IN THE DOOR JAMB SKIN TANG AT FS 207, LONGERON 15L. THE CRACKED AREA WERE TRIMMED OUT IAW ECRA 5310-04155. FILL ER AND DOUBLER WERE INSTALLED AT EACH LOCATION IAW SRM 51-10-4, 51-10-3, AND ECRA 5310-04155. 2 L 7 2 4F A6WE 2001071700149 20010717 00149 WP 2001 7 17 CALA0100632 1 20010703 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND MID CARGO RT BULKHEAD FLOOR SUPPORT CORRODED AT FS 541. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 2001071700150 20010717 00150 WP 2001 7 17 CALA0100635 1 20010706 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND LT CUSP ANGLE CORRODED ON UPPER SURFACE AT AFT END OF L-1 DOOR ENTRANCE, STA 186. THE AREA WAS REPAIRE D IAW EA 9-5310-2-A0895 AND ECRA 5310-04156. 2 L 7 2 4F A6WE 2001071700151 20010717 00151 NM 2001 7 17 CALA0100639 1 20010708 A 5414 ACCESS PANEL BOEING 737 7373T0 1384582 NM NR 1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14358 23943 INSPECTION FOUND A .5 INCH CRACK IN NR 1 ENGINE PYLON ACCESS PANEL 5727. A DOUBLER WAS INSTALLED IAW ECRA 5430-01230. 2 L 7 2 4F RT A16WE 2001071700152 20010717 00152 WP 2001 7 17 CALA0100641 1 20010708 A 3350 240001374 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 83870 48056 THE OVERHEAD EMERGENCY CEILING LIGHTS WERE FOUND INOPERATIVE AT ROWS 9-14. THE BATTERIES IN ROW 10 OVERHEAD BIN BATTERY PACK WERE REPLACED AND OPERATION CHECKED GOOD IAW MM 33-50-00. 2 L 7 2 4F A6WE 2001071700153 20010717 00153 WP 2001 7 17 CALA0100642 1 20010709 A 3350 AD4002P BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 819NY 49479 INSPECTION FOUND EMERGENCY OVERHEAD LIGHTS INOPERATIVE FROM ROWS 1-7. THE BATTERIES FOR THE OVERHEAD EMERGENCY LIGHTS W ERE REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW MM 33-50-00. 2 L 7 2 4F A6WE 2001071700154 20010717 00154 NM 2001 7 17 CALA0100643 1 20010705 A 2612 FIRE LOOP BOEING 757 757224 1384958 NM NR 1 ENGINE FAULTY A CALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 17133 29282 THE LEFT ENGINE FIRE WARNING LIGHT ON SYSTEM NR 1 LOOP ILLUMINATED WHILE CLIMBING THRU 16K FT AFTER TAKEOFF SYSTEM 2 LOO P WAS ON PLACARD. ALL CHECKLIST PROCEDURES WERE COMPLIED WITH AND THE FIRE LIGHT EXTINGUISHED WHEN THE THROTTLE WAS PUL LED BACK. ALL ENGINE INDICATIONS WERE NORMAL. THE AIRCRAFT WAS RETURNED TO SJU WHERE IT LANDED WITHOUT INCIDENT. MAIN TENANCE FOUND THE LOWER TURBINE CASE SYSTEM NR 1 LOOP AT FAULT. THE SYSTEM NR 1 LOOP WAS REMOVED AND REPLACED IAW MM 26 -11-01. THE M682 CARD IN THE P54 CARD FILE WAS REMOVED AND REPLACED. THE HP6 DUCT WAS REPLACED AS A PRECAUTIONARY DUE TO EVIDENCE OF BLOWBY. THREE WIRES FOR SYSTEM NR 2 LOOP WERE REPLACED DUE TO CHAFING. 2 L 7 2 4F RT A2NM 2001071700155 20010717 00155 NM 2001 7 17 CALA0100648 1 20010711 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59302 23353 INSPECTION FOUND A .5 INCH CRACK IN AFT BAGGAGE BIN FLOOR SUPPORT AT STA 767, RBL 14. A REPAIR WAS INSTALLED IAW SRM 53 -00-53. 2 L 7 2 4F RT A16WE 2001071700156 20010717 00156 NM 2001 7 17 CALA0100649 1 20010711 A 3350 30043213 LIGHT BOEING 737 7373T0 1384582 NM EXTERIOR INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 59302 23353 THE AFT RIGHT SERVICE DOOR EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED IAW MM 33-51-11 AND OPERATION CHECKED GOOD. 2 L 7 2 4F RT A16WE 2001071700157 20010717 00157 WP 2001 7 17 CALA0100653 1 20010712 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND R-1 DOOR JAMB DENTED AT AFT LATCHING MECHANISM. THE BAYONET ROLLER ATTACH ARM WAS REMOVED IAW SRM 51-3 0-01. A REPAIR DOUBLER AND SHIM WERE INSTALLED IAW SRM 51-30-2. A NEW DOOR STOP WAS INSTALLED IAW SRM 51-30-5. THE BA YONET ROLLER ATTACH ARM WAS REINSTALLED IAW SRM 51-30-01. 2 L 7 2 4F A6WE 2001071700158 20010717 00158 WP 2001 7 17 CALA0100655 1 20010714 A 3350 110049 CHARGER DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND EMERGENCY AISLE PATH LIGHTING IN CENTER OF AIRCRAFT INOPERATIVE. THE EMERGENCY BATTERY CHARGER NEAR TO P BEACON WAS REMOVED AND REPLACED AND OPERATION OF AISLE PATH LIGHTING CHECKED GOOD. 2 L 7 2 4F A6WE 2001071700159 20010717 00159 NM 2001 7 17 P5CA0100567 1 20010530 A 5610 6171545 WINDOW BOEING 747 747123 1384873 NM A P5CA K NONE O OTHER DE DESCENT 1 WP 23 859FT 20326 RH #1 OUTER PLY SHATTERED. R&R R1 WINDOW PER 56-11-01, INSTALLED R1 WINDOW, LEAK CHECKS GOOD REPLACED HEAT & CONTROLLER P/N ON 617154-5, S/N ON 084C-857, P/N OFF 617154-5, S/N OFF 123C-846. 2 L 7 4 4F A20WE 2001071700160 20010717 00160 NM 2001 7 17 P5CA0100581 1 20010625 A 5315 FLOORBEAM BOEING 747 747249F 1384849 NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION, FOUND MAIN DECK FLOORBEAM CORROSION ON TOP FLANGE AT STA 2260 RBL 41. REPAIR CARRIED OUT AS PER 53-11 -23 & SRM 51-40-04. 2 L 7 4 4F A20WE 2001071700161 20010717 00161 NM 2001 7 17 P5CA0100582 1 20010625 A 5314 KEELBEAM BOEING 747 747249F 1384849 NM A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION - KEEL BEAM LOWER PANEL SUPPORT BEAM CORRODED AT STA 1391 LBL 15 TO RBL 15. BLENDED OUT CORROSION AS P ER 53-10-01. CLEANED OUT DEPTH W/IN LIMIT OF 20% THICKNESS. RE-PROTECTED W/ ALODINE & PRIMER AS PER SRM 51-10-02. DIMENS IONS ARE MATERIAL THICKNESS 0.097", MAX ALLOWED DEPTH 0.019", CORROSION REMOVED 0.014". 2 L 7 4 4F A20WE 2001071700162 20010717 00162 NM 2001 7 17 P5CA0100583 1 20010625 A 5314 KEELBEAM BOEING 747 747249F 1384849 NM A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION - KEEL BEAM LOWER PANEL SUPPORT STRUCTURE CORRODED AT RBL 15 FROM STA 1273 TO 1352. INSPECT AREA AS PE R SRM 51-10-01. BLENDED OUT CORROSION AS PER 53-10-01 FOUND W/IN LIMIT OF 20% THICK. AREA RE-PROTECTED W/ ALODINE & PRIM ER AS PER SRM 51-10-02. MATERIAL THICKNESS 0.095", MAX ALLOWED DEPTH 0.019", CORROSION REMOVED 0.009". 2 L 7 4 4F A20WE 2001071700163 20010717 00163 NM 2001 7 17 P5CA0100586 1 20010715 A 7930 BYPASS VALVE BOEING 747 747123 1384873 NM A P5CA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 23 859FT 20326 FILTER BYPASS LIGHT & OIL PRESSURE LIGHT ILLUMINATED (FLICKERING). EXTINGUISHED WHEN #1 THROTTLE RETARDED TO IDLE. RETUR NED FOR LANDING. FILTER PYPASS REPLACED IN ORD INITIALLY BY MX. REPLACED PRESSURE VALVE. 2 L 7 4 4F A20WE 2001071700164 20010717 00164 NM 2001 7 17 SWAA011866 1 20010521 A 5320 6517583 BEAM BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAMS CRACKED AT LBL 17.1, RBL 17.1 & LBL 5.7. REPAIRED VERTIC AL BEAMS PER SWA RA. 2 L 7 2 4F RT A16WE 2001071700165 20010717 00165 NM 2001 7 17 SWAA011891 1 20010701 A 3350 6104791 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED SERVICE CHECK, FOUND BOTH FWD DOOR EMERGENCY EVAC SLIDE EXTERIOR LIGHTS INOP. REMOVED AND REPLACED EXI T LIGHT BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2001071700166 20010717 00166 2001 7 17 SWAA011897 4 20010702 A 2565 65C34691 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 615SW 27698 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUSTMENT. ADJUSTED EMERGENCY EV AC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001071700167 20010717 00167 NM 2001 7 17 SWAA011898 1 20010703 A 3350 100031 SIGN BOEING 737 7377H4 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 716SW 27850 OVERHEAD EMERGENCY EXIT SIGN NOT SECURE AT AFT CABIN. SECURED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2001071700168 20010717 00168 2001 7 17 SWAA011899 4 20010702 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 087SW 22903 DURING SCHEDULED C4 CHECK, FOUND BOTH AFT DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF VIEW. REPOSITIONED EVAC SLI DES PER MM. 2 L 7 2 4F A16WE 2001071700169 20010717 00169 NM 2001 7 17 SWAA011900 1 20010703 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 399WN 27693 DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2001071700170 20010717 00170 2001 7 17 SWAA011901 4 20010702 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 615SW 27698 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001071700171 20010717 00171 WP 2001 7 17 CALA0100657 1 20010716 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP AFT COCKPIT DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND CAPTAIN'S R/H SIDE AFT FLOORBOARD DELAMINATED. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLE D IAW SRM 51-30-01. 2 L 7 2 4F A6WE 2001071700172 20010717 00172 NM 2001 7 17 SWAA011903 1 20010704 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT BOTH OVERWING EXITS. RELAMPED EXIT LIGHTS PER MM. 2 L 7 2 4F RT A16WE 2001071700173 20010717 00173 NM 2001 7 17 SWAA011910 1 20010703 A 2920 3415251 CONTROL VALVE BOEING 737 7373G7 1384595 NM MLG W/W LEAKING A SWAA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 691WN 23781 DECLARED EMERGENCY, DURING CLIMB LOST A-SYSTEM HYDRAULIC FLUID, TOTAL A-HYD SYSTEM FAILURE. REMOVED AND REPLACED LANDI NG GEAR TRANSFER FLOW CONTROL VALVE AND PTU CONTROL VALVE PER MM. 2 L 7 2 4F RT A16WE 2001071700174 20010717 00174 2001 7 17 SWAA011911 4 20010705 A 2565 D31354 COVER BOEING 737 7373H4 1384600 NM SERVICE DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 607SW 27927 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND VIEW COVER LOOSE. SECURED VIEW COVER PER MM. 2 L 7 2 4F RT A16WE 2001071700175 20010717 00175 NM 2001 7 17 SWAA011912 1 20010705 A 5250 65C33828 PANEL BOEING 737 7372H4 138448C NM COCKPIT DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 090SW 22905 COCKPIT DOOR EMERGENCY EXIT PANEL LOOSE. SECURED EXIT PANEL PER MM. 2 L 7 2 4F A16WE 2001071700176 20010717 00176 NM 2001 7 17 SWAA011915 1 20010705 A 3350 BR2013 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED RON CHECK, FOUND SEVERAL EEPLS INOP AND LOOSE. REPAIRED AND SECURED EEPLS PER MM. 2 L 7 2 4F A16WE 2001071700177 20010717 00177 NM 2001 7 17 SWAA011918 1 20010703 A 3244 26078251 TIRE BOEING 737 7373H4 1384600 NM NLG BLOWN A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 326SW 23690 AIR TURNBACK. DURING TAKEOFF RT NOSE TIRE BLEW OUT DAMAGING THE FOLLOWING COMPONENTS. NLG EXTEND SENSOR CONDUIT, LWR T CAS ANTENNA, E&E ACCESS DOOR, ABRAIDABLE SHROUD NR 2 ENG, AFT ACOUSTIC PANEL NR 2 ENG AND FAN BLADES NR 2 ENG. REMOVED AND REPLACED BOTH NOSE TIRES AND WHEEL ASSY'S, SENSOR CONDUIT, TCAS ANTENNA, AND E&E DOOR. REPAIRED SHROUD. REMOVED A ND REPLACED ACOUSTIC PANEL, NR 2 ENG FAN BLADES. ALL WORK DONE PER MM. 2 L 7 2 4F RT A16WE 2001071700178 20010717 00178 NM 2001 7 17 SWAA011919 1 20010706 A 2560 P274550 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED RON CHECK, FOUND EMERGENCY FLASHLIGHT AT FWD OTBD INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2001071700179 20010717 00179 NM 2001 7 17 SWAA011920 1 20010706 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 362SW 26573 EEPLS INOP AT OVERWING EXIT. REPAIRED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001071700180 20010717 00180 2001 7 17 SWAA011921 4 20010706 A 2565 D31354 SLIDE BOEING 737 7377H4 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 401WN 29813 FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001071700181 20010717 00181 2001 7 17 SWAA011922 4 20010707 A 2565 65C34691 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUSTMENT. ADJUSTED EMERGENCY EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001071700182 20010717 00182 NM 2001 7 17 SWAA011924 1 20010705 A 3350 BR2013 LIGHT BOEING 737 7377H4 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 749SW 29801 DURING SCHEDULED RON, FOUND EEPLS INOP AT FWD CABIN. RELAMPED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001071700183 20010717 00183 NM 2001 7 17 SWAA011928 1 20010707 A 3350 BR2013 LIGHT BOEING 737 7377H4 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 739GB 29275 DURING SCHEDULED C2 CHECK, FOUND EEPLS INOP AT FWD CABIN. RELAMPED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001071700184 20010717 00184 NM 2001 7 17 SWAA011931 1 20010709 A 3350 900835A BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHT INOP AT MID CABIN CEILING. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2001071700185 20010717 00185 2001 7 17 SWAA011933 4 20010708 A 2565 61620408 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 611SW 27697 DURING SCHEDULED RON CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVA C SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001071700186 20010717 00186 NM 2001 7 17 SWAA011934 1 20010708 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 380SW 26587 DURING SCHEDULED RON CHECK, FOUND EEPLS INOP BETWEEN ROWS 18 -21. SECURED EEPLS WIRES PER MM. 2 L 7 2 4F RT A16WE 2001071700187 20010717 00187 2001 7 17 SWAA011935 4 20010701 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001071700188 20010717 00188 NM 2001 7 17 SWAA011937 1 20010707 A 3397 BR2013 WIRE BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 703SW 27837 DURING SCHEDULED SPECIAL VISIT, FOUND EEPLS INOP BETWEEN ROW'S 18-21. SECURED EEPLS WIRES PER MM. 2 L 7 2 4F RT A16WE 2001071700189 20010717 00189 NM 2001 7 17 AWXA0001971 1 20010501 A 5321 6546812185 FLOOR SUPPORT BOEING 737 7373Q8 1384670 NM L/H AFT LAV CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 D: Aft cabin floor panel support (L/H lav) has damage (drill start) from hat channel fasteners underneath.C: Located and installed new support p.o. x9525279. Installed hat channel at Sta 994-1006. 2 L 7 2 4F RT A16WE 2001071700190 20010717 00190 NM 2001 7 17 AWXA0001972 1 20010510 A 5312 WEB BOEING 737 7373Q8 1384670 NM BS 178 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 D: HFEC confirms 2ea cracks in Sta 178 bulkhead skin 1 at RBL 1 and 1 at LBL 1 WL 187. Cracks are apprx .750 in length v ertical 12 oclock to 6 oclock positionC:Cut dammaged area, HFEC no cracks noted Cal #0714. Frabricated repair doubler 20 24 T#. 040 PO # x95025244 frabricated filler from 2024T3.032 po x95024184 treated primed & top coated repair doublers & filler and installed repair doubler and filler per SRM 53-10-08 2 L 7 2 4F RT A16WE 2001071700191 20010717 00191 NM 2001 7 17 AWXA0001974 1 20010508 A 5312 6546568519 STIFFENER BOEING 737 7373Q8 1384670 NM BS 1016 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 D: Lower aft pressure bulkhead 6 oclock position radial stiffener corroded @ BL 0C: Removed damaged section of radial st iffener. Frabricated -7-8-10 +-11 repair parts and installed repair parts per DWG 65C 28106 + SRM 51-40-02 2 L 7 2 4F RT A16WE 2001071700192 20010717 00192 NM 2001 7 17 AWXA0001976 1 20010505 A 5320 6545833040 INTERCOSTAL BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 FLOOR STRUCTURE CRACKED BS 178 WL 207 LBL 25. REMOVED & REPLACED CRACKED FLOOR STRUCTURE (INTERCOSTAL) BS 178 WL 207 LBL 25 PER SRM 51-40-00 & DWG 65-45833 2 L 7 2 4F RT A16WE 2001071700193 20010717 00193 NM 2001 7 17 AWXA0001977 1 20010513 A 5312 65C27181502 MOUNT BOEING 737 7373Q8 1384670 NM 178 BULKHEAD CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 D: BS 178 bulkhead glide slope antenna mount Assy cracked at L/H corner.C: removed damaged repair- fabricated and instal led new repair REF SRM 51-70-13 and DWG 65C27181 2 L 7 2 4F RT A16WE 2001071700194 20010717 00194 NM 2001 7 17 AWXA0001978 1 20010508 A 5313 INTERCOSTAL BOEING 737 7373Q8 1384670 NM BS 178 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 D: Intercostal Cracked BS 178 WL 195 LBL 25C: Repaired Intercostal BS 178, WL 195, LBL 25 Per SRM 53-10-08 2 L 7 2 4F RT A16WE 2001071700195 20010717 00195 NM 2001 7 17 AWXA0001979 1 20010512 A 5315 69366564 SUPPORT BOEING 737 7373Q8 1384670 NM STA 927-947.5 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 D: Aft Cabin Floor Support (shear web) at RBL 0, Between STA 927-947.5 has crack at fastner holes.C: Removed shear web s upport & formed new shear support from 2024T3 0.040 P/O 9502524402. Treated, primed, top coated & installed support REF DWG PL 69-36656 SRM 51-30-01 51-10-01 & 51-20-01 2 L 7 2 4F RT A16WE 2001071700196 20010717 00196 NM 2001 7 17 AWXA0001980 1 20010505 A 5311 WEB BOEING 737 7373Q8 1384670 NM STA 178 A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 D: STA. 178 bulkhead webs L/H & R/H outboard require removal from WL 170 to WL 218 to FOM structure repairsC: Removed an d reinstalled STA 178 bulkhead Webs L/H & R/H as Needed REF SRM 51-40-02 2 L 7 2 4F RT A16WE 2001071700197 20010717 00197 NM 2001 7 17 AWXA0001982 1 20010516 A 5313 INTERCOSTAL BOEING 737 7373Q8 1384670 NM BS 178 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 D: Intercostal cracked BS 178 WL 195 RBL 25C: Repaired Per SRM 53-30-01 & 53-10-08 2 L 7 2 4F RT A16WE 2001071700198 20010717 00198 NM 2001 7 17 AWXA0001983 1 20010516 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373Q8 1384670 NM STA 328 BROKEN A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 D: G-2 track lug Broken off OTBDC: removed damaged section of seat track & replaced STA, 328-380 RBL 45.5 Per SRM 53-00- 52 2 L 7 2 4F RT A16WE 2001071700199 20010717 00199 NM 2001 7 17 AWXA0001989 1 20010712 A 5330 6545766 SKIN BOEING 737 7373G7 1384595 NM FS 500D-520 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 D: 3" crack fuselage skin FS 500 D to 520 STR 12LC: Repaired per SRM 53-00-01 Fig 201 2 L 7 2 4F RT A16WE 2001071700200 20010717 00200 CE 2001 7 17 GLBA2001146 1 20010705 A 2130 129380000113 VALVE BEECH 1900 1900D 1154162 CE ERRATIC A GLBA D RETURN TO BLOCK O OTHER CL CLIMB 1 CE 01 251GL 10416 UE251 CABIN ALTITUDE HI ILLUMINATED PRESSURIZATION WOULD NOT HOLD MORE THAN 3.O, REPLACED LEFT & RIGHT BYPASS VALVES,TEMP SENS ORS, THRU VALVES OPS CHECKED SYSTEM SATISFACTORY 2 L 7 2 4T RT A24CE 2001071800001 20010718 00001 CE 2001 7 18 C2XA01CL166 1 20010717 A 3260 11238002219 ACTUATOR BEECH 1900 1900D 1154162 CE OUT OF ADJ A C2XA K NONE J WARNING INDICATION CL CLIMB 1 SW 27 69549 UE194 CLE FLT.#3032 THE CREW REPORTED LANDING GEAR RED UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION.MAINTENANCE ADJUSTED N OSE LANDING GEAR ACTUATOR. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 2001071800002 20010718 00002 SO 2001 7 18 2001F00020 1 20010523 A 3233 ACTUATOR PIPER PA34 PA34200T 7103406 SO NLG LEAKING A K NONE K FLUID LOSS NR NOT REPORTED 1 GL 21 7693F 347770068 LANDING GEAR WOULD NOT COME OUT OF WHEEL WELLS. EMERGENCY EXTENSION PERFORMED OK. LOCATED RESERVOIR EMPTY AND FOUND SE AL INSIDE OF NOSE GEAR ACTUATOR DETERIORATED TO ALLOW ALL HYDRAULIC FLUID TO BE LOST. 1 L 7 2 3O A7SO 2001071800003 20010718 00003 EU 2001 7 18 DHL200136701 1 20010718 A 2611 CG7GF SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU A DHLA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION UK UNKNOWN 1 SO 01 362DH 84 1) FLT. DECK SMOKE LIGHT ILLUMINATED.2) REPLACED FLIGHT DECK SMOKE DETECTOR IAW MM 26-11-12. OP'S CCK GOOD AT THIS TIM E. P/N OFF CG7 GF P/N ON SAME3) STATUS: CLOSED 2 L 7 2 4F RT A35EU 2001071800004 20010718 00004 EU 2001 7 18 DHL2001367010 1 20010718 A 2611 CG7GF SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU A DHLA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION UK UNKNOWN 1 SO 01 362DH 84 1) FLT. DECK SMOKE LIGHT ILLUMINATED.2) REPLACED FLIGHT DECK SMOKE DETECTOR IAW MM 26-11-12. OP'S CCK GOOD AT THIS TIM E. P/N OFF CG7 GF P/N ON SAME3) STATUS: CLOSED 2 L 7 2 4F RT A35EU 2001071800005 20010718 00005 SO 2001 7 18 2001F00021 2 20010620 A 8520 652241 NUT CESSNA 421 421C 2076016 CE CONT O520 GTSIO520N 17032 SO ENGINE CRACKED A K NONE O OTHER IN INSP/MAINT 1 SO 03 6865Z 421C1068 DURING ANNUAL INSPECTION FOUND NUT CRACKED. NOTHING UNUSUAL NOTICED AS FAR AS INSTALLATION WAS CONCERNED. FOUND THAT N UT CRACKED IN THE CENTER OF THE V ON THE SMALLEST DIAMETER PART OF THE NUT. INSTALLED NEW NUT AND TORQUED TO SPECS. OT HER ENGINE CHECKED AND FOUND TO HAVE A DIFFERENT STYLE NUT. 1 L 7 2 3O 3 O A7CE E7CE 2001071800019 20010718 00019 NM 2001 7 18 01FDEA00572 1 20010718 A 2750 2061131 INDICATOR BOEING 727 727233 138408A NM COCKPIT INOPERATIVE A FDEA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 SO 25 220FE 20934 01-237 INBD TRAILING EDGE FLAP ASYMMETRY OCCURRED DUR FLAP EXT WITH OTBD 30 DEG, INBD LOCK OUT AT LESS THAN 2 DEG. R&R I NBD FLAP POSITION IND PER MM 7-52-021-2. OPS CK GOOD. 2 L 7 3 4F RT A3WE 2001071800022 20010718 00022 NM 2001 7 18 01FDEA00544 1 20010614 A 5510 STABILIZER BOEING 727 727277 138408S NM HORIZONTAL CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 N 409 L/H HORZ STAB UPR TRAILING EDGE BEAM HAS CORROSION 71" FROM O/B END. ** S/D ** R&R PER FEDEX EA 7-5510-57288. 2 L 7 3 4F RT A3WE 2001071800024 20010718 00024 NM 2001 7 18 2001UALA00964 1 20010608 A 5311 FRAME BOEING 737 737322 1384676 NM FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 318UA 23950 AFT PIT FRAME UPPER CHORD RADIUS BLENDED BEYOND LIMITS AT BS 847. ACCOMPLISHED FRAME REPAIR. MAJOR REPAIR ACCOMPLISHED . 2 L 7 2 4F RT A16WE 2001071800025 20010718 00025 NM 2001 7 18 2001UALA00965 1 20010608 A 5311 FRAME BOEING 737 737322 1384676 NM FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 318UA 23950 FRAME WEB GOUGED AT FASTENER HOLE UNDER REMOVED STRAP AT BS 945, STR 11R. REPLACED WEB. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001071800026 20010718 00026 NM 2001 7 18 2001UALA00966 1 20010609 A 5311 FRAME BOEING 737 737322 1384676 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 318UA 23950 RT FRAME CRACKED AT BS 188, WL 207. INSTALLED REPAIR ANGLES AND SKIN DOUBLER. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001071800027 20010718 00027 NM 2001 7 18 2001UALA00967 1 20010609 A 5312 BULKHEAD BOEING 737 737322 1384676 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 BULKHEAD WEB CRACKED AT BS 178, WL 184, RBL 1. ACCOMPLISHED DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001071800028 20010718 00028 NM 2001 7 18 2001UALA00969 1 20010610 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 FLOORBEAM CORRODED AT BS 1006, RBL 15 TO RBL 30. REPLACED FLOORBEAM UPPER T-CAP SECTION. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001071800029 20010718 00029 NM 2001 7 18 2001UALA00970 1 20010610 A 2120 UNKNOWN BOEING 757 757222 1384956 NM CABIN ODOR A UALA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 WP 29 567UA 26673 STRONG BURNED RUBBER ODOR ON TAKEOFF ROLL AT 100 KTS. UNABLE TO DUPLICATE ODOR ON GROUND. 2 L 7 2 4F RT A2NM 2001071800030 20010718 00030 NM 2001 7 18 2001UALA00971 1 20010610 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 FWD GALLEY DOOR AFT CUTOUT FRAME CRACKED. INSTALLED REPAIR ANGLE DOUBLER. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001071800031 20010718 00031 NM 2001 7 18 2001UALA00972 1 20010611 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 FLOORBEAM CORRODED STA 1640, LBL 53. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR. 2 L 7 2 4F RT A2NM 2001071800033 20010718 00033 NM 2001 7 18 2001UALA00974 1 20010610 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 317UA 23949 STRINGER CLIP CRACKED AT BS 706, STR 3L. REPLACED STRINGER CLIP. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001071800034 20010718 00034 NM 2001 7 18 2001UALA00975 1 20010610 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 317UA 23949 STRINGER CLIP CRACKED AT BS 706, STR 2L. REPLACED CLIP. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001071800035 20010718 00035 NM 2001 7 18 2001UALA00976 1 20010610 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 317UA 23949 STRINGER CLIP CRACKED AT BS 663, STR 10L. REPLACED STRINGER CLIP. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001071800036 20010718 00036 NM 2001 7 18 2001UALA00977 1 20010610 A 5312 BULKHEAD BOEING 737 737322 1384676 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 BULKHEAD WEB CRACKED IN 2 PLACES ADJACENT TO RADAR ANTENNA MOUNT FASTENERS AT BS 178, WL 201, RBL 5 TO RBL 6. REPAIRED WITH DOUBLER AND STRUCTURAL FILLERS. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001071800037 20010718 00037 NM 2001 7 18 2001UALA00978 1 20010610 A 5312 BULKHEAD BOEING 737 737322 1384676 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 BULKHEAD WEB, LWR LT ANT MOUNT INBD EDGE UPPER AND LOWER FASTENER AREA, CRACKED IN 2 PLACES AT BS 178, WL 198-201, LBL 5 -6. INSTALLED REPAIR DOUBLER. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001071800038 20010718 00038 NM 2001 7 18 2001UALA00980 1 20010610 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 317UA 23949 TOP OF FLOORBEAM HAS CORROSION. BLENDED MATERIAL LOSS OUT OF LIMITS, AT BS 1016. REMOVED CORROSION. INSTALLED REPAIR STRAP AND NEW INTERCOSTAL. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001071800039 20010718 00039 WP 2001 7 18 DHL2001803559 1 20010710 A 5280 56489332 DOOR DOUG DC8 DC873 302199C WP WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 R/H NLG MID DOOR OF NLG WITH WEAR ON LOWER SKIN.REMOVED R/H NLG MID DOOR PER SRM 51-3-0 PG 1.CLEANED TREATED AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW MID DOOR PER SRM 51-3-0.OPS CHKD PER M/M32-30-0 PG 1. 2 L 7 4 4F RT 4A25 2001071800040 20010718 00040 NM 2001 7 18 2001UALA00981 1 20010608 A 3260 SAFETY SWITCH BOEING 737 737322 1384676 NM MLG FAULTY A UALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 WP 29 325UA 23957 UNSCHEDULED LANDING DUE TO PARTIAL ELECTRICAL FAILURE. *S/D* REPLACED S105 GROUND SENSING SAFETY SWITCH. M990 GROUND S ENSING SQUAT SWITCH IN THE E11 LANDING GEAR LOGIC SWITCH REPLACED PRECAUTIONARY. 2 L 7 2 4F RT A16WE 2001071800041 20010718 00041 NM 2001 7 18 2001UALA00984 1 20010611 A 5330 SKIN BOEING 757 757222 1384956 NM FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 575UA 26689 FUSELAGE DENTED STA 1688-1701, STR 18R. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND TRIPLER. 2 L 7 2 4F RT A2NM 2001071800042 20010718 00042 NM 2001 7 18 2001UALA00985 1 20010611 A 2613 CONNECTOR BOEING 737 737322 1384676 NM NR 2 ENGINE SHORTED A UALA F D ACTIVATE FIRE EXT. RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 WP 29 329UA 24149 NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED.*S/D* FOUND LOWER FAN LOOP-B CONNECTOR SHORTED TO GROUND. REPLACED FIREWALL LOO P-B AND LOWER FAN LOOP-B CONNECTOR 2 L 7 2 4F RT A16WE 2001071800045 20010718 00045 WP 2001 7 18 0102381153 1 20010518 A 5720 SKIN DOUG DC10 DC1040 3023508 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 153US 46762 During L check, found crack in upper corners of cutout on wing leading edge. Repaired per EA11-183471. 2 L 7 3 4F A22WE 2001071800046 20010718 00046 WP 2001 7 18 0102391153 1 20010518 A 5720 STIFFENER DOUG DC10 DC1040 3023508 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 153US 46762 In L check, found corrosion on lower end of stiffener outboard of panel 143CZ of wing center section. Repaired per EA11- 182723. 2 L 7 3 4F A22WE 2001071800047 20010718 00047 WP 2001 7 18 0102401230 1 20010522 A 5753 FLAP DOUG DC10 DC1030 3023501 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 230NW 46552 In L check, found corrosion inside LH OB flap leading edge at hinge attachment area. Repaired per EA12-162200. 2 L 7 3 4F A22WE 2001071800048 20010718 00048 NM 2001 7 18 0102412288 1 20010413 A 5315 FLOORBEAM BOEING 727 727251 138408H NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 288US 21376 IN H CHECK, FOUND CORROSION ON FLOORBEAM. REPAIRED PER EA22-182212. 2 L 7 3 4F A3WE 2001071800049 20010718 00049 NM 2001 7 18 0102422288 1 20010412 A 5311 FRAME BOEING 727 727251 138408H NM CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 288US 21376 In H check, found crack in frame at second hole above floorboard. Repaired per EA22-182214. 2 L 7 3 4F A3WE 2001071800050 20010718 00050 NM 2001 7 18 0102432707 1 20010508 A 5314 KEELBEAM BOEING 727 727225 1384077 NM CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 816EA 22553 In M check, found corrosion on previous keel beam repair and on stringer aft of repair. Repaired per EA27-182225. 2 L 7 3 4F A3WE 2001071800051 20010718 00051 NM 2001 7 18 0102445517 1 20010608 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 517US 23205 IN L2 CHECK, FOUND CRACKED FLOORBEAM. REPAIRED PER EA55-183549. 2 L 7 2 4F RT A2NM 2001071800052 20010718 00052 NM 2001 7 18 0102456306 1 20010616 A 5347 SEAT TRACK BOEING 747 747451 1384940 NM CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 666US 23821 In H check, found corrosion on seat track. Repaired per EA63-182725. 2 L 7 4 4F RT A20WE 2001071800053 20010718 00053 NM 2001 7 18 0102466306 1 20010622 A 5347 SEAT TRACK BOEING 747 747451 1384940 NM CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 666US 23821 In H check, found corrosion on seat track. Repaired per EA63-184052. 2 L 7 4 4F RT A20WE 2001071800054 20010718 00054 NM 2001 7 18 0102476306 1 20010620 A 5320 FLOOR SUPPORT BOEING 747 747451 1384940 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 666US 23821 IN H CHECK, FOUND CORROSION ON FLOOR SUPPORT. REPAIRED PER EA63-183406. 2 L 7 4 4F RT A20WE 2001071800055 20010718 00055 NM 2001 7 18 0102486638 1 20010512 A 5711 FITTING BOEING 747 747251B 1384892 NM CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 638US 23549 In M check, found crack at L wing aft spar kick fitting #2 bolt hole. Repaired per EA66-162195. 2 L 7 4 4F A20WE 2001071800059 20010718 00059 NM 2001 7 18 2001UALA00991 1 20010611 A 2810 FUEL TANK BOEING 767 767322 1385200 NM RIGHT IMBALANCED A UALA O OTHER O OTHER CR CRUISE 1 WP 29 656UA 25394 RT TANK INDICATION IS ROLLING BACK, AFTER APPROX 1 HOUR, 2500 LBS LOWER THAN LEFT TANK. CREW REPORTS PROGRESS PAGE MATC HES TOTALIZER AND IMBALANCE REMAINED FOR ENTIRE FLIGHT. CAPT TRIED BALANCING BY FEEDING BOTH ENGS WITH LT TANK. 2 L 7 2 4F RT A1NM 2001071800060 20010718 00060 NM 2001 7 18 2001UALA00993 1 20010508 A 3350 BATTERY PACK BOEING 767 767222 1385122 NM CABIN FAULTY A UALA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 WP 29 614UA 21875 EMERGENCY LIGHTS COMING ON IN AFT PART OF CABIN AFTER LANDING DURING TAXI IN. *S/D* BATTERY PACK ON ORDER FROM CHICAGO OSTF NR A1551 FLT 121 AT 1039. PACK LOCATION ROW 40 SIDEWALL VENT SCREEN. CONT OF AMIS ITEM 1332004. 2 L 7 2 4F RT A1NM 2001071800061 20010718 00061 NM 2001 7 18 2001UALA00994 1 20010608 A 5320 SPLICE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 615UA 21876 STR SPLICE FITTING CORRODED BS 434 STR 35L. 2 L 7 2 4F RT A1NM 2001071800062 20010718 00062 NM 2001 7 18 2001UALA00995 1 20010608 A 5313 STRINGER BOEING 767 767222 1385122 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 615UA 21876 STR CRACKED BS 434 STR 39R. 2 L 7 2 4F RT A1NM 2001071800063 20010718 00063 NM 2001 7 18 2001UALA00996 1 20010611 A 5311 FRAME BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 615UA 21876 AFT CARGO PIT AT BS 1285, LBL 45-RBL 45, FRAME T-CAP IS CORRODED. 2 L 7 2 4F RT A1NM 2001071800064 20010718 00064 NM 2001 7 18 2001UALA00997 1 20010611 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 SHEARTIE CORRODED AT STA.588, STR.39L-39R. 2 L 7 2 4F RT A1NM 2001071800065 20010718 00065 NM 2001 7 18 2001UALA00998 1 20010606 A 4920 APU BOEING 767 767322 1385200 NM APU BAY MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 666UA 29238 APU FAILED TO START AT FL340. AFTER TURNBACK, IT DID START AT FL200. NR 1 GEN ALSO INOP, RTF. 2 L 7 2 4F RT A1NM 2001071800066 20010718 00066 NM 2001 7 18 2001UALA01000 1 20010607 A 4920 APU BOEING 767 767322 1385200 NM APU BAY MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 666UA 29238 APU WOULD NOT START IN FLIGHT AFTER 3 ATTEMPTS AT FL 300, FL320, AND FL360, RTF. 2 L 7 2 4F RT A1NM 2001071800067 20010718 00067 NM 2001 7 18 2001UALA01001 1 20010608 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 615UA 21876 SHEARTIE CORRODED BS 368 STR 38R-39R. 2 L 7 2 4F RT A1NM 2001071800068 20010718 00068 NM 2001 7 18 2001UALA01002 1 20010608 A 5320 SPLICE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 615UA 21876 STRINGER SPLICE FITTING CORRODED BS 434 STR 39L. 2 L 7 2 4F RT A1NM 2001071800069 20010718 00069 NM 2001 7 18 2001UALA01003 1 20010608 A 5313 STRINGER BOEING 767 767222 1385122 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 615UA 21876 STR CRACKED BS 434 STR 39R. 2 L 7 2 4F RT A1NM 2001071800070 20010718 00070 NM 2001 7 18 2001UALA01004 1 20010608 A 5320 SPLICE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 615UA 21876 STR SPLICE FITTING CORRODED BS 434 STR 35L. 2 L 7 2 4F RT A1NM 2001071800071 20010718 00071 NM 2001 7 18 2001UALA01005 1 20010608 A 5313 STRINGER BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 615UA 21876 STR CORRODED BS 1540-1562 STR 39R. 2 L 7 2 4F RT A1NM 2001071800072 20010718 00072 NM 2001 7 18 2001UALA01006 1 20010608 A 5313 STRINGER BOEING 767 767222 1385122 NM FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 615UA 21876 PIT STRINGER GAUGED BS 434-456 STR 39L. 2 L 7 2 4F RT A1NM 2001071800073 20010718 00073 NM 2001 7 18 2001UALA01007 1 20010608 A 5320 SPLICE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 615UA 21876 FWD PIT STR SPLICE CORRODED BS 434 STR 39R. 2 L 7 2 4F RT A1NM 2001071800076 20010718 00076 EU 2001 7 18 AWXA0001994 1 20010629 A 5313 D53480030206 STRINGER AIRBUS 320 A320231 3930325 EU FR 66. STR 43 MISDRILLED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 645AW 238 D: Fr 66 L/H STR 43 has double drilled holesC: Stringer repaired as per SRM 53-00-13 Fig. 201 from sta .3152 to 3167 2 L 7 2 4F RT A28NM 2001071800077 20010718 00077 EU 2001 7 18 AWXA0001995 1 20010629 A 5321 D5311278220000 SEAT TRACK AIRBUS 320 A320231 3930325 EU FR 12R 16R Y1292 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 645AW 238 D: Fwd galley floor support at Y1292 Fr 14R and 16R corrodedC: Fwd galley support/seat track at Y1292 FR12R-16R replaced as per A320 SRM 53-11-15 fig. 203 2 L 7 2 4F RT A28NM 2001071800078 20010718 00078 NM 2001 7 18 2001UALA01011 1 20010612 A 2612 G718505 CONTROL PANEL BOEING 737 737322 1384676 NM COCKPIT MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 356UA 24362 CARGO HEAT DETECTION SYSTEM WARNING FLICKERED BRIEFLY. NR 1 DISCHARGE LIGHT ILLUMINATED. *S/D* INSPECTION OF THE AIRCR AFT DID NOT INDICATE ANY SMOKE OR FIRE IN THE CARGO COMPARTMENTS. REPLACED CARGO COMPARTMENT SMOKE CONTROL PANEL, DIVER TER VALVE ASSY AND NR 1 BOTTLE. 2 L 7 2 4F RT A16WE 2001071800079 20010718 00079 NM 2001 7 18 0102492289 1 20010711 A 3242 21147AC BRAKE BOEING 727 727251 138408H NM NBR 3 BRAKE A NWAA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 GL 01 289US 66595 349 21377 AFTER TAXI IN, RAMP AGENT NOTIFIED CREW THAT RIGHT MAIN BRAKE WAS ON FIRE. CREW EXPEDITED DEPLANING THROUGH CABIN DOORS. GROUND PERSONNEL EXTINGUISHED FIRE. MAINTENANCE REMOVED BRAKE AND INSPECTED BRAKE FLANGE, AND AXLE FOR GALLING, CRACKS, OR DISCOLORATION. CHECKED OK. REPLACED NBR 3 BRAKE ASSEMBLY. LEAK AND OPERATIONAL CHECK GOOD. 2 L 7 3 4F A3WE 2001071800080 20010718 00080 NM 2001 7 18 0102516306 1 20010717 A 2913 VICKERS 3508806 BOEING 747 747451 1384940 NM A NWAA H DEACTIVATE SYST/CIRCUITS K FLUID LOSS UK UNKNOWN 1 GL 01 666US 404158 23821 DURING FLIGHT, RECEIVED "HYD PRES ENG 4" AND "HYD QTY LOW" MESSAGES. THE HYDRAULIC FLUID QUANTITY IN THE NBR 4 SYSTEM IN DICATED ZERO. TURNED OFF THE HYDRAULIC PUMPS FOR THE NBR 4 SYSTEM AND THE CREW DECLARED AN EMERGENCY. ALTERNATE EXTENDED THE LANDING GEAR AND THE AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE ENGINE DRIVEN HYDRAULIC PUMP. OPERATIONAL CH ECK GOOD. 2 L 7 4 4F RT A20WE 2001071800081 20010718 00081 2001 7 18 2001UALA01012 4 20010610 A 2330 ODOR BOEING 777 777222 1385219 NM CABIN DETECTED A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 794UA 26953 ELECTRICAL ODOR IN THE AREA OF ROW 13 AND 14 ON FLOOR AREA DVS SYSTEM, TURNED OFF MASTER POWER SW. CONTACTED SQAMC, REC OMMENDED THAT SYSTEM BE LEFT OFF FOR REMAINDER OF FLIGHT. *S/D* OPERATED THE VIDEO SYSTEM FOR 6:30 HOURS, VIDEO SYSTEM OPERATED NORMAL AND NO ELECTRICAL SMELL WAS NOTICED. REMOVED ACCESS COVERS BENEATH SEATS AND CHECKED THE SEAT POWER SU PPLY, VIDEO DISTRIBUTION BOXES, SEAT ELECTRONIC UNITS AND EMERGENCY LIGHT CABLES, ALL CHECKED OK. AS A PRECAUTION PACK S OPERATED FOR TWO HOURS, AND NO ELECTRICAL SMELL WAS APPARENT. 2 L 7 2 4F RT T0001SE 2001071800082 20010718 00082 NM 2001 7 18 2001UALA01013 1 20010608 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 615UA 21876 PIT FLOOR T CAP CORRODED BS 1153 RBL 45-LBL 45. 2 L 7 2 4F RT A1NM 2001071800083 20010718 00083 NM 2001 7 18 2001UALA01014 1 20010611 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 615UA 21876 AFT CARGO PIT AT BS 1285, LBL 45-RBL 45, FRAME T-CAP IS CORRODED. 2 L 7 2 4F RT A1NM 2001071800084 20010718 00084 NM 2001 7 18 2001UALA01015 1 20010611 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 SHEARTIE CORR. STA.588, AND STR. 38L-39L. 2 L 7 2 4F RT A1NM 2001071800085 20010718 00085 NM 2001 7 18 2001UALA01016 1 20010611 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 SHEARTIE CORR. AT STA.588, STR. 39L-39R. 2 L 7 2 4F RT A1NM 2001071800086 20010718 00086 NM 2001 7 18 2001UALA01017 1 20010509 A 5320 STRINGER CLIP BOEING 767 767222 1385122 NM FUSELAGE BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 500 STR 39R CLIP BROKEN. 2 L 7 2 4F RT A1NM 2001071800087 20010718 00087 EU 2001 7 18 RAIA00107014 1 20010717 A 2134 1103P0532 SWITCH AEROSP ATR72 ATR72202 8680940 EU RT ENGINE FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 723TE 283 7166-STL-RIGHT BLEED FAULT CAPTION ILLUMINATED DURING CLIMB, AIRCRAFT RETURNED FROM FLIGHT WITHOUT INCEDENT. MAINTENANCE INSPECTED AND REPLACED RIGHT BLEED AIR PRESSURE SWITCH. 2 H 7 2 4T RT A53EU 2001071800088 20010718 00088 2001 7 18 RAIA00107015 4 20010717 A 3420 HG2010AC02 COMPUTER EMB 145 EMB145ER SO AVIONICS BAY FAILED A RAIA D RETURN TO BLOCK I FLT. ATTITUDE INST. TX TAXI/GRND HDL 1 CE 03 808HK 4366 1743 145157 5284-MEM-FIRST OFFICERS AHRS FAILED DURING TAXI. MAINTENANCE INSPECTED AND REPLACED FIRST OFFICERS AHRS COMPUTER. 2 L 7 2 4F RT T00011AT 2001071800089 20010718 00089 NM 2001 7 18 2001UALA01018 1 20010509 A 5310 STRUCTURE BOEING 767 767222 1385122 NM FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 HOLES KNIFE EDGED AT BS 1350-1370 STR 34L. 2 L 7 2 4F RT A1NM 2001071800090 20010718 00090 EA 2001 7 18 COMA0160480 1 20010716 A 5320 60135006 WEB CNDAIR CL600 CL6002B19 EA CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 979CA 7159 7159 LEFT SIDE LOWER WEB OF ENG SUPPORT HAS 1.5 INCH CRACK AT FS 635, LBL 42, WL 111.09COMPLIED WITH REO 601R-53-61-366 REV B BY CUTTING AWAY DAMAGED SECTION NDT INSP AND INSTALLING FABRICATED REPAIR PARTS I/A/W REO 601R-53-61-366 REV B. 2 L 7 2 4F RT A21EA 2001071800091 20010718 00091 NM 2001 7 18 2001UALA01019 1 20010509 A 5320 WEB BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 1329-1351 RB17 TO LBL6 SHEARWEB CORRODED. 2 L 7 2 4F RT A1NM 2001081300022 20010813 00022 NM 2001 8 13 2001UALA01020 1 20010609 A 3350 900542U1 SIGN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7454U 21908 OVERHEAD EMERGENCY EXIT SIGN AT OVER WING EXIT INOPERABLE. THE BASE ASSY FAILED. REPLACED BASE ASSY. OPERATIONS CHECK NO RMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001071800092 20010718 00092 EA 2001 7 18 COMA0160481 1 20010717 A 5346 60135006 WEB CNDAIR CL600 CL6002B19 EA CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 969CA 11722 7141 DURING COMPLIANCE OF EO 53-021 (VISUAL INSPECTION OF THE ENGINE SUPPORT BEAM) FOUND RIGHT LOWER WEB OF ENGINE SUPPORT BE AM CRACKED.REPAIRED THE ENGINE SUPPORT BEAM IN ACCORDANCE WITH CRJ REO 601-53-61-366 REV B. 2 L 7 2 4F RT A21EA 2001071800093 20010718 00093 NM 2001 7 18 2001UALA01021 1 20010612 A 2150 39608831 CONTROL VALVE BOEING 727 727222 1384073 NM A/C BAY FAILED A UALA B EMER. DESCENT O OTHER CR CRUISE 1 WP 29 7293U 21571 AT CRUISE LOST RIGHT PACK. EMERGENCY DESCENT TO 24,000 FT. *S/D* FORWARD PACK VALVE FAILED. REPLACED FORWARD PACK VA LVE. OPERATIONS CHECK NORMAL. 2 L 7 3 4F A3WE 2001071800094 20010718 00094 NM 2001 7 18 2001UALA01022 1 20010613 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 CABIN FLOORBEAM UPPER FLANGES CORRODED STA 310.5, RBL 40. *S/D* RECONNECTED POWER CONNECTOR IN INSIDE OF SIDE WALL. O P CHECKS OK. 2 L 7 2 4F RT A2NM 2001071800096 20010718 00096 EA 2001 7 18 COMA0160482 1 20010718 A 5346 60135006 WEB CNDAIR CL600 CL6002B19 EA CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 951CA 13435 7091 DURING COMPLIANCE OF EO 53-021 (VISUAL INSPECTION OF THE ENGINE SUPPORT BEAM) FOUND LOWER LEFT ENGINE SUPPORT BOX BEAM S KIN CRACKED.REPAIRED THE ENGINE SUPPORT BEAM IN ACCORDANCE WITH CRJ REO 601-53-61-366 REV B. 2 L 7 2 4F RT A21EA 2001071800098 20010718 00098 EA 2001 7 18 COMA0160483 1 20010718 A 5346 60135006 WEB CNDAIR CL600 CL6002B19 EA CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 951CA 13435 7091 DURING COMPLIANCE OF EO 53-021 (VISUAL INSPECTION OF THE ENGINE SUPPORT BEAM) FOUND LOWER RIGHT ENGINE SUPPORT BOX BEAM SKIN CRACKED.REPAIRED THE ENGINE SUPPORT BEAM IN ACCORDANCE WITH CRJ REO 601-53-61-366 REV. B. 2 L 7 2 4F RT A21EA 2001071800099 20010718 00099 NM 2001 7 18 2001UALA01025 1 20010613 A 2782 654465117 ACTUATOR BOEING 737 737291 138448W NM L/E SLAT FAILED A UALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 WP 29 989UA 21751 NR 6 SLAT WILL NOT RETRACT. *S/D* REPLACED NR 6 SLAT ACTUATOR. 2 L 7 2 4F A16WE 2001071800100 20010718 00100 EU 2001 7 18 2001UALA01026 1 20010613 A 2150 758A000002 BYPASS VALVE AIRBUS 320 A320232 3930326 EU NR 2 A/C PACK FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 413UA 470 UNABLE TO CONTROL CABIN TEMPERATURE.*S/D* REPLACED NR 2 PACK TURBINE BYPASS VALVE DUE TO FAILURE FAULTED BY CFDS. IN A DDITION REPLACED NUMEROUS LEAKING DUCT SEALS IN RT PACK, NO FURTHER FAILURES REPORTED. 2 L 7 2 4F RT A28NM 2001071800101 20010718 00101 NM 2001 7 18 2001UALA01027 1 20010509 A 5320 SPLICE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 434 STR 38R SPLICE CORRODED. 2 L 7 2 4F RT A1NM 2001071800102 20010718 00102 NM 2001 7 18 2001UALA01028 1 20010509 A 5313 STRINGER BOEING 767 767222 1385122 NM FUSLEAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 434 STR 37L CRACKED AT SPLICE. 2 L 7 2 4F RT A1NM 2001071800103 20010718 00103 NM 2001 7 18 2001UALA01029 1 20010509 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 1131 STR 39L-39R SHEARTIE CORRODED. 2 L 7 2 4F RT A1NM 2001071800104 20010718 00104 NM 2001 7 18 2001UALA01030 1 20010509 A 5320 STRINGER CLIP BOEING 767 767222 1385122 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 412 STR 39R STRINGER CLIP CRACKED. 2 L 7 2 4F RT A1NM 2001071800105 20010718 00105 NM 2001 7 18 2001UALA01031 1 20010509 A 5320 CLIP BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 370 FRAME ATTCH. CLIP STR 39R CORRODED. 2 L 7 2 4F RT A1NM 2001071800106 20010718 00106 NM 2001 7 18 2001UALA01032 1 20010509 A 5320 STRINGER CLIP BOEING 767 767222 1385122 NM FUSELAGE BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 434 STR 35R CLIP BROKEN. 2 L 7 2 4F RT A1NM 2001071800107 20010718 00107 NM 2001 7 18 2001UALA01033 1 20010509 A 5320 CLIP BOEING 767 767222 1385122 NM FUSLEAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 370 STR 39L FRAMER ATTCH CLIP CORRODED. 2 L 7 2 4F RT A1NM 2001071800108 20010718 00108 NM 2001 7 18 2001UALA01035 1 20010612 A 3350 LIGHT BOEING 747 747422 1384935 NM CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY LIGHT SEAT 5J AFT EEL STRIP INOP. REPLACED EEL STRIP, OPS CKD OK. 2 L 7 4 4F RT A20WE 2001071800109 20010718 00109 NM 2001 7 18 2001UALA01036 1 20010509 A 5320 SPLICE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 434 STR 36R STRINGER SPLICE CORRODED. 2 L 7 2 4F RT A1NM 2001071800111 20010718 00111 NM 2001 7 18 2001UALA01038 1 20010509 A 5313 STRINGER BOEING 767 767222 1385122 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 456 STR 39R CRACKED. 2 L 7 2 4F RT A1NM 2001071800112 20010718 00112 NM 2001 7 18 2001UALA01039 1 20010606 A 5313 STRINGER BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 615UA 21876 BS 355 STR 39L CORRODED. 2 L 7 2 4F RT A1NM 2001071800114 20010718 00114 WP 2001 7 18 01FDEA00574 1 20010718 A 5101 SKIN DOUG DC10 DC1010 3022110 WP AFT SIDE CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 N 351 #2 ENGINE INLET AFT SIDE HAS CRACK. R&R PER IAW EA & SRM REQ. 2 L 7 3 4F A22WE 2001071800115 20010718 00115 WP 2001 7 18 01FDEA00575 1 20010718 A 5300 ABA73483 FRAME DOUG DC10 DC1010 3022110 WP CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 N 240 THERE IS CRACK ON FRAME AT Y=459, X=18 AT FRAME SPLICE INCLUDE IS A PREVIOUS REPAIR FROM X=18 TO X=18. R&R FRAME PER IAW EA & SRM. 2 L 7 3 4F A22WE 2001071800116 20010718 00116 WP 2001 7 18 GTIA010527 1 20010615 A 3350 60030431 CHARGER DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 133NK 48111 FOUND WITH NO POWER ON A/C EMERGENCY LIGHTS (OVERHEAD) BETWEEN SEATS 17 AND 21 COME ON. REMOVED AND REPLACED BATTERY CH ARGER FOR EMERGENCY OVERHEAD LIGHTS, SYSTEM OPS CHECK NORMAL IAW DC9 MM 33-50-00. NO OTHER DEFECTS NOTED. (M) 2 L 7 2 4F A6WE 2001071800117 20010718 00117 2001 7 18 GTIA010529 4 20010615 A 2230 COVER DOUG DC9 DC983 3022083 WP AUTOTHROTTLE SYS DEFECTIVE A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 602CA 49415 FLT 628 - LGA - FOUND UNABLE TO ENGAGE AUTOTHROTTLE. ITEM TRANSFERRED TO DMI IAW MEL REF 23-15-2 PLACARD INSTALLED. RE MOVED AND REPLACED LEFT THROTTLE PALM SWITCH COVER PER MD-80 MM 22-31-01. CHECK PER MM 22-01-05. INDICATES NO FAULTS T O AUTO THROTTLES SYSTEM. THIS CLEARS DMI NR 0010512-1. PLACARDS REMOVED. (M) 2 L 7 2 4F RT A6WE 2001071800118 20010718 00118 2001 7 18 GTIA010537 4 20010619 A 3460 4034241972 COMPUTER DOUG DC9 DC981 3022081 WP NR 2 FAULTY A GTIA O OTHER O OTHER CL CLIMB 1 GL 23 819NK 48016 FLL - FLT 941 - ON NR 2, DFGS AUTOPILOT KICKED OFF SEVERAL TIMES IN CLIMB NR 1 WAS FINE. REMOVED AND REPLACED NR 2 DFGC IAW MM 22-01-01. PERFORMED RTS REF MM 22-01-05. (M) 2 L 7 2 4F A6WE 2001071800119 20010718 00119 WP 2001 7 18 GTIA010544 1 20010329 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND CORROSION AND CRACKS FOUND ON LONGERON L-26 BETWEEN 2ND AND 3RD FRAME FORWARD OF MID CARGO DOOR. REMOVED FI NGER DOUBLER UNDER LONGERON L26. FORMED FINGER DOUBLER IAW MC-80 MM SRM 53-01. INSTALLED FINGER DOUBLER IAW MD-80-MM 5 1-30-2. (M) 2 L 7 2 4F RT A6WE 2001071800120 20010718 00120 WP 2001 7 18 GTIA010545 1 20010328 A 5754 RIB DOUG DC9 DC983 3022083 WP L/E SLAT GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - RIGHT WING NR 5 SLAT 4TH RIB FROM INBOARD HAS DEEP GOUGE. REMOVED DAMAGED RIB IAW MD-80 SRM 51-30-02. FORMED NEW RIB IAW MD-80 SRM 51-10-2. INSTALLED RIB IAW MD-80 SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2001071800121 20010718 00121 WP 2001 7 18 GTIA010546 1 20010330 A 5320 CLIP DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - AFT B/B BOTTOM FORWARD DOOR CUTOUT CORNER CLIP IS CRACKED. REMOVED CRACKED CLIP IAW MD-80 SRM 51-30-2. FORMED CL IP IAW MD-80 SRM 51-10-02. LOCATED AND DRILLED CLIP IAW MD-80 SRM 51-10-02. INSTALLED CLIP IAW MD-80 SRM 51-30-02. (M ) 2 L 7 2 4F RT A6WE 2001071800122 20010718 00122 WP 2001 7 18 GTIA010547 1 20010330 A 5320 SUPPORT BRACKET DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - AFT CARGO COMPARTMENT CRACKS AT LEFT BELTFRAME SUPPORT STATION 1212. REMOVED SUPPORT BRACKET IAW MD-80 SRM 51-30. FABRICATED NEW SUPPORT BRACKET IAW SRM 51-10-1. INSTALLED IAW MD-8- SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2001071800123 20010718 00123 WP 2001 7 18 GTIA010548 1 20010407 A 5311 BELTFRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND CORROSION ON BELT FRAME AT STATION 1041 BETWEEN 27L AND 27R. REMOVED CORROSION IAW SRM MD-80 SRM 51-10-3. FORMED NEW ANGLE FOR REPAIR IAW SRM MD-80 51-10-02. LOCATED AND DRILLED ANGLE IAW IAW MD-80 SRM 53-01. INSTALLED ANGLE IAW MD-80 SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2001071800124 20010718 00124 WP 2001 7 18 GTIA010549 1 20010410 A 5320 SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND MID LOWER CARGO COMPARTMENT, CRACK AT BELT FRAME SUPPORT ABOVE STRINGER 29L STATION 655. REMOVED CRACKED SU PPORT PER MD-80 SRM 51-30-2. REPAIRED SUPPORT. INSTALLED SUPPORT PER MD-80 SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2001071800125 20010718 00125 WP 2001 7 18 GTIA010560 1 20010623 A 2120 DUCT DOUG DC9 DC983 3022083 WP A/C BAY LEAKING A GTIA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 602CA 49415 DTW - FLT 9952 - TAIL COMPARTMENT HIGH TEMP LIGHT ON FOR 1 MINUTE 50 SECONDS. DURING CLIMB-OUT FROM MLB HP BLEED OFF. FOLLOWED BY QRH PROCEDURE. PERFORMED HIGH POWER ENGINE RUN IAW MD-8- MM 72-00. FOUND BOTH L/R AND RIGHT A/C TEMP HIGH SENSORS LEAKING. RESOLVED IAW MD-80 SRM 21-61-04 AND FOUND FLEX DUCT ON LEFT SIDE LEAKING. REPOSITIONED DUCT PERFORMED ADJUST TEST OF TAIL COMPARTMENT SENSOR IAW MD-80 MM. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 2001071800126 20010718 00126 WP 2001 7 18 GTIA010564 1 20010623 A 2432 2634006106 CHARGER DOUG DC9 DC982 3022082 WP E/E BAY FAULTY A GTIA H DEACTIVATE SYST/CIRCUITS O OTHER CR CRUISE 1 GL 23 801NK 48048 FLT 678 - DTW - BATTERY CHARGER PULSES LEFT 8-10 TIMES PER MINUTE. BATTERY VOLTS NORMAL. QRH COMPLIED WITH. CIRCUIT B REAKER PULLED. CHARGER CIRCUIT BREAKER. REMOVED AND REPLACED BATTERY CHARGER. OPS CHECKED GOOD PER MD-80 MM 24-30-00 . NO OTHER DISCREPANCIES NOTED. (M) 2 L 7 2 4F A6WE 2001071800127 20010718 00127 2001 7 18 GTIA010565 4 20010624 A 3421 258733511 GYRO DOUG DC9 DC932 3022066 WP COCKPIT DEFECTIVE A GTIA O OTHER O OTHER CL CLIMB 1 GL 23 133NK 48111 FLT 304 - ACY - VERTICAL SPEED WHEEL DOES NOT AGREE WITH VERTICAL SPEED IN DESCENT AND CLIMB. AT 500 IN CLIMB ON VERT S PEED WHEEL, A/C CLIMBS 2000 FPM, 500 FPM DESCENDS AIRCRAFT AS MUCH AS 2500 FPM. REMOVED AND REPLACED NR 2 VG. OPS CHEC K GOOD IAW DC-9 MM 34-27-0. NO OTHER DEFECTS NOTED. (M) 2 L 7 2 4F A6WE 2001071800129 20010718 00129 WP 2001 7 18 GTIA010566 1 20010623 A 3350 B525 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 133NK 48111 FLT 8083 - ACY - FOUND OVERWING EMERGENCY LIGHTS INOPERATIVE AT ROW 15 BOTH SIDES. REMOVED AND REPLACED TWO BATTERIES A T PACK B5-25. SYSTEM OPS CHECK GOOD PER DC-9 MM 33-53-00. (M) 2 L 7 2 4F A6WE 2001071800130 20010718 00130 WP 2001 7 18 GTIA010602 1 20010625 A 2560 S168MA MEGAPHONE DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 822NK 49392 FLT 1525 - RSW - MEGAPHONE INOPERATIVE, FORWARD RIGHT. REMOVED AND REPLACED FORWARD RIGHT MEGAPHONE. NEXT INSPECTION D UE TO 6/02. (M) 2 L 7 2 4F RT A6WE 2001071800131 20010718 00131 WP 2001 7 18 GTIA010604 1 20010622 A 3610 CLAMP DOUG DC9 DC983 3022083 WP A/C BAY LOOSE A GTIA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 602CA 49415 MLB - FLT 41 - TAIL COMPARTMENT TEMP HIGH ON CLIMB-OUT FROM DCA. QRH PROCEDURES, LIGHT EXTINGUISHED AFTER 1 MINUTE AND 45 SECONDS. TIGHTENED CLAMP ON SMALL, LEAKAGE RIGHT PNEU. DUCT SUPPLY PERFORMED EXTENDED HIGH, POWER ENGINE RUN-UP. N O TAIL HIGH LIGHT, NO DISCREPANCIES NOTED. ALL OK IAW MM 32-30-00. (M) 2 L 7 2 4F RT A6WE 2001071800132 20010718 00132 NM 2001 7 18 P2EA01105 1 20010613 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 127NJ 22886 DURING C-CHECK, FOUND LOWER FUSELAGE, PNEUMATIC GROUND CONNECTOR AREA, FROM BS 520 TO BS 540 BETWEEN STRINGER 28L TO 28R , CUTOUT SKIN WITH SHARP EDGES AND CRACK. REPAIRED FUSELAGE SKIN. CUT OUT AREA FORM BS 500B PLUS 18 TO BS 540 BETWEEN STRINGER 27L AND 27R DUE TO SHARP EDGES. CRACK AND MISSING SECTION IAW COOPESA EO COO-3-53-255-01 DATED JUNE 13, 2001. 2 L 7 2 4F A16WE 2001071800133 20010718 00133 NM 2001 7 18 P2EA01106 1 20010614 A 5754 SLAT BOEING 737 7372B7 1384560 NM LT WING DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 127NJ 22886 SJO - DURING C-CHECK, LEFT WING NR 3 LEADING EDGE SLAT WITH DELAMINATION AT TRAILING EDGE AREA, FROM SS 0.00 TO SS15.00. REPAIRED LEFT WING NR 3 SLAT P/N 65-46423-273A, S/N BN-7 DUE TO DELAMINATION BETWEEN SLAT STATION .27 AND 18.52 IAW CO OPESA EO NR COO-CMP-3-57-261-01. (M) 2 L 7 2 4F A16WE 2001071800134 20010718 00134 NM 2001 7 18 P2EA01107 1 20010614 A 5754 SLAT BOEING 737 7372B7 1384560 NM RT WING DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 127NJ 22886 SJO - DURING C-CHECK, FOUND RIGHT WING NR 6 LEADING EDGE SLAT WITH DELAMINATION AT TRAILING EDGE AREA, FROM SS 352 TO SS 360 AND FROM SS417 TO SS 430. REPAIRED RT WING NR 6 SLAT TRAILING EDGE SECTION P/N 65-46421-228A, S/N BN-19 DUE TO DEL AMINATION BETWEEN SLAT STATION 254.53 AND 385.26 IAW COOPESA EO NR COO-CMP-3-57-258-01 DATED JUN 14, 2001. (M) 2 L 7 2 4F A16WE 2001071800135 20010718 00135 NM 2001 7 18 P2EA01108 1 20010614 A 5753 SKIN BOEING 737 7372B7 1384560 NM T/E FLAP DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 127NJ 22886 DURING C-CHECK, FOUND LEFT WING INBOARD AFT FLAP LOWER SKIN WITH DELAMINATION FROM WBL 88 TO WBL 95. REPAIRED LEFT WING INBOARD AFT FLAP P/N 65-46434-139, S/N 652 DUE TO DELAMINATION AT LOWER SKIN BETWEEN WBL 88 AND 111.75 IAW COOPESA EO N R COO-CMP-3-57-260-01 DATED JUNE 13, 2001. (M) 2 L 7 2 4F A16WE 2001071800136 20010718 00136 NM 2001 7 18 P2EA01109 1 20010614 A 5751 SKIN BOEING 737 7372B7 1384560 NM AILERON DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 127NJ 22886 SJO - DURING C-CHECK, FOUND LEFT WING AILERON UPPER SKIN WITH DENTS AND LOWER SKIN WITH DELAMINATION AT WBL 480. REPAIR ED LEFT WING AILERON P/N 65-46454-23A, S/N 555 DUE TO DELAMINATION BETWEEN WBL STATION 471 AND 486 IAW COOPESA EO NR COO -CMP-3-57-259-01 DATED JUNE 14, 2001 AND DOCUMENTED ON FAA 8110-3 FORM. (M) 2 L 7 2 4F A16WE 2001071800137 20010718 00137 NM 2001 7 18 P2EA01110 1 20010620 A 5313 STRINGER BOEING 737 7372B7 1384560 NM FUSELAGE CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 127NJ 22886 SJO - DURING C-CHECK, LOWER FUSELAGE, E/E COMPARTMENT FROM BS 344 TO 360, STRINGER 25 LEFT WITH CORROSION. TRIM OF FUSE LAGE FRAME SECTION AT BS 344, AT STRINGER 25 LEFT PERFORMED DUE TO ACCESS FOR REPAIR AT STRINGER 25L. FUSELAGE STRINGER 25L REPAIRED BETWEEN BS 331 AND 360 DUE TO CORROSION IAW SRM 53-10-3 FIG 1. FUSELAGE FRAME SECTION REPAIRED AT BS 344 BETWEEN STRINGER 24 AND 26 LEFT DUE TO ACCESS IAW SRM 51-40-3 FIG 1. (M) 2 L 7 2 4F A16WE 2001071800138 20010718 00138 NM 2001 7 18 P2EA01111 1 20010702 A 5311 FRAME BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 128NJ 22892 SJO - DURING C-CHECK INSPECTION PER S/B 737-53A1173, FOUND PRESSURE BULKHEAD, BS 178 VERTICAL CHORD CRACKED AT LBL 5.7 W L 184, PRESSURE BULKHEAD BS 178 RIGHT SIDE LATERAL CHORD CRACKED AT WL 207, PRESSURE BULKHEAD BS 178 LEFT SIDE LATERAL C HORD CRACKED AT WL 207. (M) 2 L 7 2 4F A16WE 2001071800139 20010718 00139 NM 2001 7 18 P2EA01112 1 20010702 A 5312 BULKHEAD BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 128NJ 22892 DURING C-CHECK INSPECTION PER S/B 737-53A1173 PRESSURE BULKHEAD, BS 178 WEB CRACKED AT WL 234, LBL 10 INCHES, PRESSURE B ULKHEAD BS 178 WEB CRACKED AT WL 218, RBL 10.7 INCH, PRESSURE BULKHEAD BS 178, RT SIDE INTERCOSTAL CRACKED AT WL 195, PR ESSURE BULKHEAD BS 178 LT SIDE INTERCOSTAL CRACKED AT WL 195. (M) 2 L 7 2 4F A16WE 2001071800140 20010718 00140 NM 2001 7 18 P2EA01113 1 20010703 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 128NJ 22892 SJO - DURING C-CHECK, FUSELAGE BS 1026 BETWEEN STRINGER 27L AND 27R SKIN WITH DENT OUT OF LIMITS. (M) 2 L 7 2 4F A16WE 2001071800141 20010718 00141 NM 2001 7 18 P2EA01114 1 20010703 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 128NJ 22892 SJO - DURING C-CHECK, FUSELAGE FROM BS 847 TO BS 867 BETWEEN STRINGER 26L AND 26R HAS SKIN WITH DENTS OUT OF LIMITS. (M ) 2 L 7 2 4F A16WE 2001071800142 20010718 00142 NM 2001 7 18 P2EA01115 1 20010705 A 5755 SPOILER BOEING 737 7372B7 1384560 NM RT WING DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 128NJ 22892 SJO - DURING C-CHECK, RIGHT WING, SPOILER NR 6 (P/N 65-46451-61A, S/N MA6427) DELAMINATED. (M) 2 L 7 2 4F A16WE 2001071800143 20010718 00143 NM 2001 7 18 P2EA01116 1 20010706 A 5754 SKIN BOEING 737 7372B7 1384560 NM L/E FLAP DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 128NJ 22892 SJO - DURING C-CHECK, LEFT WING, OUTBOARD FORE FLAP (P/N 65-46431-251, S/N BN424) UPPER SURFACE WITH BULGED SKIN, DELAMI NATION AND DENTS. (M) 2 L 7 2 4F A16WE 2001071800144 20010718 00144 NM 2001 7 18 AWXA0002002 1 20010707 A 5315 654541041 WEB BOEING 737 737277 1384570 NM BS 712, LBL 25 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 D: Floor beam cracked @ BS 712, LBL 25C: Repaired floor beam web at BS 712, LBL 25 IAW AWA ER #15-5715-01195-SS1 2 L 7 2 4F RT A16WE 2001071800145 20010718 00145 WP 2001 7 18 ZW0A0105301 1 20010717 A 3350 58222 BATTERY PACK DOUG DC9 DC982 3022082 WP A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 926TW 49356 DURING PREFLIGHT THE FIRST CLASS EGRESS LIGHTS WERE FOUND INOP. REMOVED MOISTURE FROM EGRESS LIGHT TRACK AND REPLACED BATTERY PACK P/N 5822-2. LAST CHECK C 08/29/00 STL. ---CLOSED--- 2 L 7 2 4F A6WE 2001071800146 20010718 00146 NM 2001 7 18 QXEA0101173 1 20010703 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM DISCHARGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- EMERGENCY LIGHT ON EXTERIOR INOP. MAINTENANCE REPLACED BATTERY PACK PS3. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001071800147 20010718 00147 NM 2001 7 18 QXEA0101172 1 20010710 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM DISCHARGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PSC- EMERGENCY FLOOR STRIP LIGHTS AT DS1 AND DS2 INOP. MAINTENANCE REPLACED BATTERY POWER PACK PS5 AND FLOOR PATH STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001071900001 20010719 00001 NM 2001 7 19 OZIA200143004 1 20010712 A 3230 7144002 PSEU DORNER DO32 DO328300 NM FAILED A OZIA A UNSCHED LANDING J G WARNING INDICATION MULTIPLE FAILURE CL CLIMB 1 CE 05 430Z 2485 3127 Approximately 2 minutes after takeoff, had gear tone and other failures: 1) norm anti-skid fail, 2) proxy system "A" fai l, 3) HYD qty "A" fail, 4) ground spoilers not stowed. Apparent proxy system "A" fail or total proxy computer fial. Norm al landing extension not available. Landed with alternate gear extension. Removed and replaced PSEU IAW manufacturer's i nstruction. Ops checked all affected systems IAW manufacturer's instructions. Ops check good. Released aircraft for flig ht. 2 H 7 2 4T RT A55NM 2001081500124 20010815 00124 NM 2001 8 15 01FDEA00576 1 20010718 A 3232 69163395 FITTING BOEING 727 72725C 138400H NM NLG WW CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 DURING ROUTINE INSP FOUND SUPPORT FITTING FOR NLG DOOR ACTUATOR ROD CORRODED. *S/D* REMOVED AND REPLACED FITTING PER I AW SRM 51-30-2. 2 L 7 3 4F A3WE 2001081600079 20010816 00079 NM 2001 8 16 01FDEA00577 1 20010718 A 2782 FITTING BOEING 727 72725C 138400H NM L/E FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 DURING ROUTINE INSP FOUND SUPPORT FITTING NR 2 KRUEGER FLAP ACTUATOR SUPPORT FITTING AT FRONT SPAR CRACKED. *S/D* REMO VED AND REPLACED PER IAW SRM 57-20-1. 2 L 7 3 4F A3WE 2001081500126 20010815 00126 NM 2001 8 15 01FDEA00578 1 20010718 A 5720 FITTING BOEING 727 72725C 138400H NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 DURING ROUTINE INSP FOUND SUPPORT FITTING FOR NR 6 LEADING EDGE SLAT UP STOP CRACKED. *S/D* REMOVED AND REPLACED FITTI NGS PER IAW SRM 51-20-1. 2 L 7 3 4F A3WE 2001071900002 20010719 00002 EU 2001 7 19 SIMA200116203 1 20010611 A 6100 10223N01R00 INDICATOR SAAB SF340 340B 7860101 EU FLT DECK FAILED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 238AE 340B238 LGA - FLT 4515 - ABORT TAKEOFF RIGHT PROP ERRATCI. REMOVED AND REPLACED PROP SPEED INDICATOR IAW AMM 61-40-00. OPS CHE CK GOOD. (M) 2 L 7 2 4T RT A52EU 2001071900003 20010719 00003 EU 2001 7 19 SIMA200117601 1 20010625 A 3350 6013211 BATTERY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 329AE 340B329 SBP - FOUND CABIN EMERGENCY EXIT LIGHTS OUT. REMOVED AND REPLACED EMERGENCY BATTERY ASSEMBLY IAW SAAB AMM 33-50-00. (M ) 2 L 7 2 4T RT A52EU 2001071900004 20010719 00004 NM 2001 7 19 USAA010634 1 20010608 A 5300 FRAME BOEING 737 737301 1384611 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND FRAME CRACKED .5 INCH, BS 480, STRINGER 8L. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001071900005 20010719 00005 NM 2001 7 19 USAA010633 1 20010608 A 5300 FRAME BOEING 737 737301 1384611 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND FRAME CRACKED, BS 867, BETWEEN STRINGER 8 AND 9L. DAMAGE REMOVED, INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001071900006 20010719 00006 NM 2001 7 19 USAA010643 1 20010611 A 5330 SKIN BOEING 737 737201 1384454 NM FS 873/885 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 232US 57380 22018 TPA - FOUND SKIN CRACKED 2.5 INCH AND 2.75 INCH, STATION 873 AND 885 ABOVER 19R. INSTALLED DOUBLER .063 INCH CLAD 2024T B USING BLIND FASTENERS PER SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 2001071900007 20010719 00007 NM 2001 7 19 USAA010642 1 20010611 A 5300 SKIN BOEING 737 737201 1384454 NM BS 727A/727B CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 232US 57380 22018 TPA - FOUND SKIN CRACKED BETWEEN STATION 727A AND 727B BELOW 13L. INSTALLED DUOBELR PER SRM USING BLIND FASTENERS PER S RM 53-30-3 FIG 1 AND MPP 308-25. (M) 2 L 7 2 4F A16WE 2001071900008 20010719 00008 NM 2001 7 19 USAA010641 1 20010608 A 5300 FRAME BOEING 737 737301 1384611 NM BS 440 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND FRAME CRACKED .5 INCH BS 440, STRINGER 8R. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001071900009 20010719 00009 NM 2001 7 19 USAA010640 1 20010608 A 5310 FRAME BOEING 737 737301 1384611 NM BS 500A CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND FRAME CRACKED .5 INCH, BS 500A, STRINGER 8R. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001071900010 20010719 00010 NM 2001 7 19 USAA010657 1 20010612 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 1016 CORRODED A K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND FLOORBEAM CORRODED APPROX 14 SQUARE INCHES, BS 1016 LBL 45 TO RBL 45. REMOVED AND REPLACED T-CAP PER SRM 53 -00-51. (M) 2 L 7 2 4F RT A16WE 2001071900011 20010719 00011 NM 2001 7 19 USAA010654 1 20010612 A 5315 FLOORBEAM BOEING 737 737301 138447R NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND FLOORBEAM CORRODED APPROXIMATELY 1 SQUARE INCH AREA, BS 344, LBL 24 TO RBL 11. REMOVED AND REPLACED T-CAP S ECTION PER SRM 51-10-2 AND 53-10-51. (M) 2 L 7 2 4F RT A16WE 2001071900012 20010719 00012 NM 2001 7 19 USAA010653 1 20010612 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND FLOORBEAM CORRODED APPROXIMATELY 12 SQUARE INCH AREA, BS 328, BL 0 TO RBL 60. REMOVED AND REPLACED ENTIRE T EE CAP PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2001071900013 20010719 00013 NM 2001 7 19 USAA010651 1 20010612 A 5315 FLOORBEAM BOEING 737 737301 138447R NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND FLOORBEAM CORRODED 100 INCH BY 2 INCH AREA, BS 986, AFT ENTRY DOOR TO AFT GALLEY SERVICE DOOR. REMOVED AND REPLACED ENTIRE T-CAP PER TR 53-10-05A. (M) 2 L 7 2 4F RT A16WE 2001071900014 20010719 00014 NM 2001 7 19 USAA010649 1 20010612 A 5300 WEB BOEING 737 737301 1384611 NM BS 747-767 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND CREASE BEAM WEB CORRODED, .5 INCH BY 10 INCHES, BS 747 TO 767, STRINGER 17L. FABRICATED AND INSTALLED NEW W EB PER BOEING DRAWING NR 65-46818, SRM 51-40-02, 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001071900015 20010719 00015 NM 2001 7 19 USAA010647 1 20010612 A 5330 DOUBLER BOEING 737 737301 1384611 NM BS 360-380 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND DOUBLER DENTED .5 INCH BY .5 INCH, BS 360-380, BL 0 BELLY, E/E COOLING DUCT CUTOUT. REMOVED AND REPLACED PR EVIOUSLY INSTALLED PER SRM 51-10-02 AND BOEING DRAWING NR 65C33930. (M) 2 L 7 2 4F RT A16WE 2001071900016 20010719 00016 NM 2001 7 19 USAA010650 1 20010612 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 967 CORRODED A K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 23743 CLT - FOUND FLOORBEAM CORRODED .5 INCH, BS 967, RBL 5. REMOVED AND REPLACED ENTIRE T-CAP PER TR 53-10-05A. REMOVED AND REPLACED ENTIRE TEE CAP PER TR 53-10-05A. (M) 2 L 7 2 4F RT A16WE 2001071900017 20010719 00017 NM 2001 7 19 USAA010668 1 20010613 A 5300 STRINGER BOEING 737 737301 1384611 NM BS 1100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND STRINGER CORRODED APPROXIMATELY .5 INCH, BS 1100, STRINGER 5R. REMOVED DAMAGE, SPLICED IN NEW STRINGER SECT ION PER SRM 53-00-03, 51-30-01, 51-40-02. (M) 2 L 7 2 4F RT A16WE 2001071900018 20010719 00018 NM 2001 7 19 USAA010666 1 20010613 A 5300 DOOR FRAME BOEING 737 737301 1384611 NM BS 295 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND FRAME CRACKED INTERNAL .5 INCH, BS 295, FORWARD SERVICE DOOR CUTOUT, LOWER FORWARD CORNER. INSTALLED REPAIR ANGLES PER SRM 51-70-11. (M) 2 L 7 2 4F RT A16WE 2001071900019 20010719 00019 NM 2001 7 19 USAA010665 1 20010613 A 5310 FRAME BOEING 737 737301 1384611 NM BS 727D CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND FRAME CRACKED .5 INCH, BS 727D. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001071900020 20010719 00020 NM 2001 7 19 USAA010664 1 20010613 A 5310 FRAME BOEING 737 737301 1384611 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND FRAME CRACKED .5 INCH, BS 867, BETWEEN STRINGERS 8R AND 9R. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001071900021 20010719 00021 NM 2001 7 19 USAA010663 1 20010613 A 5300 FRAME BOEING 737 737301 1384611 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND FRAME CRACKED .5 INCH, BS 380, STRINGER 8R. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001071900022 20010719 00022 NM 2001 7 19 USAA010662 1 20010612 A 5300 WEB BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND WEB CRACKED .25 INCH AND .125 INCH, BS 178, WL 198 AT LBL 6, WL 234 AT LBL 13.3. DAMAGED REMOVED, INSTALLED DOUBLER AND FILLERS PER EO 5300V153. (M) 2 L 7 2 4F RT A16WE 2001071900023 20010719 00023 NM 2001 7 19 USAA010671 1 20010613 A 5300 SKIN BOEING 737 737301 1384611 NM BS 330 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND SKIN CRACKED .5 INCH, BS 330, 4 INCHES ABOVE STRINGER 17R. DAMAGED REMOVED, INSTALLED DOUBLER AND TRIPLER. (M) 2 L 7 2 4F RT A16WE 2001071900024 20010719 00024 NM 2001 7 19 USAA010673 1 20010613 A 5300 ATTACH ANGLE BOEING 737 737301 1384611 NM BS 290 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND ATTACH ANGLE CRACKED 1 INCH, BS 290, INTERCOSTAL BETWEEN S11R AND S12R. REMOVED AND REPLACED INTERCOSTAL AT TACH ANGLE PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001071900025 20010719 00025 WP 2001 7 19 MWEA011057 1 20010717 A 2751 WIRE DOUG DC9 DC914 3022034 WP L/FLAP XMITTER BROKEN A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 700ME 45696 STICK SHAKER CAME ON AFTER ROTATION. -- REPAIRED BROKEN WIRE ON RIGHT FLAP POSITION TRANSMITTER. 2 L 7 2 4F A6WE 2001071900026 20010719 00026 NM 2001 7 19 USAA010672 1 20010613 A 5300 ATTACH ANGLE BOEING 737 737301 1384611 NM BS 290 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 23743 CLT - FOUND ATTACH ANGLE CRACKED 1 INCH, BS 290, INTERCOSTAL BETWEEN S12R AND S13R. REMOVED AND REPLACED INTERCOSTAL AT TACH ANGLE PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001071900027 20010719 00027 NM 2001 7 19 USAA010677 1 20010613 A 5500 ATTACH ANGLE BOEING 737 737301 1384611 NM BS 1120 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND ATTACH ANGLE/FITTING CRACKED APPROXIMATELY 6 INCHES, BS 1120, H STAB CENTER SECTION, PRIME AND AUX THRUST BE AM. REMOVED AND REPLACED ATTACH FITTING ANGLE AT INTERSECTION OF PRIMARY, AUX AND THRUST BEAM PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001071900028 20010719 00028 NM 2001 7 19 USAA010675 1 20010613 A 5300 INTERCOSTAL BOEING 737 737301 1384611 NM BS 278 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND INTERCOSTAL CRACKED .5 INCH, BS 278, S14R. STOP DRILLED CRACK, INSTALLED DOUBELR PER SRM 51-70-11. (M) 2 L 7 2 4F RT A16WE 2001071900029 20010719 00029 WP 2001 7 19 USAA010684 1 20010605 A 5300 ATTACH ANGLE DOUG DC9 DC982 3022082 WP BS 1463 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 829US 41770 49429 PIT - FOUND PYLON ATTACH ANGLE CRACKED .25 INCH, LOWER PYLON ATTACH ANGLE STATION 1463 CANTED. STOP DRILLED CRACK PER T YPICAL REPAIR 54-10-06A. (M) 2 L 7 2 4F A6WE 2001071900030 20010719 00030 NM 2001 7 19 USAA010679 1 20010610 A 5300 SKIN BOEING 737 737201 1384454 NM BS 727A/727B CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 232US 57380 22018 CLT - FOUND SKIN CRACKED 1 INCH, BETWEEN BS 727A AND 727B, BELOW S13L. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER USING B LIND FASTENERS PER SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 2001071900031 20010719 00031 NM 2001 7 19 USAA010681 1 20010614 A 5330 SKIN BOEING 737 737401 1384701 NM BS 727D CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 36822 23882 CLT - FOUND SKIN CRACKED, BS 727D, LEFT SIDE, EMERGENCY LIGHT AFT OF WHEEL WELL. DAMAGE REMOVED, INSTALLED DOUBLER PER SRM 53-00-01, FIG 202. (M) 2 L 7 2 4F RT A16WE 2001071900032 20010719 00032 NM 2001 7 19 USAA010706 1 20010517 A 5300 WEB BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND WEB CRACKED .25 INCH, BS 178 BULKHEAD LOWER LT ANTENNA MOUNT. FILLER, DOUBLERS, SHIMS PER SRM 53-10-08 FIG 211. (M) 2 L 7 2 4F RT A16WE 2001071900033 20010719 00033 NM 2001 7 19 USAA010705 1 20010517 A 5300 WEB BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND WEB CRACKED .5 INCHES LONG, STATION 178 BULKHEAD ANTENNA MOUNT RIGHT. FILLER, DOUBLER, SHIMS PER SRM 53-10- 08 FIG 211. (M) 2 L 7 2 4F RT A16WE 2001071900034 20010719 00034 NM 2001 7 19 USAA010702 1 20010517 A 5300 FRAME BOEING 737 737301 1384611 NM BS 380 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND INDICATION BY HFEC IS DOUBLE FLUSH RIVET, BS 380 AT S8L. CUT OUT DAMAGE, INSTALLED FILLERS AND DOUBLER PER SRM 53-00-07 PAGE 203-206. (M) 2 L 7 2 4F RT A16WE 2001071900035 20010719 00035 NM 2001 7 19 USAA010701 1 20010517 A 5300 FRAME BOEING 737 737301 1384611 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND FRAME CRACKED .5 INCH, BS 380 AT S8R. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER PER SRM 53-00-07 FIG 201 . (M) 2 L 7 2 4F RT A16WE 2001071900036 20010719 00036 NM 2001 7 19 USAA010749 1 20010618 A 5300 SKIN BOEING 737 737201 1384454 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 51038 22796 TPA - FOUND SKIN CRACKED 1 INCH, AFT OF STATION 907 STRINGER 18L. INSTALLED DOUBLER PER EA 71383 AND SRM 53-00-01 FIG 2 23. (M) 2 L 7 2 4F A16WE 2001071900037 20010719 00037 NM 2001 7 19 USAA010707 1 20010517 A 5300 WEB BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND WEB CRACKED .5 INCH, FORWARD PRESSURE BULKHEAD STATION 178. REPLACED WEB. (M) 2 L 7 2 4F RT A16WE 2001071900038 20010719 00038 NM 2001 7 19 USAASB01182 1 20010622 A 3350 20131A BATTERY PACK BOEING 737 737301 1384611 NM AFT GALLEY INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 588US 23933 PIT - MAINTENANCE FOUND THE AFT GALLEY OVERHEAD EMERGENCY EXIT LIGHT, RIGHT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001071900039 20010719 00039 EU 2001 7 19 USAAF01034 1 20010623 A 5600 D20543406 WINDSHIELD FOKKER F28 F28MK0100 4990807 EU COCKPIT CRACKED A USAA K NONE O OTHER CR CRUISE 1 EA 19 881US 653 11333 CLT-MEM - FLT 865 - THE RIGHT FORWARD WINDSHIELD INNER PANE SHATTERED, AND HAD A LARGE BUBBLE ON THE OUTER PANE DURING F LIGHT. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FIRST OFFICERS WINDSHIELD. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT 2001071900040 20010719 00040 NM 2001 7 19 USAASB01183 1 20010625 A 3350 20131A BATTERY PACK BOEING 737 7374B7 1384702 NM INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 775AU 24933 ALB - MAINTENANCE FOUND THE EMERGENCY EVACUATION LIGHTS ON SEAT ROWS 13-19, BULLNOSE LIGHT AT ROW 20 LEFT AND SIDEWALL E XIT SIGN AT ROW 12 RIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT ROW 21 CEILING LOCATION. OP S CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001071900041 20010719 00041 NM 2001 7 19 USAABB01043 1 20010621 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 622AU 27201 BWI - MAINTENANCE FOUND THE EMERGENCY LIGHT ON SEAT ROW 29, RIGHT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED T HE BATTERY ON SEAT ROW 29, RIGHT SIDE. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2001071900042 20010719 00042 WP 2001 7 19 USAAD01130 1 20010625 A 3350 8732030153 MODULE DOUG DC9 DC981 3022081 WP PAX CABIN FAILED A USAA K NONE O OTHER CR CRUISE 1 EA 19 808US 48040 BOS-BWI - FLT 247 - THE LAST THREE ROWS OF LOW LEVEL EMERGENCY LIGHTS ILLUMINATED DURING FLIGHT. MAINTENANCE REPLACED T HE AFT LOW LEVEL EMERGENCY LIGHT CONTROL MODULE. (M) 2 L 7 2 4F A6WE 2001071900043 20010719 00043 EU 2001 7 19 USAAF01037 1 20010627 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU PAX CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 885US 11345 RIC - THE EMERGENCY LIGHTS AT THE FORWARD ENTRANCE DOOR, FORWARD SERVICE DOOR, AND UNDER THE COAT CLOSET WOULD NOT ILLUM INATE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT 2001071900044 20010719 00044 EU 2001 7 19 USAAF01036 1 20010627 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU PAX CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 867US 11312 GSO - THE EMERGENCY LIGHTS WERE INOPERATIVE IN THE CENTER CABIN. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT 2001071900045 20010719 00045 EU 2001 7 19 USAASA01030 1 20010628 A 2120 UNKNOWN AIRBUS 330 A330202 3930316 EU CABIN ODOR A USAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 EA 19 105UW 4011 0868 DCA-LGA - FLT 6848 - THE AFT LAVATORY SMOKE DETECTOR SMOKE WARNING ILLUMINATED ON CLIMB-OUT OF DCA. SMOKE ODOR WAS ALSO CONFIRMED BY A FLIGHT ATTENDANT. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED LAVA TORIES AND THE AIR CONDITIONING SYSTEM. NO FAULTS WERE FOUND. OPERATED PACKS AND NOTED NO PROBLEMS. PERFORMED ENVIRON MENTAL CONTROL SYSTEM DECONTAMINATION TASK. REPLACED RECIRCULATION AND LAVATORY FILTERS, AND AFT LAVATORY SMOKE DETECTO R AS PRECAUTION. OK FOR SERVICE. (M) 2 L 7 2 4F RT A46NM 2001071900046 20010719 00046 NM 2001 7 19 ASAA0110264 1 20010515 A 3350 883200312 RECEIVER BOEING 737 737290C 138448V NM MID CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY TRACK LIGHTS ON SEAT PALLETS 2-11 AND 4-7 INOPERATIVE. REMOVED AND REPL ACED THREE REMOTE ASSEMBLY BATTERIES AND TWO REMOTE ASSEMBLY RECEIVERS, THEN LIGHTS OPERATED NORMAL. (M) 2 L 7 2 4F A16WE 2001071900047 20010719 00047 WP 2001 7 19 ASAA0180155 1 20010503 A 3350 6011779 POWER SUPPLY DOUG DC9 DC982 3022082 WP INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 937AS 49364 OAK - DURING MAINTENANCE CHECK, OVERWING EMEREGNCY EXIT LIGHTS WERE DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED B ATTERY PACK (POWER SUPPLY). LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001071900048 20010719 00048 NM 2001 7 19 ASAA0110252 1 20010501 A 3350 8821004 BATTERY BOEING 737 737210C 1384459 NM SMOKE BARRIER INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY TRACK LIGHTS ON THE SMOKE BARRIER FAILED RECON TEST. REMOVED AND REPLAC ED REMOTE ASSEMBLY BATTERY, THEN LIGHTS OPERATED NORMAL. (M) 2 L 7 2 4F A16WE 2001072000001 20010720 00001 CE 2001 7 20 C2XA01CL168 1 20010719 A 3260 NAS1351CO8LE8P SCREW BEECH 1900 1900D 1154162 CE BROKEN A C2XA K NONE J WARNING INDICATION CL CLIMB 1 SW 27 81553 UE222 AZO FLT.#4370 THE CREW REPORTED ON TAKE OFF LANDING GEAR INTRANSIT LIGHT DID NOT EXTINGUISH WHEN LANDING GEAR WAS UP.M AINTENANCE REPLACED CAP SCREW IN CAM FOR 17 DEGREE FLAP MICROSWITCH. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT WAS RETU RNED TO SERVICE. 2 L 7 2 4T RT A24CE 2001072000002 20010720 00002 EU 2001 7 20 SABA010030 1 20010717 A 3230 1379305A155 HYDRAULIC LINE BAG JETSTM JETSTM3201 1500217 EU RT GEAR WELL LEAKING A SABA O OTHER K FLUID LOSS AP APPROACH 1 SO 33 919AE 919 Acft 919AE n flight 5198 HTS TO CLT. During descent for landing at CLT, when the landing gear was extended the gear did not respond. Both hydraulic pumps indicated zero pressure. An inflight emergency was declared. The emergency gear ex tension was selected and landing gear and flaps hand pumped down.The aircraft landed at CLT and taxied to the gate with no other problems. Maintenance removed and replaced the right landing gear radius rod up line. Due to the engine drive n pumps being run dry, both pumps were removed and replaced, hydraulic filters wire changed and hydraulic system was pur ged. 2 L 7 2 4T RT A56EU 2001072000003 20010720 00003 WP 2001 7 20 DHL2001804013 1 20010718 A 2611 SMOKE DETECTOR DOUG DC8 DC873F 302199F WP A DHLA K NONE B J L SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NO TEST IN INSP/MAINT 1 SO 01 804DH 46124 1) #5 SMOKE DETECTOR INOP2) RELAMPED SMOKE DETECTOR OPS CHECKED GOOD PER MM 26-10-5STATUS: CLOSED 2 L 7 4 4F RT 4A25 2001072000004 20010720 00004 WP 2001 7 20 DHL2001804014 1 20010719 A 2611 SMOKE DETECTOR DOUG DC8 DC873F 302199F WP A DHLA K NONE B J L SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NO TEST CR CRUISE 1 SO 01 804DH 46124 1) NO 5 SMOKE DETECTOR INOP2) MAY BE INOP PER MEL 26-6-1 DMI #6439 PLACARD INSATALLEDSTATUS: CLOSE 2 L 7 4 4F RT 4A25 2001072000005 20010720 00005 CE 2001 7 20 GLBA2001160 1 20010716 A 3200 50060285 WHEEL BEECH 1900 1900D 1154162 CE #3 BLOWN A GLBA K NONE O OTHER LD LANDING 1 CE 01 195GL 169 UE195 RIGHT MAIN GEAR SMOKING AFTER LANDING, REPLACED #3 WHEEL ASSEMBLY OPS CHECKED SYSTEM SATISFACTORY 2 L 7 2 4T RT A24CE 2001072000006 20010720 00006 SO 2001 7 20 C2XA01CL167 1 20010715 A 3350 20131A BATTERY EMB 145 EMB145ER SO CABIN DISCHARGED A C2XA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 27 14939 145030 CLE FLIGHT#3489 THE CREW REPORTED THE EMERGENCY LIGHTS OVERWING AT EXIT ROW 12 WERE INOPERATIVE.MAINTENANCE APPLIED POWE R TO THE AIRCRAFT TO CHARGE THE EMERGENCY BATTERY PACKS.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVI CE. 2 L 7 2 4F RT T00011AT 2001072000007 20010720 00007 CE 2001 7 20 GLBA2001162 1 20010717 A 7700 305399CL11 PROBE BEECH 1900 1900D 1154162 CE LEFT ENGINE OUT OF TOLERANCE A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 01 220GL UE220 LEFT ENGINE WOULD NOT MAKE POWER ON T/O ROLL, REPLACED TRIM PROBE OPS CHECKED SYSTEM SATISFACTORY 2 L 7 2 4T RT A24CE 2001072000008 20010720 00008 CE 2001 7 20 GLBA2001163 1 20010718 A 3200 50067495 BRAKE BEECH 1900 1900D 1154162 CE LEFT #1 DEFECTIVE A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 01 201YQ 996 UE201 AIR CRAFT VEERED LEFT ON T/O ROLL, INSPECTED DETERMINED LEFT BRAKE LOCKED UP, REPLACED BOTH #1&2 BRAKES OPS CHECKED SATI SFACTORY 2 L 7 2 4T RT A24CE 2001072000009 20010720 00009 WP 2001 7 20 ABXA010401 1 20010717 A 2782 ROD END DOUG DC9 DC932 3022066 WP RIGHT WING BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 900AX 47380 RIGHT WING LEADING EDGE SLAT ACTUATOR ROD END BROKEN. REPLACED THE RIGHT WING LOWER SLAT ACTUATOR ROD END IAW DC-9 MM 27 -80-05-2-10. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2001072000010 20010720 00010 NM 2001 7 20 2001UALA01346 1 20010710 A 5311 STRAP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 320UA 23952 AFT PIT DOOR CUTOUT LOWER STRAP JUST INBD OF DOOR SILL HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED.REPLACED STRAP. 2 L 7 2 4F 4 F RT A16WE E2GL 2001072000011 20010720 00011 NM 2001 7 20 2001UALA01355 1 20010712 A 5312 WEB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CRACKED A UALA L ABORTED APPROACH O OTHER IN INSP/MAINT 1 WP 29 392UA 24667 BULKHEAD WEB CRACKED AT LOWER LH RADAR MOUNT INBOARD SIDE, STA 178. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001072000012 20010720 00012 NM 2001 7 20 2001UALA01356 1 20010712 A 5313 STRINGER BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 912UA 25290 STRINGER CORRODED. STA 266 STR 22. MAJOR REPAIR ACCOMPLISHED.INSTALLED FILLERS AND STRINGER SPLICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2001072000013 20010720 00013 NM 2001 7 20 2001UALA01357 1 20010712 A 5320 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 320UA 23952 #2, #3 AND #4 STOP PAD CUTOUTS CRACKED AT FWD FRAME, DOOR 1 RIGHT. MAJOR REPAIR ACCOMPLISHED.INSTALLED NEW ANGLE DOUBLE RS. 2 L 7 2 4F 4 F RT A16WE E2GL 2001072000014 20010720 00014 NM 2001 7 20 2001UALA01358 1 20010712 A 5311 WEB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 320UA 23952 DOOR CUTOUT FRAME WEB HAS CORRODED FASTENERS. MAJOR REPAIR ACCOMPLISHED.REPLACED FWD DOOR FRAME WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2001072000016 20010720 00016 NM 2001 7 20 2001UALA01360 1 20010713 A 5730 SKIN BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE WORN A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 976UA 21598 LH WING LE SKIN WORN AT NUMBER 2 SLAT CENTER STOP. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER. 2 L 7 2 4F 4 F A16WE E2EA 2001072000017 20010720 00017 NM 2001 7 20 2001UALA01361 1 20010713 A 5315 FLOORBEAM BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 976UA 21598 FLOORBEAM T CAP CORRODED. STA 967, RBL 4 TO RBL 45. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED TCAP SPLICE REPAIR. 2 L 7 2 4F 4 F A16WE E2EA 2001072000018 20010720 00018 NM 2001 7 20 2001UALA01362 1 20010713 A 5313 STRINGER BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 976UA 21598 STRINGER CORRODED. STR 6L, STA 767. MAJOR REPAIR ACCOMPLISHED.INSTALLED STRINGER SPLICE AND REPLACED TIE CLIP. 2 L 7 2 4F 4 F A16WE E2EA 2001072000019 20010720 00019 NM 2001 7 20 2001UALA01363 1 20010713 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 320UA 23952 FUSELAGE FRAME AT FWD DOOR CUTOUT STA 295.5 AT FLOOR LEVEL HAS SMALL CRACK. MAJOR REPAIR ACCOMPLISHED.INSTALLED ANGLE D OUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001072000020 20010720 00020 NM 2001 7 20 2001UALA01364 1 20010712 A 5241 6545871132 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 911UA 29175 25255 LOWER AFT DOOR FRAME CRACKED AT VERTICAL FRAME OUTBOARD FASTENER HOLE. DOOR 1 RIGHT. MAJOR REPAIR ACCOMPLISHED.INSTALLE D FRAME DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001072000021 20010720 00021 NM 2001 7 20 2001UALA01365 1 20010712 A 5210 6545871132 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 911UA 29175 25255 DOOR 1 RIGHT, #3 AFT STOP FITTING CUTOUT CRACKED. MAJOR REPAIR ACCOMPLISHED.ACCOMPLISHED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001072000022 20010720 00022 SO 2001 7 20 SIMA200116601 1 20010615 A 3200 4131 SHUTOFF VALVE EMB 135 EMB135LR SO INOPERATIVE A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 716AE 145264 LGA - FLT 4547 - ON TAKEOFF ROLL, OUTBOARD BRAKE INOPERATIVE ON EICAS. ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENAN CE REMOVED AND REPLACED THE LEFT BRAKE SHUTOFF VALVE IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVIC E. (M) 2 L 7 2 4F RT TOOO11AT 2001072000023 20010720 00023 SO 2001 7 20 SIMA200116902 1 20010619 A 2600 14521182403 DUCT EMB 145 EMB145LR SO AFT CARGO DAMAGED A SIMA O OTHER O OTHER CR CRUISE 1 SW 21 614AE 145086 ORD - FLT 4262 - DURING FLIGHT, CREW REPORTED A NR 2 BLEED LEAK. AFTER LANDING CARGO FIRE WARNING LIGHT ILLUMINATED. C REW FIRED BOTTLES. MAINTENANCE FOUND A DAMAGED DUCT BEHIND AN AFT CARGO WALL. DUCT WAS REPLACED, OPS CHECK WAS GOOD. FIRE BOTTLES WERE REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001072000024 20010720 00024 EU 2001 7 20 SIMA20011711 1 20010612 A 5300 S53678001244 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU CORRODED A SIMA O OTHER O OTHER IN INSP/MAINT 1 SW 21 499AT 499 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE LEFT OUTBOARD, LEFT F/A, AND RIGHT F/A SEAT TRACKS CORRODED. M AINTENANCE REMOVED AND REPALCED THE SEAT TRACK IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001072000025 20010720 00025 EU 2001 7 20 SIMA20011712 1 20010612 A 5315 S5367740620802 FLOORBEAM AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA O OTHER O OTHER IN INSP/MAINT 1 SW 21 499AT 499 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED FLOORBEAM 36, 38 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED FLOORBEAMS 36 AND 38 IAW SRM 53-00-00. MAINTENANCE REPAIRED FLOORBEAM 39 IAW SRM 53-00-00 FIGURE 435. AIRCRAFT WAS RE TURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001072000026 20010720 00026 EU 2001 7 20 SIMA200116703 1 20010616 A 2700 BP234561 SWITCH AEROSP ATR42 ATR42300 8680920 EU COCKPIT INOPERATIVE A SIMA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SW 21 971NA 017 JAX - FLT 5248 - CREW REPORTED THE AILERON TRIM TO BE INOPERATIVE AT AN UNLEVEL POSITION. CAPTAIN NOTED IT TOOK ABOUT T HIRTY POUNDS OF PRESSURE TO MAINTAIN LEVEL FLIGTH. MAINTENANCE REMOVED AND REPLACED THE TRIM CONTROL PANEL IAW ATR MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001072000027 20010720 00027 EU 2001 7 20 SIMA200116704 1 20010616 A 2100 125A01 CHECK VALVE AEROSP ATR42 ATR42300 8680920 EU DAMAGED A SIMA O OTHER O OTHER CR CRUISE 1 SW 21 135MQ 135 FLT 5273 - MCO - DURING LEVEL FLIGHT AT FL180, THE CREW REPORTED A LOUD POP FOLLOWED BY A LOSS OF CABIN PRESSURE. MAINT ENANCE FOUND A CHECK VALVE DAMAGED. CHECK VALVE AND DUCT VALVE WAS INSTALLED IN WERE REMOVED AND REPLACED IAW ATR MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001072000028 20010720 00028 SO 2001 7 20 SIMA200115903 1 20010608 A 5300 ALCLAD2024T3 SKIN EMB 135 EMB135LR SO CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 703MR 145173 ABI - DURING MBV INSPECTION, FOUND LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE BELOW SRM LIMITS AFTER REMOVAL OF CORROSI ON. REMOVED AND REPAIRED CORRODED AREA BY CUTOUT. WORK DONE IAW EMB-145 SRM (1142 REV 13) 53-21-10 PARA 2 PAGE 201, 20 2, AND FIG 201 SHEET 1. (M) 2 L 7 2 4F RT TOOO11AT 2001072000029 20010720 00029 EU 2001 7 20 SIMA200117108 1 20010620 A 5315 S5367240620802 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 426AT 426 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED FLOORBEAMS 36, 38, 39 AND 40 CORRODED BEYOND LIMITS. MAINTENANCE R EMOVED AND REPLACED FLOORBEAMS IAW ATR 72 SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001072000030 20010720 00030 NM 2001 7 20 MASA01047 1 20010605 A 3300 40005130003 SWITCH DHAV DHC8 DHC8202 2809007 NM INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 434YV 434 FLT 6327 - GJT-PHX - THE EMERGENCY EXIT LIGHTS WOULD NOT TURN OFF. MAINTENANCE TROUBLESHOT AND REPLACED THE F/A'S SWITC H. OPS CHECK GOOD. THE AIRPLANE WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 2001072000031 20010720 00031 EA 2001 7 20 MASA01049 1 20010616 A 3350 20131A BATTERY CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7305V 7305 FLT 6003 - FAT-PHX - ALL EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY. OP CHECKS GO OD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001072000032 20010720 00032 EA 2001 7 20 MASA01050 1 20010614 A 3300 GE1415 LAMP CNDAIR CL600 CL6002B19 EA RT FUSELAGE BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17231 7231 FLT 6154 - PHX-SBA - PILOT REPORTED THE RIGHT FUSELAGE EXTERNAL NR 2 EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPL ACED THE LAMP. OPS CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2001072000033 20010720 00033 NM 2001 7 20 MASA01052 1 20010518 A 3300 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 455YV 455 FLT 6323 - PHX-GJT - PILOT REPORTED FORWARD LEFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. AIRCRAFT WAS FERRIED TO GJT. MA INTENANCE REMOVED AND REPLACED THE POWER SUPPLY. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 2001072000034 20010720 00034 EA 2001 7 20 MASA01060 1 20010703 A 3300 P4010021 POWER UNIT CNDAIR CL600 CL6002B19 EA FS 280 INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37228 7228 DURING ROUTINE MAINTENANCE, THE PILOT AND CO-PILOT EMERGENCY FLASHLIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERIES. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001072000035 20010720 00035 EA 2001 7 20 COMA0160484 1 20010716 A 2750 865D1007 MOTOR CNDAIR CL600 CL6002B19 EA MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 937CA 15593 2610 7044 FLAPS FAILED AT 0 DEGREES.REPLACED THE FLAP PDU. 2 L 7 2 4F RT A21EA 2001072000036 20010720 00036 EA 2001 7 20 COMA0160485 1 20010715 A 2720 CONNECTOR CNDAIR CL600 CL6002B19 EA LOOSE A COMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 01 807CA 7364 YAW DAMPENER OSCILLATIONS FOUND CONNECTION P169 LOOSE.TIGHTENED CONNECTOR AND SYSTEM FUNCTION NORMAL. 2 L 7 2 4F RT A21EA 2001072000037 20010720 00037 WP 2001 7 20 AT0100215 1 20010719 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP B5-28 INOPERATIVE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 801AT 47275 FOUND B5-28 FAILED TO OPERATE AFT ACCESSERY EMERGENCY LIGHTS. CORRECTIVE ACTION: REPLACED B5-28. IAW DC9 MM 33-50 2 L 7 2 4F A6WE 2001072000038 20010720 00038 WP 2001 7 20 AT0100216 1 20010720 A 3350 41B004ADD763 BATTERY PACK DOUG DC9 DC932 3022066 WP B5-26 INOPERATIVE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 805AT 47378 FOUND EMERGENCY LIGHTS AT ROWS 18 AND 22 FAILED TEST. CORRECTIVE ACTION: REPLACED BATTERIES IN BATTERY PACK B5-26. IAW DC9 MM 33-50 2 L 7 2 4F A6WE 2001072000039 20010720 00039 NM 2001 7 20 UPS01236369 1 20010702 A 5510 SKIN BOEING 727 72727C 138400J NM STAB STA 80 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 910UP 19117 INSPECTION TYPE:C CORROSION OF RH STAB SKIN UPPER SURFACE & RIVET PULLED @ STAB STA 80 APPX FWD OF REAR SPAR. ***CPCP** * REPAIR CARRIED OUT IAW SRM 55-10-3. 2 L 7 3 4F A3WE 2001072000040 20010720 00040 NM 2001 7 20 UPS01236373 1 20010702 A 5310 WEB BOEING 727 72727C 138400J NM BS 1183 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 910UP 19117 INSPECTION TYPE:C CORROSION ON CABIN FLOOR WEB FWD OF BS 1183 BLK OF BBL 12R ***CPCP*** WEB REPLACED IAW SRM 51-10-0 1 2 L 7 3 4F A3WE 2001072000041 20010720 00041 WP 2001 7 20 ZW0A0105401 1 20010719 A 2900 NAS16126 O-RING DOUG DC9 DC982 3022082 WP A ZW0A B EMER. DESCENT K FLUID LOSS DE DESCENT 1 CE 13 904TW 49156 ON FINAL APPROACH, LOST RIGHT HAND HYD SYSTEM DUE TO FLUID LOSS. FOUND RIGHT HAND THRUST REVERSER CONTROL VALVE PRESSUR E LINE FITTING HAD A FLAT TORN O-RING. REPLACED O-RING P/N NAS1612-6 DUE TO WEAR. LAST CHECK C 03/12/01 MCI ---CLOSED --- 2 L 7 2 4F A6WE 2001072000042 20010720 00042 NM 2001 7 20 ZW0A0105402 1 20010718 A 3350 20121 POWER SUPPLY BOEING 767 7673Q8 NM A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 634TW 28132 DURING MAINTENANCE AFT SECTION OF COACH EGRESS LIGHTS WERE FOUND INOP. IDENTIFIED POWER SUPPLY AS INOP. REPLACED EGRES S POWER SUPPLY P/N 2012-1.LAST CHECK C 10/25/00 LAX ---CLOSED--- 2 L 7 2 4F RT A1NM 2001072000043 20010720 00043 GL 2001 7 20 RAIA00107016 3 20010718 A 6110 B5JFR36C1103C PROPELLER GARRTT JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE MCAULY 5JFR36 B5JFR36C1103 GL LEFT ENGINE DAMAGED A RAIA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 03 565HK 6983 2022 75073 41082 75073 951242 7272-STL-LEFT PROPELLER TIPS DAMAGED DUE TO GROUND EQUIPMENT STRIKE. MAINTENANCE INSPECTED AND REPLACED LEFT PROPELLER, MAINTENANCE REPLACED LEFT ENGINE DUE TO PROPELLER STRIKE. 2 L 7 2 4T 4 T RT A41NM E18NE 6 C P15NE 2001072200001 20010722 00001 NM 2001 7 22 01FDEA00583 1 20010719 A 2780 651781822 ACTUATOR BOEING 727 72722 1384002 NM #5 SLAT INOPERATIVE A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 185FE 18871 01-243 AFT DEPART WHEN FLAPS WERE RETRACTED TO 2 DEG #5 SLAT W/N RETRACT. R&R ACTUATOR PER 27-81-032-4. LEAK OPS CK GOO D. 2 L 7 3 4F A3WE 2001081500123 20010815 00123 NM 2001 8 15 01FDEA00573 1 20010716 A 5312 DOUBLER DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 CENTER LG LT BULKHEAD DOUBLER BETWEEN BS 1360 - 1380 FOUND CRACKED. *S/D* REMOVED AND REPLACED DOUBLER PER SRM 51-31-0 1, 51-21-02 VOL 2. 2 L 7 3 4F RT A22WE 2001081500137 20010815 00137 NM 2001 8 15 01FDEA00586 1 20010716 A 5312 DOUBLER DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 CENTER LG RT BULKHEAD DOUBLER BETWEEN BS 1360 - 1380 FOUND CRACKED. *S/D* REMOVED AND REPLACED DOUBLER PER DWG AEA0526 . 2 L 7 3 4F RT A22WE 2001081500138 20010815 00138 NM 2001 8 15 01FDEA00587 1 20010715 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 CABIN CORROSION FOUND ON SEAT TRACK CAVITY AROUND BS 540 & X=-8. *S/D* REMOVED AND REPLACED PER SRM 53-70-00 FIG 1 VOL 1. 2 L 7 3 4F RT A22WE 2001081500140 20010815 00140 NM 2001 8 15 01FDEA00589 1 20010716 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 DAMAGED NR 3 SEAT TRACK BS 1059 MAIN CARGO COMPT. *S/D* REMOVED AND REPLACED PER SRM 53-70-00 FIG 1 VOL 1. 2 L 7 3 4F RT A22WE 2001081500141 20010815 00141 NM 2001 8 15 01FDEA00590 1 20010716 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 DAMAGED SEAT TRACK NR 8 BS 1361 TO 1401 8 IN AT MAIN CARGO DECK. *S/D* REMOVED AND REPLACED PER SRM 53-70-00 FIG 1 VOL 1. 2 L 7 3 4F RT A22WE 2001081500142 20010815 00142 NM 2001 8 15 01FDEA00591 1 20010716 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 NR 2 SEAT TRACK DAMAGED AT BS 1421 MAIN DECK COMPT. *S/D* SMOOTHED AND FOUND WITHIN LIMITS PER SRM 53-70-00 FIG 3. 2 L 7 3 4F RT A22WE 2001072300001 20010723 00001 EU 2001 7 23 C2XA01CL171 1 20010715 A 3260 D228830001 PROXIMITY SWITCH AEROSP ATR42 ATR42320 8680930 EU NOSE OUT OF ADJ A C2XA K NONE J WARNING INDICATION AP APPROACH 1 SW 27 14828 179 CLE FLT.#3076 THE CREW REPORTED SYSTEM #1 LANDING GEAR (NOSE) HAD UNSAFE INDICATION.MAINTENANCE ADJUSTED #1 SYSTEM NOS E LANDING GEAR PROXIMITY SWITCH. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001072300002 20010723 00002 SO 2001 7 23 C2XA01CL172 1 20010720 A 2611 14534610401 SWITCH EMB 145 EMB145LR SO COCKPIT DIRTY A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 13990 271 CLE FLT.#3680 THE CREW REPORTED BAGGAGE FIRE EXTINGUISHER WILL NOT TEST.MAINTENANCE CLEANED BAGGAGE FIRE EXTINGUISHER TEST BUTTON. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2001072300003 20010723 00003 WP 2001 7 23 MWEA011058 1 20010716 A 2920 AS66411LS666 PUMP DOUG DC9 DC932 3022066 WP ENGINE ACCESSORY INOPERATIVE A MWEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 31 205ME 47601 RIGHT ENGINE HYDRAULIC PUMP WOULD NOT PRODUCE OVER 1,500 PSI, RETURNED TO GATE. -- DEFERRED, REMOVED AND REPLACED PUMP . 2 L 7 2 4F A6WE 2001072300004 20010723 00004 NM 2001 7 23 2001F00119 1 20010515 A 3350 8821004 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY TRACK LIGHTS ON SEAT PALLETS 2-11 AND 4-7 INOPERATIVE. REMOVED AND REPL ACED THREE REMOTE ASSEMBLY BATTERIES AND TWO REMOTE ASSEMBLY RECEIVERS, THEN LIGHTS OPERATED NORMAL. REF ASAA0110264. (M) 2 L 7 2 4F A16WE 2001072300005 20010723 00005 NM 2001 7 23 2001F00120 1 20010612 A 2910 HYDRAULIC LINE BOEING 727 727231 1384079 NM NR 2 ENGINE CHAFED A MYWA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 808MA 21988 DURING CRUISE FLIGHT, LOST ALL 'A' HYDRAULIC SYSTEM FLUID. ACCOMPLISHED ABNORMAL CHECKLIST. DIVERTED TO INDIANAPOLIS. FOUND NR 2 ENGINE HYDRAULIC PUMP PRESSURE HOSE CHAFED AGAINST THE 13TH STAGE CSD EJECTOR DUCT. REPLACED DAMAGED HOSE P ER MM 29-10-5. SERVICED PER MM 12-4-23. LEAK CHECK ON RUNUP OK. (M) 2 L 7 3 4F A3WE 2001072300006 20010723 00006 EU 2001 7 23 2001F00121 1 20010612 A 5347 EPNE95300013023 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AT 499 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE LEFT OUTBOARD, LEFT F/A, AND RIGHT F/A SEAT TRACKS CORRODED. M AINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA2001171. (M) 2 H 7 2 4T RT A53EU 2001072300007 20010723 00007 EU 2001 7 23 2001F00122 1 20010612 A 5347 S536788001228 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AT 499 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE LEFT OUTBOARD, LEFT F/A, AND RIGHT F/A SEAT TRACKS CORRODED. M AINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA2001171. (M) 2 H 7 2 4T RT A53EU 2001072300008 20010723 00008 EU 2001 7 23 2001F00123 1 20010612 A 5315 S5367240725201 FLOORBEAM AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AT 499 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED FLOORBEAM 36, 38 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED FLOORBEAMS 36 AND 38 IAW SRM 53-00-00. MAINTENANCE REPAIRED FLOORBEAM 39 IAW SRM 53-00-00 FIGURE 435. AIRCRAFT WAS RE TURNED TO SERVICE. REF SIMA 20011712. (M) 2 H 7 2 4T RT A53EU 2001072300009 20010723 00009 EU 2001 7 23 2001F00124 1 20010612 A 5315 S5367240825902 FLOORBEAM AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AT 499 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED FLOORBEAM 36, 38 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED FLOORBEAMS 36 AND 38 IAW SRM 53-00-00. MAINTENANCE REPAIRED FLOORBEAM 39 IAW SRM 53-00-00 FIGURE 435. AIRCRAFT WAS RE TURNED TO SERVICE. REF SIMA20011712. (M) 2 H 7 2 4T RT A53EU 2001072300010 20010723 00010 EU 2001 7 23 2001F00125 1 20010620 A 5315 S5367240921802 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 426AT 426 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED FLOORBEAMS 36, 38, 39 AND 40 CORRODED BEYOND LIMITS. MAINTENANCE R EMOVED AND REPLACED FLOORBEAMS IAW ATR 72 SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REFSIMA200117108. (M) 2 H 7 2 4T RT A53EU 2001072300011 20010723 00011 EU 2001 7 23 2001F00126 1 20010616 A 2120 521581357002 CHECK VALVE AEROSP ATR42 ATR42300 8680920 EU CABIN PRESSURE DAMAGED A SIMA K NONE O OTHER CR CRUISE 1 SW 21 135MQ 135 FLT 5273 - MCO - DURING LEVEL FLIGHT AT FL180, THE CREW REPORTED A LOUD POP FOLLOWED BY A LOSS OF CABIN PRESSURE. MAINT ENANCE FOUND A CHECK VALVE DAMAGED. CHECK VALVE AND DUCT VALVE WAS INSTALLED IN WERE REMOVED AND REPLACED IAW ATR MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200116704. (M) 2 H 7 2 4T RT A53EU 2001072300012 20010723 00012 EU 2001 7 23 2001F00127 1 20010620 A 5315 S5367240725202 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 426AT 426 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED FLOORBEAMS 36, 38, 39 AND 40 CORRODED BEYOND LIMITS. MAINTENANCE R EMOVED AND REPLACED FLOORBEAMS IAW ATR 72 SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200117108. (M) 2 H 7 2 4T RT A53EU 2001072300013 20010723 00013 EU 2001 7 23 2001F00128 1 20010620 A 5315 S5367240825402 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 426AT 426 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED FLOORBEAMS 36, 38, 39 AND 40 CORRODED BEYOND LIMITS. MAINTENANCE R EMOVED AND REPLACED FLOORBEAMS IAW ATR 72 SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REFSIMA200117108. (M) 2 H 7 2 4T RT A53EU 2001072300014 20010723 00014 NM 2001 7 23 2001F00129 1 20010519 A 2612 FRF6E12535 CONNECTOR BOEING 727 72722C 138400F NM NR 3 ENGINE DAMAGED A RRXA O OTHER N FALSE WARNING CL CLIMB 1 CE 07 429EX 19100 NR 3 ENGINE FIRE LIGHT CAME ON DURING CLIMB-OUT, PERFORMED ENGINE FIRE IN FLIGHT PROCEDURE. REPAIRED SEVERAL WIRES TO F IRE TEST SWITCH. REMOVED AND REPLACED THE FIRE TEST SWITCH. REPAIRED CONNECTOR AT NR 3 ENGINE FIRE WALL. HIGH POWER E NGINE RUN OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 2001072300015 20010723 00015 NM 2001 7 23 2001F00130 1 20010518 A 2612 65249201 ACCESSORY UNIT BOEING 727 72722C 138400F NM E/E BAY FAULTY A RRXA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 429EX 19100 DURING CRUISE FLIGHT, NR 3 FIRE LIGHT ILLUMINATED AND BELL SOUNDED, FOLLOWED PROCEDURES. LEFT BOTTLE DISCHARGE LIGHT DI D NOT ILLUMINATE. FIRE HANDLE LIGHT DID NOT EXTINGUISH. INSPECTED ENGINE AND FOUND NO FIRE. REMOVED AND REPLACED FIRE DETECTION ACCY UNIT. PERFORMED TEST. GROUND TEST NORMAL. (M) 2 L 7 3 4F A3WE 2001072300016 20010723 00016 NM 2001 7 23 2001F00131 1 20010622 A 3610 652244143 DUCT BOEING 727 727225 1384077 NM NR 3 ENGINE BLOWN A RYNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 801EA 22432 NR 3 ENGINE FIRE WARNING LIGHT ILLUMINATED DURING CLIMB-OUT. REMOVED AND REPLACED BLOWN 13TH STAGE SADDLE DUCT. GROUND RUN OPERATIONAL CHECK GOOD. (M) 2 L 7 3 4F A3WE 2001072300017 20010723 00017 2001 7 23 2001F00132 4 20010528 A 3452 4061400905 TRANSPONDER BOEING 727 727259 138408J NM E/E BAY FAILED A FX7A A UNSCHED LANDING J O WARNING INDICATION OTHER TO TAKEOFF 1 SO 19 203AV 22474 TRANSPONDER FAIL LIGHT ILLUMINATED AFTER TAKEOFF, ATC WAS NOT RECEIVING TRANSPONDER SIGNAL. AIRCRAFT IS CONFIGURED WITH ONLY ONE TRANSPONDER AND RETURN FROM ARRIVAL DESTINATION WOULD NOT BE PERMISSIBLE. AIRCRAFT ADVISED TO RETURN TO DEPAR TURE STATION. AIRCRAFT SWAPPED WITH 266US AND FERRY FLIGHT CONTINUED MBJ. ATC TRANSPONDER TROUBLESHOT TO INOPERATIVE T RANSMITTER, FAIL LIGHT ILLUMINATED ON RT, REMOVED AND REPLACED TRANSMITTER, P/N 4061400-905 FROM STOCK ROOM. AIRCRAFT R ETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001072300018 20010723 00018 2001 7 23 2001F00133 4 20010530 A 3414 A4144910006 INDICATOR BOEING 727 727225 1384077 NM COCKPIT MALFUNCTIONED A MYWA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 806MA 22437 DURING TAKEOFF FIRST OFFICERS AIRSPEED INDICATOR REACHED 100 KNOTS AND STOPPED INCREASING ABOVE THAT. RETURNED TO MIAMI . REPLACED FIRST OFFICERS AIRSPEED/MACH INDICATOR. PITOT STATIC LOW LEVEL LEAK CHECK ACCOMPLISHED WITHIN LIMITS IAW MM 34-11-00. REMOVED BLOCKING TAPE. (M) 2 L 7 3 4F A3WE 2001072300019 20010723 00019 2001 7 23 MWEA011059 4 20010719 A 3440 MI585306401 TRANSCEIVER DOUG DC9 DC914 3022034 WP FWD ACCESSORY FAILED A MWEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 31 600ME 45725 RADAR SCREEN DISPLAYS "RT" AND SHOWS NO WEATHER. -- REMOVED AND REPLACED WEATHER RADAR TRANSCEIVER. 2 L 7 2 4F A6WE 2001072300020 20010723 00020 2001 7 23 MWEA011060 4 20010719 A 2215 2587788901 SERVO DOUG DC9 DC914 3022034 WP LWR FWD FUSELAGE INOPERATIVE A MWEA K NONE F FLT CONT AFFECTED TX TAXI/GRND HDL 1 GL 31 800ME 45842 WITH AUTOPILOT AND ELEVATOR SERVO OFF TRIM MOVES UNCOMMANDED NOSE UP AND NOSE DOWN. -- REPLACED ELEVATOR SERVO, OPERAT IONAL CHECK GOOD. 2 L 7 2 4F A6WE 2001072300021 20010723 00021 NM 2001 7 23 2001F00134 1 20010530 A 3411 LINE BOEING 727 727225 1384077 NM PITOT/STATIC SYS OBSTRUCTED A MYWA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 19 806MA 22437 DURING TAKEOFF ROLL, FIRST OFFICERS AIRSPEED INDICATOR READS 30 KNOTS DIFFERENT THAN CAPTAINS INDICATOR. ACCOMPLISHED R EJECTED TAKEOFF AT MIAMI. PERFORMED BRAKE COOLING INSPECTION. PERFORMED FOD CHECK ON PITOT LINES. FOUND DEBRIS, REMOV ED AND LEAK CHECKED. ALL SYSTEMS CHECK GOOD IAW MM 34-11-00. REMOVED BLOCKING TAPE. TEST FLIGHT ACCOMPLISHED ALL SYST EMS SATISFACTORY. (M) 2 L 7 3 4F A3WE 2001072300022 20010723 00022 NM 2001 7 23 2001F00135 1 20010625 A 2913 651782111 PUMP BOEING 727 727225 1384077 NM HYDRAULIC SYS DAMAGED A MYWA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 19 802MA 22433 SHORTLY AFTER GEAR RETRACTION LOST HYD SYSTEM 'A'. ACCOMPLISHED ABNORMAL PROCEDURE. RETURNED TO DFW. REMOVED AND REPL ACED NR 1 AND NR 2 ENGINE DRIVEN HYDRAULIC PUMP. RUN AND AND LEAK CHECK. REMOVED AND REPLACED NR 1 AND NR 2 ENGINE HYD RAULIC FILTER, RUN OPS AND CHECK IAW 29-11-33 ENGINE PUMP, IAW 29-11-62 FILTER. REPLACED DAMAGED 'A' SYSTEM PRESSURE PA CKAGE IAW 29-11-61, LEAK CHECK GOOD. REMOVED AND REPLACED 'A' SYSTEM RETURN TO FILTER IAW 29-11-102. LEAK CHECK GOOD. SERVICED HYD SYSTEM IAW 29-11-101. MANUAL EXT RETURNED TO FLT STATUS IAW 32-34-0 PAGE 3. (M) 2 L 7 3 4F A3WE 2001072300023 20010723 00023 NM 2001 7 23 ASAA0140061 1 20010502 A 3350 30043213 LIGHT BOEING 737 7374Q8 NM L2 DOOR INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 763AS 25100 PDX - DURING LINE CHECK,FOUND EMERGENCY EGRESS LIGHT AT L2 DOOR INOPERATIVE. RESTORED TENSIONING TO POSITIVE CONTACT AN D RELAMPED. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001072300024 20010723 00024 NM 2001 7 23 ASAA0140062 1 20010502 A 3397 8100022607 WIRE BOEING 737 7374Q8 NM CABIN DISCONNECTED A K NONE L NO TEST IN INSP/MAINT 1 NM 01 765AS 25102 GEG - BEFORE FLIGHT, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE AT ROW 21. RECONNECTED LOOSE WIRE, OPS CHECK GOOD . (M) 2 L 7 2 4F RT A16WE 2001072300025 20010723 00025 NM 2001 7 23 ASAA0140076 1 20010518 A 3397 8100022607 WIRE BOEING 737 7374Q8 NM CABIN DISCONNECTED A K NONE L NO TEST IN INSP/MAINT 1 NM 01 769AS 25103 PDX - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROWS 13-16. RECONNECTED WIRES AT ROWS 16. F LOOR TRACK LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 2001072300026 20010723 00026 NM 2001 7 23 ASAA0170003 1 20010513 A 3397 8100022608 WIRE BOEING 747 747251B 1384892 NM CABIN DISCONNECTED A K NONE L NO TEST IN INSP/MAINT 1 NM 01 612US 20357 SEA - DURING LINE MAINTENANCE, THE EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN ROWS 12 THROUGH 16. RE-CONNEC TED THE TRACK LIGHT WIRES AT ROW 16. THE LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 4 4F A20WE 2002010800162 20020108 00162 2002 1 8 ASAA0180144 4 20010418 A 2565 D29982107 WIRE HARNESS DOUG DC9 DC982 3022082 WP EVAC SLIDE FAILED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 937AS 27230 4456 49364 OAK - DURING C-CHECK, L1 DOOR EMERGENCY SLIDE HARNESS FAILED THE AMPERAGE CHECK. REPLACED L1 DOOR EMERGENCY SLIDE PER A SA TASK CARD 24425006. HARNESS CHECKED OK. (M) 2 L 7 2 4F A6WE 2001072300027 20010723 00027 WP 2001 7 23 ASAA0180156 1 20010503 A 3350 0105606003 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE O OTHER CR CRUISE 1 NM 01 947AS 53020 FLT 237 - DURING FLIGHT, FLIGHT ATTENDANT ACCIDENTALLY TURNED ON EMERGENCY LIGHTS AND DISCOVERED THAT TRACK LIGHTS IN TH E 1ST CLASS CABIN TO BE INOPERATIVE. RECONNECTED LOOSE TRACK LIGHT MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. ( M) 2 L 7 2 4F RT A6WE 2001072300028 20010723 00028 WP 2001 7 23 ASAA0180167 1 20010514 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 PDX - DURING PRE-FLIGHT, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE FROM ROW 6 FORWARD. RESEATED TRACK LIGHTING MOD ULES. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001072300029 20010723 00029 WP 2001 7 23 ASAA0180168 1 20010515 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 PDX - DURING SERVICE CHECK, FOUND SEVERAL EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN 1ST CLASS CABIN ON RIGHT SIDE. RE SEATED TRACK LIGHTING MODULES. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001072300030 20010723 00030 WP 2001 7 23 ASAA0180169 1 20010516 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 ANC - DURING LINE CHECK, FOUND SOME EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE THROUGHOUT CABIN. RESEATED TRACK LIGHTING MODULES. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001072300031 20010723 00031 2001 7 23 ASAA0180171 4 20010516 A 2565 D29982107 HARNESS DOUG DC9 DC982 3022082 WP L1 DOOR FAILED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 OAK - DURING C-CHECK, FOUND L1 DOOR EMERGENCY SLIDE HARNESS FAILED VOLTAGE CHECK. REPLACED L1 DOOR EMERGENCY SLIDE WITH SERVICEABLE SLIDE. (M) 2 L 7 2 4F A6WE 2001072300032 20010723 00032 WP 2001 7 23 ASAA0180180 1 20010524 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 LAX - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS IN 1ST CLASS CABIN WERE DETERMINED TO BE INOPERATIVE. RESEAT ED LIGHT MODULES AND COVER. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001072300033 20010723 00033 EA 2001 7 23 MASA01048 1 20010602 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 07 47239 7239 FLT 6522 - IN CMH, THE PASSENGER DOOR EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE. EXIT SIGN OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001072300034 20010723 00034 EA 2001 7 23 MASA01055 1 20010622 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 EA EXTERIOR INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 47239 7239 DURING OVERNIGHT MAINTENANCE DISCOVERED THE LEFT MIDDLE AFT EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE LIGHT. OPS CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001072300035 20010723 00035 EA 2001 7 23 MASA01056 1 20010623 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 EA CABIN DIRTY A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 47202 7202 DURING PREFLIGHT, THE PILOT REPORTED SEVERAL EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE. MAINTENANCE CLEANED THE CONNECTO RS ON THE TRACKS. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001072300036 20010723 00036 EA 2001 7 23 COMA0160486 1 20010718 A 2750 7455001 LEVER CNDAIR CL600 CL6002B19 EA INTERMITTENT A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 420CA 936 7451 FLAPS FAIL MESSAGE.COULD NOT DUPLICATE. REPLACED FLAP SELECTOR AS MOST PROBABLE CAUSE. 2 L 7 2 4F RT A21EA 2001072300037 20010723 00037 EU 2001 7 23 AWXA0001853 1 20010612 A 3310 E042901 LIGHT AIRBUS 320 A320232 3930326 EU COCKPIT BLOWN A AWXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 656AW 1079 STL - UNSCHEDULED LANDING - EMERGENCY DECLARED - 6/7/01 - FLT 116 - ABOUT 1 HR INTO FLIGHT FROM CMH TO LAS AT FL 350, UP ON TURNING THE DOME LIGHT ON A BRIGHT FLASH AND A LOUD POP IN THE AREA OF TOP C/B PANEL; THE DOME LIGHT WENT OUT; CHECKE D C/B'S, NONE POPPED. CREW SMELLED ELEC SMOKE & FUMES; DONNED OXYGEN MASKS, DECLARED EMERGENCY, PREPARED CABIN & LANDED AT STL; AFTER CLEARING THE RUNWAY CHECKED FOR FUMES, NONE PRESENT, TERMINATED EMERGENCY & TAXIED TO THE GATE. STL MX F OUND THE FIRST OFFICER'S DOME LIGHT BULB BLOWN; RELAMPED AND FUNCTIONALLY CHECKED NORMAL. VISUALLY INSPECTED WIRING BEH IND C/B PANELS 121VU & 122VU, NO DISCREPANCIES FOUND; THE A/C RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2001072300038 20010723 00038 EA 2001 7 23 COMA0160488 1 20010718 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 938CA 5923 7046 FLAPS FAILED AT 28 DEGREES.REPLACED THE LEFT HAND BPSU. 2 L 7 2 4F RT A21EA 2001072300039 20010723 00039 EU 2001 7 23 AWXA0001854 1 20010613 A 2910 S43401190 PILOT VALVE AIRBUS 320 A320231 3930325 EU HYDRAULIC SYS LEAKING A AWXA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CR CRUISE 1 WP 28 640AW 448 PHX - AIR TURNBACK - 6/5/01 - FLT 253 - EN ROUTE TO PHL ECAM MSG DISPLAYED HYD YELLOW SYS LOW LEVEL; YELLOW HYD QUANTITY INDICATED IN THE AMBER BAND; CREW COMPLIED W/ THE ECAM ACTIONS & RETURNED TO PHX MAKING AN UNEVENTFUL LANDING. MX INSP ECTED THE A/C AND FOUND THE YELLOW HYD SYS LEAK MEASUREMENT VALVE, PILOT VALVE LEAKING; THE PILOT VALVE WAS REPLACED, TH E YELLOW SYS WAS SERVICED AND LEAK CHECKS AND FUNCTIONAL CHECKS WERE GOOD IAW AMM 29-19-51-401. 2 L 7 2 4F RT A28NM 2001072300040 20010723 00040 EA 2001 7 23 COMA0160487 1 20010718 A 2750 852D10011 ACTUATOR CNDAIR CL600 CL6002B19 EA BINDING A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 812CA 60 60 7381 FLAPS FAILED AT 43 DEGREES.REPLACED THE RIGHT HAND #1 AND #2 FLAP ACTUATORS. 2 L 7 2 4F RT A21EA 2001072300041 20010723 00041 NM 2001 7 23 AWXA0001855 1 20010613 A 5270 SWITCH BOEING 737 737301 1384611 NM ENTRY DOOR OUT OF ADJ A AWXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 28 326AW 23258 DEN - ABORTED TAKEOFF - 6/9/01 - FLT 334 - ABORTED TAKEOFF AT APPROX 80 KTS DUE TO AFT ENTRY DOOR WARNING LIGHT CAME ON AND EXTINGUISHED TWICE; BRAKE COOLING COMPLIED. IN DEN MX INSPECTED THE DOOR AND FOUND IT CLOSED AND LOCKED NORMALLY; D ETERMINED TO BE AN INDICATION PROBLEM. INDICATION WAS PLACED ON MEL 52-03 COND 1; LATER THAT SAME DAY IN PHX MX ADJUSTE D THE AFT ENTRY DOOR WARNING SWITCH ACTUATOR TO SWITCH. OPERATIONAL CHECKS WERE GOOD AND NO FURTHER DISCREPANCIES HAVE BEEN REPORTED. 2 L 7 2 4F RT A16WE 2001082200216 20010822 00216 EA 2001 8 22 COMA0160489 1 20010718 A 2163 01649801 SENSOR CNDAIR CL600 CL6002B19 EA CABIN TEMP MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 938CA 7046 DISPLAY COOL CAUTION MESSAGE. REPLACED THE LOW AIR FLOW SENSOR. 2 L 7 2 4F RT A21EA 2001072300042 20010723 00042 EA 2001 7 23 COMA0160490 1 20010718 A 2750 852D10011 ACTUATOR CNDAIR CL600 CL6002B19 EA BINDING A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 812CA 2597 7381 FLAPS FAILED AT 43 DEGREES.REPLACED THE RIGHT HAND #1 AND #2 FLAP ACTUATORS. 2 L 7 2 4F RT A21EA 2001072300043 20010723 00043 NE 2001 7 23 AWXA0001856 2 20010614 A 7532 6713D070000AMDTA BLEED VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE FLUCTUATES A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 642AW 4629 1896 584 PHX - AIR TURNBACK - 6/10/01 - FLT 234 - DURING LEVEL OFF AT FL 370, NR 2 BLEED FAULTED W/ ECAM MSG; PER THE FCOM CREW T URNED OFF BLEED SWITCH AND DUE TO ICING CONDITIONS EN ROUTE TO DTW, THE A/C RETURNED TO PHX; IN PHX THE NR 2 BLEED AIR S YS WAS PLACED ON MEL 36-11-01 AND ROUTED ON A FLIGHT THAT DIDN'T REQUIRE ITS USE; PAX WERE ACCOMMODATED ON ANOTHER A/C & THE FLIGHT CONTINUED TO DTW. MX TROUBLESHOT AND FOUND BLEED PRESSURE WOULD FLUCTUATE WHEN POWER WAS PULLED BACK; NR 2 HIGH PRESSURE BLEED VALVE WAS REPLACED AND FUNCTIONAL CHECKS NORMAL; MEL CLEARED. 2 L 7 2 4F 4 F RT A28NM E40NE 2001072300044 20010723 00044 WP 2001 7 23 MWEA011066 1 20010723 A 5230 3926046503 FITTING DOUG DC9 DC932 3022066 WP FWD CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 CRACK INDICATION ON OUT DOOR PAN UPPER SIDE OF #1 AFT DOOR STOP OF FORWARD CARGO DOOR. -- STOP DRILLED CRACK AND FABRI CATED DOUBLER, LOCATED, DRILLED AND DEBURRED NEW STOP FITTING, INSTALLED STOP FITTING AND DOUBLER. 2 L 7 2 4F A6WE 2001072300045 20010723 00045 NM 2001 7 23 AWXA0001878 1 20010618 A 5315 6546810 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 24634 BS 967 RBL 4 TO RBL 18 FLOORBEAM UPPER CHORD HAS CORROSION IN SEVERAL AREAS. REMOVED AND REPLACED FLOORBEAM UPPER CHORD IAW B737-300 SRM 51-40-05 PG 6-10. 2 L 7 2 4F RT A16WE 2001072300046 20010723 00046 NM 2001 7 23 AWXA0001879 1 20010618 A 5315 6546810 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 24634 MAIN CABIN BS 967 LBL 27 TO LBL 49 FLOORBEAM UPPER CHORD HAS CORROSION UPPER AND LOWER SURFACE. REMOVED AND REPLACED FL OORBEAM UPPER CHORD IAW B737 SRM 51-40-05 PG 6-10. 2 L 7 2 4F RT A16WE 2001072300047 20010723 00047 NM 2001 7 23 AWXA0001881 1 20010617 A 5315 65C33950 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 24634 MAIN CABIN BS 986.5 BL 0 TO RBL 45 FLOORBEAM HAS SEVERAL AREAS OF CORROSION. CORROSION OUT OF LIMITS UPPER CHORD REPLAC ED IAW B737 SRM 53-00-51 PG 207-211. 2 L 7 2 4F RT A16WE 2001072300048 20010723 00048 NM 2001 7 23 AWXA0001882 1 20010617 A 5315 6546810 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 24634 MAIN CABIN, BS 947, LBL 24 TO RBL 8 FLOORBEAM UPPER CHORD, CORROSION ON UPPER AND LOWER SURFACE. CORROSION OUT OF LIMIT S. REMOVED AND REPLACED UPPER T-CHORD IAW B737 SRM 53-00-51 PG 208-211 FIG 202. 2 L 7 2 4F RT A16WE 2001072300049 20010723 00049 EU 2001 7 23 AWXA0001883 1 20010619 A 5270 WARNING SYSTEM AIRBUS 320 A320231 3930325 EU COCKPIT FALSE ACTIVATION A AWXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 646AW 271 PHX- AIR TURNBACK - FLT 752- AFTER TAKEOFF, ECAM MESSAGE AFT CARGO DOOR APPEARED AND THE AIRCRAFT WAS RETURNED TO PHX. IN PHX MAINTENANCE INSPECTED THE AFT CARGO DOOR TO ENSURE IT WAS FULLY CLOSED AND LOCKED, WHICH IT WAS. THE AFT CARGO D OOR INDICATION WAS PLACED ON MEL 52-70-01 COND .7 AND PLACARDING PROCEDURES COMPLIED WITH. AWAITING FURTHER TROUBLESHOO TING. 2 L 7 2 4F RT A28NM 2001072300050 20010723 00050 NM 2001 7 23 AWXA0001884 1 20010620 A 5315 65C33950 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 24634 MAIN CABIN BS 986.5 BL 0 TO LBL 20, FLOORBEAM HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED UPPER T-CHORD IAW B7 37-300 SRM 53-00-51 PG 207-211. 2 L 7 2 4F RT A16WE 2001072300055 20010723 00055 NM 2001 7 23 AWXA0001887 1 20010530 A 7722 FS5J10321 NUT BOEING 737 73733A 1384673 NM EGT SYS LOOSE A AWXA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 165AW 23626 72165 IAH-AIR TURNBACK- INFLIGHT SHUTDOWN - FLT 831- DURING CLIMB THE NR 1 ENGINE EGT INDICATOR RED LIGHT ILLUMINATED. THE DI GITAL AND ANALOG EGT INDICATIONS SHOWED EXCESSIVE EGT. THE INDICATIONS WERE ERRATIC AND VARIED BETWEEN 700 AND OFF SCAL E, OVER 1000. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT RETURNED TO IAH. IN IAH MAINTENANCE TROUBLESHOT AND FOUND THE U PPER WIRE LOOSE ON THE INTERFACE TERMINAL. THE NUT ON THE TERMINAL WAS TIGHTENED. MAINTENANCE SWAPPED THE EGT INDICATO RS FROM SIDE TO SIDE AND RAN THE ENGINES FOR 10 MIN AT POWER AND ALL ENGINE PARAMETERS WERE NORMAL. THE INDICATORS WERE RETURNED TO THEIR ORIGINAL POSITIONS, FUNCTIONALLY CHECKED GOOD AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2001072300056 20010723 00056 NM 2001 7 23 AWXA0001888 1 20010620 A 3412 102AH2AG PROBE BOEING 737 7373G7 1384595 NM FUSELAGE INOPERATIVE A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 309AW 32808 13838 24711 PHX AIR TURNBACK- FLT 598- AFTER TAKEOFF FROM PHX EN ROUTE TO MCI THE TOTAL AIR TEMP PROBE HEAT WENT INOPERATIVE. THE A IRCRAFT WAS RETURNED TO PHX DUE TO FORECAST ICING CONDITIONS EN ROUTE TO MCI. IN PHX MAINTENANCE TROUBLESHOT THE PROBLE M AND REPLACED THE TOTAL AIR TEMP PROBE. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2001072300057 20010723 00057 NM 2001 7 23 AWXA0001889 1 20010625 A 5753 6546434302 FLAP BOEING 737 7373G7 1384595 NM RT WING DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 24634 RT INBOARD AFT FLAP HAS AREA OF DISBOND, LOWER SURFACE OUTBOARD END. CUT OUT DISBONDED LOWER SKIN AND HONEYCOMB CORE, E TCHED, CLEANED, TREATED, APPLIED ADHESIVE PRIMER TO REPAIR AREA, FILLER, DOUBLER, AND HONEYCOMB CORE, BONDED REPAIR, IAW AWA ER 03-5751-01171-022. 2 L 7 2 4F RT A16WE 2001072300058 20010723 00058 NM 2001 7 23 AWXA0001891 1 20010626 A 5315 65468112 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MAIN DECK FLOORBEAM UPPER CHORD CORRODED BS 947 RBL 8.0. REPAIRED BS 947 FLOORBEAM IAW B737 SRM 53-00-51 FIG 202. 2 L 7 2 4F RT A16WE 2001072300059 20010723 00059 NM 2001 7 23 AWXA0001892 1 20010626 A 5311 6516300302 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 24634 DURING C-CHECK FOUND CRACK CENTER OF RADIUS WL 207 BS 178 CHORD, RBL 24. REMOVED AND REPLACED CRACKED CHORD RT SIDE BS 178 BULKHEAD IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001072300060 20010723 00060 NM 2001 7 23 AWXA0001893 1 20010626 A 5311 6516300301 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 24634 DURING C CHECK INSPECTION FOUND CRACK CENTER OF RADIUS WL 207 BS 178 BULKHEAD CHORD LBL 24. REMOVED AND REPLACED CRACKE D CHORD LT SIDE BS 178 BULKHEAD IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001072300061 20010723 00061 NM 2001 7 23 AWXA0001894 1 20010626 A 5312 65C375903 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 24634 DURING C-CHECK INSPECTION FOUND WEB CRACK EMANATING FROM BENEATH STRAP BS BULKHEAD WEB, LBL 4.8, WL 201. REPAIRED CRACK ED AREA ON BS 178 WEB, LBL 4.8, WL 201 IAW B737-300 SRM 51-40-02, 51-20-01, 53-10-08 AND AWA ER 03-5313-01159-J51. 2 L 7 2 4F RT A16WE 2001072300062 20010723 00062 NM 2001 7 23 AWXA0001895 1 20010626 A 5312 65C375903 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 24634 DURING C-CHECK INSPECTION FOUND AFT SIDE BS 178 BULKHEAD BELOW FLOOR WEB CRACKED RBL .6 TO LBL .6, WL 187. REPAIRED CRA CKED AREA BS 178 WEB, RBL .6 TO LBL .6, WL 187 IAW B737-300 SRM 51-40-02, 51-20-01, 53-10-08 FIG 24. 2 L 7 2 4F RT A16WE 2001072300063 20010723 00063 NM 2001 7 23 AWXA0001896 1 20010626 A 5312 65C375903 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 24634 DURING C-CHECK INSPECTION FOUND CRACK BS 178 BULKHEAD WEB, LBL 6.8, WL 212.7 TO 212.9. REPAIRED CRACKED AREA ON BS 178 WEB, LBL 6.8, WL 212.7 TO 212.9 IAW B737-300 SRM 51-40-02, 51-20-01, 53-10-08 FIG 211. 2 L 7 2 4F RT A16WE 2001072300064 20010723 00064 NM 2001 7 23 AWXA0001897 1 20010626 A 5312 65C375903 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 24634 DURING C-CHECK INSPECTION FOUND CRACK EMANATING FROM BENEATH STRAP BS 178 BULKHEAD WEB, RBL 6.8 FROM WL 212.4 TO 212.7. REPAIRED CRACKED AREA ON BS 178 WEB, RBL 6.8, WL 212.4 TO 212.7 IAW B737-300 SRM 51-40-02, 51-20-01, 53-10-08 FIG 211. 2 L 7 2 4F RT A16WE 2001072300065 20010723 00065 NM 2001 7 23 AWXA0001898 1 20010626 A 5312 65C375903 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 24634 DURING C-CHECK INSPECTION FOUND WEB CRACK EMANATING FROM BENEATH STRAP, BS 178, BULKHEAD, RBL 4.8, WL 201. REPAIRED CRA CKED AREA ON BS 178, BULKHEAD WEB, RBL 4.8, WL 201, IAW B737-300 SRM 51-40-02, 51-20-01 AND 53-10-08 FIG 211. 2 L 7 2 4F RT A16WE 2001072300066 20010723 00066 NM 2001 7 23 AWXA0001900 1 20010626 A 5320 693535214 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 24634 DURING C-CHECK INSPECTION FOUND MAIN CABIN, BS-727A STRINGER 1L, STRINGER TIE CLIP CRACKED. REMOVED AND REPLACED STRING ER TIE CLIP AT BS 727A, STRINGER 1L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001072300067 20010723 00067 NM 2001 7 23 AWXA0001901 1 20010626 A 5313 6545767 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 24634 STRINGER R:16 CRACKED JUST FWD OF L/E WING LIGHT RECEPTACLE BS 500C. REMOVED DAMAGED AREA FROM STR R-16 BS 500C. FORME D AND INSTALLED LL CHANNEL REPAIR AT STRINGER R-16 BS 500C ALL IAW AWA ER 03-5312-01094DD1 AND 737-300 SRM 51-40-02 PGS 3, 4, 10, 11 AND S/B 737-53-1145. 2 L 7 2 4F RT A16WE 2001072300068 20010723 00068 NM 2001 7 23 AWXA0001902 1 20010626 A 5315 65C33950 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 24634 MAIN CABIN BS 986.5 RBL 0 TO LBL 20, FLOORBEAM HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED UPPER T-CHORD IAW B 737-300 SRM 53-00-51 PG 207-211. 2 L 7 2 4F RT A16WE 2001072300069 20010723 00069 NM 2001 7 23 AWXA0001907 1 20010624 A 2530 800132000A OVEN BOEING 757 7572S7 1384962 NM GALLEY SMOKE A AWXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 905AW 23567 MCO- SMOKE IN FWD GALLEY - FLT 561 - EN ROUTE FROM PHX TO MCO THE OUTBOARD OVEN IN GALLEY GIB STARTED SMOKING. THE FLIG HT ATTENDANT TURNED THE OVEN OFF AND PULLED THE CIRCUIT BREAKER. REMOVED THE GALLEY HALON FIRE EXTINGUISHER AND STOOD B Y TO ENSURE THERE WAS NO FIRE. THE FIRE EXTINGUISHER WAS NOT USED HOWEVER CREW DID BREAK THE TAMPER PROOF SEAL. AFTER T URNING THE OVEN OFF AND PULLING THE C/B THE OVEN QUIT SMOKING. IN MCO MAINTENANCE INSPECTED THE GALLEY AND DETERMINED T HE OTHER OVENS IN OPERATIONAL STATUS. THE OUTBOARD OVEN WAS PLACED ON MEL 25-20-01, COND 1. THE TAMPER PROOF SEAL WAS REPLACED ON THE FIRE EXTINGUISHER. IN PHX THE NEXT DAY MAINTENANCE REMOVED THE OVEN AND FURTHER INSPECTED. 2 L 7 2 4F RT A2NM 2001072300070 20010723 00070 NM 2001 7 23 AWXA0001910 1 20010701 A 5330 196N3730 SKIN BOEING 757 757225 1384959 NM FUSELAGE DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 907AW 22691 DENT IN AIRCRAFT SKIN AFT OF L-4 DOOR STA 1720 BETWEEN STRINGERS 13L & 14L. CUT OUT DAMAGE 1.5 X 2.2 AREA OF SKIN, FABB ED AND INSTALLED INTERNAL DOUBLER PER 53-00-01, NDT NO CRACKS NOTED PER NTM 51-00-19. 2 L 7 2 4F RT A2NM 2001072300071 20010723 00071 NM 2001 7 23 AWXA0001916 1 20010701 A 5315 65468112 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MAIN DECK FLOORBEAM CORRODED UPPER CHORD BOTH SIDES BS 986.5 RBL 7 TO RBL 41. REPAIRED BS 986.5 FLOORBEAM UPPER CHORD I AW B737 SRM 53-00-51 FIG 202. 2 L 7 2 4F RT A16WE 2001072300072 20010723 00072 NM 2001 7 23 AWXA0001917 1 20010701 A 5315 65468112 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MAIN DECK FLOORBEAM CORRODED UPPER CHORD BOTH SIDES BS 986.5 LBL 21 TO LBL 45. REPAIRED BS 986.5 FLOORBEAM UPPER CHORD IAW B737 SRM 53-00-51 FIG 202. 2 L 7 2 4F RT A16WE 2001072300073 20010723 00073 NM 2001 7 23 AWXA0001918 1 20010702 A 5230 657952334 SKIN BOEING 737 7373G7 1384595 NM CARGO DOOR GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 DURING C-CHECK INSPECTION FOUND AFT CARGO DOOR INNER SKIN HAS HOLE GOUGED THOUGH SKIN IN FORWARD AREA. REPAIRED CARGO D OOR INNER SKIN IAW B737-300 SRM 51-70-13. 2 L 7 2 4F RT A16WE 2001072300074 20010723 00074 NM 2001 7 23 AWXA0001919 1 20010702 A 5311 6516300301 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 CRACK IN CENTER OF RADIUS BS 178 BULKHEAD CHORD WL 207 LBL 25. REMOVED AND REPLACED CHORD IAW AWA ER 03-5311-01169-DDZ. 2 L 7 2 4F RT A16WE 2001072300075 20010723 00075 NM 2001 7 23 AWXA0001921 1 20010705 A 7720 WARNING LIGHT BOEING 737 737317 138447P NM COCKPIT FALSE INDICATION A AWXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 28 336AW 23707 720754 PHX/ ABORTED TAKEOFF- FLT 271 - ON TAKEOFF ROLL, OVER 70KTS, THE NR 1, ENGINE OVER TEMP LIGHT ILLUMINATED AND EGT WAS IN DICATING APPROXIMATELY 920 DEGREES AND THE TAKEOFF WAS ABORTED. THE AIRCRAFT WAS RETURNED TO THE GATE. MAINTENANCE CHE CKED THE AMM FOR LIMITS AND FOUND NO ACTION WAS REQUIRED. CHECK THE INLET AND EXHAUST AREAS FOR CONDITION PERFORMED AND OPERATIONAL CHECK WHICH WAS GOOD AND RETURNED THE AIRCRAFT TO SERVICE REF AMM 72-00-00 PG 628A & 628B FIG 611 SHEET 1. NO FURTHER DISCREPANCIES HAVE BEEN REPORTED, NO HISTORY IN THE LAST 30 DAYS. 2 L 7 2 4F RT A16WE 2001072300076 20010723 00076 EU 2001 7 23 C2XA01IA297 1 20010713 A 3350 AD3127 BATTERY AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14815 104 IAH- DURING PREFLIGHT INSPECTION THE CREW NOTED SEVERAL EMERGENCY LIGHTS DID NOT ILLUMINATE. IAH- MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT BATTERY, PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM,NO DEF ECTS NOTED,AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001072300077 20010723 00077 EU 2001 7 23 C2XA01IA299 1 20010722 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14815 104 IAH - DURING MAINTENANCE INSPECTION, THE FORWARD LOWER EMERGENCY EXIT LIGHTS ON THE LEFT HAND AND RIGHT HAND LOWER CENTE R PANEL AND THE #1 CEILING PANEL WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY L IGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001072300078 20010723 00078 NM 2001 7 23 AWXA0001927 1 20010705 A 5330 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 311AW 24712 UPPER FUSELAGE SKIN DENTED AT B/S 360 BETWEEN STR 6R & STR 7R. REPAIRED DAMAGE TO UPPER FUSELAGE SKIN B/S 360 PER ER 03 -5331-01179-JL1. 2 L 7 2 4F RT A16WE 2001072300079 20010723 00079 NM 2001 7 23 AWXA0001931 1 20010705 A 5532 SKIN BOEING 737 7373G7 1384595 NM VERTICAL STAB DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 311AW 24712 VERT STAB L/E STA 137 DENT FOUND OUT OF LIMITS PER SRM 55-30-01. CUT OUT DAMAGED AREA HFEC NO CRACK NOTED CAL 0692, FAB RICATED DOUBLER FROM .063 2024T3 PO X95024189 AND FILLER FROM 2024T3 .040 PO X95025244 TREATED AND PRIMED. INSTALLED DO UBLER AND FILLER PER SRM 55-3001. 2 L 7 2 4F RT A16WE 2001072300080 20010723 00080 NM 2001 7 23 AWXA0001932 1 20010705 A 5312 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 23219 SIX CRACKS ON RADOME BULKHEAD CENTER OF WEB BS 178 AT THE FOLLOWING LOCATIONS WL 212 LBL 4,5 WL 200 LBL 5 WL 200 LBL 7.0 WL 198 LBL 7.0 WL 200 RBL 5.0 WL 200 RBL 7.0. REPAIRED CRACKS ON RADOME BULKHEAD CENTER WEB STA 178 PER SRM 53-10-08. 2 L 7 2 4F RT A16WE 2001072300081 20010723 00081 NM 2001 7 23 AWXA0001936 1 20010705 A 5320 651758371 STIFFENER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 23219 VERTICAL STIFFENER CRACKED BS 178 LBL 5.7 WL 185. REPAIRED PER SRM 53-10-08 FIG 205. 2 L 7 2 4F RT A16WE 2001072300082 20010723 00082 NM 2001 7 23 AWXA0001939 1 20010705 A 5330 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 23219 FUSELAGE SKIN DENT WITH LIGHTNING STRIKE AT BS 500A STR 20R TO 21R. FOUND DENT TO BE OUT OF LIMITS PER SRM 53-00-01 FIG 219, CAL 2370. REPAIRED DENT PER SRM 53-00-01 FIG 205. 2 L 7 2 4F RT A16WE 2001072300083 20010723 00083 NM 2001 7 23 AWXA0001940 1 20010705 A 5312 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 23219 CORROSION AT AFT PRESSURE BULKHEAD B/S 1016 6:00 POSITION. REPAIRED AFT PRESSURE BULKHEAD AT B/S 1016 6:00 POSITION PER ER 03-5383-01141-DD2. 2 L 7 2 4F RT A16WE 2001072300084 20010723 00084 NM 2001 7 23 AWXA0001941 1 20010705 A 5315 654680977 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 23219 FLOORBEAM STA 947 LBL 60 RBL 60 HAS CORROSION ON TOP CAP. REPAIRED TOP CAP LBL 60 TO RBL 60 PER AWA ER 03-5365-01179 DD 2. 2 L 7 2 4F RT A16WE 2001072300085 20010723 00085 NM 2001 7 23 AWXA0001942 1 20010705 A 5311 65163000301 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 23219 LT SIDE CHORD CRACKED STA 178 WL 207. REMOVED AND REPLACED SIDE CHORD. 2 L 7 2 4F RT A16WE 2001072300086 20010723 00086 NM 2001 7 23 AWXA0001943 1 20010705 A 5315 BAC1506210 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 23219 FLOORBEAM T-CAP HAS CORROSION AT STA 986 I/B OF R-2 DOOR. REMOVED AND REPLACED WITH NEW T-CAP REPAIR STA 986 LBL 28 TO RBL 50 PER EA 03-5310-01179-SS24. 2 L 7 2 4F RT A16WE 2001072300091 20010723 00091 NM 2001 7 23 AWXA0001945 1 20010709 A 5312 65163007 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 304AW 24011 WEB CRACKS AT STA 178 LBL 5.7. REMOVED FASTENERS PER SRM 51-40-2 AT REPAIR AREA. REPAIRED CRACKS PER SRM 53-10-08 FIG 209. NDT CHECKED CRACKS CONTAINMENT. FABRICATED REPAIR PARTS PER SRM 53-10-08 FIG 209 SH-3. PROTECTIVE TREATMENT FOR REPAIR PARTS PER SRM 51-20-01 FR PRIMED REPAIR PARTS PER SOPM 20-41-02. INSTALLED REPAIR PARTS PER SRM 53-10-08 FIG 209 . PAINTED AREA WHITE PER SRM 51-21-99. 2 L 7 2 4F RT A16WE 2001072300092 20010723 00092 NM 2001 7 23 AWXA0001947 1 20010709 A 5311 651630086 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 304AW 24011 FUSELAGE LT SIDE CHORD AT WL 207 STA 178 CRACKED. INSTALLED NEW 65-16300-86 SIDE CHORD AS PER DWG 65-16300 SHEET 4 FRAM E 1 TO 8. 2 L 7 2 4F RT A16WE 2001072300093 20010723 00093 NM 2001 7 23 AWXA0001948 1 20010709 A 5311 651630087 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 304AW 24011 FUSELAGE RT SIDE CHORD AT WL 207, STA 178 CRACKED. INSTALLED NEW SIDE CHORD P/N 65-16300-87 AS PER DWG 65-16300 SHEET 4 FRAME 1-8. 2 L 7 2 4F RT A16WE 2001072300094 20010723 00094 NM 2001 7 23 AWXA0001950 1 20010709 A 5330 65457744 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 304AW 24011 FUSELAGE SKIN HAS A NON STANDARD REPAIR AT RIVET LOCATION BS 727C AND 2 INCHES BELOW STRINGER 17L. FUSELAGE SKIN REPAIR ED AT BS 727C AND 2 INCHES BELOW STR 17L PER SRM 53-00-01 FIG 203 PAGE 207. 2 L 7 2 4F RT A16WE 2001072300095 20010723 00095 NM 2001 7 23 AWXA0001951 1 20010709 A 5230 65C8073525 TEE CHORD BOEING 737 7373G7 1384595 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 304AW 24011 CRACK INDICATION ON AFT CARGO DOOR LOWER AFT CORNER, LOWER WEB TO SKIN ATTACH ANGLE, CRACK, LOCATED BETWEEN TWO AFT RIVE TS WEB. AFT LOWER WEB T-CHORD REPAIRED PER SB 737-52A1079/DRW 65 C25 180 + SRM 51-40-02 PG 4. 2 L 7 2 4F RT A16WE 2001072300096 20010723 00096 NM 2001 7 23 AWXA0001952 1 20010709 A 5310 6558853 CREASE BEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 304AW 24011 BS 767-787 LT CREASE BEAM PANEL IS CORRODED. SHEAR WEB MADE AND INSTALLED AS PER DWG 65-55885-3, PART PAINTED AS PER MM 51-21-10 PG 701. 2 L 7 2 4F RT A16WE 2001072300097 20010723 00097 EU 2001 7 23 AWXA0001953 1 20010709 A 5320 D5348004320501 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 645AW 238 AFT CABIN FLOOR PANEL SUPPORT AT Y-1732R/H FR 66 SCREWS HOLES CORRODED. REMOVED CORROSION, MATERIAL REMOVED .100 (BEYON D LIMITS AS PER A320 SRM 51-72-11 PG 1). REPLACED BEAM AS PER A320 SRM 51-42-11 PAR 6. 2 L 7 2 4F RT A28NM 2001072300098 20010723 00098 NM 2001 7 23 AWXA0001955 1 20010709 A 5330 143N33203 SKIN BOEING 757 7572S7 1384962 NM FUSELAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 CREASE IN FUSELAGE EXTERIOR SKIN AT BS 456 STR L-17. REMOVED DAMAGED SECTION OF SKIN. FABRICATED AND INSTALLED REPAIR PER ER 19-5331-01172-KB1. 2 L 7 2 4F RT A2NM 2001072300099 20010723 00099 NM 2001 7 23 AWXA0001956 1 20010709 A 5315 BAC150510067 FLOORBEAM BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 FS 365 BL 0 TO RBL 60 FOUND SURFACE CORROSION ON UPPER T-CAP AT FLOORBEAM. REMOVED DAMAGED T-CAP, FABRICATED NEW T-CAP AND INSTALLED PER SRM 53-0051 FIG 203 SH 2. 2 L 7 2 4F RT A2NM 2001072300100 20010723 00100 EU 2001 7 23 AWXA0001967 1 20010707 A 5270 848401 PROXIMITY SWITCH AIRBUS 320 A320231 3930325 EU CARGO DOOR FAULTY A AWXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 28 618AW 304 CMH- DIVERTED FLIGHT - FLT 280- EN ROUTE FROM PHL TO LAS THE CREW GOT A CLASS 1 LEVEL 2 FORWARD CARGO DOOR ECAM MESSAGE. AIRCRAFT PRESSURIZATION WAS NORMAL. THE AIRCRAFT DIVERTED TO CMH MAKING AN UNEVENTFUL LANDING. IN CMH MAINTENANCE VE RIFIED THE CARGO DOOR WAS CLOSED AND LOCKED. TROUBLESHOT AND REPLACED THE FWD CARGO DOOR HANDLE PROX SW 28 WV PER AMM 5 2-71-12-401. OPERATIONAL AND BITE CHECKS WERE GOOD. 2 L 7 2 4F RT A28NM 2001072300101 20010723 00101 NM 2001 7 23 VNAA0105015 1 20010524 A 3010 CONTROL VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE DE-ICE SYS FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 441JS 206 3059 AFTER DEPARTURE, THE CREW RECEIVED A AIRFOIL DE-ICE SYSTEM FAIL. THE CAPTAIN CONTACTED MAINTENANCE CONTROL AND WAS INST RUCTED TO DIVERT TO CAK. FLIGHT 4135 DIVERTED TO CAK WHERE MAINTENANCE INSPECTED AND REPLACED THE EJECTOR FLOW CONTROL VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RE LEASED FOR SERVICE. FLIGHT 4135 CONTINUED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001072300102 20010723 00102 NM 2001 7 23 VNAA0105017 1 20010526 A 5270 TARGET DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE PAX DOOR DIRTY A VNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 427JS 3039 FLIGHT 4012 WAS CLIMBING OUT FROM PIT AND THE CREW RECEIVED A DOOR CHIME AND A RED WARNING PANEL INDICATION OF A OPEN PA SSENGER DOOR. THE FIRST OFFICER VISUALLY CHECKED THE DOOR AND DOOR HANDLE FOR SECURITY. THE LIGHT WENT OUT THEN RETURN ED. THE CREW REFERENCED THE QUICK REFERENCE HANDBOOK AND CALLED MAINTENANCE CONTROL. THE CREW WAS INSTRUCTED TO RETURN TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND CLEANED THE OVER CENTER PROXI SENSOR TARGET IN A CCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001072300103 20010723 00103 NM 2001 7 23 VNAA0105021 1 20010528 A 3610 BLEED VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RIGHT FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 460PS 4362 3061 DURING CLIMBOUT THE CREW RECEIVED A RIGHT HAND BLEED VALVE FAIL CAS MESSAGE. THE CREW CYCLED THE SYSTEM SEVERAL TIMES T HEN CALLED MAINTENANCE CONTROL. THE CREW WAS INSTRUCTED TO RETURN TO PIT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND LOW PRESSURE BLEED VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 21-00-00. OPERATIONAL CHECKS WERE PERFORME D AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001072300104 20010723 00104 NM 2001 7 23 VNAA0105022 1 20010529 A 5270 PIN DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE PAX DOOR OUT OF ADJ A VNAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 07 427JS 3039 DURING CRUISE, THE CREW RECEIVED A RED WARNING PANEL INDICATION FOR A OPEN PASSENGER DOOR. THE CREW VERIFIED THIS ON TH E SYSTEMS PAGE. THE CREW CALLED MAINTENANCE CONTROL WHO INSTRUCTED THE CREW TO RETURN TO THE FIELD. MAINTENANCE INSPEC TED AND ADJUSTED THE STAIRWAY AND HINGE ALIGNMENT PIN IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. A MAINTEN ANCE FLIGHT WAS PERFORMED WITH NO FURTHER INCIDENTS. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001072300105 20010723 00105 NM 2001 7 23 VNAA0106001 1 20010604 A 2150 1716D000 A/C PACK DORNER DO32 DO328100 2996000 NM A/C BAY FAILED A VNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 459PS 13324 3070 THE CREW REPORTED A ELECTRIC BURNING SMELL. MAINTENANCE INSPECTED AND REPLACED THE COLD AIR UNIT IN ACCORDANCE WITH DOR NIER MAINTENANCE MANUAL 21-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A45NM 2001072300106 20010723 00106 NM 2001 7 23 VNAA0106007 1 20010609 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA PW118 PW118B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA O OTHER L NO TEST TX TAXI/GRND HDL 1 GL 07 429JS 11796 926 3043 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROW 6 WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EME RGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRA FT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001072300107 20010723 00107 NM 2001 7 23 VNAA0106009 1 20010611 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA PW118 PW118B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA O OTHER L NO TEST TX TAXI/GRND HDL 1 GL 07 437JS 577 3055 THE CREW REPORTED THAT THE EMERGENCY LIGHTING IN ROWS 3 THROUGH 6 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPL ACED THE EMERGENCY BATTERY AT THE 5LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHEC KS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001072300109 20010723 00109 NM 2001 7 23 VNAA0106014 1 20010621 A 2435 8160121 GENERATOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 430JS 11767 648 3044 LT GENERATOR FAILED DURING TAKEOFF. AIRCRAFT FERRIED TO PIT, MAINTENANCE REPLACED LEFT GENERATOR AND OPERATIONAL CHECK GOOD. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001072300110 20010723 00110 2001 7 23 VNAA0106015 4 20010622 A 2210 7015327901 PANEL DORNER DO32 DO328100 2996000 NM COCKPIT FAILED A VNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 07 439JS 10711 20 3057 WHILE ON DESCENT INTO CVG, THE CREW SMELLED FUMES IN THE COCKPIT. AN EMERGENCY WAS DECLARED. ON THE GROUND MAINTENANCE INSPECTED AND FOUND BURN SMELL COMING FROM GP 300. REPLACED THE GP300 AND NO OTHER PROBLEMS WERE NOTED. 2 H 7 2 4T RT A45NM 2001072300111 20010723 00111 NM 2001 7 23 VNAA0106018 1 20010625 A 2120 4068B000002 VALVE DORNER DO32 DO328100 2996000 NM A/C BAY FAILED A VNAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 431JS 4129 3028 AFTER TAXIING FROM THE GATE, THE FLIGHT ATTENDANT NOTIFIED THE CAPTAIN THAT THERE WAS SMOKE ENTERING THE CABIN. THE CAP TAIN SHUT DOWN THE PACKS AND BLEEDS AND CONFIRMED THERE WAS SMOKE IN THE CABIN. THE CAPTAIN RETURNED TO THE GATE AND DE PLANED THE PASSENGERS. MAINTENANCE INSPECTED AND REPLACED THE PACK VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 21-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A45NM 2001072300112 20010723 00112 NM 2001 7 23 VNAA0106019 1 20010626 A 2130 22260A030201 PANEL DORNER DO32 DO328100 2996000 NM COCKPIT FAILED A VNAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 434JS 2130 3051 DURING CLIMB, AT 4200MSL, THE CREW HEARD A NOISE AND DETERMINED THERE WAS A PROBLEM WITH THE PRESSURIZATION SYSTEM. THE CREW CONTACTED MAINTENANCE CONTROL AND WENT THROUGH TROUBLESHOOTING STEPS FOR A SOLUTION BUT THE PROBLEM PERSISTED. TH E CREW WAS INSTRUCTED TO RETURN TO PIT. ON THE RETURN TO PIT THE MANUAL MODE BEGAN TO PRESSURIZE THE CABIN QUICKLY. FL IGHT 4066 LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED AND REPLACED THE PRESSURIZATION CONTROL PANEL IN ACCO RDANCE WITH DORNIER MAINTENANCE MANUAL 21-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SE RVICE. 2 H 7 2 4T RT A45NM 2001072300113 20010723 00113 NM 2001 7 23 VNAA0106020 1 20010629 A 2750 FCU DORNER DO32 DO328100 2996000 NM T/E FLAP MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 439JS 3057 AS THE CREW ADVANCED THE POWER LEVERS FOR TAKEOFF, THE CREW RECEIVED A FLAP CONTROL FAIL MESSAGE. THE CREW TAXIED ONTO THE TAXIWAY AND REFERENCED THE QUICK REFERENCE HANDBOOK AND THE MESSAGE DIDN'T CLEAR. FLIGHT 4020 THEN RETURNED TO THE GATE. MAINTENANCE INSPECTED AND RESET THE FLAP CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-00-00. OP ERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A45NM 2001072300114 20010723 00114 SO 2001 7 23 C2XA01CL169 1 20010717 A 3350 20131A BATTERY EMB 145 EMB145LR SO CABIN DISCHARGED A C2XA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 27 16918 145397 CLE FLIGHT#3944 THE CREW REPORTED THE EMERGENCY LIGHTS WERE INOPERATIVE AT THE EXIT ROW.MAINTENANCE APPLIED POWER TO AIR CRAFT AND CHARGED THE EMERGENCY LIGHT BATTERIES.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001072300115 20010723 00115 NM 2001 7 23 VNAA0107003 1 20010702 A 2530 COFFEEMAKER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE GALLEY MALFUNCTIONED A VNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 427JS 3039 THE FLIGHT ATTENDANT REPORTED THAT FUMES FROM AN OVERHEATED HOT JUG WAS MAKING HER ILL. MAINTENANCE INSPECTED AND REPLA CED THE NR 2 HOT JUG IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 25-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001072300116 20010723 00116 EU 2001 7 23 01FDEA00535 1 20010712 A 2550 LOCK AIRBUS 300 A300F4605R 3930327 EU ULD MALFUNCTIONED A FDEA B EMER. DESCENT O OTHER CR CRUISE 1 SO 25 656FE 745 HEARD NOISE IN FLT - DISCOVERED ULD IN 2R FWD BELLY NOT LOCKED DOWN. NO APPARENT DAMAGE. AC OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2001072300123 20010723 00123 NM 2001 7 23 DL72E011103 1 20010701 A 2121 215201 FAN BOEING 727 727247 138408F NM CARGO BAY FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 830WA 21482 ELECTRICAL SMELL NOTED FROM ROWS 25, GASPER FAN C/B POPPED. REPLACED GASPER FAN. 2 L 7 3 4F A3WE 2001072300124 20010723 00124 NM 2001 7 23 DL72E011105 1 20010702 A 5310 651751738 BEAM BOEING 727 727247 138408F NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 INSPECTION OF THE RT TORQUE BOX OF THE VENTRAL STAIRWAY OPENING PER AD 94-07-08 AND BAC SB 727-53-0129 REVEALED A .5 INC H LONG CRACK IN THE UPPER HORIZONTAL BEAM AT FS 1263. THE DAMAGED PART WAS REMOVED AND A NEW PART INSTALLED PER THE REQ UIREMENTS OF THE SB AND ER/A 381245-14AD. 2 L 7 3 4F A3WE 2001072300125 20010723 00125 NM 2001 7 23 DL72L010914 1 20010603 A 2750 65C158141 BRACKET BOEING 727 727232 1384082 NM T/E FLAP BROKEN A DALA A UNSCHED LANDING E F VIBRATION/BUFFET FLT CONT AFFECTED CL CLIMB 1 SO 27 511DA 21313 ON DEPARTURE HEARD THUMP SOUND ACCOMPANIED BY SHUDDER. SHORTLY AFTER OUTBOARD FLAP STUCK IN 5 DEG RANGE WITH FLAP HAND LE AT 2 DEG. RETURNED TO CVG. FOUND CABLE ATTACH BRACKET BROKEN ON LEFT I/B FLAP O/B TRACK. REPLACED CABLE ATTACH BRA CKET AND CABLE DRUM ASSY. RIGGED AND SAFETIED O/B TRACK AFT FLAP EXTENSION CABLES. OPS CK GOOD. REF M/M. INSPECTION INSPECTED RIG AND OPS CK OF DRUM ASSY PER M/M RII COMPLIED WITH. 2 L 7 3 4F A3WE 2001072300126 20010723 00126 NM 2001 7 23 DL72L010916 1 20010605 A 5310 BEAM BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 INSPECTION OF THE RT VENTRAL STAIRWAY TORQUE BOX PER BAC S/B 727-53-0129 AND AD 94-07-08 REVEALED A TYPICAL CRACK IN THE UPPER AFT HORIZONTAL BEAM AT FS 1273. THE CRACKED PART WAS REMOVED AND A NEW PART INSTALLED. THE REPAIR WAS ACCOMPLIS HED PER THE S/B AND ER/A 380994-14AD. 2 L 7 3 4F A3WE 2001072300127 20010723 00127 NM 2001 7 23 DL72L010922 1 20010606 A 5754 ANGLE BOEING 727 727232 1384082 NM L/E SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 508DA 21310 FOUND ON A2 LETTER CK, .25 INCH CRACK NR 4 SLAT T/E CHORD AT O/B TRACK CUTOUT. REPAIRED PER MM 57-54-000-8. 2 L 7 3 4F A3WE 2001072300128 20010723 00128 NM 2001 7 23 DL72L010930 1 20010608 A 5532 65174633 SKIN BOEING 727 727232 1384082 NM VERTICAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 511DA 21313 A 0.5 INCH CRACK WAS FOUND IN THE VERTICAL STABILIZER SKIN ON THE LT SIDE, AT S-11. CRACK RUNS FROM A FASTENER HOLE AT S-11 AND EXTENDS FWD FOR APPROXIMATELY 0.5 INCH. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER INSTALLED. 2 L 7 3 4F A3WE 2001072300129 20010723 00129 NM 2001 7 23 DL72L010946 1 20010608 A 5330 65545739 SKIN BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 514DA 21430 DURING AD 99-04-22 INSPECTIONS OF THE LAP SPLICE LOWER FASTENER ROWS, TWO NONCONSECUTIVE BAYS WERE FOUND WITH CRACK IND ICATIONS. THE CRACKS WERE REMOVED AND THE SKIN REPAIRED PER B727 SRM 53-30-3 FIG 5, AS MANDATED BY FAA LETTER 99-120S-1 71, DTD 3-4-99. 2 L 7 3 4F A3WE 2001072300130 20010723 00130 NM 2001 7 23 DL72L010954 1 20010612 A 2120 UNKNOWN BOEING 727 727232 1384082 NM CABIN ODOR A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 509DA 21311 EN ROUTE TO PHX PAX REPORTED SMELLING HOT ELECTRICAL ODOR NEAR SEAT ROW 17. NO SMOKE WAS REPORTED AND NO C/B`S TRIPPED. CONTRACT MTC DROPPED CEILING PANELS AND PSUS NO DAMAGE FOUND. FLIGHT CREW RAN ENGINES AND PACKS. STILL UNABLE TO DUP LICATE PROBLEM. NO HISTORY OF ANY ELECTRICAL PROBLEMS IN CHAPTER 24 OR 33. NTF . 2 L 7 3 4F A3WE 2001072300131 20010723 00131 EA 2001 7 23 COMA0160491 1 20010721 A 5312 BEAM CNDAIR CNDAIR CL600 CL6002B19 EA CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 917CA 18560 7017 BULKHEAD AT FS 559 HAS CRACKED ON VERTICAL BEAMS. THE INBOARD AND OUTBOARD POST AT RBL9 AND INBOARD POST AT LBL9 ARE CRA CKED.REPAIRED VERTICAL BEAMS AT FS 559 I/A/W WVAC EO 601R-53-2596. 2 L 7 2 4F RT A21EA 2001072300132 20010723 00132 NM 2001 7 23 DL72L011041 1 20010622 A 2131 7638101 CONTROLLER BOEING 727 727232 1384082 NM CABIN PRESSURE FAILED A DALA O OTHER O OTHER CL CLIMB 1 SO 27 507DA 21309 CABIN PRESSURIZATION FAILED IN AUTO, STBY, AND MAN AC OUTFLOW VALVE WAS CONTROLLABLE IN MAN DC ONLY. REPLACED CABIN PRE SSURE CONTROLLER AFTER VERIFYING OLD CONTROLLER BAD. OPS CHECKS OK PER MM. 2 L 7 3 4F A3WE 2001072300133 20010723 00133 NM 2001 7 23 DL72L011097 1 20010701 A 3350 900835A BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 510DA 21312 ON L/O, FOUND INTERIOR OVERWING EXIT LIGHTS ON RIGHT SIDE FLICKERING. T/S, REPLACED BATTERY CARTRIDGE ASSY. OPS CHECK N ORMAL. 2 L 7 3 4F A3WE 2001072300134 20010723 00134 NM 2001 7 23 DL72L011111 1 20010303 A 5753 RIB BOEING 727 727232 1384082 NM T/E FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 513DA 21315 INBOARD AFT RIB CRACKED ON THE NR 1 MID FLAP. REPAIRED PER M/M 57-52-0 FIG 808. 2 L 7 3 4F A3WE 2001072300135 20010723 00135 NM 2001 7 23 DL72L011128 1 20010707 A 3350 900442 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 510DA 21312 LEFT AFT OVERWING EMERGENCY EXIT LIGHT ON MCO. REPLACED M955 BATTERY CHARGER AND BATTERY. 2 L 7 3 4F A3WE 2001072300136 20010723 00136 NM 2001 7 23 DL72S010915 1 20010605 A 3232 731414 ACTUATOR BOEING 727 727225A 1384077 NM RT MLG DOOR LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 805EA 22436 COMPLETE LOSS OF A SYSTEM HYD UPON GEAR RETRACTION. FOUND RT GEAR DOOR ACTUATOR LEAKING. REPLACED SAME PER M/M. 2 L 7 3 4F RT A3WE 2001072300137 20010723 00137 EA 2001 7 23 COMA0160492 1 20010722 A 5300 601R3110116115A ANGLE CNDAIR CL600 CL6002B19 EA MISDRILLED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 963CA 7127 THE CLEAT FOR LBL27 AT F.S. 364.0 WAS MISDRILLED WHILE INCORPORATING SB601R-53-037 (TITANIUM FLOOR BEAM MOD).FABRICATED AND INSTALLED A NEW CLEAT I/A/W WVAC EO 601R-53-2583. 2 L 7 2 4F RT A21EA 2001072300138 20010723 00138 2001 7 23 DL72S010919 4 20010606 A 3436 3186304951 LIGHT BOEING 727 727225A 1384077 NM COCKPIT SHORTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 8889Z 21858 BURNING SMELL IN COCKPIT DURING CRUISE. FOUND WINDSHEAR ANNUNCIATOR LIGHT ASSEMBLIES SHORTED CAUSING BURNING SMELL IN C OCKPIT. REPLACED LIGHT ASSY. 2 L 7 3 4F RT A3WE 2001072300139 20010723 00139 NM 2001 7 23 DL72S010924 1 20010531 A 5754 651622369 FASTENER BOEING 727 727232 1384082 NM L/E SLAT LOOSE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 532DA 22045 NR 2 SLAT I/B ACTUATOR RIB FASTENERS LOOSE. REQUIRING A SKIN SPLICE PER 727 SRM CH 57-54-000-8 FIG 801. ACTUAL DAMAGE NOT RELATED TO METHOD USED TO GAIN ACCESS. REASON FOR MAJOR REPAIR CLASSIFICATION UNKNOWN. 2 L 7 3 4F A3WE 2001072300140 20010723 00140 NM 2001 7 23 DL72S010928 1 20010607 A 3350 900542 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 534DA 22047 DURING SERVICE CHECK, FOUND FWD EMERGENCY LIGHT AT 3AB INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 2001092800042 20010928 00042 SO 2001 9 28 C2XA01BT128 1 20010720 A 4920 4501968D APU EMB 145 EMB145ER SO APU BAY FAILED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 27 17928 145007 EWR---CO4141, CREW REPORTED APU FAILED INFLIGHT (ON APPROACH). ELECTRICAL ODOR IN COCKPIT ASSOCIATED WITH THE FAILURE. MAINTENANCE INSPECTED AIRCRAFT AND DETERMINED APU FAULTY, AIRCRAFT PLACED ON MEL 49-00-00 CONTROL 013729. APU REMOVED AND REPLACED. MEL CLEARED AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2001072300141 20010723 00141 NM 2001 7 23 DL72S010995 1 20010617 A 2170 22D10 COALESCER BAG BOEING 727 727225A 1384077 NM A/C BAY DIRTY A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 8890Z 21859 AT FL 310 FLIGHT CREW SMELLED STRONG ODOR OF RAW CAR GAS, F/A IN AFT OF A/C SMELLED SAME. DIVERTED TO CVG, RAN FUME CHE CKLIST IN ENTIRETY. INSPECTED E/E COMPARTMENT BAG BINS AND LAV AREAS NO GASOLINE SMELLS. RAN ENGINES PRESS A/C NO SMEL LS NOTED. REPLACED WATER SEPARATOR BAGS, INSPECTED ACMS. NO PROBLEMS NOTED. A/C OK FOR SVC. 2 L 7 3 4F RT A3WE 2001072300142 20010723 00142 NM 2001 7 23 DL72S011000 1 20010618 A 5753 6516266918 FLAP TRACK BOEING 727 727232 1384082 NM T/E FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 542DA 22391 DURING OVERHAUL , THE INBOARD TRACK ASSY WAS FOUND WITH WEAR AND CORROSION BEYOND ALLOWABLE LIMITS. TRACK WAS REPAIRED PER ER/A 401969-14AD AND BFGOODRICH DOCUMENT 57-0364. 2 L 7 3 4F A3WE 2001072300143 20010723 00143 NM 2001 7 23 DL72S011007 1 20010618 A 3350 S106 BATTERY BOEING 727 727232 1384082 NM AFT STAIRWAY DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 527DA 21587 EMERGENCY ESCAPE LIGHTS ABOVE AFT STAIRWAY DID NOT COME ON WHEN TESTED. REPLACED BATTERIES IN LIGHT ASSY AND RETESTED, CHECKS NORMAL. 2 L 7 3 4F A3WE 2001072300144 20010723 00144 NM 2001 7 23 DL72S011022 1 20010620 A 3230 65404676 ACTUATOR BOEING 727 727225A 1384077 NM NLG BYPASSING A DALA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 805EA 22436 ON GEAR EXTENSION MAIN GEAR EXTENDED NORMALLY NOSE GEAR DID NOT. FOUND LOCK ACTUATOR BYPASSING INTERNALLY. REPLACED SA ME. 2 L 7 3 4F RT A3WE 2001072300145 20010723 00145 WP 2001 7 23 CALA0100660 1 20010719 A 5330 SKIN DOUG DC9 DC982 3022082 WP STA 218 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76823 49483 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 218 JUST ABOVE LONGERON 19L. THE SKIN WAS REPAIRED IAW SRM 53-04, PAGE 218K . 2 L 7 2 4F A6WE 2001072300146 20010723 00146 NM 2001 7 23 CALA0100661 1 20010720 A 5311 FRAME BOEING 737 7373T0 1384582 NM STA 787 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14358 23943 INSPECTION FOUND FRAME DENTED AT STA 787, S25R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-70-11, FIGURE 1. 2 L 7 2 4F RT A16WE 2001072300147 20010723 00147 NM 2001 7 23 CALA0100662 1 20010720 A 5230 SKIN BOEING 737 7373T0 1384582 NM C-2 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14358 23943 INSPECTION FOUND A 0.375" CRACK IN SKIN AT C-2 DOOR LIGHTENING HOLE ABOVE INTERIOR HANDLE. A DOUBLER WAS INSTALLED IAW E CRA 5230-01613. 2 L 7 2 4F RT A16WE 2001072300148 20010723 00148 NM 2001 7 23 CALA0100663 1 20010720 A 5230 STOP FITTING BOEING 737 7373T0 1384582 NM C-2 DOOR GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14358 23943 INSPECTION FOUND C-2 DOOR FORWARD LOWER STOP FITTING GOUGED. THE STOP FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-2. 2 L 7 2 4F RT A16WE 2001072300150 20010723 00150 NM 2001 7 23 DL72S011025 1 20010621 A 5270 WARNING LIGHT BOEING 727 727232 1384082 NM COCKPIT FALSE INDICATION A DALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 27 410DA 21222 R-2 DOOR IND ILLUM ON T/O ROLL. ABORTED T/O BELOW 100 KTS. INSPECTED DOOR, NO PROBLEM NOTED. DOOR OPS NORM. CYCLED N UMEROUS TIMES, UNABLE TO DUPLICATE. 2 L 7 3 4F A3WE 2001072300151 20010723 00151 NM 2001 7 23 DL72S011034 1 20010622 A 3350 1060091102 LIGHT BOEING 727 727225A 1384077 NM GALLEY INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8875Z 21293 FWD GALLEY EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY. 2 L 7 3 4F RT A3WE 2001072300152 20010723 00152 NM 2001 7 23 DL72S011044 1 20010622 A 3350 900542 LIGHT BOEING 727 727232 1384082 NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 517DA 21433 AFT LEFT EXTERIOR EMERGENCY LIGHT INOP WHILE TESTING, DURING LAYOVER CHECK. REPLACED LIGHT RACK. 2 L 7 3 4F A3WE 2001072300153 20010723 00153 NM 2001 7 23 DL72S011060 1 20010625 A 3350 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 515DA 21431 R1 DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY BATTERIES. 2 L 7 3 4F A3WE 2001072300154 20010723 00154 NM 2001 7 23 DL72S011061 1 20010625 A 3350 900835A BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 531DA 21814 RIGHT EXT OVERWING EXIT LIGHT INOP. REPLACED BATTERY, OP CHECKS GOOD. 2 L 7 3 4F A3WE 2001072300155 20010723 00155 CE 2001 7 23 C2XA01CL173 1 20010718 A 3260 MS25237327 BULB BEECH 1900 1900D 1154162 CE COCKPIT A C2XA O OTHER L NO TEST NR NOT REPORTED 1 SW 27 87557 UE246 CLE FLIGHT#3196 THE CREW REPORTED THE RED LIGHT ON THE GEAR HANDLE WAS INOPERATIVE.MAINTENANCE REPLACED THE BULB ON THE GEAR HANDLE AND OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT A24CE 2001072300156 20010723 00156 NM 2001 7 23 DL72S011071 1 20010626 A 5754 574702572 SKIN BOEING 727 727232 1384082 NM L/E FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 539DA 22385 A 2 INCH CRACK IN NR 1 L/E FLAP OUTER SURFACE OUT OF INBD LIP HINGE CUTOUT. REPAIR PER M/M 57-53-000-8. 2 L 7 3 4F A3WE 2001072300157 20010723 00157 NM 2001 7 23 DL72S011085 1 20010627 A 3350 MODULE BOEING 727 727232 1384082 NM CABIN DEFECTIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 541DA 22387 EMERGENCY LIGHTS INOP AT ROW 27 AND BACK. THE L-2 AND R-2 DOORS LWR LIGHTS ARE INOP. REPLACED MODULE M0027 TO FIX. 2 L 7 3 4F A3WE 2001072300158 20010723 00158 NM 2001 7 23 DL72S011086 1 20010621 A 5754 SKIN BOEING 727 727232 1384082 NM L/E SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 529DA 21703 LOWER LEADING EDGE SKIN SPAR CRACKED AT ACTUATOR ARM CUTOUT. REPAIRED PER 727 AMM 57-54-000-8. 2 L 7 3 4F A3WE 2001072300159 20010723 00159 NM 2001 7 23 DL72S011095 1 20010629 A 3350 LIGHT BOEING 727 727232 1384082 NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 526DA 21586 RT EMERGENCY EXTERIOR EXIT BETWEEN OVERWING EXIT INOP. RELAMPED, OPS CHECK NORMAL PER M/M. 2 L 7 3 4F A3WE 2001072300160 20010723 00160 NM 2001 7 23 DL72S011110 1 20010704 A 3350 900542 CHARGER BOEING 727 727232 1384082 NM CABIN FAULTY A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 522DA 21582 RIGHT AFT LOWER FUSELAGE EMERGENCY LIGHT INOP. REPLACED CHARGER, CKS OK. 2 L 7 3 4F A3WE 2001072300161 20010723 00161 NM 2001 7 23 DL72S011121 1 20010706 A 2120 65609902 DUCT BOEING 727 727232 1384082 NM RT PACK BLOWN A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 537DA 22073 AIRCRAFT UNABLE TO PRESSURIZE IN CLIMBOUT. FOUND DUCT BLOWN ON RT PACK. REPLACED DUCT AND CONTROLLER PRECAUTIONARY. P RESSURIZED A/C, CHECKS OK. NO LEAKS FOUND. A/C OK FOR SERVICE. 2 L 7 3 4F A3WE 2001072300162 20010723 00162 NM 2001 7 23 DL72S011123 1 20010706 A 5753 652163261 DOUBLER BOEING 727 727232 1384082 NM T/E FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 533DA 22046 AFT CHORD ANGLE, LOWER SPAR RAIL, REPAIR DOUBLER CRACKED 37 INCHES FROM I/B END. REPAIRED ON SHOP ORDER A64256, N/R CAR D 018778. 2 L 7 3 4F A3WE 2001072300163 20010723 00163 NE 2001 7 23 DL72S011124 2 20010706 A 7200 JT8D15AHK ENGINE BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 1 MALFUNCTIONED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 520DA 66377 21471 696467 ON T/O AT 40 KTS NR 1 ENG APPEARED TO HAVE A COMPRESSOR STALL. EPR DROPPED SUDDENLY FROM 1.94 TO BELOW 1.7. AUTO PACK TRIP OCCURRED AND T/O WAS DISCONTINUED. RAN ENGINE TESTS PER PREFLIGHT HANDBOOK. UNABLE TO DUPLICATE. 2 L 7 3 4F 4 F A3WE E2EA 2001072300164 20010723 00164 NM 2001 7 23 DL72S011134 1 20010709 A 5753 651626920 FLAP TRACK BOEING 727 727232 1384082 NM T/E FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 533DA 22046 INBOARD FLAP, NR 4 INBOARD TRACK FOUND WITH CORROSION AND WEAR AT MLG AND SPOILER BEAM ATTACH PADS, AND FWD LUG AND MLG DOOR HINGE FITTING HOLES. REPAIR PER ER/A 402041-14AD. 2 L 7 3 4F A3WE 2001072300165 20010723 00165 NE 2001 7 23 DL72W010952 2 20010612 A 7200 JT8D15AHK ENGINE BOEING 727 727247 138408F NM PWA JT8 JT8D15 52051 NE NR 3 MALFUNCTIONED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 292WA 69478 22110 695220 ON T/O ROLL, NR 3 ENG INSTR WERE UNSTABLE. ABORTED AT 110 KNOTS. ON INITIAL PWR APPLICATION NR 3 ENG WAS STABLE THEN P ROGRESSIVELY BECAME UNSTABLE. NORMAL PWR USED. VERSA LUBE NR 3 ENG FUEL CONTROL. INSP MAIN CHIP DETECTOR, INSP INTAKE , EXH AND NO DEFECTS FOUND. RAN PFHB, ALL IND NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001072300166 20010723 00166 NM 2001 7 23 DL72W010991 1 20010616 A 2750 AV13J5144 BYPASS VALVE BOEING 727 7272Q8 138407W NM T/E FLAP FAILED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 831L 21826 ON FLAP RETRACTION LOST A-SYS HYD. FOUND O/B FLAP BYPASS VALVE FAILED. REMOVED AND REPLACED O/B FLAP BYPASS VALVE. 2 L 7 3 4F A3WE 2001072300167 20010723 00167 NM 2001 7 23 DL72W011018 1 20010620 A 5711 SPAR BOEING 727 727247 138408F NM RT WING CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 293WA 22111 FOUND ON F1 LETTER CK, MLG AUX SPAR CHAFED AT INBD END. REPAIRED PER MM 57-43-000-8. 2 L 7 3 4F A3WE 2001072300168 20010723 00168 NM 2001 7 23 DL72W011057 1 20010624 A 3350 900835A BATTERY PACK BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 292WA 22110 LEFT FWD AND AFT EMERGENCY EXIT EXTERIOR LIGHTS INOP. REPLACED BATTERY PACKS. 2 L 7 3 4F A3WE 2001072300169 20010723 00169 NM 2001 7 23 DL72W011058 1 20010624 A 3350 900835A BATTERY PACK BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 292WA 22110 LEFT FWD AND AFT EMERGENCY EXIT EXTERIOR LIGHT INOP. REPLACED BATTERY PACKS. 2 L 7 3 4F A3WE 2001072300170 20010723 00170 NM 2001 7 23 ZW0A0105501 1 20010722 A 3350 582240 BATTERY PACK BOEING 767 76733AER 1385230 NM RH ROW 1-2-3 A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 637TW 25403 THE EGRESS LIGHTS WERE INOPERATIVE ON RH SIDE OF CABIN, FIRST 3 ROWS. REPLACED THE BATTERY PACK. CHECK-C 1-27-01 LAX. --CLOSED-- 2 L 7 2 4F RT A1NM 2001072300171 20010723 00171 NM 2001 7 23 ASAA0140078 1 20010522 A 3350 6531914102 SLIDING WINDOW BOEING 737 737490 1384715 NM NR 2 BINDING A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 706AS 28894 SEA - DURING LINE CHECK, FOUND FIRST OFFICERS SLIDING WINDOW HARD TO OPEN AND CLOSE. REMOVED, REPLACED AND RIGGED, WIND OW IAW MM, OPS NORMAL. (M) 2 L 7 2 4F RT A16WE 2001072300172 20010723 00172 NM 2001 7 23 ASAA0110261 1 20010503 A 5200 6574583 HANDLE BOEING 737 737210C 1384459 NM L2 DOOR A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 ANC - DURING MAINTENANCE CHECK, FOUND L1 DOOR DIFFICULT TO OPERATE. CLEANED AND LUBED HANDLE AND HANDLE OPERATED NORMAL LY. (M) 2 L 7 2 4F A16WE 2001072300173 20010723 00173 EU 2001 7 23 SIMA200117301 1 20010622 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN INOPERATIVE A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 550LL 550 DFW - FOUND EMERGENCY LIGHT ON PASSENGER DOOR INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IAW AMM. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 2001072300174 20010723 00174 EU 2001 7 23 SIMA200117302 1 20010622 A 3350 1031309111 LIGHT AEROSP ATR72 ATR72212 EU CABIN INOPERATIVE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 420AT 420 MIA - MAINTENANCE REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS AT SEAT 9AB IS INOPERATIVE. MAINTENANCE REPLACED THE FL OOR LIGHT AND THE BATTERY PACK FOR THIS LIGHT IAW ATR MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001072300175 20010723 00175 2001 7 23 SIMA20011264 4 20010506 A 3100 005WS00 WEU SAAB SF340 340B 7860101 EU AVIONICS RACK A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 286AE 340B286 BOS - FLT 4749 - CREW REPORTED THE WARNING ELECTRONIC UNIT (WEU) BITE LIGHT ILLUMINATED DURING TAKEOFF. MAINTENANCE REM OVED AND REPLACED THE WEU IAW SAAB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001072300176 20010723 00176 EU 2001 7 23 SIMA20011281 1 20010508 A 3350 3071BPGPL BULB SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 21 234AE 340B234 HPN - FOUND 11BC FLOOR PROXIMITY LIGHT IS INOPERATIVE. PUT ON MEL AT THIS TIME. MAINTENANCE REPLACED THE BULB FOR THE 11BC LIGHT. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001072300177 20010723 00177 SO 2001 7 23 SIMA200115902 1 20010608 A 5300 ALCLAD2024T3 SKIN EMB 145 EMB145LR SO CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 639AE 145182 ABI - DURING MBV INSPECTION UNDER FLOOR OF AIRCRAFT, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS AT F RAME 20. REMOVED AND REPLACED CORRODED AREA. WORK DONE IAW EMB SRM 145/1142 REV 12 CHAPTER 53-21-10 PATE 201 THROUGH P AGE 204. (M) 2 L 7 2 4T RT T00011AT 2001072300178 20010723 00178 EU 2001 7 23 SIMA200116004 1 20010609 A 3350 EO1173110 SWITCH AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 135MQ 135 MIA - F/A'S PANEL EMERGENCY LIGHT SWITCH STICKS AND INOPERATIVE. REMOVED AND REPLACED SWITCH IAW AMM. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 2001072300179 20010723 00179 EU 2001 7 23 SIMA20011306 1 20010510 A 3350 1317 BULB AEROSP ATR72 ATR72212 EU MAIN DOOR INOPERATIVE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 308AE 309 DFW - DURING SCHEDULED PS-2 CHECK, FOUND THE MAIN DOOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED BULB FOR MAIN DOOR EMERGENCY LIGHT, OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001072300180 20010723 00180 EU 2001 7 23 SIMA200117109 1 20010620 A 5300 S53570203202 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 426AT 426 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED SEAT TRACKS, LEFT OUTBOARD MID, LEFT INBOARD MID, RIGHT OUTBOARD AN D RIGHT INBOARD MID CORRODED. MAINTENANCE REMOVED AND REPLACED SEAT TRACKS IAW EO E2-53MR-115. AIRCRAFT WAS RETURNED T O SERVICE. (M) 2 H 7 2 4T RT A53EU 2001072400001 20010724 00001 NM 2001 7 24 HNAA0100040 1 20010720 A 2700 659603 VALVE DHAV DHC8 DHC8102 2809003 NM LEAKING A HNAA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 EA 07 907HA 42581 011 IN FLIGHT #2 HYDRAULIC SYSTEM QUANTITY DROPPED TO 1 QUART. AIRCRAFT DIVERTED TO ISP. FOUND #2 FLIGHT SPOILER UNLOADING V ALVE LEAKING. REPLACED VALVE. 2 H 7 2 4T RT A13NM 2001072400002 20010724 00002 NM 2001 7 24 HNAA0100041 1 20010711 A 3260 841101 SENSOR DHAV DHC8 DHC8102 2809003 NM BROKEN A HNAA K NONE N FALSE WARNING AP APPROACH 1 EA 07 915HA 69 ON BOTH NORMAL AND ALTERNATE GEAR EXTENSION THE NLG UNSAFE LIGHTS REMAINED ILLUMINATED. FOUND BROKEN WIRE ON NLG DOWNLOC K PROXIMITY SENSOR. REPLACED SENSOR. 2 H 7 2 4T RT A13NM 2001072400004 20010724 00004 NM 2001 7 24 2001UALA00774 1 20010516 A 3260 656021132 ACCESSORY UNIT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE E/E BAY FAULTY A UALA O OTHER N FALSE WARNING LD LANDING 1 WP 29 7298U 21893 DURING LANDING, THE LANDING GEAR WARNING HORN SOUNDED AND A RED INDICATION OCCURRED FOR BOTH LEFT AND RIGHT MAIN GEAR. *S/D* THE LANDING GEAR ACCESSORY UNIT FAILED. REPLACED LANDING GEAR ACCESSORY UNIT PER MAINTENANCE MANUAL. RAN ENGINE PER JET RUN UP HANDBOOK. PERFORMED POWER TRANSFERS DURING ENG RUN. LANDING GEAR INDICATION NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001072400005 20010724 00005 NM 2001 7 24 2001UALA00775 1 20010518 A 3260 H1010154 SWITCH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NLG ERRATIC A UALA O OTHER N FALSE WARNING LD LANDING 1 WP 29 7252U 21399 LANDED CID UNDER AMBER ALERT DUE TO A NOSE GEAR INDICATION PROBLEM. *S/D* FOUND NOSE POSITION SWITCH S93 ERRATIC WHEN TAPPED. REPLACED S93 POSITION SWITCH PER MAINTENANCE MANUAL. OPERATIONAL CHECKS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001072400007 20010724 00007 NM 2001 7 24 2001UALA00943 1 20010604 A 2133 7133991 SEAL BOEING 727 727222 1384073 NM OUTFLOW VALVE MISSING A UALA O OTHER O OTHER DE DESCENT 1 WP 29 7277U 21424 CABIN PRESSURE CANNOT BE MAINTAINED IN DESCENT. *S/D* FOUND OUTFLOW VALVE FRAME SEAL MISSING. REPLACED FRAME SEAL. O PERATIONS CHECK NORMAL. 2 L 7 3 4F A3WE 2001072400008 20010724 00008 NM 2001 7 24 2001UALA00982 1 20010608 A 2133 3964421 VALVE BOEING 737 737322 1384676 NM CABIN PRESSURE FAILED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 349UA 24253 UNSCHEDULED LANDING. UNABLE TO MAINTAIN CABIN PRESSURE. *S/D* FAILED LEFT FLOW CONTROL VALVE AND A LOOSE APU PNEUMATI C DUCT CLAMP. SECURED LOOSE APU DUCT CLAMP, THEN REPLACED FAILED FLOW CONTROL VALVE. 2 L 7 2 4F RT A16WE 2001072400010 20010724 00010 NM 2001 7 24 2001UALA00999 1 20010606 A 2421 GENERATOR BOEING 767 767322 1385200 NM LT ENGINE FAILED A UALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 WP 29 666UA 29238 LEFT GEN TRIP EN ROUTE TO HNL WOULD NOT RESET. APU WOULD NOT START, RTF. 2 L 7 2 4F RT A1NM 2001072400011 20010724 00011 NM 2001 7 24 2001UALA01040 1 20010613 A 5330 148W4912 SKIN BOEING 777 777222 1385219 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 790UA 17723 26943 MAJOR REPAIR. RT FUSE SKIN CRACKED FWD OF HORIZ STAB CUTOUT AT FWD LWR CORNER APPROX STA 2256. *S/D* INSTALLED REPAIR PER EVA G95-7726. 2 L 7 2 4F RT T0001SE 2001072400012 20010724 00012 NM 2001 7 24 2001UALA01043 1 20010615 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 CABIN FLOORBEAM CORRODED STA 345 - 365, BL 0. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOORBEAM SUPPORT. 2 L 7 2 4F RT A2NM 2001072400014 20010724 00014 NM 2001 7 24 2001UALA01047 1 20010618 A 5320 ANGLE BOEING 757 757222 1384956 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 CABIN FLOOR STRUCTURE CORRODED STA 1640 TO 1681, LBL 57. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW J-ANGLES. 2 L 7 2 4F RT A2NM 2001072400015 20010724 00015 NM 2001 7 24 2001UALA01048 1 20010618 A 5330 SKIN BOEING 757 757222 1384956 NM FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 FUSELAGE SKIN DENTED STA 602 - 622 STR 16L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLERS ON SKIN AND REPAIR U-CHANNEL S ON STRINGER. 2 L 7 2 4F RT A2NM 2001072400016 20010724 00016 NM 2001 7 24 2001UALA01050 1 20010616 A 3350 SWITCH BOEING 747 747422 1384935 NM CABIN DEFECTIVE A UALA K NONE N FALSE WARNING NR NOT REPORTED 1 WP 29 104UA 26902 EMERGENCY LIGHTS EICAS ADVISORY MESSAGE DISPLAYED. EMERGENCY LIGHTS SWITCH NOT IN ARMED POSITION, OR SWITCH IN ARMED POS ITION AND EMERGENCY LIGHTS TURNED ON BY FLT ATTENDANT.SUPPLEMENTAL DATA UPDATE FOUND EMERGENCY LIGHT SWITCH AT 1L ATTEN DANT GUARD WAS ACTIVATED. ALSO SWITCH BULB WAS OUT. REPAIRED GUARD AND REPLACED SWITCH BULB OPS CHECKED OK. 2 L 7 4 4F RT A20WE 2001072400017 20010724 00017 NM 2001 7 24 2001UALA01052 1 20010615 A 3350 LIGHT BOEING 747 747422 1384935 NM CABIN INTERMITTENT A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 187UA 26876 EEL LIGHT FLICKERS AT 42 TO 45 LEFT AND RIGHT 46 TO 55 AND AFT GALLEY - SUPPLEMENTAL DATA UPDATE COULD NOT DUPLICATE DI SCREPANCY. JIGGLED CONNECTORS, STEPPED ON EEL LIGHT STRIP, NO DEFECTS NOTED. 2 L 7 4 4F RT A20WE 2001072400018 20010724 00018 EU 2001 7 24 2001UALA01060 1 20010617 A 5610 WINDSHIELD AIRBUS 320 A320232 3930326 EU COCKPIT CRACKED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 415UA 475 CAPTAINS WINDSHIELD OUTER PANE CRACKED 2 L 7 2 4F RT A28NM 2001072400019 20010724 00019 NM 2001 7 24 2001UALA01065 1 20010618 A 3350 LIGHT BOEING 747 747422 1384935 NM CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 188UA 26877 EEL STRIPS AT DOOR 4 CROSS ISLE AND EEL IN LEFT HAND ISLE ADJACENT TO DOOR 4L ARE INOP. SUPPLEMENTAL DATA UPDATE FOUND E EL FEEDER STRIP BAD, REMOVED BAD SECTION AND SPLICED IN NEW FEEDER STRIP. 2 L 7 4 4F RT A20WE 2001072400020 20010724 00020 NM 2001 7 24 2001UALA01066 1 20010615 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 615UA 21876 AFT CARGO PIT BS 1175 UNDER T-CAP FROM LBL 30 TO RBL 45, BOTH SIDES OF BS 1175 WEB CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED T-CAP PER SRM 53-00-51 AND 51-40-02 AND BAC DRAWING 146T1060. 2 L 7 2 4F RT A1NM 2001072400021 20010724 00021 NM 2001 7 24 2001UALA01067 1 20010615 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 615UA 21876 FWD PIT STA 544, LBL 20, T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. REPAIRED T-CAP PER SRM 53-30-07, FIG 1. 2 L 7 2 4F RT A1NM 2001072400022 20010724 00022 NM 2001 7 24 2001UALA01068 1 20010615 A 5311 FRAME BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 615UA 21876 AFT CARGO PIT AT BS 1263 AT RBL 20-35, FRAME T-CAP IS CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED T-CAP SECTION PER BAC DRAWING 146T1060 AND INSTALLED PER SRM 51-40-2. 2 L 7 2 4F RT A1NM 2001072400061 20010724 00061 NM 2001 7 24 2001UALA01069 1 20010615 A 5320 ATTACH ANGLE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 615UA 21876 CABIN BS 1263, STR 12R STRINGER ATTACH ANGLE HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. FABRICATED NEW CLIP PER BAC DRA WING 140T2101 AND INSTALLED PER SRM 51-40-2. 2 L 7 2 4F RT A1NM 2001072400106 20010724 00106 NM 2001 7 24 2001UALA01070 1 20010615 A 5320 STRINGER CLIP BOEING 767 767222 1385122 NM FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 615UA 21876 STA 434 STR 39L ELONGATED HOLE IN STRINGER CLIP. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP PER BAC DRAWING 14 0T2101 AND INSTALLED PER SRM 51-40-2. 2 L 7 2 4F RT A1NM 2001072400107 20010724 00107 NM 2001 7 24 2001UALA01071 1 20010615 A 5311 FRAME BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 615UA 21876 AFT CARGO PIT AT BS 1263 AT RBL 20-35, FRAME T-CAP IS CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED NEW T-CAP SECTIO N PER BAC DRAWING 146T1060 AND INSTALLED PER SRM 51-40-2. 2 L 7 2 4F RT A1NM 2001072400109 20010724 00109 NM 2001 7 24 2001UALA01073 1 20010615 A 5313 STRINGER BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 615UA 21876 AFT BULK PIT AT BS 1540 - 1562, STRINGER 39L IS CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED STRINGER SECTION AND SPLICE PER SRM 53-00-03 AND INSTALLED PER SRM 51-40-2. 2 L 7 2 4F RT A1NM 2001072400110 20010724 00110 NM 2001 7 24 2001UALA01074 1 20010615 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 615UA 21876 AFT CARGO PIT BS 1175 UNDER T-CAP FROM LBL 30-RBL 45, BOTH SIDES OF WEB CORRODED UNDER NUT PLATES. MAJOR REPAIR ACCOMPL ISHED. REPLACED T-CAP PER SRM 53-00-51, BAC DRAWING 146T1060 AND INSTALLED PER SRM 51-40-2. 2 L 7 2 4F RT A1NM 2001072400111 20010724 00111 NM 2001 7 24 2001UALA01075 1 20010619 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 434 STR 32L - 33L SHEAR TIE CORRODED. FABRICATED AND INSTALLED REPAIR IAW BAC DRAWING 140T2102 AND 140T1917 AND SRM 51-40-02. 2 L 7 2 4F RT A1NM 2001072400112 20010724 00112 NM 2001 7 24 2001UALA01077 1 20010616 A 3350 LIGHT BOEING 767 767322 1385200 NM CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 645UA 25280 EEL LIGHTING INOP AT SEAT 1E. SECURED EEL STRIP, OP CKS GOOD. 2 L 7 2 4F RT A1NM 2001072400113 20010724 00113 NM 2001 7 24 2001UALA01078 1 20010619 A 2560 BATTERY BOEING 727 727222 1384073 NM FLASHLIGHT DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7450U 21904 AFT EMERGENCY FLASHLIGHT INOPERABLE. REPLACED BATTERIES. OPERATIONAL CHECK NORMAL. 2 L 7 3 4F A3WE 2001102600014 20011026 00014 NM 2001 10 26 2001UALA01079 1 20010616 A 5270 SENSOR BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CARGO DOOR LOOSE A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 603UA 21864 FWD CARGO DOOR LIGHT CAME ON AT 10,000 FT. FOUND SENSOR S214 LOOSE. SECURED, OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E3NE 2001072400114 20010724 00114 NM 2001 7 24 2001UALA01080 1 20010619 A 5313 STRINGER BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 STATION 430 STRINGER 39R IS CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER REPAIR IAW SRM 53-0 0-03. 2 L 7 2 4F RT A1NM 2001072400115 20010724 00115 NM 2001 7 24 2001UALA01081 1 20010619 A 5313 STRINGER BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 412 - 434 STR 37R CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IAW SRM 53-30-03. 2 L 7 2 4F RT A1NM 2001072400116 20010724 00116 NM 2001 7 24 2001UALA01082 1 20010619 A 5313 STRINGER BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 698 STR 39R CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IAW DRAWING 143T1212 AND SRM 51-40 -02. 2 L 7 2 4F RT A1NM 2001072400117 20010724 00117 WP 2001 7 24 DHL2001803567 1 20010710 A 5313 57535461D FITTING DOUG DC8 DC873 302199C WP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 C-CHECK-R/H MLG- 3/4 CRACK IN JOINT TRAPEZOIDAL FITTING WITH LONGERON 24 AT STA. 902.000CORRECTIVE ACTION-REPAIRED CRACK ON TRAPEZOIDAL FITTING STA. 902.000 L-24R IAW FAX SEV- LIM-01-00073 H EO. SEMON# 200176 PER S/B 53-61 REV. 3 ACCOMPLISH MENT INSTRUCTIONS, CONDITION 3 FIG. # 3. (N/R # 0176) STATUS CLOSED. 2 L 7 4 4F RT 4A25 2001072400118 20010724 00118 NM 2001 7 24 2001UALA01083 1 20010619 A 5320 STRINGER CLIP BOEING 767 767222 1385122 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 437 - 537L STR CLIP CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IAW DRAWING 140T2101 AND SR M 51-40-02. 2 L 7 2 4F RT A1NM 2001072400119 20010724 00119 NM 2001 7 24 2001UALA01084 1 20010619 A 5310 STRUCTURE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 440 STR 38R CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IAW SRM 53-30-03. 2 L 7 2 4F RT A1NM 2001072400120 20010724 00120 NM 2001 7 24 2001UALA01085 1 20010619 A 5310 STRUCTURE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 544 STR 39L AND 39R CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED IAW BAC DRAWING 140T2102 AND SRM 51-40-02. 2 L 7 2 4F RT A1NM 2001072400125 20010724 00125 NM 2001 7 24 2001UALA01086 1 20010619 A 5310 STRUCTURE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 698 STR 38L - 39L CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IAW BAC DRAWING 140T2102-257 AND SRM 51-40-02. 2 L 7 2 4F RT A1NM 2001072400126 20010724 00126 NM 2001 7 24 2001UALA01087 1 20010619 A 5310 STRUCTURE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 610 STR 39R - 39L CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IAW BAC DRAWING 140T2102-331 AND SRM 51-40-02. 2 L 7 2 4F RT A1NM 2001072400127 20010724 00127 NM 2001 7 24 2001UALA01088 1 20010619 A 5320 INTERCOSTAL BOEING 767 767222 1385122 NM FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 1270 - 1280 APPROX 15 INCHES I/B AFT PIT DOOR CUTOUT FLOOR INTERCOSTAL DAMAGED. MAJOR REPAIR ACCOMPLISHED. FABRICAT ED AND INSTALLED INTERCOSTAL IAW BAC DRAWING 453T1536-5 AND SRM 51-40-02. 2 L 7 2 4F RT A1NM 2001072400128 20010724 00128 NM 2001 7 24 2001UALA01089 1 20010619 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 368 LBL 33 T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IAW SRM 53-00-07 AND 51-40-02 . 2 L 7 2 4F RT A1NM 2001072400129 20010724 00129 NM 2001 7 24 2001UALA01090 1 20010619 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 742 STR 39L - 39R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IAW BAC DRAWING 14 0T2102 - 1505 AND SRM 51-40-02. 2 L 7 2 4F RT A1NM 2001072400130 20010724 00130 NM 2001 7 24 2001UALA01091 1 20010619 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 346 STR 35L - 36L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IAW BAC DRAWING 14 0T1220-14 AND SRM 51-40-02. 2 L 7 2 4F RT A1NM 2001072400131 20010724 00131 NM 2001 7 24 2001UALA01092 1 20010619 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 544 STR 38L - 39L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IAW BAC 140T2102-2 32 AND SRM 51-40-02. 2 L 7 2 4F RT A1NM 2001072400132 20010724 00132 NM 2001 7 24 2001UALA01093 1 20010619 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 610 STR 38L - 39L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IAW BAC DRAWING 14 0T2102-232 AND SRM 51-40-02. 2 L 7 2 4F RT A1NM 2001072400133 20010724 00133 NM 2001 7 24 2001UALA01094 1 20010619 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 698 STR 38L - 39L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IAW BAC DRAWING 14 0T2102-259 AND SRM 51-40-02. 2 L 7 2 4F RT A1NM 2001072400134 20010724 00134 NM 2001 7 24 2001UALA01095 1 20010619 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 355 STR 39R - 38R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IAW BAC DRAWING 14 1T1221-68 AND SRM 51-40-02. 2 L 7 2 4F RT A1NM 2001072400136 20010724 00136 NM 2001 7 24 2001UALA01099 1 20010619 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 346 STR 33L - 34L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IAW BAC DRAWING 14 1T1221-16 AND SRM 51-40-02. 2 L 7 2 4F RT A1NM 2001072400137 20010724 00137 NM 2001 7 24 2001UALA01100 1 20010619 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 434 STR 33L - 34L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IAW BAC DRAWING 14 0T2102-1917 AND SRM 51-40-02. 2 L 7 2 4F RT A1NM 2001072400138 20010724 00138 NM 2001 7 24 2001UALA01101 1 20010619 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 610 STR 36L - 37L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IAW BAC DRAWING 14 0T2102 AND SRM 51-40-02. 2 L 7 2 4F RT A1NM 2001072400139 20010724 00139 NM 2001 7 24 2001UALA01102 1 20010619 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 544 STR 37L - 38L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IAW BAC DRAWING 14 0T2102-221 AND SRM 51-40-02. 2 L 7 2 4F RT A1NM 2001072400140 20010724 00140 EA 2001 7 24 COMA0160493 1 20010722 A 5346 60135006 WEB CNDAIR CL600 CL6002B19 EA CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 951CA 13435 7091 DURING COMPLIANCE OF EO 53-021 (VISUAL INSPECTION OF THE ENGINE SUPPORT BEAM) FOUND TOP CENTER UPPER WEB OF ENGINE SUPPO RT BEAM CRACKED.REPAIRED THE ENGINE SUPPORT BEAM IN ACCORDANCE WITH CRJ REO 601R-53-61-345. 2 L 7 2 4F RT A21EA 2001072400141 20010724 00141 NM 2001 7 24 2001UALA01104 1 20010620 A 5347 SEAT TRACK BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 1285 - 1307 SEAT TRACK CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 53-00-52 AND 51-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400142 20010724 00142 NM 2001 7 24 2001UALA01106 1 20010620 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 676 STR 38L-39L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 140T2102 AND S RM 51-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400143 20010724 00143 NM 2001 7 24 2001UALA01107 1 20010620 A 5313 STRINGER BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 742 STR 38L CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 140T2102-251 AND SRM 51-40-0 2 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400144 20010724 00144 NM 2001 7 24 2001UALA01108 1 20010620 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 610 STR 37L-38L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 140T202 AND SR M 51-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400145 20010724 00145 NM 2001 7 24 2001UALA01109 1 20010620 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 368-390 STR 38R-39R SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 141T1222-1 8 AND SRM 51-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400146 20010724 00146 EA 2001 7 24 COMA0160494 1 20010721 A 2750 853D10011 ACTUATOR CNDAIR CL600 CL6002B19 EA BINDING A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 959CA 9490 7116 FLAPS FAILED AT 42 DEGREES.REPLACED THE LEFT HAND #3 ACTUATOR. 2 L 7 2 4F RT A21EA 2001072400147 20010724 00147 EA 2001 7 24 COMA0160495 1 20010721 A 2750 853D100MD101 ACTUATOR CNDAIR CL600 CL6002B19 EA BINDING A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 959CA 12507 7116 FLAPS FAILED AT 42 DEGREES.REPLACED THE R/H #3 ACTUATOR. 2 L 7 2 4F RT A21EA 2001072400148 20010724 00148 NM 2001 7 24 2001UALA01110 1 20010610 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSLEAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 566 STR 38L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 140T2102-232 AND S RM 51-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400149 20010724 00149 NM 2001 7 24 2001UALA01111 1 20010610 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 434 STR 36L-37L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 140T2102 AND S RM 51-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400150 20010724 00150 NM 2001 7 24 2001UALA01112 1 20010620 A 5310 STRUCTURE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 437 STR 37L CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 53-30-03 AND 51-40-02 N-R. MAJO R REPAIR. 2 L 7 2 4F RT A1NM 2001072400151 20010724 00151 NM 2001 7 24 2001UALA01113 1 20010610 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 654 STR 36L-37L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 140T2102-207 A ND SRM 51-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400152 20010724 00152 NM 2001 7 24 2001UALA01114 1 20010620 A 5310 STRUCTURE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 676 STR 39R-37L CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 140T2102 AND SRM 51-40-0 2 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400153 20010724 00153 NM 2001 7 24 2001UALA01115 1 20010620 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 412 STR 38L-39L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 141T1224 AND S RM 51-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400154 20010724 00154 NM 2001 7 24 2001UALA01116 1 20010620 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 566 STR 36L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 140T2102 AND SRM 5 1-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400155 20010724 00155 NM 2001 7 24 2001UALA01117 1 20010620 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 434 STR 37L-38L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 140T2102 AND S RM 51-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400156 20010724 00156 NM 2001 7 24 2001UALA01118 1 20010620 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 140T2102-232 AND SRM 51-40-02. *S/D* FABRICATED AND INSTALL ED REPAIR IN ACCORDANCE WITH BAC DWG 140T2102-232 AND SRM 51-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400158 20010724 00158 EA 2001 7 24 COMA0160496 1 20010721 A 2750 854D100MD101 ACTUATOR CNDAIR CL600 CL6002B19 EA BINDING A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 959CA 12507 7116 FLAPS FAILED AT 42 DEGREES.REPLCED THE RIGHT HAND #4 ACTUATORS. 2 L 7 2 4F RT A21EA 2001072400159 20010724 00159 NM 2001 7 24 2001UALA01120 1 20010620 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 654-676 STR 39L-39R SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 140T2102-2 67 AND SRM 51-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001102600015 20011026 00015 NE 2001 10 26 2001UALA01121 2 20010620 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RIGHT STALLED A UALA A UNSCHED LANDING A FLAME/FIRE CL CLIMB 1 WP 29 649UA 25286 RIGHT ENGINE SURGED AND STALLED, FLAMES WERE COMING FROM THE FRONT AND BACK AFTER TAKEOFF. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 2001072400160 20010724 00160 EA 2001 7 24 COMA0160497 1 20010721 A 2750 860D10018ABC COMPUTER CNDAIR CL600 CL6002B19 EA MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 937CA 13402 7044 FLAPS FAILED WHEN ACFT POWERED UP.REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2001072400161 20010724 00161 2001 7 24 2001UALA01122 4 20010621 A 2330 1167009141 CONTROL UNIT BOEING 747 747422 1384935 NM F/A BUNKROOM FAILED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 177UA 24384 FAINT ELECTRICAL SMELL IN F/A BUNK ROOM. SEEMS TO BECOMING FROM RIGHT ARMREST OF AFT BUNK ROOM RIGHT SEAT. REMOVED PAR T THAT SEEMS TO HAVE OVERHEATED. PROBLEM SEEMS SOLVED, CONT TO SFO. *S/D* FOUND SEAT ELECTRONICS UNIT PCN 580-9110 OV ERHEATED. REPLACED SEU AND AUDIO CONTROLLER, OPS CHECKED OK REF MM 23-34-03-401 (AUDIO CONT = DIGITAL PASSENGER CONT U NIT). SEAT ELECTRONICS UNIT REFERENCED BELOW WAS FOUND TO HAVE A FAILED CAPACITOR IN THE POWER SUPPLY CIRCUIT CAUSING U NIT TO OVERHEAT. NO EVIDENCE OF CHARRING WAS NOTED ON CIRCUIT BOARD. 2 L 7 4 4F RT A20WE 2001072400162 20010724 00162 2001 7 24 2001UALA01123 4 20010621 A 3442 TRANSCEIVER AIRBUS 320 A320232 3930326 EU WEATHER RADAR FAILED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 429UA 539 WEATHER RADAR SYSTEM INOP. REPLACED SCANNER ANTENNA AND TRANSCEIVER. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 2001072400163 20010724 00163 NM 2001 7 24 2001UALA01124 1 20010621 A 2910 HYDRAULIC SYSTEM BOEING 757 757222 1384956 NM LEFT LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 507UA 24743 LEFT HYDRAULIC QUANTITY WENT TO ZERO. 2 L 7 2 4F RT A2NM 2001072400164 20010724 00164 NM 2001 7 24 2001UALA01126 1 20010622 A 5553 ATTACH FITTING BOEING 737 737322 1384676 NM VERTICAL STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 VERTICAL STABILIZER ATTACH LUGS CORRODED. MAJOR REPAIR ACCOMPLISHED. OVERSIZED BORES AND INSTALLED NEW BUSHINGS. 2 L 7 2 4F RT A16WE 2001072400165 20010724 00165 NM 2001 7 24 2001UALA01127 1 20010623 A 5311 FRAME BOEING 757 757222 1384956 NM FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 513UA 24810 FRAME DENTED STA 1420, BETWEEN STR 25L AND 26L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F RT A2NM 2001072400166 20010724 00166 NM 2001 7 24 2001UALA01128 1 20010625 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 513UA 24810 FLOORBEAM CORRODED STA 365, BL 0 TO RBL 64. MAJOR REPAIR ACCOMPLISHED. REPLACED UPPER T-CAP. 2 L 7 2 4F RT A2NM 2001072400167 20010724 00167 NM 2001 7 24 2001UALA01129 1 20010622 A 3350 BATTERY BOEING 747 747422 1384935 NM CABIN DISCHARGED A UALA K NONE O OTHER UK UNKNOWN 1 WP 29 172UA 24363 EMERGENCY LIGHT FLASHING AT ROW 56 AFT. REPLACED EEL BATTERY ABOVE 5R. CHECKED OK. 2 L 7 4 4F RT A20WE 2001072400168 20010724 00168 NM 2001 7 24 2001UALA01130 1 20010623 A 5315 FLOORBEAM BOEING 737 737291 138448W NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 997UA 22457 FLOORBEAM CRACKED AT BS 660. ACCOMPLISHED STRAP AND ANGLE REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F A16WE 2001072400169 20010724 00169 NM 2001 7 24 2001UALA01131 1 20010623 A 5310 SHEAR TIE BOEING 737 737291 138448W NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 997UA 22457 SHEAR TIE CRACKED AT BS 1040, BETWEEN STR 2L AND STR 3L. REPLACED SHEAR TIE. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F A16WE 2001072400170 20010724 00170 NM 2001 7 24 2001UALA01132 1 20010623 A 5320 STIFFENER BOEING 737 737291 138448W NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 997UA 22457 CABIN FLOOR UPPER STIFFENER CRACKED AFT SIDE AT BS 727, RBL 10. REPLACED STIFFENER. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F A16WE 2001072400171 20010724 00171 NM 2001 7 24 2001UALA01133 1 20010623 A 5311 FRAME BOEING 737 737291 138448W NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 997UA 22457 FRAME CRACKED AT BS 727, STR 17R. REMOVED DAMAGE. INSTALLED DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F A16WE 2001072400172 20010724 00172 NM 2001 7 24 2001UALA01134 1 20010623 A 5330 SKIN BOEING 737 737291 138448W NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 997UA 22457 FUSELAGE SKIN CRACKED BETWEEN BS 520 AND BS 540. ACCOMPLISHED DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F A16WE 2001072400174 20010724 00174 NM 2001 7 24 2001UALA01136 1 20010624 A 5312 BULKHEAD BOEING 737 737322 1384676 NM FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 WEAR DAMAGE ON OUTBOARD WEB AT BS 178, RBL 21, WL 203. ACCOMPLISHED REINFORCEMENT REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072400175 20010724 00175 NM 2001 7 24 2001UALA01137 1 20010624 A 5312 BULKHEAD BOEING 737 737322 1384676 NM FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 BULKHEAD WEB HAS EXCESSIVE MATERIAL LOSS AT BS 178, LBL 28, WL 216. ACCOMPLISHED DOUBLER REPAIR. MAJOR REPAIR ACCOMPLI SHED. 2 L 7 2 4F RT A16WE 2001072400176 20010724 00176 NM 2001 7 24 2001UALA01138 1 20010624 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 CABIN FLOORBEAM WEB HAS EXCESSIVE MATERIAL LOSS AT BS 1016, LBL 28. ACCOMPLISHED REINFORCEMENT REPAIR. MAJOR REPAIR AC COMPLISHED. 2 L 7 2 4F RT A16WE 2001072400178 20010724 00178 WP 2001 7 24 RRXA003570 1 20010105 A 5712 DOUGLAS RIB DOUG DC8 DC871F 302199D WP XW 5 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LEFT WING T/E REAR SPAR RIB AT STA XW 5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. --------CX-------- 2 L 7 4 4F RT 4A25 2001072400179 20010724 00179 WP 2001 7 24 RRXA003588 1 20010103 A 5730 DOUGLAS SKIN DOUG DC8 DC871F 302199D WP XW 106 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND A CRACK ON THE I/B SURFACE OF THE LEFT WING I/B FLAP AT STA XW 106, DAMAGE EXCEEDED LIM ITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-1 & 51-1-21A. 2 L 7 4 4F RT 4A25 2001072400180 20010724 00180 WP 2001 7 24 RRXA003591 1 20010108 A 5730 5611015502 PANEL DOUG DC8 DC873F 302199F WP XRS 340-419 DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO THE R/H WING BOTTOM T/E PANEL AT STA XRS 340 TO XRS 419, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIV ED PART AND INSTALLED IAW DC-8 SRM 51-3-0 2 L 7 4 4F RT 4A25 2001072400181 20010724 00181 WP 2001 7 24 RRXA003592 1 20010108 A 5755 57075312 FITTING DOUG DC8 DC873F 302199F WP #1 GND SPOILER CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT WING #1 GROUND SPOILER O/B MOUNT FITTING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLE D IAW DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001072400182 20010724 00182 WP 2001 7 24 RRXA003593 1 20010105 A 5755 57075312 FITTING DOUG DC8 DC873F 302199F WP I/B FITTING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE #1 GND SPOILER I/B MOUNT FITTING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.RECEIVED PART AND INSTALLED IAW DC-8 S RM 51-1-21 & 51-1-20D. 2 L 7 4 4F RT 4A25 2001072400183 20010724 00183 WP 2001 7 24 RRXA003595 1 20010106 A 5230 561667356 TRACK DOUG DC8 DC873F 302199F WP AFT TRACK CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE "D-PIT" DOOR AFT TRACK (3" CRACK), DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001072400184 20010724 00184 WP 2001 7 24 RRXA003597 1 20010102 A 5230 DOUGLAS SKIN DOUG DC8 DC873F 302199F WP AFT LWR CORNER CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE AFT LWR CORNER OF THE "D" PIT DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 52-2-0 FIG.2. 2 L 7 4 4F RT 4A25 2001072400185 20010724 00185 WP 2001 7 24 RRXA003598 1 20010102 A 5312 DOUGLAS ANGLE DOUG DC8 DC873F 302199F WP X35 Z-8 STA 1320 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT FOUND THE BULKHEAD ATTACH ANGLE BROKEN AND CRACKED ON THE AFT LWR CARGO COMPT AT STA 1320 X35 Z-8, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 5 1-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-3-0 ANS EO#00-316 WITH APPROVED 8110-3 DATED 12/18/00. 2 L 7 4 4F RT 4A25 2001072400186 20010724 00186 WP 2001 7 24 RRXA003599 1 20010102 A 5230 5648932401 DOOR DOUG DC8 DC873F 302199F WP LT MLG TOP DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANC EVISIT FOUND DELAMINATION IN 2 PLACES ON THE LEFT MLG TOP DOOR TO WING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-3-0 AND DC-8 M/M 32-12-1. 2 L 7 4 4F RT 4A25 2001072400187 20010724 00187 WP 2001 7 24 RRXA003601 1 20010102 A 5730 5611112 PANEL DOUG DC8 DC873F 302199F WP XRS 5-98 DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO THE R/H WING BOTTOM T/E PANEL AT STA XRS 5 TO XRS 98, DAMAGE EXC EEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001072400188 20010724 00188 WP 2001 7 24 RRXA003602 1 20010201 A 5730 56110161 PANEL DOUG DC8 DC873F 302199F WP XRS 419-435 DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO THE L/H WING BOTTOM T/E PANEL AT STA XRS 419 TO XRS 435, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIV ED PART AND INSTALLED IAW DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001072400242 20010724 00242 NM 2001 7 24 2001UALA01141 1 20010621 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 654 STR 37L-38L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 140T2102-221 A ND SRM 51-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400243 20010724 00243 NM 2001 7 24 2001UALA01142 1 20010621 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 1241 LBL 47 T-CAP CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 146T1208 AND SRM 51-40 -02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400244 20010724 00244 NM 2001 7 24 2001UALA01143 1 20010621 A 5347 SEAT TRACK BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 933 RBL 88 SEAT TRACK CORRODED. 2 L 7 2 4F RT A1NM 2001072400246 20010724 00246 NM 2001 7 24 2001UALA01145 1 20010621 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 566 STR 39L-39R SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 140T1202-331 A ND SRM 51-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400247 20010724 00247 NM 2001 7 24 2001UALA01146 1 20010621 A 5320 SPLICE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 434 STR 34R SPLICE CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR SRM 53-30-03 AND 51-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400248 20010724 00248 NM 2001 7 24 2001UALA01147 1 20010621 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 434 STR 38L-39L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 140T2102-317 A ND SRM 51-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400249 20010724 00249 NM 2001 7 24 2001UALA01148 1 20010621 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 566 STR 37L-38L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 140T2102-221 A ND SRM 51-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400250 20010724 00250 NM 2001 7 24 2001UALA01149 1 20010621 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 676 STR 36L-37L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 140T2102 AND S RM 51-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400251 20010724 00251 NM 2001 7 24 2001UALA01150 1 20010621 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 720 STR 38L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 140T2102-263 AND S RM 51-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400252 20010724 00252 NM 2001 7 24 2001UALA01151 1 20010621 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 346 STR 39L-39R SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 141T1221-13 AN D SRM 51-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400253 20010724 00253 NM 2001 7 24 2001UALA01152 1 20010621 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 720 STR 38R SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 140T2102-264 AND S RM 51-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400254 20010724 00254 NM 2001 7 24 2001UALA01153 1 20010621 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 368 STR 37L-38L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 140T2102 AND S RM 51-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400255 20010724 00255 NM 2001 7 24 2001UALA01154 1 20010621 A 5313 STRINGER BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 742 STR 38R CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 140T2102-253 AND SRM 51-40-0 2 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400256 20010724 00256 NM 2001 7 24 2001UALA01155 1 20010621 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 346 STR 37L-39L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 141T1221-67 AN D SRM 51-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400257 20010724 00257 NM 2001 7 24 2001UALA01156 1 20010621 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 632 STR 39R-39L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 140T2102-267 A ND SRM 51-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400259 20010724 00259 NM 2001 7 24 ASAA0110170 1 20010401 A 5200 6574583 HANDLE BOEING 737 737290C 138448V NM L2 DOOR STIFF A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - DURING MAINTENANCE CHECK, FOUND L2 DOOR HANDLE STIFF TO OPERATE. CLEANED AND LUBED HANDLE AND HANDLE OPERATED NOR MALLY. (M) 2 L 7 2 4F A16WE 2001072400260 20010724 00260 WP 2001 7 24 ASAA0180143 1 20010415 A 2500 3961899501 LANYARD DOUG DC9 DC983 3022083 WP EMERGENCY SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 982AS 53473 ANC - DURING PRE-FLIGHT CHECK, L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED FROM GIRT BAR. RE-SECURED LANYA RD. (M) 2 L 7 2 4F RT A6WE 2001072400261 20010724 00261 WP 2001 7 24 ASAA0180146 1 20010416 A 5600 5613217519 WINDOW DOUG DC9 DC982 3022082 WP COCKPIT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 967AS 49103 SEA - DURING PREFLIGHT CHECK, CAPTAINS SLIDING CLEARVIEW WINDOW WAS FOUND TO BE RUBBING ON WINDOW TRIM MAKING IT DIFFICU LT TO OPEN. TRIMMED WINDOW TRIM. WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001072400262 20010724 00262 WP 2001 7 24 ASAA0180115 1 20010321 A 5600 5613217520 WINDOW DOUG DC9 DC982 3022082 WP COCKPIT INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 951AS 49111 SEA - DURING PREFLIGHT CHECK, FIRST OFFICERS SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. LUBRICATED FORWARD LOCKING MECHAN ISM. WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001072400263 20010724 00263 WP 2001 7 24 ASAA0180113 1 20010325 A 2500 3961899501 LANYARD DOUG DC9 DC983 3022083 WP EMERGENCY SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 948AS 53021 ANC - DURING PRE-FLIGHT CHECK, L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD BETWEEN GIR T BAR AND SLIDE COVER. (M) 2 L 7 2 4F RT A6WE 2001072400264 20010724 00264 NM 2001 7 24 2001UALA01158 1 20010621 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 SHEAR TIE CORRODED BS 434 STR 39L-39R. *S/D* FABRICATED AND INSTALLED SHEAR TIE IN ACCORDANCE WITH BAC DWG 140T2102 AN D SRM 51-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400265 20010724 00265 SO 2001 7 24 RAIA00107023 1 20010706 A 5311 14521725001 SILL EMB 145 EMB145ER SO FRAME 19A CORRODED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 801HK 7620 145053 MX-STL-DURING MAINTENANCE CHECK FOUND CORROSION AFT OF FUSELAGE FRAME 19A AT LEFT B.L. 31. MAINTENANCE REPLACED SILL AFT OF FUSELAGE FRAME 19A AT LEFT B.L.31 IAW EMB145 SRM. 2 L 7 2 4F RT T00011AT 2001072400266 20010724 00266 SO 2001 7 24 RAIA00107024 1 20010708 A 5311 14522461011 DOUBLER EMB 145 EMB145ER SO FRAME 22 CORRODED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 801HK 7620 145053 MX-STL-DURING MAINTENANCE CHECK FOUND CORROSION FORWARD OF FUSELAGE FRAME 22 AT RIGHT B.L. 18. MAINTENANCE REPLACED DOUB LER AT FUSELAGE FRAME 22 AT RIGHT B.L. 18 IAW EMB145 SRM. 2 L 7 2 4F RT T00011AT 2001072400267 20010724 00267 SO 2001 7 24 RAIA00107025 1 20010706 A 5311 14522459003 SUPPORT EMB 145 EMB145ER SO FRAME 19A CORRODED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 801HK 7620 145053 MX-STL-DURING MAINTENANCE CHECK FOUND CORROSION FROM 3 INCHES FORWARD TO 4 INCHES AFT OF FUSELAGE FRAME 19A ON B.L..MAIN TENANCE REPLACED SUPPORT AT FUSELAGE FRAME 19A ON B.L. IAW EMB145 SRM. 2 L 7 2 4F RT T00011AT 2001072400268 20010724 00268 SO 2001 7 24 RAIA00107028 1 20010706 A 5320 14521725015 SILL EMB 145 EMB145ER SO FRAME 22A CORRODED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 801HK 7620 145053 MX-STL-DURING MAINTENANCE CHECK FOUND CORROSION FROM FORWARD OF FUSELAGE FRAME 22A AT RIGHT B.L.31.MAINTENANCE REPLACED FUSELAGE FRAME 22A SILL PLATE AT RIGHT B.L.31 IAW EMB145 SRM. 2 L 7 2 4F RT T00011AT 2001072400269 20010724 00269 NM 2001 7 24 2001UALA01159 1 20010621 A 5313 STRINGER BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 STR CORRODED BS 420 STR 34R. *S/D* FABRICATED AND INSTALLED STR REPAIR IN ACCORDANCE WITH SRM 53-00-03 AND 51-40-02 N- R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400270 20010724 00270 NM 2001 7 24 2001UALA01160 1 20010621 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 SHEAR TIE CORRODED BS 532 STRINGER 38L-39L. *S/D* FABRICATED AND INSTALLED SHEAR TIE IN ACCORDANCE WITH BAC DWG 140T21 02 AND SRM 51-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400300 20010724 00300 WP 2001 7 24 RRXA003799 1 20010117 A 5742 3647117U2 FITTING DOUG DC8 DC873F 302199F WP STA.960 L24L CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LT.WW BATHTUB FITTING AT STA. 960 AND L24L FWD SIDE, DAMAGE EXCEEDE D LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-0 FIG.2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072400325 20010724 00325 WP 2001 7 24 RRXA010501 1 20010215 A 5330 DOUGLAS DOUBLER DOUG DC8 DC871F 302199D WP STA XFS 435.789 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE BOTTOM CENTER DOUBLER AT STA XFS 435.789, DAMAGE EXCEEDED LIMITATIONS I AW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLE D IAW DC-8 SRM 51-1-4 & 51-1-21. 2 L 7 4 4F RT 4A25 2001072400326 20010724 00326 WP 2001 7 24 RRXA010502 1 20010215 A 5330 DOUGLAS PANEL DOUG DC8 DC871F 302199D WP STRESS PANEL CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE STRESS PANEL ON SHELF (F), DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW D C-8 SRM 53-2-0 FIG.1F. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072400327 20010724 00327 WP 2001 7 24 RRXA010504 1 20010216 A 5753 DOUGLAS PANEL DOUG DC8 DC871F 302199D WP STA 960-980 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H I/B FLAP TRACK COVER PANEL BETWEEN STA 960-980, DAMAGE EXCEEDED LIMI TATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-0 FIG.1B. 2 L 7 4 4F RT 4A25 2001072400329 20010724 00329 WP 2001 7 24 RRXA010508 1 20010222 A 5321 DOUGLAS PANEL DOUG DC8 DC871F 302199D WP #677 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AROUND PERIMETER TOP & BOTTOM EDGES OF CENTER COCKPIT FLOOR PANEL #677 CHAFF STRIP BROKEN, ELONGATED HOLES, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAM AGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4 AND 53-2-0. (CORROSION DAMAGE R ECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072400330 20010724 00330 WP 2001 7 24 RRXA010509 1 20010222 A 5321 DOUGLAS PANEL DOUG DC8 DC871F 302199D WP #681 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE COCKPIT FLOOR PANEL #661 AND CRACKED SCREW HOLES, DAMAGE EXCEED ED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED P ART AND INSTALLED IAW DC-8 SRM 53-2-0 AND 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072400331 20010724 00331 WP 2001 7 24 RRXA010510 1 20010222 A 5321 DOUGLAS PANEL DOUG DC8 DC871F 302199D WP #676D CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE EDGES OF THE FLOOR PANEL CAPT'S SIDE PANEL #676D, DAMAGE EXCEEDED LIMITA TIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND I NSTALLED IAW DC-8 SRM 51-1-4. 2 L 7 4 4F RT 4A25 2001072400332 20010724 00332 WP 2001 7 24 RRXA010517 1 20010207 A 5330 DOUGLAS BRACKET DOUG DC8 DC871F 302199D WP I/B END CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACKED BRACKET AT I/B END REPAIR NOT PER SRM, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. /////CORRECTIVE ACTION///// REMOVED DAMAGE. TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC -8 SRM 51-1-21 AND DC-8 SRM 51-1-4. 2 L 7 4 4F RT 4A25 2001072400333 20010724 00333 WP 2001 7 24 RRXA010518 1 20010207 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP STA 461.372 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA 461.372, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2001072400334 20010724 00334 WP 2001 7 24 RRXA010519 1 20010207 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP STA XFS 434.750 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE BOTTOM T/E FORMER AT STA XFS 434.750, DAMAGE EXCEEDED LIMITATIONS IAW DC -8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED I AW DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001072400335 20010724 00335 WP 2001 7 24 RRXA010520 1 20010207 A 5330 DOUGLAS DOUBLER DOUG DC8 DC871F 302199D WP STA XFS 435.789 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE BOTTOM DOUBLER AT STA XFS 435.789, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-14 & 51-1-21. 2 L 7 4 4F RT 4A25 2001072400336 20010724 00336 WP 2001 7 24 RRXA010521 1 20010207 A 5330 DOUGLAS DOUBLER DOUG DC8 DC871F 302199D WP STA XFS 435.789 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK BETWEEN THE SKIN ON THE BOTTOM DOUBLER AT STA XFS 435.789, DAMAGE EXCEEDED LIMI TATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR A ND INSTALLED IAW DC-8 SRM 57-1-14 & 51-1-21. 2 L 7 4 4F RT 4A25 2001072400338 20010724 00338 EU 2001 7 24 DHL2001365508 1 20010714 A 3610 1891201 HEAT EXCHANGER AIRBUS 300 A300B4203 3930306 EU CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH 149 On A-7check-discrepancy #2 engine pylon heat exchanger has 5" crack.1) Removed heat exchanger onCK Job Card C15R54113 pe r A 300 M/M 36-11-15.2) Installed air duct and rods per A 300 M/M 36-11-15.3) Installed serviceable #2 engine pre-cooler per A 300 amm 36-11-15 and leak checked and no leaks noted per A 300 AMM 36-11-00. 2 L 7 2 4F RT A35EU 2001072400339 20010724 00339 NM 2001 7 24 2001UALA01162 1 20010626 A 5311 FRAME BOEING 757 757222 1384956 NM FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 513UA 24810 AFT CARGO CIRCUMFERENTIAL FRAME DENTED STA 1400, BETWEEN STR 25L AND 26L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND STRAP REPAIR. 2 L 7 2 4F RT A2NM 2001072400340 20010724 00340 NM 2001 7 24 2001UALA01163 1 20010625 A 5311 FRAME BOEING 737 737322 1384676 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 LT VERTICAL WEB FRAME CRACKED AT BS 188. INSTALLED WEB REPAIR ANGLE. EXTENDED SKIN DOUBLER TO REPAIR THE SKIN CUTOUT. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072400341 20010724 00341 NM 2001 7 24 2001UALA01164 1 20010625 A 5320 FITTING BOEING 737 737322 1384676 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 AFT ENTRY DOORWAY ASSIST HANDLE FITTING AFT 2 FASTENER HOLES ARE CRACKED. ACCOMPLISHED REPAIR STRAP AND FRAME SPLICE ST RAP. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072400342 20010724 00342 NM 2001 7 24 2001UALA01165 1 20010624 A 5313 STRINGER BOEING 737 737322 1384676 NM FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 320UA 23952 STRINGER REPAIR AT FWD END OF WING SCAN LIGHT MISSING 6 HI-LOKS, AT BS 500C, STR 16L. INSTALLED U-CHANNEL INSIDE STRING ER, AND HI-LOKS. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072400344 20010724 00344 NM 2001 7 24 2001UALA01168 1 20010626 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 513UA 24810 FLOORBEAM T-CAP CORRODED STA 380, LBL 48 AND LBL 58. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED T-CAP SPLICE REPAIR. 2 L 7 2 4F RT A2NM 2001081300023 20010813 00023 NM 2001 8 13 2001UALA01169 1 20010625 A 2781 189915 PROXIMITY SENSOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE L/E FLAP FAULTY A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 388UA 24663 TAKEOFF ABORTED DUE TO FLAP TAKEOFF WARNING CONFIGURATION HORN. FOUND NR 4 LE FLAP INTRANSIT LIGHT ON, ON OVHD & FWD PNL . FOUND WHEN FLAPS DOWN AND TAPPED S175 LIGHTS WENT BETWEEN TRANSIT AND GREEN EXTEND. REPLACED S175 AND TESTED SEVERAL T IMES WITH ALL INDICATIONS NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2001102600016 20011026 00016 NM 2001 10 26 2001UALA01173 1 20010625 A 7603 CONTROL CABLE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE THROTTLE OUT OF ADJ A UALA O OTHER O OTHER CR CRUISE 1 WP 29 609UA 21870 THROTTLES FAILED TO MOVE TOGETHER DURING A-T OPERATION. RIGHT THROTTLE LAGS REF MM 76-11-00 P200A, 201 TO CORRECT HIGH THROTTLE FORCES OR CLUTCH PACK SLIP. ADJUSTED PUSH PULL CABLE. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E3NE 2001072400345 20010724 00345 NM 2001 7 24 2001UALA01174 1 20010626 A 5312 BULKHEAD BOEING 737 737522 138449F NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 911UA 25255 BULKHEAD HAS CRACKS AT 4 RADAR MOUNT ATTACH BRACKETS, AT BS 178. REMOVED DAMAGE. INSTALLED DOUBLER. MAJOR REPAIR ACCO MPLISHED. 2 L 7 2 4F RT A16WE 2001072400346 20010724 00346 NM 2001 7 24 2001UALA01175 1 20010626 A 5312 BULKHEAD BOEING 737 737322 1384676 NM FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 BULKHEAD WEB HAS OIL CANNING AND DENTED AND PUCKERED FASTENER HOLES, AT BS 178. ACCOMPLISHED DOUBLER REPAIR. MAJOR REP AIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072400347 20010724 00347 NM 2001 7 24 2001UALA01176 1 20010626 A 5312 BULKHEAD BOEING 737 737322 1384676 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 BULKHEAD WEB EXTERIOR SURFACE CRACKED AT FASTENER, AT BS 178, WL 234, LBL 12. ACCOMPLISHED DOUBLER REPAIR. MAJOR REPAI R ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072400348 20010724 00348 NM 2001 7 24 2001UALA01177 1 20010626 A 5312 BULKHEAD BOEING 737 737322 1384676 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 BULKHEAD WEB HAS CRACK AT 4 RADAR ANTENNA MOUNTS, AT BS 178, WL 207, BL 0. ACCOMPLISHED DOUBLER REPAIR. MAJOR REPAIR A CCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072400349 20010724 00349 NM 2001 7 24 2001UALA01178 1 20010626 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 STRINGER-FRAME CLIP CRACKED AT BS 663.75, STR 11L. REPLACED STRINGER CLIP. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072400350 20010724 00350 NM 2001 7 24 2001UALA01179 1 20010626 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 STRINGER-FRAME CLIP CRACKED AT BS 663.75, STR 10R. REPLACED STRINGER CLIP. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072400351 20010724 00351 NM 2001 7 24 2001UALA01180 1 20010626 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 STRINGER CLIP CRACKED AT BS 597, STR 2L. REPLACED STRINGER CLIP. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072400352 20010724 00352 NM 2001 7 24 2001UALA01181 1 20010626 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 STRINGER CLIP CRACKED AT BS 597, STR 3L. REPLACED STRINGER CLIP. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001081500089 20010815 00089 NM 2001 8 15 01FDEA00541 1 20010706 A 5313 STRINGER BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 221FE 20932 PILLOWING AROUND FASTENER IN CHANNEL OF STR 28L, BS 486 (C53-113-01,1). *S/D* REMOVED AND REPLACED STR PER IAW FED EX SRM 53-10-3. 2 L 7 3 4F RT A3WE 2001072400353 20010724 00353 NM 2001 7 24 2001UALA01182 1 20010626 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 CABIN FLOORBEAM CLIP CRACKED AT BS 328, RBL 32, WL 200. REPLACED CLIP. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072400354 20010724 00354 NM 2001 7 24 2001UALA01183 1 20010626 A 5310 STOP FITTING BOEING 737 737322 1384676 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 AFT GALLEY DOORWAY STOP FITTING, 2 LOWER AFT FASTENER HOLES OF DOOR ASSIST HANDLE HAVE CRACKS. ACCOMPLISHED FRAME SPLIC E STRAP REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072400355 20010724 00355 NM 2001 7 24 2001UALA01184 1 20010626 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 LT MID CABIN UPPER T-CHORD CRACKED LATERALLY IN VERTICAL LEG, JUST BELOW UPPER RADIUS FILLER, AT BS 520, LBL 24. ACCOMP LISHED ANGLE REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072400356 20010724 00356 NM 2001 7 24 2001UALA01185 1 20010626 A 5312 BULKHEAD BOEING 737 737322 1384676 NM FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 BS 178 BULKHEAD WEB HAS WEAR DAMAGE AT WL 218 O/B EDGE, AND OIL CANNING AT WL 203, RBL 21 ABOVE ACCESS HOLE. ACCOMPLISH ED DOUBLER AND TRIPLER REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072400357 20010724 00357 NM 2001 7 24 2001UALA01186 1 20010626 A 5311 FRAME BOEING 737 737322 1384676 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 320UA 23952 FUSELAGE FRAME LOWER FASTENER CRACKED LT SIDE AT BS 616. REMOVED DAMAGE. INSTALLED STIFFENER ANGLE. MAJOR REPAIR ACCO MPLISHED. 2 L 7 2 4F RT A16WE 2001072400358 20010724 00358 NM 2001 7 24 2001UALA01187 1 20010626 A 5311 FRAME BOEING 737 737322 1384676 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 320UA 23952 FORWARD PIT FRAME CRACKED AROUND TOP FASTENER, AT BS 500, LBL 1. REMOVED DAMAGE. INSTALLED REPAIR ANGLE. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072400359 20010724 00359 NM 2001 7 24 2001UALA01188 1 20010624 A 3610 CONTROL VALVE BOEING 727 727222 1384073 NM PNEUMATIC SYS FAILED A UALA O OTHER O OTHER CR CRUISE 1 WP 29 7261U 21408 AIRCRAFT UNABLE TO MAINTAIN PRESSURIZATION DURING CRUISE AT FL250. *S/D* RIGHT FLOW MODULATING VALVE WOULD NOT CLOSE. REPLACED FLOW CONTROL MODULATING VALVE. OPERATIONS CHECK NORMAL. 2 L 7 3 4F A3WE 2001081300024 20010813 00024 NM 2001 8 13 2001UALA01189 1 20010624 A 3350 900542U1 LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7270U 21417 FORWARD LOWER CEILING EMERGENCY LIGHT IS INOPERABLE. EMERGENCY LIGHT ASSY FAILED. REPLACED BATTERIES AND LAMPS, NO HEL P, REPLACED LIGHT. ASSEMBLY OPERATION IS NOW NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001072400360 20010724 00360 WP 2001 7 24 RRXA010525 1 20010207 A 2750 DOUGLAS LINK DOUG DC8 DC871F 302199D WP STA 98 GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A GOUGE AT UPPER END OF THE AFT FLAP DRIVE LINK AT STA 98, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTA LLED IAW E.O.#01-024 WITH APPROVED 8110-3 DATED 02/09/01. 2 L 7 4 4F RT 4A25 2001072400361 20010724 00361 WP 2001 7 24 RRXA010529 1 20010208 A 5730 DOUGLAS PANEL DOUG DC8 DC871F 302199D WP STA 80 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK AT SCREW HOLE TO THE UPPER WING PANEL AT STA 80, DAMAGE EXCEEDED LIMITATIONS IA W DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALL ED IAW DC-8 SRM 51-1-21 AND DC-8 SRM 57-2-0 FIG. 2A. 2 L 7 4 4F RT 4A25 2001072400362 20010724 00362 WP 2001 7 24 RRXA010531 1 20010206 A 5313 DOUGLAS SHIM DOUG DC8 DC871F 302199D WP L32R STA 1793 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE SHIM UNDER LONGERON 32R INSIDE ACCESS HOLE #60 AT STA 1793, DAMAGE EXCEE DED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW E.O.#01-024 WITH APPROVED 8110-3 DATED 02/23/01. 2 L 7 4 4F RT 4A25 2001072400363 20010724 00363 WP 2001 7 24 RRXA010533 1 20010212 A 5730 56110172 PANEL DOUG DC8 DC871F 302199D WP STA XW 106 DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE R/H WING LWR SURFACE FWD OF I/B FLAP STOP PANEL AT STA XW 106, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001072400364 20010724 00364 WP 2001 7 24 RRXA010535 1 20010212 A 5730 DOUGLAS PANEL DOUG DC8 DC871F 302199D WP STA 485 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE R/H #4 ALT 505B CAN'T WEB PANEL AT STA 485, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALL ED IAW DC-8 SRM 51-1-21 &57-2-0 FIG.2A. 2 L 7 4 4F RT 4A25 2001072400365 20010724 00365 WP 2001 7 24 RRXA010536 1 20010213 A 5730 DOUGLAS PANEL DOUG DC8 DC871F 302199D WP L/H WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H #1 ALT INSIDE TANK FWD OF MIDSPAR 485 CAN'T WEB PANEL, DAMAGE EXCEED ED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED R EPAIR AND INSTALLED IAW DC-8 SRM 57-2-0 FIG.2A & 51-1-21. 2 L 7 4 4F RT 4A25 2001072400366 20010724 00366 WP 2001 7 24 RRXA010537 1 20010131 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP STA XS 255 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XS 255, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SR M 57-2-0. 2 L 7 4 4F RT 4A25 2001072400367 20010724 00367 WP 2001 7 24 RRXA010539 1 20010131 A 5330 DOUGLAS DOUBLER DOUG DC8 DC871F 302199D WP STA XS 220.190 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP DOUBLER ABOUT 2" AT STA XS 220.190, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED I AW DC-8 SRM 51-3-0 AND DC-8 SRM 51-1-21 DC-8 DWG. 5769869 AND E.O.#01-024. 2 L 7 4 4F RT 4A25 2001072400368 20010724 00368 WP 2001 7 24 RRXA010540 1 20010131 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP STA XS 213.750 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XS 213.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC -8 SRM 51-1-21 2 L 7 4 4F RT 4A25 2001072400369 20010724 00369 WP 2001 7 24 RRXA010542 1 20010131 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP STA XFS 616.250 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA 616.250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21 & 57-2-0. 2 L 7 4 4F RT 4A25 2001072400370 20010724 00370 WP 2001 7 24 RRXA010543 1 20010131 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP STA XFS 635 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XFS 635, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0 & 51-1-21. 2 L 7 4 4F RT 4A25 2001072400371 20010724 00371 WP 2001 7 24 RRXA010544 1 20010131 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP XFS 641.250 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XFS 641.250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW D C-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001072400372 20010724 00372 WP 2001 7 24 RRXA010546 1 20010131 A 5330 DOUGLAS SKIN DOUG DC8 DC871F 302199D WP XFS 141.250-147. CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A 1 1/2" CRACK IN THE TOP L/E SKIN AND TWO DENTS BETWEEN STA XFS 141.250 TO STA XFS 147 .500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 5 1-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21 AND PRC1422-B-2. 2 L 7 4 4F RT 4A25 2001072400373 20010724 00373 WP 2001 7 24 RRXA010547 1 20010131 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP STA XS 213.750 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XS 213.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2001072400374 20010724 00374 WP 2001 7 24 RRXA010549 1 20010131 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP STA XS 250.089 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A 2 1/2" CRACK TO THE TOP FORMER AT STA XS 250.089, DAMAGE EXCEEDED LIMITATIONS IAW DC- 8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IA W DC-8 SRM 51-3-0 AND DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001072400375 20010724 00375 WP 2001 7 24 RRXA010550 1 20010131 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP XFS 255 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XFS 255, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC- 8 SRM 51-3-0 AND DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001072400376 20010724 00376 WP 2001 7 24 RRXA010551 1 20010131 A 5730 DOUGLAS ANGLE DOUG DC8 DC871F 302199D WP XS 195 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE ANGLE AT FORMER AT STA XS 195, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001072400377 20010724 00377 WP 2001 7 24 RRXA010554 1 20010131 A 5330 DOUGLAS SKIN DOUG DC8 DC871F 302199D WP XFS 253.150 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A 1" CRACK TO THE BOTTOM SKIN AT CUT-OUT FOR PYLON AT STAY XFS 253.150, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PAR T AND INSTALLED IAW DC-8 SRM 57-2-1A. 2 L 7 4 4F RT 4A25 2001072400378 20010724 00378 WP 2001 7 24 RRXA010556 1 20010131 A 5730 DOUGLAS ANGLE DOUG DC8 DC871F 302199D WP STA XS 225 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A 1" CRACK TO THE ANGLE AT CAP AT STA XS 225, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED ARE IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SR M 51-1-4 AND DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001072400379 20010724 00379 WP 2001 7 24 RRXA010558 1 20010131 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP STA XS 251.089 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A 6" CRACK TO THE TOP FORMER AT STA XS 251.089, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SR M. /////CORRECTIVE ACTIVE///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC- 8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2001072400380 20010724 00380 WP 2001 7 24 RRXA010559 1 20010130 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP STA 104.750 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT SIDE T/E FORMER AT STA 104.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2001072400381 20010724 00381 WP 2001 7 24 RRXA010560 1 20010130 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP STA ZFS 110 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT SIDE T/E FORMER AT STA ZFS 110, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2001072400382 20010724 00382 WP 2001 7 24 RRXA010562 1 20010130 A 5313 DOUGLAS STRINGER DOUG DC8 DC871F 302199D WP STR #54 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE CAN'T LWR STR #54 ON THE R/H 505B INSIDE TANK AND O/B BETWEEN STA XRS 49 5 AND 508, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW E.O.#01-024 WITH APPROVED 8110-3 DATED 03/10/01. 2 L 7 4 4F RT 4A25 2001072400383 20010724 00383 WP 2001 7 24 RRXA010563 1 20010130 A 5710 DOUGLAS FITTING DOUG DC8 DC871F 302199D WP X+69" STA 879 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE CENTER WING FRAME FITTING AT STA 879 X+69", DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTAL LED IAW DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001072400384 20010724 00384 WP 2001 7 24 RRXA010564 1 20010130 A 5710 DOUGLAS FRAME DOUG DC8 DC871F 302199D WP X+69" STA 860 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CENTER WING FRAME FITTING AT STA 860 X+68", DAMAGE EXCEEDED L IMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-24 AND DC-8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072400385 20010724 00385 WP 2001 7 24 RRXA010566 1 20010130 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP STA 448.581 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA 448.581, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2001072400386 20010724 00386 WP 2001 7 24 RRXA010567 1 20010130 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP XFS 448.581 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP FORMER AT STA XFS 448.581, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2001072400387 20010724 00387 WP 2001 7 24 RRXA010570 1 20010130 A 5730 DOUGLAS ANGLE DOUG DC8 DC871F 302199D WP XFS 188.750 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE O/B TOP GUSSET ANGLE AT STA XFS 188.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21 2 L 7 4 4F RT 4A25 2001072400388 20010724 00388 WP 2001 7 24 RRXA010571 1 20010130 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP XFS 145 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE O/B BOTTOM T/E FORMER AT STA XFS 145, DAMAGE EXCEEDED LIMITATIONS IAW DC -8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001072400389 20010724 00389 WP 2001 7 24 RRXA010572 1 20010130 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP STA XS 235 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A 8" CRACK TO THE TOP I/B FORMER AT STA XS 253, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SR M. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC -8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2001072400390 20010724 00390 WP 2001 7 24 RRXA010573 1 20010130 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP STA XS 520 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A 1" CRACK TO THE TOP I/B FORMER AT STA XS 520, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SR M. ----------CX---------- (NO CRACK) 2 L 7 4 4F RT 4A25 2001072400391 20010724 00391 WP 2001 7 24 RRXA010575 1 20010130 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP STA ZFS 98 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT SIDE T/E FORMER AT STA ZFS 98, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW D C-8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2001072400392 20010724 00392 WP 2001 7 24 RRXA010577 1 20010119 A 5730 DOUGLAS SKIN DOUG DC8 DC871F 302199D WP O/B END DENTED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A DENT AT O/B END OF THE L/E WITH BODY PUTTY INSTALLED, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. ----------CX---------- (WITHIN LIMITS) 2 L 7 4 4F RT 4A25 2001072400393 20010724 00393 WP 2001 7 24 RRXA010579 1 20010119 A 5730 DOUGLAS SKIN DOUG DC8 DC871F 302199D WP STA 23.750 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE I/B END AT STA XFS 23.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. -----------------CX--------------(WITHIN LIMITS) 2 L 7 4 4F RT 4A25 2001072400394 20010724 00394 WP 2001 7 24 RRXA010582 1 20010119 A 5347 DOUGLAS INTERCOSTAL DOUG DC8 DC871F 302199D WP XFS 163.750 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE INTERCOSTAL AT STA XFS 163.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM . /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001072400395 20010724 00395 WP 2001 7 24 RRXA010599 1 20010122 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP TOP T/E XFS 735 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XFS 735, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0 2 L 7 4 4F RT 4A25 2001072400396 20010724 00396 WP 2001 7 24 RRXA010600 1 20010122 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP TOP T/E XFS 797. CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XFS 797.500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2001072400397 20010724 00397 WP 2001 7 24 RRXA010601 1 20010122 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP XS 478.897 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XS 478.897, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC- 8 SRM 57-2-0 & 51-1-21 & 51-1-20D. 2 L 7 4 4F RT 4A25 2001072400398 20010724 00398 WP 2001 7 24 RRXA010602 1 20010122 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP XS 467.323 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XS 467.323, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC- 8 SRM 57-2-0 & 51-1-21 & 51-1-20D. 2 L 7 4 4F RT 4A25 2001072400399 20010724 00399 WP 2001 7 24 RRXA010603 1 20010122 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP XS 461.372 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XS 461.372, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW D C-8 SRM 57-2-0 & 51-1-21 & 51-1-20D. 2 L 7 4 4F RT 4A25 2001072400400 20010724 00400 WP 2001 7 24 RRXA010604 1 20010122 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP STA XS 454.976 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XS 454.976, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW D C-8 SRM 57-2-0 & 51-1-21 & 51-1-20D. 2 L 7 4 4F RT 4A25 2001072400401 20010724 00401 WP 2001 7 24 RRXA010605 1 20010122 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP STA XS 442.185 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XS 442.185, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC- 8 SRM 57-2-0 & 51-1-21 & 51-1-20D. 2 L 7 4 4F RT 4A25 2001072400402 20010724 00402 WP 2001 7 24 RRXA010606 1 20010122 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP STA XFS 372.750 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XFS 372.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC -8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2001072400403 20010724 00403 WP 2001 7 24 RRXA010607 1 20010122 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP STA XFS 304.000 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XFS 304.000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC -8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2001072400404 20010724 00404 WP 2001 7 24 RRXA010608 1 20010122 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP STA XFS 297.500 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XFS 297.500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW D C-8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2001072400405 20010724 00405 WP 2001 7 24 RRXA010615 1 20010123 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP XFS 653.750 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XFS 653.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2001072400406 20010724 00406 WP 2001 7 24 RRXA010616 1 20010123 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP XFS 826.750 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE BOTTOM T/E FORMER AT STA XFS 828.750, DAMAGE EXCEEDED LIMITATIONS IAW DC -8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED I AW DC-8 SRM 57-2-0 & 51-1-21. 2 L 7 4 4F RT 4A25 2001072400407 20010724 00407 WP 2001 7 24 RRXA010617 1 20010123 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP STA XFS 835 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XFS 835, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001072400408 20010724 00408 WP 2001 7 24 RRXA010618 1 20010123 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP STA XFS 772.500 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XFS 772.500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0 & 51-1-21. 2 L 7 4 4F RT 4A25 2001072400409 20010724 00409 WP 2001 7 24 RRXA010619 1 20010123 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP STA XFS 304.000 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE BOTTOM T/E FORMER AT STA XFS 304.000, DAMAGE EXCEEDED LIMITATIONS IAW DC -8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED I AW DC-8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2001072400410 20010724 00410 WP 2001 7 24 RRXA010620 1 20010123 A 5321 DOUGLAS INTERCOSTAL DOUG DC8 DC871F 302199D WP XFS 335.250 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE INTERCOSTAL AT STA XFS 335.250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM . /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2001072400411 20010724 00411 WP 2001 7 24 RRXA010623 1 20010123 A 5730 DOUGLAS ANGLE DOUG DC8 DC871F 302199D WP XFS 427 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE ANGLE AT FORMER AT STA XFS 427, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM . /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21 & 51-3-0. 2 L 7 4 4F RT 4A25 2001072400412 20010724 00412 WP 2001 7 24 RRXA010625 1 20010123 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP XFS 385.250 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE BOTTOM T/E FORMER AT STA XFS 385.250, DAMAGE EXCEEDED LIMITATIONS IAW DC -8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2001072400413 20010724 00413 WP 2001 7 24 RRXA010636 1 20010125 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP XS 478.897 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XS 478.897, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW D C-8 57-2-0. 2 L 7 4 4F RT 4A25 2001072400414 20010724 00414 WP 2001 7 24 RRXA010637 1 20010125 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP XS 461.372 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XS 461.372, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW D C-8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2001072400415 20010724 00415 WP 2001 7 24 RRXA010638 1 20010125 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP XS 448.581 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XS 448.581, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW D C-8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2001072400416 20010724 00416 WP 2001 7 24 RRXA010639 1 20010126 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP XS 442.185 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XS 442.185, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW D C-8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2001072400417 20010724 00417 WP 2001 7 24 RRXA010640 1 20010125 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP XFS 366.500 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XFS 366.500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2001072400418 20010724 00418 WP 2001 7 24 RRXA010641 1 20010125 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP XFS 329 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XFS 329, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PARTS AND INSTALLED IAW DC-8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2001072400419 20010724 00419 WP 2001 7 24 RRXA010642 1 20010125 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP STA 316.500 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA 316.500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 S RM 57-2-0. 2 L 7 4 4F RT 4A25 2001072400420 20010724 00420 WP 2001 7 24 RRXA010643 1 20010125 A 5730 DOUGLAS DOUBLER DOUG DC8 DC871F 302199D WP XFS 195 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK ABOUT 3" AT T/E ON THE BOTTOM DOUBLER AT STA XFS 195, DAMAGE EXCEEDED LIMITATIO NS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INST ALLED IAW DC-8 SRM 51-1-21 AND 51-1-4. 2 L 7 4 4F RT 4A25 2001072400421 20010724 00421 WP 2001 7 24 RRXA010644 1 20010125 A 5730 DOUGLAS SKIN DOUG DC8 DC871F 302199D WP XFS 422.720-335. CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON INTERNAL SKIN AT TOP DE-ICER VENT HOLES AT STA 422.750 TO XFS 335.2 50, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. ----------CX---------- 2 L 7 4 4F RT 4A25 2001072400422 20010724 00422 WP 2001 7 24 RRXA010645 1 20010125 A 5730 DOUGLAS STRINGER DOUG DC8 DC871F 302199D WP STA XRS 495-508 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE CAN'T #55 LOWER STRINGER ON THE L/H UPPER WING INSIDE TANK OF 505B O/B B ETWEEN STA XRS 495 & 508, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW E.O.#01-024 WITH APPROVED 8110-3 DATED 01/31/01. 2 L 7 4 4F RT 4A25 2001072400423 20010724 00423 WP 2001 7 24 RRXA010646 1 20010125 A 5730 DOUGLAS STRINGER DOUG DC8 DC871F 302199D WP XRS 495-508 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE CAN'T #54 STRINGER AT L/H UPPER INSIDE TANK OF 505B BETWEEN STA XRS 495- 508, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51 -1-8. FABRICATED PART AND INSTALLED IAW E.O.#01-024 WITH APPROVED 8110-3 DATED 01/31/01. 2 L 7 4 4F RT 4A25 2001072400424 20010724 00424 WP 2001 7 24 RRXA010647 1 20010125 A 5730 DOUGLAS STRINGER DOUG DC8 DC871F 302199D WP STR 51 XRS 429 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE CLIP ON STR #51 L/H UPPER INSIDE TANK OF 506A O/B BETWEEN STA XRS 428 LW R STRINGER CLIP BETWEEN LWR REAR SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DA MAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW E.O.#01-024 WITH APPROVED 8110-3 DATED 02/06/0 1. 2 L 7 4 4F RT 4A25 2001072400425 20010724 00425 WP 2001 7 24 RRXA010648 1 20010125 A 5730 DOUGLAS FITTING DOUG DC8 DC871F 302199D WP XRS 428 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE UPPER I/B ATTACH FITTING ON THE L/H UPPER INSIDE TANK OF 506A O/B AT STA XRS 428, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 S RM 51-1-8. FABRICATED PART AND INSTALLED IAW E.O.#01-024 WITH APPROVED 8110-3 DATED 02/06/01 AND DC-8 SRM 51-1-20 & MM2 7-51-12. 2 L 7 4 4F RT 4A25 2001072400426 20010724 00426 WP 2001 7 24 RRXA010651 1 20010126 A 5313 DOUGLAS LONGERON DOUG DC8 DC871F 302199D WP L24L UPPER MILL CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK IN UPPER MIL STOP APPROX 1/4" LONG AT LONGERON 24L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INST ALLED IAW E.O.#01-024 WITH APPROVED 8110-3 DATED 01/29/01. 2 L 7 4 4F RT 4A25 2001072400427 20010724 00427 WP 2001 7 24 RRXA010652 1 20010126 A 5730 DOUGLAS FITTING DOUG DC8 DC871F 302199D WP STA 5 GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A GOUGE ABOVE THE L/H FLAP TRACK FITTING & MILL STOP AT STA 5, DAMAGE EXCEEDED LIMITATI ONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INST ALLED IAW DC-8 SRM 51-3-0 AND E.O.#01-024 WITH APPROVED 8110-3 DATED 01/29/01. 2 L 7 4 4F RT 4A25 2001072400428 20010724 00428 WP 2001 7 24 RRXA010654 1 20010126 A 5330 DOUGLAS SKIN DOUG DC8 DC871F 302199D WP Y-66 Z-11 X-12 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND POPPED RIVETS BETWEEN FRAMES -12 & -32 R/H O/B EDGE OF COCKPIT FLO OR X-12 TO -32 Y-66" Z-11, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATE D AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.#01-024 WITH APPROVED 8110-3 DATED 01/31/01. (CORROS ION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072400429 20010724 00429 WP 2001 7 24 RRXA010656 1 20010126 A 5340 5691310013N FITTING DOUG DC8 DC871F 302199D WP L36L-L35L FS1690 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE AFT ACC SUPPORT FITTING AT STA 1690 BETWEEN L36L TO L35L, DAMAGE EXCEEDE D LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-21 & 53-2-5 & 51-1-20D. 2 L 7 4 4F RT 4A25 2001072400430 20010724 00430 WP 2001 7 24 RRXA010657 1 20010118 A 5730 DOUGLAS SPOILER PANEL DOUG DC8 DC871F 302199D WP I/B END #5 SPOIL TORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A TEAR TO THE I/B END OF RT WING O/B FLIGHT SPOILER LWR EDGE TRIM, DAMAGE EXCEEDED LIMI TATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001072400431 20010724 00431 WP 2001 7 24 RRXA010658 1 20010116 A 5330 DOUGLAS ANGLE DOUG DC8 DC871F 302199D WP RBL 3 1/2" FS940 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE R/H RIB ATTACH ANGLE KEEP BEAM BETWEEN MAIN GEAR DOORS AT STA 940 RBL 3 1/2", DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 5 1-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D & 51-1-4. 2 L 7 4 4F RT 4A25 2001072400432 20010724 00432 WP 2001 7 24 RRXA010659 1 20010118 A 5330 DOUGLAS SKIN DOUG DC8 DC871F 302199D WP RBL 3 1/2" FS940 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SKIN R/H AFT FILLET AREA BETWEEN STA 1100-1080 L29R TO L31R, DA MAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. ---------------CX--------------- (WITHIN LIMITS) 2 L 7 4 4F RT 4A25 2001072400433 20010724 00433 WP 2001 7 24 RRXA010660 1 20010119 A 5330 DOUGLAS SKIN DOUG DC8 DC871F 302199D WP L31L-L29L FS1080 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SKIN BETWEEN STA 1080-1100 BETWEEN L31L TO L29L, DAMAGE EXCEEDE D LIMITATIONS IAW DC-8 SRM. ---------------CX--------------- (WITHIN LIMITS) 2 L 7 4 4F RT 4A25 2001072400434 20010724 00434 WP 2001 7 24 RRXA010665 1 20010118 A 5347 DOUGLAS SEAT TRACK DOUG DC8 DC871F 302199D WP X-45" FS 120-140 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND EXCESSIVE WEAR TO THE SEAT TRACK AT STA 120-140 X-45", DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED I AW DC-8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 2001072400435 20010724 00435 WP 2001 7 24 RRXA010668 1 20010118 A 5330 DOUGLAS SKIN DOUG DC8 DC871F 302199D WP L36 FS 1160-1140 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SKIN & DOUBLER AT STA 1160-1140 L36, DAMAGE EXCEEDED LIMITATION S IAW SC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INS TALLED IAW E.O.#01-024 WITH APPROVED 8110-3 DATED 02/02/01. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072400436 20010724 00436 WP 2001 7 24 RRXA010669 1 20010118 A 5330 DOUGLAS SKIN DOUG DC8 DC871F 302199D WP L35L FS1160-1170 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SKIN AND DOUBLER AT STA 1160-1170 L35L, DAMAGE EXCEEDED LIMITAT IONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O#01-024 WITH APPROVED 8110-3 DATED 02/02/01. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072400437 20010724 00437 WP 2001 7 24 RRXA010670 1 20010118 A 5330 DOUGLAS SKIN DOUG DC8 DC871F 302199D WP L36 FS 1160-1170 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMGE INSIDE LIGHT HOLE TO THE SKIN AND DOUBLER AT STA 11160-1170 L36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRI CATED REPAIR AND INSTALLED IAW E.O.#01-024 WITH APPROVED 8110-3 DATED 02/02/01. (CORROSION DAMAGE RECORDED IN EWA CORROS ION PROGRAM). 2 L 7 4 4F RT 4A25 2001072400438 20010724 00438 WP 2001 7 24 RRXA010671 1 20010118 A 5330 DOUGLAS SKIN DOUG DC8 DC871F 302199D WP L35L FS1160-1170 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SKIN AND DOUBLER AT STA 1160 TO 1170 L35L, DAMAGE EXCEEDED LIMI TATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR A ND INSTALLED IAW E.O.#01-024 WITH APPROVED 8110-3 DATED 02/02/01. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072400439 20010724 00439 WP 2001 7 24 RRXA010672 1 20010227 A 5330 DOUGLAS DOUBLER DOUG DC8 DC871F 302199D WP "A-PIT" STA 292 BENT A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A BENT UPPER FWD CORNER TO THE DOUBLER FOR "A-PIT" CUTOUT AT STA 292, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-7 AND DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001072400440 20010724 00440 WP 2001 7 24 RRXA010673 1 20010227 A 5330 DOUGLAS DOUBLER DOUG DC8 DC871F 302199D WP A-PIT FS320-333 BENT A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A BENT TO THE UPPER FWD CORNER ON THE DOUBLER FOR "A-PIT" CUTOUT AT STA 320-333, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRI CATED PART AND INSTALLED IAW DC-8 SRM 51-1-7 & 51-1-21. 2 L 7 4 4F RT 4A25 2001072400441 20010724 00441 WP 2001 7 24 RRXA010683 1 20010228 A 5330 DOUGLAS PANEL DOUG DC8 DC871F 302199D WP L/H STA1540-1620 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE CUSP LINE PANEL AT STA 1540-1620 L/H, DAMAGE EXCEEDED LIMITATIONS IAW DC -8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001072400442 20010724 00442 WP 2001 7 24 RRXA010684 1 20010228 A 5321 DOUGLAS PANEL DOUG DC8 DC871F 302199D WP PANEL #329 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE GALLEY FLOOR PANEL AT TOP SURFACE PANEL #329, DAMAGE EXCEEDED L IMITATIONS IAAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072400443 20010724 00443 WP 2001 7 24 RRXA010686 1 20010228 A 5315 4708471 FITTING DOUG DC8 DC871F 302199D WP RBL -24" STA 300 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE FLOOR BEAM SUPPORT FITTING AT STA 300 AND RBL -24", DAMAGE EXCEEDED LIMI TATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND I NSTALLED IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001072400444 20010724 00444 WP 2001 7 24 RRXA010687 1 20010228 A 5330 DOUGLAS ANGLE DOUG DC8 DC871F 302199D WP "C-PIT" R/H AFT BROKEN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND THE "C-PIT" ANGLE BROKEN IN HALF (AFT R/H), DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SR M 51-1-4 AND DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001081300025 20010813 00025 NM 2001 8 13 2001UALA01190 1 20010624 A 5753 65413331600 ROLLER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE T/E FLAP SHEARED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 29 7277U 21424 CREW RECEIVED A SPLIT FLAP INDICATION WHILE RETRACTING FLAPS AFTER CLIMBOUT. AIRCRAFT DIVERTED TO EWR. FOUND ROLLERS ON TOGGLE ASSEMBLY FOR THE RT INBOARD FLAP TRACK SHEARED OFF. REPLACED TOGGLE ASSY. 2 L 7 3 4F 4 F A3WE E2EA 2001072400445 20010724 00445 NM 2001 7 24 2001UALA01191 1 20010623 A 5330 STRAP BOEING 727 727222 1384073 NM FUSELAGE TORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7275U 21422 TEAR STRAP UNDER SKIN IS TORN JUST FORWARD OF RT FUSELAGE JACK POINT. FABRICATED TEAR STRAP DOUBLER AND TRIPLER PER SRM 53-30-04 FIG 6. LOCATED STA 351 AND STRINGER 21R. CORRODED SKIN SUPPORT BRACKET REPLACED DURING REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 3 4F A3WE 2001072400446 20010724 00446 NE 2001 7 24 2001UALA01192 2 20010617 A 7200 ENGINE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 OVERTEMP A UALA O OTHER M OVER TEMP TO TAKEOFF 1 WP 29 7255U 21402 CREW REPORTS NR 2 EGT NEARING 620 DEGREES ON TAKEOFF. REDUCED POWER TO KEEP EGT WITHIN LIMITS. 2 L 7 3 4F 4 F A3WE E2EA 2001072400447 20010724 00447 NM 2001 7 24 2001UALA01193 1 20010626 A 5520 CHANNEL BOEING 727 727222 1384073 NM ELEVATOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7442U 21896 LT ELEVATOR INTERNAL SUPPORT CHANNEL IS CRACKED IN HALF AT STA 120. REPLACED CHANNEL PER GNMM 1-0-0-23. MAJOR REPAIR A CCOMPLISHED. 2 L 7 3 4F A3WE 2001072400448 20010724 00448 2001 7 24 2001UALA01194 4 20010608 A 2565 SLIDE BOEING 777 777222 1385219 NM CABIN FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 787UA 26939 SLIDE RAFT FAILED AIR RETENTION TEST DURING OVERHAUL. 2 L 7 2 4F RT T0001SE 2001072400449 20010724 00449 2001 7 24 2001UALA01195 4 20010621 A 2565 SLIDE AIRBUS 320 A320232 3930326 EU CABIN FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 433UA 589 SLIDE FAILED AIR RETENTION TEST DURING OVERHAUL. 2 L 7 2 4F RT A28NM 2001072400450 20010724 00450 2001 7 24 2001UALA01197 4 20010622 A 3417 HG2060AD01 COMPUTER BOEING 777 777222 1385219 NM E/E BAY FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 204UA 28713 RETURNED TO FIELD. NAV ADIRU INERTIAL YELLOW CAUTION ON EICAS. DUMPED FUEL TO MAX LANDING WEIGHT. NORMAL LANDING. *S /D* THE ADIRU FAILED AND CAUSED THE NAV ADIRU INERTIAL YELLOW CAUTION MESSAGE ON THE EICAS. THE ADIRU WAS REPLACED AND THIS CORRECTED THE PROBLEM. NO OTHER FAULTS HAVE BEEN REPORTED FOR THIS SYSTEM SINCE THE ADIRU WAS REPLACED. THE REMO VED ADIRU WILL BE SENT TO HONEYWELL FOR ANALYSIS. 2 L 7 2 4F RT T0001SE 2001072400451 20010724 00451 NM 2001 7 24 2001UALA01200 1 20010626 A 7830 WARNING LIGHT BOEING 737 737291 138448W NM COCKPIT ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 997UA 22457 DURING CLIMBOUT, NR 2 THRUST REVERSER ISOLATION VALVE LIGHT ILLUMINATED. 2 L 7 2 4F A16WE 2001072400452 20010724 00452 NM 2001 7 24 2001UALA01201 1 20010627 A 5311 FRAME BOEING 737 737322 1384676 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 320UA 23952 FRAME BELOW CREASEBEAM HAS CRACK AT BS 616, STR 17R, RBL 63. REMOVED DAMAGE. INSTALLED FILLER AND ANGLE REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072400454 20010724 00454 NM 2001 7 24 2001UALA01203 1 20010628 A 3350 CONNECTOR BOEING 747 747422 1384935 NM CABIN LOOSE A UALA K NONE L NO TEST UK UNKNOWN 1 WP 29 109UA 26906 EEL LIGHT AT SEAT 34HJK IS INOP. *S/D* SECURED CONNECTOR UNDER SEAT. OPS CK'D OK. 2 L 7 4 4F RT A20WE 2001072400455 20010724 00455 NM 2001 7 24 2001UALA01204 1 20010627 A 3350 LIGHT BOEING 747 747422 1384935 NM CABIN INOPERATIVE A UALA K NONE L NO TEST UK UNKNOWN 1 WP 29 116UA 26908 EMERGENCY CEILING LIGHT NEXT TO SEAT 35ABC IS INOP. *S/D* RELAMPED, CKD OK. 2 L 7 4 4F RT A20WE 2001072400456 20010724 00456 NM 2001 7 24 2001UALA01205 1 20010626 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 432-434 STR 35R SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED SHEAR TIE REPAIR IN ACCORDANCE WITH BAC DWG 140T 2102 AND 143T1001 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400457 20010724 00457 NM 2001 7 24 CALA0100672 1 20010723 A 5313 STRINGER BOEING 737 7373T0 1384582 NM STA 907 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14325 23455 INSPECTION FOUND AN 1/8" CRACK IN STRINGER 4R SPLICE AND STRINGER 6R SPLICE AT STA 907. THE STRINGER SPLICES WERE REMOVE D AND NEW STRINGER SPLICES WERE INSTALLED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001072400458 20010724 00458 WP 2001 7 24 CALA0100676 1 20010724 A 5330 SKIN DOUG DC9 DC982 3022082 WP FS 275 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND FUSELAGE EXTERNAL SKIN DENTED AT FS 275, LONGERON 17L. THE DENTED AREA OF SKIN WAS REMOVED IAW SRM 51-3 0-2. NEW SKIN WAS INSTALLED IAW SRM 51-30-2, 51-30-5, AND ECRA 5330-02445. 2 L 7 2 4F A6WE 2001072400459 20010724 00459 NM 2001 7 24 2001UALA01206 1 20010626 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 1263 RBL 23-38 T-CAP CORRODED. *S/D* FABRICATED AND INSTALLED T-CAP REPAIR IN ACCORDANCE WITH BAC DWG 146T1209 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400460 20010724 00460 NM 2001 7 24 2001UALA01207 1 20010626 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 1285 STR 39L-39L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED SHEAR TIE REPAIR IN ACCORDANCE WITH BAC DWG 140 T2102-520 AND 146T1210 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001102600017 20011026 00017 NM 2001 10 26 2001UALA01208 1 20010626 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 1307 STR 39L-39R SHEAR TIE CORRODED. FABRICATED AND INSTALLED SHEAR TIE REPAIR. THIS WAS A MAJOR REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001072400461 20010724 00461 NM 2001 7 24 2001UALA01209 1 20010626 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 566-567 STR 38L-39L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED SHEAR TIE REPAIR IN ACCORDANCE WITH BAC DWG 140T2102 AND 143T1205 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400462 20010724 00462 NM 2001 7 24 AWXA0002005 1 20010721 A 5313 143N3110 STRINGER BOEING 757 757225 1384959 NM STA 525 STR 24L CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 d: Stringer 24L at STA 525C: Removed damaged area on stringer, Fabricated and installed repair per SRM 53-00-03 fig 201 2 L 7 2 4F RT A2NM 2001072400463 20010724 00463 NM 2001 7 24 AWXA0002006 1 20010714 A 5315 65454104L DOUBLER BOEING 737 737277 1384570 NM BS670 LBL 24 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: Doubler on floor beam at BS 670 LBL 24 cracked.C: Removed and replaced doubler IAW B737 SRM 51-30-05 pg 5 2 L 7 2 4F RT A16WE 2001072400464 20010724 00464 NM 2001 7 24 AWXA0002007 1 20010630 A 5313 6545815 FRAME BOEING 737 737277 1384570 NM FWD FUSE CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: During "C-12" check inspection found upper lobe frame cracked BS 344, stringer 6LC: Repaired crack on upper lobe fram e BS 344, at stringer 6L IAW B737-200 SRM 53-10-4 2 L 7 2 4F RT A16WE 2001072400465 20010724 00465 NM 2001 7 24 AWXA0002008 1 20010720 A 5312 654541041 WEB BOEING 737 737277 1384570 NM BS 178 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 D: HFEC Indicates .500 crack aftside BS 178 Bulkhead pressure WEB LBL .6, WL 202C: Repaired crack in BS 178 Bulkhead pre ss web IAW AWA ER 15-5313-01198-SS4 2 L 7 2 4F RT A16WE 2001072400466 20010724 00466 NM 2001 7 24 AWXA0002009 1 20010714 A 5300 65C251804 BEAM BOEING 737 737277 1384570 NM BS 838 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 182AW 22644 D: Aft lower cargo door lower beam Tee cracked 1" at aft end BS 838C: Repaired aft lower cargo door Tower beam Tee at af t BS 838 IAW E.O. 52-33-01 2 L 7 2 4F RT A16WE 2001072400467 20010724 00467 NM 2001 7 24 AWXA0002010 1 20010708 A 5310 BAC1505100257 ANGLE BOEING 737 737277 1384570 NM BS 674 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 D: Cabin center wing box area attach angle cracked STA 674 RBL 45C: Repaired cabin center wing box area lower attach ang le BL 45R BS 674 IAW ER 15-5715-01200 DL3 2 L 7 2 4F RT A16WE 2001072400468 20010724 00468 NM 2001 7 24 AWXA0002011 1 20010720 A 5312 654541041 WEB BOEING 737 737277 1384570 NM BS 178 WL 184 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 D: HFEC Indicates 1.7" crack BS 178 BLKHD pressure Web, LBL .6, WL 184C: Removed damaged area from BS 178 bulkhead insta lled repair on 178 bulhead pressure web LBL .6 WL 184 IAW AWA ER 15-5313-01198-SS5 2 L 7 2 4F RT A16WE 2001072400469 20010724 00469 NM 2001 7 24 AWXA0002013 1 20010714 A 5312 6516300517 STRAP BOEING 737 737277 1384570 NM BS178 BL-0 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: Strap cracked on FWD side of BS 178 Bulkhead BL-0 WL 188C: Removed and replaced strap IAW BAC DWG 65-16300 and B737 S RM 51-30-2 2 L 7 2 4F RT A16WE 2001072400470 20010724 00470 NM 2001 7 24 AWXA0002014 1 20010715 A 5312 6516300511 WEB BOEING 737 737277 1384570 NM BS 178 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 D: HFEC Indicators(2EA) cracks at hi-lock fastners LBL 8 & 9, WL 234 BS 178 Bulkhead Web FWD sideC: Repaired BS 178 Bulk head WEB IAW B737 SRM 53-10-11 Pgs 1-7at WL 234, LBL 8,9 2 L 7 2 4F RT A16WE 2001072400471 20010724 00471 NM 2001 7 24 AWXA0002015 1 20010716 A 5313 6516300512 WEB BOEING 737 737277 1384570 NM BS 178 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 D: BS 178 Bulkhead web side cracked .200" out of button-head rivet hole, WL .234 RBL 10C: Repaired BS 178 Bulkhead web f wd side WL 234 RBL 10 IAW B737 SRM 53-10-11 Pgs 1-6 Fig 1 2 L 7 2 4F RT A16WE 2001072400472 20010724 00472 NM 2001 7 24 AWXA0002016 1 20010716 A 5313 6516300512 WEB BOEING 737 737277 1384570 NM BS 178 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 D: HFEC Indicates 1.3" crack, BS 178 Bulkhead web, FWD side along strap, WL 226.3 RBL 6.8C: Repaired BS 178 bulkhead web at WL 226.3 RBL 6.8 & 4.9 IAW B737 SRM 53-1011 Pgs 1-7 2 L 7 2 4F RT A16WE 2001072400473 20010724 00473 NM 2001 7 24 AWXA0002017 1 20010717 A 5312 654541041 WEB BOEING 737 737277 1384570 NM BS 708 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 D: Web cracked at BS 708, RBL 25C: Repaired floor beam web at BS 708, RBL 25 IAW AWA ER 15-5715-01195-SS1 2 L 7 2 4F RT A16WE 2001072400474 20010724 00474 NM 2001 7 24 AWXA0002018 1 20010708 A 5310 E5C377324 ANGLE BOEING 737 737277 1384570 NM RBL 24 STA 663 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 D: Cabin center wing box area angle cracked STA 663 RBL 24C: Cut out cracked area fabricated repair cord segment, splice angles & straps heated primed and installed repair cord segment, splice angles & straps IAW B737 200 SRM 51-30-2 pg 7 & 8 and AWA ER 15-5715-01193-SS4 2 L 7 2 4F RT A16WE 2001072400475 20010724 00475 NM 2001 7 24 AWXA0002020 1 20010630 A 5330 65C337253 SKIN BOEING 737 737277 1384570 NM R-2 DOOR CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 D: R-2 door upper hinge cut out has crack in the radius of lower corner of exterior skin,C: repaired R-2 Door upper hing e cut out IAW AWA ER 15-521001191-KB2 2 L 7 2 4F RT A16WE 2001072400476 20010724 00476 NM 2001 7 24 AWXA0002022 1 20010711 A 5313 654583369 INTERCOSTAL BOEING 737 73733A 1384673 NM BS 178 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 D: BS 178 R/H intercostal cracked at WL 195.7 RBL 27C: Removed and replaced intercostal per SRM 53-10-08 2 L 7 2 4F RT A16WE 2001072400477 20010724 00477 NM 2001 7 24 AWXA0002026 1 20010711 A 5313 672038 INTERCOSTAL BOEING 737 73733A 1384673 NM BS 178 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 D: BS 178 L/H intercostal is cracked WL 195.7 LBL 27C: Removed and replaced intercostal IAW SRM 53-10-08 2 L 7 2 4F RT A16WE 2001072400478 20010724 00478 NM 2001 7 24 AWXA0002027 1 20010711 A 5313 654583340 WEB BOEING 737 73733A 1384673 NM BS 178 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 D: BS 178 Bulkhead L/H intercostal web is cracked at WL 209 LBL 27C: removed damaged intercostal web installed new web I Aw SRM 51-40-02 & DRW 65-45833 2 L 7 2 4F RT A16WE 2001072400479 20010724 00479 NM 2001 7 24 AWXA0002028 1 20010708 A 5315 6545834256 FLOOR SUPPORT BOEING 737 73733A 1384673 NM STA 312 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 D: Floor support corroded STA 312 to 328 RBL 10C: Replaced support IAW 51-10-2 & 53-10-51 2 L 7 2 4F RT A16WE 2001072400480 20010724 00480 NM 2001 7 24 AWXA0002030 1 20010708 A 5315 654581283 FLOORBEAM BOEING 737 73733A 1384673 NM STA328 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 D: STA 328 Floor beam Corroded from RBL 30 to RBL 45C: Repaired per SRM 53-10-51 Fig 205 2 L 7 2 4F RT A16WE 2001072400481 20010724 00481 NM 2001 7 24 AWXA0002033 1 20010712 A 5315 654587545 ANGLE BOEING 737 73733A 1384673 NM STA 294-345 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 D: Right crease beam corroded BS 294.5 to BS 345C: repaired per SRM 51-70-11 fig 1 2 L 7 2 4F RT A16WE 2001072400482 20010724 00482 NM 2001 7 24 AWXA0002034 1 20010712 A 5330 6546881 SKIN BOEING 737 73733A 1384673 NM BS 1130 DENTED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 D: Fuselage skin at 1130 L/H STR 14L has 2ea dents in skinC: Fabricated and installed doubler repair per SRM 53-00-01 2 L 7 2 4F RT A16WE 2001072400483 20010724 00483 NM 2001 7 24 2001UALA01210 1 20010626 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 676 STR 36L-37L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED SHEAR TIE REPAIR IN ACCORDANCE WITH BAC DWG 140T 2102 AND 143T1211 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400484 20010724 00484 NM 2001 7 24 2001UALA01211 1 20010626 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 140T2102 AND 143T1205 N-R F6280N. FABRICATED AND INSTALLED R EPAIR IN ACCORDANCE WITH BAC DWG 140T2102 AND 143T1205 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400485 20010724 00485 NM 2001 7 24 2001UALA01212 1 20010626 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 1197 RBL22-35 T-CAP CORRODED. *S/D* FABRICATED AND INSTALLED T-CAP REPAIR IN ACCORDANCE WITH BAC DWG 146T1206 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400486 20010724 00486 NM 2001 7 24 2001UALA01213 1 20010626 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 1131 LBL 5 T-CAP CORRODED. *S/D* FABRICATED AND INSTALLED T-CAP REPAIR IN ACCORDANCE WITH BAC DWG 146T1060 N-R. MA JOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400487 20010724 00487 EA 2001 7 24 SWIA200110049 1 20010719 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 EA RIGHT CRACKED A SWIA O OTHER O OTHER DE DESCENT 1 NM 07 496SW 7473 RIGHT WINDSHIELD CRACKED AT 12,500 MSL @ 3.5 PSI AND 290 KTS.RIGHT WINDSHIELD REPLACED AND TESTED IAW MM TASK 56-11-0140 0-8001.P/N ON: NP-139321-10 S/N ON: 01129H7474 P/N OFF: 601R33033-10 S/N OFF: 00255H7477 2 L 7 2 4F RT A21EA 2001072400488 20010724 00488 NM 2001 7 24 2001UALA01214 1 20010626 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 347 STR 39R-39L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 141T1221 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400489 20010724 00489 NM 2001 7 24 2001UALA01215 1 20010626 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 FABRICATED AND INSTALLED SHEAR TIE REPAIR IN ACCORDANCE WITH BAC DWG 140T2102-506 AND 146T1213 N-R. *S/D* FABRICATED A ND INSTALLED SHEAR TIE REPAIR IN ACCORDANCE WITH BAC DWG. 2 L 7 2 4F RT A1NM 2001072400490 20010724 00490 NM 2001 7 24 2001UALA01216 1 20010626 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 1263 STR 36L-37L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED SHEAR TIE REPAIR IN ACCORDANCE WITH BAC DWG 140 T2102-557 AND 146T1209 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400491 20010724 00491 NM 2001 7 24 2001UALA01217 1 20010626 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 1307 STR 37L-38L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED SHEAR TIE REPAIR IN ACCORDANCE WITH BAC DWG 140 T2102-490 AND 146T1211 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400492 20010724 00492 WP 2001 7 24 RRXA010541 1 20010131 A 5330 DOUGLAS GUSSET DOUG DC8 DC871F 302199D WP XFS 195-201.250 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE GUSSET BETWEEN STA XFS 195 AND STA XFS 201.250, DAMAGE EXCEEDED LIMITATI ONS IAW DC-8 SR. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INST ALLED IAW DC-8 SRM 51-1-21 AND DC-8 SRM 51-1-4 AND DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001072400493 20010724 00493 WP 2001 7 24 RRXA010548 1 20010131 A 5730 DOUGLAS FORMER DOUG DC8 DC871F 302199D WP STA XS 227.335 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XS 227.335, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21 AND DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001072400494 20010724 00494 WP 2001 7 24 RRXA010552 1 20010131 A 5730 DOUGLAS GUSSET DOUG DC8 DC871F 302199D WP STA 195 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACKED GUSSET AT FORMER AT STA 195, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. ///// CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1 -21. 2 L 7 4 4F RT 4A25 2001072400495 20010724 00495 WP 2001 7 24 RRXA10744 1 20010314 A 5330 NPN SKIN DOUG DC8 DC871F 302199D WP L35L STA.705 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO OUTER SKIN L35L AT STA.705, DAMAGE EXCEEDED LIMITATIONS IAW DC-8SRM . /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 S RM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072400496 20010724 00496 WP 2001 7 24 RRXA10746 1 20010301 A 5313 NPN BRACE DOUG DC8 DC871F 302199D WP STA. 1916 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENACE VISIT FOUND CRACK DAMAGE TO HORZ. BRACE AT STA. 1916 AND DOOR 62, DAMAGE EXCEEDED LIMITATIONS IAW DC -8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED I AW DC-8 SRM 51-1-4 AND DC-8 SRM 51-1-0. 2 L 7 4 4F RT 4A25 2001072400497 20010724 00497 WP 2001 7 24 RRXA10749 1 20010308 A 5330 NPN SKIN DOUG DC8 DC871F 302199D WP STA772-721 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SKIN AT STA. 772-721 AND L35L-L36R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLE D IAW EO#01-024 WITH APPROVED 8110-3 DATED 03/02/01. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072400498 20010724 00498 WP 2001 7 24 RRXA10750 1 20010215 A 5720 NPN SHIM DOUG DC8 DC871F 302199D WP IB LWR FRNT SPAR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO #1 STUB WING I/B LWR. FRONT SPAR L/E SHIM, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, AND TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND I NSTALLED IAW E.O.#01-24 WITH APPROVED 8110-3 DATED 02/15/01. 2 L 7 4 4F RT 4A25 2001072400499 20010724 00499 WP 2001 7 24 RRXA10752 1 20010209 A 5312 NPN FRAME DOUG DC8 DC871F 302199D WP STA1170 L36-L35R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FUSELAGE FRAME AT STA. 1170 AND LONGERON 36 TO 35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REP AIR AND INSTALLED IAW E.O. #01-024 WITH APPROVED 8110-3 DATED 03/08/01. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROG RAM). 2 L 7 4 4F RT 4A25 2001072400500 20010724 00500 WP 2001 7 24 RRXA10753 1 20010209 A 5720 NPN BRACKET DOUG DC8 DC871F 302199D WP XFS 248 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO BRACKET AT STA. XFS248, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. //// /CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51- 1-4 AND DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001072400501 20010724 00501 WP 2001 7 24 RRXA10754 1 20010209 A 5720 NPN FORMER DOUG DC8 DC871F 302199D WP XFS 227.335 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO T/E FORMER AT STA. XFS 227.335, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SR M. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2001072400502 20010724 00502 WP 2001 7 24 RRXA10755 1 20010131 A 5720 NPN FORMER DOUG DC8 DC871F 302199D WP STA. XFS 117 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LT. SIDE T/E FORMER AT STA. ZFS 117, DAMAGE EXCEEDED LIMITATIONS IAW DC -8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.FABRICATED REPAIR AND INSTALLED IA W DC-8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2001072400503 20010724 00503 WP 2001 7 24 RRXA10756 1 20010131 A 5720 NPN FORMER DOUG DC8 DC871F 302199D WP STA. XFS 175 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LT. SIDE T/E FORMER AT STA. ZFS 175, DAMAGE EXCEEDED LIMITATIONS IAW DC -8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED I AW DC-8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2001072400504 20010724 00504 WP 2001 7 24 RRXA10757 1 20010131 A 5330 NPN SKIN DOUG DC8 DC871F 302199D WP STA. 1140-1170 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO AFT LWR. CARGO BILGE FUSELAGE SKIN AT STA. 1140-1170 AND L35L TO L3 5R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51- 1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. #01-024 WITH APPROVED 8110-3 DATED 02/02/01. SEE N/R'S 5E-026 & 5E-090. (C ORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072400505 20010724 00505 WP 2001 7 24 RRXA10758 1 20010131 A 5312 NPN DOUBLER DOUG DC8 DC871F 302199D WP STA. 1155-1170 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO AFT LWR. CARGO BILGE INTERNAL DOUBLER AT STA. 1155-1170 AND L35L TO L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW E.O. #01-024 WITH APPROVED 8110-3, DATED 02/02/01. SEE N/R'S 5E-026 & 5E-091. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072400506 20010724 00506 WP 2001 7 24 RRXA10759 1 20010328 A 5321 NPN FLOOR PANEL DOUG DC8 DC871F 302199D WP #676 CENTER FWD. CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO CENTER FWD. FLOOR PANEL AT COCKPIT PANEL #676, DAMAGE EXCEEDED LIMI TATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0 AND DC-8 SRM51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072400507 20010724 00507 WP 2001 7 24 RRXA10760 1 20010322 A 5321 NPN PANEL DOUG DC8 DC871F 302199D WP STA. 46-66 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LAV. FLOOR PANEL AT STA. 46-66, DAMAGE EXCEEDED LIMITATIONS IAW DC- 8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4 AND DC-8 SRM 51-3-0 AND DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072400508 20010724 00508 WP 2001 7 24 RRXA10761 1 20010320 A 2750 NPN BUSHING DOUG DC8 DC871F 302199D WP 2ND O/B VANE ELONGATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND ELONGATED BUSHING DAMAGE TO #3 LT. FLAP 2ND FROM O/B VANE AT 2ND O/B VANE, DAMAGE EXCEE DED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW E.O.#01-024 WITH APPROVED 8110-3 DATED 02/01/01. 2 L 7 4 4F RT 4A25 2001072400509 20010724 00509 WP 2001 7 24 RRXA10764 1 20010326 A 5720 NPN STRINGER DOUG DC8 DC871F 302199D WP STR.53 STA.495 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H WING STR.53 AT STA. 495 AND AFT HORZ. LEG, DAMAGE EXCEEDED LIMITATI ONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INS TALLED IAW E.O. #01-024 WITH APPROVED 8110-3 DATED 03/15/01. 2 L 7 4 4F RT 4A25 2001072400510 20010724 00510 NM 2001 7 24 2001UALA01218 1 20010626 A 5313 STRINGER BOEING 767 767222 1385122 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 1065-1087 STR 29L CRACKED. *S/D* FABRICATED AND INSTALLED STR REPAIR IN ACCORDANCE WITH SRM 53-00-03 AND 51-40-02 N -R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400511 20010724 00511 NM 2001 7 24 2001UALA01219 1 20010626 A 5313 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 1395 STR 39L-39R SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 140T2102-702 AND 146T1215 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400512 20010724 00512 NM 2001 7 24 2001UALA01220 1 20010626 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 566 36L-37L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED SHEAR TIE REPAIR IN ACCORDANCE WITH BAC DWG 143T2102 AND 143T1206 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400513 20010724 00513 NM 2001 7 24 2001UALA01221 1 20010625 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 610 STR 37L-38L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED SHEAR TIE REPAIR IN ACCORDANCE WITH BAC DWG 140T 2102 AND 143T1208 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400514 20010724 00514 NM 2001 7 24 2001UALA01222 1 20010625 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 610 STR 33L-34L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED SHEAR TIE REPAIR IN ACCORDANCE WITH BAC DWG 140T 2102 AND 143T1208 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400515 20010724 00515 NM 2001 7 24 2001UALA01223 1 20010625 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 1241 RBL10-RBL15 T-CAP CORRODED. *S/D* FABRICATED AND INSTALLED T-CAP REPAIR IN ACCORDANCE WITH BAC DWG 146T1208 N- R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400516 20010724 00516 NM 2001 7 24 2001UALA01224 1 20010625 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 698 STR 39L-39R SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED SHEAR TIE REPAIR IN ACCORDANCE WITH BAC DWG 143T 1212 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400517 20010724 00517 NM 2001 7 24 2001UALA01225 1 20010625 A 5347 SEAT TRACK BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 1197-1351 LBL 88 A SEAT TRACK CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 146T5214 A AND SRM 53-00-52 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400518 20010724 00518 NM 2001 7 24 2001UALA01226 1 20010625 A 5320 STRINGER CLIP BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 347 STR 36R CLIP CORRODED. *S/D* FABRICATED AND INSTALLED CLIP REPAIR IN ACCORDANCE WITH BAC DWG 141T1221 N-R. MA JOR REPAIR. 2 L 7 2 4F RT A1NM 2001072400519 20010724 00519 NM 2001 7 24 AWXA0002025 1 20010711 A 5310 654583348 CLIP BOEING 737 73733A 1384673 NM BS 178 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 D: BS 178 R/H clip is cracked at WL 209 RBL 27C: Removed and replaced clip per DWG 65-45883 and SRM 51-40-02 2 L 7 2 4F RT A16WE 2001072400520 20010724 00520 WP 2001 7 24 IXXA0100039O 1 20010721 A 2610 8989886 AMPLIFIER DOUG DC8 DC871F 302199D WP COCKPIT DEFECTIVE A IXXA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SW 11 822BX 84263 90 45813 ENROUTE FROM TOL TO LAX, DURING CRUISE THE NUMBER FOUR ENGINE FIRE WARNING LIGHT ILLUMATED ACCOMPANIED BY THE WARNING BE LL. THE FLIGHT CREW FOLLOW COMPANY EMERGENCY PROCEDURES, SECURED THE ENGINE AND DISCHARGED ONE BOTTLE. THE FLIGHT CONTIN UED TO LAX FOR AN UNEVENTFUL LANDING.MAINTENANCE INSPECTED THE ENGINE WITH NO EVIDENCE OF A FIRE. MAINTENANCE TESTED THE SYSTEM WHICH REVEALED A DEFECTIVE FIRE WARNING AMPLIFIER AND WAS REPLACED. MAINTENANCE PERFORMED A SUCCESSFUL OPERATION AL TEST IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2001072400521 20010724 00521 WP 2001 7 24 ZW0A0105601 1 20010721 A 3350 MISC0639 BATTERY PACK DOUG DC9 DC983 3022083 WP FWD OVERWING A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 979TW 53629 THE FWD OVERWING EMERGENCY LIGHTS DID NOT ILLUMINATE WITH THE SWITCH ON. REPLACED THE BATTERY PACK. CHECK-C 11-8-00. --CLOSED-- 2 L 7 2 4F RT A6WE 2001072400522 20010724 00522 NE 2001 7 24 S01472020 2 20010712 A 7200 ENGINE BOEING 747 747400 NM PWA 4056 PW4056 NE # 3 ENG SURGES W SAJF O OTHER O OTHER TO TAKEOFF 1 WP 03 14024 29219 727824 B-18207 DUE PERFORMANCE A "PACK OFF",MAX THRUST T/O PERFORMED,AT 500 FT ENG-3 SURGED,THRUST REDUCED ALL PARAMETERS NORMA L.C/A:1.IAW FIM 71-00-00,FIG 107,INSPECT ENG INLET/EXHAUST AREA,MCDS AND BLEED PORTS,BORESCOPE INSPECTED FOR COMPRESSOR/ TURBINE BLADES,ALL CONDITION NORMAL. 2.CHECK FOUND INLET GUIDE VANE OUT OF RIG AND ADJUSTED,PERFORMED ENG MAX POWER TEST SATISDIED. 3.THE MOC DECIDED TO REPLACED ENG-3 DUE SURGE ROOT CAUSE NOT IDENTIFIED,ENG REPLACED AND RUN-UP TEST NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2001072500071 20010725 00071 EU 2001 7 25 2001F00136 1 20010622 A 3350 AQS1000 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 420AT 420 MIA - MAINTENANCE REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS AT SEAT 9AB IS INOPERATIVE. MAINTENANCE REPLACED THE FL OOR LIGHT AND THE BATTERY PACK FOR THIS LIGHT IAW ATR MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200117302. (M) 2 H 7 2 4T RT A53EU 2001072500072 20010725 00072 NM 2001 7 25 2001F00137 1 20010412 A 5347 6546592503 CARGO TRACK BOEING 737 7374Q8 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 779AS 25111 PAE - DURING SI CHECK, FOUND AFT CARGO BAY FLOOR TRACK AT BS 750 TO BS 756, WL 150 AND BL 3 LEFT AND RIGHT DAMAGED. REP AIRED IAW ASA EA 5320-01378. REF ASAA010057. (M) 2 L 7 2 4F RT A16WE 2002020100092 20020201 00092 NM 2002 2 1 ASAA0110103 1 20010220 A 5320 65482836 INTERCOSTAL BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL AT BS 302, STRINGER 27L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2002020100093 20020201 00093 NM 2002 2 1 ASAA0110104 1 20010220 A 5320 651758351 STIFFENER BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND STIFFENER AT BODY STATION 178, LEFT BUTTOCK LINE 6 CRACKED. REPAIRED PER SRM. (M ) 2 L 7 2 4F A16WE 2002020100094 20020201 00094 NM 2002 2 1 ASAA0110106 1 20010221 A 5320 656211911 FLOOR SUPPORT BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT AT BS 540, RIGHT BUTTOCK LINE 2-22 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001112700115 20011127 00115 NM 2001 11 27 ASAA0110120 1 20010310 A 3234 CONTROL HANDLE BOEING 737 7372Q8C 138448S NM COCKPIT DIRTY A ASAA O OTHER J WARNING INDICATION CL CLIMB 1 NM 01 741AS 21959 ANC - AFTER DEPARTURE FROM ANC ON FLIGHT 45, THE LEFT MAIN GEAR FELL BACK DOWN BUT RETRACTED WHEN GEAR LEVER CYCLED BACK UP. FOUND GEAR HANDLE SHAFT DIRTY AND GUMMED UP. WHEN PULLED OUT IT WOULD NOT DROP INTO DETENTS. CLEANED HANDLE SHAF T AND LUBED, HANDLE TESTED WITH GEAR PINNED, HANDLE DROPS FREELY INTO DETENTS. ACCOMPLISHED GEAR SWING, OPS NORMAL. (M ) 2 L 7 2 4F A16WE 2001072500073 20010725 00073 NM 2001 7 25 ASAA0110138 1 20010320 A 5320 BAC15201397 FLOOR SUPPORT BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT ANGLE AT BS 727B, STRINGER 26L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001072500074 20010725 00074 NM 2001 7 25 ASAA0110147 1 20010322 A 5320 69353642 STRINGER CLIP BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 967, STRINGER 24L CORRODED. REPAIRED PER BOEING DRAWING. (M) 2 L 7 2 4F A16WE 2001072500075 20010725 00075 NM 2001 7 25 ASAA0110148 1 20010322 A 5320 6545833 FLOOR SUPPORT BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT AT BS 410-510, STRINGER 27R CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001072500076 20010725 00076 NM 2001 7 25 ASAA0110157 1 20010326 A 5320 69489501 ANGLE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND ANGLE AT BS 360, STRINGER 28L CORRODED. REMOVED AND REPAIRED PER BOEING DRAWING. (M) 2 L 7 2 4F A16WE 2001072500077 20010725 00077 NM 2001 7 25 ASAA0110158 1 20010326 A 5320 BAC15201397 FLOOR SUPPORT BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT ANGLE AT BS 737-947, STRINGER 27L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001072500078 20010725 00078 NM 2001 7 25 ASAA0110159 1 20010326 A 5320 BAC15201430 SUPPORT BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND SEAT TRACK SUPPORT AT BS 540-639, LBL 62 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001072500079 20010725 00079 NM 2001 7 25 ASAA0110160 1 20010327 A 5347 BAC15201331 SEAT TRACK BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND SEAT TRACK AT BS 360-390, BL 0 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001072500080 20010725 00080 WP 2001 7 25 RRXA10766 1 20010320 A 5312 NPN SPAR DOUG DC8 DC871F 302199D WP STA 781 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BOTTOM OF SPAR AT STA. 781 AND INSIDE L/H CENTER TANK THUR MID-SPAR ACCESS HOLE560E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IA W DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.#01-024 WITH APPROVED 8110-3 DATED 01/31/01. 2 L 7 4 4F RT 4A25 2001072500081 20010725 00081 WP 2001 7 25 RRXA10772 1 20010308 A 5312 NPN BULKHEAD DOUG DC8 DC871F 302199D WP C & D PIT CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE INSPECTION FOUND CRACK DAMAGE TO C & D PIT R/H BULKHEAD AT C & D PIT, DAMAGE EXCEEDS LIMITATIONS IA W DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW E.O.#01-024 WITH APPROVED 8110-3 DATED 02/23/01. 2 L 7 4 4F RT 4A25 2001072500082 20010725 00082 WP 2001 7 25 RRXA10774 1 20010113 A 5752 NPN SKIN DOUG DC8 DC871F 302199D WP STA. XW 106 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LT. WING I/B FLAP SKIN IB SURFACE AT STA. XW106, DAMAGE EXCEEDED LIMITA TIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 NDT MANUAL 06-10-01.001 AND DC-8 SRM 57-2-1 AND DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001072500083 20010725 00083 WP 2001 7 25 RRXA10775 1 20010212 A 5754 56551661 PANEL DOUG DC8 DC871F 302199D WP #2 PANEL DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LT. WING #2 SPOILER PANEL AT #2 PANEL, DAMAGE EXCEEDED LIMITATIO NS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTAL LED IAW DC-8 MM 27-61-1. 2 L 7 4 4F RT 4A25 2001072500084 20010725 00084 WP 2001 7 25 RRXA10776 1 20010103 A 5754 56551651 PANEL DOUG DC8 DC871F 302199D WP #1 PANEL DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LT. WING #1 SPOILER AT #1 PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IA W DC-8 MM 27-61-1. 2 L 7 4 4F RT 4A25 2001072500085 20010725 00085 WP 2001 7 25 RRXA10777 1 20010214 A 5754 56551671 PANEL DOUG DC8 DC871F 302199D WP #3 SPOILER DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO L/H WING #3 SPOILER PANEL AT #3 SPOILER, DAMAGE EXCEEDED LIMITAT IONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED ARE IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTA LLED IAW DC-8 MM 27-61-1. 2 L 7 4 4F RT 4A25 2001072500086 20010725 00086 WP 2001 7 25 RRXA10780 1 20010113 A 5720 NPN SKIN DOUG DC8 DC871F 302199D WP STA. XRS19-XRS90 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO L/H WING T/E AT STA. XRS 19 TO XRS 90 AND UPPER SURFACE, DAMAGE EXCEEDE D LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED RE PAIRS AND INSTALLED IAW DC-8 SRM 51-1-4 AND DC-8 SRM 51-1-21 AND DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001072500087 20010725 00087 WP 2001 7 25 RRXA10781 1 20010215 A 5752 NPN FITTING DOUG DC8 DC871F 302199D WP STA. 219 GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO LT. WING FLAP IN FITTING AT STA. 219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.#01-006 WITH APPROVED 8110-3 DATED 02/06/01. 2 L 7 4 4F RT 4A25 2001072500088 20010725 00088 WP 2001 7 25 RRXA10785 1 20010206 A 5730 56554332 PANEL DOUG DC8 DC871F 302199D WP FLAP SCISSORS DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO RT. WING SCISSORS PANEL AT FLAP SCISSORS, DAMAGE EXCEEDED LIMITA TIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INS TALLED IAW DC-8 MM 27-50-1. 2 L 7 4 4F RT 4A25 2001072500089 20010725 00089 WP 2001 7 25 RRXA10786 1 20010201 A 5312 NPN STRINGER DOUG DC8 DC871F 302199D WP STR#76 XCW23&46 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO STRINGER #76 AT STA. XCW23 AND XCW46 AND INSIDE L/H CENTER WING TAN K THRU MID SPAR ACCESS HOLE 560E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-24 AND DC-8 SRM 51-1-20D AND E.O.#0 1-006 WITH APPROVED 8110-3 DATED 01/22/01. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500090 20010725 00090 WP 2001 7 25 RRXA10787 1 20010209 A 5720 NPN SKIN DOUG DC8 DC871F 302199D WP STA. XW485.0 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LT. WING L/E AT STA. XW485.0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-4 AND DC-8 SRM 51-3-0 AND E.O.#01-006 WITH APPROVED 8110-3 DATED 01/26/01. 2 L 7 4 4F RT 4A25 2001072500091 20010725 00091 WP 2001 7 25 RRXA10788 1 20010208 A 5752 NPN SKIN DOUG DC8 DC871F 302199D WP STA. XW 62.5 DENTED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND DENT DAMAGE TO L/H I/B FLAP AT STA.XW62.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. / ////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW NDT SPM 08-00-06 AND E.O.01-006 WITH APPROVED 8110-3 DATED 02/05/01. 2 L 7 4 4F RT 4A25 2001072500092 20010725 00092 WP 2001 7 25 RRXA10789 1 20010210 A 5312 NPN STRINGER DOUG DC8 DC871F 302199D WP STA.495&508 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LOWER STRINGER #55 AT STA. 495 CAN'T AND 508 CAN'T, DAMAGE EXCEEDED LIM ITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIRA ND INSTALLED IAW DC-8 SRM 51-1-21 AND E.O.#01-006 WITH APPROVED 8110-3 DATED 02/08/01. 2 L 7 4 4F RT 4A25 2001072500093 20010725 00093 WP 2001 7 25 RRXA10790 1 20010104 A 5754 56551682 SPOILER PANEL DOUG DC8 DC871F 302199D WP #4 R/H SPOILER DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO R/H #4 SPOILER AT #4 SPOILER, DAMAGE EXCEEDED LIMITATIONS IAW DC -8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW D C-8 MM 27-61-1. 2 L 7 4 4F RT 4A25 2001072500094 20010725 00094 WP 2001 7 25 RRXA10791 1 20010104 A 5754 56551671 SPOILER PANEL DOUG DC8 DC871F 302199D WP R/H #3 SPOILER DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO R/H #3 SPOILER AT #3 R/H SPOILER, DAMAGE EXCEEDED LIMITATIONS IA W DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED I AW DC-8 MM 27-61-1 AND DC-8 MM 27-61-1. 2 L 7 4 4F RT 4A25 2001072500095 20010725 00095 WP 2001 7 25 RRXA10793 1 20010210 A 5752 5652287506N VANE DOUG DC8 DC871F 302199D WP RT.I/B FLAP VANE DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO RT. WING I/B FLAP VANE AT RT. I/B FLAP, DAMAGE EXCEEDED LIMITATI ONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTA LLED IAW DC-8 MM 27-51-15. 2 L 7 4 4F RT 4A25 2001072500096 20010725 00096 WP 2001 7 25 RRXA10794 1 20010212 A 5752 5701152502 VANE DOUG DC8 DC871F 302199D WP #4 RT FLAP VANE DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO RT. WING #4 FLAP VANE AT #4 RT. WING FLAP VANE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART A ND INSTALLED IAW DC-8 MM 27-51-14. 2 L 7 4 4F RT 4A25 2001072500097 20010725 00097 WP 2001 7 25 RRXA10796 1 20010115 A 5752 NPN SKIN DOUG DC8 DC871F 302199D WP RT.WING I/B FLAP DENTED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND DENT DAMAGE TO RT. WING I/B FLAP T/E LOWER SURFACE AT RT. WING I/B FLAP AND BEHIND #8 T IRE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51 -1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4 AND DC-8 SRM 51-1-22 AND DC-8 SRM 51-1-20 AND DC-8 SRM 51-1-15. 2 L 7 4 4F RT 4A25 2001072500098 20010725 00098 WP 2001 7 25 RRXA10798 1 20010209 A 5720 NPN ANGLE DOUG DC8 DC871F 302199D WP STA. XS 220 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO #3 PYLON WING L/E BULLNOSE AT STA. XS220, DAMAGE EXCEEDED LIMITATIONS I AW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-4 AND DC-8 SRM 51-1-24 AND D C-8 SRM 51-1-21 AND DC-8 51-1-20D. 2 L 7 4 4F RT 4A25 2001072500099 20010725 00099 WP 2001 7 25 RRXA10800 1 20010201 A 5312 NPN STRINGER DOUG DC8 DC871F 302199D WP STR#76 XCW46&23 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LWR STRINGER#76 AT STA. XCW47&23 AND INSIDE R/H CENTER TANK THRU MI D SPAR ACCESS 560E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-20D AND E.O.#01-006 WITH APPROVED 8110-3 DATED 01 /25/01. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500100 20010725 00100 WP 2001 7 25 RRXA10801 1 20010201 A 5312 NPN STRINGER DOUG DC8 DC871F 302199D WP STR#75 XCW23X=0 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO STRINGER #75 AND FWD SIDE STRINGER SPLICE AT STA. XCW 23 X=0 AND IN SIDE R/H CENTER TANK THRU MID SPAR ACCESS 560E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// R EMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.#01-006 WITH APPROVED 8110-3 DA TED 01/22/01. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500101 20010725 00101 WP 2001 7 25 RRXA10802 1 20010215 A 5720 NPN CLIP DOUG DC8 DC871F 302199D WP STA 252 CAN'T CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO ATTACH CLIP AT STA. 252 CAN'T AND R/H WING #4 MAIN INSIDE TANK THRU ACC ESS HOLE 505D AND BETWEEN STRINGER 68 & 69, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOV ED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001072500102 20010725 00102 WP 2001 7 25 RRXA10803 1 20010205 A 5752 NPN SKIN DOUG DC8 DC871F 302199D WP STA. 219 TORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND TORN DAMAGE TO FLAP SKIN AT SAT. 219 AND I/B FWD. SECTION, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTA LLED IAW DC-8 SRM 57-2-1 AND DC-8 SRM 51-1-20C. 2 L 7 4 4F RT 4A25 2001072500103 20010725 00103 WP 2001 7 25 RRXA10804 1 20010207 A 5752 NPN SUPPORT FITTING DOUG DC8 DC871F 302199D WP STA. 219 GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO RT. WING FLAP SUPPORT FITTING AT STA. 219, DAMAGE EXCEEDED LIMITATION S IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTA LLED IAW DC-8 SRM 51-1-20C AND E.O.#01-006 WITH APPROIVED 8110-3 DATED 02/05/01. 2 L 7 4 4F RT 4A25 2001072500104 20010725 00104 WP 2001 7 25 RRXA10805 1 20010215 A 5752 4760268 ATTACH ANGLE DOUG DC8 DC871F 302199D WP STA. XRS 98 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO RT. WING REAR SPAR FLAP ATTACH FITTING AT STA. XRS98, DAMAGE EXCEEDED L IMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AN D INSTALLED IAW DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001072500105 20010725 00105 WP 2001 7 25 RRXA10806 1 20010215 A 5752 NPN DRIVE LINK DOUG DC8 DC871F 302199D WP STA.319 GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO R/H O/B FLAP CENTER DRIVE LINK AT STA. 319, DAMAGE EXCEEDED LIMITATION S IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INS TALLED IAW E.O.#01-006 WITH APPROVED 8110-3 DATED 02/15/01. 2 L 7 4 4F RT 4A25 2001072500106 20010725 00106 WP 2001 7 25 RRXA10808 1 20010112 A 5742 NPN SKIN DOUG DC8 DC871F 302199D WP R/H W/W CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO SKIN AT O/B AFT END OF R/H W/W BELOW FIRE BOTTLE, DAMAGE EXCEEDED LIMIT ATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE,TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC8- SRM 53-2-0 AND DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001072500107 20010725 00107 WP 2001 7 25 RRXA10809 1 20010212 A 5312 NPN PANEL DOUG DC8 DC871F 302199D WP STA. 690-779 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO L/H KEEL BEAM STRESS PANEL AT STA. 690-779 AND L35L-L33L, DAMAGE EX CEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICAT ED PART AND INSTALLED IAW E.O.#01-006 WITH APPROVED 8110-3 DATED 01/29/01. (CORROSION DAMAGE RECORDED IN EWA CORROSION P ROGRAM). 2 L 7 4 4F RT 4A25 2001072500108 20010725 00108 WP 2001 7 25 RRXA10810 1 20010209 A 5312 NPN PANEL DOUG DC8 DC871F 302199D WP STA. 742-749 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO R/H KEEL BEAM ACCESS COVER AT STA. 742-749 AND L33R-L35R, DAMAGE EX CEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICAT ED PART AND INSTALLED IAW DC-8 SRM 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500109 20010725 00109 WP 2001 7 25 RRXA10811 1 20010131 A 5312 NPN PANEL DOUG DC8 DC871F 302199D WP 30" FROM FWD EDG CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TOR/H KEEL BEAM PANEL AT PLATE ATTACH POINT 30" FROM FWD. EDGE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRI CATED REPAIR AND INSTALLED IAW E.O.#01-006 WITH APPROVED 8110-3 DATED 01/26/01. 2 L 7 4 4F RT 4A25 2001072500110 20010725 00110 WP 2001 7 25 RRXA10812 1 20010124 A 5513 NPN SKIN DOUG DC8 DC871F 302199D WP STA. XFS178 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO L/H I/B HORZ. STAB. L/E AT STA. XFS 178, DAMAGE EXCEEDED LIMITATIONS IA W DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTAL LED IAW E.O.#01-006 WITH APPROVED 8110-3 DATED 01/12/01. 2 L 7 4 4F RT 4A25 2001072500111 20010725 00111 WP 2001 7 25 RRXA10814 1 20010122 A 5321 NPN SEAT TRACK DOUG DC8 DC871F 302199D WP PILOTS RT< WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO PILOTS SEAT TRACKS AT LT AND RT PILOTS, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001072500112 20010725 00112 WP 2001 7 25 RRXA10815 1 20010122 A 5321 NPN SEAT TRACK DOUG DC8 DC871F 302199D WP COPILOT LT&RT WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO CO-PILOTS SEAT TRACKS AT LT. AND RT. CO-PILOTS SEAT, DAMAGE EXCEEDED LIM ITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTA LLED IAW DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001072500113 20010725 00113 WP 2001 7 25 RRXA10816 1 20010122 A 5321 NPN SEAT TRACK DOUG DC8 DC871F 302199D WP LT&RT FE'S SEAT WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO F/E SEAT TRACK AT FWD & AFT FE'S SEAT, DAMAGE EXCEEDED LIMITATIONS IAW D C-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001072500114 20010725 00114 WP 2001 7 25 RRXA10817 1 20010131 A 5321 NPN PLATE DOUG DC8 DC871F 302199D WP D-PIT CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO D-PIT KICK PLATE AT D-PIT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM . /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW E.O.# 01-006 WITH APPROVED 8110-3 DATED 01/12/01. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500115 20010725 00115 WP 2001 7 25 RRXA10819 1 20010213 A 5230 NPN DOOR FRAME DOUG DC8 DC871F 302199D WP L-2 DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO L-2 DOOR FRAME AT UPPER AFT CORNER, DAMAGE EXCEEDED LIMITATIONS IAW DC -8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IA W DC-8 SRM 53-2-0 FIG. 18. 2 L 7 4 4F RT 4A25 2001072500116 20010725 00116 WP 2001 7 25 RRXA10821 1 20010122 A 5321 NPN SEAT TRACK DOUG DC8 DC871F 302199D WP STA. 220-240 X=0 WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENACE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA. 220-240 X=0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-3-0 AND DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001072500117 20010725 00117 WP 2001 7 25 RRXA10825 1 20010118 A 5312 NPN FRAME DOUG DC8 DC871F 302199D WP L32L STA.440-460 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT FRAME 460-440 AND LONGERON 32L, DAMAGE EXCEEDED LIMITATION S IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INS TALLED IAW E.O.#01-006 WITH APPROVED 8110-3 DATED 01/12/01. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500118 20010725 00118 NM 2001 7 25 ASAA0110191 1 20010403 A 2120 SMOKE BOEING 737 737290C 138448V NM COCKPIT DETECTED A ASAA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 NM 01 730AS 22577 ANC - ABORTED TAKEOFF OF FLT 151, BOTH THE FIRST OFFICERS AND OBSERVER NOTED SMOKE IN THE COCKPIT DURING TAKEOFF. BOTH PACKS WERE TURNED OFF AS AIRCRAFT CLEARED RUNWAY. ANC MAINTENANCE INSPECTED BOTH ENGINES AND APU INLETS AND EXHAUST, NO DEFECTS NOTED. RAN ENGINES AT TAKEOFF POWER AND ISOLATED PACKS, COULD NOT DUPLICATE SMOKE/SMELL. RAN APU, COULD NOT D UPLICATE SMOKE/SMELL. INSPECTED A/C BAY DUCTS AND E/E COMPARTMENT. NO DEFECTS NOTED. REPLACED BOTH WATER SEPARATOR BA GS, BOTH WERE FOUND TO BE CLEAN. AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4F A16WE 2002110800138 20021108 00138 NE 2002 11 8 ASAA0110192 2 20010403 A 7261 O-RING BOEING 737 737290C 138448V NM PWA JT8 JT8D17 52049 NE LT ENGINE NICKED A ASAA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 01 730AS 22577 688124 ANC - FLT 64 - FLIGHT ATTENDANT REPORTED CHEMICAL ODOR ON CLIMBOUT WHICH DISSIPATED AFTER A FEW MINUTES. NO OTHER REPOR TS WERE NOTED. AIRCRAFT LANDED IN JNU WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND ENGINES FOR FERRY FLIGHT TO SEA FOR TROUBLESHOOTING OF REPEAT REPORT OF CABIN/FLIGHT DECK ODOR. MAINTENANCE TROUBLESHOT AND ISOLATED TO LEFT ENGIN E. REMOVED AND REPLACED LEFT ENGINE. FOUND THE OIL FUMES IN THE CABIN WERE DUE TO THE CONDITION OF THE NR 3 BEARING HO USING O-RING (NICKED) AND PISTON RINGS (STUCK) WHICH ALLOWED OIL TO LEAK BY THE LABYRINTH SEAL AND INTO THE 6TH STAGE AI R EXTRACTION USED FOR THE CABIN. THE ENGINE WAS REPAIRED PER THE MM AND RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F A16WE E2EA 2002111200080 20021112 00080 NM 2002 11 12 ASAA0110204 1 20010406 A 2150 A/C PACK BOEING 737 737290C 138448V NM A/C BAY MALFUNCTIONED A ASAA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 01 730AS 22577 ANC - IMMEDIATELY AFTER DEPARTURE, NOTED STRONG ODOR ONLY IN COCKPIT. ODOR DISSIPATED BUT RETURNED INTERMITTENTLY OVER THE NEXT SIXTY MINUTES. UNABLE TO ISOLATE THE CAUSE OF THE ODOR. BORESCOPED AND CLEANED BOTH ENGINE BLEED AIR DUCTS AN D PACK COMPONENTS FROM ENGINE FIREWALLS TO AIR CONDITIONING DISTRIBUTION BAY. REPLACED BOTH CHECK VALVES JUST UPSTREAM FROM MIXER ASSY DUE TO CORROSION, RT PACK DUCT TRIP SENSOR DUE BENT PINS, AND COCKPIT MUFFLER ASSY DUE INSULATION WAS LO OSE. CLEANED OUT AIR DUCTS IN COCKPIT, WHICH CONTAINED MUFFLER INSULATION PARTS. SUSPECT WITH LT PACK NOT GETTING AIR TO COCKPIT RT PACK WAS GOING FULL HOT CAUSING BAD SMELL. ALSO, MUFFLER INSULATION WAS FOUND TO HAVE BAD SMELL. (M) 2 L 7 2 4F A16WE 2001072500119 20010725 00119 NM 2001 7 25 ASAA0110206 1 20010409 A 5310 66221622 SHEAR TIE BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PHD - DURING SCHEDULED C-CHECK, FOUND SHEAR TIE AT BODY STATION 460, STRINGER 18L CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001072500120 20010725 00120 NM 2001 7 25 ASAA0110237 1 20010425 A 5313 654576528 STRINGER BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PHX - DURING SCHEDULED C-CHECK, FOUND STRINGER 10R AT BS 539, CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001072500121 20010725 00121 NM 2001 7 25 ASAA0110239 1 20010428 A 5210 6574583 HANDLE BOEING 737 737290C 138448V NM L2 DOOR LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING MAINTENANCE CHECK, FOUND L2 DOOR HANDLE STIFF. LUBED HANDLE, THEN HANDLE OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2001072500122 20010725 00122 NM 2001 7 25 ASAA0110251 1 20010501 A 5320 65457842 SPLICE BOEING 737 737290C 138448V NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, BUTT SPLICE STRAP AT BS 908, STRINGER 14R CUT. REPAIRED PER EA. (M) 2 L 7 2 4F A16WE 2001072500123 20010725 00123 NM 2001 7 25 ASAA0110329 1 20010608 A 5313 6545833521 STRINGER BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER 17L AT BS 179, CRACKED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2001072500124 20010725 00124 NM 2001 7 25 ASAA0110330 1 20010608 A 5310 65518957 STRUCTURE BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND LT MLG WW CUTOUT AT BS 663-727, WATERLINE 150 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001072500125 20010725 00125 NM 2001 7 25 ASAA0110331 1 20010608 A 5313 654577758 STRINGER BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER 25L AT BS 924 CORRODED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2001072500126 20010725 00126 NM 2001 7 25 ASAA0110332 1 20010608 A 5310 69514959 SHEAR TIE BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND SHEAR TIE AT BS 924, STRINGER 19L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001072500127 20010725 00127 NM 2001 7 25 ASAA0110333 1 20010608 A 5315 654681140 FLOORBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 986.5, WATERLINE 208 CORRODED. REPAIRED PER EA. ( M) 2 L 7 2 4F RT A16WE 2001072500128 20010725 00128 NM 2001 7 25 ASAA0110334 1 20010608 A 5320 6720382 INTERCOSTAL BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND INTERCOSTAL AT BS 178, WATERLINE 207 CRACKED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2001072500129 20010725 00129 NM 2001 7 25 ASAA0110335 1 20010608 A 5414 65C1409411 SKIN BOEING 737 7372X6C 1384552 NM NACELLE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND FAIRING SKIN AT NACELLE STATION 113.79, NACELLE WATERLINE 126.14 DENTED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2001072500130 20010725 00130 NM 2001 7 25 ASAA0110406 1 20010620 A 5330 65C3674597 SKIN PANEL BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND SKIN PANEL REPAIR AT BS 727, STRINGER 23L-24L REQUIRED PERMANENT REPAIR. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001072500131 20010725 00131 NM 2001 7 25 ASAA0110407 1 20010620 A 5320 69497191 INTERCOSTAL BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL AT BS 330, STRINGER 26L-27L CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001072500132 20010725 00132 NM 2001 7 25 ASAA0110408 1 20010620 A 5311 65621791 FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 348.2, STRINGER 11L-12L GOUGED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2001072500133 20010725 00133 NM 2001 7 25 ASAA0110409 1 20010620 A 5320 656714024 FLOOR SUPPORT BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT AT BS 520-540, LBL 45 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001072500134 20010725 00134 NM 2001 7 25 ASAA0140034 1 20010309 A 5330 65C3576716 SKIN BOEING 737 737490 1384715 NM FUSELAGE PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 706AS 28895 PAE - DURING LINE CHECK, FOUND PUNCTURE IN SKIN AT BS 363 TO 371, WATER LINE 207 AND STRINGER 17L. REPAIRED IAW EA 5330 -01509. (M) 2 L 7 2 4F RT A16WE 2001072500135 20010725 00135 NM 2001 7 25 ASAA0140040 1 20010325 A 5311 651630086 FRAME BOEING 737 7374Q8 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 779AS 25111 PAE - DURING SI CHECK, FOUND SIDE CHORD ON LEFT AND RIGHT SIDE AT BS 178 AND WL 207 CRACKED. REPAIR PENDING. (M) 2 L 7 2 4F RT A16WE 2001072500136 20010725 00136 NM 2001 7 25 ASAA0140041 1 20010325 A 5315 6546809161 FLOORBEAM BOEING 737 7374Q8 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 779AS 25111 PAE - DURING SI CHECK, FOUND CORROSION ON FLOORBEAM AT BS 947, RT BL 4 AND WL 208, LEVEL II. REPAIRED PER SRM 53-00-51. (M) 2 L 7 2 4F RT A16WE 2001072500137 20010725 00137 NM 2001 7 25 ASAA0140042 1 20010325 A 5315 65C339521 FLOORBEAM BOEING 737 7374Q8 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 779AS 25111 PAE - DURING SI CHECK, FOUND CORROSION ON FLOORBEAM NUT PLATE HOLES AT BS 986.5 LBL 2 TO 43 AND WL 208, LEVEL 2. REPAIR PENDING. (M) 2 L 7 2 4F RT A16WE 2001072500138 20010725 00138 NM 2001 7 25 ASAA0140043 1 20010328 A 5330 655053138 DOUBLER BOEING 737 7374Q8 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 779AS 25111 PAE - DURING SI CHECK, FOUND EXTERNAL POWER CUT OUT INTERNAL SKIN DOUBLER IS CRACKED AT TWO LOCATIONS FORWARD LOWER CORN ER AT STATION 228 AND RBL 30 AND WL 175 TO 185. REPAIRED IAW EA 5330-01514. (M) 2 L 7 2 4F RT A16WE 2001072500139 20010725 00139 NM 2001 7 25 ASAA0140044 1 20010328 A 5320 6545872 SILL BOEING 737 7374Q8 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 779AS 25111 PAE - DURING SI CHECK, FOUND CORROSION ON MOPSILL AT BS 334, WL 208 AND RBL 57 , LEVEL II. REPLACED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2001072500140 20010725 00140 NM 2001 7 25 ASAA0140045 1 20010329 A 5320 6552878518 SILL BOEING 737 7374Q8 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 779AS 25111 PAE - DURING SI CHECK, FOUND CORROSION ON MOPSILL AT BS 943-998, LBL 52 AND WL 208 (LEVEL II) REPLACED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2001072500141 20010725 00141 NM 2001 7 25 ASAA0140046 1 20010330 A 5320 65C1612113 SUPPORT FITTING BOEING 737 7374Q8 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 779AS 25111 PAE - DURING SI CHECK, FOUND CORROSION ON GIRT BAR SUPPORT FITTING AT BS 312, WL 208, LBL 55. REPLACED IAW WITH SRM. ( M) 2 L 7 2 4F RT A16WE 2001072500142 20010725 00142 NM 2001 7 25 ASAA0140047 1 20010330 A 5320 65C1612110 SUPPORT FITTING BOEING 737 7374Q8 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 779AS 25111 PAE - DURING SI CHECK, FOUND GIRT BAR SUPPORT FITTING CORRODED AT BS 344, WL 208 AND LBL 56 (LEVEL II). REPLACED IAW SR M. (M) 2 L 7 2 4F RT A16WE 2001072500143 20010725 00143 NM 2001 7 25 ASAA0140056 1 20010411 A 5320 69353521 STRINGER CLIP BOEING 737 7374Q8 NM FUSELAGE BENT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 779AS 25111 PAE - DURING SI CHECK, FOUND AFT CARGO BAY STRINGER CLIP AT STRINGER RT, WL 158, BL 27 LEFT AND BS 727F IS BENT. REPLAC ED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2001072500144 20010725 00144 NM 2001 7 25 ASAA0140057 1 20010412 A 5347 654659249 CARGO TRACK BOEING 737 7374Q8 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 779AS 25111 PAE - DURING SI CHECK, FOUND AFT CARGO BAY FLOOR TRACK AT BS 750 TO BS 756, WL 150 AND BL 3 LEFT AND RIGHT DAMAGED. REP AIRED IAW ASA EA 5320-01378. (M) 2 L 7 2 4F RT A16WE 2001072500145 20010725 00145 NM 2001 7 25 ASAA0140058 1 20010412 A 5754 6546430184 SKIN BOEING 737 7374Q8 NM L/E FLAP PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 779AS 25111 PAE - DURING SI CHECK, FOUND RIGHT INBOARD FORE FLAP LOWER SKIN IS PUNCTURED 19 INCHES FROM INBOARD END AND 9 INCHES FRO M TRAILING EDGE. REPAIRED IAW SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2001072500146 20010725 00146 NM 2001 7 25 ASAA0140063 1 20010506 A 5210 HINGE BOEING 737 7374Q8 NM L1 DOOR LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 764AS 25101 SEA - BEFORE FLIGHT, FLIGHT ATTENDANT REPORTED L1 DOOR DIFFICULT TO OPEN. LUBED DOOR AND HINGE POINTS, OPERATIONAL CHEC K NORMAL. (M) 2 L 7 2 4F RT A16WE 2001072500147 20010725 00147 NM 2001 7 25 ASAA0140066 1 20010504 A 5311 651630087 FRAME BOEING 737 7374Q8 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 780AS 25112 PAE - DURING SI CHECK, FOUND CHORD CRACKED .25 INCH LONG AT BS 178, WL 207, AND BUTT LINE 25 LEFT AND RIGHT SIDES. REPA IRED IAW EA. (M) 2 L 7 2 4F RT A16WE 2001072500148 20010725 00148 NM 2001 7 25 ASAA0140067 1 20010504 A 5330 65C3579514 SKIN BOEING 737 7374Q8 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 780AS 25112 PAE - DURING SI CHECK, FOUND SKIN DENTED AT BS 843, WL 175, AND STRINGER 21 RT. REPAIRED IAW EA. (M) 2 L 7 2 4F RT A16WE 2001072500149 20010725 00149 NM 2001 7 25 ASAA0140068 1 20010504 A 5315 654681188 FLOORBEAM BOEING 737 7374Q8 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 780AS 25112 PAE - DURING SI CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 486.5, WL 208 AND BUTT LINE 13.5 TO 19.5. (M) 2 L 7 2 4F RT A16WE 2001072500150 20010725 00150 NM 2001 7 25 ASAA0140069 1 20010504 A 5315 65C332681 FLOORBEAM BOEING 737 7374Q8 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 780AS 25112 PAE - DURING SI CHECK, FOUND CORROSION ON UPPER CHOD OF 947 FLOORBEAM AT BS 947, WL 208, AND LBL 15 TO RBL 15. (M) 2 L 7 2 4F RT A16WE 2001072500151 20010725 00151 NM 2001 7 25 ASAA0140082 1 20010604 A 7830 315A1001563SP THRUST REVERSER BOEING 737 7374Q8 NM RT ENGINE WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 SEA - DURING C-CHECK, FOUND RIGHT ENGINE THRUST REVERSER BULLNOSE WORN IN SEVERAL AREAS FROM CONTACT WITH BLOCKER DOORS AT THE NR 1, 3 AND 5 O'CLOCK POSITIONS. REPAIRED IAW ENGINEERING AUTHORIZATION. (M) 2 L 7 2 4F RT A16WE 2001072500152 20010725 00152 NM 2001 7 25 ASAA0140083 1 20010604 A 7110 315A1562515 COWLING BOEING 737 7374Q8 NM RT ENGINE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PAE - DURING C-CHECK, FOUND RIGHT ENGINE INLET COWL OUTSIDE RIGHT SURFACE DAMAGED AT 4 O'CLOCK AND 6 INCHES FORWARD OF A FT FLANGE. REPAIRED IAW ENGINEERING AUTHORIZATION. (M) 2 L 7 2 4F RT A16WE 2001072500153 20010725 00153 NM 2001 7 25 ASAA0140084 1 20010604 A 5320 654587545 FLOOR SUPPORT BOEING 737 7374Q8 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 SEA - DURING C-CHECK, FOUND LOWER FUSELAGE AFT CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT STATION 857 LBL 12.50. REPAI RED IAW ENGINEERING AUTHORIZATION. (M) 2 L 7 2 4F RT A16WE 2001072500154 20010725 00154 NM 2001 7 25 ASAA0140085 1 20010604 A 5410 311A11111 STRUCTURE BOEING 737 7374Q8 NM NR 2 PYLON DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 SEA - DURING C-CHECK, FOUND RIGHT ENGINE STRUT PYLON NR 2 CROWN BEAM AFT BEARING BORE HAS PITTING ON INNER SURFACE. REP AIRED IAW ENGINEERING AUTHORIZATION. (M) 2 L 7 2 4F RT A16WE 2001072500155 20010725 00155 NM 2001 7 25 ASAA0140086 1 20010604 A 5510 6548237501 ATTACH FITTING BOEING 737 7374Q8 NM HORIZ STAB GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 SEA - DURING C-CHECK, FOUND RIGHT HORIZONTAL STABILIZER AFT SPAR ATTACH FITTING UPPER LUG ON FUSELAGE GOUGED. REPAIRED IAW ENGINEERING AUTHORIZATION. (M) 2 L 7 2 4F RT A16WE 2001072500156 20010725 00156 NM 2001 7 25 ASAA0140087 1 20010504 A 5330 65C3579514 SKIN BOEING 737 7374Q8 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 780AS 25112 PAE - DURING SI CHECK, FOUND SKIN DENTED AT BS 843, WL 175, AND STRINGER 21 RIGHT. (M) 2 L 7 2 4F RT A16WE 2001072500157 20010725 00157 WP 2001 7 25 RRXA10837 1 20010202 A 5312 NPN LONGERON DOUG DC8 DC871F 302199D WP STA.1260 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 34 46039 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON FITTING L34L AT STA 1260 AND C-PIT, DAMAGE EXCEEDED LIMITA TIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVE DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INST ALLED IAW DC-8 SRM 53-2-2 FIG. 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500158 20010725 00158 WP 2001 7 25 RRXA10839 1 20010215 A 5312 NPN ATTACH ANGLE DOUG DC8 DC871F 302199D WP STA.Y+14Z-7X-24 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO AFT LWR CARGO COMPARTMENT BULKHEAD DIVIDERS ATTACH ANLGE AT STA Y+14, Z -7, X-24, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 S RM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001072500159 20010725 00159 WP 2001 7 25 RRXA10855 1 20010202 A 5321 NPN PANEL DOUG DC8 DC871F 302199D WP CENTER FL. PANEL CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO CENTER FLOOR PANEL BEHIND CENTER PADISTAL EDGE BENT & CRACKED AT SCREW HOLE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 5 1-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-3-0 & 51-1-21 & 53-2-3. 2 L 7 4 4F RT 4A25 2001072500160 20010725 00160 WP 2001 7 25 RRXA10858 1 20010119 A 5321 NPN WEB DOUG DC8 DC871F 302199D WP STA 140-220 X=45 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO CABIN FLOOR BEAM WEB AT STA. 140-220 X=45, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTA LLED IAW DC-8 SRM 51-1-21 & 53-2-0. 2 L 7 4 4F RT 4A25 2001072500161 20010725 00161 WP 2001 7 25 RRXA10859 1 20010207 A 5321 NPN FLOOR PANEL DOUG DC8 DC871F 302199D WP STA 480-560 DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO FLOOR PANEL BETWEEN TRACKS 1 & 2 AT STA. 480-560, DAMAGE EXCEED ED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PA RT AND INSTALLED IAW DC-8 SRM 51-3-0 AND DOUGLAS DRAWING #5804513. 2 L 7 4 4F RT 4A25 2001072500162 20010725 00162 WP 2001 7 25 RRXA10860 1 20010309 A 5312 NPN SKIN DOUG DC8 DC871F 302199D WP STA640-610 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FILLET ATTACH HOLES AT STA. 640-610 AND L31L TO L28L, DAMAGE EXCEED ED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED RE PAIR AND INSTALLED IAW DC-8 SRM 53-2-0 AND E.O.#01-024 WITH APPROVED 8110-3 DATED 03/08/01. (CORROSION DAMAGE RECORDED I N EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500163 20010725 00163 WP 2001 7 25 RRXA10861 1 20010314 A 5312 NPN FRAME DOUG DC8 DC871F 302199D WP SAT 1140-1160 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BRACKET AT STA. 1140-1160 AND L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED I AW DC-8 SRM 51-1-20D & 51-1-4 & 53-2-0 FIG1F. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500164 20010725 00164 WP 2001 7 25 RRXA10865 1 20010203 A 5321 NPN PANEL DOUG DC8 DC871F 302199D WP PANEL #676B CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO CO-PILOTS FLOOR PANEL #676B AROUND PERIMETER, DAMAGE EXCEEDED LIMIT ATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND I NSTALLED IAW DC-8 SRM 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500165 20010725 00165 WP 2001 7 25 RRXA10866 1 20010203 A 5321 NPN PANEL DOUG DC8 DC871F 302199D WP PANEL #676A CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENACE VISIT FOUND CORROSION DAMAGE TO R/H COCKPIT FLOOR PANEL #676A, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC- 8 SRM 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500166 20010725 00166 WP 2001 7 25 RRXA10867 1 20010204 A 5321 NPN PANEL DOUG DC8 DC871F 302199D WP PANEL #676F CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO COCKPIT FLOOR PANEL #676F, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM . /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 S RM 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500167 20010725 00167 WP 2001 7 25 RRXA10868 1 20010227 A 5312 DOUGLAS FITTING DOUG DC8 DC871F 302199D WP STA1690 L30R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION TO BATH TUBE FITTING AT STA. 1690 AND L30R, DAMAGE EXCEEDED LIMITATIONS IAW D C-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW D C-8 SRM 51-1-21 & 51-1-20D & 51-1-24 & 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500168 20010725 00168 WP 2001 7 25 RRXA10869 1 20010204 A 5321 NPN PANEL DOUG DC8 DC871F 302199D WP PANEL#678 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL #678 UNDER F/E TABLE, DAMAGE EXCEEDED LIMITATIONS IAW D C-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500169 20010725 00169 WP 2001 7 25 RRXA10870 1 20010204 A 5312 NPN FITTING DOUG DC8 DC871F 302199D WP STA.1690 L32R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATH TUBE FITTING AT STA. 1690 AND L32R, DAMAGE EXCEEDED LIMITATION S IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLE D IAW DC-8 SRM 51-1-24 & 51-1-21 & 51-1-20D &51-1-3. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500170 20010725 00170 WP 2001 7 25 RRXA10871 1 20010202 A 5321 NPN PANEL DOUG DC8 DC871F 302199D WP STA55-80 X+32 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO GALLEY FLOOR TOP SURFACE PANEL #328 AT STA. 55-80 AND X+32, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICA TED PART AND INSTALLED IAW DC-8 SRM 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500171 20010725 00171 WP 2001 7 25 RRXA10872 1 20010131 A 5321 NPN PANEL DOUG DC8 DC871F 302199D WP STA55-80 X+16 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO GALLEY FLOOR TOP SURFACE PANEL #327 AT STA. 55-80 AND X+16, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICA TED PART AND INSTALLED IAW DC-8 SRM 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500172 20010725 00172 WP 2001 7 25 RRXA10885 1 20010324 A 5700 5769589 RIB DOUG DC8 DC873F 302199F WP L/H CTR L/E CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H CENTER L/E AT STA XFS 291-500 AND 304.000, DAMAGE EXCEEDED LIMITATIO NS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2, 51-1-21 AND 51- 1-20D. 2 L 7 4 4F RT 4A25 2001072500173 20010725 00173 WP 2001 7 25 RRXA10887 1 20010324 A 5310 37558451N FITTING DOUG DC8 DC873F 302199F WP FS 1220 L33L-34L CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A LARGE GAP BETWEEN O/B END FITTING AND BATHTUB FITTING AT FS 1220 AND L33L TO L34L, DA MAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-1-0 AND DWG 3755845. 2 L 7 4 4F RT 4A25 2001072500174 20010725 00174 WP 2001 7 25 RRXA10892 1 20010322 A 5700 5769589 RIB DOUG DC8 DC873F 302199F WP XFS 422.750 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB TIP ON THE L/H L/E WING CENTER AT STA XFS 422.750, DAMAGE EXCEEDED L IMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAAW DC-8 SRM 57-2-0, FIG AND 51-1 -20D. 2 L 7 4 4F RT 4A25 2001072500175 20010725 00175 WP 2001 7 25 RRXA10895 1 20010325 A 5310 2772660 SEAT TRACK DOUG DC8 DC873F 302199F WP FS590-980 LBL48 WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND THE SEAT TRACK WORN BEYOND LIMITS AT STA 590 TO 980 LBL 48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-3, FIG 8A AND 53-7-1, FIG 4. 2 L 7 4 4F RT 4A25 2001072500176 20010725 00176 WP 2001 7 25 RRXA10899 1 20010322 A 5330 57799157 DOUBLER DOUG DC8 DC873F 302199F WP FS1350 L32R CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE FINGER DOUBLER AT FS 1350 L32R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM . /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-1-21 AND DWG 5779915. 2 L 7 4 4F RT 4A25 2001072500177 20010725 00177 WP 2001 7 25 RRXA10904 1 20010328 A 5750 5655752 SKIN DOUG DC8 DC873F 302199F WP L/H O/B FLAP GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A GOUGE TO THE L/H O/B FLAP UPPER SKIN O/B OF FLAP HINGE 340, DAMAGE EXCEEDED LIMITATIO NS IAW DC-8 SRM. /////CORRECTIVE ACTION///// RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-1, FIG 2Q. 2 L 7 4 4F RT 4A25 2001072500178 20010725 00178 WP 2001 7 25 RRXA10905 1 20010328 A 5750 5642960 SKIN DOUG DC8 DC873F 302199F WP L/H I/B FLAP GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A GOUGE AT FLAP HINGE 98 L/H I/B FLAP UPPER SKIN, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-1, FIG 2Q. 2 L 7 4 4F RT 4A25 2001072500179 20010725 00179 WP 2001 7 25 RRXA10906 1 20010328 A 5310 5750864 SEAT TRACK DOUG DC8 DC873F 302199F WP STA 146 WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A WORN SEAT TRACK IN THE MAIN CABIN AT STA 130-510 AT RBL 24, DAMAGE EXCEEDED LIMITATIO NS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3 FIG 14 AND DWG 5750864. 2 L 7 4 4F RT 4A25 2001072500180 20010725 00180 WP 2001 7 25 RRXA10910 1 20010329 A 5310 DHM1630541 DOUBLER DOUG DC8 DC873F 302199F WP STA 70 RBL 30 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE BULKHEAD HORIZ. INTERCOSTAL AT STA 70 RBL 30 ABOVE L30R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21 AND 51-1-20D . 2 L 7 4 4F RT 4A25 2001072500181 20010725 00181 WP 2001 7 25 RRXA10914 1 20010403 A 5310 4550170 INTERCOSTAL DOUG DC8 DC873F 302199F WP STA 1870 @ 3'OCL CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO INTERCOSTAL #62 HOLE AT 3 O'CLOCK AT STA 1870, DAMAGE EXCEEDED LIMITATIONS I AW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-11 AND DWG 4550170. 2 L 7 4 4F RT 4A25 2001072500182 20010725 00182 WP 2001 7 25 RRXA10915 1 20010403 A 5310 5753352 FRAME DOUG DC8 DC873F 302199F WP FS 1580 L21R BENT A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A BENT FRAME AT FS 1580 L21R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIV E ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-8, 53-2-0 AND DWG 5753352. 2 L 7 4 4F RT 4A25 2001072500183 20010725 00183 WP 2001 7 25 RRXA10916 1 20010404 A 5310 SR08530027 DOUBLER DOUG DC8 DC873F 302199F WP AFT LWR MCD CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND 4 CRACKS AT AFT LWR CORNER OF MCD APPROX 3/8" LONG, DAMAGE EXCEEDED LIMITATIONS IAW DC- 8S RM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8S RM 51-1-20D, 51-1-21A AND DWG SR08530027. 2 L 7 4 4F RT 4A25 2001072500184 20010725 00184 WP 2001 7 25 RRXA10917 1 20010405 A 5730 5758382 SKIN DOUG DC8 DC873F 302199F WP XRS 421 L/H WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A 1/2" CRACK ON THE LEFT WING UPPER SKIN AT STA XRS 721 AND STRINGER 3, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 57-2-1, FI G 10 AND 51-1-11. 2 L 7 4 4F RT 4A25 2001072500185 20010725 00185 WP 2001 7 25 RRXA10918 1 20010406 A 5310 5779932 FRAME DOUG DC8 DC873F 302199F WP L10R-L11R FS 190 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND DAMAGE TO THE FRAME ON THE R/H FWD SERVICE DOOR JAMB AFT AT STA 190 BETWEEN L10R-L11R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED AND INSTALLED PART IAW DC-8 SRM 53-2-0 , FIG 2 AND 51-1-21. 2 L 7 4 4F RT 4A25 2001072500186 20010725 00186 WP 2001 7 25 RRXA10920 1 20010406 A 5310 37540511N FITTING DOUG DC8 DC873F 302199F WP A-PIT DOOR FRAME CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE A-PIT DOOR FRAME LWR #5 LATCH FITTING, DAMAGE EXCEEDED LIMITATI ONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED P ART AND INSTALLED IAW DC-8 SRM 51-1-20D AND 53-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500187 20010725 00187 WP 2001 7 25 RRXA10921 1 20010406 A 5310 464011112 FITTING DOUG DC8 DC873F 302199F WP L33L, STA 8 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FITTING AT LONGERON 33L AT STA 8, DAMAGE EXCEEDED LIMITATIONS I AW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART A ND INSTALLED IAW DC-8 SRM 51-1-21 AND 53-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500188 20010725 00188 WP 2001 7 25 RRXA10922 1 20010406 A 5710 5769811 ANGLE DOUG DC8 DC873F 302199F WP L/H CTR L/E CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H CENTER L/E SLOT ANGLE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. // ///CORRECTIVE ACTION///// FABRICATED AND INSTALLED PART IAW DC-8 SRM 51-1-21 . 2 L 7 4 4F RT 4A25 2001072500189 20010725 00189 WP 2001 7 25 RRXA10923 1 20010406 A 5730 5641252 DOUBLER DOUG DC8 DC873F 302199F WP L/H L/E XFS 304 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE INTERNAL DOUBLER LOWER SKIN L/H WING L/E AT STA XFS 304, DAMAGE EXCEEDE D LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED AND INSTALLED PART IAW DC-8 SRM 51-1-21, 51-1-20D A ND DWG 5641252. 2 L 7 4 4F RT 4A25 2001072500190 20010725 00190 WP 2001 7 25 RRXA10924 1 20010406 A 5330 5779934 SKIN DOUG DC8 DC873F 302199F WP B-PIT LWR FUSELA CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE UNDER THE FUSELAGE SKIN B-PIT SCUFF PLATE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPA IR AND INSTALLED IAW DC-8 SRM 53-2-0, FIG 20 AND 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500191 20010725 00191 WP 2001 7 25 RRXA10925 1 20010407 A 5310 5644981 FRAME DOUG DC8 DC873F 302199F WP R/H NOSE STA 58 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE FRAME ON THE R/H NOSE TUNNEL AT STA 58, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0, FIG 23 AND 51-1-21. 2 L 7 4 4F RT 4A25 2001072500192 20010725 00192 WP 2001 7 25 RRXA10927 1 20010407 A 5310 37558442 FITTING DOUG DC8 DC873F 302199F WP FS 1160 & 1180 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BATHTUB FITTING AT STA 1160 & 1180 AND L30L TO L31L, DAMAGE EXC EEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1- 8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-0, FIG 2D AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION P ROGRAM). 2 L 7 4 4F RT 4A25 2001072500193 20010725 00193 WP 2001 7 25 RRXA10928 1 20010407 A 5730 5769857 SKIN DOUG DC8 DC873F 302199F WP STA XFS 430 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE STRAP ON THE L/H WING LOWER SKIN SIDE JUST INBD OF #1 PYLON AT STA XFS 4 30, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 5 1-1-21 AND 57-2-1, FIG A. 2 L 7 4 4F RT 4A25 2001072500194 20010725 00194 WP 2001 7 25 RRXA10929 1 20010407 A 5310 5758876 FRAME DOUG DC8 DC873F 302199F WP STA 67 RH TUNNEL CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE FRAME ON THE R/H NOSE TUNNEL AT STA 67, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0, FIG 23 AND 51-1-8. 2 L 7 4 4F RT 4A25 2001072500195 20010725 00195 WP 2001 7 25 RRXA10930 1 20010407 A 5330 58920415 FLOOR PANEL DOUG DC8 DC873F 302199F WP FS 580-1000 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE MAIN CARGO FLOOR PANEL FROM STA 580 TO 867 LBL 24 TO LBL 48, DA MAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 S RM 51-1-8. FABRICATED AND INSTALLED PART IAW DWG 589041. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500196 20010725 00196 WP 2001 7 25 RRXA10931 1 20010407 A 5310 5757583 LONGERON DOUG DC8 DC873F 302199F WP L31L FS 1255 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LOWER FLANGE OF LONGERON AT FS 1255 L31L, DAMAGE EXCEEDED LIMIT ATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICA TED AND INSTALLED PART IAW DC-8 SRM 51-2-21 AND 51-1-8. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500197 20010725 00197 WP 2001 7 25 RRXA10933 1 20010407 A 5330 577991643 FINGER DOUBLER DOUG DC8 DC873F 302199F WP L31R STA 70-80 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FINGER DOUBLER AT STA 70 TO 80 AND L31R, DAMAGE EXCEEDED LIMITA TIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICAT ED AND INSTALLED PART IAW DC-8 SRM 51-1-21, 51-1-20D AND DWG 5779916. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGR AM). 2 L 7 4 4F RT 4A25 2001072500198 20010725 00198 WP 2001 7 25 RRXA10935 1 20010408 A 5240 5613836 TRACK DOUG DC8 DC873F 302199F WP DOOR #12 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A/C DOOR #12 FWD TRACK MISSING A PIECE OF METAL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-1-0, 51-1-21 AND DWG 5613836. 2 L 7 4 4F RT 4A25 2001072500199 20010725 00199 WP 2001 7 25 RRXA10938 1 20010410 A 5330 DHSK6027871 RETAINER DOUG DC8 DC873F 302199F WP C-PIT DOOR LWR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE C-PIT DOOR LOWER RETAINER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. // ///CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21 AND DH SK602-787. 2 L 7 4 4F RT 4A25 2001072500200 20010725 00200 WP 2001 7 25 RRXA10939 1 20010410 A 5730 5643000 PANEL DOUG DC8 DC873F 302199F WP R/H WING UPR T/E CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE R/H WING UPPER T/E PANEL AFT OF REAR SPAR, DAMAGE EXCEEDED LIMI TATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND IN STALLED PART IAW DC-8 SRM 51-1-9 AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500201 20010725 00201 WP 2001 7 25 RRXA10941 1 20010410 A 5730 5769600 SKIN DOUG DC8 DC873F 302199F WP LT WING O/B L/E CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LEFT WING O/B L/E SKIN BETWEEN STA'S XFS 578.75 TO 641.25, DAMA GE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RE CEIVED REPAIR AND INSTALLED IAW DH SK 602-379. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500202 20010725 00202 WP 2001 7 25 RRXA10942 1 20010410 A 2760 5642860 SKIN DOUG DC8 DC873F 302199F WP LH WING #4 SPOIL CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE L/H WING #1 SPOILER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALL ED IAW DC-8 SRM 51-1-9H AND 57-7-1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500203 20010725 00203 WP 2001 7 25 RRXA10944 1 20010411 A 5310 37558422 FITTING DOUG DC8 DC873F 302199F WP AFT LWR CARGO CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK BETWEEN LONBERON 28L AND 29L AT STA 1160, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-0, FIG 2D. 2 L 7 4 4F RT 4A25 2001072500204 20010725 00204 WP 2001 7 25 RRXA10945 1 20010411 A 5730 5769600 SKIN DOUG DC8 DC873F 302199F WP R/H WING L/E CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE R/H WING O/B L/E UPPER SKIN AT XFS 703.75, DAMAGE EXCEEDED LIMITATIONS I AW DC-8 SRM. /////CORRECTIVE ACTION///// RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-1, FIG 38. 2 L 7 4 4F RT 4A25 2001072500205 20010725 00205 WP 2001 7 25 RRXA10950 1 20010411 A 2710 5705334 AILERON DOUG DC8 DC873F 302199F WP LH I/B AIL O/B DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND BUCKLED SKIN L/H INBD AILERON UPPER LWR SKINS JUST FWD OF TAB O/B L/E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND 57-2-0, FIG 1B. 2 L 7 4 4F RT 4A25 2001072500206 20010725 00206 WP 2001 7 25 RRXA10951 1 20010412 A 5310 5616674 CHANNEL DOUG DC8 DC873F 302199F WP L34R FS1400-1420 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE UNDER STRAP ON LONGERON 34R AT STA 1400 TO 1420, DAMAGE EXCEEDED LIMIT ATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICA TED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND DAC DWG 5616674. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500207 20010725 00207 WP 2001 7 25 RRXA10952 1 20010412 A 5730 5611350 SKIN DOUG DC8 DC873F 302199F WP RH WING UPR SKIN CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON THE RH WING UPPER SKIN 10" FWD OF REAR SPAR & UNDER EXISTING DOUBLE R AT STA XRS -6, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRI MED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-1, FIG 20. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500208 20010725 00208 WP 2001 7 25 RRXA10953 1 20010412 A 5330 97549241N SKIN DOUG DC8 DC873F 302199F WP STA 1050-1350 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AFT BELLY SKIN AT STA 1050 TO 1350 L31R TO L31L, DAMAGE EXCEEDE D LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-1-0, 51-1-21 AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROG RAM). 2 L 7 4 4F RT 4A25 2001072500209 20010725 00209 WP 2001 7 25 RRXA10958 1 20010412 A 5730 5769935 SKIN DOUG DC8 DC873F 302199F WP L/H O/B SLOT CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H O/B SLOT VANE UPPER I/B SECTION, DAMAGE EXCEEDED LIMITATIONS IAW DC- 8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-8 AND 57-2-0, FIG 2A. 2 L 7 4 4F RT 4A25 2001072500210 20010725 00210 WP 2001 7 25 RRXA10959 1 20010412 A 5750 564300 PANEL DOUG DC8 DC873F 302199F WP L/H WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H WING LOWER T/E PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /// //CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-9A. 2 L 7 4 4F RT 4A25 2001072500211 20010725 00211 WP 2001 7 25 RRXA10962 1 20010412 A 5310 97540552 FITTING DOUG DC8 DC873F 302199F WP AFT LWR CARGO CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE FLOOR PANEL SUPPORT FITTING AT STA 1220 AND L35R, DAMAGE EXCEEDED LIMITA TIONS IAW DC-8 SRM. /////OPEN///// 2 L 7 4 4F RT 4A25 2001072500212 20010725 00212 WP 2001 7 25 RRXA10964 1 20010412 A 5710 564300012 STIFFENER DOUG DC8 DC873F 302199F WP R/T WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT WING T/E VERT. STIFFENER AT STA XW 75.31, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2. 2 L 7 4 4F RT 4A25 2001072500213 20010725 00213 WP 2001 7 25 RRXA10969 1 20010413 A 5310 5758878 FRAME DOUG DC8 DC873F 302199F WP FS1440 L34R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LOWER FRAME AT FS 1440 AND L34R, DAMAGE EXCEEDED LIMITATIONS IA W DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED P ART IAW DC-8 SRM 53-2-0, FIG 1B. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500214 20010725 00214 WP 2001 7 25 RRXA10972 1 20010414 A 5310 4611067501N FITTING DOUG DC8 DC873F 302199F WP L27R STA 70-80 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 27R END FITTING AT STA 70 TO 80, DAMAGE EXCEEDED LIMITATIO NS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND IN STALLED IAW DC-8 SRM 53-1-0, 51-1-21 AND DWG 46110671. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500215 20010725 00215 WP 2001 7 25 RRXA10973 1 20010414 A 5310 5613861 LONGERON DOUG DC8 DC873F 302199F WP STA35-55 L27R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON AT STA 35-55 AND L27R, DAMAGE EXCEEDED LIMITATIONS IAW DC- 8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW 5 3-3-3 FIG.2 AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500216 20010725 00216 WP 2001 7 25 RRXA10974 1 20010414 A 5330 5779913 FINGER DOUBLER DOUG DC8 DC873F 302199F WP STA610 L32L-L33R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FINGER DOUBLER AT STA 610 AND L32LTO L33R, DAMAGE EXCEEDED LIMITATI ONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INST ALLED IAW DC-8 SRM 51-1-20D AND 53-1-0 AND DWG#5779913. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500217 20010725 00217 WP 2001 7 25 RRXA10975 1 20010414 A 5310 5646671 INTERCOSTAL DOUG DC8 DC873F 302199F WP STA1460 L34R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LOWER CORD ON INTERCOSTAL AT STA 1460 AND L34R, DAMAGE EXCEEDED LIM ITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND 53-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500218 20010725 00218 WP 2001 7 25 RRXA10976 1 20010414 A 5330 5646674 WEB DOUG DC8 DC873F 302199F WP L/H MLG WW CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO TOP WEB AFT OF FLAP BOSS CABLE PULLEY AT L/H MLG WW, DAMAGE EXCEEDE D LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REP AIR AND INSTALLED IAW DHSK 602-583. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500219 20010725 00219 WP 2001 7 25 RRXA10978 1 20010414 A 5310 5613861305 LONGERON DOUG DC8 DC873F 302199F WP A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON AT STA 8-70 AND L27R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC -8 SRM 53-1-0, 51-1-20D, 51-1-21 AND DWG#5613861. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500220 20010725 00220 WP 2001 7 25 RRXA10979 1 20010414 A 5310 3755842504N FITTING DOUG DC8 DC873F 302199F WP STA1160L32L-L35L CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING AT STA 1160 AND L32L TO L35L, DAMAGE EXCEEDED LIMIT ATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECIVED PART AND INST ALLED IAW DC-8 SRM 51-1-20D, 53-1-0, AND DWG#3755842. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500221 20010725 00221 WP 2001 7 25 RRXA10981 1 20010415 A 5310 3758496U2 FITTING DOUG DC8 DC873F 302199F WP STA1140 L35R CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FITTING AT STA 1140 AND L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-1-0, 51-1-20D AND DWG#3758496. 2 L 7 4 4F RT 4A25 2001072500222 20010725 00222 WP 2001 7 25 RRXA10984 1 20010415 A 5310 564932744 LONGERON DOUG DC8 DC873F 302199F WP STA1766 L17R CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LONGERON AT STA 1766 AFT OF BULKHEAD AND HOLE#60 AND L17R, DAMAGE EXCEE DED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED P ART AND INSTALLED IAW DC-8 SRM 51-1-21, 53-1-0, 51-1-20D. 2 L 7 4 4F RT 4A25 2001072500223 20010725 00223 WP 2001 7 25 RRXA10985 1 20010415 A 5310 37558541N FITTING DOUG DC8 DC873F 302199F WP STA1200 L27L CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO BANNANA FITTING AT STA 1200 AND L27L, DAMAGE EXCEEDED LIMITATIONS IAW D C-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.RECEIVED PART AND INSTALLED IAW DC -8 SRM 51-1-21, 51-1-20D, 51-3-0. 2 L 7 4 4F RT 4A25 2001072500224 20010725 00224 WP 2001 7 25 RRXA10986 1 20010415 A 5310 3755842503 FITTING DOUG DC8 DC873F 302199F WP STA1180L32L-L33L CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING AT STA 1180 AND L32L TO L33L, DAMAGE EXCEEDED LIMIT ATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND I NSTALLED IAW DC-8 SRM 51-1-20D, DWG#3755842, AND DHSK 602-336. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500225 20010725 00225 WP 2001 7 25 RRXA10987 1 20010416 A 5310 5750298501 LONGERON DOUG DC8 DC873F 302199F WP STA605 L35R CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LONGERON AT STA 605 AND L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SR M 51-1-20D, 53-2-0 FIG.10. 2 L 7 4 4F RT 4A25 2001072500226 20010725 00226 WP 2001 7 25 RRXA10988 1 20010416 A 5310 5750298501 LONGERON DOUG DC8 DC873F 302199F WP STA605 L35L CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON AT STA 605 AND L35L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC- 8 SRM 53-2-2 FIG.10, 51-1-20D, DHSK 602-647. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500227 20010725 00227 WP 2001 7 25 RRXA10989 1 20010416 A 5730 5643000 PANEL DOUG DC8 DC873F 302199F WP XA550 - XA585 DEBONDED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND DEBONDED DAMAGE TO L/H WING UPPER PANEL AT XA550 TO XA585, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTAL LED IAW DC-8 SRM 51-3-0, 51-1-21. 2 L 7 4 4F RT 4A25 2001072500228 20010725 00228 WP 2001 7 25 RRXA10990 1 20010417 A 5730 5750864 SEAT TRACK DOUG DC8 DC873F 302199F WP STA 150-250 WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VIST FOUND WORN DAMAGE TO SEAT TRACK AT STA 150 - 250 AND LBL24 TO LBL30, DAMAGE EXCEEDED LIMITATIO NS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INS TALLED IAW DC-8 SRM 53-2-3 FIG.14. 2 L 7 4 4F RT 4A25 2001072500229 20010725 00229 WP 2001 7 25 RRXA10991 1 20010417 A 5730 576989129 ANGLE DOUG DC8 DC873F 302199F WP LH WING OB SLOT GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO I/B ATTACH ANGLE AT O/B SLOT VANE L/H WING L/E, DAMAGE EXCEEDED LIMITA TIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND IN STALLED IAW DC-8 SRM 51-1-20D AND DWG#5769891. 2 L 7 4 4F RT 4A25 2001072500230 20010725 00230 WP 2001 7 25 RRXA10992 1 20010418 A 2710 5763133 AILERON DOUG DC8 DC873F 302199F WP RH OB AILERON BENT A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND BENT DAMAGE TO R/H OUTBOARD AILERON OUTBOARD TRAILING EDGE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALL ED IAW DC-8 SRM 51-1-21A, 51-1-9A, 51-1-11, AND DWG#5763133. 2 L 7 4 4F RT 4A25 2001072500231 20010725 00231 WP 2001 7 25 RRXA10993 1 20010418 A 5500 5773845 PANEL DOUG DC8 DC873F 302199F WP STA ZR45-ZR74 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO R/H VERT STAB SKIN AT STA ZR45 TO ZR74, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALL ED IAW DC-8 SRM 51-3-0, 51-1-21, 51-1-20D, AND DWG#5773845-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500232 20010725 00232 WP 2001 7 25 RRXA10995 1 20010418 A 5730 5769857 SKIN DOUG DC8 DC873F 302199F WP XOL D16-225 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LH WING LE LWR SKIN AT STA. XOL D16-225, DAMAGE EXCEEDED LIMITATION S IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTAL LED IAW DC-8 SRM 51-1-20D, 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500233 20010725 00233 WP 2001 7 25 RRXA10996 1 20010418 A 5310 5759533 FRAME DOUG DC8 DC873F 302199F WP STA1120 L36 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT SAT 1120 AND L36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM . /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DHSK 602-260. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500234 20010725 00234 WP 2001 7 25 RRXA10997 1 20010418 A 5320 5704735 INTERCOSTAL DOUG DC8 DC873F 302199F WP STA1300 RBL33 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CRACK DAMGE TO C-PIT FLOOR SUPPORT STRAP AT STA. 1300 AND RBL33, DAMAGE EXCEEDED LIMITA TIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND IN STALLED IAW DC-8 SRM 53-2-0, 51-1-21. 2 L 7 4 4F RT 4A25 2001072500235 20010725 00235 WP 2001 7 25 RRXA10998 1 20010419 A 5730 5769859 SKIN DOUG DC8 DC873F 302199F WP XFS 257-500 GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO RT WING UPPER LE AT STA XFS257-500, DAMAGE EXCEEDED LIMITATIONS IAW DC -8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-1-20, DHSK602-706-1. 2 L 7 4 4F RT 4A25 2001072500236 20010725 00236 WP 2001 7 25 RRXA10999 1 20010419 A 5310 36469561 FITTING DOUG DC8 DC873F 302199F WP STA960 LBL60 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING AT STA 940 AND LBL60, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-1-0, DWG#63646956. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500237 20010725 00237 WP 2001 7 25 RRXA11000 1 20010419 A 5730 5769857 SKIN DOUG DC8 DC873F 302199F WP XFS 422-75 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LH LWR WING SKIN AT STA XFS422-75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D, DHSK602-828. 2 L 7 4 4F RT 4A25 2001072500238 20010725 00238 WP 2001 7 25 RRXA11002 1 20010419 A 5310 36471172 FITTING DOUG DC8 DC873F 302199F WP STA960 LBL60 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING AT STA. 960 AND LBL60, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-0FIG8, 51-1-20. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500239 20010725 00239 WP 2001 7 25 RRXA11003 1 20010419 A 5330 5779935 WEB DOUG DC8 DC873F 302199F WP STA70 LBL28 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO BULKHEAD AT STA 70 AND RBL28, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SR M 53-2-0 FIG23. 2 L 7 4 4F RT 4A25 2001072500240 20010725 00240 WP 2001 7 25 RRXA11004 1 20010419 A 5310 5750864 SEAT TRACK DOUG DC8 DC873F 302199F WP STA610-1000LBL24 WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 610-1000 AND RBL24, DAMAGE EXCEEDED LIMITATIONS IAW DC -8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC -8 SRM 53-21-03, 53-2-3 FIG8A. 2 L 7 4 4F RT 4A25 2001072500241 20010725 00241 WP 2001 7 25 RRXA11005 1 20010419 A 5730 5769759 SKIN DOUG DC8 DC873F 302199F WP STA X552 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LH WING LE SKIN AT STA X5520, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SR M 57-1-0, 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 2001072500242 20010725 00242 WP 2001 7 25 RRXA11006 1 20010419 A 5310 37540231N FITTING DOUG DC8 DC873F 302199F WP A-PIT#4LATCH CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING AT A-PIT DOOR FRAME LWR #4 LATCH, DAMAGE EXCEEDED LIMITATIO NS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALL ED IAW DC-8 SRM 53-2-0 FIG2D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500243 20010725 00243 WP 2001 7 25 RRXA11007 1 20010419 A 5310 3755843 FITTING DOUG DC8 DC873F 302199F WP STA1160L35L-L34R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING AT STA 1160 AND L35L TO L34R, DAMAGE EXCEEDED LIMIT ATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INS TALLED IAW DC-8 SRM 53-1-0, 51-1-20D, DWG#3755843. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500244 20010725 00244 WP 2001 7 25 RRXA11009 1 20010419 A 5710 4653423 FITTING DOUG DC8 DC873F 302199F WP STA XW98 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO RH WING INTERCOSTAL FITTING AT STA XW98, DAMAGE EXCEEDED LIMITATIONS IA W DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IA W DC-8 SRM 57-1-0, 51-1-20D, 51-1-21, 51-3-0. 2 L 7 4 4F RT 4A25 2001072500245 20010725 00245 WP 2001 7 25 RRXA11010 1 20010420 A 5315 5779935 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR BEAM LOWER FLANGE AT STA 902 AND LBL48-53, DAMAGE EXCEEDED LI MITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DHSK602-70 8. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500246 20010725 00246 WP 2001 7 25 RRXA11013 1 20010424 A 5310 3755822501 FITTING DOUG DC8 DC873F 302199F WP STA340 L35L-L36L CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO BATHTUB FITTING AT STA 340 AND L35L TO L36L, DAMAGE EXCEEDED LIMITATION S IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLE D IAW DC-8 SRM 51-1-20D, 53-1-0, 53-2-0 FIG2D. 2 L 7 4 4F RT 4A25 2001072500247 20010725 00247 WP 2001 7 25 RRXA11014 1 20010424 A 5310 4758514 FITTING DOUG DC8 DC873F 302199F WP STA1230 L33R CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FITTING AT L33R AND STA 1230, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SR M 51-1-20D, DWG#4758514. 2 L 7 4 4F RT 4A25 2001072500248 20010725 00248 WP 2001 7 25 RRXA11015 1 20010424 A 5310 2772660 SEAT TRACK DOUG DC8 DC873F 302199F WP STA1577-1600 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SEAT TRACK AT STA 1577-1600 AND RBL45, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLE D IAW DC-8 SRM 53-2-3 FIG8A, 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500249 20010725 00249 WP 2001 7 25 RRXA11016 1 20010424 A 5730 5643000 PANEL DOUG DC8 DC873F 302199F WP LH WING DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO PANEL AT LH WING LWR PANEL FWD OF MLG, DAMAGE EXCEEDED LIMITATIO NS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INS TALLED IAW DC-8 SRM 57-3-1, 51-1-9A. 2 L 7 4 4F RT 4A25 2001072500250 20010725 00250 WP 2001 7 25 RRXA11017 1 20010424 A 5310 46401111 FITTING DOUG DC8 DC873F 302199F WP N/WW AFT BLKD CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO N/W/W AFT LWR BLKD FITTING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. / ////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SR M 51-3-0, DWG#4640111. 2 L 7 4 4F RT 4A25 2001072500251 20010725 00251 WP 2001 7 25 RRXA11020 1 20010409 A 5310 5750864525 SEAT TRACK DOUG DC8 DC873F 302199F WP STA146-156 LBL48 WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 146-156 AND LBL48, DAMAGE EXCEEDED LIMITATIONS IAW DC- 8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW D C-8 SRM 53-2-3 FIG14. 2 L 7 4 4F RT 4A25 2001072500252 20010725 00252 WP 2001 7 25 RRXA11022 1 20010427 A 5710 2751571 SPAR CAP DOUG DC8 DC873F 302199F WP XFS32.5-XFS1117 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RH AUX TANK UPPER SPAR CAP AT XFS32.5 AND XFS1117, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAI R AND INSTALLED IAW DC-8 SRM 57-2-1 FIG37, DHSK602-004. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500253 20010725 00253 WP 2001 7 25 RRXA11024 1 20010417 A 5730 6101009 RETAINER DOUG DC8 DC873F 302199F WP STA XW743.750 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LH WING TE STATIC WICK BASE AT STA XW743.750, DAMAGE EXCEEDED LIMIT ATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SB 23-43. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500254 20010725 00254 WP 2001 7 25 RRXA11025 1 20010505 A 5230 58940255 SKIN DOUG DC8 DC873F 302199F WP C-PIT DOOR FRAME DENTED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND DENTED DAMAGE TO C-PIT CROSS SLIDE DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. //// /CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 52- 1-0, 51-1-21. 2 L 7 4 4F RT 4A25 2001072500255 20010725 00255 WP 2001 7 25 RRXA11026 1 20010505 A 5730 5769857 SKIN DOUG DC8 DC873F 302199F WP XFS341-XFS354 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LH WING CENTER LE UPPER SKIN AT STA XFS341 TO XFS354, DAMAGE EXCEED ED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PA RT AND INSTALLED IAW DC-8 SRM 57-2-1 FIG38, 51-1-20D. (CORROSION DAMAGE RECORED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500256 20010725 00256 WP 2001 7 25 RRXA11028 1 20010430 A 5730 5643000 SKIN DOUG DC8 DC873F 302199F WP LH UPPER TE PANE DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LH WING LWR TE PANEL IB OF FLAP HINGE 340, DAMAGE EXCEEDED LIMIT ATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 MM 20-15-01, 20-30-01. 2 L 7 4 4F RT 4A25 2001072500257 20010725 00257 WP 2001 7 25 RRXA11029 1 20010323 A 5310 97585044 LONGERON DOUG DC8 DC873F 302199F WP STA1168-1270 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON AT L33L AND STA 1168-1270, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-2-2 FIG10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500258 20010725 00258 WP 2001 7 25 RRXA11030 1 20010319 A 5310 37558451N FITTING DOUG DC8 DC873F 302199F WP STA 1180 L36L CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING AT STA 1180 AND L36L-L35L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-1-0, 51-1-20D, DWG#3755845. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500259 20010725 00259 WP 2001 7 25 RRXA11031 1 20010310 A 5310 5613861 LONGERON DOUG DC8 DC873F 302199F WP STA35-55 L26R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON AT STA 35-55 AND L26R, DAMAGE EXCEEDED LIMITATIONS IAW DC- 8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW D C-8 SRM 51-1-21, 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500260 20010725 00260 WP 2001 7 25 RRXA11033 1 20010404 A 5730 5758382 SKIN DOUG DC8 DC873F 302199F WP LH WING XRS74 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LH WING UPPER SKIN AT STA XRS74 AND STR #10, DAMAGE EXCEEDED LIMITATION S IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INST ALLED IAW DC-78 SRM 57-2-1 FIQ10. 2 L 7 4 4F RT 4A25 2001072500261 20010725 00261 WP 2001 7 25 RRXA11035 1 20010314 A 5330 NPN DOUBLER DOUG DC8 DC873F 302199F WP STA180-190 L31R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BULGING SKIN AT STA 180-190 AND L31R, DAMAGE EXCEEDED LIMITATIONS I AW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D AND DWG#5779916. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500262 20010725 00262 WP 2001 7 25 RRXA11038 1 20010314 A 5330 NPN DOUBLER DOUG DC8 DC873F 302199F WP STA 70-80 L31R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SKIN DOUBLER AT STA 70-80 AND L31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED I AW DWG#5649028. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM) 2 L 7 4 4F RT 4A25 2001072500263 20010725 00263 WP 2001 7 25 RRXA11039 1 20010313 A 5710 NPN SPAR CAP DOUG DC8 DC873F 302199F WP XFS32.5-XFS142 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RH AUX TANK UPPER SPAR CAP AT STA XFS32.5-XFS142, DAMAGE EXCEEDED L IMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART A ND INSTALLED IAW DC-8 SRM 51-1-25, DC-8 MM 57-20-1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500264 20010725 00264 WP 2001 7 25 RRXA11040 1 20010313 A 5730 NPN SKIN DOUG DC8 DC873F 302199F WP XOLDI6.225 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LH WING CENTER LE UPPER SKIN AT STA XOLDI 6.225 TO XFS422.75, DAMAG E EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRI CATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-1 FIG38, 51-1-21, 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PRO GRAM). 2 L 7 4 4F RT 4A25 2001072500265 20010725 00265 WP 2001 7 25 RRXA11041 1 20010317 A 5340 NPN SEAT TRACK DOUG DC8 DC873F 302199F WP STA 590 RBL60 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SEAT TRACK AT STA 590 AND RBL 60, DAMAGE EXCEEDED LIMITATIONS IAW D C-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3FIG8A, 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500266 20010725 00266 WP 2001 7 25 RRXA11042 1 20010316 A 5100 NPN ANGLE DOUG DC8 DC873F 302199F WP STA1766-1780 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RH VERT STAB SKATE ANGLE AT STA 1766-1780 AND L2R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.FABRICATED PART A ND INSTALLED IAW DC-8 SRM 53-2-5, 51-1-26. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500267 20010725 00267 WP 2001 7 25 RRXA11043 1 20010316 A 5310 NPN FITTING DOUG DC8 DC873F 302199F WP STA 1160-1220 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO ALL 6 T-BOLT FITTINGS AT STA 1160-1220 AND L33R, DAMAGE EXCEEDED LI MITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-1-11. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500268 20010725 00268 WP 2001 7 25 RRXA11044 1 20010315 A 5310 3754930 FITTING DOUG DC8 DC873F 302199F WP Y=1210,X=24 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO C-PIT DOOR LWR #6 LATCH BACK UP FITTING AT STA Y=1210, X=24R, Z=-30 , DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8 . RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500269 20010725 00269 WP 2001 7 25 RRXA11045 1 20010319 A 5310 NPN FITTING DOUG DC8 DC873F 302199F WP STA1150 L36 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON FITTIND AT STA 1150 AND L36, DAMAGE EXCEEDED LIMITATIONS I AW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500270 20010725 00270 WP 2001 7 25 RRXA11046 1 20010320 A 5330 NPN LONGERON DOUG DC8 DC873F 302199F WP STA 1050-1270 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON AT STA1050-1270 AND L36, DAMAGE EXCEEDED LIMITATIONS IAW D C-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, DWG#9758508. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500271 20010725 00271 WP 2001 7 25 RRXA11047 1 20010319 A 5310 NPN FITTING DOUG DC8 DC873F 302199F WP STA1230 L36 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING AT STA 1230 AND L36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500272 20010725 00272 WP 2001 7 25 RRXA11048 1 20010314 A 5310 3755824 FITTING DOUG DC8 DC873F 302199F WP STA300 L33R-L34R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING AT STA 300 AND L33R-L34R, DAMAGE EXCEEDED LIMITATIO NS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALL ED IAW DC-8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500273 20010725 00273 WP 2001 7 25 RRXA11049 1 20010314 A 5310 37540231N FITTING DOUG DC8 DC873F 302199F WP Y=350 X=24R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO A-PIT DOOR FITTING AT STA Y=350, X=24R, Z=-30, DAMAGE EXCEEDED LIMI TATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND IN STALLED IAW DC-8 SRM 53-2-0FIG2D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500281 20010725 00281 WP 2001 7 25 RRXA11064 1 20010105 A 5311 NPN SKIN DOUG DC8 DC871F 302199D WP STA150 L34R-L33R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SKIN AT STA 150 AND L34R TO L33R, DAMAGE EXCEEDED LIMITATIONS IAW D C-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED I AW DC-8 SRM 51-1-21, 51-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500282 20010725 00282 WP 2001 7 25 RRXA11065 1 20010110 A 5311 NPN SKIN DOUG DC8 DC871F 302199D WP STA90 L33R-L34R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SKIN AT STA90 AND L33R TO L34R, DAMAGE EXCEEDED LIMITATIONS IAW DC- 8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-0 1F, 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500283 20010725 00283 WP 2001 7 25 RRXA11066 1 20010104 A 5312 NPN ANGLE DOUG DC8 DC871F 302199D WP STA437 X=62 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO CUSP ANGLE AT STA 437, X=62, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500284 20010725 00284 WP 2001 7 25 RRXA11070 1 20010412 A 5710 5769600 RIB DOUG DC8 DC862F 3021972 WP XFS 653.75 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO L/H WING O/B L/E LOWER RIB AT STA. XFS653.75, DAMAGE EXCEEDED LIMITATIO N IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INST ALLED IAW DC-8 SRM 57-2-0 FIG#2. 2 L 7 4 4F 4A25 2001072500285 20010725 00285 WP 2001 7 25 RRXA11072 1 20010412 A 5730 5769545 SKIN DOUG DC8 DC862F 3021972 WP XFS 710 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H WING O/B L/E SKIN L/E I/B AT STA. XFS 710, DAMAGE EXCEEDED LIMITATI ON IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INS TALLED IAW DC-8 SRM 57-2-1 FIG#2H. 2 L 7 4 4F 4A25 2001072500286 20010725 00286 WP 2001 7 25 RRXA11073 1 20010412 A 5730 576960040 DOUBLER DOUG DC8 DC862F 3021972 WP XFS 572.5 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H L/E INTERNAL WRAP AROUND DOUBLER AT STA. XFS572.5, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART A ND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D AND DWG#5769600. 2 L 7 4 4F 4A25 2001072500287 20010725 00287 WP 2001 7 25 RRXA11078 1 20010419 A 5310 97563061 WEB DOUG DC8 DC862F 3021972 WP STA1310-1520 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO WEB AT STA. 1310-1520 AND RBL46, DAMAGE EXCEEDED LIMITATION IAW DC- 8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW D C-8 SRM 53-4-1 AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2001072500288 20010725 00288 WP 2001 7 25 RRXA11079 1 20010419 A 5310 3755822505N FITTING DOUG DC8 DC862F 3021972 WP A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING AT STA.540 BETWEEN L33L-L34L, DAMAGE EXCEEDED LIMIT ATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND IN STALLED IAW DC-8 SRM 53-2-0 FIG#20, 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2001072500289 20010725 00289 WP 2001 7 25 RRXA11080 1 20010419 A 5310 4641324N FITTING DOUG DC8 DC862F 3021972 WP STA1530 L32L CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LONGERON END FITTING AT STA 1530 AND L32L, DAMAGE EXCEEDED LIMITATION I AW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D. 2 L 7 4 4F 4A25 2001072500290 20010725 00290 WP 2001 7 25 RRXA11081 1 20010419 A 5230 5753157 SKIN DOUG DC8 DC862F 3021972 WP STA560 L26R-L31R NICKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND NICK DAMAGE TO FWD CARGO PIT CROOS SLIDE DOOR JAMB AFT CUT OUT EDGE OF EXT. AT STA 560 AND L26R-L31R. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. BLENDED AND FOUND TO BE WIT HIN LIMITS IAW DC-8 SRM 53-2-0 FIG.1F 2 L 7 4 4F 4A25 2001072500291 20010725 00291 WP 2001 7 25 RRXA11083 1 20010419 A 5310 5889588502 SEAT TRACK DOUG DC8 DC862F 3021972 WP STA1330 RBL26 WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK SCALLOPS AT STA. 1330 AND RBL26, DAMAGE EXCEEDED LIMITATION I AW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-7-3 FIG3D, 51-3-0, 53-21-03, 53-2-3FIG14A. 2 L 7 4 4F 4A25 2001072500292 20010725 00292 WP 2001 7 25 RRXA11085 1 20010420 A 5310 4641324N FITTING DOUG DC8 DC862F 3021972 WP STA1530-1540 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CRACKED DAMAGE TO END FITTING AT STA 1530-1540 AND L36, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IA W DC-8 SRM 51-1-20D AND DWG#4641324. 2 L 7 4 4F 4A25 2001072500293 20010725 00293 WP 2001 7 25 RRXA11086 1 20010420 A 5310 4641324N FITTING DOUG DC8 DC862F 3021972 WP STA1530-1540 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO END FITTING AT STA.1540 AND L34R, DAMAGE EXCEEDED LIMITATION IAW DC-8 S RM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND DWG#4641324. 2 L 7 4 4F 4A25 2001072500294 20010725 00294 WP 2001 7 25 RRXA11092 1 20010423 A 5310 3755827 FITTING DOUG DC8 DC862F 3021972 WP STA500 L33R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO B-PIT DOOR FRAME FWD BANANNA FITTING AT STA.500 AND L33R, DAMAGE EX CEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, DWG#3755827. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2001072500295 20010725 00295 WP 2001 7 25 RRXA11093 1 20010423 A 5310 52772660 SEAT TRACK DOUG DC8 DC862F 3021972 WP STA525 BL=0 WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA.525 AND BL=0, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-3 FIG8A, 51-3-0. 2 L 7 4 4F 4A25 2001072500296 20010725 00296 WP 2001 7 25 RRXA11094 1 20010423 A 5310 3755822 FITTING DOUG DC8 DC862F 3021972 WP STA940-960 L24R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUBE FITTING AT STA.940-960 AND L24R. /////CORRECTIVE ACTION// /// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. NO MATERIAL LOSS NOTED AFTER CLEAN UP, FOUND TO BE WITHIN LIMITS I AW DC-8 SRM 53-2-0 FIG#1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2001072500297 20010725 00297 WP 2001 7 25 RRXA11097 1 20010424 A 5750 5642970 SKIN DOUG DC8 DC862F 3021972 WP FLAP HINGE 219 GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO R/H OUTBOARD FLAP UPPER SKIN AT FLAP HINGE 219, DAMAGE EXCEEDED LIMITA TION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND I NSTALLED IAW DC-8 SRM 51-1-2B, 51-1-21. 2 L 7 4 4F 4A25 2001072500298 20010725 00298 WP 2001 7 25 RRXA11100 1 20010426 A 5310 5893553 SEAT TRACK DOUG DC8 DC862F 3021972 WP STA717-733 LBL60 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SEAT TRACK AT STA.717-733 AND LBL60, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED I AW DC-8 SRM 53-2-3 FIG#14 AND DWG#5893553. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2001072500299 20010725 00299 WP 2001 7 25 RRXA11101 1 20010427 A 5310 2772660 SEAT TRACK DOUG DC8 DC862F 3021972 WP STA1439-1442 WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA.1439-1442 AND LBL46, DAMAGE EXCEEDED LIMITATION IAW DC -8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0, 51-10-0, 53-7-2 FIG3D, 53-23-0 FIG14. 2 L 7 4 4F 4A25 2001072500300 20010725 00300 WP 2001 7 25 RRXA11105 1 20010427 A 5310 5891924 SEAT TRACK DOUG DC8 DC862F 3021972 WP STA1420-1540 BROKEN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND BROKEN DAMAGE TO SEAT TRACK AT STA.1420-1540 AND LBL26, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IA W DC-8 SRM 51-1-11, 51-3-0. 2 L 7 4 4F 4A25 2001072500301 20010725 00301 WP 2001 7 25 RRXA11106 1 20010427 A 5310 37558251 FITTING DOUG DC8 DC862F 3021972 WP STA500 L33R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUBE FITTING AT STA.500 AND L33R, DAMAGE EXCEEDED LIMITATION IA W DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0FIG2D, 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2001072500302 20010725 00302 WP 2001 7 25 RRXA11109 1 20010428 A 5346 97532571 SEAT TRACK DOUG DC8 DC862F 3021972 WP CO-PLT RT FWD WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT CO-PILOTS RT FWD, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SR M 51-3-0. 2 L 7 4 4F 4A25 2001072500303 20010725 00303 WP 2001 7 25 RRXA11111 1 20010428 A 5346 97532571 SEAT TRACK DOUG DC8 DC862F 3021972 WP CO-PILOT LH FWD WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT CO-PILOTS LEFT FWD TRACK, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IA W DC-8 SRM 51-3-0. 2 L 7 4 4F 4A25 2001072500304 20010725 00304 WP 2001 7 25 RRXA11112 1 20010428 A 5346 5888367 SEAT TRACK DOUG DC8 DC862F 3021972 WP PILOTS AFT RT WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT PILOTS AFT RT, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. / ////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0. 2 L 7 4 4F 4A25 2001072500305 20010725 00305 WP 2001 7 25 RRXA11113 1 20010428 A 5346 9753257517 SEAT TRACK DOUG DC8 DC862F 3021972 WP CO-PILOTS AFT RT WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO CO-PILOTS AFT RT SEAT TRACK, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. / ////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0. 2 L 7 4 4F 4A25 2001072500306 20010725 00306 WP 2001 7 25 RRXA11114 1 20010428 A 5100 5759335 SKIN DOUG DC8 DC862F 3021972 WP STA1240 L30R-L27 DENTED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND DENT DAMAGE TO SKIN AT STA.1240 BETWEEN L30R-L27R, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-1 FIG#7. 2 L 7 4 4F 4A25 2001072500307 20010725 00307 WP 2001 7 25 RRXA11115 1 20010428 A 5340 5755787 SEAT TRACK DOUG DC8 DC862F 3021972 WP STA1420 LBL26 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SEAT TRACK AROUND PLUG REPAIR AT STA.1420 AND LBL26, DAMAGE EXCEED ED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PAR T AND INSTALLED IAW DC-8 SRM 53-2-3 FIG#12, 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2001072500308 20010725 00308 WP 2001 7 25 RRXA11116 1 20010428 A 5310 3755826 FITTING DOUG DC8 DC862F 3021972 WP STA560 L31L-L32L CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING AT STA.560 BETWEEN L31L-L32L, DAMAGE EXCEEDED LIMI TATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND I NSTALLED IAW DC-8 SRM 53-2-0 FIG#2D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2001072500309 20010725 00309 WP 2001 7 25 RRXA11117 1 20010428 A 5310 37558241 FITTING DOUG DC8 DC862F 3021972 WP STA520 L33R-L34R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING AT STA.520 AND L33R-L34R, DAMAGE EXCEEDED LIMITATI ON IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTA LLED IAW DC-8 SRM 51-1-20D AND DWG#3755824. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2001072500310 20010725 00310 WP 2001 7 25 RRXA11118 1 20010430 A 5310 5644130 SPLICE DOUG DC8 DC862F 3021972 WP STA1557-1574 L36 MISSING A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND MISSING SPLICE FITTING AT STA.1557-1574 AND L36, DAMAGE EXCEEDED LIMITATION IAW DC-8 S RM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-2 FIG#10. 2 L 7 4 4F 4A25 2001072500311 20010725 00311 WP 2001 7 25 RRXA11119 1 20010430 A 5310 37558242 FITTING DOUG DC8 DC862F 3021972 WP STA500 L33R-L34R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING AT STA.500 AND L33R-L34R, DAMAGE EXCEEDED LIMITATI ON IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTA LLED IAW DC-8 51-1-20D, 53-2-0 FIG2D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2001072500312 20010725 00312 WP 2001 7 25 RRXA11120 1 20010422 A 5310 3755822505 FITTING DOUG DC8 DC862F 3021972 WP STA520 L33L-L34L CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENACE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING AT STA.520 AND L34L-L33L, DAMAGE EXCEEDED LIMITATIO N IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTAL LED IAW DC-8 SRM 53-2-0 FIG2D AND DWG#3755822. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2001072500313 20010725 00313 WP 2001 7 25 RRXA11121 1 20010422 A 5310 3755827505 FITTING DOUG DC8 DC862F 3021972 WP STA520 L29L-L30L CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE BATHTUB FITTING AT STA. 520 AND L30L-L29L, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALL ED IAW DC-8 SRM 53-2-0 FIG2D AND DWG#3755827. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2001072500314 20010725 00314 WP 2001 7 25 RRXA11122 1 20010422 A 5310 37558261N FITTING DOUG DC8 DC862F 3021972 WP STA520 L31L-L32L CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING AT STA.520 AND L31L-L32L, DAMAGE EXCEEDED LIMITATI ON IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTA LLED IAW DC-8 SRM 53-2-0 FIG2D AND DWG#3755826. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2001072500315 20010725 00315 WP 2001 7 25 RRXA11124 1 20010430 A 5310 5891924 SEAT TRACK DOUG DC8 DC862F 3021972 WP STA699-715 WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA.699-715 AND RBL46, DAMAGE EXCEEDED LIMITATION IAW DC- 8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW D C-8 SRM 51-3-0, 53-2-3. 2 L 7 4 4F 4A25 2001072500316 20010725 00316 WP 2001 7 25 RRXA11125 1 20010430 A 5310 5891924 SEAT TRACK DOUG DC8 DC862F 3021972 WP STA825-990 RBL46 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SEAT TRACK AT STA.825-990 AND RBL46, DAMAGE EXCEEDED LIMITATION IA W DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0, 53-21-03, 53-2-3 FIG14. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2001072500317 20010725 00317 WP 2001 7 25 RRXA11128 1 20010426 A 5310 37540252 FITTING DOUG DC8 DC862F 3021972 WP STA560 L27R CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO B-PIT DOOR FRAME VERTICAL SUPPORT FITTING AT STA.60 AND L27R, DAMAGE E XCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATE D PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND DWG#3754025. 2 L 7 4 4F 4A25 2001072500318 20010725 00318 WP 2001 7 25 RRXA11130 1 20010427 A 5310 5888367 SEAT TRACK DOUG DC8 DC862F 3021972 WP FE'S FWD TRACK WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO FE'S FWD SEAT TRACK, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORR ECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0 A ND DWG#5888367. 2 L 7 4 4F 4A25 2001072500319 20010725 00319 WP 2001 7 25 RRXA11132 1 20010427 A 5210 5615403 BEAM DOUG DC8 DC862F 3021972 WP FWD ENTRY DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FWD ENTRY DOOR INNER SKIN LOWER FLANGE, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 52-2-0 FIG2. 2 L 7 4 4F 4A25 2001072500320 20010725 00320 WP 2001 7 25 RRXA11133 1 20010503 A 5310 5891924 SEAT TRACK DOUG DC8 DC862F 3021972 WP STA910-1050 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SEAT TRACK AT STA.910-1050 AND LBL50, DAMAGE EXCEEDED LIMITATION I AW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3 FIG14. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2001072500321 20010725 00321 WP 2001 7 25 RRXA11134 1 20010503 A 5310 5891924 SEAT TRACK DOUG DC8 DC862F 3021972 WP STA870-915 LBL46 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO SEAT TRACK AT STA.870-915 AND LBL46, DAMAGE EXCEEDED LIMITATION IAW DC -8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3 FIG14. 2 L 7 4 4F 4A25 2001072500322 20010725 00322 WP 2001 7 25 RRXA11135 1 20010503 A 5310 975491313 LONGERON DOUG DC8 DC862F 3021972 WP STA500-560 L29L CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO O/B FLANGE AT STA.500-560 AND L29L, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-2 FIG10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2001072500323 20010725 00323 WP 2001 7 25 RRXA11137 1 20010504 A 5230 5649820 FRAME DOUG DC8 DC862F 3021972 WP D-PIT DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO D-PIT DOOR LOWER FRAME, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. ///// CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1 -21 AND DWG#5649820. 2 L 7 4 4F 4A25 2001072500324 20010725 00324 WP 2001 7 25 RRXA11138 1 20010504 A 5750 3652304 FITTING DOUG DC8 DC862F 3021972 WP LT WING EXH GATE WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO L/H WING EXHAUST GATE OUTBOARD FITTING, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IA W DC-8 SRM 51-1-21, 51-1-20D. 2 L 7 4 4F 4A25 2001072500325 20010725 00325 WP 2001 7 25 RRXA11139 1 20010504 A 5310 26499441N FITTING DOUG DC8 DC862F 3021972 WP STA390 L21R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FWD SERVICE DOOR AFT FRAME LWR FITTING AT STA.390 AND L21R, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICA TED PART AND INSTALLED IAW DC-8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2001072500326 20010725 00326 WP 2001 7 25 RRXA11141 1 20010425 A 5230 564535717 PAN DOUG DC8 DC862F 3021972 WP STA.1120 L32R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO C-PIT DOOR PAN (FRAME) TO LWR FWD CORNER AT STA.1120 AND L32R, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICAT ED REPAIR AND INSTALLED IAW DC-8 SRM 52-4-2 FIG3. 2 L 7 4 4F 4A25 2001072500327 20010725 00327 WP 2001 7 25 RRXA11142 1 20010505 A 5310 5891924 SEAT TRACK DOUG DC8 DC862F 3021972 WP STA1330 RBL26-46 WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA.1330 AND LBL26-LBL46, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IA W DC-8 SRM 53-7-2 FIG3D, 51-3-0, 53-2-3 FIG8A. 2 L 7 4 4F 4A25 2001072500328 20010725 00328 WP 2001 7 25 RRXA11143 1 20010505 A 5310 5755787 SEAT TRACK DOUG DC8 DC862F 3021972 WP STA1420-1470 BROKEN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND BROKEN DAMAGE TO SEAT TRACK AT STA.1420-1470 AND RBL46, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED I AW DC-8 SRM 53-7-2 FIG3D, 51-3-0, 51-1-20D, 53-2-3 FIG14A. 2 L 7 4 4F 4A25 2001072500329 20010725 00329 WP 2001 7 25 RRXA11145 1 20010403 A 5310 975580711 FRAME DOUG DC8 DC862F 3021972 WP STA1180L20L-L21L BENT A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND BENT DAMAGE TO FRAME AT STA1180 AND L20L-L21L, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM . /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DHSK 996-505. 2 L 7 4 4F 4A25 2001072500330 20010725 00330 WP 2001 7 25 RRXA11146 1 20010427 A 2780 576989110 BRACKET DOUG DC8 DC862F 3021972 WP XOLD6225 RT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H WING O/B L/E SLOT VANE, INBOARD ATTACH BRACKET AT STA. XOLD6225, D AMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FA BRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21 AND DWG#5769891. 2 L 7 4 4F 4A25 2001072500331 20010725 00331 WP 2001 7 25 RRXA11149 1 20010505 A 5310 3755822506N FITTING DOUG DC8 DC862F 3021972 WP STA500 L29L-L30L CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING AT STA500 AND L29L-L30L, DAMAGE EXCEEDED LIMITATIO N IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTAL LED IAW DC-8 SRM 53-2-0 FIG2D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2001072500332 20010725 00332 WP 2001 7 25 RRXA11150 1 20010509 A 5300 5615615 SUPPORT DOUG DC8 DC862F 3021972 WP STA208 LBL44 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H UPPER SUPPORT INSIDE THE R/H REFRIGERANT CONDENSOR DOOR AREA AT STA 208 AND LBL44, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC -8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-0 FIG1B. 2 L 7 4 4F 4A25 2001072500333 20010725 00333 WP 2001 7 25 RRXA11153 1 20010509 A 5310 58883671 SEAT TRACK DOUG DC8 DC862F 3021972 WP FE AFT SEATTRACK WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO F/E AFT SEAT TRACK, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRE CTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0 AN D DWG#5888367. 2 L 7 4 4F 4A25 2001072500334 20010725 00334 WP 2001 7 25 RRXA11154 1 20010509 A 5730 5769933 SKIN DOUG DC8 DC862F 3021972 WP RH OB SLOT VANE WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO R/H O/B SLOT VANE O/B END HAS SCREWS PULLING THRU SKIN, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAI R AND INSTALLED IAW DC-8 SRM 51-3-0, 51-1-21, 57-2-0 FIG2&3. 2 L 7 4 4F 4A25 2001072500335 20010725 00335 WP 2001 7 25 RRXA11155 1 20010510 A 5310 975491351 LONGERON DOUG DC8 DC862F 3021972 WP STA510-610 L28L CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FWD CARGO PIT L28L AT STA.510-560, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IA W DC-8 SRM 53-2-2 FIG10, DWG#9754913. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2001072500336 20010725 00336 WP 2001 7 25 RRXA11156 1 20010513 A 5310 3755822512N FITTING DOUG DC8 DC862F 3021972 WP STA520-560 L35L CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING AT STA.520-560 AND L35L, DAMAGE EXCEEDED LIMITATIO N IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTAL LED IAW DC-8 SRM 53-2-2 FIG10, 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2001072500337 20010725 00337 WP 2001 7 25 RRXA11157 1 20010513 A 5310 3755822503N FITTING DOUG DC8 DC862F 3021972 WP STA560 L34L-L35L CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING AT STA.560 AND L34L-L35L, DAMAGE EXCEEDED LIMITATI ON IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTA LLED IAW DC-8 SRM 53-2-0 FIG2D AND DWG#3755822-503N. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2001072500338 20010725 00338 WP 2001 7 25 RRXA11158 1 20010501 A 5310 9754913501 LONGERON DOUG DC8 DC862F 3021972 WP STA460-560 L36 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON AT STA.460-560 AND L36, DAMAGE EXCEEDED LIMITATION IAW DC -8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-2 FIG4C. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2001072500339 20010725 00339 NM 2001 7 25 ASAA0140089 1 20010616 A 3350 8100022601 LIGHT BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 773AS 25106 ANC - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE AT ROW 10. RECONNECTED EMERGENCY FLOOR TRACK LIGHTING WIRE. OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001072500340 20010725 00340 NM 2001 7 25 ASAA0170005 1 20010522 A 3350 8100022607 LIGHT BOEING 737 737790 13844CN NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 619AS 30164 SEA - DURING LINE MAINTENANCE, THE EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT THE FIRST CLASS DIVIDER. REPL ACED LIGHT ASSEMBLY AT THE CLASS DIVIDER. THE LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 2002010400131 20020104 00131 2002 1 4 ASAA0180107 4 20010326 A 2565 D29982107 HARNESS DOUG MD80 MD83 3023681 NM L1 DOOR FAILED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 15923 918 53471 OAK - DURING C-CHECK, L1 DOOR EMERGENCY SLIDE HARNESS FAILED THE AMPERAGE CHECK. REPLACED L1 DOOR SLIDE. (M) 2 L 7 2 4F RT 2001072500341 20010725 00341 WP 2001 7 25 RRXA11127 1 20010430 A 5310 S4889185 SEAT TRACK DOUG DC8 DC862F 3021972 WP STA345-350 LBL25 WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA.345-350 AND LBL25, DAMAGE EXCEEDED LIMITATION IAW DC- 8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW D C-8 SRM 53-2-3 FIG14. 2 L 7 4 4F 4A25 2001072500342 20010725 00342 NM 2001 7 25 0102535519 1 20010713 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 519US 23207 IN L CHECK, FOUND CRACKED FLOORBEAM. REPAIRED PER EA55-184810. 2 L 7 2 4F RT A2NM 2001072500343 20010725 00343 EU 2001 7 25 0102543210 1 20010719 A 5311 FRAME AIRBUS 320 A320211 3930320 EU CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 310NW 121 In M check, found corrosion in nutplate hole on FR 68 R/H, 1 inch from inboard flange and 1 inch above door threshold. R epaired per EA32-184166. 2 L 7 2 4F RT A28NM 2001072500344 20010725 00344 WP 2001 7 25 ASAA0180165 1 20010512 A 4910 5916083527 INTAKE DUCT DOUG DC9 DC983 3022083 WP APU CONTAMINATED A ASAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 01 950AS 26832 139 53023 SJD - ACRID HYDRAULIC ODOR IN CABIN DURING FLIGHT 214 DUE APU INLET SKYDROL CONTAMINATION. WASHED APU INLET, REPLACED C OALESCER BAG IAW MM 21-20-02, AND PERFORMED AIR QUALITY CHECK PER TASK CARD 28525011. OPERATED NORMALLY WITH NO ACRID O DOR IN CABIN. (M) 2 L 7 2 4F RT A6WE 2001072500345 20010725 00345 WP 2001 7 25 ASAA0180166 1 20010512 A 2560 3952273 LATCH DOUG DC9 DC983 3022083 WP CABIN BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 947AS 53020 PDX - DURING PRE-FLIGHT CHECK, FOUND ONE OF THE TWO L2 GIRT BAR LATCHES ON THE FLOOR BROKEN. REPLACED BROKEN LATCH. GI RT BAR INSERTION COULD THEN BE DONE PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001072500346 20010725 00346 WP 2001 7 25 RRXA11159 1 20010518 A 5330 5779936 SKIN DOUG DC8 DC862F 3021972 WP STA1220 L25R GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO EXTERIOR SKIN AT STA.1220 AND L25R, DAMAGE EXCEEDED LIMITATION IAW DC -8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IA W DC-8 SRM 53-2-1 FIG7. 2 L 7 4 4F 4A25 2001072500347 20010725 00347 WP 2001 7 25 RRXA11160 1 20010417 A 5310 37558262N FITTING DOUG DC8 DC862F 3021972 WP STA560 L33R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING SPLICE ANGLE AT STA.560 AND L33R, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART A ND INSTALLED IAW DC-8 SRM51-1-20D, 53-2-0 FIG20. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2001072500348 20010725 00348 WP 2001 7 25 RRXA11161 1 20010418 A 5310 37558262N FITTING DOUG DC8 DC862F 3021972 WP STA500 L32L CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING AT STA.500 AND L32L, DAMAGE EXCEEDED LIMITATION IA W DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0 FIG2D, 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2001072500349 20010725 00349 WP 2001 7 25 RRXA11163 1 20010403 A 5310 5644981 SKIN DOUG DC8 DC862F 3021972 WP STA212 L15L CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SKIN AT STA.212 AND L15L, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DHSK 99 6-492. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2001072500350 20010725 00350 WP 2001 7 25 RRXA11164 1 20010524 A 2710 5705334 AILERON DOUG DC8 DC873F 302199F WP L/H I/B AILERON CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO L/H INBOARD AILERON T/E WEDGE BETWEEN TRIM AND CONTROL TAB, DAMAGE EXCE EDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 57-8-1, 51-1-4, 51-1-11. 2 L 7 4 4F RT 4A25 2001072500351 20010725 00351 WP 2001 7 25 RRXA11165 1 20010526 A 5753 5642960 ANGLE DOUG DC8 DC873F 302199F WP RH I/B FLAP CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H INBOARD FLAP O/B END Z ANGLE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC- 8 SRM 51-1-21, 57-7-1. 2 L 7 4 4F RT 4A25 2001072500352 20010725 00352 WP 2001 7 25 RRXA11168 1 20010527 A 5310 56119861 ANGLE DOUG DC8 DC873F 302199F WP STA1300 L33R CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FLOOR SUPPORT ANGLE AT STA.1300 AND L33R, DAMAGE EXCEEDED LIMITATIONS I AW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALL ED IAW DHSK 606-749. 2 L 7 4 4F RT 4A25 2001072500353 20010725 00353 WP 2001 7 25 RRXA11169 1 20010527 A 5310 56119861 ANGLE DOUG DC8 DC873F 302199F WP STA.1280 L31L CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FLOOR SUPPORT ANGLE AT STA.1280 AND L31L, DAMAGE EXCEEDED LIMITATIONS I AW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALL ED IAW DHSK606-749. 2 L 7 4 4F RT 4A25 2001072500354 20010725 00354 WP 2001 7 25 RRXA11170 1 20010528 A 5330 9754058 SKIN DOUG DC8 DC873F 302199F WP A-PIT DOOR RAMP CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO A-PIT DOOR RAMP SKIN, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /// //CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51 -1-21D AND DWG#9754058. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500355 20010725 00355 WP 2001 7 25 RRXA11171 1 20010528 A 5330 9754058 ANGLE DOUG DC8 DC873F 302199F WP A-PIT DOOR RAMP CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO A-PIT DOOR RAMP I/B SUPPORT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND DWG#9754058. 2 L 7 4 4F RT 4A25 2001072500356 20010725 00356 WP 2001 7 25 RRXA11172 1 20010528 A 5330 9754058 CHANNEL DOUG DC8 DC873F 302199F WP A-PIT DOOR XSLID CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO A-PIT CROSS SLIDE DOOR RAMP AT HOLD OPEN STRUT ATTACH ANGLE, DAMAGE EXC EEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND DWG#9754058. 2 L 7 4 4F RT 4A25 2001072500357 20010725 00357 WP 2001 7 25 RRXA11173 1 20010528 A 5330 9754058 INTERCOSTAL DOUG DC8 DC873F 302199F WP A-PIT DOOR RAMP CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO A-PIT DOOR RAMP FORWARD INTERCOSTAL SUPPORT, DAMAGE EXCEEDED LIMITATION S IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTAL LED IAW DC-8 SRM 51-1-20D AND DWG#9754058. 2 L 7 4 4F RT 4A25 2001072500358 20010725 00358 WP 2001 7 25 RRXA11174 1 20010528 A 5330 5779936 SKIN DOUG DC8 DC873F 302199F WP STA1390 L33R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LOWER R/H FUSELAGE SKIN AT STA.1390 AND L33R, DAMAGE EXCEEDED LIMIT ATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-1 FIG.7. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500359 20010725 00359 WP 2001 7 25 RRXA11175 1 20010525 A 5730 5643409137 CLIP DOUG DC8 DC873F 302199F WP LT WING #4 SPOIL GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO L/H WING #4 SPOILER O/B HINGE FITTING CLIP, DAMAGE EXCEEDED LIMITATION S IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTAL LED IAW DC-8 SRM 57-1-0, 51-1-21. 2 L 7 4 4F RT 4A25 2001072500360 20010725 00360 WP 2001 7 25 RRXA11176 1 20010528 A 5730 5655752 SKIN DOUG DC8 DC873F 302199F WP STA.340 DENTED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND DENT DAMAGE TO L/H O/B LOWER T/E WEDGE LOWER SURFACE AT STA. 340, DAMAGE EXCEEDED LIMIT ATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND I NSTALLED IAW DC-8 SRM 57-7-1 FIG.4, 51-1-21A. 2 L 7 4 4F RT 4A25 2001072500361 20010725 00361 WP 2001 7 25 RRXA11177 1 20010528 A 5200 5615403 WEB DOUG DC8 DC873F 302199F WP FWD ENTRY DOOR DENTED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND DENT DAMAGE TO AFT LOWER CORNER WEB AT FORWARD ENTRY DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTAL LED IAW DC-8 SRM 51-1-21 AND DWG#5615403. 2 L 7 4 4F RT 4A25 2001072500362 20010725 00362 WP 2001 7 25 RRXA11178 1 20010528 A 5710 576946644 RIB DOUG DC8 DC873F 302199F WP STA.XFS691.25 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO L/H WING L/E UPPER RIB AT STA.XFS691.25, DAMAGE EXCEEDED LIMITATIONS IA W DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLE D IAW DC-8 SRM 57-2-0 FIG.2. 2 L 7 4 4F RT 4A25 2001072500363 20010725 00363 WP 2001 7 25 RRXA11180 1 20010528 A 5710 5769468616 RIB DOUG DC8 DC873F 302199F WP XFS 610-566.25 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H WING O/B L/E UPPER RIB AT STA.XFS610-566.25, DAMAGE EXCEEDED LIMITA TIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. HFCC INSPECTION IAW SP M 06-10-01.001. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0 FIG.2, 51-1-20D. 2 L 7 4 4F RT 4A25 2001072500364 20010725 00364 WP 2001 7 25 RRXA11181 1 20010528 A 5310 56119861 ANGLE DOUG DC8 DC873F 302199F WP STA1260 L33R CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FLOOR SUPPORT ANGLE AT STA.1260 AND L33R, DAMAGE EXCEEDED LIMITATIONS I AW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001072500365 20010725 00365 WP 2001 7 25 RRXA11182 1 20010528 A 5730 56430001 SKIN DOUG DC8 DC873F 302199F WP LT WING TOP T/E TORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND TORN SKIN DAMAGE TO L/H WING UPPER T/E SKIN AT #1 SPOILER O/B HINGE, DAMAGE EXCEEDED LI MITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0 FIG.2A, 51-1-21, 51-1-21A, 51-3-0. 2 L 7 4 4F RT 4A25 2001072500366 20010725 00366 WP 2001 7 25 RRXA11183 1 20010528 A 5752 56429601 SKIN DOUG DC8 DC873F 302199F WP R/H I/B FLAP CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H I/B FLAP I/B L/E IN TWO AREAS, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC -8 SRM 51-1-21, 57-7-1 FIG.2. 2 L 7 4 4F RT 4A25 2001072500367 20010725 00367 WP 2001 7 25 RRXA11185 1 20010528 A 5310 5779935 FRAME DOUG DC8 DC873F 302199F WP STA460 L27R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA.460 AND L27R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM . /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW DC-8 SRM 51-1-8, 53-2-0 FIG.1F. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500368 20010725 00368 WP 2001 7 25 RRXA11186 1 20010528 A 5710 57694663436 RIB DOUG DC8 DC873F 302199F WP XFS672.5-678.5 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H WING O/B L/E RIBS AT STA. XFS672.5-678.5, DAMAGE EXCEEDED LIMITATIO NS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. NDT HFCC INSP IAW SPM06-1 0-01.001. FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-2-0 FIG.2, 51-1-20D. 2 L 7 4 4F RT 4A25 2001072500369 20010725 00369 WP 2001 7 25 RRXA11190 1 20010529 A 5310 37502571 SPLICE DOUG DC8 DC873F 302199F WP STA.610 L31L CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO SPLICE AT STA.610 AND L31L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. / ////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-1-01 AND DWG#3750257. 2 L 7 4 4F RT 4A25 2001072500370 20010725 00370 WP 2001 7 25 RRXA11191 1 20010529 A 5710 5769600 RIB DOUG DC8 DC873F 302199F WP XFS616.25-622.5 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H WING O/B L/E UPPER RIB AT STA.XFS616.25-622.5, DAMAGE EXCEEDED LIMI TATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-2-0 FIG.2. 2 L 7 4 4F RT 4A25 2001072500371 20010725 00371 WP 2001 7 25 RRXA11192 1 20010529 A 5710 5769600 RIB DOUG DC8 DC873F 302199F WP XFS 653.75 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H WING L/E LOWER RIB AT STA. XFS653.75, DAMAGE EXCEEDED LIMITATIONS I AW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2001072500372 20010725 00372 WP 2001 7 25 RRXA11193 1 20010529 A 5710 576958947 DOUBLER DOUG DC8 DC873F 302199F WP XFS 337 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H WING CENTER L/E INTERNAL DOUBLER LOCATED AT DRAIN HOLE AT STA. XFS3 37, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1 -8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-120D, 51-1-21, 51-3-0 AND DHSK606-143. 2 L 7 4 4F RT 4A25 2001072500373 20010725 00373 WP 2001 7 25 RRXA11197 1 20010530 A 5750 5655752 SKIN DOUG DC8 DC873F 302199F WP STA. XRS340 GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO L/H O/B FLAP BELOW FLAP HINGE AT STA. XRS340, DAMAGE EXCEEDED LIMITATI ONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND IN STALLED IAW DC-8 SRM 57-2-1 FIG.2. 2 L 7 4 4F RT 4A25 2001072500374 20010725 00374 WP 2001 7 25 RRXA11199 1 20010530 A 7800 3057283080 SKIN DOUG DC8 DC873F 302199F WP #1 ENG T/R COWL PUNCTURED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND PUNCTURE DAMAGE TO #1 ENGINE I/B T/R COWL INNER HEAT SHIELD, DAMAGE EXCEEDED LIMITATION S IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTAL LED IAW DC-8 SRM 51-1-20D AND DC-8 MM 78-31-10. 2 L 7 4 4F RT 4A25 2001072500375 20010725 00375 WP 2001 7 25 RRXA11202 1 20010530 A 5710 5769545 RIB DOUG DC8 DC873F 302199F WP XFS 778.25 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H WING O/B L/E RIB AT STA. XFS778.25, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED I AW DC-8 SRM 57-2-0 FIG.2. 2 L 7 4 4F RT 4A25 2001072500376 20010725 00376 WP 2001 7 25 RRXA11203 1 20010530 A 5710 5769545 RIB DOUG DC8 DC873F 302199F WP XFS 785 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H WING L/E RIB AT STA. XFS785, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-2-0 FIG.2, 51-1-21. 2 L 7 4 4F RT 4A25 2001072500377 20010725 00377 WP 2001 7 25 RRXA11206 1 20010531 A 5320 5751516 INTERCOSTAL DOUG DC8 DC873F 302199F WP STA1520-1540 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO D-PIT INTERCOSTAL AT STA.1520-1540 AND L33L AND UNDER CARGO TRACK, DAMA GE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABR ICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-3-0, 51-1-20D, 51-1-21A AND DWG#5751516. 2 L 7 4 4F RT 4A25 2001072500378 20010725 00378 WP 2001 7 25 RRXA11207 1 20010601 A 5310 3751193503 FITTING DOUG DC8 DC873F 302199F WP STA1660 L21R CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO AFT ACCY. COMPARTMENT FLOOR BEAM FITTING AT STA1660 AND L21R, DAMAGE EX CEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D, 51-3-0. 2 L 7 4 4F RT 4A25 2001072500379 20010725 00379 WP 2001 7 25 RRXA11208 1 20010601 A 5310 37505751A LONGERON DOUG DC8 DC873F 302199F WP STA.660 L31L CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 31L AT STA.660, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500380 20010725 00380 WP 2001 7 25 RRXA11209 1 20010601 A 5310 2537715 FRAME DOUG DC8 DC873F 302199F WP STA1120 L31R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER LIP OF FRAME AT STA.1120 AND L31R, DAMAGE EXCEEDED LIMITATION S IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INST ALLED IAW DC-8 SRM 53-2-0 FIG.7 AND DWG#2537715. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500381 20010725 00381 WP 2001 7 25 RRXA11210 1 20010601 A 5300 3710351 ANGLE DOUG DC8 DC873F 302199F WP STA. 910 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO L/H AFT WING TO BODY FAIRING SUPPORT BRACKETT, LOWER FORWARD ANGLE AT S TA.910, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0, 51-1-11 AND DWG#3710351. 2 L 7 4 4F RT 4A25 2001072500382 20010725 00382 WP 2001 7 25 RRXA11212 1 20010602 A 5300 42543610 FITTING DOUG DC8 DC873F 302199F WP STA.1140 L33R CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TOINTERCOSTAL ATTACH FITTING AT STA.1140 AND L33R, DAMAGE EXCEEDED LIMITAT IONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INS TALLED IAW DC-8 SRM 51-20-20D AND DWG#4758514-517. 2 L 7 4 4F RT 4A25 2001072500383 20010725 00383 WP 2001 7 25 RRXA11213 1 20010602 A 5300 37584982N FITTING DOUG DC8 DC873F 302199F WP STA.1240 L35R CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO INTERCOSTAL ATTACH FITTING AT STA.1240 AND L35R, DAMAGE EXCEEDED LIMITA TIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND IN STALLED IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001072500384 20010725 00384 WP 2001 7 25 RRXA11214 1 20010602 A 5310 3754914501 FITTING DOUG DC8 DC873F 302199F WP STA270 L30R-L31R CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO A-PIT FRAME FITTING AT STA.270 AND L30R-L31R, DAMAGE EXCEEDED LIMITATIO NS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTA LLED IAW DC-8 SRM 51-1-20D, 51-1-3. 2 L 7 4 4F RT 4A25 2001072500385 20010725 00385 WP 2001 7 25 RRXA11216 1 20010604 A 5310 606453 ANGLE DOUG DC8 DC873F 302199F WP STA1640 LBL32 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO AFT ACCY COMPARTMENT FLOOR BEAM AT STA.1640 AND LBL32, DAMAGE EXCEE DED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED P ART AND INSTALLED IAW DC-8 SRM 51-1-11, 51-1-20D AND DHSK606-453. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500386 20010725 00386 WP 2001 7 25 RRXA11217 1 20010604 A 5346 S2772660 SEAT TRACK DOUG DC8 DC873F 302199F WP STA338 LBL45 WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO MAIN CABIN SEAT TRACK SCALLOPS AT STA.338 AND LBL45, DAMAGE EXCEEDED LIM ITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0, 53-2-0 FIG.8A, 51-1-20D. 2 L 7 4 4F RT 4A25 2001072500387 20010725 00387 WP 2001 7 25 RRXA11218 1 20010604 A 5300 575077615 DOUBLER DOUG DC8 DC873F 302199F WP R/H SERV. DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO UPPER FWD CORNER OF FWD R/H SERVICE DOOR, DAMAGE EXCEEDED LIMITATIONS I AW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-3-0, 51-1-21A, 53-2-0 FIG.14. 2 L 7 4 4F RT 4A25 2001072500388 20010725 00388 WP 2001 7 25 RRXA11219 1 20010604 A 5300 575077617 ANGLE DOUG DC8 DC873F 302199F WP RH SERVICE DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H FWD UPPER CORNER OF FWD R/H SERVICE DOOR, DAMAGE EXCEEDED LIMITATIO NS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTA LLED IAW DC-8 SRM 51-1-21, 51-3-0, 51-1-21A, 53-2-0 FIG14. 2 L 7 4 4F RT 4A25 2001072500389 20010725 00389 WP 2001 7 25 RRXA11220 1 20010604 A 5310 4758514509N FITTING DOUG DC8 DC873F 302199F WP STA1240 L33R CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO INTERCOSTAL FRAME ATTACH FITTING AT STA.1240 AND L33R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-11, 51-1-20D. 2 L 7 4 4F RT 4A25 2001072500390 20010725 00390 WP 2001 7 25 RRXA11222 1 20010604 A 5300 589141495 DOUBLER DOUG DC8 DC873F 302199F WP STA70 LBL24 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TOGALLEY BASE AT STA.70 AND LBL24, DAMAGE EXCEEDED LIMITATIONS IAW DC- 8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW D C-8 SRM 51-1-21 AND DWG#5841414-95. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500391 20010725 00391 WP 2001 7 25 RRXA11223 1 20010605 A 5300 3750330505 SPLICE DOUG DC8 DC873F 302199F WP STA450 L33L CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO B-PIT FITTING SPLICE AT STA.450 AND L33L, DAMAGE EXCEEDED LIMITATIONS I AW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM51-1-21. 2 L 7 4 4F RT 4A25 2001072500392 20010725 00392 WP 2001 7 25 RRXA11224 1 20010605 A 5300 3750330505 FITTING DOUG DC8 DC873F 302199F WP STA. 1180 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO MAIN CABIN R/H CUSP FITTING AT STA.1180, DAMAGE EXCEEDED LIMITATIONS IA W DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001072500393 20010725 00393 WP 2001 7 25 RRXA11225 1 20010605 A 5300 575083729 INTERCOSTAL DOUG DC8 DC873F 302199F WP STA620 L33L CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO B-PIT INTERCOSTAL AT STA.620 AND L33L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IA W DC-8 SRM 51-1-21, 51-1-20D, 53-1-0, DWG#570837. 2 L 7 4 4F RT 4A25 2001072500394 20010725 00394 WP 2001 7 25 RRXA11227 1 20010605 A 5300 47799401 GUSSET DOUG DC8 DC873F 302199F WP STA440-460 L30R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO GUSSET AT STA.440-460 AND L30R-L31R, DAMAGE EXCEEDED LIMITATIONS IA W DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND DWG#4779940. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500395 20010725 00395 WP 2001 7 25 RRXA11228 1 20010605 A 5300 4646163501N FITTING DOUG DC8 DC873F 302199F WP STA447-453 L30R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SPLICE FITTING AT STA. 447-453 AND L30R, DAMAGE EXCEEDED LIMITATION S IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTAL LED IAW DC-8 SRM 51-1-20D AND DWG#4646163. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500396 20010725 00396 WP 2001 7 25 RRXA11230 1 20010605 A 5310 NPN DOUBLER DOUG DC8 DC873F 302199F WP STA1560 LBL50 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR BEAM AT STA.1560 AND LBL50, DAMAGE EXCEEDED LIMITATIONS IAW D C-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM51-1-20D AND DWG#606-316. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500397 20010725 00397 WP 2001 7 25 RRXA11232 1 20010606 A 5346 27772650 SEAT TRACK DOUG DC8 DC873F 302199F WP STA160 LBL25 WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA.160 AND LBL25, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SR M. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3, 51-3-0. 2 L 7 4 4F RT 4A25 2001072500398 20010725 00398 WP 2001 7 25 RRXA11233 1 20010606 A 5100 3755251 FITTING DOUG DC8 DC873F 302199F WP STA270 L32R-L33R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO A-PIT FWD TORQUE BOX BATHTUB FITTING AT STA.270 AND L32R-L33R, DAMA GE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABR ICATED PART AND INSTALLED IAW DC-8 SRM 51-1-11, 51-1-20D, 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500399 20010725 00399 WP 2001 7 25 RRXA11234 1 20010607 A 5300 3614944505 FRAME DOUG DC8 DC873F 302199F WP STA1060L31R-L34R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME UPPER FRAME AT STA1060 AND L31R-L34R, DAMAGE EXCEEDED LIMITAT IONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INS TALLED IAW DC-8 SRM 51-1-20D, 51-1-21, 53-2-0 FIG.2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500400 20010725 00400 WP 2001 7 25 RRXA11235 1 20010607 A 5100 37558241 FITTING DOUG DC8 DC873F 302199F WP STA320 L33R-L34R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO A-PIT CROSS SLIDE TORQUE BOX BATHTUB FITTING AT STA.320 AND L33R-L3 4R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1 -8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-11, 51-1-20D, 53-2-0 FIG.1F. (CORROSION DAMAGE RECORDED IN EWA CORRO SION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500401 20010725 00401 WP 2001 7 25 RRXA11238 1 20010607 A 5710 5640236 BRACKET DOUG DC8 DC873F 302199F WP RH WING FIRE BOT CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H WING I/B AND O/B FIRE BOTTLE BRACKET, DAMAGE EXCEEDED LIMITATIONS I AW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-11 AND DC-8 MM 26-20-1 AND DWG#5640236. 2 L 7 4 4F RT 4A25 2001072500402 20010725 00402 WP 2001 7 25 RRXA11240 1 20010608 A 5250 4718340504 FITTING DOUG DC8 DC873F 302199F WP STA1180 L33R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO D-PIT DOOR JAMB TORQUE BOX FITTING AT STA.1180 AND L33R, DAMAGE EXC EEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DHSK606-072. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500403 20010725 00403 WP 2001 7 25 RRXA11241 1 20010608 A 5100 S2641520 ANGLE DOUG DC8 DC873F 302199F WP STA400 L33R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO B-PIT FRAME AT STA.400 AND L33R, DAMAGE EXCEEDED LIMITATIONS IAW DC -8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 53-2-0 FIG.2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500404 20010725 00404 WP 2001 7 25 RRXA11242 1 20010608 A 5730 2647420 FITTING DOUG DC8 DC873F 302199F WP STA980 BL60 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RT WW FITTING AT STA.980 AND BL60, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IA W DC-8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500405 20010725 00405 WP 2001 7 25 RRXA11243 1 20010608 A 5346 82772660 SEAT TRACK DOUG DC8 DC873F 302199F WP STA300 LBL60 WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK SCALLOPS AT STA.300 AND LBL60, DAMAGE EXCEEDED LIMITATIONS IA W DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-3-0, 53-2-3 FIG.8. 2 L 7 4 4F RT 4A25 2001072500406 20010725 00406 WP 2001 7 25 RRXA11244 1 20010608 A 5346 S2772660 SEAT TRACK DOUG DC8 DC873F 302199F WP STA952 LBL25 WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK SCALLOPS AT STA.952 AND LBL25, DAMAGE EXCEEDED LIMITATIONS IA W DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM51-1-20D, 51-3-0, 53-2-3 FIG.8. 2 L 7 4 4F RT 4A25 2001072500407 20010725 00407 WP 2001 7 25 RRXA11245 1 20010609 A 5710 5643117 PANEL DOUG DC8 DC873F 302199F WP STA. XW3 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO RT WING LOWER T/E PANEL I/B OF #1 SPOILER AT STA.XW3, DAMAGE EXCEEDED L IMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART A ND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 2001072500408 20010725 00408 WP 2001 7 25 RRXA11248 1 20010610 A 5310 5642015 FRAME DOUG DC8 DC873F 302199F WP STA1395 L28R CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FRAME AT STA.1395 AND L28R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. / ////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 53-2-0 FIG.1B. 2 L 7 4 4F RT 4A25 2001072500409 20010725 00409 WP 2001 7 25 RRXA11250 1 20010610 A 5300 5613865225 INTERCOSTAL DOUG DC8 DC873F 302199F WP L/H AFT NLG DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO L/H AFTNLG DOOR INTERCOSTAL AT L32L-L33L, DAMAGE EXCEEDED LIMITATIONS I AW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 2001072500410 20010725 00410 WP 2001 7 25 RRXA11251 1 20010610 A 5310 5641543 ANGLE DOUG DC8 DC873F 302199F WP STA70 LBL30 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FLOOR BEAM SUPPORT ANGLE STA.70 AND LBL30, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLE D IAW DC-8 SRM 51-3-0 AND DWG#5641543. 2 L 7 4 4F RT 4A25 2001072500411 20010725 00411 WP 2001 7 25 RRXA11252 1 20010610 A 5300 9754947 ANGLE DOUG DC8 DC873F 302199F WP STA1220-1228 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO C-PIT ANGLE AT STA.1220-1228 AND L27R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLE D IAW DC-8 SRM 51-1-21, 51-1-20D AND DWG#9754947. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500412 20010725 00412 WP 2001 7 25 RRXA11253 1 20010610 A 5710 56554416 BRACKET DOUG DC8 DC873F 302199F WP PNUE DUCT SUPPOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H I/B L/E PNEUMATIC DUCT SUPPORT BRACKET, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALL ED IAW DC-8 SRM 51-1-21, 51-1-20D, DWG#56555. 2 L 7 4 4F RT 4A25 2001072500413 20010725 00413 WP 2001 7 25 RRXA11254 1 20010610 A 5300 3642838 LONGERON DOUG DC8 DC873F 302199F WP STA8-70 L33L CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LONGERON AT STA. 8-70 AND L33L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SR M. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC- 8 SRM 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2001072500414 20010725 00414 WP 2001 7 25 RRXA11255 1 20010610 A 5700 43543144 DOUBLER DOUG DC8 DC873F 302199F WP STA. XS461.372 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H WING CENTER L/E AT STA. XS461.372, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IA W DC-8 SRM 51-1-20D AND 57-2-0 FIG.2. 2 L 7 4 4F RT 4A25 2001072500415 20010725 00415 WP 2001 7 25 RRXA11256 1 20010610 A 5300 475851A512 FITTING DOUG DC8 DC873F 302199F WP STA1280 L33R CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO INTERCOSTAL ATTACH FITTING AT STA. 1280 AND L33R, DAMAGE EXCEEDED LIMI TATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001072500416 20010725 00416 WP 2001 7 25 RRXA11257 1 20010610 A 5300 3642838 LONGERON DOUG DC8 DC873F 302199F WP STA55-70 L33R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FWD ACCY COMPARTMENT LONGERON AT STA.55-70 AND L33R, DAMAGE EXCEED ED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PA RT AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D AND DWG#3642838. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500417 20010725 00417 WP 2001 7 25 RRXA11259 1 20010610 A 5321 5758571 FITTING DOUG DC8 DC873F 302199F WP STA1320 L33R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SEAT TRACK SUPPORT FITTING AT STA.1320 AND L33R, DAMAGE EXCEEDED L IMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART A ND INSTALLED IAW DC-8 SRM 51-1-20D AND DWG#5758571. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500418 20010725 00418 WP 2001 7 25 RRXA11260 1 20010610 A 5312 4615293 LONGERON DOUG DC8 DC873F 302199F WP STA45 L34R CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FWD ACCY COMPARTMENT LONGERON AT STA.45 AND L34R, DAMAGE EXCEEDED LIMI TATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND DWG#4615293. 2 L 7 4 4F RT 4A25 2001072500419 20010725 00419 WP 2001 7 25 RRXA11261 1 20010610 A 5312 42543C371 STRAP DOUG DC8 DC873F 302199F WP STA35-55 LBL48 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO A/C BAY SUB-FLOOR AT STA.35-55 AND LBL48, DAMAGE EXCEEDED LIMITATI ONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND IN STALLED IAW DC-8 SRM 51-3-0 AND DHSK606673. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500420 20010725 00420 WP 2001 7 25 RRXA11262 1 20010610 A 5312 5649327 LONGERON DOUG DC8 DC873F 302199F WP L17R #60 HOLE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FITTING AT L17R AND IN #60 HOLE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC- 8 SRM 51-1-21 AND DWG#51616751. 2 L 7 4 4F RT 4A25 2001072500421 20010725 00421 WP 2001 7 25 RRXA11263 1 20010610 A 5730 57696000 DOUBLER DOUG DC8 DC873F 302199F WP RH WING DOUBLER CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H WING O/B L/E INBOARD INTERNAL DOUBLER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALL ED IAW DC-8 SRM 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 2001072500422 20010725 00422 WP 2001 7 25 RRXA11264 1 20010610 A 5312 9751002207 SLIDE DOUG DC8 DC873F 302199F WP STA280 L32R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO A-PIT FLOOR SUPPORT DOOR JAMB AT STA.280 AND L32R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500423 20010725 00423 WP 2001 7 25 RRXA11265 1 20010610 A 5330 5779936 DOUBLER DOUG DC8 DC873F 302199F WP STA1640-1670 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO AFT ACCY COMPARTMENT INTERNAL SKIN DOUBLER AT STA.1640-1670 AND L31 R-L32R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DHSK606-832. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500424 20010725 00424 WP 2001 7 25 RRXA11266 1 20010610 A 5321 607158 SEAT TRACK DOUG DC8 DC873F 302199F WP STA505 RBL45 WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK SCALLOP AT STA.505 AND RBL45, DAMAGE EXCEEDED LIMITATIONS IA W DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3 FIG.8A. 2 L 7 4 4F RT 4A25 2001072500425 20010725 00425 WP 2001 7 25 RRXA11267 1 20010610 A 5730 5643321145 FITTING DOUG DC8 DC873F 302199F WP LH WING #1 SPOIL CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LEFT WING UPPER #1 T/E SPOILER OUTBOARD HINGE FITTING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 2001072500426 20010725 00426 WP 2001 7 25 RRXA11268 1 20010610 A 5100 3754914501 FITTING DOUG DC8 DC873F 302199F WP STA340 L31R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO A-PIT FRAME BANNANA FITTING AT STA.340 AND L31R, DAMAGE EXCEEDED L IMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART A ND INSTALLED IAW DC-8 SRM 51-3-0, 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500427 20010725 00427 WP 2001 7 25 RRXA11269 1 20010610 A 5300 9753257501 SEAT TRACK DOUG DC8 DC873F 302199F WP CAPT'S SEAT TRAC WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT CAPTAINS SEAT UPPER I/B AND O/B, DAMAGE EXCEEDED LIMITATI ONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INST ALLED IAW DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001072500428 20010725 00428 WP 2001 7 25 RRXA11270 1 20010610 A 5300 3657501501N SEAT TRACK DOUG DC8 DC873F 302199F WP FO'S SEAT TRACK WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO FIRST OFFICERS SEAT TRACK I/B AND O/B, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IA W DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001072500429 20010725 00429 WP 2001 7 25 RRXA11271 1 20010610 A 5100 5750726 INTERCOSTAL DOUG DC8 DC873F 302199F WP STA440 L31R CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO B-PIT INTERCOSTAL AT STA.440 AND L31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED I AW DC-8 SRM 51-1-20D AND DWG#5750726. 2 L 7 4 4F RT 4A25 2001072500430 20010725 00430 WP 2001 7 25 RRXA11272 1 20010610 A 5100 37502571N FITTING DOUG DC8 DC873F 302199F WP STA440-460 L31R CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO B-PIT SPLICE FITTING AT STA.440-460 AND L31R, DAMAGE EXCEEDED LIMITATI ONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INST ALLED IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001072500431 20010725 00431 WP 2001 7 25 RRXA11273 1 20010610 A 5312 9754002206 SUPPORT DOUG DC8 DC873F 302199F WP STA340 L32L CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO A-PIT CROSS SLIDE DOOR JAMB FLOOR SUPPORT AT STA.340 AND L32L, DAM AGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FAB RICATED PART AND INSTALLED IAW DHSK606831. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500432 20010725 00432 WP 2001 7 25 RRXA11275 1 20010613 A 5312 561540395 WEB DOUG DC8 DC873F 302199F WP FWD ENTRY DOOR MISDRILLED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND DRILL DAMAGE TO FWD ENTRY DOOR INNER SKIN FWD LOWER WEB, DAMAGE EXCEEDED LIMITATIONS I AW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21 AND DWG#5615405. 2 L 7 4 4F RT 4A25 2001072500433 20010725 00433 WP 2001 7 25 RRXA11277 1 20010613 A 5312 5616520244 WEB DOUG DC8 DC873F 302199F WP STA515-520 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO B-PIT TORQUE BOX WEB AT STA515-520, DAMAGE EXCEEDED LIMITATIONS IA W DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4, 51-1-20D AND DWG#5616520. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500434 20010725 00434 WP 2001 7 25 RRXA11278 1 20010526 A 5730 2718809 FITTING DOUG DC8 DC873F 302199F WP STA993 BL0-BL7 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TOR/H WW STIFFNER AT STA.933 AND BL0-BL7, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IA W DC-8 SRM 51-3-0, 51-1-21 AND DWG#2718809. 2 L 7 4 4F RT 4A25 2001072500435 20010725 00435 WP 2001 7 25 RRXA11279 1 20010613 A 5720 56526853 PANEL DOUG DC8 DC873F 302199F WP STA.410 GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO L/H FLAP AT STA.410, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CO RRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-3 -0. 2 L 7 4 4F RT 4A25 2001072500436 20010725 00436 WP 2001 7 25 RRXA11280 1 20010613 A 5710 5758382 SKIN DOUG DC8 DC873F 302199F WP XRS22.750 STR#3 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO R/H UPPER WING SKIN AT STA. XRS22.750 AND STR#3, DAMAGE EXCEEDED LI MITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AN D INSTALLED IAW DC-8 SRM 57-2-0 FIG.7. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500437 20010725 00437 WP 2001 7 25 RRXA11281 1 20010613 A 5310 56165202 INTERCOSTAL DOUG DC8 DC873F 302199F WP STA515-520 L31R GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO B-PIT DOOR FWD JAMB INTERCOSTAL AT STA.515-520 AND L31R, DAMAGE EXCEED ED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PA RT AND INSTALLED IAW DC-8 SRM 51-1-20D, AND DWG#5616520. 2 L 7 4 4F RT 4A25 2001072500438 20010725 00438 WP 2001 7 25 RRXA11283 1 20010614 A 2710 5705334 DOUBLER DOUG DC8 DC873F 302199F WP AILERONPANEL#541 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO L/H I/B AILERON PANEL #541 INTERNAL DOUBLER. DAMAGE EXCEEDED LIMITATION S IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTAL LED IAW DHSK606-513. 2 L 7 4 4F RT 4A25 2001072500439 20010725 00439 WP 2001 7 25 RRXA11284 1 20010614 A 5310 565192728 ANGLE DOUG DC8 DC873F 302199F WP VERT STAB RH ANG CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO VERTICAL STAB R/H ATTACH ANGLE 10" FWD OF FWD SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 55-2-0 FIG.6. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500440 20010725 00440 WP 2001 7 25 RRXA11285 1 20010614 A 5750 5761743 HINGE DOUG DC8 DC873F 302199F WP STA219 RH FLAP CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H O/B FLAP SPRING PANEL I/B HINGE AT STA.219, DAMAGE EXCEEDED LIMITAT IONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INS TALLED IAW DC-8 SRM 51-1-21, 51-3-0. 2 L 7 4 4F RT 4A25 2001072500441 20010725 00441 WP 2001 7 25 RRXA11286 1 20010614 A 5315 5612144 FLOORBEAM DOUG DC8 DC873F 302199F WP RBL24 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOORBEAM ATS STA.1700 AND RBL 24, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DHSK606-343. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500442 20010725 00442 WP 2001 7 25 RRXA11287 1 20010614 A 5730 5758382 SKIN DOUG DC8 DC873F 302199F WP XRS261 STR13 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LT. WING UPPER SKIN AT STA. XRS261 AND STR.13, DAMAGE EXCEEDED LIMITATI ONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INST ALLED IAW DC-8 SRM 57-2-1 FIG11. 2 L 7 4 4F RT 4A25 2001072500443 20010725 00443 WP 2001 7 25 RRXA11288 1 20010614 A 5730 5758382 SKIN DOUG DC8 DC873F 302199F WP XW408 STR.6 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LT WING UPPER SKIN AT STA. XW408 AND STR.6, DAMAGE EXCEEDED LIMITAT IONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INS TALLED IAW DC-8 SRM 57-2-1 FIG21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500444 20010725 00444 WP 2001 7 25 RRXA11289 1 20010614 A 5300 3757794 FITTING DOUG DC8 DC873F 302199F WP C-PIT CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO C-PIT CROSS SLIDE DOOR FWD UPPER CUTOUT SUPPORT FITTING, DAMAGE EXCEEDE D LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PAR T AND INSTALLED IAW DC-8 SRM 51-1-20D AND DWG#3757794. 2 L 7 4 4F RT 4A25 2001072500445 20010725 00445 WP 2001 7 25 RRXA11290 1 20010615 A 5330 570913443 WEB DOUG DC8 DC873F 302199F WP STA35-40 L24-25L CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO WEB AT STA.35-40 AND L24L-L25L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SR M. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-1-0, 51-1-20D AND DWG#5709134. 2 L 7 4 4F RT 4A25 2001072500446 20010725 00446 WP 2001 7 25 RRXA11294 1 20010615 A 5230 5753890 PAN DOUG DC8 DC873F 302199F WP STA320 L32R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO A-PIT CROSS SLIDE DOOR PAN AT STA.320 AND L32R, DAMAGE EXCEEDED LIM ITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR A ND INSTALLED IAW DC-8 SRM 52-2-0 FIG2 AND 52-1-0, 51-3-0, 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500447 20010725 00447 WP 2001 7 25 RRXA11295 1 20010615 A 5310 2772660 SEAT TRACK DOUG DC8 DC873F 302199F WP STA.513 RBL25 WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA.513 AND RBL25, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SR M. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3 FIG8A. 2 L 7 4 4F RT 4A25 2001072500448 20010725 00448 WP 2001 7 25 RRXA11296 1 20010615 A 5310 5822929 FRAME DOUG DC8 DC873F 302199F WP STA.1000 L36 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA.1000 AND L36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM . /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-1-21 AND DHSK606-605. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500449 20010725 00449 WP 2001 7 25 RRXA11297 1 20010615 A 5330 561386253 DOUBLER DOUG DC8 DC873F 302199F WP STA.8-70 L30L CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION TO L/H INTERNAL DOUBLER AT STA.8-70 AND L30L-L34R, DAMAGE EXCEEDED LIMITATION S IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTAL LED IAW DC-8 SRM 53-1-0, 51-1-20D, 51-1-21 AND DWG#5613862. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500450 20010725 00450 WP 2001 7 25 RRXA11298 1 20010615 A 5310 52772660 SEAT TRACK DOUG DC8 DC873F 302199F WP STA.1480 BL.0 WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA.1480 AND BL.0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SR M. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3 FIG8A. 2 L 7 4 4F RT 4A25 2001072500451 20010725 00451 WP 2001 7 25 RRXA11299 1 20010615 A 5100 8538005 ANGLE DOUG DC8 DC873F 302199F WP STA.1750-1790 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO R/H SIDE OF VERT. STAB LWR SKATE ANGLE AT STA.1750-1790, DAMAGE EXC EEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-0-25 FIG16A. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500452 20010725 00452 WP 2001 7 25 RRXA11300 1 20010616 A 5310 5623836 DOUBLER DOUG DC8 DC873F 302199F WP STA.35-70 L34L CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO INTERNAL DOUBLER AT STA.35-70 AND L34L-L34R, DAMAGE EXCEEDED LIMITATION S IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTAL LED IAW DC-8 SRM 51-1-21 AND DWG#5623836. 2 L 7 4 4F RT 4A25 2001072500453 20010725 00453 WP 2001 7 25 RRXA11301 1 20010616 A 5300 5613836 SHEAR TIE DOUG DC8 DC873F 302199F WP STA.35 L34L CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO DOOR PAN SHEAR TIE AT STA.35 AND L34L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLE D IAW DC-8 SRM 51-1-21 AND DWG#5613836. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500454 20010725 00454 WP 2001 7 25 RRXA11302 1 20010616 A 5300 5613836 SHEAR TIE DOUG DC8 DC873F 302199F WP STA35 L34L-L34R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SHEAR TIE AT STA.55 AND L34L-L34R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IA W DC-8 SRM 51-1-21 AND DWG#5613836. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500455 20010725 00455 WP 2001 7 25 RRXA11303 1 20010616 A 5730 5611015501 PANEL DOUG DC8 DC873F 302199F WP STA.410 DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO L/H WING LOWER T/E PANEL I/B OF FLAP HINGE AT STA.410, DAMAGE EX CEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATE D PART AND INSTALLED IAW DC-8 SRM 51-1-21. (CORROSION DAMAGE RECORDE IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500456 20010725 00456 WP 2001 7 25 RRXA11304 1 20010617 A 5100 58942822 FITTING DOUG DC8 DC873F 302199F WP STA.313 L33R-L32 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO BATH TUB FITTING AT STA.313 AND L33R-L32R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLE D IAW DC-8 SRM 53-2-0 FIG2D, 51-1-21. 2 L 7 4 4F RT 4A25 2001072500457 20010725 00457 WP 2001 7 25 RRXA11305 1 20010617 A 5310 5764343509 FRAME DOUG DC8 DC873F 302199F WP STA1100 L33R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA.1100 AND L33R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SR M. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20A&D, 51-1-21, AND DWG#5764343. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500458 20010725 00458 WP 2001 7 25 RRXA11306 1 20010618 A 5100 425437851 FITTING DOUG DC8 DC873F 302199F WP STA315-340 L32R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATH TUB FITTING AT STA.315-340 AND L32R-L33R, DAMAGE EXCEEDED LIMI TATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 53-2-0 FIG2D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500459 20010725 00459 WP 2001 7 25 RRXA11307 1 20010618 A 5300 435436081 SPLICE DOUG DC8 DC873F 302199F WP STA1020 L30L CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA.1020 AND L30L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SR M. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 53-2-0, 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500460 20010725 00460 WP 2001 7 25 RRXA11312 1 20010620 A 5730 3889710 PANEL DOUG DC8 DC873F 302199F WP XRS-6 TO XRS20 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO L/H UPPER SKIN FORWARD OF CENTER SPAR AT STA. XRS-6 TO XRS20, DAMAG E EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRI CATED REPAIR AND INSTALLED IAW DHSK606-880. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500461 20010725 00461 WP 2001 7 25 RRXA11313 1 20010620 A 5710 56110113501 PANEL DOUG DC8 DC873F 302199F WP STA.219 DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO L/H WING LWR T/E PANEL INBOARD OF FLAP HINGE AT STA.219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICA TED PART AND INSTALLED IAW DC-8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500462 20010725 00462 WP 2001 7 25 RRXA11314 1 20010620 A 5100 58942821 FITTING DOUG DC8 DC873F 302199F WP STA310 L32-33R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO A-PIT BATH TUB FITTING AT STA.310 AND L32R-L33R, DAMAGE EXCEEDED LI MITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AN D INSTALLED IAW DC-8 SRM 53-2-0 FIG2D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500463 20010725 00463 WP 2001 7 25 RRXA11315 1 20010621 A 2780 2718274 DOUBLER DOUG DC8 DC873F 302199F WP LH IB SLOT VANE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND SCREWS PULLING THRU INBOARD END OF L/H INBOARD SLOT VANE, DAMAGE EXCEEDED LIMITATIONS I AW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALL ED IAW DC-8 SRM 51-1-26, 51-3-0. 2 L 7 4 4F RT 4A25 2001072500464 20010725 00464 WP 2001 7 25 RRXA11316 1 20010621 A 2710 5751186507 FITTING DOUG DC8 DC873F 302199F WP STA.339 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO L/H FLAP BASE FITTING AT STA.339, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC- 8 SRM 51-3-0, 27-2-4 FIG5. 2 L 7 4 4F RT 4A25 2001072500465 20010725 00465 WP 2001 7 25 RRXA11320 1 20010624 A 5310 561667487 ANGLE DOUG DC8 DC873F 302199F WP D-PIT DOOR JAMB CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO ANGLE AT D-PIT DOOR JAMB LOWER SEAL DEPRESSOR, DAMAGE EXCEEDED LIMITATI ONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INST ALLED IAW DC-8 SRM 51-1-21, 51-1-21A. 2 L 7 4 4F RT 4A25 2001072500466 20010725 00466 WP 2001 7 25 RRXA11322 1 20010626 A 5700 435436941 WEDGE DOUG DC8 DC873F 302199F WP STA340-410 DENTED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND DENTED DAMAGE TO L/H O/B FLAP T/E WEDGE AT STA.340-410, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED I AW DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001072500467 20010725 00467 WP 2001 7 25 RRXA11323 1 20010628 A 5300 56141605 FRAME DOUG DC8 DC873F 302199F WP STA.55 L24R CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FRAME AT STA.55 AND L24R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /// //CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51 -1-20D, 51-1-11, 53-2-0 FIG2. 2 L 7 4 4F RT 4A25 2001072500468 20010725 00468 WP 2001 7 25 RRXA11324 1 20010629 A 5310 5822929 LONGERON DOUG DC8 DC873F 302199F WP STA320 L29L CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON AT STA.320 AND L29L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC- 8 SRM 53-2-2 FIG10 AND DWG#9754913. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500469 20010725 00469 WP 2001 7 25 RRXA11325 1 20010621 A 5310 3755827501 FITTING DOUG DC8 DC873F 302199F WP STA.270 L30R CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FITTING AT STA.270 AND L30R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 2001072500470 20010725 00470 WP 2001 7 25 RRXA11328 1 20010702 A 5730 5643000 SKIN DOUG DC8 DC873F 302199F WP XRS210 LH WING DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTANCE VISIT FOUND DAMAGE TO L/H WING T/E SKIN AT STA. XRS210, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /// //CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0 FIG2A. 2 L 7 4 4F RT 4A25 2001072500471 20010725 00471 WP 2001 7 25 RRXA11329 1 20010703 A 5200 4354071 ANGLE DOUG DC8 DC873F 302199F WP STA1160 L33L CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO C-PIT CROSS SLIDE FWD JAMB TRACK GUIDES AT STA. 1160 AND L33L-L33R, DAM AGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FAB RICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0 AND DHSK606-071. 2 L 7 4 4F RT 4A25 2001072500472 20010725 00472 WP 2001 7 25 RRXA11332 1 20010713 A 5310 5646444569 INTERCOSTAL DOUG DC8 DC873F 302199F WP STA970-980 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO 4 INTERCOSTALS AT STA.970-980 AND RBL48-55 AND R/H W/W AFT FRAME, D AMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. F ABRICATED PART AND INSTALLED IAW DC-8 SRM 53-1-0, 51-1-21, 51-1-21A. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM ). 2 L 7 4 4F RT 4A25 2001072500473 20010725 00473 WP 2001 7 25 RRXA11333 1 20010714 A 5730 5751784 SKIN DOUG DC8 DC873F 302199F WP STA. XFS157-163 DENTED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND DENT DAMAGE TO L/H WING AUX TANK UPPER SKIN AT STA. XFS157-163, DAMAGE EXCEEDED LIMITAT IONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND I NSTALLED IAW DHSK 606-294. 2 L 7 4 4F RT 4A25 2001072500474 20010725 00474 WP 2001 7 25 RRXA11334 1 20010717 A 5330 5613862 SKIN DOUG DC8 DC873F 302199F WP STA-21TO70 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BELLY SKIN AT STA.-21TO70 AND L31L-L31R, DAMAGE EXCEEDED LIMITATION S IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTAL LED IAW DHSK 606-485. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500475 20010725 00475 WP 2001 7 25 RRXA11335 1 20010717 A 5310 38903881 SPLICE PLATE DOUG DC8 DC873F 302199F WP STA1580-1600 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO AFT ACCY COMPARTMENT SPLICE PLATE AT STA.1580-1600 AND LBL46, DAMAG E EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRI CATED PART AND INSTALLED IAW DC-8 SRM 53-1-0, 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001072500476 20010725 00476 WP 2001 7 25 ASAA0180174 1 20010518 A 3350 60030451 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY CEILING LIGHTS AT ROWS 8, 10 AND 12 WERE FOUND TO BE INOPERATIVE. REPLACE D THE POWER SUPPLY AND THE LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001072500477 20010725 00477 NM 2001 7 25 ASAA0140079 1 20010523 A 3350 70036611 POWER SUPPLY BOEING 737 7374Q8 NM INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 763AS 25100 ANC - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE AT ROW 21-24. REMOVED AND REPLACED POWER SUPP LY (BALLAST), OPS NORMAL. (M) 2 L 7 2 4F RT A16WE 2001072500478 20010725 00478 NM 2001 7 25 ASAA0110275 1 20010521 A 3350 883200312 RECEIVER BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - DURING A LINE MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHTING WAS FOUND TO BE INOPERATIVE ON PALLETS 6 AND 7. REP LACED THE EMERGENCY LIGHTING REMOTE RECEIVER ON PALLETS 6 AND 7. THE LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2001072500479 20010725 00479 NM 2001 7 25 ASAA0110305 1 20010526 A 3350 8821004 BATTERY PACK BOEING 737 737298C 1384490 NM DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROW 9 INOPERATIVE. REMOVED AND REPLACED BATTERY PACK THE N LIGHTS OPERATED NORMAL. (M) 2 L 7 2 4F RT A16WE 2001072500480 20010725 00480 NM 2001 7 25 ASAA0110312 1 20010529 A 3350 86210144 BATTERY BOEING 737 737290C 138448V NM MID CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING MAINTENANCE CHECK, FUOND EMERGENCY EXIT LIGHT AT SEAT PALLETS 6-7, 7-5 AND 9-3 INOPERATIVE. REMOVED AND RE PLACED REMOTE ASSEMBLY BATTERIES THEN LIGHTS OPERATED NORMAL. (M) 2 L 7 2 4F A16WE 2001072500481 20010725 00481 WP 2001 7 25 ASAA0180199 1 20010613 A 3350 6011779 POWER SUPPLY DOUG DC9 DC983 3022083 WP DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 950AS 53023 SEA - DURING LINE CHECK, RIGHT OVERWING EMERGENCY EXIT LIGHT WAS DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BATT ERY PACK (POWER SUPPLY). LIGHT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001072500482 20010725 00482 NM 2001 7 25 ASAA0110341 1 20010611 A 3350 86210144 BATTERY BOEING 737 737290C 138448V NM MID CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT IDENTIFIER ON THE SMOKE BARRIER INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY THEN EXIT IDENTIFIER OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2001072500483 20010725 00483 WP 2001 7 25 ASAA0180178 1 20010522 A 3350 60030451 POWER SUPPLY DOUG DC9 DC982 3022082 WP FWD CABIN DISCHARGED A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 933AS 49234 PHX - PRIOR TO FLT 707 - THE EMERGENCY EXIT LIGHTS FROM ROW 10 FORWARD WERE FOUND TO BE INOPERATIVE. REPLACED THE POWER SUPPLY AND THE LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 2001072500484 20010725 00484 WP 2001 7 25 ASAA0180196 1 20010609 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 951AS 49111 SEA - DURING PREFLIGHT CHECK, OVERWING EMERGENCY EXIT LIGHTS WERE DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BAT TERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001072500485 20010725 00485 NM 2001 7 25 ASAA0110320 1 20010608 A 3350 6013211 BATTERY PACK BOEING 737 7372X6C 1384552 NM INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND EMERGENCY EXIT LIGHTS AT THE RIGHT OVERWING EXIT WOULD NOT ILLUMINATE. REMOVED AN D REPLACED BATTERY PACK AND LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2001072500486 20010725 00486 NM 2001 7 25 ASAA0110146 1 20010322 A 5200 65458492 DOOR BOEING 737 737290C 138448V NM R2 DOOR STIFF A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 ANC - DURING MAINTENANCE CHECK, FOUND R2 DOOR DIFFICULT TO OPEN OR CLOSE. LUBED R2 DOOR AND DOOR OPENED NORMALLY. (M) 2 L 7 2 4F A16WE 2001072500487 20010725 00487 2001 7 25 ASAA0180170 4 20010516 A 2565 D29982121 SLIDE DOUG DC9 DC983 3022083 WP R1 DOOR OUT OF POSITION A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 37654 4776 53024 SEA - DURING PRE-FLIGHT CHECK, FOUND R1 SLIDE PACK OFF DOOR. REINSTALLED SLIDE PACK IN DOOR SHROUD. (M) 2 L 7 2 4F RT A6WE 2001072500488 20010725 00488 NE 2001 7 25 GTIA010421 2 20010523 A 7200 ENGINE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE NR 1 MALFUNCTIONED A GTIA E ENGINE SHUTDOWN J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 23 807NK 49777 EWR - FLT 1181 - DURING ENGINE START OF NR 1 LEFT ENGINE CREW OF SEVERAL 'HOT START' INDICATIONS AFTER FORWARD LEVER WAS MOVED TO 'ON' POSITION EGT ROCKETED THROUGH 500 DEGREES AT 550 DEGREES CREW RETURNED TO FUEL LEVER TO 'OFF' POSITION. EGT PEAKED AT 570-580 DEGREES MOMENTARILY THAN RAPIDLY COOLED TO LESS THAN 150 DEGREES AS ENGINE WAS MOTORED FOR 30 SECO NDS. F/A'S REPORTED A STRONG SMELL OF JET FUEL IN THE REAR CABIN AREA. ACCOMPLISHED INSPECTION OF INTAKE, EXHAUST OF N R 1 ENGINE FOUND NO DEFECT, INSPECTED FUEL LINES AND PLUMBING FOR LEAKS FOUND NONE. OPS CHECK ENGINE START SEVERAL TIME S FOUND EGT IN NORMAL RANGE ON ALL STARTS AS PER MD80 CH 80-10-00. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2001072500490 20010725 00490 EU 2001 7 25 SIMA20011213 1 20010501 A 6120 PROPELLER AEROSP ATR42 ATR42300 8680920 EU NR 1 ENGINE MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 21 971NA 017 MIA - FLT 5251 - AFTER TAKEOFF, CREW REPORTED THE NR 1 PROPELLER SPEED WENT TO ZERO. MAINTENANCE COULD NOT DUPLICATE DI SCREPANCY. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001072500491 20010725 00491 EU 2001 7 25 SIMA20011295 1 20010509 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 329AE 340B329 FLT 3003 - SAN - CREW REPORTED THE EMERGENCY LIGHTS FAIL AFTER 15 SECONDS. AIRCRAFT WAS FERRIED TO LAX FOR MAINTENANCE. MAINTENANCE REMOVED AND REPLACED BATTERY PACKS (S/N 18484, 17509) AT 141AL AND 141CZ. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001072500492 20010725 00492 EU 2001 7 25 SIMA20011311 1 20010511 A 3230 C245890001 UPLOCK AEROSP ATR72 ATR72212A 8680902 EU RT MLG FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 536AT 536 DFW - FLT 3737 - AFTER TAKEOFF FROM DFW, THE LANDING GEAR WAS RETRACTED THE RIGHT MAIN GEAR KEPT CYCLING UP AND DOWN. C REW RETURNED THE AIRCRAFT TO DFW FOR MAINTENANCE. MAINTENANCE REMOVED AND REPLACED THE MAIN LANDING GEAR UPLOCK BOX IAW ATR MM. OPERATIONAL AND LEAK CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001072500493 20010725 00493 EU 2001 7 25 SIMA20011355 1 20010515 A 3350 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 304AE 340B304 BUF - FLT 5132 - FORWARD PORTION OF EMERGENCY LIGHT SYSTEM ILLUMINATES FOR APPROXIMATELY 45 SECONDS THEN GO OUT. AIRCRA FT WAS FERRIED TO JFK FOR REPAIRS. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY UNITS 20LN, 21LN, 22LN , 23LN, AND 24LN IAW SAAB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001072500494 20010725 00494 EU 2001 7 25 SIMA20011362 1 20010516 A 3230 LATCH AEROSP ATR72 ATR72212 EU LT MLG OUT OF POSITION A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 274AT 274 MIA - FLT 5339 - AFTER TAKEOFF, WHEN GEAR SELECTED TO THE UP POSITION AND RECEIVED AN UNLOCK LIGHT ON THE OVERHEAD PANEL . CREW RECYCLED GEAR HANDLE AND GOT THE SAME RESULTS. AIRCRAFT WAS RETURNED TO MIA AND LANDED WITH NO FURTHER INCIDENT . MAINTENANCE FOUND THE LEFT MLG UPLOCK BOX LATCH IN THE UP AND LOCKED POSITION. UPLOCK BOX WAS RESET IAW ATR MM. AIR CRAFT WAS THEN RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001072500495 20010725 00495 EU 2001 7 25 SIMA20011363 1 20010516 A 3350 66363 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 382AE 340B382 LAW - FLT 3848 - CREW REPORTED FOUR SECTIONS OF FLOOR EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D EMERGENCY LIGHTS STRIPS IAW SAAB AMM 33-50-20. OPS CHECK GOOD AT THIS TIME AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001072500496 20010725 00496 EU 2001 7 25 SIMA20011374 1 20010517 A 2121 FAN AEROSP ATR72 ATR72212A 8680902 EU CABIN ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 550LL 550 FLIGHT ATTENDANT REPORTED THE SMELL OF BURNING INSULATION AROUND ROW EIGHT IN THE CABIN. THE SOURCE OF THE SMELL WAS DE TERMINED TO BE FROM THE NR 2 RECIRCULATION FAN. RECIRCULATION FAN IS ALREADY ON MEL. (M) 2 H 7 2 4T RT A53EU 2001072500497 20010725 00497 EU 2001 7 25 SIMA20011382 1 20010518 A 3350 1317 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 232AE 340B232 YUL - FLT 4748 - CREW REPORTED THE EMERGENCY LIGHTS AT ROW 14 OVERHEAD, FLOOR PROXIMITY AT ROW 5BC TO BE INOPERATIVE. M AINTENANCE REPLACED BULBS AT BOTH LOCATIONS IAW SAAB MM 33-50-20. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVI CE. (M) 2 L 7 2 4T RT A52EU 2001072500498 20010725 00498 2001 7 25 SIMA20011405 4 20010520 A 2300 5020066005 CONTROL UNIT SAAB SF340 340B 7860101 EU COCKPIT INOPERATIVE A SIMA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 263AE 340B263 ALB - FLT 5110 - CAPTAINS PUSH TO TALK STAYS IN TRANSIT POSITION AT ALL TIMES. DIVERTED TO ALB FOR MTX. MAINTENANCE RE MOVED AND REPLACED REMOTE ELECTRONIC UNIT IAW SAAB 340AMM CH 23-50-05. OPS CHECK GOOD AT THIS TIME AND AIRCRAFT WAS RET URNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001072500499 20010725 00499 EU 2001 7 25 SIMA20011407 1 20010520 A 2120 UNKNOWN SAAB SF340 340B 7860101 EU CABIN ODOR A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 21 902AE 340B269 BPT - FLT 3361 - AFTER LANDING DURING TAXI TO GATE, THE FLIGHT ATTENDANT REPORTED A STRONG ELECTRICAL ODOR THAT SEEMED T O BE COMING FROM AROUND SEAT 7A OVERHEAD. CREW CONTINUED TO GATE AND DEPLANED PASSENGERS. CREW REPORTED ODOR ONLY, NO SMOKE. MAINTENANCE COULD NOT VERIFY DISCREPANCY. WINDOW LIGHTS AND BALLASTS AT SEATS 5, 6, 7, 8 AND 9 WERE INSPECTED W ITH NO DAMAGE FOUND AND NO ELECTRICAL ODOR NOTED. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001072500500 20010725 00500 EU 2001 7 25 SIMA20011431 1 20010523 A 3350 66362 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 380AE 340B380 LAW - MAINTENANCE REPORTED THE NR 2 FLOOR PROXIMITY EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED THE FLOOR L IGHT STRIP IAW SAAB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001072500501 20010725 00501 NM 2001 7 25 AWXA0002037 1 20010718 A 5313 284N1025161 INTERCOSTAL BOEING 757 757225 1384959 NM STA 440 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 D: Intercostal cracked at STA 446 between STR 22L & 23LC: Removed cracked intercostal at STA 446-460, 23L. Installed rep lacement intercoastal at STA 440-460, 23L IAW SRM 51-40-02 Pg 4 2 L 7 2 4F RT A2NM 2001072500502 20010725 00502 NM 2001 7 25 AWXA0002038 1 20010719 A 5313 141N5150 INTERCOSTAL BOEING 757 757225 1384959 NM STA 377 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 D: Pas. Cabin RBL 54 STA 377-420 Intercostal corroded top surface around fastner holes.C: Removed intercostal, Fabbed & Installed Intercostal per SRM 51-40-02 pg 46-47 Fig 12 & SRM 57-30-01 pg 11 step 7 2 L 7 2 4F RT A2NM 2001072500503 20010725 00503 EU 2001 7 25 SIMA200114404 1 20010524 A 3150 WARNING SYSTEM SAAB SF340 340B 7860101 EU COCKPIT ACTIVATED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 219AE 340B219 DFW - FLT 3755 - DURING TAKEOFF ROLL AT APPROXIMATELY 100 KIAS, A RED CONFIGURE LIGHT ILLUMINATED WITH AN INTERMITTENT H ORN. TAKEOFF WAS ABORTED AND AIRCRAFT WAS RETURNED TO THE GATE. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPS CHEC K OF CONFIGURE WARNING SYSTEM WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001072500504 20010725 00504 EU 2001 7 25 SIMA200114606 1 20010526 A 3397 WIRE AEROSP ATR72 ATR72212A 8680902 EU CABIN LOOSE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 499AT 499 DFW - DURING SCHEDULED PHASE INSPECTION, MAINTENANCE REPORTED THE FORWARD FLOOR PROXIMITY EMERGENCY LIGHT TO BE INOPERAT IVE. MAINTENANCE FOUND WIRE LOOSE FROM SOCKET. WIRE WAS REATTACHED TO SOCKET IAW ATR AWM. OPS CHECK WAS GOOD AND AIRC RAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001072500505 20010725 00505 EU 2001 7 25 SIMA200114803 1 20010528 A 2613 WIRE SAAB SF340 340B 7860101 EU RT TAIL PIPE LOOSE A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 345SB 340B345 PVD - FLT 4528 - CREW REPORTED THE RIGHT TAIL PIPE HOT MASTER CAUTION LIGHT ILLUMINATED. MAINTENANCE FOUND LOOSE WIRE A T TAIL PIPE HOT DETECTOR 26WG. WIRE WAS RESECURED. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001072500506 20010725 00506 EU 2001 7 25 SIMA200115001 1 20010530 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 232AE 340B232 ISP - FLT 4622 - CREW REPORTED THE CABIN OVERHEAD LIGHT AT 11A TO BE INOPERATIVE. MAINTENANCE REPLACED THE BULB AT SEAT 11A EMERGENCY LIGHT. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001072500507 20010725 00507 EU 2001 7 25 SIMA200115101 1 20010531 A 3350 66362 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 386AE 340B386 DFW - MAINTENANCE REPORTED THE EMERGENCY LIGHT STRIP AT SEATS 3A AND 4A TO BE INOPERATIVE. MAINTENANCE REPLACED THE LIG HT STRIP AT 3A AND 4A IAW SAAB MM 33-50-20. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001072500508 20010725 00508 EU 2001 7 25 SIMA200115619 1 20010605 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 350CF 340B350 SBA - FLT 3037 - FORWARD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED POWERS SUPPLY AT 20LN AND 21LN (S/N 18524, 18070) IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001072500509 20010725 00509 EU 2001 7 25 SIMA200115704 1 20010606 A 3350 66362 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 371AE 340B371 SGF - FLT 3617 - FOUND FLOOR PROXIMITY EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED FLOOR PROXIMITY LIGHT STRIP IA W AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001072500510 20010725 00510 NE 2001 7 25 SIMA200115707 2 20010606 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT MALFUNCTIONED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 254AE 340B254 PSP - FLT 3091 - RIGHT ENGINE WENT TO 928 CELSIUS ON TAKEOFF. ABORTED TAKEOFF. PERFORMED GROUND ENGINE RUNS IAW 71-00- 00. FOUND ITT LIMITS WITHIN LIMITS. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 2001081500143 20010815 00143 NM 2001 8 15 01FDEA00592 1 20010703 A 5310 SHEAR TIE BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 221FE 20932 CORROSION ON FRAME SHEAR TIE BS 1166, RBL 3, WL 158. *S/D* REMOVED AND REPLACED PER IAW FEDEX EA 7-5310-57302. 2 L 7 3 4F RT A3WE 2001081500144 20010815 00144 NM 2001 8 15 01FDEA00593 1 20010713 A 5311 FRAME BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 221FE 20932 WHILE WORKING N 199 FOUND FLANGE OF FRAME BS 1070, LBL 23, WL 156 CRACKED. *S/D* REMOVED AND REPLACED PER IAW FEDEX SR M 51-40-3. 2 L 7 3 4F RT A3WE 2001072500511 20010725 00511 EU 2001 7 25 SIMA200116001 1 20010608 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 266AE 340B266 BOS - FLT 4903 - ALL EMERGENCY LIGHTS OUT. REMOVED AND REPLACED ALL EMERGENCY POWER SUPPLIES (S/N 18592, 20519, 18440, 1878, 17288) IAW AMM, LOCATION 20LN - 24LN. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001072500512 20010725 00512 EU 2001 7 25 SIMA200116005 1 20010609 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 256AE 340B256 BOS - FLT 4916 - EMERGENCY LIGHTS OVERHEAD INOPERATIVE AT 5BC, MEL ISSUED 33-13. (M) 2 L 7 2 4T RT A52EU 2001072500513 20010725 00513 EU 2001 7 25 SIMA200116102 1 20010610 A 3411 LINE SAAB SF340 340B 7860101 EU PITOT/STATIC SYS OBSTRUCTED A C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 339SB 340B339 DFW - FLT 3891 - ON TAKEOFF, CAPTAIN AIRSPEED INDICATION READ 50 KT AND FO'S READ 90 KT. ABORTED TAKEOFF. NO OTHER PRO BLEM NOTED. CLEANED OUT PITOT STATIC LINES IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001072500514 20010725 00514 EU 2001 7 25 SIMA200116105 1 20010610 A 3350 101130911 LIGHT AEROSP ATR72 ATR72212 EU CABIN BROKEN A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 308AE 309 DFW - FLT 3633 - EMERGENCY LIGHT STRIP BROKEN. REMOVED AND REPLACED EMERGENCY LIGHT STRIP AT ROW 15-17 IAW AMM 33-50-00 . OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 2001072500515 20010725 00515 EU 2001 7 25 SIMA200116202 1 20010611 A 3411 PITOT TUBE AEROSP ATR72 ATR72212 EU PITOT/STATIC SYS OBSTRUCTED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 434AT 434 DFW - FLT 3737 - F/O'S AIRSPEED INDICATOR FAILED TO REGISTER AIRSPEED AT 90 KIAS. ADU CLEARED ALL DATE AND DISPLAYED DA DC FAILURE. CLEANED BLOCKAGE FROM F/O'S PITOT TUBE IAW AMM. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001072500516 20010725 00516 EU 2001 7 25 SIMA200116204 1 20010611 A 3350 5211309111 LIGHT AEROSP ATR72 ATR72212A 8680902 EU CABIN BROKEN A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 541AT 541 DFW - FLT 3697 - EMERGENCY FLOOR LIGHT BY GALLEY CART IS BROKEN OFF. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 2001072500517 20010725 00517 SO 2001 7 25 SIMA200116205 1 20010611 A 7830 WARNING SYSTEM EMB 135 EMB135LR SO COCKPIT MALFUNCTIONED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 704PG 145174 ORD - FLT 4243 - ABORTED TAKEOFF REVERSE DISAGREE EICAS MESSAGE. PERFORMED HIGH SPEED TAXI TO VERIFY FAILURE IAW AMM. NO INDICATION WAS NOTED ON RUN. (M) 2 L 7 2 4F RT TOOO11AT 2001072500518 20010725 00518 2001 7 25 SIMA20011663 4 20010615 A 3444 WARNING SYSTEM SAAB SF340 340B 7860101 EU COCKPIT MALFUNCTIONED A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 383AE 340B383 DFW - FLT 3569 - DURING TAKEOFF, THE CREW REPORTED THE GPWS 'DON'T SINK' WARNING CAME ON. T/O WAS ABORTED. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. RADAR ALTIMETER ANTENNAS WERE CLEANED, GPWS COMPUTER WAS CHECKED FOR SECURITY, AND CO NNECTIONS TO THE RADAR ALTIMETER WERE CHECKED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001072500519 20010725 00519 EU 2001 7 25 SIMA20011671 1 20010616 A 3350 CONNECTOR SAAB SF340 340B 7860101 EU CABIN DAMAGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 243AE 340B243 JFK - FLT 5084 - CREW REPORTED AN EMERGENCY EXIT SIGN TO BE INOPERATIVE. MAINTENANCE REPAIRED CANNON PLUG 115UP IAW SAA B MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001072500520 20010725 00520 EU 2001 7 25 SIMA20011672 1 20010616 A 3150 WARNING LIGHT SAAB SF340 340B 7860101 EU COCKPIT FALSE INDICATION A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 240DS 340B240 BOS - FLT 4623 - CREW ABORTED TAKEOFF DUE TO CONFIGURE WARNING LIGHT ILLUMINATING. MAINTENANCE COULD NOT DUPLICATE DISC REPANCY. GROUND ENGINE RUN WAS COMPLIED WITH AND NO DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001072500521 20010725 00521 EU 2001 7 25 SIMA200116801 1 20010617 A 3350 SIGN SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 243AE 340B243 JFK - LEFT EMERGENCY EXIT SIGN LIGHT AT SEAT 8A IS INOPERATIVE. MAINTENANCE REPLACED FUSELAGE 39LN AND REPINNED CANNON PLUG 115UP. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001072500522 20010725 00522 EU 2001 7 25 SIMA200116802 1 20010617 A 3350 2LA00511520 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 398AM 340B398 DFW - FLT 3549 - CREW REPORTED AN OVERHEAD EMERGENCY LIGHT TO BE INOPERATIVE. LIGHT PUT ON MEL AT THIS TIME. MAINTENAN CE REPLACED THE LIGHT ASSEMBLY AT COVE 4A. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001072500523 20010725 00523 SO 2001 7 25 SIMA200116901 1 20010618 A 2740 3621001007 CONTROL UNIT EMB 135 EMB135LR SO HORIZ STAB FAILED A SIMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 713AE 145239 BOS - FLT 4649 - DURING TAXI FROM GATE, CREW REPORTED A NR 1 PITCH TRIM FAIL. AIRCRAFT WAS RETURNED TO THE GATE. MAINT ENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETU RNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001072500524 20010725 00524 SO 2001 7 25 SIMA200117105 1 20010620 A 5315 FLOORBEAM EMB 145 EMB145 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 640AE 145183 ABI - FOUND DURING MBV INSPECTION OF THE AIRCRAFT, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE BELOW SRM LIMITS AFTE R REMOVAL OF CORROSION. REPAIRED CORRODED AREA, WORK DONE IAW EMB145 SRM 1142 REV 12, 53-21-10 PARA 2 PAGE 201, 202 AND FIG 201 SHEET 1. (M) 2 L 7 2 4F RT T00011AT 2001072500525 20010725 00525 EU 2001 7 25 SIMA200117106 1 20010620 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 905AE 340B319 DFW - FLT 3752 - FOUND OVERHEAD EMERGENCY LIGHT 11A INOPERATIVE MEL 3313. (M) 2 L 7 2 4T RT A52EU 2001072500526 20010725 00526 EU 2001 7 25 SIMA200117110 1 20010620 A 3320 CONNECTOR AEROSP ATR72 ATR72212A 8680902 EU CABIN LOOSE A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 541AT 541 TUL - FLT 3828 - BURNING ODOR OBSERVED BY F/A IN CABIN AFTER ENGINE START. FOUND BALLAST CONNECTOR AT OVERHEAD BIN 3 A/ B LOOSE. TIGHTENED SAME. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 2001072500527 20010725 00527 EU 2001 7 25 SIMA200117203 1 20010621 A 3350 FST5X201A BALLAST AEROSP ATR72 ATR72212 EU CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 288AM 288 SGF - FLT 3858 - FOUND CABIN OVERHEAD EMERGENCY LIGHT BY GALLEY INOPERATIVE. REMOVED AND REPLACED FUSELAGE AT EMERGENCY LIGHT BALLAST IAW AMM. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 2001072500528 20010725 00528 SO 2001 7 25 SIMA200117401 1 20010623 A 3350 LIGHT EMB 145 EMB145LR SO CABIN MALFUNCTIONED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 647AE 145222 MSN - FLT 3426 - FOUND FLOOR EMERGENCY PROX LIGHTS FROM ROWS 12 AFT CAME ON THEN EXTINGUISHED. PERFORMED OPS CHECK TO S YSTEM IAW AMM, OPS CHECK GOOD. NO DEFECTS NOTED. (M) 2 L 7 2 4T RT T00011AT 2001072500529 20010725 00529 EU 2001 7 25 SIMA200117404 1 20010623 A 5101 STRUCTURE AEROSP ATR42 ATR42300 8680920 EU FUSELAGE VIBRATION A SIMA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 21 971NA 017 MIA - FLT 5369 - VERY STRONG VIBRATION NOTICED AFTER GEAR RETRACTION, MAX SPEED 160KIAS. RETURNED TO MIA. PERFORMED NO SE LANDING GEAR FORWARD DOOR PRELOAD CHECK AND GEAR EXTENSION AND RETRACTION IAW AMM. FOUND DOORS FLUSH AND IN CONTACT WITH STOPS. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 2001072500530 20010725 00530 EU 2001 7 25 SIMA200117501 1 20010624 A 3350 LIGHT AEROSP ATR72 ATR72212 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 355AT 355 MIA - FLT 5375 - EMERGENCY FLOOR LIGHTS INOPERATIVE AT 16B MEL. (M) 2 H 7 2 4T RT A53EU 2001072500531 20010725 00531 EU 2001 7 25 SIMA200117502 1 20010624 A 3350 2LA00511500 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 298AE 340B298 JFK - FLT 5046 - FOUND EMERGENCY OVERHEAD LIGHTS AT 9A INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AT 9A IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001072500532 20010725 00532 SO 2001 7 25 SIMA200117806 1 20010627 A 5330 SKIN EMB 145 EMB145 SO FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 640AE 145183 ABI - DURING MBV INSPECTION OF THE AIRCRAFT, TWO DENTS WERE DISCOVERED BETWEEN FRAMES 65 AND 66, AND BETWEEN STRINGERS 1 9L AND 21L. REPAIRED DAMAGE IAW EMB145 SRM (1142 REV 12) 53-31-01 PARA 2, PAGE 201, 202, 203, AND PAGE 283 FIG 201 SHEE T 1. (M) 2 L 7 2 4F RT T00011AT 2001072500533 20010725 00533 SO 2001 7 25 SIMA200117807 1 20010627 A 5315 FLOORBEAM EMB 145 EMB145 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 640AE 145183 ABI - DURING MBV INSPECTION, THE CENTER GALLEY FLOORBEAM WAS FOUND TO BE BELOW SRM LIMITS AT FRAME 20 AND 22 AFTER THE R EMOVAL OF CORROSION. REPAIRED CORRODED AREA IAW EMB145 REPAIR STATEMENT GST-2108/01 AND STANDARD SRM (145/1142 REV 10) PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2001072500534 20010725 00534 SO 2001 7 25 SIMA200117808 1 20010627 A 5315 FLOORBEAM EMB 145 EMB145 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 604AE 145183 ABI - DURING MBV INSPECTION OF THE AIRCRAFT, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE BELOW SRM LIMITS AFTER THE REMOVAL OF CORROSION. REPAIRED AREA IAW EMB145 SRM (1141 REV 12) 53-21-10 PARA 2, PAGE 201, 202 AND FIG 201 SHEET. (M) 2 L 7 2 4F RT T00011AT 2001072500535 20010725 00535 SO 2001 7 25 SIMA200117809 1 20010627 A 2520 PLATE EMB 145 EMB145 SO CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 640AE 145183 ABI - DURING AN MBV INSPECTION, THE FORWARD DIGITAL WAS FOUND BELOW SRM LIMITS AFTER REMOVAL OF CORROSION. REPAIRED COR RODED AREA IAW EMB145 REPAIR STATEMENT GST-2084-/01 AND STANDARD SRM 145/1142 REV 10 PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2001072500536 20010725 00536 EU 2001 7 25 SIMA396154 1 20010603 A 3320 SOCKET SAAB SF340 340B 7860101 EU LAVATORY BURNED A SIMA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 21 396AE 340B396 LFT - FLT 3279 - FOUND LAVATORY SMOKE LIGHT ILLUMINATED IN FLIGHT. FOUND BURNED LIGHT SOCKET, MEL'D LAVATORY. (M) 2 L 7 2 4T RT A52EU 2001072500537 20010725 00537 NE 2001 7 25 SOK2001F00000 2 20010520 A 7261 HELICOIL BOEING 737 7372L9 1384497 NM PWA JT8 JT8D17A 52049 NE NR 2 ENGINE FAULTY A SOKF E ENGINE SHUTDOWN J WARNING INDICATION LD LANDING 1 SO 23 281LF 22701 702719 CCS - FLT LR611 - DURING LANDING, ENGINE NR 2 WAS SHUTDOWN DUE TO LOSS OF OIL AND LOW OIL PRESSURE LIGHT. AT CCS STATIO N, FOUND THAT AN OIL PRESSURE FITTING CORRESPONDING TO THE OIL BYPASS PRESSURE SWITCH WAS LEAKING, CHANGED HELICOIL AT T HIS FITTING AS PER PWA MM 79-23-1 AND PWA MM 72-00 PAGE 518 DS PAR 3. ENGINE TEST WAS PERFORMED AS PER BMM 71-00. TEST RESULT WAS SATISFACTORY, THE AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 2001072500538 20010725 00538 NM 2001 7 25 TSAA0124078 1 20010620 A 2410 731753 CSD BOEING 737 7372X6C 1384552 NM NR 1 ENGINE FAILED A TSAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 13 817AL 39735 FLT 915 - HNL-LIH - DURING FLIGHT, THE LOW OIL PRESSURE LIGHT CAME ON AND THE NR 1 ENGINE CSD GENERATOR WAS DISCONNECTED AQ MAINTENANCE WAS CONTACTED AND ADVISED PILOT TO RETURN TO HNL. AIRCRAFT RETURNED TO HNL AND BLOCKED IN T 0154 HOURS WITH NO FURTHER INCIDENT. THE CSD WAS REMOVED AND REPLACED PER MM 24-11-11 AND FORM M137. LEAK AND OPERATIONS CHECK W AS GOOD WITH NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001072500539 20010725 00539 NM 2001 7 25 TSAA0132070 1 20010613 A 3260 189915 DOWNLOCK SENSOR BOEING 737 7372Y5 1384554 NM RT MLG FAILED A TSAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 WP 13 810AL 24031 INBOUND TO HNL FROM LIH - REPORTED TO MAINTENANCE CONTROL OF THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ON IN-FLIGHT. CAP TAIN PERFORMED FLYBY FOR TOWER TO CHECK GEARS DOWN WHILE F/O ALSO CHECKED BY GOING TO BACK OF AIRCRAFT. GEARS RECYCLED ONCE AND LIGHT STILL ON. TOWER ADVISED CAPTAIN GEARS SEEM TO BE DOWN AND EVERYTHING LOOKS OK. CAPTAIN LANDED AIRCRAFT WITH NO FURTHER INCIDENT. T/S TO THE RIGHT DOWNLOCK SENSOR THAT WAS REPLACED AND OPERATIONALLY CHECKED OK PER MM 32-61- 31, PAGE 401-404. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4U RT A16WE 2001072500540 20010725 00540 NM 2001 7 25 TSAA0153075 1 20010615 A 5330 6520722 BEAR STRAP BOEING 737 7372M6C 1384708 NM FUSELAGE CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 DISCOVERED CORROSION AT FORWARD CARGO DOOR BEAR STRAP (AFT UPPER CORNER). (M) 2 L 7 2 4F RT A16WE 2001072500541 20010725 00541 NM 2001 7 25 TSAA0153076 1 20010615 A 5730 6545407 SKIN BOEING 737 7372M6C 1384708 NM RT WING CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 FOUND .62 INCH CRACK DURING HEAVY CHECK AT RIGHT UPPER WING SKIN AFT EDGE BETWEEN WBL 157 AND WBL 183.4. (M) 2 L 7 2 4F RT A16WE 2001072500542 20010725 00542 NM 2001 7 25 TSAA0153079 1 20010619 A 5330 654577589 SKIN BOEING 737 737230 NM FUSELAGE DAMAGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 820AL 22138 AIRCRAFT SKIN AND FRAME DAMAGED AT BS 847 THROUGH BS 887, STRINGER 25L THROUGH STRINGER 25R. REMOVED DAMAGED AREA ,PERF ORMED HFEC INSPECTION AROUND CUT OUT NO DEFECTS NOTED. REPAIRED STRINGER S27L AT BS 847 IAW SRM 53-10-3 FIG INSTALLATIO N OF REPAIR DOUBLER COMPLETED IAW SRM 53-30-3 FIG 28. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001072500543 20010725 00543 NM 2001 7 25 TSAA0157067 1 20010605 A 5753 BUSHING BOEING 737 737282C 13844AU NM T/E FLAP ELONGATED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 826AL 23051 DISCOVERED NR 2 ENGINE AND NR 3 FLAP TRACK ASSY MOVING LATERALLY DURING SERVICE CHECK. FURTHER INVESTIGATION REVEALED C ORRODED MOUNT BOLT WASHER ASSY AND ELONGATED BUSHING. FABRICATED BUSHINGS PER BOEING DRAWING 65-46429-19. INSTALLED BU SHINGS , CLEANED AND TREATED ALL EXPOSED AREAS. REINSTALLED NR 3 FLAP TRACK ASSEMBLY AND NR 2 ENGINE. RECEIVED 8110-3 APPROVAL IAW ECO 3225. A/C RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001072500544 20010725 00544 NM 2001 7 25 TSAA0157068 1 20010601 A 5730 86210151 SKIN BOEING 737 737209 NM RT WING CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 827AL 23913 DISCOVERED CORROSION AT RIGHT WING LOWER SURFACE WS 581.5, BLENDOUT TO REMOVE ALL CORROSION, OBTAINED A SURFACE OF 125 M ICROINCHES RADIUS, CONFIRMED COMPLETE REMOVAL OF CORROSION BY 10 BY GLASS VISUAL INSPECTION, FLAP PEEN REWORKED AREAS PE R SOPM 20-10-03, APPLIED ALODINE, PRIMER AND ENAMEL TO ALL EXPOSED SURFACES, IAW ECO 3091R4. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4F RT A16WE 2001072500545 20010725 00545 NM 2001 7 25 UHLA003491 1 20010519 A 5210 85210181003 CABLE DHAV DHC8 DHC8301 NM PAX DOOR BROKEN A UHLA K NONE O OTHER TX TAXI/GRND HDL 1 NE 03 803SA 221 FLT 480 - BUF-TTN - ON ARRIVAL, REAR LOWER PASSENGER DOOR SUPPORT CABLE FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED REAR LOWER DOOR CABLE AND RETURNED AIRCRAFT TO SERVICE. REF AMR/WO 5441. (M) 2 H 7 2 4T RT A13NM 2001072500546 20010725 00546 EA 2001 7 25 UHLA013471 1 20010516 A 2120 UNKNOWN DHAV DHC8 DHC8311 1386006 EA COCKPIT ODOR A UHLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NE 03 806SA 279 FLT 202 - TTN-BED - DURING CLIMB-OUT, A STRONG HOT RUBBER ODOR WAS NOTICED IN THE CABIN AND COCKPIT. CREW RETURNED TO T TN WITHOUT ANY PROBLEMS. MAINTENANCE PERFORMED VISUAL INSPECTION AND OPS CHECK OF BLEED AIR SYSTEM AND ENGINE GROUND RU NS IAW DHMM 21-11-00 AND 71-00-00 AND WAS UNABLE TO DUPLICATE DISCREPANCY. PERFORMED MAINTENANCE CHECK FLIGHT THAT WAS S ATISFACTORY. AIRCRAFT RELEASE TO SERVICE. (M) 2 H 7 2 4T RT A13NM 2001072500547 20010725 00547 NM 2001 7 25 UIEA01058 1 20010530 A 5320 65B15034U19 FITTING BOEING 747 7472D7B 1384803 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 65332 12777 22472 DURING HFEC INSPECTION PER SB 53A2390R1, FOUND BS 1480 L/S SPLICE PLATE FITTING HOLES NR 9 AND 10 WITH CRACK INDICATIONS . REMOVED LONGERON EXTENSION STRAP. REAMED HOLES TO REMOVE CRACKS. CONFIRMED NO CRACKS. FABRICATED BUSHINGS AND INST ALLED PER STANDARD PRACTICES IAW 747-53A2390R1 TO NOMINAL SIZE OF .5625 INCH DIAMETER. REINSTALLED LONGERON EXTENSION S TRAP. REPEAT INSPECTION INTERVAL REDUCED BY 6000 CYCLES TO A THRESHOLD OF 12000 INITIAL AND 3500 REPETITIVE THEREAFTER. (M) 2 L 7 4 4F RT A20WE 2001072500548 20010725 00548 NM 2001 7 25 UIEA01059 1 20010530 A 5412 65B9410753 BULKHEAD BOEING 747 7472D7B 1384803 NM NR 4 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 65332 12777 22472 DURING INSPECTION OF NR 4 PYLON, FOUND THE REAR ENGINE MOUNT BULKHEAD UPPER T-CHORD L/S CRACKED (R/S PREVIOUSLY REPAIRED ). TRIMMED CRACK AREA AWAY. OVERSIZED HOLES IN AFFECTED AREA. HFEC INSPECTED HOLES TO ENSURE CRACK FREE AREA. NO CRA CKS FOUND. INSTALLED OVERSIZED FASTENERS PER SRM 51-30-02 AND 51-30-05. REPAIR IS INTERIM REPAIR AND MUST BE VISUALLY INSPECTED EVERY C-CHECK NOT TO EXCEED 18 MONTHS. (M) 2 L 7 4 4F RT A20WE 2001072500549 20010725 00549 NM 2001 7 25 USAA0100690 1 20010517 A 5710 STRUCTURE BOEING 737 737301 1384611 NM LT WING CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND MATING SURFACE CORRODED, 1 INCH BY 6 INCH AREA, LEFT WING 7217L OPENING. CORROSION LEVEL 1, TASK NR C57-300 -01. CLEANED CORROSION, ROTO PEENED, TREATED PER SRM 57-20-01, PAGES 213-216. (M) 2 L 7 2 4F RT A16WE 2001072500550 20010725 00550 NM 2001 7 25 USAA010594 1 20010531 A 5510 HINGE FITTING BOEING 737 7372B7 1384560 NM HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 284AU 47733 23131 CLT - FOUND STAB HINGE FITTING CORRODED APPROXIMATELY 1.5 SQUARE INCH AREA, RT CENTER SECTION FORWARD LOWER ATTACH INBOA RD CLEVIS, OUTBOARD FACE. CORROSION REMOVED, LUG REWORKED PER EA 69577. (M) 2 L 7 2 4F A16WE 2001072500551 20010725 00551 NM 2001 7 25 USAA010595 1 20010531 A 5510 HINGE FITTING BOEING 737 7372B7 1384560 NM HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 284AU 47733 23131 CLT - FOUND STAB HINGE FITTING CORRODED APPROXIMATELY 1 SQUARE INCH AREA, RIGHT CENTER SECTION, REAR SPAR, LOWER ATTACH POINT LUG. CORROSION REMOVED, LUG REWORKED PER EA 69577. (M) 2 L 7 2 4F A16WE 2001072500552 20010725 00552 NM 2001 7 25 USAA010598 1 20010601 A 5312 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 284AU 47733 23131 CLT - FOUND BULKHEAD SKIN DENTED 1 INCH BY .5 INCH BY .005 INCH DEEP, BS 1016 PRESSURE BULKHEAD, LBL 10 INCHES FROM CENT ER. INSTALLED DOUBLER PER SRM 53-10-4 FIG 3. (M) 2 L 7 2 4F A16WE 2001072500553 20010725 00553 NM 2001 7 25 CA010704023 1 20010604 A 2720 251T32251 SPRING BOEING BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E437 54555 NE CENTER BROKEN W K NONE O OTHER NR NOT REPORTED 1 CA (CAN) RUDDER PEDAL HAS A LACK OF NORMAL RESISTANCE WHEN DISPLACED. INSPECTION FOUND THAT ONE OF THE FEED BACK SPRINGS WA S BROKEN, SPRING WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2001072500554 20010725 00554 NE 2001 7 25 CA010706002 2 20010423 A 7200 LK41525 LINE RROYCE RB21122B LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B NE AT CLAMP ATTACH BROKEN W O OTHER O OTHER CL CLIMB 1 CA 10459 (CAN) AIRCRAFT DIVERTED TO YMX DUE HIGH EPR INDICATION INCREASING WITH ALTITUDE WITH ALL OTHER PARAMETERS NORMAL. MAINTE NANCE FOUND P1 LINE BROKEN AT CLAMP ATTACHMENT BETWEEN PROBE AND FFR. LINE REPLACED. ENGINE RUN C/O A/C RETURNED TO SERV ICE. 2 L 7 3 4F 4 F A23WE E12EU 2001072500559 20010725 00559 EU 2001 7 25 CA010713022 1 20010619 A 5753 FLAP AIRBUS AIRBUS 320 A320212 EU CFMINT CFM56 CFM565A3 NE FLAP FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) AFTER TAKE OFF FLAP JAMMED AT #1 POSITION. FLIGHT CREW DECLARED EMERG AND A/C LANDED WITH NO INCIDENTS. FLAP RIGGI NG WAS ACCOMPLISHED AND A/C RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A28NM E29NE 2001072500561 20010725 00561 NM 2001 7 25 USAA010599 1 20010601 A 5320 ANGLE BOEING 737 7372B7 1384560 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 284AU 47733 23131 CLT - FOUND Z-ANGLE CORRODED 1 INCH AREA, BS 360 LEFT. REMOVED DAMAGE, INSTALLED DOUBLER PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2001072500562 20010725 00562 NM 2001 7 25 USAA010600 1 20010601 A 3210 FITTING BOEING 737 7372B7 1384560 NM LT MLG CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 284AU 47733 23131 CLT - FOUND LEFT MLG BEAM FITTING CRACKED .125 INCH, .25 INCH FROM FASTENER HOLE TO EDGER ABOVE CUTOUT. TEMPORARY REPAI R PER TYPICAL REPAIR 57-40-10 PER EA 69608. (M) 2 L 7 2 4F A16WE 2001072500563 20010725 00563 NM 2001 7 25 USAA010601 1 20010601 A 5320 SPLICE BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 284AU 47733 23131 CLT - FOUND STRINGER SPLICE HAS 1 INCH CRACK, BS 360 STRINGER 15L. REMOVED DAMAGE SPLICE, INSTALLED NEW SPLICE PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2001072500564 20010725 00564 NM 2001 7 25 USAA010615 1 20010605 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 44350 23231 CLT - FOUND FUSELAGE SKIN CRACKED APPROXIMATELY .1875 INCH, BS 887, STRINGER 23R. DAMAGE REMOVED, INSTALLED REPAIR DOUB LE WITH FILLER PER SRM 53-00-01, FIG 227. (M) 2 L 7 2 4F RT A16WE 2001072500565 20010725 00565 NM 2001 7 25 USAA010616 1 20010605 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 284AU 47733 23131 CLT - FOUND FUSELAGE SKIN CRACKED APPROXIMATELY .25 INCH, BS 327 STRINGER 17R, FORWARD GALLEY SERVICE DOOR CUTOUT, AFT L OWER CORNER. DAMAGE REMOVED, INSTALLED REPAIR FILLER WITH DOUBLER AND TRIPLER PER SRM 53-30-03, FIG 26. (M) 2 L 7 2 4F A16WE 2001072500566 20010725 00566 NM 2001 7 25 USAA010617 1 20010407 A 5311 FRAME BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 270AU 22882 CLT - SIDE CHORD ANGLES HAVE CRACKS 2 INCHES ON LEFT SIDE, 1.75 INCH ON RIGHT SIDE, BS 178 LEFT AND RIGHT SIDE, BETWEEN WL 185 AND WL 216. DAMAGE REMOVED, SPLICED IN NEW SIDE CHORD SECTION P/N 651630086/87 PER E 5300V157. (M) 2 L 7 2 4F A16WE 2001072500567 20010725 00567 NM 2001 7 25 USAA010618 1 20010407 A 5320 672038501 INTERCOSTAL BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 270AU 22882 CLT - FOUND INTERCOSTALS WITH TWO CRACKS, 1.250 INCH ON RIGHT INTERCOSTAL AND 1 INCH ON LEFT, BS 178 WL 195, LEFT AND RI GHT SIDE P/N 672038501 AND 502. REMOVED AND REPLACED INTERCOSTALS PER EO 5300V157. (M) 2 L 7 2 4F A16WE 2001072500568 20010725 00568 NM 2001 7 25 USAA010619 1 20010407 A 5312 BULKHEAD BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 270AU 49760 22882 CLT - FOUND WEB, CLIP, GUSSET CRACKED .5 INCH, BS 178, WL 207. REMOVED AND REPLACED WEB, CLIP, AND GUSSET PER EO 5300V1 57. (M) 2 L 7 2 4F A16WE 2001072500569 20010725 00569 NM 2001 7 25 USAA010621 1 20010608 A 5320 WEB BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 37497 23879 CLT - FOUND FLOOR WEB CRACKED .25 INCH, BS 179, LBL 27 WL 207. REMOVED AND REPLACED WEB PER EO 5300V157. (M) 2 L 7 2 4F RT A16WE 2001072500570 20010725 00570 NM 2001 7 25 USAA010622 1 20010608 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 268AU 52489 22880 CLT - FOUND FUSELAGE SKIN HAS APPROXIMATELY .5 INCH CRACK, BS 380, FUSELAGE BELLY S-28L, COOLING DUCT CUTOUT. DAMAGE RE MOVED, INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-30-04. (M) 2 L 7 2 4F A16WE 2001072500571 20010725 00571 NM 2001 7 25 USAA010623 1 20010608 A 5320 WEB BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 23879 CLT - FOUND FLOOR WEB CRACKED .25 INCH, BS 179, RBL 27, WL 207. REMOVED AND REPLACED FLOOR WEB PER EO 5300V157. (M) 2 L 7 2 4F RT A16WE 2001072500572 20010725 00572 NM 2001 7 25 USAA010624 1 20010606 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 529AU 40446 24411 CLT - FOUND FUSELAGE SKIN CRACKED 1.5 INCH, BS 727D, STRINGER 23L. DAMAGE REMOVED, DOUBLER INSTALLED PER TYPICAL REPAIR 53-60-03. (M) 2 L 7 2 4F RT A16WE 2001072500573 20010725 00573 NM 2001 7 25 USAA010625 1 20010608 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 44706 23380 CLT - FOUND FUSELAGE SKIN CRACKED APPROX .25 INCH, BS 379, BELLY, E/E COOLING OUTLET. INSTALLED DOUBLER PER TYPICAL REP AIR 53-30-07. (M) 2 L 7 2 4F RT A16WE 2001072500574 20010725 00574 WP 2001 7 25 USAA010644 1 20010530 A 5311 BELTFRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 823US 48560 49142 PPIT - FOUND BELTFRAME CORRODED 24 INCHES BY 1 INCH, AFT SIDE OF BELTFRAME AT STATION 1309 FROM LONGERON 28 LEFT. CORRO SION LEVEL 1, TASK NR C57-53300. REMOVED CORROSION, ACCOMPLISHED FORMER SPLICE REPAIR PER SRM 53-03 FIG 3 FIG 2A. (M) 2 L 7 2 4F A6WE 2001072500575 20010725 00575 NM 2001 7 25 USAA010652 1 20010612 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND FLOORBEAM CORRODED APPROXIMATELY 3 SQUARE INCH AREA, BS 312, RBL 8. REMOVED AND REPLACED T-CAP SECTION PER SRM 53-10-51 AND 51-20-01. (M) 2 L 7 2 4F RT A16WE 2001072500576 20010725 00576 NM 2001 7 25 USAA010655 1 20010612 A 5320 ANGLE BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND Z-ANGLE CORRODED 60 INCHES BY 2 INCHES, BS 947 TO 1006, RBL 50. REMOVED AND REPLACED Z-ANGLE PER SRM 51-10- 02. (M) 2 L 7 2 4F RT A16WE 2001072500577 20010725 00577 NM 2001 7 25 USAA010656 1 20010612 A 5320 ANGLE BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND Z-ANGLE CORRODED, BS 947 TO 1006, LBL 50. REMOVED AND REPLACED Z-ANGLE PER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 2001072500578 20010725 00578 NM 2001 7 25 USAA010658 1 20010612 A 5314 KEELBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND KEEL BEAM CORRODED .25 INCH BY .050 INCH, BS 710, LBL 6.5. DAMAGED REMOVED, INSTALLED REPAIR STRAP PER EA 6 9728 AND SRM 53-60-12. (M) 2 L 7 2 4F RT A16WE 2001072500579 20010725 00579 NM 2001 7 25 USAA010659 1 20010612 A 5314 KEELBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND KEEL BEAM APPROX 6 SQUARE INCH AREA, CORROSION AT SCREW HOLES, BS 663-720, RBL 6.5. DAMAGED REMOVED, INSTAL LED REPAIR STRAP PER EA 69728 AND SRM 53-60-12. (M) 2 L 7 2 4F RT A16WE 2001072500580 20010725 00580 NM 2001 7 25 USAA010660 1 20010612 A 5320 WEB BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND HORIZONTAL WEB WITH TWO 1 INCH CRACKS ON BOTH LEFT AND RIGHT, BS 180, WL 207, RBL 24 AND LBL 24, FLOOR STRUC TURE. REMOVED AND REPLACED WEBS, LEFT AND RIGHT, PER EO 5300V157. (M) 2 L 7 2 4F RT A16WE 2001072500581 20010725 00581 NM 2001 7 25 USAA010661 1 20010612 A 5311 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND SIDE CHORDS HAVE TWO CRACKS, 1 INCH ON RIGHT SIDE, 3 INCHES ON LEFT SIDE, BS 178 WL 207. REMOVED DAMAGE, SP LICED IN NEW SIDE CHORD ANGLE PER EO 5300V157. (M) 2 L 7 2 4F RT A16WE 2001072500582 20010725 00582 NM 2001 7 25 USAA010669 1 20010613 A 5313 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND 18A SHELF CRACKED .5 INCH, RIGHT WHEEL WELL, BS 725, RBL 62. REMOVED AND REPLACED 18A SHELF PER EA 69680, A ND BOEING DRAWING NR 65-46877. (M) 2 L 7 2 4F RT A16WE 2001072500583 20010725 00583 NM 2001 7 25 USAA010670 1 20010613 A 5313 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND 18A SHELF CRACKED .5 INCH, LEFT WHEEL WELL, BS 725, LBL 62. REMOVED AND REPLACED 18A SHELF PER EA69680 AND SB 737-53-1170. (M) 2 L 7 2 4F RT A16WE 2001072500584 20010725 00584 NM 2001 7 25 USAA010674 1 20010613 A 5320 ATTACH ANGLE BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND WEB ATTACH ANGLE CRACKED 1 INCH, BS 291, BETWEEN S10R AND S11R. REMOVED AND REPLACED WEB ATTACH ANGLE. (M) 2 L 7 2 4F RT A16WE 2001072500585 20010725 00585 NM 2001 7 25 USAA010676 1 20010613 A 5414 SKIN BOEING 737 737301 1384611 NM NR 1 PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND PYLON/STRUT SKIN CRACKED .75 INCH, NR 1 ENGINE STRUT, PANEL NR 5727 OPENING, OUTBOARD AFT RADIUS. STOP DRIL LED CRACK, INSTALLED DOUBLER PER TR 54-30-07. (M) 2 L 7 2 4F RT A16WE 2001072500586 20010725 00586 NM 2001 7 25 USAA010680 1 20010615 A 5312 BULKHEAD BOEING 737 737301 1384611 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 23231 CLT - FOUND BULKHEAD WEB DENTED 3 INCHES BY .5 INCH, BS 1016 WL 156, RBL 51. DAMAGED REMOVED, INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-80-08, FIG 201. (M) 2 L 7 2 4F RT A16WE 2001072500587 20010725 00587 NM 2001 7 25 USAA010686 1 20010427 A 5230 WEB BOEING 737 737301 1384611 NM CARGO DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND WEB PANEL CORRODED 12 INCHES BY 48 INCHES AT NUT PLATE, AFT CARGO DOOR WEB PLATE. CORROSION LEVEL 1, TASK C 53-202-01. REMOVED CORRODED WEB PANEL AND REPLACED WITH NEW PANEL PER DRWG NR 65-47957. (M) 2 L 7 2 4F RT A16WE 2001072500588 20010725 00588 NM 2001 7 25 USAA010688 1 20010505 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND TOP FLANGE ENTIRE LENGTH OF FLOORBEAM CORRODED 1 INCH BY 2 INCHES, FLOORBEAM STATION 986.5. CORROSION LEVEL 1, TASK C53-107-02. TOP SECTION OF FLOORBEAM REPLACED ENTIRE LENGTH WITH BOEING KIT NR 6132505 PER TYPICAL REPAIR 53-6 0-01. (M) 2 L 7 2 4F RT A16WE 2001072500589 20010725 00589 EU 2001 7 25 C2XA01BT129 1 20010725 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU FUSELAGE FAULTY A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 15827 175 BTV---CO2930, DURING 4A INSPECTION MAINTENANCE FOUND FORWARD CABIN EMERGENCY LIGHT INOPERATIVE DURING SYSTEM CHECK. REM OVED AND REPLACED EMERGENCY BATTERY POWER PACK AT 3WL IAW ATR 42 CMM 33-51-21. OPS.CHECKED GOOD. 2 H 7 2 4T RT A53EU 2001072500590 20010725 00590 NM 2001 7 25 USAA010689 1 20010517 A 5320 WEB BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND WEB CORRODED 2 INCHES BY 3 INCHES, BS 947.5 TO 986.5, CORROSION LEVEL 1, TASK NR C53-202-01. REMOVED CORROS ION, TREAT, PRIME, FABRICATE NEW SECTIONS AND INSTALLED. (M) 2 L 7 2 4F RT A16WE 2001072500591 20010725 00591 NM 2001 7 25 USAA010691 1 20010517 A 5710 STRUCTURE BOEING 737 737301 1384611 NM LT WING CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND MATING SURFACE CORRODED 1 INCH BY 3 INCHES, LT WING 7214L. CORROSION LEVEL 1, TASK NR C57-300-01. CLEANED CORROSION, ROTO PEENED, TREATED PER SRM 57-20-01 PGS 213-216. (M) 2 L 7 2 4F RT A16WE 2001072500592 20010725 00592 NM 2001 7 25 USAA010692 1 20010517 A 5710 STRUCTURE BOEING 737 737301 1384611 NM LT WING CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND MATING SURFACE CORRODED 1 INCH BY 5 INCH AREA, LT WING 7210L OPENING. CORROSION LEVEL 1, TASK NR C57-300-01 . CLEANED CORROSION ROT PEENED, TREATED PER SRM 57-20-01 PAGES 213-216. (M) 2 L 7 2 4F RT A16WE 2001072500593 20010725 00593 NM 2001 7 25 USAA010693 1 20010517 A 5710 STRUCTURE BOEING 737 737301 1384611 NM LT WING CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND MATING SURFACE 1 INCH BY 4 INCH AREA OF CORROSION, LT WING 7202L OPENING. CORROSION LEVEL 1 TASK NR C57-300 -01. CLEANED CORROSION, ROTO PEENED, TREATED PER SRM 57-20-01 PAGES 213-216. (M) 2 L 7 2 4F RT A16WE 2001072500594 20010725 00594 NM 2001 7 25 USAA010694 1 20010505 A 5320 WEB BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND WEB PANEL CORRODED 1 INCH BY 10 INCHES, STATION 956.5 TO 967. CORRODED LEVEL 1, TASK NR C53-202-01. MFG WE B PANEL FROM STATION 947.5 TO 967 PER SRM 51-20-01/51-40-01/51-30-01/51-20-05. (M) 2 L 7 2 4F RT A16WE 2001072500595 20010725 00595 NM 2001 7 25 USAA010695 1 20010517 A 5710 STRUCTURE BOEING 737 737301 1384611 NM LT WING CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND MATING SURFACE 1 INCH BY 3 INCH, LT WING 7213L OPENING. CORROSION LEVEL 1, TASK NR C57-300-01. CLEANED COR ROSION, ROTO PEENED, TREATED PER SRM 57-20-01 PAGES 213-216. 2 L 7 2 4F RT A16WE 2001072500596 20010725 00596 NM 2001 7 25 USAA010696 1 20010517 A 5710 STRUCTURE BOEING 737 737301 1384611 NM LT WING CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND CORROSION 1 INCH BY 4 INCH AREA, LT WING 7204L OPENING. CORROSION LEVEL 1, TASK NR C57-300-01. CLEANED COR ROSION, ROTO PEENED, TREATED PER SRM 57-20-01 PAGES 213-216. (M) 2 L 7 2 4F RT A16WE 2001072500597 20010725 00597 NM 2001 7 25 USAA010697 1 20010517 A 5710 STRUCTURE BOEING 737 737301 1384611 NM LT WING CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND CORROSION 1 INCH BY 6 INCH, LT WING 7211 OPENING. CORROSION LEVEL 1, TASK NR C53-300-01. CLEANED CORROSION , ROTO PEENED, TREATED PER SRM 57-20-01 PAGE 213-216. (M) 2 L 7 2 4F RT A16WE 2001072500598 20010725 00598 SW 2001 7 25 20010606CW009 1 20010423 A 6700 071124201 SWITCH BELL 430 430 1182150 SW SLAVE CONTROL INOPERATIVE E EGRA O OTHER O OTHER NR NOT REPORTED 1 EA 17 993PA 753 49050 SLAVE CONTROL ASSEMBLY CCW/CW SWITCH INOPERATIVE.SWITCH CCW/CW PN 071124201 CORRECTIVE ACTION: REMOVED AND REPLACED SL AVE CONTROL ASSEMBLY. 1 G 7 2 3U RT H9SW 2001072500599 20010725 00599 NM 2001 7 25 2001F00138 1 20010618 A 3350 86210144 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, FOUND LEFT OVERWING EMERGENCY EXIT IDENTIFIER FAILED RECON TEST. REMOVED AND REPLACED R EMOTE LIGHT ASSEMBLY AND REMOTE ASSEMBLY BATTERY THEN EXIT LIGHTS OPERATED NORMAL. REF ASAA0110375. (M) 2 L 7 2 4F RT A16WE 2001072500600 20010725 00600 NM 2001 7 25 ASAA01040053 1 20010410 A 5320 65176880175 SILL BOEING 737 7374Q8 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 779AS 25111 PAE - DURING SI CHECK, FOUND CORROSION ON MOPSILL AT BS 344-350, LBL 56 AND WL 208. REMOVED AND REPLACE PER SRM 51-40-0 5. (M) 2 L 7 2 4F RT A16WE 2001072500601 20010725 00601 NM 2001 7 25 ASAA0110119 1 20010310 A 5210 507945178 DOOR BOEING 737 737290C 138448V NM L1 LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 ANC - DURING MAINTENANCE CHECK, FOUND L1 DOOR DIFFICULT TO OPEN. CLEANED AND LUBED L1 DOOR AND DOOR OPENED NORMALLY. ( M) 2 L 7 2 4F A16WE 2001072500602 20010725 00602 NM 2001 7 25 ASAA0110168 1 20010331 A 5210 6529994 GUIDE BOEING 737 737210C 1384459 NM L1 DOOR LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 JNU - DURING MAINTENANCE CHECK, FOUND L1 DOOR DIFFICULT TO OPEN. LUBED GUIDE ARM AND DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2001072500603 20010725 00603 NM 2001 7 25 ASAA0110271 1 20010503 A 5210 6529994 GUIDE BOEING 737 737210C 1384459 NM R1 DOOR OUT OF ADJ A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 ANC - DURING MAINTENANCE CHECK, FOUND R1 DOOR DIFFICULT TO OPEN. ADJUSTED GUIDE ARM AND DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2001072500604 20010725 00604 NM 2001 7 25 ASAA0110314 1 20010531 A 5314 65621252 KEELBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND KEEL BEAM AT BS 525-530, STRINGER 28R CORRODED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2001072500605 20010725 00605 NM 2001 7 25 ASAA0110315 1 20010531 A 5315 65671404 FLOORBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND CHORD AT BS 668-670, RBL 25 CORRODED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2001072500606 20010725 00606 NM 2001 7 25 ASAA0110317 1 20010602 A 5313 6552928594 STRINGER BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER 21L AT BS 810, CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001072500607 20010725 00607 NM 2001 7 25 ASAA0110375 1 20010618 A 3350 873100232 SIGN BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, FOUND LEFT OVERWING EMERGENCY EXIT IDENTIFIER FAILED RECON TEST. REMOVED AND REPLACED R EMOTE LIGHT ASSEMBLY AND REMOTE ASSEMBLY BATTERY THEN EXIT LIGHTS OPERATED NORMAL. (M) 2 L 7 2 4F RT A16WE 2001072500608 20010725 00608 NM 2001 7 25 ASAA0140035 1 20010417 A 5320 6517688125 SILL BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 786AS 24795 SEA - DURING 9C INSPECTION, FOUND CREASE BEAM CORROSION ON FORWARD ENTRY DOOR SILL AT BS 316 TO BS 343 AND FROM WATERLIN E 208.1 LEFT TO BUTTOCK LINE 62 LEFT HAND. REPAIRED IAW ASA EA 5310-01922 AND SRM. (M) 2 L 7 2 4F RT A16WE 2001072500609 20010725 00609 NM 2001 7 25 UPS01236386 1 20010705 A 5280 FRAME BOEING 727 72727C 138400J NM LT MLG DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 910UP 19117 INSPECTION TYPE: C, LT MLG WING DOOR (OUTER HALF) O/B DOOR FRAME AFT CORNER CRACKED. REPAIR CARRIED OUT IAW SRM 51- 20-2 & SRM 51-40-3 2 L 7 3 4F A3WE 2001072500610 20010725 00610 NM 2001 7 25 UPS01236387 1 20010703 A 5320 INTERCOSTAL BOEING 727 72727C 138400J NM BS 830 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 910UP 19117 INSPECTION TYPE:C CRACK ON INTERCOSTAL AT STR 17R AT BS 830 INTERCOSTAL REPLACED IAW SRM 51-30-1 2 L 7 3 4F A3WE 2001072500611 20010725 00611 NM 2001 7 25 UPS01236389 1 20010702 A 2780 RIB BOEING 727 72727C 138400J NM #6 SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 910UP 19117 INSPECTION TYPE:C SUSPECT CRACK IN #6 SLAT RIB, O/B OF SLAT ACTUATOR. DAMAGED RIB REPAIRED IAW SRM 57-30-3 2 L 7 3 4F A3WE 2001072500612 20010725 00612 NM 2001 7 25 UPS01236391 1 20010701 A 3200 SUPPORT BRACKET BOEING 727 72727C 138400J NM BS 910 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 910UP 19117 INSPECTION TYPE:C BS 910 FRAM FWD FLANGE LWR CORNER SUPPORT BRACKET CRACKED. REPAIR CARRIED OUT IAW SRM 51-20-01, 51 -30-2 2 L 7 3 4F A3WE 2001072500613 20010725 00613 NM 2001 7 25 UPS01236392 1 20010709 A 5310 STRINGER BOEING 727 72727C 138400J NM BS 676 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 910UP 19117 INSPECTION TYPE:C END OF STRINGER 15 @ BS 676 LH IS CRACKED. REPAIR CARRIED OUT IAW 51-30-2 & 53-10-3 2 L 7 3 4F A3WE 2001082400190 20010824 00190 NM 2001 8 24 UPS01236400 1 20010720 A 5330 SKIN BOEING 727 72727C 138400J NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 INSPECTION TYPE:N/A CORROSION AFT OF NLG WW, BELLY SKIN. REMOVED CORROSION AT BS 340 TO BS 360 BETWEEN STR 26 AND 27 RT PER SRM 51-10-01. INSTALLED LT AND RT INTERNAL DOUBLER SPLICES AND T ANGLES, INSTALLED NEW FUSELAGE SKIN IAW 727 SRM 51- 30. 2 L 7 3 4F A3WE 2001072500614 20010725 00614 EA 2001 7 25 COMA0160498 1 20010723 A 5346 601350061 WEB CNDAIR CL600 CL6002B19 EA CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 938CA 15922 15922 7046 CRACKS FOUND ON BOTTOM WEB OF RIGHT HAND SIDE ENGINE SUPPORT BEAM.REPAIRED BEAM I/A/W REO 601R-53-61-366 REV B. 2 L 7 2 4F RT A21EA 2001072500616 20010725 00616 EA 2001 7 25 COMA0160499 1 20010723 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS DE DESCENT 1 SO 01 719CA 11268 4716 7253 FLAPS FAILED.REPLACED THE LEFT HAND BPSU. 2 L 7 2 4F RT A21EA 2001072500617 20010725 00617 NM 2001 7 25 ASAA0140036 1 20010420 A 5320 6517688125 ANGLE BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 786AS 24795 SEA - DURING 92 INSPECTION, FOUND CORROSION ON L1 DOOR SKATE ANGLE UNDER AFT LEFT CORNER OF FORWARD LAVATORY FLOOR PANEL AT BS 301 TO 307 AND WATERLINE 208.1 AND BUTTOCK LINE 56.5. REPAIRED IAW EA 5310-01923. (M) 2 L 7 2 4F RT A16WE 2001072500619 20010725 00619 NM 2001 7 25 ASAA0140037 1 20010417 A 5347 FITTING BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 786AS 28606 SEA - DURING 9C INSPECTION, FOUND AFT PIT TIE DOWN FITTING AT BS 947 AND WATERLINE 165 AND RBL 13.8 CORRODED AT FLOOR PA NEL SCREW ATTACH HOLE. REPAIRED PER EA 5320-01451. (M) 2 L 7 2 4F RT A16WE 2001072500621 20010725 00621 NM 2001 7 25 ASAA0140050 1 20010410 A 5315 BAC1518940 FLOORBEAM BOEING 737 7374Q8 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 779AS 25111 PAE - DURING SI CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, LBL 29 AND WL 208. REPAIRED IAW SRM AND ASA EA 5310-01925. (M) 2 L 7 2 4F RT A16WE 2001072500623 20010725 00623 NM 2001 7 25 ASAA0140051 1 20010410 A 5315 BAC1518940 FLOORBEAM BOEING 737 7374Q8 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 779AS 25111 PAE - DURING SI CHECK, FOUND FLOORBEAM CORRODED SEVERAL PLACED NEAR NUT PLATE HOLES AT BS 986.5, RBL 5-43, AND WL208, LE VEL 1. REPAIRED IAW SRM AND ASA EA5310-01928. (M) 2 L 7 2 4F RT A16WE 2001072500624 20010725 00624 NM 2001 7 25 ASAA0140052 1 20010410 A 5320 65176880175 SILL BOEING 737 7374Q8 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 779AS 25111 PAE - DURING SI CHECK, FOUND CORROSION ON MOPSILL AT BS 325, LBL 56 AND WL 208, LEVEL 2. REMOVED AND REPLACED PER SRM 5 1-40-05. (M) 2 L 7 2 4F RT A16WE 2001072500626 20010725 00626 SW 2001 7 25 ALG2001F00000 1 20010427 A 6230 214010413105 PLATE BELL BELL 214 214ST 1182106 SW MASTER SPLINE MISMANUFACTURED B ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 391AL A421 28103 DURING REPLACEMENT OF THE DRIVEPLATE WITH THE NEW UNIT. PART IS MISMANUFACTURED: MASTER SPLINE IS MACHINED APPROXIMATE LY 45 DEGREES COUNTER CLOCKWISE FROM ITS PROPER LOCATION. 2 G 7 2 4U H10SW 2001072500627 20010725 00627 NM 2001 7 25 ASAA0140074 1 20010514 A 5315 654587545 FLOORBEAM BOEING 737 7374Q8 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 780AS 25112 PAE - DURING SI CHECK, FOUND FLOORBEAM SUPPORT ANGLE AT BS 328 TO 338, RBL 63, AND WL 208 CORRODED. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2001072500628 20010725 00628 SW 2001 7 25 ALG2001F00001 1 20010504 A 6310 206340300105 DRIVE SHAFT BELL 407 407 SW ALLSN 250C 250C47B GL MAIN ROTOR FAILED E ALGA R AUTOROTATION E F VIBRATION/BUFFET FLT CONT AFFECTED CR CRUISE 1 SW 03 917AL 2114 53381 CAE847417 IN CRUISE FLIGHT. VIBRATION IN AIRFRAME AND PEDALS INCREASING IN AMPLITUDE FROM SLIGHT TO EXTREME. WHEN THE VIBRATION REACHED THE EXTREME LEVEL, POWER WAS LOST TO THE ROTOR SYSTEM AND THE AIRCRAFT WAS AUTOROTATED TO THE WATER. INPUT DRIV ESHAFT FAILED AND WAS FOUND COMPLETELY DECOUPLED AT THE TRANSMISSION INPUT ADAPTER. 1 G 7 1 3U 3 U O H2SW E1GL 2001072500629 20010725 00629 NM 2001 7 25 ASAA0140075 1 20010514 A 5320 654587512 ANGLE BOEING 737 7374Q8 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 780AS 25112 PAE - DURING SI CHECK, FOUND CORROSION ON THE L ANGLE LOWER SILL SUPPORT OF THE GALLEY DOOR AT BS 328 TO 338, WL 208, AN D BUTT LINE 65 RT. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2001072500630 20010725 00630 NM 2001 7 25 ASAA0140077 1 20010518 A 3397 8100022607 WIRE BOEING 737 7374Q8 NM CABIN DISCONNECTED A K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHT INOPERATIVE AT ROW 20. RECONNECTED WIRES AT ROW 20. FL OOR TRACK LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 2001072500631 20010725 00631 NM 2001 7 25 ASAA0140080 1 20010524 A 3350 65C270953 BALLAST BOEING 737 7374Q8 NM CABIN FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 771AS 25104 OAK - DURING LINE CHECK, FOUND EMERGENCY EXIT LIGHT AT OVERWING EXIT INOPERATIVE. REMOVED AND REPLACED LIGHT BALLAST, O PERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2001072500632 20010725 00632 NE 2001 7 25 MALA010577 2 20010719 A 7220 162VPP11 CONNECTOR SAAB SF340 SF340A 7850100 EU CT7TP CT75A 30030 NE SHORTED A MALA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 15 76XJ 340A076 On Flight #3243, in route to MSP from CWA Right Tailpipe light came on about 30-40 miles out from MSP, crew was in the c lear with no precipitation. Shutdown Engine. About 5-10 minutes after Shutdown Right Engine, Left Engine Low Engine Oil pressure light came on. Other indications looked normal. Crew elected to restart right Engine. No Tailpipe hot after restart, During previous morning start Left Engine was very slow and Oil bypass light stayed on about four minutes. Mai ntenance Removed and replaced 162VP-P11 connector that was found shorted internally. Maintenance replaced Oil Filter, dr ained power unit oil and replenished, removed carbon from B Sump, and Delta P Ref tube. Removed and replaced Oil Pressu 2 L 7 2 4T 4 T RT A52EU E8NE 2001072500633 20010725 00633 WP 2001 7 25 ZW0A0105701 1 20010724 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP TAIL COMPT A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 966TW 53616 THREE EMERGENCY LIGHTS IN THE TAIL COMPT WERE INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 3-23-01 STL. --CLOSED-- 2 L 7 2 4F RT A6WE 2001072500634 20010725 00634 WP 2001 7 25 ZW0A0105702 1 20010724 A 3350 600304051 POWER SUPPLY DOUG DC9 DC983 3022083 WP FWD CABIN A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9627R 53597 THE EMERGENCY LIGHTS AT THE COCKPIT DOOR STAYED ON WHEN POWER REMOVED. REPLACED THE POWER SUPPLY. CHECK-C 12-17-00 JFK . --CLOSED-- 2 L 7 2 4F RT A6WE 2001072600001 20010726 00001 SW 2001 7 26 ALG2001F00002 1 20010518 A 6320 407040035101 BEVEL GEAR BELL BELL 407 407 SW TRANSMISSION CRACKED B ALGR O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 03 437AL 3695 A224 53141 TRANSMISSION MAKING METAL. BEVEL GEAR CRACKED FROM BOLT HOLE. 1 G 7 1 3U O H2SW 2001072600002 20010726 00002 GL 2001 7 26 ALG2001F00003 2 20010430 A 7250 23053299 TURBINE WHEEL RROYCE BELL 407 407 SW ALLSN 250B 250B* GL COMPRESSOR CORRODED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 58236 1874 CAT44129 53069 TURBINE RECEIVED IN SHOP FOR LOW POWER. UPON INSPECTION FOUND 1ST STAGE WHEEL BROKEN FROM SULPHADATION. REMOVED OUTER COMBUSTION CASE TO INSPECT FOR LOW POWER AND FOUND SULFADATION ON 1ST STAGE WHEEL. PIECES OF TRAILING EDGE WERE MISSING AND ONE BLADE WAS BROKEN. CAUSE FOR SULPHADATION IS UNKNOWN AT THIS TIME. 1 G 7 1 3U 3 T O H2SW E10CE 2001072600003 20010726 00003 GL 2001 7 26 ALG2001F00004 2 20010525 A 7230 23053299 COMPRESSOR WHEEL RROYCE 250C30 SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C* GL ENGINE CORRODED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 768AL 1232 CAT95299 760031 RECEIVED TURBINE FROM FIELD TO REPAIR FOR HIGH FREQUENCY AND VIBES. REMOVED OUTER COMBUSTION CASE FROM TURBINE TO INSPE CT FOR HIGH FREQUENCY AND FOUND 1ST STAGE WHEEL BLADES TO HAVE BEEN ATTACKED BY SULPHADATION. MFG SHOULD USE THE NEW GE NERATION OF COATING TO STOP THIS PROBLEM. 1 G 7 2 3U 3 U H1NE E4CE 2001072600004 20010726 00004 SW 2001 7 26 ALG2001F00005 1 20010327 A 6410 407312100101 BEARING BELL BELL 407 407 SW TRUNNION BEARING SEPARATED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 437AL 1423 A257 53141 OCCURED DURING DAILY. ELASTOMER SEPARATION. 1 G 7 1 3U O H2SW 2001072600005 20010726 00005 NE 2001 7 26 ALG2001F00006 1 20010507 A 6320 E6893672 PINION GEAR ALLSN C30S SKRSKY S76 S76A 8143006 NE N2 GEAR TRAIN SPALLED A ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 376AL 255 CAG90591 760002 UPON DISASSEMBLY OF GEARBOX FOR METAL. FOUND SPALLING AND GALLING ON GEAR TEETH CAUSING METAL CONTAMINATION AND DAMAGE TO T/M GEAR PN E6893673 S/N PG4068. ASSURE PROPER MACHINING AND MESHING OF GEAR TEETH AT FACTORY. 1 G 7 2 3U H1NE 2001072600006 20010726 00006 SW 2001 7 26 ALG2001F00007 1 20010523 A 6230 206011005105 COLLAR BELL 206 206L4 1182110 SW COLLECTIVE BROKEN B ALGR A UNSCHED LANDING F FLT CONT AFFECTED HO HOVERING 1 SW 03 176AL 572 52146 DURING HOVER ATTEMPT, NOTICED UNUSUAL AMOUNT OF COLLECTIVE INPUT WITH VERY LITTLE RESPONSE(LOCATION OFFSHORE VERMILION 2 50). COLLAR BROKE INBOARD OF CLAMP UP BOLT. COMPONENT AT BELL HELICOPTER FOR EVALUATION. PREVENTATIVE RECOMMENDATION TO BE DETERMINED UPON RECEIPT OF BELL REPORT. 1 G 7 1 3U NC H2SW 2001072600007 20010726 00007 NE 2001 7 26 ALG2001F00008 1 20010618 A 3260 PROXIMITY SWITCH SKRSKY S76 S76 8143010 NE MLG OUT OF ADJ E ALGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 03 701AL 760238 DURING TAKEOFF RT MAIN GEAR RETRACT UNSAFE LIGHTS. ADJUSTED UPLOCK PROXIMITY SWITCH ON RT MAIN GEAR, PERFORMED RETRACTI ON TEST. NO DEFECTS NOTED. 1 G 7 2 3U H1NE 2001072600008 20010726 00008 NE 2001 7 26 ALG2001F00009 1 20010623 A 6210 7615003100053 SKIN SKRSKY S76 S76A 8143006 NE MAIN ROTOR BLADE SEPARATED B ALGR K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 SO 03 164AG 3018 277 760290 AFTER SHUTDOWN A PIECE OF SKIN WAS FOUND MISSING. LOWER SURFACE SKIN PEELED AND TORN AWAY APPROXIMATELY 7.5 INCHES X 5. 0 INCHES AT APPROXIMATELY R. STA 218.5 R.STA. 226.0. 1 G 7 2 3U H1NE 2001072600009 20010726 00009 SW 2001 7 26 ALG2001F00010 1 20010531 A 2913 0113245 FILTER 01454430001 BELL 206 206B 1181511 SW HYD RESERVOIR CORRODED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 59541 427 94080217 1412 FOUND DURING FIELD MAINTENANCE INSPECTION. RUST FOUND ON FILTER ASSEMBLY BODY. 1 G 7 1 3U H2SW 2001072600010 20010726 00010 SW 2001 7 26 ALG2001F00011 1 20010606 A 6220 407310101101 BEARING BELL BELL 407 407 SW MAIN ROTOR HUB SEPARATED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 477AL A307 53203 OFFSHORE PLATFORM BY PILOT. ELASTOMERIC SEPARATED FROM SPINDLE. 1 G 7 1 3U O H2SW 2001072600011 20010726 00011 SW 2001 7 26 ALG2001F00012 1 20010530 A 6320 206040020105 PINION GEAR BELL 206 206L1 1182107 SW GEAR TOOTH CHIPPED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 2756A 1489 45256 DURING 1500 HOUR INSPECTION, FOUND CHIPPED GEAR TOOTH. THE PINION ASSEMBLY WAS SENT TO BELL. 1 G 7 1 3U H2SW 2001072600013 20010726 00013 SW 2001 7 26 AQH2001F00000 1 20010608 A 6320 23063371 SEAL BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL GEARBOX TORN A AQHR K NONE K FLUID LOSS IN INSP/MAINT 1 WP 11 51698 4010 CAE270390 1) INSTALLED NEW SEAL PN23063371, MGR-80201, REV B, OTHER MARKINGSON SEAL ARE 63005SOCN. 2) SEAL STARTED LEAKING LESS T HAN 4 HOURS AND 15 STARTS LATER, SEAL LIP IS TORN, APPEARS LIKE A RIP, SUSPECT SEAL IS NOT COMPATIBLE WITH EXXON 8380 TU RBINE OIL AND MAYBE STUCK, THEN TORE LIP. 3) THIS IS NEW STYLE SEAL, DUE TO LEAKAGE PROBLEMS THAT HAD WITH OLD STYLE SE AL PN 6854424. 4) THIS IS THE SECOND NEW STYLE (BROWN COLOR) SEAL INSTALLED AT THIS AREA, IN THIS ENGINE BY 2 DIFFEREN T FBO. IT IS INSTALLED IN THE GEARBOX AT THE STARTER GENERATOR PAD. 1 G 7 1 3U 3 U H2SW E4CE 2001072600014 20010726 00014 NM 2001 7 26 2001UALA01227 1 20010625 A 5320 STRINGER CLIP BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 347 STR 36R CLIP CORRODED. 2 L 7 2 4F RT A1NM 2001072600015 20010726 00015 NM 2001 7 26 2001UALA01228 1 20010625 A 5320 SPLICE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 428-434 STR 35L SPLICE CORRODED. *S/D* FABRICATED AND INSTALLED SPLICE REPAIR IN ACCORDANCE WITH BAC DWG 143T3001 A ND SRM 51-40-42 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072600016 20010726 00016 EU 2001 7 26 B3O2001F00000 1 20010604 A 2450 701172245A RELAY SNIAS 350 AS350B2 8680813 EU TAIL BOOM CORRODED B B3OR K NONE O OTHER IN INSP/MAINT 1 SW 03 5204Y 673 3101 DURING TAIL BOOM INSPECTION, TECHNICIAN DISCOVERED BOTH RELAYS HAD SEVERE RUST AND CORROSION ON TERMINALS AND RELAY BODY . LOCATION OF RELAYS ARE UNDER THE AFT A/C SYSTEM CONDENSOR UNIT. 1 G 7 1 3U H9EU 2001072600017 20010726 00017 NM 2001 7 26 2001UALA01229 1 20010625 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 764 STR 39L-39R SHEAR TIE CORRODED. *S/D* INSTALLED NEW SHEAR TIE IN ACCORDANCE WITH BAC DWG 143T1214 N-R. MAJOR R EPAIR. 2 L 7 2 4F RT A1NM 2001072600018 20010726 00018 EU 2001 7 26 B652001F00000 1 20010706 A 5532 10530591 SKIN BOLKMS 105 BO105LSA3 5626020 EU VERTICAL STAB CRACKED A B65A K NONE O OTHER IN INSP/MAINT 1 GL 13 202LF 4209 2014 FOUND FATIGUE CRACK IN RIGHT VERTICAL STABILIZER FIN DURING PREFLIGHT. CRACK STARTED AT FORWARD AND TOP ATTACH POINTS A ND RAN AFT FOR APPROXIMATELY 8 INCHES. CRACK WAS ON INSIDE SURFACE AT MOUNTING POINTS TO HORIZONTAL STABILIZER. 1 G 7 2 3U H3AU 2001072600019 20010726 00019 NM 2001 7 26 2001UALA01230 1 20010625 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 566-567 STR 39L-39R SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED SHEAR TIE REPAIR IN ACCORDANCE WITH BAC DWG 140T2102 AND 143T1206 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072600020 20010726 00020 EU 2001 7 26 BRM2001F00000 1 20010525 A 7700 250C28C WARNING LIGHT BOLKMS 105 BO105LSA3 5626020 EU ALLSN 250C 250C28C 03013 GL NR 2 ENGINE ACTIVATED E BRMA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 07 93LF 3331 2038 CAE280105 ON 5/25/01 ENROUTE, NR 2 ENGINE GOT A CHIP LIGHT. THE FLIGHT MANUAL CALLS OUT TO LAND AS SOON AS PRACTICAL. THE PILOT DECIDED AFTER REFERENCING THE FLIGHT MANUAL, THAT THE AIRCRAFT COULD SAFELY FLY ON ONE ENGINE. THE NR 2 ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED TO AIRPORT. INSPECTED AND RETURNED TO SERVICE IAW MM. 1 G 7 2 3U 3 U H3AU E1GL 2001072600021 20010726 00021 NM 2001 7 26 2001UALA01231 1 20010625 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 1329 STR 38L-39L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED SHEAR TIE REPAIR IN ACCORDANCE WITH BAC DWG 140 T2102-548 AND 146T1212 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072600022 20010726 00022 NM 2001 7 26 2001UALA01232 1 20010625 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 742 STR 39L-39R SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED SHEAR TIE REPAIR IN ACCORDANCE WITH BAC DWG 140T 2102 AND 143T1214 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072600025 20010726 00025 EU 2001 7 26 2001UALA01233 1 20010628 A 2933 C60AA0062 INDICATOR AIRBUS 320 A320232 3930326 EU COCKPIT FAULTY A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 420UA 489 HYDRAULIC LOW LEVEL WARNING INDICATION. *S/D* REPLACED GREEN HYDRAULIC SYSTEM RESERVOIR QUANTITY INDICATOR. 2 L 7 2 4F RT A28NM 2001072600027 20010726 00027 NM 2001 7 26 2001UALA01234 1 20010628 A 3241 WARNING LIGHT BOEING 757 757222 1384956 NM COCKPIT ILLUMINATED A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 567UA 26673 DIVERSION DUE TO AUTOBRAKES DISARMED AND ANTISKID EICAS ILLUMINATED. 2 L 7 2 4F RT A2NM 2001072600028 20010726 00028 NM 2001 7 26 2001UALA01235 1 20010625 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 500-501 STR 39L-39R SHEAR TIE CORRODED. SUPPLEMENTAL DATA UPDATE FABRICATED AND INSTALLED SHEAR TIE REPAIR IN ACCORDA NCE WITH BAC DWG 140T2102 AND 143T1203 N-R. MAJOR REPAIR 2 L 7 2 4F RT A1NM 2001072600029 20010726 00029 NM 2001 7 26 2001UALA01236 1 20010625 A 5313 STRINGER BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 428-434 STR 39L CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 53-30-03-202 N-R. MAJOR REP AIR. 2 L 7 2 4F RT A1NM 2001072600031 20010726 00031 NM 2001 7 26 2001UALA01237 1 20010625 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 347 STR 36R-38R SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED SHEAR TIE REPAIR IN ACCORDANCE WITH BAC DWG 141T 1221 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072600032 20010726 00032 EA 2001 7 26 CHI2001F00000 1 20010609 A 7714 CONNECTOR BOEING 234 234 1385049 EA N2 ACTUATOR DAMAGED A CHIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 245CH MJ022 DURING A CLIMB, CRUISE SITUATION, THE NR 1 ENGINE N2 SYSTEM, BEGAN TO OSCILLATE TOWARDS THE HIGH SIDE. THE NR 1 ENGINE WAS BROUGHT BACK TO GROUND POSITION AND THE HELICOPTER WAS RETURNED TO THE SERVICE LANDING. TROUBLESHOOTING FOUND A FAU LTY CANNON PLUG ATTACHED TO THE NR 1 N2 ACTUATOR. THE CANNON PLUG WAS REPLACED. OPERATIONALLY CHECKED GOOD AND THE HEL ICOPTER WAS RETURNED TO SERVICE. 2 G 7 2 4U H9EA 2001072600033 20010726 00033 NM 2001 7 26 2001UALA01238 1 20010625 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 1219 BL 0-RBL45 FRAME T-CAP CORRODED. *S/D* FABRICATED AND INSTALLED T-CAP REPAIR IN ACCORDANCE WITH BAC DWG 146T12 07 AND SRM 51-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072600034 20010726 00034 NM 2001 7 26 2001UALA01239 1 20010625 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 1219 STR 39L-39R SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED SHEAR TIE REPAIR IN ACCORDANCE WITH BAC DWG 140 T2102-451 AND 146T1207 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072600035 20010726 00035 NM 2001 7 26 2001UALA01240 1 20010625 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 610 STR 39L-39R SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED SHEAR TIE REPAIR IN ACCORDANCE WITH BAC DWG 140T 2102 AND 143T1208 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072600036 20010726 00036 NM 2001 7 26 2001UALA01241 1 20010625 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 1263 STR 38L-39L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED SHEAR TIE REPAIR IN ACCORDANCE WITH BAC DWG 146 T1209 AND SRM 51-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072600037 20010726 00037 NM 2001 7 26 2001UALA01242 1 20010625 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 1241 STR 39L-39R SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED IN ACCORDANCE WITH BAC DWG 140T2102-451 AND 146 T1208 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072600038 20010726 00038 NM 2001 7 26 2001UALA01243 1 20010625 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 1263 STR 39L-39R SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED SHEAR TIE REPAIR IN ACCORDANCE WITH BAC DWG 140 T2102-596 AND 146T1209 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072600039 20010726 00039 NM 2001 7 26 2001UALA01244 1 20010625 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 1153 STR 39L-39R SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED SHEAR TIE REPAIR IN ACCORDANCE WITH BAC DWG 14 0T2102-451 AND 146T1204 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072600040 20010726 00040 NM 2001 7 26 2001UALA01245 1 20010625 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 1197 STR 37L-38L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED SHEAR TIE REPAIR IN ACCORDANCE WITH BAC DWG 140 T2102-626 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072600041 20010726 00041 NM 2001 7 26 2001UALA01246 1 20010625 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 1087 RBL40-LBL40 T-CAP CORRODED. *S/D* FABRICATED AND INSTALLED T-CAP REPAIR IN ACCORDANCE WITH BAC DWG 146T1201 N- R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072600042 20010726 00042 NM 2001 7 26 2001UALA01247 1 20010625 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 1285 STR 37L-38L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED SHEAR TIE REPAIR IN ACCORDANCE WITH BAC DWG 140 T2102-511 AND 146T1210 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072600043 20010726 00043 NM 2001 7 26 2001UALA01248 1 20010625 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 368 STR 38R-39R SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED SHEAR TIE REPAIR IN ACCORDANCE WITH BAC DWG 141T 1222 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072600044 20010726 00044 NM 2001 7 26 2001UALA01249 1 20010625 A 5347 SEAT TRACK BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 355 RT SEAT TRACK CORRODED. *S/D* FABRICATED AND INSTALLED SEAT TRACK IN ACCORDANCE WITH BAC DWG 141T5121 N-R. MAJ OR REPAIR. 2 L 7 2 4F RT A1NM 2001072600045 20010726 00045 NM 2001 7 26 2001UALA01250 1 20010625 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 500 STR 36L-37L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED SHEAR TIE REPAIR IN ACCORDANCE WITH BAC DWG 140T 2102 AND 143T1203 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072600046 20010726 00046 NM 2001 7 26 2001UALA01251 1 20010625 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 1175 LBL 23-RBL23 T-CAP CORRODED. *S/D* FABRICATED AND INSTALLED T-CAP REPAIR IN ACCORDANCE WITH BAC DWG 146T1205 N -R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072600047 20010726 00047 NM 2001 7 26 2001UALA01252 1 20010625 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 1109 RBL 45-LBL45 T-CAP CORRODED. *S/D* FABRICATED AND INSTALLED T-CAP REPAIR IN ACCORDANCE WITH BAC DWG 146T1202 N -R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072600048 20010726 00048 NM 2001 7 26 2001UALA01253 1 20010625 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 620UA 21880 BS 632 STR 36L-37L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED SHEAR TIE REPAIR IN ACCORDANCE WITH BAC DWG 140T 2102 AND 143T1209 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072600049 20010726 00049 NE 2001 7 26 2001UALA01254 2 20010630 A 7230 COMPRESSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE STALLED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 401UA 435 COMPRESSOR STALL ON NUMBER TWO ENGINE. 2 L 7 2 4F 4 F RT A28NM E40NE 2001072600051 20010726 00051 EU 2001 7 26 SABA010033 1 20010725 A 2612 51224127 DETECTOR BAG JETSTM JETSTM3201 1500217 EU RIGHT ENGINE SHORTED A SABA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 SO 33 966AE 966 Aircraft 966 at the gate in CLT during preflight check. The right engine fire warning light illuminated and could not b e extinguished. No emergency was declared and no emergency procedures were used. Maintenance removed and replaced the right engine zone one fire detection loop. System ops check was good. Aircraft retrurned to service. 2 L 7 2 4T RT A56EU 2001081300026 20010813 00026 NM 2001 8 13 2001UALA01256 1 20010630 A 2781 655280733 SWITCH BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE L/E FLAP FAILED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 WP 29 926UA 1498 26648 UNSCHEDULED LANDING DUE TO NR 3 LE FLAP INTRANSIT INDICATION. REPLACED FLAP-SLAT POSITION SWITCH ACCY UNIT, M229. 2 L 7 2 4F 4 F RT A16WE E2GL 2001072600052 20010726 00052 NM 2001 7 26 2001UALA01257 1 20010702 A 5320 ANGLE BOEING 737 737522 138449F NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 910UA 25254 FLOOR ANGLE AT BASE OF DOOR IS CORRODED, AT BS 953, STR 17R. REPLACED ANGLE. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072600053 20010726 00053 NM 2001 7 26 2001UALA01258 1 20010701 A 5313 STRINGER BOEING 737 737522 138449F NM FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 911UA 25255 STRINGER 14L HAS DAMAGE AND ELONGATED HOLES JUST AFT OF LT CABIN DOOR, AT BS 986 TO BS 1016. REMOVED DAMAGE. INSTALLED STRINGER REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072600054 20010726 00054 NE 2001 7 26 EGR2001F00000 1 20010701 A 2910 7665103003053 LINE SKRSKY S76 S76A 8143006 NE HYD SYSTEM LEAKING E EGRA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 17 911LV 760281 ON PREFLIGHT INSPECTION FOUND NR 2 HYDRAULIC RESERVOIR EMPTY AND FLUID ON FLIGHT CONTROL DECK. PRESSURE LINE TO YAW ACT UATOR/ PEDAL DAMPER. PIN HOLE IN METAL LINE. PN 76651-03003-053. REMOVED AND REPLACED WITH NEW PART. 1 G 7 2 3U H1NE 2001072600055 20010726 00055 NM 2001 7 26 2001UALA01259 1 20010701 A 5311 FRAME BOEING 737 737522 138449F NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 911UA 25255 FRAME OUTER CHORD CRACKED IN RADIUS ON AFT SIDE AT BS 188, WL 208. INSTALLED ANGLE DOUBLERS, SHIMS AND FILLERS TO FRAME OUTER CHORD. REPAIRED FUSELAGE SKIN ACCESS CUT-OUT WITH SKIN DOUBLER. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072600056 20010726 00056 EU 2001 7 26 ERA2001F00001 1 20010614 A 2913 704A33690004 BELT SNIAS 350 AS350B2 8680813 EU HYD PUMP FAILED A ERAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 AL 03 187EH 190 190 2839 HYDRAULIC PUMP DRIVE BELT FAILED. HYDRAULIC CAUTION LIGHT ILLUMINATED AND HORN ACTIVATED ABOUT ONE MILE FROM LANDING LO CATION. PILOT CONTACTED CONTROL TOWER AND ADVISED HYDRAULICS HAD FAILED. ROTORCRAFT MADE UNEVENTFUL RUNNING LANDING AT AIRPORT AND SHUT DOWN. 1 G 7 1 3U H9EU 2001072600057 20010726 00057 NM 2001 7 26 2001UALA01260 1 20010629 A 5311 FRAME BOEING 737 737322 1384676 NM FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 320UA 23952 AFT PIT FRAME DENTED RT SIDE, AT BS 787, RBL 28. REMOVED DAMAGE. INSTALLED REPAIR ANGLE AND STRINGER CLIPS. MAJOR REP AIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072600058 20010726 00058 EU 2001 7 26 ERA2001F00003 1 20010614 A 2913 704A3369004 BELT SNIAS 350 AS350B2 8680813 EU HYD PUMP BROKEN E ERAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 AL 03 187EH 190 2839 HYDRAULIC PUMP DRIVE BELT FAILED. HYDRAULIC CAUTION LIGHT ILLUMINATED AND HORN ACTIVATED ABOUT ONE MILE FROM LANDING LO CATION. PILOT CONTACTED CONTROL TOWER AND ADVISED HYDRAULICS HAD FAILED. ROTORCRAFT MADE UNEVENTFUL RUNNING LANDING AT AIRPORT AND SHUT DOWN. 1 G 7 1 3U H9EU 2001072600059 20010726 00059 NM 2001 7 26 2001UALA01261 1 20010629 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 320UA 23952 CABIN FLOOR INTERCOSTAL HAS EXCESSIVE MATERIAL REMOVED AT BS 328-BS 344, RBL 48. REPLACED INTERCOSTAL. MAJOR REPAIR AC COMPLISHED. 2 L 7 2 4F RT A16WE 2001072600060 20010726 00060 NM 2001 7 26 2001UALA01262 1 20010629 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 513UA 24810 CABIN FLOORBEAM CORRODED. HEAVY MATERIAL LOSS DURING CORROSION REMOVAL AT BS 324, RBL 41 TO RBL 60. REPLACED T-CAP AND INSTALLED SUPPORT ANGLES. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A2NM 2001072600061 20010726 00061 NM 2001 7 26 2001UALA01263 1 20010629 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 513UA 24810 CABIN CREASE BEAM CORRODED. HEAVY MATERIAL LOSS DURING CORROSION REMOVAL AT BS 720-BS 760, RBL 60. REMOVED CORROSION. REPLACED CREASE BEAM ANGLE. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A2NM 2001072600062 20010726 00062 NM 2001 7 26 2001UALA01264 1 20010630 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 513UA 24810 CABIN LT CREASE BEAM CORRODED. EXCESSIVE MATERIAL LOSS DURING CORROSION REMOVAL AT BS 757. REMOVED DAMAGE. INSTALLED NEW ANGLE WITH 2 SUPPORT STRAPS. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A2NM 2001072600063 20010726 00063 NM 2001 7 26 2001UALA01265 1 20010630 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 513UA 24810 CORROSION ON RT CREASE BEAM, INBOARD CHORD, AT BS 324, RBL 60. REMOVED AND REPLACED CREASE BEAM DOUBLER. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A2NM 2001090600369 20010906 00369 NE 2001 9 6 2001UALA01267 2 20010629 A 7260 O-RING BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE RT ENGINE DAMAGED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING K J A FLUID LOSS WARNING INDICATION FLAME/FIRE CR CRUISE 1 WP 29 619UA 21879 707518 RIGHT ENGINE OIL PRESSURE WENT BELOW MIN PRESSURE NO OTHER INDICATORS. ENGINE SHUTDOWN .RETURN TO FIELD. SUPPLEMENTAL D ATA UPDATE FOUND ENGINE DRIVEN HYDRAULIC PUMP DRIVE O-RING DAMAGED, ALLOWING OIL TO ESCAPE PASSED O-RING AND OUT THE OVE RBOARD DRAIN. REPLACED O-RING 2 L 7 2 4F 4 F RT A1NM E3NE 2001072600070 20010726 00070 NM 2001 7 26 2001UALA01268 1 20010630 A 7540 WARNING LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE COCKPIT ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 674UA 29242 LEFT ENGINE BLEED LIGHT WITH ASSOCIATED HSPOV EICAS MESSAGE. 2 L 7 2 4F 4 F RT A1NM E24NE 2001072600071 20010726 00071 NM 2001 7 26 2001UALA01269 1 20010702 A 5320 FLOOR SUPPORT BOEING 737 737522 138449F NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 910UA 25254 FLOOR SUPPORT IS CORRODED AT BS 947-BS 957, RBL 24.75. REPLACED FLOOR SUPPORT. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072600072 20010726 00072 NM 2001 7 26 2001UALA01270 1 20010702 A 5311 FRAME BOEING 737 737322 1384676 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 320UA 23952 FUSE FRAME CHORD, LT SIDE, CRACKED AT BS 188, WL 207. ACCOMPLISHED FRAME REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072600073 20010726 00073 NM 2001 7 26 2001UALA01271 1 20010629 A 5320 FITTING BOEING 767 767222 1385122 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 AFT CARGO PIT AT BS 1219 AT STR 32L-34L, END FITTING CRACKED. REPLACED FITTING PER BAC DWG 146T1066 AND INSTALLED PER S RM 51-40-2. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072600074 20010726 00074 NM 2001 7 26 2001UALA01273 1 20010629 A 3211 SUPPORT FITTING BOEING 767 767222 1385122 NM RT MLG GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 RT MLG SUPPORT FITTING FOR THE KICKBOARD FITTING IS GOUGED AT STA 785. 2 L 7 2 4F RT A1NM 2001072600075 20010726 00075 NM 2001 7 26 2001UALA01274 1 20010629 A 5330 DOUBLER BOEING 767 767222 1385122 NM FUSELAGE CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 AFT FUSE REPAIR DOUBLER CHAFED AND GOUGED UNDER RT H-STAB LOWER BANANA FAIRING AT STA 1816. INSTALLED REPAIR PER SRM 53 -80-01 AND 51-40-2. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072600078 20010726 00078 NM 2001 7 26 2001UALA01277 1 20010629 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 STA 698, SHEAR TIE CORRODED BETWEEN STR 37L AND 36L. REPLACED SHEAR TIE PER BAC DWG 140T2102 AND INSTALLED PER SRM 51-4 0-2. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072600080 20010726 00080 NM 2001 7 26 2001UALA01278 1 20010629 A 5230 BEAM BOEING 767 767222 1385122 NM CARGO DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 C-2 DOOR UPPER SUPPORT BEAM CORRODED. REPAIRED BEAM WITH STRAP REPAIR. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072600081 20010726 00081 NM 2001 7 26 2001UALA01279 1 20010629 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 AFT PIT, BS 1131, LBL 43-49, STRAP ON TOP OF FLOORBEAM CORRODED. FABRICATED NEW T-CAP PER BAC DWG 146T1203 AND INSTALLE D PER SRM 51-40-2. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072600083 20010726 00083 NM 2001 7 26 2001UALA01280 1 20010629 A 5330 SKIN BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 FWD PIT BELLY SKIN BETWEEN STR 39L AND 39R, STA 434-456 IS CORRODED. REPAIRED SKIN WITH DOUBLER REPAIR AND INSTALLED PE R SRM 51-40-2. 2 L 7 2 4F RT A1NM 2001072600085 20010726 00085 NM 2001 7 26 2001UALA01281 1 20010629 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 AFT PIT CORROSION ON LOWER SIDE OF T-CAP, BS 1153 RBL 8-20. 2 L 7 2 4F RT A1NM 2001072600087 20010726 00087 NM 2001 7 26 2001UALA01282 1 20010629 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 AFT PIT SHEAR TIE CORRODED BS 1153, BL0. 2 L 7 2 4F RT A1NM 2001072600089 20010726 00089 NM 2001 7 26 2001UALA01284 1 20010629 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 AFT PIT SHEAR TIE CORRODED AT BS 1197 BETWEEN STR 39L AND 39R. 2 L 7 2 4F RT A1NM 2001082000183 20010820 00183 NM 2001 8 20 01FDEA00601 1 20010724 A 5311 FRAME DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 616FE 48747 LT FRAME AT BS 1761, STR 12 FOUND WITH 4.25 INCH CRACK. *S/D* REMOVED AND REPLACED FRAME PER SRM 53-30-00 FIG 3 VOL 1. 2 L 7 3 4F RT A22WE 2001072600091 20010726 00091 NM 2001 7 26 2001UALA01285 1 20010629 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 AFT PIT T-CAP CORRODED BS 1219, LBL6-RBL26. 2 L 7 2 4F RT A1NM 2001072600092 20010726 00092 NM 2001 7 26 2001UALA01286 1 20010629 A 5330 SKIN BOEING 767 767222 1385122 NM FUSELAGE CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 AFT FUSE SKIN CHAFED LT H-STAB UPPER BANANA FRG STA 1800. 2 L 7 2 4F RT A1NM 2001072600093 20010726 00093 NM 2001 7 26 2001UALA01287 1 20010629 A 5330 SKIN BOEING 767 767222 1385122 NM FUSELAGE CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 AFT FUSE REPAIR DOUBLER CHAFED UNDER LT H-STAB LOWER BANANA FRG STA 1800. 2 L 7 2 4F RT A1NM 2001072600094 20010726 00094 NM 2001 7 26 2001UALA01288 1 20010629 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM CORRODED CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 AFT PIT FRAME 1285 T-CAP CORRODED UNDER FLANGE RBL 18-40. 2 L 7 2 4F RT A1NM 2001072600095 20010726 00095 NM 2001 7 26 2001UALA01289 1 20010629 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 FWD CARGO PIT, BS 434 BETWEEN STR 32L AND 33L, SHEAR TIE IS CORRODED. 2 L 7 2 4F RT A1NM 2001072600097 20010726 00097 NM 2001 7 26 SWAA012000 1 20010716 A 3350 07912 COVER BOEING 737 7377H4 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 703SW 27837 EEPLS COVER BROKEN AT ROW 1. R&R EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2001072600098 20010726 00098 NM 2001 7 26 SWAA012002 1 20010715 A 3350 101114 COVER BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 380SW 26587 FWD ENTRY DOOR EMERGENCY EXIT LIGHT COVER BROKEN. R&R EXIT COVER PER MM. 2 L 7 2 4F RT A16WE 2001072600099 20010726 00099 NM 2001 7 26 SWAA012004 1 20010715 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 385SW 26600 EEPLS COVER MISSING. INSTALLED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2001072600100 20010726 00100 NM 2001 7 26 SWAA012008 1 20010710 A 5314 BAC1490 STIFFENER BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D CHECK, FOUND VERTICAL WEB STIFFENER CORRODED AT BS 328, RBL 45 & WL 207. REPAIRED STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 2001072600101 20010726 00101 NM 2001 7 26 2001UALA01290 1 20010629 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 MAIN CABIN FLOORBEAM CORRODED AROUND FASTENER HOLES BETWEEN SEAT TRACKS BS 840-889, LBL 54. 2 L 7 2 4F RT A1NM 2001072600103 20010726 00103 NM 2001 7 26 SWAA012013 1 20010717 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 394SW 27380 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS COVER MISSING AT ROW 18. INSTALLED EEPLS COVE R PER MM. 2 L 7 2 4F RT A16WE 2001072600104 20010726 00104 NM 2001 7 26 SWAA012015 1 20010717 A 2432 65C53829 BATTERY BOEING 737 7373Q8 1384670 NM E&E COMP OVERHEATED A SWAA K NONE O OTHER AP APPROACH 1 SW 07 685SW 23401 ELECTRICAL FUMES IN CABIN. R&R BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2001072600105 20010726 00105 2001 7 26 SWAA012016 4 20010712 A 2565 6556685 BRACKET BOEING 737 7373H4 1384600 NM CABIN SHEARED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 378SW 26585 DURING SCHEDULED 1/2D CHECK AT DALFORT, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT STOW HOOK ATTACH BRACKET RIVET SHEARED. R&R RIVET PER SRM. 2 L 7 2 4F RT A16WE 2001072600106 20010726 00106 NM 2001 7 26 SWAA012017 1 20010713 A 5311 6546529 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 521SW 25320 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, LBL 23 & WL 154. REPAIRED F RAME PER SRM. 2 L 7 2 4F RT A16WE 2001072600107 20010726 00107 NM 2001 7 26 SWAA012018 1 20010716 A 2761 65C26864 ACTUATOR BOEING 737 7375H4 138449D NM LH WING CRACKED A SWAA K NONE K FLUID LOSS LD LANDING 1 SW 07 528SW 26570 DURING LANDING, LOST HYD SYS A, FOUND # 0 SPOILER ACTUATOR CRACKED. R&R SPOILER ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2001072600108 20010726 00108 NM 2001 7 26 SWAA012019 1 20010716 A 5754 6573714 SLAT BOEING 737 7373T5 NM RH WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED C3 CHECK, FOUND 2 EA CRACKS AT # 5 L/E SLAT LOWER SKIN AFT ROW OF RIVETS, CRACKS ARE 1 & 5/8 IN LENGTH . REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001072600109 20010726 00109 NM 2001 7 26 SWAA012020 1 20010716 A 2731 BACB28AK04 BUSHING BOEING 737 7377H4 NM RH ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 710SW 27844 DURING SCHEDULED SERVICE CHECK, FOUND RH ELEVATOR TAB # 1 HINGE BUSHING WORN. R&R HINGE BUSHING PER MM. 2 L 7 2 4F RT A16WE 2001072600110 20010726 00110 NM 2001 7 26 SWAA012021 1 20010714 A 5510 65C25727 SKIN BOEING 737 7373Q8 1384670 NM RH HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D CHECK AT DALFORT, FOUND RH HORIZ STAB LOWER SKIN CRACKED AT REAR SPAR AT ELEV STA 83. REPAIRED SKIN PER BOEING S.B. 2 L 7 2 4F RT A16WE 2001072600111 20010726 00111 NM 2001 7 26 2001UALA01291 1 20010629 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BULK PIT FRAME AT BS 1417, SHEAR TIE BETWEEN STR 38L AND 39L IS CORRODED. 2 L 7 2 4F RT A1NM 2001072600112 20010726 00112 NM 2001 7 26 SABA010034 1 20010725 A 2930 150T383 SENSOR DHAV DHC8 DHC8102 2809003 NM RIGHT WHEEL WELL INACCURATE A SABA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 881CC 294 Aircraft 881 on flight 5012 from CLT to TLH. During climb-out from CLT the number two hydraulic hot light illuminated. No inflight emergency was declared and no emergency procedures were used. The aircraft returned to CLT and landed with no other problems. The hydraulic hot light extinguished during decent into CLT. Maintenance removed and replaced the right hydraulic system high temp sensor. System ops check was good. Aircraft returned to service. 2 H 7 2 4T RT A13NM 2001072600114 20010726 00114 NM 2001 7 26 SWAA012024 1 20010706 A 5511 6547987 RIB BOEING 737 7373Q8 1384670 NM LH HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D CHECK AT DALFORT, FOUND LH HORIZ STAB L/E, # 11 RIB CRACKED. R&R RIB PER SRM. 2 L 7 2 4F RT A16WE 2001072600115 20010726 00115 NM 2001 7 26 SWAA012025 1 20010717 A 5330 6552988 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR LOWER HINGE CUTOUT, CRACK IS .025 LONG. REPAIRED SKIN PER SWA RA. 2 L 7 2 4F RT A16WE 2001072600116 20010726 00116 NM 2001 7 26 SWAA012030 1 20010718 A 5520 65C26384 TAB BOEING 737 7373A4 1384585 NM LH ELEVATOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED C4 CHECK, FOUND LH ELEVATOR TAB INBD HINGE CUTOUT AREA CRACKED & DELAMINATED 1/8 X 1/2 . R&R TAB PER MM. 2 L 7 2 4F RT A16WE 2001072600117 20010726 00117 2001 7 26 SWAA012031 4 20010717 A 2565 6556685 BRACKET BOEING 737 7373G7 1384595 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD STOW HOOK ATTACH BRACKET RIVETS LOOSE. SECURED RIVETS PER MM. 2 L 7 2 4F RT A16WE 2001072600118 20010726 00118 NM 2001 7 26 SWAA012035 1 20010717 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 654SW 28399 EEPLS COVER MISSING AT OVERWING EXIT. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2001072600121 20010726 00121 NM 2001 7 26 SWAA012038 1 20010708 A 5310 6545409 WEB BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D CHECK AT DALFORT, FOUND WEB CRACKED AT BS 665, BBL O. REPAIRED WEB PER B OEING SB & SWA RA. 2 L 7 2 4F RT A16WE 2001072600122 20010726 00122 NM 2001 7 26 SWAA012040 1 20010718 A 3350 65C34691 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 DURING SCHEDULED C1 CHECK, FOUND OVERHEAD EMERGENCY EXIT BULL NOSE LIGHT MISSING LENS AT ROW 2 DEF. INSTALLED EXIT LENS PER MM. 2 L 7 2 4F RT A16WE 2001072600123 20010726 00123 NM 2001 7 26 SWAA012047 1 20010720 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 410, STR 10R. REPAIRED S KIN PER SRM. 2 L 7 2 4F RT A16WE 2001072600124 20010726 00124 NM 2001 7 26 SWAA012048 1 20010720 A 5310 6545409 WEB BOEING 737 7372H4 138448C NM MAIN W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESS WEB CRACKED AT BS 663+10, RBL 37. REPAIRED WEB PE R SRM. 2 L 7 2 4F A16WE 2001072600125 20010726 00125 NM 2001 7 26 SWAA012053 1 20010720 A 3350 07912 COVER BOEING 737 7377H4 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 708SW 27842 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS COVER MISSING AT ROW 8. INSTALLED EEPLS COVER PER M M. 2 L 7 2 4F RT A16WE 2001072600126 20010726 00126 NM 2001 7 26 SWAA012058 1 20010719 A 3350 65C34691 LENS BOEING 737 7372H4 138448C NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED 1/4D CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LENS CRACKED AT ROW 3. R&R EXIT LIGHT LENS PER MM. 2 L 7 2 4F A16WE 2001072600127 20010726 00127 NM 2001 7 26 SWAA012060 1 20010720 A 3350 07912 COVER BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 506SW 24183 EEPLS COVER LOOSE AT ROW 10. SECURED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2001072600128 20010726 00128 NM 2001 7 26 SWAA012062 1 20010720 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 640SW 27713 EEPLS COVERS BROKEN AT ROWS 5 & 7. R&R EEPLS COVERS PER MM. 2 L 7 2 4F RT A16WE 2001072600129 20010726 00129 NM 2001 7 26 SWAA012064 1 20010721 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 943, STR 22L, & BS 931, STR 21L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001072600130 20010726 00130 NM 2001 7 26 2001UALA01293 1 20010629 A 5320 WEB BOEING 767 767222 1385122 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 AFT PIT BS 1219, RBL 22.5 WEB BELOW T-CAP CRACKED AND FASTENER HOLE. 2 L 7 2 4F RT A1NM 2001072600132 20010726 00132 NM 2001 7 26 SWAA012069 1 20010720 A 3350 07912 COVER BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 506SW 24183 EEPLS COVER COVER LOOSE AT ROW 10. INSTALLED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2001072600133 20010726 00133 NM 2001 7 26 SWAA012070 1 20010722 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 358SW 26595 EEPLS COVER LOOSE AT OVERWING EXIT. INSTALLED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2001072600134 20010726 00134 NM 2001 7 26 SWAA012071 1 20010722 A 5710 6567172 SUPPORT FITTING BOEING 737 7373H4 1384600 NM LH & RH WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 384SW 26590 DURING SCHEDULED SERVICE CHECK, FOUND LH & RH MLG WALKING BEAM SUPPORT FITTINGS CORRODED. R&R M LG SUPPORT FITTINGS PER MM. 2 L 7 2 4F RT A16WE 2001072600135 20010726 00135 NM 2001 7 26 SWAA012074 1 20010722 A 5320 6517582 WEB BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 179, RBL 17.1 & WL 231. R&R VERTICAL BEAM WEB PER SRM. 2 L 7 2 4F A16WE 2001072600136 20010726 00136 NM 2001 7 26 SWAA012075 1 20010722 A 3350 65C27093 MODULE BOEING 737 7372H4 138448C NM CABIN ERRATIC A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 BOTH FWD DOOR EMERGENCY EXIT LIGHTS REMAIN ILLUMINATED WHEN SWITCH IS IN THE OFF POSITION. R&R DOOR EMERGENCY LIGHT CONTROL MODULE PER MM. 2 L 7 2 4F A16WE 2001072600138 20010726 00138 NM 2001 7 26 2001UALA01294 1 20010629 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 AFT PIT BS 1285, LBL 2, T-CAP WEB IS CRACKED. 2 L 7 2 4F RT A1NM 2001072600139 20010726 00139 NM 2001 7 26 SWAA012078 1 20010724 A 2560 A170033 STRAP BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 611SW 27697 EMERGENCY FLASH LIGHT STRAP BROKEN AFT LOWER. R&R STRAP PER MM. 2 L 7 2 4F RT A16WE 2001072600140 20010726 00140 NM 2001 7 26 SWAA012084 1 20010724 A 2711 6546455 TAB BOEING 737 7372H4 138448C NM RH WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED 1/4D CHECK, FOUND RH AILERON TAB DELAMINATED. R&R TAB PER MM. 2 L 7 2 4F A16WE 2001072600141 20010726 00141 NM 2001 7 26 SWAA012087 1 20010709 A 2730 DAS1026B1 BEARING BOEING 737 7373Q8 1384670 NM TAIL WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D CHECK AT DALFORT, FOUND BOTH LH & RH ELEVATOR TORQUE TUBE PUSH ROD ATTACH BEARINGS WORN. R&R PUSH ROD BEARINGS PER OHM. 2 L 7 2 4F RT A16WE 2001072600142 20010726 00142 NM 2001 7 26 SWAA012088 1 20010703 A 5310 6551698 SPLICE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D CHECK AT DALFORT, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. R&R STR SP LICE PER SRM. 2 L 7 2 4F RT A16WE 2001072600143 20010726 00143 NM 2001 7 26 2001UALA01295 1 20010629 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 AFT PIT BS 1241, LBL 26.5, T-CAP IS CORRODED. 2 L 7 2 4F RT A1NM 2001072600144 20010726 00144 NM 2001 7 26 2001UALA01296 1 20010629 A 5330 DOUBLER BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 IN RESPONSE TO BOEING ENGINEERING, DOUBLER-TRIPLER REQUIRES REPLACEMENT DUE TO CORROSION AT BS 434-456, BL-0. 2 L 7 2 4F RT A1NM 2001081300027 20010813 00027 EU 2001 8 13 2001UALA01297 1 20010701 A 2560 SENSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERG EXIT DOOR FAILED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 439UA 683 RT AFT OVER WING EXIT SLIDE IS NOT INDICATING ARMED. REPLACED RIGHT AFT EMERGENCY EXIT DOOR ARM SENSOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2001072600147 20010726 00147 EU 2001 7 26 2001UALA01298 1 20010701 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 460UA 1248 ESCAPE PATH LIGHT INOP AT SEAT 6C. REPLACED ESCAPE PATH LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A28NM 2001072600149 20010726 00149 NM 2001 7 26 2001UALA01299 1 20010704 A 2120 UNKNOWN BOEING 757 757222 1384956 NM COCKPIT ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 580UA 26698 ODOR IN FLIGHT DECK AND FORWARD CABIN AFTER LANDING . 2 L 7 2 4F RT A2NM 2001072600159 20010726 00159 NM 2001 7 26 2001UALA01301 1 20010702 A 3397 WIRE BOEING 747 747422 1384935 NM CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 TWO EEL LIGHT STRIPS (LOCATED ON LEFT AISLE WALL - AT THE TOP OF THE STAIRS) AND THE ENTIRE STAIRWAY EEL LIGHT IS INOP. SUPPLEMENTAL DATA UPDATE FOUND EEL FEEDER CABLE DAMAGED. REPLACED EEL FEEDER CABLE. 2 L 7 4 4F RT A20WE 2001072600160 20010726 00160 NM 2001 7 26 VNAA0107018 1 20010719 A 3300 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 440JS 3058 THE FLIGHT ATTENDENT REPORTED THAT THE EMERGENCY LIGHTING WAS NOT ILLUMINATING IN ROWS 7 THROUGH 9. MAINTENANCE INSPECT ED, CLEANED, AND RECONNECTED THE CONNECTOR TO THE EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00- 00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001081300028 20010813 00028 NM 2001 8 13 2001UALA01302 1 20010703 A 5230 FITTING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 171UA 24322 MAJOR REPAIR REPORTING THE 65B38230-3 AFT CARGO DOOR FORWARD ACTUATOR SUPPORT FITTING AND BRACKET WERE DAMAGED. REPAIR A CCOMPLISHED PER EVAG-7736 REV A REPAIR HAS BOEING APPROVAL AND DER APPROVAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2001072600163 20010726 00163 NM 2001 7 26 2001UALA01303 1 20010610 A 5312 146N53187 PRESSURE PANEL BOEING 757 757222 1384956 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 513UA 24810 CORROSION FOUND ON THE FORWARD EDGE OF THE AFT PRESSURE DECK AT BODY STATION 1681. INSTALLED DOUBLER REPAIR TO DAMAGED AREA. THIS WAS A MAJOR REPAIR. 2 L 7 2 4F RT A2NM 2001081300029 20010813 00029 NM 2001 8 13 2001UALA01306 1 20010627 A 3350 6013211LB BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN MISSING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7263U 21410 THE R1DOOR EMERGENCY EXIT EXTERIOR LIGHT IS INOPERABLE. BATTERY ASSY IS MISSING. INSTALLED MISSING BATTERY ASSY. OPERATI ONS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001081300030 20010813 00030 NM 2001 8 13 2001UALA01307 1 20010627 A 3350 362624 LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7276U 21423 EMERGENCY EXIT LIGHTING FROM ROW 23 TO AFT ENTRY DOOR IS INOPERABLE. EEL STRIP IS DAMAGED. REPLACED LAMPS AND COVER. OP ERATIONS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001072600171 20010726 00171 NM 2001 7 26 ASAA0110230 1 20010424 A 3350 8610144 BATTERY BOEING 737 737290C 138448V NM MID CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING MAINTENANCE CHECK, FOUND EMEREGNCY EXIT LIGHT ON THE SMOKE BARRIER WOULD NOT TEST. REMOVED AND REPLACED LI GHT ASEMBLY AND BATTERY, THEN LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2001072600172 20010726 00172 WP 2001 7 26 ASAA0180116 1 20010326 A 3350 6011779 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 951AS 38331 13683 49111 SEA - DURING PRE-FLIGHT CHECK, THE PORTABLE EMERGENCY LIGHT AND EXTERNAL OVERWING EMERGENCY LIGHTS WERE REPORTED TO HAVE BEEN TURNED ON FOR AT LEAST TEN MINUTES PRIOR TO THE CHECK. REPLACED THE COMPLETE PORTABLE EMERGENCY LIGHT ASSEMBLY AN D THE BATTERY PACK FOR THE EXTERNAL OVERWING EMERGENCY LIGHTS. ALL LIGHTS CHECKED FOR PROPER OPERATION. (M) 2 L 7 2 4F A6WE 2001072600173 20010726 00173 WP 2001 7 26 ASAA0180162 1 20010507 A 2500 3961899501 LANYARD DOUG DC9 DC983 3022083 WP DETACHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 SEA - DURING PREFLIGHT CHECK, L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD BETWEEN GIRT BAR AND SLIDE COVER. (M) 2 L 7 2 4F RT A6WE 2001072600174 20010726 00174 WP 2001 7 26 ASAA0180131 1 20010408 A 3350 6011779 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 961AS 53075 SEA - DURING PREFLIGHT CHECK, OVERWING EMEREGNCY EXIT ILGHS WERE DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BATT ERY PACK (POWER SUPPLY). LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001072600175 20010726 00175 NM 2001 7 26 ASAA0110411 1 20010622 A 3350 86210144 BATTERY BOEING 737 7372X6C 1384552 NM INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERIES THEN EXIT LIGHTS OPERATED NORMAL. (M) 2 L 7 2 4F RT A16WE 2001072600178 20010726 00178 EU 2001 7 26 C2XA01CL177 1 20010725 A 7500 32145602 SHUTOFF VALVE AEROSP ATR42 ATR42320 8680930 EU LEFT ENGINE FAILED A C2XA A O UNSCHED LANDING OTHER J WARNING INDICATION CL CLIMB 1 SW 27 21837 19481 6097 202 PIT FLIGHT#3077 THE CREW REPORTED A FIRE WARNING ON THE #1 ENGINE AFTER TAKEOFF. THE TORQUE ALSO BEGIN TO DROP TO 50% A LONG WITH THE ITT BEGAN TO RISE TO 810.THE AIRCRAFT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSP ECTED THE #1 ENGINE AND FOUND THE #1 ENGINE BLEED PRESSURE REGULATOR AND SHUTOFF VALVE HAD FAILED.THE "V" BAND CLAMP FLA NGE HAD BROKEN.THE PRESSURE REGULATOR AND SHUTOFF VALVE WAS REPLACED ALONG WITH THE "V" BAND CLAMPS.OPERATIONAL CHECKS W ERE GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A53EU 2001072600179 20010726 00179 NM 2001 7 26 2001UALA01308 1 20010628 A 3610 39271611MOD VALVE BOEING 727 727222 1384073 NM NR 3 ENGINE FAILED A UALA K NONE O OTHER DE DESCENT 1 WP 29 7446U 21900 CABIN PRESSURE CANNOT BE MAINTAINED IN DESCENT. *S/D* SUSPECT NR 3 ENG HIGH PRESSURE MODULATING VALVE. REPLACED HIGH PRESSURE MODULATING VALVE. 2 L 7 3 4F A3WE 2001072600180 20010726 00180 NM 2001 7 26 2001UALA01309 1 20010704 A 5522 SKIN BOEING 727 727222 1384073 NM ELEVATOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7448U 21902 RT ELEVATOR LOWER SKIN IS CRACKED AT STA 183. REPAIRED SKIN WITH EXTERNAL DOUBLER REPAIR PER SRM 55-20-03. CALCULATED NEW MOMENT PER SRM 51-80-07. FOUND MOMENT WITHIN LIMITS. MAJOR REPAIR ACCOMPLISHED. 2 L 7 3 4F A3WE 2001090600370 20010906 00370 NE 2001 9 6 2001UALA01310 2 20010629 A 7230 COMPRESSOR BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LT ENGINE DAMAGED A UALA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 WP 29 611UA 21872 707513 LEFT COMPRESSOR STALL AT FL390 IN LT-MOD CHOP,N1 WENT DOWN TO 74 PERCENT WHILE EGT DID NOT RISE. THE ENGINE BORESCOPE RE VEALED 9TH STAGE HPC (HIGH PRESSURE COMPRESSOR) DAMAGE WAS OUT OF ALLOWABLE LIMITS, AND ENGINE WAS REPLACED. AFTER EN GINE TEARDOWN THE DAMAGE WAS CONFINED TO THE 9TH STAGE HPC. THE PNEUMATIC SYSTEM PRE-COOLER WAS REPLACED DURING THE ENGI NE CHANGE, AND IS SUSPECT AS BEING THE CAUSE OF DAMAGE TO HPC. 2 L 7 2 4F 4 F RT A1NM E3NE 2001072600181 20010726 00181 2001 7 26 2001UALA01311 4 20010704 A 3414 INDICATOR BOEING 767 767222 1385122 NM COCKPIT UNRELIABLE A UALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 WP 29 602UA 21863 COPILOTS AIRSPEED UNRELIABLE. HUNG AT 60 KTS PRIOR TO TAKEOFF UNTIL 1000 FT. GRADUALLY ROSE TO 430 KTS. (OVERSPEED IN DICATION WITH RUDDER RATIO, AND AILERON LOCKOUT.) INDICATED 86 KTS AT GATE. 2 L 7 2 4F RT A1NM 2001072600182 20010726 00182 NM 2001 7 26 2001UALA01312 1 20010701 A 2421 GENERATOR BOEING 767 767222 1385122 NM RT ENGINE FAILED A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 605UA 21866 RT GEN DRIVE EICAS FOLLOWED BY RT GEN OFF EICAS. RESET RT GEN CONTROL THEN OPS NORMAL. FAILED TWICE MORE DIVERT TO ONT. 2 L 7 2 4F RT A1NM 2001072600185 20010726 00185 NM 2001 7 26 2001UALA01314 1 20010618 A 5320 STRINGER CLIP BOEING 737 737522 138449F NM FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 911UA 25255 AFT CABIN AT STATION 1006, STRINGER CLIP AT STRINGER 13L IS DAMAGED. ACCOMPLISHED STRINGER CLIP AT STATION 1006 AND STR INGER 13L WAS REPLACED. THIS WAS A MAJOR REPAIR. 2 L 7 2 4F RT A16WE 2001072600187 20010726 00187 NM 2001 7 26 2001UALA01315 1 20010614 A 5311 FRAME BOEING 737 737322 1384676 NM FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 320UA 23952 AFT PIT STA 787 RBL 20 FRAME UPPER FLANGE DAMAGED. REMOVED DAMAGE. VERIFIED WITH NON-DESTRUCTIVE TESTING THAT THE DAMA GE WAS REMOVED. INSTALLED PLUG RIVET, TREATED, PRIMED AND PAINTED. THIS WAS A MAJOR REPAIR. 2 L 7 2 4F RT A16WE 2001072600192 20010726 00192 NM 2001 7 26 2001UALA01317 1 20010703 A 5230 143N66213 DOOR FRAME BOEING 757 757222 1384956 NM CARGO DOOR GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 FORWARD CARGO COMPARTMENT DOOR LOWER EDGE FRAME GOUGED IN 5 PLACES. REPLACED FORWARD CARGO COMPARTMENT DOOR LOWER EDGE FRAME. THIS WAS A MAJOR REPAIR. 2 L 7 2 4F RT A2NM 2001072600193 20010726 00193 NM 2001 7 26 2001UALA01318 1 20010627 A 5330 SKIN BOEING 757 757222 1384956 NM FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 DENT FOUND APPROXIMATELY 3 FEET BELOW DOOR 3L. DOUBLER REPAIR INSTALLED WITH BLIND FASTENERS. THIS WAS A MAJOR REPAIR. 2 L 7 2 4F RT A2NM 2001072600195 20010726 00195 NM 2001 7 26 2001UALA01319 1 20010627 A 5330 SKIN BOEING 757 757222 1384956 NM FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 DENT FOUND APPROXIMATELY 2 FEET BELOW 3L DOOR. DOUBLER REPAIR INSTALLED WITH BLIND FASTENERS. THIS WAS A MAJOR REPAIR. 2 L 7 2 4F RT A2NM 2001072600198 20010726 00198 NM 2001 7 26 AWXA0002039 1 20010708 A 5310 6563453721 BEAM BOEING 737 737277 1384570 NM STA 665 LBL 24 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 D: cabin center wing box area upper attach angle cracked at access cut out STA 665 LBL 24C: repaired cabin center wing b ox area upper attach angle at access cut out STA 665 LBL 24 IAW ER 15-571507202-OL3 2 L 7 2 4F RT A16WE 2001072600199 20010726 00199 NM 2001 7 26 AWXA0002040 1 20010723 A 5311 6520723 FRAME BOEING 737 737277 1384570 NM BS 480 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 D: Verify material type of repair at BS 480 frame, STR 24R at Aft cutout of fwd cargo doorC: Removed existing repair and replaced IAW AWA ER 15-5332-01204-JS1 2 L 7 2 4F RT A16WE 2001072600200 20010726 00200 NM 2001 7 26 AWXA0002041 1 20010723 A 5311 654653112 FRAME BOEING 737 737277 1384570 NM BS 480 GOUGED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 D: Previously repaired gouge at BS 480 frame BL-0 requires reworkC: Removed old repair and repaired frame IAW AWA ER #15 -5332-01204-TB1 2 L 7 2 4F RT A16WE 2001072600201 20010726 00201 NM 2001 7 26 AWXA0002042 1 20010714 A 5347 BAC1520792 SEAT TRACK BOEING 757 757225 1384959 NM STA 395-377 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 D: Pass. Cabin BS 395-377 seat track corroded @ RBL 24 O/B flangeC: Removed damaged channel (track) IAW SRM 51-40-05 fig 39-40. Fabricated track, treated primed, installed per SRM 51-40-02 pg 26 SRM 51-20-01 pg 1-3 SRM 51-30-01 pg 11 (STA 3 95-377,RBL 24) and per engineering support, 07-07-01 2 L 7 2 4F RT A2NM 2001072600218 20010726 00218 NM 2001 7 26 2001UIA001 1 20010515 A 2131 CONTROLLER DOUG MD90 MD9030 3023690 NM CABIN PRESSURE FAILED Z D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 TW 00 17923 53534 IT HAS BEEN REPORTED THAT DURING PUSHBACK AND TAXI FOR TAKEOFF, THE CABIN PRESSURE INCREASED 8 PSID BEFORE THE FLIGHT CR EW BECAME AWARE OF THE ABNORMAL PRESSURIZATION. THE CABIN CREW REPORTED PASSENGERS DIDN'T FEEL COMFORT. ONE FEMALE PAS SENGER REQUIRED HOSPITAL TREATMENT FOR A EARDRUM BLEEDING. PRESSURE WAS NOT RELIEVED UNTIL THE ENGINES WERE SHUTDOWN. 2 L 7 2 4F RT A6WE 2001072600221 20010726 00221 NM 2001 7 26 2001UIA003 1 20010701 A 2920 HYDRAULIC LINE DHAV DHC8 DHC8301 NM HYD SYSTEM LEAKING Z O OTHER K FLUID LOSS IN INSP/MAINT 1 TW 00 15233 402 ON JULY 01, 2001, FOUND RT WING CONTAMINATED WITH HYD FLUID DURING TRANSIT CHECK. PERFORM ON BOARD HYD SYS TEST, FOUND NR 2 FLIGHT SPOILER HYD TUBE (P/N8294000-113) HAD PIN HOLE LEAD TO HYD LEAKING. TEMPORARY REPAIR WITH FLEXIBLE HOSE REP LACEMENT PER AMM29-00-00 AND 20-50-52. REPLENISHING HYD IAW AMM12-10-29. ON BOARD HYD SYS TEST NORMAL. THE A/C DELAYE D FOR 5 HRS. 2 H 7 2 4T RT A13NM 2001072600238 20010726 00238 EU 2001 7 26 A6WA200100037 1 20010606 A 5522 SCREW BAC 146 146100A 1500260 EU LT ELEVATOR MISSING A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 UPPER HINGE COVER PANEL ON LEFT HAND ELEVATOR HELD ON BY ONLY ONE SCREW; FOUR SCREWS MISSING. MAINTENANCE REMOVED AND R EPLACED MISSING SCREWS. 2 H 7 4 4F RT A49EU 2001072600240 20010726 00240 EU 2001 7 26 A6WA200100039 1 20010618 A 2910 O-RING BAC 146 146300A 1500267 EU HYD SYSTEM FAILED A A6WA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 31 612AW E3122 LOST ALL GREEN HYDRAULIC QUANTITY ON GEAR EXTENSION. MAINTENANCE REMOVED AND REPLACED O-RING ON PTU PLUG. 2 H 7 4 4F RT A49EU 2001072600241 20010726 00241 NM 2001 7 26 A6WA200100040 1 20010619 A 3234 7178011 CONTROL HANDLE DORNER DO32 DO328100 2996000 NM COCKPIT FAILED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 328PH 3006 LANDING GEAR WILL NOT RETRACT WITH HANDLE IN UP POSITION, BOTH UP AND DOWN LIGHTS ARE ON. MAINTENANCE REMOVED AND REPLA CED THE GEAR SELECTOR HANDLE ASSEMBLY. 2 H 7 2 4T RT A45NM 2001072600245 20010726 00245 NM 2001 7 26 A6WA20010038 1 20010616 A 2760 ZCV1936 SHUTTLE VALVE DORNER DO32 DO328100 2996000 NM SPOILER SYS STUCK A A6WA K NONE F FLT CONT AFFECTED DE DESCENT 1 GL 31 334PH 860 860 3012 DURING DESCENT BOTH ROLL SPOILERS DEPLOYED GIVING AILERON MISTRIM, SPOILERS REMAINED DEPLOYED FOR THE REMAINDER OF THE F LIGHT. MAINTENANCE REMOVED AND REPLACED ROLL SPOILER DOUBLE SHUTTLE VALVE. 2 H 7 2 4T RT A45NM 2001072600250 20010726 00250 NE 2001 7 26 ANCF200100013 2 20010708 A 7200 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE RIGHT MALFUNCTIONED W ANCF C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 23 583AN 53183 728145 DURING TAKEOFF ROLL EXACTLY AT VR, A YAW TO THE RIGHT WAS FELT, IMMEDIATELY RIGHT ENGINE PARAMETERS WERE OBSERVED TO FAL L TO 1.7 EPR FROM 2.04 GOING BACK UP TO NORMAL. ENGINE REMINDED NORMAL UNTIL LANDING BACK IN BOGOTA. 2 L 7 2 4F 4 F RT A6WE E9NE 2001072600257 20010726 00257 NM 2001 7 26 AT0100183 1 20010618 A 3350 6011779 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 961AT 55023 FOUND EXTERNAL EMERGENCY LIGHT BATTERY PACK WOULD NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK IAW B717 MM 33-51. 2 L 7 2 4F TR A6WE 2001072600259 20010726 00259 WP 2001 7 26 AT0100193 1 20010518 A 2540 PLATE DOUG DC9 DC932 3022066 WP LAVATORY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 840AT 47523 FOUND RIGHT LAVATORY KICK PLATE CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAI R IAW DC9 SRM 51-10-3, 53-01 FIGURE 1, 51-10-2, 51-10-4, 53-30-2. 2 L 7 2 4F A6WE 2001072600261 20010726 00261 WP 2001 7 26 AT0100195 1 20010511 A 5310 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 840AT 47523 INSTALLED PERMANENT REPAIR AT AFT CARGO DOOR JAMB UPPER CORNER. FABRICATED REPAIR DOUBLERS AND INSTALLED IAW REO-L00444 . 2 L 7 2 4F A6WE 2001072600262 20010726 00262 WP 2001 7 26 AT0100199 1 20010626 A 3350 LIGHT DOUG DC9 DC932 3022066 WP CABIN MISSING A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 845AT 47238 FOUND RED LENS AND BULB MISSING AT ROW 18. REPLACED RED LENS AND BULB AT ROW 18 IAW DC9 MM 33-21-27. 2 L 7 2 4F A6WE 2001072600264 20010726 00264 NM 2001 7 26 AT0100200 1 20010626 A 3350 BATTERY PACK BOEING 737 737284 138448R NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 470AT 21501 FOUND EMERGENCY LIGHT INOPERATIVE AT OVERWING EXIT. REMOVED AND REPLACED BATTERY PACKS AT M1051 AND M1053 IAW 737 MM 33 -51-00. 2 L 7 2 4F A16WE 2001072600266 20010726 00266 WP 2001 7 26 AT0100204 1 20010604 A 5320 RETAINER DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 819AT 47260 FOUND SEAL DEPRESSOR CRACKED AT FORWARD C-1 DOORWAY. FABRICATED REPAIR AND DOUBLER IAW DC9 SRM 53-10 FIG 817. 2 L 7 2 4F A6WE 2001072600268 20010726 00268 WP 2001 7 26 AT0100209 1 20010612 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 819AT 47260 FOUND TEMPORARY REPAIRS AT BS 996 LONGERON 3L. INSTALLED PERMANENT REPAIRS IAW REO-L00453. 2 L 7 2 4F A6WE 2001072600269 20010726 00269 WP 2001 7 26 AT0100213 1 20010630 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 824AT 47278 FOUND EMERGENCY LIGHTS OUT ON ROWS 23, 25, AND 28. REPLACED BATTERY PACK IAW DC9 MM 33. 2 L 7 2 4F A6WE 2001072600271 20010726 00271 NM 2001 7 26 AT0100214 1 20010712 A 3350 081691 SOCKET BOEING 737 7372L9 1384497 NM CABIN MISSING A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 FOUND E-PATH LAMP HOLDER ASSEMBLY MISSING AT SEAT ROW 28. REPLACED HOLDER IAW MM 33-21-27. 2 L 7 2 4F RT A16WE 2001072600273 20010726 00273 2001 7 26 AWXA0001875 4 20010617 A 2230 AUTOTHRUST SYS BOEING 757 7572G7 1384963 NM COCKPIT MALFUNCTIONED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 908AW 24233 MCO- ABORTED TAKEOFF- FLT 560- THRUST LEVERS INITIALLY ADVANCED FROM IDLE POSITION, EICAS MESSAGE AUTO THROTTLE DISCONNE CT AND AUTO THROTTLE DISCONNECT AMBER LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED BELOW 60KTS. THE AUTO THROTTLE SYSTEM WAS PLACED ON MEL 22-30-1 COND 1 AND THE FLIGHT CONTINUED TO PHX. IN PHX MAINTENANCE CHECKED CURRENT STATUS WHICH WAS GOOD. MAINTENANCE CHECKED HISTORY FOR PREVIOUS 30 DAYS, NO DISCREPANCIES FOUND. PERFORMED AUTO THROTTLE BITE TEST AND TESTED GOOD. THE MEL WAS CLEARED AND NO FURTHER DISCREPANCIES HAVE BEEN REPORTED. 2 L 7 2 4F RT A2NM 2001072600274 20010726 00274 WP 2001 7 26 CALA0100677 1 20010724 A 5330 SKIN DOUG DC9 DC982 3022082 WP STA 389 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND L/H LOWER EXTERNAL FUSELAGE SKIN DENTED AT STA 389, LONGERON 29L. THE DENT WAS COLD FORMED AND A DOUBLE R WAS INSTALLED IAW SRM 51-10-3 AND 53-05, FIGURE 38. 2 L 7 2 4F A6WE 2001072600275 20010726 00275 NM 2001 7 26 CALA0100681 1 20010725 A 5320 WEB BOEING 737 7373T0 1384582 NM STA 1016&1020 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14325 23455 INSPECTION FOUND WEB CORRODED AT STA 1020, LBL 23 AND AT STA 1016, RBL 7 - LBL 16. A NEW WEB WAS INSTALLED ON LEFT OF CE NTER BBL 0 TO LBL 38 AND A NEW WEB WAS INSTALLED ON RIGHT OF CENTER BBL 0 TO RBL 38 IAW SRM 53-10-3. 2 L 7 2 4F RT A16WE 2001072600276 20010726 00276 WP 2001 7 26 CALA0100682 1 20010725 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 693-769 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND MAIN CABIN R/H CENTER AND L/H CENTER FLOOR PANELS DELAMINATED AT FS 693-769. NEW PANELS WERE INSTALLED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001072600277 20010726 00277 WP 2001 7 26 CALA0100683 1 20010725 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 807-946 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND R/H I/B FLOOR PANELS DELAMINATED AT FS 826-927. A CENTER PANEL AT FS 886-946 AND CENTER & RIGHT CENTER PANELS AT FS 807-826 WERE FOUND DELAMINATED. NEW PANELS WERE INSTALLED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001072600278 20010726 00278 WP 2001 7 26 CALA0100684 1 20010725 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 769-886 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND L/H I/B FLOOR PANEL PUNCTURED AT FS 769-826 AND L/H I/B FLOOR PANEL AT FS 864-886 WAS DELAMINATED. THE FLOOR PANELS WERE REPLACED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001072600279 20010726 00279 WP 2001 7 26 CALA0100685 1 20010725 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 826-1003 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND CABIN CENTER FLOOR PANELS DELAMINATED AT FS 826-886 AND AT FS 945-1003. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001072600280 20010726 00280 WP 2001 7 26 CALA0100686 1 20010725 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 1079-1174 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND CABIN R/H I/B AND CENTER FLOOR PANELS AT FS 1117-1174 DELAMINATED AND CENTER PANEL AT FS 1079-1117 DELA MINATED. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001072600281 20010726 00281 WP 2001 7 26 CALA0100687 1 20010725 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 1174-1361 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND MAIN CABIN CENTER FLOOR PANELS DELAMINATED AT FS 1174-1250 AND FS 1309-1361. A R/H I/B FLOOR PANEL WAS DELAMINATED AT FS 1250-1309. A NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001072600283 20010726 00283 NM 2001 7 26 2001UALA01320 1 20010709 A 5330 SKIN BOEING 757 757222 1384956 NM FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 521UA 24891 FUSELAGE SKIN DENTED AT FUSELAGE STA 446 BETWEEN STR 24L AND 25L. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND DOUB LER. 2 L 7 2 4F RT A2NM 2001072600284 20010726 00284 NM 2001 7 26 2001UALA01322 1 20010706 A 5347 SEAT TRACK BOEING 737 737522 138449F NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 911UA 25255 AFT CABIN O/B SEAT TRACK HAS CORROSION IN SEVERAL AREAS, BS 986 - BS 1006. REPLACED RT OUTBOARD TRACK SECTION. MAJOR R EPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072600286 20010726 00286 NM 2001 7 26 2001UALA01323 1 20010706 A 5240 DOOR FRAME BOEING 737 737522 138449F NM FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 912UA 25290 FWD GALLEY DOOR AFT SIDE CRACKED AT THIRD STOP FITTING CUTOUT. REMOVED DAMAGE. INSTALLED DOUBLER. MAJOR REPAIR ACCOMP LISHED. 2 L 7 2 4F RT A16WE 2001072600287 20010726 00287 NM 2001 7 26 2001UALA01324 1 20010706 A 5311 FRAME BOEING 737 737322 1384676 NM FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 320UA 23952 AFT PIT FRAME UPPER FACE DENTED AT BS 767, RBL 24, BETWEEN STR 24R AND STR 25R. REMOVED DAMAGE. INSTALLED DOUBLER. MA JOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072600289 20010726 00289 NM 2001 7 26 2001UALA01325 1 20010707 A 5315 FLOORBEAM BOEING 737 737522 138449F NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 910UA 25254 FLOORBEAM T-CAP CORRODED AT BS 986.5, RBL 22.5- RBL 31. REPAIRED FLOORBEAM. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072600291 20010726 00291 NM 2001 7 26 2001UALA01326 1 20010707 A 5315 FLOORBEAM BOEING 737 737522 138449F NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 910UA 25254 MAIN CABIN FLOORBEAM CORRODED AT BS 294, RBL 35 RBL 38. REPAIRED T-CAP. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072600292 20010726 00292 NM 2001 7 26 2001UALA01327 1 20010707 A 5330 SKIN BOEING 737 737522 138449F NM FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 911UA 25255 EXTERIOR FUSELAGE SKIN HAS DEEP CREASE, AT BS 1000, STR 14L. ACCOMPLISHED FILLER AND DOUBLER REPAIR. MAJOR REPAIR ACCO MPLISHED. 2 L 7 2 4F RT A16WE 2001072600293 20010726 00293 NM 2001 7 26 2001UALA01328 1 20010707 A 5311 FRAME BOEING 737 737322 1384676 NM FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 320UA 23952 AFT PIT FRAME UPPER FLANGE WORN AT BS 793, RBL 24. ACCOMPLISHED DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072600294 20010726 00294 NM 2001 7 26 2001UALA01330 1 20010707 A 5330 SKIN BOEING 737 737322 1384676 NM FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 337UA 24241 FUSELAGE SKIN DAMAGED AT BS 190, BETWEEN STR 17L AND STR 18L. INSTALLED FLUSH PATCH WITH INTERNAL DOUBLER. MAJOR REPAI R ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072600295 20010726 00295 NM 2001 7 26 2001UALA01331 1 20010706 A 5312 BULKHEAD BOEING 737 737522 138449F NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 910UA 25254 VERTICAL BEAM WEB CRACKED AT PULLEY CUTOUT LOWER CORNER, AT BS 178, RBL 5.7, WL 181. REPLACED LOWER WEB. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072600296 20010726 00296 NM 2001 7 26 2001UALA01332 1 20010708 A 5311 FRAME BOEING 737 737522 138449F NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 911UA 25255 AFT PIT FRAME HAS EXCESSIVE MATERIAL LOSS AT BS 787, RBL 20. INSTALLED ANGLE DOUBLER AND STRAP REPAIR. MAJOR REPAIR AC COMPLISHED. 2 L 7 2 4F RT A16WE 2001072600297 20010726 00297 2001 7 26 2001UALA01333 4 20010704 A 3460 COMPUTER BOEING 777 777222 1385219 NM COCKPIT FAILED A UALA K NONE O OTHER CR CRUISE 1 WP 29 206UA 30212 SECONDARY ATTITUDE AIR DATA REF UNIT (SAARU) FAILED INFLIGHT. 2 L 7 2 4F RT T0001SE 2001081300031 20010813 00031 2001 8 13 2001UALA01335 4 20010703 A 3442 6225122103 TRANSCEIVER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE WEATHER RADAR FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 7271U 21418 LOST WEATHER RADAR DURING CRUISE. AIRCRAFT DIVERTED TO ORD. TRANSCEIVER FAILED. REPLACED WEATHER RADAR. OPERATIONS CHEC K NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001072600298 20010726 00298 NM 2001 7 26 2001UALA01337 1 20010709 A 5320 FLOOR SUPPORT BOEING 737 737322 1384676 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 337UA 24241 AFT PIT FLOOR SUPPORT ANGLE CORRODED AT BS 727D+6, 4TH INBD FROM RT SIDE. REMOVED DAMAGE. ACCOMPLISHED ANGLE REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072600299 20010726 00299 NM 2001 7 26 2001UALA01338 1 20010709 A 5320 FLOOR SUPPORT BOEING 737 737322 1384676 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 337UA 24241 AFT PIT FLOOR SUPPORT HAS CORROSION AT BS 727D. ACCOMPLISHED ANGLE REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072600301 20010726 00301 NM 2001 7 26 2001UALA01340 1 20010708 A 5330 SKIN BOEING 727 727222 1384073 NM FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7259U 21406 FOUND DENT ON LEFT SIDE OF FUSELAGE BEHIND RADOME AT 7 O'CLOCK POSITION, STATION 188. REPAIRED EXTERNAL FUSELAGE DENT P ER SRM 53-30-03. MAJOR REPAIR ACCOMPLISHED. 2 L 7 3 4F A3WE 2001081300033 20010813 00033 NM 2001 8 13 2001UALA01341 1 20010707 A 3350 S106 BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7445U 21899 LT CENTER OVER WING EMERGENCY EXIT LIGHT IS INOPERABLE. BATTERY WAS DISCHARGED. RECHARGED BATTERY, GROUND TEST NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001072600302 20010726 00302 NM 2001 7 26 2001UALA01342 1 20010705 A 5313 STRINGER BOEING 727 727222 1384073 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7448U 21902 STRINGER 27R IS CORRODED. REPAIRED STRINGER PER SRM 53-10-03. MAJOR REPAIR ACCOMPLISHED. 2 L 7 3 4F A3WE 2001072600303 20010726 00303 NM 2001 7 26 2001UALA01344 1 20010704 A 5522 SKIN BOEING 727 727222 1384073 NM ELEVATOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7448U 21902 RT ELEVATOR LOWER SKIN IS CRACKED AT STATION 183. REPAIRED SKIN WITH EXTERNAL DOUBLER PER SRM 55-20-03 AND CALCULATED N EW MOMENT PER SRM 51-80-07. MAJOR REPAIR ACCOMPLISHED. 2 L 7 3 4F A3WE 2001081300040 20010813 00040 NM 2001 8 13 2001UALA01345 1 20010705 A 3350 362624 LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7291U 21569 FWD LOWER LEFT DOOR EXIT LIGHT IS INOPERABLE. EEL CABLE AND EXIT LIGHT WAS DAMAGED. REPAIRED DAMAGED EEL CABLE AND REPL ACED INOPERABLE EXIT LIGHT ASSEMBLY. EMERGENCY EXIT OPERATIONS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001072600304 20010726 00304 NM 2001 7 26 2001UALA01347 1 20010710 A 2120 ODOR BOEING 737 737322 1384676 NM CABIN DETECTED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 337UA 24241 UNKNOWN ODOR IN CABIN REPORTED BY CABIN CREW. *S/D* NO CAUSE DETECTED FOR ODOR. CHECKED PACK SYSTEMS, PNEUMATIC DUCTS , ELECTRONIC COMPARTMENT, CABIN LIGHTING, AND GALLEYS EQUIPMENT WITH NO DEFECTS NOTED. 2 L 7 2 4F RT A16WE 2001081600103 20010816 00103 NM 2001 8 16 2001UALA01348 1 20010710 A 5754 TRACK BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE L/E SLAT OUT OF ADJ A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 29 994UA 22384 NR 6 SLAT WOULD NOT RETRACT. *S/D* ACCOMPLISHED ADJUSTMENT OF THE NR 6 SLAT AUXILIARY TRACKS. EXTENDED AND RETRACTED SLATS SEVERAL TIMES. NO BINDING NOTED. OPERATION SMOOTH, ALL INDICATIONS NORMAL. 2 L 7 2 4F 4 F A16WE E2EA 2001072600305 20010726 00305 NM 2001 7 26 2001UALA01349 1 20010709 A 3260 SENSOR BOEING 737 737322 1384676 NM LANDING GEAR MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 203UA 24718 UNSCHEDULED LANDING DUE TO AIR GROUND SENSOR PROBLEM. 2 L 7 2 4F RT A16WE 2001081300048 20010813 00048 NM 2001 8 13 2001UALA01350 1 20010710 A 2710 15441003 CONTROL UNIT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT FLAPERON MALFUNCTIONED A UALA J A DUMP FUEL UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 WP 29 769UA 25047 26921 45 MINUTES OUT FROM JFK (JFK-LHR) EICAS MESSAGES FOR FLIGHT CONTROL SYSTEM AND FUEL FILTER. RETURN TO JFK. FUEL DUMPED. A FLIGHT CONTROL SYS EICAS STATUS MSG WAS CAUSED BY THE RT OUTBD FLAPERON MSG 2710303 PCU DOES NOT FOLLOW COMMAND. MAIN T PERFORMED FIM TASK 27-11-817 WITH TEST PASS. RT OUT FLAPERON PCU WAS REPLACED 7/13/01. AIRPLANE HAS REPORTED NO FURTH ER FLIGHT CONTROL PROBLEMS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001082900040 20010829 00040 NM 2001 8 29 2001UALA01351 1 20010711 A 7930 8D1415 SWITCH BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE NR 1 ENGINE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 617UA 21877 707514 ENGINE (1) OIL FILTER BYPASS LIGHT FLICKERS. DIVERTED SLC. *S/D* THE OIL FILTER BYPASS SWITCH FAILED. REPLACED BYPAS S SWITCH. 2 L 7 2 4F 4 F RT A1NM E3NE 2001072600306 20010726 00306 NM 2001 7 26 2001UALA01352 1 20010711 A 7931 WARNING SYSTEM BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE COCKPIT MALFUNCTIONED A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 783UA 26950 LOW OIL PRESSURE WARNING INTERMITTENTLY COMING INTO VIEW WITH OIL PRESSURE SHOWING 211 PSI (NORMAL), ALSO WHEN OIL PRESS URE WARNING OCCURRED N1, EPR AND FF FLUCTUATING OCCURRED. AT FL390 M.84V 4 HRS AIRBORNE EICAS MSG ENG OIL PRESS L CAUTI ON APPEARED OIL PRESSURE READ NORMAL AT 210 PSI (CONT'D). 2 L 7 2 4F 4 F RT T0001SE E46NE 2001072600307 20010726 00307 EU 2001 7 26 2001UALA01353 1 20010712 A 2421 766219 IDG AIRBUS 320 A320232 3930326 EU NR 1 ENGINE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 459UA 1192 NUMBER ONE GENERATOR FAILED. *S/D* NUMBER ONE GENERATOR TRIPPED OFF AND WOULD NOT RESET. REMOVED AND REPLACED NUMBER ONE IDG AND NUMBER ONE GENERATOR CONTROL UNIT. 2 L 7 2 4F RT A28NM 2001072600308 20010726 00308 NM 2001 7 26 2001UALA01354 1 20010712 A 2782 SLAT BOEING 737 737291 138448W NM WING MALFUNCTIONED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 29 979UA 21544 NR 1 SLAT WOULD NOT RETRACT FROM FLAPS 1 TO FLAPS 0. 2 L 7 2 4F A16WE 2001072600309 20010726 00309 NM 2001 7 26 2001UALA01392 1 20010714 A 5230 SKIN BOEING 767 767322 1385200 NM CARGO DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 BULK PIT DOOR HAS SMALL DEEP DENT 14 INCHES FROM T/E AND 16 INCHES ABOVE DOOR HANDLE. 2 L 7 2 4F RT A1NM 2001072600310 20010726 00310 NE 2001 7 26 AWXA0001966 2 20010712 A 7250 V2500A1 TURBINE AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NR 2 ENGINE DAMAGED A AWXA A UNSCHED LANDING M Y OVER TEMP ENGINE STOPPAGE CR CRUISE 1 WP 28 634AW 31163 2654 091 V0089 SEA - ENGINE FAILURE - DIVERTED FLIGHT. EN ROUTE FROM YVR TO PHX THE NR 2 ENGINE EXCEEDED EGT LIMITS FOLLOWED BY ENGINE STOPPAGE. THE AIRCRAFT DIVERTED TO SEA MAKING AN UNEVENTFUL LANDING. IN SEA THE ENGINE WAS INSPECTED AND FOUND TO HAV E EXTENSIVE TURBINE DAMAGE. FURTHER INSPECTION OF THE AIRCRAFT REVEALED SEVERAL DENTS ON RT INBOARD AFT FLAP, WHICH WER E FOUND TO BE WITHIN SRM LIMITS, NO REPAIR REQUIRED. THE RT HORIZ STABILIZER L/E HAD 4 DENTS WHICH WERE ADDRESSED PER A WA ER 26-5512-01189-DD2 TO PREPARE THE AIRCRAFT FOR MAINTENANCE FERRY TO PHX AFTER THE NR 2 ENGINE WAS CHANGED. THERE W AS ALSO A SMALL GOUGE IN NR 2 FLAP TRACK FAIRING (RT WING) WHICH WAS IN LIMITS TO CONTINUE IN SERVICE. 2 L 7 2 4F 4 F RT A28NM E311NE 2001072600311 20010726 00311 NE 2001 7 26 C1HA200183004 2 20010626 A 7260 FITTING BOEING 727 7272S7 138407Z NM PWA JT8 JT8D17 52049 NE NR 1 ENGINE LOOSE A C1HA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 15 683CA 22490 ENGINE NR 1 OIL QUANTITY GAUGE ROLLED DOWN TO ZERO EN ROUTE. TEN MIN LATER LOST PRESSURE AND LIGHT ILLUMINATED. PERFOR MED PRECAUTIONARY ENGINE SHUTDOWN. FOUND LOOSE FITTING ON BOTTOM OF GEARBOX. RETORQUED PER JT8D MANUAL, INSPECTED MAIN OIL FILTER AND NO DEFECTS NOTED. RAN ENGINE AND PERFORMED LEAK CHECK, NO LEAKS NOTED. OK TO CONTINUE SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2001072600312 20010726 00312 NM 2001 7 26 ZW0A0105801 1 20010726 A 3350 80741 LAMP BOEING 767 76733AER 1385230 NM SEAT 17C A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 637TW 25403 THE EGRESS LIGHT AT CABIN SEAT 17C WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 1-27-01 LAX. --CLOSED-- 2 L 7 2 4F RT A1NM 2001072600313 20010726 00313 NE 2001 7 26 C1HA200185005 2 20010614 A 7261 FILTER BOEING 727 7272S7 138407Z NM PWA JT8 JT8D17 52049 NE NR 2 ENGINE CLOGGED A C1HA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 685CA 22492 AFTER 17 MIN NR 2 ENG OIL PRESSURE/ FILTER BYPASS LIGHT ILLUMINATED. PRECAUTIONARY ENGINE SHUT DOWN, RETURN TO ORIGINAT ION POINT. REMOVED AND REPLACED MAIN OIL FILTER, RAN ENGINE, CHECKS GOOD. PLACED FILTER ON 50 HR REINSPECT. 2 L 7 3 4F 4 F A3WE E2EA 2001072600314 20010726 00314 NM 2001 7 26 C1HA200186005 1 20010606 A 2611 CONNECTOR BOEING 727 7272S7 138407Z NM LAVATORY LOOSE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 686CA 22021 RIGHT AFT LAV SMOKE DETECTOR INOP. FOUND POWER PLUG LOOSE TIGHTENED PLUG, OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2001072600315 20010726 00315 2001 7 26 C1HA200193010 4 20010615 A 2565 SLIDE BOEING 727 727212 138407G NM L1 DOOR OUT OF POSITION A C1HA K NONE O OTHER CR CRUISE 1 GL 15 293AS 21348 ESCAPE SLIDE CAME OUT OF CASING ON L-1 DOOR DURING FLIGHT. REINSTALLED SLIDE PER MM. 2 L 7 3 4F A3WE 2001072600316 20010726 00316 NM 2001 7 26 C1HA200196006 1 20010621 A 3260 WARNING LIGHT BOEING 727 7272J4 1384006 NM COCKPIT ILLUMINATED A C1HA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 696CA 22574 UPON DEPARTURE LANDING GEAR LEFT RED DISAGREEMENT LIGHT ILLUMINATED WITH GEAR HANDLE IN UP POSITION. EXTINGUISHED WHEN PLACED IN OFF POSITION. INSTALLED GEAR PINS, OPS CHECKED. LT MLG, ALL CHECKS GOOD. COULD NOT DUPLICATE, OK FOR SERVIC E. 2 L 7 3 4F RT A3WE 2001072600317 20010726 00317 NM 2001 7 26 C1HA200197003 1 20010601 A 5270 SWITCH BOEING 727 727270 138408P NM AFT AIRSTAIR DIRTY A C1HA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 697CA 23052 AFT AIRSTAIR LIGHT ILLUMINATED ON TAXI OUT. VERIFIED DOOR UP AND LOCKED. CLEANED AND RESET SWITCH, OPS CHECKED GOOD. 2 L 7 3 4F RT A3WE 2001072600318 20010726 00318 EU 2001 7 26 C2XA01CL145 1 20010619 A 3610 650042001 DUCT AEROSP ATR42 ATR42320 8680930 EU NR 2 ENGINE LEAKING A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 21837 202 CLE FLIGHT 3793 THE CREW REPORTED A NR 2 ENGINE FIRE LIGHT AFTER TAKEOFF. THE LIGHT WAS A MOMENTARY LIGHT AND REPORTED NO FIRE. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND THAT IT WAS A NA CELLE OVERHEAT PROBLEM INSTEAD OF A FIRE LIGHT. MAINTENANCE REPLACED THE NR 2 ENGINE BLEED DUCT BALL JOINT TUBE WHICH W AS LEAKING. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A53EU 2001072600319 20010726 00319 EU 2001 7 26 C2XA01CL146 1 20010619 A 6123 4122006002R PUMP AEROSP ATR42 ATR42320 8680930 EU NR 2 PROP SHORTED A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 14828 16438 100 179 CLE FLIGHT 3226 THE CREW REPORTED THE NR 2 PROP FEATHER PUMP POWER SUPPLY CIRCUIT BREAKER POPPED. RESET AND IT POPPED A GAIN. MAINTENANCE INSPECTED AND REPLACED THE NR 2 PROP FEATHER PUMP. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS R ELEASED FOR SERVICE. 2 H 7 2 4T RT A53EU 2001072600320 20010726 00320 CE 2001 7 26 C2XA01CL147 1 20010624 A 2612 70522 FIRE LOOP BEECH 1900 1900D 1154162 CE RT ENGINE SHORTED A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 87557 UE246 CLE FLT 3307 THE CREW REPORTED RIGHT ENGINE FIRE DETECTION SYSTEM WOULD NOT TEST. MAINTENANCE REPLACED RIGHT ENGINE F IRE DETECTION CABLE ASSEMBLY. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 2001072600322 20010726 00322 2001 7 26 C2XA01CL179 4 20010725 A 6122 GOVERNOR BEECH 1900 1900D 1154162 CE LEFT ENGINE OUT OF ADJ A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 47542 UE198 CLE FLIGHT#3240 THE CREW REPORTED THE LEFT ENGINE GOES INTO FEATHER BEFORE THE FEATHER STOP.MAINTENANCE INSPECTED AND A DJUSTED THE #1 ENGINE PROPELLOR GOVERNOR FEATHER PLUNGER.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERV ICE. 2 L 7 2 4T RT A24CE 2001072600323 20010726 00323 NM 2001 7 26 F3LA200100096 1 20010716 A 3350 6013211 BATTERY PACK BOEING 737 7372P6 NM DISCHARGED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 272 3 21613 PRIOR TO DEPARTURE, MAINTENANCE REPORTED BOTH EMERGENCY OVERWING EXIT LIGHTS INOPERATIVE. MAINTENANCE IS IN THE PROCESS OF TROUBLESHOOTING THE SYSTEM. AN ADDENDUM WILL BE ISSUED WHEN REPAIR IS ACCOMPLISHED. ADDENDUM: REPLACED FORWARD AN D CENTER BATTERY PACKS PER MM 33-51-32. 2 L 7 2 4F RT A16WE 2001072700001 20010727 00001 SO 2001 7 27 C2XA01IA300 1 20010719 A 3350 RPS1B BATTERY PACK EMB 145 EMB145ER SO CABIN DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15941 145035 IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE OVERWING SECTION OF THE AISLE PATH LIGHTING WAS INOPERATI VE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001072700002 20010727 00002 SO 2001 7 27 C2XA01IA302 1 20010723 A 7100 23052650 BLEED VALVE EMB 145 EMB145LR SO ALLSN AE300 AE3007A GL #1 ENGINE INOPERATIVE A C2XA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 27 12967 145133 CAE311223 MAF - FLIGHT 3752, THE CREW REPORTED AN ATTCS NO MARGIN WARNING ON TAKE OFF ROLL. THE TAKE OFF WAS ABORTED, AND THE AIRC RAFT RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE LOWER COMPRESSOR BLEE D VALVE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2001072700008 20010727 00008 NM 2001 7 27 0102555524 1 20010722 A 2780 285N001137MODA CONTROL UNIT BOEING 727 727251 138408H NM EQUIPMENT BAY A NWAA A O UNSCHED LANDING OTHER O OTHER CL CLIMB 1 GL 01 524US 23618 ON FLAP RETRACTION AFTER TAKEOFF, FLAP MOVEMENT STOPPED BETWEEN FLAPS 1 AND FLAPS UP AND A "LEADING EDGE ASYMMETRY" EICA S MESSAGE WAS DISPLAYED. SYSTEM THEN TRIGGERED A "FLAP ISOLATION VALVE" STATUS MESSAGE. COMPLIED WITH COM PROCEDURS AND RECEIVED A "LEADING EDGE DISAGREE" MESSAGE AFTER SELECTING ALTERNATE FLAP SYSTEM. FLIGHT DECLARED AN EMERGENCY, RETURNED TO LAX, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FLAP SLAT ELECTRONICS UNIT. SYSTEM OPERATIONAL TESTS W ERE SATISFACTORY. 2 L 7 3 4F A3WE 2001072700009 20010727 00009 NM 2001 7 27 0102565649 1 20010724 A 2530 OVEN BOEING 757 757251 1384970 NM NBR 2 GALLEY A NWAA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS O OTHER CR CRUISE 1 GL 01 549US 26496 (YXJ) FLIGHT ATTENDANTS REPORTED NBR 2 GALLEY OVEN OVERHEATED WITH ALL POWER REMOVED. APPROPRIATE CIRCUIT BREAKERS WERE PULLED. OVEN WAS STILL DEEMED OVERHEATED 40 MINUTES AFTER BREAKERS WERE PULLED. FLIGHT DIVERTED TO YXJ AND LANDED WITHOU T INCIDENT. MAINTENANCE ISOLATED THE GALLEY BUSS BY DISABLING THE UTILITY BUSS FROM THE COCKPIT. THE FLIGHT CONTINUED TO DTW. MAINTENANCE INSPECTED THE OVEN CAVITY ADN WIRING WITH NO DISCREPANCIES NOTED. REPLACED THE OVEN AS A PRECAUTIO N. 2 L 7 2 4F RT A2NM 2001072700010 20010727 00010 NM 2001 7 27 0102596303 1 20010722 A 2910 HYDRAULIC LINE BOEING 747 747451 1384940 NM CASE DRAIN MOD RUPTURED A NWAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 GL 01 666US 23821 DURING CLIMB, THE AIRCRAFT LOST THE NBR 4 HYDRAULIC SYSTEM FLUID QUANTITY AND PRESSURE. CREW DECLARED AN EMERGENCY AND R ETURNED TO MNL AND LANDED WITHOUT INCIDENT. REPLACED THE HYDRAULIC RETURN LINE BETWEEN THE CASE DRAIN MODULE AND HEAT EXCHANGER, CASE DRAIN MODULE, ENGINE DRIVEN HYDRAULIC PUMP, AND AIR DRIVEN HYDRAULIC PUMP. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2001072700011 20010727 00011 NM 2001 7 27 2001UALA00874 1 20010504 A 3610 CONTROLLER BOEING 767 767322 1385200 NM PNEUMATIC SYS MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 669UA 30025 RT DUCT PRESSURE FLUCTUATES DURING DESCENT, WITH ENG RUNNING, LT & RT ISOL VLVS CLSD, AND BLD SW ON. DUCT PSI FLUCTUATE S. ETOPS VERIFICATION FLIGHT, RTF. 2 L 7 2 4F RT A1NM 2001072700014 20010727 00014 2001 7 27 2001UALA00876 4 20010528 A 2210 AUTOPILOT SYS BOEING 767 767322 1385200 NM COCKPIT MALFUNCTIONED A UALA O OTHER F FLT CONT AFFECTED DE DESCENT 1 WP 29 649UA 25286 ON DESCENT OUT OF 8,000 FEET AUTOPILOT SPD 210, FLAPS 5-WHEN SPEED BRAKE DEPLOYED PAST 1-2 TOWARDS FULL. AC REMAINED WI NGS LEVEL, BUT YOKE SHOWED 2 1-2 TO 3 DEG ON STATUS PG RT INBOARD AILERON ALMOST FULLY DEFLECTED DOWN. OK WITH NO SPEED BRAKE. UNEVENTFUL LANDING. 2 L 7 2 4F RT A1NM 2001072700015 20010727 00015 NE 2001 7 27 2001UALA00886 2 20010510 A 7200 ENGINE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE RIGHT MALFUNCTIONED A UALA K NONE R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 618UA 21878 AT LOW POWER SETTING ON CLIMB UNDER 1.20 EPR RT ENG LAGGED LT BY .15 EPR AND 15 PERCENT N1, ABOVE 1.20 EPR AT CRUISE OKA Y. ON DESCENT AT LOW ALT RT LAGGED BY .15 EPR AND 20.0 EPR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001072700018 20010727 00018 NM 2001 7 27 2001UALA01321 1 20010707 A 2130 SEAL BOEING 737 737291 138448W NM CABIN LEAKING A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 983UA 21641 UNSCHEDULED LANDING DUE TO CABIN PRESSURIZATION PROBLEMS. *S/D* DURING SINGLE PACK OPERATION, THE AIRCRAFT COULD NOT M AINTAIN PRESSURE. THE NOSE LANDING GEAR VIEW PORT HAD ALL SEALS REPLACED. 2 L 7 2 4F A16WE 2001081300036 20010813 00036 NM 2001 8 13 2001UALA01343 1 20010704 A 2742 12970003 ACTUATOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE HORIZ STAB FAILED A UALA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 WP 29 7277U 21424 CREW REPORTS A GRINDING NOISE HEAR WHEN CRUISE TRIM ENGAGED. MANUAL TRIM WAS JAMMED IN THE NOSE UP POSITION. AIRCRAFT R ETURNED TO DEN. REPLACED THE MAIN STAB TRIM ACTUATOR, CRUISE STAB TRIM ACTUATOR AND STAB BRAKE ASSY. SYSTEM OPERATIONS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001072700019 20010727 00019 NM 2001 7 27 DLM88011137 1 20010708 A 2780 4953937501 PIN DOUG MD88 MD88 3023688 NM R/H SLAT 0/1 BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DL 49538 IRR - ON L/O FOUND R/H SLAT "0" LOWER ALIGNMENT PIN BUSHING BROKEN. CORR- INSTALLED NEW ALIGNMENT PIN - CYCLED SLATS - ALL CKS NORMAL PER M/M. 2 L 7 2 4F RT A6WE 2001072700020 20010727 00020 NM 2001 7 27 DL72S011145 1 20010711 A 5330 65545783 SKIN BOEING 727 727232 1384082 NM SKIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 533DA 22046 DURING HMV CRACKS WERE FOUND IN THE STRINGER 4L LAP JOINT BETWEEN FS 970 AND FS 990. THE CRACKS WERE REPAIRED PER B727 SRM 53-30-3, FIG 5. 2 L 7 3 4F A3WE 2001072700021 20010727 00021 NM 2001 7 27 DL73K011146 1 20010711 A 5330 654577416 SKIN BOEING 737 737232 1384475 NM SKIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 317DL 23089 THE FUSELAGE SKIN AT FS 727B AND STR 18L UNDER THE WING-TO- BODY FAIRING WAS FOUND CRACKED. THE DAMAGE WAS CUT OUT AND REPAIRED WITH AN EXTERNAL DOUBLER SIMILIAR TO THAT OF S/B 737-53-1065. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001072700022 20010727 00022 NM 2001 7 27 DL75A011154 1 20010710 A 5310 143N85121 FRAME BOEING 757 757212 NM FS 620, S-25R CUT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 751AT 23125 FUSELAGE / C1 DOOR OPENING / FRAME / FS 620 / STRG. 25R-26R:FRAME WEB AND OUTER CHORD SPLICE REPAIR THE C1 DOOR OPENING LOWER SILL OUTER CHORD REQUIRED REPLACEMENT DUE TO CORROSION. TO FACILITATE REMOVAL AND INSTALLATION OF A NEW CHORD, THE OUTER CHORD AND WEB OF THE FS 620 FRAME WERE CUT BETWEEN STRINGERS 25R & 26R. THE WEB WAS SPLICED BACK TOGETHER WITH AN ALUMINUM DOUBLER AND THE CHORD WITH 2 ALUMINUM ANGLES. THE REPAIR WAS ACCOMPLISHED PER ER/A 381025-14, REV A. 2 L 7 2 4F RT A2NM 2001072700023 20010727 00023 NM 2001 7 27 DL75A011159 1 20010712 A 5330 143N33203 SKIN BOEING 757 757212 NM FS 620, S-16L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 751AT 23125 FUSELAGE / SKIN / FS 620 / STRG. 16L-17L : DENT CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND WITH SEVERAL DENTS NEAR FS 620 AND STRINGERS 16L & 17L. THE DENTS WERE REMOVED WITH A 7" X 6" CUTOUT AND A 2.5" X 3.5" CUTOUT. BOTH CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL ALUMINUM DOUBLER PER ER/A 380995-14, REV A. 2 L 7 2 4F RT A2NM 2001072700024 20010727 00024 NM 2001 7 27 DL72S011177 1 20010716 A 5300 UNK CLIP BOEING 727 727232 1384082 NM STA 1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 544DA 22493 FOUND ON E2 LETTER CK SKIN CLIP CRACKED FWD STA 1263 ABOVE STR 12R. REPAIRED PER B727 DAL DRD 53-10-4D FIG 803D. 2 L 7 3 4F A3WE 2001072700025 20010727 00025 NM 2001 7 27 DL72S011178 1 20010716 A 5300 UNK WEB BOEING 727 727232 1384082 NM STA 1214 R/H CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 544DA 22493 FOUND ON E2 LETTER CK R/H INBD VERT TORQUE BOX WEB CRACKED AT UPPER END STA 1214 R/H. REPAIRED PER MM 53-11-000-8. 2 L 7 3 4F A3WE 2001072700026 20010727 00026 NM 2001 7 27 DL73K011179 1 20010717 A 5711 654532413 SPAR CAP BOEING 737 737232 1384475 NM WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 317DL 23089 A CRACK WAS FOUND IN THE REAR SPAR UPPER CAP AT RSS 224.14. A REPAIR WAS INSTALLED PER BOEING REWORK DRAWING 65C30105. THE DAMAGE WAS FOUND DURING AN INSPECTION AT HMV. 2 L 7 2 4F RT A16WE 2001072700027 20010727 00027 NM 2001 7 27 DL73K011181 1 20010717 A 5330 654580026 SKIN BOEING 737 737232 1384475 NM SKIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 317DL 23089 A CRACK WAS FOUND IN THE FUSELAGE SKIN FORWARD OF THE LOWER AFT CORNER. THE DAMAGE WAS REPAIRED PER BOEING S/B 737-53- 1083. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001072700028 20010727 00028 NM 2001 7 27 DL72S011191 1 20010718 A 5200 UNK SEAL BOEING 727 727232 1384082 NM 1-L DOOR TORN A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 544DA 22493 ON CLIMBOUT A LOUD SQUEAL DEVELOPED FROM FORWARD LEFT DOOR. NOISE WAS TOO LOUD TO CONTINUE FLIGHT. DECENDED TO 10,000 FT AND CHANGED CABIN TO 2.0 PSID. NOISE STOPPED. CA RPD L1 DOOR SEAL. 2 L 7 3 4F A3WE 2001072700029 20010727 00029 NM 2001 7 27 DL73K011193 1 20010719 A 5551 FITTING BOEING 737 737232 1384475 NM HOR. STAB. CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 317DL 23089 CORROSION WAS FOUND RH AND LH HORIZONTAL STABILIZER ATTACH FITTINGS ON THE FACES AND BORES. THE CORROSION WAS REMOVED AND OVERSIZED BUSHINGS WERE INSTALLED PER ERA 397745-14. THE DAMAGE WAS FOUND DURING INSPECTION AT HMV. 2 L 7 2 4F RT A16WE 2001072700030 20010727 00030 NM 2001 7 27 DL73K011194 1 20010719 A 5342 FITTING BOEING 737 737232 1384475 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 317DL 23089 CORROSION WAS FOUND ON THE LUG BORES AND FACES OF THE RH ANDLH HORIZONTAL STABILIZER CLEVIS ATTACH FITTINGS. THE CORROSION WAS REMOVED AND OVERSIZED BUSHINGS INSTALLED. 2 L 7 2 4F RT A16WE 2001072700031 20010727 00031 NM 2001 7 27 DL73K011196 1 20010719 A 5330 654577518 SKIN BOEING 737 737232 1384475 NM FS 767 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 317DL 23089 THE FUSELAGE SKIN SKIN JUST FWD OF FS 767 AT STR 19R UNDER THE WING-TO-BODY FAIRING WAS FOUND CRACKED. THE CRACK WAS LIMITED TO THE SKIN ONLY AND WAS CUT OUT. THE DAMAGE WAS REPAIRED WITH AN EXTERNAL DOUBLER. THE DAMAGE WAS FOUND DURING HMV. 2 L 7 2 4F RT A16WE 2001072700032 20010727 00032 NM 2001 7 27 DL76G011202 1 20010719 A 2820 1872M82G01 MANIFOLD BOEING 767 7673P6 1385105 NM GE CF6 CF680C2B6 30025 NE #2 ENGINE CRACKED A DALA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 SO 27 153DL 33730 24985 695521 RT ENG FUEL MANIFOLD LEAK.REMOVED AND REPLACED FUEL PIPE. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS 2 L 7 2 4F 4 F RT A1NM E13NE 2001072700033 20010727 00033 NM 2001 7 27 DL73K011204 1 20010720 A 5330 SKIN BOEING 737 737232 1384475 NM FS 960, S-17L CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 304DL 23076 FUSELAGE / SKIN ASSY / AFT ENTRY DOOR (L2) / LWR FWD CORNER:CRACK REPAIR THE LOWER FORWARD CORNER OF THE AFT ENTRY DOOR CUTOUT WAS FOUND WITH A TYPICAL CRACK THROUGH THE SKIN AND UNDERLYING BEAR STRAP. THE CRACK WAS REMOVED WITH A 1.25" X 2.2" CUTOUT. THE CUTOUT WAS REPAIRED WITH A STACK-UP OF THREE EXTERNAL ALUMINUM REPAIR DOUBLERS INSTALLED PER ER/A 381368-14, REV A. 2 L 7 2 4F RT A16WE 2001072700034 20010727 00034 NM 2001 7 27 DLM88011212 1 20010722 A 2560 A1181030 STRAP DOUG MD88 MD88 3023688 NM AFT DOOR BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 960DL 49979 IRR- AFT DOOR FLASHLIGHT SEAL BROKEN CA- REPLACED SEAL 2 L 7 2 4F RT A6WE 2001072700035 20010727 00035 NM 2001 7 27 DL72S011219 1 20010704 A 5754 UNK RIB BOEING 727 727232 1384082 NM #6 SLAT TRACK CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 533DA 22046 AT HMV FOUND RIB CRACKED #3 O/B RIB OF O/B SLAT TRACK(#6 SLAT) CORR: TRIMED OUT DAMAGE FABD REPAIR DOUBLER PER MM 57-54-000-8,REMOVED SLAT TRACK,OK INSTL REPAIR,INSTLD #3 OB RIBDOUBLE R PER MM 57-54,INSTLD DOUBLER AND SLAT TRACK PER MM 57-51. 2 L 7 3 4F A3WE 2001072700036 20010727 00036 NM 2001 7 27 DL72S011223 1 20010724 A 5700 UNK ANGLE BOEING 727 727232 1384082 NM #2 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 FOUND ON MV4 1/4 CRACK IN #2 SLAT COVE SKIN ANGLE BELOW TAI DUCT. REPAIRED PER MM 57-54-000-8 2 L 7 3 4F A3WE 2001072700037 20010727 00037 NM 2001 7 27 DL72S011231 1 20010725 A 5700 UNK ANGLE BOEING 727 727232 1384082 NM RT WING SPAR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 543DA 22392 FOUND ON F1 LETTER CK NUMBER 8 SLAT ACTUATOR INBD ATTACH ANGLE CRACKED . REPAIRED PER MM 57-20-021-8. 2 L 7 3 4F A3WE 2001072700038 20010727 00038 NM 2001 7 27 DL72S011234 1 20010725 A 5700 UNK BRACKET BOEING 727 727232 1384082 NM LEFT WING L/E CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 543DA 22392 3 INCH CRACK AT #1 SLAT ACT. ATTACH I/B AND O/B BRACKET __REPAIRED PER M/M 57-20-021-8 2 L 7 3 4F A3WE 2001072700039 20010727 00039 NM 2001 7 27 DL72S011235 1 20010725 A 5700 UNK ANGLE BOEING 727 727232 1384082 NM LEFT WING L/E CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 543DA 22392 COVE SKIN ATTACH ANGLE CRACKED BELOW TAI DUCT #2 SLAT __REPAIRED PER MM 57-54-000-8 2 L 7 3 4F A3WE 2001072700040 20010727 00040 NM 2001 7 27 DL72S011236 1 20010725 A 5700 UNK ANGLE BOEING 727 727232 1384082 NM LEFT WING L/E CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 543DA 22392 COVE SKIN ATTACH ANGLE CRACKED BELOW TAI DUCT #3 SLAT __REPAIRED PER MM 57-54-000-8 2 L 7 3 4F A3WE 2001072700041 20010727 00041 NM 2001 7 27 DL72S011242 1 20010726 A 5300 UNK SKIN BOEING 727 727232 1384082 NM PNL 3903 CUTOUT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 528DA 21702 .25 INCH CRACK IN EMPENAGE SKIN AT AFT I/B CORNER OF GROUND AIR CONNECTION ACCESS DOOR CUTOUT. REPAIRED PER M/M 53-30-00 0-8 PG 2. 2 L 7 3 4F A3WE 2001072700043 20010727 00043 CE 2001 7 27 C2XA01CL150 1 20010611 A 5210 SCREW BEECH 1900 1900D 1154162 CE PAX DOOR LOOSE A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 48544 UE183 CLE FLIGHT 3104 THE CREW REPORTED THE MAIN DOOR HANDLE ON OUTSIDE OF AIRCRAFT WOULD NOT LOCK IN THE CLOSED POSITION. M AINTENANCE TIGHTENED SCREWS IN THE DOOR HANDLE BELLCRANK ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELE ASED FOR SERVICE. 2 L 7 2 4T RT A24CE 2001072700044 20010727 00044 CE 2001 7 27 C2XA01CL154 1 20010624 A 2916 RESERVOIR BEECH 1900 1900D 1154162 CE HYD SYSTEM LACK OF LUBE A C2XA K NONE J WARNING INDICATION AP APPROACH 1 SW 27 87557 UE246 CLE FLIGHT 3307 THE CREW REPORTED WHEN THE LANDING GEAR WAS EXTENDED ON FINAL APPROACH THE RIGHT GEAR WAS DELAYED FOR AB OUT ONE MINUTE. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND SERVICED THE LANDING GEAR HYDR AULIC RESERVOIR. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT A24CE 2001072700045 20010727 00045 NE 2001 7 27 C2XA01CL157 2 20010627 A 7324 FUEL LINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ENGINE LOOSE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 81553 UE222 CLE FLIGHT 3375 THE CREW REPORTED A FUEL SMELL IN THE CABIN WHILE TAXIING. THE BLEED AIR VALVES WERE ON ALONG WITH THE BLOWERS. MAINTENANCE INSPECTED AND RESECURED THE FUEL LINE ON THE FLOW DIVIDER ON THE NR 2 ENGINE. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T 4 T RT A24CE E26NE 2001072700046 20010727 00046 CE 2001 7 27 C2XA01CL158 1 20010701 A 7333 12281301 TRANSMITTER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ENGINE ERRATIC A C2XA K NONE O OTHER NR NOT REPORTED 1 SW 27 69549 3466 155 UE194 CLE THE CREW REPORTED NR 1 FUEL FLOW GAUGE FLUCTUATES. MAINTENANCE REPLACED THE NR 1 ENGINE FUEL FLOW TRANSMITTER. OPE RATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T 4 T RT A24CE E26NE 2001072700047 20010727 00047 GL 2001 7 27 C2XA01CL159 2 20010630 A 7200 23070991 ENGINE EMB 145 EMB145LR SO ALLSN AE300 AE3007A GL LEFT FLAMED OUT A C2XA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SW 27 13958 7116 2661 145085 311031 ACY-CLE FLIGHT 3489 THE CREW REPORTED THE NR 1 ENGINE FLAMED OUT CLIMBING OUT OF 28,000 FT THE AIRCRAFT DIVERTED INTO BW I AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE AND OPERATIONAL CHECKS WERE GOOD. THE AIRC RAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2001072700048 20010727 00048 EU 2001 7 27 C2XA01CL160 1 20010701 A 3231 S5397131700200 LINK AEROSP ATR42 ATR42320 8680930 EU RT MLG DOOR BROKEN A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 14832 187 CLE FLIGHT 2966 THE CREW REPORTED THE RIGHT MAIN GEAR DOOR DOES NOT CLOSE IN FLIGHT. MAINTENANCE INSPECTED AND FOUND T HE RIGHT MAIN GEAR DOOR LINK ASSEMBLY WAS BROKEN. THE LINK ASSEMBLY WAS REPLACED ALONG WITH THE MAIN GEAR DOOR ASSEMBLY . OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001072700050 20010727 00050 SO 2001 7 27 C2XA01IA259 1 20010601 A 3230 355022002 CONTROL UNIT EMB 145 EMB145LR SO LANDING GEAR MALFUNCTIONED A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 12996 145296 YUL - FLIGHT 3675, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE CREW CYCLED THE LANDING GEAR IN ACCOR DANCE WITH THE QRH, AND THE GEAR RETRACTED SUCCESSFULLY AFTER SIX ATTEMPTS. THE AIRCRAFT CONTINUED TO CLE WHERE IT LAND ED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONICS UNIT. OPERATIONALLY CHECKED THE GEA R WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO FLIGHT. 2 L 7 2 4T RT T00011AT 2001072700052 20010727 00052 SO 2001 7 27 C2XA01IA260 1 20010604 A 2530 500064001 COFFEEMAKER EMB 145 EMB145LR SO GALLEY FAULTY A C2XA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 16918 145397 IAH - FLIGHT 4028, THE CREW REPORTED A SMOKE ODOR COMING FROM THE GALLEY AREA IN FLIGHT. THE POWER FOR THE GALLEY WAS S HUT OFF AND THE CIRCUIT BREAKERS FOR THE GALLEY WERE PULLED, WITH DISSIPATION OF THE ODOR FOLLOWING. THE AIRCRAFT CONTI NUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED COFFEEMAKER, AND THE AIRCRA FT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001072700054 20010727 00054 SO 2001 7 27 C2XA01IA261 1 20010530 A 3350 RPS1B BATTERY PACK EMB 145 EMB145 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16927 145006 IAH - FLIGHT 4038, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENA NCE INSPECTED THE AIRCRAFT, RESET THE EMERGENCY LIGHT SWITCH, AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACKS, A ND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001072700057 20010727 00057 NE 2001 7 27 C2XA01IA262 2 20010605 A 7510 38E966A REGULATOR EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE LEAKING A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 17728 120182 CRP - FLIGHT 2946, THE CREW REPORTED THAT DURING FLIGHT AN ENGINE 12 DUCT LEAK LIGHT ILLUMINATED. THE CREW SHUT DOWN TH E NUMBER ONE ENGINE, AND DIVERTED TO CRP WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED T HE LEFT HAND DE-ICE PRESSURE REGULATOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2001072700058 20010727 00058 SO 2001 7 27 C2XA01IA263 1 20010604 A 2120 SMOKE EMB 120 EMB120ER 3260203 SO CABIN DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 15725 120173 SHV - THE CREW REPORTED SMOKE IN THE CABIN, MAINTENANCE RESET THE RIGHT MAIN LANDING GEAR AIR/GROUND CIRCUIT BREAKER, AN D THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001072700059 20010727 00059 SO 2001 7 27 C2XA01IA264 1 20010606 A 3350 GE1317 LIGHT EMB 145 EMB145ER SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14939 145030 CLE- DURING POST FLIGHT INSPECTION THE CREW NOTED THAT THE EMERGENCY LIGHT ABOVE ROW 11 AND 12 FAILED TO ILLUMINATE. CL E- MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BULB, PERFORMED A OPERATIONAL CHECK. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001072700060 20010727 00060 SO 2001 7 27 C2XA01IA265 1 20010610 A 3350 276005 FUSE EMB 145 EMB145 SO CABIN BLOWN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12967 145133 IAH- DURING 5A CHECK IT WAS NOTED THAT THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS FAILED TO ILLUMINATE. IAH- MAINTE NANCE REMOVED AND REPLACED THE FUSE, PERFORMED A OPERATIONAL CHECK. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001072700061 20010727 00061 SO 2001 7 27 C2XA01IA266 1 20010614 A 3030 CS500060D4A RELAY EMB 135 EMB135LR SO COCKPIT BURNED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 28518 135334 MOB- AFTER TAKEOFF OF FLIGHT 3911 DURING CLIMB, AT 10,000 FEET THE CREW RECEIVED PITOT 2 FAIL MESSAGE, ALONG WITH ELECT RIC SMOKE IN THE COCKPIT. THE AIRCRAFT RETURNED TO MOB, LANDED WITHOUT INCIDENT. MOB- MAINTENANCE TROUBLESHOT THE NUM BER 2 PITOT HEAT SYSTEM AND FOUND A BURNED RELAY ON THE RELAY PANEL. THE AIRCRAFT WAS RELEASED FOR FERRY FLIGHT FROM MO B TO IAH. IAH- MAINTENANCE REMOVED AND REPLACED RELAY K0054. PERFORMED A OPERATIONAL CHECK OF THE NUMBER 2 PITOT HEAT SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT TOOO11AT 2001072700062 20010727 00062 SO 2001 7 27 C2XA01IA267 1 20010611 A 2150 22040452 ACM EMB 120 EMB120ER 3260203 SO A/C BAY SEIZED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 16723 120169 IAH- THE CREW NOTICED A TRACE OF SMOKE IN THE CABIN. IAH- MAINTENANCE UNSTUCK THE NUMBER 2 ACM, PERFORMED AN OPERATION AL CHECK OF THE COOLING SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001072700063 20010727 00063 SO 2001 7 27 C2XA01IA268 1 20010612 A 3350 7287580509 LIGHT EMB 145 EMB145 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13997 145298 BNA- DURING PREFLIGHT THE CREW NOTED THE EMERGENCY FLOOR PATH LIGHTING AT SEATS 7 AND 8A DID NOT ILLUMINATE. BNA- MAI NTENANCE PLACED THE EMERGENCY LIGHTING SYSTEM ON MEL. LFT- MAINTENANCE REMOVED AND REPLACED THE FLOOR PATH LIGHT STRIP AT SEATS 7 AND 8A. PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED. CLEARED THE MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001072700064 20010727 00064 EU 2001 7 27 C2XA01IA271 1 20010621 A 3350 3011210 LIGHT AEROSP ATR42 ATR42320 8680930 EU PAX DOOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14815 104 IAH - DURING 2A INSPECTION, THE PASSENGER DOOR EMERGENCY LIGHT ASSEMBLY WAS FOUND TO BE INOP. MAINTENANCE REMOVED AND R EPLACED THE AFFECTED LIGHT ASSEMBLY IN ACCORDANCE WITH 33-51-24, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001072700065 20010727 00065 SO 2001 7 27 C2XA01IA272 1 20010622 A 3350 ML1317 LIGHT EMB 145 EMB145LR SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18982 145223 IAH- DURING 5A INSPECTION MAINTENANCE NOTED THAT THE AFT CEILING EMERGENCY LIGHT FAILED TO ILLUMINATE DURING OPERATIONAL TEST. IAH- MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED AND THE AI RCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001072700066 20010727 00066 EU 2001 7 27 C2XA01IA275 1 20010621 A 3350 AD3127 POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 19812 099 IAH- MAINTENANCE, WHILE PERFORMING A LINE CHECK MAINTENANCE NOTED THAT THE CABIN EMERGENCY FLOOR LIGHTS FAILED TO ILLUMI NATE DURING TEST. IAH- MAINTENANCE REMOVED AND REPLACED THE LEFT HAND FORWARD POWER SUPPLY NUMBER 2. PERFORMED A OPERA TIONAL CHECK, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001072700067 20010727 00067 SO 2001 7 27 C2XA01IA278 1 20010502 A 5720 12017063009 SUPPORT EMB 120 EMB120ER 3260203 SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 40717 120133 SJK - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, ONE SKIN SUPPORT WAS FOUND TO BE CRACKED ON THE LEFT HAND WING UPPE R SURFACE AT RIB 21. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETU RN TO SERVICE. 2 L 7 2 4T RT A31SO 2001072700069 20010727 00069 SO 2001 7 27 C2XA01IA280 1 20010426 A 5280 12019412002 STRUCTURE EMB 120 EMB120ER 3260203 SO RT MLG DOOR BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 40717 120133 SJK - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE RIGHT HAND MAIN LANDING GEAR DOOR PROFILE WAS FOUND TO BE BROKE N. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PROFILE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001072700070 20010727 00070 2001 7 27 ZW0A0105901 4 20010726 A 2565 11317 SLIDE DOUG DC9 DC931 3022065 WP L1 DOOR A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 989Z 47135 THE LEFT SIDE NUMBER 1 CABIN DOOR ESCAPE SLIDE PRESSURE WAS LOW. REPLACED THE SLIDE. CHECK-C 5-10-01 STL. --CLOSED-- 2 L 7 2 4F A6WE 2001072700074 20010727 00074 SO 2001 7 27 C2XA01IA283 1 20010626 A 4900 APU EMB 145 EMB145LR 3260212 SO APU BAY ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 13989 145271 LIT - FLIGHT 4047, THE CREW REPORTED A STRONG FUEL ODOR AT FL350 WITH BOTH BLEEDS AND PACKS SELECTED. THE AIRCRAFT LAND ED AT LIT WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT. PERFORMED OPERATIONAL TESTS WITH BOTH ENGINES RUNN ING, AND NO DEFECTS NOTED. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RETURNED TO IAH ON FLIGH T 4367 WHERE MAINTENANCE FOUND THE FUEL ODOR TO BE COMING FROM THE APU. MAINTENANCE PLACED THE APU ON MEL 49-00-00 CAT C CONTROL NUMBER 011493, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001072700075 20010727 00075 SO 2001 7 27 C2XA01IA285 1 20010630 A 3350 12021299001 LIGHT EMB 120 EMB120ER 3260203 SO EXTERIOR INOPERATIVE A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 15726 120174 IAH - THE LEFT HAND FORWARD OVERWING EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE AND PLACED ON MEL CONTROL NUMBER 013249. THE AIRCRAFT ARRIVED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY. CLEARE D THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001072700077 20010727 00077 NM 2001 7 27 USAABB01048 1 20010626 A 3350 233T321033 PANEL BOEING 767 767201 1385125 NM COCKPIT FAULTY A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 645US 23897 PHL - FLT 192 - EN ROUTE CLT-FRA, THE INTERIOR EMERGENCY LIGHTS ILLUMINATED AND COULD NOT BE TURNED OFF. THE LIGHTS ALS O VARIED IN INTENSITY FROM VERY BRIGHT TO DIM. THE FLIGHT DIVERTED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTEN ANCE REPLACED THE EMERGENCY LIGHT CONTROL PANEL. (M) 2 L 7 2 4F RT A1NM 2001072700078 20010727 00078 EU 2001 7 27 USAASA01029 1 20010627 A 3350 E0062B1A4AD0A SWITCH AIRBUS 320 A320214 EU COCKPIT SHORTED A USAA K NONE O OTHER NR NOT REPORTED 1 EA 19 122UW 1298 BOS - THE EMERGENCY LIGHTS INTERMITTENTLY ILLUMINATE WITH THE SWITCH IN THE ARMED POSITION. MAINTENANCE REPLACED OVERHE AD EMERGENCY LIGHT SWITCH (4WL). OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2001072700079 20010727 00079 NM 2001 7 27 USAASB01184 1 20010626 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM AFT CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 391US 23313 GSO - MAINTENANCE FOUND THE EMERGENCY LIGHTS ON THE SEATS IN AFT CABIN DIM. MAINTENANCE REMOVED AND REPLACED THE BATTER Y PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001072700080 20010727 00080 NM 2001 7 27 USAA010726 1 20010517 A 5300 ANGLE BOEING 737 737301 1384611 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND ANGLE CRACKED 1.5 INCHES, BS 616 BELOW STRINGER S17R. REMOVED DAMAGED, INSTALLED FILLER AND DOUBLER PER TYP ICAL REPAIR 53-62-01. (M) 2 L 7 2 4F RT A16WE 2001072700081 20010727 00081 SO 2001 7 27 C2XA01IA287 1 20010622 A 5411 12048450001 FRAME EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15725 120173 IAH - DURING 2A INSPECTION, THE LEFT HAND NACELLE LOWER HALF FRAME FOR THE OUTBOARD AFT GEAR DOOR WAS FOUND TO BE CRACKE D. MAINTENANCE PERFORMED A DOUBLER REPAIR ON THE AFFECTED FRAME IN ACCORDANCE WITH EMB120-SRM 54-20-04, AND THE AIRCRAF T WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001072700082 20010727 00082 SO 2001 7 27 C2XA01IA288 1 20010702 A 6123 CONTROLLER EMB 120 EMB120ER 3260203 SO PROPELLER MALFUNCTIONED A C2XA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 27 15726 120174 IAH - FLIGHT 3315, THE CREW REPORTED AN AUTOFEATHER ON TAKEOFF ROLL. THE CREW ABORTED TAKEOFF, AND RETURNED TO THE GATE WHERE MAINTENANCE PERFORMED OPERATIONAL TEST ON THE PROPELLER CONTROL SYSTEM WITH NO DEFECTS NOTED. THE AIRCRAFT WAS T HEN APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001072700083 20010727 00083 SO 2001 7 27 C2XA01IA289 1 20010704 A 3350 7287580501 LIGHT EMB 145 EMB145LR SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15985 145248 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT A SECTION OF THE AISLE PATH EMERGENCY EXIT LIGHTS WERE INOPERA TIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF AISLE PATH LIGHTING, AND THE AIRCRAFT WAS APPROVED FOR R ETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001072700084 20010727 00084 SO 2001 7 27 C2XA01IA290 1 20010621 A 3610 S2D226 O-RING EMB 145 EMB145LR SO PNEUMATIC SYS BROKEN A C2XA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 SW 27 15985 145248 MKE - THE CREW REPORTED A NUMBER ONE ENGINE BLEED LEAK WARNING. THE AIRCRAFT RETURNED TO MKE WITHOUT INCIDENT. MAINTEN ANCE REMOVED AND REPLACED THE O-RINGS ON THE NUMBER ONE ENGINE T-TUBE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI CE. 2 L 7 2 4T RT T00011AT 2001072700088 20010727 00088 SO 2001 7 27 C2XA01IA291 1 20010702 A 2824 293003101 CONNECTOR EMB 145 EMB145LR SO DEFUEL VALVE DIRTY A C2XA A UNSCHED LANDING K P FLUID LOSS NO WARNING INDICATION CL CLIMB 1 SW 27 16954 145072 MEM- DURING TAKEOFF THE AIR TRAFFIC CONTROL AT MEM REPORTED TO THE CREW THAT FLUID WAS COMING OFF BOTH WINGS. THE CREW NOTED THAT THE FUEL QUANTITY DECREASED BY 600 POUNDS, AND THAT FUEL TRANSFERRED TO THE LEFT WING WITH THE CROSSFEED OFF. THE AIRCRAFT RETURNED TO MEM WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THAT THE DEFUELING VALVE CONNECTOR WAS DIRTY. MAINTENANCE CLEANED THE AFFECTED CONNECTOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001072700090 20010727 00090 SO 2001 7 27 C2XA01IA293 1 20010708 A 2120 ODOR EMB 145 EMB145LR SO CABIN DETECTED A C2XA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 18982 145223 IAH - FLIGHT 3925, THE CREW REPORTED AN ELECTRICAL BURNING SMELL IN THE AFT CABIN DURING CRUISE, AND AN OCCASIONAL SMELL IN THE COCKPIT AS WELL. THE CREW DEACTIVATED THE NUMBER TWO BLEED AS A PRECAUTION WITH NO CHANGE IN ODOR. THE AIRCRAF T LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND OPERATIONALLY CHECKED THE APU AND ENGINE B LEED SYSTEMS WITH NO DEFECTS NOTED. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001072700092 20010727 00092 SO 2001 7 27 C2XA01IA294 1 20010628 A 2150 8152403 ACM EMB 145 EMB145ER SO A/C BAY FAULTY A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 12934 145019 CLE - FLIGHT 4378, THE CREW REPORTED A STRONG SMOKE SMELL WHEN OPERATING ONLY PACK ONE ON THE GROUND. MAINTENANCE REMOV ED AND REPLACED THE NUMBER ONE AIR CYCLE MACHINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001072700100 20010727 00100 SO 2001 7 27 C2XA01TY094 1 20010605 A 3220 13889 BEARING EMB 145 EMB145LR SO NLG DISINTEGRATED A C2XA K NONE E VIBRATION/BUFFET LD LANDING 1 SW 27 14920 145380 EWR FLIGHT 4142 CREW REPORTED THAT ON TOUCHDOWN THE NOSE GEAR IMMEDIATELY BEGAN TO VIBRATE. ON THE POST FLIGHT INSPEC TION THE NOSE WHEEL BEARING WAS DISCOVERED TO BE DISINTEGRATED. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR STRUT ASSEMBLY IAW EMB-145 MM 32-20-01. THE NOSE GEAR WHEELS ASSEMBLIES WERE ALSO REMOVED AND REPLACED IAW EMB-145 MM 3 2-49-05. OPERATIONAL CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001072700101 20010727 00101 SW 2001 7 27 IIF2001F00000 1 20010611 A 6520 406040016101 SHAFT BELL BELL 407 407 SW T/R GEAR BOX CORRODED B IIFR K NONE O OTHER IN INSP/MAINT 1 SW 03 407PR 2500 A887 53232 DURING THE FIRST 2500 HOUR OVERHAUL, FOUND CORROSION ON INBOARD SPLINES AND PITTING BEYOND LIMITS. PROBABLE CAUSE DUE T O BREAKDOWN GREASE. SUGGEST THAT TAIL ROTOR BUB AND BLADES ASSEMBLY NEEDS TO BE REMOVED PERIODICALLY AND SPLINES INSPEC TED AND LUBRICATED WITH PROPER GREASE, THEN REINSTALLED ON AIRCRAFT. THE ABOVE PROBLEM WAS FOUND DURING THE 2500 HOUR O VERHAUL OF THE TAIL ROTOR GEAR BOX. 1 G 7 1 3U O H2SW 2001072700102 20010727 00102 SW 2001 7 27 IIF2001F00001 1 20010611 A 6220 407101103101 PITCH HORN BELL BELL 407 407 SW MAIN ROTOR HUB CORRODED B IIFR K NONE O OTHER IN INSP/MAINT 1 SW 03 407PR 2500 A254 53232 DURING THE FIRST 2500 HOUR OVERHAUL, IT WAS FOUND THAT THE PITCH HORNS PN 407-010-103-101, HAD CORROSION AND PITTING OF AFT SURFACE OF PITCH HORN UNDER THE WEAR PLATE. PART IS BONDED TO PITCH HORN WITH METAL SET. SUGGEST THE EDGES OF PLAT E BE PROSEALED AFTER METAL SET HAS CURED. THREE OF THE FOUR PITCH HORNS HAD TO BE SCRAPPED. 1 G 7 1 3U O H2SW 2001072700103 20010727 00103 SW 2001 7 27 IIF2001F00002 1 20010611 A 6220 407010103101 PITCH HORN BELL BELL 407 407 SW MAIN ROTOR HUB CORRODED B IIFR K NONE O OTHER IN INSP/MAINT 1 SW 03 407PR 2500 A254 53232 DURING THE FIRST 2500 HOUR OVERHAUL, IT WAS FOUND THAT THE PITCH HORNS PN 407-010-103-101, HAD CORROSION AND PITTING OF AFT SURFACE OF PITCH HORN UNDER THE WEAR PLATE. PART IS BONDED TO PITCH HORN WITH METAL SET. SUGGEST THE EDGES OF PLAT E BE PRO SEALED AFTER METAL SET HAS CURED. THREE OF THE FOUR PITCH HORNS HAD TO BE SCRAPPED. 1 G 7 1 3U O H2SW 2001072700104 20010727 00104 SW 2001 7 27 IIF2001F00003 1 20010611 A 6220 407010103101 PITCH HORN BELL BELL 407 407 SW MAIN ROTOR HUB CORRODED B IIFR K NONE O OTHER IN INSP/MAINT 1 SW 03 407PR 2500 A254 53232 DURING THE FIRST 2500 HOUR OVERHAUL, IT WAS FOUND THAT THE PITCH HORNS PN 407-010-103-101, HAD CORROSION AND PITTING OF AFT SURFACE OF PITCH HORN UNDER THE WEAR PLATE. PART IS BONDED TO PITCH HORN WITH METAL SET. SUGGEST THE EDGES OF PLAT E BE PROSEALED AFTER METAL SET HAS CURED. THREE OF THE FOUR PITCH HORNS HAD TO BE SCRAPPED. 1 G 7 1 3U O H2SW 2001072700105 20010727 00105 SO 2001 7 27 C2XA01TY095 1 20010629 A 2740 3621001007 CONTROL UNIT EMB 145 EMB145 SO HORIZ STAB FAILED A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 14977 4435 4435 145175 CLT FLIGHT 4258 CREW REPORTED THAT DURING THEIR PRE-FLIGHT CHECKS THE PITCH TRIM NR 2 WAS INOPERATIVE. THE AIRCRAFT W AS MAINTENANCE FERRIED TO RIC AND THE HORIZONTAL STAB CONTROL UNIT WAS REMOVED AND REPLACED IAW EMB-145 MM 27-40-01. TH E OPERATIONAL CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001072700106 20010727 00106 SW 2001 7 27 IIF2001F00004 1 20010521 A 5302 40703080101 SKIN BELL BELL 407 407 SW HORZONTAL STAB CRACKED B IIFR K NONE O OTHER IN INSP/MAINT 1 SW 03 407JR 2225 53244 53245 WHILE COMPLYING WITH DAILY AIRCRAFT INSPECTION, FOUND A CRACK ON TAILBOOM, LEFT SIDE AT HORIZONTAL STABILIZER AREA. 1 G 7 1 3U O H2SW 2001072700107 20010727 00107 GL 2001 7 27 C2XA01TY096 2 20010630 A 7200 AE3007A1 ENGINE EMB 145 EMB145 SO ALLSN AE300 AE3007A GL LEFT MAKING METAL A C2XA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 SW 27 13958 7107 7107 145085 CAE311031 BWI FLIGHT 3489 CREW REPORTED THE LEFT HAND ENGINE FLAMED OUT CLIMBING OUT OF 28,000 FEET AT CLIMB POWER, THE ENGINE WO ULD NOT RESTART. THE AIRCRAFT LANDED AT BWI WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND E NGINE IAW CONTINENTAL EXPRESS TASK CARD 6271001, AFTER METAL WAS FOUND ON THE CHIP DETECTORS. OPERATIONAL AND LEAK CHEC KS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001072700108 20010727 00108 SO 2001 7 27 C2XA01TY097 1 20010707 A 7160 14575122005 NOSE COWL EMB 135 EMB135ER 3260203 SO LT ENGINE DENTED A C2XA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 27 14505 145192 TYS DURING A SCHEDULED INSPECTION THE LEFT HAND ENGINE INLET WAS FOUND DENTED ON THE LOWER EXTERNAL SURFACE. MAINTENAN CE ACCOMPLISHED A BLEND REPAIR IAW EMB-GST 2230/01, THE REPAIR WAS SATISFACTORY. AIRCRAFT RELEASED FOR SERVICED. 2 L 7 2 4F RT T00011AT 2001072700109 20010727 00109 NE 2001 7 27 C8GA20010013 2 20010606 A 7200 ENGINE BOEING 727 727223 1384074 NM PWA JT8 JT8D15 52051 NE NR 3 OUT OF ADJ A C8GA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 15 713AA 22469 700751 FLT 721 FROM FLL TO TOL DURING TAKEOFF NR 3 ENGINE RED LINE WHEN TAKEOFF POWER WAS APPLIED TO ENGINE. THROTTLE WAS RET ARDED APPROXIMATELY .15 EPR'S TO KEEP ENGINE FROM EXCEEDING LIMITS. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO BLOCK WITH OUT INCIDENT. PERFORMED ENGINE RUN AND TRIMMED NR 3 ENGINE IAW MM 71-00-30, ENGINE OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2001072700110 20010727 00110 NE 2001 7 27 C8GA20010015 2 20010611 A 7200 ENGINE BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE NR 3 OUT OF ADJ A C8GA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 15 713AA 22469 FLT 713 FROM JAX TO MCO. DURING THE TAKEOFF ROLL, THE NR 3 ENGINE EGT WENT TO RED LINE 630 DEGREES, THROTTLE PULLED BAC K NOT TO EXCEED EGT PARAMETERS. AIR TURNBACK TO JAX AND LANDED WITHOUT INCIDENT. PERFORMED ENGINE RUN AND ADJUSTED EGT ON NR 3 ENGINE AND SYSTEM OPS CHECK GOOD IAW MM 77-20 AND AIRCRAFT WAS RETURN TO SERVICE. 2 L 7 3 4F 4 F RT A3WE E2EA 2001072700111 20010727 00111 EU 2001 7 27 CHQA 1 20010520 A 7500 DUCT SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RT ENGINE LEAKING A CHQA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 11 123CQ 123 123 RIGHT ENGINE BLEED LEAK. 2 L 7 2 4T 4 T RT A52EU E8NE6 2001072700115 20010727 00115 NE 2001 7 27 KBMA88752 2 20010507 A 7421 9550168760 IGNITER SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE RIGHT INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 350SH 356 2957 RIGHT HAND IGNITER REPORTED INOPERATIVE. REPLACED WITH NEW IGNITER, AS REQUIRED. 1 G 7 1 3U 3 U NC H9EU E19EU 2001072700116 20010727 00116 SO 2001 7 27 CHQA2000004 1 20010528 A 5610 HANDLE EMB 145 EMB145LR SO COCKPIT VIBRATES A CHQA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 11 269 145293 AFTER TAKEOFF, CREW EXPERIENCED NOISE AND VIBRATION THROUGH LEFT WINDOW HANDLE. 2 L 7 2 4T RT T00011AT 2001072700119 20010727 00119 EU 2001 7 27 CHQA20010866 1 20010606 A 2750 CONTROL VALVE SAAB SF340 SF340A 7850100 EU T/E FLAP FAILED A CHQA K NONE F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 GL 11 108 340A108 FLAPS WON`T DEPLOY DURING LANDING. MAINTENANCE REMOVED AND REPLACED FLAP CONTROL VALVE. 2 L 7 2 4T RT A52EU 2001072700120 20010727 00120 EU 2001 7 27 CHQA200125619 1 20010619 A 7910 OIL SYSTEM SAAB SF340 SF340A 7850100 EU RT ENGINE LACK OF LUBE A CHQA D RETURN TO BLOCK O OTHER CL CLIMB 1 GL 11 125 125 A/C RETURNED TO FIELD AFTER RT OIL PRESSURE FLUX. SAME OCCURRENCE TWICE ON 6-19. MAINTENANCE SERVICED OIL LEVEL. 2 L 7 2 4T RT A52EU 2001072700121 20010727 00121 EU 2001 7 27 CHQA20013561 1 20010601 A 2613 CONNECTOR SAAB SF340 SF340A 7850100 EU RT ENGINE DIRTY A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 035 340A035 RIGHT TAIL PIPE HOT LIGHT CAME ON AFTER TAKEOFF. A/C RETURNED TO FIELD. MAINTENANCE CLEANED SENSOR CANNON PLUG. 2 L 7 2 4T RT A52EU 2001072700122 20010727 00122 NE 2001 7 27 CHQA200138531 2 20010531 A 7321 ECU SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE MALFUNCTIONED A CHQA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS UK UNKNOWN 1 GL 11 138 138 461 LEFT ENG LOSS OF PROP RPM. A/C RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED ECU. 2 L 7 2 4T 4 T RT A52EU E8NE6 2001072700123 20010727 00123 EU 2001 7 27 CHQA200150620 1 20010620 A 2421 GENERATOR SAAB SF340 SF340A 7850100 EU RT ENGINE FAILED A CHQA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC UK UNKNOWN 1 GL 11 150 150 A/C RETURNED TO FIELD AFTER RT A/C GENERATOR FAIL. MAINTENANCE REMOVED AND REPLACED RT A/C GENERATOR. 2 L 7 2 4T RT A52EU 2001072700124 20010727 00124 EU 2001 7 27 CHQA200158528 1 20010528 A 2161 CONTROLLER SAAB SF340 SF340A 7850100 EU CABIN TEMP MALFUNCTIONED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 158 340A158 RT DUCT OVERTEMP SHORTLY AFTER TAKEOFF. FOLLOWED BY RT BLEED CLOSED LIGHT. CABIN TEMP HOT UNABLE TO COOL IN MANUAL MODE . A/C RETURNED TO DEPARTURE AIRPORT. 2 L 7 2 4T RT A52EU 2001072700125 20010727 00125 2001 7 27 CHQA200158613 4 20010613 A 3418 COMPUTER SAAB SF340 SF340A 7850100 EU STALL WARNING FAULTY H CHQA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 11 158 158 A/C ABORTED TAKEOFF DUE TO RT STALL LIGHT. MAINTENANCE REMOVED AND REPLACED STALL WARNING COMPUTER. 2 L 7 2 4T RT A52EU 2001072700126 20010727 00126 EU 2001 7 27 KBMA88754 1 20010507 A 2121 47760 MOTOR SNIAS 350 AS350BA 8680817 EU FAN DEFECTIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 350SH 2957 FAN BLADE WILL NOT SEAL PROPERLY. IT APPEARS THE SHAFT IS NOT EXTENDED ENOUGH (OUT FROM THE MOTOR). 1 G 7 1 3U NC H9EU 2001072700127 20010727 00127 EU 2001 7 27 KBMA88755 1 20010512 A 2150 451400003 BELT SNIAS 350 AS350BA 8680817 EU AIR CONDITIONER BROKEN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 270SH 9 1864 AIR CONDITIONER COMPRESSOR BELT SNAPPED. REPLACED WITH NEW BELT, AS REQUIRED. 1 G 7 1 3U NC H9EU 2001072700129 20010727 00129 EU 2001 7 27 KBMA88756 1 20010513 A 2150 050143 MOTOR SNIAS 350 AS350BA 8680817 EU A/C BLOWER INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 270SH 1864 AIR CONDITIONER BLOWING WARM AIR. REPLACED WITH SERVICABLE UNIT AS REQUIRED. 1 G 7 1 3U NC H9EU 2001072700130 20010727 00130 EU 2001 7 27 KBMA88757 1 20010512 A 2150 060018 BELT SNIAS 350 AS350B2 8680813 EU AIR CONDITIONER BROKEN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 115SH 3141 AIR CONDITIONER BELT SNAPPED. REPLACED WITH NEW BELT, AS REQUIRED. 1 G 7 1 3U H9EU 2001072700131 20010727 00131 EU 2001 7 27 CHQA200196619 1 20010619 A 7910 OIL SYSTEM SAAB SF340 SF340A 7850100 EU LT ENGINE LACK OF LUBE A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 96 96 A/C ABORTED TAKEOFF AFTER LT ENGINE OIL PRESSURE INDICATION. MAINTENANCE ADDED 2 QTS OIL AND TIGHTENED DRAIN LINE. 2 L 7 2 4T RT A52EU 2001072700132 20010727 00132 2001 7 27 KBMA88758 4 20010521 A 3422 103002201 GYRO SNIAS 350 AS350B2 8680813 EU COCKPIT MALFUNCTIONED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 53SH 2009 DIRECTIONAL GYRO IS SPINNING RAPIDLY. REPLACED WITH OH UNIT, AS REQUIRED. 1 G 7 1 3U H9EU 2001072700133 20010727 00133 EU 2001 7 27 KBMA88761 1 20010519 A 2150 060018 BELT SNIAS 350 AS350BA 8680817 EU AIR CONDITIONER BROKEN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 1188P 36 2347 AIR CONDITIONER BELT BROKE. (MANUFACTURE HAS BEEN NOTIFIED, REPLACING BELTS FREE OF CHARGE.) REPLACED WITH NEW BELT AS REQUIRED. 1 G 7 1 3U NC H9EU 2001072700134 20010727 00134 SO 2001 7 27 CHQA200262528 1 20010528 A 2130 WARNING SYSTEM EMB 145 EMB145LR SO COCKPIT MALFUNCTIONED A CHQA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 11 262 145168 AFTER TAKEOFF- THERE WAS EICAS INDICATION THAT ALL PRESSURIZATION WAS LOST. A/C RETURNED TO FIELD. MAINTENANCE PERFORM ED OPERATIONAL CHECK OF PRESSURIZATION CONTROL SYSTEM. RAN GROUND AND TEST FLIGHT, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2001072700135 20010727 00135 NE 2001 7 27 KBMA88801 2 20010519 A 7421 9550168760 IGNITER SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE RIGHT INOPERATIVE E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 270SH 205 1864 RIGHT HAND IGNITER NOT WORKING PROPERLY. REPLACED WITH NEW IGNITER, AS REQUIRED. 1 G 7 1 3U 3 U NC H9EU E19EU 2001072700138 20010727 00138 WP 2001 7 27 CALA0100688 1 20010725 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 927-1155 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND CABIN L/H I/B FLOOR PANEL DELAMINATED AT FS 1079-1155 AND R/H I/B FLOOR PANEL WAS DELAMINATED AT FS 927 -1003. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001072700139 20010727 00139 WP 2001 7 27 CALA0100689 1 20010725 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP PNLS B-K DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND CABIN FLOOR PANELS B-K DELAMINATED. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001072700140 20010727 00140 WP 2001 7 27 CALA0100690 1 20010725 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP PNLS M-P DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND CABIN FLOOR PANELS M-P DELAMINATED. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001072700141 20010727 00141 NM 2001 7 27 CALA0100691 1 20010725 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM STA 967 & 986.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14325 23455 INSPECTION FOUND FLOORBEAM SECTIONS CORRODED AT STA 967, RBL 17.5 AND AT STA 986.5, RBL 16 TO LBL 46. THE FLOORBEAM SECT IONS WERE REMOVED AND REPLACED IAW ECRA 5310-03851. 2 L 7 2 4F RT A16WE 2001072700142 20010727 00142 WP 2001 7 27 CALA0100692 1 20010725 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FS 798-874 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND R/H CENTER SEAT TRACK CORRODED AT FS 798-874. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTA LLED IAW SRM 51-30-2, 51-30-5, AND 51-30-3. 2 L 7 2 4F A6WE 2001072700143 20010727 00143 WP 2001 7 27 CALA0100693 1 20010725 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 1003-1079 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND MAIN CABIN R/H I/B FLOOR PANEL DELAMINATED AT FS 1003-1079. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 53 20-01265. 2 L 7 2 4F A6WE 2001072700144 20010727 00144 WP 2001 7 27 CALA0100696 1 20010726 A 5230 SKIN DOUG DC9 DC982 3022082 WP FWD CARGO DR GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND FORWARD CARGO DOOR EXTERNAL SKIN GOUGED BELOW HANDLES. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FI GURE 1 AND 52-05. 2 L 7 2 4F A6WE 2001072700145 20010727 00145 WP 2001 7 27 CALA0100698 1 20010726 A 5330 SKIN DOUG DC9 DC982 3022082 WP STA 218 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND FUSELAGE EXTERNAL SKIN DENTED AT STA 218, LONGERON 16L AND 18L. THE DENTS WERE COLD WORKED IAW SRM 53-0 4, FIGURE 38. DOUBLERS WERE INSTALLED IAW SRM 53-10, FIGURE 38 AND 51-10-4. 2 L 7 2 4F A6WE 2001072700146 20010727 00146 WP 2001 7 27 CALA0100699 1 20010726 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP STA 798-1108 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND CABIN SEAT TRACK CORRODED AT STA 798-1108. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLE D IAW SRM 51-30-1. 2 L 7 2 4F A6WE 2001072700151 20010727 00151 EU 2001 7 27 CHQA200340618 1 20010618 A 7910 OIL SYSTEM SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RT ENGINE LACK OF LUBE A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 340 340A014 484 ON CLIMBOUT, RT ENGINE OIL PRESSURE FLUX. A/C RETURNED TO FIELD. MAINTENANCE SERVICED RT ENGINE OIL. 2 L 7 2 4T 4 T RT A52EU E8NE6 2001072700152 20010727 00152 SO 2001 7 27 CHQA279612 1 20010612 A 2750 FLAP EMB 145 EMB145LR SO WING MALFUNCTIONED A CHQA O OTHER F FLT CONT AFFECTED CL CLIMB 1 GL 11 279 145379 UNKNOWN FLAP PROBLEM. PILOT DECLARED EMERGENCY. MAINTENANCE NOTIFIED BY DISPATCH. 2 L 7 2 4T RT T00011AT 2001072700153 20010727 00153 EU 2001 7 27 CHQA3561 1 20010601 A 2613 CONNECTOR SAAB SF340 SF340A 7850100 EU RT ENGINE DIRTY A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 035 340A035 RIGHT TAILPIPE HOT LIGHT CAME ON AFTER TAKEOFF. A/C RETURNED TO FIELD. MAINTENANCE CLEANED SENSOR CANNON PLUG. 2 L 7 2 4T RT A52EU 2001072700155 20010727 00155 EU 2001 7 27 CHQA6191252 1 20010619 A 7910 OIL SYSTEM SAAB SF340 SF340A 7850100 EU RT ENGINE LACK OF LUBE A CHQA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 11 125 125 A/C ABORTED TAKEOFF AFTER RT ENGINE OIL PRESSURE FLUX. THIS IS THE SECOND OCCURRENCE OF THE DAY FOR THIS AIRCRAFT. MAI NTENANCE SERVICED OIL LEVEL. 2 L 7 2 4T RT A52EU 2001072700157 20010727 00157 WP 2001 7 27 CNAM200100016 1 20010422 A 3350 CONNECTOR DOUG DC10 DC1030 3023501 WP CABIN LOOSE A CNMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 540AX 46595 LEFT SIDE ZONE A AISLE PATH LIGHTING ILLUMINATED PRIOR TO PUSHBACK. RESEATED CONNECTOR AT BATTERY PACK. SYSTEMS TESTS GOOD PER 33-50. 2 L 7 3 4F A22WE 2001072700158 20010727 00158 WP 2001 7 27 CNMA200100014 1 20010407 A 2560 ADA3305501 ATTACH FITTING DOUG DC10 DC1030 3023501 WP L4 DOOR BROKEN A CNMA K NONE O OTHER IN INSP/MAINT 1 SW 07 540AX 46595 AFTER LANDING, FOUND L4 DOOR EMERGENCY SLIDE GIRT BAR ATTACH FITTING BROKEN ON RT SIDE. REPLACED ATTACH FITTING. 2 L 7 3 4F A22WE 2001072700160 20010727 00160 WP 2001 7 27 CNMA200100015 1 20010425 A 3350 CONNECTOR DOUG DC10 DC1030 3023501 WP CABIN LOOSE A CNMA K NONE O OTHER CR CRUISE 1 SW 07 540AX 46595 DURING FLIGHT, ONE STRIP OF EMERGENCY ESCAPE PATH LIGHTING ILLUMINATED AT LT SIDE FWD OF L2 DOOR. RESEATED CONNECTOR AT BATTERY PACK. LIGHTS WENT OUT AND TEST PROPERLY IAW MM 33-50. 2 L 7 3 4F A22WE 2001072700161 20010727 00161 WP 2001 7 27 CNMA200100017 1 20010501 A 3350 582223 POWER SUPPLY DOUG DC10 DC1030 3023501 WP CABIN DISCHARGED A CNMA K NONE O OTHER CR CRUISE 1 SW 07 540AX 46595 EMERGENCY ESCAPE PATH LIGHTING AT R3 DOOR ILLUMINATES INTERMITTENTLY DURING FLIGHT. REMOVED AND REPLACED POWER SUPPLY. 2 L 7 3 4F A22WE 2001072700162 20010727 00162 WP 2001 7 27 CNMA200100018 1 20010509 A 3350 CONNECTOR DOUG DC10 DC1030 3023501 WP CABIN LOOSE A CNMA K NONE O OTHER CR CRUISE 1 SW 07 540AX 46595 RIGHT HAND AFT ZONE-C ESCAPE PATH LIGHTING ILLUMINATED IN FLIGHT. CLEANED AND RESEATED BATTERY PACK CONNECTOR. 2 L 7 3 4F A22WE 2001072700164 20010727 00164 WP 2001 7 27 CNMA200100019 1 20010511 A 3350 CONNECTOR DOUG DC10 DC1030 3023501 WP CABIN LOOSE A CNMA K NONE L NO TEST IN INSP/MAINT 1 SW 07 540AX 46595 LEFT HAND FORWARD ESCAPE PATH LIGHTING STRIP INOP. RESECURED POWER LEAD TO LIGHT STRIP. SYSTEM TEST NORMAL IAW MM 33-5 0. 2 L 7 3 4F A22WE 2001072700165 20010727 00165 WP 2001 7 27 CNMA200100020 1 20010512 A 3397 WIRE DOUG DC10 DC1030 3023501 WP CABIN BROKEN A CNMA K NONE L NO TEST IN INSP/MAINT 1 SW 07 540AX 46595 ZONE-C LEFT HAND AFT ESCAPE PATH LIGHTING INOP. REPAIRED BROKEN WIRE ON POWER LEAD TO LIGHT STRIP. SYSTEM TEST NORMAL IAW MM 33-50. 2 L 7 3 4F A22WE 2001072700166 20010727 00166 WP 2001 7 27 CNMA200100021 1 20010410 A 3350 EMBS1392 BATTERY PACK DOUG DC10 DC1030 3023501 WP CABIN DISCHARGED A CNMA K NONE L NO TEST IN INSP/MAINT 1 SW 07 720AX 48252 EMERGENCY LIGHT TEST FAILED. REPLACED NR 4 EMERGENCY LIGHTING POWER SUPPLY AND BATTERY. 2 L 7 3 4F A22WE 2001072700167 20010727 00167 WP 2001 7 27 CNMA200100022 1 20010416 A 3350 582223 BATTERY PACK DOUG DC10 DC1030 3023501 WP CABIN DISCHARGED A CNMA K NONE L NO TEST IN INSP/MAINT 1 SW 07 720AX 48252 L1 AND R1 DOOR EMERGENCY LIGHTS ILLUMINATE INTERMITTENTLY. REPLACED BOTH L1 AND R1 EMERGENCY LIGHT BATTERY PACKS. 2 L 7 3 4F A22WE 2001072700168 20010727 00168 WP 2001 7 27 CNMA200100023 1 20010426 A 3350 EMSE299A BATTERY PACK DOUG DC10 DC1030 3023501 WP CABIN DISCHARGED A CNMA K NONE L NO TEST IN INSP/MAINT 1 SW 07 720AX 48252 EMERGENCY LIGHTS DO NOT TEST. REPLACED MID CABIN BATTERY PACK. 2 L 7 3 4F A22WE 2001072700169 20010727 00169 WP 2001 7 27 CNMA200100024 1 20010527 A 3350 582223 BATTERY PACK DOUG DC10 DC1030 3023501 WP CABIN DISCHARGED A CNMA K NONE L NO TEST IN INSP/MAINT 1 SW 07 540AX 46595 L4 DOOR EMERGENCY TRACK LIGHTING ILLUMINATES INTERMITTENTLY. REPLACED BATTERY PACK. SYSTEM OPERATION CHECKS GOOD IAW M M 33-50. 2 L 7 3 4F A22WE 2001072700172 20010727 00172 WP 2001 7 27 CNMA200100025 1 20010606 A 7603 C803833 LEVER DOUG DC10 DC1010 3022110 WP GE CF6 CF66K 30020 NE COCKPIT STUCK A CNMA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 SW 07 450AX 46942 451319 AT FLIGHT LEVEL 360 NR 2 ENG THROTTLE BECAME JAMMED AT A POWER SETTING OF 94 PERCENT N1. REPEATED ATTEMPTS WERE MADE TO FREE THROTTLE LEVER, NONE SUCCESSFUL. AFTER ENGINE SHUTDOWN N1 READ 10-13 PERCENT, N2 READ .7 TO 0 PERCENT 2 ENGINE. APPROACH AND LANDING WAS THEN EXECUTED. 2 L 7 3 4F 4 F A22WE E23EA 2001081700081 20010817 00081 WP 2001 8 17 ARWAA0010718 1 20010722 A 3233 4771392501 PIN DOUG DC8 DC863 302198A WP PWA JT3D JT3D7 52039 NE RT MLG ACTUATOR BROKEN A ARWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 345JW 3662 3662 46042 ON DEPARTURE TAKEOFF OUT OF MIAMI, GEAR NOT LATCHED LIGHT ILLUMINATES WITH GEAR IN UP POSITION. ABNORMAL CHECKLIST PERF ORMED. LANDED WITHOUT INCIDENT. OVERWEIGHT LANDING WEIGHT INSPECTION COMPLETED. UPON INSPECTION OF THE AIRCRAFT, THE RIGHT HAND MAIN GEAR ACTUATOR RETRACT PIN WAS FOUND BROKEN. REMOVED AND REPLACED RETRACT PIN WITH NEW PART (SN-AGA349). ALL WORK ACCOMPLISHED IAW MFG RECOMMENDED PROCEDURES. OPERATIONAL AND FUNCTIONAL CHECKS COMPLETED, AND FOUND SATISFAC TORY. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4 F 4A25 1E8 2001072700173 20010727 00173 WP 2001 7 27 ABXA010408 1 20010720 A 5311 99196132 FRAME DOUG DC9 DC932F 3022067 WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 RIGHT SIDE FUSELAGE FRAME 617 WAS CRACKED ON THE FORWARD SIDE JUST UNDER FLOOR CUSP ON TOP ROW OF FASTENERS. REPAIRED AR EA IAW REA D953-41707MR. 2 L 7 2 4F A6WE 2001072700174 20010727 00174 2001 7 27 ABXA010409 4 20010726 A 2565 101623303 SLIDE BOEING 767 767231 1385131 NM CABIN DEPLOYED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 702AX 22566 THE CREW INADVERTANTLY DEPLOYED THE EMERGENCY ESCAPE SLIDE. NO SLIDE INFLATION. REPLACED THE MAIN ENTRY DOOR SLIDE IAW B 767 MM 25-66-00. 2 L 7 2 4F RT A1NM 2001072700175 20010727 00175 WP 2001 7 27 IXXA0100040O 1 20010724 A 2610 898463 ELEMENT DOUG DC8 DC871F 302199D WP ENGINE DEFECTIVE A IXXA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SW 11 822BX 84264 91 45813 ENROUTE FROM LAX TO TOL, DURING CRUISE THE NUMBER FOUR FIRE WARNING LIGHT ILLUMINATED ACCOMPANIED BY THE WARNING BELL. T HE FLIGHT CREW FOLLOWED COMPANY EMERGENCY PROCEDURES, SECURED THE ENGINE AND DISCHARGED BOTH BOTTLES. THE FLIGHT RETURNE D TO LAX FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE ENGINE WITH NO EVIDENCE OF A FIRE. FURTHER INSPECTION REVE ALED THREE FIRE SENSEING ELEMENTS DEFECTIVE AND A ELECTRICAL CONNECTOR. MAINTENANCE REPLACED THE ELEMENTS AND ELECTRICAL CONNECTOR AND PERFORMED A SUCCESSFUL OPERATIONAL CHECK. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2001081500156 20010815 00156 NM 2001 8 15 01FDEA00603 1 20010725 A 5315 FLOORBEAM BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSION ON UPPER CHORD OF BS 1030 FLOORBEAM RBL 55, RBL 15 - LBL 13. *S/D* REMOVED AND REPLACED FLOORBEAM PER SRM 53 -10-8 FIG 3. 2 L 7 3 4F A3WE 2001081500157 20010815 00157 NM 2001 8 15 01FDEA00604 1 20010723 A 5310 SHEAR TIE BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSION FWD BAY BS 720D, LBL 25, WL 150 SHEAR TIE. *S/D* REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-4. 2 L 7 3 4F A3WE 2001081700043 20010817 00043 NM 2001 8 17 01FDEA00605 1 20010725 A 5315 FLOORBEAM BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSION ON UPPER CHORD BS 1050 FLOORBEAM RBL 35, RBL 12, RBL 18, WL 208. *S/D* REMOVED AND REPLACED UPPER CHORD PER SRM 53-10-8. 2 L 7 3 4F A3WE 2001081500159 20010815 00159 NM 2001 8 15 01FDEA00606 1 20010716 A 5311 FRAME BOEING 727 727247 138408F NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 DAMAGE ON FRAME, BS 380 BETWEEN STR 11-12L. *S/D* REMOVED AND REPLACED FRAME PER SRM 53-10-4. 2 L 7 3 4F A3WE 2001072700176 20010727 00176 NM 2001 7 27 01FDEA00607 1 20010726 A 5270 H111086 SWITCH BOEING 727 72725C 138400H NM DOORS INOPERATIVE A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 116FE 19298 DUR TEST FLT AT 12000 CLIMB MC DOOR LIGHT CAME ON. ADJUSTED MC DOOR WARN MICROSWITCHES, AND OPS CK GOOD PER IAW FEDEX MM 52-70-000-5. 2 L 7 3 4F A3WE 2001072700177 20010727 00177 NE 2001 7 27 RAIA00107033 2 20010725 A 7412 31058865 EXCITER JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RIGHT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 571HK 3312 41090 76097 7229-GRR-RIGHT ENGINE WILL NOT START. MAINTENANCE INSPECTED AND REPLACED THE RIGHT ENGINE IGNITION EXCITER BOX. 2 L 7 2 4T 4 T RT A41NM E18NE 2001072700179 20010727 00179 EU 2001 7 27 OLJ2001F00000 1 20010614 A 5530 365A13301723 STUD UROCOP AEROSP SA365 SA365N1 8680668 EU VERTICAL FIN DEPARTED E OLJA K NONE O OTHER IN INSP/MAINT 1 EA 13 896LL 6294 RIGHT HAND VERTICAL FIN DEPARTED AIRCRAFT DURING FLIGHT. CAUSE: FATIGUE ON ONE STUD LEADING TO FAILURE OF OTHER STUDS. 1 G 7 2 3U H10EU 2001072700181 20010727 00181 SW 2001 7 27 PN12001F00000 1 20010604 A 6230 407040038101 MAST BELL 407 407 SW MAIN ROTOR CORRODED B PN1R K NONE O OTHER IN INSP/MAINT 1 EA 17 203HA 942 53023 COMPLETED 60 MONTH MAST INSPECTION, FOUND CORROSION ON MAST POLE IN AREA ON RETAINING NUT THREADS, AND THE RETAINING NUT THAT WAS BEYOND ALLOWABLE LIMITS IAW PRODUCT SUPPORT EVALUATION. REPLACED MAST POLE AND RETAINING NUT. THERE WAS NO T ORQUE ON THE RETAINING NUT WHEN REMOVED FOR THE INSPECTION AND THE PRO-SEAL WAS NOT SEALING AGAINST THE MAST POLE, THUS CAUSING MOISTURE AND CORROSION ON THE POLE AND RETAINING NUT. 1 G 7 1 3U O H2SW 2001072700182 20010727 00182 SW 2001 7 27 PN12001F00001 1 20010614 A 6520 206040425135 CASE BELL 206 206B 1181511 SW T/R GEAR BOX MISDRILLED B PN1R K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 17 6NJ 301 4534 TAIL ROTOR GEAR BOX USE SAFETY WIRE HOLES DRILLED OF CENTER AND THRU WALL OF TABS. REPLACED CASE AND DUPLEX BEARING. 1 G 7 1 3U H2SW 2001072700183 20010727 00183 2001 7 27 R7MR33078 4 20010417 A 2210 9910991 HEAD UROCOP EC135 EC135P1 8680990 EU REMOTE CONTROL INOPERATIVE A R7MR K NONE L NO TEST IN INSP/MAINT 1 NM 07 135N 116 0086 UNIT INOPERATIVE. NO DISPLAY. REPLACED WITH LOANER UNIT SN JH1032 CORRECTED PROBLEM. 1 G 7 2 3U O H88EU 2001072700185 20010727 00185 2001 7 27 DHL2001362019 4 20010608 A 2211 COMPUTER AIRBUS 300 A300B4103 3930104 EU AUTOPILOT SYS MALFUNCTIONED A DHLA K NONE O OTHER CR CRUISE 1 SO 01 362DH 84 NR 1 AUTOPILOT WOULD NOT ENGAGE. RESET NR 1 LOGIC MONITOR COMPUTER GROUND CHECKS GOOD PER M/M 22-10-00. 2 L 7 2 4F RT A35EU 2001072700186 20010727 00186 2001 7 27 DHL2001362020 4 20010614 A 2230 COMPUTER AIRBUS 300 A300B4203 3930306 EU AUTOTHROTTLE SYS MALFUNCTIONED A DHLA K NONE O OTHER AP APPROACH 1 SO 01 362DH 84 AUTO THROTTLES WON'T REMAIN ENGAGED WHEN ON APPROACH. CLEANED AND RE-SEATED A/T COMPUTER PER M/M 22-30-00. GROUND OP C HECKS GOOD. 2 L 7 2 4F RT A35EU 2001072700187 20010727 00187 EU 2001 7 27 DHL2001362022 1 20010709 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU COCKPIT MALFUNCTIONED A DHLA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 362DH 84 CABIN SMOKE DETECTORS ILLUMINATED ON S/O PANEL. RETURNED AIRCRAFT TO BLOCKS. COOLED CABIN, RESET LIGHTS AND OPS NORMAL IAW MM 26-14-00. 2 L 7 2 4F RT A35EU 2001072700188 20010727 00188 SO 2001 7 27 RAIA00107034 1 20010723 A 5610 163500112 WINDSHIELD EMB 145 EMB145ER SO COCKPIT CRACKED A RAIA B EMER. DESCENT O OTHER CR CRUISE 1 CE 03 807HK 4595 145157 5294-PIT-FIRST OFFICERS WINDOW CRACKED IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED FIRST OFFICERS WINDSHIELD PANEL. 2 L 7 2 4F RT T00011AT 2001072700189 20010727 00189 2001 7 27 DHL2001363006 4 20010608 A 2211 COMPUTER AIRBUS 300 A300B4103 3930104 EU AUTOPILOT SYS MALFUNCTIONED A DHLA K NONE O OTHER CR CRUISE 1 SO 01 363DH 085 AUTOPILOT NR 1 WILL NOT ENGAGE. RESEATED ALL THREE A/P, F/O COMPUTERS. NR 1 A/P OP CHECKS GOOD PER M/M 22-10-00. NO F AULTS IN SELF TEST. 2 L 7 2 4F RT A35EU 2001072700190 20010727 00190 EA 2001 7 27 COMA0160500 1 20010726 A 2740 83963 CONTROL UNIT CNDAIR CL600 CL6002B19 EA FAILED A COMA O OTHER K FLUID LOSS AP APPROACH 1 SO 01 943CA 5805 7062 ON FINAL APPROACH INTO CVG THE PITCH TRIM CAUTION MESSAGE ACTIVATED.REPLACED THE HORIZONTAL STABILIZER TRIM CONTROL UNIT . 2 L 7 2 4F RT A21EA 2001072700191 20010727 00191 EU 2001 7 27 DHL2001363007 1 20010622 A 3242 BRAKE AIRBUS 300 A300B4203 3930306 EU RT MLG VIBRATION A DHLA D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 SO 01 363DH 85 VIBRATION AND NOISE ASSOCIATED WITH RIGHT BRAKE APPLICATION. BLED NR 8 BRAKE. SYSTEM OPS CK GOOD PER MM 32-42-0. 2 L 7 2 4F RT A35EU 2001072700192 20010727 00192 EU 2001 7 27 DHL2001363008 1 20010622 A 2913 PUMP AIRBUS 300 A300B4203 3930306 EU NR 2 ENGINE FAILED A DHLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 363DH 85 GREEN PUMP NR 2 ENGINE DRIVEN PUMP FAILED. REMOVED AND REPLACED PUMP. 2 L 7 2 4F RT A35EU 2001072700193 20010727 00193 NM 2001 7 27 R7MR33263 1 20010127 A 6220 900R3100002105 BEARING DOUG MD900 MD900 3027375 NM MAIN ROTOR WORN A R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 901CF 4396 90000012 ELASTOMERIC LAMINATES WORN BEYOND SERVICEABLE LIMITS, WHICH IS CAUSING DIFFICULTY WITH BALANCING THE MAIN ROTOR HEAD ASS EMBLY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 2001072700194 20010727 00194 EU 2001 7 27 DHL2001363009 1 20010620 A 3260 LIGHT AIRBUS 300 A300B4203 3930306 EU COCKPIT INOPERATIVE A DHLA K NONE O OTHER UK UNKNOWN 1 SO 01 363DH 85 ON FWD GEAR INDICATOR RIGHT MAIN LIGHT INOP NORMAL INDICATION ON S/O PANEL. RELAMPED, OPS CKS GOOD IAW M/M 32-61-00. 2 L 7 2 4F RT A35EU 2001072700195 20010727 00195 NM 2001 7 27 R7MR33264 1 20010127 A 6720 900F2421545105 BEARING DOUG MD900 MD900 3027375 NM TAIL ROTOR WORN A R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 901CF 294 90000012 THRUSTER BEARING RACE, WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 2001072700196 20010727 00196 EU 2001 7 27 DHL2001363010 1 20010710 A 2613 LOOP AIRBUS 300 A300B4203 3930306 EU OVERHEAT SYS FAILED A DHLA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 363DH 85 LEFT HAND MAN FAULT DET B-LOOP DOES NOT TEST GOOD ON GROUND. DEFERRED AS PER MEL 36-12-03 CAT C ASSIGNED DMI 6314 PLACA RD LT MANIFOLD B-LOOP. REF: DMI 6314 LEFT HAND MAN FAULT DET B-LOOP DOES NOT TEST GOOD ON GROUND. REPLACED OVERHEAT DE T CONT UNIT PER: MM 26-16-11, OPS CK GOOD. CLEARED DMI #6314 2 L 7 2 4F RT A35EU 2001072700197 20010727 00197 NM 2001 7 27 R7MR33265 1 20010127 A 2820 900P3663102101 VALVE DOUG MD900 MD900 3027375 NM PWA PW206 PW206A NE FUEL SYSTEM LEAKING A R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 901CF 815 90000012 FRANGIBLE SELF SEALING VALVE, LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U NC H19NM E42NE 2001072700198 20010727 00198 EA 2001 7 27 COMA0160501 1 20010726 A 2740 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 EA FAILED A COMA O OTHER K FLUID LOSS AP APPROACH 1 SO 01 943CA 5805 7062 ON FINAL APPROACH INTO CVG THE PITCH TRIM CAUTION MESSAGE ACTIVATED.REPLACED THE MOTOR CONTROL UNIT. 2 L 7 2 4F RT A21EA 2001072700199 20010727 00199 2001 7 27 R7MR33270 4 20010214 A 3457 071015530200 ANTENNA BOLKMS 117 BK117B1 5626012 EU GPS SYSTEM INOPERATIVE A R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 911VU 908 7141 KA 92 ANTENNA, UNIT INOPERATIVE. GPS WILL NOT PICK UP SATELITE LINK. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2001072700200 20010727 00200 2001 7 27 DHL2001364020 4 20010619 A 2565 WARNING SYSTEM AIRBUS 300 A300B4203 3930306 EU SLIDE FAILED A DHLA K NONE L NO TEST UK UNKNOWN 1 SO 01 364DH 141 SLIDE ALARM ON RT DOOR DOES NOT SOUND WHEN TESTED. SLIDE ALARM OPS CHECKS NORMAL IAW MM REF 52-70-00. 2 L 7 2 4F RT A35EU 2001072700201 20010727 00201 NM 2001 7 27 R7MR33279 1 20010312 A 7722 304534402 HARNESS DOUG MD900 MD900 3027375 NM T6 WIRING SHORTED A R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 901CF 1163 90000012 T6 WIRING HARNESS, INTERNAL SHORT. FAILED RESISSTENCE CHECK. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 2001072700202 20010727 00202 2001 7 27 R7MR33280 4 20010323 A 3160 B19030MA DISPLAY SNIAS 350 AS350B3 8680954 EU COCKPIT INOPERATIVE A R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 52281 678 VEMD 350B3, FLIGHT INFORMATION INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 2001072700203 20010727 00203 2001 7 27 R7MR33281 4 20010429 A 3160 B19030MC02 DISPLAY SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT INOPERATIVE A R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 397LG 94 3268 VEMD (ASTAR AFTER 3018) INTERMITTENT SCREEN 2 INOPERATIVE. REPLACED WITH NEW UNITS, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2001072700204 20010727 00204 EU 2001 7 27 R7MR33289 1 20010322 A 6730 SC5084 SERVO SNIAS 350 AS350B3 8680954 EU CYCLIC STICK STUCK A R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 52281 622 SERVO CONTROL FRONT WITH LOCK, CYCLIC STICKS WITH FORE/AFT INPUTS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 2001072700205 20010727 00205 EU 2001 7 27 R7MR33290 1 20010410 A 6730 SC5084 SERVO SNIAS 350 AS350B 8680801 EU CYCLIC STICK INOPERATIVE A R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 52281 14 CYCLIC WOULD NOT MOVE FORWARD IN FLIGHT. PILOT REPORTS 7 TO 8 LBS PRESSURE TO MOVE CYCLIC. REPLACED WITH NEW UNIT, COR RECTED PROBLEM. 1 G 7 1 3U H9EU 2001072700206 20010727 00206 NE 2001 7 27 R7MR33301 2 20010425 A 7320 0292958050 VALVE SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE ENGINE INOPERATIVE A R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 397LG 236 3268 COMPLETE VALVE ASSEMBLY, UNIT INOPERATIVE. HAS DELAYED SHUT-DOWN. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E00054EN 2001072700210 20010727 00210 EU 2001 7 27 DHL2001364021 1 20010623 A 5312 BULKHEAD AIRBUS 300 A300B4203 3930306 EU FUSELAGE GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 REF: COMPLY WITH INSPECTION OF AFT PRESS BULKHEAD. COMPLIED WITH INSPECTION OF AFT PRESSURE BULKHEAD. REF: 2M INSPECTI ON REVEALED GOUGE AFT OF LEFT HAND DRAIN HOLE, FRAME 80 STA 4944 AT 1 INCH INBOARD OF STR 56L. GOUGE EXTENDS THRU INNER ATTACHMENT ANGLE AND INTO OUTER ATTACHMENT ANGLE. 2 L 7 2 4F RT A35EU 2001072700212 20010727 00212 EU 2001 7 27 R7MR33321 1 20010412 A 7714 430106202 PICKUP BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ELETRO SPEED INOPERATIVE A R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 7060G 252 7173 NGP SPEED ELECRTOMAGNETIC SPEED PICKUP, UNIT INOPERATIVE. N1 INDICATOR ERRATIC. CHECK ENGINE LIGHT STAYS ON. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 2001072700213 20010727 00213 EU 2001 7 27 DHL2001366015 1 20010619 A 3260 LIGHT AIRBUS 300 A300B4203 3930306 EU COCKPIT INOPERATIVE A DHLA K NONE L NO TEST UK UNKNOWN 1 SO 01 366DH 249 RIGHT LANDING GEAR GREEN LIGHT INOP. RELAMPED OPS CK GOOD PER MM 33-15-80. 2 L 7 2 4F RT A35EU 2001072700216 20010727 00216 EU 2001 7 27 R7MR33329 1 20010105 A 6320 350A32040000M PUMP SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE GEARBOX OIL INOPERATIVE A R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 6099P 811 OIL PUMP - AFTER ENGINE WARMS THE MGB OIL PRESSURE GOES DOWN TO 1.9 BARS. AFTER SEVERAL SWITCH REPLACEMENTS IT WAS DECI DED THAT THE OIL PUMP WAS CAUSE OF PROBLEM. THE FIRST OCCURRENCE FOR LOW OIL PRESSURE WAS ON 1/5/01 WHICH BRINGS THE PU MP TO WITHIN THE ONE YEAR WARRANTY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2001072700217 20010727 00217 SW 2001 7 27 R7MR33330 1 20010421 A 5240 9003005A9 LATCH BELL 407 407 SW ALLSN 250C 250C47B GL DOOR WORN A R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 911LN 298 911LN LATCH, WORN BEYOND SERVICEABLE LIMITS. REMOVED AND REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2001072700218 20010727 00218 SW 2001 7 27 R7MR33332 1 20010308 A 6310 406040316101 ADAPTER BELL 407 407 SW ALLSN 250C 250C47B GL ENG/TRANS COUP WORN B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 911LN 184 53446 WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. NOTE: TRYING TO LOCATE DISCREPANT PART. 1 G 7 1 3U 3 U O H2SW E1GL 2001072700219 20010727 00219 SW 2001 7 27 R7MR33335 1 20010327 A 2400 M835362028M RELAY BELL 407 407 SW ELECTRICAL INOPERATIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 911LN 242 53446 UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U O H2SW 2001072700220 20010727 00220 SW 2001 7 27 R7MR33336 1 20010410 A 2110 COMPRESSOR BELL 407 407 SW AIR CONDITIONING DRAGGING B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 911LN 53446 COMPRESSOR DRAGS CAUSING DRIVE BELT FAILURE. DISCREPANT UNIT SCRAPPED LOCALLY. REPLACED WITH NEW UNIT, CORRECTED PROBL EM. 1 G 7 1 3U O H2SW 2001072700221 20010727 00221 EU 2001 7 27 R7MR33339 1 20010508 A 7810 117651121 TAILPIPE BOLKMS 117 BK117A4 5626017 EU ENGINE CRACKED B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 127HH 40 7060 CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2001072700222 20010727 00222 2001 7 27 R7MR33351 4 20010515 A 2210 BUSHING BOLKMS 117 BK117A3 5626015 EU ACTUATOR WORN B R7MR K NONE K FLUID LOSS IN INSP/MAINT 1 NM 07 163BK 00302 7063 BUSHINGS WORN BEYOND SERVICEABLE LIMITS AND ALSO LEAKS HYDRAULIC FLUID. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2001072700223 20010727 00223 EU 2001 7 27 R7MR33353 1 20010411 A 7603 1564T1005 ACTUATOR BOLKMS 105 BO105S 5626006 EU THROTTLE INOPERATIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 485EC S754 UNIT INOPERATIVE, N2 TRIM ON NR 1 ENGINE DOES NOT WORK. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3EU 2001072700224 20010727 00224 WP 2001 7 27 RT22001F00000 1 20010612 A 6320 369D2512711 GEAR HUGHES 369 369E 4470707 WP TRANSMISSION BROKEN B RT2R A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION NR NOT REPORTED 1 GL 11 98SP 1214 0117E 1) PILOT REPORTED BANG FOLLOWED BY AIRCRAFT VIBRATION, NO CAUTION LIGHT ILLUMINATED. PILOT MADE PRECAUTIONARY LANDING. 2) MAINTENANCE FOUND LARGE PIECE OF METAL ON CHIP DETECTOR STANDING UP TOO LARGE TO FALL OVER AND BRIDGE GAP ON CHIP DE TECTOR. 3) TRANSMISSION REMOVED, GEAR PN 369D2512711 SER NR 0055701092 FOUND TO HAVE A TOOTH BROKEN OFF, MFG HAS TAKEN GEAR TO PERFORM HARDNESS TEST. 1 G 7 1 3U H3WE 2001072700225 20010727 00225 EU 2001 7 27 S9HA265Y 1 20010514 A 2913 1502780 PUMP SNIAS 350 AS350BA 8680817 EU HYDRAULIC SYS FAILED E S9HA O OTHER O OTHER NR NOT REPORTED 1 WP 19 352HH 2714 TOTAL PUMP/HYDRAULIC FAILURE ON GROUND. 2ND OCCURANCE THIS COMPANY LOCATION, BUT NOT THIS AIRCRAFT. 1 G 7 1 3U NC H9EU 2001072700226 20010727 00226 EU 2001 7 27 SDRS2001002 1 20010525 A 6710 BEARING UROCOP BOLKMS 117 BK117A3 5626015 EU BELLCRANK FAILED E R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 163BK 7063 THE AC EXPERIENCED ABNORMAL UNCOMMANDED YAW AND ROLL MOTION ON LANDING. LATERAL CYCLIC BELLCRANK CENTER BEARING FOUND T O HAVE FAILED. THIS CAUSED THE BELLCRANK TO HAVE EXCESSIVE PLAY RESULTING IN LOSS OF POSITIVE CYCLIC CONTROL. AC PERFO RMED SUCCESSFUL LANDING WITHOUT DAMAGE, HOWEVER THE LOSS OF CONTROL WAS QUITE SEVERE. AN INSPECTION OF THE BELL CRANK B EARING ON 6/19/2001, FOUND THAT THE BEARINGS WERE MISSING. THE PART MAY HAVE AS MUCH AS 6065 HRS. IT APPEARS THAT THE BALLBEARING INSTALLATION SLOTS MAY HAVE LINED UP AND ALLOWED THE BALLBEARINGS TO BE EJECTED FROM THE BEARING, ONE AT A T IME. 1 G 7 2 3U H13EU 2001072700227 20010727 00227 NE 2001 7 27 SW032001B3673 2 20010531 A 7314 P94B12209 PUMP SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1B 6OO30 NE FUEL SYSTEM FAILED B B3OR O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 5204Y 728 3101 FUEL PUMP FAILED DURING FLIGHT. NO FLIGHT ABORT. 1 G 7 1 3U 3 U H9EU E19EU 2001072700228 20010727 00228 EU 2001 7 27 TI12001F00000 1 20010501 A 5302 1053025151 FRAME UROCOP BOLKMS 117 BK117A3 5626015 EU TAIL BOOM CRACKED B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 1140H 7078 DURING ROUTINE INSPECTION THE 10L FRAME WAS SOUND CRACKED THROUGH ON LEFT HAND SIDE. 1 G 7 2 3U H13EU 2001072700229 20010727 00229 EU 2001 7 27 TI12001F00001 1 20010501 A 5302 1053025151 FRAME UROCOP BOLKMS 117 BK117A3 5626015 EU TAIL BOOM CRACKED B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 4493X S7038 DURING ROUTINE INSPECTION, A CRACK WAS FOUND ON THE 10L FRAME AT THE 10 OCLOCK CUTOUT FOR THE OMEGA DOUBLER ON THE UPPER PORTION, EXTENDING UP .5000 INCHES THEN GOING ACROSS .6250 INCHES TO THE TOOLING HOLE, AND STARTING UP AGAIN AT THE OTH ER END OF THE TOOLING HOLE AND EXTENDING 1 INCH AND THEN STOPPING AT A RIVET HOLE. 1 G 7 2 3U H13EU 2001072700230 20010727 00230 EU 2001 7 27 TI12001F00002 1 20010501 A 5302 1053025151 FRAME UROCOP BOLKMS 117 BK117A1 5626010 EU TAIL BOOM CRACKED B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 117LF 7928 7013 7013 DURING ROUTINE INSPECTION A CRACK WAS FOUND ON THE 10L FRAME ON THE UPPER RIGHT CORNER AT THE UPPER OMEGA CUT OUT AFTER CLEANING AREA, FOUND ADDITIONAL CRACK ON SAME CUT OUT. 1 G 7 2 3U H13EU 2001072700231 20010727 00231 EA 2001 7 27 COMA0160505 1 20010725 A 2750 857SD10015 DRIVE SHAFT CNDAIR CL600 CL6002B19 EA BINDS A COMA O OTHER O OTHER AP APPROACH 1 SO 01 934CA 7042 DURING APPROACH INTO CVG FLAP FAIL MESSAGE APPEARED AT 41 DEGREES.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "SECOND EVENT" MAINTENANCE ACTION, PARAGRAPH (B)3(D AND E)4. REPLACED #1 FLEX DRIVE FOR THE RIGHT SIDE. 2 L 7 2 4F RT A21EA 2001072700232 20010727 00232 NM 2001 7 27 UPS01236022 1 20010515 A 5330 SKIN BOEING 727 727247 138408F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE:C, CORROSION ON CROWN SKIN BS 848 4 INCHES BELOW STR 7L. BLENDED CORROSION AT BS 848 4 INCHES BELOW STR 7L IN AN AREA OF 1 X 2 INCHES. REMOVED .032 INCH FROM ORIGINAL THICKNESS OF .090 INCH FOUND TO BE OUT OF LIMITS IAW SR M 53-30-1 PG 1 2B. REPAIRED AREA IAW SRM 53-30-3. 2 L 7 3 4F A3WE 2001072700233 20010727 00233 EA 2001 7 27 COMA0160506 1 20010725 A 2750 857SD10017 DRIVE SHAFT CNDAIR CL600 CL6002B19 EA BINDS A COMA O OTHER O OTHER AP APPROACH 1 SO 01 934CA 7042 DURING APPROACH INTO CVG FLAP FAIL MESSAGE APPEARED AT 41 DEGREES.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "SECOND EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 3 (D AND E)4. REPLACED #2 FLEX DRIVE FOR THE LEFT SIDE. 2 L 7 2 4F RT A21EA 2001072700234 20010727 00234 NM 2001 7 27 UPS01236026 1 20010531 A 5730 PANEL BOEING 727 72751C 1384015 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:C, 1 INCH CRACK ON PANEL, UPPER SURFACE OF WING, JUST FWD OF I/B AILERON ON RIGHT WING, I/B EDGE OF PANE L. REPAIRED PER SRM 51-40-2. 2 L 7 3 4F A3WE 2001072700235 20010727 00235 NM 2001 7 27 UPS01236032 1 20010611 A 2612 WARNING LIGHT BOEING 727 72725C 138400H NM MLG WW FALSE INDICATION A IPXA O OTHER N FALSE WARNING TO TAKEOFF 1 SO 01 951UP 19850 INSPECTION TYPE:N/A WHEEL WELL FIRE LIGHT ILLUMINATED AFTER TAKEOFF. LIGHT WENT OUT AFTER GEAR EXTENTSION. A/C FLOWN T O SDF WITH LANDING GEAR DOWN AT 250 KTS. 2ND PAGE/ REF ITEM 1 PREVIOUS LOG PAGE WHEEL WELL FIRE WARN LIGHT ON AFTER GEA R RETRACTION. NO DEFECTS NOTED, TESTED W/W FIRE DETECTION SYSTEM 26-12-01 AND INSPECTED BRAKES AND TIRES, APU DUCTING A ND APU EXHAUST ALL NORMAL. SUSPECT QUICK TURN AND WARM BRAKES. OK FOR SERVICE. REF SIGN OFF PREVIOUS LOG PAGE: INSPEC TED BRAKES PER M/M 32-41-31 INSPECTED TIRES PER M/M 32-45-01 AND GMM CHAPTER 10-2-1 TIRE PRESSURES PER 12-15-31. 2 L 7 3 4F A3WE 2001072700236 20010727 00236 NM 2001 7 27 UPS01236033 1 20010530 A 5755 SKIN BOEING 727 72751C 1384015 NM SPOILER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:C, CRACK FOUND IN TRAILING EDGE SKIN ADJACENT NR 3 SPOILER PANEL HINGE INBOARD HINGE. CRACK REPAIRED IA W SRM. 2 L 7 3 4F A3WE 2001072700237 20010727 00237 EA 2001 7 27 COMA0160507 1 20010725 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA OUT OF RIG A COMA O OTHER O OTHER AP APPROACH 1 SO 01 934CA 10679 7042 DURING APPROACH INTO CVG FLAP FAIL MESSAGE APPEARED AT 41 DEGREES.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "SECOND EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 3 (D AND E) 4. REPLACED THE RIGHT BRAKE POSITIONING SENSING UNIT. 2 L 7 2 4F RT A21EA 2001072700238 20010727 00238 NM 2001 7 27 UPS01236098 1 20010614 A 2612 65249203 FIRE LOOP BOEING 727 72725C 138400H NM NLG WW CONTAMINATED A IPXA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 931UP 19858 INSPECTION TYPE:N/A WHEEL WELL FIRE LIGHT AND BELL CAME ON ON APPROACH AT APPROX 3000 FT MSL WHEN GEAR EXTENDED, LIGHT E XTINGUISHED. NO APPARENT DAMAGE OR PROBLEMS ON LANDING. INSPECTED ALL WHEEL WELL FIRE LOOPS FOR GROUNDS. FOUND CONTAM INATION IN THE NOSE WHEEL WELL FIRE LOOP CONNECTOR CAUSING LOOP TO SHORT TO GROUND. CLEANED AND RE-SECURED CONNECTOR. R/I FIRE DETECTION UNIT AS PRECAUTIONARY. OP'S CHECKS GOOD AS PER M/M 26-12-00 ADJ/TEST. OK FOR SERVICE. 2 L 7 3 4F A3WE 2001072700239 20010727 00239 NM 2001 7 27 UPS01236101 1 20010526 A 5330 SKIN BOEING 727 72725C 138400H NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:C, INDICATION OF MATERIAL LOSS GREATER THAN 10 8/0 IN THE SKIN AT CIRCUMFERENTIAL JOINT BS 441 BETWEEN S 17R AND S 20R FORWARD PANEL. CUT DAMAGED AREA ON STA 441 BETWEEN STA 17R AND STA 20R PER DRAWING 69-62161. INSTALLED DOUBLER REPAIR IN CUT OUT AREA PER UPS EO B727 5310-1371E APPENDIX 8.5 AND DRAWING 69-62161. 2 L 7 3 4F A3WE 2001072700240 20010727 00240 NM 2001 7 27 UPS01236103 1 20010527 A 5711 SPAR BOEING 727 72725C 138400H NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:C, LEFT WING REAR SPAR UPPER CHORD AT WING STATION APPROX CRACK INDICATION IS ABOUT 2 INCHES LONG OUTBOA RD OF NR 1 FUEL SOV. REMOVE CRACK AT REAR SPAR UPPER CHORD AT WS 190 AND INSTALL FILLER AND DOUBLER REPAIR AS PER BOEIN G DRAWING 65C196447, REMOVED AND REPLACED STIFFENER AT WS 192 AS PER BOEING DWG 65C19647 AND B727 SRM 51-30-2, INSTALLED WEB REPAIR ON LT WING RIB AFT AT WBL 928 PER B727- SRM 51-40-2. 2 L 7 3 4F A3WE 2001072700241 20010727 00241 NM 2001 7 27 UPS01236104 1 20010527 A 5314 KEELBEAM BOEING 727 72725C 138400H NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:C KEEL BEAM BS 900 APPROX APU COMPARTMENT ACCESS PANEL SHOWS A HOLE AND CRACKED AREA. CUT DAMAGED AREA AT KEEL BEAM ACCESS PANEL BS 900 APU COMPARTMENT AS PER B727 SRM 51-10-1, INSTALLED DOUBLER ON KEEL BEAM ACCESS PANEL AS PER B727 SRM 51-40-2 FIG 1. 2 L 7 3 4F A3WE 2001072700242 20010727 00242 NM 2001 7 27 UPS01236138 1 20010606 A 5320 SILL BOEING 727 727247 138408F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE:C, FOUND CORROSION ON AFT CARGO DOOR CUTOUT LOWER SILL CHORD AT BS 950+19. REPAIRED CHORD IAW SRM 51-40 -4, 53-10-1, 51-10-1, 51-30-2. 2 L 7 3 4F A3WE 2001072700243 20010727 00243 NM 2001 7 27 UPS01236152 1 20010619 A 3350 BATTERY BOEING 727 7272A1 138407F NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE:N/A EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES. 2 L 7 3 4F A3WE 2001072700244 20010727 00244 EA 2001 7 27 COMA0160508 1 20010725 A 2750 853D10011 ACTUATOR CNDAIR CL600 CL6002B19 EA LEAKING A COMA O OTHER O OTHER AP APPROACH 1 SO 01 934CA 13562 7042 DURING APPROACH INTO CVG FLAP FAIL MESSAGE APPEARED AT 41 DEGREES.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "SECOND EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 3 AND (D AND E) 4. REPLACED #3 FLAP ACTUATOR FOR THE RIGHT SIDE. 2 L 7 2 4F RT A21EA 2001072700245 20010727 00245 NM 2001 7 27 UPS01236153 1 20010619 A 5310 SHEAR TIE BOEING 727 727247 138408F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE:C, WHILE WORKING FUSELAGE DISCOVERED SHEAR TIE CORRODED BS 970, RBL 8 OUTBOARD OF STR 29R. CORROSION FO UND TO BE OUT OF LIMITS. CUT OUT DAMAGED SHEAR TIE, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-4. 2 L 7 3 4F A3WE 2001072700246 20010727 00246 NM 2001 7 27 UPS01236172 1 20010625 A 3350 BATTERY PACK BOEING 727 727185C 138406N NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACKS, OPS NORMAL. 2 L 7 3 4F A3WE 2001072700247 20010727 00247 NM 2001 7 27 UPS01236179 1 20010614 A 5312 65C15764139119 BULKHEAD BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE:C, AFT PRESSURE BULKHEAD BS 1183 CRACK OF FWD FLANGE OF BL 17.8 LEFT VERTICAL BEAM AT WL 273 APPROX. RE PAIRED/ MODIFIED PER EO B727-5310-11743-B APP C AND E. 2 L 7 3 4F A3WE 2001072700248 20010727 00248 NM 2001 7 27 UPS01236181 1 20010613 A 5330 DOUBLER BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE:C, CRACK FOUND IN SKIN DOUBLER AT F+N WINDOW POST RT AT WINDOW CUTOUT, RADIUS AT POINT E THROUGH XRAY IN SPECTION. REPAIR CARRIED OUT PER UPS EO B727-5310-0012 APPENDIX D. 2 L 7 3 4F A3WE 2001072700249 20010727 00249 EA 2001 7 27 COMA0160509 1 20010725 A 2750 852D10011 ACTUATOR CNDAIR CL600 CL6002B19 EA BINDS A COMA O OTHER O OTHER AP APPROACH 1 SO 01 934CA 15885 7042 DURING APPROACH INTO CVG FLAP FAIL MESSAGE APPEARED AT 41 DEGREES.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "SECOND EVENT" MAINTENANCE ACTION, PARAGRAPH (B)3(D AND E)4. REPLACED #1 FLAP ACTUATOR FOR THE RIGHT SIDE. 2 L 7 2 4F RT A21EA 2001072700250 20010727 00250 NM 2001 7 27 UPS01236182 1 20010613 A 5754 RIB BOEING 727 72722C 138400F NM L/E SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE:C, NUMBER ONE SLAT HAS CRACK IN RIB O/B OF I/B TRACK. REPAIRED IAW SRM 57-50-3. 2 L 7 3 4F A3WE 2001072700251 20010727 00251 NM 2001 7 27 UPS01236412 1 20010706 A 5310 FRAME BOEING 727 72727C 138400J NM LH WHEEL WELL CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 914UP 19246 INSPECTION TYPE:C LH WHEEL WELL TOP OB EXPOSED PORTION OF BS 930 FRAME IS CRACKED IB S IDE TOP INSTALL REPAIR AS PER REPAIR ORDER AVHM 233RO-1. ENGINEERING FILE NO 727-53-20023. MAT USED 310 1/2 HD .080 BOTTOM DOUBLER 15X8" TOP DOU BLE R 6X6", TOP STRAP 20X1 2 L 7 3 4F A3WE 2001072700252 20010727 00252 NM 2001 7 27 UPS01236413 1 20010711 A 5320 FLOOR SUPPORT BOEING 727 72727C 138400J NM LAV FLOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 914UP 19246 INSPECTION TYPE:N/A LAV FLOOR SUPPORT CORRODED RBL 40 BS290 TP BS 312 REMOVED CORROSION AT LAV FLOOR SUPPORT RBL 40 BS290 TO BS 312 MATERI AL LOSS .050 FOUND OUT OF LIMITS AS PER B727 SRM 51-30-02 REPLACED F LOOR MATERIAL USE 60-8265 T ANGLE 8" TREAT AND PRIMED PER B727-SRM 5 1-10-1 2 L 7 3 4F A3WE 2001082400237 20010824 00237 NM 2001 8 24 UPS01536406 1 20010725 A 2730 COMPUTER BOEING 757 75724APF 1384969 NM COCKPIT FAULTY A IPXA K NONE F FLT CONT AFFECTED LD LANDING 1 SO 01 458UP 25479 INSPECTION TYPE:N/A PILOT REPORT, YOKE STIFF IN PITCH MODE. ACCOMPLISHED FIM 27-31-00 FIG 105 ELEV CTRLS BINDING. REMOVE D AND REPLACED ELEV FEEL COMPUTER PER MM 27-31-19; ELEVATOR SYS PASSED THE ELEV FEEL SYS FORCES TEST ACFT OK FOR SERVICE . 2 L 7 2 4F RT A2NM 2001072700253 20010727 00253 NM 2001 7 27 UPS01236183 1 20010614 A 5753 65216518 ATTACH FITTING BOEING 727 72722C 138400F NM FLAP TRACK CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE:C, NR 5 FLAP TRACK FWD ATTACH LUG HAS CORROSION ON BORE LANDING GEAR FWD TRUNNION SUPPORT BEARING PIN. ATTACH LUG REPLACED. 2 L 7 3 4F A3WE 2001072700254 20010727 00254 EA 2001 7 27 COMA0160510 1 20010725 A 2750 85D100MD91 ACTUATOR CNDAIR CL600 CL6002B19 EA BINDS A COMA O OTHER O OTHER AP APPROACH 1 SO 01 934CA 13761 7042 DURING APPROACH INTO CVG FLAP FAIL MESSAGE APPEARED AT 41 DEGREES.COMPLIED WTIH AD 98-20-01 FLAP CAUTION MESSAGE "SECOND EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 3(D AND E) 4. REPLACED #2 FLAP ACTUATOR FOR THE RIGHT SIDE. 2 L 7 2 4F RT A21EA 2001072700255 20010727 00255 NM 2001 7 27 UPS01236190 1 20010616 A 3211 659999091726 TRUNNION BOEING 727 72722C 138400F NM RT MLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE:C, RT MLG TRUNNION FITTING HAS CORROSION AND SUSPECT CRACKING AROUND INBD SPECIAL STUD HOLE ON INBD FLAN GE. TRUNNION FITTING REPLACED. 2 L 7 3 4F A3WE 2001072700256 20010727 00256 2001 7 27 UPS01236193 4 20010626 A 3418 WIRE BOEING 727 7272A1 138407F NM STALL WARNING BROKEN A IPXA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 01 213UP 21341 INSPECTION TYPE:N/A AT ROTATION STICK SHAKER BEGAN AND CONTINUED UNTIL AIRCRAFT LANDED AND NOSE WHEEL TOUCHED DOWN. REP AIRED BROKEN WIRE W1129-301-22R AT STA-560 PER WDM-20-30-12. OP CHECKED STALL WARNING SYSTEM PER MM 34-18-00. OPS CHEC KS GOOD. 2 L 7 3 4F A3WE 2001072700257 20010727 00257 NM 2001 7 27 0102596306 1 20010722 A 2910 HYDRAULIC LINE BOEING 747 747451 1384940 NM CASE DRAIN MOD RUPTURED A NWAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 GL 01 666US 23821 DURING CLIMB, THE AIRCRAFT LOST THE NBR 4 HYDRAULIC SYSTEM FLUID QUANTITY AND PRESSURE. CREW DECLARED AN EMERGENCY AND R ETURNED TO MNL AND LANDED WITHOUT INCIDENT. REPLACED THE HYDRAULIC RETURN LINE BETWEEN THE CASE DRAIN MODULE AND HEAT EXCHANGER, CASE DRAIN MODULE, ENGINE DRIVEN HYDRAULIC PUMP, AND AIR DRIVEN HYDRAULIC PUMP. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2001072700258 20010727 00258 2001 7 27 UPS01236195 4 20010626 A 3418 WIRE BOEING 727 7272A1 138407F NM STALL WARNING BROKEN A IPXA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 213UP 21341 INSPECTION TYPE:C, AT ROTATION STICK SHAKER BEGAN AND CONTINUED UNTIL AIRCRAFT LANDED AND NOSE WHEEL TOUCHED DOWN. REPA IRED BROKEN WIRE W1129-301-22R AT STA 560 PER WDM 20-30-12 OP CHECKED STALL WARNING SYSTEM PER MM 34-18-00, OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2001072700259 20010727 00259 EA 2001 7 27 COMA0160511 1 20010725 A 2750 853D10012 ACTUATOR CNDAIR CL600 CL6002B19 EA LEAKING A COMA O OTHER O OTHER AP APPROACH 1 SO 01 934CA 11644 7042 DURING APPROACH INTO CVG FLAP FAIL MESSAGE APPEARED AT 41 DEGREES.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "SECOND EVENT" MAINTENANCE ACTION, PARAGRAPH (B)3(D AND E)4. REPLACED THE #3 LEFT FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2001072700261 20010727 00261 EA 2001 7 27 COMA0160512 1 20010725 A 5300 60034017351 ANGLE CNDAIR CL600 CL6002B19 EA CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 963CA 11979 7127 FORWARD J-ANGLE AT FS 280 BETWEEN LBL9 AND RBL9 CORRODED.REMOVED AND REPLACED I/A/W WVAC EO 601R-53-2576. 2 L 7 2 4F RT A21EA 2001072700262 20010727 00262 EA 2001 7 27 COMA0160513 1 20010725 A 5300 601R31527221 ANGLE CNDAIR CL600 CL6002B19 EA CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 963CA 11979 7127 THRESHOLD SUPPORT ANGLES AT PAX DOOR CORRODED.REMOVED AND REPLACED I/A/W WVAC EO 601R-53-2575. 2 L 7 2 4F RT A21EA 2001072700263 20010727 00263 EA 2001 7 27 COMA0160514 1 20010725 A 5300 601R31527141 CHANNEL CNDAIR CL600 CL6002B19 EA CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 963CA 11979 7127 FORWARD AND AFT PAX DOOR U-CHANNELS CORRODED.REMOVED AND REPLACED U-CHANNELS I/A/W WVAC EO 601R-53-2584. 2 L 7 2 4F RT A21EA 2001072700264 20010727 00264 EA 2001 7 27 COMA0160515 1 20010723 A 2750 601R580071 HARNESS CNDAIR CL600 CL6002B19 EA CORRODED A COMA O OTHER S AFFECT SYSTEMS CR CRUISE 1 SO 01 937CA 7044 FLAPS FAILED DURING CRUISE FLIGHT.REPLACED THE R/H BPSU WIRING HARNESS. 2 L 7 2 4F RT A21EA 2001072700265 20010727 00265 EA 2001 7 27 COMA0160516 1 20010725 A 5300 601R3866949 DOUBLER CNDAIR CL600 CL6002B19 EA CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 926CA 18280 7027 DOUBLER P/N 601R38669-49 FWD OF SERVICE DOOR IS CORRODED.REMOVED AND REPLACED I/A/W WVAC EO 601R-53-2587. 2 L 7 2 4F RT A21EA 2001072700266 20010727 00266 NM 2001 7 27 UPS01236216 1 20010630 A 2433 TRANSFORMER BOEING 727 72722C 138400F NM COCKPIT MALFUNCTIONED A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 942UP 19101 INSPECTION TYPE:N/A, SMELLED SMOKE IN THE COCKPIT THEN FOUND NR 1 TR BREAKER POPPED. *S/D* REMOVED AND REPLACED NR 1 T R CHECKS GOOD IAW MM 24-30-51. THIS CLEARS M218279. 2 L 7 3 4F A3WE 2001072700267 20010727 00267 NM 2001 7 27 UPS01236244 1 20010705 A 3350 LIGHT BOEING 727 72751C 1384015 NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE:PFLT COCKPIT EMERGENCY LIGHT ABOVE DOOR VERY DIM. REMOVED AND REPLACED BATTERIES, OPS CHECK OK AS PER M M 33-50-01. 2 L 7 3 4F A3WE 2001072700268 20010727 00268 EA 2001 7 27 COMA0160517 1 20010725 A 5300 60034017373 ANGLE CNDAIR CL600 CL6002B19 EA CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 926CA 18280 7027 VERTICAL J ANGLE CLIPS LOCATED INSIDE CBP1/CBP2 AT BL9 LEFT AND RIGHT ARE CRACKED.REMOVED AND REPLACED I/A/W WVAC EO 601 R-53-2586. 2 L 7 2 4F RT A21EA 2001072700269 20010727 00269 EA 2001 7 27 COMA0160518 1 20010725 A 5300 601R3114863 THRESHOLD CNDAIR CL600 CL6002B19 EA CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 926CA 18280 7027 LBL42 THRESHOLD JUST AFT OF PAX DOOR CORRODED.REMOVED AND REPLACED THRESHOLD WEB I/A/W WVAC EO 601R-53-2590A. 2 L 7 2 4F RT A21EA 2001072700270 20010727 00270 NM 2001 7 27 UPS01236259 1 20010620 A 5311 FRAME BOEING 727 72721C 138400M NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 INSPECTION TYPE:C, LEFT WW FRAME 930 HAS PREVIOUS REPAIR WITH STOP HOLE, BUT IS CONTINUING UPWARDS AFTER STOP HOLE FRAME BELOW FLOOR BS 930. PERFORMED HFEC INSP ON I/B FLANGE AS PER NDT MANUAL PART 6-51-00-01 FIG 4. CRACK AT 1/4 BOLTS HOL E APPROX .5 INCH DOWN FROM PRESSURE WEB, INSTALL DOUBLER REPAIR AS PER EO B727-5310-2611. 2 L 7 3 4F A3WE 2001072700271 20010727 00271 EA 2001 7 27 COMA0160519 1 20010725 A 5300 60034017351 ANGLE CNDAIR CL600 CL6002B19 EA CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 926CA 18280 7027 FORWARD J ANGLE AT FS 280 BETWEEN LBL9 AND RBL9 CORRODED.REMOVED AND REPLACED FORWARD J ANGLE I/A/W WVAC EO 601R-53-2588 . 2 L 7 2 4F RT A21EA 2001072700272 20010727 00272 NM 2001 7 27 UPS01236261 1 20010620 A 5312 BULKHEAD BOEING 727 72721C 138400M NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 INSPECTION TYPE:C, RT WHEEL WELL FWD LOWER FRAME SHOWS CRACK DAMAGE AT BS 870 RBL 4.5. REMOVED FASTENERS AT DAMAGED ARE A SRM 51-30-2, CUTOUT WEB DAMAGED AREA APPROX 1 X 1.5 INCH SRM 51-40-2 AT BS 870 RBL 4.5 HFEC INSP CUT OUT IAW M/M 51-00 -00 PART 6 FIG 4. INSTALLED DOUBLER REPAIR AS PER B727 SRM 51-40-2 INSTALLED EXTRUDED REPAIR AT RT W/W LOWER FRAME RBL 4.5 AS PER B727 SRM-51-40-4 FIG 1. 2 L 7 3 4F A3WE 2001072700273 20010727 00273 EA 2001 7 27 COMA0160521 1 20010725 A 2750 FLAP CNDAIR CL600 CL6002B19 EA A COMA O OTHER O OTHER DE DESCENT 1 SO 01 938CA 7046 DURING DESCENT INTO GRR FLAP FAIL MESSAGE APPEARED AT 42 DEGREES.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIRST E VENT" MAINTENANCE ACTION, PARAGRAPH (B)1,2,3 (A,B,C AND E). FLAP SYSTEM WAS RESET. 2 L 7 2 4F RT A21EA 2001072700274 20010727 00274 NM 2001 7 27 UPS01236283 1 20010703 A 5310 STRUCTURE BOEING 727 72727C 138400J NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 910UP 19117 INSPECTION TYPE:C, SUSPECT CRACK AT FASTENER HOLE BS 474 STR 5R. REPAIR CARRIED OUT IAW SRM 53-30-3. 2 L 7 3 4F A3WE 2001072700275 20010727 00275 EA 2001 7 27 COMA0160522 1 20010724 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 967CA 7134 WITH EMERGENCY LIGHTS ARMED, THE OFF INDICATION IS ILLUMINATED.DEFERRED MAINT PER MEL. 2 L 7 2 4F RT A21EA 2001072700276 20010727 00276 EA 2001 7 27 COMA0160504 1 20010725 A 2750 857SD10015 DRIVE SHAFT CNDAIR CL600 CL6002B19 EA BINDS A COMA O OTHER O OTHER AP APPROACH 1 SO 01 934CA 7042 DURING APPROACH INTO CVG FLAP FAIL MESSAGE APPEARED AT 41 DEGREES.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "SECOND EVENT" MAINTENANCE ACTION, PARAGRAPH (B)3 AND (D AND E)4. REPLACED #3 FLEX DRIVE FOR THE RIGHT SIDE. 2 L 7 2 4F RT A21EA 2001072700277 20010727 00277 NM 2001 7 27 UPS01236284 1 20010701 A 5320 ANGLE BOEING 727 72727C 138400J NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 909UP 19115 INSPECTION TYPE:C, RT MLG SUPPORT ANGLE CORRODED AT PRESSURE DECK SURFACE 2 AREAS, RBL 23 BS 880 TO 882. RT MLG SUPPOR T ANGLE REPLACED IAW SRM 51-40-4. 2 L 7 3 4F A3WE 2001072700278 20010727 00278 EU 2001 7 27 MALA010578 1 20010723 A 3610 HE832731 ISOLATION VALVE BAC 146 AVRO146RJ85A 1500097 EU DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 501XJ E2208 DURING FLIGHT #3622 TO SDF YELLOW HYDRAULIC HI TEMP LIGHT ILLUMINATED. QHR WITH ENGINE #2 PUMP OFF HIGH TEMP WENT OUT. A/C DIVERTED TO CVG. MAINTENANCE SWAPPED YELLOW AND GREEN TEMP SWITCHES IAW AMM 29-33-11. PN HE83273-1 REMOVED AND REPLA CED YELLOW ISOLATION VALVE PN HTE9531-3, SN/OFF FRTR010AW SN/ON 988VB113 IAW AMM 29-10-14 OPS AND LEAK CHECK GOOD. 2 H 7 4 4F RT A49EU 2001073000001 20010730 00001 SW 2001 7 30 WP012001B2838 1 20010522 A 6730 MS995404 PLUG BELL 206 206L1 1182107 SW ALLSN 250C 250C28 03013 GL M/R SERVO CRACKED B XJ2R K NONE O OTHER IN INSP/MAINT 1 WP 01 104HC 3581 45500 RECEIVED SERVO PN 206-076-062-003 SN RH1269 FOR OVERHAUL AND FOUND DURING EVALUATION AFTER DISASSEMBLY PN MS9954-04 PLUG CRACKED UNDER THE HEAD. 1 G 7 1 3U 3 U H2SW E1GL 2001073000002 20010730 00002 SW 2001 7 30 WP012001B2839 1 20010522 A 2913 NAS1351332P SCREW BELL 212 212 1181420 SW HYD PUMP CORRODED B XJ2R K NONE O OTHER IN INSP/MAINT 1 WP 01 181W 3764 35058 RECEIVED HYDRAULIC PUMP PN 212-076-011-101, SN 253750 FOR OVERHAUL WITH THE FOUR SCREWS HOLDING THE PORT CAP THE HEADS W ERE MISSING PN NAS1351-3-32P. THE SCREW SHANK SHOW SIGNS OF HYDROGEN EMBRITTLEMENT AND RUST. 1 G 7 1 4U H4SW 2001073000003 20010730 00003 NE 2001 7 30 WPO12001B2579 2 20010416 A 7532 0292153330 SLEEVE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE BLEED VALVE WORN A K NONE O OTHER IN INSP/MAINT 1 WP 13 223LA 999 609 3278 9670 SB CALLS FOR THE INSTALLATION OF A SLEEVE IN THE BLEED VALVE BOSS. THIS SLEEVE DEVELOPED ROTATIONAL MOVEMENT AND CAUSED WEAR DAMAGE TO ITSELF, THE BOS ON M02, AND TO THE BLEED VALVE. THIS SLEEVE WAS INSTALLED AT TIME OF MANUFACTURE. 1 G 7 1 3U 3 U H9EU E19EU 2001073000004 20010730 00004 EU 2001 7 30 XSF2001F00000 1 20010523 A 2432 23761 BATTERY SNIAS 350 AS350B2 8680813 EU TAILBOOM FAILED E XSFA O OTHER M J OVER TEMP WARNING INDICATION AP APPROACH 1 WP 13 964SA 2931 AIRCRAFT WAS ON FINAL APPROACH TO AIRPORT WHEN BATTERY OVER TEMP LIGHT ILLUMINATED. PILOT TURNED OFF GENERATOR SYSTEM A ND LANDED. THE BATTERY WAS DISCONNECTED AND ALLOWED TO COOL. BATTERY WAS REPLACED WITH A SERVICEABLE UNIT. INSPECTION OF REMOVED BATTERY INDICATED LOW WATER LEVELS AND ONE DEAD CELL. AIRCRAFT HAD SAT FOR SEVERAL MONTHS WITHOUT BEING OPE RATED, THEN RETURNED TO HEAVY, DAILY USAGE. RECOMMEND MORE FREQUENT CONDITION CHECKS OF BATTERIES INSTALLED IN AIRCRAFT . 1 G 7 1 3U H9EU 2001073000005 20010730 00005 NM 2001 7 30 ANCF200100011 1 20010522 A 2612 0202KOS600 HARNESS BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E437 54555 NE LT ENGINE CHAFED W ANCF E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 23 321LF 26269 30711 LEFT ENGINE FIRE WARNING WITH EICAS MESSAGE “LT ENGINE FIRE”, FIRE INDICATION STOPPED WHEN FIRE SWITCH PULLED. CORRECTI VE ACTION:THE FIRE DETECTOR HARNESS WERE CHECKED AND FOUND CHAFING, IT WAS ISOLATED, THE TURBINE OVERHEAT SWITCH S10140 WAS FOUND GROUNDED AND THE RESISTANCE ABOVE 20 OHMS IT WAS REPLACED, LEFT POWER PLANT WAS CHECKED AFTER IN-FLIGHT SHUT D OWN, NO EVIDENCE OF FIRE WAS FOUND, RUN UP TEST WAS ACCOMPLISHED IAW AMM 71-00-00-6 AND 26-13-01, TASK CARD 71-00-206-01 5. 2 L 7 2 4F 4 F RT A2NM E12EU 2001073000010 20010730 00010 CE 2001 7 30 CA010523014 1 20010428 A 3230 CONNECTOR BEECH 200 B200C 1152924 CE PWA PT6 PT6A42 52043 NE PRESSURE SWITCH DAMAGED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 7705 (CAN) AFTER TAKEOFF FLT CREW REPORTED THEY WERE UNABLE TO GET L/G TO RETRACT FULLY, OR EXTEND TO DOWN POSITION. ALL C/BS WERE CHECKED TO NO AVAIL. THE GEAR WAS EXTENDED BY USING THE EMERGENCY BLOW DOWN PROCEDURE. THREE GREEN INDICATORS WERE ATTAINED AND VISUALLY CONFIRMED FROM THE GROUND. THE AIRCRAFT LANDED NORMALLY. UPON INSPECTING THE SYSTEM, IT WAS FOUND THAT THE HYD PRESSURE SWITCH HAD A BROKEN PIN. THIS OPEN CIRCUIT SIMULATED THE SYSTEM AS BEING AT OPERATING PRESSURE.GE AR CHECKED OK AFTER SWITCH REPLACEMENT. 1 L 7 2 4T 4 T A24CE E4EA 2001082000184 20010820 00184 NM 2001 8 20 01FDEA00612 1 20010724 A 5311 FRAME DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 616FE 48747 LT FRAME AT BS 1621 STR 12 FOUND 3 INCH CRACK. *S/D* REMOVED AND REPLACED FRAME PER SRM 53-30-30 FIG 1 VOL 1. 2 L 7 3 4F RT A22WE 2001073000016 20010730 00016 EU 2001 7 30 UPS01136160 1 20010622 A 3240 BRAKE ASSY AIRBUS A300 A300F4622R 3930360 EU RT MLG MALFUNCTIONED A IPXA K NONE M OVER TEMP LD LANDING 1 SO 01 129UP 0814 INSPECTION TYPE:N/A AIRCRAFT PULLED RIGHT ON LANDING WHEN BRAKES APPLIED AND RIGHT BRAKE TEMP ROSE TO 300 DEGREES MORE T HAN LEFT. PERFORMED INSPECTION/CHECK OF BRAKES AND ANTI SKID SYSTEM. BLED BRAKES. PERFORMED NORMAL HIGH SPEED TAXI CH ECK, USING GREEN AND YELLOW SOURCES. 2 L 7 2 4F RT A35EU 2001073000017 20010730 00017 NM 2001 7 30 UPS01236156 1 20010620 A 3230 UPLOCK BOEING 727 72731C 1384011 NM NLG FAILED A IPXA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 925UP 19230 INSPECTION TYPE:N/A NOSE LANDING GEAR TOOK 4 CYCLES TO EXTEND MANUAL EXTENSION WAS NO HE LP. *S/D* REF WDM 32-64-01 RE MOVED AND REPLACED WIRE BETWEEN S96 & S93. REMOVED AND ADJUSTED CORRECTLY. REMOVED AND REPLACED NLG LOCK ACT W/REF 32- 33-11, PERFORMED NLG MANUAL EXT W/REF 32-34-00. REMOVED AND REPLACED NLG LOCK SW W/REF MM 32-61-21, ALL ITEM R/R OPS CH ECK AND LEAK CHECK GOOD. NLG SWING AND MANUAL EXTENSION NORMAL, OK TO CONTINUE. 2 L 7 3 4F A3WE 2001073000018 20010730 00018 NM 2001 7 30 UPS01236254 1 20010709 A 2612 65249203 COMPUTER BOEING 727 72725C 138400H NM E/E BAY FAULTY A IPXA K NONE N FALSE WARNING AP APPROACH 1 SO 01 951UP 19850 INSPECTION TYPE:N/A, WHEN THROTTLES RETARDED AT 4000 FT ON APPROACH, WHEEL WELL FIRE LIGHT CAME ON. WENT OUT AS SOON AS GEAR DOWN. INSPECTED WHEEL WELL FIRE LOOP, FOUND AREA OF CONTACT ON AIRFRAME REPOSITION FIRE LOOP. CHANGED FIRE AND O VERHEAT COMPUTER AS A PRECAUTION. REMOVED AND REPLACED IAW MM-26-10, OPS NORMAL AT THIS TIME. 2 L 7 3 4F A3WE 2001073000022 20010730 00022 NM 2001 7 30 UPS01236286 1 20010704 A 5330 STRAP BOEING 727 72727C 138400J NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 909UP 19115 INSPECTION TYPE:C, DURING RECTIFICATION OF CORROSION BETWEEN TEAR STRAP SKIN AT BS 680 S6L, INDICATIONS OF SUSPECT CORRO SION ALSO FOUND AT BS 660 S4L TO S3L AT TEAR STRAP. NEW TEAR STRAP INSTALLED IAW SRM 53-30-4. 2 L 7 3 4F A3WE 2001073000023 20010730 00023 NM 2001 7 30 UPS01236289 1 20010702 A 5330 STRAP BOEING 727 72727C 138400J NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 909UP 19115 INSPECTION TYPE:C, SUSPECT CORROSION AT TEAR STRAP LOCATION BS 580 S4R TO S3R. REPAIR CARRIED OUT IAW SRM 51-10-6, SRM 53-30-3. 2 L 7 3 4F A3WE 2001073000024 20010730 00024 NM 2001 7 30 UPS01236299 1 20010629 A 5330 STRAP BOEING 727 72727C 138400J NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 909UP 19115 INSPECTION TYPE:C, SUSPECT CORROSION AT TEAR STRAP LOCATION BS 560 S4R TO S3R. REPAIR CARRIED OUT IAW SRM 51-30-2 & SRM 53-30-3. 2 L 7 3 4F A3WE 2001073000025 20010730 00025 NM 2001 7 30 UPS01236302 1 20010706 A 5312 PRESSURE PANEL BOEING 727 72727C 138400J NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 909UP 19115 INSPECTION TYPE:C, CRACKS FOUND AT 2 FASTENER HOLES AT PRESSURE DECK UPPER SURFACE AT BS 880 - 890 RBL 23. REPAIR CARRI ED OUT IAW DRAWING 65-89360 & SRM 53-10-9 & SRM 51-30-2. 2 L 7 3 4F A3WE 2001073000026 20010730 00026 NM 2001 7 30 UPS01236304 1 20010702 A 5320 WEB BOEING 727 72727C 138400J NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 909UP 19115 INSPECTION TYPE:C, CORROSION ON CABIN FLOOR WEB FWD OF BS 1183 BLK AT BBL 15L. REPAIR CARRIED OUT IAW SRM 51-40-2. 2 L 7 3 4F A3WE 2001073000027 20010730 00027 NM 2001 7 30 UPS01236310 1 20010629 A 5330 STRAP BOEING 727 72727C 138400J NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 910UP 19117 INSPECTION TYPE:C, SUSPECT CORROSION AT TEAR STRAP LOCATION BS 680 BETWEEN S6L AND S5L. DAMAGE REPAIRED IAW SRM PROCEDU RES. 2 L 7 3 4F A3WE 2001073000028 20010730 00028 NM 2001 7 30 UPS01236312 1 20010702 A 5312 PRESSURE PANEL BOEING 727 72727C 138400J NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 909UP 19115 INSPECTION TYPE:C, DURING NDT INSP OF RT MLG WHEEL WELL PRESSURE WEB CRACK WAS FOUND ON WEB AT BS 940 RBL 33 APPROX. RE PAIR CARRIED OUT IAW SRM 51-10-01, 51-30-2 & DRAWING 659360. 2 L 7 3 4F A3WE 2001073000029 20010730 00029 NM 2001 7 30 UPS01236368 1 20010629 A 5330 STRAP BOEING 727 72727C 138400J NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 910UP 19117 INSPECTION TYPE:C, SUSPECT CORROSION AT TEAR STRAP LOCATION BS 560 S4R TO S3R. REPAIR CARRIED OUT IAW SRM 51-30-2 & SRM 32-30-3. 2 L 7 3 4F A3WE 2001073000030 20010730 00030 NM 2001 7 30 UPS01236370 1 20010701 A 5320 SUPPORT BOEING 727 72727C 138400J NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 910UP 19117 INSPECTION TYPE:C, RT MLG SUPPORT ANGLE CORRODED AT PRESSURE DECK SURFACE 2 AREAS, RBL 23 BS 880 TO 882. RT MLG SUPPOR T ANGLE REPLACED IAW SRM 51-40-4. 2 L 7 3 4F A3WE 2001073000031 20010730 00031 NM 2001 7 30 UPS01236371 1 20010702 A 5330 STRAP BOEING 727 72727C 138400J NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 910UP 19117 INSPECTION TYPE:C, SUSPECT CORROSION AT TEAR STRAP LOCATION BS 580 S4R TO S3R. REPAIR CARRIED OUT IAW SRM 51-10-6, SRM 32-30-3. 2 L 7 3 4F A3WE 2001073000032 20010730 00032 NM 2001 7 30 UPS01236372 1 20010702 A 5320 WEB BOEING 727 72727C 138400J NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 910UP 19117 INSPECTION TYPE:C, CORROSION ON CABIN FLOOR WEB FWD OF BS 1183 BLK AT BBL 15L. REPAIR CARRIED OUT IAW SRM 51-40-2. 2 L 7 3 4F A3WE 2001073000033 20010730 00033 NM 2001 7 30 UPS01236380 1 20010720 A 3350 LIGHT BOEING 727 7272A1 138407F NM CREW DOOR MALFUNCTIONED A IPXA K NONE O OTHER UK UNKNOWN 1 SO 01 213UP 21341 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT OVER CREW ENTRY DOOR ILLUM IN FLIGHT. *S/D* REMOVED AND REPLACED ENTRY DOOR E MERGENCY EXIT LIGHT GROUND OPS NORMAL. 2 L 7 3 4F A3WE 2001073000034 20010730 00034 NM 2001 7 30 UPS01236385 1 20010704 A 5330 STRAP BOEING 727 72727C 138400J NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 910UP 19117 INSPECTION TYPE:C, DURING RECTIFICATION OF CORROSION BETWEEN TEAR STRAP SKIN AT BS 680 S6L INDICATIONS OF SUSPECT CORROS ION ALSO FOUND AT BS 660 S4L TO S3L AT TEAR STRAP. NEW TEAR STRAP INSTALLED IAW SRM 53-30-4. 2 L 7 3 4F A3WE 2001073000035 20010730 00035 NM 2001 7 30 UPS01236388 1 20010706 A 5312 PRESSURE PANEL BOEING 727 72727C 138400J NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 910UP 19117 INSPECTION TYPE:C CRACKS FOUND AT 2 FASTENER HOLES AT PRESSURE DECK UPPER SURFACE AT BS 880 - 890 RBL 23. REPAIR CARRIE D OUT IAW DRAWING 65-89360 & SRM 53-10-9 & SRM 51-30-2. 2 L 7 3 4F A3WE 2001073000037 20010730 00037 NM 2001 7 30 UPS01236390 1 20010702 A 5312 PRESSURE PANEL BOEING 727 72727C 138400J NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 910UP 19117 INSPECTION TYPE:C, DURING NDT INSP OF RT MLG WHEEL WELL PRESSURE WEB CRACK WAS FOUND ON WEB AT BS 940 RBL 33 APPROX. RE PAIR CRACKED OUT IAW SRM 51-10-01, 51-30-2 & DRAWING 659360. 2 L 7 3 4F A3WE 2001073000040 20010730 00040 NM 2001 7 30 UPS01436030 1 20010608 A 3350 BATTERY PACK BOEING 747 747259B NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 527UP 21730 INSPECTION TYPE:N/A, EMERGENCY LIGHT INOP IN UPPER DECK MOST AFT LIGHT. RELAMPED, NO HELP. REPLACED EMERGENCY EXIT LIG HT BATTERY PACK AND CKS GOOD. 2 L 7 4 4F RT A20WE 2001073000042 20010730 00042 CE 2001 7 30 CA010529011 1 20010327 A 5711 AG751204 SPAR BOEING 75 A75N1 1380134 CE CONT R670 R670* 17016 SO RT WING CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 577 (CAN) AIRCRAFDT HEAVILY INSPECTED FOLLOWING GROUND LOOP. CRACK DISCOVERED PROPOGATING FROM AILRON CENTRE HINGE BOLT HOLE AND EXTENDING FOR SEVERAL FEET FOLLOWING THE GRAIN LINE. WING WAS REMOVED FROM AIRCRAFT, AND REAR SPAR WAS SPLICE REPAI RED.. . . . 1 Q 7 1 3R 3 R A743 E162 2001073000043 20010730 00043 NM 2001 7 30 UPS01436077 1 20010530 A 5415 FASTENER BOEING 747 747123 1384873 NM NR 4 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C NR 4 PYLON ATTACH FITTING TAPER LOCK FASTENER FOUND 4EA CRACKED. REF ATTACHED SKETCH. LOCKS REPLAC ED AS PER EO 747-5740-12227-A. 2 L 7 4 4F A20WE 2001073000044 20010730 00044 NM 2001 7 30 UPS01436078 1 20010604 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C, M/D - BS 1562 - 1564 RBL 97 SEAT TRACK FOUND CRACKED. M/D BS 1550 - 1630 RBL 98 TIE DOWN TRACK REPAI RED AS PER SRM 53-10-05 FIGURE 1. 2 L 7 4 4F A20WE 2001073000046 20010730 00046 CE 2001 7 30 CA010529014 1 20010427 A 6120 3011543 BRACKET CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE MCAULY 3AF34C 3GFR34C703 GL PROPELLER MISSING W K NONE O OTHER IN INSP/MAINT 1 CA 287 (CAN) DURING INSPECTION THE GUIDE PIN/BRACKET ASSEMBLY WHICH IS USED TO KEEP THE CARBON BLOCK IN THE BETA RING WAS FOUND MISSING. WITH ENOUGH PLAY IN THE SYSTEM THIS MIGHT ALLOW THE BLOCK TO COME OUT OF THE RING. THIS WOULD AFFECT PROPELLER OPERATION IN THE BETA RODE ALLOWING THE BLADE ANGLE TO EXCEED THE PRIMARY BLADE ANGLE (TO FINE OF A PITCH) IN LOW POWER OPERATION (I.E. DESCENT). THIS WOULD ALSO AFFECT REVERSE OPERATION. PART APPEARS TO BE MISSING SINCE AIRCRAFT WAS NEW. . 1 H 7 1 3T 3 T A37CE E4EA 5 C P60GL 2001073000047 20010730 00047 NM 2001 7 30 UPS01436079 1 20010604 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C M/D - BS 1598 - 1600 RBL 97 SEAT TRACK FOUND CRACKED. M/D BS 1550 - 1630 RBL 98 TIE DOWN TRACK REPAIR ED AS PER SRM 53-10-05 FIGURE 1 WORK DETAIL REF NRC 6286 CWS 303296 SRWS 918522. 2 L 7 4 4F A20WE 2001073000049 20010730 00049 NM 2001 7 30 UPS01436080 1 20010604 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C M/D - BS 1818 RBL 97 SEAT TRACK FOUND CRACK. M/D - BS 1750 - 1950 RBL 98 TIE DOWN TRACK REPAIRED AS P ER SRM 53-10-05 FIGURE 1. WORK DETAILS REF NRC 6282 CWS 326457, 334309. 2 L 7 4 4F A20WE 2001073000050 20010730 00050 NM 2001 7 30 UPS01436081 1 20010604 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C, M/D - BS 1800 RBL 97 SEAT TRACK FOUND CRACK. M/D BS 1750 - 1950 RBL 98 TIE DOWN TRACK REPAIRED AS PE R SRM 53-10-05 FIGURE 1. WORK DETAILS REF NRC 6282 CWS 326457, 334309. 2 L 7 4 4F A20WE 2001073000052 20010730 00052 NM 2001 7 30 UPS01436082 1 20010604 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C M/D - BS 1893 - 1896 RBL 97 SEAT TRACK FLANGE FOUND CRACKED. M/D - BS 1750 - 1950 RBL 98 TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIGURE 1. WORK DETAILS REF NRC 6282 CWS 326457, 334309 SRWS 918557. 2 L 7 4 4F A20WE 2001073000054 20010730 00054 NM 2001 7 30 UPS01436083 1 20010604 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C M/D - BS 1880 RBL 97 SEAT TRACK FOUND CRACKED. M/D BS 1750 - 1950 RBL 98 TIE DOWN TRACK REPAIRED AS P ER SRM 53-10-05 FIGURE 1. WORK DETAILS REF NRC 6282 CWS 326457, 334309 SRWS 918557. 2 L 7 4 4F A20WE 2001073000055 20010730 00055 NM 2001 7 30 CA010529018 1 20010429 A 3213 66132651 NUT BOEING 65196604 BOEING 727 72722C 138400F NM PWA JT8 JT8D7A 52053 NE SUPPORT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 12432 018YS46 (CAN) LT MAIN GEAR OLEO WOULD NOT HOLD AIR CHARGE. OLEO FOUND LOW SEVERAL TIMES AND RECHARGED. UPON INVESTIGATION IT WAS FOUND THAT THE RETAINING NUT FOR THE UPPER OLEO SUPPORT TUBE WAS CRACKED, CAUSING AIR LEAKAGE. FURTHER INVESTIGATION AL SO REVEALED CORROSION ON THE THREADS OF THE SUPPORT TUBE. SUPPORT TUBE AND NUT WERE REPLACED.. . 2 L 7 3 4F 4 F A3WE E2EA 2001073000057 20010730 00057 NM 2001 7 30 UPS01436084 1 20010604 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C M/D - BS 1780 RBL 97 SEAT TRACK FOUND CRACK. M/D BS 1750 - 1950 RBL 98 TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1. 2 L 7 4 4F A20WE 2001073000059 20010730 00059 NM 2001 7 30 UPS01436085 1 20010604 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C, M/D - BS 2170 LBL 11 O/B SEAT TRACK FLANGE CRACKED. M/D BS 2150 - 2190 LBL 11 TIE DOWN TRACK REPAIRE D AS PER SRM 53-10-05 FIGURE 14. 2 L 7 4 4F A20WE 2001073000062 20010730 00062 NM 2001 7 30 UPS01436086 1 20010531 A 5310 DOOR FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C, M/D - L5 DOOR FWD CUTOUT BETWEEN STR 24 & 25 CRACKED. REPAIRED AS PER SRM 53-10-04 FIG 34. 2 L 7 4 4F A20WE 2001073000063 20010730 00063 EU 2001 7 30 CA010530002 1 20010508 A 2750 274 CONTROLLER PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL TE FLAPS FAILED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA (CAN) FLAPS WOULD NOT EXTEND. FOUND FLAP CONTROL CIRCUIT BREAKER POPPED. AIRCRAFT LANDED WITH ZERO FLAPS. FLAP CIRCUIT B REAKER RESET ON GROUND. FLAP CONTROL WARNING UNIT (FCWU) RESET. FLAP OPERATIONAL TEST, SATISFACTORY. FCWU MAINTENANCE CO DES READ FOR TROUBLESHOOTING. CONTINUE TO TROUBLESHOOT. . . 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001073000064 20010730 00064 NM 2001 7 30 UPS01436087 1 20010604 A 5313 LONGERON BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C M/D - BS 1960 - 1980 S2L STRINGER END FOUND CRACKED. M/D BS 1960 - 1980 STR 2L REPAIRED AS PER SRM 53 -10-03 FIGURE 4. 2 L 7 4 4F A20WE 2001073000066 20010730 00066 NM 2001 7 30 UPS01436088 1 20010531 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C FX EXTERIOR SKIN FOUND CHAFING MARK AT S40R BS 1920 AREA. FX EXTERIOR SKIN AT BS 1920 STR 40R REPAIR AS PER SRM 53-30-03 FIGURE 17. WORK DETAIL REFER CWS. 2 L 7 4 4F A20WE 2001073000067 20010730 00067 CE 2001 7 30 CA010530004 1 20010503 A 2752 BRUSHES CESSNA 210 210R 2073458 CE CONT O520 IO520L 17032 SO MCAULY D3A34 D3A34C404 GL TE FLAP MOTOR WORN W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 3570 (CAN) PILOT REPORTED HE HAD TO MAKE A FLAPLESS LANDING AS FLAPS WOULD NOT LOWER TO SELECTED POSITION ON APPROACH. NO MOV EMENT OF FLAPS NOTED BY VISUAL CHECK. INVESTIGATION REVEALED THAT THE FLAP MOTOR WAS RECEIVING POWER BUT NO MOVEMENT OF MOTOR SHAFT WAS NOTICED . MOTOR WAS REMOVED, INSPECTION REVEALED THAT THE MOTOR BRUSHES WERE EXCESSIVELY WORN CAUSING LI TTLE IF ANY CONTACT WITH MOTOR SLIP RING. MOTOR WAS REPLACED WITH SERVICEABLE SPARE AND FLAP SYSTEM CHECKS PERFORMED AS PER AIRCRAFT MAINTENANCE MANUAL. ALL FOUND SATISFACTORY.. 1 H 7 1 3O 3 O RT 3A21 E5CE 5 C P47GL 2001073000068 20010730 00068 NM 2001 7 30 UPS01436089 1 20010601 A 5320 CLIP BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C, LT BS 320 NOSE WHEEL WELL VERTICAL BEAM CLIP FOUND CRACKED AT NR 1 COUNT FROM TOP AS MARKED. LT BS 3 20 NOSE W/W VERTICAL BEAM NR 1 CRACKED CLIP REPLACED AS PER SRM 51-10-01 AND EO B747-5310-0574 APPROX D. 2 L 7 4 4F A20WE 2001073000069 20010730 00069 EU 2001 7 30 CA010530006 1 20010501 A 7931 315 INDICATOR PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL OIL PRESS MALFUNCTIONED W O OTHER N FALSE WARNING CR CRUISE 1 CA 234 (CAN) CREW REPORTED THAT THE ENGINE OIL PRESSURE INDICATION FLICKERED AND DROPPED TO ZERO, THEN CAME BACK TO NORMAL. A S ECOND FLICKER OF THE SAME NATURE REOCCURRED. THE INDICATION REMAINED NORMAL THEREAFTER. MAINTENACNE REMOVED THE EIS (ENG INE INSTRUMENTATION SYSTEM)PANEL, CLEANED PLUG P533, REINSTALLED PANEL AND SUBSEQUENT GROUND RUNS REVEALED NO FAULTS. TH E EIS PANEL HAD BEEN REPLACED FOR THE SAME SNAG ON 2001-01-19 AT 1745.1 HOURS. REPLACED ON 2000-11-29 SNAG ENTERED "EIS PANEL INTERMITTENT" AT 1648.6 HOURS. REPLACED ON 2000-10-27 UNKNOW REASON AT 1532.1 HOURS.. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001073000070 20010730 00070 NM 2001 7 30 UPS01436090 1 20010603 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C M/D - BS 2340 RBL 40 HAT SECTION FOUND CORRODED. M/D BS 2340 RBL 40 HAT SECTION REPLACED PER SRM 51-1 0-01 PG 8. 2 L 7 4 4F A20WE 2001073000071 20010730 00071 EU 2001 7 30 CA010530008 1 20010502 A 2434 9789601090 BRACKET PILATS 5243212158 PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL GEN BRUSHES WORN W K NONE O OTHER IN INSP/MAINT 1 CA 71 100041 (CAN) GENERATOR 2 WAS REMOVED TO PERFORM A GENERATOR 2 DRIVE INSPECTION, AS THE UNIT WAS ON THE BENCH, IT WAS QUITE CONV ENIENT TO INSPECT THE BRUSHES. THE BRUSHES WERE FOUND WITH EXCESSIVE WEAR GIVEN THE AMOUNT OF TIME SINCE INSTALLATION (7 1.0 HOURS). . . 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001073000072 20010730 00072 NM 2001 7 30 UPS01436091 1 20010531 A 5320 FLOOR SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C, FWD CARGO STA 1000 RBL 60 CABIN FLOOR SUPPORT FOUND CRACKED. FWD CARGO STA 1000 RBL 60 CABIN FLOOR S UPPORT REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001073000074 20010730 00074 NM 2001 7 30 UPS01436092 1 20010603 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C M/D - BS 1720 RBL 81 TO 95 FLOORBEAM UPPER CHORD UPPER AND LOWER SURFACE FOUND CORROSION. M/D FLOORBE AM AT BS 1720 RBL 68 - 120 REPAIRED PER SRM 51-40-04 FIG 1. 2 L 7 4 4F A20WE 2001073000075 20010730 00075 NM 2001 7 30 UPS01436093 1 20010603 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C M/D - BS 1904 TO 1910 RBL 97 SEAT TRACK FLANGE FOUND CORRODED. M/D BS 1750 - 1950 RBL 98 TIE DOWN TRA CK REPAIRED AS PER SRM 53-10-05 FIG 1. REF NRC 6282 CWS 326457, 334309. 2 L 7 4 4F A20WE 2001073000077 20010730 00077 EU 2001 7 30 CA010530010 1 20010502 A 2422 MGH182100 INVERTER AMD FALC20 FALCON20D5 2730003 EU GE CF700 CF7002D2 30010 NE NR 1 SHORTED W B A EMER. DESCENT UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CR CRUISE 1 CA 6910 (CAN) CABIN PRESSURIZATION IS AC POWERED FROM NR 1 INVERTER. WHEN NR 1 INVERTER FAILED, THE CREW HAD INDICATIONS IN THE COCKPIT OF LOSS OF PRESSURIZATION AND NR 1 INVERTER. THE CREW DID NOT SELECT THE STANDBY INVERTER TO THE NR 1 POSITION, WHICH RESULTED IN A LOSS OF CABIN PRESSURIZATION. ATTACHED WITH THIS REPORT IS A ROTABLE HISTORY AND COMPONENT STATUS OF THE INVERTER P/N MGH182-100 S/N AJ2326A. IT IDENTIFIES COMPLIANCE OF 300 HOUR BRUSH INSPECTION AND CONDITION MONITORIN G AS STATED BY CHAPTER 5 OF THE FALCON 20 MAINTENANCE MANUAL RECOMMENDATED TBOS AND AIRWORTHY LIMITATIONS. 2 L 7 2 4F 4 F RT A7EU E7EA 2001073000078 20010730 00078 WP 2001 7 30 CA010531002 1 20010423 A 2131 21011403 CONTROLLER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE CABIN FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) AT FLIGHT LEVEL 350, THE PRESSURE LIGHT WARNING CAME ON. THE QRH APPLIED, THE CABIN ALTITUDE WENT TO 10,000 FEET T HEN TO 11,000 FEET, THE CREW MANUALLY DEPLOYED THE MASKS. REPLACED BOTH AUTOMATIC CABIN PRESSURE CONTROLLER AND THE PASS ENGER OXYGEN CYLINDER ALSO CLEANED AND STOWED ALL OF THE OXYGEN MASKS. CABIN OXYGEN SYSTEM AND STATIC LEAK CHECK CARRIED OUT. . . 2 L 7 2 4F 4 F A6WE E2EA 2001073000079 20010730 00079 NM 2001 7 30 UPS01436095 1 20010603 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C M/D - BS 1603 TO 1610 RBL 97 SEAT TRACK FLANGE FOUND CORROSION. M/D BS 1550 - 1630 RBL 98 TIE DOWN TR ACK REPAIRED AS PER SRM 53-10-05 FIGURE 1. REF NRC 6286. 2 L 7 4 4F A20WE 2001073000080 20010730 00080 NM 2001 7 30 UPS01436096 1 20010603 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C M/D - BS 2040 LBL 11 - RBL 11 FLOORBEAM FOUND CORRODED. M/D FLOORBEAM AT BS 2040 LBL 2 - RBL 11.33 RE PAIRED PER SRM 51-40-04 FIG 1. 2 L 7 4 4F A20WE 2001073000082 20010730 00082 NM 2001 7 30 UPS01436107 1 20010603 A 5320 FLOOR SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C M/D - BS 1580 LBL 114 FLOOR SUPPORT CORROSION FOUND. M/D BS 1580 LBL 114 FLOOR SUPPORT REPAIRED PER S RM 51-40-03 FIG 1. 2 L 7 4 4F A20WE 2001073000085 20010730 00085 NM 2001 7 30 UPS01436108 1 20010614 A 5730 SKIN BOEING 747 747123 1384873 NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C, RHW FUEL TANK ACCESS PNL 652AB CUTOUT FOUND CORRODED. RHW FUEL TANK ACCESS PNL 652AB CUTOUT SKIN COR ROSION REMOVED NDT CRACK CHECK CARRIED OUT, NIL CRACK, SHOT PEEN CARRIED OUT AS PER RS R57-26-34665. 2 L 7 4 4F A20WE 2001073000087 20010730 00087 NM 2001 7 30 CA010531009 1 20010429 A 2913 SHAFT ABEX BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E437 54555 NE HYD PUMP SHEARED W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA MX369230 (CAN) DURING CRUISE FLIGHT CREW REPORTED R/H ENGINE HYDRAULIC PRESSURE LOW LIGHT CAME ON WITH ECIAS MESSAGE "R/H ENG EDP ". AIRCRAFT DIVERTED AND LANDED. R/H EDP FOUND SHAFT SHEARED, PUMP REPLACED, FILTERS REPLACED AND SYSTEM FLUSHED AS PER AMM 29-11-00 AND 29-11-05. AIRCRAFT RETURNED TO SERVICE.. . 2 L 7 2 4F 4 F RT A2NM E12EU 2001073000090 20010730 00090 NM 2001 7 30 UPS01436109 1 20010605 A 5320 SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C FX - BODY FAIRING SUPPORT FOUND CORRODED AT BS 880 BL 0 - LBL 45. LT BODY FAIRING SUPPORT STA 880 BET WEEN LBL 30 - LBL 50 REPAIRED PER SRM 53-50-05 FIG 2. 2 L 7 4 4F A20WE 2001073000092 20010730 00092 NM 2001 7 30 UPS01436110 1 20010605 A 5320 SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C FX - RT BODY FAIRING SUPPORT FOUND CORRODED AT BS 880 BL 0 - RBL 45. RT BODY FAIRING SUPPORT AT BS 88 0 BETWEEN BL 0 - RBL 45 REPAIRED PER SRM 53-50-04 FIG 2. 2 L 7 4 4F A20WE 2001073000095 20010730 00095 NM 2001 7 30 UPS01436111 1 20010602 A 5312 PRESSURE PANEL BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C, NOSE W/W TOP PNL WEB FOUND CRACKED AT STA 285 - 290 RBL 10 BWL 190 UPPER SURFACE. NOSE W/W TOP PANEL STA 285 - 290 RBL 10 BWL 190 CRACKED WEB REPAIRED AS PER RS R53-18-34659. 2 L 7 4 4F A20WE 2001073000096 20010730 00096 NM 2001 7 30 UPS01436113 1 20010603 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C, M/D - BS 2010 RBL 11 SEAT TRACK O/B FLANGE CORROSION FOUND. BS 1970 TO 2050 RBL 11 SEAT TRACK REPLAC EMENT PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2001073000097 20010730 00097 NM 2001 7 30 UPS01436114 1 20010603 A 5320 FLOOR SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C M/D - BS 2120 - 2150 RBL106 FLOOR SUPPORT CORROSION FOUND. M/D BS 2140 - 2150 RBL106 FLOOR SUPPORT RE PAIRED PER SRM 51-40-03 FIG 1. 2 L 7 4 4F A20WE 2001073000098 20010730 00098 NM 2001 7 30 CA010621008 1 20010613 A 5260 85210097105 HAND RAIL DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE AIRSTAIR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING ROUTINE INSPECTION IT WAS DISCOVERED THAT THE UPPER NEWELS IN BOTH THE FORWARD AND AFT HANDRAILS ON THE AIR STAIR DOOR WERE CRACKED ACROSS A LIGHTENING RADIUS AT THE INBOARD SECTION OF THE CASTING. THE CRACKED MEMBERS WERE REPLA CED AND THE AIRCRAFT RETURNED TO SERVICE. TTAF 35,370HRS, TCAF 47,337 CYCLES WC1770. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001073000099 20010730 00099 NM 2001 7 30 UPS01436115 1 20010604 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C M/D - BS 1740 RBL 11 SEAT TRACK FLANGE CRACKED. M/D BS 1730 - 1790 RBL 11 TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 14. 2 L 7 4 4F A20WE 2001073000100 20010730 00100 NM 2001 7 30 CA010621009 1 20010611 A 3250 73250021103 HOUSING DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE STEERING TILLER WORN W K NONE O OTHER IN INSP/MAINT 1 CA 26616 (CAN) DURING INVESTIGATION OF EXCESSIVE PLAY IN THE STEERING TILLER, IT WAS DISCOVERED THAT THE CENTERING SPRING P/N 732 50025-105 HAD WORN SUBSTANTIAL GROOVES INTO THE TILLER HOUSING P/N 73550021-103, CAUSING THE CENTERING ACTION POF THE SP RING TO BE LESS EFFECTIVE. THE HOUSING WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001073000101 20010730 00101 NM 2001 7 30 UPS01436116 1 20010603 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C M/D - BS 2260 RBL 22 FLOORBEAM CORROSION FOUND. M/D FLOORBEAM AT BS 2260 LBL 5 - RBL 48 REPAIRED PER SRM 51-40-04 FIG 1. 2 L 7 4 4F A20WE 2001081500164 20010815 00164 NM 2001 8 15 01FDEA00615 1 20010729 A 5311 FRAME BOEING 727 727247 138408F NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 FUSELAGE FRAME AT BS 560 HAS DENTS ON UPPER FLANGE ADJACENT TO STR 24L. *S/D* REMOVED AND REPLACED FRAME PER IAW SRM 5 1-40-3. 2 L 7 3 4F A3WE 2001081600173 20010816 00173 NM 2001 8 16 01FDEA00616 1 20010729 A 5311 FRAME BOEING 727 727247 138408F NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 DENT IN TOP FLANGE OF FRAME. *S/D* REMOVED AND REPLACED FRAME PER SRM 51-40-3. 2 L 7 3 4F A3WE 2001081500165 20010815 00165 NM 2001 8 15 01FDEA00617 1 20010729 A 5311 FRAME BOEING 727 727247 138408F NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 THREE DENTS IN TOP FLANGE OF BS 950F FRAME LBL 28-36, WL 150. *S/D* REMOVED AND REPLACED FRAME PER IAW SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2001081600174 20010816 00174 NM 2001 8 16 01FDEA00618 1 20010729 A 5311 FRAME BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 UPPER FLANGE OF BS 1050 FRAME HAS OPEN HOLE AND CORROSION UNDER LT FLOOR TO SIDEWALL SUPPORT. EXCEED SRM LIMITS PER 53- 10-01. *S/D* REMOVED AND REPLACED FRAME PER SRM 51-20-2, 51-40-3, 51-30-2. 2 L 7 3 4F A3WE 2001081700044 20010817 00044 NM 2001 8 17 01FDEA00619 1 20010729 A 5311 FRAME BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 UPPER FLANGE BS 1050 FRAME HAS OPEN HOLE WITH CORROSION UNDER RT FLOOR TO SIDEWALL SUPPORT. *S/D* REMOVED AND REPLACED FRAME PER SRM 51-40-3 FIG 1 & EA. 7-5310-58481. 2 L 7 3 4F A3WE 2001081500166 20010815 00166 NM 2001 8 15 01FDEA00620 1 20010729 A 5315 FLOORBEAM BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSION (C53-224-04) IN AND AROUND NUT PLATE HOLES ON LWR CHORD OF BS 1110 FLOORBEAM, RBL 12, 22, 32, WL 200. *S/D* REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8 FIG 8. 2 L 7 3 4F A3WE 2001081700045 20010817 00045 NM 2001 8 17 01FDEA00621 1 20010727 A 5314 KEELBEAM BOEING 727 727247 138408F NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 RIGHT KEEL BEAM HAS CRACK AT BS 870 LOWER CHORD VERTICAL FLANGE. *S/D* REMOVED AND REPLACED KEEL BEAM PER EA 7-5310-58 491. 2 L 7 3 4F A3WE 2001073000102 20010730 00102 NM 2001 7 30 CA010621011 1 20010608 A 3230 DSC252B4012 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE DRAG STRUT ACT LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) INVESTIGATING OF A HYDRAULIC LEAK IN THE NLG BAY RESULTED IN REPLACEMENT OF ONE OF THE DRAG STRUT ACTUATOR FLEX LI NES. 13348 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001073000103 20010730 00103 NM 2001 7 30 UPS01436118 1 20010604 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C M/D - BS 2180 - 2220 S2R STRINGER END FOUND CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4. 2 L 7 4 4F A20WE 2001073000104 20010730 00104 NM 2001 7 30 CA010621012 1 20010608 A 5260 85210097105 HAND RAIL DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE AIRSTAIR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING ROUTINE INSPECTION IT WAS DISCOVERED THAT THE UPPER NEWELS IN BOTH THE FORWARD AN AFT HANDRAILS ON THE AIRS TAIR DOOR WERE CRACKED ACROSS A LIGHTENING RADIUS AT THE INBOARD SECTION OF THE CASTING. THE CRACKED MEMEBERS WERE REPLA CED AND THE AIRCRAFT RETURNED TO SERVICE. TTAF35370HRS,TCAF47337CYCLES WC 1770. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001073000105 20010730 00105 NM 2001 7 30 UPS01436119 1 20010604 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C M/D - BS 2160 - 2180 S2R STRINGER END FOUND CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4. 2 L 7 4 4F A20WE 2001073000106 20010730 00106 NM 2001 7 30 CA010621013 1 20010611 A 3250 73250021103 HOUSING DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE STEERING TILLER WORN W K NONE O OTHER IN INSP/MAINT 1 CA 26616 (CAN) DURING INVESTIGATION OF EXCESSIVE PLAY IN THE STEERING TILLER, IT WAS DISCOVERED THAT THE CENTERING SPRING P/N 732 50025105 HAD WORN SUBSTANTIAL GROOVES INTO THE TILLER HOUSING P/N 73250021103 CAUSING THE CENTERING ACTION OF THE SPRING TO BE LESS EFFECTIVE. THE HOUSING WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001073000107 20010730 00107 NM 2001 7 30 UPS01436120 1 20010606 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C M/D BS 380 STR 24R FRAME WEB FOUND CRACKED. M/D BS 380 STR 24R FRAME WEB REPAIRED AS PER RS R53-12-34 662. 2 L 7 4 4F A20WE 2001073000108 20010730 00108 NM 2001 7 30 CA010621015 1 20010608 A 3230 DSC252B4012 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE DRAG STRUT ACT LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) INVESTIGATING OF HYDRAULIC LEAK IN THE NLG BAY RESULTED IN REPLACEMENT OF ONE OF THE DRAG STRUT ACTUATOR FLEX LINE S. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001073000109 20010730 00109 NM 2001 7 30 UPS01436124 1 20010530 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C CRACK REVEALED AT LT NR 1 MED CUTOUT FRAME AT BS 434 FRAME WEB AREA AT NR 5 FASTENER HOLE BY APPROX .5 INCH LONG IAW ATTACH FIGURE. LT NR 1 MED CUTOUT FWD FRAME BS 434 WEB REPAIRED AS PER EO B747-5310-12889-A APPROX F. 2 L 7 4 4F A20WE 2001073000111 20010730 00111 NM 2001 7 30 UPS01436136 1 20010531 A 5312 BULKHEAD BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C, NOSE W/W BS 400 BHD PRESSURE PAN FOUND 2 CRACKS BY APPROX 1 X .5 INCH LONG AS MARKED. NOSE W/W BS 40 0 BULKHEAD PRESSURE PAN REPLACED AS PER DWG 624U0005 SHEET 7. 2 L 7 4 4F A20WE 2001073000112 20010730 00112 NM 2001 7 30 UPS01436137 1 20010531 A 5210 STOP FITTING BOEING 747 747123 1384873 NM L1 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C M/D - L1 DOOR FWD LOWER STOP FITTING CRACK. STOP FITTING REPLACED AS PER SRM 51-10-01 PAGE 8. DOOR R IG AND OPERATION CHECK C/OUT SATISFACTORY. 2 L 7 4 4F A20WE 2001073000113 20010730 00113 NM 2001 7 30 UPS01436140 1 20010604 A 5320 SPLICE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C M/D - BS 1960 S12R STRINGER SPLICE FOUND CRACKED. STRINGER SPLICE REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2001073000114 20010730 00114 NM 2001 7 30 UPS01436141 1 20010604 A 5313 STRINGER BOEING 747 747132 1384882 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C M/D - BS 1990 RT STR 13 STRINGER CRACKED. HFEC INSPECTION C/OUT AS PER NTM PART 6 51-00-00 FIG 4 NIL CRACK FOUND. 2 L 7 4 4F A20WE 2001073000115 20010730 00115 NM 2001 7 30 UPS01436142 1 20010604 A 5310 SHEAR TIE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C M/D - BS 1880 RT BETWEEN STR 13 - 14 FOUND SHEAR TIE CRACK. M/D BS 1880 STR 13R - 14R SHEAR TIE REPLA CED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001073000116 20010730 00116 NM 2001 7 30 UPS01436143 1 20010615 A 5347 CARGO TRACK BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C, FWD CARGO COMPT TIE DOWN TRACK FOUND CRACKED AT LBL 25 BS 560 - 570 AREA AS MARKED. TIE DOWN TRACK R EPAIRED AS PER SRM 53-10-05 FIG 5. 2 L 7 4 4F A20WE 2001073000117 20010730 00117 CE 2001 7 30 CA010621017 1 20010606 A 2822 SWITCH BEECH 18 TC45G 1151016 CE PWA R985 R985AN14B 52008 NE HARTZL HCB3R HCB3R302 GL BOOST PUMP FAILED W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN) THE SWITCH IS USED TO OPERATE THE PRIME SOLONOID AND BOOST PUMP FOR LEFT TO RIGHT ENGINE. THE SWITCH CASE BURNT TH ROUGH BY THE CENTRE CONTACT, WHICH HAS POWER ALL THE TIME. THE PILOT COULD SMELL BURING AND SEE SMOKE. THE SWITCH WAS NO T IN USE AT THE TIME AS ITS ONLY USED ON STARTUP. 1 L 7 2 3R 3 R A765 5E1 5 C P28EA 2001073000118 20010730 00118 NM 2001 7 30 UPS01436144 1 20010607 A 5712 RIB BOEING 747 747123 1384873 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C RHW NR 3 FUEL TANK WS 557.42 WING INTERSPAR RIB WEB CRACK. REPAIR C/OUT AS PER SRM 57-10-05. 2 L 7 4 4F A20WE 2001073000121 20010730 00121 NM 2001 7 30 UPS01436145 1 20010608 A 5210 SKIN BOEING 747 747123 1384873 NM L1 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C M/D - L1 DR EXTERIOR SURFACE FOUND CRACKED AT APPROX BS 460 WL 220. SKIN REPAIRED AS PER SRM 52-10-02 FIG 9. 2 L 7 4 4F A20WE 2001073000124 20010730 00124 NM 2001 7 30 UPS01436165 1 20010624 A 3350 69B460601 PLATE BOEING 747 747123 1384873 NM COCKPIT FAULTY A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:N/A EMERGENCY LIGHT PNL SWITCH DOES NOT AGREE WITH PANEL POSITION INDICATION. REMOVED AND REPLACED LIGH T PLATE AS PER EO B747-3350-14819, SWITCH AND LIGHT PLATE AGREE. 2 L 7 4 4F A20WE 2001073000126 20010730 00126 NM 2001 7 30 UPS01436167 1 20010624 A 3350 LIGHT BOEING 747 747121 1384871 NM COCKPIT INTERMITTENT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT OVER COCKPIT IS INTERMITTENT. REPLACED LIGHT ASSY, OPS CHECK NORMAL. 2 L 7 4 4F A20WE 2001073000128 20010730 00128 NM 2001 7 30 UPS01436168 1 20010622 A 5220 HANDLE BOEING 747 747212B 1384886 NM EMERGENCY DOOR MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:N/A UPPER DECK EMERGENCY ESCAPE DOOR HANDLE INTERMITTENTLY DOES NOT STOW ONCE OPENED, THIS DOES NOT LET THE DOOR OPEN NORMALLY. THE EXTERIOR HANDLE JAMS INTO DOOR SILL. OPS CHECKED DOOR PER MM 52-130 PG 9, CHECKS GOOD. 2 L 7 4 4F A20WE 2001073000130 20010730 00130 NM 2001 7 30 UPS01436192 1 20010627 A 3350 69B4601024 MODULE BOEING 747 747123 1384873 NM CABIN DEFECTIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS COME ON WITH SWITCH IS OFF-POSITION. REPLACED EMERGENCY LIGHT MODULE AS PER M M 33-51-09. TEST OK AS PER MM 33-51-00. OK TO CONTINUE P/N ON, OFF 69B46010-24, S/N ON 001415 OFF-00 329. 2 L 7 4 4F A20WE 2001073000131 20010730 00131 EA 2001 7 30 CA010621035 1 20010525 A 2910 LINE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE NR MLG WW LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) MAINTENANCE INVESTIGATION OF A HYDRAULIC FLUID LEAK IN THE NR 1 MLG BAY RESULTED IN THE REPLACEMENT OF THE DOOR OP EN LINE TO THE SEQUENCE VALVE. THE LINE WAS LEAKING FROM A PINHOLE AT A FACTORY BEND. TTAF 23453, TCAF 34772. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001073000132 20010730 00132 NM 2001 7 30 UPS01436214 1 20010628 A 3350 BATTERY PACK BOEING 747 747SR46 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:N/A 2 EMERGENCY EXIT DOOR SLIDE LIGHTS INOP. REMOVED AND REPLACED CREW DOOR BATTERY PACK IAW B747 MM 33 -51-04, OPS CHECKS GOOD. 2 L 7 4 4F A20WE 2001073000133 20010730 00133 NE 2001 7 30 CA010621036 3 20010306 A 6114 STOP 22D30403 DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985AN14B 52008 NE HAMSTD 22D 22D30 NE PROP PITCH SHEARED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 91 167681 (CAN) ON APPROACH THE ENGINE RPM INCREASED RAPIDLY AND THE AIRCRAFT SUDDENLY LOST ALTITUDE. THE PILOT WAS ABLE TO MAINTA IN CONTROL BY OPERATING THE ENGINE IN THE UPPER LIMIT OF THE RPM RANGE. THE AIRCRAFT WAS SUCCESSFULLY LANDED ATTHE RAPID DES JOACHIMS WATER BASE. (CYDJ). INVESTIGATION REVEALED THE BLADES AT A REST POSITION ESTIMATED AT CLOSE TO ZERO DEGREE S. THE DOME WAS REMOVES AND BOTH STOP DOWEL WERE FOUND TO BE SHEARED. THE COMPANY WILL ENLIST THE NTSB LAB FOR ASSISTANC E.CORROSION INITIATED FATIGUE FRACTURE. 1 H 7 1 3R 3 R A806 5E1 5 C P736 2001073000134 20010730 00134 NM 2001 7 30 CA010621037 1 20010529 A 8011 AJA4N176 CONTACTOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE STARTER FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WHEN MAINTENANCEAPPLIED GROUND POWER TO THE AIRCRAFT, THE # 1 ENGINE STARTER ENGAGED POWER WAS REMOVED FROM THE AI RCRAFT AND THE STARTER CONTACTOR FOR # 1 ENGINE WAS REPLACED, ALONG WITH THE STARTER-GENERATOR. TIME IN SERVICE FOR THE STARTER CONTACTOR COULD NOT BE DETERMINED AS THESE COMPONENTS ARE NOT TRACKED. WC 1758. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001073000135 20010730 00135 EA 2001 7 30 CA010621038 1 20010525 A 2150 ACM DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE ACM BAY CONTAMINATED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 11894 1998 (CAN) DURING SCHEDULED REPLACEMENT OF THE FORWARD ECS HEAT EXCHANGER AND CONDENSER/MIXER, THE FORWARD AIR CYCLE MACHINE WAS FOUND TO BE CONTAMINATED WITH OIL. THE ACM WAS REPLACED. THIS UNIT HAD ONLY BEEN IN SERVICE FOR 1998 HOURS SINCE OVE RHAUL AND MODIFICATION BY HAMILTION SUNSTRAND. WC 160 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001073000136 20010730 00136 2001 7 30 CA010621039 4 20010604 A 3418 90610004 COMPUTER DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE STALL WARNING FAILED W O OTHER J WARNING INDICATION NR NOT REPORTED 1 CA (CAN) THE FLIGHT CREW REPORTED NR 2 STALL WARNING /STICK PUSH CAUTION LIGHT ILLUMINATED DURING FLIGHT. THE STALL WARING COMPUTER WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. THESTALL WARNING COMPUTER HAD BEEN REPAIRED 194 HOURS P REVIOUS TO THIS OCCURRENCE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001073000137 20010730 00137 NE 2001 7 30 UPS01436215 2 20010630 A 7200 ENGINE BOEING 747 747123F NM PWA JT9 JT9D7A 52054 NE NR 3 MALFUNCTIONED A IPXA E ENGINE SHUTDOWN J M WARNING INDICATION OVER TEMP DE DESCENT 1 SO 01 677UP 20391 685681 INSPECTION TYPE:N/A THRUST LEVERS CLOSED INSIDE BRUCK 1200 AGL. NR 3 ENG OIL PRESS LIGHT ON, EGT 952 GEN LIGHT ON AIRSP EED 165 KTS. FF 0 N2 & N1 LOW (NEAR 0). INSPECTED 3.5 BLEED VLVS FOR FOD, FUEL PUMP FP12 PRESSURE CHECKED AND REPLACED FUEL PUMP FILTER PER MM 73-11-02. REPLACED FUEL CONTROL MAIN FILTER PER MM 73-21-02. CHECKED FUEL CONDITION ACTUATOR PER MM 71-00-42. OPERATED ENGINE AT IDLE AND T/O PWR PER MM 71-00-00. NO FAULTS FOUND. BORESCOPED ENG PER 72-00-00. WINDMILL INSP PER 72-00-00, NO FAULT 2 L 7 4 4F 4 F A20WE E20EA 2001073000138 20010730 00138 NM 2001 7 30 UPS01436219 1 20010626 A 5320 SUPPORT BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C FX - BODY FAIRING SUPPORT FRAME STA 880 LBL 50 - RBL 50 FOUND CORROSION. FX - BODY FAIRING SUPPORT RE PAIR AT BS 880 FROM LBL 50 - RBL 50. 2 L 7 4 4F A20WE 2001073000139 20010730 00139 NM 2001 7 30 UPS01436220 1 20010626 A 5320 SUPPORT BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C FX - BODY FAIRING SUPPORT FRAME STA 840 LBL 50 - RBL 50 FOUND CORROSION. FX - BODY FAIRING SUPPORT RE PAIR AT BS 840 FROM RBL 9 - RBL 25. 2 L 7 4 4F A20WE 2001073000140 20010730 00140 EU 2001 7 30 CA010621041 1 20010511 A 2750 676101005 CONTROL UNIT BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE TE FLAPS LEAKING W O OTHER K FLUID LOSS NR NOT REPORTED 1 CA (CAN) INVESTIGATION INTO A HYDRAULIC LEAK RESULTED IN REPLACEMENT OF THE FLAP POWER UNIT WHICH WAS FOUND TO BE LEAKING F ROM AN OUTPUT SHAFT CAVITY DRAIN. THIS POWER UNIT WAS AN EXCHANGE UNIT AND HAD BEEN INSTALLED FOR 498 HOURS. 17719 2 H 7 4 4F 4 F RT A49EU E6NE 2001073000141 20010730 00141 NM 2001 7 30 UPS01436221 1 20010626 A 5320 SUPPORT BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C FX - BODY FAIRING SUPPORT FRAME STA 960 LBL 110 - RBL 60 FOUND CORROSION. BS 960 BODY FAIRING SUPPORT FROM RBL 19 - RBL 21 REPAIR. 2 L 7 4 4F A20WE 2001073000142 20010730 00142 NM 2001 7 30 CA010622001 1 20010518 A 2435 23088002A STARTER GEN DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 2 FAILED W O OTHER J WARNING INDICATION NR NOT REPORTED 1 CA 8911 24 (CAN) THE FLIGHT CREW REPRTED THAT NR 2 D.C GENERATOR CAUTION LIGHT ILLUMINATED DURING FLIGHT. MAINTENANCE REPLAED THE S TARTER-GENERATOR AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001073000143 20010730 00143 NM 2001 7 30 UPS01436222 1 20010625 A 5311 FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C M/D - BS 220, S14CR - S14DR FRAME FOUND CRACKED. REPAIRED FRAME PER SRM 53-10-04 FIG 4. 2 L 7 4 4F A20WE 2001073000144 20010730 00144 NM 2001 7 30 UPS01436223 1 20010626 A 5311 FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C, RT BS 300 FRAME BETWEEN STR 39R AND 40R FOUND 2 FASTENER HOLE CRACKED AT FRAME WEB. PLS REFER ATTACH ED SKETCH. RT BS 300 STR 39R TO 40R AREA FRAME WEB REPAIRED AS PER SRM 51-40-03. 2 L 7 4 4F A20WE 2001073000145 20010730 00145 NM 2001 7 30 UPS01436224 1 20010626 A 5312 BULKHEAD BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C, RT BS 320 NOSE WHEEL WELL VERTICAL BEAM WEB FOUND CRACK AT NR 3 INSULATION BLANKET STAND - OFF HOLE ( COUNT FROM TOP) APPROX .1875 INCH RUNNING UPWARD AS MARKED. RT BS 320 NOSE WHEEL WELL VERTICAL BEAM WEB REPLACED AS PER SRM 51-10 -01. 2 L 7 4 4F A20WE 2001073000146 20010730 00146 NM 2001 7 30 UPS01436225 1 20010626 A 5312 BULKHEAD BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C RT BS 300 NOSE WHEEL WELL VERTICAL BEAM WEB FOUND CRACK AT NR 3 INSULATION BLANKET STAND - OFF HOLE (C OUNT FROM TOP) APPROX .25 INCH AND .375 INCH RUNNING UPWARD AND DOWNWARD RESPECTIVELY. VERTICAL BEAM WEB REPLACED AS PE R SRM 51-10-01 AT RT BS 300 NOSE WHEEL WELL AREA. 2 L 7 4 4F A20WE 2001073000149 20010730 00149 EA 2001 7 30 CA010622005 1 20010523 A 5320 H100211K1829 PIN DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE BULKHEAD DETERIORATED W K NONE O OTHER IN INSP/MAINT 1 CA 22550 (CAN) FLIGHT CREW REPORTED THE ROLL CONTROL WAS STIFF ON THE GROUND AND IN THE AIR. MAINTENANCE INVESTIGATION REVEALED T HAT THE LT AFT CARGO BULKHEAD RETENTION PIN WAS NOT IN THE LOCATING RECEPTACLE ON THE FUSELAGE FRAME. THIS ALLOWED THE P ANEL AND ATTACHED PULLEY COVER TO FLEX AFT, CONTACTING THE PULLEYS CARRYING THE ROLL SPOILER ACTUATING CABLES,CAUSING DR AG ON SYSTEM. FURTHER INVESTIGATION OF THE PANEL ASSY REVELED THAT THE CENTRE AND UPPER HINGES THAT ATTACH THE TWO BULKH EAD PANELS TOGETHER WERE DETERIORATED TO THE POINT THAT THEY ALLOWED THE PANEL TO FLEX AFT WHEN A LOAD WAS PLACED AGAINS T THEM AND DISENGAGE THE LOCATING PIN. THE PIN SECTIONS WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001073000150 20010730 00150 CE 2001 7 30 CA010622006 1 20010525 A 2731 NAS30266517 CONTROL CABLE BEECH 90 C90 1152913 CE PWA PT6 PT6A21 52043 EA HARTZL HCB3T HCB3TN3 GL TRIM SERVO FAILED W A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 CA 7604 (CAN) ELEVATOR TRIM WOULD NOT FUNCTION AT TOP CLIMB. ELECTRIC TRIM MOTOR APPEARED TO FUNCTION NORMALLY BUT NO TRIM CONTR OL MOVEMENT AVAILABLE. MANUAL TRIM DID NOT ACTUATE CONTROL SERVICE. MANUAL TRIM WHEEL WOULD ONLY FREE WHEEL, NO TRIM CON TROL AVAILABLE. AIRCRAFT RETURNED TO DEPARTURE AIRPORT. AOG TEAM SENT TO REPAIR AIRCRAFT. TRIM CABLE FOUND TO HAVE FAILE D. ONE SIXTEENTH CABLE FRAYED AND BROKEN IN AREA OF TRIM SEREVO TRAVEL. CABLE REPLACED AND ELECTRIC TRIM SERVO REPLACED. BOTH PARTS SENT FOR NSPECTION. FLEET AIRCRAFT ALL INSPECTED (LIMITED TO KING AIR C90 WITH " CENTURY FOUR" AUTO PILOT SY STEM)CABLE DATA- ORGINAL MANUFACTURER UNKNOWN-11393 CYCLES-7603.6 HRS 1 L 7 2 3T 4 T 3A20 E4EA 6 C P15EA 2001073000151 20010730 00151 NM 2001 7 30 UPS01436226 1 20010626 A 5312 141U11073 BULKHEAD BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C, LT BS 320 NOSE WHEEL WELL VERTICAL BEAM WEB FOUND CRACK AT NR 3 INSULATION BLANKET STAND - OFF HOLE ( COUNT FROM TOP) APPROX .3125 INCH RUNNING UPWARD. VERTICAL BEAM WEB REPAIRED AND REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001073000152 20010730 00152 NM 2001 7 30 UPS01436227 1 20010626 A 5312 141U11073 BULKHEAD BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C LT BS 320 NOSE WHEEL WELL VERTICAL BEAM WEB FOUND 1 FASTENER HOLE COMMON TO THE FRAME CRACKED, PLS REF ER THE ATTACH SKETCH. VERTICAL BEAM WEB REPLACED AS PER SRM 51-10-01 & REFER NRC 5251 FOR DETAIL. 2 L 7 4 4F A20WE 2001073000153 20010730 00153 NM 2001 7 30 UPS01436228 1 20010626 A 5312 141U11075 BULKHEAD BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C, LT BS 300 NOSE WHEEL WELL VERTICAL BEAM WEB FOUND CRACK AT NR 3 INSULATION BLANKET STAND-OFF HOLE (CO UNT FROM TOP) APPROX .375 INCH AND .5 INCH RUNNING UPWARD AND DOWNWARD RESPECTIVELY. LT BS 300 NOSE WHEEL WELL VERTICAL WEB REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001073000154 20010730 00154 NM 2001 7 30 UPS01436229 1 20010626 A 5311 FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C, RT BS 320 FRAME BETWEEN STR 39R AND 41R FOUND 4 FASTENER HOLE CRACKED AT FRAME WEB AND FRAME INNER CH ORD, PLS REFER ATTACHED SKETCH. RT BS 320 FRAME REPAIRED AT STR 39R - 41R AS PER SRM 51-40-03 AND FRAME INNER CHORD REP LACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001073000155 20010730 00155 NM 2001 7 30 CA010622013 1 20010522 A 2131 CONTROLLER BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE CABIN PRESSURE MALFUNCTIONED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 18608 14907 (CAN) AFTER TAKEOFF AIRCRAFT WOULD NOT PRESSURIZE IN STANDBY MODE. FLIGHT RETURNED.CABIN PRESSURZATION CONTROLLER REPLAC ED. 2 L 7 2 4F 4 F A16WE E2EA 2001073000156 20010730 00156 NM 2001 7 30 UPS01436231 1 20010628 A 5330 SKIN BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C EMP - TAIL COMPT SKIN CRACKED AT FASTENER HOLE, BS 2658 BETWEEN STR 11R AND STR 12R. CRACKED EXTERNA L SKIN AT BS 2658 BETWEEN STR R11 & R12 AREA REPAIRED AS PER SRM 53-30-03 FIG 1A. 2 L 7 4 4F A20WE 2001073000157 20010730 00157 NM 2001 7 30 UPS01436232 1 20010628 A 5330 SKIN BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C EMP - TAIL COMPT LT SKIN CRACKED AT FASTENER HOLE, BS 2658 BETWEEN STR 11L AND STR 12L. CRACKED EXTER NAL SKIN AT BS 2658 BETWEEN STR L11 & L12 AREA REPAIRED AS PER SRM 53-30-03 FIG 1A. 2 L 7 4 4F A20WE 2001073000158 20010730 00158 NM 2001 7 30 UPS01436233 1 20010625 A 5320 70750050IN WEB BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C M/D - BS 500 S-16L WEB FOUND CRACKED. REPLACED BRACKET AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001073000159 20010730 00159 NM 2001 7 30 CA010622014 1 20010515 A 3040 0802071001 CONTROLLER DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE DEICE SYSTEM FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS HO HOVERING 1 CA 4383 (CAN) THE FLIGHT CREW REPORTED THAT THEY SMELLED SMOKE IN THE COCKPIT. APPROXIMATELY 2 MINUTES IN TO THEIR INVESTIGATION , SMOKE WAS SEEN COMING FROM THE F/Q'S WINDSHIELD TERMIALS. THE W/S HEAT WAS TURNED OFF AND THE WINDSCREEN INNER PLY SUB SEQUENTLY SHATTERED. THE WIDSCREEN AND THE W/S HEAT CONTROLLER WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. W INDSCREEN: P/N NP157901-12, S/N 97045H8632, H AD ACCUMULATED 11691 CYCLES AND 8740 HOURS SINCE NEW. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001073000160 20010730 00160 NM 2001 7 30 UPS01436234 1 20010625 A 5311 FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C M/D - BS 400 S-14R FRAME FLANGE FOUND CRACKED. INSTALLED REINFORCED DOUBLER PER SRM 51-30-02. 2 L 7 4 4F A20WE 2001073000161 20010730 00161 NM 2001 7 30 CA010622015 1 20010515 A 3310 BA80061 BALLAST DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE CABIN FAILED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) MAINTENANCE INVESTIGATION OF A "BURNT" SMELL IN THE CABIN DURING MAINTENANCE REVEALED AN OVERHEATED BALLAST FOR TH E CABIN OVERHEAD FLUORESCENT LIGHTS. THE BALLAST AND LIGHTS ASSEMBLIES WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVIC E. TTAF 24743, TCAF 33783 CYCLES 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001073000162 20010730 00162 NM 2001 7 30 UPS01436235 1 20010625 A 5320 WEB BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C M/D - BS 380-400, S-14R WEB FOUND CRACKED. REPAIRED SUPPORT WEB PER SRM 51-40-03 FIG 1. 2 L 7 4 4F A20WE 2001073000163 20010730 00163 NM 2001 7 30 UPS01436236 1 20010626 A 5311 FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C, RT BS 320 FRAME AT SKIN ATTACH FLANGE BETWEEN STR 39R AND 40R FOUND CRACKED APPROX .25 INCH AS MARKED . RT BS 320 FRAME ATT SHEAR TIE BETWEEN S39R - S40R REPAIRED AS PER SRM 51-40-03. 2 L 7 4 4F A20WE 2001073000164 20010730 00164 NM 2001 7 30 UPS01436237 1 20010704 A 3350 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:N/A CREW SERVICE DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED CREW SERVICE DOOR LIGHT ASSY IAW B747 MM 33-51-07, OPS CHECKS GOOD. 2 L 7 4 4F A20WE 2001073000165 20010730 00165 NM 2001 7 30 UPS01436245 1 20010627 A 5311 FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C U/D - BS 360 LT STR 4 & 3A FRAME CRACKED. REPAIRED FRAME AS PER SRM 53-10-04 FIG 18. 2 L 7 4 4F A20WE 2001073000166 20010730 00166 NM 2001 7 30 UPS01436246 1 20010626 A 5311 FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C U/D - BS 480 S-10AR FRAME FOUND CRACKED. REPAIRED FRAME AS PER SRM 53-10-04 FIG 11. 2 L 7 4 4F A20WE 2001073000167 20010730 00167 NM 2001 7 30 UPS01436247 1 20010626 A 5311 FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C U/D - BS 500 S-10AR TO S-11R FRAME FOUND CRACKED. REPAIRED FRAME AS PER SRM 53-10-04 FIG 11. 2 L 7 4 4F A20WE 2001073000168 20010730 00168 NM 2001 7 30 UPS01436248 1 20010626 A 5311 FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C U/D - BS 460 S-11L TO S-12L FRAME FOUND CRACKED. REPAIRED FRAME AS PER SRM 53-10-04 FIG 11. 2 L 7 4 4F A20WE 2001073000169 20010730 00169 NM 2001 7 30 UPS01436249 1 20010626 A 5311 FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C U/D - BS 480 S-11L TO S-12L FRAME FOUND CRACKED. REPAIRED FRAME PER SRM 53-10-04 FIG 11. 2 L 7 4 4F A20WE 2001073000170 20010730 00170 NM 2001 7 30 UPS01436250 1 20010626 A 5311 FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C U/D - BS 460 S-11R FRAME FOUND CRACKED. REPAIRED FRAME PER SRM 53-10-04 FIG 11. 2 L 7 4 4F A20WE 2001073000171 20010730 00171 NM 2001 7 30 UPS01436251 1 20010626 A 5720 TEE CHORD BOEING 747 747212B 1384886 NM LT WING BULGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C LHW - UPPER SURFACE L/E FIXED PANEL BUTT JOINT AREA FOUND BULGE AT ILES 997 AFT OF NR 7 V.C. FLAP AS M ARKED. L/E FIXED PANEL SUPPORT T-CHORD REPLACED AND RIB REINSTALLED AS PER SRM 51-30-02, 51-10-01 L/E PNEUMATIC DUCT TR USS ROD AND TORQUE SHAFT REMOVED AND RECONNECTED AS PER MM 36-11-00, 20-51-01, 27-81-05. 2 L 7 4 4F A20WE 2001073000172 20010730 00172 NM 2001 7 30 UPS01436269 1 20010707 A 3350 BATTERY PACK BOEING 747 747121 1384871 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:N/A EMERGENCY BATTERY PACK IS DEAD. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-51-04. 2 L 7 4 4F A20WE 2001073000173 20010730 00173 NM 2001 7 30 UPS01436270 1 20010709 A 3350 BATTERY PACK BOEING 747 747123F NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:N/A FOUND EXIT LIGHT INOP AT UPPER DECK CREW SERVICE DOOR CEILING. REMOVED AND REPLACED BATTERY PACK AS SY RT-SIDE EXIT LIGHT, OPS TEST OK. PER MM 33-51- 00, P/N OFF/ON 9008-3-5A, S/N OFF 5941, SN ON 75833. 2 L 7 4 4F A20WE 2001073000174 20010730 00174 NM 2001 7 30 UPS01436271 1 20010627 A 5521 SPAR BOEING 747 747212B 1384886 NM ELEVATOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C EMP - RT OUT/B ELEVATOR INTERIOR FRONT SPAR UPPER CHORD FOUND SURFACE CORROSION AT ELEV STA 310 TO STA 390 AS MARK. THE RT O/B ELEVATOR FRONT SPAR UPPER CHORD BETWEEN ELEV STA 310 AND 390 AREA CORROSION CLEANED UP. BLEND OUT AREA OUT OF ALLOWABLE LIMIT AS PER SRM 55-20-01 FIG 1.4. REPAIR WAS CARRIED OUT IAW SRM 51- 40-04. ELEVATOR BALAN CE ALSO C/OUT AS PER SRM 51-80-02 AFTER REPAIR. 2 L 7 4 4F A20WE 2001073000175 20010730 00175 NM 2001 7 30 UPS01436272 1 20010625 A 5311 FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C M/D - BS 400, S-15L TO S-16L FRAME FOUND CRACKED. REPAIRED FRAME PER HXRS R53-12-34671, BETWEEN S-15L TO S-16L BS 400 LT. 2 L 7 4 4F A20WE 2001073000176 20010730 00176 NM 2001 7 30 UPS01436273 1 20010625 A 5320 FITTING BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C CRACK REVEALED ON LT BS 1241 BULKHEAD CANTED PRESSURE DECK FITTING AT THE AFT HOLE AREA BY APPROX 0.08 0 INCH LONG RUNNING FWD DOWN DIRECTION AS PER ATTACH SKETCH. LH BS 1241 BULKHEAD CANTED PRESSURE DECK FITTING AFT BOLT HOLE CRACKED AREA REWORKED AS PER HAECO REPAIR SCHEME R-53-41-34669 WORK DETAIL REFER ATT CWS. 2 L 7 4 4F A20WE 2001073000178 20010730 00178 NM 2001 7 30 UPS01436274 1 20010626 A 5311 FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C LT SIDE BS 1241 BULKHEAD FORWARD HOLE FOUND CRACKED AT BULKHEAD FRAME FORGING O/B EDGE APPROX 0.040 IN CH RUNNING UP. PLS REFER TO ATTACH SKETCH FOR DETAILS. LT SIDE BS 1241 BULKHEAD FRAME FORGING FWD HOLE REWORKED AS PER EO B747-5310-0323-L APPENDIX H AND HAECO REPAIR SCHEME R-53-41-346 69. 2 L 7 4 4F A20WE 2001073000180 20010730 00180 NM 2001 7 30 UPS01436278 1 20010626 A 5210 ANGLE BOEING 747 747212B 1384886 NM L5 DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C M/D - L5 DOOR BS 2238 BETWEEN 1 X 2 FRAME WL 230 NR 4 WEB (COUNT FROM LOWER) ATT INTERIOR ANGLE HEAVY CORROSION. REPLACED L5 DOOR INNER ANGLE PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001073000182 20010730 00182 NM 2001 7 30 UPS01436279 1 20010709 A 3350 69B4601036 COVER BOEING 747 747123F NM CABIN BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:N/A, EMERGENCY LIGHT SWITCH COVER BROKEN. REMOVED AND REPLACED EMERGENCY LIGHTS MODULE AND OPS CHECK OK PER MM 33-51-09. 2 L 7 4 4F A20WE 2001073000186 20010730 00186 NM 2001 7 30 UPS01436296 1 20010712 A 5330 SKIN BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C FX - NLG AFT CUTOUT SKIN FOUND CRACKED AT SCREW HOLE AREA LT BS 400 S45L LBL 24 AREA. NLG W/W AFT CUT OUT LT BS 400 S45L LBL 24 SKIN CRACKED AREA REPAIRED AS PER EO B747-5330-3520-E WORK DETAIL REFER ATTACH CWS. 2 L 7 4 4F A20WE 2001073000187 20010730 00187 CE 2001 7 30 CA010622027 1 20010603 A 5347 50150191 CHANNEL CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO MCAULY 3AF32C 3AF32C505 GL SEAT SUPPORT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) SEAT PEDESTAL LOOSE-INVESTIGATION SHOWED LOWER CHANNEL CRACKED AND SEVERAL SCREWS BROKEN & MISSING SUCH THAT PEDES TAL COULD MOVE ON FLOOR STRUCTURE. 1 L 7 2 3O 3 O A7CE E8CE 5 C P22EA 2001073000189 20010730 00189 NM 2001 7 30 UPS01436395 1 20010725 A 2710 AILERON BOEING 747 747121 1384871 NM WINGS MALFUNCTIONED A IPXA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 SO 01 691UP 19641 INSPECTION TYPE:N/A PRE-FLT- AILERONS BND WHEN YOKE IS TURNED LEFT. BINDING OCCURS APPR E LEFT LIMIT FURTHER DEFLECTION OF THE LEFT SPOILER IS IND ON THE CP I WHEN AILERONS ARE FORCED PAST THE BINDING POINT. *S/D* PERFORMED AILERON CONTROL SYSTEM TROUBLESHOOTING STEPS 1-3 WITH NO DEFECTS OR BINDING NOTED. AILERON CONTROL SYSTEM OPS CHKS GOOD AS PER MM 27-1 1-00 OK FOR SERVICE 2 L 7 4 4F A20WE 2001073000190 20010730 00190 NM 2001 7 30 UPS01536024 1 20010606 A 2910 1154K0232 HYDRAULIC LINE BOEING 757 75724APF 1384969 NM HYD SYSTEM LEAKING A IPXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SO 01 406UP 23728 INSPECTION TYPE:N/A PIREP-LEFT HYD QUANTITY DECREASED TO ZERO AND SYSTEM PRESSURE LIGHT ILLUMINATED (SHUT OFF ENG AND EL ECTRICAL PUMPS WHEN PRESSURE LIGHTS ED). FOUND RT MLG DOWNLOCK ACTUATOR FLEX LINE WORN (LEAKING). REMOVED AND REPLACED LINE P/N -115-04K0232, HYDRAULIC SYS REPLENISHMENT PER MM 29-18 LT ENG DRIVEN HYD PUMP INSPECTED PER MM 29-11-05, NO CO NTAMINATION NOTED SYSTEM TESTED SERVICEABLE. 2 L 7 2 4F RT A2NM 2001073000191 20010730 00191 NM 2001 7 30 UPS01536139 1 20010608 A 5347 BAC15202472 SEAT TRACK BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 402UP 23724 INSPECTION TYPE:C CORROSION ON SEAT TRACK FROM BS 1075 - 1120, LBL 46 WL 208 IN THE MAIN CARGO COMPARTMENT. REMOVED AND REPLACED SEAT TRACK FROM BS 1075 - 1120 LBL 46, WL 208 PER SRM 51-40-02, SRM 51-40-02, SRM 51-40-08 PG 1-17 MM 51-21-01 . 2 L 7 2 4F RT A2NM 2001073000193 20010730 00193 NM 2001 7 30 UPS01536155 1 20010609 A 5347 SEAT TRACK BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 402UP 23724 INSPECTION TYPE:C, CORROSION (CP53-131-01.00-01) ON SEAT TRACK AROUND NUT PLATE HOLES FROM BS 1040 - 1050, LBL 1 TO RBL 1, WL 208 IN MAIN CARGO COMPARTMENT. FOUND LONGITUDINAL BEAM OUT OF LIMITS AT 1045, LBL 1. REPLACED LONGITUDINAL BEAM FROM BS 900 - 1060 WORK DONE IAW SRM 51-10-02, 53-00-51, 53-40-02, 51-40-05. 2 L 7 2 4F RT A2NM 2001073000194 20010730 00194 NM 2001 7 30 UPS01536394 1 20010725 A 2121 COOLING FAN BOEING 757 75724APF 1384969 NM COCKPIT FAILED A IPXA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 SO 01 423UP 25325 INSPECTION TYPE:N/A DIVERSION-SMOKE IN FLT DECK. NOTED NOISE AT FO INST PANEL WX RADAR DISPLAYED ON EFIS AS INOP, RADAR TURNED OFF EQUIP OVERHT DISPLAYED, I NST SW DISPLAYED, CAPTS AND FO ADI BLANK SELECTED ALTN EFI-NO HELP, COMPLETED EQUIP OVERFT ****SUPPLEMENTAL MRR*** PER 21-58-23-4 R&R F/D SUPPLY FAN NR1 PER 21-58-06-4 R&R FWD EQUIP SUPPLY FAN NR2 AN D RELAY K344, PER MM 21-58-06-4 & 21-58-23-4 SYSTEM TEST NORMAL. PN OFF/ON 731378 SN ON 2857 SN OFF 1929 POS F/D FAN PN ON/OFF 731376 S/N ON 2175 SN OFF 0931 POS FWD EQUIP ON OFF 9123-8072 SN ON SN ON TAG 0557457 OFF 055757A WX RADAR TEST NORMAL 2 L 7 2 4F RT A2NM 2001073000197 20010730 00197 NM 2001 7 30 UPS01636194 1 20010627 A 2761 1542600 CAP BOEING 767 76734AF 1385212 NM SPOILER ACTUATOR LOOSE A IPXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 320UP 27747 INSPECTION TYPE:N/A INBOUND LOG WRITE UP: CENTER HYDRAULIC QUANTITY DECREASED TO .31. SYSTEM DEPRESSURIZED AND LEAK C ONTINUED. SPOILER ACTUATOR PANEL NR 9, FOUND SAFETY WIRE ON CAP, PT 1542661 IPC REF 27-61-02-01 WAS BROKEN AND CAP WAS LOOSE. REMOVED AND REPLACED O-RING P/N NAS1602-910 & SECURED FILTER CAP. 2 L 7 2 4F RT A1NM 2001073000205 20010730 00205 NM 2001 7 30 UPS01636401 1 20010724 A 3010 278053704 ANTI-ICE VALVE BOEING 767 76734AF 1385212 NM RT WING INOPERATIVE A IPXA K NONE J WARNING INDICATION TO TAKEOFF 1 SO 01 316UP 27744 INSPECTION TYPE:ETOP PILOT REPORT-ICE SW SELECTED FROM ON TO OFF EICAS MSG REMAINED ILLUMINATED . LIGHT AND MSG OCCURRED ON T/O ROLL LIGHT AND MESSAGE NOT DISPLAYED WITH SWITCH IN THE ON POSITION REF LOG PAGE 698091. *S/D* R/R WING TAI CON T RELAY K414. R/R RH WING TAI VALVE AS PER M/M 30-11 -02 OPS CHK AND LEAK CHECK NML. PER MM 30-11-02 VALVE PN ON AND OFF 278053704 SN OFF 3404FP 2 L 7 2 4F RT A1NM 2001073000207 20010730 00207 NM 2001 7 30 CA010625003 1 20010610 A 5330 SKIN BOEING 737 737201 1384454 NM PWA JT8 JT8D9A 52048 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 58358 (CAN) CRACK IN FUSELAGE SKIN LEFT SIDE, 8 INCHES AFT. OF STATION 750 AT STRINGER 17L.REPAIRED AS PER SRM 53-30-3, TABLE 1, PAGES 87, 88 & 88A. 2 L 7 2 4F 4 F A16WE E2EA 2001073000209 20010730 00209 NE 2001 7 30 UPS01836021 2 20010606 A 7200 ENGINE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE NR 3 FLAMED OUT A IPXA E ENGINE SHUTDOWN X ENGINE FLAMEOUT CR CRUISE 1 SO 01 818UP 46108 INSPECTION TYPE:N/A NR 3 ENG FLAME-OUT IN CRUISE WITH NO KNOWN CAUSE. FL370 A/S M.80.OAT-54C 10.5 LBS ON FUEL. FOLLOWE D FLAME-OUT CHECKLIST AND ENG RELIGHT WITH NO PROBLEMS. OPERATED NORMALLY REMINDER OF FLIGHT. CHECKED ENGINE IN ACCORD ANCE M/M 71-00-00 PAGE 165. ALSO REMOVED AND REPLACED FUEL FILTER P/N 7588133, PACKING AND SEALS M-25988-1-156 1 EACH M 25988-1-123 TWO EACH. ENGINE RUNUP AND CHECK FOR OPERATION AND LEAKS. FUEL FILTER REPLACED IN ACC 73-10-02. 2 L 7 4 4F 4 F RT 4A25 E2GL 2001073000210 20010730 00210 WP 2001 7 30 UPS01836023 1 20010607 A 2923 57155A PUMP DOUG DC8 DC871F 302199D WP HYD SYSTEM LEAKING A IPXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 706UP 46056 INSPECTION TYPE:N/A HYD LOSS DOWN TO APPROX 6 GAL BYPASSED PUMPS. RAN LOSS OF HYD FLUID OR PRESS AND WAS ABLE TO CONFI GURE WITH GEAR AND FULL FLAPS - FLUID LEAKING AFTER LANDING RT SIDE R-R RUDDER STANDBY PUMP PN 57155A. OPS AND LEA K CHECKED OK. DURING ENG RUNS FOUND BOTH EDP LEAKING. REPLACING BOTH PUMPS. 2 L 7 4 4F RT 4A25 2001073000211 20010730 00211 NM 2001 7 30 UPS01236432 1 20010729 A 5310 SKIN BOEING 727 72762C 138402C NM RH WHEEL WELL CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 912UP 19244 INSPECTION TYPE:N/A CRACKS AT RH WHEEL WELL AREA STA 870 ***MRR FILED AS OPEN*** 2 L 7 3 4F A3WE 2001082200217 20010822 00217 EA 2001 8 22 COMA0160502 1 20010727 A 5346 601350061 BEAM CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 963CA 11979 7127 FOUND CRACK ON LEFT AND RIGHT SIDE LOWER WEB OF ENGINE SUPPORT BEAM - FORWARD, INBOARD OF ACCESS PANEL. REPAIRED THE EN GINE SUPPORT BEAM LOWER RIGHT AND LEFT WEB IAW CANADAIR REO 601R-53-61-366. 2 L 7 2 4F RT A21EA 2001073000212 20010730 00212 EA 2001 7 30 COMA0160503 1 20010727 A 5300 601350061 WEB CNDAIR NA CNDAIR CL600 CL6002B19 EA CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 937CA 16092 NA 7044 ENGINE SUPPORT BEAM APPEARS TO BE CRACKED IN THE AFT CENTER AREA OF THE UPPER SURFACE PROTRUDIG FROM BOTH ENDS OF FASTEN ER HOLE CAREA MARKED BUTTLINE 8.5K.PERFORMED TEMPORARY REPAIR TO ENGINE SUPPORT BEAM UPPER AND LOWER WEBS PER REO 601R-5 3-61-345. 2 L 7 2 4F RT A21EA 2001073000213 20010730 00213 WP 2001 7 30 UPS01836061 1 20010612 A 2701 CONTROL COLUMN DOUG DC8 DC871F 302199D WP COCKPIT LACK OF LUBE A IPXA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:N/A DURING FLIGHT CONTROL CHECK ELEVATOR EXHIBITED NON-UNIFORM MOVEMENT WHICH RELEASED FROM FORWARD POSI TION AS YOKE TRAVELED FROM ITS MOST FWD POSITION AFT STOP AFT IT STOPPED ITS TRAVEL FOR 1-2 SECONDS FROM CONTINUED TO NO RMAL POSITION *S/D* LUBED CONTROL COLUMN AREA AND ELEVATOR CONTROL SYSTEM. PERFORMED INSPECTION/CHECK OF ELEVATOR AND TAB ASSY. OPS CHECKS GOOD. 2 L 7 4 4F RT 4A25 2001073000214 20010730 00214 WP 2001 7 30 UPS01836063 1 20010604 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2,3 RIGHT WING INBOARD L/E LOWER SKIN HAS INTERGRANULAR CORROSION AT XFS193. REPAIRED SKIN IAW EO DC8- 5720-7767-A. 2 L 7 4 4F RT 4A25 2001073000215 20010730 00215 EU 2001 7 30 MALA010583 1 20010708 A 5320 SEAT TRACK SAAB SF340 SF340A 7850100 EU CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 76XJ 340A076 DURING 4-K CHECK IN CWA, CARGO SEAT TRACK LBL 18.3 STA 619-687 HAS HEAVY CORROSION. MAINTENANCE REMOVED PAINT AND ORROS ION FROM RH TRACK RBL 18.3 IAW SRM 51-70-40. SEE DISC #4 FOR ALODINE. 2 L 7 2 4T RT A52EU 2001073000216 20010730 00216 EU 2001 7 30 MALA010584 1 20010708 A 5320 7253799457 SEAT TRACK SAAB SF340 SF340A 7850100 EU CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 76XJ 340A076 DURING 4K-CHECK IN CWA, CENTER AISLE SEAT TRACK BLO IN CARGO AREA HAS CORROSION. MAINTENANCE REMOVED AND REPLACED BLO C ARGO SEAT TRACK PN 7253799-457 AND REPAIRED BEAM-379. 2 L 7 2 4T RT A52EU 2001073000217 20010730 00217 NE 2001 7 30 MALA010594 2 20010722 A 7220 GEE367252 ENGINE SAAB SF340 SF340A 7850100 EU CT7TP CT75A 30030 NE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 79XJ 340A079 DURING FLIGHT #2906, FROM DTW LH CHIP DETECT LIGHT ILLUMINATED AFTER DEPARTURE FROM DTW. AT UNDER 1000' AGL. ALL ENGINE PARAMETERS NORMAL. QRH WAS COMPLETED MX NOTIFIED. AIR RETURN TO DTW. MAINTENANCCE REPLACED LH ENGINE S/N ON GE-E-3672 52. IAW JC #7100-301 PERFORMED TYPE 1 AND 11 BREAK IN RUNS, NO DISCREPANCIES NOTED. LEAK CHECK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2001073000218 20010730 00218 WP 2001 7 30 UPS01836064 1 20010606 A 5320 3750257503N SPLICE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2,3 STA 1040 - 1060 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257, AND SRM 53-1-0, 51-1-20D. 2 L 7 4 4F RT 4A25 2001073000219 20010730 00219 WP 2001 7 30 UPS01836065 1 20010606 A 5320 3750257U1 SPLICE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2,3 STA 1040 - 1060 LONG 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257, AND SRM 53-1-0, 51-1-20D. 2 L 7 4 4F RT 4A25 2001081600164 20010816 00164 NE 2001 8 16 ARWA0010720 2 20010728 A 7510 361615 BOLT DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE NR 1 ENGINE SHEARED A ARWA E ENGINE SHUTDOWN J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 19 8968U 46069 67150 DURING FL 350 AND AS CRUISE ALTITUDE, THE NR 1 ENGINE OIL PRESSURE LIGHT ILLUMINATED AND THE EGT BECAME ERRATIC. PERFOR M CHECKLIST, SHUT DOWN ENGINE AT 0819Z, OIL PRESSURE READING 45 PSI. ON LANDING SMELLED BURNING SMELL IN COCKPIT. LAND ED WITHOUT INCIDENT. INSPECTION OF THE NR 1 ENGINE REFLECTS REVEALED PYLON HARNESS BURNS NEAR THE ANTI-ICE MANIFOLD ASS Y. CAUSE WAS DUE TO THE FWD ANTI-ICE COUPLING ASSY (P/N-735138) LOOSE, DUE TO HAVING A SHEARED BOLT (361615). BOLT, WA SHER AND NUT WERE REPLACED WITH NEW PARTS, AND TORQUE IAW STANDARD PRACTICES. REMOVED AND REPLACED DAMAGE WIRING. PERFO RMED ENGINE RUN TEST AND PNEUMATIC SYSTEM CHECKS AND FOUND SATISFACTORY. 2 L 7 4 4F 4 F 4A25 1E8 2001073000220 20010730 00220 WP 2001 7 30 UPS01836066 1 20010605 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2,3 RIGHT WING OUTBOARD L/E HAS CRACKED UPPER RIB AT XFS 572.5, AND LOWER RIB AT XFS 566.25. REPAIRED RIBS IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001073000221 20010730 00221 WP 2001 7 30 UPS01836067 1 20010605 A 5730 576960039 DOUBLER DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2,3 RIGHT WING OUTBOARD L/E UPPER INTERNAL DOUBLER IS CRACKED AT XFS 572.5. REMOVED, FABRICATED AND RE PLACED DOUBLER IAW DWG 5769600, AND SRM 57-1-0, 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001073000222 20010730 00222 WP 2001 7 30 UPS01836068 1 20010604 A 5712 576946711 RIB DOUG DC8 DC871F 302199D WP RT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2,3 RIGHT WING OUTBOARD L/E RIB WEB IS TORN AT XW 761. REMOVED, FABRICATED, AND REPLACED WEB IAW DWG 5 769467 AND SRM 57-1-0, 51-1-21. 2 L 7 4 4F RT 4A25 2001073000223 20010730 00223 WP 2001 7 30 UPS01836071 1 20010601 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2,3 TRANSFERRED FROM LOG PAGE 9645247, REF DMI D-188382 CRACK ON LEFT WING L/E OUTBOARD OF NR 2 PYLON A T XW 257. REPAIRED SKIN IAW DC8-5720-4087 APPX C. 2 L 7 4 4F RT 4A25 2001073000224 20010730 00224 WP 2001 7 30 UPS01836072 1 20010608 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2,3 LEFT WING O/B RIB IS CRACKED AT XFS 653. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001073000225 20010730 00225 WP 2001 7 30 UPS01836073 1 20010608 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2,3 LEFT WING OUTBOARD L/E RIBS ARE CRACKED AT XFS 791.25, XFS 755.75. REPAIRED RIBS IAW SRM 57-2-0 FI G 2. 2 L 7 4 4F RT 4A25 2001073000226 20010730 00226 WP 2001 7 30 UPS01836074 1 20010608 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2,3 LEFT WING OUTBOARD L/E RIBS ARE CRACKED AT XFS 722.5, XFS 728.75. REPAIRED RIBS IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001073000227 20010730 00227 WP 2001 7 30 UPS01836075 1 20010603 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2,3 LEFT WING UPPER SKIN IS CRACKED AT XRS 74 AT STRINGER 10. REPAIRED SKIN IAW SRM 57-2-1 FIG 10. 2 L 7 4 4F RT 4A25 2001073000229 20010730 00229 WP 2001 7 30 UPS01836076 1 20010606 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C1 EXTERNAL FUSELAGE STA 1740 L28R - L30R SKIN HAS A BULGE AND ONE FASTENER HEAD BELOW SKIN. REMOVED FA STENER IAW DC8 SRM 51-1-21. REMOVED CORROSION IAW DC8 SRM 51-1-8, FOUND TO BE OUT-OF-LIMITS IAW DC8 SRM 53. FAB EXTERN AL DOUBLER FINGER DOUBLER AND FILLER IAW DC8 SRM 53-2-1. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 2001073000230 20010730 00230 WP 2001 7 30 UPS01836126 1 20010617 A 5610 WINDOW DOUG DC8 DC873F 302199F WP COCKPIT OUT OF ADJ A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:N/A, F/O SLIDING WINDOW WOULD NOT OPEN. ADJUSTED WINDOW. 2 L 7 4 4F RT 4A25 2001073000231 20010730 00231 WP 2001 7 30 UPS01836127 1 20010606 A 5320 37558452N FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C23 STA 1160 LONG 35L BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3 755845 AND SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 2001073000232 20010730 00232 WP 2001 7 30 UPS01836128 1 20010605 A 5320 3754473U1 SPLICE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2,3 STA 380 - 400 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754473 AND SRM 53-1-0, 51-1-20D. 2 L 7 4 4F RT 4A25 2001073000233 20010730 00233 WP 2001 7 30 UPS01836129 1 20010603 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2,3 RIGHT WING UPPER SKIN IS CRACKED AT STA XW 402 AT STRINGER 10. REPAIRED SKIN IAW SRM 57-2-1 FIG 21 . 2 L 7 4 4F RT 4A25 2001073000234 20010730 00234 WP 2001 7 30 UPS01836130 1 20010605 A 5730 580273631 DOUBLER DOUG DC8 DC871F 302199D WP RT WING BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2,3 RIGHT WING OUTBOARD L/E STUB WING LOWER INTERNAL DOUBLER IS BROKEN AT XOLDO 67.5. REMOVED, FABRICA TED, AND REPLACED DOUBLER IAW DWG 5802736 AND SRM 57-2-1 FIG 14A. 2 L 7 4 4F RT 4A25 2001073000235 20010730 00235 WP 2001 7 30 UPS01836131 1 20010607 A 5720 5769857304 INTERCOSTAL DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2,3 RIGHT WING CENTER L/E INTERCOSTAL IS CRACKED AT XS 454.976. REMOVED AND REPLACED INTERCOSTAL IAW D WG 5769857 AND SRM 57-1-0, 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001073000236 20010730 00236 WP 2001 7 30 UPS01836133 1 20010607 A 5510 37014272 FITTING DOUG DC8 DC871F 302199D WP HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2,3 RIGHT HORIZONTAL STAB T-FITTING AT I/B LOWER SECTION FWD OF FRONT SPAR IS CRACKED AT APPROX 47.5. REMOVED AND REPLACED FITTING IAW DWG 3701427 AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001073000237 20010730 00237 WP 2001 7 30 UPS01836146 1 20010605 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C1 AFT PIT FS 1160, L36-L35 BATHTUB FITTING IS CRACKED. REMOVED DAMAGED FITTING, FABBED SPLICE ANGLES, ALODINED AND PRIMED. INSTALLED NEW FITTING AND SPLICE ANGLES IAW DC8 SRM 53-2-0, 51-1-8, 51-1-20D. 2 L 7 4 4F RT 4A25 2001073000238 20010730 00238 WP 2001 7 30 UPS01836147 1 20010604 A 5414 SKIN DOUG DC8 DC873F 302199F WP NR4 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C1 NR 4 PYLON O/B WEB PNL FWD ACCESS HOLE HAS APPROX 1 INCH CRACK ON LWR SIDE. REMOVED FASTENER -22 & - 28 IAW REO G08127 DC8 SRM 51-1-21 51-1-20D & 51 -3-0 MAT ID FOR -3 -5 DOUBLERS .125 7075-T6 PO 340779 IAW REO G08127. L OCATED AND DRILLED -3 -5 DOUBLERS IAW REOG008127 DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED -22 -28 STIFFENERS AND -3 -5 DOUBLERS IAW REO G08127 DC8 SRM 51-1-11, 51-1-20D, 51-1-21, 51-3-0. 2 L 7 4 4F RT 4A25 2001073000239 20010730 00239 WP 2001 7 30 UPS01836148 1 20010529 A 2810 FASTENER DOUG DC8 DC873F 302199F WP RT WING LOOSE A IPXA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C1 1 FASTENER LEAKING FUEL AT XRS 500 BOTTOM NR 4 ALT. REMOVED FASTENER IAW DC8 SRM 51-1-20D OVERSIZED HOLE FOR BUSHING INSTALLATION AS REQD PER REO G0123, FABBED BUSHING AND INSTALLED PER REO G0812 3. INSTALLED NEW DOUBLE R -502 IAW DC8 SRM 51-1-20D AND REO G08123. 2 L 7 4 4F RT 4A25 2001073000240 20010730 00240 WP 2001 7 30 UPS01836149 1 20010530 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C1 AFT PIT FS 1140 L35R INTERCOSTAL ATTACH FITTING IS CRACK. REMOVED AND REPLACED NEW FITTING IAW DC8 S RM 51-1-20D. 2 L 7 4 4F RT 4A25 2001073000241 20010730 00241 WP 2001 7 30 UPS01836150 1 20010531 A 5230 STOP FITTING DOUG DC8 DC873F 302199F WP CARGO DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C1 AFT PIT D-DOOR LT STOP CORRODED. REPLACED DOOR STOP IAW DC8 SRM 51-1-24. 2 L 7 4 4F RT 4A25 2001073000242 20010730 00242 WP 2001 7 30 UPS01836157 1 20010621 A 2121 FAN DOUG DC8 DC873F 302199F WP COCKPIT FAILED A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 880UP 46080 INSPECTION TYPE:N/A, STRONG ELECTRICAL BURNING SMELL SUSPECTED PACK SMOKE. WITH LEFT PACK AND RECIRC FAN OFF SMELL DISS IPATED. RAN ALL 4 ENGINES, OPERATED BOTH PACKS PER MM 21-55-00. NO ABNORMALITIES NOTED. FOUND RECIRC FAN INOP AND TO BE SOURCE OF ODOR. DEFERRED RECIRC FAN PER MEL 21-16. 2 L 7 4 4F RT 4A25 2001073000243 20010730 00243 CE 2001 7 30 C2XA01CL180 1 20010725 A 3260 1143610441 SWITCH BEECH 1900 1900D 1154162 CE FAILED A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 81556 UE239 CLE FLIGHT#3135 THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT WITHOUT USING THE DOWN LOCK RELEASE BUTTON.MAINTENA NCE REPLACED THE RIGHT MAIN LANDING GEAR DOWN POSITION SWITCH AND SAFETY SQUAT SWITCH.OPERATIONAL CHECKS WERE GOOD.THE A IRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT A24CE 2001073000244 20010730 00244 WP 2001 7 30 UPS01836161 1 20010621 A 5330 ACCESS PANEL DOUG DC8 DC873F 302199F WP FUSELAGE LOOSE A IPXA B EMER. DESCENT O OTHER NR NOT REPORTED 1 SO 01 840UP 46140 INSPECTION TYPE:N/A PASSING 12,000 FEET LOUD BANG FROM RT FRONT SIDE OF AIRCRAFT FOLLOWED BY AIRCRAFT DEPRESSURIZATION. SUSPECT HAIL STORM PRIOR TO TAKEOFF EMERGENCY ACCESS FOR F/O SLIDING WINDOW DISLODGED RE-INSTALLED ACCESS PNL, OK FOR C ONTINUED SERVICE. 2 L 7 4 4F RT 4A25 2001073000245 20010730 00245 WP 2001 7 30 UPS01836162 1 20010622 A 3244 TIRE DOUG DC8 DC871F 302199D WP NLG WORN A IPXA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 SO 01 706UP 46056 INSPECTION TYPE:N/A BTB - REJECTED TAKEOFF AT80 KIAS DUE TO VIOLENT SHAKING AND THUMPING SOUNDS DURING TAKEOFF ROLL. SU SPECTED BLOWN NOSE TIRE. FOUND LEFT AND RIGHT NOSE TIRES WORN UNEVEN. SUSPECT OUT OF ROUND PER MM 32-50-00. REMOVED A ND REPLACED LEFT AND RIGHT NOSE TIRES. 2 L 7 4 4F RT 4A25 2001073000246 20010730 00246 WP 2001 7 30 UPS01836169 1 20010622 A 3350 MODULE DOUG DC8 DC873F 302199F WP COCKPIT DEFECTIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:N/A EMERGENCY LIGHT MODE PANEL UNARMED STAYS ON IN ARMED POSITION. FOUND PANEL DEFECTIVE REPLACED EMERG ENCY LIGHTS MODULE AND OPS CHECKS NORMAL. 2 L 7 4 4F RT 4A25 2001073000247 20010730 00247 WP 2001 7 30 UPS01836175 1 20010621 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW MM 33-50-01, OPS CHECKS GOOD . 2 L 7 4 4F RT 4A25 2001073000248 20010730 00248 WP 2001 7 30 UPS01836191 1 20010625 A 3350 5708458503 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT BATTERY PACK DISCHARGED. REMOVED AND REPLACED EMERGENCY BATTERY PACK, CKS OK P /N ON-OFF 5708458-503, S/N OFF FT L 158 ON 2085. 2 L 7 4 4F RT 4A25 2001073000249 20010730 00249 WP 2001 7 30 UPS01836196 1 20010606 A 5320 37592581N SPLICE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2 STA 1260 - 1280 LONG 35L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3759258 AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001073000250 20010730 00250 WP 2001 7 30 UPS01836197 1 20010603 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT XW 0. REPAIRED SKIN IAW SRM 57-2-1 FIG 20. 2 L 7 4 4F RT 4A25 2001073000251 20010730 00251 WP 2001 7 30 UPS01836198 1 20010606 A 5320 3754916501N FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2 STA 1228 LONG 31R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754916 AND SRM 53-1- 0, 51-1-20D. 2 L 7 4 4F RT 4A25 2001073000252 20010730 00252 WP 2001 7 30 UPS01836199 1 20010603 A 5320 3750727513 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2 STA 804 RIGHT KEEL BEAM FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750727 SRM 51-1-20 D, 51-1-21, 51-3-0. 2 L 7 4 4F RT 4A25 2001073000253 20010730 00253 WP 2001 7 30 UPS01836200 1 20010604 A 5320 3754918U1 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2 STA 1190 LONG 21R RT CUSP TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754918 AND SRM 51-1-20D, 51-3-0. 2 L 7 4 4F RT 4A25 2001073000254 20010730 00254 WP 2001 7 30 UPS01836201 1 20010606 A 5320 37592221N FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2 STA 1260-1280 LONG 34R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3759222 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001073000255 20010730 00255 WP 2001 7 30 UPS01836202 1 20010606 A 5320 3755847501N FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2 STA 1150 AT LONG 33R BANANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755847 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001073000256 20010730 00256 WP 2001 7 30 UPS01836203 1 20010614 A 5542 56550776 SKIN PANEL DOUG DC8 DC871F 302199D WP RUDDER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2 RIGHT RUDDER PANEL IS CORRODED BEYOND LIMITS AT ZR 253. REMOVED, FABRICATED, AND REPLACED SKIN IAW D WG 5655077 AND EO M-5100-11491-B. 2 L 7 4 4F RT 4A25 2001073000257 20010730 00257 WP 2001 7 30 UPS01836204 1 20010604 A 5320 561229857 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2 STA -60 AT LBL 53 SUBFLOOR FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACE D DOUBLER IAW DWG 5612298 AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001073000258 20010730 00258 WP 2001 7 30 UPS01836205 1 20010603 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2 STA 61-63 INNER SKIN IS CORRODED BEYOND LIMITS, BETWEEN LONG 36 AND LONG 35R. REPAIRED SKIN IAW 8110 -3 APPROVED DH SK 705-086. 2 L 7 4 4F RT 4A25 2001073000259 20010730 00259 WP 2001 7 30 UPS01836206 1 20010603 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2 MAIN CABIN SEAT TRACK IS CORRODED BEYOND LIMITS AT STA 610 LBL 59. REPAIRED SEAT TRACK IAW SRM 53-2- 3 FIG 8A. 2 L 7 4 4F RT 4A25 2001073000260 20010730 00260 WP 2001 7 30 UPS01836207 1 20010606 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2 STA 1340 FRAME IS CORRODED BEYOND LIMITS AT LONG 36. REPAIRED FRAME IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001073000261 20010730 00261 WP 2001 7 30 UPS01836208 1 20010606 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2 STA 1360 FRAME IS CORRODED BEYOND LIMITS AT LONG 36. REPAIRED FRAME IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001073000262 20010730 00262 WP 2001 7 30 UPS01836209 1 20010606 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2 STA 1400 FRAME IS CORRODED BEYOND LIMITS AT LONG 35R. REPAIRED FRAME IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001073000263 20010730 00263 WP 2001 7 30 UPS01836210 1 20010606 A 5542 565507780 SKIN PANEL DOUG DC8 DC871F 302199D WP RUDDER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2 RUDDER TRAILING EDGE IS CORRODED BEYOND LIMITS AT APPROX ZR 168 P/N 5655077-80, JUST ABOVE RUDDER TAB . REMOVED, FABRICATED AND REPLACED RUDDER SKIN PANEL IAW DWG 5655077 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001073000264 20010730 00264 WP 2001 7 30 UPS01836211 1 20010603 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2 MAIN CABIN SEAT TRACK SCALLOPS ARE BROKEN AT STA 1600 RBL 48. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A. 2 L 7 4 4F RT 4A25 2001073000265 20010730 00265 WP 2001 7 30 UPS01836212 1 20010603 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C2 MAIN CABIN SEAT TRACK HAS BROKEN SCALLOPS AND PLUG GOUGED BETWEEN STA 765-781 LBL 24. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A. 2 L 7 4 4F RT 4A25 2001073000266 20010730 00266 WP 2001 7 30 UPS01836217 1 20010630 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:N/A EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED BATTERY PACK. 2 L 7 4 4F RT 4A25 2001073000267 20010730 00267 WP 2001 7 30 UPS01836218 1 20010619 A 5230 HINGE DOUG DC8 DC873F 302199F WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C2 AFT PIT C3 RAMP PANEL FOLDING DOOR HINGE IS CRACKED. REMOVED AND REPLACED HINGE (REP) DC8 SRM 51-3-2 , 51-3-0. 2 L 7 4 4F RT 4A25 2001073000268 20010730 00268 WP 2001 7 30 UPS01836238 1 20010627 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C2 AFT PIT STA 1240 BETWEEN L35R-L34R FITTING CRACKED. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D, RE C'D LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001073000269 20010730 00269 WP 2001 7 30 UPS01836240 1 20010629 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C2 AFT PIT LONGERON 34L CRACKED FS 1482-1487. REMOVED DAMAGED PART OF LONGERON, INSTALLED NEW PART OF L ONGERON AND NEW SPLICE. 2 L 7 4 4F RT 4A25 2001073000270 20010730 00270 WP 2001 7 30 UPS01836242 1 20010630 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C2 AFT PIT FS 1220 - 1228 FITTING AT L31R HAS EXFOLIATED CORROSION. REMOVED AND REPLACED NEW FITTING IA W DC8 SRM 51-3-0 & 51-1-20D. 2 L 7 4 4F RT 4A25 2001073000271 20010730 00271 WP 2001 7 30 UPS01836243 1 20010630 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C2 AFT PIT STA 1230 INSIDE TORQUE BOX AT L32R FITTING CRACK. REMOVED AND REPLACED (2) BANANA FITTING (4 ) EACH LONGERON END FITTINGS AND SUPPORT ANGLE AT RT JAMB AREA IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001073000272 20010730 00272 WP 2001 7 30 UPS01836262 1 20010619 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C2 FWD CARGO PIT AT FS 200 ABOVE LONG 36 FRAME IS CORRODED AT LONGERON ATTACH FITTINGS. REMOVED CORROSI ON IAW DC8 SRM 51. FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. 2 L 7 4 4F RT 4A25 2001073000273 20010730 00273 WP 2001 7 30 UPS01836264 1 20010706 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:X2 FWD CARGO PIT AT FS 500 - 520 INTERCOSTAL AT LONG 33R IS CRACKED. REMOVED OLD INTERCOSTAL, FABBED NE W PART TREATED AND PRIMED NEW PART, DRILLED, INSTALLED NEW PART ALL IAW DC8 SRM 51-1-8 AND DAC DWG 5616 520 & SRM 51-1-2 0D. 2 L 7 4 4F RT 4A25 2001073000274 20010730 00274 WP 2001 7 30 UPS01836265 1 20010630 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:X2 AFT PIT FS 1152 FITTING AT L31R-L33R IS CRACKED. REMOVED BANANA FITTINGS AT STA 1152 & 1160 IAW DC8 SRM 51-1-20D, REC' D LOCATED AND DRILLED NEW FITTING AT STA 1152 IAW DC8 SRM 51-1-24 AND REINSTALLED NEW FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001073000275 20010730 00275 WP 2001 7 30 UPS01836266 1 20010702 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C2 AFT PIT FS 1270 LONGERON 35L CRACKED. REMOVED CRACKED SECTION OF LONGERON IAW DC8 SRM 51-1-20D, RECE IVED NEW SECTION, FAB'D P/N 3758593-1, LOCATED AND DRILLED HOLES IAW DC8 SRM 51-1-24, INSTALLED SECTION OF LONGERON IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001073000276 20010730 00276 WP 2001 7 30 UPS01836267 1 20010619 A 5320 SPLICE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C2 AFT PIT FS 1270 L35L SPLICE FITTING IS CRACKED. REMOVED SPLICE IAW DC8 SRM 51-1-20D, FOUND LONGERON SPLICE FITTING CRACKED. RCVD NEW SPLICE PN 3759253-1N LOCATED, DRILLED AND DEBURRED FITTING IAW DC8 SRM 51-1-24. INSTA LLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001073000279 20010730 00279 WP 2001 7 30 UPS01836268 1 20010619 A 5320 SPLICE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:X2 FWD CARGO PIT AT FS 600-620 LONG 31R SPLICE FITTING CRACKED. REMOVED SPLICE FITTING DRILLED NEW FITT ING IAW DC8 SRM 51-1-24, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001073000280 20010730 00280 WP 2001 7 30 UPS01836316 1 20010705 A 5320 4772397U1 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 STA 1772 LONG 10R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397 AND SRM 53-1- 0, 51-1-20D. 2 L 7 4 4F RT 4A25 2001073000281 20010730 00281 WP 2001 7 30 UPS01836317 1 20010705 A 5320 4772397U1 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 STA 1774 LONG 10L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397 AND SRM 53-1- 0, 51-1-20D. 2 L 7 4 4F RT 4A25 2001073000282 20010730 00282 WP 2001 7 30 UPS01836318 1 20010706 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 RIGHT WING LOWER SKIN IS CRACKED AT STRINGER 64 AT O/B END. REPAIRED SKIN IAW EO DC8-5730-9004 APPX E. 2 L 7 4 4F RT 4A25 2001073000283 20010730 00283 WP 2001 7 30 UPS01836319 1 20010625 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 COMPLY WITH EO DC8-5330-12073-A, STA 25 LONG 10L FOUND TWO SKIN CRACKS AFTER DOUBLER WAS REMOVED. RE PAIRED SKIN IAW SRM 53-2-0 FIG 15. 2 L 7 4 4F RT 4A25 2001073000284 20010730 00284 WP 2001 7 30 UPS01836320 1 20010705 A 5320 4772397U1 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 STA 1774 LONG 17L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397 AND SRM 53-1- 0, 51-1-20D. 2 L 7 4 4F RT 4A25 2001073000285 20010730 00285 WP 2001 7 30 UPS01836321 1 20010626 A 5320 975850737 GUSSET DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 STA 1240 UPPER GUSSET IS CRACKED AT LONG 34R. REMOVED, FABRICATED AND REPLACED GUSSET IAW DWG 975850 7 AND SRM 53-1-0, 51-1-20D. 2 L 7 4 4F RT 4A25 2001073000286 20010730 00286 WP 2001 7 30 UPS01836322 1 20010625 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 341. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001073000287 20010730 00287 WP 2001 7 30 UPS01836323 1 20010627 A 5730 576960036 DOUBLER DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 RIGHT WING INTERNAL DOUBLER IS CRACKED AT XFS 597.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DW G 5769600 AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001073000288 20010730 00288 WP 2001 7 30 UPS01836324 1 20010626 A 5320 4641326N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 STA 1690 LONG 22L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641326 AND SRM 51-1- 20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001073000289 20010730 00289 WP 2001 7 30 UPS01836325 1 20010702 A 5320 3750257503N SPLICE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 STA 1040-1060 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND S RM 51-1-20D. 2 L 7 4 4F RT 4A25 2001073000290 20010730 00290 WP 2001 7 30 UPS01836326 1 20010626 A 5320 3754041501N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 STA 320 BANANA FITTING IS CRACKED AT 27L. REMOVED AND REPLACED FITTING IAW DWG 3754041 AND SRM 51-1- 20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001073000291 20010730 00291 WP 2001 7 30 UPS01836327 1 20010626 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 LEFT WING L/E LOWER SKIN IS CRACKED AT XFS 597.5. REPAIRED SKIN IAW EO DC8-5720-4087. 2 L 7 4 4F RT 4A25 2001073000292 20010730 00292 WP 2001 7 30 UPS01836328 1 20010626 A 5320 4641326N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 STA 1690 LONG 35R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641326 AND SRM 51-1- 20D. 2 L 7 4 4F RT 4A25 2001073000293 20010730 00293 WP 2001 7 30 UPS01836329 1 20010625 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 RIGHT WING L/E UPPER SKIN IS CRACKED AT XFS 200. REPAIRED SKIN IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001073000294 20010730 00294 WP 2001 7 30 UPS01836330 1 20010626 A 5711 DOUBLER DOUG DC8 DC873F 302199F WP LT WING BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 LEFT WING LOWER FRONT SPAR STRAP AND DOUBLER ARE BROKEN AT XS 520. REMOVED, FABRICATED AND REPLACED DOUBLER AND STRAP IAW SRM 57-2-1 FIG 14A. 2 L 7 4 4F RT 4A25 2001073000295 20010730 00295 WP 2001 7 30 UPS01836331 1 20010626 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 STA 1680 FRAME IS CRACKED AT LONG 21R. REPAIRED FRAME IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001073000296 20010730 00296 WP 2001 7 30 UPS01836332 1 20010625 A 5320 WEB DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 STA 354 CUSP MEMBRANE IS CRACKED AT LONG 21L. REPAIRED MEMBRANE IAW SRM 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 2001073000297 20010730 00297 WP 2001 7 30 UPS01836333 1 20010625 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 RIGHT WING L/E UPPER SKIN IS CRACKED AT XFS 572.5. REPAIRED SKIN IAW SRM 57-2-1 FIG 38. 2 L 7 4 4F RT 4A25 2001073000298 20010730 00298 WP 2001 7 30 UPS01836334 1 20010625 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 STA 1620 LONG 20R LOWER FWD CORNER SKIN IS CRACKED AT R-2 DOOR. REPAIRED SKIN IAW SRM 53-2-0 FIG 17. 2 L 7 4 4F RT 4A25 2001073000299 20010730 00299 WP 2001 7 30 UPS01836335 1 20010626 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT XRS 105 AT STRINGER 14. REPAIRED SKIN IAW SRM 57-2-1 FIG 10. 2 L 7 4 4F RT 4A25 2001073000300 20010730 00300 WP 2001 7 30 UPS01836336 1 20010626 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 RIGHT WING LOWER L/E SKIN IS CORRODED BEYOND LIMITS AT XFS 722. REPAIRED SKIN IAW SRM 57-2-0 FIG 2A. 2 L 7 4 4F RT 4A25 2001073000301 20010730 00301 WP 2001 7 30 UPS01836337 1 20010629 A 5320 45976431N ATTACH FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 STA 35 FRAME ATTACH FITTING IS CORRODED BEYOND LIMITS AT LONG 21R. REMOVED AND REPLACED FITTING IAW DWG 4597643 AND SRM 53-1-0, 51-1-21, 51-3-0. 2 L 7 4 4F RT 4A25 2001073000302 20010730 00302 WP 2001 7 30 UPS01836338 1 20010630 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 STA 1100-1120 LBL 46 SEAT TRACK IS CORRODED BEYOND LIMITS. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A . 2 L 7 4 4F RT 4A25 2001073000305 20010730 00305 2001 7 30 AWXA0001826 4 20010604 A 3431 VOR SYSTEM AIRBUS 320 A320231 3930325 EU COCKPIT MALFUNCTIONED A AWXA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 WP 28 640AW 448 PHX - AIR TURNBACK - 6/2/01 - FLT 73 - ON DEPARTURE CLIMBOUT OF PHX THE AIRCRAFT LOST VOR NR 1, VOR NR 2, ILS NR 1 & ILS NR 2; THE AIRCRAFT RETURNED TO PHX. IN PHX MAINTENANCE RESET NR 1 & NR 2 RMP NAV SWITCHES AND CIRCUIT BREAKERS; CYCLED NR 1 & NR 2 FMGC CIRCUIT BREAKERS AND PERFORMED ADIRU REALIGNMENT. PERFORMED AFS TEST 22-96-00-501 W/ NO FAULTS NOTED. PERFORMED NR 1 & NR 2 VOR, ILS AND ADIRU'S BITE TEST W/ NO FAULTS NOTED AND NR 1 & NR 2 RMP BITE TEST W/ NO FAULTS NOT ED. THE AIRCRAFT WAS RETURNED TO SERVICE AND NO FURTHER DISCREPANCIES HAVE BEEN REPORTED. 2 L 7 2 4F RT A28NM 2001073000317 20010730 00317 EU 2001 7 30 CA010625030 1 20010526 A 2161 9599020135 CONTROL VALVE PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL CABIN TEMP FAILED W O OTHER O OTHER CR CRUISE 1 CA 526 526 (CAN) WHEN IN CRUISE THE TEMPERATURE IN THE A/C STARTED TO GET VERY WARM THE ECS SWITCH WAS TURNED TO MANUAL AND TURNED DOWN. IT GOT VERY HOT SO ECS SWITCH WAS TURNED OFF AND BACK ON. THE HEAT THAN WENT TO THE COLD POSITION AND COULD NOT BE ADJUSTED. TRIP CONTINUED HOME WITH JUST THE ELECTRIC HEATERS. THE CONTROL VALVE WAS CHANGED AND EVERYTHING WORKED FINE. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001073000332 20010730 00332 EU 2001 7 30 CA010626001 1 20010315 A 3310 SD190470020 BALLAST FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU CABIN FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA (CAN) PILOTS REPORTED THEY NOTICED A TOXIC SMELL (ACRID ODOUR)IN THE COCKPIT. OXYGEN MASKS WERE DONNED BY THE FLIGHT CRE W AND AN EMERGENCY WAS DECLARED FOR PRIORITY LANDING. THE AIRCRAFT RETURNED TO AND LANDED WITHOUT INCIDENT. THE CREW REP ORTS THE SMELL SEEMED TO BE COMING FROM THE OVER HEAD PANEL.THE AIRCRAFT WAS INSPECTED IN AND DEEMED SAFE FOR FERRY FLIG HT. AIRCFRAFT FLEW T O AMDHAD ITS CREW OXYGEN TOPPED UP AND REPOSITIONED. MAINTENANCE FOUND THE CENTER RED GLARE SHIELD LIGHT BALLAST TO BE FAULT. THE BALLAST WAS REMOVED AND THE SYSTEM WAS MEL'D (33-01-CATB. AIRCRAFT RETURNED TO SERVICE WI THNO FURTHER INCIDENTS TO REPORT (MEL REMAINS IN AFFECT AT TIME OF WRITING SDR). 2 L 7 2 4F 4 F RT A20EU E2EU 2001073000333 20010730 00333 EU 2001 7 30 CA010626002 2 20010525 A 7200 ENGINE FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU NR 2 FAILED W A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 CA (CAN) THE NR 2 ENGINE FAILED IN FLT ROUTE TO SAINT JOHN, NB. PILOTS RPT THAT IN LEVEL CRUISE FLT A LOUD BAND WAS HEARD, FOLLOWED BY SEVERE VIBRATIONS WHICH SUBSIDED WHEN ENGINE WAS BROUGHT BACK TO 80% NH TGT-OIL PRESSURE WAS NORMAL AT THIS POINT. DECISION WAS MADE TO DIVERT A/C TO QUE CITY (YQB). TEN MINS OUT OF YQB VIBRATIONS AGAIN WORSE-THE CREW ELECTED TO SHUTDOWN ENGINE . A/C LANDED INYQB W/O INCID. (NORMAL LDG). INIT INVEST. BY YQB MAINT FOUND LP2 TURBINE BLADES HARDTO T URN ALONG WITH A CHUNK OF METAL STICKING UP INTO THEAIRSTREAM IN THE EXHAUST COLLECTOR.MAINT REPLD ENGINE S/N: ON 9259 & EXHAUST COLLECTOR. GROUND RUNS COMPLETED WITH NO FAULT FOUND 2 L 7 2 4F 4 F RT A20EU E2EU 2001073000334 20010730 00334 EU 2001 7 30 CA010626004 1 20010518 A 2435 230481127 BRUSHES LUCAS 23085024 PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL STARTER GEN SHORTED W K NONE O OTHER IN INSP/MAINT 1 CA 99259 (CAN) DURING OVERHAUL OF REF. STARTER-GEN, DAMAGE TO ACCESS COVER & ONE BRUSH'S SHUNT WIRES FOUND. THIS DAMAGE CONSISTED OF BURNING MARKS ON COVER & BURNT &MELTED STRANDS OF BRAIDED SHUNT WIRES ON BRUSH. APPROX. 1/4 OF TOTAL BRUSH SHYNT WIR ES WERE BURNT THROUGH. CAUSE OF THIS IS INCORRECT INST OF COVER ON STARTER-GEN. JOINING BRACKETS OF COVER WERE LOCATED O VER #1 BRUSH, INSTEAD OF OVER A SUPPORT RIB OF BEARING SUPPORT ASSY.THIS ALLOWED BRUSH SHUNT WIRES TO TOUCH COVER & SHOR T TO GROUND. CONTINUED OP IN A SHORTED CONDITION CO ULD RESULT IN BRUSH SHUNTS BURNING THROUGH & CAUSING GEN FAILURE: BE CAUSE PC-12 IS A SINGLE ENGINE IFR A/C, THE 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001073000338 20010730 00338 WP 2001 7 30 CALA0100702 1 20010727 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP STA 1108-1309 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND L/H SEAT TRACK CORRODED AT STA 1108-1309. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK AND SPLICE WE RE INSTALLED IAW SRM 51-30-1. 2 L 7 2 4F A6WE 2001073000339 20010730 00339 NM 2001 7 30 CALA0100706 1 20010727 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM STA 1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14325 23455 INSPECTION FOUND FLOORBEAM CORRODED AT STA 1016, LBL 21 TO LBL 35. A CAP WAS INSTALLED ON BEAM IAW ECRA 5310-03851, REV A. 2 L 7 2 4F RT A16WE 2001073000340 20010730 00340 WP 2001 7 30 CALA0100708 1 20010728 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP COCKPIT DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND COPILOT'S I/B FLOOR PANEL DELAMINATED. THE FLOOR PANEL WAS REMOVED AND A NEW FLOOR PANEL WAS INSTALLED IAW SRM 53-30-01, 53-21-0, SHEET 23, 51-30-1, AND 51-30-2. 2 L 7 2 4F A6WE 2001073000341 20010730 00341 WP 2001 7 30 CALA0100709 1 20010729 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 389-408 PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND CABIN R/H I/B FLOOR PANEL PUNCTURED AT FS 389-408. A NEW PANEL WAS INSTALLED IAW ECRA 5320-01265 AND SR M 51-30-1. 2 L 7 2 4F A6WE 2001073000342 20010730 00342 WP 2001 7 30 CALA0100710 1 20010729 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FS 1174-1309 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND L/H O/B SEAT TRACK CORRODED AT FS 1174-1309. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTAL LED IAW SRM 51-30-1 AND 51-10-3. 2 L 7 2 4F A6WE 2001073000343 20010730 00343 WP 2001 7 30 CALA0100711 1 20010729 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 1079-1155 BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND CABIN L/H O/B FLOOR PANELS BROKEN OFF AT FASTENER HOLES AT FS 1079-1155 AND FS 1155-1250. THE PANELS WE RE REPAIRED IAW SRM 51-70-1. 2 L 7 2 4F A6WE 2001073000344 20010730 00344 WP 2001 7 30 CALA0100712 1 20010729 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 160-200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND FORWARD ENTRY FLOOR PANEL AT R-1 DOOR JAMB CORRODED, FS 160-200, RBL 48. THE FLOOR PANEL AND SUPPORT WE RE REMOVED AND A NEW FLOOR PANEL AND SUPPORT WERE INSTALLED IAW SRM 51-10-4, 53-30-1, AND 51-30-1. 2 L 7 2 4F A6WE 2001073000345 20010730 00345 WP 2001 7 30 CALA0100713 1 20010729 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FS 1032-1309 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND CABIN L/H CENTER SEAT TRACK CORRODED AT FS 1032-1309. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK W AS INSTALLED IAW SRM 51-30-1, 51-30-2, 51-30-5, 51-10-4, 51-10-3, AND 53-05, FIGURE 4F. 2 L 7 2 4F A6WE 2001073000346 20010730 00346 WP 2001 7 30 CALA0100714 1 20010729 A 5330 SKIN DOUG DC9 DC982 3022082 WP FS 494 & 522 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND L/H EXTERIOR FUSELAGE SKIN DENTED AT FS 522 ABOVE L25 AND AT FS 494 ABOVE L25. THE DENTS WERE COLD WORK ED IAW SRM 53-04, FIGURE 38. A DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 53-04, FIGURE 38, 51-10-4, AND 51-30-2. 2 L 7 2 4F A6WE 2001073000347 20010730 00347 WP 2001 7 30 MWEA011078 1 20010730 A 5740 SS0957000315 RIB DOUG DC9 DC932 3022066 WP LEFT WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 LEFT WING #3 SLAT DRIVER OUTBOARD FITTING HAS A SMALL 1/8" CRACK ACROSS THE SIDE TO SIDE GUIDE ROLLER LOBE. -- REMOVED CRACKED RIB, LOCATED BOTH INBOARD AND OUTBOARD FITTING, INSTALLED RIB. 2 L 7 2 4F A6WE 2001073000348 20010730 00348 WP 2001 7 30 MWEA011079 1 20010730 A 5310 99577397 SHEAR TIE DOUG DC9 DC932 3022066 WP STATION 945 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 SHEAR TIE CRACKED AT STATION 945 BETWEEN LONGERON 14 AND 15 RIGHT SIDE. -- REMOVED SHEAR TIE SECTION, FABRICATED NEW S ECTION AND SHEAR TIE SPLICE, INSTALLED NEW SHEAR TIE SECTION AND SPLICE. 2 L 7 2 4F A6WE 2001073000349 20010730 00349 2001 7 30 CA010626016 4 20010529 A 3445 WIRE 070101480001 LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE TCAS ARCED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) REMOVING THE TCAS CONTROL PANEL ON THE CAPT SIDE FOR PART NUMBER VERIFICATION, SPARKES AND ARCING WHERE OBSERVED C OMING OUT OF THE BUNDLE BEHIND THE PANEL. CB PULLED AND SOURCE INVESTIGATED FOUND SEVERVAL WIRES WITH THE INSULATION MIS SING DUE TO WIRE CHAFFING. WIRING WILL BEREPAIRED AND THE WIRE BUNDLE RE-ROUTED TO AVOID CHAFFING. 2 L 7 3 4F 4 F A23WE E12EU 2001073000350 20010730 00350 NM 2001 7 30 ZW0A0106005 1 20010727 A 3350 65801003 CONNECTOR BOEING 767 76733AER 1385230 NM A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 637TW 25403 DURING MAINTENANCE SEATS 1-2-3 JH WERE INOP, THE CAUSE WAS WEAR. REPLACED FLEX CALE CONNECTORS P/N 65801-003 AND RELAMP ED ASSY.WITH P/N 97F9705.LAST CHECK C 01/27/01 LAX ---CLOSED--- 2 L 7 2 4F RT A1NM 2001073000351 20010730 00351 NM 2001 7 30 ZW0A0106006 1 20010729 A 3350 80751 LAMP BOEING 767 76733AER 1385230 NM A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 637TW 25403 DURING MAINTENANCE THE EGRESS LIGHTS AT SEAT 32 C WERE INOP DUE TO WEAR. RELAMPED PER MM 33-51-00 WITH P/N 8075-1.LAST CHECK C 01/27/01 LAX ---CLOSED--- 2 L 7 2 4F RT A1NM 2001073000352 20010730 00352 NM 2001 7 30 ZW0A0106002 1 20010728 A 3350 6100928 LAMP BOEING 767 7673Q8 NM A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 634TW 28132 DURING PRE FLIGHT EGRESS LIGHTS AT SEAT 17J WERE INOP DUE TO WEAR. REPLACED 2 EA LAMPS P/N 6100928 AND 1 EA LENDS P/N S 417N509-2SMI.LAST CHECK C 10/25/01 LAX ---CLOSED--- 2 L 7 2 4F RT A1NM 2001073000353 20010730 00353 WP 2001 7 30 ZW0A0106003 1 20010727 A 2612 473597407 DETECTOR DOUG DC9 DC982 3022082 WP A ZW0A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 13 913TW 49184 DURING CRUSE FLIGHT 253 HAD A INDICATION OF SMOKE IN THE AFT. CARGO BIN. THE FLIGHT CREW MADE AN UNSCHEDULED LANDING AND FIRED THE AFT CARGO BIN FIRE BOTTLE. CAUSE- FALSE WARNING. REPLACED #1 AND 2 FIRE BOTTLES P/N 892857, FILTER ASSEMBLY, AFT CARGO BIN CELL AND DETECTORS #1-2-3 IN AFT CARGO BIN. LAST CHECK C 12/18/00 STL. ---CLOSED--- 2 L 7 2 4F A6WE 2001073000354 20010730 00354 EA 2001 7 30 SWIA200110064 1 20010728 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 EA COPILOT CRACKED A SWIA O OTHER O OTHER DE DESCENT 1 NM 07 423SW 7456 RIGHT WINDSHIELD INNER PANE CRACKED.COPILOT'S WINDSHIELD REPLACED IAW CRJ MM 56-11-01-400-801. 2 L 7 2 4F RT A21EA 2001073100001 20010731 00001 SO 2001 7 31 C2XA01IA304 1 20010727 A 7100 ALLSN EMB 145 EMB145LR SO ALLSN AE300 AE3007A GL A C2XA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SW 27 14993 311159 145289 CAE311159 CLT - FLIGHT 4083, THE CREW REPORTED THAT THE NUMBERONE ENGINE EXPERIENCED AN UNCOMMANDED SHUTDOWN OF FLIGHT. THE CREW T RIED TO RESTART THE ENGINE WITH NO SUCCESS, AND DIVERTED TO CLT WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR FILED OPEN AWAITING FINAL DETERMINATION OF CAUSE... 2 L 7 2 4T 4 F RT T00011AT TE6CH 2001073100002 20010731 00002 EU 2001 7 31 C2XA01IA306 1 20010729 A 3397 W192858322 WIRE AEROSP ATR42 ATR42320 8680930 EU BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14815 104 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT GALLEY OVERHEAD EMERGENCY EXIT LIGHT WAS INOP. MAINTENANCE REP AIRED A BROKEN WIRE ON THE AFFECTED LIGHT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001073100003 20010731 00003 NM 2001 7 31 USAA010727 1 20010517 A 5300 ANGLE BOEING 737 737301 1384611 NM BS 454 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND ANGLE CRACKED .5 INCH, BS 454 AT OUTBOARD FLOOR PANEL SUPPORT ANGLE. MANUFACTURED NEW CLIP AND INSTALLED, H EAT TREAT. (M) 2 L 7 2 4F RT A16WE 2001073100004 20010731 00004 NM 2001 7 31 USAA010725 1 20010517 A 5300 ANGLE BOEING 737 737301 1384611 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND ANGLE CRACKED 1.5 INCH, BS 616 BELOW S17L. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 53-62-01. (M) 2 L 7 2 4F RT A16WE 2001073100005 20010731 00005 NM 2001 7 31 USAA010724 1 20010517 A 5300 FRAME BOEING 737 737301 1384611 NM BS 500C CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND FRAME CRACKED .5 INCH, BS 500C AT STRINGER 8R. ROUTED OUT DAMAGE, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 53-10-14 AND EA 70647. (M) 2 L 7 2 4F RT A16WE 2001073100006 20010731 00006 NM 2001 7 31 USAA010723 1 20010517 A 5300 FRAME BOEING 737 737301 1384611 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND FRAME CRACKED .25 INCH, BS 480 AT STRINGER 8R. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER PER TYPICAL REP AIR 53-10-14 AND EA 70650. (M) 2 L 7 2 4F RT A16WE 2001073100007 20010731 00007 NM 2001 7 31 USAA010721 1 20010516 A 5700 ANGLE BOEING 737 737301 1384611 NM BS 540 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND ANGLE CRACKED 1 INCH, STATION 540 RIGHT WING ROOT 2 INCHES ABOVE STRINGER 22R. REMOVED DAMAGE, INSTALLED FI LLER AND REPAIR ANGLE PER TR 53-50-03. (M) 2 L 7 2 4F RT A16WE 2001073100008 20010731 00008 NM 2001 7 31 USAA010720 1 20010516 A 5700 ANGLE BOEING 737 737301 1384611 NM BS 540 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND ANGLE CRACKED 1 INCH, STATION 540 LEFT WING ROOT 2 INCHES ABOVE STRINGER. REMOVED DAMAGED AREA, INSTALLED F ILLER, REPAIR ANGLE PER TR 53-50-03. (M) 2 L 7 2 4F RT A16WE 2001073100009 20010731 00009 NM 2001 7 31 USAA010719 1 20010516 A 5300 FRAME BOEING 737 737301 1384611 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND FRAME CRACKED 1 INCH, BS 867 BETWEEN 58L-59L. INSTALLED DOUBLER PER T/R 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001073100010 20010731 00010 NM 2001 7 31 USAA010718 1 20010517 A 5310 FRAME BOEING 737 737301 1384611 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND FRAME CRACKED 1 INCH, BS 787 BETWEEN 58L AND 59L. INSTALLED DOUBLER PER T/R 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001073100011 20010731 00011 NM 2001 7 31 USAA010717 1 20010516 A 5300 WEB BOEING 737 737301 1384611 NM CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND WEB CRACKED .5 INCH, AT BL0 B5712 BELOW FLOORBEAM CAP, LEFT SIDE. INSTALLED REPAIR DOUBLERS PER EA 71067. (M) 2 L 7 2 4F RT A16WE 2001073100012 20010731 00012 NM 2001 7 31 USAA010716 1 20010517 A 5300 CLIP BOEING 737 737301 1384611 NM BS 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND CLIP CRACKED .25 INCH, BS 639 AT S11L. MANUFACTURED, HEAT TREATED, INSTALLED CLIP PER BOEING PRINT 66-24112 41-1. (M) 2 L 7 2 4F RT A16WE 2001073100013 20010731 00013 NM 2001 7 31 USAA010715 1 20010517 A 5300 WEB BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND WEB CRACKED .25 INCHES IN LENGTH, STATION 178 BULKHEAD LBL 5.7 WL 210 UPPER ANTENNA MOUNT. REPAIRED FILLER, DOUBLER AND SHIMS PER SRM 53-10-08 FIG 211. (M) 2 L 7 2 4F RT A16WE 2001073100014 20010731 00014 NM 2001 7 31 USAA010714 1 20010517 A 5310 WEB BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND WEB CRACKED .5 INCH, STATION 178 BULKHEAD LBL 5.7 WL 200, LOWER ANTENNA MOUNT. REPAIRED FILLER, DOUBLER AND SHIMS PER SRM 53-10-08 FIG 211. (M) 2 L 7 2 4F RT A16WE 2001073100015 20010731 00015 NM 2001 7 31 USAA010713 1 20010517 A 5300 ANGLE BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND ANGLE CRACKED .125 INCH, STATION 178 BULKHEAD LEFT CHORD ANGLE AT WL 207. REPAIRED FILLER, DOUBLER AND SHIM S PER SRM 53-10-08 FIG 211. (M) 2 L 7 2 4F RT A16WE 2001073100016 20010731 00016 NM 2001 7 31 USAA010712 1 20010517 A 5300 ANGLE BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND ANGLE CRACKED .125 INCH, STATION 178 BULKHEAD RIGHT CHORD ANGLE AT WL 207. REPAIRED DOUBLER, CHORD, CLIPS, SPLICE ANGLE PER SRM 53-10-08. (M) 2 L 7 2 4F RT A16WE 2001073100017 20010731 00017 NM 2001 7 31 USAA010711 1 20010517 A 5300 WEB BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND WEB CRACKED 5 INCHES, STATION 178 BULKHEAD RIGHT FLOOR WEB AT WL 207. REMOVED AND REPLACED FLOORWEB. (M) 2 L 7 2 4F RT A16WE 2001073100018 20010731 00018 NM 2001 7 31 USAA010708 1 20010517 A 5300 WEB BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND WEB CRACKED .75 INCH, STATION 178 BULKHEAD WL 184. REPAIRED FILLERS, DOUBLERS AND SHIMS PER SRM 53-10-08 FI G 211. (M) 2 L 7 2 4F RT A16WE 2001073100019 20010731 00019 EU 2001 7 31 USAAF01040 1 20010630 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU PAX CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 895US 11380 IND- THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE AT BOTH LAVATORIES, LAVATORY AREAS, AND THE AFT CABIN CEILING. MAINTEN ANCE REPLACED THE BATTERY PACK. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT 2001073100020 20010731 00020 NM 2001 7 31 USAASB01185 1 20010626 A 3200 BACC18Z3R CIRCUIT BREAKER BOEING 737 7373B7 1384580 NM FLT COMPT FAULTY A USAA O OTHER O OTHER DE DESCENT 1 EA 19 527AU 23862 EWR - FLT 432 - IN PREPARATION FOR LANDING AT EWR, FROM PIT, CREW RECEIVED A RED NOSE GEAR UNSAFE LIGHT WITHOUT ANY GEAR INDICATIONS. CREW CHECKED CIRCUIT BREAKERS AND ACCOMPLISHED QUICK REF HANDBOOK PROCEDURES. CREW RECYCLED GEAR BUT STI LL ONLY THE RED NOSE GEAR UNSAFE LIGHT ILLUMINATED WITH NO OTHER LIGHTS. A/C WENT INTO HOLDING PATTERN TO TROUBLESHOOT AND MANUALLY DEPLOY THE GEAR. CREW RECHECKED CIRCUIT BREAKERS AND FOUND THE AIR/GROUND RELAY AND LIGHTS CIRCUIT BREAKER PARTIALLY POPPED (NO WHITE SHOWING). CREW RESET CIRCUIT BREAKER AND RECEIVED THREE GEAR GREEN LIGHTS. CREW RECYCLED G EAR AND FOUND OPERATION/INDICATION NORMAL. FLIGHT PROCEEDED AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECL 2 L 7 2 4F RT A16WE 2001073100021 20010731 00021 NM 2001 7 31 USAASB01186 1 20010627 A 2150 3964982 CONTROL VALVE BOEING 737 7374B7 1384702 NM LEFT PACK BAY FAULTY A USAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 432US 25507 24554 LGA - FLT 508 - EN ROUTE FROM CLT TO LGA - AT FL250, CAPTAIN REPORTED THE CABIN ALTITUDE WARNING HORN BEGAN SOUNDING. C REW DESCENDED AIRCRAFT TO FL100 AND CONTINUED ONTO LGA. MAXIMUM CABIN ALTITUDE WAS 9,5000 FEET. FLIGHT LANDED AT LGA W ITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT PACK FLOW CONTROL VALVE. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001073100022 20010731 00022 NM 2001 7 31 USAASB01187 1 20010628 A 2700 1817389 TRANSMITTER BOEING 737 737401 1384701 NM FAULTY A USAA K NONE F FLT CONT AFFECTED DE DESCENT 1 EA 19 407US 13349 23877 CLT - FLT 1157 - IN PREPARATION FOR LANDING AT CLT, FROM ORD, CREW REPORTED A SPLIT FLAP INDICATION AS FLAPS WERE STUCK AT 7 DEGREES. FLIGHT LANDED WITHOUT FURTHER INCIDENT WITH NO EMERGENCY BEING DECLARED. MAINTENANCE REMOVED AND REPLACE D THE RIGHT FLAP POSITION TRANSMITTER PER MM 27-58-12. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001073100023 20010731 00023 NM 2001 7 31 USAA010747 1 20010619 A 5330 SKIN BOEING 737 737301 1384611 NM BS 727DE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 41925 23510 PIT - FOUND SKIN CRACKED 2.75 INCH, STRINGER 23 BS 727DE. REPAIRED PER SRM 53-30-00 WITH DOUBLER MEASURING 16 BY 10.5 P ER WRM 53-30-00 PAGE 201, FIG 201. (M) 2 L 7 2 4F RT A16WE 2001073100024 20010731 00024 NM 2001 7 31 USAA010746 1 20010615 A 5300 SKIN BOEING 737 7373B7 1384580 NM CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 524AU 43790 23859 PIT - FOUND SKIN CRACKED 4.75 INCHES BY 4.75 INCH AREA, BETWEEN FRAME 500B AND 500C, S5L, 4 INCHES AFT OF 500C. REPAIRE D PCW, 4.75 INCHES CIRCULAR DOUBLER INSTALLED PER SRM 53-00-01 FIG 208. (M) 2 L 7 2 4F RT A16WE 2001073100025 20010731 00025 NM 2001 7 31 USAA010745 1 20010615 A 5300 SKIN BOEING 737 7373B7 1384580 NM BS 500 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 524AU 43790 23859 PIT - FOUND SKIN CRACKED 8 INCHES BY 6 INCH AREA, BETWEEN FRAME STATION 500C AND 500D, S5L, 6 INCHES AFT 500C. REPAIR P CW, 8 INCHES BY 6 INCH DOUBLER INSTALLED PER SRM 53-00-01 FIG 201. (M) 2 L 7 2 4F RT A16WE 2001073100026 20010731 00026 NM 2001 7 31 USAA010744 1 20010615 A 5300 SKIN BOEING 737 7373B7 1384580 NM BS 556 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 524AU 43790 23859 PIT - FOUND SKIN CRACKED 6 INCHES BY 7 INCHES, FRAME STATION 556, STRINGER 5L. REPAIRED PCW, 6 INCHES BY 7 INCH DOUBLER INSTALLED PER SRM 53-00-01 FIG 202. (M) 2 L 7 2 4F RT A16WE 2001073100027 20010731 00027 NM 2001 7 31 USAA010743 1 20010615 A 5300 SKIN BOEING 737 7373B7 1384580 NM FS 580 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 524AU 43790 23859 PIT - FOUND SKIN CRACKED 5 INCHES BY 7 INCHES, FRAME STATION 580, S5L. REPAIR PCW, 5 INCHES BY 7 INCH DOUBLER INSTALLED PER SRM 53-00-01 FIG 202. (M) 2 L 7 2 4F RT A16WE 2001073100028 20010731 00028 NM 2001 7 31 USAA010710 1 20010517 A 5310 BULKHEAD BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND BULKHEAD CRACKED .125 INCH, STATION 178 BETWEEN LBL 5.7 AND 17. REPAIRED DOUBLER, FILLER PER SRM 53-10-08 P AGES 265-269. (M) 2 L 7 2 4F RT A16WE 2001073100029 20010731 00029 NM 2001 7 31 USAA010740 1 20010517 A 5300 FRAME BOEING 737 737301 1384611 NM BS 440 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND FRAME CRACKED .5 INCH, BS 440 AT STRINGER 8R. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER PER TYPICAL REPA IR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001073100030 20010731 00030 NM 2001 7 31 USAA010739 1 20010517 A 5300 CLIP BOEING 737 737301 1384611 NM BS 360 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND CLIP CRACKED .25 INCH, BS 360 AT S13L. FABRICATED, HEAT TREATED AND INSTALLED PER SRM 53-00-07 FIG 205. (M ) 2 L 7 2 4F RT A16WE 2001073100031 20010731 00031 NM 2001 7 31 USAA010738 1 20010517 A 5300 FRAME BOEING 737 737301 1384611 NM BS 440 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND FRAME CRACKED .25 INCH, BS 440 AT S8L. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 53-1 0-14. (M) 2 L 7 2 4F RT A16WE 2001073100032 20010731 00032 NM 2001 7 31 USAA010737 1 20010517 A 5300 FRAME BOEING 737 737301 1384611 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND FRAME CRACKED .25 INCH, BS 747 AT S8R. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 53-1 0-14. (M) 2 L 7 2 4F RT A16WE 2001073100033 20010731 00033 NM 2001 7 31 USAA010736 1 20010517 A 5300 FRAME BOEING 737 737301 1384611 NM BS 663 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND FRAME CRACKED .25 INCH, BS 663 AT S2L. CUT OUT DAMAGE, INSTALLED DOUBLER PER SRM 53-00-07 FIG 208, SRM 51-7 0-13, SRM 53-60-08, SRM 53-60-08. (M) 2 L 7 2 4F RT A16WE 2001073100034 20010731 00034 NM 2001 7 31 USAA010735 1 20010517 A 5300 SKIN BOEING 737 737301 1384611 NM BS 947 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND SKIN CRACKED .25 INCH, BS 947 AT STRINGER 11R. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-60-01. (M) 2 L 7 2 4F RT A16WE 2001073100035 20010731 00035 NM 2001 7 31 USAA010732 1 20010501 A 5300 FRAME BOEING 737 737301 1384611 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND FRAME CRACKED .75 INCH, BS 867 BETWEEN S8R AND S9R. CUT OUT DAMAGE AND INSTALLED DOUBLER PER TYPICAL REPAIR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001073100036 20010731 00036 NM 2001 7 31 USAA010731 1 20010501 A 5310 BEAM BOEING 737 737301 1384611 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND BEAM CRACKED 1 INCH, BS 867 BETWEEN S8L AND S9L. REMOVED DAMAGE, INSTALLED DOUBLER PER TYPICAL REPAIR 53-10 -14. (M) 2 L 7 2 4F RT A16WE 2001073100037 20010731 00037 NM 2001 7 31 USAA010730 1 20010502 A 5300 BELTFRAME BOEING 737 737301 1384611 NM BS 633 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND BELTFRAME CRACKED .25 INCH, STATION 633 S2L. INSTALLED DOUBLER PER 53-00-7 FIG 209. (M) 2 L 7 2 4F RT A16WE 2001073100038 20010731 00038 NM 2001 7 31 USAA010729 1 20010505 A 5300 BEAM BOEING 737 737301 1384611 NM BS 712 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND BEAM CRACKED .5 INCH, BL0 FLOORBEAM AT BS 712. MANUFACTURED AND INSTALLED FILLERS AND DOUBLER PER EA 71067 AND SRM 51-70-13. (M) 2 L 7 2 4F RT A16WE 2001073100039 20010731 00039 WP 2001 7 31 CA010626017 1 20010522 A 5230 1613510103 ACCESS PANEL LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE CARGO DOOR MISSING W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) AFTER ARRIVAL FROM CUN DURING THE ACCOMPLISMENT OF THE TRIP CHECK, MAINTENANCE DISCOVERED THE C2 CARGO DOOR MANUAL LOCK ACCESS PANEL LOWER HALF MISSING, BELIEVED THAT IT OPENED IN CUN BY GROUND HANDLERS AND NOT PROPERLY LATCHED. AIRCR AFT RELEASED AS PER CDL AND NEW ACCESS DOOR ORDERED. 2 L 7 3 4F 4 F A23WE E12EU 2001073100042 20010731 00042 NM 2001 7 31 CA010626021 1 20010510 A 2612 PIN BOEING 737 737201 1384454 NM PWA JT8 JT8D9A 52048 NE CONNECTOR BENT W A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CA (CAN) DURING CLIMB FIRE WARNING INDICATION WAS OBSERVED ON NR 2 ENGINE. AIRCRAFT RETURNING WITHOUT INCIDENT. UPPER & LOW ER FIRE LOOP WAS REPLACED ALONG WITH FIRE DETECTION UNIT. GROUND CHECKED SERVICEABLE. DURING SUBSEQUENT FLIGHT FIRE WARN ING INDICATION WAS OBSERVED. DURING INSPECTATION THE CANNON PLUG TO THE FIRE DETECTION UNIT IN THE PYLON WAS FOUND WITH A BENT PIN /ANOTHER PUSHED BACK CANNON PLUG WAS REPAIRED/CHECK SERVICABLE. NO FURTHER PROBLEMS DURING SUBSEQUENT FLIGHT. 2 L 7 2 4F 4 F A16WE E2EA 2001073100048 20010731 00048 NM 2001 7 31 CA010626038 1 20010511 A 2150 6806404 ACM BOEING 767 767375 NM GE CF6 CF680C2B6F 30025 NE RIGHT SEIZED W C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CA 8466 8466 (CAN) DURING TAKEOFF, THE COCKPIT/CABIN FILLED WITH SMOKE. AIR CONDITIONING SUSPECTED. AIRCRAFT RETURNED. DEFFERRED AS P ER MEL 21-51-07. RIGHT HAND ACM FOUND SEIZED. 2 L 7 2 4F 4 F RT A1NM E13NE 2001073100049 20010731 00049 2001 7 31 DHL2001365018 4 20010627 A 3140 75741034 COMPUTER AIRBUS 300 A300B4203 3930306 EU ENGINE MALFUNCTIONED A DHLA K NONE O OTHER CR CRUISE 1 SO 01 365DH 149 N1 COMPUTER SWITCHED FROM CR TO GA MODE AND KICKED OFF AUTO THROTTLE SYS. REPEATED BACK TO GA AFTER RESETTING TO CR AN D TO CL MODES. AFTER 5 MINUTES, SYSTEM REVERTED TO NORMAL OPERATION. REPLACED N1 LIMIT COMPUTER IAW M/M REF 31-42-11. OPS CHECKED GOOD AT THIS TIME. ALL P/N 757410-34, S/N OFF 148, S/N ON 56. 2 L 7 2 4F RT A35EU 2001073100051 20010731 00051 EU 2001 7 31 DHL2001366016 1 20010626 A 2611 WARNING LIGHT AIRBUS 300 A300B4203 3930306 EU COCKPIT ILLUMINATED A DHLA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 01 366DH 249 SMOKE LIGHT ANNUNCIATOR ON MWP ALONG WITH FORWARD RIGHT CABIN SMOKE LIGHT ON S/O PANEL ILLUMINATED. COMPLETED EMER CHEC KLIST PER EMER CHECK LIST IN AOM. RAN PACKS AT VARIOUS TEMP SETTINGS, PERFORMED TEST OF CABIN SMOKE DETECTION SYSTEM IA W M/M 26-14-00. NO DEFECTS NOTED, COULD NOT DUPLICATE. 2 L 7 2 4F RT A35EU 2001073100052 20010731 00052 EU 2001 7 31 DHL2001366017 1 20010630 A 3260 LIGHT AIRBUS 300 A300B4203 3930306 EU COCKPIT DEFECTIVE A DHLA K NONE O OTHER LD LANDING 1 SO 01 366DH 249 UPON LANDING GEAR EXTENSION NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE. PERFORMED ABNORMAL PROCEDURE PER AOM. CYCLED ANN UNCIATOR LIGHT DIM SWITCH AND LIGHT ILLUMINATED. RELAMPED NOSE GEAR GREEN LIGHT IAW MM 33-15-80. OP'S CK GOOD. 2 L 7 2 4F RT A35EU 2001073100053 20010731 00053 EU 2001 7 31 DHL2001366018 1 20010708 A 2120 DUCT AIRBUS 300 A300B4203 3930306 EU A/C BAY UNSECURE A DHLA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 366DH 249 CABIN SMOKE DETECTORS ILLUMINATED DURING TAXI. FOUND RT PACK SUPPLY DUCT UNSECURED AT MAIN DECK PLENUM DISCONNECT POINT . RESECURED SAME, PERFORMED OPERATIONAL CHECK OF CABIN SMOKE DETECTOR SYSTEM PER A300 M/M REF 26-14-00, NO FAULTS NOTED . 2 L 7 2 4F RT A35EU 2001073100054 20010731 00054 EU 2001 7 31 DHL2001367006 1 20010611 A 2710 VL35B1 ACTUATOR AIRBUS 300 A300B4203 3930306 EU AILERON FAILED A DHLA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 01 367DH 265 LOW SPEED AILERON WOULD NOT DISCONNECT AFTER TAKEOFF. COMPLETED ABNORMAL PROCEDURES AND AILERON STILL WOULD NOT DISCONN ECT. REMOVED AND REPLACED RT LOW SPEED ACTUATOR. OPS CHECKED GOOD PER MM 27-11-48. 2 L 7 2 4F RT A35EU 2001073100055 20010731 00055 EU 2001 7 31 DHL2001367007 1 20010626 A 2751 INDICATOR AIRBUS 300 A300B4203 3930306 EU COCKPIT FAULTY A DHLA A UNSCHED LANDING O OTHER UK UNKNOWN 1 SO 01 367DH 265 WITH FLAP/SLAT LEVER SELECTED TO 20/25 DEGREES FLAP INDEX INDICATED 17 DEGREES AND FLAP TAPE INDICATED ZERO DEGREES. AB NORMAL PROCEDURE 6.2.16 COMPLETED. REMOVED AND REPLACED FLAP / SLAT SPOILER INDICATOR, OPS NORMAL PER MM 27-55-1. 2 L 7 2 4F RT A35EU 2001073100059 20010731 00059 EU 2001 7 31 DHL2001367008 1 20010627 A 5730 SKIN AIRBUS 300 A300B4203 3930306 EU LT WING DENTED A DHLA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 367DH 265 FOUND DENT IN LT WING LOWER SKIN I/B OF RIB 19 AND FWD OF STRINGER 12. HFEC INSPECTION REQ ON WING SKIN I/B OF RIB 19 AN D FWD OF STR 12 (DENT AREA) AND STR 12 IN THE AREA OF THE DENT. TRANSFERRED TO DMI PER GMM 3.5 CAT 1, OK IAW AIRBUS CUS TOMER SERV DIRECTIVE 942-014499/002/2001 OK FOR 50 FLIGHT CYCLES CTRL 6223E INSTALLED HFEC INSP C/W IAW A300 NDTM 57-30- 11 S/N 0514 NO DEFECTS NOTED. SUP - DURING LOADING OF THE AIRCRAFT FOUND DENT IN LEFT WING LOWER SKIN I/B OF RIB 19 AND FWD OF STRINGER 12 CAUSED BY CARGO LOADER. SUP-1 FLAP PEEN AREA AT LT WING LWR SKIN I/B OF RIB 19 AND FRONT OF STRINGE R 12 IAW RAS/BAE 0618/2001 ISSUE A. SUP - 2, ALODINED BASE AREA AT LT WING LWR SKIN I/B OF RIB-19. 2 L 7 2 4F RT A35EU 2001073100062 20010731 00062 EU 2001 7 31 DHL2001367011 1 20010715 A 2611 WARNING LIGHT AIRBUS 300 A300B4203 3930306 EU COCKPIT ILLUMINATED A DHLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 367DH 265 UPON TAXI OUT, NUMEROUS SMOKE LIGHTS ILLUMINATED. FOUND MAIN CARGO DECK AT 90 DEGREES F AND MAIN DECK NOT LOADED TO FUL L CAPACITY. RAN ENGINES WITH BOTH PACKS ON FULL COLD FOR 45 MIN AND BROUGHT A/C UPPER DECK TO 80 DEGREES AND BELOW. OP S CHECK OF SMOKE DET. 2 L 7 2 4F RT A35EU 2001073100064 20010731 00064 2001 7 31 DHL2001702013 4 20010717 A 2210 AUTOPILOT SYS BOEING 727 72730C 1384009 NM COCKPIT INTERMITTENT A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 702DH 19793 AUTOPILOT ROLL CONTROL INTERMITTENT. WHEN MALFUNCTIONING AUTO PILOT ENGAGES AND ROLLS SHARPLY UNCOMMANDED. CANNOT DUPL ICATE, NO HISTORY. FOUND OPS CHECK GOOD ON GROUND IAW 727 MM 22-11-01. 2 L 7 3 4F A3WE 2001073100065 20010731 00065 EA 2001 7 31 CA010627009 1 20010627 A 2750 C3CF4187 ROD DHAV DHC3 DHC3 2800202 EA TE FLAPS WORN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) FLAP ROD WORN BETWEEN ROLLERS. 1 H 7 1 3R A815 2001101900084 20011019 00084 2001 10 19 DHL2001702014 4 20010717 A 2297 CONNECTOR BOEING 727 72730C 1384009 NM AUTOPILOT SYS CONTAMINATED A DHLA K NONE F FLT CONT AFFECTED NR NOT REPORTED 1 SO 01 702DH 19793 AUTOPILOT IS INOPERATIVE IN ALL ROLL MODES AIRCRAFT ROLLED HARD TO LEFT IN MANUAL MODE AND WAS UNRESPONSIVE TO INPUTS. C LEANED OXIDATION FROM ROLL SERVO CANNON PLUG CONTACTS. OPS CHECK OF AUTOPILOT GOOD PER MM 22-00. 2 L 7 3 4F A3WE 2001073100067 20010731 00067 NM 2001 7 31 DHL2001705513 1 20010415 A 5312 PRESSURE PANEL BOEING 727 72722C 138400F NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C-CHECK, NOSE GEAR WHEEL WELL RT SIDEWALL PANEL IS CRACKED BS 285.6 WL 158. CRACK RUNNING ALONG FAST ROWS-2 PLACES.- MRD 2. REMOVED FASTENERS AND PAINT AT NWW. RT SIDEWALL BS 285 WL 158 TO VERIFY CRACK ENDS AS PER B727 SRM 51-30-2. AC COMPLISHED HFEC INSP OF NWW RT SIDE WALL PANEL BS 285 WL 158 IAW B727 MANUAL NDT 51-00-00 PART 6 FIG 4. CRACKS VERIFIED AND MARKED ENDS OF CRACKS. CUT OUT DAMAGE SECTION 4.5 X 5.25 INCH AT NOSE GEAR WW RT WEB BS 285.6 AS OER B727 ACCORDAN CE TO S/B 727 -53-0065. ACCOMPLISHED HFEC INSP OF DAMAGE CUT-OUT SECT IAW B727 NDT MANUAL PART 6 51-00-00 FIG 4. NO FU RTHER CRACK PROGRESSION NOTED. FABRICATED EXTERNAL DOUBLER REPAIR AT NOSE WW RT. 2 L 7 3 4F A3WE 2001073100072 20010731 00072 NM 2001 7 31 DHL2001705544 1 20010613 A 5320 FITTING BOEING 727 72722C 138400F NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 ON LINE CHECK- BS 870 FITTING TO HORIZ BEAM RT WHEEL WELL SPLICE TEE IS CORRODED AT APPROX W/L 175. REMOVED SPLICE TEE AT BS 870 FITTING TO HORIZ BEAM RT W/W APPROX W/L 175 AS PER B-727 SRM 51-30-2. TRIMMED FITTING HORIZ FLANGES B/S 870 AP PROX W/L 175 AS PER BOEING DRAWING 65-78694. 2 L 7 3 4F A3WE 2001073100074 20010731 00074 NM 2001 7 31 DHL2001705545 1 20010614 A 5320 PLATE BOEING 727 72722C 138400F NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 ON LINE CHECK- BACK UP PLATE FOR INSPECTION HOLE AT STA 870 RBL 62 HAS CORROSION. REMOVED PRODUCTION DOUBLER AT STA 870 RBL 62 AND ACCESS PANEL. FABRICATED AND INSTALLED NEW PRODUCTION DOUBLER PER B-727 SRM 51-30-2 AND 53-10-1. 2 L 7 3 4F A3WE 2001073100076 20010731 00076 2001 7 31 DHL2001707007 4 20010608 A 2210 AUTOPILOT SYS BOEING 727 72722 1384002 NM COCKPIT MALFUNCTIONED A DHLA K NONE F FLT CONT AFFECTED DE DESCENT 1 SO 01 707DH 18321 WHEN OPERATING AUTOPILOT IN MANUAL MODE USING TURN MODE AUTOPILOT WILL NOT TURN RIGHT. ALL OTHER FUNCTIONS NORMAL. DEF FERED TO DMI 5936, PER MEL 22-1 CAT B, ITEM PLACARD. OPS CHECKED IAW MM 22-11-01, SYSTEM GROUND CHECKS GOOD. PER CREW COMMENT & B727 AUTO-PILOT WRITE UP GUIDE ACFT CKS GOOD IN FLT. THIS ACTION CLEARS DMI 5936. 2 L 7 3 4F A3WE 2001073100079 20010731 00079 NM 2001 7 31 DHL2001707008 1 20010621 A 3241 BRAKE BOEING 727 72722 1384002 NM MLG MALFUNCTIONED A DHLA K NONE O OTHER TO TAKEOFF 1 SO 01 707DH 18321 AT 38 DEGREES C IN SMF, ANTI-SKID REPEATEDLY RELEASED AS T/O THRUST WAS SET WITH BRAKES ON. FORWARD MOVEMENT OF ACFT WA S MINIMAL. DID NOT OBSERVE RELEASE LIGHTS (DID NOT LOOK). ANTI-SKID NORMAL ON LANDING. ANTI-SKID SYS IS DEFERRED PER M EL32-5, ASSIGNED DMI 6103 -SP32-5 APPLIES-INSPECTED BRAKES AND MLG WIRE HARNESS, RESEATED A/S CONTROL BOX. PERFORMED A/ S TEST PER MM 32-42-0. ALL CHECK OKAY CLEARED DMI 6103. 2 L 7 3 4F A3WE 2001073100081 20010731 00081 NM 2001 7 31 DHL2001708006 1 20010621 A 2730 401602723 COMPUTER BOEING 727 72725 1384006 NM ELEVATOR FAULTY A DHLA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 708DH 18275 DURING CRUISE FLT ELEVATOR FEEL DIFF PRESSURE LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURE. ELEVATOR FEEL DIFF PRES SURE LIGHT STAYED ILLUMINATED. REPLACED ELEVATOR FEEL COMPUTER PER MM REF 27-30-111. OPS CK GOOD. 2 L 7 3 4F A3WE 2001073100083 20010731 00083 NM 2001 7 31 DHL2001708007 1 20010706 A 2761 CONTROLLER BOEING 727 72725 1384006 NM SPOILER MALFUNCTIONED A DHLA K NONE F FLT CONT AFFECTED UK UNKNOWN 1 SO 01 708DH 18275 WHEN DEPLOYING FLIGHT SPOILERS AIRCRAFT ROLLS RT, WHEN STOWING FLIGHT SPOILERS AIRCRAFT ROLLS ABRUPTLY TO THE RT. INSPE CTED ALL SPOILERS FOR DELAM, NONE NOTED. NO ACTUATORS BYPASSING AND LIFT OFF NORMAL. PICK UP NORMAL A&B SYS PER MM 270 0. 2 L 7 3 4F A3WE 2001073100085 20010731 00085 2001 7 31 DHL2001709009 4 20010614 A 2210 AUTOPILOT SYS BOEING 727 72782C 1384026 NM COCKPIT MALFUNCTIONED A DHLA K NONE O OTHER CR CRUISE 1 SO 01 709DH 19968 AT FL350 WITH A/P ENGAGED AND ELEVATOR IN A OR B MODE, A/P PITCHES UP AND WILL NOT HOLD ALTITUDE. (BEGINS ALTITUDE OSCI LLATION AND OVER CORRECTS WITH TRIM). AUTOPILOT DEFERRED PER DHL MEL 22-1 CAT B, DMI 6023 PLACARD INSTALLED. COULD NOT DUPLICATE ON GROUND. SWAPPED CAPTS AND AUCX GYRO FOR TROUBLESHOOTING. OPS CHECKS GOOD IAW B727 MM 23-11-01 AND 34-22- 21. DMI 6023 CLEARED. 2 L 7 3 4F A3WE 2001073100086 20010731 00086 NM 2001 7 31 DHL2001712007 1 20010620 A 2720 POINTER BOEING 727 72729 1384007 NM COCKPIT OUT OF POSITION A DHLA K NONE O OTHER CL CLIMB 1 SO 01 712DH 19401 REQUIRED WRITE UP - AIRCRAFT REQUIRED 1.5 UNITS OF RIGHT TRIM ON RUDDER DURING CLIMBOUT. CRUISE AILERON TRIM 0. FOUND POINTER ON RUDDER TRIM KNOB JUMPED TRACK. CENTERED RUDDER, REINSTALLED TRIM KNOB PER 27-20-0 ADJ/TEST CKS GOOD. 2 L 7 3 4F A3WE 2001073100087 20010731 00087 2001 7 31 DHL2001715007 4 20010629 A 2211 COMPUTER BOEING 727 727155C 138404Z NM AUTOPILOT SYS FAULTY A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 715DH 19618 WITH AUTOPILOT A SERVO SELECTED, A/C PITCHES UP AND DOWN. OK WITH SERVO B SELECTED. DEFFERED AUTO PILOT A-MODE PER MEL 22-1-11A, CAT C, DMI 6211. PLACARDS INSTALLED. T/S SYS ORDERED PITCH COMPUTER. PARTS IN CVG AS PER MXC DMI 6211 CON TINUES. REMOVED AND REPLACED PITCH CONTROL CHANNEL PER M/M 22-11-121, OPS CK NORMAL. THIS CLEARS DMI 6211 PLACARD REMO VED. 2 L 7 3 4F A3WE 2001073100088 20010731 00088 NM 2001 7 31 DHL2001717009 1 20010627 A 5753 SKIN BOEING 727 72723 1384004 NM T/E FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 LEFT INBD MID FLAP HAS 2.5 INCH CRACK AFT (UPPER) AREA STA 251 JUST BELOW INBD FLAP GIMBLE ACCESS PANEL. REMOVED LT INB D FORE, MID AND AFT FLAP ASSYS IAW MM 27-51-1, 27-51-2 & 27-51-3 31499 OK TO INSTALL 8134 6/27/01. INSTALLED LEFT I/B FORE, MID AND AFT FLAP ASSY'S IAW M/M CHPT'S 27-51-1, 27-51-2, 27-51-3. PERFORMED RIG AND OPS CHECK OF FLAP SYSTEM (LEF T I/B ) OPS AND RIG CHECK GOOD.STATUS: CLOSED 2 L 7 3 4F A3WE 2001073100089 20010731 00089 NM 2001 7 31 DHL2001717010 1 20010703 A 3230 LOCK ACTUATOR BOEING 727 72723 1384004 NM NLG MALFUNCTIONED A DHLA L ABORTED APPROACH J WARNING INDICATION LD LANDING 1 SO 01 717DH 19389 NOSE WHEEL WOULD NOT EXTEND AND HAD TO BE MANUALLY EXTENDED C/W ABNORMAL PROCEDURE. REMOVED AND REPLACED NOSE GEAR LOCK ACTUATOR. RETRACTION CK GOOD IAW B727 MM 32-33-11 PAGE 401-403 RII. 2 L 7 3 4F A3WE 2001101900085 20011019 00085 NM 2001 10 19 DHL2001717013 1 20010711 A 3610 DUCT BOEING 727 72723 1384004 NM BLEED AIR SYS LEAKING A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 717DH 19389 ON CLIMB, LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED ABOUT 10,000 FT. WHILE RETURNING TO AIRPORT, LIGHT WENT OUT ABOUT 1 MIN AFTER GOING TO IDLE THRUST ON ALL ENGS. ACCOMPLISHED RESISTANCE CHECKS IN KEEL BEAM AREA READING 3 MOHMS, AFT STAI R AREA READING 4 MOHMS AFT CARGO PIT READING 3 MOHMS. RAN AIRCRAFT AND FOUND LEAK IN AFT CARGO PIT NR 1 ENG DUCT (CENTE R). 2 L 7 3 4F A3WE 2001073100090 20010731 00090 NM 2001 7 31 DHL2001717014 1 20010710 A 2613 INSULATOR BOEING 727 72723 1384004 NM OVERHEAT SYS OUT OF POSITION A DHLA K NONE N FALSE WARNING DE DESCENT 1 SO 01 717DH 19389 LOWER AFT BODY OVERHEAT ILLUMINATED IN FLT APPROX 10 SEC ON DESCENT INTO IAH. PRIOR TO ACCOMPLISHMENT OF ABNORMAL PROCE DURE LIGHT EXTINGUISHED. REPOSITIONED INSULATORS ON SECTION 48 LEFT DETECTOR ELEMENT. RAN ENGINES, BLEEDS, PACKS AND A NTI-ICE SYSTEMS. OP CKS GOOD IAW B727 MM 26-14 & DHL JRH. 2 L 7 3 4F A3WE 2001073100091 20010731 00091 NM 2001 7 31 DHL2001717015 1 20010716 A 2612 106087713 FIRE LOOP BOEING 727 72723 1384004 NM NR 1 ENGINE DEFECTIVE A DHLA K NONE L NO TEST UK UNKNOWN 1 SO 01 717DH 19389 NR 1 ENG FIRE WARNING WILL NOT TEST. REMOVED AND REPLACED NR 1 ENG FIRE LOOP AND PERFORMED ADJ/TEST PER 26-11-02 B727 M /M OPS CHECK SERVICEABLE P/N ON OFF 10-60877-13, S/N ON 58803, S/N OFF 59648. 2 L 7 3 4F A3WE 2001073100092 20010731 00092 NM 2001 7 31 DHL2001721004 1 20010627 A 2510 808737625 SEAT BOEING 727 727228 NM COCKPIT DEFECTIVE A DHLA K NONE O OTHER UK UNKNOWN 1 SO 01 721DH 19545 F/O SEAT BACK WILL NOT STAY LOCKED IN PLACE. WHEN WEIGHT OR PRESSURE IS PUT ON SEAT BACK, IT UNLOCKS AND MOVES TO FULL AFT (RECLINE) POSITION. F/O SEAT REMOVED AND REPLACED IAW M/M 25-10-42 OPS CK GOOD. OLD P/N 808737-619, OLD S/N 324, N EW P/N 808737-625, NEW S/N 293. 2 L 7 3 4F A3WE 2001073100093 20010731 00093 NM 2001 7 31 DHL2001724005 1 20010622 A 3040 WINDSHIELD WIPER BOEING 727 727228 NM RAIN REMOVAL SYS INOPERATIVE A DHLA K NONE L NO TEST UK UNKNOWN 1 SO 01 724DH 19862 F/O WINDSHIELD WIPER INOP IN MED AND INTERMITTENT IN HIGH. DEFERRED F/O WINDSHIELD WIPER SPEEDS MED AND HIGH PER MEL 30 -16-1 DMI 6122 PLACARDS INSTALLED. REMOVED AND REPLACED F/O WIPER ASSY IAW MM 30-42-11. OPERATIONAL CHECK OK. THIS CL EARS DMI 6122 PLACARD REMOVED. 2 L 7 3 4F A3WE 2001073100094 20010731 00094 NM 2001 7 31 DHL2001724006 1 20010628 A 2920 HYDRAULIC LINE BOEING 727 727228 NM HYDRAULIC SYS CHAFED A DHLA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 724DH 19862 HYDRAULIC SYS-B NR 2 PUMP LOW PRESS CAV LIGHT ILLUMINATED. ABNORMAL PROC ACCOMP. LIGHT REMAINED ON. B-SYSTEM HYD QTY GAUGE NEEDLE FLUX BETWEEN 1.80 AND FULL HYD PRESS. FOUND FLEX LINE CHAFED THROUGH ON NR 1 B-PUMP REM AND REP FLEX LINE, LK AND OPS CK GOOD IAW 727 MM 20-10-12. SERVICED HYDRAULICS AND B-SYS HEAD PRESSURE, OPS CK GOOD IAW 727 MM 12. 2 L 7 3 4F A3WE 2001073100095 20010731 00095 2001 7 31 DHL2001727020 4 20010622 A 2211 25858052 COMPUTER BOEING 727 727228 NM AUTOPILOT SYS DEFECTIVE A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 727DH 20204 AUTO PILOT BANKS 10 DEG LEFT IN MANUAL MODE WITH TURN KNOB IN LEVEL DETENT AND OCCASIONALLY BANKS HARD RIGHT IN SAME CON FIGURATION. NAV MODE WORKS NORMALLY. REMOVED AND REPLACED ROLL CHANNEL IAW BMM REF 22-11-1. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2001073100096 20010731 00096 2001 7 31 DHL2001727021 4 20010626 A 2211 COMPUTER BOEING 727 727228 NM AUTOPILOT SYS MALFUNCTIONED A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 727DH 20204 WHEN IN NAV/LOC MODE A/P CARRIES RIGHT WING 7 DEGREES LOW. WHEN DISENGAGING FROM NAV/LOC MODE TO MANUAL MODE, WINGS RAP IDLY RETURN TO LEVEL. RESEATED AUTOPILOT ROLL COMPUTER PER B-727 MM 22-11-111 AND RESEATED AUTOPILOT MODE CONTROL PANEL PER B-727 MM 22-11-181. PERFORMED BITE TEST PER B-727 MM 22-00 TO ROLL CHANNEL, CK GOOD. 2 L 7 3 4F A3WE 2001073100097 20010731 00097 NM 2001 7 31 DHL2001727022 1 20010711 A 2150 CONNECTOR BOEING 727 727228 NM RT A/C PACK LOOSE A DHLA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 01 727DH 20204 ON LANDING ELP RIGHT PACK TRIPPED OFF, CAUSED SMOKE IN COCKPIT. NOTE. FLIGHT TIMER ON GROUND CONTINUED TO RUN. SECURED RT PACK TEMP CONNECTOR. TIGHTENED PNEUMATIC DUCT FROM APU TO RT PACK. CLEANED Z-BAR PROXIMITY SENSORS. FLIGHT TIMER OPS CHECK GOOD. CHECK ENGINES AND PACKS FOR SMOKE, NONE FOUND IAW B727 MM 21-20-1. 2 L 7 3 4F A3WE 2001073100098 20010731 00098 2001 7 31 DHL2001741011 4 20010622 A 2211 4030951901 COMPUTER BOEING 727 7272Q9 138448M NM AUTOPILOT SYS DEFECTIVE A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 741DH 21931 WHILE THE AUTO PILOT WAS TURNING AIRCRAFT TOWARD HEADING BUG (APPROX 60 DEG TURN) THE AUTO PILOT PUT THE AIRCRAFT IN A 3 5 DEG TO 40 DEG BANKING TURN. REMOVED AND REPLACED ROLL CONTROL CHANNEL WITH SERVICEABLE PART IAW MM 22-11-101. OPS CH ECK GOOD ON GROUND. 2 L 7 3 4F RT A3WE 2001073100100 20010731 00100 NM 2001 7 31 DHL2001741012 1 20010620 A 5250 69415425 KNOB BOEING 727 7272Q9 138448M NM COCKPIT DOOR DEFECTIVE A DHLA K NONE O OTHER UK UNKNOWN 1 SO 01 741DH 21931 COCKPIT DOOR WILL NOT UNLOCK FROM OUTSIDE COCKPIT. REMOVED AND REPLACED COCKPIT DOOR KNOB IAW M/M 52-00. 2 L 7 3 4F RT A3WE 2001073100104 20010731 00104 NM 2001 7 31 DHL2001741518 1 20010319 A 5310 STOP FITTING BOEING 727 7272Q9 138448M NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 C2 CARGO DOOR FRAME LOWER AFT DOOR STOP HAS A CRACK INDICATION. REMOVED LOWER AFT DOOR STOP AND FASTENERS OF SEAL RETAI NERS FOR S/M ACCESS AS PER B727SRM 51-30-2. PERFORMED HFEC INSP PER B727NDT MANUAL PART 6 51-00-00 FIG 4 NO CRACK INDIC ATION FOUND. FABRICATED DOUBLER REPAIR AT C2 CARGO DOOR FRAME MAT USED 7075T6 .080, TREATED AND PRIMED AS PER B727 SRM 51-10-2. MAT USED PO 8318131 AND LOT 417911 SIZE OF REPAIR 15.25 X 4.25 INCH INSTALLED REPAIR ACCORDING TO SB727-53A019 9 PART 111 FIG 3. INSTALLED LOWER AFT DOOR STOP AND LOWER SEAL RETAINERS AS PER B727 SRM 51-30-2. SEAL WITH PRC AS PER B727 SRM 51-20-4. OPS CKECK AFT LOWER STOP CHECK GOOD MM 21-31-0. 2 L 7 3 4F RT A3WE 2001073100106 20010731 00106 NM 2001 7 31 DHL2001741519 1 20010616 A 5330 SKIN BOEING 727 7272Q9 138448M NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 ON LINE CHECK- IMPACT DAMAGE TO SKIN AT STA 1342 RIGHT SIDE NEAR AFT CORNER OF AIRSTAIRS APPROX WATERLINE STA 190. REMO VED FASTENERS AT SKIN AT STA 1342 RIGHT SIDE NEAR AFT CORNER OF AIRSTAIRS WATERLINE STA 190 APPROX PER B 727 SRM 51-30-2 TO GAIN ACCESS TO IMPACTED AREA. FOUND ATTACH ANGLES BENT AT STA 1342 RT AND WATERLINE STA 190, REWORKED FLANGE ANGLES PER B727 SRM 54-30-3. PERFORMED HFEC INSP PER B-727 NDT MANUAL PART 6-51-00-00 FIG 4. CRACK INDICATION FOUND ON SKIN SUPPORT ANGLE 2 INCHES LONG STOPPED DRILLED HOLES AT ENDS OF CRACK ON SUPPORT ANGLE PER B-727 SRM 51-10-1. CUT OUT DAMA GED UPPER LAYER OF BONDED SKIN AT STA 1342 AND WATERLINE STA 190 SIZE OF REMOVED SKIN 10 X 1 INCH. 2 L 7 3 4F RT A3WE 2001073100108 20010731 00108 NM 2001 7 31 DHL2001743009 1 20010616 A 2612 FIRE WARNING BOEING 727 727225 1384077 NM COCKPIT FALSE INDICATION A DHLA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 743DH 22438 AT ALTITUDE LOWER FWD CARGO FIRE WARNING SOUNDED, DISPLAY INDICATED FWD CARGO FIRE. CANCELLED BELL, LIGHT WENT OUT. FO LLOWED BY FWD INOP DISPLAY. DIVERTED OKLA. DEFERRED LOWER CARGO FIRE DETECTION / SUPPRESSION MX INDICATOR PER MEL 26-1 9-1A CAT B DMI 6054. 2 L 7 3 4F A3WE 2001073100113 20010731 00113 2001 7 31 DHL2001743010 4 20010616 A 3414 106092232 INDICATOR BOEING 727 727225 1384077 NM COCKPIT FAULTY A DHLA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 743DH 22438 AIRSPEED DIFFERS - CAPT 100 KTS, F/O'S 125 KTS. REPLACED F/O'S MACH AIRSPEED INDICATOR. 2 L 7 3 4F A3WE 2001073100115 20010731 00115 NM 2001 7 31 DHL2001743011 1 20010710 A 3260 LIGHT BOEING 727 727225 1384077 NM COCKPIT INOPERATIVE A DHLA K NONE N FALSE WARNING AP APPROACH 1 SO 01 743DH 22438 DURING GEAR EXTENSION INTO MCO, THE NOSE GEAR DOOR LIGHT DID NOT ILLUMINATE ON THE 2ND OFFICERS PANEL. THE NOSE GEAR LI GHT ON THE SECOND OFFICERS ANNUNCIATOR PANEL DURING LANDING GEAR EXTENSION AND RETRACTION DOES NOT ILLUMINATE PER DHL AO M CHP/SEC 26.21 PG 4 SEC 5. 2 L 7 3 4F A3WE 2001073100118 20010731 00118 NM 2001 7 31 DHL2001747 1 20010622 A 2780 SWITCH BOEING 727 727224 1384076 NM L/E SLAT FAILED A DHLA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 01 747DH 22253 NR 2 SLAT WOULD NOT RETRACT DURING FLAP RETRACTION. COMPLETED ABNORMAL PROCEDURES, PROBLEM STILL OCCURRED. RETURNED TO KTUS. REMOVED AND REPLACED SLAT SWITCH. OPS CHECK GOOD IAW 727 MM 27-81-00. 2 L 7 3 4F A3WE 2001073100119 20010731 00119 NM 2001 7 31 DHL2001747001 1 20010622 A 2780 SWITCH BOEING 727 727224 1384076 NM L/E SLAT FAILED A DHLA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 01 747DH 22253 NR 2 SLAT WOULD NOT RETRACT DURING FLAP RETRACTION. COMPLETED ABNORMAL PROCEDURES, PROBLEM STILL OCCURRED. RETURNED TO KTUS. REMOVED AND REPLACED SLAT SWITCH. OPS CHECK GOOD IAW 727 MM 27-81-00. 2 L 7 3 4F A3WE 2001073100123 20010731 00123 NM 2001 7 31 DHL2001747002 1 20010614 A 2612 FIRE LOOP BOEING 727 727224 1384076 NM NR 3 ENGINE OUT OF POSITION A DHLA K NONE N FALSE WARNING UK UNKNOWN 1 SO 01 747DH 22253 FIRE PROTECTION SYSTEM DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED ENG NR 3. REPOSITIONED FIRE LOOP REF B727 MM 26-11-12. 2 L 7 3 4F A3WE 2001073100124 20010731 00124 CE 2001 7 31 CA010628007 1 20010618 A 8012 3013109 CONTROLLER BEECH 99 99A 1154003 CE PWA PT6 PT6A28 EA HARTZL HCB3T HCB3TN3 GL STARTER OUT OF ADJ W O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 CA 2342 (CAN) SN 12348 START CONTROL WOULD CAUSE THE ENGINE TO POP ON START UP. UNIT REPLACED AND AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3T 4 T A14CE E4EA 6 C P15EA 2001073100125 20010731 00125 NM 2001 7 31 DHL2001747003 1 20010629 A 2612 FIRE LOOP BOEING 727 727224 1384076 NM NR 3 ENGINE OUT OF POSITION A DHLA K NONE N FALSE WARNING CR CRUISE 1 SO 01 747DH 22253 ENGINE NR 3 FIRE PROTECTION SYSTEM DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED IN FLIGHT HAS PREVIOUS WRITE UP ON 0 6/28/01. MEL 26-9-1 DMI 6209 ENG NR 3 FIRE PROTECTION SYSTEM DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED IN FLIGHT HAS P REVIOUSLY WRITE-UP ON 6-28-01. DEFERRED PER MEL 26-9-1 DMI 6209. MEL 26-9-1 DMI 6209 CLEANED AND REPOSITION NR 3 ENG F IRE LOOP TEST GOOD IAW DHL B727 MM 26-11-001. THIS CLEARS DMI 6209 PLACARD REMOVED. 2 L 7 3 4F A3WE 2001073100126 20010731 00126 CE 2001 7 31 CA010628008 1 20010628 A 5741 10140255S BOLT BEECH 99 B99 1154004 CE PWA PT6 PT6A28 EA HARTZL HCB3T HCB3TN3 GL WING FITTING DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 5720 5720 (CAN) DURING INSPECTION ON SPAR, WHEN BOLT WAS BEING INSTALLED IT WAS FOUND THAT AFTER FINAL TORQUE THE BOLT COULD STILL BETURNED QUITE EASILY. BOLT WAS REMOVED AND MAINTENANCE FOUND THAT THREADS WERE RAGGED AND CAUSING THE NUT TO BIND ON T HE BOLT. THIS IS THE SECOND CASE WE HAVE SEEN IN THE LAST 6 MONTHS. 1 L 7 2 3T 4 T A14CE E4EA 6 C P15EA 2001073100127 20010731 00127 CE 2001 7 31 CA010628009 1 20010618 A 5741 10140243S BOLT BEECH 99 B99 1154004 CE PWA PT6 PT6A28 EA HARTZL HCB3T HCB3TN3 GL RT WING FITTING DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 7583 7583 (CAN) DURING INSPECTION THE THREADS OF THE BOLTS WERE FOUND TO HAVE JOGGED THREADS. 1 L 7 2 3T 4 T A14CE E4EA 6 C P15EA 2001073100128 20010731 00128 NM 2001 7 31 DHL2001747004 1 20010630 A 2612 FIRE LOOP BOEING 727 727224 1384076 NM NR 3 ENGINE OUT OF POSITION A DHLA K NONE N FALSE WARNING CR CRUISE 1 SO 01 747DH 22253 ENG NR 3 FIRE PROTECTION SYS DETECTOR GROUND LIGHT ILLUMINATED IN FLIGHT. ENG NR 3 RE-POSITIONED FIRE LOOP IAW B-727 MM 26-11-000. 2 L 7 3 4F A3WE 2001073100129 20010731 00129 NM 2001 7 31 DHL2001747500 1 20010401 A 5753 SPAR BOEING 727 727200 138407E NM T/E FLAP CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK, LEFT OTBD T/E MID FLAP, MID SPAR HAS CORROSION NEAR INBD END CLOSE OUT R/O. CORROSION BEYOND LIMITS PER SRM 57 -50-2 (EXFOLIATED). REPAIR PER B727 SRM 51-40-4 FIG 1. REMOVED DAMAGED SECTION OF 'T' EXTRUSION PER 51-40-4 & 51-30-2. MATERIAL 2024-0 O.O71 PO 47255 PER INSTRUCTIONS. FABRICATED REPAIR ANGLES PER 51-40-4 FROM 2024 0.071. HEAT TREATED TO T4 PER CERTS, PO 90073. RECEIVED NEW T-EXTRUSION BAC 1505-100450 2024T3511 PO 89384; IAW SRM 57-50-2 PG 10 & 11. DR ILLED REPAIR PARTS (T-EXTRUSION & (2 EA) ANGLES) PER SRM 51-40-4 FIG 1, OKAY TO ALODINE AND PRIME. (REF N/R 1251-12-001 697) 2 L 7 3 4F RT A3WE 2001073100130 20010731 00130 NM 2001 7 31 DHL2001747501 1 20010402 A 5320 ANGLE BOEING 727 727200 138407E NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK - FWD CARGO STA 480, FS 560 - S26R ANGLE CRACKED. REMOVED CRACKED ANGLE PER SRM 51-30-2. FABRICATED NEW ANGLE FROM 7075 T6 0.050 PER SRM 51-10-5 & ORIGINAL. TREATED PER SRM 51-10-2 AND PRIMED PER 51-20-11. INSTALLED ANGLE PER SR M 51-30-2. (REF N/R 1252-90-001969) 2 L 7 3 4F RT A3WE 2001073100131 20010731 00131 NM 2001 7 31 DHL2001747502 1 20010405 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK - THE STA 360 FRAME AT STR L IS CRACKED. CUT OUT DAMAGE IN FRAME PER HAC DWG 2950 AND FABRICATED REPAIR DOUBLE RS AND FILLER. INSTALLED DOUBLERS, FILLER AND STRINGER CLIP PER HAC DWG 2950 AND 727 SRM 51-30-2 PG 14-14A. COMPLETED I AW EO 22253-01-002. (REF N/R 1252-90-001984) 2 L 7 3 4F RT A3WE 2001073100132 20010731 00132 NM 2001 7 31 DHL2001747503 1 20010321 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK - REMOVED AND REPLACED EXISTING REPAIR AT BS 1223 S26L. REPAIR PER SRM 53-30-3. FABRICATED AND LOCATED NEW REPA IR DOUBLER .HFEC IND NO CRACKS OR CORROSION FOUND. TREATED PARTS PER SRM 51-10-2 PG 3-4 AND PRIMED PER SOPM 20-41-02. INSTALLED PER SRM 53-30-3 FIG 25. 2 L 7 3 4F RT A3WE 2001073100133 20010731 00133 NM 2001 7 31 DHL2001747504 1 20010321 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK - REMOVED AND REPLACED EXISTING REPAIR AT BS 1223 S26R. REPAIR PER SRM 53-30-3. REMOVED EXISTING REPAIR AT STA 1223 S26R IAW SRM 51-30-2. FABRICATED NEW REPAIR DOUBLER IAW SRM 53-303 FIG 25. 2 L 7 3 4F RT A3WE 2001073100134 20010731 00134 NM 2001 7 31 DHL2001747505 1 20010320 A 5320 WEB BOEING 727 727200 138407E NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK - CORROSION JUST INBD OF RT AFT LAV DUMP HOLE IN FLOOR JUST FWD OF STA 1183. CUT OUT DAMAGED AREA AT FLOOR WEB PER B727 SRM 51-40-2 PG 1-6. FABRICATED AND LOCATED HOLES IN DOUBLER PLATE AND FILLER PER B727 SRM 51-40-2 PG 1-6. ALOD INED PER SRM 51-10-2 PG 1. PRIMED PARTS PER B727 SOPM 20-41-02 PG 1-20. (REF N/R 1252-02-001947) 2 L 7 3 4F RT A3WE 2001073100136 20010731 00136 NM 2001 7 31 DHL2001747506 1 20010320 A 5320 STRUCTURE BOEING 727 727200 138407E NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK, CORROSION ON LT AFT LAV FLOOR JUST INBD OF FRAME 1166 LT. REPAIR PER SRM REMOVED AND REPLACED MOP SILL. REMOV ED DAMAGED AREA PER 727 SRM 51-40-2. ALODINED PARTS PER 727 SRM 51-10-2. PRIMED REPAIR PARTS PER SOPM 20-41-2. INSTALL ED REPAIR PARTS (-2,-3 & SPACER SHIM) PER 727 SRM 51-40-2. 2 L 7 3 4F RT A3WE 2001073100137 20010731 00137 NM 2001 7 31 DHL2001747507 1 20010321 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK, FWD CARGO PIT ST 580 S 27L, FLOORBEAM CRACKED. REMOVED CRACKED AND DAMAGED PORTION OF Z-ANGLE IAW 51-10-04 FIG 4 PER SRM. ALODINED PER SRM 51-10-2. PRIMED PER SRM SOPM 20-41-02. INSTALLED PARTS PER SRM 53-10-5 FIG 4 SHEET 2 AND FASTENERS IAW SRM 51-30. 2 L 7 3 4F RT A3WE 2001073100140 20010731 00140 NM 2001 7 31 DHL2001747508 1 20010417 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK, REMOVE EXISTING REPAIR AT STA 950 STR 28R ON 950 CHORD BETWEEN STR 28-26R TO VERIFY IF REPAIR LEGAL WITH ANY DA TA THEN INSTALL APPROVED REPAIR. FABBED, LOCATED, DRILLED AND DEBURRED FILLER & TRIPPLER IAW 727 SRM 51-30-5. 2 L 7 3 4F RT A3WE 2001073100141 20010731 00141 CE 2001 7 31 CA010628022 1 20010518 A 5510 07326021232114 CHANNEL CESSNA 12330008 CESSNA 185 A185F 2072821 CE CONT O520 IO520D 17032 SO MCAULY 2A34C D2A34C58 GL STABILIZER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 2571 (CAN) PREVIOUS FILED SDR FOR CRACKED STABILIZER- HINGE REINFORCMENT P/N 0732101-4 AFTER REMOVAL OF THE REINFORCEMENT CH- RT WAS FOUND CRACK IN P/N 0732602-2/1232114-1 CRACK IN 07323603-1. LOWER RADIUS LT SIDE STA 6 INCH. LENGTH OF COACH I". 1 H 7 1 3O 3 O 3A24 E5CE 5 C P3EA 2001073100142 20010731 00142 NM 2001 7 31 DHL2001747509 1 20010313 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK, TOP CAP OF FLOORBEAM FS 400 RBL 18 HAS EXFOLIATED CORROSION ON BOTTOM-SIDE AT FLOORBOARD SCREW HOLE. ALODINED PER B727 SRM 51-10-2 PG 1. FABRICATED ANGLES -2 & -3 AND LOCATED HOLES PER B727 SRM 53-10-8 PG 44-48. ALODINED PER B727 SRM 51-10-2 PG 1. PRIMED ALL PARTS PER B727 SOPM 20-41-02 PG 1-20. 2 L 7 3 4F RT A3WE 2001073100143 20010731 00143 NM 2001 7 31 DHL2001747510 1 20010302 A 5347 SEAT TRACK BOEING 727 727200 138407E NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK, SEAT TRACK SECTION BETWEEN STA 1030-970 LBL 45.0 HAS AREAS OF SURFACE CORROSION 69-46, 47. REMOVED CORROSION I AW SRM 53-10-1 0.005 MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW SRM 53-10-01 FIG 3 SHT 5. ALODINED SEAT TRACK IAW SRM 51-10-2. PRIMED IAW SRM 51-40-5. 2 L 7 3 4F RT A3WE 2001073100145 20010731 00145 NM 2001 7 31 DHL2001747511 1 20010212 A 5347 SEAT TRACK BOEING 727 727200 138407E NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK, SEAT TRACK SECTION 930-870 LBL 45.5 HAS AREA OF SURFACE CORROSION. REMOVED FASTENERS ON SEAT TRACK TO CLEAN UP CORROSION PER SRM 51-30-2. CLEANED CORROSION ON SEAT TRACK PER SRM 51-10-6, SEAT TRACK WITHIN LIMITS IAW SRM 53-10-1 P G 15-16. ALODINE TREATED SEAT TRACK IAW 51-10-2 PG 1-2. REINSTALLED FASTENERS ON SEAT TRACK IAW 51-30-2. 2 L 7 3 4F RT A3WE 2001073100146 20010731 00146 NM 2001 7 31 DHL2001747513 1 20010222 A 5347 SEAT TRACK BOEING 727 727200 138407E NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK, SEAT TRACK SECTION STA 1034 AND FWD 1050-1070 RBL 22.45 CORRODED. SEAT TRACK IS VISUALLY OUT OF ALLOWABLE DAMA GE LIMITS AT FS 1040, 1053, AND 1060 RBL 22.45 PER SRM 53-10-1 FIG 3. 2 L 7 3 4F RT A3WE 2001073100147 20010731 00147 NM 2001 7 31 DHL2001747514 1 20010212 A 5320 FLOOR SUPPORT BOEING 727 727200 138407E NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK, FLOORBOARD SUPPORT AT APPROX STA 1034 RBL 22.45 CORRODED AROUND FASTENER HOLE. REMOVED CORROSION PER 51-10-6. 2 L 7 3 4F RT A3WE 2001073100148 20010731 00148 NM 2001 7 31 DHL2001747515 1 20010302 A 5347 SEAT TRACK BOEING 727 727200 138407E NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK - SEAT TRACK SECTION STA 970-870 HAS AREAS OF LIGHT CORROSION RBL 22.45. REMOVED CORROSION IAW SRM 53-10-1 0.005 . MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW SRM 53-10-01 FIG 3 SHT 5. ALODINED SEAT TRACK IAW SRM 51-10-2, PRIMED IA W SRM 51-40-5. 2 L 7 3 4F RT A3WE 2001073100149 20010731 00149 NM 2001 7 31 DHL2001747516 1 20010212 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK, STRINGER 16L STA 354.2-344 CRACKED. REMOVED DAMAGE ON INTERCOASTAL IAW SRM 51-40-2. INSTALLED REPAIR DOUBLER I AW SRM 51-40-2. 2 L 7 3 4F RT A3WE 2001073100150 20010731 00150 NM 2001 7 31 DHL2001747517 1 20010212 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK, STRINGER 15L STA 720B CRACKED. CUT OUT DAMAGED AREA OF STRINGER PER SRM 53-10-3 FIG 5. HFEC PER BOEING NDT PA RT 6, 51-00-00. INSTALLED REPAIR PARTS PER SRM 53-10-3 FIG 5. 2 L 7 3 4F RT A3WE 2001073100151 20010731 00151 NM 2001 7 31 DHL2001747519 1 20010212 A 5730 SKIN BOEING 727 727200 138407E NM LT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK, LEFT WING INBD L/E OF WING-TIP EXISTING REPAIR DAMAGED. REMOVED EXISTING FILLER REPAIRED MINOR DENT AND GOUGE IAW 727 SRM 51-40-01 PG 1-5. 2 L 7 3 4F RT A3WE 2001073100152 20010731 00152 NM 2001 7 31 DHL2001747520 1 20010212 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK, FLOORBEAM TOP CAP STA 1110 BL 0 CORRODED AROUND FASTENER HOLE. 2 L 7 3 4F RT A3WE 2001073100153 20010731 00153 NM 2001 7 31 DHL2001747522 1 20010322 A 5347 BAC1520792 SEAT TRACK BOEING 727 727200 138407E NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK, SEAT TRACK SECTION STA 680-520 RBL 22.45 HAS SURFACE CORROSION. TWO LUGS DAMAGED OUT OF LIMITS AT STA 530. FOU ND DEEP GOUGE IN TRACK OUT OF LIMITS. 2 L 7 3 4F RT A3WE 2001073100154 20010731 00154 NM 2001 7 31 DHL2001747523 1 20010222 A 5347 SEAT TRACK BOEING 727 727200 138407E NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK, SEAT TRACK SECTION STA 680-500 RBL 45.5 HAS SURFACE CORROSION. SEAT TRACK GOUGED AND OUT OF LIMIT, STA 665.SEA T TRACK FLANGE CORRODED. 2 L 7 3 4F RT A3WE 2001073100155 20010731 00155 SO 2001 7 31 CA010628025 2 20010615 A 8530 CLGIR VALVE GUIDE CONT CESSNA 172 172A 2072404 CE CONT O300 O300C 17022 SO MCAULY 1C172 1C172* GL CYLINDER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1198 (CAN) CYL REMOVED FOR LOW COMRESSION, DUE TO WORN VALVE GUIDE AND VALVE. 1 H 7 1 3O 3 O 3A12 E253 5 N P910 2001073100156 20010731 00156 EA 2001 7 31 CA010628026 2 20010628 A 8520 BEARING CESSNA 172 172C 2072408 CE FRNKLN 6AV335 6A335B 27020 EA MCAULY 2A31C 2A31C21 GL CRANKSHAFT FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA 200 (CAN) ON CLIMB OUT OF EVA LAKE ENGINE NOISE STARTED GETTING LOUDER AND WITHIN 10-15 SECONDS YOU COULD HEAR A METAL SCREE CHING SOUND. FOLLOWED BY A LOUD TAPPING THEN A FINAL BIG BANG WHEN ROD BROKE, CABIN FILLED WITH SMOKE. 1 H 7 1 3O 3 O NT 3A12 E244 5 C P919 2001073100157 20010731 00157 NM 2001 7 31 DHL2001747524 1 20010301 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK, SEAT TRACK STA 720D-700 RBL 45.5 HAS CORROSION. 2 L 7 3 4F A3WE 2001073100158 20010731 00158 NM 2001 7 31 DHL2001747525 1 20010313 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK, SEAT TRACK SECTION STA 850.95-760.95 RBL 45.5 HAS SURFACE CORROSION. REMOVED CORROSION ON SEAT TRACK SURFACE F ROM STA 850.95-760.95 RBL 45.5 IAW B727 SRM 51-10-1 PG 12-13. 2 L 7 3 4F A3WE 2001073100159 20010731 00159 NM 2001 7 31 DHL2001747526 1 20010306 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK, SEAT TRACK SECTION STA 950A-870 RBL 45.5 HAS SURFACE CORROSION. REMOVED CORROSION AT SEAT TRACK RBL 45.5 STA 8 70-950A. 2 L 7 3 4F A3WE 2001073100160 20010731 00160 NM 2001 7 31 DHL2001747527 1 20010215 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK, SEAT TRACK SECTION STA 990-950A RBL 45.5 HAS SURFACE CORROSION. REMOVED CORROSION ON SEAT TRACK RBL 45.5 STA 9 50A-990. 2 L 7 3 4F A3WE 2001073100161 20010731 00161 NM 2001 7 31 DHL2001747528 1 20010307 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK, SEAT TRACK SECTION STA 851.95 TO 870 RBL 45.5 HAS CORROSION ON INBOARD SECTION OF FLANGE AROUND FASTENER HEADS. 2 L 7 3 4F A3WE 2001073100162 20010731 00162 NM 2001 7 31 DHL2001747529 1 20010313 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK, BODY FRAME STA 930 STRINGER 14 UPPER FRAME LOWER SECTION CRACKED JUST BELOW RIVET. VERIFIED CRACK 0.75 INCH IN LENGTH. RUNNING INBD FROM EDGE OF FRAME. ALSO FOUND CRACK APPROX 1.5 INCH ABOVE AND OUTBD OF ORIGINAL CRACK RUNNING I NBD AND OUTBD OF FASTENER HOLE APPROX 0.25 INCH IN EACH DIRECTION. 2 L 7 3 4F A3WE 2001073100163 20010731 00163 NM 2001 7 31 DHL2001747530 1 20010227 A 5230 ANGLE BOEING 727 727224 1384076 NM CARGO DOOR CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK, C1 DOOR LOWER EDGE RIBS CORRODED AND DENTED. CORROSION PROGRESSES BENEATH LEVELING COMPOUND. REMOVED LEVELING COMPOUND AND 4 LOWER DOOR ANGLES IAW 727 SRM 51-30-2. ANGLE LOWER BEAM CORRODED. 2 L 7 3 4F A3WE 2001073100164 20010731 00164 EU 2001 7 31 CA010628027 1 20010522 A 5755 1386B000001 CONTROLLER AIRBUS 330 A330202 3930316 EU SPOILER SERVO MALFUNCTIONED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 4933 (CAN) ON APPROACH AT 400 FT AND WHEN AUTOPILOT DISCONNECTED THE AIRCRAFT EXPERIENCED A SIGNIFICANT LEFT ROLL WHICH REQUI RED COMPENSATING SIDE STICK INPUT FOR THE FLARE. ON TAXI IN, MAINTENANCE NOTED THE L/H SPOILER 5 DEPLOYED AND OPERATIONA L CHECK OF SPOILERS ELOYED ALL BUT THE NR 5 RT. BOTH LT AND RT NR 5 SPOILERS HAVE PREVIOUSLY BEEN DEACTIVATED DUE TO A M EL DEFERRRAL ON THE LT UNIT. THE ADPM DEACTIVATION PROCEDURE WAS CONFIRMED CARRIED OUT SATISFACTORY, BY PHYSICAL INSPECT ION ON BOTH NR 5 SPOILERS FOUND LT WOULD MOVE. MAINTENANCE REPLACED THE LT SPOILER SERVOCONTROL AND THE SYSTEM FUNCTION CHECKEDSATISFACTORY. 2 L 7 2 4F RT A46NM 2001073100165 20010731 00165 NM 2001 7 31 DHL2001747531 1 20010223 A 5330 SKIN BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK, FWD PIT CORROSION ON FUSELAGE SKIN S26L FS 720-FS 720A (BELOW TRANSITION PANEL). REMOVED CORROSION PER 51-10-6 . MARKED AREA AND CUT OUT DAMAGED PORTION OF UPPER AND LOWER SKIN PER 727 SRM 53-30-3 FIG 5. 2 L 7 3 4F A3WE 2001073100166 20010731 00166 NM 2001 7 31 DHL2001747532 1 20010222 A 5720 STIFFENER BOEING 727 727224 1384076 NM RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 C-CHECK, RT WING FWD UPPER AND LOWER SPAR STIFFENERS, RT & LT OF NR 5 L/E FLAP ACTUATOR HAVE MED CORROSION. 2 L 7 3 4F A3WE 2001073100167 20010731 00167 NM 2001 7 31 DHL2001747533 1 20010313 A 5320 ANGLE BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK, ANGLE CORRODED AFT OF STA 1166 BY LAV SERVICE DOOR AFT PIT. REMOVED AFT LAV SERVICE DOOR AND PAN IAW SRM 51-30 -2, REMOVED CORROSION PER SRM 51-10-6 ON L-ANGLE AND WEB. 2 L 7 3 4F A3WE 2001073100168 20010731 00168 NM 2001 7 31 DHL2001747534 1 20010222 A 5720 STIFFENER BOEING 727 727224 1384076 NM RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK, RT WING FWD SPAR STIFFENER HAS LIGHT CORROSION UNDERNEATH PRIMER, JUST OUTBOARD OF NR 5 FLAP ACTUATOR. 2 L 7 3 4F A3WE 2001073100169 20010731 00169 NM 2001 7 31 DHL2001747535 1 20010306 A 5314 KEELBEAM BOEING 727 727224 1384076 NM FUSELAGE GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK, KEEL BEAM LOWER CHORD INSIDE RT MLG W/W, GOUGED AND CHAFED BY MLG DOOR HINGE AT AFT HINGE AND FWD HINGE. 2 L 7 3 4F A3WE 2001073100170 20010731 00170 SW 2001 7 31 CA010628028 1 20010628 A 2750 12395 PULLEY BBAVIA 8 8GCBC 1220803 SW LYC O360 O360C2E 41514 EA MCAULY 1A200 1A200* GL FLAP SYSTEM SEIZED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ON 100 HR, INSPECTION TECHICIAN DISCOVERED 2 FLAP SYSTEM PULLEYS INSIDE FUSELAGE SEIZED AND FLATS WORN INTO THEM F ROM CABLE RUBBING. THIS IS AN ONGOING PROBLEM FOR US AS ALMOST EVERY 100 HR INSP. WE ARE FINDING THIS AND OFTEN HAVE TO CHANGE CABLES ALSO. PULLEYS ARE MADE OF SOLID ACUMINUM RIDING ON A STEEL INSERT WITH NO BEARING. EVEN WITH FREQUENT LUBR ICATION THE PROBLEM PERSISTS. MANHOURS TO REPAIR IS HIGH/DIFFICULT LOCATION TO WORK IN. 1 H 7 1 3O 3 O A21CE E286 5 N P874 2001073100171 20010731 00171 NM 2001 7 31 2001F00139 1 20010424 A 3350 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT ON THE SMOKE BARRIER WOULD NOT TEST. REMOVED AND REPLACED LI GHT ASSEMBLY AND BATTERY, THEN LIGHT OPERATED NORMALLY. REF ASAA0110230. (M) 2 L 7 2 4F A16WE 2001073100172 20010731 00172 NM 2001 7 31 2001F00141 1 20010501 A 5311 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 29SW 21340 FOUND LOWER FUSELAGE BS 663.75 LBL 25 INCHES WL 208 CHORD CRACKED. THE DAMAGED AREA WAS REPAIRED PER SB 737-53-1184. ( M) 2 L 7 2 4F A16WE 2001073100173 20010731 00173 NM 2001 7 31 2001F00142 1 20010501 A 5242 SKIN BOEING 737 7372H4 138448C NM E/E DOOR CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 29SW 21340 FOUND RIGHT AFT CORNER SKIN OF E/E COMPARTMENT DOOR HAS CRACK. THE DAMAGED AREA WAS REPAIRED IAW SRM 52-00-3 FIGURE 5. (M) 2 L 7 2 4F A16WE 2001073100174 20010731 00174 NM 2001 7 31 2001F00143 1 20010501 A 5320 SPLICE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 29SW 21340 FOUND PASSENGER CABIN BS 540, STRINGER 11R SPLICE HAS CRACK. THE PART WAS REPLACED IAW SRM 51-10-1 PAGE 8 AS RM 51-30-2 . (M) 2 L 7 2 4F A16WE 2001073100175 20010731 00175 NM 2001 7 31 2001F00144 1 20010501 A 5320 SPLICE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 29SW 21340 FOUND PASSENGER CABIN BS 540 STRINGER 11R SPLICE HAS CRACK. THE PART WAS REPLACED IAW SRM 51-10-1 PAGE 8 AND 51-30-2. (M) 2 L 7 2 4F A16WE 2001073100176 20010731 00176 NM 2001 7 31 2001F00145 1 20010526 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 29SW 21340 THE FUSELAGE SKIN AT BS 890 BETWEEN STRINGER 20R AND 21R WAS FOUND DENTED. THE DAMAGED AREA WAS REPAIRED IAW BOEING FAX COO-SJD-01-00392M DATED 6/11/2001. (M) 2 L 7 2 4F A16WE 2001073100177 20010731 00177 NM 2001 7 31 2001F00146 1 20010527 A 5315 BAC1518399 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 29SW 21340 FOUND PASSENGER CABIN, STATION 947 FLOORBEAM UPPER FLANGE CORRODED AT LBL 50. THE CORRODED FLOORBEAM SECTION WAS REMOVE D AND A NEW SECTION WAS INSTALLED IAW EO COO-3-53-233-01. (M) 2 L 7 2 4F A16WE 2001073100178 20010731 00178 NM 2001 7 31 2001F00147 1 20010501 A 5755 654645258 SKIN BOEING 737 7372H4 138448C NM SPOILER DELAMINATED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 29SW 21340 THE UPPER SKIN OF THE NR 5 SPOILER WAS FOUND DELAMINATED. THE DAMAGED AREA WAS REPAIRED IAW EO COO-CMP-3-57-248-01 DATE D JUNE 8-01. (M) 2 L 7 2 4F A16WE 2001073100179 20010731 00179 NM 2001 7 31 2001F00148 1 20010501 A 5755 654645258 SPOILER BOEING 737 7372H4 138448C NM WING DELAMINATED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 29SW 21340 THE GROUND SPOILER NR 4 WAS FOUND DELAMINATED IN SEVERAL PLACED. THE DAMAGED AREA WAS REPAIRED IAW EO COO-CMP-3-57-247- 01. (M) 2 L 7 2 4F A16WE 2001073100180 20010731 00180 NM 2001 7 31 ASAA0110113 1 20010228 A 5330 6573742 SKIN BOEING 737 737290C 138448V NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT BS 440-480, STRINGER 26R DENTED. (M) 2 L 7 2 4F A16WE 2001073100182 20010731 00182 SO 2001 7 31 CA010628030 2 20010628 A 8500 ENGINE CESSNA 180 180A 2072604 CE CONT O470 O470K 17026 SO NACELLE CONTAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA 870 870 (CAN) ENGINE LOST OIL PRESS AT NORMAL OPERATING RPM. FURTHER INSPECTION REVEALED CONTAMINATION IN OIL SCREENS, LOOSE ROD S, PROBABLE MAIN BEARING SHOT. ENGINE REPLACED IN A/C WITH FACTORY 1 H 7 1 3O 3 O 5A6 E273 2001073100183 20010731 00183 NM 2001 7 31 ASAA0110115 1 20010305 A 5320 6548283 INTERCOSTAL BOEING 737 737290C 138448V NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL AT BS 340-360, BUTTOCK LINE 0 WITH ELONGATED HOLES. (M) 2 L 7 2 4F A16WE 2001073100185 20010731 00185 NM 2001 7 31 USAA010765 1 20010619 A 5300 STRINGER BOEING 737 737201 1384454 NM BS 967 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 51038 22796 CLT - FOUDN STRINGER CORRODED 10 SQUARE INCHES, BS 967, STRINGER 27L. REMOVED AND REPLACED STRINGER SPLICE PER SRM 53-1 0-3, FIG 1. (M) 2 L 7 2 4F A16WE 2001073100186 20010731 00186 NM 2001 7 31 USAA010766 1 20010617 A 5300 SKIN BOEING 737 737201 1384454 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 51038 22796 TPA - FOUND SKIN CRACKED 1 INCH, BS 907, STRINGER 18L. DAMAGED REMOVED, REPAIR DOUBLER INSTALLED PER SRM 53-00-01, AND EA 7183. (M) 2 L 7 2 4F A16WE 2001073100187 20010731 00187 WP 2001 7 31 USAAD01136 1 20010711 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 91 802US 48036 BOS - THE AFT LOW LEVEL EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F A6WE 2001073100188 20010731 00188 EU 2001 7 31 USAAF01043 1 20010708 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU PAX CABIN FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 865US 11308 GSO - SEVERAL EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED A BATTERY PACK. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT 2001073100189 20010731 00189 NM 2001 7 31 USAASB01197 1 20010708 A 3350 20131A BATTERY BOEING 737 737301 1384611 NM INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 23234 DCA - FOUND MID-CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A16WE 2001073100190 20010731 00190 EU 2001 7 31 ASOA01097 1 20010626 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72 EU FUSELAGE INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 533AS 11409 460 DURING HANGAR MAINTENANCE IN MCN, EMERGENCY EXIT SIGN BY SERVICE DOOR WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND RE PLACED EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2001073100191 20010731 00191 SO 2001 7 31 ASOA01095 1 20010626 A 3350 03091022 CONNECTOR EMB 120 EMB120 3260201 SO CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 236AS 120049 DURNG HANGAR MAINTENANCE IN TXK, MAINTENANCE FOUND EMERGENCY TRACK LIGHTING INOPERATIVE AT ROW 1, 2 AND 6, 7. MAINTENAN CE REPAIRED FAULTY CONNECTIONS ON THE EMERGENCY TRACK LIGHTING. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001073100192 20010731 00192 EU 2001 7 31 ASOA01094 1 20010625 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72 EU CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 643AS 413 DURING HANGAR MAINTENANCE IN MCN, MAINTENANCE FOUND EMERGENCY LIGHT ON PAX DOOR INOPERATIVE. MAINTENANCE REMOVED AND RE PLACED THE EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2001073100193 20010731 00193 2001 7 31 HALA0100166 4 20010707 A 2200 COMPUTER DOUG DC10 DC1010 3022110 WP A HALA O OTHER O OTHER CL CLIMB 1 WP 13 153AA 46708 ATB - FLT 22 - DURING CLIMB-OUT AT 225 KTS WHEN RETRACTION SLATS, STICK SHAKER ACTIVATED. WE RE-EXTENDED THE SLATS AND STICK SHAKER STOPPED. NOTE SLAT RESET LIGHT STAYED ON. FOUND NR 2 AOA AND A/T S/C COMPUTER FAIL. REMOVED AND REPLACED NR 2 AOA AND A/T S/C COMPUTER PER M/M. SYSTEM BITE TEST OK. (M) 2 L 7 3 4F A22WE 2001073100194 20010731 00194 WP 2001 7 31 HALA0100163 1 20010707 A 3200 INDICATOR DOUG DC9 DC951 3022051 WP A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 674MC 47735 FLT 123 - HNL - AFTER DEPARTURE, NOSE GEAR WAS RETRACTED, NOSE GEAR UNSAFE LIGHT WAS ILLUMINATED. LOWERED GEAR AND HAD A GREEN LIGHT. RETURNED TO HONOLULU, WHERE AN UNEVENTFUL WAS MADE. REMOVED AND REPLACED MLG POSITION INDICATOR POSITIO N CONTROL BOX. NOSE GEAR SWING AND OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 2001073100195 20010731 00195 NM 2001 7 31 UIEA01072 1 20010711 A 5400 65B941383 FITTING BOEING 747 747243B 1384830 NM NR 1 PYLON CRACKED A UIEA O OTHER O OTHER IN INSP/MAINT 1 EA 15 518MC 23476 DURING INSPECTION, FOUND THE NR 1 PYLON STRUT TO DIAGONAL BRACE FITTING CRACKED IN THE COMMON RADIUS OF THE HORIZONTAL T O VERTICAL SUPPORT FLANGE ALONG WITH ONE SHEARED FASTENER. REMOVED PYLON, REMOVED FITTING, FOUND RADIUS FILLER NOT INST ALLED. PERFORMED HFEC OPEN HOLE INSPECTION FOR ADDITIONAL CRACKING. NO CRACKS FOUND. INSTALLED NEW FITTING AND SEAL B ACK UP PLATE IAW SB747-54A2208 AND 747-54A2196. REINSTALLED PYLON. (M) 2 L 7 4 4F A20WE 2001073100196 20010731 00196 NM 2001 7 31 UIEA01073 1 20010711 A 5400 65B941383 FITTING BOEING 747 747243B 1384830 NM NR 4 PYLON CRACKED A UIEA O OTHER O OTHER IN INSP/MAINT 1 EA 15 518MC 62573 23476 DURING INSPECTION, FOUND THE NR 4 PYLON STRUT TO DIAGONAL BRACE FITTING WITH ONE SHEARED FASTENER. OVERSIZED HOLE, HFEC OF OVERSIZED HOLE INDICATED A DEFECT IN THE ATTACH FITTING. REMOVED PYLON, REMOVED FITTING, FOUND RADIUS FILLER NOT IN STALLED. PERFORMED HFEC OPEN HOLE INSPECTION FOR ADDITIONAL CRACKING. NO CRACKS FOUND. INSTALLED NEW FITTING AND SEAL BACK-UP PLATE IAW SB747-54A2208 AND 747-54A2196. REINSTALLED PYLON. (M) 2 L 7 4 4F A20WE 2001073100197 20010731 00197 WP 2001 7 31 AALA20011317 1 20010629 A 2600 5938323 DETECTOR DOUG DC9 DC983 3022083 WP NR 2 ENGINE DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 591AA 53254 DFW - FLT 395 - EN ROUTE DFW-YVR - ON CLIMB-OUT, RIGHT SIDE FIRE WARNING LIGHT, BELL, AND AURAL CAME ON. ACCOMPLISHED E NGINE SHUTDOWN PROCEDURES. RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED FIRE LOOP ASSEMBLY AND CONNECTOR . ACCOMPLISHED FUNCTIONAL CHECKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001073100198 20010731 00198 WP 2001 7 31 AALA20011341 1 20010620 A 5300 LONGERON DOUG DC9 DC982 3022082 WP FS 160 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7521A 49898 TUL - FOUND L4L HAS A CRACK AROUND FASTENERS AT STATION 160. INSTALLED NEW LONGERON AND LONGERON SPLICE PER SRM 53-02 F IG 18. (M) 2 L 7 2 4F A6WE 2001073100199 20010731 00199 WP 2001 7 31 AALA20011359 1 20010626 A 5300 SKIN DOUG DC9 DC982 3022082 WP FS 218 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7521A 49898 TUL - FOUND DENT ON LEFT SIDE OF AIRCRAFT BELOW FIRST PLUGGED WINDOW, APPROX 3 FEET BELOW RED STRIPE. CUT OUT ONE INCH HOLE TO REMOVE DAMAGE AND INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M) 2 L 7 2 4F A6WE 2001073100200 20010731 00200 WP 2001 7 31 AALA20011358 1 20010625 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7521A 49898 TUL - FOUND FLOORBEAM HAS CORROSION IN LAVATORY PAN HOLES STATION 1322 RIGHT AFT LAVATORY. REMOVED CORROSION PER SRM 51 -10-3. INSTALLED REPAIR PER ESO 80559 DATED 6-22-2001. (M) 2 L 7 2 4F A6WE 2001073100201 20010731 00201 WP 2001 7 31 AALA20011357 1 20010626 A 5300 FRAME DOUG DC9 DC982 3022082 WP FS 1485 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7521A 49898 TUL - FOUND FRAME 1485 IS CRACKED ON RIGHT SIDE OF STAIRS CUTOUT AT STAIR ACT CASTING. CUT OUT DAMAGED SECTION OF FRAME . INSTALLED REPAIR AS PER AARD 53-10-00-33. (M) 2 L 7 2 4F A6WE 2001073100202 20010731 00202 WP 2001 7 31 AALA20011355 1 20010619 A 5300 SKIN DOUG DC9 DC982 3022082 WP FS 218 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7521A 49898 TUL - FOUND FUSELAGE SKIN DAMAGED WITH TEMPORARY REPAIR AT STATION 218 BETWEEN LONGERON 21L AND 23L. INSTALLED DOUBLER PER SRM 53-04 FIG 12B SHEET 3. (M) 2 L 7 2 4F A6WE 2001073100203 20010731 00203 WP 2001 7 31 AALA20011347 1 20010616 A 5322 SHEAR TIE DOUG DC9 DC982 3022082 WP FS 1437 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7521A 49898 TUL - FOUND SHEAR TIE CRACKED STATION 1437 BETWEEN LONGERON 3 LEFT AND 4 LEFT. REMOVED AND REPLACED SHEAR TIE PER SRM 5 1-01. (M) 2 L 7 2 4F A6WE 2001073100204 20010731 00204 NM 2001 7 31 ASAA0110116 1 20010305 A 5311 6546259501 FRAME BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 440, STRINGER 26R CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001073100206 20010731 00206 NM 2001 7 31 ASAA0110122 1 20010314 A 5320 693535214 CLIP BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 727B, LBL 6 CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001073100207 20010731 00207 NM 2001 7 31 ASAA0110123 1 20010314 A 5320 STRINGER CLIP BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 787, LBL 16 CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001073100208 20010731 00208 NM 2001 7 31 ASAA0110124 1 20010314 A 5320 693535214 STRINGER CLIP BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 747, RBL 6 CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001073100209 20010731 00209 NM 2001 7 31 ASAA0110125 1 20010314 A 5320 693535214 STRINGER CLIP BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 747, RBL 7 CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001073100210 20010731 00210 NM 2001 7 31 ASAA0110126 1 20010314 A 5320 693535214 STRINGER CLIP BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP BS 727B, RBL 9 CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001073100211 20010731 00211 NM 2001 7 31 ASAA0110127 1 20010314 A 5320 693535214 STRINGER CLIP BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 727B, RBL 7 CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001073100212 20010731 00212 NM 2001 7 31 ASAA0110128 1 20010314 A 5320 693535214 STRINGER CLIP BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 727A, RBL 8 CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001073100214 20010731 00214 NM 2001 7 31 ASAA0110129 1 20010314 A 5320 693535214 STRINGER CLIP BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 616, RBL 6 CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001073100216 20010731 00216 NM 2001 7 31 ASAA0110130 1 20010314 A 5320 693535214 STRINGER CLIP BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 597, RBL 8 CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001073100218 20010731 00218 NM 2001 7 31 ASAA0110131 1 20010314 A 5320 693535214 STRINGER CLIP BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 597, RBL 5 CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001073100219 20010731 00219 NM 2001 7 31 ASAA0110132 1 20010314 A 5320 693535214 STRINGER CLIP BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 578, RBL 8 CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001073100221 20010731 00221 NM 2001 7 31 ASAA0110133 1 20010314 A 5320 693535214 STRINGER CLIP BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 639, LBL 4 CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001073100222 20010731 00222 NM 2001 7 31 ASAA0110134 1 20010314 A 5320 655496080 SPLICE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND SHEAR TIE SPLICE STRAP AT BS 360-372, STRINGER 28L CORRODED. REPAIRED PER SRM. ( M) 2 L 7 2 4F A16WE 2001073100223 20010731 00223 NM 2001 7 31 ASAA0110135 1 20010320 A 5310 6546563 SHEAR TIE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 727B, STRINGER 26L-28L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001073100224 20010731 00224 NM 2001 7 31 ASAA0110137 1 20010320 A 5320 BAC15201397 FLOOR SUPPORT BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT ANGLE AT BS 767, STRINGER 27R CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001073100225 20010731 00225 NM 2001 7 31 ASAA0110139 1 20010321 A 5320 BAC15201397 FLOOR SUPPORT BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND FLOORBOARD SUPPORT TRACK AT BS 737-874, STRINGER 27L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001073100226 20010731 00226 NM 2001 7 31 ASAA0110140 1 20010321 A 5320 BAC15201397 FLOOR SUPPORT BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND FLOORBOARD SUPPORT TRACK AT BS 737-947, LEFT BUTTOCK LINE 10 CORRODED. REPAIRED P ER SRM. (M) 2 L 7 2 4F A16WE 2001073100227 20010731 00227 NM 2001 7 31 ASAA0110141 1 20010321 A 5320 65557966 ANGLE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND ANGLE AT BS 357, LBL 15 CORRODED. REMOVED, FABRICATED AND REPLACED ANGLE PER BOEI NG DRAWING. (M) 2 L 7 2 4F A16WE 2001073100228 20010731 00228 NM 2001 7 31 ASAA0110142 1 20010321 A 5320 6545833154 FLOOR SUPPORT BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT AT BS 270-277, RBL 11 CORRODED. REMOVED, FABRICATED AND REPLACED FL OOR SUPPORT PER BOEING DRAWING. (M) 2 L 7 2 4F A16WE 2001073100229 20010731 00229 NM 2001 7 31 ASAA0110143 1 20010321 A 5320 65549061 STRAP BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND STRAP AT BS 500, BL 0 TO LBL 55 CORRODED. (M) 2 L 7 2 4F A16WE 2001073100230 20010731 00230 NM 2001 7 31 ASAA0110144 1 20010321 A 5315 65549052 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 420, BL 0 TO LBL 55 CORRODED. REPAIRED PER EA. (M) 2 L 7 2 4F A16WE 2001073100231 20010731 00231 NM 2001 7 31 ASAA0110145 1 20010321 A 5330 6545778 SKIN PANEL BOEING 737 737290C 138448V NM FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND EXTERIOR SKIN PANEL HAS A DEEP CHAFE MARK AT BS 794 NEAR THE AFT DOOR EDGE. REPAI RED PER SRM. (M) 2 L 7 2 4F A16WE 2001073100232 20010731 00232 NM 2001 7 31 ASAA0110149 1 20010322 A 5315 65549063 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 500B, BL 0 - LBL 55 CORRODED. REPAIRED PER EA. (M) 2 L 7 2 4F A16WE 2001073100233 20010731 00233 NM 2001 7 31 ASAA0110152 1 20010326 A 5320 69514718 CLIP BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND SHEAR CLIP AT BS 360, STRINGER 26L-27L CORRODED. REPAIRED PER BOEING DRAWING. (M ) 2 L 7 2 4F A16WE 2001073100234 20010731 00234 NM 2001 7 31 ASAA0110153 1 20010326 A 5320 65458335 FLOOR SUPPORT BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT AT BS 270, LBL 11, RBL 11 CORRODED. REPAIRED PER BOEING DRAWING. ( M) 2 L 7 2 4F A16WE 2001073100235 20010731 00235 NM 2001 7 31 ASAA0110154 1 20010326 A 5313 6545800118 STRINGER BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER 26R AT BS 270, CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001073100236 20010731 00236 CE 2001 7 31 CA010628047 1 20010528 A 2612 HARNESS BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA FIRE DETECTION MISMANUFACTURED W E A ENGINE SHUTDOWN UNSCHED LANDING W N INADEQUATE Q C FALSE WARNING NR NOT REPORTED 1 CA 15754 (CAN) AFTER A FALSE FIRE WARNING. ENGINE WAS SHUTDOWN. WHILE TROUBLESHOOTING. FOUND POWER FOR AUTO IGNITION SYSTEM WAS BLEEDING THROUGH WET WIRE INSULATION & INTO FIRE DETECT SYSTEM THROUGH IT'S WIRE INSULATION. THIS TOOK PLACE IN MAIN WIR E BUNDLE FOR RT ENG. FWD OF FIRE WALL. WIRES WERE DRIED & TEMPORARILY REPAIRED WITH SHRINK TUBE & SYSTEMS WERE TESTED. F URTHER INVEST. ON AN OTHER BEECH A100 S/N B152: FOUND THAT WITH A METER IN DRY WIRE BUNDLE THERE WERE NO VOLTAGE, WHEN W IRE BUNDLE WAS SPRAYED WITH WATER. I COULD GET AS HIGH AS 8. UDC SEEPING THROUGH INSULATION OF WIRES. AUTO IGNITION & FI RE DETECT WIRES ARE SAME TYPE OF WIRE WITH OUTER BRAID FOR HEAT. 1 L 7 2 3T 4 T A14CE E4EA 2001073100238 20010731 00238 NM 2001 7 31 ASAA0110155 1 20010326 A 5320 693537213 ANGLE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND TEE CAP ATTACHING ANGLE AT BS 312, STRINGER 27L-28L CORRODED. REPAIRED PER BOEING DRAWING. (M) 2 L 7 2 4F A16WE 2001073100239 20010731 00239 NM 2001 7 31 CA010628054 1 20010529 A 3242 211473 KEY BOEING 727 727243 138408D NM PWA JT8 JT8D15 52051 NE BRAKE ASSY MISSING W K NONE O OTHER IN INSP/MAINT 1 CA 204 (CAN) ON SERVICE CHECK INSPECTION NR 2 MAIN GEAR BRAKE ASSY, PISTON HOUSING FOUND DAMAGED BEYOND LIMITS DUE TO NR 2 MAIN WHEEL ASSY. MISSING A BRAKE KEY. NR 2 MAIN GEAR BRAKE ASSY AND NR 2 MAIN WHEEL ASSY REPLACED IN ACCORDANCE WITH MAINTEN ANCE MANUAL. NO FURTHER DEFECTS NOTED IN THE LAST FIVE FLIGHT LEGS. 2 L 7 3 4F 4 F RT A3WE E2EA 2001073100240 20010731 00240 GL 2001 7 31 CA010628056 3 20010607 A 6114 BOLT HCB3TN3DY DHAV DHC3 DHC3 2800202 EA PWA PT6 PT6A135 52043 NE HARTZL HCB3T HCB3TN3 GL LATCH SHEARED W O OTHER O OTHER TX TAXI/GRND HDL 1 CA BUA21735 (CAN) UPON COMPLETION OF THE FLIGHT THE PILOT SHUT DOWN THE ENGINE WITH THE PROPELLOR ON ZERO PITCH. AFTER THE ENGINE HA D COMPLETELY SHUT DOWN AND STOPPED THE PILOT FOUND THAT THE PROPELLER HAD MOVED TOWARDTHE FEATHER POSITION RATHER THAN S TAYING IN THE ZERO PITCH LOCK POSITION. UPON INVESTIGATING THE ENGINEER FOUND THAT ONE OF THE BOLTS HAD SHEARD ON EACH O F THE 3 ZERO PITCH LATCHES. THE PROPELLOR AND CONTROL SYSTEM WAS INSPECTED FOR OTHER DAMAGE NONE WAS FOUND. THE ZERO PIT CH LATCH SYSTEM WAS REMOVED FROM THE PROPELLER HAS NOT CAUSED ANY FURTHER INTERFERENCE AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 H 7 1 3R 4 T A815 E4EA 6 C P15EA 2001073100241 20010731 00241 CE 2001 7 31 CA010628057 1 20010628 A 2612 473275 FIRE DETECTOR BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA HARTZL HCB4T HCB4TN3 GL LT ENGINE MALFUNCTIONED W A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CA (CAN) PILOT SHUT DOWN LT ENGINE DUE TO FIRE LIGHT "ON". AIRCRAFT LANDED AND IT WAS CONFIRMED THAT THERE WAS NO FIRE. NR 2 FLAME DETECTOR WAS FOUND AT FAULT. UNIT REPLACED AND AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3T 4 T A14CE E4EA 6 C P40EA 2001073100242 20010731 00242 WP 2001 7 31 CA010628058 2 20010531 A 7210 31039772 IDLER GEAR SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE GEARBOX FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 2149 2149 (CAN) ACCESSORY IDLER GEAR ASSY, SER NR OP-23704CA WAS REMVD AT HOT SECTION INSP/GEAR BOX INSP DUE TO IDLER GEAR FOUND R UBBING ON ACCESSORY IDLER GEAR HOUSING. BACK FACE OF GEAR IS CONTACTING HOUSING. IT APPEARS THAT THRUST FEATURE OF 2 INT EGRAL OF 2 INTEGRAL BEARIINGS HAS FAILED. THIS PART HAS ONLY 2149 HRS TSN. THIS IDLER GEAR ASSY ISTHE LATEST PART CONFIG AS PER HONEYWELL ALERT SB- A72-0998. SUSPECT INTERNAL BEARINGS ARE PART NO 3108041-2. HONEYWELL'S MAINT MANUAL HAS NO C RITERIA ON HOW TO REMOVEAND INSPECT THESE BEARINGS. AN INSP & REPL PROC WAS AVAILABLE FOR OLDER STYLE ACCESSORY IDLER GE AR ASSY...PMI ISSUE. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 2001073100243 20010731 00243 NM 2001 7 31 ASAA0110238 1 20010428 A 3350 873203041 CONTROL UNIT BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS IN THE MID CABIN INOPERATIVE. REMOVED AND REPLACED CONTROL MODULE, THEN LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 2001073100245 20010731 00245 NM 2001 7 31 ASAA0110304 1 20010524 A 5210 6529994 GUIDE BOEING 737 737210C 1384459 NM L1 DOOR OUT OF ADJ A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 ANC - DURING MAINTENANCE CHECK, FOUND L1 DOOR DIFFICULT TO CLOSE. ADJUSTED GUIDE ARM AND DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2001073100246 20010731 00246 NM 2001 7 31 ASAA0110316 1 20010531 A 5313 6552928103 STRINGER BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER 27R AT BS 490, CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001073100247 20010731 00247 NM 2001 7 31 ASAA0110321 1 20010608 A 5311 6546532515 FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 480, STRINGER 2R CRACKED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2001073100248 20010731 00248 NM 2001 7 31 ASAA0110322 1 20010608 A 5311 651758348 FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND CHORD AT BS 178, WATERLINE 184 CRACKED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2001073100250 20010731 00250 NM 2001 7 31 ASAA0110323 1 20010608 A 5312 6516300510 BULKHEAD BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND WEB AT BS 178, WATERLINE 234 CRACKED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2001073100252 20010731 00252 NM 2001 7 31 ASAA0110324 1 20010608 A 5312 6516300510 BULKHEAD BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND WEB AT BS 178, WATERLINE 218 CRACKED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2001073100253 20010731 00253 NM 2001 7 31 ASAA0110325 1 20010608 A 5311 651630086 FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND CHORD AT BS 178, WATERLINE 207 CRACKED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2001073100255 20010731 00255 NM 2001 7 31 ASAA0110326 1 20010608 A 5311 651630087 FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND CHORD AT BS 178, WATERLINE 195-207 CRACKED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2001073100257 20010731 00257 NM 2001 7 31 ASAA0110327 1 20010608 A 5330 654577870 SKIN PANEL BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND SKIN PANEL AT BS 951, WATERLINE 246 CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001073100258 20010731 00258 NM 2001 7 31 ASAA0110328 1 20010608 A 5330 654577246 SKIN PANEL BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND SKIN PANEL FASTENER HOLE AT BS 835, WATERLINE 299 DAMAGED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2001073100260 20010731 00260 NM 2001 7 31 ASAA0110410 1 20010620 A 5320 69514763 INTERCOSTAL BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL LINK AT BS 520-540, LBL 45 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001073100262 20010731 00262 NM 2001 7 31 ASAA0110412 1 20010622 A 5320 6936675502 ATTACH ANGLE BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND ATTACH ANGLE AT BS 480, RBL 74 HAS ELONGATED HOLES. REPAIRED PER BOEING DRAWING. (M) 2 L 7 2 4F RT A16WE 2001073100266 20010731 00266 NM 2001 7 31 ASAA0110413 1 20010622 A 5310 6546563 SHEAR TIE BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 927, STRINGER 27L-27R CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001073100269 20010731 00269 EU 2001 7 31 CA010629030 1 20010511 A 2432 9717516104 CONNECTOR PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL BATTERY DIRTY W H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 CA 1401 (CAN) CRUISE ON HOMEWARD LEG OF FLT PILOT NOTICED ON OV ERHEAD ELECTICAL PANEL THAT BATTERY NR 2 DISPLAY WAS INDICATING A DECREASING VOLTAGE WITH AN INCREASING NEGATIVE AMPS. GEN. NR 2 IND WAS INDICATING A VIRTUAL ZERO AMPS WITH A 29.3 VOLT S. WITH NO OTHER WARNINGS INDICATED PILOT DECIDED TO EIMINATE NR 2 BATTERY BY SWITCHING OFF NR 2 BATTERY MASTER SWITCH. UPONRETURN ING TO BASE A RUNUP WAS CONDUCTED & IT WAS DETERMINED THAT 32 GEN MUST NOT BE ON LINE IN SYS VIA NR 2 GEN REL AY. CONNECTOR WAS REMVD FROM RELAY (PILATUS P/N 9717516104 & WAS CLEAED WITH A CONTACT CLEANER & RE-ATTACHED, POST RUNU P INDICATED THAT ALL SYSS WERE NOW FUNCTIONING PROPERLY. MULTIPLE ATTEM 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001073100270 20010731 00270 EU 2001 7 31 CA010629031 1 20010412 A 2434 HED60CR132200 BRUSHES 5243212158 PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL GENERATOR WORN W K NONE O OTHER IN INSP/MAINT 1 CA 207 207 100049 (CAN) DUE TO PREMATURE WEAR OF NR 2 GEN BRUSHED PILATUS ISSD A S/B (S/B 24-016) TO ADDR ISSUE BY INTRODUCING A NEW LONGE R WEARING BRUSH BLOCK ASSY WHICH IS FIELD REPLABLE. PRIOR TO THE S/B WE FOUND BRUSHES ON ORIGLY INST GEN S/N 100092 WITH .686.2 TAT HRS WAS VERY WORN & CAUSED AN OFFLINE SITUATION. GEN WAS REPLD WITH S/N 100049. AT 1124.2 TAT (778 CYC) GEN S/N 100049 BRUSHES WERE REPLD DUE TO WORN AS PER S/B 24-016. AS A RESULT OF OPERATOR INPUT, PER FAILURE RATE OF THESE BR USHES IT WAS DECIDED TO CHECK THESE BRUSHED AT AROUND 200HRS IN S ERVICE. THESE BRUSHES WERE FOUND TO BE EXTERMELY WORN & ON POINT OF FAILURE: THIS BRUSH ASSY WAS INSERVICE FOR 207HRS 144 CYC. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001073100275 20010731 00275 NM 2001 7 31 ASAA0110415 1 20010622 A 5320 6546531 ANGLE BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND ANGLE AT BS 440, STRINGER 27R DAMAGED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001073100276 20010731 00276 NM 2001 7 31 ASAA0140060 1 20010424 A 3397 WIRE BOEING 737 7374Q8 NM CABIN DAMAGED A K NONE L NO TEST IN INSP/MAINT 1 NM 01 756AS 25097 SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 16. REPAIR WIRES, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001073100278 20010731 00278 NM 2001 7 31 ASAA0170002 1 20010415 A 5210 66185732 LEVER BOEING 737 737790 13844CN NM L1 DOOR LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 607AS 29751 PDX - DURING PREFLIGHT, CREW REPORTED L1 DOOR HINGE RELEASE LEVER DIFFICULT TO OPERATE. CLEANED AND LUBRICATED LEVER. DOOR THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 2001073100280 20010731 00280 NM 2001 7 31 ASAA0170004 1 20010521 A 3397 8100022608 WIRE BOEING 737 737790 13844CN NM CABIN DISCONNECTED A K NONE L NO TEST IN INSP/MAINT 1 NM 01 617AS 30542 SEA - DURING LINE MAINTENANCE, THE EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN ROWS 15 THROUGH 18. RE-CONNEC TED THE TRACK LIGHT WIRES AT ROW 18. THE LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 2001073100283 20010731 00283 WP 2001 7 31 ASAA0180128 1 20010409 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 962AS 53076 SEA - DURING LINE CHECK, OVERHEAD EMERGENCY LIGHTS AT ROWS 8-12 WERE DETERMINED TO BE INOPERATIVE. REMOVED AND REPLACED ASSOCIATED BATTERY PACK. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001073100284 20010731 00284 WP 2001 7 31 ASAA0180129 1 20010409 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SEA - DURING LINE CHECK, FORWARD CABIN PORTABLE EMERGENCY LIGHT WAS DETERMINED TO BE INOPERATIVE. REPLACED LIGHT ASSEMB LY. LIGHT THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001073100286 20010731 00286 WP 2001 7 31 ASAA0180130 1 20010408 A 3397 0105606005 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 NM 01 951AS 49111 PDX - DURING SERVICE CHECK, EMERGENCY FLOOR TRACK LIGHTING AT ROW 6 WAS DETERMINED TO BE INOPERATIVE. REPAIRED BROKEN C ONNECTOR WIRE AND RESECURED. TRACK LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 2001073100287 20010731 00287 NM 2001 7 31 CA010703003 1 20010611 A 5330 SKIN BOEING 737 737201 1384454 NM PWA JT8 JT8D9A 52048 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 52900 (CAN) CRACK IN FUSELAGE SKIN LEFT SIDE, BETWEEN FUSELAGE STATIONS 747 AND 767, STRINGER 17L. REPAIR AS PER SRM 53-30-3, TABLE 1, METHOD 1, PAGES 87,88,88A. 2 L 7 2 4F 4 F A16WE E2EA 2001073100288 20010731 00288 NM 2001 7 31 CA010703004 1 20010610 A 5330 SKIN BOEING 737 737201 1384454 NM PWA JT8 JT8D9A 52048 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 58358 (CAN) CRACK IN FUSELAGE SKIN LEFT SIDE, 8 INCHES AFT. OF STATION 750 AT STRINGER 17L. REPAIRED AS PER SRM 53-30-3, TABLE 1, METHOD 1, PAGES 87,88, 88A. 2 L 7 2 4F 4 F A16WE E2EA 2001073100289 20010731 00289 WP 2001 7 31 ASAA0180150 1 20010424 A 3350 0105606003 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 SEA - DURING PRE-FLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN 1ST CLASS CABIN. RECONNECTED LOOSE CON NECTOR TO FLOOR TRACK LIGHTS MODULES. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001073100290 20010731 00290 WP 2001 7 31 CALA0100715 1 20010729 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FS 845-1032 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND R/H I/B SEAT TRACK CORRODED AT FS 845-1032. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALL ED WITH SPLICES IAW SRM 53-05, FIGURE 4F AND 51-10-3. 2 L 7 2 4F A6WE 2001073100291 20010731 00291 WP 2001 7 31 CALA0100716 1 20010729 A 5310 SPACER DOUG DC9 DC982 3022082 WP MID CARGO DR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND MID CARGO DOOR LOWER JAMB BEAM SPACER CORRODED AROUND RIVNUTS. THE SPACER WAS REMOVED AND A NEW SPACER WAS INSTALLED IAW SRM 51-30-4 AND 51-10-4. 2 L 7 2 4F A6WE 2001073100292 20010731 00292 WP 2001 7 31 CALA0100718 1 20010730 A 5754 SKIN DOUG DC9 DC982 3022082 WP LH "0" SLAT DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND L/H "0" SLAT EXTERNAL SKIN DENTED. THE SKIN AND ATTACHING PARTS WERE REMOVED IAW SRM 51-30-6 AND 51-30- 1. A DOUBLER WAS INSTALLED IAW SRM 57-09, FIGURE 10A. THE SKIN AND ATTACHING PARTS WERE REINSTALLED IAW SRM 51-30-6 AND 51-30-1. 2 L 7 2 4F A6WE 2001073100293 20010731 00293 NM 2001 7 31 CALA0100723 1 20010730 A 5320 ANGLE BOEING 737 7373T0 1384582 NM STA 944-991.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14325 23455 INSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED AT STA 944-991.5. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001073100294 20010731 00294 NM 2001 7 31 CALA0100724 1 20010730 A 5414 SKIN BOEING 737 7373T0 1384582 NM #1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77303 23354 INSPECTION FOUND A 1" CRACK IN #1 PYLON SKIN PANEL #5727L. A REPAIR WAS INSTALLED IAW ECRA 5430-01230. 2 L 7 2 4F RT A16WE 2001073100295 20010731 00295 WP 2001 7 31 CALA0100725 1 20010730 A 5543 SKIN DOUG DC9 DC982 3022082 WP RUDDER TAB DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND RUDDER CONTROL TAB SKIN DENTED IN THE LOWER LEFT SIDE. THE RUDDER TAB WAS REMOVED IAW MM 27-20-02. THE TAB WAS REPAIRED, WEIGHED, AND BALANCED IAW SRM 55-40-1. THE TAB WAS INSTALLED AND THROW CHECKS WERE COMPLETED IAW MM 27 -20-02. 2 L 7 2 4F A6WE 2001073100296 20010731 00296 NM 2001 7 31 CALA0100727 1 20010730 A 5330 SKIN BOEING 737 7373T0 1384582 NM @ DORSAL FIN GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14325 23455 INSPECTION FOUND FUSELAGE SKIN GOUGED AT FORWARD END ON DORSAL FIN MOUNT AREA. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53 -00-01. 2 L 7 2 4F RT A16WE 2001073100297 20010731 00297 EA 2001 7 31 COMA0160520 1 20010725 A 5300 601R3103077 PLATE CNDAIR CL600 CL6002B19 EA INCORRECT A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 926CA 18280 7027 TWO SPLICE PLATES P/N 601R310300-77 WERE FABRICATED INCORRECTLY BY MANUFACTURE.REMOVED AND REPLACED SPLICE PLATES I/A/W WVAC EO 601R-53-2609. 2 L 7 2 4F RT A21EA 2001073100298 20010731 00298 WP 2001 7 31 ASAA0180151 1 20010427 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 933AS 49234 SEA - DURING LINE CHECK, BATTERIES FOR THE OVERHEAD EMERGENCY LIGHTS IN MID CABIN WERE DETERMINED TO HAVE LOW CHARGE. R EMOVED AND REPLACED ASSOCIATED BATTERY PACKS. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001073100299 20010731 00299 CE 2001 7 31 CA010703006 1 20010601 A 2913 1153800025 PUMP BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA HYD SYSTEM MISINSTALLED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) RECEIVED MOTOR P/N 115-380002-5 S/N 1783 FROM TRANSPORT CANADA STICK INSTALLED THE O/H MOTOR ON THE AIRCRAFT AS PE R WIRING DIAGRAM IN WESTERN AIRCRAFT MAINTENANCE MANUAL. FOUND THAT THE HYDRAULIC PUMP ROTATION WAS INCORRECT. THE WIRI NG DIAGRAM WAS REVERITIED AGAINST THE COMPONENT THAT WAS INTIALLY REMOVED AND FOUND TO BE CONNECTED AS PER THE WIRING DI AGRAM AND ROTATION IN THE CORRECT ROTATION. THE MOTOR RECEIVED FRIN FIELD AVIATION P/N 115-380002-5 INCORRECTLY WIRED IN TERNALLY. P/N 115-38002-5 S/N 1788 WAS REMOVED FROM THE AIRCRAFT AND RETURNED TO THE SUPPLIER AND ANOTHER MOTOR WAS THEN ORDERED. ---PMI ISSUE. 1 L 7 2 4T 4 T A24CE E4EA 2001073100300 20010731 00300 WP 2001 7 31 ASAA0180152 1 20010427 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 964AS 53078 SEA - DURING LINE CHECK, MID CABIN OVERHEAD EMERGENCY LIGHTS NEAR OVERWING EXITS WERE DETERMINED TO BE INOPERATIVE. REM OVED AND REPLACED ASSOCIATED BATTERY PACK. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001073100301 20010731 00301 WP 2001 7 31 ASAA0180153 1 20010427 A 2121 6054577 FAN DOUG DC9 DC983 3022083 WP CABIN FAILED A ASAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 01 949AS 53022 SEA - HAZE AND ELECTRICAL ODOR NOTED IN PASSENGER CABIN DURING FLIGHT. REMOVED AND REPLACED AIR CONDITIONING RECIRCULAT ION FAN. SYSTEM THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001073100303 20010731 00303 WP 2001 7 31 ASAA0180154 1 20010429 A 3350 0105606003 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 PDX - DURING PREFLIGHT, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN FIRST CLASS. REPAIRED CONNECTION. LIGHTS THE N OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001073100304 20010731 00304 EU 2001 7 31 CA010703011 1 20010625 A 2742 9787314203R ACTUATOR PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL PITCH TRIM NOISY W K NONE O OTHER IN INSP/MAINT 1 CA 2072 2072 (CAN) PITCH TRIM ACTUATOR FAILED ROUTINE FUNCTION CHECK. PRIMARY MOTOR SOUNDS ROUGH WHEN ACTUATED. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001073100305 20010731 00305 CE 2001 7 31 CA010703012 1 20010621 A 2761 262218722 STRUCTURE CESSNA 26221872 CESSNA 208 208 2073702 CE PWA PT6 PT6A114A 52043 NE MCAULY 3AF34C 3GFR34C703 GL SPOILER LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING INSPECTION FOUND THAT ATTACHMENT RIVETS AT RT SPOILER OUTBOARD ATTACHMENT ARM WERE LOOSE. RIVETS REPLACED 2 ND A/C THAT PROBLEM WAS DISCOVERED ON. 1 H 7 1 3T 3 T NT A37CE E4EA 5 C P60GL 2001073100306 20010731 00306 WP 2001 7 31 ASAA0180157 1 20010506 A 3350 0105606003 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 SEA - DURING PRE-FLIGHT CHECK, FOUND FIRST FOUR EMERGENCY TRACK LIGHTS IN 1ST CLASS CABIN TO BE INOPERATIVE. RECONNECTE D LOOSE TRACK LIGHT MODULE CONNECTORS. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001073100307 20010731 00307 WP 2001 7 31 ASAA0180158 1 20010505 A 3350 0105606003 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 ANC - DURING PRE-FLIGHT CHECK, FOUND 1ST CLASS CABIN EMERGENCY TRACK LIGHTING TO BE INOPERATIVE. RECONNECTED LOOSE TRAC K LIGHT MODULE CONNECTORS. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001073100310 20010731 00310 EA 2001 7 31 COMA0160525 1 20010728 A 5300 BEAM CNDAIR CL600 CL6002B19 EA MISDRILLED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 963CA 11979 7127 TRANSVERSE BEAM AT FS 333, RBL9 HAS TWO EXISTING MISDRILLED FASTENER HOLES IN LOWER FLANGE.REPAIRED I/A/W WVAC EO 601R-5 3-2577. 2 L 7 2 4F RT A21EA 2001073100311 20010731 00311 EA 2001 7 31 COMA0160526 1 20010729 A 5300 HST10AG8 FASTENER CNDAIR CL600 CL6002B19 EA IMPROPER A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 937CA 7044 WHILE ACCOMPLISHING CANADAIR REO 601R-53-61-345, THE REPAIR CALLS OUT FOR THE USE OF TWO HST 10AG8 HI LITES FOR INSTALLA TION IN THE STANDOFF . PROPER GRIP LENGTH IF NOT AVAILABLE.INSTALLED HL18PB8-XX HI-LOK SWITCH HL70-8 COLLARS IN PLACE OF THE HST10AG8 HI LITES I/A/W WVAC EO 601R-53-2618. 2 L 7 2 4F RT A21EA 2001073100312 20010731 00312 EA 2001 7 31 COMA0160527 1 20010728 A 5300 601R38303253 ANGLE CNDAIR CL600 CL6002B19 EA CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 926CA 18280 7027 SERVICE DOOR SILL ANGLE IS CORRODED.REMOVED AND REPLACED I/A/W WVAC EO 601R-53-2589A. 2 L 7 2 4F RT A21EA 2001073100313 20010731 00313 EA 2001 7 31 COMA0160528 1 20010730 A 5300 60135006 WEB CNDAIR CL600 CL6002B19 EA CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 912CA 19096 7011 CRACK AT LOWER WEB OF ENGINE SUPPORT BEAM AT LEFT FWD INBD CORNER 2" IN LENGTH.REPAIRED DAMAGE I/A/W REO 601R-53-61-3666 . 2 L 7 2 4F RT A21EA 2001073100314 20010731 00314 WP 2001 7 31 ABXA010414 1 20010131 A 5300 577992549 SKIN DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AX 46126 EXTERIOR FUSELAGE, BULGING SKIN NEAR FLAPPER AT STATION 110, LONGERON 36. REMOVED FLAPPER VALVE IAW REA D853-39745MR. FA BBED FILLER AND FINGER DOUBLER IAW REA D853-39745MR. ALODINED AND PRIMED IAW DC-8 SRM 51-1-8. INSTALLED FILLER, FINGER D OUBLER AND FLAPPER VALVE IAW DC-8 SRM 51-1-21, 51-1-20D, AND REA D853-39745MR. 2 L 7 4 4F 4A25 2001073100315 20010731 00315 WP 2001 7 31 ABXA010415 1 20010205 A 5700 SKIN DOUG DC8 DC863F 302198F WP LEFT WING GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AX 46126 LEFT WING LEADING EDGE STAB WING ABOVE #2 ENGINE, OUTBOARD END OF VANE HAD SEVERAL HOLES WITH VERY DEEP GOUGES CAUSED BY DIMPLE WASHERS, APPROXIMATELY W/STA. 225.0 REMOVED SEAL ASSEMBLY, FABRICATED REPAIR DOUBLER IAW REA D857-39765MR. ALOD INED AND PRIMED IAW DC-8 SRM 51-1-8. INSTALLED REPAIR DOUBLER IAW REA D857-39765MR. INSTALLED SEAL ASSEMBLY IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 2001073100316 20010731 00316 2001 7 31 COMA0160529 4 20010728 A 3140 6229820008 COMPUTER CNDAIR CL600 CL6002B19 EA SATURATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 729CA 1160 7265 NUMEROUS AURAL AND CAUTION WARNINGS DURING FLIGHT.REMOVED WATER FROM #2 DCU CANNON PLUB. 2 L 7 2 4F RT A21EA 2001073100317 20010731 00317 WP 2001 7 31 ASAA0180159 1 20010504 A 3350 0105606003 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 ANC - DURING PRE-FLIGHT CHECK, FOUND FORWARD STRIP OF EMERGENCY TRACK LIGHTING TO BE INOPERATIVE. RECONNECTED LOOSE TRA CK LIGHT MODULE CONNECTOR AT FOURTH LIGHT. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001073100318 20010731 00318 NE 2001 7 31 CA010703022 2 20010627 A 7200 ALF502R5 BEARING BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NR 4 ENGINE MAKING METAL W K NONE O OTHER IN INSP/MAINT 1 CA 26942 250 (CAN) DURING ROUTINE INSPECTION NR 4 ENGINE FULL FLOW CHIP DETECTOR WAS FOUND TO HAVE "CONDITION 2" CONTAMINATION. THE E NGINE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. TEARDOWN REVEALED THAT THE PRE MOD NR 2 BEARING PACK LOCATI NG PIN HAD SHEARED AND ALLOWED THE BEARING TO SPIN, CAUSING THE CONTAMINATION. 2 H 7 4 4F 4 F RT A49EU E6NE 2001073100320 20010731 00320 WP 2001 7 31 ASAA0180160 1 20010506 A 3350 0105606003 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 ANC - DURING PRE-FLIGHT CHECK, FOUND FIRST SIX EMERGENCY TRACK LIGHTS IN 1ST CLASS CABIN TO BE INOPERATIVE. RECONNECTED LOOSE TRACK LIGHT MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001073100321 20010731 00321 EU 2001 7 31 CA010703027 1 20010614 A 2612 1734362450 FIRE DETECTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ROTOL R390 R3904123F27 NE LT ENGINE MALFUNCTIONED W E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 CA (CAN) FLT 3725 DEPARTING WINNIPEG EXPERIENCED A LT TAILPIPE HOTLIGHT. ENGINE WAS SHUTDOWN & BECAUSE OF BAD WEATHER A/C D IVERTED TO KENORA. ENROUTE LH ENGINE WAS RESTARTED & FUNCTI ONED NORMALLY WITH NO ABNORMAL IND.S. MAINTENACE INVEST. REV EALED WATER INGRESS AT ELECT. CONNECTIONS FOR L/H FIRE DETECTOR. OLD SEALANT WAS REMVD & CONECTION CLEA NED AND INSP. TH ERE BEING NO EVIDENCE OF EFECTS CONNECTIONS WERE RESEALED & SYS FUNCTION TESTED. FUNCTION TEST WA NORMAL & A/C RELEASED TO SERVICE. THERE IS A KNOWN PROBL EM WITH THIS FIRE DETECTOR & WATER CONTAMINATION. WEATHE WAS BAD TIME OF INCID., SAA B SB- 340-26-020 REFERS 2 L 7 2 4T 4 T RT A52EU E8NE 6 C P31NE 2001073100322 20010731 00322 WP 2001 7 31 ASAA0180161 1 20010507 A 3350 2550325 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 967AS 49103 SEA - DURING PRE-FLIGHT, THE FORWARD CABIN PORTABLE EMERGENCY LIGHT WAS DETERMINED TO BE INOPERATIVE. REPLACED BATTERY. LIGHT THEN OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 2001073100323 20010731 00323 WP 2001 7 31 ASAA0180163 1 20010507 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 PDX - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE AT ROWS 6, 7 AND 8. REPLACED TRACK LIGHTING B ASE AND COVER IAW EA 3350-01014. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001073100324 20010731 00324 CE 2001 7 31 CA010703031 1 20010623 A 2421 DIODE CESSNA 310 310R 2074245 CE CONT O520 IO520MB 17032 SO ALTERNATOR FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 2284 (CAN) ON JUNE 23/01 THE PILOT SNAGGED HIS A/C AS THE LT ALTERNATOR BEING U/S/. UPON INSPECTION THE ALTERNATOR HAD A HOL E ON THE SIDE OF IT. REMOVED THE ALTERNATOR & BEFORE INSTALLING A NEW ONE, INSPECTED INSIDE THE ENGINE FROM WHERE THE AL TERNATOR WS REMOVED. FOUND THE GEAR INSIDE THE ENGINE THAT IS CONNECTED TO THE CRANKSHAFT THE TURNS THE ALTERNATOR HAD I TS BELTS SHEARED & WAS FREE FROM THE CRANKSHAFT. WHAT HAPPENED WAS THE ALTERNATOR DIODE FELL OFF & JAMMED THE ALTERNATOR AT THIS TIME ANOTHER DIODE ARCED THE CAST OF THE ALTERNATOR & MADE THE HOLE. THE PINS FOR THE GEAR THEN BROKE ALONG THE KEY ON THE ALTERNATOR SHAFT BRAKE, & THE SHAFT ALSO BENT. 1 L 7 2 3O 3 O 3A10 E5CE 2001073100326 20010731 00326 NM 2001 7 31 2001UALA01010 1 20010612 A 5314 KEELBEAM BOEING 737 737322 1384676 NM FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 KEEL BEAM LT LOWER CHORD OUTBOARD FLANGE, TWO HOLES WORN STA 712 - 720. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REP AIR AND FREEZE PLUGS. 2 L 7 2 4F RT A16WE 2001073100329 20010731 00329 NM 2001 7 31 2001UALA01041 1 20010610 A 3150 WARNING HORN BOEING 777 777222 1385219 NM COCKPIT ACTIVATED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 767UA 26918 ABORTED TAKEOFF AT APPROX 80 KTS DUE TO ENG FAILURE WARNING HORN SOUNDING. 2 L 7 2 4F RT T0001SE 2001073100331 20010731 00331 NE 2001 7 31 2001F00149 2 20010705 A 7200 ENGINE BOEING 737 737296 1384486 NM PWA JT8 JT8D17A 52049 NE NR 2 DAMAGED A RJEF C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 SO 25 232TA 22277 709402 SAL - FLT TA220 - DURING INITIAL TAKEOFF, A STRONG NOISE WAS HEARD, WHEN APPLYING TAKEOFF TRUST, REJECTED THE TAKEOFF AN D STRONG VIBRATION WAS FELT IN THE NR 2 ENGINE. ENGINE SHUTDOWN WAS ACCOMPLISHED, AIRCRAFT RETURNED TO GATE. DUE TO IN TERNAL DAMAGES, ENGINE NR 2 WAS CHANGED (S/N IN P-688012B) PER MM 71-00-00. ENGINE RUN-UP CHECK WAS PERFORMED ACCORDING TO MM 71-09-100. ENGINE TRIMMING WAS PERFORMED ACCORDING TO MM 71-09-246, PAGE 208 AND AIRCRAFT RETURNED TO NORMAL OPE RATION. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 2001073100332 20010731 00332 EA 2001 7 31 COMA0160530 1 20010728 A 3010 INDICATOR CNDAIR CL600 CL6002B19 EA A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 987CA 7199 WING OVERHEAT WARNING.COULD NOT DUPLICATE. SYSTEM CHECKS NORMAL. 2 L 7 2 4F RT A21EA 2001073100333 20010731 00333 EA 2001 7 31 COMA0160531 1 20010728 A 5270 DOOR CNDAIR CL600 CL6002B19 EA A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 809CA 7366 CABIN DOOR OUTER HANDLE CAUTION MESSAGE.DEFERRED MAINTENANCE PER M.E.L. 2 L 7 2 4F RT A21EA 2001073100334 20010731 00334 NM 2001 7 31 DHL2001747536 1 20010508 A 5754 651622172 SLAT BOEING 727 727224 1384076 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK, RT WING NR 5 SLAT L/E, INBOARD TRACK SEAL CUT OUT CRACKED. SEEN FROM TOP OF L/E. REMOVED RT WING NR 5 LEADING EDGE SLAT TO FOM PED 27-81-11. NDT REG FOR CRACK DIMENSION. CRACK DIMENSION CHECKED IAW NTM 727 51-06-00, PART 1 FROM THE EDGE 0.616" LENGTH. 2 L 7 3 4F A3WE 2001073100335 20010731 00335 EA 2001 7 31 COMA0160532 1 20010727 A 5270 840534 SWITCH CNDAIR CL600 CL6002B19 EA OUT OF ADJ A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 920CA 7022 CABIN DOOR OUTER HANDLE CAUTION MESSAGE.ADJUSTED DOOR HANDLE PROXIMITY SWITCH. 2 L 7 2 4F RT A21EA 2001073100338 20010731 00338 NE 2001 7 31 CA010704002 2 20010628 A 7200 366A54108800 ACCUMULATOR SNIAS 350 AS350D 8680803 EU LYC LTS101 LTS101600A 41560 NE ENGINE CRACKED W A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 CA (CAN) ENGINE DROOPED AT HIGH POWER SETTINGS. COMPLETE AIR SYSTEM WAS CHECKED FOR LEAKS. NO LEAKS WERE FOUND AT FITTINGS AND UNITS SEEMED SECURE. VISUAL INSPECTION OF ACCUMLATOR REVEALED NO APPARENT DEFECTS.GROUND RUN WAS CARRIED OUT BUT ENG INE WOULD NOT ACCELERATE PAST 60 PERCENT NG. LEAK DETECTOR SOLUTION WAS THEN APPLIED TO AIR SYSTEM DURING GROUND RUN AND A LEAK WAS REVEALED AT THE BASE OF THE ACCUMULATOR. THE DEFECT WAS NOT VISUALLY APPARENT WIHOUT LEAK DETECTOR SOLUTION. THE ACCUMULATOR WAS REPLACED. AIRCRAFT RUN AND FOUND SERVICEABLE. AIRCRAFT RETURNED TO SERVICE. NOTE; THIS IS SECOND OC CURENCE OF F AILURE OF THE ACCUMLATOR IN LESS THAN 12 MONTHS. (DIFFERENT AIRCRAFT). 1 G 7 1 3U 3 U H9EU E5NE 2001073100339 20010731 00339 NE 2001 7 31 CA010704003 2 20010628 A 7310 430163701 MANIFOLD SNIAS 350 AS350D 8680803 EU LYC LTS101 LTS101600A2 41560 NE FUEL SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 241 (CAN) FUEL FOUND ON ENGINE DECK DURING DAILY INSPECTION. GROUND RUN AND LEAK CHECKPERFORMED. FUEL FOUND EMANATING FROM L EAK IN FUEL MANIFOLD ASSEMBLY. MANIFOLD REPLACED AND LEAK CHECK CARRIED OUT. SYSTEM CHECKED SERVICEABLE AND AIRCRAFT RET URNED TO SERVICE. LEAKING MANIFOLD HAD LOW CYCLE LIFE SINCE NEW AT OCCURRENCE. 1 G 7 1 3U 3 U H9EU E5NE 2001073100341 20010731 00341 NE 2001 7 31 CA010704016 2 20010613 A 7260 RB211535E4 SHAFT BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E437 54555 NE GEARBOX FAILED W A UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 CA 28455 9267 (CAN) DURING CRUISE PILOT REPORTED ENGINE OIL PRESSURE DROP AND QTY DROP, VIBS STARTED TO INCREASE AND THE FLIGHT CREW E LECTED TO SHUT DOWN THE ENGINE IN ACCORDANCE WITH QRH PROCEDURES. AIRCRAFT DIVERTED AND RETURNED TO GANDER. MAINTENANCE INSPECTED THE LP COULD NOT ROTATE BY HAND, MCD'S INSPECTED EXERNAL ONE LARGE FLAKE AND INTERNAL TO GEARBOX FULL OF PARIC ALES. SCAVENGE FILTER HAD LIGHT CONTAINATION AND NO EXTERNAL VISUAL OIL LEAKS WHERE NOTICED. SUSPECT TOWER SHAFT FROM IP TO GEARBOX FAILURE, ENGINE REPLACED AND AIRCRAFT RETURNED TO SERVICE. AWAITING SHOP FINDINGS. 2 L 7 2 4F 4 F RT A2NM E12EU 2001073100342 20010731 00342 WP 2001 7 31 CA010704019 1 20010619 A 4930 0215726 FUEL BOWL LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE APU CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) ON PREPARING AIRCRAFT FOR DEPARTURE MAINTENANCE EXPERIENCED AN APU HUNG START ABORTED, ON INVESTIGATION FOUND APU FILTER BOWL CRACKED. 3RD OCCURANCE OF DEFECT. PUMP AND FILTER BOWL ASSEMBLY HAD BEEN PREVIOUSLY REPLACED DUE TO COULD NO T DISCOVER WHY 2ND OCCURANCE HAD HAPPENED. FILTER BOWL REPLACED TO RECTIFY FUEL LEAK AND APU DIACTIVATED IN ACCORDANCE W ITH THE MEL, AIRCRAFT DISPATCHED. APU SCHEDULED TO BE REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 2001073100343 20010731 00343 WP 2001 7 31 CA010704020 1 20010613 A 4930 10552E HEAT EXCHANGER LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE FUEL HEATER CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) FUEL LEAK AT HEAT EXCHANGER CORE. 2 L 7 3 4F 4 F A23WE E12EU 2001073100344 20010731 00344 WP 2001 7 31 CA010704021 1 20010629 A 4930 0215726 FUEL BOWL LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE APU CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) AFTER ARRIVAL IN PUJ NOT ABLE TO START APU, ON WALK AROUND FOUND FUEL LEAK COMING FROM APU, INVESTIGATED FOUND FUE L BOWL COVER LEAKING. MAINTENANCE REPLACED FUEL BOWL/LEAKCHECKED AND RETURNED AIRCRAFTTO SERVICE. 2 L 7 3 4F 4 F A23WE E12EU 2001073100346 20010731 00346 NM 2001 7 31 DHL2001747537 1 20010307 A 5320 FLOOR SUPPORT BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK, CORROSION UNDER NUT PLATES ON 4 FLOOR SUPPORTS FS 950A. REMOVED CORROSION FROM 4 AREAS ON FLOOR SUPPORTS IAW 7 27 SRM 51-10-6 PG 6, 4 (RBL 5, RBL 10, LBL 5, LBL 10). RBL 5, RBL 10, AND LBL 5. 2 L 7 3 4F A3WE 2001073100347 20010731 00347 SW 2001 7 31 CA010704025 1 20010628 A 6310 206040222005 SHAFT BELL 206L BELL 206 206L 1181522 SW ALLSN 250C 250C20R2 GL FREEWHEEL UNIT CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 462 BMB10179 (CAN) DURING AN UNSCHEDULED MAINTENANCE REMOVAL OF THE UNIT IT WAS NOTED THAT THERE WAS EXCESSIVE PITTING CORROSION ON T HE INNER SHAFT IN THE AREA WHERE THE FELT WIPER OF THE FORWARD SEAL RIDES. THE WIPER APPEARS TO ABSORB MOISTURE AND HOLD S IT IN CONTACT WITH THE SHAFT SURFACE RESULTING IN PITTING CORROSION. THE OLD STYLE SEAL (WHICH NO LONGER PROCURABLE) D ID NOT HAVE A FELT WIPER AND THUS IT DID NOT CAUSE THIS PITTING CORROSION ON THE SHAFT. THE FORWARD SEAL (P/N 206-340-20 4-101) HAD 462.8 HOURS SINCE NEW.THE SHAFT WAS REPLACED DUE TO PITTING BEYOND LIMITS. WE HAVE NOW HAD FIVE SHAFTS REPLAC ED DUETO THE SAME PROBLEM WHICH SEEMS TO BE IN THE DEIGN OF THE SEAL. 1 G 7 1 3U 3 U H2SW E4CE 2001073100349 20010731 00349 NE 2001 7 31 CA010706001 2 20010408 A 7200 ENGINE AIRBUS 330 A330322 3930325 EU RROYCE RB211 RB211TRENT77 NE NR 1 FAILED W C ABORTED TAKEOFF X ENGINE FLAMEOUT TO TAKEOFF 1 CA 9231 1281 (CAN) DURING DEPARTURE FLIGHT CREW APPLIED POWER TO START TO TAXI & NR 1 ENGINE FLAMED-OUT WITH AN ECAM WARNING OF STALL . DUE TO NO AUDIABLE STALL WAS OBSERVED, THE CREW RESTARTED THE ENGINE & ACCOMPLISHED A POWER RUN, NO FURTHER FAULT WAS OBSERVED AND THEY DEPARTED WITH THE AIRCRAFT. UPON AIRCRAFT RETURNED, AS A PRECAUTIONARY MEASURE, MAINTENANCE ACCOMPLISH ED THE AMM STALL/SURGE INSPECTION AS PER TASK #72-00-00-200--208, NO FAULT WAS NOTED & AIRCRAFT RETURNED TO SERVICE. NOT E: PREVIOUS OCCURENCES JAN 2000, AND AUG 2000 WITH THE SAME S/N AND AIRPORT LOCATION. 2 L 7 2 4F 4 F RT A46NM E39NE 2001073100350 20010731 00350 NM 2001 7 31 DHL2001747538 1 20010227 A 5720 SUPPORT BOEING 727 727224 1384076 NM RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 D-CHECK, RT WING L/E LOWER INBOARD FAIRING SUPPORT HAS LIGHT CORROSION IN END OF SUPPORT. REMOVED PART IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2001073100351 20010731 00351 WP 2001 7 31 CA010706003 1 20010420 A 2782 72003A ACTUATOR LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE SLATS WORN W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA (CAN) DURING TAKEOFF LEADING EDGE SLAT TRANSIT LIGHT CAME ILLUMINATED ON FLAP/SLAT INDICTOR WHEN A/C REACHED 80 KTS, REJ ECTED TAKEOFF OCCURRED. AFTER INVESTIGATION BY MAINTENANCE, NR 1 SLAT ACTUATOR FOUND WITH EXCESSIVE RADIAL PLAY AT JACKS CREW. ACTUATOR REPLACED AND SENSOR ADJUSTED. HIGH SPEED TAXI CARRIEDOUT AND CHECKED SERVICEABLE. 2 L 7 3 4F 4 F A23WE E12EU 2001102400103 20011024 00103 WP 2001 10 24 DHL2001801007 1 20010622 A 2130 CONTROL UNIT DOUG DC8 DC873F 302199F WP CABIN PRESSURE MALFUNCTIONED A DHLA K NONE O OTHER CR CRUISE 1 SO 01 801DH 46033 AT CRUISE ALT IN BOTH MANUAL AND AUTO PRESSURIZATION AND AT ALL FLOW SETTINGS, CABIN CLIMBS AND DESCENDS UP TO 700 FPM A ND WILL NOT STABILIZE AT CONSTANT PRESSURE. INSP OUTFLOW VALVE OPERATION, NO DEFECTS NOTED. PRESSURIZED A/C TO 7 PSI O N GROUND, DECAY CHECKED GOOD. AUTO AND MANUAL PRESSURIZATION CHECK GOOD PER MM 21-30-0. 2 L 7 4 4F RT 4A25 2001073100359 20010731 00359 WP 2001 7 31 DHL2001802008 1 20010609 A 2841 B17522W INDICATOR DOUG DC8 DC873 302199C WP COCKPIT DEFECTIVE A DHLA A UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 SO 01 802DH 46076 NR 1 MAIN FUEL TANK QUANTITY AT 2000 LBS WITH NO FUEL QUANTITY LOW LIGHT ILLUMINATED. REMOVED AND REPLACED NR 1 MAIN FU EL QTY GAUGE PER MM 28-41-0 AND CALIBRATED GAUGE. 2 L 7 4 4F RT 4A25 2001103000002 20011030 00002 WP 2001 10 30 DHL2001802009 1 20010620 A 2510 SPRING DOUG DC8 DC873 302199C WP PILOT SEAT LACK OF LUBE A DHLA K NONE O OTHER UK UNKNOWN 1 SO 01 802DH 46076 CAPT'S SEAT INTERMITTENTLY DOES NOT LOCK INTO POSITION ON TRACKS. LUBED TRACK & SPRING MECHANISM OP CK GOOD IAW 25-11-1 2 L 7 4 4F RT 4A25 2001073100361 20010731 00361 NE 2001 7 31 CA010711001 1 20010622 A 5246 S6130801425 ACCESS PANEL SKRSKY SKRSKY S61 S61N 8142104 NE GE CT58 CT581401 30011 NE LT ENGINE DISTORTED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) AS THE A/C DEPARTED THE HELI PAD, THE LT ENGINE DOOR OPENED. THE FLIGHT CREW LANDED AT THE END OF THE RUNWAY & ATT EMPTED TO CLOSE THE DOOR. THEY WERE UNSUCCESSFUL DUE TO THE BENT HINGE. THE A/C WAS TAXIED BACK TO THE HANGAR & THE LT E NGINE DOOR WAS REPLACED WITH A SERVICEABLE UNIT. THE UNSERVICEABLE LT ENGINE ACCESS DOOR WAS ROUTED FOR HINGE REPLACEME NT. 2 G 7 2 4U 4 U 1H15 1E3 2001073100363 20010731 00363 SW 2001 7 31 CA010711005 1 20010706 A 6320 212030104101 LINK BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE MAIN ROTOR BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WHILE TRACKING & BALANCING THE MAIN ROTOR SYS THE PILOT & ENGINEER COULD FEEL AN UNUSUAL VERTICAL VIBS,ON THE NEXT FLIGHT UNUSUAL LATERAL VIBS,ENGINEER MADE ADJUSTMENT TO M/R SYS BUT THE READING ONTHEEQUIPMENT STILL READ ROUGH.WHILE R UNNING ON THE GROUND A SIDE PANEL TO THE TRANSMISSION AREA WAS REMOVED.THE ENGINEER ASKED THE PILOT TO ADD A LITTLE POSI TIVE COLLECTIVE.IT WAS OBSERVED THAT THETRANSMISSION MOVED UP ABOUT 3/4 OF AN INCH.IT WAS NOTICED THAT THE LIFT LINK WAS BROKEN ON THE UPPER END WHERE IT IS ATTACHEDTO THE TRANSMISSION. 1 G 7 1 4U 4 U H1SW E17EA 2001073100364 20010731 00364 EU 2001 7 31 CA010711006 1 20010612 A 7160 HTE920036 VALVE 200038 SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE INTAKE SEIZED W K NONE O OTHER IN INSP/MAINT 1 CA 8686 M500GB299 (CAN) FAILED TO OPERATE WHEN TESTED (PARTICLE SEPARATOR ACTUATOR).ENGINE INTAKE. 1 G 7 1 3U 3 U H9EU E19EU 2001073100366 20010731 00366 EA 2001 7 31 COMA0160533 1 20010728 A 3010 434419883 SWITCH CNDAIR CL600 CL6002B19 EA MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 943CA 7062 WING OVERHEAT MESSAGE.REPLACED THE BACKUP OVERHEAT SWITCH. 2 L 7 2 4F RT A21EA 2001073100367 20010731 00367 EA 2001 7 31 COMA0160534 1 20010727 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 EA BURNED OUT A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 785CA 7326 LEFT HAND EMERGENCY LIGHT IS INOPERABLE.REPLACED THE LIGHT BULB. 2 L 7 2 4F RT A21EA 2001073100368 20010731 00368 NE 2001 7 31 DHL2001803006 2 20010609 A 7240 9992M85P01 PLUG DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE NR 2 ENGINE UNSECURE A DHLA F E A ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 803DH 46123 692182 NR 2 ENG FIRE WARNING. BOTH A & B LOOP. EMERGENCY CHECKLIST RUN - AFT FIRE BOTTLE DISCHARGED. FOUND COMBUSTER BORESCO PE PLUGS, 1 AND 3 O'CLOCK, IMPROPERLY SECURED. RESECURED 2 BORESCOPE PLUGS PER CFM M/M 72-42-00. PERFORMED VISUAL INSP ECTION OF ENGINE AND COWL PER M/M 71-00. NO DEFECTS NOTED. 2 L 7 4 4F 4 F RT 4A25 E2GL 2001073100369 20010731 00369 EA 2001 7 31 COMA0160535 1 20010729 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA A COMA O OTHER S AFFECT SYSTEMS IN INSP/MAINT 1 SO 01 945CA 7069 EMERG LIGHTS ILLUMINATED WITH SWITCH IN AUTO POSITION.FOUND CANNON PLUG JB-6 DISCONNECTED. SECURED CONNECTOR AND SYSTEM TEST NORMAL. 2 L 7 2 4F RT A21EA 2001073100370 20010731 00370 NM 2001 7 31 2001UALA00903 1 20010601 A 2916 O-RING BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE A UALA A UNSCHED LANDING F FLT CONT AFFECTED LD LANDING 1 WP 29 7280U 21558 LANDED LAX UNDER AMBER ALERT DUE TO LOSS OF HYDRAULIC PRESSURE. SUPPLEMENTAL DATA UPDATE FOUND ELEVATOR FEEL COMPUTER "A " SYSTEM FILTER CAP O-RING CUT AND LEAKING. REPLACED O-RING AND FILTER PER MM. SERVICED HYDRAULIC SYSTEM AND LEAK CHECKE D OK. 2 L 7 3 4F 4 F A3WE E2EA 2001073100371 20010731 00371 NM 2001 7 31 2001UALA00928 1 20010603 A 7331 GASKET BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LEAKING A UALA O OTHER K FLUID LOSS IN INSP/MAINT 1 WP 29 605UA 21866 ENGINE FUEL FLOW TRANSMITTER AFT GASKET ASSY HAS A RUNNING FUEL LEAK. SUPPLEMENTAL DATA UPDATE RPL. FUEL FLOW TRANSMITTE R OUTLET SIDE GASKET AND O-RING ON #2 ENGINE PER MM OPS AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E3NE 2001073100372 20010731 00372 NM 2001 7 31 2001UALA01405 1 20010713 A 2780 40173 SWITCH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LEFT WING FAILED A UALA K NONE J WARNING INDICATION CR CRUISE 1 WP 29 7456U 21910 LEADING EDGE FLAP AMBER LIGHT INDICATION OCCURRED AFTER CLIMBOUT. AIRCRAFT CONTINUED TO MIA. SUPPLEMENTAL DATA UPDATE FO UND #2 LEADING EDGE FLAP SWITCH FAULTY AND REPLACED SWITCH. 2 L 7 3 4F 4 F A3WE E2EA 2001073100373 20010731 00373 NM 2001 7 31 2001UALA01410 1 20010717 A 3350 900835A BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7462U 21916 EMERGENCY EXIT LIGHTS ABOVE BOTH LEFT OVERWING EXIT DOORS ARE INOPERABLE. SUPPLEMENTAL DATA UPDATE REPLACED BATTERY PAC K, OPERATIONS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001073100374 20010731 00374 NM 2001 7 31 2001UALA01417 1 20010721 A 5315 CHANNEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 515UA 24840 CABIN FLOOR SUPPORT STRUCTURE CORRODED. STA 1660-1680, RBL 65. MAJOR REPAIR ACCOMPLISHED.INSTALLED NEW J-CHANNEL. 2 L 7 2 4F 4 F RT A2NM E17NE 2001073100375 20010731 00375 NM 2001 7 31 2001UALA01440 1 20010723 A 5315 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 515UA 24840 CABIN FLOOR INBOARD CREASE BEAM CORRODED. STA 720-740, LBL 59. MAJOR REPAIR ACCOMPLISHED.INSTALLED NEW CREASE BEAM AND Z-ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001073100376 20010731 00376 NM 2001 7 31 2001UALA01475 1 20010725 A 5315 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 515UA 24840 CABIN FLOOR INTERCOSTAL CORRODED. STA 365 TO 377, RBL 10. MAJOR REPAIR ACCOMPLISHED.INSTALLED NEW INTERCOSTAL AND GALL EY SUPPORT CHANNEL. 2 L 7 2 4F 4 F RT A2NM E17NE 2001080100001 20010801 00001 SO 2001 8 1 C2XA01IA307 1 20010725 A 3350 110049 POWER SUPPLY EMB 145 EMB145LR SO CABIN INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16981 145208 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT SOME EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001080100002 20010801 00002 WP 2001 8 1 AALA20011345 1 20010608 A 5300 SEAT TRACK DOUG DC9 DC982 3022082 WP FS 1174-1308 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7521A 49898 TUL - FOUND CORROSION ON SEAT TRACK NR 1. REMOVED CORRODED SEAT TRACK NR 1 AND INSTALLED NEW SEAT TRACK NR 1 FROM FS 11 74-1308 SRM 51-01. (M) 2 L 7 2 4F A6WE 2001080100003 20010801 00003 WP 2001 8 1 AALA20011344 1 20010625 A 5300 SKIN DOUG DC9 DC982 3022082 WP FS 237 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7521A 49898 TUL - FOUND FUSELAGE SKIN GOUGED STATION 237 LONGERON 20L. CUT OUT 1 INCH HOLE TOO REMOVE DAMAGE AND INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M) 2 L 7 2 4F A6WE 2001080100004 20010801 00004 WP 2001 8 1 AALA20011343 1 20010619 A 5300 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1174-1308 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7521A 49898 TUL - FOUND CORROSION ON SEAT TRACK NR 3. REMOVED CORRODED SEAT TRACK NR 3 AND INSTALLED NEW TRACK FROM FS 1164 THRU 13 08 SRM 53-05. (M) 2 L 7 2 4F A6WE 2001080100005 20010801 00005 WP 2001 8 1 AALA20011342 1 20010620 A 5322 SHEAR TIE DOUG DC9 DC982 3022082 WP FS 1456 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7521A 49898 TUL - FOUND SHEAR TIE CRACKED LBL 10 INCHES STATION 1456 ABOVE 'Y' DUCT. INSTALLED NEW SHEAR TIE PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2001080100006 20010801 00006 WP 2001 8 1 AALA20011340 1 20010618 A 5300 SKIN DOUG DC9 DC982 3022082 WP FS 242 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7521A 49898 TUL - FOUND DENT RIGHT FUSELAGE 5 FEET AFT OF SERVICE DOOR. INSTALLED DOUBLER PER SRM 53-04 FIG 12B. (M) 2 L 7 2 4F A6WE 2001080100007 20010801 00007 WP 2001 8 1 AALA20011378 1 20010628 A 5300 BEAM DOUG DC9 DC983 3022083 WP FS 1155-1211 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 433AA 49451 TUL - FOUND CORROSION ALONG LONGERON 28 LOWER DOOR CUTOUT BEAM AFT CARGO. INSTALLED REPAIR DOUBLER PER SRM 53-10-00-3 F IG 2. (M) 2 L 7 2 4F RT A6WE 2001080100008 20010801 00008 WP 2001 8 1 AALA20011379 1 20010625 A 5100 995773927B STIFFENER DOUG DC9 DC983 3022083 WP FS 1287 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 433AA 49451 TUL - FOUND VERY DEEP DENTS IN FUSELAGE FRAME ON AFT SIDE STATION 1287 BELOW LONGERON 17L. REMOVED OLD STIFFENER/SHEAR TIE. INSTALLED DUPLICATED PART OF 2024-T0, HEAT TREATED TO T-3, .050 THICK DUPLICATED (DUPLICATED ON SHOP ORDER 2202530 DATED 6/21/01). INSTALLED PER SRM 51-30-05 AFTR TREAT/PRIME. (M) 2 L 7 2 4F RT A6WE 2001080100009 20010801 00009 WP 2001 8 1 AALA20011280 1 20010624 A 3397 WIRE DOUG DC9 DC982 3022082 WP AFT CABIN SHORTED A K NONE L NO TEST IN INSP/MAINT 1 SW 21 287AA 49299 BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT SIGN AT AFT CABIN INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT W IRES AT LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001080100010 20010801 00010 WP 2001 8 1 AALA20011277 1 20010621 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 241AA 49254 ORD - DURING OVERNIGHT MAINTENANCE, OVERWING EMERGENCY EXIT LIGHTS AT FORWARD OVERWING EXIT INOPERATIVE. REPLACED OVERW ING EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001080100011 20010801 00011 WP 2001 8 1 AALA20011275 1 20010620 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP AFT ACCESSORY INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 218AA 49168 TPA - DURING OVERNIGHT MAINTENANCE, TWO EMERGENCY LIGHTS ABOVE TAIL CONE ESCAPE SLIDE INOPERATIVE. REPLACED BATTERY PAC K. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001080100012 20010801 00012 WP 2001 8 1 AALA20011257 1 20010616 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 33502 49739 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 28 DIM. RE-SECURED EMERGENCY EXIT LIGHT CONNECTOR. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001080100013 20010801 00013 NM 2001 8 1 AALA20011314 1 20010626 A 5310 WEB BOEING 727 727223 1384074 NM FS 1183 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 869AA 21374 TUL - FOUND CRACK, AFT FACE OF FS 1183 PRESSURE BULKHEAD IN TAIL SKID WELL. STOP DRILLED CRACK AND INSTALLED DOUBLER PE R SRM 53-10-2. (M) 2 L 7 3 4F A3WE 2001080100014 20010801 00014 NM 2001 8 1 AALA20011312 1 20010626 A 5100 BEAM BOEING 727 727223 1384074 NM FS 265-266 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 869AA 21374 TUL - FOUND STATION 265 LBL CORROSION ON FLOORBEAM. INSTALLED REPAIR PER ESO 11697 DATED 6/25/2001. (M) 2 L 7 3 4F A3WE 2001080100015 20010801 00015 NM 2001 8 1 AALA20011313 1 20010621 A 5100 STIFFENER BOEING 727 727227 1384078 NM CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AA 20732 TUL - FOUND VERTICAL STIFFENER CORRODED. REMOVED AND REPLACED STIFFENER 51-10-00. (M) 2 L 7 3 4F A3WE 2001080100016 20010801 00016 WP 2001 8 1 AALA20011380 1 20010628 A 5300 SEAT TRACK DOUG DC9 DC983 3022083 WP FS 1194 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 433AA 49451 TUL - FOUND CORROSION ON NR 3 SEAT TRACK STATION 1194 AROUND SCREW HOLE SEAT TRACK FLANGE. BLENDED OUT CORROSION AND IN STALLED REPAIR STRAP PER 53-20-00-13 SRM. (M) 2 L 7 2 4F RT A6WE 2001080100017 20010801 00017 WP 2001 8 1 AALA20011381 1 20010620 A 5300 SEAT TRACK DOUG DC9 DC983 3022083 WP FS 232 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 433AA 49451 TUL - FOUND CORROSION ON SEAT TRACK NR 5 AT STATION 232-237. SEAT TRACK PLUG REPAIR COMPLETED AS PER SRM 53-05 FIG 4A. (M) 2 L 7 2 4F RT A6WE 2001080100018 20010801 00018 WP 2001 8 1 AALA20011383 1 20010702 A 5330 SKIN DOUG DC9 DC983 3022083 WP FS 1380 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 433AA 49451 TUL - FOUND FUSELAGE SKIN CRACKED AT RIVET ABOVE RIGHT ENGINE PYLON STATION 1380. STOP DRILLED CRACK AND INSTALLED DOUB LER PER SRM 53-30-00-02 PAGE 1. (M) 2 L 7 2 4F RT A6WE 2001080100019 20010801 00019 WP 2001 8 1 AALA20011385 1 20010621 A 5300 LONGERON DOUG DC9 DC983 3022083 WP FS 160 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 433AA 49451 TUL - FOUND LONGERON 4 LEFT CRACKED IN RADIUS AT STATION 160. CUT OFF DAMAGED LONGERON AND INSTALLED NEW SECTION PER SR M 53-02 PAG 48-53 FIG 18. (M) 2 L 7 2 4F RT A6WE 2001080100020 20010801 00020 WP 2001 8 1 AALA20011386 1 20010621 A 5330 SKIN DOUG DC9 DC983 3022083 WP FS 1380 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 433AA 49451 TUL - FOUND CRACK IN FUSELAGE SKIN STATION 1380, ABOVE L14L, ABOVE LEFT ENGINE PYLON. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER SRM 53-30-00-02. (M) 2 L 7 2 4F RT A6WE 2001080100021 20010801 00021 WP 2001 8 1 AALA20011387 1 20010622 A 5100 991556223 STIFFENER DOUG DC9 DC983 3022083 WP FS 1338 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 433AA 49451 TUL - FOUND FS 1338 PRESSURE BULKHEAD FORWARD FACE UPPER 12 O'CLOCK STIFFENER IS CRACKED .75 INCH AT UPPER MOST END OF A TTACHMENT. REMOVED AND REPLACED VERTICAL STIFFENER ABOVE VAULT DOOR PER MM 51-01. (M) 2 L 7 2 4F RT A6WE 2001080100022 20010801 00022 WP 2001 8 1 AALA20011388 1 20010623 A 5300 SKIN DOUG DC9 DC983 3022083 WP FS 473-481 A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 433AA 49451 TUL - FOUND LIGHTNING STRIKES IN FUSELAGE SKIN STATION 473 TO 481 LONGERON 7 LEFT. INSTALLED DOUBLER PER SRM 53-04 FIG 38 SHEET 24-36-37-38. (M) 2 L 7 2 4F RT A6WE 2001080100023 20010801 00023 WP 2001 8 1 AALA20011289 1 20010620 A 5300 SEAT TRACK DOUG DC9 DC983 3022083 WP FS 1196-1300 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 433AA 49451 TUL - FOUND CORROSION ON TRACK NR 2 AT STATION 1196-1206 AND 1300. CORROSION REMOVED, SEAT TRACK PLUGS INSTALLED TWO LO CATIONS STATION 1196-1206 AND STATION 1300 PER SRM 53-05 FIG 4A. (M) 2 L 7 2 4F RT A6WE 2001080100024 20010801 00024 WP 2001 8 1 AALA20011390 1 20010620 A 5300 SEAT TRACK DOUG DC9 DC983 3022083 WP FS 1300 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 433AA 49451 TUL - FOUND CORROSION ON SEAT TRACK NR 3 AT STATION 1300. CORROSION REMOVED AND SEAT TRACK PLUG INSTALLED PER SRM 53-05 , FIG 4A. (M) 2 L 7 2 4F RT A6WE 2001080100025 20010801 00025 WP 2001 8 1 AALA20011391 1 20010620 A 5300 SEAT TRACK DOUG DC9 DC983 3022083 WP FS 1088 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 433AA 49451 TUL - FOUND CORROSION IN TRACK NR 6 AT STATION 1088. REMOVED DAMAGED AREA SEAT TRACK, TREATED AND PRIMED. INSTALLED SE AT TRACK PLUG PER SRM 53-05 FIG 4A, PRIMED AND TREATED AND PAINTED PLUG. (M) 2 L 7 2 4F RT A6WE 2001080100026 20010801 00026 WP 2001 8 1 AALA20011392 1 20010622 A 5300 SKIN DOUG DC9 DC983 3022083 WP FS 454 A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 433AA 49451 TUL - FOUND LIGHTNING STRIKE PRODUCED ONE BURN HOLE .125 INCH IN DIAMETER AT STATION 454 LONGERON 7 LEFT. REMOVED DAMAG E AND INSTALLED DOUBLER PER SRM 53-04-00 FIG 18 SHEET 24-38. (M) 2 L 7 2 4F RT A6WE 2001080100027 20010801 00027 WP 2001 8 1 AALA20011393 1 20010626 A 5300 WEB DOUG DC9 DC983 3022083 WP FS 218 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 433AA 49451 TUL - FOUND CORROSION STATION 218 RBL 12. INSTALLED DOUBLER PER AARD 53-00-00-02. (M) 2 L 7 2 4F RT A6WE 2001080100028 20010801 00028 WP 2001 8 1 AALA016059 1 20010620 A 3350 6011779 POWER SUPPLY DOUG DC9 DC987 3022087 WP CABIN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 754RA 49641 CCI - RIGHT AFT OVERWING EMERGENCY EXIT IGHT BATTERY SUPPLY INOPERATIVE. REPLACED BATTERY SUPPLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 2001080100029 20010801 00029 WP 2001 8 1 AALA016060 1 20010627 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 754RA 49641 CCI-LAX - ROW 17, 18, 19 AND 20 EMERGENCY AISLE LIGHTS INOPERATIVE. REPLACED BATTERY PACK LOCATED AFT RIGHT OVERWING EX IT ROW. OPS NORMAL. (M) 2 L 7 2 4F RT A6WE 2001080100030 20010801 00030 WP 2001 8 1 AALA20011346 1 20010619 A 5322 SHEAR TIE DOUG DC9 DC982 3022082 WP FS 1456 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7521A 49898 TUL - FOUND SHEAR TIE CRACKED AT STATION 1456 BETWEEN LONGERON 1/2 RIGHT. INSTALLED NEW SHEAR TIE PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2001080100032 20010801 00032 WP 2001 8 1 DHL2001803507 1 20010630 A 5350 STRUCTURE DOUG DC8 DC873 302199C WP TAIL CONE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 TAIL CONE-RT ELEVATOR BRUSH COVER INNER STRUCTURE CRACKED 1.25. PERFORMED STOP HOLE PER SRM 53-2-0 FIG 1B. FABRICATED DOUBLER WITH ALCLAD (2420T3 0.025) PER SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED PER SRM 51-1-8, INSTALLED DOUBLER PER SRM 53-20 FIG 1 B. 2 L 7 4 4F RT 4A25 2001080100033 20010801 00033 WP 2001 8 1 DHL2001803508 1 20010623 A 5532 SKIN DOUG DC8 DC873 302199C WP VERTICAL STAB DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 VERTICAL STABILIZER L/E SHOWS 3.52 IN DENT AT ZFS 123.500. CUT OUT DAMAGED AREA PER SRM 55-2-1 PG 17. FABRICATED FILLE R (ALCLAD 7075 T6,0.050) PER SRM 55-2-1. FABRICATED DOUBLER (ALCLAD 7075-T6 0.050) PER SRM 55-2-1 PG 17. CLEANED, TREA TED AND PRIMED PER SRM 51-1-8 B. INSTALLED DOUBLER PER SRM 55-2-1 PG 17. 2 L 7 4 4F RT 4A25 2001080100034 20010801 00034 WP 2001 8 1 DHL2001803509 1 20010630 A 5330 SKIN DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 FUSELAGE EXTERNAL SKIN SHOWS CRACK (0.500 IN LENGTH) AT STA -13.000, L-1DR. CUT OUT DAMAGED SKIN PER SRM 53-2-1 FIG 7 SH EET 4.5. INSTALLED FILLER AND DOUBLER AND NEW FASTENERS PER SRM 51-20-20D PG 9. 2 L 7 4 4F RT 4A25 2001080100035 20010801 00035 WP 2001 8 1 DHL2001803510 1 20010625 A 5320 ANGLE DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 FWD CARGO LINING SUPPORT ANGLE SHOWS .25 IN CRACK L-31 RT STA 480.000. 2 L 7 4 4F RT 4A25 2001080100036 20010801 00036 WP 2001 8 1 DHL2001803511 1 20010626 A 5320 ANGLE DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 FWD CARGO COMPT LINING SUPPORT ANGLE CRACKED .25 IN AT STA 460.000, L31L. 2 L 7 4 4F RT 4A25 2001080100037 20010801 00037 WP 2001 8 1 DHL2001803512 1 20010626 A 5320 ANGLE DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 FWD CARGO COMPT LINING SUPPORT ANGLE CRACKED .25 IN AT STA 460.000, L31L. 2 L 7 4 4F RT 4A25 2001080100038 20010801 00038 WP 2001 8 1 DHL2001803513 1 20010626 A 5320 FLOOR SUPPORT DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 FWD CARGO COMPT FLOOR SUPPORT ANGLE CRACKED (1/4 IN) AT STA 5000.000. 2 L 7 4 4F RT 4A25 2001080100039 20010801 00039 WP 2001 8 1 DHL2001803514 1 20010626 A 5320 ANGLE DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 FWD CARGO COMPT LINING SUPPORT ANGLE CRACKED .375 IN AT STA 620.000 L-29R. 2 L 7 4 4F RT 4A25 2001080100040 20010801 00040 WP 2001 8 1 DHL2001803515 1 20010626 A 5320 FLOOR SUPPORT DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 FWD CARGO COMPT-FLOOR SUPPORT ANGLE CRACKED 1 IN AT STA 500.000 L-34W. 2 L 7 4 4F RT 4A25 2001080100041 20010801 00041 WP 2001 8 1 DHL2001803516 1 20010626 A 5320 FLOOR SUPPORT DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 FWD CARGO COMPT, FLOOR SUPPORT ANGLE CRACKED (O/B) 1.5 IN AT STA 560.00 L-35L TO L-35R. 2 L 7 4 4F RT 4A25 2001080100042 20010801 00042 WP 2001 8 1 DHL2001803517 1 20010626 A 5320 ANGLE DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 FWD CARGO COMPT LINING SUPPORT ANGLE CRACKED (1/2 IN) AT STA 100.00 L-31L. 2 L 7 4 4F RT 4A25 2001080100043 20010801 00043 WP 2001 8 1 DHL2001803518 1 20010626 A 5320 ANGLE DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 FWD CARGO COMPT-LINING SUPPORT ANGLE CRACKED (3/4 IN) AT STA 360.000 L-33L. 2 L 7 4 4F RT 4A25 2001080100044 20010801 00044 WP 2001 8 1 DHL2001803519 1 20010623 A 5343 FITTING DOUG DC8 DC873 302199C WP RT MLG CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 RT MLG TRAPEZOIDAL LWR END, STOP DRILLED CRACK (6.125 IN ) CONTINUES .5 IN BEYOND STOP DRILL AT STA 896.12. STOP DRILLE D CRACK (.375 DIA), INSPECTED WITH NDT, CRACK DOES NOT CONTINUE PER SEQ-LIM 0100070H 06-20-01. 2 L 7 4 4F RT 4A25 2001080100045 20010801 00045 WP 2001 8 1 DHL2001803520 1 20010622 A 5320 ANGLE DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 FWD CARGO COMPT - LINING SUPPORT ANGLE CRACKED (.25 IN) AT STA 400.00 L-31L. 2 L 7 4 4F RT 4A25 2001080100046 20010801 00046 WP 2001 8 1 DHL2001803521 1 20010626 A 5320 ANGLE DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 FWD CARGO LINING SUPPORT ANGLE SHOWS 2 EA 1.5 IN CRACKS BETWEEN L-33 TO L34 RT STA 480.000. 2 L 7 4 4F RT 4A25 2001080100047 20010801 00047 WP 2001 8 1 DHL2001803522 1 20010625 A 5320 ANGLE DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 FWD CARGO LINING SUPPORT ANGLE WITH .5 IN CRACK AT L 32 LT AT STA 80.000. 2 L 7 4 4F RT 4A25 2001080100048 20010801 00048 WP 2001 8 1 DHL2001803524 1 20010625 A 5320 ANGLE DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 FWD CARGO COMPT- LINING SUPPORT ANGLE CRACKED 1.5 IN AT STA 600, L31R. 2 L 7 4 4F RT 4A25 2001080100049 20010801 00049 WP 2001 8 1 DHL2001803525 1 20010626 A 5320 FLOOR SUPPORT DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 FWD CARGO COMPT- FLOOR SUPPORT ANGLE CRACKED 1.5 INCH AT STA 580, L-34R. 2 L 7 4 4F RT 4A25 2001080100050 20010801 00050 WP 2001 8 1 DHL2001803526 1 20010626 A 5320 ANGLE DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 FWD CARGO COMPT- LINING SUPPORT ANGLE CRACKED 1 INCH AT STA 620, L-31R. 2 L 7 4 4F RT 4A25 2001080100051 20010801 00051 WP 2001 8 1 DHL2001803527 1 20010626 A 5320 ANGLE DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 FWD CARGO COMPT - LINING SUPPORT ANGLE CRACKED (.25 INCH) AT STA 600, L-31L. 2 L 7 4 4F RT 4A25 2001080100052 20010801 00052 WP 2001 8 1 DHL2001803528 1 20010625 A 5320 ANGLE DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 FWD CARGO COMPT- LINING SUPPORT ANGLE CRACKED (1.5 INCH) AT STA 460, L-31R. 2 L 7 4 4F RT 4A25 2001080100053 20010801 00053 WP 2001 8 1 DHL2001803529 1 20010625 A 5320 ANGLE DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 FWD CARGO COMPT- LINING SUPPORT ANGLE CRACKED (.5 INCH) AT STA 460, L-29L. 2 L 7 4 4F RT 4A25 2001080100054 20010801 00054 WP 2001 8 1 DHL2001803530 1 20010626 A 5320 ANGLE DOUG DC8 DC873 302199C WP FUSELAGE BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 FWD CARGO COMPT- LINING SUPPORT ANGLE BROKEN AT STA 440, L-27L. 2 L 7 4 4F RT 4A25 2001080100055 20010801 00055 WP 2001 8 1 DHL2001803531 1 20010623 A 5320 ANGLE DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 RT FUSELAGE WALL EXT VERTICAL ANGLE SHOWS .5 INCH CRACK AT STA 980. 2 L 7 4 4F RT 4A25 2001080100056 20010801 00056 WP 2001 8 1 DHL2001803532 1 20010616 A 7110 SKIN DOUG DC8 DC873 302199C WP NR 3 COWLING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C-CK, ENGINE NR 3 HAD 1.5 INCH CRACK ON EXTERNAL SKIN OF TRANSLATING COWL LT (UPPER BORDER) AT 11 O'CLOCK. 2 L 7 4 4F RT 4A25 2001080100057 20010801 00057 WP 2001 8 1 DHL2001803533 1 20010614 A 5753 DOUBLER DOUG DC8 DC873 302199C WP T/E FLAP BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C-CK, RT WING- EXT PATCH ON OUTBOARD FLAP UPPER SKIN NEAR STA XW 219.00 SHOWS .3125 INCH BREAK APPROX. 2 L 7 4 4F RT 4A25 2001080100058 20010801 00058 WP 2001 8 1 DHL2001803534 1 20010615 A 5720 ANGLE DOUG DC8 DC873 302199C WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CK, RT WING - WING TO FUSELAGE FILLET SUPPORT ANGLE CRACKED (2 INCHES) AT XW 908-XCW 69.5. 2 L 7 4 4F RT 4A25 2001080100059 20010801 00059 WP 2001 8 1 DHL2001803535 1 20010616 A 7830 SKIN DOUG DC8 DC873 302199C WP THRUST REVERSER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C-CK, NR 2 ENGINE - RT THRUST REVERSER INTERNAL SKIN CRACKED 2 INCHES AT 3 O'CLOCK POSITION. 2 L 7 4 4F RT 4A25 2001080100060 20010801 00060 WP 2001 8 1 DHL2001803536 1 20010618 A 5350 FAIRING DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C-CK, RT WING TO FUSELAGE UPPER FAIRING SHOWS 1 INCH BREAK AT STA 834. 2 L 7 4 4F RT 4A25 2001080100061 20010801 00061 WP 2001 8 1 DHL2001803537 1 20010614 A 5350 RADOME DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C-CK, RADOME- 2 (EA) .25 INCH CRACKS ON RADOME LOWER LIP (INNER PART). PERFORMED STOP HOLE IAW SRM 53-2-0 FIG 1B, FA BRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 2001080100063 20010801 00063 NM 2001 8 1 CA010712002 1 20010630 A 2910 82970010301 TUBE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM CHAFED W D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 CA 26879 (CAN) A PASSENGER ADVISED THE FLIGHT CREW THAT HE HAD NOTICED A PUDDLE OF FLUID UNDER THE RIGHT NACELLE AFTER THE AIRCRA FT HAD STOPPED. THE FLIGHT CREW CONFIRMED THE LEAK AS HYDRAULIC FLUID.MAINTENANCE FOUND THE RETURN LINE FROM THE ANTI-SK ID VALVE HAD BEEN CHAFED BY THE FIRE DETECTION LOOP ALONG THE UPPER OUTBOARD SIDE OF THE NACELLE. THE LINE WAS REPLACED AND A LL FURTHER CHECKS WERE COMPLETED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001080100066 20010801 00066 EU 2001 8 1 CA010713008 1 20010617 A 2913 704A33690004 BELT SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE GEARBOX FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA 467 (CAN) FRAYING AT SEAM. THESE BELT ARE GOOD FOR 600 HOURS. WE HAD TO REPLACE THIS BELT EARLY AS WE THOUGHT IT WOULD NOT G O THE FULL 600 HOURS DUE TO THE FRAYING AT ITS SEAM. 1 G 7 1 3U 3 U NC H9EU E19EU 2001080100068 20010801 00068 WP 2001 8 1 DHL2001803538 1 20010705 A 2750 37701441 TORQUE TUBE DOUG DC8 DC873 302199C WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 RT WING O/B SLOT TORQUE TUBE CRANK (LT SIDE) SHOWS CRACK. REMOVED AND REPLACED RIGHT O/B SLOT TORQUE TUBE CRANK PER OHM 27-37-4 PAGE 1-2, SRM 51-3-1 PG 1 ON NON ROUTINE 1385 FOR OPS CHK. 2 L 7 4 4F RT 4A25 2001080100069 20010801 00069 NM 2001 8 1 DHL2001745006 1 20010729 A 5720 BRACKET BOEING 727 727224 1384076 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 COVE PANEL BRACKETS BELOW OUTBD END OF NR 13 SPOILER CRACKED LT WING LEADING EDGE VENT PANEL OUTER SKIN MISSING COVE PAN EL BRACKETS BELOW OUTBD END NR 12 SPOILER BROKEN OUT. REMOVED & REPLACED 1 EA T/E COVE PNL SUPPORT CHANNEL PER B727 SRM 51-10-1 & 51-30-2. REPAIRED BY FIBERGLASS OVERLAY REPAIR IAW B727 SRM 51-40-8. 2 L 7 3 4F A3WE 2001080100070 20010801 00070 WP 2001 8 1 DHL2001803539 1 20010706 A 5280 DOOR FRAME DOUG DC8 DC873 302199C WP LT MLG DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 LT MAIN LANDING GEAR DOOR,1 IN CRACK IN DOOR FRAME ANGLE AT STA 960.00. 2 L 7 4 4F RT 4A25 2001080100071 20010801 00071 WP 2001 8 1 DHL2001803540 1 20010704 A 5320 ANGLE DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 NOSE LANDING GEAR WHEEL WELL .25 IN CRACK ON FRAME REINFORCING ANGLE, STA 119.L-33L. 2 L 7 4 4F RT 4A25 2001080100072 20010801 00072 WP 2001 8 1 DHL2001803541 1 20010704 A 5320 ANGLE DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 NOSE LANDING GEAR WHEEL WELL .5 IN CRACK ON FRAME REINFORCING ANGLE STA 119, L-33R. 2 L 7 4 4F RT 4A25 2001080100073 20010801 00073 WP 2001 8 1 DHL2001803542 1 20010704 A 5753 FITTING DOUG DC8 DC873 302199C WP T/E FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 RT EXTERNAL FLAP HINGE SUPPORT INNER FITTING AT XF 409 SHOWS 0500 IN LENGTH CRACK ON LOWER SURFACE. 2 L 7 4 4F RT 4A25 2001080100074 20010801 00074 WP 2001 8 1 DHL2001803543 1 20010704 A 5753 FITTING DOUG DC8 DC873 302199C WP T/E FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 RT EXTERNAL FLAP HINGE SUPPORT INNER FITTING AT XF 409 SHOWS 0500 IN LENGTH CRACK ON LOWER SURFACE. 2 L 7 4 4F RT 4A25 2001080100075 20010801 00075 WP 2001 8 1 DHL2001803546 1 20010630 A 5314 KEELBEAM DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 RT MAIN LANDING GEAR WHEEL WELL KEEL BEAM INNER RIB SHOWS 1 INCH CRACK AT STA 920. 2 L 7 4 4F RT 4A25 2001080100076 20010801 00076 WP 2001 8 1 DHL2001803548 1 20010701 A 5730 SKIN DOUG DC8 DC873 302199C WP LT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 LT WING L/E SKIN EXHAUST GATE BROKEN APPROX 1.5 INCH. REMOVED DAMAGED SKIN PER SRM 51-1-21 PG 1. FABRICATED SKIN (2024 -T3 0.032) PER SRM 57-2-1 FIG 1. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED NEW SKIN PER SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2001080100078 20010801 00078 WP 2001 8 1 DHL2001803549 1 20010701 A 5312 PRESSURE PANEL DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 NLG NOSE TUNNELS STRUCTURES SHOW 3 INCH CRACK ON FRAME NEAR STA 12 AND LONG 33 RT. 2 L 7 4 4F RT 4A25 2001080100079 20010801 00079 WP 2001 8 1 DHL2001803550 1 20010706 A 5730 SKIN DOUG DC8 DC873 302199C WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 RT WING L/E LOWER SKIN SHOWS .5 INCH CRACK AT XW 485.000. 2 L 7 4 4F RT 4A25 2001080100081 20010801 00081 WP 2001 8 1 DHL2001803551 1 20010706 A 5522 SKIN DOUG DC8 DC873 302199C WP ELEVATOR DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 RT ELEVATOR LOWER SKIN DEFLECTED STA XE 132-246. 2 L 7 4 4F RT 4A25 2001080100083 20010801 00083 WP 2001 8 1 DHL2001803552 1 20010708 A 5522 SKIN DOUG DC8 DC873 302199C WP ELEVATOR DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 RT ELEVATOR LOWER SKIN SHOWS 2 INCH DENT BETWEEN STA XE 256.250 AND XE 260.937. 2 L 7 4 4F RT 4A25 2001080100084 20010801 00084 WP 2001 8 1 DHL2001803553 1 20010708 A 5522 SKIN DOUG DC8 DC873 302199C WP ELEVATOR DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 LT ELEVATOR LOWER PART SHOWS SKIN DEFLECTED BETWEEN STA XE 288.375 TO XE 297.2347. 2 L 7 4 4F RT 4A25 2001080100085 20010801 00085 WP 2001 8 1 DHL2001803554 1 20010708 A 5522 SKIN DOUG DC8 DC873 302199C WP ELEVATOR DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 LT ELEVATOR LOWER PART SHOWS SKIN DEFLECTED AT XE 94.500 TO XE 112.906. 2 L 7 4 4F RT 4A25 2001080100086 20010801 00086 WP 2001 8 1 DHL2001803556 1 20010706 A 5522 SKIN DOUG DC8 DC873 302199C WP ELEVATOR DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 RT ELEVATOR LOWER PART SHOWS SKIN DEFLECTED FROM XE.65.156 TO XE.117.599. 2 L 7 4 4F RT 4A25 2001080100087 20010801 00087 NM 2001 8 1 0102622709 1 20010610 A 5531 RIB BOEING 727 727225 1384077 NM CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 818EA 22555 During M check, found corrosion in the vertical stabilizer tension tie rib mount hole. Repaired per EA27-182234. 2 L 7 3 4F A3WE 2001080100088 20010801 00088 NM 2001 8 1 0102632709 1 20010604 A 5315 NUT PLATE BOEING 727 727225 1384077 NM CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 818EA 22555 During M check, found corrosion under nut plates installed under cargo floor support. Repaired per EA27-182243. 2 L 7 3 4F A3WE 2001080100089 20010801 00089 NM 2001 8 1 0102642709 1 20010602 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 818EA 22555 DURING M CHECK, FOUND CORROSION ON FLOORBEAM. REPAIRED PER EA27-182241. 2 L 7 3 4F A3WE 2001080100090 20010801 00090 NM 2001 8 1 0102652709 1 20010530 A 5314 KEELBEAM BOEING 727 727225 1384077 NM CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 818EA 22555 During M check, found corrosion on outboard flange of LH keel beam. Repaired per EA27-182237. 2 L 7 3 4F A3WE 2001080100091 20010801 00091 NM 2001 8 1 0102665519 1 20010716 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 519US 23207 DURING L CHECK, FOUND CRACK IN FLOORBEAM. REPAIRED PER EA55-184811. 2 L 7 2 4F RT A2NM 2001080100092 20010801 00092 WP 2001 8 1 DHL2001803557 1 20010708 A 5753 SKIN DOUG DC8 DC873 302199C WP T/E FLAP DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 LEFT WING EXTERNAL FLAP LOWER SKIN SHOWS .75 INCH (2 EA) DENTS AT STA XW 230.00. 2 L 7 4 4F RT 4A25 2001080100093 20010801 00093 WP 2001 8 1 DHL2001803558 1 20010708 A 5522 SKIN DOUG DC8 DC873 302199C WP ELEVATOR DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 RT ELEVATOR UPPER SKIN SHOWS DENTS XF 271.000 TO XH 283.000. 2 L 7 4 4F RT 4A25 2001080100094 20010801 00094 WP 2001 8 1 DHL2001803560 1 20010708 A 5730 SKIN DOUG DC8 DC873 302199C WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 RT WING LOWER SKIN SURFACE SHOWS 1 INCH CRACK AT STA XFS 300. 2 L 7 4 4F RT 4A25 2001080100095 20010801 00095 WP 2001 8 1 DHL2001803561 1 20010708 A 5730 SKIN DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 LT WING L/E LOWER SKIN SURFACE SHOWS 1.500 INCH CRACK AT STA XFS 597.500. 2 L 7 4 4F RT 4A25 2001080100096 20010801 00096 WP 2001 8 1 DHL2001803562 1 20010706 A 5310 DOUBLER DOUG DC8 DC873 302199C WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AFT CARGO COMPT AFT DOOR JAMB PATCH WORN AT STA 1440.00 L-29 TO L-32R. 2 L 7 4 4F RT 4A25 2001080100097 20010801 00097 WP 2001 8 1 DHL2001803563 1 20010706 A 5522 SKIN DOUG DC8 DC873 302199C WP ELEVATOR DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 RT ELEVATOR UPPER PART SHOWS SKIN WITH 1/2 IN 3 EA DENTS FROM XE 55.062 TO XE 39.531. 2 L 7 4 4F RT 4A25 2001080100098 20010801 00098 WP 2001 8 1 DHL2001803564 1 20010708 A 5753 SKIN DOUG DC8 DC873 302199C WP T/E FLAP DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 LT WING EXTERNAL FLAP LOWER SKIN SHOWS 2 INCH DENT AND 4 INCH DEEP SCRATCH STA XW.159 (XF 213 TO 169). 2 L 7 4 4F RT 4A25 2001080100099 20010801 00099 2001 8 1 DHL2001804010 4 20010619 A 2210 AUTOPILOT SYS DOUG DC8 DC873F 302199F WP COCKPIT MALFUNCTIONED A DHLA K NONE O OTHER AP APPROACH 1 SO 01 804DH 46124 A/P TRACKS 1-1/2 DOTS LOW COUPLED ON F/O SIDE ON G/S. PERFORMED OPS CHECK OF A/P LOCALIZER AND GLIDE PATH. CHECKS OK B OTH SIDES IAW 22-10-0 PG 207. 2 L 7 4 4F RT 4A25 2001080100100 20010801 00100 2001 8 1 DHL2001804011 4 20010619 A 2210 AUTOPILOT SYS DOUG DC8 DC873F 302199F WP COCKPIT MALFUNCTIONED A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 804DH 46124 A/P EXCEEDS 30 DEG BANK IN HEADING SELECT MODE ON F/O SIDE. PERFORMED OPS CHECK OF A/P HEADING SELECT MODE. CHECKS OK BOTH SIDES IAW 22-10-0 PG 206 STEP H. 2 L 7 4 4F RT 4A25 2001080100101 20010801 00101 NE 2001 8 1 DHL2001805014 2 20010608 A 7200 CFM562C1 ENGINE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C1 13802 NE NR 3 POWER LOSS A DHLA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 01 805DH 46125 693537 DURING CLIMB FROM FL310 TO 350 ENG NR 3 SPOOLED BACK TO IDLE THRUST. THRUST LEVER HAD NO EFFECT. DURING RELIGHT ATTEMP T N2 WOULD NOT ACCELERATE ABOVE 11%, N1 30%, N2 10% OR PRESS 3 PSI TIME 2 HOURS. REMOVED AND REPLACED NR 3 ENG IAW MM 7 1-00, OPS CHECKS OK PER JRH 12.2 CHAPT 13.1 THRU 5. 2 L 7 4 4F 4 F RT 4A25 E2GL 2001102900058 20011029 00058 2001 10 29 DHL2001805015 4 20010706 A 2211 452080041942 COMPUTER DOUG DC8 DC873F 302199F WP AUTOPILOT SYS FAULTY A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 805DH 46125 IN CRUISE WITH AUTOPILOT IN AUX NAV INS NR 1, AIRCRAFT WOULD SUDDENLY ROLL RIGHT AND DIVERT FROM COURSE. OPS OK ON SYST EM NR 2. PERFORMED SYSTEM TEST. NR 1 INS SHOWED CODE 4 DURING ALIGNMENT. REMOVED AND REPLACED NR 1 INU. PERFORMED RO LL CHANNEL CHECK; FAILED CHECK S1-1. REMOVED AND REPLACED ROLL COMPUTER. AUTOPILOT AND INS OPS CHECKED OK IAW MM 22-12 -1 AND SMM 34-44-0. 2 L 7 4 4F RT 4A25 2001080100102 20010801 00102 WP 2001 8 1 DHL2001806002 1 20010621 A 2752 MOUNT DOUG DC8 DC873F 302199F WP T/E FLAP CRACKED A DHLA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 01 806DH 46002 ASYMMETRICAL FLAP CONDITION ON APPROACH OUTER NEEDLE FAILED TO EXTEND, PASSED 23. ROLL TENDENCY FELT. EMERGENCY DECLAR ED. FOUND RT INBOARD ACT MOUNT LUG CRACKED. INSPECTED AREA, NO OTHER DAMAGE NOTED. REMOVED AND REPLACED ACT ASSY IAW 27-59-9. SERVICED AND BLED FLAP LOCKOUT CYLINDERS IAW M/M 27-51-10. 2 L 7 4 4F RT 4A25 2001101900086 20011019 00086 WP 2001 10 19 DHL2001806003 1 20010710 A 3297 CONNECTOR DOUG DC8 DC873F 302199F WP NLG LOOSE A DHLA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 806DH 46002 UPON INITIAL GEAR EXTENSION NOSE GEAR DOWN AND LOCKED LIGHT DID NOT ILLUMINATE. ABNORMAL PROCEDURE, CYCLED LANDING GEAR AFTER SECOND EXTENSION, ALL GEAR INDICATED DOWN. FOUND LOOSE CANNON PLUG ON NOSE LIMIT SW. CLEANED AND INSTALLED CANN ON PLUG, OPS CK GOOD IAW DC-8 MM 32-60-0. 2 L 7 4 4F RT 4A25 2001080100103 20010801 00103 WP 2001 8 1 DHL2001806632 1 20010419 A 5753 5751189503 FITTING DOUG DC8 DC873F 302199F WP T/E FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK, LT WING FLAP HINGE SUPPORT FITTING SHOWS 0.750 INCH CRACK AT STA 409. REMOVED CRACKED FITTING AT STA 409 IAW S RM 51-1-20D PAGE 21. CLEANED, TREATED, AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PAGE 21 . 2 L 7 4 4F RT 4A25 2001080100104 20010801 00104 WP 2001 8 1 DHL2001806637 1 20010311 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK, LT WING L/E RIB LWR PORT .5 INCH CRACK AT STA XFS 642 - 250. 2 L 7 4 4F RT 4A25 2001080100105 20010801 00105 WP 2001 8 1 DHL2001806638 1 20010313 A 3010 DIFFUSER DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK, LT WING L/E ANTI-ICE DIFFUSER 1 INCH CRACK AT LOWER PART STA AFS 766.500 - XFS 766.950. 2 L 7 4 4F RT 4A25 2001080100106 20010801 00106 WP 2001 8 1 DHL2001806639 1 20010305 A 5753 FITTING DOUG DC8 DC873F 302199F WP T/E FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK, LT WING VERIFY POSSIBLE CRACK ON FITTING FROM O/B FLAP STA 406.000. PERFORMED HFEC INSPECTION IAW DC-8 NON-DES TRUCTIVE TESTING STANDARD PRACTICE MANUAL PART 6. 2 L 7 4 4F RT 4A25 2001080100108 20010801 00108 NM 2001 8 1 DL72L011148 1 20010703 A 5320 69648411 FITTING BOEING 727 727232 1384082 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 504DA 21306 FOUND DURING MV4 CORROSION VISIT NRC 54 CORROSION ON STR 27R END FITTING AT STA 740, OUTBD SIDE OF STR BEHIND RAM AIR DU CT. 2 L 7 3 4F A3WE 2001080100109 20010801 00109 NM 2001 8 1 DL72L011149 1 20010711 A 2780 40174 SWITCH BOEING 727 727232 1384082 NM L/E FLAP OUT OF ADJ A DALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 27 505DA 21307 AT 5 DEG FLAPS NR 3 L/E FLAP DID NOT EXTEND FULLY CYCLED. ACCORDING TO CHECKLIST BUT DID NOT EXTEND. ADJUSTED NR 3 L/E FLAP SWT RAN FLAPS TO 5 DEG AND BACK ALL IND NORMAL. 2 L 7 3 4F A3WE 2001080100111 20010801 00111 NM 2001 8 1 DL72L011151 1 20010711 A 5311 651751090 FRAME BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 509DA 21311 INSPECTION OF THE RT TORQUE BOX STRUCTURE FOR THE VENTRAL STAIRWAY PER BAC S/B 727-53-0129 AND AD 94-07-08 REVEALED A CR ACK IN THE INBD LONGITUDINAL UPPER CHORD AND A CRACK IN THE GUSSET AND BEAM AT FS 1273. 2 L 7 3 4F A3WE 2001080100112 20010801 00112 NM 2001 8 1 DL72L011163 1 20010711 A 5532 SKIN BOEING 727 727232 1384082 NM VERTICAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 509DA 21311 THE LT VERTICAL STABILIZER SKIN WAS FOUND WITH A 1 INCH CRACK EMANATING FROM A FASTENER HOLE NEAR THE REAR SPAR JUST ABO VE THE STAB-TO-FUSELAGE SKIN ATTACH ANGLE. 2 L 7 3 4F A3WE 2001080100113 20010801 00113 NM 2001 8 1 DL72L011164 1 20010713 A 3350 900542 POWER SUPPLY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 511DA 21313 ON STBY POWER FIRST CLASS EMERGENCY EXIT LIGHT INOP. REPLACED PWR SUPPLY. 2 L 7 3 4F A3WE 2001080100114 20010801 00114 NM 2001 8 1 DL72L011197 1 20010719 A 2910 B-NUT BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE HYDRAULIC SYS LOOSE A DALA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 512DA 62003 21314 696579 SLOW LEAK (FLUID LOSS) A HYDROL SYSTEM PUMPS SHUT DOWN PRIOR TO TOTAL FLUID LOSS. SERVICED A HYD RESERVOIR 8 PTS. FOUN D B-NUT LEAKING PYLON NR 1. SECURED B-NUT LEAK CKS OK. SECURED PYLON PNL. 2 L 7 3 4F 4 F A3WE E2EA 2001080100115 20010801 00115 NM 2001 8 1 DL72L011200 1 20010718 A 3350 02019241001 LIGHT BOEING 727 727232 1384082 NM CABIN DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 509DA 21311 RT FWD OVERWING EMERGENCY LIGHT LENS MISSING AND LIGHT ASSEMBLY DAMAGED. REPLACED LIGHT LENS AND REMOVED AND REPLACED L IGHT ASSEMBLY PER MM, OPS CHECK GOOD. 2 L 7 3 4F A3WE 2001080100116 20010801 00116 NM 2001 8 1 DL72L011206 1 20010719 A 5330 65545664 SPLICE BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 510DA 21312 LFEC OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 480 & 680 INDICATED CRACKS. INTERNAL MFEC INSPECTION CONFIRMED A CR ACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN BETWEEN FS 500 & 520 AND ANOTHER BETWEEN FS 560 & 580. 2 L 7 3 4F A3WE 2001080100117 20010801 00117 NM 2001 8 1 Q0MF200107068 1 20010703 A 4920 38007021 APU BOEING 737 737823 13844BZ NM APU BAY INOPERATIVE W Q0MF O OTHER M J OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 WP 03 879 30636 OUR AIRPLANE, B-16805, HAD APU AUTO-SHUTDOWN AFTER 3 OR 4 SOUNDS OF SURGE.APU BITE CHECK FOUND THAT MSG 49-21015 OVERTEM P SHUTDOWN¨. IAW MEL 49-1, CAT.¡§C¡¨, C/F TO DD ITEM. FURTHER CHECK, FOUND THAT THERE ARE MANY METAL CHIPS IN THE GEARB OX. REPLACED THE APU AT JULY 8, 2001. 2 L 7 2 4F RT A16WE 2001080100118 20010801 00118 NM 2001 8 1 DL72L011217 1 20010720 A 5313 65564413 STRINGER BOEING 727 727232 1384082 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 504DA 21306 STRINGER 29L WAS FOUND BADLY CORRODED BETWEEN FS 950E AND FS 980. 2 L 7 3 4F A3WE 2001080100119 20010801 00119 NM 2001 8 1 DL72L011222 1 20010724 A 3350 1315 LIGHT BOEING 727 727232 1384082 NM CABIN INTERMITTENT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 507DA 21309 LEFT AFT DOOR EMERGENCY EXIT LIGHT INTERMITTENTLY BLINKING EMERGENCY EXIT OVER CENTER CABIN IS INTERMITTENTLY BLINKING. RELAMPED LIGHT OVER LEFT AFT DOOR AND CENTER AISLE LIGHT OPERATION NORMAL. 2 L 7 3 4F A3WE 2001080100120 20010801 00120 NM 2001 8 1 DL72S011139 1 20010709 A 2782 1U109592 ACTUATOR BOEING 727 727225A 1384077 NM L/E SLAT DEFECTIVE A DALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 27 8875Z 21293 ON FLAP RETRACTION AFTER T/O AMBER L/E FLAP LIGHT ON FWD PANEL REMAINED ILLUMINATED. NR 1 SLAT LIGHT ON S/O PANEL REMAI NED ILLUMINATED. FLAPS 5 AND LOWER SHOWED NORMAL IND. REPLACED NR 1 SLAT ACTUATOR. FLAP/SLAT INDICATION OPS, CHECKS O K. 2 L 7 3 4F RT A3WE 2001080100121 20010801 00121 NM 2001 8 1 DL72S011141 1 20010710 A 5753 65192709 FLAP TRACK BOEING 727 727232 1384082 NM T/E FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 537DA 22073 INBOARD FLAP, NR 4 INBOARD TRACK WAS FOUND WITH CORROSION AND WEAR AT THE MLG AND SPOILER BEAM ATTACH PADS AND MLG DOOR HINGE FITTING HOLES. REPAIR PER ER/A 402062-14AD 2 L 7 3 4F A3WE 2001080100122 20010801 00122 NM 2001 8 1 DL72S011144 1 20010711 A 2782 IUIII0 ACTUATOR BOEING 727 727225A 1384077 NM L/E FLAP LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 8891Z 21860 HYD A SYST QUANTITY AND PRESSURE LOSS WELL AFTER GEAR AND FLAP RETRACTION. COMPLETED POM. FOUND NR 6 KRUEGER FLAP ACTU ATOR LEAKING, REPLACED SAME. REMOVED AND REPLACED BOTH A SYS HYD PUMP CASE DRAIN FILTERS, NO CONTAMINATION FOUND. SERV ICED HYD SYS, LEAK CHECKS GOOD. 2 L 7 3 4F RT A3WE 2001080100123 20010801 00123 NM 2001 8 1 DL72S011150 1 20010711 A 5312 BULKHEAD BOEING 727 727232 1384082 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 545DA 22494 WHILE ACCOMPLISHING INSPECTION OF THE FS 1183 BULKHEAD AFT ENTRY DOOR FRAMES AT RBL 17.8 PER AD 99-18-05 AND BAC S/B 727 -53-0210, 2 FASTENER HOLES WERE ELONGATED. 2 L 7 3 4F A3WE 2001080100124 20010801 00124 NM 2001 8 1 DL72S011195 1 20010719 A 5311 651632678 FRAME BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 533DA 22046 THE RT FS 784 FRAME HAS A SMALL CRACK EMANATING FROM THE FIRST HOLE ABOVE THE FLOOR LINE IN THE INNER CHORD. 2 L 7 3 4F A3WE 2001080100125 20010801 00125 NM 2001 8 1 DL72S011203 1 20010720 A 3350 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 538DA 22076 PAX SEAT 19F EMERGENCY LIGHT INOP. REPLACED SEAT LIGHT ASSY. 2 L 7 3 4F A3WE 2001080100126 20010801 00126 NM 2001 8 1 DL72S011218 1 20010204 A 5754 ANGLE BOEING 727 727232 1384082 NM L/E SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 533DA 22046 AT HMV FOUND ANGLE CRACKED UNDER I/B UP STOP NR 6 SLAT. 2 L 7 3 4F A3WE 2001080100127 20010801 00127 NM 2001 8 1 DL72S011225 1 20010724 A 3350 9000835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 516DA 21432 LEFT AFT OVERWING LIGHT INOP. REPLACED BATTERY PACK, CHECKS NORMAL. 2 L 7 3 4F A3WE 2001080100128 20010801 00128 NM 2001 8 1 DL72S011226 1 20010725 A 5320 65561293 WEB BOEING 727 727232 1384082 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 533DA 22046 CORROSION WAS FOUND ON THE C2 DOOR SILL WEB AT FS 970. THE DAMAGE WAS FOUND DURING AN INSPECTION AT HMV. 2 L 7 3 4F A3WE 2001080100129 20010801 00129 NM 2001 8 1 Q0MF200107069 1 20010720 A 3310 69607643 MODULE BOEING 737 737* NM P6 PANEL FAILED W Q0MF L ABORTED APPROACH O OTHER AP APPROACH 1 WP 03 1321 30664 DURING APPROACH TO KHH AFTER THE LANDING-GEAR EXTENSION, THERE WAS NO INDICATION OF THE L/G AT THE EXT POSITION ON THE C ENTRAL INSTRUMENT PANEL. BUT THE INDICATIONS OF THE L/G EXT POSITION ON THE OVERHEAD PANEL WERE NORMAL. THE CREW MADE A GO-AROUND, RETRACTED AND EXTENDED THE L/G ONCE MORE. AFTER THAT, THEY MADE A LOW APPROACH AND LANDED NORMALLY. IAW FIM 32-09-801, BITE PSEU. NO FAULT FOUND. THEN DO THE ¡§LT¡¨ TEST ON GROUND. FOUND THAT THE L/G IND, WINDOW HEAT SYS A L/H, HYD ELEC PUMP IND, ENG FIRE L/R IND, FUEL JET PUMP ¡¨LT¡¨ WERE OUT OF FUNCTION. IAW WIM 33-18-11 PAGE 101, REPLACED M ASTER TEST RELAY AND MASTER DIM MODULE. IAW AMM 33-18-00, GROUND OPERATION TEST, AND THE FUNCTION BACK TO NORMAL. IA 2 L 7 2 4F RT A16WE 2001080100130 20010801 00130 NM 2001 8 1 DL72S011227 1 20010725 A 5753 65192708 FLAP TRACK BOEING 727 727232 1384082 NM T/E FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 533DA 22046 INBOARD FLAP, NR 4 TRACK WAS FOUND WITH CORROSION AND WEAR AT THE MLG AND SPOILER BEAM ATTACH PADS, FWD ATTACH LUGS, MLG DOOR HINGE FITTING ATTACH HOLES, TOGGLE DETENT HOLE, AND CLIP ASSY AND SPACER BAR ATTACH HOLES. 2 L 7 3 4F A3WE 2001080100131 20010801 00131 NM 2001 8 1 DL72S011232 1 20010725 A 5720 STIFFENER BOEING 727 727232 1384082 NM WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 543DA 22392 FOUND ON F-1 CK 1 INCH CRACK L/E WING VERTICAL SPAR STIFFENER O/B SIDE OF NUMBER 6 SLAT O/B TRACK. 2 L 7 3 4F A3WE 2001080100132 20010801 00132 NM 2001 8 1 DL72S011237 1 20010726 A 5311 658261425 FRAME BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 533DA 22046 THE UPPER FAIL-SAFE CHORD OF THE FS 720B FRAME WAS FOUND CRACKED INBOARD OF STR 26L. THE DAMAGE WAS FOUND DURING INSP AT HMV. 2 L 7 3 4F A3WE 2001080100133 20010801 00133 NM 2001 8 1 DL72S011241 1 20010723 A 5713 STRINGER BOEING 727 727232 1384082 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 533DA 22046 AT HMV FOUND STRINGER CRACKED UPPER STRINGER 10 AT LT WS 629-00. 2 L 7 3 4F A3WE 2001080100134 20010801 00134 NM 2001 8 1 DL72W011024 1 20010621 A 5240 DOOR BOEING 727 727247 138408F NM L2 DOOR NOT CLOSED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 290WA 22108 ON CLIMBOUT AFT FLT ATTENDANT CALLED UP TO REPORT LOUD HISSING NOISE AT LEFT AFT SERVICE DOOR. RTN TO ATL. FOUND DOOR IMPROPERLY CLOSED. CYCLED DOOR, CLOSES NORMALLY. 2 L 7 3 4F A3WE 2001080100135 20010801 00135 NM 2001 8 1 DL72W011107 1 20010703 A 2612 FIRE WARNING BOEING 727 727247 138408F NM COCKPIT FALSE INDICATION A DALA F D ACTIVATE FIRE EXT. RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 295WA 22532 ON TAXI OUT AFT CARGO FIRE WARING LIGHT ILLUMINATED WITH INTERMITTENT BELL. CREW FOLLOWED HARD CARD AND DISCHARGED NR 1 BOTTLE IAW POM. FOUND BAGS WET AND SMALL AMOUNT OF WATER ON FLOOR. NO EVIDENCE OF FIRE. SUSPECT WATER VAPOR SET OFF A LARM. REPLACED NR 1 BOTTLE. RAN TEST OF DET SYSTEM, CKS GOOD. 2 L 7 3 4F A3WE 2001080100136 20010801 00136 NM 2001 8 1 DL72W011209 1 20010721 A 2432 23013 CHARGER BOEING 727 727247 138408F NM E/E BAY SMOKE A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 291WA 22109 FOUND ESS TRANSFORMER RECTIFIER INOP AND SMOKING. REPLACED BATTERY CHARGER DUE TO SMOKING AND BATTERY AND BUS PROTECTI ON PNL AND ESS TR. 2 L 7 3 4F A3WE 2001080100137 20010801 00137 NM 2001 8 1 S01252018 1 20010522 A 5210 MS20470B524 SHEAR PIN BOEING 747 747209B NM MAIN DECK CARGO SHEARED W SAJF O OTHER J WARNING INDICATION CL CLIMB 1 WP 03 24308 B-18771 MAIN DECK CARGO DOOR WARNING LIGHT CAME ON DURING INITIAL CLIMB. C/A:1.AFTER L/D,FOUND MASTER LATCH EXT HANDLE SHEAR PIN SHEARED AND HANDLE NOT LOCK POSITION. 2.REPLACED SHEAR PIN PER 747 MM 52-32-06. 3.ADJUST MASTER LATCH LOCK MEC HANISM PER 747 MM 52-32-00, AND CHECK DOOR OPEN/CLOSE FUNCTION NORMAL. 4.PFM CBN PRESSURIZATION WITH DP 5 PSI,CHECK NO A IR LEAKING AND MAIN DECK CARGO IND WAS NORMAL. 5.DO ONE-TIME INSPECTION PER EON 742-52-633753-012 FOR 747-200 FLEET. 2 L 7 4 4F RT A20WE 2001080100138 20010801 00138 NM 2001 8 1 DL733010925 1 20010605 A 5320 654583340 WEB BOEING 737 737347 1384647 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 304WA 23345 DURING INSPECTION PER SB 737-53A1173 REVISION 3, FOUND COCKPIT FLOOR WEBS JUST AFT OF 178 BULKHEAD CRACKED. 2 L 7 2 4F RT A16WE 2001080100139 20010801 00139 NM 2001 8 1 AWXA0002050 1 20010727 A 5313 65548325 STIFFENER BOEING 737 737277 1384570 NM BS 1098 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: Web support beam at R/H APU torque box BS 1098 has exfoliated corrosion on stiffener.C: Repaired web support beam sti ffener IAW B737 SRM 51-40-3 Fig 1 Pgs. 1-6 and BAC DWG 65-54832 2 L 7 2 4F RT A16WE 2001080100140 20010801 00140 NM 2001 8 1 AWXA0002051 1 20010726 A 5313 654540919 STIFFENER BOEING 737 737277 1384570 NM BS 727 LBL 17 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: Pressure web stiffener cracked at BS 727, LBL 17, WL 202C: Removed and replaced stiffener IAW B737 SRM 51-30-2 Pg 8 2 L 7 2 4F RT A16WE 2001080100141 20010801 00141 NM 2001 8 1 AWXA0002047 1 20010702 A 5330 654576953 SKIN BOEING 737 737277 1384570 NM SECTION 43 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: During "C-12" check inspection found belly skin cracked approx BS 520 STR 27 RT at Fwd OTBD corner of ground air cond itioning service doorC: Repaired crack at BS 520 STR 27 RT IAW AWA engineering repair No 15-01193-SS3 2 L 7 2 4F RT A16WE 2001080100142 20010801 00142 NM 2001 8 1 AWXA0002052 1 20010628 A 5310 654577518 SKIN BOEING 737 737277 1384570 NM SECTION 46 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: L2 Door upper hinge fuselage cut out cracked BS 979C: Repaired R2 Door fuselage skin upper hinge cut out IAW B737 SDR M 53-30-3 2 L 7 2 4F RT A16WE 2001080100143 20010801 00143 NM 2001 8 1 AWXA0002053 1 20010628 A 5310 6545778 SKIN BOEING 737 737277 1384570 NM SECTION 46 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: R2 door fuselage skin upper hinge cut out is cracked BS 947C: repaired R2 door fuselage skin upper hinge cut out IAW B737 SRM 53-30-3 Pg 78 & 78B 2 L 7 2 4F RT A16WE 2001080100144 20010801 00144 NM 2001 8 1 AWXA0002054 1 20010730 A 5312 654541041 WEB BOEING 737 737277 1384570 NM BS 178 WL 189 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: BS 178 Bulkhead Web cracked 3 places at WL 189 between RBL .6 and LBL .6C: Repaired BS 178 Bulkhead web IAW E.R. 15-5 312-01194-SS1 2 L 7 2 4F RT A16WE 2001080100145 20010801 00145 NM 2001 8 1 DL733010931 1 20010608 A 2612 PIN BOEING 737 737347 1384647 NM CFMINT CFM56 CFM563B2 13802 EU CONNECTOR BURNED A DALA F ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 SO 27 3301 23581 23181 60294 ON DESCENT DFW THE APU DET INOP LIGHT ON FIRE PANEL ILLUM. FOLLOWED POM PROCEDURE. APU AND APU BLEEDS WERE OFF AT THE TIME. ON FINAL THE APU FIRE WARN ILLUM. FOLLOWED POM PROCEDURE AND DISCHARGE FIRE BOTTLE. APU FIRE WARN REMAINED ILLU M FOR 3-5 MINUTES. EXTINGUISHED ON TAXI IN. APU DET INOP LIGHT WENT OUT ON TAXI IN. FOUND CONNECTOR D594 PINS BURNT. REPLACED SAME. REPLACED APU FIRE BOTTLE. OP CKS GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 2001080100147 20010801 00147 NM 2001 8 1 DL733010932 1 20010608 A 5240 SKIN 6545871523 BOEING 737 73735B NM R1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 221DL 930 23970 DOOR SKIN CRACKED N/R 123 C-1 CK OPN 8727 IN DFW. ITEM:R-1 DOOR SKIN CRACKED AT LOWER HINGE CUTOUT AT AFT UPPER AND LOW ER CORNERS. STOP DRILLED AND REMOVED CRACK AT UPPER AND LWR CORNERS PER SRM 52-00-01. PERFORMED HFEC PER NDT PART 6 CH 51-00-00, FIG 4. MADE UP DOUBLER PER SRM 52-00-01. OK TO INSTALL. INSTALLED REPAIR PER SRM 52-00-01. 2 L 7 2 4F RT A16WE 2001080100168 20010801 00168 NM 2001 8 1 DL733010933 1 20010607 A 5240 SKIN 6545871523 BOEING 737 73735B NM R1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 221DL 930 23970 DOOR SKIN CRACKED N/R 122 C-1 CK OPN 8727 IN DFW. ITEM: R-1 DOOR SKIN CRACKED AT UPPER HINGE CUTOUT AT LOWER AFT CORNER. 2 L 7 2 4F RT A16WE 2001080100172 20010801 00172 NM 2001 8 1 DL733010996 1 20010617 A 3350 1619 LIGHT BOEING 737 737330 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 241DL 23833 2L EMERGENCY LIGHT INOP. RELAMPED LIGHT. 2 L 7 2 4F RT A16WE 2001080100175 20010801 00175 NM 2001 8 1 DL733011010 1 20010618 A 5330 65737437 SKIN BOEING 737 737347 1384647 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 304WA 23345 THE FUSELAGE BELLY SKIN WAS GOUGED, DENTED AND PUNCTURED AT SEVERAL LOCATIONS BETWEEN FS 400 & 470 AND BETWEEN STRINGERS 26L & 26R. 2 L 7 2 4F RT A16WE 2001080100181 20010801 00181 NM 2001 8 1 DL733011063 1 20010625 A 3350 0201720001 LIGHT BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 947WP 23376 FOUND DURING SVC CK - IN-SEAT ESCAPE PATH LIGHT AT SEAT ROW 10FED INOP. REBULBED, NO HELP. REPLACED LIGHT ASSY, OPS NO RMAL. 2 L 7 2 4F RT A16WE 2001080100184 20010801 00184 NM 2001 8 1 DL733011064 1 20010625 A 3350 1317 LIGHT BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 947WP 23376 FOUND DURING SVC CK - EMERGENCY AISLE ILLUMINATION LIGHT LOCATED 2 INCHES BELOW LATCH FOR OVERHEAD BIN 17/18FED INOP. R EBULBED, OPN NORMAL. 2 L 7 2 4F RT A16WE 2001080100185 20010801 00185 NM 2001 8 1 DL733011161 1 20010711 A 5312 651630084 BULKHEAD BOEING 737 737347 1384647 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 303WA 23183 INSPECTION OF THE BL 17.1 AND BL 5.7 VERTICAL BEAMS OF THE AFT SIDE OF THE FS 178 BULKHEAD PER BAC S/B 737-53A1225. REV EALED A CRACK IN THE RBL 5.7 BEAM WEB AT WL 185 AND IN THE LBL 17.1 BEAM WEB AT WL 230. THE WEBS OF ALL 4 BEAMS WERE RE MOVED AND NEW WEBS INSTALLED TO REPAIR/MODIFY THE BEAMS PER ER/A 381260-14, REV A. 2 L 7 2 4F RT A16WE 2001080100189 20010801 00189 NM 2001 8 1 DL733011190 1 20010716 A 5330 SKIN BOEING 737 737330 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242DL 23834 A CRACK INDICATION WAS NOTED AT AN EXISTING GOUGE TRIMOUT LOCATION AT THE FWD EDGE OF THE C1 DOOR CUTOUT ABOVE THE LOWER CORNER. 2 L 7 2 4F RT A16WE 2001080100190 20010801 00190 EA 2001 8 1 COMA0160523 1 20010727 A 5346 601350061 WEB CNDAIR CL600 CL6002B19 EA CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 962CA 12502 7123 FOUND CRACK ON LEFT AND RIGHT SIDE LOWER WEB OF ENGINE SUPPORT - FWD, INBD OF ACCESS PANEL.REPAIRED ENGINE SUPPORT BEAM LEFT AND RIGHT LOWER WEB I/A/W CANADAIR REO 601R-53-61-366. 2 L 7 2 4F RT A21EA 2001080100191 20010801 00191 EA 2001 8 1 COMA0160524 1 20010728 A 5300 601R3111357 CLIP CNDAIR CL600 CL6002B19 EA A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 926CA 7027 AT FS 280 EXISTING HOLE FALLS INTO RADIUS OF INBOARD CLIPS 2 EACH AT RBL9.REMOVED, FABRICATED AND INSTALLED I/A/W WVAC E .O. 601R-53-2613. 2 L 7 2 4F RT A21EA 2001080100192 20010801 00192 NM 2001 8 1 DL738011142 1 20010710 A 3412 102LA2AG PROBE BOEING 737 737832 13844CF NM TAT SYSTEM INOPERATIVE A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 377DA 29625 AT FL350 LOST BOTH A/PS AND BOTH F/AS ; NO VNAV INFO IN FMS; A/THROTTLES INOP. REPLACED TAT PROBE. TAT PROBE INDICATIO N NORMAL. PERFORMED DFCS OPS TEST AND LAND VERIFY TEST. ALL TEST GOOD. PERFORMED ADIRU TEST. ADIRU TEST GOOD. PERFO RMED FMC OPS TEST. FMC OPS TEST GOOD. AUTOTHROTTLE BITE TEST GOOD. 2 L 7 2 4F RT A16WE 2001080100193 20010801 00193 NM 2001 8 1 DL73K010949 1 20010612 A 5553 FITTING BOEING 737 737232 1384475 NM VERTICAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 320DL 23092 CORROSION WAS FOUND ON THE VERTICAL STABILIZER FUSELAGE ATTACH LUGS. CORROSION WAS REMOVED FROM THE FACES, BORES AND O VERSIZED BUSHINGS WERE INSTALLED PER ERA 397615-14 AT HMV. 2 L 7 2 4F RT A16WE 2001080100194 20010801 00194 NM 2001 8 1 DL73K010951 1 20010612 A 5342 ATTACH FITTING BOEING 737 737232 1384475 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 320DL 23092 CORROSION WAS FOUND ON THE RT FUSELAGE CLEVIS LUGS FOR THE HORIZONTAL STABILIZER. CORROSION WAS REMOVED FROM SOME OF TH E FACES, BORES AND OVERSIZED BUSHINGS WERE INSTALLED. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001080100195 20010801 00195 NM 2001 8 1 DL73K010964 1 20010614 A 5551 ATTACH FITTING BOEING 737 737232 1384475 NM HORIZ STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 320DL 23092 CORROSION WAS FOUND ON THE RT HORIZONTAL STABILIZER ATTACH LUGS. CORROSION WAS REMOVED FROM SEVERAL FACES, BORES AND OV ERSIZED REPAIR BUSHINGS WERE INSTALLED PER ERA 397635-14 AT HMV. 2 L 7 2 4F RT A16WE 2001080100196 20010801 00196 NM 2001 8 1 DL73K010966 1 20010613 A 7722 SELOC19DJ INDICATOR BOEING 737 737232 1384475 NM COCKPIT FAILED A DALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 27 321DL 23093 ABORTED T/O DUE TO NR 2 EGT FAILED TO ZERO AT T/O POWER, APPROX 50 KTS. RETURNED TO GATE. REPLACED NR 2 ENGINE EGT IND ICATOR. RAN ENGINE TO T/O POWER. ALL INDICATIONS CHECK NORMAL. EGT OPN NOW OK. 2 L 7 2 4F RT A16WE 2001080100197 20010801 00197 EA 2001 8 1 COMA0160540 1 20010729 A 5610 NP1393215 WINDSHIELD CNDAIR CL600 CL6002B19 EA CRACKED A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 807CA 3108 7364 PILOTS WINDSHIELD CRACKED.REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 2001080100198 20010801 00198 EA 2001 8 1 COMA0160539 1 20010729 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 929CA 7035 EMERGENCY LIGHT ROW 11 IS INOPERABLE.DEFERRED MAINTENANCE PER M.E.L. 2 L 7 2 4F RT A21EA 2001080100199 20010801 00199 EA 2001 8 1 COMA0160538 1 20010727 A 2720 RUDDER CNDAIR CL600 CL6002B19 EA A COMA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 01 797CA 7344 VERY NOTICEABLE YAWING MOTION INFLIGHT.COULD NOT DUPLICATE. CHEDCKED YAW DAMPNERS AND RUDDER SYSTEM. NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 2001080100200 20010801 00200 NM 2001 8 1 DL73K010979 1 20010615 A 5314 6546877130 KEELBEAM BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 328DL 23100 THE RT STRINGER 18A SHEAR BEAM AT FS 727 WAS FOUND WITH A 2 INCH CRACK. THE CRACK IS SIMILAR TO BAC S/B 737-53-1170, EX CEPT THE SB IS NOT EFFECTIVE FOR THIS AIRCRAFT. THE CRACK WAS STOP DRILLED AND REPAIRED WITH A STEEL REPAIR CHANNEL PER ER/A 381094-14, REV C. 2 L 7 2 4F RT A16WE 2001080100206 20010801 00206 EA 2001 8 1 COMA0160537 1 20010726 A 2740 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 EA MALFUNCTIONED A COMA O OTHER F FLT CONT AFFECTED UK UNKNOWN 1 SO 01 999CA 15347 1472 7230 STABILIZER CHANNEL #2 WILL NOT ENGAGE.REPLACED THE TRIM ACTUATOR M.C.U. 2 L 7 2 4F RT A21EA 2001080100216 20010801 00216 EA 2001 8 1 COMA0160536 1 20010731 A 5346 60135006 WEB CNDAIR CL600 CL6002B19 EA CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 927CA 17670 7031 DURING COMPLIANCE OF EO 53-021 (VISUAL INSPECTION OF THE ENGINE SUPPORT BEAM) FOUND UPPER WEB OF ENGINE SUPPORT BEAM CRA CKED.REPAIRED THE ENGINE SUPPORT BEAM IN ACCORDANCE WITH CRJ REO 601-53-61-345. 2 L 7 2 4F RT A21EA 2001080100217 20010801 00217 2001 8 1 01FDEA00627 4 20010731 A 3414 PITOT LINE AIRBUS 310 A310222 3930315 EU DIRTY A FDEA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 SO 25 452FE 313 01-254 AIRSPEED IND ON T/O ROLL ON CAPT'S PFD IND. STBY A/S & F/O'S A/S IND 75-80 KNOTS. BLEW AIR INTO PITOT SYSTEM, D IRT CAME OUT. PERF LEAK CK OF ADC 1 PITOT LINE, AIRSPEED ON PILOTS PFD WORK NORM. 2 L 7 2 4F RT A35EU 2001081500169 20010815 00169 NM 2001 8 15 01FDEA00630 1 20010731 A 5312 PRESSURE PANEL BOEING 727 72722 1384002 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 149FE 19087 CRACK INSIDE RIGHT NOSE WHEEL WELL SIDE PANEL BS 268, RBL 23, WL 188. *S/D* REMOVED AND REPLACED SKIN PER SRM 51-30-2. 2 L 7 3 4F A3WE 2001080100218 20010801 00218 NM 2001 8 1 01FDEA00633 1 20010731 A 5330 SKIN BOEING 727 72722 1384002 NM FUSELAGE LOWER BULGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 149FE 19087 N 306 BULGE IN SKIN NEAR LAP JOINT AT BS 298 BETWEEN STR 17L & 18L. ** S/D ** COMING 2 L 7 3 4F A3WE 2001080100219 20010801 00219 NM 2001 8 1 DL73K010980 1 20010615 A 5310 65479564 DOOR FRAME BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 331DL 23103 THE UPPER SILL BEAM OF THE C2 DOOR CUTOUT SURROUND STRUCTURE WAS FOUND WITH A CRACK IN THE BEAM WEB AT FS 818. 2 L 7 2 4F RT A16WE 2001080100220 20010801 00220 NM 2001 8 1 DL73K010982 1 20010615 A 2133 7110035 OUTFLOW VALVE BOEING 737 737247 138448D NM CABIN PRESSURE FAILED A DALA O OTHER O OTHER CL CLIMB 1 SO 27 242WA 158398 23516 AT 23,000 FEET STARTED TO FEEL CABIN RISING AND GOT THE ALT HORN. CABIN WAS AT 11,000 FEET AND CLIMBING 1000 FPM. STAR TED DESCENT AUTO SYS FAILED TO STBY BUT CABIN KEPT CLIMBING UNTIL A/C PASSED THROUGH ACTUAL ALTITUDE. REPLACED PRESSURE CONTROLLER AND AFT OUTFLOW VALVE PER MM. 2 L 7 2 4F A16WE 2001080100221 20010801 00221 NE 2001 8 1 DL73K010986 2 20010616 A 7532 658385 BLEED VALVE BOEING 737 737232 1384475 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE MALFUNCTIONED A DALA O OTHER O OTHER TO TAKEOFF 1 SO 27 329DL 23101 709226 SHORTLY AFTER T/O NR 2 ENGINE EGT REACHED 640 FOR 3 TO 4 SECONDS. INSPECTED INLET AND EXHAUST, NO DEFECTS. CHECKED EPR SYSTEM WITH P/S TEST BOX INDICATION GOOD. NO LEAKS. LUBED BLEED VALVES AND REPLACED PRBC PERFORMED PFHB TEST E - J AN D X. TESTS GOOD. RAN ENGINE FOR 3 MINUTES EGT WITHIN LIMITS. 2 L 7 2 4F 4 F RT A16WE E2EA 2001080100222 20010801 00222 NM 2001 8 1 DL73K011052 1 20010624 A 3260 SAFETY SWITCH BOEING 737 737247 138448D NM MLG FAULTY A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 242WA 23516 A/C DEPRESSURIZED, HAD TO DESCEND TO CONTROL CABIN. CABIN ALTITUDE REACHED 13,000 FEET WITH A/C DESCENDING BACK DOWN TH ROUGH 13,000 FEET AND THEN DESCENDED WITH AIRCRAFT TO TOUCHDOWN. REPLACED LDG SAFETY SWITCHES. OPS CHECKS GOOD. 2 L 7 2 4F A16WE 2001080100223 20010801 00223 NM 2001 8 1 DL73K011065 1 20010623 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 313DL 23085 THE FUSELAGE SKIN AND BONDED DOUBLER ARE CRACKED AT THE R-2 DOOR UPPER HINGE CUTOUT. THE UNDERLYING BEARSTRAP IS NOT DA MAGED. THE CRACK MEASURES .375 INCH. REPAIRED PER ER/A 381177-14. 2 L 7 2 4F RT A16WE 2001080100226 20010801 00226 NE 2001 8 1 DL73K011093 2 20010629 A 7200 JT8D15AHK ENGINE BOEING 737 737232 1384475 NM PWA JT8 JT8D15 52051 NE NR 1 FAILED A DALA C ABORTED TAKEOFF Y ENGINE STOPPAGE TO TAKEOFF 1 SO 27 324DL 45253 23096 709131 NR 1 ENGINE FAILURE ON TAKEOFF. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A16WE E2EA 2001080100228 20010801 00228 NM 2001 8 1 DL73K011100 1 20010702 A 5512 SKIN BOEING 737 737232 1384475 NM HORZ STAB DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 317DL 23089 LEADING EDGE OF LT HORIZONTAL STAB HAD SKIN DENTED OUT OF LIMITS. 2 L 7 2 4F RT A16WE 2001080100234 20010801 00234 NM 2001 8 1 DL73K011140 1 20010709 A 5714 6545410225 DOUBLER BOEING 737 737247 138448D NM WING BOX CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 INSPECTION OF THE LONGITUDINAL FLOORBEAM AT RBL 24 ABOVE THE CENTER WING BOX REVEALED A CRACK IN THE REINFORCING DOUBLER OF THE BEAM WEB AT FS 678 ADJACENT TO A CABLE CUTOUT. 2 L 7 2 4F A16WE 2001080100237 20010801 00237 NM 2001 8 1 DL73K011157 1 20010712 A 2913 623337 PUMP BOEING 737 737232 1384475 NM NR 2 ENGINE DEFECTIVE A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 311DL 23083 HYD SYSTEM A PUMP 2/ LOW PRESSURE. REMOVED AND REPLACED RT EDP, REPLACED CASE DRAIN AND A SYS FILTERS SERV HYD, LEAK CK S GOOD. 2 L 7 2 4F RT A16WE 2001080100238 20010801 00238 NM 2001 8 1 DL73K011166 1 20010712 A 3350 BPS73 POWER SUPPLY BOEING 737 737232 1384475 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 306DL 23078 EMERGENCY LIGHTS AT ROWS 1 - 4 AND ROWS 10 - 16 INOP. FOUND BAD PWR SUPPLY FOR ROWS 1 - 4 AND A BAD SLICE AT ROW 10. R EPLACED SPLICE AND PWR SUPPLY. CHECKS GOOD. 2 L 7 2 4F RT A16WE 2001080100239 20010801 00239 NM 2001 8 1 DL73K011180 1 20010717 A 5342 ATTACH FITTING BOEING 737 737232 1384475 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 317DL 23089 THE FUSELAGE CLEVIS LUGS AND THE VERTICAL FIN ATTACHMENT LUGS WERE FOUND CORRODED IN THE BORES AND THE FACES. THE CORRO SION WAS REMOVED AND OVERSIZED BUSHINGS INSTALLED. THE DAMAGE WAS FOUND DURING HMV. 2 L 7 2 4F RT A16WE 2001080100240 20010801 00240 NM 2001 8 1 DL73K011184 1 20010717 A 2120 AIR DUCT BOEING 737 737232 1384475 NM CABIN LEAKING A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 316DL 23088 FUMES IN CABIN AND COCKPIT. STRONGEST SMELL IN FIRST 5 ROWS OR SO. SMELLED LIKE RUBBER BURNING. NOTICED AT 2500 FT AB OUT 2 MINUTES AFTER DEPARTURE. FOUND GASPER AIR DUCT LEAKING AND RETAPED. 2 L 7 2 4F RT A16WE 2001080100241 20010801 00241 NM 2001 8 1 DL73K011199 1 20010719 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 304DL 23076 FOUND FUSELAGE SKIN AT LOWER FORWARD CORNER OF L-2 DOOR CUTOUT WITH 0.75 INCH CRACK. ALSO FOUND BEARSTRAP AT THAT LOCAT ION WITH 1.5 INCH CRACK. REPAIRED PER SRM 53-30-3. 2 L 7 2 4F RT A16WE 2001080100252 20010801 00252 NM 2001 8 1 DL73K011228 1 20010725 A 2131 7638101 CONTROLLER BOEING 737 737232 1384475 NM CABIN PRESSURE FAILED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 332DL 23104 UNABLE TO PRESSURIZE AIRCRAFT WITH LEFT PACK. REPLACED PRESSURIZATION CONTROLLER, GROUND OPS OK. CLEANED RT PACK COMPR ESSOR DISCHARGE SW S2. RT PACK OPS OK. 2 L 7 2 4F RT A16WE 2001080100257 20010801 00257 NM 2001 8 1 DL73K011229 1 20010725 A 7120 654685014 SUPPORT FITTING BOEING 737 737232 1384475 NM ENGINE MOUNT DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 301DL 23073 THE FWD ENGINE MOUNT SUPPORT FITTING ASSY WAS FOUND WITH DAMAGED MOUNT HOLES. THE HOLES WERE OVERSIZED TO CLEAN UP ALL DAMAGE. REPAIR PER ER/A 402105-14AD. 2 L 7 2 4F RT A16WE 2001080100261 20010801 00261 EU 2001 8 1 MTNA200109 1 20010731 A 2612 D890N FIRE LOOP FOKKER F27 F27MK500 4990629 EU A MTNA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SO 33 716FE 10471 During take off and climb out of LCK. the right engine fire warning light illuminated. The crew performed the emergency check list procedures, declared an emergency and returned to LCK. The aircraft landed with out further incident. 2 H 7 2 4T A817 2001080100262 20010801 00262 NM 2001 8 1 DL757010927 1 20010607 A 3330 1308 LIGHT BOEING 757 757232 1384965 NM CABIN BURNED OUT A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 604DL 22811 BURNING SMELL BY AFT GALLEY JUMPSEAT READING LIGHT. LIGHT WAS TURNED OFF AND SMELL DISSIPATED. INSPECTED SWITCH ASSY L IGHT ASSY WIRES AND ALL ATTACHING PIECES FOR CONDITION AND SECURITY. NO DEFECTS FOUND. INSPECTED BULB. FOUND BULB AT END OF SERVICE LIFE. FOUND ADJACENT BUGEYE HOSE LOOSE IN CEILING. REATTACHED HOSE. REBULBED AND OPERATED LIGHT. NOW CKS OKAY. 2 L 7 2 4F RT A2NM 2001080100263 20010801 00263 NM 2001 8 1 DL757010939 1 20010609 A 5220 80330033 RESERVOIR BOEING 757 757232 1384965 NM L2 DOOR DISCHARGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 6700 30337 23745 WHILE ATTEMPTING TO CLOSE THE L2 PASSENGER DOOR TO FACILITATE MAINTENANCE ON THE DOOR HINGE COVER PLATE,THE DOOR EMERGEN CY POWER RESERVOIR WAS INADVERTENTLY DISCHARGED. THE POWER RESERVOIR WAS REPLACED AS PER THE APPLICABLE MAINTENANCE MAN UAL AND WAS RIGGED PER MANUAL. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2001080100264 20010801 00264 CE 2001 8 1 60701N28CK 1 20010608 A 3230 1EN18 SWITCH LEAR 25 25 5170506 CE TRUNNION DEFECTIVE E KKFA K NONE O OTHER IN INSP/MAINT 1 GL 23 28CK 045 AIRCRAFT HYDRAULIC PRESSURE FLUCTUATES. FOUND RIGHT M.L.G. TRUNNION SWITCH OUT OF RIG CAUSING INBOARD GEAR DOORS TO CYC LE SEVERAL TIMES DURING RETRACTION. ADJUSTED RIGHT M.L.G. TRUNNION SWITCH AND PERFORMED GEAR RETRACTIONS PER THE LEARJE T SERVICE MANUAL. OPERATION CHECK AND HYDRAULIC PRESSURE WAS NORMAL. 2 L 7 2 4J A10CE 2001080100265 20010801 00265 CE 2001 8 1 AJP2001F00000 1 20010517 A 5712 082217579 RIB CESSNA 310 310R 2074245 CE LT WING CRACKED A AJPA K NONE O OTHER IN INSP/MAINT 1 GL 11 1914G 7829 310R0059 WHILE PERFORMING INSPECTION, SHORT CRACKS (APPROX .1250 - .3750), FOUND IN CENTER RIB, CRACKS ARE AS DESCRIBED AND ILLUS TRATED IN SB. SUSPECTED CAUSE: EXCESSIVE CYCLES, EXCESSIVE YAW, WHILE LANDING AND TAXIING. NO AD OR STC RELATIONSHIP ADDRESSES INSPECTION AREAS AND REPAIR PROCEDURES. 1 L 7 2 3O 3A10 2001080100266 20010801 00266 CE 2001 8 1 AJP2001F00001 1 20010517 A 5712 082217574 RIB CESSNA 310 310R 2074245 CE RT WING CRACKED A AJPA K NONE O OTHER IN INSP/MAINT 1 GL 11 1914G 7829 310R0059 WHILE PERFORMING INSPECTION, SHORT CRACKS (.1250 - .3750) FOUND IN CENTER RIB, CRACKS ARE AS DESCRIBED AND ISSUSTRATED I N SB. SUSPECTED CAUSE: EXCESSIVE CYCLES, EXCESSIVE YAW WHILE LANDING/ TAXIING. NO AD OR STR RELATED TO FAILURE. 1 L 7 2 3O 3A10 2001080100267 20010801 00267 CE 2001 8 1 AJP2001F00002 1 20010517 A 5730 08220009 SKIN CESSNA 310 310R 2074245 CE WINGS CRACKED A AJPA K NONE O OTHER IN INSP/MAINT 1 GL 11 1914G 7829 310R0059 WHILE PERFORMING INSPECTION, CRACKS DISCOVERED IN LEFT AND RIGHT HAND UPPER INBOARD SKINS, THESE CRACKS ARE APPROX 2 INC HES LONG (RIGHT) AND 4.5 INCHES LONG (LEFT) CRACKS IN NEARBY LOCATION ADDRESSED BY SB, SUSPECTED CAUSE: EXCESSIVE YAW LANDING/TAXIING, EXCESSIVE CYCLES. 1 L 7 2 3O 3A10 2001080100268 20010801 00268 NE 2001 8 1 B2P2001F00000 3 20010702 A 6111 C7921 BEARING BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA HARTZL HCE4A HCE4A3I NE BLADE BEARING DAMAGED B B2PR K NONE O OTHER IN INSP/MAINT 1 SO 17 49543 10465 3463 UE181 HJ440 PROPELLER WAS RECEIVED FOR O/H WITH EXCESSIVE GREASE LEAKAGE FROM ALL BLADES. WHEN PROP WAS DISASSEMBLED, THE HUB UNIT WAS FILLED WITH EXCESSIVE AMOUNTS OF GREASE. UPON FURTHER INSPECTION, THE GREASE WAS FOUND TO CONTAIN SEVERAL PIECES OF THE BLADE BEARING RACE. THE BEARING RACE WAS SHATTERED INTO SEVERAL SMALL PIECES. THE SHATTERED BEARING CAUSED DAMAGE D TO THE HUB RETENTION AREA. 2 L 7 2 4T 3 T RT A24CE E2NE 5 C P10NE 2001080100269 20010801 00269 SW 2001 8 1 BSA2001F00000 1 20010603 A 2910 27810322682 HYDRAULIC LINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE331* 01514 WP HYD SYSTEEM CHAFED A BSAA K NONE O OTHER IN INSP/MAINT 1 NM 05 60NE 760B HYDRAULIC PRESSURE LOW LIGHT CAME ON DURING CLIMBOUT APPROX 25 MILES OUT. CREW SELECTED GEAR DOWN. ALL HYDRAULIC PRESS URE WAS LOST SHORTLY AFTER THAT. CREW COMPLETED FLAPS UP LANDING WITH NO FURTHER INCIDENT. APPARENT CAUSE: HYDRAULIC F LUID LEAK CAUSED LOSS OF ALL HYDRAULIC FLUID. CORRECTIVE ACTION: LINE WAS REPLACED. FAILED HYDRAULIC LINE HAD CHAFED AGAINST FUEL FEED LINE IDENTIFICATION TAPE UNTIL WALL THICKNESS WAS THIN ENOUGH TO ALLOW LINE TO CRACK. FUEL LINE DID N OT SUFFER ANY APPRECIABLE WEAR. REPLACING ALL OF THESE RIGID PART NUMBER TUBES WITH FLEX LINES THROUGH ATTRITION IAW SB . 2 L 7 2 4T 3 T RT A8SW E2WE 2001080100270 20010801 00270 SW 2001 8 1 BSA2001F00001 1 20010510 A 2121 A047D67 FAN SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE331* 01514 WP CABIN FAILED A BSAA K NONE O OTHER IN INSP/MAINT 1 NM 05 704C 39 704 DURING TAXI INTO STATION, THE FRESH AIR FAN QUIT. CREW NOTICED A BURNING SMELL, TURNED THE FRESH AIR FAN SWITCH OFF AND PULLED FAN CIRCUIT BREAKER. FRESH AIR FAN BLADE ASSEMBLY FAILED. CORRECTION ACTION: FOUND BLOWER FAN BROKEN, THIS HA D JAMMED THE MOTOR, CAUSING THE MOTOR TO GET HOT. THE FAN WAS REPLACED, AND THE MOTOR WAS GROUND RUN FOR AN EXTENDED TI ME TO VERIFY OPERATION. NO FURTHER DEFECTS WERE NOTED. THIS IS THE THIRD FAILURE OF THIS FAN BLADE ASSEMBLY. 2 L 7 2 4T 3 T RT A8SW E2WE 2001080100271 20010801 00271 NM 2001 8 1 2001F00153 1 20010625 A 2913 651782111 PUMP BOEING 727 727225 1384077 NM NR1&2 ENGINE FAILED A MYWA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SO 19 802MA 22433 SHORTLY AFTER GEAR RETRACTION LOST HYD SYSTEM 'A'. ACCOMPLISHED ABNORMAL PROCEDURE. RETURNED TO DFW. REMOVED AND REPL ACED NR 1 AND NR 2 ENGINE DRIVEN HYD PUMP. RUN AND LEAK CHECK. REMOVED AND REPLACED NR 1 AND NR 2 ENGINE HYD FILTER, R UN OPS AND LEAK CHECK IAW 29-11-33 ENGINE PUMP, IAW 29-11-62 FILTER. REPLACED DAMAGED 'A' SYSTEM PRESSURE PACKAGE IAW 2 9-11-61, LEAK CHECK GOOD. REMOVED AND REPLACED 'A' SYSTEM RETURN FILTER IAW 29-11-102, LEAK CHECK GOOD. SERVICED HYDRA ULIC SYSTEM IAW 29-11-101. MANUAL EXT RETURNED TO FLT STATUS IAW 32-34-0 PAGE 3. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001080100272 20010801 00272 NM 2001 8 1 BSY2001F00000 1 20010601 A 3260 327 BULB PIPER PA60 PA60600 7106001 NM MLG INDICATOR BURNED OUT A BSYA K NONE O OTHER IN INSP/MAINT 1 GL 07 8073J 600556180 RIC M.I.R. LEFT GEAR, NO DOWN AND LOCK LIGHT. REMOVED AND REPLACED BULB. OPS CHECK GOOD. 1 M 7 2 3O RT A17WE 2001080100273 20010801 00273 CE 2001 8 1 BSY2001F00001 1 20010509 A 3230 583800901 MOTOR BEECH 58 58 1152740 CE MLG MALFUNCTIONED E BSYA K NONE O OTHER IN INSP/MAINT 1 GL 07 1847F TH1291 (MDW) M.I.R. GEAR SELECTED DOWN, NOTHING HAPPENED AT FIRST, THEN CAME DOWN OK. MAINTENANCE JACKED AIRCRAFT, COULD NOT DUPLICATE. REMOVED AND REPLACED LANDING GEAR MOTOR AND DYNAMIC BRAKE RELAY FOR PRECAUTIONARY MEASURES. 1 L 7 2 3O 3A16 2001080100274 20010801 00274 CE 2001 8 1 BSY2001F00002 1 20010509 A 3230 SM5007 RELAY BEECH 58 58 1152740 CE MLG MALFUNCTIONED E BSYA K NONE O OTHER IN INSP/MAINT 1 GL 07 1847F TH1291 (MDW) M.I.R. GEAR SELECTED DOWN, NOTHING HAPPENED AT FIRST, THEN CAME DOWN, OK. MAINTENANCE JACKED AIRCRAFT, COULD NOT DUPLICATE. REMOVED AND REPLACED LANDING GEAR MOTOR AND DYNAMIC BRAKE RELAY FOR PRECAUTIONARY MEASURES. 1 L 7 2 3O 3A16 2001080100275 20010801 00275 NM 2001 8 1 BSY2001F00003 1 20010530 A 7603 600035549 THROTTLE CABLE PIPER PA60 PA60600 7106001 NM RT ENGINE BROKEN E BSYA K NONE O OTHER IN INSP/MAINT 1 GL 07 6076L 600713796122 RIC M.I.R. RIGHT ENGINE THROTTLE CABLE BROKE ON CLIMB OUT, RETURNE TO AIRPORT. REMOVED AND REPLACED THROTTLE CABLE O PS GOOD. 1 M 7 2 3O RT A17WE 2001080100276 20010801 00276 NM 2001 8 1 2001F00154 1 20010629 A 2750 PULLEY BOEING 727 727225 1384077 NM T/E FLAP BINDING A MYWA A UNSCHED LANDING F FLT CONT AFFECTED TO TAKEOFF 1 SO 19 803MA 22434 AFTER TAKEOFF, DURING FLAP RETRACTION, FLAP AT 2 DEGREE OUTBOARD FLAPS WENT ASYMMETRIC. RETURNED TO MIAMI. TROUBLESHOT SYSTEM. FOUND PULLEY AT NR 7 FLAP CANOE BINDING, CAUSING IMPROPER INDICATION. FREED PULLEY, PERFORMED OPERATIONAL CHE CK OF FLAP SYSTEM SEVERAL TIMES IAW 27-51-0. ALL FUNCTIONAL CHECKS NORMAL ON GROUND. FLAPS RESET TO NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001080100277 20010801 00277 NM 2001 8 1 2001F00155 1 20010629 A 2741 32EN614 SWITCH BOEING 727 727225 1384077 NM STABILIZER SHORTED A MYWA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 19 802MA 22433 DURING TAKEOFF ROLL WHEN THRUST LEVER ADVANCED TAKEOFF WARNING HORN SOUNDED. AIRCRAFT TAKEOFF CONFIGURATION CHECK, HORN COULD NOT BE SILENCED. ABORTED TAKEOFF. TROUBLESHOT SYSTEM FOUND STABILIZER UPPER LIMIT TAKEOFF WARNING SWITCH INOPER ATIVE. REMOVED AND REPLACED SWITCH IAW MM 32-26-24. OPS CHECKED GOOD IAW MM 31-26-01. RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 3 4F A3WE 2001080100278 20010801 00278 NM 2001 8 1 2001F00156 1 20010705 A 5270 C21002 SWITCH BOEING 727 727276 138408R NM AIRSTAIR FAULTY A FX7A C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 19 908PG 20951 DURING TAKEOFF, ROLL AFT AIRSTAIR LIGHT INDICATION ILLUMINATED. AIRCRAFT ABORTED TAKEOFF WITHOUT INCIDENT OR EMERGENCY. AIR AIRSTAIR SYSTEM INSPECTED AND TROUBLESHOT TO FAULTY MICROSWITCH INDICATION, AFT AIRSTAIR LIGHT ENTERED INTO DMI PE R MEL 52-6. AIRCRAFT RETURNED TO SERVICE WITH 60 MINUTE DELAY. (M) 2 L 7 3 4F RT A3WE 2001080100279 20010801 00279 NM 2001 8 1 2001F00157 1 20010627 A 5753 651924550A FLAP BOEING 727 727231 1384079 NM RT WING DAMAGED A FX7A K NONE D INFLIGHT SEPARATION DE DESCENT 1 SO 19 24343 21630 RIGHT INBOARD TRAILING EDGE FLAP HALF OF HONEYCOMB MISSING AND OTHER HALF DAMAGED, UPON LANDING IN (GYE). ALL THREE ENG INES INSPECTED. REMOVED AND REPLACED FLAP ASSEMBLY OPS AND RIGGED IAW MM 27-51-00. RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 3 4F A3WE 2001080100280 20010801 00280 SO 2001 8 1 BTV2001F00000 1 20010529 A 2770 BRACKET GULSTM G1159 G1159B 3953535 SO RUDDER FRACTURED B BTVR K NONE O OTHER IN INSP/MAINT 1 GL 23 344AA 123 DURING A ROUTINE SCHEDULED INSPECTION, A MECHANIC NOTED THE RUDDER GUST LOCK HOOK SUPPORTING STRUCTURE WAS FRACTURED. F URTHER INVESTIGATION FOUND THREE PIECES THAT MAKE UP THE 1159C20509 ASSEMBLY (2 EA 115920509-13 ANGLES AND 1 EA 1159C205 09-35 ANGLE) WERE FRACTURED. SINCE THE GUST LOCK WAS STILL FUNCTIONAL THE OPERATOR WASN'T AWARE OF THE PROBLEM, THEREFO RE IT CANT BE DETERMINED WHEN OR HOW THE DEFECT OCCURRED. MOST LIKELY THE RUDDER GUST LOCK WAS OVERSTRESSED AT SOME POI NT EITHER BY USE USING HYDRAULIC SYSTEM POWER OR SOME LARGE, EXTERNAL FORCE. (WIND). NEW PARTS WERE PROCURED AND INSTAL LED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A12EA 2001080100281 20010801 00281 SO 2001 8 1 BTV2001F00002 1 20010629 A 3240 AHM10195 ROTOR DUNLOP GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE BRAKE ASSY FAILED B BTVR K NONE O OTHER IN INSP/MAINT 1 GL 23 588GA XP016 588 DURING A ROUTINE SCHEDULED BRAKE INSPECTION IT WAS NOTED THAT NR 3 BRAKE, OUTBOARD DRIVE ROTOR KEYS WERE FRACTURED. AFT ER REMOVING THE WHEEL IT WAS NOTED THAT ALL EIGHT FORWARD SIDE DRIVE CLIPS WERE FAILED. MFG IS INVESTIGATING. A SERVIC EABLE BRAKE WAS INSTALLED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A12EA E00057EN 2001080100282 20010801 00282 NM 2001 8 1 2001F00158 1 20010501 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 29SW 21340 FOUND CORROSION ON THE FUSELAGE SKIN AT BS 967, STRINGER 27R. (M) 2 L 7 2 4F A16WE 2001080100283 20010801 00283 NM 2001 8 1 CW12001F00000 1 20010502 A 3010 BYLB521581 ANTI-ICE VALVE AMD FALC50 FALCON2000 2730170 NM WING INTERMITTENT B CW1R K NONE O OTHER IN INSP/MAINT 1 EA 11 790M 2 19 INTERMITTENT FAILURE OF THE WING ANIT-ICE SYSTEM CAUSING COCKPIT INDICATION TO GO FROM GREEN TO AMBER. SUPPORT VALVE IS STICKING. 2 K 7 3 4F RT A50NM 2001080100284 20010801 00284 NM 2001 8 1 CW12001F00001 1 20010502 A 3010 BYLB521881 ANTI-ICE VALVE AMD FALC50 FALCON2000 2730170 NM WING FAILED B CW1R K NONE O OTHER IN INSP/MAINT 1 EA 11 790M 19 INTERMITTENT FAILURE OF THE WING ANTI-ICE SYSTEM, CAUSING COCKPIT INDICATION TO GO FROM GREEN TO AMBER. SUSPECT VALVE I S STICKING. 2 K 7 3 4F RT A50NM 2001080100285 20010801 00285 NM 2001 8 1 CW12001F00002 1 20010502 A 3010 BYLB521881 ANTI-ICE VALVE AMD FALC50 FALCON2000 2730170 NM WING FAILED B CW1R K NONE O OTHER IN INSP/MAINT 1 EA 11 790M 32 19 INTERMITTENT FAILURE OF THE WING ANTI-ICE SYSTEM CAUSING COCKPIT INDICATION TO GO FROM GREEN TO AMBER. SUSPECT VALVE IS STICKING. 2 K 7 3 4F RT A50NM 2001080100286 20010801 00286 NM 2001 8 1 2001F00159 1 20010501 A 5313 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 29SW 21340 FOUND CRACK IN PASSENGER CABIN BS 727 PLUS 9 AT STRINGER NR 1. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-3 FIGURE 3. (M) 2 L 7 2 4F A16WE 2001080100287 20010801 00287 NM 2001 8 1 CW12001F00003 1 20010502 A 3010 BYLB521881 ANTI-ICE VALVE AMD FALC50 FALCON2000 2730170 NM WING INTERMITTENT B CW1R K NONE O OTHER IN INSP/MAINT 1 EA 11 790M 3321 19 INTERMITTENT FAILURE OF THE WING ANTI-ICE SYSTEM CAUSING COCKPIT INDICATION TO GO FROM GREEN TO AMBER. SUSPECT VALVE IS STICKING. 2 K 7 3 4F RT A50NM 2001080100288 20010801 00288 NM 2001 8 1 2001F00160 1 20010501 A 5313 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 29SW 21340 FOUND CRACK IN PASSENGER CABIN BS 767 STRINGER 9R. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-3 FIGURE 3. (M) 2 L 7 2 4F A16WE 2001080100289 20010801 00289 CE 2001 8 1 DEL2001F00000 1 20010419 A 3260 8A1011 SWITCH LEAR 35 35A 5170602 CE COCKPIT INOPERATIVE A DELA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CE 03 902JC 227 AT APPROX VR WHEN THE WHEELS LEFT GROUND, NOTICED SIGNIFICANTLY HIGHER LEVEL OF WIND NOISE. CONTINUED TO FLY THE AC UNT IL WE WERE AT A SAFE ALTITUDE. LOOKED IN BACK OF AC AND NOTICED SOME FAINT SMOKE, SO WE TOOK OUT OUR SMOKE GOGGLES AND HAD THEM STANDING BY AS SMOKE WAS NOT THICK, BUT STILL THERE. WE NOTICED THE CABIN ALTITUDE WAS NOT CLIMBING, THE DIFF ERENTIAL READ AROUND 6.5 PSID AND THE ACTUAL AC ALTITUDE WAS AT 10,000. CYCLED THE LEFT SWITCH FROM ON TO EMERG TO OFF AND BACK TO ON. DID THE SAME WITH THE RIGHT SWITCH. AT THAT TIME THE EXTREMELY LOUD SOUND OF RUSHING AIR STOPPED AND T HE EXTREME HEAT SLOWLY STOPPED. WE WERE VECTORED BACK TO APRT FOR UNEVENTFUL APPROACH AND LANDING. 2 L 7 2 4F A10CE 2001080100290 20010801 00290 NM 2001 8 1 2001F00161 1 20010501 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 SW 21 29SW 21340 FOUND FUSELAGE SKIN WAS FOUND DENTED AT BS 429 BETWEEN STRINGER 21R AND STRINGER 22R. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-30-3 FIGURE 1. (M) 2 L 7 2 4F A16WE 2001080100291 20010801 00291 CE 2001 8 1 DEL2001F00001 1 20010419 A 3610 4201654 VALVE LEAR 35 35A 5170602 CE BLEEDAIR INOPERATIVE E DELA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 03 902JC 227 AT APPROX VR WHEN THE WHEELS LEFT GROUND, NOTICED SIGNIFICANTLY HIGHER LEVEL OF WIND NOISE. CONTINUED TO FLY THE AC UNT IL WE WERE AT A SAFE ALTITUDE. LOOKED IN BACK OF AC AND NOTICED SOME FAINT SMOKE, SO WE TOOK OUT OUR SMOKE GOGGLES AND HAD THEM STAND BY AS SMOKE WAS NOT THICK, BUT STILL THERE. WE NOTICED THE CABIN ALTITUDE WAS NOT CLIMBING, THE DIFFEREN TIAL READ AROUND 6.5 PSID AND THE ACTUAL AC ALTITUDE WAS AT 10,000. CYCLED THE LEFT SWITCH FROM ON TO EMERG TO OFFAND B ACK TO ON. DID THE SAME WITH THE RIGHT SWITCH AT THAT TIME THE EXTREMELY LOUD SOUND OF RUSHING AIR STOPPED AND THE EXTR EME HEAT SLOWLY STOPPED. WE WERE VECTORED BACK TO APRT FOR UNEVENTFUL APPROACH AND LANDING. 2 L 7 2 4F A10CE 2001080100292 20010801 00292 CE 2001 8 1 DIN2001F00000 1 20010625 A 2100 66002101 CHECK VALVE LEAR 35 35A 5170602 CE AIR INLET MISLOCATED B DINR O OTHER O OTHER NR NOT REPORTED 1 EA 13 258G 5490 443 CHECK VALVES ON LEFT SIDE, RIGHT SIDE OF CABIN INSTALLED WITH HINGE NOT AT 12 OCLOCK POSITION. RIGHT VALVE AT 5 OCLOCK, LEFT VALVE AT 2 OCLOCK. FACTORY ORIGINAL TORQUE SEAL WITH INSPECTORS STAMP ON IT HAD NEVER BEEN BROKEN. VALVES REMOVE D AND INSPECTED AND REINSTALLED IN CORRECT POSITION. 2 L 7 2 4F A10CE 2001080100293 20010801 00293 CE 2001 8 1 DXT2001F00000 1 20010524 A 3230 664062217 CONTROL CABLE CESSNA 560 560XL 2076702 CE EMR GEAR RELEASE CHAFED B K NONE O OTHER IN INSP/MAINT 1 GL 07 670QS 20 5605170 CABLE RUN JUST FWD OF BATTERY COMPARTMENT, I/B SIDE OF HYDRAULIC PRESSURE LINE RUBBING ON BULKHEAD. 2 L 7 2 4F RT A22CE 2001080100294 20010801 00294 CE 2001 8 1 DXT2001F00001 1 20010614 A 3240 215671 BRAKE CESSNA 750 750 2076810 CE MLG LOOSE E DXTA K NONE O OTHER IN INSP/MAINT 1 GL 07 979QS 7500079 SPECIAL BOLTS BETWEEN STRIKER AND PISTON HOUSING WERE LOOSE AND WERE BACKED OFF APPROX 114 INCH. BRAKE TORQUE BUTTON HA S WORN A GROOVE AROUND THE INNER CIRCUMFERENCE AT THE WHEEL. 2 L 7 2 4J RT T00007WI 2001080100295 20010801 00295 NM 2001 8 1 E8V2001F00000 1 20010626 A 5520 65B05759 BALANCE WEIGHT BOEING BOEING 747 747400 NM STAB BROKEN B E8VY K NONE O OTHER IN INSP/MAINT 1 WP 03 405EV 38062 000992 27142 DURING C10 CHECK FOUND RIGHT HORIZONTAL STABILIZER PANEL BROKEN. AFTER INSPECTION FOUND RIGHT OUTBOARD ELEVATOR SUPPORT ING RIBS OF BALANCE WEIGHT WAS BROKEN. WHICH CAUSED THE BALANCE WEIGHT FALLING DOWN AND DAMAGED TO THE ELEVATOR PANEL. INFORMED MFG IMMEDIATELY AND NEGOTIATED FOR NEW ELEVATOR. REPLACED THE RIGHT OUTBOARD ELEVATOR PER MM AND CONDITION BA CK TO NORMAL. 2 L 7 4 4F RT A20WE 2001080100296 20010801 00296 2001 8 1 2001F00150 4 20010702 A 3454 20707503305 RECEIVER AIRBUS 300 A300B4203 3930306 EU VOR SYSTEM FAULTY A RJEF A UNSCHED LANDING O OTHER DE DESCENT 1 SO 25 59139 139 SAL - FLT TA807 - BEFORE APPROACH, THE NR 1 VOR NEEDLE WENT DIRECTLY TO THE EAST AND WEST POSITIONS AND THEN THE NR 2 VO R REMAINED IN THE 'TO' POSITION AND THE NR 1 AUTOPILOT DID NOT CAPTURE ALTITUDE. THE AIRCRAFT RETURNED TO SAL STATION F OR MAINTENANCE. MAINTENANCE PERSONNEL PERFORMED TROUBLESHOOTING PROCEDURES AND FOUND THE NR 1 AND NR 2 VOR RECEIVERS FA ULTY. REPLACED THE FAULTY RECEIVERS (S/N 2333 AND 1974) ACCORDING TO AMM 34-55-31. OPERATIONAL CHECK WAS PERFORMED, PE R AMM 22-12-00 AND IT WAS WORKING NORMALLY. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A35EU 2001080100297 20010801 00297 EU 2001 8 1 2001F00152 1 20010612 A 2130 9201A01 ACTUATOR AIRBUS 300 A300B4203 3930306 EU CABIN PRESSURE INOPERATIVE A WRNA K NONE J WARNING INDICATION TO TAKEOFF 1 SO 05 506TA 207 GROUND AUXILIARY FAULT LIGHT REMAINED ON AFTER TAKEOFF AND DURING CLIMB. AIRCRAFT LANDED NORMAL. REMOVED AND REPLACED AUXILIARY VALVE ACTUATOR IAW 21-31-17. OPS CHECKED GOOD. CLEAR DMI NR 1879. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A35EU 2001080100298 20010801 00298 CE 2001 8 1 C2XA01CL181 1 20010730 A 3260 1293640371 CIRCUIT BOARD BEECH 1900 1900D 1154162 CE CABIN FAILED A C2XA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 SW 27 87555 UE234 CLE FLIGHT# 3104 THE CREW REPORTED THE LANDING GEAR WARNING HORN FAILED TO SOUND OFF WHEN THE THROTTLES ARE RETARDED.MAI NTENANCE INSPECTED AND REPLACED PRINTED CIRCUIT BOARD # 173.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR S ERVICE.. 2 L 7 2 4T RT A24CE 2001080100299 20010801 00299 WP 2001 8 1 AALA016061 1 20010628 A 3350 3102806 LIGHT DOUG DC9 DC987 3022087 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 754RA 49641 CCI-LAX - MID CABIN EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED FUSE IN AFT OVERWING EXIT SIGN. OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 2001080100300 20010801 00300 WP 2001 8 1 AALA016062 1 20010619 A 3350 3102806 FUSE DOUG DC9 DC983 3022083 WP CABIN BLOWN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 882RA 49949 LAX-CCI - ROW 14-17 SEAT EMERGENCY LIGHTS AND FORWARD LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FUSE IN FORWARD LEFT OVERWING EMERGENCY EXIT LIGHT BATTERY PACK, OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 2001080100301 20010801 00301 SO 2001 8 1 FFK2001F00000 2 20010530 A 7414 10785126107 MAGNETO PIPER PA32 PA32R300 7103213 SO LYC 0540 IO540K1G5D 41532 SO ENGINE DAMAGED A FFKR K NONE O OTHER IN INSP/MAINT 1 SO 06 4451X 1135 32R7680018 PILOT REPORTED DEAG MAGNETO. INSPECTED MAGNETO TO BE MISSING INTERNAL GEAR TEETH. REMOVED AND REPLACED MAGNETO WITH SE RVICEABLE PART. 1 L 7 1 3O 3 O A3SO 1E4 2001080100302 20010801 00302 WP 2001 8 1 AALA20011247 1 20010613 A 2910 HYDRAULIC LINE DOUG DC9 DC982 3022082 WP HYDRAULIC SYS CHAFED A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 431AA 49343 ORD - FLT 390 - EN ROUTE ORD-LGA, ABOUT 20 MINUTES INTO FLIGHT LOST ALL FLUID AT RIGHT SIDE HYDRAULIC SYSTEM. RETURNED ORD AND LANDED WITHOUT FURTHER INCIDENT. REPLACED LINE AT RIGHT SIDE HYDRAULIC ELECTRIC PUMP. SERVICED HYDRAULIC SYSTE M. LEAK CHECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001080100303 20010801 00303 WP 2001 8 1 AALA20011259 1 20010617 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 505AA 49799 BOS - FOUND DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT PORTABLE ASSEMBLY INOPERATIVE. REPLACED EMERGENCY EXIT L IGHT PORTABLE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001080100304 20010801 00304 WP 2001 8 1 AALA20011261 1 20010619 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP A/C BAY BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 493AA 49731 DFW - DURING OVERNIGHT MAINTENANCE, TAIL COMPARTMENT EMERGENCY EXIT LIGHT ASSEMBLY AT SIDEWALL BROKEN. REPLACED EMERGEN CY EXIT LIGHT ASSEMBLY AT SIDE WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001080100306 20010801 00306 2001 8 1 FWT2001F00001 4 20010111 A 3416 A386891005 ALTIMETER DOUG DC8 DC871F 302199D WP COCKPIT ERRATIC A FWTA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 872SJ 46040 ON CLIMB OUT MIA AT 17,000 CAPT. ALTIMETER BECAME ERRACTIC AND STICKING AND GIVING ERRONEOUS READINGS, LOG BOOK, PAGE 20 1510. REMOVED AND REPLACED CAPT. ALTIMETER, ACCOMPLISHED PITOT STATIC SYSTEM LEAK CHECK AND OPS CHECK- FOUND NORMAL IAW MM. PITOT STATIC TESTER 10100164, BARFIELD CAL DATE 10-10-00, DUE RECALIBRATION, DATE 01-10-2001. 2 L 7 4 4F RT 4A25 2001080100308 20010801 00308 NE 2001 8 1 AALA20011308 2 20010627 A 7320 766342 VALVE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 1 ENGINE LEAKING A AALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 01 285AA 49297 CLT - FLT 1855 - EN ROUTE CLT-DFW - ON CLIMB-OUT, DETECTED LEFT SIDE ENGINE STALL. RETURNED CLT AND LANDED WITHOUT FURT HER INCIDENT. REPLACED LEFT SIDE ENGINE. REPLACED LEFT SIDE FUEL P AND D VALVE. ACCOMPLISHED LEAK CHECK. NO LEAKS NO TED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F A6WE E9NE 2001080100311 20010801 00311 SW 2001 8 1 GXPA0113 1 20010618 A 7921 OIL COOLER SWRNGN SA226 SA226TC 8780404 SW LT ENGINE FAILED E GXPA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 23 164GA TC281 AIRCRAFT RETURNED BACK TO AIRPORT DUE TO LEFT ENGINE OIL TEMP REDLINE AFTER TAKE OFF. CORRECTIVE ACTION: REMOVED AND R EPLACED LEFT ENGINE OIL COOLER, ON GROUND RUN OIL TEMP IS WITHIN LIMITS. OPS AND LEAK CHECK GOOD. 2 L 7 2 4T RT A8SW 2001080100312 20010801 00312 WP 2001 8 1 AALA20011310 1 20010627 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 266AA 49291 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 15D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBL Y AT SEAT 15D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001080100313 20010801 00313 GL 2001 8 1 C2XA01BT133 2 20010731 A 7200 AE3007A1P ENGINE EMB 145 EMB145LR SO ALLSN AE300 AE3007A GL FAULTY A C2XA O OTHER O OTHER UK UNKNOWN 1 SW 27 15973 4774 3164 145159 CAE311172 EWR/BTV---CO3626, CREW REPORTED "AIRCRAFT FILLED WITH FUMES DURING FLIGHT. A CONSTANT LIGHT SMELL OF FUEL/OIL SOMETIMES IT GOT STRONG"...MAINTENANCE TROUBLESHOT TO INTERNAL ENGINE OIL LEAK AIRCRAFT MAINTENANCE FERRIED TO BTV FOR ENGINE CHAN GE. REMOVED AND REPLACED ENGINE IN BTV. GROUND RUN OPS.CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4T 4 F RT T00011AT TE6CH 2001080100314 20010801 00314 EU 2001 8 1 HDNA610E 1 20010627 A 6711 LN47112B RING UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206A NE CYCLIC STICK MISSING E HDNA K NONE O OTHER IN INSP/MAINT 1 SW 03 911KB 2427 0013 DURING 100 HUR INSPECTION, FOUND A RETAINING RING MISSING. THE RING SECURES A BELLCRANK TO THE CYCLIC SHAFT ASSEMBLY. THIS ALLOWED THE BELLCRANK TO SHIFT UP AND DOWN ON THE SHAFT APPROX 0.5 INCH. WHEN THE BELLCRANK SHIFTS UP IT CONTACTS BRACKET PN L671M 1005240 WHICH PREVENTS THE BELLCRANK FROM COMMING OFF OF THE SHAFT. 1 G 7 2 3U 3 U O H88EU E42NE 2001080100315 20010801 00315 NM 2001 8 1 AALA20011311 1 20010626 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 686AA 25343 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT LEFT SIDE OVERWING EXIT DOOR BROKEN. REPLACED EMERGENCY EXI T LIGHT ASSEMBLY AT OVERWING EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001080100316 20010801 00316 NM 2001 8 1 IU62001F00000 1 20010529 A 2781 69358521 SLEEVE BOEING 737 737* NM BLOCKING VLV ASY CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 SLEEVE (145) IS CRACKED. FATIGUE. 2 L 7 2 4F RT A16WE 2001080100317 20010801 00317 NM 2001 8 1 IU62001F00001 1 20010529 A 2760 654494710 HOUSING BOEING BOEING 737 737* NM SPOILER LOCK CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 3938 HOUSING IS CRACKED ON THE SIDE OPPOSITE THE PORTS. PROBABLE CAUSE:737-SL-27-135 PROVIDE A REPAIR TO INCLUDE USE OF PN 65-44947-15 HOUSING ON ALL ACTUATORS, A MODIFICATION KIT TO THE LATEST CONFIGURATION PN 65-44851-14 OR REPLACEMENT HOUSI NGS MADE OF 15-5 PH STEEL OR 7075-T73 FORGINGS FOR ALL THE DASH NUMBER ACTUATORS. 2 L 7 2 4F RT A16WE 2001080100318 20010801 00318 NM 2001 8 1 IU62001F00003 1 20010627 A 3610 31628086 GUIDE ALIDSG BOEING 757 757 UTILUSE NM PILOT VALVE SEPARATED E IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 604 MALFUNCTION: PACKING, PN 561-515-0003, IS SEPARATING FROM THE GUIDE ASSEMBLY CAUSING THE OVERPRESSURE SWITCHER TO FAIL . THE PACKING IS INSTALLED USING ADHESIVE ECCOBOND 104. PROBABLE CAUSE: THE ADHESIVE APPEARS TO BREAKDOWN UNDER HEAT AND/OR HAS A REACTION WITH THE LUBRICANT, BRAYCOTE 601, CAUSING THE PACKING TO SEPARATE. UNIT TSR 773:22 HOURS BEFORE F AILURE. 2 L 7 2 4F RT A2NM 2001080100319 20010801 00319 WP 2001 8 1 AALA20011316 1 20010629 A 3230 HANDLE DOUG DC9 DC982 3022082 WP MLG OUT OF POSITION A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 7544A 53026 BWI - FLT 539 - EN ROUTE BWI-ORD, MAIN LANDING GEAR WOULD NOT RETRACT. RETURNED BWI AND LANDED WITHOUT FURTHER INCIDENT . RE-STOWED MAIN LANDING GEAR DOOR BYPASS HANDLE. INSPECTED MAIN LANDING GEAR AND DOORS. NO DEFECTS NOTED. SYSTEM GR OUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001080100320 20010801 00320 NM 2001 8 1 IU62001F00004 1 20010627 A 2760 654494710 HOUSING BOEING BOEING 757 757 UTILUSE NM SPOILER LOCK CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 49043 4360 HOUSING IS CRACKED UNDER THE RETRACT PORT. PROVIDE A REPAIR TO INCLUDE USE OF PN 65-44947-15 HOUSING ON ALL ACTUATORS, A MODIFICATION KIT TO THE LATEST CONFIGURATION PN 65-44851-14 OR REPLACEMENT HOUSINGS MADE OF 15-5 PH STEEL OR 7075-T73 FORGINGS FOR ALL THE DASH NUMBER ACTUATORS. 2 L 7 2 4F RT A2NM 2001080100321 20010801 00321 NM 2001 8 1 IU62001F00005 1 20010627 A 3240 511531 HOUSING PNEUDRAULICS BOEING 757 757* NM SHUTTLE VALVE CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 4063 HOUSING IS CRACKED INSIDE THE MOUNTING HOLE. FATIGUE, DEFECT IN THE CASTING OF THE HOUSING AND/OR OVERTORQUING OF BOLT INSTALLATION. IMPROVE DESIGN OR CHANGE THE MATERIAL OF THE HOUSING FOR INCREASED STRENGTH AND RELIABILITY. 2 L 7 2 4F RT A2NM 2001080100322 20010801 00322 NM 2001 8 1 IU62001F00006 1 20010613 A 2730 401606223 HOUSING MOOG BOEING 727 727 UTILSYS NM COMPUTER CORRODED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 562R HOUSING ASSEMBLY IS CORRODED ON THE SEAL PLATE SURFACE, IN THE CHECK VALVE PORTS AND BOLT HOLES. HOUSING ASSEMBLY IS MA DE FROM MAGNESIUM ALLOY AND IS EXTREMELY SUSCEPTIBLE TO DISSIMILAR METAL CORROSION AND CRACKS. 2 L 7 3 4J RT A3WE 2001080100323 20010801 00323 WP 2001 8 1 AALA20011339 1 20010621 A 5230 5936038501 BEAM DOUG DC9 DC982 3022082 WP CARGO DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 01 7521A 49898 TUL - FOUND AFT CARGO DOOR BEAM CORRODED, STATION 1160-1205. INSTALLED NEW DOOR BEAM SRM 51-30-5 FIG 2. (M) 2 L 7 2 4F A6WE 2001080100324 20010801 00324 NM 2001 8 1 IU62001F00007 1 20010613 A 3243 654458212 HOUSING BOEING BOEING 737 737* NM SHUTOFF VALVE CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 10416 1187 HOUSING ASSEMBLY IS CRACKED THROUGH BETWEEN BOTH VALVE BORES. STRESS FATIGUE. 2 L 7 2 4F RT A16WE 2001080100325 20010801 00325 NM 2001 8 1 IU62001F00008 1 20010613 A 2923 6544683 HOUSING BOEING BOEING 737 737* NM STNBY MODULE CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 26652 1562 HOUSING IS CRACKED AT PORT NR 1. FOUND DURING PROOF PRESSURE TEST. FATIGUE. 2 L 7 2 4F RT A16WE 2001080100326 20010801 00326 NM 2001 8 1 IU62001F00009 1 20010613 A 2730 4016146302 CAP MOOG BOEING 727 727* NM FEEL CONTROL ERODED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 419 SEALING SURFACE OF THE CAP ASSEMBLY HAS EROSION AND PITTING. DISSIMILAR METAL CORROSION. MADE FROM MAGNESIUM. 2 L 7 3 4F RT A3WE 2001080100327 20010801 00327 WP 2001 8 1 AALA20011348 1 20010618 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7521A 49898 TUL - FOUND THREE SCRATCHES FLOOR MEMBRANE BETWEEN FLOOR TRACK 1/2 STATION 1216-1217. CUTOUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-01 FIG 4. (M) 2 L 7 2 4F A6WE 2001080100328 20010801 00328 WP 2001 8 1 AALA20011349 1 20010614 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7521A 49898 TUL - FOUND LOWER SIDE OF RIGHT CUSP CORRODED AT STATION 526. REMOVED CORROSION, INSTALLED CUSP DOUBLER PER SRM 53-01 F IG 4 SHEET 3. (M) 2 L 7 2 4F A6WE 2001080100329 20010801 00329 NM 2001 8 1 IU62001F00010 1 20010614 A 2730 401611565 HOUSING MOOG BOEING 727 727* NM FEEL CONTROL ERODED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 419 SEALING SURFACE OF ELBOW HOUSING HAS EROSION AND PITTING. DISSIMILAR METAL CORROSION. MADE FROM MAGNESIUM. 2 L 7 3 4F RT A3WE 2001080100330 20010801 00330 NM 2001 8 1 IU62001F00011 1 20010614 A 2730 40161462 CAP MOOG BOEING 727 727* NM FEEL CONTROL ERODED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 419 SEALING SURFACE OF THE CAP ASSEMBLY HAS EROSION AND PITTING. DISSIMILAR METAL CORROSION. MADE FROM MAGNESIUM. 2 L 7 3 4F RT A3WE 2001080100331 20010801 00331 WP 2001 8 1 AALA20011356 1 20010628 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7521A 49898 TUL - FOUND CORROSION ON FLOORBEAMS AROUND NUTPLATE HOLES. REMOVED CORROSION BY REAMING HOLES AND INSTALLING FREEZE PLU GS PER ESO80559 DATED 6-27-2001. (M) 2 L 7 2 4F A6WE 2001080100332 20010801 00332 WP 2001 8 1 IY22001F00000 2 20010530 A 7200 30756332 CARBON SEAL AMD FALC10 FALCON10 2730101 EU GARRTT TFE731 TFE7312 01518 WP ENGINE FAILED B IY2R K NONE O OTHER IN INSP/MAINT 1 SW 15 10HE 8422 111 BACKGROUND: POST SB CARBON SEALS HAVE COMMON PROBLEM WITH SEAL RUNNERS FAILING DUE TO CARBON BUILDUP. THE SEAL RUNNER IS MFG FROM CERAMIC MATERIAL AND TENDS TO BREAK DUE TO THIS CO-KING. RESULTS: TYPICAL DAMAGE SUSTAINED FROM THIS RUNN ER FAILURE IS AS FOLLOWS; 1)NR 5 BEARING FAILS, CAUSING THE HPC TO SHAFT FORWARD. 2) HP TURBINE COUPLER TO CONTACT HP DIFFUSER. 3) PREFLIGHT SHUTDOWN. 4)EXTREME AMOUNT OF LUBE SYSTEM CONTAMINATION. RECOMMENDATIONS: SB, WHICH IS TO REDUCE OIL COKING. THE NR 4/NR 5 CARBON SEALS HAVE BEEN A PROBLEM FOR SOME TIME. THERE HAVE BEEN SEVERAL GENERATIONS OF SEALS FOR HPC, WITH NO PERMANENT FIX. 2 L 7 2 4F 4 F A33EU E6WE 2001080100333 20010801 00333 WP 2001 8 1 AALA20011360 1 20010627 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7521A 49898 TUL - FOUND CUSP CRACKED OUTBOARD OF NR 5 SEAT TRACK STATION 248. INSTALLED REPAIR STRIP (DOUBLER) PER ESO 80559 DATED 6/27/2001. (M) 2 L 7 2 4F A6WE 2001080100334 20010801 00334 EA 2001 8 1 J8G2001F00000 2 20010629 A 7250 ALF502L2C BEARING CNDAIR CL600 CL6001A11 1900302 EA LYC ALF502 ALF502* 41580 EA NR 2 DEFECTIVE E J8GA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 23 710HL 4524 1050 LF03009S FLIGHT CREW NOTICED SMOKE IN THE CABIN AFTER TAKE-OFF FROM AIRPORT. THE AIRCRAFT RETURNED TO THE AIRPORT WITH NO FURTHE R INCIDENT. INITIAL TROUBLESHOOTING INDICATED EXCESSIVE OIL PRESENCE AT NR 2 BEARING ON THE RIGHT ENGINE. DEFECT WITH NR 2 BEARING CONFIRMED REMOVED ENGINE, WILL INSTALL ANOTHER ENGINE WITH TSOH. 2 L 7 2 4F 4 F RT A21EA E6NE 2001080100335 20010801 00335 WP 2001 8 1 AALA20011361 1 20010704 A 2910 HYDRAULIC LINE DOUG DC9 DC982 3022082 WP HYDRAULIC SYS LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 405A 49316 DFW - FLT 2405 - EN ROUTE DFW-LAX, CLIMBING THROUGH 800 FEET, LEFT PRESSURE LOW LIGHT ILLUMINATED AND LEFT HYDRAULIC PRE SSURE INDICATED ZERO. LEFT HYDRAULIC QUANTITY INDICATED ONE QUART. ACCOMPLISHED RED BOOK PROCEDURE. RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. RE-TORQUED LEFT THRUST REVERSER CONTROL VALVE LINE. ACCOMPLISHED LEAK CHECK. NO LEAK S NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001080100336 20010801 00336 WP 2001 8 1 AALA20011377 1 20010621 A 5310 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 433AA 49451 TUL - FOUND WEB EAR CRACKED AFT OF FORWARD ENTRY DOOR AT STATION 208, LONGERON L15 DOOR JAMB. REPAIRED WITH REPAIR STRA P PER AARD 53-10-00-11. (REPAIR 11- PAX DOOR JAMB INNER SKIN REPAIR - MAJOR) 2 L 7 2 4F RT A6WE 2001080100337 20010801 00337 WP 2001 8 1 AALA20011382 1 20010621 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 433AA 49451 TUL - FOUND CORROSION ON CUSP AT 522-528 RIGHT. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-00-00-02 AND SRM 53 -01 FIG 4. (M) 2 L 7 2 4F RT A6WE 2001080100338 20010801 00338 WP 2001 8 1 AALA20011384 1 20010627 A 5320 ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 433AA 49451 TUL - FOUND ANGLE CRACKED STATION 1474 LEFT OF VERTICAL STABILIZER. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER PER AAR D 53-10-00-2. (M) 2 L 7 2 4F RT A6WE 2001080100339 20010801 00339 WP 2001 8 1 ASAA0180164 1 20010511 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 948AS 53021 SEA - DURING PRE-FLIGHT, FOUND SEVEN (3 RED AND 4 WHITE) EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN OVERWING EXIT AREA. REPLACED TRACK LIGHTING LAMPS. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001080100340 20010801 00340 WP 2001 8 1 ASAA0180175 1 20010518 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SJC - PRIOR TO FLT 319 - THE EMERGENCY FLOOR TRACK LIGHT COVER WAS FOUND TO BE MISSING AND THE LIGHTS INOPERATIVE AT ROW 7. INSTALLED MISSING COVER AND RECONNECTED WIRING TO LAMP MODULE AT ROW 7, LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001080100341 20010801 00341 WP 2001 8 1 ASAA0180176 1 20010519 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 961AS 53075 SEA - DURING MAINTENANCE CHECK, THE PORTABLE EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE PORTABLE EM ERGENCY LIGHT ASSEMBLY AND THE LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001080100342 20010801 00342 WP 2001 8 1 ASAA0180177 1 20010521 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 PHX - PRIOR TO FLT 711 - THE EMERGENCY FLOOR TRACK LIGHTS AT ROW 6 WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING TO LIGHT ASSEMBLY AND THE LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001080100343 20010801 00343 WP 2001 8 1 ASAA0180183 1 20010526 A 3350 STUD DOUG DC9 DC982 3022082 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 951AS 49111 PDX - DURING LINE CHECK, AFT CABIN OVERHEAD STANDBY LIGHTS AT ROW 18 AND 19 WERE DETERMINED TO BE INOPERATIVE. TIGHTENE D LOOSE GROUND STUD. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001080100344 20010801 00344 WP 2001 8 1 ASAA0180184 1 20010529 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 NM 01 954AS 49387 SEA - DURING LINE CHECK, DETERMINED THAT EMERGENCY EXIT LIGHT AT AFT DOOR WAS INOPERATIVE. REPAIRED BROKEN CONNECTOR WI RE. LIGHT THEN OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 2001080100345 20010801 00345 2001 8 1 ASAA0180189 4 20010605 A 2565 D29984109 SLIDE DOUG DC9 DC983 3022083 WP CABIN FAILED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 969AS 40866 4887 53063 OAK - DURING C-CHECK, AFT REAR DOOR EMERGENCY SLIDE HARNESS FAILED SYSTEM CHECK. REPLACED EMERGENCY SLIDE PER T/C 24653 002. SYSTEM CHECKED OK. (M) 2 L 7 2 4F RT A6WE 2001080100346 20010801 00346 WP 2001 8 1 ASAA0180195 1 20010608 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 LAX - PRIOR TO FLIGHT, THE EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 7. SECURED FLOOR TRACK LIGHTING A T ROW 7. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001080100347 20010801 00347 WP 2001 8 1 ASAA0180198 1 20010611 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DAMAGED A K NONE L NO TEST IN INSP/MAINT 1 NM 01 974AS 53450 FAI - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE ROWS 1 THROUGH 6. REPAIRED FLOOR WIRING AT ROW 3. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001080100348 20010801 00348 WP 2001 8 1 ASAA0180207 1 20010624 A 3350 0105606003 MODULE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 LAX - DURING PRE-FLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE FROM ROW 3 FORWARD. RECONNECTED LIGHT MOD ULE SOCKET. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001080100349 20010801 00349 2001 8 1 ASAA0180208 4 20010622 A 2565 D29985107 SLIDE DOUG DC9 DC983 3022083 WP L2 DOOR UNSERVICEABLE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 962AS 2103 2103 53076 SFO - DURING PREFLIGHT CHECK, FOUND L2 DOOR EMERGENCY SLIDE INFLATION PRESSURE LOW. REPLACED L2 DOOR SLIDE PER MM 25-62 -00. (M) 2 L 7 2 4F RT A6WE 2001080100350 20010801 00350 SO 2001 8 1 ASOA01096 1 20010626 A 3350 LIGHT EMB 120 EMB120 3260201 SO CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 236AS 120049 DURING GROUND INSPECTION IN DFW, CREW FOUND FLOOR EMERGENCY LIGHTS AT ROW 5 AS WELL AS THE EXIT SIGN ON THE FIGHT ATTEND ANT CLOSET, AND NUMEROUS CEILING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE INSPECTED THE FUSES AND POWER SUPPLIES FOR T HE EMERGENCY LIGHTING SYSTEM. ALL OPERATIONAL CHECKS WERE NORMAL. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001080100351 20010801 00351 NM 2001 8 1 UPS01236438 1 20010720 A 5310 6518915212 FRAME BOEING 727 72727C 138400J NM BS320 STR22R TO DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 909UP 19115 INSPECTION TYPE:C FRAME DAMAGED AT BS 320 STR22R STR27R (HOLES DAMAGED) FRAME REPLACED IAW SRM 51-30-02 AND DRWG 65- 18420 2 L 7 3 4F A3WE 2001080100352 20010801 00352 NM 2001 8 1 UPS01236445 1 20010730 A 5310 BULKHEAD BOEING 727 72762C 138402C NM RH MLG BULKHEAD CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 912UP 19244 INSPECTION TYPE:N/A RT MLG WHEEL WELL FWD BULKHEAD BELOW APU EXHAUST HAS CRACKS AROUND U PPER INBOARD CANNON PLUG RECEPT ICLE STA 870 ****MRR FILED AS OPEN*** AIRCRAFT FERRIED TO GSO REPAIR IN PROGRESS FERRY FLIGHT TO GSO 2 L 7 3 4F A3WE 2001080100353 20010801 00353 SO 2001 8 1 ASOA01099 1 20010629 A 3350 AGC1 FUSE EMB 120 EMB120 3260201 SO CABIN BLOWN A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 240AS 120060 DURING GROUND INSPECTION IN ATL, MAINTENANCE FOUND AFT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND RE PLACED A BLOWN FUSELAGE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001080100354 20010801 00354 SO 2001 8 1 ASOA01101 1 20010701 A 3350 10130115 SIGN EMB 120 EMB120 3260201 SO CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 240AS 120060 DURING HANGAR MAINTENANCE IN TXK, MAINTENANCE FOUND ILLUMINATED EXIT SIGN FORWARD OF EXIT LATCH BROKE IN TWO. MAINTENAN CE REMOVED AND REPLACED ILLUMINATED EXIT SIGN FORWARD OF EXIT LATCH. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001080100355 20010801 00355 NE 2001 8 1 BJNA010701 2 20010704 A 7250 TURBINE BOEING 737 737282 13844AT NM PWA JT8 JT8D17A 52049 NE NR 2 ENGINE FAILED A BJNA E C ENGINE SHUTDOWN ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 11 789TM 23046 709439 ON TAKEOFF, HEARD LOUD BOOM FROM NR 2 ENGINE. ABORTED TAKEOFF. FOUND NR 2 ENGINE HAD SUSTAINED A CONTAINED TURBINE FAI LURE. REMOVED AND ENGINE S/N 709439, AND SENT TO SHOP FOR EVALUATION. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 2001080100356 20010801 00356 NM 2001 8 1 GAIA01217ST 1 20010706 A 5200 SKIN BOEING 727 727223 1384074 NM BS 1125 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED C-3 DOOR SKIN CRACKED AT OUTER HANDLE COVER PLATE BS 1125 BETWE EN STRINGER 23-24 RIGHT, FILGHT STAR AIRCRAFT SERVICES, INC. ACCOMPLISHED NR 3 CARGO DOOR SKIN REPAIR AT BS 1125, STRIN GER 23-24R IAW B727 SRM 52-00-3 FIG 4. (M) 2 L 7 3 4F A3WE 2001080100357 20010801 00357 NM 2001 8 1 GAIA01223ST 1 20010706 A 5700 ANGLE BOEING 727 727223 1384074 NM WS 343 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED RIGHT WING LEADING EDGE CAVITY UPPER ATTACH ANGLE CRACKED AT SL AT STATION .260, WL 343. ACCOMPLISHED RIGHT WING LEADING EDGE CAVITY UPPER ATTACH ANGLE REPLACEMENT WS 343, SLAT STATIO N .260 IAW B727 SRM 57-20-2 AND SRM 51-30-2. (M) 2 L 7 3 4F A3WE 2001080100358 20010801 00358 NM 2001 8 1 GAIA01226ST 1 20010706 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 312 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN DOG HOUSE AREA, FLOORBEAM T-CAP IS CORRODED AT BS 312 LBL 3. ACCOMPLISHED BS 312 FLOORBEAM UPPER CHORD REPAIR AT LBL 3 IAW B727 SRM 53-10-2 FIG 7 AND SRM 51-40-3 FIG 1. (M) 2 L 7 3 4F A3WE 2001080100359 20010801 00359 NM 2001 8 1 GAIA01228ST 1 20010706 A 5300 FRAME BOEING 727 727223 1384074 NM BS 720 DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN FORWARD CARGO FRAME BS 720 HAS 2 DENTS AT STRINGER 25L. ACC OMPLISHED BS 720 FRAME REPAIR AT STRINGER 25L IAW B727 SRM 51-40-3 FIG 1 AND SRM 53-10-2 FIG 3. (M) 2 L 7 3 4F A3WE 2001080100360 20010801 00360 NM 2001 8 1 GAIA01229ST 1 20010706 A 5300 FRAME BOEING 727 727223 1384074 NM BS 720 DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN FORWARD CARGO FRAME BS 720 HAD A DENT BELOW STRINGER 25R. A CCOMPLISHED BS 720 FRAME REPAIR AT STRINGER 25R IAW B27 SRM 51-40-3 FIG 1 AND SRM 53-10-2 FIG 3. (M) 2 L 7 3 4F A3WE 2001080100361 20010801 00361 NM 2001 8 1 GAIA01230ST 1 20010706 A 5300 FRAME BOEING 727 727223 1384074 NM BS 1110 DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN AFT CARGO FRAME BS 1110 HAS A DENT AT STRINGER 26L. ACCOMPL ISHED BS 1110 FRAME REPAIR AT STRINGER 26L IAW B727 SRM 51-40-3 FIG 1 AND SRM 53-40-2 FIG 5. (M) 2 L 7 3 4F A3WE 2001080100362 20010801 00362 NM 2001 8 1 GAIA01231ST 1 20010706 A 5300 STRINGER BOEING 727 727223 1384074 NM BS 720B CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED STRINGER 15R CRACKED AT FORWARD END OF WING SCANNING LIGHT CUT OUT BS 720B PLUS 5. ACCOMPLISHED STRINGER 15R REPAIR AT BS 720B PLUS 5 IAW B727 SRM 53-10-2 FIG 5. (M) 2 L 7 3 4F A3WE 2001080100363 20010801 00363 NM 2001 8 1 GAIA01232ST 1 20010706 A 5300 FRAME BOEING 727 727223 1384074 NM BS 720 DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 720 FRAME DENTED IN RADIUS BETWEEN STRINER 16-17 LEFT. ACCO MPLISHED BS 720 FRAME REPAIR AT STRINER 16-17L IAW B727 SRM 53-10-2 FIG 3 AND SRM 51-40-3 FIG 1. (M) 2 L 7 3 4F A3WE 2001080100364 20010801 00364 NM 2001 8 1 GAIA01233ST 1 20010706 A 5300 STRINGER BOEING 727 727223 1384074 NM BS 720B CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED STRINGER 15L CRAKED AT AFT END OF LEFT WING SCANNING LIGHT BS 7 20B PLUS 15. ACCOMPLISHED STRINGER 15L REPAIR AT BS 720B PLUS 15 IAW B727 SRM 53-10-3 FIG 5. (M) 2 L 7 3 4F A3WE 2001080100365 20010801 00365 NM 2001 8 1 GAIA01234ST 1 20010706 A 5300 STRINGER BOEING 727 727223 1384074 NM BS 720B CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED STRINGER 15L CRACKED AT FORWARD END OF LEFT WING SCANNING LIGHT BS 720B PLUS 5. ACCOMPLISHED STRINGER 15L REPAIR AT BS 720B PLUS 5 IAW B727 SRM 53-10-3 FIG 5. (M) 2 L 7 3 4F A3WE 2001080100366 20010801 00366 NM 2001 8 1 GAIA01235ST 1 20010706 A 5300 ANGLE BOEING 727 727223 1384074 NM BS 1338 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN THE AFT AIRSTAIR, THE LOWER TORQUE BOX TO BS 1342 LOWER SPAN WISE CHORD STIFFENER ATTACH ANGLE IS CRACKED AT BS 1338, RBL 20, WL 200. ACCOMPLISHED STIFFENER ATTACH ANGLE REPLACEMEN T BS 1338, RBL 20, WL 200 IAW B727 SRM 51-40-3 FIG 1 AND SRM 53-10-2 FIG 7. (M) 2 L 7 3 4F A3WE 2001080100367 20010801 00367 NM 2001 8 1 GAIA01236ST 1 20010706 A 5300 WEB BOEING 727 727223 1384074 NM BS 620 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 620 FRAME FORWARD WEB CRACKED THROUGH SEAL RETAINER FASTENER HOLES ABOVE STRINGER 25 RT. ACCOMPLISHED BS 620 FRAME WEB REPAIR AT STRINGER 2R IAW B727 SRM 51-40-2 FIG 1 AND SRM 53- 10-2 FIG 3. (M) 2 L 7 3 4F A3WE 2001080100368 20010801 00368 NM 2001 8 1 GAIA01237ST 1 20010706 A 5300 WEB BOEING 727 727223 1384074 NM BS 328 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED WEB AT BS 328 LBL 45 CORRODED, FLIGHTSTAR AIRCRAFT SERVICES, IN C. ACCOMPLISHED FLOORWEB REPLACEMENT BS 295-351, LBL 15-45 IAW B727 SRM 51-40-2 AND SRM 53-10-2 FIG 2. (M) 2 L 7 3 4F A3WE 2001080100369 20010801 00369 NM 2001 8 1 GAIA01246ST 1 20010706 A 5300 SEAT TRACK BOEING 727 727223 1384074 NM BS 520-540 A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED SEAT TRACK AT BS 520-540, LBL 45.5 HAS ELONGATED HOLES. ACCOMP LISHED SEAT TRACK REPLACEMENT AT BS 480-550, LBL 45.5 IAW B727 SRM 53-10-5 FIG 1. (M) 2 L 7 3 4F A3WE 2001080100370 20010801 00370 NM 2001 8 1 GAIA01247ST 1 20010706 A 5330 SKIN BOEING 727 727223 1384074 NM BS 344 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED L1 DOOR AFT UPPER CORNER FRAME IS CRACKED 1.5 INCH BS 344, STRI NGER 5L-6L. ACCOMPLISHED FORWARD ENTRY DOOR UPPER CUT OUT SKIN/FRAME REPAIR IAW S/B 727-53-0186 (ACTUAL CRACK WAS IN DO OR CUTOUT SKIN/DOUBLER). (M) 2 L 7 3 4F A3WE 2001080100371 20010801 00371 NM 2001 8 1 GAIA01248ST 1 20010706 A 5330 SKIN BOEING 727 727223 1384074 NM BS 215 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BULGING SKIN AND DISHED FASTENER HEADS AT BS 215, STRINGER 24R. ACCOMPLISHED FUSELAGE SKIN LONGITUDINAL LAP SPLICE REPAIR IAW B727 SRM 53-30-3 FIG 14. (M) 2 L 7 3 4F A3WE 2001080100372 20010801 00372 NM 2001 8 1 GAIA01249ST 1 20010706 A 5300 ANGLE BOEING 727 727223 1384074 NM BS 950E CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED C-2 DOOR CUT OUT FORWARD FRAME LOWER STANCHION ADAPTER ATTACH A NGLE BROKEN AT BS 950E, STRINGER 26R. ACCOMPLISHED STANCHION ADAPTER ATTACH ANGLE REPLACEMENT BS 950E, STRINGER 26R IAW B727 SRM 53-10-2 FIG 3 AND SRM 51-40-3. (M) 2 L 7 3 4F A3WE 2001080100373 20010801 00373 NM 2001 8 1 GAIA01250ST 1 20010706 A 5300 WEB BOEING 727 727223 1384074 NM BS 178 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 21 6827 20180 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 178 BULKHEAD WEB IS CRACKED AT APPROXIMATELY WL 218, LBL 12 (POSITION 1L PER W/C 2210). ACCOMPLISHED BS 178 BULKHEAD WEB REPAIR AT LBL 12, WL 218 (POSITION 1L) PER KHA W/C 2210. (M) 2 L 7 3 4F A3WE 2001080100374 20010801 00374 NM 2001 8 1 GAIA01251ST 1 20010706 A 5300 FRAME BOEING 727 727223 1384074 NM BS 1090 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED C-3 CARGO DOOR CUT OUT FORWARD OUTBOARD CHORD IS CRACKED 1.5 IN CH BS 1090, STRINGER 24R. ACCOMPLISHED BS 1090 FRAME REPAIR AT STRINGER 24R IAW B727 SRM 53-10-2 FIG 5 AND SRM 51-40-3 FIG 1. (M) 2 L 7 3 4F A3WE 2001080100375 20010801 00375 NM 2001 8 1 GAIA01252ST 1 20010706 A 5320 WEB BOEING 727 727223 1384074 NM BS 1225 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED RIGHT TORQUE BOX LIGHTNING HOLE AT STATION 1225 HAS A CRACK 1 I NCH LONG. ACCOMPLISHED RIGHT TORQUE BOX WEB REPAIR AT BS 1225 IAW B727 SRM 51-40-2 AND SRM 53-10-2 FIG 6. (M) 2 L 7 3 4F A3WE 2001080100376 20010801 00376 NM 2001 8 1 GAIA01253ST 1 20010706 A 5300 WEB BOEING 727 727223 1384074 NM BS 178 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 178 BULKHEAD CRACKED AT RBL 2, WL 198, ALSO STIFFENERS (HORI ZONTAL) ABOVE WL 200 AND BELOW WL 196 ARE CRACKED AT RBL 5. ACCOMPLISHED BS 178 BULKHEAD WEB REPAIR AND STIFFENERS REPL ACEMENT WL 196-200, RBL 2-5 IAW B727 SRM 53-10-9 FIG 4 AND SRM 53-10-2 FIG 1. (M) 2 L 7 3 4F A3WE 2001080100377 20010801 00377 NM 2001 8 1 GAIA01254ST 1 20010701 A 5300 WEB BOEING 727 727223 1384074 NM BS 260 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WS DISCOVERED VERTICAL CRACK NOSE WHEEL WELL LEFT WEB BS 260, WL 160. ACCOMPL ISHED WEB REPAIR BS 260, WL 160 IN LEFT NWW IAW B727 SRM 51-40-2 FIG 1 AND SRM 53-10-2 FIG 2. (M) 2 L 7 3 4F A3WE 2001080100378 20010801 00378 NM 2001 8 1 GAIA01255ST 1 20010706 A 5300 SKIN BOEING 727 727223 1384074 NM BS 294-310 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BULGING SKIN, POPPED FASTENER HEADS, CORROSION ALONG STRINGER 2 4L, BS 294-310. ACCOMPLISHED FUSELAGE SKIN LAP REPAIR AT BS 294-310, STRINGER 24L IAW B727 SRM 53-30-3 FIG 5. (M) 2 L 7 3 4F A3WE 2001080100379 20010801 00379 NM 2001 8 1 GAIA01257ST 1 20010706 A 5300 FRAME BOEING 727 727223 1384074 NM BS 380 A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 380 FRAME HAS SEVERAL HOLES IN THE INBOARD RADIUS BETWEEN ST RINGER 4-7L. ACCOMPLISHED BS 380 FRAME REPAIR STRINGER 4-7. IAW B727 SRM 53-10-4 FIG 1. FASI NON ROUTINE 08343. (M) 2 L 7 3 4F A3WE 2001080100380 20010801 00380 NM 2001 8 1 P2EA01122 1 20010707 A 2100 16804UA2 INDICATOR BOEING 737 7372T5 NM INOPERATIVE A P2EA J O DUMP FUEL OTHER O OTHER CR CRUISE 1 CE 05 120NJ 22979 MCI - FLT 350 - DURING CRUISE AT 33,000 FEET CABIN RATE OF CHANGE WAS PLUS 250 FEET PER MINUTE AND CABIN PRESSURE WAS AT 9,500 FEET AND SHOULD BE AT 800 FEET FOR NORMAL. STANDBY WAS SELECTED WITH NO IMPROVEMENT. DURING DESCENT WITH THROTT LES AT IDLE, CABIN RATE OF CHANGE INCREASED TO PLUS 1000 FEET PER MINUTE. WAS ONLY ABLE TO DESCENT SLOWLY WITH DRAG DEV ICES AND POWER UP AT 1.6 TO 1.4 EPR TO GET CABIN TO DECREASE GRADUALLY. FOUND RATE OF CLIMB INDICATOR NEEDLE STICKING. REMOVED AND REPLACED RATE OF CLIMB INDICATOR. OPS CHECKS GOOD PER BOEING MM 21-31-0. (M) 2 L 7 2 4F RT A16WE 2001080100381 20010801 00381 WP 2001 8 1 HALA0100160 1 20010705 A 3200 PIN DOUG DC10 DC1010 3022110 WP A HALA O OTHER O OTHER IN INSP/MAINT 1 WP 13 153AA 46708 LAS - FLT 3 - FOUND LEFT MLG TRUCK SWIVEL PIN APPEARS TO BE COMING OUT ON INBOARD SIDE OF TRUCK. JACKED AIRCRAFT, REINS TALLED PIN PR MM 32-12-01. NO FURTHER ACTION REQUIRED PER TULSA TECH. (M) 2 L 7 3 4F A22WE 2001080100382 20010801 00382 NM 2001 8 1 TSAA0133081 1 20010707 A 3300 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM PAX CABIN INOPERATIVE A TSAA O OTHER O OTHER NR NOT REPORTED 1 WP 13 816AL 23122 REPLACED NR 3 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001080100383 20010801 00383 NM 2001 8 1 TSAA0133082 1 20010707 A 3300 86210066 BATTERY PACK BOEING 737 737282 13844AT NM PAX CABIN INOPERATIVE A TSAA O OTHER O OTHER IN INSP/MAINT 1 WP 13 824AL 23045 REPLACED NR 1 AND NR 4 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OP CHECK OK. AIRCRAFT RETURNED TO SERVIC E. (M) 2 L 7 2 4F RT A16WE 2001080200002 20010802 00002 CE 2001 8 2 JGV2001F00000 1 20010523 A 2810 0500118117 LINE CESSNA 172 172P 2072436 CE FUEL DIST CHAFED A JGVA K NONE K FLUID LOSS IN INSP/MAINT 1 CE 09 55121 10140 17275114 AIRCRAFT ARRIVED FOR INSPECTION WITH STRONG FUEL ODOR IN CABIN AND FUEL LEAKING FROM BELLY SKIN SEAM. FOUND AFT CABIN C ARPET SOAKED WITH FUEL. REMOVED TRIM FROM RIGHT AFT DOOR PEST AREA, FOUND THAT AILERON CABLE HAD BEEN CHAFING ON THE FU EL LINE IN THIS AREA FOR QUITE SOME TIME AND FINALLY CHAFED THROUGH LINE. REMOVED AND REPLACED FUEL LINE. INSPECTED AI LERON CABLE AND FOUND TO BE SERVICEABLE. RECOMMEND A ONE TIME INSPECTION OF THIS AREA, LEFT AND RIGHT SIDES, TO SEE IF CHAFING CONDITION EXISTS. 1 H 7 1 3O NT 3A12 2001080200003 20010802 00003 CE 2001 8 2 JGV2001F00002 1 20010615 A 3240 215592 DISK CESSNA 525 525 2076601 CE BRAKE ASSY BROKEN A JGVR K NONE O OTHER IN INSP/MAINT 1 CE 09 810SS 1325 5250137 WHILE PERFORMING ROUTINE INSPECTION ON AIRCRAFT, IT WAS DISCOVERED THAT THE OUTBOARD ROTATING DISK ON THE LEFT BRAKE WAS BROKEN INTO THREE PIECES. THE PIECES FELL OUT OR THE BRAKE ASSEMBLY WHEN THE WHEEL WAS REMOVED FROM THE AIRCRAFT. 1 L 7 2 4F RT A1WI 2001080200004 20010802 00004 EU 2001 8 2 JGV2001F00003 1 20010711 A 5620 D25W342120503 WINDOW ISRAEL 1125 ASTRASPX 4500205 EU GARRTT TFE731 TFE731* 01518 WP CABIN DAMAGED B JGVR K NONE O OTHER IN INSP/MAINT 1 CE 09 43RJ 25 136 LEFT NR 1,2,3,4, AND 5 WINDOWS AND RIGHT 1,2,3,4,5, AND 6 WINDOWS HAVE RAZOR BLADE SCRATCHES AT VARIOUS POINTS IN THE RA DIUSED NON VIEWABLE AREA, THIS IS STRESS AREA OF WINDOW. ASSOCIATED WINDOW SEALS ARE CUT AS WELL. IT APPEARS THE WINDO WS WERE TRIMMED OF SEALANT (SQUEEZE OUT) WITH A RAZOR BLADE AFTER WINDOW INSTALLATION. THIS CAUSED CUTTING OF THE WINDO W SEAL AND SCORING OF THE WINDOW IN VARIOUS AREAS AROUND THE PERIMETER OF THE WINDOW. REMOVAL OF WINDOW FOR ABOVE PROBL EM, NOTICED THAT HEADS OF RIVETS AROUND WINDOW WERE INTERFERING WITH THE SEAL AND WINDOW. SEAL WAS FOUND TO HAVE HOLES, WINDOW EDGE HAD BEEN CHIPPED OR DENTED WITH RIVET HEAD. MFG NOTIFIED, TO BE EVALUATED. 2 L 7 2 4F 4 F RT A16NM E6WE 2001080200005 20010802 00005 EU 2001 8 2 JGV2001F00004 1 20010711 A 5620 D25W342120503 WINDOW ISRAEL 1125 ASTRASPX 4500205 EU GARRTT TFE731 TFE731* 01518 WP CABIN DAMAGED B JGVR K NONE O OTHER IN INSP/MAINT 1 CE 09 1125S 26 134 LEFT NR 1,2,3,4, AND 5 WINDOWS AND RIGHT NR1,2,3,4,5, AND 6 WINDOWS HAVE RAZOR BLADE SCRATCHES AT VARIOUS POINTS IN THE RADIUSED NON-VIEWABLE AREA, THIS IS A STRESS AREA OF THE WINDOW. THE ASSOCIATED WINDOW SEALS ARE CUT AS WELL. APPEARS THE WINDOWS WERE TRIMMED OF SEALANT (SQUEEZE OUT) WITH A RAZOR BLADE AFTER WINDOW INSTALLATION. THIS CAUSED CUTTING OF THE WINDOW SEAL AND SCORING OF THE WINDOW IN VARIOUS AREAS AROUND THE PERIMETER OF THE WINDOW. UPON REMOVAL OF THE WIND OW FOR ABOVE PROBLEM, IT WAS NOTICED THAT THE SHOP HEADS OF RIVETS AROUND PERIMETER OF WINDOW WERE INTERFERING WITH SEAL AND WINDOW. SEAL WAS FOUND TO HAVE HOLES AT LOCATION AND THE WINDOW EDGE HAD BEEN CHIPPED OR INDENTION OF RIVET. 2 L 7 2 4F 4 F RT A16NM E6WE 2001080200006 20010802 00006 EU 2001 8 2 JGV2001F00005 1 20010711 A 5620 D25W342120503 WINDOW ISRAEL 1125 ASTRASPX 4500205 EU GARRTT TFE731 TFE731* 01518 WP CABIN DAMAGED B JGVR K NONE O OTHER IN INSP/MAINT 1 CE 09 75GX 23 137 LEFT NR 1,2,3,4, AND 5 WINDOWS AND RIGHT NR 1,2,3,4,5, AND 6 WINDOWS HAVE THE RAZOR BLADE SCRATCHES AT VARIOUS POINTS IN THE RADIUSED NON-VIEWABLE AREA, THIS IS A STRESS AREA OF THE WINDOW. THE ASSOCIATED WINDOW SEALS ARE CUT AS WELL. WIN DOWS WERE TRIMMED OF SEALANT (SQUEEZE-OUT) WITH RAZOR BLADE AFTER WINDOW INSTALLATION. THIS CAUSED CUTTING OF THE WINDO W SEAL AND SCORING OF THE WINDOW AROUND THE PERIMETER OF THE WINDOW. UPON REMOVAL OF WINDOWS, IT WAS NOTICED THAT THE S HOP HEADS OF RIVETS WERE INTERFERING WITH THE SEAL AND WINDOW. SEAL WAS FOUND TO HAVE HOLES AND WINDOW EDGE HAD BEEN CH IPPED OR HAD INDENTATION OF RIVET HEAD. 2 L 7 2 4F 4 F RT A16NM E6WE 2001080200007 20010802 00007 EU 2001 8 2 JGV2001F00006 1 20010711 A 5620 D25W342120503 WINDOW ISRAEL 1125 ASTRASPX 4500205 EU GARRTT TFE731 TFE731* 01518 WP CABIN DAMAGED B JGVR K NONE O OTHER IN INSP/MAINT 1 CE 09 80GX 34 138 LEFT NR 1,2,3,4, AND 5 WINDOWS AND RIGHT NR 1,2,3,4,5, AND 6 WINDOWS HAVE RAZOR BLADE SCRATCHES AT VARIOUS POINTS IN THE RADIUSED NON-VIEWABLE AREA, THIS IS A STRESS AREA OF THE WINDOW. THE WINDOW SEALS ARE CUT AS WELL. THE WINDOWS WERE T RIMMED OF SEALANT (SQUEEZE-OUT) WITH A RAZOR BLADE AFTER WINDOW INSTALLATION. THIS CAUSED CUTTING OF WINDOW SEAL AND SC ORING OF THE WINDOW IN VARIOUS AREAS AROUND THE PERIMETER OF THE WINDOW. UPON REMOVAL OF THE WINDOW FOR ABOVE PROBLEM W AS NOTICED THAT THE SHOP HEADS OF RIVETS AROUND THE PERIMETER OF THE WINDOW WERE INTERFERING WITH THE SEAL AND WINDOW. SEAL WAS FOUND TO HAVE HOLES AT THESE LOCATIONS AND WINDOW EDGE HAD BEEN CHIPPED OR HAD INDENTATION OF RIVET HEAD. 2 L 7 2 4F 4 F RT A16NM E6WE 2001080200008 20010802 00008 EU 2001 8 2 JGV2001F00007 1 20010711 A 5620 D25W342120503 WINDOW ISRAEL 1125 ASTRASPX 4500205 EU GARRTT TFE731 TFE731* 01518 WP CABIN DAMAGED B JGVR K NONE O OTHER IN INSP/MAINT 1 CE 09 58GX 26 135 LEFT NR 1,2,3,4, AND 5 WINDOWS AND RIGHT NR 1,2,3,4,5, AND 6 WINDOWS HAVE RAZOR BLADE SCRATCHES AT VARIOUS POINTS IN THE RADIUSED NON-VIEWABLE AREA, THIS IS A STRESS ARE OF THE WINDOW. THE WINDOW SEALS ARE CUT AS WELL. IT APPEARS THE WIND OWS WERE TRIMMED OF SEALANT (SQUEEZE OUT) WITH A RAZOR BLADE AFTER WINDOW INSTALLATION. THIS CAUSED CUTTING OF WINDOW S EAL AND SCORING OF WINDOW. UPON REMOVAL OF THE WINDOW FOR ABOVE PROBLEM, IT WAS NOTICED THAT SHOP HEADS OF RIVETS AROU ND PERIMETER OF WINDOW WERE INTERFERING WITH THE SEAL AND WINDOW. SEAL WAS FOUND TO HAVE HOLES IN THESE LOCATIONS AND W INDOW EDGE HAD BEEN CHIPPED OR INDENTATION OF RIVET HEAD. 2 L 7 2 4F 4 F RT A16NM E6WE 2001080200009 20010802 00009 NE 2001 8 2 JYD2001F00000 1 20010510 A 6220 6510311020102 HINGE PIN SKRSKY S64 S64F NE PWA JFTD12 JFTD12A4A 52047 NE MAIN ROTOR HEAD CRACKED A JYDR K NONE O OTHER IN INSP/MAINT 1 NM 09 223AC 3024 999 64086 S-64F MAIN ROTOR HEAD HINGE PINS DO OCCASIONALLY CRACK FROM DAMPER NUT SAFETY HOLES (APPROX 15 PER CENT OF THE TIME), BU T TYPICALLY THE CRACKS TRAVEL OUTBOARD TO THE EDGE OF THE HINGE PIN. HINGE PIN SN A04100236 CRACKED INBOARD THROUGH THE THREADS INTO THE THREAD RELIEF AND STARTED AROUND THE HINGE PIN. APPROX LENGTH OF CRACK AROUND THE THREAD RELIEF IS .6 0 INCH. 2 G 7 2 4U 4 U H6EA E15EA 2001080200010 20010802 00010 CE 2001 8 2 KKF2001F00000 1 20010621 A 2731 M39029218 SOCKET LEAR 24 24A 5170304 CE VERTICAL STAB FAILED D KKFA K NONE O OTHER IN INSP/MAINT 1 GL 23 63CK 119 PRIMARY PITCH TRIM FAILED, WILL TRIM NOSE UP BUT NOT NOSE DOWN. REPLACED 3 SOCKETS IN CONNECTOR P1023 AT 2 SPEED TRIM B OX PINS B,C, AND D. PERFORMED TRIM SYSTEM CHECKS. 2 L 7 2 4J A10CE 2001080200011 20010802 00011 EA 2001 8 2 L5V2001F00000 1 20010613 A 4920 320283211 FLAPPER VALVE CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF343A 30015 NE APU WORN B L5VR K NONE O OTHER IN INSP/MAINT 1 SW 05 46F 5055 APU CHECK VALVE LOCATED ABOVE APU LOAD CONTROL VALVE FLAPPERS HAVE WORN THRU RETAINING PIN CAUSING FLAPPER TO COME LOOSE AND DROP DOWN INTO THE BUTTERFLY MECHANISM OF THE LOAD CONTROL VALVE. THIS CAUSES THE LOAD CONTROL VALVE NOT TO CLOSE. 2 L 7 2 4F 4 F RT A21EA E15NE 2001080200012 20010802 00012 NM 2001 8 2 GAIA01218ST 1 20010706 A 5312 PRESSURE PANEL BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION , IT WAS DISCOVERED THAT THE NLG WW LEFT WEB IS CRACKED HORIZONTALLY AT BS 240-250, WL 180. ACC OMPLISHED LEFT NOSE WHEEL WELL WEB CRACK REPAIR AT BS 240-250, WL 180 IAW B727 SRM 51-40-2 FIG 1 AND SRM 53-10-2 FIG 2. (M) 2 L 7 3 4F A3WE 2001080200013 20010802 00013 NM 2001 8 2 GAIA01219ST 1 20010706 A 5312 PRESSURE PANEL BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION ,DISCOVERED 2 CRACKS IN NWW CEILING RECESSED WEB AT BS 285, RBL 4-8 AND BS 290, BL 0. ACCOMPLIS HED NOSE WHEEL WELL RECESSED CEILING WEB CRACK REPAIR AT BS 285-290, BL 0 RBL 8 IAW B727 SRM 51-40-2 FIG 1 AND SRM 53-10 -2 FIG 2. (M) 2 L 7 3 4F A3WE 2001080200014 20010802 00014 NE 2001 8 2 LN32001F00000 2 20010123 A 7421 FHE246 IGNITER BEECH MU300 400BEECH CE PWA JT15 JT15D5 52112 NE ENGINE UNAPPROVED PART B LN3R K NONE O OTHER IN INSP/MAINT 1 WP 07 64VM 183 RJ1 WE ARE PERFORMING A PHASE A INSPECTION AGAIN 183.6 HOURS LATER. REMOVED ENGINE IGNITORS IN AN UNAIRWORTHY CONDITION. F OUND ALL FOUR IGNITORS IN AN UNAIRWORTHY CONDITION. THE CENTER ELECTRODE IS ABLE TO MOVE BACK AND FORTH INSIDE IGNITOR. TAKING THE IGNITOR IN HAND AND LIGHTLY SHAKING YOU CAN HEAR AND SEE CENTER ELECTRODE MOVING FORE AND AFT INSIDE IGNITO R BODY. FOLLOWING IS THE DATA FOUND ON THE IGNITOR BODY, ALL 4 IGNITOR S/N LISTED: (NR 1-99076345), NR 2-99076289, NR 3-99076330, NR 4-99076342. 2 H 7 2 4F 4 F RT A16SW E25EA 2001080200015 20010802 00015 NE 2001 8 2 LN32001F00001 2 20010123 A 7421 FHE2464 IGNITER BEECH MU300 400BEECH CE PWA JT15 JT15D5 52112 NE ENGINE DEFECTIVE B LN3R K NONE O OTHER IN INSP/MAINT 1 WP 07 64VM 183 RJ1 WE ARE PERFORMING A PHASE A INSPECTION AGAIN 183.6 HOURS LATER. REMOVED ENGINE IGNITORS FROM BOTH ENGINES FOR INSPECTIO N ONLY. FOUND ALL FOUR IGNITORS IN AN UNAIRWORTHY CONDITION. THE CENTER ELECTRODE IS ABLE TO MOVE BACK AND FORTH INSID E IGNITOR. TAKING THE IGNITOR IN HAND AND LIGHTLY SHAKING, YOU CAN HEAR AND SEE CENTER ELECTRODE MOVING FORE AND AFT IN SIDE IGNITOR BODY . FOLLING IS THE DATA FOUND ON THE IGNITOR BODY, SN LISTED: NR 1-99076345, (NR 2-99076289), NR 3 -99076330, NR 4-99076342. 2 H 7 2 4F 4 F RT A16SW E25EA 2001080200016 20010802 00016 NM 2001 8 2 GAIA01220ST 1 20010706 A 5312 PRESSURE PANEL BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION, IT WAS DISCOVERED RIGHT MAIN WHEEL WELL PRESSURE WEB IS CRACKED AT BS 948, RBL 65, WL 200. ACC OMPLISHED RIGHT MAIN WHEEL WELL PRESSURE DECK CRACK REPAIR AT BS 948, RBL 65, WL 200 IAW BOEING DRAWING 65-89360. (M) 2 L 7 3 4F A3WE 2001080200017 20010802 00017 NE 2001 8 2 LN32001F00002 2 20010123 A 7421 FHE2464 IGNITER BEECH MU300 400BEECH CE PWA JT15 JT15D5 52112 NE ENGINE DEFECTIVE B LN3R K NONE O OTHER IN INSP/MAINT 1 WP 07 64VM 183 RJ1 WE ARE PERFORMING A PHASE A INSPECTION AGAIN 183.6 HOURS LATER. REMOVED ENGINE IGNITORS IN AN UNAIRWORTHY CONDITION. T HE CENTER ELECTRODE IS ABLE TO MOVE BACK AND FORTH INSIDE IGNITOR. TAKING THE IGNITOR IN HAND AND LIGHTLY SHAKING YOU C AN HEAR AND SEE CENTER ELECTRODE MOVING FORE AND AFT INSIDE IGNITOR BODY. FOLLOWING IS THE DATA FOUND ON THE IGNITOR BO DY, SN: NR1-99076345, NR2-99076289,( NR3-99076330), NR4-99076342. 2 H 7 2 4F 4 F RT A16SW E25EA 2001080200018 20010802 00018 NE 2001 8 2 LN32001F00003 2 20010123 A 7421 FHE2464 IGNITER BEECH MU300 400BEECH CE PWA JT15 JT15D5 52112 NE ENGINE DEFECTIVE B LN3R K NONE O OTHER IN INSP/MAINT 1 WP 07 64VM RJ1 WE ARE PERFORMING A PHASE A INSPECTION AGAIN 183.6 HOURS LATER. REMOVED ENGINE IGNITORS FROM BOTH ENGINES FOR INSPECTIO N ONLY. FOUND ALL FOUR IGNITORS IN AN UNAIRWORTHY CONDITION. THE CENTER ELECTRODE IS ABLE TO MOVE BACK AND FORTH INSID E IGNITOR. TAKING THE IGNITOR IN HAND AND LIGHTLY SHAKING, YOU CAN HEAR AND SEE CENTER ELECTRODE MOVING FORE AND AFT IN SIDE IGNITOR BODY. FOLLOWING IS THE DATA FOUND ON THE IGNITOR BODY, SN: NR1-99076345, NR2-99076289, NR3-99076330, (NR 4-99076342) 2 H 7 2 4F 4 F RT A16SW E25EA 2001080200019 20010802 00019 NM 2001 8 2 GAIA01221ST 1 20010706 A 5312 PRESSURE PANEL BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION, IT WAS DISCOVERED LEFT MAIN WHEEL WELL PRESSURE WEB IS CRACKED AT BS 948, LBL 65, WL 200. ACCO MPLISHED LEFT MAIN WHEEL WELL PRESSURE DECK CRACK REPAIR AT BS 948, LBL 65, WL 200 IAW BOEING DRAWING 65-89360. (M) 2 L 7 3 4F A3WE 2001080200020 20010802 00020 2001 8 2 LU42001F00000 4 20010628 A 6122 C4170 IDLER GEAR HARTZL PIPER PA23 PA23250 7102308 SO GOVERNOR CRACKED B LU4R K NONE O OTHER IN INSP/MAINT 1 SO 17 63807 B6681T 277754131 IDLER GEAR, NUMEROUS INDICATIONS AT BASE OF TEETH EXTENDING AROUND CORNER. 1 L 7 2 3O 1A10 2001080200022 20010802 00022 NM 2001 8 2 GAIA01222ST 1 20010706 A 5730 SKIN BOEING 727 727223 1384074 NM LT WING CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION ,IT WAS DISCOVERED LEFT WING INBOARD INTERNAL LEADING EDGE SKIN, ACCESS THROUGH PANEL 6301, L/E STATION 130.5 IS CRACKED AROUND SEVERAL FASTENERS. ACCOMPLISHED LEFT WING INBOARD INTERNAL LEADING EDGE SKIN CRACK REPA IR AT WS 130.5 IAW B727 SRM 57-30-4 FIG 3. (M) 2 L 7 3 4F A3WE 2001080200024 20010802 00024 NM 2001 8 2 GAIA01224ST 1 20010706 A 5730 SKIN BOEING 727 727223 1384074 NM RT WING CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION, IT WAS DISCOVERED RIGHT WING LEADING EDGE CAVITY LOWER SKIN CRACKED. ACCOMPLISHED RIGHT WING L EADING EDGE LOWER SKIN REPAIR AT WS 474 IAW B727 SRM 57-30-4 FIG 1. (M) 2 L 7 3 4F A3WE 2001080200025 20010802 00025 WP 2001 8 2 M8B2001F00000 1 20010620 A 3213 ARG7026501 BOLT DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE RT AFT AXLE SHEARED I M8BB D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 33 10MB 29871 6311 47907 455928 PRE DEPARTURE CHECKS FOUND RIGHT MAIN LANDING GEAR AFT AXLE BOLT HAD HEXAGONAL HEAD SHEARED OFF. PROBABLE CAUSE: FATIG UE, STRESS. 2 L 7 3 4F 4 F RT A22WE E23EA 2001080200026 20010802 00026 NM 2001 8 2 GAIA01225ST 1 20010706 A 5312 BULKHEAD BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION , IT WAS DISCOVERED IN 2 CRACKS AT FASTENER LOCATIONS BS 178, RBL 10, WL 235. ACCOMPLISHED BS 1 78 BULKHEAD WEB REPAIR AT RBL 10, WL 235 IAW B727 SRM 53-10-9 FIG 4. (M) 2 L 7 3 4F A3WE 2001080200027 20010802 00027 NM 2001 8 2 GAIA01227ST 1 20010706 A 5311 FRAME BOEING 727 727223 1384074 NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION, IT WAS DISCOVERED IN FORWARD CARGO FRAME BS 700 HAS 2 DENTS AT STRINGER 25L AND 24L. ACCOMPLIS HED BS 700 FRAME REPAIR AT STRINGER 25L AND 24L IAW B727 SRM 51-40-4 FIG 1 AND SRM 53-10-2 FIG 3. (M) 2 L 7 3 4F A3WE 2001080200028 20010802 00028 NM 2001 8 2 GAIA01256ST 1 20010706 A 5730 SKIN BOEING 727 727223 1384074 NM RT WING CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING A LTC INSPECTION, IT WAS DISCOVERED RIGHT WING UPPER SURFACE LEADING EDGE SKIN CRACKED IN 2 PLACES AT AFT END OF NR 6 SLAT OUTBOARD HOOK SEAL CUTOUT. (M) 2 L 7 3 4F A3WE 2001080200029 20010802 00029 NM 2001 8 2 GAIA01258OP 1 20010709 A 3350 100679 LIGHT BOEING 727 727214 138407R NM L1 DOOR INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 750US 21512 DURING ROUTINE MAINTENANCE AT PHX, IT WAS DISCOVERED THAT THE L1 DOOR POSITION EMERGENCY EXIT LIGHT WAS INOPERATIVE. RE MOVED AND REPLACED THE L1 DOOR POSITION EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONALLY CHECKS GOOD. THE AIRCRAFT WAS RET URNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001080200030 20010802 00030 2001 8 2 GTIA010550 4 20010428 A 3460 COMPUTER DOUG DC9 DC983 3022083 WP COCKPIT FAULTY A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - P1 AT VARIOUS TIMES DURING FLIGHT, FLT GUIDANCE SYSTEM WOULD DEFAULT TO HEADING HOLD. NR 1 FGC REPLACED PER MD-80 MM 22-01-01. SYSTEM RETURNED TO SERVICE CHECK GOOD PER MD-80 MM 22-01-05. (M) 2 L 7 2 4F RT A6WE 2001080200031 20010802 00031 2001 8 2 GTIA010551 4 20010428 A 3460 COMPUTER DOUG DC9 DC983 3022083 WP COCKPIT FAULTY A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - P2 COULD NOT ARM ILS OR VOR/LOC AUTOPILOT OR FLIGHT DIRECTOR. REMOVED AND REPLACED NR 1 DFGC PER MD-80 MM 22-01-0 1 SYSTEM OPS CHECK GOOD PER MD-80 MM 22-01-05. (M) 2 L 7 2 4F RT A6WE 2001080200032 20010802 00032 2001 8 2 GTIA010552 4 20010425 A 2230 AUTOTHRUST SYS DOUG DC9 DC983 3022083 WP COCKPIT FAULTY A GTIA K NONE O OTHER AP APPROACH 1 GL 23 808NK 49504 FTW - AUTOTHROTTLE WILL NOT STAY ENGAGED AT APPROACH. REMOVED AND REPLACED IAW MD-80 MM 22-01-02. SYSTEM GROUND TEST G OOD. (M) 2 L 7 2 4F RT A6WE 2001080200033 20010802 00033 WP 2001 8 2 HALA0100148 1 20010626 A 3230 PLATE DOUG DC9 DC951 3022051 WP RT MLG LOOSE A HALA K NONE O OTHER CR CRUISE 1 WP 13 601AP 47658 FLT 170 - HNL - FOUND RIGHT MLG UNSAFE LIGHT CAME ON IN CRUISE. RESECURED RIGHT GEAR UPLATCH STRIKER PLATE. OK FOR SER VICE. (M) 2 L 7 2 4F RT A6WE 2001080200034 20010802 00034 WP 2001 8 2 HALA0100150 1 20010626 A 2910 FITTING DOUG DC10 DC1030 3023501 WP HYDRAULIC SYS LEAKING A HALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 13 68060 47850 LAX - FLT 32 - NR 1 SYSTEM HYDRAULIC FAILURE. DIVERTED TO LAX, WHERE AN UNEVENTFUL LANDING WAS MADE. FOUND NR 1 SYSTEM HYDRAULIC LINE AT THE UNION TO THE STAB TRIM BRAKE LEAKING. ALSO, PRECAUTIONARY CHECKED ENGINE DRIVEN HYDRAULIC MODULE AND SYSTEM RETURN FILTER, NO CONTAMINATION FOUND. SERVICED NR 1 HYDRAULIC RESERVOIR AFTER MAINTENANCE COMPLETED, LEAK CHECK OF FILTER OK. (M) 2 L 7 3 4F A22WE 2001080200035 20010802 00035 NM 2001 8 2 HALA0100168 1 20010710 A 2923 BYG70005515 PUMP BOEING 717 717200 1383700 NM HYDRAULIC SYS MALFUNCTIONED A HALA D RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 480HA 45 55125 HNL - FLT 520 - RIGHT HYDRAULIC TEMPERATURE HIGH LIGHT ON. REMOVED AND REPLACED AUX PUMP OPS CHECK, LEAK CHECK OK, PER MM 29-21-01. (M) 2 L 7 2 4F TR A6WE 2001080200036 20010802 00036 NM 2001 8 2 P2EA01117 1 20010703 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 128NJ 22892 SJO - DURING C-CHECK, FUSELAGE BS 1026 BETWEEN STRINGER 27 LEFT AND 27 RIGHT SKIN WITH DENT OUT OF LIMITS. FUSELAGE SKI N SECTION REPAIRED FROM BS 1016 TO BS 1033, BETWEEN STRINGERS 26 LEFT AND 26 RIGHT DUE TO DENT IAW SRM 53-30-3, FIG 28. (M) 2 L 7 2 4F A16WE 2001080200037 20010802 00037 NM 2001 8 2 P2EA01118 1 20010703 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 128NJ 22892 SJO - DURING C-CHECK, FUSELAGE FROM BS 847-867 BETWEEN STRINGER 26 LEFT AND 27 LEFT SKIN WITH DENTS OUT OF LIMITS. (M) 2 L 7 2 4F A16WE 2001080200038 20010802 00038 WP 2001 8 2 P2EA01119 1 20010709 A 5280 DOOR DOUG DC9 DC983 3022083 WP RT MLG NOT CLOSED A P2EA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CE 05 131NJ 49846 MCI - FLT 105 - AFTER GEAR RETRACTION FOLLOWING TAKEOFF, AIRCRAFT HAD LOAD NOISE AND VIBRATION. INSPECTION FOUND AIRCRA FT RIGHT GEAR DOOR DOWN AND UNLOCKED. INSPECTED DOOR FOR DAMAGE AND NO DAMAGE WAS FOUND, CLOSED AND SECURED DOOR IAW AI RCRAFT MM 32-30-00. (M) 2 L 7 2 4F RT A6WE 2001080200039 20010802 00039 NE 2001 8 2 P2EA01121 2 20010710 A 7200 ENGINE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE NR 1 MALFUNCTIONED A P2EA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 CE 05 132NJ 49780 MCI - FLT 506 - DURING ENGINE START, NR 1 ENGINE EGT STARTED FLASHING, ANTICIPATED HOT START, ABORTED START AT 450C. PE RFORMED ENGINE START AND RUN, FOUND THE NR 1 ENGINE EGT TO BE WITHIN LIMITS FOR GROUND OPERATION IAW AIRCRAFT MAINTENANC E MANUAL 72-00-02. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2001080200040 20010802 00040 NM 2001 8 2 ABXA010402 1 20010718 A 3350 1000679 LIGHT BOEING 767 767281 1385109 NM CABIN INTERMITTENT A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 767AX 22785 PORTABLE EMERGENCY EXIT LIGHT ASSEMBLY WAS FLICKERING ABOVE THE CREW DOOR. REPLACED THE PORTABLE EMERGENCY EXIT LIGHT A SSEMBLY IAW B767 AMM 33-51-00. OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2001080200041 20010802 00041 WP 2001 8 2 ABXA010404 1 20010717 A 3350 60030451 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 981AX 47273 EMERGENCY OVERHEAD LIGHTS INOPERATIVE. REPLACED THE EMERGENCY LIGHTS POWER SUPPLY IAW DC-9 MM. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2001080200042 20010802 00042 WP 2001 8 2 ABXA010405 1 20010719 A 2752 39129645501 ACTUATOR DOUG DC9 DC932 3022066 WP T/E FLAP BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 984AX 47258 SPLIT FLAP INDICATION FROM 15 DEGREES TO ZERO DEGREES. MECHANICS FOUND THE LEFT OUTBOARD FLAP ACTUATOR WITH BROKEN MOUN TING EAR. REPLACED THE LEFT OUTBOARD FLAP ACTUATOR IAW DC-9 AMM 27-52-02-2-0001. NO LEAKS NOTED. 2 L 7 2 4F A6WE 2001080200043 20010802 00043 WP 2001 8 2 ABXA010406 1 20010718 A 7830 3959012501 CONTROL ROD DOUG DC9 DC932 3022066 WP NR 1 ENGINE MALFUNCTIONED A ABXA K NONE O OTHER LD LANDING 1 GL 23 903AX 47427 NR 1 THRUST REVERSER UNLOCKED BUT DID NOT DEPLOY. REPLACED THE NR 1 THRUST REVERSER UNLOCK CONTROL ROD ASSEMBLY. COMPL IED WITH ADJUSTMENT TEST OF NR 1 THRUST REVERSER SYSTEM IAW DC-9 MM. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2001080200044 20010802 00044 NM 2001 8 2 ABXA010407 1 20010725 A 3260 LIGHT BOEING 767 767281 1385109 NM COCKPIT INOPERATIVE A ABXA L ABORTED APPROACH O OTHER AP APPROACH 1 GL 23 788AX 23021 RIGHT GEAR GREEN DOWN LIGHT FAILED TO ILLUMINATE WITH GEAR HANDLE DOWN. EICAS MESSAGE NOT DISPLAYED. DOOR AND GEAR AMB ER LIGHTS WERE EXTINGUISHED. CREW ELECTED TO DO A GO-AROUND AND A GEAR RECYCLE. RELAMPED RIGHT GEAR DOWN AND LOCKED. INDICATION OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2001080200045 20010802 00045 WP 2001 8 2 ABXA010410 1 20010725 A 3230 UPLOCK DOUG DC8 DC863 302198A WP RT MLG OUT OF ADJ A ABXA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 825AX 46115 RED GEAR UNSAFE LIGHT CAME ON AT CRUISE AND THE RIGHT GEAR DOOR LANDING GEAR AND LIGHT WENT OUT. PERFORMED LANDING GEAR DOOR SWITCH TEST AND ADJ/TEST MAIN GEAR DOOR. CLOSED PROXIMITY SWITCH. BOTH CHECKED GOOD. ADJUSTED DOOR UPLATCH TURN BUCKLES IAW DC-8 MM 32-30-00-2. CLEANED AND LUBED SWITCHES. SYSTEM CHECKED GOOD ON THE GROUND. 2 L 7 4 4F 4A25 2001080200046 20010802 00046 WP 2001 8 2 ABXA010411 1 20010724 A 2810 FITTING DOUG DC9 DC941 302207N WP LT MLG WW CRACKED A ABXA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 23 956AX 47620 DURING PREFLIGHT, CREW REPORTED FUEL SEEP FROM THE WHEEL WELL AREA. INSPECTION FOUND A CRACK 1 INCH LONG ABOVE THE SKI FITTING NEAR THE VERTICAL ATTACH FITTING IN THE LEFT WHEEL WELL. 2 L 7 2 4F A6WE 2001080200047 20010802 00047 NM 2001 8 2 ABXA010413 1 20010727 A 2120 ODOR BOEING 767 767281 1385109 NM CABIN DETECTED A ABXA K NONE O OTHER TO TAKEOFF 1 GL 23 787AX 23020 THERE WAS AN OIL SMELL FROM THE ENVIRONMENTAL SYSTEM ON TAKEOFF. REMOVED LEFT AND RIGHT CHECK VALVES (ENGINE SUPPLY) AN D INSPECTED FOR OIL CONTAMINATION, NONE FOUND. REINSTALLED VALVES IAW B767 MM 36-20. RAN BOTH PACKS ON ENGINE PNEUMATI CS, FULL HOT AND COLD AND AT VARIOUS POWER SETTINGS. NO ODOR NOTED. ENGINES RUN IAW B767-10A. OPERATED BOTH PACKS WIT H APU AND EXTERNAL PNEUMATIC SUPPLIES. NO ODOR NOTED. REMOVED APU BLEED AIR DUCT AT APU AND APU BLEED AIR VALVE. NO V ISIBLE OIL CONTAMINATION FOUND. REINSTALLED BLEED AIR DUCT AND BLEED AIR VALVE. LEAK AND OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2001080200048 20010802 00048 WP 2001 8 2 ABXA010416 1 20010201 A 5311 FRAME DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AX 46126 FORWARD LOWER CARGO, STATION 420, CRACK ON FRAME AT LONGERON 31 LEFT. 2 L 7 4 4F 4A25 2001080200049 20010802 00049 WP 2001 8 2 ABXA010417 1 20010309 A 5710 STRUCTURE DOUG DC8 DC863F 302198F WP LT WING LEAKING A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 SPAR CAP LEAKED FUEL JUST INBOARD OF NR 1 PYLON AT S - 64 DOUBLER. REMOVED DOUBLER AND TRIPLER. FABRICATED REPAIR DOUB LERS AND INSTALLED IAW ABX REA D857-40311MR AND DAC DWG SRO8570013. 2 L 7 4 4F 4A25 2001080200050 20010802 00050 NM 2001 8 2 DL733010985 1 20010616 A 2150 A/C PACK BOEING 737 73735B NM A/C BAY FAILED A DALA O OTHER O OTHER CL CLIMB 1 SO 27 221DL 23970 AFTER T/O, A/C WILL NOT PRESSURIZE WITH LEFT PACK IN AUTO AND RT PACK ON DEFERRAL. REPAIRED RT PACK. PRESSURIZED AIRCR AFT, OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2001080200051 20010802 00051 NM 2001 8 2 DL73K011031 1 20010621 A 5210 STOP FITTING BOEING 737 737247 138448D NM L1 DOOR OUT OF ADJ A DALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 27 243WA 23517 PASSING 10,000 FEET IN CLIMBOUT FWD F/A REPORTED THUMP NOISE AT LEFT FWD ENTRY DOOR. WHILE CONTINUING CLIMB CAPT WENT B ACK TO ACCESS NOISE/SOURCE. LEVELED AT FL230 FOR 4 MINUTES, DECIDED OK FOR CONTINUE. PASSING FL280, IN COCKPIT BOTH PI LOTS HEARD LOUD THUMP AND FELT ASSOC VIBRATION THROUGH FLOORING, HALTED CLIMB AT FL290. PRESS CONTROLLER AUTO 33000, 5 PSID INDICATED. REMOVED DOOR LINER AND SIDEWALL AFT OF L1 DOOR TO INSP, NO VISIBLE DAMAGE FOUND. ADJ DOOR STOPS ON DOO R FRAME. PRESSURIZED TO 6.5 PSID. 2 L 7 2 4F A16WE 2001080200052 20010802 00052 NM 2001 8 2 DL757010941 1 20010610 A 3320 D77311001 BALLAST BOEING 757 757232 1384965 NM CABIN DEFECTIVE A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 6708D 30480 STRONG ELECTRICAL HOT WIRE SMELL AT MID GALLEY WHEN FLUORESCENT LIGHT TURNED OFF SMELL DISSIPATED. REMOVED CEILING PANE L IN MID GALLEY INSPECTED ALL WIRING IN OVERHEAD, INCLUDING WIRING TO BALLAST AND LIGHTING SOCKET. REMOVED AND REPLACED LIGHTING BALLAST FOR PRECAUTION. INSPECTED COFFEEMAKERS AND WIRING. FOUND COFFEEMAKER 1 WITH COFFEE GRIME. CLEANED C OFFEEMAKER 1. POWERED C/M LIGHTS AND ENT SYS FOR 2 HOURS, NO SMELL NOTED. 2 L 7 2 4F RT A2NM 2001080200053 20010802 00053 NM 2001 8 2 DL757010944 1 20010610 A 3350 LIGHT BOEING 757 757232 1384965 NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 628DL 22918 R1 EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT. 2 L 7 2 4F RT A2NM 2001080200054 20010802 00054 NE 2001 8 2 MAC15501 3 20010530 A 6111 L106FA0 BLADE MCAULY BAG JETSTM JETSTM3201 1500217 EU MCAULY 4HFR34 4HFR34C653 NE PROPELLER CRACKED B PAIR K NONE O OTHER IN INSP/MAINT 1 SO 05 915AE 8443 4479 920887 915 920887 DURING EDDY CURRENT INSPECTION FOUND EVIDENCE OF A POSSIBLE CRACK IN THE BLADE AT THE 43.500 IN. STATION. WILL SEND BLA DE TO MCCAULEY FOR EVALUATION AND FINAL INSPECTION. 2 L 7 2 4T RT A56EU 6 C 3PNE 2001080200055 20010802 00055 NM 2001 8 2 DL757010947 1 20010610 A 2800 43367310011026 SWITCH BOEING 757 757232 1384965 NM COCKPIT DEFECTIVE A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 684DA 27104 SMOKE BEHIND OVERHEAD FUEL BOOST PUMP PANEL IN COCKPIT. FOUND RT FWD BOOST PUMP SWITCH AT FAULT. REPLACE SAME. 2 L 7 2 4F RT A2NM 2001080200056 20010802 00056 GL 2001 8 2 ME42001F00000 3 20010326 A 6110 HCB4MP3AM10877K SPRING BEECH 1900 1900 1154160 CE HARTZL HCB4M HCB4MP3 GL PROPELLER BROKEN B ME4R K NONE O OTHER IN INSP/MAINT 1 SO 19 125BA 570 UB6 FW778 HARTZELL PROPELLER MODEL NUMBER HC-B4MP-3A/M10877K WITH SERIAL NUMBER FW778 WAS RECEIVED FOR HUB REPLACEMENT IAW AD NOTE 96-18-14. DURING THE DISASSEMBLY, THE SPRING, PN A3496, IN THE SPRING KIT ASSEMBLY WAS NOTED BROKEN. TALKING WITH THE FLIGHT CREW, THEY STATED NO ABNORMALITIES WERE NOTED. PROPELLER HUB (NEW HUB SN FWA3613) AND SPRING REPLACED, PROPELLE R REASSEMBLED, REINSTALLED ON THE AIRCRAFT, DYNAMIC BALANCED AND OPS CHECK GOOD. 2 L 7 2 4T RT A24CE 6 C P56GL 2001080200057 20010802 00057 NM 2001 8 2 DL757010987 1 20010616 A 2510 613617411 POWER CABLE BOEING 757 757232 1384965 NM COCKPIT DEFECTIVE A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 644DL 23998 F/O ELECTRIC SEAT INOP. SPARK AND SMOKE OBSERVED FROM ELECTRICAL POWER CORD TO SEAT. REPLACED SEAT POWER CABLES. OPS OK. 2 L 7 2 4F RT A2NM 2001080200058 20010802 00058 NM 2001 8 2 DL757010992 1 20010616 A 3350 767 LIGHT BOEING 757 757232 1384965 NM R3 DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 624DL 22914 FOUND ON L/O, R-3 EMERGENCY DOOR LIGHT INOP. RELAMPED SAME. 2 L 7 2 4F RT A2NM 2001080200059 20010802 00059 NE 2001 8 2 DL757010993 2 20010617 A 7200 PW2037 ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 LACK OF LUBE A DALA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 27 608DA 44221 22815 716448 EN ROUTE DFW-ATL, GOT A LOW OIL QTY EICAS MSG, LEFT ENGINE OIL QTY READ 0. OIL PRESSURE MIN IN RED, CAPT PER POM SHUT E NGINE DOWN. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001080200060 20010802 00060 NM 2001 8 2 DL757011019 1 20010620 A 2910 271N61192 HYDRAULIC LINE BOEING 757 757232 1384965 NM RT MLG LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 685DA 27588 LT HYD QTY AND PRESSURE LOST IN FLT. FOUND RIGHT MLG DOWNLOCK ACTUATOR PRESSURE LINE LEAKING. REPLACED LINE. LEAK CHE CKS OK. 2 L 7 2 4F RT A2NM 2001080200061 20010802 00061 NE 2001 8 2 N32B2001002 2 20010523 A 8530 356993 CYLINDER DOUG DC6 DC6A 3021706 WP PWA R2800 R2800* 52026 NE NR 2 ENGINE CRACKED A NACA K NONE O OTHER IN INSP/MAINT 1 AL 03 7780B 624 624 45372 A625WJP NR 3 ENGINE FEATHERED AT 00172, DUE TO RUNNING ROUGH. 2 L 7 4 4R 4 R 6A3 5E8 2001080200063 20010802 00063 WP 2001 8 2 MWEA011092 1 20010802 A 5310 59114279 LONGERON DOUG DC9 DC932 3022066 WP STATION 965 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 LONGERON 17 CRACKED AT STATION 965 LEFT SIDE VIEWABLE WITH MIRROR ON BOTTOM SIDE. -- REMOVED DAMAGED LONGERON SECTION, FABRICATED NEW SECTION AND LONGERON SPLICE, INSTALLED LONGERON ASSOCIATED ITEMS AND LONGERON SPLICE. 2 L 7 2 4F A6WE 2001080200064 20010802 00064 WP 2001 8 2 MWEA011093 1 20010802 A 5230 59101417 PAN DOUG DC9 DC932 3022066 WP FWD CARGO DOOR TORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 FORWARD CARGO DOOR INNER PAN IS TORN BY A BN FASTENER AT THE AFT END AT BEAM #3. -- REMOVED DAMAGE, FABRICATED AND IN STALLED REPAIR. DOUBLER. 2 L 7 2 4F A6WE 2001080200065 20010802 00065 WP 2001 8 2 MWEA011094 1 20010802 A 5755 3923258504 SUPPORT BRACKET DOUG DC9 DC932 3022066 WP RIGHT WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 RIGHT WING OUTBOARD SPOILER TORSION BAR SUPPORT BRACKET IS CRACKED. -- REMOVED SUPPORT BRACKET, INSTALLED NEW SUPPORT BRACKET. 2 L 7 2 4F A6WE 2001080200066 20010802 00066 NE 2001 8 2 DL757011037 2 20010621 A 7200 PW2037RTC ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 MALFUNCTIONED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 694DA 29726 727289 FL 1000 AGL WHILE SELECTING CLIMB POWER HEARD LOUD BANG AND FELT JOLT. PASSENGER REPORTED FLASH. ALL ENGINE INDICATION NORMAL. PER FIM PERFORMED BORO OF 6-18 STAGE COMPRESSOR AND 1-2 STAGES TURBINE BLADES. ALL OK. INSTALLED ALL BORO PL UGS AND PAD DRIVE. CHECKED CHIP DETECTORS AND REPLACED OIL SCREEN. NO METAL NOTED. ALL CKS GOOD PER FIM 71-05-00, NR 1 SVA CHANGED PER SET-UP. 2 L 7 2 4F 4 F RT A2NM E17NE 2001080200067 20010802 00067 CE 2001 8 2 NT22001F00000 1 20010625 A 5312 0823400109 BULKHEAD CESSNA 414 414 2075908 CE CONT O520 TSIO520* 17040 SO FUSELAGE CRACKED B NT2R K NONE O OTHER IN INSP/MAINT 1 CE 07 105GB 4896 4140644 DURING ANNUAL INSPECTION, THE LEFT TIP TANK AFT SUPPORT BULKHEAD PN 0823400-109, WAS FOUND TO BE CRACKED. THE CRACK WA S LOCATED APPROXIMATELY .2500 INCH ABOVE THE TOP ADJUST HOLE THAT ATTACHES THE FORWARD DOUBLER TOT THE -109 BULKHEAD. T HE CRACK WAS APPROX 2 INCHES LOG, EXTENDING THRU THE BEND RADIUS. AT THIS TIME, ALL DISCREPANCY'S HAVE BEEN LIMITED TO LEFT SIDE. 1 L 7 2 3O 3 O RT A7CE E8CE 2001080200068 20010802 00068 NE 2001 8 2 DL757011042 2 20010622 A 7261 TUBE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE CLOGGED A DALA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 27 661DN 24972 726701 AT FLT LVL 330 IN CRUISE, NOTICED OIL PRESS LIGHT FLICKERING. LOOKED AT OIL PRESS IND, IT WAS RED. RT OIL PRESS LIGHT CAME ON STEADY, OIL QTY WAS AT 0. FOUND NR 5 BEARING SCAVENGE TUBE CLOGGED WITH CARBON. CORRECTED SAME. 2 L 7 2 4F 4 F RT A2NM E17NE 2001080200069 20010802 00069 NE 2001 8 2 PAI2001F00000 3 20010530 A 6111 L106FA0 BLADE BAG JETSTM JETSTM3201 1500217 EU MCAULY 4HFR34 4HFR34C653 NE PROPELLER CRACKED B PAIR K NONE O OTHER IN INSP/MAINT 1 SO 05 915AE 920887 915 920887 DURING EDDY CURRENT INSPECTION, FOUND EVIDENCE OF A POSSIBLE CRACK IN THE BLADE AT THE 43.500 IN STATION. WILL SEND BLA DE TO MCCAULEY FOR EVALUATION AND FINAL INSPECTION. 2 L 7 2 4T RT A56EU 6 C 3PNE 2001080200070 20010802 00070 NM 2001 8 2 DL757011048 1 20010623 A 2530 831620403MODA OVEN BOEING 757 757232 1384965 NM GALLEY MALFUNCTIONED A DALA H DEACTIVATE SYST/CIRCUITS O OTHER CR CRUISE 1 SO 27 632DL 23613 F/C AFT OVEN WORKING INTERMITTENTLY, MAY HAVE SEEN SPARKS ABOVE BUN WARMER. OVEN APPEARS TO OPERATE NORMAL AT GATE. FO R PRECAUTION C/B PULLED AND COLLARED. OVEN FWD TO MCO AND PLACARD. 2 L 7 2 4F RT A2NM 2001080200071 20010802 00071 NM 2001 8 2 DL757011053 1 20010624 A 2910 271N64111063 LINE BOEING 757 757232 1384965 NM NLG WW BROKEN A DALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 27 611DL 22818 A/C ATB WITH LT HYD SYS FAILURE. FOUND LINE IN NOSE WHEEL WELL BROKEN TO NLG SEQUENCING VALVE. REPLACED LINE. 2 L 7 2 4F RT A2NM 2001080200072 20010802 00072 EU 2001 8 2 PIV2001F00000 1 20010624 A 6120 GOVERNOR STBROS SD3 SD360 8100606 EU PROPELLER OUT OF RIG A PIVA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 WP 13 711PK SH3696 PILOTS ADVANCED POWER LEVER TO OBTAIN T/O POWER. NOTICED RIGHT ENGINE DID NOT OBTAIN REQUIRED TORQUE FOR T/O. TAKE OFF WAS ABORTED AND AIRCRAFT RETURNED TO BASE. PRIOR: A PROP GOVERNOR WAS REPLACED DUE TO TORQUE CREEPING UP BY 500 LBS. PROP GOVERNOR WAS RIGGED ACCORDINGLY TO MM AND GROUND RUN WAS PERFORMED BEFORE RELEASE, AFTER RELEASE IS WHEN THE INCIDE NT HAPPENED. AFTER: PROP TORQUE INDICATOR WAS REPLACED AND STILL SAME UNSAT REPORTS. RIGGING THEN WAS RECHECKED TO MA KE SURE NO STRECHING OR SETTING OCCURRED. MAINTENANCE FOUND PROP GOVERNOR RESET ARM NOT MAKING CONTACT WITH ITS STOP. FURTHER RIGGING WAS TAKEN TO ASSURE CONTACT, GROUND RUN PERFORMED. RESULTS SATISFACTORY, AC RETURN TO SERVICE. 2 H 7 2 4T A41EU 2001080200073 20010802 00073 NM 2001 8 2 DL757011062 1 20010625 A 3520 9700C1AF20D OXYGEN BOTTLE BOEING 757 757232 1384965 NM R2 DOOR LOW A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 684DA 27104 R2 DOOR PAX O2 BOTTLE LOW. REPLACED BOTTLE. 2 L 7 2 4F RT A2NM 2001080200074 20010802 00074 SO 2001 8 2 R2J2001F00000 1 20010523 A 3230 CH20261 TORQUE LINK PIPER PA31 PA31350 7103110 SO MLG CORRODED B R2JR K NONE O OTHER IN INSP/MAINT 1 EA 21 13FS 318352024 WHILE PERFORMING LANDING GEAR CHECKLIST ITEM ON ANNUAL INSPECTION FOUND BUBBLES IN PAINT ON LANDING GEAR TORQUE LINKS, A DJACENT TO LANDING GEAR SQUAT SWITCH MOUNTING HOLE. FOUND SEVERE EXFOLIATION CORROSION UNDER PAINT: STC HOLDER CONTACT ED AND LINKS WERE REPLACED WITH NEW FAA-PMA FACTS. STEEL SWITCH IS MOUNTED ON ALUMINUM LINK AND IS LOCATED IN ENGINE EX HAUST STREAM. THIS AREA NEEDS EXTRA CLOSE INSPECTION- LINK FAILURE COULD CAUSE LOSS OF CONTROL ON LANDING. 1 L 7 2 3O A20SO 2001080200075 20010802 00075 NM 2001 8 2 DL757011104 1 20010703 A 3350 20131A BATTERY BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 669DN 25142 LEFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY, OP CKS GOOD. 2 L 7 2 4F RT A2NM 2001080200076 20010802 00076 EA 2001 8 2 RU32001F00000 1 20010703 A 4930 38826081H COVER CNDAIR CL600 CL6002B16 1900305 EA APU BROKEN E RU3A K NONE O OTHER IN INSP/MAINT 1 SW 15 87 5190 APU MODEL NUMBER GTCP 36-150RJ. THE LOW PRESSURE FUEL FILTER COVER MOUNTING EAR WAS COMPLETELY BROKEN OFF THE COVER WHE RE THE MOUNTING BOLT ATTACHES THE COVER TO THE FUEL CONTROL. APU CONTINUED TO RUN AFTER EAR BROKE OFF. 2 L 7 2 4F RT A21EA 2001080200077 20010802 00077 NM 2001 8 2 DL757011112 1 20010704 A 5330 141N38517 SKIN BOEING 757 757232 1384965 NM FUSELAGE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 640DL 23994 THE FUSELAGE SKIN WAS FOUND WITH A GOUGE AT FS 283 ABOVE THE STRINGER 20R SKIN LAP SPLICE. 2 L 7 2 4F RT A2NM 2001080200078 20010802 00078 CE 2001 8 2 S8A2001F00000 1 20010530 A 3213 MS24665357 PIN CESSNA 208 208B 2073701 CE LT MLG STRUT MISSING B S8AR K NONE O OTHER IN INSP/MAINT 1 SO 05 802AA 208B0873 UPON INITIAL 200 HOUR INSPECTION SINCE NEW, AC, FOUND LEFT LOWER LIFT STRUT MISSING THE COTTER PIN THAT SAFETIES THE NUT AND BOLT SECURING THE LIFT STRUT TO THE FUSELAGE. MAINTENANCE MANUAL SPECIFIES SNUG TIGHT THEN ADVANCE TO PIN ALIGNMEN T AND SAFETY. THE WAS EVIDENCE OF BOLT AND NUT MOVEMENT. 1 H 7 1 3T A37CE 2001080200079 20010802 00079 NM 2001 8 2 DL757011130 1 20010707 A 3397 WIRE BOEING 757 757232 1384965 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 628DL 22918 EMERGENCY EXIT LIGHT INOP AT 2R DOOR. REPAIRED BROKEN WIRES. 2 L 7 2 4F RT A2NM 2001080200080 20010802 00080 CE 2001 8 2 SD92001F00000 1 20010517 A 2121 57033 BLOWER CESSNA 500 560CESSNA 2076750 CE COCKPIT DEFECTIVE E SD9A O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 07 832QB 5600110 FLIGHT DECK AREA OF AIRCRAFT EXPERIENCED SMOKE. THE SOURCE OF SMOKE WAS THE DEFOG BLOWER MOTOR ASSEMBLY. (NOTE: CIRCUI T BREAKER DID NOT TRIP) 2 L 7 2 4F RT A22CE 2001080200081 20010802 00081 2001 8 2 DL757011165 4 20010713 A 3413 0665000110 INDICATOR BOEING 757 757232 1384965 NM COCKPIT DEFECTIVE A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 626DL 22916 NO SHUTDOWN OF RIGHT ENGINE AT GATE IN DFW WITH GROUND POWER CONNECTED, ELECTRICAL SMOKE POURED OUT OF F/O INSTURMENT PA NEL ON RIGHT HAND SIDE. SECONDARY INDICATION WAS F/O VSI BLANKED OUT WITH NO DISPLAY. PULLED OUT ALL F/O'S INSTRUMENT PANELS AND INSPECTED INSTRUMENTS AND WIRING. FOUND F/O'S VSI INDICATOR WITH EVIDENCE OF SMOKE BURN. REPLACED INDICATOR . OPS GOOD. OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2001080200082 20010802 00082 EA 2001 8 2 SH52001F00000 1 20010618 A 2842 601621571 FLOAT SWITCH CNDAIR CL600 CL6002B16 1900305 EA TAIL TANK FAILED B SH5R O OTHER O OTHER NR NOT REPORTED 1 NE 03 307FX 4897 5179 REMOVED AND REPLACED THE TAILTANK FUEL PUMP AFTER THE CIRCUIT BREAKER POPPED WHILE DOING A FUEL TRANSFER FUNCTIONAL CHEC K. UPON TRYING THE FUNCTIONAL CHECK AGAIN, IT WAS FOUND THAT THE PUMP RAN CONTINUOUSLY IN THE ARM POSITION. ARCING WAS FOUND ON THE POSITIVE TERMINAL OF THE PUMP THAT WAS REMOVED. IT WAS FOUND THAT THE LOW LEVEL FLOAT SWITCH WAS NOT SHUT TING THE PUMP OFF. NEED TO IMPROVE SHUT OFF SWITCH OR ADD BACK UP SYSTEM TO PREVENT THE PUMP FROM RUNNING WITH THE TANK EMPTY. 2 L 7 2 4F RT A21EA 2001080200083 20010802 00083 NE 2001 8 2 DL757011173 2 20010715 A 7200 PW2037RTC ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 SURGES A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 610DL 26602 22817 726715 RIGHT ENG SURGED ON TAKEOFF BETWEEN 80 AND 95 KTS. TWO LARGE SURGES AND DISCONTINUED AT 95 KTS. EPCS PAGE SHOWED P SVA F/B INT. T/S PER FIM. NO FAULTS IN CIRCUIT BETWEEN EEC AND SVA. CLEANED C/PS. RAN ENG TO T/O PWR REF PFHB. NO SURG ES - SVA MSG DID NOT RE-APPEAR. 2 L 7 2 4F 4 F RT A2NM E17NE 2001080200084 20010802 00084 WP 2001 8 2 STZ2001F00000 2 20010613 A 7320 FUEL CONTROL LEAR 35 35LEAR 5170600 CE GARRTT TFE731 TFE73122B 01518 WP NR 2 ENGINE MALFUNCTIONED E STZA K NONE O OTHER IN INSP/MAINT 1 AL 03 90WR 35022 P74147C ON IFR APPROACH, LEVEL AT 3400 FEET IN CLOUDS, AIRSPEED JUST UNDER 200 KNOTS, THE PILOT DROPPED FLAPS, EXTENDED GEAR, AN D REDUCED POWER TO 62 PERCENT. AT THIS POINT, THE NR 2 ENGINE FLAMED OUT. THE PILOT CALLED MISSED APPROACH AND DECLARE D EMERGENCY. HE THEN SECURED THE ENGINE IAW THE CHECKLIST AND HEADED BACK TO HOME BASE AND VFR CONDITIONS. AT 10,000 H E ATTEMPTED A SUCCESSFUL RESTART. AFTER LANDING, ON THE TAXI IN THE ENGINE FLAMED OUT AGAIN. IT IS SUSPECTED THAT THE FUEL CONTROL UNIT IS FAULTY. 2 L 7 2 4F 4 F A10CE E6WE 2001080200085 20010802 00085 NM 2001 8 2 DL757011198 1 20010719 A 2421 GENERATOR BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE FAILED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 644DL 31669 23998 716585 RIGHT GEN FAILED DURING TAKEOFF ROLL. RIGHT ENGINE DRIVE AND RIGHT ENGINE GEN OFF EICAS MSGS. TAKEOFF ABORTED. FWD TO MCO AND PLACARD MEL 24-00-01. 2 L 7 2 4F 4 F RT A2NM E17NE 2001080200088 20010802 00088 NM 2001 8 2 DL75A011118 1 20010705 A 5310 146N851210 DOOR FRAME BOEING 757 757212 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 751AT 23125 THE LOWER SILL CAP OF THE C2 DOOR SURROUND STRUCTURE WAS BADLY CORRODED AND REQUIRED REPLACEMENT. 2 L 7 2 4F RT A2NM 2001080200090 20010802 00090 NM 2001 8 2 DL75A011160 1 20010712 A 5330 143N853017 BEAR STRAP BOEING 757 757212 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 751AT 23125 THE C2 DOOR SURROUND BEARSTRAP AT FS 1380 WAS FOUND WITH TWO AREAS OF CORROSION AT STRINGERS 22R AND 23R. 2 L 7 2 4F RT A2NM 2001080200092 20010802 00092 NE 2001 8 2 DL75A011210 2 20010717 A 7311 471111172 COOLER BOEING 757 757212 NM PWA 2037 PW2037 NE NR 2 ENGINE LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 751AT 23125 716503 ACFT DIVERTED TO MIA EN ROUTE TO BOG DUE TO RT ENG LOW OIL QTY. FOUND ENG FUEL OIL COOLER. F/O COOLER LEAKING AT ENG O IL INLET ELBOW ADAPTER. REPLACED F/O COOLER. LEAK CHECK NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2001080200094 20010802 00094 CE 2001 8 2 TIM2001F00000 1 20010516 A 2720 CONTROL CABLE BEECH 99 99A 1154003 CE RUDDER FRAYED B K NONE O OTHER IN INSP/MAINT 1 NM 07 99GH 38271 U112 DURING A DETAILED INSPECTION OF THE CONTROL CABLES, THE RUDDER CABLE WAS FOUND TO BE FRAYED ABOUT 3 INCHES AFT OF A PULL EY IN THE BILGE JUST AFT OF THE AIR STAIR DOOR. THE AFFECTED RUDDER CABLE WAS REMOVED AND THE OTHER INSPECTED FOR SIMIL AR DAMAGE. NO DAMAGE FOUND. THIS DISCREPANCY APPEARS TO THE RESULT OF NORMAL WEAR AS THERE WAS NO CONTRIBUTING FACTORS TO CAUSE SUCH WEAR. 1 L 7 2 3T A14CE 2001080200095 20010802 00095 CE 2001 8 2 TIM2001F00002 1 20010618 A 2730 1156100163 COLLAR BEECH BEECH 99 99 1154002 CE PWA PT6 PT6A27 52043 EA LEFT ELEVATOR CRACKED E TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 4381Y 37440 U71 DURING AN INSPECTION IT WAS DISCOVERED THAT THE LEFT OUTBOARD ELEVATOR TORQUE TUBE COLLAR HAD A CRACK EXTENDING FROM A T APER PIN HOLE. A REVIEW OF THE MAINTENANCE INSTRUCTIONS REVEALED THE POSSIBILITY OF OVERTORQUE. THIS PARTICULAR PROBLE M COULD HAVE BEEN EITHER MAINTENANCE OR NORMAL WEAR. A DISCUSSION OF PROPER MAINTENANCE PROCEDURES REGARDING THE TORQUE TUBE TOOD PLACE WITH THE MECHANICS INVOLVED. 1 L 7 2 3T 4 T A14CE E4EA 2001080200096 20010802 00096 EA 2001 8 2 TIM2001F00003 2 20010516 A 7322 252444076 FUEL CONTROL BEECH 99 99 1154002 CE PWA PT6 PT6* 52043 EA LEFT ENGINE MALFUNCTIONED E TIMA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 NM 07 95WA 277 U6 ENGINE REPORTEDLY BACKFIRED AND SURGED AT HIGH POWER SETTINGS WHEN MAKING CHANGES IN POWER SETTING. ENGINE PASSED ALL G ROUND PERFORMANCE CHECKS SO A FCU WAS REPLACED FOR TROUBLESHOOTING. ITS UNKNOWN WHAT CAUSED THE FCU TO MALFUNCTION DURI NG THE ACCELERATION MODE. 1 L 7 2 3T 3 T A14CE E2NE 2001080200097 20010802 00097 NM 2001 8 2 DL764010937 1 20010609 A 2450 766302E BPCU BOEING 767 767432ER NM E/E BAY FAULTY A DALA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 SO 27 825MH 29696 AT FL 370 LOST F/D - AUTOTHROTTLES AND A/P LATER WE GOT L/E SLAT DISAGREE CAUTION MSG ALONG WITH NUMEROUS ADVISORY MSGS. AILERON LOCKOUT AND STBY BUS OFF, ALSO NOTICED THAT DC STBY BUS C/B AND BUS DISTR C/B HAD POPPED AFTER LANDING. ONCE ON GROUND MTC RESET CBS, ALL MSGS CLEARED. INSPECTED BATTERY AND CHARGER, CKS OK. INSPECTED RELAYS K105-K109 CKS OK. BPCU SHOWED NO FAULTS. REPLACED BPCU AS PRECAUTIONARY. MTC FERRIED TO ATL ON 9936. REPLACED OVERHEAD PANEL, K109¥ K10 6 AND K104 RELAYS STDBY POWER FOR PRECAUTION. 2 L 7 2 4F RT A1NM 2001080200098 20010802 00098 CE 2001 8 2 TIM2001F00004 1 20010618 A 2720 505243269 ARM BEECH 99 99 1154002 CE RUDDER PEDEL WORN E TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 99GH 38271 U112 DURING INSPECTION, THE RUDDER PEDAL PIVOT HOLES WERE FOUND TO BE ELONGATED. THE WEAR APPEARS TO BE NORMAL. THE RUDDER PEDAL ARM WAS REPLACED WITH A SERVICEABLE ARM AND SAFTIED AND LUBED. SINCE THE RUDDER PEDAL IS A HIGH USE ASSEMBLY, A HEAVIER LUBRICATING MEDIUM SHOULD BE CONSIDERED. A LIGHT GREASE MIGHT PROVIDE BETTER PROTECTION AGAINST WEAR. 1 L 7 2 3T A14CE 2001080200099 20010802 00099 NM 2001 8 2 DL764010945 1 20010610 A 5753 RIVET BOEING 767 767432ER NM T/E FLAP SHEARED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 837MH 29710 DAMAGE FOUND ON ARRIVAL. LT WING OUTBOARD FLAP WELL CLOSURE PANEL L/E RIVETS 30 SHEARED OFF. SUPPORT ROD UPPER CLEVIS ATTACH BRACKET ELONGATED. CLOSURE PANEL WIGGLE STRIP DAMAGED WHEN RIVETS PULLED THRU. REATTACHED BRACKET. UNABLE TO D O PERMANENT REPAIR. OK FOR FERRY FLIGHT. REPLACED BRACKET AND WIGGLE PLATES PER BAC DWG 113T1663. 2 L 7 2 4F RT A1NM 2001080200100 20010802 00100 EA 2001 8 2 TJ42001F00000 1 20010620 A 3411 GT3153R STATIC PORT CNDAIR CL604 CL604 EA FUSELAGE DAMAGED B TJ4R K NONE O OTHER IN INSP/MAINT 1 GL 11 15SP 6045402 WHILE TROUBLESHOOTING A STATIC LEAK ON THE EMERGENCY STATIC SYSTEM, I FOUND A PIN HOLE IN THE CASTING OF THE STATIC PORT . THIS PIN HOLE WAS INSIDE THE PRESSURE VESSLE AND WAS LEAKING AT A RATE OF 200 FPM. THIS PROBLEM IS NOT DETECTABLE UNL ESS ONE IS CHECKING THE STATIC SYSTEM. FEEL THIS COULD BE A SAFETY HAZZARD IF THE PILOTS HAD TO RELY ON THE EMERGENCY STATIC SYSTEM, DUE TO A POSSIBLE DIFFERANCE IN ACTUAL ALTITUDE AND INDICATED ALTITUDE ON AN APPROACH TO LAND. 2 L 7 2 4F RT A21EA 2001080200101 20010802 00101 NM 2001 8 2 DL764011026 1 20010620 A 2781 114T41457 TARGET BOEING 767 767432ER NM L/E SLAT BROKEN A DALA O OTHER N FALSE WARNING AP APPROACH 1 SO 27 826MH 29697 L/E SLAT ASYM ON APPROACH WHEN FLAPS 20 SELCETED AT APPROX 205 KIAS, LANDING COMPLETED AT FLAPS 20. REPLACED PROX TARGE T ON LT WING L/E SLAT. 2 L 7 2 4F RT A1NM 2001080200102 20010802 00102 WP 2001 8 2 UG82001F00000 2 20010629 A 7314 307085057 PUMP RAYTHN DH125 HAWKER800 7450004 CE GARRTT TFE731 TFE7315R 01518 WP RT ENGINE MALFUNCTIONED E UG8A K NONE O OTHER IN INSP/MAINT 1 GL 13 980DC 3322 258267 P91656 RIGHT ENGINE FUEL (PRESSURE) ANNUNICIATOR ILLUMINATED. ENGINE DRIVEN FUEL PUMP PERFORMANCE DEGRADING. REPLACED ENGINE DRIVEN FUEL PUMP WITH AN OVERHAULED UNIT. 2 L 7 2 4F 4 F RT A3EU E6WE 2001080200103 20010802 00103 NM 2001 8 2 DL764011054 1 20010624 A 5754 114T41457 BOLT BOEING 767 767432ER NM L/E SLAT FAILED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 829MH 29700 LEADING EDGE SLAT TRACK BOLT FAILED ALLOWING PROX TARGET AND BEARING TO DEPART AIRCRAFT. REPLACED BOLT. 2 L 7 2 4F RT A1NM 2001080200104 20010802 00104 SO 2001 8 2 UG8AD01016 1 20010531 A 2432 407611 BATTERY GULSTM G1159 GIV 3980115 SO RROYCE TAY TAYMK6118 NE BATTERY BAY FAILED E UG8A K NONE O OTHER IN INSP/MAINT 1 GL 23 940DC 1052 NUMBER 2 BATTERY FAILED (DEAD). APPARENT CAUSE: GROUND SERVICE BUS WAS LEFT ENERGIZED. REPLACE NR 2 BATTERY. AIRCRA FT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A12EA A25NE 2001080200105 20010802 00105 EU 2001 8 2 UO22001F00000 1 20010621 A 2810 MS2952132 FLAPPER VALVE ISRAEL GALAXY GALAXY 4500307 EU FUEL SYSTEM LEAKING B UO2R K NONE K FLUID LOSS IN INSP/MAINT 1 GL 19 622SV 015 THE AIRCRAFT CREW REPORTED THAT WHEN THE PLANE SAT OVERNIGHT, THE CENTER TANK WOULD HAVE MORE FUEL IN THE MORNING. WHEN THE NEW WING ROOT FLAPPER VALVES WERE INSTALLED THE FUEL MIGRATION CEASED. THE OLD (REMOVED) FLAPPER VALVES WERE MISSI NG THEIR RETENTION SPRINGS ALLOWING FOR A BAD SEAL. CAUSE: NO RETENTION SPRINGS ON THE FLAPPER VALVES. 2 L 7 2 4F RT A53NM 2001080200106 20010802 00106 EU 2001 8 2 UO22001F00001 1 20010621 A 5310 4AS353504530 SHOCK MOUNT ISRAEL GALAXY GALAXY 4500307 EU FWD FUEL TANK CHAFED B UO2R K NONE O OTHER IN INSP/MAINT 1 GL 19 62GX 20 031 A REPAIR WAS GENERATED TO CORRECT FOR A POSSIBLE METAL TO METAL CHAFING PROBLEM. AN INSPECTION REVEALED THAT THE UPPER AFT EDGE OF THE FORWARD FUEL TANK INTERFERES WITH THE FORWARD LOWER CORNERS OF THE FLAP DRIVE MOTOR SHOCK MOUNT SUPPORTS . PROBABLE CAUSE: MFG ENGINEERING AND QUALITY CONTROL. 2 L 7 2 4F RT A53NM 2001080200107 20010802 00107 EU 2001 8 2 UO22001F00002 1 20010619 A 5310 4AS353504531 SHOCK MOUNT ISRAEL GALAXY GALAXY 4500307 EU FWD FUEL TANK CHAFED B UO2R K NONE O OTHER IN INSP/MAINT 1 GL 19 60GX 24 028 A REPAIR WAS GENERATED TO CORRECT FOR A POSSIBLE METAL TO METAL CHAFING PROBLEM. AN INSPECTION REVEALED THAT THE UPPER AFT EDGE OF THE FORWARD FUEL TANK INTERFERES WITH THE FORWARD LOWER CORNERS OF THE FLAP DRIVE MOTOR SHOCK MOUNT SUPPORTS HAT SECTIONS. PROBABLE CAUSE: MANUFACTURE ENGINEERING AND QUALITY CONTROL. 2 L 7 2 4F RT A53NM 2001080200108 20010802 00108 GL 2001 8 2 DL764011176 2 20010716 A 7200 CF680C2B8F ENGINE BOEING 767 767432ER NM GE CF6 CF680C2* GL NR 2 SURGES A DALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 27 828MH 2365 29699 706121 AFTER T/O RIGHT ENG SURGED 3 TIMES WITH ENGINE PARAMETERS FLUCTUATING. HOWEVER ENGINE REMAINED RUNNING AND AFTER LANDIN G VIBES WENT TO 4.8. MAINT WAITING ON ENGINE FROM ATL 2 L 7 2 4F 4 F RT A1NM E23EA 2001080200109 20010802 00109 EU 2001 8 2 UO22001F00003 1 20010619 A 5320 4A3582510012 CHANNEL ISRAEL GALAXY GALAXY 4500307 EU RADIO RACK MISDRILLED B UO2R K NONE O OTHER IN INSP/MAINT 1 GL 19 60GX 24 028 AN ELONGATED FASTENER HOLE WAS MIS DRILLED FROM THE MANUFACTURER. A REPAIR WAS GENERATED FOR THE RIGHT HAND RADIO RACK SUPPORT CHANNEL. PROBABLE CAUSE: MANUFACTURING 2 L 7 2 4F RT A53NM 2001080200110 20010802 00110 NM 2001 8 2 DL764011183 1 20010716 A 3350 D71701100 BATTERY PACK BOEING 767 767432ER NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 834MH 29707 ON PRE-DEPARTURE CHECK FOUND AFT LEFT CABIN EMERGENCY LIGHT DO NOT OPERATE. REPLACED BATTERY PACK AT 48GF SIDEWALL. OP S NORMAL. 2 L 7 2 4F RT A1NM 2001080200111 20010802 00111 EU 2001 8 2 UO22001F00005 1 20010716 A 4997 WIRE ISRAEL GALAXY GALAXY 4500307 EU PWA 306 PW306B NE APU START MISINSTALLED B K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 19 62GX 20 20 031 POWER AND GROUND WIRES ROUTED TO APU STARTER THROUGH FIRE WALL WERE ROUTED 180 DEGREES OUT OF SEQUENCE AND SUBSEQUENTLY CONNECTED TO WRONG SIDE OF APU STARTER. THIS CONDITION EXISTED FROM THE MANUFACTURER. ADDITIONAL WIRE MARKINGS DESIGNA TING GROUND AND POWER CABLES SHOULD BE UTILIZED. 2 L 7 2 4F 4 F RT A53NM E35NE 2001080200112 20010802 00112 EU 2001 8 2 UO22001F00006 1 20010716 A 4997 WIRE ISRAEL GALAXY GALAXY 4500307 EU PWA 306 PW306B NE APU START MISINSTALLED B K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 19 90GX 25 25 040 POWER AND GROUND WIRE ROUTED TO APU STARTER THROUGH FIRE WALL WER ROUTED 180 DEGREES OUT OF SEQUENCE AND CONNECTED TO WR ONG SIDE OF APU STARTER. THIS CONDITION EXISTED FROM THE MANUFACTURER. ADDITIONAL WIRE MARKINGS DESIGNATING GROUND AND POWER CABLES SHOULD BE UTILIZED. 2 L 7 2 4F 4 F RT A53NM E35NE 2001080200113 20010802 00113 WP 2001 8 2 V3E2001F00000 1 20010228 A 3221 5910449527 MOUNT DOUG DC9 DC931 3022065 WP NLG CRACKED B V3EY K NONE O OTHER IN INSP/MAINT 1 WP 33 976 21158 48147 UPON REMOVAL OF NOSE LANDING GEAR, IAW MM AND JOB CARD T932-204, FOR OVERHAUL REASON. FOUND THAT THE LOWER OUTBOARD EAR OF THE NOSE LANDING GEAR WHICH ATTACHES THE RETURN ACTUATOR, WAS CRACKED OFF THE NOSE LANDING GEAR. TOTAL CYCLES 21,15 8, TIME SINCE OVERHAUL IS 21,158, TIME REMAINING IS 842 CYCLES. 2 L 7 2 4F A6WE 2001080200114 20010802 00114 CE 2001 8 2 VJ32001F00000 1 20010703 A 2421 648843 ALTERNATOR BEECH 33 F33A 1151425 CE TERMINAL POST DEFECTIVE A VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 5540P 106 CE1335 NUT ON AUX TERMINAL POST IS STRIPED AND LOOSE IN CASE. REMOVED FROM ENGINE AND SENT IN FOR WARRANTY. 1 L 7 1 3O 3A15 2001080200115 20010802 00115 CE 2001 8 2 VWY2001F00000 1 20010419 A 5312 082340063 BULKHEAD CESSNA 402 402B 207590P CE MAIN FUEL TANK CRACKED E VWYA K NONE O OTHER IN INSP/MAINT 1 SW 17 1577T 402B0546 WHILE PERFORMING 100 HOUR OR ANNUAL INSPECTIONS WE ARE FINDING THE AFT BULKHEAD ON THE MAIN FUEL TANKS CRACKED AT THE IN BOARD SIDE BEND RADIUS WHERE IT ATTACHES TO THE WING. ALL CRACKS ON ALL THE BULKHEADS WERE IN THE SAME GENERAL AREA. W E HAVE FOUND THAT BOTH THE LEFT AND RIGHT BULKHEADS ON OUR 402B0546 WERE CRACKED, BOTH WERE REPLACED. 1 L 7 2 3O A7CE 2001080200116 20010802 00116 GL 2001 8 2 WP2001B2495 1 20010511 A 3350 770703 POWER SUPPLY BOMBDR BD700 BD7001A10 1390006 GL CABIN UNSECURE A K NONE L NO TEST IN INSP/MAINT 1 SW 15 700AQ 24 9025 WHEN POWER SUPPLY WAS OPENED, WE DISCOVERED HARDWARE TO HAVE WORKED LOOSE AND WAS MOVING AROUND INSIDE OF THE BOX. ONE BOLT HAD LOGED ITSELF BETWEEN A TERMINAL STRIP AND THE BOX SIDEWALL (THE BOLT WAS WELDED IN PLACE) WASHERS WERE DISCOVER ED ELSEWHERE IN THE BOX. CAUSE: FAILURE TO SECURE BOLT IN PLACE. SUGGEST TIGHTER QUALITY MEASURES FOR INSPECTING THE P OWER SUPPLY. 2 L 7 2 4F RT T00003NY 2001080200120 20010802 00120 NM 2001 8 2 DL767010926 1 20010605 A 5311 148T27409 FRAME BOEING 767 767232 1385132 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 101DA 22213 ACCOMPLISHMENT OF PERMANENT REPAIR FOR CRACKED CHORD PER SB 767-53-0078. 2 L 7 2 4F RT A1NM 2001080200121 20010802 00121 SO 2001 8 2 WVBA2001037 1 20010620 A 2822 RG908J7AM PUMP PIPER PA31 PA31350 7103110 SO FUEL SYSTEM FAILED A WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 27755 518 317852148 PILOT REPORTED FUEL PRESSURE 50 PSI AT CRUISE POWER SETTINGS. PUMP WOULD NOT ADJUST WITHIN PARAMETERS. NO MID ADJUSTME NT. PUMP WAS REMOVED AND REPLACED. 1 L 7 2 3O A20SO 2001080200122 20010802 00122 SO 2001 8 2 WVBA2001038 1 20010620 A 2822 RG908J7AM PUMP PIPER PA31 PA31350 7103110 SO FUEL SYSTEM FAILED A WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 4082T 392 318152089 PILOT REPORTED DECREASE IN FUEL PRESSURE AT CRUISE POWER SETTINGS. PUMP WAS REMOVED AND REPLACED. 1 L 7 2 3O A20SO 2001080200123 20010802 00123 SO 2001 8 2 WVBA2001039 1 20010706 A 2822 RG090J4AM PUMP PIPER PA31 PA31350 7103110 SO FUEL SYSTEM FAILED A WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 59829 341 317652081 DURING PRE-INSPECTION RUN UP, IT WAS OBSERVED THAT THE FUEL PRESSURE WAS 34 PSI AT 1500 RPM. THE PUMP WAS ADJUSTED UP . 5000 TURN AND WAS STILL 34 PSI (LOW RED LINE) FROM IDLE TO 1900 RPM. PUMP WAS REMOVED FROM SERVICE. 1 L 7 2 3O A20SO 2001080200125 20010802 00125 WP 2001 8 2 Y2PA01015 1 20010508 A 3234 TWA418282 SWITCH DOUG DC9 DC915F 3022037 WP GEAR DOWN SWITCH INOPERATIVE E Y2PA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 23 197US 47155 RIGHT MAIN GEAR LIGHTS WOULD NOT ILLUMINATE WITH LANDING GEAR DOWN. CREW ACCOMPLISHED COM PROCEDURE AND MADE LOW FLY OV ER. TOWER CONFIRMED RIGHT MAIN GEAR APPEARED DOWN. CREW DECLARED EMERGENCY AND REQUESTED CRASH AND FIRE EQUIPMENT STAN DBY. AIRCRAFT MADE A NORMAL LANDING WITHOUT FURTHER INCIDENT. AFTER LANDING THE F/O PINNED THE RIGHT MAIN GEAR. EMERG ENCY WAS CANCELED AND AIRCRAFT TAXIED TO GATE. MAINTENANCE WAS CONTRACTED TO TROUBLESHOOT PROBLEM. MAINTENANCE REPLACE D THE RIGHT S1-82 GEAR DOWN SWITCH WHICH WAS INOPERATIVE. IN ADDITION WIRE 6200J2Y WAS RE TERMINATED AT TERMINAL 5. TH E SYSTEM WAS THEN OPERATIONALLY CHECKED GOOD IAW DC9 MM. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001080200127 20010802 00127 NM 2001 8 2 DL767011056 1 20010619 A 5720 112T5086 FITTING BOEING 767 767232 1385132 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 104DA 22216 WHILE ACCOMPLISHING THE STRUT IMPROVEMENT PROGRAM MODIFICATION ON THE LT WING SUPPORT STRUCTURE, A CRACK INDICATION WAS FOUND IN THE O/B ROW 2ND HOLE FROM BOTTOM COMMON TO THE RIB NR 8 ENGINE SUPPORT FITTING, THE FRONT SPAR, AND THE FRONT S PAR WEB. ER/A 397658-14AD. 2 L 7 2 4F RT A1NM 2001080200128 20010802 00128 SO 2001 8 2 YAD2001F00002 2 20010601 A 8530 VALVE SUPAIRPART CESSNA 207 207A 2073604 CE CONT O520 IO520F 17032 SO CYLINDER ASY STUCK E YADA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 AL 03 75941 1353 52J9914661 20700656 247599R AIRCRAFT DEPARTED AIRPORT AND ENGINE BEGAN RUNNING VERY ROUGH, AIRCRAFT RETURNED TO THE AIRPORT (UNABLE TO MAINTAIN POWE R OR ALTITUDE). MAINTNEANCE FOUND NR 6 CYLINDER HAD BORKEN AND BENT PUSHRODS. FURTHER INVESTIGATION REVEALED A BENT PU SHROD IN NR 2 CYLINDER. SUSPECT STUCK/STICKING VALVES CAUSED FAILURE. ALL CYLINDERS WERE INSTALLED FACTORY NEW AT ENGI NE O/H ON 10/15/1999. 1 H 7 1 3O 3 O A16CE E5CE 2001080200129 20010802 00129 SO 2001 8 2 YAD2001F00003 2 20010601 A 8530 VALVE SUPAIRPART CESSNA 207 207A 2073604 CE CONT O520 IO520F 17032 SO NR 6, NR2 CYL STUCK E YADA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 AL 03 75941 1353 52J9914711 20700656 247599R AIRCRAFT DEPARTED AIRPORT AND ENGINE BEGAN RUNNING VERY ROUGH, AIRCRAFT RETURNED TO THE AIRPORT (UNABLE TO MAINTAIN POWE R OR ALTITUDE). MAINTENANCE FOUND NR 6 CYLINDER HAD BROKEN AND BENT PUSHRODS. FURTHER INVESTIGATION REVEALED A BENT PU SHROD IN NR 2 CYLINDER. SUSPECT STUCK/STICKING VALVES CAUSED FAILURE. ALL CYLINDERS WERE INSTALLED FACTORY NEW AT ENGI NE OVERHAUL ON 10/15/1999. 1 H 7 1 3O 3 O A16CE E5CE 2001080200130 20010802 00130 NM 2001 8 2 DL767011147 1 20010711 A 3350 767 LIGHT BOEING 767 767232 1385132 NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 111DN 22223 THE 2L EXTERIOR EMERGENCY LIGHT INOP. RELAMPED, CHECKS OK. 2 L 7 2 4F RT A1NM 2001080200131 20010802 00131 NM 2001 8 2 DL767011185 1 20010717 A 3350 BPS73 POWER SUPPLY BOEING 767 767232 1385132 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 111DN 22223 LEFT AFT CEILING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY. CHECKS GOOD. 2 L 7 2 4F RT A1NM 2001080200132 20010802 00132 SO 2001 8 2 YNT2001F00000 1 20010410 A 2433 9B4024A TRANSFORMER GULSTM G1159 G1159 3953505 SO TRANS RECTIFIER SHORTED E YNTA O OTHER O OTHER NR NOT REPORTED 1 SW 09 35GZ 1205 465 POSITIVE TERMINAL ON TRANSFORMER RECTIFIER WAS GLOWING RED WHEN INSTALLED WITH POWER APPLIED. THIS WAS FOUND DURING ROUT INE INSPECTION. THERE WAS NO INDICATION THAT THE AIRCRAFT WIRING HAD ANY EFFECT ON THIS MALFUNCTION. AIRCRAFT CIRCUIT BREAKER DID NOT TRIP. THE POSITIVE TERMINAL LUG ON RECTIFIER WAS VERY DISCOLORED LIKE THERE WAS TORCH APPLIED TO THE T ERMINAL. THE PLASTIC INSULATOR WAS ALSO DISCOLORED AND MELTED DUE TO EXTREME HEAT. I BELIEVE THAT THE UNIT ITSELF HAS THE DEFECT. POSSIBLE DIRECT SHORT TO GROUND CAUSING MALFUNCTION. THE ATTACHMENT LUG LEADING INSIDE BOX WAS NOTICED TO BE REPOSITIONED. UNIT IS GOING TO BE SENT TO A QUALIFIED REPAIR CENTER FOR BENCH CHECK. CAUSE: UNKNOWN AT THIS TIME. 2 L 7 2 4F RT A12EA 2001080200133 20010802 00133 EU 2001 8 2 Z4MR601462A 1 20010714 A 2820 RG9570R1 GASKET PILATS PC12 PC1245 EU RELIEF VALVE LEAKING B Z4MR K NONE K FLUID LOSS IN INSP/MAINT 1 WP 27 325MW 325 A RANDOM INSPECTION OF THE FUEL PUMP REVEALED FUEL LEAKING FROM THE ENGINE DRIVEN LOW PRESSURE FUEL PUMP RELIEF VALVE GA SKET. THIS PUMP INCORPORATES THE SAME (OR VERY SIMILAR) RELIEF VALVE AND GASKET ASSEMBLY USED ON ROTARY FUEL PUMP WHICH WAS THE SUBJECT OF THE AD DIRECTING COMPLIANCE WITH SB RELIEF VALVE COVER CAP SCREW RECURRING TORQUE CHECK. A TORQUE C HECK OF THE CAP SCREWS WAS ACCOMPLISHED IAW SB AND ALL WERE FOUND BELOW THE TORQUE SPECIFICATION. OTHER PUMPS INSPECTED WERE ALSO FOUND TO BE LEAKING AND UNDER TORQUE. 1 L 7 1 3T RT A78EU 2001080200134 20010802 00134 NM 2001 8 2 DL767011215 1 20010718 A 5311 148T31101 FRAME BOEING 767 767232 1385132 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 107DL 22219 DURING INSPECTION OF THE 1809 BULKHEAD PER S/B 767-53-0078 R.2, CRACKS WERE FOUND IN THE LT AND RT CHORDS REQUIRING PERM ANENT MODIFICATION (SPLICING IN NEW SECTION OF CHORD PER THE SERVICE BULLETIN). ER/A 397806-14AD. 2 L 7 2 4F RT A1NM 2001080200135 20010802 00135 NM 2001 8 2 DL76G010955 1 20010612 A 5610 141T480119 WINDSHIELD BOEING 767 767332 1382001 NM COCKPIT CRACKED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 1610D 119C4049 30594 CAPTS WINDSHIELD OUTER LAYER SHATTERED. REPLACED LT FWD WINDSHIELD AND WINDOW HEAT CONTROLLER PER M/M TORQUED PER ERA 3 88709-14. ALL CHECKS GOOD. 2 L 7 2 4F RT A1NM 2001080200136 20010802 00136 NM 2001 8 2 DL76G010971 1 20010611 A 5311 148T27409 FRAME BOEING 767 7673P6 1385105 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1501P 24983 INSPECTION OF THE FS 1809 BULKHEAD PER BAC SB 767-53-0078 AND AD 2001-09-13 REVEALED A CRACK IN THE LT OUTER CHORD. TH E CRACKED SECTION OF CHORD WAS CUT OFF AND A NEW SECTION SPLICE IN PER THE REQUIREMENTS OF THE S/B AND PER ER/A 381053- 14AD. 2 L 7 2 4F RT A1NM 2001080200137 20010802 00137 NM 2001 8 2 DL76G011021 1 20010620 A 2530 828450407M0DA OVEN BOEING 767 7673P6 1385105 NM GALLEY FAULTY A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 153DL 24985 AIR TURNBACK DUE TO SMOKE IN CABIN. FOUND OVEN IN MID GALLEY AT FAULT. REPLACED SAME. 2 L 7 2 4F RT A1NM 2001080200140 20010802 00140 NM 2001 8 2 DL76G011116 1 20010705 A 3010 2780537104 VALVE BOEING 767 767332 1382001 NM RT WING FAILED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 1607B 30388 T/O DISCONTINUED. RT WING ANTI-ICE VALVE ILLUMINATED, APPROX 100 KNOTS. REMOVED AND REPLACED WING TAI VALVE. OPS CKS OK. PERFORMED ENG RUN VALVE LIGHT REMAINED OFF. CK OK PER M/M. 2 L 7 2 4F RT A1NM 2001080200141 20010802 00141 EA 2001 8 2 COMA0160541 1 20010718 A 2162 01649801 SENSOR CNDAIR CL600 CL6002B19 EA MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 938CA 7046 DISPLAY COOL CAUTION MESSAGE.REPLACED THE LOW AIR FLOW SENSOR. 2 L 7 2 4F RT A21EA 2001080200142 20010802 00142 2001 8 2 DL76G011125 4 20010707 A 3460 4058650950 FMC BOEING 767 767332 1382001 NM COCKPIT MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 1604R 30180 DUAL FMC FAIL. LEG PAGES BLANK ON BOTH CALLS. UNABLE TO ENTER ANY FIX LEGS ON BOTH CDU'S. RESET C/BS. BITE HISTORY O N BOTH CDU'S SHOW NO FAULTS. NO FMC FAILURES / LIGHTS. AS PRECAUTION REMOVED BOTH CDU, CLEAN FILTERS INSPECT CONNECTOR S AND REINSTALL. CDU'S OPERATIONAL NORMAL. 2 L 7 2 4F RT A1NM 2001080200143 20010802 00143 NM 2001 8 2 DL76G011126 1 20010707 A 2910 272T1200176 HYDRAULIC LINE BOEING 767 767332 1382001 NM HYDRAULIC SYS SEPARATED A DALA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 27 1612T 30575 RT HYDRAULIC SYSTEM QUANTITY AND PRESSURE WENT TO ZERO DURING DESCENT AND APPROACH. ACCOMPANIED BY A SPOILERS EICAS MES SAGE. NO ABNORMAL CONTROL INPUTS WERE FELT. ACCOMPLISHED PROCEDURES PER POM. FOUND HYD PRESSURE LINE TO NR 7 SPOILER PCA SEPARATED FROM PCA. LINE FAILED AT SWAGE. REPLACED SAME. 2 L 7 2 4F RT A1NM 2001080200144 20010802 00144 NM 2001 8 2 DL76G011172 1 20010714 A 2121 FAN BOEING 767 767332 1382001 NM CABIN FAULTY A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 1605 30198 DIVERTED TO YQX DUE TO SMOKE IN CABIN. FOUND RT RECIRC FAN AT FAULT. FWD TO MCO PER MEL 21-25-01A. 2 L 7 2 4F RT A1NM 2001080200145 20010802 00145 NM 2001 8 2 DL76G011220 1 20010724 A 2150 6806404 A/C PACK BOEING 767 7673P6 1385105 NM A/C BAY MALFUNCTIONED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 155DL 25269 LEFT PACK PRODUCED EXCESSIVE ODOR. TURNED IT OFF. OPERATED LT PACK FOR 1 HR ON GROUND. NO ABNORMAL SMELL IN CABIN. C HECKED PACK INLET. FOUND OK. 2 L 7 2 4F RT A1NM 2001080200146 20010802 00146 2001 8 2 DL76G011221 4 20010724 A 3460 4058650931 CDU BOEING 767 767324 NM COCKPIT FAILED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 394DL 92011567 27394 CAPTS FMC CDU WENT BLANK. REPLACED CDU. FMS OPS CHECKS OK. 2 L 7 2 4F RT A1NM 2001080200147 20010802 00147 NM 2001 8 2 DL76K011158 1 20010712 A 3350 BPS7 BATTERY PACK BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 174DZ 29693 AFT LEFT EXTERIOR EMER LIGHTS INOP. REPLACED BATTERY PACK. 2 L 7 2 4F RT A1NM 2001080200148 20010802 00148 NM 2001 8 2 DL76K011167 1 20010713 A 5414 313T2100 FAIRING BOEING 767 767332 1382001 NM NR 2 ENGINE SEPARATED A DALA A UNSCHED LANDING D INFLIGHT SEPARATION CR CRUISE 1 SO 27 173DZ 29692 0 DURING FLT BALL CAP FAIRING DEPARTED A/C CAUSING DAMAGE TO THE NR 7/8 SLATS AND STRUCTURE UNDERNEATH FAIRING. INSPECTED AREA REPLACED UPPER RT FWD PYLON FAIRING AND REPAIRED DAMAGE ON NR CARDS 1-11. REPLACED 8 SLAT ON N/R CARD 10 A ROUTIN E JIC OPN 7008AD ON CARDS 1-2. ON, OFF A 271004046 30 825. 2 L 7 2 4F RT A1NM 2001080200151 20010802 00151 NE 2001 8 2 DL76L010968 2 20010607 A 7200 PW40603 BEARING BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 199DN 15776 28456 727753 FOUND METAL ON MCD. REINSPECTION SHOWED MORE FINES. ANALYSIS REVEALED BEARING MATERIAL. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 2001080200152 20010802 00152 NM 2001 8 2 DL76L011032 1 20010621 A 2421 755358 IDG BOEING 767 767332 1382001 NM LT ENGINE FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 193DN 28450 DIVERTED TO JFK DUE TO LT IDG FAILED AND GEN BREAKER TRIPPED. REPLACED LT IDG. 2 L 7 2 4F RT A1NM 2001080200153 20010802 00153 NM 2001 8 2 AWXA0002055 1 20010708 A 5714 BAC1505100257 ANGLE BOEING 737 737277 1384570 NM BS 674 BL45R CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 D: Cabin center wing box area lower attach angle cracked STA 674 RBL 45C: Repaired cabin center wing box area lower atta ch angle B.L 45R BS 674 IAW ER 155715-01200 OL3 2 L 7 2 4F RT A16WE 2001080200154 20010802 00154 NM 2001 8 2 AWXA0002057 1 20010714 A 5311 654541041 WEB BOEING 737 737277 1384570 NM BS 706-716 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 D: Floor beam web cracked 5 places BS 706-716 BL-0.C: Repaired floor beam web IAW AWA ER 15-5715-01193-SS2 2 L 7 2 4F RT A16WE 2001080200155 20010802 00155 NM 2001 8 2 AWXA0002058 1 20010716 A 5311 6545833U40 WEB BOEING 737 737277 1384570 NM BS 180 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 D: Cockpit floor web cracked, BS 180, RBL 22, WL 207 at edge of cut-outC: removed & replaced floor web at BS 180, RBL 22 , WL 207 IAW AWA ER 15-5311-01186-SS3 2 L 7 2 4F RT A16WE 2001080200156 20010802 00156 NM 2001 8 2 AWXA0002061 1 20010716 A 5312 6516300517 STRAP BOEING 737 737277 1384570 NM BS 178 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 D: BS 178 Bulkhead web fwd side, BL0 strap cracked, WL 184C: Fabricated Strap IAW boeing DWG # 65-16300 and installed st rap IAW B737 SRM 51-30-2 pg 2 at BS 178, WL 184, BL0 2 L 7 2 4F RT A16WE 2001080200157 20010802 00157 NM 2001 8 2 AWXA0002062 1 20010717 A 5313 6545833U40 WEB BOEING 737 737277 1384570 NM BS 180 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 D: Cockpit floor web cracked, BS 180, LBL 22, WL 207 at edge of cut-outC: Removed & replaced cockpit floor web IAW AWA E R #15-5311-01186-SS3 at BS 180, WL 207, LBL 22 2 L 7 2 4F RT A16WE 2001080200158 20010802 00158 NM 2001 8 2 AWXA0002064 1 20010629 A 5313 6546568 WEB BOEING 737 737277 1384570 NM BS 1016 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 D: Aft. pressure bulkhead web at the 8th and 9th fastener holes above S-7L, 2 ea cracks were noted on the S-8L and one a t S-9LC: Repaired Aft pressure bulkhead web at the 8th and 9th fastener holes above S-7L, S-8L and S-9L IAW AWA ER 15-53 83-1205-KB1 2 L 7 2 4F RT A16WE 2001080200159 20010802 00159 EU 2001 8 2 DHL2001363015 1 20010728 A 5400 NOSE COWL AIRBUS 300 A300B4203 3930306 EU CRACKED A DHLA O OTHER O OTHER IN INSP/MAINT 1 SO 01 363DH 85 On "A" check discrepancy--- #2 engine nose cowl lip cracked at 2 places, at the 8 0' clock position.1) Routed out cracke d areas 3 each places nose lip 8 o' clock position I.A.W. A300 S.R.M. 54-30-00 page 731/732 figure 719 view K.2) made do ubler repair from 2024-0 .071 lot# 8000N9vux P/O 8316399 and heat treated to 2024 T4 I.A.W. avborne Process Specs. 98PMS I .247PS-01.3) Prep treat and primed areas I.A.W. A-300 S.R.M. 54-30-00.4) Installed doublers repair on cracked areas I. A.W. A300 S.R.M. 54-30-00 page 731 and sealed all edges.5) Cleaned area for F.O.D. 2 L 7 2 4F RT A35EU 2001080200160 20010802 00160 EA 2001 8 2 COMA0160542 1 20010725 A 5346 60135006 WEB CNDAIR CL600 CL6002B19 EA CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 933CA 16892 7040 WHILE PERFORMING REPAIR TO THE ENGINE SUPPORT BEAM PER REO 53-61-345 A CRACK WAS NOTED ON THE UNDER LAYING EXTRUDED ANGL E P/N 601-35006-7 CRACK APPROX 5/16".THE CRACK WAS REPAIRED I/A/W CANADAIR REO 601R-53-61-394. 2 L 7 2 4F RT A21EA 2001080200161 20010802 00161 EA 2001 8 2 COMA0160543 1 20010725 A 5346 60135006 WEB CNDAIR CL600 CL6002B19 EA CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 933CA 16892 7040 CRACK ON ENGINE SUPPORT BEAM UPPER SKIN.REPAIRED I/A/W REO 601R-53-61-345. 2 L 7 2 4F RT A21EA 2001080200162 20010802 00162 NM 2001 8 2 DL76L011045 1 20010622 A 3610 77328810 SHUTOFF VALVE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE FAILED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 191DN 28448 727717 ON TAKEOFF DUCT PRESS FLUCTUATED PLUS MINUS 15 PSI. REPLACED PRSOV PER MM. CKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2001080200163 20010802 00163 NM 2001 8 2 DL76L011239 1 20010726 A 2530 811150417 COFFEEMAKER BOEING 767 767332 1382001 NM GALLEY DIRTY A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 174DN 24802 FLT DIVERTED TO BOS WITH BURNING SMELL IN AFT GALLEY. REMOVED ALL AFT COFFEEMAKERS AND CLEANED AREA OF COFFEE RESIDUE. INSPECTED AFT GALLEY FOR OTHER SOURCE OF SMELL. NONE FOUND. REPLACED NR 1 AND NR 3 COFFEEMAKERS PRECAUTIONARY. 2 L 7 2 4F RT A1NM 2001080200164 20010802 00164 NE 2001 8 2 DL76L011240 2 20010725 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 MALFUNCTIONED A DALA K NONE O OTHER AP APPROACH 1 SO 27 183DN 29249 27110 724686 HEARD A THUMP ON RIGHT SIDE DURING APPROACH. PASSENGER ON RIGHT SIDE SAW A FLASH OF LIGHT AT THE SAME TIME. NO ABNORMA L ENGINE INDICATIONS, BUT SUSPECT SMALL COMPRESSOR STALL. REMOVED AND REPLACED RIGHT ENGINE PER ROUTINE CARD DECK 1-27 . 2 L 7 2 4F 4 F RT A1NM E24NE 2001080200165 20010802 00165 NM 2001 8 2 DL76S010929 1 20010514 A 5330 SKIN BOEING 767 767332 1382001 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 SKIN DAMAGE AT STA 368 AND STRINGER 33R. ER/A 397613-14. 2 L 7 2 4F RT A1NM 2001080200166 20010802 00166 NM 2001 8 2 DL76S010934 1 20010608 A 2612 GASKET BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE THERMOCOUPLE LEAKING A DALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 27 135DL 41045 3178 25145 580113 LT ENG FIRE INDICATIONS SHORTLY AFTER TAKEOFF THROTTLE. RETARDED TO IDLE AND FIRE INDICATION WENT OUT. FOUND ALL THERM OCOUPLE GASKETS LEAKING. REPLACED GASKETS, CK OK ON RUN. 2 L 7 2 4F 4 F RT A1NM E13NE 2001080200167 20010802 00167 NM 2001 8 2 SCAN01330 1 20010614 A 3520 106051312 MANIFOLD BOEING 727 7272J4 1384006 NM CABIN LEAKING A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 285SC 21676 DURING HEAVY MAINTENANCE INSPECTION THE OXYGEN MANIFOLD FAILS LEAK CHECK AT PSU 24RH. REPLACED MANIFOLD IAW B727 MM 352 131, LEAK CHECK AND OPS CHECK GOOD IAW B727 MM 352100. 2 L 7 3 4F RT A3WE 2001080200168 20010802 00168 NM 2001 8 2 SCNA01037 1 20010602 A 3350 POWER SUPPLY BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 211DB 20766 DURING A MAINTENANCE LINE CHECK THE EMERGENCY LIGHTS ABOVE THE RIGHT OVERWING EXIT DOORS WERE FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY FOR THE EMERGENCY LIGHTS OVER THE RIGHT OVERWING EXIT DOORS. 2 L 7 3 4F RT A3WE 2001080200169 20010802 00169 NM 2001 8 2 SCNA01038 1 20010526 A 3350 LIGHT BOEING 727 727282 138408T NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 281SC 21949 DURING A MAINTENANCE LINE INSPECTION THE EMERGENCY EXIT LIGHT ABOVE 1L WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY AT 1L. 2 L 7 3 4F RT A3WE 2001080200170 20010802 00170 NM 2001 8 2 SCNA01039 1 20010531 A 2612 FIRE LOOP BOEING 727 727259 138408J NM NR 2 ENGINE CHAFED A SCNA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 289SC 20765 DURING CLIMBOUT FROM MKE ENGINE NUMBER 2 HAD FIRE INDICATIONS, COMPLIED WITH COM, AND RETURNED TO MKE. THE FIRE DETECTI ON LOOP ON THE BOTTOM OF THE ENGINE WAS FOUND TO BE CHAFING. REPOSITIONED LOOP AND CLAMP. CORRECTED SEVERAL SMALL AIR LEAKS. 2 L 7 3 4F A3WE 2001080200171 20010802 00171 NM 2001 8 2 SCNA01040 1 20010603 A 7722 JG298A5 INDICATOR BOEING 727 7272J4 1384006 NM COCKPIT DEFECTIVE A SCNA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 15 290SC 20764 DURING TAKEOFF ROLL AT 80 KTS IN MBJ, THE NUMBER THREE EPR WOULD NOT GO BEYOND 1.5. ABORTED THE TAKEOFF. REMOVED AND R EPLACED THE NUMBER THREE EPR INDICATOR. 2 L 7 3 4F RT A3WE 2001080200173 20010802 00173 NM 2001 8 2 SCNA01041 1 20010519 A 3350 6013 BATTERY PACK BOEING 727 7272M7 138407S NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 294SC 21202 DURING A MAINTENANCE LINE CHECK THE MID CABIN EMERGENCY FLOOR TRACK LIGHTING WAS FOUND INOPERATIVE. REMOVED AND REPLACE D THE POWER SUPPLY AND THE BATTERY PACK. 2 L 7 3 4F A3WE 2001080200174 20010802 00174 EA 2001 8 2 COMA0160546 1 20010730 A 3397 59465 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 940CA 7048 EMERGENCY FLOOR PATH LIGHTING INOPERATIVE FROM ROW 10 AFT. REPLACED CONNECTOR WIRE. 2 L 7 2 4F RT A21EA 2001080200175 20010802 00175 EA 2001 8 2 COMA0160548 1 20010731 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA MALFUNCTIONED A COMA O OTHER O OTHER AP APPROACH 1 SO 01 981CA 7810 3342 7163 FLAPS FAILED AT 20 DEGREES.REPLACED THE RIGHT HAND BPSU. 2 L 7 2 4F RT A21EA 2001080200176 20010802 00176 EA 2001 8 2 COMA0160549 1 20010731 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA MALFUNCTIONED A COMA O OTHER O OTHER AP APPROACH 1 SO 01 938CA 14905 7046 FLAPS FAILED AT 41 DEGREES.REPLACED THE RIGHT HAND BPSU. 2 L 7 2 4F RT A21EA 2001080200177 20010802 00177 EA 2001 8 2 COMA0160550 1 20010731 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA MALFUNCTIONED A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 932CA 9863 5069 7038 FLAPS FIALED AT 20 DEGREES.REPLACED THE RIGHT HAND BPSU. 2 L 7 2 4F RT A21EA 2001080200178 20010802 00178 NM 2001 8 2 SCNA01042 1 20010529 A 3350 BATTERY BOEING 727 727224 1384076 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 296SC 22449 DURING A MAINTENANCE LINE CHECK THE AFT ENTRY EMERGENCY LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED TWO BATTERIES . 2 L 7 3 4F A3WE 2001080200179 20010802 00179 NM 2001 8 2 SCNA01043 1 20010606 A 2120 DUCT BOEING 727 727227 1384078 NM A/C BAY CONTAMINATED A SCNA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 275AF 22092 DURING TAXI OUT FROM THE GATE, HYDRAULIC FLUID HAZE WAS DETECTED IN THE AFT CABIN. FOUND AND REMOVED HYDRAULIC RESIDUE FROM DUCTING IN AFT STAIRWELL. ALSO, FOUND AND REMOVED DEBRIS FROM DUCTS. 2 L 7 3 4F A3WE 2001080200180 20010802 00180 2001 8 2 SCNA01044 4 20010612 A 3415 SWITCH BOEING 727 727282 138408T NM T/O WARNING SYS FAULTY A SCNA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 15 281SC 21949 DURING TAKEOFF ROLL, WHEN THE POWER WAS ADVANCED THE TAKEOFF WARNING HORN SOUNDED. ABORTED TAKEOFF, VERIFIED SPEED BRAK ES STOWED, FLAPS 15 DEGREES, TRIM 6.7 AUTOPACK NORMAL. REMOVED AND REPLACED UPPER TAKEOFF WARNING SWITCH (STABILIZERS). 2 L 7 3 4F RT A3WE 2001080200181 20010802 00181 NM 2001 8 2 SCNA01320 1 20010526 A 5315 FLOORBEAM BOEING 727 7272J4 1384006 NM FUSELAGE CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 285SC 21676 DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMIT MAIN CABIN FLOOR STRUCTURE AT STATION 344 RBL 19, F LOORBEAM. 2 L 7 3 4F RT A3WE 2001080200183 20010802 00183 NM 2001 8 2 SCNA01321 1 20010527 A 5315 FLOORBEAM BOEING 727 7272J4 1384006 NM FUSELAGE CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 285SC 21676 DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON FLOORBEAM AT STA 1070, LBL 58. 2 L 7 3 4F RT A3WE 2001080200185 20010802 00185 NM 2001 8 2 SCNA01322 1 20010528 A 5315 FLOORBEAM BOEING 727 7272J4 1384006 NM FUSELAGE CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 285SC 21676 DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON THE UPPER FLANGE OF THE FLOORBEAM AT BS 1130, R BL 28 TO RBL 36. 2 L 7 3 4F RT A3WE 2001080200186 20010802 00186 NM 2001 8 2 SCNA01323 1 20010526 A 5347 SEAT TRACK BOEING 727 7272J4 1384006 NM FUSELAGE CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 285SC 21676 DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON THE SEAT TRACK AT STA 380 TO 420 RBL 24. 2 L 7 3 4F RT A3WE 2001080200188 20010802 00188 NM 2001 8 2 SCNA01324 1 20010615 A 3520 225047 CONTROL UNIT BOEING 727 7272J4 1384006 NM CABIN FAILED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 285SC 21676 DURING HEAVY MAINTENANCE INSPECTION THE ELECTRO PNEUMATIC FLOW CONTROL UNIT FAILS AUTOMATIC DROP TEST. REMOVED AND REPL ACED FLOW CONTROL UNIT IAW B727 MM 352111. OPS CHECK NORMAL IAW B727 MM 352100. 2 L 7 3 4F RT A3WE 2001080200190 20010802 00190 NM 2001 8 2 SCNA01325 1 20010614 A 3520 11501302 MANIFOLD BOEING 727 7272J4 1384006 NM CABIN LEAKING A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 285SC 21676 DURING HEAVY MAINTENANCE INSPECTION THE OXYGEN MANIFOLD AT PSU 4L FAILS LEAK CHECK. REPLACED PSU OXYGEN MANIFOLD PER B7 27 MM 252131. LEAK CHECK AND OPS CHECK GOOD IAW B727 MM 352100. 2 L 7 3 4F RT A3WE 2001080200191 20010802 00191 NM 2001 8 2 SCNA01326 1 20010614 A 3520 106051312 MANIFOLD BOEING 727 7272J4 1384006 NM CABIN LEAKING A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 285SC 21676 DURING HEAVY MAINTENANCE INSPECTION THE OXYGEN MANIFOLD AT PSU 16R FAILS LEAK CHECK. REPLACED PSU OXYGEN MANIFOLD PER B7 27 MM 352131. LEAK CHECK AND OPS CHECK GOOD IAW B727 MM 352100. 2 L 7 3 4F RT A3WE 2001080200192 20010802 00192 NM 2001 8 2 SCNA01327 1 20010614 A 3520 10605131 MANIFOLD BOEING 727 7272J4 1384006 NM CABIN LEAKING A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 285SC 21676 DURING HEAVY MAINTENANCE INSPECTION THE OXYGEN MANIFOLD AT PSU 24R FAILS LEAK CK. REPLACED PSU OXYGEN MANIFOLD PER B727 MM 352131. LEAK CHECK AND OPS CHECK GOOD IAW B727 MM 352100. 2 L 7 3 4F RT A3WE 2001080200193 20010802 00193 NM 2001 8 2 SCNA01328 1 20010614 A 3520 106051312 MANIFOLD BOEING 727 7272J4 1384006 NM CABIN LEAKING A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 285SC 21676 DURING HEAVY MAINTENANCE INSPECTION THE OXYGEN MANIFOLD AT PSU 18RH FAILS LEAK CHECK. REPLACED PSU OXYGEN MANIFOLD PER B727 MM 352131. LEAK CHECK AND OPS CHECK GOOD IAW B727 MM 352100. 2 L 7 3 4F RT A3WE 2001080200195 20010802 00195 NM 2001 8 2 SCNA01329 1 20010614 A 3520 106051312 MANIFOLD BOEING 727 7272J4 1384006 NM CABIN LEAKING A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 285SC 21676 DURING HEAVY MAINTENANCE INSPECTION THE OXYGEN MANIFOLD FAILS LEAK CHECK AT PSU 20 LT. REPLACED MANIFOLD IAW B727 MM 35 2131. LEAK CHECK AND OPS CHECK GOOD IAW B727 MM 352100. 2 L 7 3 4F RT A3WE 2001080200197 20010802 00197 NM 2001 8 2 SCNA01331 1 20010527 A 5347 SEAT TRACK BOEING 727 7272J4 1384006 NM FUSELAGE CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 285SC 21676 DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON THE SEAT TRACK AT STA 1070 TO 1135 LBL 22. 2 L 7 3 4F RT A3WE 2001080200199 20010802 00199 NM 2001 8 2 SCNA01332 1 20010529 A 5347 SEAT TRACK BOEING 727 7272J4 1384006 NM FUSELAGE CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 285SC 21676 DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON SEAT TRACK AT STA 420 RBL 45. 2 L 7 3 4F RT A3WE 2001080200200 20010802 00200 NM 2001 8 2 SCNA01333 1 20010526 A 5347 SEAT TRACK BOEING 727 7272J4 1384006 NM FUSELAGE CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 285SC 21676 DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON SEAT TRACK AT STA 344 - 380 RBL 24. 2 L 7 3 4F RT A3WE 2001080200201 20010802 00201 NM 2001 8 2 SCNA01334 1 20010526 A 5347 SEAT TRACK BOEING 727 7272J4 1384006 NM FUSELAGE CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 285SC 21676 DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON SEAT TRACK STA 420 - 440 RBL 24. 2 L 7 3 4F RT A3WE 2001080200203 20010802 00203 NM 2001 8 2 SCNA01335 1 20010614 A 3520 106051311 MANIFOLD BOEING 727 7272J4 1384006 NM CABIN LEAKING A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 285SC 21676 DURING HEAVY MAINTENANCE INSPECTION THE OXYGEN MANIFOLD AT PSU 3L FAILS LEAK CHECK. REPLACED MANIFOLD IAW B727 MM 35213 1. OPS AND LEAK CHECK NORMAL IAW B727 MM 352100. 2 L 7 3 4F RT A3WE 2001080200205 20010802 00205 NM 2001 8 2 SCNA01336 1 20010528 A 3211 658595221 BEAM BOEING 727 7272J4 1384006 NM LT MLG CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 285SC 21676 DURING HEAVY MAINTENANCE CHECK CORROSION WAS FOUND OUT OF LIMITS ON THE LEFT HAND MAIN LANDING GEAR SUPPORT BEAM. THE C ORROSION WAS AT THE SITE OF THE HOLE FOR THE GEAR ACTUATOR SUPPORT PIN BUSHING. THE CORROSION WAS AT THE UPPER FORWARD END OF THE HOLE, EXTENDING APPROXIMATELY 0.14 INCH RADIALLY, AND APPROXIMATELY 0.80 INCH AFT INTO THE GEAR BEAM. 2 L 7 3 4F RT A3WE 2001080200207 20010802 00207 NM 2001 8 2 SCNA01337 1 20010628 A 3350 10617891007 SIGN BOEING 727 7272J4 1384006 NM CABIN FAILED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE INSPECTION THE RT AFT OVERWING EXIT DOOR EMERGENCY SIGN FAILED LUMINOUS CHECK. REMOVED AND REP LACED EMERGENCY EXIT SIGN IAW B727 MM 335031. 2 L 7 3 4F RT A3WE 2001080200209 20010802 00209 NM 2001 8 2 SCNA01338 1 20010703 A 3350 1000677 LIGHT BOEING 727 7272J4 1384006 NM R1 DOOR INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE INSPECTION THE EMERGENCY EXIT LIGHT ABOVE THE R1 DOOR WAS FOUND INOPERATIVE. REMOVED AND REPLA CED LIGHT ASSEMBLY IAW B727 MM 3350101. OPS CHECK NORMAL IAW B727 MM 3350001. 2 L 7 3 4F RT A3WE 2001080200211 20010802 00211 NM 2001 8 2 SCNA01339 1 20010703 A 3350 LIGHT BOEING 727 7272J4 1384006 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE INSPECTION THE EMERGENCY LIGHT AFT OF L1 DOOR WAS FOUND INOPERATIVE. RELAMPED LIGHT IAW B727 M M 335041 AND TESTED GOOD IAW B727 MM 335001. 2 L 7 3 4F RT A3WE 2001080200212 20010802 00212 NM 2001 8 2 SCNA01340 1 20010628 A 3350 616053053 SIGN BOEING 727 7272J4 1384006 NM CABIN FAILED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE INSPECTION THE RT FWD OVERWING EXIT DOOR EMERGENCY AND PULL SIGNS FAILED LUMINOSITY INSPECTION. REMOVED AND REPLACED SIGNS IAW B727 MM 335041. 2 L 7 3 4F RT A3WE 2001080200214 20010802 00214 NM 2001 8 2 SCNA01701 1 20010719 A 2611 SMOKE DETECTOR BOEING 727 7272J4 1384006 NM LAVATORY MALFUNCTIONED A SCNA K NONE N FALSE WARNING IN INSP/MAINT 1 GL 15 290SC 20764 SMOKE DETECTOR IN RIGHT AFT LAVATORY BEEPS CONTINUALLY. REMOVED AND REPLACED SMOKE DETECTOR. 2 L 7 3 4F RT A3WE 2001080200215 20010802 00215 NM 2001 8 2 SCNA01702 1 20010728 A 3350 BATTERY BOEING 727 7272K3 138400D NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 291SC 22770 AFT AIRSTAIR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED AFT AIRSTAIR EMERGENCY LIGHT BATTERIES. OPS GOOD. 2 L 7 3 4F RT A3WE 2001080200216 20010802 00216 NM 2001 8 2 SCNA01703 1 20010724 A 3241 CONTROL UNIT BOEING 727 7272M7 138407S NM ANTISKID SYS MALFUNCTIONED A SCNA K NONE O OTHER TX TAXI/GRND HDL 1 GL 15 294SC 22449 AT SLOW SPEEDS, LESS THAN 20 KIAS THERE IS VIRTUALLY NO BRAKING ACTION WITH THE ANTI SKID ON, BUT OK WITH IT OFF. REMOV ED AND REPLACED ANTI-SKID CONTROL UNIT. 2 L 7 3 4F A3WE 2001080200217 20010802 00217 2001 8 2 SCNA01704 4 20010727 A 3436 WARNING SYSTEM BOEING 727 727224 1384076 NM COCKPIT FALSE ACTIVATION A SCNA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 15 296SC 22449 FALSE WINDSHEAR WARNING AT 500 FT AGL, GO-AROUND WINDSHEAR AHEAD. NO FAULTS NOTED. 2 L 7 3 4F A3WE 2001080200218 20010802 00218 NM 2001 8 2 SCNA01705 1 20010721 A 2612 FIRE WARNING BOEING 727 727225 1384077 NM COCKPIT MALFUNCTIONED A SCNA K NONE N FALSE WARNING UK UNKNOWN 1 GL 15 282SC 22558 CARGO FIRE B-LOOP FAIL LIGHTS REMAIN ILLUMINATED. PERFORMED TEST AND FOUND NORMAL. 2 L 7 3 4F A3WE 2001080200219 20010802 00219 NM 2001 8 2 SCNA01706 1 20010726 A 2612 WARNING SYSTEM BOEING 727 727282 138408T NM COCKPIT FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 281SC 21949 APU FIRE BELL DID NOT SOUND DURING TEST. REMOVED AND REPLACED WARNING BOX, OPS GOOD. 2 L 7 3 4F RT A3WE 2001080200220 20010802 00220 NM 2001 8 2 SWAA011948 1 20010709 A 5513 BACB28AK04 BUSHING BOEING 737 7377H4 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 726SW 27858 DURING SCHEDULED SERVICE CHECK SWA SI 11075-55, FOUND LT ELEVATOR TAB HINGE BUSHINGS WORN AT HINGE'S NR 2, 3 & 4. REMOV ED AND REPLACED HINGE BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2001080200221 20010802 00221 NM 2001 8 2 SWAA011949 1 20010709 A 3350 300432 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 633SW 27936 DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY LIGHT AT LT OVERWING EXTERIOR INOP. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001080200222 20010802 00222 NM 2001 8 2 SWAA011950 1 20010709 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 633SW 27936 DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY EXIT LIGHT AT OVERWING CENTER CABIN INOP. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001080200223 20010802 00223 NM 2001 8 2 SWAA011951 1 20010709 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 633SW 27936 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001080200224 20010802 00224 NM 2001 8 2 SWAA011952 1 20010710 A 2560 P2070001 BATTERY BOEING 737 7372H4 138448C NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 089SW 22904 EMERGENCY FLASHLIGHTS AT AFT CABIN INOP. REMOVED AND REPLACED FLASHLIGHT BATTERIES PER MM. 2 L 7 2 4F A16WE 2001080200225 20010802 00225 NM 2001 8 2 SWAA011953 1 20010709 A 3350 101074 SIGN BOEING 737 7373A4 1384585 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED 1/4D CHECK, FOUND OVERWING EMERGENCY EXIT SIGN LOOSE AT LT CABIN INTERIOR. SECURED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2001080200226 20010802 00226 NM 2001 8 2 SWAA011954 1 20010710 A 3350 65C27095 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED RON CHECK, FOUND CABIN EMERGENCY EXIT LIGHTS INOP. RECHARGED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2001080200227 20010802 00227 2001 8 2 SWAA011955 4 20010709 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED EMERGENCY EVAC SLI DE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001080200228 20010802 00228 NM 2001 8 2 SWAA011956 1 20010710 A 3350 65C34691 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED C2 CHECK, FOUND OVERHEAD BULL NOSE EMERGENCY LIGHT LENS LOOSE AT ROWS 16 DEF & 18 DEF. SECURED BULL NO SE LENS PER MM. 2 L 7 2 4F RT A16WE 2001080200230 20010802 00230 2001 8 2 SWAA011957 4 20010710 A 2565 65C19901 WIRE ROPE BOEING 737 7373A4 1384585 NM EVAC SLIDE FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE FRAYED AND MISROUTED. REMOVED AND REPLACED EVAC SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2001080200232 20010802 00232 2001 8 2 SWAA011958 4 20010709 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001080200233 20010802 00233 NM 2001 8 2 SWAA011961 1 20010710 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 307SW 22947 OVERHEAD BULL NOSE EXIT LIGHT INOP AT ROW 1 & 2 DEF. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2001080200234 20010802 00234 NE 2001 8 2 HNAA0100043 2 20010801 A 7200 310450001 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE SMOKE A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 982HA 29056 5789 380 120709 CREW REPORTED SMOKE/MIST FORMED IN THE CABIN AND COCKPIT. WHEN ENGINE BLEEDS WERE TURNED OFF SMOKE DISSIPATED. REPLACED #1 ENGINE. 2 H 7 2 4T 4 T RT A13NM E20NE 2001080200235 20010802 00235 NM 2001 8 2 SWAA011962 1 20010710 A 3350 BR2013 LIGHT BOEING 737 7372T4 1384492 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 EEPLS LIGHT MISSING AND WIRES NOT SECURE AT ROW NR 3. INSTALLED EEPLS LIGHT AND SECURED WIRES PER MM. 2 L 7 2 4F A16WE 2001080200237 20010802 00237 NM 2001 8 2 SWAA011968 1 20010706 A 3350 300432 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 633SW 27936 DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY LIGHT INOP AT FWD ENTRY. REMOVED AND REPLACED EMERGENCY LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001080200238 20010802 00238 2001 8 2 SWAA011972 4 20010711 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001080200240 20010802 00240 2001 8 2 SWAA011973 4 20010711 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED A1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER M M. 2 L 7 2 4F A16WE 2001080200241 20010802 00241 EA 2001 8 2 HNAA0100044 1 20010731 A 3232 82970014009 ACTUATOR DHAV DHC8 DHC8311 1386006 EA LEAKING A HNAA K NONE K FLUID LOSS CR CRUISE 1 EA 07 326EN 16349 234 AIRCRAFT LOST MOST OF #2 HYDRAULIC SYSTEM FLUID. FOUND #2 MAIN LANDING GEAR DOORS AFT ACTUATOR LEAKING. REPLACED ACTUATO R. 2 H 7 2 4T RT A13NM 2001080200243 20010802 00243 2001 8 2 SWAA011983 4 20010711 A 2565 22D22901157 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001080200247 20010802 00247 NM 2001 8 2 SWAA011984 1 20010711 A 3610 32145525 SHUTOFF VALVE BOEING 737 7373Y0 1384671 NM NR 2 ENGINE FAILED A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 682SW 23496 DECLARED EMERGENCY AFTER APPROX 20 MIN AT FL 350, CABIN WARNING HORN SOUNDED, CABIN ALTITUDE WAS AT 11,000 FT AND CLIMBI NG. INITIATED DESCENT. CABIN ALTITUDE CONTINUED TO CLIMB TO APPROX 20,000 FT. PASSENGER OXYGEN MASKS DEPLOYED. ON DE SCENT NOTICED RIGHT PACK DUCT SHOWING ZERO PRESSURE. AIRCRAFT WAS UNABLE TO HOLD CABIN PRESSURE ON ONE PACK. NO ASSOCI ATED BLEED OR PACK LIGHTS. F/A FWD ENTRY DOOR HAD LOUD PRESSURIZATION SQUEAL DURING DESCENT. FOUND NR 2 ENG PRSOV INOP . DEFERRED PER MEL & MX FERRY TO PHX FOR REPAIR. AT PHX REMOVED AND REPLACED NR 2 ENG PRSOV & 2 EA PNEU BLEED LINES, R EMOVED AND REPLACED OUTFLOW VALVE AND RESEATED FWD ENTRY DOOR PRESS. SEAL PER MM OPS 2 L 7 2 4F RT A16WE 2001080200249 20010802 00249 NM 2001 8 2 SWAA011985 1 20010709 A 2730 6963523 BEARING BOEING 737 7373Q8 1384670 NM ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D-CHECK, FOUND RT ELEVATOR PUSH ROD ATTACH BEARING WORN. REMOVED AND REPLACED BEARING AND SLEEVE PER M M. 2 L 7 2 4F RT A16WE 2001080200251 20010802 00251 NM 2001 8 2 SWAA011989 1 20010712 A 3350 65C34691 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 645SW 28330 DURING SCHEDULED C1 CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 23. REMOVED AND REPLAC ED EXIT LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001080200252 20010802 00252 NM 2001 8 2 SWAA011992 1 20010712 A 3350 6104789 BATTERY PACK BOEING 737 7372K6 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED RON CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT LT FWD EXTERIOR. REMOVED AND REPLACED BATTERY PACK PER M M. 2 L 7 2 4F RT A16WE 2001080200254 20010802 00254 2001 8 2 SWAA011993 4 20010714 A 2565 1061323 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED RON CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EME RGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001080200255 20010802 00255 2001 8 2 SWAA011994 4 20010714 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 063SW 22061 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001080200257 20010802 00257 NM 2001 8 2 SWAA011995 1 20010713 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 388SW 26591 EEPLS LOOSE AT MID CABIN. REMOVED AND REPLACED EEPLS LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001080200258 20010802 00258 NM 2001 8 2 SWAA011996 1 20010712 A 3350 900835A BATTERY PACK BOEING 737 7372K6 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP FWD CABIN. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2001080200260 20010802 00260 NM 2001 8 2 SWAA011998 1 20010715 A 2750 65C27503 TRANSMISSION BOEING 737 7373H4 1384600 NM T/E FLAP INOPERATIVE A SWAA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 07 613SW 27931 DURING APPROACH FLAPS WOULD NOT PASS 2.1 POSITION. FOUND NR 3 T/E FLAP TRANSMISSION INOP ALONG WITH DAMAGE TO AFT LT WI NG BODY FAIRING, NR 4 FLAP TRACK ATTACH CASTING, INBOARD MID FLAP FAIRING. REMOVED AND REPLACED NR 3 FLAP TRANSMISSION, NR 4 FLAP TRACK ATTACH CASTING. REPAIRED LT WING BODY FAIRING PER SWA RA AND REMOVED INBOARD MID FLAP FAIRING PER CDL, MX FERRY TO DAL FOR REPAIRS. 2 L 7 2 4F RT A16WE 2001080200263 20010802 00263 NM 2001 8 2 SWAA012001 1 20010716 A 3350 BR2013 TRACK BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 656SW 28401 EEPLS TRACK LOOSE. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001080200265 20010802 00265 2001 8 2 SWAA012003 4 20010715 A 2565 D31591 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 606SW 27926 DURING SCHEDULED A2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC S LIDE PER MM. 2 L 7 2 4F RT A16WE 2001080200276 20010802 00276 2001 8 2 SWAA012005 4 20010715 A 2565 D31354 SLIDE BOEING 737 7372T4 1384492 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001080200277 20010802 00277 NM 2001 8 2 SWAA012006 1 20010716 A 3350 300432 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 361SW 26572 DURING SCHEDULED SERVICE CHECK, FOUND RT FWD EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001080200278 20010802 00278 NM 2001 8 2 SWAA012007 1 20010716 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 361SW 26572 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT AFT CABIN. RELAMPED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001080200279 20010802 00279 NM 2001 8 2 SWAA012010 1 20010716 A 5753 6546435 SKIN BOEING 737 7373A4 1384585 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING WALK AROUND INSPECTION FOUND RT OUTBOARD AFT FLAP DELAMINATED 8 INCH DIAMETER ON UPPER AND LOWER SURFACE. REMOVE D AND REPLACED RT OUTBOARD AFT FLAP ASSY PER MM. 2 L 7 2 4F RT A16WE 2001080200280 20010802 00280 NM 2001 8 2 SWAA012011 1 20010715 A 5510 185A410132 HINGE BRACKET BOEING 737 7377H4 NM HORIZ STAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 708SW 27842 DURING SCHEDULED SERVICE CHECK, FOUND BOTH HORIZ STAB NR 4 HINGE PLATE BEARINGS WORN. REMOVED AND REPLACED HORIZ STAB H INGE PLATES PER SWA RA. 2 L 7 2 4F RT A16WE 2001080200281 20010802 00281 NM 2001 8 2 SWAA012012 1 20010717 A 3350 BR2013 TRACK BOEING 737 7373T5 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK LOOSE AT ROW 8. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001080200282 20010802 00282 NM 2001 8 2 SWAA012014 1 20010716 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 394SW 27380 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT ROWS 12 & 13. RECONNECTED WIRE PER MM. 2 L 7 2 4F RT A16WE 2001080200283 20010802 00283 NM 2001 8 2 SWAA012022 1 20010716 A 2752 MS9391130ZE MOTOR BOEING 737 7372H4 138448C NM T/E FLAP LEAKING A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 086SW 22827 (AIR TURNBACK) AFTER GEAR RETRACTION AT 400 FT BOTH A-HYD PUMP LOW PRESS LIGHTS ILLUMINATED, HYD SYSTEM QTY INDICATED 0. FOUND T/E FLAP HYD MOTOR LEAKING. REMOVED AND REPLACED FLAP MOTOR AND CASE FILTERS PER MM. 2 L 7 2 4F A16WE 2001080200284 20010802 00284 WP 2001 8 2 ARWAA0010719 1 20010724 A 3230 4771392501 PIN DOUG DC8 DC863F 302198F WP LT MLG BROKEN A ARWA O OTHER J WARNING INDICATION CL CLIMB 1 SO 19 661AV 1007 45969 ON DEPART FROM (SYCJ) LG WAS RETRACTED AND BOTH GEAR AND DOOR UNSAFE LTS ILLUMINATED. ABNORMAL PROCEDURES FOLLOWED. ON G EAR EXTENSION, A LOUD NOISE WAS HEARD FOLLOWED BY THREE GREEN LIGHTS. PROCEEDED TO DESTINATION ((SMJP) WITH GEAR SELECTE D DOWN. ON POST FLIGHT FOUND RETRACT CYL ON LT MLG. DETACHED FROM UPPER MAIN STRUT CYLINDER. BOSS IS MISSING ON GEAR C YL, AND RETRACT CYL IS HANGING FROM UPPER SWIVEL.INSPECTION OF LT MAIN LANDING GEAR AREA FOUND BROKEN GEAR ACTUATOR RETR ACT PIN. REMOVED DAMAGE PIN AND INSTALLED NEW PIN. ALL WORK ACCOMPLISHED IAW MFG RECOMMENDATIONS. WHILE ON JACKS, COM PLETED GEAR FUNCTIONAL TEST OF GEAR AND INDICATIONS SYSTEMS. 2 L 7 4 4F 4A25 2001080200285 20010802 00285 NM 2001 8 2 SWAA012023 1 20010717 A 3244 2607825 TIRE BOEING 737 7375H4 138449D NM NLG DAMAGED A SWAA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 SW 07 508SW 24185 (ABORTED TAKEOFF) SEVERE VIBRATION FELT AT NOSE WHEELS. FOUND TREAD LOSS AT NR 2 NLG TIRE, CAUSING DAMAGE TO THE NLG B Y-PASS VALVE, AFT E&E DOOR AND RT MLG DOOR OPEN/CLOSE ROD ASSY. REMOVED AND REPLACED BOTH NLG TIRE AND WHEEL ASSY'S. R EMOVED AND REPLACED NLG BY-PASS VALVE. REMOVED AND REPLACED AFT E&E DOOR. REMOVED AND REPLACED RT MLG DOOR ROD ASSY PE R MM & SWA RA. 2 L 7 2 4F RT A16WE 2001080200287 20010802 00287 2001 8 2 SWAA012026 4 20010718 A 2565 63551101 SLIDE BOEING 737 7377H4 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 742SW 29278 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001080200288 20010802 00288 EA 2001 8 2 COMA0160547 1 20010730 A 4920 38004883 APU CNDAIR CL600 CL6002B19 EA SMOKE A COMA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 01 915CA 11912 72 7013 SMOKE IN CABIN AND COCKPIT WHEN USING APU BLEED AIR.REPLACED THE APU. 2 L 7 2 4F RT A21EA 2001080200289 20010802 00289 EA 2001 8 2 COMA0160545 1 20010730 A 2720 6229815704 COMPUTER CNDAIR CL600 CL6002B19 EA MALFUNCTIONED A COMA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 01 797CA 49 7344 YAW DAMPNER DROPPED OFF LINE DURING TAXI CHECKS.REPLACED THE #1 FCC-4000. 2 L 7 2 4F RT A21EA 2001080200290 20010802 00290 EA 2001 8 2 COMA0160551 1 20010801 A 2760 270007 PCU CNDAIR CL600 CL6002B19 EA MALFUNCTIONED A COMA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 01 959CA 5906 7116 CONFIG SPOILERS WARNING DURING T/O.REPLACED THE LEFT HAND FLIGHT SPOILER OUTBOARD PCU. 2 L 7 2 4F RT A21EA 2001080200291 20010802 00291 SO 2001 8 2 COMA0110131 1 20010801 A 3150 ATG120TR PROXIMITY SWITCH EMB 120 EMB120RT SO MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 267CA 120259 TAKE OFF TRIM AURAL WARNING. REPLACED DEFECTIVE ELEV. TRIM PROXIMITY SENSOR. 2 L 7 2 4T RT A31SO 2001080200292 20010802 00292 NM 2001 8 2 SWAA012027 1 20010718 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 521SW 25320 DURING SCHEDULED D-CHECK, FOUND EEPLS MISSING AT FWD END. INSTALLED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001080200293 20010802 00293 NM 2001 8 2 SWAA012029 1 20010718 A 3350 610478 BATTERY PACK BOEING 737 7373A4 1384585 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED BC4 CHECK, FOUND EEPLS COVER MISSING AND EEPLS INOP AT OVERWING EXIT. INSTALLED COVER, REMOVED AND REP LACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2001080200294 20010802 00294 NM 2001 8 2 SWAA012032 1 20010718 A 3350 65C34691 LIGHT BOEING 737 7373Y0 1384671 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 308SA 23498 DURING SCHEDULED A1 CHECK, FOUND LT AFT BULL NOSE EMERGENCY LIGHT INOP. RELAMPED BULL NOSE LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001080200296 20010802 00296 2001 8 2 SWAA012033 4 20010718 A 2565 D31354 SLIDE BOEING 737 7372K6 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001080200297 20010802 00297 2001 8 2 SWAA012034 4 20010718 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001080200298 20010802 00298 NM 2001 8 2 SWAA012036 1 20010718 A 2910 6544548 B-NUT BOEING 737 7373H4 1384600 NM HYDRAULIC SYS LOOSE A SWAA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 354SW 25219 (DECLARED EMERGENCY) DURING FLIGHT LOST A-SYSTEM HYD. FOUND AUTOPILOT SERVO PRESS LINE LOOSE, TIGHTENED B-NUT PER MM. 2 L 7 2 4F RT A16WE 2001080200299 20010802 00299 SO 2001 8 2 COMA0110132 1 20010801 A 3350 10130115 LIGHT EMB 120 EMB120RT SO BROKEN A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 462CA 120264 EMERGENCY LIGHT AT ROW 5 IS BROKEN.REPLACED LIGHT ASSY. 2 L 7 2 4T RT A31SO 2001080200302 20010802 00302 NM 2001 8 2 SWAA012039 1 20010719 A 2730 6545166 BEARING BOEING 737 7373H4 1384600 NM ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 634SW 27937 DURING SCHEDULED C4 CHECK, SWA SI 11052-55, LT & RT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT& RT UPPER ELEVATOR PUSH ROD BEARINGS PER MM. 2 L 7 2 4F RT A16WE 2001080200303 20010802 00303 NM 2001 8 2 SWAA012041 1 20010719 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED 1/2D CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LOOSE AT ROW 23 DEF. SECURED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001080200304 20010802 00304 NM 2001 8 2 SWAA012042 1 20010719 A 3350 65C34691 LENS BOEING 737 7373A4 1384585 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 BULL NOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 5 DEF. INSTALLED EXIT LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2001080200305 20010802 00305 NM 2001 8 2 SWAA012043 1 20010719 A 3350 BR2013 LIGHT BOEING 737 7373A4 1384585 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 674AA 23252 EEPLS INOP AT ROW 20. REMOVED AND REPLACED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001080200307 20010802 00307 2001 8 2 SWAA012044 4 20010717 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 AFT ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001080200308 20010802 00308 2001 8 2 SWAA012045 4 20010719 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 089SW 22904 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001080200310 20010802 00310 2001 8 2 SWAA012046 4 20010719 A 2565 D31354 SLIDE BOEING 737 7377H4 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 748SW 29800 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF THE CONTAINER. REINSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001080200311 20010802 00311 NM 2001 8 2 SWAA012050 1 20010721 A 3350 65C27093 BALLAST BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 601WN 27695 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BALLAST PER MM. 2 L 7 2 4F RT A16WE 2001080200313 20010802 00313 NM 2001 8 2 SWAA012051 1 20010719 A 3350 300432 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP RT AFT EXTERIOR. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001080200314 20010802 00314 NM 2001 8 2 SWAA012052 1 20010721 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM SERVICE DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001080200316 20010802 00316 NM 2001 8 2 SWAA012054 1 20010721 A 2730 65C35943 BEARING BOEING 737 7377H4 NM ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 729SW 27861 DURING SCHEDULED C4 CHECK, BOTH ELEVATORS FAILED FREE PLAY CHECK. REMOVED AND REPLACED BEARINGS AT ELEVATOR TORQUE TUBE PER MM. 2 L 7 2 4F RT A16WE 2001080200317 20010802 00317 NM 2001 8 2 SWAA012055 1 20010705 A 3350 610478 BATTERY PACK BOEING 737 737317 138447P NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHTS INOP AT AFT CABIN. REMOVED AND REPLACED LIGHT BATTERY PACK PER M M. 2 L 7 2 4F RT A16WE 2001080200318 20010802 00318 2001 8 2 SWAA012056 4 20010719 A 2565 D31354 SLIDE BOEING 737 7373G7 1384595 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001080200320 20010802 00320 NM 2001 8 2 SWAA012057 1 20010719 A 3350 BR2013 LIGHT BOEING 737 7373A4 1384585 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED C4 CHECK, FOUND EPLS LOOSE AT AFT CABIN. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001080200321 20010802 00321 2001 8 2 SWAA012059 4 20010720 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 527SW 26569 FWD SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001080200322 20010802 00322 NM 2001 8 2 SWAA012061 1 20010720 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 651SW 27721 EEPLS LOOSE AT OVERWING EXIT. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001080200323 20010802 00323 NM 2001 8 2 SWAA012063 1 20010722 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 394SW 27380 EEPLS WIRES LOOSE. RECONNECTED EEPLS WIRES PER MM. 2 L 7 2 4F RT A16WE 2001080200324 20010802 00324 NM 2001 8 2 SWAA012065 1 20010722 A 3350 6556633 LIGHT BOEING 737 7377H4 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 718SW 27852 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED OVERWING EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001080200325 20010802 00325 NM 2001 8 2 SWAA012066 1 20010721 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 378SW 26585 DURING SCHEDULED 1/4D CHECK, FOUND EEPLS INOP AT ROW 20. REMOVED AND REPLACED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001080300001 20010803 00001 GL 2001 8 3 ALG2001F00013 2 20010516 A 7210 23068295 GEAR ALLSN C30S SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30P 03013 GL NR 2 PTO CORRODED E ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 917QS CAG90750 760217 UPON REMOVAL FROM BOX AND VISUAL INSPECTION, FOUND CORROSION PITTING ON GEAR SURFACE, GEAR TEETH, AND BEARING JOURNAL. C/W BLACK OXIDE PROCEDURE AT FACTORY BEFORE RELEASING PART. 1 G 7 2 3U 3 U H1NE E1GL 2001080300002 20010803 00002 GL 2001 8 3 ALG2001F00014 2 20010516 A 7260 23068295 GEAR ALLSN C30S SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL PTO GEAR CORRODED E ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 709AL CAG90048 760278 UPON REMOVAL FROM BOX AND VISUAL INSPECTION, FOUND CORROSION PITTING ON GEAR SURFACE, GEAR TEETH, AND BEARING JOURNAL. C/W BLACK OXIDE PROCEDURE AT FACTORY BEFORE RELEASING PART. 1 G 7 2 3U 3 U H1NE E1GL 2001080300003 20010803 00003 NE 2001 8 3 ALG2001F00015 1 20010626 A 3230 LANDING GEAR SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30P 03013 GL MAIN MALFUNCTIONED E ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 709AL 760278 AFTER TAKEOFF, THE LANDING GEAR FAILED TO RETRACT. PERFORMED FUNCTION CHECK OF THE LANDING GEAR AND COULD NOT DUPLICATE . THE LANDING GEAR WAS EXTENDED AND RETRACTED APPROXIMATELY 13 TIMES AND FUNCTIONED NORMALLY. 1 G 7 2 3U 3 U H1NE E1GL 2001080300004 20010803 00004 EA 2001 8 3 EHA2001F00001 2 20010605 A 7321 252499613 FUEL CONTROL BELL 212 212 1181420 SW PWA PT6 PT6* 52043 EA NR2 ENGINE FAILED E EHAA K NONE O OTHER IN INSP/MAINT 1 AL 03 212EV 218 218 30881 CPPS61764 ON INITIAL START IN AFCU POSITION, RUN-UP AND SUBSEQUENT THROTTLE BACK TO FLT IDLE. NR 2 ENG N1 WAS OBSERVED 49 PER CEN T. WHEN THROTTLE WAS ADVANCED, 100 PER CENT NR 2 WAS ACHIEVED PRIOR TO REACHING HIGH SIDE STOP ON THROTTLE TWIST GRIP ( LINEAR ACTUATOR WAS IN FULL DECREASE POSITION) PILOTS OBSERVATION WAS THAT THROTTLE POSITION AT 100 PER CENT NR2 AND FLT IDLE DUP THESE FINDINGS. OBSERVATIONS WERE IDENTICAL WHEN SOLONOID WAS CHECKED AND FOUND OPERATIVE. DUE TO HIGH SIDE MALFUNCTION, NR 2 GOVERNOR WAS REMOVED AND INSTALLED ON NR 1 ENG. ALL NR 1 PARAMETERS CHECKED NORMAL. A REPLACEMENT AF CU WAS INSTALLED ON NR2 ENG, AND THE AFFECTED ENG MAINTND FUEL SCHEDULING ABNORMALITIES. FLT CKS OK, RETURN TO SERVICE. 1 G 7 1 4U 3 T H4SW E2NE 2001080300005 20010803 00005 NM 2001 8 3 DL757011192 1 20010718 A 3520 80300002 GENERATOR BOEING 757 757232 1384965 NM LAV O2 SYS DISCHARGED A DALA K NONE O OTHER DE DESCENT 1 SO 27 677DL 25982 OVERHEAD PANEL HOT TO TOUCH W/ ACCOMP ODOR MID LAV F/O SIDE. POSS O2 GEN. CABIN PRESS NORMAL. UPON INSP FOUND MID LAV O2 GEN DISCHARGED. CREW REPORTS MASKS WERE IMPROPERLY STOWED. SUSPECT DISCHARGED BY PAX, REP O2 GEN PER MM 35-21-04-4. OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2001080300006 20010803 00006 WP 2001 8 3 RRXA11337 1 20010726 A 5330 57503656 DOOR DOUG DC8 DC873F 302199F WP STA. 705 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO R/H KEEL PRESSURE PANEL AT STA. 705, DAMAGE EXCEEDED LIMITATIONS IA W DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001080300007 20010803 00007 WP 2001 8 3 RRXA1136 1 20010726 A 5330 5750365 SKIN DOUG DC8 DC873F 302199F WP STA 600-680 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LOWER BELLY SKIN AT STA. 600-680 AND L33R-L34L, DAMAGE EXCEEDED LIM ITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED SKIN REP AIR AND INSTALLED IAW DHSK791-456 REV.A WITH APPROVED 8110-3. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001080300008 20010803 00008 NM 2001 8 3 DL76S010953 1 20010612 A 2120 UNKNOWN BOEING 767 767332 1382001 NM COCKPIT ODOR A DALA O OTHER J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 120DL 23279 AT FL 410 TERRAIN SYSTEM STARTED WARNING OF TERRAIN, NOTICED ODOR OF MELTING PLASTIC. CK UNDER O-CARE SHIELD WIRING OR ODOR FOUND FIBERGLASS ON F/O ALT. REPOSITION, OK. DROPPED O/H PNL, ALL NORMAL. DROPPED C/B BOS NORMAL. CK E/E BUNDLE S P51 PNL AREA NORMAL. CK APU NORMAL. GROUND PROX WING TEST OK. SET UP TO REPLACE THE ENHANCED GPWS COMPUTER PER M/M 34-4 6-01-4. 2 L 7 2 4F RT A1NM 2001080300009 20010803 00009 EU 2001 8 3 RAIA00107035 1 20010731 A 2430 51539019E GCU JETAIR JETSTM JETSTM4101 1500501 EU ELEC BAY FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 563HK 11886 2570 41079 5393-BWI-LEFT GENERATOR FELL OFF LINE, AMBER CAPTION ILLUMINATED DURING TAXI. MAINTENANCE INSPECTED AND REPLACED LEFT GE NERATOR CONTROL UNIT. 2 L 7 2 4T RT A41NM 2001080300010 20010803 00010 2001 8 3 RAIA00108001 4 20010801 A 3160 7003110 DISPLAY JETAIR JETSTM JETSTM4101 1500501 EU INST PANEL FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 552HK 13218 4414 41057 7446-STL-RIGHT LOWER EFIS TUBE (EHSI) FAILED DURING CLIMB. MAINTENANCE INSPECTED AND REPLACED RIGHT LOWER EFIS TUBE. 2 L 7 2 4T RT A41NM 2001080300011 20010803 00011 NE 2001 8 3 DL76S011008 2 20010618 A 7321 8063508 MEC BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 2 ENGINE MALFUNCTIONED A DALA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 SO 27 138DL 25409 580125 DURING FLIGHT NR 2 ENGINE WOULD NOT RESPOND TO THROTTLE MOVEMENT. ENGINE SHUT DOWN, LANDED SINGLE ENGINE. CHECKED THRO TTLE CABLES, ALL SECURE. REMOVED AND REPLACED MECPRE M/M. LEAK AND RUN CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E13NE 2001080300012 20010803 00012 NM 2001 8 3 DL76S011011 1 20010619 A 3350 767 LIGHT BOEING 767 767332 1382001 NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 121DE 23435 R-1 DOOR EXTERIOR EMERGENCY LIGHT INOP. REPLACED BULB, OP CK GOOD. 2 L 7 2 4F RT A1NM 2001080300014 20010803 00014 NM 2001 8 3 DL76S011012 1 20010619 A 3350 PIN BOEING 767 767332 1382001 NM LIGHT HARNESS BACKED OUT A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 135DL 25145 PAX SEAT 31A EMERGENCY LIGHTS WON`T TEST. FOUND PULLED/BACKED OUT PIN IN SEAT HARNESS. REPAIRED SAME. 2 L 7 2 4F RT A1NM 2001080300015 20010803 00015 NM 2001 8 3 DL76S011039 1 20010621 A 5311 148T274010 FRAME BOEING 767 767332 1382001 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 121DE 23435 BOLT HOLE HFEC INSPECTION OF FASTENERS COMMON TO THE RT FWD OUTER CHORD OF THE FS 1809.5 BULKHEAD INDICATED SMALL CRACKS IN 3 FASTENER HOLES. THE HOLES ARE COMMON TO THE INSPECTION AREA OF BAC S/B 767-53-0078 AND AD 2001-09-13. THE CRACKE D SECTION OF CHORD WAS CUT AND REMOVED AND A NEW SECTION INSTALLED PER THE S/B AND ER/A 381135-14AD. 2 L 7 2 4F RT A1NM 2001080300016 20010803 00016 NM 2001 8 3 DL76S011040 1 20010621 A 5311 148T27409 FRAME BOEING 767 767332 1382001 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 121DE 23435 BOLT HOLE HFEC INSPECTION OF THE LT FWD OUTER CHORD OF THE FS 1809.5 BULKHEAD REVEALED A SMALL CRACK IN A FASTENER HOLE. THE FASTENER LOCATION IS COMMON TO THE INSPECTION AREA OF BAC S/B 767-53-0078 AND AD 2001-09-13. THE CRACKED SECTION OF CAP WAS CUT AND REMOVED AND A NEW SECTION INSTALLED PER THE S/B AND ER/A 381134-14AD. 2 L 7 2 4F RT A1NM 2001080300017 20010803 00017 NM 2001 8 3 DL76S011074 1 20010626 A 2420 490167502 HARNESS BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE APU BURNED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 131DN 12022 24852 P125 WORKING MCO APU ELEC INOP. FOUND GENERATOR FEEDER CABLE BURNT. CABLE SENT TO SHOP WITH OLD GENERATOR. REPLACED CABLE. 2 L 7 2 4F 4 F RT A1NM E13NE 2001080300018 20010803 00018 NM 2001 8 3 DL76S011076 1 20010627 A 3350 HARNESS BOEING 767 767332 1382001 NM CABIN DEFECTIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 129DL 24079 SEAT 37A EMERGENCY LIGHT INOP ON TEST. REPLACED LIGHT HARNESS. 2 L 7 2 4F RT A1NM 2001080300019 20010803 00019 NE 2001 8 3 DL76S011153 2 20010711 A 7200 CF680A2 ENGINE BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 2 MALFUNCTIONED A DALA E A ENGINE SHUTDOWN UNSCHED LANDING M E OVER TEMP VIBRATION/BUFFET CL CLIMB 1 SO 27 131DN 42061 2848 24852 580322 RT ENG EGT EXCEEDED 979 DURING T/O. N2 VIBS 5.0 AND RT HP BLEED LIGHT ON. AIRCRAFT RETURNED TO ATL AND ON APPROACH IN TO ATL RT ENG WAS SHUTDOWN BY CREW DUE EGT CONTINUING TO RISE. REMOVED AND REPLACED NR 2 ENG. 2 L 7 2 4F 4 F RT A1NM E13NE 2001080300020 20010803 00020 NM 2001 8 3 SWAA012160 1 20010730 A 2710 6546455 TAB HINGE BOEING 737 7373H4 1384600 NM LH WING WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 636WN 27709 DURING SCHEDULED 1/2D CHECK, FOUND PLAY AT AILERON TAB INBD HINGE, LH WING. R&R AILERON TAB HI NGE PER SWA ACO # 7197-27. 2 L 7 2 4F RT A16WE 2001080300021 20010803 00021 NM 2001 8 3 SWAA012161 1 20010731 A 2731 BACB28AK04 BUSHING BOEING 737 7373H4 1384600 NM RH ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 350SW 24409 DURING SCHEDULED BC4 CHECK, FOUND RH ELEVATOR TAB INBD HINGE BUSHING WORN. R&R HINGE BUSHING PER M M. 2 L 7 2 4F RT A16WE 2001080300022 20010803 00022 NM 2001 8 3 SWAA012167 1 20010730 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 EEPLS COVER LOOSE AT OVERWING EMERGENCY EXIT. SECURED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2001080300023 20010803 00023 NM 2001 8 3 SWAA012143 1 20010725 A 3350 07912 COVER BOEING 737 7377H4 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 750SA 29802 EEPLS COVER LOOSE AT ROW 1. IINSTALLED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2001080300024 20010803 00024 NM 2001 8 3 SWAA012148 1 20010730 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 EEPLS COVER LOOSE AT OVERWING EMERGENCY EXIT. REINSTALLED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2001080300025 20010803 00025 NM 2001 8 3 SWAA012149 1 20010729 A 3242 2601042 BRAKE ASSY BOEING 737 7372H4 138448C NM LH MLG SEIZED A SWAA O OTHER S AFFECT SYSTEMS IN INSP/MAINT 1 SW 07 062SW 22060 # 1 MLG BRAKE ASSY SEIZED UP AT THE GATE. R&R BRAKE ASSY PER MM. 2 L 7 2 4F A16WE 2001080300026 20010803 00026 NM 2001 8 3 SWAA012150 1 20010728 A 5310 6546541 WEB BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D CHECK, FOUND PRESS WEB CRACKED AT BS 664, LBL 33 & WL 202. REPAIRED WEB PER SWA T1-353-046. 2 L 7 2 4F RT A16WE 2001080300027 20010803 00027 NM 2001 8 3 SWAA012152 1 20010727 A 5330 6545768 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D CHECK, FOUND BILGE INTERNAL SKIN CORRODED AT BS 500C+19, RBL 5. REP AIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001080300028 20010803 00028 NM 2001 8 3 SWAA012153 1 20010724 A 5310 6546529 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D CHECK, FOUND BILGE FRAME SHEAR TIE CORRODED AT BS 500D, RBL 5. R&R SHEAR TIE P ER SRM. 2 L 7 2 4F RT A16WE 2001080300029 20010803 00029 NM 2001 8 3 SWAA012154 1 20010729 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM AFT SVC DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001080300030 20010803 00030 NM 2001 8 3 SWAA012156 1 20010712 A 5511 6547987 RIB BOEING 737 7373Q8 1384670 NM LH HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D CHECK AT DALFORT, FOUND LH HORIZ STAB RIB CRACKED AT L/E, STA 161.04, # 11 RIB. R&R RIB PER SRM. 2 L 7 2 4F RT A16WE 2001080300031 20010803 00031 NM 2001 8 3 SWAA012171 1 20010722 A 5313 BAC1498 STRINGER BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D CHECK, FOUND STRINGER 25L CORRODED AT BS 352. REPAIRED STR PER S RM. 2 L 7 2 4F RT A16WE 2001080300032 20010803 00032 NM 2001 8 3 SWAA012173 1 20010726 A 5310 6517582 WEB BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D CHECK, FOUND 2 EA CRACKS AT VERTICAL BEAM WEB AT BS180, RBL 17.1, WL 183 & WL 226. R&R VERTICAL BEAM WEB PER BFG ER. 2 L 7 2 4F RT A16WE 2001080300033 20010803 00033 NM 2001 8 3 SWAA012174 1 20010716 A 5310 6517582 WEB BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17.1 & WL 225. REPAIRED WEB PER BFG ER. 2 L 7 2 4F RT A16WE 2001080300034 20010803 00034 NM 2001 8 3 SWAA012175 1 20010730 A 5310 6516300 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 390SW 26593 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND 2 EA CRACKS AT BULKHEAD WEB, BS 178, LBL 5.5, WL 202-201 & WL 199.5-199.0. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001080300035 20010803 00035 NM 2001 8 3 SWAA012176 1 20010731 A 5330 6545769 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 313SW 23335 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515, STR 12L & BS 505, STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001080300036 20010803 00036 NM 2001 8 3 SWAA012178 1 20010731 A 3350 07912 COVER BOEING 737 7377H4 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 750SA 29802 DURING SCHEDULED C3 CHECK, FOUND EEPLS COVERS CRACKED AT NUMEROUS LOCATIONS IN CABIN. R&R EE PLS COVERS PER MM. 2 L 7 2 4F RT A16WE 2001080300037 20010803 00037 NM 2001 8 3 SWAA012181 1 20010731 A 2761 6544851 ACTUATOR BOEING 737 7373H4 1384600 NM LH WING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED A1 CHECK, FOUND # 4 GROUND SPOILER ACTUATOR UPPER ATTACH LOBE BROKEN. R&R # 4 GROUND SPOILER ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2001080300038 20010803 00038 NM 2001 8 3 SWAA012117 1 20010728 A 3350 07912 COVER BOEING 737 7377H4 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 751SW 29803 EEPLS COVER MISSING AT ROW 1. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2001080300039 20010803 00039 NM 2001 8 3 SWAA012118 1 20010728 A 3350 07912 COVER BOEING 737 7373T0 1384582 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 684WN 23941 EEPLS COVER MISSING AT ROW 5. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2001080300040 20010803 00040 NM 2001 8 3 SWAA012119 1 20010727 A 3350 07912 COVER BOEING 737 7373A4 1384585 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 EEPLS COVER MISSING AT OVERWING EXIT. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2001080300041 20010803 00041 NM 2001 8 3 SWAA012120 1 20010728 A 3350 07912 COVER BOEING 737 7372T4 1384492 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED A1 CHECK, FOUND EEPLS COVER MISSING AT FWD END. INSTALLED COVER PER MM. 2 L 7 2 4F A16WE 2001080300042 20010803 00042 2001 8 3 SWAA012125 4 20010726 A 2565 6557463 BRACKET BOEING 737 7373H4 1384600 NM AFT SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 389SW 26592 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR GIRT BAR BRACKET LOOSE. SECURED GIRT BAR B RACKET PER MM. 2 L 7 2 4F RT A16WE 2001080300043 20010803 00043 NM 2001 8 3 SWAA012129 1 20010728 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR UPPER HINGE CUTOUT, CRACK IS 5/32. REPAIRED SKIN PER SWA RA. 2 L 7 2 4F RT A16WE 2001080300044 20010803 00044 NM 2001 8 3 SWAA012130 1 20010726 A 5710 6959886 FITTING BOEING 737 737301 1384611 NM LH WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED C3 CHECK, FOUND LH MLG BEAM HANGER FITTING CRACKED AT FWD END. R&R FITTING P ER ALM INV. # SWA 10410. 2 L 7 2 4F RT A16WE 2001080300045 20010803 00045 NM 2001 8 3 SWAA012131 1 20010725 A 5710 6959886 FITTING BOEING 737 7373Q8 1384670 NM RH WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D CHECK, FOUND RH MLG BEAM FITTING CRACKED AT D HOLE. REPAIRED FITTING PER BFG ER. 2 L 7 2 4F RT A16WE 2001080300046 20010803 00046 NM 2001 8 3 SWAA012132 1 20010726 A 2731 BACB28AK04 BUSHING BOEING 737 737317 138447P NM RH ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED C2 CHECK, RH ELEVATOR TAB FAILED FREE PLAY CHECK. R&R INBD ELEVATOR TAB HING E BUSHING PER MM. 2 L 7 2 4F RT A16WE 2001080300047 20010803 00047 NM 2001 8 3 SWAA012135 1 20010724 A 5310 6546546 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED BETWEEN STR'S 8L & 9L, BS 490, BS 807, BS 827, BS 787 & BS 767. REPAIRED FRAMES PER BFG ER. 2 L 7 2 4F RT A16WE 2001080300048 20010803 00048 NM 2001 8 3 SWAA012136 1 20010724 A 5310 6546529 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED BETWEEN STR'S 8R & 9R, BS 380, BS 767, BS 480, BS 440 & BS 807. REPAIRED FRAMES PER BFG ER. 2 L 7 2 4F RT A16WE 2001080300049 20010803 00049 NM 2001 8 3 SWAA012138 1 20010723 A 5310 6546529 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RBL 66 & WL 200. REPAIRED FRAME PER SWA T1-153-018. 2 L 7 2 4F RT A16WE 2001080300050 20010803 00050 NM 2001 8 3 SWAA012140 1 20010728 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 366SW 26577 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001080300051 20010803 00051 NM 2001 8 3 SWAA012092 1 20010716 A 5310 6516300 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 637SW 27710 DURING SCHEDULED 1/2D CHECK, FOUND WEB CRACKED AT BS 178+2, RBL 17.1 & WL 230. R&R WEB PER BFG ER. 2 L 7 2 4F RT A16WE 2001080300052 20010803 00052 NM 2001 8 3 SWAA012095 1 20010709 A 5320 6546539 WEB BOEING 737 7373Q8 1384670 NM FUSELAGE CHAFED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D CHECK, FOUND LH OVERWING EMERGENCY CUT OUT SILL WEB CHAFED AT BS 635 & 643, WL 221. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001080300053 20010803 00053 NM 2001 8 3 SWAA012097 1 20010725 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STR 21L. REPAIRED SKIN PER S RM. 2 L 7 2 4F RT A16WE 2001080300054 20010803 00054 NM 2001 8 3 SWAA012098 1 20010723 A 5330 6518420 WINDOW POST BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED SERVICE CHECK, FOUND LH WINDOW POST CRACKED AT # 1 SLIDING WINDOW. REPAIRED WINDOW POST PER SRM. 2 L 7 2 4F RT A16WE 2001080300055 20010803 00055 NM 2001 8 3 SWAA012099 1 20010724 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 639SW 27712 EEPLS LOOSE & MISSING COVERS AT MID CABIN. SECURED EEPLS & INSTALLED COVERS PER MM. 2 L 7 2 4F RT A16WE 2001080300056 20010803 00056 NM 2001 8 3 SWAA012103 1 20010726 A 5310 6546529 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 13L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2001080300057 20010803 00057 NM 2001 8 3 SWAA012105 1 20010726 A 5311 6546543 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RBL 66. REPAIRED FR AME PER BFG T1-153-018. 2 L 7 2 4F RT A16WE 2001080300058 20010803 00058 NM 2001 8 3 SWAA012106 1 20010726 A 3350 079123 COVER BOEING 737 7372T4 1384492 NM CABIN FLOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 EEPLS TRACK COVERS MISSING. INSTALLED TRACK COVERS PER MM. 2 L 7 2 4F A16WE 2001080300059 20010803 00059 NM 2001 8 3 SWAA012107 1 20010725 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN FLOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 750SA 29802 EEPLS COVER LOOSE AT ROW 1. R&R TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001080300060 20010803 00060 NM 2001 8 3 SWAA012109 1 20010725 A 5312 6517583 BEAM BOEING 737 7372H4 138448C NM FUSELAGE NOSE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM CRACKED APRROX 2 LONG, RBL 5.7, WL 183. R EPAIRED BEAM PER SWA RA. 2 L 7 2 4F A16WE 2001080300061 20010803 00061 NM 2001 8 3 SWAA012111 1 20010726 A 5330 6545763 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED APPROX 3.35 LONG, BS 380, STR 10L. REPA IRED SKIN PER SWA RA AND SRM. 2 L 7 2 4F RT A16WE 2001080300062 20010803 00062 NM 2001 8 3 SWAA012113 1 20010726 A 5311 6546546 FRAME BOEING 737 7373Q8 1384670 NM AFT CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D CHECK, FOUND BS 867 FUSELAGE FRAME CRACKED BETWEEN STRS 8R-9R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001080300063 20010803 00063 NM 2001 8 3 SWAA012116 1 20010726 A 3610 BACC10 CLAMP BOEING 737 7377H4 NM AFT CABIN BROKEN A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 404WN 27892 DIVERSION.----------- DURING CLIMB OUT OF ABQ, A LOUD NOISE AND VIBRATION FELT AT THE AFT GALLEY AREA. FOUND APU PNEU SUPPLY DUCT CLAMP BROKEN. R&R CLAMP. OPS CK GOOD. 2 L 7 2 4F RT A16WE 2001080300065 20010803 00065 NE 2001 8 3 DL76S011205 2 20010720 A 7200 CF680A2 ENGINE BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 2 OVERTEMP A DALA C ABORTED TAKEOFF M OVER TEMP TO TAKEOFF 1 SO 27 116DL 50031 23275 580210 RT ENG OVERTEMP ON T/O. EGT943 T/O DISCONTINUED AT 90K. CHECKED INLET AND EXH, RAN ENG PER PFHB MAX PWR ASSURANCE TEST. CLEARED EICAS COMPUTER, MSG 943 FOR 3 SEC OVERTEMP AREA A-MCC ADVISED. 2 L 7 2 4F 4 F RT A1NM E13NE 2001080300066 20010803 00066 2001 8 3 DL777010940 4 20010610 A 2330 1301273111REVP VIDEO UNIT BOEING 777 777232 1385232 NM CABIN MALFUNCTIONED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 860DA 29951 ABOUT 2.5 HOURS AFTER TAKEOFF AN ODOR APPEARED IN THE FORWARD CABIN IN THE VICINITY OF ROWS 4-5. A SOURCE WAS NOT FOUND . THE SMELL MOVED AS FAR AS ROW 2 THEN DISSIPATED WITHIN 15 MINS. THE SMELL WAS CHEMICAL NOT STRONG. THE VIDEO CONTRO LS FOR SEATS 5C AND 5G WERE LOST. FOUND BURNT SMELL FROM SEAT 5 C/G AVU. REMOVED AND REPLACED SEAT AVU, OPS GOOD RAN F OR 2.5 HOURS. 2 L 7 2 4F RT T00001SE 2001080300067 20010803 00067 NM 2001 8 3 DL777011122 1 20010705 A 2530 ODOR BOEING 777 777232 1385232 NM AFT GALLEY DETECTED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 864DA 29736 SULFER/ELECTRICAL SMELL AFT GALLEY TURNED OFF CHILLERS AND OTHER GALLEY ELEC EQUIP AND SMELL DISSIPATED. RAN GALLEY COM PONENTS AFT GALLEY, NO UNUSUAL SMELL NOTED. 2 L 7 2 4F RT T00001SE 2001080300068 20010803 00068 NE 2001 8 3 DL78K011027 2 20010618 A 7314 PUMP BOEING 737 737832 13844CF NM CFMINT CFM567 CFM567B2US 13802 NE NR 2 ENGINE FAULTY A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 395DN 30773 NR 2 ENGINE SHUTS DOWN AFTER REACHING IDLE. T/S PER FIM 73-06-00-810-807 FOUND FUEL PUMP PRESSURE LOW PER AMM 73-11-01- 200-802. REPLACED FUEL PUMP PER AMM 73-11-01-4. LEAK CHECK AND OPS CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 2001080300069 20010803 00069 2001 8 3 VNAA0107025 4 20010730 A 3400 COMPUTER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 434JS 3051 DURING THE TAKE OFF ROLL, THE CREW RECEIVED A FLIGHT GUIDANCE COMPUTER FAIL CAS MESSAGE. THE CREW ABORTED TAKE OFF. WH EN EXITTING THE RUNWAY THE COMPUTER RESET AND AFTER CONFERRING WITH MAINTENANCE CONTROL, WAS CLEARED FOR ANOTHER TAKE O FF ATTEMPT. FLIGHT 4019 DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001080300070 20010803 00070 NE 2001 8 3 DL78K011033 2 20010619 A 7320 HMU BOEING 737 737832 13844CF NM CFMINT CFM567 CFM567B2US 13802 NE NR 2 ENGINE FAULTY A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 395DN 1393 876469 30773 876469 DURING PREFLT, FOUND NR 2 ENG SHUT DOWN INADVERTENTLY AND WOULD NOT RESTART. FOUND HMU INOP. REPLACED HMU. 2 L 7 2 4F 4 F RT A16WE E2GL 2001080300071 20010803 00071 NM 2001 8 3 DL78K011171 1 20010714 A 3350 D71701100 BATTERY PACK BOEING 737 737832 13844CF NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 3738B 30382 FWD EMERGENCY LIGHTS AT L1 DOOR INOP. REPLACED BATTERY PACK M1675, OPS NORMAL. 2 L 7 2 4F RT A16WE 2001080300074 20010803 00074 NM 2001 8 3 DL78K011174 1 20010715 A 8011 35059458 STARTER BOEING 737 737832 13844CF NM GE CFM56 CFM567B24 NE NR 1 ENGINE FAILED A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 3731T 30775 876629 NR 1 ENG STARTER SHEARED ON INITIAL START. REPLACED NR 1 ENG STARTER AND SERVICED. WINDMILLED ENG AND NO LEAKS ON DUCT . OPN CHECKS NORMAL. 2 L 7 2 4F 4 F RT A16WE E00055EN 2001080300076 20010803 00076 WP 2001 8 3 DLL10010942 1 20010610 A 3350 LIGHT LKHEED 1011 10113851 5265010 WP EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 730DA 193C1199 R4 EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT. 2 L 7 3 4F A23WE 2001080300080 20010803 00080 WP 2001 8 3 DLL10010959 1 20010613 A 2120 DUCT LKHEED 1011 10113851 5265010 WP A/C BAY SEPARATED A DALA O OTHER B M SMOKE/FUMES/ODORS/SPARKS OVER TEMP LD LANDING 1 SO 27 730DA 193C1199 ON APPROACH AFTER GEAR DOWN APPROX 1300 FT, LOUD BANG FOLLOWED BY AIR CONDITIONING SMOKE ON TOUCHDOWN AND B-AREA OVERHEA T. FOUND INLET DUCT GOING TO NR 2 ACM SEPARATED WILL NEED DUCT, GASKETS, AND HARDWARE. LOCKED OUT NR 2 PACK FLOW CONTR OL VALVE PER MEL 21-21-01B. 2 L 7 3 4F A23WE 2001080300082 20010803 00082 WP 2001 8 3 DLL10010961 1 20010613 A 2120 SMOKE LKHEED 1011 10113851 5265010 WP CABIN DETECTED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 730DA 193C1199 ON LANDING F/A REPORTED SMOKE IN THE CABIN. MTC IN PROGRESS. TROUBLESHOOTING CAUSE OF SMOKE. 2 L 7 3 4F A23WE 2001080300086 20010803 00086 WP 2001 8 3 DLL10010999 1 20010618 A 5312 1504400 WEB LKHEED 1011 10113851 5265010 WP FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 728DA 193C1173 INSPECTION OF THE FS 1212 BULKHEAD WEB PER AD 2000-16-08 REVEALED A .5 INCH CRACK AT LBL 30. THE CRACK WAS ROUTED OUT O F THE WEB AND REPAIRED WITH TWO ALUMINUM DOUBLERS PER LAC SB 093-53-277 AND DOCUMENTED PER ER/A 381118-14AD. 2 L 7 3 4F A23WE 2001080300088 20010803 00088 NM 2001 8 3 DLM11010956 1 20010612 A 2611 PC1604 BATTERY DOUG MD11 MD11 3023602 NM LAVATORY DISCHARGED A DALA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SO 27 803DE 48474 LAV 1L SMOKE DETECTOR WILL NOT TURN OFF. REPLACED BATTERY. 2 L 7 3 4F RT A22WE 2001080300089 20010803 00089 NM 2001 8 3 DLM11010983 1 20010616 A 3350 6044113 BATTERY DOUG MD11 MD11 3023602 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 802DE 48473 ON EMERGENCY LIGHT TEST NR 3 BATTERY FOUND BAD. REPLACED SAME. 2 L 7 3 4F RT A22WE 2001080300091 20010803 00091 NM 2001 8 3 DLM11011004 1 20010618 A 3241 60060812 TRANSDUCER DOUG MD11 MD11 3023602 NM ANTISKID SYS FAILED A DALA K NONE O OTHER LD LANDING 1 SO 27 806DE 48477 NR 10 TIRE BLOWN ON LANDING. REPLACED NR 10 ANTISKID TRANSDUCER. 2 L 7 3 4F RT A22WE 2001080300093 20010803 00093 NM 2001 8 3 DLM11011006 1 20010618 A 2611 PC1604 BATTERY DOUG MD11 MD11 3023602 NM LAVATORY MISSING A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 802DE 48473 FOUND DOOR 4L AFT LAV SMOKE ALARM INOP. FOUND 9V BATTERY HAD BEEN REMOVED AND MISSING. INSTALLED BATTERY AND SECURED C OVER BY SAFETY WIRE. NO EVIDENCE OF FIRE IN LAV AND SMOKE ALARM OPS OK. 2 L 7 3 4F RT A22WE 2001080300094 20010803 00094 NM 2001 8 3 DLM11011015 1 20010620 A 7931 O-RING DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 1 ENGINE LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 804DE 24260 733752 48475 733752 NR ONE ENGINE LOSING OIL. QTY DOWN TO ONE. FOUND O-RING AT BOTTOM OF OIL PRESSURE TRANSMITTER TO BE LEAKING. REPLACED O-RING. REPLACED TRANSMITTER AS PRECAUTION. 2 L 7 3 4F 4 F RT A22WE E24NE 2001080300095 20010803 00095 NM 2001 8 3 DLM11011072 1 20010626 A 2120 UNKNOWN DOUG MD11 MD11 3023602 NM CABIN ODOR A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 815DE 48624 SLIGHT ODOR OF SMOKE IN FWD BUSINESS CLASS LT AISLE AT O/H BIN LEVEL. ODOR EVENTUALLY DISSIPATED AFTER SELECTING ECON O FF. NO SMOKING TO OFF AND FASTEN SEAT BELTS TO OFF. REMOVE CEILING PANELS AT ROW 2/3/4 AND INSP OVERHEAD. REMOVE NO SM OKING/FASTEN SEAT BELTS ASSY AND READING LIGHTS ASSY AT SAME. INSP FLOUR LIGHT BALLAST AND WIRING ALL AREAS, NO TROUBLE FOUND. RAN RECIRC FANS AND NO SMOKING/FASTEN SEAT BELT LIGHTS ON GROUND. ALL OKAY. NO SMOKE OR ODOR NOTED. 2 L 7 3 4F RT A22WE 2001080300096 20010803 00096 NM 2001 8 3 DLM11011099 1 20010701 A 3397 WIRE DOUG MD11 MD11 3023602 NM CABIN DISCONNECTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 813DE 48600 ON L/O FOUND EMERGENCY LIGHTS AT SEAT 32¥ 33¥ 34, 35 INOP. RECONNECTED WIRE SPLICE AT SEAT 32¥, ALL SEAT LIGHTS OK. 2 L 7 3 4F RT A22WE 2001080300097 20010803 00097 NM 2001 8 3 DLM11011131 1 20010707 A 3350 60404113 BATTERY PACK DOUG MD11 MD11 3023602 NM COCKPIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 804DE 48475 NR 1 EMERGENCY LIGHT BATTERY FAILED TEST. REPLACED SAME. 2 L 7 3 4F RT A22WE 2001080300098 20010803 00098 NM 2001 8 3 DLM11011152 1 20010712 A 2560 61020 BATTERY DOUG MD11 MD11 3023602 NM FLASHLIGHT DISCHARGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 808DE 48479 LED ON EMERGENCY FLASHLIGHT AT 4R NOT FLASHING. REPLACED BATTERY LIGHT, OPN CHECKS NORMAL. 2 L 7 3 4F RT A22WE 2001080300099 20010803 00099 NM 2001 8 3 DLM11011156 1 20010712 A 3350 LENS DOUG MD11 MD11 3023602 NM CABIN DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 812DE 48601 PASSENGER SEAT 121B EMERGENCY TRACK FLOOR LIGHT DAMAGED. REPLACED LENS. 2 L 7 3 4F RT A22WE 2001080300101 20010803 00101 NM 2001 8 3 DLM88010917 1 20010510 A 2433 TRANSFORMER DOUG MD88 MD88 3023688 NM E/E BAY OVERHEATED A DALA K NONE M OVER TEMP IN INSP/MAINT 1 SO 27 942DL 49815 FWD E/E ABOVE TR L-2 HAS EVIDENCE OF HIGH HEAT TEMPERATURE DUE TO INSULATION BLANKET DAMAGE AND WORN FRAME AT STA 48 LBL 2D. REMOVED AND REPLACED L-2 TRANSFORMER RECTIFIER, OPS CHECK GOOD PER M/M. 2 L 7 2 4F RT A6WE 2001080300102 20010803 00102 NM 2001 8 3 DLM88010921 1 20010430 A 8011 STARTER DOUG MD88 MD88 3023688 NM NR 1 ENGINE SPARKS A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 942DL 28412 49815 20233 NR 1 ENGINE STARTER EMITTING SPARKS DURING ENGINE SPIN. REPLACED STARTER PER M/M 80-10-01-2. REINSTALLED START VALVE. 2 L 7 2 4F RT A6WE 2001080300103 20010803 00103 NM 2001 8 3 DLM88010935 1 20010609 A 3230 LANDING GEAR DOUG MD88 MD88 3023688 NM NLG MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 930DL 49717 ON T/O NOSE GEAR FAILED TO RETRACT, HEAVY GRINDING AUDIBLE -RED LIGHT IN HANDLE. INSPECTED AND SERVICED NOSE STRUT PER M/M 32-21-02-3-1. CHECKED PROX SENSORS AND CLEANED SAME, ALL CHECKED NORMAL. PERFORMED NOSE GEAR SWING, ALL NORMAL. C HECKED WHEEL BEARINGS AND TIRE CONDITION, ALL CHECKED OK. 2 L 7 2 4F RT A6WE 2001080300104 20010803 00104 NM 2001 8 3 DLM88010936 1 20010609 A 2160 32185831 CONTROL VALVE DOUG MD88 MD88 3023688 NM A/C BAY FAULTY A DALA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 SO 27 909DE 53418 AT 31,000 FT RT PACK AIR STUCK IN COLD POSITION, WOULD NOT MOVE. LEFT PACK SUPPLY PRESS DROPPED TO ZERO MOMENTARILY CAU SING CABIN ALT TO CLIMB. DESCEND TO 10,000 FT AND IT HAPPENED AGAIN. ATL MCC 2100Z. FOUND RT PACK MIX VALVE STICKING. REPLACED RT PACK TEMP CONTROL VALVE. RT PACK OPS AND LEAK CHECKS GOOD. 2 L 7 2 4F RT A6WE 2001080300106 20010803 00106 NM 2001 8 3 DLM88010972 1 20010614 A 5752 5955493502 PANEL DOUG MD88 MD88 3023688 NM AILERON TAB MISSING A DALA K NONE D INFLIGHT SEPARATION CR CRUISE 1 SO 27 935DL 49722 CLOSE OUT PANEL FOR AILERON TRIM TAB O/B BEARING TOP COVER MISSING. REPLACED SAME. 2 L 7 2 4F RT A6WE 2001080300107 20010803 00107 NM 2001 8 3 DLM88010973 1 20010614 A 3350 LIGHT DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 920DL 49644 PAX SEAT 37DE EMERGENCY LIGHT INOP ON MTC TEST. REPLACED LIGHT ASSY, NOW TESTS NORMAL. 2 L 7 2 4F RT A6WE 2001080300110 20010803 00110 NM 2001 8 3 DLM88010975 1 20010614 A 2421 38005041 GENERATOR DOUG MD88 MD88 3023688 NM APU SHORTED A DALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 27 956DL 10073 49887 P80512 INFLIGHT ATL-EWR APU GENERATOR DROPPED OFFLINE AND WOULD NOT RESET. FLIGHT DIVERTED TO KCVG. FOUND APU GENERATOR FIELD SHORTED. REPLACED APU ASSY PER MM. LEAK CHECKS OK. OPS NORMAL. 2 L 7 2 4F RT A6WE 2001080300111 20010803 00111 NM 2001 8 3 DLM88010994 1 20010617 A 2530 4110001137 COFFEEMAKER DOUG MD88 MD88 3023688 NM GALLEY SMOKE A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 997DL 53364 AFT GALLEY COFFEEMAKER SMOKING. REMOVED AND REPLACED AFT COFFEEMAKER. A/C RIGHT SIDE COFFEEMAKER OPS CHECKS NORMAL. 2 L 7 2 4F RT A6WE 2001080300112 20010803 00112 NM 2001 8 3 DLM88010998 1 20010614 A 3350 922710127 LIGHT DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 941DL 49814 FOUND ON LAYOVER OVERWING EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY. 2 L 7 2 4F RT A6WE 2001080300113 20010803 00113 NM 2001 8 3 DLM88011014 1 20010620 A 2530 50459 OVEN DOUG MD88 MD88 3023688 NM GALLEY MALFUNCTIONED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 997DL 53364 SHORTLY AFTER T/O STRONG ELECT SMELL IN COCKPIT AND FWD GALLEY AREA RETURNED TO FIELD. FOUND BURNING SMELL COMING FROM F/C GALLEY OVEN. REPLACED OVEN AND FOOD CARRIER. OPERATED NEW OVEN, CKS GOOD AND SMELL GONE. 2 L 7 2 4F RT A6WE 2001080300118 20010803 00118 NM 2001 8 3 DLM88011028 1 20010621 A 4970 B75A CHIP DETECTOR DOUG MD88 MD88 3023688 NM APU LEAKING A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 905DE 10077 53410 P80499 SHORTLY AFTER TAKEOFF, F/A REPORTED HAZE IN CABIN WITH ALL 3 SMOKE ALARMS GOING OFF. SMELLED LIKE BURNING SMELL. CAME OUT OF OVERHEAD DUCTING. RETURNED TO PHX. FOUND APU MAG CHIP DETECTOR LEAKING AND OIL INGESTED IN APU INTAKE. REPLAC ED CHIP DETECTOR AND PERFORMED DUCT BURN OUT PROCEDURE PER M/M 36-10-00-2. 2 L 7 2 4F RT A6WE 2001080300119 20010803 00119 NM 2001 8 3 DLM88011049 1 20010623 A 3350 0201991008 LIGHT DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 986DL 53313 03C EMERGENCY TRACK LIGHT INOP. REPLACED LIGHT ASSY 333201532, NOW TESTS OK. 2 L 7 2 4F RT A6WE 2001080300120 20010803 00120 NM 2001 8 3 DLM88011050 1 20010624 A 2421 976J2528 GENERATOR DOUG MD88 MD88 3023688 NM RT ENGINE FAILED A DALA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CL CLIMB 1 SO 27 962DL 49981 SHORTLY AFTER TAKEOFF AC CROSSTIE LOCKOUT MESSAGE ILLUMINATED. APPROXIMATELY 5 MINUTES LATER, RIGHT GEN OFF, RT AC BUS OFF AND RT DC OFF. REPLACED GENERATOR. 2 L 7 2 4F RT A6WE 2001080300121 20010803 00121 NM 2001 8 3 DLM88011059 1 20010625 A 7500 CLAMP DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE BROKEN A DALA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 909DE 29866 53418 725603 ON INITIAL APPROACH THE LEFT ENGINE FIRE WARNING BOTH A AND B LOOPS ILLUMINATED. WARNING CEASED WHEN THROTTLE PULLED BA CK TO IDLE. FOUND HIGH STAGE BLEED CLAMP BROKEN. REPLACED SAME. 2 L 7 2 4F 4 F RT A6WE E9NE 2001080300122 20010803 00122 NM 2001 8 3 DLM88011078 1 20010627 A 4990 38005041 APU DOUG MD88 MD88 3023688 NM APU BAY LEAKING A DALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 967DL 11175 53116 P80185 FLT ATTENDANTS SMELLED AN ELECTRICAL BURNING ODOR, A LITE HAZE ALSO APPEARED. AFT LAV SMOKE DETECTORS WERE INTERMITTENT LY SOUNDING FOR APPROX 2 MINUTES THEN WENT OFF COMPLETELY. PERFORMED OPN 5088. NO ELECTRICAL SMELL NOTED. REPL ACED APU DUE TO OIL LEAK REF ITEM 3. PERFORMED DUCT BURNOUT. REPLACED WATER SEPARATOR BAGS. RAN ENGS TO TAKEOFF POWER . NO SMELL OR HAZE NOTED. 2 L 7 2 4F RT A6WE 2001080300123 20010803 00123 NM 2001 8 3 DLM88011083 1 20010628 A 3510 MC1004101 OXYGEN MASK DOUG MD88 MD88 3023688 NM COCKPIT FAILED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 934DL 49721 RTG, CAPTS O2 MASK FAILED AND DEPLETED SYSTEM. REPLACED MASK AND SERVICED O2. 2 L 7 2 4F RT A6WE 2001080300124 20010803 00124 NM 2001 8 3 DLM88011092 1 20010629 A 2160 BOOT DOUG MD88 MD88 3023688 NM A/C BAY SPLIT A DALA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 SO 27 915DL 49546 TAIL COMP TEMP HIGH LIGHT CAME ON AT CLIMB PWR AT 22,000 FEET, ALSO MASTER WARNING. REPLACED BLOWN BOOT FROM CABIN TEMP CONTROL VALVE. 2 L 7 2 4F RT A6WE 2001080300125 20010803 00125 NM 2001 8 3 DLM88011106 1 20010703 A 2450 947F9463 CONTROL PANEL DOUG MD88 MD88 3023688 NM E/E BAY OVERHEATED A DALA D RETURN TO BLOCK B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 923DL 49705 RT A/C BUS OFF MSG PRIOR TO TAKEOFF WITH ACCOMPANYING AHRS 2 BASIC LIGHT. SLIGHT ODOR OF ELECTRICAL FUMES AFTER ATTEMPT AT POWER TRANSFER AT GATE. REPLACED AC BUS CONTROL PANEL. 2 L 7 2 4F RT A6WE 2001080300126 20010803 00126 NM 2001 8 3 DLM88011108 1 20010704 A 4910 INLET DOUG MD88 MD88 3023688 NM APU BAY CONTAMINATED A DALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 922DL 9982 49646 P80201 AFTER TAKEOFF, FLIGHT ATTENDANTS REPORTED SMOKE IN CABIN WITH MULTIPLE LEVEL SMOKE DETECTORS GOING OFF. IMMEDIATE LANDI NG AT JFK. FOUND OIL IN APU COMPT AND APU INLET AREA. CLEANED INLET, PERFORMED DUCT BURNOUT. 2 L 7 2 4F RT A6WE 2001080300127 20010803 00127 NM 2001 8 3 DLM88011115 1 20010704 A 3350 6011779 BATTERY PACK DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 998DL 53370 FOUND ON LAYOVER, AFT EXTERIOR EMERGENCY LIGHTS INOP. REPLACED OVERWING EXIT LIGHTS POWER SUPPLY AND BATTERY PACK PER M /M. OPS CHECK GOOD. 2 L 7 2 4F RT A6WE 2001080300129 20010803 00129 NM 2001 8 3 DLM88011169 1 20010714 A 3610 5953625521 DUCT DOUG MD88 MD88 3023688 NM A/C BAY CRACKED A DALA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 SO 27 962DL 49981 TAIL COMPARTMENT HIGH MESSAGE DURING CLIMB. FOUND CRACKED BLEED DUCT AT RIGHT ACM. REPLACED SAME. LEAK CHECKS GOOD. 2 L 7 2 4F RT A6WE 2001080300130 20010803 00130 NE 2001 8 3 DLM88011182 2 20010717 A 7230 SEAL DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE LEAKING A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 922DL 49646 AFTER TAKEOFF PASSING 3K FEET THE AFT RIGHT LAV SMOKE DETECTOR ACTIVATED. NO OTHER SIGN OF SMOKE OR FIRE DETECTED FROM CABIN CREW. CKD APU INLET, NTF. BOROSCOPED NR 1 ENGINE, FOUND EVIDENCE OF OIL LEAKING NR 3 SEAL AREA. REPLACED NR 1 E NGINE PER ROUTINE CARD DECK TRANS. 2 L 7 2 4F 4 F RT A6WE E9NE 2001080300131 20010803 00131 EU 2001 8 3 MALA010605 1 20010727 A 5270 SWITCH SAAB SF340 340B 7860101 EU STUCK A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 445XJ 340B445 During Flight # 2807, Cargo Door Warning light coming on after Takeoff. Air return to MSP. Maintenance found switch 7D D stuck at close position due to wrong adjustment re-adjusted switch 7DD and 19DD IAW SF340 MM Chap 52-70-15-4. All che cks good. 2 L 7 2 4T RT A52EU 2001080300132 20010803 00132 EU 2001 8 3 MALA010607 1 20010801 A 7330 216118216 BLEED BAND BAC 146 AVRO146RJ85A 1500097 EU DEFECTIVE A MALA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 GL 15 514XJ E2330 During Flight #3460, unable to attain over 81% N1, on #1 Engine. Air return to MSP. Maintenance removed and replaced # 1 Engine Bleed Band PN 2-161-182-16 IAW AMM 75-30-04. Leak and Ops check good. 2 H 7 4 4F RT A49EU 2001080300134 20010803 00134 NM 2001 8 3 DLM88011187 1 20010717 A 3350 RPS1 POWER SUPPLY DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 904DL 49535 EMERGENCY ESCAPE AISLE LIGHTS ROWS 24-38 INOP. REPLACED AFT EMERGENCY LIGHT POWER SUPPLY. 2 L 7 2 4F RT A6WE 2001080300135 20010803 00135 NM 2001 8 3 DLM88011188 1 20010718 A 2530 4110001137 COFFEEMAKER DOUG MD88 MD88 3023688 NM GALLEY MALFUNCTIONED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 909DE 53418 AFT GALLEY OUTBOARD COFFEEMAKER PRODUCED ELECTRICAL SMOKE. PULLED C/B. REPLACED DISPENSER. NEW UNIT CKS OK AND DOES N OT PRODUCE ANY ABNORMAL ODORS AFTER 30 MINS OPERATION. 2 L 7 2 4F RT A6WE 2001080300136 20010803 00136 NE 2001 8 3 DLM88011201 2 20010711 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 MALFUNCTIONED A DALA E ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 27 938DL 20505 49811 726865 AT 1000 FT AGL ENG ROLLED BACK TO 4-5 N1. NOISE AND VIBE WAS FELT THROUGH ENTIRE A/C. 2 MINS LATER WITH MINIMAL INDICA TIONS, OIL PRESSURE WAS LOST AND ENGINE WAS SHUTDOWN. ACFT ARRIVED AT DNTC WHERE NR 1 ENG WAS REMOVED AND REPLACED WITH ENG SERIAL 725998. 2 L 7 2 4F 4 F RT A6WE E9NE 2001080300150 20010803 00150 2001 8 3 DLM88011207 4 20010720 A 2216 D17751 TRIM MOTOR DOUG MD88 MD88 3023688 NM AUTOPILOT SYS FAULTY A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 977DL 53258 A/P C/BS POPPED. A/P TRIM LIGHT ILLUM. A/P TRIM INOP. RESET C/BS. D11 POPPED 2ND TIME. PRIMARY TRIM FUNCTIONED ENTI RE TIME. REPLACED ALTERNATE STABILIZER TRIM MOTOR PER M/M. PERFORM RTS TEST ON BOTH DFGCS. BOTH PASS/GO. STAB TRIM N OW OPS NORMAL. 2 L 7 2 4F RT A6WE 2001080300151 20010803 00151 NM 2001 8 3 DLM88011213 1 20010722 A 3350 023071BPEGPL LIGHT DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 960DL 49979 EMERGENCY LIGHT INOP AT SEAT 25. RELAMPED PER M/M, CHECKS NORMAL. 2 L 7 2 4F RT A6WE 2001080300152 20010803 00152 NM 2001 8 3 DLM88011214 1 20010721 A 2910 7936913563 HYDRAULIC LINE DOUG MD88 MD88 3023688 NM HYDRAULIC SYS LEAKING A DALA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 27 917DL 49573 RT ENG HYD PUMP PRESS LINE LEAKING IN AFT BAG BIN BEHIND RT AFT BULKHEAD. INSTALLED NEW HYD LINE, RAN NR 2 ENG PER PFHB . NO LEAKS, ALL CHECKS NORMAL PER M/M. 2 L 7 2 4F RT A6WE 2001080300153 20010803 00153 NM 2001 8 3 DLM88011233 1 20010725 A 7830 CONTROL VALVE DOUG MD88 MD88 3023688 NM THRUST REVERSER LEAKING A DALA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 913DE 49956 AFTER 2 HOURS IN CRUISE HYDRAULIC QTY WAS 4. TURNED OFF LT PUMP QTY INDICATED 7-16. USED LT PUMP FOR APPROACH. AFTER BALANCING HYD QTY DECREASE TO 2. FOUND LT T/R CONTROL VLV LEAKING AT B-NUT. TIGHTENED SAME. 2 L 7 2 4F RT A6WE 2001080300154 20010803 00154 NM 2001 8 3 DLM90010974 1 20010614 A 3350 07912 LENS DOUG MD90 MD9030 3023690 NM CABIN DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 PAX SEAT 3C EMERGENCY LIGHT DAMAGED. REPLACED LENS AND LIGHT BULB. 2 L 7 2 4F RT A6WE 2001080300155 20010803 00155 NM 2001 8 3 DLM90011069 1 20010626 A 4940 STARTER DOUG MD90 MD9030 3023690 NM APU MALFUNCTIONED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 904DA 6930 53384 P1049 ON APU START ATTEMPT AT THE GATE IN SNA. SMOKE WAS OBSERVED COMING FROM APU COMPARTMENT. MTC OPENED COMPT AND OBSERVED THE STARTER GLOWING RED. FIRE DEPT DISCHARGED HALON INTO COMPT. CTC MTC ADVISED THERE WERE FLAMES INITIALLY WHEN DOOR WAS OPENED. REPLACED APU. 2 L 7 2 4F RT A6WE 2001080300156 20010803 00156 NM 2001 8 3 DLM90011079 1 20010627 A 5312 9953015507 BULKHEAD DOUG MD90 MD9030 3023690 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 914DN 53394 THE FS 1520 CANTED BULKHEAD WEB WAS FOUND CRACKED ALONG THE WEB SPLICE JOGGLE LINES AT STRINGER 8L AND 8R. THE CRACKED SECTIONS OF WEB WERE CUTOUT TO REMOVE THE DAMAGE. THE WEB AND SPLICE WERE RESTORED BY THE INSTALLATION OF 2 ALUMINUM R EPAIR DOUBLERS AT EACH LOCATION PER ER/A 381189-14, REV A. 2 L 7 2 4F RT A6WE 2001080300157 20010803 00157 NM 2001 8 3 DLM90011114 1 20010704 A 2421 28B5278 GENERATOR DOUG MD90 MD9030 3023690 NM NR 1 ENGINE MAKING METAL A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SO 27 904DA 53384 LT AC FAULT MSG IN FLT, LT GEN OIL FILTER STATUS MSG. FOUND METAL IN GEN FILTER. REPLACED GEN, OP CHECKS OK. 2 L 7 2 4F RT A6WE 2001080300158 20010803 00158 NM 2001 8 3 DLM90011127 1 20010706 A 2121 6459401 FAN DOUG MD90 MD9030 3023690 NM CABIN MALFUNCTIONED A DALA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DE DESCENT 1 SO 27 912DN 53392 WHEN THROTTLES WERE RETARDED AT APPROX 16K RT PNEU SYS FAULT LIGHT ILLUMINATED ON OAP. POM PROCEDURES COMPLIED WITH NO EFFECT. ACCOMPANIED BY F/A REPORT OF A BURNING ELECTRICAL SMELL IN AFT CABIN AREA. REPLACED RECIRC FAN. 2 L 7 2 4F RT A6WE 2001080300161 20010803 00161 NM 2001 8 3 DLM90011132 1 20010708 A 3222 MS288892 VALVE DOUG MD90 MD9030 3023690 NM NLG STRUT LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 905DA 53385 NOSE GEAR WOULD NOT RETRACT. FOUND SERVICING VALVE ON STRUT LEAKING. REPLACED SAME. 2 L 7 2 4F RT A6WE 2001080300164 20010803 00164 NM 2001 8 3 DLM90011224 1 20010724 A 3350 RPS1B POWER SUPPLY DOUG MD90 MD9030 3023690 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 901DA 53381 EMERGENCY PATH LIGHTS FROM SEAT 34 AFT INOP. REPLACED POWER SUPPLY, CKS GOOD. 2 L 7 2 4F RT A6WE 2001080300169 20010803 00169 NE 2001 8 3 HNAA0100035 3 20010608 A 6111 SFA13S1ROA SKIN DHAV DHC8 DHC8311 1386006 EA HAMSTD 14SF 14SF15 NE NR 2 PROP DEPARTED A HNAA K NONE D E INFLIGHT SEPARATION VIBRATION/BUFFET AP APPROACH 1 EA 07 327EN 8274 426 261 910233 ON APPROACH AT 200 FEET, CREW AND FLIGHT ATTENDANT HEARD A LOUD BANG FOLLOWED BY AIRFRAME VIBRATION FELT THROUGHOUT THE CABIN AND FLIGHT DECK. FOUND NUMBER TWO PROP, NUMBER ONE BLADE MISSING THE NICKLE SHEATH. REMOVED AND REPLACED PROP BL ADE. 2 H 7 2 4T RT A13NM 6 C P7NE 2001080300172 20010803 00172 WP 2001 8 3 IXXA0100027 1 20010315 A 5230 PAN DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 79927 2852 46065 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE LOWER C-PIT CARGO DOOR FORWARD DOOR PAN. REPAIR ACCOMPLI SHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION A NEW DOOR PAN IN ACCORDANCE WITH DACO DRAWING 5704349 AN D ENGINEERING ORDER 52-DC8-1781. 2 L 7 4 4F RT 4A25 2001080300179 20010803 00179 WP 2001 8 3 IXXA0100033 1 20010320 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 79927 2852 46065 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE EXTERNAL PLATING AFT OF THE L-1 DOOR LOWER AFT CORNER. 2 L 7 4 4F RT 4A25 2001080300181 20010803 00181 WP 2001 8 3 IXXA0100038 1 20010705 A 3230 UPLOCK DOUG DC8 DC862 3021970 WP RT MLG LACK OF LUBE A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 728PL 80195 954 45918 EN ROUTE FROM HIK TO SUU, THE LANDING GEAR NOT LATCH LIGHT ILLUMINATED DURING THE LANDING GEAR UPLATCH CHECK. THE FLIGH T CREW CYCLED THE LANDING GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO SUU FOR AN UNEVENT FUL LANDING. MAINTENANCE INSPECT THE LANDING GEAR WHICH REVEALED THE RIGHT MAIN GEAR UPLATCH MECHANISM LACKING LUBRICAT ION. MAINTENANCE CLEANED AND LUBRICATION THE UPLATCH MECHANISM, PERFORMED A SUCCESSFUL OPERATIONAL CHECK IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2001080300200 20010803 00200 EU 2001 8 3 MALA010510 1 20010524 A 2421 31342043 GENERATOR SAAB SF340 340B 7860101 EU LT ENGINE DEFECTIVE A MALA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 15 450XJ 450 DURING FLIGHT 2772, BGM/DTW THE LT AC GENERATOR FAILED ON ARRIVAL INTO DTW. AC GEN STARTED TO SMOKE AND SPARK ON APPROA CH. DECLARED AN EMERGENCY, SHUTDOWN ENGINE ON THE GROUND IN DTW. MX REPLACED LT AC GEN P/N 31342-043, S/N ON 96023. R EPLACED THE AC GCU P/N 51634-002, S/N ON 96026. FOUND LT PGB DAMAGED DURING LT AC GEN CHANGE, MX REPLACED LT ENGINE P/ N CT7-9B S/N ON GE-E785121, REPLACED LT PGB P/N 5074T51610, S/N ON IHI00461. DURING ENGINE CHANGE NOTED BACKSHELL OF CO NNECTOR 1XAP1 FOR LT AC GEN DAMAGED, MX PERFORMED TEMPORARY REPAIR OF CONNECTOR AND ASSOCIATED GROUNDING HARNESS. 2 L 7 2 4T RT A52EU 2001080300201 20010803 00201 2001 8 3 MALA010511 4 20010604 A 3451 6226263001 TRANSCEIVER SAAB SF340 340B 7860101 EU COCKPIT DEFECTIVE A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 444XJ 444 DURING FLIGHT NR 2804 OUT OF DTW, DME DISPLAY ASSOCIATED WITH NR 1 NAV RADIO, DISPLAYED ON LOWER EFIS TUBE-LOWER LEFT CO RNER OF TUBE, IS INOPERATIVE. DME DISPLAY ASSOCIATED WITH NR 2 NAV RADIO DISPLAYS NORMALLY. DME DISPLAY FOR NR 1 NAV R ADIO FUNCTIONS AND DISPLAYS NORMALLY ON GROUND. MAINTENANCE REPLACED DME XCVR P/N ON 622-6263-001, S/N ON 4664, P/N OFF 622-6263-003, S/N OFF 1891. MAINTENANCE FOUND CHAFED WIRE AT CONNECTOR TO DISTANCE DATA ADAPTER. REPAIRED WIRE IAW SF 340 MM, CHAP 20 AND DME CHECKS GOOD IAW SF340 MM 34-53-00. 2 L 7 2 4T RT A52EU 2001080300202 20010803 00202 EU 2001 8 3 MALA010512 1 20010606 A 3020 447301 MODULE SAAB SF340 SF340A 7850100 EU DE-ICE SYS FAULTY A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 119XJ 119 OUTBOUND OF DTW, THE LT AND RT INTAKE HEAT LIGHTS WOULD ILLUMINATE ON FLIGHT 2984. MAINTENANCE REPLACED DE-ICE PANEL P/ N 7239042-503, S/N ON FFV989 AND WEU P/N 006WS00. MAINTENANCE REPLACED THE LT DE-ICE MODULE P/N 44730-1, S/N OFF A00061 , S/N ON A00462. RAN AC FOR 30 MINUTES NO FAULTS ILLUMINATED ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2001080300203 20010803 00203 2001 8 3 MALA010513 4 20010608 A 3425 COMPUTER SAAB SF340 340B 7860101 EU COCKPIT FAULTY A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 454XJ 454 DURING FLIGHT 3266 OUT OF DTW, NR 2 AHRS INTERMITTENT IN FLIGHT. FLICKERS AND GIVES ATT AND HEADING COMPARATORS. MAINT ENANCE REPLACED NR 2 AHRS COMPUTER. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2001080300204 20010803 00204 EU 2001 8 3 MALA010515 1 20010610 A 5610 7256100501 WINDSHIELD SAAB SF340 340B 7860101 EU COCKPIT CRACKED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 454XJ 454 ON DEPARTURE LT FRONT WINDSHIELD LIGHT ILLUMINATED AND TWO MINUTES LATER THE WINDSHIELD CRACKED. AIR TURNBACK TO BGM. MAINTENANCE REPLACED LT FRONT WINDSHIELD IAW SF-340, AMM CHAPTER 56-10-05-4. 2 L 7 2 4T RT A52EU 2001080300205 20010803 00205 EU 2001 8 3 MALA010516 1 20010614 A 7931 CONNECTOR SAAB SF340 SF340A 7850100 EU LT ENGINE LOOSE A MALA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 GL 15 41XJ 340A041 ON DESCENT TO LNK LEFT ENGINE OIL PRESSURE DROPPED TO ZERO AND CWP LIGHT ILLUMINATED. A ACCOMPLISHED QRH CHECKLIST AND MADE A PRECAUTIONARY SHUTDOWN OF LEFT ENGINE. MAINTENANCE INSPECTED LT ENGINE FOUND OIL QUANTITY AT NORMAL LEVEL. RESE CURED CANNON PLUG AT TRANSMITTER. RAN ENGINE OIL PRESSURE IN NORMAL. OPS CHECK GOOD OF OIL PRESSURE INDICATION. 2 L 7 2 4T RT A52EU 2001080300206 20010803 00206 EU 2001 8 3 MALA010518 1 20010531 A 2730 7227705644 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 434XJ 434 DURING 4K-CHECK IN CWA, LT I/B CABIN ELEVATOR CABLE CHAFED. MAINTENANCE REPLACED LT I/B ELEVATOR CABLE P/N 7227705-644 IAW SAAB AMM 27-31-15. SEE 409 NR 125174 FOR RIG AND TRAVEL CHECKS. 2 L 7 2 4T RT A52EU 2001080300207 20010803 00207 EU 2001 8 3 MALA010519 1 20010601 A 2720 7227105582 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 434XJ 434 FOUND DURING 4K-CHECK IN CWA, RT AFT SINGLE RUDDER CABLE IN CIRCUIT I IS CHAFED. MAINTENANCE REPLACED RT AFT SINGLE RUD DER CABLE IN CIRCUIT I P/N 7227105-582 IAW SAAB AMM 27-21-25. SEE 409 CARD 125176 FOR RIGGING AND TRAVEL CHECKS. 2 L 7 2 4T RT A52EU 2001101900021 20011019 00021 NM 2001 10 19 DHL2001746001 1 20010801 A 5752 TAB BOEING 727 727224 1384076 NM AILERON DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 LT O/B AILERON LWR SURFACE 2 AREAS DELAMINATED. AREA OF DELAMINATION LT O/B AILERON TRIM TAB & NOT THE AILERON ITSELF. REMOVED AND REPLACED LT O/B AILERON BAL TAB. OPS CHECKED SERVICEABLE. 2 L 7 3 4F A3WE 2001080300208 20010803 00208 EU 2001 8 3 MALA010520 1 20010601 A 2730 7227105712 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 434XJ 434 FOUND DURING 4K-CHECK IN CWA, LT O/B ELEVATOR CABLE IN CABIN IS CHAFED. MAINTENANCE REPLACED LT O/B ELEVATOR CABLE P/N 7227105-712 IAW SAAB AMM 27-31-15. SEE 409 CARD 125174 FOR RIG AND TRAVEL CHECKS. 2 L 7 2 4T RT A52EU 2001080300209 20010803 00209 EU 2001 8 3 MALA010521 1 20010531 A 2730 7227105712 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 434XJ 434 FOUND DURING 4K-CHECK IN CWA, RT O/B ELEVATOR CABLE IN CABIN IS CHAFED. MAINTENANCE REPLACED RT O/B ELEVATOR CABLE IN C ABIN P/N 7227105-712 IAW SF3 AMM 27-31-15. 2 L 7 2 4T RT A52EU 2001080300210 20010803 00210 EU 2001 8 3 MALA010522 1 20010601 A 2720 7227105562 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 434XJ 434 FOUND DURING 4K-CHECK IN CWA, RT O/B RUDDER CABLE IN CIRCUIT I IS CHAFED. MAINTENANCE REPLACED RT O/B RUDDER CABLE IN C IRCUIT I P/N 7227105-562 IAW SAAB AMM 27-21-25. 2 L 7 2 4T RT A52EU 2001080300211 20010803 00211 EU 2001 8 3 MALA010523 1 20010601 A 2710 7227151522 CONTROL CABLE SAAB SF340 340B 7860101 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 434XJ 434 FOUND DURING 4K-CHECK IN CWA, RT O/B AILERON WING CABLE CHAFED. MAINTENANCE REPLACED RT O/B FWD AILERON WING CABLE P/N 7227151-522 IAW SAAB AMM 27-11-25. 2 L 7 2 4T RT A52EU 2001080300212 20010803 00212 EU 2001 8 3 MALA010524 1 20010601 A 2730 7227705644 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 434XJ 434 FOUND DURING 4K-CHECK IN CWA, RT I/B ELEVATOR CABLE IN CABIN IS CHAFED. MAINTENANCE REPLACED RT I/B ELEVATOR CABLE IN C ABIN P/N 7227705-644, IAW SR3 AMM 27-31-15. 2 L 7 2 4T RT A52EU 2001080300213 20010803 00213 EU 2001 8 3 MALA010525 1 20010601 A 2720 7227105582 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 434XJ 434 FOUND DURING 4K-CHECK IN CWA, LT AFT RUDDER CABLE CIRCUIT I IS CHAFED. MAINTENANCE REPLACED LT AFT RUDDER CABLE CIRCUIT I P/N 7227105-582, IAW SF3 AMM 27-21-25. 2 L 7 2 4T RT A52EU 2001080300214 20010803 00214 EU 2001 8 3 MALA010526 1 20010601 A 2720 7227105562 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 434XJ 434 FOUND DURING 4K-CHECK IN CWA, LT O/B RUDDER CABLE IN DUAL CIRCUIT I IS CHAFED. MAINTENANCE REPLACED LT O/B RUDDER CABLE IN DUAL CIRCUIT I P/N 7227105-562 IAW SF3 AMM 27-21-25. 2 L 7 2 4T RT A52EU 2001080300215 20010803 00215 EU 2001 8 3 MALA010527 1 20010601 A 2710 7227105613 CONTROL CABLE SAAB SF340 340B 7860101 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 434XJ 434 FOUND DURING 4K-CHECK IN CWA, LT O/B FWD AILERON CABLE CHAFED AFT OF STA 294. MAINTENANCE REMOVED AND REPLACED LT O/B F WD AILERON CABLE P/N 7227105-613 IAW SAAB AMM 27-11-25. 2 L 7 2 4T RT A52EU 2001080300217 20010803 00217 EU 2001 8 3 MALA010528 1 20010601 A 2710 7227105624 CONTROL CABLE SAAB SF340 340B 7860101 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 434XJ 434 FOUND DURING 4K-CHECK IN CWA, RHOB FWD CABIN AILERON CABLE CHAFED AFT OF STA 294. MAINTENANCE REPLACED RHOB FWD CABIN A ILERON CABLE P/N 7227105-624 IAW SAAB AMM 27-11-25. 2 L 7 2 4T RT A52EU 2001080300218 20010803 00218 EU 2001 8 3 MALA010529 1 20010601 A 2710 7227105614 CONTROL CABLE SAAB SF340 340B 7860101 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 434XJ 434 FOUND DURING 4K-CHECK IN CWA, RHIB FWD CABIN AILERON CABLE CHAFED (FORWARD OF WING BOX). MAINTENANCE REMOVED AND REPLAC ED RHIB FWD CABIN AILERON CABLE P/N 7227105-614 IAW SAAB AMM 27-11-25. 2 L 7 2 4T RT A52EU 2001080300221 20010803 00221 EU 2001 8 3 MALA010530 1 20010601 A 2710 7227105623 CONTROL CABLE SAAB SF340 340B 7860101 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 434XJ 434 FOUND DURING 4K-CHECK IN CWA, LHIB FWD CABIN CABLE CHAFED (FORWARD OF WING BOX). MAINTENANCE REMOVED AND REPLACED LHIB FWD CABIN AILERON CABLE P/N 7227105-623 IAW SAAB AMM 27-11-25. 2 L 7 2 4T RT A52EU 2001080300223 20010803 00223 EU 2001 8 3 MALA010531 1 20010604 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 434XJ 434 FOUND DURING 4K-CHECK IN CWA, LT CENTER AISLE SEAT TRACK LBL 18.3 IB FLOOR BOARD FLANGE CORROSION AT APPROXIMATELY STA 6 65. 2 L 7 2 4T RT A52EU 2001080300224 20010803 00224 EU 2001 8 3 MALA010532 1 20010604 A 5320 7253721439 WEB SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 434XJ 434 FOUND DURING 4K-CHECK IN CWA, WEBBING BETWEEN STA 288 AND 294 HAS CORROSION. 2 L 7 2 4T RT A52EU 2001080300225 20010803 00225 EU 2001 8 3 MALA010533 1 20010605 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 434XJ 434 FOUND DURING 4K-CHECK IN CWA, RT CENTER AISLE SEAT TRACK BL 0 HAS DEEP CORROSION ON I/B SIDE WALL BETWEEN APPROXIMATELY STA 632-645.5. 2 L 7 2 4T RT A52EU 2001080300226 20010803 00226 EU 2001 8 3 MALA010534 1 20010606 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 434XJ 434 FOUND DURING 4K-CHECK IN CWA, LT CENTER AISLE SEAT TRACK LBL 18.3 HAS HEAVY CORROSION AT STA 294-378. 2 L 7 2 4T RT A52EU 2001080300227 20010803 00227 EU 2001 8 3 MALA010535 1 20010606 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 434XJ 434 FOUND DURING 4K-CHECK IN CWA, RT CENTER AISLE SEAT TRACK BL 0 FWD PORTION HAS HEAVY CORROSION STARTING AT STA 294. 2 L 7 2 4T RT A52EU 2001080300228 20010803 00228 NE 2001 8 3 MALA010537 2 20010616 A 7321 6071T20P16 CONTROL UNIT SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 441XJ 340B441 AFTER TAKEOFF IN DTW, FLIGHT 3250, RT PROP RPM DROPPED TO ZERO. RESET C/B R6 RIGHT PROP SPEED, NEEDLE FLUCTUATED BUT RE MAINED AT ZERO. AFTER APPROXIMATELY 10 MINUTES, RIGHT PROP SPEED RETURNED TO NORMAL, BUT INTERMITTENTLY DROPPED TO ZERO AND BACK AGAIN TO NORMAL. MAINTENANCE REPLACED RT DECU IAW AMM 2CT7 MM. P/N 6071T20P16, SN/OFF LMDT2106, SN/ON LMDT21 59. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2001080300230 20010803 00230 EU 2001 8 3 MALA010538 1 20010618 A 2913 521449 PUMP BAC 146 AVRO146RJ85A 1500097 EU HYDRAULIC SYS MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 533XJ E2367 DURING FLIGHT 3685 FROM MEM, THE GREEN HYDRAULIC HI TEMP CAUTION LIGHT ILLUMINATED. FOLLOWED QRH, AIR RETURN TO DTW. M AINTENANCE REPLACED NR 3 EDP IAW AMM 29-10-17 (201). OPS CHECK GOOD. P/N ON AND OFF 521449, S/N ON MX639940, S/N OFF M X619638. REPLACED GREEN HYDRAULIC TEMP SWITCH IAW AMM 29-33-11. OPS AND LEAK CHECK GOOD. P/N HE83273-1, S/N ON 1364TW , S/N OFF 1368TW. 2 H 7 4 4F RT A49EU 2001080300233 20010803 00233 NM 2001 8 3 SWAA011941 1 20010707 A 5312 6517582 BULKHEAD BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17.1, WL 180. REPAIRED WEB PER SWA RA. 2 L 7 2 4F RT A16WE 2001080300234 20010803 00234 NM 2001 8 3 SWAA011943 1 20010628 A 5315 6546804 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 521SW 25320 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 312, WL 208. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2001080300235 20010803 00235 NM 2001 8 3 SWAA011976 1 20010712 A 5311 6517583 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL CHORD CRACKED AT BS 178, LBL 5.7 & WL 184. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2001080300236 20010803 00236 NM 2001 8 3 SWAA011978 1 20010706 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 633SW 27936 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 308, LBL 11 TO LBL 19. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2001080300237 20010803 00237 NM 2001 8 3 SWAA011980 1 20010712 A 5320 6517582 BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL BEAM WEB CRACKED .125 IN AT BS 180, LBL 5.7 & WL 180. REPAIRED WEB PER SWA RA. 2 L 7 2 4F RT A16WE 2001080300238 20010803 00238 NM 2001 8 3 SWAA011990 1 20010703 A 5320 6551698 SPLICE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2001080300239 20010803 00239 NM 2001 8 3 SWAA011997 1 20010708 A 5314 65621257 KEELBEAM BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM CORRODED AT BS 520, STR 28L. REPAIRED KEEL BEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2001080300240 20010803 00240 NM 2001 8 3 SWAA011999 1 20010715 A 2750 65C27503 TRANSMISSION BOEING 737 7373H4 1384600 NM T/E FLAP FAILED A SWAA K NONE F FLT CONT AFFECTED NR NOT REPORTED 1 SW 07 613SW 27931 DURING SCHEDULED SPECIAL VISIT CHECK DUE TO NR 3 T/E FLAP TRANSMISSION FAILURE, (MX FERRY TO DAL). REMOVED AND REPLACED LT INBD AFT FLAP, LT INBD FORE FLAP. REMOVED AND REPLACED LT WING BODY FAIRING, REMOVED AND REPLACED CRACKED LT INBD M ID FLAP FAIRING ATTACH PLATE, REPAIRED LT WING TO BODY FAIRING AFT SUPPORT FRAME PER SWA RA & MM. 2 L 7 2 4F RT A16WE 2001080300241 20010803 00241 NM 2001 8 3 SWAA012009 1 20010706 A 5320 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED 2 EA AT BS 559, STR 11R & BS 767, STR 22R. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001080300242 20010803 00242 NM 2001 8 3 SWAA012028 1 20010703 A 5320 6551698 SPLICE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2001080300243 20010803 00243 NM 2001 8 3 SWAA012037 1 20010715 A 5311 BAC5602 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D-CHECK, FOUND Z-FRAMES CRACKED AT BS 807 & BS 867, STR 9L. REPAIRED Z-FRAMES PER SRM. 2 L 7 2 4F RT A16WE 2001080300244 20010803 00244 2001 8 3 SWAA012049 4 20010712 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM EVAC SLIDE MISROUTED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 378SW 26585 DURING SCHEDULED 1/4D CHECK, FOUND BOTH AFT DOOR EMERGENCY EVAC SLIDE LATCH ASSY CABLES MISROUTED. REROUTED CABLES PER MM. 2 L 7 2 4F RT A16WE 2001080300245 20010803 00245 2001 8 3 SWAA012067 4 20010723 A 2565 D31354 SLIDE BOEING 737 7377H4 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 764SW 27878 FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001080300246 20010803 00246 NM 2001 8 3 SWAA012068 1 20010723 A 3350 6574550 LIGHT BOEING 737 7377H4 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 714CB 27848 EEPLS INOP AND MISSING COVER AT ROW 13. REMOVED AND REPLACED EEPLS LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001080300247 20010803 00247 NM 2001 8 3 SWAA012072 1 20010722 A 3350 300432 LIGHT BOEING 737 7372H4 138448C NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 068SW 22357 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT FWD SERVICE DOOR EXTERIOR. RELAMPED EXIT LIGHT PER M M. 2 L 7 2 4F A16WE 2001080300248 20010803 00248 2001 8 3 SWAA012073 4 20010722 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 074SW 22674 DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER M M. 2 L 7 2 4F A16WE 2001080300249 20010803 00249 NM 2001 8 3 SWAA012076 1 20010724 A 3350 BR2013 LIGHT BOEING 737 7372T4 1384492 NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 EEPLS DAMAGED AT ROW 1. REPAIRED EEPLS PER MM. 2 L 7 2 4F A16WE 2001080300250 20010803 00250 NM 2001 8 3 SWAA012077 1 20010723 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 EEPLS LOOSE AT ROW 11. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001080300251 20010803 00251 NM 2001 8 3 SWAA012079 1 20010723 A 3350 BR2013 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 641SW 27714 EEPLS LOOSE AND COVER MISSING AT OVERWING EXIT. INSTALLED COVER AND SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001080300252 20010803 00252 NM 2001 8 3 SWAA012080 1 20010724 A 3350 20131A BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT AFT CABIN. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2001080300253 20010803 00253 2001 8 3 SWAA012081 4 20010724 A 2565 1061323 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 387SW 26602 DURING SCHEDULED RON CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001080300254 20010803 00254 2001 8 3 SWAA012082 4 20010723 A 2565 61323468 SLIDE BOEING 737 7375H4 138449D NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 502SW 24179 FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001080300256 20010803 00256 2001 8 3 SWAA012083 4 20010723 A 2565 D31354 SLIDE BOEING 737 7373G7 1384595 NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 683SW 24008 DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUSTMENT. ADJUSTED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001080300257 20010803 00257 NM 2001 8 3 SWAA012085 1 20010724 A 5315 6546804 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 663, BL 0. REMOVED AND REPLACED CHORD PER SWA AC O. 2 L 7 2 4F A16WE 2001080300258 20010803 00258 NM 2001 8 3 SWAA012086 1 20010718 A 5320 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 19R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001080300262 20010803 00262 NM 2001 8 3 SWAA012089 1 20010725 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM ENTRY DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 074SW 22674 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT PER MM. 2 L 7 2 4F A16WE 2001080300263 20010803 00263 NM 2001 8 3 SWAA012090 1 20010724 A 3350 BR2013 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED C4 CHECK, FOUND EEPLS LOOSE, MISSING LENS AND INOP AT ROW 18. REMOVED AND REPLACED EEPLS ASSY PER MM. 2 L 7 2 4F A16WE 2001080300264 20010803 00264 NM 2001 8 3 SWAA012091 1 20010725 A 3350 90083 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD EMERGENCY LIGHT INOP AT AFT CABIN. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2001080300265 20010803 00265 NM 2001 8 3 SWAA012093 1 20010719 A 5320 6551698 SPLICE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2001080300266 20010803 00266 NM 2001 8 3 SWAA012094 1 20010720 A 5315 6546804 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D-CHECK, FOUND UPPER FLOORBEAM CHORD CORRODED AT BS 328, BETWEEN RBL 0-65, WL 208. REPAIRED FLOORBEAM CHORD PER SRM. 2 L 7 2 4F RT A16WE 2001080300267 20010803 00267 2001 8 3 SWAA012096 4 20010725 A 2565 61621 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 376SW 26584 AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY TORN AND FRAYED. REMOVED AND REPLACED EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001080300268 20010803 00268 NM 2001 8 3 SWAA012100 1 20010726 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 639SW 27712 EEPLS TRACK COVER LOOSE AT ROW 18. REMOVED AND REPLACED EEPLS TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001080300269 20010803 00269 NM 2001 8 3 SWAA012101 1 20010726 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 710SW 27844 EEPLS TRACK COVER BROKEN AT ROW 3. REMOVED AND REPLACED EEPLS FLOOR TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2001080300270 20010803 00270 NM 2001 8 3 SWAA012102 1 20010725 A 3350 6551698 SPLICE BOEING 737 7377H4 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 750SA 29802 DURING SCHEDULED D-CHECK, FOUND STR SPLICE CRACKS AT BS 360, STR 4L & BS 907, STR 4R. REMOVED AND REPLACED STR SPLICES PER SRM. 2 L 7 2 4F RT A16WE 2001080300271 20010803 00271 NM 2001 8 3 SWAA012104 1 20010726 A 5315 6546804 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 312, BETWEEN LBL 12 & RBL 12. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2001080300272 20010803 00272 NM 2001 8 3 UPS01436451 1 20010718 A 5310 DOUBLER BOEING 747 747200 NM R4 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 1 INSPECTION TYPE:C M/D- R4 DOOR FWD CUTOUT BTN STR 24 X 25 CUTOUT CRK. FABRICATED / REPAIRED / INSTALLED DOUBLERS PER SRM 53-10-04 FIG 84. 2 L 7 4 4F RT A20WE 2001080300273 20010803 00273 NM 2001 8 3 UPS01436454 1 20010721 A 5310 65B0765834 STRINGER BOEING 747 747200 NM BS 280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 1 INSPECTION TYPE:C NOSE - W/W TUNNEL BS 280 STR 41R STRINGER FOUND CRACKED. NOSE W/W TUNNEL BS 280 STR 41R REPLACXED AS PER SRM 51-10-01 2 L 7 4 4F RT A20WE 2001080300274 20010803 00274 NM 2001 8 3 UPS01436485 1 20010723 A 5330 654U60751635 FITTING BOEING 747 747200 NM R1 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 1 INSPECTION TYPE:C M/D - R1 DOOR, DOOR AFT CUTOUT MOST LOWER STOP FITTING CRK. R1 DOOR AFT CUTOUT MOST LOWER STOP FIT TING REPLACED AND DR STOP ADJUSTMENT AS PER MM 52-11-01, LOW GATE ASSY INSTALLATION AND RIGGING PER MM 52-09-00 AND SRM 51-10-01 2 L 7 4 4F RT A20WE 2001080300275 20010803 00275 EU 2001 8 3 SIMA200114401 1 20010524 A 7600 531704 CONTROLLER SAAB SF340 340B 7860101 EU COCKPIT FAILED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 283AE 340B283 ALB - FLT 4891 - CONFIG WARNING LIGHT ON TAKEOFF. REMOVED AND REPLACED CONTROL QUADRANT IAW SAAB AMM 76-10-05. OPS CHE CK GOOD. (M) 2 L 7 2 4T RT A52EU 2001080300276 20010803 00276 EU 2001 8 3 SIMA200114406 1 20010524 A 7600 531704 CONTROLLER SAAB SF340 340B 7860101 EU COCKPIT FAILED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 283AE 340B283 ALB - FLT 4891 - CREW REPORTED A CONFIGURE LIGHT DURING TAKEOFF. MAINTENANCE REMOVED AND REPLACED THE CONTROL QUADRANT ASSEMBLY IAW SAAB MM 76-10-05. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001080300277 20010803 00277 EU 2001 8 3 SIMA200114905 1 20010529 A 3350 LIGHT AEROSP ATR72 ATR72212 EU CABIN MALFUNCTIONED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 274AT 274 MIA - FLT 5363 - CREW REPORTED THE EMERGENCY LIGHTS STAY ON WITH ENGINES RUNNING AND EMERGENCY LIGHT SWITCH IN THE ARM P OSITION. MAINTENANCE RESET THE EMERGENCY LIGHT BREAKER AND OPS CHECK WAS GOOD. NO OTHER DEFECTS NOTED AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001080300278 20010803 00278 SO 2001 8 3 SIMA200119301 1 20010712 A 3350 7287580 LIGHT EMB 145 EMB145LR SO CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 631AE 145139 MSN - FLT 4044 - DURING PRE-FLIGHT INSPECTION, CREW REPORTED THE AFT FLOOR PROXIMITY EMERGENCY LIGHTS DID NOT ILLUMINATE . MAINTENANCE REPLACED THE AFT LIGHT STRIP IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE . (M) 2 L 7 2 4T RT T00011AT 2001080300279 20010803 00279 SO 2001 8 3 SIMA200119802 1 20010717 A 3350 7281103507 MODULE EMB 145 EMB145LR SO CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 614AE 145086 TOL - FLT 4350 - CREW REPORTED THE CABIN EMERGENCY LIGHTS NOT CONTROLLABLE FROM THE FLIGHT ATTENDANTS PANEL. MAINTENANC E REMOVED AND REPLACED THE FLIGHT ATTENDANTS LIGHTING CONTROL MODULE IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RE TURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001080300280 20010803 00280 SO 2001 8 3 SIMA200119913 1 20010718 A 3240 0132AFU1 SENSOR EMB 145 EMB145LR SO BRAKE SYS FAULTY A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 628AE 145124 LBB - FLT 3668 - ABORTED TAKEOFF, NR 1 BRAKE TEMP INDICATOR FLUCTUATED. REMOVED AND REPLACED NR 1 BRAKE TEMP SENSOR IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT T00011AT 2001080300281 20010803 00281 NM 2001 8 3 UHLA003593 1 20010618 A 3260 864202 TARGET DHAV DHC8 DHC8* NM NLG OUT OF ADJ A UHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NE 03 803SA 20265 221 FLT 208 - TTN-BED, ON TAKEOFF, NOSE GEAR WOULD NOT RETRACT. CREW RETURNED TO THE FIELD. MAINTENANCE ADJUSTED NOSE GEAR TARGET, CLEANED AND LUBED RETRACTION ACTUATOR. OPS CHECKED NOSE GEAR SEVERAL TIMES, NO DEFECTS NOTED. AIRCRAFT RELEAS ED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 2001080300282 20010803 00282 NM 2001 8 3 UHLA003599 1 20010619 A 3297 WIRE DHAV DHC8 DHC8* NM NLG WW BROKEN A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NE 03 803SA 20273 221 FLT 212 - TTN-BED - AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT. CREW RETURNED TO FIELD AND AIRCRAFT FERRIED TO BUF. MA INTENANCE FOUND BROKEN WIRING IN NOSE GEAR DOWNLOCK SENSOR HARNESS. REPAIRED AND REROUTED WIRING TO NOSE GEAR DOWNLOCK SENSOR HARNESS. OPS CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 2001080300283 20010803 00283 NM 2001 8 3 UHLA013661 1 20010704 A 3230 CONNECTOR DHAV DHC8 DHC8* NM COCKPIT LOOSE A UHLA O OTHER J WARNING INDICATION AP APPROACH 1 NE 03 802SA 8315 250 FLT 287 - GSO-TTN - LANDING GEAR WOULD NOT EXTEND WHEN SELECTED DOWN ARRIVING IN TTN. ALTERNATE GEAR EXTENSION AND LAND ING UNEVENTFUL. AIRCRAFT FERRIED TO BUF. CANNON PLUG AT GEAR CONTROL UNIT RESECURED. LANDING GEAR OPS CHECK GOOD. (M ) 2 H 7 2 4T RT A13NM 2001080300284 20010803 00284 NM 2001 8 3 USAA010698 1 20010516 A 5320 ANGLE BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND ANGLE PLATE ATTACH 2 INCHES BY 6 INCH, BETWEEN 767 AND 793 FORWARD SIDE OF AFT CARGO DOOR OPEN. CORROSION L EVEL 1, TASK C53-208-01. CLEANED CORROSION FROM ANGLE AND REPAIRED ANGLE PLATE PER SRM 51-21-21. (M) 2 L 7 2 4F RT A16WE 2001080300285 20010803 00285 NM 2001 8 3 USAA010699 1 20010505 A 5320 CLIP BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND SKIN CLIP CORRODED 1 INCH BY 4 INCH AREA EXFOLIATED, SKIN CLIP AFT SIDE STATION 967 STRINGER 25L AND 26L. C ORROSION LEVEL 2, TASK NR C53-208-01. REMOVED AND REPLACED WITH SECTION OF NEW SKIN CLIP PER SRM 53-00-03. (M) 2 L 7 2 4F RT A16WE 2001080300286 20010803 00286 NM 2001 8 3 USAA010700 1 20010504 A 5320 1138788 ANGLE BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 23931 PIT - FOUND Z-ANGLE CORRODED 1 INCH BY 6 INCHES, AT DOOR SILL OF AFT ENTRANCE DOOR. CORROSION LEVEL 1, TASK NR C53-107- 01. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M) 2 L 7 2 4F RT A16WE 2001080300287 20010803 00287 WP 2001 8 3 CALA0100728 1 20010731 A 5522 SKIN DOUG DC9 DC982 3022082 WP R/H ELEVATOR GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND R/H ELEVATOR SKIN LOWER SURFACE JUST OUTBOARD OF #2 HINGE MOUNTING PAD GOUGED. THE SKIN PANEL WAS REMOV ED AND A NEW SKIN PANEL WAS INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 2001080300288 20010803 00288 NM 2001 8 3 CALA0100729 1 20010731 A 5320 WEB BOEING 737 7373T0 1384582 NM STA 312 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14325 23455 INSPECTION FOUND A 1/4" CRACK IN STRESS WEB AT FLOORBEAM ATTACH POINT, STA 312, BL 0. THE WEB WAS REMOVED AND REPLACED I AW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001080300289 20010803 00289 WP 2001 8 3 CALA0100730 1 20010731 A 5311 FRAME DOUG DC9 DC982 3022082 WP FS 522 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND MID CARGO FRAME CORRODED AT FS 522 BETWEEN LONGERONS 28L AND 28R. THE CORRODED AREA OF FRAME WAS REMOVE D AND A REPAIR WAS INSTALLED IAW SRM 53-03 AND 51-30-5. 2 L 7 2 4F A6WE 2001080300290 20010803 00290 WP 2001 8 3 CALA0100733 1 20010803 A 5280 CHANNEL DOUG DC9 DC982 3022082 WP L/H MLG DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND A 1" CRACK IN L/H MLG DOOR CHANNEL AT FORWARD END OF DOOR JUST ABOVE DOOR SEAL. A REPAIR DOUBLER WAS IN STALLED IAW EA 9-5281-2-A0904 AND ECRA 5280-01267. 2 L 7 2 4F A6WE 2001080300291 20010803 00291 WP 2001 8 3 CALA0100734 1 20010803 A 5230 ANGLE DOUG DC9 DC982 3022082 WP FWD CARGO DR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND A 1" CRACK IN T-ANGLE AT FORWARD CARGO DOOR UPPER INTERNAL PAN AFT OF FORWARD HINGE. THE T-ANGLE WAS RE MOVED AND A NEW T-ANGLE WAS INSTALLED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 2001080300293 20010803 00293 WP 2001 8 3 ZW0A0106201 1 20010801 A 3350 408822101 POWER SUPPLY DOUG DC9 DC982 3022082 WP A ZW0A K NONE O OTHER CR CRUISE 1 CE 13 915TW 49186 DURING CRUSE THE EGRESS LIGHTS AT ROW 14 THRU 22 ON RIGHT SIDE OF CABIN ILLUMINATED DUE TO WEEK BATTERY. REPLACED EGRES S LIGHT POWER SUPPLY FOR ROWS 14 THRU 22 P/N408822-101.LAST CHECK C 07/12/01 STL. ---CLOSED--- 2 L 7 2 4F A6WE 2001080300294 20010803 00294 WP 2001 8 3 ZW0A0106202 1 20010802 A 3350 58222 POWER SUPPLY DOUG DC9 DC982 3022082 WP A ZW0A K NONE O OTHER CR CRUISE 1 CE 13 915TW 49186 DURING CRUSE THE EGRESS LIGHTS AT ROWS 14 THRU 22 CAME ON AND OFF WITH SWITCH IN THE ARMED POSITION, DUE TO INTERNAL FA ILURE. REPLACED POWER SUPPLY WITH P/N 5822-2. PER MM 33-59-00LAST CHECK C 07/12/01 STL. ---CLOSED--- 2 L 7 2 4F A6WE 2001080300295 20010803 00295 SO 2001 8 3 LR7A01054 1 20010802 A 5330 SKIN LKHEED 382 382G 526414U SO FS 892 DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 4590 DURING THRU FLIGHT WALK AROUND FOUND FS 892 SKIN DENTED AT RBL 61, WL 189.REPAIRED IAW SRM SMP 583-51-140-12. M1 LP 132 97. 2 H 7 4 4T A1SO 2001080400001 20010804 00001 NM 2001 8 4 01FDEA00638 1 20010803 A 5310 FRAME BOEING 727 727247 138408F NM UPPER FLANGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 N 665 UPR FLANGE AT BS 1090 FRAME HAS OPEN HOLE WITH CORROSION UNDER R/H FLOOR TO SIDEWALL SUPPORT (C53-111-01(3)). ** S/D ** COMING 2 L 7 3 4F A3WE 2001081600175 20010816 00175 NM 2001 8 16 01FDEA00639 1 20010803 A 5313 STRINGER BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSION (C53-111-01, 2) ON STR 28 RT BS 500. *S/D* REMOVED AND REPLACED STR PER SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 2001081600176 20010816 00176 NM 2001 8 16 01FDEA00641 1 20010803 A 5530 SHEAR TIE BOEING 727 727247 138408F NM VERTICAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CRACKED SHEAR TIE FOR VERTICAL STAB SKIN AT RIB NR 3 BETWEEN STR 6R & 7R. *S/D* REMOVED AND REPLACED SHEAR TIE PER SRM 51-30-2. 2 L 7 3 4F A3WE 2001081600177 20010816 00177 NM 2001 8 16 01FDEA00642 1 20010803 A 5311 FRAME BOEING 727 727247 138408F NM FUSELAGE BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 FRAME BENT BS 680 ABOVE STR 24L. *S/D* REMOVED AND REPLACED FRAME PER SRM 51-40-3. 2 L 7 3 4F A3WE 2001081600178 20010816 00178 NM 2001 8 16 01FDEA00643 1 20010803 A 5311 FRAME BOEING 727 727247 138408F NM FUSELAGE BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 FRAME BENT AT STR 22R. *S/D* REMOVED AND REPLACED FRAME PER SRM 51-40-3. 2 L 7 3 4F A3WE 2001081600179 20010816 00179 NM 2001 8 16 01FDEA00644 1 20010803 A 5310 SHEAR TIE BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSION (C53-111-02, 2) FWD CARGO BAY BS 720C, RBL 25, WL 150 SHEAR TIE AFT SIDE OF FRAME. *S/D* REMOVED AND REPLACE D SHEAR TIE PER SRM 51-30-5, 51-30-2 & MM 51-20-011-7. 2 L 7 3 4F A3WE 2001081600180 20010816 00180 NM 2001 8 16 01FDEA00645 1 20010803 A 5310 SHEAR TIE BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSION (C53-111-02, 2) FWD CARGO BAY BS 720A, RBL 25, WL 150 SHEAR TIE AFT SIDE OF FRAME. *S/D* REMOVED AND REPLACE D SHEAR TIE PER SRM 51-30-5, 51-30-2, 53-10-4. 2 L 7 3 4F A3WE 2001081700047 20010817 00047 NM 2001 8 17 01FDEA00646 1 20010803 A 5315 FLOORBEAM BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 WHILE WORKING CARD N 734 DISCOVERED CORROSION ON TOP CHORD OF FLOORBEAM AT BS 328, RBL 15, WL 208. *S/D* REMOVED AND R EPLACED FLOORBEAM PER SRM 53-10-8, 51-10-2, 51-30-2. 2 L 7 3 4F A3WE 2001081600181 20010816 00181 NM 2001 8 16 01FDEA00647 1 20010803 A 5315 FLOORBEAM BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSION (C53-224-01, 3) ON FLOORBEAM AT 950D AND RBL 20-25. *S/D* REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8. 2 L 7 3 4F A3WE 2001081700048 20010817 00048 NM 2001 8 17 01FDEA00649 1 20010803 A 5315 FLOORBEAM BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSION (C53-224-01, 1) BS 344, WL 208, LBL 50-RBL 25. *S/D* REMOVED AND REPLACED FLOORBEAM PER SR DWG 27-53-007. 2 L 7 3 4F A3WE 2001081700049 20010817 00049 NM 2001 8 17 01FDEA00650 1 20010803 A 5315 FLOORBEAM BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSION (C53-224-01, 1) BS 328, WL 208, LBL 24. *S/D* REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8 FIG 9. 2 L 7 3 4F A3WE 2001081700050 20010817 00050 NM 2001 8 17 01FDEA00651 1 20010803 A 5313 STRINGER BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSION (C53-111-01, 2) ON STR 28 LT BS 600. *S/D* REMOVED AND REPLACED STR PER SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 2001080600001 20010806 00001 EU 2001 8 6 EHA2001F00002 1 20010302 A 6320 6894471 GEARBOX BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20B 03013 GL NR 1 ENGINE FAILED A EHAA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 AL 03 500KM 6830 1604 S76 NR 1 ENGINE TORQUE REMAINED AT 60 PER CENT WHEN ENGINE TRANSITIONED FROM HIGH TORQUE TO GROUND IDLE. OPERATION ABOVE 60 PER CENT APPEARED NORMAL. CAUSE DETERMINED TO BE FAILURE OF THE TORQUE METER TO BLEED PRESSURE DURING ENGINE TORQUE TR ANSITION. ENGINE GEARBOX REMOVED AND REPLACED. 1 G 7 2 3U 3 U H3EU E4CE 2001080600002 20010806 00002 EA 2001 8 6 EHA2001F00003 2 20010626 A 7200 PT6T3 ENGINE BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA NR 2 FAILED A EHAA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION AP APPROACH 1 AL 03 5017H 8780 1556 30930 ON APPROACH TO REMOTE LANDING ZONE, WAITING FOR PREVIOUS A/C TO DEPART, PILOT WAS HOLDING IN PATTERN FOR LANDING AT APPR OXIMATELY 50 KNOTS AND 400 FEET AGL. WHILE HOLDING, PILOT HEARD ENGINE OUT WARNING AUDIO AND VERIFIED NR 2 ENGINE POWER LOSS. HE THEN EXECUTED A SINGLE ENGINE LANDING TO A CONFINED AREA WITH DAMAGE TO M/R BLADE, T/R BLADES, AND SYNCHRONIZ ED ELEVATOR. THE A/C WAS THEN SHUT DOWN. AWAITING A/C EXTRACTION AND TEARDOWN FOR FURTHER DETAILS. 1 G 7 1 4U 4 U H4SW E22EA 2001080600003 20010806 00003 NM 2001 8 6 DL76L010958 1 20010613 A 3520 417T4200216 OXYGEN SYSTEM BOEING 767 767332 1382001 NM CABIN MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 178DN 25143 DURING INSPECTION OF OXYGEN MASK EO PER AD FOUND NO OXYGEN EQUIPMENT IN PSU ABOVE SEATS 20 A AND B. NO OXYGEN GENERATOR OR MASKS OR ANYTHING. EO 1-85011-12AD REPLACED PSU AND OXYGEN GEN. ON, OFF A 351001259, B 353201010. 2 L 7 2 4F RT A1NM 2001080600004 20010806 00004 NM 2001 8 6 DLM11011211 1 20010722 A 2150 27400622 ACTUATOR DOUG MD11 MD11 3023602 NM A/C PACK MALFUNCTIONED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 804DE 192995 48475 CLIMBING THROUGH 10,000 MSL ON TAKEOFF, A SMOKE DETECTOR IN THE CREW REST FACILITY ACTIVATED. WITH THE DOOR OPEN FROM T HE COCKPIT COULD SMELL A HOT ODOR. RETURNED TO KENNEDY. UNEVENTFUL LANDING. INSPECTED A/C FOR EVIDENCE OF ANY FIRE, NO NE FOUND. SUSPECT PAC O/HEAT ON CLIMBOUT AND ALT ALERT HORN WENT OFF IN CREW REST AREA AND ODOR FROM O/HEATED PAC IN CA BIN. BIT CK ACC-1. FAULTED PK1 RAD ACT. REPLACED ACT AND COALESCER SOCKS. OPERATED PAC. NO ODOR AND PAC, OPS NORMAL. 2 L 7 3 4F RT A22WE 2001080600005 20010806 00005 EU 2001 8 6 MALA010514 1 20010609 A 2701 CONTROL COLUMN SAAB SF340 SF340A 7850100 EU COCKPIT STIFF A MALA K NONE F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 15 89XJ 089 ON FLIGHT 3201 FROM MCW, INFLIGHT NEEDS USE OF EXCESSIVE FORCE TO MANIPULATE FLIGHT CONTROLS. AC NEEDS TWO HANDS TO FLY . GETS WORSE WITH GEAR AND FLAPS DOWN, AND FLAG WILL COME ON IN BIG TURNS SOMETIMES. MAINTENANCE INSPECTED FLIGHT CONT ROLS VISUALLY NO VISIBLE DEFECTS MOVED FLIGHT CONTROLS, OR GROUND APPEAR TO OPERATE ON REGULAR AIRCRAFT HAS BEEN INSPECT ED AND IS SAFE FOR FERRY FLIGHT FROM MSP TO CWA FOR REPAIR. MX ISOLATED LT & RT FUSELAGE AILERON SYSTEMS. INSPECTED AS SOCIATED AILERON BELLCRANK AND BEARING AND ROLL DISCONNECT UNITS. COMPLETED AILERON MOVEMENT CHECK CONTROL WHEEL FORCE CHECK, TENSION CHECK OF CONTROL CABLES AND AILERON CLEARANCE CHECK IAW SAAB AMM 27-11-00-6. 2 L 7 2 4T RT A52EU 2001080600007 20010806 00007 NE 2001 8 6 MALA010517 2 20010609 A 7260 CHIP DETECTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE CONTAMINATED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 452XJ 452 RIGHT ENGINE CHIP DETECTOR LIGHT ILLUMINATED ON INITIAL CLIMBOUT. RAN QRH, ENGINE PARAMETERS WERE NORMAL. AIR RETURN T O OMA. MAINTENANCE REMOVED RIGHT ENGINE CHIP DETECTOR, INSPECTED FOUND TWO SMALL SLIVERS, PRESERVED FOR INSPECTION. RE INSTALLED CHIP DETECTOR. LEAK CHECKED GOOD. AC TO BE FERRIED FROM OMA TO MSP FOR COMPLETION OF MAINTENANCE PROCEDURES. MAINTENANCE COMPLIED WITH MAINTENANCE PROCEDURES OUTLINED IN GE MM SEI 576 72-00-00. FAULT ISOLATION TABLE 104 TROUBL E 10. MATERIAL IS DETERMINED TO BE ALLOWABLE PER TABLE 104, FIG 1 & 2. OPS AND LEAK CHECK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2001080600010 20010806 00010 EU 2001 8 6 MALA010539 1 20010619 A 2910 HYDRAULIC LINE SAAB SF340 340B 7860101 EU HYDRAULIC SYS LEAKING A MALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 15 48XJ 048 DURING FLIGHT 3103 OUT OF MSP, HYDR CWP LIGHT CAME ON AFTER T/O. MAIN ACCUMULATOR PRESSURE DROPPED TO ZERO. EM STAYED UP. WENT THRU THE QRH AND THE GEAR CAME DOWN HAD TO PUMP THE FLAPS DOWN. AIR RETURN TO MSP. MAINTENANCE COMPLETED MM 409 107664 REPLACED NLG RETRACTION ACTUATOR LINE. REPLACED LT AND RT SEPARATION BOLTS. REFER TO WORK CARD FOR DETAILS, OPS AND LEAK CHECK GOOD. 2 L 7 2 4T RT A52EU 2001080600012 20010806 00012 EU 2001 8 6 MALA010540 1 20010615 A 2910 4204001 POWER UNIT BAC 146 AVRO146RJ85A 1500097 EU HYDRAULIC SYS MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 GL 15 532XJ E2366 GREEN HYDRAULIC SYSTEM HIGH TEMPERATURE LIGHT ILLUMINATED EN ROUTE TO DSM. A/C DIVERTED TO MSP. MAINTENANCE FOUND LARG E HISTORY. PTU NOT CYCLING WHEN IN ON POSITION, REPLACED PTU P/N 4204001 IAW AMM 32-20-17. REPLACED LANDING GEAR SELE CTOR VALVE FOR T/S IAW AMM 32-30-17 P/N HTE9490-4. OPS AND LEAK CHECK GOOD. 2 H 7 4 4F RT A49EU 2001080600013 20010806 00013 EU 2001 8 6 MALA010543 1 20010628 A 7714 231300701 CONTROLLER BAC 146 AVRO146RJ85A 1500097 EU NR 4 ENGINE FAULTY A MALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 518XJ E2337 NR 4 ENGINE FAILED INFLIGHT DURING FLIGHT 3426, SHOWED OVERSPEED-LOW PRESSURE. NR 4 ENGINE SHUTDOWN INFLIGHT, A/C RETUR NED TO MSP. MAINTENANCE PERFORMED RESISTANCE AND MEGGER CHECK OF ENGINE INSULATION. CHECK AND MEGGER CHECK OF PRIMARY OVERSPEED PICK-UP LEAD NR 4 ENGINE. INSTALLED SERVICEABLE CONTROLLER P/N 2-313-007-01 S/ N ON 1270, S/N OFF 1408 IAW HO NEYWELL MM, CHECK CHIP COLLECTORS FOR METAL NR 4 ENGINE. ALL CHIP DETECTORS CHECK GOOD, NO FOREIGN MATERIAL FOUND. 2 H 7 4 4F RT A49EU 2001080600014 20010806 00014 EU 2001 8 6 MALA010544 1 20010621 A 2720 7227105582 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 403XJ 340B403 DURING 4K-CHECK, RT FUSELAGE AFT CIRCUIT I SINGLE RUDDER CABLE CHAFED. MAINTENANCE REMOVED CABLE AND INSTALLED NEW P/N 7227105-582 IAW SAAB MM 27-21-25. SEE 409 24308 FOR RIGGING. 2 L 7 2 4T RT A52EU 2001080600015 20010806 00015 EU 2001 8 6 MALA010548 1 20010623 A 5410 STRUCTURE SAAB SF340 340B 7860101 EU RT NACELLE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 403XJ 340B403 FOUND DURING 4K-CHECK IN CWA, RT NACELLE LOWER I/B CHAFED AT STA 227. REPAIRED IAW SAAB STATEMENT 340 SDS002027, EO S54 055. MAINTENANCE REPAIRED CHAFED AREA IAW SAAB STATEMENT. 2 L 7 2 4T RT A52EU 2001080600017 20010806 00017 EU 2001 8 6 MALA010549 1 20010623 A 2710 7227105613 CONTROL CABLE SAAB SF340 340B 7860101 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 403XJ 340B403 FOUND DURING 4K-CHECK IN CWA, LHOB FWD FUSELAGE AILERON CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED LHOB FWD FUSELAG E AILERON P/N 7227105-613. FOR RIG AND OPS CHECK SEE 409 024306. 2 L 7 2 4T RT A52EU 2001080600018 20010806 00018 EU 2001 8 6 MALA010550 1 20010623 A 2710 7227105621 CONTROL CABLE SAAB SF340 340B 7860101 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 403XJ 340B403 FOUND DURING 4K-CHECK IN CWA, LT AND RT FWD FUSELAGE AILERON CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED LHIB FWD FU SELAGE AILERON CABLE IAW SF3 AMM 27-11-25 P/N 7227105-623. FOR RIG AND OPS CHECK SEE 409 024306. 2 L 7 2 4T RT A52EU 2001080600019 20010806 00019 EU 2001 8 6 MALA010551 1 20010623 A 2710 7227105624 CONTROL CABLE SAAB SF340 340B 7860101 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 403XJ 340B403 FOUND DURING 4K-CHECK IN CWA, RHOB FWD FUSELAGE AILERON CABLE CHAFED. REMOVED AND REPLACED CABLE IAW SF3 AMM 27-11-25. P/N ON 7227105-624 FOR RIG AND OPS CHECK SEE 409 024306. 2 L 7 2 4T RT A52EU 2001080600020 20010806 00020 EU 2001 8 6 MALA010552 1 20010623 A 2710 7227105614 CONTROL CABLE SAAB SF340 340B 7860101 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 403XJ 340B403 FOUND DURING 4K-CHECK IN CWA, RHIB FWD FUSELAGE AILERON CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED RHIB FWD FUSELAG E AILERON CABLE IAW SF3 AMM 27-11-25 P/N ON 7227105-614. FOR RIG AND OPS CHECK SEE 409 024306. 2 L 7 2 4T RT A52EU 2001080600021 20010806 00021 EU 2001 8 6 MALA010553 1 20010624 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 403XJ 340B403 FOUND DURING 4K-CHECK IN CWA, FOUND CORROSION IN CARGO SEAT TRACK BL 0 BETWEEN STA 640 - 687. MAINTENANCE REMOVED AND R EPLACED SEAT TRACK SECTION IAW EO S53060, BETWEEN STA 619 - 687. 2 L 7 2 4T RT A52EU 2001080600024 20010806 00024 EU 2001 8 6 MALA010557 1 20010624 A 2730 7227105712 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 403XJ 340B403 FOUND DURING 4K-CHECK IN CWA, LHOB FWD FUSELAGE ELEVATOR CABLE CHAFED. MAINTENANCE REPLACED LHOB ELEVATOR CABLE P/N 722 7105-712 IAW SF340 AMM 27-31-15 FOR RIGGING SEE 409 024307. 2 L 7 2 4T RT A52EU 2001080600026 20010806 00026 EU 2001 8 6 MALA010558 1 20010624 A 2730 722705644 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 403XJ 340B403 FOUND DURING 4K-CHECK IN CWA, LHIB FWD FUSELAGE ELEVATOR CABLE CHAFED. MAINTENANCE REPLACED LHIB ELEVATOR CABLE P/N 722 7705-644 IAW SF 340A MM 27-31-15, FOR RIGGING SEE 409 024307. 2 L 7 2 4T RT A52EU 2001080600028 20010806 00028 EU 2001 8 6 MALA010559 1 20010624 A 2730 7227150712 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 403XJ 340B403 FOUND DURING 4K-CHECK IN CWA, RHOB FWD FUSELAGE ELEVATOR CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED RHOB CABLE P/N 7227105-712 IAW SF340A MM 27-31-15. 2 L 7 2 4T RT A52EU 2001080600030 20010806 00030 EU 2001 8 6 MALA010560 1 20010624 A 2730 7227705644 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 403XJ 340B403 FOUND DURING 4K-CHECK IN CWA, RHIB FUSELAGE ELEVATOR CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED I/B CABLE P/N 72277 05-644 IAW SF340A MM 27-31-15. 2 L 7 2 4T RT A52EU 2001080600032 20010806 00032 EU 2001 8 6 MALA010561 1 20010625 A 2720 7227105562 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 403XJ 340B403 FOUND DURING 4K-CHECK IN CWA, LHOB FUSELAGE DUAL CIRCUIT I RUDDER CABLE CHAFED. MAINTENANCE REPLACED LHOB FUSELAGE DUAL CIRCUIT RUDDER CABLE P/N 7227105-562, IAW SF340 27-21-25-4. 2 L 7 2 4T RT A52EU 2001080600033 20010806 00033 EU 2001 8 6 MALA010562 1 20010625 A 2720 7227105571 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 403XJ 340B403 FOUND DURING 4K-CHECK IN CWA, LHIB FUSELAGE DUAL CIRCUIT I RUDDER CABLES CHAFED. MAINTENANCE REPLACED LHIB FUSELAGE DUA L CIRCUIT RUDDER CABLE P/N 7227105-571 IAW SF340 27-21-25-4. 2 L 7 2 4T RT A52EU 2001080600035 20010806 00035 EU 2001 8 6 MALA010563 1 20010625 A 2720 7227105571 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 403XJ 340B403 FOUND DURING 4K-CHECK IN CWA, RHIB FUSELAGE DUAL CIRCUIT I RUDDER CABLE CHAFED. MAINTENANCE REPLACED RHIB FUSELAGE DUAL CIRCUIT RUDDER CABLE P/N 7227105-571 IAW SF340 27-21-25-4. 2 L 7 2 4T RT A52EU 2001080600037 20010806 00037 EU 2001 8 6 MALA010564 1 20010625 A 2720 7227105562 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 403XJ 340B403 FOUND DURING 4K-CHECK IN CWA, RHOB FUSELAGE DUAL CIRCUIT I RUDDER CABLE CHAFED. MAINTENANCE REPLACED CABLE P/N 7227105- 562 IAW SF340 27-21-25-4. 2 L 7 2 4T RT A52EU 2001080600039 20010806 00039 EU 2001 8 6 MALA010565 1 20010630 A 2720 7227105582 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 403XJ 340B403 FOUND DURING 4K-CHECK IN CWA, LT FUSELAGE AFT CIRCUIT I SINGLE RUDDER CABLE CHAFED. MAINTENANCE REMOVED CABLE AND INSTA LLED NEW CABLE P/N 7227105-582 IAW SAAB MM 27-21. 2 L 7 2 4T RT A52EU 2001080600042 20010806 00042 EU 2001 8 6 MALA010566 1 20010630 A 2930 HE83273 SWITCH BAC 146 AVRO146RJ85A 1500097 EU HYDRAULIC SYS FAULTY A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 523XJ E2348 DURING FLIGHT, GREEN HYDRAULIC HIGH TEMP LIGHT CAME ON. COMPLETED QRH AND LANDED IN MSP 30L. AIR RETURN TO MSP. MAINT ENANCE REMOVED AND REPLACED TEMP SWITCH IAW AMM 29-33-11. P/N HE83273 S/N OFF 1296TW. LEAK CHECK GOOD. 2 H 7 4 4F RT A49EU 2001080600043 20010806 00043 EU 2001 8 6 MALA010567 1 20010701 A 2934 SWITCH SAAB SF340 SF340A 7850100 EU HYDRAULIC SYS DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 46XJ 340A046 DURING FLIGHT 2735, HYDRAULIC CAUTION LIGHT ON IN FH-MAIN AND EMERGENCY ACCUMULATORS LOW-DID MEMORY ITEMS GEAR HANDLE DO WN NO LEFT GEAR. PULLED EMERGENCY LANDING GEAR HANDLE, ALL GEAR DOWN. A/C DIVERTED TO CRW. MAINTENANCE REMOVED AND RE PLACED SEPARATION BOLTS AND HYDRAULIC PRESSURE SWITCH. 2 L 7 2 4T RT A52EU 2001080600045 20010806 00045 EU 2001 8 6 MALA010568 1 20010702 A 2424 CONNECTOR SAAB SF340 340B 7860101 EU GCU DIRTY A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 441XJ 340B441 AFTER TAKEOFF ON FLIGHT 3251, THE RT AC GEN LIGHT CAME ON. DID QRH, LIGHT REMAINED ON. AIR RETURN TO MSP. MAINTENANCE CLEANED CANNON PLUG AT GCU, RAN ENGINE PERFORMED OPS CHECKS ALL GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2001080600046 20010806 00046 NM 2001 8 6 01FDEA00653 1 20010802 A 5330 DOUBLER DOUG MD11 MD11 3023602 NM CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 SNRM 220 CENTER LAND GEAR RH BULKHEAD DOUBLER BETWEEN BS 1361-1381 FND CRACKED. ** S/D ** COMING 2 L 7 3 4F RT A22WE 2001082800135 20010828 00135 NM 2001 8 28 01FDEA00654 1 20010802 A 5312 DOUBLER DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 CENTER LAND GEAR LT BULKHEAD DOUBLER BETWEEN BS 1361-1381 CRACKED. REMOVED AND REPLACED SRM 51-31-01 VOL 2. 2 L 7 3 4F RT A22WE 2001080600047 20010806 00047 EU 2001 8 6 MALA010569 1 20010701 A 3230 85106RC84SNB CONNECTOR SAAB SF340 SF340A 7850100 EU LANDING GEAR DEFECTIVE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 142XJ 142 WHILE COMPLETING EMERGENCY EXTENSION CHECKS FOR THE LANDING GEAR AND SEPARATION BOLT DUAL BRIDGE WIRE CONTINUITY CHECKS FOUND NO VOLTS AVAILABLE TO BOLT. UPON DISASSEMBLY OF CANNON PLUG FOUND FOUR WIRE BROKE. ONCE AGAIN SUSPECT ROUTING OF WIRES PUTTING TO MUCH STRESS ON THE CONNECTION POINTS (WIRES CRIMPED TO PINS),DURING ELECTRICAL TEST OF RT SEPARATION B OLT ELECTRICAL HARNESS CONNECTOR, FOUND 28 VOLTS NOT GETTING TO CONNECTOR. MAINTENANCE REMOVED AND REPLACED RT SEPARATI ON BOLT CANNON PLUG P/N 851-06RC8-4SNB IAW PC7635 SAAB REPAIR KIT AND WIRING DIAGRAM. OPS TEST OK. 2 L 7 2 4T RT A52EU 2001080600048 20010806 00048 NE 2001 8 6 MALA010571 2 20010707 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RIGHT MALFUNCTIONED A MALA E D ENGINE SHUTDOWN RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 68XJ 340A068 DURING START THE RT ENGINE WOULD NOT COME OUT OF GROUND IDLE WHEN THE POWER LEVERS WERE ADVANCED TO MIN/MAX RANGE THE EN GINE (PROP) DID NOT RESPOND. AFTER ABOUT 5 SECONDS WITH THE CL IN THE MIN/MAX RANGE CREW SAW SMOKE COMING OUT OF NACELL E AND SMELLED SMOKE IN COCKPIT. CREW SHUTDOWN ENGINE. MAINTENANCE INSPECTED RT ENGINE FOUND NO OIL LEAK OR DAMAGE, OIL LEVEL WITHIN LIMIT. RAN AC AND PERFORMED ALL ENGINE RUNS IAW GEMM 72, ALL CHECK GOOD. NO SMOKE NOTICED WHEN START RT E NGINE. 2 L 7 2 4T 4 T RT A52EU E8NE6 2001080600050 20010806 00050 EU 2001 8 6 MALA010573 1 20010709 A 3610 6303250 PERISEAL BAC 146 AVRO146RJ85A 1500097 EU BLEED AIR LEAKING A MALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 GL 15 503XJ E2310 ON FLIGHT 3691 LT YELLOW/GREEN HIGH TEMP ASSOCIATED PACK 1. A/C DIVERTED TO MEM. MAINTENANCE REPLACED 2 PERI-SEALS ON LT Y-DUCT P/N 630-3-250, AND 2 PERI-SEALS ON DUCT BELOW NR 1 PACK VALVE, OPERATED SYSTEM, LEAK CHECK GOOD. NO FAULTS NO TED IAW AMM 21-09-11. 2 H 7 4 4F RT A49EU 2001080600061 20010806 00061 EU 2001 8 6 MALA010574 1 20010606 A 2750 676601004 BRAKE ASSY BAC 146 AVRO146RJ85A 1500097 EU T/E FLAP MALFUNCTIONED A MALA K NONE F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 15 511XJ E2325 DURING FLIGHT 3420, GFK/MSP SELECTING FLAPS 0-18 DEGREES THE FLAP FAULT AND FLAP INOP LIGHTS ILLUMINATED. A ZERO FLAP L ANDING WAS MADE WITH TOUCHDOWN SPEED OF 174 KTS. MAINTENANCE SERVICED ALL 4 JACKSCREW BALL NUTS, RT 2 & 3 SCREW JACK GE AR BOXES, ADJUSTED NR 2 DRIVE CHAIN TENSION, REPLACED RT ASYMMETRY BRAKE P/N 676601004, S/N ON DAW 126-98. OPERATED FLA PS FULL RANGE NUMEROUS TIMES ALL CHECKED GOOD. 2 H 7 4 4F RT A49EU 2001080600062 20010806 00062 EU 2001 8 6 MALA010575 1 20010710 A 7933 4053T73P01 BULB SAAB SF340 SF340A 7850100 EU ENGINE FAULTY A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 114XJ 340A114 ON FLIGHT 3139, CREW REPORTED THE LT OIL TEMP (ENGINE) IS HIGH. A/C RETURNED TO MSP. MAINTENANCE REPLACED LT OIL TEMP BULB P/N 4053T73P01, S/N ON EGNAD727, S/N OFF GEN30288 IAW 79-00-00 P437, OPS AND LEAK CHECK GOOD. REPLACED LT ENGINE O IL. LEAK CHECK GOOD. 2 L 7 2 4T RT A52EU 2001080600063 20010806 00063 EU 2001 8 6 MALA010576 1 20010718 A 7722 6058T28P01 THERMOCOUPLE SAAB SF340 340B 7860101 EU LT ENGINE DEFECTIVE A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 429XJ 340B429 DURING CLIMBOUT LT ITT READ UP TO 100 DEGREES LOWER THAN RH ENGINE (ALSO FLUCTUATED NUMEROUS TIMES) SET TORQUES, FUEL FL OW AND NG'S WERE DISPLAYING NORMAL INDICATIONS. AIR TURNBACK TO MSP. MAINTENANCE PERFORMED ITT FUNCTIONAL CHECK IAW TA SK CARD 772001-1 OHMED YELLOW HARNESS, ALL CHECKS GOOD. CLEANED CANNON PLUG WP41 AT ECU. PERMANENTLY SWAPPED ITT INDIC ATORS FROM LEFT TO RIGHT, REMOVED AND REPLACED THERMOCOUPLE ASSEMBLY P/N 6058T28P01, S/N OFF 6BDA, S/N ON 60B6432E. 2 L 7 2 4T RT A52EU 2001080600072 20010806 00072 EU 2001 8 6 MALA010579 1 20010717 A 7722 6058T28P01 THERMOCOUPLE SAAB SF340 340B 7860101 EU LT ENGINE DEFECTIVE A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 429XJ 340B429 DURING FLIGHT 2978 DURING CLIMB LEFT ITT READ UP TO 100 DEGREES LOWER THAN RIGHT ENGINE, ALSO FLUCTUATED NUMEROUS TIMES. SET TORQUES, FUEL FLOW ENGINES WERE DISPLAYING NORMAL INDICATIONS. AIR RETURN TO MSP. MAINTENANCE PERFORMED ITT FUNC TIONAL CHECK IAW TASK CARD 772001-1. OHMED YELLOW HARNESS, ALL CHECKS GOOD. CLEANED CANNON PLUG AT ECU. PERMANENTLY S WAPPED ITT INDICATORS P/N 10221N01T00 FROM LEFT TO RIGHT. REPLACED THERMOCOUPLE ASSY P/N 6058T28P01 SN/OFF 68DA6036 SN/ ON 6086432E. PERFORMED GPA RUNS, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2001080600076 20010806 00076 EU 2001 8 6 MALA010580 1 20010704 A 2720 7227105582 CONTROL CABLE SAAB SF340 SF340A 7850100 EU RUDDER WORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 76XJ 340A076 DURING 4K-INSPECTION IN CWA, LT AFT SINGLE RUDDER CABLE WORN CIRCUIT I. MAINTENANCE REMOVED AND REPLACED CABLE P/N 7227 105-582. LT AFT SINGLE RUDDER CABLE REPLACED IAW SF340 AMM 27-21-25-4. 2 L 7 2 4T RT A52EU 2001080600078 20010806 00078 EU 2001 8 6 MALA010581 1 20010704 A 2710 7227105522 CONTROL CABLE SAAB SF340 SF340A 7850100 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 76XJ 340A076 DURING 4K-CHECK IN CWA, FWD O/B CABLE OF RT AILERON WING IS CHAFED. MAINTENANCE REMOVED AND REPLACED CABLE P/N 7227105- 522, IAW SF 340 27-11-25-4, SEE 409 023522 FOR RIGGING AND SAFETY. 2 L 7 2 4T RT A52EU 2001080600080 20010806 00080 EU 2001 8 6 MALA010582 1 20010705 A 2710 7227151522 CONTROL CABLE SAAB SF340 SF340A 7850100 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 76XJ 340A076 DURING 4K-CHECK IN CWA, O/B FWD LT AILERON WING CABLE IS CHAFED. MAINTENANCE REPLACED LHOB FWD AILERON WING CABLE IAW S R3 AMM 27-11-25 P/N 7227151-522. SEE 409 023522 FOR RIGGING AND SAFETY. 2 L 7 2 4T RT A52EU 2001080600083 20010806 00083 EU 2001 8 6 MALA010585 1 20010709 A 2730 7227105712 CONTROL CABLE SAAB SF340 SF340A 7850100 EU ELEVATOR WORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 76XJ 340A076 DURING 4K-CHECK IN CWA, RHOB ELEVATOR CABLE WORN FWD FUSELAGE. MAINTENANCE REMOVED AND REPLACED RHOB FWD FUSELAGE ELEVA TOR CABLE P/N 7227105-712 IAW SF3 AMM 27-31. 2 L 7 2 4T RT A52EU 2001080600085 20010806 00085 EU 2001 8 6 MALA010586 1 20010709 A 2720 7227105562 CONTROL CABLE SAAB SF340 SF340A 7850100 EU RUDDER WORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 76XJ 340A076 DURING 4K-INSPECTION IN CWA, LHOB RUDDER CABLE WORN DUAL CIRCUIT. MAINTENANCE REPLACED LHOB RUDDER CABLE P/N 7227105-56 2 IAW SRM 340 AMM 27-21-25. 2 L 7 2 4T RT A52EU 2001080600087 20010806 00087 EU 2001 8 6 MALA010587 1 20010709 A 2720 7227105562 CONTROL CABLE SAAB SF340 SF340A 7850100 EU RUDDER WORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 76XJ 340A076 DURING 4K-INSPECTION IN CWA, RHOB RUDDER CABLE WORN, DUAL CIRCUIT. MAINTENANCE REPLACED RHOB RUDDER CABLE P/N 7227105-5 62 IAW SR340 AMM 27-21-25. 2 L 7 2 4T RT A52EU 2001080600089 20010806 00089 EU 2001 8 6 MALA010588 1 20010711 A 5414 SKIN SAAB SF340 SF340A 7850100 EU RT NACELLE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 76XJ 340A076 DURING 4K-CHECK IN CWA, FOUND RT NACELLE I/B SIDE WHERE FILLET PANEL INTERSECTS IS CHAFED. MAINTENANCE INSTALLED REPAIR ON I/B SKIN OF RT NACELLE IN I/B WING FAIRING CHAFED AREA. 2 L 7 2 4T RT A52EU 2001080600090 20010806 00090 EU 2001 8 6 MALA010589 1 20010712 A 5414 SKIN SAAB SF340 SF340A 7850100 EU LT NACELLE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 76XJ 340A076 DURING 4K-HEAVY CHECK IN CWA, LT NACELLE I/B SKIN IS CHAFED WHERE FILLET PANEL SEAL CONTACTS SKIN. 2 L 7 2 4T RT A52EU 2001080600091 20010806 00091 EU 2001 8 6 MALA010590 1 20010713 A 5311 FRAME SAAB SF340 SF340A 7850100 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 76XJ 340A076 DURING 4K-HEAVY CHECK IN CWA, FUSELAGE BOTTOM FRAME AT STA 272 IS CORRODED. MAINTENANCE REPAIRED IAW EOS53099. 2 L 7 2 4T RT A52EU 2001080600093 20010806 00093 EU 2001 8 6 MALA010592 1 20010716 A 5312 PRESSURE PANEL SAAB SF340 SF340A 7850100 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 76XJ 340A076 DURING 4K-HEAVY INSPECTION IN CWA, LT FLT DECK FLOOR NEAR PEDESTAL AREA HAS CORROSION. MAINTENANCE REPAIRED CORROSION A REA ON LT FLT DECK FLOOR NEAR PEDESTAL. 2 L 7 2 4T RT A52EU 2001080600095 20010806 00095 EU 2001 8 6 MALA010593 1 20010725 A 2150 11341941 MOTOR SAAB SF340 340B 7860101 EU CABIN MALFUNCTIONED A MALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 408XJ 340B408 DURING FLIGHT 3224 OUT OF YQK, WHILE LOADING PAX HAD SMOKE IN CABIN WITH AN ELECTRICAL SMELL. SMOKE APPEARED TO BE COMI NG FROM BELOW THE SEATS ON THE RT SIDE. THE SMOKE STOPPED WHEN POWER WAS TURNED OFF. MAINTENANCE FOUND SMOKING COMPONE NT TO BE SUPPLEMENTAL AC MOTOR. REPLACED THE AC COMPRESSOR MOTOR P/N 1134194-1, S/N ON 1600, S/N OFF 812 IAW CMM AAR SF 340 AIR COND SYSTEM, 10/4/2 OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2001080600096 20010806 00096 EU 2001 8 6 MALA010595 1 20010720 A 2710 D97648 ACTUATOR SAAB SF340 340B 7860101 EU AILERON FAULTY A MALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 15 403XJ 340B403 DURING FLIGHT 3052 MAIN AILERON TRIM RUNAWAY. LEFT WING HAD STRONG DOWNLOAD FORCES. TRIM INDICATOR INDICATED FULL-UP O N INDICATOR, UNABLE TO NEUTRALIZE FORCES WITH MAIN TRIM STANDBY TRIM WORKED. AIR RETURN TO RHI. MAINTENANCE FOUND LT A ILERON TRIM ACTUATOR TO BE FAULTY. REMOVED AND REPLACED LT AILERON TRIM ACTUATOR P/N D97648, S/N OFF 96H19190, S/N ON 91K1575-127 IAW SAAB MM 27-12-10. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2001080600098 20010806 00098 EU 2001 8 6 MALA010596 1 20010727 A 3040 SHIELD SAAB SF340 SF340A 7850100 EU RAIN PROTECTION DEBONDED A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 76XJ 340A076 DURING FLIGHT 2820, DOOR HAS NOISE COMING FROM BOTTOM. AIR RETURN TO MSP. MAINTENANCE FOUND RAIN SHIELD DISBONDED, RE- SECURED SEAL AS REQUIRED. SECURITY CHECK GOOD. 2 L 7 2 4T RT A52EU 2001080600099 20010806 00099 NE 2001 8 6 MALA010597 3 20010727 A 6140 INDICATOR SAAB SF340 340B 7860101 EU ROTOL R354 R3544123F13 NE COCKPIT MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 450XJ 340B450 DURING FLIGHT 2743, RT PROP SPEED INDICATOR ERRATIC AND THEN FAILED IN FLIGHT. AIR RETURN TO DTW. MAINTENANCE GROUND R AN AND TAXI AIRCRAFT FOR APPROXIMATELY 1 HOUR, COULD NOT DUPLICATE. ALL CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 6 C P61GL 2001080600100 20010806 00100 EU 2001 8 6 MALA010598 1 20010727 A 2432 501122804 POWER SUPPLY SAAB SF340 340B 7860101 EU E/E BAY FAULTY A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 590MA 340B181 DURING FLIGHT NR 3666, EMERGENCY BATTERY LIGHT ILLUMINATED OUTBOUND. AIR RETURN TO DTW. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY P/N 501-1228-04, S/N ON 4684, S/N OFF 1606 IAW MAL TASK CARD 243502. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2001080600101 20010806 00101 EU 2001 8 6 MALA010599 1 20010606 A 5260 C14647 HAND RAIL BAC 146 AVRO146RJ85A 1500097 EU AIRSTAIR CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 505XJ E2313 DURING C-CHECK IN CVG, MAINTENANCE FOUND CORROSION ON O/B AIRSTAIR RAIL. CORROSION IS ENTIRE LENGTH OF RAIL AND IS EXFO LIATING BEYOND SRM LIMITS 53-00-32 101. MAINTENANCE REPLACED O/B AIRSTAIR RAIL P/N C14647 IAW BAE SRM 53-00-32. 2 H 7 4 4F RT A49EU 2001080600102 20010806 00102 EU 2001 8 6 MALA010600 1 20010514 A 5320 HC533J0800002U SILL BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 506XJ E2314 DURING C-CHECK IN CVG, EVIDENCE OF CORROSION FOUND ON LT DOOR SILL PLATE AREA. REMOVE CORROSION FOR FURTHER EVALUATION. MAINTENANCE REPLACED LT DOOR SILL PLATES (REAR) P/N HC533JO321-002U AND HC533J0800-002U IAW SRM 51-41-00. 2 H 7 4 4F RT A49EU 2001080600103 20010806 00103 EU 2001 8 6 MALA010601 1 20010605 A 5320 HC538508210024 SILL BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 505XJ E2313 DURING C-CHECK IN CVG, CORROSION FOUND ON AFT Z-MEMBER 0.012 INCH DEEP BEYOND LIMITS, LT AFT DOOR SILL PLATE AREA. MAINT ENANCE REPLACED SILL PLATE P/N HC53850821-0024 IAW SRM 51-43-00 AND 51-23-00. 2 H 7 4 4F RT A49EU 2001080600104 20010806 00104 EU 2001 8 6 MALA010602 1 20010603 A 5320 HC538J0821002U SILL BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 505XJ E2313 DURING C-CHECK IN CVG, FOUND CORROSION ON FWD Z-MEMBER 0.008 INCH DEEP, ALSO CRACKED 0.075 INCH LENGTH BEYOND LIMITS. L T AFT DOOR SILL PLATE AREA. MAINTENANCE REPLACED SILL PLATE P/N HC538J0821-002U IAW SRM 51-43-00, AND 51-23-00. 2 H 7 4 4F RT A49EU 2001080600105 20010806 00105 EU 2001 8 6 MALA01591 1 20010715 A 5330 DOUBLER SAAB SF340 SF340A 7850100 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 76XJ 340A076 DURING 4K-HEAVY CHECK IN CWA, RT FUSELAGE MIDDLE 2 ICE SHIELDS ARE DENTED. MAINTENANCE REMOVED ICE SHIELD AND REPAIRED FUSELAGE IAW EO S53005, REINSTALLED ICE SHIELD. PAINTED AS REQUIRED. 2 L 7 2 4T RT A52EU 2001080600106 20010806 00106 NM 2001 8 6 PCAA0106050 1 20010614 A 2120 UNKNOWN DHAV DHC8 DHC8102 2809003 NM CABIN ODOR A PCAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 13 843EX 335 ROC- FLIGHT 3604. FLIGHT ATTENDANT REPORTED STRONG BURNING ODOR IN CABIN DURING FLIGHT. MAINTENANCE RAN APU BLEED SYST EM AND BOTH ENGINE BLEEDS. INSPECTED ALL CABIN INTERIOR LIGHTING, INSPECTED BOTH ENGINE INTAKES AND ACM. AVIONICS SYST EMS INSPECTED FOR BURNED COMPONENTS, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001080600107 20010806 00107 NM 2001 8 6 PCAA0106051 1 20010614 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A PCAA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 13 820EX 019 BOS-FLIGHT 3553. CREW REPORTED EMERGENCY EXIT LIGHTING 20 PERCENT INOPERATIVE. MAINTENANCE RECONNECTED FLOOR LIGHTING PLUG AT LEFT SIDE, REPLACED LIGHTING STRIP AT ROW 9 RIGHT SIDE, AND REPLACED SEVERAL JUMPERS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001080600108 20010806 00108 NM 2001 8 6 PCAA0106053 1 20010615 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM LAVATORY BROKEN A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 832EX 280 MDT- MAINTENANCE DISCOVERED LAV OVERHEAD LIGHTS BLOW OUT EMERGENCY LIGHTS WHEN LAV IS IN USE. AFTER TROUBLESHOOTING FOU ND LAV LIGHT OCCUPIED CIRCUIT BOARD FEEDING 28 VOLTS DC GROUND INTO EMERGENCY LIGHTS OVERHEAD PANEL CIRCUIT BOARD. SHOR T CIRCUIT ISOLATED. OPERATIONAL CHECK GOOD. REPAIRED BROKEN WIRES AND REINSTALLED LAV OVERHEAD SWITCH ASSEMBLY. EMERG ENCY LIGHT BATTERY IN POSITION L20 FOUND INOPERATIVE. BATTERY IN POSITION L20 REPLACED. OPERATIONAL CHECK GOOD. AIRCR AFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001080600109 20010806 00109 NM 2001 8 6 PCAA0106054 1 20010616 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 847EX 333 BGM- DURING ROUTINE MAINTENANCE VISIT FOUND EMERGENCY LIGHTING IN TRACK HAD ONE LIGHT OUT. TWO BROKEN WIRES REPAIRED IN HARNESS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001080600110 20010806 00110 NM 2001 8 6 PCAA0106060 1 20010620 A 5210 GUIDE DHAV DHC8 DHC8102 2809003 NM PAX DOOR OUT OF ADJ A PCAA K NONE O OTHER TX TAXI/GRND HDL 1 EA 13 816EX 329 BUF- FLIGHT 3585. CREW REPORTED UNABLE TO OPEN MAIN CABIN DOOR. MAINTENANCE INSTALLED BUMPER FOR AIRSTAIR DOOR OUTER H ANDLE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.ON 21 JUNE 2001 ITH FLIGHT 3705 CREW REPORTED UNABLE TO OP EN PASSENGER DOOR FROM OUTSIDE OF AIRCRAFT. MAINTENANCE RESHIMMED DOOR GUIDE STOP IN ACCORDANCE WITH DASH 8 MAINTENANCE MANUAL 52-10-00. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001080600111 20010806 00111 NM 2001 8 6 PCAA0106061 1 20010623 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN DAMAGED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 805EX 228 MDT- DURING ROUTINE MAINTENANCE VISIT FLOOR PATH EMERGENCY LIGHTS AT SEAT 8D FOUND INOPERATIVE. TROUBLESHOOTING FOUND W IRE CAME APART TO FLOOR CONNECTOR. CONNECTOR REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001080600112 20010806 00112 NM 2001 8 6 PCAA0106062 1 20010624 A 5210 8SC0156 STRUT DHAV DHC8 DHC8102 2809003 NM PAX DOOR WEAK A PCAA K NONE O OTHER TX TAXI/GRND HDL 1 EA 13 805EX 228 MDT- FLIGHT 3749. CREW REPORTED PASSENGER DOOR WILL NOT OPEN OR CLOSE PROPERLY. MAINTENANCE REPLACED OVER CENTER GAS S TRUT AND LUBRICATED. OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2001080600113 20010806 00113 NM 2001 8 6 PCAA0107063 1 20010629 A 3350 1010951 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 830EX 155 MDT- DURING ROUTINE MAINTENANCE VISIT EMERGENCY LIGHT ON FLOOR FOUND TO BE INOPERATIVE. LIGHT ASSEMBLY ON FLOOR REPLACE D AT ROW 8. OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2001080600114 20010806 00114 NM 2001 8 6 PCAA0107064 1 20010629 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN DISCONNECTED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 819EX 016 MDT- DURING ROUTINE MAINTENANCE VISIT LIGHT ON FLOOR AT ROWS 5 & 6 DF FOUND TO BE INOPERATIVE. FOUND PLUG TO BE OFF VIS TA LIGHT SECTION AT 5 6 DF. PLUG REINSTALLED. OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2001080600115 20010806 00115 2001 8 6 PCAA0107065 4 20010629 A 3423 C5C COMPASS DHAV DHC8 DHC8102 2809003 NM COCKPIT LEAKING A PCAA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 13 819EX 24463 016 BWI- FLIGHT 3684. CREW REPORTED VERY STRONG ODOR IN COCKPIT SMELLING LIKE LACQUER THINNER. MAINTENANCE INSPECTED RADAR ALTIMETER CONTROLLER AND CABIN PRESSURE CONTROLLER. FOUND MAGNETIC COMPASS LEAKING. MAGNETIC COMPASS REPLACED AND NEW CORRECTION CARD INSTALLED IN AIRCRAFT. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001080600116 20010806 00116 NE 2001 8 6 PCAA0107066 2 20010704 A 7200 PW120A ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LEFT MALFUNCTIONED A PCAA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 13 844EX 20752 1147 339 121100 ROC- FLIGHT 3943 AT 700 FT 8 MINUTES OUT WHILE ON DESCENT TOWARD ROC FROM LGA, SMOKE SMELL IN CABIN AND COCKPIT WHEN NR 1 BLEED SWITCH IS ON. NO VISIBLE SMOKE OBSERVED. EMERGENCY DECLARED, AIRCRAFT LANDED IN ROC WITHOUT INCIDENT. MAINTEN ANCE VERIFIED SMOKE COMING FROM LEFT ENGINE. LEFT ENGINE REPLACED IN ACCORDANCE WITH COMPANY JOB CARD 008-7101-349, LEA K AND OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2003012100249 20030121 00249 NM 2003 1 21 PCAA0107067 1 20010710 A 5315 85310380 FLOORBEAM DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 810EX 308 DURING SCHEDULED A INSPECTION NOSE GEAR WELL FLOORBEAM AT STATION X97 FOUND CRACKED. REPAIR STRAP INSTALLED PER DEHAVIL LAND REPAIR DRAWING RD 8-53-5993 AS AN INTERIM REPAIR FOR 250 HOURS AT WHICH A PERMANENT REPAIR WILL BE INSTALLED. DEHA VILLAND HAD ISSUED REPAIR DRAWING RD8-53-6016 ALLOWING REPETITIVE INSPECTIONS AT 250 HOUR INTERVAL UNTIL PERMANENT REPAI R AT C CHECK IS ACCOMPLISHED. PERMANENT REPAIR APPLIED IN ACCORDANCE WITH REPAIR DRAWING RD8-53-6016 ON 17 JANUARY 2003 DURING C INSPECTION AT PIEDMONT AIRLINES. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001080600117 20010806 00117 NM 2001 8 6 PCAA0107068 1 20010710 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 819EX 016 DURING ROUTINE MAINTENANCE VISIT RIGHT SIDE OF EMERGENCY LIGHTS IN CABIN FOUND TO BE INOPERATIVE. BROKEN WIRE REPAIRED IN EMERGENCY LIGHT WIRE HARNESS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001080600118 20010806 00118 NM 2001 8 6 PCAA0107069 1 20010714 A 5312 PRESSURE PANEL DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 809EX 302 DURING ROUTING MAINTENANCE VISIT RIGHT SIDE NOSE COMPARTMENT FLOOR CRACKED. CRACK REPAIRED IN ACCORDANCE WITH DEHAVILLA ND REPAIR DRAWING RD 8-53-3893. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001080600119 20010806 00119 NM 2001 8 6 PCAA0107070 1 20010714 A 3350 TERMINAL DHAV DHC8 DHC8102 2809003 NM FA PANEL DAMAGED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 818EX 235 DURING ROUTINE MAINTENANCE VISIT EMERGENCY LIGHTS FOUND TO FLICKER WHEN SELECTED ON FROM THE FLIGHT ATTENDANTS PANEL. T ERMINAL END REPAIRED AT FLIGHT ATTENDANTS LIGHT SWITCH. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001080600120 20010806 00120 NM 2001 8 6 PCAA0107072 1 20010714 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 820EX 019 DURING ROUTINE MAINTENANCE VISIT 2 LIGHTS FOUND INOPERATIVE ON RIGHT SIDE OF EMERGENCY EXIT FLOOR PATH LIGHTING. BROKEN WIRE ON CONNECTOR RESOLDERED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001080600121 20010806 00121 WP 2001 8 6 RRXA010034 1 20010131 A 3230 MECHANISM DOUG DC8 DC873F 302199F WP NLG OUT OF ADJ A RRXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 795FT 46103 AFTER T/O ACFT DIDN'T GROUND SHIFT; COULD NOT RETRACT MLG. ADJUSTED NOSE GEAR GROUND SHIFT MECHANISM IAW DC-8 M/M CH 32 -23-01, OP CHKS GOOD. 2 L 7 4 4F RT 4A25 2001081500179 20010815 00179 NM 2001 8 15 01FDEA00655 1 20010806 A 5311 FRAME BOEING 727 727247 138408F NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 FUSELAGE FRAME BS 580 UPPER FLANGE HAS DAMAGE BETWEEN STR 23L & 25L. *S/D* REMOVED AND REPLACED FRAME PER SRM 51-4-3 P G 1-6. 2 L 7 3 4F A3WE 2001081500180 20010815 00180 NM 2001 8 15 01FDEA00657 1 20010806 A 5330 SKIN BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 UPON REMOVAL OF STR ON N1173 FOUND CORROSION ON INNER SKIN AT BS 950A+3 TO 950A+6 AT STR 25L (C53-111-01-3). *S/D* REM OVED AND REPLACED SKIN PER SRM 53-30-3 FIG 3. 2 L 7 3 4F A3WE 2001081700051 20010817 00051 NM 2001 8 17 01FDEA00658 1 20010806 A 5330 SKIN BOEING 727 727247 138408F NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CRACK IN FUSELAGE SKIN AT BS 1097.5 1 INCH RIGHT OF STRINGER 1. *S/D* REMOVED AND REPLACED SKIN PER EA 7-5310-58485. 2 L 7 3 4F A3WE 2001081700052 20010817 00052 NM 2001 8 17 01FDEA00659 1 20010804 A 5315 FLOORBEAM BOEING 727 727247 138408F NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 BS 740 FLOORBEAM IS DAMAGED UNDER NUT PLATE LBL 52, AFT FLANGE. *S/D* REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-4 F IG 4. 2 L 7 3 4F A3WE 2001081700053 20010817 00053 NM 2001 8 17 01FDEA00660 1 20010806 A 5310 SHEAR TIE BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSION (C53-111-02, 2) FWD CARGO BAY BS 660, BL 0, WL 147 SHEAR TIE. *S/D* REMOVED AND REPLACED SHEAR TIE PER SRM 5 3-10-4 FIG 15. 2 L 7 3 4F A3WE 2001080600124 20010806 00124 SO 2001 8 6 SIMA200118101 1 20010630 A 3350 375921 SIGN EMB 135 EMB135LR SO CABIN INOPERATIVE A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 737MW 145396 BOS - FLT 4969 - CREW REPORTED THE EMERGENCY EXIT SIGN ABOVE THE AISLE EMERGENCY EXIT TO BE INOPERATIVE, AND WITH SWITCH ES SET TO ARMED THE EMERGENCY LIGHT NOT ARMED CAUTION ILLUMINATED SEVERAL TIMES. MAINTENANCE REMOVED AND REPLACED THE A ISLE EMERGENCY LIGHT. THE EMERGENCY LIGHST NOT ARMED CAUTION LIGHT COULD NOT BE DUPLICATED. OPERATIONAL CHECK OF EMERG ENCY LIGHT SYSTEM WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001080600125 20010806 00125 EU 2001 8 6 SIMA200119706 1 20010712 A 5300 7253813485 FRAME SAAB SF340 340B 7860101 EU FS 677 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 340RC 340B340 ABI - DURING MBV INSPECTION, FOUND FRAME 677 TO BE DAMAGED ON THE RIGHT ABOVE WL 73.5 DAMAGE WAS REPAIRED IAW SRM AND AI RCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001080600126 20010806 00126 EU 2001 8 6 SIMA200119705 1 20010712 A 5300 7253813117 FRAME SAAB SF340 340B 7860101 EU DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 340RC 340B340 ABI - DURING MBV INSPECTION MAINTENANCE, FOUND FRAME 668 TO BE DAMAGED ON THE RIGHT SIDE ABOVE WL 73.5 DAMAGED WAS REPAI RED IAW SAAB SRM AND AIRCRACT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001080600127 20010806 00127 CE 2001 8 6 SIMA200119704 1 20010712 A 5300 7253813007 FRAME BEECH 55 95C55 1152708 CE FS 658.5 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 340B TE333 ABI - DURING MBV INSPECTION MAINTENANCE, FOUND FRAME 658.5 TO HAVE WEB DAMAGE ON THE RIGHT SIDE ABOVE WL 73.5 DAMAGE WAS REPAIRED IAW SAAB 340 SRM AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 1 L 7 2 3O 3A16 2001080600128 20010806 00128 EU 2001 8 6 SIMA200119702 1 20010712 A 5300 7253814451 FRAME SAAB SF340 340B 7860101 EU DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 340RC 340B340 ABI - DURING MBV INSPECTION, MAINTENANCE FOUND FRAME 630.12 WAS DAMAGED ON THE RIGHT SIDE ABOVE WL 73.5. DAMAGE WAS REP AIRED IAW SAAB SRM AND AIRCRAFT WS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001080600129 20010806 00129 NM 2001 8 6 USAA010873 1 20010718 A 5300 SKIN BOEING 737 7373B7 1384580 NM BS 1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 45591 22957 TPA - FOUND PRESSURE BULKHEAD SKIN CORRODED APPROX 4 SQUARE INCH AREA, BS 1016, BETWEEN S28L AND S28R. DAMAGE REMOVED, INSTALLED DOUBLER PER EA 85096 AND SB 737-53A-1075. (M) 2 L 7 2 4F RT A16WE 2001080600130 20010806 00130 NM 2001 8 6 USAA010877 1 20010718 A 5315 FLOORBEAM BOEING 737 7373B7 138447F NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND FLOORBEAM CORRODED, ENTIRE LENGTH OF FLOORBEAM, BS 294.5 STRINGER 17L TO 17R. CORROSION LEVEL 1, TASK NR C5 3-107-02. DAMAGE REMOVED, INSTALLED DOUBLER PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2001080600131 20010806 00131 NM 2001 8 6 USAA010878 1 20010718 A 5315 FLOORBEAM BOEING 737 7373B7 138447F NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND FLOORBEAM CORRODED 18 INCH AREA, BS 986.5, BL 0 TO RBL 18. CORROSION LEVEL 1, TASK NR C53-107-02. REMOVED AND REPLACED T-CAP PER TYPICAL REPAIR 53-10-05A. (M) 2 L 7 2 4F RT A16WE 2001080600132 20010806 00132 NM 2001 8 6 USAA010882 1 20010718 A 5300 STRINGER BOEING 737 7373B7 1384580 NM BS 1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 45591 22957 TPA - FOUND STRINGER CORRODED 4 INCH AREA, STRINGER 26 RIGHT AT STATION 1016. CORROSION LEVEL 2. REPAIRED STRINGER PER SRM 53-00-02 FIG 201. (M) 2 L 7 2 4F RT A16WE 2001080600133 20010806 00133 NM 2001 8 6 USAA010883 1 20010719 A 5310 FRAME BOEING 737 7373B7 1384580 NM BS 1006 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND FRAME CORRODED 6 SQUARE INCH AREA, BS 1006, STRINGER 23R TO FLOOR LEVEL. CORROSION LEVEL 1 TASK NR C53-107- 02. REMOVED DAMAGE, INSTALLED REPLACEMENT FRAME SECTION PER SRM 51-10-02, 51-40-02, 51-40-03. (M) 2 L 7 2 4F RT A16WE 2001080600134 20010806 00134 NM 2001 8 6 USAA010886 1 20010719 A 5310 STRINGER BOEING 737 7373B7 1384580 NM BS 1006-1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND STRINGER CORRODED 6 INCHES BY 1 INCH AREA, BS 1006 TO 1016, STRINGER 26R. REMOVED DAMAGE, SPLICED IN NEW ST RINGER SECTION PER SRM 51-40-04 AND BAC DRAWING NR 65-45776. (M) 2 L 7 2 4F RT A16WE 2001080600135 20010806 00135 NM 2001 8 6 USAA010887 1 20010719 A 5300 STRINGER BOEING 737 7373B7 1384580 NM BS 907-927 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND STRINGER CORRODED 14 INCHES BY 2.5 INCHES, BS 907 TO 927, S25L, BELOW AFT CARGO FLOOR. REMOVED AND REPLACED STRINGER PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2001080600136 20010806 00136 NM 2001 8 6 USAA010888 1 20010719 A 5310 SHEAR TIE BOEING 737 7373B7 1384580 NM BS 807 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND SHEAR TIE CORRODED 1 INCH BY 5 INCH AREA, BS 807, BETWEEN RBL 15 TO 20, AT BELLY SKIN LEVEL. FABRICATED AND REPLACED SHEAR TIE PER SRM 51-10-01 AND BAC DRAWING NR 69-43277. (M) 2 L 7 2 4F RT A16WE 2001080600137 20010806 00137 NM 2001 8 6 USAA010891 1 20010719 A 5230 CHANNEL BOEING 737 7373B7 1384580 NM CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND CHANNEL CORRODED 5 SQUARE INCH AREA CORRODED, AFT CARGO DOOR, LOWER WILL STRUCTURE. REMOVED AND REPLACED CH ANNEL PER SRM 51-10-01 AND 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001080600138 20010806 00138 NM 2001 8 6 USAA010898 1 20010720 A 5300 FRAME BOEING 737 7373B7 1384580 NM BS 727B CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND FRAME CORRODED 14 INCH AREA, BS 727B, LEFT AND RIGHT KEEL BEAMS, LOWER FLANGE. REMOVED DAMAGE, INSTALLED NE W FRAME SECTION PER SRM 51-40-02 AND 51-40-05. (M) 2 L 7 2 4F RT A16WE 2001080600140 20010806 00140 2001 8 6 RRXA011045 4 20010529 A 3442 TRANSCEIVER DOUG DC8 DC873F 302199F WP WEATHER RADAR DEFECTIVE A RRXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 15 605AL 46106 DURING CLIMBOUT, RADAR SMOKING CONTINUOUSLY AND TOTALLY UNUSABLE. REMOVED AND REPLACED WX R/T IAW DC-8 MM 34-40-2. GRO UND CHECK AND OPS GOOD. 2 L 7 4 4F RT 4A25 2001080600142 20010806 00142 NM 2001 8 6 AWXA0002065 1 20010717 A 5310 146N51806 ANGLE BOEING 757 757225 1384959 NM BS 1661 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 D: Aft cargo compartment BS 1661 RBL intercostal topflange cracked.C: replaced angle IAW SRM 53-60-51 2 L 7 2 4F RT A2NM 2001080600143 20010806 00143 NM 2001 8 6 AWXA0002067 1 20010801 A 5310 14N827146 PAN BOEING 757 757225 1384959 NM EXT.POWER RECEPT CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 D: Ext. Power recep. Mounting holes are cracked.C: removed & installed new pan part #14N8271-46 IAW SRM 51-40-02 pg 3,4, 5,11,12 2 L 7 2 4F RT A2NM 2001080600144 20010806 00144 NM 2001 8 6 AWXA0002069 1 20010730 A 5311 65C3453721 CHANNEL BOEING 737 737277 1384570 NM BS 665 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: BS 665 LBL 24 upper chord Cracked.C: Stop drilled and repaired BS 665 LBL 24 WL 207 chord crack IAW AWA ER 15-5702-01 211-JS1 2 L 7 2 4F RT A16WE 2001080600145 20010806 00145 2001 8 6 RRXA011046 4 20010613 A 3421 HARNESS DOUG DC8 DC873F 302199F WP COCKPIT DEFECTIVE A RRXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 792FT 46046 F/O`S GYRO FAILED ON CLIMB IN BOTH NORMAL AND AUX POSITION. REPLACED EXISTING HARNESS IAW 34-2-2 WITH NEW WIRE F/R50-11 9 FORWARD OF F/O'S PANEL BACK TO R50-61 RADIO RACK SHELF NR 3 OPERATIONAL CK IAW DC8 MM CHAP 34-25-0 (CK GOOD). 2 L 7 4 4F RT 4A25 2001080600148 20010806 00148 WP 2001 8 6 RRXA011047 1 20010613 A 2612 ELEMENT DOUG DC8 DC871 302199A WP NR 1 ENGINE FAULTY A RRXA F E A ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 15 811AL 46099 INTERMITTENT FIRE INDICATION ON NR 1 ENG FIRED BOTH BOTTLES AND SHUT DOWN ENG FIRE INDICATIONS STILL WERE INTERMITTENT. WHEN FIRE LIGHT IN HANDLE INTERMITTENT WENT OUT, FIRE TEST WOULD NOT TEST. REMOVED AND REPLACED NR 1 ENG FIRE SENSIN G ELEMENTS IAW DC-8 SEVENTY SERIES M/M 26-10-1. NR 1 ENG FIRE WARNING SYSTEM OPS CHECKS GOOD IAW DC-8 SEVENTY SERIES M /M 26-10-1. NO DEFECTS NOTED. 2 L 7 4 4F 4A25 2001080600153 20010806 00153 WP 2001 8 6 RRXA011048 1 20010619 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 AFTER LANDING DISCOVERED CORROSION ON OUTER FUSELAGE, LEFT LOWER SIDE AT FS 1320. 2 L 7 4 4F RT 4A25 2001080600154 20010806 00154 NM 2001 8 6 0102696717 1 20010801 A 3040 W80710 TERMINAL BOEING 747 747251F 1384898 NM WINDOW L1 BROKEN A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 01 617US 21121 DURING FLIGHT, SMOKE EMMITTED FROM THE ELECTRICAL CONNECTION ON THE LOWER LEFT SIDE OF FLIGHT DECK WINDOW L1. TURNED OFF WINDOW HEAT AND PULLED CIRCUIT BREAKER AND THE SMOKE DISSIPATED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT I NCIDENT. REPLACED WINDOW HEAT TERMINAL D419. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2001080600155 20010806 00155 NM 2001 8 6 0102716612 1 20010801 A 3350 6104781 BATTERY PACK BOEING 747 747251B 1384892 NM D &E ZONES INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING LINE CHECK, FOUND AN OVERWING EXTERIOR EMERGENCY LIGHT INOPERATIVE AND THE LEFT EMERGENCY ESCAPE PATH LIGHTING IN OPERATIVE IN 'D' AND 'E' ZONES. REPLACED BATTERY PACKS. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F A20WE 2001080600156 20010806 00156 NM 2001 8 6 0102736614 1 20010731 A 3350 69B4601036 MODULE BOEING 747 747251B 1384892 NM A NWAA K NONE O OTHER UK UNKNOWN 1 GL 01 614US 20359 DURING PREFLIGHT CHECK, FOUND EMERGENCY LIGHTS WILL NOT ARM. REPLACED EMERGENCY LIGHTS CONTROL MODULE. OPERATIONAL CH ECK NORMAL. 2 L 7 4 4F A20WE 2001080600157 20010806 00157 NM 2001 8 6 0102746641 1 20010731 A 3350 6042225 POWER SUPPLY BOEING 747 747212B 1384886 NM EMER PATH LTS A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 641NW 21941 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE BETWEEN SEAT ROWS 35-45R. REPLACED POWER SUPPLY A ND BATTERY PACK. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F A20WE 2001080600170 20010806 00170 NM 2001 8 6 SWAA012108 1 20010725 A 3350 BR2013 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED 1/4D CHECK, FOUND 3 EEPLS INOP. REMOVED AND REPLACED LIGHT ASSY'S PER MM. 2 L 7 2 4F A16WE 2001080600171 20010806 00171 2001 8 6 SWAA012110 4 20010725 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM R2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001080600172 20010806 00172 NM 2001 8 6 SWAA012112 1 20010725 A 3350 300432 SOCKET BOEING 737 7373H4 1384600 NM EXTERIOR CORRODED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED PMC CHECK, FOUND FWD ENTRY DOOR EXTERNAL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT SOCKET DUE TO CORROSION PER MM. 2 L 7 2 4F RT A16WE 2001080600173 20010806 00173 NM 2001 8 6 SWAA012114 1 20010726 A 5311 BAC5602 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D-CHECK, FOUND 2 Z-FRAMES CRACKED, STR 9R, BS 807 AND BS 887. REPAIRED FRAMES PER SRM. 2 L 7 2 4F RT A16WE 2001080600174 20010806 00174 NM 2001 8 6 SWAA012115 1 20010726 A 2742 6355B000103 ACTUATOR BOEING 737 7377H4 NM STABILIZER INOPERATIVE A SWAA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SW 07 739GB 29275 AIR TURNBACK, STAB TRIM MOTOR INOP. REMOVED AND REPLACED STAB TRIM ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2001080600175 20010806 00175 NM 2001 8 6 SWAA012121 1 20010728 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED C3 CHECK, FOUND EEPLS LOOSE AT AFT GALLEY. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001080600176 20010806 00176 NM 2001 8 6 SWAA012122 1 20010727 A 3350 BR2013 LIGHT BOEING 737 7377H4 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 714CB 27848 EEPLS LOOSE. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001080600177 20010806 00177 NM 2001 8 6 SWAA012123 1 20010727 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 394SW 27380 EEPLS INOP FROM ROW 15 TO ROW 22. REPAIRED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001080600178 20010806 00178 NM 2001 8 6 SWAA012124 1 20010727 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 AFT ENTRY DOOR EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 2001080600179 20010806 00179 NM 2001 8 6 SWAA012126 1 20010726 A 3350 6556633 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 366SW 26577 DURING SCHEDULED C1 CHECK, FOUND RT EMERGENCY EXIT WINDOW OVERHEAD LIGHT LENS LOOSE. SECURED EXIT LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2001080600180 20010806 00180 NM 2001 8 6 SWAA012127 1 20010726 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 636WN 27709 DURING SCHEDULED 1/2D CHECK, FOUND FRAME CHORD CRACKED AT BS 616, RT SIDE LOWER END. REPAIRED CHORD PER SWA RA. 2 L 7 2 4F RT A16WE 2001080600181 20010806 00181 NM 2001 8 6 SWAA012128 1 20010717 A 5315 6546804 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 947.5, LBL 52. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2001080600182 20010806 00182 NM 2001 8 6 SWAA012133 1 20010722 A 5315 6546804 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 312, BETWEEN LBL 12 & RBL 12. REPAIRED FLOORBEAM C HORD PER SRM. 2 L 7 2 4F RT A16WE 2001080600183 20010806 00183 NM 2001 8 6 SWAA012134 1 20010723 A 3350 6556633 LENS BOEING 737 7373Q8 1384670 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D-CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LENS BROKEN AT LT OVERWING EXIT. REMOVED AND REPLACED EXI T LENS PER MM. 2 L 7 2 4F RT A16WE 2001080600184 20010806 00184 NM 2001 8 6 SWAA012137 1 20010729 A 5320 6551698 SPLICE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2001080600185 20010806 00185 NM 2001 8 6 SWAA012139 1 20010723 A 5320 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIPS CRACKED AT BS 440, STR'S 4L & 4R, BS 380, STR 8L & BS 360, STR 4 L. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001080600186 20010806 00186 2001 8 6 SWAA012141 4 20010727 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 367SW 26578 FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001080600187 20010806 00187 NM 2001 8 6 SWAA012142 1 20010728 A 3350 100885 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 304SW 22944 EEPLS LOOSE AT FWD SECTION. SECURED EEPLS, REPAIRED WIRING, REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2001080600188 20010806 00188 NM 2001 8 6 SWAA012144 1 20010729 A 3350 BR2013 LIGHT BOEING 737 7373A4 1384585 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 680AA 23505 EEPLS LOOSE AT ROW 5. INSTALLED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001080600189 20010806 00189 NM 2001 8 6 SWAA012145 1 20010729 A 3350 100885 HOUSING BOEING 737 737301 1384611 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY HOUSING FUSE BROKEN. REMOVED AND REPLACED BATTERY HOUSING PER MM. 2 L 7 2 4F RT A16WE 2001080600190 20010806 00190 NM 2001 8 6 SWAA012146 1 20010729 A 3350 BR2013 COVER BOEING 737 7372T4 1384492 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED C4 CHECK, FOUND EEPLS LOOSE IN SEVERAL PLACES AND MISSING SEVERAL COVERS. SECURED EEPLS AND INSTALLED COVERS. 2 L 7 2 4F A16WE 2001080600191 20010806 00191 NM 2001 8 6 SWAA012147 1 20010729 A 3397 BR2013 WIRE BOEING 737 7375H4 138449D NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 524SW 26566 EEPLS INOP IN NUMEROUS PLACES. RECONNECTED WIRES PER MM. 2 L 7 2 4F RT A16WE 2001080600192 20010806 00192 NM 2001 8 6 SWAA012151 1 20010721 A 5320 6554892 WEB BOEING 737 7373Q8 1384670 NM FUSELAGE CANNING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D-CHECK, FOUND VERTICAL WEB IS OIL CANNED AT BS 312, RBL 28 & WL 206. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001080600193 20010806 00193 NM 2001 8 6 SWAA012155 1 20010721 A 5523 6573782 TAB BOEING 737 7373Q8 1384670 NM LT ELEVATOR DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D-CHECK, FOUND LT ELEVATOR TAB DELAMINATED AT INBOARD CORNER. REPAIRED TAB PER SRM. 2 L 7 2 4F RT A16WE 2001080600194 20010806 00194 NM 2001 8 6 SWAA012157 1 20010728 A 3211 6959886 FITTING BOEING 737 7373H4 1384600 NM LT & RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 382SW 26588 DURING SCHEDULED SVC CHECK, FOUND LT & RT MLG WALKING BEAM HANGER FITTINGS CORRODED. REMOVED AND REPLACED LT AND RT HAN GER FITTING'S PER ALM WORK CARDS AND MM. 2 L 7 2 4F RT A16WE 2001080600195 20010806 00195 NM 2001 8 6 SWAA012158 1 20010728 A 5320 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 520SW 25319 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4R. REMOVED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001080600196 20010806 00196 NM 2001 8 6 SWAA012159 1 20010728 A 5315 6546804 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D-CHECK, FOUND CABIN FLOORBEAM CRACKED AT BS 727B, RT OUTBOARD. REPAIRED FLOORBEAM PER DLF XEA & SRM. 2 L 7 2 4F RT A16WE 2001080600197 20010806 00197 NM 2001 8 6 SWAA012162 1 20010730 A 3350 610978 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT DOOR LIGHTS INOP, BOTH AFT EXTERIOR LIGHTS. REMOVED AND REPLACED LIGHT BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2001080600198 20010806 00198 2001 8 6 SWAA012163 4 20010730 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 073SW 22673 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001080600199 20010806 00199 NM 2001 8 6 SWAA012164 1 20010731 A 2560 P2070001 FLASHLIGHT BOEING 737 7377H4 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 700GS 27835 AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001080600200 20010806 00200 NM 2001 8 6 SWAA012165 1 20010731 A 3397 BR2013 WIRE BOEING 737 7375H4 138449D NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 524SW 26566 EEPLS INOP BETWEEN ROWS 12 & 15. RECONNECTED WIRES PER MM. 2 L 7 2 4F RT A16WE 2001080600201 20010806 00201 NM 2001 8 6 SWAA012166 1 20010730 A 3350 65C34691 LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 OVERHEAD BIN BULL NOSE EMERGENCY LIGHT LOOSE AT ROW 7 ABC. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001080600202 20010806 00202 NM 2001 8 6 SWAA012168 1 20010731 A 3350 300432 LENS BOEING 737 7372H4 138448C NM SERVICE DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED RON CHECK, FOUND FWD SVC DOOR EMERGENCY EXTERIOR EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F A16WE 2001080600203 20010806 00203 2001 8 6 SWAA012169 4 20010731 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001080600204 20010806 00204 2001 8 6 SWAA012170 4 20010731 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001080600205 20010806 00205 NM 2001 8 6 SWAA012172 1 20010724 A 5315 6546804 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D-CHECK, FOUND AFT CABIN FLOORBEAM UPPER T-CHORD CORRODED AT BS 1016, LBL 10. REPAIRED CHORD. 2 L 7 2 4F RT A16WE 2001080600206 20010806 00206 NM 2001 8 6 SWAA012177 1 20010721 A 5315 6546804 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 309.9, LBL 11, FWD CABIN. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2001080600207 20010806 00207 NM 2001 8 6 SWAA012179 1 20010731 A 3350 BR2013 LIGHT BOEING 737 7377H4 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 717SA 27851 EEPLS LOOSE AT ROW 1. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001080600208 20010806 00208 NM 2001 8 6 SWAA012180 1 20010801 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 384SW 26590 EEPLS LOOSE. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001080600209 20010806 00209 NE 2001 8 6 SWIA200110006 2 20010617 A 7532 97962641 BLEED VALVE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE MALFUNCTIONED A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 NM 07 565SW 120340 SMELLED SMOKE ON TAKEOFF. RETURNED TO LAX. REPLACED LEFT ENGINE HIGH PRESSURE BLEED VALVE. RAN ENGINE. OPS CHECK GOO D. P/N: 979626-4-1, S/N ON: 2461, S/N OFF: 2020. 2 L 7 2 4T 4 T RT A31SO E20NE 2001080600210 20010806 00210 SO 2001 8 6 SWIA200110007 1 20010619 A 2910 HYDRAULIC LINE EMB 120 EMB120ER 3260203 SO HYDRAULIC SYS LEAKING A SWIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 07 190SW 120050 WHEN SELECTING GEAR UP ON TAKEOFF, EXPERIENCED COMPLETE LOSS OF HYDRAULIC GREEN SYSTEM. RETURNED TO SLC. REPLACED FLEX LINE LEFT GEAR OUTBOARD LINE OVER DRAG BRACE. 2 L 7 2 4T RT A31SO 2001080600211 20010806 00211 SO 2001 8 6 SWIA200110008 1 20010620 A 2730 PROXIMITY SWITCH EMB 120 EMB120ER 3260203 SO ELEVATOR FAULTY A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 562SW 120336 UPON APPLICATION OF TAKEOFF POWER RECEIVED TRIM AURAL WARNING. REPLACED ELEVATOR RIGHT TRIM PROXIMITY SENSOR WITH SERVI CEABLE UNIT IAW MM 27-32-05. ADJUSTED PROXIMITY SWITCH IAW MM 27-32-00. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2001080600213 20010806 00213 EA 2001 8 6 SWIA200110009 1 20010629 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA CARGO BAY MALFUNCTIONED A SWIA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 NM 07 405SW 7029 SMOKE CARGO MESSAGE AND ASSOCIATED AURAL WARNINGS SOUNDED MOMENTARILY AND THEN EXTINGUISHED. REMOVED AND REPLACED FORWA RD AND AFT SMOKE DETECTORS. OPS CHECK GOOD ON BOTH. FWD S/N ON 2012, S/N OFF 2130, AFT S/N ON 2875, S/N OFF 0326. 2 L 7 2 4F RT A21EA 2001080600214 20010806 00214 SO 2001 8 6 SWIA200110010 1 20010706 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 308SW 59 47 120326 MIDDLE EMERGENCY LIGHTS INOP. REMOVED AND REPLACED MIDDLE ELBP IAW 33-50-02. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001080600216 20010806 00216 SO 2001 8 6 SWIA200110011 1 20010705 A 3350 FUSE EMB 120 EMB120ER 3260203 SO CABIN BLOWN A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 308SW 120326 EMERGENCY LIGHT STRIP IN AISLE INOP. REMOVED AND REPLACED FUSE. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001080600217 20010806 00217 EA 2001 8 6 SWIA200110012 1 20010707 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA T/E FLAP MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION LD LANDING 1 NM 07 406SW 7030 FLAPS FAIL MESSAGE AT RETRACTION AFTER LANDING, FLAPS AT 30 DEGREES. UPON POWER DOWN AT GATE AND RE-POWERING, MESSAGE W ENT AWAY. REMOVED AND REPLACED RIGHT BPSU WITH SERVICEABLE UNIT IAW 27-51-10. FLAPS OPS CHECK GOOD. P/N ON: 855D100- 9, S/N ON: 393B, P/N OFF: 855D100-7, S/N OFF: 206. 2 L 7 2 4F RT A21EA 2001080600219 20010806 00219 SO 2001 8 6 SWIA200110013 1 20010702 A 2752 3430001003 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP WEAK A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 NM 07 218SW 120287 MULTIPLE FLAP DISAGREEMENT WHEN SET TO 45 DEGREES. NORMAL LANDING FLAPS 25 DEGREES. INSPECTED FLAP TRACKS FOR BROKEN/L OOSE HARDWARE, ALL OK. OPERATED ON GROUND, CHECK OK. LUBED ROLLERS CLEANED TRACKS, GROUND OPS GOOD. FOUND LEFT OUTBOA RD FLAP ACTUATOR TO BE WEAK. REPLACED LEFT OUTBOARD FLAP IAW CHAPT 27-50-00 EMB MM. CLEARED ALL FLAP FAULTS. SYSTEM O PS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2001080600223 20010806 00223 NE 2001 8 6 SWIA200110014 2 20010704 A 7200 ENGINE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RIGHT MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 215SW 120281 T6 WARNING OCCURRED AFTER ROTATION WITH TAKEOFF POWER AT CHART VALUE. PEEKED AT 816 DEGREES C AND REDUCED POWER RIGHT S IDE. RAN AIRCRAFT TO TARGET TORQUE IN SLC. BLEEDS CLOSED. MADE 100 PERCENT TORQUE. AT 796 DEGREES T6 WITHIN LIMITS P ER MM 71-00-00. 2 L 7 2 4T 4 T RT A31SO E20NE 2001080600226 20010806 00226 SO 2001 8 6 SWIA200110015 1 20010705 A 3260 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO RT MLG DEFECTIVE A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 560SW 120334 LANDING GEAR LEVER WOULD NOT RELEASE FROM DOWN POSITION ON TAKEOFF. PERFORMED ALTERNATE GEAR RETRACTION PROCEDURE PER T HE QRH. REMOVED AND REPLACED RIGHT STRUT GROUND PROXIMITY SENSOR. CYCLED LANDING GEAR SEVERAL TIMES. OPS AND LEAK CHE CKS GOOD IAW EMB120 MM 32-01-01. P/N: 20505-001-01. 2 L 7 2 4T RT A31SO 2001080600230 20010806 00230 SO 2001 8 6 SWIA200110017 1 20010709 A 5230 SEAL EMB 120 EMB120ER 3260203 SO CARGO DOOR FAILED A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 563SW 120338 CABIN ALT LIGHT ILLUMINATED AND OXYGEN MASKS DEPLOYED. FOUND CARGO DOOR SEAL BLOWN OUT AT TOP AFT PORTION AND BOTTOM AF T PORTION. REPAIRED SEAL AS NEEDED. PRESSURIZED AIRCRAFT AND STOWED OXYGEN MASKS. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2001080600231 20010806 00231 SO 2001 8 6 SWIA200110018 1 20010630 A 5330 ACCESS PANEL EMB 120 EMB120ER 3260203 SO FUSELAGE OPEN A SWIA A UNSCHED LANDING P NO WARNING INDICATION TO TAKEOFF 1 NM 07 295SW 120322 DOOR CONTROL ACCESS PANEL OPENED DURING TAKEOFF ROLL. RETURNED TO LAX. INSPECTED DOOR. NO DEFECT FOUND. RELATCHED DO OR. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001080600234 20010806 00234 SO 2001 8 6 SWIA200110019 1 20010705 A 5753 12033043501 FLAP TRACK EMB 120 EMB120RT SO T/E FLAP DEFECTIVE A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 156CA 120156 FLAP DISAGREEMENT AFTER TAKEOFF WHEN MOVING FLAPS FROM 15 DEGREES TO 0 DEGREES. APPEARS TO BE NACELLE FLAPS REPEATEDLY. PERFORMED FLAP INSPECTION AND FLAP TROUBLESHOOTING. REMOVED LEFT INBOARD FLAP. REPLACED ALL ROLLERS IAW 27-50-12 AND REPLACED OUTBOARD TRACK FOR LEFT INBOARD FLAP IAW 57-53-00. REMOVED AND REPLACED RIGHT INBOARD FLAP AFTER ROLLER CHANG E IAW 27-50-12. P/N: PE61026-1, TRACK P/N: 120-33043-501. 2 L 7 2 4T RT A31SO 2001080600235 20010806 00235 SO 2001 8 6 SWIA200110020 1 20010709 A 3150 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO COCKPIT FALSE ACTIVATION A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 293SW 120320 ON TAKEOFF ROLL AT ABOUT 95 KTS, AURAL WARNING (TAKEOFF, BRAKE, TRIM, FLAPS) WAS ACTIVATED. TAKEOFF WAS ABORTED. UPDAT E 7/10/2001: TAKEOFF TRIM AURAL WARNING GOES OFF WITH THE INDICATOR .5 INCH WITHIN THE GREEN BAND. POWERED DOWN SYSTEM. TEST NO GOOD. RE-RACKED AND POWERED DOWN SYSTEM. OPS CHECK GOOD AT THIS TIME. UPDATE 7/10/2001: ADJUSTED TRIM PROX IMITY SENSORS IAW 27-32-06. GROUND OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2001080600237 20010806 00237 SO 2001 8 6 SWIA200110021 1 20010603 A 5230 CABLE EMB 120 EMB120ER 3260203 SO CARGO DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 209SW 120269 BOTH TOP, OUTBOARD CABLES ON CARGO DOOR CORRODED. FOUND DURING C-CHECK. REMOVED AND REPLACED BOTH OUTBOARD CABLES IAW MM 52-31-00. P/N 120-32772-003, P/N 120-32772-007. 2 L 7 2 4T RT A31SO 2001080600238 20010806 00238 SO 2001 8 6 SWIA200110022 1 20010709 A 2841 CONNECTOR EMB 120 EMB120ER 3260203 SO COCKPIT LOOSE A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 290SW 120317 RIGHT HAND FUEL QUANTITY GAUGE FLUCTUATES APPROXIMATELY 300 LBS. DEFERRED PER MEL. FOUND LOOSE BACKSHELL ON THE RIGHT FUEL QUANTITY INDICATOR CANNON PLUG. TIGHTENED BACKSHELL. PERFORMED OPS CHECK IAW MM 28-42-00. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001080600239 20010806 00239 EA 2001 8 6 SWIA200110023 1 20010707 A 3620 355483255 DETECTOR CNDAIR CL600 CL6002B19 EA PNEUMATIC SYS FAULTY A SWIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 07 496SW 7473 WING ANTI-ICE SWITCH ON OR OFF, ANTI-ICE DUCT MASTER WARNING MESSAGE ILLUMINATED. COMPLIED WITH QRH PROCEDURES. RETUR NED TO SLC. REPLACED LEFT WHEEL WELL DUCT LEAK DETECTOR. P/N ON 35548-3-255, OPS CHECK GOOD IAW 36-12-00 AND 36-21-04. 2 L 7 2 4F RT A21EA 2001080600241 20010806 00241 SO 2001 8 6 SWIA200110024 1 20010608 A 5320 SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 1117H 120120 LEFT FRAME 9 SUPPORT UNDER FORWARD DIRECT VISION WINDOW CRACKED. REPAIRED IAW EMB 120 SERVICE BULLETIN 120-53-0045 DATE D AUG 6, 92. REWORK TO INNER REINFORCING PLATE ATTACHING WINDSHIELD POST TO FRAME 9. 2 L 7 2 4T RT A31SO 2001080600248 20010806 00248 WP 2001 8 6 UPS01836339 1 20010630 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 STA 1100 TO 1120 RBL 24 SEAT TRACK IS CORRODED BEYOND LIMITS. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A. 2 L 7 4 4F RT 4A25 2001080600249 20010806 00249 WP 2001 8 6 UPS01836341 1 20010710 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C1,3 INTERCOSTAL CRACKED IN FWD END OF UPPER RADIUS LONG 31L STA 1620 - 1640 AFT ACCESSORY COMPT. 2 L 7 4 4F RT 4A25 2001080600256 20010806 00256 WP 2001 8 6 UPS01836342 1 20010716 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C1,3 DAMAGED FRAME AT FASTENER HOLE AND MISSING MOUNT CLIP AT FRAME 180 26R. FOUND FRAME DAMAGE TO BE C RACKED FLANGE AT ATTACHMENT HOLE. 2 L 7 4 4F RT 4A25 2001080600259 20010806 00259 WP 2001 8 6 UPS01836343 1 20010710 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C1,3 STA 470 TRACK G HAS CORROSION DOWN CTR. FOUND TO BE BEYOND ALLOWABLE LIMITS IAW DC8 SRM 53-2-3 FIG 12. 2 L 7 4 4F RT 4A25 2001080600261 20010806 00261 WP 2001 8 6 UPS01836345 1 20010702 A 5730 576958989 DOUBLER DOUG DC8 DC873F 302199F WP RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 RIGHT WING L/E LIFT TRANSDUCER DOUBLER IS CORRODED BEYOND LIMITS BETWEEN STA XFS 372.75 TO XFS 379. 2 L 7 4 4F RT 4A25 2001080600262 20010806 00262 WP 2001 8 6 UPS01836346 1 20010705 A 5320 WEB DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 MAIN CABIN CUSP MEMBRANE IS CORRODED BEYOND LIMITS AT STA 1580 LBL 48-50. REPAIRED WEB IAW SRM 53-2- 0 FIG 23. 2 L 7 4 4F RT 4A25 2001080600263 20010806 00263 WP 2001 8 6 IXXA0100041S 1 20010315 A 5340 INTERCOSTAL DOUG DC8 DC871F 302199D WP NOSE CORRODED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 820BX 79927 2852 46065 DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON INTERCOSTAL AT FUSELAGE STATION 8 LONGERON 35 RIGHT. REPAIR ACCOMPLISHED REMOVAL OF INTERCOSTAL, FABRICATION AND INSTALLATION AN NEW INTERCOSTAL IN ACCORDANCE WITH DOUGLAS DRAWING 5615530 AND ENINEERING ORDER 53-DC8-1779. 2 L 7 4 4F RT 4A25 2001080600264 20010806 00264 WP 2001 8 6 IXXA0100042S 1 20010315 A 5311 FRAME DOUG DC8 DC871F 302199D WP MAIN CABIN GOUGED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 820BX 79927 2852 46065 DURING ROUTINE C CHEACK INSPECTION, A GOUGE WAS DETECTED ON FUSELAGE FRAME AT FUSELAGE STATION 1520, LONGERON 17 LEFT. R EPAIR ACCOMPLISHED BLENDED GOUGE AND FABRICATED AND INSTALLED REPAIR DOUBLEERS IN ACCORDANCE WITH DOUGLAS STRUCTURAL REP AIR MANUAL AND ENGINEERING ORDER 53-DC8-1768. 2 L 7 4 4F RT 4A25 2001080600265 20010806 00265 WP 2001 8 6 IXXA0100043S 1 20010308 A 5712 RIB DOUG DC8 DC871F 302199D WP LEFT WING GOUGED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 820BX 79927 2852 46065 DURING ROUTINE C CHECK INSPECTION, A GOUGE WAS DETECTED ON THE LEFT WING LEADING EDGE RIB AT STATION XFS 445. REPAIR ACC OMPLISHED FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEE RING ORDER 57-DC8-1767. 2 L 7 4 4F RT 4A25 2001080600266 20010806 00266 WP 2001 8 6 IXXA0100044S 1 20010308 A 5712 RIB DOUG DC8 DC871F 302199D WP RIGHT WING CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 820BX 79927 2852 46065 DURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON THE RIGHT WING LEADING EDGE RIB BETWEEN ACCESS PANELS 519A AN D 519B. REPAIR ACCOMPLISHED FABRICATION AND INSTALLATION OF REPAIR ANGLE IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MA NUAL AND ENGINEERING ORDER 57-DC8-1765. 2 L 7 4 4F RT 4A25 2001080600267 20010806 00267 WP 2001 8 6 IXXA0100045S 1 20010313 A 5312 STIFFENER DOUG DC8 DC871F 302199D WP NOSE CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 820BX 79927 2852 46065 DURING ROUTINE C CHECK INSPECTION, CRACKS WERE DETECTED ON THE FORWARD BULKHEAD LOWER STIFFENER AT FUSELAGE STATION -156 . REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTUAL REPAIRE MANUAL AND ENGINEERING ORDER 53-DC8-1771. 2 L 7 4 4F RT 4A25 2001080600268 20010806 00268 WP 2001 8 6 IXXA0100047S 1 20010308 A 5712 RIB DOUG DC8 DC871F 302199D WP CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 820BX 79927 2852 46065 DURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON THE RIGHT WING LEADING EDGE LOWER RIB OUTBOARD ACCESS PANEL 5 18. REPAIR ACCOMPLISHED STOP DRILLING CRACK, FABRICATION AND INSTALLATION A REPAIR ANGLE IN ACCORDANCE WITH DOUGLAS STRU CTURAL REPAIR MANUAL 57-2-0 AND ENGINEERING ORDER 57-DC8-1764. 2 L 7 4 4F RT 4A25 2001080600269 20010806 00269 WP 2001 8 6 IXXA0100048S 1 20010307 A 5101 57043495 PAN DOUG DC8 DC871F 302199D WP CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 820BX 79927 2852 46065 DURING ROUTINE C CHECK INSPECTION, THE "A" PIT BASKET DOOR AFT CENTER SECTION DOOR PAN WAS FOUND CRACKED. REPAIR ACCOMPL ISHED REMOVAL OF DAMAGED PAN, FABRICATION AN INSTALLATION A NEW SIDE PAN IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MA NUAL, DACO DRAWING 5704349 AND ENGINEERING ORDER 52-DC8-1763. 2 L 7 4 4F RT 4A25 2001080600270 20010806 00270 WP 2001 8 6 UPS01836349 1 20010630 A 5320 4772397U1 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 STA 1772 LONG 17R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397 AND SRM 53-1- 0, 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001080600271 20010806 00271 WP 2001 8 6 UPS01836350 1 20010628 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 STA 1773 LONG 17R IS CRACKED. REPAIRED LONGERON IAW SRM 53-2-3 FIG 5. 2 L 7 4 4F RT 4A25 2001080600272 20010806 00272 WP 2001 8 6 UPS01836351 1 20010625 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 397.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001080600273 20010806 00273 WP 2001 8 6 UPS01836352 1 20010626 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 678.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001080600274 20010806 00274 WP 2001 8 6 UPS01836353 1 20010624 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 FUSELAGE SKIN IS CRACKED AT STA 1766 AT LONG 15R. REPAIRED SKIN IAW SRM 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 2001080600275 20010806 00275 WP 2001 8 6 UPS01836354 1 20010626 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 STA 1620 - 1660 SEAT TRACK IS CORRODED BEYOND LIMITS AT BL 0. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A. 2 L 7 4 4F RT 4A25 2001080600278 20010806 00278 WP 2001 8 6 UPS01836355 1 20010627 A 5511 5654549502 SPAR CAP DOUG DC8 DC873F 302199F WP HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 RIGHT HORIZONTAL STAB UPPER FORMER/CAP IS CRACKED AT XFS 47.5. REMOVED AND REPLACED CAP IAW DWG 5654 549 AND SRM 55-1-0, 51-1-20D, 51-1-21, 51-3-0. 2 L 7 4 4F RT 4A25 2001080600280 20010806 00280 WP 2001 8 6 UPS01836356 1 20010625 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 STA 160 LONG 10R FUSELAGE SKIN IS CRACKED AT FWD UPPER CORNER OF R-1 DOOR OPENING. REPAIRED SKIN IAW SRM 53-2-0 FIG 14. 2 L 7 4 4F RT 4A25 2001080600281 20010806 00281 WP 2001 8 6 UPS01836357 1 20010625 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 STA 1600 AT LONG 20L FWD LOWER CORNER OF L-2 DOOR FUSELAGE SKIN IS CRACKED. REPAIRED SKIN IAW SRM 53 -2-0 FIG 18. 2 L 7 4 4F RT 4A25 2001080600282 20010806 00282 WP 2001 8 6 UPS01836358 1 20010625 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 STA 940 - 960 LONG 24L IS CRACKED. REPAIRED LONGERON IAW SRM 53-2-2 FIG 5. 2 L 7 4 4F RT 4A25 2001080600283 20010806 00283 WP 2001 8 6 UPS01836359 1 20010626 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT STA XRS 79. REPAIRED SKIN IAW SRM 57-2-1 FIG 10. 2 L 7 4 4F RT 4A25 2001080600284 20010806 00284 WP 2001 8 6 UPS01836360 1 20010626 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT XRS 74 STRINGER 10. REPAIRED SKIN IAW SRM 57-2-1 FIG 10. 2 L 7 4 4F RT 4A25 2001080600285 20010806 00285 WP 2001 8 6 UPS01836361 1 20010626 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT XRS 79 AT STRINGER 9. REPAIRED SKIN IAW SRM 57-2-1 FIG 10. 2 L 7 4 4F RT 4A25 2001080600287 20010806 00287 WP 2001 8 6 UPS01836362 1 20010626 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT XRS 79 AT STRINGER 15. REPAIRED SKIN IAW SRM 57-2-1 FIG 10. 2 L 7 4 4F RT 4A25 2001080600288 20010806 00288 WP 2001 8 6 UPS01836374 1 20010705 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 RIGHT WING I/B LOWER SKIN IS CRACKED AT XFS 570. REPAIRED SKIN IAW EO DC8-5720-7767-A. 2 L 7 4 4F RT 4A25 2001080600289 20010806 00289 WP 2001 8 6 UPS01836375 1 20010710 A 5320 3640887N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 STA 980 LBL 24 T-FITTING IS CRACKED IN SUB FLOOR. REMOVED AND REPLACED FITTING IAW DWG 3640887 AND S RM 53-1-0, 51-3-1, 51-1-20D. 2 L 7 4 4F RT 4A25 2001080600291 20010806 00291 WP 2001 8 6 UPS01836376 1 20010713 A 5312 PRESSURE PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 STA 980 LBL 24 PRESSURE WEB IS CORRODED BEYOND LIMITS. REPAIRED PRESSURE WEB IAW 8110-3 APPROVED DH SK 807-306. 2 L 7 4 4F RT 4A25 2001080600292 20010806 00292 WP 2001 8 6 UPS01836377 1 20010626 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 STA 1580 LBL 24 FLOORBEAM IS CORRODED BEYOND LIMITS. REPAIRED FLOORBEAM IAW 8110-3 APPROVED DH SK 80 7-644. 2 L 7 4 4F RT 4A25 2001080600293 20010806 00293 WP 2001 8 6 UPS01836378 1 20010626 A 5320 4641326 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 STA 1690 LONG 33R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641326 AND SRM 51-3- 1, 51-1-21. 2 L 7 4 4F RT 4A25 2001080600294 20010806 00294 WP 2001 8 6 UPS01836379 1 20010625 A 5711 SPAR CAP DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 STA 855 LT WING REAR SPAR LOWER CAP IS CRACKED FROM XCW 0 TO XCW 10. REPAIRED SPAR IAW 8110-3 APPROV ED DH SK 807-357. 2 L 7 4 4F RT 4A25 2001080600295 20010806 00295 WP 2001 8 6 UPS01836381 1 20010709 A 5320 3754918U1 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 STA 1188 LONG 20R UPPER CUSP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW 3754918 AND SRM 53 -1-0, 51-1-20D. 2 L 7 4 4F RT 4A25 2001080600297 20010806 00297 WP 2001 8 6 UPS01836382 1 20010711 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C2 RIGHT WING L/E LOWER RIB IS CRACKED AT XFS 622.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001080600299 20010806 00299 WP 2001 8 6 UPS01836384 1 20010720 A 3350 LIGHT DOUG DC8 DC873F 302199F WP ENTRY DOOR INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:N/A, LIGHT INOP IN EMERGENCY LIGHT ASSY AT ENTRY DOOR. RELAMPED AS REQ, EMERGENCY LIGHTS CK GOOD. 2 L 7 4 4F RT 4A25 2001080600300 20010806 00300 WP 2001 8 6 UPS01836396 1 20010719 A 5312 BULKHEAD DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C1,3 LT AFT PRESSURE BULKHEAD STA 1766 L11L IS CRACKED. 2 L 7 4 4F RT 4A25 2001080600302 20010806 00302 WP 2001 8 6 UPS01836398 1 20010719 A 5320 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C1/3 FS 680 L10R LONGERON END FITTING CRACKED. REMOVED CRACKED 3779762-1 LONGERON END FITTING. INSTALLE D NEW LONGERON END FITTING IAW DC8 SRM 51-3-0, 51-1-23 AND 51-1-24. 2 L 7 4 4F RT 4A25 2001080600304 20010806 00304 NM 2001 8 6 UPS01M36158 1 20010411 A 5347 S49291477075T65 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 250UP INSPECTION TYPE:C MAIN DECK, SEAT TRACK RBL 75 CORRODED AT BS 898 TO BS 822. 2 L 7 3 4F RT A22WE 2001080600313 20010806 00313 NM 2001 8 6 VNAA0107007 1 20010704 A 2520 PSU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN MALFUNCTIONED A VNAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 434JS 3051 FLIGHT 4012 WAS APPROXIMATELY 50 NM NE OF LEX AND THE FLIGHT ATTENDANT NOTIFIED THE CREW OF A BURNING SMELL IN THE CABIN . THE CAPTAIN VERIFIED THE SMELL. THE CAPTAIN DETERMINED IT WAS COMING FROM THE FORWARD PART OF THE CABIN. THE CREW C ONTACTED DISPATCH AND MAINTENANCE CONTROL AND WERE ADVISED TO DIVERT TO THE NEAREST SUITABLE AIRPORT. MECHANICS FROM DAY INSPECTED AND REPLACED THE PASSENGER SERVICE UNIT AT 3A IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 25-00-00. OPERA TIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. AFTER FURTHER TROUBLESHOOTING, OF THE PASSENGER SERVICE UNIT, IT IS SUSPECTED THAT THERE WAS A CONNECTION PROBLEM. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001080600316 20010806 00316 NM 2001 8 6 VNAA0107008 1 20010706 A 2432 DTSP400L BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NR 2 DEFECTIVE A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 436JS 11570 3052 THE CREW RECEIVED A BATTERY OVERHEAT INDICATION ON THE RED WARNING PANEL APPROXIMATELY TEN MINUTES OUT OF DAY. THE CREW CONTACTED MAINTENANCE CONTROL AND WAS ADVISED TO RETURN TO DAY. MAINTENANCE INSPECTED AND REPLACED THE NR 2 BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RETURNED T O SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001080600317 20010806 00317 WP 2001 8 6 CALA0100737 1 20010803 A 5320 WEB DOUG DC9 DC982 3022082 WP STA 370 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND FORWARD CARGO TORQUE BOX WEB CORRODED AROUND FASTENER HOLES AT STA 370. THE TORQUE BOX WEB AND SUPPORT ANGLE WERE REMOVED IAW SRM 51-10-4 AND 51-30-2. A REPAIR WEB AND SUPPORT ANGLE WERE INSTALLED IAW SRM51-30-2. 2 L 7 2 4F A6WE 2001080600318 20010806 00318 WP 2001 8 6 CALA0100738 1 20010803 A 5230 BRACKET DOUG DC9 DC982 3022082 WP FWD CARGO DR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND A 1" CRACK IN T-BRACKET OF FORWARD CARGO DOOR UPPER INTERNAL PAN FORWARD OF AFT HINGES. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 2001080600319 20010806 00319 WP 2001 8 6 CALA0100739 1 20010803 A 5522 SKIN DOUG DC9 DC982 3022082 WP R/H ELEVATOR GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND R/H ELEVATOR LOWER SKIN SURFACE O/B OF TRIM TAB PUSH ROD FAIRING GOUGED. THE SKIN WAS REMOVED AND A REP AIR DOUBLER WAS INSTALLED IAW SRM 51-70-2 AND 55-03. 2 L 7 2 4F A6WE 2001080600320 20010806 00320 WP 2001 8 6 CALA0100741 1 20010804 A 5311 FRAME DOUG DC9 DC982 3022082 WP FS 1271 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND FRAME CORRODED AT FS 1271 FROM LONGERON 27L TO 27R. THE CORRODED AREA OF FRAME WAS CUT OUT IAW SRM 53-0 3, FIGURE 2A. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 2A, 53-10-3, AND 53-03, FIGURE 2A. 2 L 7 2 4F A6WE 2001080600321 20010806 00321 NM 2001 8 6 VNAA0107010 1 20010708 A 2131 CONTROLLER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN PRESSURE MALFUNCTIONED A VNAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 434JS 3051 DURING CLIMBOUT THE CABIN FAILED TO PRESSURIZE AND MAINTENANCE DECIDED TO MEL THE PRESSURIZATION. DUE TO FUEL CONSIDERA TION AT THE LOWER ALTITUDE FLIGHT 4021 DIVERTED TO DAY FOR REFUELING. FLIGHT 4021 THEN CONTINUED TO PIT WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001080600323 20010806 00323 NM 2001 8 6 VNAA0107013 1 20010709 A 3150 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 426JS 3038 DURING THE TAKEOFF ROLL, THE CREW RECEIVED A ENGINE MISCOMPARE CAS MESSAGE. THE CREW ABORTED TAKEOFF AND EXITED THE RUN WAY. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND THE MESSAGE CLEARED. FLIGHT 4043 WAS CLEARED FOR ANOTHER TAKEO FF ATTEMPT AND DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001080600324 20010806 00324 2001 8 6 JBXA000312 4 20010803 A 3417 8220372140 ADC CNDAIR CL600 CL6002B19 EA FAILED A JBXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 05 583ML 7327 Discrepancy : Takeoff roll differance in IAS of 20 knots also IAS caution in F/O's display during rollout abort had EFIS Comp MON caution and T/O Config. Corrective Action : Removed and reinstalled #1 ADC Removed and replaced #2 ADC I-A-W A MM 34-13-01 ops check good. 2 L 7 2 4F RT A21EA 2001080600326 20010806 00326 2001 8 6 VNAA0107015 4 20010712 A 3425 7015327901 FLIGHT DIR DORNER DO32 DO328100 2996000 NM COCKPIT SHORTED A VNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 422JS 11479 1591 3018 FLIGHT 4172 WAS BOARDED AND MAINTENANCE NEEDED TO REPLACE THE VERTICAL SPEED BUTTON ON THE FLIGHT DIRECTOR PANEL. A SHO RT OCCURRED AND THE COCKPIT FILLED WITH SMOKE. THE PASSENGERS WERE DEPLANED AND FLIGHT 4172 WAS CANCELED. MAINTENANCE INSPECTED AND REPLACED THE FLIGHT DIRECTOR PANEL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 22-00-00. OPERATIONAL TE STED WERE COMPLETED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A45NM 2001080600330 20010806 00330 NM 2001 8 6 VNAA0107016 1 20010716 A 3246 26104851 WHEEL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NLG VIBRATION A VNAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 07 436JS 201 3052 AFTER ROTATION, THE CREW FELT A VIBRATION COMING FROM THE NOSE GEAR. THE CREW LOWERED THE GEAR ASSUMING THAT THERE WAS A BLOWN TIRE. MAINTENANCE CONTROL REQUESTED FLIGHT 4169 CONTINUE TO PIT FOR MAINTENANCE BUT THE CREW FELT IT WOULD BE S AFER TO LAND BACK AT AZO. THE CREW DECLARED AN EMERGENCY AND LANDED AT AZO WITH NO FURTHER INCIDENTS. MAINTENANCE INSP ECTED AND REPLACED THE NOSE WHEELS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERF ORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001080600332 20010806 00332 NM 2001 8 6 VNAA0107017 1 20010716 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 438JS 10794 391 3056 THE CREW REPORTED THAT THE EMERGENCY LIGHTING WAS NOT ILLUMINATING AT ROWS 8 TO 10. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 7LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WE RE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001080600335 20010806 00335 NM 2001 8 6 VNAA0107020 1 20010720 A 2432 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE MAIN BATTERY MALFUNCTIONED A VNAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 07 431JS 3028 EN ROUTE TO CLT, THE CREW RECEIVED A MAIN BATTERY OVERHEAT CAS MESSAGE. FLIGHT 4044 RETURNED TO CAK FOR MAINTENANCE. M AINTENANCE INSPECTED AND REPLACED A TEMPERATURE SENSOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIO NAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001080600337 20010806 00337 NM 2001 8 6 Z0A0106004 1 20010727 A 2530 ODOR BOEING 717 717200 1383700 NM GALLEY DETECTED A ZW0A H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 13 416TW 55083 DURING CRUISE THERE WAS A BURNING ELECTRICAL ODOR IN THE FWD GALLEY. THE CREW TURNED OFF POWER TO THE FWD GALLEY. ALL EQUIPMENT IN AND AROUND THE GALLEY WERE CHECKED. THERE WERE NO PARTS REPLACED AND THE CONDITION COULD NOT BE DUPLICATED . LAST CHECK C NONE. 2 L 7 2 4F TR A6WE 2001080600339 20010806 00339 WP 2001 8 6 ZW0A0102901 1 20010531 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND CORROSION ON NUMBER 2 SEAT TRACK AT LBL 44 INCHES STA 1031 TO 1309. REPLACED TRACK AT STA 10 31 TO 1307, LBL 44 INCHES, PER SRM 53-05, PAGE 11, SRM 53-24-0, AND IPC 53-40-00. 2 L 7 2 4F RT A6WE 2001082400232 20010824 00232 NM 2001 8 24 UPS01436533 1 20010803 A 5330 SKIN BOEING 747 747200 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 524UP INSPECTION TYPE:IN BELLY SKIN AT STA 700 TO STA.780 AT LT SIDE ABOUT 24 INCHES FROM BOTTOM CENTER OF SKIN HAS 4 INCH CRA CK WITH SEVERE CORROSION. CUT OUT DAMAGE (CORROSION) AS PER SRM 51-10. VERIFIED DAMAGE REMOVED INTERIM REPAIR COMPLETED AS PER EO B747-5330-15107A. NO REINSPECTIONS, PERMANENT REPAIR BY "C" CHECK. 2 L 7 4 4F RT A20WE 2001080600340 20010806 00340 WP 2001 8 6 ZW0A0102902 1 20010531 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND CORROSION ON CABIN MEMBRANE AT STA 598 TO 617, LT SIDE. 2 L 7 2 4F RT A6WE 2001080600341 20010806 00341 WP 2001 8 6 ZW0A0102903 1 20010531 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT IN MID CARGO COMPT FOUND CORROSION ON LOWER AND UPPER SIDE OF MEMBRANE, BETWEEN STA 655 AND 674. 2 L 7 2 4F RT A6WE 2001080600343 20010806 00343 WP 2001 8 6 ZW0A0102904 1 20010601 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND CORROSION ON LONGERONS 26L, 25L, AND 24L JUST FWD OF STA 1338. 2 L 7 2 4F RT A6WE 2001080600347 20010806 00347 WP 2001 8 6 ZW0A0102905 1 20010531 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND CORROSION ON LONGERON 23R, BETWEEN STA 1322 AND 1338. 2 L 7 2 4F RT A6WE 2001080600349 20010806 00349 WP 2001 8 6 ZW0A0102906 1 20010531 A 5347 GALLEY TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND CABIN GALLEY TIE DOWN CORRODED AT STA 211, RBL 11. 2 L 7 2 4F RT A6WE 2001080600351 20010806 00351 WP 2001 8 6 ZW0A0102907 1 20010601 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND LUGS ON TRACK NUMBER 1 HAD BEEN GROUND AT AN ANGLE, STA 860 TO 916. 2 L 7 2 4F RT A6WE 2001080600353 20010806 00353 WP 2001 8 6 ZW0A0103001 1 20010531 A 5320 DOUBLER DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 929TW 48014 DURING CHECK-C MAINT FOUND OLD REPAIR ON MEMBRANE HAD CRACKED, STA 905 TO 927, LONGERON 18R. REPLACED DOUBLER PER SRM 5 3-01, PAGE 9. 2 L 7 2 4F A6WE 2001080600354 20010806 00354 WP 2001 8 6 ZW0A0103003 1 20010605 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 907TW 49165 DURING CHECK-C MAINT FOUND LIGHT CORROSION ON METAL FLOOR PANEL APPROX STA 197 TO 200, RBL 52 TO 57. REMOVED AND FABRIC ATED NEW PANEL. 2 L 7 2 4F A6WE 2001080600355 20010806 00355 WP 2001 8 6 ZW0A0103004 1 20010604 A 5312 BULKHEAD DOUG DC9 DC982 3022082 WP FUSELAGE WORN A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 929TW 48014 DURING CHECK-C MAINT FOUND WORN AREA ON STRINGER 1380, BULKHEAD, UPPER LT SIDE, FWD FACE APPROX 11 O'CLOCK. INSTALLED 0 .050 DOUBLER OVER RUB AREA PER SRM 53-01. 2 L 7 2 4F A6WE 2001080600358 20010806 00358 WP 2001 8 6 ZW0A0103005 1 20010605 A 5320 BRACKET DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 929TW 48014 DURING CHECK-C MAINT IN THE FWD CARGO COMPT FOUND CRACK IN TRACK TO FORMER BRACKET, STA 237, FWD SIDE, BETWEEN LONGERON 27 AND 28L, AND BETWEEN LONGERON 27 AND 28R. 2 L 7 2 4F A6WE 2001080600360 20010806 00360 WP 2001 8 6 ZW0A0103006 1 20010605 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 929TW 48014 DURING CHECK-C MAINT FOUND ANGLE CORRODED AT STA 1155, LONGERON 29R TO 28R, AND AT STA 1212, STRINGER 29R TO 28R. REMOV ED CORRODED ANGLES AND REPLACED WITH NEW. 2 L 7 2 4F A6WE 2001080600362 20010806 00362 WP 2001 8 6 ZW0A0103008 1 20010605 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND CABIN FLOOR TRACK NUMBER 6 HAD INNER GRANULAR CORROSION AT STA 482. REMOVED CORRODED SECTION OF NUMBER 6 TRACK AT STA 482. 2 L 7 2 4F RT A6WE 2001080600364 20010806 00364 WP 2001 8 6 ZW0A0103009 1 20010606 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9615W 53562 DURING CHECK-C MAINT FOUND CLASS 3 REPAIR INSTALLED AT STA 235, LONGERON 17L TO 18L. REMOVED OLD REPAIR. CUT OUT DAMAG ED SKIN AND INSTALLED FLUSH CLASS 1 REPAIR PER SRM 53-10-107. 2 L 7 2 4F RT A6WE 2001080600365 20010806 00365 WP 2001 8 6 ZW0A0103010 1 20010606 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9615W 53562 DURING CHECK-C MAINT FOUND FUSELAGE DENT IN SKIN AT STA 229, LONGERON 19L, A 2 IN CLASS 3 REPAIR INSTALLED. REMOVED OLD REPAIR DOUBLER AND DAMAGED SKIN. INSTALLED REPAIR PER SRM 53-10-107. PLUGGED HOLES AND INSTALLED FASTENERS PER SRM 51 -30. PAINTED ON WORK ORDER. 2 L 7 2 4F RT A6WE 2001080600368 20010806 00368 WP 2001 8 6 ZW0A0103011 1 20010606 A 5320 STRUCTURE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9615W 53562 DURING CHECK-C MAINT FOUND FUSELAGE CRACK IN RT AFT ACCESS SECTION VENT BOX AT STA 1510. CRACK STOP DRILLED FOR INTERIM REPAIR PER ARA 13888. ACCOMPLISHED EDDY CURRENT PER NDT 53-00-03 PART AND CRACK CONTAINED. STOP DRILLED CRACK. REPAI RED PER SRM 53-01 FIG 2. 2 L 7 2 4F RT A6WE 2001080600369 20010806 00369 NM 2001 8 6 ZW0A0103201 1 20010609 A 3350 80741 LIGHT BOEING 767 76733AER 1385230 NM CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 637TW 25403 THE EGRESS LIGHTS WERE INOPERATIVE AT SEATS 17A AND 32A. REPLACED FLEX LAMPS AT BOTH LOCATIONS. CHECK-C 1-27-01 LAX. 2 L 7 2 4F RT A1NM 2001080600370 20010806 00370 WP 2001 8 6 ZW0A0103202 1 20010608 A 3350 58222 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ZW0A K NONE O OTHER CR CRUISE 1 CE 13 9305N 49395 IN FLIGHT THE EGRESS LIGHTS AT ROWS 15 TO 22 ILLUMINATED. REPLACED THE BATTER PACK. CHECK-C 5-7-01 STL. 2 L 7 2 4F RT A6WE 2001080600372 20010806 00372 WP 2001 8 6 ZW0A0103203 1 20010608 A 3350 58222 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ZW0A K NONE O OTHER CR CRUISE 1 CE 13 904TW 49156 THE EGRESS LIGHTS CAME ON INTERMITTENTLY IN FLIGHT. REPLACED THE POWER SUPPLY. CHECK-C 5-18-2001. 2 L 7 2 4F A6WE 2001080600374 20010806 00374 NM 2001 8 6 ZW0A0103204 1 20010608 A 3350 80761 LIGHT BOEING 767 7673Y0 NM CABIN MISSING A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 638TW 26205 THE EGRESS LIGHT WAS MISSING AT SEAT ROW 3. INSTALLED NEW FLEX LAMP. CHECK-C 5-12-01 LAX. 2 L 7 2 4F RT A1NM 2001080600390 20010806 00390 SO 2001 8 6 C2XA01CL183 1 20010805 A 3231 21180100009 ACTUATOR EMB 145 EMB145LR SO NOISY A C2XA O OTHER O OTHER CL CLIMB 1 SW 27 14950 7689 145061 CLE FLIGHT#4119 THE CREW REPORTED THEY HEARD A "BANG" NOISE DURING GEAR RETRACTION.THE SOUND WA S COMING FROM THE NOSE A REA.MAINTENANCE INSPECTED AND REPLACED THE LEFT NOSE GEAR DOOR ACTUATOR.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RE LEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001080600404 20010806 00404 CE 2001 8 6 GLBA2001173 1 20010805 A 3200 1123640215 CIRCUIT BOARD BEECH 1900 1900D 1154162 CE A119 INTERMITTENT A GLBA D RETURN TO BLOCK O OTHER CL CLIMB 1 CE 01 195GL 675 UE195 WARNIG HORN AND INTRANSIT LIGHT WITH GEAR RETRACTED, REPLACED PCB OPS CHECKED SATISFACTORY 2 L 7 2 4T RT A24CE 2001080600405 20010806 00405 NE 2001 8 6 MALA010608 2 20010803 A 7530 BLEED BAND BAC 146 AVRO146RJ85A 1500097 EU LF507 LF5071F NE DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 508XJ E2318 During Flight #3592 #1 Engine on climbout exceeded N1 Ref Temp. Air turnback to DTW. Maintenance removed and replaced #1 Engine Bleed Band. All checks good. 2 H 7 4 4F 4 F RT A49EU E6NE 2001080600406 20010806 00406 EU 2001 8 6 MALA010610 1 20010801 A 3260 801801 PROXIMITY SWITCH BAC 146 AVRO146RJ85A 1500097 EU DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 535XJ E2371 During Flight #3610, Nose gear would not retract after Takeoff. Red Transition light on handle and Indicator. Air Turn back to MSP. Maintenance found uplock Proximity sensor bad. Replaced Proximity switch PN 8-018-01. IAW AMM 32-60-21. Ops checks of switch and gear swings all good. 2 H 7 4 4F RT A49EU 2001080600407 20010806 00407 EU 2001 8 6 C2XA01BT136 1 20010706 A 5100 S5367240822801 DOUBLER AEROSP ATR42 ATR42320 8680930 EU CORRODED A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 93840 271 YUL---CO4370, DURING 3C CHECK IN YUL MAINTENANCE FOUND AT FRAME 39 RIGHTHAND SIDE STATION 14 DOUBLER CORRODED....REMOVED AND REPLACED DOUBLER IAW ATR42 SRM 51-25-01 AND ATR42 SRM 51-25-04. 2 H 7 2 4T RT A53EU 2001080600408 20010806 00408 NM 2001 8 6 EISA20010105 1 20010702 A 5330 NPN SKIN BOEING BOEING 727 727225 1384077 NM #2 ENGINE INTAKE CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 354PA NSN 20624 AT STA. 1323 THRU ACCESS DOOR IN 'S' DUCT FOR INTAKE #2 ENGINE 7 O'CLOCK POS. HAS A CRACK.FOUND DURING 'B' CHECK.CORRECT IVE ACTION:REMOVED DAMAGED AREA IAW B727 SRM 54-10-3, FIG. 10. FABRICATED REPAIR PARTS IAW B727 SRM 54-10-3, FIG. 10. TR EATED, PRIMED & INSTALLED REPAIR IAW B727 SRM 51-10-6 & 51-30-2. 2 L 7 3 4F A3WE 2001080600409 20010806 00409 NM 2001 8 6 EISA20010108 1 20010721 A 7932 JT8D15 ENGINE BOEING 727 727277 138408S NM PWA JT8 JT8D15 52051 NE INOPERATIVE A EISA A E UNSCHED LANDING ENGINE SHUTDOWN Y ENGINE STOPPAGE CR CRUISE 1 SW 07 275WC 49370 20549 695359 #1 ENG LOSING OIL QTY, OIL TEMP ON THE RISE, LOSING OIL PRESS. ENGINE #1 SHUT DOWN.CORRECTIVE ACTION:#1 ENGINE TO BE REM OVED. 2 L 7 3 4F 4 F RT A3WE E2EA 2001080600410 20010806 00410 NE 2001 8 6 EISA20010109 2 20010726 A 7530 JT8D7B ENGINE PWA BOEING 727 727223 1384074 NM PWA JT8 JT8D7B 52053 NE #1 INOPERATIVE A EISA E A ENGINE SHUTDOWN UNSCHED LANDING Y ENGINE STOPPAGE TO TAKEOFF 1 SW 07 314NE 59182 649221 19495 649221 JUST AFTER ROTATION, SEVERAL COMPRESSOR STALLS WERE HEARD. GAUGES FOR #1 ENGINE SHOWED SOME FLUCTUATION; ENG. FAIL LIGHT FLASHED. ACCOMPANIED BY AUTO PACK TRIP. AIR TURN BACK TO INDIANAPOLIS.CORRECTIVE ACTION:INSP. INLET AND EXHAUST, NO DA MAGE NOTED, R/R PRBC PER MM 75-31. NO HELP.R/R #1 ENGINE PER EOI FORM 67201-GRD RUN UP NORMAL. TEST FLIGHT OPS CK #1 ENG INE NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001080600411 20010806 00411 EU 2001 8 6 C2XA01BT137 1 20010706 A 5310 S5357260120100 FRAME AEROSP ATR42 ATR42320 8680930 EU CRACKED A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 93840 271 YUL---CO4370, DURING 3C CINSPECTION MAINTENANCE FOUND AT RIGHTHAND POSITION FR 25 CRACK IN HYDRAULIC PASS-THROUGH....REP AIRED IAW COEX EC 5310-01194. 2 H 7 2 4T RT A53EU 2001080600412 20010806 00412 WP 2001 8 6 ZW0A0106304 1 20010804 A 3350 60030451LB BATTERY PACK DOUG DC9 DC983 3022083 WP A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9622A 53593 DURING MAINTENANCE THE EXIT LIGHT OVER THE RIGHT AND LEFT OVER WING EXITS WERE INOP DUE TO WEAR.REPLACED BATTERY PACK P/ N 60-0304-51LB.LAST CHECK C 07/25/01 STL ---CLOSED--- 2 L 7 2 4F RT A6WE 2001080600413 20010806 00413 WP 2001 8 6 ZW0A0106305 1 20010804 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC983 3022083 WP A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9622A 53593 DURING MAINTENANCE THE EGRESS LIGHTS BETWEEN ROW 25 AND 26 WERE INOP. DUE TO WEAR. REPLACED POWER SUPPLY P/N 60-0304-51 LB PER MM 33-51-00.LAST CHECK C 07/25/01 STL. ---CLOSED--- 2 L 7 2 4F RT A6WE 2001080600414 20010806 00414 EU 2001 8 6 C2XA01BT138 1 20010706 A 5310 S5357260120000 FRAME AEROSP ATR42 ATR42320 8680930 EU CRACKED A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 93840 271 YUL---CO4370, DURING 3C INSPECTION YUL MAINTENANCE REPORTED THAT CRACK WAS FOUND ON FR 25 WL 2327 L/H. SIDE IN HYDRAULIC PASS-THROUGH.....REPAIR WAS MADE IAW COEX EC 5310-01194. 2 H 7 2 4T RT A53EU 2001080600415 20010806 00415 EU 2001 8 6 C2XA01BT139 1 20010718 A 5310 S5357260120100 FRAME AEROSP ATR42 ATR42320 8680930 EU CORRODED A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 14830 184 YUL---CO4378, DURING 4C INSPECTION YUL MAINTENANCE FOUND R/H. HYDRAULIC CUTOUT AT FR25 TO BE CRACKED....REPAIRED IAW COE X EC 5310-01196. 2 H 7 2 4T RT A53EU 2001080600416 20010806 00416 EU 2001 8 6 C2XA01BT140 1 20010718 A 5310 S5357260120000 FRAME AEROSP ATR42 ATR42320 8680930 EU CORRODED A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 14830 184 YUL---CO4378, DURING 4C INSPECTION YUL MAINTENANCE FOUND L/H. HYDRAULIC CUTOUT AT FRAME 25 CRACKED....REPAIRED IAW COEX EC 5310-01196. 2 H 7 2 4T RT A53EU 2001080600417 20010806 00417 EU 2001 8 6 C2XA01BT141 1 20010718 A 5300 S5317220625801 BEAM AEROSP ATR42 ATR42320 8680930 EU CORRODED A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 14830 184 YUL---CO4378, DURING 4C INSPECTION YUL MAINTENANCE FOUND FLOOR BEAM (IN COCKPIT) AT FR9 TO BE CORRODED....MAINTENANCE RE MOVED AND REPLACED (NEW) BEAM IAW ATR42 SRM 51-25-01. 2 H 7 2 4T RT A53EU 2001080600418 20010806 00418 EA 2001 8 6 SWIA200110081 1 20010802 A 2120 SENSOR CNDAIR CL600 CL6002B19 EA A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 418SW 7446 ARINC COOL CAUTION MESSAGE, ALL PHASES OF FLIGHT AND GROUND. REPLACED ARINC COOL FLOW SENSOR. MOUNT BOLTS AND CONNECTO R SECURE. OPS CHECK OK. P/N: 009519-05 S/N OFF: 0531 2 L 7 2 4F RT A21EA 2001080700001 20010807 00001 EU 2001 8 7 C2XA01CL189 1 20010804 A 3260 D22924010 SWITCH AEROSP ATR42 ATR42320 8680930 EU LT. GEAR DEFECTIVE A C2XA K NONE J WARNING INDICATION CR CRUISE 1 SW 27 14825 170 ROC FLT.#3116 THE CREW REPORTED LEFT MAIN LANDING GEAR UNLOCK LIGHT ON SYSTEM #1 SHOWS UNLOCKED INDICATION.MAINTENANCE REPLACED AFT. LEFT MAIN GEAR DOWNLOCK SWITCH. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001080700002 20010807 00002 NE 2001 8 7 C2XA01IA311 2 20010803 A 7300 78639010 HMU EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE #2 ENGINE UNSERVICEABLE A C2XA A D UNSCHED LANDING RETURN TO BLOCK R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 27 16729 13244 3436 120185 115314 IAH - FLIGHT 3050, THE CREW REPORTED THAT THE NUMBER TWO ENGINE EXPERIENCED A SUDDEN POWER LOSS ON CLIMBOUT. THE AIRCRAF T RETURNED TO IAH WITHOUT INCIDENT WHER MAINTENANCE REMOVED AND REPLACED THE AFFECTED HYDROMECHANICAL METERING UNIT IN A CCORDANCE WITH PW118 M/M 73-21-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2001080700016 20010807 00016 NM 2001 8 7 2001F00162 1 20010111 A 5730 65B145967RT PANEL BOEING 747 747230B 1384889 NM LT WING CRACKED A Q2SA K NONE O OTHER IN INSP/MAINT 1 GL 23 744SA 22363 DURING PREFLIGHT, FOUND LEFT WING UPPER PANEL ASSEMBLY ABOVE NR 2 ENGINE PYLON AND ABOVE NR 1 SLAT CRACKED APPROXIMATELY 48 INCHES LONG FROM FORWARD TO AFT OF PANEL. REMOVED, REPAIRED AND REINSTALLED PANEL ASSEMBLY. REPAIRED IAW SRM 51-40 -09 AND 51-40-12. (M) 2 L 7 4 4F A20WE 2001080700017 20010807 00017 SO 2001 8 7 ASOA01102 1 20010630 A 2750 FCU EMB 120 EMB120ER 3260203 SO T/E FLAP MALFUNCTIONED A ASOA K NONE F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 SO 11 503AS 120275 FLT 4059 - DURING DESCENT INTO ATL, CAPTAIN REPORTED A FLAP CONTROL FAULT. CREW DECLARED AN EMERGENCY AS A PRECAUTION A ND LANDED AIRCRAFT SAFELY IN ATL WITH ZERO FLAPS. MAINTENANCE RERACKED THE FLAP CONTROL UNIT. AFTER CYCLING THE FLAP F IVE TIMES, THE DISCREPANCY COULD NOT BE DUPLICATED. MAINTENANCE LUBED THE TRACK AND ACTUATOR, AS WELL AS CLEANED AND RE SEATED CANNON PLUG. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001080700022 20010807 00022 SO 2001 8 7 MASA01068 1 20010714 A 2730 COMPUTER EMB 145 EMB145 SO ELEVATOR MALFUNCTIONED A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 836MJ 145359 FLT 5869 - DCA-CHS - RETURNED TO DCA DUE TO MAIN PITCH TRIM SYSTEM INOPERATIVE AFTER TAKEOFF. MAINTENANCE RESET IC6001 COMPUTER SYSTEM. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001080700024 20010807 00024 EA 2001 8 7 MASA01069 1 20010715 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 EA CABIN LOOSE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27318 7318 FLT 6150 - COS-PHX - THE CREW REPORTED THE EMERGENCY ESCAPE FLOOR PATH LIGHT STRIP AMBER SECTION OVERWING EXIT WAS NOT I LLUMINATING. MAINTENANCE TROUBLESHOT AND FOUND A LOOSE CONNECTOR AT THE BEGINNING OF THE AMBER STRIP. MAINTENANCE RESE CURED THE CONNECTOR. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2001080700027 20010807 00027 EA 2001 8 7 MASA01071 1 20010717 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA CABIN MALFUNCTIONED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37228 7228 FLT 6070 - DURING OVERNIGHT MAINTENANCE, FOUND THE FLOOR PROX LIGHTING STRIPS TWO THROUGH FIVE INOPERATIVE. THE AIRCRAF T WAS FERRIED TO PHX. PHX COULD NOT DUPLICATE THE DISCREPANCY. MAINTENANCE SUSPECTED THE BATTERY PACK WAS LOW AND CHAR GED DURING FLIGHT. COULD NOT DUPLICATE. OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO FLIGHT. (M) 2 L 7 2 4F RT A21EA 2001080700033 20010807 00033 NM 2001 8 7 P2EA01123 1 20010705 A 5755 654645161A SPOILER BOEING 737 7372B7 1384560 NM RT WING DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 128NJ 22892 SJO - DURING C-CHECK, FOUND RIGHT WING SPOILER NR 6 (P/N 65-46451-61A, S/N MA6427) DELAMINATED. RIGHT WING SPOILER NR 6 REPAIRED DUE TO DELAMINATION. (M) 2 L 7 2 4F A16WE 2001080700034 20010807 00034 NM 2001 8 7 P2EA01126 1 20010713 A 5753 SKIN BOEING 737 7372B7 1384560 NM T/E FLAP CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 128NJ 22892 SJO - DURING C-CHECK, FOUND LEFT OUTBOARD MID FLAP AT FORE FLAP CENTER TRACK CAVITY, SKIN WITH CRACK. REPAIRED LEFT WIN G OUTBOARD MID FLAP, CENTER TRACK CAVITY SKIN SECTION DUE TO CRACK IAW COOPESA EO NR COO-3-57-332-01. (M) 2 L 7 2 4F A16WE 2001080700045 20010807 00045 NM 2001 8 7 P2EA01127 1 20010706 A 5754 6546431251 SKIN BOEING 737 7372B7 1384560 NM L/E FLAP DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 128NJ 22892 SJO - DURING C-CHECK, FOUND LEFT WING, OUTBOARD FORE FLAP (P/N 65-46431-251, S/N BN424) UPPER SURFACE WITH BUDGED SKIN, DELAMINATION AND DENTS. LEFT WING, OUTBOARD FORE FLAP (P/N 65-46431-251, S/N BN424) , NEW PART INSTALLED (P/N 65-46431- 243, S/N BN188). (M) 2 L 7 2 4F A16WE 2001080700047 20010807 00047 WP 2001 8 7 P2EA01128 1 20010716 A 2760 SPOILER DOUG DC9 DC982 3022082 WP WING MALFUNCTIONED A P2EA K NONE F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 CE 05 130NJ 49222 LGA - FLT 150 - WHILE LANDING, AUTO SPOILERS WOULD NOT ARM. 'DO NOT USE' LIGHT WAS NOT ILLUMINATED. DEFERRED PER MEL 2 7-19-01 PLACED ON CONTROL ITEM NR M130709 PER MX CONTROLLER. S/D - PERFORMED AUTO SPOILER SYSTEM LANDING MODE TEST, SYS TEM OPS CHECKS GOOD IAW AIRCRAFT MM 27-60-00. (M) 2 L 7 2 4F A6WE 2001080700048 20010807 00048 2001 8 7 P2EA01129 4 20010716 A 2230 AUTOTHRUST SYS DOUG DC9 DC982 3022082 WP COCKPIT MALFUNCTIONED A P2EA K NONE O OTHER TO TAKEOFF 1 CE 05 130NJ 49222 MCI - FLT 945 - WITH AUTO THROTTLES ENGAGED DURING TAKEOFF, CRUISE AND DESCENT, A SCHEDULED POWER CHANGE PRODUCES EPR SP LIT OF .40 TO .50. THE RIGHT THROTTLE MOVES IN THE CORRECT DIRECTION WITH LIMITED MOVEMENT. THE LEFT THROTTLE TRAVELS IN THE CORRECT DIRECTION WITH EXCESSIVE MOVEMENT TO COMPENSATE FOR THE RIGHT THROTTLE. DEFERRED AUTO THROTTLE PER MEL 2 2-15-20, CI NR M130708 PER MX CONTROL. PERFORMED RETURN TO SERVICE NR 1 AND NR 2, AUTO THROTTLE SYSTEM OPS CHECK GOOD P ER A/C MM 22-01-05. (M) 2 L 7 2 4F A6WE 2001080700050 20010807 00050 2001 8 7 P2EA01131 4 20010718 A 2230 AUTOTHRUST SYS DOUG DC9 DC987 3022087 WP COCKPIT MALFUNCTIONED A P2EA K NONE O OTHER CL CLIMB 1 CE 05 132NJ 49780 MCI - FLT 704 - AUTO-THROTTLE SWITCH REPEATEDLY TRIPPED OFF DURING INITIAL CLIMB AND CRUISE. DEFERRED AUTO-THROTTLE SYS TEM PER MEL 22-15-20 PLACED ON CONTROL ITEM M132722 PER MAINTENANCE CONTROL MIC. (M) 2 L 7 2 4F RT A6WE 2001080700051 20010807 00051 2001 8 7 P2EA01132 4 20010718 A 2230 AUTOTHRUST SYS BOEING 737 7372B7 1384560 NM COCKPIT INOPERATIVE A P2EA K NONE O OTHER NR NOT REPORTED 1 CE 05 128NJ 22892 FLT 8140 - MCI - AUTO THROTTLE INOPERATIVE, DEFERRED PER MEL 22-04, CONTROL NR M128719, PER MX CONTROL MCGRATH. (M) 2 L 7 2 4F A16WE 2001080700055 20010807 00055 NM 2001 8 7 P2EA01133 1 20010720 A 5270 WARNING LIGHT BOEING 737 737230 NM COCKPIT ILLUMINATED A P2EA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 05 124NJ 22122 FLT 554 - MCI - AFTER PUSH BACK FROM GATE AND AFTER APPLICATION OF AIRCRAFT POWER, THE AFT SERVICE DOOR UNSAFE LIGHT ILL UMINATED. RETURNED TO THE GATE. INSPECTED THE AIRCRAFT L2 DOOR, OPEN AND CLOSED DOOR NORMALLY. NO DEFECTS FOUND. (M) 2 L 7 2 4F RT A16WE 2001080700065 20010807 00065 SO 2001 8 7 SIMA200115904 1 20010608 A 2730 CONTROLLER EMB 145 EMB145LR SO ELEVATOR MALFUNCTIONED A SIMA K NONE F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SW 21 627AE 145121 DFW - FLT 3350 - UNCOMMANDED PITCH TRIM MOVEMENT FROM 4 DEGREES TO 2 DEGREES DOWN WHILE TAXIING. PERFORMED OPS CHECK OF PITCH TRIM SYSTEM IAW AMM. COULD NOT DUPLICATE, NO DEFECT NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001080700069 20010807 00069 SO 2001 8 7 SIMA200117001 1 20010619 A 7830 SWITCH EMB 135 EMB135LR SO TRHUST REVERSER OUT OF ADJ A SIMA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 21 704PG 145174 CMH 0 FLT 4853 - DURING CLIMB-OUT, NR 2 ENGINE SURGING. ENGINE WAS SHUTDOWN AND RETURNED TO BASE. ADJUSTED RIGHT LOWER OUTBOARD SHOOK AND SHIMMED RIGHT OUTBOARD SWITCH IAW AMM 78-21-01 TR NR 78-15 EO EB-7800-011R1 WAS COMPLIED WITH. AIRC RAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001080700070 20010807 00070 NM 2001 8 7 PCAA0108078 1 20010803 A 3230 8Z4827051 BRACKET DHAV DHC8 DHC8102 2809003 NM LEFT NACELLE WORN A PCAA O OTHER O OTHER IN INSP/MAINT 1 EA 13 805EX 228 MDT- DURING ROUTINE MAINTENANCE VISIT LEFT MAIN GEAR UPLOCK ACTUATOR DAMPNER BRACKET FOUND LOOSE. LEFT DAMPNER BRACKET R EPLACED IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL 51-10-00.AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001080700071 20010807 00071 NM 2001 8 7 PCAA0108079 1 20010803 A 3230 8Z4827051 BRACKET DHAV DHC8 DHC8102 2809003 NM RIGHT NACELLE LOOSE A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 829EX 146 MDT. DURING ROUTINE MAINTENANCE VISIT RIGHT MAIN GEAR UPLOCK ACTUATOR SURGE DAMPNER BRACKET FOUND LOOSE. RIVETS REPLACED IN SURGE DAMPNER MOUNT BRACKET. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001080700078 20010807 00078 SO 2001 8 7 SIMA200119001 1 20010702 A 5315 FLOORBEAM EMB 135 EMB135LR SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 705AE 145184 ABI - DURING MBV INSPECTION MAINTENANCE REPORTED THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. AFTER REMOVA L OF CORROSION IT WAS FOUND TO BE OUT OF LIMITS. OMEGA BEAM WAS REPAIRED IAW EMB SRM AND AIRCRAFT WAS RETURNED TO SERVI CE. (M) 2 L 7 2 4F RT TOOO11AT 2001080700079 20010807 00079 EU 2001 8 7 SIMA200119401 1 20010713 A 3350 SOCKET SAAB SF340 340B 7860101 EU CABIN DAMAGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 323AE 340B323 JFK - FLT 5157 - CREW REPORTED THE FLOOR PROXIMITY LIGHT AT SEAT 9B TO BE INOPERATIVE. LIGHT WAS PUT ON MEL AT THIS TIM E. MAINTENANCE FOUND A DAMAGED LIGHT SOCKET. LIGHT SOCKET WAS REPAIRED IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AI RCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001080700222 20010807 00222 SO 2001 8 7 SIMA200119402 1 20010713 A 3350 7287580509 LIGHT EMB 135 EMB135LR SO CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 728AE 145328 CMH - MAINTENANCE REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS AT SEATS 7 AND 8 ARE INOPERATIVE. MAINTENANCE REPLACED THE FLOOR LIGHT STRIP IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001080700227 20010807 00227 SO 2001 8 7 SIMA200119701 1 20010705 A 5315 FLOORBEAM EMB 135 EMB135LR SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 702AE 145164 ABI - DURING MBV INSPECTION, CORROSION WAS FOUND ON THE LEFT OMEGA BEAM AT FRAME 20. BEAM WAS REPAIRED IAW EMB SRM AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001080700228 20010807 00228 EU 2001 8 7 SIMA200119703 1 20010712 A 5512 7251001023 SKIN SAAB SF340 340B 7860101 EU HORIZ STAB DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 340RC 340B340 ABI - DURING MBV INSPECTION MAINTENANCE FOUND TWO DENTS BEYOND SRM LIMITS ON THE HORIZONTAL STABILIZER LOWER SKIN. DENT S WERE REPAIRED IAW SAAB REPAIR STATEMENT 340SDS002078 PARA 4. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001080700229 20010807 00229 NM 2001 8 7 USAA010667 1 20010613 A 5310 DOOR FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND FRAME REVEAL CRACKED 1 INCH, FORWARD SERVICE DOOR, TOP SURROUND FRAME. REMOVED AND REPLACED FRAME REVEAL. (M) 2 L 7 2 4F RT A16WE 2001080700230 20010807 00230 NM 2001 8 7 USAA010704 1 20010518 A 2710 43712 BELLCRANK BOEING 737 737301 1384611 NM AILERON BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 23931 PIT - FOUND BELLCRANK HAD .75 INCH SECTION BROKEN OUT, RT INBOARD AILERON HINGE ASSY. NOTCHED OUT TOP OF FITTING, REMOV ED LOWER FLANGE, INSTALLED TWO MACHINED DOUBLERS PER EA 71077. (M) 2 L 7 2 4F RT A16WE 2001080700231 20010807 00231 NM 2001 8 7 USAA010722 1 20010516 A 5730 SKIN BOEING 737 737301 1384611 NM LT WING DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND WING LEADING EDGE DELAMINATED 6 INCHES BY 8 INCH AREA, LEFT WING LEADING EDGE AT STATION 559. REMOVED DAMAG ED LAYERS, DRILLED OUT BRACKET FOR MOUSE TRAP PER SRM 51-70-17. (M) 2 L 7 2 4F RT A16WE 2001080700232 20010807 00232 NM 2001 8 7 USAA010728 1 20010517 A 5200 SKIN BOEING 737 737301 1384611 NM DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND SKIN CRACKED .095 INCH, LOWER HINGE CUTOUT. ROUTED OUT CRACK AND INSTALLED DOUBLER PER SRM 52-10-01 S/B 737 -52-1096. (M) 2 L 7 2 4F RT A16WE 2001080700233 20010807 00233 NM 2001 8 7 USAA010733 1 20010517 A 5320 WEB BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND ANGLE WEB CRACKED 1 INCH, UNDER AFT SERVICED DOOR SILL PLATE. MANUFACTURED AND INSTALLED NEW WEB PER BOEING DRAWING 65.45855. (M) 2 L 7 2 4F RT A16WE 2001080700234 20010807 00234 NM 2001 8 7 USAA010734 1 20010517 A 5414 SKIN BOEING 737 737301 1384611 NM PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 43712 23931 PIT - FOUND PYLON SKIN CRACKED 1 INCH, UPPER RIGHT CORNER OF PANEL 5724L OPENING. STOP DRILLED CRACK, INSTALLED DOUBLER PER TYPICAL REPAIR 54-50-07. (M) 2 L 7 2 4F RT A16WE 2001080700247 20010807 00247 NM 2001 8 7 USAA010741 1 20010610 A 5542 SKIN BOEING 737 7373B7 1384580 NM RUDDER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 524AU 43790 23859 PIT - FOUND RUDDER DELAMINATION .75 INCH BY .375 INCH AREA, FORWARD LOWER SKIN CORNER. REPAIRED PER EA 71466 PER SRM 51 60-07, 51-70-17 FIG 18 OF BOEING MM. (M) 2 L 7 2 4F RT A16WE 2001080700248 20010807 00248 NM 2001 8 7 USAA010748 1 20010619 A 5313 STRINGER BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 51038 22796 TPA - FOUND STRINGER CORRODED 10 SQUARE INCHES, PREVIOUSLY SPLICED SECTION OF STRINGER 27L AT STATION 967. CORROSION LE VEL 1. SPLICED IN NEW SECTION OF STRINGER USING SPLICES RETAINED FROM PREVIOUS REPAIR PER SRM 53-10-3 FIG 1. (M) 2 L 7 2 4F A16WE 2001080700249 20010807 00249 NM 2001 8 7 USAA010750 1 20010616 A 5312 BULKHEAD BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 37497 23879 CLT - FOUND BULKHEAD WEB WITH FOUR CRACKS, 1 WAS .125 INCH, AND 3 WERE .5 INCH, BS 178 WL 189 TO 203, LBL 5.5 TO RBL 5.7 . DAMAGE REMOVED, REPAIR DOUBLER INSTALLED PER EO 5300V153 AND SRM 53-10-08. (M) 2 L 7 2 4F RT A16WE 2001080700250 20010807 00250 NM 2001 8 7 USAA010751 1 20010616 A 5312 BULKHEAD BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 243US 52043 22445 CLT - FOUND BULKHEAD WEB WITH NUMEROUS CRACKS RANGING FROM .125 INCH TO .75 INCH, BS 178 WL 207 TO 234, LBL 12.6 TO RBL 11.7. DAMAGE REMOVED, REPAIR DOUBLER INSTALLED PER EO 5300V153, EA 69807 AND 69774. (M) 2 L 7 2 4F A16WE 2001080700251 20010807 00251 NM 2001 8 7 USAA010752 1 20010616 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 243US 52043 22445 CLT - FOUND VERTICAL CHORD WITH TWO CRACKS EACH 1 INCH LONG, BS 178 WL 181 AT RBL 5.7 AND WL 184 AT LBL 5.7. DAMAGE REM OVED, INSTALLED REPAIR ANGLES ADN STRAPS PER EO 5300V155. (M) 2 L 7 2 4F A16WE 2001080700252 20010807 00252 NM 2001 8 7 USAA010753 1 20010616 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 243US 52043 22445 CLT - FOUND SIDE CHORDS WITH TWO CRACKS .25 INCH AT RBL 26, 1 INCH AT LBL 24, BS 178 WL 195 AT LBL 24 AND WL 207 AT RBL 26. DAMAGED SECTION REMOVED, INSTALLED CHORD SPLICE REPAIR PER EO 5300V157. (M) 2 L 7 2 4F A16WE 2001080700253 20010807 00253 NM 2001 8 7 USAA010754 1 20010616 A 5312 BULKHEAD BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 37497 23879 CLT - FOUND BULKHEAD WEB WITH 3 CRACKS ALL .5 INCHES LONG, BS 178, WL 198 AT LBL 5.7 AND RBL 5.7, WL 212 AT RBL 5.7. DA MAGED REMOVED, INSTALLED REPAIR DOUBLER PER EO 5300V153. (M) 2 L 7 2 4F RT A16WE 2001080700254 20010807 00254 NM 2001 8 7 USAA010902 1 20010720 A 5310 SHEAR TIE BOEING 737 7373B7 1384580 NM BS 947.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND FRAME SHEAR TIE CORRODED .5 INCH BY .5 INCH, BS 947.5, BETWEEN S27L AND S26L. CORROSION LEVEL 1, TASK NR C5 3-208-01. REMOVED AND REPLACED SHEAR TIE PER SRM 51-01-2. (M) 2 L 7 2 4F RT A16WE 2001080700255 20010807 00255 NM 2001 8 7 USAA010850 1 20010628 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 EA 19 576US 43413 23741 PIT - FOUND FLOORBEAM CORRODED 3 INCHES BY 30 INCHES, STATION 328 NR 3 GALLEY 10 INCHES RIGHT OF C/L TO FORWARD SERVICE DOOR. CUT OUT CORROSION OF FLOORBEAM T-CAP, SPLICED IN NEW SECTION PER PER RM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2001080700256 20010807 00256 NM 2001 8 7 USAA010895 1 20010720 A 5300 FITTING BOEING 737 7373B7 1384580 NM BS 727 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND FITTING CORRODED 3 INCHES BY 2 INCH AREA, BS 727, STRINGER 27R, AFT CARGO COMPARTMENT. CORROSION LEVEL 2 TA SK NR C53-202-01. FABRICATED AND INSTALLED FITTING PER BAC DRAWING NR 65-73746 AND SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001080700257 20010807 00257 NM 2001 8 7 USAA010894 1 20010720 A 5300 SKIN PANEL BOEING 737 7373B7 1384580 NM BS 663-685 BUCKLED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND SKIN PANEL BUCKLED APPROXIMATELY 3 SQUARE INCHES, KEEL BEAM STATION 663 TO 685. REMOVED AND REPLACED KEEL B EAM LOWER PANEL PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001080700258 20010807 00258 NM 2001 8 7 USAA010870 1 20010716 A 5200 6545871523 SKIN BOEING 737 7373B7 1384580 NM FWD SERV DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 45591 22957 TPA - FOUND DOOR EXTERIOR SKIN CRACKED .25 INCH, FORWARD SERVICE DOOR, LOWER HINGE CUTOUT. INSTALLED REPAIR DOUBLER PER SRM 52-10-01 PAGE 201 AND SB 737-52-1096. (M) 2 L 7 2 4F RT A16WE 2001080700259 20010807 00259 NM 2001 8 7 USAA010869 1 20010716 A 5300 6552873159 SKIN BOEING 737 7373B7 1384580 NM AFT ENTRY DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 45591 22957 TPA - FOUND DOOR EXTERIOR SKIN CRACKED .25 INCH, AFT ENTRY DOOR, UPPER HINGE CUTOUT. INSTALLED DOUBLER PER SRM 52-10-01 AND SERVICE BULLETIN 737-52-1096. (M) 2 L 7 2 4F RT A16WE 2001080700260 20010807 00260 NM 2001 8 7 USAA010863 1 20010608 A 5300 65465292 STRINGER BOEING 737 737301 1384611 NM BS 440 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 576US 43413 23741 PIT - FOUND STRINGER CRACKED 1 INCH, STATION 440 STRINGER 8 RIGHT. INSTALLED DOUBLER PER SRM T/R 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001080700261 20010807 00261 NM 2001 8 7 USAA010927 1 20010719 A 5300 BULKHEAD BOEING 737 737401 1384701 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 412US 37299 23881 PIT - FOUND BULKHEAD WITH CRACKS, ONE AT 1 INCH, ONE AT 1.125 INCH, TWO AT 1.5 INCH AND TWO AT .125 INCH, BS 178 LBL 5.7 WL 216; BL 0, WL 184 - WL 195; RBL 5. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER PER SRM 53-10-08, EO 5300V152, EO 5 300V153. (M) 2 L 7 2 4F RT A16WE 2001080700262 20010807 00262 WP 2001 8 7 USAA010921 1 20010629 A 5200 4913947501 FITTING DOUG DC9 DC981 3022081 WP CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 827US 52853 48049 PIT - FOUND FITTING CRACKED 4.5 INCHES, MAIN ENTRY DOOR UPPER HINGE FITTING BROKEN AT BASE. REPLACED WITH IDENTICAL PAR T NR. (M) 2 L 7 2 4F A6WE 2001080700263 20010807 00263 NM 2001 8 7 USAA010858 1 20010531 A 5300 STRAP BOEING 737 737301 1384611 NM BS 312 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 576US 43413 23741 PIT - FOUND STRAP CRACKED TWO PLACES .5 INCH ON BOTH FORWARD SIDES, STATION 312 BOTTOM FLOORBEAM SUPPORT STRAP 10 INCHES LEFT C/L. DEFECTIVE PART REPLACED WITH IDENTICAL PART. REPLACED RIVETS PER SRM 52-40-02. (M) 2 L 7 2 4F RT A16WE 2001080700264 20010807 00264 NM 2001 8 7 USAA010857 1 20010609 A 5300 BELTFRAME BOEING 737 737301 1384611 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 576US 43413 23741 PIT - FOUND BELTFRAME CRACKED 1 INCH, STATION 787 BELTFRAME ABOVE S9R. INSTALLED REPAIR DOUBLER PER T/R 53-1014. (M) 2 L 7 2 4F RT A16WE 2001080700265 20010807 00265 NM 2001 8 7 USAA010856 1 20010609 A 5300 BELTFRAME BOEING 737 737301 1384611 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 576US 43413 23741 PIT - FOUND BELTFRAME CRACKED .25 INCH, STATION 480 S8. DOUBLER INSTALLED PER SRM T/R 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001080700266 20010807 00266 NM 2001 8 7 USAA010847 1 20010716 A 5300 SKIN BOEING 737 7373B7 1384580 NM BS 380 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46295 22950 CLT - FOUND FUSELAGE SKIN WITH PREVIOUSLY INSTALLED DOUBLER 41 INCHES BY 23 INCHES, BS 380, STRINGER 26 TO 27R. INSTALL ED NEW DOUBLER PER EO 5300V258 AND TR 53-30-07. (M) 2 L 7 2 4F RT A16WE 2001080700267 20010807 00267 NM 2001 8 7 USAA010846 1 20010716 A 5300 SKIN BOEING 737 7373B7 1384580 NM BS 500B GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND FUSELAGE SKIN DENTED WITH GOUGE 2 INCHES IN DIAMETER, BS 500B BETWEEN STRINGERS 25 AND 26R. DAMAGE REMOVED, INSTALLED REPAIR PER SRM 53-00-01, FIG 210. (M) 2 L 7 2 4F RT A16WE 2001080700268 20010807 00268 NM 2001 8 7 USAA010845 1 20010716 A 5315 FLOORBEAM BOEING 737 7373B7 138447F NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND FLOORBEAM WITH ELONGATED CLIPNUT HOLES .125 INCH AND .25 INCH, BS 328, LBL 28. INSTALLED REPAIR ANGLES PER SRM 53-10-51, FIG 206. (M) 2 L 7 2 4F RT A16WE 2001080700269 20010807 00269 NM 2001 8 7 USAA010844 1 20010716 A 5300 FRAME BOEING 737 7373B7 1384580 NM BS 807 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND FRAME WITH HOLE .375 INCH, BS 807, AT TIE CLIP FOR STRINGER 27R. INSTALLED DOUBLER PER SRM 51-70-11. (M) 2 L 7 2 4F RT A16WE 2001080700270 20010807 00270 NM 2001 8 7 USAA010843 1 20010716 A 5300 FRAME BOEING 737 7373B7 1384580 NM BS 1064 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND FRAME DENTED 1 INCH DIAMETER, BS 1064, 2 INCHES OUTBOARD OF STRINGER 2R. DAMAGED REMOVED, INSTALLED DOUBLER PER EA 69827. (M) 2 L 7 2 4F RT A16WE 2001080700271 20010807 00271 NM 2001 8 7 USAA010842 1 20010716 A 5300 FRAME BOEING 737 7373B7 1384580 NM BS 500A A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 22950 CLT - FOUND FRAME WITH TWO HOLES .1875 INCH, BS 500A, RIGHT SIDE TRANSITION ANGLE, FORWARD CARGO HOLD. DAMAGE REMOVED, INSTALLED FRAME SPLICE PER EA 85041. (M) 2 L 7 2 4F RT A16WE 2001082000191 20010820 00191 WP 2001 8 20 ARWA0010802 1 20010802 A 7830 WIRE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE THRUST REVERSER BURNED A ARWA E ENGINE SHUTDOWN J G WARNING INDICATION MULTIPLE FAILURE CL CLIMB 1 SO 19 6661A 45969 67098 AFT T/O NR 3 ENG T/R LT ILLUM, NR 3 ENG ANTI-ICE VLV LT CAME ON. NR 3 ENG OIL PRESS LT CAME ON, NR 3 ENGINE OIL PRESS G AUGE READ ZERO. FOLLOWED ABNORM CKLIST FOR OIL PRESS LIGHT, INFLIGHT SHUTDOWN. ON APPR NR 3 ENG ANTI-ICE VLV CB TRIPPE D, GRD COOLING & BLOWAWAY JET CB UNABLE TO RESET. R&R NR 3 ENG CTR INTER ANTI-ICING AIR MANIFOLD IAW MM75-10-0. REPAIR ED WIRES FOR T/R INDICATOR SYS, ANTI-ICE SYS, OIL PRESS INDICATOR SYS, BLOWAWAY JET VLV, AND FIRE WARNING SYSTEM NR 3 PY LON CONNECTOR R-315, R5-40, R-36 IAW MM 20-50-1. RESET BLOWOUT PNL, CKD OIL LEVEL, AND SECURED OIL CAP. R&R OIL PRESS, DIFF SW IAW MM79-33-0. OPS CK NR 3 ENG INDICATION SYS, RUN-UP AND FUNCTIONAL TEST ALL SYS, FOUND NORM INDICATION. 2 L 7 4 4F 4 F 4A25 1E8 2001080700272 20010807 00272 NM 2001 8 7 USAA010755 1 20010616 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 37497 23879 CLT - FOUND LEFT AND RIGHT SIDE CHORDS WITH 3 CRACKS, .25 INCH, 2 INCHES, AND 3 INCHES, BS 178, WL 207 AND LBL AND RBL 2 6, WL 202 AT LBL 27. DAMAGED REMOVED, INSTALLED SPLICE CHORD REPAIRS PER EO 5300V157. (M) 2 L 7 2 4F RT A16WE 2001081600165 20010816 00165 NE 2001 8 16 ARWA0010801 2 20010802 A 7260 MO6569AC GEARBOX LKHEED 1011 1011385114 WP RROYCE RB211 RB211524B4 54555 NE NR 1 ENGINE DAMAGED A ARWA E ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SO 19 260FA 1158 14780 NR 1 ENGINE FAILED IN FLIGHT. N1 (O%), N2 (15%), N3 (0%), OIL PRESS (0%), WITH VIBRATION. EMERGENCY CHECK LIST CARRIED OUT. NO HYDRAULIC PRESSURE. CONTINUED TO MIAMI, LANDED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED NR 1 ENGINE HI GH SPEED EXTERNAL GEARBOX MODULE ASSY IAW MM 72-00-06. RUN-UP, LEAK CHECK, ALL SYSTEMS CHECK NORMAL IAW 71-00-00 AND MF G RECOMMENDATIONS. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A23WE E12EU 2001080700273 20010807 00273 NM 2001 8 7 USAA010756 1 20010622 A 5330 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 35767 23985 TPA - FOUND FUSELAGE SKIN CRACKED .75 INCH, BS 294, MED LOWER HINGE CUTOUT BETWEEN S13L AND 14L. REPAIR DOUBLER INSTALL ED PER SRM 53-10-01, FIG 205. (M) 2 L 7 2 4F RT A16WE 2001080700274 20010807 00274 NM 2001 8 7 USAA010757 1 20010622 A 5314 KEELBEAM BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 51038 22796 CLT - FOUND KEEL BEAM CORRODED 1 INCH DIAMETER BY .020 INCH DEEP, BS 727 PLUS 16, S27L. CORROSION REMOVED, AND REPAIR I NSTALLED PER EA 94208, ALONG WITH ACCESS SKIN REPAIR PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 2001080700275 20010807 00275 NM 2001 8 7 USAA010764 1 20010620 A 5314 KEELBEAM BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 51038 22796 TPA - FOUND LEFT HAND KEEL BEAM CORRODED .75 INCH DIAMETER BY .020 INCH DEEP, BS 727 PLUS 16, LOWER SURFACE. DAMAGE REM OVED, KEEL BEAM REPAIRED PER EA 94208. ACCESS REQUIRES SKIN REPAIR PER SRM 53-30-3, FIG 6. (M) 2 L 7 2 4F A16WE 2001080700276 20010807 00276 NM 2001 8 7 USAA010876 1 20010718 A 5320 CPN1123759 ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND CREASEBEAM ANGLE CORRODED 40 INCHES, BS 947.5 AFT SERVICE DOOR FRAME. CORROSION LEVEL 1, TASK NR C53-107-02 . REMOVED AND REPLACED Z-ANGLE AND WEB PER SRM 51-10-2, 51-40-2, AND 53-60-15. (M) 2 L 7 2 4F RT A16WE 2001080700277 20010807 00277 NM 2001 8 7 USAA010881 1 20010719 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH AREA, BS 1016 LBL 6 TO LBL 34. CORROSION LEVEL 1, TASK NR C53-202-01. REMOVED AND REPLACED T-CAP PER TYPICAL REPAIR 53-10-05A. (M) 2 L 7 2 4F RT A16WE 2001080700278 20010807 00278 NM 2001 8 7 USAA010885 1 20010719 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND FLOORBEAM CORRODED 4 INCHES BY 2 INCH AREA, BS 1006, LBL 8 TO LBL 12. REPLACED UPPER T-CAP PER EA 69770 AND TR 53-10-05A. (M) 2 L 7 2 4F RT A16WE 2001080700279 20010807 00279 NM 2001 8 7 USAA010889 1 20010719 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND FRAME CORRODED 10 INCHES BY 1 INCH AREA, BS 807 LBL 5 TO RBL 5, AFT CARGO. REMOVED DAMAGE, INSTALLED REPAIR DOUBLER PER SRM 53-00-07 AND 51-40-02. (M) 2 L 7 2 4F RT A16WE 2001080700280 20010807 00280 NM 2001 8 7 USAA010890 1 20010719 A 5320 6552878097 ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND Z-ANGLE CORRODED 4 INCHES BY 40 INCHES AFT ENTRY DOOR SILL. CORROSION LEVEL 1, TASK C53-202-01. REMOVED AN D REPLACED Z-ANGLE PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2001080700281 20010807 00281 NM 2001 8 7 USAA010892 1 20010719 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND FRAME CHORD CORRODED 1 INCHES BY 3 INCHES, BS 500D, RBL 7, FORWARD CARGO FLOOR. CORRODED LEVEL 1 TASK NR C5 3-208-01. DAMAGE REMOVED, INSTALLED REPAIR ANGLES EPR EA 69842. (M) 2 L 7 2 4F RT A16WE 2001080700284 20010807 00284 NM 2001 8 7 USAA010893 1 20010719 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND Z-CHORD CORRODED 4 INCHES BY 1 INCH AREA, BS 270, RBL 6. DAMAGED REMOVED, INSTALLED Z-CHORD REPAIR KIT PER TR 53-20-08. (M) 2 L 7 2 4F RT A16WE 2001080700286 20010807 00286 NM 2001 8 7 USAA010896 1 20010720 A 5314 KEELBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND KEEL BEAM CORRODED 5 SQUARE INCHES, BS 767, RIGHT KEEL BEAM SPLICE. CORROSION LEVEL 2 TASK NR C53-202-01. REMOVED KEEL BEAM, REMOVED CORROSION, REINSTALLED KEEL BEAM AND REPAIR DOUBLER/TRIPLER PER EA 69835. (M) 2 L 7 2 4F RT A16WE 2001080700289 20010807 00289 NM 2001 8 7 USAA010987 1 20010720 A 5314 KEELBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND LOWER CHORD OUTBOARD FLANGE CORRODED 1 INCHES BY 22 INCH, BS 673-695 RIGHT, BS 693-727 KEEL BEAMS. CORROSIO N LEVEL 2 TASK C53-100-01. REMOVED DAMAGE, INSTALLED REPAIR STRAPS LEFT AND RIGHT SIDE PER EA 69794. (M) 2 L 7 2 4F RT A16WE 2001080700290 20010807 00290 EU 2001 8 7 USAABA01005 1 20010526 A 3620 P3C0040800 SENSOR AIRBUS 330 A330323 EU PNEUMATIC SYS FAULTY A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 674UW 342 PHL - FLT 740 - EN ROUTE PIT-LGW, CREW RECEIVED THE ECAM WARNING 'AIR ENG 2 BLEED FAULT.' DUE TO WEATHER RESTRICTIONS, FLIGHT DIVERTED TO PHL AND LANDED WITH NO FURTHER PROBLEM. MAINTENANCE REPLACED THE EXCHANGER OUT TEMPERATURE SENSOR. (M) 2 L 7 2 4F RT A46NM 2001080700291 20010807 00291 EU 2001 8 7 USAABA01006 1 20010614 A 3350 32146220 POWER SUPPLY AIRBUS 330 A330323 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 672UW 333 PHL - DURING TEST, THE NR 2R EPSU FAULTED. MAINTENANCE REPLACED THE EPSU. (M) 2 L 7 2 4F RT A46NM 2001080700292 20010807 00292 NE 2001 8 7 USAABB01026 2 20010520 A 7200 ENGINE BOEING 757 757225 1384959 NM RROYCE RB211 RB211535E4 54555 NE LEFT MALFUNCTIONED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 618AU 22210 31217 SFO - FLT 56 - AFTER TAKEOFF APPROX 1000 FEET AGL, CREW HEARD LOUD BANG AND NOTED NUMEROUS WARNINGS ON THE LEFT ENGINE, AS WELL AS LIGHT SMOKE IN THE COCKPIT. ENGINE WAS SHUT DOWN. FLIGHT RETURNED TO SFO AND LANDED WITHOUT FURTHER INCIDEN T. MAINTENANCE ACTION PENDING. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2001080700293 20010807 00293 NM 2001 8 7 USAABB01032 1 20010528 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 624AU 27245 CLT - FOUND FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001080700294 20010807 00294 NM 2001 8 7 USAABB01036 1 20010610 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 625VJ 27246 CLT - MAINTENANCE FOUND THE EMERGENCY EXIT AISLE LIGHT, AT SEAT ROW 4, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TH E EMERGENCY EXIT AISLE LIGHT AT SEAT ROW 4. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2001080700295 20010807 00295 NM 2001 8 7 USAABB01038 1 20010605 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 624AU 27245 CLT - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 26 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001080700296 20010807 00296 NM 2001 8 7 USAABB01039 1 20010605 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 630AU 27808 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE AT ROW 18. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001080700297 20010807 00297 NM 2001 8 7 USAABB01040 1 20010605 A 3350 9221009 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 633AU 27811 DCA - FOUND EXIT IDENTIFIER BATTERIES LOW AT DOORS L1 AND R4. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2001080700298 20010807 00298 NM 2001 8 7 USAABB01041 1 20010618 A 3350 873100151REV12 LIGHT BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 602AU 22196 MCO - MAINTENANCE FOUND THE EMERGENCY LIGHT MOUNTED AT SEAT 33 WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE EME RGENCY LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2001080700299 20010807 00299 NM 2001 8 7 USAABB01042 1 20010620 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 610AU 27122 BWI - MAINTENANCE FOUND THE RIGHT EMERGENCY AISLE LIGHT ASSEMBLY BROKEN/INOPERATIVE. MAINTENANCE REMOVED AND REPLACED T HE EMERGENCY AISLE LIGHT ASSEMBLY IN ASSOCIATION WITH MM. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2001080700300 20010807 00300 NM 2001 8 7 USAABB01044 1 20010622 A 3350 873100251REV14 LIGHT BOEING 757 7572B7 1384964 NM R2 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 628AU 27806 LAX - MAINTENANCE FOUND THE R2 DOOR EMERGENCY EXIT IDENTIFIER LIGHT ASSEMBLY BROKEN/INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE R2 DOOR EMERGENCY EXIT IDENTIFIER LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2001080700301 20010807 00301 NM 2001 8 7 USAABB01046 1 20010616 A 3397 WIRE BOEING 767 767201 1385125 NM CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 EA 19 646US 23898 PHL - FOUND SIDEWALL LIGHTS ABOVE OVERWING EXIT INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRES AT LEFT SIDEWALL LIGHT D ISCONNECT D03096. (M) 2 L 7 2 4F RT A1NM 2001080700302 20010807 00302 WP 2001 8 7 USAAD01123 1 20010608 A 3350 873100272 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 825US 49237 PIT - THE EMERGENCY LIGHT ASSEMBLY AT SEAT 20 LEFT SIDE DOES NOT TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBL Y AT ROW 20 LEFT SIDE. (M) 2 L 7 2 4F A6WE 2001080700303 20010807 00303 NM 2001 8 7 AWXA0002073 1 20010803 A 5311 65C34537 WEB BOEING 737 737277 1384570 NM BS 705-720 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: 5 Cracks in web below BL24L seat track BS 705-720C: Repaired web IAW AWA ER 15-5715-01200-DL4 2 L 7 2 4F RT A16WE 2001080700304 20010807 00304 NM 2001 8 7 AWXA0002076 1 20010803 A 5310 65475951 SPAR BOEING 737 737277 1384570 NM SS-0 REAR SPAR GOUGED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: LH Horizontal stabilizer I/B upper attach lug at rear spar has 2 gougesC: repaired LH horizontal stabilizer rear spar upper attach lug IAW er 15-5510-1204-DD2 2 L 7 2 4F RT A16WE 2001080700305 20010807 00305 NM 2001 8 7 AWXA0002079 1 20010709 A 5310 6552928564 STRINGER BOEING 737 737277 1384570 NM FS 727A CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: Aft pit exfoliation corrosion STA 727A STR 26LC: replaced damaged section of STR from 727 to midway between STA 727A & 727B & splice per SRM 53-10-3 Fig 1 DET. 6 or DET 7 2 L 7 2 4F RT A16WE 2001080700306 20010807 00306 NM 2001 8 7 AWXA0002081 1 20010711 A 5312 654583340 WEB BOEING 737 737277 1384570 NM WL 207 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 D: Bulkhead 178 intercostal on LH side cracked @ WL 207 aft side chord NDT confirmed.C: Web replaced per ref DWG 65-4583 3-40 & SRM 51-30-2 Pg 5 alodine & primed per SRM 51-10-2 Pg 7 2 L 7 2 4F RT A16WE 2001080700307 20010807 00307 NM 2001 8 7 AWXA0002082 1 20010706 A 5313 672038112 INTERCOSTAL BOEING 737 737277 1384570 NM WL 195 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 183AW 22654 D: E.T. INSP reveals cracks in intercostal on both LH & RH sides @ WL 195, just AFT 178 Each intercostal has one crack.C : LH & RH intercostal replaced per ref DWG 65-16300 SHT.3 & SRM 51-30-2 pg 2-3 2 L 7 2 4F RT A16WE 2001080700308 20010807 00308 NM 2001 8 7 AWXA0002084 1 20010719 A 5347 65468136 SEAT TRACK BOEING 737 737277 1384570 NM STA 360-947 NICKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 D: Nicks on LBL 24.75 seat track at various locations from STA 360-947C: Nicks blended and assessed per SRM 53-10-1 pg 1 8 STA 520-540 track replaced per SRM 51-30-2 pg 8 2 L 7 2 4F RT A16WE 2001080700309 20010807 00309 NM 2001 8 7 AWXA0002085 1 20010724 A 5347 BAC1520792 SEAT TRACK BOEING 737 737277 1384570 NM STA 360-947 NICKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 D: Various nicks found along seat track LBL 45-50 STA 360-947C: Nicks dressed and assessed per SRM 51-10-1 Pg 18 STA 540 -564 track repaired per SRM 53-10-5 Fig 2 Pg 2-5 2 L 7 2 4F RT A16WE 2001080700310 20010807 00310 NM 2001 8 7 AWXA0002086 1 20010724 A 5313 6545776564 STRINGER BOEING 737 737277 1384570 NM STA 727 -727A CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 183AW 22654 D: S-26L STA 727-727A +10 corroded beyond limits.C: S-26L STA 727-727A +10 repaired per SRM 53-10-3 Fig 1 pg 2 and SRM 5 1-30-2 pg 2 & 8 2 L 7 2 4F RT A16WE 2001080700311 20010807 00311 NM 2001 8 7 AWXA0002087 1 20010726 A 5347 BAC1520792 SEAT TRACK BOEING 737 737277 1384570 NM STA 360-947 NICKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 D: Seat track RBL 45-50 STA 360-947 is nicked @ various locations.C: Track blended and protected per SRM 53-10-1 pg 18. STA 520-540 track replaced per SRM 51-30-2 Pg * STA 827 track repaired per SRM 53-10-5 pg 3, and SRM 51-30-2 PG 8 2 L 7 2 4F RT A16WE 2001080700312 20010807 00312 NM 2001 8 7 AWXA0002089 1 20010726 A 5330 6545778501 SKIN BOEING 737 737277 1384570 NM AFT SERV.CUT OUT CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 D: Aft service doorway Fwd Lwr corner cutout is cracked.C: Crack repaired as per SRM 53-30-3 Fig 24 pg 83-86H 2 L 7 2 4F RT A16WE 2001080700313 20010807 00313 NM 2001 8 7 AWXA0002094 1 20010802 A 5330 6545775 SKIN BOEING 737 737277 1384570 NM A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 183AW 22630 D: Fuselage R/H Skin STA 727-777 STR 14R-20R found to have several existing skin repairs adjacent to each other.C: repai red per ER 15-5331-01206-SS3 2 L 7 2 4F RT A16WE 2001080700314 20010807 00314 NM 2001 8 7 AWXA0002088 1 20010726 A 5347 BAC1520792 SEAT TRACK BOEING 737 737277 1384570 NM A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 D: Seat track @ RBL 24-75 STA 360-947 Nicked at Various Locations.C: Track blended at various locations and Assessed Per SRM 53-10-1 Pg 18. Track repaired per SRM 51-30-2 PG 8, SRM 53-10-5 pg 2, SRM 53-10-1 pg 8, SRM 53-10-5 PG 8 2 L 7 2 4F RT A16WE 2001080700315 20010807 00315 WP 2001 8 7 USAAD01126 1 20010615 A 3222 STRUT DOUG DC9 DC981 3022081 WP NLG LACK OF LUBE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 813US 48093 ORD-PIT - FLT 1556 - AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED W ITHOUT INCIDENT. MAINTENANCE SERVICED THE NOSE LANDING GEAR STRUT. (M) 2 L 7 2 4F A6WE 2001080700316 20010807 00316 WP 2001 8 7 USAAD01128 1 20010614 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 829US 49429 CLT - THE CEILING EMERGENCY LIGHTS A SEAT ROWS 20 THROUGH 24 ILLUMINATE WITH THE POWER SHUTOFF. MAINTENANCE REPLACED TH E EMERGENCY LIGHT POWER SUPPLY. (M) 2 L 7 2 4F A6WE 2001080700317 20010807 00317 WP 2001 8 7 USAAD01133 1 20010708 A 2131 21171802 CONTROLLER DOUG DC9 DC981 3022081 WP CABIN PRESSURE FAILED A USAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 801US 7908 48037 TPA-PIT - FLT 302 - THE CABIN ALTITUDE WARNING LIGHT ILLUMINATED AT 28,000 FEET. THE CREW STARTED AN EMERGENCY DESCENT BUT THE OXYGEN MASKS DEPLOYED. THE OXYGEN MASKS ABOVE SEATS 1A AND C DID NOT DEPLOY. THE AIRCRAFT LANDED AT ITS DESTIN ATION WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 PRESSURIZATION CONTROLLER AND ADJUSTED THE OXYGEN MASK RELEASE LA TCH FOR SEAT 1A AND C. (M) 2 L 7 2 4F A6WE 2001080700318 20010807 00318 EU 2001 8 7 USAAF01022 1 20010510 A 3230 LANDING GEAR FOKKER F28 F28MK0100 4990807 EU NLG LACK OF LUBE A USAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 19 865US 11308 PIT-SBN - FLT 1152 - ON APPROACH INTO SBN, THE NOSE LANDING GEAR DID NOT INDICATE DOWN. A GO AROUND WAS MADE WITH THE G EAR BEING CYCLED. THE GEAR WAS LOWERED AGAIN, AND THIS TIME RECEIVED AN ALL GREEN INDICATION. FLIGHT LANDED WITHOUT FU RTHER INCIDENT. MAINTENANCE LUBED THE NOSE LANDING GEAR. FUNCTIONALLY TESTED OK. (M) 2 L 7 2 4F RT 2001080700319 20010807 00319 EU 2001 8 7 USAAF01033 1 20010615 A 2170 5391 COALESCER BAG FOKKER F28 F28MK0100 4990807 EU A/C BAY CONTAMINATED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 887US 11349 TRI-CLT - FLT 242 - THE AIRCONDITIONING PACKS PRODUCED AN ODOR DURING CRUISE AND WOULD NOT COOL THE CABIN. THE FLIGHT C ONTINUED AND LANDED IN CLT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT WATER SEPARATOR BAG AND REPAIRED A LEAK AT THE DUCT ON THE AIR CYCLE MACHINE. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT 2001080700320 20010807 00320 EU 2001 8 7 USAAF01038 1 20010629 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN MALFUNCTIONED A USAA K NONE O OTHER AP APPROACH 1 EA 19 880US 11331 CLT - THE EMERGENCY LIGHTS AT THE EMERGENCY OVERWING EXITS DO NOT ILLUMINATE WITH THE LANDING GEAR DOWN. MAINTENANCE RE SET CIRCUIT BREAKER G-17. OPERATIONALLY CHECK OK. (M) 2 L 7 2 4F RT 2001080700321 20010807 00321 EU 2001 8 7 USAAF01039 1 20010630 A 3350 9EL00621200 SIGN FOKKER F28 F28MK0100 4990807 EU CABIN UNSERVICEABLE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 896US 11391 RDU - THE RIGHT OVERWING EXIT SIGN WAS FOUND IN POOR CONDITION. MAINTENANCE REPLACED THE EXIT SIGN. OPERATIONALLY CHEC KED OK. (M) 2 L 7 2 4F RT 2001080700322 20010807 00322 EU 2001 8 7 USAAF01041 1 20010703 A 3350 6040681 POWER SUPPLY FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 867US 11312 IND - THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE IN THE MIDDLE CABIN AREA. MAINTENANCE REPLACED THE NR 5 POWER SUPPLY UNIT. OPERATIONALLY CHECK OK. (M) 2 L 7 2 4F RT 2001080700323 20010807 00323 EU 2001 8 7 USAAF01042 1 20010704 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN MALFUNCTIONED A USAA K NONE O OTHER AP APPROACH 1 EA 19 890US 11365 CLT - THE OVERWING EXIT LIGHTS DO NOT ILLUMINATE WHEN THE LANDING GEAR IS DOWN. MAINTENANCE RESET CIRCUIT BREAKER 17G. OPERATIONALLY CHECK OK. (M) 2 L 7 2 4F RT 2001080700324 20010807 00324 EU 2001 8 7 USAASA01023 1 20010607 A 3350 32145410 POWER SUPPLY AIRBUS 330 A330202 3930316 EU CABIN DISCHARGED A USAA K NONE L NO TEST NR NOT REPORTED 1 EA 19 108UW 1061 CLT - FOUND THE EMERGENCY EXIT LIGHTS FAILED TO ILLUMINATE, AT THE LEFT OVERWING EXIT AND OVERHEAD AISLE, WITH THE NO SM OKING LIGHTS SELECTED ON. THE LIGHTS CAME ON WHEN THE EMERGENCY LIGHTS WERE SWITCHED ON. MAINTENANCE REPLACED THE EMER GENCY POWER SUPPLY UNIT AT THE LEFT OVERWING EXIT. OPS CHECKED OK. (M) 2 L 7 2 4F RT A46NM 2001080700326 20010807 00326 EU 2001 8 7 USAASA01026 1 20010620 A 3350 LIGHT AIRBUS 320 A320214 EU CABIN MALFUNCTIONED A USAA K NONE O OTHER NR NOT REPORTED 1 EA 19 122UW 1298 PHL - THE EMERGENCY EXIT LIGHTS CAME ON WHEN THE NO PERSONAL ELECTRONIC DEVICES SWITCH WAS TURNED ON. MAINTENANCE CYCLE D THE EMERGENCY LIGHTING SWITCH AND THE NO PERSONAL ELECTRONIC DEVICES SWITCH. BOTH SWITCHES CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2001080700328 20010807 00328 EA 2001 8 7 COMA0160553 1 20010805 A 5346 60137019 WEB CNDAIR CL600 CL6002B19 EA CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 949CA 14137 7080 ENGINE SUPPORT BEAM IS CRACKED ON CENTER OF TOP WEB.PERFORMED A TEMPORARY MAJOR REPAIR TO CRACKED ENGINE SUPPORT BEAM I/ A/W CANADAIR REO 601R-53-61-315 REV B. 2 L 7 2 4F RT A21EA 2001080700329 20010807 00329 EU 2001 8 7 USAASA01027 1 20010620 A 3230 LANDING GEAR AIRBUS A319 A319112 EU NLG & MLG MALFUNCTIONED A USAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 19 764US 1369 PIT-PHL - FLT 1161 - ON TAKEOFF, THE LANDING GEAR DID NOT RETRACT UNTIL RECYCLED. ON LANDING, RECEIVED AMBER LANDING GE AR SYSTEM DIS MESSAGE. THE MESSAGE THEN CLEARED AND ALL SYSTEMS RETURNED TO NORMAL. THE FLIGHT LANDED WITHOUT INCIDENT . MAINTENANCE PERFORMED THE CENTRAL FAULT DISPLAY SYSTEM (CFDS) AND BITE CHECKS OF LANDING GEAR CONTROL AND INTERFACE U NIT'S (LGCIU) ONE AND TWO. BOTH SYSTEMS CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2001080700330 20010807 00330 EU 2001 8 7 USAASA01028 1 20010626 A 3350 321430 BATTERY PACK AIRBUS A319 A319112 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 719US 1084 PIT - THE EMERGENCY LIGHTS SYSTEM FAILED THE EMERGENCY POWER SUPPLY TEST. MAINTENANCE REPLACED THE LEFT EMERGENCY POWER SUPPLY UNIT BATTERY PACK. PERFORMED THE EMERGENCY LIGHT TEST. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2001080700334 20010807 00334 EA 2001 8 7 COMA0160554 1 20010805 A 5346 60137019 WEB CNDAIR CL600 CL6002B19 EA CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 949CA 14137 7080 ENGINE SUPPORT BEAM LOWER WEB CRACKED ON RIGHT SIDE.PERFORMED A MAJOR REPAIR TO ENGINE SUPPORT BEAM LOWER WEB I/A/W CANA DAIR REO 601R-53-61-366 REV C. 2 L 7 2 4F RT A21EA 2001080700342 20010807 00342 EA 2001 8 7 COMA0160556 1 20010803 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 807CA 7364 CEILING EMERGENCY LIGHTING ABOVE ROW TWO IS INOPERATIVE.TRANSFERRED INOPERATIVE EMERGENCY LIGHTING TO DDL PER MEL 33-51- 01. 2 L 7 2 4F RT A21EA 2001080700343 20010807 00343 NM 2001 8 7 USAASB01120 1 20010429 A 3230 LANDING GEAR BOEING 737 7372B7 1384560 NM NLG & MLG MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 288AU 23135 TPA - FLT 2714 - ON CLIMB-OUT FROM TPA, THE RT MLG RED LIGHT ILLUMINATED. CREW CYCLED GEAR. WITH GEAR HANDLE UP, BOTH MLG RED LIGHTS ILLUMINATED. WITH GEAR HANDLE IN OFF, THE LT MLG CAME DOWN AND WENT GREEN WHILE NLG AND RT MLG STAYED OF F. WITH GEAR HANDLE IN DOWN POSITION, ALL THREE GEAR INDICATIONS WERE GREEN. FLIGHT RETURNED TO FIELD AND LANDED WITHO UT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE PERFORMED MLG EXTENSION AND RETRACTION TEST. CYCLED GEAR REPEATEDL Y. COMPLETELY LUBED LT AND RT MLG. ALSO, FOUND RT MLG RED INDICATION ON P2-3 PANEL JAMMED IN SOCKET. REMOVED AND REPLA CED LIGHT ASSEMBLY. CYCLED ALL GEAR AGAIN. OPS CHECK NORMAL. (M) 2 L 7 2 4F A16WE 2001080700345 20010807 00345 NM 2001 8 7 USAASB01133 1 20010511 A 2131 7638101 CONTROLLER BOEING 737 737301 1384611 NM CABIN PRESSURE FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 591US 36094 23936 BOS - FLT 1116 - ON CLIMB-OUT FROM BOS, EN ROUTE PHL AT 6,000 FEET, THE CABIN RATE OF CLIMB WAS FLUCTUATING FROM 3,000 F EET PER MINUTE TO 2,000 FEET PER MINUTE IN AUTO MODE. MANUAL MODE WAS INOPERATIVE. AIRCRAFT FAILED TO PRESSURIZE, SO T HE FLIGHT RETURNED TO FIELD AT BOS AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER. OPS CHECK PER MM 21-31-00. ALL SYSTEMS CHECK NORMAL. MANUAL MODE CHECKED NORMAL ON THE GROUND. (M) 2 L 7 2 4F RT A16WE 2001080700348 20010807 00348 EA 2001 8 7 COMA0160557 1 20010805 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 EA FAULTY A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 431CA 413 7472 FAINT ELECTRICAL ODOR FROM THE GALLEY AREA DISCOVERED AFTER LANDING.REPLACED THE EMERGENCY LIGHTING POWER SUPPLY BATTERY PACK. 2 L 7 2 4F RT A21EA 2001080700349 20010807 00349 NM 2001 8 7 USAASB01137 1 20010513 A 3350 20131A BATTERY PACK BOEING 737 7374B7 1384702 NM GALLEY DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 780AU 24997 CLT - DURING OVERNIGHT CHECK, MAINTENANCE FOUND NUMEROUS EMERGENCY LIGHTS IN THE AFT GALLEY INOPERATIVE. MAINTENANCE RE MOVED AND REPLACED THE RIGHT BATTERY PACK IN THE AFT GALLEY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001080700350 20010807 00350 EA 2001 8 7 COMA0160558 1 20010805 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA A COMA O OTHER S AFFECT SYSTEMS IN INSP/MAINT 1 SO 01 420CA 7451 LEFT MOST AFT CABIN CEILING EMERGENCY LIGHT IS INOPERATIVE.DEFERRED INOPERATIVE EMERGENCY LIGHT PER MEL 33-51-01. 2 L 7 2 4F RT A21EA 2001080700352 20010807 00352 NM 2001 8 7 USAASB01138 1 20010516 A 3350 20121 CHARGER BOEING 737 7373B7 1384580 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 395US 23317 CLE - MAINTENANCE FOUND THE EMERGENCY LIGHTS IN NR 2 AND NR 3 BULL NOSE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED T HE BATTERY CHARGER ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001080700354 20010807 00354 2001 8 7 USAASB01141 4 20010520 A 3417 406100901 ADC BOEING 737 737301 1384611 NM E/E BAY FAILED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 EA 19 577US 32116 23742 PVD - FLT 310 - ON TAKEOFF FROM DCA, EN ROUTE TO PVD, CREW DETECTED AN ACRID SMELL IN THE COCKPIT. SMELL WENT AWAY EVEN TUALLY. CREW REPORTED THAT THEY HAD NO V-NAV, THE FIRST OFFICERS ALTIMETER WAS OFF AND THE AUTOTHROTTLES WERE INOPERATI VE. FLIGHT CONTINUED AND LANDED AT PVD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 2 AIR DATA COMPUT ER. SYSTEM FUNCTIONAL CHECK PERFORMED AND FOUND SATISFACTORY PER MM. (M) 2 L 7 2 4F RT A16WE 2001080700356 20010807 00356 NM 2001 8 7 USAASB01143 1 20010522 A 3350 6013211 BATTERY PACK BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 262AU 22868 BWI - THE FORWARD DOOR EMERGENCY EXIT SIGNS AND EXTERIOR SLIDE ESCAPE LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK AND POWER PACK MODULE. (M) 2 L 7 2 4F A16WE 2001080700358 20010807 00358 NM 2001 8 7 USAASB01144 1 20010523 A 3350 GROUND WIRE BOEING 737 7374B7 1384702 NM COCKPIT BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 434US 24556 PHL - PILOT REPORTED THAT THE FLIGHT DECK EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE FOUND A BROKEN GROUND WIRE. REPA IRED GROUND WIRE. FLIGHT DECK EMERGENCY LIGHT OPERATIONALLY CHECKS GOOD. (M) 2 L 7 2 4F RT A16WE 2001080700360 20010807 00360 NM 2001 8 7 USAASB01145 1 20010524 A 3350 900835A POWER SUPPLY BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 270AU 22882 BWI - THE FORWARD CABIN EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (M) 2 L 7 2 4F A16WE 2001080700362 20010807 00362 NM 2001 8 7 USAASB01149 1 20010529 A 3350 30043229 LIGHT BOEING 737 737201 1384454 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 249US 22756 IAD - MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT OVERWI NG EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 2001080700364 20010807 00364 NM 2001 8 7 USAASB01155 1 20010602 A 3350 500000043 CHARGER BOEING 737 7372B7 1384560 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 273AU 22885 LGA - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE OVERWING EMERGENCY EXIT LOCATOR LIGHT INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE CHARGER ASSEMBLY AND BATTERY PACK M1052 (P/N 9008-3-5A). OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 2001080700369 20010807 00369 EA 2001 8 7 COMA0160559 1 20010805 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA A COMA O OTHER S AFFECT SYSTEMS IN INSP/MAINT 1 SO 01 786CA 7333 THE EMERGENCY FLOOR LIGHTING FROM ROW 9 AFT IS INOPERATIVE.REMOVED, CLEANED AND RE-SECURED ELECTRICAL CONNECTOR FOR AFFE CTED EMERGENCY LIGHTING. 2 L 7 2 4F RT A21EA 2001080700370 20010807 00370 EA 2001 8 7 COMA0160560 1 20010805 A 2751 855D100275B SENSOR CNDAIR CL600 CL6002B19 EA FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 932CA 1 7038 FLAP FAIL CAUTION MESSAGE AT 2 DEGREES DURING APPROACH INTO CVG, CREW DECLARED AN EMERGECY, AIRCRAFT LANDED SAFELY.REPLA CED THE RIGHT BRAKE AND POSITION SENSING UNIT. 2 L 7 2 4F RT A21EA 2001080700371 20010807 00371 EA 2001 8 7 COMA0160555 1 20010730 A 5300 60135006 WEB CNDAIR CL600 CL6002B19 EA CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 976CA 11434 7151 CRACKS FOUND AT LEFT AND RIGHT LOWER SKIN ACCESS PANELS.REPAIRED CRACKS IN LEFT AND RIGHT LOWER ENGINE SUPPORT BEAM I/A/ W REO 601R-53-61-366. 2 L 7 2 4F RT A21EA 2001080700372 20010807 00372 EA 2001 8 7 COMA0160561 1 20010804 A 3260 UPLOCK TARGET CNDAIR CL600 CL6002B19 EA A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 810CA 7370 DURING CLIMB-OUT OF YYZ, GEAR DISAGREE WARNING MESSAGE DISPLAYED, AIRCRAFT RTURNED TO THE FIELD.ADJUSTED ONE PROXIMITY S ENSOR TARGET, GEAR RETRACTION TEST WAS SATISFACTORY. 2 L 7 2 4F RT A21EA 2001080700373 20010807 00373 EA 2001 8 7 COMA0160562 1 20010804 A 2751 860D10018ABC FCU CNDAIR CL600 CL6002B19 EA FAULTY A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 965CA 3437 7131 DURING APPROACH INTO CVG, THE FLAP CAUTION MESSAGE ACTIVATED WHEN FLAPS WERE SELECTED TO 45 DEGREES.REPLACED THE FLAP EL ECTRONIC CONROL UNIT. 2 L 7 2 4F RT A21EA 2001080700374 20010807 00374 NM 2001 8 7 USAASB01156 1 20010602 A 2910 65C268091072 HYDRAULIC LINE BOEING 737 7373B7 1384580 NM HYDRAULIC SYS LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 389US 23311 DCA - FLT 2299 - AFTER T/O , AS THE LANDING GEAR RETRACTED, RECEIVED A RED LIGHT FOR THE RT MLG. THEN RECEIVED A RED LIG HT FOR THE A SYS HYDRAULIC. CONTINUED TO CLIMB TO FL190 THEN PERFORMED PROCEDURES FOR A SYS HYDRAULIC FAILURE. DECLARED AN EMERGENCY AND RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT MLG ACTUATOR PRESSURE LINE AND SPOILER B SYS RETURN LINE LEAKING AND CHAFED AGAINST ONE ANOTHER. REMOVED AND REPLACED HYDRAULIC LINES. REMOVED AND REP LACED THE A SYS ELECTRIC HYDRAULIC PUMP (P/N MPEV3-056-9A) AND NR 1 ENG DRIVEN HYDRAULIC PUMP (P/N 65075-06) AS PRECAUTI ON. SERVICED HYDRAULICS. OPS CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001080700375 20010807 00375 SO 2001 8 7 SIMA200117902 1 20010628 A 3234 CONTROL HANDLE EMB 145 EMB145LR SO COCKPIT MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 600BK 145044 IND- FLT 9760 - DURING CLIMB, CREW REPORTED THE LANDING GEAR HANDLE COULD NOT BE MOVED TO THE UP POSITION. EICAS SHOWED A LANDING GEAR AIR/GROUND FAIL MESSAGE. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL CHECK OF LANDING GEA R RETRACT EXTEND SYSTEM WAS GOOD IAW EMB MM. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001080700376 20010807 00376 NM 2001 8 7 USAA010780 1 20010702 A 5320 SPLICE BOEING 737 7372B7 1384560 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 282AU 23115 CLT - FOUND STRINGER SPLICE CORRODED 1 INCH BY 4 INCHES, BS 986.5, STRINGER 27L. REMOVED AND REPLACED STRINGER SPLICE P ER SRM 53-10-3 FIG 1. (M) 2 L 7 2 4F A16WE 2001080700377 20010807 00377 EA 2001 8 7 COMA0160563 1 20010804 A 5280 601R751461 VALVE CNDAIR CL600 CL6002B19 EA FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 915CA 37 7013 AFTER TO FROM CVG THE NOSE GEAR DOOR WARNING MESSAGE ACTIVATED, AIRCRAFT SAFELY TO THE FIELD.REPLACED THE NOSE LANDING G EAR SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2001080700378 20010807 00378 EA 2001 8 7 COMA0160552 1 20010805 A 5346 60137019 WEB CNDAIR CL600 CL6002B19 EA CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 949CA 14137 7080 ENGINE SUPPORT BEAM LOWER WEB CRACKED ON LEFT SIDE.PERFORMED A MAJOR REPAIR TO ENGINE SUPPORT BEAM LOWER NIB I/A/W CANAD AIR REO 601R-53-61-366 REV C. 2 L 7 2 4F RT A21EA 2001080700379 20010807 00379 EA 2001 8 7 COMA0160544 1 20010801 A 5346 60135006 WEB CNDAIR CL600 CL6002B19 EA CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 932CA 16929 7038 ENG SUPPORT BEAM UPPER WEB CRACKED.REPAIRED I/A/W REO 601R-53-61-345. 2 L 7 2 4F RT A21EA 2001080700380 20010807 00380 NM 2001 8 7 USAA010797 1 20010612 A 3221 SUPPORT FITTING BOEING 737 7372B7 1384560 NM NLG CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 282AU 43853 23115 PIT - FOUND SUPPORT FITTING CORRODED .020 INCH - .010 INCH, NOSE GEAR RIGHT TRUNNION SUPPORT FITTING BORE. REAMED BORE, INSTALLED SLEEVE PER EA 71444. (M) 2 L 7 2 4F A16WE 2001080700381 20010807 00381 NM 2001 8 7 USAA010855 1 20010607 A 5320 FLOOR SUPPORT BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 576US 43413 23741 PIT - FOUND FLOOR SUPPORT CORRODED 1 INCH BY 1 INCH SPOT, STATION 727C CHANNEL NR 5 FLOOR SUPPORT. BLENDED PER 53-60-51 FIG 101. CORROSION LEVEL 1. (M) 2 L 7 2 4F RT A16WE 2001080700382 20010807 00382 NM 2001 8 7 USAA010867 1 20010710 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 44174 23232 CLT - FOUND FUSELAGE SKIN CRACKED 1.25 INCH, BS 887, STRINGER 23R. INSTALLED REPAIR DOUBLER PER SRM 51-00-01. (M) 2 L 7 2 4F RT A16WE 2001080700383 20010807 00383 NM 2001 8 7 USAA010874 1 20010718 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND FRAME UPPER FLANGE DENTED, 1 INCH LONG, BS 747 RBL 24 AFT CARGO FLOOR. DAMAGE REMOVED, INSTALLED DOUBLER PE R TYPICAL REPAIR 53-60-07. (M) 2 L 7 2 4F RT A16WE 2001080700384 20010807 00384 NM 2001 8 7 USAA010875 1 20010718 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FUSELAGE GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND BULKHEAD WEB GOUGED .016 INCH DEEP BY .150 INCH LONG, BS 178 WL 176 LBL 5.5. TRIMMED OUT DAMAGE, INSTALLED REPAIR DOUBLER PER EO 5300V153 AND EA 69798. (M) 2 L 7 2 4F RT A16WE 2001080700385 20010807 00385 EA 2001 8 7 COMA0160564 1 20010802 A 3260 16400105 DRAG BRACE CNDAIR CL600 CL6002B19 EA MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 931CA 16568 7037 NLG UNSAFE INDICATION.REPLACED THE NLG DRAG BRACE. 2 L 7 2 4F RT A21EA 2001080700386 20010807 00386 NM 2001 8 7 USAA010884 1 20010718 A 5240 6545871523 SKIN BOEING 737 7373B7 1384580 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 45591 22957 TPA - FOUND DOOR EXT SKIN CRACKED .25 INCH, FORWARD SERVICE DOOR, UPPER HINGE CUTOUT. REPAIR DOUBLER INSTALLED PER SRM 52-10-01 PAGE 201 AND SB 737-52-1096. (M) 2 L 7 2 4F RT A16WE 2001080700387 20010807 00387 EA 2001 8 7 COMA0160565 1 20010802 A 2750 7455001 CONTROL SWITCH CNDAIR CL600 CL6002B19 EA MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS LD LANDING 1 SO 01 818CA 577 7408 FLAPS FAILED AT 26 DEGREES AFTER LANDING.REPLACED THE FLAP SELECTOR CONROL HANDLE ASSY. 2 L 7 2 4F RT A21EA 2001080700388 20010807 00388 NM 2001 8 7 USAA010899 1 20010720 A 5314 KEELBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND KEEL BEAM STRINGER CORRODED 3 INCHES BY 4 INCH AREA, BS 727D TO E, LEFT KEEL BEAM. CORROSION LEVEL 2, TASK NR C53-202-01. REMOVED KEEL BEAM, REMOVED CORROSION, REINSTALLED KEEL BEAM AND REPAIR DOUBLER/TRIPLER PER EA 69835. (M ) 2 L 7 2 4F RT A16WE 2001080700389 20010807 00389 NM 2001 8 7 USAA010900 1 20010720 A 5314 KEELBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND KEEL BEAM CHORD CORRODED 6 INCHES BY 2 INCHES, BS 500C PLUS 9 TO 500D, RBL 7. DAMAGE REMOVED, INSTALLED REP AIR ANGLES PER SRM 53-30-12 FIG 202, EA 69842. (M) 2 L 7 2 4F RT A16WE 2001080700390 20010807 00390 NM 2001 8 7 USAA010901 1 20010720 A 5310 SHEAR TIE BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND FRAME SHEAR TIE CORRODED 14 INCH AREA, BS 727A, LBL 7 AND RBL 7. CORROSION LEVEL 1 TASK NR C53-202-01. REM OVED AND REPLACED SHEAR TIE PER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 2001080700391 20010807 00391 NM 2001 8 7 USAA010903 1 20010720 A 5551 ATTACH FITTING BOEING 737 7373B7 1384580 NM HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND ATTACH LUG FITTING CORRODED .75 INCH TOTAL SURFACE AREA, LEFT HORIZONTAL STABILIZER CENTER SECTION, FRONT LO WER FORWARD LUG. CORROSION REMOVED, FABRICATED AND INSTALLED NEW BUSHING PER SRM 55-10-10. (M) 2 L 7 2 4F RT A16WE 2001080700392 20010807 00392 EA 2001 8 7 COMA0160566 1 20010801 A 2751 855D1009 SENSOR CNDAIR CL600 CL6002B19 EA FAULTY A COMA K NONE S AFFECT SYSTEMS CR CRUISE 1 SO 01 932CA 0 7038 FLAP FAIL CAUTION MESSAGE DURING CRUISE FLIGHT, CREW DECLARED AN EMERGENCY, LANDED SAFELY AT GSP DESTINATION CITY.REPLAC ED THE RIGHT BRAKE AND POSITION SENSING UNIT. 2 L 7 2 4F RT A21EA 2001080700393 20010807 00393 NM 2001 8 7 USAA010904 1 20010720 A 5551 ATTACH FITTING BOEING 737 7373B7 1384580 NM HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND LUG ATTACH FITTING CORRODED APPROX 5 INCH AREA, LEFT HORIZONTAL STABILIZER CENTER SECTION, REAR SPAR FORWARD LUG, FORWARD FACE. LUG SPOT FACED TO DEPTH OF .070 INCH PER SRM 55-10-10 GRAPH II. (M) 2 L 7 2 4F RT A16WE 2001080700394 20010807 00394 NM 2001 8 7 USAA010905 1 20010720 A 5551 ATTACH FITTING BOEING 737 7373B7 1384580 NM HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 22950 CLT - FOUND UPPER ATTACH LUGS APPROX .5 INCH TOTAL AREA, CORRODED, LEFT HORIZONTAL STABILIZER CENTER SECTION, FRONT SPAR . REAMED CLEVIS TO REMOVE CORROSION, MACHINED AND INSTALLED NEW BUSHING PER SRM 55-10-10. (M) 2 L 7 2 4F RT A16WE 2001080700395 20010807 00395 EA 2001 8 7 COMA0160567 1 20010806 A 5320 60034017351 ANGLE CNDAIR CL600 CL6002B19 EA CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 978CA 10541 7158 THE FWD "J" ANGLE AT FS 280, LBL9 TO RBL9 AT WL 73.5 IS CORRODED.REPLACED DISCREPANT PART I/A/W WVAC EO 601R-53-2631. 2 L 7 2 4F RT A21EA 2001080700397 20010807 00397 NM 2001 8 7 USAA010906 1 20010713 A 5312 BULKHEAD BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 35919 23989 CLT - FOUND NUMEROUS CRACK .2 INCH TO 1 INCH, BULKHEAD WEB BS 178 WL 198 TO 213, LBL 6.5 TO RBL 6.5. DAMAGE REMOVED, RE PAIR DOUBLER INSTALLED PER SRM 53-10-08 FIG 211, EA 85068, AND EO 5300V153. (M) 2 L 7 2 4F RT A16WE 2001080700400 20010807 00400 NM 2001 8 7 USAA010907 1 20010713 A 5312 BULKHEAD BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 35919 23989 CLT - FOUND TWO CRACKS 1 INCH LONG, BS 178, WL 195 AT RBL 7, WL 202 AT LBL 5.7. REMOVED AND REPLACED WEB STRAPS PER SRM 53-10-08, 53-10-02, 51-40-02 AND EO 5300V155. (M) 2 L 7 2 4F RT A16WE 2001080700402 20010807 00402 NM 2001 8 7 USAA010908 1 20010713 A 5312 BULKHEAD BOEING 737 737401 1384701 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 35919 23989 CLT - FOUND BULKHEAD WEB BLIND FASTENER INSTALLED DOUBLER, BS 178, WL 195 TO 203, RBL 17 TO RBL 27 APPROX 10 INCHES BY 1 2 INCHES. REMOVED DOUBLER, INSTALLED NEW DOUBLER PER SRM 53-10-08 FIG 211, EA 85068, AND EO 5300V153. (M) 2 L 7 2 4F RT A16WE 2001080700404 20010807 00404 NM 2001 8 7 USAA010909 1 20010713 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 35919 23989 CLT - FOUND SIDE CHORD CRACKED 1 INCH, BS 178, RIGHT SIDE WL 207. REMOVED DAMAGED SECTION, SPLICED IN NEW CHORD SECTION PER EO 5300V157. (M) 2 L 7 2 4F RT A16WE 2001080700405 20010807 00405 EA 2001 8 7 COMA0160568 1 20010806 A 5320 60034017351 ANGLE CNDAIR CL600 CL6002B19 EA CORRODED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 975CA 7150 THE FWD J ANGLE AT F.S. 280 BETWEEN LBL9.0 AND RBL9.0 IS CORRODED.REMOVED AND REPLACED THE FWD J ANGLE AT FS 280 BETWEEN LBL9.0 AND RBL9.0 P/N 600-34017-351 I/A/W WVAC E.O. 601R-53-2624. 2 L 7 2 4F RT A21EA 2001080700406 20010807 00406 NM 2001 8 7 USAA010910 1 20010713 A 5312 6545833040 PRESSURE PANEL BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 35919 23989 CLT - FOUND FLOORWEB CRACKED .25 INCH, BS 180, WL 207, RBL 28. REMOVED AND REPLACED FLOOR WEB PER SRM 51-40-02 AND EO 5 300V157. (M) 2 L 7 2 4F RT A16WE 2001080700407 20010807 00407 EA 2001 8 7 COMA0160569 1 20010805 A 2610 35592400 LOOP CNDAIR CL600 CL6002B19 EA FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 934CA 7042 LEFT 14TH STAGE DUCT WARNING MESSAGE DURING CRUISE FLIGHT, CREW DELCARED AN EMERGENCY, CREW SHUT-DOWN THE LEFT ENGINE DU RING FLIGHT.REPLACED THE LEFT 14TH STAGE OVER-HEAT DETECTION LOOP. 2 L 7 2 4F RT A21EA 2001080700408 20010807 00408 NM 2001 8 7 USAA010922 1 20010718 A 5320 69482042 CLIP BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 528AU 40898 24410 PIT - FOUND SKIN CLIP CRACKED .0001 BY .75 INCH, STATION 360 ABOVE 15L. INSTALLED REPAIR ANGLE PER SRM 53-00-07 AND 51- 10-02. (M) 2 L 7 2 4F RT A16WE 2001080700409 20010807 00409 NM 2001 8 7 USAA010923 1 20010720 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 507AU 46595 23382 PIT - FOUND VERTICAL CHORD CRACKED 1 INCH, BS 178 LBL 5. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLERS PER EO 5300V155. (M) 2 L 7 2 4F RT A16WE 2001080700410 20010807 00410 NM 2001 8 7 USAA010924 1 20010720 A 5347 65538444 TRACK BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 528AU 40898 24410 PIT - FOUND TIE DOWN RAIL.25 INCH BY .5 INCH, TIE DOWN RAIL RIGHT STATION 787-927. CORROSION LEVEL 1. DEFECTIVE PART R EPLACED WITH IDENTICAL PART PER 51-20-05, 07, 51-40-02, 03. (M) 2 L 7 2 4F RT A16WE 2001080700411 20010807 00411 SO 2001 8 7 COMA0110133 1 20010806 A 2751 FLAP TRACK EMB EMB 120 EMB120RT SO A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 269CA 1263 DURING LANDING APPROACH INTO EYW WHEN FLAPS WERE SELECTED FROM 25 TO 45 DEGREES, FLAP DISAGREE CAUTION ACTIVATED.REPLACE D THE FLAP ROLLERS FOR THE LEFT INBOARD FLAP AND THE RIGHT OUTBOARD FLAP. 2 L 7 2 4T RT A31SO 2001080700412 20010807 00412 NM 2001 8 7 USAA010925 1 20010720 A 5347 65538443 TRACK BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 528AU 40898 24410 PIT - FOUND TIE DOWN RAIL CORRODED .25 INCH BY .5 INCH, TIE DOWN RAIL STATION 787-927. DEFECTIVE PART REPLACED WITH IDE NTICAL PART PER 51-20-05, 07, 51-40-02, 03. (M) 2 L 7 2 4F RT A16WE 2001080700413 20010807 00413 NM 2001 8 7 USAA010928 1 20010718 A 5313 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 45591 22957 TPA - FOUND STRINGER CORRODED 4 INCHES, STRINGER 26 RIGHT AT STATION 1016. CORROSION LEVEL 2. REPAIRED STRINGER PER SR M 53-00-03 FIG 201. (M) 2 L 7 2 4F RT A16WE 2001080700414 20010807 00414 NM 2001 8 7 USAA010929 1 20010718 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 412US 37299 23881 PIT - FOUND VERTICAL CHORD CRACKED 1.5 INCHES, BS 178 RBL 5.7 WL 184. CUT OUT DAMAGED AREA, INSTALLED FILLER AND DOUBLE RS PER SRM 53-10-08, FIG 205 EA 71759, EO 5300V155. (M) 2 L 7 2 4F RT A16WE 2001080700415 20010807 00415 NM 2001 8 7 USAA010931 1 20010718 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 412US 37299 23881 PIT - FOUND SIDE CHORD CRACKED TWO PLACES 1 INCH, LBL 24 WL 207 WL 195. CUT OUT DAMAGED SECTION AND SPLICED IN NEW PER SRM 53-10-08, EO 5300V157. (M) 2 L 7 2 4F RT A16WE 2001080700416 20010807 00416 NM 2001 8 7 USAA010932 1 20010718 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 412US 37299 23881 PIT - FOUND SIDE CHORD HAS TWO CRACKS 1 INCH EACH, RBL 24 WL 207 WL 195. CUT OUT DAMAGED SECTION AND SPLICED IN NEW PER SRM 53-10-08, EO 5300V157. (M) 2 L 7 2 4F RT A16WE 2001080700417 20010807 00417 EU 2001 8 7 USAASA01038 1 20010722 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319112 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 715UW 6933 1051 BOS - THE EMERGENCY LIGHTS FAILED THE TEST ON THE CABIN INTERCOMMUNICATION DATA SYSTEM. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 11WL. (M) 2 L 7 2 4F RT A28NM 2001080700418 20010807 00418 NM 2001 8 7 USAASB01161 1 20010605 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 784AU 25023 BWI - MAINTENANCE FOUND THE LEFT FORWARD INTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND RE PLACED THE BATTERY PACK (P/N 2013-1A) AND CHARGER ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001080700419 20010807 00419 NM 2001 8 7 USAASB01167 1 20010607 A 3397 WIRE BOEING 737 737401 1384701 NM CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 EA 19 421US 23988 PVD - MAINTENANCE FOUND THE EMERGENCY LIGHT AT THE LAST SEAT ROW INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE BENEAT H THE SEAT. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001080700420 20010807 00420 NM 2001 8 7 USAASB01168 1 20010607 A 3350 BR9279108 LIGHT BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 437US 24559 ALB - PILOT REPORTED THAT THE EMERGENCY EXIT LIGHT ON SEAT 12C IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EME RGENCY EXIT IDENTIFIER LIGHT AT SEAT 12C. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001080700421 20010807 00421 NM 2001 8 7 USAASB01174 1 20010615 A 3350 500000043 CHARGER BOEING 737 7372B7 1384560 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 272AU 22884 BWI - MAINTENANCE FOUND THE AFT OVERHEAD EMERGENCY LIGHT BETWEEN ROW 19 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED T HE BATTERY PACK (P/N 9008-3-5A) AND CHARGER ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 2001080700422 20010807 00422 NM 2001 8 7 USAASB01177 1 20010616 A 3350 1012621 LIGHT BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 391US 23313 BWI - MAINTENANCE FOUND THE FLOOR LEVEL OVERWING EMERGENCY EXIT LIGHT BROKEN/INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001080700423 20010807 00423 NM 2001 8 7 USAASB01179 1 20010619 A 3350 BR9279109 SIGN BOEING 737 7372B7 1384560 NM CABIN BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 275AU 22887 BDL - THE LEFT OVERWING EMERGENCY EXIT SIGN WAS BROKEN. MAINTENANCE REPLACED THE EMERGENCY EXIT SIGN ASSEMBLY. (M) 2 L 7 2 4F A16WE 2001080700424 20010807 00424 NM 2001 8 7 USAASB01181 1 20010620 A 3350 900835A BATTERY BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 261AU 22867 BOS - THE PASSENGER CABIN CEILING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES . (M) 2 L 7 2 4F A16WE 2001080700425 20010807 00425 NM 2001 8 7 USAASB01196 1 20010707 A 3350 1010731 SIGN BOEING 737 7374B7 1384702 NM R2 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 784AU 25023 PHL - FOUND REAR EMERGENCY EXIT SIGN FOR THE R2 DOOR INOPERATIVE. MAINTENANCE REPLACED THE ASSEMBLY. (M) 2 L 7 2 4F RT A16WE 2001080700426 20010807 00426 NE 2001 8 7 WRN2001F00000 2 20010422 A 7250 TURBINE BLADES LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE ENGINE FAILED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 311EA 193A1012 10390 INSPECTION REVEALED IP TURBINE BLADE FAILURE. REMOVED AND REPLACED ENGINE IAW TRADEWINDS CARD L2-130-A01 AND FORMS TWM- 7103B AND TWM-7103BB. AIRCRAFT RUN AND LEAK CHECKED SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F 4 F A23WE E12EU 2001080700427 20010807 00427 NE 2001 8 7 WRN2001F00001 2 20010412 A 7230 COMPRESSOR LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE ENGINE STALLED A WRNA C ABORTED TAKEOFF R E J PARTIAL RPM/PWR LOSS VIBRATION/BUFFET WARNING INDICATION TO TAKEOFF 1 SO 05 311EA 193A1012 ON TAKEOFF ROLL AT 125 KNOTS, NR 1 ENGINE HAD COMPRESSOR STALL. VIBRATION INDICATOR AT 2 UNITS WITH CAUTION LIGHT ON. AIRCRAFT RETURNED TO GATE. PREPARATION FOR TWO ENGINE FERRY BEING ACCOMPLISHED IAW LOCKHEED MM AND TRADEWINDS GMM FOR E NGINE CHANGE AT MAINTENANCE BASE. (M) 2 L 7 3 4F 4 F A23WE E12EU 2001080700436 20010807 00436 EA 2001 8 7 SWIA200110016 1 20010709 A 5240 DOOR CNDAIR CL600 CL6002B19 EA NLG OPEN A SWIA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 NM 07 412SW 7101 ON DEPARTURE AT SPEED ABOVE 280 KNOTS, LOUD HIGH PITCH SOUND FROM FRONT OF AIRCRAFT. RETURNED TO SLC. FOUND SMALL DOOR , FOR NOSE DOOR SWITCH, OPEN. NO DAMAGE NOTED ON DOOR. CLOSED AND LATCHED DOOR. 2 L 7 2 4F RT A21EA 2001080700437 20010807 00437 WP 2001 8 7 ABXA010426 1 20010724 A 5300 99234359 ANGLE DOUG DC9 DC931 3022065 WP LT WHEEL WELL CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 SUPPORT STRUT MOUNT ANGLE CRACKED AT UPPER OUTBOARD SIDE OF THE LEFT WHEEL WELL. REPLACED ANGLE AND INSTALLED IAW DC-9 S RM 51-30-5. 2 L 7 2 4F A6WE 2001080700438 20010807 00438 WP 2001 8 7 ABXA010427 1 20010725 A 5300 591140617 LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 LONGERON 3 LEFT WAS CRACKED AT F.S. 160. REPAIRED AREA IAW DC-9 SRM 53-02, FIGURE 18. 2 L 7 2 4F A6WE 2001080700439 20010807 00439 WP 2001 8 7 ABXA010428 1 20010725 A 5300 99155351 INTERCOSTAL DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 LEVEL ONE CORROSION ON UPPER SURFACE OF INTERCOSTALS AT LONGERON 28 RIGHT AND 28 LEFT, BETWEEN F.S. 579 AND F.S. 598. BL ENDED AND TREATED CORROSION ON INTERCOSTAL AT LONGERON 28 RIGHT - 28 LEFT, F.S. 579-598, IAW DC-9 SRM 53. 2 L 7 2 4F A6WE 2001080700440 20010807 00440 WP 2001 8 7 ABXA010429 1 20010725 A 5300 39123471 FRAME DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 CRACK IN FRAME AT F.S. 408, LONGERON 29 RIGHT, UPPER SURFACE, JUST INBOARD OF DOOR CUT OUT WEB. REMOVED DAMAGED FRAME SE CTION. SPLICED SECTION IAW DC-9 SRM 53-03, FIGURE 2A. SPLICES D05904-3-7S-11 FROM DRAWING K05906. 2 L 7 2 4F A6WE 2001080700441 20010807 00441 NM 2001 8 7 C1HA200193011 1 20010803 A 3260 SWITCH BOEING 727 727212 138407G NM RIGHT MLG A C1HA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 293AS 21348 Rt. MLG unsafe lite illuminated during taxi.ACTION TAKEN:Pinned gear adjusted RT.MLG downlock switch actuator checks nor mal removed gear pins. 2 L 7 3 4F A3WE 2001080700442 20010807 00442 NM 2001 8 7 F3LA200100097 1 20010805 A 3244 314396 TIRE BOEING 737 7373Q8 1384670 NM SEPARATED A F3LA A UNSCHED LANDING K FLUID LOSS TO TAKEOFF 1 NM 03 318FL 26293 AIR TURN BACK. FLIGHT CREW REPORTED LOSS OF "A" SYSTEM HYDRAULICS. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITHO UT INCIDENT. MAINTENANCE PERFORMED AN OVERWEIGHT INSPECTION. FOUND NO. 2 MLG TIRE LOST CAP ON TAKEOFF, DAMAGING INBD. FORE FLAP, MID FLAP AND AFT FLAP. ALSO DAMAGED HYDRAULIC LINE TO MAIN GEAR CONTROL MODULE. REPAIR IS IN PROCESS. AN A DDENDUM WILL BE ISSUED WHEN REPAIR IS ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001080700443 20010807 00443 EU 2001 8 7 MALA010619 1 20010531 A 7810 LF07629 ENGINE BAC 146 AVRO146RJ85A 1500097 EU A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 505XJ E2313 During C-Check in CVG, during Tailpipe removal for Inspection, noted crack in casing 1 1/2" Aft of 4th Turbine Wheel at 1 o'clock position. Dimensions 3.500 L. Maintenance removed Engine SN LF07643, Installed new Engine SN/LF07629 refer to Task Card 7100-502 Power Plant removal and installation. 2 H 7 4 4F RT A49EU 2001080700444 20010807 00444 EU 2001 8 7 MALA010622 1 20010531 A 5410 HC716H9025000 STIFFENER BAC 146 AVRO146RJ85A 1500097 EU A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 505XJ E2313 Found during C-Check, #1 Engine nose Cowl Fwd Bulkhead has one stiffenrer cracked (32). Maintenance replaced #32 Stiffe ner PN HC716H9025-000, #1 Engine Nose Cowl IAW BAe SRM 54-10-11. 2 H 7 4 4F RT A49EU 2001080800005 20010808 00005 NM 2001 8 8 VNAA0107014 1 20010711 A 7700 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ECU DIRTY A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 436JS 3052 DURING THE TAKEOFF ROLL, THE CREW RECEIVED A ELECTRONIC CONTROL UNIT FAIL LIGHT AND A GENERATOR OFF LINE LIGHT. OUT STA TION MAINTENANCE INSPECTED AND CLEANED THE ELECTRONIC CONTROL UNIT CANNON PLUG IN ACCORDANCE WITH DORNIER MAINTENANCE MA NUAL 77-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001080800006 20010808 00006 WP 2001 8 8 ZW0A0103002 1 20010604 A 2133 MOUNT DOUG DC9 DC982 3022082 WP OUTFLOW VALVE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 907TW 49165 DURING CHECK-C MAINT FOUND BULGE IN FUSELAGE SKIN AND RIVET HEAD POPPING ABOVE LONGERON 22, BETWEEN OUTFLOW VALVE AND AF T LAV DUMP. INSTALLED NEW OUTFLOW MOUNT RING PER SPM 5-20-01 AND SRM 51-30-02. 2 L 7 2 4F A6WE 2001080800008 20010808 00008 WP 2001 8 8 ZW0A0103101 1 20010605 A 2120 COUPLING DOUG DC9 DC982 3022082 WP CABIN PRESSURE DEFECTIVE A ZW0A B G A EMER. DESCENT O2 MASK DEPLOYED UNSCHED LANDING O OTHER CR CRUISE 1 CE 13 941AS 49925 WHILE CREW WAS TROUBLESHOOTING A CABIN TEMPERATURE PROBLEM THE CABIN BEGAN TO CLIMB UNCONTROLLABLY. THE CREW INITIATED AN EMERGENCY DESCENT, MANUALLY DROPPED THE OXY MASKS, AND MADE AN UNSCHEDULED LANDING AT JFK. FOUND RT PACK RAM AIR COU PLING TO HEAT EXCHANGER AND RUBBER COUPLING FOR INLET WATER SEPARATOR ASSY WERE BOTH BAD. REPLACED COUPLING P/N 5956186 -501. CHECK-C 2-23-01 STL. 2 L 7 2 4F A6WE 2001080800009 20010808 00009 NM 2001 8 8 ZW0A0103205 1 20010610 A 3350 767 LIGHT BOEING 767 7673Y0 NM R4 DOOR INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 640TW 25411 THE SLIDE LIGHT WAS INOPERATIVE AT THE RT SIDE NUMBER 4 CABIN DOOR. REPLACED THE LAMP. CHECK-C 5-15-00. 2 L 7 2 4F RT A1NM 2001080800010 20010808 00010 WP 2001 8 8 ZW0A0103206 1 20010610 A 2910 B-NUT DOUG DC9 DC983 3022083 WP HYDRAULIC SYS LOOSE A ZW0A A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 13 9616G 53563 SMOKE WAS OBSERVED FROM THE LEFT AFT LAVATORY AND AFT CABIN. FOUND HYDRAULIC LEAK FWD OF THE APU INLET DOORS. TIGHTENE D B-NUT ON A HYDRAULIC LINE AT THE LEFT THRUST REVERSER CONTROL VALVE. CHECK-C 8-18-00 JFK. 2 L 7 2 4F RT A6WE 2001080800011 20010808 00011 2001 8 8 ZW0A0103301 4 20010611 A 2397 WIRE DOUG DC9 DC982 3022082 WP PA SYSTEM CHAFED A ZW0A K NONE O OTHER NR NOT REPORTED 1 CE 13 905TW 49157 CREW REPORTED THE PA SYSTEM WAS INOPERATIVE FROM THE AFT FLIGHT ATTENDANT POSITION. FOUND SEVERAL WIRES HAD SHORTED AND BURNED FROM RUBBING ON A LIGHTENING HOLE. A COUPLE OF THE WIRES HAD BURNED THRU. DEACTIVATED AFFECTED SYSTEMS, CAPPED WIRES, AND MAINTENANCE FERRIED THE AIRCRAFT TO MCI, WHERE ALL DAMAGED WIRES WERE REPAIRED. THE LIGHTENING HOLE GROMMET WAS ALSO REPLACED. CHECK-C 4-12-01 MCI. 2 L 7 2 4F A6WE 2001080800012 20010808 00012 WP 2001 8 8 ZW0A0103401 1 20010608 A 5320 ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9615W 53562 DURING CHECK-C MAINT AT THE AFT ACCESSORY COMPT FOUND A CRACK IN ANGLE ON SIDE, LT VENT BOX AT STA 1510. INSTALLED NEW ANGLE ON ACFT WITH RIVETS PER SRM 51-10-02, PAGE 2. 2 L 7 2 4F RT A6WE 2001080800013 20010808 00013 WP 2001 8 8 ZW0A0103402 1 20010608 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 929TW 48014 DURING CHECK-C MAINT FOUND A CRACK IN MEMBRANE AT LONGERON 18R, STA 1302. REMOVED DAMAGED AREA AND REPAIRED PER SRM 53- 01 AND 51-30-2. 2 L 7 2 4F A6WE 2001080800014 20010808 00014 WP 2001 8 8 ZW0A0103403 1 20010608 A 5230 FITTING DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 929TW 48014 DURING CHECK-C MAINT THE FWD CARGO DOOR T-ANGLE WAS CRACKED APPROX 16 INCHES FWD OF AFT END AT TOP OF DOOR. REPLACED CR ACKED FITTING PER SRM 51-01, PAGE 1, ITEM C. 2 L 7 2 4F A6WE 2001080800015 20010808 00015 NM 2001 8 8 ZW0A0103404 1 20010612 A 5754 DOUBLER BOEING 767 7673Q8 NM L/E SLAT LOOSE A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 636TW 30301 THE RT WING NUMBER 8 SLAT HAD A REPAIR ON THE INBD EDGE THAT WAS LOOSE. A 6 IN BY 3 IN DOUBLER INSTALLED PER SRM 51-70- 10. APPLIED METAL TO METAL HOT BOND 250 DEG APPROX PER 57-71-10. CHECK-C 1-7-01 LAX. 2 L 7 2 4F RT A1NM 2001080800017 20010808 00017 WP 2001 8 8 ZW0A0103501 1 20010613 A 2170 17946081 SEPARATOR DOUG DC9 DC983 3022083 WP A/C BAY CONTAMINATED A ZW0A H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 13 9624T 53594 SMOKE AND ODOR APPEARED IN REAR CABIN. SWITCHED OFF THE LT AIR CONDITIONING PACK. FOUND LT PACK WATER SEPARATORS CONTA MINATED. REPLACED BOTH WATER SEPARATORS. CHECK-C 9-21-00 JFK. 2 L 7 2 4F RT A6WE 2001080800019 20010808 00019 WP 2001 8 8 ZW0A0103502 1 20010612 A 7830 WARNING LIGHT DOUG DC9 DC982 3022082 WP COCKPIT ILLUMINATED A ZW0A E ENGINE SHUTDOWN J E F WARNING INDICATION VIBRATION/BUFFET FLT CONT AFFECTED DE DESCENT 1 CE 13 909TW 49170 AT 19,000 FEET IN DESCENT RT ENGINE THRUST REVERSER UNLOCK LIGHT CAME ON. CREW REPORTED SOME VIBRATION AND YAW. THE EN GINE WAS SHUT DOWN. THE INVESTIGATION ON WHAT HAPPENED CONTINUES. CHECK-C 4-27-01 MCI. 2 L 7 2 4F A6WE 2001080800028 20010808 00028 WP 2001 8 8 ZW0A0103503 1 20010607 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 929TW 48014 DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT HAD CORROSION AT STA 180, RBL 9 TO 43. REPLACED SUPPORT PER SPM 6-70-01, PAGE 3 PARAGRAPH 4. 2 L 7 2 4F A6WE 2001080800031 20010808 00031 WP 2001 8 8 ZW0A0103504 1 20010607 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 929TW 48014 DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOORBEAM, STA 218 CENTERLINE. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-01 PAGE 1. 2 L 7 2 4F A6WE 2001080800035 20010808 00035 WP 2001 8 8 ZW0A0103505 1 20010607 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 929TW 48014 DURING CHECK-C MAINT FOUND LONGERON 17L CRACKED AT EACH HI-LOK TO FORMER 217, AT BOTH ATTACH POINTS TO FORMER 313, AT AT TACH POINT TO FORMER STA 256, AT BOTTOM HI-LOK TO FORMER 275, AND AT HI-LOK AND CONNECTION TO FORMER 237. REPLACED LONG ERON 17L FROM STA 228 TO 322 PER SRM 53-02, FIG 18. 2 L 7 2 4F A6WE 2001082200215 20010822 00215 SO 2001 8 22 COMA0110134 1 20010806 A 2751 COMPUTER EMB 120 EMB120RT SO T/E FLAP SYS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 269CA 1263 DURING LANDING APPROACH INTO MCO WHEN FLAPS WERE SELECTED FROM 25 TO 45 DEGREES AUDIBLE FLAP CAUTION ACTIVATED, CREW DEC LARED AN EMERGENCY AND LANDED SAFELY. INTERROGATED THE FLAP COMPUTER AND FOUND NUMEROUS FAULT CODES. CLEARED FAULT COD ES, PERFORMED OPERATIONAL CHECK WITH NO FURTHER DISCREPANCIES. 2 L 7 2 4T RT A31SO 2001080800036 20010808 00036 WP 2001 8 8 ZW0A0103506 1 20010607 A 5230 FLANGE DOUG DC9 DC983 3022083 WP CARGO DOOR CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DURING CHECK-C MAINT FOUND FWD SIDE OF FWD CARGO DOOR FLANGE INBD CRACKED OUT BELOW THE FWD CAM LATCH. STOP DRILLED AND REPAIRED PER SRM 52-05-26A. INSTALLED FASTENERS PER SRM 51-30-2 AND 51-30-5. TREATED PARTS PER SRM 51-10-3. 2 L 7 2 4F RT A6WE 2001080800037 20010808 00037 WP 2001 8 8 ZW0A0103507 1 20010607 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9615W 53562 DURING CHECK-C MAINT FOUND CORROSION ON UNDER SIDE OF LT TRACK SPLICE IN AFT CARGO COMPT, STA 1212 TO 1225. REMOVED SPL ICE. CLEANED CORROSION PER SPM 6-80-01. OTBD SECTION REPLACED WITH NEW PART PER SPM 6-70-01. TREATED PARTS PER SRM 51 -10-3. INSTALLED SPLICE USING SRM 51-30-5. 2 L 7 2 4F RT A6WE 2001080800038 20010808 00038 WP 2001 8 8 ZW0A0103508 1 20010607 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9615W 53562 DURING CHECK-C MAINT IN AFT CARGO COMPT FOUND CORROSION ON LT TRACK, STA 1250 TO 1287. REPLACED TRACK FROM FACTORY SPLI CE, STA 1216 TO AFT END PER SPM 6-70-01, SRM 51-30-2, AND SPM 6-30-07. 2 L 7 2 4F RT A6WE 2001080800039 20010808 00039 WP 2001 8 8 ZW0A0103509 1 20010607 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9615W 53562 DURING CHECK-C MAINT IN AFT CARGO COMPT FOUND CORROSION ON RT TIE DOWN TRACK, STA 1271 TO 1287 AND STA 1212 TO 1231. RE MOVED OLD TRACK AND REPLACED WITH NEW. INSTALLED FASTENERS PER SRM 51-30-2 AND 51-30-3. PRIMED AND PAINTED PER SRM 51- 10-3. 2 L 7 2 4F RT A6WE 2001080800040 20010808 00040 NM 2001 8 8 ZW0A0103601 1 20010615 A 3350 767 LIGHT BOEING 767 7673Q8 NM CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 635TW 28207 THE EGRESS LIGHTS WERE INOPERATIVE AT SEATS 1C, 2C, AND 24H. REPLACED LIGHT ASSEMBLY AT 1C, AND RESEATED THE CONNECTOR AT SEATS 2C AND 24H. CHECK-C 2-22-01 LAX. 2 L 7 2 4F RT A1NM 2001080800041 20010808 00041 NM 2001 8 8 ZW0A0103702 1 20010616 A 3397 WIRE BOEING 767 7673Y0 NM CABIN DAMAGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 640TW 25411 THE AFT FACING COACH WALL EGRESS LIGHT WAS INOPERATIVE. REPAIRED WIRES. CHECK-C 5-15-00. 2 L 7 2 4F RT A1NM 2001080800042 20010808 00042 WP 2001 8 8 ZW0A0103703 1 20010612 A 5312 BULKHEAD DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 929TW 48014 DURING CHECK-C MAINT IN AFT ACCY COMPT FOUND CRACKED WEB APPROX 2 INCHES ON STA 1485 CANTED BULKHEAD, APPROX 10 O'CLOCK POSITION. STOP DRILLED CRACK. REPAIRED WEB PER SRM 53-01, PAGE 9. 2 L 7 2 4F A6WE 2001080800043 20010808 00043 WP 2001 8 8 ZW0A0103704 1 20010612 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 929TW 48014 DURING CHECK-C MAINT FOUND CANTED FRAME AT STA 1463, 2 O'CLOCK POSITION, WAS CRACKED AT HI-LOKS. REPAIRED PER SRM 53-01 , FIG 2 SHEET 3. 2 L 7 2 4F A6WE 2001080800044 20010808 00044 WP 2001 8 8 ZW0A0103705 1 20010613 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 929TW 48014 DURING CHECK-C MAINT A GOUGE WAS FOUND IN THE BOTTOM FLANGE OF THE CABIN FLOORBEAM, STA 408, RBL 2 INCH. BLENDED GOUGE IN BOTTOM FLANGE OF CABIN FLOORBEAM, STA 408, RBL 2 IN. FABRICATED REPAIR ANGLE AND REPAIR STRAP AND PHENOLIC RUB STRIP PER SSRM 53-60-103, PAGE 201 AND 202, AND SRM 51-10-3. SEALED PARTS PER SRM 51-20-0. INSTALLED PARTS WITH D-RIVETS PE R SSRM 53-60-103, PAGE 201. 2 L 7 2 4F A6WE 2001080800045 20010808 00045 WP 2001 8 8 ZW0A0103706 1 20010613 A 5730 PANEL DOUG DC9 DC982 3022082 WP LT WING DENTED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 929TW 48014 DURING CHECK-C MAINT ON LT WING FOUND NUMEROUS DENTS ON TRAILING EDGE PANEL IN FRONT OF AILERON. INSTALLED NEW PANEL P/ N 5812737-501 PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-02 AND ARA 17765. 2 L 7 2 4F A6WE 2001080800046 20010808 00046 WP 2001 8 8 ZW0A0103707 1 20010613 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 929TW 48014 DURING CHECK-C MAINT IN FWD CABIN FOUND CORROSION ON MEMBRANE AT STA 197 TO 200, UNDER FWD EDGE OF NUMBER 1 CHAIR TRACK. INSTALLED REPAIR PER SRM 51-70-4 ON MEMBRANE AT STA 197 TO 200 UNDER NUMBER 1 CHAIR TRACK. TREATED PER SRM 51-10-03 P AGE 46 ITEM 3. INSTALLED REPAIR WITH RIVETS PER SRM 51-30-2. CUT OUT CORROSION ON TURN OVER CARD. 2 L 7 2 4F A6WE 2001080800047 20010808 00047 WP 2001 8 8 ZW0A0103708 1 20010614 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 929TW 48014 DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR SUPPORT AT STA 183, LBL 44. FLOOR SUPPORT REMOVED AND NEW SUPPORT F ABRICATED AND INSTALLED PER SPM 6-70-1 AND SRM 51-30-2. 2 L 7 2 4F A6WE 2001080800048 20010808 00048 WP 2001 8 8 ZW0A0103709 1 20010614 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 929TW 48014 DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT CRACKED AT STA 1098, BETWEEN LONGERON 26R AND 25R. FLOOR SUPPORT WAS REM OVED AND SENT TO SHOP TO BE WELDED PER SSRM 53-00-106, PAGE 201. REINSTALLED PER SRM 51-30-2, FIG 1. 2 L 7 2 4F A6WE 2001080800049 20010808 00049 WP 2001 8 8 ZW0A0103801 1 20010616 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9302B 49528 FOUND THE REPAIR ON THE FUSELAGE, BELOW AND AFT OF THE LEFT SIDE NUMBER 2 CABIN DOOR, HAD RIVET CENTERS NOT PROPERLY PUL LED AND RIVETS WERE HIGH, STA 1196 BETWEEN LONGERON 19L AND 20L. REMOVED CLASS III REPAIR AND INSTALLED CLASS I REPAIR PER ARA 17423. CHECK-C 10-16-00 STL. 2 L 7 2 4F RT A6WE 2001080800050 20010808 00050 WP 2001 8 8 ZW0A0103802 1 20010617 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9302B 49528 FOUND LONGERON 19L DAMAGED AT APPROX STA 1202. REPLACED LONGERON 19L AT STA 1202 PER SRM 53-02, FIG 18, AND ARA 17424. CHECK-C 10-16-00 STL. 2 L 7 2 4F RT A6WE 2001080800051 20010808 00051 WP 2001 8 8 ZW0A0103803 1 20010617 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 954U 49426 FOUND 2 HI-LOKS PULLED THRU FUSELAGE SKIN AT LONGERON 24L, AFT AND BELOW THE LAV SERVICE DOOR. CUT OUT DAMAGED LONGERON . SPLICED IN NEW SECTION PER SRM 53-02, FIG 18. CHECK-C 10-20-00 MCI. 2 L 7 2 4F A6WE 2001080800052 20010808 00052 WP 2001 8 8 ZW0A0103901 1 20010619 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 929TW 48014 DURING CHECK-C MAINT FOUND AT CANTED FRAME NUMBER 1497, 11 O'CLOCK POSITION A DOUBLE ROW OF HI-LOKS WERE CRACKED OUT. I NSTALLED WEB REPAIR PER SRM 51-70-11 AND SRM 53-01. INSTALLED FASTENERS PER SRM 51-30-2. STOP DRILLED CRACK. 2 L 7 2 4F A6WE 2001080800053 20010808 00053 WP 2001 8 8 ZW0A0104001 1 20010624 A 2170 17946081 COALESCER BAG DOUG DC9 DC983 3022083 WP A/C BAY CONTAMINATED A ZW0A K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CE 13 9412W 53187 CREW REPORTED SULFUR SMELL IN CABIN CAUSING PASSENGER DISCOMFORT. REPLACED BOTH WATER SEPARATOR BAGS. CHECK-C 9-7-00 S TL. 2 L 7 2 4F RT A6WE 2001080800054 20010808 00054 NM 2001 8 8 ZW0A0104002 1 20010621 A 3350 363674 LIGHT BOEING 757 757231 1384950 NM LAVATORY INOPERATIVE A ZW0A K NONE O OTHER CR CRUISE 1 CE 13 705TW 28479 THE EGRESS LIGHT WAS INOPERATIVE AT THE D-LAVATORY. REPLACED THE FLEX LAMP. CHECK-C 6-12-01 LAX. 2 L 7 2 4F RT A2NM 2001080800055 20010808 00055 WP 2001 8 8 ZW0A0104101 1 20010624 A 5350 TAIL CONE DOUG DC9 DC983 3022083 WP FUSELAGE DEPARTED A ZW0A A UNSCHED LANDING J WARNING INDICATION LD LANDING 1 CE 13 9615W 53562 DURING TAKEOFF ON A TEST FLIGHT OUT OF A MAJOR CHECK, THE TAIL CONE UNSAFE LIGHT ILLUMINATED. CREW ELECTED TO GO AROUND AND LAND. DURING LANDING THE TAIL CONE DEPARTED FROM THE AIRCRAFT AND LANDED ON THE RUNWAY, AND THE TAIL CONE EVACUATI ON SLIDE DEPLOYED. RIGGED THE TAIL CONE LATCHES PER MM 53-53-00. 2 L 7 2 4F RT A6WE 2001080800056 20010808 00056 WP 2001 8 8 ZW0A0104201 1 20010625 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 9627R 53597 THE EXIT LIGHT AT THE FWD EXIT DOOR HAD LENS FALLING OFF, THE COCKPIT CEILING EMERGENCY EXIT LIGHT WAS INOPERATIVE, THE EGRESS EXIT LIGHT AT THE AFT GALLEY DOOR WAS INOPERATIVE, THE EGRESS LIGHT ON THE FLOOR FROM SEAT 30D TO AFT LAV WAS INO PERATIVE, AND THE EGRESS LIGHT AT SEAT 14D WAS INOPERATIVE. REPLACED EXIT LIGHT P/N 0105610-001, REPLACED LAMP P/N AML -43, REPLACED LAMP P/N 2232, SECURED LOOSE CONNECTOR AT SEAT 30D, AND REPLACED LAMP P/N 7732 AT SEAT 14D. CHECK-C 12-17 -00 JFK. 2 L 7 2 4F RT A6WE 2001080800058 20010808 00058 NM 2001 8 8 ZW0A0104304 1 20010624 A 5320 SUPPORT BOEING 767 7673Y0 NM FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 640TW 25411 THE FWD CARGO COMPT BALL MAT J-BEAM SUPPORT AT DOOR SILL WAS CRACKED AT 8 PLACES, STA 500 THRU 600. REPLACED FWD CARGO BALL MAT J-BEAM ASSEMBLY, SERVICEABLE HARDWARE PER SRM 51-10-02, PAGE 12, AND IPC 76-25-52-05. CHECK-C 5-15-00. 2 L 7 2 4F RT A1NM 2001080800059 20010808 00059 NM 2001 8 8 ZW0A0104403 1 20010701 A 5532 PANEL BOEING 757 757231 1384950 NM VERTICAL STAB DENTED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 727TW 30340 ON THE RT SIDE OF THE VERTICAL STABILIZER, THE FWD ALUMINUM HONEYCOMB PANEL AT STA 92.250 HAD 24 GROUPS OF DENTS TOO CLO SE TOGETHER AND OUT OF LIMITS PER SRM 55-30-01. ALL DENTS DEPTH WITHIN LIMITS. APPROX 125 DENTS TOTAL. REPAIRED PER A RA 17707. NO CHECK-C. 2 L 7 2 4F RT A2NM 2001080800060 20010808 00060 WP 2001 8 8 ZW0A0104501 1 20010702 A 5313 LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 982PS 47251 LONGERON 6R CRACKED AT STATION 639 APROX .25 INCH. REPAIRED LONGERON PER SRM 53-02 FIG 18. LAST CHECK C 5-31-00 STL. 2 L 7 2 4F A6WE 2001080800061 20010808 00061 WP 2001 8 8 ZW0A0104502 1 20010702 A 5313 LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 982PS 47251 LONGERON 5R AT STATION 639 CRACKED APPROX .5 INCH. REMOVED DAMAGED LONGERON SECTION. REPLACED WITH DACO P/N 2777922-4 PER SRM 53-02 FIG 18. LAST CHECK C 5-31-00 STL. 2 L 7 2 4F A6WE 2001080800062 20010808 00062 WP 2001 8 8 ZW0A0104503 1 20010702 A 5313 LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 982PS 47251 LONGERON 5R AT STA 699 WAS CRACKED APPROX .5 INCH. REMOVED DAMAGED LONGERON 5R AND REPLACED WITH P/N 2777922-4 PER SRM 53-02 FIG 18. CHECK-C 5-31-00 STL. 2 L 7 2 4F A6WE 2001080800063 20010808 00063 WP 2001 8 8 ZW0A0104504 1 20010702 A 5313 LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 982PS 47251 LONGERON 5R AT STA 680 WAS CRACKED APPROX .25 INCH. REMOVED DAMAGED LONGERON 5R SECTION. REPLACED WITH P/N 2777922-4 P ER SRM 53-02 FIG 18. CHECK-C 5-31-00 STL. 2 L 7 2 4F A6WE 2001080800064 20010808 00064 NE 2001 8 8 ZW0A0104702 2 20010707 A 7321 430219 EEC BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE RT ENGINE FAILED A ZW0A A UNSCHED LANDING R X PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT CL CLIMB 1 CE 13 702TW 28162 4908 IN CLIMB THE RT ENG STALLED THEN SHUT ITSELF DOWN. FLIGHT RETURNED TO STL. REPLACED THE EEC STATOR, P/N 430219, AND TH E EEC ROTOR, P/N 46038. CHECK-C 6-12-01 LAX. 2 L 7 2 4F 4 F RT A2NM E17NE 2001080800065 20010808 00065 WP 2001 8 8 ZW0A0104703 1 20010702 A 5753 WEDGE DOUG DC9 DC982 3022082 WP T/E FLAP DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 929TW 48014 DURING CHECK-C MAINT THE RT WING T/E FLAP T/E WEDGE WAS DAMAGED ON THE BOTTOM SIDE APPROX 6 FT INBD OF THE OTBD END. RE MOVED AND REPLACED THE OTBD 13 .75 OF TRAILING EDGE WEDGE PER SRM 57-03 FIG 9 PAGE 12. 2 L 7 2 4F A6WE 2001080800066 20010808 00066 WP 2001 8 8 ZW0A0104704 1 20010702 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 922TW 48013 DURING CHECK-C MAINT FOUND CRACK IN LT MAIN GEAR WHEEL WELL FWD SHELF ATTACH ANGLE, FWD LOWER INBD CORNER OF WHEEL WELL. REMOVED AND REPLACED ANGLE WITH FABRICATED PART PER SPM 6-70-01, AND SRM 51-30-5. 2 L 7 2 4F A6WE 2001080800068 20010808 00068 NM 2001 8 8 ZW0A0104801 1 20010708 A 3350 767 LIGHT BOEING 767 767200 1385120 NM EXTERIOR INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 635TW 28207 R/S EMERGENCY EXIT LIGHT INOP FWD OF AFT CARGO DOOR. NORMAL WEAR, RELAMPED. LAST CHECK C 6/8/01 JFK. 2 L 7 2 4F RT A1NM 2001080800069 20010808 00069 NM 2001 8 8 0102762710 1 20010709 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 820EA 22557 DURING "M" CHECK FOUND CORROSION ON UPPER CHORD OF FLOORBEAM. REPAIRED PER EA 27-184389. 2 L 7 3 4F A3WE 2001080800070 20010808 00070 NM 2001 8 8 0102772710 1 20010711 A 5744 HINGE FITTING BOEING 727 727225 1384077 NM CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 820EA 22557 During "M" check found corrosion on LH inboard aileron hinge fitting. Repaired per EA 27-184387. 2 L 7 3 4F A3WE 2001080800071 20010808 00071 NM 2001 8 8 0102786730 1 20010711 A 5711 SPAR BOEING 747 7472J9F 1384806 NM CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 630US 21668 During "L" check found corrosion on upper surface of RH wing inboard trailing edge midflap aft spar. Repaired per EA 67- 184306. 2 L 7 4 4F RT A20WE 2001080800072 20010808 00072 NM 2001 8 8 ZW0A0104802 1 20010708 A 3350 1317 LIGHT BOEING 767 767200 1385120 NM CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 635TW 28207 EMERGENCY AISLE LIGHT OVERHEAD INOP ROW 45L. RELAMPED MFG P/N 1317. 2 L 7 2 4F RT A1NM 2001080800073 20010808 00073 NM 2001 8 8 ZW0A0104803 1 20010708 A 3397 WIRE BOEING 767 767200 1385120 NM CABIN LOOSE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 635TW 28207 EGRESS LIGHTS INOP ROW 42L TO ROW 45L. SECURED WIRING AT EGRESS LAMP AT ROW 42L. NO PARTS CHANGED. 2 L 7 2 4F RT A1NM 2001080800074 20010808 00074 NM 2001 8 8 ZW0A0104804 1 20010710 A 3397 WIRE BOEING 767 767200 1385120 NM CABIN LOOSE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 635TW 28207 EGRESS LIGHTS INOP AT ROW 1L TO 18L. SECURED WIRING AT EGRESS LAMP 18L, NO PARTS CHANGED. 2 L 7 2 4F RT A1NM 2001080800075 20010808 00075 WP 2001 8 8 ZW0A0104806 1 20010708 A 5313 LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 988Z 47134 CRACK IN LONGERON AT STATION 617 FRAME .5 INCH LONG. REPAIRED LONGERON IAW DAC REWORK DRAWING SR09530128 AND SRM 53-02. 2 L 7 2 4F A6WE 2001080800076 20010808 00076 NM 2001 8 8 ZW0A0104901 1 20010708 A 3350 8100022002 LIGHT BOEING 767 7673Q8 NM GALLEY INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 636TW 30301 THE AFT LEFT GALLEY EGRESS LIGHT STRIP WAS INOPERATIVE. REPLACED THE LIGHT STRIP. CHECK-C 1-7-01 LAX. 2 L 7 2 4F RT A1NM 2001080800077 20010808 00077 WP 2001 8 8 ZW0A0104902 1 20010708 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE PUNCTURED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 922TW 48013 DURING CHECK-C MAINT FOUND PUNCTURE IN FLOOR MEMBRANE AT STA 196, LBL 55. INSTALLED DOUBLER REPAIR PER SRM 53-01, FIG 2 . 2 L 7 2 4F A6WE 2001080800078 20010808 00078 WP 2001 8 8 ZW0A0104903 1 20010708 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 922TW 48013 DURING CHECK-C MAINT THE CABIN FLOOR SUPPORT AT STA 160 TO 200, LBL 55, WAS CORRODED. REMOVED CORRODED PART AND FABRICA TED NEW SUPPORT AND INSTALLED PER SPM 6-70-01 AND SRM 51-30-5. 2 L 7 2 4F A6WE 2001080800079 20010808 00079 WP 2001 8 8 ZW0A0104904 1 20010708 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 922TW 48013 DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT FITTINGS AT RBL 55, STA 202, 217, AND 208. REMOVED AND REPLACED F ITTINGS PER SPM 6-70-01 AND SRM 51-30-05. 2 L 7 2 4F A6WE 2001080800082 20010808 00082 WP 2001 8 8 ZW0A0104905 1 20010709 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 923TW 49379 DURING CHECK-C MAINT FOUND CHAIR TRACK CORROSION AT STA 1030 TO 1211 LBL 22 INCHES, STA 1079 TO 1136 LBL 22 INCHES, STA 1136 AND LBL 22 INCHES, AND HOLES DRILLED IN BOTTOM OF TRACK AT LBL 22 INCHES STA 1136 TO 1170. REPLACED TRACK FROM STA 1030 TO 1211 PER SRM 53-05, LBL 22 INCHES. 2 L 7 2 4F A6WE 2001080800085 20010808 00085 NE 2001 8 8 ZW0A0105001 2 20010712 A 7200 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D217C 52053 NE LEFT MALFUNCTIONED A ZW0A E A ENGINE SHUTDOWN UNSCHED LANDING E B VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 13 9413T 53188 1209 A LOUD NOISE WAS HEARD FROM THE LT ENGINE AND THE AIRCRAFT SHUTTERED. SMOKE APPEARED IN THE COCKPIT. ENGINE WAS SHUT D OWN AND AIRCRAFT LANDED AT SZL. EMERGENCY EVACUATION WAS ACCOMPLISHED. CHECK-C 8-10-00 STL. 2 L 7 2 4F 4 F RT A6WE E9NE 2001080800088 20010808 00088 WP 2001 8 8 ZW0A0105002 1 20010712 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 922TW 48013 DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 183, RBL 44. MADE AND INSTALLED NEW FLOOR SUPPORT PER SPM 6-70-01 AND SRM 51-30-2. 2 L 7 2 4F A6WE 2001080800090 20010808 00090 WP 2001 8 8 ZW0A0105003 1 20010712 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 922TW 48013 DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 190 TO 194, RBL 44. MADE AND INSTALLED FLOOR SUPPORT PER S PM 6-70-01 AND SRM 51-30-2. 2 L 7 2 4F A6WE 2001080800092 20010808 00092 WP 2001 8 8 ZW0A0105004 1 20010712 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 922TW 48013 DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 185 TO 190, RBL 44. MADE AND INSTALLED FLOOR SUPPORT PER S PM 6-70-01 AND SRM 51-30-2. 2 L 7 2 4F A6WE 2001080800094 20010808 00094 WP 2001 8 8 ZW0A0105005 1 20010711 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 922TW 48013 DURING CHECK-C MAINT FOUND CORROSION AT RBL 15, STA 200. MADE AND INSTALLED FLOOR SUPPORT PER SPM 6-70-01 AND SRM 51-30 -2. 2 L 7 2 4F A6WE 2001080800097 20010808 00097 WP 2001 8 8 ZW0A0105006 1 20010712 A 5320 FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 922TW 48013 DURING CHECK-C MAINT IN THE NOSE GEAR WHEEL WELL FOUND CRACK IN FITTING AT STA 69, LBL 16, THE INBD FITTING AT PRESSURE PANEL. REMOVED CRACKED FITTING AND INSTALLED NEW FITTING, P/N 4912385-501N, PER SPM 6-70-01, SECTION B.2. 2 L 7 2 4F A6WE 2001080800099 20010808 00099 WP 2001 8 8 ZW0A0105007 1 20010712 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 923TW 49379 DURING CHECK-C MAINT FOUND CANTED FORMER CRACKED, LOWER END OF STA 1485, OTBD OF STAIR CUTOUT. STOP DRILLED CRACK AND I NSTALLED DOUBLER PER 53-01 FIG 2. INSTALLED FASTENERS PER SRM 51-30-5 AND 51-30-2. 2 L 7 2 4F A6WE 2001080800101 20010808 00101 WP 2001 8 8 ZW0A0105008 1 20010712 A 5730 SKIN DOUG DC9 DC982 3022082 WP LT WING PUNCTURED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 923TW 49379 DURING CHECK-C MAINT FOUND PUNCTURE HOLE IN LT WING L/E APPROX 8 INCHES FWD OF FRONT SPAR, 13 INCHES AFT AND OTBD OF NUM BER 1 SLAT ANTI-ICE TUBE ON LT WING L/E. REMOVED ALL DAMAGE AND INSTALLED TYPICAL REPAIR PER SRM 57-06A, PAGE 11, AND S RM 51-01 PARAGRAPH 3, ITEM B1-62 PAGE 2. 2 L 7 2 4F A6WE 2001080800103 20010808 00103 WP 2001 8 8 ZW0A0105009 1 20010711 A 5320 GUSSET DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 923TW 49379 DURING CHECK-C MAINT FOUND FACTORY GUSSET ON TOP OF FORMER SPLICE CORRODED, STA 1174 AND LBL 30. REPLACED CORRODED STRA P WITH NEW ONE PER DRAWING 9936073. 2 L 7 2 4F A6WE 2001080800104 20010808 00104 WP 2001 8 8 ZW0A0105010 1 20010712 A 5320 GUSSET DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 923TW 49379 DURING CHECK-C MAINT FOUND GUSSET ON TOP OF FORMER CORRODED, STA 1155 AND LBL 28. REPLACED CORRODED STRAP WITH NEW ONE PER DRAWING 9936067. 2 L 7 2 4F A6WE 2001080800105 20010808 00105 WP 2001 8 8 ZW0A0105011 1 20010712 A 5320 GUSSET DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 923TW 49379 DURING CHECK-C MAINT FOUND GUSSET ON FORMER RING FACTORY SPLICE WAS CORRODED, STA 1193. REPLACED PART PER SRM 51-01 AND DRAWING 9936073. 2 L 7 2 4F A6WE 2001120300096 20011203 00096 NE 2001 12 3 ZW0A0105101 2 20010715 A 7250 798209 BLADE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE LT ENGINE FRACTURED A ZW0A E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 CE 13 956U 49701 3218 AT 3500 FEET IN CLIMB HEARD ONE COMPRESSOR STALL FROM THE LT ENGINE THEN ENGINE PARAMETERS ALL DECLINED. COMPLETED ENGI NE SHUT DOWN PROCEDURE AND RETURNED TO SJC. FOUND TURBINE DAMAGE AND REPLACED THE ENGINE. FOUND ONE NINTH STAGE COMPRE SSOR BLADE HAD FRACTURED IN DOVETAIL ROOT SECTION. TWO OTHER NINTH STAGE BLADES FRACTURED IN AIRFOIL SECTION AND ALSO H AD CRACK INDICATIONS IN ROOT SECTION. 2 L 7 2 4F 4 F A6WE E9NE 2001080800108 20010808 00108 WP 2001 8 8 ZW0A0105102 1 20010716 A 2910 HYDRAULIC LINE DOUG DC9 DC931 3022065 WP HYDRAULIC SYS LEAKING A ZW0A O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 CE 13 986Z 47589 AFTER GEAR EXTENSION HYDRAULIC QUANTITY INDICATED ZERO. AT THE GATE INDICATED 4 QUARTS. FOUND FAILED FLARE ON THE HYD LINE AT THE LT MLG BUNGEE. REFLARED THE LINE. CHECK-C 11-13-00 STL. 2 L 7 2 4F A6WE 2001083001036 20010830 01036 WP 2001 8 30 IXXA0100049O 1 20010731 A 2731 3654950522 CONTROL CABLE DOUG DC8 DC871F 302199D WP ELEVATOR TAB BROKEN A IXXA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SW 11 799AL 69159 1876 45922 DURING TAXI AT ANU, BINDING OF THE ELEVATOR WAS EXPERIENCED WHILE THE FLIGHT CREW WAS PERFORMING THE FLIGHT CONTROL CHEC K. THE AIRCRAFT RETURNED TO THE BLOCKS. MAINTENANCE INSPECTED THE AIRCRAFT FLIGHT CONTROLS WHICH REVEALED A DEFECTIVE RIGHT ELEVATOR CONTROL TAB CABLE. MAINTENANCE REPLACED THE CONTROL CABLE IN ACCORDANCE WITH THE DOUGLAS MAINTENANCE MAN UAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2001080800110 20010808 00110 WP 2001 8 8 ZW0A0105103 1 20010710 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 922TW 48013 DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR SUPPORT, STA 1250, BETWEEN NUMBER 1 AND 2 CHAIR TRACKS, LBL 22 TO 44 . FABRICATED AND INSTALLED NEW FLOOR SUPPORT FITTING FROM 7075-T6 EXTRUSION PER SPM 6-70-01. 2 L 7 2 4F A6WE 2001080800112 20010808 00112 WP 2001 8 8 ZW0A0105104 1 20010711 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 922TW 48013 DURING CHECK-C MAINT FOUND CORROSION IN CABIN AT RBL 11, STA 209. REMOVED SUPPORT AND MADE NEW PART PER DRAWING PL99365 35 ITEM 57, AND INSTALLED WITH HI-LOKS PER SRM 51-30-0. 2 L 7 2 4F A6WE 2001080800114 20010808 00114 WP 2001 8 8 ZW0A0105105 1 20010711 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 922TW 48013 DURING CHECK-C MAINT FOUND CORROSION AT STA 198 AND RBL 44, AND AT STA 200 RBL 11. INSTALLED FLOOR SUPPORT AT BOTH LOCA TIONS PER SPM 6-70-01 AND RIVETS PER SRM 51-30-2. 2 L 7 2 4F A6WE 2001080800116 20010808 00116 WP 2001 8 8 ZW0A0105106 1 20010711 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 922TW 48013 DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT IN CABIN AT STA 180, RBL 8 TO 44. INSTALLED NEW SUPPORT PER SPM 6 -70-01. INSTALLED FASTENERS PER SRM 51-30-2. 2 L 7 2 4F A6WE 2001080800118 20010808 00118 WP 2001 8 8 ZW0A0105107 1 20010711 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 922TW 48013 DURING CHECK-C MAINT FOUND CORROSION ON NUMBER 2 FLOOR TRACK AT RBL 22, STA 1080 TO 1250. REPLACED TRACK PER SPM 6-70-0 1 AND SRM 53-05, FIG 4. PRIMED PER SRM 51-10-3. REMOVED CORROSION PER SPM 6-80-01. 2 L 7 2 4F A6WE 2001080800120 20010808 00120 WP 2001 8 8 ZW0A0105108 1 20010712 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 922TW 48013 DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 200, LBL 6 TO RBL 6. REMOVED OLD SUPPORT AND MADE NEW SUPP ORT FROM STOCK. PAINTED AND ALODINED PER SRM 51-10-3 ITEM 30 AND 23. INSTALLED WITH RIVETS PER SRM 51-30-2. SEALED SU PPORT PER SRM 51-20-0. 2 L 7 2 4F A6WE 2001080800122 20010808 00122 WP 2001 8 8 ZW0A0105109 1 20010712 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 922TW 48013 DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 160 TO 200, LBL 7. REMOVED OLD FLOOR SUPPORT AND MADE NEW. 2 L 7 2 4F A6WE 2001080800125 20010808 00125 WP 2001 8 8 ZW0A0105110 1 20010712 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 922TW 48013 DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 194 TO 202, LBL 15. REMOVED OLD SUPPORT AND MADE NEW SUPPO RT. 2 L 7 2 4F A6WE 2001080800127 20010808 00127 WP 2001 8 8 ZW0A0105111 1 20010712 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 922TW 48013 DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 170 TO 200, RBL 7. FOUND CORRODED BEYOND LIMITS AND FABRIC ATED NEW FLOOR SUPPORT. 2 L 7 2 4F A6WE 2001080800129 20010808 00129 WP 2001 8 8 ZW0A0105112 1 20010710 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 923TW 49379 DURING CHECK-C MAINT FOUND AFT ACCY COMPT CANTED FORMER CRACKED AT LOWER END AT STA 1474, OTBD OF STAIR CUTOUT ON RT SID E. REPAIRED PER SRM 53-01 PAGE 10. MATERIAL PER SRM 53-14-4 PAGE 14. 2 L 7 2 4F A6WE 2001080800130 20010808 00130 WP 2001 8 8 ZW0A0105113 1 20010710 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 923TW 49379 DURING CHECK-C MAINT IN AFT CARGO COMPT FOUND CORROSION ON ANGLE IN AFT LOWER CORNER OF DOOR JAM. REMOVED AND REPLACED CORNER ANGLE AND INSTALLED HI-LOKS PER SRM 51-30-5. SEALED PER SRM 51-20-0. 2 L 7 2 4F A6WE 2001080800133 20010808 00133 NM 2001 8 8 USAA010788 1 20010710 A 5300 FRAME BOEING 737 7374B7 1384702 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 31193 24811 CLT - FOUND FRAME CRACKED .125 INCH, BS 787 BETWEEN STRINGERS 8 AND 9R. REPAIR DOUBLER INSTALLED PER TYPICAL REPAIR 53- 10-14. (M) 2 L 7 2 4F RT A16WE 2001080800134 20010808 00134 NM 2001 8 8 USAA010787 1 20010710 A 5300 FRAME BOEING 737 7374B7 1384702 NM BS 727D CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 31193 24811 CLT - FOUND FRAME CRACKED .125 INCH, BS 727D, BETWEEN STRINGERS 8 AND 9R. REPAIR DOUBLER INSTALLED PER TYPICAL REPAIR 5 3-10-14. (M) 2 L 7 2 4F RT A16WE 2001080800135 20010808 00135 NM 2001 8 8 USAA010786 1 20010710 A 5310 FRAME BOEING 737 7374B7 1384702 NM BS 727B CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 31193 24811 CLT - FOUND FRAME CRACKED .125 INCH, BS 727B, BETWEEN STRINGERS 8 AND 9R. REPAIR DOUBLER INSTALLED PER TYPICAL REPAIR 5 3-10-14. (M) 2 L 7 2 4F RT A16WE 2001080800136 20010808 00136 NM 2001 8 8 USAA010785 1 20010710 A 5310 FRAME BOEING 737 7374B7 1384702 NM BS 500D CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 31193 24811 CLT - FOUND FRAME CRACKED .125 INCH, BS 500D, BETWEEN STRINGER 8 AND 9R. REPAIR DOUBLER INSTALLED PER TYPICAL REPAIR 53 -10-14. (M) 2 L 7 2 4F RT A16WE 2001080800137 20010808 00137 NM 2001 8 8 USAA010784 1 20010710 A 5300 FRAME BOEING 737 7374B7 1384702 NM BS 400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 31193 24811 CLT - FOUND FRAME CRACKED .125 INCH, BS 400, BETWEEN STRINGER 8 AND 9L. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53- 10-14. (M) 2 L 7 2 4F RT A16WE 2001080800138 20010808 00138 NM 2001 8 8 USAA010783 1 20010710 A 5310 FRAME BOEING 737 7374B7 1384702 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 31193 24811 CLT - FOUND FRAME CRACKED .25 INCH, BS 380, BETWEEN STRINGERS 8 AND 9L. REPAIR DOUBLER INSTALLED PER TYPICAL REPAIR 53- 10-14. (M) 2 L 7 2 4F RT A16WE 2001080800139 20010808 00139 NM 2001 8 8 USAA010779 1 20010702 A 5300 WEB BOEING 737 737401 1384701 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 408US 37673 23878 CLT - FOUND WEB CRACKED .5 INCH, BS 178 WL 207 AT RIGHT SIDE CHORD. DAMAGE REMOVED, INSTALLED DOUBLER PER EO 5300V157. (M) 2 L 7 2 4F RT A16WE 2001080800140 20010808 00140 NM 2001 8 8 USAA010839 1 20010716 A 5300 FRAME BOEING 737 7373B7 1384580 NM BS 360 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND FRAME STIFFENER CRACKED .5 INCH, RESULTING IN MISSING MATERIAL, BS 360, LEFT SIDE OF A/C AT FRAME, WL 215. INSTALLED STRAP AND FILLER PER EA 85025. (M) 2 L 7 2 4F RT A16WE 2001080800141 20010808 00141 NM 2001 8 8 USAA010838 1 20010716 A 5300 WEB BOEING 737 7373B7 1384580 NM BS 947.8 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND WEB CRACKED INTERIOR CABIN 1 INCH, BS 947.8, AFT ENTRY DOOR, UPPER HINGE CUTOUT. INSTALLED RE-INFORCING STR AP PER EA 69847. (M) 2 L 7 2 4F RT A16WE 2001080800142 20010808 00142 NM 2001 8 8 USAA010837 1 20010716 A 5300 BEAM BOEING 737 7373B7 1384580 NM BS 707-711 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND BEAM CRACKED .5 INCH, BS 707 TO 711, BBL 0, LOWER ROW OF FASTENERS. INSTALLED REPAIR DOUBLER PER EA 69679 A ND SB 737-57-1210 FIG 5. (M) 2 L 7 2 4F RT A16WE 2001080800143 20010808 00143 NM 2001 8 8 USAA010835 1 20010716 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 727D CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND FUSELAGE SKIN CRACKED .8 INCH, BETWEEN BS 727D AND E, BL 0. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER SR M 51-10-2, 51-20-01, 51-40-00 AND 53-00-01 FIG 202. (M) 2 L 7 2 4F RT A16WE 2001080800144 20010808 00144 NM 2001 8 8 USAA010834 1 20010716 A 5300 FRAME BOEING 737 7373B7 1384580 NM BS 954 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND FRAME CRACKED 3 INCHES, BS 954, BETWEEN STRINGER 9 AND 10R, INNER RADIUS. DAMAGE REMOVED, INSTALLED NEW PAR TS PER SRM 51-40-03, 51-40-02 AND BAC DRAWING NR J65-46561. (M) 2 L 7 2 4F RT A16WE 2001080800145 20010808 00145 NM 2001 8 8 USAA010832 1 20010716 A 5300 DOOR FRAME BOEING 737 7373B7 1384580 NM BS 294.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND DOOR FRAME CRACKED TWO PLACES 1 INCH EACH, BS 294.5, RBL 55, STRINGER 17R. INSTALLED REPAIR DOUBLER PER SRM 51-70-11. (M) 2 L 7 2 4F RT A16WE 2001080800146 20010808 00146 NM 2001 8 8 USAA010831 1 20010716 A 5300 FRAME BOEING 737 7373B7 1384580 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND FRAME CRACKED 1 INCH, BS 616, RIGHT CREASE BEAM, INNER CHORD ANGLE. DAMAGE REMOVED, INSTALLED REPAIR ANGLE AND FILLER PER TYPICAL REPAIR 53-62-01. (M) 2 L 7 2 4F RT A16WE 2001080800147 20010808 00147 NM 2001 8 8 USAA010830 1 20010716 A 5300 SKIN BOEING 737 7373B7 1384580 NM BS 727C CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND FUSELAGE SKIN CRACKED .25 INCH, BS 727C, STRINER 24L. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER SRM 53-0 0-01, FIG 225. (M) 2 L 7 2 4F RT A16WE 2001080800148 20010808 00148 NM 2001 8 8 USAA010829 1 20010716 A 5300 FRAME BOEING 737 7373B7 1384580 NM BS 847 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND FRAME CRACKED APPROX .25 INCH, BS 847, BETWEEN STRINGER 8 AND 9R. INSTALLED REPAIR DOUBLER PER TYPICAL REPA IR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001080800149 20010808 00149 NM 2001 8 8 USAA010828 1 20010716 A 5300 FRAME BOEING 737 7373B7 1384580 NM BS 847 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND FRAME CRACKED APPROXIMATELY .25 INCH, BS 847, BETWEEN STRINGER 8 AND 9L. INSTALLED REPAIR DOUBLER PER TYPIC AL REPAIR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001080800150 20010808 00150 NM 2001 8 8 USAA010827 1 20010624 A 5315 FLOORBEAM BOEING 737 7374B7 138449C NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 30946 24781 PIT - FOUND 6 INCHES OF CORROSION AT FLOORBEAM 328 LT OUTBOARD OF LBL 45. CORROSION LEVEL 1. SPLICED IN SECTION OF UPP ER CHORD, TREATED, PRIMED, SEALED PER SRM 53-10-51, 51-40-02. (M) 2 L 7 2 4F RT A16WE 2001080800151 20010808 00151 NM 2001 8 8 USAA010826 1 20010716 A 5300 FRAME BOEING 737 7373B7 1384580 NM BS 887 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND FRAME CRACKED .25 INCH, BS 887 BETWEEN STRINGER 8 AND 9L. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-10 -14. (M) 2 L 7 2 4F RT A16WE 2001080800152 20010808 00152 NM 2001 8 8 USAA010824 1 20010716 A 5300 TIE CLIP BOEING 737 7373B7 1384580 NM BS 663 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND TIE CLIP CRACKED TWO PLACES .25 INCH, BS 663, STRINGER 10R. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001080800153 20010808 00153 NM 2001 8 8 USAA010823 1 20010624 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 30946 24781 PIT - FOUND FLOORBEAM CORRODED 2 INCHES, CLIP NUT ON FLOORBEAM 328 LEFT. CORROSION LEVEL 1. SPLICED IN SECTION OF UPPE R CHORD, TREATED, PRIMED, SEALED PER SRM 53-10-51, 51-40-02. (M) 2 L 7 2 4F RT A16WE 2001080800154 20010808 00154 NM 2001 8 8 USAA010822 1 20010519 A 5315 FLOORBEAM BOEING 737 7374B7 138449C NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 24781 PIT - FOUND FLOORBEAM CORRODED 2 INCHES BY 4 INCHES, FLOORBEAM 360 LEFT. CORROSION LEVEL 1. REMOVED AREAS OF LIGHT COR ROSION, TREATED, PRIMED PER SRM 53-10-15. (M) 2 L 7 2 4F RT A16WE 2001080800155 20010808 00155 NM 2001 8 8 USAA010814 1 20010716 A 5300 FRAME BOEING 737 7373B7 1384580 NM BS 807 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND FRAME CRACKED .25 INCH, BS 807, BETWEEN STRINGER 8 AND 9R. INSTALLED DOUBLER PER TYPICAL REPAIR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001080800156 20010808 00156 NM 2001 8 8 USAA010813 1 20010624 A 5310 ANGLE BOEING 737 7374B7 1384702 NM CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 30946 24781 PIT - FOUND ANGLE CORRODED 1 INCH BY 30 INCH AREA, BETWEEN SERVICE DOOR FRAME THRESHOLD SUPPORT. REPLACED CORRODED SUPP ORT ANGLE PER SRM 53-10-15AS. (M) 2 L 7 2 4F RT A16WE 2001080800157 20010808 00157 NM 2001 8 8 USAA010810 1 20010619 A 5330 SKIN BOEING 737 737301 1384611 NM BS 23 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 41925 23510 PIT - FOUND SKIN CRACKED 2.75 INCH, STRINGER 23 BS 727D-E. DOUBLER REPAIR PER SRM 53-30-00 PAGE 201, FIG 201. (M) 2 L 7 2 4F RT A16WE 2001080800158 20010808 00158 NM 2001 8 8 USAA010807 1 20010612 A 5300 SKIN BOEING 737 737301 1384611 NM A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 43853 23232 PIT - FOUND SKIN OIL CANNING 12 INCH BY 12 INCH, 178 BULKHEAD BETWEEN WL 195-207 BL 17L AND BL 17R. ACCOMPLISHED EXTERN AL DOUBLER, REMOVED DAMAGE PER SRM 53-10-08 FIG 211. (M) 2 L 7 2 4F RT A16WE 2001080800159 20010808 00159 NM 2001 8 8 USAA010806 1 20010613 A 5300 SKIN PANEL BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 43853 23232 PIT - FOUND BULKHEAD SKIN PANEL CRACKED 1.5 INCH, STATION 178 BULKHEAD WL 201 AND 204 LBL 5.7. CUT OUT, INSTALLED DOUBL ER PER SRM 53-10-08 FIG 211. (M) 2 L 7 2 4F RT A16WE 2001080800160 20010808 00160 NM 2001 8 8 USAA010805 1 20010612 A 5300 SKIN PANEL BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 43853 23232 PIT - FOUND BULKHEAD SKIN PANEL CRACKED 2 INCHES STOP DRILLED, STATION 178 RBL 5.7 WL 201. CUT OUT, INSTALLED DOUBLER P ER SRM 53-10-08 FIG 211. (M) 2 L 7 2 4F RT A16WE 2001080800161 20010808 00161 NM 2001 8 8 USAA010804 1 20010615 A 5310 FRAME BOEING 737 7373B7 1384580 NM FS 663.75 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 524AU 43790 23859 PIT - FOUND FRAME CRACKED 2 INCHES, FS 663.75 AT ST-1C1-26-3R-2R AND 3L. REPAIRED PER EA 71500 AND SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 2001080800162 20010808 00162 NM 2001 8 8 USAA010801 1 20010703 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 727E CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 520AU 41843 23706 PIT - FOUND SKIN CRACKED 1.125 INCH, RIGHT SIDE STATION 727E STRINGER 24 RIGHT. CUT OUT DAMAGE, INSTALLED EXT DOUBLER P ER SRM 53-00-01 FIG 201. (M) 2 L 7 2 4F RT A16WE 2001080800163 20010808 00163 NM 2001 8 8 USAA010791 1 20010710 A 5300 FRAME BOEING 737 7374B7 1384702 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 31193 24811 CLT - FOUND FRAME CRACKED .125 INCH, BS 867, BETWEEN STRINGERS 8 AND 9R. REPAIR DOUBLER INSTALLED PER TYPICAL REPAIR 53 -10-14. (M) 2 L 7 2 4F RT A16WE 2001080800164 20010808 00164 NM 2001 8 8 USAA010790 1 20010710 A 5300 FRAME BOEING 737 7374B7 1384702 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 31193 24811 CLT - FOUND FRAME CRACKED .25 INCH, BS 867, BETWEEN STRINGERS 8 AND 9L. REPAIR DOUBLER INSTALLED PER TYPICAL REPAIR 53- 10-14. (M) 2 L 7 2 4F RT A16WE 2001080800165 20010808 00165 NM 2001 8 8 USAA010789 1 20010710 A 5310 FRAME BOEING 737 7374B7 1384702 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 31193 24811 CLT - FOUND FRAME CRACKED .125 INCH, BS 827, BETWEEN STRINGERS 8 AND 9R. REPAIR DOUBLER INSTALLED PER TYPICAL REPAIR 53 -10-14. (M) 2 L 7 2 4F RT A16WE 2001080800167 20010808 00167 2001 8 8 UPS01836166 4 20010622 A 2565 SLIDE DOUG DC8 DC873F 302199F WP DOOR OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:N/A DEPARTURE-ESCAPE SLIDE GIRT BAR WOULD NOT LOCK IN PLACE. *S/D* REPACKED SLIDE, OPS CHECKS GOOD REF M217781. 2 L 7 4 4F RT 4A25 2001080800168 20010808 00168 WP 2001 8 8 ZW0A0105201 1 20010710 A 5320 THRESHOLD DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 923TW 49379 DURING CHECK-C MAINT FOUND IN THE AFT CARGO COMPT THE BOTTOM OF THE DOOR THRESHOLD WAS CORRODED FROM STA 1162 TO 1205. REMOVED SPACER. FABRICATED NEW SPACER PER SRM 53-05, FIG 63 SHEET 8. INSTALLED HI-LOKS PER SRM 51-30-5 AND INSTALLED S EALER PER SRM 51-20-0. 2 L 7 2 4F A6WE 2001080800169 20010808 00169 WP 2001 8 8 ZW0A0105202 1 20010710 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 923TW 49379 DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND CORROSION ON THE ANGLE IN THE FWD LOWER CORNER OF THE DOOR JAM. REMOV ED AND REPLACED CORNER ANGLE AND INSTALLED HI-LOKS PER SRM 51-30-5. SEALED PER SRM 51-20-0. 2 L 7 2 4F A6WE 2001080800171 20010808 00171 WP 2001 8 8 ZW0A0105203 1 20010711 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 923TW 49379 DURING CHECK C-FOUND MEMBRANE AT STATION 1231 ON LEFT SIDE OF CABIN DAMAGED BY ARCING POWER LEADS. REPAIRED PER SRM 53- 01 PAGE 14 AND SRM 51-30-01. MCI 2 L 7 2 4F A6WE 2001080800174 20010808 00174 WP 2001 8 8 ZW0A0105204 1 20010711 A 5320 991186021N FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 923TW 49379 DURING CHECK-C, A FORMER FOOT WAS FOUND CRACKED IN THE AFT ACCY COMPARTMENT AT STATION 1451 BETWEEN NR 1 AND NR 3 LEFT L ONGERON. REPLACED FORMER FOOT WITH P/N 9911860-21N AND -17 TIE CLIP PER DRAWING 9911860, INSTALLED RIVETS PER SRM 51-30 -2. MCI 2 L 7 2 4F A6WE 2001121700106 20011217 00106 NE 2001 12 17 ZW0A0105302 2 20010717 A 7250 5002201031 BLADE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE ENGINE FRACTURED A ZW0A B A EMER. DESCENT UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 CE 13 9406W 53126 3208 DURING CLIMB OUT NUMBER ONE ENGINE FAILED. FLIGHT RETURNED TO MIA FOUND TURBINE DAMAGE. CHANGED NUMBER ONE ENGINE. A FIRST STAGE TURBINE BLADE FRACTURED DUE TO OVER STRESS, DAMAGING ALL PARTS AFT OF THE FIRST STAGE TURBINE. 2 L 7 2 4F 4 F RT A6WE E9NE 2001080800176 20010808 00176 WP 2001 8 8 ZW0A0105303 1 20010713 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 922TW 48013 DURING CHECK-C MAINT FOUND CABIN FLOORBEAM FITTING CRACKED AT STA 1308, LBL 35. REMOVED AND REPLACED FITTING PER SRM 51 -30-5. 2 L 7 2 4F A6WE 2001080800177 20010808 00177 WP 2001 8 8 ZW0A0105304 1 20010713 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 922TW 48013 DURING CHECK-C MAINT FOUND HOLE IN MEMBRANE UNDER CABIN FLOOR, STA 1090 AND LBL 45. INSTALLED DOUBLER REPAIR PER SRM 53 -01, FIG 2. 2 L 7 2 4F A6WE 2001080800180 20010808 00180 WP 2001 8 8 ZW0A0105305 1 20010713 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 922TW 48013 DURING CHECK-C MAINT ON LT SIDE OF CABIN FOUND CRACKS AT STA 160, LONGERON 3L AND 4L. REPAIRED PER SRM 53-02 FIG 18. 2 L 7 2 4F A6WE 2001080800182 20010808 00182 WP 2001 8 8 ZW0A0105306 1 20010716 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 923TW 49379 DURING CHECK-C MAINT FOUND CORROSION IN FLOOR SUPPORT FASTENER HOLES, STA 160 TO 200, RBL 45. REPLACED FLOOR SUPPORT WI TH P/N S2929169 EXTRUSION. 2 L 7 2 4F A6WE 2001080800183 20010808 00183 NM 2001 8 8 ZW0A0105403 1 20010717 A 2761 SUPPORT BOEING 717 717200 1383700 NM SPOILER CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 406TW 55073 DURING MAINTENANCE THE OUTBOARD SPOILER HOLD DOWN ACTUATOR SUPPORT WAS FOUND CRACKED .75 INCH LONG. REPLACED SUPPORT PE R EMLR 72096 LAST CHECK C (NO CHECK C). 2 L 7 2 4F TR A6WE 2001080800184 20010808 00184 WP 2001 8 8 ZW0A0105404 1 20010717 A 5711 SPAR CAP DOUG DC9 DC982 3022082 WP RT WING CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 923TW 49379 DURING CHECK-C MAINT FOUND EYEBROW CRACK IN RT WING UPPER SPAR CAP AT OTBD FLAP HINGE INBD GUIDE PIN. INSTALLED DOUGLAS REPAIR DOUBLER PER DRAWING JO60272-501 AND PER ARA 17773. 2 L 7 2 4F A6WE 2001080800185 20010808 00185 NM 2001 8 8 ZW0A0105405 1 20010716 A 5330 SKIN BOEING 757 7572Q8 1384972 NM FUSELAGE DENTED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 706TW 28165 DURING CHECK-C MAINT FOUND STATION 650 STRINGER 17L, 4 FOOT FWD OF THE LEFT SIDE NUMBER 2 CABIN DOOR, WITH 2 EACH SMOOTH DENTS. THE FWD DENT WAS .75 IN BY .75 IN BY .1875 IN DEEP. AFT DENT WAS 1 IN BY 1 IN BY .0625 IN DEEP. CUT OUT DAMAG ED SKIN AND INSTALLED DOUBLER PER SRM 53-00-01. 2 L 7 2 4F RT A2NM 2001080800186 20010808 00186 WP 2001 8 8 ZW0A0105406 1 20010717 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 922TW 48013 DURING CHECK-C MAINT THE INTERCOSTAL BETWEEN FLOOR SUPPORTS AT STA 782, ZERO BL WAS CRACKED AND BROKEN. INSTALLED DOUBL ER ON INTERCOSTAL. USED 4-5, 5-6, AND 5-7 AD RIVETS PER SRM 53-10-104, PAGE 201 FIG 201. 2 L 7 2 4F A6WE 2001080800187 20010808 00187 WP 2001 8 8 ZW0A0105407 1 20010717 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 922TW 48013 DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR TRACK, LBL 44, STA 1136 TO 1174, AND 1174 TO 1231. CLEANED MINOR CO RROSION STA 1200 TO 1231 PER SPM 6-80-01. TREATED PER SRM 51-10-3. REMOVED TRACK AT STA 1080 TO 1200 AND REPLACED WITH NEW TRACK SECTION. 2 L 7 2 4F A6WE 2001080800188 20010808 00188 WP 2001 8 8 ZW0A0105408 1 20010717 A 5330 DOUBLER DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 922TW 48013 DURING CHECK-C MAINT FOUND FINGER DOUBLER CORRODED ON OTBD SIDE OF LONGERON 26L, STA 788, MID CARGO COMPT. REPLACED FIN GER DOUBLER PER SPM 6-80-01 AND FASTENERS PER SRM 51-30-0. 2 L 7 2 4F A6WE 2001080800189 20010808 00189 WP 2001 8 8 ZW0A0105409 1 20010717 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 922TW 48013 DURING CHECK-C MAINT IN THE AFT CABIN FOUND TOP OF FLOORBEAM STA 1322 WAS CORRODED AT LBL 15 TO SIDEWALL. REMOVED CORRO SION MECHANICALLY PER SPM 6-80-1. INSTALLED REPAIR PER SRM 53-05, FIG 20A. 2 L 7 2 4F A6WE 2001080800190 20010808 00190 WP 2001 8 8 ZW0A0105410 1 20010718 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 923TW 49379 DURING CHECK-C MAINT FOUND CORROSION ON MEMBRANE AT STA 147 TO 167, LBL 5 TO LBL 10. CUT OUT TWO AREAS OF CORROSION. R EMOVED REMAINING CORROSION PER SPM 6-80-01. MADE REPAIR DOUBLERS PER SRM 53-01. INSTALLED WITH SEALER PER SRM 51-30-2. 2 L 7 2 4F A6WE 2001080800191 20010808 00191 WP 2001 8 8 ZW0A0105411 1 20010713 A 5753 WEDGE DOUG DC9 DC983 3022083 WP T/E FLAP DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 THE RT WING INBD FLAP WAS DAMAGED. REPLACED THE DAMAGED INBD T/E WEDGE PER CMM 37-50-01. CHECK-C 6-19-01 MCI. 2 L 7 2 4F RT A6WE 2001080800192 20010808 00192 NM 2001 8 8 ZW0A0105502 1 20010720 A 3350 LEAD BOEING 767 7673Y0 NM CABIN DAMAGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 638TW 26205 THE ORANGE OVERLAY EGRESS LIGHTS WERE INOPERATIVE AT THE LT SIDE AND RT SIDE MOST FWD CABIN DOORS. REPAIRED FLOOR LEADS AT CARPET SEAMS. CHECK-C 5-12-01 LAX. 2 L 7 2 4F RT A1NM 2001080800193 20010808 00193 NM 2001 8 8 ZW0A0105503 1 20010721 A 3397 WIRE BOEING 767 7673Y0 NM CABIN BROKEN A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 640TW 25411 THE EGRESS LIGHTS ON LT SIDE OF CABIN, ROWS 17 TO 22, WERE INOPERATIVE. REPAIRED BROKEN WIRE AT ROW 18. CHECK-C 5-15-0 0. 2 L 7 2 4F RT A1NM 2001080800194 20010808 00194 WP 2001 8 8 ZW0A0105504 1 20010720 A 5280 DOOR DOUG DC9 DC983 3022083 WP RT MLG CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9616G 53563 DURING CHECK-C MAINT THE AFT OTBD CORNER OF THE RT GEAR DOOR WAS CRACKED. REPAIRED PER SRM 52-05, FIG 28. INSTALLED MS 2044AD6 RIVETS. 2 L 7 2 4F RT A6WE 2001080800195 20010808 00195 WP 2001 8 8 ZW0A0105505 1 20010720 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 922TW 48013 DURING CHECK-C MAINT LONGERON 20R HAD TWO CRACKS, ABOVE FLAP BUS CABLE PULLEYS, STA 1003. REPAIRED LONGERON 20R PER ARA 17777. 2 L 7 2 4F A6WE 2001080800196 20010808 00196 WP 2001 8 8 ZW0A0105506 1 20010720 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 922TW 48013 DURING CHECK-C MAINT FOUND CRACK IN LONGERON 20L ABOVE FLAP BUS CABLE PULLEYS, STA 1003. REPAIRED LONGERON 20L PER ARA 17776. 2 L 7 2 4F A6WE 2001080800197 20010808 00197 NM 2001 8 8 ZW0A0105602 1 20010717 A 2761 SUPPORT BOEING 717 717200 1383700 NM SPOILER CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 406TW 55073 THE RT WING OTBD SPOILER HOLD DOWN ACTUATOR SUPPORT WAS CRACKED .75 INCH LONG. REPLACED THE SUPPORT PER EMLR 72096. NO CHECK-C. 2 L 7 2 4F TR A6WE 2001080800198 20010808 00198 WP 2001 8 8 ZW0A0105703 1 20010719 A 5320 FITTING DOUG DC9 DC982 3022082 WP FUSELAGE BROKEN A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 922TW 48013 DURING CHECK-C MAINT FOUND BROKEN FITTING, P/N 5956034-552, AT STA 788 BETWEEN LONGERON 27R AND 28R. REPLACED BROKEN FI TTING. TREATED AND PRIMED AND INSTALLED PER SRM 51-10-3. INSTALLED PER SRM 51-30-5 AND SRM 51-30-1. 2 L 7 2 4F A6WE 2001080800199 20010808 00199 WP 2001 8 8 ZW0A0105704 1 20010718 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 923TW 49379 DURING CHECK-C MAINT IN THE FWD CABIN FOUND FLOOR SUPPORT WITH CORROSION AT STA 168, RBL 10. INSTALLED NEW FLOOR SUPPOR T WITH HLT 436 HI-LOKS, A SUBSTITUTION FOR MID FASTENER PER SRM 51-60-0. 2 L 7 2 4F A6WE 2001082100158 20010821 00158 CE 2001 8 21 C2XA01CL191 1 20010806 A 6123 5038912147 SWITCH BEECH 1900 1900D 1154162 CE RT ENGINE FAULTY A C2XA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION AP APPROACH 1 SW 27 47542 9786 UE198 CLE FLIGHT3007 THE CREW REPORTED THAT ON FINAL APPROACH, THOUGHT A PROPELLER HAD AUTOFEATHERED. THE AIRCRAFT LANDED WI THOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE AUTOFEATHER LOW PRESSURE SWITCH. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT A24CE 2001080800200 20010808 00200 WP 2001 8 8 ZW0A0105705 1 20010722 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 923TW 49379 DURING CHECK-C MAINT IN THE AFT CARGO COMPT FROM STA 1041 TO 1145, AT LBL 16, THE LT TIE DOWN TRACK WAS CORRODED IN NUME ROUS LOCATIONS ALONG THE TRACK. 2 L 7 2 4F A6WE 2001080800201 20010808 00201 WP 2001 8 8 ZW0A0105706 1 20010723 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 923TW 49379 DURING CHECK-C MAINT IN THE AFT ACCY COMPT THE LONGERON END WAS CRACKED AT STA 1418, LONGERON 2L. REPLACED CRACKED LONG ERON PER SRM 53-14-4, FIG 2. REPAIRED WITH SPLICE SECTION PER SRM 53-02, FIG 7. SHIMMED REPAIR PART AS NECESSARY. 2 L 7 2 4F A6WE 2001080800202 20010808 00202 WP 2001 8 8 ZW0A0105707 1 20010723 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 923TW 49379 DURING CHECK-C MAINT AT STA 1145 TO 1221, LBL 16 IN, THE LT TIE DOWN TRACK WAS CORRODED IN NUMEROUS LOCATIONS ALONG TRAC K. INSTALLED TIE DOWN TRACK STA 1150 TO 1320. HI-LOK ATTACHED PER SRM 51-30-4, AND RIVETS PER SRM 51-30-02. 2 L 7 2 4F A6WE 2001080800204 20010808 00204 WP 2001 8 8 ZW0A0105708 1 20010718 A 5753 SKIN DOUG DC9 DC983 3022083 WP T/E FLAP CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 971TW 53621 DURING CHECK-C MAINT FOUND .625 INCH DENT IN THE LOWER SURFACE OF THE RT FLAP, 20 INCHES UP FROM THE AFT EDGE IN LINE WI TH INBD TIRE. CRACK WAS DETECTED WITH EDDY CURRENT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 57-01, FIG 3. 2 L 7 2 4F RT A6WE 2001080800207 20010808 00207 NM 2001 8 8 ZW0A0105802 1 20010725 A 3350 LIGHT BOEING 757 757231 1384950 NM CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 708TW 28480 THE EMERGENCY LIGHT AT THE LEFT SIDE NUMBER 2 AND RT SIDE NUMBER 3 CABIN DOORS, AND THE EMERGENCY FLASHLIGHT AT THE LEFT SIDE NUMBER 2 DOOR, WERE INOPERATIVE. REPLACED LAMP P/N 767 FOR BOTH EMERGENCY LIGHTS, AND REPLACED FLASHLIGHT BATTERI ES P/N 179208. CHECK-C 3-29-00 LAX. 2 L 7 2 4F RT A2NM 2001080800208 20010808 00208 WP 2001 8 8 ZW0A0105803 1 20010722 A 3350 408822101 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 9677W 53627 THE COCKPIT OVERHEAD EMERGENCY LIGHTS DID NOT ILLUMINATE DURING TEST. REPLACED THE POWER SUPPLY BATTERIES. CHECK-C 11- 9-00 JFK. 2 L 7 2 4F RT A6WE 2001080800210 20010808 00210 NM 2001 8 8 ZW0A0105804 1 20010726 A 3397 WIRE BOEING 767 7673Q8 1385142 NM CABIN DISCONNECTED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 636TW 30301 THE EGRESS LIGHTS WERE INTERMITTENT AT CABIN ROW 1C THRU 3C. RECONNECTED WIRING. CHECK-C 1-8-01 LAX. 2 L 7 2 4F RT A1NM 2001080800213 20010808 00213 WP 2001 8 8 ZW0A0105805 1 20010724 A 5730 DOUBLER DOUG DC9 DC983 3022083 WP LT WING CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9616G 53563 DURING CHECK-C MAINT ON LT WING L/E FOUND CRACK AT DOUBLER, INSIDE LOWER L/E OF WING, 3.5 INCHES INBD OF NUMBER 6 TRACK. REPAIRED CRACKED DOUBLER BY INSTALLING REPAIR DOUBLER PER SSRM 57-40-103, FIG 201. 2 L 7 2 4F RT A6WE 2001080800215 20010808 00215 NM 2001 8 8 ZW0A0106001 1 20010729 A 3350 80741 LIGHT BOEING 767 7673Y0 NM CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 640TW 25411 DURING PREFLIGHT EGRESS LIGHTING AT SEATS 17AC TO 22AC WERE INOP DUE TO WEAR. REPLACED EGRESS LIGHTING STRIP AT SEAT 17 AC WITH P/N 8074-1. 2 L 7 2 4F RT A1NM 2001080800216 20010808 00216 NM 2001 8 8 ZW0A0106007 1 20010729 A 3350 LIGHT BOEING 767 76733AER 1385230 NM CABIN DISCONNECTED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 637TW 25403 DURING MAINTENANCE THE EGRESS LIGHTS AT SEAT 17C WERE INOP DUE TO WEAR. RECONNECTED LAMP ASSY PER MM 33-51-00. LAST CH ECK C 01/27/01 LAX. 2 L 7 2 4F RT A1NM 2001080800217 20010808 00217 NM 2001 8 8 ZW0A0106008 1 20010729 A 3350 CONNECTOR BOEING 767 76733AER 1385230 NM CABIN DIRTY A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 637TW 25403 DURING MAINTENANCE THE EGRESS LIGHTS A R1 DOOR WERE INOP DUE TO WEAR. CLEANED FLOOR FLEX CONNECTORS PER MM 33-51-00. 2 L 7 2 4F RT A1NM 2001080800230 20010808 00230 NM 2001 8 8 USAA010776 1 20010702 A 5312 BULKHEAD BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 408US 37673 23878 CLT - FOUND BULKHEAD WEB CRACKED NUMEROUS AREAS .5 INCH TO 1.5 INCH, BS 178, WL 186 TO 234, LBL 12 TO RBL 6.5. DAMAGE R EMOVED, INSTALLED REPAIR DOUBLER AND FILLERS PER EO 5300V153 AND EA 69888. (M) 2 L 7 2 4F RT A16WE 2001080800233 20010808 00233 NM 2001 8 8 USAA010777 1 20010702 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 408US 37673 23878 CLT - FOUND SIDE CHORDS CRACKED TWO PLACES 1.5 INCH EACH, BS 178 WL 207 LEFT AND RIGHT. DAMAGE REMOVED, SPLICED IN NEW CHORD SECTION PER EO 5300V157. (M) 2 L 7 2 4F RT A16WE 2001080800235 20010808 00235 NM 2001 8 8 USAA010778 1 20010702 A 5312 PRESSURE PANEL BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 408US 37673 23878 CLT - FOUND FLOORWEB CRACKED .5 INCH, BS 178 WL 207 LEFT SIDE. REMOVED AND REPLACED WEB PER EO 5300V157. (M) 2 L 7 2 4F RT A16WE 2001080800239 20010808 00239 NM 2001 8 8 USAA010782 1 20010705 A 5512 SKIN BOEING 737 7374B7 1384702 NM HORIZ STAB DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 31193 24811 CLT - FOUND STAB SKIN WITH PREVIOUSLY INSTALLED DOUBLER, 57 INCHES LONG WIDTH VARIES FROM 4 INCHES TO 5 INCHES, LEFT HOR IZONTAL STABILIZER, SS 111.10 TO 166.30 AT REAR SPAR. DAMAGE REMOVED, INSTALLED DOUBLER PER EA'S 85064 AND 69880. (M) 2 L 7 2 4F RT A16WE 2001080800241 20010808 00241 NM 2001 8 8 USAA010798 1 20010612 A 3221 TRUNNION BOEING 737 737301 1384611 NM NLG CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 43853 23232 PIT - FOUND FITTING HAS CORROSION PITTING, DEEPEST .021 INCH, NOSE GEAR SHOCK STRUT LEFT TRUNNION FITTING. REAMED BORE, INSTALLED SLEEVE PER EA 71444. (M) 2 L 7 2 4F RT A16WE 2001080800246 20010808 00246 NM 2001 8 8 USAA010809 1 20010716 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND SIDE CHORD CRACKED TWO PLACES, 1.75 INCHES ON LEFT SIDE, 1 INCH ON RIGHT SIDE, BS 178, WL 207, LEFT AND RIGH T SIDE. DAMAGE REMOVED, SPLICED IN NEW REPAIR SECTION PER EO 5300V157. (M) 2 L 7 2 4F RT A16WE 2001080800247 20010808 00247 NM 2001 8 8 USAA010812 1 20010716 A 5312 PRESSURE PANEL BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND FLOORWEB CRACKED TWO PLACES .5 INCH, BS 178 WL 207, LEFT AND RIGHT SIDE. REMOVED AND REPLACED FLOORWEB PER EO 5300V157 AND SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 2001080800250 20010808 00250 NM 2001 8 8 USAA010819 1 20010624 A 5320 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 30946 24781 PIT - FOUND Z-ANGLE CORRODED 2 INCH BY 56 INCH AREA, BETWEEN BEAM 282 AND 338. CORROSION LEVEL 1, TASK NR C53-107-02. REPLACED Z-ANGLE, TREATED, PRIMED PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2001080800252 20010808 00252 NM 2001 8 8 USAA010820 1 20010624 A 5320 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 30946 24781 PIT - FOUND SUPPORT ANGLE CORRODED 2 INCH BY 4 INCH AREA, FLOOR SUPPORT LBL 10 BETWEEN 328 AND 344. CORROSION LEVEL 1, TASK NR C53-107-02. REPLACED FLOOR SUPPORT PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2001080800255 20010808 00255 NM 2001 8 8 USAA010821 1 20010624 A 5320 FLOOR SUPPORT BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 30946 24781 PIT - FOUND SUPPORT ANGLE CORRODED 2 INCH BY 4 INCH AREA, FLOOR SUPPORT LBL 10 BETWEEN 312 AND 328. CORROSION LEVEL 1, TASK C53-107-02. REPLACED FLOOR SUPPORT PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2001080800258 20010808 00258 NM 2001 8 8 USAA010833 1 20010716 A 5320 69374024 ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND SUPPORT ANGLE CRACKED 5 INCHES, BS 290 TO 294.5, RBL 55, INBOARD CREASE BEAM ANGLE. REMOVED AND REPLACED SU PPORT ANGLE PER SRM 51-01-02. (M) 2 L 7 2 4F RT A16WE 2001080800260 20010808 00260 NM 2001 8 8 USAA010836 1 20010716 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND FRAME CRACKED ON VHF ANTENNA .25 INCH AND 2.5 INCH, BS 727D, LBL 1.5 AND RBL 1.5. REMOVED DAMAGE, INSTALLED REPAIR DOUBLER PER SRM 51-70-11. (M) 2 L 7 2 4F RT A16WE 2001080800262 20010808 00262 NM 2001 8 8 USAA010840 1 20010716 A 5330 BEAR STRAP BOEING 737 7373B7 1384580 NM FUSELAGE GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46295 22950 CLT - FOUND SKIN/BARE STRAP GOUGED AND DEFORMATION, 1 INCH BY 2.9 INCHES, BS 440, LOWER FORWARD CORNER OF CARGO DOOR CUT OUT. INSTALLED DOUBLER AND TRIPLER PER EA 69856. (M) 2 L 7 2 4F RT A16WE 2001080800264 20010808 00264 NM 2001 8 8 USAA010841 1 20010716 A 5410 FITTING BOEING 737 7373B7 1384580 NM NR 2 PYLON GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 46925 22950 CLT - FOUND BULKHEAD FITTING .75 INCH GOUGE, NACELLE STATION 254.525, NR 2 PYLON. BLENDOUT AND ROTO-PEEN. (M) 2 L 7 2 4F RT A16WE 2001080800300 20010808 00300 NM 2001 8 8 USAASB01135 1 20010511 A 3244 TIRE BOEING 737 7374B7 1384702 NM RT MLG SEPARATED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 445US 24863 MCO - FLT 722 - ON CLIMB-OUT FROM MCO,CAPT REPORTED THE FWD MAIN ENTRY DOOR WAS LEAKING AND THE AIRCRAFT WOULD NOT PRESS URIZE NORMALLY. FLIGHT RETURNED TO FIELD AND LANDED 5,000 LBS OVERWEIGHT. NO EMERGENCY WAS DECLARED. MAINTENANCE REPORT ED THAT THE RT OUTBOARD MLG TIRE WAS BLOWN AND POSSIBLY SOME FLAP DAMAGE. MX INSPECTED THE FWD MAIN ENTRY DOOR SEAL AND THE OPERATION AND PROPER LOCKING OF THE DOOR. PRESSURIZED AIRCRAFT TO 5 PSI. NO LEAKAGE DETECTED. CABIN PRESSURE WAS S TEADY. REMOVED AND REPLACED NR 4 MLG WHEEL ASSY DUE TO TREAD SEPARATION WHICH WAS DETERMINED TO HAVE OCCURRED ON T/O BY LOCATION OF CARCASS ON RUNWAY. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2001080800306 20010808 00306 NM 2001 8 8 USAASB01160 1 20010604 A 2750 FLAP BOEING 737 7372B7 1384560 NM LT WING JAMMED A USAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 EA 19 269AU 22881 EWR - FLT 2671 - DURING DESCENT, AIRCRAFT ENCOUNTERED TRAILING EDGE FLAP ASYMMETRY. CAPTAIN REQUESTED TO LAND AT EWR IN STEAD OF LGA DUE TO THE HIGHER LANDING SPEEDS FOR THIS TYPE OF FAILURE. AFTER LANDING AT EWR, WITHOUT INCIDENT, CAPTAIN REPORTED THAT THE LT JACKSCREW HAD FORCED THE LT FLAP INTO THE LEFT AILERON AND JAMMED IT. AN EMERGENCY WAS DECLARED. S/D MX MADE TEMPORARY SHEET METAL REPAIRS AND REPLACED THE OUTBOARD LT FLAP BALL SCREW AND NUT ASSY, JACKSCREW TRANSMISS ION, LT OUTBOARD FLAP ASSEMBLY, LT AILERON TAB, LT FLAP OUTBOARD SEQUENCE CARRIAGE, LT FLAP INBOARD AND OUTBOARD FLAP TO GGLES, AND THE LT FLAP OUTBOARD CANOE FAIRING. THE AIRCRAFT WAS THEN FERRIED FOR PERMANENT SHEET METAL REPAIRS. (M) 2 L 7 2 4F A16WE 2001080800308 20010808 00308 WP 2001 8 8 ABXA010430 1 20010725 A 5300 2912347501 FRAME DOUG DC9 DC931 3022065 WP FWD CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 CRACK IN FRAME F.S. 389, LONGERON 29 RIGHT, UPPER SURFACE, JUST INBOARD OF DOOR CUT OUT WEB. REPAIRED FRAME AT STATION 3 89, LONGERON 29 RIGHT IAW DC-9 SRM 53. 2 L 7 2 4F A6WE 2001080800309 20010808 00309 WP 2001 8 8 ABXA010431 1 20010725 A 5311 59114481 FRAME DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 LEVEL TWO CORROSION ON FRAME AT FS 256, LONGERON 30. REMOVED 2 EACH FASTENERS TO GAIN ACCESS. BLENDED AREA IAW DC-9 SRM 51-10-3. CHECKED AREA FOR THICKNESS. FOUND TO BE OUT OF LIMITS. REPAIRED AREA IAW DC-9 SRM 53-03, FIGURE 2A, PAGE 4E. IN STALLED 2 EACH FASTENERS IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2001080800310 20010808 00310 WP 2001 8 8 ABXA010432 1 20010725 A 5300 991075521 WEB DOUG DC9 DC931 3022065 WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 RIGHT CUSP WEB WAS CRACKED 7 INCHES AFT OF STATION 917 FLOORBEAM. REPAIRED CRACK IAW DC-9 SRM 53-01, FIGURE 2. 2 L 7 2 4F A6WE 2001080800311 20010808 00311 WP 2001 8 8 ABXA010434 1 20010725 A 5300 S49258487075T665 TRACK DOUG DC9 DC931 3022065 WP CABIN CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 LEVEL 1 CORROSION AND EXFOLIATION ON CENTER TRACK AT F.S. 325. REPLACED SEAT TRACK SECTION IAW DC-9 SSRM K05406. 2 L 7 2 4F A6WE 2001080800312 20010808 00312 NM 2001 8 8 USAASB01170 1 20010610 A 3244 6558256275 TIRE BOEING 737 737301 1384611 NM RT MLG SEPARATED A USAA O OTHER J WARNING INDICATION TO TAKEOFF 1 EA 19 340US 198 23237 PIT - FLT 1185 - CAPT REPORTED ON T/O FROM PIT, THE NR 3 MLG TIRE TREAD HAD SEPARATED AND CAUSED A RT MLG UNSAFE LIGHT T O ILLUMINATE. CREW RECYCLED GEAR AND RECEIVED THREE GREEN LIGHTS. UPON PREPARATION FOR LANDING, CREW RECEIVED THE SAME RT MLG LANDING GEAR UNSAFE LIGHT AGAIN DURING GEAR EXTENSION. CREW RECYCLED GEAR AND RECEIVED THREE GREEN LIGHTS. A F LYBY WAS REQUESTED TO ENSURE GEAR WAS DOWN AND THE FIRST OFFICER CHECKED THE ALIGNMENT STRIPES TO ENSURE GEAR WAS LOCKED . (M) 2 L 7 2 4F RT A16WE 2001080800313 20010808 00313 NM 2001 8 8 USAASB01171 1 20010611 A 3350 15AT17 SWITCH BOEING 737 737401 1384701 NM COCKPIT DEFECTIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 MIA - DURING PREFLIGHT, PILOT REPORTED THAT THE EMERGENCY EXIT LIGHTS ILLUMINATED WHILE NORMAL ELECTRICAL AC/DC POWER TO ALL BUSSES WAS AVAILABLE. LIGHTS WOULD NOT EXTINGUISH. MAINTENANCE REMOVED AND REPLACED A DEFECTIVE EMERGENCY LIGHT A RMING SWITCH ON THE COCKPIT P5 OVERHEAD PANEL. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001080800314 20010808 00314 NE 2001 8 8 2001F00163 2 20010421 A 7240 RB211535C COMBUSTION LINER BOEING 757 757200 1384950 NM RROYCE RB211 RB211535* NE ENGINE CRACKED Z K NONE O OTHER IN INSP/MAINT 1 CE 07 GBIKJ 29957 22181 SB RB21172C728 DATED NOV.29/99, ON INSPECTING THE EXTERIOR OF THE AREA OF CONCERN, THE FOLLOWING ITEMS WERE FOUND: 1) T HERE ARE 3 CRACKS AROUND THE CIRCUMFERENCE OF THE COMBUSTION CASE TOTALING APPROXIMATELY 15 INCHES. 2) THIS CONDITION IS BEYOND THE LIMITS SPECIFIED ON THE SB. 2 L 7 2 4F 4 F RT A2NM E12EU 2001080800343 20010808 00343 EU 2001 8 8 BAQ2001F00000 1 20010711 A 6520 4639003007 GEARBOX BOLKMS 117 BK117B1 5626012 EU TAIL ROTOR CRACKED E BAQA K NONE O OTHER IN INSP/MAINT 1 EA 03 955ME 3059 7243 WHILE DURING PRE-FLIGHT (DAILY) OF AIRCRAFT, FOUND TR 90 PERCENT GEAR BOX LOOSE. REMOVED GEAR BOX AND FOUND STUDS LOOSE ON GEAR BOX. INSPECTED FITTING AND ALSO FOUND CRACKED. 1 G 7 2 3U H13EU 2001080800344 20010808 00344 CE 2001 8 8 CJP2001F00000 1 20010622 A 2910 2407004408 HYDRAULIC LINE LEAR 25 25D 5170514 CE GE CJ610 CJ610* 30006 NE HYDRAULIC SYS CHAFED A CJPA K NONE O OTHER IN INSP/MAINT 1 NM 03 600GM 2939 290 TUBE ASSEMBLY WAS FOUND CHAFED DURING A SCHEDULED INSPECTION OF HYDRAULIC PLUMBING IN TAILCONE. THE TUBE ASSEMBLY WAS R EPLACED WITH A NEW TUBE ASSEMBLY. AIRCRAFT HAS HAD AFFECTED TUBE ASSEMBLY PREVIOUSLY REPLACED BY COMPLIANCE WITH SB 25- 336. TUBE ASSEMBLYS IN TAILCONE CAN BE DIFFICULT TO INSPECT UNLESS VIEWED PROPERLY. A THROUGH VISUAL INSPECTION AT SCH EDULED INSPECTIONS AND WHEN THREE-WAY VALVES ARE REMOVED IS RECOMMENDED. 2 L 7 2 4J 4 J A10CE 1E16 2001080800345 20010808 00345 SO 2001 8 8 COZ2001F00000 1 20010618 A 5210 BRACKET GULSTM G1159 G1159A 3970109 SO CABIN DOOR BROKEN A COZA K NONE O OTHER IN INSP/MAINT 1 WP 27 684AT 8355 339 MAIN CABIN DOOR ACTUATOR UPPER ATTACH BRACKET BROKEN IN HALF. BREAKAGE CAUSED HORIZONTAL ATTACHMENT FLANGE TO SHEAR UPW ARDS. 2 L 7 2 4F A12EA 2001080800346 20010808 00346 WP 2001 8 8 EHA2001F00000 2 20010306 A 7200 TPE33110R511 ENGINE CASA C212 C212CC 2410204 EU GARRTT TPE331 TPE331* 01514 WP NR 2 FAILED E EHAA A UNSCHED LANDING J Y WARNING INDICATION ENGINE STOPPAGE DE DESCENT 1 AL 03 422CA 7077 3976 238 P37098C ON DOWNWIND LEG AT 2000 FEET, AGL PILOT NOTICED NR 2 ENGINE TQ. GAUGE READ 0. COPILOT VISUAL OF NR 2 PROP REPORTED AS F EATHERED. E HANDLE ACTIVATED AND UNEVENTFUL LANDING MADE. SUBSEQUENT ENGINE START FAILED. NEXT START ATTEMPT FOLLOWI NG DAY FOR TROUBLESHOOTING NORMAL, AFTER 2 MINUTE GROUND RUN NR 2 ENGINE CHIP DETECTOR ILLUMINATED AND ENGINE WAS SHUT D OWN. OIL FILTER INSPECTION REVEALED NO METAL CONTENT. ENGINE REMOVE FROM SERVICE AND SENT TO REPAIR FACILITY FOR INSPE CTION/ REPAIR. 2 H 7 2 4T 3 T A43EU E2WE 2001080800348 20010808 00348 CE 2001 8 8 GUU2001F00019 1 20010706 A 5520 1016200111 HINGE BRACKET BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA ELEVATOR CORRODED E GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 150GA 23980 UC150 DURING SCHEDULED MAINTENANCE, LEFT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANUL AR CORROSION. REMOVED AND REPLACED LEFT ELEVATOR OUTBOARD HINGE BRACKET. NOTE: TIME SINCE LAST INSPECTION: 180.1 2 L 7 2 4T 4 T RT A24CE E4EA 2001080800349 20010808 00349 CE 2001 8 8 GUU2001F00020 1 20010628 A 3233 1143800415 ACTUATOR BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA RT MLG FAILED E GUUA O OTHER J WARNING INDICATION CL CLIMB 1 SO 17 151GA UC171 AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. TROUBLESHOT SYSTEM, FOUND RIGHT MAIN LANDING GEAR ACTUATOR BYPASSING INT ERNALLY. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR ACTUATOR. PERFORMED LANDING GEAR EXTENSION AND RETRACTION. OPER ATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A24CE E4EA 2001080800351 20010808 00351 CE 2001 8 8 R2J2001F00002 1 20010720 A 2133 1035982 PIN BEECH 90 E90 1152914 CE PWA PT6 PT6A27 52043 EA OUTFLOW VALVE BROKEN A R2JR K NONE O OTHER IN INSP/MAINT 1 EA 21 1205S 5000 LW319 WHILE TROUBLE SHOOTING LOW CABIN DIFFERENTIAL PRESSURE FOUND THAT THE OUTFLOW VALVE CONE WOULD HANG OPEN AT TIMES. VALV E REMOVED AND INSPECTED. FOUND THAT GUIDE PIN THAT GUIDES CONE TO KEEP IT FROM COCKING WAS BROKEN. OVERHAULED EXCHANGE VALVE WAS INSTALLED. CAUSE OF PIN FAILURE, UNKNOWN. 1 L 7 2 3T 4 T 3A20 E4EA 2001080800358 20010808 00358 SO 2001 8 8 YAD2001F00004 2 20010608 A 7322 6297032 CONTROL VALVE CESSNA 207 207A 2073604 CE CONT O520 IO520F 17032 SO FUEL CONTROL DEFECTIVE A YADA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 AL 03 75941 1 20700656 AIRCRAFT RUN UP FOR TAKEOFF AND ENGINE BEGAN RUNNING VERY ROUGH. AIRCRAFT RETURNED TO RAMP. PILOT COMMENTED THAT MIXTU RE WAS NOT CORRECT AT IDLE OR AT POWER AND THAT THROTTLE CONTROL FELT SPRING LOADED. MAINTENANCE FOUND THROTTLE CONTROL VALVE, ON FUEL CONTROL, STIFF AND BUSHING MOVING. REMOVED AND REPLACED UNIT. 1 H 7 1 3O 3 O A16CE E5CE 2001080800359 20010808 00359 SO 2001 8 8 YAD2001F00005 2 20010608 A 8530 SA52000A20P CYLINDER CESSNA 207 207A 2073604 CE CONT O520 IO520F 17032 SO ENGINE DAMAGED A YADA A UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CL CLIMB 1 AL 03 75941 1353 20700656 247599R AIRCRAFT DEPARTED AIRPORT AND ENGINE BEGAN RUNNING VERY ROUGH. AIRCRAFT RETURNED TO THE AIRPORT (UNABLE TO MAINTAIN POW ER OR ALTITUDE). MAINTENANCE FOUND NR 4 CYLINDER HAD BROKEN AND BENT PUSHRODS. THE EXHAUST VALVE PUSHROD WAS FOUND BRO KEN FOR ABOUT 8 INCHES IN LENGTH. FURTHER INVESTIGATION REVEALED A BENT PUSHROD IN NR 2 CYLINDER. SUSPECT STUCK/ STICK ING VALVES CAUSED FAILURE. ALL CYLINDERS WERE INSTALLED FACTORY NEW AT ENGINE OVERHAUL. 1 H 7 1 3O 3 O A16CE E5CE 2001080800360 20010808 00360 EU 2001 8 8 ZYWA100153 1 20010108 A 5260 14860011 ACTUATOR AEROSP AS365 AS365N2 8680815 EU PAX DOOR FAILED A ZYWA K NONE O OTHER NR NOT REPORTED 1 GL 09 365WM 350 6429 STEP DOES NOT RETRACT OR EXTEND. REMOVED AND REPLACED STEP ACTUATOR. 1 G 7 2 3U RT H10EU 2001080800361 20010808 00361 2001 8 8 ZYWA100159 4 20010108 A 2211 41800491350 COMPUTER AEROSP AS365 AS365N2 8680815 EU TMECA ARRIEL ARRIEL1 60030 NE AUTOPILOT SYS FAULTY A ZYWA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 09 365WM 2941 6429 AIRCRAFT PORPOISES WITH PITCH LANE 2 ENGAGED IN BASIC AP MODE (INTERMITTENTLY). REMOVED AND REPLACED COMPUTER. 1 G 7 2 3U 3 U RT H10EU E19EU 2001080800379 20010808 00379 WP 2001 8 8 CALA0100742 1 20010805 A 5753 MOUNT DOUG DC9 DC982 3022082 WP R/W I/B FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND R/H WING I/B FLAP HINGE #2 CORRODED IN BOTTOM MOUNT HOLE. THE HOLE WAS REAMED AND TWO BUSHINGS WERE INS TALLED IAW EA 9-2750-2-A0914 AND ECRA 2750-01333. 2 L 7 2 4F A6WE 2001080800380 20010808 00380 WP 2001 8 8 CALA0100743 1 20010807 A 5280 PAN DOUG DC9 DC982 3022082 WP L/H MLG DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72821 49481 INSPECTION FOUND A 1" CRACK IN L/H MLG I/B DOOR PAN AT LEADING EDGE. THE DOOR PAN WAS REMOVED AND REPLACED IAW SRM 51-30 -2, 51-30-3, 51-30-8, AND 51-10-2. 2 L 7 2 4F A6WE 2001080800381 20010808 00381 NM 2001 8 8 S01732021 1 20010728 A 3241 215152 BRAKE ASSY BOEING 747 747400 NM PWA 4056 PW4056 NE # 5 MWT W SAJF O OTHER O OTHER LD LANDING 1 WP 03 28710 B18202 1.A/C ACHIEVING AT GATE,# 5 MWT ASSY CAUGHT FIRE REPORT GRD STAFF. NOTE:BRK TEMP 2, TIRE PRESSURE 200 PSI. 2.THE SMOKE & FLAME ON # 5 MWT WAS SUBSTANTIALLY OBSERVED,THE FLAME SUSTAINED A FEW SECONDS BEFORE APPLYING FIRE EXTINGQUISHER .C/A:1.TLB 0114368-2 RECORDED THAT # 5 MWT & BRK UNIT WERE REPLACED,SYSTEM WAS RESUMED NORMAL. 2.EON 744-32-634053-006 W AS ISSUED FOR A DETAILED BENCH CHECK,WHICH REVEALED THAT THE FUNCTION IS NORMAL. BUT SOME RESIDUE GREASE REMAINED ON THE PISTON HOUSING, HEAT SINK & PISTONS. THESE AREA SHOULD BE FREE OF GREASE. 3.AMM 12-21-01 SHOULD BE FOLLOWED WHICH PREVE NTS THE MLG BRK FIRE UNDER NORMAL BREAKING DUE TO EXCESSIVE GREASE & RESIDUAL CLEANING FLUIDS IN THESE AREA. 2 L 7 4 4F 4 F RT A20WE E24NE 2001080900001 20010809 00001 NE 2001 8 9 EVA004 2 20010807 A 7200 CF680C2D1F ENGINE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE STAGES 6 TO 8 BROKEN W QOCF O OTHER E VIBRATION/BUFFET CR CRUISE 1 WP 03 16418 2958 48778 1. A/C B-16408 :Captain report: In cruise found No.1 Engine Vibration 3.0 and EGT higher than other engine.2. On ground check found some metal chips in tail pipe. Request BSI.3.BSI found No.1 Engine HPC Stage 6 had several blades severe dam age. 4.Engine Change and run-up test noraml. 2 L 7 3 4F 4 F RT A22WE E31N3 2001080900002 20010809 00002 SO 2001 8 9 C2XA01IA313 1 20010807 A 2100 32144143 VALVE EMB 120 EMB120ER 3260203 SO FUSELAGE INOPERATIVE A C2XA D A RETURN TO BLOCK UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 15732 120195 IAH - FLIGHT 2928, THE CREW REPORTED SMOKE IN THE CABIN DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHO UT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND PACK CONTROL VALVE, AND THE AIRCRAFT WAS APPROVED FOR RETUR N TO SERVICE. 2 L 7 2 4T RT A31SO 2001080900008 20010809 00008 WP 2001 8 9 MWEA010824 1 20010524 A 5520 9918480502 WEB DOUG DC9 DC932 3022066 WP RT ELEVATOR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 RIGHT ELEVATOR MOST INBOARD LOWER SIDE HAS TWO LOOSE RIV-NUTS ON STRUCTURE. -- REMOVED AND REPLACED TWO RIV-NUTS. REMO VED, LOCATED AND DRILLED WEB, FABRICATED DOUBLER AND FILLER AND INSTALLED REPAIR AND WEB. 2 L 7 2 4F A6WE 2001080900012 20010809 00012 WP 2001 8 9 MWEA010839 1 20010605 A 5330 59114081 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 FUSELAGE SKIN HAS MULTIPLE DENTS FROM STATION 229 TO 258 AND FROM LONGERON 3L TO 7L. REMOVED DAMAGED AREA, FABRICATED AN D INSTALLED REPAIR PIECES. 2 L 7 2 4F A6WE 2001080900015 20010809 00015 WP 2001 8 9 MWEA010840 1 20010605 A 5330 59360043 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 FUSELAGE SKIN FROM STATION 712 TO 731 AND LONGERON 29L TO 29R IS SEVERELY CORRODED. LOCATED FUSELAGE SKIN, FABRICATED FI NGER AND INSTALLED SKIN. 2 L 7 2 4F A6WE 2001080900018 20010809 00018 WP 2001 8 9 MWEA010841 1 20010605 A 5330 59360073 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 FUSELAGE SKIN HAS TWO PREVIOUS REPAIRS (ONE AT STATION 1211.0 AT LONGERON 23 RIGHT & 24 RIGHT AND ONE REPAIR AT STATION 1231 AT LONGERON 22 RIGHT & 23 RIGHT) REMOVED SKIN, FABRICATED FILLER, NEW SKIN,DOUBLERS, FINGER DOUBLERS, INSTALLED REP AIR. 2 L 7 2 4F A6WE 2001080900021 20010809 00021 WP 2001 8 9 MWEA010842 1 20010605 A 5313 STRINGER DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 CENTER FUEL TANK STRINGER 21 AT STATION XCW 42LEFT HAS THE STRINGER CLIP REMOVED TO INSTALL REPAIR TO STRINGER FLANGE, C LIP REQUIRES REPLACEMENT. LOCATED AND INSTALLED NEW CLIP. 2 L 7 2 4F A6WE 2001080900022 20010809 00022 WP 2001 8 9 MWEA010844 1 20010605 A 5310 59101419 DOOR FRAME DOUG DC9 DC981 3022081 WP CARGO DOOR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 REPAIR FORWARD CARGO DOOR JAMB TO ACCOMMODATE ENGINEERING ORDER 2-52-0003, REPAIRED. 2 L 7 2 4F A6WE 2001080900023 20010809 00023 WP 2001 8 9 MWEA010845 1 20010605 A 5310 991960381 SHEAR TIE DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 SHEAR TIE IN AFT CARGO COMPARTMENT HAS A DENT, GOUGES AND 5 ELONGATED HOLES FOR FUSELAGE SKIN RIVETS, LOCATED BETWEEN LO NGERON 22R AT STATION 1231. REMOVED SHEAR TIE, FABRICATED AND DRILLED REPAIR ATTACH ANGLE AND INSTALLED SHEAR TIE. 2 L 7 2 4F A6WE 2001080900024 20010809 00024 NE 2001 8 9 CNMA200100029 2 20010806 A 7260 969M16P03 BEARING DOUG DC10 DC1010 3022110 WP GE CF6 CF66K 30020 NE #3 ENG FAILED A CNMA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 SW 07 360AX 46706 451149 DURING CLIMBOUT #3 ENGINE OIL STRAINER CLOGGED LIGHT CAME ON AND THROTTLE WAS REDUCED AND LIGHT WENT OUT. SHORTLY THERE AFTER OIL QTY DROPPED TO "0" AND ENGINE WAS SHUT DOWN PER COM PROCEDURES. ACCOMPLISHED FUEL DUMP INFLIGHT. REMOVED AND REPLACED RADIAL MID SHAFT AND TRANSFER GEAR BOX DRAIN LINE DUE TO RADIAL MIDSHAFT BEARING FAILURE. REMOVED AND REPLACED LUBE AND SCAVENGE PUMP AND MAIN OIL SCREEN. LK AND OPS CKD GOOD IAW GE MM. 2 L 7 3 4F 4 F A22WE E23EA 2001080900026 20010809 00026 WP 2001 8 9 MWEA010846 1 20010605 A 5730 59305025 SKIN DOUG DC9 DC981 3022081 WP LT WING DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 PREVIOUS REPAIR LEFT WING UPPER SURFACE TRAILING EDGE AT STATION XCW 121.0 HAS 5 EACH PREVIOUS BLEND AREAS. 2 L 7 2 4F A6WE 2001080900028 20010809 00028 WP 2001 8 9 MWEA010847 1 20010605 A 5330 5911401181 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 PREVIOUS REPAIR AT LEFT EXTERIOR FUSELAGE STATION 200-237 LONGERON 19 LEFT TO 21 LEFT. REMOVED PREVIOUS REPAIR, FABRICAT ED AND INSTALLED REPAIR DOUBLER AND SHIMS. 2 L 7 2 4F A6WE 2001080900031 20010809 00031 WP 2001 8 9 MWEA010848 1 20010605 A 5330 5911401181 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 FUSELAGE SKIN HAS A .375 INCH CRACK AT STATION 201 7/8 (2ND RIVET FROM 200 STATION) LONGERON 22 LEFT. -- REMOVED CRACK , FABRICATED AND INSTALLED FILLER PLUG, SHIM AND DOUBLER. 2 L 7 2 4F A6WE 2001080900035 20010809 00035 WP 2001 8 9 MWEA010849 1 20010605 A 5310 4911475524 SHEAR TIE DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 CENTER FUEL TANK UPPER SHEAR TIE CRACKED BETWEEN STRINGERS 4 AND 5 AT XCW 0 RIGHT. REMOVED UPPER SHEAR TIE AND SHIM, INS TALLED NEW UPPER SHEAR TIE AND SHIM. 2 L 7 2 4F A6WE 2001080900043 20010809 00043 WP 2001 8 9 MWEA010850 1 20010605 A 5313 593643423 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 CENTER CARGO COMPARTMENT LONGERON 29 LEFT HAS SEVERAL AREAS OF TOOLING MARKS AND CORROSION FROM STATION 541 TO 579. REMO VED CORROSION, BLENDED TOOL MARKS, DRILLED NEW LONGERON, INSTALLED INTERCOSTAL AND ANGLES. 2 L 7 2 4F A6WE 2001080900044 20010809 00044 WP 2001 8 9 MWEA010852 1 20010605 A 5711 J06016529N SPAR DOUG DC9 DC981 3022081 WP LT WING DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 PREVIOUS REPAIR, LEFT WING AFT SPAR AFT SIDE STATION XRS 164. REMOVED REPAIR, DRILLED AND INSTALLED LOWER SPAR T SECTION . 2 L 7 2 4F A6WE 2001080900045 20010809 00045 WP 2001 8 9 MWEA010853 1 20010605 A 5330 5920323249 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 FUSELAGE SKIN HAS A DENT WITH A GOUGE AT STATION 449, ABOVE LONGERON 23 RIGHT. BLENDED GOUGE, CUT OUT DAMAGED SECTION, I NSTALLED REPAIR. 2 L 7 2 4F A6WE 2001080900046 20010809 00046 WP 2001 8 9 MWEA010854 1 20010605 A 5330 5920323249 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 FUSELAGE SKIN HAS A DENT AT STATION 475, 2 INCHES BELOW LONGERON 23 RIGHT. FABRICATED REPAIR DOUBLERS AND SKIN, INSTALLE D REPAIR. 2 L 7 2 4F A6WE 2001080900047 20010809 00047 WP 2001 8 9 MWEA010856 1 20010605 A 5320 99100787 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FORWARD ENTRY SUBFLOOR WEB HAS LIGHT CORROSION AROUND GALLEY MOUNT STATION 210 RBL 11. REMOVED CORROSION, STOP DRILLED C RACK, FABRICATED, LOCATED, DRILLED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 2001080900049 20010809 00049 WP 2001 8 9 MWEA010857 1 20010605 A 5320 99100787 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FORWARD ENTRY SUBFLOOR WEB HAS LIGHT CORROSION AROUND GALLEY MOUNT STATION 217 RBL 11. REMOVED DAMAGE, FABRICATED AND IN STALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001080900051 20010809 00051 WP 2001 8 9 MWEA010858 1 20010605 A 5311 991184356 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 CENTRAL FRAME STATION 1168.8 HAD CHAFED AREA ON AFT SIDE THAT RUNS FROM 10 INCHES LEFT OF BOTTOM CENTERLINE TO JUST BELO W RIGHT EXTERNAL RAIN GUTTER. BLENDED AREA, LOCATED, DRILLED AND INSTALLED NEW FRAME. 2 L 7 2 4F A6WE 2001080900053 20010809 00053 WP 2001 8 9 MWEA010859 1 20010605 A 5321 995791917 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 CABIN FLOORBOARD E1 HAS CORROSION FORWARD END. REMOVED CORROSION, REMOVED DAMAGED AREA, FABRICATED AND LOCATED AND INSTA LLED DOUBLER AND FILLER. 2 L 7 2 4F A6WE 2001080900054 20010809 00054 WP 2001 8 9 MWEA010860 1 20010605 A 5311 995821519 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 CORROSION AND BARE METAL ON FRAME AT STATION 917 BETWEEN LONGERON 29 RIGHT AND 28 LEFT. REMOVED CORROSION ON FRAME, REMO VED DAMAGED SECTION OF FRAME, FABRICATED NEW ANGLE AND PLATES, INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001080900056 20010809 00056 WP 2001 8 9 MWEA010861 1 20010605 A 5347 74529523 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 NR 2 SEAT TRACK IS GOUGED IN TOP TRACK CHANNEL STATION 923. LOCATED, DRILLED AND INSTALLED PLUG AND CHANNEL. 2 L 7 2 4F A6WE 2001080900057 20010809 00057 WP 2001 8 9 MWEA010862 1 20010605 A 5313 76378133 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 UPPER FUSELAGE LONGERON 8 RIGHT HAS DAMAGE STATION 945. REMOVED DAMAGED LONGERON, FABRICATED AND DRILLED REPAIR PARTS, I NSTALLED NEW LONGERON SECTION AND SPLICES. 2 L 7 2 4F A6WE 2001080900058 20010809 00058 WP 2001 8 9 MWEA010863 1 20010605 A 5313 76378133 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 UPPER FUSELAGE LONGERON 8 LEFT HAS DAMAGE ON FLANGE STATION 928. LOCATED, DRILLED AND INSTALLED NEW LONGERON SECTION. 2 L 7 2 4F A6WE 2001080900059 20010809 00059 WP 2001 8 9 MWEA010864 1 20010605 A 5313 591140137 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 CORROSION BETWEEN LONGERON 30 AND SKIN, AND ON LONGERON 30 FROM STATION 110 TO 134. REMOVED, LOCATED AND INSTALLED NEW L ONGERON. 2 L 7 2 4F A6WE 2001080900060 20010809 00060 WP 2001 8 9 MWEA010865 1 20010605 A 5311 99115124 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 COCKPIT FRAME STATION 133.425 HAS MODERATE CORROSION RIGHT SIDE ABOVE CUSP. REMOVED, LOCATED, DRILLED AND INSTALLED FRAM E AND FITTING. 2 L 7 2 4F A6WE 2001080900061 20010809 00061 WP 2001 8 9 MWEA010867 1 20010605 A 5320 5956034537 CLIP DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 INTERCOSTAL TO FRAME ATTACH CLIP HAS AN ELONGATED HOLE WHERE IT TIES INTO STATION 996 BETWEEN LONGERON 27-28 LEFT. REMOV ED CLIP, FABRICATED, LOCATED, DRILLED AND INSTALLED ATTACH CLIP. 2 L 7 2 4F A6WE 2001080900063 20010809 00063 SO 2001 8 9 RAIA00108003 1 20010804 A 3240 31550 TIRE EMB 145 EMB145ER SO LT/RT MAIN FAILED A RAIA O OTHER Z SIGNIFICANT FAILURE REPORT LD LANDING 1 CE 03 809HK 145187 5266-PIT-UPON LANDING IN MEM, ALL FOUR MAIN TIRES FAILED. M,AINTENANCE INSPECTED AND REPLACED ALL FOUR MAIN TIRES, PERFO RMED OPERATIONAL CHECK, SYSTEMS CHECKED GOOD. PERFORMED CMC MAINTENANCE DOWNLOAD, NO FAULTS FOUND. 2 L 7 2 4F RT T00011AT 2001080900064 20010809 00064 SO 2001 8 9 RAIA00108004 1 20010807 A 3242 31550 WHEEL EMB 145 EMB145ER SO RT O/B FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 807HK 4703 1065 145119 5264-PIT-DURING TAXI RIGHT OUTBOARD BRAKE HOT LIGHT ILLUMINATED. MAINTENANCE INSPECTED AND FOUND RIGHT OUTBOARD MAIN WHE EL ASSEMBLY HUB FLANGE CRACKED. MAINTENANCE REPLACED THE RIGHT OUTBOARD WHEEL ASSEMBLY AND BRAKE ASSEMBLY. 2 L 7 2 4F RT T00011AT 2001080900065 20010809 00065 EU 2001 8 9 RAIA00108005 1 20010807 A 2400 A2104F PDU JETAIR JETSTM JETSTM4101 1500501 EU ELEC BAY FAILED A RAIA D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 CE 03 568HK 11005 10698 41086 7140-STL-RIGHT GENERATOR FELL OFF LINE DURING TAXI. MAINTENANCE INSPECTED AND REPLACED THE LEFT PDU (POWER DISTRIBUTION UNIT). 2 L 7 2 4T RT A41NM 2001080900066 20010809 00066 2001 8 9 RAIA00108006 4 20010808 A 3160 7003652902 DISPLAY AEROSP ATR42 ATR42300 8680920 EU INST PNL FAILED A RAIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 421TE 5912 102 PIA-7121-ELECTRICAL SMOKE COMING FROM INSTRUMNET PANEL, AIRCRAFT ON GROUND AT GATE. MAINTENANCE INSPECTED AND FOUND INST RUMENT PANEL ADU (DISPLAY UNIT) CAUSING ELECTRICAL SMOKE. MAINTENANCE REPLACED THE ADU. 2 H 7 2 4T RT A53EU 2001080900067 20010809 00067 EU 2001 8 9 RAIA00108007 1 20010808 A 3230 877701 CONTROL HANDLE JETAIR JETSTM JETSTM4101 1500501 EU INST PNL FAILED A RAIA B EMER. DESCENT O OTHER DE DESCENT 1 CE 03 561HK 12312 41077 7439-CMI-UPON APPROACH NORMAL LANDING GEAR EXTENSION WAS INOPERATIVE, CREW PERFORMED EMERGENCY GEAR EXTENSION AND LANDED WITHOUT INCEDENT. MAINTENANCE INSPECTED AND REPLACED INSTRUMENT PANEL LANDING GEAR HANDLE, PERFORMED OPERATIONAL CHECK OF THE LANDING GEAR EXTENSION AND RETRACTION SYSTEM. 2 L 7 2 4T RT A41NM 2001080900070 20010809 00070 WP 2001 8 9 MWEA010868 1 20010605 A 5311 59114481 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 STATION 294 ABOVE LONGERON 29 LEFT, 30 AND 29 RIGHT CORRODED AT FASTENERS. REMOVED CORROSION, LOCATED, DRILLED AND INSTA LLED REPAIR PARTS. 2 L 7 2 4F A6WE 2001080900077 20010809 00077 WP 2001 8 9 MWEA010869 1 20010605 A 5320 4925315505 CLIP DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 UPPER FUSELAGE LONGERON 10 LEFT SHOVEL CLIP CRACKED STATION 682. REMOVED DAMAGED SHOVEL CLIP, DRILLED AND INSTALLED NEW SHOVEL CLIP. 2 L 7 2 4F A6WE 2001080900078 20010809 00078 WP 2001 8 9 MWEA010870 1 20010605 A 5347 59108207 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 MODERATE CORROSION ON TOP OF NR 1 SEAT TRACK STATION 235. CUT AND REMOVED CORRODED PORTION, LOCATED, DRILLED AND INSTALL ED NEW TRACK AND SPLICE. 2 L 7 2 4F A6WE 2001080900079 20010809 00079 WP 2001 8 9 MWEA010871 1 20010605 A 5311 995773917 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 UPPER FUSELAGE FRAME STATION 945 J CHANNEL HAS DAMAGE IN RADIUS INBOARD OF LONGERON 8 RIGHT. REMOVED FRAME, LOCATED DRI LLED AND INSTALLED NEW FRAME, INSTALLED FRAME DOUBLER. 2 L 7 2 4F A6WE 2001080900080 20010809 00080 WP 2001 8 9 MWEA010872 1 20010605 A 5320 99101517 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 CRACK ON BOTTOM SIDE OF SUBFLOOR NEAR CUSP AREA FROM STATION 616 TO 613 RIGHT SIDE. FABRICATED AND INSTALLED REPAIR DOUB LER. 2 L 7 2 4F A6WE 2001080900081 20010809 00081 WP 2001 8 9 MWEA010873 1 20010605 A 5320 4912460501 FITTING DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 TEE FITTING CORRODED STATION 917 BELOW WEB ON AFT CARGO DOOR JAMB. REMOVED FITTING, FABRICATED, LOCATED AND INSTALLED NE W FITTING. 2 L 7 2 4F A6WE 2001080900082 20010809 00082 WP 2001 8 9 MWEA010874 1 20010605 A 5320 99115057 ANGLE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 ANGLE AT STATION 83.5 AT APPROXIMATELY X12 RIGHT CRACKED VISIBLE THROUGH PANEL 4402A. STOP DRILLED CRACK, FABRICATED REP AIR PARTS, FABRICATED, LOCATED AND DRILLED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001080900083 20010809 00083 WP 2001 8 9 MWEA010875 1 20010605 A 5320 99115057 ANGLE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 ANGLE AT STATION 83.5 AT APPROXIMATELY X12 LEFT CRACKED VISIBLE THROUGH PANEL 4401A. STOP DRILLED CRACK, FABRICATED REPA IR PARTS, FABRICATED, LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001080900085 20010809 00085 WP 2001 8 9 MWEA010876 1 20010605 A 5311 9912243227 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 CRACK IN STATION 965 FORMER, BETWEEN LONGERONS 15 LEFT AND 16 LEFT. DRILLED REPLACEMENT SHEAR TIE, FABRICATED AND INSTAL LED NEW SPLICE ANGLE. 2 L 7 2 4F A6WE 2001080900087 20010809 00087 WP 2001 8 9 MWEA010877 1 20010605 A 5347 99578551 SEAT TRACK DOUG DC9 DC932 3022066 WP COCKPIT WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FIRST OFFICERS FORWARD OUTBOARD SEAT TRACK WORN. REMOVED SEAT TRACK, BLENDED DAMAGE, FABRICATED AND INSTALLED REPAIR STR AP. 2 L 7 2 4F A6WE 2001080900088 20010809 00088 WP 2001 8 9 MWEA010878 1 20010605 A 5347 99578551 SEAT TRACK DOUG DC9 DC932 3022066 WP COCKPIT WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 CAPTAINS FORWARD OUTBOARD SEAT TRACK WORN ON THE SIDE. REMOVED SEAT TRACK, BLENDED DAMAGE, FABRICATED AND INSTALLED REPA IR STRAP. 2 L 7 2 4F A6WE 2001080900089 20010809 00089 WP 2001 8 9 MWEA010879 1 20010606 A 5320 991050313 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 1 INCH CRACK ON SUBFLOOR AT STATION 960 MOST OUTBOARD LIGHTENING HOLE BELOW PHENOLIC FLOOR SUPPORT RAIL RIGHT SIDE. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001080900091 20010809 00091 WP 2001 8 9 MWEA010880 1 20010606 A 5620 5912285509 WINDOW FRAME DOUG DC9 DC932 3022066 WP CABIN CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 CABIN WINDOW NR 25 LEFT SIDE, WINDOW PAN HAS A CRACK AT TO FORWARD CORNER. FABRICATED AND INSTALLED DOUBLER AND FILLER. 2 L 7 2 4F A6WE 2001080900092 20010809 00092 WP 2001 8 9 MWEA010881 1 20010606 A 5620 5912285505 WINDOW FRAME DOUG DC9 DC932 3022066 WP CABIN CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 CABIN WINDOW NR 24 LEFT SIDE, WINDOW PAN HAS A CRACK AT TOP FORWARD CORNER. FABRICATED AND INSTALLED DOUBLER AND FILLER. 2 L 7 2 4F A6WE 2001080900093 20010809 00093 WP 2001 8 9 MWEA010883 1 20010606 A 5330 59123508 DOUBLER DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 SKIN DOUBLER AT STATION 83.5 PART NUMBER 5912350-8 RIGHT SIDE HAS CORROSION ON OUTBOARD FLANGE. FABRICATED AND INSTALLED NEW DOUBLER. 2 L 7 2 4F A6WE 2001080900094 20010809 00094 WP 2001 8 9 MWEA010884 1 20010606 A 5311 995773925 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 STATION 945 HAS A CRACKED FORMER BETWEEN LONGERON 15 AND 16 LEFT. REMOVED FORMER, FABRICATED, LOCATED, DRILLED AND INSTA LLED NEW FORMER. 2 L 7 2 4F A6WE 2001080900095 20010809 00095 WP 2001 8 9 MWEA010885 1 20010606 A 5313 59114277 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 LONGERON 17 RIGHT CRACKED AT 965 BULKHEAD ATTACH POINT UPPER AND LOWER. REMOVED LONGERON SECTION, LOCATED AND INSTALLED NEW LONGERON. 2 L 7 2 4F A6WE 2001080900096 20010809 00096 WP 2001 8 9 MWEA010886 1 20010606 A 5313 59114279 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 LONGERON 17 RIGHT CRACKED AT 945 FRAME LOWER ATTACH POINT. REMOVED LONGERON SECTION, LOCATED AND INSTALLED NEW LONGERON. 2 L 7 2 4F A6WE 2001080900100 20010809 00100 WP 2001 8 9 MWEA010887 1 20010608 A 2170 1808492 COALESCER BAG DOUG DC9 DC982 3022082 WP A/C BAY DIRTY A MWEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 31 808ME 48070 ON ROTATION AND CLIMB CREW NOTICED STRONG ACIDIC BURNT ODOR IN COCKPIT AND CABIN. INSPECTIONS OF ALL POSSIBLE AREAS FOR ODOR OR FOREIGN SUBSTANCE. LEFT AND RIGHT COALESCER BAGS CHANGED, AIRCRAFT TEST FLOWN. 2 L 7 2 4F A6WE 2001080900102 20010809 00102 WP 2001 8 9 MWEA010888 1 20010611 A 5310 995821517 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 OVERSIZED HOLE ON STATION 917 SHEAR TIE ABOVE LONGERON 30. FABRICATED AND INSTALLED STRAP. 2 L 7 2 4F A6WE 2001080900104 20010809 00104 WP 2001 8 9 MWEA010894 1 20010611 A 5320 99100787 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 SUBFLOOR CRACKED UNDER SEAT TRACK NR 3 AT STATION 218. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001080900105 20010809 00105 WP 2001 8 9 MWEA010895 1 20010611 A 5311 5911448523 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 VERTICAL FACE OF STATION 465 HAS A SMALL CRACK AT RIVET BETWEEN LONGERON 28 AND 27 LEFT. REMOVED DAMAGED SECTION, FABRIC ATED REPAIR ANGLE, DOUBLER AND FILLER, INSTALLED REPAIR PARTS. 2 L 7 2 4F A6WE 2001080900106 20010809 00106 WP 2001 8 9 MWEA010896 1 20010611 A 5321 995791921 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 CABIN FLOORBOARD NR E10 HAS A CRACK BY ONE HOLE. 2 L 7 2 4F A6WE 2001080900107 20010809 00107 WP 2001 8 9 MWEA010897 1 20010611 A 5321 995791921 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 CABIN FLOORBOARD E-10 IS CRACKED AND CHAFED AT AFT END AND ONE HAT CHANNEL HAS SMALL CRACK ON AFT EDGE. FORMED AND FABRI CATED PARTS, ASSEMBLED HATS TO FLOORBOARD. 2 L 7 2 4F A6WE 2001080900108 20010809 00108 WP 2001 8 9 MWEA010898 1 20010611 A 5347 59108203 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FORWARD ENTRY NR 2 SEAT TRACK HAS LIGHT CORROSION FROM STATION 202-205. BLENDED CORROSION, REMOVED SECTION OF SEAT TRACK , DRILLED SEAT TRACK. 2 L 7 2 4F A6WE 2001080900110 20010809 00110 WP 2001 8 9 MWEA010899 1 20010611 A 5347 59108203 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 NR 3 SEAT TRACK HAS AREAS OF MODERATE CORROSION STATION 228-265. REMOVED SEAT TRACK SECTION, FABRICATED DRILLED AND INST ALLED NEW SEAT TRACK SECTION. 2 L 7 2 4F A6WE 2001080900113 20010809 00113 WP 2001 8 9 MWEA010900 1 20010611 A 5320 99236685 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FORWARD ENTRY SUBFLOOR WEB HAS SEVERAL 1 INCH BY 1 INCH AREAS OF LIGHT CORROSION AND BARE METAL STATION 159 LBL 1.5, LBL 4, LBL, 7, RBL 2, RBL 5, RBL 8 AND RBL 11. REMOVED CORROSION, FABRICATED LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001080900115 20010809 00115 WP 2001 8 9 MWEA010901 1 20010611 A 5320 99236685 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FORWARD ENTRY SUBFLOOR WEB HAS SEVERAL 1 INCH BY 1 INCH AREAS OF LIGHT CORROSION AND BARE METAL STATION 148 LBL 1.5, LBL 4, LBL 7, LBL 11, RBL 2, RBL 5, RBL 8 AND RBL 11. REMOVED CORROSION, FABRICATED, LOCATED, DRILLED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 2001080900117 20010809 00117 WP 2001 8 9 MWEA010902 1 20010611 A 5310 995821439 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 CORROSION ON SHEAR TIE AND ANGLE BRACKET FOR LEFT FLOOR SUPPORT AT STATION 897 BETWEEN LONGERONS 28 AND 27 LEFT. REMOVED CORROSION, FABRICATED, LOCATED, DRILLED AND INSTALLED SHEAR TIE AND ANGLE. 2 L 7 2 4F A6WE 2001080900119 20010809 00119 WP 2001 8 9 MWEA010903 1 20010611 A 5321 995792821 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 CABIN FLOORBOARD E15 HAS A TORN CORNER. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001080900122 20010809 00122 WP 2001 8 9 MWEA010904 1 20010611 A 5321 995791919 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 CABIN FLOORBOARD E11 HAS TWO ELONGATED HOLES. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001080900124 20010809 00124 WP 2001 8 9 MWEA010905 1 20010611 A 5315 5910347443 FLOORBEAM DOUG DC9 DC932 3022066 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 GOUGE ON BOTTOM OF CABIN FLOOR BEAM AT STATION 917 ABOUT 2 INCHES RIGHT OF CENTER INTERCOSTAL. FABRICATED, DRILLED AND I NSTALLED REPAIR DOUBLERS. 2 L 7 2 4F A6WE 2001080900128 20010809 00128 WP 2001 8 9 MWEA010910 1 20010612 A 5321 99579233 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 CABIN FLOORBOARD B-6 IS CHAFED IN 2 PLACES. REMOVED DAMAGE, FABRICATED 2 EA DOUBLERS, INSTALLED REPAIR FILLERS AND DOUBL ERS. 2 L 7 2 4F A6WE 2001080900131 20010809 00131 WP 2001 8 9 MWEA010911 1 20010612 A 5330 5911427 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 STATION 980 SKIN IS CRACKED BELOW LONGERON 14 RIGHT. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER, DOUBLER AND SHIMS. 2 L 7 2 4F A6WE 2001080900132 20010809 00132 WP 2001 8 9 MWEA010912 1 20010612 A 5313 27779224 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 LONGERON 16 RIGHT AT STATION 965 HAS ONE BADLY ELONGATED HOLE. REMOVED DAMAGED AREA, LOCATED AND DRILLED NEW SECTION OF LONGERON, FABRICATED, LOCATED, DRILLED AND INSTALLED SPLICE REPAIR. 2 L 7 2 4F A6WE 2001080900133 20010809 00133 WP 2001 8 9 MWEA010913 1 20010612 A 5410 991550030 CLIP DOUG DC9 DC932 3022066 WP RT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 RT PYLON AFT SPAR, TOP SUPPORT CLIP HAS A CRACK, LOCATED INBOARD OF AFT ISOLATOR. REMOVED CLIP, FABRICATED AND INSTALLED SUPPORT CLIP. 2 L 7 2 4F A6WE 2001080900134 20010809 00134 WP 2001 8 9 MWEA010914 1 20010612 A 5410 991550029 ANGLE DOUG DC9 DC932 3022066 WP LT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 LT PYLON INTERCOSTAL AFT OF APRON HAS A CRACKED ATTACH BRACKET AT TOP END. REMOVED CRACKED ANGLE, FABRICATED AND INSTALL ED NEW ANGLE. 2 L 7 2 4F A6WE 2001080900135 20010809 00135 WP 2001 8 9 MWEA010915 1 20010612 A 5321 99579249 FLOOR PANEL DOUG DC9 DC932 3022066 WP CABIN CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 FLOOR PANEL B7 HAS AREAS OF DEEP CHAFFING. REMOVED CHAFED HAT CHANNEL, FABRICATED AND INSTALLED HAT CHANNEL. 2 L 7 2 4F A6WE 2001080900136 20010809 00136 WP 2001 8 9 MWEA010916 1 20010612 A 5321 995792713 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 FLOOR PANEL E7 HAS A CRACKED OUT FASTENER HOLE. REMOVED DAMAGED AREA, FABRICATED DOUBLER AND FILLER, INSTALLED REPAIR PA RTS. 2 L 7 2 4F A6WE 2001080900139 20010809 00139 WP 2001 8 9 MWEA010917 1 20010612 A 5321 995791921 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 FLOOR PANEL B8 UPPER SURFACE IS CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS. 2 L 7 2 4F A6WE 2001080900140 20010809 00140 WP 2001 8 9 MWEA010918 1 20010612 A 5321 995792926 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 FLOOR PANEL E10 HAS AREA OF CORROSION ON LOWER SURFACE. BLENDED CORROSION, FABRICATED AND INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001080900141 20010809 00141 WP 2001 8 9 MWEA010919 1 20010612 A 5321 99579191 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 FLOOR PANEL E1 HAS AREAS OF SEVERE CORROSION ON LOWER SURFACE. BLENDED AREA, REMOVED DAMAGED AREA, FABRICATED REPAIR DOU BLER AND FILLER, INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001080900142 20010809 00142 SO 2001 8 9 LR7A01055 1 20010805 A 5730 398852 PANEL LKHEED 382 382G 526414U SO RH CWS 202-207 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 44117 2167 4763 DURING SCHEDULED C2 INSPECTION SCHEDULED REPAIR FOR TIME LIMITED LMAS ENGINEERING DISPOSITON FOR RH CENTER WING LOWER SU RFACE, AFT PANEL CORROSION BLENDOUT AT CWS 202-207, FS 575-590.ACCOMPLISHED REPAIR IAW LAC MEA 382-57-01-032. NR 2001. 2 H 7 4 4T A1SO 2001080900143 20010809 00143 SO 2001 8 9 LR7A01056 1 20010805 A 5320 BEAM LKHEED 382 382G 526414U SO FS 577-597 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2167 4763 DURING SCHEDULED C2 INSPECTION PER JOB CARD HC3209 FOUND FS 577 - 597 RMLG UPPER WHEEL WELL BEAM CRACKED AT RBL 70 , WL 236.REPLACED BEAM IAW SRM SMP 583 57-20-02 (12). NR 2007. 2 H 7 4 4T A1SO 2001080900144 20010809 00144 SO 2001 8 9 LR7A01057 1 20010805 A 5330 SKIN LKHEED 382 382G 526414U SO FS 869-1001 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2167 4763 DURING SCHEDULED C2 INSPECTION PER JOB CARD HC5303 FOUND LH FS 869 - 1001 FUSELAGE SKIN CRACKED AT LBL 61, WL 194-270 AN D HIGH DENSITY OF PREVIOUS REPAIRS.REPAIRED IAW LAC MEA 382-53-01-047. NR 2051. 2 H 7 4 4T A1SO 2001080900145 20010809 00145 SO 2001 8 9 LR7A01059 1 20010805 A 5330 SKIN LKHEED 382 382G 526414U SO FS 777E-817E DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2167 4763 DURING SCHEDULED C2 INSPECTION PER JOB CARD HC5303 FOUND FS 777E -817E BELLY SKIN DENTED AND SCRATCHED LBL 61 TO RBL 61. REPLACED BELLY SKIN IAW SRM SMP 583-53-10 PG 2. NR 2055. 2 H 7 4 4T A1SO 2001080900146 20010809 00146 SO 2001 8 9 LR7A01060 1 20010805 A 5330 SKIN LKHEED 382 382G 526414U SO FS 697-737 DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2167 4763 DURING SCHEDULED C2 INSPECTION PER JOB CARD HC5303 FOUND FS 697 - 737 BELLY SKIN WITH SEVERAL DENTS AT LBL 61 TO RBL 61. REPLACED BELLY SKIN IAW SRM SMP 583-53-10 PG 4. NR 2056. 2 H 7 4 4T A1SO 2001080900147 20010809 00147 SO 2001 8 9 LR7A01061 1 20010805 A 5311 FRAME LKHEED 382 382G 526414U SO FS 970 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2167 4763 DURING SCHEDULED C2 INSPECTION PER JOB CARD HSP5330 FOUND FS 970 LH UPPER RING SEGMENT CRACKED AT LBL 61, WL 256.REPAIRE D IAW SRM SMP 583-51-140-19. NR 2077. 2 H 7 4 4T A1SO 2001080900148 20010809 00148 SO 2001 8 9 LR7A01062 1 20010805 A 5311 FRAME LKHEED 382 382G 526414U SO FS 277 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2167 4763 DURING SCHEDULED C2 INSPECTION PER JOB CARD HC05297 FOUND FS 277 LH RING SEGMENT CRACKED AT LBL 63, WL 146.REPAIRED IAW SRM SMP 583-51-140-21. NR 2083. 2 H 7 4 4T A1SO 2001080900149 20010809 00149 SO 2001 8 9 LR7A01063 1 20010805 A 5321 FLOOR PANEL LKHEED 382 382G 526414U SO FS 245-345E WARPED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2167 4763 DURING SCHEDULED C2 INSPECTION PER JOB CARD HC05297 FOUND FS 245 - 345E RH FLOOR PANEL WARPED AND CORRODED AT RBL 16 - 5 2, WL 146.REPLACED FLOOR PANEL IAW SRM SMP 583-53-40-05. NR 2119. 2 H 7 4 4T A1SO 2001080900150 20010809 00150 SO 2001 8 9 LR7A01064 1 20010805 A 5321 FLOOR PANEL LKHEED 382 382G 526414U SO FS 737E-817E WARPED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2167 4763 DURING SCHEDULED C2 INSPECTION PER JOB CARD HC05297 FOUND FS 737E - 817E CENTER FLOOR PANEL WARPED AND CORRODED AT BL 0, WL 146.REPLACED FLOOR PANEL IAW SRM SMP 583-53-40-05. NR 2121. 2 H 7 4 4T A1SO 2001080900151 20010809 00151 SO 2001 8 9 LR7A01065 1 20010805 A 5330 SKIN LKHEED 382 382G 526414U SO FS 840 GOUGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2167 4763 DURING SCHEDULED C2 INSPECTION PER JOB CARD HC05297 FOUND LH FS 840 RAMP ACTUATOR CUTOUT AREA GOUGED AT LBL 63, WL 180.R EPAIRED IAW LAC MEA 382-53-01-034 NR 2133. 2 H 7 4 4T A1SO 2001080900152 20010809 00152 SO 2001 8 9 LR7A01066 1 20010805 A 5312 CAP LKHEED 382 382G 526414U SO FS 537 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2167 4763 DURING SCHEDULED C2 INSPECTION PER JOB CARD HC3209 FOUND LH FS 537 BOW BEAM CAP CRACKED AT LBL 61, WL 206.REPAIRED IAW S RM SMP 583-53-40-14. NR 2134. 2 H 7 4 4T A1SO 2001080900153 20010809 00153 SO 2001 8 9 LR7A01067 1 20010805 A 5321 FLOOR PANEL LKHEED 382 382G 526414U SO FS 245-345E WARPED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2167 4763 DURING SCHEDULED C2 INSPECTION PER JOB CARD HC05297 FOUND FS 245 - 345E RH FLOOR PANEL WARPED AND CORRODED AT LBL 16 - 42, WL 146.REPLACED FLOOR PANEL IAW SRM SMP 583-53-40-05. NR 2143. 2 H 7 4 4T A1SO 2001080900154 20010809 00154 SO 2001 8 9 LR7A01068 1 20010805 A 5311 LS4010 FRAME LKHEED 382 382G 526414U SO FS 277 & 317 ELONGATED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2167 4763 DURING SCHEDULED C2 INSPECTION NR 2098 ACCOMLISHMENT (CURB PANEL REPLACEMENT) FOUND FS 277 AND FS 317 LOWER RING SEGMENT S WITH ELONGATED HOLES AT LBL 64, WL 152.REPAIRED IAW LAC MEA 382-53-01-052. NR 2166. 2 H 7 4 4T A1SO 2001080900155 20010809 00155 SO 2001 8 9 LR7A01069 1 20010805 A 5311 LS4010 FRAME LKHEED 382 382G 526414U SO FS 762E-772E ELONGATED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2167 4763 DURING SCHEDULED C2 INSPECTION NR 2098 ACCOMLISHMENT (CURB PANEL REPLACEMENT) FOUND FS 762E, 767E AND 772E LOWER RING SE GMENTS WITH ELONGATED HOLES AT LBL 64, WL 154.REPAIRED IAW LAC MEA 382-53-01-052. NR 2166. 2 H 7 4 4T A1SO 2001080900156 20010809 00156 SO 2001 8 9 LR7A01070 1 20010805 A 5311 LS4010 FRAME LKHEED 382 382G 526414U SO FS 677 & 807E ELONGATED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2167 4763 DURING SCHEDULED C2 INSPECTION NR 2098 ACCOMLISHMENT (CURB PANEL REPLACEMENT) FOUND FS 677 AND 807E LOWER RING SEGMENTS WITH ELONGATED HOLES AT LBL 64, WL 151.REPAIRED IAW LAC MEA 382-53-01-052. NR 2166. 2 H 7 4 4T A1SO 2001080900157 20010809 00157 SO 2001 8 9 LR7A01071 1 20010805 A 5311 LS4010 FRAME LKHEED 382 382G 526414U SO FS 341E-807E MISDRILLED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2167 4763 DURING SCHEDULED C2 INSPECTION NR 2098 ACCOMLISHMENT (CURB PANEL REPLACEMENT) FOUND FS 341E, 677, 762E, 767E, 772E & 807 E LOWER RING SEGMENTS WITH MISDRILLED HOLES AT LBL 64, WL 152.REPAIRED IAW LAC MEA 382-53-01-052. NR 2166. 2 H 7 4 4T A1SO 2001080900158 20010809 00158 SO 2001 8 9 LR7A01072 1 20010805 A 5311 LS4010 FRAME LKHEED 382 382G 526414U SO FS 757E-801E ELONGATED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2167 4763 DURING SCHEDULED C2 INSPECTION NR 2098 ACCOMLISHMENT (CURB PANEL REPLACEMENT) FOUND FS 757E,777E, 797E & 801E LOWER RING SEGMENTS WITH ELONGATED HOLES AT RBL 64, WL 154.REPAIRED IAW LAC MEA 382-53-01-052. NR 2166. 2 H 7 4 4T A1SO 2001080900159 20010809 00159 SO 2001 8 9 LR7A01073 1 20010805 A 5311 LS4010 FRAME LKHEED 382 382G 526414U SO FS 336-807E MISDRILLED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2167 4763 DURING SCHEDULED C2 INSPECTION NR 2098 ACCOMLISHMENT (CURB PANEL REPLACEMENT) FOUND FS 336, 702, 707, 711, 716, 722, 727 , 732, 737, 757E, 777E, 781E, 797E, 801E AND 807E LOWER RING SEGMENTS WITH MISDRILLED HOLES AT RBL 64, WL 152.REPAIRED I AW LAC MEA 382-53-01-052. NR 2166. 2 H 7 4 4T A1SO 2001080900160 20010809 00160 SO 2001 8 9 LR7A01074 1 20010805 A 5330 SKIN LKHEED 382 382G 526414U SO FS 737E-817E DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2167 4763 DURING SCHEDULED C2 INSPECTION PER JOB CARD HC5303 FOUND RH FS 737E - 817E FUSELAGE SKIN DENTED IN SEVERAL LOCATIONS RBL 65, WL 146 - 166REPAIRED IAW LAC MEA 382-53-01-045. NR 2173. 2 H 7 4 4T A1SO 2001080900161 20010809 00161 SO 2001 8 9 LR7A01075 1 20010805 A 5330 SKIN LKHEED 382 382G 526414U SO FS 777E-817E DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2167 4763 DURING SCHEDULED C2 INSPECTION PER JOB CARD HC5303 FOUND LH FS 777E - 817E FUSELAGE SKIN DENTED IN SEVERAL LOCATIONS LBL 65, WL 146 - 160.REPAIRED IAW LAC MEA 382-53-01-046. NR 2174. 2 H 7 4 4T A1SO 2001080900163 20010809 00163 WP 2001 8 9 MWEA010920 1 20010612 A 5321 995791820 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 FLOOR PANEL F1 PREVIOUS REPAIR IS BENT. REMOVED REPAIR, FABRICATED HAT SECTION, INSTALLED HAT CHANNELS. 2 L 7 2 4F A6WE 2001080900165 20010809 00165 WP 2001 8 9 MWEA010921 1 20010612 A 5321 991559811 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 FLOOR PANEL E6 AT STATION 579 IS CRACKED. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER. 2 L 7 2 4F A6WE 2001080900166 20010809 00166 WP 2001 8 9 MWEA010922 1 20010612 A 5321 995791819 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 FLOOR PANEL A7 AT STATION 756 IS CRACKED. REMOVED DAMAGED END OF FLOOR PANEL, FABRICATED AND INSTALLED FILLER MATERIAL A ND DOUBLER. 2 L 7 2 4F A6WE 2001080900167 20010809 00167 WP 2001 8 9 ZW0A0106401 1 20010807 A 3350 60030451 POWER SUPPLY DOUG DC9 DC982 3022082 WP TAIL COMPT A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 940AS 49825 FOUR EMERGENCY CEILING LIGHTS WERE INOPERATIVE IN THE TAIL COMPARTMENT OVER THE WALKWAY. REPLACED THE POWER SUPPLY. CH ECK-C 6-23-01 STL. --CLOSED-- 2 L 7 2 4F A6WE 2001080900168 20010809 00168 WP 2001 8 9 MWEA010923 1 20010612 A 5320 99100785 WEB DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 SUBFLOORING FASTENER HOLES LOCATED UNDERNEATH SEAT TRACK NR 4 BETWEEN STATION 218 TO APPROXIMATELY 245 ARE ELONGATED. FA BRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 2001080900169 20010809 00169 WP 2001 8 9 MWEA010924 1 20010612 A 5321 9919160211 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 CABIN FLOOR PANEL B9 HAS A HOLE IN TOP SURFACE NEAR CENTER OF PANEL. REMOVED FLOORBOARD, REPAIRED AND INSTALLED. 2 L 7 2 4F A6WE 2001080900174 20010809 00174 WP 2001 8 9 MWEA010925 1 20010612 A 5320 9915558201 STIFFENER DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 RIGHT LAV BOTTOM AFT PRESSURE BULKHEAD 996 STIFFENER FRAME WEB PORTION IS CRACKED AT OUTBOARD END. STOP DRILLED CRACK, F ABRICATED AND INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F A6WE 2001080900176 20010809 00176 WP 2001 8 9 MWEA011117 1 20010809 A 5230 5912494501 PAN DOUG DC9 DC932 3022066 WP FWD CARGO DOOR GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 FORWARD CARGO DOOR JAMB PAN IS GOUGED APPROXIMATELY 10" AFT OF THE LOWER AFT DOOR STOP. -- BLENDED GOUGE, LOCATED AND INSTALLED NEW LOWER PAN. 2 L 7 2 4F A6WE 2001080900177 20010809 00177 WP 2001 8 9 MWEA010926 1 20010612 A 5330 5911427 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 LEFT LAV SKIN IS CRACKED 2 INCH BELOW LONGERON 14 LEFT STATION 990. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAI R DOUBLER AND FILLER. 2 L 7 2 4F A6WE 2001080900180 20010809 00180 WP 2001 8 9 MWEA010927 1 20010612 A 5330 5911427 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 LEFT LAV SKIN IS CRACKED JUST BELOW SHEAR TIE AND ABOVE LONGERON 16 LEFT STATION 980. REMOVED DAMAGED AREA, FABRICATED D OUBLER AND FILLER, LOCATED AND DRILLED REPAIR PARTS, INSTALLED DOUBLER, FILLER AND SHIM. 2 L 7 2 4F A6WE 2001080900185 20010809 00185 WP 2001 8 9 MWEA010929 1 20010612 A 5330 5911427 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 RIGHT LAVATORY SKIN IS CRACKED AT STATION 990 APPROXIMATELY 2.5 INCH CRACK 2 INCHES BELOW LONGERON 14 RIGHT. REMOVED DAM AGED SKIN, FABRICATED AND INSTALLED DOUBLER, FILLER AND SHIM. 2 L 7 2 4F A6WE 2001080900186 20010809 00186 WP 2001 8 9 MWEA010931 1 20010612 A 5347 2914913 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 NR 4 SEAT TRACK CORRODED FROM STATION 200-237. REMOVED CORROSION, FABRICATED NEW SEAT TRACK SECTION, INSTALLED SEAT TRAC K AND SPLICES. 2 L 7 2 4F A6WE 2001080900187 20010809 00187 WP 2001 8 9 MWEA010932 1 20010612 A 5321 9957826 FLOORBOARD DOUG DC9 DC932 3022066 WP COCKPIT CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 FLOORBOARD SKIN CORRODED BETWEEN FIRST OFFICERS AFT SEAT TRACK, FORWARD OF STATION 160. BLENDED CORRODED AREA, MADE NEW SKIN. 2 L 7 2 4F A6WE 2001080900188 20010809 00188 WP 2001 8 9 MWEA010935 1 20010612 A 5410 995819310 WEB DOUG DC9 DC932 3022066 WP RT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 RIGHT PYLON WEB IS CRACKED APPROXIMATELY 6 INCHES BELOW FIRE EXTINGUISHER DISCHARGE TUBE. FABRICATED AND INSTALLED REPAI R DOUBLERS. 2 L 7 2 4F A6WE 2001080900189 20010809 00189 WP 2001 8 9 MWEA010936 1 20010612 A 5620 5912285515 WINDOW FRAME DOUG DC9 DC932 3022066 WP CABIN CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 RIGHT CABIN WINDOW FRAME BETWEEN STATION 639-658 INNER DOUBLER CRACKED AT LOWER AFT CORNER. FABRICATED REPAIR, INSTALLED STACKED ANGLE REPAIR. 2 L 7 2 4F A6WE 2001080900190 20010809 00190 WP 2001 8 9 MWEA010937 1 20010612 A 5311 59356509 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 FRAME STATION 699 LEFT HAS AN APPROXIMATELY 3.5 INCH CRACK IN LOWER POCKET AFT HORIZONTAL AND VERTICAL FLANGE AREA. REMO VED TWO MOUNT BRACKETS FROM FRAME, FABRICATED SHIM, LOCATED AND DRILLED HOLES IN DOUBLER, LOCATED AND INSTALLED COVER, I NSTALLED DOUBLER AND TAPERED WEDGES. 2 L 7 2 4F A6WE 2001080900192 20010809 00192 WP 2001 8 9 MWEA010938 1 20010612 A 5310 J06011940 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 RIGHT LAVATORY SHEAR TIE CRACKED ON FRAME 980 JUST BELOW LONGERON 14 RIGHT. LOCATED, DRILLED AND INSTALLED NEW SHEAR TIE . 2 L 7 2 4F A6WE 2001080900193 20010809 00193 NM 2001 8 9 0102805520 1 20010730 A 3250 271N61191 LINE BOEING 757 757251 1384970 NM LT WHEEL WELL RUPTURED A NWAA O OTHER K FLUID LOSS AP APPROACH 1 GL 01 520US 23208 ON GEAR EXTENSION, THE LEFT HYDRAULIC SYSTEM QUANTITY DECREASED TO ZERO AND A "L HYD SYS PRESS" MESSAGE WAS DISPLAYED. F LIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR DOWNLOCK RETURN LINE. OPERATIONAL TEST S WERE SATISFACTORY. 2 L 7 2 4F RT A2NM 2001080900194 20010809 00194 NM 2001 8 9 0102816631 1 20010805 A 3350 6042225 POWER SUPPLY BOEING 747 747251B 1384892 NM A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 631US 23111 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE IN ZONES 'B' AND 'C'. REPLACED POWER SUPPLY AND B ATTERY. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F A20WE 2001080900195 20010809 00195 WP 2001 8 9 MWEA010939 1 20010612 A 5320 99118573 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 INTERCOSTAL JUST ABOVE AND INBOARD OF YAW DAMPENER ACTUATOR IS CRACKED. REMOVED CRACKED INTERCOSTAL, FABRICATED AND INST ALLED NEW INTERCOSTAL. 2 L 7 2 4F A6WE 2001080900197 20010809 00197 EU 2001 8 9 C2XA01BT146 1 20010731 A 5300 S5397450221402 INTERCOSTAL AEROSP ATR42 ATR42320 8680930 EU CORRODED A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 14819 156 YUL---CO4372, DURING 1C INSPECTION YUL MAINTENANCE FOUNDINTERCOSTAL TO BE CORRODED BETWEEN FRAMES 27A AND 28A AT STRINGE R(S) 19R AND 19L.....MAINTENANCE REMOVED AND REPLACED INTERCOSTAL WITH NEW PART IAW ATR42 SRM 51-25-01. 2 H 7 2 4T RT A53EU 2001080900198 20010809 00198 WP 2001 8 9 MWEA010940 1 20010612 A 5230 391402550IN FITTING DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 AFT CARGO DOOR FORWARD NR 5 BEAM END FITTING CRACKED. REMOVED CRACK AND FITTING, POSITIONED AND DRILLED NEW FITTING, INS TALLED NEW FITTING. 2 L 7 2 4F A6WE 2001080900201 20010809 00201 WP 2001 8 9 MWEA010941 1 20010612 A 5410 59132623 ANGLE DOUG DC9 DC932 3022066 WP RT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 STATION 980 ANGLE ON THE TOP OF RIGHT PYLON IS CRACKED. REMOVED DAMAGED ANGLE, FABRICATED NEW ANGLE AND REPAIR STRAPS, I NSTALLED REPAIR PARTS. 2 L 7 2 4F A6WE 2001080900202 20010809 00202 WP 2001 8 9 MWEA010942 1 20010608 A 5313 591141581 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 CRACKED LONGERON AT LONGERON 5 LEFT AND BS 738. REMOVED DAMAGED SECTION OF LONGERON 5 LEFT AND SPLICE IN NEW SECTION. 2 L 7 2 4F A6WE 2001080900203 20010809 00203 WP 2001 8 9 MWEA010943 1 20010609 A 5313 591141513 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 CRACKED LONGERON AT BS 738 AND LONGERON 4 LEFT. REMOVED DAMAGED SECTION OF LONGERON 4 LEFT AND SPLICE IN NEW SECTION. 2 L 7 2 4F A6WE 2001080900204 20010809 00204 EU 2001 8 9 C2XA01BT147 1 20010727 A 5300 S5368201500601 VENTURI AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 14819 156 YUL---CO4372, DURING 1C INSPECTION YUL MAINTENANCE FOUND LAV VENTURI TO BE CORRODED....REMOVED AND REPLACED WITH NEW VEN TURI IAW ATR42 SRM 51-25-01. 2 H 7 2 4T RT A53EU 2001080900208 20010809 00208 EA 2001 8 9 COMA0160571 1 20010728 A 5300 601R38303253 ANGLE CNDAIR CL600 CL6002B19 EA CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 926CA 18280 7027 SERVICE DOOR SILL ANGLE IS CORRODED.REMOVED AND REPLACED I/A/W WVAC EO 601R-53-2589A. 2 L 7 2 4F RT A21EA 2001080900209 20010809 00209 EA 2001 8 9 COMA0160572 1 20010731 A 5346 60135006 WEB CNDAIR CL600 CL6002B19 EA CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 927CA 17670 7031 DURING COMPLIANCE OF EO 53-021 (VISUAL INSPECTION OF THE ENGINE SUPPORT BEAM) FOUND UPPER WEB OF ENGINE SUPPORT BEAM CRA CKED.REPAIRED THE ENGINE SUPPORT BEAM IN ACCORDANCE WITH CRJ REO 601-53-61-345. 2 L 7 2 4F RT A21EA 2001080900210 20010809 00210 EU 2001 8 9 C2XA01BT148 1 20010728 A 2500 S2541000700000 FITTING AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 14819 156 YUL---CO4372, DURING 1C INSPECTION IN YUL MAINTENANCE FOUND LAVATORY ATTACHMENT BRACKET(FITTING) IN SEAT TRACK TO BE COR RODED....REMOVED AND REPLACED ATTACHMENT FITTING WITH NEW PART IAW ATR42 JIC 25-45-21-RAI-10000-014. 2 H 7 2 4T RT A53EU 2001080900211 20010809 00211 SO 2001 8 9 COMA0110135 1 20010801 A 3150 ATG120TR PROXIMITY SWITCH EMB 120 EMB120RT SO MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 267CA 120259 TAKE OFF TRIM AURAL WARNING.REPLACED DEFECTIVE ELEV. TRIM PROXIMITY SENSOR. 2 L 7 2 4T RT A31SO 2001080900212 20010809 00212 EA 2001 8 9 COMA0160570 1 20010806 A 5320 60034017351 ANGLE CNDAIR CL600 CL6002B19 EA CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 978CA 10541 7158 THE FWD "J" ANGLE AT FS 280, LBL9 TO RBL9 AT WL 73.5 IS CORRODED.REPLACED DISCREPANT PART I/A/W WVAC EO 601R-53-2631. 2 L 7 2 4F RT A21EA 2001080900214 20010809 00214 WP 2001 8 9 MWEA010945 1 20010612 A 2751 WIRE DOUG DC9 DC915 3022036 WP T/E FLAP DAMAGED A MWEA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 GL 31 300ME 45718 ON TAKE OFF STALL WARNING CAME ON AT 150 FEET WITH NORMAL AIRCRAFT CLIMB AND ALTITUDE. REPLACED AND REPAIRED WIRING AT P 1-62 FLAP POSITION TRANSMITTER. 2 L 7 2 4F A6WE 2001080900215 20010809 00215 WP 2001 8 9 ZW0A0106501 1 20010807 A 3350 58222 BATTERY PACK DOUG DC9 DC982 3022082 WP MID SECTION A ZW0A K NONE O OTHER CR CRUISE 1 CE 13 925TW 49357 THE CENTER SECTION OF EGRESS LIGHTS ILLUMINATED WITH THE SWITCH IN EITHER ARMED OR ON POSITION. REPLACED THE BATTERY PA CK. CHECK-C 7-29-01 STL. --CLOSED-- 2 L 7 2 4F A6WE 2001080900216 20010809 00216 WP 2001 8 9 ZW0A0106503 1 20010808 A 3350 58222 POWER SUPPLY DOUG DC9 DC982 3022082 WP ROW 9 A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 925TW 49357 THE EGRESS LIGHT STRIP ROWS 7 TO 14 CAME ON INTERMITTENTLY. REPLACED THE POWER SUPPLY. CHECK-C 7-29-01 STL. --CLOSED-- 2 L 7 2 4F A6WE 2001080900220 20010809 00220 EA 2001 8 9 COMA0160573 1 20010807 A 2760 CONTROL UNIT CNDAIR CL600 CL6002B19 EA A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 781CA 7312 DURING TAKE OFF CONFIG SPOILERS MESSAGE ACTIVATED AT 40 KNOTS, ABORTED TAKE OFF AND RETURNED TO GATE.PERFORMED RESET OF THE SPOILER ELECTRONIC CONTROL UNIT. 2 L 7 2 4F RT A21EA 2001080900225 20010809 00225 WP 2001 8 9 MWEA010947 1 20010611 A 4920 3812761 APU DOUG DC9 DC932 3022066 WP APU BAY LEAKING A MWEA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 401ME 47133 SMOKE IN AFT CABIN DURING TAXI INTO GATE. INSPECTED AND FOUND APU TO HAVE OIL IN COMPRESSOR, REMOVED AND REPLACED COALES CER BAGS. REMOVED AND REPLACED APU. 2 L 7 2 4F A6WE 2001080900231 20010809 00231 WP 2001 8 9 MWEA010980 1 20010614 A 2120 UNKNOWN DOUG DC9 DC914 3022034 WP CABIN ODOR A MWEA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 600ME 45725 PRIOR TO PUSH BACK 3 PASSENGERS NOTIFIED THE FLIGHT ATTENDANT THAT THEY SMELLED AN ELECTRICAL ODOR COMING FROM THE A/C V ENTS. NOTE: WATER VAPOR IS COMING FROM THE VENTS. RAN LEFT AND RT PACKS, NO ODOR NOTED. INSPECTED AFT ASSY, LT AND RT AC M'S OK, CHECKED APU COMPARTMENT NO DEFECTS NOTED. RAN LEFT AND RIGHT ENGINES WITH LEFT AND RT PACKS ON, NO ODOR NOTED BY MAINTENANCE, CREW OR PASSENGERS, OK FOR SERVICE. 2 L 7 2 4F A6WE 2001080900232 20010809 00232 2001 8 9 COMA0160574 4 20010808 A 2220 CONTROLLER CNDAIR CL600 CL6002B19 EA A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 814CA 7387 DURING FLIGHT CONTROL CHECK AT FULL DEFLECTION THE #2 YAW DAMPER DROPPED OFF LINE.PERFORMED SYSTEM RESET PER FIM, OPERAT IONAL CHECK WAS SATISFACTORY. 2 L 7 2 4F RT A21EA 2001080900236 20010809 00236 EA 2001 8 9 COMA0160577 1 20010808 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 958CA 7111 CENTER FUSELAGE ON RIGHT EXTERIOR OF FUSELAGE FOUND INOPERATIVE.DEFERRED INOPERATIVE EXTERIOR EMERGENCY LIGHT PER MEL. 2 L 7 2 4F RT A21EA 2001080900237 20010809 00237 EA 2001 8 9 COMA0160578 1 20010808 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 946CA 7072 FLOOR EMERGENCY LIGHTING FOR ROWS 9 THROUGH 12 FOUND INOPERATIVE.CLEANED CONNECTOR CONTACTS FOR AFFECTED LIGHTING, OPERA TIONAL CHEECK WAS SATISFACTORY. 2 L 7 2 4F RT A21EA 2001080900238 20010809 00238 WP 2001 8 9 MWEA010986 1 20010616 A 7931 CONNECTOR DOUG DC9 DC914 3022034 WP RT ENGINE LOOSE A MWEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 31 700ME 45696 DURING TAXI OUT, RIGHT ENGINE OIL PRESSURE BEGAN FLUCTUATING BETWEEN 30-45 PSI. ENGINE WAS SHUT DOWN AND RETURNED TO GAT E. FOUND LOOSE CANNON PLUG AT NO.2 ENGINE OIL PRESSURE TRANSMITTER, RE-TIGHTENED CANNON PLUG. 2 L 7 2 4F A6WE 2001080900240 20010809 00240 WP 2001 8 9 MWEA010998 1 20010619 A 3260 801801 PROXIMITY SENSOR DOUG DC9 DC932 3022066 WP LT MLG FAULTY A MWEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 502ME 48132 LEFT MAIN RED UNSAFE LIGHT STAYED ON AFTER GEAR RETRACTED. REMOVED AND REPLACED LEFT MAIN GEAR UPLOCK PROX SENSOR. 2 L 7 2 4F A6WE 2001080900248 20010809 00248 NE 2001 8 9 MWEA011000 2 20010625 A 7321 7436024 FUEL CONTROL DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7B 52053 NE RT ENGINE FAULTY A MWEA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 401ME 47133 RIGHT ENGINE SURGE OF EPR & N1 1.80 TO 1.88, 4 PERCENT VARIABLE ON N1 AT ALL POWER SETTINGS. REMOVED AND REPLACED FUEL C ONTROL UNIT ON RIGHT ENGINE. 2 L 7 2 4F 4 F A6WE E2EA 2001080900250 20010809 00250 NE 2001 8 9 EVA003 2 20010803 A 7320 CF680C2D1F ENGINE DOUG MD11 MD11 3023602 NM GE CF6 CF680C2D1F 30025 NE NR 2 FLAMED OUT W QOCF A UNSCHED LANDING R X J PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 WP 03 22781 9584 48415 704163 1. AIRCRAFT B-16103 DURING CRUISE 5 MINUTES BEFORE TOD, "ENG 2 RPM LO" LEVEL 2 ALERT APPEARED. FOLLOWED CHECK LIST, AIR RESTART WAS SUCCESSFUL.2. ON GROUND, CHECK CFDS NO RELATED FUALT FOUND.3. CHECK ENGINE CONDITION ALL NORMAL. EEC TEST PA SS. PERFORM ENGINE RUN CHECK NORMAL PER MM 71-00-00.4. NEXT SEVERAL FLIGHTS, ENGINE 2 OPERTION WERE NORMAL.5. ON AUG/05, FOR MAINTENANCE PREVENTION, REPLACED THE HMU AND OPERATION CHECK NORMAL. 2 L 7 3 4F 4 F RT A22WE E31N3 2001080900251 20010809 00251 WP 2001 8 9 MWEA011001 1 20010626 A 7931 42D110 PRESSURE SWITCH DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE RT ENGINE FAILED A MWEA E ENGINE SHUTDOWN N FALSE WARNING AP APPROACH 1 GL 31 212ME 47701 667201 ON APPROACH TO MILWAUKEE, RIGHT ENGINE OIL PRESSURE LOW LIGHT CAME ON, OIL PRESSURE WAS 42 PSI, OIL TEMP 110 DEGREES CEL CIUS. SHUT OFF ENGINE, ENGINE WINDMILLED FOR TEN MINUTES WITH OIL PRESSURE AT 42-43 PSI. REMOVED AND REPLACED RIGHT ENGI NE LOW OIL PRESSURE WARNING SWITCH, REF 78-32-1. INSPECTED ENGINE OIL FILTER AND CHIP DETECTORS AND FOUND NO FOREIGN OBJ ECTS REF 72-00 (ENGINE WINDMILLING PROCEDURE). RAN ENGINE AND FOUND OIL PRESSURE AND TEMPERATURE TO BE GOOD, NO LEAKS NO TED. 2 L 7 2 4F 4 F A6WE E2EA 2001080900252 20010809 00252 WP 2001 8 9 MWEA011008 1 20010629 A 2133 20219741 ACTUATOR DOUG DC9 DC982 3022082 WP OUTFLOW VALVE FAILED A MWEA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 GL 31 810ME 48072 AFTER TAKE OFF UNABLE TO MAINTAIN CABIN PRESSURE. REPLACED OUTFLOW VALVE ACTUATOR. SYSTEM TESTED GOOD. 2 L 7 2 4F A6WE 2001080900253 20010809 00253 NM 2001 8 9 QXEA011300 1 20010801 A 2420 DH103024600CS2B INVERTER DHAV DHC8 DHC8102 2809003 NM DEFECTIVE A QXEA K NONE O OTHER CR CRUISE 1 NM 09 825PH 16448 213 GEG-ELECTRICAL SMELL NOTICED IN FLIGHT. REMOVED AND REPLACED INVERTER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERV ICE. 2 H 7 2 4T RT A13NM 2001080900254 20010809 00254 EU 2001 8 9 QXEA011301 1 20010802 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU INOPERATIVE A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 484US 11234 SEA-TWO EACH EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED CIRCUIT BOARDS ON BOTH FORWARD EXIT SIGNS. OPERATIONAL CHECKS GO OD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001080900255 20010809 00255 2001 8 9 MWEA011010 4 20010702 A 3422 2587794 FLUX DETECTOR DOUG DC9 DC981 3022081 WP RT WING FAILED A MWEA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 812ME 48006 DURING CLIMB OUT CAPTAIN HEADING FAILED. REPLACE FLUX VALVE. 2 L 7 2 4F A6WE 2001080900258 20010809 00258 WP 2001 8 9 MWEA011011 1 20010702 A 3260 HARNESS DOUG DC9 DC932 3022066 WP NLG DEFECTIVE A MWEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 31 301ME 47190 NO NOSE LANDING GEAR SAFE (GREEN EXTENDED) OR OTHER LIGHT OR VISUAL INDICATION. REMOVED AND REPLACED UP LIMIT SWITCH WIR ING HARNESS, CLEANED NOSE GEAR VIEWING COMPONENTS. 2 L 7 2 4F A6WE 2001080900259 20010809 00259 WP 2001 8 9 MWEA011012 1 20010707 A 5320 593643451 INTERCOSTAL DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 805ME 48031 INTERCOSTAL AT STATION 465-484 CRACKED. REPAIRED PER ASB A53-188 FIGURE 1. 2 L 7 2 4F A6WE 2001080900260 20010809 00260 WP 2001 8 9 MWEA011013 1 20010707 A 5330 593643451 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 805ME 48031 FUSELAGE SKIN UNDER LOWER VHF ANTENNA CRACKED. INSTALLED DOUBLER PER ASB A53-188 FIGURE 1. 2 L 7 2 4F A6WE 2001080900261 20010809 00261 WP 2001 8 9 MWEA011049 1 20010716 A 5754 99234022 RIB DOUG DC9 DC932 3022066 WP L/E SLAT CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 RIGHT WING NR 1 SLAT INBOARD IDLER TRACK, OUTBOARD RIB HAS EXFOLIATION CORROSION AROUND TRACK DOOR FORWARD HINGE BOSS. R EMOVED CORROSION, DRILLED NEW INBOARD AND OUTBOARD IDLER TRACK RIBS, INSTALLED NEW INBOARD AND OUTBOARD IDLER TRACK RIBS . LEVEL 2 CORROSION. 2 L 7 2 4F A6WE 2001080900262 20010809 00262 2001 8 9 MWEA011051 4 20010704 A 2565 100502121 SLIDE DOUG DC9 DC982 3022082 WP SERVICE DOOR MALFUNCTIONED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 EVACUATION SLIDE ON AFT SERVICE DOOR WAS INFLATED BUT DID NOT DEPLOY. AIRCRAFT FERRIED TO MILWAUKEE AND SLIDE REPLACED. 2 L 7 2 4F A6WE 2001080900264 20010809 00264 WP 2001 8 9 MWEA011052 1 20010717 A 5730 99117731 SKIN DOUG DC9 DC914 3022034 WP LT WING DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 LEFT WING LEADING EDGE HAS EIGHT DENTS BETWEEN XRS 214-267. REMOVED DAMAGED AREAS, FABRICATED AND LOCATED EXTERNAL DOUBL ER, FABRICATED INTERNAL FILLER AND DOUBLER, LOCATED AND DRILLED INTERNAL FILLERS AND DOUBLER, INSTALLED EXTERNAL DOUBLER . 2 L 7 2 4F A6WE 2001080900265 20010809 00265 EU 2001 8 9 MALA010637 1 20010724 A 5310 SEAT TRACK SAAB SF340 340B 7860101 EU A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 436XJ 340B436 Found during 4K-check, LH Center Aisle Seat Track LBL 18.3 has corrosion that is out of limits at approximately Sta 299. Maintenance c/w EO S53060 on Left Center Aisle Seat Track. From Fuselage Sta 297 to approximately Fuslage Sta 377. 2 L 7 2 4T RT A52EU 2001080900266 20010809 00266 NM 2001 8 9 USAA010760 1 20010630 A 5330 SKIN BOEING 737 737301 1384611 NM BS 727E CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 337US 43789 23235 CLT - FOUND SKIN CRACKED 2 INCHES, BS 727E, STRINGER 22R AND 23R. DAMAGE REMOVED, REPAIR DOUBLER AND TRIPLER INSTALLED PER EA 71604. (M) 2 L 7 2 4F RT A16WE 2001080900267 20010809 00267 NM 2001 8 9 USAA010761 1 20010622 A 5200 SKIN BOEING 737 737401 1384701 NM CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 35767 23985 CLT - FOUND AFT CARGO DOOR SKIN CRACKED .5 INCH, HANDLE CUTOUT, AFT UPPER CORNER. DAMAGE REMOVED, INSTALLED REPAIR DOUB LER PER SRM 52-30-03. (M) 2 L 7 2 4F RT A16WE 2001080900268 20010809 00268 NM 2001 8 9 USAA010762 1 20010621 A 5300 SKIN BOEING 737 737401 1384701 NM BS 294.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 35767 23985 CLT - FOUND FUSELAGE SKIN CRACKED .75 INCH, BS 294.5, MED LOWER HINGE CUTOUT. INSTALLED REPAIR DOUBLER PER SRM 53-10-01 , FIG 205. (M) 2 L 7 2 4F RT A16WE 2001080900269 20010809 00269 NM 2001 8 9 USAA010763 1 20010628 A 5300 SKIN BOEING 737 7374B7 1384702 NM BS 727D CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 429US 34226 24551 CLT - FOUND SKIN CRACKED 1.5 INCH, BS 727D, STRINGER 23R. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 5 3-60-03. (M) 2 L 7 2 4F RT A16WE 2001080900270 20010809 00270 NM 2001 8 9 USAASB01209 1 20010719 A 2700 2061141 INDICATOR BOEING 737 7374B7 1384702 NM FLIGHT COMPT FAILED A USAA O OTHER F FLT CONT AFFECTED DE DESCENT 1 EA 19 439US 42101 24781 CLT - FLT 1528 - IN PREPARATION FOR LANDING AT CLT, FROM MIA, THE TRAILING EDGE FLAPS FAILED TO EXTEND WHEN SELECTED. T HE LEADING EDGE DEVICES DID DEPLOY TO FULL EXTEND. THE FLAP POSITION INDICATOR SHOWED A SMALL SPLIT AT ONE UNIT AND THE TRAILING EDGE CIRCUIT BREAKER WAS FOUND TRIPPED. C REW ACCOMPLISHED QUICK REF HANDBOOK PROCEDURES, DECLARED AN EMERGENC Y AND DETERMINED IT WAS SAFE TO LAND IN FLAP CONFIGURATION. FLIGHT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE. MAI NTENANCE INSPECTED AND OPERATED TRAILING EDGE FLAPS IN NORMAL AND ALTERNATE MODES. PERFORMED OPERATIONAL TEST OF ASYMME TRY SYSTEM AND FOUND THE FLAP POSITION INDICATOR STUCK ON ONE UNIT REGARDLESS OF FLAP POSITION. REPLACED INDICATOR PER 2 L 7 2 4F RT A16WE 2001080900271 20010809 00271 NM 2001 8 9 USAA010849 1 20010629 A 5300 ANGLE BOEING 737 737301 1384611 NM BS 294.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 576US 43413 23741 PIT - FOUND ANGLE CRACKED 3 INCHES, STATION 294.5 RIGHT WL 208.1 CREASE BEAM TO FLOOR STRUCTURE. REPLACED ANGLE PER T/R . (M) 2 L 7 2 4F RT A16WE 2001080900272 20010809 00272 NM 2001 8 9 USAA010848 1 20010625 A 5300 BEAM BOEING 737 737301 1384611 NM BS 208.1 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 576US 43413 23741 PIT - FOUND BEAM CORRODED IN THREE AREAS 1 INCH BY 1 INCH, STATION 208.1 RIGHT UNDER GALLEY NR 1. CORROSION LEVEL 1, TA SK NR C53-107-01. CLEANED AND TREATED PER C/N 53-46-53500-C-005. (M) 2 L 7 2 4F RT A16WE 2001080900273 20010809 00273 NM 2001 8 9 USAA010854 1 20010628 A 5300 ANGLE BOEING 737 737301 1384611 NM BS 270 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 576US 43413 23741 PIT - FOUND ANGLE CORRODED 1 INCH BY 18 INCH AREA, FORWARD SIDE FLOORBEAM STATION 270, WL 207.5 COCKPIT ENTRANCE. CORRO SION LEVEL 1, TASK NR C53-107-01. REMOVED CORRODED HORIZONTAL FLANGE FROM Z-CHORD, REPLACED WITH REPAIR ANGLE PER EA 71 097. (M) 2 L 7 2 4F RT A16WE 2001080900274 20010809 00274 NM 2001 8 9 USAASB01211 1 20010722 A 3350 1000679 LIGHT BOEING 737 737201 1384454 NM PAX CABIN FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 245US 22751 LGA - THE AFT SERVICE DOOR EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. (M) 2 L 7 2 4F A16WE 2001080900275 20010809 00275 WP 2001 8 9 USAAD01137 1 20010725 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 828US 48028 IND - SEVERAL LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001080900276 20010809 00276 NM 2001 8 9 USAA010868 1 20010718 A 5300 SKIN BOEING 737 737201 1384454 NM CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 255AU 50988 22797 CLT - FOUND UPPER WING SKIN CRACKED .25 INCH, LEFT WING WBL 165.5 AT REAR SPAR, BS 178. INSTALLED DOUBLER AND TRIPLER P ER EA 85075. (M) 2 L 7 2 4F A16WE 2001080900277 20010809 00277 NM 2001 8 9 USAA010864 1 20010718 A 5300 SKIN BOEING 737 737201 1384454 NM BS 303 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 255AU 50988 22797 CLT - FOUND SKIN CRACKED .0625 INCH, BS 303, WL 259.88 MED UPPER HINGE CUTOUT. INSTALLED REPAIR DOUBLER PER SRM 53-30-3 AND EA 85093. (M) 2 L 7 2 4F A16WE 2001080900278 20010809 00278 NM 2001 8 9 USAA010768 1 20010705 A 5300 FRAME BOEING 757 757225 1384959 NM BS 1540 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 54141 22198 CLT - FOUND FRAME DENTED .5 INCH DIAMETER, BS 1540, OUTBOARD OF S26L. DAMAGE REMOVED, FABRICATED AND INSTALLED DOUBLER AND STRINGER TIE CLIPS PER TR 53-60-01, AND EA 69860. (M) 2 L 7 2 4F RT A2NM 2001080900279 20010809 00279 NM 2001 8 9 USAA010769 1 20010705 A 5300 SKIN BOEING 757 757225 1384959 NM BS 902 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND SKIN PREVIOUSLY INSTALLED DOUBLER, BS 902, S3R. DOUBLER INSTALLED PER SRM 53-00-01, FIG 203. (M) 2 L 7 2 4F RT A2NM 2001080900280 20010809 00280 NM 2001 8 9 USAA010770 1 20010705 A 5400 CHANNEL BOEING 757 757225 1384959 NM BS 310.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 54141 22198 CLT - FOUND CHANNEL CRACKED .75 INCH, BS 310.5, LBL 20, FORWARD SIDE OF FLOORBEAM. REMOVED AND REPLACED PER SRM 51-40-0 2. (M) 2 L 7 2 4F RT A2NM 2001080900281 20010809 00281 NM 2001 8 9 USAA010771 1 20010705 A 5300 TIE CLIP BOEING 757 757225 1384959 NM BS 1620 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 54141 22198 CLT - FOUND TIE CLIP CRACKED IN TWO PLACES .5 INCH EACH, BS 1620, S18R. REMOVED AND REPLACED TIE CLIP PER SRM 51-40-00. (M) 2 L 7 2 4F RT A2NM 2001080900282 20010809 00282 NM 2001 8 9 USAA010772 1 20010705 A 5300 SKIN BOEING 757 757225 1384959 NM BS 423 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 54141 22198 CLT - FOUND FUSELAGE SKIN WITH PREVIOUSLY INSTALLED DOUBLER 2.5 INCHES BY 3 INCHES, BS 423, BETWEEN S16L AND S17L. DOUB LER INSTALLED PER SRM 53-00-01, FIG 206. (M) 2 L 7 2 4F RT A2NM 2001080900283 20010809 00283 NM 2001 8 9 USAA010773 1 20010705 A 5300 SKIN BOEING 757 757225 1384959 NM BS 1620 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 54141 22198 CLT - FOUND FUSELAGE SKIN WITH PREVIOUSLY INSTALLED DOUBLER 8.5 INCHES BY 11.5 INCHES, BS 1620, BETWEEN S17L AND S19L. DOUBLER INSTALLED PER EA 66107-A, SRM 53-60-01 FIG 101 AND 53-00-01 FIG 204. (M) 2 L 7 2 4F RT A2NM 2001081000076 20010810 00076 EU 2001 8 10 C2XA01IA316 1 20010809 A 3350 0341516 FUSE AEROSP ATR42 ATR42320 8680930 EU CABIN BLOWN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 42836 200 IAH - DURING MAINTENANCE INSPECTION, THE EMERGENCY FLOOR LIGHTING AT SEAT 2B WAS FOUND TO BE INOPERATIVE, MAINTENANCE RE MOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY FUSE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001081000077 20010810 00077 EU 2001 8 10 C2XA01IA317 1 20010804 A 3350 0341516 FUSE AEROSP ATR42 ATR42320 8680930 EU CABIN BLOWN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14815 104 IAH - FLIGHT 4079, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT SEVERAL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTE NANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY FUSE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO S ERVICE. 2 H 7 2 4T RT A53EU 2001081000078 20010810 00078 SO 2001 8 10 C2XA01IA318 1 20010810 A 3350 D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203 SO CABIN DAMAGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16723 120169 IAH - DURING MAINTENANCE INSPECTION, SEVERAL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPL ACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001081000079 20010810 00079 SO 2001 8 10 C2XA01IA319 1 20010810 A 3350 BS2197 BATTERY PACK EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16723 120169 IAH - DURING MAINTENANCE INSPECTION, SEVERAL EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001081000080 20010810 00080 WP 2001 8 10 MWEA010996 1 20010618 A 2420 914F5674 RELAY DOUG DC9 DC981 3022081 WP ART INOPERATIVE A MWEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 31 807ME 48033 ON TAKE OFF ROLL AS POWER INCREASED SOUNDED LIKE RELAYS SWITCHING AND A.R.T. ACTIVATED. VERIFIED MOMENTARY BUS SWITCHING ACTIVATED A.R.T. REPLACED RIGHT GENERATOR RELAY. 2 L 7 2 4F A6WE 2001081000081 20010810 00081 WP 2001 8 10 MWEA011009 1 20010701 A 3260 CONTROL CABLE DOUG DC9 DC915 3022036 WP LANDING GEAR OUT OF RIG A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 900ME 45841 UNABLE TO RAISE LANDING GEAR AFTER TAKE OFF UNABLE TO TURN NOSE WHEEL AND NO AUTO PRESSURIZATION INITIALLY BUT IT STARTE D WORKING 15 MINUTES INTO FLIGHT. RIGGED GROUND SENSING CABLES. 2 L 7 2 4F A6WE 2001081000086 20010810 00086 2001 8 10 GTIA010660 4 20010715 A 2565 D29982113 SLIDE DOUG DC9 DC982 3022082 WP L1 DOOR DEFECTIVE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FLL - FLT 171 - L1 SLIDE PACK CAME APART WHEN OPENING AIRCRAFT DOOR. REMOVED AND REPLACED L1 SLIDE ASSEMBLY IAW MM 25-6 2-00. (M) 2 L 7 2 4F A6WE 2001081000089 20010810 00089 WP 2001 8 10 P2EA01134 1 20010721 A 3230 DOOR LATCH DOUG DC9 DC987 3022087 WP LT MLG OUT OF ADJ A P2EA K NONE N FALSE WARNING AP APPROACH 1 CE 05 132NJ 49780 FLT 154 - LGA - UPON REAR RETRACTION THE LEFT MAIN GEAR TRANSIT/POSITION LIGHT REMAINED ILLUMINATED. RECYCLED LANDING G EAR PER QRH, LIGHT REMAINED ILLUMINATED. COMPLIED WITH ALL QRH PROCEDURES AND LIMITATIONS CONTINUED FLIGHT. ADJUSTED A ND SHIMMED THE LEFT MAIN GEAR DOOR LATCH MECHANISM AND SWUNG GEAR IAW AIRCRAFT MM 32-31-04. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 2001081000094 20010810 00094 NM 2001 8 10 P2EA01137 1 20010722 A 2130 VALVE BOEING 737 737230 NM CABIN PRESSURE FAILED A P2EA O OTHER O OTHER DE DESCENT 1 CE 05 124NJ 22122 FLT 940 - MCI - ON DESCENT TO 12,000 FEET POWER AT IDLE, CABIN NI 700 FEET DESCENT. WHEN ADVANCING POWER AT 12,000 TO 1 .3 EPR CABIN SHOWED DESCENT OF 2000 FEET WITH NOTICEABLE PRESSURE CHANGE IN OUR EARS. IN DESCENT TO 12,000 FEET WITH PO WER AT IDLE SHOWED 400 FEET CLIMB AND WHEN ADVANCED TO 1.1 EPR WENT TO 1000 FEET DESCENT THEN STABILIZED AT 500-700 FOOT DESCENT. KEPT POWER UP FOR REMAINDER OF FLIGHT. REMOVED AND REPLACED NR 2 ENGINE MOD VALVE P/N 392716-1-1 AND NR 1 EN GINE BLEED AIR SHUTOFF VALVE P/N 67-2905-001 AND REPLACED FLEX LINE AT THE 450 DEGREE SENSOR AS138-04-0084. COMPRESSION AND PRESSURIZATION OPS CHECKED NORMAL. (M) 2 L 7 2 4F RT A16WE 2001081000095 20010810 00095 NM 2001 8 10 USAA010759 1 20010624 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 590US 43303 23935 CLT - FOUND SKIN CRACKED 1.25 INCH, BS 727D, STRINGER 23R. DAMAGE REMOVED,INSTALLED REPAIR DOUBLER PER SRM 53-00-01, FI G 202. (M) 2 L 7 2 4F RT A16WE 2001081000096 20010810 00096 NM 2001 8 10 USAA010774 1 20010705 A 5312 PRESSURE PANEL BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 31193 24811 CLT - FOUND PRESSURE WEB HAS 10 CRACKS, SMALLEST IS .150 INCH, LARGEST IS 1.7 INCH, BS 178 WL 188 TO 213, BETWEEN RBL 6. 5 AND LBL 10. DAMAGE REMOVED, DOUBLER AND FILLERS INSTALLED PER EO 5300V153 AND SRM 53-10-08, FIG 211. (M) 2 L 7 2 4F RT A16WE 2001081000097 20010810 00097 NM 2001 8 10 USAA010775 1 20010705 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 31195 24811 CLT - FOUND SIDE CHORD CRACKED TWO PLACES .9 INCH BY 1.6 INCH, BS 178, WL 207, RBL 28 AND LBL 28. DAMAGE REMOVED, SPLIC ED IN NEW CHORD SECTION PER EO 5300V157. (M) 2 L 7 2 4F RT A16WE 2001081000098 20010810 00098 NM 2001 8 10 USAA010781 1 20010709 A 5315 FLOORBEAM BOEING 767 767201 1385125 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 646US 57991 23898 CLT - FOUND FLOORBEAM CORRODED 3 INCHES BY 4 INCHES, BS 287, RBL 64. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER EA 85 042. (M) 2 L 7 2 4F RT A1NM 2001081000099 20010810 00099 NM 2001 8 10 USAA010792 1 20010710 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 24811 CLT - FOUND FLOORBEAM CORRODED 2 INCH BY 18 INCH AREA, BS 947 LBL 12 TO RBL 6. DAMAGE REMOVED, REPLACED T-CAP PER TYPIC AL REPAIR 53-60-02. (M) 2 L 7 2 4F RT A16WE 2001081000100 20010810 00100 NM 2001 8 10 USAA010793 1 20010710 A 5320 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 31193 24811 CLT - FOUND Z-ANGLE CORRODED 2 INCH BY 40 INCH AREA, BS 947 TO 987, LBL 52 AT AFT ENTRY DOOR. REMOVED AND REPLACED Z-AN GLE PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001081000101 20010810 00101 NM 2001 8 10 USAA010794 1 20010710 A 5320 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 31193 24811 CLT - FOUND Z-ANGLE CORRODED 2 INCH BY 53 INCH AREA, BS 947 TO 1000, AFT SERVICE DOOR. REMOVED AND REPLACED Z-ANGLE PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001081000102 20010810 00102 NM 2001 8 10 USAA010795 1 20010710 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 31193 24811 CLT - FOUND FLOORBEAM CORRODED 2 INCH BY 90 INCH AREA, BS 987, DOOR TO DOOR. REMOVED AND REPLACED FLOORBEAM T-CAP PER T YPICAL REPAIR 53-60-01. (M) 2 L 7 2 4F RT A16WE 2001081000103 20010810 00103 NM 2001 8 10 USAA010796 1 20010710 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 31193 24811 CLT - FOUND FLOORBEAM CORRODED 24 INCH AREA, BS 344, LBL 12 TO RBL 12. DAMAGE REMOVED, REPLACED T-CAP SECTION PER SRM 5 3-10-51. (M) 2 L 7 2 4F RT A16WE 2001081000104 20010810 00104 NM 2001 8 10 USAA010815 1 20010624 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 30946 24781 PIT - FOUND BEAM T-CAP CORRODED 2 INCH BY 29 INCH AREA, BEAM 312 BETWEEN LBL 10 AND RBL 19. CORROSION LEVEL 1, TASK NR C53-107-02. REPLACED SECTION OF T-CAP, TREATED AND PRIMED PER SRM 53-10-51, 51-40-02. (M) 2 L 7 2 4F RT A16WE 2001081000105 20010810 00105 NM 2001 8 10 USAA010816 1 20010624 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 30946 24781 PIT - FOUND T-CAP CORRODED 2 INCH BY 62 INCH AREA, BEAM 328 BETWEEN B10 AND RBL 62. SPLICED IN SECTION OF UPPER CHORD, TREATED, PRIMED, SEALED PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2001081000106 20010810 00106 NM 2001 8 10 USAA010817 1 20010624 A 5320 STRAP BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 30946 24781 PIT - FOUND FLOOR SUPPORT STRAP CORRODED 16 INCHES BY 3 INCHES UPPER SURFACE, STATION 328-344. CORROSION LEVEL 1, TASK NR C53-107-02. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2001081000107 20010810 00107 EU 2001 8 10 SABA010037 1 20010810 A 3350 311701 BATTERY BAG JETSTM JETSTM3201 1500217 EU CABIN DISCHARGED A SABA D RETURN TO BLOCK Z SIGNIFICANT FAILURE REPORT IN INSP/MAINT 1 SO 33 959AE 959 Aircraft 959 on flight 5010 from CLT TO SOP. At departure time the emergency lights failed to test. No emergency decla red. Maintenance removed and replaced no 3 and no 4 emergency light battery. Ops check good. Aircraft retuned to serv ice. 2 L 7 2 4T RT A56EU 2001081000109 20010810 00109 NM 2001 8 10 USAA010818 1 20010624 A 5320 SUPPORT BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 30946 24781 PIT - FOUND GALLEY SUPPORT CORRODED, 3 INCH BY 15 INCH AREA, STATION 338 RBL 47 TO RBL 62. (M) 2 L 7 2 4F RT A16WE 2001081000111 20010810 00111 NM 2001 8 10 USAA010825 1 20010624 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 30946 24781 PIT - FOUND FLOORBEAM CORRODED 32 INCH AREA, Z-ANGLE AFT FORWARD ENTRANCE FROM FLOORBEAM. (M) 2 L 7 2 4F RT A16WE 2001081000113 20010810 00113 NM 2001 8 10 USAA010851 1 20010628 A 5347 SEAT TRACK BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 576US 43413 23741 PIT - FOUND SEAT TRACK CORRODED 3 INCHES BY 6 INCHES, NR 2 GALLEY SEAT TRACK STATION 328 AFT. (M) 2 L 7 2 4F RT A16WE 2001081000115 20010810 00115 NM 2001 8 10 USAA010852 1 20010628 A 5347 SEAT TRACK BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 576US 43413 23741 PIT - FOUND SEAT TRACK CORRODED 3 INCH BY 6 INCH, NR 2 GALLEY MIDDLE SEAT TRACK STATION 328 GOING AFT. (M) 2 L 7 2 4F RT A16WE 2001081000118 20010810 00118 NM 2001 8 10 USAA010853 1 20010529 A 5347 SEAT TRACK BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 576US 43413 23741 PIT - FOUND SEAT TRACK CORRODED 3 INCHES BY 6 INCHES, NR 2 GALLEY OUTBOARD SEAT TRACK STATION 328 GOING AFT. (M) 2 L 7 2 4F RT A16WE 2001081000119 20010810 00119 NM 2001 8 10 USAA010859 1 20010613 A 5320 BEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 576US 43413 23741 PIT - FOUND BEAM CORRODED 1 INCH BY 36 INCH AREA, BS 986.6. CORROSION LEVEL 1. REPAIRED PER TR 53-10-05, BAC 1505-1008 80. (M) 2 L 7 2 4F RT A16WE 2001081000121 20010810 00121 NM 2001 8 10 USAA010860 1 20010613 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 576US 43413 23741 PIT - FOUND BEAM CORRODED 1 INCH BY 4 INCHES, BS 967 UPPER T-CAP. CORROSION LEVEL 1. REPLACED PER 53-00-51. (M) 2 L 7 2 4F RT A16WE 2001081000123 20010810 00123 NM 2001 8 10 USAA010861 1 20010613 A 5320 6546812169 SUPPORT BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 576US 43413 23741 PIT - FOUND SUPPORT CORRODED 1 INCH BY 1 INCH, STATION 967-986 AND 18.25 RBL. CORROSION LEVEL 1. REPLACED WITH PART NR 65-46812-169. (M) 2 L 7 2 4F RT A16WE 2001081000124 20010810 00124 NM 2001 8 10 USAABB01067 1 20010720 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 617AU 27148 BWI - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 29 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLIES. (M) 2 L 7 2 4F RT A2NM 2001081000126 20010810 00126 NM 2001 8 10 USAABB01068 1 20010720 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 616AU 27147 CLT - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 6, 9, 23 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2001081000128 20010810 00128 NM 2001 8 10 USAABB01069 1 20010720 A 3350 8731002511REV14 SIGN BOEING 757 7572B7 1384964 NM R4 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 616AU 27147 CLT - FOUND L4 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE EXIT IDENTIFIER ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001081000129 20010810 00129 NM 2001 8 10 USAABB01070 1 20010721 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 614AU 27145 CLT - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 4 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001081000130 20010810 00130 NM 2001 8 10 USAABB01071 1 20010722 A 3350 20121 CHARGER BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 609AU 22205 BDL - FOUND EMERGENCY LIGHTS AT ROWS 9, 10, 12, 14, 18 AND THE L2 DOOR INOPERATIVE. MAINTENANCE REPLACED THE M733 BATTE RY CHARGER AND PACK. (M) 2 L 7 2 4F RT A2NM 2001081000131 20010810 00131 NM 2001 8 10 USAASB01210 1 20010720 A 3350 900835A POWER SUPPLY BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 255AU 22797 BWI - MAINTENANCE FOUND THE MID-CABIN OVERHEAD EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTER Y SUPPLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 2001081000132 20010810 00132 WP 2001 8 10 MWEA011061 1 20010723 A 5347 59305667 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 MODERATE CORROSION IN NR 4 SEAT TRACK FORWARD OF GALLEY MOUNT AT STATION 237. 2 L 7 2 4F A6WE 2001081000133 20010810 00133 WP 2001 8 10 MWEA011062 1 20010723 A 5320 992341718 FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 NR 4 SEAT TRACK SUPPORT FITTING AT STATION 905 IS CRACKED. 2 L 7 2 4F A6WE 2001081000134 20010810 00134 WP 2001 8 10 MWEA011063 1 20010723 A 5320 992341717 FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 NR 1 SEAT TRACK SUPPORT FITTING AT STATION 905 IS CRACKED. 2 L 7 2 4F A6WE 2001081000135 20010810 00135 WP 2001 8 10 MWEA011065 1 20010723 A 5347 59305667 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 EXFOLIATION CORROSION IN NR 2 SEAT TRACK AT FASTENER HOLE AT STATION 1268. 2 L 7 2 4F A6WE 2001081000136 20010810 00136 WP 2001 8 10 MWEA011067 1 20010720 A 2450 976J2544 CONTROL PANEL DOUG DC9 DC981 3022081 WP COCKPIT MALFUNCTIONED A MWEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 31 804ME 48030 AFTER ENGINE START LEFT GENERATOR DROPPED OFF LINE WITH A/C CROSS TIE LIGHT ON. GENERATOR AND CROSSTIE RESET. REPLACED L EFT GENERATOR CONTROL PANEL, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 2001081000137 20010810 00137 WP 2001 8 10 MWEA011068 1 20010724 A 5753 5930476502 SKIN DOUG DC9 DC982 3022082 WP T/E FLAP CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 SUSPECTED LIGHTENING STRIKE ON TOP OF RIGHT FLAP AT APPROXIMATELY STATION 251. CLEANED DIRT AND CORROSION, REMOVED DAMAG ED AREA, FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001081000138 20010810 00138 WP 2001 8 10 MWEA011069 1 20010724 A 5347 59305478 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 MODERATE CORROSION IN NR 3 SEAT TRACK FORWARD OF GALLEY MOUNT AT STATION 237. 2 L 7 2 4F A6WE 2001081000139 20010810 00139 WP 2001 8 10 MWEA011070 1 20010724 A 5347 59366631 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 AFT CARGO COMPARTMENT NUMEROUS AREAS OF LIGHT TO MODERATE CORROSION ON LEFT CARGO TRACK FROM STATION 1003 TO 1322. 2 L 7 2 4F A6WE 2001081000140 20010810 00140 WP 2001 8 10 MWEA011071 1 20010724 A 5347 5936663505 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 AFT CARGO COMPARTMENT RIGHT CARGO TRACK FROM STATION 1212 TO 1322 HAS AREAS OF LIGHT TO MODERATE CORROSION. 2 L 7 2 4F A6WE 2001081000141 20010810 00141 WP 2001 8 10 MWEA011072 1 20010724 A 5320 593666093 SPLICE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 AFT PIT LEFT CARGO TRACK SPLICE PLATE AT STATION 1221.5 NUMEROUS AREAS OF LIGHT TO MODERATE CORROSION. 2 L 7 2 4F A6WE 2001081000142 20010810 00142 NE 2001 8 10 MWEA011073 2 20010724 A 7200 ENGINE DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217C 52053 NE LEFT OVERTEMP A MWEA E ENGINE SHUTDOWN M OVER TEMP CL CLIMB 1 GL 31 807ME 48033 P725472D LEFT THROTTLE RESTRICTED EGT 650 DEGREES CELSIUS FOR APPROXIMATELY FIVE MINUTES. -- LEFT ENGINE REPLACED DUE TO OVER T EMP EGT. 2 L 7 2 4F 4 F A6WE E9NE 2001081000145 20010810 00145 WP 2001 8 10 MWEA011075 1 20010724 A 3260 3912891501 FITTING DOUG DC9 DC932 3022066 WP LT MLG WORN A MWEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 204ME 47680 DURING CLIMB 17,000 FEET, GEAR DOOR LIGHT CAME ON, SO MAINTENANCE CONTROL DIVERTED AIRCRAFT TO MILWAUKEE MAINTENANCE BAS E. REMOVED AND REPLACED LEFT AND RIGHT MAIN GEAR DOOR SENSORS, AND LEFT MAIN GEAR FITTING. 2 L 7 2 4F A6WE 2001081000163 20010810 00163 CE 2001 8 10 DEB2001F00000 1 20010628 A 5210 504301775 BOLT BEECH 300 300BEECH 1152930 CE PWA PT6 PT6A60A 52043 NE CABIN DOOR BROKEN B DEBR K NONE O OTHER IN INSP/MAINT 1 CE 03 391MT 4347 FA111 FOUND LATCH BOLT BROKEN WHILE ATTEMPTING TO OPEN THE CABIN DOOR. BREAK WAS IN THREADS. 2 L 7 2 4T 4 T A24CE E4EA 2001081000164 20010810 00164 2001 8 10 COMA0160575 4 20010808 A 2220 6229968001 ACTUATOR CNDAIR CL600 CL6002B19 EA EMPENNAGE FAULTY A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 814CA 2700 7387 BOTH YAW DAMPERS DROPPED OFF LINE DURING TAXI OUT, AIRCRAFT RETURNED TO THE GATE.REPLACED THE #2 YAW DAMPER LINEAR ACTUA TOR. 2 L 7 2 4F RT A21EA 2001081000165 20010810 00165 EA 2001 8 10 COMA0160576 1 20010808 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA CABIN BURNED OUT A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 420CA 7451 EMERGENCY LIGHT BY LAVATORY FOUND TO BE INOPERATIVE.REPLACED LIGHT BULB IN INOPERATIVE EMERGENCY LIGHT ASSEMBLY. 2 L 7 2 4F RT A21EA 2001081000168 20010810 00168 EA 2001 8 10 COMA0160579 1 20010808 A 5346 WEB CNDAIR CL600 CL6002B19 EA BEAM CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 975CA 11462 7150 CRACKS FOUND ON LEFT HAND AND RIGHT HAND LOWER WEBS OF ENGINE SUPPORT BEAM F.S. 625.30.REPAIRED LEFT HAND AND RIGHT HAND LOWER WEBS OF ENGINE SUPPORT BEAM I/A/W CANADAIR REO 601R-53-61-366 REV C. 2 L 7 2 4F RT A21EA 2001081000169 20010810 00169 NM 2001 8 10 USAA010758 1 20010621 A 5300 SKIN BOEING 757 7572B7 1384964 NM BS 700 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 623AU 26162 27244 CLT - FOUND SKIN WITH PREVIOUSLY INSTALLED REPAIR 8 INCH BY 8 INCH, BS 700, STRINGER 23R. REPAIR DOUBLER PER SRM 53-00- 01, FIG 203. (M) 2 L 7 2 4F RT A2NM 2001081000170 20010810 00170 SO 2001 8 10 ASOA01104 1 20010710 A 3350 D36604001 BATTERY EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 262AS 19697 120146 FLT 4962 - DURING GROUND INSPECTION IN DFW, CREW REPORTED EMERGENCY LIGHT NR 3 BATTERY IS NOT HOLDING A CHARGE. MAINTEN ANCE REMOVED AND REPLACED EMERGENCY BATTERY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001081000171 20010810 00171 SO 2001 8 10 ASOA01106 1 20010710 A 3397 M2275941249 WIRE EMB 120 EMB120ER 3260203 SO CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SO 11 639AS 120283 FLT 4228 - DURING GROUND INSPECTIN IN ATL, CREW REPORTED EMERGENCY EXIT SIGN AT ROW 1 DOES NOT ILLUMINATE. MAINTENANCE FOUND BROKEN WIRES ON EMERGENCY EXIT SIGN AND REPLACED THEM. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001081000172 20010810 00172 SO 2001 8 10 ASOA01107 1 20010712 A 3397 M2275941249 WIRE EMB 120 EMB120ER 3260203 SO CABIN DISCONNECTED A K NONE L NO TEST IN INSP/MAINT 1 SO 11 505AS 120279 DURING MAINTENANCE IN MCN, FORWARD SECTION OF EMERGENCY LIGHT TRACK HAD A WIRE DISCONNECTED. MAINTENANCE RECONNECTED EM ERGENCY LIGHT TRACK WIRE AND REPLACED EMERGENCY LIGHT LENS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001081000173 20010810 00173 NE 2001 8 10 ASOA01049S 2 20010428 A 7200 214C40183 SWITCH EMB 120 EMB120 3260201 SO PWA 118 PW118 NE COCKPIT INTERMITTENT A ASOA A E UNSCHED LANDING ENGINE SHUTDOWN Y ENGINE STOPPAGE CL CLIMB 1 SO 11 236AS 120049 115146 FLT 4063 - DURING CLIMB-OUT FROM ATL, AT APPROXIMATELY 15,000 MSL, AIRCRAFT EXPERIENCED LEFT ENGINE FLAME OUT. AIRCRAFT RETURNED TO AND LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE HYDROMECHANICAL UNIT. TEARDOWN REPORTS FROM PRECISION ELECTRONICS REVEAL THE ENGINE FAILURE WAS CAUSED BY THE COMBINATION OF A BAD 14K PRESSURE SWITCH AND OUT OF TOLERANCE CALIBRATION ON THE HMU. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 2001081000174 20010810 00174 NM 2001 8 10 USAA010865 1 20010707 A 5300 SKIN BOEING 737 7372B7 1384560 NM CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 51802 22881 CLT - FOUND FUSELAGE SKIN CRACKED, AFT END OF AIRSTAIR HANDLE CUTOUT. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-30 -03. (M) 2 L 7 2 4F A16WE 2001081000175 20010810 00175 NM 2001 8 10 USAA010880 1 20010715 A 5300 ANGLE BOEING 737 737201 1384454 NM BS 303.9 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 255AU 50988 22797 CLT - FOUND WEB ANGLE CRACKED 1.25 INCH, BS 303.9, STRINGER 10L. REMOVED AND REPLACED ANGLE PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2001081000176 20010810 00176 NM 2001 8 10 USAASB01215 1 20010727 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM FWD CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 523AU 23858 LGA - MAINTENANCE FOUND THE EMERGENCY LIGHT ABOVE THE FORWARD GALLEY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001081000177 20010810 00177 NM 2001 8 10 USAA010872 1 20010718 A 5300 STIFFENER BOEING 737 7373B7 1384580 NM BS 1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 45591 22957 TPA - FOUND STIFFENER CORRODED APPROXIMATELY 3 SQUARE INCHES, BS 1016, BETWEEN S28L AND S28R, AFT PRESSURE BULKHEAD. FO RMED SECTION REPAIR INSTALLED PER SRM 51-70-11, SRM 53-80-08, SB 737-53A-1075, AND EA 85096. (M) 2 L 7 2 4F RT A16WE 2001081000178 20010810 00178 NM 2001 8 10 AALA20011333 1 20010702 A 2500 OVEN BOEING 767 767223 1385123 NM F/C GALLEY DIRTY A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 320AA 22321 GLA - FLT 52 - EN ROUTE ORD-GLA, DETECTED SMOKE AT FIRST CLASS NR 2 GALLEY OVEN. PULLED CIRCUIT BREAKER. LANDED GLA WI THOUT FURTHER INCIDENT. REMOVED DEBRIS AT NR 2 OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001081000179 20010810 00179 NM 2001 8 10 AALA20011416 1 20010711 A 3350 SOCKET BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 354AA 24035 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT INOPERATIVE SEAT 24J. RECONNECTED SOCKET TO EMERGENCY LIGHT SEAT 24 J. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001081000180 20010810 00180 NM 2001 8 10 AALA20011418 1 20010715 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN LOOSE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 376AN 25445 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT INOPERATIVE SEAT 37H. REPAIRED LOOSE WIRE TO WALL/SEAT CONNECTOR FO R SEAT 37H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001081000181 20010810 00181 NM 2001 8 10 AALA20011428 1 20010716 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 21 379AA 25448 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING SEATS 3A AND 3B INOPERATIVE. REPLACED CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHTING SEATS 3A AND 3B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001081000182 20010810 00182 NM 2001 8 10 AALA20011431 1 20010716 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 352AA 24033 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHT SEAT 29H INOPERATIVE. RESEATED CONNECTOR TO EMERGENCY E SCAPE PATH LIGHT SEAT 29H. SYTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001081000183 20010810 00183 NM 2001 8 10 AALA20011430 1 20010716 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 352AA 24033 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTS SEAT 17H THROUGH 23H INOPERATIVE. RESEATED CONNECTOR T O BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001081000184 20010810 00184 NM 2001 8 10 AALA20011464 1 20010717 A 3350 LIGHT BOEING 777 777223 1385213 NM G3 GALLEY INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 794AN 30256 DFW - DURING OVERNIGHT MAINTENANCE, RIGHT FORWARD G3 GALLEY EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED RIGHT FORWARD G3 GALLEY EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001081000185 20010810 00185 2001 8 10 COMA0160580 4 20010808 A 3442 6229302003 ANTENNA CNDAIR CL600 CL6002B19 EA NOSE FAULTY A COMA K NONE O OTHER CL CLIMB 1 SO 01 767CA 1696 7285 DURING CLIMB OUT OF CVG THE WEATHER RADAR SYSTEM SEEMED TO BE INOPERATIVE WITH TILT SETTINGS HAVING NO IMPACT ON DISPLAY .REPLACED THE WEATHER RADAR RECEIVER/TRANSMITTER ANTENNA. 2 L 7 2 4F RT A21EA 2001081000186 20010810 00186 EA 2001 8 10 COMA0160581 1 20010808 A 3260 STRUT CNDAIR CL600 CL6002B19 EA A COMA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 960CA 7117 NOSE LANDING GEAR DISAGREEMENT AFTER TAKE OFF FROM TYS, AIRCRAFT RETURNED TO THE FIELD.PERFORMED FULL SERVICE OF THE NLG SHOCK STRUT TO ALLOW FULL EXTENSION OF STRUT UNDER A NO-LOAD CONDITION. 2 L 7 2 4F RT A21EA 2001081000188 20010810 00188 SO 2001 8 10 BSY2001F00005 1 20010709 A 3260 487862 DOWNLOCK SWITCH PIPER PA31 PA31350 7103110 SO RT MLG FAULTY E BSYA K NONE N FALSE WARNING AP APPROACH 1 GL 07 40978 318152199 (SDF) MIR GOING INTO SDF RIGHT MAIN GEAR, NO DOWN AND LOCK INDICATION. REMOVED AND REPLACED DEFECTIVE DOWN AND LOCK S WITCH. OPS CHECK GOOD. 1 L 7 2 3O A20SO 2001081000189 20010810 00189 CE 2001 8 10 BSY2001F00006 1 20010709 A 3260 327 LIGHT BEECH 58 58 1152740 CE CONT O520 IO520* 17032 SO COCKPIT INOPERATIVE D BSYA K NONE N FALSE WARNING AP APPROACH 1 GL 07 456WW TH444 PHL MIR RIGHT MAIN GEAR, NO DOWN AND LOCK INDICATION. REMOVED AND REPLACED DOWN AND LOCK BULB. OPS CHECK GOOD. 1 L 7 2 3O 3 O 3A16 E5CE 2001081000190 20010810 00190 CE 2001 8 10 MJ12001F00000 1 20010607 A 2810 S461 FLAPPER VALVE LEAR 35 35A 5170602 CE WING TIP TANK DEFECTIVE B MJ1R O OTHER K FLUID LOSS NR NOT REPORTED 1 EA 11 633DS 139 362 FLAPPER VALVE SEAL PN S-461 FOR LEFT AND RIGHT WING TIP TANKS WERE INSTALLED IAW SB 35/36-28-10 ON 02/19/01 AIRCRAFT HO URS 8,167.3 CUSTOMER ARRIVED AT OUR FACILITY ON 06/04/2001 AIRCRAFT HOURS 8306.9 WITH REPORTED DISCREPANCY AS FOLLOW: I NVESTIGATE TIP TANK FLAPPER VALVES BYPASSING FUEL. INVESTIGATION REVEALED LEFT AND RIGHT TIP TANK TO WING FLAPPER VALVE S FORWARD AND AFT POSITIONS PN S-461 WERE SWOLLEN AND DEFORMED PERMITTING FUEL FROM WING TO BYPASS INTO THE TIP TANKS. 2 L 7 2 4F A10CE 2001081000191 20010810 00191 2001 8 10 COMA0160582 4 20010808 A 2220 6229968001 ACTUATOR CNDAIR CL600 CL6002B19 EA EMPENNAGE FAULTY A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 814CA 2700 7387 BOTH YAW DAMPERS DROPPED OFF LINE DURING TAXI OUT, AIRCRAFT RETURNED TO THE GATE.REPLACED THE #2 YAW DAMPER LINEAR ACTUA TOR. 2 L 7 2 4F RT A21EA 2001081000192 20010810 00192 EU 2001 8 10 R7MR33372 1 20010504 A 6420 704A33633116 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR WORN A R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 96LG 467 2817 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM 1 EACH KIT PART NUMBER 355A091036-01 CORRECTED PROBLEM. 4 HALF SHELLS EQUALS 1 KIT. TRB SN LOCATED AT AEC SHOP UNDER RMH PO 2001-002957. THIS MMIR FOR HALF SHELLS BEING REPLACED UNDER AEC QUOTE 873-01. 1 G 7 1 3U 3 U H9EU E19EU 2001081000193 20010810 00193 EU 2001 8 10 R7MR33378 1 20010423 A 7931 DK040 TRANSMITTER BOLKMS 105 BO105CBS 5626008 EU OIL PRESSURE FAILED A R7MR O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 825LF 40 796 UNIT INOPERATIVE. OIL PRESSURE GAUGE PEGGED HIGH. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H3EU 2001081000194 20010810 00194 EU 2001 8 10 R7MR33387 1 20010327 A 6420 1053170023 BEARING BOLKMS 117 BK117A4 5626017 EU TAIL ROTOR WORN A R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 127HH 384 7060 WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2001081000196 20010810 00196 GL 2001 8 10 R7MR33420 2 20010607 A 7320 23072731 HMU BELL 407 407 SW ALLSN 250C 250C47B GL ENGINE FAILED A R7MR O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 911LN 411 53446 FADEC FAULT. LIGHT CAME ON DURING FLIGHT AND COULD NOT BE EXPLAINED, SO IT WAS OPTED TO REPLACE THE HMU. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2001081000197 20010810 00197 EU 2001 8 10 R7MR33447 1 20010119 A 6340 IPT20RT1100080G TRANSMITTER BOLKMS 117 BK117B1 5626012 EU MAIN ROTOR INOPERATIVE A R7MR O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 911VU 531 7141 UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2001081000198 20010810 00198 EU 2001 8 10 R7MR33448 1 20010119 A 6340 IPT20RT1100080G TRANSMITTER BOLKMS 117 BK117B1 5626012 EU MAIN ROTOR INOPERATIVE A R7MR O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 911VU 266 7141 UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2001081000199 20010810 00199 EU 2001 8 10 R7MR33457 1 20010201 A 5210 11724274101 GUIDE BOLKMS 117 BK117B1 5626012 EU PAX DOOR WORN A R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 71703 529 7227 WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2001081000200 20010810 00200 EU 2001 8 10 R7MR33459 1 20010116 A 2460 SP461310 SWITCH BOLKMS 117 BK117B1 5626012 EU DC SYSTEM WORN A R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 71703 656 7227 WORN BEYOND SERVICEABLE LIMITS. WILL NOT STAY IN CLOSED POSITION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2001081000201 20010810 00201 EU 2001 8 10 R7MR33477 1 20010525 A 6230 1051011305 BELLOWS BOLKMS 117 BK117B2 5626013 EU MAIN ROTOR TORN A R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 117BK 865 7229 BELLOWS IS TORN AROUND CLAMP AND FOLD AREAS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H13EU 2001081000202 20010810 00202 EU 2001 8 10 R7MR33479 1 20010501 A 7712 G555674 TRANSDUCER BOLKMS 117 BK117B1 5626012 EU ENGINE TORQUE INOPERATIVE A R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 10UM 377 7231 UNIT INOPERATIVE. GAUGE WENT TO -0-. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2001081000203 20010810 00203 2001 8 10 R7MR33480 4 20010525 A 2210 9910991 HEAD UROCOP EC135 EC135P1 8680990 EU REMOTE CONTROL INOPERATIVE A R7MR K NONE L NO TEST IN INSP/MAINT 1 NM 07 135N 44 0086 DISPLAY INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U O H88EU 2001081000204 20010810 00204 EU 2001 8 10 R7MR33481 1 20010418 A 2121 004B4128S FAN UROCOP EC135 EC135P1 8680990 EU COCKPIT INOPERATIVE A R7MR K NONE L NO TEST IN INSP/MAINT 1 NM 07 135N 115 0086 UNIT INOPERATIVE. RESISTOR UNIT HAS OPEN CIRCUIT FROM MIN AND MAX PINS TO THE FAN MOTOR PIN. FAN WILL NOT OPERATE AT L OW SETTINGS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U O H88EU 2001081000205 20010810 00205 SW 2001 8 10 R7MR33496 1 20010616 A 2121 ES731861 BLOWER BELL 407 407 SW ALLSN 250C 250C47B GL CABIN INOPERATIVE A R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 911LN 447 53446 UNIT INOPERATIVE. RUNS FOR A SHORT AMOUNT OF TIME THEN SHUTS DOWN. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2001081000206 20010810 00206 EU 2001 8 10 R7MR33498 1 20010710 A 2432 RG355 BATTERY SNIAS 350 AS350B2 8680813 EU DC SYSTEM DISCHARGED A R7MR K NONE L NO TEST IN INSP/MAINT 1 NM 07 93LG 434 2654 WILL NOT HOLD CHARGE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 2001081000207 20010810 00207 EU 2001 8 10 R7MR33508 1 20010604 A 6730 SC5084 SERVO SNIAS 350 AS350B2 8680813 EU MAIN ROTOR LEAKING A R7MR K NONE K FLUID LOSS IN INSP/MAINT 1 NM 07 102LN 954 3065 LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 2001081000208 20010810 00208 EU 2001 8 10 R7MR33509 1 20010601 A 2432 45043003 BATTERY BOX UROCOP EC135 EC135P1 8680990 EU DC SYSTEM INOPERATIVE A R7MR K NONE L NO TEST IN INSP/MAINT 1 NM 07 135SJ 1680 0054 UNIT INOPERATIVE. RECEIVED CODES 6,1, F AND R. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U O H88EU 2001081000209 20010810 00209 EU 2001 8 10 R7MR33510 1 20010601 A 2450 45023500 ELECTRICAL BOX UROCOP EC135 EC135P1 8680990 EU ELECTRICAL SYS CORRODED A R7MR O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 135SJ 0054 UNIT INOPERATIVE. FAULT CODES. CORRODED PC CARDS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U O H88EU 2001081000210 20010810 00210 SW 2001 8 10 R7MR33511 1 20010622 A 7714 407375008101 INDICATOR BELL 407 407 SW DUAL TACH DEFECTIVE A R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 407SJ 621 53422 UNIT INOPERATIVE. TACH STICKS IN SELF TEST MODE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U O H2SW 2001081000211 20010810 00211 SW 2001 8 10 R7MR33512 1 20010622 A 7714 407375008101 INDICATOR BELL 407 407 SW DUAL TACH INOPERATIVE A R7MR K NONE L NO TEST IN INSP/MAINT 1 NM 07 407SJ 53422 UNIT INOPERATIVE UPON INSTALLATION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U O H2SW 2001081000212 20010810 00212 2001 8 10 R7MR33514 4 20010529 A 3160 B19030MB01 DISPLAY SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT DEFECTIVE A R7MR K NONE N FALSE WARNING IN INSP/MAINT 1 NM 07 103LN 1050 3128 UNIT INOPERATIVE. FALSE ERROR CODES. SCREEN FLICKERS INTERMITTENTLY. INSTALLED SN COULD BE 552. REPLACED WITH NEW UN IT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2001081000213 20010810 00213 NE 2001 8 10 R7MR3390 2 20010609 A 7250 70BM041720 TURBINE SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE ENGINE FAILED A R7MR O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 103LN 318 3128 HIGH OIL CONSUMPTION (SMOKING). THIS IS THE SECOND OCCURRENCE FOR OIL CONSUMPTION. REPLACED WITH NEW UNIT, CORRECTED P ROBLEM. . 1 G 7 1 3U 3 U H9EU E00054EN 2001081000214 20010810 00214 CE 2001 8 10 YAD2001F00006 1 20010618 A 2822 RA5326 DIAPHRAGM LEAR BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA FUEL PUMP DAMAGED A YADA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 03 1566C 1930 B1525 UC36 PILOT FOUND FUEL LEAKING OUT OF NR 1 ENGINE DRAIN MANIFOLD. DETERMINED THAT THE DIAPHRAGM IN THE PUMP HAD FAILED AND AL LOWED FUEL TO DRAIN OUT OF THE DRAIN MANIFOLD. DUE TO THE COMMON FAILURE OF THE FUEL PUMP DIAPHRAGM (AND ASSOCIATED FUE L VENTING-SB71-3307) TO CORRECT PROBLEM WITH THE FUEL PUMP, INVESTIGATION REVEALED CUTS IN THE DIAPHRAGM CAUSED BY THE SHARP EDGES OF OF DIAPHRAGM PLATE PN RA5361 CREATED AT PRODUCTION. FAILURE OF DIAPHRAGM CAUSES FUEL TO BE DISCHARGED OU T OF THE VENT PORT OF THE PUMP PRESS REGULATOR AND OVERBOARD OR INTO THE ENGINE ACCESSORY AREA. EITHER DRAIN LOCATION C AN CREATE A FIRE HAZARD. 2 L 7 2 4T 4 T RT A24CE E4EA 2001081000215 20010810 00215 CE 2001 8 10 YAD2001F00007 1 20010618 A 2822 RA5326 DIAPHRAGM LEAR BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA FUEL PUMP LEAKING A YADA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 01 1566C 1930 B1525 UC36 PILOT FOUND FUEL LEAKING OUT OF NR 1 ENGINE DRAIN MANIFOLD. THIS AC IS IN COMPLIANCE WITH SB 71-3307 THAT INCORPORATED A DRAIN LINE FROM THE LOW PRESS FUEL PUMP TO THE DRAIN MANIFOLD. DETERMINED THAT DIAPHRAGM IN THE PUMP HAD FAILED AND A LLOWED FUEL TO DRAIN OUT OF DRAIN MANIFOLD. THE VENTED FUEL HAD COVERED THE LEFT MAIN LANDING GEAR WHEELS AND BRAKES. THIS COULD CAUSE FIRE HAZARD IF THE BRAKES BECAME HOT AND/OR SPARKED AFTER LANDING. DUE TO THE COMMON FAILURE OF THE FU EL PUMP DIAPHRAGM (AND ASSOCIATED FUEL VENTING). TO CORRECT PROBLEM WITH THE FUEL PUMP(SMOOTHING EDGES OF DIAPHRAGM PLA TE PN RA5361) AND RELOCATING THE PUMP DRAIN LINE TO THE ENG BREATHER LINE (VENTING OUT BEHIND THE GEAR WELL). 2 L 7 2 4T 4 T RT A24CE E4EA 2001081000217 20010810 00217 EU 2001 8 10 ZYWA100154 1 20010310 A 7931 9560137630 SWITCH AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE FAILED A ZYWA K NONE P NO WARNING INDICATION NR NOT REPORTED 1 GL 09 365SJ 3276 6018 FAILS TO ILLUMINATE LIGHT WHEN NO PRESSURE PRESENT, NO CONTACT. REMOVED AND REPLACED SWITCH. 1 G 7 2 3U 3 U H10EU E19EU 2001081000218 20010810 00218 NM 2001 8 10 2001F00166 1 20010723 A 3350 AMC02R03R CONNECTOR BOEING 757 757236 NM CABIN DISCONNECTED A N8TA K NONE L NO TEST IN INSP/MAINT 1 WP 19 545NA 29944 FOUND FLOOR ESCAPE PATH LIGHTING LENS MISSING AT ROW 12 AND AT ROW 25, LIGHT INOPERATIVE. AT ROW 12 REPLACED LENS, P/N 81000-22701. AT ROW 25 RECONNECTED CONNECTOR SYSTEM, OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2001081000219 20010810 00219 NM 2001 8 10 2001F00167 1 20010716 A 2913 3508806 PUMP BOEING 757 757200 1384950 NM NR 1 ENGINE FAILED A N8TA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 19 512NA 26962 NR 1 ENGINE EDP EICAS STATUS MESSAGE, LOW PRESSURE LIGHT AND STATUS MESSAGE POWER XFER CAME ON. AIRCRAFT RETURNED TO ST ATION, AN UNEVENTFUL LANDING WAS ACCOMPLISHED. REPLACED ENGINE DRIVEN HYDRAULIC PUMP, OPERATIONAL CHECK GOOD. POWER TR ANSFER UNIT OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2001081000220 20010810 00220 NM 2001 8 10 2001F00168 1 20010714 A 2110 692914 CHECK VALVE BOEING 727 727276 138408R NM CABIN PRESSURE STUCK A FX7A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 908PG 20951 FLT 990 - AIRCRAFT UNABLE TO PRESSURIZE IN AUTO OR NORMAL AFTER TAKEOFF. AIRCRAFT RETURNED TO MIAMI WITHOUT INCIDENT OR EMERGENCY. TROUBLESHOT AIRCRAFT PRESSURIZATION SYSTEM AND FOUND GROUND A/C CHECK VALVE LOOSE AND STUCK OPEN FROM GROUN D A/C ON ORIGINAL DEPARTURE FLIGHT. RESECURED AND LUBRICATED GROUND A/C CHECK VALVE. OPS CHECKED OK. AIRCRAFT RETURNE D TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2001081000221 20010810 00221 2001 8 10 2001F00170 4 20010709 A 3425 5223122012 ADI BOEING 727 727231 1384079 NM COCKPIT INOPERATIVE A FX7A A UNSCHED LANDING I FLT. ATTITUDE INST. CL CLIMB 1 SO 19 24343 21630 DURING CLIMB-OUT, NR 2 ADI BECAME INOPERATIVE. AIRCRAFT RETURNED TO MIAMI WITHOUT INCIDENT OR EMERGENCY. TROUBLESHOT T O FAULTY NR 2 ADI. REMOVED AND REPLACED ADI AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001081000222 20010810 00222 EU 2001 8 10 2001F00171 1 20010729 A 3244 TIRE AIRBUS 300 A300B4203 3930306 EU NLG DEFLATED A RJEF C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 23 68142 142 SAL - AT THE BEGINNING OF TAKEOFF ROLL OF FLT TA808, THE AIRCRAFT SLIPPED AND THE NOSE LANDING GEAR WHEELS WENT INTO THE GRASS RUNWAY. THE AIRCRAFT RETURNED TO THE CARGO AREA FOR MAINTENANCE WITHOUT OTHER INCIDENT. INSPECTION WAS PERFORME D PER AIRCRAFT MM 05-51-24. PHASE ONE WITH THE FOLLOWING RESULTS, NOSE WHEEL NR 2 WAS FOUND DEFLATED, BOTH WHEELS NR 1 AND NR 2 WERE REPLACED PER MM 12-37-32. ALSO, MAIN LANDING WHEEL NR 3 WAS FOUND WITH A CUT OUT OF LIMITS AND WAS REPLAC ED PER MM 12-37-32. NO OTHER DAMAGE WAS FOUND. THE AIRCRAFT STEERING WAS OPERATIONAL TESTED PER AIRCRAFT MM 32-51-00. NO ABNORMAL OPERATION WAS NOTED. (M) 2 L 7 2 4F RT A35EU 2001081000223 20010810 00223 NM 2001 8 10 AALA20011415 1 20010710 A 2530 MS252575 INDICATOR BOEING 767 767323 1385205 NM GALLEY SHORTED A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 399AN 29606 ORD - FLT 42 - AFTER TAKEOFF, FIRST CLASS GALLEY POWER ON INDICATOR LIGHT SHORTED CAUSING SMOKE IN GALLEY. CIRCUIT BREA KER PULLED AND POWER TO GALLEY SECURED FOR DURATION OF FLIGHT. REPLACED FIRST CLASS GALLEY POWER ON INDICATOR LIGHT ASS EMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001081000224 20010810 00224 NM 2001 8 10 SPAA0100042 1 20010604 A 3350 900835A BATTERY BOEING 737 7372T4 1384492 NM DISCHARGED A SPAA O OTHER L NO TEST IN INSP/MAINT 1 WP 28 703S 22529 ACCOMPISHMENT OF PREFLIGHT CHECK FOUND OVERWING EMERGENCY EXIT LIGHT INTERMITTANT. REPLACED BATTERY PAC IAW BOEING MM 33 -51-81 OPS CHECK GOOD 2 L 7 2 4F A16WE 2001081000225 20010810 00225 NM 2001 8 10 AALA20011442 1 20010717 A 3350 LIGHT BOEING 777 777223 1385213 NM G3 GALLEY INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 794AN 30256 DFW - DURING OVERNIGHT MAINTENANCE, LEFT FORWARD EMERGENCY EXIT LIGHT AT G3 GALLEY INOPERATIVE. REPLACED LIGHT ASSEMBLY AT G3 GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001081000226 20010810 00226 NM 2001 8 10 AALA20011443 1 20010716 A 3350 1000679 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39356 24037 LAX - DURING OVERNIGHT MAINTENANCE, CREW EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHEC KED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001081000227 20010810 00227 NM 2001 8 10 AALA20011444 1 20010715 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 679AN 29589 MIA - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY ESCAPE PATH LIGHTS LAST ROW INOPERATIVE. REPLACED LIGHTS TO F IRST CLASS, LAST ROW EMERGENCY ESCAPE PATH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001081000228 20010810 00228 GL 2001 8 10 ASOA01108 2 20010713 A 7200 ENGINE AEROSP ATR72 ATR72 EU ALLSN AE300 AE3007A GL NR 2 FAILED A ASOA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 11 643AS 413 FLT 4171 - DURING FLIGHT FROM ATL-GNV, PILOT RECEIVED AN INTERMITTENT OIL PRESSURE LIGHT. PILOT DECLARED AN EMERGENCY A ND DIVERTED THE AIRCRAFT TO AYS. AIRCRAFT LANDED IN AYS WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RIGHT ENGIN E. THE NR 2 SCAVENGE OIL FILTER WAS FULL OF METAL. THE CAUSE CANNOT BE DETERMINED UNTIL THE ENGINE IS TORN DOWN. (M) 2 H 7 2 4T 4 F RT TE6CH 2001081000229 20010810 00229 EA 2001 8 10 ASOA01109 1 20010714 A 3397 64645 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SO 11 833AS 7246 FLT 4768 - DURING GROUND INSPECTION AT MYR, MAINTENANCE DISCOVERED 1 CABIN FLOOR PATH LIGHTING STRIP AT ROW 7 INOPERATIV E. MAINTENANCE REMOVED AND REPLACED TWO BROKEN CABLE ASSEMBLIES, ONE AT ROW 7 AND ONE AT ROW 13. OPERATIONAL CHECKS GO OD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2001081000230 20010810 00230 NM 2001 8 10 SPAA0100043 1 20010618 A 5230 SWITCH BOEING 737 7372T4 1384492 NM BENT A SPAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 703S 22529 ON CLIMB-OUT FROM RNO, AFT CARGO DOOR WARNING LIGHT ILLUMINATED. RETURNED TO RNO. INVESTIGATION REVEALED AFT CARGO DOOR TO BE CLOSED AND SECURED. PLACE ITEM ON MEL 52-3, DEPARTED RNO TO BOI. AFTER ARRIVAL IN BOI, ADJUSTED AFT CARGO DOOR WAR NING SWITCH. CLEARED MEL, PLACARDS REMOVED. 2 L 7 2 4F A16WE 2001081000231 20010810 00231 EU 2001 8 10 ASOA01111 1 20010721 A 3350 S9251338500000 CONTROL PANEL AEROSP ATR72 ATR72 EU COCKPIT FAULTY A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 530AS 453 FLT 4308 - DURING GROUND INSPECTION AT ATL, CREW OBSERVED EMERGENCY LIGHTS STAYED ON. THEN, WHEN EXTINGUISHED, THE LIGH TS WOULD NOT COME BACK ON. MAINTENANCE REMOVED AND REPLACED THE ANTI-ICE/SIGN PANEL ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT 2001081000232 20010810 00232 NE 2001 8 10 ASOA01112 2 20010722 A 7200 ENGINE EMB 120 EMB120 3260201 SO PWA 118 PW118 NE LEFT FAILED A ASOA A UNSCHED LANDING J X WARNING INDICATION ENGINE FLAMEOUT CR CRUISE 1 SO 11 236AS 120049 115146 FLT 4254 - DURING CRUISE FLIGHT FROM ILM TO ATL, THE LEFT ENGINE FAILED. AN EMERGENCY WAS DECLARED. AIRCRAFT DIVERTED TO AGS AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE. THE MRR REMAINS OPEN PENDING RESULTS OF TEARDOWN REPORT. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 2001081000233 20010810 00233 EU 2001 8 10 ASOA01113 1 20010722 A 3350 3011210 LIGHT AEROSP ATR72 ATR72 EU PAX DOOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 532AS 12169 458 DURING HANGAR MAINTENANCE IN MCN, EMERGENCY LIGHT ON PASSENGER DOOR STEP INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY STAIR LIGHT ASSEMBLY ON PASSENGER DOOR STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2001081000234 20010810 00234 NM 2001 8 10 USAA010767 1 20010705 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 54141 22198 CLT - FOUND FLOORBEAM CORRODED APPROXIMATELY 2 INCH AREA, BS 1320 RBL 62. DAMAGE REMOVED, REPAIR DOUBLER INSTALLED PER SRM 53-00-51, FIG 205. (M) 2 L 7 2 4F RT A2NM 2001081000236 20010810 00236 NM 2001 8 10 USAA010866 1 20010713 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 255AU 50988 22797 CLT - FOUND VERTICAL CHORD CRACKED .25 INCH, BS 178, LBL 5.7, WL 184. DAMAGE REMOVED, INSTALLED REPAIR ANGLES AND STRAP PER EO 5300V155. (M) 2 L 7 2 4F A16WE 2001081000237 20010810 00237 NM 2001 8 10 USAA010871 1 20010717 A 5320 FLOOR SUPPORT BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 45591 22957 TPA - FOUND FLOOR SUPPORT BEAM CORRODED 3 SQUARE INCH AREA, BS 807 PLUS 6, RBL 13.8, AFT CARGO. INSTALLED REPAIR DOUBLE R PER SRM 53-00-53 FIG 201. (M) 2 L 7 2 4F RT A16WE 2001081000238 20010810 00238 NM 2001 8 10 USAA010879 1 20010715 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 255AU 50988 22797 CLT - FOUND SIDE CHORDS WITH TWO CRACKS LEFT AND RIGHT .250 INCH, BS 178 WL 206 RBL 28 AND LBL 28. DAMAGE SECTION REMOV ED, SPLICED IN NEW CHORD SECTION PER EO 5300V157. (M) 2 L 7 2 4F A16WE 2001081000239 20010810 00239 NM 2001 8 10 SPAA0100044 1 20010807 A 3350 900542 CHARGER BOEING 737 7372T4 1384492 NM A SPAA O OTHER O OTHER IN INSP/MAINT 1 WP 28 703S 22529 PREFLIGHT CHECK FOUND CENTER AISLE CEILING EMERGENCY EXIT LIGHT INTERMITTANT. REPLACED BATTERY CHARGER IAW BMM 33-51-71, OPS CHECK GOOD. 2 L 7 2 4F A16WE 2001081000240 20010810 00240 NE 2001 8 10 USAABB01066 2 20010718 A 7324 1303M31G12 MANIFOLD BOEING 767 7672B7 1385107 NM GE CF6 CF680C2B2 30025 NE LT ENGINE LEAKING A USAA C ABORTED TAKEOFF K X FLUID LOSS ENGINE FLAMEOUT TO TAKEOFF 1 EA 19 653US 24894 695134 PIT - FLT 48 - ON TAKEOFF ROLL IN PIT, THE LEFT ENGINE REACHED 80 PERCENT N1 AND THEN FAILED. THE TAKEOFF WAS ABORTED A T 60 KNOTS. THE FLIGHT RETURNED TO THE GATE, WHERE IT WAS NOTED THAT FUEL WAS LEAKING FROM THE LEFT ENGINE. MAINTENANC E FOUND A FUEL PRESSURE MANIFOLD FAILED (FRACTURED AT THE B-NUT) FOR THE FUEL NOZZLE IN THE 9:30 POSITION (ALF). (M) 2 L 7 2 4F 4 F RT A1NM E13NE 2002020700074 20020207 00074 NE 2002 2 7 USAASA01037 2 20010720 A 7200 ENGINE AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE NR 1 FAILED A USAA F A ACTIVATE FIRE EXT. UNSCHED LANDING E A Y VIBRATION/BUFFET FLAME/FIRE ENGINE STOPPAGE CL CLIMB 1 EA 19 106US 1044 779573 JFK - FLT 6808 - EN ROUTE LGA-BOS, WHILE CLIMBING THROUGH FL080, FELT MULTIPLE COMPRESSION STALLS AND OBSERVED SHOTS OF FLAME FROM THE LEFT SIDE OF THE AIRCRAFT. THE NR 1 ENGINE THROTTLE WAS MOVED TO IDLE, HOWEVER, THE ENGINE INDICATED SHU TDOWN. THE FLIGHT DIVERTED TO JFK AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE ASSEMBLY AND THE N R 1 ENGINE FORWARD EXTINGUISHER BOTTLE. (M) 2 L 7 2 4F 4 F RT A28NM E2GL 2001081000241 20010810 00241 NE 2001 8 10 USAASB01204 2 20010716 A 7200 ENGINE BOEING 737 737301 1384611 NM GE CFM56 CFM56* 13802 NE NR 2 MALFUNCTIONED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING E M VIBRATION/BUFFET OVER TEMP CR CRUISE 1 EA 19 342US 23511 725745 MSY - FLT 239 - EN ROUTE FROM CLT-IAH - AT FL350, THE CREW FELT A JOLT AND THEN A NR 2 ENGINE VIBRATION ALONG WITH A RIS E IN EGT. FLIGHT ATTENDANT REPORTED SEEING A FLASH FROM THE NR 2 ENGINE. CREW SHUT DOWN THE NR 2 ENGINE, DECLARED AN E MERGENCY AND DIVERTED TO MSY WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS 20 MINUTES. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE ASSEMBLY. OPS CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F 4 F RT A16WE E2GL 2001081000242 20010810 00242 NM 2001 8 10 USAASB01214 1 20010725 A 3397 WIRE BOEING 737 7373B7 1384580 NM CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 EA 19 375US 22954 EWR - MAINTENANCE FOUND THE LOW LEVEL EMERGENCY ESCAPE PATH LIGHT, AT SEAT ROW 20, INOPERATIVE. MAINTENANCE FOUND A BRO KEN RED WIRE, AT SPLICE, UNDER SEAT ROW 20C. REMOVED AND REPLACED SPLICE. OPERATIONAL CHECK OF LIGHT GOOD. (M) 2 L 7 2 4F RT A16WE 2001081000243 20010810 00243 EU 2001 8 10 JBXA000315 1 20010808 A 7720 TAY65015 POWERPLANT FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAY65015 54557 NE OVERTEMP A JBXA A UNSCHED LANDING M OVER TEMP TO TAKEOFF 1 SO 05 110ML 11486 #1 ENGINE OVERTEMPERATURE/860 DEGREE'S FARENHEIT. CORRECTIVE ACTION: PERFORMED TAY SB 77-1454 IAW TAY 77-1454. CHANGE RE SISTOR AFROM CM TO CK. PERFORMED ACCEL AND DECELL CHECKS AND IGV SCHEDULING CHECK IAW TAY 71-00-00. 2 L 7 2 4F 4 F RT E25NE 2001081000244 20010810 00244 WP 2001 8 10 ZW0A0106602 1 20010809 A 3350 60030431 POWER SUPPLY DOUG DC9 DC983 3022083 WP B5-103 A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 976TW 53626 THE FORWARD OVERWING EMERGENCY EXIT LIGHTS STAYED ON WITH POWER OFF. REPLACED THE POWER SUPPLY. CHECK-C 11-8-00 STL. - -CLOSED-- 2 L 7 2 4F RT A6WE 2001081000245 20010810 00245 NM 2001 8 10 ZW0A0106603 1 20010809 A 3350 6100928 LAMP BOEING 767 7673Q8 NM SEE TEXT A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 636TW 30301 THE EGRESS LIGHTS AT SEATS 1HJ AND 44HJ WERE INOPERATIVE. REPLACED THE LAMP AT BOTH LOCATIONS. CHECK-C 1-7-01 LAX. -- CLOSED-- 2 L 7 2 4F RT A1NM 2001081000246 20010810 00246 NM 2001 8 10 F3LA200100099 1 20010808 A 3350 VARIOUS BATTERY BOEING 737 7372L9 1384497 NM A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 270FL 36 22733 PRIOR TO DEPARTURE, MAINTENANCE REPORTED OVERHEAD EXIT LOCATOR SIGN FOR OVERWING EMERGENCY EXITS, FIXED EXIT LIGHTS ON S IDE OF EMERGENCY EXITS AND EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. FERRIED AIRCRAFT TO DEN. REPLACED BATTERIES, PERFORMED OPERATIONAL TEST AND CHECKED OKAY. 2 L 7 2 4F RT A16WE 2001081000247 20010810 00247 EU 2001 8 10 RAIA00108008 1 20010809 A 6120 31057165 GOVERNOR JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE MCAULY 5JFR36 B5JFR36C1103 GL LEFT ENGINE FAILED A RAIA E ENGINE SHUTDOWN Z SIGNIFICANT FAILURE REPORT DE DESCENT 1 CE 03 550HK 9883 3905 41039 75018 951478 5403-RIC-LEFT ENGINE OVERSPEED, 105.9% ON DESCENT, WOULD NOT COME DOWN, CREW PERFORMED ENGINE SHUTDOWN, LANDED WITHOUT I NCEDENT. MAINTENANCE INSPECTED AND REPLACED THE LEFT ENGINE PROPELLER GOVERNOR, PERFORMED CHECK FLIGHT, SYSTEM OPERATED NORMALLY. 2 L 7 2 4T 4 T RT A41NM E18NE 6 C P15NE 2001081300001 20010813 00001 SO 2001 8 13 C2XA01IA321 1 20010810 A 4900 1165650 FUEL LINE EMB 120 EMB120ER 3260203 SO APU LOOSE A C2XA O OTHER O OTHER UK UNKNOWN 1 SW 27 16731 120190 IAH - FLIGHT 3301, THE CREW REPORTED A STRONG FUEL SMELL IN THE CABIN. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE RESECURED THE FUEL LINE ON THE APU FUEL PUMP.THE APU WAS OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WAS A PPROVED FOR RETUNRN TO SERVICE. THE DISCREPANCY REPEATED ON FLIGHT 3525. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT AND MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE APU OIL TO BE LOW. MAINTENANCE SERVICED THE APU OIL AND DETERMINED THA T THE FUMES WERE CAUSED BY THE APU AUTO SHUTDOWN. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001081300002 20010813 00002 SO 2001 8 13 C2XA01IA322 1 20010810 A 3350 20131A BATTERY PACK EMB 145 EMB145LR SO DISCHARGED A C2XA O OTHER L NO TEST IN INSP/MAINT 1 SW 27 13964 4744 145123 SLW - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE AISLE PATH LIGHTING AT ROW 11-12 WAS INOPERATIVE. THE AIR CRAFT WAS FERRIED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK. AND THE AIRCR AFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001081300003 20010813 00003 SO 2001 8 13 C2XA01IA323 1 20010809 A 2100 22045402 ACM EMB 120 EMB120ER 3260203 SO FROZEN A C2XA O OTHER O OTHER UK UNKNOWN 1 SW 27 16723 120169 EFD - FLIGHT 3517, THE CREW REPORTED A SMOKE LIGHT ON THE MAP WITH THE ASSOCIATED AURAL WARNING. FUMES WERE REPORTED, AN D THE PACKS WERE BLOWING HOT. THE AIRCRAFT LANDED AT EFD WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE NUMBER TWO PACK ON MEL 21-50-2/C CONTROL NUMBER 014549, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR FIL ED OPEN AWAITING FINAL FIX.... 2 L 7 2 4T RT A31SO 2001081300008 20010813 00008 WP 2001 8 13 ARWA0010803 1 20010807 A 7900 730376 SEAL DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE A ARWA E ENGINE SHUTDOWN K FLUID LOSS AP APPROACH 1 SO 19 802BN 45909 671379 LOG PAGE 53334. DISCREPANCY: ON FINAL APPROACH SHUT DOWN #3 ENGINE DUE TO RAPID DROP IN OIL QUANTITY AND PRESSURE. CO RRECTIVE ACTION: REMOVED HOUSING AND SEAL FROM FUEL BOOST PUMP DRIVE ON # 3 ENGINE GEAR BOX. INSTALLED SEAL (SEAL P/N 730376) AND HOUSING TO FUEL BOOST PUMP DRIVE AND PACKING. REQUIRES RUN UP CHECK. 2 L 7 4 4F 4 F 4A25 1E8 2001081300009 20010813 00009 NM 2001 8 13 2001UALA00370 1 20010325 A 2742 251N20518 ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE HORIZ STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 HORIZONTAL STABILIZER TRIM ACTUATOR PRIMARY BRAKE FAILURE INSIDE UNIT. FOUND EXTREME CORROSION INSIDE AND OUTSIDE OF UNI T. BREAKDOWN OF GREASE DUE TO EXCESSIVE WATER INSIDE UNIT. REPLACED ACTUATOR. 2 L 7 2 4F 4 F RT A2NM E17NE 2001081300017 20010813 00017 NM 2001 8 13 2001UALA00929 1 20010528 A 7603 CONTROL CABLE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE THRUST LEVER OUT OF RIG A UALA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 29 614UA 21875 ENG LOW THRUST OTHER THAN TAKEOFF. FAULT CODED. L ENG EPR.04. (MCT-CLB FROM FL350 TO FL390 WITH THRUST LEVER FIREWALL. R EPLACED TRANSDUCER AND RIGGED THRUST CONTROL CABLE PER MM 2 L 7 2 4F 4 F RT A1NM E3NE 2001081300018 20010813 00018 NM 2001 8 13 2001UALA00944 1 20010604 A 3350 58791 RECEPTACLE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7275U 21422 FLOOR EEL STRIPS INOPERABLE. THE RECEPTACLE WAS DAMAGED. REPLACED RECEPTACLE CABLE EEL RECEPTACLE OPERATIONS CHECK NOR MAL. 2 L 7 3 4F 4 F A3WE E2EA 2001081300021 20010813 00021 2001 8 13 2001UALA00960 4 20010607 A 3422 25883024 GYRO BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE E/E BAY FAILED A UALA K NONE J WARNING INDICATION NR NOT REPORTED 1 WP 29 7261U 21408 CAPTAIN'S HSI DIRECTIONAL GYRO FLAG IN VIEW INTERMITTENTLY, THE DIRECTIONAL GYRO FAILED. REPLACED NR 1 DIRECTIONAL GYRO. OPERATION CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001081300038 20010813 00038 WP 2001 8 13 RRXA010058 1 20010717 A 3213 1710016CR0301 HOSE DOUG DC8 DC873F 302199F WP A RRXA O OTHER K FLUID LOSS LD LANDING 1 WP 15 602AL 45991 ON LANDING ROLL LOST HYD PRESS AND QTY *** CORRECTIVE ACTION *** FOUND HOSE ON R/H BOGIE TRIM CYL HAD SEPARATED FROM F ITTING- R AND R HOSE IAW 20-12-0 LK CK GOOD 2 L 7 4 4F RT 4A25 2001081300052 20010813 00052 WP 2001 8 13 AALA20011467 1 20010717 A 2400 976J2528 GENERATOR DOUG DC9 DC983 3022083 WP ENGINES DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 436AA 49454 MSP - FLT 1103 - EN ROUTE ORD-SEA - LEFT GENERATOR TRIPPED IN FLIGHT. RESET AND TRIPPED AGAIN AFTER FIVE MINUTES. AIR INTERRUPTED AND LANDED MSP WITHOUT INCIDENT. REPLACED LEFT AND RIGHT GENERATOR CONTROL UNITS. SYSTEM GROUND CHECKED NO RMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001081300053 20010813 00053 WP 2001 8 13 AALA20011449 1 20010719 A 3350 8034001 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 242AA 49255 DFW - DURING OVERNIGHT MAINTENANCE CEILING MOUNTED EMERGENCY EXIT LIGHT AT ROW 25 THROUGH 26 INOPERATIVE. REPLACED CEIL ING MOUNTED EMERGENCY EXIT LIGHT BATTERY PACK. SYTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001081300054 20010813 00054 WP 2001 8 13 AALA20011450 1 20010719 A 3350 TERMINAL DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 245AA 49257 DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS OVERHEAD EMERGENCY EXIT ESCAPE PATH LIGHTING INOPERATIVE. REPLACED TERM INAL ON BATTERY PACK TO FIRST CLASS EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001081300055 20010813 00055 WP 2001 8 13 AALA20011451 1 20010719 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 228AA 49178 DFW - DURING OVERNIGHT MAINTENANCE, CEILING MOUNTED EMERGENCY EXIT LIGHT AT ROW 13 THROUGH 16 INOPERATIVE. REPLACED CEI LING MOUNTED EMEREGNCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001081300056 20010813 00056 WP 2001 8 13 AALA20011454 1 20010722 A 3350 100105901 CHARGER DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 432AA 49350 DFW - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY LIGHTS AT SEAT ROW 9 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT C HARGER ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001081300057 20010813 00057 WP 2001 8 13 AALA20011455 1 20010722 A 3350 100105901 CHARGER DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 432AA 49350 DFW - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY LIGHTS AT SEAT ROW 25 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY CHARGER ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001081300058 20010813 00058 WP 2001 8 13 AALA20011456 1 20010722 A 3350 AB51 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 463AA 49593 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING FORWARD SECTION DIM. REPLACED EMERGENCY EXIT LIGHT BAT TERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001081300059 20010813 00059 WP 2001 8 13 AALA20011457 1 20010722 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 463AA 49593 DFW - DURING OVERNIGHT MAINTENANCE, CENTER OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED OVERHEAD EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001081300060 20010813 00060 EU 2001 8 13 AALA20011181 1 20010527 A 2500 OVEN AIRBUS 300 A300B4605R 3930308 EU F/C GALLEY DIRTY A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 14068 511 LHR - FLT 156 - EN ROUTE-LHR - DETECTED SMOKE AT FORWARD FIRST CLASS OVEN. TURNED OFF OVEN. LANDED LHR WITHOUT FURTHER INCIDENT. CLEANED FIRST CLASS OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2001081300061 20010813 00061 EU 2001 8 13 AALA20011200 1 20010604 A 5300 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FS 1923-2135 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7076A 610 TUL - FOUND CORROSION ON SEAT TRACK BETWEEN FRAMES 29 AND 33 BEYOND MANUAL BLENDOUT LIMITS IN NUMEROUS AREAS. REMOVED A ND REPLACED CORRODED SEAT TRACK SECTION FROM FRAME 29 TO FRAME 33 IAW SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 2001081300062 20010813 00062 NM 2001 8 13 AALA20011199 1 20010606 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 707AA 22464 TUL - FOUND CORROSION ON UNDERSIDE OF FLOORBEAM AT DOOR SILL AREA FRAME 62 INBOARD OF ROLLOUT DEVICE. CORROSION IS HALF WAY THROUGH FLOORBEAM. INSTALLED FABRICATED SECTION OF FLOORBEAM AT DOOR SILL AREA STATION 4097 (FRAME 62) PER SRM 51- 72-10. (M) 2 L 7 3 4F A3WE 2001081300063 20010813 00063 EU 2001 8 13 SIMA200120001 1 20010719 A 5100 7253721427 INTERCOSTAL SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 284AE 340B284 SBP - RIGHT INTERCOSTAL CORRODED FROM STATION 236.5 TO STATION 258.0. REMOVED AND REPLACED INTERCOSTAL IAW SAAB SRM 51- 20-21, 51-20-41 AND 51-20-50. (M) 2 L 7 2 4T RT A52EU 2001081300064 20010813 00064 EU 2001 8 13 SIMA200120002 1 20010719 A 5100 7253721447 ANGLE SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 284AE 340B284 SBP - LEFT ANGLE THAT ATTACHES TO THE RIGHT INTERCOSTAL IS CORRODED FROM STATION 236.5 TO STATION 258. REMOVED AND REPL ACED LEFT ANGLE IAW SAAB SRM 51-20-21, 51-20-41 AND 51-20-50. (M) 2 L 7 2 4T RT A52EU 2001081300065 20010813 00065 EU 2001 8 13 SIMA200120004 1 20010719 A 5100 7253722001 ANGLE SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 284AE 340B284 SBP - LEFT ANGLE AT STATION 258 IS CORRODED. REMOVED AND REPLACED ANGLE IAW SAAB SRM 51-40-21. (M) 2 L 7 2 4T RT A52EU 2001081300066 20010813 00066 EU 2001 8 13 SIMA200120005 1 20010719 A 5100 7253719871 TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 284AE 340B284 SBP - AIRSTAIRS TRACK CORRODED. REMOVED AND REPLACED CORRODED TRACK IAW SRM. (M) 2 L 7 2 4T RT A52EU 2001081300067 20010813 00067 EU 2001 8 13 SIMA200120006 1 20010719 A 5100 7253711245 ANGLE SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 284AE 340B284 SBP - LEFT ANGLE CORRODED FROM STATION 272 AND 288. REMOVED AND REPLACED ANGLE IAW SAAB SRM 51-40-21. (M) 2 L 7 2 4T RT A52EU 2001081300068 20010813 00068 EU 2001 8 13 SIMA200120007 1 20010719 A 5100 7253721439 WEB SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 284AE 340B284 SBP - WEB REINFORCEMENT IS CORRODED AT STATION 294. REMOVED AND REPLACED WEB REINFORCEMENT IAW SAAB SRM 51-40-21. (M) 2 L 7 2 4T RT A52EU 2001081300069 20010813 00069 EU 2001 8 13 SIMA200120008 1 20010719 A 5100 7253742409 TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 284AE 340B284 SBP - FOUND SEAT TRACK AT BL 36 RIGHT IS CORRODED AT LEG ATTACH POINTS. REMOVED AND REPLACED TRACK ASSEMBLY IAW SAAB SR M 51-20-43, AND 51-70-40. (M) 2 L 7 2 4T RT A52EU 2001081300070 20010813 00070 EU 2001 8 13 SIMA200120009 1 20010719 A 5100 7253711147 FLOOR SUPPORT SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 284AE 340B284 SBP - RIGHT FLOOR SUPPORT ANGLE AT BL 34 IS CORRODED AT FORWARD END. REMOVED AND REPLACED FLOOR SUPPORT IAW SAAB SRM 51 -40-21. (M) 2 L 7 2 4T RT A52EU 2001081300071 20010813 00071 EU 2001 8 13 SIMA200120010 1 20010719 A 5300 7253725191 SEAT TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 284AE 340B284 SBP - FOUND CABIN SEAT TRACK AT STATION BL 00.0 IS CORRODED ON THE LOWER INBOARD FLANGE EXTENDING FROM ENTRY WAY TO CARG O AREA, TRACK WAS PREVIOUSLY GROUND. REMOVED AND REPLACED TRACK ASSEMBLY IAW SAAB SRM 53-70-60. (M) 2 L 7 2 4T RT A52EU 2001081300072 20010813 00072 EU 2001 8 13 SIMA200120013 1 20010719 A 5100 7253711145 SUPPORT SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 284AE 340B284 SBP - FOUND LEFT FORWARD FLOOR SUPPORT AT STATION BL 34 IS CORRODED ON THE LOWER PORTION. REMOVED AND REPLACED FLOOR SU PPORT IAW SAAB SRM 51-40-21. (M) 2 L 7 2 4T RT A52EU 2001081300073 20010813 00073 EU 2001 8 13 SIMA200120014 1 20010719 A 3200 7257162006 SUPPORT FITTING SAAB SF340 340B 7860101 EU RIGHT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 284AE 340B284 SBP - RIGHT MAIN LANDING GEAR DRAG BRACE BEARING SUPPORT HOUSING CORRODED. REMOVED AND REPLACED SUPPORT FITTING IAW SAA B AMM 57-40-05. (M) 2 L 7 2 4T RT A52EU 2001081300074 20010813 00074 EU 2001 8 13 SIMA200120023 1 20010719 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 338SB 340B338 ABI - DURING MBV, FRAME 658.5 WAS FOUND TO HAVE WEB DAMAGE ON THE RIGHT SIDE ABOVE WL 73.5. REMOVED AND REPLACED LOWER PORTION OF FRAME 658.5 AT THE FACTORY SPLICES. WORK DONE IAW SAAB 340 SRM (72LKS 3079 REV 37) 51-40-21, 51-40-22, 51-20 -50, 51-40-40, 51-20-42, 51-20-43, CPM (72LKS 5585 REV 2) 20-20-00 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT A52EU 2001081300075 20010813 00075 WP 2001 8 13 USAAD01135 1 20010711 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 811US 48043 CLT - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001081300076 20010813 00076 NM 2001 8 13 USAABB01057 1 20010708 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM ROW 18 INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 624AU 27245 LAX - FOUND FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE AT ROW 18. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2001081300077 20010813 00077 NM 2001 8 13 USAABB01056 1 20010706 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM ROW 4 INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 632AU 27810 BWI - FOUND FLOOR LEVEL EMERGENCY LIGHT BATTERY LOW AT ROW 4. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2001081300078 20010813 00078 NM 2001 8 13 USAASB01194 1 20010707 A 3350 6104789 BATTERY BOEING 737 7372B7 1384560 NM AFT CARGO BIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274AU 22886 BWI - THE LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY . (M) 2 L 7 2 4F A16WE 2001081300079 20010813 00079 WP 2001 8 13 USAAD01131 1 20010706 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801US 48037 IND - THE LOW LEVEL EMERGENCY LIGHTS AND THE RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES AND THE REMOTE RECEIVER. THE OVERWING EMERGENCY EXIT LIGHT WAS REPLACE D. THE GREEN CUEING LIGHT ON THE OVERWING EMERGENCY LIGHT WAS INTERMITTENT BUT THE LIGHT FUNCTIONED NORMALLY AS AN EMER GENCY LIGHT. THE LIGHT ASSEMBLY WAS PLACED ON MEL AND THE AIRCRAFT DISPATCHED. (M) 2 L 7 2 4F A6WE 2001081300081 20010813 00081 NE 2001 8 13 2001UALA01397 2 20010717 A 7321 783600 EEC BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT ENGINE FAILED A UALA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 WP 29 560UA 26660 726576 RIGHT ENGINE ROLLBACK ON TAKEOFF. PRIMARY ENGINE CONTROL MESSAGE P-EEC, P275-16. REPLACED EEC. CHECKED SENSE LINES, FOUN D SECURE. ANOTHER WRITE UP OCCURRED AFTER THE EEC WAS REPLACED FOR ENGINE ROLL BACK AT START. THE LOWER PB WATER TRAP VE NT HOLE WAS FOUND CLOGGED. ENGINE OPERATION HAS BEEN NORMAL SINCE THEN. THE PROBLEM LIKELY OCCURRED DUE TO A COMBINATION OF THE EEC PB TRANSDUCER AND THE CLOGGED LINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001081300083 20010813 00083 NM 2001 8 13 2001UALA01406 1 20010714 A 2752 V62983 MOTOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE T/E FLAP LEAKING A UALA A UNSCHED LANDING K F J FLUID LOSS FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 29 7445U 21899 INBOARD FLAPS INDICATION LIGHT ILLUMINATED WHILE RAISING FLAPS. AIRCRAFT RETURNED TO DEN. FOUND INBD FLAP HYD MOTOR LEA KING. REMOVED AND FOUND BEARINGS ROUGH, REPLACED WITH NEW REF MM27-53-19. CYCLED FLAPS SEVERAL TIMES, SYSTEM OPERATION N ORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001081300088 20010813 00088 2001 8 13 2001UALA01409 4 20010712 A 2350 G2121 AUDIO PANEL BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE COCKPIT FAILED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 7282U 21560 CREW REPORTS INTERMITTENT FAILURE OF NR 1 AND NR 2 RADIOS. AIRCRAFT RETURNED TO DEN. CAPTAIN'S AUDIO PANEL FAILED. REPLA CED CAPTAIN AUDIO SELECT PANEL PER MM. OPERATIONS CHECK NORMAL 2 L 7 3 4F 4 F A3WE E2EA 2001081300091 20010813 00091 EU 2001 8 13 2001UALA01415 1 20010718 A 2910 B-NUT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYDRAULIC SYS LOOSE A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 460UA 1248 FLIGHT CREW REPORTING LOSS OF GREEN HYDRAULIC SYSTEM. FOUND LEFT LANDING GEAR DOOR UPLOCK HYDRAULIC LINE B-NUT LOOSE. TI GHTENED NUT AND SERVICED SYSTEM. PRESSURIZED AND NO LEAKS FOUND. 2 L 7 2 4F 4 F RT A28NM E40NE 2001081300093 20010813 00093 NM 2001 8 13 2001UALA01418 1 20010722 A 5312 PRESSURE PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 515UA 24840 CABIN FLOOR PRESSURE DECK CORRODED. STA 1680, RBL 9.5. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2001081300095 20010813 00095 NM 2001 8 13 2001UALA01419 1 20010722 A 5312 PRESSURE PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 515UA 24840 CABIN FLOOR PRESSURE DECK CORRODED. STA 1965, RBL 52. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2001081300097 20010813 00097 NM 2001 8 13 2001UALA01420 1 20010722 A 5310 STRUCTURE BOEING 777 777222 1385219 NM FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 796UA 26931 MAJOR REPAIR: DENTED AND GOUGE 18 INCHES AFT OF NR 4 LT. MED CUTOUT 8 INCHES UP FROM THRESHOLD. REPAIRED DOUBLER PER S RM 53-00-01 AT APPROX. BS 2087 S-26L. 2 L 7 2 4F RT T0001SE 2001081300104 20010813 00104 NM 2001 8 13 AWXA0002099 1 20010802 A 5310 65C80735115 SEAT BOEING 737 737277 1384570 NM STA 1006-1016 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 D: Aft cabin R/H track F.STN.1006-1016 RBL 45 corroded.C: R/H floor track F.STN.1006-1016 RBL 45 DRAW 65C80735 - part no . 65C80735-115 and IAW SRM 51-10-1 Page 8,9,10 2 L 7 2 4F RT A16WE 2001081300105 20010813 00105 NM 2001 8 13 AWXA0002100 1 20010803 A 5313 654687782 WEB BOEING 737 737277 1384570 NM STA 727 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 D: S-18A R/H shear beam web cracked.C: Replaced web 65-46877-82 per DWG 65-46877 - 76 INST. IAW SRM 51-10-1 page 8,9,10 2 L 7 2 4F RT A16WE 2001081300106 20010813 00106 NM 2001 8 13 2001UALA01422 1 20010720 A 2752 V62983 SCREW BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FLAP MOTOR MISSING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION UK UNKNOWN 1 WP 29 7261U 21408 LOSS OF HYDRAULIC FLUID IN THE 'A' SYSTEM. FOUND FLAP DRIVE MOTOR SHAFT SEAL PLATE MISSING SCREWS AND O-RING POPPED OUT. REPLACED FLAP DRIVE MOTOR AND SERVICED HYD SYS. OPERATIONS AND LEAK CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001081300107 20010813 00107 NM 2001 8 13 2001UALA01423 1 20010720 A 5312 BULKHEAD BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 912UA 25290 3 GOUGES ON FWD PRESSURE BULKHEAD. 1 GOUGE AT BS 178, LBL 16, WL 208. 2 AT BS 178, LBL 22, WL 197. INSTALLED DOUBLER RE PAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082200051 20010822 00051 NE 2001 8 22 2001UALA01424 2 20010719 A 7200 ENGINE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 FIRE A UALA K NONE A FLAME/FIRE LD LANDING 1 WP 29 7283U 21561 700441 UPON LANDING FLAMES CAME OUT OF NR 1 ENGINE THRUST REVERSERS WHEN THRUST REVERSERS WERE MOVED TO STOWED POSITION. *S/D* REPORT OF FLAMES OUT OF THE THRUST REVERSER WAS REPORTED BY OPERATIONS VEHICLE AND NO CAUSE HAS BEEN FOUND. THE THRUS T REVERSER WAS OPERATED SEVERAL TIMES AND AT DIFFERENT POWER SETTINGS PER MM 72-05-00 AND NO ABNORMAL INDICATIONS WERE P RESENT. NO FLAMES. THERE HAVE BEEN NO REPORTS OF PROBLEMS WITH THE THRUST REVERSER BEFORE OR AFTER THIS EVENT. 2 L 7 3 4F 4 F A3WE E2EA 2001081300110 20010813 00110 NM 2001 8 13 2001UALA01425 1 20010722 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 320UA 23952 FWD GALLEY DOOR FRAME CRACKED NR 2, NR 3, AND NR 4 STOPS. REMOVED DAMAGE. INSTALLED REPAIR ANGLE. MAJOR REPAIR ACCOMPLI SHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001081300111 20010813 00111 NM 2001 8 13 2001UALA01426 1 20010722 A 5230 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 320UA 23952 AFT CARGO DOOR, EXTERIOR SKIN UPPER LT CORNER CRACKED. INSTALLED DOUBLER. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082200044 20010822 00044 NM 2001 8 22 2001UALA01427 1 20010719 A 3260 FZH6DE10SL3S CONNECTOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NLG FAULTY A UALA K NONE N FALSE WARNING AP APPROACH 1 WP 29 7252U 21399 NOSE GEAR RED LIGHT ON WHEN GEAR EXTENDED. *S/D* REPLACED CONNECTOR D298. OPERATIONS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001081300113 20010813 00113 NM 2001 8 13 2001UALA01428 1 20010722 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 320UA 23952 AFT CARGO DOOR, DAMAGE HOLE THROUGH BOTH UPPER AND LOWER FRAMES AND STRAP ANGLE. REPLACED UPPER AND LOWER FRAMES, AND S TRAP ANGLE. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001081300114 20010813 00114 NM 2001 8 13 2001UALA01429 1 20010722 A 5230 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOOR CANNING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 320UA 23952 AFT CARGO DOOR, EXTERIOR SKIN DENTED AND OIL CANNING. INSTALLED DOUBLER. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082200045 20010822 00045 NM 2001 8 22 2001UALA01430 1 20010719 A 3242 211473U1 BRAKE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT MLG FIRE A UALA K NONE A FLAME/FIRE TX TAXI/GRND HDL 1 WP 29 7280U 21558 LEFT OUTBOARD LANDING GEAR BRAKES CAUGHT ON FIRE APPROX 3 MINUTES AFTER PARKING BRAKES SET. *S/D* INSPECTION ACCOMPLIS HED WITH NR 1 & NR 2 BRAKES REMOVED, NO DEFECTS FOUND. REPLACED NR 1 AND NR 2 BRAKES AS PRECAUTIONARY. OPERATIONS CHEC K NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001081300115 20010813 00115 NM 2001 8 13 2001UALA01431 1 20010722 A 5230 CROSSBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 320UA 23952 AFT CARGO DOOR, LOWER CROSS BEAM WEB CRACKED. REPLACED LOWER CROSS BEAM WEB. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001081300116 20010813 00116 NM 2001 8 13 2001UALA01433 1 20010722 A 5312 BULKHEAD BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 MAJOR REPAIR ACCOMPLISHED TO AFT PRESSURE BLKHD 6:00 POSITION. 2 L 7 2 4F 4 F RT A1NM E24NE 2001081300118 20010813 00118 NM 2001 8 13 2001UALA01435 1 20010722 A 2432 WARNING SYSTEM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT ACTIVATED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 663UA 27160 "MAIN BATT CHGR" MESSAGE DISPLAYED ON EICAS. 2 L 7 2 4F 4 F RT A1NM E24NE 2001081300119 20010813 00119 NM 2001 8 13 2001UALA01436 1 20010720 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE L1 DOOR BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 DOOR 1L EMER EXIT LIGHT IS BROKEN. 2 L 7 2 4F 4 F RT A1NM E24NE 2001081300120 20010813 00120 NM 2001 8 13 2001UALA01437 1 20010722 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 668UA 30024 EEL LIGHTS INOP LEFT SIDE FROM ROW 35 TO AFT DOOR. 2 L 7 2 4F 4 F RT A1NM E24NE 2001082900043 20010829 00043 NE 2001 8 29 2001UALA01438 2 20010718 A 7321 FUEL CONTROL BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE ENGINE OUT OF RIG A UALA O OTHER O OTHER CR CRUISE 1 WP 29 619UA 21879 RIGHT THROTTLE AHEAD. THROTTLES NOT ALIGNED WITHIN 1 INCH AT KNOB AT SAME EPR AT ALL POWER SETTINGS. ENGINES OUT OF TRI M AT PART POWER. TRIMMED ENGINES TO PART POWER TRIM CHARTS. 2 L 7 2 4F 4 F RT A1NM E3NE 2001081300121 20010813 00121 NM 2001 8 13 2001UALA01439 1 20010723 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 515UA 24840 CABIN FLOOR INNER CREASE BEAM CORRODED. STA 740-780, RBL 60. MAJOR REPAIR ACCOMPLISHED.INSTALLED J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2001081300122 20010813 00122 NM 2001 8 13 2001UALA01441 1 20010723 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 515UA 24840 CABIN FLOOR BEAM CORRODED. STA 365, RBL1-RBL 27. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2001081300124 20010813 00124 NM 2001 8 13 2001UALA01442 1 20010723 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 515UA 24840 CABIN FLOOR INNER CREASE BEAM CORRODED. STA 900-1040 RBL 70-75. MAJOR REPAIR ACCOMPLISHED.INSTALLED NEW CREASE BEAM AN D WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2001082900044 20010829 00044 NM 2001 8 29 2001UALA01444 1 20010720 A 7110 COWLING BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7263U 21410 NR 2 ENGINE LOWER FORWARD COWLING MATING FLANGE, FOUND 3 CRACKS, ONE 8 INCHES LONG, THE OTHERS 3.5 INCHES LONG. ALSO, T HERE IS A HOLE WORN THRU COWL MATING FLANGE. REPAIRED COWL AND SPLICED IN NEW FLANGE. MAJOR REPAIR ACCOMPLISHED. 2 L 7 3 4F 4 F A3WE E2EA 2001081300128 20010813 00128 NM 2001 8 13 2001UALA01445 1 20010722 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7289U 21567 RIGHT SIDE OF FUSELAGE 6 INCHES AFT OF FORWARD LAV SERVICE PANEL, PAINT IS BUBBLING AND SKIN IS BULGING IN A 6 INCH DIAM ETER AREA. 2 L 7 3 4F 4 F A3WE E2EA 2001081300129 20010813 00129 NM 2001 8 13 2001UALA01446 1 20010719 A 5350 NUT PLATE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE TAIL CONE LOOSE A UALA K NONE E VIBRATION/BUFFET CR CRUISE 1 WP 29 7275U 21422 VIBRATION AT M .80, INCREASES WITH AIRSPEED, AND LEFT TURNS, STAYS THE SAME WITH SPOILERS EXTENDED. FOUND NUTPLATES ON T AIL CONE REQUIRING REPLACEMENT. NUTPLATES ALLOWED TAIL CONE TO VIBRATE. 2 L 7 3 4F 4 F A3WE E2EA 2001081300130 20010813 00130 NE 2001 8 13 2001UALA01447 2 20010723 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 VIBRATION A UALA O OTHER E VIBRATION/BUFFET CR CRUISE 1 WP 29 548UA 25396 EXCESSIVE VIBRATION IN THE NUMBER 2 ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001081300133 20010813 00133 NM 2001 8 13 2001UALA01448 1 20010723 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 EXTERNAL FUSELAGE SKIN CRACKED AT BS727D, STR24L. INSTALLED REPAIR DOUBLER. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001081300135 20010813 00135 NM 2001 8 13 2001UALA01449 1 20010723 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 EXTERNAL FUSELAGE SKIN CRACKED AT BS727D, STR24R. INSTALLED REPAIR DOUBLER. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001081300140 20010813 00140 NE 2001 8 13 2001UALA01450 2 20010722 A 7532 32289516 VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT ENGINE FAILED A UALA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 29 550UA 25398 726523 REJECTED T/O AT 50 KNOTS. RIGHT ENGINE EPR ROLLED BACK FROM 1.2 TO 1.1. WHILE ACCOMPLISHING AN ENGINE RUN TO TROUBLESHOO T THE PROBLEM, AT 1.1 EPR 14TH STAGE BLEED VALVE SOUNDED LIKE IT WAS OPEN. THE 14TH STAGE CONVERTER VALVE WAS REPLACED (CONVERTER VALVE IS THE CONTROLLING ITEM FOR THE BLEED VALVE). 2 L 7 2 4F 4 F RT A2NM E17NE 2001081300142 20010813 00142 NM 2001 8 13 2001UALA01451 1 20010720 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE L1 DOOR BROKEN A UALA K NONE O OTHER AP APPROACH 1 WP 29 657UA 27112 DOOR 1L EMER EXIT LIGHT IS BROKEN. 2 L 7 2 4F 4 F RT A1NM E24NE 2001081300144 20010813 00144 NM 2001 8 13 2001UALA01453 1 20010722 A 5312 BULKHEAD BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 MAJOR REPAIR ACCOMPLISHED TO AFT PRESSURE BLKHD 6:00 POSITION. 2 L 7 2 4F 4 F RT A1NM E24NE 2001081300153 20010813 00153 NE 2001 8 13 2001UALA01454 2 20010719 A 7200 ENGINE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LEFT MALFUNCTIONED A UALA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 WP 29 614UA 21875 WHILE CRUISE FL 410 FOR WEATHER, AVOIDING EXPECTED LIGHT-MOD CHOP. LIGHT PRECIP W-IGNITION CON. LT ENG LOSS THRUST . EN GINE RELIT DURING DESCENT TO FL 310 ON ITS OWN. FA'S REPORT LOUD NOISE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001081300154 20010813 00154 NM 2001 8 13 2001UALA01455 1 20010723 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 566 STR 39L-39R SHEAR TIE CORRODED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001081300155 20010813 00155 NM 2001 8 13 2001UALA01456 1 20010723 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 676 STR 39L-39R SHEAR TIE CORRODED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001081300156 20010813 00156 NM 2001 8 13 2001UALA01457 1 20010723 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 548 STR 39L-39R SHEAR TIE CORRODED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001081300157 20010813 00157 NM 2001 8 13 01FDEA00665 1 20010731 A 5320 WEB BOEING 727 72722 1384002 NM FUSELAGE TOP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 149FE 19087 N 833 DUR ROUTINE INSP A CRACK FND IN WEB BETWEEN BS 1176.9 & 1183, LBL 46, WL 208. R&R WEB PER IAW FEDEX SRM 51-40-8. 2 L 7 3 4F A3WE 2001081300158 20010813 00158 NM 2001 8 13 01FDEA00669 1 20010808 A 2613 CONTROL UNIT BOEING 727 727225 1384077 NM E&E COMPARTMENT FAULTY A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SO 25 461FE 22548 01-268 DUR FLT WITH ENG ANTI-ICE OPEN LWR AFT BODY O/H LIGHT ILLUM. R&R FIRE DET O/H DETECTOR PER MM 20-10-017-2. TEST GOOD. 2 L 7 3 4F A3WE 2001082000186 20010820 00186 NM 2001 8 20 01FDEA00672 1 20010731 A 5320 BRACKET BOEING 727 72722 1384002 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 149FE 19087 DURING ROUTINE INSP DISCOVERED MCD THRESHOLD AFT LWR CORNER SEAL DEPRESSOR ATTACH BRACKET CRACKED BS 619, WL 207. *S/D* REMOVED AND REPLACED SEAL DEPRESSOR ATTACH BRACKET PER SRM 51-30-2. 2 L 7 3 4F A3WE 2001082000187 20010820 00187 NM 2001 8 20 01FDEA00673 1 20010731 A 5320 BRACKET BOEING 727 72722 1384002 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 149FE 19087 DMCD THRESHOLD FWD LWR CORNER SEAL DEPRESSOR ATTACH BRACKET CRACKED AT BS 481, WL 207. *S/D* REMOVED AND REPLACED SEAL DEPRESSOR ATTACH BRACKET PER SRM 51-30-2. 2 L 7 3 4F A3WE 2001081300159 20010813 00159 NM 2001 8 13 01FDEA00674 1 20010731 A 5313 STRINGER BOEING 727 72722 1384002 NM FUSELAGE LOWER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 149FE 19087 N 1426 STRINGER 16L CRACKED AT BS 623. ** S/D ** COMING 2 L 7 3 4F A3WE 2001081300160 20010813 00160 NM 2001 8 13 01FDEA00675 1 20010809 A 5310 STRINGER BOEING 727 727233 138408A NM FUSELAGE LOWER CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277FE 22042 N 548 STR 29L CORRODED AT BS 960. R&R STR PER IAW FEDEX SRM 51-40-4 & 51-30-2. 2 L 7 3 4F RT A3WE 2001081300161 20010813 00161 NM 2001 8 13 2001UALA01458 1 20010723 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 588 STR 37L-38L SHEAR TIE CORRODED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001081300162 20010813 00162 NM 2001 8 13 2001UALA01459 1 20010723 A 5230 SKIN BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CARGO DOOR BENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 AFT PIT CARGO DOOR FWD BOTTOM CORNER SKIN BENT. 2 L 7 2 4F 4 F RT A1NM E3NE 2001081600106 20010816 00106 NM 2001 8 16 2001UALA01460 1 20010724 A 2910 AC11504K0232 HYDRAULIC LINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE HYDRAULIC SYS RUPTURED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 509UA 24763 AFTER TAKEOFF LOST LEFT HYDRAULIC SYSTEM. *S/D* LEFT DOWNLOCK ACTUATOR HOSE RUPTURED. REPLACED HOSE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001081300163 20010813 00163 NM 2001 8 13 2001UALA01462 1 20010725 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7297U 21892 FUSELAGE SKIN CRACK LOCATED JUST AFT OF NR 2 VHF ANTENNA, LEFT OUTBOARD BETWEEN 4TH AND 5TH ROW OF RIVETS. CRACK IS APP ROX. 1.75 INCHES LONG. FUSELAGE SKIN CRACK BETWEEN STATION 1030 AND 1070 STR 28L. DAMAGE CUTOUT, EDDY CURRENT, AND DOU BLER INSTALLED PER SRM 53-30-03 CAT B REPAIR. 2 L 7 3 4F 4 F A3WE E2EA 2001081300164 20010813 00164 NE 2001 8 13 NACA20010029 2 20010811 A 7230 356993 CYLINDER PWA CB3 DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE #2 ENGINE CRACKED A NACA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 AL 03 779TA 514 514 P35317 45529 P35317 DISCREPANCEY: Precautionary shut down #2 engine due to running rough, #4 and #7 cylinder low compression.CORRECTIVE ACTI ON: Replaced #4 cylinder. 2 L 7 4 4R 4 R A781 5E8 2001081300165 20010813 00165 NM 2001 8 13 PCAA0108084 1 20010809 A 2120 PW120A ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RIGHT SMOKE A PCAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 13 808EX 16942 2275 299 PCE121348 ALB-BUF FLIGHT#3592. WHEN ON DECENT FOR LANDING THE SMOKE ALARM WENT OFF. SMOKE WAS IN BOTH THE FLIGHT DECK AND CABIN. M AINTENANCE REPLACED RIGHT ENGINE IN ACCORDANCE WITH ALLEGHENY JOBCARD 008-7101-349. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2001081300166 20010813 00166 NM 2001 8 13 PCAA0108083 1 20010810 A 3350 6104781 BATTERY DHAV DHC8 DHC8102 2809003 NM FORWARD CEILING POWER LOSS A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 816EX 329 MDT- DURING ROUTINE MAINTENANCE VISIT SEVERAL FLOOR EMERGENCY LIGHTS FOUND INOPERATIVE. REPLACED FIRST 2 EMERGENCY LIGHT S AND REPLACED FORWARD CEILING BATTERY PACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091400087 20010914 00087 NM 2001 9 14 2001UALA01463 1 20010721 A 2130 7110024 CONTROL PANEL BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE COCKPIT FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7261U 21408 CABIN PRESSURIZATION ELECTRONIC SYSTEM IN MANUAL THERE IS NO OUTFLOW VALVE INDICATOR MOVEMENT WITH FUNCTION SWITCH IN AC MANUAL. VALVE VISUALLY OBSERVED AND IS NOT MOVING. THE CONTROL PANEL FAILED. REPLACED CONTROL PANEL. OPERATIONS CHEC K NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001081300167 20010813 00167 NM 2001 8 13 2001UALA01464 1 20010719 A 3350 LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE AFT AIRSTAIRS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7286U 21564 AFT AIRSTAIR EMERGENCY LIGHT HAS ONE BULB BURNED OUT RELAMPED. OPERATIONAL CHECK GOOD 2 L 7 3 4F 4 F A3WE E2EA 2001091400088 20010914 00088 NE 2001 9 14 2001UALA01465 2 20010720 A 7200 ENGINE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 MALFUNCTIONED A UALA A UNSCHED LANDING M OVER TEMP TO TAKEOFF 1 WP 29 7259U 21406 700058 NR 3 ENG EGT LIMITED T/O FROM DEN. COMMAND EPR 2.06. TARGET N1 X-CK 98.1. AT 2.06 EPR, NR 3 ENG N1 95 PERCENT AND EGT R EACHED 630 DEG FOR 2 SEC. REDUCED POWER TO KEEP EGT IN LIMITS. A CHECK OF THE INLET AND EXHAUST AND PERFORM THE MAX EGT CHECK PER JRH 2-7-35. ALL WAS NORMAL. PERFORMED FUEL NOZZLE BORESCOPE INSPECTION AND NO DISTRESS NOTED. AIRCRAFT HAS HAD NO DISCREPANCIES FOR EGT SINCE. 2 L 7 3 4F 4 F A3WE E2EA 2001091400089 20010914 00089 NM 2001 9 14 2001UALA01466 1 20010722 A 2710 AILERON BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT WING OUT OF ADJ A UALA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 WP 29 7252U 21399 CREW REPORTS RIGHT HAND WING OUTBOARD AILERON, INBOARD TRAILING EDGE MAKING CONTACT. CHECKED ADJUSTMENT OF FLAP AND ADJU STED AILERON. OPERATIONS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001081300168 20010813 00168 NM 2001 8 13 2001UALA01467 1 20010718 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7449U 21903 AFT PIT BILGE AREA CORROSION IN SKIN LT SIDE, BETWEEN STR 28L AND 29L, STA 970-990. 2 L 7 3 4F 4 F A3WE E2EA 2001081300169 20010813 00169 NM 2001 8 13 2001UALA01468 1 20010723 A 2130 CONTROLLER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN PRESSURE MALFUNCTIONED A UALA K NONE O OTHER CR CRUISE 1 WP 29 7259U 21406 AT FL240 WHEN THROTTLES PULLED BACK TO FLIGHT IDLE, CABIN PRESSURE STARTED CLIMBING AT 2000 FPM. WHEN CARGO HEAT VALVE C LOSED, CABIN PRESSURIZATION RETURNED TO NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001091400094 20010914 00094 NM 2001 9 14 2001UALA01470 1 20010724 A 2923 69287276 PUMP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE HYDRAULIC SYS LEAKING A UALA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 7466U 21920 CREW REPORTS LOSS OF B-SYSTEM BRAKE PRESSURE, ALSO REPORTS FLUID COMING FROM THE GEAR ON TAXI OUT. REPLACED NR 2 ENGINE B-SYSTEM HYDRAULIC PUMP. SYSTEM TESTS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001082900045 20010829 00045 NM 2001 8 29 2001UALA01471 1 20010718 A 5310 SHEAR TIE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7449U 21903 AFT PIT BILGE, CORROSION IN SHEAR TIE AFT SIDE OF FRAME 1130 BETWEEN STR 27L AND 28L. REPAIRED SHEAR TIE PER MM 53-10-29 . MAJOR REPAIR ACCOMPLISHED. 2 L 7 3 4F 4 F A3WE E2EA 2001082900047 20010829 00047 NM 2001 8 29 2001UALA01472 1 20010718 A 5310 SHEAR TIE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7449U 21903 AFT PIT BILGE, CORROSION IN SHEAR TIE FORWARD SIDE BETWEEN STR 28L AND 29L AT FRAME STA 1010. REPAIRED SHEAR TIE PER MM 53-10-29. MAJOR REPAIR ACCOMPLISHED. 2 L 7 3 4F 4 F A3WE E2EA 2001091400095 20010914 00095 2001 9 14 2001UALA01473 4 20010718 A 3444 5224255001 CONNECTOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE GROUND PROX SYS INTERMITTENT A UALA K NONE J WARNING INDICATION NR NOT REPORTED 1 WP 29 7449U 21903 RADIO ALTIMETER FAULT WITH ASSOCIATED GPWS FAIL. INTERMITTENT CONNECTION CAUSED THE FAULT. REMOVED AND REINSTALLED ANT RAD ALT TX ANTENNAS. SECURED SOFT MATE CONNECTOR RAD ALT. OPERATIONS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001081300170 20010813 00170 NM 2001 8 13 2001UALA01477 1 20010725 A 5310 DOOR FRAME BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 990UA 21980 FWD CARGO DOOR FRAME DAMAGED AT LOWER FORWARD CORNER. REPLACED FRAME. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F A16WE E2EA 2001081300172 20010813 00172 NM 2001 8 13 2001UALA01479 1 20010725 A 5312 BULKHEAD BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 918UA 25385 BULKHEAD WEB CRACKED AT LT WEATHER ANTENNA UPPER MOUNT, AT BS178. INSTALLED DOUBLER. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001081300173 20010813 00173 NM 2001 8 13 0102832710 1 20010709 A 5311 FRAME BOEING 727 727225 1384077 NM CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 820EA 22557 During "M" check found corrosion on frame inner flange pilot hole at edge of fastener hole. Repaired per EA 27-184374. 2 L 7 3 4F A3WE 2001081300174 20010813 00174 EU 2001 8 13 RAIA00108010 1 20010810 A 2430 23095002 GENERATOR JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILED A RAIA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 CE 03 568HK 6557 31 41086 7496-STL-RIGHT GENERATOR FELL OFF LINE DURING FLIGHT. MAINTENANCE INSPECTED AND REPLACED RIGHT STARTER GENERATOR. 2 L 7 2 4T RT A41NM 2001081300175 20010813 00175 EU 2001 8 13 RAIA00108011 1 20010803 A 2120 23403564 HEAT EXCHANGER AEROSP ATR72 ATR72202 8680940 EU RT AIR/COND BAY FAILED A RAIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 722TE 6015 513 220 7116-STL-CABIN ATTENDANT SAID SMOKE WAS COMING OUT OF CABIN AIR VENTS. MAINTENANCE INSPECTRD AND DEFERRED THE RIGHT BLEE D SYSTEM PER MEL. MAINTENANCE REPLACED THE RIGHT HEAT EXCHANGER. 2 H 7 2 4T RT A53EU 2001081300176 20010813 00176 NM 2001 8 13 2001UALA01480 1 20010726 A 3320 LIGHT BOEING 777 777222 1385219 NM CABIN ODOR A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 WP 29 219UA 30551 HOT BURNING ELEC SMELL COMING FROM THE COVE LIGHTS, SEEMS TO BE IN THE DIM POS.TRIED TURNING OFF ALL CABIN LIGHTS, NO SU CCESS. ALSO READING LIGHTS STUCK IN NORMAL, WOULD NOT TURN OFF PER CREW. PULLED CB'S 02,03,H04,09,L02,03,07,10 AS PRECA UTION. ALSO PULLED CB D10 AND C10 ON P210 PANEL. 2 L 7 2 4F RT T0001SE 2001081300177 20010813 00177 NM 2001 8 13 2001UALA01481 1 20010726 A 5320 STRINGER CLIP BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 990UA 21980 STRINGER CLIP DAMAGED, AT BS500B, STR1L. REPLACED STRINGER CLIP. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F A16WE E2EA 2001081300178 20010813 00178 NM 2001 8 13 2001UALA01482 1 20010726 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 913UA 25291 LOWER FUSELAGE SKIN GOUGE HAS EXCESSIVE MATERIAL LOSS, AT BS887, STR27L. INSTALLED DOUBLER. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001081300179 20010813 00179 NM 2001 8 13 2001UALA01483 1 20010726 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 914UA 25381 FRAME WEB ON FWD SIDE, BELOW FLOOR LEVEL JUST OB OF INBD CHORD, HAS EXCESSIVE MATERIAL LOSS, AT BS616.5. REMOVED DAMAGE . INSTALLED REPAIR DOUBLER. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001081300180 20010813 00180 NM 2001 8 13 2001UALA01484 1 20010726 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 914UA 25381 CABIN FLOORBEAM CAP IS CORRODED AT FASTENER HOLE, AT BS294.5, RBL45. INSTALLED FLOOR CAP REPAIR. MAJOR REPAIR ACCOMPLIS HED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001081300182 20010813 00182 NM 2001 8 13 2001UALA01486 1 20010724 A 3350 LIGHT BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 605UA 21866 EEL LIGHTS INOP RIGHT SIDE FROM ROW 1 THRU ROW 11. 2 L 7 2 4F 4 F RT A1NM E3NE 2001081300183 20010813 00183 NM 2001 8 13 2001UALA01487 1 20010725 A 5310 DOOR FRAME BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE BENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 FWD PIT DOOR FRAME, FWD TOP CORNER WEB BENT. 2 L 7 2 4F 4 F RT A1NM E3NE 2001081300184 20010813 00184 NM 2001 8 13 2001UALA01488 1 20010725 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 1241 RBL8-RBL20 T CAP CORRODED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001081300185 20010813 00185 NM 2001 8 13 2001UALA01489 1 20010725 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 1285 LBL0-LBL33 T CAP CORRODED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001081300186 20010813 00186 NM 2001 8 13 2001UALA01490 1 20010725 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 434-456 STR 34L CORRODED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001081300187 20010813 00187 NM 2001 8 13 2001UALA01491 1 20010725 A 5320 ATTACH ANGLE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 1087 RBL 25 INTERCOSTAL ATTACH ANGLE CRACKED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001081300188 20010813 00188 NM 2001 8 13 2001UALA01492 1 20010725 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 720 STR 36R-37R SHEAR TIE CORRODED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001081300189 20010813 00189 NM 2001 8 13 2001UALA01493 1 20010725 A 5310 STRUCTURE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 434 STR 36L-37L CORRODED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001081300190 20010813 00190 NM 2001 8 13 2001UALA01494 1 20010725 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 434-478 STR 35L CORRODED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001081300191 20010813 00191 NM 2001 8 13 2001UALA01495 1 20010725 A 5320 SPLICE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 434 STR 35L SPLICE CORRODED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001081300193 20010813 00193 NM 2001 8 13 2001UALA01497 1 20010725 A 5320 WEB BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 1273-1280 RBL6 WEB CORRODED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001081300194 20010813 00194 NM 2001 8 13 2001UALA01498 1 20010725 A 5320 ATTACH ANGLE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 1087 LBL25 INTERCOSTAL ATTACH ANGLE CRACKED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001081300195 20010813 00195 NM 2001 8 13 2001UALA01499 1 20010725 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 434 STR 34R CORRODED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001081300196 20010813 00196 NM 2001 8 13 2001UALA01500 1 20010725 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 434 STR 35R CORRODED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001081300197 20010813 00197 NM 2001 8 13 2001UALA01501 1 20010725 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 434 STR 34R CORRODED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001081300198 20010813 00198 NM 2001 8 13 2001UALA01502 1 20010725 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 434 STR 37L-38L SHEAR TIE CORRODED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001081300199 20010813 00199 NM 2001 8 13 2001UALA01503 1 20010725 A 5320 BRACKET BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 FS 581 RBL40 CANNON PLUG BRACKET BROKEN. 2 L 7 2 4F 4 F RT A1NM E3NE 2001081300200 20010813 00200 EU 2001 8 13 DHL2001362023 1 20010718 A 3231 A2519903 VALVE AIRBUS 300 A300B4203 3930306 EU MLG FAILED A DHLA O OTHER J WARNING INDICATION IN INSP/MAINT 1 SO 01 362DH 84 WHEN SELECTING GEAR DOWN THREE RED GEAR UNSAFE WARNINGS APPEARED. RAN THE PROCEDURE AND MANUALLY EXTENDED GEAR. INSTALLE D SAFETY GEAR PINS. REMOVED & REPLACED LANDING GEAR ELECTRO VALVE IAW 32-31-12. OPS CKS GOOD IAW MM 32-31-12. 2 L 7 2 4F RT A35EU 2001081300203 20010813 00203 EU 2001 8 13 DHL2001362024 1 20010722 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU CARGO BAY MALFUNCTIONED A DHLA K NONE N FALSE WARNING NR NOT REPORTED 1 SO 01 362DH 84 SMOKE DETECTOR LIGHTS ILLUMINATED. NO SMOKE VISUALLY DETECTED. AFT CARGO TEMPS WERE 90 DEGREES PLUS. APPLIED EXTERNAL CO NDITIONED AIR CART AND CYCLED CIRCUIT BREAKERS AND CARGO COMPARTMENT ISOLATION VALVES IAW A300 MM SUPP. 26-11-00. OPERA TIONAL CHECK SERVICEABLE. 2 L 7 2 4F RT A35EU 2001081300204 20010813 00204 EU 2001 8 13 DHL2001362025 1 20010806 A 3260 LIGHT AIRBUS 300 A300B4203 3930306 EU COCKPIT INOPERATIVE A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 362DH 84 NOSE GEAR LIGHT DOWN AND LOCKED INOP FRONT PANEL. R/R LANDING GEAR IND UNIT AS PER MM 32-61-00. 2 L 7 2 4F RT A35EU 2001081300205 20010813 00205 EU 2001 8 13 DHL2001362026 1 20010806 A 3260 CONNECTOR AIRBUS 300 A300B4203 3930306 EU COCKPIT LOOSE A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 362DH 84 NOSE GEAR DOWN AND LOCKED LIGHT (GREEN) NOT WORKING ON FORWARD PANEL. RESEATED CANNON PLUG BEHIND INDICATOR.OPS CK NORMA L PER 33-15-80. 2 L 7 2 4F RT A35EU 2001081300206 20010813 00206 WP 2001 8 13 CALA0100746 1 20010808 A 5240 INTERCOSTAL DOUG DC9 DC982 3022082 WP R-1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND A 7" CRACK IN R-1 DOOR INNER INTERCOSTA UNDER HINGE ATTACH POINT. THE R-1 DOOR WAS REMOVED IAW MM 52-41 -00. THE CRACK WAS STOP DRILLED AND A REPAIR CAP AND FITTING WERE INSTALLED IAW SRM 52-05, FIGURE 5. REINSTALLED R-1 DOO R IAW MM 52-41-00. 2 L 7 2 4F A6WE 2001081300207 20010813 00207 WP 2001 8 13 CALA0100747 1 20010808 A 5342 ATTACH ANGLE DOUG DC9 DC982 3022082 WP STA 1463 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72821 49481 INSPECTION FOUND A 3/4" CRACK COMING FROM RIVET HOLE IN R/H SIDE VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE AT STA 146 3. THE CRACKED AREA WAS CUT OUT AND A REPAIR ANGLE WAS INSTALLED IAW SRM 53-05, FIGURE 23. 2 L 7 2 4F A6WE 2001081300208 20010813 00208 NM 2001 8 13 CALA0100749 1 20010808 A 5315 FLOORBEAM BOEING 737 737524 1384721 NM STA 986.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 24633 27901 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, LBL 4, LBL 30, AND RBL 38. A STRAP DOUBLER WAS INSTALLED AT EACH LOCAT ION IAW SRM 53-00-51. 2 L 7 2 4F RT A16WE 2001081300209 20010813 00209 WP 2001 8 13 CALA0100750 1 20010809 A 5311 FRAME DOUG DC9 DC982 3022082 WP STA 1474 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72821 49481 INSPECTION FOUND A 2" CRACK IN TAIL COMPARTMENT CANTED FRAME AT STA 1474, LEFT LOWER SIDE, BY VENT BOX DRAIN HOSE. REPAI RED IAW ECRA 5310-04173. 2 L 7 2 4F A6WE 2001081300210 20010813 00210 WP 2001 8 13 CALA0100756 1 20010810 A 5313 LONGERON DOUG DC9 DC982 3022082 WP STA 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72821 49481 INSPECTION FOUND A 10" CRACK AT END OF LONGERON 2L AT STA 1418. A HAT SECTION REPAIR SPLICE WAS INSTALLED IAW SRM 53-02, FIGURE 18. 2 L 7 2 4F A6WE 2001081300211 20010813 00211 WP 2001 8 13 CALA0100757 1 20010810 A 5330 SKIN DOUG DC9 DC982 3022082 WP STA 435-510 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72821 49481 THE R/H FUSELAGE SKIN WAS DENTED BETWEEN FORWARD CARGO DOOR AND RIGHT TURN OFF LIGHT AT STA 435-510 BETWEEN LONGERONS 20 R AND 21R. A FLUSH SKIN PANEL REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 12C. 2 L 7 2 4F A6WE 2001081300212 20010813 00212 NM 2001 8 13 CALA0100758 1 20010811 A 3350 GROUND WIRE BOEING 737 737524 1384721 NM O/H EMER LT LOOSE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14628 27532 THE OVERHEAD EMERGENCY LIGHT AT L-1 DOOR FAILED TO ILLUMINATE DURING EMERGENCY LIGHT CHECK. MAINTENANCE FOUND NUT BACKED OFF OF GROUND 622 GROUNDING STUD AND GROUND WIRE LOOSE. THE NUT WAS REPLACED AND THE GROUND WIRE WAS SECURED. OPERATION AL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2001081300213 20010813 00213 EU 2001 8 13 DHL2001362027 1 20010807 A 2613 HARNESS AIRBUS 300 A300B4203 3930306 EU OVERHEAT SYS FAULTY A DHLA K NONE L NO TEST NR NOT REPORTED 1 SO 01 362DH 84 MANIFOLD FAULT DETECT LOOPS ON LT SELECT WONT TEST ON BOTH. DEFERRED LT LOOP "A" IAW MEL 36-12-03."B" TESTS OK. REPLACED WIRE HARNESS 81HF IN AIRCONDITIONING COMPARTMENT FOR 'A' LOOP MAINFOLD FAULT DETECTION OPS CKS GOOD PER MM 26-16-00. 2 L 7 2 4F RT A35EU 2001081300214 20010813 00214 NM 2001 8 13 ABXA010436 1 20010809 A 2160 32155801 VALVE BOEING 767 767281 1385109 NM DEFECTIVE A ABXA K NONE G MULTIPLE FAILURE AP APPROACH 1 GL 23 783AX 1249 23016 FLIGHT DECK TEMP. CONTROL FAILED TO CONTROL DESIRED TEMP. IN AUTO OR MANUAL. ALSO NO TEMP. CONTROL WITH ANY SELECTOR. DU RING APPROACH, NAV EQUIPMENT BEGAN ERONEOUS INDICATIONS, AUTO PILOT DISENGAGED, F/O'S DU-1 FAILED, THEN F/O'S DU-2 FAILE D. F/O'S FMC FAILED, G/A FUNCTION ALSO FAILED. SUSPECT DUE TO UNCONTROLLABLE TEMP. CONTROL. REPLACED FLIGHT DECK ZONE DU CT OVERHEAT RELAY PER BLOCK 41. REPLACED TRIM AIR PRESSURE REGULATING VALVE IAW B767 AMM 21-61-06-4. OPS CHECKED GOOD. C OMPLIED WITH B767 FIM 21-60-00. 2 L 7 2 4F RT A1NM 2001081300215 20010813 00215 WP 2001 8 13 ABXA010437 1 20010731 A 5311 9923409502 FRAME DOUG DC9 DC941 302207N WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 990AX 47493 FRAME AT STATION 737 RIGHT UPPER FORWARD FLANGE WAS CRACKED. REPLACED FRAME AT STATION 737 RIGHT IAW DC-9 SRM. 2 L 7 2 4F A6WE 2001081300216 20010813 00216 WP 2001 8 13 ABXA010438 1 20010731 A 5300 49125391N FITTING DOUG DC9 DC941 302207N WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 990AX 47493 LOWER AFT INBOARD FITTING CRACKED AT 1041 BULKHEAD LEFT. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 2001081300217 20010813 00217 WP 2001 8 13 ABXA010439 1 20010731 A 5300 491627041 FITTING DOUG DC9 DC941 302207N WP LEFT KEEL CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 990AX 47493 FRAME TO HAT CHANNEL FITTING INBOARD VERTICAL LEG CRACKED AT STATION 600, LONGERON 29 LEFT. REPLACED FITTING IAW DC-9 SR M 51-30-5. 2 L 7 2 4F A6WE 2001081300218 20010813 00218 EU 2001 8 13 DHL2001362028 1 20010811 A 7810 NOZZLE AIRBUS 300 A300B4203 3930306 EU NR 2 ENGINE CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 84 AT A4 CHECK NR 2 ENG EXHAUST NOZZLE CHAFFED THROUGH AT 8 O'CLOCK POSITION. REMOVED AND REPLACED NR 2 ENG EXHAUST NOZZLE PER A300 MM 78-00-00 2 L 7 2 4F RT A35EU 2001081300219 20010813 00219 NM 2001 8 13 ZW0A0106701 1 20010811 A 3350 6100928 LAMP BOEING 767 7673Y0 NM L2 DOOR A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 632TW 24953 THE EGRESS LIGHT FWD OF THE RH SIDE NUMBER 2 CABIN DOOR WAS INOPERATIIVE. REPLACED THE LAMP. CHECK-C 3-22-01 LAX. --C LOSED-- 2 L 7 2 4F RT A1NM 2001081300220 20010813 00220 WP 2001 8 13 ARWA0010804 1 20010813 A 5101 STRINGER DOUG DC8 DC861F 3021953 WP CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING SCHEDULED MAINTENANCE:FOUND 2 INCH CRACK AT STATION 940 STRINGER 23R.CORRECTIVE ACTION:REPAIRED I.A.W. E.O. DRAWI NG # AS11300 DATED 08/09/01 2 L 7 4 4F 4A25 2001081300221 20010813 00221 WP 2001 8 13 ARWA0010805 1 20010813 A 5313 STRINGER DOUG DC8 DC861F 3021953 WP FUSELAGE CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING SCHEDULED MAINTENANCE:FOUND 2 INCH CRACK AT STATION 940 STRINGER 23R.REPAIRED IAW EO DRAWING NR AS11300 DATED 08/ 09/01 2 L 7 4 4F 4A25 2001081300222 20010813 00222 NM 2001 8 13 AWXA0002102 1 20010811 A 5310 65457788 SKIN BOEING 737 7373G7 1384595 NM CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 332AW 23384 D: 1/4" crack at right aft service door lower hinge cut out BS 948C: removed damaged and installed repair doubler IAW B7 37 SRM 53-60-01 figure 207 sheet 1-8 2 L 7 2 4F RT A16WE 2001081300223 20010813 00223 NM 2001 8 13 AWXA0002109 1 20010801 A 5312 6573741219 DOUBLER BOEING 737 73733A 1384673 NM BS 318 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 D: R1 door lower aft corner repair doubler fwd edge cracked 1/4" at taper fuselage cut out BS 318C: removed and replaced tapered filler 2 L 7 2 4F RT A16WE 2001081300224 20010813 00224 NM 2001 8 13 AWXA0002107 1 20010802 A 5313 672038U2 INTERCOSTAL BOEING 737 73733A 1384673 NM INTERCOSTAL CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 D: RT Intercostal cracked BS 178 BLKHD. RBL 24 WL 195 confirmed HFECC: Removed and replaced Intercostal IAW B737-300 SRM 51-40-02 pg 22 2 L 7 2 4F RT A16WE 2001081300225 20010813 00225 NM 2001 8 13 AWXA0002106 1 20010809 A 5313 146N5187 INTERCOSTAL BOEING 757 7572S7 1384962 NM STA 680 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 903AW 23323 D: Fwd cargo compartment FBSTA 680 RBL 27 intercostal top flange cracked.C: Removed cracked top flange. Drilled end inst alled new top flange per SRM 51-30-01 pg 1 51-40-02 fig 12 pg 7 2 L 7 2 4F RT A2NM 2001081400001 20010814 00001 EU 2001 8 14 DHL2001362029 1 20010812 A 7110 CHANNEL AIRBUS 300 A300B4203 3930306 EU T/R COWLING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 84 A4 CHECK NR 2 ENG O/B REVERSER COWL, BUMPER HAT SECTION HAS A CRACK. REMOVED & REPLACED NR 2 ENG O/B REVERSER COWL, BUMP ER HAT SECTION IAW A-300-SRM-51-30-30 PAGE 8 2 L 7 2 4F RT A35EU 2001081400002 20010814 00002 EU 2001 8 14 DHL2001363011 1 20010730 A 5320 RETAINER AIRBUS 300 A300B4203 3930306 EU FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 A CHECK - SEAL DEPRESSOR DAMAGED AT NR 2 LOWER CARGO DOOR CUTOUT, AFT UPPER VERTICAL AREA BELOW CORNER FOR APPROX 8 INCH ES. REMOVED DAMAGED SEAL DEPRESSOR AT NR 2 LOWER CARGO DOOR BELOW AFT UPPER CORNER. STOP DRILLED CRACK IN SEAL DEPRESSOR . INSTALLED TEMPORARY REPAIR. 2 L 7 2 4F RT A35EU 2001081400003 20010814 00003 EU 2001 8 14 DHL2001363012 1 20010730 A 2550 PANEL AIRBUS 300 A300B4203 3930306 EU CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 A CHECK-- LOWER AFT BLOW OUT PANEL 44L, HAS CRACK AT UPPER EDGE. REPAIRED LOWER AFT CARGO BLOW-OUT PANEL 44L. 2 L 7 2 4F RT A35EU 2001081400005 20010814 00005 EU 2001 8 14 DHL2001363013 1 20010728 A 5412 BULKHEAD AIRBUS 300 A300B4203 3930306 EU NR 1 PYLON CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 A CHECK--CORROSION AT LWR SURFACE AT NR 1 PYLON LWR BULKHEAD AFT OF ENGINE MOUNT SHIM PLATE. REMOVED CORROSION FROM LOWE R SURFACE AT NR 1 PYLON AFT OF ENGINE MOUNT SHIM PLATE IAW A300 SRM 51-40-11 2 L 7 2 4F RT A35EU 2001081400006 20010814 00006 EU 2001 8 14 DHL2001363014 1 20010728 A 5330 SKIN AIRBUS 300 A300B4203 3930306 EU FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 A CHECK -- RT FUSELAGE SKIN, 2 DENTS, BETWEEN NR 2 AND NR 3 AFT CARGO DOORS. STRAIGHTENED DENTED AREAS OF EXTERNAL SKIN (2 PLACES) IAW A300 SRM 51-40-1. 2 L 7 2 4F RT A35EU 2001101900082 20011019 00082 EU 2001 10 19 DHL2001364022 1 20010720 A 5320 ATTACH ANGLE AIRBUS 300 A300B4203 3930306 EU FUSELAGE GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 INSPECTION REVEALED GOUGE AFT OF LEFT HAND DRAIN HOLE FRAME 80 STA 4944, 1 INCH INBOARD OF STR 56L. GOUGE EXTENDS THRU INNER ATTACHMENT ANGLE AND INTO OUTER ATTACHMENT ANGLE. 2 L 7 2 4F RT A35EU 2001081400007 20010814 00007 EU 2001 8 14 DHL2001364023 1 20010729 A 2720 COMPUTER AIRBUS 300 A300B4203 3930306 EU RUDDER MALFUNCTIONED A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 364DH 141 SYSTEM 2 RUDDER TRAVEL NR 2 WILL NOT STAY ON, ACCOMPLISHED ABNORMAL PROCEDURE. REPLACED NR 2 ART FEEL COMPUTER .OPS CHEC K NORMAL AS PER 27-20-00. 2 L 7 2 4F RT A35EU 2001081400008 20010814 00008 EU 2001 8 14 DHL2001365019 1 20010717 A 5411 RIB AIRBUS 300 A300B4203 3930306 EU NR 2 PYLON CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH 149 NR 2 PYLON VERTICAL STIFFENER RIB 15 HAS 2 CRACKSREPAIRED CRACKED RIB FITTING 15 ON NR 2 PYLON. 2 L 7 2 4F RT A35EU 2001081400009 20010814 00009 WP 2001 8 14 ABXA010441 1 20010812 A 5700 4912005506 FITTING DOUG DC9 DC941 302207N WP LEFT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 956AX 47620 DURING REPLACEMENT OF THE LEFT WING LOWER AFT SPAR, INSPECTION FOUND WING BULKHEAD ATTACH FITTING CRACKED. REPLACED FITT ING IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2001081400010 20010814 00010 WP 2001 8 14 ABXA010442 1 20010812 A 5700 4912005503 FITTING DOUG DC9 DC941 302207N WP LEFT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 956AX 47620 DURING REPLACEMENT OF THE LEFT WING LOWER AFT SPAR, INSPECTION FOUND WING BULKHEAD ATTACH FITTING CRACKED. LOCATED AT ST ATION XRS 111, STRINGER 11. REPLACED FITTING IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2001081400011 20010814 00011 EU 2001 8 14 DHL2001365020 1 20010721 A 2560 SMOKE BARRIER AIRBUS 300 A300B4203 3930306 EU COCKPIT DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH 149 SMOKE VAPOR BARRIER HAS TWO HOLES CUT IN IT.R&R VAPOR BARRIER IAW CMM 25-50-02 2 L 7 2 4F RT A35EU 2001081400012 20010814 00012 NM 2001 8 14 CA010808061 1 20010803 A 2612 356644400 FIRE LOOP BOEING 727 727227 1384078 NM PWA JT8 JT8D9A 52048 NE LT WHEEL WELL CORRODED W O OTHER N FALSE WARNING AP APPROACH 1 CA (CAN) ON FINAL APPROACH INTO YMX PILOTS RECIEVED WHEEL WELL FIRE INDICATION, WHEEL WELL LIGHT ON WITH THE FIRE BELL.PILO TS CARRIED OUT EMERGENCY CHECKLIST DECLARED AN EMERGENCY. PILOTS LANDED WITH NO FURTHER PROBLEMS. UPON INSPECTION IT W AS NOTED THAT THE CONNECTOR FOR THE FIRE LOOP WAS CORRODED. THE FIRE LOOP WAS REPLACED AND FUNCTION TESTED. THE AIRCRA FT WAS THEN RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2001081400014 20010814 00014 NM 2001 8 14 2001UALA01403 1 20010718 A 3230 AC11504K0232 HOSE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RUPTURED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 543UA 25698 DURING CLIMBOUT PASSING 18000, L HYD QTY EICAS CAME ON. LEFT HYDRAULIC PUMPS WERE SHUTOFF. SUPPLEMENTAL DATA UPDATE LEFT GEAR DOWN LOCK ACTUATOR HOSE RUPTURED. REPLACED DOWN LOCK HOSE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001081400015 20010814 00015 NM 2001 8 14 2001UALA01524 1 20010727 A 2781 WIRE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE #1 SLAT BROKEN A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 664UA 29236 LE SLAT ASYM EICAS MSG DISPLAYED DURING FLAP RETRACTION. RETURNED TO FIELD. SUPPLEMENTAL DATA UPDATE CAUSE: A BROKEN WIR E (401-002-20) IN THE SLAT SKEW SYSTEM SIMULATED A TRIPPED SLAT SKEW SWITCH INDICATING A SLAT SKEWED (ASYMMETRY) CONDITI ON. THE FLAP/SLAT ELECT UNIT (FSEU) RECEIVED THE SIGNAL SENSING A SKEWED CONDITION AND INITIATED SLAT/FLAP FAILURE PROT ECTION SHUT DOWN AND ILLUMINATED THE AMBER 'LE SLAT' LIGHT AND 'LE SLAT ASYM' EICAS MESSAGE . CORRECTION: THE SUBJECT W IRE HARNESS WAS REPLACED. THE FLAP/SLAT SYSTEM WAS OPERATIONALLY CHECKED PER APPLICABLE MAINTENANCE MANUAL. ALL OPS CH ECK NORMAL WITH NO REPORTED DISCREPANCIES. 2 L 7 2 4F 4 F RT A1NM E24NE 2001081400016 20010814 00016 NM 2001 8 14 2001UALA01561 1 20010722 A 5210 AN960C516L WASHER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE DPLOY BAR A UALA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 WP 29 655UA 25393 DURING EMERGENCY EVACUATION DOOR 2L FAILED TO FULLY OPEN. SUPPLEMENTAL DATA UPDATE FOUND SNAP RING AND WASHER (CMM 25-66 -30-1003 ITEM 65 & 70 RESPECTIVELY) MISSING ON AFT SEPARATOR LINK ASSY (CMM 25-66-30-1003 ITEM 80)REPLACED PARTS AS NECE SSARY; REINSTALLED ASSEMBLY AND PERFORMED ESCAPE SLIDE DEPLOYMENT SIMULATION WITH NO DEFECTS NOTED.RING MFG P/N MS166 24-4031 2 L 7 2 4F 4 F RT A1NM E24NE 2001081400017 20010814 00017 NM 2001 8 14 2001UALA01597 1 20010803 A 2780 31EN16 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 521UA 24891 DURING FLAP RETRACTION ON TAKEOFF LEADING EDGE CAUTION LIGHT AND LEADING EDGE ASSYM EICAS MSG ILLUMINATED. FLIGHT CONTRO L NOT AFFECTED SUPPLEMENTAL DATA UPDATE LEADING EDGE SLAT LOSS SENSOR SWITCH FAILED.REPLACED RIGHT INBOARD LEADING EDGE LOSS SENSOR SWITCH S10338. 2 L 7 2 4F 4 F RT A2NM E17NE 2001081400018 20010814 00018 NM 2001 8 14 2001UALA01612 1 20010804 A 3230 AC11504K0232 HOSE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RUPTURED A UALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 WP 29 506UA 24627 TOTAL LOSS OF LEFT HYDRAULIC SYSTEM FLUID AFTER TAKEOFF. SUPPLEMENTAL DATA UPDATE LEFT GEAR DOWNLOCK ACTUATOR HOSE RUPTU RED. REPLACED HOSE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001081400019 20010814 00019 NM 2001 8 14 2001UALA01613 1 20010804 A 2780 31EN16 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 504UA 24625 "LE SLAT ASYM" EICAS MSG AND "LEADING EDGE" CAUTION LIGHT CAME ON IN CRUISE. NO FLAP MOVEMENT WITH HANDLE, ALTERNATE FLA PS WORKED FINE. SUPPLEMENTAL DATA UPDATE LEADING EDGE SLAT LOSS SENSOR SWITCH FAILED.REPLACED RIGHT INBOARD LEADING EDGE LOSS SENSOR SWITCH S10338. 2 L 7 2 4F 4 F RT A2NM E17NE 2001081400020 20010814 00020 NM 2001 8 14 2001UALA01643 1 20010801 A 5300 SEAT TRACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 179UA 25158 STA 1840 TO 1856 24" RBL SEAT TRACK OTBD FLANG CRACK. SUPPLEMENTAL DATA UPDATE MRR ENTERED IN ERROR SEAT TRACKS ARE NOT PSE'S. 2 L 7 4 4F 4 F RT A20WE E24NE 2001081400021 20010814 00021 NM 2001 8 14 2001UALA01645 1 20010801 A 5311 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 EXTERNAL FUSELAGE SKIN DENTED STA 625 TO 637 AT SKIN LAP STRINGER 14L. MAJOR REPAIR ACCOMPLISHED FOR STRINGER REPAIR. EXTERNAL SKIN FLEXED BACK. 2 L 7 2 4F 4 F RT A2NM E17NE 2001081400022 20010814 00022 EU 2001 8 14 2001UALA01647 1 20010806 A 2910 VT477 INDICATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 447UA 836 ON CLIMB, RECEIVED YELLOW HYDRAULIC RESERVOIR OVERHEAT WARNING. SUPPLEMENTAL DATA UPDATE FOUND YELLOW SYSTEM OVER SERVIC ED. REMOVED EXCESS HYDRAULIC FLUID AND ALSO REPLACED REMOTE HYDRAULIC QUANTITY INDICATOR FOR A STUCK NEEDLE TO PREVENT RECURRENCE. 2 L 7 2 4F 4 F RT A28NM E40NE 2001081400024 20010814 00024 EU 2001 8 14 DHL2001365021 1 20010714 A 5311 FRAME AIRBUS 300 A300B4203 3930306 EU FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH 149 A-1 CHECK--MAIN CABIN RT FWD SIDE AT TOP OF GILL LINER FRAME DENTED AND CRACKED FR 22. CUT OUT DAMAGED FRAME IN MAIN CAB IN RT FWD SIDE AT TOP OF GILL LINER. INSTALLED REPAIR. 2 L 7 2 4F RT A35EU 2001081400025 20010814 00025 EU 2001 8 14 DHL2001365022 1 20010714 A 3610 1891201 HEAT EXCHANGER AIRBUS 300 A300B4203 3930306 EU NR 2 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH 149 A-7 CHECK - NR 2 ENGINE PYLON HEAT EXCHANGER HAS 5 INCH CRACK. REMOVED AND REPLACED HEAT EXCHANGER. 2 L 7 2 4F RT A35EU 2001081400026 20010814 00026 EU 2001 8 14 DHL2001365023 1 20010714 A 5411 RIB AIRBUS 300 A300B4203 3930306 EU NR 2 PYLON CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH 149 A-7 CHECK - NR 2 PYLON O/B RIB 15 HAS RIVET MISSING AND RIB ON BACK SIDE CRACKED. REMOVED VERTICAL RIB AFT OF OVAL ACCES S DOOR ON O/B SIDE OF NR 2 ENG PYLON THD-A300-SRM-54-10.3) STOP DRILLED CRACKS ON RIB, INSTALLED REPAIR ANGLE. 2 L 7 2 4F RT A35EU 2001081400027 20010814 00027 EU 2001 8 14 DHL2001365025 1 20010727 A 3260 LIGHT AIRBUS 300 A300B4203 3930306 EU COCKPIT INOPERATIVE A DHLA K NONE N FALSE WARNING NR NOT REPORTED 1 SO 01 365DH 149 PILOT'S RT MLG GREEN LIGHT IS OUT OF SERVICE, ACCOMPLISHED MAIN LANDING GEAR ABNORMAL LANDING WITHOUT EVENT. RELAMPED AN D OPS CK'D RT MAIN GRN LIGHT PER MM 32-61-00. 2 L 7 2 4F RT A35EU 2001081400028 20010814 00028 EU 2001 8 14 DHL2001365026 1 20010802 A 2510 SHOULDER BELT AIRBUS 300 A300B4203 3930306 EU COCKPIT LACK OF LUBE A DHLA K NONE O OTHER NR NOT REPORTED 1 SO 01 365DH 149 SHOULDER HARNESS ON COCKPIT JUMPSEAT WILL NOT EXTEND PROPERLY. LUBED SHOULDER HARNESS LOCK CABLE IAW MM 25-11-14. 2 L 7 2 4F RT A35EU 2001081400029 20010814 00029 EU 2001 8 14 C2XA01BT151 1 20010814 A 3350 FST5X201A FUSE AEROSP ATR42 ATR42320 8680930 EU BLOWN A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 14833 188 BTV---CO2930, DURING 3A INSPECTION MAINTENANCE FOUND EMERGENCY LIGHT IN PASSENGER DOOR TO BE INOPERATIVE. MAINTENANCE R EMOVED AND REPLACED FUSE IN POWER SUPPLY IAW ATR42 CMM 33-51-21. OPS.CHECKED GOOD. 2 H 7 2 4T RT A53EU 2001081400030 20010814 00030 EU 2001 8 14 DHL2001365027 1 20010802 A 2611 CG7GF SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU COCKPIT MALFUNCTIONED A DHLA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 365DH 149 FLT DECK SMOKE LIGHT ILLUMINATED ON 2ND OFFICERS PANEL AND MWP. REPLACED FLT DECK SMOKE DETECTOR IAW M/M 26-11-12 OPS CK IS GOOD ALL P/N CG7GF S/N OFF 3066 S/N ON 2872. 2 L 7 2 4F RT A35EU 2001081400031 20010814 00031 EU 2001 8 14 DHL2001365029 1 20010811 A 2612 FIRE LOOP AIRBUS 300 A300B4203 3930306 EU NR 2 ENGINE FAILED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 365DH 149 NR 2 ENG FIRE DETECTION LOOP A WILL NOT TEST. DEFERRED PER MEL 26-13-03. STATUS: OPEN 2 L 7 2 4F RT A35EU 2001081400032 20010814 00032 EU 2001 8 14 DHL2001366019 1 20010721 A 7110 BRACKET AIRBUS 300 A300B4203 3930306 EU NR 1 COWLING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 366DH 249 A1 CHECK - NR 1 ENG O/B COWL CENTER LATCH HAS 2 S/M ANGLE BRACKETS CRACKED (T/R DOOR CENTER)REMOVED BRACKETS (2 EACH),W ELDED, AND INSTALLED BRACKETS (2 EACH) AT NR 1 ENG O/B COWL CENTER LATCH AS PER A300 M/M 71-13-00 2 L 7 2 4F RT A35EU 2001102300075 20011023 00075 EU 2001 10 23 DHL2001366020 1 20010824 A 2621 FIRE BOTTLE AIRBUS 300 A300B4203 3930306 EU APU DEFECTIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 366DH 249 APU AUTOMATIC FIRE SHUTDOWN SYSTEM WILL NOT TEST. REPLACED APU FIRE EXTINGUISHER BOTTLE AND CARTRIDGE ASSEMBLY IAW M/M 2 6-22-11. OPS CHECKED GOOD. 2 L 7 2 4F RT A35EU 2001081400033 20010814 00033 EU 2001 8 14 DHL2001366022 1 20010803 A 3040 4099593 WINDSHIELD WIPER AIRBUS 300 A300B4203 3930306 EU WINDSHIELD WORN A DHLA K NONE O OTHER NR NOT REPORTED 1 SO 01 366DH 249 WINDSHIELD WIPERS INEFFECTIVE ON BOTH SIDES. RAI BOTH WINDSHIELD WIPER BLADES IAW MM 30-40-13. OPS CHECKED GOOD. P/N OF F 4099593 P/N ON 4099593 2 L 7 2 4F RT A35EU 2001081400034 20010814 00034 EU 2001 8 14 DHL2001366504 1 20010721 A 7830 FAIRING AIRBUS 300 A300B4203 3930306 EU NR 2 T/R DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 366DH 249 A1 CHECK - REMOVED APPROX 24 INCHES OF FILLET FAIRING INSIDE REVERSER COWL AT 6:00 O/B SIDE OF NR 2 ENGINE . INSTALLED N EW FLUSH DOUBLER IAW 54-41-10. 2 L 7 2 4F RT A35EU 2001081400035 20010814 00035 EU 2001 8 14 DHL2001366505 1 20010721 A 7110 BRACKET AIRBUS 300 A300B4203 3930306 EU NR 1 COWLING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 366DH 249 A1 CHECK - NR 1 ENG O/B COWL CENTER LATCH HAS 2 S/M ANGLE BRACKETS CRACKED (T/R DOOR CENTER)REMOVED BRACKETS(2 EACH) WE LDED, AND INSTALLED BRACKETS (2 EACH) AT NR 1 ENG O/B COWL CENTER LATCH AS PER A300 M/M 71-13-00 2 L 7 2 4F RT A35EU 2001081400036 20010814 00036 EU 2001 8 14 DHL2001366506 1 20010723 A 7830 SUPPORT AIRBUS 300 A300B4203 3930306 EU NR 2 T/R CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 366DH 249 A CHECK - NR 2 ENGINE THRUST REVERSER BLOCKER DOOR SEAL SUPPORT AT 7 O'CLOCK POSITION IS CRACKED. REMOVED DAMAGED AREA N R 2 ENGINE T/R BLOCKER DOOR SEAL SUPPORT I/A/W A-300 SRM 51-30-30. INSTALLED REPAIR DOUBLER I/A/W A-300 SRM 54-00-00 FIG URE 706. 2 L 7 2 4F RT A35EU 2001081400037 20010814 00037 EU 2001 8 14 DHL2001366507 1 20010722 A 7110 COWLING AIRBUS 300 A300B4203 3930306 EU NR 2 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 366DH 249 A CHECK - NR 2 ENGINE AFT COWLING AT 7 O'CLOCK HAS A CRACK.STOP DRILLED CRACK. INSTALLED DOUBLER REPAIR AS PER A-300 SRM 54-00-00 FIGURE 708. 2 L 7 2 4F RT A35EU 2001081400038 20010814 00038 EU 2001 8 14 DHL2001367013 1 20010803 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU CABIN MALFUNCTIONED A DHLA K NONE N FALSE WARNING UK UNKNOWN 1 SO 01 367DH 265 SMOKE DETECTOR 14R STATION 1813 LIGHT IN COCKPIT CAME ON AT 75F. R&R NUMBER 14 SMOKE DETECTOR AS PER MM 26-11-00, GROUND OPS NORMAL. 2 L 7 2 4F RT A35EU 2001081400039 20010814 00039 NM 2001 8 14 DHL2001705004 1 20010809 A 2612 POWER UNIT BOEING 727 72722C 138400F NM APU FAILED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 705DH 19191 APU FIRE TEST INOP. REMOVED & REPLACED POWER UNIT IAW 26-15-0 OPS CHECK NORMAL. 2 L 7 3 4F A3WE 2001081400040 20010814 00040 NE 2001 8 14 DHL2001707009 2 20010804 A 7532 BLEED VALVE BOEING 727 72722 1384002 NM PWA JT8 JT8D7B 52053 NE NR 1 ENGINE FAILED A DHLA E ENGINE SHUTDOWN J WARNING INDICATION TO TAKEOFF 1 SO 01 707DH 18321 T/O THRUST LEFT MANIFOLD DUCT PRESSURE ROSE TO 100PSI DEFERRED PER MAINT. CONTROL 36-11-1 MB. WHEN ATTEMPTING TO START E NGINES TO CHECK PRESSURIZATION, NR 1 ENG WOULD NOT START. NO DUCT PRESSURE DROP AND START VALVE OPEN LIGHT DID NOT ILLU MINATE. RESET C/B- NO HELP. R&R BLEED CONTROL VALVE NR 1 ENG. OPS CK'S GOOD IAW M/M 36-10-1. NO LEAKS NOTED. 2 L 7 3 4F 4 F A3WE E2EA 2001081400041 20010814 00041 NM 2001 8 14 DHL2001707010 1 20010804 A 7930 SWITCH BOEING 727 72722 1384002 NM PWA JT8 JT8D7B 52053 NE NR 2 ENGINE MALFUNCTIONED A DHLA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 707DH 18321 NR 2 ENGINE OIL PRESSURE LIGHT CAME ON DIM DURING FLIGHT. COULD EXTINGUISH LIGHT BY RETARDING THRUST TO IDLE INITIALLY. BUT EVENTUALLY CAME ON AT IDLE. OIL TEMP READING 135. QUANTITY DECREASED FROM 4.2 GAL AT T/O. R&R MAIN OIL FILTER, FOUND SOME CARBON BB'S NO METAL. RAN ENG PER JRH 5.2 TO T/O THRUST AND PERFORMED POWER ASSURANCE RUN AFTER PERFORMING LOW PO WER LEAK CHECK & ENG OIL PRESS & TEMP CHECK. REEXAMINED MAIN OIL. SCREEN NO FOD FOUND, REINSTALLED & CLOSED ENG TRIM SHE ET SENT TO POWERPLANT, PERFORMED BREATHER TEST PER P/W M/M 72-00, CHECKS NORMAL ENG OK FOR SERV. REPLACED NR 2 ENG OIL F ILTER BY-PASS SWITCH PER M/M 79-33-2 OPS CHECK & LEAK CHECK SERVICEABLE P/N & S/N ON OFF. 2 L 7 3 4F 4 F A3WE E2EA 2001081400042 20010814 00042 NM 2001 8 14 DHL2001708009 1 20010721 A 2612 FIRE LOOP BOEING 727 72725 1384006 NM NR 1 ENGINE OUT OF POSITION A DHLA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 708DH 18275 ENGINE NR 1 DETECTOR CIRCUIT GRD WAS ILLUMINATED ON TAXI OUT FROM MCO. FOUND NR 1 ENG LOOP TOUCHING A BRACKET. REPOSITIO NED LOOP. SYS NOW OPS CHECK NORMAL PER M/M 26-11-0. 2 L 7 3 4F A3WE 2001081400043 20010814 00043 NM 2001 8 14 AALA20014037 1 20010525 A 5300 148N3138 STRAP BOEING 757 757223 1384957 NM A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 689AA 25731 AFW - FOUND STRAPS AT STATION 1825 JUST BELOW STRINGER 3R HAD INTERGRANULAR CORROSION AT NUT PLATE ATTACH HOLES. TRIMME D OUT DAMAGED AREA PER SRM. REMOVED ALL CORROSION/CRACK PER SRM. FABRICATED REPAIR STRAP 7075-T6AL .125 THICK ALODINE AND PRIMED. INSTALLED PARTS WET WITH BMS 595 SEALANT AND USE EXISTING FASTENER. (M) 2 L 7 2 4F RT A2NM 2001081400044 20010814 00044 NM 2001 8 14 AALA20011370 1 20010707 A 3350 PIN BOEING 757 757223 1384957 NM A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 640A 24598 MIA - DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY EXIT LIGHT AT SEAT 22D INOPERATIVE. RE-SEATED EMEREGNCY EXIT PIN AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001081400045 20010814 00045 WP 2001 8 14 USAAD01134 1 20010709 A 3350 AD4002P BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 809US 48041 IND - THE LOW LEVEL EMERGENCY LIGHTS AND THE LEFT AFT EXIT WINDOW SIDEWALL LIGHT FAILED TO TEST. MAINTENANCE REPLACED T HE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001081400046 20010814 00046 NM 2001 8 14 USAASB01190 1 20010703 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM MID CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 524AU 23859 PIT - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT ROWS 9 AND 11 THROUGH 16 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001081400047 20010814 00047 NM 2001 8 14 USAASB01188 1 20010630 A 3350 6104789 BATTERY PACK BOEING 737 7372B7 1384560 NM FWD CARGO COMPT INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 284AU 23131 THE L1 AND L2 EXTERIOR EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK. (M) 2 L 7 2 4F A16WE 2001081400048 20010814 00048 NM 2001 8 14 USAABB01052 1 20010701 A 3350 9221009 BATTERY BOEING 757 7572B7 1384964 NM L2 DOOR DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 27122 BDL - FOUND THE L2 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2001081400049 20010814 00049 NM 2001 8 14 CALA0100760 1 20010813 A 5230 SKIN BOEING 737 7373T0 1384582 NM C-2 DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14325 23455 INSPECTION FOUND THREE DENTS IN C-2 DOOR SKIN AT TEN INCHES FROM AFT SIDE AND FROM FIVE INCHES ABOVE PAINT LINE TO THIRT EEN INCHES ABOVE PAINT LINE. THE DENTED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 52-00-01. 2 L 7 2 4F RT A16WE 2001081400050 20010814 00050 NM 2001 8 14 DHL2001708010 1 20010722 A 2612 FIRE LOOP BOEING 727 72725 1384006 NM NR 1 ENGINE GROUNDED A DHLA K NONE N FALSE WARNING CR CRUISE 1 SO 01 708DH 18275 NR 1 FIRE PROTECTION DET CIRCUIT GRD LIGHT ILLUMINATED IN FLT. FOUND ON ENG NR 1 FIRE PROTECTION LOOP WAS GROUNDING ON ENGINE COWLING, REPOSITIONED LOOP IAW B727 M/M 26-11-000 OPS CHECK SERVICEABLE. 2 L 7 3 4F A3WE 2001081400051 20010814 00051 NM 2001 8 14 PCAA0108089 1 20010809 A 3350 82410162005 CONTROL BOX DHAV DHC8 DHC8102 2809003 NM FALSE ACTIVATION A PCAA K NONE O OTHER LD LANDING 1 EA 13 806EX 263 LGA FLIGHT#3533. DURING TAXI EMERGENCY LIGHTS CYCLED ON AND OFF. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY AND FOUND S YSTEM TO BE OPERATING NORMALLY. AIRCRAFT RETURNED TO SERVICE.BWI FLIGHT#3538 PROBLEM REOCCURED AS EMERGENCY LIGHTS CYCLE D ON AND OFF DURING LANDING. MAINTENANCE REPLACED EMERGENCY LIGHT CONTROL BOX. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001081400052 20010814 00052 NM 2001 8 14 DHL2001709010 1 20010719 A 2612 FIRE LOOP BOEING 727 72782C 1384026 NM NR 1 ENGINE INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 709DH 19968 NR 1 ENGINE FIRE DETECTION SYSTEM WILL NOT TEST NR 1 ENG FIRE WALL TEST INOP. INSTALLED OVERHAULED ENGINE SENSOR LOOP I AW WITH B-M/M 26-11-021 R&R FIRE SENSOR/RESPONDER IAW B-727 M/M 26-11-31 ON NR 1 ENG, OPS CHECK SERVICEABLE. 2 L 7 3 4F A3WE 2001081400053 20010814 00053 NM 2001 8 14 DHL2001715010 1 20010810 A 5330 SKIN BOEING 727 727155C 138404Z NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 BELOW RIGHT CORNER OF MAIN CARGO DOOR (APPROX 3 FEET) A 4 INCH BY 1/4 GASH IN SKIN APPROX 1/4 DEEP. AREA IS ALSO DENTED, ALSO 2 AREAS ADJACENT TO GASH ARE DOWN TO BARE METAL. CUTOUT DAMAGED AREA. FABRICATED DOUBLER REPAIR & FILLER. REPAIR M ADE TO DAMAGED SKIN AT STA 600 AND STR 26L PER BOEING MESSAGE DHLR0108010. 2 L 7 3 4F A3WE 2001081400054 20010814 00054 NE 2001 8 14 DHL2001717016 2 20010720 A 7200 ENGINE BOEING 727 72723 1384004 NM PWA JT8 JT8D7B 52053 NE NR 3 ENGINE MALFUNCTIONED A DHLA K NONE X ENGINE FLAMEOUT AP APPROACH 1 SO 01 717DH 19389 653994 NR 3 ENGINE QUIT ON FINAL APPROACH. UPON COMPLETION OF MX PERFORMED POWER ASSURANCE RUN OF NR 3 ENG. IAW DHL JRH 7.7 & 7.8. ALL PARAMETERS NORMAL. OK FOR SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2001081400055 20010814 00055 NM 2001 8 14 DHL2001717017 1 20010720 A 7333 PACKING BOEING 727 72723 1384004 NM PWA JT8 JT8D7B 52053 NE FUEL FLOW TRANS DETERIORATED A DHLA K NONE K J FLUID LOSS WARNING INDICATION UK UNKNOWN 1 SO 01 717DH 19389 653994 NR 3 ENGINE FUEL FLOW INDICATES 1000PPH HIGHER THAN 1 AND 2 ENGINES. ALL OTHER ENGINE PARAMETERS NORMAL NR 3 POWER LEVE R READS 1&2 POWER LEVERS BY 2 INCHES. FOUND FUEL FLOW TRANSMITTER OUTLET PACKING DETERIORATED & TRANSMITTER LEAKING SEVE RELY. REPLACED PACKING IAW B727 M/M 73-31-1. GRND RAN ENGINE PER JRH 7.8. NO LEAKS NOTED. ALL IND NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001081400056 20010814 00056 NM 2001 8 14 DHL2001720011 1 20010721 A 3310 LIGHT BOEING 727 727228 NM COCKPIT MISINSTALLED A DHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 720DH SMOKE APPEARS NEAR S/O PANEL FLUORESCENT LIGHT.LIGHTS POP BREAKER.FOUND AFT TABLE LIGHT IMPROPERLY INSTALLED & HEATING I NSULATION. REIN-STALLED LIGHT ASSY. 2 L 7 3 4F A3WE 2001081400057 20010814 00057 NM 2001 8 14 DHL2001721005 1 20010720 A 2781 TRANSMITTER BOEING 727 727228 NM L/E FLAP FAILED A DHLA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 721DH 19544 NR 2 LE FLAP FAILED TO RETRACT. ACCOMPLISHED ABNORMAL PROCEDURE THEN COULD NOT GET NR 2 LE FLAP TO EXTEND. ACCOMPLISHE D ABNORMAL PROCEDURE LANDED OK. REMOVED AND REPLACED NR 2 LE FLAP POSITION TRANSMITTER IAW 27-82-1. 2 L 7 3 4F A3WE 2001081400058 20010814 00058 NM 2001 8 14 DHL2001726002 1 20010805 A 2611 CIRCUIT BREAKER BOEING 727 727228 NM COCKPIT FAILED A DHLA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 726DH 20409 NR 1 FWD SMOKE DETECTOR LIGHT CAME ON ON PUSH BACK. MAIN DECK CARGO DETECTOR LOOP 2 CIRCUIT BKR WOULD NOT RESET AFTER BE ING PULLED TO RESET ISOLATION VALVES. R&R C/B 9001WH PER WDM 26-11-14. OPS CK SERVICEABLE. SMOKE DET SERVICEABLE PER 26 -11-00. 2 L 7 3 4F A3WE 2001081400059 20010814 00059 NM 2001 8 14 DHL2001726003 1 20010805 A 2613 OVERHEAT LOOP BOEING 727 727228 NM OVERHEAT SYS FAULTY A DHLA B A EMER. DESCENT UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 726DH 20409 LOWER AFT BODY LIGHT ILLUMINATED DURING CLIMB AT 15000 FT. PERFORMED ABNORMAL PROCEDURE. UPON REDUCING THRUST ON NR 1 EN GINE, LIGHT EXTINGUISHED. RETURNED TO CVG. R&R OVERHEAT DETECTION SENSING ELEMENT WITH SERVICEABLE UNIT IAW B MM 26-14-1 . 2 L 7 3 4F A3WE 2001081400061 20010814 00061 2001 8 14 DHL2001727023 4 20010721 A 2210 AUTOPILOT SYS BOEING 727 727228 NM COCKPIT MALFUNCTIONED A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 727DH AUTOPILOT ON SYSTEM A&B JERKS BACK AND FORTH WHEN MAKING TURNS. SOMETIMES THE A/C ROLL IS VIOLENT. THE CONTROL WHEEL OSC ILLATES WITH THESE JERKY TURNS. RESET AUTOPILOT C/B, RERACKED AND CLEANED AUTOPILOT ELEC UNITS CHECK OPS IS GOOD PER D HL MM 22 20. 2 L 7 3 4F A3WE 2001081400062 20010814 00062 2001 8 14 DHL2001727024 4 20010724 A 2213 CONTROL UNIT BOEING 727 727228 NM AUTOPILOT SYS DEFECTIVE A DHLA K NONE F FLT CONT AFFECTED AP APPROACH 1 SO 01 727DH 20204 AUTO-PILOT ON AUTOGLIDE SLOPE ABOUT 300 AGL STAB OUT OF TRIM LIGHT ILLUMINATED THEN AIRCRAFT AGGRESSIVELY WENT NOSE DOWN , BELOW GLIDE SLOPE.REPLACED PITCH CONTROL UNIT IAW B727 MM 22-11-101 OPS CK GOOD 2 L 7 3 4F A3WE 2001081400063 20010814 00063 NM 2001 8 14 DHL2001727025 1 20010807 A 2612 POWER UNIT BOEING 727 727228 NM FIRE DETECTION INOPERATIVE A DHLA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 01 727DH 20204 DURING PREFLIGHT, APU FIRE TEST BECAME INOP.REMOVED AND REPLACED FIRE TEST POWER UNIT IAW 26-15-0. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2001081400064 20010814 00064 NM 2001 8 14 DHL2001740004 1 20010731 A 2612 CONNECTOR BOEING 727 7272Q9 138448M NM FIRE LOOP CONTAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 ENGINE NR 2 A FIRE LOOP INTERMITTENT DURING TEST.REMOVED, CLEANED EXCESS OIL FROM CONNECTORS, RETIGHTENED AND SAFETIED. CHECKED ALL HOLDING CLAMPS, ALL FOUND SECURED. PERFORMED TEST IAW MM 26-11-01 PAGE 501 & 502. NO FAULTS NOTED. 2 L 7 3 4F RT A3WE 2001081400065 20010814 00065 EU 2001 8 14 DHL2001362030 1 20010811 A 7110 COWLING AIRBUS 300 A300B4203 3930306 EU NR 2 ENGINE CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 84 A4 CHECK - NR 2 ENG I/B AFT CORE COWL, CHAFED AT 6 O'CLOCK POSITION AT AFT SECTION. REMOVED AND REPLACED THE NR 2 ENGIN E I/B AFT CORE COWLING AFT SECTION STRIP PER THE A300 MM 71-13-00 2 L 7 2 4F RT A35EU 2001081400066 20010814 00066 EU 2001 8 14 DHL2001362031 1 20010811 A 7110 COWLING AIRBUS 300 A300B4203 3930306 EU NR 2 ENGINE CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 84 A4 CHECK - NR 2 ENG O/B AFT CORE COWL, CHAFFED AT 5 O'CLOCK POSITION AFT SECTION. REMOVED AND REPLACED TRAILING EDGE CLO SE OUT AT NR 2 ENGINE O/B AFT CORE COWL IAW A300 MM 71-13-00 2 L 7 2 4F RT A35EU 2001081400067 20010814 00067 NM 2001 8 14 DHL2001715009 1 20010808 A 3150 WARNING SYSTEM BOEING 727 727155C 138404Z NM COCKPIT MALFUNCTIONED A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 715DH 19618 TAKEOFF WARNING CAME ON AT THE TAKEOFF ROLL, TAXIED CLEAR OF THE RUNWAY AND CYCLED THE FLAPS,TRIM AND SPEED BRAKE SYSTEM WENT BACK TO NORMAL. PERFORMED TAKEOFF WARNING SYS TEST CHECKS GOOD IAW B-727 M/M 31-26-0. 2 L 7 3 4F A3WE 2001081400068 20010814 00068 NM 2001 8 14 DHL2001741013 1 20010731 A 2710 CONTROL VALVE BOEING 727 7272Q9 138448M NM AILERON FAULTY A DHLA O OTHER F J FLT CONT AFFECTED WARNING INDICATION UK UNKNOWN 1 SO 01 741DH 21931 AFTER TURNING ON B-PUMP AILERON SYSTEM B FAILURE LIGHT REMAINED ILLUMINATED 3000PSI NOTED FOR B SYSTEM WITH AILERONS VER Y DIFFICULT TO MOVECLEANED OXIDATION FROM AILERON B SYSTEM SOV AND FROM AIL PRESSURE SWITCH. MANUALLY CYCLED SOV AND IT WOULD DRIVE BACK TO CLOSED.INSPECTED AILERON B SYSTEM LIMIT SWITCH FOR LOOSE WIRE, NONE FOUND,CYCLED B SYSTEM. DURING TA XI THE B SYSTEM AILERON LIGHT ILLUMINATED ON 2 OCCASIONS. EACH FOR 15 TO 20 SECONDS. EACH TIME THE B SYSTEM AILERON SWIT CH WAS CYCLED AND THE PROBLEM CLEARED. REMOVED AND REPLACED B SYS AILERON CONTROL VALVE IAW B727-200 MM 27-10-142, OPS CHECK GOOD REMOVED AND REPLACED PLUG D128 ON SYS B AILERON SHUT-OFF VALVE. 2 L 7 3 4F RT A3WE 2001081400070 20010814 00070 NM 2001 8 14 DHL2001741014 1 20010814 A 2611 SMOKE DETECTOR BOEING 727 7272Q9 138448M NM MAIN CARGO BAY CONTAMINATED A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 741DH 21931 CARGO SMOKE LIGHT ILLUMINATED AT FL 350 0200 ZULU. RAN SMOKE SOURCE IDENTIFICATION CHECKLIST. CHECKED AFT CARGO FOR SMOK E OR FIRE INDICATIONS; FOUND NONE. FOR PRECAUTIONARY PURPOSES, REQUESTED PRIORITY HANDLING FROM ATC TO ATL. LIGHT STAYE D ILLUMINATED UNTIL 3000 FT MSL 0221 ZULU. LIGHT REMAINED OUT AFTER 3000 FT MSL. LANDED WITHOUT INCIDENT AT 0224Z. NO SM OKE OR FIRE INDICATION FOUND ON GROUND. INSPECTED ALL SMOKE DETECTORS IN THE MAIN CARGO DECK. FOUND NR 2 SMOKE DETECTOR SLOW TO RESPOND WHEN PTT. NR 2 SMOKE DETECTOR WAS WET. REMOVED AND REPLACED NR 2 SMOKE DETECTOR IAW MM 26-00-0. OPS CHE CKED GOOD.STATUS: CLOSED 2 L 7 3 4F RT A3WE 2001081400072 20010814 00072 NM 2001 8 14 DHL2001742008 1 20010731 A 2612 CONNECTOR BOEING 727 727225 1384077 NM FIRE LOOP LOOSE A DHLA K NONE N FALSE WARNING NR NOT REPORTED 1 SO 01 742DH 21290 GROUND DETECTOR LIGHT ILLUMINATED FOR NR 3 ENGINE FIRE PROTECTION SYSTEM. REPOSITIONED NR 3 FIRE LOOP AND SECURED FIRE L OOP FWD CONNECTOR OPS CHECK GOOD ALL IAW 727 MM 26-11-012. 2 L 7 3 4F A3WE 2001081400074 20010814 00074 NM 2001 8 14 DHL2001742009 1 20010801 A 2612 FIRE LOOP BOEING 727 727225 1384077 NM FIRE DETECTION FAULTY A DHLA K NONE N FALSE WARNING NR NOT REPORTED 1 SO 01 742DH 21290 THE FIRE PROTECTION SYSTEM P6-3 NR 3 DETECTOR CIRCUIT GRID LIGHT IS ILLUMINATED. REMOVED AND REPLACED FIRE LOOP ASSY IA W BMM 26-11-12 OPS CHECK NORMAL IAW BMM 26-11-0. 2 L 7 3 4F A3WE 2001081400075 20010814 00075 NM 2001 8 14 DHL2001742010 1 20010802 A 2612 ISOLATOR BOEING 727 727225 1384077 NM FIRE DETECTION WORN A DHLA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 742DH 21290 FIRE PROTECTION SYSTEM P6-3 NR 3 DETECTOR CIRCUIT BRD LIGHT IS ILLUMINATED. FOUND 3EA CLAMP ISOLATORS WORN THROUGH, ALLO WING LOOP TO TOUCH METAL CLAMPS, FOUND 1EA INCORRECT CLAMP WHICH IS USED ON A DUAL LOOP SYS. REMOVED AND REPLACED 3EA CLAMP ISOLATORS IAW MM 26-11-12. 2 L 7 3 4F A3WE 2001081400076 20010814 00076 NM 2001 8 14 DHL2001742011 1 20010806 A 2612 CONNECTOR BOEING 727 727225 1384077 NM FIRE LOOP DAMAGED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 742DH 21290 DURING PREDEPARTURE CHECK NR 3 ENGINE FIRE DETECTION WOULD NOT TEST. REPAIRED CONNECTOR AT NR 3 ENGINE FIRE LOOP IAW DHL B727 MM 20-11-0 OPS CHECK GOOD IAW DHL B727 MM 26-11-00. 2 L 7 3 4F A3WE 2001081400077 20010814 00077 NM 2001 8 14 DHL2001742012 1 20010808 A 2612 FIRE LOOP BOEING 727 727225 1384077 NM NR 3 ENGINE OUT OF POSITION A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 742DH 21290 DURING CLIMBOUT NR 3 ENG GROUND CIRCUIT DETECTOR LIGHT ILLUMINATED. ON ROLLOUT AFTER LANDING THE LIGHT WENT OUT. FOUND N R 3 FIRE LOOP CHAFING ON PREVIOUS REPAIR TO COWLING. REPOSITIONED FIRE LOOP IAW DHL B727 M/M 26-11-00. OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2001081400078 20010814 00078 NM 2001 8 14 DHL2001745007 1 20010729 A 5755 SKIN BOEING 727 727224 1384076 NM SPOILER CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 NR 8 SPOILER UPPER SURFACE HAS AREA OF CORROSION. REMOVED CORROSION IAW B727 SRM 51-10-6. 2 L 7 3 4F A3WE 2001081400079 20010814 00079 NM 2001 8 14 DHL2001745008 1 20010729 A 5753 SKIN BOEING 727 727224 1384076 NM T/E FLAP CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 LT OUTBD MIDFLAP HAS NUMEROUS AREAS OF SURFACE CORROSION ON UPPER LT OUTBD MIDFLAP HAS 2 FASTENERS HEADS MISSING AFT OF UPPER SURFACE. 2 L 7 3 4F A3WE 2001081400080 20010814 00080 NM 2001 8 14 DHL2001745009 1 20010802 A 2510 SEAT BOEING 727 727224 1384076 NM COCKPIT LACK OF LUBE A DHLA K NONE O OTHER NR NOT REPORTED 1 SO 01 745DH 20665 CAPTAINS SEAT DOES NOT ADJUST UP OR DOWN. LUBRICATED ALL MOVING PARTS AS PER B727-200 MM 25-10-41 OPS CHECK GOOD NO DEFE CTS NOTED. 2 L 7 3 4F A3WE 2001081400081 20010814 00081 EA 2001 8 14 COMA0160583 1 20010813 A 5320 60034017595 ANGLE CNDAIR CL600 CL6002B19 EA FLOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 964CA 12120 7129 THE AFT J-ANGLE AT FS280.0 IS CORRODED BETWEEN LBL9 AND RBL9.REPAIRED AFT J-ANGLE AT FS 280.0 BETWEEN LBL9 AND RBL9 I/A/ W WVAC EO 601R-53-2642. 2 L 7 2 4F RT A21EA 2001081400082 20010814 00082 EA 2001 8 14 COMA0160584 1 20010813 A 5320 60034017351 ANGLE CNDAIR CL600 CL6002B19 EA FLOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 964CA 12120 7129 THE FWD J-ANGLE AT FS280 BETWEEN LBL9.0 AND RBL 9.0 IS CORRODED.REPLACED FWD J-ANGLE AT FS280.0 BETWEEN LBL9.0 AND RBL9. 0 I/A/W WVAC EO 601R-53-2641. 2 L 7 2 4F RT A21EA 2001081400083 20010814 00083 EA 2001 8 14 COMA0160585 1 20010813 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 915CA 7013 THE EMERGENCY LIGHTING DID NOT OPERATE FOR 30 SECONDS AFTER SELECTING ON.PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTI NG SYSTEM, NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2001081400084 20010814 00084 EA 2001 8 14 COMA0160586 1 20010813 A 2730 DAMPER CNDAIR CL600 CL6002B19 EA A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 776CA 7293 YAW DAMPER #2 WOULD NOT ENGAGE DURING TAXI-OUT, AIRCRAFT RETURNED TO THE GATE.CLEANED THE ELECTRICAL CONNECTOR FOR #2 YA W DAMPER. 2 L 7 2 4F RT A21EA 2001081400085 20010814 00085 EA 2001 8 14 COMA0160587 1 20010813 A 2751 860D10018ABC FCU CNDAIR CL600 CL6002B19 EA AVIONICS BAY FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 818CA 1183 7408 DURING DESCENT INTO CVG THE FLAP CAUTION MESSAGE ACTIVATED AT 20 DEGREE FLAP POSITON.REPLACED THE FLAP ELECTRONIC CONTRO L UNIT. 2 L 7 2 4F RT A21EA 2001081400086 20010814 00086 EA 2001 8 14 COMA0160588 1 20010813 A 3150 6229820008 CONTROL UNIT CNDAIR CL600 CL6002B19 EA AVIONICS BAY FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SO 01 821CA 13739 7420 DURING CLIMB OUT OF CVG AILERON AND RUDDER TRIM SHOWED FULL SCALE DEFLECTION WITH NO EICAS RELATED MESSAGES. AIRCRAFT RE TURNED TO THE FIELD WITH ALL CONTROL SURFACES FUNCTIONING PROPERLY.REPLACED THE DATA CONCENTRATOR UNIT (DCU-4000). 2 L 7 2 4F RT A21EA 2001081400087 20010814 00087 EA 2001 8 14 COMA0160589 1 20010810 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 932CA 7038 FLOOR EMERGENCY STRIP LIGHTING IS INOPERATIVE.REPAIRED WIRING. 2 L 7 2 4F RT A21EA 2001081400088 20010814 00088 NM 2001 8 14 DHL2001745010 1 20010804 A 2612 FIRE WARNING BOEING 727 727224 1384076 NM COCKPIT FALSE ACTIVATION A DHLA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 745DH 20665 AFTER TAKE OFF AT DAL LOWER CARGO FIRE WARNING & BELL CAME ON AFTER TAKE OFF AT DAL LOWER CARGO FIRE WARNING & BELL CAME ON. RAN ENGINE AT REPORTED POWER SETTINGS AND OPERATED PRESSURIZATION SYS RAN ENGINE AT REPORTED POWER SETTINGS AND OPE RATED PRESSURIZATION SYS PER JRH CHAPT 7 AND 6.3 NO LEAKS NOTED NO DEFECTS NOTED. 2 L 7 3 4F A3WE 2001081400089 20010814 00089 NM 2001 8 14 DHL2001745011 1 20010803 A 3350 BATTERY BOEING 727 727224 1384076 NM CABIN DISCHARGED A DHLA K NONE L NO TEST NR NOT REPORTED 1 SO 01 745DH 20665 EMERGENCY EXIT LIGHT ABOVE MAIN ENTRY DOOR DOES NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES IAW B727 MM 33-50-22 OPS CHECK GOOD. 2 L 7 3 4F A3WE 2001081400090 20010814 00090 EA 2001 8 14 COMA0160590 1 20010811 A 7830 THRUST REVERSER CNDAIR CL600 CL6002B19 EA A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 940CA 7048 YELLOW #2 THRUST REVERSER UNLOCK MESSAGE APPEARED DURING CLIMB OUT OF ATW, CREW SELECTED TO DIVERT TO MKE, AIRCRAFT LAND ED SAFELY.DEFERRED THE RIGHT THRUST REVERSER IN ACCCORDANCE WITH MEL. 2 L 7 2 4F RT A21EA 2001081400091 20010814 00091 NM 2001 8 14 DHL2001745012 1 20010803 A 3350 LIGHT BOEING 727 727224 1384076 NM COCKPIT NOT SEATED A DHLA K NONE O OTHER NR NOT REPORTED 1 SO 01 745DH 20665 EXIT LIGHT ABOVE COCKPIT CABIN DOOR STAYS ILLUMINATED. SEATED EXIT LIGHT ASSY.AS PER B727-200 MM CHAP 33-50-11.OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. 2 L 7 3 4F A3WE 2001081400092 20010814 00092 EA 2001 8 14 COMA0160591 1 20010811 A 3240 BRAKE CNDAIR CL600 CL6002B19 EA A COMA K NONE S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 937CA 7044 DURING LANDING AT BNA THE AIRCRAFT PULLED TO THE LEFT DURING APPLICATION OF BRAKES, AIRCRAFT TAXIED SAFELY TO THE GATE.I NSPECTED BRAKES AND PERFORMED OPERATIONAL CHECK, NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2001081400093 20010814 00093 NM 2001 8 14 0102845501 1 20010725 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 501US 23190 DURING H-CHECK FOUND CRACK IN FLOORBEAM UPPER CAP. REPAIRED PER EA 55-183746. 2 L 7 2 4F RT A2NM 2001081400094 20010814 00094 EA 2001 8 14 COMA0160592 1 20010810 A 2611 473052 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA CARGO BAY FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 926CA 5206 7027 THE CARGO SMOKE WARNING ACTIVATED DURING PUSHBACK WHILE STARTING #1 ENGINE, NO SMOKE NOTED, AIRCRAFT WAS RE-POSITIONED A T GATE.REPLACED FAULTY CARGO SMOKE DETECTOR. 2 L 7 2 4F RT A21EA 2001081400095 20010814 00095 EA 2001 8 14 COMA0160593 1 20010810 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 932CA 7038 FLOOR EMERGENCY STRIP LIGHTING IS INOPERATIVE.REPAIRED WIRING. 2 L 7 2 4F RT A21EA 2001081400096 20010814 00096 NM 2001 8 14 DHL2001747542 1 20010720 A 5730 SKIN BOEING 727 727224 1384076 NM LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 DURING LINE INSPECTION FOUND CORROSION AT LEFT WING FWD LOWER SKIN AT APPROXIMATELY WS 190. REMOVED CORROSION PER B727 S RM 57-10-6 FROM LEFT WING AT APPROXIMATELY WS 190 MATERIAL LOSS .103 INCHES WITHIN LIMITS PER BOEING TELEX DHL-CVG-01-00 004H. HFEC INSP ACCOMPLISHED AT FASTENER HOLES AND BLEND AREAS NO CRACK INDICATION PER B727 NDT MANUAL PART 6 51-00-00 F IG 1 AND 4. 2 L 7 3 4F A3WE 2001081400097 20010814 00097 2001 8 14 DHL2001801009 4 20010731 A 2210 2588789901 AUTOPILOT SYS DOUG DC8 DC873F 302199F WP COCKPIT MALFUNCTIONED A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 801DH 46033 AUTOPILOT DOES UNCOMMANDED DISENGAGE, WILL NOSE DOWN WITH ATTEMPTED REENGAGE. TRIM NORMAL AFTER DISENGAGE. REPLACED AUTO PILOT PITCH CHANNEL OPS CHECKS GOOD IAW DC8 MM 22-13-1 PN ON 2588789-901 S/N ON 0180236. 2 L 7 4 4F RT 4A25 2001081400098 20010814 00098 WP 2001 8 14 DHL2001802010 1 20010808 A 2560 SMOKE BARRIER DOUG DC8 DC873 302199C WP COCKPIT TORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 VAPOR BARRIER HAS 2 TEARS. INTERIM REPAIR PERFORMED ON VAPOR BARRIER PER DHL ENGINEERING MEMO MEM-01-0002 BARRIER DEFFER ED IAW MEL GMM 3.5. 2 L 7 4 4F RT 4A25 2001081400099 20010814 00099 WP 2001 8 14 DHL2001803008 1 20010725 A 2120 SMOKE DOUG DC8 DC873 302199C WP COCKPIT DETECTED A DHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 803DH 46123 SMOKE IN COCKPIT DURING CLIMB SHORTLY AFTER TURNING ON ENGINE ANTI-ICE. PERFORMED APPROPRIATE CHECK LIST AND SMOKE CLEAR ED.PERFORMED ENGINE RUN PER JRH CHAP 11 COULD NOT DUPLICATE SMOKE IN COCKPIT PERFORMED PNEUMATIC SYS CHECK REF JRH 12.2 LT MANIFOLD IS HIGH NR 1 ENGINE BLEED IN AUTO OR HIGH AND WITH ENGINE ANTI ICE ON LEAK CHECK. 2 L 7 4 4F RT 4A25 2001081400100 20010814 00100 WP 2001 8 14 DHL2001803009 1 20010728 A 3246 WHEEL DOUG DC8 DC873 302199C WP NLG DEFECTIVE A DHLA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 803DH 46123 DURING TAXI OPTNS ACFT DRIFTS RIGHT REQUIRING CONSTANT LEFT NOSE WHEEL STEERING INPUTS TO MAINTAIN CENTERLINE. REMOVED & REPLACED BOTH LEFT & RIGHT NOSE WHEEL ASSEMBLIES AS PER MM 32-40. OK FOR SERVICE. 2 L 7 4 4F RT 4A25 2001081400101 20010814 00101 WP 2001 8 14 DHL2001803010 1 20010802 A 3260 PROXIMITY SENSOR DOUG DC8 DC873 302199C WP RT MLG DOOR DIRTY A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 803DH 46123 DURING LANDING GEAR UPLATCH CHECK DOORS NOT LATCHED LIGHT AND RIGHT GEAR DOOR UNSAFE LIGHT REMAINED ILLUMINATED ABNORMAL PROCEDURE PERFORMED. CLEANED GREASE OFF RIGHT GEAR DOOR PROX SENSOR. GROUND OPS CHECK DOOR, OK PER 32-31-04. 2 L 7 4 4F RT 4A25 2001081400102 20010814 00102 WP 2001 8 14 DHL2001803565 1 20010702 A 5753 RIB DOUG DC8 DC873 302199C WP T/E FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 C-CHECK - RT I/B FLAP JOINT INNER RIB SHOWS 4 EA CRACKS 1 INCH AT XW 129.000. PERFORMED STOP HOLE, FABRICATED REINFORCIN G ANGLE, AND INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001081400103 20010814 00103 WP 2001 8 14 DHL2001803566 1 20010710 A 3240 CONTROL CABLE DOUG DC8 DC873 302199C WP BRAKE SYS FRAYED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 C CHECK - FIRST OFFICER'S LT. BRAKE NR 85 RUN CABLE FRAYED. REMOVED AN REPLACED FRAYED RUN CABLE NR 85 AND PERFORMED ADJ USTMENT AN TEST OF WHEEL BRAKE SYSTEM IAW. MM 32-41-0 PAGE 201-205. 2 L 7 4 4F RT 4A25 2001081400104 20010814 00104 WP 2001 8 14 DHL2001804500 1 20010806 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 D-CHECK-RT WING L/E UPPER RIB CRACKED .50 INCH AT XFS 608.00. STOP DRILLED CRACK IAW SRM 57-2-0 FIG.2. FABRICATE DOUBLE R AND INSTALLED DOUBLER ON RIB IAW SRM 57-2-0.FIG2 AND SRM 5101-21, PG1. 2 L 7 4 4F RT 4A25 2001081400105 20010814 00105 NM 2001 8 14 AALA20011369 1 20010707 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 363AA 24044 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 31AB INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT CO NNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001081400106 20010814 00106 NM 2001 8 14 AALA20011368 1 20010707 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 363AA 24044 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 17HJ INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT AS SEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001081400107 20010814 00107 NM 2001 8 14 AALA20011336 1 20010703 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 393AN 29430 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 19B AND 22B INOPERATIVE. RE-SECURED EMERGENCY EXIT LIG HT CONNECTOR AT SEAT 19B AND 22B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001081400108 20010814 00108 NM 2001 8 14 AALA20011364 1 20010702 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 320AA 22321 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 37B INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT CONNE CTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001081400109 20010814 00109 NM 2001 8 14 AALA20011365 1 20010630 A 3350 CONNECTOR BOEING 777 777223 1385213 NM L3 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 770AN 29578 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L3 DOOR INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT CONNECTOR AT L3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001081400110 20010814 00110 NM 2001 8 14 AALA20011324 1 20010603 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 374AA 25201 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 28B INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT CONNE CTOR AT SEAT 28B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001081400111 20010814 00111 NM 2001 8 14 AALA20011321 1 20010629 A 3350 SOCKET BOEING 767 767223 1385123 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 312AA 22315 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 32HJ INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET AT SEAT 32HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001081400112 20010814 00112 NM 2001 8 14 AALA20011352 1 20010628 A 3350 LIG5714 LIGHT BOEING 727 727223 1384074 NM FS 1342 INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 889AA 21527 TUL - FOUND AFT VENTRAL STAIR ENTRANCE EMERGENCY EXIT LIGHT DIM DURING 10 MINUTE TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. (M) 2 L 7 3 4F A3WE 2001081400113 20010814 00113 NM 2001 8 14 AALA20011353 1 20010702 A 5300 WEB BOEING 727 727223 1384074 NM BS 870 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 889AA 21527 TUL - FOUND CRACKS IN STATION 870 WEB EXTENDING FROM FASTENER BELOW LOAD CONTROL VALVE ON BULKHEAD. INSTALLED REPAIR DO UBLER PER SRM 53-10-02. (M) 2 L 7 3 4F A3WE 2001081400114 20010814 00114 NM 2001 8 14 AALA20011354 1 20010702 A 5100 STIFFENER BOEING 727 727223 1384074 NM BS 870 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 889AA 21527 TUL - FOUND CRACK IN VERTICAL STIFFENER 4 INCHES FROM BOTTOM RIGHT WHEEL WELL AT APU DISCHARGE CUT OUT. REMOVED AND REP LACED VERTICAL STIFFENER PER DRAWING 65-18636 AND ESO 11697 6/28/2001. (M) 2 L 7 3 4F A3WE 2001081400115 20010814 00115 NM 2001 8 14 AALA20011366 1 20010628 A 5300 SKIN BOEING 727 727223 1384074 NM FS 1206 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 889AA 21527 TUL - FOUND FUSELAGE SKIN CRACKED, EXTENDING FROM WIRE BUNDLE ACCESS HOLE DOWN THROUGH AFT LOWER BOLT HOLE. STOP DRILLE D CRACK, NDT CHECKED, AND INSTALLED A TITANIUM DOUBLER PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 2001081400116 20010814 00116 NM 2001 8 14 AALA20011362 1 20010703 A 2900 A718822 VALVE BOEING 727 727223 1384074 NM RT ELEVATOR LEAKING A AALA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SW 21 889AA 21527 DFW - FLT 1216 - EN ROUTE DFW-PHL, IN FLIGHT B QUANTITY HYDRAULIC SYSTEM AND PRESSURE DECREASED TO ZERO. RETURNED DFW A ND LANDED WITHOUT FURTHER INCIDENT. REPLACED RIGHT SIDE ELEVATOR TRANSFER VALVE AND RIGHT SIDE ELEVATOR POWER CONTROL. (M) 2 L 7 3 4F A3WE 2001081400117 20010814 00117 NM 2001 8 14 AALA20011399 1 20010630 A 5100 WEB BOEING 727 727227 1384078 NM BS 203 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 726AA 20733 TUL - FOUND RIGHT NOSE GEAR PRESSURE DECK HAS VISUAL INDICATION OF CRACK AT RIVET ABOVE PANEL AT STATION 203. INSTALLED DOUBLER PER SRM 51-40-2 USING .063 2024 T-3 WITH .1875 INCH MS20470D RIVETS AND SIX .1875 INCH HI-LOCKS. (M) 2 L 7 3 4F A3WE 2001081400118 20010814 00118 NM 2001 8 14 AALA20011403 1 20010706 A 5300 SKIN BOEING 727 727227 1384078 NM BS 294.5-335 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 726AA 20733 TUL - FOUND SKIN BULGING IN AREA PREVIOUSLY WORKED, SKATE ANGLE (APPEARS TO BE RE-CORRODING) JUST ABOVE RIGHT NOSE GEAR STRUT DOOR .294.5 TO 335. SKIN BULGING AROUND REPAIR AREA FASTENERS, SIX INCHES ABOVE SKATE ANGLE STATION 295-333. REP AIRED AREA PER ESO 11697 DATED 7/6/2001. (M) 2 L 7 3 4F A3WE 2001081400119 20010814 00119 NM 2001 8 14 AALA20011408 1 20010703 A 5300 STRINGER BOEING 727 727227 1384078 NM FS 720E CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 726AA 20733 TUL - FOUND CORROSION ON STRINGER 23R STATION 720E. REPLACED STRINGER SECTION 720D PLUS 10 TO 720E PLUS 10 SPLICED EPR SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 2001081400120 20010814 00120 NM 2001 8 14 AALA20011406 1 20010704 A 5300 SKIN BOEING 727 727227 1384078 NM FS 235 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 726AA 20733 TUL - FOUND FUSELAGE SKIN CRACKED AT STATION 235 STRINGER 22L. REPAIRED CRACK PER SRM 53-30-3 FIG 3 SHEET 4, CLOSE TO E XISTING REPAIR DOUBLER. INCORPORATED ONE LARGE DOUBLER 16 INCHES BY 8 INCHES TO COVER BOTH AREAS. (M) 2 L 7 3 4F A3WE 2001081400121 20010814 00121 NM 2001 8 14 AALA20011405 1 20010705 A 5311 BELTFRAME BOEING 727 727227 1384078 NM FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 726AA 20733 TUL - FOUND BELT FRAME DENTED STATION 1050 AT STRINGER 25R. INSTALLED BELT FRAME REPAIR PER SRM 51-40-3 PAGE 1. (M) 2 L 7 3 4F A3WE 2001081400122 20010814 00122 NM 2001 8 14 AALA20011404 1 20010705 A 5300 STRINGER BOEING 727 727227 1384078 NM BS 1145 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 726AA 20733 TUL - FOUND CORROSION IN BOTTOM OF STRINGER 26R. REPAIRED STRINGER PER SRM SB 53-10-3 AND BOTTOM WITH BOLTS, NUTS AND W ASHERS THRU STRINGER CLIP AND STRINGER SIDES. (M) 2 L 7 3 4F A3WE 2001081400123 20010814 00123 WP 2001 8 14 AALA20011373 1 20010707 A 2400 100105901 CHARGER DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 413AA 49324 BUF- FLT 307 - EN ROUTE LGA-ORD, DURING CLIMB BATTERY CHARGER LIGHT ILLUMINATED. DIVERTED BUF AND LANDED WITHOUT FURTHE R INCIDENT. REPLACED BATTERY CHARGER. REPLACED LEFT AND RIGHT SIDE BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001081400124 20010814 00124 WP 2001 8 14 GTIA010645 1 20010711 A 2500 100505107 SLIDE DOUG DC9 DC982 3022082 WP A GTIA O OTHER O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 DFW - FOUND L2 SLIDE PACK DEPLOYED. REMOVED AND REPLACED L2 SLIDE PACK IAW MD-80 MM 25-62-00. (M) 2 L 7 2 4F A6WE 2001081400125 20010814 00125 WP 2001 8 14 GTIA010642 1 20010705 A 3350 60030451 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 603CA 49508 FLL - FOUND 80 PERCENT OF TAIL COMPARTMENT LIGHTS INOPERATIVE. CONNECTED WIRE AT SECOND TAIL COMP CEILING LIGHT, REPLAC ED LAMP ON INBOARD LIGHT, LEFT SIDE ABOVE EVACUATION SLIDE. REPLACED EMERGENCY BATTERY PACK ASSEMBLY IN AFT LAVATORY AF T POSITION. OPS CHECK NORMAL IAW MM 33-50-00. (M) 2 L 7 2 4F A6WE 2001081400126 20010814 00126 WP 2001 8 14 GTIA010637 1 20010707 A 2500 D29982107 SLIDE DOUG DC9 DC983 3022083 WP A GTIA O OTHER O OTHER IN INSP/MAINT 1 GL 23 824NK 53015 DTW - FOUND R1 DOOR SLIDE PACK PRESSURE GAUGE NEEDLE IS IN THE RED 'NO GO' SECTION. REMOVED AND REPLACED R1 DOOR EMERGE NCY ESCAPE SLIDE IAW MD-80 MM CH 25-62-00. (M) 2 L 7 2 4F RT A6WE 2001081400127 20010814 00127 WP 2001 8 14 GTIA010635 1 20010706 A 3350 60030431 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 816NK 49140 FLL - FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK FOR TAIL COMPART MENT EMERGENCY LIGHTS. OPS CHECK NORMAL IAW MM 33-50-00. (M) 2 L 7 2 4F A6WE 2001081500001 20010815 00001 WP 2001 8 15 DHL2001804501 1 20010802 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 RT WING L/E UPPER RIB CRACKED .50 INCH AT XFS 741.00STOP DRILLED CRACK, FABRICATED DOUBLER, AND INSTALLED DOUBLER IAW SR M 52-2-0, FIG 2 AND SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2001081500002 20010815 00002 WP 2001 8 15 DHL2001804502 1 20010806 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 RT WING L/E UPPER RIB CRACKED .50 INCH AT XFS 633.00STOP DRILLED CRACKED, FABRICATED DOUBLER, AND INSTALLED DOUBLER IAW SRM 52-2-0, FIG 2 AND SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2001081500003 20010815 00003 WP 2001 8 15 DHL2001804503 1 20010810 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 D CHECK - RT WING L/E UPPER RIB CRACKED .5 INCH AT XFS 622. STOP DRILLED CRACK, FABRICATED DOUBLER, AND INSTALLED DOUBLE R IAW SRM 57-2-0 FIG 2 & 51-1-21 PG 7. 2 L 7 4 4F RT 4A25 2001081500004 20010815 00004 WP 2001 8 15 DHL2001804504 1 20010810 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 D CHECK - RT WING L/E UPPER RIB CRACKED .50 INCH AT XFS 629. STOP DRILLED CRACK, FABRICATED DOUBLER, AND INSTALLED DOUBL ER IAW SRM 57-2-0 FIG 2 & 51-1-21 PG 7. 2 L 7 4 4F RT 4A25 2001081500005 20010815 00005 WP 2001 8 15 DHL2001804505 1 20010810 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 D CHECK - RT WING L/E UPPER RIB CRACKED .50 INCH AT XFS 636. STOP DRILLED CRACK, FABRICATED DOUBLER, AND INSTALLED DOUBL ER IAW SRM 57-2-0 FIG 2 & 51-1-21 PG 7. 2 L 7 4 4F RT 4A25 2001081500006 20010815 00006 WP 2001 8 15 DHL2001804506 1 20010810 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 D CHECK - RT WING L/E UPPER RIB CRACKED .50 INCH AT XFS 594.66. STOP DRILLED CRACK, FABRICATED DOUBLER, AND INSTALLED DO UBLER IAW SRM 57-2-0 FIG 2 & 51-1-21 PG 7. 2 L 7 4 4F RT 4A25 2001081500007 20010815 00007 WP 2001 8 15 DHL2001804507 1 20010810 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 D CHECK - RT WING L/E UPPER RIB CRACKED .50 INCH AT XFS 615. STOP DRILLED CRACK, FABRICATED DOUBLER, AND INSTALLED DOUBL ER IAW SRM 57-2-0 FIG 2 & 51-1-21 PG 7. 2 L 7 4 4F RT 4A25 2001081500008 20010815 00008 WP 2001 8 15 DHL2001804508 1 20010810 A 5350 FAIRING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 D CHECK - RT UPPER SECTION, FAIRING CRACKED 3 INCHES AT STA 1849.250. CUT FAIRING DAMAGED AREA FABRICATED FILLER & DOUBL ER, AND INSTALLED IAW SRM 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 2001081500009 20010815 00009 WP 2001 8 15 DHL2001804509 1 20010810 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 D-CHECK, FITTING CRACKED .250 INCH FROM STA 1760-1766 LONG-17R. REMOVED AND REPLACED CRACKED FITTING AT STA 1760-1766 L ONG-17R IAW SRM. 2 L 7 4 4F RT 4A25 2001081500010 20010815 00010 WP 2001 8 15 DHL2001804510 1 20010810 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 D-CHECK, MIDSHIP ACCESSARY COMPT PRESS BLKHD TO L-25L JOINT INTERCOSTAL SHOWS 2EA CRACKS (.50 INCH) STA 660-680. REMOVED CRACKED INTERCOSTAL IAW SRM 53-2-0 PG 1. CLEANED, TREATED, & PRIMED IAW 51-1-1B. INSTALLED INTERCOSTAL IAW SRM 51-1-21A PG 1. 2 L 7 4 4F RT 4A25 2001081500011 20010815 00011 WP 2001 8 15 DHL2001804511 1 20010810 A 5350 FAIRING DOUG DC8 DC873F 302199F WP FUSELAGE DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 D-CHECK, FUSELAGE FILLET NR 261H EXTERNAL SKIN DELAMINATED 2 INCHES. REPAIRED LT WING TO FUSELAGE FILLET NR 261H EXTERNA L SKIN WITH HYSOL & ARALDITE IAW SRM 51-1-9 PG 1-2. 2 L 7 4 4F RT 4A25 2001081500012 20010815 00012 WP 2001 8 15 DHL2001804512 1 20010810 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 D-CHECK, RT WING L/E UPPER RIB CRACKED 0.50 INCH AT XFS 804. STOP DRILLED, FABRICATED DOUBLER, AND INSTALLED IAW SRM 57- 2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001081500013 20010815 00013 WP 2001 8 15 DHL2001804513 1 20010810 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 D-CHECK, RT WING L/E UPPER RIB CRACKED .5 INCH AT XFS 841. STOP DRILLED, FABRICATED DOUBLER, AND INSTALLED IAW SRM 57-2- 0 FIG 2. 2 L 7 4 4F RT 4A25 2001081500014 20010815 00014 WP 2001 8 15 DHL2001804514 1 20010810 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 D-CHECK, RT WING L/E UPPER RIB CRACKED .5 INCH AT XFS 823. STOP DRILLED, FABRICATED DOUBLER, AND INSTALLED IAW SRM 57-2- 0 FIG 2. 2 L 7 4 4F RT 4A25 2001081500015 20010815 00015 WP 2001 8 15 DHL2001804515 1 20010810 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 D-CHECK, RT WING L/E UPPER RIB CRACKED .5 INCH AT XFS 811. STOP DRILLED, FABRICATED DOUBLER, AND INSTALLED IAW SRM 57-2 -0 FIG 2. 2 L 7 4 4F RT 4A25 2001081500016 20010815 00016 WP 2001 8 15 DHL2001804516 1 20010810 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 D-CHECK, RT WING L/E UPPER RIB CRACKED .5 INCH AT XFS 817. STOP DRILLED, FABRICATED DOUBLER AND INSTALLED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001081500017 20010815 00017 WP 2001 8 15 DHL2001804517 1 20010803 A 5511 RIB DOUG DC8 DC873F 302199F WP HORIZ STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 RT HORIZ STABILIZER L/E INNER RIB CRACKED .5 INCH AT XFS 47.5. STOP DRILLED CRACK, FABRICATED REINFORCING ANGLE, AND INS TALLED ANGLE PER SRM 55-2-0 FIG 2 &51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2001081500018 20010815 00018 WP 2001 8 15 DHL2001804518 1 20010803 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 FUSELAGE EXTERIOR ANGLE CRACKED 1 INCH AT STA 630 BETWEEN L31 AND L32R. REMOVED AND REPLACED CRACKED ANGLE PER SRM 51-1- 21 PG 7. 2 L 7 4 4F RT 4A25 2001081500019 20010815 00019 WP 2001 8 15 DHL2001804519 1 20010803 A 5320 WEB DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 EXTERIOR FUSELAGE WEB 1 INCH CRACKED STA 680 L-30L.STOP DRILLED CRACK, FABRICATED DOUBLER, AND INSTALLED DOUBLER PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 2001081500020 20010815 00020 WP 2001 8 15 DHL2001804520 1 20010805 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 EXTERIOR FUSELAGE REINFORCING ANGLE .5 INCH CRACK AT STA 761 LBL 22.0 (LOWER SECTION)REMOVED AND REPLACED CRACKED REINFO RCING ANGLE PER SRM 51-1-20D PG 21. 2 L 7 4 4F RT 4A25 2001081500021 20010815 00021 WP 2001 8 15 DHL2001804521 1 20010808 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 LT WING UPPER SKIN SURFACE SHOWS A 1 INCH CRACK AT STA XLS 421 STL. CUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AN D DOUBLER PER SRM 57-2-1. 2 L 7 4 4F RT 4A25 2001081500022 20010815 00022 WP 2001 8 15 DHL2001804522 1 20010808 A 5320 SUPPORT DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 WING TO FUSELAGE FAIRING SUPPORT CRACKED 1 IN AT STA 640 BETWEEN L-21 ANDL-22L.REMOVED AND REPLACED CRACKED SUPPORT PER SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2001081500023 20010815 00023 WP 2001 8 15 DHL2001804523 1 20010809 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 EXTERIOR WEB .5 INCH CRACK AT STA 812 LBL 55. REMOVED AND REPLACED CRACKED ANGLE PER SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2001081500024 20010815 00024 WP 2001 8 15 DHL2001805016 1 20010731 A 3230 UPLOCK DOUG DC8 DC873F 302199F WP LT MLG OUT OF ADJ A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 805DH 46125 AFTER T/O UPLATCH CHECK FAIL GEAR NOT LATCH LIGHT AND LT GEAR UNSAFE LIGHT ILLUM W/AURAL WIND SOUND ACCOMPANYING LIGHTS. SOUNDS OF GEAR IN WIND PERFORMED ABNORMAL PROCEDURE - ON HELP.ACCOMPLISHED T/SHOOTING AND FOUND MAIN GEAR UPLATCH MECH INTERMITTENTLY ON LT GEAR. ACCOMPLISH MINOR ADJUSTMENT ON LT MAIN DOOR FOLLOW UP MECH AND ON LT GEAR ACTUATOR.PERFORM O P CHECK SEVERAL TIMES FOUND OK . 2 L 7 4 4F RT 4A25 2001081500025 20010815 00025 WP 2001 8 15 DHL2001805018 1 20010810 A 5610 WINDOW DOUG DC8 DC873F 302199F WP COCKPIT LACK OF LUBE A DHLA K NONE O OTHER UK UNKNOWN 1 SO 01 805DH 46125 CAPT'S SLIDING SIDE WINDOW STICKING. LUBED WINDOW TRACK. OP CK GOOD IAW DC-8 M/M 56-00. 2 L 7 4 4F RT 4A25 2001081500026 20010815 00026 WP 2001 8 15 DHL2001806005 1 20010724 A 2611 SMOKE DETECTOR DOUG DC8 DC873F 302199F WP SMOKE DETECTION MALFUNCTIONED A DHLA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 806DH 46002 DURING SMOKE DETECTION CHECK APPEARS MESSAGE "AC6781 FALSE ALARM" ON CDU. R&R SMOKE DETECTOR UNIT IAW MM26-15-05. TESTED SMOKE DETECTION SYSTEM OK NOW. 2 L 7 4 4F RT 4A25 2001081500027 20010815 00027 WP 2001 8 15 DHL2001806006 1 20010801 A 5753 PLANK DOUG DC8 DC873F 302199F WP T/E FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 LEFT WING OUTBOARD FLAP INBOARD HINGE BASE OUTBOARD PLANK CRACKED. NR1301 REMOVED & INSTALLED LT O/B FLAP AS PER DC-8 M/ M 27-51-2 OPS CHECKS OK AS PER DC-8 M/M 27-50-0. 2 L 7 4 4F RT 4A25 2001081500028 20010815 00028 WP 2001 8 15 DHL2001806007 1 20010801 A 5753 564270505 PLANK DOUG DC8 DC873F 302199F WP T/E FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 ON LINE CHECK, LEFT WING OUTBOARD FLAP INBD HINGE BASE OUTBOARD PLANK CRACKED. REMOVED AND REPLACED FLAP AS PER DC8 MAIN TENANCE MANUAL 27-51-2.3) OPS CHECK L/H O/B FLAP AS PER DC8 M/M 27-50-0 OPS CHECK OK 2 L 7 4 4F RT 4A25 2001081500029 20010815 00029 WP 2001 8 15 DHL2001806008 1 20010806 A 5610 BRACKET DOUG DC8 DC873F 302199F WP COCKPIT WINDOW OUT OF POSITION A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 F/O SIDE WINDOW WILL NOT OPEN FULLY. REPOSITIONED WINDOW BRACKET OPS CK OK IAW MM 56-20-2. 2 L 7 4 4F RT 4A25 2001081500030 20010815 00030 WP 2001 8 15 DHL2001807020 1 20010811 A 3260 DOWNLOCK SWITCH DOUG DC8 DC873F 302199F WP LT MLG DEFECTIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 807DH 45990 LEFT GEAR DOWN & LOCKED INDICATION INOP. NOSE GEAR DOWN & LOCKED INDICATION INOP. REMOVED AND REPLACED LT GEAR DOWN LOCK SWITCH IAW 32-60-0 OPS CHECKED GOOD. REMOVED AND REPLACED THE NOSE DOWN LOCK CANNON PLUG IAW AWM 32-1-0 & STANDARD PRAC TICES 20-00-0. OPS CHECKED GOOD IAW 32-60-0. 2 L 7 4 4F RT 4A25 2001081500031 20010815 00031 WP 2001 8 15 DHL2001807021 1 20010811 A 5522 SKIN DOUG DC8 DC873F 302199F WP ELEVATOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 FOUND 3 INCH CRACK LT ELEVATOR ON UPPER SURFACE APPROX 9 INCHES AFT OF INBOARD HINGE CUT OUT.INSTALLED REPAIR LT UPPER E LEVATOR SKIN PER SRM 55-2-1 FIG 1B & SRM 51-4-8, ALSO PER BOEING LETTER M/C D800-0038. 2 L 7 4 4F RT 4A25 2001081500032 20010815 00032 CE 2001 8 15 0010 1 20010718 A 5312 5042002857 BULKHEAD BEECH 90 E90 1152914 CE FUSELAGE CRACKED E CIEA K NONE O OTHER IN INSP/MAINT 1 NM 03 989GM 13443 LW109 DURING COMPLIANCE OF A 13,000 CYCLE INSPECTION CRACKS WERE FOUND ON BOTH THE LEFT AND RIGHT SIDE OF THE AIRCRAFT AT FUSE LAGE BULKHEAD 176.5. SMALL CRACKS WERE FOUND AT THE POINT WHERE THE BULKHEAD AND FLOOR MEET. A CRACK WAS FOUND AT THE LEFT 176.5 BULKHEAD FROM THE CUTOUT FOR THE NR 10 STRINGER TOWARDS A PEAR SHAPED LIGHTENING HOLE APPROXIMATELY 1 INCH I N LENGTH. RIVETS HEADS WERE FOUND MISSING ON THE ANGLE BRACKET WHICH ATTACHES THE BULKHEAD TO THE STRINGER AT THE FLOOR LEVEL. 1 L 7 2 3T 3A20 2001081500033 20010815 00033 CE 2001 8 15 0011 1 20010725 A 5311 5042002857 FRAME BEECH 90 E90 1152914 CE PWA PT6 PT6A28 EA HARTZL HCB3T HCB3TN3 GL FUSELAGE CRACKED E CIEA K NONE O OTHER IN INSP/MAINT 1 NM 03 987GM 9635 LW65 DURING COMPLIANCE OF THE 13,000 LANDING INSPECTION ON THE FUSELAGE BULKHEADS CRACKS WERE FOUND ON THE 176.5 BULKHEAD ON BOTH THE LEFT AND RIGHT SIDE OF THE AIRCRAFT. THE CRACKS ARE ON THE BULKHEAD FRAME P/N 50-420028-57 AND 50-420028-58, N EAR THE BOTTOM OF THE UNIT WHERE THERE IS A CUTOUT FOR CHANNEL P/N 50-420014-229 AND CHANNEL P/N 50-420014-230. THE CRA CKS ARE ABOUT .75 INCH LONG, AND ARE FROM THE CUTOUT MOVING IN AN UPWARD DIRECTION. 1 L 7 2 3T 4 T 3A20 E4EA 6 C P15EA 2001081500034 20010815 00034 NM 2001 8 15 01FDEA00676 1 20010809 A 5320 PANEL BOEING 727 727233 138408A NM FUSELAGE LOWER CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277FE 22042 N 546 R/H TRANSITION PANEL CORRODED BETWEEN BS 1030-1090. R&R PANEL PER IAW FEDEX SRM 51-20-1, 51-30-2. 2 L 7 3 4F RT A3WE 2001081700057 20010817 00057 NM 2001 8 17 01FDEA00682 1 20010811 A 5311 FRAME BOEING 727 727247 138408F NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 DENT IN TOP FLANGE OF FRAME AT BS 970, LBL 46, WL 162 AFT CARGO BAY. *S/D* REMOVED AND REPLACED FRAME PER SRM 51-40-3. 2 L 7 3 4F A3WE 2001081700058 20010817 00058 NM 2001 8 17 01FDEA00683 1 20010811 A 5313 STRINGER BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 FUSELAGE STR 27L HAS GOUGE ON O/B SIDE WITH CORROSION AT BS 482 (C53-111-01, 2). *S/D* REMOVED AND REPLACED STR PER SR M 57-40-3. 2 L 7 3 4F A3WE 2001081500035 20010815 00035 NM 2001 8 15 01FDEA00678 1 20010731 A 5313 STRINGER BOEING 727 72722 1384002 NM FUSELAGE LOWER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 149FE 19087 N 1426 STRINGER 16L CRACKED AT BS 623. ** S/D ** COMING 2 L 7 3 4F A3WE 2001081500036 20010815 00036 EU 2001 8 15 01FDEA00681 1 20010811 A 5210 PLACARD AIRBUS 310 A310222 3930315 EU LM CABIN DOOR UNLOCKED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 417FE 333 01-273 ECAM CAUTION IND LM CABIN UNLOCKED. INSTALLED PLACARD. 2 L 7 2 4F RT A35EU 2001081700059 20010817 00059 NM 2001 8 17 01FDEA00684 1 20010811 A 5313 STRINGER BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 FUSELAGE STR CHANNEL STR 27L IS CORRODED AT BS 474 ON O/B SIDE (C53-111-01, 2). *S/D* REMOVED AND REPLACED STR PER MM 52-20-011-7, SRM 51-30-2. 2 L 7 3 4F A3WE 2001081700060 20010817 00060 NM 2001 8 17 01FDEA00685 1 20010813 A 5320 STIFFENER BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSION ON VERTICAL STIFFENER AT BS 740 BULKHEAD JUST O/B OF STR 26R, WL 145 - 151. *S/D* REMOVED AND REPLACED PER S RM 51-10-2, 51-30-2. 2 L 7 3 4F A3WE 2001081700061 20010817 00061 NM 2001 8 17 01FDEA00686 1 20010813 A 5315 FLOORBEAM BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSION (C53-224-01, 3) ON TOP OF FLOORBEAM BS 950, BL 0 TO RBL 25, WL 208. *S/D* REMOVED AND REPLACED FLOORBEAM PER SRM 51-30-2, 51-30-5, 51-30-8. 2 L 7 3 4F A3WE 2001081500037 20010815 00037 NM 2001 8 15 01FDEA00688 1 20010813 A 5310 SHEAR TIE BOEING 727 727247 138408F NM CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 N 671 CORROSION EMANATING UNDER SHEAR TIE AT BS 1148 BETWEEN STR 27 AND 28L. ** S/D ** COMING 2 L 7 3 4F A3WE 2001081500038 20010815 00038 NM 2001 8 15 01FDEA00692 1 20010813 A 5315 FLOORBEAM BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 NR 877 CORROSION (C53-111-01(3)) ON LOWER FLANGE OF FLOORBEAM 1050 RBL 35, WL 202. ** S/D ** COMING 2 L 7 3 4F A3WE 2001082800138 20010828 00138 NM 2001 8 28 01FDEA00700 1 20010813 A 5315 FLOORBEAM BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 CORROSION ON LWR CHORD OF 1130 FLOORBEAM LWR FLANGE AROUND FASTENER HOLES LT SIDE TO RT SIDE. REMOVED AND REPLACED LOWER CHORD PER EA 7-5310-59239. 2 L 7 3 4F A3WE 2001081500039 20010815 00039 NM 2001 8 15 01FDEA00701 1 20010810 A 5315 FLOORBEAM BOEING 727 727247 138408F NM UPPER FLANGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 CORROSION ON FLOORBEAM UPPER FLANGE BS 344, LBL 3-20, WL 208. 2 L 7 3 4F A3WE 2001081700067 20010817 00067 NM 2001 8 17 01FDEA00702 1 20010813 A 5315 FLOORBEAM BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSION ON TOP OF FLOORBEAM BS 950, BL 0-RBL 25, WL 208. *S/D* REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-1, 51-30 -2, 51-30-5, 51-30-8. 2 L 7 3 4F A3WE 2001081500040 20010815 00040 NM 2001 8 15 01FDEA00703 1 20010813 A 5310 FRAME BOEING 727 727247 138408F NM UPPER FLANGE DENTED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 N 852 DENT IN UPPER FLANGE OF FRAME AT BS 970, WL 150, LBL 30. ** S/D ** COMING 2 L 7 3 4F A3WE 2001081500041 20010815 00041 NM 2001 8 15 01FEA00704 1 20010814 A 5310 FRAME BOEING 727 727247 138408F NM CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 N 701 CORROSION ON FRAME BS 580, RBL 10, WL 148. ** S/D ** COMING 2 L 7 3 4F A3WE 2001081500042 20010815 00042 NM 2001 8 15 01FDEA00706 1 20010813 A 5310 STRINGER CLIP BOEING 727 727247 138408F NM CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 N 1017 FUSELAGE STR CLIP AT STR 232 IS CRACKED AT BS 580. R&R CLIP. 2 L 7 3 4F A3WE 2001081500043 20010815 00043 NM 2001 8 15 01FDEA00707 1 20010813 A 5310 SHEAR TIE BOEING 727 727247 138408F NM CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 N 992 CRACKED SHEAR TIE BS 720, LBL 4, WL 148. ** S/D ** R&R SHEAR TIE. 2 L 7 3 4F A3WE 2001081700069 20010817 00069 NM 2001 8 17 01FDEA00708 1 20010813 A 5311 FRAME BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 BS 1148 FRAME HAS BULGE IN CENTER WEB OF STR 29R. *S/D* REMOVED AND REPLACED FRAME PER SRM 53-10-3. 2 L 7 3 4F A3WE 2001081700070 20010817 00070 NM 2001 8 17 01FDEA00709 1 20010813 A 5310 SHEAR TIE BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSION FWD CARGO BAY BS 640, RBL 3, WL 147 SHEAR TIE. *S/D* REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-4. 2 L 7 3 4F A3WE 2001081700071 20010817 00071 NM 2001 8 17 01FDEA00710 1 20010813 A 5313 STRINGER BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSION ON STRINGER 23R, BS 397. *S/D* REMOVED AND REPLACED STR PER SRM 53-10-3 & EA 7-5310-58479. 2 L 7 3 4F A3WE 2001081700072 20010817 00072 NM 2001 8 17 01FDEA00711 1 20010813 A 5320 SPLICE BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSION (C53-111-02, 2) FWD CARGO BAY BS 640 - 644, RBL 23, WL 150 STR 26R. *S/D* REMOVED AND REPLACED STRINGER SPLI CE. 2 L 7 3 4F A3WE 2001081500044 20010815 00044 NM 2001 8 15 01FDEA00712 1 20010813 A 5310 SHEAR TIE BOEING 727 727247 138408F NM CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 N 1008 CORROSION ON SHEAR TIE AT BS 720C BL0, WL 148 R&R SHEAR TIE PER IAW SRM 51-20-1. 2 L 7 3 4F A3WE 2001081700073 20010817 00073 NM 2001 8 17 01FDEA00713 1 20010813 A 5313 STRINGER BOEING 727 727247 138408F NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 AFT STRINGER ATTACHMENT ON LT LEADING EDGE WING ILLUM LIGHT IS CRACKED. *S/D* REMOVED AND REPLACED STR ON LEFT L/E WIN G LIGHT PER SRM 53-10-3. 2 L 7 3 4F A3WE 2001081700074 20010817 00074 NM 2001 8 17 01FDEA00714 1 20010813 A 5320 STRINGER CLIP BOEING 727 727247 138408F NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 STRINGER CLIP CRACKED BS 804.5, STR 7L. *S/D* REMOVED AND REPLACED CLIP PER SRM 51-30-2. 2 L 7 3 4F A3WE 2001081500045 20010815 00045 CE 2001 8 15 0012 1 20010725 A 5320 50420014229 CHANNEL BEECH 90 E90 1152914 CE PWA PT6 PT6A28 EA HARTZL HCB3T HCB3TN3 GL FUSELAGE CRACKED E CIEA K NONE O OTHER IN INSP/MAINT 1 NM 03 989GM 13443 LW109 DURING THE PROCESS OF REPAIRING CRACKS IN THE BULKHEAD AT STATION 176.5 ON BOTH THE LEFT AND RIGHT SIDE CRACKS IN THE LE FT CHANNEL P/N 50-420014-229 AND RIGHT CHANNEL P/N 50-420018-230, IN THE RADIUS AREA OF THE BEND ON THE SKIN SIDE OF THE CHANNEL. THE CRACK WAS ABOUT .5 INCH FORWARD OF BULKHEAD 176.5 TO ABOUT .5 INCH AFT OF BULKHEAD 176.5. THE CRACK WAS VERY DIFFICULT TO SEE AT FIRST. ONCE THE AREA WAS CLEANED IT APPEARED AS A VERY THIN PENCIL LINE. 1 L 7 2 3T 4 T 3A20 E4EA 6 C P15EA 2001081500046 20010815 00046 CE 2001 8 15 0013 1 20010803 A 5743 5012007717 SUPPORT BRACKET BEECH 90 E90 1152914 CE RT MLG CRACKED E CIEA K NONE O OTHER IN INSP/MAINT 1 NM 03 63BV 10864 LW256 THE RIGHT INBOARD LANDING GEAR ACTUATOR SUPPORT BRACKET IS CRACKED AT THE BOTTOM AREA OF THE BRACKET WHERE IT ATTACHES T O THE WING SPAR STRUCTURE. THE WING SPAR STRUCTURE IS NOT EFFECTED BY THIS CRACK. THE CRACK IS APPROXIMATELY .5 INCH LO NG AND IS THE RADIUS OF THE FLANGE OF THE BRACKET. THE PART NUMBER OF THE SUPPORT BRACKET IS 50-120077-17. 1 L 7 2 3T 3A20 2001081500047 20010815 00047 NM 2001 8 15 0100570 1 20010702 A 5730 PANEL BOEING 747 747122 1384872 NM LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LT WING PANEL AT L/E 4TH PANEL FROM FUSELAGE DELAMINATED. REMOVED AND REPLACED LT WING PANEL L/E 4TH FORM FUSELAGE AS P ER SRM 51-30-02. 2 L 7 4 4F A20WE 2001081500048 20010815 00048 NM 2001 8 15 0100571 1 20010625 A 5320 SUPPORT BOEING 747 747249F 1384849 NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION AT STA 500 - 520 LBL 37 FLOORBEAM SUPPORT STRUCTURE SPLICE INTERCOSTAL. REPAIR CARRIED OUT AS PER SRM 53-10-05. 2 L 7 4 4F A20WE 2001081500049 20010815 00049 NM 2001 8 15 0100572 1 20010626 A 5230 SKIN BOEING 747 747249F 1384849 NM MIAN CARGO DOOR BULGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 MAIN DECK CARGO DOOR EXTERNAL SKIN BULGING AT LATCH ACCESS PANEL CUT OUT (2ND FROM FWD). DAMAGED AREA TRIMMED OUT AND A FILLER AND STRAP INSTALLED PER BOEING TELEX SIA-SIN -01-00947H FAA FORM 8110-3 DATED JUNE 21. 2 L 7 4 4F A20WE 2001081500050 20010815 00050 NM 2001 8 15 0100573 1 20010625 A 5320 NUT BOEING 747 747249F 1384849 NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION FOUND ON AIRCON PANEL SUPPORT STRUCTURE AT LOWER SURFACE AT RBL 53 STA 1170 & 1152. REMOVED AND REPLA CED CORRODED ANCHOR NUT, BLEND OUT CORROSION AS PER SRM 53-10-01. 2 L 7 4 4F A20WE 2001081500051 20010815 00051 NM 2001 8 15 0100575 1 20010625 A 5320 SUPPORT BOEING 747 747249F 1384849 NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 CORROSION FOUND ON KEEL BEAM LOWER PANEL SUPPORT STRUCTURE AT RBL 15 FROM STA 1391 TO STA 1437. BLENDED OUT CORROSION A S PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001081500052 20010815 00052 NM 2001 8 15 0100576 1 20010625 A 5320 STRUCTURE BOEING 747 747249F 1384849 NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 CORROSION FOUND BEHIND ATTACHMENT FLANGE OF WING TO BODY FAIRING SUPPORT RIB AT STA 1480 LBL 75 TO LBL 90. REMOVED CHOR D AND AFFECTED AREA PER IAW SRM 53-10-01 AND SRM 51-30-00. 2 L 7 4 4F A20WE 2001081500053 20010815 00053 NM 2001 8 15 0100577 1 20010625 A 5315 FLOORBEAM BOEING 747 747249F 1384849 NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 CORROSION FOUND ON MAIN DECK FLOORBEAM STA 2240 RBL 54 TOP OF CHORD. REPAIR CARRIED OUT AS PER SRM 53-11-23 & SRM 51-40 -04. 2 L 7 4 4F A20WE 2001081500054 20010815 00054 NM 2001 8 15 0100578 1 20010622 A 5520 BALANCE WEIGHT BOEING 747 747249F 1384849 NM ELEVATOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 CORROSION FOUND ON LEFT O/B ELEVATOR BALANCE WEIGHT. NUT BLAST PER 747 SL-55-07 FINISH PER 747-32-55-07. 2 L 7 4 4F A20WE 2001081500055 20010815 00055 NM 2001 8 15 0100579 1 20010625 A 5320 THRESHOLD BOEING 747 747249F 1384849 NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 CORROSION FOUND AT STA 460 - 480 NR 1 RT FWD ENTRY DOOR THRESHOLD PLATE UNDERNEATH FLOORBEAM. REPAIR CARRIED OUT AS PER SRM 51-40-02. 2 L 7 4 4F A20WE 2001081500056 20010815 00056 NM 2001 8 15 0102506311 1 20010716 A 3350 GUARD BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE J WARNING INDICATION CR CRUISE 1 GL 01 671US 26477 DURING FLIGHT, CREW RECEIVED EMERGENCY LIGHTS EICAS MESSAGE. FOUND FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH GUARD COVER LOOSE AND ACTIVATING THE SWITCH. REPOSITIONED AND SECURED SWITCH GUARD COVER BASE. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001081500057 20010815 00057 NM 2001 8 15 0102525527 1 20010715 A 2450 734285C CONTROL UNIT BOEING 757 757200 1384950 NM E/E BAY FAULTY A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 527US 41232 38356 23842 ON DEPARTURE FROM SFO, BOTH ENGINE EPR INDICATIONS WERE ABNORMAL BUT OTHER ENGINE INSTRUMENTS WERE WITHIN PARAMETERS. D URING CLIMB, STATUS MESSAGES APPEARED FOR BOTH ENGINE OIL COOLERS AND REVERSER CONTROL VALVES. THE FLIGHT RETURNED TO S FO AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE BUSS POWER CONTROL UNIT WITH A SERVICEABLE UNIT. SUBSEQUENT S YSTEM TESTS WERE SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2001081500058 20010815 00058 NM 2001 8 15 0102575508 1 20010720 A 2910 AS11508K0322 HYDRAULIC LINE BOEING 757 757251 1384970 NM NLG WW RUPTURED A NWAA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 01 508US 23197 ON APPROACH AFTER GEAR AND FLAPS 30 EXTENSION, THE LEFT HYDRAULIC SYSTEM QUANTITY INDICATION FELL TO ZERO. FLIGHT LANDE D WITHOUT INCIDENT AND WAS TOWED TO THE GATE. MAINTENANCE REPLACED A RUPTURED FLEX LINE IN THE NOSE WHEEL WELL. THE SY STEM WAS SERVICED, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A2NM 2001081500059 20010815 00059 WP 2001 8 15 0102609925 1 20010723 A 2170 117946081 SEPARATOR DOUG DC9 DC932 3022066 WP A/C BAY MALFUNCTIONED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 925US 47472 AFTER TAKEOFF, FLIGHT ATTENDANTS REPORTED SMOKE IN THE CABIN. DECLARED AN EMERGENCY AND RETURNED TO MEM WITH AN UNEVENT FUL LANDING. MAINTENANCE REPLACED THE RIGHT WATER SEPARATOR. INSPECTED TAIL. LEAK AND OPERATIONAL CHECK GOOD. AIRCRA FT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001081500060 20010815 00060 2001 8 15 0102611230 4 20010716 A 2330 CONTROL PANEL DOUG DC10 DC1030 3023501 WP CABIN FAILED A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 230NW 46552 DURING CRUISE, FLIGHT ATTENDANT REPORTED ELECTRICAL BURNING ODOR AT SEAT 3A. TURNED OFF RECIRCULATION FAN AND READING L IGHT AND CONTINUED TO DTW. LANDED WITHOUT INCIDENT. REPLACED THE OVERHEAD DECODER. OPERATIONAL CHECK GOOD. 2 L 7 3 4F A22WE 2001081500061 20010815 00061 NM 2001 8 15 0102672298 1 20010725 A 2910 7577741 HYDRAULIC LINE BOEING 727 727251 138408H NM RT MLG RUPTURED A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 298US 22152 DURING CLIMB AND JUST AFTER GEAR RETRACTION, THE A-SYSTEM HYDRAULIC FAILED. CREW FOLLOWED COM PROCEDURE AND DIVERTED TO BOS AND MADE UNEVENTFUL LANDING. MAINTENANCE REPLACED RUPTURED FLEX LINE ON RIGHT MAIN LANDING GEAR UPLOCK ACTUATOR. LEAK AND OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 2001081500062 20010815 00062 NM 2001 8 15 0102686626 1 20010729 A 2612 CIRCUIT BOARD BOEING 747 747251B 1384892 NM FIRE DETECTION FAULTY A NWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 01 626US 21708 DURING CRUISE, THE WHEEL WELL FIRE DETECTION LIGHT, BELL, AND MASTER CAUTION CAME ON. AIRCRAFT RETURNED TO SEA AND AND LANDED WITHOUT INCIDENT. REPLACED THE FIRE DETECTION AND WARNING CARDS A9 AND A17, AND RIGHT SEGMENT OF FIRE DETECTOR M 694. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2001081500063 20010815 00063 NM 2001 8 15 0102706636 1 20010802 A 3350 LIGHT BOEING 747 747251B 1384892 NM EXTERIOR INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 636US 23547 DURING LINE CHECK, FOUND NR 2 RIGHT EXTERIOR FIXTURE EMERGENCY LIGHTS AND 1L AND 1R PASSENGER OVERHEAD LIGHTS INOPERATIV E. REPLACED EXTERIOR LIGHT ASSEMBLY AND POWER SUPPLIES. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F A20WE 2001081500064 20010815 00064 NM 2001 8 15 0102726307 1 20010801 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 667US 24222 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT LAV DOOR 4L, LAV DOOR 2L, AND ROW 10AB. RECONNEC TED WIRING AT SEAT 10AB LIGHT ASSEMBLY AND LAV DOOR 4L. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001081500065 20010815 00065 NM 2001 8 15 0102756304 1 20010729 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 664US 23819 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT PASSENGER DOOR 3R BETWEEN SEATS 10-12R AND 25L. REPLACED LIGHT ASSEMBLIES. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001081500066 20010815 00066 NM 2001 8 15 0102796302 1 20010805 A 2120 PAN BOEING 747 747451 1384940 NM CABIN DAMAGED A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 662US 23720 DURING CRUISE, PASSENGER ENTERTAINMENT SYSTEM BECAME INOPERATIVE. FLIGHT ATTENDANT ATTEMPTED NUMEROUS SYSTEM RESETS FOL LOWED BY THE SMELL OF SMOKE IN A-ZONE. SMOKE SMELL DISAPPEARED WHEN SYSTEM WAS TURNED OFF AND LEFT OFF. REPAIRED DRIP BASIN ABOVE PROJECTOR BECAUSE OF WATER DRIPPINGS. REPLACED PROJECTOR AS A PRECAUTION. 2 L 7 4 4F RT A20WE 2001081500067 20010815 00067 NM 2001 8 15 0102826308 1 20010804 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 668US 24223 DURING LINE CHECK (PEK), FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE BETWEEN ROWS 40-45L. SECURED LOOSE CONNECTION . OPERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001081500068 20010815 00068 CE 2001 8 15 0118 1 20010713 A 2130 6420001 VALVE BEECH MU300 400A 1155402 CE CABIN PRESSURE FAILED E DJFA B A EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 445CW RK45 AIRCRAFT WAS AT 35,000 FT WHEN THERE WAS A SOUND OF RUSHING AIR ACCOMPANIED BY SMOKE IN THE CABIN AND THE COCKPIT. THE PILOT DECLARED AN EMERGENCY AND DESCENDED TO THE NEAREST AIRPORT (LAS) AND LANDED WITHOUT INCIDENT. THE PROBLEM WAS THA T THE EMERGENCY PRESSURIZATION CAME ON DUE TO THE FAILURE OF THE EMERGENCY PRESS VALVE. UNIT WAS REPLACED AND AIRCRAFT WAS TEST FLOWN AND WAS FOUND TO BE OK. 2 H 7 2 4F RT A16SW 2001081500069 20010815 00069 CE 2001 8 15 0119 1 20010720 A 3260 SQUAT SWITCH CESSNA 500 550 2076604 CE LT MLG OUT OF ADJ E DJFA B A EMER. DESCENT UNSCHED LANDING O OTHER CR CRUISE 1 EA 23 270CW 5500570 AIRCRAFT WAS FLYING AT 37,000 FT WHEN THE PILOTS HEARD A LOUD HISS. CABIN STARTED TO CLIMB 6000 FT/MIN. THE PILOTS DEC LARED AN EMERGENCY AND DESCENDED, LANDED IN WILLIAMSPORT PA WITH NO FURTHER INCIDENT. THE CAUSE OF THE PROBLEM WAS THE LT SQUAT SWITCH WAS OUT OF ADJUSTMENT WHICH CAUSED THE AIRCRAFT TO DEPRESSURIZE. THE SWITCH WAS ADJUSTED AND THE AIRCRA FT WAS TEST FLOWN AND WAS FOUND TO BE OK. 1 L 7 2 4F A22CE 2001081500070 20010815 00070 CE 2001 8 15 0120 1 20010727 A 7830 SWITCH BEECH MU300 400A 1155402 CE PWA JT15 JT15D4 52112 NE THRUST REVERSER OUT OF ADJ E DJFA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 EA 23 431CW RK31 PILOTS HAD TO SHUT DOWN THE NR 1 ENGINE DUE TO A LEFT T/R DEPLOY LIGHT CAME ON. IT WAS A PRECAUTIONARY SHUTDOWN. DURIN G DESCENT THE T/R LIGHT WENT OUT AND THE PILOT RESTARTED THE ENGINE AND LANDED WITH NO FURTHER INCIDENCES. ADJUSTED THE T/R DEPLOY SWITCH AND OPS CHECKED OK. 2 H 7 2 4F 4 F RT A16SW E1NE 2001081500105 20010815 00105 NM 2001 8 15 01FDEA00548 1 20010714 A 5320 PANEL BOEING 727 727233 138408A NM CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277FE 22042 DURING ROUTINE INSP LT TRANSITION PANEL IN AFT BAG BIN FOUND CRACKED AT BS 1060. *S/D* REMOVED AND REPLACED PANEL PER SRM 51-20-1, 51-30-2. 2 L 7 3 4F RT A3WE 2001081500111 20010815 00111 NM 2001 8 15 01FDEA00549 1 20010714 A 5320 PANEL BOEING 727 727233 138408A NM CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277FE 22042 DURING ROUTINE INSP LT TRANSITION PANEL IN AFT BAG BIN FOUND CRACKED AT BS 990. *S/D* REMOVED AND REPLACED PNL PER SRM 51-20-1, 51-30-2. 2 L 7 3 4F RT A3WE 2001081500115 20010815 00115 NM 2001 8 15 01FDEA00557 1 20010714 A 5320 CLIP BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277FE 22042 DURING ROUTINE INSP SHEAR TIE CLIP AT STR 23L, BS 580 FOUND CRACKED. R&R CLIP PER SRM 51-20-1, 51-30-2. 2 L 7 3 4F RT A3WE 2001081500116 20010815 00116 NE 2001 8 15 01FDEA00562 2 20010713 A 7200 ENGINE BOEING 727 72722 1384002 NM PWA JT8 JT8D7B 52053 NE NR 3 FAULTY A FDEA F E A ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING A FLAME/FIRE CL CLIMB 1 SO 25 189FE 19082 654539 ENGINE FIRE NR 3 AFT T/O AT 100 FT. FIRED BOTH BOTTLES. *S/D* REMOVED AND REPLACED NR 3 ENG PER WORK CARD 70T0501-03. OK FOR SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2001081500117 20010815 00117 2001 8 15 01FDEA00563 4 20010712 A 3414 INDICATOR DOUG DC10 DC1030F 3023504 WP COCKPIT INOPERATIVE A FDEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 25 313FE 48311 REJECTED T/O DUE TO NO AIRSPEED ON CAPT SIDE. 2 L 7 3 4F RT A22WE 2001121200036 20011212 00036 WP 2001 12 12 01FDEA00564 1 20010716 A 5320 AGA31515 SUPPORT DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 PANEL SUPPORT COMMON TO STANCHION HAS CORRODED. REMOVED AND REPLACED CORROSION PER IAW INSTRUCTIONS, EA 8-5310-52551 ST EP 7 & DC10 SRM 53-50-00 FIG 1 & 14. 2 L 7 3 4F RT A22WE 2001121200037 20011212 00037 WP 2001 12 12 01FDEA00565 1 20010716 A 5311 FRAME DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 FRAME CORRODED IN NR 2 AIR CONDITION BAY FWD LEFT SIDE. REMOVED AND REPLACED FRAMES PER EA 8-5310-56130 & SRM 53-12-01, 53-30-00. 2 L 7 3 4F RT A22WE 2001121200038 20011212 00038 WP 2001 12 12 01FDEA00566 1 20010716 A 5311 FRAME DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 FRAME HAS 1 CRACK AT FASTENER LOCATION AND 1 DOUBLE AT FASTENER. FAB, INSTALLED AND REPAIRED HOLE PER IAW EA 8-5310-561 30 & DC10 SRM 53-12-01 FIG 12, SHT 1 & 53-30-00 FIG 5. 2 L 7 3 4F RT A22WE 2001081500119 20010815 00119 WP 2001 8 15 01FDEA00568 1 20010716 A 5311 FRAME DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 LWR FWD CORNER TO AFT CARGO DOOR OPENING, FRAME CORRODED BEYOND LIMITS. FAB DOUBLER, FILLER AND SHIMS PER IAW EA 8-5310 -52551 & DC10 SRM 53-50-00. 2 L 7 3 4F RT A22WE 2001081500120 20010815 00120 WP 2001 8 15 01FDEA00569 1 20010716 A 5311 FRAME DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 AFT CARGO PIT FRAME CORRODED. REMOVED AND REPLACED FRAME PER IAW EA 8-5310-52551 & DC10 SRM 53-50-00 FIG 1 SHT 1. 2 L 7 3 4F RT A22WE 2001081500121 20010815 00121 EU 2001 8 15 01FDEA00570 1 20010717 A 2612 FIRE WARNING AIRBUS 310 A310 EU NR 1 ENGINE MALFUNCTIONED A FDEA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SO 25 416FE 288 ON CLIMBOUT NR 1 ENG FIRE WARNING. COMPLETED ECAM FIRE PROC, SHUTDOWN ENG. FIRED BOTTLES. REMOVED BOTH FIRE BOTTLES A ND SQUIBS. RAN ENG AT HIGH POWER CK DUCTS, NO LEAKS NOTED. 2 L 7 2 4F RT A35EU 2001081500122 20010815 00122 EU 2001 8 15 01FDEA00571 1 20010714 A 3411 PITOT LINE AIRBUS 310 A310203 EU NR 2 ADC LOOSE A FDEA K NONE J WARNING INDICATION NR NOT REPORTED 1 SO 25 429FE 364 TWO ADC INOP F/O AIRSPEED AND ALTITUDE ERRONEOUS. SECURED NR 2 ADC PITOT LINE AT ADC PER AMM 34-10-00-501 PG 501. GROU ND TEST GOOD. 2 L 7 2 4F RT A35EU 2001081500127 20010815 00127 WP 2001 8 15 01FDEA00579 1 20010717 A 3030 CONTROLLER DOUG DC10 DC1030F 3023504 WP ANTI-ICE SYS INOPERATIVE A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 302FE 46801 ON ROTATION ENG 2 A/I DISAGREE LIGHT ILLUM (SW OFF) COMPL W/RED TABS. FLT RECORDER CAUTION LIGHT ILLUM ON S/O PNL AND A OA HT C/B POPPED. REMOVED AND REPLACED HEATER CONTROLLER/MONITOR PER MM 30-35-01-2. PER OPS TEST PER 30-30-00-2, SYS O PS NORM. WRI ASSIGNED TO NR 2 A/I (30-20-7682) WRI ASSIGNED TO FLT REC LT (31-30-7681). 2 L 7 3 4F RT A22WE 2001081500131 20010815 00131 WP 2001 8 15 01FDEA00580 1 20010718 A 5511 ALC705217 RIB DOUG DC10 DC1010F 3022111 WP HORZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 058FE 46705 LT HORIZONTAL STAB INBD CTR L/E OTBD RIB LWR CHORD STRAP SUPPORT CRACKED. CRACK 6 INCHES LONG IN CHORD RADIUS AT STA XF S-241.28. *S/D* REMOVED AND REPLACED RIB CHORD PER SRM 51-00-01 & EA 8-5510-56793. 2 L 7 3 4F A22WE 2001081500133 20010815 00133 WP 2001 8 15 01FDEA00581 1 20010718 A 5510 ALC750212 ANGLE DOUG DC10 DC1010F 3022111 WP HORZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 058FE 46705 RIGHT HORIZ STAB CTR L/E OUTBOARD SIDE UPPER ROW NUTPLATE RETAINER/LAND HAS 2 FT CRACK AT STA XFS 166. *S/D* REMOVED A ND REPLACED CHORD ANGLE PER SRM 55-10-01. 2 L 7 3 4F A22WE 2001081500135 20010815 00135 2001 8 15 01FDEA00584 4 20010720 A 3417 HG480B13 ADC BOEING 727 727233 138408A NM E/E BAY FAILED A FDEA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 223FE 20935 ON ROTATION CAPT AIRSPEED IND MACH AND A/S BARREL OFF FLAG CAME INTO VIEW. REMOVED AND REPLACED AIR DATA COMPUTER. PER FORMED BITE TEST. ALL SYS OK FOR SERVICE. 2 L 7 3 4F RT A3WE 2001081500136 20010815 00136 EU 2001 8 15 01FDEA00585 1 20010720 A 3230 CYLINDER AIRBUS 310 A310200 3930310 EU LT MLG CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 451FE 303 LEFT MLG DOWNLOCK CYLINDER AT STRUT BRACE CTD MISSING ATTACHMENT PIN. CYLINDER CRACKED AT 2 PLACES. 2 L 7 2 4F RT A35EU 2001081500139 20010815 00139 NM 2001 8 15 01FDEA00588 1 20010715 A 5312 BULKHEAD DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 AFT FX INTERNAL FOUND CREW REST FWD BULKHEAD AT BS 2014.982 WITH FITTING QTY 1 CRACKED AT RBL 20. *S/D* REMOVED AND RE PLACED BULKHEAD AND FITTING PER SRM 51-33-01, DWG AJL7140. 2 L 7 3 4F RT A22WE 2001081500145 20010815 00145 NM 2001 8 15 01FDEA00594 1 20010722 A 2710 WARNING SYSTEM DOUG MD11 MD11F 3023600 NM COCKPIT ACTIVATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 614FE 48528 01-246 AFT T/O DURING FLAP/SLAT RETRACT GOT AILERON DEFLECT DISAGREE ALERT. RAN CHECKLIST UNABLE TO CORRECT. 2 L 7 3 4F RT A22WE 2001081500146 20010815 00146 EU 2001 8 15 01FDEA00595 1 20010725 A 3230 LANDING GEAR AIRBUS 310 A310222 3930315 EU NLG & MLG MALFUNCTIONED A FDEA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 SO 25 447FE 251 AFT T/O GEAR WOULD NOT RETRACT SYS 1, SYS 2 OK. GOT WARNING, ATS PITCH TRIM PRESS AND PITOT HEAT FAULTS. 2 L 7 2 4F RT A35EU 2001081500147 20010815 00147 NM 2001 8 15 01FDEA00596 1 20010724 A 2613 65249203 OVERHEAT LOOP BOEING 727 727233 138408A NM OVERHEAT SYS MALFUNCTIONED A FDEA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SO 25 257FE 20939 LWR AFT BODY O/H LIGHT ISOLATED LEAK BETWEEN BLD VLV AND PACK VLV. REMOVED AND REPLACED FIRE DETECTOR PER MM 26-14-000- 5. OPS CHECK GOOD ON GROUND. 2 L 7 3 4F RT A3WE 2001081500148 20010815 00148 NM 2001 8 15 UPS01236610 1 20010802 A 5330 WEB BOEING 727 72725C 138400H NM NOSE WW L/H SIDE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:C NLG WHEEL EWLL. L/H SIDE WALL AREA HAS CRACK APPROX. BS244 BELOW ACCESS PANEL 3122. REMOVED FASTE NERS ON NLG L/H WHEEL WELL L/H SIDE WEB AREA APPROX BS 244 BELOW ACCESS PANEL 3122 AS PER SRM 51-30-02. CUT OUT DAMAGE AREA AS PER B727 SRM 51-40-02 APPROX 1"X3.5" HFEC PERFORMANCE AS PER B727 TPG 51-00-00 FIG 4. DOUBLER REPAIR INSTALLED AS PER B727 SRM 52-40-02. 2 L 7 3 4F A3WE 2001081500149 20010815 00149 NM 2001 8 15 UPS01236611 1 20010802 A 5310 WEB BOEING 727 72725C 138400H NM NLG WW BS 250 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:C NLG WHEEL WELL L/H SIDE WEB AREA HAS CRACK APPROX BS 250 BELOW ACCESS PANEL 3122 REMOVED FASTENERS ON NLG WHEEL WELL L/H SIDE WEB AREA APPROX BS250 BELOW ACCESS PANEL 3122 AS PER B727 SRM 51-30-2. CUT OUT DAMAGE AREA AS PER B727 SRM 51-40-2. PERFORMANCE HFEC INSP AS PER B727 NDT 31-00-00 FIG 4, NO CRACK FOUND. INSTALLED BOUBLER REPAI R AS PER B727 SRM 51-40-02. 2 L 7 3 4F A3WE 2001081500150 20010815 00150 NM 2001 8 15 UPS01236612 1 20010802 A 5310 WEB BOEING 727 72725C 138400H NM NLG WW BS 240 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:C NLG WHEEL WELL R/H SIDEWALL AREA HSA CRACK APPROX BS 240 BELOW ACCESS PANEL 3122. REMOVED FASTENER S AT R/H SIDE BS 240 CUT OUT DAMAGE AREA AS PER B727 SRM 51-40-02. PERFORMANCE NDT INSP AS PER B727 NDT 51-00-00 FIG 4. FOUND NO CRACK. INSTALLED REPAIR AT NOSE LANDING GEAR R/H WEB AREA BS 240 BELOW ACCESS PANEL AS PER B727 SRM 51-40-2. 2 L 7 3 4F A3WE 2001081500151 20010815 00151 NM 2001 8 15 UPS01236613 1 20010731 A 5310 WEB BOEING 727 72725C 138400H NM BS 1180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:C MAIN CABIN LEFT AFT LAV, BS 1180 OUTBOARD FLOOR WEB CRACK. REMOVED AND REPLACED FLOOR WEB (DITCHIN G PANEL) AT BS 1180 LBL 55 REF B727 SRM 51-10-01 AND 51-30-02 MATERIAL USED 2024 T3/.020" ALUMINUM. 2 L 7 3 4F A3WE 2001081500152 20010815 00152 NM 2001 8 15 01FDEA00598 1 20010717 A 5530 STRUCTURE BOEING 727 727247 138408F NM VERTICAL STAB CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CHAFE AT VERT STAB L/E RIGHT FRONT SPAR FIN BS 55.8 TO 47.0 O/B SIDE. 2 L 7 3 4F A3WE 2001081500153 20010815 00153 NM 2001 8 15 01FDEA00599 1 20010720 A 5315 FLOORBEAM BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSION IN AND AROUND NUT PLATE HOLES ON LOWER CHORD OF BS 1130 FLOORBEAM RBL 50 - LBL 25, WL 200. REMOVED AND REPLACE D FLOORBEAM PER IAW FEDEX EA 7-5310-59209. 2 L 7 3 4F A3WE 2001081500154 20010815 00154 NM 2001 8 15 01FDEA00600 1 20010725 A 2781 SENSOR DOUG MD11 MD11F 3023600 NM L/E SLAT DEFECTIVE A FDEA K NONE N FALSE WARNING CL CLIMB 1 SO 25 609FE 48549 ON DEPARTURE GOT SLAT DISAGREE AT 300 FLAPS 25 DEG GEAR COMING UP ALERT CONTINUE. RAN CHECKLIST. R&R SLAT POS SENSORS P ER MM 27-84-02, 27-84-03. 2 L 7 3 4F RT A22WE 2001081500155 20010815 00155 EU 2001 8 15 01FDEA00602 1 20010726 A 5270 WARNING SYSTEM AIRBUS 300 A300F4605R 3930327 EU COCKPIT ACTIVATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 673FE 780 DURING CLIMBOUT ECAM WARN AFT CARGO DOOR NOT CLOSED. CABIN PRESS NORM. 2 L 7 2 4F RT A35EU 2001081500158 20010815 00158 EU 2001 8 15 MALA010645 1 20010810 A 7710 503J177612 TORQUE SENSOR SAAB SF340 SF340A 7850100 EU A MALA O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 15 68XJ 340A068 During Climbout on Flight #3380 at approximately 65% TRQ I tried to reduce Left Engine power. Initially no response. T RQ shot down to 25 to 30%. After small power applications RQ would surge to 65 to 70%. Engine was only stable between 3 0 to 40% TRQ. Maintenance replaced Torque sensor PN 503J177612 SN/off 51M2A608 SN/on 51M2A786. IAW CHp 74-20 Ops check good at this time. 2 L 7 2 4T RT A52EU 2001081500160 20010815 00160 WP 2001 8 15 01FDEA00610 1 20010727 A 5320 THRESHOLD DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 058FE 46705 CENTER CARGO DOOR FWD CORNER DOOR SILL THRESHOLD HAS HEAVY SURFACE CORROSION FWD OF NR 1 SPOOL FITTING. *S/D* REMOVED AND REPLACED DOUBLER AND HI-LOKS PER EA 8-5310-56792. 2 L 7 3 4F RT A22WE 2001081500161 20010815 00161 WP 2001 8 15 01FDEA00611 1 20010727 A 5320 THRESHOLD DOUG DC10 DC1010F 3022111 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 058FE 46705 CENTER CARGO DOOR AFT CORNER DOOR SILL THRESHOLD HAS HEAVY SURFACE CORROSION JUST AFT OF NR 5 SPOOL FITTING. *S/D* REM OVED AND REPLACED PER SRM 51-21-01, 51-31-01 VOL II. 2 L 7 3 4F A22WE 2001081500162 20010815 00162 WP 2001 8 15 01FDEA00613 1 20010727 A 5320 FLOOR SUPPORT DOUG DC10 DC1010F 3022111 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 050FE 47804 MAIN CABIN FLOORBOARD CROSSBEAM SUPPORT IS CORRODED. *S/D* REMOVED AND REPLACED SUPPORT PER IAW SRM 51-21-01, 51-10-01 . 2 L 7 3 4F A22WE 2001081500163 20010815 00163 WP 2001 8 15 01FDEA00614 1 20010727 A 5347 SEAT TRACK DOUG DC10 DC1010F 3022111 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 050FE 47804 MAIN CABIN SEAT TRACK IS SPLIT AND CRACKED AT O/B CLIP LUG. *S/D* REMOVED AND REPLACED TRACK PER SRM 53-60-01 FIG 1, 5 5-31-01. 2 L 7 3 4F A22WE 2001081500167 20010815 00167 NM 2001 8 15 01FDEA00625 1 20010730 A 3232 69163394 FITTING BOEING 727 72722 1384002 NM NLG CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 149FE 19087 DURING INSP FOUND SUPPORT FITTING FOR NOSE LANDING GEAR DOOR ACTUATOR RODS CORRODED. R&R FITTING PER SRM 51-30-2. 2 L 7 3 4F A3WE 2001081500168 20010815 00168 EU 2001 8 15 QXEA0101347 1 20010813 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 GEG - EMERGENCY EXIT SIGN, ROW 8, INOPERABLE. REMOVED AND REPLACED CIRCUIT BOARD. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001081500172 20010815 00172 2001 8 15 01FDEA00628 4 20010730 A 3442 ANTENNA DOUG DC10 DC1030 3023501 WP WEATHER RADAR MALFUNCTIONED A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 308FE 48297 BOTH CAPT AND F/O RADAR DISPLAY BEGAN TO SPOKE. REMOVED AND REPLACED WEATHER RADAR ANTENNA AND PLATE AS PER MM 34-41-01 -2. GROUND CHECK OK. 2 L 7 3 4F A22WE 2001081500173 20010815 00173 2001 8 15 01FDEA00629 4 20010731 A 3442 RADAR DOUG DC10 DC1030 3023501 WP WEATHER RADAR MALFUNCTIONED A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 308FE 48297 RADAR SPOKING BOTH SYSTEMS ALL RANGES ALL GAINS SETTINGS REPEAT WRITEUP. 2 L 7 3 4F A22WE 2001081500174 20010815 00174 NM 2001 8 15 01FDEA00636 1 20010803 A 2752 MS9391130ZE4C MOTOR BOEING 727 727233 138408A NM T/E FLAP LEAKING A FDEA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 25 219FE 21102 INBOARD FLAP DRIVE HYD MOTOR LEAKING IN LT WHEEL WELL. REMOVED AND REPLACED MOTOR PER 727 200 MM 27-51-062-4. LEAK CHE CK GOOD. 2 L 7 3 4F RT A3WE 2001081500176 20010815 00176 NM 2001 8 15 01FDEA00637 1 20010803 A 5330 SKIN BOEING 727 727247 138408F NM FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 OUTER SKIN CHAFED LT SIDE BS 720D+15, STR 19L. R&R SKIN PER SRM 53-30-1, 53-30-3. 2 L 7 3 4F A3WE 2001081500177 20010815 00177 NM 2001 8 15 01FDEA00640 1 20010803 A 5330 SKIN BOEING 727 727247 138408F NM FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 FUSELAGE SKIN CHAFED BS 720D+15, STR 19 RT. R&R SKIN PER SRM 51-30-1, 53-30-2. 2 L 7 3 4F A3WE 2001081500178 20010815 00178 NM 2001 8 15 01FDEA00652 1 20010803 A 2750 FLAP BOEING 727 727233 138408A NM RT WING OUT OF ADJ A FDEA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 25 223FE 20935 DURING CLIMB EXPERIENCED MILD A/C VIBRATION. FOUND RT OUTBOARD TRAILING EDGE FLAP WITH TOO MUCH PLAY. ADJUSTED GAP BET WEEN ROLLERS AS PER MM 27-51-011-5. CHECK OK. 2 L 7 3 4F RT A3WE 2001081500181 20010815 00181 2001 8 15 01FDEA00661 4 20010803 A 3442 ANTENNA DOUG DC10 DC1030 3023501 WP WEATHER RADAR MALFUNCTIONED A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 308FE 48297 REPEAT WRITE UP WX RADAR RETURNS BOTH SYS SHOW BLANK AREA IN A SPOKE PATTERN. REMOVED AND REPLACED ANTENNA PER IAW MD D C10-30 AMM 34-41-01-2. 2 L 7 3 4F A22WE 2001081500182 20010815 00182 2001 8 15 01FDEA00662 4 20010806 A 3442 RADAR DOUG DC10 DC1030 3023501 WP WEATHER RADAR FAULTY A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 308FE 48297 REPEAT WRITE UP NR 1 RADAR SYS UNSATISFACTORY WITH HEAVY SIDE RETURNS. 2 L 7 3 4F A22WE 2001081500183 20010815 00183 2001 8 15 01FDEA00663 4 20010802 A 3442 RADAR DOUG DC10 DC1030 3023501 WP WEATHER RADAR MALFUNCTIONED A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 308FE 48297 AFT 38 MIN RADAR STARTED SPOKING. REMOVED AND REPLACED RADOME MM 53-51-00-2. REMOVED AND REPLACED WX RADAR ANTENNA PED ESTAL MM 34-41-01-2. 2 L 7 3 4F A22WE 2001081500185 20010815 00185 WP 2001 8 15 2001F00176 1 20010709 A 3350 9721050 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 809US 48041 IND - THE LOW LEVEL EMERGENCY LIGHTS AND THE LEFT AFT EXIT WINDOW SIDEWALL LIGHT FAILED TO TEST. MAINTENANCE REPLACED T HE EMERGENCY LIGHT BATTERIES. REF USAAD01134. (M) 2 L 7 2 4F A6WE 2001081500186 20010815 00186 NM 2001 8 15 2001F00177 1 20010710 A 2910 68153 HYDRAULIC LINE BOEING 727 727222 1384073 NM HYDRAULIC SYS CRACKED A RYNA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CE 07 7645U 20039 'A' SYSTEM HYDRAULIC FAILURE AFTER TAKEOFF. EMERGENCY DECLARED. COMPLIED WITH ALL CHECK LISTS. AIRCRAFT LANDED WITHOU T INCIDENT. REMOVED AND REPLACED HYDRAULIC PRESSURE TUBE ON RIGHT ELEVATOR POSITION CONTROL UNIT. LEAK AND OPERATIONAL CHECK GOOD. (M) 2 L 7 3 4F A3WE 2001081500187 20010815 00187 NM 2001 8 15 2001F00178 1 20010704 A 5280 69179571 HINGE BRACKET BOEING 727 72777C 1380420 NM LT MLG DOOR OUT OF ADJ A RYNA O OTHER J WARNING INDICATION CL CLIMB 1 CE 07 526PC 20370 MAIN GEAR DOOR WILL NOT LOCK UP POSITION. GEAR INDICATED DOWN AND LOCKED WHEN CYCLED. PERFORMED ALL COMPANY PROCEDURES AND CHECKLIST. AIRCRAFT LANDED WITHOUT INCIDENT. ADJUSTED AND RESECURED FORWARD LEFT MAIN GEAR DOOR HINGE PLATE. LUB RICATED MAIN GEAR AND DOORS. JACKED AIRCRAFT. OPS CHECK OF GEAR GOOD. (M) 2 L 7 3 4F A3WE 2001081500188 20010815 00188 NM 2001 8 15 2001F00179 1 20010501 A 5755 654645151A SKIN BOEING 737 7372H4 138448C NM SPOILER DELAMINATED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 29SW 21340 THE UPPER SKIN OF SPOILER NR 8 WAS FOUND DELAMINATED. THE DAMAGED AREA WAS REPAIRED IAW EO COO-CMP-3-57-246-01. (M) 2 L 7 2 4F A16WE 2001081500189 20010815 00189 EA 2001 8 15 COMA0160594 1 20010814 A 5346 60135066 WEB CNDAIR CL600 CL6002B19 EA BEAM CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 978CA 10541 7158 DURING ENGINE BOX BEAM INSPECTION FOUND A 2" CRACK ON L/H LOWER SKIN ACCESS PANEL OUTBD OF LBL36.20 AND A 1.75" CRACK ON THE R/H LOWER SKIN ACCESS PANEL OUTBD OF RBL 36.20.PERFORMED A MAJOR REPAIR BETWEEN FS 625.30 AND 640.00 TO L/H AND R/H LOWER ENGINE SUPPORT BEAM AT LBL 36.20 AND RBL 36.20 BY REMOVING DAMAGED AREAS AND INSTALLING REPAIR PARTS I/A/W CANADA IR REO 601R-53-61-366 REV C. 2 L 7 2 4F RT A21EA 2001081500190 20010815 00190 NM 2001 8 15 2001F00180 1 20010527 A 5315 BAC1518399 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 29SW 21340 FOUND PASSENGER CABIN, STATION 947 FLOORBEAM UPPER FLANGE CORRODED AT LBL 50. THE CORRODED FLOORBEAM SECTION WAS REMOVE D AND A NEW SECTION WAS INSTALLED IAW EO COO-3-53-233-01. (M) 2 L 7 2 4F A16WE 2001081500191 20010815 00191 NM 2001 8 15 2001F00181 1 20010501 A 5755 654645258 SKIN BOEING 737 7372H4 138448C NM SPOILER DELAMINATED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 29SW 21340 THE GROUND SPOILER NR 4 WAS FOUND DELAMINATED IN SEVERAL PLACED. THE DAMAGED AREA WAS REPAIRED IAW EO COO-CMP-3-57-247- 01. (M) 2 L 7 2 4F A16WE 2001081500192 20010815 00192 NM 2001 8 15 2001F00182 1 20010501 A 5755 654645258 SKIN BOEING 737 7372H4 138448C NM SPOILER DELAMINATED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 29SW 21340 THE UPPER SKIN OF THE NR 5 SPOILER WAS FOUND DELAMINATED. THE DAMAGED AREA WAS REPAIRED IAW EO COO-CMP-3-57-248-01, DAT ED JUNE 08, 2001. (M) 2 L 7 2 4F A16WE 2001081500193 20010815 00193 NM 2001 8 15 2001F00183 1 20010526 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 29SW 21340 THE FUSELAGE SKIN AT BS 890 BETWEEN STRINGER 20R AND 21R WAS FOUND DENTED. THE DAMAGED AREA WAS REPAIRED IAW BOEING FAX COO-SJD-01-003292MM DATED 6/11/2001. (M) 2 L 7 2 4F A16WE 2001081500194 20010815 00194 EA 2001 8 15 COMA0160595 1 20010814 A 2760 270007 PCU CNDAIR CL600 CL6002B19 EA ELECTRICAL BAY FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 979CA 3930 7159 AFTER PUSH BACK AT CVG, SPOILERS FAULT STATUS MESSAGE WOULD NOT EXTINQUISH, AIRCRAFT RETURNED TO THE GATE.REPLACED THE F LIGHT SPOILER POWER CONTROL UNIT. 2 L 7 2 4F RT A21EA 2001081500195 20010815 00195 EA 2001 8 15 COMA0160596 1 20010814 A 5270 DOOR CNDAIR CL600 CL6002B19 EA A COMA D RETURN TO BLOCK J WARNING INDICATION CR CRUISE 1 SO 01 973CA 7146 THE CABIN DOOR OUTER HANDLE CAUTION MESSAGE ACTIVATED DURING CRUISE FLIGHT AFTER DEPARTING CVG, CREW SELECTED TO DIVERT TO IND, AIRCRAFT LANDED SAFELY.ADJUSTED THE CABIN DOOR INNER HANDLE CAM TENSIONER. 2 L 7 2 4F RT A21EA 2001081500196 20010815 00196 NM 2001 8 15 C1HA200193013 1 20010805 A 2613 CLAMP BOEING 727 727212 138407G NM LOOSE A C1HA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 293AS 21348 AT FL330 eng #1 strut overheat lite on followed COM pulled pwr back to 85% N1 on descent and lite went out at FL 290.ACT ION TAKEN:Removed lwr pylon panels found pre-cooler clamps loose tightened leak checked and no leaks noted reinstalled p anels OK for service. 2 L 7 3 4F A3WE 2001081500197 20010815 00197 NM 2001 8 15 C1HA200193015 1 20010807 A 2130 39608831 FLOW VALVE BOEING 727 727212 138407G NM L/H FAILED A C1HA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 293AS 21348 Could not control pressurization after takeoff in all modes. Overweight landing made at 175,000lbs. back at MSP.ACTION T AKEN:R&R'd L/H flow control valve pressurized A/C ops check normal A/C OK for service. Also secured ground wire. Overwei ght landing inspection accomplished no defects noted. 2 L 7 3 4F A3WE 2001081500198 20010815 00198 NM 2001 8 15 C1HA200181012 1 20010729 A 2611 1011C POWER UNIT BOEING 727 7272S7 138407Z NM ONLY FAILED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 681CA 22020 Fire bells inop in firwall test position.ACTION TAKEN:T/S and found #1 operating power unit bad R&R'd and ops checked go od. 2 L 7 3 4F A3WE 2001081500199 20010815 00199 NM 2001 8 15 C1HA200181013 1 20010802 A 2611 10607724 WARNING SYSTEM BOEING 727 7272S7 138407Z NM ONLY FAILED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 681CA 22020 Engine fire test bell weak on 1st engine fire test inop on other two engines.ACTION TAKEN:Replaced aural warning box ops checked good. 2 L 7 3 4F A3WE 2001081500200 20010815 00200 NM 2001 8 15 C1HA200181014 1 20010804 A 3232 SWITCH BOEING 727 7272S7 138407Z NM DIRTY A C1HA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 681CA 22020 On departure landing gear was retracted and handle moved to off the rt. gear door lite illuminated followed COM procedur es and lite went off.ACTION TAKEN:cleaned door door lock switches, cables, and macheanisms checked normal. 2 L 7 3 4F A3WE 2001081600001 20010816 00001 SO 2001 8 16 C2XA01IA325 1 20010810 A 2130 222201TO11400 CONTROLLER EMB 120 EMB120ER 3260203 SO COCKPIT INOPERATIVE A C2XA O OTHER O OTHER UK UNKNOWN 1 SW 27 15730 120187 IAH - FLIGHT 3284, THE CREW REPORTED THAT THE AIRCRAFT LOST ALL PRESSURIZATION AT 19000 FEET. THE CREW DESCENDED TO 9000 FEET IN AUTO MODE, AND THE AIRCRAFT SLOWLY BEGAN PRESSURIZING. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTE NANCE REMOVED AND REPLACED THE PRESSURIZTION CONTROLLER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001081600002 20010816 00002 SO 2001 8 16 C2XA01IA326 1 20010813 A 3350 RPS1B BATTERY PACK EMB 145 EMB145LR SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13964 145123 IAH - DURING MAINTENANCE INSPECTION, THE AISLE PATH LIGHTING AT SEATS 8A THRU 12A WAS FOUND TO BE INOPERATIVE. MAINTENAN CE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001081600003 20010816 00003 EU 2001 8 16 RAIA00108012 1 20010809 A 6120 B5JFR36C1103C PROPELLER JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE MCAULY 5JFR36 B5JFR36C1103 GL LEFT ENGINE OVERSPEED A RAIA E B ENGINE SHUTDOWN EMER. DESCENT Z SIGNIFICANT FAILURE REPORT DE DESCENT 1 CE 03 550HK 12484 3622 41039 75018 951478 5422-EWR-DURING DESCENT THE LEFT ENGINE RPM WENT TO 105.9%, CREW PERFORMED ENGINE SHUTDOWN, AIRCRAFT LANDED WITHOUT INCE DENT. MAINTENANCE INSPECTED AND REPLACED THE LEFT PROPELLER. PERFORMED A MAINTENANCE CHECK FLIGHT, AIRCRAFT OPERATED NOR MALLY. 2 L 7 2 4T 4 T RT A41NM E18NE 6 C P15NE 2001081600004 20010816 00004 EU 2001 8 16 RAIA00108013 1 20010813 A 7330 TNAS1024K1511 TRANSMITTER JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RIGHT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 555HK 11895 1867 41072 76095 7086-STL-DURING TAXI THE RIGHT FUEL FLOW GAUGE SHOWED DASHED LINES, CREW RETURNED TO GATE. MAINTENANCE INSPECTED AND REP LACED THE RIGHT ENGINE FUEL FLOW TRANSDUCER. 2 L 7 2 4T 4 T RT A41NM E18NE 2001081600005 20010816 00005 NM 2001 8 16 DL76P011245 1 20010726 A 5330 146T35311 SKIN BOEING 767 767332 1382001 NM STA 1373, 1395 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1402A 25989 FUSELAGE SKIN DENTED 4" FWD OF STA 1395, AT S-34R AND STA 1373 BETWEEN S-34R AND S-35R. BOTH DAMAGE LOCATIONS ARE TRIMM ED OUT AND DOUBLER/TRIPLER INSTALLED. CORRECTIVE ACTION: ER/A 397815-14 2 L 7 2 4F RT A1NM 2001081600006 20010816 00006 NM 2001 8 16 DL757011247 1 20010725 A 5330 143N34205 SKIN BOEING 757 757232 1384965 NM FS 630, S-25R DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 638DL 23761 FUSELAGE / SKIN / FS 620-640 / STRG. 24R-25R : DAMAGE CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND DENTED AND GOUGED BETWEEN FS 620& 640 AND BETWEEN STRINGERS 24R & 25R. THE DAMAGE WAS REMOVED WITH A 1.7" X 4.2" CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 381397-14. 2 L 7 2 4F RT A2NM 2001081600007 20010816 00007 NM 2001 8 16 DL76G011252 1 20010728 A 2900 272T1200176 LINE BOEING 767 767332 1382001 NM #7 SPOILER CRACKED A DALA O OTHER K FLUID LOSS CR CRUISE 1 SO 27 1612T 30575 RT HYD SYSTEM FLUID LOSS.REPLACED NO.7 SPOILER ACTUATOR LINE WITH TEMP LINE.FWD TO MCO. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS 2 L 7 2 4F RT A1NM 2001081600008 20010816 00008 NM 2001 8 16 DL72S011264 1 20010730 A 5310 65176843 FRAME BOEING 727 727232 1384082 NM FRAME CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 533DA 22046 A 2" CRACK WAS FOUND AT THE FS 416 AFT FRAME OF THE R1 DOOR CUTOUT. THE CRACK WAS CUT OUT AND A REPAIR ANGLE INSTALLED. THE DAMAGE WAS FOUND AT HMV. 2 L 7 3 4F A3WE 2001081600009 20010816 00009 NM 2001 8 16 DL73K011265 1 20010730 A 5310 65465682 WEB BOEING 737 737232 1384475 NM PRESSURE WEB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 317DL 23089 CORROSION WAS FOUND ON THE AFT PRESSURE DOME WEB AT BL 0. THE CORROSION WAS CUT OUT AND A REPAIR DOUBLER INSTALLED. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001081600010 20010816 00010 NM 2001 8 16 DL733011269 1 20010729 A 5330 65458001112 SKIN BOEING 737 7373B7 1384580 NM FS 311, RBL 10 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952WP 23378 FUSELAGE / SKIN / FS 311 / RBL 10 : DENT REPAIR NEAR TCAS ANTENNA DOUBLER THE FUSELAGE SKIN WAS DENTED BY GROUND EQUIPMENT AT FS 311 AND RBL 10, ADJACENT TO THE TCAS ANTENNA CUTOUT REINFORCING DOUBLER. THE DOUBLER WAS REMOVED AND THE DENTS CUTOUT. A NEW ALUMINUM DOUBLER WAS INSTALLED TO REPLACE THE ANTENNA DOUBLER AND TO REPAIR THE DENT CUTOUTS PER ER/A 381241-14, REV B. 2 L 7 2 4F RT A16WE 2001081600011 20010816 00011 NM 2001 8 16 DL76K011278 1 20010802 A 3350 0000 CONNECTOR BOEING 767 767332 1382001 NM CABIN SEPARATED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 172DZ 29691 AISLE SIDE WHITE EMRGENCY LITE INOP AT 3EF. SECURED CONNECTION ON ASSEMBLY. 2 L 7 2 4F RT A1NM 2001081600012 20010816 00012 NM 2001 8 16 DLM88011281 1 20010802 A 2900 AE7055381 HOSE DOUG MD88 MD88 3023688 NM NBR 1 ENG RUPTURED A DALA O OTHER K FLUID LOSS CR CRUISE 1 SO 27 902DE 53379 LT HYD PRESS LOW LIGHT ILLUMINATED ON OAP HYD PRESS WAS ZERO///FOUND PRESS LINE ON LT ENG LEAKING. REPLD LINE 2 L 7 2 4F RT A6WE 2001081600013 20010816 00013 NM 2001 8 16 DL76L011282 1 20010803 A 2120 6066223 FAN 6066223 BOEING 767 767332 1382001 NM LWR FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 186DN 451859 27962 EICAS ADVISORY L RECIR FAN AND INOP LIGHT ON OVERHEAD PANEL.PRIOR TO EICAS MESSAGE - STRONG ELECTRICAL SMELL OF SMOKE IN ALL CABINS. REPLACED FAN ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS 2 L 7 2 4F RT A1NM 2001081600014 20010816 00014 NM 2001 8 16 DL72S011304 1 20010808 A 5330 65545664 SKIN BOEING 727 727232 1384082 NM FS 490, S-28R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 FUSELAGE / SKIN / FS 485-500 / STRG. 27R-28R : CORROSION CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND CORRODED BETWEEN FS 485 & 500 AND BETWEEN STRINGERS 27R & 28R. THE CORROSION WAS REMOVED WITH A 13.5" X 8.25" CUTOUT. THE CUTOUT WAS REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS INSTALLED PER ER/A 381459-14, REV A. 2 L 7 3 4F A3WE 2001081600015 20010816 00015 NM 2001 8 16 DL73K011309 1 20010810 A 5311 FRAME BOEING 737 737232 1384475 NM CABIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 325DL 23097 FS 767, 827, 847 AND 907 FRAMES WERE FOUND WITH THE TYPICAL CRACKS NOTED IN S/B SIIA 737-358. THE CRACKS WERE REMOVED AND REPAIRED PER SRM 51-40-3, FIGURE 1. THE DAMAGE WAS FOUND DURING HMV. 2 L 7 2 4F RT A16WE 2001081600016 20010816 00016 NM 2001 8 16 DL76G011319 1 20010811 A 3350 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM M1209 FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 16065 30199 ON LAYOVER RT OVERWING EXIT EMERGENCY LIGHTS NO TEST REMOVED AND REPLACED EMERGENCY LT POWER SUPPLY M1209 CHECKS GOOD O N TEST 2 L 7 2 4F RT A1NM 2001081600017 20010816 00017 EU 2001 8 16 RAIA00108015 1 20010814 A 2120 2C0015 SEAL JETAIR JETSTM JETSTM4101 1500501 EU LEFT L/E FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 559HK 13313 41075 9545-RIC-LEFT DUCT FAIL CAPTION ILLUMINATED DURING TAXI. MAINTENANCE INSPECTED AND REPLACED LEFT LEADING EDGE BLEED LINE DUCT SEALS. 2 L 7 2 4T RT A41NM 2001081600018 20010816 00018 NM 2001 8 16 VNAA0108005 1 20010809 A 3500 22260A030201 CONTROL UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA O OTHER J O WARNING INDICATION OTHER CL CLIMB 1 GL 07 431JS 6392 2557 3028 DURING CLIMB OUT THE CREW RECEIVED A RED WARNING PANEL INDICATION AND A CABIN ALTITUDE CAS MESSAGE. THE CREW REFERENCED THE QUICK REFERENCE HANDBOOK THEN ADVISED MAINTENANCE CONTROL FLIGHT 4014 WAS RETURNING TO PIT. MAINTENANCE INSPECTED AND REPLACED THE PRESSURE CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 35-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001081600019 20010816 00019 2001 8 16 VNAA0108007 4 20010813 A 3400 BRAKE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE A VNAA C ABORTED TAKEOFF J O WARNING INDICATION OTHER TO TAKEOFF 1 GL 07 459PS 3070 DURING THE TAKE OFF ROLL, THE CREW RECEIVED A HIGH BRAKE TEMPERATURE CAS MESSAGE. THE CREW ABORTED TAKE OFF AND EXITTE D THE RUNWAY AND ALLOWED THE BRAKES TO COOL. FLIGHT 4092 WAS CLEARED FOR ANOTHER TAKE OFF ATTEMPT AND DEPARTED WITH N O FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001081600020 20010816 00020 NM 2001 8 16 01FDEA00715 1 20010731 A 5320 BRACKET BOEING 727 72722 1384002 NM FUSELAGE LOWER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 149FE 19087 N 836 HFEC IND CRACK IN FAILSAFE CHORD AT BS 560, STR 21L, WL 178. R&R CHORD PER SRM 51-20-1 & 51-30-2. 2 L 7 3 4F A3WE 2001082800140 20010828 00140 NM 2001 8 28 01FDEA00720 1 20010815 A 5310 SHEAR TIE BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 CORROSION ON FRAME SHEAR TIE BS 1130, WL 148, RBL 24. REMOVED AND REPLACED SHEAR TIE PER SRM 51-10-3, 51-20-1, 51-10-2. 2 L 7 3 4F A3WE 2001082800141 20010828 00141 NM 2001 8 28 01FDEA00721 1 20010812 A 5311 FRAME BOEING 727 727247 138408F NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 DENT IN FRAME FLANGE AT BS 560, STR 24L. REMOVED AND REPLACED FRAME PER SRM 51-30-2. 2 L 7 3 4F A3WE 2001083100151 20010831 00151 NM 2001 8 31 01FDEA00722 1 20010812 A 5311 FRAME BOEING 727 727247 138408F NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 FRAME 970 DENTED BETWEEN S 25L AND S 26L. REMOVED AND REPLACED FRAME PER SRM 51-40-3, 51-30-1. 2 L 7 3 4F A3WE 2001083100155 20010831 00155 NM 2001 8 31 01FDEA00723 1 20010812 A 5311 FRAME BOEING 727 727247 138408F NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 FRAME DENTED BS 990 AT S 25L. REMOVED AND REPLACED FRAME PER SRM 51-40-3 & EA 7-5310-59284. 2 L 7 3 4F A3WE 2001083100157 20010831 00157 NM 2001 8 31 01FDEA00724 1 20010813 A 5320 WEB BOEING 727 727247 138408F NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 WEB CRACKED BS 344, LBL 12, WL 208. REMOVED AND REPLACED WEB PER EA 7-5310-59259. 2 L 7 3 4F A3WE 2001081700076 20010817 00076 NM 2001 8 17 01FDEA00726 1 20010815 A 5310 SHEAR TIE BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSION (C53-111-02, 2) FWD CARGO BAY BS 700, RBL 9, WL 148 SHEAR TIE FWD & AFT SIDE OF FRAME. REMOVED AND REPLACED S HEAR TIE PER SRM 53-10-4 FIG 15. 2 L 7 3 4F A3WE 2001081600021 20010816 00021 NM 2001 8 16 01FDEA00727 1 20010813 A 5310 FRAME BOEING 727 727247 138408F NM UPR FLANGE DENTED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 N 852 DENT IN UPR FLANGE OF FRAME BS 970, WL 150, LBL 30. ** S/D ** COMING 2 L 7 3 4F A3WE 2001081600022 20010816 00022 NM 2001 8 16 01FDEA00728 1 20010810 A 5710 BUSHING BOEING 727 727233 138408A NM LEFT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277FE 22042 N 971 RH FWD TERMINAL PIN BUSHING CORRODED. R&R BUSHING PER IAW 57-41-011-4. 2 L 7 3 4F RT A3WE 2001082800139 20010828 00139 NM 2001 8 28 01FDEA00719 1 20010815 A 5315 FLOORBEAM BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 CORROSION (C53-111-01, 3) AROUND FASTENER HOLES LWR FLANGE OF 1070 FLOORBEAM BL 0 TO RBL 55. REMOVED AND REPLACED FLANGE PER SRM 53-10-8 FIG 8. 2 L 7 3 4F A3WE 2001081700065 20010817 00065 NM 2001 8 17 01FDEA00691 1 20010813 A 5310 65436833 SHEAR TIE BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSION (C53-113-01-1) ON SHEAR TIE BS 660 BETWEEN STR 25R & 26R. *S/D* REMOVED AND REPLACED SHEAR TIE PER SRM 51-30 -5. 2 L 7 3 4F A3WE 2001081700063 20010817 00063 NM 2001 8 17 01FDEA00689 1 20010813 A 5315 FLOORBEAM BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSION ON FLOORBEAM BS 1070, WL 200, LBL 65-RBL 65. *S/D* REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8, 51-30-2. 2 L 7 3 4F A3WE 2001081700064 20010817 00064 NM 2001 8 17 01FDEA00690 1 20010813 A 5330 SKIN BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSION AT STR 25R AT BS 415 AT STR 9. *S/D* REMOVED AND REPLACED SKIN PER EA 7-5310-58485. 2 L 7 3 4F A3WE 2001081600023 20010816 00023 NM 2001 8 16 01FDEA00729 1 20010810 A 5710 BUSHING BOEING 727 727233 138408A NM LEFT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277FE 22042 N 970 LH FWD TERMINAL PIN BUSHING CORRODED. R&R BUSHING PER 57-41-011-4. 2 L 7 3 4F RT A3WE 2001081600024 20010816 00024 NM 2001 8 16 01FDEA00730 1 20010810 A 5320 SEAT TRACK BOEING 727 727233 138408A NM FUSELAGE TOP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277FE 22042 N 915 #5 MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 1050-1070. R&R SEAT TRACK PER SRM 53-10-5. 2 L 7 3 4F RT A3WE 2001081600025 20010816 00025 NM 2001 8 16 01FDEA00731 1 20010810 A 5320 FITTING BOEING 727 727233 138408A NM FUSELAGE LOWER CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277FE 22042 N 960 NOSE LAND GEAR FWD FITTING CORRODED. R&R FITTING PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2001081600026 20010816 00026 NM 2001 8 16 01FDEA00732 1 20010810 A 5320 INTERCOSTAL BOEING 727 727233 138408A NM FUSELAGE TOP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277FE 22042 N 907 INTERCOSTAL BETWEEN #3 & 4 MAIN CABIN SEAT TRACK BS 1040 CORRODED. R&R INTERCOSTAL PER SRM 53-10-1. 2 L 7 3 4F RT A3WE 2001081600027 20010816 00027 NM 2001 8 16 01FDEA00733 1 20010810 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE TOP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277FE 22042 N 905 BS 1030 FUSELAGE FLOORBEAM CORRODED BETWEEN NR 3 & 4 SEAT TRACKS. R&R FLOORBEAM PER SRM 53-10-8. 2 L 7 3 4F RT A3WE 2001081600028 20010816 00028 NM 2001 8 16 01FDEA00734 1 20010810 A 5310 STRINGER BOEING 727 727233 138408A NM FUSELAGE LOWER CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277FE 22042 N 549 STR 29L CORRODED FROM BS 950E-950F. R&R STRINGER PER SRM 51-40-4, 51-30-2. 2 L 7 3 4F RT A3WE 2001081600029 20010816 00029 NM 2001 8 16 SWAA012183 1 20010801 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 314SW 23336 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, BETWEEN STR'S 14L &15L RE PAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001081600030 20010816 00030 NM 2001 8 16 SWAA012184 1 20010801 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 314SW 23336 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737, STR 18R. REPAIRED S KIN PER SRM. 2 L 7 2 4F RT A16WE 2001081600031 20010816 00031 NM 2001 8 16 SWAA012185 1 20010801 A 5310 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17 & WL 184. REPAIRED WEB PER SWA RA. 2 L 7 2 4F RT A16WE 2001081600032 20010816 00032 NM 2001 8 16 SWAA012186 1 20010802 A 3350 101114 LENS BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 EMERGENCY EXIT LIGHT LENS BROKEN ABOVE ROW 7 ABC. R&R LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001081600033 20010816 00033 NM 2001 8 16 SWAA012187 1 20010802 A 5330 65C33756 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 314SW 23336 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 300, STR 18R. REPAIRED SKI N PER SRM. 2 L 7 2 4F RT A16WE 2001081600034 20010816 00034 2001 8 16 SWAA012188 4 20010801 A 2565 65C16820 FITTING BOEING 737 7373H4 1384600 NM AFT SVC DOOR. LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 353SW 24889 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR GIRT BAR HOOK FLOOR ATTACH FITTING LOOSE. S ECURED FITTING PER MM. 2 L 7 2 4F RT A16WE 2001081600035 20010816 00035 NM 2001 8 16 SWAA012193 1 20010803 A 3350 07912 COVER BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 524SW 26566 EEPLS COVER LOOSE. SECURED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2001081600036 20010816 00036 NM 2001 8 16 SWAA012197 1 20010803 A 2731 BACB28AM07 BEARING BOEING 737 7373H4 1384600 NM TAIL WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 606SW 27926 DURING SCHEDULED C4 CHECK, BOTH LH & RH ELEVATORS FAILED FREE PLAY CHECK. INSTALLED ELEVATOR P USH ROD BEARINGS PER MM. 2 L 7 2 4F RT A16WE 2001081600037 20010816 00037 NM 2001 8 16 SWAA012198 1 20010728 A 5311 6546529 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D CHECK, FOUND FRAME SHEAR TIE CORRODED AT BS 480, LBL 10 & WL149. R&R S HEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2001081600038 20010816 00038 NM 2001 8 16 SWAA012200 1 20010731 A 5310 6547978 CREASE BEAM BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 520SW 25319 DURING SCHEDULED D CHECK, FOUND CREASE BEAM CRACKED AT BS 520, LBL 59. REPAIRED CREASE BE AM PER SRM. 2 L 7 2 4F RT A16WE 2001081600039 20010816 00039 NM 2001 8 16 GAIA01284 1 20010723 A 3350 15AT41 SWITCH BOEING 727 727222 1384073 NM O/H PANEL INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 90AX 20040 DURING PERIODIC SERVICE CHECK, THE EMERGENCY EXIT LIGHT 'ARM AND ON' SWITCH WOULD NOT TURN LIGHTS OFF. MAINTENANCE REMV OED AND REPLACED EMERGENCY EXIT LIGHT 'ARM AND ON' SWITCH. SYSTEM WAS OPERATINOAL CHECKED OK PER BOEING 727 MM CHAP 33- 50. (M) 2 L 7 3 4F A3WE 2001081600040 20010816 00040 NM 2001 8 16 SWAA012203 1 20010803 A 5320 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED SPECIAL, FOUND A .75 LONG VERTICAL BEAM WEB CRACK AT BS 179, LBL 17.1 & WL 227. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001081600041 20010816 00041 NM 2001 8 16 TSAA0153085 1 20010712 A 5300 6545871517 SKIN BOEING 737 7372S2C 138448G NM CRACKED A TSAA O OTHER O OTHER IN INSP/MAINT 1 WP 13 806AL 21927 FOUND FUSELAGE SKIN CRACKED AT FORWARD GALLEY DOOR UPPER DOOR HINGE CUTOUT. TRIMMED OUT DAMAGE AREA TO MAINTAIN A MINIM UM RADIUS OF .70 INCH, HFEC INSPECTION AROUND CUTOUT AREA NO DEFECTS NOTED. FABRICATED AND INSTALLED .50 INCH 2024-T3 F ILLER AND .063 INCH CRES DOUBLER WITH CHAMFERED EDGES, REMOVED ALL NICKS, BURRS, SCRATCHES, GOUGES AND SHARP EDGES FROM SKIN AND ALL REPAIR PARTS IAW SRM 53-30-3 FIG 20 AND ECO 3233. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2001081600042 20010816 00042 NM 2001 8 16 TSAA0153090 1 20010723 A 5330 65523254 SKIN BOEING 737 7372Q9 138448M NM BS 727 CRACKED A K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 IDENTIFIED 1.5 INCH FUSELAGE SKIN CRACK AT BS 727, S16R. REMOVED TWO PREVIOUS REPAIRS IN THE IMMEDIATE AREA, TRIM OUT D AMAGED AREA, HFEC INSPECTION COMPLETED AROUND TRIM AREA NO DEFECTS NOTED, .040 INCH INSURANCE CUT COMPLETED, VISUALLY IN SPECTED AREA UNDER REPAIR DOUBLERS NO DEFECTS NOTED, FABRICATED AND INSTALLED .032 INCH 2024-T3 DOUBLER AND .050 INCH 20 24-T3 TRIPLER, FINISHED ALL BARE ALUMINUM WITH ALODINE AND TWO COATS OF BMS 10-11 TYPE 1 PRIMER, INSTALLED COUNTERSINK R EPAIR WASHERS AT EXISTING COUNTERSINK LOCATIONS UNDER REPAIR DOUBLER, INSTALLED REPAIR PARTS WITH BMS 5-95 SEALANT BETWE EN FAYING SURFACES AND AROUND EDGES OF REPAIR. INSTALLED ALL FASTENERS WET WITH BMS-5-95 SEALANT, APPLIED CORROSION INH 2 L 7 2 4F A16WE 2001081600043 20010816 00043 WP 2001 8 16 USAA010803 1 20010601 A 5300 FRAME DOUG DC9 DC981 3022081 WP BS 1497 CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 812US 53328 48092 PIT - FOUND FRAME CHAFED .25 INCH, STATION 1497 CANTED AT L17R. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-01 FIG 2. (M) 2 L 7 2 4F A6WE 2001081600044 20010816 00044 WP 2001 8 16 USAA010808 1 20010627 A 5310 FRAME DOUG DC9 DC981 3022081 WP BS 1485 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 827US 53144 48049 PIT - FOUND FRAME CRACKED 2 INCHES, CANTED STATION 1485 AT LONGERON 3L. STOP DRILLED CRACK, INSTALLED DOUBLER PER SRM 5 3-01 FIG 2. (M) 2 L 7 2 4F A6WE 2001081600045 20010816 00045 WP 2001 8 16 USAA010800 1 20010703 A 5300 SKIN DOUG DC9 DC982 3022082 WP BS 1437 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 830US 41348 49443 PIT - FOUND SKIN CRACKED .5 INCH, STATION 1437 L3L. CUT OUT DAMAGE, INSTALLED DOUBLER AND FILLERS PER SRM 53-04 FIG 27. (M) 2 L 7 2 4F A6WE 2001081600046 20010816 00046 NM 2001 8 16 USAASB01206 1 20010717 A 3350 1000679 LIGHT BOEING 737 7372B7 1384560 NM PAX CABIN FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 283AU 23116 ALB - THE AFT SERVICE DOOR EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. (M) 2 L 7 2 4F A16WE 2001081600047 20010816 00047 NM 2001 8 16 USAABB01064 1 20010715 A 3350 SWITCH BOEING 767 767201 1385125 NM F/A PANEL INOPERATIVE A USAA K NONE O OTHER NR NOT REPORTED 1 EA 19 648US 23900 FRA - THE EMERGENCY EXIT LIGHT AT THE LEFT OVERWING EXIT FLICKERS ON AND OFF. MAINTENANCE TIGHTENED A LOOSE EMERGENCY L IGHT SWITCH ON THE FORWARD FLIGHT ATTENDANT'S PANEL. (M) 2 L 7 2 4F RT A1NM 2001081600048 20010816 00048 NM 2001 8 16 USAABB01047 1 20010624 A 2500 3971003 CART BOEING 767 7672B7 1385107 NM AFT GALLEY INOPERATIVE A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 652US 24765 BOS - FLT 14 - APPROXIMATELY 35 MINUTES AFTER DEPARTURE, AN ELECTRICAL BURNING SMELL WAS NOTED IN THE AFT GALLEY. THE C REW WAS UNABLE TO LOCATE THE SOURCE. THE FLIGHT DIVERTED TO BOS AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE DETER MINED THAT THE SMELL WAS COMING FROM AN OVEN CART WHICH WAS REMOVED FROM THE AIRCRAFT. (M) 2 L 7 2 4F RT A1NM 2001081600049 20010816 00049 NM 2001 8 16 USAASB01208 1 20010718 A 3350 1619 LIGHT BOEING 737 7374B7 138449C NM EXTERIOR UNSECURE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 439US 24781 BWI - MAINTENANCE FOUND THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE RESECURED THE RIGHT FORWARD EXTERIOR EMERGENCY EXIT BULB INTO ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001081600050 20010816 00050 NM 2001 8 16 USAA010614 1 20010605 A 5300 FRAME BOEING 757 757225 1384959 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 51539 22192 CLT - FOUND FRAME CRACKED .75 INCH, BS 520, BETWEEN S24L AND S25L. DAMAGED REMOVED, INSTALLED FRAME REPAIR DOUBLER PER EA 69565A. (M) 2 L 7 2 4F RT A2NM 2001081600051 20010816 00051 NM 2001 8 16 USAA010620 1 20010608 A 5300 SKIN BOEING 757 757225 1384959 NM BS 584 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 51539 22192 CLT - FOUND FUSELAGE INNER SKIN CORRODED APPROXIMATELY 2 SQUARE INCHES, BS 584, STRINGER 28R. REMOVED DAMAGE, INSTALLED DOUBLER AND TRIPLER PER EA 69643. (M) 2 L 7 2 4F RT A2NM 2001081600052 20010816 00052 NM 2001 8 16 USAA010611 1 20010605 A 5300 SKIN BOEING 757 757225 1384959 NM BS 555-572 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 51539 22192 CLT - FOUND INNER SKIN SURFACE CORRODED APPROXIMATELY 10 SQUARE INCHES, BS 555 TO 572, STRINGER 28R. DAMAGE REMOVED, IN STALLED REPAIR DOUBLER AND TRIPLER PER EA 69643. (M) 2 L 7 2 4F RT A2NM 2001081600053 20010816 00053 WP 2001 8 16 HALA0100178 1 20010715 A 2400 BATTERY DOUG DC9 DC951 3022051 WP A HALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 13 649HA 47715 HNL - FLT 119 - SMOKE COMING FROM E/E COMPARTMENT, SUSPECT BATTERY RUNAWAY, PULLED BATTERY/CHARGER C/B. REMOVED AND REP LACED BATTTERY AND CHARGER, OPS CHECK OF BATTERY CHARGING AND CYCLING OK. (M) 2 L 7 2 4F RT A6WE 2001081600054 20010816 00054 EA 2001 8 16 MASA01062 1 20010708 A 3300 58728 COVER CNDAIR CL600 CL6002B19 EA CABIN DIRTY A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 27191 7191 FLT 8700 - CMH-ORD - ON PREFLIGHT, CAPTAIN REPORTED DIM EMERGENCYN FLOOR TRACK LIGHTING. MAINTENANCE CLEANED THE TOP CO VER OF THE TRACK LIGHTING SYSTEM ASSEMBLY. OPS CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2001081600055 20010816 00055 NM 2001 8 16 SWAA012209 1 20010805 A 3350 285A178010 CONTROL PANEL BOEING 737 7377H4 NM CABIN ERRATIC A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 405WN 27893 OVERHEAD BULL NOSE EMERGENCY LIGHTS OPERATE INTERMITTENTLY DURING FLIGHT. R&R F/A'S LIGHT CONTROL PANEL PER MM. 2 L 7 2 4F RT A16WE 2001081600056 20010816 00056 NM 2001 8 16 SWAA012215 1 20010807 A 5311 6546546 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 520SW 25319 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT STR 8L, BS 400, BS 787 & BS 827. RE PAIRED FUSELAGE FRAMES PER SRM & BFG ER. 2 L 7 2 4F RT A16WE 2001081600057 20010816 00057 NM 2001 8 16 SWAA012216 1 20010807 A 5311 6546546 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 520SW 25319 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT STR 8R, BS 400, BS 747, BS 787 & BS 867. REPAIRED FUSELAGE FRAMES PER SRM & BFG ER. 2 L 7 2 4F RT A16WE 2001081600058 20010816 00058 NM 2001 8 16 SWAA012219 1 20010730 A 5310 BAC1503 STIFFENER BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 665WN 23497 DURING SCHEDULED 1/4D CHECK AT DALFORT, FOUND STIFFENER CRACKED AT BS 178, LH & WL 195. REPAIRE D STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 2001081600059 20010816 00059 NM 2001 8 16 SWAA012220 1 20010806 A 5330 6545766 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 324, STR 17R. REPAIRED SKIN PE R BFG ER. 2 L 7 2 4F RT A16WE 2001081600060 20010816 00060 2001 8 16 SWAA012221 4 20010802 A 2565 6557463 BRACKET BOEING 737 7373Y0 1384671 NM AFT SVC DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 665WN 23497 DURING SCHEDULED 1/4D CHECK AT DALFORT, FOUND CORRODED NUTPLATE AT AFT SVC DOOR EMERGENCY EVAC SLIDE AFT MOUNT BRACKET. R&R BRACKET NUTPLATE PER SRM. 2 L 7 2 4F RT A16WE 2001081600061 20010816 00061 NM 2001 8 16 SWAA012222 1 20010807 A 3350 207377 LENS BOEING 737 7377H4 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 713SW 27847 EEPLS LENS MISSING AT ROW 7. INSTALLED EEPLS LENS PER MM. 2 L 7 2 4F RT A16WE 2001081600062 20010816 00062 NM 2001 8 16 SWAA012224 1 20010806 A 5310 6545410 BEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D CHECK, FOUND LONGITUDINAL BEAM CRACKED AT BS 727B, RBL 45 & WL 208. REP AIRED BEAM PER BFG ER. 2 L 7 2 4F RT A16WE 2001081600063 20010816 00063 NM 2001 8 16 SWAA012225 1 20010804 A 5310 6545410 WEB BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D CHECK, FOUND LOGITUDINAL BEAM WEB CRACKED AT BS 706-708, BL 0 & LBL 25, WL 203. REPAIRED WEB PER BFG ER. 2 L 7 2 4F RT A16WE 2001081600064 20010816 00064 NM 2001 8 16 SWAA012229 1 20010809 A 3350 101114 LENS BOEING 737 7372T4 1384492 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED A2 CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED EXIT LIGHT LENS PER MM. 2 L 7 2 4F A16WE 2001081600065 20010816 00065 NM 2001 8 16 SWAA012231 1 20010808 A 3350 207377 LENS BOEING 737 7377H4 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 713SW 27847 EEPLS LENS MISSING AT ROW 7. INSTALLED EEPLS LENS PER MM. 2 L 7 2 4F RT A16WE 2001081600066 20010816 00066 NM 2001 8 16 SWAA012233 1 20010809 A 3350 207377 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 EEPLS LENS LOOSE IN FWD CABIN. SECURED EEPLS LENS PER MM. 2 L 7 2 4F RT A16WE 2001081600067 20010816 00067 NM 2001 8 16 SWAA012235 1 20010809 A 5310 6545409 WEB BOEING 737 7373H4 1384600 NM MAIN WHEEL WELL CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED 1/2D CHECK, FOUND BEADED WEB CRACKED AT BS 663, LBL 32. REPAIRED WEB PER SWA T1-353-046. 2 L 7 2 4F RT A16WE 2001081600068 20010816 00068 NM 2001 8 16 SWAA012236 1 20010808 A 5310 6516352 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D CHECK, FOUND FWD CARGO DOOR CUTOUT FRAME CRACKED AT BS 492, RBL 36 & WL 159. REPAIRED FRAME PER BFG ER. 2 L 7 2 4F RT A16WE 2001081600069 20010816 00069 NM 2001 8 16 SWAA012262 1 20010813 A 3350 07912 COVER BOEING 737 7377H4 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 700GS 27835 EEPLS COVER BROKEN FWD CABIN. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2001081600070 20010816 00070 NM 2001 8 16 SWAA012265 1 20010813 A 5754 6573714 SLAT BOEING 737 7373H4 1384600 NM RH WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED 1/2D CHECK, FOUND # 6 SLAT LOWER SKIN CRACKED INBD OF ACTUATOR. REPAIRED SLAT PE R SRM. 2 L 7 2 4F RT A16WE 2001081600071 20010816 00071 NM 2001 8 16 SWAA012266 1 20010811 A 5320 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL BEAM WEB CRACKED .50 LONG AT BS 185, RBL 17.1 & WL 227. R&R VERTICAL BEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2001081600072 20010816 00072 NM 2001 8 16 SWAA012267 1 20010812 A 5310 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIES CORRODED AT BS 827 BETWEEN STR 27R & STR 27L. R EPAIRED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 2001081600073 20010816 00073 NM 2001 8 16 SWAA012269 1 20010810 A 5310 6517582 WEB BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 074SW 22674 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED AT BS 180, RBL 17.1 & WL 227. R&R VERTICAL BEAM WEB PER SRM. 2 L 7 2 4F A16WE 2001081600080 20010816 00080 NM 2001 8 16 01FDEA00597 1 20010725 A 7830 LINE BOEING 727 7272S2F 1384O81 NM THRUST REVERSER LEAKING A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION UK UNKNOWN 1 SO 25 213FE 22935 NR 1 ENG STRUT O/H IL FOR 5 SEC. RAN RED TABS WING A/I SWITCH WAS CK. SYS TEST GOOD. REMOVED AND REPLACED LEAKING FLE X LINE PER SMP AND OPS CK NORM PER MM 26-14-000-5. 2 L 7 3 4F A3WE 2001081600081 20010816 00081 2001 8 16 SWAA012240 4 20010805 A 2565 6557463 FITTING BOEING 737 7375H4 138449D NM AFT SVC DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 520SW 25319 DURING SCHEDULED D CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING ANCHOR NUT BROKEN. R&R GIRT BAR FITTING ANCHOR NUT PER MM. 2 L 7 2 4F RT A16WE 2001081600082 20010816 00082 2001 8 16 SWAA012245 4 20010809 A 2565 65C34691 GIRT BAR BOEING 737 7373Y0 1384671 NM AFT SVC DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 682SW 23496 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUSTMENT. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001081600083 20010816 00083 NM 2001 8 16 SWAA012248 1 20010808 A 3350 07912 COVER BOEING 737 7377H4 NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 778SW 27883 EEPLS COVER DAMAGED AT OVERWING EXIT ROW. R&R EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2001081600084 20010816 00084 NM 2001 8 16 SWAA012253 1 20010809 A 5310 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 379SW 26586 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIES CORRODED BETWEEN STR 26L & 26R AT BS 767, BS 787 & BS 807. REPAIRED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 2001081600085 20010816 00085 NM 2001 8 16 SWAA012255 1 20010703 A 5330 6546529 SHEAR TIE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, STR 14R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F A16WE 2001081600086 20010816 00086 NM 2001 8 16 SWAA012256 1 20010709 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGERS 15L & 15R CRACKED BETWEEN BS 520 & BS 540. REPA IRED STR PER SRM. 2 L 7 2 4F A16WE 2001081600087 20010816 00087 NM 2001 8 16 SWAA012257 1 20010808 A 2731 DAS42101 BEARING BOEING 737 7375H4 138449D NM RH ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 520SW 25319 DURING SCHEDULED D CHECK, FOUND RH ELEVATOR TAB ROD END BEARINGS WORN. R&R ELEVATOR TAB ROD END BEA RINGS PER OHM. 2 L 7 2 4F RT A16WE 2001081600088 20010816 00088 NM 2001 8 16 SWAA012274 1 20010813 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED C2 CHECK, FOUND LH OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED EXIT LIG HT LENS PER MM. 2 L 7 2 4F RT A16WE 2001081600089 20010816 00089 NM 2001 8 16 SWAA012276 1 20010814 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 1 1/2 LONG AT BS 430, STR 10R. REP AIRED SKIN PER SWA RA . 2 L 7 2 4F A16WE 2001081600090 20010816 00090 NM 2001 8 16 SWAA012278 1 20010813 A 5311 6547951 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 068SW 22357 DURING SCHEDULED PM CHECK, FOUND AFT CARGO DOOR CUT OUT FRAME CORRODED AT BS 792, BOTTOM RH CORNER. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2001081600091 20010816 00091 NM 2001 8 16 01FDEA00664 1 20010731 A 5311 FRAME BOEING 727 72722 1384002 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 149FE 19087 HFEC IND A CRACK IN THE FAIL-SAFE CHORD AT BS 560, STR 21L, WL 178. 2 L 7 3 4F A3WE 2001081600092 20010816 00092 NM 2001 8 16 01FDEA00667 1 20010807 A 3230 656021123 ACCESSORY UNIT BOEING 727 7272S2F 1384O81 NM E/E BAY FAILED A FDEA O OTHER E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 25 204FE 22926 AFT T/O LG LEVER W/N RAISE PAST OFF POS. LOUD NOISE AND VIB OCCURRED WITH NOSE WHEEL. REMOVED AND REPLACED LAND POSITI ON WARN ASSY UNIT PER MM 32-09-121-4. 2 L 7 3 4F A3WE 2001081600093 20010816 00093 NM 2001 8 16 01FDEA00670 1 20010809 A 5311 FRAME BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 UPPER FLANGE OF BS 1090 FRAME HAS OPEN HOLE WITH CORROSION UNDER LT FLOOR TO SIDEWALL SUPPORT. 2 L 7 3 4F A3WE 2001081600094 20010816 00094 EU 2001 8 16 01FDEA00671 1 20010810 A 2920 HYDRAULIC SYSTEM AIRBUS 310 A310 EU YELLOW SYS FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 410FE 356 ON CLIMB LOST YELLOW SYS HYD QTY WENT TO RED DOT. PERF EMERGENCY CHECKLIST PER ECAM AND RED TABS. 2 L 7 2 4F RT A35EU 2001081600095 20010816 00095 NM 2001 8 16 1304 1 20010802 A 5230 STRUCTURE DHAV DHC8 DHC8102 2809003 NM CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - CARGO DOOR DAMAGED AT FORWARD STRUCTURE CABLE FEED-THROUGH BY CABLE CHAFING. REPAIRED IAW HORIZON AIR EA 9-52-122 . 2 H 7 2 4T RT A13NM 2001081600097 20010816 00097 WP 2001 8 16 ARWA0010806 1 20010815 A 7100 UL19659 FAN BLADE LKHEED 1011 1011385114 WP RROYCE RB211 RB211524B402 54555 NE BINDING A ARWA E ENGINE SHUTDOWN E VIBRATION/BUFFET CR CRUISE 1 SO 19 260FA 1158 14734 During cruise # 2 engine shut down due to vibration enroute to CLO. Continue Flt., landing CLO.Corrective Action: Insp ected # 2 engine IAW MM fault isolation 71-91-00, configuration 2, figure 103, and no damage found. Blades # 11 and # 1 2 found to be locked. Cleaned and lubricated midspan clappers IAW MM 72-31-05 and performed vibration survey # 11 IAW M M 71-00-00. Virbration found to be without limits at all monitor modes. Engine # 2 found serviceable, and the aircraft was returned to service. 2 L 7 3 4F 4 F A23WE E12EU 2001081600101 20010816 00101 NM 2001 8 16 2001UALA00854 1 20010801 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 1131 RBL 45 FLOORBEAM T-CAP CORRODED. *S/D* FABRICATED AND INSTALLED T-CAP REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001081600104 20010816 00104 EU 2001 8 16 2001UALA01394 1 20010714 A 3610 342B030000 THERMOSTAT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE BLEED AIR FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 406UA 454 NR 1 ENGINE BLEED FAULT DISPLAYED ON UPPER ECAM SCREEN. *S/D* REPLACED CONTROL THERMOSTAT AS FAULTED IN CENTRALIZED F AULT DISPLAY SYSTEM. IN ADDITION, THE HEAT EXCHANGER OUTLET TEMPERATURE SENSOR AND BLEED MANAGEMENT COMPUTER WERE REPLA CED PRECAUTIONARY. NO FURTHER FAULTS NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2001081600105 20010816 00105 NM 2001 8 16 2001UALA01416 1 20010718 A 2121 EVT3454G BLOWER AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE E/E BAY FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 827UA 1022 AVIONICS VENT FAULT AND A SUBSEQUENT AVIONICS EXTRACT FAULT. *S/D* REPLACED AVIONICS BLOWER FAN AND SYSTEM FILTER, NO OTHER DAMAGE NOTED. NO FURTHER FAULTS. 2 L 7 2 4F 4 F RT A28NM E40NE 2001082900041 20010829 00041 NE 2001 8 29 2001UALA01434 2 20010720 A 7321 FCU BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE NR 3 ENGINE OUT OF ADJ A UALA O OTHER O OTHER CL CLIMB 1 WP 29 620UA 21880 709617 NR 3 ENGINE REPORT POWER FLUCTUATES SYMPTOMS OR PATTERN ALONG WITH FAULT CODES FRM CODE 7321 XD. RT ENG EPR+EGT FLUCTUA TES AFTER PWR CHNG IN CLRWX CON DURING CLIMB EPR+-. CAUSE BY BLEED VALVE CYCLING DUE TO DECELERATION SCHEDULE BEING TO C LOSE TO THE STEADY STATE OPERATING BAND. THE TT2 SENSOR (TOTAL TEMPERATURE) PROBE FOR THE FUEL CONTROL (FCU) WAS REPLA CED. THE FINAL FIX WAS ADJUSTING THE FCU DECELERATION SCHEDULE, AWAY FROM THE OPERATING BAND. 2 L 7 2 4F 4 F RT A1NM E3NE 2001103000010 20011030 00010 NE 2001 10 30 2001UALA01461 2 20010721 A 7321 8088001 FMU BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LT ENGINE DEFECTIVE A UALA O OTHER O OTHER CR CRUISE 1 WP 29 771UA 20638 20638 26932 777008 L ENG EPR FLUX APPROX. .02 AT CRUISE. ALL OTHER ENG PARAMETERS FOLLOW FLUCTUATION. AUTOTHROTTLE DISCONNECT NO HELP. SU PPLEMENTAL DATA UPDATE REPLACED FUEL METERING UNIT P/N 808800-1 S/N F32614 AT PART TOTAL TIME 20638. EPR FLUX HAS NOT REOCCURRED TO DATE ON ENGINE W/ NEW FMU. UNIT WAS TESTED, DISCOVERED BAD MPSOV PROXIMITY SENSOR. DURING OVERHAUL DISC OVERED WEAR ON MPSOV, LVDT HOUSING AND PISTON. PARTS REPLACED AND UNIT RELEASED FOR SERVICE (MR73205-33). P/N:806829-1, 808678-1,811399-11,811399-21, 2 L 7 2 4F 4 F RT T0001SE E46NE 2001081600107 20010816 00107 EU 2001 8 16 2001UALA01586 1 20010801 A 3610 7850027 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE BLEED AIR FAULTY A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 435UA 613 UNSCHEDULED LANDING DUE TO LOSS OF NR 1 ENGINE BLEED. *S/D* FOUND LEAKING CLAMPS AT GROUND AIR START CONNECTION (FIXED PROBLEM ON NR 1 BLEED), AND REPLACED NR 2 BLEED AIR MONITORING COMPUTER FOR NR 2 BLEED PROBLEM. NO FURTHER DISCREPANCI ES HAVE BEEN REPORTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2001081600108 20010816 00108 NE 2001 8 16 2001UALA01599 2 20010802 A 7261 50J04101 TUBE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE RT ENGINE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 221UA 380 30552 222156 UNSCHEDULED ENGINE REMOVAL DUE TO CRACK IN NR 3 BEARING OIL PRESSURE TUBE FOUND DURING INSPECTION. PRATT & WHITNEY REC ALLED CERTAIN P/N 50J041-01 OIL TUBES DUE TO POTENTIAL CRACKING AT CONTAMINATED WELD BEAD, AND NOTIFIED US OF THE POSSIB ILITY THAT NR 3 BEARING OIL PRESSURE TUBES SUBJECT TO RECALL MAY HAVE BEEN INSTALLED AT MANUFACTURE OF BOTH ENGINES ON A IRPLANE N221UA. ENGINES WERE INSPECTED PER P&W SI 76F-01. THE LEFT ENGINE PASSED, BUT A CRACKED TUBE WAS FOUND IN THE RIGHT ENGINE. THE ENGINE WAS REMOVED AND SENT TO P&W. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001081600109 20010816 00109 NM 2001 8 16 2001UALA01600 1 20010804 A 5347 SEAT TRACK BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 913UA 25291 AFT CABIN RT FLOOR SECTION OF SEAT TRACK AT BS 986 - BS 1016, RBL 39 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. REPLACE D SEAT TRACK. 2 L 7 2 4F 4 F RT A16WE E2GL 2001081600110 20010816 00110 NM 2001 8 16 2001UALA01601 1 20010804 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 913UA 25291 FWD CABIN FLOORBEAM UPPER CORD HAS EXCESSIVE MATERIAL REMOVED AT BS 312, LBL 14, 20, 23 AND LBL 57. MAJOR REPAIR ACCOMP LISHED. REMOVED DAMAGED T-CAP, SPLICE IN NEW SECTION REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001081600111 20010816 00111 NE 2001 8 16 2001UALA01602 2 20010803 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 FAILED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 532UA 25072 NR 2 ENGINE INFLIGHT SHUTDOWN. ENG IND SHOWED LOW OIL PRESS AND NO N1 OR N2 ROTATION. IFSD OCCURRED IN CRUISE FLT. 2 L 7 2 4F 4 F RT A2NM E17NE 2001081600112 20010816 00112 NM 2001 8 16 2001UALA01603 1 20010805 A 5310 CREASE BEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 913UA 25291 CABIN RT CREASE BEAM WEB HAS TWO ELONGATED HOLES BETWEEN BS 907 TO 927, WL 208. MAJOR REPAIR ACCOMPLISHED. REPLACED WE B. 2 L 7 2 4F 4 F RT A16WE E2GL 2001081600113 20010816 00113 NM 2001 8 16 2001UALA01604 1 20010805 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 914UA 25381 STA 188 FRAME IS CRACKED IN BEND RADIUS ON RT SIDE AT WL 207, EXTENDING ABOVE AND BELOW WL 207. MAJOR REPAIR ACCOMPLISH ED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001081600114 20010816 00114 NM 2001 8 16 2001UALA01605 1 20010806 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 FUSELAGE SKIN CRACKED FUSE STA 727D ON STR 24RT. MAJOR REPAIR ACCOMPLISHED. DOUBLER AND FILLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001081600115 20010816 00115 NM 2001 8 16 2001UALA01606 1 20010806 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 322UA 23954 CABIN STA 787 FRAME JUST ABOVE STR 9R IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE AND INSTALLED FUSE CROWN F RAME REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082200049 20010822 00049 NM 2001 8 22 2001UALA01607 1 20010802 A 5522 183W00613 SKIN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE ELEVATOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 217UA 30550 545 DAMAGE FOUND ON LT ELEVATOR UPPER SURFACE, APPROX 18 INCHES OUTBOARD OF INBOARD EDGE AND 18 INCHES FWD OF T/E PUNCTURE I S APPROX 1.75 INCHES IN DIAMETER AND 1.25 INCHES DEEP. *S/D* MAJOR REPAIR: ACP REPAIR ON LT ELEVATOR PER SRM. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001091400097 20010914 00097 NM 2001 9 14 2001UALA01609 1 20010805 A 2913 69287276 PUMP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE HYDRAULIC SYS FAILED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 7282U 21560 AIRCRAFT EXPERIENCED B-HYDRAULIC SYSTEM ZERO QUANTITY INDICATION DURING CRUISE. AIRCRAFT CONTINUED TO ORD. THE NR 1 ENG INE HYDRAULIC PUMP FAILED. REPLACED NR 1 ENGINE HYDRAULIC PUMP, SYSTEM TESTS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001081600116 20010816 00116 NM 2001 8 16 2001UALA01610 1 20010803 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 176UA 24383 EMERGENCY CEILING LIGHT 58 ABC AISLE INOP. 2 L 7 4 4F 4 F RT A20WE E24NE 2001090600373 20010906 00373 NM 2001 9 6 2001UALA01614 1 20010803 A 2612 CONTROL UNIT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FIRE DETECTION MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 906UA 25006 UNSCHEDULED LANDING DUE TO FIRE BELL ACTIVATION. REMOVED AND REPLACED FIRE OVERHEAT DETECTOR CONTROL UNIT AND ENG/APU FI RE CONTROL MODULE. PERFORMED OPERATIONAL TEST AND AIRCRAFT WAS RETURNED TO REVENUE SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082900050 20010829 00050 EU 2001 8 29 2001UALA01616 1 20010805 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 443UA 820 FUSELAGE SKIN DAMAGED AT FRAME 73 TO FRAME 74 BETWEEN STRINGER 31 LEFT TO 33 LEFT. MAJOR REPAIR ACCOMPLISHED. FOUR SHE AR TIES REPLACED AND STRINGER SPLICE ACCOMPLISHED. FILLER AND DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A28NM E40NE 2001081600118 20010816 00118 NM 2001 8 16 2001UALA01618 1 20010802 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 181UA 25278 EMERGENCY EXIT SIGN AT ROW 22B HAS SOME LAMPS INOP. 2 L 7 4 4F 4 F RT A20WE E24NE 2001081600119 20010816 00119 NE 2001 8 16 2001UALA01619 2 20010804 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEFT VIBRATION A UALA K NONE E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 WP 29 575UA 26689 LEFT ENG VIB IND FLUCTUATES BETWEEN 1.0 & 1.5 IN CRUISE AT 350. VIB FELT THROUGHOUT AIRCRAFT AND INCREASES INVERSELY WI TH THROTTLE. FOUND METAL IN THE TAILPIPE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001081600120 20010816 00120 NM 2001 8 16 2001UALA01620 1 20010807 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 913UA 25291 AFT CABIN FLOORBEAM UPPER T-CAP HAS CORROSION AT BS 947.5 LBL 15. INSTALLED REINFORCING STRAP AND ANGLE DOUBLER. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001081600121 20010816 00121 NM 2001 8 16 2001UALA01621 1 20010807 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 913UA 25291 AFT CABIN FLOORBEAM T-CAP HAS CORROSION STA 947.5 RBL 25 TO RBL 33. REMOVED DAMAGE. INSTALLED REINFORCEMENT REPAIR. M AJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001081600122 20010816 00122 NM 2001 8 16 2001UALA01622 1 20010806 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 322UA 23954 STA 727E STR 9R FUSELAGE BODY FRAME CRACKED AT FASTENER HOLE FOR PSU RAIL ATTACH BRACKET. REAMED HOLE TO REMOVE DAMAGE. MANUFACTURED AND INSTALLED DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001081600123 20010816 00123 NM 2001 8 16 2001UALA01623 1 20010806 A 5230 WEB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 344UA 24248 FWD CARGO DOOR TORQUE TUBE CTR BRG SUPPORT WEB CRACKED. WEB REPLACED. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001102600018 20011026 00018 NM 2001 10 26 2001UALA01625 1 20010804 A 5270 834403 PROXIMITY SENSOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY EXIT FAILED A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 673UA 29241 RIGHT FWD EMERGENCY DOOR EICAS MSG. REPLACED DOOR PROXIMITY SENSOR. 2 L 7 2 4F 4 F RT A1NM E24NE 2001101200051 20011012 00051 NE 2001 10 12 2001UALA01626 2 20010729 A 7200 53L032 BLADE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE FRACTURED A UALA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION NR NOT REPORTED 1 WP 29 647UA 18457 18457 25284 727677 VIBRATION ON NR 1 ENGINE, EEC MODE EICAS ILLUMINATED, EGT FLUCTUATED BETWEEN 120 AND 180 AT IDLE, EPR INDICATION LOST, N 1 & N2 INDICATIONS NORMAL. CREW ELECTED TO SHUT DOWN ENGINE AND RETURN TO FIELD. *S/D* 1 EA T2 BLADE FAILED AT THE PL ATFORM. 2 EA ADJACENT BLADES WERE BROKEN OFF AT MID SPAN. THE RESULTANT HIGH N2 VIBRATION CAUSED THE P4.95 MANIFOLD TO FAIL WHICH CAUSED LOSS OF EPR INDICATION AND REVERSION TO ALTERNATE MODE. ENGINE WAS REMOVED FOR REFURBISHMENT. 2 L 7 2 4F 4 F RT A1NM E24NE 2001081600125 20010816 00125 NM 2001 8 16 2001UALA01629 1 20010801 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 740 STR 39L-39R SHEAR TIE CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091400099 20010914 00099 NE 2001 9 14 2001UALA01630 2 20010803 A 7321 KD4A019 RELAY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT FUEL CONTROL FAILED A UALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 29 643UA 25093 724378 LEFT ENG DIFFICULT TO SHUTDOWN. DELAYED SHUTDOWN OF LEFT ENGINE AT GATE ARRIVAL. REPLACED FUEL/IGNITION CONTROL RELAY K -D4A019 IN P36 MISC ELECTRICAL EQUIPMENT PANEL. 2 L 7 2 4F 4 F RT A1NM E24NE 2001091400100 20010914 00100 NM 2001 9 14 2001UALA01632 1 20010805 A 2150 213W31204 DOOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE RT RAM AIR DAMAGED A UALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 29 205UA 28714 EN ROUTE FROM FRA TO DEN AIRCRAFT DIVERTED TO LHR DUE TO VIBRATION ON THE RIGHT SIDE OF THE AIRPLANE. FOUND RT RAM AIR I NLET DOOR FAILED RESULTING IN VIBRATION AND DAMAGE TO RAM AIR INLET DUCT. DOOR ASSY WAS REPLACED AND INLET DUCT WAS REP AIRED. A/C RETURNED TO REVENUE SERVICE WITHOUT FURTHER INCIDENT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001081600126 20010816 00126 NM 2001 8 16 2001UALA01633 1 20010807 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 913UA 25291 AFT CABIN FLOOR BEAM UPPER T-CAP HAS CORROSION AT BS 947.5 LBL 15. MAJOR REPAIR ACCOMPLISHED. INSTALLED REINFORCING ST RAP AND ANGLE DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001081600127 20010816 00127 NM 2001 8 16 2001UALA01634 1 20010807 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 322UA 23954 STA 178 BULKHEAD SKIN IS DENTED AT FASTENER HOLES WL 184.5 RBL 5 THRU LBL 4. MAJOR REPAIR ACCOMPLISHED. DENTS STRAIGHT ENED, HOLES ENLARGED AND HFEC INSPECTED. DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001081600128 20010816 00128 NM 2001 8 16 2001UALA01635 1 20010807 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 322UA 23954 STA 178 BULKHEAD WEB IS CRACKED AT RT UPPER RADAR MOUNT UPPER OUTBOARD SIDE. MAJOR REPAIR ACCOMPLISHED. DAMAGE CUT OUT , DOUBLER MANUFACTURED AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001081600129 20010816 00129 NM 2001 8 16 2001UALA01636 1 20010807 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 322UA 23954 STA 747 FRAME WEB FASTENER HOLE IS OVERSIZED WITH CRACK INDICATION AT STR 9R. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED FRAME WEB ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001090600374 20010906 00374 NM 2001 9 6 2001UALA01638 1 20010804 A 2530 8800010000 OVEN BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FWD GALLEY CONTAMINATED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 612UA 21873 FIRST GALLEY OVEN IS SMOKING. THE MECHANIC CLEANED FOOD FOUND IN THE OVEN. OPS CHECKED OKAY. 2 L 7 2 4F 4 F RT A1NM E3NE 2001102600019 20011026 00019 NM 2001 10 26 2001UALA01639 1 20010803 A 5270 834403 PROXIMITY SENSOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE OVERWING EXIT FAILED A UALA O OTHER N FALSE WARNING CR CRUISE 1 WP 29 673UA 29241 RIGHT FWD (OVERWING EXIT) DOOR LIGHT ILLUMINATED IN FLIGHT WENT OUT ON LANDING. REPLACED DOOR PROXIMITY SENSOR. 2 L 7 2 4F 4 F RT A1NM E24NE 2001090600375 20010906 00375 NM 2001 9 6 2001UALA01640 1 20010806 A 3350 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 198UA 28716 EMERGENCY LIGHT INOP, AFT GALLEY RIGHT WALL. FOUND LOOSE CONNECTION AT SEAT TRACK. REPLACED AISLE EEL STRIP, CARPET SECU RED, EEL CKS GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2001081600130 20010816 00130 2001 8 16 2001UALA01642 4 20010802 A 2565 7A146722 SLIDE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 120UA 29166 DOOR 1 RIGHT HAND SLIDE RAFT FAILED AIR RETENTION TEST DURING FIRST SHOP OVERHAUL. FOUND HOLE IN RAFT INFLATABLE LOWER TUBE ASPIRATOR TUBE. HOLE APPEARS TO BE CAUSED DURING PACKING. HOLE WILL BE REPAIRED PER VENDOR'S CMM 25-66-19. 2 L 7 4 4F 4 F RT A20WE E24NE 2001081600131 20010816 00131 NM 2001 8 16 2001UALA01644 1 20010808 A 5320 ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 322UA 23954 RIGHT CABIN DOOR CUTOUT SUPPORT RIB ANGLE IS CRACKED AT STA 291, 32 INCHES ABOVE CREASE BEAM. REMOVED AND INSTALLED NEW ANGLE. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001081600132 20010816 00132 NM 2001 8 16 2001UALA01646 1 20010808 A 7933 OIL SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEFT OVERTEMP A UALA K NONE M J OVER TEMP WARNING INDICATION DE DESCENT 1 WP 29 578UA 26694 ON DESCENT WITH POWER AT IDLE, LEFT OIL TEMPERATURE REDLINED TILL LANDING. 2 L 7 2 4F 4 F RT A2NM E17NE 2001081600133 20010816 00133 NM 2001 8 16 2001UALA01648 1 20010808 A 5310 STRUCTURE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 434 STR 37R-38R CORRODED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082200066 20010822 00066 NM 2001 8 22 2001UALA01649 1 20010808 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 1307-1310 STR 37R SPLICE CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082200068 20010822 00068 NM 2001 8 22 2001UALA01651 1 20010808 A 5347 SEAT TRACK BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 1307-1310 STR 37R SPLICE CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SEAT TRACK. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082200069 20010822 00069 NM 2001 8 22 2001UALA01652 1 20010808 A 5320 STRINGER CLIP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 1307-1310 STR 37R SPLICE CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STR CLIP REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082200070 20010822 00070 NM 2001 8 22 2001UALA01653 1 20010808 A 5347 SEAT TRACK BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 808 - 860 RBL 55 SEAT TRACK CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SEAT TRACK. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082200071 20010822 00071 NM 2001 8 22 2001UALA01654 1 20010808 A 5347 SEAT TRACK BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 347 RBL 50 SEAT TRACK CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SEAT TRACK REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082200072 20010822 00072 NM 2001 8 22 2001UALA01655 1 20010808 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 1300 STR 37R CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STR REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082200073 20010822 00073 NM 2001 8 22 2001UALA01656 1 20010808 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 1300 STR 37R CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STR REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082200074 20010822 00074 NM 2001 8 22 2001UALA01657 1 20010808 A 5320 SPLICE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 1461-1480 STR 35L SPLICE CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STR SPLICE REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082200075 20010822 00075 NM 2001 8 22 2001UALA01658 1 20010808 A 5320 SPLICE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 1307-1310 STR 37R SPLICE CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW STRINGER SPLICE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001081600135 20010816 00135 NM 2001 8 16 2001UALA01659 1 20010808 A 5270 WARNING SYSTEM AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE COCKPIT ACTIVATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 841UA 1545 FORWARD CABIN DOOR PRESSURE FAULT DISPLAYED ON UPPER ELECTRONIC CENTRALIZED AIRCRAFT MONITORING SCREEN. 2 L 7 2 4F 4 F RT A28NM E40NE 2001081600136 20010816 00136 NE 2001 8 16 RAIA00108016 2 20010810 A 7200 TPE33114GR ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE LEFT ENGINE POWER LOSS A RAIA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CE 03 554HK 11436 41067 75090 5360-BWI-LEFT ENGINE DID NOT ACHIEVE TARGET TORQUE DURING TAKEOFF, CREW ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLA CED THE LEFT ENGINE. 2 L 7 2 4T 4 T RT A41NM E18NE 2001082900053 20010829 00053 NM 2001 8 29 2001UALA01660 1 20010810 A 2440 WIRE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EXTERNAL POWER SHORTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 674UA 29242 NR 4 GAUGE COPPER WIRE DAMAGED DUE TO ELECTRICAL SHORT WITH E&E DOOR CONTACT. NR 4 GAUGE COPPER WIRE IS JUST TO THE RIG HT OF E&E DOOR OPENING TOWARDS THE FWD SIDE. APU POWER WIRE ETOPS CRITICAL SYSTEM. SPLICED IN FOOT LONG SECTION OF 4 GA UGE WIRE INTO APU POWER CABLE. SPLICE IS IN BUNDLE JUST TO THE RIGHT OF THE E&E DOOR, UNDER DOOR WHEN OPENED. OPS CHEC K OK ON APU AND EXTERNAL POWER. REPLACED SPLICE BY E&E DOOR FOR WIRE W230-14 AND RAN NEW WIRE TO K114 EXTERNAL POWER CO NTACTOR, RELUGGED. OPERATIONAL TESTS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2001091400101 20010914 00101 EU 2001 9 14 2001UALA01661 1 20010809 A 2730 31075440 SERVO AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ELEVATOR DEFECTIVE A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 WP 29 457UA 1146 ELEVATOR AILERON COMPUTER WARNING FAULT. A/C HAD HISTORY OF ELAC 1 PITCH FAULT AND ELAC 2 -RELATED PROBLEMS. IT WAS DET ERMINED THAT THE LEFT GREEN ELEVATOR SERVO CONTROL 34CE1 NEEDED TO BE REPLACED. OPS TEST WAS ACCOMPLISHED. 2 L 7 2 4F 4 F RT A28NM E40NE 2001081600137 20010816 00137 NM 2001 8 16 2001UALA01662 1 20010809 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 LEFT FUSELAGE SKIN DENTED STA 618 STR 16L. 2 L 7 2 4F 4 F RT A2NM E17NE 2001081600138 20010816 00138 NM 2001 8 16 2001UALA01664 1 20010809 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST UK UNKNOWN 1 WP 29 122UA 29168 EMERGENCY CEILING LIGHT INOP AT 3 LEFT MAIN ENTRY DOOR. RELAMPED, OP CHECKED GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2001081600139 20010816 00139 NM 2001 8 16 2001UALA01665 1 20010808 A 3350 POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 172UA 24363 EMERGENCY LIGHTS INOP, 55H THROUGH 61H EELS. REPLACED POWER SUPPLY, OPS CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2001081600140 20010816 00140 NM 2001 8 16 AWXA0002119 1 20010811 A 5310 BAC14902763 FRAME BOEING 757 7572S7 1384962 NM FS 1400 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 903AW 23323 D: Frame bent on upper flange at end of previous repair FS 1400 LBL 40 Aft pit.C: Found to be cracked, removed damaged a rea of flange fabricated repair parts and installed per 757 SRM 51-40-02 Pgs 3-4 2 L 7 2 4F RT A2NM 2001081600141 20010816 00141 NM 2001 8 16 2001UIA004 1 20010612 A 2710 CONTROL CABLE DHAV DHC8 DHC8201 2809001 NM AILERON WORN Z K NONE O OTHER IN INSP/MAINT 1 TW 00 17201 522 ON JUN 12 2001, PERFORMED FLIGHT CONTROL CABLE INSPECTION DURING C 01 CHECK. FOUND THE BOTH SIDE AILERON CONTROL, LOCAT ION AT WING STA YW189.970, WAS WORN. REPLACED WORN CABLE PER AMM 27-12-36 AND OPERATIONAL CHECK CONDITION NORMAL. 2 H 7 2 4T RT A13NM 2001081600142 20010816 00142 NM 2001 8 16 DHL2001726004 1 20010815 A 3350 1000679 LIGHT BOEING 727 727228 NM A DHLA O OTHER O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 1) ON SERVICE CHECK FOUND L-1 DOOR EMERGENCY EXIT LIGHT DIM.2) REMOVED AND REPLACED L-1 DOOR EXIT LIGHT ASSY. OPS CK N ORMAL IAW M/M 33-50-111STATUS: CLOSED 2 L 7 3 4F A3WE 2001081600143 20010816 00143 NM 2001 8 16 2001UIA005 1 20010719 A 3040 CONTROLLER DHAV DHC8 DHC8301 NM COCKPIT MALFUNCTIONED Z A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 TW 00 15219 381 AIR TURNBACK DUE TO LT PILOT'S WINDSHIELD HEATER WITH SMOKE ON JUL 19 2001, BEING CHECK, TERMINAL LUG BURN OUT AND WINDS HIELD TEMPERATURE CONTROLLER FUNCTIONED IMPROPERLY. REPLACED WINDSHIELD TEMPERATURE CONTROLLER AND TERMINAL AND OPERATI ONAL CHECK NORMAL PER AMM30-41-00. 2 H 7 2 4T RT A13NM 2001081600144 20010816 00144 NM 2001 8 16 2001UIA006 1 20010730 A 2910 DSC252A40272 HYDRAULIC LINE DHAV DHC8 DHC8301 NM NR 3 BRAKE BROKEN Z O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 TW 00 15225 405 DURING AFTER LANDING TAXI PHASE, HYD SYS FAIL. (QUANTITY CHECK L/H:1.8QT, R/H:0 QT), A/C STOP AT RUNWAY. INSPECTION FO UND NR 3 BRAKE HYD HOSE BROKEN. REPLACED NEW NR 3 BRAKE HOSE PER AMM 32-42-00 AND REPLENISHED HYD LIQUID OPERATIONAL NO RMAL. 2 H 7 2 4T RT A13NM 2001081600145 20010816 00145 NE 2001 8 16 A6WA200100041 2 20010628 A 7200 ALF502 ENGINE BAC 146 146200A 1500266 EU LYC ALF502 ALF502R 41580 NE NR 3 FAILED A A6WA C ABORTED TAKEOFF Y ENGINE STOPPAGE TO TAKEOFF 1 GL 31 156TR 19863 2740 E2156 LF05446A DURING TAKEOFF FLIGHT CREW HEARD LOUD POP, NR 3 ENGINE FAILED AT APPROX 70 KTS. ABORTED TAKEOFF C/W CHECKLIST AND RETUR NED TO GATE, NORMAL BREAKING APPLIED. MAINTENANCE REMOVED AND REPLACED NR 3 ENGINE. 2 H 7 4 4F 4 F A49EU E6NE 2001081600146 20010816 00146 EA 2001 8 16 HNAA0100048 1 20010814 A 3350 82410162007 CONTROL BOX DHAV DHC8 DHC8311 1386006 EA INOPERATIVE A HNAA K NONE N FALSE WARNING CR CRUISE 1 EA 07 326EN 234 EMERGENCY LIGHTS ILLUMINATED IN FLIGHT. REPLACED EMERGENCY LIGHTS CONTROL BOX. 2 H 7 2 4T RT A13NM 2001081600147 20010816 00147 NM 2001 8 16 A6WA200100043 1 20010619 A 3234 7178011 CONTROL HANDLE DORNER DO32 DO328100 2996000 NM COCKPIT DEFECTIVE A A6WA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 31 328PH 1 1 3006 LANDING GEAR WILL NOT RETRACT WITH HANDLE IN UP POSITION, BOTH UP AND DOWN LIGHTS ON. MAINTENANCE REMOVED AND REPLACED GEAR SELECTOR HANDLE ASSY, OPS CHECK AND GEAR SWINGS GOOD. 2 H 7 2 4T RT A45NM 2001081600148 20010816 00148 NM 2001 8 16 A6WA200100044 1 20010713 A 2121 011291500 FAN DORNER DO32 DO328100 2996000 NM E/E BAY FAULTY A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 332PH 6974 6974 3010 STRONG BURNING ODOR IN COCKPIT AND CABIN. MAINTENANCE FOUND AVIONICS FAN PREVIOUSLY MEL EMITTING STRONG BURNING ODOR. REMOVED AND REPLACED HX FAN. 2 H 7 2 4T RT A45NM 2001081600149 20010816 00149 EU 2001 8 16 A6WA200100046 1 20010727 A 2932 506521 TRANSMITTER BAC 146 146200A 1500266 EU HYDRAULIC SYS FAILED A A6WA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 31 291UE 20830 698 E2084 LOSS OF HYDRAULIC QUANTITY YELLOW SYSTEM. MAINTENANCE REMOVED AND REPLACED YELLOW SYSTEM HYDRAULIC PRESSURE TRANSMITTER . 2 H 7 4 4F A49EU 2001081600150 20010816 00150 WP 2001 8 16 ABXA010418 1 20010726 A 3350 5708458503 BATTERY PACK DOUG DC8 DC863 302198A WP CABIN DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 821AX 423 46116 DURING SERVICE CHECK, FOUND CIRCUIT BREAKER FOR EMERGENCY LIGHT BATTERY CHARGER TRIPPED. WOULD NOT RESET. REPLACED DEF ECTIVE EMERGENCY LIGHT BATTERY PACK ASSEMBLY. OPS CHECKED GOOD IAW DC-8 MM 33-50-01-2. 2 L 7 4 4F 4A25 2001081600151 20010816 00151 NE 2001 8 16 ABXA010419 2 20010730 A 7200 ENGINE BOEING 767 767200 1385120 NM GE CF6 CF680A 30025 NE RIGHT VIBRATION A ABXA K NONE E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 GL 23 785AX 23018 580153 DURING CLIMB, RIGHT ENGINE VIBRATION 2.0 TO 2.2, SOME VIBRATION FELT. DURING ALL OTHER PHASES OF FLIGHT, NO VIBRATION F ELT. OPENED COWLING AND CHECKED FOR LOOSE DUCTS, ETC. NO DEFECTS. PERFORMED BITE OF AVM AND EEC, NO DEFECTS NOTED AND NO MAINTENANCE MESSAGES. SYSTEM CHECKED GOOD IAW B767 AMM 77-37-00-5. 2 L 7 2 4F 4 F RT A1NM E13NE 2001081600152 20010816 00152 WP 2001 8 16 ABXA010420 1 20010801 A 3260 PROXIMITY SWITCH DOUG DC8 DC863 302198A WP RT MLG DOOR MALFUNCTIONED A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 825AX 46115 AFTER GEAR RETRACTION RECEIVED RED GEAR UNSAFE LIGHT ILLUMINATION WITH UNSAFE LIGHT ILLUMINATED WITH GEAR UP. RAN ABNOR MAL PROCEDURES AND RECEIVED RIGHT MAIN LANDING GEAR DOOR NOT LATCHED LIGHT MOMENTARILY THEN RIGHT MAIN LANDING GEAR DOOR LIGHT WENT OUT ACCOMPANIED BY RED GEAR UNSAFE LIGHT GOING OUT. THEN DURING DESCENT, RECEIVED ABOVE INDICATION AGAIN. COMPLIED WITH ADJ/TEST OF MAIN GEAR DOOR CLOSED PROXIMITY SWITCH. FOUND RIGHT GEAR DOOR PROXIMITY SWITCH TO BE MALFUNCT IONING. REPLACED GEAR DOOR CLOSED PROXIMITY SWITCH IAW DC-8 MM 32-60-00-2. COMPLIED WITH ADJ/TEST OF MAIN GEAR DOOR CL OSED PROXIMITY SWITCH AGAIN. SYSTEM OPS CHECKED GOOD. NO OTHER DEFECTS NOTED. 2 L 7 4 4F 4A25 2001081600153 20010816 00153 WP 2001 8 16 ABXA010421 1 20010731 A 3350 GROUND WIRE DOUG DC8 DC863F 302198F WP CABIN DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 EMERGENCY EXIT LIGHTS WOULD NOT DISARM. REPAIRED GROUND WIRE (L622C22N) AS REQUIRED. WIRE SHORTED TO 115 AC SIDE OF TE RMINAL OF LIGHT ASSEMBLY CAUSING OVERHEATED WIRE. OPS CHECKED GOOD IAW DC-8 MM 33-50-01. 2 L 7 4 4F 4A25 2001081600154 20010816 00154 WP 2001 8 16 ABXA010422 1 20010731 A 2432 2634006106 BATTERY DOUG DC9 DC933F 302207A WP E/E BAY OVERHEATED A ABXA K NONE B M SMOKE/FUMES/ODORS/SPARKS OVER TEMP IN INSP/MAINT 1 GL 23 935AX 2291 47413 AIRCRAFT BATTERIES WERE OVERHEATED. REPLACED MAIN AIRCRAFT BATTERIES, BATTERY CHARGER, AND BATTERY TEMP. SENSOR. NOTE: CREW REPORTED SMOKE FROM THE E & E COMPARTMENT. CALLED CFR AND EVACUATED THE AIRCRAFT. 2 L 7 2 4F A6WE 2001081600155 20010816 00155 WP 2001 8 16 ABXA010423 1 20010802 A 2150 ACM DOUG DC9 DC931 3022065 WP A/C BAY MALFUNCTIONED A ABXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 23 949AX 47325 TOP OF DESCENT SAW AND SMELLED ELECTRIC SMOKE IN COCKPIT. SMOKE CLEARED THEN RECURRED. REQUESTED PRIORITY LANDING. LA NDING NORMAL. NO ABNORMAL ELECTRICAL INDICATIONS. CHECKED ELECTRICAL SYSTEM FOR BURNING, NOTHING FOUND. RAN ENGINES A ND APU PRESSURE A/C FAINT SMELL OF SMOKE NOTED. NOTICED LEFT PACK OUTPUT VERY LOW BUT PRESSURE NORMAL. FOUND LEFT ACM MOTOR OIL LOW, CHECKED WATER SEPARATOR. FOUND EVIDENCE OF OIL IN SOCK AND SOCK SMELLED BURNED. REPLACED SOCK. REPLACE D LEFT COOLING TURBINE. OPS CHECKED GOOD IAW DC-9 MM 21-51-01-2-0002. 2 L 7 2 4F A6WE 2001081600156 20010816 00156 WP 2001 8 16 ABXA010425 1 20010808 A 3350 5708458503 BATTERY PACK DOUG DC8 DC863F 302198F WP CABIN SHORTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AX 46126 EMERGENCY BATTERY PACK WAS SHORTED INTERNALLY. REPLACED EMERGENCY BATTERY PACK. OPS CHECKED GOOD IAW DC-8 MM. 2 L 7 4 4F 4A25 2001081600157 20010816 00157 WP 2001 8 16 ABXA010433 1 20010725 A 5320 99100787 WEB DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 UPPER CARGO, SUB FLOOR WAS CRACKED AROUND FLOOR SUPPORT AT FS 190 AND RIGHT BUTT LINE 50. REPAIRED SUB FLOOR IAW DC-9 S RM 53-01, FIGURE 2, SHEET 3. 2 L 7 2 4F A6WE 2001081600158 20010816 00158 WP 2001 8 16 ABXA010435 1 20010813 A 2916 O-RING DOUG DC8 DC863 302198A WP HYD RESERVOIR LEAKING A ABXA K NONE K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 23 818AX 46075 GENERAL HYDRAULIC SYSTEM QUANTITY DECREASED FROM FULL TO JUST ABOVE STAND PIPE DURING INITIAL CLIMB. REPACKED O-RING AT RESTRICTOR VALVE GOING TO THE ASPIRATOR ON THE MAIN HYDRAULIC RESERVOIR. LEAK CHECKED GOOD. SERVICED HYDRAULIC SYSTEM . 2 L 7 4 4F 4A25 2001081600159 20010816 00159 WP 2001 8 16 ABXA010440 1 20010731 A 5320 491627041 FITTING DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 990AX 47493 FRAME TO HAT CHANNEL FITTING OUTBOARD VERTICAL LEG CRACKED AT STATION 600, LONGERON 29 RIGHT. REPLACED FITTING IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2001081600160 20010816 00160 WP 2001 8 16 ABXA010443 1 20010810 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 947AX 880 47004 EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE EMERGENCY LIGHT BATTERY PACK POWER SUPPLY IAW DC-9 MM. OPS CHECKED GOO D. 2 L 7 2 4F A6WE 2001081600161 20010816 00161 WP 2001 8 16 ABXA010444 1 20010810 A 3260 TARGET DOUG DC9 DC933F 302207A WP RT MLG DOOR LOOSE A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 931AX 47384 RIGHT GEAR UNSAFE LIGHT STAYED ON WITH GEAR HANDLE IN THE UP POSITION. RECYCLED GEAR AND COMPLIED WITH ABX ABNORMAL PRO CEDURES. FOUND THE MAIN LANDING GEAR POSITION WARNING SWITCH CAUGHT ON THE RIGHT GEAR DOOR LATCH STRIKER WHICH WAS LOOS E. INSTALLED SHIMMY ON STRIKER. TESTED RIGHT MAIN LANDING GEAR POSITION AND WARNING SWITCH IAW DC-9 MM 32-60-01-2-0101 . OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2001081600162 20010816 00162 NM 2001 8 16 AWXA0002115 1 20010812 A 5310 146N3511 SKIN BOEING 757 7572S7 1384962 NM STA 1510 DENTED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 903AW 23323 D: Lwr fuselage at STA 1510 STR 27L has dent 1" L x .5w x .095DC: removed intercostal cut out damage NDT no cracks noted INSTLD repair parts -fillers doublers IAW SRM 53-00-01 pg 206 and NDT SRM 51-00-19 and reinstalled intercostal SRM 51-4 0-02 2 L 7 2 4F RT A2NM 2001081600166 20010816 00166 NM 2001 8 16 AT0100218 1 20010723 A 3350 K2081740009G FAIRING BOEING 717 717200 1383700 NM CABIN BROKEN A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 948AT 55011 EMERGENCY LIGHT FAIRING IN SEAT ARM REST BROKEN. REPLACED BROKEN LIGHT FAIRINGS IAW AVIO CMN 25-24. 2 L 7 2 4F TR A6WE 2001081600167 20010816 00167 NM 2001 8 16 AT0100219 1 20010801 A 3350 K2081740009G PLATE BOEING 717 717200 1383700 NM CABIN BROKEN A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 954AT 55016 FOUND EMERGENCY PATH LIGHT BACKING PLATE BROKEN AT ROW 21. REPLACED BACKING PLATE. 2 L 7 2 4F TR A6WE 2001081600168 20010816 00168 EU 2001 8 16 AWXA0001968 1 20010714 A 2911 D9347025400600 B-NUT AIRBUS 320 A320231 3930325 EU HYD ACCUMULATOR LOOSE A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 28 621AW 053 PHX - AIR TURNBACK - FLT 682 - AFTER TAKEOFF FROM PHX DURING CLIMB EN ROUTE TO EWR THE YELLOW HYDRAULIC SYSTEM QUANTITY STARTED TO DECREASE AND BECAME DEPLETED. THE AIRCRAFT WAS RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. MAINTENANCE FOUND SIGNS OF LEAKAGE AT THE YELLOW SYSTEM ACCUMULATOR. THE AREA WAS CLEANED, THE SYSTEM SERVICED AND LEAK CHECK PERFO RMED. THE ELBOW ASSY B-NUT ON TOP OF THE ACCUMULATOR WAS FOUND TO BE LEAKING. THE B-NUT WAS CHECKED AND FOUND TO BE LO OSE, THE B-NUT WAS TIGHTENED AND A LEAK CHECK PERFORMED, NO FURTHER LEAKAGE WAS NOTED AND THE AIRCRAFT WAS RETURNED TO S ERVICE. 2 L 7 2 4F RT A28NM 2001081600169 20010816 00169 NM 2001 8 16 AWXA0001973 1 20010508 A 5312 6546568524 BULKHEAD BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 AFT PRESSURE BULKHEAD LOWER 6 O`CLOCK POSITION CORROSION ON BULKHEAD WEB RBL 3 TO LBL 3. REPAIRED PER ER 03-5383-01141- DD2 & ER 03-5383-01141-DD4. 2 L 7 2 4F RT A16WE 2001081600170 20010816 00170 WP 2001 8 16 ZW0A0106901 1 20010815 A 2780 3916322613 WIRE DOUG DC9 DC982 3022082 WP FLAP BUSS BROKEN A ZW0A D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 CE 13 902TW 49153 ON ARRIVAL AT THE GATE THE LEADING EDGE SLATS WOULD NOT RETRACT. REPLACED BROKEN FLAP BUS WIRE, RUN 208B. REFERENCE IPC 27-30-00 FIGURE 2B ITEM 32. CHECK-C 2-5-01 STL. --CLOSED-- 2 L 7 2 4F A6WE 2001081600182 20010816 00182 NM 2001 8 16 2001F00190 1 20010501 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CANNING A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 29SW 21340 THE FUSELAGE SKIN WAS FOUND WITH OIL CANNING. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-30-3 FIGURE 3. (M) 2 L 7 2 4F A16WE 2001081600183 20010816 00183 NM 2001 8 16 2001F00191 1 20010501 A 5313 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 29SW 21340 FOUND STRINGER CRACKED AT BS 312, STRINGER 4 RIGHT. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-3 FIGURE 3. (M) 2 L 7 2 4F A16WE 2001081600184 20010816 00184 NM 2001 8 16 2001F00192 1 20010501 A 5311 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 29SW 21340 FOUND CRACK IN FRAME STATION BS 344 STRINGER 6 LEFT. THE DAMAGED AREA WAS REPAIRED IAW SRM 51-40-3 FIGURE 1. (M) 2 L 7 2 4F A16WE 2001081600185 20010816 00185 NM 2001 8 16 2001F00193 1 20010501 A 5320 ANGLE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 29SW 21340 FOUND LOWER FUSELAGE, BS 727 BULKHEAD, BLO WL 208 ANGLE CRACKED. DAMAGED AREA WAS REPAIRED PER SB 737-53-1053. (M) 2 L 7 2 4F A16WE 2001081600186 20010816 00186 NM 2001 8 16 2001F00194 1 20010501 A 5313 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 29SW 21340 AT STRINGER 27L FROM BS 1006 TO BS 1016, CORROSION WAS FOUND. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-3 FIGURE 1. (M) 2 L 7 2 4F A16WE 2001081600187 20010816 00187 NM 2001 8 16 2001F00195 1 20010501 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 29SW 21340 THE FLOORBEAM WAS FOUND CORRODED AT BS 328, RBL 32. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-9 FIGURE 6. (M) 2 L 7 2 4F A16WE 2001081600188 20010816 00188 NM 2001 8 16 2001F00196 1 20010501 A 5313 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 29SW 21340 FOUND STRINGER AT STATION BS 727B STRINGER 9 LEFT HAS CRACK. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-3 FIG 3. (M) 2 L 7 2 4F A16WE 2001081600189 20010816 00189 NM 2001 8 16 USAA010597 1 20010531 A 5300 FRAME BOEING 757 757225 1384959 NM BS 1701 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 51539 22192 CLT - FOUND FRAME CORRODED 2 INCHES BY 12 INCH AREA, BS 1701, BETWEEN STRINGERS 27L AND 28L. DAMAGE REMOVED, FABRICATED AND INSTALLED REPAIR DOUBLER PER EA 67935. (M) 2 L 7 2 4F RT A2NM 2001081600190 20010816 00190 NM 2001 8 16 USAA010581 1 20010531 A 5300 WEB BOEING 757 757225 1384959 NM BS 660 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 51539 22192 CLT - FOUND WEB CRACKED .5 INCH, BS 660, 14L. REMOVED DAMAGED WEB, FABRICATED AND INSTALLED NEW WEB PER BAC DRAWING 143 N8339 AND SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 2001081600191 20010816 00191 NM 2001 8 16 USAA010580 1 20010531 A 5300 STRINGER BOEING 757 757225 1384959 NM BS 640 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 51539 22192 CLT - FOUND STRINGER CRACKED 2 INCHES, BS 640, 16L. DAMAGE AREA REMOVED, INSTALLED STRINGER SPLICE AND DOUBLER PER SRM 53-00-03. (M) 2 L 7 2 4F RT A2NM 2001081600192 20010816 00192 NM 2001 8 16 USAA010516 1 20010508 A 5300 STRAP BOEING 757 757225 1384959 NM BS 365-377 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 51539 22192 CLT - FOUND STABILIZING STRAP WITH PREVIOUSLY INSTALLED DOUBLER, 6 SQUARE INCH AREA, BS 365 TO 377, LBL 25. REMOVED AND REPLACED DOUBLER PER 53-10-51 FIG 202. (M) 2 L 7 2 4F RT A2NM 2001081600193 20010816 00193 NM 2001 8 16 USAA010606 1 20010605 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM BS CORRODED A K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 51539 22192 CLT - FOUND FLOORBEAM CORRODED APPROXIMATELY 6 SQUARE INCH AREA NUT PLATE HOLES, BS 345, RBL 12 TO RBL 52. REMOVED DAMA GED AREA, INSTALLED NEW T-CAP PER TYPICAL REPAIR 53-15-01. (M) 2 L 7 2 4F RT A2NM 2001081600194 20010816 00194 NM 2001 8 16 USAASB01213 1 20010721 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM MID CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 523AU 23858 ALB - MAINTENANCE FOUND THE EMERGENCY LIGHTS FOR THE RIGHT OVERWING EXIT SIGN, BULLNOSE LIHTS AT ROWS 5 AND 8 LEFT SIDE, CEILING EXIT SIGN AT ROW 7, RIGHT CEILING EXIT SIGN AT ROW 10 AND THE EXIT SIGN OVER FORWARD SERVICE DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK LOCATED IN THE CEILING ABOVE EXIT ROW 10, RIGHT SIDE. OPERATIONAL CH ECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001081600195 20010816 00195 WP 2001 8 16 AALA20011419 1 20010711 A 2100 CLAMP DOUG DC9 DC982 3022082 WP TAIL COMPT LOOSE A AALA A UNSCHED LANDING J O WARNING INDICATION OTHER CL CLIMB 1 SW 21 584AA 53247 DFW - FLT 2441 - EN ROUTE DFW-LAX, TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. PERFORMED EMERGENCY CHECKLIST RETURNIN G DFW WITHOUT INCIDENT. FOUND ACM DUCT DETACHED FROM BOOT. RESECURED LOOSE CLAMP. SYSTEM GROUND CHECKED NORMAL OPERAT ION. (M) 2 L 7 2 4F A6WE 2001081600196 20010816 00196 NM 2001 8 16 AALA20011412 1 20010705 A 5300 STRINGER BOEING 727 727227 1384078 NM BS 440 A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 731AA 20738 TUL - FOUND RIVETS HEADS POPPED AND SKIN BULGED AT STRINGER 21R JUST AFT OF STRINGER 440. REMOVED CORRODED SECTION OF S TRINGER 21R AND INSTALLED STRINGER SPLICE PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 2001081600197 20010816 00197 NM 2001 8 16 2001F00197 1 20010501 A 5313 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 29SW 21340 FOUND STRINGER CRACKED AT BS 440, STRINGER 4 RIGHT. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-3 FIGURE 3. (M) 2 L 7 2 4F A16WE 2001081700001 20010817 00001 NM 2001 8 17 01FDEA00699 1 20010812 A 5310 FRAME BOEING 727 727247 138408F NM DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 N 885 DENTS IN FRAME FLANGE AT BS 600 BETWEEN STR 23L AND 25L. ** S/D ** COMING 2 L 7 3 4F A3WE 2001081700002 20010817 00002 NM 2001 8 17 01FDEA00696 1 20010813 A 5310 FRAME BOEING 727 727247 138408F NM UPPER FLANGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 N 669 UPR FLANGE OF BS 1130 FRAME HAS 2 EA OPEN HOLES WITH CORROSION UNDER L/H FLOOR TO SIDEWALL SUPPORT C53-111-01(3). ** S/D ** COMING 2 L 7 3 4F A3WE 2001081700003 20010817 00003 NM 2001 8 17 01FDEA00697 1 20010813 A 5310 WEB BOEING 727 727247 138408F NM RH STUB BEAM CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 N 795 R/H STUB BEAM FWD AND AFT WEB CRACKED BS 848, RBL 60, WL 202. ** S/D ** COMING 2 L 7 3 4F A3WE 2001081700004 20010817 00004 NM 2001 8 17 01FDEA00698 1 20010811 A 5311 FRAME BOEING 727 727247 138408F NM BS 1110 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 HOLE & CORROSION IN UPR FLANGE OF FRAME AT BS 1110. R&R FRAME PER SRM 51-40-3. 2 L 7 3 4F A3WE 2001081700005 20010817 00005 NM 2001 8 17 01FDEA00704 1 20010814 A 5310 SHEAR TIE BOEING 727 727247 138408F NM FRAME CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 N 701 CORROSION ON FRAME BS 580, RBL 10, WL 148. ** S/D ** R&R SHEAR TIE PER SRM 53-10-4 FIG 14. 2 L 7 3 4F A3WE 2001081700006 20010817 00006 WP 2001 8 17 AT0100220 1 20010713 A 5280 DOOR DOUG DC9 DC932 3022066 WP NOSE GEAR OPEN A ZZDA K NONE O OTHER TO TAKEOFF 1 SO 15 836AT 47397 LOUD RUMBLE AFTER TAKE-OFF. CORRECTIVE ACTION: INSPECTED NOSE LANDING GEAR DOOR LINKAGE, HINGES AND NO DEFECTES NOTED. CLOSED NOSE LANDING GEAR DOOR AND CONFIRMED LATCH CHECK. IAW DC9 MM 32-00, 52-00 2 L 7 2 4F A6WE 2001081700007 20010817 00007 WP 2001 8 17 AT0100221 1 20010813 A 7931 SEAL DOUG DC9 DC932 3022066 WP HYD PUMP LEAKING A ZZDA E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 SO 15 818AT 47320 AT LEVEL OFF "OIL PRESSURE LOW" LIGHT FLICKERED. FOLLOWED BY LOW OIL PRESSURE INDICATION OF APPROXIMATELY 30PSI. OIL Q UANTITY DROPPED TO 0 (ZERO). AT ENGINE IDLE OIL QUANTITY RETURNED TO 2 QUARTS. PRECAUTIONARY LANDING, SINGEL ENGINE OP ERATION. CORRECTIVE ACTION: REMOVED AND REPLACED GARLOCK SEAL FOR HYDRAULIC PUMP AND REPLACED STRAINER AND O-RINGS. IAW DC9 MM 79-31, 72-61 2 L 7 2 4F A6WE 2001081700008 20010817 00008 WP 2001 8 17 CALA0100761 1 20010815 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 256-313 PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND CABIN FLOOR PANEL PUNCTURED AT FS 256-313. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IA W SRM 51-30-1 AND ECRA 5320-01265. 2 L 7 2 4F A6WE 2001081700009 20010817 00009 WP 2001 8 17 CALA0100763 1 20010816 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FS 1308-1322 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND INTERCOSTAL CORRODED AT FS 1308-1322, LONGERONS 27L-28L. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOS TAL WAS INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 2001081700010 20010817 00010 EA 2001 8 17 2001F00200 2 20010707 A 7320 3035279 LINE DHAV DHC7 DHC7102 2802708 EA PWA PT6 PT6A50 52043 EA NR 4 ENGINE CRACKED A GUUA O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 19 706GA 53 FLT 1253 - HAV - AFTER TAKEOFF, AT 4,800 FEET, NR 4 ENGINE EXPERIENCED A POWER LOSS. PERFORMED ENGINE FAILURE IN FLIGHT CHECK LIST. REMOVED AND REPLACED NR 4 ENGINE P3 LINE. RAN ENGINE. OPERATIONAL CHECK NORMAL. (M) 2 H 7 4 4T 4 T A20EA E4EA 2001081700011 20010817 00011 NM 2001 8 17 2001F00202 1 20010703 A 5730 65B145967RT PANEL BOEING 747 747230B 1384889 NM LT WING CRACKED A Q2SA K NONE O OTHER IN INSP/MAINT 1 GL 23 744SA 22363 DURING PREFLIGHT, FOUND LEFT WING UPPER PANEL ASSEMBLY ABOVE NR 2 ENGINE PYLON AND ABOVE NR 1 SLAT CRACKED APPROXIMATELY 48 INCHES LONG FROM FORWARD TO AFT OF PANEL. REMOVED, REPAIRED AND REINSTALLED PANEL ASSEMBLY. REPAIRED IAW SRM 51-40 -09 AND 51-40-12. (M) 2 L 7 4 4F A20WE 2001083001005 20010830 01005 CE 2001 8 30 GLBA2001164 1 20010719 A 2130 1013800213 VALVE BEECH 1900 1900D 1154162 CE CABIN PRESSURE FAILED A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 254GL UE254 WOULD NOT PRESSURIZE CABIN ON CLIMB OUT, REPLACED SOLENOID VALVE OPS CHECKED SYSTEM SATISFACTORY 2 L 7 2 4T RT A24CE 2001081700012 20010817 00012 CE 2001 8 17 GLBA2001170 1 20010723 A 2800 MS2466021A SWITCH BEECH 1900 1900D 1154162 CE INOPERATIVE A GLBA D RETURN TO BLOCK O OTHER CR CRUISE 1 CE 01 255GL UE255 FUEL TRANSFERING WITH SWITCH IN THE OFF POSITION, REPLACED TRANSFER SWITCH OPS CHECKED SYSTEM SATISFACTORY 2 L 7 2 4T RT A24CE 2001081700013 20010817 00013 NM 2001 8 17 AWXA0002122 1 20010714 A 5313 654541046 DOUBLER BOEING 737 737277 1384570 NM BS 670 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: Doubler on floor beam at BS 670 LBL 24 crackedC: Removed and replaced doubler IAW B737 SRM 51-30-5 Pg 5 2 L 7 2 4F RT A16WE 2001081700014 20010817 00014 NM 2001 8 17 AWXA0002123 1 20010630 A 5311 6545815 FRAME BOEING 737 737277 1384570 NM FWD FUSE CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: During "D" check inspection found upper lobe frame cracked BS 344 Stringer 6LC: Repaired crack on upper lobe frame BS 344, at stringer 6L Iaw B737-200 SRM 53-10-4 2 L 7 2 4F RT A16WE 2001081700015 20010817 00015 NM 2001 8 17 AWXA0002126 1 20010707 A 5310 BAC1505100155 ANGLE BOEING 737 737277 1384570 NM BS 1130 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: R/H torque box aft side duct support angle corroded at screw holes approx BS 1130 on side web of torque boxC: Removed and replaced support angle at R/H torque box B.S. 1130 IAW 737 SRM 51-30-2 Pgs 2,3 & 32 2 L 7 2 4F RT A16WE 2001081700016 20010817 00016 NM 2001 8 17 AWXA0002127 1 20010629 A 5311 654653112 FRAME BOEING 737 737277 1384570 NM BS 460 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: Fus frame @ BS 460 bent and cracked at S 26R to S 28LC: Formed and installed repair parts IAW 737-200 SRM 51-30-2 Pg 2&3 2 L 7 2 4F RT A16WE 2001081700017 20010817 00017 NM 2001 8 17 AWXA0002129 1 20010710 A 5300 6568940111 ANGLE BOEING 737 737277 1384570 NM SECTION 48 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: During "D" check inspection found frame angle aft side 1088 bulkhead, top side of torque box at duct inlet corrodedC: Removed and replaced frame angle aft side 1088 Bulkhead top side or torque box at duct inlet IAW B737 SRM 51-30-2 2 L 7 2 4F RT A16WE 2001081700018 20010817 00018 NM 2001 8 17 AWXA0002131 1 20010702 A 5330 654574953 SKIN BOEING 737 737277 1384570 NM SECTION 43 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: During "D" check inspection found belly skin cracked approx BS 520 STR 27 RT at OTBD corner of groud air conditioning service doorC: repaired crack at BS 520 STR 27 RT IAW engineering repair No 15-5331-01193-SS3 2 L 7 2 4F RT A16WE 2001081700019 20010817 00019 NM 2001 8 17 AWXA0002132 1 20010723 A 5312 6546572515 STIFFENER BOEING 737 737277 1384570 NM BS 1088 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: Stiffener on FWD side of BS 1088 Bulkhead corroded at RBL 27 WL 240 to 228C: Removed and replaced stiffener IAW B737 SRM 51-30-2 pg 2&3 2 L 7 2 4F RT A16WE 2001081700020 20010817 00020 NM 2001 8 17 AWXA0002134 1 20010723 A 5310 654540919 STIFFENER BOEING 737 737277 1384570 NM BS 727 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: Pressure web stiffener cracked BS 727 LBL 8 WL 202C: Removed and replaced pressure web stiffener IAw B737 SRM 51-30-2 pg 8 2 L 7 2 4F RT A16WE 2001081700021 20010817 00021 NM 2001 8 17 AWXA0002135 1 20010726 A 5310 BAC1498160 STRINGER BOEING 737 737277 1384570 NM BS 907 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: Corrosion on STR 25R at BS 907 String Splice.C: Removed String & String Splice and attach angles, replaced string and splices and attach parts, fabed splices and string IAW B737 SRM 53-10-3 2 L 7 2 4F RT A16WE 2001081700022 20010817 00022 NM 2001 8 17 AWXA0002136 1 20010726 A 5311 654540919 STIFFENER BOEING 737 737277 1384570 NM BS 727 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: Pressure web stiffener cracked at BS 727, LBL 17, WL 202C: Removed and replaced stiffener IAW B737 SRM 51-30-2 pg 8 2 L 7 2 4F RT A16WE 2001081700023 20010817 00023 NM 2001 8 17 AWXA0002137 1 20010727 A 5311 65548325 STIFFENER BOEING 737 737277 1384570 NM BS 1098 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: Web support beam at R/H APU torque box BS 1098 has exfoliated corrosion on stiffenerC: Repaired web support beam stif fener IAW B737 SRM 51-40-3 Fig 1 pgs 1-6 and BAC DWG 65-54-832 2 L 7 2 4F RT A16WE 2001081700024 20010817 00024 NM 2001 8 17 AWXA0002139 1 20010628 A 5311 654577518 SKIN BOEING 737 737277 1384570 NM SECTION 46 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: L2 door upper hinge fuselage cut out cracked BS 937C: Repaired R-2 Door fuselage skin upper hinge cut out IAW B737 SR M 53-30-3 2 L 7 2 4F RT A16WE 2001081700025 20010817 00025 NM 2001 8 17 AWXA0002140 1 20010628 A 5330 6545778 SKIN BOEING 737 737277 1384570 NM SECTION 46 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: R2 door fuselage skin upper hinge cut out is cracked BS 947.C: Repaired R2 door fuselage skin upper hinge cut out IAW B737 SRM 53-30-3 2 L 7 2 4F RT A16WE 2001081700026 20010817 00026 NM 2001 8 17 AWXA0002141 1 20010628 A 5330 654577660 SKIN BOEING 737 737277 1384570 NM SECTION 46 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: Bulge in fuselage skin exterior approx BS 800 STR 26 RTC: Repaired section of fuselage skin approx BS 800 STR 26 RT I AW AWA ER 15-5361-01205-JS1 2 L 7 2 4F RT A16WE 2001081700027 20010817 00027 NM 2001 8 17 AWXA0002142 1 20010708 A 5311 6546539 FRAME BOEING 737 737277 1384570 NM SECTION 46 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: Frame cracked at lower fastener hole BS 616 between LT STR 17 & 18 2 L 7 2 4F RT A16WE 2001081700028 20010817 00028 NM 2001 8 17 AWXA0002143 1 20010730 A 5312 654541041 WEB BOEING 737 737277 1384570 NM BS 178 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: BS 178 bulkhead web cracked 3 places at WL 189 between RBL .6 and LBL .6C: Repaired BS 178 bulkhead web IAW AWA E.R. 15-5312-01194-SS1 2 L 7 2 4F RT A16WE 2001081700029 20010817 00029 NM 2001 8 17 AWXA0002144 1 20010730 A 5311 65C3453721 CHANNEL BOEING 737 737277 1384570 NM BS 665 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: BS 665 LBL 24 upper chord cracked.C: Stop drilled and repaired BS 665 LBL 24 WL 207 chord crack IAW AWA ER 155702-012 11-JS1 2 L 7 2 4F RT A16WE 2001081700030 20010817 00030 NM 2001 8 17 AWXA0002145 1 20010731 A 5313 BAC1498160 STRINGER BOEING 737 737277 1384570 NM BS 360 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: Bulge in skin with cupped fastener heads approx BS 360 STR 28 LTC: Repaired corrosion on lower tee chord and skin at BS 360 STR 28 LT IAW AWA ER 15-5314-01212-DL1 2 L 7 2 4F RT A16WE 2001081700031 20010817 00031 NM 2001 8 17 AWXA0002148 1 20010803 A 5313 BAC1498159 STRINGER BOEING 737 737277 1384570 NM BS 375 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: 2 SQ IN. corrosion found on stringer 26LT at BS 375C: Repaired stringer 26LT at BS 375 IAW B737 SRM 53-10-3 Fig 1 Pgs 1-10 2 L 7 2 4F RT A16WE 2001081700032 20010817 00032 NM 2001 8 17 AWXA0002149 1 20010803 A 5313 65C3453715 WEB BOEING 737 737277 1384570 NM BS705- 720 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: 5 Cracks inweb below BL 24L Seat track BS 705-720C: Repaired web IAW ER 15-5715-01200-DL4 2 L 7 2 4F RT A16WE 2001081700033 20010817 00033 NM 2001 8 17 AWXA0002151 1 20010803 A 5315 65C345373 BEAM BOEING 737 737277 1384570 NM BS 706-717 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: BS 706-717 BL.07 transverse floor beam cracked 8 EA PlacesC: Repaired beam IAW AWA ER 15-5702-01209-DD2 2 L 7 2 4F RT A16WE 2001081700034 20010817 00034 NM 2001 8 17 AWXA0002152 1 20010803 A 5310 65475951 SPAR BOEING 737 737277 1384570 NM SS-0 REAR SPAR GOUGED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: LH horizontal stabilizer I/B upper attach lug at rear spar has 2 gouges.C: Repaired LH horizontal stabilizer rear spa r upper attach lug IAW AWA ER 15-5510-01204-DD2 2 L 7 2 4F RT A16WE 2001081700035 20010817 00035 NM 2001 8 17 AWXA0002157 1 20010804 A 5312 6546572501 ANGLE BOEING 737 737277 1384570 NM BS 1088 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: Corrosion on torque box outlet support (BS 1088 bulkhead)C: Removed and replaced BS 1088 outlet support angle IAW BAC DWG 65-46572 and B737 SRM 51-10-6 Pg 4-6, 53-10-1 fig 8n Pg 4-5, 51-10-2 pg 7-8, 51-30-5 pg 5 and 51-30-2 pg 32 2 L 7 2 4F RT A16WE 2001081700036 20010817 00036 NM 2001 8 17 AWXA0002159 1 20010814 A 5313 149N712521 INTERCOSTAL BOEING 757 7572S7 1384962 NM FS 879-900 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 903AW 23323 D: Wing to body fairing support at LBL 7 corroded on lower I/B surfaces from FS 879-900C: Removed damaged part, fabricat ed repair part and installed per 757 SRM 51-40-02 pg 1 and drawing 149n7125 2 L 7 2 4F RT A2NM 2001082800144 20010828 00144 NM 2001 8 28 01FDEA00740 1 20010814 A 5311 FRAME BOEING 727 727247 138408F NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 BS 1070 FRAME IS CRUSHED OVER STR 26R. REMOVED AND REPLACED FRAME PER SRM 51-40-3. 2 L 7 3 4F A3WE 2001081700037 20010817 00037 WP 2001 8 17 ZW0A0107001 1 20010815 A 2610 474007 PANEL DOUG DC9 DC982 3022082 WP COCKPIT A ZW0A F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 13 958U 49703 THE MID CARGO COMPARTMENT FIRE DETECTOR LIGHT CAME ON. CREW FIRED BOTH BOTTLES AND MADE AN UNSCHEDULED LANDING AT RIC. THE DETECTION SYSTEM WAS PLACARDED INOPERATIVE PER MEL AND THE AIRCRAFT FERRIED TO STL FOR CORRECTIONS. THE COCKPIT CONT ROL PANEL WAS FOUND SHORTED AND REPLACED. CHECK-C 6-22-01 STL. --CLOSED-- 2 L 7 2 4F A6WE 2001081700038 20010817 00038 EA 2001 8 17 COMA0160597 1 20010816 A 5270 DOOR LATCH CNDAIR CL600 CL6002B19 EA A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 937CA 7146 DURING CRUISE FLIGHT RECEIVED A CABIN DOOR OUTER HANDLE MESSAGE, CREW DECLARED AN EMERGENCY AND DIVERTED TO SDF, AIRCRAF T LANDED SAFELY.PERFORMED RE-RIGGING OF THE CABIN DOOR HANDLE MECHANISM. 2 L 7 2 4F RT A21EA 2001081700039 20010817 00039 EA 2001 8 17 COMA0160598 1 20010816 A 3260 LANDING GEAR CNDAIR CL600 CL6002B19 EA A COMA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 708CA 7235 AFTER TAKE OFF FROM GSP RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN WARNING, CREW DECLARED AN EMERGENCY AND RETURNED TO TH E FIELD, AIRCRAFT LANDED SAFELY.ADJUSTED THE NOSE LANDING GEAR PROXIMITY SENSOR AND SERVICED THE STRUT. 2 L 7 2 4F RT A21EA 2001081700040 20010817 00040 EA 2001 8 17 COMA0160599 1 20010816 A 2613 VALVE CNDAIR CL600 CL6002B19 EA A COMA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SO 01 962CA 7123 DURING CLIMB OUT OF CVG RECEIVED A LEFT JET PIPE OVERHEAT CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND RETURNED TO TH E FIELD, AIRCRAFT LANDED SAFELY.REPOSITIONED AND TIGHTENED CLAMPS FOR THE LEFT 14TH STAGE SHUT FOF VALVE AND CHECK VALVE . 2 L 7 2 4F RT A21EA 2001081700041 20010817 00041 EA 2001 8 17 COMA0160600 1 20010815 A 7930 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 EA A COMA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 821CA 7420 DURING TAKE OFF FROM CVG THE LEFT ENGINE OIL PRESSURE INDICTED ZERO, CREW SELECTED TO ABORT AND RETURN TO THE GATE.RESET CIRCUIT BREAKER 1M1. 2 L 7 2 4F RT A21EA 2001081700042 20010817 00042 EA 2001 8 17 COMA0160601 1 20010816 A 5300 60034017351 ANGLE CNDAIR CL600 CL6002B19 EA FLOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 971CA 11671 7145 FORWARD J ANGLE AT FS 280 BETWEEN LBL9 AND RBL 9 IS CORRODED.REMOVED AND REPLACED FORWARD J ANGLE I/A/W WVAC EO 601R-53- 2640. 2 L 7 2 4F RT A21EA 2001081700046 20010817 00046 EA 2001 8 17 COMA0160602 1 20010816 A 5300 601R31527221 ANGLE CNDAIR CL600 CL6002B19 EA DOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 971CA 11671 7145 PASSENGER DOOR LOWER THRESHOLD CORRODED.REMOVED AND REPLACED THRESHOLD SUPPORT ANGLE I/A/W WVAC EO 601R-53-2643. 2 L 7 2 4F RT A21EA 2001081700054 20010817 00054 NM 2001 8 17 01FDEA00666 1 20010805 A 2750 FLAP BOEING 727 727233 138408A NM WINGS VIBRATION A FDEA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 25 223FE 20935 EXCESSIVE FLT CONTROL VIB. INSP FLAPS AND FAIRING FOR ADJ AND MISSING ROLLERS. FOUND OK PER MM 27-51-001-5 & MM 27-51- 011-5. 2 L 7 3 4F RT A3WE 2001081700055 20010817 00055 NM 2001 8 17 01FDEA00677 1 20010809 A 3234 SOLENOID BOEING 727 7272S2F 1384O81 NM COCKPIT FAILED A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 216FE LANDING GEAR FAILED TO RETRACT ON DEPART. REMOVED AND REPLACED LANDING GEAR LEVER LOCK SOLENOID IN REF 727-200 MM 32-31 -016-4. CHECK GOOD. 2 L 7 3 4F A3WE 2001081700056 20010817 00056 WP 2001 8 17 01FDEA00679 1 20010811 A 3620 LIGHT DOUG DC10 DC1010CF 3023502 WP COCKPIT ILLUMINATED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 061FE 46973 NR 3 MANIFOLD FAIL LIGHT ILLUM. RED TABS ACCOMPLISHED. 2 L 7 3 4F RT A22WE 2001081700062 20010817 00062 NM 2001 8 17 01FDEA00687 1 20010813 A 5310 SHEAR TIE BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSION (C53-111-02, 2) FWD CARGO BAY BS 720D, RBL 16, WL 150 SHEAR TIE. *S/D* REMOVED AND REPLACED SHEAR TIE PER SR M 53-10-4 FIG 15. 2 L 7 3 4F A3WE 2001082800136 20010828 00136 NM 2001 8 28 01FDEA00693 1 20010813 A 5330 SKIN BOEING 727 727247 138408F NM FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 EXTERIOR SKIN CHAFED AT BS 720D+12" STR 19R. REMOVED AND REPLACED REPAIR DOUBLER PER 53-30-3 FIG 4. 2 L 7 3 4F A3WE 2001082800137 20010828 00137 NM 2001 8 28 01FDEA00694 1 20010813 A 5330 SKIN BOEING 727 727247 138408F NM FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 EXTERIOR SKIN CHAFED AT BS 720D+12, STR 19L. REMOVED AND REPLACED REPAIR DOUBLER PER SRM 53-30-3 FIG 4. 2 L 7 3 4F A3WE 2001081700066 20010817 00066 WP 2001 8 17 01FDEA00695 1 20010814 A 5754 ARB158376 CAP DOUG DC10 DC1010F 3022111 WP L/E SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 383FE 46616 LEFT WING SLAT INBOARD END CAP CRACKED IN NUMEROUS PLACES. UPON REMOVAL OF END CAP FOUND 1 OTHER INTERNAL RIB CRACKED. 2 L 7 3 4F A22WE 2001081700068 20010817 00068 NM 2001 8 17 01FDEA00705 1 20010813 A 5313 STRINGER BOEING 727 727247 138408F NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 BS 480, STR 8L DOUBLE HOLES AND DAMAGE. REMOVED AND REPLACED STR PER EA 7-5310-59211 & SRM 53-10-3. 2 L 7 3 4F A3WE 2001081700075 20010817 00075 WP 2001 8 17 01FDEA00718 1 20010814 A 2720 ABH72391 ARM DOUG DC10 DC1010 3022110 WP RUDDER PEDAL CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 391FE 46625 CAPT'S RUDDER PEDAL TORQUE TUBE ARM ASSY CRACKED AT I/B SIDE INPUT ROD ATTACH POINT RT RUDDER PEDAL. *S/D* REMOVED AND REPLACED RT ARM ASSY PER DAC CMM 27-21-02. 2 L 7 3 4F A22WE 2001081700077 20010817 00077 NM 2001 8 17 01FDEA00735 1 20010814 A 5542 SKIN BOEING 727 727247 138408F NM RUDDER TORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 UPPER FWD LT CORNER OF LWR RUDDER HAS SECTION OF OUTER SKIN TORN. REMOVED AND REPLACED RUDDER PER EA 7-5540-58476. 2 L 7 3 4F A3WE 2001081700078 20010817 00078 WP 2001 8 17 01FDEA00736 1 20010816 A 2781 PROXIMITY SENSOR DOUG DC10 DC1030F 3023504 WP L/E SLAT FAULTY A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 309FE 48298 SLAT DISAGREE LIGHT ILLUMINATED. FOLLOW RED TABS. REMOVED AND REPLACED PROX BOX PER IAW MM 32-61-01-2. OPS CHECK GOOD . 2 L 7 3 4F RT A22WE 2001081700079 20010817 00079 NM 2001 8 17 A6WA200100045 1 20010713 A 2120 SMOKE DORNER DO32 DO328100 2996000 NM COCKPIT DETECTED A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 335LS 3035 SMOKE IN COCKPIT. MAINTENANCE RAN LEFT AND RIGHT PACKS IN ALL CONFIGURATIONS. OP CHECK NORMAL, NO EVIDENCE OF SMOKE IN COCKPIT. 2 H 7 2 4T RT A45NM 2001081700080 20010817 00080 NM 2001 8 17 SPAAO1OOO45 1 20010815 A 3350 10617837 HOUSING BOEING 737 7372T4 1384492 NM INTERMITTENT A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 Fwd ceiling emergency exit light intermittant. Replaced exit light housing assembly per BMM 33-51-11. ops check good 2 L 7 2 4F A16WE 2001081700082 20010817 00082 NM 2001 8 17 AWXA0001975 1 20010505 A 5320 6545833640 WEB BOEING 737 7372Q8 138448K NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 FLOOR STRUCTURE CRACKED BS 178 WL 207 RBL 25 CONFIRMED VISUAL HFEC CAL 0769. REMOVED DAMAGED INTERCOSTAL WEB, ALSO REMO VED CRACKED CLIP, FAB NEW WEB AND CLIP PER SRM 53-10-51 AND 51-30-11. TREATED, PRIMED AND TOP COATED AND INSTALLED AT B S 178 WL 207 RBL 25 REF DWG 65-45833. 2 L 7 2 4F RT A16WE 2001081700083 20010817 00083 WP 2001 8 17 RRXA11352 1 20010614 A 5310 56441300 SKIN DOUG DC8 DC873F 302199F WP FS1793RSTR 26 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND EMPINNAGE EXT SKIM, FS 1793, R STR 26, HAS HEAVY CORR EXFOLIATION AROUND A FASTNER, *** CORRECTIVE ACTION *** CUT OUT DAMAGE AREA, FABRICATED REPAIR DOUBLER PER SRM 53-5-0 FIG 46A18, FILLER PER SRM 53-2-0 F IG 1D AND INSTALLED REPAIR PARTS PER SRM 51-1-21 AND 53-2-0 FIG 10. 2 L 7 4 4F RT 4A25 2001081700084 20010817 00084 WP 2001 8 17 RRXA11353 1 20010617 A 5310 5644130 SKIN DOUG DC8 DC873F 302199F WP STA 1781 - 1793 GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND EMPINNAGE SKIN L/H SIDE OF #60 PANEL HAS A GOUGE WITH FILLER IN PORTIONS OF IT. FROM L ONG 26L TO 36 STA 1781 TO 1793. *** CORRECTIVE ACTION *** REMOVED FILLER AND FASTENER PER SRM 51-1-21, CUT OUT DAMAGE P ER SRM 53-2-0 FIG 1D, FABRICATED REPAIR DOUBLER PER SRM 53-2-0 FIG 1D. INSTALLED CONICAL WASHERS PER SRM 51-1-26, INSTA LLED DOUBLER PER SRM 51-1-26. 2 L 7 4 4F RT 4A25 2001081700085 20010817 00085 WP 2001 8 17 RRXA11357 1 20010619 A 5310 5613862 ANGLE DOUG DC8 DC873F 302199F WP R/H CUSP CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND R/H CABIN CUSP FWD END CUSP ANGLE CRACKED. *** CORRECTIVE ACTION *** REPAIRED CUSPANGL E IAW DC8 SRM 53-2-0 FIG 1B, LOWER SIDE STA 825 LONG 21R. 2 L 7 4 4F RT 4A25 2001081700086 20010817 00086 WP 2001 8 17 RRXA11358 1 20010619 A 5710 5769589 RIB DOUG DC8 DC873F 302199F WP RT WING L/E CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND R/H WING CENTER L/E RIB STA XFS 397 CRACKED UPPER AFT END. *** CORRECTIVE ACTION *** REPAIRED RIB IAW DC8 SRM 57-2-0 FIG 2 2 L 7 4 4F RT 4A25 2001081700087 20010817 00087 WP 2001 8 17 RRXA11359 1 20010619 A 5710 5769589 RIB DOUG DC8 DC873F 302199F WP R/H WING L/E CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND R/H WING CENTER L/E STA XFS 372 CRACKED UPPER AFT END. *** CORRECTIVE ACTION *** REPAI RED RIB IAW DC8 SRM 57-2-0 FIG 2 2 L 7 4 4F RT 4A25 2001081700088 20010817 00088 WP 2001 8 17 RRXA11360 1 20010619 A 5710 5769589 RIB DOUG DC8 DC873F 302199F WP R/H WING L/E CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND R/H WING CENTER L/E XFS 393 RIB CRACKED UPPER AFT END. *** CORRECTIVE ACTION *** REPA IRED RIB IAW DC8 SRM 57-2-0 FIG 2 2 L 7 4 4F RT 4A25 2001081700089 20010817 00089 WP 2001 8 17 RRXA11362 1 20010620 A 5310 375857042 FITTING DOUG DC8 DC873F 302199F WP FS1172 L35L CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND C PIT FITTING FWD SIDE OF FRAME 1172 L35L CRACKED AT TOP FLANGE. *** CORRECTIVE ACTION *** REMOVED AND REPLACED FITTING IAW DWG 3758570, AND DC8 SRM 53-1-0 AND 51-1-20 D. 2 L 7 4 4F RT 4A25 2001081700090 20010817 00090 WP 2001 8 17 RRXA11363 1 20010620 A 5310 37584962N FITTING DOUG DC8 DC873F 302199F WP STA 1160 L35R CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND C PIT FITTING FWD SIDE FRAME 1160 L35R IS CRACKED. *** CORRECTIVE ACTION *** REMOVED A ND REPLACED PN 3758496-2N PER 51-1-20D 2 L 7 4 4F RT 4A25 2001081700091 20010817 00091 WP 2001 8 17 RRXA11364 1 20010621 A 5710 5769589 RIB DOUG DC8 DC873F 302199F WP LH WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND L/H WING CENTER L/E STA XFS 310 RIB CRACKED AFT UPPER END. *** CORRECTIVE ACTION *** REPAIRED RIB IAW DC8 SRM 57-2-0 FIG 2 2 L 7 4 4F RT 4A25 2001081700092 20010817 00092 WP 2001 8 17 RRXA11365 1 20010622 A 5700 SKIN DOUG DC8 DC873F 302199F WP R/H L/E XFS 300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND R/H WING L/E SKIN DISBONDED & CORROSION AT XFS 300. *** CORRECTIVE ACTION *** REMOVED CORROSION, THICKNESS 0.82 - 0.88, MATERIAL LOSS WITHIN LIMITS. TREATED AND PRIMMED IAW SRM 51-1-8 AND 57-5-0 FIG 7 RESP ECTIVELY 2 L 7 4 4F RT 4A25 2001081700093 20010817 00093 WP 2001 8 17 RRXA11367 1 20010623 A 5710 5769589 RIB DOUG DC8 DC873F 302199F WP RH WING MID LE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND R/H WING MID L/E UPPER RIB TIP CRACKED AT STA XS461. *** CORRECTIVE ACTION *** REMOVED FASTENER PER SRM 51-1-21. STOP DRILLED CRACK PER SRM 57-2-0 FIG 2 PG 9 NOT VERIFIED CRACK TERMINATES AT STOP DRILL PER SPM0G10-01.001. FABRICATED REPAIR PARTS AND INSTALLED THEM PER SRM 57-2-0 FIG 2, SRM 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2001081700094 20010817 00094 WP 2001 8 17 RRXA11368 1 20010623 A 5710 5769589 RIB DOUG DC8 DC873F 302199F WP RH WING MID LE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND R/H WING MID L/E UPPER RIB TIP CRACKED STA XS 473.5. *** CORRECTIVE ACTION *** REMOVE D FASTENER PER SRM 51-1-21 STOP DRILLED CRACK PER SRM 57-2-0 FIG 2, NDT DETERMINED CRACK TERMINATES AT STOP DRILL PER SR M 06-10-01.001. FABRICATED AND INSTALLED REPAIR PART PER SRM 57-2-0 FIG 2, SRM 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2001081700095 20010817 00095 WP 2001 8 17 RRXA11369 1 20010623 A 5710 5769589 RIB DOUG DC8 DC873F 302199F WP RH WING MID LE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND R/H WING MID L/E UPPER RIB TIP CRACKED STA 480. *** CORRECTIVE ACTION *** REMOVED FAST ENER PER SRM 51-1-21. STOP DRILLED CRACK PER SRM 57-2-0 FIG 2. NDT DETERMINED CRACK TEMINATED AT STOP DRILL PER SPM 06 -10-01.001, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 57-2-0 FIG 2, SRM, SRM 51-1-21 AND 51-1-20D 2 L 7 4 4F RT 4A25 2001081700096 20010817 00096 WP 2001 8 17 RRXA11371 1 20010623 A 5310 5769589 RIB DOUG DC8 DC873F 302199F WP LH WING CTR LE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND L/H CENTER L/E @ XS461 RIB IS CRACKED AT UPPER SKIN END. *** CORRECTIVE ACTION *** ST OP DRILLED CRACK PER SRM 57-2-0 FIG 2. NDT CRACK TERMINATED PER SPM 06-10-01.001. FABRICATED AND INSTALLED REPAIR PART S PER SRM 57-2-0 FIG 2 AND SRM 51-1-21 AND 51-1-20D 2 L 7 4 4F RT 4A25 2001081700097 20010817 00097 WP 2001 8 17 RRXA11372 1 20010623 A 5310 5750917 SEAT TRACK DOUG DC8 DC873F 302199F WP STA 550-590 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND CORROSION ON SEAT TRACK MAIN CABIN STA 550-590 LBL48 - LBL63. *** CORRECTIVE ACTION ** * REMOVED AND REPLACED CORRODED FASTENER IAW SRM51-3-0. SPLICED CORRODED SEAT TRACK IAW SRM 53-2-3 FIG 8A AND 51-3-0. 2 L 7 4 4F RT 4A25 2001081700098 20010817 00098 WP 2001 8 17 RRXA11373 1 20010626 A 5710 576953054 RIB DOUG DC8 DC873F 302199F WP RH LE XFS 329.0 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND R/H CTR L/E XFS 329.0 LWR WAS CRACKED. *** CORRECTIVE ACTION *** REMOVED AND REPLACED RIB AND REINSTALLED IAW SRM 51-1-20D AND DWG 5769530-54. 2 L 7 4 4F RT 4A25 2001081700099 20010817 00099 WP 2001 8 17 RRXA11374 1 20010625 A 5310 5613860101 DOUBLER DOUG DC8 DC873F 302199F WP L21R STA 25-8 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND FUSELAGE BULGED, POSSIBLE INTERNAL CORROSION @ L21R STA 25 - 8. *** CORRECTIVE ACTION *** REMOVED FASTENER, REMOVED CORRODED DOUBLER. FABRICATED AND INSTALLED REPLACEMENT PART IAW DWG 561386-5613861 AND S RM 51-1-21-1 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2001081700100 20010817 00100 WP 2001 8 17 RRXA11375 1 20010625 A 5730 5769857 SKIN DOUG DC8 DC873F 302199F WP RH WIN XFS 300 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND R/H WING L/E STA XFS 300 LWR SKIN CRACKED AT FASTENER HOLE. *** CORRECTIVE ACTION *** REPAIRED SKIN IAW 8110-3 APPROVED DH SK 873-883 2 L 7 4 4F RT 4A25 2001081700101 20010817 00101 WP 2001 8 17 RRXA11377 1 20010627 A 5310 55976461 FRAME DOUG DC8 DC873F 302199F WP STA 55 L24L CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND FRAME STA 55 L24L CRACKED. *** CORRECTIVE ACTION *** REMOVED DAMAGED AREA IAW SRM 53-3 -3, FABRICATED AND INSTALLED REPLACEMENT PARTS IAW SRM 53-3-3 FIG 3, 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2001081700102 20010817 00102 WP 2001 8 17 RRXA11378 1 20010627 A 5310 3754473501 FITTING DOUG DC8 DC873F 302199F WP STA 1290 L31L CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND CPIT L31L SPLICE FITTING CRACKED. *** CORRECTIVE ACTION *** REMOVED AND REPLACED FITTI NG IAW SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001081700103 20010817 00103 WP 2001 8 17 RRXA11379 1 20010627 A 5710 5770407502 FITTING DOUG DC8 DC873F 302199F WP RT WING L/E CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND R/H WING CTR L/E STA XFS 404-400 FITTING CRACKED. *** CORRECTIVE ACTION *** REMOVED A ND REPLACED FITTING IAW DWG # 5770409, SRM 51-1-20, 51-1-21 AND 51-1-21A 2 L 7 4 4F RT 4A25 2001081700104 20010817 00104 WP 2001 8 17 RRXA11380 1 20010629 A 5310 3755847501N FITTING DOUG DC8 DC873F 302199F WP STA 1172 L33R CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND FITTING CRACKED IN CPIT FWD TORQUE BOX STA 1172 L33R. *** CORRECTIVE ACTION *** REMOVE D AND REPLACED PER SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001081700105 20010817 00105 WP 2001 8 17 RRXA11381 1 20010629 A 5310 37558411 FITTING DOUG DC8 DC873F 302199F WP STA1220 L33R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND CORRODED BATH TUB FITTING AT STA 1220 L33R - L34R. *** CORRECTIVE ACTION *** REMOVED A ND REPLACED CORRODED BATH TUB FITTING AT STA 1220 L33R - L34R IAW SRM 51-1-20 2 L 7 4 4F RT 4A25 2001081700106 20010817 00106 WP 2001 8 17 RRXA11382 1 20010630 A 5720 425469361 DOUBLER DOUG DC8 DC873F 302199F WP RH WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND R/H WING UPPER CUTOUTS FOR #1 SPOILER MID HINGES ARE DISTORTED/BENT UPWARD. ***CORRECT IVE ACTION *** FABRICATED DOUBLERS INSTALLED DOUBLERS IAW SRM 57-2-0 FIG 2A 2 L 7 4 4F RT 4A25 2001081700107 20010817 00107 WP 2001 8 17 RRXA11383 1 20010630 A 5310 3754946502 FITTING DOUG DC8 DC873F 302199F WP R/H CUSP CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND R/H LWR CUSP TO FLOOR BEAM SUPPORT FITTING CRACKED AT STA 1220. *** CORRECTIVE ACTION *** REMOVED AND REPLACED FITTING IAW SRM 51-1-21 AND 51-1-21D 2 L 7 4 4F RT 4A25 2001081700108 20010817 00108 WP 2001 8 17 RRXA11384 1 20010620 A 2710 8736703 FILLER DOUG DC8 DC873F 302199F WP R/H AILERON CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND R/H O/B AILERON UPPER ACCESS FOR THE O/B DAMPERS HAS TORN SKIN AT CUTOUT PERIMETER. * ** CORRECTIVE ACTION *** FABRICATED AND INSTALLED FILLERS IAW DHSK 873-670, SRM 51-1-5, 51-1-11, 51-1-21 2 L 7 4 4F RT 4A25 2001081700109 20010817 00109 WP 2001 8 17 RRXA11385 1 20010620 A 5512 42546095 SKIN DOUG DC8 DC873F 302199F WP STA 1903 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND EMPENNAGE EXT SKIN CRACKED LT SIDE AT STA 1903, UPPER SIDE HORIZONTAL STAB. REMOVED AN D REPLACED SKIN IAW SRM 51-1-20, 51-1-11, FABRICATED SKIN IAW SRM 53-5-3 FIG 2 2 L 7 4 4F RT 4A25 2001081700110 20010817 00110 WP 2001 8 17 RRXA11386 1 20010629 A 5310 3779919IN SPLICE DOUG DC8 DC873F 302199F WP STA 1340 L36 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND D PIT L36 SPLICE FITTING CRACKED STA 1340. *** CORRECTIVE ACTION *** REMOVED AND REPLA CED CRACKED FITTING IAW SRM 51-1-20D AND 51-1-11. 2 L 7 4 4F RT 4A25 2001081700111 20010817 00111 WP 2001 8 17 MWEA011127 1 20010816 A 5310 49122791 STOP DOUG DC9 DC932 3022066 WP Zone 800 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 REMOVE FORWARD CARGO JAMB, LOWER TWO CARGO DOOR STOPS TO FOM. -- MAINTENANCE FOUND FORWARD STOP TO BE CRACKED. REMOVE D AND REPLACED NEW STOP. 2 L 7 2 4F A6WE 2001081700112 20010817 00112 WP 2001 8 17 MWEA011128 1 20010816 A 5310 99577393 FRAME DOUG DC9 DC932 3022066 WP STATION 945 MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 TWO MISDRILLED HOLES AT STATION 945 LONGERON 14 LEFT ON FRAME. -- FABRICATED AND INSTALLED REPAIR ANGLES. 2 L 7 2 4F A6WE 2001081700113 20010817 00113 WP 2001 8 17 MWEA011129 1 20010816 A 5310 99577399 SHEAR TIE DOUG DC9 DC932 3022066 WP STATION 945 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 SHEAR TIE AT STATION 945 LEFT SIDE BETWEEN LONGERON 16 AND 14 CRACKED IN RADIUS 2 PLACES. -- FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F A6WE 2001081700114 20010817 00114 NM 2001 8 17 AWXA0001984 1 20010716 A 5753 7220L PANEL BOEING 737 737300 1384610 NM T/E FLAP DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23499 LEFT I/B MIDFLAP T/E PANEL 722OL APPROX 18 INCHES I/B OF O/B END HOT BOND REPAIR NOT ACCOMPLISHED PER SRM 51-70-10. REP AIRED LEFT I/B MID FLAP T/E PANEL 7220L WITH A HOT BOND RCF SRM 57-53-02 & SRM 51-70-10. 2 L 7 2 4F RT A16WE 2001081700115 20010817 00115 NM 2001 8 17 AWXA0001985 1 20010716 A 5753 7220L PANEL BOEING 737 737300 1384610 NM T/E FLAP DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23499 LEFT INBOARD MID FLAP T/E PANEL 7220L APPROX 15 INCHES OUTBOARD END, HOT BOND REPAIR WAS NOT ACCOMPLISHED PER SRM 51-70- 10. REPAIRED LEFT INBOARD MID FLAP T/E PANEL 7220L WITH HOT BOND PER SRM 57-53-02 & 51-70-10. 2 L 7 2 4F RT A16WE 2001081700116 20010817 00116 NM 2001 8 17 AWXA0001986 1 20010505 A 5210 SKIN BOEING 737 7373Q8 1384670 NM ENTRY DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 AFT ENTRANCE DOOR SKIN CRACKED AT UPPER HINGE CUTOUT LOWER RADIUS. REPAIRED PER SRM 52-00-01 FIG 202. 2 L 7 2 4F RT A16WE 2001081700117 20010817 00117 NM 2001 8 17 AWXA0001987 1 20010523 A 5320 STIFFENER BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 BS 178 LBL 5.7 WL 182 VERTICAL STIFFENER CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 5 3-10-08. 2 L 7 2 4F RT A16WE 2001081700118 20010817 00118 NM 2001 8 17 AWXA0001988 1 20010524 A 5753 6546486 SKIN BOEING 737 7373Q8 1384670 NM T/E FLAP DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 RIGHT O/B FOREFLAP I/B AND LOWER SURFACE HOT BOND REPAIR NOT ACCOMPLISHED PER SRM 51-70-10. REPAIRED RIGHT O/B FOREFLAP I/B END LOWER SURFACE PER SRM 57-53-02 AND SRM 51-70-10 WITH METAL TO METAL HOT BOND + ER 03-5100-00223-BAIA. 2 L 7 2 4F RT A16WE 2001081700119 20010817 00119 NM 2001 8 17 AWXA0001990 1 20010716 A 5330 6545775 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 CRACK AT LT FUSELAGE SKIN EXTENDING FROM UNDER PREVIOUS REPAIR STA 747 STR 25L. REPAIRED PER AWA ENGINEERING REPAIR 03- 5331-01192JS1. 2 L 7 2 4F RT A16WE 2001081700120 20010817 00120 NM 2001 8 17 AWXA0001991 1 20010715 A 3260 189915 UPLOCK SENSOR BOEING 737 737317 138447P NM LT MLG DEFECTIVE A AWXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 336AW 23707 AIR TURNBACK- FLT 592- AFTER TAKEOFF WHEN THE LANDING GEAR WAS RETRACTED THE LEFT MAIN GEAR RED GEAR UNSAFE LIGHT REMAIN ED ILLUMINATED. THE CREW EXTENDED THE GEAR AND GOT 3 GREEN LIGHTS. THE GEAR WAS CYCLED UP AGAIN AND THE LEFT MLG RED LI GHT REMAINED ILLUMINATED. THE CREW SELECTED GEAR DOWN AND RETURNED TO PHX MAKING AN UNEVENTFUL LANDING. IN PHX MAINTE NANCE TROUBLE SHOT AND CHANGED THE LT MAIN LANDING GEAR UPLOCK SENSOR PER AMM 32-61-21. OPERATIONAL CHECKS WERE GOOD. NO FURTHER DISCREPANCIES HAVE BEEN REPORTED. 2 L 7 2 4F RT A16WE 2001081700121 20010817 00121 NM 2001 8 17 AWXA0001992 1 20010715 A 5347 654N02438 SEAT TRACK BOEING 757 757225 1384959 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 PASSENGER CABIN SEAT TRACK TOP FLANGE CORRODED AROUND FASTENER HOLES B/S 420, RBL 44. REMOVED AND REPLACED SEAT TRACK S UPPORT B/S 420, RBL 44, IAW SRM 51-40-02 FIG 12 PAGE 42. 2 L 7 2 4F RT A2NM 2001081700122 20010817 00122 EU 2001 8 17 AWXA0001993 1 20010629 A 5320 D53472189020185 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 645AW 238 AFT CABIN FLOOR SUPPORT AT Y1292 RT FR 68 SCREW HOLES DAMAGED. REPLACED FLOOR SUPPORT PER SRM 53-41-11. 2 L 7 2 4F RT A28NM 2001081700123 20010817 00123 EU 2001 8 17 AWXA0001996 1 20010629 A 5320 D5347217220300 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 645AW 238 AFT CABIN FLOOR SUPPORT AT Y1162 FR 66R AND 69R SCREW CLIP ATTACH HOLE CORRODED. AFT GALLEY FLOOR SUPPORT AT Y1162 FR66 R-69R REPLACED AS PER A320 SRM 51-42-11 PAGE 1. 2 L 7 2 4F RT A28NM 2001081700124 20010817 00124 EU 2001 8 17 AWXA0001997 1 20010629 A 5320 D531128020200 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 645AW 238 FWD GALLEY FLOOR SUPPORT AT Y-81 FR 14R, 15R AND 16R CORRODED. FWD GALLEY FLOOR SUPPORT AT Y-81 FR12R-16R REPLACED AS P ER A320 SRM 53-11-15 FIG 203. 2 L 7 2 4F RT A28NM 2001081700125 20010817 00125 EU 2001 8 17 AWXA0001998 1 20010707 A 5320 D53472090002 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 645AW 238 AFT CABIN FLOOR PANEL SUPPORT AT Y-765 LT FR 66 TO FR68 SCEW HOLES CORRODED. REMOVED CORROSION, MATERIAL REMOVED .035 I NCH (BEYOND LIMITS AS PER A320 SRM 53-41-14). REPLACED BEAM AS PER A320 SRM 51-42-11 PG 1. 2 L 7 2 4F RT A28NM 2001081700126 20010817 00126 EU 2001 8 17 AWXA0001999 1 20010707 A 5315 D5348004320501 FLOORBEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 645AW 238 AFT CABIN FLOOR PANEL SUPPORT AT Y-1732 RT FR 66 SCREW HOLES CORRODED. REMOVED CORROSION, MATERIAL REMOVED .100 INCH (B EYOND LIMITS AS PER SRM 51-72-11 PG 1). REPLACED BEAM AS PER A320 SRM 51-42-11 PAR 6. 2 L 7 2 4F RT A28NM 2001081700127 20010817 00127 NM 2001 8 17 AWXA0002001 1 20010715 A 5320 654N02438 SUPPORT BOEING 757 757225 1384959 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 PASSENGER CABIN SEAT TRACK B/S 400 RBL 26 TO B/S 420 CORRODED. REMOVED CROWN SEAT TRACK STA 400 TO STA 420, REMOVED SUP PORT BEAM, INSTALLED NEW SUPPORT BEAM, REINSTALLED SEAT TRACK, CHANNELS AND INTERCOSTAL PER SRM 51-40-02 PAGE 11 & 12. 2 L 7 2 4F RT A2NM 2001081700128 20010817 00128 NM 2001 8 17 AWXA0002003 1 20010714 A 5315 141N51131 FLOORBEAM BOEING 757 757225 1384959 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 PASSENGER CABIN FLOORBEAM BS 377, BL 0 TO LBL 24, UPPER T-CAP TOP FLANGE AND LOWER SURFACE CORRODED. CUT OUT DAMAGED SE CTION OF UPPER T-CAP FLOORBEAM. FABRICATED NEW SECTION OF BEAM AND REPAIR SPLICE ANGLES AND INSTALLED ALL THE NEW REPAI R PARTS AND PREVIOUSLY REMOVED FLOOR STRUCTURE IN SURROUNDING AREA IAW B757 SRM 53-00-51, FIG 203 & B757 SRM 51-40-2. N EW SECTION FROM RBL 35 RO LBL 72, STA 377. 2 L 7 2 4F RT A2NM 2001081700129 20010817 00129 NM 2001 8 17 AWXA0002004 1 20010720 A 7722 WL202EED6 INDICATOR BOEING 737 73733A 1384673 NM COCKPIT FAILED A AWXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 165AW 47489 14 23626 PHX -AIR TURNBACK- FLT 173- AFTER TAKEOFF FROM PHX THE NR 1 ENGINE EGT INDICATOR WENT TO ZERO AND THE AIRCRAFT RETURNED TO PHX. THE AIRCRAFT LANDED OVERWEIGHT AT 124.3 THOUSAND LBS AND 200 FPM SINK RATE. AN OVERWEIGHT LANDING INSPECTION W AS PERFORMED WITH NO DISCREPANCIES NOTED. PHX MAINTENANCE REMOVED AND REPLACED THE NR 1 EGT INDICATOR AND PERFORMED THE SYSTEM TEST PER AMM 77-22-00. THE EGT HARNESS WAS INSPECTED AND A RESISTANCE CHECK WAS PERFORMED FROM THE INDICATOR TO THE TERMINAL BLOCK ON ENGINE NR 1. NO DISCREPANCIES WERE NOTED. THE ENGINE WAS RUN TO TAKEOFF POWER AND ALL INDICATIO NS WERE NORMAL. NO FURTHER DISCREPANCIES HAVE BEEN REPORTED. 2 L 7 2 4F RT A16WE 2001082000001 20010820 00001 EU 2001 8 20 C2XA01IA331 1 20010816 A 3230 S2918052100260 VALVE AEROSP ATR42 ATR42320 8680930 EU FUSELAGE INOPERATIVE A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 27 15816 105 IAH - FLIGHT 3422, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT EXTEND UNDER NORMAL EXTENSION. THE CREW MANUALLY EX TENDED THE LANDING GEAR AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE LOCKED THE LANDING GEAR IN THE DOWN POSITION AND PLACED THE GEAR ON MEL 32-31-03/C CONTROL NUMBER 014836, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCR AFT RETURNED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR HYDRAULIC SELECTOR VALVE, CLEARED THE MEL, A ND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001082000035 20010820 00035 CE 2001 8 20 GUU2001F00022 1 20010630 A 2612 24412886 FIRE LOOP BEECH 1900 1900C 1154161 CE PWA PT6 PT6* 52043 EA LT ENGINE SHORTED A GUUA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SO 17 143GA UC145 DURING TAXI, LEFT T-HANDLE ILLUMINATED THEN EXTINGUISHED TWICE. CORRECTIVE ACTION: REMOVED AND REPLACED FORWARD FIRE L OOP. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 3 T RT A24CE E2NE 2001082000037 20010820 00037 NM 2001 8 20 R7MR33368 1 20010613 A 3110 245602609000 LIGHT DOUG MD900 MD900 3027375 NM PWA PW206 PW206A NE COCKPIT INOPERATIVE A R7MR O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 901CF 342 90000012 UNIT INOPERATIVE, CAUSING IIDS FAULT 2=10, SECONDARY ELEMENT FAILURE. LAMP IS SUBASSEMBLY TO IIDS ASSEMBLY, IIDS SN 008 251-012 IS CURRENTLY INSTALLED AND HAS BEEN MORE RELIABLE THAN PREVIOUS INSTALLATIONS; THEREFORE REMSA IS ORDERING JUST THE LAMP ASSEMBLY AS OPPOSED TO ORDERING THE ENTIRE IIDS. 1 G 7 2 3U 3 U NC H19NM E42NE 2001082000043 20010820 00043 NM 2001 8 20 PCAA0108090 1 20010816 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM # 1 CARGO BAY FALSE ACTIVATION A PCAA K NONE N FALSE WARNING TO TAKEOFF 1 EA 13 834EX 17023 5954 285 PHL-3643. CREW REPORTED CARGO SMOKE ANNUNCIATOR ILLUMINATED INTERMITTENTLY AFTER TAKEOFF. MAINTENANCE REPLACED #2 SMOK E DETECTOR. OPERATIONAL CHECK GOOD. #1 SMOKE ISOLATED MEL 26-8 ISSUED. #1 SMOKE DETECTOR REPLACED 17AUG.2001. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001082000050 20010820 00050 EU 2001 8 20 TI1R001388 1 20010107 A 6520 4639003007 TRANSMISSION BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR MAKING METAL B TI1R O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 05 317MC 2447 7505 TAIL ROTOR TRANS, CHIP LIGHT ILLUMINATED, FOUND SEVERAL LARGE FLAT FLAKES ON PLUG. REMOVED AND REPLACED. 1 G 7 2 3U 3 U NC H13EU E19EU 2001082000052 20010820 00052 WP 2001 8 20 2001F00173 1 20010706 A 3350 872100191 RECEIVER DOUG DC9 DC981 3022081 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 801US 48037 IND - THE LOW LEVEL EMERGENCY LIGHTS AND THE RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES AND THE REMOTE RECEIVER. THE OVERWING EMERGENCY EXIT LIGHT WAS REPLACE D. THE GREEN CUEING LIGHT ON THE OVERWING EMERGENCY LIGHT WAS INTERMITTENT BUT THE LIGHT FUNCTIONED NORMALLY AS AN EMER GENCY LIGHT. THE LIGHT ASSEMBLY WAS PLACED ON MEL AND THE AIRCRAFT DISPATCHED. REF USAAD01131. (M) 2 L 7 2 4F A6WE 2001082000053 20010820 00053 WP 2001 8 20 2001F00174 1 20010706 A 3350 873100272 LIGHT DOUG DC9 DC981 3022081 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 801US 48037 IND - THE LOW LEVEL EMERGENCY LIGHTS AND THE RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES AND THE REMOTE RECEIVER. THE OVERWING EMERGENCY EXIT LIGHT WAS REPLACE D. THE GREEN CUEING LIGHT ON THE OVERWING EMERGENCY LIGHT WAS INTERMITTENT BUT THE LIGHT FUNCTIONED NORMALLY AS AN EMER GENCY LIGHT. THE LIGHT ASSEMBLY WAS PLACED ON MEL AND THE AIRCRAFT DISPATCHED. REF USAAD01131 (M) 2 L 7 2 4F A6WE 2001082000054 20010820 00054 NM 2001 8 20 2001F00184 1 20010501 A 5755 654645151A SKIN BOEING 737 7372H4 138448C NM SPOILER DELAMINATED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 29SW 21340 THE UPPER SKIN OF SPOILER NR 8 WAS FOUND DELAMINATED. THE DAMAGED AREA WAS REPAIRED IAW EO COO-CMP-3-57-246-01. (M) 2 L 7 2 4F A16WE 2001082000055 20010820 00055 NM 2001 8 20 2001F00185 1 20010501 A 5753 654643089 FLAP BOEING 737 7372H4 138448C NM WING WORN A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 29SW 21340 THE UPPER SURFACE OF THE INBOARD FORE FLAP WAS SHOWING WEAR. THE DAMAGED AREA WAS REPAIRED IAW EO COO-CMP-A57-243-01, D ATED JUNE 06-01. (M) 2 L 7 2 4F A16WE 2001082000056 20010820 00056 NM 2001 8 20 2001F00186 1 20010501 A 5754 6546423251 SLAT BOEING 737 7372H4 138448C NM WING DELAMINATED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 29SW 21340 THE NR 3 SLAT WAS FOUND DELAMINATED. THE DAMAGED AREA WAS REPAIRED IAW EO COO-CMP-3-57-239-01. (M) 2 L 7 2 4F A16WE 2001082000057 20010820 00057 NM 2001 8 20 2001F00187 1 20010501 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 29SW 21340 FOUND FLOORBEAM AT BS 520 RBL 25 INCH LOWER CHORD HAS CRACK. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-9 FIGURE 7. ( M) 2 L 7 2 4F A16WE 2001082000058 20010820 00058 NM 2001 8 20 2001F00188 1 20010501 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 29SW 21340 FOUND FLOORBEAM FOUND CRACKED AT BS 520 RBL 25 WL 208. THE DAMAGED AREA WAS REPAIRED IAW SB 737-53-1120. (M) 2 L 7 2 4F A16WE 2001082000059 20010820 00059 NM 2001 8 20 2001F00189 1 20010501 A 5311 FRAME BOEING 737 7372H4 138448C NM FUSELAGE DAMAGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 29SW 21340 THE FRAME WAS FOUND WITH ELONGATED HOLES AT BS 328 BETWEEN STRINGER 2R AND STRINGER 3R. THE DAMAGED AREA WAS REPAIRED I AW SRM 53-10-4 FIGURE 1. (M) 2 L 7 2 4F A16WE 2001082000060 20010820 00060 NM 2001 8 20 2001F00198 1 20010715 A 3610 66360040165 DUCT BOEING 747 747212B 1384886 NM NR 3 ENGINE CHAFED A EIAA B EMER. DESCENT B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DE DESCENT 1 NM 09 485EV 20712 ORD - FLT 7554 - UPON INITIAL DESCENT INTO ORD, A/C STARTED TO FILL UP WITH SMOKE AND FUMES. AT APPROX THE SAME TIME TH E NR 3 SYSTEM SHOWED LEAKAGE. APPLICABLE EMERGENCY CHECKLISTS WERE PERFORMED AND THE CREW REQUESTED AN IMMEDIATE APPROA CH TO RUNWAY. AIRCRAFT WAS IMMEDIATELY INSPECTED FOR FIRE OR DAMAGE. NONE FOUND. MAINTENANCE CREW INSPECTED NR 3 ENGI NE AND FOUND A CHAFED/RUPTURED HYDRAULIC LINE AND PNEUMATIC DUCT. REF EIA2001232. (M) 2 L 7 4 4F A20WE 2001082000061 20010820 00061 CE 2001 8 20 2001F00199 1 20010627 A 2170 12950231 NOZZLE BEECH 1900 1900D 1154162 CE LT WING CLOGGED A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 19 38537 UE158 FLT 9177 - EYW - DURING TAXI PASSENGER IN SEAT 2A REPORTED HE SAW SMOKE AT HIS FEET AND SMELLED BURNING ODOR. INSPECTED AIRCRAFT AND NO TRACE OF BURNING SMELL WAS DETECTED WITH AIRCRAFT AT HIGH POWER. RAN WITH ALL ENVIRONMENTAL SYSTEMS ON . ONLY CONDENSATION OBSERVED. REMOVED AND REPLACED FOG NOZZLE. OPS CHECK NORMAL. (M) 2 L 7 2 4T RT A24CE 2001082000062 20010820 00062 NM 2001 8 20 2001F00201 1 20010714 A 2750 66218291 FLAP BOEING 727 72721 1384003 NM RT WING OUT OF ADJ A RYNA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CE 07 357QS 19259 MODERATE VIBRATION DURING CLIMB-OUT, ABOVE 260 KNOTS. VIBRATION STOPPED WHEN APPLYING SPEED BRAKES. FUEL DUMPED. RETU RNED TO AIRPORT WITH NO INCIDENT. ADJUSTED UPPER ECCENTRICS ON INBOARD RIGHT FLAP. OPERATIONAL CHECK GOOD. (M) 2 L 7 3 4F A3WE 2001082000063 20010820 00063 EU 2001 8 20 AALA20011127 1 20010508 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70072 515 TUL - FOUND CORROSION ON FRAME 11A AT BOTTOM SECTION OF FRAME 11 AND STRINGER 49L, CORROSION ON LEFT LOWER NWW TORQUE BO X CHORD ANGLE AT FRAME 11 AND STRINGER 49L. COMPLETED REPAIR PER ESO 30595 D=05-18-01. (M) 2 L 7 2 4F RT A35EU 2001082000064 20010820 00064 WP 2001 8 20 AT0100223 1 20010817 A 3350 43 BULB DOUG DC9 DC932 3022066 WP TAILCONE BLOWN A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 818AT 47320 FOUND THE TAIL CONE EMERGENCY RELEASE HANDLE LIGHT INOPERATIVE. CORRECTIVE ACTION: REPLACED BULBS WITH PR4. IAW DC9 MM 33-50. 2 L 7 2 4F A6WE 2001082000065 20010820 00065 NE 2001 8 20 AALA20011249 2 20010613 A 7230 COMPRESSOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE LT ENGINE STALLED A AALA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SW 21 469AA 49599 718509 SFO - FLT 892 - EN ROUTE SFO-DFW, DURING TAKEOFF ROLL, CREW REPORTED A LEFT SIDE COMPRESSOR STALL. ABORTED TAKEOFF. RE TURNED SFO GATE WITHOUT FURTHER INCIDENT. ACCOMPLISHED BORESCOPE INSPECTION IAW THE MM. NO DEFECTS FOUND. SYSTEM GROU ND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F A6WE E9NE 2001082000066 20010820 00066 NM 2001 8 20 AALA20011315 1 20010628 A 2120 CLAMP BOEING 757 757223 1384957 NM A/C BAY BROKEN A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 689AA 25731 DFW - FLT 2155 - SHORTLY AFTER LEVEL OFF AT FL370 GOT CABIN ALT WARNING. CHECKED CABIN PRESSURE AND IT WAS 10,000 FEET. DESCENT INITIATED AND CABIN IMMEDIATELY BEGAN A DESCENT AS WELL. ONLY THING UNUSUAL NOTED JUST PRIOR TO INCIDENT WAS A HOWLING/SQUEALING TYPE NOISE WAS HEARD IN THE COCKPIT FOR ABOUT 1 MINUTE. NO SUCH NOISE WAS HEARD BY FLIGHT ATTENDANT S IN THE MAIN CABIN. BITE CHECKED NR 1 AND NR 2 CABIN PERSSURE CONTROL, PSI'D AIRCRAFT, FOUND LEFT PACK SUPPLY DUCT CLA MP BROKEN. REMOVED AND REPLACED CLAMP, PSI'D AIRCRAFT. OPS CHECK AND LEAK CHECKS OK. OK FOR SERVICE. (M) 2 L 7 2 4F RT A2NM 2001082000067 20010820 00067 NM 2001 8 20 AALA20011319 1 20010613 A 5320 WEB BOEING 727 727223 1384074 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 881AA 21520 TUL - FOUND SMALL CRACK AT RIVET IN TOP OF VERTICAL WEB STATION 1280. CRACK WAS STOPPED DRILLED AND DOUBLER INSTALLED P ER SRM 51-40-2 FIG 1. (M) 2 L 7 3 4F A3WE 2001082000068 20010820 00068 NM 2001 8 20 AALA20011320 1 20010629 A 3350 1001191 LIGHT BOEING 757 757223 1384957 NM L2 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 647AM 24605 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PORTABLE LIGHT AT L2 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT PORTA BLE LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001082000069 20010820 00069 NM 2001 8 20 AALA20011322 1 20010629 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 661AA 25295 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 16D BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001082000070 20010820 00070 NM 2001 8 20 AALA20011323 1 20010630 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 661AA 25295 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 17D BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001082000071 20010820 00071 NM 2001 8 20 AALA20011326 1 20010630 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 640A 24598 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 24D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBL Y AT SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001082000072 20010820 00072 WP 2001 8 20 AALA20011327 1 20010630 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 485AA 49678 LAX - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT BROKEN. REPLACED SEAT MOUNTED EMERGENCY EXIT LIGH T ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001082000073 20010820 00073 NM 2001 8 20 AALA20011330 1 20010630 A 3350 CONTACTOR BOEING 777 777223 1385213 NM L3 DOOR DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 770AN 29578 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L3 DOOR INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT CONTACT A T L3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001082000074 20010820 00074 NM 2001 8 20 AALA20011332 1 20010629 A 2421 IDG BOEING 777 777223 1385213 NM LT ENGINE FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 770AN 29578 NRT - LEFT ENGINE GENERATOR FAILED IN FLIGHT, ONE RESET ATTEMPTED. CHECKED IDG FEEDER WIRES AT PYLON DISCONNECT, FOUND OK. REPLACED LEFT IDG AND GCU PER MM AND SYSTEM CHECKS OK ON ENGINE RUN. (M) 2 L 7 2 4F RT T00001SE 2001082000075 20010820 00075 NM 2001 8 20 AALA20011334 1 20010702 A 3350 1000679 LIGHT BOEING 767 767323 1385205 NM COCKPIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 368AA 25195 MIA - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT AT FLIGHT DECK INOPERATIVE. REPLACED OVERHEAD EMERGEN CY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001082000076 20010820 00076 NM 2001 8 20 AALA20011350 1 20010629 A 5730 SKIN BOEING 727 727223 1384074 NM WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 889AA 21527 TUL - FOUND CORROSION ON LOWER WING SKIN AT RBL 18 STRINGER 4. INSTALLED DOUBLER, TRIPLER AND QUAD TRIPLER PER SRM 57-3 0-3. (M) 2 L 7 3 4F A3WE 2001082000077 20010820 00077 NM 2001 8 20 AALA20011351 1 20010702 A 5730 SKIN BOEING 727 727223 1384074 NM WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 889AA 21527 TUL - FOUND CORROSION ON LOWER WING SKIN LBL 25 AT STRINGER 6. REMOVED CORROSION. INSTALLED DOUBLER AND TRIPLER PER SR M 57-30-3. (M) 2 L 7 3 4F A3WE 2001082000078 20010820 00078 WP 2001 8 20 AALA20011371 1 20010708 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 487AA 49680 DFW - DURING OVERNIGHT MAINTENANCE FLIGHT ATTENDANT FORWARD EMERGENCY EXIT PORTABLE LIGHT INOPERATIVE. REPLACED PORTABL E EMERGENCY EXIT FLIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001082000079 20010820 00079 WP 2001 8 20 AALA20011372 1 20010708 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 233AA 49180 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001082000081 20010820 00081 NM 2001 8 20 AALA20011374 1 20010707 A 2932 O-RING BOEING 757 757223 1384957 NM HYDRAULIC SYS LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 650AA 24608 DEN - FLT 278 - EN ROUTE DFW-ANC, DETECTED HYDRAULIC QUANTITY INDICATION ILLUMINATE. DIVERTED DEN AND LANDED WITHOUT FU RTHER INCIDENT. REPLACED RIGHT PRESSURE SWITCH O-RING. SERVICED HYDRAULIC SYSTEM. LEAK CHECKS GOOD. SYSTEM GROUND CH ECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001082000083 20010820 00083 NM 2001 8 20 AALA20011401 1 20010706 A 5311 FRAME BOEING 727 727227 1384078 NM FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 726AA 20733 TUL - FOUND BELT FRAME DENTED AT STATION 1050 OVER STRINGER 26L. CUT OUT DAMAGE AND INSTALLED BELT FRAME REPAIR PER 53- 10-4 PAGE 1. (M) 2 L 7 3 4F A3WE 2001082000085 20010820 00085 NM 2001 8 20 AALA20011402 1 20010706 A 5330 SKIN BOEING 727 727227 1384078 NM FUSELAGE BULGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 726AA 20733 TUL - FOUND SKIN BULGING AT RIVETS, RIVETS DISHED ON SKIN LAP 24R STATION 343 TO 360. REPAIRED AREA PER SRM 53-30-4 FIG 16. (M) 2 L 7 3 4F A3WE 2001082000086 20010820 00086 NM 2001 8 20 AALA20011407 1 20010704 A 5311 FRAME BOEING 727 727227 1384078 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 726AA 20733 TUL - FOUND BELT FRAME CRACKED STATION 312 BETWEEN STRINGER 13, 14 RIGHT SIDE FORWARD LAVATORY. REMOVED DAMAGED SECTION . INSTALLED DOUBLER REPAIR PER RM 53-10-4. (M) 2 L 7 3 4F A3WE 2001082000088 20010820 00088 NM 2001 8 20 AALA20011411 1 20010709 A 3221 TRUNNION BOEING 727 727227 1384078 NM NLG CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 731AA 20738 TUL - FOUND CORROSION IN NOSE GEAR TRUNNION FITTINGS. CORROSION REMOVED, NOSE GEAR TRUNNION FITTINGS WERE REBORED AND R EBUSHED PER ESO 11697 DATED 7/6/2001. (M) 2 L 7 3 4F A3WE 2001082000090 20010820 00090 WP 2001 8 20 AALA20011448 1 20010719 A 3350 LIGHT DOUG DC9 DC982 3022082 WP R1 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 226AA 49176 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT AT R1 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AND BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001082000092 20010820 00092 WP 2001 8 20 AALA20011452 1 20010719 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 228AA 49178 DFW - DURING OVERNIGHT MAINTENANCE, AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY FOR AFT OVERWING EX IT SIGN. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001082000094 20010820 00094 NM 2001 8 20 EIAA2001232 1 20010715 A 2910 65B6017089 HYDRAULIC LINE BOEING 747 747212B 1384886 NM NR 3 ENGINE CHAFED A EIAA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 09 485EV 20712 ORD - FLT 7554 - UPON INITIAL DESCENT INTO ORD, A/C STARTED TO FILL UP WITH SMOKE AND FUMES. AT APPROX THE SAME TIME TH E NR 3 SYSTEM SHOWED LEAKAGE. APPLICABLE EMERGENCY CHECKLISTS WERE PERFORMED AND THE CREW REQUESTED AN IMMEDIATE APPROA CH TO RUNWAY. AIRCRAFT WAS IMMEDIATELY INSPECTED FOR FIRE OR DAMAGE. NONE FOUND. MAINTENANCE CREW INSPECTED NR 3 ENGI NE AND FOUND A CHAFED/RUPTURED HYDRAULIC LINE AND PNEUMATIC DUCT. (M) 2 L 7 4 4F A20WE 2001082000103 20010820 00103 WP 2001 8 20 GTIA010628 1 20010702 A 2750 SWITCH DOUG DC9 DC981 3022081 WP T/E FLAP LOOSE A GTIA O OTHER N FALSE WARNING TO TAKEOFF 1 GL 23 818NK 48018 DTW - FLT 1521 - ON POWER ADVANCE AT TAKEOFF WITH AIRCRAFT CONFIGURED 'FLAP' AURAL WARNING CAME ON. RETRACTED AND LOWER ED FLAPS AND SLATS STILL HAD WARNING. FOUND FLAP TAKEOFF SWITCH LOOSE ON MOUNT AND MISSING SCREWS. REPLACED SCREWS AND REPOSITIONED SCREWS IAW MM 27-53-01. UNIT OPS CHECKS GOOD. NO DEFECTS NOTED. (M) 2 L 7 2 4F A6WE 2001082000105 20010820 00105 WP 2001 8 20 GTIA010646 1 20010711 A 3350 FUSE DOUG DC9 DC982 3022082 WP BATTERY CHARGER BLOWN A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 804NK 49104 FLL - FOUND EMERGENCY PATH LIGHTING AFT CABIN INOPERATIVE. FOUND F1 FUSE IN BATTERY CHARGER 'OPEN' IN AFT 'PACK' ALSO F OUND LAMP MODULE SHORTED. REPLACED PICO FUSE P/N Z76005 AND LAMP MODULE, PERFORMED EMERGENCY PATH LIGHTING TEST REF MM 33-52-00, OPS CHECK OK. (M) 2 L 7 2 4F A6WE 2001082000108 20010820 00108 WP 2001 8 20 GTIA010649 1 20010712 A 3350 60030431 BATTERY PACK DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 805NK 48058 FLL - FOUND OVERWING EXITS LEFT AND RIGHT FORWARD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT PA CK FOR CABIN OVERWING FORWARD EMERGENCY EXIT, EXIT LIGHTS LEFT AND RIGHT. OPS CHECK OK IAW MM 33-50-00. (M) 2 L 7 2 4F A6WE 2001082000109 20010820 00109 WP 2001 8 20 GTIA010657 1 20010716 A 3350 60030431 BATTERY PACK DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 819NK 48016 DTW - FLT 594 - CEILING EMERGENCY STANDBY LIGHTS ARE OUT ABOVE ROWS 7, 16, 17, 18, 19, 20, 27, 32. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK T STATION 671 IAW MD80 MM 33-53-01. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2001082000110 20010820 00110 2001 8 20 GTIA010658 4 20010715 A 3421 2587335113 GYRO DOUG DC9 DC983 3022083 WP NR 2 FAULTY A GTIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 23 814NK 49619 FLL - FLT 41 - AUTO PILOT JERKS UP AND DOWN IN PITCH MODE (UNCOMFORTABLE) IN EITHER DFGC 1 OR 2 WHEN VERTICAL GYRO SW SE T AT RIGHT ON AUXILIARY, AUTO PILOT VERY SMOOTH BOTH 1 AND 2 DFGC. REMOVED AND REPLACED NR 2 VERTICAL GYRO, OPS CHECK N ORMAL IAW MM 34-23-00 AND RIGHTS CHECK ACCOMPLISHED OK IAW MM 22-01-05. (M) 2 L 7 2 4F RT A6WE 2001082000111 20010820 00111 WP 2001 8 20 GTIA010670 1 20010718 A 3350 60930431 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 800NK 49144 MYR - FOUND EMERGENCY LIGHTS AT SERVICE DOOR AFT CENTER AISLE DON'T ILLUMINATE. TROUBLESHOT AND FOUND BATTERY PACK AT B 5-107 TO BE DEFECTIVE REMOVED AND REPLACED BATTERY PACK MM 33-52-00 EMERGENCY LIGHTS OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2001082000112 20010820 00112 NE 2001 8 20 GTIA010671 2 20010721 A 7230 COMPRESSOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 2 ENGINE STALLED A GTIA O OTHER R PARTIAL RPM/PWR LOSS AP APPROACH 1 GL 23 800NK 49144 709816 NR 2 ENGINE HAD A COMPRESSOR STALL/PARTIAL POWER FAILURE DURING FINAL APPROACH AND LANDING INTO DTW ENGINE POWER EXCEEDE D THAT QA LIMIT BY APPROX .05 FOR IMMEDIATELY PRIOR TO STALL/POWER LOSS. REMOVED AND REPLACED NR 2 ENGINE IAW MM 71-00- 00. (M) 2 L 7 2 4F 4 F A6WE E9NE 2001082000113 20010820 00113 WP 2001 8 20 GTIA010672 1 20010721 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A K NONE L NO TEST IN INSP/MAINT 1 GL 23 800NK 49144 DTW - FOUND AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. REPAIRED WIRING AT AFT SECTION OF EMERGENCY FLOO R TRACK LIGHTING, OPS CHECKED GOOD IAW MD80 MM 33-53-01. (M) 2 L 7 2 4F A6WE 2001082000114 20010820 00114 2001 8 20 GTIA010674 4 20010721 A 2210 4034242934 CONTROL PANEL DOUG DC9 DC981 3022081 WP COCKPIT MALFUNCTIONED A GTIA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 811NK 48017 FLT 967 - MCO - YAW DAMP ANNUNCIATOR ON IN FLIGHT. REMOVED AND REPLACED DIGITAL FLIGHT GUIDANCE CONTROL PANEL SYSTEM. GROUND CHECKS GOOD IAW MM 22-00-00. (M) 2 L 7 2 4F A6WE 2001082000115 20010820 00115 WP 2001 8 20 HALA0100175 1 20010715 A 3260 PROXIMITY SWITCH DOUG DC9 DC951 3022051 WP LT MLG INTERMITTENT A HALA K NONE N FALSE WARNING CR CRUISE 1 WP 13 662HA 47742 HNL - FLT 165 - LEFT UNSAFE GEAR 'RED' LIGHT DOES INTERMITTENT OFF/ON IN FLIGHT, ENGINES AT IDLE. GEAR SWING, ALL LIGHT S CHECK GOOD. PRECAUTIONARY REPLACED UP PROXIMITY SWITCH AND PLUG. BITE CHECK OF PROXIMITY BOX OK. (M) 2 L 7 2 4F RT A6WE 2001082000116 20010820 00116 NM 2001 8 20 HALA0100176 1 20010715 A 2701 CONTROL COLUMN BOEING 717 717200 1383700 NM COCKPIT DISCONNECTED A HALA K NONE F FLT CONT AFFECTED TX TAXI/GRND HDL 1 WP 13 475HA 55121 FLT 345 - OGG - DURING FLIGHT CONTROL CHECK, THE LEFT AND RIGHT COLUMNS DISCONNECTED DURING ELEVATOR CHECK. RE-SET CONT ROL COLUMN PER MM 27-31-10-44-801. OPS CHECK OK. (M) 2 L 7 2 4F TR A6WE 2001082000117 20010820 00117 WP 2001 8 20 HALA0100186 1 20010719 A 3297 WIRE DOUG DC9 DC951 3022051 WP RT MLG BROKEN A K NONE N FALSE WARNING CR CRUISE 1 WP 13 601AP 47658 FLT 317 - HNL - FOUND RIGHT GEAR UNSAFE LIGHT (RED) CAME ON AND WENT OUT TWICE INBOUND TO HNL. FOUND RIGHT MLG DOWNLOCK SENSOR WIRES BROKEN. REPLACED RIGHT MLG DOWNLOCK SENSOR ASSEMBLY CONDITION AND SECURITY CHECK AND TEST OK. (M) 2 L 7 2 4F RT A6WE 2001082000124 20010820 00124 EU 2001 8 20 SIMA200119801 1 20010717 A 2611 7211121000A SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY MALFUNCTIONED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 901AE 340B401 DFW - FLT 3343 - DURING TAKEOFF, CREW REPORTED A CARGO SMOKE WARNING . CREW DECLARED AND EMERGENCY AND AIRCRAFT WAS RET URNED TO DFW. MAINTENANCE REMOVED AND REPLACED THE FORWARD AND AFT SMOKE DETECTORS (S/N A1594/A4231) IAW SAAB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. MAINTENANCE ALSO REPLACED THE FIRE BOTTLE. (M) 2 L 7 2 4T RT A52EU 2001082000125 20010820 00125 EU 2001 8 20 SIMA200120003 1 20010719 A 5320 7253711245 PLATE SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 284AE 340B284 SBP - LEFT KICK PLATE AT STATION 294 IS CORRODED. REMOVED AND REPLACED KICK PLATE IAW SAAB SRM 51-40-21 AND 51-40-40. (M) 2 L 7 2 4T RT A52EU 2001082000127 20010820 00127 EU 2001 8 20 SIMA200120011 1 20010719 A 5347 7253799383 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 284AE 340B284 SBP - FOUND CABIN SEAT TRACK AT STATION BL 18.3 LEFT IS CORRODED ON THE LOWER FLANGE FORWARD END. PERFORMED SPLICE PROC EDURE IAW SAAB SRM 53-70-60. (M) 2 L 7 2 4T RT A52EU 2001082000128 20010820 00128 EU 2001 8 20 SIMA200120012 1 20010719 A 5347 7253799459 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 284AE 340B284 CABIN SEAT TRACK AT STATION BL 18.3 LEFT IS CORRODED ON THE UPPER FLANGE IN THE CARGO AREA. PERFORMED SPLICE PROCEDURE IAW SAAB SRM 53-70-60. (M) 2 L 7 2 4T RT A52EU 2001082000129 20010820 00129 EU 2001 8 20 SIMA200120015 1 20010719 A 3211 725700182 TRUNNION SAAB SF340 340B 7860101 EU RT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 284AE 340B284 SBP - FOUND RIGHT MAIN LANDING GEAR TRUNNION BEARING SUPPORT HOUSING CORRODED. REMOVED AND REPLACED TRUNNION HOUSING IA W SAAB AMM 57-40-00. (M) 2 L 7 2 4T RT A52EU 2001082000130 20010820 00130 EU 2001 8 20 SIMA200120016 1 20010719 A 3213 AIR830645 STRUT SAAB SF340 340B 7860101 EU LT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 284AE 340B284 SBP - FOUND MAIN LANDING GEAR ASSEMBLY IS CORRODED AT THE ATTACH LUG FOR THE DRAG BRACE LINK. REMOVED AND REPLACED LAND ING GEAR ASSEMBLY IAW SAAB AMM 32-11-05. (M) 2 L 7 2 4T RT A52EU 2001082000131 20010820 00131 EU 2001 8 20 SIMA200120017 1 20010719 A 3213 AIR830645 STRUT SAAB SF340 340B 7860101 EU RT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 284AE 340B284 SBP - FOUND RIGHT MAIN LANDING GEAR ASSEMBLY IS CORRODED AT THE ATTACH LUG FOR THE DRAG BRACE LINK. REMOVED AND REPLACE D LANDING GEAR ASSEMBLY IAW SAAB AMM 32-11-05. (M) 2 L 7 2 4T RT A52EU 2001082000132 20010820 00132 EU 2001 8 20 SIMA200120018 1 20010719 A 5743 7257500067 FITTING SAAB SF340 340B 7860101 EU RT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 284AE 340B284 SBP - FOUND RIGHT MAIN LANDING GEAR SUPPORT FITTING CONNECTION LINK IS CORRODED AT ATTACH BOLT HOLES. REMOVED AND REPLA CED LINK FITTING ASSEMBLY IAW SAAB AMM 57-40-05. (M) 2 L 7 2 4T RT A52EU 2001082000133 20010820 00133 EU 2001 8 20 SIMA200120019 1 20010719 A 5743 7257500067 FITTING SAAB SF340 340B 7860101 EU LT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 284AE 340B284 SBP - FOUND LEFT MAIN LANDING GEAR SUPPORT FITTING CONNECTING LINK IS CORRODED AT ATTACH BOLT HOLES. REMOVED AND REPLAC ED LINK FITTING ASSEMBLY IAW SAAB AMM 57-40-05. (M) 2 L 7 2 4T RT A52EU 2001082000134 20010820 00134 EU 2001 8 20 SIMA200120020 1 20010719 A 2720 7327200561 ATTACH FITTING SAAB SF340 340B 7860101 EU COCKPIT CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 284AE 340B284 SBP - PILOTS RUDDER PEDAL CONSOLE FORWARD ATTACH POINTS CORRODED. REMOVED AND REPLACED RUDDER PEDAL CONSOLE IAW SAAB AM M 27-21-05. (M) 2 L 7 2 4T RT A52EU 2001082000135 20010820 00135 EU 2001 8 20 SIMA200120021 1 20010719 A 2720 7327200561 ATTACH FITTING SAAB SF340 340B 7860101 EU COCKPIT CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 284AE 340B284 SBP - FOUND CO-PILOTS RUDDER PEDAL CONSOLE FORWARD ATTACH POINTS CORRODED. REMOVED AND REPLACED RUDDER PEDAL CONSOLE IA W SAAB AMM 27-21-05. (M) 2 L 7 2 4T RT A52EU 2001082000136 20010820 00136 EU 2001 8 20 SIMA200120022 1 20010719 A 3211 7257500181 TRUNNION SAAB SF340 340B 7860101 EU LT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 284AE 340B284 SBP - FOUND LEFT MAIN LANDING GEAR TRUNNION BEARING SUPPORT HOUSING CORRODED. REMOVED AND REPLACED TRUNNION HOUSING IAW SAAB AMM 57-40-00. (M) 2 L 7 2 4T RT A52EU 2001082000137 20010820 00137 EU 2001 8 20 SIMA200120024 1 20010719 A 5321 FLOOR PANEL SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 340RC 340B340 ABI - DURING AN MBV INSPECTION, FOUND GALLEY FLOOR CORRODED BEYOND LIMITS AT FRAME STATION 258. REPAIRED CORRODED IAW S AAB 340 REPAIR STATEMENT 340SDS002076 PARA 1. (M) 2 L 7 2 4T RT A52EU 2001082000138 20010820 00138 NM 2001 8 20 TSAA0153083 1 20010701 A 5311 65C372772 FRAME BOEING 737 7372S5C 1384499 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 DISCOVERED CRACK PROPAGATING FROM FORWARD FASTENER HOLE AT BS 727 CHORD STRINGER S-18L, DURING SCHEDULED INSPECTION VERI FIED BY METHOD OF HFEC AND ULTRASONIC INSPECTION. INSTALLED REPAIR AND AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001082000139 20010820 00139 NM 2001 8 20 TSAA0153084 1 20010701 A 5311 65C372772 FRAME BOEING 737 7372S5C 1384499 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 DISCOVERED CRACK PROPAGATING FROM THE AFT TO FORWARD FASTENER HOLE AT BS 727 CHORD STRINGER S18R DURING SCHEDULED INSPEC TION VERIFIED BY METHOD OF HFEC AND ULTRASONIC INSPECTION. INSTALLED REPAIR AND AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001082000140 20010820 00140 NM 2001 8 20 USAA010515 1 20010508 A 5320 ANGLE BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 51539 22192 CLT - FOUND FAIL/SAFE ANGLE CRACKED .5 INCH, BS 600 STRINGER 16R. CRACK REMOVED, INSTALLED DOUBLER PER SRM 53-70-11. ( M) 2 L 7 2 4F RT A2NM 2001082000141 20010820 00141 NM 2001 8 20 USAA010532 1 20010510 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 51339 22192 CLT - FOUND FLOORBEAM T-CAP CORRODED IN SIX LOCATIONS EACH ONE IS 1 INCH BY 1 INCH AREA, BS 377.7, LBL 63 TO RBL 63. RE MOVED DAMAGE AND INSTALLED REPAIR FILLER AND DOUBLER PER 53-00-51 FIG 205. (M) 2 L 7 2 4F RT A2NM 2001082000142 20010820 00142 NM 2001 8 20 USAA010574 1 20010531 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 51539 22192 CLT - FOUND FLOORBEAM CORRODED APPROXIMATELY 10 SQUARE INCHES AT SCREW HOLES, BS 365, RBL 15 TO RBL 62. DAMAGE REMOVED, REPLACED T-CAP PER TYPICAL REP 53-15-01. (M) 2 L 7 2 4F RT A2NM 2001082000143 20010820 00143 NM 2001 8 20 USAA010575 1 20010531 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 51539 22192 CLT - FOUND FLOORBEAM CORRODED APPROX 10 INCHES, BS 345, BL 0 TO LBL 45. DAMAGE REMOVED, REPLACED T-CAP PER TYPICAL REP AIR 53-15-01. (M) 2 L 7 2 4F RT A2NM 2001082000144 20010820 00144 NM 2001 8 20 USAA010576 1 20010531 A 5320 FLOOR SUPPORT BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 51539 22192 CLT - FOUND FLOOR SUPPORT BEAM CORRODED, BS 1715, RBL 46. REMOVED DAMAGE, REPLACED BEAM AND ANGLES PER SRM 51-10-2. (M ) 2 L 7 2 4F RT A2NM 2001082000145 20010820 00145 NM 2001 8 20 USAA010577 1 20010531 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 51539 22192 CLT - FOUND FLOORBEAM CORRODED APPROXIMATELY 24 SQUARE INCHES, BS 1661, LBL 55 TO RBL 55. DAMAGE REMOVED, REPLACED T-CA P PER EA 69718. (M) 2 L 7 2 4F RT A2NM 2001082000146 20010820 00146 NM 2001 8 20 USAA010578 1 20010531 A 5320 WEB BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 51539 22192 CLT - FOUND DOOR SILL WEB CORRODED 1 INCH BY 4 INCH AREA, BS 1671 LBL 56.5. FABRICATED AND INSTALLED NEW WEB PER SRM 51 -10-02. (M) 2 L 7 2 4F RT A2NM 2001082000147 20010820 00147 NM 2001 8 20 USAA010579 1 20010531 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 51539 22192 CLT - FOUND FLOORBEAM CORRODED 6 INCH BY 6 INCH AREA, BS 1681, BL 0 TO RBL 55. REMOVED DAMAGE, REPLACED BEAM AND FLOOR PAN PER SRM 53-00-51. (M) 2 L 7 2 4F RT A2NM 2001082000148 20010820 00148 NM 2001 8 20 USAA010604 1 20010605 A 5313 STRINGER BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 51539 22192 CLT - FOUND STRINGER CORRODED 4 INCH AREA, BS 600 TO 660, STRINGER 28L. REMOVED DAMAGE, INSTALLED STRINGER SPLICE REPAI R PER SRM 53-00-03, FIG 201. (M) 2 L 7 2 4F RT A2NM 2001082000149 20010820 00149 NM 2001 8 20 USAA010605 1 20010605 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 51539 22192 CLT - FOUND FLOORBEAM CORRODED 3 INCH BY 2 INCH AREA OF CORROSION, BS 1320, RBL 22. REMOVED DAMAGED T-CAP, INSTALLED NE W T-CAP PER TYPICAL REPAIR 53-15-01 AND EA 69751. (M) 2 L 7 2 4F RT A2NM 2001082000150 20010820 00150 NM 2001 8 20 USAA010607 1 20010605 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 22192 CLT - FOUND FLOORBEAM CORRODED 1 INCH AREA, BS 360, RBL 13. REMOVED DAMAGE, INSTALLED DOUBLER PER RM 53-10-51. (M) 2 L 7 2 4F RT A2NM 2001082000151 20010820 00151 NM 2001 8 20 USAA010608 1 20010605 A 5311 FRAME BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 51539 22192 CLT - FOUND FRAME CORRODED APPROX 1 INCH, BS 540, STRINGER 25L. REMOVED DAMAGE, INSTALLED FRAME DOUBLER REPAIR PER EA 6 9565A. (M) 2 L 7 2 4F RT A2NM 2001082000152 20010820 00152 NM 2001 8 20 USAA010609 1 20010605 A 5310 SHEAR TIE BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 22192 CLT - FOUND SHEAR TIE CORRODED 1 INCH BY 4 INCH AREA, BS 1701, BETWEEN S28L AND S28R. REMOVED AND REPLACED SHEAR TIE CL IPS PER SRM 51-20-01 AND EA 69735. (M) 2 L 7 2 4F RT A2NM 2001082000153 20010820 00153 NM 2001 8 20 USAA010610 1 20010605 A 5313 STRINGER BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 51539 22192 CLT - FOUND STRINGER CORRODED APPROXIMATELY 8 SQUARE INCH AREA, BS 555 TO 600, STRINGER 28R. DAMAGE REMOVED, INSTALLED STRINGER SPLICE REPAIR PER SRM 53-30-03. (M) 2 L 7 2 4F RT A2NM 2001082000154 20010820 00154 NM 2001 8 20 USAA010612 1 20010605 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 51539 22192 CLT - FOUND FLOORBEAM T-CAP CORRODED, APPROXIMATELY 2 INCH BY 6 INCH AREA, BS 324, LBL 23 TO LBL 41. DAMAGE REMOVED, RE PAIR STRAP AND SLEEVE INSTALLED PER SRM 53-10-08 FIG 101, 51-20-07, AND EA 69647. (M) 2 L 7 2 4F RT A2NM 2001082000156 20010820 00156 NM 2001 8 20 USAA010613 1 20010605 A 5311 FRAME BOEING 757 757225 1384959 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 51539 22192 CLT - FOUND FRAME CHORD BURNED APPROXIMATELY .75 INCH, BS 255, RBL 43, WL 180. DAMAGE REMOVED, INSTALLED DOUBLER WITH F ILLER REPAIR PER SRM 53-00-07 FIG 201, AND EA 69684. (M) 2 L 7 2 4F RT A2NM 2001082000157 20010820 00157 NM 2001 8 20 USAA010645 1 20010612 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 51539 22192 CLT - FOUND FUSELAGE SKIN CORRODED .5 INCH BY 1 INCH AREA, BS 690, BELLY, LEFT FORWARD ANTENNA MOUNT. DAMAGE REMOVED, F ABRICATED AND INSTALLED REPAIR DOUBLER, TRIPLER AND FILLERS PER EA 69727. (M) 2 L 7 2 4F RT A2NM 2001082000158 20010820 00158 NM 2001 8 20 USAA010646 1 20010612 A 5320 CHANNEL BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 51539 22192 CLT - FOUND U-CHANNEL CORRODED 20 INCHES BY 2 INCH AREA, BS 560-580, BETWEEN STRINGERS 27R AND 28R. FABRICATED AND INST ALLED NEW U-CHANNEL PER SRM 53-30-04 AND 51-10-02. (M) 2 L 7 2 4F RT A2NM 2001082000159 20010820 00159 NE 2001 8 20 USAABB01037 2 20010609 A 7200 ENGINE BOEING 767 767201 1385125 NM GE CF6 CF680C2B2 30025 NE NR 2 MALFUNCTIONED A USAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 EA 19 647US 23899 LAX - DESCENT THRU FL170 INTO LAX, CREW REPORTED THE NR 2 ENGINE HAD UNSPOOLED AND HAD NO THROTTLE RESPONSE DURING A 1, 500 FPM DESCENT. NO RESTART WAS ATTEMPTED. NO OTHER ENGINE ABNORMAL INDICATIONS NOTED. CREW SHUT DOWN THE ENGINE, DECLAR ED AN EMERGENCY. LANDED WITHOUT INCIDENT.MX STARTED ENGINE ON THE GROUND. TROUBLESHOOTING PROCEDURES LEAD MX TO RETURN THE ENGINE TO SERVICE AS NO WATER WAS FOUND IN THE A/C FUEL SUMPS, THE INLET/EXHAUST INSP FOUND NO FOD OR PARTICLES, CHI P DETECTORS/FILTERS WERE CLEAN AND THE ENGINE HIGH POWER RUNS WERE ACCEPTABLE. MX DID REMOVE AND REPLACED THE NR 2 ENGI NE HIGH PRESSURE FUEL PUMP AND FUEL PRESSURE TRANSDUCER AS PRECAUTION. LEAK CHECK AND POWER RUN GOOD. (M) 2 L 7 2 4F 4 F RT A1NM E13NE 2001082000160 20010820 00160 NM 2001 8 20 USAABB01045 1 20010624 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 604AU 22199 LAX - FOUND LOW LEVEL EMERGENCY LIGHTS INOPERATIVE AT ROWS 1, 4, 22, 29 AND 33. MAINTENANCE REPLACED THE BATTERIES. (M ) 2 L 7 2 4F RT A2NM 2001082000161 20010820 00161 NM 2001 8 20 USAABB01049 1 20010627 A 3350 8731002511REV14 SIGN BOEING 757 7572B7 1384964 NM R3 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 626AU 27303 LAX - FOUND R3 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001082000162 20010820 00162 NM 2001 8 20 USAABB01050 1 20010627 A 2840 CN1156562 PLUG BOEING 767 7672B7 1385107 NM FUEL SYSTEM DEFECTIVE A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 651US 24764 PHL - FLT 126 - EN ROUTE PHL-LGW, CREW NOTED THAT THE CENTER FUEL TANK QUANTITY INDICATION AND THE FUEL TOTALIZER HAD GO NE BLANK. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT AUXILIARY HARNESS AND NR 2 PROBE, WHICH DID NOT SOLVE THE PROBLEM. THE LEFT AND RIGHT BUSSING PLUGS WERE THEN REPLACED. (M) 2 L 7 2 4F RT A1NM 2001082000163 20010820 00163 NM 2001 8 20 USAABB01051 1 20010701 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 610AU 27122 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 29 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001082000164 20010820 00164 NM 2001 8 20 USAABB01053 1 20010629 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 615AU 27146 SFO - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 1, 4, 6, 29 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. ( M) 2 L 7 2 4F RT A2NM 2001082000165 20010820 00165 NM 2001 8 20 USAABB01055 1 20010703 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 615AU 27146 LAX - FOUND FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE AT ROWS 9, 18, 23 AND 26. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2001082000166 20010820 00166 NE 2001 8 20 USAABB01058 2 20010707 A 7530 C8E389 CONTROL UNIT BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE FAULTY A USAA A UNSCHED LANDING B E SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET CR CRUISE 1 EA 19 628AU 23682 27806 31327 IND - FLT 89 - EN ROUTE PIT-SAN, CREW NOTED AN ODOR AND ALSO HAD A LEFT ENGINE VIBRATION. THE FLIGHT DIVERTED TO IND AN D LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED A BORESCOPE INSPECTION, AND INSPECTED THE INLET COWL, LOW PRES SURE COMPRESSOR BLADES, NOSE COWL FAIRING AND EXHAUST SYSTEM FOR EVIDENCE OF FOD. NO DISCREPANCIES WERE NOTED. THE OIL FILTERS AND MAG CHIP DETECTORS WERE ALSO CHECKED WITH NO DISCREPANCIES NOTED. TROUBLESHOOTING PROCEDURES INDICATED THE REPLACEMENT OF THE BVCU, WHICH WAS ACCOMPLISHED. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2001082000167 20010820 00167 NM 2001 8 20 USAABB01059 1 20010710 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 624AU 27245 BOS - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 18 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001082000168 20010820 00168 NM 2001 8 20 USAABB01060 1 20010711 A 7500 285T111515 CIRCUIT BOARD BOEING 767 7672B7 1385107 NM LT ENGINE FAULTY A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 653US 24894 PHL - FLT 14 - AFTER TAKEOFF FROM PHL, THE LEFT ENGINE BLEED LIGHT ILLUMINATED WITH SELECTION OF ENGINE ANTI-ICE. THE D UCT PRESSURE DECREASED TO FIVE PSI. THE PRESSURE RETURNED TO NORMAL WITH THE ANTI-ICE OFF. DUE TO DESTINATION WEATHER CONDITIONS, THE FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE COULD NOT DUPLICATE THE CONDITI ON ON THE GROUND. THE LEFT ENGINE BLEED CARD WAS REPLACED AS A PRECAUTION. VERIFICATION FLIGHT WAS FLOWN WITH NO FURTH ER PROBLEMS. (M) 2 L 7 2 4F RT A1NM 2001082000169 20010820 00169 NM 2001 8 20 USAABB01062 1 20010713 A 3350 86210066REV9 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 604AU 22199 BWI - FOUND LOW LEVEL EMERGENCY LIGHTS AT ROWS 6 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2001082000170 20010820 00170 NM 2001 8 20 USAABB01063 1 20010713 A 3350 873100151REV9 LIGHT BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 604AU 22199 BWI - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 18 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001082000171 20010820 00171 EU 2001 8 20 USAAF01049 1 20010717 A 3810 660709 TIMER FOKKER F28 F28MK0100 4990807 EU LAVATORY MALFUNCTIONED A USAA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 EA 19 897US 11392 STL-PIT - FLT 9281 - SLIGHT FUMES WERE NOTICED COMING FROM BOTH LAVATORIES, AND SMOKE DETECTORS ACTIVATED FOR A BRIEF TI ME DURING CRUISE FLIGHT. FLIGHT LANDED IN PIT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT AND RIGHT LAVATORY F AUCET TIMERS. LEAK CHECKED AND OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT 2001082000172 20010820 00172 EU 2001 8 20 USAASA01031 1 20010630 A 3350 CONNECTOR AIRBUS A319 A319112 EU L1 DOOR LOOSE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 721UW 1095 PIT - THE EMERGENCY LIGHTS TEST FAILED ON THE WEEKLY CHECK. MAINTENANCE SECURED A LOOSE CONNECTOR ON THE L1 DOOR SLIDE. THE SYSTEM TESTED OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2001082000173 20010820 00173 EU 2001 8 20 USAASA01033 1 20010709 A 3350 32145510 POWER SUPPLY AIRBUS A319 A319112 EU CABIN FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 717UW 5433 1069 PHL - THE LEFT EMERGENCY POWER SUPPLY UNIT FAULTED. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2001082000174 20010820 00174 EU 2001 8 20 USAASA01034 1 20010712 A 3350 32145510 POWER SUPPLY AIRBUS A319 A319112 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 700UW 3135 885 PIT - THE FORWARD EMERGENCY POWER SUPPLY UNIT FAILED THE EMERGENCY LIGHT SYSTEM TEST. MAINTENANCE REPLACED THE FORWARD EMERGENCY POWER SUPPLY UNIT. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2001082000175 20010820 00175 EU 2001 8 20 USAASA01035 1 20010714 A 3350 CONTACTOR AIRBUS 320 A320* EU L4 DOOR OUT OF ADJ A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 174US 1492 PHL - THE 4L EXIT DOOR EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE ADJUSTED THE CONTACTS IN THE LIGHT ASSEMB LY. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A46NM 2001082000176 20010820 00176 EU 2001 8 20 USAASA01036 1 20010718 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319112 EU CABIN FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 738US 2935 1254 CLT - RECEIVED 'EPSU INT LOAD EMER L' MESSAGE ON THE CABIN INTERCOMMUNICATIONS DATA SYSTEM DURING THE EMERGENCY LIGHTS T EST. MAINTENANCE REPLACED AN EMERGENCY POWER SUPPLY UNIT (11WL). OPS CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2001082000177 20010820 00177 NM 2001 8 20 USAASB01191 1 20010705 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 428US 24550 ALB - DURING OPERATIONAL TEST OF EMERGENCY LIGHTS, MAINTENANCE FOUND THE FORWARD SERVICE DOOR EMERGENCY LIGHTS WENT INOP ERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK (P/N 2013-1A) WITH NO HELP. REMOVED AND REPLACED THE CHARGE R ASSEMBLY. SYSTEM NOW OPERATIONALLY CHECKS GOOD. (M) 2 L 7 2 4F RT A16WE 2001082000178 20010820 00178 NM 2001 8 20 USAASB01198 1 20010712 A 3350 30043229 SOCKET BOEING 737 7373B7 1384580 NM EXTERIOR CORRODED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 505AU 23380 EWR - MAINTENANCE FOUND THE FORWARD MAIN ENTRY DOOR EXTERIOR EMERGENCY EVACUATION LIGHT INOPERATIVE. MAINTENANCE CLEANE D CORROSION FROM THE LIGHT SOCKET. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001082000179 20010820 00179 NM 2001 8 20 USAASB01199 1 20010710 A 3350 3004321 LIGHT BOEING 737 7373B7 1384580 NM EXTERIOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 521AU 23856 EWR - FOUND AFT GALLEY DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A16WE 2001082000180 20010820 00180 NM 2001 8 20 USAASB01205 1 20010717 A 3397 WIRE BOEING 737 7373B7 1384580 NM CABIN DAMAGED A K NONE L NO TEST IN INSP/MAINT 1 EA 19 505AU 23380 EWR - MAINTENANCE FOUND THE LAST ROW OF LOW LEVEL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPAIRED THE WIRING. OPS C HECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001082000181 20010820 00181 NM 2001 8 20 USAASB01207 1 20010718 A 3350 6104789 BATTERY PACK BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 274AU 22886 TPA - AFT LEFT AND RIGHT EVACUATION SLIDE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT B ATTERY PACKS. (M) 2 L 7 2 4F A16WE 2001082000182 20010820 00182 CE 2001 8 20 0014 1 20010814 A 5311 1014300263 FRAME BEECH 200 200BEECH 1152920 CE FUSELAGE CRACKED E CIEA K NONE O OTHER IN INSP/MAINT 1 NM 03 69PD 16205 BB58 DURING COMPLIANCE OF THE 15,000 RECURRING STRUCTURAL INSPECTION, A CRACK WAS FOUND IN THE RIGHT FUSELAGE FRAME AT FS 207 .125, AT APPROXIMATELY WL 99.0. THE CRACK WAS APPROXIMATELY .75 INCH LONG AND STARTS AT A PEAR SHAPED LIGHTENING HOLE A ND EXTENDS IN AN UPWARD DIRECTION. 1 L 7 2 4T A24CE 2001082000185 20010820 00185 WP 2001 8 20 01FDEA00634 1 20010801 A 3260 WARNING SYSTEM DOUG DC10 DC1030F 3023504 WP COCKPIT MALFUNCTIONED A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 313FE 48311 ON T/O FROM ALT RED LIGHT ON LMG STAYED ON. RAN RED TAB PROC, LIGHT STAYED ON. NO FAULT FOUND SWAPPED PILOTS DISPLAY P LUG ON PROX BOX TO ALTERNATE POS, A/C DISPATCH IAW MEL 32-8C. 2 L 7 3 4F RT A22WE 2001082000188 20010820 00188 NM 2001 8 20 01FDEA00680 1 20010811 A 2120 656E DUCT BOEING 727 727225 1384077 NM A/C BAY LEAKING A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SO 25 461FE 22548 LWR BODY O/H LIGHT ILLUM. REMOVED AND REPLACED NR 2 PACK DUCT. LEAK CHECK GOOD. 2 L 7 3 4F A3WE 2001082000189 20010820 00189 WP 2001 8 20 01FDEA00737 1 20010815 A 5320 AEA720343 SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 053FE 47807 MAIN CABIN FLOORBEAM SUPPORT CRACKED AT BS 1259, LBL 83. 2 L 7 3 4F A22WE 2001082000190 20010820 00190 NM 2001 8 20 01FDEA00738 1 20010816 A 2120 DUCT BOEING 727 727233 138408A NM E/E BAY KINKED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 257FE 20939 NO RACK COOLING LIGHT ILLUM. REPOSITIONED KINKED DUCT PER MM 21-58-001. 2 L 7 3 4F RT A3WE 2001082800143 20010828 00143 NM 2001 8 28 01FDEA00739 1 20010720 A 5311 FRAME BOEING 727 727247 138408F NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 FUSELAGE FRAME BS 600 UPPER FLANGE HAS DENTS FROM STR 23L TO MIDPOINT STR 24L AND 25L. REMOVED AND REPLACED FRAME PER SR M 51-40-3. 2 L 7 3 4F A3WE 2001082000192 20010820 00192 NM 2001 8 20 AWXA0002012 1 20010714 A 5311 6516300302 FRAME BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 RIGHT BS 178 CHORD CRACKED AT WL 207 RBL 24. REMOVED AND REPLACED CHORD IAW ER 15-5311-01185-SS1. 2 L 7 2 4F RT A16WE 2001082000193 20010820 00193 NM 2001 8 20 AWXA0002019 1 20010707 A 5230 65C80735182 DOOR FRAME BOEING 737 737277 1384570 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 FWD CARGO DOOR LOWER CORNER FRAME CRACKED AT AFT LOWER STOP FITTING. REMOVED AND REPLACED LOWER AFT CORNER FRAME AT FWD CARGO DOOR IAW EO 52-31-04. 2 L 7 2 4F RT A16WE 2001082000194 20010820 00194 NM 2001 8 20 AWXA0002021 1 20010711 A 5312 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 FWD PRESSURE BULKHEAD BS178 CENTER WEB CRACKED RBL 5 & 7 WL 195 AND 210. REPAIRED PER SRM 83-10-08. 2 L 7 2 4F RT A16WE 2001082000195 20010820 00195 NM 2001 8 20 AWXA0002023 1 20010711 A 5320 651758351 STIFFENER BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 LBL 5.7 WL 182 VERTICAL CHORD IS CRACKED BS 178. ACCOMPLISHED REPAIR PER SRM 53-10-08. 2 L 7 2 4F RT A16WE 2001082000196 20010820 00196 NM 2001 8 20 AWXA0002024 1 20010711 A 5311 65163006301 FRAME BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 BS 178 LT SIDE CHORD IS CRACKED AT WL 204 LBL 27. REMOVED AND REPLACED SIDE CHORD PER SRM 51-10-2. 2 L 7 2 4F RT A16WE 2001082000197 20010820 00197 NM 2001 8 20 AWXA0002029 1 20010708 A 5315 654581099 FLOORBEAM BOEING 737 73733A 1384673 NM FUSELAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 STA 312 FLOORBEAM HAS NON SRM REPAIR. REPAIRED PER SRM 53-10-51. 2 L 7 2 4F RT A16WE 2001082000198 20010820 00198 NM 2001 8 20 AWXA0002031 1 20010712 A 5330 6546881 SKIN BOEING 737 73733A 1384673 NM FUSELAGE DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 DEEP DENT IN FUSE SKIN BS 1074 LBL 8. REPAIRED PER SRM 53-00-01 FIG 202. 2 L 7 2 4F RT A16WE 2001082000199 20010820 00199 NM 2001 8 20 AWXA0002032 1 20010705 A 5330 6546881 SKIN BOEING 737 73733A 1384673 NM FUSELAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 CREASE IN FUSELAGE SKIN BS 1120 LT STR 14L. REPAIRED PER SRM 53-00-01 FIG 202. 2 L 7 2 4F RT A16WE 2001082000200 20010820 00200 NM 2001 8 20 AWXA0002035 1 20010716 A 5330 6545688585 SKIN BOEING 737 73733A 1384673 NM FUSELAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 KEEL SKIN HAD 2 TEMPORARY REPAIRS STA 661 TO 726.5. REMOVED AND REPLACED SKIN PER AWA ER 03-5331-01193-SS1. 2 L 7 2 4F RT A16WE 2001101200107 20011012 00107 NM 2001 10 12 AWXA0002036 1 20010721 A 2611 100064901 SMOKE DETECTOR BOEING 737 7373G7 1384595 NM CARGO BAY FAULTY A AWXA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 155AW 2119 23777 AIR TURNBACK, AFTER TAKEOFF THE AFT CARGO COMPARTMENT FIRE WARNING LIGHT ILLUMINATED WITH ASSOCIATED AURAL WARNING. THE CREW DISCHARGED THE NR 1 FIRE EXTINGUISHER AFTERWARDS THE FIRE INDICATION WAS STILL PRESENT. THE ACFT WAS 15 MIN OUT A ND RETURNED TO PHX LANDING WITHOUT INCIDENT. THE FIRE DEPT MET THE ACFT AND DETERMINED THERE WAS NO FIRE OR SMOKE. DUE TO THE SERIOUS NATURE OF THIS INCIDENT THE FOLLOWING COMPONENTS WERE REPLACED NR 1 THRU NR 7 AFT SMOKE DETECTOR UNITS, CENTRAL CONTROL UNIT, DIVERTER VALVE, METERING VALVE AND BOTH FIRE BOTTLES (DUE TO DISCHARGE). TWO SMOKE DETECTOR UNITS HAD BAD SENSORS. SMOKE DETECTOR UNIT - MFG: SECURAPLANE - P/N: 100-0649-01 - S/N 9190, TT 169 - TC 114. 2 L 7 2 4F RT A16WE 2001082000201 20010820 00201 NM 2001 8 20 AWXA0002043 1 20010723 A 2910 AS11504K0232 HYDRAULIC LINE BOEING 757 757225 1384959 NM RT MLG LEAKING A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 28 915AW 22209 LAS- UNSCHEDULED LANDING- FLT 46 - AFTER DEPARTURE FROM FLL EN ROUTE TO LAS THE AIRCRAFT LOST LEFT HYDRAULIC SYSTEM QUAN TITY AND DIVERTED TO MCO. THE AIRCRAFT MADE AN UNEVENTFUL, OVER WEIGHT LANDING (231,000LBS). IN MCO MAINTENANCE TROUBL ESHOT AND FOUND A RT MAIN LANDING GEAR DOWNLOCK LINE LEAKING. THE LINE WAS REPLACED. THE HYDRAULIC PUMP CASE DRAIN FIL TERS WERE REMOVED AND INSPECTED, FILTERS WERE CLEAN. NEW FILTERS WERE INSTALLED AND THE HYDRAULIC SYSTEM SERVICED AND L EAK CHECKS PERFORMED. NO FURTHER LEAKS WERE NOTED. AN OVERWEIGHT LANDING INSPECTION WAS PERFORMED PER AWA TASK CARD I8 M51601 WITH NO DISCREPANCIES NOTED. 2 L 7 2 4F RT A2NM 2001082000202 20010820 00202 EU 2001 8 20 AWXA0002044 1 20010723 A 3240 NAS16128 PACKING MESSIER AIRBUS 320 A320232 3930326 EU PARK BRAKE VALVE DAMAGED A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 652AW H2314 0953 BDL- EMERGENCY LANDING - FLT 402 - EN ROUTE FROM PHX RO BDL THE CREW FOUND YELLOW HYDRAULIC QUANTITY DECREASING AND TURN ED THE YELLOW SYSTEM HYD PUMP OFF PRIOR TO GETTING A RESERVOIR LOW LEVEL WARNING. ON APPROACH THE YELLOW HYD SYSTEM WAS LOST AND THE CREW CALLED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT. TECHNICIANS WERE SENT FROM CMH TO BDL TO TROUBLESHOOT. FOUND THE MIDDLE AND LOWER PACKINGS ON THE PARKING BRAKE VALVE BROKEN/CUT. THE PACKINGS WERE REPLACED, THE HYD SYSTEM SERVICED AND SYSTEM LEAK CHECKS PERFORMED USING BOTH THE ELECTRIC PUMP AND ENGINE DRIVEN HYD PUMP. NO FU RTHER LEAKS WERE FOUND. 2 L 7 2 4F RT A28NM 2001082000203 20010820 00203 NM 2001 8 20 AWXA0002045 1 20010711 A 5311 6516300301 FRAME BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 BS 178 PRESSURE BULKHEAD LEFT HAND CHORD CRACKED AT WL 195 AFT SIDE IN RADIUS. REMOVED AND REPLACED LEFT HAND CHORD AT BS 178 (P/N 65-16300-301) IAW ER 15-5311-01186-SS2. 2 L 7 2 4F RT A16WE 2001082000204 20010820 00204 NM 2001 8 20 AWXA0002046 1 20010718 A 5753 113N35002 FLAP BOEING 757 757225 1384959 NM LT WING CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 LEFT O/B FORE FLAP LEADING EDGE I/B AREA WS 397-438 HAS SEVERAL CHAFED MARKS. BLENDED OUT CHAFED AREAS, ORIG MAT .080-M AT LOSS .020, OUT OF LIMITS, CUT OUT DAMAGE. FABBED REPAIR PLATE DOUBLERS AND STRAPS IAW SRM 57-33-01. INSTALLED PARTS IAW SRM 57-53-01 FIG 202. 2 L 7 2 4F RT A2NM 2001082000205 20010820 00205 NM 2001 8 20 AWXA0002049 1 20010723 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 FS 395 STR 21-L EXTERNAL DOUBLER NOT PER SRM. REMOVED EXISTING REPAIR DOUBLER. FABRICATED AND INSTALLED REPAIR DOUBLER PER AWA ER 19-5331-01198-SS1. 2 L 7 2 4F RT A2NM 2001082000206 20010820 00206 NM 2001 8 20 AWXA0002059 1 20010716 A 5320 6720382 INTERCOSTAL BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 BS 178 BULKHEAD, RT INTERCOSTAL CRACKED, WL 195, RBL 23. REMOVED AND REPLACED RT INTERCOSTAL AT BS 178, WL 195, RBL 23 IAW B737 SRM 51-30-2 PG 2-3. 2 L 7 2 4F RT A16WE 2001082000207 20010820 00207 NM 2001 8 20 AWXA0002060 1 20010716 A 5320 6720381 INTERCOSTAL BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 LT INTERCOSTAL CRACKED, LBL 24, WL 195, AFT SIDE BELOW FLOOR, BS 178 BULKHEAD. REMOVED AND REPLACED LT INTERCOSTAL IAW B737 SRM 51-30-2 PG 2 AT LBL 24, WL 195, BS 178. 2 L 7 2 4F RT A16WE 2001082000208 20010820 00208 NM 2001 8 20 AWXA0002063 1 20010710 A 5315 6623737 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 BS 725 BL 24LT SEAT TRACK LOWER ATTACH FLANGE CRACKED. REMOVED CRACK FROM SEAT TRACK LOWER ATTACH FLANGE, INSTALLED REP AIR ON SEAT TRACK LOWER ATTACH FLANGE IAW ER 15-5715-01202-DL3. 2 L 7 2 4F RT A16WE 2001082000209 20010820 00209 NM 2001 8 20 AWXA0002068 1 20010706 A 5315 BAC1518399 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 CORROSION ON FLOOR BS 947 RBL 43.0 TOP AND BOTTOM OF UPPER FLANGE. CUT OUT CORRODED SECTION OF BS 947 RBL 43 FLOORBEAM UPPER FLANGE. INSTALLED REPAIR IAW B737 SRM 53-10-9 FIG 3. 2 L 7 2 4F RT A16WE 2001082000210 20010820 00210 NM 2001 8 20 AWXA0002070 1 20010731 A 5311 6545409602 FRAME BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 BS 663.75 PRESSURE DECK COMPRESSION CHORD CRACKED AT LBL 24. REPAIRED COMPRESSION CHORD IAW AWA ER 15-5715-01195-SS2. 2 L 7 2 4F RT A16WE 2001082000211 20010820 00211 NM 2001 8 20 AWXA0002077 1 20010805 A 3230 65546004 CYLINDER BOEING 737 73733A 1384673 NM RT MLG FAULTY A AWXA O OTHER O OTHER AP APPROACH 1 WP 28 509DC 11473 23636 PHX-EMERGENCY LANDING -FLT 229- ON LANDING GEAR EXTENSION THE CREW HEARD A LOUD NOISE AND THE ACFT YAWED TO THE LEFT. A LL INDICATIONS WERE NORMAL AND ALL PRESSURE OK. AS A PRECAUTION THE CREW CALLED OUT EMERGENCY EQUIPMENT AND MADE AN UNE VENTFUL LANDING. MX JACKED THE ACFT AND PERFORMED GEAR SWINGS. THE RIGHT MAIN LANDING GEAR CAME OUT SLIGHTLY AFTER THE LEFT. THE RT MAIN LANDING TRANSFER CYLINDER WAS CHANGED DUE TO THE PISTON STICKING. THE RT HYD MODULE P/N 65-4469-5, S/N 3904 TTSN 44822:52 TCSN 29724 ALSO REPLACED AS A PRECAUTION. ALL FUNCTIONAL CHECKS WERE NORMAL. 2 L 7 2 4F RT A16WE 2001082000212 20010820 00212 NM 2001 8 20 AWXA0002078 1 20010804 A 5314 65621251 KEELBEAM BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 OIL CANNING AND LOOSE RIVETS ON KEEL BEAM PANEL BS 663-673. REPAIRED FASTENER HOLES IN KEEL BEAM CHORD AND REPAIRED PAN EL IAW AWA ER 155315-01215-DL3. 2 L 7 2 4F RT A16WE 2001082000213 20010820 00213 NM 2001 8 20 AWXA0002080 1 20010708 A 5311 651630086 FRAME BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 BULKHEAD 178 CHORD CRACKED AT WL 207 LT SIDE ABOVE AND BELOW FLOOR -NDT- CONFIRMED. LEFT LWR CHORD P/N 65-16300-86 REPL ACED PER REF DWG 65-16300 & SRM 51-30-2 PG 2-3. RESTORED SURFACE FINISH PER AWA 51-21-0 PG 1 & SRM 51-20-4 PG 4. 2 L 7 2 4F RT A16WE 2001082000214 20010820 00214 EU 2001 8 20 DHL2001365032 1 20010818 A 5200 FAIRING AIRBUS 300 A300B4203 3930306 EU A DHLA O OTHER O OTHER IN INSP/MAINT 1 SO 01 365DH 149 On weekly check discrepance-FWD Lower cargo door cutout lower fairing has cracks and gauges at several places.1) Cut out damaged (cracked) areas and fabricated fillers I.A.W. A-300-SRM 51-40-11.2) O.K. to treat, prime and install repair ins talled fillers at FWD. lower fairing I.A.W. A-300 SRM 5140-11.3) Treated and Primed fillers and backup plates I.A.W.-A30 0-SRM-51-40-12 before installing 2 L 7 2 4F RT A35EU 2001082000215 20010820 00215 NM 2001 8 20 AWXA0002083 1 20010708 A 5320 651758348 STIFFENER BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22654 BULKHEAD 178 VERTICAL CHORD AT LBL 5.7 CRACKED IN RADIUS AT WL 190 NDT CONFIRMED. REPAIRED PER REF SRM 53-10-11 FIG 8 S MT 1-20 HFEC PER 737 NDT PT.6 51-00-00. PARTS CAD PLATED ON WIP R445976 REPROTECT PARTS PER SRM 51-10-2. SEALED PER SR M 51-20-4 PG 4, INSTALLED REPAIR PARTS PER SRM 51-30-2 PGS 2-3 & 5. 2 L 7 2 4F RT A16WE 2001082000216 20010820 00216 NM 2001 8 20 AWXA0002090 1 20010731 A 5330 6549917 SKIN BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 LIGHT CORROSION ON SURFACE FOUND UNDERNEATH VHF ANTENNA COVER AT BS 777 & BL 0. CORROSION REMOVED PER SRM 53-30-1 FIG 1 PG 1. MADE AND INSTALLED NEW ANGLES PER DWG 65-49917 P/N 65-49917-11 AND 65-49917-12. INSTALLED NEW DOUBLERS AND FILL ER PER SRM 53-30-3 FIG 1 SHT 1-A & SRM 51-30-2 PG 2-3. 2 L 7 2 4F RT A16WE 2001082000217 20010820 00217 NM 2001 8 20 AWXA0002091 1 20010707 A 5312 65163007 BULKHEAD BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 INSP OF STA 178 BLKHD FWD FACE REVEALS SEVEN CRACK INDICATIONS. LOCATIONS ARE AS FOLLOWS LBL 8/WL 228, LBL 4/WL 216, RB L 12/WL 216, LBL 12/ WL 216, LBL 1/WL 200, RBL 1/WL187, & LBL 1/WL 187. REPAIRED PER ER NR 15-5313-01212-DD1 HFEC PER 7 37 NDT MAN, PT 6 51-00-00 REP SRM 51-30-2 PGS 2-3 & 5 SRM 51-20-4 PG 4 & PER MM 51-21-0 PG 1. 2 L 7 2 4F RT A16WE 2001082000218 20010820 00218 NM 2001 8 20 AWXA0002092 1 20010729 A 5312 65163007 BULKHEAD BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 NDT FOUND CRACKS AT BS 178 WL 222 LBL 3 AND BS 178 WL 222 RBL 3. DAMAGED REPAIRED PER ER 15-5313-01212-DD1. 2 L 7 2 4F RT A16WE 2001082000219 20010820 00219 NM 2001 8 20 AWXA0002093 1 20010801 A 5210 507945178 DOOR FRAME BOEING 737 737277 1384570 NM ENTRY DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 FWD ENTRY DOOR AFT FRAME AND INNER WEB CRACKED. REPAIRED DOOR AFT FRAME AS PER SRM 51-40-3 PG 1-6. REPAIRED DOOR WEB A S PER SRM 51-40-2 PG 1-3. 2 L 7 2 4F RT A16WE 2001082000220 20010820 00220 NM 2001 8 20 AWXA0002095 1 20010801 A 5330 65458061133 SKIN BOEING 737 737200 1384453 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 FWD ENTRY DOORWAY AFT LWR CORNER OF CUTOUT IS CRACKED. HFEC INSP OF HOLES ACCOMPLISHED PER 737 NDT MAN PT 6 51-00-00. ACCOMPLISHED SB 737-53-1083R FOG .2 & FIG 4. 2 L 7 2 4F A16WE 2001082000221 20010820 00221 NM 2001 8 20 AWXA0002096 1 20010803 A 5315 6545409602 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 CABIN FLOORBEAM AREA ANGLE CRACKED BS 663.75 RBL 24. REPAIRED BS 663 BEAM UPPER CHORD IAW AWA ER 15-5715-01195-SS2. 2 L 7 2 4F RT A16WE 2001082000222 20010820 00222 NM 2001 8 20 AWXA0002097 1 20010806 A 2810 L95F50603 RELIEF VALVE AIRBUS A319 A319132 NM LT WING TANK FRACTURED A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 825AW 400 1527 APPROX 30 MIN AFTER DEPARTURE A CENTER TANK AUTO FEED FAULT OCCURRED. LT MAIN FUEL QUANTITY WAS 1500 LBS LESS THAN THE RT SIDE. LT SIDE CONTINUED FEEDING WITH LT FUEL TANK PUMPS OFF. THE ACFT DIVERTED TO DFW. MX FOUND THE CENTER TANK TO LT TANK OVER PRESSURE PROTECTOR FRACTURED. THE OVER PRESSURE PROTECTOR WAS REPLACED. AFTERWARDS THERE WAS STILL A SLI GHT AMOUNT OF INCREASE RT TANK VS LT TANK WITH ENGINES RUNNING AND BOTH RT TANK PUMPS ON, X-FEED OPEN. WITH X-FEED CLOSE D OPERATION WAS NORMAL. MX REPLACED THE LT AIR RELEASE VALVE PER AMM 28-21-41. OPS CHECKS WERE GOOD. VALVE, AIR RELEASE - MFG: FLIGHT REFUELING LTD P/N: FRH 280002, S/N FR238BF - LOC: LT WING - COND : LEAKING T.T.: 400 - T.C. : 165 2 L 7 2 4F RT A28NM 2001082000223 20010820 00223 NM 2001 8 20 AWXA0002101 1 20010802 A 5320 654681291 FLOOR SUPPORT BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 AFT CABIN - CORROSION ON FLOOR SUPPORT BEAMS BETWEEN STN 1000-1010 LBL 45. REPLACED BOTH FLOOR SUPPORT PER DRAW 65-4681 2 PART NUMBER 65-46812-87 AND 65-46812-91 IAW SRM 51-10-1 PAGE 8, 9, 10. 2 L 7 2 4F RT A16WE 2001082000224 20010820 00224 NM 2001 8 20 AWXA0002104 1 20010811 A 5315 BAC1505100617 FLOORBEAM BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 903AW 23323 FWD CARGO COMPT STA 700 RBL 48 FLOORBEAM UPPER T-CAP VERTICAL LEG CRACKED. NDT VERIFIED CRACK, NDT VERIFIED CRACK REMOV ED, FABRICATED T-CHORD TO BAC 1505 - 1006 17/7077 R284269 FABRICATED SPLICES, INSTALLED ALL REPAIR PARTS PER SRM 53-00-5 1. 2 L 7 2 4F RT A2NM 2001082000225 20010820 00225 NM 2001 8 20 AWXA0002105 1 20010809 A 5330 146N3531 SKIN BOEING 757 7572S7 1384962 NM FUSELAGE CANNING A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 903AW 23323 LWR FUSELAGE SKIN AT STA 1590, BL 0 IS BULGED AT PREVIOUS REPAIR. REMOVED EXISTING REPAIR, FOUND SKIN TO BE OIL CANNED, CUT OUT DAMAGE FABBED DOUBLER, FILLERS AND SKINS. INSTALLED REPAIR PARTS IAW SRM 53-00-01 51-30-01-FIG 206. 2 L 7 2 4F RT A2NM 2001082000226 20010820 00226 NM 2001 8 20 AWXA0002108 1 20010731 A 5315 6546811 FLOORBEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 CORROSION ON FLOORBEAM BS 986.5 RBL 18 TO LBL 18. REMOVED AND REPLACED T-CHORD IAW B737 PER SRM 53-60-51 PGS 105-114. 2 L 7 2 4F RT A16WE 2001082000227 20010820 00227 EU 2001 8 20 AWXA0002110 1 20010814 A 5347 D53112092200 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 FR Y765 LT SEAT TRACK CORRODED. REPLACED SEAT TRACK NR 1 FROM FR 16 TO FR 20 AS PER SRM 53-11-15 PAGE 6. 2 L 7 2 4F RT A28NM 2001082000228 20010820 00228 NM 2001 8 20 AWXA0002112 1 20010810 A 5315 BAL1518338 FLOORBEAM BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 903AW 23323 CABIN FS 377.7 LBL 3 FLOORBEAM TOP T-CAP HAS CORROSION AT SCREW TOP AND BOTTOM SURFACE. REMOVED DAMAGED UPPER CHORD, FA BRICATED AND INSTALLED REPAIR PARTS (UPPER CHORD) PER SRM 53-00-51 FIG 203. 2 L 7 2 4F RT A2NM 2001082000229 20010820 00229 NM 2001 8 20 AWXA0002075 1 20010707 A 5315 65C1717313 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 LOWER T-CHORD CRACKED BS 717 BL 0 BELOW CABIN FLOOR. REPAIRED IAW AWA ER 15-5702-01209-DD2. 2 L 7 2 4F RT A16WE 2001082000230 20010820 00230 NM 2001 8 20 AWXA0002113 1 20010810 A 5315 BAC1505100617 FLOORBEAM BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 903AW 23323 FWD CARGO COMPT FBSTA 700 RBL 48 FLOORBEAM UPPER T-CAP VERTICAL LEG CRACKED. NDT VERIFIED CRACK, REMOVED CRACKED AREA, NDT VERIFIED CRACK REMOVED, FABRICATED T-CHORD TO BAC 1505-100617/ 7077 R 824269, FABRICATED SPLICES, AND INSTALLED ALL REPLACED PARTS PER SRM 52-00-51. 2 L 7 2 4F RT A2NM 2001082000231 20010820 00231 NM 2001 8 20 AWXA0002114 1 20010810 A 5320 143N526011 ANGLE BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 903AW 23323 FWD CARGO COMPARTMENT FBSTA 664/ INTERCOSTAL TOP FLANGE CRACKED BL 0. REMOVED L-ANGLE IAW SRM 51-40-02 PG 16, DRILLED N EW PART P/N 143N52601-1 R861987 PER SRM 51-10-02 PG 16. INSTALLED L-ANGLE IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2001082000232 20010820 00232 EA 2001 8 20 SWIA200110105 1 20010815 A 2120 FILTER CNDAIR CL600 CL6002B19 EA A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 423SW 7456 ON CLIMBOUT FROM SLC DISPLAY COOL MESSAGE APPEARED. WE FOLLOWED QRH AND SELECTED FLT ALT. WAITED 60 SECONDS, MESSAGE D ID NOT EXTINGUISH. QRH DIRECTED US TO TURN SW TO STDBY, MESSAGE EXTINGUISHED AT THAT TIME. WE CONTACTED MX THROUGH ATL RADAR AND WERE DIRECTED TO RETURN TO SLC.INSTALLED NEW FILTER FOR DISPLAY COOL SYSTEM. OPS CHECK GOOD IN NORM, FLT ALT , GND ALT. 2 L 7 2 4F RT A21EA 2001082000233 20010820 00233 WP 2001 8 20 AALA20011394 1 20010709 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 214AA 49162 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 21 INOPERATIVE. RE-SEATED EMERGENCY EXIT LIGHT CONNECT OR AT SEAT 21. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001082000234 20010820 00234 WP 2001 8 20 AALA20011395 1 20010709 A 3350 SOCKET DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 73444 49470 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 9D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET A T SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001082000235 20010820 00235 WP 2001 8 20 AALA20011397 1 20010707 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 203AA 49145 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUN D CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001082000236 20010820 00236 WP 2001 8 20 AALA20011398 1 20010710 A 3350 SOCKET DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70425 49337 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 18 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET A T SEAT 18. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001082000237 20010820 00237 WP 2001 8 20 AALA20011458 1 20010722 A 3350 8039001 BATTERY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 244AA 49256 DFW - DURING OVERNIGHT MAINTENANCE, CEILING MOUNTED EMERGENCY EXIT LIGHT AT ROW 15 INOPERATIVE. REPLACED CEILING MOUNTE D EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001082000238 20010820 00238 WP 2001 8 20 AALA20011459 1 20010720 A 3350 8039001 BATTERY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 452AA 49553 DFW - DURING OVERNIGHT MAITNENANCE, CEILING MOUNTED EMERGENCY EXIT LIGHT AT ROW 13 THROUGH 16 INOPERATIVE. REPLACED CEI LING MOUNTED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001082000239 20010820 00239 WP 2001 8 20 AALA20011437 1 20010722 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 478AA 49653 DFW - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK TO CEILING EMERGEN CY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001082000240 20010820 00240 WP 2001 8 20 AALA20011440 1 20010718 A 3350 P4010049 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS OVERHEAD EMERGENCY EXIT LIGHTING INOPERATIVE. REPLACED BATTERY PACK TO FIRST CLASS EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001121300041 20011213 00041 WP 2001 12 13 AALA20011465 1 20010718 A 3350 CHARGER DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 418AA 49329 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIR DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGH T BATTERY CHARGER AT AFT AIRSTAIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001082000241 20010820 00241 WP 2001 8 20 AALA20011461 1 20010720 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 241AA 49254 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOD LIGHT ROW 7 THROUGH 11 INOPERATIVE. REPLACED EMERGENCY EXIT FL OOD LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001082000242 20010820 00242 WP 2001 8 20 AALA20011453 1 20010719 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 403A 49314 LAX - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHTS SEATS ROW 1 THROUGH 20 DIM. SPLICED WIRES TO EME RGENCY EXIT LIGHTS AT ROW 13. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001082000243 20010820 00243 WP 2001 8 20 AALA20011432 1 20010715 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7530 49922 DFW - DURING OVERNIGHT MAINTENANCE, RIGHT AFT OVERWING EMERGENCY ESCAPE PATH LIGHT DIM. REPLACED BATTERY FOR RIGHT AFT OVERWING EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001082000244 20010820 00244 WP 2001 8 20 AALA20011433 1 20010717 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 586AA 53249 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS STATION 140 TO 213 DIM. REPLACED BATTERY PACK FOR EMERGENCY EXIT ESCAPE PATH LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001082000245 20010820 00245 WP 2001 8 20 AALA20011427 1 20010716 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AA 49293 DFW - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY EXIT CEILING LIGHTS STATION 1133 TO 1209 INOPERATIVE. REPLACED BATT ERY PACK FOR EMERGENCY EXIT CEILING LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001082000246 20010820 00246 WP 2001 8 20 AALA20011429 1 20010716 A 3350 AB51 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 437AA 49455 DFW - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY L IGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001082000247 20010820 00247 WP 2001 8 20 AALA20011425 1 20010717 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 494AA 49732 ORD - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT CEILING LIGHTS IN AFT SECTION INOPERATIVE. REPLACED BATTERY PACK FOR AFT EMERGENCY EXIT CEILING LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001121300040 20011213 00040 WP 2001 12 13 AALA20011426 1 20010716 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 271AA 49293 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT CEILING LIGHTS STATION 642 TO 755 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT CEILING LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001082000248 20010820 00248 2001 8 20 AALA20011116 4 20010516 A 3100 D22501000 HARNESS AIRBUS 300 A300B4605R 3930308 EU WHEEL WELL DAMAGED A AALA K NONE N FALSE WARNING AP APPROACH 1 SW 21 59081 639 JFK - - FLT 1384 - EN ROUTE BGI-JFK, LEFT AND RIGHT MAIN LANDING GEAR INDICATED NO GREEN ARROW WHEN GEAR LOWERED. REPAI RED MAIN LANDING GEAR ELECTRICAL HARNESS AND REPLACED INOPERATIVE SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2001082000249 20010820 00249 NM 2001 8 20 AALA20011363 1 20010705 A 3350 PIN BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 928AN 29528 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 19 INOPERATIVE. RE-SEATED EMERGENCY EXIT LIGHT CONNECT OR PIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2001082000250 20010820 00250 NM 2001 8 20 AALA20011325 1 20010630 A 3350 CONNECTOR BOEING 737 737823 13844BZ NM COCKPIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 948AN 30086 LAX - DURING OVERNIGHT MAINTENANCE, COCKPIT EMERGENCY EXIT DOME LIGHT INOPERATIVE. RE-SEATED COCKPIT EMERGENCY EXIT DOM E LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2001082000251 20010820 00251 NM 2001 8 20 AALA20011375 1 20010706 A 2500 D31038201 SLIDE BOEING 767 767223 1385123 NM R1 DOOR INOPERATIVE A AALA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 324AA 22325 LAX - FLT 3 - UPON ARRIVAL, R1 DOOR INADVERTENTLY DEPLOYED. SLIDE PARTIALLY DEPLOYED. REPLACED R1 DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001082000252 20010820 00252 NM 2001 8 20 AALA20011396 1 20010709 A 2170 5723863 PACKING BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 386AA 27060 DFW - FLT 1539 - EN ROUTE MIA-SFO, DETECTED WATER COMING DOWN AT CENTER OF CABIN. TURNED OFF ALL VIDEO MONITORS. DIVER TED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED LEFT WATER EXTRACTOR PACKING. LEAK CHECKS GOOD. SYSTEM GROUND C HECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001082000253 20010820 00253 EA 2001 8 20 MASA01072 1 20010718 A 3350 5925720131A POWER SUPPLY CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37228 7228 FLT 5891 - CLT - EXPERIENCED FLOOR TRACK LIGHTS 2 THROUGH 5 WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NR 2 INVERTER AND THE POWER SUPPLY. OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001082000254 20010820 00254 WP 2001 8 20 USAA010951 1 20010728 A 5200 DOUBLER DOUG DC9 DC981 3022081 WP CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 808US 53979 48040 PIT - FOUND DOUBLER/ANGLE CRACKED .75 INCH, AFT PSG CABIN DOOR JAMB, LEFT UPPER FRAME. REMOVED DOUBLER, INSTALLED DOUBL ER ANGLE PER SRM 53-05 FIG 30A. (M) 2 L 7 2 4F A6WE 2001082000255 20010820 00255 EU 2001 8 20 USAAF01058 1 20010728 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU PAX CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 859US 11293 GSO - THE EMERGENCY MARKER LIGHTS IN THE ENTRY AREA WOULD NOT ILLUMINATE. MAINTENANCE REPLACED THE NR 1 BATTERY PACK. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT 2001082000256 20010820 00256 EU 2001 8 20 USAA010934 1 20010725 A 5300 FRAME FOKKER F28 F28MK0100 4990807 EU FS 21736 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 857US 27063 11289 PIT - FOUND FRAME CRACKED 4 INCHES, FS 21736 BETWEEN STRINGER 3 AND THROUGH UPPER C-CHANNEL. INSTALLED TWO REPAIR ANGLE S PER EA 71597. (M) 2 L 7 2 4F RT 2001082000257 20010820 00257 EU 2001 8 20 USAAF01051 1 20010724 A 2600 892480 EXTINGUISHER FOKKER F28 F28MK0100 4990807 EU PAX CABIN DISCHARGED A USAA F ACTIVATE FIRE EXT. N FALSE WARNING NR NOT REPORTED 1 EA 19 897US 11392 CLT-IND - FLT 476 - THE WATER FIRE EXTINGUISHER DISCHARGED INTO THE LAVATORY TRASH BIN IN FLIGHT. NO SMOKE OR FIRE WAS DETECTED. THE FLIGHT LANDED WITHOUT INCIDENT IN IND. MAINTENANCE REPLACED THE WATER BOTTLE EXTINGUISHER. OK FOR SERVI CE. (M) 2 L 7 2 4F RT 2001082000258 20010820 00258 EU 2001 8 20 USAAF01052 1 20010725 A 2500 D31873101 SLIDE FOKKER F28 F28MK0100 4990807 EU PAX CABIN A USAA O OTHER O OTHER IN INSP/MAINT 1 EA 19 854US 11282 PIT - DURING THE A-CHECK, THE FORWARD RIGHT EXIT DOOR SLIDE GIRT BAR WAS FOUND UNATTACHED TO THE SLIDE GIRT. MAINTENANC E ATTACHED THE SLIDE GIRT BAR. OK FOR SERVICE. (M) 2 L 7 2 4F RT 2001082000259 20010820 00259 EU 2001 8 20 USAA010811 1 20010607 A 5300 SKIN FOKKER F28 F28MK0100 4990807 EU BS 24011/24611 DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 868US 11313 PIT - FOUND SKIN DELAMINATED 10 INCHES BY 12 INCHES, LEFT AND RIGHT LAVATORIES, STATION 24011 AND 24611 STRINGER 51 AND 53. INSTALLED RIVETS IN LEFT AND RIGHT LAVATORIES PER EA. (M) 2 L 7 2 4F RT 2001082000260 20010820 00260 EU 2001 8 20 USAA010802 1 20010701 A 5300 SKIN FOKKER F28 F28MK0100 4990807 EU BS 27026-27526 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 857US 27063 11289 PIT - FOUND SKIN WITH HEAT DAMAGE 8 INCH BY 12 INCH AREA, STATION 27026-27526 STRINGER 46-50. REMOVED HEAT DAMAGE, INST ALLED REPLACEMENT SKIN/DOUBLER PER EA 54649 AND TYP REPAIR 53-40-01. (M) 2 L 7 2 4F RT 2001082000261 20010820 00261 EU 2001 8 20 USAA010799 1 20010714 A 5300 BEAM FOKKER F28 F28MK0100 4990807 EU BS 22516-26026 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 860US 26975 11295 PIT - FOUND APU INLET RIGHT BEAM WITH HOLE 2.5 INCHES BY 4 INCHES APU AIR INLET BEAM, FUSELAGE RIGHT STATION 22516-26026 . MANUFACTURED REPAIR SPLICE AND CORNER BRACKET RIGHT SIDE APU INLET SCOOP PER EA. (M) 2 L 7 2 4F RT 2001082100001 20010821 00001 WP 2001 8 21 RRXA11387 1 20010630 A 5340 SRC8530021 DOUBLER DOUG DC8 DC873F 302199F WP STA 160 L11R CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND FUSELAGE EXT SKIN FWD UPPER CORNER OF R/H FWD SERVICE DOOR JAMB IS CRACKED 4 FASTENERS STA 160 L11R - L12R. *** CORRECTIVE ACTION *** REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PART AND INSTALLED IAW 53-2 -0 FIG 14. 2 L 7 4 4F RT 4A25 2001082100002 20010821 00002 WP 2001 8 21 RRXA11388 1 20010701 A 5511 565450181 STIFFENER DOUG DC8 DC873F 302199F WP HORIZ STAB R/H CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND CRACKED STIFFENER AT IN R/H HORIZ STAB AT XFS 60. *** CORRECTIVE ACTION *** REMOVED, F ABRICATED AND REPLACED CRACKED STIFFENER. 2 L 7 4 4F RT 4A25 2001082100003 20010821 00003 WP 2001 8 21 RRXA11390 1 20010702 A 5310 4758514U511 FITTING DOUG DC8 DC873F 302199F WP STA 1260 L33R CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND C-PIT FITTING AFT SIDE OF STA 1260 L33R IS CRACKED. *** CORRECTIVE ACTION *** REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0 2 L 7 4 4F RT 4A25 2001082100004 20010821 00004 WP 2001 8 21 RRXA11392 1 20010702 A 5710 463662U501 CLAMP DOUG DC8 DC873F 302199F WP RH WG XRS761 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND R/H WING O/B L/E STA XRS 761 PNEUMATIC DUCT LOWER BRACKET CRACKED, FOUND 2 NUT PLATE BR OKEN. *** CORRECTIVE ACTION *** REMOVED AND REPLACED NUT PLATES, REMOVED AND REPLACED BRACKETS IAW SRM 51-1-21 AND 51- 30 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2001082100005 20010821 00005 WP 2001 8 21 RRXA11393 1 20010702 A 5310 6141605 FRAME DOUG DC8 DC873F 302199F WP STA 55 L24R CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND FUSELAGE FRAME STA 55 CRACKED AT L24R. *** CORRECTIVE ACTION *** REPAIRED FRAME AT STA 55 BETWEEN L21R TO BETWEEN L26R AND L27R IAW SRM 53-3-3 FIG 3 2 L 7 4 4F RT 4A25 2001082100006 20010821 00006 WP 2001 8 21 RRXA11394 1 20010703 A 5310 4758514517 FITTING DOUG DC8 DC873F 302199F WP STA 1160 L33R CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND C-PIT FITTING FWD OF STA 1160 AT L33R I/B IS CRACKED. *** CORRECTIVE ACTION *** REMOVE D FITTING IAW DC-8 SRM 51-1-20D 751-1-21, FABRICATED REPLACEMENT FITTING IAW DC8 DWG 4758514. INSTALLED REPLACEMENT FI TTING IAW DC8 SRM51-1-20D 2 L 7 4 4F RT 4A25 2001082100007 20010821 00007 WP 2001 8 21 RRXA11395 1 20010703 A 5310 26499432N CLIP DOUG DC8 DC873F 302199F WP STA 159 L21L CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND FRAME TO CUSP CLIPBROKEN STA 159 L21L INSIDE TORQUE BOX. *** CORRECTIVE ACTION *** REM OVED AND REPLACED CLIP IAW DC8 SRM 51-1-20D AND 51-1-8 2 L 7 4 4F RT 4A25 2001082100008 20010821 00008 WP 2001 8 21 RRXA11396 1 20010703 A 5210 4640272 ATTACH FITTING DOUG DC8 DC873F 302199F WP STA 159 L21L CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND R/H SERVICE DOOR LWR HINGE ATTACH FITTING STA 159 CRACKED. *** CORRECTIVE ACTION *** R EMOVED AND REPLACED FITTING IAW SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001082100009 20010821 00009 WP 2001 8 21 RRXA11397 1 20010704 A 5310 54755395 SEAT TRACK DOUG DC8 DC873F 302199F WP STA 1080 L13 L48 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND CORREDED SEAT TRACK STA 1080 L13 - L48. *** CORRECTIVE ATION *** SPLICED SEAT TRACK ST A 1060 - STA 1120 L13 - L48. INSTALLED REPLACEMENT PART IAW SRM 53-7-3 FIG 3D AND 53-2-3 FIG 14 AND 51-3-0. 2 L 7 4 4F RT 4A25 2001082100010 20010821 00010 WP 2001 8 21 RRXA11399 1 20010705 A 5720 5769589 RIB DOUG DC8 DC873F 302199F WP RT WG XFS 710 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND R/H O/B L/E UPPER RIB STA XFS 710 CRACKED. *** CORRECTIVE ACTION *** INSTALLED DOUBLER PER SRM 57-2-0 2 L 7 4 4F RT 4A25 2001082100011 20010821 00011 WP 2001 8 21 RRXA11400 1 20010706 A 5300 37729161 FITTING DOUG DC8 DC873F 302199F WP STA 140 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND MAIN CARGO DOOR LATCH FITTING BACK-UP FITTING CRACKED BELOW CUSP ANGLE STA 140 AND CUSP JOINT TO LBL 48. *** CORRECTIVE ACTION *** REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 3772916 AND DC8 SRM 51-1 -20D AND 53-1-0 2 L 7 4 4F RT 4A25 2001082100012 20010821 00012 WP 2001 8 21 RRXA11401 1 20010701 A 5310 3758467IN FITTING DOUG DC8 DC873F 302199F WP STA 1140 L35L CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND C-PIT AFT SIDE OF STA 1140 L35L FITTING CRACKED. *** CORRECTIVE ACTION *** REMOVED CRA CKED FITTING PER SRM 51-1-20 AND INSTALLED NEW FITTING PER SRM 51-1-20 AT AFT SIDE OF STA 1140 L35L 2 L 7 4 4F RT 4A25 2001082100013 20010821 00013 WP 2001 8 21 RRXA11403 1 20010709 A 5710 575470133 CLIP DOUG DC8 DC873F 302199F WP RH CTR WG L/E CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND R/H CTR WING L/E HAS A CRACKED CLIP XOLDI 6.225. *** CORRECTIVE ACTION *** REMOVED DAM AGED CLIP, FOUND FRAM CRACKED, STOP DRILLED CRACK. FABRICATED CLIP AND DOUBLER IAWIAW DC8 DRW 5754701 AND SRM 57-2-0 FI G 2. INSTALLED CLIP AND DOUBLER IAW DC8 SRM 51-1-20D AND 51-3-0 2 L 7 4 4F RT 4A25 2001082100014 20010821 00014 WP 2001 8 21 RRXA11408 1 20010713 A 5310 37558451 FITTING DOUG DC8 DC873F 302199F WP CPIT STA 1200 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND C PIT BATH TUB FITTING STA 1200 L35L TO L36L HAS LIGHT CORROSION AT AFT UPPER O/B CORN ER. *** CORRECTIVE ACTION *** REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20. FABRICATED REPAIR ANGLES IAW DC8 SRM 5 3-2-0 FIG 1F, INSTALLED ALL PARS IAAW DC8 SRM 53-2-0 FIG 1F AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001082100022 20010821 00022 EU 2001 8 21 C2XA01IA333 1 20010820 A 3350 0341516 FUSE AEROSP ATR42 ATR42320 8680930 EU CABIN BLOWN A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 14815 104 GPT - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT HAND FRONT ROW EMERGENCY EXIT LIGHT WOULD NOT ILLUMIN ATE. THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT FUSE, AND THE A IRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001082100028 20010821 00028 NM 2001 8 21 COOSDR010075 1 20010820 A 5755 65799525DHL SKIN BOEING 737 737230 NM PWA JT8 JT8D17 52049 NE SPOILER DELAMINATED E EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 767TW 20258 LEFT WING, GROUND SPOILER NR 4, PN 6579952-5 DHL, MD-364 UPPER SKIN DELAMINATED. 2 L 7 2 4F 4 F RT A16WE E2EA 2001082100029 20010821 00029 NM 2001 8 21 COOSDR010076 1 20010820 A 5755 65799527 SKIN BOEING 737 737230 NM PWA JT8 JT8D17 52049 NE SPOILER DELAMINATED E EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 767TW 20258 RIGHT WING, FLIGHT SPOILER NR 8 PN 65-79952-7, MA-532, UPPER SKIN DELAMINATED. 2 L 7 2 4F 4 F RT A16WE E2EA 2001082100030 20010821 00030 NM 2001 8 21 COOSDR010077 1 20010820 A 5754 6546421165 SKIN BOEING 737 737230 NM PWA JT8 JT8D17 52049 NE L/E SLAT DELAMINATED E EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 767TW 20258 LEFT WING, SLAT NR 1, PN 65-46421-165, SN 132 UPPER SKIN DELAMINATED. 2 L 7 2 4F 4 F RT A16WE E2EA 2001082100032 20010821 00032 NM 2001 8 21 COOSDR010079 1 20010820 A 5753 6546435236 SKIN BOEING 737 737230 NM PWA JT8 JT8D17 52049 NE T/E FLAP DELAMINATED E EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 767TW 20258 RIGHT WING, OUTBOARD AFT FLAP PN 65-46435-236, SN 333, UPPER SKIN DELAMINATED. 2 L 7 2 4F 4 F RT A16WE E2EA 2001082100034 20010821 00034 NM 2001 8 21 COOSDR010080 1 20010820 A 5753 654643090 SKIN BOEING 737 737230 NM T/E FLAP DELAMINATED E EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 767TW 20258 RIGHT WING, INBOARD FORE FLAP, PN 65-46430, SN BN803, UPPER SKIN DELAMINATED. 2 L 7 2 4F RT A16WE 2001082100035 20010821 00035 NM 2001 8 21 COOSDR010081 1 20010820 A 5753 65ND273011 SKIN BOEING 737 737230 NM PWA JT8 JT8D17 52049 NE T/E FLAP DELAMINATED E EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 767TW 20258 LEFT WING, INBOARD AFT FLAP, PN 65ND27301-1, SN BN-2. LOWER AND UPPER SKIN DELAMINATED. 2 L 7 2 4F 4 F RT A16WE E2EA 2001082100037 20010821 00037 NM 2001 8 21 COOSDR010082 1 20010820 A 5753 65ND273012 SKIN BOEING 737 737230 NM PWA JT8 JT8D17 52049 NE T/E FLAP DELAMINATED E EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 767TW 20258 RIGHT WING, INBOARD AFT FLAP PN 65ND-27301-2, SN BN2, LOWER AND UPPER SKIN DELAMINATED. 2 L 7 2 4F 4 F RT A16WE E2EA 2001082100038 20010821 00038 NM 2001 8 21 2001UALA00959 1 20010607 A 3200 189915 SENSOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BROKEN A UALA K NONE O OTHER TO TAKEOFF 1 WP 29 7465U 21919 UNABLE TO MOVE GEAR HANDLE PAST OFF POSITION. SUPPLEMENTAL DATA UPDATE FOUND BROKEN WIRE AT AIR SAFETY SENSOR. REPLACED AIR SAFETY SENSOR. OPERATION CHECK NORMAL . 2 L 7 3 4F 4 F A3WE E2EA 2001082100039 20010821 00039 NM 2001 8 21 2001UALA01401 1 20010717 A 2400 MR24298 CONTROL UNIT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 314UA 23675 UNSCHEDULED LANDING DUE TO ELECTRICAL PROBLEMS. FLIGHT CREW REPORTED A SUSTAINED LOSS OF CAPTAINS INSTRUMENTS IN FLIGHT. BOTH CAPTIANS EFIS DISPLAYS WENT BLANK, THE NO.1 GENERATOR BUS DROPPED OFF LINE, THE NO.2 BUS FAILED TO PICK UP THE NO. 1 TRANSFER BUS LOAD, AND THE C819 NO.1 TRANSFER BUS NORMAL CIRCUIT BREAKER TRIPPED. SUPPLEMENTAL DATA UPDATE THE PROBL EM COULD NOT BE DUPLICATED ON THE GROUND. THE NO. 1 TRANSFER BUS NORMAL RELAY (R3) WAS REPLACED. IN ADDITION, THE NO.1 AND NO.2 GENERTAOR CONTROL UNITS WERE REPLACED AS PRECAUTIONARY. TAXI RUNS FAILED TO DUPLICATE THE PROBLEM, AND THE AFF ECTED SYSTEMS OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082100040 20010821 00040 NM 2001 8 21 2001UALA01504 1 20010728 A 3246 161N16253 AXLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FRACTURED A UALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 29 532UA 7111 25072 RIGHT REAR TIRE RIGHT TRUCK AXLE FAILED PRIOR TO TAKEOFF. RIGHT REAR AXLE SHEARED OFF. SUPPLEMENTAL DATA UPDATE A CHROME GRINDING DEFECT ON THE 4.5 INCH OUTER DIAMETER CAUSED CIRCUMFERENTIAL CRACKING AND THE EVENTUAL FAILURE OF THIS AXLE. T HE GRINDING DEFECT HAS CHARACTERISTICS CONSISTENT WITH A GRINDING WHEEL PLUNGE MANEUVER. THIS DEFECT WAS IN THE MAXIMUM BENDING STRESS LOCATION FOR THIS AXLE, A MOST CRITICAL AND WORST PLACE FOR ANY DEFECT ON THIS PART. REPLACED AXLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001082100041 20010821 00041 NM 2001 8 21 2001UALA01681 1 20010620 A 5754 114W41508 SLAT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 772UA 26930 HAIL DAMAGE DENTED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001082100042 20010821 00042 NM 2001 8 21 2001UALA01682 1 20010811 A 2420 729825 IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 515UA 24840 L GEN OFF AND L GEN DRIVE EICAS MSG'S DISPLAYED. SUPPLEMENTAL DATA UPDATE IDG CHECK VALVE FITTING LEAKING.REPLACED IDG. 2 L 7 2 4F 4 F RT A2NM E17NE 2001082100043 20010821 00043 NM 2001 8 21 2001UALA01684 1 20010813 A 5313 CLIP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE BS 1087 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BS 1087 STR 39R FRAME ATTACH CLIP CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED ATTACH CLIP. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082100045 20010821 00045 CE 2001 8 21 OIB2001F00000 1 20010608 A 3350 246213 BATTERY PACK CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE COCKPIT MALFUNCTIONED E OIBA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NE 05 550CA 5675 5500152 AIRCRAFT WAS TAXING TO THE RUNWAY FOR TAKE OFF WHEN THE PILOTS SMELLED A BURNING ODOR, THEN SAW SMOKE COMING FROM THE CO CKPIT HEADLINER. THEY NOTIFIED THE TOWER THAT THEY HAD SMOKE IN THE COCKPIT, PULLED OFF TO THE SIDE AND ASKED FOR THE F IRE TRUCKS TO STANDBY (PRECAUTIONARY). THE AIRCRAFT WAS TOWED TO THE FBO. THE CAUSE OF THE SMOKE WAS DETERMINED TO BE THE EMERGENCY LIGHTING BATTERY PACK. PROBABLE CAUSE WAS A DIODE FAILURE, RESULTING IN A BURNED BATTERY PACK. EMERGENCY LIGHTING SYSTEM WAS MEL D AND THE AIRCRAFT RETURNED TO HOME BASE. BATTERY PACK INSTALLED 6-30-01. 1 L 7 2 4F 4 F A22CE E1NE 2001082100046 20010821 00046 NM 2001 8 21 2001UALA01710 1 20010814 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE BS 287 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 287 STR 4L LIGHTNING DAMAGE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STR REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082100047 20010821 00047 WP 2001 8 21 DHL2001804535 1 20010815 A 5312 4772397U1 FITTING DOUG DC8 DC873F 302199F WP A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 REAR PRESSURE BULKHEAD FITTING AT STA 1366 L17R CRACKED 1 IN.REMOVED CRACKED FITTINGPER SRM 51-1-20 PG 21.CLEANED TREATE D AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-1-20-D PG 9 2 L 7 4 4F RT 4A25 2001082100048 20010821 00048 NE 2001 8 21 TI1R001394 2 20010112 A 7323 430121204 GOVERNOR BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ENGINE MALFUNCTIONED B TI1R O OTHER O OTHER NR NOT REPORTED 1 SW 05 117VU 7211 GOVERNOR - FITTING LOOSE ON GOVERNOR, CAUSING ENGINE TO BE UNCONTROLLABLE AT ALL POWER SETTINGS. CHASING THE TORQUE NEE DLES. ALSO ENGINE SURGES ABOUT 20 PERCENT N2 AT FULL POWER. REMOVED AND REPLACED. 1 G 7 2 3U 3 U H13EU E5NE10 2001082100051 20010821 00051 EU 2001 8 21 TI1R001400 1 20010123 A 3310 1179203103 CONTROL UNIT BOLKMS 117 BK117A3 5626015 EU COCKPIT FAULTY B TI1R O OTHER O OTHER NR NOT REPORTED 1 SW 05 527MB 7103 CONTROL UNIT - SHUTS DOWN ON FULL BRIGHT. REMOVED AND REPLACED. 1 G 7 2 3U H13EU 2001082100052 20010821 00052 2001 8 21 TI1R001401 4 20010122 A 2211 11788292 COMPUTER BOLKMS 117 BK117A3 5626015 EU SPAS FAILED B TI1R O OTHER O OTHER NR NOT REPORTED 1 SW 05 4493X S7038 SPAS-COMPUTER, DC VOLTAGE IN, NO VOLTAGE OUT. REMOVED AND REPLACED. 1 G 7 2 3U H13EU 2001082100053 20010821 00053 EU 2001 8 21 TI1R001402 1 20010207 A 7714 1179405303 INDICATOR BOLKMS 117 BK117B2 5626013 EU TMECA ARRIEL ARRIEL1 60030 NE TRIPLE TACH ERRATIC B TI1R O OTHER O OTHER NR NOT REPORTED 1 SW 05 912SM 86 7150 TRIPLE TACH - NR 1 NEEDLE BOUNCES BETWEEN 30 AND 60 PERCENT AT ENGINE IDLE- ROTOR NEEDLE GIVING WRONG INDICATION. REMOV ED AND REPLACED. 1 G 7 2 3U 3 U NC H13EU E19EU 2001082100057 20010821 00057 2001 8 21 TI1R001407 4 20010126 A 3160 06604021111 SYMBOL GENERATOR BELL 230 230 1182149 SW COCKPIT DEFECTIVE B TI1R O OTHER O OTHER NR NOT REPORTED 1 SW 05 4UV 23019 SG465 - WOULD NOT ALLOW AUTOPILOT TO ENGAGE. REMOVED AND REPLACED. 1 G 7 2 3U NC H9SW 2001082100058 20010821 00058 EU 2001 8 21 TI1R001408 1 20010220 A 2435 150SG122Q STARTER GEN SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE WORN B TI1R O OTHER O OTHER NR NOT REPORTED 1 SW 05 350AZ 1103 3127 STARTER GENERATOR, COMMUTATOR WORN/ PITTED, BRUSHES WORN. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2001082100059 20010821 00059 2001 8 21 TI1R001423 4 20010325 A 3421 5040017926 GYRO BOLKMS 117 BK117A3 5626015 EU ATTITUDE ERRATIC B TI1R O OTHER O OTHER NR NOT REPORTED 1 SW 05 1140H 7078 ATTITUDE GYRO, SPINS ERRATICALLY. REMOVED AND REPLACED. 1 G 7 2 3U H13EU 2001082100060 20010821 00060 EU 2001 8 21 TI1R001424 1 20010218 A 6520 350A33215300 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR WORN B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 40751 821 3154 BEARING, WORN. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2001082100061 20010821 00061 2001 8 21 TI1R001427 4 20010403 A 3421 5040017908 GYRO SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE ATTITUDE TUMBLES B TI1R O OTHER O OTHER NR NOT REPORTED 1 SW 05 40751 942 ATTITUDE GYRO, TUMBLES, REF AEC RMA R303539. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2001082100062 20010821 00062 EA 2001 8 21 COMA0160603 1 20010817 A 2751 7455001 CONTROL HANDLE CNDAIR CL600 CL6002B19 EA COCKPIT FAULTY A COMA K NONE J WARNING INDICATION DE DESCENT 1 SO 01 995CA 184 7229 FLIGHT 5336. DURING DESCENT INTO CVG, RECEIVED A FLAP FAIL CAUTION AT 25 DEGREE FLAP POSITION, CREW DECIDED TO DECLARE A N EMERGENCY, AIRCRAFT LANDED SAFELY.REPLACED THE FLAP CONTROL HANDLE. 2 L 7 2 4F RT A21EA 2001082100064 20010821 00064 EA 2001 8 21 COMA0160604 1 20010817 A 3620 355523255 SENSING ELEMENT CNDAIR CL600 CL6002B19 EA RIGHT GEARWELL FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 986CA 7174 FLIGHT #5432. DURING TAXI OUT WHEN THRUST LEVERS WERE ADVANCED, RIGHT ANTI-ICE DUCT MESSAGE DISPLAYED, AIRCRAFT RETURNED TO THE GATE.REPLACED THE RIGHT GEARWELL SENSING ELEMENT. 2 L 7 2 4F RT A21EA 2001082100065 20010821 00065 EA 2001 8 21 COMA0160616 1 20010819 A 3260 864808 PSEU CNDAIR CL600 CL6002B19 EA ELECTRICAL BAY FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 933CA 2140 7040 FLIGHT #5776. DURING TAXI OUT OF HSV RECEIVED A PROXIMITY SYSTEM FAULT STATUS MESSAGE ON ELECTRONIC DISPLAY #2, AIRCRAFT RETURNED TO THE GATE.REPLACED THE PROXIMITY SENSING ELECTRONIC UNIT. 2 L 7 2 4F RT A21EA 2001082100066 20010821 00066 SO 2001 8 21 2001F00204 1 20010719 A 3070 115677114 DRAIN MAST GULSTM G1159 GIV 3980115 SO ICE PROTECTION OVERTEMP A UG8A K NONE M OVER TEMP IN INSP/MAINT 1 GL 23 940DC 1052 PTK - FLT 1647 - AFT WATER SYSTEM DRAIN MAST HEATER SHOWS SIGNS OF OVERHEATING. DRAIN MAST HEATER ELEMENT OVERTEMP. RE PLACED DRAIN MAST ASSEMBLY WITH NEW UNIT. (M) 2 L 7 2 4F RT A12EA 2001082100067 20010821 00067 NM 2001 8 21 2001F00203 1 20010707 A 5210 60B1000019 DOOR SEAL BOEING 747 747230B 1384889 NM L1 DOOR LOOSE A Q2SA I J A CABIN DEPRESSURIZATION DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 743SA 22671 AIR TURN BACK, AT APPROXIMATELY 1.0 PSI DIFFERENTIAL, A BANG WAS HEARD ACCOMPANIED BY A LOUD ROAR AND AN L-1 DOOR LIGHT. DEPRESSURIZED AIRCRAFT AND L1 DOOR LIGHT WENT OUT. VISUALLY INSPECTED DOOR LATCHES AND OPERATION OF L1 DOOR AND CONFI RMED DOOR WAS NOT SHUT PROPERLY. RE-SECURED DOOR SEAL RETAINER ON UPPER AFT CORNER OF DOOR AND REPLACED LOWER DOOR SEAL . PRESSURIZED AIRCRAFT CABIN AND LEAKED CHECKED GOOD. (M) 2 L 7 4 4F A20WE 2001082100069 20010821 00069 EA 2001 8 21 COMA0160614 1 20010820 A 3320 2LA00663611 PSU CNDAIR CL600 CL6002B19 EA CABIN FAULTY A COMA K NONE S AFFECT SYSTEMS CR CRUISE 1 SO 01 927CA 17718 7031 FLIGHT #5877. THE PASSENGER SIGN CIRCUIT BREAKER TRIPPED DURING TAXI OUT OF DAY, AIRCRAFT RETURNED TO THE GATE. REPLACED SHORTED PASSENGER SERVICE UNIT AT SEAT 7AB. 2 L 7 2 4F RT A21EA 2001082100070 20010821 00070 NM 2001 8 21 AALA20011410 1 20010706 A 5510 BEAM BOEING 727 727227 1384078 NM HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 731AA 20738 TUL - FOUND LEFT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM CORRODED SS136 TO SS142. REMOVED CORROSION, INSTALLED D OUBLER REPAIR PER ESO 11697 DATED 7-6-01. (M) 2 L 7 3 4F A3WE 2001082100071 20010821 00071 WP 2001 8 21 AALA20011436 1 20010718 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 593AA 53256 DFW - DURING OVERNIGHT MAINTENANCE, PORTABLE EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED PORTABLE EMERGENCY EXIT LIGHT A SSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001082100072 20010821 00072 EA 2001 8 21 COMA0160613 1 20010820 A 3350 BC10020004 LIGHT CNDAIR CL600 CL6002B19 EA A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 785CA 7326 FLIGHT #N/A. EMERGENCY CEILING LIGHT AT ROW 13 IS INOPERATIVE.REPLACED THE EMERGENCY FLOOD LIGHT BULB AT ROW 13. 2 L 7 2 4F RT A21EA 2001082100073 20010821 00073 2001 8 21 MASA01061 4 20010708 A 2562 4530150 ELT CNDAIR CL600 CL6002B19 EA FUSELAGE INTERMITTENT A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 17275 7275 WHILE PERFORMING AN ELT FUNCTIONAL CHECK, THE ELT WAS DISCOVERED TO BE INTERMITTENT. MAINTENANCE REMOVED AND REPLACED T HE ELT AND BATTERY PACK. OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001082100074 20010821 00074 EA 2001 8 21 MASA01085 1 20010805 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 EA EXTERIOR INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77278 7278 WHILE PERFORMING ROUTINE SERVICE, FOUND EXTERIOR EMERGENCY LIGHT AT FS 491.50L INOPERATIVE. REMOVED AND REPLACED BULB I AW AMM 33-51-21. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2001082100075 20010821 00075 EA 2001 8 21 COMA0160612 1 20010820 A 2900 PUMP CNDAIR CL600 CL6002B19 EA A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 969CA 7141 FLIGHT #5995. DURING TAXI OUT FROM CVG THE CIRCUIT BREAKER FOR HYDRAULIC PUMP 3A TRIPPED, AIRCRAFT RETURNED TO THE GATE. TRANSFERRED THE ALTERNATING CURRENT MOTOR PUMP 3A TO THE DEFERRED DISCREPANCY LIST PER MEL. 2 L 7 2 4F RT A21EA 2001082100076 20010821 00076 EU 2001 8 21 USAAF01053 1 20010725 A 5220 DOOR FOKKER F28 F28MK0100 4990807 EU EMERGENCY EXIT UNSECURE A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 857US 11289 PIT - FLT 1472 - EN ROUTE PIT-SDF, DURING CLIMB-OUT, THE COVER FOR THE EMERGENCY DOOR EMERGENCY RELEASE HANDLE AND SOME SAFETY WIRE FELL OFF. THE EMERGENCY DOOR EMERGENCY RELEASE HANDLE WAS FOUND TO BE IN THE INCORRECT POSITION. THE FLIGH T RETURNED TO FIELD IN PIT. THE CABIN PRESSURE EQUALIZED AFTER LANDING, AND THE EMERGENCY EXIT DOOR FELL OUT OF THE EME RGENCY EXIT OPENING ONTO THE EMERGENCY ROW SEATS. (M) 2 L 7 2 4F RT 2001082100077 20010821 00077 EU 2001 8 21 USAAF01059 1 20010728 A 3350 6040681 POWER SUPPLY FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 890US 11365 IND - THE FLOOR EMERGENCY LIGHTS, GALLEY EXIT SIGN, AND NR 1 AISLE LIGHT IN FIRST CLASS WERE INOPERATIVE. MAINTENANCE R EPLACED A POWER SUPPLY. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT 2001082100078 20010821 00078 EU 2001 8 21 USAAF01061 1 20010730 A 2612 FIRE DETECTOR FOKKER F28 F28MK0100 4990807 EU APU MALFUNCTIONED A USAA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 897US 11392 TRI - FLT 896 - EN ROUTE PIT-CLT, AT FL310, RECEIVED AN APU FIRE WARNING. THE FIRE EXTINGUISHING SYSTEM AUTOMATICALLY D ISCHARGED. THE FLIGHT DIVERTED TO TRI AND LANDED SAFELY. MAINTENANCE INSPECTED THE APU ENCLOSURE AND THE TAIL COMPARTM ENT. NO SIGNS OF A FIRE WRE FOUND. (M) 2 L 7 2 4F RT 2001082100079 20010821 00079 WP 2001 8 21 01FDEA00741 1 20010818 A 5101 STRUCTURE DOUG DC10 DC1010 3022110 WP FUSELAGE VIBRATION A FDEA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 25 397FE 46631 AFTER T/O PASSING 235 KTS & CLIMBING THROUGH APPROX 4000 FT ACFT BEGAN TO VIB WITH LOUD NOISE COMING FROM BELOW & AFT OF PILOT SEATS. PACKS TURNED OFF, NO HELP. THROTTLES BACK TO IDLE, NO HELP. FLAPS DOWN TO 22 GEAR DOWN 210 KTS, NO HELP . GEAR UP 180 KTS, VIB WENT AWAY. 2 L 7 3 4F A22WE 2001082100080 20010821 00080 NM 2001 8 21 AWXA0002121 1 20010714 A 5312 6516300517 STRAP BOEING 737 737277 1384570 NM BS 178 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 D: Strap cracked on fwd side of BS 178 bulkhead BL-0 WL 188C: Removed and replaced strap IAW DWG 65-16300 and B737 SRM 5 1-30-2 2 L 7 2 4F RT A16WE 2001082800145 20010828 00145 NM 2001 8 28 01FDEA00742 1 20010817 A 2923 CONNECTOR DOUG MD11 MD11 3023602 NM AUX HYD PUMP SHORTED A FDEA K NONE B A SMOKE/FUMES/ODORS/SPARKS FLAME/FIRE IN INSP/MAINT 1 SO 25 584FE 48436 DURING HYD OPS USING AUX PUMPS FOR FLT CNTRL RIGGING, FOUND NR 1 AUX HYD PUMP ELECTRICAL CONNECTOR SHORTED CAUSING SPARK S AND SUBSEQUENT FIRE TO SURROUNDING AREA. REMOVED AND REPLACED WIRINGS PER WDM 20-31-15. 2 L 7 3 4F RT A22WE 2001082100081 20010821 00081 WP 2001 8 21 ABXA010445 1 20010817 A 2780 SEAL DOUG DC8 DC861 3021952 WP CONTROL VALVE LEAKING A ABXA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 23 849AX 45891 LOSS OF HYDRAULICS DURING CLIMB, HAPPENED ABOUT WHEN GEAR UPLATCH CHECK WAS ACCOMPLISHED. DURING HYDRAULIC PRESSURE CHE CK (TERMINAL AREA) HYDRAULIC QUANTITY DECREASED. FOUND SLOT CONTROL VALVE SEALS LEAKING. REPACKED VALVE. SERVICED HYD RAULIC SYSTEM. SYSTEM CHECKED GOOD IAW DC-8 AMM 27-80-04-2. 2 L 7 4 4F 4A25 2001082100082 20010821 00082 WP 2001 8 21 ABXA010446 1 20010818 A 2701 YOKE DOUG DC8 DC863F 302198F WP COCKPIT JAMMED A ABXA K NONE F FLT CONT AFFECTED AP APPROACH 1 GL 23 814AX 46041 ELEVATOR CONTROL YOKE JAMMED ON FINAL APPROACH. YOKE WOULD ONLY GO TO THE NEUTRAL POSITION ON THE ELEVATOR POSITION IND ICATOR. VERIFIED ELEVATOR CONTROL COLUMN JAM IN NOSE DOWN POSITION. INSPECTION REVEALED ELEVATOR RIGGING FIXTURE LINK CONTACTED LOWER ELEVATOR CONTROL COLUMN RIGHT SIDE. FOUND RIGGING FIXTURE LINK RETRACT SPRING INSTALLED INCORRECTLY. R EMOVED SPRING AND INSTALLED CORRECTLY TO ENSURE TENSION FOR LINK RETRACTION. ELEVATOR OPS CHECKED GOOD IAW DC-8 AMM 27- 30-00-0-0006. 2 L 7 4 4F 4A25 2001082100083 20010821 00083 WP 2001 8 21 ARWA0010807 1 20010812 A 2612 614F20025 CIRCUIT BOARD LKHEED 1011 1011385114 WP FIRE DETECTION BURNED A ARWA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 19 260FA 193A1158 NR 2 ENGINE FIRE DETECTION LOOP-A ON STEADY, LOOP-B INTERMITTENT, FIRE BELL INTERMITTENT, SHUT DOWN ENGINE AS PER AFM AT 21:15Z. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED 1A3 ILCB IAW MM 33-17-00, REPAIRED WIRE CONNECTORS ON P712 & P713 ON ENGINE FIREWALL GROUND OPS NORMAL IAW MM 26-11-00. 2 L 7 3 4F A23WE 2001082100085 20010821 00085 NM 2001 8 21 AWXA0002072 1 20010803 A 2910 6558192 HYDRAULIC LINE BOEING 737 737277 1384570 NM NR 1 PYLON LOOSE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 HYDRAULIC PRESSURE LINE AT TRANSITION THROUGH PYLON, LOOSE, NR 1 PYLON. REPAIRED NR 1 HYDRAULIC PRESSURE LINE WALL PYLO N IAW AWA ER 15-5412-01202-DL1. 2 L 7 2 4F RT A16WE 2001082100087 20010821 00087 NM 2001 8 21 AWXA0002116 1 20010813 A 5320 149N7130 SUPPORT BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 903AW 23323 WING TO BODY FAIRING SUPPORT AT STA 900 IS CORRODED ON THE LOWER SURFACE FROM LBL 10 TO RBL 10 (MARKED 5452651). CUT OU T CORRODED AREA, FABRICATED REPAIR PARTS AND INSTALLED PARTS PER SRM 51-40-02 PG 1. 2 L 7 2 4F RT A2NM 2001082100088 20010821 00088 NM 2001 8 21 AWXA0002117 1 20010813 A 5320 146N54121 FLOOR SUPPORT BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 903AW 23323 CORROSION AROUND PLATE NUTS ON UPPER FLANGE OF CARGO FLOOR SUPPORT INTERCOSTAL FS 1360, BETWEEN STR 26R AND STR 27R (UPP ER AND LOWER SURFACE OF FLANGE). REMOVED FLOOR SUPPORT IAW SRM 51-40-02. FABRICATED SUPPORT FLOOR PER SRM 51-30-4 PG 1 1 & 20 AND ENGINEERING SUPPORT IAW SRM 51-40-02 PG 1-2. 2 L 7 2 4F RT A2NM 2001082100089 20010821 00089 NM 2001 8 21 AWXA0002118 1 20010814 A 5320 141N827146 PAN BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 903AW 23323 EXTERNAL POWER SERVICE PAN IS CRACKED AT THE UPPER FWD AND UPPER AFT CORNERS OF PLUG RECEPTACLE. REMOVED AND REPLACED T HE EXTERNAL POWER SERVICE PAN P/N 14N8271-46 PER 757 SRM 51-40-02 PG 3. 2 L 7 2 4F RT A2NM 2001082100090 20010821 00090 EU 2001 8 21 AWXA0002120 1 20010814 A 5330 D53112242200 SKIN AIRBUS 320 A320231 3930325 EU FUSELAGE DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 DENT IN FUSELAGE AT FRAME 23 BETWEEN STRINGERS 25L & 24L. REMOVED PREVIOUS REPAIR. FABRICATED AND INSTALLED SKIN DOUBL ER REPAIR AS PER A320 SRM 53-00+10 FIGURE 203 PAGES 206C TO 208B PAINTED AS PER AMM 51-75-00-001. 2 L 7 2 4F RT A28NM 2001082100091 20010821 00091 NM 2001 8 21 AWXA0002124 1 20010714 A 5311 6516300302 FRAME BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 RIGHT BS 178 CHORD CRACKED AT WL 207 RBL 24. REMOVED AND REPLACED CHORD IAW ER 15-5311-01185-SS1. 2 L 7 2 4F RT A16WE 2001082100092 20010821 00092 NM 2001 8 21 AWXA0002125 1 20010715 A 5311 6516300301 FRAME BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 LEFT BS 178 CHORD CRACKED AT WL 195 LBL 24. REMOVED AND REPLACED LEFT BS 178 CHORD IAW AWA ER 15-5311-01185-SS1 AND AWA ER 15-5313-01200-JS1. 2 L 7 2 4F RT A16WE 2001082100093 20010821 00093 NM 2001 8 21 AWXA0002128 1 20010723 A 5412 6558192 FIREWALL BOEING 737 737277 1384570 NM NR 1 PYLON DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 E1 HYDRAULIC PRESSURE LINE AT TRANSITION THOUGH PYLON, LOOSE; NR 1PYLON. REPAIRED NR 1 ENG FIRE WALL PYLON IAW ER 15-54 12-01202-DL1. 2 L 7 2 4F RT A16WE 2001082100094 20010821 00094 NM 2001 8 21 AWXA0002130 1 20010723 A 5320 656894011 ANGLE BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 LEFT ANGLE ON BS 1088 BULKHEAD CORRODED AT WL 243 RBL 23 TO RBL 32. REMOVED AND REPLACED LEFT ANGLE IAW B737 SRM 51-30- 2. 2 L 7 2 4F RT A16WE 2001082100095 20010821 00095 NM 2001 8 21 AWXA0002133 1 20010723 A 5320 6546572527 ANGLE BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 T-ANGLE FWD SIDE OF BS 1088 BULKHEAD CORRODED AT RBL 33 WL 228 TO 240. REMOVED AND REPLACED T-ANGLE IAW B737 SRM 51-30- 2 PG 2&3. 2 L 7 2 4F RT A16WE 2001082100096 20010821 00096 NM 2001 8 21 AWXA0002138 1 20010701 A 5315 6545810519 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 DURING D-CHECK INSPECTION FOUND CORROSION ON MAIN CABIN FLOORBEAM BS 312 LBL 8 TO RBL 14 WL 207.5. REMOVED CORROSION AN D REPAIRED FLOORBEAM BS 312 IAW B737 SRM 53-10-9. 2 L 7 2 4F RT A16WE 2001082100097 20010821 00097 NM 2001 8 21 AWXA0002146 1 20010731 A 5311 6545409602 FRAME BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 BS 663.75 PRESSURE DECK COMPRESSION CHORD CRACKED AT LBL 24. REPAIRED COMPRESSION CHORD IAW ER 15-5715-01195-SS2. 2 L 7 2 4F RT A16WE 2001082100098 20010821 00098 NM 2001 8 21 AWXA0002147 1 20010706 A 5315 BAC1518399 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 CORROSION ON FLOORBEAM BS 947 RBL 43.0 TOP AND BOTTOM OF UPPER FLANGE. CUT OUT CORRODED SECTION OF BS 947 RBL 43 FLOORB EAM UPPER FLANGE. INSTALLED REPAIR IAW B737 SRM 53-10-9 FIG 3. 2 L 7 2 4F RT A16WE 2001082100099 20010821 00099 NM 2001 8 21 AWXA0002150 1 20010707 A 5311 65C1717313 FRAME BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 LOWER T-CHORD CRACKED BS 717 BL 0 BELOW CABIN FLOOR. REPAIRED IAW AWA ER 15-5702-01209-DD2. 2 L 7 2 4F RT A16WE 2001082100100 20010821 00100 NM 2001 8 21 AWXA0002153 1 20010803 A 5320 6545409602 ANGLE BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 CABIN FLOORBEAM AREA ANGLE CRACKED BS 663.75 RBL 24. REPAIRED BS 663.75 BEAM UPPER CHORD IAW AWA ER 15-5715-01195-SS2. 2 L 7 2 4F RT A16WE 2001082100101 20010821 00101 NM 2001 8 21 AWXA0002155 1 20010804 A 5315 6546588107 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 CORROSION ON FLOORBEAM BS 1016 LBL 33.5 TOP AND BOTTOM OF UPPER FLANGE. REPAIRED BS 1016 FLOORBEAM UPPER CHORD IAW AWA ER 15-5365-01209-DD1. 2 L 7 2 4F RT A16WE 2001082100102 20010821 00102 NM 2001 8 21 AWXA0002156 1 20010714 A 5320 655966431 SPLICE BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 DURING INSPECTION FOUND STRINGER SPLICE AT BS 360 STR 27R CORRODED. REMOVED AND REPLACED STRINGER SPLICE BS 360 AT STR 27R IAW B737 SRM 51-30-2. 2 L 7 2 4F RT A16WE 2001082100103 20010821 00103 NM 2001 8 21 AWXA0002158 1 20010804 A 5314 65621251 KEELBEAM BOEING 737 737277 1384570 NM FUSELAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 OIL CANNING AND LOOSE RIVETS ON KEEL BEAM PANEL BS 663-673. REPAIRED FASTENER HOLES IN KEEL BEAM CHORD AND REPAIRED PAN EL IAW AWA ER 15-5315-01215-DL. 2 L 7 2 4F RT A16WE 2001082100104 20010821 00104 NM 2001 8 21 AWXA0002160 1 20010815 A 5754 114N3030 SKIN BOEING 757 7572S7 1384962 NM L/E SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 903AW 23323 LEFT WING NR 2 SLAT CRACKED AT FASTENER HOLE, LWR SURFACE STA 595. CUT OUT DAMAGE PER SRM 51-70-13 FIG 1. FABBED DOUBL ER & SLIMS IAW SRM 57-43-13 FIG 1. INSTALLED REPAIR PARTS PER SRM 51-40-02. 2 L 7 2 4F RT A2NM 2001082100105 20010821 00105 EU 2001 8 21 AWXA0002161 1 20010816 A 5320 D53112087200 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 FR 16-20 Y 254 LT FLOOR SUPPORT CORRODED. REPLACED FLOOR SUPPORT RAIL FROM FR12 TO 24 AS PER SRM 53-11-14 PG 37, 205-21 0 FIG 8 AND 202. 2 L 7 2 4F RT A28NM 2001082100106 20010821 00106 EU 2001 8 21 AWXA0002162 1 20010816 A 5320 D53112091203 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 FR 16-20 Y -254 RT FLOOR SUPPORT CORRODED. REPLACED FLOOR SUPPORT RAIL AS PER SRM 53-11-14 PG 37 AND DWG D53110858. 2 L 7 2 4F RT A28NM 2001082100107 20010821 00107 EU 2001 8 21 AWXA0002163 1 20010816 A 5347 D53112091203 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 FR 20 Y -754 RT SEAT TRACK CORRODED. REPLACED SEAT TRACK/FLOOR SUPPORT RAIL AS PER SRM 53-11-14 PG 37 AND DWG D53110858 . 2 L 7 2 4F RT A28NM 2001082100108 20010821 00108 NM 2001 8 21 AWXA0002164 1 20010815 A 5754 114N3030 SKIN BOEING 757 7572S7 1384962 NM L/E SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 903AW 23323 LT WING NR 2 SLAT CRACKED AT FASTENER HOLE, LWR SURFACE STA 595. CUT OUT DAMAGE PER SRM 51-70-13 FIG 1. FABBED DOUBLER S & SLIMS IAW SRM 52-43-13 FIG 1. INSTALLED REPAIR PARTS PER SRM 51-40-02. 2 L 7 2 4F RT A2NM 2001082100109 20010821 00109 CE 2001 8 21 B3OR20010007 1 20010720 A 7722 3028022 HARNESS CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE LT ENGINE DETERIORATED B B3OR O OTHER O OTHER IN INSP/MAINT 1 SW 03 5408G 461 461 5500666 PCE71427 DUR HI-PWR ENG RUN, NOTICED LT ENG ITT AT 690 DEG. ITT CLIMBED, REDUCED PWR IN ORDER NOT TO EXCEED 700 DEG RED LINE OF ITT. A 5 PT PERFORMANCE RUN PERF AT P&W REQUEST. ITT AT 695 DEG. CHECKED T1 HARNESS & T6 THERMOCOUPLES. RESISTANCE O F BOTH OF THE HARNESS' WITHIN PUBLISHED LIMITS. 2 OF THE T6 THERMOCOUPLES HAD DIFFERENT P/N THAN THE OTHERS. CHANGED T HE 2 T6 THERMOCOUPLES WITH THE DIFFERENT P/N. ENG WAS CHECKED FOR BLEED AIR LEAKS, NONE FOUND. ANOTHER 5 PT PERFORMANC E RUN CONDUCTED, SAME RESULTS. ITT AT 695 DEG. CHANGED STATOR VANE ICE VALVE. A RUN WAS CONDUCTED, ITT AT 690 DEG. C HANGED T1 THERMOCOUPLE HARNESS, AN ENGINE PERFORMANCE RUN COMPLETED. THE ITT DROPPED TO 660 DEGREES. 1 L 7 2 4F 4 F A22CE E1NE 2001082100110 20010821 00110 NM 2001 8 21 UPS01236657 1 20010811 A 5310 STRINGER BOEING 727 72727C 138400J NM BS 400 S6R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 908UP 19114 INSPECTION TYPE:C ON FURTHER INSPECTION STRINGER S6R FOUND CRACKED AT BS 400 REPAIRED PER SRM 2 L 7 3 4F A3WE 2001082100111 20010821 00111 NM 2001 8 21 UPS01236658 1 20010815 A 5330 STRINGER BOEING 727 72727C 138400J NM BS400 S18R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 908UP 19114 INSPECTION TYPE:C ON INSPECTION OF FUSELAGE STRINGERS AT BS 400 WHERE ACCESSABLE, STRI NGER 18R AT BS 400 FOUND TO BE CR ACKED. STRINGER REPAIRED IAW SRM. 2 L 7 3 4F A3WE 2001082100112 20010821 00112 NM 2001 8 21 UPS01236660 1 20010811 A 5310 STRINGER BOEING 727 72727C 138400J NM BS 400 S16L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 908UP 19114 INSPECTION TYPE:C ON FURTHER INSPECTION FOR ACCESS, S16L FOUND CRACKED AT BS 400 REPAIRED IAW SRM 2 L 7 3 4F A3WE 2001082100113 20010821 00113 NM 2001 8 21 UPS01236661 1 20010811 A 5310 STRINGER BOEING 727 72727C 138400J NM BS 400 S15L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 908UP 19114 INSPECTION TYPE:C ON FURTHER INSPECTION FOR ACCESS S15L FOUND CRACKED AT BS 400 REPAIRED IAW SRM 2 L 7 3 4F A3WE 2001082100114 20010821 00114 NM 2001 8 21 UPS01536490 1 20010802 A 7100 ENGINE BOEING 757 75724APF 1384969 NM LEFT ENGINE UNSERVICEABLE A IPXA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 01 417UP 23904 INSPECTION TYPE:N/A ATB-LEFT ENGINE FAILED AT T/O LOAD COMPRESSOR STALL WAS HEARD. FLAM ES WERE SEEN COMING FROM ENGINE PARTS. STRUCTURAL DAMAGE TO AIRCRAFT WAS NOTED ***SUPPLEMENTAL MRR*** R&R LEFT ENGINE PER TC 5001 AND TESTED ENGIN E PER TC 5002. RUN CHECK S GOOD. S/N ON P726529 PFF 717936. REMOVED AND REPLACED TRAILING EDG E FLAPS PER 27-51-02/401 S TEPS D(2)THRU(D7), (D9) CORRECTIVE ACTION CONTINUES ON LOG PAGE 74903 2 L 7 2 4F RT A2NM 2001082100115 20010821 00115 NM 2001 8 21 C1HA200181008 1 20010708 A 3310 SWITCH BOEING 727 7272S7 138407Z NM COCKPIT MALFUNCTIONED A C1HA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 681CA 22020 SMOKE EMITTED FROM INSTRUMENT PANEL INDICATOR LIGHTS, MASTER DIMMING DC BUS 1 DC BUS 2 POPPED. REMOVED AND REPLACED MAS TER DIM AND TEST CARD, SYSTEM CHECKS NORMAL. 2 L 7 3 4F A3WE 2001082100116 20010821 00116 NM 2001 8 21 C1HA200181009 1 20010717 A 3350 900542 BATTERY PACK BOEING 727 7272S7 138407Z NM CABIN DISCHARGED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 681CA 22020 LEFT EMERGENCY OVERWING EXIT LIGHTS INOP. REPLACED BATTERY PACK FOR LT FWD OVERWING EXIT LIGHTS, OPS CHECK NORMAL. 2 L 7 3 4F A3WE 2001082100117 20010821 00117 NM 2001 8 21 C1HA200181010 1 20010718 A 3397 WIRE BOEING 727 7272S7 138407Z NM CABIN DISCONNECTED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 681CA 22020 AISLE OVERWING EXIT MARKER LIGHT INOP. RESECURED WIRE AT CANNON PLUG, OPS CHECKS NORMAL. 2 L 7 3 4F A3WE 2001082100118 20010821 00118 NM 2001 8 21 C1HA200181011 1 20010722 A 2781 GROUND WIRE BOEING 727 7272S7 138407Z NM NR 8 SLAT DISCONNECTED A C1HA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 15 681CA 22020 UPON TAKING RWY, NR 8 SLAT WENT TO AMBER. CYCLED SEVERAL TIMES, NO HELP. RETURNED TO GATE. FOUND BAD GROUND AT NR 8 S LAT DOWNLOCK SWITCH. REPAIRED GROUND, OPS CK GOOD. 2 L 7 3 4F A3WE 2001082100119 20010821 00119 2001 8 21 C1HA200184007 4 20010705 A 2565 116110015 SLIDE BOEING 727 7272S7 138407Z NM R2 DOOR UNSERVICEABLE A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 684CA 22491 DOOR 2R EMERGENCY ESCAPE SLIDE PRESSURE GAUGE READS ZERO. REMOVED AND REPLACED R-2 DOOR SLIDE. 2 L 7 3 4F A3WE 2001082100120 20010821 00120 NM 2001 8 21 C1HA200193014 1 20010805 A 2613 OVERHEAT LOOP BOEING 727 727212 138407G NM NR 1 STRUT OUT OF POSITION A C1HA O OTHER N FALSE WARNING CR CRUISE 1 GL 15 293AS 21348 NR 1 STRUT OVERHEAT AT FL330, REDUCED PWR TO 80 PERCENT LIGHT WENT OUT. REPOSTIONED LOOP FOR STRUT OVERHEAT PER MM 36-2 2-1, OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2001082100121 20010821 00121 NM 2001 8 21 C1HA200194014 1 20010706 A 2120 ODOR BOEING 727 727290 138408W NM CABIN DETECTED A C1HA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 294AS 22146 DURING TAXI OUT AT LAS PAX AND FA COMPLAINED OF STRONG FUEL ODOR IN THE CABIN AND REPORTED SEEING A HAZE. RETURNED TO G ATE. PERFORMED ENG RUNS PACKS ON APU ON GENS ONLINE INSPECTED VENTRAL STAIR AREA, WHEEL WELL AREA, CABIN CHECKED FOR FU MES AND ODOR. COULD NOT DUPLICATE. CHECKED A/C FOR FUEL LEAKS, INSP APU SHROUD AREA, NO LEAKS NOTED. 2 L 7 3 4F A3WE 2001082100122 20010821 00122 NM 2001 8 21 C1HA200194015 1 20010805 A 3510 280001 REGULATOR BOEING 727 727290 138408W NM COCKPIT MALFUNCTIONED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 294AS 22146 F/O'S O2 MASK DOES NOT TEST PROPERLY. REMOVED AND REPLACED F/O'S OXYGEN REGULATOR, OPS AND LEAK CHECK GOOD. 2 L 7 3 4F A3WE 2001082100123 20010821 00123 NM 2001 8 21 C1HA200195012 1 20010703 A 5330 SKIN BOEING 727 727290 138408W NM FUSELAGE DAMAGED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 DAMAGE TO FUSELAGE AT APPROX 6 INCHES AFT OF TOP AFT CORNER OF ELECTRICAL CONNECTOR PANEL HOLE APPROX 1' X 4". REPAIRED PER SRM 53-30-3. 2 L 7 3 4F A3WE 2001082100124 20010821 00124 NM 2001 8 21 C1HA200195013 1 20010723 A 3397 WIRE BOEING 727 727290 138408W NM CABIN DISCONNECTED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 295AS 22147 LEFT FWD OVERWING EMERGENCY LIGHT WALL ASSY INOP. INSPECTED LIGHT AND FOUND WIRING TO LIGHT DISLODGED. RECONNECTED LIG HT ASSY TO WALL SOCKET. OPS CHECKED NORMAL. 2 L 7 3 4F A3WE 2001082100125 20010821 00125 NM 2001 8 21 C1HA200195014 1 20010725 A 3350 900542 POWER SUPPLY BOEING 727 727290 138408W NM CABIN DISCHARGED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 295AS 22147 EXTERIOR EMERGENCY LIGHT ON AFT CARGO DOOR INOP. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AT STA 950A +10, CHE CKS NORMAL. 2 L 7 3 4F A3WE 2001082100126 20010821 00126 2001 8 21 C1HA200196009 4 20010705 A 2312 064100400 TRANSCEIVER BOEING 727 7272J4 1384006 NM VHF FAILED A C1HA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 696CA 22574 NR 2 VHF COM WILL NOT TRANSMIT OR RECEIVE. AIR RETURN OVERWEIGHT LANDING MADE 175,000 LBS, SMOOTH. REPLACED NR 2 VHF T RANSCEIVER CHECKS GOOD. OVERWEIGHT LANDING INSPECTION ACCOMPLISHED. 2 L 7 3 4F RT A3WE 2001082100127 20010821 00127 NM 2001 8 21 C1HA200196010 1 20010716 A 3350 110049 BATTERY PACK BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 696CA 22574 INSPECTION FOUND PATH LIGHTING FROM SEAT ROW 26 AFT INOP. REMOVED AND REPLACED BATTERY PACK CHECKS NORMAL. 2 L 7 3 4F RT A3WE 2001082100128 20010821 00128 NM 2001 8 21 C1HA200196011 1 20010718 A 3350 116049 CHARGER BOEING 727 7272J4 1384006 NM CABIN FAILED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 696CA 22574 ESCAPE PATH LIGHTING INOP. REPAIRED WIRES AND REPLACED BATTERY CHARGER, ASSY CHECKS NORMAL. 2 L 7 3 4F RT A3WE 2001082100129 20010821 00129 EU 2001 8 21 C2XA01BT130 1 20010731 A 3350 LIGHT AEROSP ATR42 ATR42320 8680930 EU EXTERIOR LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 34817 152 BTV---CO2930, DURING 1A INSPECTION MAINTENANCE FOUND EXTERIOR EMERGENCY LIGHTS 5WL AND 22WL ARE INOPERATIVE. FOUND BULB S LOOSE IN SOCKETS, REPOSITIONED AND ADJUSTED BULBS. OPS CHECKED GOOD. 2 H 7 2 4T RT A53EU 2001082100130 20010821 00130 SO 2001 8 21 C2XA01BT131 1 20010730 A 2910 14531063419 HYDRAULIC LINE EMB 145 EMB145LR SO HYDRAULIC SYS CHAFED A C2XA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 27 16987 145261 EWR---CO3033, CREW REPORTED, HYDRAULIC SYSTEM NR 1 FAILED INFLIGHT QUANTITY WENT TO ZERO. AIRCRAFT AIR RETURNED TO NEWA RK AND LANDED UNEVENTFULLY. MAINTENANCE FOUND A CHAFED HYDRAULIC HOSE. REMOVED AND REPLACED HYDRAULIC HOSE, SERVICED H YDRAULIC FLUID, OPS AND LEAKED CHECKED GOOD IAW EMB145 MM 29-10-03. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2001082100131 20010821 00131 SO 2001 8 21 C2XA01BT132 1 20010731 A 3234 8271011 CONTROL HANDLE EMB 145 EMB145ER SO COCKPIT FAULTY A C2XA K NONE J WARNING INDICATION CL CLIMB 1 SW 27 14933 145018 EWR---CO4292, CREW REPORTED LANDING GEAR DID NOT RETRACT ON TAKEOFF. INDICATIONS SHOWED GEAR DOWN. CYCLED HANDLE, LAND ING GEAR CAME UP AND INDICATED UP. NOSE GEAR DOORS STAYED OPEN. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL LEVER IAW EMB145 MM 32-32-02. OPERATIONALLY CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2001082100132 20010821 00132 EU 2001 8 21 C2XA01BT134 1 20010803 A 3350 SOCKET AEROSP ATR42 ATR42320 8680930 EU PAX DOOR DIRTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14832 187 BTV---CO2930, DURING 3A INSPECTION MAINTENANCE FOUND EMERGENCY LIGHT ON PASSENGER DOOR STEP TO BE INOPERATIVE. MAINTENA NCE CLEANED SOCKET AND RESECURED BULB. OPS CHECKED GOOD. 2 H 7 2 4T RT A53EU 2001082100133 20010821 00133 NM 2001 8 21 C1HA200183005 1 20010728 A 5200 SEAL BOEING 727 7272S7 138407Z NM AIRSTAIR DOOR LOOSE A C1HA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 683CA 22490 Loud high pitch sound coming from aft bulkhead above door.Return to DFW.overweight landing made smooth.ACTION TAKEN:Trou bleshot in reported area found no structual damage. After visual inspection of sta.1183 bulkhead and crown area sta. 114 0 to 1183 pressurized aircraft and unable to duplicate reported noise. Test flew aircraft and duplicated noise. Found sm all leak at bottom of vault door. Accomplished seal repair IAW 52-0-01. pressurized no leak noted. 2 L 7 3 4F A3WE 2001082100135 20010821 00135 EU 2001 8 21 C2XA01BT135 1 20010803 A 2435 STARTER GEN AEROSP ATR42 ATR42320 8680930 EU NR 2 ENGINE FAULTY A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 17831 185 EWR---CO3208, CREW REPORTED DURING TAXI/GROUND HOLD THAT DC GENERATOR ENGINE NR 2 WAS INOPERATIVE (AIRCRAFT HAD SMOKE IN THE CABIN. MAINTENANCE REMOVED AND REPLACED THE NR 2 STARTER GENERATOR AND NR 2 GENERATOR CONTROL UNIT IAW ATR42 JIC 2 4-32-81. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001082100136 20010821 00136 EU 2001 8 21 C2XA01BT142 1 20010807 A 3350 CONNECTOR AEROSP ATR42 ATR42320 8680930 EU CABIN DISCONNECTED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 26826 172 BTV---DURING 1A INSPECTION MAINTENANCE FOUND EMERGENCY LIGHTING INOPERATIVE ON AISLE LIGHTS BETWEEN ROWS 3 AND 4. MAINT ENANCE RECONNECTED CANNON PLUG 33WL ON SECOND ROW OF FLOOR PROXIMITY LIGHTING. OPS CHECKED GOOD. 2 H 7 2 4T RT A53EU 2001082100137 20010821 00137 SO 2001 8 21 C2XA01BT143 1 20010806 A 3350 7287580503 LIGHT EMB 145 EMB145LR SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12922 145338 BTV---CO3944, DURING RON OF AIRCRAFT MAINTENANCE CLEARED EMERGENCY FLOOR PATH PROXIMITY LIGHT STRIP INOPERATIVE AT SEAT 16 AND 17A MEL (REFERENCE MEL 33-50-00/2 PLACARD 014103). REMOVED AND REPLACED EMERGENCY FLOOR PATH PROXIMITY LIGHT ST RIP AT SEAT 16 AND 17A IAW EMB145 MM 33-50-12. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2001082100138 20010821 00138 EU 2001 8 21 C2XA01BT144 1 20010723 A 5311 FRAME AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14819 156 YUL---CO4372, DURING 1C INSPECTION MAINTENANCE FOUND AT FRAME 25 RIGHTHAND HYDRAULIC LINE CUTOUT IS CRACKED. REPAIRED I AW COEX EC 5310-01199. 2 H 7 2 4T RT A53EU 2001082100139 20010821 00139 EU 2001 8 21 C2XA01BT145 1 20010731 A 5311 FRAME AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14819 156 YUL---CO4372, DURING 1C INSPECTION MAINTENANCE FOUND AT FRAME 25 LEFTHAND HYDRAULIC LINE CUTOUT TO BE CRACKED. REPAIRED IAW COEX EC 5310-01199. 2 H 7 2 4T RT A53EU 2001082100140 20010821 00140 EU 2001 8 21 C2XA01BT149 1 20010730 A 5311 FRAME AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CRACKED A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 14819 156 YUL---CO4372, DURING 1C INSPECTION IN YUL MAINTENANCE FOUND FRAME 9 WEB TO BE CRACKED ON LEFTHAND SIDE OF PEDESTAL. REP AIRED IAW COEX EC 5310-01198. 2 H 7 2 4T RT A53EU 2001082100141 20010821 00141 EU 2001 8 21 C2XA01BT150 1 20010725 A 5330 DOUBLER AEROSP ATR42 ATR42320 8680930 EU FUSELAGE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14819 156 YUL---CO4372, DURING 1C INSPECTION MAINTENANCE FOUND PATCH OVERSKIN AT FRAME 25 STRINGER 15R AND 16R DAMAGED BY REFUELIN G DOOR. REPAIRED IAW ATR42 SRM 53-00-00 FIGURE 403. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001082100142 20010821 00142 SO 2001 8 21 C2XA01BT152 1 20010812 A 3260 PROXIMITY SWITCH EMB 145 EMB145LR SO NLG FAULTY A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 12922 145338 TYS---CO4148, CREW REPORTED LANDING GEAR AIR/GROUND FAIL AND ENGINE 1/2 REVERSER DISAGREE (LIGHTS CAME ON), AIR RETURNED BACK TO TYS AND LANDED UNEVENTFULLY. MAINTENANCE FOUND NOSE LANDING GEAR PROXIMITY SWITCH PROBLEM, PROPERLY INSTALLED NOSE PROXIMITY WOW SWITCH REFERENCE EMB145 MM 32-61-01. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2001082100143 20010821 00143 EU 2001 8 21 C2XA01BT153 1 20010813 A 2120 SMOKE AEROSP ATR42 ATR42320 8680930 EU COCKPIT DETECTED A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 16824 166 ACK---CO3223, CREW REPORTED ELECTRICAL SMOKE MASTER (WARNING ILLUMINATED) AND SMOKE IN COCKPIT. AIRCRAFT RETURNED TO TH E GATE. MAINTENANCE INSPECTED BOTH ENGINE COMPARTMENTS, AIR CONDITIONING PACK COMPARTMENTS, AND ELECTRICAL COMPARTMENTS AND NO DEFECTS NOTED. RAN ENGINES IAW ATR42 MM 72-00-00 AND PACKS IAW ATR42 MM 21-10-00. NO SMOKE OR DEFECTS NOTED. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001082100144 20010821 00144 EU 2001 8 21 C2XA01BT154 1 20010815 A 3234 F96GA0102 CONTROL HANDLE AEROSP ATR42 ATR42320 8680930 EU COCKPIT INTERMITTENT A C2XA O OTHER O OTHER CL CLIMB 1 SW 27 11835 194 EWR---CO3195, CREW REPORTED GEAR HANDLE STUCK IN DOWN POSITION AFTER TAKEOFF. USED RETRACTION OVERRIDE TO RETRACT THE G EAR. FLIGHT CONTINUED ON TO NEWARK, AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE FOUND LANDING GEAR SELECTOR HANDLE TO BE INTERMITTENT WOULD NOT RELEASE. REMOVED AND REPLACED LANDING GEAR SELECTOR HANDLE IAW 32-31-81. OPS CHECKED GOOD. AIR CRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001082100145 20010821 00145 SO 2001 8 21 C2XA01CL164 1 20010714 A 4920 4501968C APU EMB 145 EMB145LR SO TAIL FAILED A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 13989 271 BNA FLT 4046, THE CREW REPORTED APU AUTOSHUT DOWN CAUSING SMOKE IN AIRCRAFT. MAINTENANCE REPLACED APU. OPERATIONAL CHE CKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2001082100146 20010821 00146 SO 2001 8 21 C2XA01CL165 1 20010716 A 3350 375901 LIGHT EMB 145 EMB145ER SO CABIN INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 14939 030 CLE FLT 4270 THE CREW REPORTED FORWARD PART OF ROW 12 OVERHEAD EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2001082100147 20010821 00147 CE 2001 8 21 C2XA01CL170 1 20010721 A 2612 1013645801 PRINTED CKT BOAR BEECH 1900 1900D 1154162 CE FIRE DETECTION DEFECTIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 87551 UE206 CLE FLT 3001 THE CREW REPORTED NR 2 ENGINE FIRE LOOP WILL NOT TEST. MAINTENANCE REPLACED ANNUNCIATOR FAULT DETECTION S YSTEM PRINTED CIRCUIT BOARD. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 2001082100148 20010821 00148 SO 2001 8 21 C2XA01CL174 1 20010719 A 3234 8271011 CONTROL HANDLE EMB 145 EMB145ER SO COCKPIT FAILED A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 14940 145033 CLE FLIGHT 4051 THE CREW REPORTED ON TAKEOFF THE LANDING GEAR WOULD NOT RETRACT WITHOUT USING THE DOWNLOCK RELEASE BUTTO N. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR CONTROL LEVER. OPERATIONAL CHE CKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001082100149 20010821 00149 GL 2001 8 21 C2XA01CL175 2 20010725 A 7200 23070402 ENGINE EMB 135 EMB135ER 3260203 SO ALLSN AE300 AE3007A GL NR 1 FAILED A C2XA B A EMER. DESCENT UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 SW 27 14508 3355 3355 145220 CAE311325 CLE FLIGHT 3722 THE CREW REPORTED THE NR 1 ENGINE FAILED AT 2800 FT WITH NO ABNORMAL INDICATIONS PRIOR TO FAILURE. THE AIRCRAFT DIVERTED TO CMH AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE AND OPERATIONAL CHEC KS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001082100150 20010821 00150 EU 2001 8 21 C2XA01CL176 1 20010724 A 3350 1011309111 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST NR NOT REPORTED 1 SW 27 34820 159 CLE FLIGHT 3279 THE CREW REPORTED THE EMERGENCY AISLE PATH LIGHTING WAS INOPERATIVE AT ROW 7. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL 33-50-02. MAINTENANCE REPLACED THE EMERGENCY AISLE LIGHTING CENTER SECTION. OPERATIONAL CHECKS WERE G OOD. 2 H 7 2 4T RT A53EU 2001082100151 20010821 00151 SO 2001 8 21 C2XA01CL178 1 20010725 A 3240 429513 CONTROL UNIT EMB 145 EMB145LR SO COCKPIT DEFECTIVE A C2XA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 27 15912 460 460 145439 CLE FLIGHT 4172 THE CREW REPORTED THE BRAKES ARE GRABBING EXTREMELY HARD. MAINTENANCE REPLACED THE BRAKE CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2001082100152 20010821 00152 SO 2001 8 21 C2XA01CL182 1 20010801 A 2612 14521330405 MODULE EMB 145 EMB145LR SO COCKPIT FAULTY A C2XA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SW 27 13914 145430 CLE FLIGHT 4094 THE CREW REPORTED A APU FIRE EICAS MESSAGE INFLIGHT WITH THE APU RUNNING. THE CREW SHUT DOWN THE APU A ND CLOSED THE FUEL SOLENOID VALVE FOR THE APU AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND NO E VIDENCE OF A FIRE. REPLACED THE APU CONTROL MODULE AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SER VICE. 2 L 7 2 4T RT T00011AT 2001082100153 20010821 00153 SO 2001 8 21 C2XA01CL184 1 20010803 A 3230 355022002MOD2 CONTROL UNIT EMB 145 EMB145LR SO COCKPIT FAILED A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 19966 145131 CLE FLIGHT 4233 THE CREW REPORTED A LOUD NOISE AND VIBRATION UNDER THE FLIGHT DECK ON CLIMB OUT. RECYCLED THE LANDING G EAR AND RECEIVED A LANDING GEAR LEVER DISAGREE MESSAGE. THE GEAR WAS RECYCLED AGAIN, RECEIVED 3 GREEN DOWN AND LOCK IND ICATIONS. THE AIRCRAFT RETURNED AND LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEA R ELECTRONIC UNIT AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001082100154 20010821 00154 SO 2001 8 21 C2XA01CL185 1 20010728 A 5312 1454794403 FIREWALL EMB 135 EMB135LR SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15527 145413 CLE MAINTENANCE DURING ACCOMPLISHMENT OF SB 145-49-0009 AND 145-49-0018 MAINTENANCE FOUND THE APU FIREWALL CRACKED IN SE VERAL PLACES. THE AIRCRAFT WAS RELEASED IAW EMBRAER AUTHORIZATION GST 2630/01. MAINTENANCE REPLACED THE APU FIRE WALL. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT TOOO11AT 2001082100155 20010821 00155 WP 2001 8 21 0102939852 1 20010425 A 5344 DOOR FRAME DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 761NC 47709 During L check at Dothan, found .071" thick aluminum doubler cracked at the upper FWD corner of entry door jamb. Fabrica ted repair doublers and installed per EA98-182679. 2 L 7 2 4F RT A6WE 2001082100156 20010821 00156 SO 2001 8 21 C2XA01CL186 1 20010730 A 5312 1454794403 FIREWALL EMB 135 EMB135LR SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17524 145399 CLE MAINTENANCE DURING ACCOMPLISHMENT OF SB 145-49-009 AND 145-49-0018 MAINTENANCE FOUND THE APU FIREWALL WAS CRACKED. THE AIRCRAFT WAS RELEASED IAW EMBRAER AUTHORIZATION GST 2647/01. MAINTENANCE REPLACED THE APU FIREWALL. OPERATIONAL CH ECKS WERE GOOD OF THE APU. 2 L 7 2 4F RT TOOO11AT 2001082700296 20010827 00296 SO 2001 8 27 C2XA01CL187 1 20010803 A 5312 1454794403 FIREWALL EMB 145 EMB145LR SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16918 145397 CLE MAINTENANCE DURING ACCOMPLISHMENT OF SB 145-49-0009 AND 145-49-0018 MAINTENANCE FOUND THE APU FIREWALL WAS CRACKED. THE AIRCRAFT WAS RELEASED IAW EMBRAER AUTHORIZATION GST2706/01. MAINTENANCE REPLACED THE APU FIREWALL. OPERATIONAL CH ECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2001082700297 20010827 00297 SO 2001 8 27 C2XA01CL188 1 20010805 A 5312 1454794403 FIREWALL EMB 145 EMB145LR SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14916 145415 CLE MAINTENANCE DURING ACCOMPLISHMENT OF SB145-49-0009 AND 145-49-0018 MAINTENANCE FOUND THE APU FIREWALL WAS CRACKED. THE AIRCRAFT WAS RELEASED IAW EMBRAER AUTHORIZATION GST2711/01. MAINTENANCE REPLACED THE APU FIREWALL. OPERATIONAL CHE CKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2001082100157 20010821 00157 SO 2001 8 21 C2XA01CL190 1 20010802 A 3350 7287580501 LIGHT EMB 145 EMB145LR SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14952 145067 CLE FLIGHT 3742 THE CREW REPORTED THE EMERGENCY AISLE LIGHTING STRIP WAS OUT AT ROW 7/8. MAINTENANCE REPLACED THE LIGHT ING STRIP AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001082100159 20010821 00159 CE 2001 8 21 C2XA01CL192 1 20010807 A 6123 5038912147 SWITCH BEECH 1900 1900D 1154162 CE LT ENGINE FAULTY A C2XA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION AP APPROACH 1 SW 27 81553 324 UE222 CLE FLIGHT 3106 THE CREW REPORTED THE NR 2 PROPELLER AUTOFEATHERED ON APPROACH. THE AIRCRAFT LANDED WITHOUT FURTHER INC IDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE AUTOFEATHER LOW PRESSURE SWITCH. OPERATIONAL CHECKS WERE GOO D. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT A24CE 2001082100161 20010821 00161 EA 2001 8 21 COMA0160611 1 20010819 A 2751 7805013 LEVER CNDAIR CL600 CL6002B19 EA COCKPIT FAULTY A COMA K NONE J WARNING INDICATION DE DESCENT 1 SO 01 409CA 4879 7441 FLIGHT #5286. dURING DESCENT INTO AVP RECEIVED A FLAP FAIL CAUTION MESSAGE AT 8 DEGREE FLAP POSITION, CREW DECIDED TO DE CLARE AN EMERGECY, AIRCRAFT LANDED SAFELY.REPLACED THE FLAP CONTROL LEVER. 2 L 7 2 4F RT A21EA 2001082100162 20010821 00162 EA 2001 8 21 COMA0160610 1 20010819 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 EA A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 932CA 7038 FLIGHT #5719. DURING TAXI OUT OF CVG DISCOVERED SECOND CEILING EMERGENCY LIGHT INOPERATIVE, AIRCRAFT RETURNED TO THE GAT E.REPLACED SPENT EMERGENCY LIGHT BULB. 2 L 7 2 4F RT A21EA 2001082100165 20010821 00165 EA 2001 8 21 COMA0160609 1 20010819 A 3260 16124101 STRUT CNDAIR CL600 CL6002B19 EA LANDING GEAR FAULTY A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 932CA 4068 7038 FLIGHT #5719. AFTER TAKE OFF FROM CVG RECEIVED A GEAR DISAGREE AND NOSE GEAR DOOR OPEN MESSAGE, CREW DECLARED AN EMERGEN CY, RETURNED TO THE FIELD AND LANDED SAFELY.REPLACED THE LOWER NOSE LANDING GEAR STRUT. 2 L 7 2 4F RT A21EA 2001082100167 20010821 00167 2001 8 21 COMA0160608 4 20010818 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA A COMA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 797CA 7344 FLIGHT #5235. DURING TAXI OUT RECEIVED A STALL FAIL CAUTION MESSAGE, AIRCRAFT RETURNED TO THE GATE.RESET THE STALL PROTE CTION COMPUTER. 2 L 7 2 4F RT A21EA 2001082100168 20010821 00168 EA 2001 8 21 COMA0160607 1 20010818 A 2760 601R591473 CONTROL UNIT CNDAIR CL600 CL6002B19 EA ELECTRICAL BAY FAULTY A COMA K NONE J WARNING INDICATION CR CRUISE 1 SO 01 938CA 13122 7046 FLIGHT #5624. DURING CRUISE FLIGHT RECEIVED A GROUND LIFT DUMP MESSAGE, CREW SELECTED MANUAL DISARM AND MESSAGE CLEARED. REPLACED THE #2 SPOILER ELECTRONIC CONTROL UNIT. 2 L 7 2 4F RT A21EA 2001082100170 20010821 00170 EA 2001 8 21 COMA0160606 1 20010818 A 7930 1153P0012 SWITCH CNDAIR CL600 CL6002B19 EA RIGHT ENGINE FAULTY A COMA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 912CA 7011 FLIGHT #5967. DURING TAXI OUT RECEIVED A "CAS MISCOMP" STATUS MESSAGE, AIRCRAFT RETURNED TO THE GATE.REPLACED THE RIGHT ENGINE LOW OIL PRESSURE SWITCH. 2 L 7 2 4F RT A21EA 2001082100175 20010821 00175 EA 2001 8 21 COMA0160605 1 20010819 A 2751 860D10018 FCU CNDAIR CL600 CL6002B19 EA ELECTRICAL BAY FAULTY A COMA K NONE J WARNING INDICATION DE DESCENT 1 SO 01 409CA 1319 7441 FLIGHT #5286. DURING DESCENT INTO AVP RECEIVED A FLAP FAIL CAUTION MESSAGE AT 8 DEGREE FLAP POSITION, CREW DECIDED TO DE CLARE AN EMERGENCY, AIRCRAFT LANDED SAFELY.REPLACED THE FLAP ELECTRONIC CONTROL UNIT. 2 L 7 2 4F RT A21EA 2001082100186 20010821 00186 WP 2001 8 21 RRXA11411 1 20010714 A 5310 2772660 SEAT TRACK DOUG DC8 DC873F 302199F WP FS 690 RRL 24 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND CABIN SEA TRACK HAS BROKEN LUGS F/S 690 RBL 24. *** CORRECTIVE ACTION *** REMOVED DAMA GED SECTION OF SEAT TRACK IAW 53-2-3 AND SRM 51-3-0. FABRICATED SEAT TRACK SECTION AND SPLICES IAW DC-8 SRM 53-2-3 FIG 8A. TREATED AND PRIMED IAW DC8 SRM 51-2-8. INSTALLED SEAT TRACK AND SPLICES IAW DC8 SRM 53-2-3 FIG 8A. 2 L 7 4 4F RT 4A25 2001082100187 20010821 00187 WP 2001 8 21 RRXA11412 1 20010714 A 5300 3754930 FITTING DOUG DC8 DC873F 302199F WP STA 1168 L33R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND C-PIT BACK UP FITTING FOR #1 LWRT LATCH HAS HEAVY CORROSION ON FWD SIDE STA 1168 BETWEE N L33R I/B AND L32R O/B. *** CORRECTIVE ACTION *** REMOVED BACKUP FITTING , REF SRM 51-1-20D. RECEIVED NEW FITTING AND CLIPS. TRIMMED NEW PARTS REF SRM 51-1-8. INSTALLED NEW BACKUP FITTING AND CLIPS REF SRM 51-1-20D AND CLIPS PER DC8 SR M 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 2001082100188 20010821 00188 WP 2001 8 21 RRXA11413 1 20010714 A 5310 9754022503N FITTING DOUG DC8 DC873F 302199F WP RH CUSP STA 280 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND R/H CUSP LWR FLOOR BEAM TO CUSP FITTING CRACKED STA 280. *** CORRECTIVE ACTION *** REM OVED CRACKED FITTING, INSTALLED REPLACEMENT PART IAW SRM 51-1-21 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001082100189 20010821 00189 WP 2001 8 21 RRXA11415 1 20010716 A 5310 3755897U502 FITTING DOUG DC8 DC873F 302199F WP CPIT STA 1248 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND LWR CARGO PIT C FRAME FITTING CRACKED AT L33R O/B SIDE STA 1248. *** CORRECTIVE ACTION *** REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D, 53-1-0 AND DWG 63755847 2 L 7 4 4F RT 4A25 2001082100190 20010821 00190 WP 2001 8 21 RRXA11416 1 20010716 A 5310 3750257U1 FITTING DOUG DC8 DC873F 302199F WP FS1050 L31R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND LWR CARGO COMPARTMENT C-PIT LONG SPLICE FITTING CORRODED AT STA 1050 L31R *** CORRECTI VE ACTION *** REMOVED AND REPLACED FITTING IAW DC8 SRM 53-1-0, 51-1-20D AND DWG 3750257 2 L 7 4 4F RT 4A25 2001082100191 20010821 00191 WP 2001 8 21 RRXA11417 1 20010717 A 5310 5758878 ANGLE DOUG DC8 DC873F 302199F WP FS 1040 L36 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND LWR CARGO COMPT C-PIT ATTACH ANGLE CORRODED AT STA 1040 L36. *** CORRECTIVE ACTION *** REPAIRED FRAME IAW 8110-3 APPROVED DHSK 873-510 2 L 7 4 4F RT 4A25 2001082100192 20010821 00192 WP 2001 8 21 RRXA11418 1 20010718 A 2780 5769581501 DOOR DOUG DC8 DC873F 302199F WP R/H I/B L/E WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND R/H I/B SLOT UPPER PANEL CRACKED. *** CORRECTIVE ATION *** NDT MARKED END OF CRACK REF NDT SPM 06-10-01001. OPENED SLOT DOOR IAW MM 27-80-1, STOP DRILLED CRACK PER DHSK 873-943. FABRICATED DOUBLER IAW DHS K 873-943, INSTALLED DOUBLER IAW DHSK 873-943. OPS CHECK OF SLOT DOOR ACCOMPLISHED ON NR 86548. 2 L 7 4 4F RT 4A25 2001082100193 20010821 00193 WP 2001 8 21 RRXA11419 1 20010720 A 5310 4611067N FITTING DOUG DC8 DC873F 302199F WP STA 70 L34R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND LONGERON TIE FITTING CORRODED BEYOND LIMITS AT STA 70 L34R. *** CORRECTIVE ACTION *** REMOVED AND REPLACED PER DC8 SRM 51-1-21,51-1-21D, 51-3-0 AND DWG 4611067 2 L 7 4 4F RT 4A25 2001082100194 20010821 00194 WP 2001 8 21 RRXA11420 1 20010720 A 5310 4611067N FITTING DOUG DC8 DC873F 302199F WP STA 70-78 L23R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 0 46091 DURING A MAINTENANCE VISIT FOUND AT STA 70 L23R LONGERON TIE FITTING CORRODED BEYOND LIMITS. *** CORRECTIVE ACTION *** REMOVED AND REPLACED PER DC8 SRM 51-1-21, 51-1-21D, 51-3-0 AND DWG 6464067 2 L 7 4 4F RT 4A25 2001082100195 20010821 00195 WP 2001 8 21 RRXA11425 1 20010728 A 5310 59764619 FORMER DOUG DC8 DC873F 302199F WP FS64 L22L CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND F/S 64 LBL 55 FORMER FOR L1 DOOR HAS A 1 3/4" CRACK AT L22L. *** CORRECTIVE ACTION *** STOP DRILLED CRACK IAW SRM 53-2-0 FIG 1B. FABRICATED REPAIR ANGLES IAW SRM 53-2-0 FIG 1B, INSTALLED REPAIR ANGLES IAW SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001082100196 20010821 00196 WP 2001 8 21 RRXA11426 1 20010729 A 5310 5614945501 FRAME DOUG DC8 DC873F 302199F WP STA 580 L35 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND FRAME AT STA 580 HAS CORROSION BETWEEN L35L - L35R. *** CORRECTIVE ACTION *** REMOVED AND REPLACED FRAME SECTION IAW DC8 SRM 53-2-0 FIG 2, FABBED SPLICE ANGLES AND STRAPS IAW DC8 SRM 53-2-0 FIG 2. INSTALL ED SPLICE ANGLES AND STRAPS IAW DC8 SRM 53-2-0FIG 2, 51-1-21, AND 51-1-20D. 2 L 7 4 4F RT 4A25 2001082100197 20010821 00197 WP 2001 8 21 RRXA11427 1 20010729 A 5310 3702969 LONGERON DOUG DC8 DC873F 302199F WP FS58070 L35 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND STABLONGERONS (2 EACH) AT STA 58-70, L35L AND L35R HAVE HEAVY CORROSION. *** CORRECTIV E ACTION *** LONGERONS FOUND OUT OF LIMITS PER SRM 53-2-0 FIG 1F AND SRM 53-3-3. FABRICATED 2EA REPLACEMENT LONGERONS P ER DWG 3702969 AND INSTALLED IAW DWG 3702969, DC8 SRM 53-1-0, SRM 51-1-21 AND SRM51-1-20D. 2 L 7 4 4F RT 4A25 2001082100198 20010821 00198 WP 2001 8 21 RRXA11429 1 20010729 A 5310 4611067N FITTING DOUG DC8 DC873F 302199F WP FS 70 L22R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND LONGERON TIE FITTING AT FS 70 AND L22R HAS EXFOLIATION CORROSION. *** CORRECTIVE ACTIO N *** REMOVED AND REPLACED LONGERON TIE FITTING IAW DC8 SRM 51-1-21, 51-1-20D,51-3-0 AND DWG 464067N 2 L 7 4 4F RT 4A25 2001082100199 20010821 00199 WP 2001 8 21 RRXA11430 1 20010729 A 5310 5614945 FRAME DOUG DC8 DC873F 302199F WP FS1120 L35 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND FRAME AT FS 1120 HAS HEAVY CORROSION BETWEEN LONGERONS 35L - 35R. *** CORRECTIVE ACTIO N *** CUT OUT DAMAGED AREA OF FRAME IAW SRM 53-2-0 FIG2. FRABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED IAW SRM 53 -2-0 FIG 2 2 L 7 4 4F RT 4A25 2001082100200 20010821 00200 WP 2001 8 21 RRXA11433 1 20010719 A 5310 527776604 SEAT TRACK DOUG DC8 DC873F 302199F WP FS 1030-1040 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND CABIN SEAT TRACK DAMAGED AT FS1030 TO FS 1040 RBL 24. *** CORRECTIVE ACTION *** REMOVE D, FABRICATED AND REPLACED SEAT TRACK FS 990 - FS1210 RBL24 IAW SRM 53-2-2A, 53-2-3 FIG 14, 51-1-8, 51-3-0 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2001082100201 20010821 00201 WP 2001 8 21 RRXA11436 1 20010730 A 5300 97549483 WEB DOUG DC8 DC873F 302199F WP CPIT STA 1180 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND TORQUE BOX WEB IN C-PIT HAS LITE SURFACE CORROSION AND IS MIS DRILLED. *** CORRECTIVE ACTION *** FABRICATED REPLACEMENT PER DAC DWG 9754948 AND INSTALLED PER DC8 SRM 51-1-21 AND 51-1-20D STA 1180 L31R 2 L 7 4 4F RT 4A25 2001082100202 20010821 00202 WP 2001 8 21 RRXA11438 1 20010730 A 5300 5754761502 FRAME DOUG DC8 DC873F 302199F WP STA 1140 L31 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND FRAME AT STA 1140 L31L TO L34R WITH NUMEROUS MISDRILLED HOLES. *** CORRECTIVE ACTION * ** REPLACED FRAME AT STA 1140 L31L TO L34R DUE TO MUMEROUS MISDRILLED HOLES PER DHSK 873-816 2 L 7 4 4F RT 4A25 2001082100203 20010821 00203 WP 2001 8 21 RRXA11439 1 20010730 A 5300 2772660 SEAT TRACK DOUG DC8 DC873F 302199F WP STA 160 LBL63 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND CORROSION ON SEAT TRACK AT STA 46-330 LBL63. *** CORRECTIVE ACTION *** REPLACED CORROD ED SEAT TRACK AT STA 160 LBL63 PER DC8 SRM 53-7-1 FIG 9 AND SRM 53-2-3 FIG 8A. 2 L 7 4 4F RT 4A25 2001082100204 20010821 00204 WP 2001 8 21 RRXA11440 1 20010730 A 5300 56119433 FRAME DOUG DC8 DC873F 302199F WP STA 70 L21L L21R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND CORROSION ON FRAME AT STA 70 BELOW CUSP FROM L21L TO L21R. *** CORRECTIVE ACTION *** R EPLACED STA 70 FRAME BELOW CUSP FROM L21L TO L21R DUE TO CORROSION, REF DC8 SRM 51-1-21, 51-1-21D, 51-3-0, 51-9-0, 51-1- 11, 53-2-5 AND SRO 8538006 2 L 7 4 4F RT 4A25 2001082100205 20010821 00205 WP 2001 8 21 RRXA11441 1 20010730 A 5300 3755841501 FITTING DOUG DC8 DC873F 302199F WP STA 1200 L33 L34 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND CRACKED FITTING AT STA 1200 L33R - L34R. *** CORRECTIVE ACTION *** REPLACED CRACKED FI TTING AT STA 1200 L33R TO L34R PER DC8 SRM 53-2-0 FIG 20 2 L 7 4 4F RT 4A25 2001082100206 20010821 00206 WP 2001 8 21 RRXA11442 1 20010730 A 5300 57727879 WEB DOUG DC8 DC873F 302199F WP STA 280 L21 L20 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND WEB CRACKED AT STA 280 L21L TO L20L. *** CORRECTIVE ACTION *** FABRICATED AND INSTALLE D REPLACEMENT PART PER DHSK 873948. 2 L 7 4 4F RT 4A25 2001082100207 20010821 00207 WP 2001 8 21 RRXA11444 1 20010731 A 5330 5597646 WEB DOUG DC8 DC873F 302199F WP FS 70 TRQ BOX CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND AT FS 70 WEB ON TORQUE BOX AFT SIDE OF FWD ENTRY DOOR CRACKED. *** CORRECTIVE ACTION * ** REMOVED WEB, FABRICATED AND INSTALLED WEB AND DOUBLER IAW SRM 51-1-20D, 53-2-0, 51-1-21 AND DWG 5642063 2 L 7 4 4F RT 4A25 2001082100208 20010821 00208 WP 2001 8 21 RRXA11446 1 20010802 A 5310 5779912 LONGERON DOUG DC8 DC873F 302199F WP FS550 L23L CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND LONGERON 23L AT FS 550 FWD OF APU EXHAUST IS CORRODED BEYOND LIMITS. *** CORRECTIVE AC TION *** REMOVED, FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION PER DWG 5779912 AND DC8 SRM 51-1-20D AND 53-1-0 2 L 7 4 4F RT 4A25 2001082100209 20010821 00209 WP 2001 8 21 RRXA11447 1 20010803 A 5310 5616674 WEB DOUG DC8 DC873F 302199F WP D PIT DOOR MISDRILLED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND D PIT DOOR TORQUE BOX FWD LWR WEB HAS 4 EACH MISDRILLED NUTPLATES AND DRILLED RIVIT HEA DS. *** CORRECTIVE ACTION *** REMOVED WEB, FABRICATED REPAIR AND INSTALLED IAW SRM 53-2-0 FIG 53, 53-4-1 FIG 51, 51-1-8 , 53-2-0 FIG 2, 53-2-0 FIG 1D AND DWG 5641015 2 L 7 4 4F RT 4A25 2001082100210 20010821 00210 WP 2001 8 21 RRXA11449 1 20010805 A 5330 5644981 FLOOR PANEL DOUG DC8 DC873F 302199F WP PILOT SEAT CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUNDSUB FLOOR PANEL UNDER PILOTS SEAT CRACKED 2EA PLACES. ***CORRECTIVE ACTION *** STOP DRI LLED CRACKS, TERMINATED, FABRICATED AND INSTALLED DOUBLERS IAW SRM 53-2-0 FIG 1D AND 1B, 51-1-8, 51-1-21,51-1-20D AND 06 -10-001 2 L 7 4 4F RT 4A25 2001082100211 20010821 00211 WP 2001 8 21 RRXA11450 1 20010806 A 5330 5644130 DOUBLER DOUG DC8 DC873F 302199F WP FS1620L32 L33 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND AF ACCY COMPT HEAVY CORROSION ON INTERNAL SKIN DOUBLER BETWEEN FS 1620 AND 1640 L32L L3 3L *** CORRECTIVE ACTION *** BLENDED AREA FOUND TO BE OUT OF LINITS IAW DC8 SRM 51-1-8 AND 53-2-0 FIG 1. REMOVED DAMAG ED AREA OF INTERNAL DOUBLER IAW DC8 SRM 53-2-1 FIG 7. FABRICATED AND INSTALLED DOUBLER AND FILLER PER DHSK 873-487 2 L 7 4 4F RT 4A25 2001082100212 20010821 00212 WP 2001 8 21 RRXA11451 1 20010806 A 5330 5616199 DOUBLER DOUG DC8 DC873F 302199F WP FS1620 -1640 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND AFT ACCY COMPT HEAVY CORROSION ON INTERNAL SKIN DOUBLER, AREA PREVIOUSLY BLENDED. FS 1 620 - 1640 L32R - L33R. *** CORRECTIVE ACTION *** REMOVED DAMAGED INTERNAL DOUBLER, FABRICATED AND INSTALLED PER DHSK 8 73-024. 2 L 7 4 4F RT 4A25 2001082100213 20010821 00213 WP 2001 8 21 RRXA11452 1 20010806 A 2750 27727511 LINK DOUG DC8 DC873F 302199F WP XW340 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND LH FLAP #3 ACTUATOR COMP LINKS (XW340) CORRODED ON SIDE FACE. *** CORRECTIVE ACTION ** * REMOVED CORROSION ON #3 FLAP ACTUATER LH PER SRM 27-28-7 TEMP REV 27-38. WITHIN LIMITS CAD PLATED PER DC8 OHM 2-13 2 L 7 4 4F RT 4A25 2001082100214 20010821 00214 WP 2001 8 21 RRXA11453 1 20010806 A 5310 5758878 SHEAR TIE DOUG DC8 DC873F 302199F WP FS1140 L35 L36 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND AFT PIT AT FS1140 BETWEEN LONGERON 35R AND 36 HAS SHEER TIE BLOWN OUT WITH CORROSION. *** CORRECTIVE ACTION *** CUT OUT DAMAGED SECTION OF SHEAR TIE IAW DC8 SRM 53-2-0 FIG 2A. FABRICATED REPLACEMENT SHEAR TIE AND SPLICE AND INSTALLED PER DC8 SRM 53-2-0 FIG 2A 2 L 7 4 4F RT 4A25 2001082100215 20010821 00215 WP 2001 8 21 RRXA11456 1 20010807 A 5310 52772660 SEAT TRACK DOUG DC8 DC873F 302199F WP FS 760 RBL48 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND CABIN SEAT TRACK IS CORRODED AT FS 760 RBL48. *** CORRECTIUVE ACTION *** SEAT TRACK FO UND OUT OF LIMITS PER DC8 SRM 53-2-3 FIG 12. REMOVED DAMAGED SECTION OF SEAT TRACK PER DC8 SRM 51-30-. FABRICATED SEAT TRACK AND SPLINE AND INSTALLED PER DHSK 837677 2 L 7 4 4F RT 4A25 2001082100216 20010821 00216 WP 2001 8 21 RRXA11457 1 20010807 A 5510 DHM43546287 BUSHING DOUG DC8 DC873F 302199F WP HORIZ BLKD CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND R/H WOKING BLKD OF CONSTANT SECTION OF HORIZ HAS HEAVY CORROSION. *** CORRECTIVE ACTIO N *** REMOVED CORROSION PER SRM 51-1-8, FABRICATED AND INSTALLED REPAIR BUSHING PER REF DHSK 873-297 AND CHAPTER 12 AND 13 . 2 L 7 4 4F RT 4A25 2001082100217 20010821 00217 WP 2001 8 21 RRXA11458 1 20010807 A 5310 87321615 ANGLE DOUG DC8 DC873F 302199F WP STA 35 L26-L25 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND A/C BAY R/H SIDE FRAME HAS EXFOLIATION BETWEEN L26 AND L25 STA 35. *** CORRECTIVE ACTI ON *** REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLE PER REF DHSK 873-216-15 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001082100227 20010821 00227 WP 2001 8 21 ARWA0010808 1 20010818 A 2120 BOOT DOUG DC8 DC862 3021970 WP LT RAM DUCT OUT OF ADJ A ARWA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 SO 19 810BN 45905 DURING UPLATCH CK DOORS NOT LATCHED LIGHT ILUMINATED. ACCOMPLISHED ABNORMAL CK LIST AND NO HELP. SLIGHT VIBRATION ON C OCKPIT FLOOR DURING ENTIRE FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. CHECK ADJUSTMENT LT MAIN DOOR UPLATCH MECHANISM I AW MM 32-31-4, OPS CKD IAW MM 32-30-0, FOUND NORMAL. REPOSITION BOOT AT LT RAM DUCT OF NASI FLOW CONTROL SYSTEM IAW NAS I MM 21-1-01, OPS CK NORMAL PER ST466CH STC. 2 L 7 4 4F 4A25 2001082100228 20010821 00228 EU 2001 8 21 C2XA01BT155 1 20010815 A 2160 6411343 SWITCH AEROSP ATR42 ATR42320 8680930 EU TEMP CONTROL FAULTY A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 14828 179 BDL---CO3325, CREW REPORTED DURING PREFLIGHT BURNING SMELL COMING FROM AIRCRAFT AIR CONDITIONING VENTS AND NR 2 PACK FAI L, BLEED VALVE FAIL. AIRCRAFT INSPECTED AND MAINTENANCE FERRIED TO NEWARK. AFTER ARRIVAL IN EWR, MAINTENANCE INSPECTED NR 2 AIR CYCLE MACHINE, HEAT EXCHANGER, AND ASSOCIATED DUCTING FOR DAMAGE, DEFECTS AND LEAKS, NONE NOTED. RAN NR 2 ENG INE FOR 45 MINUTES WITH NR 2 PACK SELECTED, NO SMELL OR SMOKE NOTED, DUCT TEMPERATURE BELOW 4 DEGREES CENTIGRADE COOLING SATISFACTORY. REMOVED AND REPLACED BOTH TEMPERATURE CONTROL OVER TEMPERATURE SWITCHES IAW ATR42 JIC 36-11-64. OPS CHE CKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001082100229 20010821 00229 SO 2001 8 21 C2XA01IA295 1 20010712 A 3320 7287103507 MODULE EMB 145 EMB145 SO CABIN FAULTY A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 14953 145071 MKE- WHILE AT THE GATE FLIGHT 4052 THE CREW NOTED A BURNING ODOR FROM AROUND THE FLIGHT ATTENDANT LIGHTING CONTROL PANE L. THE SYSTEM WAS PLACED ON MEL, AND THE AIRCRAFT WAS RELEASED TO SERVICE. IAH- MAINTENANCE REMOVED AND REPLACED THE CABIN LIGHTING CONTROL MODULE, PERFORMED A OPERATIONAL CHECK. NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001082100230 20010821 00230 SO 2001 8 21 C2XA01IA298 1 20010723 A 3350 3025103 LIGHT EMB 135 EMB135LR SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13955 145075 IAH - DURING C-CHECK INSPECTION, THE LEFT HAND OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R EMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT TOOO11AT 2001082100231 20010821 00231 SO 2001 8 21 C2XA01IA301 1 20010723 A 3231 12008364001 DOOR EMB 120 EMB120ER 3260203 SO LT MLG UNLATCHED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 27716 120128 ACT - FLIGHT 2943, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO ACT WITHOUT INCI DENT, WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LEFT HAND MAIN LANDING GEAR DOOR TO BE UNLATCHED. MAINTENA NCE LATCHED THE GEAR DOOR, OPERATIONAL CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001082100232 20010821 00232 2001 8 21 C2XA01IA305 4 20010726 A 2350 509111 CONTROL PANEL EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 16723 120169 AEX- WHILE PARKED AT THE GATE THE CREW NOTED THAT THE CAPT AUDIO PANEL WAS SMOKING. AEX- MAINTENANCE SWAPPED THE CAPT S AUDIO CONTROL PANEL WITH THE F/O`S AUDIO CONTROL PANEL, AND THE AIRCRAFT WAS RELEASED IAW MEL. IAH- MAINTENANCE PLAC ED THE AUDIO CONTROL PANELS IN THEIR ORIGINAL POSITIONS AND REMOVED AND REPLACED THE CAPT`S AUDIO CONTROL PANEL. PERFOR MED A OPERATIONAL CHECK, NO DEFECTS NOTED. CLEARED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001082100233 20010821 00233 SO 2001 8 21 C2XA01IA308 1 20010806 A 5315 14521699001 FLOORBEAM EMB 145 EMB145LR SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16944 145045 IAH - DURING C-CHECK INSPECTION, THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REPAIRED TH E AFFECTED SECTION OF OMEGA BEAM IN ACCORDANCE WITH EMB-145 SRM 53-21-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SE RVICE. 2 L 7 2 4T RT T00011AT 2001082100234 20010821 00234 SO 2001 8 21 C2XA01IA309 1 20010806 A 5320 14522226003 GUSSET EMB 145 EMB145LR SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16944 145045 IAH - DURING C-CHECK INSPECTION, THE RIGHT HAND DIGITAL RECESS CENTER GUSSET WAS FOUND TO BE CORRODED. MAINTENANCE REMO VED AND REPLACED THE AFFECTED GUSSET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001082100235 20010821 00235 SO 2001 8 21 C2XA01IA310 1 20010806 A 5320 13500095003 CHANNEL EMB 145 EMB145ER SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16944 145045 IAH - DURING C-CHECK INSPECTION, THE RIGHT HAND DIGITAL RECESS HAT SECTION WAS FOUND TO BE CORRODED. MAINTENANCE REMOVE D AND REPLACED THE AFFECTED HAT SECTION, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001082100236 20010821 00236 NE 2001 8 21 C2XA01IA312 2 20010803 A 7314 5009986C PUMP EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NR 2 ENGINE FAULTY A C2XA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 27 16729 11344 4904 120185 115314 IAH - FLIGHT 3050, THE CREW REPORTED THAT THE NUMBER TWO ENGINE EXPERIENCED A SUDDEN POWER LOSS DURING CLIMBOUT. THE AI RCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE DRIVEN FUEL PUMP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2001082100237 20010821 00237 EU 2001 8 21 C2XA01IA314 1 20010807 A 2435 8260121 STARTER GEN AEROSP ATR42 ATR42320 8680930 EU RT ENGINE FAILED A C2XA A UNSCHED LANDING J H B WARNING INDICATION ELECT. POWER LOSS-50 PC SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 97841 17596 199 280 THE NUMBER TWO DC GEN FAULTED IN FLIGHT WITH BUS TWO FALLING OFFLINE WITH ALL ASSOCIATED EQUIPMENT. DUR APPROACH GREEN HYD SYS LO PRESSURE INDICATOR ILLUMINATED. THE CREW MANUALLY EXTENDED THE GEAR, LANDED WITHOUT INCIDENT. ON LANDING T HE NOSEWHEEL STEERING WAS INOP WITH NO WARNINGS, AFTER SELECTING HYD CROSSFEED THE GREEN SYS CAME TO NORMAL PRESSURE, AN D THE STEERING BEGAN OPERATION. AFTER TAXIING CLEAR OF RUNWAY 15L THE CREW REPORTED SMOKE IN THE COCKPIT. MX INSPECTED THE ACFT AND REMOVED AND REPLACED THE NUMBER TWO DC GENERATOR, PERFORMED OPERATIONAL CHECKS OF THE AFFECTED SYSTEMS WIT H NO DEFECTS NOTED. THE ACFT WAS THEN TEST FLOWN SATISFACTORILY, AND SUBSEQUENTLY APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001082100238 20010821 00238 SO 2001 8 21 C2XA01IA315 1 20010802 A 3350 7287580501 LIGHT EMB 145 EMB145LR SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14952 145067 CLE - FLIGHT 3742, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE AISLE PATH EMERGENCY LIGHTS AT ROWS EIGHT AND NINE WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT STRIP AND THE AIRCRAFT WAS APPROV ED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001082100239 20010821 00239 SO 2001 8 21 C2XA01IA327 1 20010809 A 3350 7287580501 LIGHT EMB 145 EMB145LR SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15980 145202 DAY - DURING MAINTENANCE INSPECTION, THE AISLE PATH EMERGENCY LIGHTS AT ROWS 12-15 WERE FOUND TO BE INOPERATIVE. MAINTE NANCE INSPECTED THE AIRCRAFT AND PLACED THE AFFECTED SECTION OF LIGHT STRIP ON MEL 33-50-00-2 CAT C, CONTROL NUMBER 0146 39, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 08/11/01 THE AIRCRAFT RETURNED TO EWR WHERE MAINTENANCE REM OVED AND REPLACED THE EMERGENCY LIGHT STRIP AT ROWS 12 THRU 15. REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETU RN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001082100240 20010821 00240 EU 2001 8 21 C2XA01IA332 1 20010817 A 3350 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14833 188 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT REAR AISLE PATH LIGHTS WERE INOPERATIVE. MAINTENANCE PLACED THE AFFECTED BULBS ON MEL 33-50-02/C CONTROL NUMBER 014846, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001082100241 20010821 00241 SO 2001 8 21 C2XA01TY098 1 20010719 A 5315 14521721009 FLOORBEAM EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14508 145220 TYS DURING A SCHEDULED INSPECTION THE FORWARD DIGITAL PLATE, LOCATED JUST AFT OF COCKPIT ENTRANCE WAS FOUND TO HAVE SEV ERAL AREAS OF CORROSION. MAINTENANCE ACCOMPLISHED THE DOUBLER REPAIR IAW EMB GST 2405-01, THE REPAIR WAS SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001082100242 20010821 00242 SO 2001 8 21 C2XA01TY099 1 20010719 A 5313 13500400017 STRINGER EMB 135 EMB135ER 3260203 SO FUSELAGE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14508 145220 TYS DURING A SCHEDULED INSPECTION, STRINGER 19L BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE CHAFED. MAINTENANCE ACCOMPLIS HED THE BLEND OUT REPAIR IAW EMB GST 2412/01, THE REPAIR WAS SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001082100243 20010821 00243 GL 2001 8 21 C2XA01TY100 2 20010727 A 7200 AE3007A1P ENGINE EMB 145 EMB145 SO ALLSN AE300 AE3007A GL LEFT FAILED A C2XA A UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 SW 27 14993 4673 4673 145289 CAE311159 CLT FLIGHT 4083. CREW REPORTED THAT THE LEFT HAND ENGINE FAILED IN FLIGHT, ATTEMPTED RESTARTS WERE UNSUCCESSFUL. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE ENGINE TO BE SEIZED-UP AND METAL ON THE CHIP DETECTORS. THE ENGINE WAS REMOVED AND REPLACED IAW CONTINENTAL EXPRESS TASK CARD 627100 1, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001082100244 20010821 00244 SO 2001 8 21 C2XA01TYS101 1 20010812 A 3260 852701 PROXIMITY SENSOR EMB 145 EMB145 SO NLG CRACKED A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 12922 2118 2118 145338 TYS FLIGHT 4148, RECEIVED A LANDING GEAR AIR/GROUND FAULT DURING CLIMBOUT. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTH ER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NOSE GEAR PROXIMITY SENSOR FACE TO BE CRACKED. THE SENSO R WAS REMOVED AND REPLACED, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001082100245 20010821 00245 NM 2001 8 21 01FEDA00745 1 20010815 A 5330 SKIN BOEING 727 727247 138408F NM A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 N0901 CORROSION (TASK NO C53-132-01-1) ON EXTERNAL SKIN AROUND FASTENER HOLES FROM BS 700 - 720+10 STR 24R TO 27L (M ARKED). S/D COMING ***** 2 L 7 3 4F A3WE 2001082800147 20010828 00147 NM 2001 8 28 01FDEA00746 1 20010820 A 5313 STRINGER BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 CORROSION ON STR 26R BS 720E +10 TO 720D +11. REMOVED AND REPLACED STRINGER PER SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 2001082800149 20010828 00149 NM 2001 8 28 01FDEA00748 1 20010817 A 5313 STRINGER BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 CORROSION ON STR 27R BS 720F + 10 THROUGH 740 (FUSE 295). REMOVED AND REPLACED STRINGER. 2 L 7 3 4F A3WE 2001082100246 20010821 00246 WP 2001 8 21 CALA0100658 1 20010717 A 3350 AD4002P BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 57837 49582 INSPECTION FOUND THE OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT ROWS 22-26. THE EMERGENCY LIGHT BATTERIES WERE REMOVED AN D REPLACED IAW MM 33-53-00 AND OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 2001082100247 20010821 00247 NM 2001 8 21 CALA0100659 1 20010717 A 5711 SPAR BOEING 737 7373T0 1384582 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14358 23943 INSPECTION FOUND A CRACK INDICATION IN NR 2 HOLE OF LT WING REAR SPAR UPPER CHORD AT GEAR BEAM CASTING ATTACH POINT. TH E HOLE WAS REAMED AND THE CRACK WAS FOUND TO EXCEED 0.500 INCH MAX REAM LIMIT. THE REAR SPAR UPPER CHORD WAS REMOVED AN D REPLACED FROM INBOARD END TO RSS 284 USING A SPLICE REPAIR IAW ECRA 5720-01855 AND ECRA 5360-01059. 2 L 7 2 4F RT A16WE 2001082100248 20010821 00248 NM 2001 8 21 CALA0100664 1 20010720 A 3350 20121 CHARGER BOEING 737 737524 1384721 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17640 28901 THE EMERGENCY LIGHT BATTERY PACK AT STA 727C, LBL 68 WOULD NOT CHARGE OR TEST. THE CHARGER AND BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-51. 2 L 7 2 4F RT A16WE 2001082100249 20010821 00249 WP 2001 8 21 CALA0100665 1 20010722 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND CABIN SUBFLOOR PUNCTURED AT FS 160, RBL 12 AND FS 180, RBL 10. THE PUNCTURED AREAS WERE REMOVED IAW SR M 53-01, FIGURE 1. A REPAIR DOUBLER AND FILLER WERE INSTALLED AT EACH LOCATION IAW SRM 53-01, FIGURE 1, 51-10-3, 51-30- 1, AND 51-30-2. 2 L 7 2 4F A6WE 2001082100250 20010821 00250 WP 2001 8 21 CALA0100666 1 20010722 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND A 3 INCH CRACK IN FORWARD ENTRY CUSP WEB AT FS 158, RBL 3. THE CRACKED AREA WAS CUT OUT AND A REPAIR D OUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 2001082200001 20010822 00001 WP 2001 8 22 USAAD01145 1 20010802 A 3200 833703 SENSOR DOUG DC9 DC981 3022081 WP NLG BAY INOPERATIVE A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 19 826US 48026 RSW-CLT - FLT 714 - THE RED NOSE GEAR LIGHT ILLUMINATED AFTER LANDING GEAR RETRACTION. THE CHECK LIST PROCEDURES WERE A CCOMPLISHED, HOWEVER, THE NOSE GEAR LIGHT REMAINED ON FOR THE REST OF THE FLIGHT. THE LANDING GEAR INDICATED NORMAL WHE N THE LANDING GEAR WAS EXTENDED FOR LANDING. MAINTENANCE REMOVED AND REPLACED D1-31 POSITION SWITCH. OPERATIONALLY CHE CKED OK. (M) 2 L 7 2 4F A6WE 2001082200002 20010822 00002 EU 2001 8 22 USAAF01062 1 20010802 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU PAX CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 864US 11306 PIT - THE FORWARD FLOOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED A BATTERY PACK. OPERATIONALLY CH ECKED OK. (M) 2 L 7 2 4F RT 2001082200003 20010822 00003 NM 2001 8 22 USAABB01080 1 20010806 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 631AU 27809 BWI - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 26 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2001082200004 20010822 00004 WP 2001 8 22 USAAD01144 1 20010802 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 807US 48039 TPA - THE EMERGENCY PACK WILL NOT TEST ROW 11. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONALLY CHECKE D OK. (M) 2 L 7 2 4F A6WE 2001082200005 20010822 00005 NM 2001 8 22 USAASB01220 1 20010802 A 3350 6104789 BATTERY PACK BOEING 737 7372B7 1384560 NM CARGO COMPT INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 278AU 22890 TPA - DURING OVERNIGHT CHECK, MAINTENANCE FOUND BOTH AFT EXTERIOR ESCAPE SLIDE EMERGENCY LIGHTS INOPERATIVE. MAINTENANC E REMOVED AND REPLACED THE BATTERY PACK IN THE AFT CARGO COMPARTMENT, RIGHT SIDE. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A16WE 2001082200006 20010822 00006 WP 2001 8 22 USAAD01146 1 20010805 A 3350 873100191 RECEIVER DOUG DC9 DC981 3022081 WP PAX CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 803US 48035 CLT - THE AFT OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMEREGNCY LIGHTS REMOT E RECEIVER. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F A6WE 2001082200007 20010822 00007 NE 2001 8 22 VNAA0108001 2 20010108 A 7200 A5651 GOVERNOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE FAILED A VNAA O OTHER O OTHER CL CLIMB 1 GL 07 458PS 3068 PHL - FLT 4152 - DURING CLIMB-OUT PASSING THROUGH 18,000 FEET, THE RIGHT ENGINE STARTED TO SURGE 6 TO 7 PERCENT. THE CR EW REFERENCED THE QUICK REFERENCE HANDBOOK, CALLED MAINTENANCE CONTROL, THEN RETURNED TO PHL. MAINTENANCE INSPECTED AND REPLACED THE OVERSPEED GOVERNOR IAW DORNIER MM 72-00-00. OPS CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR S ERVICE. (M) 2 H 7 2 4T 4 T RT A45NM E20NE 2001082200008 20010822 00008 NM 2001 8 22 GAIA01286OP 1 20010728 A 2700 10607916 INDICATOR BOEING 727 727223 1384074 NM INSTRUMENT PANEL INOPERATIVE A GAIA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 6808 19483 FLT 302 - GEG-SEA - ON DEPARTURE, INBOARD FLAPS FAILED TO RETRACT FROM TAKEOFF SETTING. AIRCRAFT MADE AN UNEVENTFUL RET URN LANDING AT GEG. FOUND INBOARD FLAP POSITION INDICATOR INOPERATIVE. REMOVED AND REPLACED INBOARD FLAP POSITION INDI CATOR. OPS CHECK OF INDICATOR AND SYSTEM CHECKS GOOD PER B727 MM 27-52-21. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001082200009 20010822 00009 NM 2001 8 22 GAIA01289ST 1 20010806 A 5500 HINGE PIN BOEING 727 727251 138408H NM HORIZ STABILIZER CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED WHILE COMPLYING WITH BOEING ALERT LETTER M-7200-01-01732, FOUN D LEFT HORIZONTAL STAB INNER HINGE PIN CRACKED. REPLACED LEFT INNER STAB HINGE PIN IAW BOEING SERVICE BULLETIN B727-55- 86. (M) 2 L 7 3 4F A3WE 2001082200010 20010822 00010 NM 2001 8 22 GAIA01288ST 1 20010806 A 5340 SEAT TRACK BOEING 727 727251 138408H NM BS 480-625 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING AN LTC INSPECTION AT FLIGHSTAR, IT WAS DISCOVERED SEAT TRACK AT RBL 24.75 IS CORRODED FROM BS 480-520 AND CHAFFED UNDER PALLET LOCK LOCATION BS 610-625. ACCOMPLISHED SEAT TRACK REPAIR IAW B727 SRM 53-10-5 FIG 1. (M) 2 L 7 3 4F A3WE 2001082200011 20010822 00011 NM 2001 8 22 GAIA01287ST 1 20010806 A 5300 SEAT TRACK BOEING 727 727251 138408H NM BS 620-640 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED CORROSION ON SEAT TRACK BS 620-640 AND CHAFED BS 610-620 UNDER PALLET LOCK LOCATION RBL 45.50. ACCOMPLISHED SEAT TRACK REPAIR IAW B727 SRM 53-10-5 FIG 3. (M) 2 L 7 3 4F A3WE 2001082200012 20010822 00012 EU 2001 8 22 USAAF01029 1 20010526 A 2900 D71811403 TUBE FOKKER F28 F28MK0100 4990807 EU TAIL SECTION CRACKED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 857US 11289 PIT-CLT - FLT 347 - AFTER TAKEOFF, A VERY STRONG ODOR OF SKYDROL WAS NOTED IN THE CABIN. FLIGHT RETURNED TO THE FIELD I N PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A CRACKED FLAIR ON THE RIGHT HYDRAULIC LINE TO THE PRESSUR E FILTER. REPLACED THE CRACKED LINE. PERFORMED HIGH POWER ENGINE RUN. LEAK CHECKED GOOD. NO ODOR WAS DETECTED. OK F OR SERVICE. (M) 2 L 7 2 4F RT 2001082200013 20010822 00013 NM 2001 8 22 USAABB01075 1 20010802 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 622AU 27201 CLT - FOUND FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE AT ROWS 1 AND 18. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2001082200014 20010822 00014 NM 2001 8 22 USAABB01076 1 20010802 A 3350 9221009 BATTERY BOEING 757 7572B7 1384964 NM R3 DOOR INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 622AU 27201 CLT - FOUND R3 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2001082200015 20010822 00015 EU 2001 8 22 USAAF01047 1 20010715 A 4900 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU PAX CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 867US 11312 IND - THE RIGHT OVERWING EMERGENCY EXIT LIGHTS AND THE FLOOR EMERGENCY LIGHTS IN ROW 4-8 WERE FOUND INOPERATIVE. MAINTE NANCE REPLACED BATTERY PACKS. OPS CHECKED OK. (M) 2 L 7 2 4F RT 2001082200016 20010822 00016 EU 2001 8 22 USAAF01046 1 20010713 A 4900 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU PAX CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 898US 11398 CLT - THE AFT FLOOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK FOR THE FLOOR EMERGENCY LIGHTS. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT 2001082200017 20010822 00017 EU 2001 8 22 USAAF01044 1 20010712 A 2611 SA308 SMOKE DETECTOR FOKKER F28 F28MK0100 4990807 EU LAVATORY MALFUNCTIONED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 898US 11398 ATL-CLT - FLT 536 - AFTER TAKEOFF AND CLIMBING THROUGH FL090, FLIGHT ATTENDANTS REPORTED SMOKE ALARMS IN BOTH AFT LAVATO RIES WERE RINGING. NO SMOKE WAS NOTICED. THE FLIGHT RETURNED TO FIELD AS A PRECAUTION, AND LANDED WITHOUT INCIDENT. M AINTENANCE REPLACED SMOKE DETECTORS IN BOTH LAVATORIES. OPS CHECKED OK. (M) 2 L 7 2 4F RT 2001082200021 20010822 00021 NM 2001 8 22 DHL2001724008 1 20010818 A 3260 656021132 ACCESSORY UNIT BOEING 727 727228 NM DEFECTIVE A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 724DH 19862 1) ON TAKE OFF, GEAR UNSAFE WARNING HORN SOUNDED WHEN GEAR HANDLE WAS SELECTED TO THE 'UP' POSITION. RETURNED TO MTY.2) TROUBLESHOT LANDING GEAR POSITION WARNING SYSTEM IAW WDM 32-64-03. REMOVED & REPLACED THE LANDING GEAR ACCESSORY UNIT .STATUS: CLOSED 2 L 7 3 4F A3WE 2001100100089 20011001 00089 WP 2001 10 1 SABA010042 2 20010818 A 7310 8975131 FILTER BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE331* 01514 WP LT ENGINE DIRTY A SABA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 33 963AE 963 P66102C AIRCRAFT 963 ON FLIGHT 5121 CLT TO HKY. DURING TAKEOFF ROLL THE LEFT ENGINE FUEL FILTER BYPASS LIGHT ILLUMINATED. TAKE OFF WAS ABORTED. NO EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO THE GATE WITH NO OTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE FUEL FILTER. GROUND AND OPS CHECK WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 3 T RT A56EU E2WE 2001082800146 20010828 00146 NM 2001 8 28 01FDEA00743 1 20010815 A 5311 FRAME BOEING 727 727247 138408F NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 FOUR DENTS IN FRAME FLANGE AT BS 580 BET STR 22L - 25L. REMOVED AND REPLACED FRAME PER SRM 51-30-2. 2 L 7 3 4F A3WE 2001082200022 20010822 00022 NM 2001 8 22 01FDEA00744 1 20010811 A 5330 SKIN BOEING 727 727247 138408F NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 WHILE WORKING CARD 7-5310-7-2301G2 PT 1 FOUND DAMAGED FASTENER HOLES. REPAIRED PER SRM 53-30-03 FIG 3A. 2 L 7 3 4F A3WE 2001082800150 20010828 00150 NM 2001 8 28 01FDEA00749 1 20010818 A 5313 STRINGER BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 CORROSION IN BOTTOM OF STR 27L BS 950E +16. REMOVED AND REPLACED STR PER SRM 53-10-1 FIG 1. 2 L 7 3 4F A3WE 2001082800154 20010828 00154 NM 2001 8 28 01FDEA00750 1 20010819 A 5315 FLOORBEAM BOEING 727 727247 138408F NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 THREE CRACKED HOLES IN BS 344 FLOORBEAM WEB. *S/D* REMOVED AND REPLACED FLOORBEAM WEB PER SRM 51-40-2. 2 L 7 3 4F A3WE 2001082800155 20010828 00155 NM 2001 8 28 01FDEA00751 1 20010819 A 5310 CREASE BEAM BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 CORROSION ON UNDERSIDE OF CREASE BEAM WEB BS 344 LBL 65 WL 208. REMOVED AND REPLACED CREASE BEAM WEB PER SRM 51-40-2 FIG 1. 2 L 7 3 4F A3WE 2001082800156 20010828 00156 NM 2001 8 28 01FDEA00752 1 20010818 A 5320 SPLICE BOEING 727 7272D4 138407U NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 CORROSION (C53-113-01,1) ON STR 27R AT BS 482. REMOVED AND REPLACED SPLICE PER SRM 51-10-2, 51-20-4, 51-30-2. 2 L 7 3 4F A3WE 2001083000946 20010830 00946 NM 2001 8 30 01FDEA00753 1 20010818 A 5311 FRAME BOEING 727 7272D4 138407U NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 UPPER FLANGE AT BS 640 FRAME IS CRACKED AT FLOOR SUPPORT ATTACH POINT AT RBL 2.5 & LBL 2.5 WL 155. REMOVED AND REPLACED PER SRM 51-40-3. 2 L 7 3 4F A3WE 2001082800157 20010828 00157 NM 2001 8 28 01FDEA00754 1 20010818 A 5311 FRAME BOEING 727 7272D4 138407U NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 BS 660 FRAME UPPER FLANGE CRACKED AT FLOOR SUPPORT ATTACH POINTS, RB. 8.5 WL 155. REMOVED AND REPLACED UPPER FLANGE PER SRM 51-40-3. 2 L 7 3 4F A3WE 2001082800148 20010828 00148 NM 2001 8 28 01FDEA00747 1 20010820 A 5320 SPLICE BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 CORROSION AROUND FASTENERS BS 1177 WL 208 1 INCH I/B OF SKIN (UNDERSIDE). REMOVED AND REPLACED SPLICE ANGLE PER SRM 53-1 0-1, 51-30-1. 2 L 7 3 4F A3WE 2001082800158 20010828 00158 NM 2001 8 28 01FDEA00755 1 20010820 A 5230 HINGE BOEING 727 727227 1384078 NM CARGO DOOR GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 479FE 21461 TOP HINGE AT MID POINT HAS A HINGE LOBE W/DEEP GOUGE GROOVE IN IT. REMOVED AND REPLACED HINGES PER DWG B72-53-070 & EA 7 -5230-59057 & EO 7-5230-7-5000. 2 L 7 3 4F A3WE 2001082800159 20010828 00159 NM 2001 8 28 01FDEA00756 1 20010820 A 5210 HINGE BOEING 727 727227 1384078 NM DOOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 479FE 21461 HINGE HAS SEVERAL LOBES ON DOOR AND ACFT WITH ELONGATED HINGE PIN HOLES. REMOVED AND REPLACED PER EA 7-5230-59057 & EO 7 -5230-7-5000. 2 L 7 3 4F A3WE 2001082200025 20010822 00025 NM 2001 8 22 01FDEA00757 1 20010820 A 5230 HINGE BOEING 727 727227 1384078 NM CARGO DOOR CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 479FE 21461 TOP FWD HINGE SEGMENTS ARE RUBBING HARD, DOOR SIDE AND FUSELAGE SIDE. 2 L 7 3 4F A3WE 2001082200027 20010822 00027 NM 2001 8 22 01FDEA00758 1 20010820 A 2710 AILERON DOUG MD11 MD11F 3023600 NM RT WING MALFUNCTIONED A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 603FE 48459 AILERON DEFLECT DISAGREE LIGHT ILLUM'D LEVEL 2 ALERT ON FLAP RETRACTION. COMPLETED QRH PROCEDURES, LIGHT REMAINED ILLUM 'D. CONFIG PAGE SHOWED RIGHT OUTBOARD AILERON EXTENDED. HARD RIGHT AILERON CONTROL REQ'D THIS INPUT ALL THE WAY TO TOU CHDOWN. 2 L 7 3 4F RT A22WE 2001082200031 20010822 00031 NM 2001 8 22 01FDEA00759 1 20010819 A 3241 6005342 CONTROL UNIT DOUG MD11 MD11F 3023600 NM ANTI SKID SYS FAILED A FDEA L A ABORTED APPROACH UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 25 604FE 48460 LEFT ANTI SKID FAIL ALERT ON SHORT FINAL TO SFS HEAVY RAIN AND WET RUNWAY. EXERCISED GO-AROUND AND DIVERTED TO RPLL. G OT SAME A/S ALERT. RAN RED TAB AND LANDED AT RPLL. REMOVED AND REPLACED A/S CONTROL UNIT PER MM 32-45-01-4 & PERF'D R- T-S TEST PER MM 32-45-01-5, ALL PASSED. 2 L 7 3 4F RT A22WE 2001082200035 20010822 00035 NM 2001 8 22 2001UALA00961 1 20010605 A 3260 189915 UPLOCK SENSOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT MLG FAILED A UALA K NONE N FALSE WARNING CL CLIMB 1 WP 29 7292U 21570 AFTER GEAR RETRACTION LEFT MLG RED UNSAFE INDICATION ILLUMINATED WITH GEAR HANDLE IN EITHER OFF OR UP POSITION. *S/D* FOUND LEFT MLG UPLOCK SENSOR OPEN. REPLACED SENSOR AND GEAR LIGHTS NORMAL DURING OPERATIONAL CHECK. 2 L 7 3 4F 4 F A3WE E2EA 2001082200039 20010822 00039 NM 2001 8 22 2001UALA01402 1 20010717 A 2420 MR24236 CIRCUIT BREAKER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT FAULTY A UALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 WP 29 314UA 23675 ACFT RETURNED TO FIELD DUE TO NR 1 GEN PROBLEMS. ON CLIMB, FLIGHT REPORTED LOSS OF NR 1 GEN BUS & SUSTAINED LOSS OF CAP TAINS INSTRUMENTS: BOTH CAPT'S EFIS DISPLAYS WENT BLANK, NR 1 GEN BUS OFF LIGHT ILLUM, NR 1 TRANSFER BUS OFF LIGHT ILLU M AND C819 NR 1 TRANSFER BUS NORMAL C/B POPPED. *S/D* MX PERSONNEL COULD NOT DUPLICATE ON THE GROUND. THE FOLLOWING W AS REPLACED: R349 NR 1 TRANSFER BUS CONTROL RELAY, R350 NR 2 TRANSFER BUS CONTROL RELAY, 801 NR 1 GEN POWER CIRCUIT BREA KER, C819 NR 1 TRANSFER BUS NORMAL BREAKER, P5-4 CONTROL MODULE, AND T4 CURRENT TRANSFORMER. WIRING WAS ALSO CHECKED BE TWEEN C819 AND R3 N R1 TRANSFER RELAY, C820 NR 1 TRANSFER BUS ALTERNATE BREAKER AND R3, AND AT THE T212J TERMINAL STRIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082200041 20010822 00041 NM 2001 8 22 2001UALA01407 1 20010718 A 3260 PROXIMITY SWITCH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT MLG MALFUNCTIONED A UALA K NONE N FALSE WARNING DE DESCENT 1 WP 29 7272U 21419 LEFT MAIN GEAR INDICATION LIGHT ILLUMINATED DURING DESCENT. LANDED WITHOUT INCIDENT. REPLACED A9 CARD AND DOWNLOCK POS ITION PROXIMITY SWITCH. OPS CHECK CHECKED NORMAL. NO OTHER OBVIOUS DISCREPANCIES. 2 L 7 3 4F 4 F A3WE E2EA 2001082200042 20010822 00042 SO 2001 8 22 C2XA01CL193 1 20010818 A 3600 8151138 HOSE EMB 145 EMB145ER SO BLOWN A C2XA B E EMER. DESCENT ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 SW 27 17928 145007 CLE FLIGHT#3860 THE CREW SHUT DOWN THE #1 ENGINE ON LANDING INTO CLEVELAND DUE TO A #1 ENGINE BLEED LEAK WARNING AND PRE SSURIZATION PROBLEM.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND FOUND THE BLEED DUCT HOSE HAD BLOWN OFF BETWEEN THE ACM AND THE HEAT EXCHANGER FOR THE # 1 PACK.THE HOSE WAS REPLACED AND OPERATIONAL CHECKS WERE GOO D.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001082200043 20010822 00043 NM 2001 8 22 2001UALA01408 1 20010713 A 3242 211473U1 BRAKE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 SMOKE A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 WP 29 7457U 21911 TOWER REPORTED SMOKE COMING FROM THE LANDING GEAR DURING LANDING. *S/D* NR 2 BRAKE HAD BEEN REPLACED FLIGHT PRIOR. PO SSIBLE THAT SMOKE DUE TO RESIDUAL HYD FLUID FROM ACCOMPLISHMENT OF BRAKE CHANGE. BRAKE INSPECTED AND TESTED NORMAL. NO FURTHER ACTION TAKEN. 2 L 7 3 4F 4 F A3WE E2EA 2001082200046 20010822 00046 NM 2001 8 22 2001UALA01527 1 20010726 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 190UA 26879 EMERGENCY EEL LIGHT INOP UNDER CLOSET JUST FORWARD OF LAV 104. *S/D* REPLACED EEL STRIP, CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2001082200047 20010822 00047 NM 2001 8 22 2001UALA01559 1 20010731 A 5610 WINDOW BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT LEAKING A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 26UA 23958 UNSCHEDULED LANDING DUE TO FLIGHT OFFICER'S SLIDING WINDOW LEAKING. *S/D* WINDOW WAS REMOVED AND REINSTALLED. HAS NO HISTORY OF PREVIOUS LEAKS. HAS BEEN FLYING WITHOUT PROBLEMS SINCE WINDOW REINSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082200048 20010822 00048 NM 2001 8 22 2001UALA01593 1 20010802 A 3250 CONTROL CABLE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NLG STEERING OBSTRUCTED A UALA A UNSCHED LANDING F FLT CONT AFFECTED TX TAXI/GRND HDL 1 WP 29 7281U 21559 CREW REPORTS STEERING TILLER BINDS, ESPECIALLY IN A LEFT TURN. *S/D* FOUND OBSTRUCTION IN NOSE METERING VALVE CABLE SY STEM. CLEARED OBSTRUCTION AND INSPECTED CABLE SYSTEM. OPS CHECKS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001082200052 20010822 00052 EU 2001 8 22 SIMA200121401 1 20010802 A 2900 497682 HOSE SAAB SF340 340B 7860101 EU NOSE GEAR W/W BROKEN A SIMA K NONE K FLUID LOSS CR CRUISE 1 SW 21 272AE 340B272 ICT - FLT 3750 - CREW REPORTED THE HYDRAULIC LIGHT CAME ON IN FLIGHT. CREW HAD TO BLOW THE LANDING GEAR DOWN FOR LANDIN G. MAINTENANCE FOUND A BROKEN LINE AT THE NOSE LANDING GEAR RETRACT ACTUATOR LINE WAS REMOVED AND REPLACED IAW SAAB MM. LEAK CHECK WAS GOOD, MAIN LANDING GEAR EXPLOSIVE BOLTS WERE REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001082200053 20010822 00053 EA 2001 8 22 MASA01057 1 20010623 A 2100 AE0804AA1 FAN CNDAIR CL600 CL6002B19 EA BURNED OUT A MASA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 27172 7172 FLT 6583 - CMH-BDL - PILOT REPORTED SMOKE IN THE COCKPIT. THE PILOT DIVERTED TO AVP AFTER DECLARING AN EMERGENCY. MAIN TENANCE DISCOVERED THAT THE DISPLAY COOLING FAN WAS THE CAUSE OF THE SMOKE. MAINTENANCE REPLACED THE FAN. THE PLANE WA S FERRIED TO CMH TO HAVE THE OXYGEN GENERATORS REPLACED. (M) 2 L 7 2 4F RT A21EA 2001082200054 20010822 00054 EA 2001 8 22 MASA01082 1 20010802 A 3300 1317 LAMP CNDAIR CL600 CL6002B19 EA INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7305V 7305 FLT 6700 - DURING ROUTINE MAINTENANCE IT WAS DISCOVERED THAT THE FORWARD EXTERIOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE RELAMPED. OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001082200055 20010822 00055 NM 2001 8 22 GAIA01283ST 1 20010806 A 5315 FLOORBEAM BOEING 727 727251 138408H NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING AN TLC INSPECTION, IT WAS DISCOVERED BS 680 FLOORBEAM UPPER CHORD CORRODED AT RBL 2-LBL 24, WL 208. ACCOMPLISHED FLOORBEAM UPPER CHORD REPAIR IAW B727 SRM 53-10-8, FIG 3. (M) 2 L 7 3 4F A3WE 2001082200056 20010822 00056 NM 2001 8 22 GAIA01282ST 1 20010806 A 5300 INTERCOSTAL BOEING 727 727251 138408H NM BS 360 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED INTERCOSTAL BETWEEN BS 360 AND 380 AT STRINGER 5R IS CRACKED O N FORWARD INBOARD END. ACCOMPLISHED INTERCOSTAL REPAIR IAW B727 SRM 51-40-3, FIG 1 AND 53-10-2, FIG 3. (M) 2 L 7 3 4F A3WE 2001082200057 20010822 00057 NM 2001 8 22 GAIA01279ST 1 20010806 A 5200 WEB BOEING 727 727251 138408H NM BS 1110 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN AFT CARGO C-3 DOOR LOWER FORWARD WEB AND STRAP IS DENTED AN D CRACKED AT STRINGER 26R. ACCOMPLISHED WEB AND STRAP REPAIR IAW B727 SRM 52-30-1, FIG 6 AND 51-40-2 FIG 1. (M) 2 L 7 3 4F A3WE 2001082200058 20010822 00058 NM 2001 8 22 GAIA01278ST 1 20010806 A 5300 FRAME BOEING 727 727251 138408H NM BS 1110 DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN LOWER AFT CARGO, FRAME BS 1110 HAS A DENT IN THE RADIUS ABO VE STRINGER 26L. ACCOMPLISHED FRAME REPAIR IAW B727 SRM 51-40-3, FIG 1 AND 53-10-2 FIG 5. (M) 2 L 7 3 4F A3WE 2001082200059 20010822 00059 NM 2001 8 22 GAIA01277ST 1 20010806 A 5300 FRAME BOEING 727 727251 138408H NM BS 950C DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN LOWER AFT CARGO, FRAME BS 950C HAS A DENT AT STRINER 26L. ACCOMPLISHED FRAME REPAIR IAW B727 SRM 51-40-3 FIG 1 AND 53-10-2, FIG 5. (M) 2 L 7 3 4F A3WE 2001082200060 20010822 00060 NM 2001 8 22 GAIA01276ST 1 20010806 A 5300 STRINGER BOEING 727 727251 138408H NM BS 720B CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED STRINGER 15 LEFT IS CRACKED AT BS 720B PLUS 15. ACCOMPLISHED STRINGER REPAIR IAW B727 SRM 53-10-3, FIG 5. (M) 2 L 7 3 4F A3WE 2001082200061 20010822 00061 NM 2001 8 22 GAIA01275ST 1 20010806 A 5300 STRINGER BOEING 727 727251 138408H NM BS 720B CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED STRINGER 15 RIGHT IS CRACKED AT BS 720B PLUS 15. ACCOMPLISHED STRINGER REPAIR IAW B727 SRM 53-10-3, FIG 5. (M) 2 L 7 3 4F A3WE 2001082200062 20010822 00062 NM 2001 8 22 GAIA01274ST 1 20010806 A 5300 FRAME BOEING 727 727251 138408H NM BS 640 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 640 IS CRACKED AND ENTERED BETWEEN STRINGER 16 AND 17R. AC COMPLISHED FRAME REPAIR IAW B727 SRM 51-40-3, FIG 1 AND 53-10-2, FIG 3. (M) 2 L 7 3 4F A3WE 2001082200063 20010822 00063 NM 2001 8 22 GAIA01273ST 1 20010806 A 5300 FRAME BOEING 727 727251 138408H NM BS 580 DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 580 FRAME DENTED BETWEEN STRINGER 15 AND 16. ACCOMPLISHED FRAME REPAIR IAW B727 SRM 51-40-3, FIG 1 AND 53-10-2, FIG 3. (M) 2 L 7 3 4F A3WE 2001082200064 20010822 00064 NM 2001 8 22 GAIA01270ST 1 20010806 A 5300 FRAME BOEING 727 727251 138408H NM BS 380 DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 380 FRAME DENTED BETWEEN STRINGER 5-6I. ACCOMPLISHED FRAME REPAIR IAW B727 SRM 53-10-4, FIG 2. (M) 2 L 7 3 4F A3WE 2001082200065 20010822 00065 NM 2001 8 22 GAIA01269ST 1 20010806 A 5300 FRAME BOEING 727 727251 138408H NM BS 400 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 400 FRAME CRACKED AND DENTED BETWEEN STRINGER 7-8R. ACCOMP LISHED FRAME REPAIR IAW B727 SRM 53-10-4, FIG 1. (M) 2 L 7 3 4F A3WE 2001082200076 20010822 00076 NM 2001 8 22 2001UALA01666 1 20010810 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 322UA 23954 CABIN STA 294.5 FLOORBEAM FROM RBL 19 TO RBL 35 HAS NUMEROUS AREAS AFTER CORROSION REMOVAL WITH EXCESS MTRL LOSS EXCEEDI NG 14 PERCENT. MAJOR REPAIR ACCOMPLISHED. REPAIRED, REPLACED FLOORBEAM UPPER CAP SPLICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091400102 20010914 00102 NM 2001 9 14 2001UALA01667 1 20010812 A 2701 65C2552921 MODULE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CONTROL COLUMN FAULTY A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 921UA 25388 UNSCHEDULED LANDING DUE TO ELECTRICAL TRIM SYSTEM AND RELATED CIRCUIT BREAKER PROBLEMS. REPLACED COLUMN CUTOUT SWITCHING MODULE. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082200077 20010822 00077 NM 2001 8 22 2001UALA01669 1 20010810 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 322UA 23954 CABIN STA 616-639 S17R CREASE BEAM WEB CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082200078 20010822 00078 NM 2001 8 22 2001UALA01670 1 20010812 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 322UA 23954 STA 179 STR 17 RT CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082200079 20010822 00079 NM 2001 8 22 2001UALA01671 1 20010812 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 322UA 23954 STA 179 STR 17 LT CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082200080 20010822 00080 NE 2001 8 22 NACA20010030 2 20010821 A 7200 R2800 ENGINE DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE #1 POWER LOSS A NACA C E D ABORTED TAKEOFF ENGINE SHUTDOWN RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 AL 03 99330 1980 1980 43576 P34804 DISCRPANCY: Power loss #1 engine @ T.O. power @ 95 kts. BMEP & M.P. massive drop.CORRECTIVE ACTION: Performed engine run to field barometric and T.O. power settings multiple times. All parameters found to be satisfactory per NAC DC-6 Ops ma nual. 2 L 7 4 4R 4 R 6A3 5E8 2001090600377 20010906 00377 NM 2001 9 6 2001UALA01673 1 20010812 A 2121 FAN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN FAILED A UALA H DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 WP 29 183UA 25379 ELECTRIC BURN ODOR IN CABIN FOLLOWED BY STATUS MSG "RECIRCULATING FAN UPPER L". TURNED OFF UPPER RECIRCULATING FANS AND ODOR DISSIPATED. PRESENT LEC FAULT MSG "FAIL-L WIRING FAIL". THE LEFT OVERHEAD RECIRCULATION FAN EXPERIENCED A BEARING FAILURE. FAN WAS REPLACED. 2 L 7 4 4F 4 F RT A20WE E24NE 2001082200081 20010822 00081 NM 2001 8 22 2001UALA01674 1 20010813 A 5320 FILLER BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 913UA 25291 AFT PIT STA 727A FRAME RADIUS FILLER IS BROKEN AT RBL 24. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED FILLER AND STRAP. 2 L 7 2 4F 4 F RT A16WE E2GL 2001101200062 20011012 00062 NM 2001 10 12 2001UALA01675 1 20010813 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 324UA 23956 LT MID CABIN STA 685 STR 10L STRINGER TO FRAME CLIP CRACKED AT STRINGER LWR AFT RIVET HOLE. *S/D* MAJOR REPAIR ACCOMPL ISHED. REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2001110600097 20011106 00097 NM 2001 11 6 2001UALA01676 1 20010813 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 324UA 23956 STA 727E STR 4R CLIP CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082200083 20010822 00083 NM 2001 8 22 2001UALA01677 1 20010813 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 324UA 23956 STA 727E STR 4R CLIP CRACKED. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082200084 20010822 00084 NM 2001 8 22 2001UALA01685 1 20010813 A 5330 SKIN BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BS 1219 STR 11L FUSELAGE SKIN DENTED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082200085 20010822 00085 NM 2001 8 22 2001UALA01686 1 20010813 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BS 676-677 STR 39L SHEAR TIE CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082200086 20010822 00086 NM 2001 8 22 2001UALA01687 1 20010813 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BS 654-655 STR 39L-39R SHEAR TIE CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REPAIR . 2 L 7 2 4F 4 F RT A1NM E3NE 2001082200087 20010822 00087 NM 2001 8 22 2001UALA01688 1 20010813 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BS 566 STR 38R-39R SHEAR TIE CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082200088 20010822 00088 NM 2001 8 22 2001UALA01690 1 20010813 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BS 1417 STR 39R-39L SHEAR TIE CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082200089 20010822 00089 NM 2001 8 22 2001UALA01691 1 20010813 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BS 1241-1263 STR 38L-39L SHEAR TIE CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REPA IR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082200090 20010822 00090 NM 2001 8 22 2001UALA01692 1 20010813 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BS 1241-1263 STR 37L-38L SHEAR TIE CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REPA IR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082200091 20010822 00091 NM 2001 8 22 2001UALA01693 1 20010813 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BS 434 STR 36L-37L SHEAR TIE CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090700038 20010907 00038 NM 2001 9 7 2001UALA01694 1 20010813 A 2520 INSULATION BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN CONTAMINATED A UALA K NONE B H SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC DE DESCENT 1 WP 29 184UA 25380 BURNING GARBAGE SMELL DURING DESCENT. ALL ELECTRICAL POWER LOST TO FIRST CLASS SEATS. SUPPLEMENTAL DATA UPDATE LAXMM FOU ND NO ELECTRICAL SMELL, OPS CHECKED VIDEO SYSTEM FOR 6 HRS. POWERED ALL SEATS ALL DAY, ALL SEATS OPERATE NORMAL. CHECKED ALL SYSTEM C-B'S, CHECKED ALL CONNECTORS ON VIDEO BUFFER BOX, REPLACED VIDEO BUFFER BOX AND SYSTEM CONTROL UNIT PRECAUT IONARY. POSSIBLE CAUSE: STRONG SMELL FROM INSIDE THE FWD CARGO COMPARTMENT, BENEATH THE FLOOR PANELS EXTREMELY DIRTY. CO NTAMINATED INSULATION BLANKET UNDER FLOOR AT STA. 900-920.CLEANED AND DEODORIZED FWD. CARGO COMP'T. AREA. 2 L 7 4 4F 4 F RT A20WE E24NE 2001090600378 20010906 00378 NM 2001 9 6 2001UALA01695 1 20010810 A 3350 417U75631 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 175UA 24382 EMERGENCY EXIT OVERHEAD LIGHT ASSEMBLY AT SEATS 17GH INOP. LIGHT ASSEMBLY INOP. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2001090700046 20010907 00046 NE 2001 9 7 2001UALA01696 2 20010811 A 7230 COMPRESSOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 3 ENGINE SURGES A UALA C E ABORTED TAKEOFF ENGINE SHUTDOWN R A J PARTIAL RPM/PWR LOSS FLAME/FIRE WARNING INDICATION TO TAKEOFF 1 WP 29 182UA 15987 15987 25279 727354 NR 3 ENGINE STALLED ON TAKE OFF, FLAMES REPORTED OUT TAILPIPE, EGT OVER TEMPTED OVER 820 DEGREES FOR 15 SECONDS, PEAK EG T 848 DEGREES. CREW WRITE-UP, ENGINE FIRE WARNING NR 3 ENGINE ON TAKE OFF. ENGINE FIRE-DAMAGE CHECKLIST ACCOMPLISHED. TO WER OBSERVED SLIGHT FLAME OUT TAIL PIPE ON TAKE OFF. EXTINGUISHED AFTER SHUTDOWN. THE ENGINE HAD A GROUP 3 SURGE ON TAKE OFF. NO INDICATION OF ENGINE FIRE. SOME TORCHING FROM TAILPIPE DURING SURGE.GROUP 3 SURGES ARE BEING MANAGED PER AD 2001 -15-12 2 L 7 4 4F 4 F RT A20WE E24NE 2001082200093 20010822 00093 NM 2001 8 22 2001UALA01697 1 20010814 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BS 588 STR 36L-37L SHEAR TIE CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082200094 20010822 00094 NM 2001 8 22 2001UALA01698 1 20010814 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BS 1307 STR 38R-39R SHEAR TIE CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082200096 20010822 00096 NM 2001 8 22 2001UALA01699 1 20010814 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BS 1351 STR 38L-39L SHEAR TIE CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082200097 20010822 00097 NM 2001 8 22 2001UALA01700 1 20010814 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BS 588 STR 37L-38L SHEAR TIE CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082200099 20010822 00099 NM 2001 8 22 2001UALA01701 1 20010814 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BS 1417 STR 38L-39L SHEAR TIE CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082200100 20010822 00100 NM 2001 8 22 2001UALA01702 1 20010815 A 5230 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 322UA 23954 AFT CARGO DOOR HAS DAMAGE ON OUTER SKIN. *S/D* MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED AREA AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082200105 20010822 00105 NM 2001 8 22 2001UALA01703 1 20010814 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BS 1395 LBL40-45 T-CAP CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CAP REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082200107 20010822 00107 NM 2001 8 22 2001UALA01704 1 20010814 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BS 1351 STR 36L-37L SHEAR TIE CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082200108 20010822 00108 NM 2001 8 22 2001UALA01705 1 20010814 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BS 500 STR 35L-36L SHEAR TIE CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082200109 20010822 00109 NM 2001 8 22 2001UALA01706 1 20010815 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 324UA 23956 AFT PIT STA 787, STR 25L STRINGER CLIP IS BROKEN. *S/D* MAJOR REPAIR ACCOMPLISHED. ACP BY REPLACING STRINGER TO FRAME CLIP STA 787 STR 25L. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082200111 20010822 00111 NM 2001 8 22 2001UALA01707 1 20010814 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 301 STR 5L-6L NEED TO FAB SHEAR TIE TO ACCOMODATE TEAR STRAP REPAIR. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED A ND INSTALLED SHEARTIE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082200112 20010822 00112 NM 2001 8 22 2001UALA01709 1 20010814 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 297 STR 2L-3L NEED TO FAB SHEAR TIE TO ACCOMODATE TEAR STRAP. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INST ALLED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082200114 20010822 00114 NM 2001 8 22 2001UALA01711 1 20010814 A 2612 FIRE DETECTOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE WHEEL WELL INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 665UA 29237 WHEEL WELL FIRE DETECTION WILL NOT TEST. 2 L 7 2 4F 4 F RT A1NM E24NE 2001082200116 20010822 00116 NM 2001 8 22 2001UALA01712 1 20010814 A 5210 ROLLER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE DOOR WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 650UA 25287 ROLLER AT TOP OF DOOR IS WORN AND DAMAGE. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED DOOR ASSY. 2 L 7 2 4F 4 F RT A1NM E24NE 2001091900032 20010919 00032 NE 2001 9 19 2001UALA01713 2 20010814 A 7250 TURBINE BLADES BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 726580 NUMBER 1 ENGINE LPT 3 BLADE IS CRACKING WITH SULFIDATION. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001082200120 20010822 00120 NE 2001 8 22 ARWA0010809 2 20010818 A 7200 ENGINE LKHEED 1011 1011385114 WP RROYCE RB211 RB211524B402 54555 NE NR 2 VIBRATION A ARWA E ENGINE SHUTDOWN E VIBRATION/BUFFET CR CRUISE 1 SO 19 260FA 193A1158 NR 2 ENGINE VIBRATION SPIKED AT 2.8 SHUT DOWN ENGINE. AIRCRAFT LANDED WITHOUT INCIDENT. 2 L 7 3 4F 4 F A23WE E12EU 2001082200121 20010822 00121 NM 2001 8 22 AWXA0002165 1 20010816 A 2120 214N50423 DUCT BOEING 757 7572G7 1384963 NM CARGO BAY SPLIT A AWXA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 28 910AW 24523 FLT 776 LAS - BW, UPON DEPARTURE A LOUD NOISE AND REVERBERATION CABIN ALT REMAINED AT FIELD ALT. RETURNED TO LAS. REPL ACED DUCT, RAN ACFT AND PRESSURIZED TO MORE THAN 3 PSI. ALL INDICATIONS NORMAL. 2 L 7 2 4F RT A2NM 2001082200122 20010822 00122 NM 2001 8 22 C1HA200182010 1 20010729 A 2612 473597402 FIRE DETECTOR BOEING 727 7272S7 138407Z NM CARGO BAY FAULTY A C1HA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 682CA 22019 ONE HOUR INTO FLIGHT-LEVEL 330 AFT CARGO FIRE DETECTION ACTIVATE DFDR APPROX 5 SEC THEN SHUTOFF. RAN EMERGENCY CHECKLIS T PROCEDURE. HALF WAY THOUGH CHECKLIST CARGO FIRE DETECTION ACTIVATED FOR 2ND TIME. EXTINGUISHED BOTTLE NR 1 INTO CARG O HOLD PER CHECKLIST AND DIVERTED TO IAH OVERWEIGHT LANDING MADE AT IAH. REPLACED AFT NR 1 AND NR 5 CARGO FIRE DETECTOR S. REPLACED FIRE DEPLETED FIRE BOTTLE. OVERWEIGHT LANDING INSPECTION MADE. 2 L 7 3 4F A3WE 2001082200123 20010822 00123 NM 2001 8 22 C1HA200186008 1 20010729 A 2150 6056751 FAN BOEING 727 7272S7 138407Z NM A/C BAY FAILED A C1HA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 686CA 22021 RIGHT PACK TRIPPED OFF AT 180 DEGREES. EXPERIENCED HEAVY SMOKE IN CABIN. PAX USED O2 BELOW LIMITS. REMOVED AND REPLAC ED PACK FAN, OPS CHECKED NORMAL. REPLACED PAX O2 BOTTLE. 2 L 7 3 4F A3WE 2001082200124 20010822 00124 NE 2001 8 22 C1HA200196013 2 20010804 A 7200 ENGINE BOEING 727 7272J4 1384006 NM PWA JT8 JT8D* NE NR 2 FLAMED OUT A C1HA O OTHER X ENGINE FLAMEOUT DE DESCENT 1 GL 15 696CA 22574 689989 UPON DESCENT INTO DFW NR 2 ENG FLAMED OUT. FOLLOWED RE-LIGHT PROCEDURE. ENG CONFIRMED TO OPERATE NORMALLY WITH NO FURT HER PROBLEMS. TROUBLESHOT IAW JT8D MM TROUBLE SHOOTING -07A CH. 72-00 STEPS 1, 2, 3 REQ'D SKIP TO STEP 27. CHECKED FUE L PUMP AND FCU FILTERS AND AIRCRAFT FUEL SYSTEM FOR WATER OR CONTAMINATION PER STEP 27. NO WATER OR CONTAMINATION WAS F OUND. FILTERS REPLACED AS PRECAUTION SKIPPED TOM STEP 29 AND OPS CHECK OF FUEL HEAT SYSTEM WAS NORMAL. SKIP TO STEP 31 INSTRUCTIONS TO RETURN ENGINE TO SERVICE. NO TROUBLE FOUND OK FOR SERVICE. 2 L 7 3 4F 4 F RT A3WE E2EA 2001082200125 20010822 00125 EA 2001 8 22 COMA0160617 1 20010820 A 5300 601R3103077 PLATE CNDAIR CL600 CL6002B19 EA FLOOR IMPROPER A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 981CA 7163 TWO SPLICE PLATES WERE FABED INCORRECTLY BY MANUFACTURER.FABRICATED TWO DOUBLER PLATES, REWORKED SPLICE PLATES, INSTALLE D DOUBLER PLATES AND INSTALLED REWORKED SPLICE PLATES I/A/W WVAC E.O. 601R-53-2654. 2 L 7 2 4F RT A21EA 2001082200126 20010822 00126 EA 2001 8 22 COMA0160618 1 20010820 A 5300 60034017595 ANGLE CNDAIR CL600 CL6002B19 EA FLOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 981CA 9940 7163 AFT "J" ANGLE AT F.S. 280.00 CORRODED.REMOVED AND REPLACED AFT "J" ANGLE AT F.S. 280.00 BY FABRICATING NEW ANGLE AND INS TALLING I/A/W WVAC EO 601R-53-2650. 2 L 7 2 4F RT A21EA 2001082200127 20010822 00127 EU 2001 8 22 C2XA01BT156 1 20010817 A 3260 WARNING SYSTEM AEROSP ATR42 ATR42320 8680930 EU COCKPIT MALFUNCTIONED A C2XA K NONE N FALSE WARNING AP APPROACH 1 SW 27 99838 259 EWR---CO3223, CREW REPORTED, GEAR NOT DOWN WARNING IN FLIGHT AT 4000 FEET. STARTED DESCENT AND PULLED POWER LEVERS BACK TO FLIGHT IDLE. AIRCRAFT LANDED UNEVENTFULLY IN EWR. MAINTENANCE INSPECTED AND PERFORMED BITE MEMORY RECALL TEST ON T HE PSEU REFERENCE ATR42 MM 32-61-83. NO FAULTS FOUND AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001082200128 20010822 00128 SO 2001 8 22 C2XA01IA296 1 20010713 A 2150 A/C PACK EMB 120 EMB120ER 3260203 SO AC BAY MALFUNCTIONED A C2XA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 27 16729 120185 BPT- FLIGHT 3083, AFTER TAKEOFF THE CREW NOTED SMOKE IN THE CABIN, THE LAV SMOKE ALARM ACTIVATED, (RT PACK FAIL FIVE MIN UTES PRIOR TO SMOKE), AND THE AIRCRAFT RETURNED TO BPT WITHOUT INCIDENT. BPT- MAINTENANCE INSPECTED THE AIRCRAFT AND TH E RIGHT PACK WAS PLACED ON MEL AND THE AIRCRAFT WAS RELEASED TO SERVICE. IAH- MAINTENANCE PERFORMED AN OPERATIONAL CHE CK OF THE RT PACK, NO DEFECTS NOTED. CLEARED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001082200129 20010822 00129 EU 2001 8 22 C2XA01IA334 1 20010820 A 3260 8525LGR8B3ASNH CONNECTOR AEROSP ATR42 ATR42320 8680930 EU NLG DIRTY A C2XA K NONE O OTHER CL CLIMB 1 SW 27 15818 153 IAH - FLIGHT 29990, THE CREW REPORTED THAT THE LANDING GEAR WAS SLOW TO RETRACT. THE AIRCRAFT LANDED AT IAH WITHOUT INC IDENT. MAINTENANCE CLEANED THE NOSE LANDING GEAR WEIGHT ON WHEELS CANNON PLUG. OPERATIONALLY CHECKED THE RETRACTION/EX TENSION SYSTEM WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001082200130 20010822 00130 NM 2001 8 22 C8GA20010016 1 20010720 A 5210 DOOR BOEING 727 727223 1384074 NM ENTRY NOT CLOSED A C8GA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 15 708AA 22465 FLT 4201 FROM SAT TO DFW. DURING CLIMB, THE DOOR WARNING LIGHT CAME ON IN FLIGHT AND COULD NOT PRESSURIZED THE AIRCRAFT . AIR TURNBACK TO SAT AND LANDED WITHOUT INCIDENT. PERFORMED FORWARD ENTRY DOOR OPERATION AND INSPECTION, INSPECTED LA TCHES AND LOCK CAM AND FOUND DOOR OPERATING NORMAL IAW MM 52-11-01. SYSTEM OPS CHECK GOOD AND AIRCRAFT RETURN TO SERVIC E. 2 L 7 3 4F A3WE 2001082200131 20010822 00131 EA 2001 8 22 COMA0160619 1 20010820 A 5300 60034017351 ANGLE CNDAIR CL600 CL6002B19 EA FLOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 981CA 9940 7163 THE FWD "J" ANGLE AT F.S. 280.00 BETWEEN LBL9 AND RBL9 IS CORRODED.REMOVED AND REPLACED FWD "J" ANGLE USING NEW PART NUM BER 600-34017-351 ANGLE I/A/W WVAC EO 601R-53-2649. 2 L 7 2 4F RT A21EA 2001082200132 20010822 00132 WP 2001 8 22 CALA0100667 1 20010722 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND A 3.5 INCH CRACK IN FORWARD ENTRY CUSP WEB AT FS 161, RBL 5. THE CRACKED AREA WAS ROUTED OUT AND A REP AIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 2001082200133 20010822 00133 WP 2001 8 22 CALA0100668 1 20010722 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND FORWARD ENTRY CUSP WEB CORRODED AT FS 180-200 BETWEEN RBL 7 AND LBL 10. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 2001082200134 20010822 00134 WP 2001 8 22 CALA0100669 1 20010722 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND FORWARD ENTRY CUSP WEB CORRODED AT FS 160-209, LBL 42-50. THE FASTENERS WERE REMOVED AND THE CORRODED AREA WAS CUT OUT IAW SRM 51-10-4 AND 53-01, FIGURE 2. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-10-2, 51-10-3, AND 51-3 0-2. 2 L 7 2 4F A6WE 2001082200135 20010822 00135 WP 2001 8 22 CALA0100671 1 20010723 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND FORWARD ENTRY CUSP WEB CORRODED BETWEEN FS 200 AND 205, LBL 10 TO RBL 10. A REPAIR DOUBLER WAS INSTALL ED IAW SRM 53-01, FIGURE 1 AND 51-30-2. 2 L 7 2 4F A6WE 2001082200136 20010822 00136 WP 2001 8 22 CALA0100673 1 20010724 A 5530 PLATE DOUG DC9 DC982 3022082 WP VERTICAL STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76823 49483 INSPECTION FOUND I/B AND O/B RT VERTICAL STABILIZER SUPPORT PLATES CORRODED. THE I/B AND O/B RT VERTICAL STABILIZER SUP PORT PLATES WERE REMOVED AND REPLACED IAW EA SA003-5530-01238, SRM 51-10-2. 2 L 7 2 4F A6WE 2001082200137 20010822 00137 WP 2001 8 22 CALA0100674 1 20010724 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND FORWARD ENTRY CUSP WEB CRACKED BETWEEN FS 160 AND 200, RBL 30. THE CRACKED AREA WAS CUT OUT AND A REPA IR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 2001082200138 20010822 00138 WP 2001 8 22 CALA0100675 1 20010724 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND FUSELAGE SKIN CREASED AT STA 180, LONGERON 23R. THE CREASED AREA WAS CUT OUT IAW SRM 53-04, FIGURE 12, PAGE 35. A REPAIR DOUBLER AND FINGER DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 12, PAGE 35, 51-10-4, 53-30-5, AND 51 -30-2. 2 L 7 2 4F A6WE 2001082200139 20010822 00139 WP 2001 8 22 CALA0100678 1 20010725 A 5511 SPAR DOUG DC9 DC982 3022082 WP HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76823 49483 INSPECTION FOUND LT HORIZONTAL STABILIZER FORWARD UPPER SPAR AFT BARREL NUT HOLE AND BOLT HOLE CORRODED. REPAIRS WERE P ERFORMED IAW ECRA 5511-01061. 2 L 7 2 4F A6WE 2001082200140 20010822 00140 EA 2001 8 22 COMA0160620 1 20010818 A 5346 601350061 WEB CNDAIR CNDAIR CL600 CL6002B19 EA BEAM CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 964CA 12120 7129 R/H AND L/H SIDES OF THE ENGINE SUPPORT BEAM ASSY ARE CRACKED ON THE LOWER WEB.REPAIRED R/H AND L/H OUTBD LOWER ENGINE S UPPORT BEAM WEB I/A/W CANADAIR REO 601R-53-61-366. 2 L 7 2 4F RT A21EA 2001082200141 20010822 00141 NM 2001 8 22 CALA0100679 1 20010725 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM STA 1006-1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14325 23455 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1006-1016, LBL 5. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 53-10-3. 2 L 7 2 4F RT A16WE 2001082200142 20010822 00142 NM 2001 8 22 CALA0100680 1 20010725 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14325 23455 INSPECTION FOUND LT AFT LAV WALL SUPPORT CORRODED AT STA 1013, LBL 5 AND H STRAP CORRODED AT STA 1012, LBL 5, UNDER LAV WALL SUPPORT. THE SUPPORT AND STRAP WERE REMOVED AND REPLACED IAW SRM 53-10-3. 2 L 7 2 4F RT A16WE 2001082200143 20010822 00143 WP 2001 8 22 CALA0100694 1 20010726 A 5320 SILL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76823 49483 INSPECTION FOUND AFT CARGO DOOR JAMB SILL CORRODED AT STA 1155-1212. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 63. 2 L 7 2 4F A6WE 2001082200144 20010822 00144 WP 2001 8 22 CALA0100695 1 20010726 A 5530 PLATE DOUG DC9 DC982 3022082 WP VERTICAL STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76823 49483 INSPECTION FOUND I/B AND O/B LEFT VERTICAL STABILIZER SUPPORT PLATES FOR HORIZONTAL STABILIZER PIVOT BOLT CORRODED IN AN D AROUND BOLT HOLES. THE SUPPORT PLATES WERE REMOVED AND REPLACED IAW WORK CARD 08-5530-1-0005. 2 L 7 2 4F A6WE 2001082200145 20010822 00145 WP 2001 8 22 CALA0100697 1 20010726 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND RT FUSELAGE EXTERNAL SKIN DENTED AND GOUGED BELOW NR 2 ENGINE APRON AT STA 1309. THE DAMAGED AREA WAS REMOVED IAW SRM 53-04, FIGURE 38. A REPAIR DOUBLER AND SKIN PLUG WAS INSTALLED IAW SRM 53-04, FIGURE 38 AND 51-30-2. 2 L 7 2 4F A6WE 2001082200146 20010822 00146 WP 2001 8 22 CALA0100700 1 20010727 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND CUSP WEB CRACKED AFT OF L-2 DOOR AT STA 1174, LBL 60. THE CUSP WEB WAS REMOVED AND A NEW CUSP WEB WAS INSTALLED IAW SRM 51-30-2 AND 51-30-1. 2 L 7 2 4F A6WE 2001082200147 20010822 00147 EA 2001 8 22 COMA0160621 1 20010817 A 5346 WEB CNDAIR CL600 CL6002B19 EA BEAM CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 964CA 12120 7129 UPPER CENTER ENGINE SUPPORT BEAM HAS 1/2 CRACK (CENTER AFT).PERFORMED A TEMPORARY REPAIR I/A/W CANADAIR REO 601R-53-61-3 45 REV B. 2 L 7 2 4F RT A21EA 2001082200148 20010822 00148 WP 2001 8 22 CALA0100701 1 20010727 A 5230 PAN DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND DOOR PAN CRACKED AROUND BOTTOM STOP AT AFT CARGO DOOR AFT SIDE. A DOUBLER AND FILLER WERE INSTALLED IA W SRM 52-05, FIGURE 1 & 4 AND ECRA 5230-01540. 2 L 7 2 4F A6WE 2001082200150 20010822 00150 WP 2001 8 22 CALA0100703 1 20010727 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76823 49483 INSPECTION FOUND FORWARD CARGO DOOR LOWER JAMB CORRODED UNDER DOOR STOPS AT STA 389-408. THE DOOR JAMB WAS REPAIRED IAW ECRA 5310-04165. 2 L 7 2 4F A6WE 2001082200151 20010822 00151 WP 2001 8 22 CALA0100704 1 20010727 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND R-1 DOOR CUSP ANGLE CORRODED AT FS 203. THE CORRODED SECTION OF CUSP ANGLE WAS CUT OUT IAW SRM 51-30-1 . A CUSP ANGLE AND SPLICE WERE INSTALLED IAW SRM 53-05, FIGURE 55, SHEET 2. 2 L 7 2 4F A6WE 2001082200152 20010822 00152 WP 2001 8 22 CALA0100705 1 20010727 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND CUSP WEB CORRODED AT FS 200-237, RBL 44 TO RBL 56. THE CORRODED SECTION OF CUSP WEB WAS REMOVED AND A NEW CUSP WEB WAS INSTALLED IAW SRM 51-30-02. 2 L 7 2 4F A6WE 2001082200153 20010822 00153 NM 2001 8 22 CALA0100707 1 20010727 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14325 23455 INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 540, BL 0. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 5 1-10-02. 2 L 7 2 4F RT A16WE 2001082200154 20010822 00154 WP 2001 8 22 CALA0100717 1 20010730 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND CUSP WEB CORRODED AT FS 160 - 200, RBL 35 TO RBL 50. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED I AW SRM 51-30-2 AND 53-10-1. 2 L 7 2 4F A6WE 2001082200155 20010822 00155 NM 2001 8 22 CALA0100719 1 20010730 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14325 23455 INSPECTION FOUND FLOOR SUPPORT CORRODED AT FASTENER HOLES, STA 294-312, LBL 12. THE FLOOR SUPPORT WAS REMOVED AND REPLA CED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 2001082200156 20010822 00156 NM 2001 8 22 CALA0100720 1 20010730 A 5320 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14325 23455 INSPECTION FOUND A 1INCH CRACK IN WEB ANGLE AT STA 927-947.5, BL 0. THE WEB ANGLE WAS REMOVED AND REPLACED IAW SRM 51-1 0-02. 2 L 7 2 4F RT A16WE 2001082200157 20010822 00157 NM 2001 8 22 CALA0100721 1 20010730 A 5320 FITTING BOEING 737 7373T0 1384582 NM CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14325 23455 INSPECTION FOUND L-1 DOOR AFT GIRT BAR LATCH MOUNT CORRODED. THE GIRT BAR LATCH MOUNT WAS REMOVED AND REPLACED IAW SRM 51-40-00. 2 L 7 2 4F RT A16WE 2001082200158 20010822 00158 NM 2001 8 22 CALA0100722 1 20010730 A 5320 FITTING BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14325 23455 INSPECTION FOUND GALLEY MOUNTS CORRODED AT STA 946.5, LBL 14 AND RBL 8. THE GALLEY MOUNTS WERE REMOVED AND REPLACED IAW SRM 53-10-03. 2 L 7 2 4F RT A16WE 2001082200159 20010822 00159 NM 2001 8 22 CALA0100726 1 20010730 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14325 23455 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 947.5-967, RBL 18. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-40-00. 2 L 7 2 4F RT A16WE 2001082200160 20010822 00160 WP 2001 8 22 CALA0100731 1 20010731 A 5320 SPLICE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND LONGERON 29L SPLICE CORRODED IN FORWARD CARGO AREA AT FS 225. THE LONGERON SPLICE WAS REMOVED AND A NE W SPLICE WAS INSTALLED IAW SRM 53-01, FIGURE 1, 51-30-2, 51-10-4, AND 51-30-5. 2 L 7 2 4F A6WE 2001082200161 20010822 00161 NM 2001 8 22 CALA0100732 1 20010802 A 5320 SPLICE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14325 23455 INSPECTION FOUND STRINGER 4L SPLICE CRACKED AT STA 907. THE SPLICE WAS REMOVED AND REPLACED IAW SRM 53-00-03, FIGURE 20 3. 2 L 7 2 4F RT A16WE 2001082200162 20010822 00162 WP 2001 8 22 SABA010043 2 20010820 A 7314 89778025 FUEL CONTROL BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UHR WP INOPERATIVE A SABA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 33 963AE 963 66250 Aircraft 963 on lfight 5136 from LYH to CLT. During takeoff roll the right engine fuel pressure warning light came on. The takeoff was aboorted. No emergency was declared and no emergency proecdures were used. Aircraft returned to the gate with no other problems. Maintenance removed and replaced the right engine fuel control. Ground run and ops check was good. Aircraft returned to service. 2 L 7 2 4T 4 T RT A56EU E4WE 2001082200163 20010822 00163 NM 2001 8 22 CALA0100735 1 20010705 A 2421 GENERATOR BOEING 737 7373Q8 1384670 NM NR 1 ENGINE FAILED A CALA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 09 17386 26321 THE NR 1 GEN BUS OFF LIGHT AND GEN OFF BUS LIGHT CAME ON DURING CLIMBOUT OF LAX AT FL320. QRH PROCEDURES FOR BUS OFF WER E FOLLOWED, BUT DID NOT RE-ESTABLISH GEN. THE APU WAS STARTED AND THE APU FIRE LIGHT AND WARNING BELLS ACTIVATED. THE APU WAS SHUTDOWN AND THE FIRE BOTTLE WAS DISCHARGED. THE ACFT WAS RETURNED TO LAX WHERE IT LANDED WITHOUT INCIDENT. IN SPECTION FOUND NO EVIDENCE OF FIRE DAMAGE. THE APU WAS INSPECTED, NO AIR LEAKS OR CHAFED FIRE LOOPS WERE FOUND. THE APU WAS RUN AND OPERATION CHECKED GOOD AND THE APU FIRE WARNING COULD NOT BE DUPLICATED. THE APU FIRE BOTTLE WAS REPLACED IAW MM 26-22-11. THE NR 1 ENGINE GENERATOR WAS REPLACED IAW MM 24-21-11 AND OPERATION CHECKED GOOD. 2 L 7 2 4F RT A16WE 2001082200164 20010822 00164 WP 2001 8 22 CALA0100736 1 20010803 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND A 1 INCH CRACK IN L-1 DOOR TORQUE BOX WEB TANG. THE CRACKED AREA OF WEB TANG WAS TRIMMED OUT AND A DOU BLER AND FILLER WERE INSTALLED IAW EA 9-5314-2-A0905 AND ECRA 5310-04170. 2 L 7 2 4F A6WE 2001082200165 20010822 00165 EA 2001 8 22 COMA0160622 1 20010819 A 5311 6013600130 DOUBLER CNDAIR CL600 CL6002B19 EA BEAM CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 920CA 18424 7022 THE FRAME AT FS640 HAD A CRACKED DOUBLER P/N 601-36001-30, ON THE RIGHT SIDE IN THE ENGINE BEAM AREA.REMOVED DISCREPANCY DOUBLER AND INSTALLED A NEW DOUBLER I/A/W WVAC EO 601R-53-2658. 2 L 7 2 4F RT A21EA 2001082200166 20010822 00166 NM 2001 8 22 CALA0100740 1 20010803 A 5510 HINGE PIN BOEING 737 7373T0 1384582 NM HORIZ STAB BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77303 23354 INSPECTION FOUND LT HORIZONTAL STABILIZER HINGE PIN AND INSERT BROKEN. THE HINGE PIN AND INSERT WERE REMOVED AND REPLAC ED IAW MM 27-41-31. 2 L 7 2 4F RT A16WE 2001082200167 20010822 00167 WP 2001 8 22 CALA0100744 1 20010807 A 5753 SKIN DOUG DC9 DC982 3022082 WP T/E FLAP DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND RT WING O/B FLAP O/B TRAILING EDGE SKIN LOWER SURFACE DENTED. THE SKIN WAS REMOVED IAW SRM 51-30-2 AND THE SUPPORT RIBS WERE FOUND DAMAGED. NEW RIBS AND A REPAIR DOUBLER WERE INSTALLED AND THE SKIN WAS REINSTALLED IAW SRM 51-10-4, 51-10-3, 57-01, FIGURE 3, AND 51-30-2. 2 L 7 2 4F A6WE 2001082200168 20010822 00168 WP 2001 8 22 CALA0100745 1 20010807 A 5240 PAN DOUG DC9 DC982 3022082 WP R1 DOOR GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND R-1 DOOR LOWER PAN GOUGED AT RIVNUTS. THE PAN SUPPORT WAS REMOVED FOR ACCESS IAW SRM 51-30-02. A REPA IR ANGLE AND DOUBLER WAS INSTALLED IAW ECRA 5240-01386. THE SUPPORT PAN WAS REINSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 2001082200169 20010822 00169 NM 2001 8 22 UPS01236664 1 20010815 A 5330 STRINGER BOEING 727 72727C 138400J NM BS400 S18R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 908UP 19114 INSPECTION TYPE:C ON INSPECTION OF FUSELAGE STRINGERS AT BS 400 WHERE ACCESSABLE, S18R AT BS 400 FOUND TO BE CRACKED. STRINGER REPAIR CARRIED IAW SRM PROCEDURES 2 L 7 3 4F A3WE 2001082200170 20010822 00170 NM 2001 8 22 UPS01236666 1 20010810 A 5310 FRAME BOEING 727 72727C 138400J NM BS 930 LWR CRNR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 908UP 19114 INSPECTION TYPE:C CRACK BS 930 R/H FLANGE I/B LOWER CORNER RADIUS REPAIRED PER SRM ADDENDUM B727-5310-2611B 2 L 7 3 4F A3WE 2001082200171 20010822 00171 NM 2001 8 22 UPS01236673 1 20010809 A 5330 SKIN BOEING 727 72727C 138400J NM BS 400 S16L15L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 908UP 19114 INSPECTION TYPE:C SKIN CRACKS BS 400 BETWEEN S16L AND 15L CRACKS REPAIRED IAW SRM 2 L 7 3 4F A3WE 2001082200172 20010822 00172 NM 2001 8 22 UPS01236675 1 20010811 A 5310 STRINGER BOEING 727 72727C 138400J NM BS400S16R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 908UP 19114 INSPECTION TYPE:C ON FURTHER INSPECTION FOR ACCESS S16R FOUND CRACKED AT BS 400 REPAIRED IAW SRM. 2 L 7 3 4F A3WE 2001082200173 20010822 00173 NM 2001 8 22 UPS01236676 1 20010811 A 5310 STRINGER BOEING 727 72727C 138400J NM BS 400 S15R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 908UP 19114 INSPECTION TYPE:C ON FURTHER INSP FOR ACCESS S15R AT BS 400 FOUND TO BE CRACKED REPAIRED IAW SRM 2 L 7 3 4F A3WE 2001082200174 20010822 00174 NM 2001 8 22 UPS01236677 1 20010811 A 5310 STRINGER BOEING 727 72727C 138400J NM BS400S9R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 908UP 19114 INSPECTION TYPE:C ON FURTHER INSPECTION S9R FOUND CRACKED AT BS 400 STRINGER REPAIRED IAW SRM. 2 L 7 3 4F A3WE 2001082200175 20010822 00175 NM 2001 8 22 UPS01236678 1 20010811 A 5310 STRINGER BOEING 727 72727C 138400J NM BS400 S3R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 908UP 19114 INSPECTION TYPE:C ON FURTHER INSPECTION S3R FOUND CRACKED AT BS 400 REPAIRED PER SRM. 2 L 7 3 4F A3WE 2001082200176 20010822 00176 NM 2001 8 22 UPS01236679 1 20010811 A 5310 STRINGER BOEING 727 72727C 138400J NM BS 400 S6L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 908UP 19114 INSPECTION TYPE:C ON FURTHER INSPECTION S6L AT BS 400 FOUND TO BE CRACKED. DAMAGED STRINGER REPAIRED IAW SRM 53-10-3 2 L 7 3 4F A3WE 2001082200177 20010822 00177 NM 2001 8 22 UPS01236680 1 20010809 A 5350 FRAME BOEING 727 72727C 138400J NM FAIRING 3430 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 908UP 19114 INSPECTION TYPE:C BODY FAIRING #3430 HAS CORRODED FRAME AT R/H GND FAN LOUVRE DOOR AFT CUTOUT. FRAME FABRICATED AND INSTALLED PER SRM 2 L 7 3 4F A3WE 2001082200178 20010822 00178 NM 2001 8 22 UPS01236681 1 20010809 A 5330 SKIN BOEING 727 72727C 138400J NM BS 400 S15-16R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 908UP 19114 INSPECTION TYPE:C SKIN CRACKS BS 400 BETWEEN S16R 15R REPAIRED IAW SRM 2 L 7 3 4F A3WE 2001082200179 20010822 00179 NM 2001 8 22 CALA0100748 1 20010808 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14325 23455 INSPECTION FOUND AFT BAGGAGE BIN CENTER FLOOR SUPPORT CORRODED AT STA 727D, RBL 18. A NEW SUPPORT AND REPAIR ANGLES WER E INSTALLED IAW SRM 51-20-01. 2 L 7 2 4F RT A16WE 2001082200180 20010822 00180 WP 2001 8 22 CALA0100751 1 20010809 A 5510 PLATE DOUG DC9 DC982 3022082 WP HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72821 49481 INSPECTION FOUND HORIZONTAL STABILIZER PIVOT PLATES CORRODED AT RIGHT O/B AND RIGHT I/B LUG BORES. THE PIVOT PLATES WER E REMOVED AND REPLACED IAW EA 5530-01238. 2 L 7 2 4F A6WE 2001082200181 20010822 00181 WP 2001 8 22 CALA0100752 1 20010809 A 5510 PLATE DOUG DC9 DC982 3022082 WP HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72821 49481 INSPECTION FOUND HORIZONTAL STABILIZER PIVOT PLATE CORRODED AT LEFT I/B LUG BORES. THE PIVOT PLATES WERE REMOVED AND RE PLACED IAW EA 5530-01238. 2 L 7 2 4F A6WE 2001082200182 20010822 00182 WP 2001 8 22 CALA0100753 1 20010809 A 5320 FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72821 49481 INSPECTION FOUND A 2 INCH CRACK IN TAIL COMPARTMENT SUPPORT FITTING BETWEEN CANTED FRAMES 1463 AND 1485 AT LOWER AFT SID E. THE SUPPORT FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-10-4. 2 L 7 2 4F A6WE 2001082200183 20010822 00183 NM 2001 8 22 CALA0100754 1 20010810 A 3350 D71702030 CHARGER BOEING 737 737724 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 24706 28767 INSPECTION FOUND EMERGENCY AISLE PATH LIGHTING INOPERATIVE FROM 15AB TO 21AB. THE BATTERY CHARGER WAS REMOVED AND REPLA CED IAW MM 33-51-06. 2 L 7 2 4F RT A16WE 2001082200184 20010822 00184 WP 2001 8 22 CALA0100755 1 20010810 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72821 49481 INSPECTION FOUND A .25 INCH CRACK IN TAIL COMPARTMENT LEFT VENTRAL BOX SUPPORT ANGLE AT CANTED FRAME STA 1474. THE SUPP ORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-05. 2 L 7 2 4F A6WE 2001082200185 20010822 00185 WP 2001 8 22 CALA0100759 1 20010813 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 71828 49488 THE FORWARD ENTRY PORTABLE EMERGENCY LIGHT ASSEMBLY BATTERIES WOULD NOT CHARGE. THE LIGHT ASSEMBLY NICAD BATTERIES WERE REPLACED AND OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 2001082200186 20010822 00186 WP 2001 8 22 CALA0100762 1 20010815 A 5411 SPAR DOUG DC10 DC1030 3023501 WP NR 3 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59083 47926 INSPECTION FOUND A 2 INCH CRACK IN NR 3 PYLON LOWER SPAR WEB AT FAN DUCT CUTOUT. A REPAIR ANGLE AND STIFFENER WERE INST ALLED IAW SRM 54-20-00, FIGURE 19A. 2 L 7 3 4F A22WE 2001082200187 20010822 00187 NE 2001 8 22 CHQ00001 2 20010710 A 7261 PUMP SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ENGINE DAMAGED A CHQA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 11 CHQ 140 367300 PILOT REPORTED LOW OIL PRESSURE IN FLIGHT. ENG SHUTDOWN AND DIVERSION. MAINTENANCE REPAIRED C/B SUMP PUMP. 2 L 7 2 4T 4 T RT A52EU E8NE6 2001082200188 20010822 00188 EU 2001 8 22 CHQ00002 1 20010711 A 2611 SMOKE DETECTOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE E/E BAY MALFUNCTIONED A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 CHQ 101 GEE367364 AVIONICS SMOKE LIGHT ILLUMINATED AFTER TAKEOFF. MAINTENANCE REMOVED AND REPLACED AVIONICS SMOKE DETECTOR. 2 L 7 2 4T 4 T RT A52EU E8NE6 2001082200189 20010822 00189 SO 2001 8 22 CHQ00003 1 20010712 A 3620 FILTER EMB 145 EMB145LR SO BLEED AIR CLOGGED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 CHQ 145226 NR 1 BLEED OVER TEMP LIGHT ILLUMINATED ON CLIMBOUT. CREW RETURNED TO FIELD. MAINTENANCE UNPLUGGED CLOGGED FILTER ON SE NSING LINE. 2 L 7 2 4T RT T00011AT 2001082200190 20010822 00190 NM 2001 8 22 AWXA0002170 1 20010803 A 5313 65457768 STRINGER BOEING 737 73733A 1384673 NM STR 26R CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 D: Stringer 26R BS 1006-1016 corrodedC: removed and replaced stringer IAW 737-300 SRM 51-40-02 pgs 10-11 2 L 7 2 4F RT A16WE 2001082200191 20010822 00191 NM 2001 8 22 AWXA0002171 1 20010818 A 5313 140N1530 STRINGER BOEING 757 7572S7 1384962 NM STA 1450-1465 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 903AW 23323 D: Fuselage skin bulged between STA 1450-1465 Stringer 28 L/HC: Bulging caused by corroded stringer, out of limits, Remo ved Damaged area fabricated repairparts and installed per 757 SRM 51-40-02, 53-0001 fig 201, DWG 14683820, and SRM 51-20 -06, 53-60-03 fig 1 2 L 7 2 4F RT A2NM 2001082200192 20010822 00192 EU 2001 8 22 CHQ00004 1 20010714 A 7931 CONNECTOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE LOOSE A CHQA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 GL 11 CHQ 340A140 GEE367300 A/C RETURNED TO FIELD AFTER LT PROP GEAR BOX OIL PRESSURE FLUX. MAINTENANCE RESECURED LOOSE CANNON PLUGS. 2 L 7 2 4T 4 T RT A52EU E8NE6 2001082200193 20010822 00193 EU 2001 8 22 CHQ00005 1 20010717 A 7930 CHIP DETECTOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE MALFUNCTIONED A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 CHQ 340A146 367149 LT CHIP DETECTOR LIGHT CAME ON SHORTLY AFTER TAKEOFF. A/C RETURNED TO FIELD. MAINTENANCE INSPECTED AND FOUND GOOD FOR SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE6 2001082200194 20010822 00194 EU 2001 8 22 CHQ00006 1 20010719 A 3260 DOWNLOCK SWITCH SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LANDING GEAR FAULTY A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 CHQ 340A118 367359 LANDING GEAR WOULD NOT RETRACT ON TAKEOFF. A/C RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED DOWNLOCK SWITCH. 2 L 7 2 4T 4 T RT A52EU E8NE6 2001082200195 20010822 00195 EU 2001 8 22 CHQ00007 1 20010719 A 2931 INDICATOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE COCKPIT FAILED A CHQA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 11 CHQ 150 MAIN HYD PRESS GAUGE READING ZERO DURING CRUISE. A/C RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED INDICATOR. 2 L 7 2 4T 4 T RT A52EU E8NE6 2001082200196 20010822 00196 EU 2001 8 22 CHQ00008 1 20010720 A 3260 DOWNLOCK SWITCH SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LANDING GEAR DIRTY A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 CHQ 340A118 367359 LANDING GEAR WOULD NOT RETRACT ON TAKEOFF. A/C RETURNED TO FIELD. MAINTENANCE CLEANED DOWNLOCK SWITCH. 2 L 7 2 4T 4 T RT A52EU E8NE6 2001082200197 20010822 00197 EU 2001 8 22 CHQ00009 1 20010721 A 7931 CONNECTOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE LOOSE A CHQA A UNSCHED LANDING N FALSE WARNING UK UNKNOWN 1 GL 11 CHQ 340A140 GEE367300 A/C RETURNED TO FIELD AFTER LT OIL PROP PRESSURE INDICATION. MAINTENANCE SECURED CANNON PLUGS. 2 L 7 2 4T 4 T RT A52EU E8NE6 2001082200198 20010822 00198 EU 2001 8 22 CHQ00010 1 20010724 A 3230 RELAY SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LANDING GEAR FAILED A CHQA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 GL 11 CHQ 340A118 367359 GEAR WON`T RETRACT EXCEPT FOR IN OVERRIDE. A/C RETURNED TO FIELD. MAINTENANCE REMOVED AND REPAIRED RELAYS. 2 L 7 2 4T 4 T RT A52EU E8NE6 2001082200199 20010822 00199 SO 2001 8 22 CHQ00011 1 20010726 A 5200 SWITCH EMB 145 EMB145LR SO DOOR OUT OF ADJ A CHQA A UNSCHED LANDING N FALSE WARNING UK UNKNOWN 1 GL 11 261 145144 A/C RETURNED TO FIELD. EICAS DOORS WARNING MSG. MAINTENANCE ADJUSTED MICROSWITCH. 2 L 7 2 4T RT T00011AT 2001082200200 20010822 00200 EU 2001 8 22 CHQ00012 1 20010727 A 7930 CHIP DETECTOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE DIRTY A CHQA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 GL 11 118 118 357 LEFT OIL CHIP DETECTOR LIGHT ON. REMOVED INSPECTED / CLEANED. 2 L 7 2 4T 4 T RT A52EU E8NE6 2001082200201 20010822 00201 EU 2001 8 22 CHQ00014 1 20010810 A 2910 HYDRAULIC SYSTEM SAAB SF340 SF340A 7850100 EU FUSELAGE FAILED A CHQA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 CHQ 006 HYD SYSTEM FAIL. 2 L 7 2 4T RT A52EU 2001082200202 20010822 00202 2001 8 22 CHQ00015 4 20010810 A 3442 RADAR SAAB SF340 SF340A 7850100 EU COCKPIT FAILED A CHQA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 CHQ 043 RADAR SYSTEM FAILED. 2 L 7 2 4T RT A52EU 2001082200203 20010822 00203 2001 8 22 CHQ00016 4 20010811 A 3425 INDICATOR SAAB SF340 SF340A 7850100 EU COCKPIT FAILED A CHQA A UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 GL 11 CHQ 095 CREW LOST BOTH F/O EFIS TUBES. 2 L 7 2 4T RT A52EU 2001082200204 20010822 00204 SO 2001 8 22 CHQ00017 1 20010813 A 2740 CONTROL UNIT EMB 145 EMB145 SO ELEVATOR FAILED A CHQA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 CHQ 279 CAPT MAIN PITCH TRIM INOP. 2 L 7 2 4F RT T00011AT 2001082200205 20010822 00205 EU 2001 8 22 CHQ00018 1 20010816 A 2435 STARTER GEN SAAB SF340 SF340A 7850100 EU RT ENGINE FAILED A CHQA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 CHQ 004 RIGHT GENERATOR FAILURE. 2 L 7 2 4T RT A52EU 2001082200206 20010822 00206 NE 2001 8 22 CHQ00019 2 20010819 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LEFT FLUCTUATES A CHQA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 CHQ 138 461 LEFT ENGINE FLUCTUATIONS. 2 L 7 2 4T 4 T RT A52EU E8NE6 2001082200207 20010822 00207 EU 2001 8 22 CHQ00020 1 20010618 A 2910 HYDRAULIC SYSTEM SAAB SF340 SF340A 7850100 EU FUSELAGE FAILED A CHQA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 11 CHQ 128 LOST HYD PRESS AND QTY IN FLIGHT. DECLARED EMERGENCY. 2 L 7 2 4T RT A52EU 2001082200209 20010822 00209 WP 2001 8 22 CNMA200100027 1 20010722 A 3350 LIGHT DOUG DC10 DC1030 3023501 WP CABIN MALFUNCTIONED A CNMA K NONE O OTHER CR CRUISE 1 SW 07 540AX 46595 FLOOR EMERGENCY ESCAPE LIGHTING ILLUMINATED IN MID SERVICE ON LT FWD SIDE OF ZONE B. RESET POWER TRANSFER, OPS CHECKED SEVERAL TIMES SATISFACTORY. 2 L 7 3 4F A22WE 2001082200210 20010822 00210 WP 2001 8 22 CNMA200100028 1 20010802 A 7933 WIRE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 2 ENGINE BROKEN A CNMA E ENGINE SHUTDOWN J M WARNING INDICATION OVER TEMP CL CLIMB 1 SW 07 630AX 46596 517690 NR 2 ENG OIL TEMP HIGH AFTER TAKEOFF, ENG SHUTDOWN. REPAIRED BROKEN WIRE AT ADEL CLAMP ON ENG IAW 20-30-01. ENGINE GRO UND RUN, OPS CHECKED OK. 2 L 7 3 4F 4 F A22WE E23EA 2001082200211 20010822 00211 WP 2001 8 22 ZW0A0107101 1 20010817 A 3230 387 LAMP DOUG DC9 DC983 3022083 WP A ZW0A K NONE O OTHER LD LANDING 1 CE 13 9305N 49395 DURING LANDING THE RIGHT MAIN LANDING GEAR LIGHT DID NOT ILLUMINATE, DUE TO BURNED OUT BULB. REPLACED LIGHT BULB P/N 38 7.LAST CHECK C 05/07/01 STL. --- CLOSED --- 2 L 7 2 4F RT A6WE 2001082200212 20010822 00212 NM 2001 8 22 ZW0A0107103 1 20010820 A 3350 20121 FUSE BOEING 767 7673Q8 1385142 NM CABIN BLOWN A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 634TW 28132 DURING PREFLIGHT THE EGRESS LIGHTING BETWEEN ROWS 24 AND 36 WERE INOP, DUE TO NORMAL USAGE. REPLACED TWO (2) FUSED P/N 2 012-1 PER MM33-51-07. LAST CHECK C 10/25/00 LAX --- CLOSED --- 2 L 7 2 4F RT A1NM 2001082200213 20010822 00213 WP 2001 8 22 CNMA200100030 1 20010810 A 3350 BATTERY PACK DOUG DC10 DC1030 3023501 WP CABIN MALFUNCTIONED A CNMA K NONE O OTHER LD LANDING 1 SW 07 540AX 46595 THE 4L TRACK LIGHTING CAME ON LANDING. RESET BATTERY PACK, OPS CHECKED GOOD. 2 L 7 3 4F A22WE 2001082200214 20010822 00214 WP 2001 8 22 CNMA200100031 1 20010811 A 3350 BATTERY PACK DOUG DC10 DC1030 3023501 WP CABIN MALFUNCTIONED A CNMA K NONE O OTHER CL CLIMB 1 SW 07 540AX 46595 B-ZONE FLOOR TRACK LIGHTING CAME ON AFTER T/O, WOULD NOT RESET. RESET FLOOR TRACK BATTERY PACK, SYS OPS CHECK NORMAL ON GROUND. 2 L 7 3 4F A22WE 2001082200218 20010822 00218 NM 2001 8 22 01FDEA00761 1 20010821 A 3230 69163394 FITTING BOEING 727 727233 138408A NM LANDING GEAR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 280FE 22347 N00108 DURING ROUTINE INSPECTION - DISCOVERED SUPPORT FITTING FOR NOSE LANDING GEAR DOOR ACTUATOR RODS TO BE CORRODED. S/D COMING ***** 2 L 7 3 4F RT A3WE 2001082200219 20010822 00219 EA 2001 8 22 COMA0160623 1 20010821 A 2760 SPOILER CNDAIR CL600 CL6002B19 EA A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 988CA 7204 FLIGHT #5243. DURING TAXI OUT OF CVG RECEIVED A SPOILERON FAULT STATUS MESSAGE, AIRCRAFT RETUREND TO THE GATE.PERFORMED RESET OF SPOILERON SYSTEM. 2 L 7 2 4F RT A21EA 2001082200220 20010822 00220 WP 2001 8 22 RRXA11428 1 20010729 A 5310 3755843502N FITTING DOUG DC8 DC873F 302199F WP FS1180 L35 - L34 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND BAHTUB FITTING IS CRACKED AT STA 1180 BETWEEN L35R AND L34R. *** CORRECTIVE ATION *** REMOVED AND REPLACED BATH TUB FITTING IAW DC8 SRM 53-2-0 FIG 20 AND DWG 63755843 2 L 7 4 4F RT 4A25 2001082200221 20010822 00221 NM 2001 8 22 C1HA200195015 1 20010820 A 5600 WINDOW BOEING 727 727290 138408W NM CAPT. L-1 LEAKING A C1HA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 295AS 22147 Captains L-1 window not sealed. Top right corner extremly loud. Pressure fluctuations Returned to DFW.ACTION TAKEN:Seale d L-1 window and retorqued window ops check good. 2 L 7 3 4F A3WE 2001082200222 20010822 00222 NM 2001 8 22 C1HA200185009 1 20010817 A 3350 900835A BATTERY PACK BOEING 727 7272S7 138407Z NM DISCHARGED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 685CA 22492 Emergency light (exterior) located over right wing and between overwing exits is inop.ACTION TAKEN:Removeed and replaced exterior ener. light battery pack cks good. 2 L 7 3 4F A3WE 2001082200223 20010822 00223 NM 2001 8 22 C1HA200185010 1 20010819 A 3610 10604951 ISOLATION VALVE BOEING 727 7272S7 138407Z NM #1 FAILED A C1HA D RETURN TO BLOCK G J M MULTIPLE FAILURE WARNING INDICATION OVER TEMP TX TAXI/GRND HDL 1 GL 15 685CA 22492 On taxi out had double pack trip and cooling fan CB popped. Ran C/B reset procedure and pack trip off procedure. Re-cont inued taxi and had double pack trip and cooling fan control breaker popped again and had right duct overheat light.ACTIO N TAKEN:Removed and replaced left isolation valve ops checked normal. 2 L 7 3 4F A3WE 2001082200224 20010822 00224 NM 2001 8 22 C1HA200193016 1 20010817 A 2613 CLAMP BOEING 727 727212 138407G NM #1 13TH STGBLEED LOOSE A C1HA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 293AS 21348 Upon initial power reduction #1 eng strut overheat illuminated all eng parameters normal during running pocedure the lig ht went out was on for about 1 min. never reilluminated during decent approach &final.ACTION TAKEN:inspected #1 engine s trut area found clamps inboard of bleed valve to have small leak tightened clamps on bled duct ran #1 eng. no further le aks noted. 2 L 7 3 4F A3WE 2001082200225 20010822 00225 NM 2001 8 22 C1HA200193017 1 20010818 A 7930 OIL FILTER BOEING 727 727212 138407G NM #2 ENG CLOGGED A C1HA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 293AS 21348 #2 filter bypass light illuminated returned to gate.ACTION TAKEN:Removed and inspected main oil filter found to have eve dence of coking replaced filter. 2 L 7 3 4F A3WE 2001082200226 20010822 00226 EA 2001 8 22 COMA0160624 1 20010821 A 2720 6229968001 DAMPENER CNDAIR CL600 CL6002B19 EA EMPENNAGE FAULTY A COMA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 01 960CA 12612 7117 FLIGHT #5960. AT THE GATE READY FOR PUSH-BACK RECEIVED YAW DAMPER #1 INOPERATIVE MESSAGE.REPLACED THE #1 YAW DAMPER. 2 L 7 2 4F RT A21EA 2001082200227 20010822 00227 2001 8 22 COMA0160625 4 20010820 A 2200 8220259001 MOUNT CNDAIR CL600 CL6002B19 EA BELLY FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 917CA 2716 7017 FLIGHT #5800. DESTINATION CVG. DURING CRUISE FLIGHT THE AUTO PILOT FAILED @ FL28. EXCESSIVE INPUT FORCE WAS REQUIRED FOR AILERON CONTROL, FLIGHT WAS DIVERTED TO IAD AND LANDED SAFELY.REPLACED THE PRIMARY AILERON SERVO MOUNT (SMT-87A). 2 L 7 2 4F RT A21EA 2001082200228 20010822 00228 NM 2001 8 22 C1HA200197005 1 20010818 A 3350 20131A BATTERY PACK BOEING 727 727270 138408P NM AFT DISCHARGED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 697CA 23052 R-2, L-2 and aft entry door emergency exit identifiers inop.ACTION TAKEN:Removed and replaced battery pack ops check nor mal. 2 L 7 3 4F RT A3WE 2001082200229 20010822 00229 NM 2001 8 22 ZW0A0107201 1 20010820 A 3350 80731 LAMP BOEING 767 76733AER 1385230 NM A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 637TW 25403 THE EGRESS LIGHT WAS INOPERATIVE AT THE LEFT REAR LAV. REPLACED THE LAMP. CHECK-C 1-27-01 LAX. --CLOSED--- 2 L 7 2 4F RT A1NM 2001082200230 20010822 00230 EU 2001 8 22 MALA010648 1 20010816 A 3230 MS2740017 RELAY SAAB SF340 SF340A 7850100 EU A MALA L ABORTED APPROACH O OTHER LD LANDING 1 GL 15 119XJ 340A119 During Flight #7274 F7 Circuit Breaker popped when extending gear at MSP. Crew reset C/B and recycled gear normally. Ma intenance replaced Relay at 10GA PN MS27400-17 and 8GA PN M3536/2-024L. Cycled Gear. Ops check good. 2 L 7 2 4T RT A52EU 2001082200231 20010822 00231 EU 2001 8 22 MALA010649 1 20010818 A 7600 M83726282001P RELAY SAAB SF340 SF340A 7850100 EU CT7TP CT75A 30030 NE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 48XJ During Flight 3281, F1 Open Amber light came on after Takeoff-light remained on during flight and after Landing. Air tu rnback to MSP. Maintenance removed and replaced Relay 82KA PN M83726-28-2001P. Ops check good IAW AMM 76-10-60-5. 2 L 7 2 4T 4 T RT A52EU E8NE 2001082200232 20010822 00232 NM 2001 8 22 2001F00207 1 20010804 A 3040 ANTI-ICE SYSTEM BOEING 747 7472D7B 1384803 NM COCKPIT MALFUNCTIONED A UIEA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 523MC 21782 DURING CLIMB-OUT, THE CREW NOTICED A STRONG BURNING SMELL IN THE COCKPIT. TURNED OFF R2 AND 3 WINDOW HEAT AND THE SMELL DISSIPATED. PULLED CB'S FOR L2-R3 AND L3-R2 WINDOW HEAT. AFTER APPROXIMATELY 3 MORE HOURS THE ODOR RETURNED. THIS TI ME SMOKE CAME FROM LOWER LEFT CORNER OF L1 WINDOW. SCORCHING OBSERVED ON GLASS. SWITCHED OFF AND CB PULLED. A/C DIVER TED TO DXB. (M) 2 L 7 4 4F RT A20WE 2001082200233 20010822 00233 NM 2001 8 22 2001F00208 1 20010127 A 5297 WIRE ROPE BOEING 757 75723A 1384967 NM R4 DOOR OUT OF ADJ A K NONE O OTHER IN INSP/MAINT 1 WP 19 541NA 24291 R4 DOOR FAILED THE EMERGENCY POWER ACTUATION CABLE SYSTEM TEST. ADJUSTED DOOR EMERGENCY ACTUATION CABLE, FUNCTIONAL CHE CK GOOD. (M) 2 L 7 2 4F RT A2NM 2001082200234 20010822 00234 NM 2001 8 22 2001F00209 1 20010727 A 5297 WIRE ROPE BOEING 757 75723A 1384967 NM L2 DOOR OUT OF ADJ A K NONE O OTHER IN INSP/MAINT 1 WP 19 541NA 24291 L2 DOOR FAILED THE EMERGENCY POWER ACTUATION CABLE SYSTEM TEST. ADJUSTED DOOR EMERGENCY ACTUATION CABLE, FUNCTIONAL CHE CK GOOD. (M) 2 L 7 2 4F RT A2NM 2001082200235 20010822 00235 NM 2001 8 22 2001F00210 1 20010727 A 5297 WIRE ROPE BOEING 757 75723A 1384967 NM R2 DOOR OUT OF ADJ A K NONE O OTHER IN INSP/MAINT 1 WP 19 541NA 24291 R2 DOOR FAILED THE EMERGENCY POWER ACTUATION CABLE SYSTEM TEST. ADJUSTED DOOR EMERGENCY ACTUATION CABLE, FUNCTIONAL CHE CK GOOD. (M) 2 L 7 2 4F RT A2NM 2001082200236 20010822 00236 NM 2001 8 22 2001F00211 1 20010727 A 5297 WIRE ROPE BOEING 757 75723A 1384967 NM R1 DOOR OUT OF ADJ A K NONE O OTHER IN INSP/MAINT 1 WP 19 541NA 24291 R1 DOOR FAILED THE EMERGENCY POWER ACTUATION CABLE SYSTEM TEST. ADJUSTED DOOR EMERGENCY ACTUATION CABLE, FUNCTIONAL CHE CK GOOD. (M) 2 L 7 2 4F RT A2NM 2001082200237 20010822 00237 NM 2001 8 22 AALA20014040 1 20010605 A 5315 FLOORBEAM BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 689AA 25731 AFW - FOUND INNER T-CHORD HAS CORROSION REMOVAL ON UPPER AND LOWER SURFACE. REQUEST APPROVAL TO CONTINUE IN SERVICE AFT ER FOLLOWING NOTES LISTED IN 53-60-15-1 SRM PAGE 108. REMOVED EXISTING FASTENER. REMOVED CORROSION PER SRM. (M) 2 L 7 2 4F RT A2NM 2001082200238 20010822 00238 NM 2001 8 22 GAIA01267ST 1 20010806 A 5320 STRAP BOEING 727 727251 138408H NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING AN LTC INSPECTION , IT WAS DISCOVERED FLOORBEAM LOWER CHORD STABILIZATION STRAP IS CRACKED AT BS 328, RBL 25. AC COMPLISHED FLOORBEAM LOWER CHORD STABILIZATION STRAP REPAIR IAW B727 SRM 53-10-8, FIG 6. (M) 2 L 7 3 4F A3WE 2001082200239 20010822 00239 NM 2001 8 22 GAIA01268ST 1 20010806 A 5320 STRAP BOEING 727 727251 138408H NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING AN LTC INSPECTION, IT WAS DISCOVERED FLOORBEAM LOWER CHORD STABILIZATION STRAP IS CRACKED/BROKEN AT BS 360, LBL 2 5. ACCOMPLISHED FLOORBEAM LOWER CHORD STABILIZATION STRAP REPAIR IAW B727 SRM 53-10-8, FIG 6. (M) 2 L 7 3 4F A3WE 2001082200240 20010822 00240 NM 2001 8 22 GAIA01271ST 1 20010806 A 5315 FLOORBEAM BOEING 727 727251 138408H NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING AN LTC INSPECTION, IT WAS DISCOVERED LONGITUDINAL FLOOR BEAM UPPER CHORD EXFOLIATED BS 760-780 AND 800-820, INBOA RD LEG, RBL 45.5. ACCOMPLISHED FLOOR BEAM UPPER CHORD REPLACEMENT IAW B727 SRM 53-10-2 AND 51-30-5. (M) 2 L 7 3 4F A3WE 2001082200241 20010822 00241 NM 2001 8 22 GAIA01272ST 1 20010806 A 5530 WEB BOEING 727 727251 138408H NM VERTICAL STAB CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING AN LTC INSPECTION, IT WAS DISCOVERED STATION 1300 LEFT AND RIGHT CORNERS ON WEB HAVE .5 INCH CRACK. ACCOMPLISHED UPPER TORQUE BOX WEB REPAIR IAW B727 SRM 55-30-2, FIG 2 AND 51-40-2, FIG 1. (M) 2 L 7 3 4F A3WE 2001082200242 20010822 00242 NM 2001 8 22 GAIA01280ST 1 20010806 A 5347 FITTING BOEING 727 727251 138408H NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING AN LTC INSPECTION, IT WAS DISCOVERED CARGO TIE DOWN FITTING CRACKED BS 620, RBL 24, FORWARD CARGO PIT. ACCOMPLIS HED CARGO TIE DOWN FITTING REPLACEMENT IAW B727 SRM 51-30-2. (M) 2 L 7 3 4F A3WE 2001082200243 20010822 00243 NM 2001 8 22 GAIA01281ST 1 20010806 A 5743 SUPPORT BOEING 727 727251 138408H NM RT WING CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING AN LTC INSPECTION, IT WAS DISCOVERED RIGHT MAIN LANDING GEAR BEAM SUPPORT HAS UPPER LUG CRACKED. ACCOMPLISHED SU PPORT PIN REPLACEMENT AND TRIMMED RETAINER BOLT LUGS IAW SERVICE BULLETIN B727-57-0153, REV 4. (M) 2 L 7 3 4F A3WE 2001082200244 20010822 00244 NM 2001 8 22 GAIA01290ST 1 20010806 A 5230 WEB BOEING 727 727251 138408H NM CARGO DOOR CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING AN LTC INSPECTION, IT WAS DISCOVERED AFT CARGO DOOR C-3 INSIDE WEB IS CRACKED. ACCOMPLISHED INNER WEB REPAIR IAW B727 SRM 51-40-2 FIG 1 AND 52-30-1 FIG 6. (M) 2 L 7 3 4F A3WE 2001082200245 20010822 00245 NM 2001 8 22 GAIA01292OP 1 20010808 A 2781 CONNECTOR BOEING 727 727214 138407R NM L/E SLAT LOOSE A GAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 751US 21513 FLT 741 - PDX-OMA - NR 8 SLAT INDICATED 'INTRANSIT' AFTER RETRACTION. DUMPED FUEL TO LANDING WEIGHT. AIRCRAFT MADE AN UNEVENTFUL LANDING IN PDX. CLEANED AND RECONNECTED NR 8 SLAT CANNON PLUG AT ACTUATOR. PERFORMED NUMEROUS CYCLES OF SLA TS/FLAPS. SYSTEM OPERATES NORMALLY ON GROUND. THIS AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001082200246 20010822 00246 EA 2001 8 22 MASA01067 1 20010714 A 4970 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA APU MALFUNCTIONED A MASA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 77195 7195 FLT 9511 - ATL-PHL - HIGH APU OIL TEMP IN FLIGHT. THE AIRCRAFT HAS THE NR 1 GENERATOR DEFERRED. THE APU WAS A REQUIRED ITEM FOR THE NR 1 GENERATOR BEING MEL'D. THE CREW DECLARED AN EMERGENCY AND LANDED IN CLT. MAINTENANCE PERFORMED AND OPS CHECK AND COULD NOT DUPLICATE. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001082200247 20010822 00247 NM 2001 8 22 MASA01074 1 20010724 A 3350 6519020 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN BROKEN A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 445YV 445 DURING ROUTINE MAINTENANCE, FOUND THE NR 1 EMERGENCY ESCAPE PATH LIGHT HOUSING WAS BROKEN IN THE PAX COMPARTMENT. REMOV ED AND REPLACED ESCAPE LIGHTING, OPS CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 2001082200248 20010822 00248 SO 2001 8 22 MASA01078 1 20010727 A 3350 MS27473E10F35S CONNECTOR EMB 145 EMB145 SO CABIN DISCONNECTED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 828MJ 145218 FLT 5875 - DISCOVERED THE LAST THREE FLOOR EMERGENCY PROX LIGHTS INOPERATIVE. MAINTENANCE RESECURED THE NR 6 INVERTER C ANNON PLUG. OPS CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001082200249 20010822 00249 SO 2001 8 22 MASA01080 1 20010729 A 2612 SENSOR EMB 145 EMB145 SO LAVATORY DIRTY A MASA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 833MJ 145327 FLT 5770 - DCA-BTV - RETURNED TO DCA DUE TO LAV SMOKE MASTER WARNING CAME ON AFTER TAKEOFF. MAINTENANCE CLEANED THE LAV SMOKE SENSOR. OPS CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001082200250 20010822 00250 SO 2001 8 22 MASA01081 1 20010731 A 3320 LIGHT EMB 145 EMB145 SO GALLEY INOPERATIVE A MASA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 831MJ 145273 FLT 5853 - GALLEY OVERHEAD LIGHT BURNED OUT EMITTING A HOT PLASTIC SMELL. MAINTENANCE CLEANED OUT THE SODE AND RELAMPED . OPS CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001082200252 20010822 00252 SO 2001 8 22 SIMA200120201 1 20010721 A 3350 1100049 BATTERY EMB 135 EMB135LR SO CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 738NR 145401 CHA - FLT 4418 - CREW REPORTED TWO SECTIONS OF FLOOR PROXIMITY EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT POWER SUPPLY BATTERY IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001082200253 20010822 00253 EU 2001 8 22 SIMA200120701 1 20010724 A 5414 SKIN SAAB SF340 340B 7860101 EU LT NACELLE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 338SB 340B338 ABI - DURING AN HMBV INSPECTION, MAINTENANCE FOUND DAMAGE IN THE LEFT NACELLE EXTERIOR SKIN. DAMAGE WAS REPAIRED IAW SA AB REPAIR STATEMENT 340SDS002123. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001082200254 20010822 00254 SO 2001 8 22 SIMA200120801 1 20010727 A 3244 315501 TIRE EMB 135 EMB135LR SO MLG DAMAGED A SIMA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SW 21 703MR 145173 BOS - FLT 5056 - DURING TAKEOFF, THE NR 3 TIRE SHREDDED. CREW WAS INFORMED BY ATC. CREW CIRCLED TO BURN OFF FUEL AND T HEN LANDED WITHOUT FURTHER INCIDENT. EMERGENCY WAS DECLARED BY FLIGHT CREW. NR 3 MAIN TIRE WAS REMOVED AND REPLACED IA W EMB MM. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001082200255 20010822 00255 SO 2001 8 22 SIMA200121901 1 20010731 A 2530 BEAM EMB 135 EMB135LR SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 706RG 145194 ABI - DURING MBB INSPECTION, FOUND CORROSION ON THE GALLEY CENTER BEAM. CORROSION WAS REMOVED AND REPAIR WAS CARRIED OU T IAW EMB REPAIR STATEMENT. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001082200256 20010822 00256 SO 2001 8 22 SIMA200121902 1 20010731 A 5315 FLOORBEAM EMB 135 EMB135LR SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 706RG 145194 ABI - DURING MBV INSPECTION, MAINTENANCE FOUND CORROSION ON THE OMEGA BEAM AT FRAME 20. CORROSION WAS REMOVED AND REPAI R WAS CARRIED OUT IAW EMB SRM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001082200257 20010822 00257 SO 2001 8 22 SIMA200121903 1 20010731 A 5315 FLOORBEAM EMB 135 EMB135LR SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 706RG 145194 ABI - DURING MBV INSPECTION, MAINTENANCE FOUND CORROSION ON THE LEFT CENTER OMEGA BEAM AT FRAME 20. CORROSION WAS REMOV ED AND REPAIR WAS CARRIED OUT IAW EMB SRM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001082200259 20010822 00259 NM 2001 8 22 USAABB01077 1 20010801 A 3350 20121 CHARGER BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 628AU 27806 LAX - FOUND M733 EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE M-733 BATTERY CHARGER ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001082200260 20010822 00260 NM 2001 8 22 USAABB01078 1 20010803 A 3350 873100151REV12 LIGHT BOEING 757 757225 1384959 NM CABIN DEFECTIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 602AU 22196 BDL - FLOOR LEVEL EMERGENCY LIGHT ILLUMINATED WITH POWER ON AIRCRAFT. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001082200261 20010822 00261 NM 2001 8 22 USAABB01079 1 20010805 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 619AU 27198 CLT - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 1, 4, AND 26 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2001082200262 20010822 00262 EU 2001 8 22 USAAF01028 1 20010525 A 2170 5391 COALESCER BAG FOKKER F28 F28MK0100 4990807 EU AC BAY DIRTY A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 EA 19 857US 11289 STL-PIT - FLT 288 - UPON APPLICATION ON TAKEOFF THRUST, A STRONG, ACRID, MUSTY ODOR DEVELOPED IN THE COCKPIT AND AFT CAB IN AREAS. FLIGHT LANDED IN PIT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT AND RIGHT COALESCER BAGS. LEAK CHE CKED GOOD. RAN THE APU AND BOTH ENGINES. NO ODOR WAS DETECTED. VISUALLY INSPECTED THE APU AND ACM COMPARTMENTS FOR LE AKS. NONE WERE NOTED. (M) 2 L 7 2 4F RT 2001082200263 20010822 00263 EU 2001 8 22 USAAF01045 1 20010712 A 2611 SMOKE DETECTOR FOKKER F28 F28MK0100 4990807 EU LAVATORY MALFUNCTIONED A USAA K NONE N FALSE WARNING CL CLIMB 1 EA 19 898US 11398 ATL-CLT - FLT 1536 - AT FL100, THE SMOKE ALARMS BEGAN TO CHIME IN THE AFT LAVATORY. THE CHIME STOPPED A MINUTE LATER. NO SMOKE WAS OBSERVED. FLIGHT LANDED IN CLT WITHOUT INCIDENT. (M) 2 L 7 2 4F RT 2001082200264 20010822 00264 EU 2001 8 22 USAAF01048 1 20010717 A 2120 ODOR FOKKER F28 F28MK0100 4990807 EU CABIN DETECTED A USAA A UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 897US 11392 STL-CLT - FLT 1249 - THE LAVATORY SMOKE ALARM BEGAN TO CHIME AND AN ODOR OF SMOKE WAS PRESENT IN THE AFT CABIN AREA DURI NG CLIMB. THE FLIGHT RETURNED TO FIELD IN STL AND LANDED WITHOUT INCIDENT. MAINTENANCE RAN ENGINES AND APU. NO ODOR W AS DETECTED. THE TAIL SECTION AND AFT CARGO COMPARTMENTS WERE THEN INSPECTED FOR LEAKS AND FOR SIGNS OF SMOKE OR FIRE. NONE WERE FOUND. THE CABIN, LAVATORIES, AND LIGHTING BALLASTS IN THE AFT CABIN WERE ALSO INSPECTED. NO DEFECTS WERE F OUND. OK FOR SERVICE. (M) 2 L 7 2 4F RT 2001082200265 20010822 00265 EU 2001 8 22 USAASA01032 1 20010630 A 3350 32145510 POWER SUPPLY AIRBUS A321 A321211 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 166US 1170 1436 PHL - THE EMERGENCY LIGHTS TEST FAILED. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNITS AT FIN LOCATIONS 12WL AND 15W L. THE SYSTEM TESTED OK FOR SERVICE (M) 2 L 7 2 4F RT A28NM 2001082200266 20010822 00266 EU 2001 8 22 USAASA01039 1 20010731 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 174US 724 1492 PHL - THE EMERGENCY LIGHT SYSTEM WILL NOT TEST. MAINTENANCE REPLACED AN EMERGENCY POWER SUPPLY UNIT. (M) 2 L 7 2 4F RT A28NM 2001082200267 20010822 00267 2001 8 22 USAASB01218 4 20010801 A 2565 D19859103 POWER UNIT BOEING 737 737301 1384611 NM ESCAPE SLIDE FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 575US 23740 CLT - DURING ANNUAL OPERATIONAL CHECK OF THE FORWARD RIGHT SERVICE DOOR ESCAPE SLIDE, THE SLIDE DEPLOYED NORMALLY BUT TH E SLIDE MOUNTED EMERGENCY LIGHTS FAILED TO ILLUMINATE. SLIDE OPERATIONAL CHECK FAILED. MAINTENANCE FOUND THE POWER UNI T ASSEMBLY FOR THE ESCAPE SLIDE MOUNTED LIGHTS HAD FAILED. MAINTENANCE REMOVED AND REPLACED THE FORWARD RIGHT SERVICE D OOR ESCAPE SLIDE ASSEMBLY. TWO ADDITIONAL OPERATIONAL CHECKS ARE SCHEDULED TO BE CONDUCTED AT THE FORWARD RIGHT SERVIC E DOOR POSITION. (M) 2 L 7 2 4F RT A16WE 2001082200268 20010822 00268 2001 8 22 VNAA0108002 4 20010805 A 3460 COMPUTER DORNER DO32 DO328100 2996000 NM COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 438JS 3056 PIT - FLT 4066 - DURING THE TAKEOFF ROLL, THE CREW RECEIVED A FGC LAP FAIL CAS MESSAGE. THE CREW ABORTED TAKEOFF. AS F LIGHT 4066, EXITED THE RUNWAY THE MESSAGE CLEARED AND MAINTENANCE CONTROL REQUESTED THAT THE FLIGHT CONTINUE TO CAE. FL IGHT THEN DEPARTED WITH NO FURTHER INCIDENTS. (M) 2 H 7 2 4T RT A45NM 2001082300001 20010823 00001 SO 2001 8 23 C2XA01CL195 1 20010822 A 3350 20131A BATTERY EMB 145 EMB145LR SO DISCHARGED A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 13964 13118 145123 CLE FLT. #3369 THE CREW REPORTED 2 FLOOR EMERGENCY LIGHT STRIPS INOPERTIVE.MAINTENANCE REPLACED #3 EMERGENCY FLOOR LI GHTING BATTERY PACK AND CHARGER BASE. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT WAS RELEASED TO SERVICE. 2 L 7 2 4T RT T00011AT 2001082300004 20010823 00004 WP 2001 8 23 RRXA010065 1 20010810 A 7722 CONNECTOR DOUG DC8 DC873F 302199F WP #4EGT HARN LOOSE A RRXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 602AL 45991 ON CLIMB OUT #4 EGT GAUGE FAILED (ANALOG & DIGITAL) ALL ENG INDICTORS NORMAL. AFTER 40 MIN #4 EGT GUAGE STARTED WORKIN G AGAIN. *** CORRECTIVE ACTION *** FOUND EGT HARNESS CONNECTOR NOT PROPERLY SECURED ON #4 EGT INDICATOR. SECURED CONN ECTOR ON #4 EGT INDIC ATOR. INSPECTED EGT PIGTAIL HARNESS ON #4 ENGINE. PERFORMED EGT INDICATOR TEST IAW DC-8MM 77-20-1 5  AND #5 EGT INDICATION GOOD. 2 L 7 4 4F RT 4A25 2001082300005 20010823 00005 NM 2001 8 23 0102856641 1 20010815 A 3350 POWER SUPPLY BOEING 747 747212B 1384886 NM EMER ESC PATH LT A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 641NW 21941 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE IN ZONE 'B'. REPLACED THE EMERGENCY LIGHTS POWER SUPPLY. OPEATIONAL CHECK NORMAL. 2 L 7 4 4F A20WE 2001082300006 20010823 00006 NM 2001 8 23 0102886628 1 20010813 A 2932 50234 TRANSMITTER BOEING 747 747251B 1384892 NM NBR 3 HYD SYSTEM LEAKING A NWAA A UNSCHED LANDING K FLUID LOSS UK UNKNOWN 1 GL 01 628US 64090 1370 22389 DURING FLIGHT, THE HYDRAULIC FLUID QUANTITY INDICATED LOW IN THE NBR 3 SYSTEM. AIRCRAAFT RETURNED TO NRT AND LANDED WITH OUT INCIDENT. REPLACED THE HYDRAULIC PRESSURE TRANSMITTER. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2001082300007 20010823 00007 WP 2001 8 23 0102919852 1 20010812 A 3260 PROXIMITY SWITCH DOUG DC9 DC951 3022051 WP NLG BROKEN A NWAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 01 761NC 47709 DURING APPROACH FOR LANDING AFTER GEAR SELECTED DOWN, RED NOSE GEAR UNSAFE LIGHT ILLUMINATED. FOLLOWED COM PROCEDURE WIT H NO CHANGE IN STATUS. FLIGHT PERFORMED ONE GO-AROUND AND LANDED WITHOUT INCIDENT. REPLACED A BROKEN NOSE GEAR DOWNLO CK PROXIMITY SWITCH. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 2001082300008 20010823 00008 CE 2001 8 23 0015 1 20010821 A 3222 50810034 TORQUE LINK BEECH 90 E90 1152914 CE MLG CRACKED E CIEA K NONE O OTHER IN INSP/MAINT 1 NM 03 63BV 980 LW256 DURING THE COMPLIANCE OF RAYTHEON RECURRING SERVICE BULLETIN 32-3134, INSPECTION OF THE MAIN LANDING GEAR TORQUE KNEE'S, CRACKS WERE FOUND IN THE RADIUS AREA OF THE UPPER TORQUE KNEE, ON EACH SIDE OF THE SINGLE LUG. THE CRACK IN THIS WAS I N THE AREA NOTED TO BE INSPECTED ON THE SERVICE BULLETIN. THE TOTAL TIME AND TOTAL LANDINGS ON THE SPECIFIC UNIT ARE UN KNOWN. THIS UNIT WAS INSPECTED AT 980 LANDINGS PRIOR TO THIS AND UNIT WAS FOUND TO BE OK AT THAT TIME. 1 L 7 2 3T 3A20 2001082300009 20010823 00009 CE 2001 8 23 0016 1 20010822 A 3222 50810034 TORQUE LINK BEECH 90 E90 1152914 CE MLG CRACKED E CIEA K NONE O OTHER IN INSP/MAINT 1 NM 03 87CH 840 LW20 DURING INSPECTION OF UPPER TORQUE KNEE PER THE REQUIREMENTS OF RAYTHEON REOCCURRING SERVICE BULLETIN 32-3134, THE LEFT U PPER TORQUE KNEE ON ONE OF THE MAIN GEARS WAS NOTED TO BE CRACKED IN THE RADIUS OF THE SINGLE LUG. THIS CRACK WAS IN LO CATION NOTED TO BE REVIEWED BY THE SERVICE BULLETIN. THIS UNIT WAS INSPECTED AT 840 LANDING PRIOR TO THIS AND WAS FOUND TO BE OKAY. 1 L 7 2 3T 3A20 2001082300010 20010823 00010 CE 2001 8 23 0121 1 20010816 A 5210 99120754 SEAL CESSNA 500 550 2076604 CE PAX DOOR DAMAGED E DJFA B A EMER. DESCENT UNSCHED LANDING O OTHER CR CRUISE 1 EA 23 270CW 5500570 AIRCRAFT WAS FLYING AT FL39, HEARD AN AIR NOISE NEAR THE CABIN DOOR. STARTED TO LOOSE PRESSURIZATION. DECLARED AN EMER GENCY AND DESCENDED TO A SAFE ALTITUDE. DIVERTED TO LIT AND LANDED WITHOUT INCIDENT. MX DETERMINED THE CABIN DOOR SEAL WAS BAD AND REPLACED WITH NEW, THE AIRCRAFT WAS TEST FLOWN AND FOUND TO BE OK. 1 L 7 2 4F A22CE 2001082300011 20010823 00011 EU 2001 8 23 01FDEA00760 1 20010822 A 2421 GENERATOR AIRBUS 300 A300F4605R 3930327 EU APU FAILED A FDEA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 25 669FE 774 CLIMBING OVER ATLANTIC OCEAN INTO LINE OF THUNDERSTORMS WITH NR 2 GEN ALREADY INOP. AT ABOUT FL 200 APU GEN FAULTED & W /N RESET, ELECTED TO RETURN TO FLL. 2 L 7 2 4F RT A35EU 2001092600057 20010926 00057 WP 2001 9 26 01FDEA00762 1 20010821 A 5720 SPLICE DOUG DC10 DC1010 3022110 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 390FE 46624 FWD RT WING ROOT, SPLICE FITTING AT FUSELAGE TO WING FRONT SPAR LWR CHORD IS CRACKED BETWEEN TWO FASTENER HOLES. NDT VE RIFIED STA 1156 XCW 118. REMOVED AND REPLACED DOUBLER PER EA 58-5710-59060. 2 L 7 3 4F A22WE 2001082300012 20010823 00012 2001 8 23 COMA0160626 4 20010820 A 2200 6224404001 SERVO CNDAIR CL600 CL6002B19 EA BELLY FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 917CA 690 7017 FLIGHT #5800. DESTINATION CVG, DURING CRUISE FLIGHT THE AUTO PILOT FAILED @ FL28. EXCESSIVE INPUT FORCE WAS REQUIRED FOR AILERON CONTROL, FLIGHT WAS DIVERTED TO IAD AND LANDED SAFELY.REPLACED THE PRIMARY AILERON SERVO (SVO-85A). 2 L 7 2 4F RT A21EA 2001082300013 20010823 00013 NM 2001 8 23 01FDEA00763 1 20010822 A 2613 WARNING LIGHT BOEING 727 727233 138408A NM OVERHEAT DETECT MALFUNCTIONED A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 SO 25 270FE 22035 ON CLIMBOUT LWR AFT BODY OVERHEAT LIGHT ILLUM'D BET 180 & 200 ACCOMP RED TAB PROCED & THE LIGHT CK'D GOOD ON TEST & CONT INUED FLT ON NR 1 BLEED & PACK. RED TABS SAID LEAK IS BET NR 3 BLEED VALVE & NR 2 PACK VALVE. RAN ENGS AND CND CK'D AL L LOOPS IN AFT AIRSTAIRS & APU AREAS, NO DEFECTS NOTED. RAN ENGS AND CK'D BLEED AIR SYS PER 727-200 JRH, NO LEAK NOTED. 2 L 7 3 4F RT A3WE 2001082300014 20010823 00014 WP 2001 8 23 AT0100224 1 20010822 A 2130 DUCT DOUG DC9 DC932 3022066 WP LOOSE A ZZDA K NONE J WARNING INDICATION CR CRUISE 1 SO 15 832AT 47451 CABIN PRESSURE LIGHT ILLUMINATED. CORRECTIVE ACTION: TIGHTENED LOOSE DUCT OPS CHECKED GOOD IAW DC9 MM 21-30. 2 L 7 2 4F A6WE 2001082800160 20010828 00160 NM 2001 8 28 01FDEA00764 1 20010822 A 3610 COUPLING BOEING 727 7272D4 138407U NM PNEUMATIC SYS LEAKING A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SO 25 287FE 21849 LWR AFT BODY OVERHEAT LIGHT ILLUM'D AFTER LEVEL OFF, ACCOMP'D RED TABS, RED TABS CONFIRMED NR 3 BLEED LEAK BET BLEED VAL VE & PACK VALVE. REMOVED AND REPLACED COUPLING, SLEEVE, RING AND RETAINER PER SMP. 2 L 7 3 4F A3WE 2001101200056 20011012 00056 NE 2001 10 12 2001UALA01627 2 20010801 A 7200 ENGINE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE NR 2 MALFUNCTIONED A UALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 WP 29 607UA 21868 IN CRUISE LEFT ENG EPR APPROX 1.3 EPR HIGHER THEN RT ENG WITH ALL OTHER PARA EQUAL. IN CLIMB WITH THROTTLES EQUAL RT PA RA'S MUCH HIGHER THEN LEFT. LOUD RESONANCE SOUND ROWS 19-24 DURING PWR CHANGES. *S/D* THE NR 2 ENGINE WAS REPLACED FO R DIFFERENCES IN EPR BETWEEN ENGINES AND PERFORMANCE DETERIORATION. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082900054 20010829 00054 NM 2001 8 29 2001UALA01668 1 20010812 A 3610 REGULATOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BLEED AIR FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 323UA 23955 UNSCHEDULED LANDING DUE TO UNABLE TURN OFF LEFT BLEED SYSTEM. THE NR 1 ENGINE BLEED AIR REGULATOR FAILED OPEN. REPLACED NR 1 ENGINE BLEED AIR REGULATOR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082300016 20010823 00016 NM 2001 8 23 AWXA0002167 1 20010727 A 5523 6502579619 TAB BOEING 737 7373B7 1384580 NM ELEVATOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 332AW 23384 LEFT ELEVATORS TAB CRACKED AT ALL HINGE CUTOUTS AND INBOARD EDGE. BONDED GRAPHITE OVERLAYS REPAIRS TO HINGE CUTOUT AREA S AND INBOARD END IAW B737 SRM 51-70-19. WEIGHED TAB AND RESTORED FINISH IAW B737 SRM 51-00-06. 2 L 7 2 4F RT A16WE 2001082300017 20010823 00017 EU 2001 8 23 AWXA0002172 1 20010807 A 5320 D53112067201 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 FR 20 TO FR 21 Y-1732 R/11 FLOOR SUPPORT CORRODED. REPAIRED AS PER AWA ER 26-5311-01277-DL1. 2 L 7 2 4F RT A28NM 2001082300018 20010823 00018 GL 2001 8 23 C2XA01CL194 2 20010820 A 7530 23070418 TUBE EMB 135 EMB135LR SO ALLSN AE300 AE3007A GL NR 1 ENGINE BROKEN A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 17521 145378 LGA-MSN FLIGHT 3465 DURING FLIGHT THE CREW REPORTED HIGH ITT AND HIGH FUEL FLOW ON THE NR 1 ENGINE. THE AIRCRAFT DIVERT ED INTO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND THE NR 1 ENGINE START BLEED CONT ROL VALVE TUBE ASSEMBLY TO BE BROKEN. THE TUBE IS FROM THE DIFFUSER TO THE START BLEED CONTROL VALVE. THE TUBE WAS REP LACED AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT TOOO11AT TE6CH 2001082300019 20010823 00019 EU 2001 8 23 DHL2001363018 1 20010821 A 2612 CONNECTOR AIRBUS 300 A300B4203 3930306 EU FIRE LOOP DIRTY A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 363DH 85 ENGINE NR 1 LOOP-A LIGHT WILL NOT ILLUMINATE WHEN LOOP-A IS TESTED. DEFERRED NR 1 ENGINE LOOP-A IAW MEL 26-12-01. DMI 6815. FOUND HIGH RESISTANCE AT NR 1 ENGINE LOOP-A NACELLE CONNECTORS. CLEANED CONNECTORS AND RESISTANCE CHECKS GOOD. NR 1 ENGINE A-LOOP TESTS GOOD PER MM 26-12-00. THIS CLEARS DMI 6815. 2 L 7 2 4F RT A35EU 2001082300020 20010823 00020 EU 2001 8 23 DHL2001365030 1 20010817 A 2612 CONNECTOR AIRBUS 300 A300B4203 3930306 EU FIRE LOOP CORRODED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 365DH 149 DURING PRE-DEPARTURE CHECK, ENGINE NR 2 LOOP-B TEST NOT FUNCTIONING. TRANSFERRED TO DMI 6780 PER MEL-26-13-03 CAT C. 0 8/18/2001 REMOVED AND REPLACED FIRE DETECTION BOX; NO HELP. ITEM REMAINS ON DEFERRAL. NOTE: BOX DID TEST GOOD. REMOV ED CORROSION AND RETIGHTENED NR 2 ENGINE B-LOOP CONNECTORS. SYSTEM OPS CHECKED GOOD PER A300 MM 26-12-00, CLEARING DMI 6780. 2 L 7 2 4F RT A35EU 2001082300021 20010823 00021 EU 2001 8 23 DHL2001365031 1 20010818 A 5751 SKIN AIRBUS 300 A300B4203 3930306 EU AILERON DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH 149 LEFT WING I/B AILERON DELAMINATED. REMOVED LT ALLSPEED AILERON IAW AMM 27-11-28. AREA INSPECTED LT ALLSPEED AILERON CO MPARTMENT, NO VISABLE DEFECT NOTED. REMOVED AND REPLACED TOP AND BOTTOM SKIN PLANKS IAW A-300 SRM 51-42-20 AND 57-56-12 . REINSTALLED LT ALLSPEED AILERON IAW 27-11-28, OPS CHECK PERFORMED OK IAW SAME REF. 2 L 7 2 4F RT A35EU 2001082300023 20010823 00023 EU 2001 8 23 DHL2001366021 1 20010805 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU CABIN MALFUNCTIONED A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 366DH 249 UPPER MAIN DECK SMOKE DETECTORS FWD LT AND RT WILL NOT EXTINGUISH. COOLED A/C WITH A/C CART AFTER A/C COOLED SYSTEM, TE STED NORMAL PER A300 M/M 26-11-14. 2 L 7 2 4F RT A35EU 2001082300025 20010823 00025 NM 2001 8 23 DHL2001712009 1 20010818 A 3350 SWITCH BOEING 727 72729 1384007 NM CABIN LACK OF LUBE A DHLA K NONE L NO TEST UK UNKNOWN 1 SO 01 712DH 19401 EMERGENCY EXIT ARMING SWITCH-GUARD DOES NOT MOVE SWITCH FROM ON TO ARMED WHEN GUARD IS CLOSED. LUBED SWITCH, OPS CHECKE D GOOD IAW 727 MM 20-60-02. 2 L 7 3 4F A3WE 2001082300028 20010823 00028 NE 2001 8 23 RAIA00108018 2 20010816 A 7300 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RT ENGINE LOOSE A RAIA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 CE 03 564HK 41081 76092 5369-EWR-RIGHT ENGINE INDICATED RPM DROP TO 48%, CREW PERFORMED PRECAUTIONARY ENGINE SHUTDOWN, AIRCRAFT LANDED WITHOUT I NCEDENT. MAINTENANCE INSPECTED AND FOUND LOOSE CANNON PLUG CONNECTOR ON THE RIGHT FUEL PRESSURE TRANSDUCER. MAINTENANCE RESECURED CONNECTOR AND PERFORMED OPERATIONAL CHECK OF RIGHT ENGINE. OPERATIONAL CHECK OF RIGHT ENGINE CHECKED GOOD, AIR CRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T 4 T RT A41NM E18NE 2001082300029 20010823 00029 2001 8 23 RAIA00108017 4 20010812 A 3442 7008470822 RECEIVER JETAIR JETSTM JETSTM4101 1500501 EU RADOME FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 559HK 7270 594 41075 5363-EWR-ON TAXI OUT WEATHER RADAR WOULD NOT PAINT ANY WEATHER OR GROUND RETURNS. MAINTENANCE INSPECTED AND REPLACED WEA THER RADAR RECEIVER/TRANSMITTER. 2 L 7 2 4T RT A41NM 2001082300030 20010823 00030 NM 2001 8 23 DHL2001717018 1 20010818 A 2612 INSULATOR BOEING 727 72723 1384004 NM FIRE LOOP BROKEN A DHLA K NONE N FALSE WARNING CR CRUISE 1 SO 01 717DH 19389 ENGINE FIRE DETECTION LIGHT FOR ENGINE NR 3 ON P6-3 PANEL OCCASIONALLY ILLUMINATES DURING CRUISE FLIGHT. LIGHT DEFERRED PER DHL MEL 26-9. PLACARD INSTALLED DMI 6791 CAT C. FOUND BROKEN INSULATION AND FIRE LOOP CONNECTOR CHAFING AGAINST B RACKET. PROVIDED CLEARANCE AND REPAIRED INSULATION. SYSTEM OPS CHECKED GOOD PER B-727 MM 26-11-0, CLEARING DMI 6791. 2 L 7 3 4F A3WE 2001082300031 20010823 00031 WP 2001 8 23 DHL2001804524 1 20010811 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 MAIN CARGO COMPT CTR FLOOR TRACK LUG WORN AT STA 70.00. CUT OUT DAMAGED LUG AT MAIN CARGO COMPT CTR FLOOR TRACK STA 70. 00 IAW SRM 53-2-3 PG 17-19. FABRICATED TRACK PLUG (P/N 52772660) IAW 57-2-3 PG 17-19. INSTALLED CTR FLOOR TRACK PLUG AT MAIN CARGO COMPT STA 70.00 IAW SRM 53-2-3 PG 17-19 AND SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2001082300032 20010823 00032 WP 2001 8 23 DHL2001804525 1 20010811 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 MAIN CARGO COMPT 2 LT FLOOR TRACK LUG WORN AT STA 220.00. CUT OUT DAMAGED LUG AT MAIN CARGO COMPT NR 2 LT FLOOR TRACK STA 220.00 IAW SRM 53-2-3 PG 17-19. FABRICATED TRACK PLUG (P/N S2772660) IAW 57-2-3 PG 17-19. INSTALLED CTR FLOOR TRAC K PLUG AT MAIN CARGO COMPT STA 220.00 IAW SRM 53-2-3 PG 17-19 AND SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2001082300033 20010823 00033 WP 2001 8 23 DHL2001804526 1 20010805 A 5751 SKIN DOUG DC8 DC873F 302199F WP AILERON DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 RT OUTBOARD AILERON UPPER SKIN SURFACE DENTED AT STA XRS 659. CUT DAMAGED AREA IAW 57-2-1 PAR 16. FABRICATED DOUBLER A ND INSTALLED ON RT OUTBOARD AILERON UPPER SKIN SURFACE IAW SRM 57-2-1 PAR 16, SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2001082300034 20010823 00034 WP 2001 8 23 DHL2001804527 1 20010809 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP COCKPIT BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 COCKPIT F/E FWD & AFT SEAT TRACKS BROKEN. REMOVED BROKEN SEAT TRACKS IAW SRM 51-8-0 PAR 1. INSTALLED NEW SEAT TRACKS I AW SRM 51-8-0. 2 L 7 4 4F RT 4A25 2001082300035 20010823 00035 WP 2001 8 23 DHL2001804528 1 20010811 A 5751 AILERON DOUG DC8 DC873F 302199F WP RT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 RT OUTBOARD AILERON T/E DENTED STA XRS693.00-XRS 727.00. REMOVED RT OUTBOARD AILERON T/E DEFORMED (STA XRS 693.00-727.0 0 IAW SRM 57-1-21A PG 1.FABRICATED NEW T/E IAW SRM 57-2-1 PAR 16. INSTALLED NEW T/E IAW SRM 51-1-21A. 2 L 7 4 4F RT 4A25 2001082300036 20010823 00036 NM 2001 8 23 AWXA0002168 1 20010803 A 5313 655162829 STRINGER BOEING 737 73733A 1384673 NM STR 26L CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 D: BS 947 STR 26L corrodedC: Removed stringer , repaired & reinstalled stringer 26L @ BS 907-1016 IAW Boeing 737 SRM 53- 00-03 pg 201-207, 51-40-02 pg 3-4, 51-20-01 pg 10 & 47 & 51-20-00 pg 1 2 L 7 2 4F RT A16WE 2001082300037 20010823 00037 NM 2001 8 23 AWXA0002169 1 20010803 A 5313 655162812 STRINGER BOEING 737 73733A 1384673 NM STR 27R CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 D: Stringer 27R corroded at BS 965C: Removed , repaired & reinstalled stringer 27R @ BS 907-1016 IAW boeing 737 SRM 53-0 0-03 pg 101-102, 53-00-03 pg 201-207, 51-20-01 pgs 1,10 &47 & 51-40-02 pg 3-4 2 L 7 2 4F RT A16WE 2001082300046 20010823 00046 2001 8 23 RAIA00108020 4 20010821 A 3420 HG2010AC02 COMPUTER EMB 145 EMB145ER SO AVIONICS BAY FAILED A RAIA D RETURN TO BLOCK I FLT. ATTITUDE INST. TX TAXI/GRND HDL 1 CE 03 808HK 4444 145157 5263-ERI-NUMBER TWO AHRS FAILED PRIOR TO TAKE OFF ROLL. MAINTENANCE INSPECTED AND REPLACED THE NUMBER TWO AHRS COMPUTER. 2 L 7 2 4F RT T00011AT 2001082300047 20010823 00047 EU 2001 8 23 RAIA00108021 1 20010821 A 2435 8260121 STARTER AEROSP ATR42 ATR42300 8680920 EU LEFT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 423TE 24779 2055 119 7326-STL-LEFT ENGINE WOULD NOT START, STARTER WOULD NOT STAY ENGAGED ABOVE 10% NH. MAINTENANCE INSPECTED AND REPLACED TH E LEFT ENGINE STARTER/GENERATOR. 2 H 7 2 4T RT A53EU 2001082300049 20010823 00049 SO 2001 8 23 ASOA01115 1 20010723 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 267AS 19965 120198 FLT 4147 - DURING GROUND INSPECTION IN ATL, EMERGENCY LIGHTS AT ROW 5 WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D A BAD EMERGENCY LGIHT BATTERY PACK. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001082300050 20010823 00050 SO 2001 8 23 ASOA01117 1 20010725 A 3397 M2275941249 WIRE EMB 120 EMB120 3260201 SO CABIN CHAFED A K NONE L NO TEST IN INSP/MAINT 1 SO 11 265AS 120170 DURING GROUND INSPECTION IN DFW, SOME EMERGENCY LIGHTS IN CABIN WERE INOPERATIVE. MAINTENANCE REPAIRED CHAFED WIRING ON CABIN EMERGENCY FLOOR LIGHTING. (M) 2 L 7 2 4T RT A31SO 2001082300051 20010823 00051 SO 2001 8 23 ASOA01119 1 20010728 A 5300 SKIN EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 285AS 120265 WHILE PERFORMING HANGAR INSPECTION IN MCN, BELLY SKIN CORROSION WAS FOUND AT THE TCAS ANTENNA, FRAME 21 AT STRINGERS 21 LEFT TO 19 RIGHT. MAINTENANCE REPAIRED CORROSION IAW ASA EO120-53-0164. THIS EO OUTLINES THE REPAIR FOR N285AS. AIRCR AFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001082300052 20010823 00052 SO 2001 8 23 ASOA01121 1 20010729 A 3350 D36604001 BATTERY PACK EMB 120 EMB120 3260201 SO CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 245AS 120075 FLT 4934 - DURING GROUND INSPECTION IN DFW, FLIGHT ATTENDANT REPORTED AFT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REM OVED AND REPLACED EMERGENCY LGIHT BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001082300053 20010823 00053 NM 2001 8 23 TSAA0153098 1 20010727 A 5300 6545813508 SKIN BOEING 737 737209 NM FWD SERV DOOR CRACKED A TSAA O OTHER O OTHER IN INSP/MAINT 1 WP 13 827AL 23913 IDENTIFIED 1.25 INCH SKIN CRACK AT FORWARD SERVICE DOOR LOWER AFT SECTION. (M) 2 L 7 2 4F RT A16WE 2001082300054 20010823 00054 NM 2001 8 23 TSAA0133091 1 20010712 A 3300 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM PAX CABIN INOPERATIVE A TSAA O OTHER O OTHER IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED NR 6 FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2001082300055 20010823 00055 NM 2001 8 23 TSAA0133093 1 20010725 A 3300 9221009 BATTERY PACK BOEING 737 7372X6C 1384552 NM PAX CABIN INOPERATIVE A TSAA O OTHER O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED AFT SERVICE DOOR IDENT POWER PACK DUE TO LOW VOLTAGE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001082300056 20010823 00056 NM 2001 8 23 TSAA0133094 1 20010720 A 3300 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM PAX CABIN INOPERATIVE A TSAA O OTHER O OTHER IN INSP/MAINT 1 WP 13 817AL 39735 REPLACED NR 1 FLOOR EMERGENCY LGIHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001082300057 20010823 00057 NM 2001 8 23 TSAA0133095 1 20010718 A 3300 86210066 BATTERY PACK BOEING 737 737282 13844AT NM CABIN CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 824AL 23045 AFT ENTRY DOOR EMEREGNCY IDENT LIGHT INOPERATIVE. REPLACED BATTERY PACK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001082300058 20010823 00058 NM 2001 8 23 TSAA0133096 1 20010718 A 3300 6013211 BATTERY PACK BOEING 737 737282 13844AT NM CABIN CORRODED A TSAA O OTHER O OTHER IN INSP/MAINT 1 WP 13 824AL 23045 FOUND LEFT OVERWING EMERGENCY IDENT LIGHT INOPERATIVE. REPLACED BATTERY PACK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001082300059 20010823 00059 EU 2001 8 23 USAAF01057 1 20010727 A 3350 362624 LIGHT FOKKER F28 F28MK0100 4990807 EU PAX CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 889US 11358 PIT - THE EMERGENCY EXIT TRACK LIGHTING AT ROWS 9 AND 10 WERE INOPERATIVE. MAINTENANCE REPLACED THE TRACK LIGHTING STRI P. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT 2001082300060 20010823 00060 WP 2001 8 23 USAAD01141 1 20010730 A 3350 9721055 BATTERY DOUG DC9 DC982 3022082 WP PAX CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 829US 49429 BOS - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001082300061 20010823 00061 WP 2001 8 23 USAAD01140 1 20010729 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 826US 48026 IND - ON LOW LEVEL EMERGENCY LIGHT AND THE LEFT AND RIGHT EXIT PATH LIGHTS A PASSENGER SEAT ROW 19 WERE INOPERATIVE. MA INTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001082300062 20010823 00062 WP 2001 8 23 USAAD01139 1 20010728 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 812US 48092 PIT - THE CEILING MOUNTED EMERGENCY LIGHTS A PASSENGER SEAT ROWS 11-16 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERG ENCY LIGHTS BATTERIES. (M) 2 L 7 2 4F A6WE 2001082300063 20010823 00063 NM 2001 8 23 GAIA01266ST 1 20010806 A 5320 INTERCOSTAL BOEING 727 727251 138408H NM BS 298 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED INTERCOSAL UPPER FLANGE CRACKED AT BS 298, RBL 12 ABOVE PULLEY BRACKET. ACCOMPLISHED INTERCOSTAL REPLACEMENT IAW B727 SRM 53-10-2, FIG 7 AND 51-30-2. (M) 2 L 7 3 4F A3WE 2001082300064 20010823 00064 NM 2001 8 23 GAIA01265ST 1 20010806 A 5320 ANGLE BOEING 727 727251 138408H NM BS 312 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED FLOOR SUPPORT ATTACH ANGLE CRACKED AT BS 312, LBL 12 IS CRACKE D. ACCOMPLISHED FLOOR SUPPORT ATTACH ANGLE REPLACEMENT IAW B727 SRM 53-10-2, FIG 7, 51-20-1, FIG 7 AND 51-30-2. (M) 2 L 7 3 4F A3WE 2001082300065 20010823 00065 NM 2001 8 23 GAIA01264ST 1 20010806 A 5300 ANGLE BOEING 727 727251 138408H NM BS 304-312 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED FLOOR SUPPORT ATTACH ANGLE CRACKED AT BS 304-312, LBL 20 PLUS 30. ACCOMPLISHED FLOOR SUPPORT ATTACH ANGLE REPLACEMENT IAW B727 SRM 51-20-1 AND 51-20-2. (M) 2 L 7 3 4F A3WE 2001082300066 20010823 00066 NM 2001 8 23 GAIA01263ST 1 20010806 A 5300 FITTING BOEING 727 727251 138408H NM BS 720 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED CARGO TIE DOWN FITTING CRACKED BS 720A, LBL 24, LBL 24, WL 156 , FORWARD CARGO PIT. ACCOMPLISHED CARGO TIE DOWN FITTING REPLACEMENT IAW B727 SRM 51-30-2. (M) 2 L 7 3 4F A3WE 2001082300067 20010823 00067 NM 2001 8 23 GAIA01262ST 1 20010806 A 5200 WEB BOEING 727 727251 138408H NM BS 420 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED E/E COMPARTMENT DOOR, RIGHT WEB HAS TWO CRACKS EMANATING FROM PUNCTURE. ACCOMPLISHED WEB REPAIR BS 420 IAW B727 SRM 51-40-2, FIG 1. (M) 2 L 7 3 4F A3WE 2001082300068 20010823 00068 NM 2001 8 23 GAIA01261ST 1 20010806 A 5242 DOOR FRAME BOEING 727 727251 138408H NM E&E BAY DOOR CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING AN LTC INSPECTION, DISCOVERED E/E COMPARTMENT DOOR FRAME LEFT AFT SIDE AFT SIDE OF FRAME LOWER CORNER CRACKED. A CCOMPLISHED BS 420 FRAME REPAIR IAW B727 SRM 51-40-3, FIG 1. (M) 2 L 7 3 4F A3WE 2001082300069 20010823 00069 NM 2001 8 23 GAIA01260ST 1 20010806 A 5500 ELEVATOR BOEING 727 727251 138408H NM CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED RIGHT ELEVATOR HAD CORROSION, BOTTOM SIDE, ELEVATOR STATION 66 , AREA IS MARKED. ACCOMPLISHED ELEVATOR SKIN REPAIR IAW B727 SRM 55-20-3, FIG 1. (M) 2 L 7 3 4F A3WE 2001082300070 20010823 00070 EA 2001 8 23 MASA01051 1 20010518 A 4900 3800488 APU CNDAIR CL600 CL6002B19 EA AFT FUSELAGE INOPERATIVE A MASA O OTHER J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 07 17275 7275 FLT 6072 - ON APPROACH TO PHX, THE CAPTAIN STARTED THE APU AND HAD AN OIL PRESSURE LOW CAUTION MSG IN FLIGHT, FOLLOWED B Y A SMALL AMOUNT OF SMOKE IN COCKPIT. CREW SHUT DOWN THE APU AND LANDED WITHOUT INCIDENT. MAINTENANCE DEFERRED THE APU AND THE AIRCRAFT WAS RETURNED TO SERVICE. APU REMOVED AND REPLACED. OP CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2001082300071 20010823 00071 EA 2001 8 23 MASA01076 1 20010726 A 3350 81079390 LIGHT CNDAIR CL600 CL6002B19 EA CABIN MISSING A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27173 7173 DURING ROUTINE MAINTENANCE IT WAS DISCOVERED THAT THE FLOOR EMERGENCY LIGHT ARROW STRIPS WERE MISSING. MAINTENANCE INST ALLED THE THREE MISSING STRIPS. OPS CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001082300072 20010823 00072 EA 2001 8 23 NSVA0105 2 20010804 A 7230 COMPRESSOR BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA RT ENGINE STALLED A NSVA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 EA 27 210CJ UC110 32204 PILOT WAS IN FLIGHT AND FOUND THE TRIM WHEEL DIFFICULT TO MOVE AFTER ADVANCING POWER LEVERS. WHILE TRYING TO DUPLICATE PROBLEM IN FLIGHT BY ADVANCING AND RETARDING THROTTLES, THE PILOT REPORTED AN INSTANTANEOUS AND MOMENTARY SHUTDOWN OF TH E RIGHT ENGINE. MAINTENANCE PERFORMED GROUND RUN OF ENGINE AND VISUAL INSPECTION OF TRIM WHEEL AND CONTROL TAB, NO DEFE CTS NOTED, CHECKED NORMAL. QUALITY CONTROL INTERVIEWED PILOT AND DETERMINED THAT THE PILOT DID NOT ACCOMPLISH A RESTART OF ENGINE DUE TO THE FACT THAT THE ENGINE DID NOT SHUTDOWN IN FLIGHT. IT WAS SUSPECTED THAT THE PILOT EXPERIENCED A CO MPRESSOR STALL ACCORDING TO HIS ACCOUNTS. (M) 2 L 7 2 4T 4 T RT A24CE E4EA 2001082300073 20010823 00073 WP 2001 8 23 DHL2001804529 1 20010811 A 5751 AILERON DOUG DC8 DC873F 302199F WP RT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 RT OUTBOARD AILERON T/E DENTED STA XRS 727.00-XRS 763.00. REMOVED RT OUTBOARD AILERON T/E DEFORMED STA XRS 727.00-763.0 0. FABRICATED NEW T/E IAW SRM 57-2-1 PAR 16. INSTALLED NEW T/E IAW SRM 51-1-21A, SRM 57-2-1 PAR 16. 2 L 7 4 4F RT 4A25 2001082300076 20010823 00076 WP 2001 8 23 DHL2001804530 1 20010813 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AFT ACCY COMPT INTERCOSTAL FLANGE BROKEN 2 INCHES, STA 1723.000 THRU STA 1746.00, L-23R TO L25R. REMOVED FASTENERS IAW SRM 51-1-21 PG 7 AND SRM 51-3-0 PG 7. FABRICATED REINFORCING ANGLE AND INSTALLED AT INTERCOSTAL FLANGE IAW SRM 53-2-0 2C/2F AND 51-1-21, PG 1, AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001082300077 20010823 00077 WP 2001 8 23 DHL2001804531 1 20010813 A 5751 SKIN DOUG DC8 DC873F 302199F WP AILERON DEFORMED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AILERON T/E SKIN DEFORMED (STA XRS.693-659). REMOVED DEFORMED SKIN PER SRM 51-2-1. FABRICATED FILLER AND DOUBLER PER SR M 53-2-0. INSTALLED FILLER AND DOUBLER PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 2001082300078 20010823 00078 WP 2001 8 23 DHL2001804532 1 20010811 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AFT PAX DOOR HAS 1 INCH CRACK AT AFT UPPER CORNER STA 1660. CUT DAMAGED AREA PER SRM 53-2-0 PG 127-128. FABRICATED FIL LER AND DOUBLER PER SRM 53-2-0 PG 127/128. CLEANED AND TREATED, FABRICATED PARTS PER SRM 51-1-8B. INSTALLED FILLER AND DOUBLER AND TRIPLER PER SRM 53-2-0 PG 127/128. 2 L 7 4 4F RT 4A25 2001082300079 20010823 00079 WP 2001 8 23 DHL2001804533 1 20010814 A 5512 SKIN DOUG DC8 DC873F 302199F WP HORIZ STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 LT HORIZ STABILIZER LOWER SKIN HAS A 1 INCH CRACK AT STA XE 29.812. REMOVED CRACKED SKIN FROM LT HORIZ STAB PER SRM 51- 1-21 PG 1. FABRICATED NEW SKIN INSTALLED NEW SKIN PER SRM 53-2-1 AND 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2001082300085 20010823 00085 SW 2001 8 23 CA010808001 1 20010802 A 6310 TPE33110UA511G ENGINE SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP LEFT MALFUNCTIONED W C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 CA 91 (CAN) DURING TAKE OFF ROLL THE LT ENGINE WOULD NOT REACH REQUIRED TOURQUE, AS THE THROTTLE ADVANCED THE TORQUE BEGAN TO DECREASE, THE TAKEOFF WAS ABORTED. THE LT ENGINE WAS REMOVED FOR TEARDOWN AND INSPECTION. 2 L 7 2 4T 4 T RT A8SW E4WE 2001082300086 20010823 00086 2001 8 23 COMA0160628 4 20010820 A 2200 272007 PCU CNDAIR CL600 CL6002B19 EA WING FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 917CA 16198 7017 FLIGHT #5800. DESTINATION CVG, DURING CRUISE FLIGHT THE AUTO PILOT FAILED @ FL28. EXCESSIVE INPUT FORCE WAS REQUIRED FOR AILERON CONTROL, FLIGHT WAS DIVERTED TO IAD AND LANDED SAFELY.REPLACED THE LEFT INBOARD AILERON POWER CONTROL UNIT. 2 L 7 2 4F RT A21EA 2001082300088 20010823 00088 2001 8 23 RAIA00108022 4 20010805 A 2350 22100203 SWITCH EMB 145 EMB145ER SO COCKPIT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 802HK 7517 145066 5264-PIT-TRANSMIT SWITCH ON FIRST OFFICERS PANEL STUCK. MAINTENANCE INSPECTED AND DEFERRED PER MEL. MAINTENANCE REPLACED TRANSMIT SWITCH ON FIRST OFFICERS PANEL. 2 L 7 2 4F RT T00011AT 2001082300089 20010823 00089 SO 2001 8 23 RAIA00108023 1 20010811 A 2422 PC251123F INVERTER EMB 145 EMB145ER SO ELECTRICS BAY FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 805HK 5322 145096 5258-GSP-115 VOLT AC BUS OFF CAPTION ILLUMINATED DURING TAXI. MAINTENANCE INSPECTED AND DEFERRED PER MEL. MAINTENANCE RE PLACED STATIC INVERTER. 2 L 7 2 4F RT T00011AT 2001082300090 20010823 00090 EA 2001 8 23 COMA0160630 1 20010820 A 2751 855D1009 BPSU CNDAIR CL600 CL6002B19 EA WING FAULTY A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 818CA 17510 7408 FLIGHT #5822. DESTINATION CVG, DURING DESCENT RECEIVED FLAP CAUTION MESSAGE AT 30 DEGREE FLAP POSITON, CREW DECLARED AN EMERGENCY.REPLACED THE LEFT BRAKE AND POSITION SENSING UNIT. 2 L 7 2 4F RT A21EA 2001082300091 20010823 00091 EA 2001 8 23 COMA0160631 1 20010820 A 2751 7455001 HANDLE CNDAIR CL600 CL6002B19 EA COCKPIT FAULTY A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 818CA 354 7408 FLIGHT #5822. DESTINATION CVG, DURING DESCENT RECEIVED FLAP CAUTION MESSAGE AT 30 DEGREE FLAP POSITON, CREW DECLARED AN EMERGENCY AND LANDED SAFELY.REPLACED THE FLAP CONTROL HANDLE ASSEMBLY. 2 L 7 2 4F RT A21EA 2001082300092 20010823 00092 NM 2001 8 23 DL72E011268 1 20010731 A 3350 1000677 SIGN BOEING 727 727247 138408F NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 831WA 21483 L1 EXIT SIGN INOP IN EMERG MODE. REPLACED L1 EMER LIGHT ASSY. 2 L 7 3 4F A3WE 2001082300094 20010823 00094 2001 8 23 COMA0160632 4 20010820 A 3418 3094334 TRIM SWITCH CNDAIR CL600 CL6002B19 EA COCKPIT FAULTY A COMA K NONE J WARNING INDICATION CR CRUISE 1 SO 01 937CA 7044 FLIGHT #5877. DURING CRUISE FLIGHT RECEIVED A STALL FAIL MESSAGE WHILE ABOVE STALL SPEED.REPLACED THE FLIGHT OFFICERS PI TCH TRIM SWITCH. 2 L 7 2 4F RT A21EA 2001082300096 20010823 00096 NM 2001 8 23 DL72E011317 1 20010810 A 3350 1000677 LIGHT BOEING 727 727247 138408F NM AIRSTAIRS INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 282WA 21484 DURING LAYOVER CHECK FOUND EMERGENCY EXIT LIGHT ASSY AT AFT AIRSTAIRS INOP. WOULD NOT ILLUMINATE DURING EMERGENCY LIGHT CHECK, OR WHEN TEST SWITCH MOVED FROM ARM TO ON. REPLACED LIGHT ASSY AND BATTERIES. OPERATIONAL CHECKS NORMAL 2 L 7 3 4F A3WE 2001082300097 20010823 00097 EA 2001 8 23 COMA0160629 1 20010820 A 2751 860D10018ABC FCU CNDAIR CL600 CL6002B19 EA ELECTRICAL BAY FAULTY A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 818CA 5193 7408 FLIGHT #5822. DESTINATION CVG, DURING DESCENT RECEIVED FLAP CAUTION MESSAGE AT 30 DEGREE FLAP POSITION, CREW DELCARED AN EMERGENCY AND LANDED SAFELY.REPLACED THE FLAP ELECTRONIC CONTROL UNIT. 2 L 7 2 4F RT A21EA 2001082300098 20010823 00098 NE 2001 8 23 DL72E011334 2 20010814 A 7230 658385 CONTROL VALVE BOEING 727 727247 138408F NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE FAILED A DALA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 282WA 21484 695851 EXPERIENCED COMPRESSOR STALL ON NR 2 ENGINE AT 20 KTS ON TAKEOFF ROLL. ABORTED TAKE OFF. REPLACED NR 2 PRBC. 2 L 7 3 4F 4 F A3WE E2EA 2001082300099 20010823 00099 NM 2001 8 23 DL72L011283 1 20010803 A 3320 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 505DA 21307 ON LAYOVER FOUND 4CD FASTEN SEAT BELT LIGHT INOP. C/A RELAMPED OPS CKS GOOD 2 L 7 3 4F A3WE 2001082300102 20010823 00102 NM 2001 8 23 DL72L011286 1 20010805 A 3350 MS1557081 LIGHT BOEING 727 727232 1384082 NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 507DA 21309 RIGHT OVERWING EMERGENCY LIGHT BETWEEN EXTERIOR EMERGENCY EXIT DOORS INOP. RELAMPED. CHECKS OKAY 2 L 7 3 4F A3WE 2001082300106 20010823 00106 NM 2001 8 23 DL72L011292 1 20010806 A 3230 1U10851 VALVE BOEING 727 727232 1384082 NM RT MLG WW LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 503DA 21305 SYSTEM A HYDRAULICS FAILURE AFTER GEAR RETRACTION. PRESSURE ZERO, FLUID ZERO. A SYSTEM PUMPS SHUT OFF IAW CHECKLIST APP ROX 5 MIN. FOUND LOCK ASSY VALVE LEAKING IN RT MLG WW. REMOVED AND REPLACE R/H SIDE LOLOCK ASSY VALVE PER M/M JACKED A/C AND CYCLED GEAR. OPS CK OK. 2 L 7 3 4F A3WE 2001082300112 20010823 00112 NE 2001 8 23 DL72S011271 2 20010801 A 7200 JT8D15AHK ENGINE BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 1 MAKING METAL A DALA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 27 521DA 66170 21472 695325 NR 1 ENG OIL FILTER BYPASS LT ILLUM. C/W POM PROCEDURE. LT DID NOT GO OUT. ENG SHUTDOWN. CA REPLACED NR 1 ENG OIL FILTER , LK CK GOOD. FOUND METAL ON MAIN OIL CHIP DET. PERFORMED ENG PENALTY RUN PER M/M. ON RE-INSP OF CHIP DET FOUND METAL AG AIN. REPLACED NR 1 ENG. 2 L 7 3 4F 4 F A3WE E2EA 2001082300113 20010823 00113 NM 2001 8 23 DL72S011291 1 20010806 A 3350 S106 BATTERY BOEING 727 727225A 1384077 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8891Z 21860 EMERGENCY EXIT LIGHT AT BOTTOM OF AFT AIRSTAIRS INOP. REPLACED BATTERIES AND BATTERY HOLDER OPS CKD NML. 2 L 7 3 4F RT A3WE 2001082300114 20010823 00114 NM 2001 8 23 DL72S011293 1 20010723 A 5312 BULKHEAD BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 1/4 INCH CRACK ON 870 BULKHEAD AFT SIDE BELOW APU LOAD CONT BOX. REPAIRED PER SRM 53-10-9. 2 L 7 3 4F A3WE 2001082300115 20010823 00115 NM 2001 8 23 DL72S011294 1 20010723 A 5754 ATTACH ANGLE BOEING 727 727232 1384082 NM L/E SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 NR 7 SLAT COVE SKIN ATTACH ANGLE CRACKED INBD OF INDB UP STOP. REPAIRED PER M/M 57-54-000-8 2 L 7 3 4F A3WE 2001082300116 20010823 00116 NM 2001 8 23 DL72S011298 1 20010804 A 5310 6516350314 BEAM BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 FUSELAGE BULKHEAD AT FS 1183, RBL 8, WL 182 VERTICAL BEAM CRACKED. A 1 INCH TYPICAL CRACK WAS FOUND ON THE RBL 8 VERTICA L BEAM OF THE FS 1183 BULKHEAD EXTENDING FROM THE LOWER END OF THE BEAM AT WL 182. THE CRACK IS TYPICAL OF THOSE DOCUM ENTED PER BAC S/B 727-53-0175. THE CRACK WAS REPAIRED WITH A REPAIR ANGLE PER THE SB AND PER ER/A 381430-14. 2 L 7 3 4F A3WE 2001082300117 20010823 00117 NM 2001 8 23 DL72S011300 1 20010807 A 5310 DOOR FRAME BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 FUSELAGE C1 DOOR OPENING FWD FRAME AT FS 560 CRACKED. INSPECTION OF THE C1 DOOR CUTOUT SURROUND FRAME WEBS PER AD 99-23- 13 REVEALED A TYPICAL CRACK IN THE FWD FRAME WEB BELOW THE LIGHT SWITCH WEB CUTOUT ALONG THE OUTER CHORD ATTACHMENT L OCATIONS. 2 L 7 3 4F A3WE 2001082300118 20010823 00118 NM 2001 8 23 DL72S011307 1 20010809 A 2782 1U1110 ACTUATOR BOEING 727 727232 1384082 NM L/E FLAP LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 516DA 21432 ON FINAL APPROACH PRIOR TO GEAR EXT WITH FLAPS 5 DEG AND HAD INDICATION OF A LOSS OF A SYSTEM HYD. REPLACED A SYSTEM FI LTERS. REPLACED LEADING EDGE FLAP ACTUATOR FOR LEAKING 2 L 7 3 4F A3WE 2001082300119 20010823 00119 NM 2001 8 23 DL72S011333 1 20010814 A 5320 65C13874 BEAM BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 538DA 22076 INSPECTION OF THE VENTRAL STAIRWAY TORQUE BOX STRUCTURE PER BAC S/B 727-53-0129 AND AD 94-07-08 REVEALED TYPICAL CRACKS IN THE RT HORIZONTAL BEAM AT FS 1263 & 1273. THE CRACKED STRUCTURE WAS REMOVED AND REPLACED WITH NEW STRUCTURE PER ER /A 381539-14AD. 2 L 7 3 4F A3WE 2001082300120 20010823 00120 NM 2001 8 23 DL72S011339 1 20010814 A 5311 65175061 FRAME BOEING 727 727232 1384082 NM FUSELAGE WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 538DA 22076 THE INNER CHORD OF THE RH FS 1303 FRAME WAS FOUND WITH A 1INCH AREA OF WEAR ON THE INNER FLANGE JUST ABOVE THE VENTRAL S TAIRWAY TORQUE BOX DUE TO CONTACT WITH A LOOSE HYDRAULIC LINE CLAMP. THE DAMAGED AREA OF FLANGE WAS TRIMMED OUT. THE CHORD WAS REPAIRED PER ER/A 381540-14, REV A. 2 L 7 3 4F A3WE 2001082300121 20010823 00121 NM 2001 8 23 DL733011297 1 20010807 A 3150 655449938 WARNING SYSTEM BOEING 737 737347 1384647 NM E/E BAY MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 307WA 23440 CABIN PRESSURE WARNING SOUNDED IN FLIGHT, WOULD NOT SILENCE. PRESSURE GOOD. REPLACED AURAL WARNING UNIT AND CABIN ALT SW ITCH. 2 L 7 2 4F RT A16WE 2001082300122 20010823 00122 NE 2001 8 23 DL733011306 2 20010808 A 7321 8063201 MEC BOEING 737 737347 1384647 NM GE CFM56 CFM563B1 13802 NE NR 1 ENGINE FAILED A DALA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 311WA 23597 721132 NR 1 ENGINE FAILED TO REACH TAKEOFF ON TAKEOFF ROLL. TAKEOFF ABORTED AT APPROX 65 KTS. REPLACED ENGINE MEC. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082300123 20010823 00123 NM 2001 8 23 DL733011308 1 20010809 A 3350 02019241007 LIGHT BOEING 737 73735B NM CABIN DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 221DL 23970 LAV AFT RT EMERGENCY TRACK LIGHT DAMAGED , LIGHT ASSY REPLACED, CHK OK. 2 L 7 2 4F RT A16WE 2001082300124 20010823 00124 NM 2001 8 23 DL738011312 1 20010810 A 3244 325240210 TIRE BOEING 737 737832 13844CF NM NLG FAILED A DALA O OTHER E VIBRATION/BUFFET TO TAKEOFF 1 SO 27 373DA 29621 NA NOSE GEAR VIBRATION AT APPROX 110 KTS ON T/O ROLL. TOWER REPORTED DEBRIS ON THE RUNWAY AND CONFIRMED THAT WE HAD A NOSE TIRE FAILURE . REPLACED TIRE. 2 L 7 2 4F RT A16WE 2001082300125 20010823 00125 NM 2001 8 23 DL73E011285 1 20010704 A 3350 900835A BATTERY PACK BOEING 737 7372S3 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 369DL 21776 ON INSPECTION FOUND EMERGENCY LIGHTS IN CEILING OF CABIN, ALL POSITIONS INOP. BOTH CABIN OVERWING EMERGENCY LIGHTS INOP ALSO. REPLACED FWD, MID AND AFT LEFT BATTERY PACKS PER MM. CKS NORMAL. 2 L 7 2 4F RT A16WE 2001082300126 20010823 00126 NM 2001 8 23 DL73E011295 1 20010806 A 3350 S106 BATTERY BOEING 737 7372S3 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 367DL 21774 ON INSPECTION FOUND AFT LEFT OVER DOOR EMERGENCY EXIT SIGN INOP. REPLACED BATTERIES PER MM. OPN NORMAL 2 L 7 2 4F RT A16WE 2001082300127 20010823 00127 NM 2001 8 23 DL73E011336 1 20010813 A 3350 900835A BATTERY PACK BOEING 737 7372S3 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 369DL 21776 ON INSPECTION FOUND OVERWING EMERGENCY EXIT LIGHTS INOP IN CABIN. REPLACED MID LEFT BATTERY PACK PER MM. OPN NORMAL. 2 L 7 2 4F RT A16WE 2001082300128 20010823 00128 NM 2001 8 23 ZW0A0107302 1 20010822 A 3350 97F9705 PIN BOEING 767 76733AER 1385230 NM A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 637TW 25403 THE EGRESS LIGHTS WERE INOPERATIVE AT THE NUMBER 3 CABIN DOOR, LH AND RH SIDE. REPAIRED BROKEN CONNECTOR PIN AT THE LH S IDE NUMBER 3 DOOR. CHECK-C 1-27-01 LAX. --CLOSED-- 2 L 7 2 4F RT A1NM 2001082300129 20010823 00129 EA 2001 8 23 COMA0160633 1 20010822 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 986CA 7174 DURING PRE-FLIGHT INSPECTION CREW FOUND THE EMERGENCY FLOOR LIGHTING ON THE RIGHT SIDE OF THE CABIN INOPERATIVE.RE-SECUR ED LOOSE CONNECTOR FOR THE RIGHT SIDE FLOOR EMERGENCY TRACK LIGHTS. 2 L 7 2 4F RT A21EA 2001082300130 20010823 00130 NM 2001 8 23 DL73E011337 1 20010813 A 3350 900542 BATTERY PACK BOEING 737 7372S3 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 369DL 21776 ON INSPECTION FOUND FWD, MID, AND AFT OVERHEAD EMERGENCY EXIT LIGHTS INOP IN CABIN. REPLACED FWD BATTERY PACK, MID RT BA TTERY PACK AND CHARGER ASSY AND AFT BATTERY PACK AND CHARGER ASSY. OPN OF ALL EMERGENCY LIGHTS NOW NORMAL. 2 L 7 2 4F RT A16WE 2001082300131 20010823 00131 2001 8 23 DL73K011284 4 20010804 A 2565 D31354438 SLIDE BOEING 737 737247 138448D NM L1 DOOR OUT OF POSITION A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 376DL 23603 L1 DOOR SLIDE CAME OUT OF CASE. C/A REPLACED SLIDE. 2 L 7 2 4F A16WE 2001082300132 20010823 00132 EA 2001 8 23 COMA0160634 1 20010822 A 2720 NAS620418D BOLT CNDAIR CL600 CL6002B19 EA EMPENNAGE MISLOCATED A COMA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 960CA 12613 7117 FLIGHT #5424. DURING CRUISE FLIGHT DESTINATION YYZ WITH THE AUTOPILOT ENGAGED, RT RUDDER TRIM OF 1.5 UNITS AND LT. DOWN AILERON TRIM OF .5 UNITS HAD TO BE SET TO KEEP STRAIGHT AND LEVEL FLIGHT.UPON INVESTIGATION FOUND THE LOWER MOUNTING BOL T FOR THE #1 YAW DAMPER LINEAR ACTUATOR NOT INSTALLED CORRECTLY, REMOVED AND CORRECTLY-REINSTALLED LOWER MOUNTING BOLT. 2 L 7 2 4F RT A21EA 2001082300133 20010823 00133 NM 2001 8 23 DL73K011290 1 20010806 A 2121 606850 FAN BOEING 737 737232 1384475 NM COCKPIT UNSERVICEABLE A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 311DL 23083 ON LANDING, COCKPIT FILLED WITH SMOKE, TURNED GASPER AND PACKS OFF. AT GATE DETERMINED SMOKE WAS COMING IN WHEN RT PACK WAS TURNED ON. CA FOUND CONTROL CABIN AIR FLOW FAN C/B POPPED. FWD TO MCO AND PLACARD PER MEL 21-00-30A 2 L 7 2 4F RT A16WE 2001082300134 20010823 00134 EA 2001 8 23 COMA0160635 1 20010822 A 2740 601R517063 CONTROL PANEL CNDAIR CL600 CL6002B19 EA COCKPIT FAULTY A COMA K NONE F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 01 929CA 17494 7035 FLIGHT #5322. WHILE PARKED AT THE GATE AT EVV STABILIZER TRIM CHANNEL #2 WOULD NOT ENGAGE.REPLACED STAB/MACH TRIM PANEL ASSEMBLY. 2 L 7 2 4F RT A21EA 2001082300135 20010823 00135 NM 2001 8 23 DL73K011296 1 20010805 A 5330 654577416 SKIN BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 FUSELAGE SKIN WAS FOUND WITH A 1 INCH CRACK AT STRINGER 19L AT FS 767. THE CRACK WAS JUST ABOVE THE WAFFLE DOUBLER AT T HE STRINGER. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL DOUBLER PER THE B737 SRM AND ER/A 381488 -14. 2 L 7 2 4F A16WE 2001082300136 20010823 00136 NM 2001 8 23 DL73K011310 1 20010810 A 5315 6546800508 FLOORBEAM BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 325DL 23097 THE FS 520 FLOORBEAM WAS FOUND CRACKED AT RBL & LBL 24. THE CRACKS ARE TYPICAL S/B 737-53-1120. THE CRACKS WERE STOP DR ILLED AND REPAIRED PER THE S/B. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001082300138 20010823 00138 NM 2001 8 23 DL73K011320 1 20010812 A 5210 HINGE PIN BOEING 737 737247 138448D NM L1 DOOR OUT OF POSITION A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 244WA 23518 PILOT REP - LOUD SQUEAL FROM L1 ENTRY DOOR UPPER HINGE AREA. FOUND UPPER HINGE/SEAL FLOATING BRACKET HINGE PIN OFF . REI NSTALLED PIN AND HINGE. PRESS A/C TO 4.5 DIFF PRESS CKS OK 2 L 7 2 4F A16WE 2001082300139 20010823 00139 NM 2001 8 23 DL73K011340 1 20010814 A 5314 6546877143 KEELBEAM BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 330DL 23102 THE LT STRINGER 18A SHEAR BEAM AT FS 727 WAS FOUND WITH A 1 INCH CRACK EMANATING FROM THE EDGE OF THE WEB. THE CRACK IS TYPICAL OF THOSE SHOWN IN BAC S/B 737-53-1066, HOWEVER THE S/B IS NOT EFFECTIVE FOR THIS AIRCRAFT. THE CRACK WAS STOP D RILLED AND REPAIRED PER ER/A 381542-14, REV A. 2 L 7 2 4F RT A16WE 2001082300140 20010823 00140 2001 8 23 DL757011257 4 20010729 A 3460 4052500962 FMC BOEING 757 757232 1384965 NM E/E BAY FAILED A DALA D RETURN TO BLOCK J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 6701 30187 WHILE LINING UP FOR T/O, MASTER WARNING LIGHTS WENT OFF ALONG WITH FMC DISCREET LIGHT AND F/O FMS CDU BLANKED. SHORTLY A FTERWARDS A BURNING ELEC SMELL WAS IN CABIN AND FLIGHT DECK. A/C RTB AND CONTRACT MTC FOUND RT FMS COMPUTER BURNED UP. M TC REMOVED COMPUTER, ALLOWED TO VENT AND COOL DOWN. RE-INSTALLED COMPUTER AND DISPATCHED WITH RT FMC INOP WITH C/B'S PUL LED 2 L 7 2 4F RT A2NM 2001082300141 20010823 00141 WP 2001 8 23 CALA0100764 1 20010819 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 1117-1174 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND MAIN CABIN CENTER FLOOR PANEL DELAMINATED AT FS 1117-1174. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 532 0-01265. 2 L 7 2 4F A6WE 2001082300142 20010823 00142 WP 2001 8 23 CALA0100767 1 20010822 A 3233 59370365501 CYLINDER DOUG DC9 DC981 3022081 WP R/H MLG INOPERATIVE A CALA A D UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 09 14880 32804 48044 THE R/H MLG WOULD NOT RETRACT AND THE GEAR DOOR AMBER LIGHT REMAINED ILLUMINATED.AFTER TAKEOFF FROM EWR. THE LEFT MAIN A ND NOSE GEAR WERE SLOW TO RETRACT AND THE R/H MAIN REMAINED DOWN DURING GEAR RECYCLING. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE R/H MLG ACTUATOR CYLINDER AND RESTRICTOR PER MM 32-32-02. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A6WE 2001082300143 20010823 00143 WP 2001 8 23 CALA0100768 1 20010823 A 5320 CHANNEL DOUG DC9 DC982 3022082 WP NWW CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND AFT NOSE WHEEL WELL AFT DOOR CHANNEL AT L/H O/B SIDE. THE CHANNEL WAS REMOVED AND REMOVED IAW SRM 51-30 -02. 2 L 7 2 4F A6WE 2001082300144 20010823 00144 WP 2001 8 23 CALA0100769 1 20010823 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 673-763 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND CABIN L/H FLOOR PANEL DELAMINATED AROUND INSERT HOLES AT FS 673-763. A NEW FLOOR PANEL WAS INSTALLED IA W ECRA 5320-01265. 2 L 7 2 4F A6WE 2001082300145 20010823 00145 WP 2001 8 23 CALA0100770 1 20010823 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 150-160 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND COCKPIT FLOOR PANEL DELAMINATED AT FS 150-160, LBL 8-12. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320- 01265. 2 L 7 2 4F A6WE 2001082300146 20010823 00146 WP 2001 8 23 CALA0100771 1 20010823 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 1079-1250 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND CENTER CABIN FLOOR PANELS AT FS 1117-1174 AND FS 1174-1250 DELAMINATED. LEFT HAND CABIN FLOOR PANELS WE RE FOUND DELAMINATED AT FS 1079-1155 AND FS 1155-1250. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001082300147 20010823 00147 WP 2001 8 23 CALA0100772 1 20010823 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 826-886 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND CABIN CENTER FLOOR PANEL DELAMINATED AT FS 826-886. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265 . 2 L 7 2 4F A6WE 2001082300148 20010823 00148 WP 2001 8 23 CALA0100774 1 20010823 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FWD ENTRY DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND CABIN FORWARD ENTRY FLOOR PANEL C & J DELAMINATED. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001082300149 20010823 00149 WP 2001 8 23 CALA0100775 1 20010823 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 1250-1347 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND CABIN CENTER FLOOR PANELS DELAMINATED AT FS 1250-1309 AND FS 1309-1347. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001082300150 20010823 00150 WP 2001 8 23 CALA0100776 1 20010823 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 120-160 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND COCKPIT CENTER FLOOR PANEL DELAMINATED AT FS 120-160. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-012 65. 2 L 7 2 4F A6WE 2001082300151 20010823 00151 WP 2001 8 23 CALA0100777 1 20010823 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 254-313 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND CABIN CENTER FLOOR PANEL DELAMINATED AT FS 254-313. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265 . 2 L 7 2 4F A6WE 2001082300152 20010823 00152 WP 2001 8 23 CALA0100778 1 20010823 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 1250-1309 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND CABIN L/H FLOOR PANEL DELAMINATED AT FS 1250-1309. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001082300153 20010823 00153 NE 2001 8 23 DL757011258 2 20010729 A 7200 PW2037RTC ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 MALFUNCTIONED A DALA E ENGINE SHUTDOWN O OTHER AP APPROACH 1 SO 27 665DN 46106 25013 716359 NR 1 ENGINE HAD A AUDIBLE SURGE WHILE ON APPROACH TO STT. THE ENGINE WAS SHUTDOWN BY THE CREW. CONTRACT MTC FOUND METAL GRIT IN THE TAILPIPE 2 L 7 2 4F 4 F RT A2NM E17NE 2001082300154 20010823 00154 NM 2001 8 23 DL757011259 1 20010729 A 3411 PITOT LINE BOEING 757 757232 1384965 NM COCKPIT OBSTRUCTED A DALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 27 615DL 22822 ON TAKEOFF ROLL F/O AIRSPEED LAGGED CAPTS AIRSPEED BY 30KTS. FOUND F/O PITOT TUBE OBSTRUCTED. CLEARED OBSTRUCTION AND B LEW PITOT LINE CLEAR FROM ADC. LEAK CKS GOOD PER FIM. 2 L 7 2 4F RT A2NM 2001082300155 20010823 00155 NM 2001 8 23 DL757011260 1 20010729 A 3040 141T480149 TERMINAL BOEING 757 757232 1384965 NM COCKPIT BURNED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 681DA 26957 A/C DIVERTED TO DEN WITH SMOKE IN COCKPIT. FOUND TERMINAL ON LEFT NR 1 WINDOW FOR WINDOW HEAT BURNT WHERE TERMINAL BLOCK IS BONDED TO WINDOW SURFACE AT LOWER LEFT CORNER OF WINDOW. 2 L 7 2 4F RT A2NM 2001082300156 20010823 00156 NM 2001 8 23 DL757011261 1 20010729 A 3350 0L3071BPEGPL LIGHT BOEING 757 757232 1384965 NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 643DL 23997 ON LAYOVER CK FOUND LT WING EXTERIOR EMER LIGHT INOP. RELAMPED SAME AND CKS GOOD. 2 L 7 2 4F RT A2NM 2001082300157 20010823 00157 NE 2001 8 23 DL757011311 2 20010810 A 7261 FILTER BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE DIRTY A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 654DL 49213 24394 716307 RT OIL FILTER LIGHT ILLUM AT FL350 CRUISE THROTTLE REDUCED TO IDLE LIGHT REMAINED ILLUM ENG WAS SHUTDOWN ON DESCENT TO D FW. C/A REPLACED OIL FILTER. 2 L 7 2 4F 4 F RT A2NM E17NE 2001082300158 20010823 00158 NE 2001 8 23 DL757011314 2 20010810 A 7200 PW2037RTC ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 MALFUNCTIONED A DALA A UNSCHED LANDING J Y WARNING INDICATION ENGINE STOPPAGE CL CLIMB 1 SO 27 617DL 41974 22907 716481 RT ENG SEC CONTROL STATUS MSG THEN AFTER LEVEL OFF RT ENG STATOR CAUTION MSG, ENG SHUTDOWN. C/A REPLACED ENGINE, FCU, &E EC PER MM,PERFORMED TEST 7 14 AND 15 FROM PFHB. OPS CHKD AND LEAK CHKD OK 2 L 7 2 4F 4 F RT A2NM E17NE 2001082300159 20010823 00159 NM 2001 8 23 DL757011329 1 20010813 A 3350 20131A BATTERY PACK BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 606DL 22813 ALL FIRST CLASS EMERGENCY TRACK LIGHTING INOP. REPLACED F/C BATTERY PACK. CKS GOOD. 2 L 7 2 4F RT A2NM 2001082300160 20010823 00160 NM 2001 8 23 DL757011330 1 20010813 A 3350 BPS73 POWER SUPPLY BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 606DL 22813 RT OVERWING LIGHT EMER EXIT SIGN INOP. REPLACED PWR SUPPLY AND BATT PACK. 2 L 7 2 4F RT A2NM 2001082300161 20010823 00161 NM 2001 8 23 DL757011331 1 20010814 A 2560 BATTERY BOEING 757 757232 1384965 NM FLASHLIGHT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 663DN 24992 FOUND FWD FLIGHT ATTENDANT INBD EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY AND STRAP OPS CK OK 2 L 7 2 4F RT A2NM 2001082300162 20010823 00162 NE 2001 8 23 DL764011244 2 20010727 A 7200 CF680C2B8F ENGINE BOEING 767 767432ER NM GE CF6 CF680C2B7 NE NR 2 FAILED A DALA C ABORTED TAKEOFF A P FLAME/FIRE NO WARNING INDICATION TO TAKEOFF 1 SO 27 835MH 2244 29708 706206 WHILE CREW WAS TAKING THE RUNWAY IN FLL AND THE POWER WAS ADVANCED THEY OBSERVED 3 EXTREMELY LOUD BANGS WITH NO SUPPOR TING ABNORMAL ENGINE INDICATIONS. WHEN THE POWER WAS REDUCED THEY WERE ADVISED BY ANOTHER CARRIER THAT FLAMES AND DEBRI S WERE SEEN EXITING THE RIGHT ENGINE. UPON RETURNING TO THE GATE FLLML INSPECTED THE INLET AND TAIL PIPE AREA AND FOUND METAL SPATTER AND DEBRIS IN THE TAILPIPE SETTING UP ENGINE CHANGE. 2 L 7 2 4F 4 F RT A1NM E13NE 2001082300163 20010823 00163 NM 2001 8 23 DL764011270 1 20010725 A 2751 FLAP BOEING 767 767432ER NM WINGS MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 835MH 29708 ON CLIMBOUT HAD FLAP T/E DISAGREE. ADVISED TO RETURN. MTC RELEASED PER FIM PROCEDURE 27-51-00 WITH FSEU FAULT MESSAGE 27-51104. 2 L 7 2 4F RT A1NM 2001082300164 20010823 00164 NM 2001 8 23 DL767011305 1 20010807 A 5311 148T27405004 FRAME BOEING 767 767232 1385132 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 103DA 22215 INSPECTION OF THE FS 1809.5 OUTER CHORDS PER AD 2001-09-13 AND BAC S/B 767-53-0078 REVEALED CRACKS EMANATING FROM TWO FASTENER HOLES IN THE RT FWD CHORD AND ONE HOLE IN THE RT AFT CHORD. THE AFT CHORD WAS COMPLETELY REPLACED AND THE UPPE R SECTION OF THE FWD CHORD WAS REMOVED AND A NEW SECTION SPLICE IN PER THE S/B INSTRUCTIONS. THE REPAIRS WERE DOCUMENTE D PER ER/A 381425-14AD. 2 L 7 2 4F RT A1NM 2001082300165 20010823 00165 NM 2001 8 23 DL767011324 1 20010810 A 5412 311T12313 BULKHEAD BOEING 767 767232 1385132 NM NR 1 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 108DL 22220 DURING ACCOMPLISHMENT OF PYLON SIP MODIFICATION,CRACK INDICATIONS WERE FOUND IN THE MID STRUT BULKHEAD IN AREA COMMON TO THE UPPER SPAR FITTING. 2 L 7 2 4F RT A1NM 2001082300166 20010823 00166 NM 2001 8 23 DL767011325 1 20010810 A 5312 148T3110 BULKHEAD BOEING 767 767232 1385132 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 108DL 22220 CRACKS FOUND IN THE STA 1809 BULKHEAD AREA, COMMON TO THE SKIN AND THE FWD OUTER CHORD, LT SIDE OF AIRCRAFT. 2 L 7 2 4F RT A1NM 2001082300167 20010823 00167 NM 2001 8 23 DL767011326 1 20010810 A 5320 148T25122 FITTING BOEING 767 767232 1385132 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 108DL 22220 CRACK INDICATIONS FOUND IN THE STA 1809 BULKHEAD COMMON TO THE SPLICE FITTING, FWD OUTER CHORD AND LONGERON FITTING. 2 L 7 2 4F RT A1NM 2001082300168 20010823 00168 NM 2001 8 23 DL767011335 1 20010814 A 2121 6066223 FAN BOEING 767 767232 1385132 NM MANIFOLD BAY DEFECTIVE A DALA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 SO 27 106DA 22218 DURING APPROACH SMOKE PRESENT IN COCKPIT. SHORTLY AFTER THE LEFT RECIRC FAN EICAS MSG APPEARED. TURNED LEFT RECIRC FAN O FF. SMOKE DID DISSIPATE AFTER LDG. CONTRACT MTC FOUND THE LEFT RECIRC FAN C/B IN, BUT POPPED WHEN BARELY TOUCHED. ALSO C /B WAS VERY HOT TO THE TOUCH. REPLACED RECIRC FAN 2 L 7 2 4F RT A1NM 2001082300169 20010823 00169 NM 2001 8 23 DL76G011246 1 20010727 A 5512 182T32001 SKIN BOEING 767 7673P6 1385105 NM HORIZ STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 154DL 25241 CORROSION FOUND ON THE UPPER SURFACE SKIN OF THE LT HORIZONTAL STABILIZER. DAMAGE LOCATED OVER STRINGER 3 BETWEEN RIBS 2 AND 3 APPROXIMATELY AT RT STA 2.5. 2 L 7 2 4F RT A1NM 2001082300170 20010823 00170 NM 2001 8 23 DL76G011262 1 20010730 A 2530 ODOR BOEING 767 767332 1382001 NM GALLEY DETECTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 1604R 30180 ATB FOR ELECTRICAL SMELL IN AFT GALLEY...CREW TURNED OFF OVENS AND RECIRC FANS AND UTILITY BUSSES AND SMELL DISSIPAT ED. MAD MTC INVESTIGATING. 2 L 7 2 4F RT A1NM 2001082300171 20010823 00171 NM 2001 8 23 DL76G011267 1 20010728 A 2910 272T1200176 HYDRAULIC LINE BOEING 767 767332 1382001 NM HYDRAULIC SYS FAILED A DALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 1612T 783 30575 NR 7 SPOILER CONTROL ACTUATOR PRESSURE LINE AT ACTUATOR PULLED OUT OF B-NUT BREAKING LINE AND CAUSING COMPLETE LOSS OF R IGHT HYDRAULIC SYSTEM FLUID. REPLACED LINE. 2 L 7 2 4F RT A1NM 2001082300172 20010823 00172 NM 2001 8 23 DL76G011318 1 20010811 A 5610 WINDOW BOEING 767 767332 1382001 NM COCKPIT CRACKED A DALA K NONE O OTHER LD LANDING 1 SO 27 1607B 30388 F/O RT WINDOW CRACKED ON LANDING. REPLACED SAME. 2 L 7 2 4F RT A1NM 2001082300173 20010823 00173 NM 2001 8 23 DL76G011327 1 20010809 A 5410 FITTING BOEING 767 7673P6 1385105 NM NR 1 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 156DL 25354 THE INBOARD FITTING ON THE NR 1 PYLON WAS FOUND WITH CRACKS IN THE TYPICAL LOCATION AS SHOWN IN S/B 767-54-0081. 2 L 7 2 4F RT A1NM 2001082300174 20010823 00174 NM 2001 8 23 DL76K011266 1 20010730 A 3240 161T113617 ROD BOEING 767 767332 1382001 NM NR 8 BRAKE BROKEN A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 176DZ 29697 LANDING GEAR DISAGREE WITH GEAR DOOR ADVISORY WHEN GEAR HANDLE PLACED UP AFTER T/O. NR 8 BRAKE ANTI-ROTATION ROD BROKE. REPLACED BRAKE AND LINE. 2 L 7 2 4F RT A1NM 2001082300175 20010823 00175 NM 2001 8 23 DL76L011243 1 20010726 A 2913 PUMP BOEING 767 767332 1382001 NM HYDRAULIC SYS LEAKING A DALA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 178DN 25143 4 HOURS INTO FLIGHT, CTR HYD "RSVR" LIGHT AND "CTR HYD QTY" EICAS MESSAGE CAME ON. CTR HYD QUANTITY INDICATED 0.47RF. SWITCHED OFF ELEC PUMPS AND QTY CONTINUED TO DECREASE. SWITCHED ELEC PUMPS BACK ON AND ADP OFF AND QUANTITY CONTINUED TO DECREASE. SWITCHED ALL PUMPS OFF AND QTY LOSS STOPPED. CA FOUND LEAK ON ADP PRESSURE & CASE DRAIN FILTER MODULE. REPLA CED PACKINGS AND LEAK CHECK THEN OK. 2 L 7 2 4F RT A1NM 2001082300176 20010823 00176 NE 2001 8 23 DL76L011289 2 20010805 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 LEAKING A DALA O OTHER B K SMOKE/FUMES/ODORS/SPARKS FLUID LOSS TO TAKEOFF 1 SO 27 183DN 40958 724158 27110 724158 ON T/O FROM BRU REPORTED SMOKE IN CABIN.CLEARED AFTER 15 MINUTES OF FLT.ATL MTC FOUND OIL LEAKING FROM SPINNER. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 2001082300177 20010823 00177 2001 8 23 DL76L011315 4 20010811 A 3460 222700059B DAU BOEING 767 767332 1382001 NM E/E BAY FAILED A DALA H DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 27 196DN 28453 STATUS MSG IN-FLT, FLT DATA ACQ. PULLED C/B J7 AND J8. ELEC SMELL JUST PRIOR TO MESSAGE. REPLACED DFDAU AND FLT DATA REC PER MM. OPS NORMAL. MTC REPORTED DFDAU HAD STRONG ELEC SMELL. 2 L 7 2 4F RT A1NM 2001082300178 20010823 00178 NM 2001 8 23 DL76P011251 1 20010727 A 7930 1A6473 CHIP DETECTOR BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 144DA 27584 727678 THE MAIN ENGINE CHIP DETECTOR BOSS SLOTS (3 EA) HAD BEGUN TO FAIL (CRACK) AT THE WEAKEST AREA OF THE BOSS. REPLACED THE BOSS AND DETECTOR 2 L 7 2 4F 4 F RT A1NM E24NE 2001082300179 20010823 00179 NM 2001 8 23 DL76S011253 1 20010728 A 3350 1317 LIGHT BOEING 767 767332 1382001 NM AFT DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 133DN 24982 LT AFT DOOR EXT EMERGENCY LIGHT INOP RELAMPED. CKS OK. 2 L 7 2 4F RT A1NM 2001082400002 20010824 00002 NM 2001 8 24 SWAA012279 1 20010815 A 3350 D71702001 BATTERY BOEING 737 7377H4 NM CABIN WEAK A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 794SW 30605 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR & AFT CENTER AISLE EMERGENCYEXIT LIGHTS DIM. R&R BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2001082400003 20010824 00003 NM 2001 8 24 SWAA012280 1 20010815 A 3350 65C34691 LENS BOEING 737 7373Y0 1384671 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 682SW 23496 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING AT ROW 9 DEF. INS TALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2001082400004 20010824 00004 NM 2001 8 24 SWAA012283 1 20010814 A 2731 65C2638 TAB BOEING 737 7373A4 1384585 NM ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED C4 CHECK, FOUND PLAY AT RH ELEVATOR TAB ATTACH ASSY. R&R ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2001082400005 20010824 00005 NM 2001 8 24 SWAA012284 1 20010815 A 2731 BACB28AK04 BUSHING BOEING 737 7377H4 NM ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 731SA 27863 DURING SCHEDULED A1 CHECK, LH ELEVATOR TAB FAILED FREE PLAY CHECK. R&R ELEVATOR TAB BUSHING P ER MM. 2 L 7 2 4F RT A16WE 2001082400006 20010824 00006 NM 2001 8 24 SWAA012285 1 20010812 A 5310 BAL1517 ANGLE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 519SW 25318 DURING SCHEDULED D CHECK AT DALFORT, FOUND 'Z' FRAME ANGLES CRACKED AT STR 8L, BS 400, BS 787 & BS 907. REPAIRED ANGLES PER SRM. 2 L 7 2 4F RT A16WE 2001082400007 20010824 00007 NM 2001 8 24 SWAA012286 1 20010814 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 1 1/2 LONG AT BS 847, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001082400008 20010824 00008 NM 2001 8 24 SWAA012287 1 20010814 A 5310 6546568 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED 1/2D CHECK, FOUND FWD BULKHEAD WEB CRACKED AT BS 1016, STR 2R. REPAIRED WE B PER SRM. 2 L 7 2 4F RT A16WE 2001082400009 20010824 00009 NM 2001 8 24 SWAA012288 1 20010814 A 5310 6516300 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 357SW 26594 DURING SCHEDULED SPECIAL VISIT, FOUND WEB CRACKED .125 LONG ST BS 178, LBL 90 & WL 234. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001082400010 20010824 00010 NM 2001 8 24 SWAA012290 1 20010812 A 5310 B6516300 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 397SW 27691 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, LWR RH ANTENNA MOUNT. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001082400011 20010824 00011 NM 2001 8 24 SWAA012291 1 20010813 A 2731 183A8100 TAB BOEING 737 7377H4 NM ELEVATOR DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 755SA 27871 DURING SCHEDULED A2 CHECK, FOUND LH ELEVATOR TAB DELAMINATED AT STA 74-94, TRAILING EDGE UPPER SKIN. REPAIRED TAB PER SWA RA. 2 L 7 2 4F RT A16WE 2001082400012 20010824 00012 NM 2001 8 24 SWAA012312 1 20010818 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED 1/4D CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LOOSE AT ROW 14 ABC. SECURED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001082400013 20010824 00013 NM 2001 8 24 SWAA012314 1 20010816 A 5310 6962014 STIFFENER BOEING 737 7373H4 1384600 NM MLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL STIFFENER CRACKED AT MLG W/W, BS 663 & LBL 6.15. REPAIRED STIFFENER PER SWA RA. 2 L 7 2 4F RT A16WE 2001082400014 20010824 00014 NM 2001 8 24 SWAA012315 1 20010818 A 5315 6546804 BEAM BOEING 737 7373H4 1384600 NM CABIN FLOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED 1/2D CHECK, FOUND FLOOR BEAM CRACKED AT BS 947, LBL 56. REPAIRED FLOOR BE AM PER SRM. 2 L 7 2 4F RT A16WE 2001082400015 20010824 00015 NM 2001 8 24 SWAA012316 1 20010816 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED BC3 CHECK, FOUND FUSELAGE SKIN CRACKED 3.750 INCHES LONG AT BS 935, STR 26R REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001082400016 20010824 00016 NM 2001 8 24 SWAA012317 1 20010809 A 5754 65C26686 SLAT BOEING 737 7375H4 138449D NM LH WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 520SW 25319 DURING SCHEDULED D CHECK, FOUND # 2 L/E SLAT DELAMINATED AT T/E WEDGE OTBD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2001082400017 20010824 00017 NM 2001 8 24 SWAA012318 1 20010811 A 5313 65C27314 CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 520SW 25319 DURING SCHEDULED D CHECK, FOUND STR CLIP CRACKED AT BS 277, STR 10R. R&R STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001082400018 20010824 00018 NM 2001 8 24 SWAA012319 1 20010818 A 2731 BACB28AK04 BUSHING BOEING 737 7377H4 NM RH ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 782SA 29808 DURING SCHEDULED SERVICE CHECK, FOUND RH ELEVATOR TAB # 2 HINGE BUSHING WORN. R&R HINGE BUSHING PER MM. 2 L 7 2 4F RT A16WE 2001082400019 20010824 00019 NM 2001 8 24 SWAA012322 1 20010813 A 5710 6567172 BEAM BOEING 737 7375H4 138449D NM RH WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 520SW 25319 DURING SCHEDULED D CHECK, FOUND RH MLG STABILIZER BEAM CORRODED AT AFT INBD SIDE. R&R STAB BEAM PER MM. 2 L 7 2 4F RT A16WE 2001082400020 20010824 00020 NM 2001 8 24 SWAA012323 1 20010817 A 5315 6546804 BEAM BOEING 737 7373H4 1384600 NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED 1/2D CHECK, FOUND FLOOR BEAMS CORRODED AT BS 727E & BS 772, LBL 12. REPAIR ED FLOOR BEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2001082400021 20010824 00021 NM 2001 8 24 SWAA012324 1 20010816 A 5310 6517583 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED 1/4D CHECK, FOUND ( 2 EA ) WEB CRACKS AT BS 178, LBL 5.1, WL 201 & WL 199. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001082400022 20010824 00022 NM 2001 8 24 SWAA012325 1 20010816 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED BC3 CHECK, FOUND ( 3 EA ) FUSELAGE SKIN CRACKS AT STR 4R, BS 410, BS 520 & BS 482. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001082400023 20010824 00023 NM 2001 8 24 SWAA012326 1 20010817 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED BC3 CHECK, FOUND FUSELAGE SKIN CRACKED 3 INCHES LONG AT BS 747, STR 10R. REPAI RED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001082400024 20010824 00024 NM 2001 8 24 SWAA012327 1 20010809 A 5710 6567172 FITTING BOEING 737 7375H4 138449D NM LH WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 520SW 25319 DURING SCHEDULED D CHECK, FOUND LH MLG SUPPORT BEAM AFT HANGER FITTING CORRODED. R&R FITTING PER MM. 2 L 7 2 4F RT A16WE 2001082400025 20010824 00025 NM 2001 8 24 SWAA012328 1 20010812 A 5310 6546529 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 520SW 25319 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT FWD CARGO DOOR LOWER CUT OUT AT BS 452, RBL 41. R&R FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2001082400026 20010824 00026 NM 2001 8 24 SWAA012329 1 20010813 A 5710 6545321 SPAR BOEING 737 7375H4 138449D NM LH WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 520SW 25319 DURING SCHEDULED D CHECK, FOUND LH REAR SPAR UPPER CHORD CRACKED AT WBL 157. R&R REAR SPAR UPPER CHORD SECTION PER BFG ER . 2 L 7 2 4F RT A16WE 2001082400027 20010824 00027 NM 2001 8 24 SWAA012334 1 20010819 A 3350 01792 COVER BOEING 737 7375H4 138449D NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 504SW 24181 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVERS CRACKED AT FWD CABIN. R&R EEPLS COVERS PER MM. 2 L 7 2 4F RT A16WE 2001082400028 20010824 00028 NM 2001 8 24 SWAA012337 1 20010819 A 3350 101074 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY EXIT LIGHT COVER LOOSE ABOVE ROW 18 ABC. R&R LIG HT COVER PER MM. 2 L 7 2 4F RT A16WE 2001082400029 20010824 00029 NM 2001 8 24 SWAA012339 1 20010815 A 5310 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 519SW 25318 DURING SCHEDULED D CHECK AT DALFORT, FOUND STR CRACKED AT BS 907, STR 4R. REPAIRED STR PER SRM. 2 L 7 2 4F RT A16WE 2001082400030 20010824 00030 NM 2001 8 24 SWAA012340 1 20010812 A 5310 6546529 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 519SW 25318 DURING SCHEDULED D CHECK AT DALFORT, FOUND FUSELAGE FRAME CRACKED ( 2 EA ) AT BS 420, BETWEEN STR 15R & STR 17R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001082400031 20010824 00031 NM 2001 8 24 SWAA012341 1 20010820 A 5520 65C26384 TAB BOEING 737 7373H4 1384600 NM LH ELEVATOR DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 373SW 26581 DURING SCHEDULED SERVICE CHECK, FOUND LH ELEVATOR TAB DELAMINATED AT T/E. R&R ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2001082400032 20010824 00032 NM 2001 8 24 SWAA012342 1 20010819 A 2731 BACB28AK04 BUSHING BOEING 737 7377H4 NM RH ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 724SW 27856 DURING SCHEDULED SERVICE CHECK, RH ELEVATOR TAB FAILED FREE PLAY CHECK. R&R BUSHINGS AT HIN GES # 2, # 3 & # 4 PER MM. 2 L 7 2 4F RT A16WE 2001082400033 20010824 00033 NM 2001 8 24 SWAA012343 1 20010812 A 5310 6546569 TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 519SW 25318 DURING SCHEDULED D CHECK AT DALFORT, FOUND SHEAR TIE CRACKED AT BS 967, STR 7L. REPAIR ED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2001082400034 20010824 00034 NM 2001 8 24 SWAA012344 1 20010815 A 5310 65C27314 CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 520SW 25319 DURING SCHEDULED D CHECK, FOUND STR CLIP CRACKED AT BS 482, STR 19L. R&R CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001082400035 20010824 00035 NM 2001 8 24 SWAA012345 1 20010815 A 5313 6551698 SPLICE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 519SW 25318 DURING SCHEDULED D CHECK AT DALFORT, FOUND STR SPLICE CRACKED AT BS 907, STR 4L. R& R STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2001082400036 20010824 00036 NM 2001 8 24 SWAA012346 1 20010820 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED 1/2D CHECK, FOUND FWD CARGO DOOR CUTOUT FRAME CRACKED AT BS 492, STR 23R. REPAIRED FRAME PER SWA T1-653-044. 2 L 7 2 4F RT A16WE 2001082400037 20010824 00037 NM 2001 8 24 SWAA012347 1 20010818 A 5310 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED 1/4D CHECK, FOUND ( 2 EA ) VERTICAL WEBS CRACKED AT BS 180, RBL 17.1, WL 227 AND BS 184, RBL 17.1, WL 232. R&R VERTICAL WEBS PER SRM. 2 L 7 2 4F RT A16WE 2001082400038 20010824 00038 NM 2001 8 24 SWAA012350 1 20010817 A 3510 6546835 MASK BOEING 737 7373H4 1384600 NM COCKPIT LOOSE A SWAA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SW 07 379SW 26586 ( AIR TURNBACK )……………………..LEAK IN CREW OXYGEN SYSTEM. FOUND O'RING LOOSE IN CAPT O2 MASK ASSY, REPOSITIONED O'RING PER MM 2 L 7 2 4F RT A16WE 2001082400039 20010824 00039 NM 2001 8 24 SWAA012352 1 20010821 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER MISSING AT AFT CABIN. INSTALLED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2001082400040 20010824 00040 NM 2001 8 24 SWAA012353 1 20010821 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER & END CAP MISSING AT ROW # 1. INSTALLED COVER & END CAP PER MM. 2 L 7 2 4F RT A16WE 2001082400041 20010824 00041 NM 2001 8 24 SWAA012357 1 20010821 A 5310 141A880 POST BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED 1/4D CHECK, FOUND CAPTAINS WINDOW POST CRACKED .2 INCHES LONG AT UPPER INBD CORNER. REPAIRED POST PER SRM. 2 L 7 2 4F RT A16WE 2001082400042 20010824 00042 NM 2001 8 24 SWAA012358 1 20010806 A 5310 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 520SW 25319 DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 277, STR 10R. REPAIRED STR PER SRM. 2 L 7 2 4F RT A16WE 2001082400043 20010824 00043 NM 2001 8 24 SWAA012359 1 20010819 A 5310 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEBS CRACKED ( 2 EA ) AT BS 178, WL 232, RBL 17.1 & LBL 17.1. R&R WEBS PER SRM. 2 L 7 2 4F RT A16WE 2001082400044 20010824 00044 NM 2001 8 24 SWAA012360 1 20010820 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED ( 3 EA ) AT BS 500C, STR 15L, BS 520, STR 8R, BS 787, STR 20R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001082400045 20010824 00045 NM 2001 8 24 SWAA012361 1 20010821 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED ( 2 EA ) BOTH 3 INCHES LONG AT BS 500 & BS 500B, STR 10R. REPAIRED SKIN PER SWA RA. 2 L 7 2 4F RT A16WE 2001082400046 20010824 00046 NM 2001 8 24 SWAA012362 1 20010821 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19R. REPAIRED SKIN PER SR M. 2 L 7 2 4F RT A16WE 2001082400047 20010824 00047 NM 2001 8 24 SWAA012363 1 20010817 A 5310 65C27314 CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED D CHECK, FOUND STR CLIPS CRACKED ( 7 EA ) AT BS 727A, STR'S 7R & 7L, BS 727B, STR'S 7R, 7L, 6R, 6L, BS 887, STR 4L. R&R STR CLIPS PER SRM. 2 L 7 2 4F A16WE 2001082400048 20010824 00048 NM 2001 8 24 SWAA012365 1 20010815 A 5310 6546525 ANGLE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 519SW 25318 DURING SCHEDULED D CHECK AT DALFORT, FOUND MAIN FRAME 'Z' ANGLE CRACKED AT BS 380, STR 8R. REPAIRED ' Z' ANGLE PER SRM. 2 L 7 2 4F RT A16WE 2001082400049 20010824 00049 NM 2001 8 24 SWAA012367 1 20010821 A 5754 6573714 SLAT BOEING 737 7373H4 1384600 NM LH WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED 1/2D CHECK, FOUND # 1 L/E SLAT CRACKED AT MID AUX TRACK CUTOUT. R&R SLAT PER MM. 2 L 7 2 4F RT A16WE 2001082400050 20010824 00050 NM 2001 8 24 SWAA012368 1 20010821 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 314SW 23336 DURING SCHEDULED C1 CHECK, FOUND OVERHEAD BULLNOSE EMERGENCY LIGHT LENS LOOSE AT ROW 22 ABC. S ECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001082400051 20010824 00051 NM 2001 8 24 SWAA012369 1 20010821 A 5310 6516300 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178 UPPER CORNER. R&R W EB PER SWA ACO. 2 L 7 2 4F RT A16WE 2001082400052 20010824 00052 NM 2001 8 24 SWAA012370 1 20010821 A 5310 6516300 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED ( 2 EA ) 1 INCH LONG, AT BS 178, WL 188, BLO. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001082400053 20010824 00053 NM 2001 8 24 SWAA012371 1 20010821 A 5754 6573714 SLAT BOEING 737 7373H4 1384600 NM LH WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED C1 CHECK, FOUND # 1L/E SLAT CRACKED APPROX 1/2 INCH AT 2ND AUX TRACK CUTOUT. REPAIR ED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2001082400055 20010824 00055 NM 2001 8 24 0103026615 1 20010819 A 3350 6042225 POWER SUPPLY BOEING 747 747251B 1384892 NM ZONE D A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 615US 20360 DURING LINE CHECK, EMERGENCY ESCAPE PATH LIGHTING EXTINGUISHED AFTER ONLY 70 SECONDS OF TEST PERIOD. REPLACED POWER S UPPLIES M419 AND M422. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F A20WE 2001082400057 20010824 00057 NM 2001 8 24 0103036311 1 20010819 A 3350 6042225 POWER SUPPLY BOEING 747 747451 1384940 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 671US 26477 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE IN 'E' ZONE RIGHT SIDE. REPLACED POWER SUPPLY. OPE RATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001082400058 20010824 00058 NM 2001 8 24 0103046634 1 20010820 A 3350 6042225 POWER SUPPLY BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 634US 22234 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE IN 'E' ZONE AND OUTSIDE FUSELAGE MOUNTED EMERGENCY L IGHT INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHT POWER SUPPLY, BATTERY PACK, AND OUTSIDE LAMP. OPERATIONAL CHEC K NORMAL. 2 L 7 4 4F RT A20WE 2001082400083 20010824 00083 WP 2001 8 24 CALA0100779 1 20010823 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 945-1003 TORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND CABIN CENTER FLOOR PANEL TORN BY INSERT HOLE AT FS 945-1003. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5 320-01265. 2 L 7 2 4F A6WE 2001082400084 20010824 00084 WP 2001 8 24 CALA0100781 1 20010823 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 927-1003 PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND CABIN L/H FLOOR PANEL PUNCTURED AT FS 927-1003. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001082400085 20010824 00085 WP 2001 8 24 CALA0100782 1 20010823 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 693-765 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND CABIN R/H FLOOR PANEL DELAMINATED AT FS 693-765. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001082400086 20010824 00086 WP 2001 8 24 CALA0100783 1 20010823 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 1003-1079 PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND CABIN L/H AND R/H FLOOR PANELS PUNCTURED AT FS 1003-1079. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320 -01265. 2 L 7 2 4F A6WE 2001082400087 20010824 00087 NM 2001 8 24 CALA0100784 1 20010824 A 5313 STRINGER BOEING 737 7373T0 1384582 NM STA 500C-500D CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND A 1" CRACK IN STRINGER 16R AT STA 500C-500D. THE CRACKED SECTION OF STRINGER WAS REMOVED AND A NEW SECT ION WAS INSTALLED IAW SRM 53-30-03. 2 L 7 2 4F RT A16WE 2001082400088 20010824 00088 NM 2001 8 24 CALA0100785 1 20010824 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM STA 1006 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND FLOORBEAM CORRODED AT STA 1006, LBL 18. THE "T" CAP OF FLOORBEAM WAS REMOVED AND REPLACED IAW ECRA 5310 -03851. 2 L 7 2 4F RT A16WE 2001082400089 20010824 00089 2001 8 24 DL73K011342 4 20010815 A 2213 4038891916 COMPUTER BOEING 737 737232 1384475 NM E/E BAY FAULTY A DALA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 306DL 23078 ON APPROACH COPILOT ADI GOT COMPUTER FLAG, AIRSPEED BUG FLAG AND COURSE SELECTOR DID NOT RESPOND TO CHANGES. SLIGHT ELEC TRICAL SMELL IN FWD GALLEY. FOUND FCC PWR SUPPLY BURNT REPLACED "B" FCC PREFORMED COMPUTER TEST PER MAINTENANCE MANUAL 22-11-331 SYSTEM CHECKED NORMAL 2 L 7 2 4F RT A16WE 2001082400092 20010824 00092 NM 2001 8 24 SCNA01343 1 20010807 A 5322 SEAT TRACK BOEING 727 727225 1384077 NM STA 1078 LBL 55 CORRODED A SCNA O OTHER O OTHER IN INSP/MAINT 1 GL 15 282SC 22558 DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON THE SEAT TRACK AT STA 1078 LBL 55. REMOVED CORR OSION IAW B727 SRM 511006. REMOVED DAMAGED AREA IAW B727 SRM 513002. FABRICATED NEW SEAT TRACK PER SAMPLE FROM BAC 15207 92. TREATED AND PRIMED IAW B727 SRM 511002 AND MM 512002. INSTALLED IAW B727 SRM 513002. 2 L 7 3 4F A3WE 2001082400095 20010824 00095 NM 2001 8 24 DL777011332 1 20010814 A 2432 263BA1012 BATTERY BOEING 777 777232 1385232 NM E/E BAY FAILED A DALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 SO 27 860DA 29951 MAIN BATT FAILED PRIOR TO DEPT MTC MSG24-13054. REPLACED MAIN BATT AND BATT CHARGER PRECAUTIONARY PER MM. BATT P /N 263BA101-2 S/N 1484 OFF. 2 L 7 2 4F RT T00001SE 2001082400096 20010824 00096 NM 2001 8 24 VNAA0108010 1 20010818 A 2100 5413C000 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA O OTHER O OTHER CL CLIMB 1 GL 07 459PS 1982 3070 WHILE CLIMBING OUT FROM PIT, THE CREW NOTICED THE CABIN TEMPERATURE WAS 95 DEGREES. THE CREW TRIED THE TEMPERATURE CONT ROL VALVE IN BOTH MANUAL AND AUTO MODES WITH NO EFFECT. THE CREW DECIDED TO RETURN TO PIT. MAINTENANCE INSPECTED AND R EPLACED THE TEMPERATURE CONTROL VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 21-00-00. OPERATIONAL CHECKS WERE P ERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001082400098 20010824 00098 NM 2001 8 24 DLM11011249 1 20010727 A 2530 348100 CHILLER DOUG MD11 MD11 3023602 NM GALLEY DEFECTIVE A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 810DE 48565 HEAVY ELEC BURNING SMELL FROM FWD GALLEY NOTED IN COCKPIT ALSO FLT ATTENDANT PULLED BREAKERS. CA FD OVEN 102 HAS ELEC SM ELL. REPLACED OVEN AND CHILLER, CKS GOOD. 2 L 7 3 4F RT A22WE 2001082400099 20010824 00099 NM 2001 8 24 VNAA0108012 1 20010819 A 2100 DOOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE A VNAA O OTHER O OTHER CL CLIMB 1 GL 07 423JS 3032 DURING CLIMB, THE CABIN PRESSURE WAS CLIMBING WITH THE AIRCRAFT. AFTER CLIMBING TO 8000 FT MSL THE CABIN PRESSURE WAS I NDICATING 7500 FT MSL. FLIGHT 4030 RETURNED TO PIT WHERE MAINTENANCE INSPECTED AND FOUND THE AVIONICS MAINTENANCE DOOR IMPROPERLY INSTALLED. MAINTENANCE INSTALLED THE AVIONICS MAINTENANCE DOOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001082400100 20010824 00100 NM 2001 8 24 VNAA0108013 1 20010819 A 2600 51653151 CONTROL BOX DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RH FAILED A VNAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 427JS 16342 3039 AFTER TAXIING FROM THE GATE, THE CREW RECEIVED A RIGHT HAND LOOP FAIL ON THE RED WARNING PANEL. THE CREW FOLLOWED THE Q UICK REFERENCE HANDBOOK THEN CALLED MAINTENANCE CONTROL AFTER CONFIRMING THERE WAS NO FIRE. MAINTENANCE CONTROL REQUEST ED THE CREW RETURN TO THE GATE WHERE MAINTENANCE INSPECTED AND REPLACED THE FIRE CONTROL BOX IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001082400101 20010824 00101 NM 2001 8 24 VNAA0108008 1 20010815 A 3200 7178011 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA O OTHER J O WARNING INDICATION OTHER DE DESCENT 1 GL 07 426JS 3464 3038 ON APPROACH TO AZO, THE GEAR WAS SELECTED DOWN AND THE CREW RECEIVED NO GEAR INDICATION. THE CREW FOLLOWED THE QUICK RE FERENCE HANDBOOK AND MANUALLY LOWERED THE GEAR. THE MAIN GEAR WAS GREEN BUT THE NOSE SHOWED IN TRANSIT. THE CREW DID A FLY BY TO ENSURE GEAR WAS DOWN. FLIGHT 4172 THEN LANDED WITH NO FURTHER INCIDENTS. ONCE ON THE GROUND, OUTSTATION MAI NTENANCE CAME OUT AND PINNED THE GEAR BEFORE TAXIING TO THE GATE. THE AIRCRAFT WAS FERRIED TO PIT WHERE MAINTENANCE REM OVED AND REPLACED THE LANDING GEAR SELECTOR VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. THE AIRCRAFT WAS THEN FERRIED TO CAK WHERE THE OPERATIONAL CHECKS WERE COMPLETED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001082400113 20010824 00113 NM 2001 8 24 DLM11011254 1 20010728 A 3597 WIRE DOUG MD11 MD11 3023602 NM CABIN SHORTED A DALA K NONE O OTHER LD LANDING 1 SO 27 809DE 48480 O2 MASKS DROPPED ON LANDING, SEVERAL MASKS PULLED BY PASSENGERS AND O2 GENERATORS STARTED. FOUND WIRING SHORTED TO CABIN LIGHTS SIDEWALL CONTROL WIRING AT 4L F/A SEAT. REPAIRED WIRING. STOWED O2 MASKS PER M/M 35-21 AND GENERATORS REPLACED. 2 L 7 3 4F RT A22WE 2001082400114 20010824 00114 NM 2001 8 24 DLM11011256 1 20010728 A 3597 WIRE DOUG MD11 MD11 3023602 NM CABIN SHORTED A DALA K NONE O OTHER LD LANDING 1 SO 27 809DE 48480 02 MASKS ON LANDING DROPPED - FOUND WIRING SHORTED AT 4L F/A SEAT - REPAIRED SAME 2 L 7 3 4F RT A22WE 2001082400119 20010824 00119 NM 2001 8 24 DLM11011263 1 20010730 A 2121 6054578 FAN DOUG MD11 MD11 3023602 NM CABIN NOISY A DALA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 807DE 48478 ORIGINAL DEPARTED NGO. ELECTRICAL FUMES DETECTED ONE HOUR INTO FLIGHT. STRONGEST ODOR IN FORWARD CABIN CLOSE TO THE STAR WARS PANEL DIVERTED TO NARITA. LANDING WEIGHT 425,000LBS. PERFORMED ENTIRE CABIN INSPECTION. FOUND NR 2 RECIRCULATION FAN MAKING EXCESSIVE NOISE DEACTIVATED NR 2 RECIC-FAN AND DEACTIVATED NR 4 RECIRC-FAN DUE TO HIGH SERVICE TIME AS PRECA UTION FWD FAN TO MCO AND PLAC REF MEL 21-22-03 LANDING WEIGHT WITHIN LIMITS NO INSPECTION REQUIRED PER M/M. RMVD AND REP L 4 RECIRC FAN. REPL 2 RECIRC FAN. OPS CK GOOD 2 L 7 3 4F RT A22WE 2001082400124 20010824 00124 NM 2001 8 24 DLM11011328 1 20010813 A 2430 SM601BA15A30 RCCB DOUG MD11 MD11 3023602 NM ELECTRICAL SYS FAILED A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 802DE 48473 WHILE VERIFYING BOTH RCCBS B1-1649 AND B1-391 TO BE IN OPEN STATE REFERENCE MEL 28-22-06E L2 FWD AUX PUMP LOW PRESSURE C ONDITION RCCB BI-1649 L2 PUMP WOULD NOT GO TO THE OPEN CONDITION, STUCK IN THE CLOSE CONDITION. REMOVED AND REPLACED RCC B B1-1649 PER M/M PERFORMED SATISFACTORY OPERATIONAL CHECK PER M/M . 2 L 7 3 4F RT A22WE 2001082400127 20010824 00127 NM 2001 8 24 DLM88011273 1 20010801 A 2621 8981501 FIRE BOTTLE DOUG MD88 MD88 3023688 NM TAIL LOW A DALA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 960DL 49979 AFTER TAKE OFF AGENT 2 LOW LIGHT ILLUMINATED. C/A RPLD AGENT 2 BOTTLE CKS GOOD. 2 L 7 2 4F RT A6WE 2001082400133 20010824 00133 NM 2001 8 24 DLM88011274 1 20010801 A 2120 CLAMP DOUG MD88 MD88 3023688 NM A/C BAY LOOSE A DALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 SO 27 960DL 49979 TAIL COMP TEMP HIGH LIGHT ILLUMINATED AFTER T/O LIGHT, EXTINGUISHED AFTER RT PACK TURNED OFF. C/A FOUND HOT AIR COMING F ROM RT ACM TURBINE CLAMP AT 1200 O'CLOCK TIGHTEN SAME CKS GOOD. 2 L 7 2 4F RT A6WE 2001082400139 20010824 00139 NM 2001 8 24 DLM88011276 1 20010802 A 3097 WIRE DOUG MD88 MD88 3023688 NM WINDOW SENSOR EXPOSED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 933DL 49720 WINDOW R1 SENSOR SMOKED WHEN ANTI-FOG TURNED ON AND CAPTS ADI WENT BLANK THEN RETURNED. CA FOUND TERMINAL ON THERMAL SWI TCH FOR ANTI FOG SYS. INSULATION CRACKED AND RUBBING ON CONTACT SPRING. RE ROUTED WIRES ON HEATING ELEMENT SENSOR 2 L 7 2 4F RT A6WE 2001082400144 20010824 00144 NM 2001 8 24 DLM88011280 1 20010803 A 7110 2190060501 SKIN DOUG MD88 MD88 3023688 NM NOSE COWL DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DL 49532 THE NOSE COWL ACOUSTIC BARREL BACKSKIN WAS FOUND DELAMINATED REPAIR PER ER/A . 2 L 7 2 4F RT A6WE 2001082400147 20010824 00147 NE 2001 8 24 DLM88011301 2 20010808 A 7230 COMPRESSOR DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE STALLED A DALA E A ENGINE SHUTDOWN UNSCHED LANDING R E B PARTIAL RPM/PWR LOSS VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 966DL 34398 53115 718086 AT 280FL NR 1 ENG HAD A COMPRESSOR STALL WITH VIBRATION. IT WAS FOLLOWED BY SMOKE IN THE CABIN. THE CREW KEPT THE ENG RU NNING UNTIL 3000 FT WHEN THE VIBRATION INCREASED. THE CREW THEN SHUT DOWN THE ENG REPLACED ENGINE. 2 L 7 2 4F 4 F RT A6WE E9NE 2001082400149 20010824 00149 NM 2001 8 24 DLM88011313 1 20010810 A 3350 0201720001 LIGHT DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 907DL 49538 EMERGENCY LIGHTS AT 3C INOP. REPLACED LIGHT ASSY. 2 L 7 2 4F RT A6WE 2001082400151 20010824 00151 NM 2001 8 24 DLM88011316 1 20010811 A 2170 COALESCER BAG DOUG MD88 MD88 3023688 NM A/C BAY DIRTY A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 905DE 53410 SMOKE IN CABIN, PERFORMED DUCT BURNOUT. REPLACED COALESCER BAG. 2 L 7 2 4F RT A6WE 2001082400153 20010824 00153 NM 2001 8 24 DLM88011321 1 20010812 A 2170 COALESCER BAG DOUG MD88 MD88 3023688 NM A/C BAY DIRTY A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 981DL 53268 SMOKE IN CABIN, PERFORMED DUCT BURNOUT AND REPLACED COALESCER BAGS. 2 L 7 2 4F RT A6WE 2001082400160 20010824 00160 NM 2001 8 24 KPVA200116 1 20010726 A 3300 82410162003 CONTROL BOX DHAV DHC8 DHC8103 1386005 NM AVIONICS RACK FAILED A KPVA K NONE O OTHER TX TAXI/GRND HDL 1 WP 13 805WP 16914 353 HNL - FLT 1639 - EMERGENCY LIGHTS WILL NOT TURN OFF EXCEPT IN 'ARMED' POSITION WITH BATTERY POWER ON. TROUBLE SHOT SYST EM AND DETERMINED THE SYSTEM CONTROL BOX FAILED. REMOVED AND REPLACED EMERGENCY LIGHTS CONTROL BOX, OPERATIONAL CHCK OF SYSTEM COMPLIED WITH GOOD. (M) 2 H 7 2 4T RT A13NM 2001082400161 20010824 00161 SO 2001 8 24 MASA01075 1 20010725 A 5600 WINDSHIELD EMB 145 EMB145 SO CRACKED A MASA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 826MJ 145214 FLT 5866 - CLT-XNA - DECLARED AN EMERGENCY AND DIVERTED TO CHA DUE TO THE PILOTS WINDSHIELD CRACKING. AFTER AN UNEVENTF UL LANDING MAINTENANCE WAS CALLED. REMOVED AND REPLACED THE PILOTS WINDSHIELD. OP CHECKS GOOD. THE AIRCRAFT WAS RETUR NED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001082400162 20010824 00162 EA 2001 8 24 MASA01043 1 20010522 A 2700 601R930303 TRANSMITTER CNDAIR CL600 CL6002B19 EA DEFECTIVE A MASA B EMER. DESCENT N FALSE WARNING AP APPROACH 1 SW 07 37208 7208 FLT 5778 - DURING APPROACH TO LANDING AT CLT DECLARED AN EMERGENCY BECAUSE OF WHAT THE CAPT THOUGHT WAS A FLAP FAIL PROB LEM. MAINTENANCE WAS CALLED AFTER UNEVENTFUL LANDING. MAINTENANCE TROUBLE SHOT THE SYSTEM AND FOUND OUT IT WAS AN INDI CATION PROBLEM. THE INDICATION DISCREPANCY AS MEL'D THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001082400163 20010824 00163 NM 2001 8 24 UIEA01074 1 20010724 A 5300 SKIN BOEING 747 7472D3B 1384805 NM BS 1814 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 506MC 73880 21252 DURING HFEC INSPECTION FOUND THE LOWER AFT CARGO COMPARTMENT DOOR CUTOUT, UPPER FORWARD CORNER SKIN CRACKED AT STATION 1 814, STRINGER 27R. CRACK TRIMMED AWAY. FILLER AND REPAIR DOUBLER FABRICATED AND INSTALLED PER STANDARD PRACTICES IAW S RM 53-30-03 FIG 60 TYPE 1. REINSPECTION REQUIRED AFTER INSTALLATION OF REPAIR AT 15000 CYCLES INITIAL AND REPETITIVLY A T 3000 CYCLES THEREAFTER. (M) 2 L 7 4 4F RT A20WE 2001082400164 20010824 00164 NM 2001 8 24 UIEA01093 1 20010730 A 5300 65B0794256 FRAME BOEING 747 747230B 1384889 NM BS 320 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 508MC 21644 DURING HFEC INSPECTION PER AD 96-26-04 REFERENCES SB 747-53A2293 FOUND FRAME STATION 320 RIGHT CRACKED AT AN INSULATION BLANKET STUD MOUNTING HOLE. REMOVED FRAME. REPLACED FRAME WITH P/N 65B07942-564 PER SB 747-53A2293 IAW SRM 51-30-02. (M) 2 L 7 4 4F A20WE 2001082400165 20010824 00165 NM 2001 8 24 UIEA0192 1 20010730 A 5300 65B0794251 FRAME BOEING 747 747230B 1384889 NM BS 280 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 508MC 21644 DURIN HFEC INSPECTION PER AD 96-26-04 REFERENCE SB 747-53A2293 FOUND FRAME STATION 280 LEFT CRACKED AT TWO PLACES. EACH CRACK WAS APPROXIATELY .250 INCH LONG, ONE EMINATING FROM AN INSULATION BLANKET STUD MOUNTING HOLE, THE OTHER FROM A GU SSET FASTENER HOLE TO END OF FRAME. REMOVED FRAME AND CRACKED GUSSET ANGLE. FABRICATED REPLACEMENT GUSSET ANGLE PER BO EING DRAWING 65B07942, TREATED AND PRIME PAINTED PER SRM 51-10-02. REPLACED FRAME WITH P/N 65B07942-335 AND GUSSET ANGL E PER SB 747-53A2293 IAW SRM 51-30-02. (M) 2 L 7 4 4F A20WE 2001082400166 20010824 00166 NM 2001 8 24 UIEA01090 1 20010726 A 5300 65B011968 FITTING BOEING 747 7472D3B 1384805 NM BS 1480 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 506MC 21252 DURING INSPECTION FOUND BS 1480 LEFT AND RIGHT INBOARD HORIZONTAL SUPPORT FITTINGS CORRODED AT THE ATTACHMENT TO THE BOD Y GEAR TRUNNION, VERTICAL SUPPORT FITTING. REMOVED BUSHINGS FROM BOLT HOLES. BLENDED LOCAL CORROSION. SPOT FACED AREA AROUND BOLT HOLES. PERFORMED OPEN HOLE HFEC INSPECTION TO INSURE NO CORROSION OR CRACKS. PERFORMED PENETRANT INSPECTI ON TO INSURE NO CRACKS OR CORROSION. NO ADDITIONAL CORROSION OR CRACKS FOUND. FLAP PEENED AREA, TREATED AND PRIME PAIN TED AREA. FABRICATED NEW SHORTER BUSHING AND INSTALLED. FILLED SPOT FACE VOID WITH BMS-95 SEALANT DURING REINSTALLATIO N PROCESS. (M) 2 L 7 4 4F RT A20WE 2001082400167 20010824 00167 NM 2001 8 24 UIEA01088 1 20010725 A 5300 65B100056 WEB BOEING 747 7472D3B 1384805 NM BS 1480 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 506MC 73880 21252 DURING INSPECTION FOUND WEB CORRODED BEHIND BS 1480 INBOARD BODY GEAR VERTICAL TRUNNION SUPPORT. CORROSION BLENDED PER SRM 51-10-01. PERFORMED HFEC OF BLENDED AREA TO INSURE CRACK AND CORROSION FREE. NO CRACKS OR CORROSION. MEASURED BLE ND AREAS. FABRICATED FILLERS AND CONTOURED TO FIT THE BLEND OUT AREAS. ALODINED AND PRIME PAINTED FILLERS AND BLENDED AREA. OVERSIZED EXISTING HOLES, REINSTALLED FASTENERS. (M) 2 L 7 4 4F RT A20WE 2001082400168 20010824 00168 NM 2001 8 24 UIEA01087 1 20010725 A 5300 65B1059545 FITTING BOEING 747 7472D3B 1384805 NM BS 1480 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 506MC 21252 DURING INSPECTION FOUND LEFT AND RIGHT BODY GEAR INBOARD TRUNNION SUPPORT FITTINGS CORRODED AT BS 1480 AFT SIDE OF LUG A T LONGERON ATTACH POINT. CLEANED CORROSION, SPOT FACED AFFECTED AREAS, FLAP PEENED, TREATED, PRIME PAINTED. PENETRANT INSPECTION PERFORMED. NO CRACKS FOUND. HFEC INSPECTION PERFORMED. NO CRACKS FOUND. FABRICATED REPLACEMENT HOLE BUSHI NGS EQUAL TO THE NEW THICKNESS. FABRICATED FILLER WASHERS TO RETURN TO ORIGINAL THICKNESS. INSTALLED FILLERS AND BUSHI NGS. REINSTALLED SERVICEABLE BOLTS AND RESTORED AREA. (M) 2 L 7 4 4F RT A20WE 2001082400169 20010824 00169 NM 2001 8 24 UIEA01086 1 20010725 A 5300 65B1508769 SHIM BOEING 747 7472D3B 1384805 NM BS 1241 A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 506MC 21252 DURING INSPECTION FOUND SHIMS MIGRATING FROM BS 1240 LEFT/RIGHT BULKHEAD UPPER CHORD FITTING. REMOVED BOLTS IN AFFECTED AREA, TRIMMED SECTION OF MIGRATED SHIM. FABRICATED REPLACEMENT SHIM FROM SOLID MATERIAL, ALODINED AND PRIME PAINTED. REINSTALLED REMOVED BOLTS. AREA TO BE REINSPECTED EVERY C-CHECK UNTIL ENTRIRE SHIM IS REPLACED. (M) 2 L 7 4 4F RT A20WE 2001082400170 20010824 00170 NM 2001 8 24 UIEA01085 1 20010725 A 5300 65B1046241 FITTING BOEING 747 7472D3B 1384805 NM LT/RT TRUNNION CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 506MC 73880 21252 DURING INSPECTION FOUND BOTH LEFT AND RIGHT MAIN LANDING BODY GEAR UPPER TRUNNION FITTING HAVE CORROSION IN THE FORWARD BOLT HOLE POCKET. REMOVED CORROSION PER SRM 51-10-01. MEASURED AND SPOT FACED AREA. PERFORMED PENETRANT INSPECTION PE RFORMED. NO CRACKS FOUND. OPEN HOLE HFEC INSPECTION PERFORMED. NO CRACKS FOUND. AREA FLAP PEENED AND TREATED. SHORT ER BOLT SUBSITUTED. LANDING GEAR REINSTALLED. (M) 2 L 7 4 4F RT A20WE 2001082400171 20010824 00171 NM 2001 8 24 UIEA01083 1 20010725 A 5400 322U00004 ANGLE BOEING 747 7472D3B 1384805 NM A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 506MC 21252 DURING INSPECTION FOUND NR 4 PYLON REAR ENGINE MOUNT OUTBOARD UPPER BULKHEAD ANGLE CRACKED AT FIRST FASTENER COMMON TO T HE CENTER LINE OF PYLON. PYLON HAS KIN CAP IN PLACE (PCW). TRIMMED AWAY CRACKS. FABRICATED STRAP AND ANGLE. OVERSIZED EXISTING HOLES IN REPAIR AREA AND INSTALLED PARTS PER STANDARD PRACTICES REPLACING EXISTING COLLARS WITH STEEL COLLARS RELATED TO STEEL PARTS AND ALUMINUM COLLARS RELATED TO ALUMINUM OR TITANIUM PARTS. (M) 2 L 7 4 4F RT A20WE 2001082400172 20010824 00172 NM 2001 8 24 UIEA01082 1 20010725 A 5300 65B0171515 FRAME BOEING 747 7472D3B 1384805 NM BS 440 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 506MC 73880 21252 DURING INSPECTION FOUND FRAME AN INNER CHORD CRACKED AT BS 440 STRINGER 15R TO EXISTING FASTENER. HFEC INSPECTED EXISTI NG FASTENER HOLE TO INSURE CONTAINMENT OF CRACK. NO ADDITIONAL CRACKS FOUND. FABRICATED REPLACEMENT DOUBLER AND NEW CL IP. PROCURRED NEW REPLACEMENT INNER CHORD. INSTALLED DOUBLER, CLIP AND INNER CHORD PER STANDARD PRACTICES OF THE SRM. CONTINUE CURRENT INSPECTION REQUIREMENTS PE SB 747-53A2265 UNTIL SB 53-2272 IS COMPLETED AT OR BEFORE 20,000 CYCLES. ( M) 2 L 7 4 4F RT A20WE 2001082400173 20010824 00173 NM 2001 8 24 UIEA01081 1 20010725 A 5300 65B01717516 FRAME BOEING 747 7472D3B 1384805 NM BS 480 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 506MC 21252 DURING INSPECTION FOUND FRAME WEB CRACKED AT BS 480 BETWEEN STRINGER 15 AND 16R CUT OUTS. STOP DRILLED CRACKS. FABRICA TED REPLACEMENT DOUBLER. INSTALLED DOUBLER PER STANDARD PRACTICES OF THE SRM. CONTINUE CURRENT INSPECTION REQUIREMENTS PER SB 747-53A2265 UNTIL SB 53-2272 IS COMPLETED AT OR BEFORE 20,000 CYCLES. (M) 2 L 7 4 4F RT A20WE 2001082400174 20010824 00174 NM 2001 8 24 UIEA01080 1 20010725 A 5300 65B01718519 WEB BOEING 747 7472D3B 1384805 NM BS 500 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 506MC 21252 DURING INSPECTION FOUND FRAME WEB CRACKED AT BS 500, STRINGER 9L AND STRINGER 8 TO 10AR. STOP DRILLED ALL CRACKS. FABR ICATED REPLACEMENT DOUBLERS. INSTALLED DOUBLER AT STRINGER 9L LOCATION AND AT STRINGER 8 TO 10AR LOCATION PER STANDARD PRACTICES OF THE SRM. CONTINUE CURRENT INSPECTION REQUIREMETNS PER SB 747-53A2265 UNTIL SB 53-2272 IS COMPLETED AT OR B EFORE 20,000 CYCLES. (M) 2 L 7 4 4F RT A20WE 2001082400175 20010824 00175 NM 2001 8 24 UIEA01079 1 20010725 A 5300 65B017165003 FRAME BOEING 747 7472D3B 1384805 NM BS 460 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 506MC 73880 21252 DURING INSPECTIN FOUND FRAME WEB CRACKED AT BS 460, STRINGER 13AL AT TWO LOCATIONS COMMON TO THE FRAME AND DOUBLER. HFE C INSPECTED EXISTING FASTENER HOLES IN WEB FOR CRACK CONTAINMENT. NO ADDITIONAL CRACKS FOUND. FABRICATED REPLACEMENT D OUBLERS, FILLERS AND NEW STRINGER TIE CLIP. INSTALLED PER STANDARD PRACTICES IAW SRM. CONTINUE CURRENT INSPECTION REQU IREMENTS PER SB 747-53A2265 UNTIL SB 53-2272 IS COMPLETED AT OR BEFORE 20,000 CYCLES. (M) 2 L 7 4 4F RT A20WE 2001082400176 20010824 00176 NM 2001 8 24 UIEA01078 1 20010725 A 5300 65B017155003 FRAME BOEING 747 7472D3B 1384805 NM BS 440 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 506MC 73880 21252 DURING INSPECTION FOUND FRAME AND CHORD CRACKED AT BS 440, STRINGER 13AL/14L. CRACK IS APPROX 1 INCH LONG. CHORD IS CO MPLETELY SEVERED. HFEC INSPECTED EXISTING FASTENER HOLE IN FRAME FROM CRACK CONTAINMENT. NO ADDITIONAL CRACKS FOUND. FABRICATED REPLACEMENT DOUBLERS, FILLERS AND TWO NEW STRINGER TIE CLIPS. INSTALLED PER STANDARD PRACTICES. REPLACED SE VERED CHORD WITH NEW CHORD. INSTALLED PER STANDARD PRACTICES IAW SRM. CONTINUE CURRENT INSPECTION REQUIREMENTS PER SB 747-53A2265 UNTIL SB 53-2272 IS COMPLETED AT OR BEFORE 20,000 CYCLES. (M) 2 L 7 4 4F RT A20WE 2001082400177 20010824 00177 NM 2001 8 24 UIEA01077 1 20010725 A 5300 65B01713503 FRAME BOEING 747 7472D3B 1384805 NM BS 400 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 506MC 73880 21252 DURING INSPECTION FOUND FRAME CRACKED AT BS 400, STRINGER 15L CUT OUT. CRACK IS APPROXIMATELY .30 INCH LONG RUNNING FRO M STRINGER CUT OUT TO FASTENER HOLE. HFEC INSPECTED EXISTING FASTENER HOLE FOR CRACK CONTAINMENT. NO ADDITIONAL CRACKS FOUND. FABRICATED REPLACEMENT DOUBLER AND TIRPLER AND NEW STRINGER TIE CLIP. INSTALLED PER STANDARD PRACTICES. CONTI NUE CURRENT INSPECTION REQUIREMENTS PER SB 747-53A2265 UNTIL SB 53-2272 IS COMPLETED AT OR BEFORE 20,000 CYCLES. (M) 2 L 7 4 4F RT A20WE 2001082400178 20010824 00178 NM 2001 8 24 UIEA01076 1 20010725 A 5300 65B017121 WEB BOEING 747 7472D3B 1384805 NM BS 380 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 506MC 73880 21252 DURING INSPECTIN FOUND FRAME WEB CRACKED AT BS 380 FROM STRINGER 23L CUTOUT. TRIMMED AWAY CRACKED AREA. FABRICATED REP LACEMENT DOUBLER AND TWO ANGLES. INSTALLED PER STANDARD PRACTICES. CONTINUE CURRENT INSPECTION REQUIREMENTS PER SB 747 -53A2265 UNTIL SB 53-2272 IS COMPLETED AT OR BEFORE 20,000 CYCLES. (M) 2 L 7 4 4F RT A20WE 2001082400179 20010824 00179 EA 2001 8 24 ASOA01100 1 20010630 A 3350 487190 CONNECTOR CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 865AS 7507 FLT 4403 - DURING GROUND INSPECTION IN ATL, CREW REPORTED THE LAST 2 SECTIONS OF FLOOR EMERGENCY LIGHTS INOPERATIVE. MA INTENANCE RESECURED EMERGENCY LIGHT WIRING CONNECTOR AT THE LAST 2 SECTIONS. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2001082400183 20010824 00183 NM 2001 8 24 DLM90011303 1 20010808 A 3241 60060791R FUSE DOUG MD90 MD9030 3023690 NM LT MLG WW BROKEN A DALA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 905DA 53385 RT HYD SYS DUMPED ON TAXI OUT. A/C RETURN TO GATE. CONTRACT MTC FOUND RT OTBD ANTI-SKID CONTROL VALVE FUSE BROKEN FROM VALVE. REPLACED SAME. 2 L 7 2 4F RT A6WE 2001082400188 20010824 00188 NM 2001 8 24 DLM90011344 1 20010815 A 3350 4113030LF00101 BATTERY PACK DOUG MD90 MD9030 3023690 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 901DA 53381 OVERWING EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. CKS GOOD. 2 L 7 2 4F RT A6WE 2001082400189 20010824 00189 EU 2001 8 24 UPS01136402 1 20010725 A 2170 COALESCER BAG AIRBUS A300 A300F4622R 3930360 EU LT A/C PACK CONTAMINATED A IPXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 128UP 0813 INSPECTION TYPE:N/A CREW REPORTED THAT THEY HAD A SMOKE SMELL IN THE COCKPIT AND THAT THE NR 1 IDG WHICH AS ON DEFERRAL WAS READING 120C ON THE OIL TEMP WHILE THE NR 2 OIL TEMP WAS READING 90C. R&R LT PACK COALESCER BAG IAW MM 21-51-16, REF TSM 21-20-00, FIG 210 , OPER BOTH AC PACKS WITH TEMP SEL IN COLD AND HOT FOR SEVERAL MINUTES USING APU AIR AND NR 1 & NR 2 ENG BLEED AIR DURING HI PWR RUN. NO EVIDENCE OF SMOKE AND SYS OPER NORMALLY 2 L 7 2 4F RT A35EU 2001082400191 20010824 00191 NM 2001 8 24 UPS01236405 1 20010725 A 3350 BATTERY PACK BOEING 727 727172C 1384058 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 916UP 19808 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS DO NOT WORK REPLACED BATTERY PACK. OPS CHECKS NORMAL, REF 33-50-01 2 L 7 3 4F A3WE 2001082400192 20010824 00192 2001 8 24 UPS01236410 4 20010727 A 2210 DAMPENER BOEING 727 72722C 138400F NM RUDDER FAILED A IPXA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED NR NOT REPORTED 1 SO 01 942UP 19101 INSPECTION TYPE:N/A 2 RUDDER HARD OVERS IN FLIGHT PILOT NOTICED LOWER YAW DAMPENER INDICATOR MOVED LEFT. LOWER YAW DAM PENER SWITCH WAS TURNED OFF AND FLIGHT CONTINUED WITH NO FURTHER PROBLEMS. R&R LOWER YAW DAMPENER COUPLER PER MM 22-11-1 31 FAILED YAW DAMPENER CHANNEL. OPS CHECK G14 SWITCH POSITION 5 TRANSFER VALVE BALANCE MM 22-00 -00 P 507 14818 7/28/01 R/R YAW DAMPENER PER 22-11-131 NO DEFECTS NOTED OK FOR SERVICE. 2 L 7 3 4F A3WE 2001082400193 20010824 00193 NM 2001 8 24 UPS01236411 1 20010710 A 5310 BEAM BOEING 727 72727C 138400J NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 914UP 19246 INSPECTION TYPE:N/A AFT PRESSURE BULKHEAD VERTICAL BEAM LBL 17.8 WL 264.5 SHOW CRACK RUNNING FROM STOP DOOR CUT OUT TO O /B CHORD. CUT OUT DAMAGED SECTION OF VERTICAL BEAM AT W/L 249 IAW UPS EO B727-53 10-11743 APPENDIX E INSTALLED NEW SECTI ON AND REMOVED PARTS IAW EO N O B727-5310-1174 APPENDIX E. 2 L 7 3 4F A3WE 2001082400194 20010824 00194 NM 2001 8 24 UPS01236414 1 20010709 A 5312 PRESSURE PANEL BOEING 727 72727C 138400J NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 914UP 19246 INSPECTION TYPE:N/A NLG WW LT SIDE WALL CRACK INDICATION BETWEEN FASTENERS BS 235 AND LOWER OF FWD ACCESS. REMOVE ACCESS NR 3122 FOR ACCESS REPAIR AS PER B727SRM 51-30-02 CUT OUT DAMAGED AREA AS PER B727 SRM 51-30-02, SIZE OF CUT 2X1 INCH A CCOMPLISHED NDT ON CUT OUT AND NO CRACKS NOTED. 2 L 7 3 4F A3WE 2001082400197 20010824 00197 WP 2001 8 24 SABA010044 2 20010824 A 7320 8974575 VALVE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UAR 01514 WP LEFT ENGINE BYPASSING A SABA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 33 961AE 961 66102 Aircraft 963 on flight 5100 from CLT to HTS. During takioff roll the left engine would not respond to power lever movem ent Takeoff was aborted. No evergency procedures were used. After the aircraft cleared the runway, the crew performed a ground run. The left engine only made 25% torque. The aircraft returned to the gate with no other problems. Mainte nance removed and replaced the left engine TTL valve. Ground run was performed. Ops checked good. Aircraft returned t o service. 2 L 7 2 4T 4 T RT A56EU E4WE 2001082400198 20010824 00198 NM 2001 8 24 UPS01236434 1 20010727 A 5320 ANGLE BOEING 727 72727C 138400J NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 INSPECTION TYPE:N/A FRAME ANGLE CRACKED STA 351 JUST AFT OF O/B AFT CORNER OF ACCESS PANEL BEHIND NLG RT SIDE CUTOUT DAM AGED ANGLE PER SRM 51-10-01 PERFORMED HFEC INSPECTION OF CUTOUT AREA NO CRACKS NOTED REPAIRED PER B727 5330 15208. 2 L 7 3 4F A3WE 2001082400199 20010824 00199 NM 2001 8 24 UPS01236436 1 20010717 A 5320 65251102 FITTING BOEING 727 72727C 138400J NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 909UP 19115 INSPECTION TYPE:C SUSPECT CRACK AT TAIL SKID COMPT, RT UPPER TENSION TIE END FITTING CRACK CONFIRMED BY NDT, FITTING REP LACED IAW DRAWING. 2 L 7 3 4F A3WE 2001082400200 20010824 00200 NM 2001 8 24 UPS01236437 1 20010731 A 5312 PRESSURE PANEL BOEING 727 72727C 138400J NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 909UP 19115 INSPECTION TYPE:C CRACK IN MLG WEB BS 938 O/B AFT CORNER ADJACENT TO STR 18A LWR FASTENER ROW IN RT MLG WW CRACK DRESSED OUT AND NDT CONFIRMED REMOVAL SRM51-10-1 WEB REPAIRED IAW SRM 51-20-02. 2 L 7 3 4F A3WE 2001082400202 20010824 00202 NM 2001 8 24 UPS01236439 1 20010718 A 5320 654661117 BRACKET BOEING 727 72727C 138400J NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 909UP 19115 INSPECTION TYPE:C CRACK ON EDGE OF FLOOR PANEL SUPPORT BRACKET AT STA 755 LBL 50. NEW BRACKET FITTED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 2001082400204 20010824 00204 NM 2001 8 24 UPS01236440 1 20010717 A 5330 SKIN BOEING 727 72727C 138400J NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 909UP 19115 INSPECTION TYPE:C CORROSION ON LAP S24R BS 295 CPCP NEAR REPAIR REQUIRED SKIN REPLACEMENT WHICH ENCOMPASSED THIS DAMAGE , SKIN REPLACED. 2 L 7 3 4F A3WE 2001082400205 20010824 00205 NM 2001 8 24 UPS01236443 1 20010728 A 3350 BATTERY BOEING 727 72730C 1384009 NM CABIN DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 918UP 19008 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS EXTINGUISH SHORTLY AFTER TURNED ON. REPLACED BATT IN FWD AFT EMERG LIGHT ASSY OPS CHECKS GOOD. 2 L 7 3 4F A3WE 2001082400206 20010824 00206 NM 2001 8 24 UPS01236444 1 20010730 A 5320 FITTING BOEING 727 72727C 138400J NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 INSPECTION TYPE:IN FRAME FOOT ANGLE AT FS 351 BETWEEN STRINGERS 24R AND 25R IS SEVERELY CORRODED. THIS IS UNDER FLOOR PA NEL ON RT SIDE OF NLG WW ENCLOSURE ON THE INSIDE. R&R FRAME FOOT ASSY PER SRM 51-30-02. 2 L 7 3 4F A3WE 2001082400207 20010824 00207 NM 2001 8 24 UPS01236460 1 20010716 A 5230 65263375 HINGE BOEING 727 72727C 138400J NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 909UP 19115 INSPECTION TYPE:C MAIN CARGO DOOR FWD AND AFT HINGES CRACKED. ON INVESTIGATION HINGES FOUND CORRODED BEYOND LIMITS, HING ES REPLACED IAW OHM 20-50-01 2 L 7 3 4F A3WE 2001082400208 20010824 00208 NM 2001 8 24 UPS01236476 1 20010722 A 5320 65852082 FITTING BOEING 727 72727C 138400J NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 909UP 19115 INSPECTION TYPE:C TAIL SKID LT LWR TENSION TIE REAR TERMINAL FITTING CRACKED. LT LWR TENSION TIE AFT FITTING REMOVED AND NEW ONE INSTALLED IAW DRAWING 65-25992. 2 L 7 3 4F A3WE 2001082400209 20010824 00209 NM 2001 8 24 UPS01236530 1 20010803 A 3350 BATTERY BOEING 727 72727C 138400J NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 914UP 19246 INSPECTION TYPE:IN ILLEGIBLE EXIT LIGHT AT MAIN ENTRY DOOR INOP. REPLACED ILLEGIBLE EXIT LIGHT BATTERY AND OPS CHECK AS PER B727 M/M 33-50-00. 2 L 7 3 4F A3WE 2001082400210 20010824 00210 2001 8 24 UPS01236532 4 20010805 A 2565 SLIDE BOEING 727 72751C 1384015 NM CABIN INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:IN MAIN CABIN SLIDE INOP REF DEF M220206 FWD ENTRY SLIDE DEPLOYED. REPLACED SLIDE AND LATCH ASSY REF 25- 60-14. 2 L 7 3 4F A3WE 2001082400211 20010824 00211 NM 2001 8 24 UPS01236604 1 20010805 A 5753 FAIRING BOEING 727 72730C 1384009 NM T/E FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:PFLT LT INBD FLAP LT OUTBD CANOE FIXED FAIRING HAS A CRACK ON AFT UPPER CORNER OF PREVIOUS REPAIR. DEFFE RRED PER MMOC 2 L 7 3 4F A3WE 2001082400212 20010824 00212 NM 2001 8 24 UPS01236605 1 20010811 A 2611 CONTROL UNIT BOEING 727 727185C 138406N NM SMOKE DETECTION FAULTY A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE:PFLT D/D M220970 LOWER AFT CARGO SMOKE DETECTOR. SUP SYS INOP. INSTALLED CONTROL UNIT IAW MM 26-18-04. REQUIRES ADJ/TEST KSM 55919 PERFORMED SMOKE DETECTOR / CONFIG MODULE ADJ/TEST MM 26-18-01 AND LOWER CARGO COMP SMOKE DE TECTION ADJ/TEST MM 26-18-00. NO DEFECTS NOTED. OK FOR SERVICE. 2 L 7 3 4F A3WE 2001090700213 20010907 00213 NE 2001 9 7 UPS01236663 2 20010820 A 7310 PACKING BOEING 727 727247 138408F NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE DAMAGED A IPXA C E ABORTED TAKEOFF ENGINE SHUTDOWN X ENGINE FLAMEOUT TO TAKEOFF 1 SO 01 209UP 21698 INSPECTION TYPE:N/A BTB/RTO - NR 2 ENGINE FLAMED OUT. NR 2 ENGINE WOULD NOT ADVANCE WAS BELOW IDLE 50 PERCENT N2. FOUND PACKING IN COUPLING NUT SHREDDED AND NO FERRULE INSTALLED. R&R PACKING AND INSTALLED FERRULE IAW JT8D MM 73-12-1. LEAK C K GOOD. RETURN AIRCRAFT TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2001082400213 20010824 00213 NM 2001 8 24 UPS01436422 1 20010723 A 5330 2024730050IN SKIN BOEING 747 747200 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 1 INSPECTION TYPE:C-2 M/D L5 DOOR FWD CUTOUT BETWEEN STR 15 & 16 CUTOUT CRACKED. REPAIRED L5 DOOR FWD UPPER CUTOUT AS PER SRM 53-10-04 FIG 91. 2 L 7 4 4F RT A20WE 2001082400214 20010824 00214 NM 2001 8 24 UPS01436423 1 20010723 A 5320 WEB BOEING 747 747200 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 1 INSPECTION TYPE:C-2 U/D BS 330 STR 12L ATT WEB CRACKED. REPAIRED WEB AS PER SRM 51-40-02. 2 L 7 4 4F RT A20WE 2001082400215 20010824 00215 NM 2001 8 24 UPS01436424 1 20010723 A 5311 BACR15BB6D6C FRAME BOEING 747 747200 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 1 INSPECTION TYPE:C2 U/D BS 320 BETWEEN STR 2L AND 3L WEB CRACKED. REPAIRED FRAME WEB PER SRM 51-40-02. (NDT CONFIRM NO CR ACK BEYOND STOP HOLE AFTER STOP HOLE DRILLED PER SRM 51-10-01). 2 L 7 4 4F RT A20WE 2001082400216 20010824 00216 NM 2001 8 24 UPS01436425 1 20010723 A 5311 FRAME BOEING 747 747200 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C2 U/D BS 380 STR 6L AND 7L FRAME INNER CHORD CRACKED. REPAIRED FRAME INNER CHORDS & WEB AS PER SRM 53-1 0-04 FIG 98 (NDT C/OUT PER NDT MANUAL PT.6, 51-00-00 FIG04 CONFIRMED; RESULT: NO CRACK REVEALED AT TRIM OFF AREA NO CRAC K BEYOND STOP HOLE ). 2 L 7 4 4F RT A20WE 2001082400217 20010824 00217 NM 2001 8 24 UPS01436446 1 20010729 A 3350 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:N/A MAIN DECK ENTRY EMERGENCY LIGHTS ON LT SIDE HAS ONE INOP LAMP. R&R BOTH BULBS, OPS CHKS GOOD. 2 L 7 4 4F A20WE 2001082400218 20010824 00218 NM 2001 8 24 UPS01436448 1 20010727 A 5330 SKIN BOEING 747 747200 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:N/A FUSELAGE SKIN DAMAGE BS 2040 - 2160, LOWER SURFACE. REMOVED DAMAGE AND REPAIRED AREA IAW SRM 53-30-0 3 FIG 1 2 L 7 4 4F RT A20WE 2001082400219 20010824 00219 NM 2001 8 24 UPS01436450 1 20010718 A 5310 DOOR FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C M/D L2 DOOR FWD CUTOUT FRAME FOUND CRACKED AS MARKED. REPAIRED L2 DOOR CUTOUT FWD FRAME AS PER SRM 53- 10-04 FIG 84. 2 L 7 4 4F A20WE 2001082400220 20010824 00220 NM 2001 8 24 UPS01236684 1 20010809 A 5330 SKIN BOEING 727 72727C 138400J NM BS660 S19R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 908UP 19114 INSPECTION TYPE:C AREA OF LIGHT SURFACE CORROSION ON SKIN AT BS660 S19R ***CPCP*** AREA REPAIRED IAW APPENDIX 8.3 OF EO B727-5330-0509 2 L 7 3 4F A3WE 2001082400221 20010824 00221 NM 2001 8 24 UPS01236685 1 20010810 A 5100 69165541 INTERCOSTAL BOEING 727 72727C 138400J NM BS315 APRX CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 908UP 19114 INSPECTION TYPE:C INTERCOSTAL CRACKED ABOVE DRAG BRACE FITTING SUPPORT INTERCOSTAL REPLACED IAW DRWG 65-18417 2 L 7 3 4F A3WE 2001082400222 20010824 00222 NM 2001 8 24 UPS01236686 1 20010813 A 5310 6516350304 INTERCOSTAL BOEING 727 72727C 138400J NM BS1183WL230RBL62 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 908UP 19114 INSPECTION TYPE:C SUSPECT CRACK AT R/H BS 1183 WL 230 OUTBD LWR CORNER OF INTERCOSTAL AT RBL 62.5 INTERCOSTAL REPLAC ED IAW DWG 65-16350 2 L 7 3 4F A3WE 2001082400223 20010824 00223 NM 2001 8 24 UPS01236688 1 20010811 A 3270 6585208 TERMINAL BOEING 727 72727C 138400J NM BS1203 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 908UP 19114 INSPECTION TYPE:C L/H UPPER TENSION TIE CRACKED IN TAIL SKID BAY FABRICATED TERMINAL IAW DWG 65-85208, REMOVED / INS TALLED PER SRM 2 L 7 3 4F A3WE 2001082400224 20010824 00224 NM 2001 8 24 UPS01236689 1 20010813 A 5310 STIFFENER BOEING 727 72727C 138400J NM BS870 BL0 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 908UP 19114 INSPECTION TYPE:C WING CENTRE SECTION UPPER SKIN STIFFENER LWR CHORD IS CORRODED AT BS 870 RBL0. ***CPCP*** DAMAGED SECTION REMOVED AND NEW SECTION SPLICED IAW SRM 2 L 7 3 4F A3WE 2001082400225 20010824 00225 NM 2001 8 24 UPS01236690 1 20010816 A 5710 STRINGER BOEING 727 72727C 138400J NM WCS S1 BLO CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 908UP 19114 INSPECTION TYPE:C SUSPECT CRACK IN CENTRE SECTION UPPER STRINGER S1 IN THE WING CENTRE TANK STRINGER REPAIRED IAW SR M 57-10-04 FIG 2 2 L 7 3 4F A3WE 2001082400226 20010824 00226 NM 2001 8 24 UPS01436452 1 20010718 A 5310 DOOR FRAME BOEING 747 747217B 1384899 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C M/D R2 DOOR FWD CUTOUT FRAME FOUND CRACKED AS MARKED. FABRICATED / REPAIRED DOUBLERS AS PER SRM 53-10- 04 FIG 84. 2 L 7 4 4F A20WE 2001082400229 20010824 00229 NM 2001 8 24 UPS01436486 1 20010718 A 5312 141U10878 PRESSURE PANEL BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C NLG WW, BS 400 PRESSURE PAN CRACK FOUND APPROX 1 INCH LONG. NLG WW BS 400 BULKHEAD PRESSURE PAN REPLAC ED AS PER SRM 51- 10-01 AND INSTALLED AS PER BOEING DWG 624U0005 SHT 1 - 9. 2 L 7 4 4F A20WE 2001082400230 20010824 00230 NM 2001 8 24 UPS01436487 1 20010718 A 5320 65B0183713 STRUCTURE BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C M/D L1 DOOR FWD CUTOUT FRAME LWR REVEAL FOUND CRACKED AS MARKED. FASTENERS OF L1 DOOR FWD CUTOUT FRAME LWR REVEAL INSTALLED AS PER MM 52-11-01 AND SRM 51-10-01 FOR LWR REVEAL REPLACEMENT DONE, DR RIGGING AND OPERATIONAL TE ST DONE FOUND " SATIS " PER MM 52-11-01. 2 L 7 4 4F A20WE 2001082400231 20010824 00231 NM 2001 8 24 UPS01436516 1 20010802 A 3350 LIGHT BOEING 747 747200 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:N/A CREW ENTRY EMERG EXIT LIGHT INOP. INSTALLED LIGHT ASSY TESTED EMERGENCY LIGHT SYSTEM OPS. 2 L 7 4 4F RT A20WE 2001082400233 20010824 00233 NM 2001 8 24 UPS01436655 1 20010815 A 5220 DOOR BOEING 747 747123 1384873 NM COCKPIT LACK OF LUBE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:N/A EMERGENCY EXIT DOOR FOR ESCAPE SLIDE AT COCKPIT BINDS WHEN OPENING OR CLOSING. ADJUSTED LATCH AND LU BED TRACK SLIDE OPERATES NORMAL NO BINDING. 2 L 7 4 4F A20WE 2001082400234 20010824 00234 NM 2001 8 24 UPS01436656 1 20010818 A 3350 51356B37 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:N/A STA 350 RT CEILING LIGHT MISSING LENS AND INOP EMERGENCY EXIT LIGHT. REPLACED EMERGENCY LIGHT ASSY A T CEILING STA 350 RT CHKS GOOD. 2 L 7 4 4F A20WE 2001082400239 20010824 00239 NM 2001 8 24 UPS01536408 1 20010727 A 5230 PRIORITY VALVE BOEING 757 75724APF 1384969 NM CARGO DOOR DEFECTIVE A IPXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 475UP 28845 INSPECTION TYPE:N/A ATB FOR LOUD NOISE AND MCD DOOR EICAS WARNING IND DURING T/O LIGHT ILLUMINATED AT MAIN STRUT EXTENSI ON ON T/O ACCOMPANIED FROM A THUMP FROM THE CARGO AREA. DECLARED EMERGENCY AND RETURNED. ON DOWN WIND THE LIGHT EXTINGUI SHED. TROUBLE SHOT MAIN CARGO DOOR TO A DEFECTIVE PRIORITY VALVE (PV2) AS PER B757 MM 52-32-00. PERFORMED OPS CHECK AND LEAK CHECK OF MCD SYSTEM AS PER MM 52-32-00 SYSTEMS CHECK OK. 2 L 7 2 4F RT A2NM 2001082400240 20010824 00240 NM 2001 8 24 AWXA0002179 1 20010814 A 5313 149N712521 INTERCOSTAL BOEING 757 7572S7 1384962 NM FS 879-900 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 903AW 23323 D: Wing to body fairing support at LBL 7 corroded an lower I/B surfaces from FS 879-900.C; Removed damaged part, fabrica ted repair part and installed per 757 SRM 51-40-02 pg 1 and drawing 149N7125 2 L 7 2 4F RT A2NM 2001082400241 20010824 00241 NM 2001 8 24 AWXA0002181 1 20010816 A 5313 146N5390 INTERCOSTAL BOEING 757 7572S7 1384962 NM STR26R CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 903AW 23323 D: Aft cargo intercostal between STA 1360 to 1380 at STR -26 R/H is corroded.C: Removed intercostal and "L" angle per SR M 51-40-02 pg 1. Drilled and installed new intercostal and "L" angle at STA 1360-1380 IAW SRM 51-40-02 pg 1 2 L 7 2 4F RT A2NM 2001082400242 20010824 00242 NM 2001 8 24 AWXA0002182 1 20010818 A 5313 140N1530 STRINGER BOEING 757 7572S7 1384962 NM STA1450-1465 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 903AW 23323 D: Fuselage skin bulged between sta 1450-1465 stringer 28 L/HC: Bulging caused by corroded stringer, out of limits, remo ved damaged area fabricated repair parts and installed per 737 SRM 51-40-02, 53-00-03 fig 201 DWG 14683820, and SRM 51-2 0-01, 53-60-03 fig 1 2 L 7 2 4F RT A2NM 2001082400243 20010824 00243 2001 8 24 UPS01536562 4 20010809 A 3445 INDICATOR BOEING 757 75724APF 1384969 NM COCKPIT DEFECTIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 434UP 25465 INSPECTION TYPE:IN TCAS IND LIGHTING DIM. CREW INDICATED SAFETY OF FLIGHT CAPTAINS VSI/TCAS IND WITH COCKPIT LTS IN ANY POSITION IS TOO DIM TO READ. LIGHTING LEVEL COMES UP TO READABLE ONLY IF OVERHEAD MAP LTS ARE ON FULL THIS IS NOT A SAFE LIGHTING MODE FOR A NIGHT VISUAL APPROACH. REMOVED AND REPLACED CAPTAINS VSI/TCAS INDICATOR, OPERATIONAL TEST GOOD IAW MM 34-45-00 2 L 7 2 4F RT A2NM 2001082400244 20010824 00244 NM 2001 8 24 UPS01536614 1 20010815 A 5610 141T4800 WINDOW BOEING 757 75724APF 1384969 NM COCKPIT LEAKING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 439UP 25470 INSPECTION TYPE:N/A F/O'S R1 WINDOW AIR LEAK. R&R WINDOW IAW UPS MX FUNCTION CARD 5063 2 L 7 2 4F RT A2NM 2001082400246 20010824 00246 WP 2001 8 24 UPS01836430 1 20010723 A 5320 WEB DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C1/3 SUBFLOOR WEB AT FS 15 RBL 40 IS CRACKED. CUT OUT DAMAGE IN WEB & FABBED NEW REPAIR DOUBLERS & FILLE RS INSTALLED FILLER & DOUBLER IAW SRM. 2 L 7 4 4F RT 4A25 2001082400247 20010824 00247 WP 2001 8 24 UPS01836431 1 20010729 A 5610 WINDOW DOUG DC8 DC871F 302199D WP COCKPIT OUT OF ADJ A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:N/A CAPT SLIDE WINDOW WILL NOT OPEN. PERFORMED ADJUSTMENT OF CAPTS SLIDING WINDOW PER MM 56-10-03 OPS CK GOOD 2 L 7 4 4F RT 4A25 2001082400248 20010824 00248 WP 2001 8 24 UPS01836433 1 20010707 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 STA 1700 FLOORBEAM UPPER FLANGE IS CORRODED BEYOND LIMITS AT LBL 24. REPAIRED FLOORBEAM IAW 8110-3 AP PROVED DH SK 807-264 2 L 7 4 4F RT 4A25 2001082400249 20010824 00249 WP 2001 8 24 UPS01836441 1 20010717 A 5320 38877991N SPLICE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 STA 440-460 LONG 14L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3887799,AND SRM. 51-1-20D, 51-1-21 2 L 7 4 4F RT 4A25 2001082400250 20010824 00250 WP 2001 8 24 UPS01836442 1 20010709 A 5320 3779498501 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 STA 857 LONG 19L INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 377949 8,AND SRM 51-3-0 2 L 7 4 4F RT 4A25 2001082400251 20010824 00251 WP 2001 8 24 UPS01836465 1 20010709 A 5320 47504191N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 STA 1200 LONG 20R INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750419 ,AND SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001082400252 20010824 00252 WP 2001 8 24 UPS01836467 1 20010708 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 STA 1620 LT AFT ENTRY DOOR FRAME WEB IS CRACKED BELOW LOWER HINGE. REPAIRED WEB IAW SRM 53-2-0 FIG 1B 2 L 7 4 4F RT 4A25 2001082400253 20010824 00253 WP 2001 8 24 UPS01836468 1 20010715 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 STA -67 FLOORBEAM IS CORRODED BEYOND LIMITS AT LBL 60. REPAIRED FLOORBEAM IAW 8110-3 APPROVED DH SK 8 74-130 2 L 7 4 4F RT 4A25 2001082400254 20010824 00254 WP 2001 8 24 UPS01836469 1 20010710 A 5330 561229873 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 FINGER DOUBLER IS CORRODED BEYOND LIMITS AT STA -60 AT LBL 16. REMOVED,FABRICATED,AND REPLACED DOUBLE R IAW DWG 5612298,AND SRM 51-1-21 2 L 7 4 4F RT 4A25 2001082400255 20010824 00255 WP 2001 8 24 UPS01836470 1 20010709 A 5330 57799157 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 STA 1350 LONG 35L-35R FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED,FABRICATED,AND REPLACED DOUBL ER IAW DWG 5779915,AND SRM 51-1-20D,51-1-21 2 L 7 4 4F RT 4A25 2001082400256 20010824 00256 WP 2001 8 24 UPS01836471 1 20010710 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 STA 1160-1180 LONG 28L IS CORRODED BEYOND LIMITS. REPAIRED LONGERON IAW SRM 53-2-2 FIG 10 2 L 7 4 4F RT 4A25 2001082400257 20010824 00257 WP 2001 8 24 UPS01836478 1 20010716 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C1/3 MAIN CABIN AT STA 740-810 & LBL 47 SEAT TRACK HAS CORROSION INBD & OTBD SIDES OF SEAT TRACK AROUND FASTENER HOLES (UNDER SIDE). REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SEAT TR ACK, FABED NEW SEAT TR ACK, AND INSTALLED NEW SEAT TRACK IAW UPS SRM ADDENDUM & DC8 SRM 51-1-8 2 L 7 4 4F RT 4A25 2001082400258 20010824 00258 WP 2001 8 24 UPS01836479 1 20010712 A 5320 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C1/3 STA 1220 L35L TO L34L Z FITTING CORRODED. REMOVED AND REPLACED FITTING 2 L 7 4 4F RT 4A25 2001082400259 20010824 00259 WP 2001 8 24 UPS01836481 1 20010725 A 5320 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C1/3 AFT PIT FS 1228 L35R-L34R Z FITTING IS CRACKED. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-24 & 51-1- 20D 2 L 7 4 4F RT 4A25 2001082400260 20010824 00260 WP 2001 8 24 UPS01836492 1 20010709 A 5320 5750540501N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 STA 660-680 LONG 11R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 5750540, AND SRM 51 -1-20D 2 L 7 4 4F RT 4A25 2001082400261 20010824 00261 WP 2001 8 24 UPS01836493 1 20010709 A 5320 3779659U501 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 STA 902-920 LONG 8R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659,AND SRM 53-1 -0,51- 1-20D,51-1-21 2 L 7 4 4F RT 4A25 2001082400262 20010824 00262 WP 2001 8 24 UPS01836494 1 20010709 A 5320 4612650U FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 STA 8 LONG 33R END FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 4612650U,A ND SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001082400263 20010824 00263 WP 2001 8 24 UPS01836495 1 20010709 A 5320 38877991N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 STA 440-460 LONG 17L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3887799,AND SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001082400264 20010824 00264 WP 2001 8 24 UPS01836496 1 20010705 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 STA 1723 LONG 15R FUSELAGE SKIN IS CRACKED. REPAIRED SKIN IAW SRM 53-2-1 FIG. 7 2 L 7 4 4F RT 4A25 2001082400265 20010824 00265 WP 2001 8 24 UPS01836497 1 20010709 A 5320 47516392 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 STA 798 LONG 18R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 475163 9,AND SRM 51-1-21 2 L 7 4 4F RT 4A25 2001082400266 20010824 00266 WP 2001 8 24 UPS01836498 1 20010709 A 5320 3779762U501 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 STA 660-680 LONG 10R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779762,AND SRM 51- 1-20D, 51-1-21 2 L 7 4 4F RT 4A25 2001082400267 20010824 00267 WP 2001 8 24 UPS01836499 1 20010709 A 5320 5887375548 CLIP DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 STA 680 LONG 18R INTERCOSTAL ATTACH CLIP IS CRACKED. REMOVED,FABRICATED,AND REPLACED CLIP IAW DWG 588 7375,AND SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001082400268 20010824 00268 WP 2001 8 24 UPS01836500 1 20010711 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 RIGHT WING LE UPPER RIB IS CRACKED AT XFS 585. REPAIRED RIB IAW SRM 57-2-0 FIG 2 2 L 7 4 4F RT 4A25 2001082400269 20010824 00269 WP 2001 8 24 UPS01836501 1 20010711 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C2 RIGHT WING LE UPPER RIB IS CRACKED AT XFS 641. REPAIRED RIB IAW SRM 57-2-0 FIG 2 2 L 7 4 4F RT 4A25 2001082400270 20010824 00270 WP 2001 8 24 UPS01836502 1 20010711 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 RIGHT WING LE LOWER RIB IS CRACKED AT XFS 616. REPAIRED RIB IAW SRM 57-2-0 FIG 2 2 L 7 4 4F RT 4A25 2001082400271 20010824 00271 WP 2001 8 24 UPS01836503 1 20010711 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 RIGHT WING LE LOWER RIB IS CRACKED AT XFS 609. REPAIRED RIB IAW SRM 57-2-0 FIG 2 2 L 7 4 4F RT 4A25 2001082400272 20010824 00272 WP 2001 8 24 UPS01836504 1 20010711 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 RIGHT WING LE UPPER RIB IS CRACKED AT XFS 760. REPAIRED RIB IAW SRM 57-2-0 FIG 2 2 L 7 4 4F RT 4A25 2001082400273 20010824 00273 WP 2001 8 24 MWEA011132 1 20010822 A 5310 99155583 FORMER DOUG DC9 DC932 3022066 WP AFT PRESS BULK CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 APB FORWARD SIDE, TOP LEFT SUPPROT HAS A CRACK LOCATED ON INBOARD END. -- FABRICATED AND INSTALLED SUPPORT. 2 L 7 2 4F A6WE 2001082400274 20010824 00274 WP 2001 8 24 UPS01836505 1 20010711 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 RIGHT WING LE UPPER RIB IS CRACKED AT XFS 697.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2 2 L 7 4 4F RT 4A25 2001082400275 20010824 00275 WP 2001 8 24 UPS01836506 1 20010711 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 RIGHT WING LE UPPER RIB RIB IS CRACKED AT XFS 691.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2 2 L 7 4 4F RT 4A25 2001082400276 20010824 00276 WP 2001 8 24 UPS01836507 1 20010711 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 RIGHT WING LE UPPER RIB IS CRACKED AT XFS 672.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2 2 L 7 4 4F RT 4A25 2001082400277 20010824 00277 WP 2001 8 24 UPS01836508 1 20010709 A 5320 37558722 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 STA 1260 LONG 20R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED,AND REPLACED FITTING IAW DWG 37558 72,AND SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001082400278 20010824 00278 WP 2001 8 24 UPS01836509 1 20010710 A 5320 3755842505N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 STA 1180 BATHTUB FITTING IS CRACKED BETWEEN LONG 27L-28L. REMOVED AND REPLACED FITTING IAW DWG 375584 2,AND SRM 53-2-0 FIG 2D 2 L 7 4 4F RT 4A25 2001082400279 20010824 00279 WP 2001 8 24 UPS01836510 1 20010710 A 5320 WEB DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 STA 1447 D-PIT TORQUE BOX WEB IS CRACKED AT LONG 32R. REPAIRED WEB IAW SRM 53-2-0 FIG 1D 2 L 7 4 4F RT 4A25 2001082400280 20010824 00280 WP 2001 8 24 UPS01836511 1 20010711 A 5320 WEB DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 STA 1550 AT LONG 21L CUSP MEMBRANE IS CRACKED. REPAIRED MEMBRANE IAW EO DC8-5330-2159 2 L 7 4 4F RT 4A25 2001082400281 20010824 00281 WP 2001 8 24 UPS01836512 1 20010710 A 5320 37558272N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 STA 280 LONG 33R BANANA FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 37558 27,AND SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001082400282 20010824 00282 WP 2001 8 24 UPS01836513 1 20010710 A 5320 37558411 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 STA 1220 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG 33R-34R. REMOVED AND REPLACED FITTING IAW DWG 3755841,AND SRM 53-2-0 FIG 2D 2 L 7 4 4F RT 4A25 2001082400283 20010824 00283 WP 2001 8 24 UPS01836514 1 20010710 A 5320 37558441N1 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 STA 1180 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG 31L-32L. REMOVED AND REPLACED FITTING IAW DWG 3755844,AND SRM 53-2-0 FIG 2D 2 L 7 4 4F RT 4A25 2001082400284 20010824 00284 WP 2001 8 24 UPS01836515 1 20010711 A 5312 PRESSURE PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 STA -77 LT NOSE TUNNEL PRESSURE WEB IS CRACKED AT LBL 60. REPAIRED WEB IAW SRO 8530026 2 L 7 4 4F RT 4A25 2001082400285 20010824 00285 WP 2001 8 24 UPS01836519 1 20010712 A 5320 FLOOR SUPPORT DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C1/3 FLOOR SUPPORT CORRODED. REMOVED AND REPLACED SUPPORT. 2 L 7 4 4F RT 4A25 2001082400286 20010824 00286 WP 2001 8 24 UPS01836522 1 20010801 A 5320 3755822515N FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C1/3 FWD BAG PIT Z FITTING CRACKED AT FS 300 LONGERON 27L. INSTALLED NEW Z FITTING P/N 3755822-515N IAW DC8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001082400287 20010824 00287 WP 2001 8 24 UPS01836523 1 20010710 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C1/3 SEAT TRACK E AT STA 980 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK. 2 L 7 4 4F RT 4A25 2001082400288 20010824 00288 WP 2001 8 24 UPS01836550 1 20010808 A 5230 SKIN DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:IN PIT 33 DOOR LOWER SKIN CRACKED AFT LWR CARGO FWD DOOR BOTTOM EDGE OF SKIN DOUBLER, TORN & CRACKED IN 2 PLACES. FOUND PERVIOUS REPAIR FILLER DAMAGED, NO DAMAGE TO INTERNAL DOUBLER REMOVED AND REPLACED FILLER IAW SRM 51-2- 0. 2 L 7 4 4F RT 4A25 2001082400290 20010824 00290 NM 2001 8 24 UPS01636634 1 20010817 A 5210 DOOR BOEING 767 767300 1385204 NM FWD CABIN LEAKING A IPXA K NONE O OTHER NR NOT REPORTED 1 SO 01 330UP 27756 INSPECTION TYPE:N/A PILOT REP, FWD ENTRY DOOR SQUEALING. BUILT UP THRESHOLD AND PRESSURIZED A/C LEAK CHECKS GOOD. 2 L 7 2 4F RT A1NM 2001082400291 20010824 00291 EU 2001 8 24 C2XA01IA335 1 20010820 A 3350 0341516 FUSE AEROSP ATR42 ATR42320 8680930 EU CABIN BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14815 104 GPT- DURING PERFLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHT ON THE FORWARD CABIN LEFT SIDE FRONT ROW FAILED TO ILLUMI NATE. THE AIRCRAFT WAS INSPECTED AND RELEASED FOR FERRY FLIGHT FORM GPT to IAH. IAH- MAINTENANCE REMOVED AND REPLACED A FUSE, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVE D FOR RETURN TO SARVICE. 2 H 7 2 4T RT A53EU 2001082500001 20010825 00001 SO 2001 8 25 CX2A01IA336 1 20010824 A 3350 1155981 SOCKET EMB 120 EMB120ER 3260203 SO CABIN BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 34712 120111 IAH- DURING 1A/2A INSPECTION IT WAS NOTED THAT THE FORWARD RED EMERGENCY AISLE PATH LIGHT FAILED TO ILUMINATE. IAH- M AINTENANCE REMOVED AND REPLACED THE FORWARD RED EMERGENCY AISLE LIGHT SOCKET, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001082500002 20010825 00002 EU 2001 8 25 C2XA01IA337 1 20010820 A 3350 0341516 FUSE AEROSP ATR42 ATR42320 8680930 EU CABIN BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14833 188 IAH- DURING POST FLIGHT INSPECTION THE CREW NOTED THAT THE AISLE PATH LIGHT IN THE LEFT REAR OF THE CABIN FAILED TO ILL UMINATE. IAH- MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT FUSE, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOT ED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SARVICE. 2 H 7 2 4T RT A53EU 2001083100160 20010831 00160 NM 2001 8 31 01FDEA00770 1 20010827 A 3233 FITTING BOEING 727 7272D4 138407U NM MLG ACTUATOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 MLG ACTUATOR SUPPORT FITTING COMMON TO 348.2 BULKHEAD CRACKED. REMOVED AND REPLACED FITTING PER MM 32-33-011-4 & SRM 51- 30-2. 2 L 7 3 4F A3WE 2001082700046 20010827 00046 NM 2001 8 27 UPS01236683 1 20010823 A 2920 BACH8C08NN0290 HYDRAULIC LINE BOEING 727 72727C 138400J NM HYDRAULIC SYS LEAKING A IPXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 907UP 19118 INSPECTION TYPE:N/A SHORTLY AFTER TAKEOFF SYSTEM B ELECTRIC SYSTEM LOW PRESSURE LIGHT ILLUMINATED. SYSTEM B QTY INDICATE D 0. EMERGENCY CHECKLISTS ACCOMPLISHED AND LANDING WAS UNEVENTFUL. FOUND OUTLET LINE OF NR 2 B PUMP LEAKING. PERFORMED A N INTERIM HOSE REPAIR PER GMM 3-24-1. SERVICED HYDRAULICS AND CKD PSI AND LK CKD NORM (TEMP FLEX LINES INSTALLED AND SEC URED) DEFERRED INTERIM HOSE REPAIR PER GMM CHAPTER 3. 2 L 7 3 4F A3WE 2001082700047 20010827 00047 NM 2001 8 27 UPS01236687 1 20010810 A 5320 STRAP BOEING 727 72727C 138400J NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 908UP 19114 INSPECTION TYPE:C ON NDT INSP, CRACK INDICATION FOUND IN REINFORCING STRAP OF MID GALLEY DOOR CUTOUT FWD UPPER CORNER. REPAIR CARRIED OUT PER UPS EO B727-5330-2695 APPENDIX 8.2 2 L 7 3 4F A3WE 2001100900045 20011009 00045 NM 2001 10 9 UPS01236693 1 20010823 A 2720 CONTROL UNIT BOEING 727 72730C 1384009 NM RUDDER MALFUNCTIONED A IPXA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 SO 01 918UP 19008 WITH RUDDER TRIMMED TO ZERO 12 DEGREE LEFT AILERON REQUIRED TO HOLD WINGS LEVEL DEPLOYING SPEED BRAKE SLIGHTLY FIXES PRO BLEM. INSPECTED SPOILERS NO DEFECTS FOUND INSPECTED FLIGHT CONTROLS GEN MX PRACTICES 27-00-00 PAGE 201, 203 NO DEFE CT FOUND HOWEVER SUSPECT FUEL INBALANCE READING SAME DIP STICKS DIFFER BY TWO INCHES FURTHER T/S REQUIRED REFERENCE D 222078. 2 L 7 3 4F A3WE 2001082700051 20010827 00051 NM 2001 8 27 UPS01636435 1 20010730 A 2130 4203651 VALVE BOEING 767 767300 1385204 NM A/C BAY FAILED A IPXA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 01 311UP 27741 INSPECTION TYPE:ETOP AT FL350 CABIN ALT STARTED TO CLIMB AND SHORTLY THEREAFTER, THE RT PACK WENT OFFLINE WITH ASSOCIATE D "FLT DECK SUP FLOW" MSG. FOLLOWED QRH AND SWITCHED PRESSURIZATION TO MANUAL. WITH OUTFLOW VALVE CLOSED CABIN WAS STILL CLIMBING. EMERGENCY DESCENT TO 10,000 FT INITIATED. R&R OVER RIDE VALVE PER MM21-58-20 OP CHECK NORMAL PN, 420365-1 SN OFF 1231A ON 1453A 2 L 7 2 4F RT A1NM 2001082700054 20010827 00054 WP 2001 8 27 UPS01836409 1 20010727 A 2750 CYLINDER DOUG DC8 DC871F 302199D WP T/E FLAP LACK OF LUBE A IPXA K NONE F FLT CONT AFFECTED TO TAKEOFF 1 SO 01 748UP 45948 INSPECTION TYPE:N/A AIRCRAFT TURNS HARD LEFT DURING TAXI AND T/O. WHEN FLAPS ARE LOWERED ACFT BANKS LEFT 10 DEGREES. VIS UALLY INSPECTED FLAP MECHANISM, NO DEFECTS NOTED T/S PER MM 27-50-00. FOUND OUTBOARD LOCK CYLINDER LOW, SERVICED AND BLE D PER MM 27-51-10. FLAPS OPS CKD OK. 2 L 7 4 4F RT 4A25 2001082700055 20010827 00055 WP 2001 8 27 RRXA003573 1 20010105 A 5730 PANEL DOUG DC8 DC871F 302199D WP RT WING CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RIGHT WING T/E PANEL LWR FROM STA XRS 5 TO XRS 98, DAMAGE EXCEE DED LIMITATIONS IAW DC-8 SRM. 2 L 7 4 4F RT 4A25 2001082700056 20010827 00056 WP 2001 8 27 RRXA003594 1 20010106 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE UNDER RT LONGERON 24 SUPPORT FITTING AT STA 920 RT W/W Y-920 X-66, DAM AGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATD REPAIR AND INSTALLED IAW EO 00-316 WITH APPROVED 8110-3 DATED 12/12/00. 2 L 7 4 4F RT 4A25 2001082700057 20010827 00057 WP 2001 8 27 UPS01836521 1 20010720 A 5753 FITTING DOUG DC8 DC871F 302199D WP T/E FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C1/3 LT WING FLAP HINGE SUPPORT FITTING XF 409.6673 INBOARD CRACKED AS MARKED. REMOVED FLAP LEADING EDGE S I/B & O/B OF FLAP HINGE FITTING TO FOM. LOCATED & DRILLED NEW BASE FITTING. INSTALLED BUSHINGS, INSTALLED SPRING COVER , TRACK BASE FITTING COVER PLATES LEADING EDGE ATTACH ANGLES, FLAP FAIRING ATTACH ANGLE & LEADING EDGES IAW DC8 SRM 510D , 51. 2 L 7 4 4F RT 4A25 2001082700063 20010827 00063 WP 2001 8 27 UPS01836531 1 20010806 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:IN LEADING EDGE CRACKED O/B OF NR 3 ENGINE. CRACK LOWER RT LEADING EDGE JUST OUTBD NR 3 ENG, BELOW INBD FIRE BOTTLE ACCESS DOOR. COMING FROM SCREW HOLE APPROX 1/2 INCH LONG. VIS AND PAGE PEN INSP CONFIRMS CRACK APPROX 1/2 IN CH AS NOTED. HFEC CONFIRMS CRACK, INTERIM REPAIR PERFORMED IAW UPS EO DC8 5720-4087-B STEP THRU A (1) (C). 2 L 7 4 4F RT 4A25 2001082700067 20010827 00067 WP 2001 8 27 UPS01836560 1 20010809 A 5610 SLIDING WINDOW DOUG DC8 DC871F 302199D WP COCKPIT LEAKING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:IN FOUND F/O'S SLIDING WINDOW LEAKING AIR AT TOP APPROX MID POSITION OF SEAL. APPROX 1/2 PSID. REMOVED & REPLACED RT SLIDING WINDOW IAW MM 56-10-03. 2 L 7 4 4F RT 4A25 2001082700070 20010827 00070 WP 2001 8 27 UPS01836561 1 20010809 A 5230 SKIN DOUG DC8 DC873F 302199F WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:IN 2 ADJACENT CRACKS AND DISTORTION IN PIT 31 DOOR LOWER EDGE NR 1 PIT DOOR HAS 2 CRACKS IN LOWER SKIN A PPROX 14 INCHES FROM TRAILING EDGE. TRIMMED OUT DAMAGED SKIN ENCOMPASSING BOTH CRACKS AND INSTALLED NEW FASTENER, PER EO DC8-5230-14302. 2 L 7 4 4F RT 4A25 2001082700073 20010827 00073 WP 2001 8 27 UPS01836564 1 20010713 A 5330 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C1/3 REPLACE FUSELAGE AFT CENTER SECTION INTERNAL DOUBLER FROM FS 1100-1260 L27R-L33L (CORROSION). REMOV ED INTERNAL DOUBLER IAW DC8 SRM 51-1-24. TRIM NEW DOUBLER LOCATE AND DRILL EXISTING FASTENER HOLES IAW DC8 SRM 51-1-24 A ND INSTALL INTERNAL DOUBLER IAW DC8 SRM 51-1-20D & 51-1-21. 2 L 7 4 4F RT 4A25 2001082700077 20010827 00077 WP 2001 8 27 UPS01836568 1 20010716 A 5320 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C1/3 AFT CARGO CROSS SLIDE DOOR JAM T FITTING 3 (EA) HAS CORROSION UNDERNEATH CASTING. REMOVED CORROSION MAT'L OUT OF LIMITS IAW DC8 SRM 53-2-0. RECEIVED NEW FITTING (2 EACH) P/N 3755772-501 TORQUE BOX LATCH ASSY LOCATED AND DRILLED HOLES IAW DC8 SRM 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001082700080 20010827 00080 WP 2001 8 27 UPS01836569 1 20010718 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C1/3 AFT PIT FS 1300 AT L36 FRAME IS CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 SRM 5 3-2-0. FABRICATED -49 REPAIR STRAP IAW DC8 SRM 53-2-0. INSTALLED -49 REPAIR STRAP IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001082700083 20010827 00083 WP 2001 8 27 UPS01836570 1 20010712 A 5320 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C1/3 AFT PIT FS 1220 L32R-L33R ZEE FITTING HAS CORROSION. REMOVED CORROSION IAW DC8 SRM 51-1-8. FOUND MA T'L OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED FITTING IAW DC8 SRM 51-1-20D. RECEIVED NEW FITTING P/N 3755840-1 LOCATED A ND DRILLED HOLES IAW DC8 SRM 51-1-24 AND INSTALLED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001082700086 20010827 00086 WP 2001 8 27 UPS01836579 1 20010810 A 2611 BATTERY DOUG DC8 DC873F 302199F WP SMOKE DETECTOR DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:IN LOWER FWD BELLY SMOKE DETECTOR INOP. REMOVED AND REPLACED BATTERIES IN SMOKE DETECTOR UNIT S/N 4706 P ERFORMED CHECK AS PER M/M 26-18-01 OPS CHECK NORMAL. 2 L 7 4 4F RT 4A25 2001082700088 20010827 00088 WP 2001 8 27 UPS01836581 1 20010805 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 RIGHT WING CENTER L/E. UPPER RIB IS CRACKED AT XFS 379. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001082700090 20010827 00090 WP 2001 8 27 UPS01836582 1 20010805 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 RIGHT WING L/E. LOWER RIB IS CRACKED AT XFS 778.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001082700091 20010827 00091 WP 2001 8 27 UPS01836583 1 20010805 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 RIGHT WING L/E. LOWER SKIN IS CRACKED AT XFS 841.25. REPAIRED SKIN IAW DC8-5720-7767-A. 2 L 7 4 4F RT 4A25 2001082700093 20010827 00093 WP 2001 8 27 UPS01836584 1 20010805 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 RIGHT WING L/E. LOWER RIBS ARE CRACKED AT XFS 791.25,XFS 797.5, XFS 803.75. REPAIRED RIBS IAW SRM 5 7-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001082700096 20010827 00096 WP 2001 8 27 UPS01836585 1 20010801 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 LEFT WING L/E. LOWER SKIN IS CRACKED AT XFS 572.5. REPAIRED SKIN IAW DC8-5720-4087-B. 2 L 7 4 4F RT 4A25 2001082700097 20010827 00097 WP 2001 8 27 UPS01836586 1 20010805 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 RIGHT WING L/E SKIN IS CRACKED 2 PLACES AT XW 485. REPAIRED SKIN IAW DC8-5720-7767-A, AND SRM 57-2- 1 FIG 2H. 2 L 7 4 4F RT 4A25 2001082700099 20010827 00099 WP 2001 8 27 UPS01836587 1 20010805 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 RIGHT WING L/E LOWER SKIN IS CRACKED AT XFS 597.5. REPAIRED SKIN IAW DC8-5720-7767-A. 2 L 7 4 4F RT 4A25 2001082700101 20010827 00101 WP 2001 8 27 UPS01836588 1 20010805 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 LEFT WING L/E RIB IS CRACKED AT XFS 585. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001082700102 20010827 00102 WP 2001 8 27 UPS01836589 1 20010805 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 LEFT WING L/E RIB IS CRACKED AT XFS 760. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001082700104 20010827 00104 WP 2001 8 27 UPS01836590 1 20010805 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 RIGHT WING L/E LOWER RIBS ARE CRACKED AT XFS 822.5, XFS 828.75. REPAIRED RIBS IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001082700106 20010827 00106 WP 2001 8 27 UPS01836591 1 20010805 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 LEFT WING L/E RIB IS CRACKED AT XFS 615. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001082700108 20010827 00108 WP 2001 8 27 UPS01836592 1 20010805 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 329. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001082700111 20010827 00111 WP 2001 8 27 UPS01836593 1 20010805 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 RIGHT WING L/E SKIN IS CRACKED AT XFS 878. REPAIRED SKIN IAW SRM 57-2-1 FIG 2B. 2 L 7 4 4F RT 4A25 2001082700114 20010827 00114 WP 2001 8 27 UPS01836594 1 20010801 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 LEFT WING L/E UPPER SKIN HAS SCREWS PULLING THRU SKIN AT XFS 883. REPAIRED SKIN IAW SRM 57-2-1 FIG 2H. 2 L 7 4 4F RT 4A25 2001082700115 20010827 00115 WP 2001 8 27 UPS01836595 1 20010802 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 LEFT WING L/E LOWER RIB IS CRACKED AT XRS 162. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001082700117 20010827 00117 WP 2001 8 27 UPS01836596 1 20010805 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 RIGHT WING L/E LOWER RIB IS CRACKED AT XFS 603. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001082700118 20010827 00118 WP 2001 8 27 UPS01836597 1 20010806 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 797.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001082700120 20010827 00120 WP 2001 8 27 UPS01836598 1 20010804 A 5730 576960039 DOUBLER DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 LEFT WING L/E INTERNAL DOUBLER IS CRACKED AT XW 485. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769600, AND SRM 51-1-21,51-1-21A. 2 L 7 4 4F RT 4A25 2001082700122 20010827 00122 WP 2001 8 27 UPS01836599 1 20010805 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 772.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001082700125 20010827 00125 WP 2001 8 27 UPS01836600 1 20010805 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 RIGHT WING L/E UPPER SKIN IS CRACKED AT XFS 710. REPAIRED SKIN IAW DC8-5720-7767-A. 2 L 7 4 4F RT 4A25 2001082700126 20010827 00126 WP 2001 8 27 UPS01836601 1 20010805 A 5754 576993322 DOUBLER DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 RIGHT WING OB SLOT VANE INTERNAL DOUBLER IS CRACKED AT XS 520. REMOVED, FABRICATED, AND REPLACED DO UBLER IAW DWG 5769933, AND SRM 51-1-21,51-1-21A. 2 L 7 4 4F RT 4A25 2001082700129 20010827 00129 WP 2001 8 27 UPS01836602 1 20010801 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 LEFT WING L/E LOWER SKIN IS CRACKED AT XFS 635. REPAIRED SKIN IAW DC8-5720-4087-B. 2 L 7 4 4F RT 4A25 2001082700132 20010827 00132 WP 2001 8 27 UPS01836603 1 20010713 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C1/3 REPLACE FUSELAGE AFT CENTER SECTION EXTERIOR SKIN FROM FS 1050-1350 L31R-L31L DUE TO CORROSION. REMOVED AFT BELLY SKIN FROM FS 1050-1350. TRIM NEW SKIN LOCATE DRILL EXISTING FASTENER HOLES AND COUNTERSINK HOLES IAW DC8 SRM 51-1-24. INSTALL NEW SKIN IAW DC8 SRM 51-1-20D & 51-1-21. 2 L 7 4 4F RT 4A25 2001082700135 20010827 00135 WP 2001 8 27 UPS01836606 1 20010814 A 5753 FLAP DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:PFLT LEFT WING INBOARD FLAP HAS A CRACK ON INBOARD TRAILING EDGE NEXT TO FUSELAGE AND BENT. REMOVED PREV IOUS SKIN REPAIR. REPAIRED IN REF SRM 57-20-0. 2 L 7 4 4F RT 4A25 2001082700136 20010827 00136 WP 2001 8 27 UPS01836607 1 20010813 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:PFLT EMERGENCY LIGHTS INOP. R/R EMERGENCY LIGHTS BATTERY PACK. OPS CKS GOOD AT THIS TIME. 2 L 7 4 4F RT 4A25 2001082700139 20010827 00139 WP 2001 8 27 UPS01836615 1 20010804 A 5320 4750418U1 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 STA 1160 LONG 19R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 475 0418, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001082700141 20010827 00141 WP 2001 8 27 UPS01836616 1 20010806 A 5320 37797621N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 STA 680-700 LONG 8L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779762, AND SRM 5 1-1-20D. 2 L 7 4 4F RT 4A25 2001082700144 20010827 00144 WP 2001 8 27 UPS01836617 1 20010806 A 5320 47516402 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 STA 822 LONG 18R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4751 640, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001082700146 20010827 00146 WP 2001 8 27 UPS01836618 1 20010806 A 5320 3754041501N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 STA 320 BANANA FITTING IS CRACKED AT LONG 26L. REMOVED AND REPLACED FITTING IAW DWG 3754041, AND SR M 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001082700149 20010827 00149 WP 2001 8 27 UPS01836619 1 20010808 A 5313 564932743 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 STA 1770 LONG 17L IS CRACKED. REMOVED, FABRICATED, AND REPLACED LONGERON IAW DWG 5649327, AND SRM 5 1-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001082700151 20010827 00151 WP 2001 8 27 UPS01836620 1 20010806 A 5320 37794982 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 STA 857 LONG 18L INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779 498, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001082700152 20010827 00152 WP 2001 8 27 UPS01836621 1 20010807 A 5320 37552222 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 STA 822 FLOORBEAM ATTACH FITTING IS CRACKED AT LBL 24. REMOVED AND REPLACED FITTING IAW DWG 3755222 , AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001082700153 20010827 00153 WP 2001 8 27 UPS01836623 1 20010808 A 5320 4772397U1 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 STA 1770 LONG 17L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397, AND SRM 51- 1-20D, AND 51-1-21. 2 L 7 4 4F RT 4A25 2001082700154 20010827 00154 WP 2001 8 27 UPS01836624 1 20010806 A 5320 3779762U1 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 STA 680-700 LONG 7L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779762, AND SRM 5 1-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001082700155 20010827 00155 WP 2001 8 27 UPS01836625 1 20010805 A 5711 580273631 DOUBLER DOUG DC8 DC873F 302199F WP RT WING SPAR BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 RIGHT WING LOWER FRONT SPAR HAS DOUBLER BROKEN AT XS 520. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW SRM 57-2-1 FIG 14A, AND DWG 5802736. 2 L 7 4 4F RT 4A25 2001082700156 20010827 00156 WP 2001 8 27 UPS01836626 1 20010803 A 5711 SPAR CAP DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 RIGHT WING REAR SPAR LOWER CAP IS CRACKED AT XCW 0. REPAIRED SPAR IAW 8110-3 APPROVED DK SK 809-649 . 2 L 7 4 4F RT 4A25 2001082700157 20010827 00157 WP 2001 8 27 UPS01836627 1 20010801 A 5720 46495971N FITTING DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 LEFT WING T/E SUPPORT FITTING IS CRACKED OUTBOARD SIDE OF FLAP HINGE 410 CANOE FITTING. REMOVED AND REPLACED FITTING IAW DWG 4649597, AND SRM 51-1-20D, 51-3-0. 2 L 7 4 4F RT 4A25 2001082700158 20010827 00158 WP 2001 8 27 UPS01836628 1 20010801 A 5312 PRESSURE PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 RIGHT MLG WHEEL WELL IB. BULKHEAD SUPPORT WEB IS CRACKED STA 879 RBL 4. REPAIRED WEB IAW SRM 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 2001082700159 20010827 00159 WP 2001 8 27 UPS01836631 1 20010805 A 5320 5755032 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 STA 1710 RBL 10, MAIN CABIN FLOOR SUPPORT IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLA CED FLOOR SUPPORT IAW DWG 5755032. 2 L 7 4 4F RT 4A25 2001082700160 20010827 00160 WP 2001 8 27 UPS01836632 1 20010805 A 5512 SKIN DOUG DC8 DC873F 302199F WP HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 RT HORIZ STAB L/E LOWER SKIN IS CORRODED BEYOND LIMITS AT XFS 178. REPAIRED SKIN IAW SRM 55-2-1 FIG 4. 2 L 7 4 4F RT 4A25 2001082700162 20010827 00162 WP 2001 8 27 UPS01836633 1 20010805 A 5512 SKIN DOUG DC8 DC873F 302199F WP HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 LT HORIZ STAB L/E UPPER SKIN IS CORRODED BEYOND LIMITS AT XFS 178. REPAIRED SKIN IAW SRM 55-2-1 FIG 4. 2 L 7 4 4F RT 4A25 2001082700163 20010827 00163 WP 2001 8 27 UPS01836635 1 20010806 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 STA 1735 LONG 15L IS CRACKED. REPAIRED LONGERON IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2001082700164 20010827 00164 WP 2001 8 27 UPS01836636 1 20010806 A 5320 38877991 SPLICE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 STA 440-460 LONG 17L, SPLICE FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 3887799, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001082700165 20010827 00165 WP 2001 8 27 UPS01836637 1 20010805 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 410.25. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001082700166 20010827 00166 WP 2001 8 27 UPS01836638 1 20010805 A 5730 DOUBLER DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 RIGHT WING L/E NR 3 STUBWING LOWER DOUBLER IS CRACKED AT OPENING ABOVE PYLON CUTOUT. REMOVED, FABRI CATED, AND REPLACED REPAIR DOUBLER IAW SRM 57-2-1A. 2 L 7 4 4F RT 4A25 2001082700168 20010827 00168 WP 2001 8 27 UPS01836639 1 20010806 A 5320 5750540502 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 STA 660-680 LONG 11L END FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 5750 540, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001082700169 20010827 00169 WP 2001 8 27 UPS01836640 1 20010807 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 LEFT WING L/E UPPER SKIN IS CRACKED AT XFS 666.25. REPAIRED SKIN IAW SRM 57-2-1 FIG 38. 2 L 7 4 4F RT 4A25 2001082700170 20010827 00170 WP 2001 8 27 UPS01836641 1 20010808 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1,3 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 722.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001082700171 20010827 00171 WP 2001 8 27 UPS01836642 1 20010808 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 835.75, XFS 853.75. REPAIRED RIBS IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001082700172 20010827 00172 WP 2001 8 27 UPS01836644 1 20010808 A 5754 577013821 ANGLE DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 LEFT WING L/E IB SLOT VANE IB ATTACH ANGLE IS CRACKED AT XILD .7095. REMOVED, FABRICATED, AND REPLA CED ANGLE IAW DWG 5770138, AND SRM 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 2001082700173 20010827 00173 WP 2001 8 27 AALA016077 1 20010725 A 3350 4096043 LAMP DOUG DC9 DC982 3022082 WP TAIL CONE INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 821RA 49931 CCI-RNO - EMERGENCY LIGHT AT TAIL CONE INOPERATIVE. REMOVED AND REPLACED LAMP. OPS NORMAL. (M) 2 L 7 2 4F A6WE 2001082700174 20010827 00174 NM 2001 8 27 USAA010980 1 20010806 A 5300 FRAME BOEING 757 757225 1384959 NM BS 1520 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 54141 22198 CLT - FOUND FRAME DENTED .5 INCH IN DIAMETER, STATION 1520 ABOVE STRINGER 26L. REPAIR DOUBLER INSTALLED PER EA 69860. (M) 2 L 7 2 4F RT A2NM 2001082700175 20010827 00175 NM 2001 8 27 USAA010986 1 20010806 A 5300 FRAME BOEING 757 757225 1384959 NM BS 1540 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 54141 22198 CLT - FOUND FRAME DENTED .5 INCH, BS 1540 AT S26L. DOUBLER INSTALLED PER EA NR 69860. (M) 2 L 7 2 4F RT A2NM 2001082700176 20010827 00176 NM 2001 8 27 USAA010983 1 20010806 A 5300 FRAME BOEING 757 757225 1384959 NM BS 1540 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 54141 22198 CLT - FOUND FRAME DENTED 1 INCH DIAMETER, BS 1540 2 INCH BELOW STRINGER 25R. REPAIR DOUBLER INSTALLED PER EA NR 69860 A ND TR 53-60-01A. (M) 2 L 7 2 4F RT A2NM 2001082700177 20010827 00177 NM 2001 8 27 USAA010988 1 20010806 A 5300 FRAME BOEING 757 757225 1384959 NM BS 1580 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 54141 22198 CLT - FOUND FRAME CRACKED .5 INCH, STATION 1580. DOUBLER INSTALLED PER EA 69860. (M) 2 L 7 2 4F RT A2NM 2001082700178 20010827 00178 NM 2001 8 27 USAA010981 1 20010806 A 5300 FRAME BOEING 757 757225 1384959 NM BS 1620 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 54141 22198 CLT - FOUND FRAME DENTED .5 INCH IN DIAMETER, STATION 1620 BETWEEN SR 25L AND 26L. DOUBLER INSTALLED PER EA 69860. (M) 2 L 7 2 4F RT A2NM 2001082700179 20010827 00179 NM 2001 8 27 USAA010982 1 20010806 A 5300 FRAME BOEING 757 757225 1384959 NM BS 660 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 54141 22198 CLT - FOUND FRAME DENTED .5 INCH BY .125 INCH DEEP, BS 660 AT S23L. REPAIR DOUBLER INSTALLED PER EA 69873. (M) 2 L 7 2 4F RT A2NM 2001082700180 20010827 00180 NM 2001 8 27 USAA010985 1 20010806 A 5300 FRAME BOEING 757 757225 1384959 NM BS 560 GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 54141 22198 CLT - FOUND FRAME GOUGED .125 INCH, BS 560 AT S22 LEFT. DOUBLER INSTALLED PER EA NR 85030. (M) 2 L 7 2 4F RT A2NM 2001082700181 20010827 00181 NM 2001 8 27 USAA010984 1 20010806 A 5300 FRAME BOEING 757 757225 1384959 NM BS 560 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 54141 22198 CLT - FOUND FRAME DENTED APPROX .5 INCH BY .125 INCH DEEP, BS 560 AT S24L. INSTALLED DOUBLER PER EA 85030. (M) 2 L 7 2 4F RT A2NM 2001082700182 20010827 00182 NM 2001 8 27 USAA010977 1 20010806 A 5310 FRAME BOEING 757 757225 1384959 NM BS 540 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 54141 22198 CLT - FOUND FRAME DENTED APPROX .5 INCH WIDE BY .125 INCH DEEP, STATION 540 AT S24L. REPAIRED DOUBLER PER EA 85029. (M ) 2 L 7 2 4F RT A2NM 2001082700183 20010827 00183 NM 2001 8 27 USAA010976 1 20010806 A 5330 SKIN BOEING 757 757225 1384959 NM BS 750 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND FUSELAGE SKIN WITH 1 INCH DIAMETER CUTOUT, PREVIOUSLY INSTALLED REPAIR, STATION 750 AND S25L. DOUBLER REMOV ED, INSTALLED NEW DOUBLER WITH RETAINED OLD FILLER PER SRM 53-00-01 FIG 203 AND EA 85084. (M) 2 L 7 2 4F RT A2NM 2001082700184 20010827 00184 NM 2001 8 27 USAA010964 1 20010723 A 5300 SKIN BOEING 757 7572B7 1384964 NM BS 740 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 632AU 22219 27810 CLT - FOUND SKIN DENTED APPROX 3 INCHES BY 6 INCHES, BS 740 PLUS 1 INCH, BETWEEN S15R AND S16R. INSTALLED DOUBLER PER E A 85087. (M) 2 L 7 2 4F RT A2NM 2001082700185 20010827 00185 NM 2001 8 27 USAA010991 1 20010806 A 5400 STRUT BOEING 757 757225 1384959 NM CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 54142 22198 CLT - FOUND STRUT CRACKED 1.5 INCH, NR 2 PYLON INER CHORD FITTING AT LOWER INBOARD FASTENER HOLE. REPLACED NR 2 PYLON P ER EA 85062, BOEING REPAIR NR 6-1171-RE-989. (M) 2 L 7 2 4F RT A2NM 2001082700186 20010827 00186 NM 2001 8 27 USAABB01081 1 20010813 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 619AU 27198 BOS - FOUND FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE AT ROW 4. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2001082700187 20010827 00187 NM 2001 8 27 USAASB01193 1 20010705 A 5200 BAC1521522 SEAL BOEING 737 7374B7 1384702 NM FWD ENTRY DOOR LEAKING A USAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 781AU 25020 MSY - FLT 429 - EN ROUTE FROM CLT-MSY, 140 NAUTICAL MILES AWAY FROM MSY AT FL350, THE CREW REPORTED A CABIN PRESSURIZATI ON LOSS WITH THE CABIN ALTITUDE WARNING HORN SOUNDING. CAPTAIN DESCENDED FLIGHT TO FL130 WHERE THE CABIN STABILIZED AT CABIN ALTITUDE OF 10,000 FEET. NO OXYGEN MASKS WERE DEPLOYED. CAPTAIN DECLARED AN EMERGENCY FOR PRIORITY HANDLING AS T HUNDERSTORMS WERE IN THE MSY AREA. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MX FOUND THE FORWARD ENTRY DOOR SEAL, TORN AND LEAKING AT THE LOWER RT CORNER. REPAIRED SEAL ON FWD ENTRY DOOR AND PROGRAMMED FOR REPLACMENT. PRESSURIZED AIRCRAF T AND PERFORMED LEAKAGE RATE CHECK PER MM 05-51-91. LEAKAGE RATE WITHIN LIMITS. (M) 2 L 7 2 4F RT A16WE 2001082700188 20010827 00188 NM 2001 8 27 USAASB01201 1 20010715 A 5200 BAC1521522 SEAL BOEING 737 7374B7 1384702 NM FWD ENTRY DOOR FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 445US 24863 CLT - FLT 1157 - SHORTLY AFTER TAKEOFF FROM CLT, EN ROUTE TO PBI, THE CABIN DEPRESSURIZED AT ABOUT 4,500 FEET. AIR WAS REPORTEDLY LEAKING FROM THE FORWARD MAIN ENTRY DOOR. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDEN T. NO OXYGEN MASKS WERE DEPLOYED AND NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE FORWARD ENTRY DOO R ASSIST SPRING PER MM 52-11-41. ALSO, REMOVED AND REPLACED FORWARD ENTRY DOOR SEAL. REMOVED AND REINSTALLED SAME DOOR ASSEMBLY PER JOB CARD. PRESSURIZED AIRCRAFT. PRESSURIZATION CHECKS GOOD. (M) 2 L 7 2 4F RT A16WE 2001082700189 20010827 00189 NM 2001 8 27 USAA010950 1 20010728 A 5300 SKIN BOEING 737 7374B7 1384702 NM A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 441US 30772 24812 PIT - FOUND SKIN WITH OVAL WEAR MARK, .071 INCH .375 INCH DIAMETER, RIGHT A/C BAY ABOVE ACM VALVE CENTER TANK LOWER SKIN . REAMED DAMAGE TO .25 INCH DIAMETER, INSTALLED FASTENER SAME SIZE AS HOLE PER EA 71719. (M) 2 L 7 2 4F RT A16WE 2001082700190 20010827 00190 NM 2001 8 27 USAA010949 1 20010725 A 5500 ELEVATOR BOEING 737 7374B7 1384702 NM A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 441US 30772 24812 PIT - FOUND ELEVATOR HAS CARBON DELAMINATION, .040 INCH DEEP BY .25 INCH DIAMETER, BOTTOM SIDE OF ELEVATOR 52 INCHES FRO M BOTTOM END. REPAIR PER SRM 55-20-1 AND 51-70-17 PER EA 71791. (M) 2 L 7 2 4F RT A16WE 2001082700191 20010827 00191 NM 2001 8 27 USAA010953 1 20010730 A 5300 BULKHEAD BOEING 737 7374B7 1384702 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 33083 24552 PIT - FOUND BULKHEAD WITH THREE CRACKS 1 INCH EACH, BS 178 LBL/RBL 6 INCHES BELOW WL 207 AND BL0 WL 184. CUT OUT DAMAGE D AREAS, INSTALLED DOUBLER AND FILLERS PER EO 5300V153. (M) 2 L 7 2 4F RT A16WE 2001120700018 20011207 00018 NM 2001 12 7 TSAA0124102 1 20011116 A 2420 941D3352 CIRCUIT BREAKER BOEING 737 7372S5C 1384499 NM COCKPIT FAULTY A TSAA O OTHER O OTHER CR CRUISE 1 WP 13 802AL 22148 FLT 950 - HNL-ITO - AFTER TAKEOFF DURING FLIGHT, THE NR 2 THRUST REVERSER AND NR 2 AFT FUEL PUMP CIRCUIT BREAKERS POPPED /TRIPPED. RESET NORMAL AND AFTER SEVERAL MINUTES THE SAME CIRCUIT BREAKERS POPPED/TRIPPED AGAIN. THE AIRCRAFT RETURNED TO HNL WITH NO FURTHER INCIDENT. REPLACED THE NR 2 GENERATOR CONTROL CIRCUIT BREAKER. OPS CHECK SYSTEM OK. OK FOR SE RVICE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001082700192 20010827 00192 NM 2001 8 27 TSAA0133108 1 20010809 A 3350 86210066 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN INOPERATIVE A K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 REPLACED NR 6 EMERGENCY FLOOR BATTERY PACKS DUE TO INOPERATIVE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2001082700193 20010827 00193 NM 2001 8 27 TSAA0133106 1 20010814 A 3300 86210066 BATTERY PACK BOEING 737 73725A 1384481 NM CABIN INOPERATIVE A TSAA O OTHER O OTHER IN INSP/MAINT 1 WP 13 819AL 23791 REPLACED NR 6 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001082700194 20010827 00194 WP 2001 8 27 UPS01836645 1 20010811 A 5320 3754473501 SPLICE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 STA 1260-1280 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754473, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001082700195 20010827 00195 WP 2001 8 27 UPS01836646 1 20010809 A 5511 RIB DOUG DC8 DC873F 302199F WP HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 RT HORIZONTAL STAB L/E UPPER RIB IS CRACKED AT XFS 88. REPAIRED RIB IAW SRM 55-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001082700197 20010827 00197 WP 2001 8 27 UPS01836647 1 20010808 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 RIGHT WING L/E RIB IS CRACKED AT XFS 304. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001082700200 20010827 00200 WP 2001 8 27 UPS01836648 1 20010807 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 LEFT WING L/E UPPER SKIN IS CRACKED AT XFS 316.5 AND HAS A ELONGATED HOLE AT XFS 329. REPAIRED SKIN IAW 8110-3 APPROVED DH SK 866-235. 2 L 7 4 4F RT 4A25 2001082700203 20010827 00203 WP 2001 8 27 UPS01836649 1 20010808 A 5730 576958991 DOUBLER DOUG DC8 DC873F 302199F WP RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 RIGHT WING L/E INTERNAL DOUBLER IS CORRODED BEYOND LIMITS AT XFS 366.5. REMOVED, FABRICATED, AND RE PLACED DOUBLER IAW DWG 5769589, AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001082700207 20010827 00207 WP 2001 8 27 UPS01836650 1 20010809 A 5320 561229865 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 COCKPIT SUBFLOOR FINGER DOUBLER IS CORRODED BEYOND LIMITS AT STA -25 TO -8 LBL 69. REMOVED, FABRICA TED, AND REPLACED DOUBLER IAW DWG 5612298, AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001082700209 20010827 00209 WP 2001 8 27 UPS01836651 1 20010808 A 5751 5764617U51 PANEL DOUG DC8 DC873F 302199F WP LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 LEFT WING OUTBOARD AILERON INBD WEIGHTED PANEL IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED WEIG HTED PANEL IAW DWG 5764617, AND SRM 57-1-0, 51-3-0. 2 L 7 4 4F RT 4A25 2001082700211 20010827 00211 WP 2001 8 27 UPS01836654 1 20010808 A 5730 576958929 DOUBLER DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 LEFT WING L/E INTERNAL DOUBLER IS CRACKED AT XW 257. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769589, AND SRM 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 2001082700212 20010827 00212 WP 2001 8 27 UPS01836682 1 20010817 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:N/A EMERG LIGHTS INOP. REMOVED AND REPLACED EMERG LIGHT BATTERY PACK. OPS CHECKS GOOD. 2 L 7 4 4F RT 4A25 2001082700213 20010827 00213 WP 2001 8 27 UPS01836691 1 20010808 A 5320 4772397U1 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 STA 1770 LONG 17R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397, AND SRM 51- 1-20D. 2 L 7 4 4F RT 4A25 2001082700214 20010827 00214 WP 2001 8 27 UPS01836692 1 20010814 A 5320 37552221 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 STA 742 RBL 24 FLOORBEAM ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755222, A ND DWG 51-1-20D. 2 L 7 4 4F RT 4A25 2001092400203 20010924 00203 WP 2001 9 24 UPS01836694 1 20010823 A 2740 179894 COMPENSATOR DOUG DC8 DC873F 302199F WP HORIZ STAB FAULTY A IPXA K NONE F FLT CONT AFFECTED NR NOT REPORTED 1 SO 01 801UP 46101 INSPECTION TYPE:N/A PIREP-EXCESSIVE PITCH TRIM STAB INOP. FOUND PTC ACTUATOR EXTENDED WITH POWER REMOVED. INDICATES AFTE R LIFT OFF THE ACFT REQUIRES 1 TO 2 UNITS NOSE DOWN 16 TRIM. REPLACED PITCH TRIM COMPENSATOR ACTUATOR IAW 27-30-06 OPS C K GOOD. 2 L 7 4 4F RT 4A25 2001082700217 20010827 00217 WP 2001 8 27 UPS01836695 1 20010806 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 STA 35 FRAME IS CRACKED AT LONG 24R. REPAIRED FRAME IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001082700220 20010827 00220 WP 2001 8 27 UPS01836696 1 20010808 A 5313 S16167574800 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 STA 1770 LONG 17R IS CRACKED. REMOVED, FABRICATED, AND REPLACED LONGERON IAW DWG S1616757, AND SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001082700223 20010827 00223 WP 2001 8 27 UPS01836697 1 20010806 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 STA 1260-1280 LONG 35R IS CRACKED. REPAIRED LONGERON IAW 8110-3 APPROVED DH SK 809-818. 2 L 7 4 4F RT 4A25 2001082700225 20010827 00225 WP 2001 8 27 UPS01836698 1 20010806 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 STA 1260-1280 LONG 34R IS CRACKED. REPAIRED LONGERON IAW 8110-3 APPROVED DH SK 809-819. 2 L 7 4 4F RT 4A25 2001082700234 20010827 00234 WP 2001 8 27 2001F00215 1 20010729 A 3350 9721050 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 826US 48026 IND - ON LOW LEVEL EMERGENCY LIGHT AND THE LEFT AND RIGHT EXIT PATH LIGHTS A PASSENGER SEAT ROW 19 WERE INOPERATIVE. MA INTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. REF USAAD01140. (M) 2 L 7 2 4F A6WE 2001082700235 20010827 00235 NM 2001 8 27 2001F00216 1 20010808 A 3260 SENSOR BOEING 737 7372K5 138448X NM LANDING GEAR OUT OF ADJ A EGEF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 231TA 22596 GUA - FLT 970 - LANDING GEAR LEVER GOT STUCK IN THE OFF POSITION AFTER TAKEOFF, IT TOOK SEVERAL TRIES TO BRING LANDING G EAR UP, IT OCCURRED AFTER TAKEOFF IN FLIGHT FROM SJO TO GUA. ADJUSTED LANDING GEAR SAFETY SENSOR TO CORRECT GAP, AS PER AMM 32-09-200 AND PERFORMED SEVERAL LANDING GEAR EXTENSIONS/RETRACTIONS INCLUDING MANUAL EXTENSION, OPERATION WAS NORMA L AS PER AMM 32-32-0 AND 32-33-0. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001082700237 20010827 00237 WP 2001 8 27 RRXA010050 1 20010610 A 7931 41822044 TRANSMITTER DOUG DC8 DC873F 302199F WP OIL PRESSURE FAILED A RRXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 15 795FT 46103 REJECTED T/O AT DAY, GREATER 60 KTS, NR 2 OIL PRESSURE GAUGE SHOWED AT LEAST 15 PSI HIGHER THAN OTHERS, AND APPEARED TO CONTINUE TO CLIMB. REMOVED AND REPLACED NR 2 ENGINE OIL PRESSURE TRANSMITTER IAW M/M 79-32-1. OPS CHECKS GOOD IAW M/M 71-00-00. 2 L 7 4 4F RT 4A25 2001082700238 20010827 00238 2001 8 27 RRXA010051 4 20010613 A 3421 GYRO DOUG DC8 DC873F 302199F WP COCKPIT FAILED A RRXA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 15 792FT 46046 F/OS GYRO FAILED ON CLIMB IN BOTH NORMAL AND AUX POSITION. REPLACED EXISTING HARNESS IAW 34-2-2 WITH NEW WIRE F/R50-11 9 FORWARD OF FO'S PANEL BACK TO R50-61 RADIO RACK SHELF NR 3 OPERATIONAL CK I/A/W DC8 M.M CHAP 34-25-0 (CK GOOD) 2 L 7 4 4F RT 4A25 2001082700239 20010827 00239 WP 2001 8 27 RRXA010053 1 20010621 A 5280 ACG7060501 LINK DOUG DC10 DC1010F 3022111 WP NLG DOOR FAILED A RRXA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 15 68044 46903 AFTER LANDING GEAR RETRACTION, VERY NOTICEABLE VIBRATION FROM FRONT PART OF ACFT. INCREASED VIBRATION WITH SPEED INCREAS E. LOWERED LANDING GEAR, VIBRATION STILL PRESENT. LANDING GEAR OPERATION NORMAL. FOUND BAD NOSE GEAR DOOR DRIVE LIN K. REMOVED AND REPLACED NOSE GEAR DOOR DRIVE LINK IAW DC-10 MM 32-36-01 PG 201. CYCLED DOOR SEVERAL TIMES ON GROUND, OPS CHECK NORMAL. 2 L 7 3 4F A22WE 2001082700240 20010827 00240 WP 2001 8 27 RRXA010054 1 20010623 A 2760 10111042 ACCUMULATOR DOUG DC8 DC871F 302199D WP SPOILER FAILED A RRXA O OTHER J WARNING INDICATION CR CRUISE 1 WP 15 8085U 45975 SPOILER PUMP INOP. FOUND SPOILER ACCUMULATOR BLADDER BLOWN AND SPOILER RESERVIOR EMPTY. REMOVED AND REPLACED SPOILER ACCUMULATOR AND SERVICED SPOILER RESERVOIR IAW MM 29-12-02. SPOILER PUMP OP CK GOOD IAW M/M 27-63-25. 2 L 7 4 4F RT 4A25 2001082700241 20010827 00241 WP 2001 8 27 RRXA010055 1 20010627 A 2612 WARNING SYSTEM DOUG DC8 DC871 302199A WP NR 1 ENGINE ACTIVATED A RRXA F E A ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 15 811AL 46099 JUST PRIOR TO STARTING APPROACH EXPERIENCE FIRE WARNING ON NR 1 ENGINE FOLLOWED QRH. SHUT DOWN ENGINE AND BOTH BOTTLES F IRED. REPAIRED DAMAGED WIRING AT P10-7000 TO AFT FIRE LOOP ON NR 1 ENGINE IAW DC-8 M/M 20-50-1. CK'D ALL WIRING AND F IRE LOOPS ON NR 1 ENGINE. ALL CHECKED GOOD & FIRE WARNING SYS OPS CKS GOOD IAW DC-8 M/M 26-10-0 & 26-10-1. NO DEFECTS NO TED. 2 L 7 4 4F 4A25 2001082700242 20010827 00242 WP 2001 8 27 RRXA010056 1 20010627 A 3240 37038375 PAD DOUG DC8 DC873F 302199F WP SPIN BRAKES FAILED A RRXA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 15 831AL 46146 ON DEPARTURE GEAR HANDLE UP NOSE GEAR HAD EXTREME NO ISE AS IF NOSE WHEELS WERE SPINNING AND RUBBING. ALSO HAD EXTREME V IBRATION, GEAR HANDLE PUT BACK DOWN, VIBRATION CONTINUED WITH GEAR DOWN, WHEN ACFT BANKED IN FLT NOSE GEAR HAD LOUD BAN G. BOTH GEAR UP INDICATIONS AND GEAR DOWN INDICATIONS WERE NORMAL. REMOVED AND REPLACED 8 EA NOSE WHEEL SPIN BRAKE PADS IAW DC-8 MM 32-40-3. JACKED AND RETRACTED NLG, OPS CK NORMAL IAW DC-8 MM 32-30-0. INSPECTED NLG WHEEL WELL AND NLG ST RUT AND TIRES NO DEFECTS NOTED 2 L 7 4 4F RT 4A25 2001082700243 20010827 00243 WP 2001 8 27 RRXA010057 1 20010629 A 5720 FAIRING DOUG DC10 DC1030F 3023504 WP WING DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 47816 47816 UPON WALKAROUND, DISCOVERED DAMAGE TO WING FILLET FAIRING. PERFORMED TEMPORARY REPAIR PER BOECOM EAF-IND-01- 00059H. I NSTALLED EXTERNAL DOUBLER AND COVERED WITH SPEED TAPE. TAPE TO BE INSPECTED EACH FLIGHT. 2 L 7 3 4F RT A22WE 2001082700244 20010827 00244 WP 2001 8 27 RRXA010059 1 20010719 A 3510 BOTTLE DOUG DC8 DC871F 302199D WP CREW OXYGEN LEAKING A RRXA K NONE L NO TEST IN INSP/MAINT 1 WP 15 997GE 45667 AFTER SERVICING OXYGEN OF UPPER CREW BOTTLE - BOTTLE WAS INSTALLED & DURING TURN ON AT BOTTLE OXYGEN LINE & REGULATOR RUPTURED & CAUSED FLASH FIRE "A" PIT OXYGEN BOTTLE AREA. INSPECTED PURGED AND LEAK CHECKED CREW OXYGEN SYSTEM IAW OPS 4.901 AND TEST DRAWING 7649000 WORK PROCEDURE RECORDED ON JAC EMERY 358-001. R&R CREWS OXYGEN REGULATOR IAW DC-8 MM 35- 10-4. NOTED LEAK CHECK. R&R LINE TO CREWS OXYGEN IAW DC-8 MM 20-12-0 & 20-13 -0 NEED LEAK CHECK. 2 L 7 4 4F RT 4A25 2001082700245 20010827 00245 2001 8 27 RRXA010060 4 20010809 A 3421 2587733512 GYRO DOUG DC8 DC873F 302199F WP COCKPIT FAILED A RRXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 961R 46133 CAPT'S VG FAILURE AFTER TAKEOFF. R&R CAPT'S VG IAW DC8 MM 34-25-0. OPS CHECKS GOOD.REMOVED & REPLACED CAPTS. ADI SYSTEM CHECKS GOOD IAW DC-8 MM 34-25-0 NO DEFECTS NOTED 2 L 7 4 4F RT 4A25 2001082700246 20010827 00246 NE 2001 8 27 RRXA010061 2 20010725 A 7200 ENGINE DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE NR 4 FLAMED OUT A RRXA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 WP 15 8076U 45941 NR 4 ENGINE IN FLIGHT FLAME OUT 35000. IAW UAL M/M 71-00-40 PGS 201-206 POWER LOSS/FLAME- OUT INVESTIGATED & CHECKED THE FOLLOWING: ENGINE INLET/ EXHAUST, CHIP DETECTORS, MAIN FUEL PUMP, FUEL CTRL.,NR 3 ENGINE FUEL BOOST PUMP, IGNITOR, FUEL QTY CHECKED LINE LEAKAGE CHECKED. NR 4 MAIN AND NR 4 ALT FUEL SELECTORS CHECKED, SUMPED ALL TANKS FOR WATER/ DEBRIS. F OUND NOT DISCREPANCYS. PERFORMED MAX POWER RUN IAW EWA JRH,FOUND ALL PARAMETERS NORMAL. 2 L 7 4 4F 4 F RT 4A25 E2GL 2001082700247 20010827 00247 WP 2001 8 27 RRXA010062 1 20010804 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP CARGO BAY DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8084U 45974 UPPER DECK CARGO FLOOR AT STA 781, 30 AND TO THE RT HAS A HOLE. REPAIRED GOUGE IN FLOOR PANEL IAW DC-8 SRM 53-2-3 FI G 6. 2 L 7 4 4F RT 4A25 2001082700248 20010827 00248 WP 2001 8 27 RRXA010063 1 20010804 A 5751 STRUCTURE DOUG DC10 DC1030F 3023504 WP LT ELEVATOR TORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 833LA 46937 LT INBOARD ELEVATOR TRAILING EDGE CAP TORN, 4 IN. BY 2 IN. AREA. REPAIRED PER DC-10 SRM 55-30-00 P2-P4, ELEVATOR TRAILI NG EDGE REPAIRS PER 55-30-00, TRAIL EDGE REPAIR P 1,3. A6. 2 L 7 3 4F RT A22WE 2001082700249 20010827 00249 WP 2001 8 27 RRXA010064 1 20010807 A 7722 65003003 INDICATOR DOUG DC8 DC871F 302199D WP NR 1 ENGINE FAILED A RRXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 8084U 45974 NR 1 EGT REACHED 907 DEGREES C FOR APPROX 8 SEC ON MAX POWER T/O. 92 PERCENT N2 & 28 DEGREES C OAT AT DAY. FOUND NR 1 ENGINE EGT INDICATOR READS 24-34 DEGREES HIGH. NO DEFECTS ON HARNESS R&R NR 1 EGT INICATOR 077-20-1, CK GOOD WITH TEST SET, ENGINE RUN REQUIRED. SEE LOG BOOK 00211-01 ITEM 2. NR 1 ENGINE EGT INDICATOR OPERATES NORMAL ON ENGINE RUN, DC-8 M/M 71-00. 2 L 7 4 4F RT 4A25 2001082700250 20010827 00250 WP 2001 8 27 RRXA010503 1 20010218 A 5755 SKIN DOUG DC8 DC871F 302199D WP NR 2 SPOILER BROKEN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A BROKEN CORNER OF NR 2 GROUND SPOILER BAY ON LT WING NOT SPOILER, DAMAGE EXCEEDED LIMI TATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57 -2-0 FIG.4. 2 L 7 4 4F RT 4A25 2001082700251 20010827 00251 WP 2001 8 27 RRXA010506 1 20010222 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND DISCOLORATION TO THE SKIN ON INSIDE TANK AT LT LWR WING FUEL VENT BOX UPPER SKIN BETWEE N STRINGERS NR 1 & 2, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRI CATED PART AND INSTALLED IAW E.O.#01-024 WITH APPROVED 8110-3 DATED 01/31/01. 2 L 7 4 4F RT 4A25 2001082700255 20010827 00255 WP 2001 8 27 RRXA010515 1 20010207 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND ELONGATED SCREW HOLES ON THE LWR I/B T/E AT STA XFS 7.500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-26 AND DC-8 SRM 51-1-14 AND DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001082700256 20010827 00256 WP 2001 8 27 RRXA010516 1 20010207 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A 1 1/2 INCH CRACK AND (2) DENTS TO THE SKIN TOP I/B AT STA XFS 141.250 TO 147.5, DAMAG E EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 55-2-1. 2 L 7 4 4F RT 4A25 2001082700257 20010827 00257 WP 2001 8 27 RRXA010522 1 20010207 A 5740 FITTING DOUG DC8 DC871F 302199D WP LT WING CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A PITTED CANOE FITTING UNDER FLAP ROLLER TRACKS LT WING AT STA 219, DAMAGE EXCEEDED LIM ITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM E .O.#01-024 WITH APPROVED 8110-3 DATED 02/09/01. 2 L 7 4 4F RT 4A25 2001082700258 20010827 00258 WP 2001 8 27 RRXA010523 1 20010207 A 5740 FITTING DOUG DC8 DC871F 302199D WP LT WING CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A PITTED CANOE FITTING UNDER FLAP ROLLER TRACKS LT WING AT STA 340, DAMAGE EXCEEDED LIM ITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.#01-02 4 WITH APPROVED 8110-3 DATED 02/09/01. 2 L 7 4 4F RT 4A25 2001082700259 20010827 00259 WP 2001 8 27 RRXA010524 1 20010207 A 5740 FITTING DOUG DC8 DC871F 302199D WP LT WING CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A PITTED CANOE FITTING UNDER FLAP ROLLER TRACKS LT WING AT STA 410, DAMAGE EXCEEDED LIM ITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.01-024 WITH APPROVED 8110-3 DATED 02/09/01. 2 L 7 4 4F RT 4A25 2001082700260 20010827 00260 WP 2001 8 27 RRXA010526 1 20010207 A 5740 FITTING DOUG DC8 DC871F 302199D WP RT WING CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A PITTED CANOE FITTING UNDER FLAP ROLLER TRACKS ON THE RT WING AT STA 340, DAMAGE EXCEE DED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O .01-024 WITH APPROVED 8110-3 DATED 02/09/01. 2 L 7 4 4F RT 4A25 2001082700261 20010827 00261 WP 2001 8 27 RRXA010527 1 20010207 A 5740 FITTING DOUG DC8 DC871F 302199D WP RT WING CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A PITTED CANOE FITTING UNDER ROLLER TRACKS ON THE RT WING AT STA 98, DAMAGE EXCEEDED LI MITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. 01-0 24 WITH APPROVED 8110-3 DATED 02/09/01. 2 L 7 4 4F RT 4A25 2001082700262 20010827 00262 WP 2001 8 27 RRXA010528 1 20010208 A 5330 PANEL DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AROUND PARAMETER OF THE BOTTOM PANEL BELOW LT STRESS PANEL, DAMAGE EXC EEDED LIMITATIONS IAW DC-8 SRM. 2 L 7 4 4F RT 4A25 2001082700263 20010827 00263 WP 2001 8 27 RRXA010530 1 20010206 A 5740 FITTING DOUG DC8 DC871F 302199D WP WING GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A GOUGE TO THE AFT END OF THE CANOE FITTING AT STA 219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. 2 L 7 4 4F RT 4A25 2001082700264 20010827 00264 NE 2001 8 27 2001F00219 2 20010722 A 7320 714810 VALVE BOEING 727 72751C 1384015 NM PWA JT8 JT8D7B 52053 NE NR 1 ENGINE INOPERATIVE A RYNA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION AP APPROACH 1 CE 07 413EX 19206 ON APPROACH, AFTER THROTTLES WERE RETARDED, NR 1 ENGINE SPOOLED DOWN AS NORMAL. WHEN POWER WAS APPLIED, NR 1 ENGINE FAI LED TO SPOOL UP. AFTER LANDING, NR 1 THROTTLE WAS CYCLED BACK AND FORTH WITH N1, N2 OR FUEL FLOW. ENGINE HAD SHUT DOWN . NR 1 GENERATOR THAN TRIPPED OFF LINE. REMOVED AND REPLACED NR 1 P/D VALVE AND LOCK WASHER. ENGINE RUN AND LEAK CHEC KED. (M) 2 L 7 3 4F 4 F A3WE E2EA 2001082700265 20010827 00265 NM 2001 8 27 2001F00220 1 20010704 A 2910 6517840409 HYDRAULIC LINE BOEING 727 72782C 1384026 NM LT WING LEAKING A RYNA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 CE 07 528PC 19597 TOTAL LOSS OF A SYSTEM HYDRAULICS. COMPLIED WITH EMERGENCY CHECKLIST OF HYDRAULIC SYSTEM FAILURE. EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED SPOILER PRESSURE LINE AND RETURN LINE IN LEFT WING. SERVICED W ITH SKYDROL. OPERATIONAL AND LEAK CHECK GOOD. (M) 2 L 7 3 4F A3WE 2001082700266 20010827 00266 NM 2001 8 27 2001F00221 1 20010704 A 2910 6517840411 HYDRAULIC LINE BOEING 727 72782C 1384026 NM LT WING LEAKING A RYNA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 CE 07 528PC 19597 TOTAL LOSS OF A SYSTEM HYDRAULICS. COMPLIED WITH EMERGENCY CHECKLIST OF HYDRAULIC SYSTEM FAILURE. EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED SPOILER PRESSURE LINE AND RETURN LINE IN LEFT WING. SERVICED W ITH SKYDROL. OPERATIONAL AND LEAK CHECK GOOD. (M) 2 L 7 3 4F A3WE 2001082700267 20010827 00267 NM 2001 8 27 2001F00222 1 20010725 A 5311 65B01718520 FRAME BOEING 747 7472D3B 1384805 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 506MC 73880 21252 DURING INSPECTION FOUND FRAME WEB CRACKED AT BS 500, STRINGER 9L AND STRINGER 8 TO 10AR. STOP DRILLED ALL CRACKS. FABR ICATED REPLACEMENT DOUBLERS. INSTALLED DOUBLER AT STRINGER 9L LOCATION AND AT STRINGER 8 TO 10AR LOCATION PER STANDARD PRACTICES OF THE SRM. (M) 2 L 7 4 4F RT A20WE 2001082700268 20010827 00268 WP 2001 8 27 2001F00223 1 20010712 A 5320 2403110100145 ANGLE CVAC 240 24027 2422642 WP NLG WW CRACKED A JRAA K NONE O OTHER IN INSP/MAINT 1 GL 11 152JR 283 A CRACK WAS DISCOVERED IN THE NOSE GEAR WHEEL WELL BEAM ANGLE IN THE PROCESS OF PERFORMING A PREFLIGHT INSPECTION ON THE AIRCRAFT. REPAIRS ARE TO BE AFFECTED IAW FAA APPROVED REPAIR, DATED 12/24/54, IAW SRM SECTION 2, PAGE 203, AND 204. ( M) 2 L 7 2 4R A793 2001082700269 20010827 00269 WP 2001 8 27 2001F00224 1 20010712 A 5320 2403110100145 ANGLE CVAC 240 24027 2422642 WP NLG WW CRACKED A JRAA K NONE O OTHER IN INSP/MAINT 1 GL 11 152JR 283 A CRACK WAS DISCOVERED IN THE NOSE GEAR WHEEL WELL BEAM ANGLE IN THE PROCESS OF PERFORMING A PREFLIGHT INSPECTION ON THE AIRCRAFT. REPAIRS ARE TO BE AFFECTED IAW FAA APPROVED REPAIR, DATED 12/24/54, IAW SRM SECTION 2 PAGE 203, AND 204. (M ) 2 L 7 2 4R A793 2001082700270 20010827 00270 NE 2001 8 27 2001F00225 2 20010606 A 8500 ENGINE CVAC 340 340CVAC 242270A WP PWA R2800 R2800* 52026 NE NR 2 MALFUNCTIONED A JRAA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. A FLAME/FIRE IN INSP/MAINT 1 GL 11 157JR 284 DURING AN ATTEMPT TO PERFORM A MAINTENANCE RUN ON THE NR 2 ENGINE, THE ENGINE BECAME FLOODED AND BACKFIRED, RESULTING IN A MINOR COWLING FIRE. THE TECHNICIAN THEN PERFORMED AN EMERGENCY SHUT DOWN, AND PULLED THE T-HANDLE FOR THE NR 2 ENGIN E, FOLLOWED BY THE ACTIVATION OF THE NR 2 ENGINE FIRE BOTTLE. THE SUPPORTING GROUND 'FIRE GUARD', THEN FOLLOWED UP WITH THE ACTIVATION OF AN ADDITIONAL GROUND STAND BY FIRE BOTTLE TO ASSURE THE EXTINGUISHING OF THE FIRE. THE FIRE WAS EXTI NGUISHED WITH NO RESULTING DAMAGE TO THE ENGINE, ENGINE WIRING, ACCESSORIES, OR ANY OTHER COMPONENTS ON, OR WITHIN THE E NGINE COWLING. (M) 2 L 7 2 4R 4 R 6A6 5E8 2001082700271 20010827 00271 NM 2001 8 27 0102866307 1 20010815 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 667US 24222 DURING LINE CHECK (PEK), FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE BETWEEN SEAT ROWS 16L-18L. REPAIRED LIGHTING. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001082700272 20010827 00272 NM 2001 8 27 0102876637 1 20010806 A 3320 LIGHT BOEING 747 747251B 1384892 NM L1 DOOR OVERHEATED A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 637 23548 DURING FLIGHT, ATTENDANT LIGHT AT PASSENGER DOOR 1L OVERHEATED AND SMOKE WAS OBSERVED. VISUAL INSPECTION AND OPERATIONA L CHECK NORMAL. 2 L 7 4 4F A20WE 2001082700273 20010827 00273 NM 2001 8 27 0102892768 1 20010813 A 3233 LINE BOEING 727 7272B7 138407L NM RT MLG RUPTURED A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 728RW 21741 ON TAKEOFF A-SYSTEM HYDRAULIC FLUID LOSS AT ROTATION. THE RIGHT MAIN GEAR WOULD NOT RETRACT. CREW FOLLOWED COM PROCEDU RE AND MANUALLY EXTENDED THE RIGHT GEAR. FLIGHT RETURNED TO SLC AND MADE AN UNEVENTFUL LANDING. MAINTENANCE REPLACED R UPTURED RETRACT ACTUATOR FLEX LINE ON RIGHT MAIN LANDING GEAR. LEAK AND OPERATIONAL CHECK GOOD. 2 L 7 3 4F A3WE 2001082700274 20010827 00274 WP 2001 8 27 0102929871 1 20010812 A 2170 17946081 SEPARATOR DOUG DC9 DC951 3022051 WP A/C BAY SEPARATED A NWAA B EMER. DESCENT O OTHER CR CRUISE 1 GL 01 780NC 48102 AIRCRAFT LOST CABIN PRESSURIZATION DURING CRUISE AT 31,000 FEET. CREW FOLLOWED COM PROCEDURE AND EMERGENCY DESCENDED TO 10,000 FEET. CABIN CLIMBED 700-800 FPM WITH THROTTLES AT IDLE. CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTEN ANCE FOUND WATER SEPARATOR CANISTER SEPARATED. REPLACED THE LEFT WATER SEPARATOR. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2001082700275 20010827 00275 WP 2001 8 27 0102941228 1 20010818 A 5280 BOLT DOUG DC10 DC1030 3023501 WP LT MLG DOOR BACKED OUT A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 228NW 46578 ON WALKAROUND, FOUND LEFT MAIN LANDING GEAR DOOR EXTENDED. SUBSEQUENT INSPECTION FOUND SUPPORT BOLT IN MAIN LANDING GEA R SIDE BRACE ATTACH FITTING BACKING OUT. REMOVED, INSPECTED, AND REINSTALLED SIDE BRACE ATTACH FITTING WITH NEW BOLTS A ND BARREL NUTS. OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 2001082700276 20010827 00276 NM 2001 8 27 0102952275 1 20010817 A 2421 GENERATOR BOEING 727 727251 138408H NM NR 3 ENGINE MALFUNCTIONED A NWAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 01 275US 21154 DURING TAKEOFF AT 110 KTS, THE NR 3 GENERATOR BREAKER TRIPPED FOLLOWED BY NR 1 AND NR 2 BUSS TIE BREAKER LIGHTS. TAKEOF F WAS ABORTED AT APPROXIMATELY 120 KTS. CREW FOLLOWED COM PROCEDURE AND RESET ALL CIRCUIT BREAKERS, TRANSFORMER RECTIFI ERS, AND BUSS TIE BREAKERS WITH NO ANNUNCIATOR OR PARALLEL LIGHTS ILLUMINATING. MSP MAINTENANCE REPLACED CSD AND GENER ATOR. LEAK AND OPERATIONAL CHECK NORMAL. 2 L 7 3 4F A3WE 2001082700277 20010827 00277 NM 2001 8 27 0102966634 1 20010814 A 2120 DUCT BOEING 747 747227B 1384888 NM CABIN LEAKING A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 634US 22234 DURING CLIMB, (AMS) WATER LEAKING IN THE AREA OF SEAT 10J AND AN ELECTRICAL SMELL EMITTED AROUND DOOR 3L. TURNED OFF GA LLEY POWER AND SMELL DISSIPATED. AIRCRAFT RETURNED TO AMS AND LANDED WITHOUT INCIDENT. REPLACED AIR CONDITIONING DUCT ABOVE SEAT 10J AND OPERATIONALLY CHECKED ELECTRICAL SYSTEM TO DETERMINE SOURCE OF SMELL WITH NO FAULTS FOUND. OPERATION AL CHECK GOOD. 2 L 7 4 4F A20WE 2001082700278 20010827 00278 NM 2001 8 27 0102976308 1 20010816 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 668US 24223 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT ROW 1L, 4L, 51L, 66R, 21-31L AT LAV 2R, DOOR 4R, AND AT AFT GALLEY. REPAIRED WIRING AT 66 AND 4 AND RECONNECTED WIRING AT 21. RELAMPED AND REPLACED LIGHT FIXTURES. OP ERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001082700279 20010827 00279 NM 2001 8 27 0102986310 1 20010821 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 670US 24227 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE AT SEAT 9R, BETWEEN SEATS 2-4L, 26-31R, 51-65R, AND AT LAVATORY DOOR 2R. RESEATED ELECTRICAL CONNECTORS. REPLACED LIGHT ASSEMBLIES AND LAMPS AS REQUIRED. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001082700280 20010827 00280 NM 2001 8 27 0102996302 1 20010821 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN DAMAGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 662US 23720 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE BETWEEN SEAT ROWS 30-39R, 26-41L, 10-21R, AND AT LAV ATORY DOOR 4R2. REPAIRED WIRING AND RESEATED ELECTRICAL CONNECTORS. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001082700281 20010827 00281 NM 2001 8 27 0103006309 1 20010818 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 669US 24224 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT ROW 35 AND AT ROW 52R. REPLACED LAMPS, OPERATION AL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001082700282 20010827 00282 NM 2001 8 27 0103016306 1 20010817 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 666US 23821 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT PASSENGER DOOR 1L. RECONNECTED WIRING, OPERATION AL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001083100159 20010831 00159 NM 2001 8 31 01FDEA00767 1 20010824 A 5310 SHEAR TIE BOEING 727 7272D4 138407U NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 CORROSION C53-113-01(1) ON FRAME BS 720 LBL 4 TO RBL 4 WL 149 AFT SIDE OF FRAME. REMOVED AND REPLACED SHEAR TIE 51-30-2 , 51-31-000-2, 51-20-1, 51-20-021-7, 51-20-031-7. 2 L 7 3 4F A3WE 2001082700283 20010827 00283 WP 2001 8 27 01FDEA00768 1 20010824 A 3260 WARNING SYSTEM DOUG DC10 DC1010 3022110 WP COCKPIT MALFUNCTIONED A FDEA K NONE N FALSE WARNING CL CLIMB 1 SO 25 389FE 46623 RT MAIN GEAR INDICATED ON RETRACTION, RECYCLED GEAR, WORKED OK, INDICATION ON BOTH FRONT AND REAR PANELS. PERFORMED TES T AT PROX BOX PER MM 32-61-01-2 CK GOOD. INSPECTED RT MLG, PROX SW AND TARGET, CK OK FOR SERVICE. 2 L 7 3 4F A22WE 2001082700284 20010827 00284 EU 2001 8 27 01FDEA00769 1 20010824 A 2610 CONTROLLER AIRBUS 310 A310 EU FIRE PROTECTION MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 408FE 257 PDIS WRI 26-12-5025 AT ABOUT 1500 AFT MAIN DECK CARGO LOOP-A ILLUMINATED, FOLLOWED BY LOOP-B AND RED SMOKE LIGHT & ECAM FIRE WARNING. DECLARED EMER AND RETURNED TO LAND. REMOVED AND REPLACED AFT UPPER CARGO SMOKE DETECTION CONTROLLER AND TESTED PER MM 26-19-00. RAN BOTH ENGINES AND RAN A/C PACK SYS USING BLEED AIR. NO SMOKE OR ODOR NOTED IN CABIN, PER JR H SMOKE DETECTION SYS SHOWED NO FAULTS. 2 L 7 2 4F RT A35EU 2001082700285 20010827 00285 2001 8 27 ARWA0010810 4 20010822 A 3442 WIRE DOUG DC8 DC863 302198A WP WX RADAR DAMAGED A ARWA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 345JW 46042 NR 1 WEATHER RADAR INOP AFTER TAKEOFF. AIRCRAFT RETURN TO KMIA AND LANDED WITHOUT INCIDENT. REPAIRED COAXIAL WIRE ON R ADAR INDICATOR CONNECTOR IAW MM 20-50-1, OPERATIONAL CHECK NORMAL IAW MM 34-41-0. 2 L 7 4 4F 4A25 2001082700286 20010827 00286 WP 2001 8 27 RRXA010532 1 20010202 A 3210 BOSS DOUG DC8 DC871F 302199D WP LT & RT MLG CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION TO THE MLG STRUT ASSY. RETRACT PIN BOSS & RETRACK PIN BY DOING MA-AI-3210-01: 03, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTA LLED IAW MA-A1-3210-01:03 AND E.O#01-024 WITH APPROVED 8110-3 DATED 02/02/01 AND DC-8 S/B 32-102 AND DC-8 MM 32-30-0. 2 L 7 4 4F RT 4A25 2001082700287 20010827 00287 WP 2001 8 27 AT0100225 1 20010715 A 2611 SMOKE DETECTOR DOUG DC9 DC932 3022066 WP CARGO BAY MALFUNCTIONED A ZZDA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 15 824AT 47278 FORWARD CARGO FIRE DETECTOR LIGHT ILLUMINATED WITH THE MASTER CAUTION LIGHT. EMERGENCY WAS DECLARED AND NR 2 FIRE BOTTL E WAS DISCHARGED AND AFT TAIL CONE SLIDE WAS DEPLOYED. INSPECTED THE FORWARD CARGO, E & E, FORWARD CABIN, AND COCKPIT A REAS FOR EVIDENCE OF SMOKE OR OVERHEATED CONDITIONS WITH NO FAULTS FOUND. REPLACED NR 2 FIRE BOTTLE AND SQUIB. REPLACE D ALL SIX FORWARD CARGO COMPARTMENT SMOKE DETECTORS AS PRECAUTIONARY. AFT TAIL CONE SLIDE WAS REPLACED. 2 L 7 2 4F A6WE 2001082700288 20010827 00288 EU 2001 8 27 AWXA0002173 1 20010814 A 5347 D53112092200 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 FR 20 Y765 LT SEAT TRACK CORRODED. REPLACED SEAT TRACK NR 1 FROM FR 16 TO 20 AS PER SRM 53-11-15 PAGE 6. 2 L 7 2 4F RT A28NM 2001082700289 20010827 00289 EU 2001 8 27 AWXA0002174 1 20010814 A 5330 D53112242200 SKIN AIRBUS 320 A320231 3930325 EU FUSELAGE DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 DENT IN FUSELAGE AT FRAME 23 BETWEEN STRINGERS 25L & 24L. REMOVED PREVIOUS REPAIR. FABRICATED AND INSTALLED SKIN DOUBL ER AS PER A320 SRM 53-00-10 FIGURE 203 PAGES 206C TO 208B. 2 L 7 2 4F RT A28NM 2001082700290 20010827 00290 EU 2001 8 27 AWXA0002175 1 20010816 A 5347 D53112091203 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 FR 20 Y-754 RT SEAT TRACK CORRODED. REPLACED SEAT TRACK/FLOOR SUPPORT RAIL AS PER SRM 53-11-14 PG 37 AND DWG D53110858. 2 L 7 2 4F RT A28NM 2001082700291 20010827 00291 EU 2001 8 27 AWXA0002176 1 20010816 A 5320 D53112091203 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 FR 16-20 Y-254 RT FLOOR SUPPORT CORRODED. REPLACED FLOOR SUPPORT RAIL AS PER SRM 53-11-14 PG 37 AND DWG D53110858. 2 L 7 2 4F RT A28NM 2001082700292 20010827 00292 EU 2001 8 27 AWXA0002177 1 20010816 A 5320 D53112087200 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 FR 16-20 Y 254 LT FLOOR SUPPORT CORRODED. REPLACED FLOOR SUPPORT RAIL FROM FR 12 TO 24 AS PER SRM 53-11-14 PG 37, 205-2 10 FIG 8 AND 202. 2 L 7 2 4F RT A28NM 2001082700293 20010827 00293 EU 2001 8 27 AWXA0002178 1 20010817 A 5320 D53112067201 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 FR 20 TO FR 21 Y-1732 RT FLOOR SUPPORT CORRODED. REPAIRED AS PER AWA ER 26-5311-01277DL1. 2 L 7 2 4F RT A28NM 2001082700294 20010827 00294 NM 2001 8 27 AWXA0002180 1 20010815 A 5754 114N3030 SKIN BOEING 757 7572S7 1384962 NM L/E SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 903AW 23323 LT WING NR 2 SLAT CRACKED AT FASTENER HOLE, LWR SURFACE STA 595. CUT OUT DAMAGE PER SRM 51-70-13 FIG 1. FABBED DOUBLER AND SLIMS IAW SRM 57-43-13 FIG 1, INSTALLED REPAIR PARTS PER SRM 51-40-02. 2 L 7 2 4F RT A2NM 2001082700295 20010827 00295 NM 2001 8 27 AWXA0002183 1 20010822 A 5311 111N20073 FRAME BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 903AW 23323 FOUND CORROSION IN THE CONDITIONED AIR BAY AT STA 900 BETWEEN STRINGERS 28 LT AND 28 RT. REMOVED CORRODED SECTION OF LW R CHORD AT STA 900 BETWEEN STR 28 LT & STR RT. FABBED AND INSTALLED REPAIR PARTS PER ER 19-5311-01234-DL3. 2 L 7 2 4F RT A2NM 2001082700298 20010827 00298 SO 2001 8 27 C2XA01CL196 1 20010817 A 3350 LIGHT EMB 145 EMB145ER SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14939 145030 CLE FLIGHT 3638 THE CREW REPORTED EMERGENCY LIGHT AISLE PATH LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGH T STRIP. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001082700299 20010827 00299 SO 2001 8 27 C2XA01CL197 1 20010823 A 2530 CBC16707 CONNECTOR EMB 135 EMB135ER 3260203 SO GALLEY BURNED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 14508 145220 CLE FLIGHT 3692 THE CREW REPORTED A BURNING SMELL IN THE CABIN. MAINTENANCE INSPECTED AND FOUND THE GALLEY HOT JUG RECE PTACLE TO BE BURNT. THE RECEPTACLE CONNECTOR WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001082700300 20010827 00300 NM 2001 8 27 CALA0100765 1 20010822 A 5320 SPLICE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND A .125 INCH CRACK IN STRINGER SPLICE 4L AT STA 907. THE STRINGER SPLICE WAS REMOVED AND REPLACED IAW S RM 51-10-02. 2 L 7 2 4F RT A16WE 2001082700301 20010827 00301 WP 2001 8 27 CALA0100766 1 20010823 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND BELT FRAME CORRODED AT LOWER J IN AFT PIT AT STA 1271 BETWEEN LONGERONS 29R AND 29L. THE BELT FRAME WA S REPAIRED IAW SRM 53-03. 2 L 7 2 4F A6WE 2001082700302 20010827 00302 WP 2001 8 27 CALA0100773 1 20010823 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND FORWARD ENTRY FLOOR PANEL CORRODED AT FS 160-200, LBL 8-44. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5 320-01265. 2 L 7 2 4F A6WE 2001082700303 20010827 00303 NM 2001 8 27 CALA0100780 1 20010823 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 294-312, LBL 12. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001082700304 20010827 00304 2001 8 27 COMA0160627 4 20010820 A 2210 270003 PCU CNDAIR CL600 CL6002B19 EA LT WING FAULTY A COMA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SO 01 917CA 18636 7017 DURING CRUISE FLIGHT THE AUTO PILOT FAILED AT FL28. EXCESSIVE INPUT FORCE WAS REQUIRED FOR AILERON CONTROL, FLIGHT WAS DIVERTED TO IAD AND LANDED SAFELY. REPLACED THE LEFT OUTBOARD SPOILERON POWER CONTROL UNIT. 2 L 7 2 4F RT A21EA 2001082700305 20010827 00305 WP 2001 8 27 CALA0100786 1 20010824 A 5330 SKIN DOUG DC9 DC982 3022082 WP FS 264-285 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND L/H FORWARD FUSELAGE EXTERIOR SKIN DENTED BELOW #2 CABIN WINDOW AT FS 264-285, LONGERON 16-18L. THE DEN TED SECTION OF SKIN WAS REMOVED AND NEW SKIN WAS INSTALLED IAW ECRA 5330-02445 AND SRM 51-30-2. 2 L 7 2 4F A6WE 2001082700306 20010827 00306 WP 2001 8 27 CALA0100787 1 20010824 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 1079-1174 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND CABIN CENTER AND R/H FLOOR PANELS DELAMINATED AT FS 1079-1117 AND R/H FLOOR PANEL DELAMINATED AT FS 111 7-1174. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001082700307 20010827 00307 WP 2001 8 27 CALA0100788 1 20010824 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 826-927 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND R/H CABIN FLOOR PANEL DELAMINATED AT FS 826-864 AND R/H CABIN FLOOR PANEL CRACKED AT FS 889-927. NEW FL OOR PANELS WERE INSTALLED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001082700308 20010827 00308 WP 2001 8 27 CALA0100789 1 20010824 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 1193-1309 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND CABIN R/H FLOOR PANELS DELAMINATED AT FS 1193-1250 AND FS 1250-1309. NEW FLOOR PANELS WERE INSTALLED IA W ECRA 5320-01265. 2 L 7 2 4F A6WE 2001082700309 20010827 00309 WP 2001 8 27 CALA0100791 1 20010824 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 769-826 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND CABIN CENTER AND L/H FLOOR PANELS DELAMINATED AT FS 769-807 AND FS 769-826. A R/H FLOOR PANEL AT FS 769 -807 WAS FOUND TORN AT EDGES. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001082700310 20010827 00310 WP 2001 8 27 CALA0100792 1 20010824 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 1003-1079 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND CABIN CENTER FLOOR PANEL DELAMINATED AT FS 1003-1079. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-012 65. 2 L 7 2 4F A6WE 2001082700311 20010827 00311 WP 2001 8 27 CALA0100793 1 20010824 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 245-390 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND CABIN R/H FLOOR PANEL DELAMINATED AT FS 245-313 AND A CREASE IN FLOOR PANEL AT FS 313-390. NEW FLOOR PA NELS WERE INSTALLED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001082700312 20010827 00312 WP 2001 8 27 CALA0100794 1 20010824 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FWD ENTRY DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND CABIN FORWARD ENTRY FLOOR PANEL DELAMINATED. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001082700313 20010827 00313 WP 2001 8 27 CALA0100797 1 20010825 A 5311 FRAME DOUG DC9 DC982 3022082 WP STA 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND A 2" CRACK IN TAIL COMPARTMENT CANTED FRAME AT STA 1418, L2R AND A 4" CRACK IN FRAME AT L2L. THE CRACKE D SECTION OF FRAME WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-30-5 AND 53-03, FIGURE 32. 2 L 7 2 4F A6WE 2001082700314 20010827 00314 WP 2001 8 27 CALA0100798 1 20010825 A 5311 FRAME DOUG DC9 DC982 3022082 WP STA 1446 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND A 2" CRACK IN TAIL COMPARTMENT CANTED FRAME AT STA 1446, L2L. THE FRAME WAS REMOVED AND REPLACED AT STA 1446 IAW SRM 51-30-2. 2 L 7 2 4F A6WE 2001082700315 20010827 00315 WP 2001 8 27 CALA0100799 1 20010825 A 5310 PAN DOUG DC9 DC982 3022082 WP STA 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND FORWARD BAGGAGE BIN JAMB PAN CORRODED AT MID LOWER EDGE STA 344. A NEW PAN SECTION WAS INSTALLED IAW SR M 53-05, FIGURE 44. 2 L 7 2 4F A6WE 2001082700316 20010827 00316 WP 2001 8 27 CALA0100800 1 20010824 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 160-256 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND FORWARD ENTRY FLOOR PANELS WITH BROKEN AND CORRODED INSERTS AT FS 160-200, LBL 8 TO RBL 6 AND AT FS 200 -256. 2 L 7 2 4F A6WE 2001082700317 20010827 00317 NM 2001 8 27 CALA0100802 1 20010825 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM STA 294 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 294, LBL 28 TO RBL 14. THE CORRODED SECTION OF CHORD WAS CUT OUT AND A NEW SECTION WAS SPLICED IN IAW SRM 53-10-51, FIGURE 205. 2 L 7 2 4F RT A16WE 2001082700318 20010827 00318 NM 2001 8 27 CALA0100803 1 20010826 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM STA 312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND TOP OF FLOORBEAM CORRODED AT STA 312, LBL 24 TO RBL 23. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED A ND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001082700319 20010827 00319 NM 2001 8 27 CALA0100805 1 20010825 A 5320 ANGLE BOEING 737 7373T0 1384582 NM STA 294-312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND FLOOR SUPPORT ANGLE CORRODED AT STA 294-312, RBL 12. A NEW FLOOR SUPPORT ANGLE WAS INSTALLED IAW SRM 51 -10-02. 2 L 7 2 4F RT A16WE 2001082700320 20010827 00320 WP 2001 8 27 CALA0100806 1 20010826 A 3350 252005 FUSE DOUG DC10 DC1030 3023501 WP BATTERY PACK BLOWN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12064 47862 INSPECTION FOUND L-4 AND R-4 DOOR LOWER EXIT LIGHT INOPERATIVE. THE FUSE IN EMERGENCY LIGHT BATTERY PACK U1-165 WAS REMO VED AND REPLACED IAW WDM 33-52-04 AND OPERATION CHECKED GOOD. 2 L 7 3 4F A22WE 2001082700321 20010827 00321 WP 2001 8 27 CALA0100808 1 20010826 A 5347 SEAT TRACK DOUG DC10 DC1030 3023501 WP STA 800-824 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17085 47957 INSPECTION FOUND MAIN DECK SEAT TRACK CORRODED AT X = 107.25 AND Y = 800-824. THE CORRODED SECTION OF SEAT TRACK WAS REM OVED AND A NEW SEAT TRACK SECTION WAS SPLICED IN IAW SRM 53-70-00, FIGURE 1. 2 L 7 3 4F A22WE 2001082700322 20010827 00322 WP 2001 8 27 ZW0A0107502 1 20010825 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9305N 49395 THE CABIN OVERHEAD EMERGENCY LIGHTS ILLUMINATED WHEN POWER WAS REMOVED FROM THE AIRCRAFT. REPLACED THE BATTERY PACK. CH ECK-C 5-7-01 STL. --CLOSED-- 2 L 7 2 4F RT A6WE 2001082700323 20010827 00323 NM 2001 8 27 DHL2001717019 1 20010822 A 5280 HINGE BOEING 727 72723 1384004 NM RT MLG DOOR LOOSE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 A9-CHECK; RT MLG STRUT DOOR FWD HINGE CASTING LOOSE IN DOOR. REMOVED AND REPLACED RT MLG STRUT DOOR IAW B727 MM 32-12-1 1. PERFORMED OPS CHECK ON RT MLG STRUT DOOR IAW B727 MM 32-12-11 & 32-32-0, OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2001082700324 20010827 00324 NM 2001 8 27 DHL2001726005 1 20010823 A 2611 SMOKE DETECTOR BOEING 727 727228 NM CARGO BAY INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 726DH 20409 AFT LOWER CARGO SMOKE DETECTOR INOP. RESET 7110 SMOKE DETECTOR AFT CARGO COMPARTMENT IAW MM SUP 26-16-00. OPS CHECKED N ORMAL. 2 L 7 3 4F A3WE 2001082700325 20010827 00325 2001 8 27 SWAA012182 4 20010801 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED RON CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001082700326 20010827 00326 NM 2001 8 27 SWAA012189 1 20010801 A 2910 65C26091170 HYDRAULIC LINE BOEING 737 7373T5 NM LT MLG LEAKING A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 694SW 23061 AIR TURNBACK, DECLARED EMERGENCY. LOSS OF A-SYSTEM HYDRAULIC PRESSURE. QUANTITY DROPPED TO ZERO AFTER RAISING THE GEAR AND FLAPS. REMOVED AND REPLACED WORN LT MLG ACTUATOR HYD LINE PER MM. 2 L 7 2 4F RT A16WE 2001082700327 20010827 00327 2001 8 27 SWAA012190 4 20010803 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT DOORS OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 063SW 22061 BOTH AFT DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF VIEW. REPOSITIONED EVAC SLIDES PER MM. 2 L 7 2 4F A16WE 2001082700328 20010827 00328 NM 2001 8 27 SWAA012191 1 20010803 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 344SW 24152 EEPLS LOOSE AT OVERWING EXIT. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001082700329 20010827 00329 NM 2001 8 27 SWAA012192 1 20010803 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 394SW 27380 EEPLS LOOSE AND INOP BETWEEN ROWS 13 TO 23. RECONNECTED WIRES AND SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001082700330 20010827 00330 NM 2001 8 27 SWAA012194 1 20010803 A 3350 610478 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED SERVICE CHECK, FOUND BOTH LT & RT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PA CKS PER MM. 2 L 7 2 4F A16WE 2001082700331 20010827 00331 NM 2001 8 27 SWAA012195 1 20010804 A 3350 610478 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2001082700332 20010827 00332 2001 8 27 SWAA012196 4 20010805 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 646SW 28331 FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001082700333 20010827 00333 NM 2001 8 27 SWAA012199 1 20010730 A 5315 6546804 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D-CHECK, FOUND AFT CABIN FLOORBEAM CRACKED AT BS 665, BBL 0. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2001082700334 20010827 00334 NM 2001 8 27 SWAA012201 1 20010802 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD PRESS WEB CRACKED, RBL 15 & WL 207. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 2001082700335 20010827 00335 NM 2001 8 27 SWAA012202 1 20010803 A 5312 6545409 PRESSURE PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED SPECIAL VISIT, FOUND BEADED PRESS WEB CRACKED 2 EA AT BS 663, RBL 38 & LBL 32. REPAIRED PRESS WEB PER SWA T1-253-032. 2 L 7 2 4F RT A16WE 2001082700336 20010827 00336 NM 2001 8 27 SWAA012204 1 20010803 A 5320 10133 TEE CHORD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED SPECIAL VISIT, FOUND T-CHORD CRACKED AT BS 178, LBL 5, WL 185. REPAIRED T-CHORD PER SRM. 2 L 7 2 4F RT A16WE 2001082700337 20010827 00337 NM 2001 8 27 SWAA012205 1 20010805 A 3211 6959886 FITTING BOEING 737 737317 138447P NM LT & RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED SERVICE CHECK, FOUND LT & RT MLG WALKING BEAM HANGER FITTINGS CORRODED. REMOVED AND REPLACED LT & RT H ANGER FITTING'S PER ALM WORK CARDS & MM. 2 L 7 2 4F RT A16WE 2001082700338 20010827 00338 NM 2001 8 27 SWAA012206 1 20010803 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 643SW 27716 EEPLS LOOSE AT OVERWING EXIT. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001082700339 20010827 00339 NM 2001 8 27 SWAA012207 1 20010802 A 3350 65C27093 LIGHT BOEING 737 7373Q8 1384670 NM SERVICE DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D-CHECK, FOUND EMERGENCY EXIT LIGHTS BROKEN AT AFT ENTRY DOOR AND FWD SVC DOOR. REMOVED AND REPLACED E XIT LIGHTS PER MM. 2 L 7 2 4F RT A16WE 2001082700340 20010827 00340 NM 2001 8 27 SWAA012208 1 20010726 A 5315 6546804 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED IN FWD CABIN AT BS 294.5, LBL 11. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2001082700341 20010827 00341 NM 2001 8 27 SWAA012210 1 20010806 A 3350 100033 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 606SW 27926 DURING SCHEDULED SERVICE CHECK, FOUND LT EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001082700342 20010827 00342 NM 2001 8 27 SWAA012211 1 20010806 A 3350 BR9442 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 655WN 28400 DURING SCHEDULED A2 CHECK, FOUND EMERGENCY EVAC SLIDE LIGHT INOP AT FWD F/A STA. RELAMPED EVAC SLIDE LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001082700343 20010827 00343 2001 8 27 SWAA012212 4 20010807 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 AFT ENTRY DOOR EMERGENCY EVAC SLIDE ASSY LOOSE. SECURED AFT ENTRY EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001082700344 20010827 00344 NM 2001 8 27 SWAA012213 1 20010807 A 5753 6573731 FLAP BOEING 737 7372H4 138448C NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED SERVICE CHECK, FOUND RT WING INBOARD T/E FLAP DELAMINATED AT INBOARD EDGE. REPAIRED RT WING T/E AFT FL AP PER SRM. 2 L 7 2 4F A16WE 2001082700345 20010827 00345 NM 2001 8 27 SWAA012214 1 20010806 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 384SW 26590 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKS AT WL 199, LBL 5 & WL 202, RBL 5. REPAIRED FWD BULKHEA D WEB PER SRM. 2 L 7 2 4F RT A16WE 2001082700346 20010827 00346 NM 2001 8 27 SWAA012217 1 20010807 A 2782 6544551 ACTUATOR BOEING 737 7373H4 1384600 NM L/E FLAP FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 645SW 28330 AIR TURNBACK, RT WING L/E FLAP TRANSIT LIGHT ILLUMINATED. REMOVED AND REPLACED NR 3 L/E FLAP ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2001082700347 20010827 00347 NM 2001 8 27 SWAA012218 1 20010807 A 2782 6544551 ACTUATOR BOEING 737 7373A4 1384585 NM L/E FLAP FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 680AA 23505 AIR TURNBACK, RT WING L/E FLAP TRANSIT AND NR 3 L/E DEVICE LIGHTS ILLUMINATED. REMOVED AND REPLACED NR 3 L/E FLAP ACTUA TOR PER MM. 2 L 7 2 4F RT A16WE 2001082700348 20010827 00348 2001 8 27 SWAA012223 4 20010807 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 063SW 22061 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001082700349 20010827 00349 NM 2001 8 27 SWAA012226 1 20010808 A 3350 11583310 LIGHT BOEING 737 7377H4 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 771SA 27879 DURING SCHEDULED SERVICE CHECK, FOUND RT EMERGENCY EXIT WINDOW LIGHT INOP AT ROW 11. REMOVED AND REPLACED EXIT LIGHT AS SY PER MM. 2 L 7 2 4F RT A16WE 2001082700350 20010827 00350 NM 2001 8 27 SWAA012227 1 20010809 A 3350 90083 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED A2 CHECK, FOUND 3 EMERGENCY EXIT CEILING LIGHTS INOP. REMOVED AND REPLACED EXIT LIGHT BATTERY PACKS PE R MM. 2 L 7 2 4F A16WE 2001082700351 20010827 00351 2001 8 27 SWAA012228 4 20010808 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT DOORS OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 605SW 27956 DURING SCHEDULED C1 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF VIEW. REPOSITIONED BO TH EVAC SLIDES PER MM. 2 L 7 2 4F RT A16WE 2001082700352 20010827 00352 2001 8 27 SWAA012230 4 20010808 A 2565 C31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001082700353 20010827 00353 2001 8 27 SWAA012232 4 20010809 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 645SW 28330 FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001082700354 20010827 00354 NM 2001 8 27 SWAA012234 1 20010808 A 2560 65C34691 GIRT BAR BOEING 737 7377H4 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 736SA 27868 FWD ENTRY DOOR EVAC SLIDE GIRT BAR WOULD NOT ALIGN WITH BRACKETS. REPOSITIONED GIRT BAR PER MM. 2 L 7 2 4F RT A16WE 2001082700355 20010827 00355 NM 2001 8 27 SWAA012237 1 20010808 A 5240 6545849 RETAINER BOEING 737 737301 1384611 NM SERVICE DOOR OUT OF POSITION A SWAA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SW 07 659SW 23229 AIR TURNBACK, AFTER TAKEOFF A/C CABIN WOULD NOT PRESSURIZE. F/A REPORTED NOISE FROM AFT SVC DOOR. REPOSITIONED AFT SVC DOOR PRESS SEAL RETAINER PER MM. 2 L 7 2 4F RT A16WE 2001082700356 20010827 00356 2001 8 27 SWAA012238 4 20010809 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REINSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001082700357 20010827 00357 NM 2001 8 27 SWAA012239 1 20010812 A 2560 P2070001 FLASHLIGHT BOEING 737 7373T5 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 696SW 23064 AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2001082700358 20010827 00358 2001 8 27 SWAA012241 4 20010810 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 317WN 24068 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER M M. 2 L 7 2 4F RT A16WE 2001082700359 20010827 00359 2001 8 27 SWAA012242 4 20010811 A 2565 63562101 SLIDE BOEING 737 7377H4 NM SERVICE DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 738CB 27870 AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT AND DEPLOYED. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001082700360 20010827 00360 2001 8 27 SWAA012243 4 20010809 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 624SW 27934 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001082700361 20010827 00361 2001 8 27 SWAA012244 4 20010811 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001082700362 20010827 00362 NM 2001 8 27 SWAA012246 1 20010809 A 3350 65C27093 LIGHT BOEING 737 7373Y0 1384671 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 682SW 23496 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001082700363 20010827 00363 NM 2001 8 27 SWAA012247 1 20010810 A 3350 6556633 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT BOTH OVERWING EXITS. RELAMPED EXIT LIGHTS PER MM. 2 L 7 2 4F A16WE 2001082700364 20010827 00364 NM 2001 8 27 SWAA012249 1 20010809 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 376SW 26584 EMERGENCY EXIT LIGHT LENS FELL OUT AT LT OVERWING EXIT. INSTALLED EXIT LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2001082700365 20010827 00365 NM 2001 8 27 SWAA012250 1 20010810 A 5720 65C26714 STRUCTURE BOEING 737 7375H4 138449D NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED SERVICE CHECK, FOUND LT WING L/E CRACKED NEAR NR 1 KRUEGER FLAP, CRACK IS .4375. REPAIRED L/E PER SWA RA. 2 L 7 2 4F RT A16WE 2001082700366 20010827 00366 NM 2001 8 27 SWAA012251 1 20010710 A 5320 655966425 SPLICE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STR SPLICE PER SR M. 2 L 7 2 4F A16WE 2001082700367 20010827 00367 NM 2001 8 27 SWAA012252 1 20010808 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIPS CORRODED AT STR 26R, BS 727E, BS 767 & BS 787. REMOVED AND REPLACED S TR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001082700368 20010827 00368 NM 2001 8 27 SWAA012254 1 20010810 A 2731 65C308781 TAB BOEING 737 7373Y0 1384671 NM ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 682SW 23496 DURING SCHEDULED C2 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2001082700369 20010827 00369 NM 2001 8 27 SWAA012258 1 20010810 A 3211 6959886 FITTING BOEING 737 7373A4 1384585 NM MLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 680AA 23505 DURING SCHEDULED C1 CHECK, FOUND MLG WALKING BEAM FWD ATTACH HANGER FITTING CRACKED AT WBL 135.5. REMOVED AND REPLACED ATTACH FITTING BY ALM, SWA W/W 10418. 2 L 7 2 4F RT A16WE 2001082700370 20010827 00370 2001 8 27 SWAA012259 4 20010812 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001082700371 20010827 00371 NM 2001 8 27 SWAA012260 1 20010812 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM ENTRY DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 380SW 26587 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001082700372 20010827 00372 NM 2001 8 27 SWAA012261 1 20010812 A 3350 6104781 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT RT OVERWING AND AFT EXTERIOR. REMOVED AND REPLACED EXIT LIGHT BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2001082700373 20010827 00373 NM 2001 8 27 SWAA012263 1 20010812 A 3350 101114 LENS BOEING 737 7375H4 138449D NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 524SW 26566 RT OVERWING EMERGENCY EXIT LIGHT LENS FELL OFF. SECURED EXIT LENS PER MM. 2 L 7 2 4F RT A16WE 2001082700374 20010827 00374 NM 2001 8 27 SWAA012264 1 20010813 A 5753 6546435238 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED PM CHECK, FOUND RT T/E OUTBOARD AFT FLAP DELAMINATED ON INBOARD END, APPROX 11. REMOVED AND REPLACED A FT FLAP PER MM. 2 L 7 2 4F RT A16WE 2001082700375 20010827 00375 NM 2001 8 27 SWAA012268 1 20010811 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 500C & BS 500D, STR 25R. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001082700376 20010827 00376 2001 8 27 SWAA012270 4 20010812 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001082700377 20010827 00377 NM 2001 8 27 SWAA012271 1 20010813 A 2612 100012701 FIRE WARNING BOEING 737 7375H4 138449D NM E/E BAY MALFUNCTIONED A SWAA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 07 521SW 25320 DECLARED EMERGENCY, FWD CARGO FIRE LIGHT ILLUMINATED EN ROUTE TO PHX. THE LIGHT WAS EXTINGUISHED AFTER 30 SEC'S. THE C ARGO SYSTEM WAS ARMED AND THE DISCHARGE BUTTON DEPRESSED. PERFORMED CARGO FIRE SUPPRESSION SYSTEM TEST PER MM AND FOUND NO FAULTS. REMOVED AND REPLACED NR 2 CARGO FIRE BOTTLE FOR COMPANY CONVENIENCE PER MM. NOTE NR 2 CARGO FIRE BOTTLE W AS NOT DISCHARGED. CHANGED ONLY FOR CONVENIENCE. REMOVED FIRE DET CENTRAL CONTROL UNIT PER MM. 2 L 7 2 4F RT A16WE 2001082700378 20010827 00378 NM 2001 8 27 SWAA012272 1 20010809 A 5320 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 519SW 25318 DURING SCHEDULED D-CHECK, FOUND STR TIE CLIP CRACKED AT BS 380, STR 10L. REMOVED AND REPLACED STR TIE CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001082700379 20010827 00379 2001 8 27 SWAA012273 4 20010814 A 2565 D31354 SLIDE BOEING 737 7377H4 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 745SW 29491 FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001082700380 20010827 00380 NM 2001 8 27 SWAA012275 1 20010814 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED A2 CHECK, FOUND EXTERNAL EMERGENCY EXIT LIGHT INOP AT RT AFT FUSELAGE. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001082700381 20010827 00381 NM 2001 8 27 SWAA012277 1 20010813 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM AT BS 987, LBL 17 TO LBL 44.5. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2001082700382 20010827 00382 NM 2001 8 27 SWAA012281 1 20010815 A 3350 610478 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 627SW 27935 DURING SCHEDULED RON, FOUND FWD RT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EXIT LIGHT BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2001082700383 20010827 00383 NM 2001 8 27 SWAA012282 1 20010814 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED C3 CHECK, FOUND EEPLS INOP AT MID AND AFT CABIN. RELAMPED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001082700384 20010827 00384 NM 2001 8 27 SWAA012289 1 20010812 A 5311 963820 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 397SW 27691 DURING SCHEDULED SPECIAL VISIT, FOUND BOTH LT AND RT SIDE CHORDS CRACKED AT BS 178, WL 207-208. REMOVED AND REPLACED BO TH CHORDS PER SWA ACO. 2 L 7 2 4F RT A16WE 2001082700385 20010827 00385 NE 2001 8 27 SWAA012292 2 20010814 A 7230 COMPRESSOR BOEING 737 7375H4 138449D NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE STALLED A SWAA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 07 508SW 24185 723134 AIR TURNBACK, IN-FLIGHT ENG SHUT DOWN, DECLARED EMERGENCY. DURING CLIMB NR 1 ENG ENCOUNTERED 3 COMPRESSOR STALLS WITH-I N 3 MINUTES. AFTER RETURNING TO OAK FOUND PIECES OF METAL INSIDE NR 1 ENG TAIL PIPE. REMOVED AND REPLACED NR 1 ENG PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082700386 20010827 00386 NM 2001 8 27 SWAA012307 1 20010817 A 3350 65C27095 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED RON, FOUND FWD ENTRY AND FWD SVC DOOR EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PAC K PER MM. 2 L 7 2 4F A16WE 2001082700387 20010827 00387 NM 2001 8 27 SWAA012308 1 20010817 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 385SW 26600 DURING SCHEDULED C1 CHECK, FOUND EEPLS INOP AT SEVERAL LOCATIONS. RELAMPED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001082700388 20010827 00388 WP 2001 8 27 DHL2001804536 1 20010817 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AFT FUSELAGE INTERIOR LONGERON 17 RT CRACKED 3.5 INCH AT STA 1766. REMOVED AND REPLACED LONGERON PER SRM 51-1-20D PG 9 AND SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2001082800001 20010828 00001 SO 2001 8 28 C2XA01IA340 1 20010827 A 5510 14525351001 BUSHING EMB 145 EMB145LR SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12957 145080 IAH - DURING C-CHECK INSPECTION, THE FIXED BUSHINGS ON THE HORIZONTAL STABILIZER ATTACHMENT WERE FOUND TO BE CORRODED. M AINTENANCE REMOVED AND REPLACED THE AFFECTED BUSHINGS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001082800002 20010828 00002 WP 2001 8 28 DHL2001804551 1 20010823 A 5347 2955978 SEAT TRACK DOUG DC8 DC873F 302199F WP WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 FWD CARGO COMPT RT TRACK SHOWS 2-1/2 IN CRACKS ALSO CORROSION AND WEAR BETWEEN STA 360.000 AND 460.000.REMOVED R/H TRACK AT STA 360.000 TO 460.000 PER SRM 51-3-0 PG 1.CLEANED TERATED AND PRIMED PER SRM 51-1-8B.INSTALLED NEW TRACK PER SRM 51 -3-0 PG 1 2 L 7 4 4F RT 4A25 2001082800003 20010828 00003 WP 2001 8 28 RRXA010534 1 20010212 A 5730 56488962 PANEL DOUG DC8 DC871F 302199D WP RT WING CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RT WING UPPER WING T/E PANEL BETWEEN STA XRS 693 TO XRS 624, DA MAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED I AW DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001082800004 20010828 00004 WP 2001 8 28 RRXA010538 1 20010131 A 5340 BRACKET DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE ANGLE BRACKET BETWEEN STA XS 250.089 AND XS 252, DAMAGE EXCEEDED LIMITAT IONS IAAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-2 1. 2 L 7 4 4F RT 4A25 2001082800005 20010828 00005 WP 2001 8 28 RRXA010545 1 20010131 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND ELONGATED SCREW HOLE ON THE O/B TOP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2001082800006 20010828 00006 WP 2001 8 28 RRXA010553 1 20010131 A 5330 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND AN AREA OF METAL BROKEN OUT AT THE CORNER ON THE BOTTOM SKIN DOUBLER AT STA XS 250.089, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTAL LED IAW DC-8 SRM 57-2-0 AND DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001082800007 20010828 00007 WP 2001 8 28 RRXA010555 1 20010131 A 5730 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A SCREW PULLING THROUGH SKIN AND HOLES ELONGATED ON THE SLOT L/E PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-2-1A AND 51-1-21. 2 L 7 4 4F RT 4A25 2001082800008 20010828 00008 WP 2001 8 28 RRXA010557 1 20010131 A 5730 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND SCREWS PULLING THROUGH THE SKIN AT THE I/B SLOT VANE, DAMAGE EXCEEDED LIMITATIONS IAW D C-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-9. 2 L 7 4 4F RT 4A25 2001082800009 20010828 00009 WP 2001 8 28 RRXA010565 1 20010130 A 5730 PANEL DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES TO THE BOTTOM SLOT PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REM OVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4. 2 L 7 4 4F RT 4A25 2001082800010 20010828 00010 WP 2001 8 28 RRXA010568 1 20010130 A 5730 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND ELONGATED SCREW HOLES ON THE BOTTOM T/E BETWEEN STA XFS 85.000 TO STA XFS 91.250, DAMAG E EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IA W DC-8 SRM 51-1-21 AND DC-8 SRM 51-1-4. 2 L 7 4 4F RT 4A25 2001082800011 20010828 00011 WP 2001 8 28 RRXA010569 1 20010130 A 5730 PANEL DOUG DC8 DC871F 302199D WP WING DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES ON THE BOTTOM SLOT PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RE MOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW 51-1-22 AND 51-1-4. 2 L 7 4 4F RT 4A25 2001082800012 20010828 00012 WP 2001 8 28 RRXA010574 1 20010130 A 5730 SKIN DOUG DC8 DC871F 302199D WP WING DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A BROKEN OUT BOLT HOLE ON THE TOP PLATE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REM OVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2001082800013 20010828 00013 WP 2001 8 28 RRXA010580 1 20010119 A 5730 SKIN DOUG DC8 DC871F 302199D WP WING DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND AN ELONGATED SCREW HOLE TO THE TOP T/E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMO VED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-2-1. 2 L 7 4 4F RT 4A25 2001082800014 20010828 00014 WP 2001 8 28 RRXA010583 1 20010119 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP COCKPIT DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND ELONGATED LOCK HOLES TO THE CAPT'S RT AFT SEAT TRACK, DAMAGE EXCEEDED LIMITATIONS IAW D C-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001082800015 20010828 00015 WP 2001 8 28 RRXA010584 1 20010119 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP COCKPIT DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND ELONGATED LOCK HOLES TO THE CAPT'S LT AFT SEAT TRACK, DAMAGE EXCEEDED LIMITATIONS IAW D C-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001082800016 20010828 00016 WP 2001 8 28 RRXA010585 1 20010119 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP COCKPIT WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND DEEP WEAR AREAS TO THE CAPT'S RT FWD SEAT TRACK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND DC-8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 2001082800017 20010828 00017 WP 2001 8 28 RRXA010586 1 20010119 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP COCKPIT DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND ELONGATED LOCK HOLES TO THE FO'S RT AFT SEAT TRACK, DAMAGE EXCEEDED LIMITATIONS IAW DC- 8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3 AND DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001082800018 20010828 00018 WP 2001 8 28 RRXA010587 1 20010119 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP COCKPIT DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES TO THE FO'S LT AFT SEAT TRACK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM . REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3 AND DC-8 SRM 51-1 -20D. 2 L 7 4 4F RT 4A25 2001082800019 20010828 00019 WP 2001 8 28 RRXA010588 1 20010119 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP COCKPIT WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND DEEP WEAR TO THE FO'S RT FWD SEAT TRACK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REM OVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001082800020 20010828 00020 WP 2001 8 28 RRXA010589 1 20010119 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP COCKPIT WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND DEEP WEAR TO THE FO'S LT FWD SEAT TRACK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REM OVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001082800021 20010828 00021 WP 2001 8 28 RRXA010590 1 20010119 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND EXCESSIVE WEAR TO THE SEAT TRACK AT STA 1040 X+46", DAMAGE EXCEEDED LIMITATIONS IAW DC- 8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3 FIG.8A. 2 L 7 4 4F RT 4A25 2001082800022 20010828 00022 NM 2001 8 28 2001F00228 1 20010702 A 5311 FRAME BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 128NJ 22892 DURING C-CHECK INSPECTION PER S/B 737-53A1173, PRESSURE BULKHEAD BS 178 LEFT SIDE LATERAL CHORD CRACKED AT WL 207. REPLA CED LEFT SIDE CHORD FROM WL230 TO 188.5, LEFT SIDE WEB REPLACED FROM LBL 16 TO LBL 29, ACCOMPLISHED IAW S/B 737-53A1173 REV 3, SECTION III PART XI PARAGRAPH I/K FIG 71/72. (M) 2 L 7 2 4F A16WE 2001082800023 20010828 00023 EU 2001 8 28 DHL2001365035 1 20010823 A 2611 CG7GF DETECTOR AIRBUS 300 A300B4203 3930306 EU WILL NOT TEST A DHLA O OTHER L NO TEST IN INSP/MAINT 1 SO 01 365DH 149 1) ELEC & CARGO SMOKE DETECT PANEL 54VU DETECT FAULT MI AMBER. FLT DECK WILL NOT TEST.2) REMOVED & REPLACED FLIGHT DEC K SMOKE DETECTOR IAW M/M REF # 26-11-12. OPERATIONALLY CHECKED GOOD. 3) STATUS: CLOSED. 2 L 7 2 4F RT A35EU 2001082800024 20010828 00024 EU 2001 8 28 2001F00229 1 20010816 A 7540 7455967505 HARNESS AIRBUS 320 A320233 EU IAE V2527 V2527A5 NE NR 1 ENGINE DAMAGED A RJEF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 941LF 461 SAL - FLT 390 - DURING CLIMB, THE CAPTAIN REPORTED AIR ENGINE 1 BLEED ABNORMAL PRESSURE, AIR ENGINE 1 BLEED FAULT AND HY D GREEN ENG 1 PUMP LOW PRESSURE. THE AIRCRAFT RETURNED TO SAL STATION FOR MAINTENANCE. AFTER LANDING, MAINT TECH PERFOR MED FAULT ANALYSIS, IN ORDER TO FIND THE CAUSE OF THAT REPORT. DURING INSPECTION, THE ELECTRICAL HARNESS OF THE ENGINE H AD SEVERAL CHAFFING AND BURNED AREAS INCLUDING THE PRV, AND HP BLEED VALVE ELECTRICAL CONNECTOR. REMOVED AND REPLACED T HE ELECTRICAL HARNESS OF THE PRV AND HP BLEED VALVE, TIGHTENED THE PRV SENSE LINE ENGINE NR 1. REMOVED AND REPLACED THE HYD PRESSURE SWITCH OF THE HYD GREEN SYSTEM ENGINE NR 1 IAW AMM 29-11-17. THE A/C WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F RT A28NM E40NE 2001082800025 20010828 00025 WP 2001 8 28 RRXA010609 1 20010122 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND EXCESSIVE WEAR TO THE SEAT TRACK AT STA 940-960 X-49, DAMAGE EXCEEDED LIMITATIONS IAW D C-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3 & 53-2-3 F IG.8A. 2 L 7 4 4F RT 4A25 2001082800026 20010828 00026 EU 2001 8 28 2001F00230 1 20010816 A 2932 501310000 PRESSURE SWITCH AIRBUS 320 A320233 EU HYDRAULIC SYS FAILED A RJEF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 941LF 461 SAL - FLT 390 - DURING CLIMB, THE CAPTAIN REPORTED AIR ENGINE 1 BLEED ABNORMAL PRESSURE, AIR ENGINE 1 BLEED FAULT AND HY D GREEN ENG 1 PUMP LOW PRESSURE. THE AIRCRAFT RETURNED TO SAL STATION FOR MAINTENANCE. AFTER LANDING, MAINTENANCE TECHNI CIAN PERFORMED FAULT ANALYSIS, IN ORDER TO FIND THE CAUSE OF THAT REPORT. DURING INSPECTION, THE ELECTRICAL HARNESS OF T HE ENGINE HAD SEVERAL CHAFFING AND BURNED AREAS INCLUDING THE PRV, AND HP BLEED VALVE ELECTRICAL CONNECTOR. REMOVED AND REPLACED THE ELECTRICAL HARNESS OF THE PRV AND HP BLEED VALVE, TIGHTENED THE PRV SENSE LINE ENGINE NR 1. REMOVED AND REP LACED THE HYD PRESSURE SWITCH OF THE HYD GREEN SYSTEM ENGINE NR 1 IAW AMM 29-11-17. THE A/C WAS RETURNED TO SERVICE.(M) 2 L 7 2 4F RT A28NM 2001082800027 20010828 00027 WP 2001 8 28 RRXA010610 1 20010122 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND EXCESSIVE WEAR TO THE SEAT TRACK AT STA 420 X=0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3 FIG.8A. 2 L 7 4 4F RT 4A25 2001082800028 20010828 00028 EU 2001 8 28 2001F00231 1 20010815 A 2913 4205400 PUMP AIRBUS 320 A320233 EU NR 1 ENGINE FAILED A RJEF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 941LF 461 SAL - FLT 390 - DURING CLIMB, THE CAPTAIN REPORTED AIR ENG 1 BLEED ABNORMAL PRESSURE, AIR ENG 1 BLEED FAULT AND HYD GREE N ENG 1 PUMP LOW PRESSURE. THE AIRCRAFT RETURNED TO SAL STATION FOR MAINTENANCE. AFTER LANDING, MAINTENANCE TECHNICIAN PERFORMED FAULT ANALYSIS, IN ORDER TO FIND THE CAUSE OF THAT REPORT. DURING INSPECTION OF THE ENGINE, THE ELECTRICAL H ARNESS OF THE ENGINE WAS OBSERVED WITH SEVERAL CHAFFING AND BURNED AREAS INCLUDING THE PRV, AND HP BLEED VALVE ELECTRICA L CONNECTOR DAMAGED. AT THIS TIME A/C REMAINS ON GROUND. (M) 2 L 7 2 4F RT A28NM 2001082800029 20010828 00029 CE 2001 8 28 2001F00232 1 20010806 A 3260 951F04 LIGHT BEECH 1900 1900D 1154162 CE COCKPIT INOPERATIVE A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 19 69547 UE189 FLT 9505 - EYW/TPA - LANDING GEAR DOWNLOCK INDICATOR HAS ONE LAMP INOPERATIVE. REPLACED BURNED LAMP INOPERATIVE. REPLA CED BURNED LAMP IN DOWNLOCK INDICATOR. OPERATIONAL CHCK SATISFACTORY. (M) 2 L 7 2 4T RT A24CE 2001082800030 20010828 00030 CE 2001 8 28 2001F00233 1 20010801 A 2620 WARNING LIGHT BEECH 1900 1900D 1154162 CE COCKPIT ILLUMINATED A GUUA O OTHER J WARNING INDICATION CR CRUISE 1 SO 19 53545 UE185 FLT 9144 - FPO/FLL - DURING FLIGHT, LEFT FIRE EXTINGUISHER DISCHARGE LIGHT CAME ON. SECURED FIRE SQUIB WIRES ON LEFT SI DE. SYSTEM OPS TEST NORMAL. (M) 2 L 7 2 4T RT A24CE 2001082800031 20010828 00031 CE 2001 8 28 2001F00234 1 20010731 A 2620 WARNING LIGHT BEECH 1900 1900D 1154162 CE COCKPIT ILLUMINATED A GUUA O OTHER J WARNING INDICATION CR CRUISE 1 SO 19 53545 UE185 FLT 9476 - MCO/MIA - DURING FLIGHT, LEFT FIRE EXTINGUISHER DISCHARGE LIGHT CAME ON. INSPECTED SYSTEM. CLEANED WIRES OF OIL. SYSTEM OPS TEST NORMAL. (M) 2 L 7 2 4T RT A24CE 2001082800032 20010828 00032 WP 2001 8 28 RRXA010611 1 20010122 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND EXCESSIVE WEAR TO THE SEAT TRACK AT STA 859-879 X-49, DAMAGE EXCEEDED LIMITATIONS IAW D C-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3 FIG.8A. 2 L 7 4 4F RT 4A25 2001082800033 20010828 00033 WP 2001 8 28 RRXA010612 1 20010122 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND EXCESSIVE WEAR TO THE SEAT TRACK AT STA 320-340 X=0, DAMAGE EXCEEDED LIMITATIONS IAW DC -8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3 FIG.8A. 2 L 7 4 4F RT 4A25 2001082800034 20010828 00034 WP 2001 8 28 RRXA010613 1 20010122 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND EXCESSIVE WEAR TO THE SEAT TRACK AT STA 320-340 X=+20, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3 & 53-2-3 FIG.8A. 2 L 7 4 4F RT 4A25 2001082800035 20010828 00035 WP 2001 8 28 RRXA010614 1 20010122 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A WORN SEAT TRACK AT STA 857-879 X=0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVE D DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3 FIG8A. 2 L 7 4 4F RT 4A25 2001082800036 20010828 00036 CE 2001 8 28 2001F00235 1 20010728 A 2620 WARNING SYSTEM BEECH 1900 1900D 1154162 CE FIRE PROTECTION MALFUNCTIONED A C2XA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 19 53545 UE185 FLT 9481 - PBI/TPA - DURING FLIGHT, LEFT ENGINE FIRE EXTINGUISHER DISCHARGE ANNUNCIATOR CAME ON. PERFORMED OPERATIONAL TEST OF LEFT ENGINE FIRE EXTINGUISHER ANNUNCIATOR. COULD NOT DUPLICATE. OPERATIONAL TEST NORMAL. (M) 2 L 7 2 4T RT A24CE 2001082800037 20010828 00037 WP 2001 8 28 RRXA010622 1 20010123 A 5730 DOUBLER DOUG DC8 DC871F 302199D WP WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE BOTTOM DOUBLER ABOUT 20 INCHES INSIDE L/E AT STA XFS 427, DAMAGE EXCEEDE D LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-4 &57-2-0 &51-1-20D. 2 L 7 4 4F RT 4A25 2001082800038 20010828 00038 CE 2001 8 28 2001F00236 1 20010726 A 2910 1013880175 HYDRAULIC LINE BEECH 1900 1900C 1154161 CE RT MLG LEAKING A GUUA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 19 139GA UC126 FLT 9495 - MIA/FPO - DURING POST FLIGHT WALK AROUND, NOTICED RIGHT MLG HYDRAULIC LINE RUPTURED. REMOVED AND REPLACED RI GHT MLG HYDRAULIC LINE. OPS CHECK NORMAL. (M) 2 L 7 2 4T RT A24CE 2001082800039 20010828 00039 WP 2001 8 28 RRXA010624 1 20010123 A 5720 FORMER DOUG DC8 DC871F 302199D WP WING CHAFED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND THE DE-ICER DUCT CHAFED DEEP INTO FORMER AT STA XFS 416, DAMAGE EXCEEDED LIMITATIONS IA W DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-2-0 & 51-1- 20D. 2 L 7 4 4F RT 4A25 2001082800040 20010828 00040 WP 2001 8 28 RRXA010633 1 20010125 A 5730 SKIN DOUG DC8 DC871F 302199D WP WING DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND ELONGATED SCREW HOLES TO THE SKIN AT STA 304, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-1. 2 L 7 4 4F RT 4A25 2001082800041 20010828 00041 WP 2001 8 28 RRXA010634 1 20010126 A 5730 SKIN DOUG DC8 DC871F 302199D WP WING DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES IN REPAIR STRAP ON THE O/B SLOT VANE AT STA XS 520.168, DAMAGE EXCEEDE D LIMITATIONS IAW DC-8 SRM. 2 L 7 4 4F RT 4A25 2001082800042 20010828 00042 WP 2001 8 28 RRXA010635 1 20010125 A 5730 SKIN DOUG DC8 DC871F 302199D WP WING DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND ELONGATED SCREW HOLES AT STA XS 520.166, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REM OVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-1. 2 L 7 4 4F RT 4A25 2001082800043 20010828 00043 WP 2001 8 28 RRXA010649 1 20010125 A 5730 PANEL DOUG DC8 DC871F 302199D WP WING DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES TO THE BOTTOM SLOT PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RE MOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4. 2 L 7 4 4F RT 4A25 2001082800044 20010828 00044 WP 2001 8 28 RRXA010650 1 20010126 A 5730 SKIN DOUG DC8 DC871F 302199D WP WING DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND SCREWS PULLING THROUGH SKIN ON THE SLOT VANE I/B END, DAMAGE EXCEEDED LIMITATIONS IAW D C-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001082800045 20010828 00045 CE 2001 8 28 2001F00212 1 20010722 A 5520 1016200111 HINGE BRACKET BEECH 1900 1900C 1154161 CE ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 139GA 26315 UC126 DURING SCHEDULED MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANU LAR CORROSION. REMOVED AND REPLACED RIGHT ELEVATOR OUTBOARD HINGE BRACKET. (M) 2 L 7 2 4T RT A24CE 2001082800046 20010828 00046 WP 2001 8 28 RRXA010653 1 20010126 A 5321 FINGER DOUBLER DOUG DC8 DC871F 302199D WP COCKPIT DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND SEVERAL POPPED RIVETS TO THE COCKPIT SUB-FLOOR BETWEEN FRAMES X-32 & X-52 Y-20 Z-11, DA MAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21 AND DC-8 SRM 53-2-0 FIG.1F. 2 L 7 4 4F RT 4A25 2001082800047 20010828 00047 WP 2001 8 28 RRXA010655 1 20010126 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOORBEAM CENTER WING STA 879, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW E.O.01-024 WITH APPROVED 8110-3 DATED 01/29/01. 2 L 7 4 4F RT 4A25 2001082800048 20010828 00048 NE 2001 8 28 2001F00213 2 20010727 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LEFT MALFUNCTIONED A GUUA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 17 81536 11091 UE152 FLT 9501 - EYW/TPA - DURING FLIGHT, NR 1 ENGINE HAS A RAPID INCREASE IN ITT AND FUEL FLOW. PRECAUTIONARY SHUTDOWN ENGIN E. REMOVED AND REPLACED NR 1 ENGINE. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 2001082800049 20010828 00049 NM 2001 8 28 2001F00214 1 20010729 A 3610 312N1533811 DUCT BOEING 757 757200 1384950 NM BLEED AIR CRACKED A N8TA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 WP 19 512NA 26962 LEFT STRUT OVERHEAT EICAS MESSAGE FOLLOWED BY LT ENGINE OVERHEAT EICAS MESSAGE. ENGINE BLEED SHUT OFF AND AIRCRAFT RETU RNED TO DEPARTURE STATION AND MADE AN UNEVENTFUL LANDING. INVESTIGATION REVEALED CRACKED DUCT. (M) 2 L 7 2 4F RT A2NM 2001082800050 20010828 00050 CE 2001 8 28 2001F00218 1 20010714 A 2620 WARNING LIGHT BEECH 1900 1900D 1154162 CE COCKPIT ILLUMINATED A GUUA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 19 53545 UE185 FLT 9481 - PBI-TPA - DURING FLIGHT, LEFT ENGINE FIRE DISCHARGE ANNUNCIATOR ILLUMINATED. PERFORMED OPERATIONAL TEST OF L EFT ENGINE. DISCHARGE ANNUNCIATOR, OPS TEST NORMAL. (M) 2 L 7 2 4T RT A24CE 2001082800051 20010828 00051 WP 2001 8 28 2001F00226 1 20010714 A 3240 H2445 TUBE DOUG DC3 DC3C 3021457 WP LT MGL BRAKE CRACKED A JRAA E D ENGINE SHUTDOWN RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 376AS 27047 PRIOR TO TAKEOFF, RUPTURED LEFT MAIN WHEEL BRAKE EXPANDER TUBE. THE RUPTURE CAUSED A HYDRAULIC FLUID LOSS AND SUBSEQUEN T LEFT BRAKE LOSS. THE AIRCRAFT WAS STOPPED WITH REVERSE THRUST AND THE ENGINES SHUTDOWN. NORTH OPS WAS ADVISED OF THE SITUATION BY VICTOR RADIO. SMOKE JUMPERS AND SPOTTERS WERE DEPLANED. TOWED A/C BACK TO RAMP. THE ENTIRE LEFT MAIN WH EEL, TIRE, AND BRAKE ASSY WAS REPLACED WITH AN OVERHAULED UNIT. THE LEAKING BRAKE/HYDRAULIC FLUID WAS CONTAINED AND CLE ANED UP. THE NEXT MORNING A TAXI CHECK WAS PERFORMED TO DOUBLE-CHECK THE SYSTEM. ALL OPERATIONS WERE NORMAL. (M) 2 L 7 2 4R A669 2001082800052 20010828 00052 WP 2001 8 28 RRXA010661 1 20010118 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND EXCESSIVE WEAR TO THE SEAT TRACK AT STA 140-160 X-24, DAMAGE EXCEEDED LIMITATIONS IAW D C-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-2-3. 2 L 7 4 4F RT 4A25 2001082800053 20010828 00053 WP 2001 8 28 RRXA010662 1 20010118 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND EXCESSIVE WEAR TO THE SEAT TRACK AT STA 140-160 X=0, DAMAGE EXCEEDED LIMITATIONS IAW DC -8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0 AND DC-8 SR M 53-2-3 FIG. 14. 2 L 7 4 4F RT 4A25 2001082800054 20010828 00054 NM 2001 8 28 2001F00227 1 20010702 A 5311 FRAME BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 128NJ 22892 DURING C-CHECK INSPECTION PER S/B 737-53A1173, PRESSURE BULKHEAD BS 178 RIGHT SIDE LATERAL CHORD CRACKED AT WL 207. PRE SSURE BULKHEAD BS 178 RIGHT LATERAL CHORD REPLACED FROM WL 230 TO 188.5 DUE TO CRACK RT SIDE WEB REPLACED FROM RBL 16 TO RBL 29, WORK ACCOMPLISHED IAW S/B 737-53A1173 REV 3, SECTION III PART XI PARA I/K FIG 71 AND 72. (M) 2 L 7 2 4F A16WE 2001082800055 20010828 00055 WP 2001 8 28 RRXA010663 1 20010119 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND EXCESSIVE WEAR TO THE SEAT TRACK AT STA 140-160 X+45, DAMAGE EXCEEDED LIMITATIONS IAW D C-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3 FIG. 14. 2 L 7 4 4F RT 4A25 2001082800056 20010828 00056 WP 2001 8 28 RRXA010664 1 20010118 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND EXCESSIVE WEAR TO THE SEAT TRACK AT STA 140-160 X+-45, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3 FIG. 14. 2 L 7 4 4F RT 4A25 2001082800057 20010828 00057 EA 2001 8 28 ASOA01098 1 20010627 A 2910 601R7528637 HYDRAULIC LINE CNDAIR CL600 CL6002B19 EA HYDRAULIC SYS CHAFED A ASOA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 11 834AS 7254 FLT 4751 - DURING FLIGHT FROM ROA TO ATL, PILOT REPORTED ALL FLUID IN THE LEFT HYDRAULIC SYSTEM LOST. AN EMERGENCY WAS DECLARED. AIRCRAFT RETURNED AND LANDED SAFELY IN ROA. MAINTENANCE INSPECTED AIRCRAFT AND FOUND THE HYDRAULIC RESERVOIR SUMP SUCTION LINE CHAFED. MAINTENANCE REPAIRED CHAFED LINE AS WELL AS REMOVED AND REPLACED THE LEFT HYDRAULIC ENGINE D RIVEN PUMP. LEAK AND OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001082800058 20010828 00058 EA 2001 8 28 ASOA01114 1 20010722 A 2910 AE7120312 HYDRAULIC LINE CNDAIR CL600 CL6002B19 EA RT ENGINE RUPTURED A ASOA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 11 863AS 7487 FLT 4696 - DURING FLIGHT FROM ATL TO SWF, PILOT SAW RIGHT SIDE HYDRAULIC QUANTITY AND PRESSURE INDICATIONS AT ZERO. AN EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO ATL WITH NO FURTHER INCIDENTS. MAINTENANCE FOUND PRESSURE LINE ON THE RIG HT ENGINE TO BE RUPTURED. MAINTENANCE REMOVED AND REPLACED HYDRAULIC PRESSURE LINE ON RIGHT ENGINE. THE ENGINE DRIVEN PUMP WAS ALSO REPLACED DUE TO IT OPERATING WITHOUT FLUID FOR 46 MINUTES. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT RE TURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001082800059 20010828 00059 WP 2001 8 28 RRXA010667 1 20010118 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND EXCESSIVE WEAR TO THE SEAT TRACK AT STA 240-260 X-59, DAMAGE EXCEEDED LIMITATIONS IAW D C-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3 FIG. 14. 2 L 7 4 4F RT 4A25 2001082800060 20010828 00060 WP 2001 8 28 RRXA010674 1 20010227 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND AN IMPROPER REPAIR TO THE MAIN CARGO FLOOR PANEL AT STA 80 TO 340E, DAMAGE EXCEEDED LIM ITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 5 1-1-21 AND DC-9 SRM 53-2-3. 2 L 7 4 4F RT 4A25 2001082800061 20010828 00061 WP 2001 8 28 RRXA010675 1 20010227 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A GOUGE TO THE FWD SIDE OF FRAME ON THE R/H FWD TYPE I DOOR FRAME SEAL AT STA 370, DAMA GE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21 & 53-2-0. 2 L 7 4 4F RT 4A25 2001082800062 20010828 00062 WP 2001 8 28 RRXA010676 1 20010227 A 5320 FLANGE DOUG DC8 DC871F 302199D WP DOOR SEAL CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT FWD TYPE I DOOR FRAME SEAL FLANGE LWR END, DAMAGE EXCEEDED LIMITATION S IAAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21 AND DC-8 SRM 53-2-0. 2 L 7 4 4F RT 4A25 2001082800063 20010828 00063 NE 2001 8 28 ASOA01116 2 20010724 A 7200 ENGINE EMB 120 EMB120 3260201 SO GE CT7TP CT79B 30030 NE RIGHT FAILED A ASOA E A ENGINE SHUTDOWN UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 11 243AS 120072 FLT 4830 - DURING FLIGHT FROM DFW TO TUL, CREW REPORTED SMELLING SMOKE IN THE CABIN. AFTER ISOLATING THE RIGHT BLEED AN D RIGHT PACK THE SMOKE STILL DIDN'T CLEAR. THE CREW THEN RECEIVED A RIGHT ENGINE LOW OIL PRESSURE WARNING AND NOTED THE GAUGE WAS FLUCTUATING. THE RIGHT ENGINE OIL PRESSURE DROPPED BELOW 40 PSID. AT THIS TIME THE RIGHT ENGINE WAS SHUT DO WN. AIRCRAFT RETURNED TO DFW AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE. (M) 2 L 7 2 4T 4 T RT A31SO E8NE 2001082800064 20010828 00064 WP 2001 8 28 RRXA010677 1 20010227 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE CENTER WING FLOOR BEAM AT STA 857 X+60, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW E.O.#01-024 WITH APPROVED 8110-3 DATED 02/26/01. 2 L 7 4 4F RT 4A25 2001082800065 20010828 00065 NM 2001 8 28 AWXA0002184 1 20010729 A 5315 6546811 BEAM BOEING 737 7373B7 1384580 NM BS 986.5 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 332AW 23384 D: Corrosion on floor beam BS 986.5 LBL 9.0 to LBL 44.0 upper flange.C: Removed corrosion, corrosion out limits, fabrica ted repair strap, and installed IAW 737-300 SRM 51-10-2 pg 6, 53-60-51, pg 114, 53-00-51, pg 212-215, 51-21-00, pg 701. 2 L 7 2 4F RT A16WE 2001082800066 20010828 00066 NM 2001 8 28 AWXA0002185 1 20010729 A 5315 6546811 BEAM BOEING 737 7373B7 1384580 NM BS 1005.5 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 332AW 23384 D: Corrosion on floor beam upper flange BS 1005.5 LBL 6.5.C: Corrosion removal out of limits, fabricated & installed rep air strap IAW B737 SRM 53-00-51 pg 212-215 2 L 7 2 4F RT A16WE 2001082800067 20010828 00067 NM 2001 8 28 AWXA0002187 1 20010729 A 5311 6545409245 WEB BOEING 737 737300 1384610 NM BS 664 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 332AW 23384 D: Lt wheel well pressure web cracked B.S. 664 LBL 32.C: Repaired Lt wheel well pressure web at B.S. LBL 32 IAW AWA ER # 03-5712-01226-DL1 2 L 7 2 4F RT A16WE 2001082800068 20010828 00068 NM 2001 8 28 AWXA0002189 1 20010801 A 5311 6545833040 WEB BOEING 737 73733A 1384673 NM BS 180 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 D: Cockpit floor web cracked LBL 24,WL 207,BS 180C: Removed and replaced floor web IAW ER 03-5311-01218-001 2 L 7 2 4F RT A16WE 2001082800069 20010828 00069 NM 2001 8 28 AWXA0002190 1 20010805 A 5330 6552988 SKIN BOEING 737 73733A 1384673 NM BS948 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 D: L2 door fuselage upper hinge cut out cracked BS 948C: Removed damaged area and installed repair IAW 737 SRM 53-60-01 Fig 205 pgs 210-212 2 L 7 2 4F RT A16WE 2001082800070 20010828 00070 2001 8 28 ASOA01120 4 20010729 A 3425 6229336400 COMPUTER CNDAIR CL600 CL6002B19 EA E/E BAY INOPERATIVE A A ASOA A UNSCHED LANDING J I F WARNING INDICATION FLT. ATTITUDE INST. FLT CONT AFFECTED CL CLIMB 1 SO 11 847AS 1794 7335 FLT 4752 - ON CLIMB-OUT FROM MYR, CAPTAIN RECEIVED BOTH 'STAB TRIM' AND 'MACH TRIM' CAUTION MESSAGES THE CAPTAIN WAS AB LE TO RE-ENGAGE THE STAB AND MACH TRIM ONLY AFTER ENGAGING THE AUTOPILOT. THEN THE 'AP PITCH TRIM INOP' AND 'AP TRIM NO SE DOWN' CAUTION MESSAGES ILLUMINATED. AT THIS POINT AN EMERGENCY WAS DECLARED. AIRCRAFT DIVERTED TO CHS AND HAD AN OV ER GROSS LANDING WITHOUT INCIDENT. MAINTENANCE PERFORMED AN OVER GROSS LANDING INSPECTION. NO DEFECTS WERE NOTED. MAI NTENANCE ALSO REORIENTED THE NR 2 ATTITUDE HEADING REFERENCE SYSTEM. OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F RT A21EA 2001082800071 20010828 00071 NM 2001 8 28 GAIA01259ST 1 20010806 A 5330 SKIN BOEING 727 727251 138408H NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING AN LTC INSPECTION, IT WAS DISCOVERED A DENT ON FUSELAGE SKIN ABOVE NR 3 ENGINE AT BS 1263, STRINGER 7R. ACCOMPLI SHED FUSELAGE SKIN REPAIR AT BS 1263, STRINGER 7R, IAW B727 SRM 53-03-3 FIG 3. (M) 2 L 7 3 4F A3WE 2001082800073 20010828 00073 EU 2001 8 28 CA010823016 1 20010815 A 5311 S5357260120000 FRAME AEROSP ATR42320 AEROSP ATR42 ATR42320 8680930 EU PWA 120 PW120 NE HAMSTD 14RF 14RF9 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 24560 179 (CAN) - CRACK FOUND ON FRAME 25 LT, HYD CUT OUT. CRACK STOP DRILLED IAW CONTINENTAL EXPRESS EC 23/0-01200. 2 H 7 2 4T 4 T RT A53EU E20NE 6 C P11NE 2001082800074 20010828 00074 WP 2001 8 28 CALA0100809 1 20010827 A 5320 WEB DOUG DC9 DC982 3022082 WP STA 1463 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND WEB CRACKED IN FOUR PLACES AT CANTED FRAME STA 1463, I/B OF LONGERON 7L. THE WEB AND STIFFENERS WERE RE MOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2, 51-30-1, AND 51-10-4. 2 L 7 2 4F A6WE 2001082800075 20010828 00075 NM 2001 8 28 CALA0100810 1 20010827 A 5320 MOUNT BOEING 737 7373T0 1384582 NM RH AFT GALLEY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND R/H AFT O/B GALLEY MOUNT CORRODED. THE GALLEY MOUNT WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001082800076 20010828 00076 NM 2001 8 28 CALA0100811 1 20010827 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM STA 907-947.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND L/H I/B SEAT TRACK CORRODED AT STA 907-947.5. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001082800077 20010828 00077 WP 2001 8 28 CALA0100812 1 20010827 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FS 250-788 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND MAIN DECK R/H SEAT TRACK CORRODED AT FS 250-788. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS IN STALLED IAW SRM 51-30-5 AND 53-05, FIGURE 4F. 2 L 7 2 4F A6WE 2001082800078 20010828 00078 WP 2001 8 28 CALA0100813 1 20010827 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 927-1003 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND CABIN FLOOR PANEL DELAMINATED AT FS 927-1003. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001082800079 20010828 00079 WP 2001 8 28 CALA0100814 1 20010828 A 5347 SEAT TRACK DOUG DC10 DC1030 3023501 WP STA 1860 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17085 47957 INSPECTION FOUND MAIN DECK SEAT TRACK CORRODED AT Y = 1860, X = -60.00, JUST AFT OF R-4 ATTENDANT SEAT. THE CORRODED SEC TION OF SEAT TRACK WAS CUT OUT AND A NEW SECTION OF SEAT TRACK WAS INSTALLED USING SPLICE HAT AND SPLICE PLATE IAW SRM 5 3-70-00, FIGURE 1. 2 L 7 3 4F A22WE 2001082800080 20010828 00080 NM 2001 8 28 GAIA01299OP 1 20010821 A 3234 CONTROL HANDLE BOEING 727 727251 138408H NM COCKPIT STIFF A GAIA K NONE N FALSE WARNING CL CLIMB 1 SW 07 252US 19971 FLT 2019 - PHX-MHR - ON TAKEOFF, THE GEAR RETRACTED NORMAL, THE GEAR HANDLE WAS ABOUT TWO INCHES SHORT OF BEING IN THE F ULL UP POSITION. RETURNED THE GEAR HANDLE TO OFF POSITION AND WAS DIFFICULT TO MOVE. RECYCLED THE HANDLE TO UP AND THE H ANDLE MOVED ALL THE WAY TO THE UP POSITION. THE HANDLE WAS POSITIONED TO THE OFF POSITION. DURING CRUISE, THE RT MLG RED LIGHT ILLUM. NO ABNORMAL VIBRATIONS NOTED AND GEAR EXTENDED NORMALLY DURING APPROACH. CONTINUED APPROACH AND LANDED WIT HOUT FURTHER DIFFICULTIES. INSPECTED, CLEANED AND LUBED ASSOCIATED LINKAGE, PULLEYS AND CABLES ON THE GEAR HANDLE SYS. TESTED GEAR HANDLE WITH AND WITHOUT HYD POWER. OPS CHECKS GOOD. CYCLED MLG DOORS AND NO RED LIGHT NOTED. (M) 2 L 7 3 4F A3WE 2001082800081 20010828 00081 2001 8 28 GTIA010684 4 20010721 A 2210 4034242934 CONTROL PANEL DOUG DC9 DC981 3022081 WP COCKPIT DEFECTIVE A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 811NK 48017 FLT 967 - MCO - CIRCUIT BREAKER FOR DFGS SWITCH A POSITION C17 POPPED DID NOT RESET. TROUBLESHOT DFGS NR 1 AND NR 2 FOU ND DEFECTIVE DIGITAL FLT GUIDANCE CONTROL PANEL. REMOVED AND REPLACED FLIGHT GUIDANCE CONTROL PANEL IAW MM 22-01-02. S YSTEMS GROUND CHECK GOOD IAW MM 22-00-00. (M) 2 L 7 2 4F A6WE 2001082800082 20010828 00082 WP 2001 8 28 GTIA010688 1 20010712 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 DALLO 53012 DTW - FOUND SEVERAL OVERHEAD EMERGENCY LIGHTS INOPERATIVE 34C, 31D, 26D, 23D, 20D, 16D, 12C, 12D, 10C, 10D, 8C, 8D, 4D, 1C. FOUND SOCKET LOOSE RESECURED AND REPLACED BATTERY PACK, OPS CHECK NORMAL IAW MD80 MM 33-53-00. (M) 2 L 7 2 4F RT A6WE 2001082800083 20010828 00083 SO 2001 8 28 MASA01083 1 20010801 A 5250 14531574401 HANDLE EMB 145 EMB145 SO PAX DOOR LOOSE A MASA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 836MJ 145359 FLT 5877 - THE INTERIOR PASSENGER DOOR FELL OFF. MAINTENANCE INSPECTED HANDLE AND ATTACHING HARDWARE THEN REINSTALLED H ANDLE. OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001082800084 20010828 00084 NM 2001 8 28 P2EA01124 1 20010702 A 5320 STIFFENER BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 128NJ 22892 DURING C-CHECK INSPECTION PER S/B 737-53A1173, PRESSURE BULKHEAD BS 178 VERTICAL CHORD CRACKED AT LBL 57 WL 184. PRESSU RE BULKHEAD BS 178 VERTICAL CHORD REPAIRED AT LBL 57 FROM WL 178.4 TO 196.5 DUE TO CRACK IAW 53-10-11 FIG 8. (M) 2 L 7 2 4F A16WE 2001082800086 20010828 00086 NM 2001 8 28 USAA010648 1 20010612 A 5300 SKIN BOEING 737 737301 1384611 NM BS 895-907 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 43098 23743 CLT - FOUND SKIN WITH PREVIOUSLY INSTALLED DOUBLER, 11 INCH BY 12.25 INCH, BS 895-907, STRINGER 16 AND 17L. DOUBLER HAS BEEN INSTALLED PER SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2001082800087 20010828 00087 NM 2001 8 28 TSAA0124097 1 20010727 A 2400 BACC18W7 CIRCUIT BREAKER BOEING 737 7372X6C 1384552 NM P6 PANEL A TSAA E D ENGINE SHUTDOWN RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 13 816AL 23122 FLT 242 - LIH-OGG - THE CREW NOTICED A STRONG ELECTRICAL SMELL COMING FROM THE CENTER OF THE CABIN DURING DESCENT. SMEL L DISSIPATED AFTER LANDING. MAUI MAINTENANCE PERSONNEL INSPECTED AND RELEASED THE AIRCRAFT WHEN NO EVIDENCE OF ELECTRIC AL FUMES OR ORIGIN COULD BE LOCATED. AGAIN EXPERIENCED AN ELECTRICAL ODOR THAT WAS CONCENTRATED IN THE FORWARD CABIN. HNL MAINTENANCE REPLACED THE NR 3 TR RECTIFIER AND RELEASED THE AIRCRAFT FOR FLIGHT. AFTER PUSHBACK AND STARTING BOTH E NGINES, THE CREW HAD VISIBLE SMOKE IN THE CABIN. THE CREW EXECUTED THE CHECKLIST ON PAGE 4-2 IN THE QRH, SHUTDOWN BOTH ENGINES AND HAD THE AIRCRAFT TOWED BACK TO THE GATE. REMOVED AND REPLACED THE NR 3 TRANSFORMER RECTIFIER (2X), EQUIPMEN 2 L 7 2 4F RT A16WE 2001082800088 20010828 00088 NM 2001 8 28 AALA20011577 1 20010731 A 5300 SKIN BOEING 727 727227 1384078 NM FS 1148-1166 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 720AA 20613 TUL - FOUND CORROSION ON INTERIOR OF SKIN BETWEEN STATION 1148 AND STATION 1166 BETWEEN STRINGER 22L AND 23L. INSTALLED REPAIR DOUBLER PER ESO 11697 DATED JULY 27, 2001. (M) 2 L 7 3 4F A3WE 2001082800089 20010828 00089 NM 2001 8 28 AALA20011579 1 20010730 A 5100 WEB BOEING 727 727227 1384078 NM FS 219 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 720AA 20613 TUL - FOUND LEFT PRESSURE WALL IS CRACKED JUST BELOW DOOR CABLE QUAD. INSTALLED DOUBLER PER ESO 11697 7/30/01. (M) 2 L 7 3 4F A3WE 2001082800090 20010828 00090 NM 2001 8 28 AALA20011585 1 20010731 A 5300 SKIN BOEING 727 727227 1384078 NM FS 685 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 716AA 20608 TUL - FOUND LIGHT CORROSION AROUND FLAPPER DRAIN BETWEEN 28R AND BLO STATION 685. INSTALLED DOUBLER PER SRM 53-30-3 050 7075 T-6 9 INCH BY 9 INCH FOUR ROWS EACH SIDE .1875 RIVETS. (M) 2 L 7 3 4F A3WE 2001082800091 20010828 00091 NM 2001 8 28 AALA20011586 1 20010731 A 5300 STRINGER BOEING 727 727227 1384078 NM BS 994 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 716AA 20608 TUL - FOUND STRINGER 29R CORRODED ON LOWER FLANGE AT STATION 998. INSTALLED NEW STRINGER SECTION WITH SPLICE PER SRM 53 -10-3. (M) 2 L 7 3 4F A3WE 2001082800092 20010828 00092 NM 2001 8 28 AALA20011376 1 20010706 A 2500 D31038201 SLIDE BOEING 757 757223 1384957 NM GALLEY DOOR INOPERATIVE A AALA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 647AM 24605 LGA - FLT 1132 - GALLEY SLIDE INADVERTENTLY UNSUCCESSFULLY DEPLOYED. REPLACED SLIDE. SYSTEM GROUND CHECKED NORMAL OPER ATION. (M) 2 L 7 2 4F RT A2NM 2001082800093 20010828 00093 WP 2001 8 28 AALA20011495 1 20010724 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 463AA 49593 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS ROW 28 THROUGH 31 INOPERATIVE. REPLACED EMERGENCY EXIT ESCAPE PATH LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001082800094 20010828 00094 WP 2001 8 28 AALA20011507 1 20010727 A 3350 8039001 BATTERY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7538A 49992 DFW - DURING OVERNIGHT MAINTENANCE, CEILING MOUNTED EMERGENCY EXIT LIGHTS IN AFT CABIN INOPERATIVE. REPLACED CEILING MO UNTED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001082800095 20010828 00095 WP 2001 8 28 AALA20011515 1 20010729 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 266AA 49291 PHX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTING FROM ROW 20 AFT INOPERATIVE. RECONNECTED LOOSE WIRE AT SEAT 21. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001082800096 20010828 00096 WP 2001 8 28 AALA20011517 1 20010729 A 3350 P401005111 MODULE DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 491AA 49684 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS FROM SEAT 20 AFT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT MODULE AND BATTERY PACK. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001082800097 20010828 00097 WP 2001 8 28 AALA20011553 1 20010731 A 3350 P4010049 BATTERY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER CR CRUISE 1 SW 21 286AA 49298 DFW - FLT 1940 - EN ROUTE PDX-DFW - EMERGENCY EXIT FLOOR PATH LIGHTING FROM ROW 19 TO AFT OF AIRCRAFT ILLUMINATED INTERM ITTENTLY THROUGHOUT FLIGHT. LANDED DFW WITHOUT INCIDENT. REPLACED BOTH MID BATTERY PACKS AND CHARGERS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001082800098 20010828 00098 EU 2001 8 28 AALA20011463 1 20010722 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN DISCONNECTED A AALA K NONE O OTHER CR CRUISE 1 SW 21 19059 469 JFK - EN ROUTE MIA-JFK - EMERGENCY ESCAPE PATH LIGHTS CAME ON INTERMITTENTLY IN CABIN AND AT 1R DOOR. AIR INTERRUPTED A ND LANDED JFK WITHOUT INCIDENT. RESEATED DISCONNECTED CONNECTOR AT ROW 17G. SYSTEM GROUND CHECKED NORMAL OPERATION. ( M) 2 L 7 2 4F RT A35EU 2001082800099 20010828 00099 NM 2001 8 28 AALA20011520 1 20010727 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 308AA 22314 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHT ROW 31H INOPERATIVE. RESEATED CONNECTOR FOR EMERGE NCY EXIT ESCAPE PATH LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001082800100 20010828 00100 NM 2001 8 28 AALA20011511 1 20010720 A 2900 LINE BOEING 727 727200 138407E NM AFT ACCY LEAKING A AALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SW 21 706AA 22463 DFW - FLT 1744 - EN ROUTE DFW-DTW - AIR INTERRUPTED WITH HYDRAULIC SYSTEM 'A' LOSS OF QUANTITY AND PRESSURE. RETURNED T O DFW LANDED WITHOUT INCIDENT. REPLACED LEFT ELEVATOR PACK HYDRAULIC LINE. SERVICED SYSTEM. LEAK AND OPERATIONAL CHEC K OK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A3WE 2001082800101 20010828 00101 NM 2001 8 28 AALA20011491 1 20010723 A 3350 PIN BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 351AA 24032 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 22B INOPERATIVE. RE-SEATED EMERGENCY EXIT LIGHT CONNEC TOR PIN AT ROW 22B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001082800102 20010828 00102 NM 2001 8 28 TSAA0133092 1 20010720 A 3350 86210066 BATTERY PACK BOEING 737 7372Y5 1384554 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 810AL 24031 REPLACED NR 2 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4U RT A16WE 2001082800103 20010828 00103 NM 2001 8 28 UIEA01075 1 20010724 A 5315 FLOORBEAM BOEING 747 7472D3B 1384805 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 506MC 21252 DURING INSPECTION FOUND FLOORBEAM WEB CRACKED AT BS 270 NEAR STRINGER 13 BOTH LEFT AND RIGHT SIDE. FASTENERS REMOVED, O PEN HOLE HFEC INSPECTION PERFORMED TO ENSURE NO OTHER CRACKS. NO ADDITIONAL CRACKS FOUND. FABRICATED REPLACEMENT DOUBL ERS AND CLIP. INSTALLED PER STANDARD PRACTICES. (M) 2 L 7 4 4F RT A20WE 2001082800104 20010828 00104 NM 2001 8 28 UIEA01084 1 20010725 A 5730 SKIN BOEING 747 7472D3B 1384805 NM LT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 506MC 73880 21252 DURING INSPECTION, FOUND CORROSION INSIDE THE LEFT WING BOOST PUMP HOUSING AT WS 677 ON THE UPPER WING SKIN SURFACE LIP EXPOSED WITHIN THE HOUSING. CORROSION REMOVED, POLISHED, SHOT PEENED, TREATED AND MEASURED. AREA FILLED IN WITH EPOCAS T. ROTART DOOR LATCH CHANGED TO NYLON ASSEMBLY. (M) 2 L 7 4 4F RT A20WE 2001082800105 20010828 00105 NM 2001 8 28 UIEA01089 1 20010725 A 5320 65B1000843 FITTING BOEING 747 7472D3B 1384805 NM FUSELAGE CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 506MC 21252 DURING INSPECTION FOUND CORROSION AT BS 1480 LEFT AND RIGHT BULKHEAD CAP FITTINGS. CORROSION BLENDED PER SRM 51-10-01. PERFORMED HFEC OF BLENDED AREA TO INSURE CRACK AND CORROSION FREE. NO CRACKS OR CORROSION. MEASURED BLENDED AREAS. O VERSIZED EXISTING HOLES AND INSTALLED SLEEVED BOLTS IN HOLES. SPOT FACED HOLES TO REMOVE SURFACE CORROSION. FABRICATED FILLER WASHER TO MAINTAIN ORIGINAL THICKNESS. TREATED AND PRIME PAINTED AREA AND REPAIR FILLERS. REPLACED OUTER CHORD P/N 65B14681U3 ON BOTH LEFT AND RIHT SIDE. (M) 2 L 7 4 4F RT A20WE 2001082800106 20010828 00106 NM 2001 8 28 UIEA01091 1 20010726 A 5512 SKIN BOEING 747 7472D3B 1384805 NM HORIZ STAB CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 506MC 21252 DURING INSPECTION FOUND CORROSION ON HORIZONTAL STABILIZER SKIN PANELS RIGHT STAB STATION 160 LOWER SKIN FRONT SPAR, RIG HT STAB STATION 173 AT SPLICE STRINGER LOWER SKIN AFT PANEL, LEFT STAB STATION 173 SPLICE STRINGER LOWER FORWARD SKIN AN D AT LEFT STABILIZER STATION 165.75 UPPER FRONT SKIN PANEL. (M) 2 L 7 4 4F RT A20WE 2001082800107 20010828 00107 NM 2001 8 28 USAA010862 1 20010614 A 5320 SUPPORT BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 576US 43413 23741 PIT - FOUND CARGO PANEL SUPPORT ANGLE CORRODED 1 INCH BY 3 INCH, STATION 787 FROM S19L TO S24L. BLENDED PER 53-00-07. (M) 2 L 7 2 4F RT A16WE 2001082800108 20010828 00108 NM 2001 8 28 USAA010952 1 20010730 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 33083 24552 PIT - FOUND SIDE CHORD CRACKED 1.5 INCH, BS 178 LBL 24 WL 207. CUT OUT DAMAGED SECTION AND SPLICED IN NEW PER EO 5300V1 57. (M) 2 L 7 2 4F RT A16WE 2001082800109 20010828 00109 NM 2001 8 28 USAA010954 1 20010730 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 33083 24552 PIT - FOUND SIDE CHORD CRACKED 2 INCHES, BS 178 RBL 24 WL 207. CUT OUT DAMAGED SECTION AND SPLICED IN NEW PER EO 5300V1 57. (M) 2 L 7 2 4F RT A16WE 2001082800110 20010828 00110 NM 2001 8 28 USAA010955 1 20010731 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 533AU 40106 24515 PIT - FOUND BULKHEAD WITH HOLE .3125 INCH IN DIAMETER, BS 178 WL 209 LBL 27.75. OVERSIZED FASTENER HOLE TO REMOVE DAMAG E PER EA 71779. (M) 2 L 7 2 4F RT A16WE 2001082800111 20010828 00111 NM 2001 8 28 USAA010979 1 20010806 A 5320 STRAP BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 54141 22198 CLT - FOUND STABILIZER STRAP CRACKED 1 INCH, BS 560, LBL 42. FABRICATED AND INSTALLED DOUBLER AND FILLER PER EA 85163. (M) 2 L 7 2 4F RT A2NM 2001082800112 20010828 00112 NM 2001 8 28 USAA010990 1 20010806 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 54141 22198 CLT - FOUND SKIN CORRODED APPROXIMATELY 2 SQUARE INCHES, BS 580 BL 0. DAMAGED REMOVED, DOUBLER, TRIPLER, AND FILLER INST ALLED PER EA 85116 AND SRM 53-01-01, 53-40-08. (M) 2 L 7 2 4F RT A2NM 2001082800113 20010828 00113 NM 2001 8 28 USAA010992 1 20010806 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 54141 22198 CLT - FOUND SKIN CORRODED APPROXIMATELY 2 SQUARE INCHES, BS 620 BL 0. DAMAGED REMOVED, DOUBLER, TRIPLER AND FILLER INSTA LLED PER EA 85116. (M) 2 L 7 2 4F RT A2NM 2001082800114 20010828 00114 EU 2001 8 28 USAA01933 1 20010801 A 7110 23098023 NOSE COWL AIRBUS 330 A330323 EU LT ENGINE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 672UW 333 FOUND DAMAGE TO LEFT ENGINE NOSE COWLING. DURING PILOT WALKAROUND FOUND A 12 INCH CRACK 99 INCHES FROM GROUND AND A 5 I NCH CRACK 61 INCHES FROM GROUND ON LEFT SIDE OF THE LEFT ENGINE NOSE COWLING. COWLING REMOVED AND REPLACED WITH LIKE PA RT IAW 71-61-401 S/N OFF 771001-AH0155 S/N ON 771001-000133. (M) 2 L 7 2 4F RT A46NM 2001082800115 20010828 00115 NM 2001 8 28 USAABB01073 1 20010729 A 3350 873100151REV12 LIGHT BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 600AU 22192 LAX - FOUND FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001082800116 20010828 00116 WP 2001 8 28 RRXA010678 1 20010227 A 5220 GUARD DOUG DC8 DC871F 302199D WP PAX DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK IN 2 PLACES TO THE R-1 DOOR SILL GUARD, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SR M. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.#01-024 WITH APPROVED 8110 -3 DATED 02/15/01. 2 L 7 4 4F RT 4A25 2001082800117 20010828 00117 NM 2001 8 28 USAABB01083 1 20010813 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 600AU 22192 SFO - FOUND FLOOR LEVEL EMERGENCY LIGHT BATTERY PACKS LOW AT ROWS, 1, 4, 6, 9, 18, 23, 26, 29 AND 33. MAINTENANCE REPLA CED THE ASSOCIATED BATTERIES. (M) 2 L 7 2 4F RT A2NM 2001082800118 20010828 00118 WP 2001 8 28 USAAD01138 1 20010728 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 825US 49237 EWR - THE CEILING MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 12-15 WOULD NOT EXTINGUISH WITH THE SHIPS POWER OFF. MAINTENANC E REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (M) 2 L 7 2 4F A6WE 2001082800119 20010828 00119 WP 2001 8 28 RRXA010679 1 20010227 A 5730 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CENTER WING SKIN AT STA 960-980 X+45", DAMAGE EXCEEDED LIMITATI ONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-2 1 & 53-2-0 FIG. 1F. 2 L 7 4 4F RT 4A25 2001082800120 20010828 00120 WP 2001 8 28 USAAD01142 1 20010731 A 3231 DOOR DOUG DC9 DC981 3022081 WP NLG NOT CLOSED A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 802US 48036 TPA-PIT - FLT 302 - AFTER TAKEOFF AND THE LANDING GEAR WAS RETRACTED, THERE WAS A LOUD VIBRATION FROM THE NOSE WHEEL DOO RS. THE LANDING GEAR WAS CYCLED WITH THE SAME RESULTS. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR DOORS OPEN. ALL LINKAGE WAS INSPECTED ALONG WITH THE NOSE STRUT EXTENSION AND CONDITI ON OF THE NOSE WHEEL WELL. NO DISCEPANCIES WERE FOUND. THE NOSE GEAR DOORS WERE CLOSED AND THE DOOR MECHANISM WAS CHEC KED FOR PROPER OPERATION. (M) 2 L 7 2 4F A6WE 2001082800121 20010828 00121 WP 2001 8 28 RRXA010680 1 20010228 A 5730 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FUEL TANK PANEL LAND 506B AT STA XRS 110 TO 125 S-69 TO S-71, D AMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTAL LED IAW E.O. #01-024 WITH APPROVED 8110-3 DATED 01/29/01 AND DC-8 SRM 57-2-1 FIG.36. 2 L 7 4 4F RT 4A25 2001082800122 20010828 00122 WP 2001 8 28 RRXA010681 1 20010228 A 5320 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A 2.5 INCH CRACK INSIDE BATH TUB FITTING LWR HORIZ. SURFACE TO LT LONGERON 24 STA 860, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTA LLED IAW DC-8 SRM 53-2-0 & 53-2-2 FIG.5. 2 L 7 4 4F RT 4A25 2001082800123 20010828 00123 WP 2001 8 28 RRXA010682 1 20010228 A 5320 STRUCTURE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE CUSP RAIL AT STA 210-380 RT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001082800124 20010828 00124 WP 2001 8 28 RRXA010685 1 20010228 A 5330 HAND RAIL DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE SIDE RAIL AT STA 90-220 RT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. R EMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21 AND DC-8 SRM 51-1-4. 2 L 7 4 4F RT 4A25 2001082800125 20010828 00125 WP 2001 8 28 RRXA010891 1 20010325 A 5330 47731551 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE MISDRILLED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A DRILLED END FITTING AT RADIUS AT STA 1687 L21R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D AND DWG 4773155. 2 L 7 4 4F RT 4A25 2001082800126 20010828 00126 WP 2001 8 28 RRXA10507 1 20010222 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP COCKPIT DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND ELONGATED LOCK HOLES ON THE FE'S FWD SEAT TRACK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. REMOVED DAMAGE, TREATED AREAIAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001082800127 20010828 00127 WP 2001 8 28 RRXA10666 1 20010118 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND EXCESSIVE WEAR TO THE SEAT TRACK AT STA 70 X+45, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3 FIG.14 AND DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001082800128 20010828 00128 NM 2001 8 28 USAASB01200 1 20010707 A 3260 PROXIMITY SWITCH BOEING 737 737301 1384611 NM RT MLG DIRTY A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 19 558AU 23512 DCA - FLT 556 - ON DEPARTURE FROM TPA, EN ROUTE TO DCA, THE RIGHT MLG RED AND GREEN LIGHTS REMAINED ILLUMINATED AFTER GE AR RETRACTION AND GEAR LEVER IN OFF POSITION. CREW ACCOMPLISHED QUICK REF HANDBOOK PROCEDURES AND RECYCLED LANDING GEAR . CREW RECEIVED NORMAL GEAR INDICATION AND CONTINUED FLIGHT ONTO DCA. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTEN ANCE CHECKED THE RIGHT MLG AND DOWNLOCK PROXIMITY SWITCHES AND CLEANED. CHECKED LOGIC CARDS FOR THE RT MLG AND RESEATED . PINNED GEAR AND RAISED AND LOWERED GEAR HANDLE. GEAR INDICATION CHECKS GOOD. (M) 2 L 7 2 4F RT A16WE 2001082800129 20010828 00129 WP 2001 8 28 RRXA10742 1 20010312 A 5340 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND GOUGING DAMAGE TO RT. CANOE FITTING TOP FWD 3 INCHES AT RT. STA 340, DAMAGE EXCEEDED LI MITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. #01-0 24 WITH APPROVED 8110-3 DATED 02/26/01. 2 L 7 4 4F RT 4A25 2001082800130 20010828 00130 NM 2001 8 28 USAASB01203 1 20010716 A 2120 ODOR BOEING 737 7373B7 1384580 NM COCKPIT DETECTED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 19 517AU 23703 DAY - FLT 1661 - ON DESCENT FROM 10,000 FEET INTO DAY, FROM CLT, CAPTAIN DECLARED AN EMERGENCY DUE TO A STRONG ELECTRICA L SMOKE ODOR IN THE AFT CABIN. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RAN ENGINES, RAN AIR CONDITIONING P ACKS IN HIGH, BREWED COFFEE IN COFFEEMAKERS AND CHECKED FOR ODOR. NO ODOR NOTED. ALSO, CHECKED OVERHEAD LIGHTS. NO EL ECTRICAL SMOKE ODOR NOTED IN AFT CABIN. (M) 2 L 7 2 4F RT A16WE 2001082800131 20010828 00131 NM 2001 8 28 USAASB01216 1 20010730 A 3350 990835A BATTERY BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 248US 22755 BWI - THE EMERGENCY EXIT SIGN AT SEAT ROW 10 WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY SUPPLY ASSEMBLY. (M) 2 L 7 2 4F A16WE 2001082800132 20010828 00132 NM 2001 8 28 USAASB01217 1 20010730 A 3397 WIRE BOEING 737 7373B7 1384580 NM CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 EA 19 526AU 23861 EWR - MAINTENANCE FOUND THE AFT RED LIGHT IN THE FLOOR MOUNTED LOW LEVEL ESCAPE PATH LIGHT SYSTEM INOPERATIVE. MAINTENA NCE FOUND A BROKEN BLACK WIRE AT LIGHT SOCKET. SPLICED BROKEN WIRE. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001082800133 20010828 00133 WP 2001 8 28 RRXA10743 1 20010312 A 5330 PANEL DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO L/H STRESS PANEL AT KEEL BEAM, AT STA 740, DAMAGE EXCEEDED LIMITATI ONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4. 2 L 7 4 4F RT 4A25 2001082800134 20010828 00134 NM 2001 8 28 USAASB01228 1 20010811 A 3350 CONNECTOR BOEING 737 7373B7 1384580 NM CABIN DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 522AU 23857 TPA - MAINTENANCE FOUND THE EMERGENCY LIGHT AT SEAT ROW 6C INOPERATIVE. MAINTENANCE FOUND THE PLUG DISCONNECTED. RECON NECTED PLUG AND STOWED. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001082800142 20010828 00142 NM 2001 8 28 01FDEA00725 1 20010824 A 2170 COALESCER BAG BOEING 727 7272S2F 1384O81 NM A/C BAY DIRTY A FDEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 217FE 13395 ELECTRICAL SMELL IN COCKPIT FROM AIR COND VENTS. REMOVED AND REPLACED BOTH COALESCER BAGS PRECAUTIONARY PER MM 21-55-05 1-4. CND ODORS AT THIS TIME. 2 L 7 3 4F A3WE 2001082800151 20010828 00151 WP 2001 8 28 RRXA10745 1 20010301 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VIST FOUND ELONGATED HOLE DAMAGE TO SKIN AT FWD OF MLG DOORS, DAMAGE ECXEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 51-3-0. 2 L 7 4 4F RT 4A25 2001082800152 20010828 00152 WP 2001 8 28 RRXA10747 1 20010301 A 5542 SKIN DOUG DC8 DC871F 302199D WP RUDDER DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND HOLE DAMAGE TO SKIN AT HOLE 62 AND RUDDER POWER PACK LEDGE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND ISTALLED IAW SRM 51-1-4 AND DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001082800153 20010828 00153 WP 2001 8 28 RRXA10748 1 20010301 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND GOUGED AND DENTED DAMAGE TO SKIN AT STA.1890 AND TAIL POST SUPPORT, DAMAGE EXCEEDED LIM ITAIONS IAW DC-8 SRM. REMOVED DAMAGE AND TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-2-1 AND DC-8 SRM 53-2-0. 2 L 7 4 4F RT 4A25 2001082800161 20010828 00161 NM 2001 8 28 01FDEA00766 1 20010823 A 5340 FITTING DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 CENTER GEAR AIRFRAME SIDE LT PILLOW BLOCK FITTING HAS CORROSION PITTING AT MATING SURFACE AND GUIDE PIN HOLE. REMOVED AN D REPLACED PER SRM 53-40-00. 2 L 7 3 4F RT A22WE 2001082800162 20010828 00162 EU 2001 8 28 01FDEA00771 1 20010817 A 2910 HYDRAULIC LINE AIRBUS 310 A310200 3930310 EU HYDRAULIC SYS LEAKING A FDEA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 413FE 397 RDU GREEN HYD LOW LEVEL. ACCOMPLISH CKLIST AND DECLARED EMERGENCY. 2 L 7 2 4F RT A35EU 2001082800163 20010828 00163 NE 2001 8 28 ABXA010447 2 20010817 A 7200 ENGINE BOEING 767 767281 1385109 NM GE CF6 CF680A 30025 NE ENGINE VIBRATION A ABXA K NONE E VIBRATION/BUFFET CL CLIMB 1 GL 23 786AX 23019 CLIMB READING WAS 2.7, CRUISE READING WAS 1.3, ENGINE PARAMETERS NORMAL. OTHER INDICATION WAS AUDIBLE NOISE AND VIBRATI ON FOLLOWING THRUST CHANGE. CLEANED AND INSPECTED HOLD OPEN RODS FOR FAN COWL IAW B767 MM 77-11-10-2. VIBRATION LEVELS WERE FOUND TO BE WITHIN LIMITS PER ABX INFLIGHT AIRBORNE VIBRATION MONITORING GUIDELINE FOR B767/6E, CF680A ENGINE DATE D 03/27/2001. 2 L 7 2 4F 4 F RT A1NM E13NE 2001082800164 20010828 00164 WP 2001 8 28 RRXA10751 1 20010215 A 5720 PLATE DOUG DC8 DC871F 302199D WP NR 4 STUB WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO NR 4 STUB WING I/B LWR. FRONT SPAR L/E SHIM PLATE AT I/B LWR. FRONT SPA R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE AND TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.01-024 WITH APPROVED 8110-3 DATED 02/15/01. 2 L 7 4 4F RT 4A25 2001082800165 20010828 00165 WP 2001 8 28 RRXA10762 1 20010320 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND HOLE DAMAGE TO TAIL CONE SKIN AT STA.1902 AND RT 14 INCHES O/B AND 8 INCHES AFT OF ACCE SS DOOR NR 62, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED N EW PART AND INSTALLED IAW DC-8 SRM 51-1-5, DC-8 SRM 53-2-0, AND DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001082800166 20010828 00166 WP 2001 8 28 RRXA10763 1 20010326 A 5720 FITTING DOUG DC8 DC871F 302199D WP WING GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND GOUGE DAMAGE TO LT. WING CANOE FITTING AT STA.340, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. 01-024 WITH APPROVED 8 110-3 DATED 03/23/01. 2 L 7 4 4F RT 4A25 2001082800167 20010828 00167 WP 2001 8 28 RRXA10765 1 20010322 A 5310 DOOR FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO RT. MLG BODY DOOR AT AFT O/B CORNER FRAME, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. #01-024 WITH A PPROVED 8110-3 DATED 03/13/01. 2 L 7 4 4F RT 4A25 2001082800168 20010828 00168 WP 2001 8 28 RRXA10767 1 20010322 A 5513 SKIN DOUG DC8 DC871F 302199D WP HORIZONTAL STAB DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENCE VISIT FOUND HOLE DAMAGE TO HORZ STAB RT. ELEVATOR AT STA. XE 228.000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. 01-024 WITH APPRO VED 8110-3 DATED 02/25/01. 2 L 7 4 4F RT 4A25 2001082800169 20010828 00169 WP 2001 8 28 RRXA10768 1 20010319 A 5230 SKIN DOUG DC8 DC871F 302199D WP CARGO DOOR GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO A-PIT DOOR SEAL FRAME & DOOR SKIN AT THE A-PIT, DAMAGE EXCEEDED LIMITA TIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. 01-024 W ITH APPROVED 8110-3 DATED 03/13/01. 2 L 7 4 4F RT 4A25 2001082800170 20010828 00170 NE 2001 8 28 ABXA010448 2 20010824 A 7320 LINE DOUG DC9 DC941 302207N WP PWA JT8 JT8D15 52051 NE NR 2 ENGINE BROKEN A ABXA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 23 956AX 47620 DURING CRUISE, THE NR 2 ENGINE AT 240, A LOUD BANG OCCURRED WITH AN IMMEDIATE DROP IN THE EPR FROM 1.85 TO 1.60. N1 AND N2 DROPPED APPROXIMATELY 20 PERCENT FROM THE PREVIOUS SETTING. NO OTHER WARNING INDICATED. EMERGENCY DECLARED. AIR DI VERTED INTO STL. FOUND PS4 LINE AT THE TOP OF THE ENGINE BROKEN AT THE FITTING. REPLACED THE PS4 LINE PER REA D971-420 69. GROUND RAN ENGINE TO TAKEOFF POWER AND CHECKED ANTI-SURGE BLEED SCHEDULING IAW DC-9 AMM 71-00-00-5. ALL SYSTEMS OP S CHECKED GOOD. 2 L 7 2 4F 4 F A6WE E2EA 2001082800171 20010828 00171 WP 2001 8 28 RRXA10769 1 20010319 A 5320 BRACKET DOUG DC8 DC871F 302199D WP CARGO DOOR SEAL WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO A-PIT DOOR SEAL FRAME AT A-PIT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM . REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O 01-024 WITH APPROVED 8110-3 DATED 03/13/01. 2 L 7 4 4F RT 4A25 2001082800172 20010828 00172 WP 2001 8 28 ABXA010450 1 20010820 A 3260 0080004003 CONTROL BOX DOUG DC8 DC863 302198A WP E/E BAY DEFECTIVE A ABXA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 825AX 46115 RED GEAR UNSAFE LIGHT ILLUMINATED. LANDING GEAR AND DOOR LATCHING SELECTOR INDICATED RIGHT MAIN DOOR UNLATCHED. FOLLOW ED ABNORMAL PROCEDURE AND ALL INDICATIONS RETURNED TO NORMAL. REPLACED THE GEAR PROXIMITY CONTROL BOX IAW DC-8 MM 32-10 -00. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 2001082800173 20010828 00173 WP 2001 8 28 RRXA10770 1 20010319 A 5310 SKIN DOUG DC8 DC871F 302199D WP DOOR FRAME CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGED TO A-PIT DOOR SEAL FRAME WORN/CRACKED OUT INCLUDING SKIN--LOC CENTER SECT ION OF DOOR AT A-PIT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRI CATED REPAIR AND INSTALLED IAW E.O. 01-024 WITH APPROVED 8110-3 DATED 03/13/01. 2 L 7 4 4F RT 4A25 2001082800174 20010828 00174 WP 2001 8 28 RRXA10771 1 20010416 A 3260 7000010202 SWITCH DOUG DC8 DC871F 302199D WP MLG FAILED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND UNSAFE LIGHT DAMAGE TO LT MLG UNSAFE LIGHT (RED) STAYS ON & NO L/H MLG GREEN LIGHT AFTE R SEVERAL GEAR CYLES, GOT GREEN LIGHT ONLY AFTER STEEP BANKS AT LT. SIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REM OVED DAMAGE, TREATED IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 MM 32-60-0 AND DC-8 MM 32-20-00. 2 L 7 4 4F RT 4A25 2001082800175 20010828 00175 WP 2001 8 28 ABXA010451 1 20010821 A 3241 420531B CONTROL BOX DOUG DC8 DC861 3021952 WP E/E BAY DEFECTIVE A ABXA O OTHER O OTHER LD LANDING 1 GL 23 843AX 46017 DURING LANDING ROLLOUT, ANTI-SKID FELT TO BE CYCLING IN EXCESS. DURING TAXI, WITH ANTI-SKID ARMED AND TAXI SPEEDS APPRO XIMATELY 10 KNOTS, BRAKES SEEMED TO LOOSE EFFECTIVENESS AND MAY BE RELEASING INTERMITTENTLY. REPLACED THE ANTI-SKID CON TROL BOX IAW DC-8 MM 32. OPS CHECKED GOOD. CYCLED BRAKES SEVERAL TIMES, CHECKED GOOD. 2 L 7 4 4F 4A25 2001082800176 20010828 00176 WP 2001 8 28 ABXA010452 1 20010823 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 956AX 47620 EMERGENCY EVACUATION LIGHTS WOULD NOT TEST. REPLACED THE EMERGENCY LIGHTS BATTERIES. OPS CHECKED GOOD IAW DC-9 AMM 33- 53-02-4. 2 L 7 2 4F A6WE 2001082800177 20010828 00177 WP 2001 8 28 RRXA10773 1 20010317 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING TOOL DAMAGE A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND TOOLING MARK DAMAGE TO LWR. WING SKIN UPPER SURFACE AT STA. XRS 507.625 AND STR. 54, DA MAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALL ED IAW E.O. 01-024 WITH APPROVED 8110-3 DATED 03/09/01. 2 L 7 4 4F RT 4A25 2001082800178 20010828 00178 WP 2001 8 28 RRXA10778 1 20010122 A 5755 5769581501 PANEL DOUG DC8 DC871F 302199D WP LT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LT WING I/B SLOT PANEL AT LT I/B SLOT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. PEMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2001082800179 20010828 00179 WP 2001 8 28 ABXA010453 1 20010823 A 2133 REGULATOR VALVE DOUG DC9 DC932F 3022067 WP A/C BAY STUCK A ABXA G O2 MASK DEPLOYED O OTHER CR CRUISE 1 GL 23 904AX 47040 CABIN PRESSURIZATION WOULD NOT HOLD 5.4 PSI AT FL250, WOULD NOT HOLD MAX DIFFERENTIAL. WITH ENGINE ANTI-ICE ON, WOULD N OT HOLD CABIN BELOW 10,000 FEET. PNEUMATIC PRESSURE GAUGE INDICATED 30 PSI IN CRUISE WITH PNEUMATIC CROSSFEEDS CLOSED. AFTER PRESSURE WAS BLEED OFF WITH AIRFOIL ANTI-ICE, THE 30 POUNDS OF PNEUMATIC PRESSURE RETURNED IN APPROXIMATELY 10 SE CONDS. CREW DONNED THEIR OXYGEN MASKS DUE TO THE CONDITION. FOUND THE LEFT AIR CONDITIONING PRESSURE REGULATOR VALVE S TUCK OPEN. REPLACED THE LEFT AIR CONDITIONING PRESSURE REGULATOR VALVE IAW DC-9 MM 21-31-01-2-0003. 2 L 7 2 4F A6WE 2001082800180 20010828 00180 WP 2001 8 28 RRXA10779 1 20010122 A 5755 VANE DOUG DC8 DC871F 302199D WP LT WING DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND ELONGATED HOLE DAMAGE TO LT WING O/B SLOT VANE AT O/B SIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-4 AND DC-8 SRM 57-2-1 AND DC-8 SRM 51-1-16. 2 L 7 4 4F RT 4A25 2001082800181 20010828 00181 SO 2001 8 28 C2XA01IA338 1 20010827 A 5315 14522226003 FLOORBEAM EMB 145 EMB145LR SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12957 145080 IAH - DURING C-CHECK INSPECTION, THE CENTER FLOORBEAM FROM FRAME 59 TO 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF FLOORBEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001082800182 20010828 00182 SO 2001 8 28 C2XA01IA339 1 20010827 A 5315 14522461003 FLOORBEAM EMB 145 EMB145LR SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12957 145080 IAH - DURING C-CHECK INSPECTION, THE RIGHT HAND FLOORBEAM AT FRAME 20 TO FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF FLOORBEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001082800183 20010828 00183 SO 2001 8 28 C2XA01IA341 1 20010827 A 5510 14524979001 BUSHING EMB 145 EMB145LR SO HORIZ STAB CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12957 145080 IAH - DURING C-CHECK INSPECTION, THE HORIZONTAL STABILIZER SLIDING BUSHINGS WERE FOUND TO BE CORRODED. MAINTENANCE REMO VED AND REPLACED THE AFFECTED BUSHINGS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001082800184 20010828 00184 SO 2001 8 28 C2XA01IA342 1 20010827 A 5510 14524979001 BEARING EMB 145 EMB145LR SO HORIZ STAB CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12957 145080 IAH - DURING C-CHECK INSPECTION, THE LEFT HAND AND RIGHT HAND HORIZONTAL STABILIZER SPHERICAL BEARING HOUSINGS WERE FOUN D TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEARINGS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO S ERVICE. 2 L 7 2 4T RT T00011AT 2001082800185 20010828 00185 WP 2001 8 28 RRXA10782 1 20010117 A 5730 SKIN DOUG DC8 DC871F 302199D WP WING DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND ELONGATED HOLE DAMAGE TO SEVERAL L/E FASTENERS THRU EDGE OF SKIN AT STA. XFS 470, DAMAG E EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0 AND DC-8 SRM 51-1-4 AND DC-8 SRM 57-2-1. 2 L 7 4 4F RT 4A25 2001082800186 20010828 00186 SO 2001 8 28 C2XA01IA343 1 20010825 A 2120 SMOKE EMB 135 EMB135ER 3260203 SO CABIN DETECTED A C2XA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 SW 27 14514 135303 CLL - FLIGHT 4134 THE CREW REPORTED A LAV SMOKE WARNING AND AND VISIBLE SMOKE PRESENT ON APPROACH TO IAH. THE AIRCRAFT WAS DIVERTED TO CLL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, GROUND RAN BOTH PACKS FROM EN GINE BLEED AND APU BLEED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001082800187 20010828 00187 WP 2001 8 28 RRXA10783 1 20010124 A 4980 EXHAUST GATE DOUG DC8 DC871F 302199D WP APU CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO RT EXHAUST GATE T/E AT GATE T/E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20C AND E.O.01-00 6 WITH APPROVED 8110-3 DATED 01/12/01. 2 L 7 4 4F RT 4A25 2001082800188 20010828 00188 SO 2001 8 28 C2XA01IA344 1 20010823 A 2120 RAM AIR DOOR EMB 120 EMB120ER 3260203 SO FUSELAGE OPEN A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 15732 120195 IAH - FLIGHT 3561, THE CREW REPORTED SMOKE IN THE COCKPIT AFTER TAKEOFF. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED W ITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE RAM AIR DOORS TO BE IN THE OPEN POSITION. MAINTENANC E CLOSED THE RAM AIR DOORS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001082800189 20010828 00189 SO 2001 8 28 C2XA01IA345 1 20010827 A 2911 884240011 ACCUMULATOR EMB 120 EMB120ER 3260203 SO MLG WW DISCHARGED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 16718 120136 IAH - FLIGHT 3518, THE CREW REPORTED THAT THE LEFT MAIN LANDING GEAR WOULD NOT RETRACT UNLESS CYCLED TWICE. THE AIRCRAF T RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE SERVICED THE MAIN LANDING GEAR ACCUMULATOR, AND THE AIR CRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001082800190 20010828 00190 WP 2001 8 28 RRXA10784 1 20010209 A 5730 SKIN DOUG DC8 DC871F 302199D WP NR 3 STUB WING DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND ELONGATED HOLE DAMAGE TO WING L/E AT NR 3 ENGINE PYLON, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O 01-006 WITH APPROV ED 8110-3 DATED 01/10/01. 2 L 7 4 4F RT 4A25 2001082800191 20010828 00191 SO 2001 8 28 C2XA01IA346 1 20010824 A 2150 A/C PACK EMB 145 EMB145LR SO A/C BAY MALFUNCTIONED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 15912 145439 SAV - FLIGHT 3925, THE CREW REPORTED A STRONG BURNING SMELL WITH SOME SMOKE IN THE AIRCRAFT. THE AIRCRAFT LANDED AT SAV WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE NUMBER TWO PACK ON MEL 21-51-00 CAT-C CONTROL NUMBER 014914, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001082800192 20010828 00192 WP 2001 8 28 RRXA10792 1 20010104 A 5755 56551662 PANEL DOUG DC8 DC871F 302199D WP NR 2 SPOILER MISREPAIRED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND IMPROPER REPAIR TO RT NR 2 SPOILER AT NR 2 RT SPOILER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FEBRICATED REPAIR AND INSTALLED IAW DC-8 MM 27-61-1. 2 L 7 4 4F RT 4A25 2001082800193 20010828 00193 WP 2001 8 28 RRXA10795 1 20010115 A 5753 SKIN DOUG DC8 DC871F 302199D WP RT WING TE FLAP DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND HOLE DAMAGE TO RT. WING I/B FLAP LWR. SURFACE AT RT WING I/B FLAP BEHIND NR 7 TIRE, DAM AGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED IAW DC-8 SRM 51-1-8. FRABICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-1 FIG. 2Q AND DC-8 SRM 51-1-21A. 2 L 7 4 4F RT 4A25 2001082800194 20010828 00194 GL 2001 8 28 C2XA01TY102 2 20010825 A 7200 23070401 ENGINE EMB 145 EMB145 SO ALLSN AE300 AE3007A GL RIGHT MALFUNCTIONED A C2XA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 27 22971 7093 7093 145149 CAE311058 AVL FLIGHT 3664. CREW REPORTED THAT THEY RECEIVED ENGINE NR 2 ATTCS NO MARGIN MESSAGE ON TAKE-OFF ROLL. MAINTENANCE I NSPECTED THE ENGINE AND AFTER SEVERAL ATTEMPTS TO CORRECT THE DISCREPANCY THE AIRCRAFT WAS FERRIED TO TYS. THE RIGHT HA ND ENGINE WAS REMOVED AND REPLACED IAW CONTINENTAL EXPRESS TASK CARD 6271001, ALL OPERATIONAL AND LEAK CHECKS WERE SATIS FACTORY. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001082800195 20010828 00195 WP 2001 8 28 CALA0100790 1 20010824 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND RT CABIN FLOOR PANEL CREASED AT FS 466-542. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265. 2 L 7 2 4F A6WE 2001082800196 20010828 00196 WP 2001 8 28 RRXA10797 1 20010130 A 5730 PANEL DOUG DC8 DC871F 302199D WP RT WING MISDRILLED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND HOLE DAMAGE TO RT WING LWR FUEL TANK ACCESS PANEL AT PANEL 514I, DAMAGE EXCEEDED LIMITA TIONS IAW DC-8 SRM. REMOVED DAMAGE,TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.#01-006 WI TH APPROVED 8110-3 DATED 01/17/01. 2 L 7 4 4F RT 4A25 2001082800197 20010828 00197 WP 2001 8 28 CALA0100795 1 20010824 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND CUSP WEB CRACKED AND CORRODED AT FS 218-239, LBL 44 TO LBL 55. THE WEB WAS REMOVED AND A NEW WEB WAS I NSTALLED IAW SRM 51-30-2, 51-10-3, AND 51-30-5. 2 L 7 2 4F A6WE 2001082800198 20010828 00198 WP 2001 8 28 RRXA10799 1 20010209 A 5730 SKIN DOUG DC8 DC871F 302199D WP NR 4 STUB WING DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND ELONGATION DAMAGE TO NR 4 STUB WING L/E AT FWD OF SLOT PANEL, DAMAGE EXCEEDED LIMITATIO NS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-20 A AND E.O. 01-006 WITH APPROVED 8110-3 DATED 01/15/01. 2 L 7 4 4F RT 4A25 2001082800199 20010828 00199 NM 2001 8 28 CALA0100796 1 20010825 A 3350 20121 CHARGER BOEING 737 7373T0 1384582 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12318 23369 INSPECTION FOUND EMERGENCY EXIT LIGHT INOPERATIVE AT LT WING TRAILING EDGE. THE CHARGER AND BATTERY ASSEMBLY WAS REMOVE D AND REPLACED AND OPERATION CHECKED GOOD. 2 L 7 2 4F RT A16WE 2001082800200 20010828 00200 WP 2001 8 28 RRXA10807 1 20010221 A 5410 PLATE DOUG DC8 DC871F 302199D WP NR 3 PYLON CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO WING L/E SHIM PLATE AT I/B NR3 ENG. PYLON, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.#01-006 WITH AP PROVED 8110-3 DATED 02/19/01. 2 L 7 4 4F RT 4A25 2001082800201 20010828 00201 WP 2001 8 28 RRXA10813 1 20010213 A 5523 SKIN DOUG DC8 DC871F 302199D WP RT ELEVATOR TAB DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND DAMAGE TO RT. ELEVATOR CONTROL TAB AT O/B CORNER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. 01-006 WITH APPROVED 81 10-3 DATED 02/01/01 AND DC-8 SRM 51-20-0. 2 L 7 4 4F RT 4A25 2001082800202 20010828 00202 WP 2001 8 28 RRXA10818 1 20010116 A 5230 DOUBLER DOUG DC8 DC871F 302199D WP CARGO DOOR BENT A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND BENT DAMAGE TO A-PIT DOOR CUTOUT AT UPPER AFT ADGE, DAMAGE EXCEEDED LIMITATIONS IAW DC- 8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLEDM IAW DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001082800203 20010828 00203 WP 2001 8 28 RRXA10820 1 20010112 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND IMPROPER REPAIR DAMAGE TO D-PIT DOOR KICK PLATE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001082800204 20010828 00204 WP 2001 8 28 RRXA10822 1 20010124 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND EXCESSIVE WEAR DAMAGE TO SEAT TRACK AT STA. 140-160 X+45, DAMAGE EXCEEDED LIMITATIONS I AW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001082800205 20010828 00205 WP 2001 8 28 RRXA10823 1 20010124 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND EXCESSIVE WEAR DAMAGE TO SEAT TRACK AT STA. 260-280 X+45, DAMAGE EXCEEDED LIMITATIONS I AW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001082800206 20010828 00206 WP 2001 8 28 CALA0100801 1 20010825 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND A .5 INCH CRACK IN TAIL COMPARTMENT LEFT VENT BOX FORWARD UPPER SUPPORT ANGLE. THE SUPPORT ANGLE WAS R EMOVED AND A NEW SUPPORT ANGLE WAS INSTALLED IAW SRM 51-30-0. 2 L 7 2 4F A6WE 2001082800207 20010828 00207 WP 2001 8 28 RRXA10824 1 20010124 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND EXCESSIVE WEAR DAMAGE TO SEAT TRACK AT STA. 240 X+25, DAMAGE EXCEEDED LIMITATIONS IAW D C-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-21 AND DC-8 SR M 51-3-0. 2 L 7 4 4F RT 4A25 2001082800208 20010828 00208 WP 2001 8 28 RRXA10826 1 20010117 A 5320 PLATE DOUG DC8 DC871F 302199D WP CARGO THRESHOLD CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO B-PIT DOOR KICK PLATE AT B-PIT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SR M. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW E.O.01-006 WITH APPROVED 8110-3 DATED 01/12/01. 2 L 7 4 4F RT 4A25 2001082800209 20010828 00209 NM 2001 8 28 CALA0100804 1 20010825 A 5345 MOUNT BOEING 737 7373T0 1384582 NM GALLEY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND GALLEY FLOOR MOUNT CORRODED AT STA 292, RBL 12. A NEW GALLEY FLOOR MOUNT WAS INSTALLED IAW SRM 51-10-0 2. 2 L 7 2 4F RT A16WE 2001082800210 20010828 00210 CE 2001 8 28 GLBA2001189 1 20010827 A 7700 311701101A BLEED VALVE BEECH 1900 1900D 1154162 CE RIGHT ENGINE WORN A GLBA A UNSCHED LANDING O OTHER TO TAKEOFF 1 CE 01 184GL 1669 UE184 RIGHT ENGINE TEMP LIMITED ON T/O, INSPECTED FOOUND BLEED VALVE FAULTY, REPLACED OPS CHECKED SYSEM SATISFACTORY 2 L 7 2 4T RT A24CE 2001082800211 20010828 00211 NM 2001 8 28 CALA0100807 1 20010826 A 3397 WIRE BOEING 737 737524 1384721 NM CABIN SHORTED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 24633 27901 THE EMERGENCY AISLE LIGHTING AT ROWS 5-9 LEFT WOULD NOT ILLUMINATE DURING TEST. MAINTENANCE FOUND SEAT 8 MOUNTED EMERGE NCY LIGHT WIRING SHORTED. THE SHORTED SECTION OF WIRING WAS REPAIRED IAW WDM 33-51-41. 2 L 7 2 4F RT A16WE 2001082800212 20010828 00212 EU 2001 8 28 DHL2001363019 1 20010825 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU CABIN MALFUNCTIONED A DHLA O OTHER N FALSE WARNING IN INSP/MAINT 1 SO 01 363DH 85 SMOKE DETECTOR R5 ILLUMINATED IN BLOCKS. COOLED CABIN. RESEATED C/B. SYSTEM OPS CHECKED NORMAL PER 26-14-00. 2 L 7 2 4F RT A35EU 2001082800213 20010828 00213 EU 2001 8 28 DHL2001365033 1 20010824 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU EQUIP BAY INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 365DH 149 MINIMUM EQUIPMENT BAY SMOKE DETECTOR WILL NOT TEST. REMOVED AND REPLACED MINIMUM EQUIPMENT BAY SMOKE DETECTOR IAW AMM 2 6-11-12. OPS CHECKED SERVICEABLE. 2 L 7 2 4F RT A35EU 2001082800214 20010828 00214 EU 2001 8 28 DHL2001365034 1 20010825 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU CABIN ACTIVATED A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 365DH 149 THREE CABIN SMOKE DETECTORS ILLUMINATED AFTER TAKEOFF WITH MASTER WARNING SMOKE LIGHT AND CHIME. PERFORMED FUNCTIONAL T EST OF MAIN DECK SMOKE DETECTION SYSTEM IAW AMM SUP A300 PAX-FREIGHTER CONVERSION MANUAL. OPS CHECKED SERVICEABLE. NO DEFECTS NOTED IAW 26-11-0. 2 L 7 2 4F RT A35EU 2001082800215 20010828 00215 WP 2001 8 28 MWEA011149 1 20010827 A 5310 992345311 FRAME DOUG DC9 DC932 3022066 WP STATION 637 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 KEEL BEAM AREA LEFT SIDE, FRAME STATION 637 END CLIP HAS A CRACK ON OUTBOARD END. -- REMOVED AND REPLACED FRAME SEGMEN T. 2 L 7 2 4F A6WE 2001082800216 20010828 00216 WP 2001 8 28 MWEA011151 1 20010827 A 5310 99577403 ANGLE DOUG DC9 DC932 3022066 WP STATION 622 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 KEEL BEAM AREA RIGHT SIDE, FRAME STATION 622 IS CRACKED ON OUTBOARD END. -- FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F A6WE 2001082800217 20010828 00217 WP 2001 8 28 MWEA011156 1 20010827 A 5310 99581673 INTERCOSTAL DOUG DC9 DC932 3022066 WP STATION 899 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 AFT CARGO BAY HAS A DENTED INTERCOSTAL BETWEEN FLOOR BEAMS 899 AND 918 AT AIRCRAFT CENTER LINE. -- FABRICATED AND INST ALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001082800218 20010828 00218 WP 2001 8 28 MWEA011157 1 20010827 A 5310 3912239511 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP STATION 408 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FORWARD CARGO COMPARTMENT FRAME AND FLOOR SUPPORT HAVE A CRACK AT STATION 408 AT LONGERON 26 LEFT. -- FABRICATED AND I NSTALLED SPLICED REPAIR. WELDED AND INSTALLED FLOOR SUPPORT. 2 L 7 2 4F A6WE 2001082800219 20010828 00219 WP 2001 8 28 MWEA011159 1 20010827 A 5310 9915558235 CLIP DOUG DC9 DC932 3022066 WP STATION 996 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 TIE CLIP CRACKED THAT ATTACHES HORIZONTAL STIFFENER TO APB AT LONGERON LEFT 15 STATION 996. -- REMOVED AND REPLACED TI E CLIP. 2 L 7 2 4F A6WE 2001082800220 20010828 00220 WP 2001 8 28 MWEA011160 1 20010827 A 5310 9915558237 CLIP DOUG DC9 DC932 3022066 WP STATION 996 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 TIE CLIP CRACKED THAT ATTACHES HORIZONTAL STIFFENER TO AFT PRESSURE BULKHEAD BETWEEN LONGERONS 15 LEFT AND 16 LEFT STATI ON 996. -- REMOVED AND REPLACED NEW TIE CLIP. 2 L 7 2 4F A6WE 2001082800221 20010828 00221 WP 2001 8 28 MWEA011161 1 20010827 A 5310 9915558241 CLIP DOUG DC9 DC932 3022066 WP STATION 996 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 TIE CLIP CRACKED THAT ATTACHES HORIZONTAL STIFFENER TO AFT PRESSURE BULKHEAD BETWEEN LONGERONS 16 LEFT AND 17 LEFT STATI ON 996. -- REMOVED AND REPLACED TIE CLIP. 2 L 7 2 4F A6WE 2001082800222 20010828 00222 WP 2001 8 28 MWEA011163 1 20010827 A 5310 591013046N SHEAR TIE DOUG DC9 DC932 3022066 WP STATION 996 OUT OF TOLERANCE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 AFT CARGO BAY STATION 996 SHEAR TIE IS BLENDED OUT OF LIMITS BETWEEN LONGERON 23 TO 26 RIGHT. -- REMOVED AND REPLACED SHEAR TIE. 2 L 7 2 4F A6WE 2001082800223 20010828 00223 WP 2001 8 28 MWEA011165 1 20010827 A 5310 9915558257 FORMER DOUG DC9 DC932 3022066 WP STATION Z14 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 ON FORWARD SIDE OF AFT PRESSURE BULKHEAD, LEFT SIDE FORMER AT STATION Z14 HAS CRACK AT OUTBOARD END. -- REMOVED AND RE PLACED FORMER. 2 L 7 2 4F A6WE 2001082800224 20010828 00224 WP 2001 8 28 MWEA011166 1 20010827 A 5310 9915558141 FORMER DOUG DC9 DC932 3022066 WP STATION Z34 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 AFT PRESSURE BULKHEAD FORMER ON LEFT SIDE STATION Z34 IS CRACKED ON OUTBOARD END. (FORWARD SIDE OF APB). -- REMOVED AND REPLACED FORMER. 2 L 7 2 4F A6WE 2001082800225 20010828 00225 WP 2001 8 28 MWEA011167 1 20010827 A 5310 9915558145 FORMER DOUG DC9 DC932 3022066 WP STATION Z24 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 ON FORWARD SIDE OF AFT PRESSURE BULKHEAD, LEFT SIDE STATION Z24 FORMER IS CRACKED ON OUTBOARD EDGE. -- FABRICATED AND INSTALLED FORMER. 2 L 7 2 4F A6WE 2001082800226 20010828 00226 WP 2001 8 28 MWEA011168 1 20010827 A 5230 59101573 DOUBLER DOUG DC9 DC932 3022066 WP CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 AFT CARGO DOOR OUTER SKIN HAS SEVERAL CHAFED AREAS ALONG AND ABOVE #4 BEAM LINE. -- FABRICATED AND INSTALLED SKIN REPA IR. 2 L 7 2 4F A6WE 2001082800227 20010828 00227 WP 2001 8 28 MWEA011169 1 20010827 A 5230 59101573 DOUBLER DOUG DC9 DC932 3022066 WP CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 AFT CARGO DOOR OUTER SKIN IS CHAFED ON BACK SIDE BETWEEN BEAMS #2 & #3 FORWARD EDGE. -- FABRICATED AND INSTALLED REPAI R DOUBLER. 2 L 7 2 4F A6WE 2001082800228 20010828 00228 WP 2001 8 28 MWEA011171 1 20010827 A 5230 59101573 DOUBLER DOUG DC9 DC932 3022066 WP GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 AFT CARGO DOOR, OUTER SKIN, 4 INCHES FORWARD OF AFT EDGE AT BEAM #4 SKIN IS GOUGED. -- FABRICATED AND INSTALLED REPAIR DOUBLER AND SHIMS. 2 L 7 2 4F A6WE 2001082800229 20010828 00229 WP 2001 8 28 MWEA011174 1 20010827 A 5330 59568791 DOUBLER DOUG DC9 DC932 3022066 WP STATION 160 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 PAX DOOR JAMB LOWER FORWARD CORNER AT STATION 160, WEB CRACKED. -- FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001082800230 20010828 00230 WP 2001 8 28 MWEA011176 1 20010827 A 5330 99100785 DOUBLER DOUG DC9 DC932 3022066 WP STATION 218 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FLOOR WEB IS CRACKED AT STATION 218, 1/2 INCH UNDER AND 3 INCH OUTBOARD OF #3 SEAT TRACK. -- FABRICATED AND INSTALLED FILLER AND DOUBLER. 2 L 7 2 4F A6WE 2001082800231 20010828 00231 WP 2001 8 28 MWEA011177 1 20010827 A 5330 9911842117 DOUBLER DOUG DC9 DC932 3022066 WP STATION 1132 CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 SKIN CHAFED AT RIGHT GUSSET, AT STATION 1132. -- FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001082800232 20010828 00232 WP 2001 8 28 MWEA011178 1 20010827 A 5330 5910228137 DOUBLER DOUG DC9 DC932 3022066 WP STATION 1097 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 LIGHTNING STRIKE AT CANTED STATION 1097 LONGERON 11 LEFT. -- FABRICATED AND INSTALLED REPAIR DOUBLER AND INSTALLED COU NTERSINK FILLERS. 2 L 7 2 4F A6WE 2001082800233 20010828 00233 WP 2001 8 28 MWEA011179 1 20010827 A 5330 99101516 DOUBLER DOUG DC9 DC932 3022066 WP STATION 598 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 CABIN SUBFLOOR IS CRACKED AT STATION 598 RIGHT SIDE. -- FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001082800234 20010828 00234 WP 2001 8 28 MWEA011180 1 20010827 A 5340 3916209502 SEAT TRACK DOUG DC9 DC932 3022066 WP STATION 680 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 #4 SEAT TRACK ATTACHMENT FITTING IS CRACKED AT STATION 680. -- REMOVED AND REPLACED SEAT TRACK FITTING. 2 L 7 2 4F A6WE 2001082800235 20010828 00235 WP 2001 8 28 MWEA011150 1 20010827 A 5310 3924029 CLIP DOUG DC9 DC932 3022066 WP STATION 609 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 KEEL BEAM FORWARD END CLIP ON, LEFT SIDE IS CRACKED AND FASTENER HEAD IS SHEARED OFF, LOCATED AT STATION 609 BOTTOM END. -- FABRICATED AND INSTALLED FITTING/CLIP. 2 L 7 2 4F A6WE 2001082800236 20010828 00236 EU 2001 8 28 DHL2001366023 1 20010826 A 2620 RELAY AIRBUS 300 A300B4203 3930306 EU EXTINGUISH SYS FAILED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 366DH 249 DURING APU FIRE EXTINGUISHING CIRCUIT OPERATIONAL CHECK, STEP C: APU AUTO EXTINGUISHING CIRCUIT DOES NOT PASS. DEFERRED APU AUTO FIRE SHUTDOWN SYSTEM. REMOVED AND REPLACED 32WF RELAY ON 250VU. SYSTEM OPERATIONAL CHECKED OK IAW MM 26-22-00 . 2 L 7 2 4F RT A35EU 2001082800237 20010828 00237 EU 2001 8 28 DHL2001366024 1 20010828 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU CABIN MALFUNCTIONED A DHLA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 366DH 249 FOLLOWING THE SMOKE DETECTOR TEST, ONE TO TWO ZONE LIGHTS REMAINED ILLUMINATED. COOLED AIRCRAFT. CABIN SYSTEM OPERATIO NALLY CHECKED GOOD PER M/M SUPP 26-11-0. 2 L 7 2 4F RT A35EU 2001082800239 20010828 00239 NM 2001 8 28 2001UALA01750 1 20010819 A 5300 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 516UA 24860 CABIN FLOOR INNER CREASE BEAM BELOW DOR 2L DRAIN GUTTER HAS EXCESSIVE CORROSION STA.700 TO 720 LBL70" STRINGER 17L. MAJ OR REPAIR ACCOMPLISHED. REMOVED SECTION OF INNER CREASE BEAM L-ANGLE Z ANGLE IN DOORWAY FROM STA.665 TO 754 AT FACTORY S PLICES INSTALLED NEW PART. 2 L 7 2 4F 4 F RT A2NM E17NE 2001082800240 20010828 00240 NM 2001 8 28 2001UALA01751 1 20010817 A 5315 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 516UA 24860 RIGHT HAND CABIN FLOOR WEB BETWEEN INNER AND OUTER CREASE BEAM CORD WAS CORODED AT STA 1021 RBL 68. MAJOR REPAIR ACCOMP LISHED. MANUFACTURED REPLACEMENT WEB FROM 7075-0 HEAT TREATED TO T6 INSTALLED NEW WEB BETWEEN STA.1020-1039 RBL68 STRING ER 17R. 2 L 7 2 4F 4 F RT A2NM E17NE 2001082800241 20010828 00241 NM 2001 8 28 2001UALA01755 1 20010818 A 3350 582213 POWER SUPPLY BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 EMERGENCY ESCAPE PATH LIGHTS COME ON INTERMITENTLY RIGHT SIDE IN BUSINESS AND FIRST CLASS. SUPPLEMENTAL DATA UPDATE REP LACED EMERGENCY ESCAPE PATH POWER SUPPLY M9030, OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082800242 20010828 00242 NM 2001 8 28 2001UALA01765 1 20010821 A 5310 6516318101 FRAME BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7261U 21408 RIB INTERCOSTAL STATION 360 IS CRACKED LENGTHWISE, AND STRINGER SUPPORT UNDER INTERCOSTAL IS BENT. SUPPLEMENTAL DATA UP DATE REPAIRED FRAME AT BS 380 BETWEEN STRINGERS S15 AND S16 AT THE ASSOCIATED SKIN ATTACHMENT.MAJOR REPAIR ACCOMPLISHED 2 L 7 3 4F 4 F A3WE E2EA 2001082800243 20010828 00243 2001 8 28 2001UALA01766 4 20010821 A 2565 PLUG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 LEFT EMERGENCY ESCAPE SQUIB DID NOT TEST IN TEST 1. ALL TEST IN TEST 2. FOUND CANNON PLUG ON SQUIB LOOSE, REINSTALLED CANNON PLUG, AND PERFORMED SQUIB TEST. TESTED NORMAL IN BOTH LEFT AND RIGHT IN TEST 1 AND 2. 2 L 7 2 4F 4 F RT A2NM E17NE 2001082800244 20010828 00244 2001 8 28 2001UALA01767 4 20010818 A 2565 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 545UA 25323 LEFT EMERGENCY ESCAPE SLIDE SQUIB TEST FAILED IN #1 TEST POSITION. CLEANED TEST SWITCH, SLIDE SQUIB CHECK OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2001082800245 20010828 00245 NM 2001 8 28 2001UALA01773 1 20010822 A 2910 HOSE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE KINKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 511UA 24799 #2 ENGINE MAIN HYDRAULIC SUPPLY LINE, FROM FIREWALL TO RIGID LINES FOUND TWISTED AND KINKED WITH APPROXIMATELY 3/4 TWIS T AND COLLAPSED BENEATH SHIELDING. REPLACED HYDRAULIC SUPPLY LINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001082800246 20010828 00246 NM 2001 8 28 2001UALA01783 1 20010822 A 5320 CLIP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE BODY STATION 347 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION STRINGER 37R ATTACH CLIP CRACKED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTAL LED ATTACH CLIP IN ACCORDANCE WITH BAC DWG 141T3220. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082800247 20010828 00247 NM 2001 8 28 2001UALA01787 1 20010822 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE BODY STATION 527 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 527 STRINGER 34L CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STR INGER SPLICE REPAIR IN ACCORDANCE WITH SRM 53-00-03. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090600381 20010906 00381 NM 2001 9 6 2001UALA01794 1 20010823 A 5320 SPLICE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BS 434 STRINGER 39L SPLICE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER SPLICE REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090600382 20010906 00382 NM 2001 9 6 2001UALA01795 1 20010823 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1080-1087 STRINGER 37R CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082800248 20010828 00248 NM 2001 8 28 2001UALA01800 1 20010824 A 5313 DOOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE STATION 605 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 519UA 24872 1 EA DENT IN FRONT OF DOOR 2L AT STATION 605 STRINGER 16LH. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2001090600386 20010906 00386 NM 2001 9 6 2001UALA01805 1 20010823 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 325-434 STRINGER 39L CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW STRINGER. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090600387 20010906 00387 NM 2001 9 6 2001UALA01806 1 20010823 A 5320 SPLICE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 440 STRINGER 36R SPLICE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SPLICE REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090600389 20010906 00389 NM 2001 9 6 2001UALA01808 1 20010823 A 5320 SPLICE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 434 STRINGER 34L SPLICE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER SPLICE REPAI R. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090600390 20010906 00390 NM 2001 9 6 2001UALA01809 1 20010823 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 714-723 STRINGER 34L CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082800249 20010828 00249 NM 2001 8 28 2001UALA01813 1 20010823 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE BODY STATION 325 A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BS-325-434 STRINGER 39R NECESSARY TO FAB STRINGER TO FACILITATE OTHER MAINTENANCE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER SECTION. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090600394 20010906 00394 NM 2001 9 6 2001UALA01814 1 20010823 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 478 STRINGER 39R CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090600397 20010906 00397 NM 2001 9 6 2001UALA01817 1 20010823 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1065-1087 STRINGER 28L CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090700067 20010907 00067 NM 2001 9 7 2001UALA01823 1 20010823 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 588 STRINGER 38L CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090700071 20010907 00071 NM 2001 9 7 2001UALA01826 1 20010823 A 5320 SPLICE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 412-456 STRINGER 39R SPLICE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER SPLICE R EPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082800250 20010828 00250 NM 2001 8 28 DHL2001709011 1 20010825 A 2612 FIRE LOOP BOEING 727 72782C 1384026 NM NR 1 ENGINE OUT OF POSITION A DHLA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 709DH 19968 NR 1 ENGINE FIRE DETECTOR CIRCUIT AND LIGHT ILLUMINATED. REPOSITIONED FIRE LOOP. OPS CHECKED GOOD IAW DHL 727 MM CH 26- 11-00. 2 L 7 3 4F A3WE 2001082800251 20010828 00251 NM 2001 8 28 DHL2001712010 1 20010828 A 3350 SWITCH BOEING 727 72729 1384007 NM COCKPIT DEFECTIVE A DHLA O OTHER O OTHER UK UNKNOWN 1 SO 01 712DH 19401 EMERGENCY EXIT LIGHT ARMING SWITCH DOES NOT OPERATE PROPERLY. REMOVED AND REPLACED SWITCH GUARD. OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2001082800252 20010828 00252 NM 2001 8 28 DHL2001717020 1 20010824 A 2612 FIRE LOOP BOEING 727 72723 1384004 NM NR 2 ENGINE OUT OF POSITION A DHLA O OTHER N FALSE WARNING UK UNKNOWN 1 SO 01 717DH 19389 NR 2 FIRE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED. PERFORMED FIRE DETECTOR SYSTEM TEST. LIGHT EXTINGUISHED. FOUND BR ACKET ON NR 2 ENGINE FIRE LOOP TOUCHING LOOP. RE-POSITIONED LOOP IAW B-727 M/M 26-11-22. SYSTEM OPS CHECKED SERVICEABL E. 2 L 7 3 4F A3WE 2001082800253 20010828 00253 WP 2001 8 28 DHL2001804537 1 20010815 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AFT ACCY COMPT BATH TUB FITTING CRACKED AT STA 169.000-1700.000, L34 B. REMOVED AND REPLACED BATH TUB FITTING PER SRM 5 1-1-20-D PG 9 AND 21. 2 L 7 4 4F RT 4A25 2001082800254 20010828 00254 WP 2001 8 28 DHL2001804538 1 20010817 A 5230 INTERCOSTAL DOUG DC8 DC873F 302199F WP CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AFT CARGO AFT DOOR LINK UPPER PART INTERCOSTAL CRACKED 3 INCHES. FABRICATED DOUBLER PER SRM 52-20 FIG 2 AND INSTALLED DO UBLER AND NEW FASTENERS PER SRM 52-2-0 FIG 2 AND SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2001082800255 20010828 00255 WP 2001 8 28 DHL2001804539 1 20010820 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 RT WING T/E LOWER PANEL SKIN DELAMINATED STA XW 5.000. REMOVED LOWER PANEL SKIN PER SRM 57-2-3 FIG 4A. FABRICATED NEW S KIN PER SRM 57-2-3 FIG 4A AND INSTALLED NEW SKIN PER SRM 57-2-3 FIG 4A. 2 L 7 4 4F RT 4A25 2001082800256 20010828 00256 WP 2001 8 28 DHL2001804540 1 20010816 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 MAIN CARGO COMPT 1-LT FLOOR TRACK LUG WORN STA 1580. TRIMMED OUT DAMAGED AREA OF FLOOR TRACK PER SRM 53-2-3 PG 17-19. FABRICATED TRACK PLUG (P/N 52772660) PER SRM 53-2-3 PG 17-19. INSTALLED TRACK PLUG PER SRM 53-2-3 PG 17-19. 2 L 7 4 4F RT 4A25 2001082800257 20010828 00257 WP 2001 8 28 DHL2001804541 1 20010817 A 5500 ACCESS PANEL DOUG DC8 DC873F 302199F WP EMPENNAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 EMPENNAGE 76 RT ACCESS PANEL SKIN CRACKED 1 INCH. REMOVED DAMAGED AREA PER SRM 55-2-0 FIG 2. FABRICATED REINFORCEMENT A ND PLATE PER SRM 56-2-0 FIG 2. INSTALLED REINFORCEMENT AND PLATE PER SRM 55-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001082800258 20010828 00258 WP 2001 8 28 DHL2001804542 1 20010816 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 D-CHECK; FLT COMPT- ANGLE LINKED TO FLOORBEAM CORRODED STA 52 NEAR L-22R RBL 60. CUT OUT CORRODED AREA. FABRICATED FILLE R IAW SRM 53-2-0 FIG 2. INSTALLED FILLER & DOUBLER (LT & RT). 2 L 7 4 4F RT 4A25 2001082800259 20010828 00259 WP 2001 8 28 DHL2001804543 1 20010819 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 D-CHECK; MAIN CARGO COMPT 3 LT FLOOR TRACK LUG WORN AT STA 380. TRIMMED OUT DAMAGED AREA OF 3 LT FLOOR TRACK STA 380 IA W SRM 53-2-3 PG 17-19. FABRICATED TRACK PLUG (P/N S2772666) IAW SRM 53-2-3 PG 17-19. INSTALLED TRACK PLUG IAW SRM 53-2- 3 PG 17-19. 2 L 7 4 4F RT 4A25 2001082800260 20010828 00260 WP 2001 8 28 DHL2001804544 1 20010819 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 D-CHECK; MAIN CARGO COMPT 3 LT FLOOR TRACK LUG WORN AT STA 360. TRIMMED OUT DAMAGED AREA OF 3 LT FLOOR TRACK STA 360 IA W SRM 53-2-3 PG 17-19. FABRICATED TRACK PLUG (P/N S2772666) IAW SRM 53-2-3 PG 17-19. INSTALLED TRACK PLUG IAW SRM 53-2- 3 PG 17-19. 2 L 7 4 4F RT 4A25 2001082800261 20010828 00261 WP 2001 8 28 DHL2001804545 1 20010819 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 D-CHECK; MAIN CARGO COMPT 3 LT FLOOR TRACK LUG WORN AT STA 660. TRIMMED OUT DAMAGED AREA OF 3 LT FLOOR TRACK STA 660 IA W SRM 53-2-3 PG 17-19. FABRICATED TRACK PLUG (P/N S2772660) IAW SRM 53-2-3 PG 17-19. INSTALLED TRACK PLUG IAW SRM 53-2- 3 PG 17-19. 2 L 7 4 4F RT 4A25 2001082800262 20010828 00262 WP 2001 8 28 DHL2001804546 1 20010821 A 5280 SKIN DOUG DC8 DC873F 302199F WP NLG DOOR DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 D-CHECK; NLG DOOR RT DENTED AT FS 38. REMOVED DENTED SKIN FROM NLG DOOR RT IAW SRM 51-1-21 PG 1. FABRICATED SKIN IAW SR M 52-5-2 PG 2. INSTALLED NEW SKIN AT NLG DOOR RT IAW SRM 52-5-2 PG 2 & SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2001082800263 20010828 00263 WP 2001 8 28 DHL2001804547 1 20010823 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 D-CHECK; FWD CARGO COMPT- LT TRACK SHOWS .5 INCH CRACK AT STA 400. REMOVED CRACKED TRACK IAW SRM 51-3-0 PG 1. INSTALLED NEW TRACK ON FWD CARGO COMPT STA 400 IAW SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2001082800264 20010828 00264 WP 2001 8 28 ZW0A0107601 1 20010827 A 3350 MISC0639 BATTERY PACK DOUG DC9 DC983 3022083 WP A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9404V 53140 THE AFT OVERWING EXIT LIGHT WAS INOPERATIVE ON TEST. REPLACED THE BATTERY PACK. CHECK-C 1-22-01 MCI. --CLOSED-- 2 L 7 2 4F RT A6WE 2001082800265 20010828 00265 WP 2001 8 28 DHL2001804548 1 20010823 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 D-CHECK; FWD CARGO COMPT- RT TRACK SHOWS 3 EA .5 INCH CRACKS AND WEAR FROM STA 160.000 TO STA 260.000. REMOVED DAMAGED RT CRACKED TRACK IAW SRM 51-3-0 PG 1. INSTALLED NEW TRACK ON FWD CARGO COMPT STA 160.000 TO STA 260.000 IAW SRM 51-3-0 P G 1. 2 L 7 4 4F RT 4A25 2001082800266 20010828 00266 WP 2001 8 28 DHL2001804549 1 20010823 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 D-CHECK; FWD CARGO COMPT- LT TRACK SHOWS 2 EA .5 INCH CRACKS AT STA 540.000. REMOVED CRACKED TRACK IAW SRM 51-3-0 PG 1. INSTALLED NEW TRACK ON FWD CARGO COMPT STA 540.000 IAW SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2001082800267 20010828 00267 WP 2001 8 28 DHL2001804550 1 20010824 A 5230 DOOR FRAME DOUG DC8 DC873F 302199F WP CARGO DOOR BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 UPPER CARGO DOOR FRAME PLATE BROKEN AND DEFORMED (STA 157-240). FABRICATED DOUBLER PER SRM 52-2-0 FIG 2. INSTALLED DOU BLER PER SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2001082800268 20010828 00268 WP 2001 8 28 DHL2001805019 1 20010818 A 5610 WINDOW DOUG DC8 DC873F 302199F WP COCKPIT BINDING A DHLA K NONE O OTHER UK UNKNOWN 1 SO 01 805DH 46125 CAPTAIN'S WINDOW WILL NOT OPEN FULLY. CAPTAIN'S WINDOW BINDING ON AFT WINDOW TRIM. REMOVED TRIM WINDOW, OPS CHECKS GOO D PER MM 56-10-3. 2 L 7 4 4F RT 4A25 2001082800271 20010828 00271 NM 2001 8 28 EISA20010083 1 20010516 A 2612 CONNECTOR BOEING 727 727225 1384077 NM FIFRE DETECTION DIRTY A EISA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 354PA 20624 DURING CLIMB PASSING THROUGH 14,000 FT FIRE ALARM CAME ON, AS WELL AS FORWARD FIRE MESSAGE INDICATION. ALARM EXTINGUISH ED 3 MINUTES LATER PRIOR TO ACCOMPLISHING APPROPRIATE CHECKLIST. FOUND DIRTY CONNECTOR. CLEANED CONNECTOR IAW M/M 26-1 5. SYSTEM CHECKS NORMAL. 2 L 7 3 4F A3WE 2001082800272 20010828 00272 NM 2001 8 28 EISA20010084 1 20010521 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM L1 DOOR INOPERATIVE A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6815 19490 L-1 EMERGENCY EXIT LIGHT WILL NOT CHARGE. 2 L 7 3 4F A3WE 2001082800273 20010828 00273 NM 2001 8 28 EISA20010086 1 20010412 A 5311 FRAME BOEING 727 727223 1384074 NM FUSELAGE CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 702NE 22460 FRAME CRACKED AT STATION 1110 SHEAR TIE CRACKED AT STATION 1130, BETWEEN STRINGERS 24 & 25R. FABRICATED SHEAR TIE REPA IR FORWARD AND AFT SIDE OF FRAME, IAW SRM 53-10-4. FABRICATED REPAIR SECTION FOR FRAME IAW SRM 53-10-4, AND INSTALLED R EPAIR PARTS, IAW SRM 51-10-2, 51-30-2. 2 L 7 3 4F A3WE 2001082800274 20010828 00274 NM 2001 8 28 EISA20010088 1 20010412 A 5313 STRINGER BOEING 727 727223 1384074 NM FUSELAGE DENTED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 702NE 22460 STRINGER 24 RIGHT DAMAGED AT STATION 1099. REFORMED DENT TO ORIGINAL CONTOUR IAW SRM 51-10-1, EO 01-112 WITH APPROVED 8 110-3 DATED 04-15-2001. 2 L 7 3 4F A3WE 2001082800275 20010828 00275 NM 2001 8 28 EISA20010090 1 20010505 A 5320 T631201 SPLICE BOEING 727 7272A7 138407K NM FUSELAGE CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 STRINGER AT BS 680 27 RIGHT SPLICE IS CORRODED. REMOVED AND REPLACED STRINGER SPLICE, INSTALLED NEW SPLICE IAW SRM 53-1 0-3, 51-10-2, M/M 51-21-31. 2 L 7 3 4F A3WE 2001082800276 20010828 00276 NM 2001 8 28 EISA20010091 1 20010504 A 5210 SKIN BOEING 727 7272M7 138407S NM L1 DOOR CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 742RW 21952 L-1 LOWER DOOR HINGE AT FUSELAGE SKIN CRACKED. REPAIRED CRACK, ROUTING OUT AND FABRICATING AND INSTALLING REPAIR FILLER AND DOUBLER IAW 727 SB 727-53-0198 REV 1 FIGURE 4 DATED 07-25-1991. 2 L 7 3 4F A3WE 2001082800277 20010828 00277 NM 2001 8 28 EISA20010099 1 20010616 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM FUSELAGE CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 FLOORBEAM IS CRACKED IN THE RT MID CABIN AT BS 848, UNDER THE O/B, RT SEAT TRACK APPROX 10 INCHES LONG IN LENGTH. REMOV ED CRACKED SECTION. FABRICATED AND INSTALLED A NEW WEB, WEB SPLICE AND T-CAP REPAIRS IAW B727 SRM 51-40-2 FIG 1 & 51-30 -2. 2 L 7 3 4F A3WE 2001082800278 20010828 00278 NM 2001 8 28 EISA20010100 1 20010617 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM FUSELAGE CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 AFT PIT-CABIN FLOORBEAM BS 1110 RBL 22 AFT SIDE EXFOLIATED AT NUT CLIP. CUT OUT CORRODED SECTION OF THE UPPER FLANGE OF FLOORBEAM, FABRICATED AND INSTALLED FILLER AND DOUBLER REPAIRS IAW B727 SRM 53-10-8 FIG 1. 2 L 7 3 4F A3WE 2001082800279 20010828 00279 NM 2001 8 28 EISA20010101 1 20010617 A 5310 CREASE BEAM BOEING 727 727223 1384074 NM FUSELAGE CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 LT FUSELAGE CREASE BEAM WEB IS CRACKED AT BS 1090 FLOOR LEVEL. CUT OUT CRACKED AREA. FABRICATED AND INSTALLED WEB AND FILLER ANGLE. REPAIRS IAW B727 SRM 51-30-2, 51-10-1, 51-40-2, 51-10-2 AND MM 51-22-11. 2 L 7 3 4F A3WE 2001082800280 20010828 00280 NM 2001 8 28 EISA20010102 1 20010620 A 5320 652427627 FITTING BOEING 727 727223 1384074 NM FUSELAGE CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 AFT STRINGER 18 LT & STA 1183 FWD SIDE OF BULKHEAD END FITTING HAS CORROSION BLOW-OUT. FOUND DURING B-CHECK. REMOVED E ND FITTING AT STRINGER 18 LT STA 1183 FWD SIDE BULKHEAD IAW B727 SRM 51-30-02. REMOVED CORROSION IAW B727 SRM 51-10-6 O RIGINAL MATERIAL THICKNESS .125 AFTER BLEND-OUT .000, OUT OF LIMITS IAW B727 SRM 51-10-6. INSTALLED REPLACEMENT FITTING IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2001082800281 20010828 00281 NM 2001 8 28 EISA20010103 1 20010628 A 3350 1000679 LIGHT BOEING 727 727200 138407E NM L1 DOOR INOPERATIVE A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 702NE 22460 EMERGENCY LIGHT OUT L1 DOOR, OPERATES DIMLY. REMOVED AND REPLACED LIGHT ASSY IAW MM 33. OPS CHECK GOOD. 2 L 7 3 4F RT A3WE 2001082800282 20010828 00282 NM 2001 8 28 EISA20010104 1 20010706 A 3260 387 LIGHT BOEING 727 727223 1384074 NM COCKPIT INOPERATIVE A EISA K NONE N FALSE WARNING AP APPROACH 1 SW 07 314NE 19495 DURING APPROACH NOSE GEAR DOWN AND LOCKED LIGHT INOP. WOULD NOT PRESS TO TEST. RELAMPED BULB. 2 L 7 3 4F A3WE 2001082800283 20010828 00283 NE 2001 8 28 EISA20010110 2 20010728 A 7200 ENGINE BOEING 727 727225 1384077 NM PWA JT8 JT8D7B 52053 NE NR 3 FLAMED OUT A EISA D RETURN TO BLOCK X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 SW 07 352PA 20616 655881 NR 3 ENGINE FLAME-OUT ON TAXI. MOTORED ENG TO REMOVE EXCESS FUEL, RAN ENG AND OPS CHECK OK. 2 L 7 3 4F 4 F A3WE E2EA 2001082800284 20010828 00284 NM 2001 8 28 ERKR 1 20010703 A 3350 SIGN BOEING 737 7372K9 1384494 NM CABIN MISSING B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 714A 23405 EMERGENCY LIGHTING MISSING, EXIT SIGNS AT L-1, 2, R-1, 2 AND OVERWING EXITS. EMERGENCY PATH LIGHTING MISSING. INSTALLI NG NEW SYSTEM. 2 L 7 2 4F A16WE 2001082900001 20010829 00001 WP 2001 8 29 RRXA10827 1 20010207 A 5230 SKIN DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO A-PIT DOOR SKIN AT FWD. CENTER SECTION, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001082900002 20010829 00002 WP 2001 8 29 RRXA10828 1 20010214 A 5230 SPAR DOUG DC8 DC871F 302199D WP CARGO DOOR DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND ROUTED OUT DAMAGE TO C-PIT DOOR SPAR AT RT SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4 AND DC-8 SRM 51 -1-20D AND DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001082900003 20010829 00003 WP 2001 8 29 RRXA10829 1 20010125 A 5230 SKIN DOUG DC8 DC871F 302199D WP CARGO DOOR DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND ROUTED OUT DAMAGE TO C-PIT DOOR MID LIGHTING HOLE AT RT MID C-PIT DOOR, BAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. 0 1-006 WITH APPROVED 8110-3 DATED 01/11/01. 2 L 7 4 4F RT 4A25 2001082900004 20010829 00004 WP 2001 8 29 RRXA10830 1 20010124 A 5230 SKIN DOUG DC8 DC871F 302199D WP CARGO DOOR DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND ROUTED OUT DAMAGE TO C-PIT DOOR LIGHTING HOLE AT LT MID LIGHTNING HOLE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.#0 1-006 WITH APPROVED 8110-3 DATED 01/11/01. 2 L 7 4 4F RT 4A25 2001082900005 20010829 00005 WP 2001 8 29 RRXA10831 1 20010126 A 5230 SKIN DOUG DC8 DC871F 302199D WP CARGO DOOR DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND ROUTED OUT DAMAGE TO C-PIT DOOR AT FWD/MID LIGHTNING HOLE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. 01-006 WITH AP PROVED 8110-3 DATED 01/10/01. 2 L 7 4 4F RT 4A25 2001082900006 20010829 00006 WP 2001 8 29 RRXA10832 1 20010116 A 5230 DOUBLER DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CRACK DAMGE TO C-PIT DOOR AT FWD. LT DOUBLER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001082900007 20010829 00007 WP 2001 8 29 RRXA10833 1 20010122 A 5230 DOUBLER DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANACE VISIT FOUND CRACK DAMAGE TO C-PIT DOOR AT FWD. RT. DOUBLER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001082900008 20010829 00008 WP 2001 8 29 RRXA10834 1 20010119 A 5230 BRACKET DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO D-PIT DOOR AT AFT ROLLER ATTACH BRACKET, DAMAGE EXCEEDED LIMITATIONS IA W DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 MM 52-32-1. 2 L 7 4 4F RT 4A25 2001082900009 20010829 00009 WP 2001 8 29 RRXA10835 1 20010131 A 5230 FRAME DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO D-PIT DOOR FRAME DOUBLER AT AFT TOP CORNER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001082900010 20010829 00010 WP 2001 8 29 RRXA10836 1 20010124 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO MAIN CABIN FLOOR BEAM AT STA. 1723 AND LBL 8 TO 24 ON T CORD, DAMAG E EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21 AND DC-8 SRM51-3-0. 2 L 7 4 4F RT 4A25 2001082900011 20010829 00011 WP 2001 8 29 RRXA10838 1 20010202 A 5230 RETAINER DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO D-PIT DOOR AT LWR. AFT DOOR RETAINER, DAMAGE EXCEEDED LIMITATIONS IAW D C-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21 AND DC-8S RM 51-1-20D AND DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001082900012 20010829 00012 WP 2001 8 29 RRXA10840 1 20010202 A 5540 BRACE DOUG DC8 DC871F 302199D WP RUDDER CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO RUDDER LOAD FEEL UNIT SUPPORT SIDE BRACE AT UPPER AND LOWER, DAMAGE EXC EEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC- 8 SRM 51-1-21 AND DC-8SRM51-1-20D. 2 L 7 4 4F RT 4A25 2001082900013 20010829 00013 WP 2001 8 29 RRXA10841 1 20010207 A 5414 PANEL DOUG DC8 DC871F 302199D WP NR 3 PYLON DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND HOLE ELONGATED DAMAGE TO NR 3 PYLON PANEL AT PANEL 392A, DAMAGE EXCEEDED LIMITATIONS IA W DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PARTS AND INSTALLED IAW DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001082900014 20010829 00014 WP 2001 8 29 RRXA10842 1 20010206 A 3210 BOSS DOUG DC8 DC871F 302199D WP MLG CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RETRACT PIN BOSS AT MLG SHOCK STRUT ASSSEMBLY, DAMAGE EXCEEDED LIMI TATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. 01-006 WITH APPROVED 8110-3 DATED 01/06/01. 2 L 7 4 4F RT 4A25 2001082900015 20010829 00015 WP 2001 8 29 RRXA10843 1 20010125 A 5730 SKIN DOUG DC8 DC871F 302199D WP NR 2 STUB WING CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO 2 ENGINE STUB WING SKIN AT STA. XFS 238, DAMAGE EXCEEDED LIMITATION S IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-20C AND E.O. 01-006 WITH APPROVED 8110-3 DATED 01/10/01. 2 L 7 4 4F RT 4A25 2001082900016 20010829 00016 WP 2001 8 29 RRXA10844 1 20010125 A 5730 SKIN DOUG DC8 DC871F 302199D WP NR 2 STUB WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO NR 2 ENGINE STUB WING SKIN AT STA. XFS 238, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. 01-006 WITH APPROVED 8110-3 DATED 01/10/01. 2 L 7 4 4F RT 4A25 2001082900017 20010829 00017 WP 2001 8 29 RRXA10845 1 20010206 A 5730 56110111 PANEL DOUG DC8 DC871F 302199D WP LT WING DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LT. WING T/E PANEL LWR. SURFACE AT STA. XW106, DAMAGE EXCEEDED L IMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 MM 57-30 -0. 2 L 7 4 4F RT 4A25 2001082900018 20010829 00018 WP 2001 8 29 RRXA10846 1 20010206 A 5730 5611015501 PANEL DOUG DC8 DC871F 302199D WP LT WING DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LT. WING T/E PANEL LWR. SURFACE AT STA. XW350, DAMAGE EXCEEDED L IMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 MM 57-30 -0. 2 L 7 4 4F RT 4A25 2001082900019 20010829 00019 WP 2001 8 29 RRXA10847 1 20010207 A 5730 5611013409 PANEL DOUG DC8 DC871F 302199D WP LT WING DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LT. WING T/E PANEL LWR. SURFACE AT STA. XRS 170, DAMAGE EXCEEDE D LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 5 1-1-21 & 51-1-24 & 51-3-0. 2 L 7 4 4F RT 4A25 2001082900020 20010829 00020 WP 2001 8 29 RRXA10848 1 20010207 A 5730 5611002501 PANEL DOUG DC8 DC871F 302199D WP LT WING DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LT. WING UPPER SURFACE T/E PANEL OVER MAIN LANDING GEAR AT STA X W5 TO XW 47, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001082900021 20010829 00021 WP 2001 8 29 RRXA10849 1 20010206 A 5730 56110011F PANEL DOUG DC8 DC871F 302199D WP LT WING DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LT. WING UPPER SURFACE UX-SPAR PANEL OVER MAIN LANDING GEAR AT S TA. XW5 TO XW33, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED P ART AND INSTALLED IAW DC-8 SRM 51-3-0 & 51-1-24. 2 L 7 4 4F RT 4A25 2001082900022 20010829 00022 WP 2001 8 29 RRXA10850 1 20010104 A 5280 56489321N SKIN DOUG DC8 DC871F 302199D WP LT MLG DOOR DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LT MLG UPPER DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RE MOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 MM 32-10-3. 2 L 7 4 4F RT 4A25 2001082900023 20010829 00023 WP 2001 8 29 RRXA10851 1 20010205 A 5730 56110101 PANEL DOUG DC8 DC871F 302199D WP RT WING DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LWR. WING PANEL AT RT AUX. SPAR, DAMAGE EXCEEDED LIMITATIONS IA W DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001082900024 20010829 00024 WP 2001 8 29 RRXA10852 1 20010202 A 5730 PANEL DOUG DC8 DC871F 302199D WP WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO UPPER T/E PANEL HINGE FOR SPOILER AT STA. 219, DAMAGE EXCEEDED LIMITA TIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1- 21 & 57-2-0. 2 L 7 4 4F RT 4A25 2001082900025 20010829 00025 WP 2001 8 29 RRXA10853 1 20010203 A 5730 561101492 PANEL DOUG DC8 DC871F 302199D WP RT WING DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO RT LWR. T/E PANEL AT STA XRS 219 TO XRS 340, DAMAGE EXCEEDED LI MITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-3- 0. 2 L 7 4 4F RT 4A25 2001082900026 20010829 00026 WP 2001 8 29 RRXA10854 1 20010206 A 5280 SKIN DOUG DC8 DC871F 302199D WP RT MLG DOOR DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO R/H MLG UPPER O/B DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SR M. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 MM 32-12-1 AND DC-8 SRM 51-3-0 . 2 L 7 4 4F RT 4A25 2001082900027 20010829 00027 WP 2001 8 29 RRXA10856 1 20010207 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP FUSELAGE DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO UPPER CARGO COMPT. FLOOR PANEL AT STA. 580-590 X=45-55, DAMAG E EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0 AND DOUGLAS DRAWING 5804513. 2 L 7 4 4F RT 4A25 2001082900028 20010829 00028 WP 2001 8 29 RRXA10857 1 20010117 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT FOUND HOLE DAMAGE TO FLOOR PANEL AT STA. 55 X= -40, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM . REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-4 & 53-2-0. 2 L 7 4 4F RT 4A25 2001082900029 20010829 00029 WP 2001 8 29 RRXA10862 1 20010228 A 5730 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO INTERNAL SKIN LT WW AT STA. 857-879 AND LBL 0-68.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SR M 51-3-0 & 53-2-0 FIG.1F. 2 L 7 4 4F RT 4A25 2001082900030 20010829 00030 WP 2001 8 29 RRXA10863 1 20010220 A 5310 DOOR FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO ACCESS HOLE 60 DOOR FRAME AT STA. 1793-1766 AND L34L-L34R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW D C-8 SRM 51-1-21 & 51-1-24 & 51-1-4. 2 L 7 4 4F RT 4A25 2001082900031 20010829 00031 WP 2001 8 29 RRXA10864 1 20010207 A 5321 PRESSURE PANEL DOUG DC8 DC871F 302199D WP COCKPIT FLOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION AND CRACK DAMAGE TO COCKPIT FLOOR PANEL 682A, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4. 2 L 7 4 4F RT 4A25 2001082900033 20010829 00033 WP 2001 8 29 RRXA10874 1 20010320 A 5340 3755822513N FITTING DOUG DC8 DC873F 302199F WP STA 300 L34R-35R CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE BATHTUB FITTING AT STA 300 BETWEEN L34R TO L35R, DAMAGE EXCEEDED LIMITAT IONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAAW DC-8 SRM 53-2-0, FIG 2B. 2 L 7 4 4F RT 4A25 2001091400051 20010914 00051 NM 2001 9 14 01FDEA00772 1 20010828 A 5320 FITTING BOEING 727 727247 138408F NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 LT WHEEL WELL TIE STRAP AT BS 940-950 FITTING IS CRACKED AT STR 18A. REMOVED AND REPLACED TIE STRAP PER SRM 51-30-5, 51- 30-2. 2 L 7 3 4F A3WE 2001092700061 20010927 00061 NM 2001 9 27 01FDEA00773 1 20010827 A 5310 BEAM BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 280FE 22347 MAIN CABIN DOOR UPPER CUTOUT SILL BEAM CRACKED AT BS 606 BETWEEN STR 2L & 3L. REMOVED AND REPLACED BEAM PER EA 7-5310-33 368. 2 L 7 3 4F RT A3WE 2001091200040 20010912 00040 NM 2001 9 12 01FDEA00774 1 20010827 A 5347 CARGO TRACK BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 280FE 22347 MAIN CABIN CARGO TRACK CRACKED AT BS 615 BL 0. REMOVED AND REPLACED TRACK PER SRM 53-10-5. 2 L 7 3 4F RT A3WE 2001091200041 20010912 00041 NM 2001 9 12 01FDEA00775 1 20010827 A 5312 PRESSURE PANEL BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 280FE 22347 NOSE WHEEL WELL SIDE PANEL WEB ABOVE LT FWD NLG DOOR CRACKED BS 234-236, WL 168. REMOVED AND REPLACED WEB PER SRM 51-20- 1. 2 L 7 3 4F RT A3WE 2001091200043 20010912 00043 NM 2001 9 12 01FDEA00776 1 20010827 A 5313 STRINGER BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 280FE 22347 STR 28R CRACKED AT BS 704. REMOVED AND REPLACED STR PER SRM 53-30-3. 2 L 7 3 4F RT A3WE 2001091200046 20010912 00046 NM 2001 9 12 01FDEA00777 1 20010827 A 5320 SUPPORT BRACKET BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 280FE 22347 RT FAIRING SUPPORT BRACKET CRACKED AT BS 720 AT STR 28R. REMOVED AND REPLACED BRACKET PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 2001091200050 20010912 00050 NM 2001 9 12 01FDEA00782 1 20010828 A 5340 69139004 PIN BOEING 727 727233 138408A NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 280FE 22347 FLANGE ON RT FWD TERMINAL PIN CRACKED BS 740. REMOVED AND REPLACED PIN PER MM 57-41-001-4. 2 L 7 3 4F RT A3WE 2001082900034 20010829 00034 WP 2001 8 29 RRXA10875 1 20010322 A 5712 5769589 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LEFT WING L/E UPPER RIB AT STA X5497-401, DAMAGE EXCEEDED LIMITATIONS IA W DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2. 2 L 7 4 4F RT 4A25 2001082900035 20010829 00035 WP 2001 8 29 RRXA10876 1 20010322 A 5712 5769589 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB ON THE LEFT WING L/E AT STA XFS 578375, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2. 2 L 7 4 4F RT 4A25 2001082900036 20010829 00036 WP 2001 8 29 RRXA10877 1 20010322 A 5712 5769589 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB ON THE LEFT WING L/E AT STA XF 5660, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2. 2 L 7 4 4F RT 4A25 2001082900037 20010829 00037 NM 2001 8 29 PCAA0108094 1 20010823 A 3350 6104781 BATTERY DHAV DHC8 DHC8102 2809003 NM POSITION 100 POWER LOSS A PCAA O OTHER O OTHER IN INSP/MAINT 1 EA 13 844EX 339 MDT- DURING ROUTINE MAINTENANCE VISIT EMERGENCY LIGHT BATTERY SERIAL NUMBER 37PA FOUND INOPERATIVE. BATTERY REPLACED. OP ERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2001082900038 20010829 00038 NM 2001 8 29 PCAA0108095 1 20010824 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM POSITION 300 POWER LOSS A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 845EX 21034 344 BGM- DURING ROUTINE MAINTENANCE VISIT FORWARD TOP LEFT EGRESS LIGHT FOUND TO BE VERY DIM. EMERGENCY LIGHT POWER SUPPLY C ONTROL BOX AND BATTERY PACK FOR POSITION 300 REPLACED. EMERGENCY LIGHTS OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2001082900042 20010829 00042 WP 2001 8 29 RRXA10878 1 20010322 A 5712 5769589 RIB DOUG DC8 DC873F 302199F WP LEFT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB LEFT WING L/E AT STA XFS 616.25 AND 622.5, DAMAGE EXCEEDED LIMITATIO NS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2. 2 L 7 4 4F RT 4A25 2001082900046 20010829 00046 NM 2001 8 29 HNAA0100051 1 20010820 A 5744 85710828 BRACKET DHAV DHC8 DHC8102 2809003 NM CRACKED A HNAA K NONE Z SIGNIFICANT FAILURE REPORT IN INSP/MAINT 1 EA 07 938HA 33506 152 AILERON CONTROL QUADRANT MOUNTING BRACKET ON L/H WING REAR SPAR FOUND CRACKED AT OUTBOARD END OF THE LOWER FLANGE TO 1/1 6" BEYOND THE FIRST RIVET HOLE. REPAIRED IAW ESR8-57-01-012A. 2 H 7 2 4T RT A13NM 2001082900048 20010829 00048 NM 2001 8 29 2001UALA01522 1 20010728 A 3260 806007 CIRCUIT BOARD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RT MLG FAULTY A UALA K NONE N FALSE WARNING AP APPROACH 1 WP 29 331UA 24192 LANDED UNDER AMBER ALERT DUE TO RIGHT MAIN LANDING GEAR LIGHT INTERMITTENTLY CHANGED FROM GREEN TO RED TO GREEN ON FINAL APPROACH. REPLACED LANDING GEAR LOGIC CARDS M981 AND M982 MAIN LANDING GEAR SYSTEM OPERATIONAL TESTED GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082900049 20010829 00049 NM 2001 8 29 2001UALA01528 1 20010727 A 2121 732591F FAN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DEFECTIVE A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 180UA 46937 25224 SMELL OF ELECTRICAL SMOKE, STRONGEST NEAR AFT GALLEY LOWER DECK. UTILITY BUSSES DROPPED OFF, SWITCHES WERE TURNED OFF, SYSTEM WENT TO SMOKE CLEARING MODE, SMELL WENT AWAY, UTILITY BUSSES LEFT OFF. THE RIGHT OVERHEAD RECIRCULATION FAN WAS FOUND DEFECTIVE. THE FAN WAS REPLACED AND NO FURTHER PROBLEMS WERE REPORTED. 2 L 7 4 4F 4 F RT A20WE E24NE 2001082900051 20010829 00051 2001 8 29 2001UALA01637 4 20010803 A 3414 4039891903 INDICATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT FAILED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 651UA 25389 RTO AT 85 KTS. COPILOT MACH AIRSPEED INDICATOR (MASI) SHOWED ZERO KTS AND A-S WARNING FLAGD 80 KTS DURING TAKEOFF. TAKE OFF ABORTED WITH RTO ENGAGED FOR 3-5 SECONDS. REPLACED THE COPILOT MASI. 2 L 7 2 4F 4 F RT A1NM E24NE 2001082900052 20010829 00052 WP 2001 8 29 RRXA10879 1 20010322 A 5712 5769589 RIB DOUG DC8 DC873F 302199F WP LEFT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB ON THE LEFT WING L/E AT STA XFS 641.25, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2. 2 L 7 4 4F RT 4A25 2001082900055 20010829 00055 NM 2001 8 29 2001UALA01741 1 20010817 A 5240 DOOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LAV SERVICE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 365UA 24534 RIGHT SIDE AFT OF FWD LAV SERVICE DOOR HAS A DENT. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE, INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082900056 20010829 00056 WP 2001 8 29 CALA0100815 1 20010828 A 5230 SKIN DOUG DC10 DC1030 3023501 WP FWD CARGO DR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17085 47957 INSPECTION FOUND A 1" CRACK IN FORWARD CARGO DOOR SKIN(DOUBLER) ON LATCH ACCESSORY DOOR CUTOUT AREA. THE CRACKED AREA WA S CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-00-01, FIGURE 9. 2 L 7 3 4F A22WE 2001082900057 20010829 00057 NM 2001 8 29 CALA0100816 1 20010829 A 3350 D71702030 CHARGER BOEING 737 737724 NM ROW 15-20 INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 24706 28767 THE EMERGENCY LIGHTS ON SEATS AT ROWS 15-20 WOULD NOT ILLUMINATED WHEN TESTED. TROUBLESHOOTING FOUND M1672 AND M1670 BAT TERY CHARGERS FAILED. THE BATTERY CHARGERS WERE REMOVED AND REPLACED IAW MM 33-51-06 AND OPERATION OF THE LIGHTS TESTED GOOD. 2 L 7 2 4F RT A16WE 2001082900058 20010829 00058 NM 2001 8 29 2001UALA01742 1 20010818 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 324UA 23956 LT FUSELAGE INTERCOSTAL CRACKED AT STA 294.5 STR 16L, AT DOOR CUTOUT SUPPORT. MAJOR REPAIR ACCOMPLISHED. INTERCOSTAL W EB WAS REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082900059 20010829 00059 NM 2001 8 29 2001UALA01743 1 20010819 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 324UA 23956 BS 294.5 AT RT CREASE BEAM, FLOOR LEVEL, DOOR CUTOUT FRAME HAS CRACK ON INNER FLANGE. MAJOR REPAIR ACCOMPLISHED. DAMAG E WAS REMOVED AND ANGLE DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001101200065 20011012 00065 NM 2001 10 12 2001UALA01745 1 20010819 A 7930 1B1276 BRACKET BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE FAILED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 528UA 25018 726607 NR 1 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. *S/D* LOSS OF OIL QUANTITY AND PRESSURE DUE TO A HOLE WORN IN THE LINE . REPLACED OIL OUT LINE FROM FOX TO AOX AND SUPPORT BRACKET ON NR 1 ENG. 2 L 7 2 4F 4 F RT A2NM E17NE 2001082900061 20010829 00061 WP 2001 8 29 RRXA10880 1 20010322 A 5310 5758874 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 36 AT STA 140-160, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SR M. REMOVED DAMAGED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-4-1, FI G 28 AND DWG 5758874. 2 L 7 4 4F RT 4A25 2001082900062 20010829 00062 WP 2001 8 29 RRXA10881 1 20010322 A 5340 37549301N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE C-PIT DOOR FRAME LOWER NR 4 LATCH BACKUP FITTING , DAMAGE EXCEE DED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-1-0, 51-1-20D AND DWG 3754930-1N. 2 L 7 4 4F RT 4A25 2001090700047 20010907 00047 NM 2001 9 7 2001UALA01747 1 20010819 A 5320 DRAIN VALVE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE FAILED A UALA B EMER. DESCENT O OTHER CR CRUISE 1 WP 29 922UA 26642 AIRCRAFT MADE A RAPID DESCENT FROM FL240 TO 10000 FEET DUE TO A PRESSURIZATION PROBLEM. TWO DRAIN VALVES WERE FOUND FAIL ED OPEN. THE FAILED DRAIN VALVES WERE REPLACED, THEN ADJUSTMENT/TEST PROCEDURE WERE ACCOMPLISHED ON THE PRESSURIZATION S YSTEM. A TEST FLIGHT WAS ACCOMPLISHED FOR SYSTEM INTEGRITY. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091900034 20010919 00034 NM 2001 9 19 2001UALA01748 1 20010818 A 2613 356254255 SENSING ELEMENT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE OVERHEAT DETECT FAULTY A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 364UA 24533 UNSCHEDULED LANDING DUE TO WING BODY OVERHEAT INDICATION. MAINTENANCE REPLACED AFT LOOP (SECTION 58) DETECTOR. ALSO REP LACED BOTH LOAD CONTROL VALVE CLAMPS. PERFORMED LEAK TEST FROM APU TO AFT PRESSURE BULKHEAD. NO LEAK WAS DETECTED. WI NG BODY OVERHEAT DETECTION TESTED GOOD (NO OVERHEAT LIGHT) AND AIRCRAFT WAS RETURNED TO REVENUE SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082900063 20010829 00063 NM 2001 8 29 2001UALA01749 1 20010818 A 5230 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 322UA 23954 AFT CARGO DOOR HAS DAMAGE TO OUTER SKIN. REMOVED DAMAGED AREA. INSTALLED DOUBLER. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001090700051 20010907 00051 NM 2001 9 7 2001UALA01752 1 20010817 A 4940 MR49902 PRESSURE SWITCH BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE APU DEFECTIVE A UALA K NONE J WARNING INDICATION NR NOT REPORTED 1 WP 29 667UA 600 29239 61905 APU NO START WITH 3 ATTEMPTS APU FAULT EICAS. REPLACED STARTER REF MM49-41-01 AND ECU REF MM 49-61-05. NO HELP. APU STIL L WOULD NOT START. ECU SHOWED NR 1 SPEED SENSOR. REPLACED APU BATTERY AND NR 1 MONOPOLE RUNS FOR APPROX 15 MIN THEN SHU TS DOWN. REPLACED AND INSTALLED GENERATOR FILTER DELTA PRESSURE SWITCH PER MM 49-27-15, APU WAS RUN FOR 1HR, OPS CHECK O K. 2 L 7 2 4F 4 F RT A1NM E24NE 2001082900064 20010829 00064 NM 2001 8 29 2001UALA01754 1 20010819 A 3350 57761 BATTERY PACK BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN INTERMITTENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 EMERGENCY ESCAPE PATH LIGHTING ILLUMINATED INTERMITTENTLY ON LEFT CABIN AISLE FROM DOOR 1L THROUGH ROW 6 AND FROM ROW 25 AFT AND FROM ROWS 7-15 (LEFT SIDE ONLY). REPLACED 3 BATTERY PACKS, CHECKS OK. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082900065 20010829 00065 NM 2001 8 29 2001UALA01756 1 20010816 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 EMERGENCY LIGHTS INOP, OUTSIDE LEFT UPPER TWO ASSEMBLIES. 2 L 7 4 4F 4 F RT A20WE E24NE 2001082900066 20010829 00066 NE 2001 8 29 2001UALA01757 2 20010820 A 7250 TURBINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 NUMBER 1 ENGINE LPT 3RD STAGE FAILED BORESCOPE INSPECTION. 2 L 7 2 4F 4 F RT A2NM E17NE 2001091900036 20010919 00036 NM 2001 9 19 2001UALA01758 1 20010820 A 2913 4205401 PUMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE FAILED A UALA H DEACTIVATE SYST/CIRCUITS J K WARNING INDICATION FLUID LOSS CR CRUISE 1 WP 29 510UA 24780 LEFT ENGINE DRIVEN PUMP OVERHEAT LIGHT ILLUMINATED. PUMP DEACTIVATED, 30 MINUTES LATER LEFT SYSTEM LOST ALL FLUID. PUMP FAILED INTERNALLY. REPLACED LEFT ENGINE DRIVEN PUMP. 2 L 7 2 4F 4 F RT A2NM E17NE 2001082900067 20010829 00067 NM 2001 8 29 2001UALA01759 1 20010820 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 322UA 23954 CABIN STATION 616 RIGHT HAND OVERWING FRAME INBOARD CHORD TO STUB BEAM JOINT IS CRACKED. MAJOR REPAIR ACCOMPLISHED. RE MOVED DAMAGE, MANUFACTURED AND INSTALLED FILLER & ANGLE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082900068 20010829 00068 NM 2001 8 29 2001UALA01760 1 20010820 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 322UA 23954 CABIN STATION 616 RIGHT HAND SIDE OVERWING FRAME STUB END WEB AREA DAMAGED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE, MANUFACTURED AND INSTALLED NEW WEB SECTION AND DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082900070 20010829 00070 NM 2001 8 29 2001UALA01763 1 20010820 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 324UA 23956 RIGHT HAND OVERWING FRAME BODY STATION 616 INNER CHORD CRACKED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE. INSTALLED STIFFENING ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082900071 20010829 00071 NM 2001 8 29 2001UALA01764 1 20010821 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 324UA 23956 MID CABIN FRAME CHORD WEB AT BS 616L IS CRACKED. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082900072 20010829 00072 EU 2001 8 29 2001UALA01768 1 20010821 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN WILL NOT TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 415UA 475 EMERGENCY LIGHT TEST FAILED. 2 L 7 2 4F 4 F RT A28NM E40NE 2001082900073 20010829 00073 NM 2001 8 29 2001UALA01769 1 20010823 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 FUSELAGE SKIN DAMAGED STATION 963 TO 996 STRINGER 21LT-22LT. MAJOR REPAIR ACCOMPLISHED. DAMAGED SKIN REMOVED, FILLER A ND DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082900074 20010829 00074 NM 2001 8 29 2001UALA01770 1 20010822 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 324UA 23956 BS 178 BULKHEAD WL 188, BL 0 LEFT HAND SIDE WEB IS CRACKED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND REPAIR WITH DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082900075 20010829 00075 NM 2001 8 29 2001UALA01771 1 20010822 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 324UA 23956 CABIN FLOORBEAM STATION BS 294.5 UPPER FLANGE BLENDED TO 25 PERCENT MATERIAL LOSS AT RBL 23. MAJOR REPAIR ACCOMPLISHED. BY BLENDING AREA HFEC FOR CRACKS AND INSTALLING DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082900077 20010829 00077 NM 2001 8 29 DHL2001747005 1 20010823 A 3230 LANDING GEAR BOEING 727 727224 1384076 NM LT & RT MLG MALFUNCTIONED A DHLA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 747DH 22253 UPON APPR & GEAR EXTENSION THE NOSE, LT & RT MAIN GEAR GREEN & RED LIGHTS ILLUMIN. DOOR LIGHT WAS EXTINGUISHED, TAIL SK ID LIGHT WAS ILLUMIN WITH S/O GEAR DOOR LIGHTS EXTINGUISHED. SECONDARY GEAR INDICATIONS INDICATED NORM DOWN & LOCKED AL L GEARS. CYCLED GEAR, LT GEAR & NOSE RETRACTED NORM. RT GEAR GREEN LIGHT EXTINGUISHED, RED LIGHT & DOORS LIGHT REMAINE D ILLUMIN S/O RT GEAR LIGHT REMAINED ILLUMIN. ABOUT 45 SEC AFTER NOSE AND LT MAIN CYCLED UP, RT MAIN SUDDENLY RETRACTED WITH A THUMP AND ALL LIGHTS EXTINGUISHED. SELECTED GEAR DOWN, GEAR AND DOORS CYCLED DOWN NORM. FLY-BY, ALL APPEARED N ORM. LANDING NORM. LUBED RT MLG, SWUNG GEAR SEVERAL TIMES, ALL INDICATIONS NORM IAW B727 MM 32-32-0. 2 L 7 3 4F A3WE 2001082900078 20010829 00078 EA 2001 8 29 DJFA200100014 1 20010413 A 3242 5002523 BRAKE CNDAIR CL600 CL6002B16 1900305 EA MLG SEIZED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 653CW 5053 UPON REPLACING MAIN LANDING GEAR BRAKE ASSEMBLY, WHEEL LOCKED UP AFTER BRAKE APPLICATION. INVESTIGATION FOUND CARBON DI SKS WERE REPAIRED BY MATING TWO WORN PIECES TOGETHER. THIS IS DONE BY AIRCRAFT BRAKING SYSTEMS 2 FOR 1 PROGRAM. THE AD DITIONAL CLEARANCE INDUCED BY MATING TWO DISKS INTO ONE AND MULTIPLYING BY THE NUMBER OF DISKS IN A BRAKE CREATES A COND ITION THAT WILL NOT ALLOW ENOUGH CLEARANCE FOR THE DISKS TO TURN AFTER THE BRAKE PISTONS RELAX. THIS CONDITION, IF UNNO TICED, COULD LEAD TO OVERHEATING OF THE BRAKE SYSTEM AND BRAKE FAILURE OR FIRE. 2 L 7 2 4F RT A21EA 2001082900079 20010829 00079 EA 2001 8 29 DJFA200100015 1 20010413 A 3242 5002523 BRAKE CNDAIR CL600 CL6002B16 1900305 EA MLG SEIZED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 653CW 5053 UPON REPLACING MAIN LANDING GEAR BRAKE ASSEMBLY, WHEEL LOCKED UP AFTER BRAKE APPLICATION. INVESTIGATION FOUND CARBON DI SKS WERE REPAIRED BY MATING TWO WORN PIECES TOGETHER. THIS IS DONE BY AIRCRAFT BRAKING SYSTEMS 2 FOR 1 PROGRAM. THE AD DITIONAL CLEARANCE INDUCED BY MATING TWO DISKS INTO ONE AND MULTIPLYING BY THE NUMBER OF DISKS IN A BRAKE CREATES A COND ITION THAT WILL NOT ALLOW ENOUGH CLEARANCE FOR THE DISKS TO TURN AFTER THE BRAKE PISTONS RELAX. THIS CONDITION, IF UNNO TICED, COULD LEAD TO OVERHEATING OF THE BRAKE SYSTEM AND BRAKE FAILURE OR FIRE. 2 L 7 2 4F RT A21EA 2001082900080 20010829 00080 NM 2001 8 29 DL76L011288 1 20010805 A 2701 YOKE BOEING 767 767332 1382001 NM COCKPIT ERRATIC A DALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 27 192DN 28449 ON CLIMBOUT PASS 250 KTS THE YOKE STARTED TO OSCILLATE IN THE ELEVATOR WITH OR WITHOUT THE AUTOPILOT ON. IT DID SLIGHTL Y DAMPER WITH THE LT AUTOPILOT BUT NOT THE CNTR OR RT AUTOPILOT. THOROUGHLY INSPECTED AIRCRAFT, UNABLE TO DUPLICATE. 2 L 7 2 4F RT A1NM 2001082900081 20010829 00081 NM 2001 8 29 EISA20010076 1 20010424 A 2197 WIRE BOEING 727 727277 138408S NM CABIN PRESSURE DAMAGED A EISA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 275WC 20549 AIRCRAFT LOST PRESSURE AT FL 250, AIR TURNBACK TO IND. REMOVED AND REPLACED 13TH STAGE MOD VALVE PER M/M 36-12, NO HELP ITEM REMAINS OPEN. FERRIED AIRCRAFT FOR MAINT. FOUND DAMAGED WIRE SPLICE IN E-4 POWER SHEILD. REPAIRED PER M/M 21, OP S CHECK NORMAL. 2 L 7 3 4F RT A3WE 2001082900082 20010829 00082 NM 2001 8 29 EISA20010077 1 20010430 A 2130 STATIC LINE BOEING 727 727277 138408S NM CABIN PRESSURE LOOSE A EISA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 275WC 20549 AIRCRAFT LOST CABIN PRESSURE ON CLIMBOUT. AIR TURNBACK. SECURED STATIC LINE TO PRESSURE CONTROLLER IAW M/M 31-30-0. R EPLACED DAMAGED WIRE SPLICE TO FLOW CONTROL RELAY IN E-4 POWER SHIELD PER M/M 21-00 & 20-30-22. 2 L 7 3 4F RT A3WE 2001082900083 20010829 00083 NE 2001 8 29 EISA20010106 2 20010716 A 7314 PUMP BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE FAILED A EISA H DEACTIVATE SYST/CIRCUITS X ENGINE FLAMEOUT CR CRUISE 1 SW 07 353PA 20622 NR 2 ENGINE QUIT RUNNING AT FL190. OIL PRESSURE WENT TO 20 PSI. SHUT ENGINE DOWN AT 2250Z, DECLARED EMERGENCY. MADE U NEVENTFUL LANDING. (WINDMILLING PRESSURE). REMOVED AND REPLACED NR 2 ENGINE HP FUEL PUMP. 2 L 7 3 4F 4 F A3WE E2EA 2001082900084 20010829 00084 NM 2001 8 29 EISA20010107 1 20010719 A 2130 GROUND WIRE BOEING 727 7272M7 138407S NM CABIN PRESSURE LOOSE A EISA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 721RW 21200 A/C WOULD NOT PRESSURIZE (ALL MODES). RESECURED GROUND TO FLOW CONTROL VALVES (SHARD GRND FOR BOTH). A/C PRESSURIZATIO N AND PNEUMATIC SYSTEMS, OPS OK. 2 L 7 3 4F A3WE 2001082900085 20010829 00085 NM 2001 8 29 ERKR200100132 1 20010618 A 5720 655220914 FITTING BOEING 737 737247 138448D NM LT WING CRACKED B L7RA K NONE O OTHER IN INSP/MAINT 1 WP 07 902WC 19613 DURING A-CHECK INSPECTION FOUND THE LEFT HAND SWING LINK FITTING CRACKED. REMOVED AND REPLACED LEFT HAND SWING LINK FIT TING PER BOEING 737 MM 57-20-01 AND BOEING DWR 65-46400 REV G SH:0001. 2 L 7 2 4F A16WE 2001082900086 20010829 00086 NM 2001 8 29 ERKR200100133 1 20010619 A 5310 65B0187029 SHEAR TIE BOEING 747 747SR46 NM FUSELAGE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 478EV 21033 CRACKED SHEAR TIE AT LIGHTENING HOLES BETWEEN STA 340-STA 360, WL.199.80. THE CRACK WAS FOUND AT A LIGHTENING HOLE IN S HEAR TIE LOCATED BETWEEN STA 340 AND STA 360, WL 199.80. REMOVED AND REPLACED THE DAMAGED SHEAR TIE PER ECRA 478-53-125 -2. 2 L 7 4 4F A20WE 2001082900087 20010829 00087 NM 2001 8 29 ERKR200100134 1 20010619 A 5720 65B116146 BEAM BOEING 747 747SR46 NM RT WING CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 478EV 21033 CRACKED UPPER T-CHORD OF RT WING T/E BEAM AT WING 235.20. THE CRACK WAS FOUND IN THE UPPER T-WING TRAILING EDGE BEAM AT WBL 235.20. THE REPAIR WAS ACCOMPLISHED BY REMOVING AND REPLACING THE DAMAGED AREA OF THE CHORD WITH NEWLY FABRICATED CHORD, REPAIR STRAPS AND REPAIR ANGLES PER ECRA 478-57-106-2. 2 L 7 4 4F A20WE 2001082900088 20010829 00088 NM 2001 8 29 ERKR200100135 1 20010619 A 5710 65B108211 SPLICE BOEING 747 747SR46 NM WING CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 478EV 21033 LEFT AND RIGHT BS 1241 REAR SPAR- ANGLE SPLICE. THIS ECRA SPLICES IN A NEW SECTION OF 65B10821-1 ANGLE ON BOTH SIDES UP TO THE INBOARD EDGES OF THE BULKHEAD FITTINGS. REPAIR IS ACCOMPLISHED USING A SPLICE ANGLE AT LBL 80 AND RBL 80. ADDI TIONALLY THE TAPERSHANK FASTENERS REMOVED DURING ACCOMPLISHMENT OF THE SB 747-57-2263 ARE REPLACED WITH STRAIGHT SHANK H I-LOK FASTENERS PER THIS ECRA 478-57-107-2. 2 L 7 4 4F A20WE 2001082900089 20010829 00089 NM 2001 8 29 ERKR200100136 1 20010625 A 5330 SKIN BOEING 747 747238B 1384828 NM FUSELAGE DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 307TW 20009 EXISTING FUSELAGE SKIN REPAIR AT STA 2424, S-46L- S-51L. 2 L 7 4 4F A20WE 2001082900090 20010829 00090 NM 2001 8 29 ERKR200100137 1 20010626 A 5330 SKIN BOEING 747 747238B 1384828 NM FUSELAGE DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 307TW 20009 STA 2484, S-15R FUSELAGE SKIN DAMAGED. 2 L 7 4 4F A20WE 2001082900091 20010829 00091 NM 2001 8 29 ERKR200100138 1 20010626 A 5330 SKIN BOEING 747 747238B 1384828 NM FUSELAGE DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 307TW 20009 EXISTING FUSELAGE SKIN REPAIR AT STA 2436, S-46R - S-51R. 2 L 7 4 4F A20WE 2001082900092 20010829 00092 NM 2001 8 29 ERKR200100139 1 20010626 A 5330 SKIN BOEING 747 747238B 1384828 NM FUSELAGE DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 307TW 20009 EXISTING REPAIR - FUSELAGE SKIN, STA 2290- 2315, STR 46R - 50R. 2 L 7 4 4F A20WE 2001082900093 20010829 00093 NM 2001 8 29 ERKR200100140 1 20010626 A 5330 SKIN PANEL BOEING 747 747238B 1384828 NM FUSELAGE DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 307TW 20009 REPAIR OF SKIN PANEL, FS 2360-2377, STR 40R-40L. 2 L 7 4 4F A20WE 2001082900094 20010829 00094 NM 2001 8 29 ERKR200100141 1 20010626 A 5330 SKIN PANEL BOEING 747 747238B 1384828 NM FUSELAGE DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 307TW 20009 REPAIR OF SKIN PANEL, FS 2160, STR 46L. 2 L 7 4 4F A20WE 2001082900095 20010829 00095 NM 2001 8 29 ERKR200100142 1 20010626 A 5330 SKIN PANEL BOEING 747 747238B 1384828 NM FUSELAGE DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 307TW 20009 REPAIR OF SKIN PANEL, FS 2020 TO 2144, STR 48R TO 49L. 2 L 7 4 4F A20WE 2001082900096 20010829 00096 NM 2001 8 29 AWXA0002191 1 20010822 A 5310 65184201 SKIN BOEING 737 73733A 1384673 NM BS 338 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 D: L1 door fuselage cutout lower aft corner cracked 1/4" out of fastener hole BS338.C: Repaired skin at L1 door cutout l ower aft corner IAW AWA ER 03-5330-01234-DD1 2 L 7 2 4F RT A16WE 2001082900097 20010829 00097 NM 2001 8 29 ERKR200100143 1 20010626 A 5710 SPLICE PLATE BOEING 747 747238B 1384828 NM WING DAMAGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 307TW 20009 WING REAR SPAR LOWER SPLICE PLATE - HOLE - K COUNTERBORED. 2 L 7 4 4F A20WE 2001082900098 20010829 00098 NM 2001 8 29 ERKR200100145 1 20010823 A 5240 HINGE DOUG MD90 MD9030 3023690 NM GALLEY DOOR GOUGED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 P4MDG 53579 AFT GALLEY/SERVICE DOOR HINGE ARM GOUGED 2 PLACES AS MARKED. BLENDED GOUGES ON AFT GALLEY SERVICE DOOR HINGE PER MD-90 SRM 52-00-01 PG 3. 2 L 7 2 4F RT A6WE 2001082900099 20010829 00099 NM 2001 8 29 ERKR200100146 1 20010824 A 5320 STRAP BOEING 747 747212B 1384886 NM FUSELAGE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 485EV 20712 REPAIR OF CRACK STRAP COMMON TO STA 2231 FRAME, B/T WL 200-220. 2 L 7 4 4F A20WE 2001082900100 20010829 00100 NM 2001 8 29 ERKR200100147 1 20010824 A 5330 SKIN BOEING 747 747212B 1384886 NM FUSELAGE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 485EV 20712 LOWER AFT CARGO DOOR OPENING, UPPER CORNER CRACKS. 2 L 7 4 4F A20WE 2001082900101 20010829 00101 NM 2001 8 29 ERKR200100148 1 20010824 A 5414 SKIN BOEING 747 747212B 1384886 NM NR 4 PYLON CHAFED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 485EV 20712 CHAFED NR 4 PYLON SKIN AND EXISTING DOUBLER AT NAC STA 233-238. 2 L 7 4 4F A20WE 2001082900102 20010829 00102 WP 2001 8 29 ERKR200100149 1 20010824 A 5230 SKIN DOUG DC9 DC915F 3022037 WP CARGO DOOR DAMAGED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 916F 47044 UPPER CARGO DOOR OUTER SKIN DAMAGED. 2 L 7 2 4F A6WE 2001082900103 20010829 00103 WP 2001 8 29 ERKR200100150 1 20010827 A 5230 59101575 PAN DOUG DC9 DC915F 3022037 WP CARGO DOOR CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 916F 47044 CRACKED INNER DOOR PAN ON AFT CARGO PIT DOOR (P/N: 5910157-5). 2 L 7 2 4F A6WE 2001082900104 20010829 00104 WP 2001 8 29 ERKR200100151 1 20010827 A 5210 DOUBLER DOUG DC9 DC915F 3022037 WP L1 DOOR CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 916F 47044 L1 DOOR UPPER FWD CORNER INNER DOUBLER CRACK. 2 L 7 2 4F A6WE 2001082900105 20010829 00105 WP 2001 8 29 ERKR200100153 1 20010827 A 5313 LONGERON DOUG DC9 DC915F 3022037 WP FUSELAGE CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 916F 47044 LONGERON 30 CORROSION - FS 285. 2 L 7 2 4F A6WE 2001082900106 20010829 00106 NM 2001 8 29 AALA20011490 1 20010723 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 353AA 24034 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 23B INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT CONNE CTOR AT SEAT 23B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001082900107 20010829 00107 NM 2001 8 29 AALA20011489 1 20010723 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN INOPERATIVE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 353AA 24034 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 29B INOPERATIVE. REPAIRED BROKEN WIRE AT SEAT 29B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001082900108 20010829 00108 NM 2001 8 29 AALA20011526 1 20010729 A 2700 8000000016 TRANSMITTER BOEING 757 757223 1384957 NM AFT ACCY INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 185AN 32379 MIA - FLT 922 - EN ROUTE MIA-LPB, STABILIZER TRIM EICAS MESSAGE AND STABILIZER TRIM CAUTION LIGHT ILLUMINATED. RETURNED TO MIA LANDING WITHOUT INCIDENT. REPLACED RIGH STABILIZER TRIM MODULE TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERA TION. (M) 2 L 7 2 4F RT A2NM 2001082900109 20010829 00109 NM 2001 8 29 AALA20011519 1 20010727 A 3350 02019241005 LIGHT BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 913AN 29514 SNA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH FLOOR LIGHT AT FORWARD GALLEY BROKEN. REPLACED EMERGENCY EXIT ESCAPE PATH FLOOD LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2001082900110 20010829 00110 NM 2001 8 29 AALA20011462 1 20010718 A 5300 SKIN BOEING 727 727223 1384074 NM FS 1050 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 883AA 21522 TUL - FOUND FUSELAGE SKIN RIVET SHEARED AT STATION 1050 INBOARD OF STRINGER 27R NEAR REPAIR DOUBLER, CORROSION ON SKIN. FOUND RIVET SHEARED FROM CORROSION. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 2001082900111 20010829 00111 NM 2001 8 29 AALA20011460 1 20010718 A 5300 WEB BOEING 727 727223 1384074 NM FS 870 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 883AA 21522 TUL - FOUND CRACK IN FORWARD AND AFT SIDE OF 870 WEB AT APU LOAD CONTROL DISCHARGE CUT-OUT. INSTALLED REPAIR DOUBLER PE R SRM 53-10-2 FIG 1, SHEET 2. (M) 2 L 7 3 4F A3WE 2001082900112 20010829 00112 NM 2001 8 29 AALA20011485 1 20010719 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 873AA 21385 TUL - FOUND RIGHT BUTT LINE 10 CORROSION ON TOP OF FLOORBEAM STATION 380. REPAIRED FLOORBEAM PER 53-10-08. (M) 2 L 7 3 4F A3WE 2001082900113 20010829 00113 NM 2001 8 29 AALA20011484 1 20010717 A 5300 STRINGER BOEING 727 727223 1384074 NM FS 340 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 873AA 21385 TUL - FOUND CRACKS IN UPPER LEG STRINGER 5R AT STATION 340. ROUTED OUT CRACKED AREAS, INSTALLED TWO J-ANGLE REPAIRS PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 2001082900114 20010829 00114 NM 2001 8 29 AALA20011483 1 20010718 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 873AA 21385 TUL - FOUND CORROSION ON THE TOP OF THE FLOORBEAM AND FAST HOLES STATION 380 RBL 20-60. CUT OUT AND REMOVED CORROSION A ND INSTALLED REPAIRS PER 53-10-8 PAGE 9A AND 9B AND 53-10-8 FIG 1 STIFFENER REPAIRS AND FILLERS. (M) 2 L 7 3 4F A3WE 2001082900115 20010829 00115 WP 2001 8 29 AALA20011475 1 20010712 A 5300 LONGERON DOUG DC9 DC982 3022082 WP FS 160 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 522AA 49899 TUL - FOUND CRACK AROUND FASTENER AT FS 160 LONGERON 4L. REMOVED LONGERON FROM FS 149-174. INSTALLED NEW LONGERON AND SPLICED PER SRM 53-02 FIG 18 AND SRM 53-14-1. (M) 2 L 7 2 4F A6WE 2001082900116 20010829 00116 WP 2001 8 29 AALA20011479 1 20010716 A 5300 FRAME DOUG DC9 DC982 3022082 WP FS 712 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7522A 49899 TUL - FOUND DAMAGE TO CARGO FRAME STATION 712, BETWEEN 26L AND 27L. INSTALLED DOUBLER PER AARD 53-10-00-4. (M) 2 L 7 2 4F A6WE 2001082900117 20010829 00117 WP 2001 8 29 AALA20011480 1 20010711 A 5100 TRACK DOUG DC9 DC982 3022082 WP FS 1174-1307 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7522A 49899 TUL - FOUND CORROSION BEYOND MM LIMITS SEAT TRACK NR 1 STATION 1174-1307. INSTALLED NEW SECTION OF TRACK PER SRM 51-10. 2 L 7 2 4F A6WE 2001082900118 20010829 00118 WP 2001 8 29 AALA20011481 1 20010720 A 5300 SKIN DOUG DC9 DC982 3022082 WP FS 266 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7522A 49899 TUL - FUOND FUSELAGE SKIN DENTED AT RIVET STATION 266 ABOVE LONGERON 23R. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PE R SRM 53-04 FIG 38 SHEET 24. (M) 2 L 7 2 4F A6WE 2001082900119 20010829 00119 WP 2001 8 29 AALA20011482 1 20010718 A 5300 FRAME DOUG DC9 DC982 3022082 WP FS 1485 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7522A 49899 TUL - FOUND RIGHT CANT FRAME 1485, RT LOWER END, IS WORN AND CRACKED FROM CONTACT WITH ACTUATOR CASTING. INSTALLED REPA IR DOUBLER AS PER AARD 53-10-00-33 AND RE-INSTALLED FRAME STIFFENER. (M) 2 L 7 2 4F A6WE 2001082900120 20010829 00120 NM 2001 8 29 AALA20011409 1 20010709 A 5300 SHEAR TIE BOEING 727 727227 1384078 NM FS 720A CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 726AA 20733 TUL - FOUND CORROSION ON SHEAR TIE BS 720A AT STRINGER 28. REMOVED CORROSION AND REMOVED DAMAGED AREA, AND REPAIRED PER SRM 53-10-04. (M) 2 L 7 3 4F A3WE 2001082900121 20010829 00121 WP 2001 8 29 AALA20011474 1 20010713 A 5300 SEAT TRACK DOUG DC9 DC982 3022082 WP FS 435 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7522A 49899 TUL - FOUND CORROSION ON SEAT TRACK NR 4, STATION 435. CUT OUT CORRODED AREA AND INSTALLED PLUG PER HARD 53-20-00-10. (M) 2 L 7 2 4F A6WE 2001082900122 20010829 00122 WP 2001 8 29 AALA20011470 1 20010709 A 5300 SEAT TRACK DOUG DC9 DC982 3022082 WP FS 1200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7522A 49899 TUL - FOUND CORROSION ON SEAT TRACK NR 2, STATION 1200. REMOVED CORROSION, INSTALLED SEAT TRACK PLUG PER SRM 53-05 FIG 4A. (M) 2 L 7 2 4F A6WE 2001082900123 20010829 00123 WP 2001 8 29 AALA20011471 1 20010716 A 5300 SKIN DOUG DC9 DC982 3022082 WP FS 249 A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7522A 49899 TUL - FOUND SEVERAL DEEP TOOL MARKINGS AROUND RIVET HEAD RIGHT STATION 249 LONGER 21R, FUSELAGE SKIN. INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M) 2 L 7 2 4F A6WE 2001082900124 20010829 00124 WP 2001 8 29 AALA20011512 1 20010723 A 3200 SENSOR DOUG DC9 DC982 3022082 WP NR 1 BRAKE DEFECTIVE A AALA K O NONE OTHER J O WARNING INDICATION OTHER DE DESCENT 1 SW 21 7526A 49918 SFO - FLT 1782 - EN ROUTE DFW-SFO - DURING FINAL DESCENT, DECLARED EMERGENCY LANDING DUE TO NR 1 BRAKE EXCESSIVE HIGH TE MPERATURE. LANDED SFO WITHOUT INCIDENT. REPLACED NR 1 BRAKE TEMP SENSOR. PERFORMED OPS CHECK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001082900125 20010829 00125 WP 2001 8 29 AALA20011509 1 20010721 A 5600 59515841 WINDOW DOUG DC9 DC982 3022082 WP CABIN CRACKED A AALA A UNSCHED LANDING J O WARNING INDICATION OTHER CL CLIMB 1 SW 21 7525A 49917 BNA - FLT 1379 - EN ROUTE PIT-DFW, AIR INTERRUPTED TO BNA DUE TO CRACKED WINDOW AT 14A. LANDED BNA WITHOUT INCIDENT. R EPLACED CRACKED WINDOW AT 14A. PRESSURIZATION AND LEAK CHECK OK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001082900126 20010829 00126 NM 2001 8 29 USAA010935 1 20010725 A 5300 SKIN BOEING 757 757225 1384959 NM BS 373 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND LIGHTNING STRIKE ON FUSELAGE SKIN, BS 373 BETWEEN S25R AND S26R. PREVIOUSLY INSTALLED .21875 RIVET PER SRM 53-00-01, FIG 207. (M) 2 L 7 2 4F RT A2NM 2001082900127 20010829 00127 NM 2001 8 29 USAA010916 1 20010725 A 5300 FRAME BOEING 757 757225 1384959 NM BS 580 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND FRAME DENTED APPROX .25 INCH IN DIAMETER, BS 580 ABOVE S23L. INSTALLED REPAIR DUOBLER PER EA 69872. (M) 2 L 7 2 4F RT A2NM 2001082900128 20010829 00128 NM 2001 8 29 USAA010917 1 20010725 A 5300 FRAME BOEING 757 757225 1384959 NM BS 600 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND FRAME DENTED APPROX .25 INCH IN DIAMETER, BS 600 BETWEEN S23L AND S24L. INSTALLED REPAIR DOUBLER PER EA 698 74. (M) 2 L 7 2 4F RT A2NM 2001082900129 20010829 00129 NM 2001 8 29 USAA010914 1 20010725 A 5300 FRAME BOEING 757 757225 1384959 NM BS 620 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND FRAME DENTED APPROXIMATELY .25 INCH IN DIAMETER, BS 620 AT S24L. INSTALLED REPAIR DOUBLER PER EA 69875. (M ) 2 L 7 2 4F RT A2NM 2001082900130 20010829 00130 NM 2001 8 29 USAA010918 1 20010725 A 5300 FRAME BOEING 757 757225 1384959 NM BS 700 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND FRAME DENTED APPROXIMATELY .5 INCH, BS 700 AT S23L. INSTALLED REPAIR DOUBLER PER EA 85014. (M) 2 L 7 2 4F RT A2NM 2001082900131 20010829 00131 NM 2001 8 29 USAA010919 1 20010725 A 5400 DOUBLER BOEING 757 757225 1384959 NM NR 1 PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND PYLON INT DOUBLER CRACKED .5 INCH, NR 1 PYLON PP STATION 107, LOWER FORWARD CORNER, PANEL NR 433AL. INSTALL ED REPAIR DOUBLER PLATE PER EA 85055. (M) 2 L 7 2 4F RT A2NM 2001082900132 20010829 00132 NM 2001 8 29 USAA010912 1 20010725 A 5300 STRINGER BOEING 757 757225 1384959 NM BS 466 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND STRINGER CRACKED, BS 466, STRINGER 21R. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER SRM 53-00-03. (M) 2 L 7 2 4F RT A2NM 2001082900133 20010829 00133 NM 2001 8 29 USAA010913 1 20010725 A 5300 FRAME BOEING 757 757225 1384959 NM BS 1340 GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND FRAME GOUGED APPROXIMATELY .25 INCH, BS 1340 AT S26L. REPAIR DOUBLER INSTALLED PER TYPICAL REPAIR 53-60-01. (M) 2 L 7 2 4F RT A2NM 2001082900134 20010829 00134 NM 2001 8 29 USAA010915 1 20010725 A 5300 DOUBLER BOEING 757 757225 1384959 NM BS 640 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND A 2 INCH AREA OF FRAME CORRODED, BS 640, MID CHORD, BETWEEN S25R AND S26R. CORROSION REMOVED, INSTALLED REP AIR DOUBLER PER SRM 51-10-02. (M) 2 L 7 2 4F RT A2NM 2001082900135 20010829 00135 NM 2001 8 29 USAA010920 1 20010725 A 5300 WEB BOEING 757 757225 1384959 NM BS 1380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND CREASE BEAM WEB CRACKED APPROXIMATELY .25 INCH, JUST FORWARD OF BS 1380, RBL 64. INSTALLED REPAIR DOUBLER A ND CREASE BEAM ANGLE PER SRM 51-70-13. (M) 2 L 7 2 4F RT A2NM 2001082900136 20010829 00136 NM 2001 8 29 USAA010926 1 20010725 A 5300 SEAT TRACK BOEING 757 757225 1384959 NM BS 440 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND SEAT TRACK CORRODED 1 INCH BY 1 INCH AREA, BS 440, LBL 45. CORROSION LEVEL 1, TASK NR C53-231-02. DAMAGE R EMOVED, SPLICED IN REPAIR SECTION PER SRM 53-00-52. (M) 2 L 7 2 4F RT A2NM 2001082900137 20010829 00137 WP 2001 8 29 USAAD01147 1 20010807 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 807US 48039 IND - THE SEAT MOUNTED EMERGENCY LIGHT AT ROW 30 WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY AT ROW 3 0. OPS CHECKED OK. (M) 2 L 7 2 4F A6WE 2001082900138 20010829 00138 NM 2001 8 29 USAASB01225 1 20010808 A 3350 6104789 BATTERY PACK BOEING 737 737201 1384454 NM INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 257AU 22799 BWI - MAINTENANCE FOUND THE FORWARD EXTERIOR ESCAPE SLIDE EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 2001082900139 20010829 00139 NM 2001 8 29 USAA010911 1 20010719 A 5300 FRAME BOEING 757 757225 1384959 NM BS 1600 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND FRAME DENTED .5 INCH IN DIAMETER, BS 1600, BETWEEN S25R AND S26R. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER EA 69860. (M) 2 L 7 2 4F RT A2NM 2001082900140 20010829 00140 NM 2001 8 29 USAASB01223 1 20010806 A 3350 3114981 SOCKET BOEING 737 737401 1384701 NM INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 408US 23878 CLT - MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY EXIT LIGHT, THAT ILLUMINATES THE AREA AFT OF THE FLAPS, INOPERATIVE . MAINTENANCE REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY EXIT LIGHT SOCKET. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001082900141 20010829 00141 EU 2001 8 29 USAASA01041 1 20010804 A 5600 NP1653115 WINDSHIELD AIRBUS 330 A330202 3930316 EU COCKPIT CRACKED A USAA H DEACTIVATE SYST/CIRCUITS A FLAME/FIRE CL CLIMB 1 EA 19 102UW 5947 0844 DCA - FLT 6875 - EN ROUTE LGA-DCA, WHILE CLIMBING THROUGH FL180, THE CAPTAINS WINDSHIELD OUTER PANEL SHATTERED, ACCOMPAN IED WITH BRIEF ARCING. QRH PROCEDURES WERE FOLLOWED. THE FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTE NANCE REPLACED THE CAPTAINS WINDSHIELD AND CHECKED THE WINDSHIELD HEAT. THE WINDSHIELD HEAT CHECKED OK. (M) 2 L 7 2 4F RT A46NM 2001082900142 20010829 00142 NM 2001 8 29 USAABB01065 1 20010715 A 7100 P3A0410 ROD END BOEING 767 7672B7 1385107 NM LEFT WORN A USAA O OTHER E VIBRATION/BUFFET CR CRUISE 1 EA 19 655US 25257 LGW - FLT 189 - EN ROUTE CDG-CLT, CREW NOTED LEFT ENGINE LOW TURBINE VIBRATION INDICATION IN THE 4.8-5.0 RANGE. FLIGHT DIVERTED TO LGW AND LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE REPLACED THE LEFT COMPRESSOR REAR FRAME VIBRATION TRAN SDUCER. DUE TO PREVIOUS WRITE-UP, THIS SYSTEM WAS PLACED ON MEL FOR FURTHER TROUBLESHOOTING. S/D - UPON FURTHER INVEST IGATION, MAINTENANCE FOUND THE STARTER DUCT LINK ASSEMBLY ROD END WORN. THE VIBRATIONS FROM TEH LINK ASSEMBLY WERE BEIN G PICKED UP BY THE AVM. (M) 2 L 7 2 4F RT A1NM 2001082900143 20010829 00143 EU 2001 8 29 USAAF01063 1 20010805 A 3200 1HE16 SWITCH FOKKER F28 F28MK0100 4990807 EU MLG A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 862US 11300 PIT - FLT 1851 - EN ROUTE PIT-ATL - AFTER TAKEOFF, THE LANDING GAER WOULD NOT RETRACT. THE FLIGHT RETURNED TO FIELD IN PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE GROUND/FLIGHT SWITCH. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT 2001082900144 20010829 00144 NM 2001 8 29 USAA010948 1 20010725 A 5300 PLATE BOEING 757 757225 1384959 NM BS 1675 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND SILL WEB PLATE CORRODED, 8 INCH AREA, BS 1675, L-4 DOOR. CORROSION LEVEL 2, TASK NR C53-251-02. REMOVED AN D REPLACED WEB PLATE PER SRM 51-10-02. (M) 2 L 7 2 4F RT A2NM 2001082900145 20010829 00145 NM 2001 8 29 USAA010947 1 20010725 A 5300 SKIN BOEING 757 757225 1384959 NM BS 1280 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 54141 22198 CLT - FOUND FUSELAGE SKIN CORRODED 4.6 INCHES BY 3.2 INCHES, BS 1280 S29L. CORROSION REMOVED, INSTALLED REPAIR DOUBLER PER EA 62117A. (M) 2 L 7 2 4F RT A2NM 2001082900146 20010829 00146 WP 2001 8 29 ERKR200100154 1 20010827 A 5311 FRAME DOUG DC9 DC915F 3022037 WP FUSELAGE DAMAGED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 916F 47044 FRAME HAS ELONGATED FASTENER HOLE, FS 303, L15 LEFT. 2 L 7 2 4F A6WE 2001082900147 20010829 00147 WP 2001 8 29 RRXA10882 1 20010322 A 5340 37549301N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE C-PIT DOOR FRAME NR 5 LATCH BACKUP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 5 1-1-20D, 53-1-0 AND DWG 3754930-1N. 2 L 7 4 4F RT 4A25 2001082900148 20010829 00148 WP 2001 8 29 RRXA10883 1 20010322 A 5340 37549301N FITTING DOUG DC8 DC873F 302199F WP FUSELAEGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE C-PIT DOOR FRAME NR 2 LATCH BACKUP FITTING, DAMAGE EXCEEDED LIM ITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC- 8 SRM 51-1-20D, 53-1-0 AND DWG 3754930-1N. 2 L 7 4 4F RT 4A25 2001082900149 20010829 00149 NM 2001 8 29 F3LA200100076 1 20010604 A 7711 FITTING BOEING 737 7372P6 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE LOOSE A F3LA C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 NM 03 272 489 21613 688655 REJECTED TAKEOFF. FLIGHT CREW REPORTED NR 2 ENGINE EGT EXCEEDED RED RADIAL. AN ADDENDUM WILL BE ISSUED WHEN CAUSE OF F AILURE AND CORRECTIVE ACTION IS KNOWN. ADDENDUM: PERFORMED EPR SYSTEM TEST AND FOUND NR 2 ENGINE PT7 FITTING LOOSE. T IGHTENED PT7 FITTING, PERFORMED SECOND EPR SYSTEM TEST AND CHECKED OKAY. PERFORMED TRIM PROCEDURE PER MM 71-09-200 AND OPERATIONAL CHECK. ALL PARAMETERS CHECKED OKAY. 2 L 7 2 4F 4 F RT A16WE E2EA 2001082900150 20010829 00150 WP 2001 8 29 RRXA10884 1 20010322 A 5730 5769589 SKIN DOUG DC8 DC873F 302199F WP LT WING L/E CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE FWD DRAIN HOLE ON THE LT WING O/B L/E LWR SKIN AT STA XFS 597.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-21D AND SH SK 602-627. 2 L 7 4 4F RT 4A25 2001082900151 20010829 00151 WP 2001 8 29 RRXA10886 1 20010324 A 5330 37558452N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE TOOL DAMAGE A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A DRILL START TO THE BATHTUB FITTING AT STA 1228 AND L35L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-1-0 AND DWG 3755845. 2 L 7 4 4F RT 4A25 2001082900152 20010829 00152 WP 2001 8 29 RRXA10889 1 20010324 A 5730 5751784 DOUBLER DOUG DC8 DC873F 302199F WP LT WING AUX TANK CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LH AUX TANK UPPER SPAR CAP BETWEEN STA XFS 1.25 TO XFS 113.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED P ART AND INSTALLED IAW DH SK 602-748. 2 L 7 4 4F RT 4A25 2001082900153 20010829 00153 WP 2001 8 29 RRXA10890 1 20010325 A 5340 3750545502W FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE SPLICE FITTING AT LONGERON 35R AT STA 1050, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-3-0, 53-1-0 AND DWG 370545. 2 L 7 4 4F RT 4A25 2001082900154 20010829 00154 WP 2001 8 29 RRXA10893 1 20010321 A 5753 5642960 SKIN DOUG DC8 DC873F 302199F WP LT WING TE FLAP CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND DAMAGE TO THE LEFT I/B FLAP T/E OTBD END, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FA BRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21 AND DWG 3652279. 2 L 7 4 4F RT 4A25 2001082900155 20010829 00155 WP 2001 8 29 RRXA10894 1 20010325 A 5340 3754914501 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TORQUE BOX BANANA FITTING AT STA 1150 L31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND 53-1-0. 2 L 7 4 4F RT 4A25 2001082900156 20010829 00156 WP 2001 8 29 RRXA10896 1 20010325 A 5340 37558422N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BATHTUB FITTING AT STA 1160 L29L TO L30L, DAMAGE EXCEEDED LIMIT ATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-1-0 AND DWG 3755842. 2 L 7 4 4F RT 4A25 2001082900157 20010829 00157 WP 2001 8 29 RRXA10897 1 20010322 A 5712 5769589 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB TIP LT WING L/E AT STA XFS 385-250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2. 2 L 7 4 4F RT 4A25 2001082900158 20010829 00158 WP 2001 8 29 RRXA10898 1 20010322 A 5712 5769589 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB TIP ON THE LT CENTER L/E AT STA XFS 341.500, 354.800 & 360.250, DAMA GE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2. 2 L 7 4 4F RT 4A25 2001082900159 20010829 00159 WP 2001 8 29 RRXA10900 1 20010322 A 5712 5769545 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIGHT WING L/E RIB (UPPER) AT STA XFS 816.250, DAMAGE EXCEEDED LIMITATIO NS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2. 2 L 7 4 4F RT 4A25 2001082900160 20010829 00160 WP 2001 8 29 RRXA10901 1 20010322 A 5340 37558451N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BATHTUB FITTING AT STA 1220 BETWEEN L34R TO L35R AND L35R TO L3 6R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PA RT AND INSTALLED IAW DC-8 SRM 53-1-1, 51-1-20D AND DWG 3755845. 2 L 7 4 4F RT 4A25 2001082900161 20010829 00161 WP 2001 8 29 RRXA10902 1 20010328 A 5310 47732951 SUPPORT BRACKET DOUG DC8 DC873F 302199F WP CARGO DOOR CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE MCD SUPPORT BRACKET FWD NR 7 LATCH SPOOL, DAMAGE EXCEEDED LIMIT ATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001082900162 20010829 00162 WP 2001 8 29 RRXA10903 1 20010328 A 5230 47732952 SUPPORT BRACKET DOUG DC8 DC873F 302199F WP CARGO DOOR CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE MCD BRACKET FWD NR 1 LATCH SPOOL, DAMAGE EXCEEDED LIMITATIONS I AW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 5 1-3-0. 2 L 7 4 4F RT 4A25 2001082900163 20010829 00163 WP 2001 8 29 RRXA10907 1 20010329 A 5347 5757583 SEAT TRACK DOUG DC8 DC873F 302199F WP FS420-590 RBL60 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SEAT TRACK IN THE MAIN CABIN AT STA 420-585 RBL 60, DAMAGE EXCE EDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALL ED IAW DC-8 SRM 53-2-3 FIG 14. 2 L 7 4 4F RT 4A25 2001082900164 20010829 00164 WP 2001 8 29 RRXA10908 1 20010329 A 5313 3754095102 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 35R AT STA 120-140, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 53-2-2, FI G 10 AND DWG 3754045. 2 L 7 4 4F RT 4A25 2001082900165 20010829 00165 WP 2001 8 29 RRXA10909 1 20010329 A 5321 435056961 FLOORBOARD DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AROUND/UNDER ROLLER TRACK RECEPTACLE MAIN CABIN FLOOR BOARD AT STA 122 RBL 36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIV ED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-3, FIG 10. 2 L 7 4 4F RT 4A25 2001082900166 20010829 00166 WP 2001 8 29 RRXA10911 1 20010329 A 5730 5769859 SKIN DOUG DC8 DC873F 302199F WP RT WING GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND 3 DEEP GOUGES AT RT WING UPPER L/E AT STA XFS 257.500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED DOUBLER AND INSTALLED IAW DHK 602-706-1. 2 L 7 4 4F RT 4A25 2001082900167 20010829 00167 NM 2001 8 29 F3LA200100077 1 20010526 A 5320 FLOOR SUPPORT BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 318FL 3049 26301 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR SUPPORT CHANNEL AT BS 727D, LBL 17.2, CORRODED. MAINT ENANCE REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-70-11. 2 L 7 2 4F RT A16WE 2001082900168 20010829 00168 WP 2001 8 29 RRXA10912 1 20010329 A 5330 57503659 PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE EXTERIOR OF R/H BELLY STRESSED PANEL NEAR STA 687 L33R-L35R, DA MAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PANEL AND INSTALLED IAW DWG 4750365-9. 2 L 7 4 4F RT 4A25 2001082900169 20010829 00169 WP 2001 8 29 RRXA10913 1 20010331 A 5330 5750365 PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LT BELLY STRESS PANEL AT STA 687 L33L-L35L, DAMAGE EXCEEDED LIM ITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PANEL AND INSTALLED IAW DC-8 SRM 51-3-0 AND DWG 5750365. 2 L 7 4 4F RT 4A25 2001082900170 20010829 00170 NM 2001 8 29 F3LA200100078 1 20010526 A 5320 FLOOR SUPPORT BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 318FL 3049 26301 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR SUPPORT CHANNEL AT BS 769, LBL 17.2, CORRODED. MAINTE NANCE REMOVED AND REPLACED FLOOR SUPPORT FROM BS 727 TO BS 807 PER SRM 51-70-11. 2 L 7 2 4F RT A16WE 2001082900171 20010829 00171 WP 2001 8 29 RRXA10919 1 20010406 A 5712 5769589 RIB DOUG DC8 DC873F 302199F WP LT WING CHAFED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A HOLD CHAFFED THROUGH THE RIB ON THE LT L/E AT STA 5510, DAMAGE EXCEEDED LIMITATIONS I AW DC-8 SRM. FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2. 2 L 7 4 4F RT 4A25 2001082900172 20010829 00172 NM 2001 8 29 F3LA200100079 1 20010526 A 5320 FLOOR SUPPORT BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 318FL 3049 26301 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR SUPPORT CHANNEL AT BS 767, LBL 12.5, CORRODED. MAINTE NANCE REMOVED DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER PER SRM 51-70-11, PAGES 4 THRU 7. 2 L 7 2 4F RT A16WE 2001082900173 20010829 00173 WP 2001 8 29 RRXA10926 1 20010406 A 5340 3755822513N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE BATHTUB FITTING ON FWD SIDE OF STA 340 BETWEEN L34R-35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-0, FIG 2D AND 51-1-20D. 2 L 7 4 4F RT 4A25 2001082900174 20010829 00174 NM 2001 8 29 F3LA200100080 1 20010526 A 5320 FLOOR SUPPORT BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 318FL 3049 26301 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR SUPPORT CHANNEL AT BS 792, RBL 8.1, CORRODED. MAINTEN ANCE FABRICATED AND REPAIRED FLOOR SUPPORT CHANNEL PER SRM 53-00-53, FIG 201, SRM 51-40-02 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2001082900175 20010829 00175 WP 2001 8 29 RRXA10932 1 20010407 A 5347 5758876 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND BROKEN LUGS ON THE SEAT TRACK AT STA 1590 AND 1640 LBL 48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED AND INSTALLED PART IAW DC-8 SRM 51-3-0 AND 53-2-3, FIG 8A. 2 L 7 4 4F RT 4A25 2001082900176 20010829 00176 NM 2001 8 29 F3LA200100081 1 20010526 A 5320 FLOOR SUPPORT BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 318FL 3049 26301 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR SUPPORT CHANNEL AT BS 727D, LBL 12.5, CORRODED. MAINT ENANCE REMOVED DAMAGED AREA AND INSTALLED REPAIR PER SRM 51-70-11. 2 L 7 2 4F RT A16WE 2001082900177 20010829 00177 WP 2001 8 29 RRXA10934 1 20010408 A 5320 5645332105 SUPPORT DOUG DC8 DC873F 302199F WP STA 860 LBL 55 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT MLG W/W PRESSURE WEB SUPPORT ANGLE AT STA 860 LBL 55.0, DAMAGE EXCEED ED LIMITATIONS IAW DC-8 SRM. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D AND DWG 5645332. 2 L 7 4 4F RT 4A25 2001082900178 20010829 00178 NM 2001 8 29 F3LA200100082 1 20010526 A 5320 FLOOR SUPPORT BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 318FL 3049 26301 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR SUPPORT CHANNEL AT BS 727D, LBL 8.1, CORRODED. MAINTE NANCE REMOVED DAMAGED AREA AND INSTALLED REPAIR PER SRM 51-70-11. 2 L 7 2 4F RT A16WE 2001082900179 20010829 00179 WP 2001 8 29 RRXA10936 1 20010408 A 5720 5769928217 CLIP DOUG DC8 DC873F 302199F WP LT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H WING CENTER L/E O/B END ATTACH CLIP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0 AND DWG 5769928. 2 L 7 4 4F RT 4A25 2001082900180 20010829 00180 NM 2001 8 29 F3LA200100083 1 20010526 A 5320 FLOOR SUPPORT BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 318FL 3049 26301 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR SUPPORT CHANNEL AT BS 727D, LBL 3.0 CORRODED. REMOVED DAMAGED AREA AND INSTALLED REPAIR PER SRM 51-70-11. 2 L 7 2 4F RT A16WE 2001082900181 20010829 00181 WP 2001 8 29 RRXA10937 1 20010408 A 5740 97532971 ATTACH ANGLE DOUG DC8 DC873F 302199F WP LT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING CENTER L/E VERT. ATTACH ANGLE AT LOWER END AT STA XS 520, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED PART AND INSTALLED IAAW DC-8 SRM 51-1-20D AND DWG 9753297. 2 L 7 4 4F RT 4A25 2001082900182 20010829 00182 NM 2001 8 29 F3LA200100084 1 20010526 A 5320 FLOOR SUPPORT BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 318FL 3049 26301 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR SUPPORT CHANNEL AT BS 767, LBL 8.0, CORRODED. MAINTEN ANCE REMOVED DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER PER SRM 51-70-11, PAGES 4 THRU 7. 2 L 7 2 4F RT A16WE 2001082900183 20010829 00183 WP 2001 8 29 RRXA10940 1 20010410 A 5314 5758874 CAP DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE UNDER SKIN OF C-PIT ON BEAVER TAIL (KEEL CAP) AT STA 1080 L36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND IN STALLED IAW DC-8 SRM 51-1-20D AND DH SK602-633. 2 L 7 4 4F RT 4A25 2001082900184 20010829 00184 NM 2001 8 29 F3LA200100085 1 20010526 A 5320 FLOOR SUPPORT BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 318FL 3049 26301 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR SUPPORT CHANNEL AT BS 767, LBL 3.0, CORRODED. MAINTEN ANCE REMOVED DAMAGED AREA AND FABRICATED AND INSTALLED ANGLE PER SRM 51-70-11. 2 L 7 2 4F RT A16WE 2001082900185 20010829 00185 WP 2001 8 29 RRXA10943 1 20010410 A 5730 580273659 DOUBLER DOUG DC8 DC873F 302199F WP LT WING L/E CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TEE DOUBLER LOWER LT WING AT STA XW 467, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DH SK 602-746 AND 8110-3. 2 L 7 4 4F RT 4A25 2001082900186 20010829 00186 NM 2001 8 29 F3LA200100086 1 20010526 A 5320 FLOOR SUPPORT BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 318FL 3049 26301 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR SUPPORT CHANNEL AT BS 767, RBL 3.0, CORRODED. MAINTEN ANCE REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-70-11 AND 51-40-02. 2 L 7 2 4F RT A16WE 2001082900187 20010829 00187 WP 2001 8 29 RRXA10946 1 20010411 A 5730 5643000 PANEL DOUG DC8 DC873F 302199F WP RT WING CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RT WING LOWER T/E PANEL O/B OF FLAP HINGE 410, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. NO DELAMINATION NOTED, NO ACTION REQUIRED. 2 L 7 4 4F RT 4A25 2001082900188 20010829 00188 WP 2001 8 29 RRXA10947 1 20010411 A 5340 37558541 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BATHTUB FITTING AT STA 1160 TO 1220 AND L34R TO L33R, DAMAGE EX CEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC- 8 SRM 51-1-21 AND 53-2-0, FIG 26. 2 L 7 4 4F RT 4A25 2001082900189 20010829 00189 NM 2001 8 29 F3LA200100087 1 20010526 A 5320 FLOOR SUPPORT BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 318FL 3049 26301 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR SUPPORT CHANNEL AT BS 767, RBL 8.10, CORRODED. MAINTE NANCE REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-00-53. 2 L 7 2 4F RT A16WE 2001082900190 20010829 00190 NM 2001 8 29 F3LA200100088 1 20010526 A 5320 FLOOR SUPPORT BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 318FL 3049 26301 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR SUPPORT CHANNEL AT BS 767, RBL 13.8, CORRODED. MAINTE NANCE REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-60-53 AND 51-40-02. 2 L 7 2 4F RT A16WE 2001082900191 20010829 00191 NM 2001 8 29 F3LA200100089 1 20010526 A 5320 FLOOR SUPPORT BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 318FL 3049 26301 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR SUPPORT CHANNEL AT BS 727D, RBL 3.0, CORRODED. MAINTE NANCE REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-70-11. 2 L 7 2 4F RT A16WE 2001082900192 20010829 00192 NM 2001 8 29 F3LA200100093 1 20010625 A 5320 WEB BOEING 737 7372L9 1384497 NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 2967 22734 DURING C-1 CHECK, FLIGHT CREW REPORTED SEVERAL CRACKS FROM RIVET HOLE BEHIND THE 178 BULKHEAD IN THE FLOOR STRUCTURE AT BS 180, WL 207. MAINTENANCE REMOVED CRACKS FROM RIVET HOLE AND INSTALLED REPAIR PARTS PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001082900193 20010829 00193 2001 8 29 SWAA012309 4 20010817 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 331SW 23695 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001082900194 20010829 00194 NM 2001 8 29 SWAA012310 1 20010818 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 656SW 28401 EEPLS LOOSE AT ROW 16. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001082900195 20010829 00195 NM 2001 8 29 SWAA012311 1 20010817 A 3350 6104781 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED RON, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2001082900196 20010829 00196 NM 2001 8 29 SWAA012313 1 20010816 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED A1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001082900197 20010829 00197 NM 2001 8 29 SWAA012320 1 20010817 A 5330 6546881 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CANNING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 520SW 25319 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN OIL CANNED AT BS 1026, BETWEEN STR 27L & 27R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001082900198 20010829 00198 NM 2001 8 29 SWAA012321 1 20010812 A 5712 6545444 RIB BOEING 737 7375H4 138449D NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 520SW 25319 DURING SCHEDULED D-CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT STR 2, WBL 135.5. REPAIRED CHORD PER BFG ER. 2 L 7 2 4F RT A16WE 2001082900199 20010829 00199 2001 8 29 SWAA012330 4 20010818 A 2565 D31354 SLIDE BOEING 737 7377H4 NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 738CB 27870 AFT ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001082900200 20010829 00200 2001 8 29 SWAA012331 4 20010820 A 2565 D31354 SLIDE BOEING 737 7372T4 1384492 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001082900201 20010829 00201 2001 8 29 SWAA012332 4 20010818 A 2565 D31354 SLIDE BOEING 737 7377H4 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 708SW 27842 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER M M. 2 L 7 2 4F RT A16WE 2001082900202 20010829 00202 2001 8 29 SWAA012333 4 20010818 A 2565 D31354 SLIDE BOEING 737 7377H4 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 708SW 27842 DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER M M. 2 L 7 2 4F RT A16WE 2001082900203 20010829 00203 NM 2001 8 29 SWAA012335 1 20010817 A 3350 6104789 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT AFT CABIN. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2001082900204 20010829 00204 NM 2001 8 29 SWAA012336 1 20010819 A 3397 BR2013 WIRE BOEING 737 7375H4 138449D NM CABIN DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 504SW 24181 DURING SCHEDULED C2 CHECK, FOUND EEPLS INOP AND COVER BROKEN AT ROWS NR 1 & 2. REPAIRED EEPLS WIRES AND REMOVED AND REP LACED COVER PER MM. 2 L 7 2 4F RT A16WE 2001082900205 20010829 00205 NM 2001 8 29 SWAA012338 1 20010818 A 3350 300432 LIGHT BOEING 737 7373H4 1384600 NM SERVICE DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED 1/4D CHECK, FOUND EXTERIOR EMERGENCY LIGHT INOP AFT OF FWD SVC DOOR. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2001082900206 20010829 00206 2001 8 29 SWAA012348 4 20010820 A 2565 D31354 SLIDE BOEING 737 7377H4 NM FWD ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 789SW 29816 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001082900207 20010829 00207 WP 2001 8 29 RRXA10948 1 20010411 A 5320 5646674 STRUCTURE DOUG DC8 DC873F 302199F WP LT WING W/W CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LT WING W/W TOP OF W/W O/B ABOVE AFT OF FLAP BUSS CABLE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND I NSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D AND DH SK 602-583. 2 L 7 4 4F RT 4A25 2001082900208 20010829 00208 WP 2001 8 29 RRXA10949 1 20010411 A 5320 5646674 STRUCTURE DOUG DC8 DC873F 302199F WP LT WING WW CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON THE LT WING W/W ABOVE TRUNION FITTING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DH SK 602 -583. 2 L 7 4 4F RT 4A25 2001082900209 20010829 00209 WP 2001 8 29 RRXA10954 1 20010412 A 5330 9754924 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION AND A CRACK TO THE SKIN AT FS 1440 L32R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-0, FIG 21 AND DH SK 602-601. 2 L 7 4 4F RT 4A25 2001082900210 20010829 00210 WP 2001 8 29 RRXA10955 1 20010412 A 5347 5758876 SEAT TRACK DOUG DC8 DC873F 302199F WP STA 500 RBL 48 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND ELONGATED SCALLOPS ON THE MAIN CABIN SEAT TRACK AT STA 500 AND RBL 48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3, FIG 8A AND 53-7-2 FIG 2A. 2 L 7 4 4F RT 4A25 2001082900211 20010829 00211 NM 2001 8 29 SWAA012349 1 20010818 A 2910 280205 FUSE BOEING 737 7377H4 NM MLG WW FAILED A SWAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 07 731SA 27863 DIVERSION, UPON FLAP RETRACTION ON DEPARTURE, L/E FLAP TRANSIT LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED L/E FLA PS SLAT HYD FUSE PER MM. 2 L 7 2 4F RT A16WE 2001082900212 20010829 00212 NM 2001 8 29 SWAA012351 1 20010817 A 2782 6544551 ACTUATOR BOEING 737 7373H4 1384600 NM L/E FLAP FAILED A SWAA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SW 07 390SW 26593 AIR TURNBACK, AFTER TAKEOFF THE RT INBOARD L/E FLAP WOULD NOT RETRACT. REMOVED AND REPLACED NR 3 KRUEGER FLAP ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2001082900213 20010829 00213 2001 8 29 SWAA012354 4 20010820 A 2565 D31354 SLIDE BOEING 737 7377H4 NM FWD ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 789SW 29816 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001082900214 20010829 00214 2001 8 29 SWAA012355 4 20010820 A 2565 61621 SLIDE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 608SW 27928 DURING SCHEDULED RON, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001082900215 20010829 00215 NM 2001 8 29 SWAA012356 1 20010819 A 3350 300432 LIGHT BOEING 737 7372T4 1384492 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT LT EXTERIOR OVERWING. RELAMPED PER MM. 2 L 7 2 4F A16WE 2001082900216 20010829 00216 NM 2001 8 29 SWAA012364 1 20010821 A 2782 381800 ACTUATOR BOEING 737 7377H4 NM L/E SLAT FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 731SA 27863 AIR TURNBACK, AFTER TAKEOFF L/E EDGE TRANSIT LIGHT STAYED ILLUMINATED. REMOVED AND REPLACED NR 2 L/E SLAT ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2001082900217 20010829 00217 NM 2001 8 29 SWAA012366 1 20010821 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 376SW 26585 DURING SCHEDULED 1/4D CHECK, FOUND EEPLS INOP AT ROW 20. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001082900218 20010829 00218 EA 2001 8 29 COMA0160636 1 20010826 A 5346 60135006962 ANGLE CNDAIR CL600 CL6002B19 EA AFT EQUIP BAY CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 920CA 18424 7022 SKIN ATTACH ANGLE AT TOP RT 0/B END OF ENGINE SUPPORT BEAM WAS CRACKED.REMOVED DAMAGED ANGLE AND INSTALLED NEW ANGLE I/A /W CRJ SRM 51-42-21 AND 51-42-20. 2 L 7 2 4F RT A21EA 2001082900219 20010829 00219 EA 2001 8 29 COMA0160637 1 20010826 A 5346 WEB CNDAIR CL600 CL6002B19 EA AFT EQUIP BAY CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 920CA 18424 7022 ENGINE SUPPORT BEAM IN AFT EQUIPMENT BAY WAS CRACKED AT TWO PLACES IN THE CENTER SECTION OF THE BEAM.REMOVED DAMAGED ARE AS OF ENGINE SUPPORT BEAM AND REPAIRED BEAM BY INSTALLING ANGLE DOUBLERS I/A/W BOMBARDIER REO 601R-53-61-345 REV B. 2 L 7 2 4F RT A21EA 2001082900220 20010829 00220 NM 2001 8 29 VNAA0107023 1 20010729 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 423JS 11404 113 3032 THE CREW REPORTED THAT SOME OF THE EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMER GENCY BATTERY AT THE 4LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFO RMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001082900221 20010829 00221 NM 2001 8 29 VNAA0107024 1 20010729 A 5270 SWITCH DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE AIR DOOR OUT OF ADJ A VNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 460PS 3061 AFTER DEPARTING PIT, THE CREW RECEIVED A GROUND/AIR DOOR OPEN INDICATION ON THE RED WARNING PANEL. FLIGHT 4141 RETURNED TO PIT WHERE MAINTENANCE INSPECTED AND ADJUSTED THE MICROSWITCH IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001082900222 20010829 00222 NM 2001 8 29 VNAA0108003 1 20010806 A 3150 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 426JS 3038 DURING THE TAKEOFF ROLL, THE CREW RECEIVED A TAKEOFF CONFIGURATION CAS MESSAGE AND ABORTED TAKEOFF. THE CREW RESET THE SYSTEM AND ATTEMPTED ANOTHER TAKEOFF. FLIGHT 4156 DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001082900225 20010829 00225 EA 2001 8 29 COMA0160638 1 20010825 A 5346 601R5361345 WEB CNDAIR CL600 CL6002B19 EA BEAM CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 18424 7022 ENGINE SUPPORT BEAM CRACKED IN TWO PLACES AT F.S. 640.00 CENTER SECTION UPPER AND LOWER WEBS.REPAIRED ENGINE SUPPORT BEA M AT F.S. 640.00 CENTER SECTION UPPER AND LOWER WEBS I/A/W CANADAIR R.E.O. 601R-53-61-345 REV B. 2 L 7 2 4F RT A21EA 2001082900226 20010829 00226 2001 8 29 VNAA0108009 4 20010816 A 3460 COMPUTER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 442JS 3060 DURING THE TAKEOFF ROLL, THE CREW RECEIVED A FGC HEADING HOLD FAIL AMBER CAS MESSAGE AND ABORTED TAKEOFF. THE CREW RESE T THE SYSTEM AND WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4042 DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001082900227 20010829 00227 2001 8 29 VNAA0108011 4 20010818 A 3460 COMPUTER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 438JS 3056 DURING THE TAKEOFF ROLL, THE CREW RECEIVED A FLIGHT GUIDANCE COMPUTER FAIL MESSAGE AND ABORTED TAKEOFF. THE MESSAGE CLE ARED BY ITSELF AND THE CREW CALLED MAINTENANCE CONTROL WHO ADVISED THE CREW TO ATTEMPT ANOTHER TAKEOFF. FLIGHT 4094 THE N DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001082900228 20010829 00228 NM 2001 8 29 2001UALA01774 1 20010822 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 324UA 23956 AFT CABIN RIGHT HAND SIDE STRINGER 18R CRACKED AND BENT BETWEEN STATION 927 AND 947 BELOW CREASE WEB. MAJOR REPAIR ACCO MPLISHED. STRINGER REPAIRED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082900229 20010829 00229 NM 2001 8 29 2001UALA01775 1 20010822 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 324UA 23956 FORWARD PIT FRAME STATION 500 IS CRACKED AT VERTICAL SUPPORT ANGLE FOR ANTENNA RBL 15. MAJOR REPAIR ACCOMPLISHED. INST ALLED FRAME REPAIR . 2 L 7 2 4F 4 F RT A16WE E2GL 2001082900230 20010829 00230 NM 2001 8 29 2001UALA01776 1 20010822 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 324UA 23956 FORWARD PIT FRAME STATION 500 IS CRACKED 2 PLACES AT VERTICAL SUPPORT ANGLE FOR ANTENNA MOUNT LBL 1.5. MAJOR REPAIR ACC OMPLISHED. FRAME REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091900041 20010919 00041 NM 2001 9 19 2001UALA01777 1 20010821 A 2730 162005102 COMPUTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ELEVATOR FAILED A UALA K NONE F FLT CONT AFFECTED LD LANDING 1 WP 29 596UA 28749 LANDING FLARE CONTROL PRESSURE TWICE THE NORMAL EFFORT (PITCH PRESSURE EXTREMELY HIGH). FAILURE OF THE ELEVATOR FEEL COM PUTER CAUSED THE EXTRA FORCE REQUIRED TO OPERATE THE CONTROL COLUMN. REPLACED THE ELEVATOR FEEL COMPUTER. 2 L 7 2 4F 4 F RT A2NM E17NE 2001082900231 20010829 00231 NM 2001 8 29 2001UALA01778 1 20010822 A 5320 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 516UA 24860 CABIN FLOOR INTERCOSTAL BETWEEN STA 324 AND 418, BL 0, HAS CORROSION ON UPPER SURFACE. MAJOR REPAIR ACCOMPLISHED. REMO VED AND INSTALLED NEW INTERCOSTAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2001082900232 20010829 00232 NM 2001 8 29 2001UALA01779 1 20010822 A 5330 PLATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 516UA 24860 CABIN AFT DECK PLATE CORRODED, STA 1681, RBL 1.5 TO RBL 52. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER ON DECK PLATE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001082900233 20010829 00233 NM 2001 8 29 2001UALA01780 1 20010822 A 5330 PLATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 516UA 24860 CABIN AFT DECK PLATE CORRODED, STA 1681, RBL 1.5 TO RBL 52. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER ON DECK PLATE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001082900234 20010829 00234 NM 2001 8 29 2001UALA01781 1 20010822 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1219 STRINGER 35L-36L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE RE PAIR IN ACCORDANCE WITH BAC DWG 140T2102 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082900235 20010829 00235 NM 2001 8 29 2001UALA01784 1 20010822 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1417 STRINGER 38R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REPAIR IN ACCORDANCE WITH BAC DWG 140T2102 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082900236 20010829 00236 NM 2001 8 29 2001UALA01785 1 20010822 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1307 STR 35L-36L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REPAIR IN ACCORDANCE WITH BAC DWG 140T2102 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082900237 20010829 00237 NM 2001 8 29 2001UALA01786 1 20010822 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 287 RBL 55 FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM REPAIR IN ACC ORDANCE WITH SRM 53-00-51. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082900238 20010829 00238 WP 2001 8 29 RRXA10956 1 20010412 A 5750 56514111 EXHAUST GATE DOUG DC8 DC873F 302199F WP LT WING WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A WORN EXHAUST GATE LT FLAP L/E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED PART AND INSTALLED IAAW DC-8 SRM 51-1-21A, 51-1-21 AND DWG 56414111. 2 L 7 4 4F RT 4A25 2001082900239 20010829 00239 WP 2001 8 29 RRXA10957 1 20010412 A 5321 5892041 FLOOR PANEL DOUG DC8 DC873F 302199F WP CABIN CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AROUND/UNDER ROLLER TRACKS RECEPTACLE MAIN CABIN FLOORBOARD AT FS 122 RBL 36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICA TED PART AND INSTALLED IAW DC-8 SRM 53-2-3, FIG 10 AND 51-1-20. 2 L 7 4 4F RT 4A25 2001082900240 20010829 00240 WP 2001 8 29 RRXA10960 1 20010412 A 5311 155727879 FRAME DOUG DC8 DC873F 302199F WP CABIN PUNCTURED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A LARGE PUNCTURE IN THE RADIUS OF THE MAIN CABIN FRAME 280 AT LONGERON 20L, DAMAGE EXCE EDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DH SK 602-459. 2 L 7 4 4F RT 4A25 2001082900241 20010829 00241 NM 2001 8 29 2001UALA01788 1 20010822 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1153 STRINGER 39R-38R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE RE PAIR IN ACCORDANCE WITH BAC DWG 140T2102 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082900242 20010829 00242 WP 2001 8 29 RRXA10961 1 20010412 A 5330 56149747 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SKIN AT STA 190 AND L36 TO L34R, DAMAGE EXCEEDED LIMITATIONS IA W DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51 -1-21, 51-1-20D, 53-1-0 AND DWG 5779925. 2 L 7 4 4F RT 4A25 2001090700055 20010907 00055 NM 2001 9 7 2001UALA01789 1 20010820 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM CABIN DAMAGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 785UA 26954 SEAT 1E AFTER EMERGENCY LIGHT DOES NOT WORK. FORWARD EMERGENCY LIGHT WORKS OK. LIGHT ASSEMBLY FOUND DAMAGED. REPLACED LI GHT ASSEMBLY. OPS CHECKED GOOD. 2 L 7 2 4F RT T0001SE 2001082900243 20010829 00243 NM 2001 8 29 2001UALA01791 1 20010823 A 5241 PLATE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE GALLEY DOOR MISALIGNED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 322UA 23954 AFT GALLEY DOOR BODY TORQUE TUBE UPPER AND LOWER SERPENTINE PLATES DO NOT ALIGN PROPERLY. MAJOR REPAIR ACCOMPLISHED. R EPLACED BODY T-T UPPER BEARING CASTING. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091400115 20010914 00115 NM 2001 9 14 2001UALA01792 1 20010822 A 3350 CONNECTOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7254U 21401 EMERGENCY EXIT LIGHTS AT SEAT 18C TO 24C ARE INOPERABLE. REPAIRED BAD CONNECTION. OPERATIONS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001101200066 20011012 00066 NM 2001 10 12 2001UALA01793 1 20010823 A 3350 582214 BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7448U 21902 EMERGENCY EXIT LIGHTS OVER LT OVERWING EXIT ARE INOPERABLE. *S/D* REPLACED BATTERY PACK. OPERATIONS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001090600383 20010906 00383 NM 2001 9 6 2001UALA01796 1 20010823 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1241-1263 STR 37R-38R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REP AIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082900244 20010829 00244 NM 2001 8 29 2001UALA01797 1 20010823 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 516UA 24860 CABIN FLOORBEAM 365 CORRODED AT RBL 15, 24, 30, 36, 48. MAJOR REPAIR ACCOMPLISHED. REMOVED T-CAP, INSTALLED NEW T-CAP WITH SUPPORT ANGLES AND STRAPS. 2 L 7 2 4F 4 F RT A2NM E17NE 2001082900245 20010829 00245 EA 2001 8 29 COMA0160639 1 20010825 A 5346 6013600130 DOUBLER CNDAIR CL600 CL6002B19 EA BEAM CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 18424 7022 F.S. 640.00 HAS A CRACKED DOUBLER ON THE R/H SIDE OF THE ENGINE BEAM AREA.REMOVED AND REPLACED CRACKED DOUBLER F.S. 640. 00 ON R/H SIDE OF THE ENGINE BEAM AREA I/A/W WVAC EO 601R-53-2658. 2 L 7 2 4F RT A21EA 2001082900246 20010829 00246 NM 2001 8 29 2001UALA01798 1 20010823 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 516UA 24860 AFT CABIN FLOORBEAM STATION 1640, RBL 12 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED REINFORCING ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2001090600384 20010906 00384 NM 2001 9 6 2001UALA01803 1 20010823 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1153 STRINGER 39L-39R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REP AIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090600385 20010906 00385 NM 2001 9 6 2001UALA01804 1 20010823 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1175-1197 STRINGER 39R-38R SHEAR TIE CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICAT ED AND INSTALLED SHEAR TIE REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090600388 20010906 00388 NM 2001 9 6 2001UALA01807 1 20010823 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1285 STRINGER 38R-39R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REP AIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090600391 20010906 00391 NM 2001 9 6 2001UALA01810 1 20010823 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 588 STRINGER 33L-34L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REPA IR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090600392 20010906 00392 NM 2001 9 6 2001UALA01811 1 20010823 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 434-456 STRINGER 38R CRACKED AND CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER REP AIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090600393 20010906 00393 NM 2001 9 6 2001UALA01812 1 20010823 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 610 STRINGER 37L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090600395 20010906 00395 NM 2001 9 6 2001UALA01815 1 20010823 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1285 STRINGER 37L-38L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REP AIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090600396 20010906 00396 NM 2001 9 6 2001UALA01816 1 20010823 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 434 STRINGER 33L-34L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER REPAI R. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090600398 20010906 00398 NM 2001 9 6 2001UALA01818 1 20010823 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1307 STRINGER 37L-38L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REP AIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090600399 20010906 00399 NM 2001 9 6 2001UALA01819 1 20010823 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1395 STRINGER 36R-37R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REP AIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082900247 20010829 00247 WP 2001 8 29 RRXA10963 1 20010412 A 5340 37558431N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BATHTUB FITTING AT STA 1180 BETWEEN L35L & L34R, DAMAGE EXCEED ED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SR M 53-1-01, 51-1-20D AND DWG 3755843. 2 L 7 4 4F RT 4A25 2001090700063 20010907 00063 NM 2001 9 7 2001UALA01820 1 20010823 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1373 STRINGER 37L-38L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REP AIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090700065 20010907 00065 NM 2001 9 7 2001UALA01821 1 20010823 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1373 STRINGER 36L-37L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REP AIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090700066 20010907 00066 NM 2001 9 7 2001UALA01822 1 20010823 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1153 STRINGER 38L-39L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE RE PAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090700068 20010907 00068 NM 2001 9 7 2001UALA01824 1 20010823 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1219-1241 STRINGER 38L-37L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TI E REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082900248 20010829 00248 EA 2001 8 29 COMA0160640 1 20010824 A 5270 840534 SWITCH CNDAIR CL600 CL6002B19 EA MAIN ENTRANCE DO FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 941CA 7050 FLIGHT #5612. DURING CLIMB OUT OF LIT AT 9000 FT. RECEIVED A CABIN DOOR OUTER HANDLE CAUTION MESSAGE, AIRCRAFT RETURNED TO THE FIELD.REPLACED D117 PROXIMITY SWITCH IN MAIN CABIN DOOR. 2 L 7 2 4F RT A21EA 2001082900249 20010829 00249 WP 2001 8 29 RRXA10965 1 20010412 A 5730 5644654111 SKIN DOUG DC8 DC873F 302199F WP RT WING MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND 2 HOLES IN THE R/H WING T/E WEDGE AT STA XW 761, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20, 57-2-0, FIG 2A AND DWG 5644654. 2 L 7 4 4F RT 4A25 2001090700069 20010907 00069 NM 2001 9 7 2001UALA01825 1 20010823 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 478 STRINGER 35R-36R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REPA IR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082900250 20010829 00250 NM 2001 8 29 ABXA010449 1 20010822 A 2730 COMPUTER BOEING 767 767231 1385131 NM ELEVATOR FAULTY A ABXA K NONE F E FLT CONT AFFECTED VIBRATION/BUFFET AP APPROACH 1 GL 23 702AX 22566 CREW REPORTED ELEVATOR CONTROL SURFACE PRESSURE MUCH HIGHER THAN NORMAL. AIRCRAFT WAS DIFFICULT TO ROTATE ON TAKEOFF. A VIBRATION WAS ALSO FELT IN THE CONTROL YOKE THREE TIMES ON APPROACH TO ILN. REPLACED THE ELEVATOR FEEL COMPUTER IAW B 767 AMM 27-31-19-4. ADJUSTED ELEVATOR BODY CABLES IAW B767 AMM 27-31-00-5. EVALUATION FLIGHT SATISFACTORY. 2 L 7 2 4F RT A1NM 2001082900251 20010829 00251 EA 2001 8 29 COMA0160641 1 20010823 A 3350 64645 LIGHT CNDAIR CL600 CL6002B19 EA FLOOR FAULTY A COMA K NONE S AFFECT SYSTEMS IN INSP/MAINT 1 SO 01 431CA 7472 FLIGHT #5339. DURING PRE-FLIGHT AT CVG FOUND SECTION OF FLOOR EMERGENCY LIGHTING INOPERATIVE.REPLACED EMERGENCY FLOOR L IGHT TRACKS ROWS 2 THROUGH 5 ON RIGHT SIDE OF CABIN. 2 L 7 2 4F RT A21EA 2001082900252 20010829 00252 WP 2001 8 29 ABXA010454 1 20010826 A 2611 100064901 SMOKE DETECTOR DOUG DC8 DC863F 302198F WP CARGO BAY DEFECTIVE A ABXA K NONE N FALSE WARNING CR CRUISE 1 GL 23 819AX 45927 DURING CRUISE, LOWER CARGO SMOKE DETECTOR YELLOW MAINTENANCE LIGHT ILLUMINATED WITH GREEN LIGHT ILLUMINATED. REPLACED S MOKE DETECTOR UNIT AT AD CNT. DUE TO FALSE ALARM FAULT CODE IAW DC-8 MM 26-15-00-4. SYSTEM OPS CHECKED GOOD. 2 L 7 4 4F 4A25 2001082900253 20010829 00253 WP 2001 8 29 ABXA010455 1 20010815 A 3150 WARNING SYSTEM DOUG DC8 DC861 3021952 WP COCKPIT MALFUNCTIONED A ABXA K NONE N FALSE WARNING UK UNKNOWN 1 GL 23 847AX 46031 YELLOW MAINTENANCE LIGHT ILLUMINATED WITH GREEN SYSTEM OK. LED ILLUMINATED AND NO MALFUNCTION CODES DISPLAYED. CREW DE FERRAL IAW MEL 26-10-3A. MAINTENANCE ACTION REQUIRED. CDU MX TEST INDICATED AC 4725 FALSE ALARM, RESET BREAKERS. FINA L CDU INDICATION SYSTEM OK IAW DC-8 MM 26-15-00-0-0001. 2 L 7 4 4F 4A25 2001082900254 20010829 00254 WP 2001 8 29 RRXA10966 1 20010413 A 5311 5754671502 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON THE UPPER FLANGE AT FS 1140 BETWEEN L34L TO L34R, DAMAGE EXCEEDED L IMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0, FIG 1F, 53-2-0 AND DSK 602-652. 2 L 7 4 4F RT 4A25 2001082900255 20010829 00255 NM 2001 8 29 AWXA0002186 1 20010731 A 5320 65C3760729 STIFFENER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 332AW 23384 AFT SIDE BS 178 BLKHD WEB, LBL 4.8, VERTICAL TEE CRACKED 1.5 INCH INBOARD SIDE RADIUS WL 185. REPAIRED CRACKED VERTICAL TEE BS 178 BULKHEAD LBL 4.8 IAW B737-300 SRM 53-10-8 PG 223-240 FIG 205. 2 L 7 2 4F RT A16WE 2001082900256 20010829 00256 SO 2001 8 29 C2XA01CL198 1 20010827 A 3320 7287501621 HARNESS EMB 145 EMB145ER SO CABIN DEFECTIVE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 14937 145026 CLE FLIGHT 4109 THE CREW REPORTED SMOKE APPEARED FROM CABIN LIGHTS ABOVE SEAT 1A. MAINTENANCE INSPECTED AND REPLACED TH E UPPER CABIN LIGHT HARNESS ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001082900257 20010829 00257 NM 2001 8 29 F3LA200100098 1 20010805 A 2720 654486112 PCU BOEING 737 73736E NM RUDDER MALFUNCTIONED A F3LA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 03 315FL 4957 25159 CLIMBOUT, 8 TO 10 UNCONTL RUDDER INPUTS, STRONG ENOUGH TO FEEL ACFT RESPOND. TURNED AUTOPILOT & YAW DAMPER ON & OFF, NO EFFECT. PROBLEM DISAPPEARED. CLIMBOUT, NR 1 ENG SURGED THRU 18,000 FT. TURNED AUTOTHROTTLE ON & OFF, NO EFFECT. REA CHING 18000 FT ENG RAN SMOOTH. REPLACED RUDDER PCU, RIGGED & PERF OPS CHK OF RUDDER PCU, YAW DAMPER COUPLER & FOUND NO DISCREP & ACCOMP FLT CONTL MOVEMENT CHK. THE DFDR & CVR WERE REMOVED FOR READ OUT. NO SIGNIF RUDDER MOVEMENT OR YAW OB SERVED. READ OUT SHOWED FLUX OF NR 1 ENG BEGUN 18000' & STAB 24,000'. PERF PWR ASSURANCE CHK & BORESCOPE INSPEC OF NR 1 ENG & PERF TROUBLESHOOT FOR SURGING ENG, NO FAULTS FOUND. ACCOMP TEST FLT, NO ENG SURGE OR UNCONTL RUDDER INPUT. 2 L 7 2 4F RT A16WE 2001082900258 20010829 00258 NM 2001 8 29 F3LA200100100 1 20010821 A 2910 B-NUT BOEING 737 7372L9 1384497 NM HYDRAULIC SYS LOOSE A F3LA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 03 271FL 22734 AIR TURNBACK, FLIGHT CREW REPORTED LOSS OF A-SYSTEM HYDRAULIC PRESSURE AND QUANTITY. TIGHTENED NR 1 ENGINE SUPPLY LINE B-NUT, REPLACED NR 1 ENGINE CASE DRAIN FILTER. PERFORMED LEAK CHECK AND OPERATIONAL CHECK AND CHECKED OKAY. 2 L 7 2 4F RT A16WE 2001082900259 20010829 00259 EA 2001 8 29 COMA0160642 1 20010823 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA A COMA K NONE S AFFECT SYSTEMS IN INSP/MAINT 1 SO 01 431CA 7472 FLIGHT #5570. DURING PRE-FLIGHT INSPECTION AT GRR FOUND SECTION OF RIGHT FLOOR EMERGENCY LIGHTING INOPERATIVE.CLEANED A ND RE-SEATED AFFECTED FLOOR EMERGENCY LIGHTING STRIPS, OPERATIONAL CHECK WAS SATISFACTORY. 2 L 7 2 4F RT A21EA 2001082900260 20010829 00260 NM 2001 8 29 F3LA200100101 1 20010821 A 2760 CONTROL CABLE BOEING 737 7372L9 1384497 NM LT SPOILER BROKEN A F3LA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 NM 03 270FL 3439 22733 ON WALKAROUND PRIOR TO FLIGHT, MAINTENANCE REPORTED LT SPOILER CABLE BROKEN. FABRICATED AND INSTALLED REPLACEMENT SPOIL ER CABLE PER MM 27-09-111 AND MM 20-10-91. ADJUSTED AND TESTED SYSTEM PER MM 27-61-00. 2 L 7 2 4F RT A16WE 2001082900262 20010829 00262 EA 2001 8 29 COMA0160643 1 20010823 A 2751 855D1007 BPSU CNDAIR CL600 CL6002B19 EA WING FAULTY A COMA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 01 981CA 9945 7163 FLIGHT #5620. WHILE AT THE GATE RECEIVED FLAP FAIL CAUTION MESSAGE WHEN FLAP LEVER WAS SELECTED TO 20 DEGREES.REPLACED T HE LEFT BRAKE AND POSITION SENSING UNIT. 2 L 7 2 4F RT A21EA 2001082900263 20010829 00263 WP 2001 8 29 RRXA10967 1 20010413 A 3210 5643000 PANEL DOUG DC8 DC873F 302199F WP RT MLG CHAFED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A GOUGE TO THE WING PANEL ABOVE RT MLG INBD END, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 51-3-0, MM 20-16-02 AND DH SR#4446. 2 L 7 4 4F RT 4A25 2001082900264 20010829 00264 EA 2001 8 29 COMA0160644 1 20010823 A 2751 860D10018ABC FCU CNDAIR CL600 CL6002B19 EA ELECTRICAL BAY FAULTY A COMA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 01 981CA 3555 7163 FLIGHT #5620. WHILE AT THE GATE RECEIVED FLAP FAIL CAUTION MESSAGE WHEN FLAP LEVER WAS SELECTED TO 20 DEGREES.REPLACED T HE FLAP ELECTRONIC CONTROL UNIT. 2 L 7 2 4F RT A21EA 2001082900265 20010829 00265 WP 2001 8 29 RRXA10968 1 20010413 A 5311 5755069 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE STUB FRAME AFT SIDE OF TORQUE BOX AT D-PIT DOOR AT FS 1446 AND L34R, DAM AGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0, FIG 1B. 2 L 7 4 4F RT 4A25 2001082900266 20010829 00266 WP 2001 8 29 RRXA10971 1 20010413 A 5755 56551682 SKIN DOUG DC8 DC873F 302199F WP RT WING SPOILER DENTED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND A DENT TO THE RT WING NR 4 SPOILER UPPER SURFACE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED PART, TREATED AND PRIMED, INSTALLED PART IAW DC-8 SRM 51-21-00, 57-2-3. 2 L 7 4 4F RT 4A25 2001082900267 20010829 00267 CE 2001 8 29 2001F00237 1 20010726 A 3260 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE LANDING GEAR DIRTY A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 19 16540 UE172 FLT 9316 - MHH/FLL - DURING FLIGHT, LANDING GEAR UNSAFE RED HANDLE LIGHTS ILLUMINATED WITH LANDING GEAR RETRACTED. CLEA NED UPLOCK SWITCHES AND CYCLED LANDING GEAR THREE TIMES. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4T RT A24CE 2001082900268 20010829 00268 WP 2001 8 29 RRXA10977 1 20010414 A 5520 57638335700911 CAP DOUG DC8 DC873F 302199F WP LTELEVATOR DEBONDED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND DEBONDING DAMAGE TO REPAIR AT LT ELEVATOR O/B END T/E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21 AND 51- 1-21A AND 51-1-11 AND DC-8 MM 23-60-0. 2 L 7 4 4F RT 4A25 2001082900269 20010829 00269 WP 2001 8 29 RRXA10980 1 20010414 A 5340 37549301 FITTING DOUG DC8 DC873F 302199F WP DOOR FRAME CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO C-PIT DOOR FRAME LWR NR 3 LATCH, BACKUP FITTING, DAMAGE EXCEEDED LI MITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1- 20D, 53-1-0, AND DWG#3754930. 2 L 7 4 4F RT 4A25 2001082900270 20010829 00270 CE 2001 8 29 2001F00238 1 20010725 A 2621 CONNECTOR BEECH 1900 1900D 1154162 CE LT ENGINE LOOSE A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 19 81536 UE152 FLT 9122 - NAS/FLL - DURING FLIGHT, LEFT FIRE BOTTLE DISCHARGE LIGHT COMES ON INTERMITTENTLY. SECURED LOOSE CONNECTION AT LEFT ENGINE FIRE BOTTLE SQUIB. SYSTEM OPS CHECK NORMAL. (M) 2 L 7 2 4T RT A24CE 2001082900271 20010829 00271 EA 2001 8 29 COMA0160645 1 20010828 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA A COMA K NONE S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 943CA 7062 FLIGHT #5780. DURING PRE-FLIGHT INSPECTION DISCOVERED THE FLOOR EMERGENCY LIGHTING BETWEEN ROWS 9 AND 13 TO BE INOPERATI VE.RE-CONNECTED AFFECTED FLOOR EMERGENCY LIGHTING STRIP. 2 L 7 2 4F RT A21EA 2001082900272 20010829 00272 WP 2001 8 29 RRXA10982 1 20010415 A 5315 5779933 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SEAT TRACK AT STA 1580-1600 AND LBL45, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-8 AND DHSK 602-497. 2 L 7 4 4F RT 4A25 2001082900273 20010829 00273 WP 2001 8 29 RRXA10983 1 20010415 A 5315 5779933 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO MAIN CABIN FLOOR BEAM AT STA 1640 AND LBL48, DAMAGE EXCEEDED LIMITA TIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-0 FIG.1B AND DHSK 602-751. 2 L 7 4 4F RT 4A25 2001082900274 20010829 00274 WP 2001 8 29 RRXA10994 1 20010418 A 5320 5645322 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO SUPPORT ANGLE AT STA 860 AND LBL55, DAMAGE EXCEEDED LIMITATIONS IAW DC- 8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D, 5 3-1-0 AND DWG 5645332. 2 L 7 4 4F RT 4A25 2001082900275 20010829 00275 WP 2001 8 29 RRXA11001 1 20010419 A 5310 5755603 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND BLEND OUT DAMAGE TO FRAME AT STA 1280 AND L34L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SR M. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-0 FIG2, 51-1-20D. 2 L 7 4 4F RT 4A25 2001082900276 20010829 00276 NM 2001 8 29 2001F00240 1 20010702 A 5312 BULKHEAD BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 128NJ 22892 DURING C-CHECK INSPECTION PER SB 737-53A1173, PRESSURE BULKHEAD BS 178 WEB CRACKED AT WL 218, RBL 10.7. PRESSURE BULKHE AD BS 178 WEB REPAIRED FROM RBL 1.5 TO 18 BETWEEN WL 237 AND 230.5 SRM 53-10-11 FIG 1 DET II. REF P2EA01125. (M) 2 L 7 2 4F A16WE 2001082900277 20010829 00277 WP 2001 8 29 RRXA11008 1 20010419 A 5347 2772660 SEAT TRACK DOUG DC8 DC873F 302199F WP STA1400 LBL48 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO MAIN CABIN SEAT TRACK AT STA 1400 AND LBL48, DAMAGE EXCEEDED LIMITA TIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 53-2- 3 FIG8A. 2 L 7 4 4F RT 4A25 2001082900278 20010829 00278 WP 2001 8 29 RRXA11011 1 20010415 A 5720 9887427 WEB DOUG DC8 DC873F 302199F WP RT WING CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RH WING LOWER FALSE SPAR AFT OF MLG TRUNION AT STA XW75, DAMAGE EXC EEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D, DWG 9887427. 2 L 7 4 4F RT 4A25 2001082900279 20010829 00279 EA 2001 8 29 COMA0160646 1 20010827 A 3030 CONTROLLER CNDAIR CL600 CL6002B19 EA A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 957CA 7109 FLIGHT #5716. DURING TAXI OUT FOR TAKE OFF FROM RDU RECEIVED A LEFT PITOT STATIC HEAT CAUTION MESSAGE, AIRCRAFT RETURNED TO THE GATE.PERFORMED RESET OF THE LEFT AIR DATA SENSOR HEATER CONTROLLER CIRCUIT BREAKER. 2 L 7 2 4F RT A21EA 2001082900280 20010829 00280 NM 2001 8 29 2001F00241 1 20010702 A 5320 INTERCOSTAL BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 128NJ 22892 SJO - DURING C-CHECK INSPECTION PER S/B 737-53A1173, PRESSURE BULKHEAD BS 178 RIGHT INTERCOSTAL CRACKED WL 195. PRESSUR E BULKHEAD BS 178 INTERCOSTAL REWORKED AT RBL 24.67 WL 195 IAW SRM 53-10-1 FIG 10. (M) 2 L 7 2 4F A16WE 2001082900281 20010829 00281 NM 2001 8 29 2001F00242 1 20010702 A 5320 INTERCOSTAL BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 128NJ 22892 DURING C-CHECK INSPECTION PER S/B 737-53A1173, PRESSURE BULKHEAD BS 178 LEFT SIDE INTERCOSTAL CRACKED AT WL 195. PRESSU RE BULKHEAD BS 178 INTERCOSTAL REWORKED AT LBL 24.67 WL 195 IAW SRM 53-10-1 FIG 10. (M) 2 L 7 2 4F A16WE 2001082900282 20010829 00282 EA 2001 8 29 COMA0160647 1 20010827 A 3260 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 EA A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 999CA 7230 FLIGHT #5486. DURING TAXI-OUT FOR TAKE-OFF AT CAK RECEIVED A PROXIMITY SYSTEM FAULT CAUTION MESSAGE, AIRCRAFT RETURNED T O THE GATE.RESET TRIPPED #2 WEIGHT-ON-WHEEL CIRCUIT BREAKER. 2 L 7 2 4F RT A21EA 2001082900283 20010829 00283 EA 2001 8 29 COMA0160648 1 20010827 A 2710 COMPUTER CNDAIR CL600 CL6002B19 EA A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 729CA 7265 FLIGHT #5329. DURING TAKE OFF ROLL RECEIVED AN AILERON CONFIGURATION WARNING MESSAGE, ABORTED TAKE-OFF AND RETURNED TO T HE GATE.PERFORMED AN OPERATIONAL CHECK OF THE AILERON TRIM SYSTEM, DISCREPANCY COULD NOT BE DUPLICATED BY MAINTENANCE. 2 L 7 2 4F RT A21EA 2001082900284 20010829 00284 EA 2001 8 29 2001F00243 2 20010614 A 7314 DIAPHRAGM BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA FUEL PUMP RUPTURED A YADA O OTHER K FLUID LOSS NR NOT REPORTED 1 AL 03 1566C UC36 POST RAYTHEON AIRCRAFT SERVICE BULLETIN 71-3307, ENGINE DRIVEN LOW PRESSURE FUEL PUMP DRAIN MOD. EXPERIENCED A FAILURE OF THE LOW PSI ENGINE DRIVEN FUEL PUMP ON THE NR 1 ENGINE. THE RESULT OF THE DIAPHRAGM RUPTURE WAS TO HAVE FUEL VENTED OUT OF THE NACELLE THROUGH THE MANIFOLD DRAIN. THE FUEL, THAT WAS VENTED OUT, COVERED THE LEFT MAIN LANDING GEAR WHEELS AND BRAKES. SUBMITTER STATES THEY CONSIDER THIS A FIRE HAZARD, AS THE BRAKES WERE STILL SOAKED WITH FUEL WHEN THE AIRC RAFT ARRIVED ON THE RAMP FOR PUMP REPLACEMENT. (M) 2 L 7 2 4T 4 T RT A24CE E4EA 2001082900285 20010829 00285 EA 2001 8 29 COMA0160649 1 20010827 A 3230 SENSOR CNDAIR CL600 CL6002B19 EA A COMA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 918CA 7018 FLIGHT #5572. AFTER TAKE OFF FROM GRB RECEIVED A NOSE LANDING GEAR DISAGREE CAUTION MESSAGE, AIRCRAFT RETURNED TO THE FI ELD.ADJUSTED THE NOSE LANDING GEAR PS3GA PROXIMITY SENSOR, OPERATIONAL GEAR SWING WAS SATISFACTORY. 2 L 7 2 4F RT A21EA 2001082900286 20010829 00286 WP 2001 8 29 RRXA11012 1 20010423 A 5530 57025791 TAB DOUG DC8 DC873F 302199F WP LT ELEVATOR DEBONDED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND DEBONDED DAMAGE TO LH ELEVATOR IB CORNER OF GEARED TAB, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-9A, DC-8 MM 27-30-3. 2 L 7 4 4F RT 4A25 2001082900287 20010829 00287 EA 2001 8 29 COMA0160650 1 20010827 A 2751 865D1007 DRIVE GEAR CNDAIR CL600 CL6002B19 EA CENTER WING FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 784CA 4764 7319 FLIGHT #5494. DURING CHA APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT 45 DEGREE FLAP POSITON, AIRCRAFT LANDED SAFELY .REPLACED THE FLAP POWER DRIVE UNIT. 2 L 7 2 4F RT A21EA 2001082900288 20010829 00288 EA 2001 8 29 COMA0160651 1 20010827 A 2751 855D1009 BPSU CNDAIR CL600 CL6002B19 EA LEFT WING FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 784CA 4764 7319 FLIGHT #5494. DURING CHA APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT 45 DEGREE FLAP POSITION, AIRCRAFT LANDED SAFEL Y.REPLACED THE LEFT BRAKE AND POSITION SENSING UNIT. 2 L 7 2 4F RT A21EA 2001082900289 20010829 00289 EA 2001 8 29 COMA0160652 1 20010826 A 5350 4926201 RADOME CNDAIR CL600 CL6002B19 EA NOSE BURNED A COMA K NONE O OTHER CR CRUISE 1 SO 01 943CA 14864 7062 FLIGHT #5628. DURING CRUSIE FLIGHT AIRCRAFT ENCOUNTERED A LIGHTNING STRIKE, CREW REPORTED SMOKE/BURNING SMELL IN CABIN A ND GALLEY AREA. AIRCRAFT CONTINUED FLIGHT TO IAD AND LANDED SAFELY.REPLACED THE RADOME. 2 L 7 2 4F RT A21EA 2001082900290 20010829 00290 EA 2001 8 29 COMA0160653 1 20010826 A 2900 AE4096G0060000 HOSE CNDAIR CL600 CL6002B19 EA LT MLG EQUIP BAY LEAKING A COMA O OTHER S AFFECT SYSTEMS DE DESCENT 1 SO 01 936CA 16682 7043 FLIGHT #5878. HYRAULIC #3 LOW PRESSURE CAUTION MESSAGE RECEIVED DURING DESCENT INTO ORD. HYDRAULIC SYNOPTIC PAGE INDIC ATED ZERO PERCENT QUANTITY IN #3 SYSTEM, ACCOMPLISHED QRH PROCEDURE; EXTENDING LANDING GEAR MANUALLY. AIRCRAFT LANDED S AFELY AND WAS TOWED TO THE GATE.REPLACED LEAKING HYDRAULIC PUMP 3A PRESSURE HOSE ASSEMBLY. 2 L 7 2 4F RT A21EA 2001082900291 20010829 00291 EA 2001 8 29 COMA0160654 1 20010824 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN DIRTY A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 967CA 7134 FLIGHT 5557. CREW MEMBER DISCOVERED EMERGENCY EXIT LIGHTING AT ROW 8D INOPERATIVE. REMOVED, CLEANED AND RE-INSTALLED CO NNECTOR FOR AFFECTED LIGHTING. 2 L 7 2 4F RT A21EA 2001082900292 20010829 00292 EA 2001 8 29 COMA0160655 1 20010826 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN DAMAGED A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 978CA 7158 EMERGENCY EXIT LIGHT BY MAIN CABIN DOOR (BELOW "PULL"SIGN) IS INOPERATIVE. RE-WIRED EMERGENCY EXIT LIGHT. 2 L 7 2 4F RT A21EA 2001082900293 20010829 00293 SO 2001 8 29 COMA0110136 1 20010826 A 7710 SEDLOC29J INDICATOR EMB 120 EMB120RT SO COCKPIT FAULTY A COMA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 SO 01 264CA 19166 1256 FLIGHT #5053. DURING APPLICATION OF POWER FOR TAKE OFF AT MCO THE #2 NH ANALOG INDICATION FAILED, AIRCRAFT RETURNED TO THE GATE.REPLACED THE NH/NL INDICATOR. 2 L 7 2 4T RT A31SO 2001083000907 20010830 00907 WP 2001 8 30 RRXA11018 1 20010421 A 5730 5611017P PANEL DOUG DC8 DC873F 302199F WP LT WING DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LH WING LWR TE PANEL AT FLAP HINGE 98, DAMAGE EXCEEDED LIMITATIO NS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0, 51 -1-9A. 2 L 7 4 4F RT 4A25 2001083000908 20010830 00908 WP 2001 8 30 RRXA11019 1 20010411 A 5310 56410169 SHEAR TIE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO SHEAR TIE AT STA 1420 AND L34R AND L36R, DAMAGE EXCEEDED LIMITATIONS I AW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-3 -0. 2 L 7 4 4F RT 4A25 2001083000909 20010830 00909 WP 2001 8 30 RRXA11021 1 20010426 A 3213 51591015507 STRUT DOUG DC8 DC873F 302199F WP LT MLG BROKEN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND BROKEN DAMAGE TO LT MLG STRUT ASSY GEAR AT LT WW, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 MM 32-11-1. 2 L 7 4 4F RT 4A25 2001083000910 20010830 00910 WP 2001 8 30 RRXA11023 1 20010311 A 5310 5616306 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RT WW DOOR FRAME AT STA 883, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0 FIG2B, DWG 56163 06, DC-8 SRM 53-1-01, 51-1-21. 2 L 7 4 4F RT 4A25 2001083000911 20010830 00911 WP 2001 8 30 RRXA11027 1 20010430 A 2780 57695831N STRUCTURE DOUG DC8 DC873F 302199F WP LT MLG DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CRACKED DAMAGE TO DOOR AT LT OB SLOT UPPER CENTER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 MM 27-80-01. 2 L 7 4 4F RT 4A25 2001083000912 20010830 00912 WP 2001 8 30 RRXA11032 1 20010327 A 5730 5769600 SKIN DOUG DC8 DC873F 302199F WP LT WING DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND SCREWS PULLING THROUGH SKIN AT STA XFS 710 ON LT WING OB LE, DAMAGE EXCEEDED LIMITATION S IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-1 FI G2H. 2 L 7 4 4F RT 4A25 2001083000913 20010830 00913 WP 2001 8 30 RRXA11034 1 20010314 A 5310 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FINGER DOUBLER AT STA 180-200 AND L31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0 1F, 5 1-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 2001083000914 20010830 00914 WP 2001 8 30 RRXA11036 1 20010314 A 5330 DMU92 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO ANTENNA MOUNT PLATE AND SKIN AT STA 367-373, DAMAGE EXCEEDED LIMITA TIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-3-01. 2 L 7 4 4F RT 4A25 2001083000915 20010830 00915 WP 2001 8 30 RRXA11037 1 20010314 A 5330 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO ANTENNA PAD AT STA 87-93 AND L36, DAMAGE EXCEEDED LIMITATIONS IAW D C-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-11, 51-3-0. 2 L 7 4 4F RT 4A25 2001083000916 20010830 00916 WP 2001 8 30 RRXA11050 1 20010314 A 5310 37540231N LATCH DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO A-PIT DOOR FRAME LWR NR 1 LATCH AT STA Y=285, X=24R, Z=-30, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC- 8 SRM 51-1-20D, 2 L 7 4 4F RT 4A25 2001083000921 20010830 00921 WP 2001 8 30 MWEA011187 1 20010829 A 5310 992190415 INTERCOSTAL DOUG DC9 DC932 3022066 WP STATION 918 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 AFT CARGO BAY HAS A DENTED INTERCOSTAL BETWEEN FLOOR BEAMS 918-937 AT AIRCRAFT CENTERLINE. -- FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001083000922 20010830 00922 WP 2001 8 30 MWEA011188 1 20010829 A 5310 99577395 SHEAR TIE DOUG DC9 DC932 3022066 WP STATION 946 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 SHEAR TIE CRACKED BETWEEN LONGERONS 14 RIGHT AND 15 RIGHT AT STATION 946. -- FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F A6WE 2001083000923 20010830 00923 WP 2001 8 30 MWEA011190 1 20010829 A 5310 9915558145 FORMER DOUG DC9 DC932 3022066 WP STATION Z24 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 ON FORWARD SIDE OF AFT PRESSURE BULKHEAD, LEFT SIDE STATION 24 FORMER IS CRACKED ON OUTBOARD EDGE. -- FABRICATED AND I NSTALLED FORMER 2 L 7 2 4F A6WE 2001083000924 20010830 00924 WP 2001 8 30 MWEA011196 1 20010829 A 5330 2024T3080 DOUBLER DOUG DC9 DC932 3022066 WP STATION 898 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 LIGHTNING STRIKE DAMAGE AT UPPER AFT CORNER OF WINDOW #35 LEFT CUTOUT. -- FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001083000925 20010830 00925 WP 2001 8 30 MWEA011197 1 20010829 A 5330 591142863 DOUBLER DOUG DC9 DC932 3022066 WP STATION 1019 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FUSELAGE SKIN DENTED AT STATION 1019 BELOW RIGHT THRUST REVERSER BYPASS DOOR. -- FABRICATED AND INSTALLED FILLER AND D OUBLERS. 2 L 7 2 4F A6WE 2001083000926 20010830 00926 WP 2001 8 30 MWEA011201 1 20010829 A 5330 5911410502 DOUBLER DOUG DC9 DC932 3022066 WP STATION 587 MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 LONGERON 18 RIGHT CUSP TEE LOWER FLANGE HAS A MISDRILLED HOLE AT STTION 587 COMMON TO THE SKIN AND TEE. -- FABRICATED AND INSTALLED FINGER DOUBLER, FILLER, AND EXTERNAL DOUBLER. 2 L 7 2 4F A6WE 2001083000929 20010830 00929 WP 2001 8 30 RRXA11067 1 20010412 A 5712 5769600 RIB DOUG DC8 DC862F 3021972 WP LT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LT WING O/B L/E UPPER RIBS AT STA. XFS 635 TO 641.25 AND XFS 610, DAMAG E EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAOR AND INSTALLED IA W DC-8 SRM 57-2-0 FIG 2 2 L 7 4 4F 4A25 2001083000930 20010830 00930 WP 2001 8 30 RRXA11068 1 20010412 A 5712 5769600 RIB DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO RT WING O/B L/E LOWER RIB AT STA. XFS603.75. DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2. 2 L 7 4 4F 4A25 2001083000931 20010830 00931 WP 2001 8 30 RRXA11069 1 20010412 A 5712 5769545 RIB DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CRACK TO LT WING O/B L/E UPPER RIBS AT STA. XFS 803.75 TO 791.25 AND XFS 766.25. DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.. FABRICATED REPAIR AND INSTALLED IA W DC-8 SRM 57-2-0 FIG 2. 2 L 7 4 4F 4A25 2001083000932 20010830 00932 WP 2001 8 30 RRXA11071 1 20010412 A 5712 5769545 RIB DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO RT WING O/B L/E LOWER RIB AT STA. XFS 791.25, 785, 772.5, DAMAGE EXCEED ED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 S RM 57-2-0 FIG 2 AND DRAWING 5769941. 2 L 7 4 4F 4A25 2001083000933 20010830 00933 WP 2001 8 30 RRXA11074 1 20010413 A 5320 5759335 SHIM DOUG DC8 DC862F 3021972 WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT REQUIRED TO REPLACE CLASS 3 REPAIR TO LT SIDE AFT OF FILLET FAIRING AT STA. 1200-1220, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED CLASS 3 REPAIR AND INSTALLE D CLASS 1 REPAIR IAW DC-8 SRM 53-2-1 FIG 7 AND 51-1-21. 2 L 7 4 4F 4A25 2001083000934 20010830 00934 WP 2001 8 30 RRXA11075 1 20010414 A 5320 5644140 STIFFENER DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO AFT SIDE OF APB HORIZ STIFFNER INSIDE HOLE 60 AT STA 1606 AND BL=0 AND 24 ABOVE FLOOR LEVEL, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICA TED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-0 FIG 1B. 2 L 7 4 4F 4A25 2001083000935 20010830 00935 WP 2001 8 30 RRXA11076 1 20010415 A 5340 4641324N FITTING DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LONG END FITTING AT STA. 1530-1540 AND L32R, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0 AND D WG 4641324. 2 L 7 4 4F 4A25 2001083000936 20010830 00936 WP 2001 8 30 RRXA11077 1 20010418 A 5340 4641326N FITTING DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO END FITTING AT STA 1520-1530 AND L32L, DAMAGE EXCEEDED LIMITATION IAW D C-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND DWG 4 641326. 2 L 7 4 4F 4A25 2001083000937 20010830 00937 WP 2001 8 30 RRXA11082 1 20010419 A 5330 5759332 SKIN DOUG DC8 DC862F 3021972 WP FUSELAGE SCRATCHED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND SCRATCH DAMAGE TO EXTERIOR FUSELAGE SKIN AT STA. 410 AND L11R. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. BURNISHED SCRATCH IAW DC-8 SRM 53-2-0 FIG1F, NDT INSPECTED AND FOUND TO BE WITHIN LIMITS IAW DC-8 SRM 53-1-0. 2 L 7 4 4F 4A25 2001083000938 20010830 00938 WP 2001 8 30 RRXA11084 1 20010420 A 5340 4641324525N FITTING DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO AFT LONGERON END FITTING AT STA. 1530 AND L28L, DAMAGE EXCEEDED LIMITAT ION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51 -1-20D. 2 L 7 4 4F 4A25 2001083000939 20010830 00939 WP 2001 8 30 RRXA11087 1 20010420 A 5315 5759332 FLOORBEAM DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR BEAM AT STA. 1540 AND LBL26, DAMAGE EXCEEDED LIMITATION IAW D C-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DHMSK996-554. 2 L 7 4 4F 4A25 2001083000940 20010830 00940 WP 2001 8 30 RRXA11088 1 20010421 A 5340 4641324N FITTING DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LONGERON END FITTING AT STA 1530-1540 AND L30R, DAMAGE EXCEEDED LIMITAT ION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D, DWG#4641324N. 2 L 7 4 4F 4A25 2001083000941 20010830 00941 WP 2001 8 30 RRXA11089 1 20010421 A 5320 5772785 WEB DOUG DC8 DC862F 3021972 WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND 8EA OPEN HOLES AND DRILL BIT DAMAGE TO INTERNAL FRAME AT STA340 AND L11L, DAMAGE EXCEED ED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 52-2-0 FIG#2 AND 51-1-21. 2 L 7 4 4F 4A25 2001083000942 20010830 00942 2001 8 30 RAIA00108024 4 20010823 A 3418 C850175 VANE JETAIR JETSTM JETSTM4101 1500501 EU RT FUSELAGE FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 551HK 16152 41040 7092-STL-RIGHT STALL CAPTION ILLUMINATED DURING TAXI. MAINTENANCE INSPECTED AND REPLACED THE RIGHT AOA VANE. 2 L 7 2 4T RT A41NM 2001083000943 20010830 00943 EU 2001 8 30 RAIA00108025 1 20010826 A 2613 51653151 DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 559HK 13381 41075 5402-EWR-RIGHT OVERHEAT CAPTION ILLUMINATED DURING TAXI. MAINTENANCE INSPECTED AND REPLACED RIGHT OVERHEAT DETECTION CON TROL UNIT. 2 L 7 2 4T RT A41NM 2001083000944 20010830 00944 EU 2001 8 30 RAIA00108026 1 20010827 A 2432 407817 BATTERY JETAIR JETSTM JETSTM4101 1500501 EU ELECTRICS BAY FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 558HK 10174 115 41071 5373-BWI-RIGHT BATTERY CAPTION ILLUMINATED DURING TAXI. MAINTENANCE INSPECTED AND REPLACED THE NUMBER 2 MAIN BATTERY. 2 L 7 2 4T RT A41NM 2001083000945 20010830 00945 WP 2001 8 30 RRXA11090 1 20010421 A 5310 5772787 DOUBLER DOUG DC8 DC862F 3021972 WP DOOR FRAME DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND DAMAGE TO MAIN CARGO DOOR CUT OUT AFT FRAME SEAL AT 18 INCHES FROM UPPER END, DAMAGE EX CEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 53-2-0 FIG 2. 2 L 7 4 4F 4A25 2001083100161 20010831 00161 NM 2001 8 31 01FDEA00778 1 20010829 A 2133 OUTFLOW VALVE BOEING 727 727233 138408A NM CABIN PRESSURE FAILED A FDEA O OTHER O OTHER CL CLIMB 1 SO 25 282FE 22349 DURING CLIMB CABIN PRESS FAILED TO STOP AT 8.6 PSI (YELLOW BAND). SYS DID NOT SWITCH TO STBY. REMOVED AND REPLACED OUTF LOW VALVE & PRESSURE SELECTOR PNL. OK PER MM 21-31-000-5. 2 L 7 3 4F RT A3WE 2001083000947 20010830 00947 WP 2001 8 30 01FDEA00780 1 20010828 A 3260 WARNING LIGHT DOUG DC10 DC1010 3022110 WP COCKPIT ILLUMINATED A FDEA K NONE J WARNING INDICATION CL CLIMB 1 SO 25 389FE 46623 RT MLG RED TRANSITION LIGHT STAYED ON AFT RAISING GEAR, CYCLED LG PER RED TAB & LIGHT EXTINGUISHED, REPEAT. 2 L 7 3 4F A22WE 2001083000948 20010830 00948 NM 2001 8 30 01FDEA00781 1 20010828 A 5330 SKIN BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 280FE 22347 A .5 INCH CRACK AND CORROSION ON SKIN AT BS 680-720 AT STR 28R. 2 L 7 3 4F RT A3WE 2001083000949 20010830 00949 NM 2001 8 30 01FDEA00783 1 20010827 A 2497 WIRE DOUG MD11 MD11F 3023600 NM RT WING DAMAGED A FDEA K NONE G MULTIPLE FAILURE CL CLIMB 1 SO 25 601FE 48401 WIRE BUNDLES IN RT WING ROOT LEADING EDGE BURNT. 2 L 7 3 4F RT A22WE 2001091400114 20010914 00114 NM 2001 9 14 2001UALA01753 1 20010817 A 5220 411T2025 SEAL BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE EMERGENCY EXIT OUT OF POSITION A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 617UA 21877 EMERGENCY EXIT, AIR LEAK NOISE. FOUND DOOR SEAL FOLDED ON LOWER AFT CORNER OF EMERGENCY DOOR. LUBED SEAL AND INSTALLED DOOR PROPERLY. EMAC 60 5220 000ZE, PERFORMS A GENERAL VISUAL OF THE O/W EMERGENCY EXIT ON A 1C FREQUENCY. 2 L 7 2 4F 4 F RT A1NM E3NE 2001083000951 20010830 00951 WP 2001 8 30 CNMA200100032 1 20010828 A 3350 CONNECTOR DOUG DC10 DC1030 3023501 WP CABIN LOOSE A CNMA K NONE O OTHER CR CRUISE 1 SW 07 540AX 46595 EMERGENCY AISLE LIGHTS ILLUMINATED FROM ROW 35 AFT. RESET BATTERY CONNECTORS, OPS CHECKED OK. 2 L 7 3 4F A22WE 2001083000952 20010830 00952 EU 2001 8 30 DHL2001366025 1 20010829 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU CABIN MALFUNCTIONED A DHLA B A EMER. DESCENT UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 366DH 249 UPON ROTATION SMOKE LIGHT ON MWP ILLUMINATED. ON SECOND OFFICER'S PANEL R2 LIGHT FOLLOWED BY R4, R5, L3, & L5. THEN D URING DOWNWIND, ALL LIGHTS WENT OUT. NO SMOKE FOUND IN CABIN. RAN PACKS AND COOLED CABIN OFF. CABIN SMOKE DETECTION S YSTEM OPS CHECKS NORMAL IAW M/M 26-14-00. NO DEFECTS NOTED. 2 L 7 2 4F RT A35EU 2001083000953 20010830 00953 WP 2001 8 30 DHL2001803011 1 20010829 A 2611 SMOKE DETECTOR DOUG DC8 DC873 302199C WP CABIN INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 803DH 46123 DURING PREFLIGHT NR 3 SMOKE DETECTOR WOULD NOT TEST. 2 L 7 4 4F RT 4A25 2001083000954 20010830 00954 WP 2001 8 30 DHL2001804552 1 20010826 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 RT WING SKIN CRACKED 1.5 INCH AT XFS 597.500. STOP DRILLED CRACK PER SRM 57-2-0 PG 2. FABRICATED DOUBLER AND INSTALLED D OUBLER PER EO DHL010812 EO 2594 AND EO 2001259, SRM 51-1-20D, PG 9-51 1-2. 2 L 7 4 4F RT 4A25 2001083000955 20010830 00955 WP 2001 8 30 DHL2001804553 1 20010827 A 5753 SKIN DOUG DC8 DC873F 302199F WP T/E FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 LEFT OUTBOARD T/E FLAP .5 INCH CRACK ON UPPER SKIN, STA XFS 415-453. REMOVED DAMAGED SKIN AND INSTALLED NEW SKIN PER DH L EO 010804, EO 2566, EO 2001302, SRM 51-1-21 PG 1, SRM 51-1-15 PG 1. 2 L 7 4 4F RT 4A25 2001083000956 20010830 00956 WP 2001 8 30 DHL2001804554 1 20010826 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 LT WING STUB WING UPPER SKIN SURFACE SHOWS A .75 INCH CRACK AT XFS 207.5. STOP DRILLED CRACK. INSTALLED DOUBLER PER DHL EO 010820, EO2601, EO 2001293, SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2001083000957 20010830 00957 NM 2001 8 30 ERKR200100155 1 20010829 A 5311 FRAME BOEING 747 747212B 1384886 NM FUSELAGE DAMAGED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 485EV 20712 REPAIR OF FRAME OUTER WEB FS 670, S31R TO 36R. 2 L 7 4 4F A20WE 2001083000958 20010830 00958 WP 2001 8 30 ERKR200100156 1 20010829 A 5230 PAN DOUG DC9 DC915F 3022037 WP CARGO DOOR DAMAGED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 915F 47061 MAIN DECK CARGO DOOR, INNER PAN SKIN, ELONGATED HOLES. 2 L 7 2 4F A6WE 2001083000959 20010830 00959 WP 2001 8 30 ERKR200100159 1 20010829 A 5210 DOUBLER DOUG DC9 DC915F 3022037 WP ENTRY DOOR CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 915F 47061 CRACKED INTERNAL DOUBLER IN FWD LT ENTRANCE DOOR. 2 L 7 2 4F A6WE 2001083000960 20010830 00960 WP 2001 8 30 ERKR200100160 1 20010829 A 5315 FLOORBEAM DOUG DC9 DC915F 3022037 WP FUSELAGE DAMAGED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 915F 47061 REPAIR OF FLOORBEAM, FS 786, RBL 12 TO RBL 28. REMOVED AND REPLACED THE DAMAGED SECTION OF ANGLE BETWEEN RBL 12 AND RBL 28. 2 L 7 2 4F A6WE 2001083000961 20010830 00961 WP 2001 8 30 ERKR200100161 1 20010829 A 5320 CHANNEL DOUG DC9 DC915F 3022037 WP FUSELAGE DAMAGED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 915F 47061 REPAIR OF CARGO ROLLER TRAY CHANNEL, FS 313 - 332, RBL 12. REMOVED AND REPLACED THE DAMAGED PORTION OF CHANNEL. 2 L 7 2 4F A6WE 2001083000962 20010830 00962 WP 2001 8 30 ERKR200100162 1 20010829 A 5742 FITTING DOUG DC9 DC915F 3022037 WP LT WING DAMAGED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 915F 47061 LT TRAPEZOIDAL FITTING ELONGATED HOLE. 2 L 7 2 4F A6WE 2001083000963 20010830 00963 WP 2001 8 30 ERKR200100163 1 20010829 A 5730 SKIN DOUG DC9 DC915F 3022037 WP LT WING DAMAGED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 915F 47061 DAMAGED MOUNTING HOLE ON LT WING LEADING EDGE AT XFS STA 168.75. 2 L 7 2 4F A6WE 2001083000964 20010830 00964 WP 2001 8 30 ERKR200100164 1 20010829 A 5313 LONGERON DOUG DC9 DC915F 3022037 WP FUSELAGE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 915F 47061 AT STATION 275 TO STATION 447 L-17 RT, LONGERON CRACKED AT FRAME ATTACH POINTS. REMOVED AND REPLACED LONGERON 17 RT PER SRM 51-30-2 AND EO 53-DC9-944-99 REV A. 2 L 7 2 4F A6WE 2001083000965 20010830 00965 NM 2001 8 30 F3LA200100102 1 20010824 A 5310 INTERCOSTAL BOEING 737 737301 1384611 NM CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3491 23257 DURING C-3 CHECK, INSPECTION REPORTED CRACK IN INTERCOSTAL AT BS 178, WL 195, LBL 24. MAINTENANCE REPAIRED INTERCOSTAL PER SRM 737-300 MM 53-10-08. 2 L 7 2 4F RT A16WE 2001083000966 20010830 00966 NE 2001 8 30 FE5F200100012 2 20010828 A 7250 1B8501 TURBINE BOEING 757 757* NM PWA 2037 PW2037 NE LT ENGINE DAMAGED Z FE5F C E ABORTED TAKEOFF ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 03 CTEXT 27204 727136 B757 A/C REG NR B-27007 ON TAKEOFF ROLL, JUST AS PILOT ADVANCED THROTTLES, A BANG WAS HEARD FROM LT ENG AND THEN EGT ROS E, RPM DROPPED. PILOT ABORTED TAKEOFF AND IAW QRH SHUT DOWN THE ENG. INITIAL INSPECTION REVEALED N1 IS SEIZED BUT N2 C AN BE ROTATED. BORESCOPE INSPECTION REVEALED FROM 1ST STAGE THRU 3RD STAGE TURBINE ARE ALL DAMAGED AND ONE OF 1ST STAGE TURBINE BLADE UNDER-PLATFORM FRACTURED. THIS ENG WILL BE SHIP TO P&W FOR REPAIR AND FURTHER INVESTIGATION. 2 L 7 2 4F 4 F RT A2NM E17NE 2001083000967 20010830 00967 NE 2001 8 30 GLBA2001116 2 20010601 A 7321 311875702 FCU BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ENGINE MALFUNCTIONED A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 118UX 2067 UE118 LEFT ENGINE TORQUE AND FUEL FLUX. REPLACED FUEL CONTROL, OPS CHECKED SATISFACTORY. 2 L 7 2 4T 4 T RT A24CE E26NE 2001083000968 20010830 00968 NM 2001 8 30 F3LA200100103 1 20010824 A 5310 INTERCOSTAL BOEING 737 737301 1384611 NM CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3491 52042 DURING C-3 CHECK, INSPECTION REPORTED CRACK IN INTERCOSTAL AT BS 178, WL 195, RBL 24. MAINTENANCE REPAIRED INTERCOSTAL PER SRM 737-300 MM 53-10-08. 2 L 7 2 4F RT A16WE 2001083000969 20010830 00969 2001 8 30 GLBA2001117 4 20010601 A 2297 WIRE BEECH 1900 1900D 1154162 CE YAW DAMPER CHAFED A GLBA O OTHER F FLT CONT AFFECTED CL CLIMB 1 CE 01 154GL UE154 UNCOMMANDED YAW DAMP. REPAIRED CHAFED WIRE. 2 L 7 2 4T RT A24CE 2001083000970 20010830 00970 NE 2001 8 30 GLBA2001118 3 20010605 A 6140 1143800663 INDICATOR BEECH 1900 1900D 1154162 CE HARTZL HCE4A HCE4A3A NE COCKPIT FLUCTUATES A GLBA O OTHER N FALSE WARNING CR CRUISE 1 CE 01 204GL 68 UE204 PROP RPM FLUX. REPLACED LEFT INDICATOR. 2 L 7 2 4T RT A24CE 5 C P10NE 2001083000971 20010830 00971 2001 8 30 GLBA2001119 4 20010606 A 3425 COMPUTER EMB 120 EMB120ER 3260203 SO COCKPIT FAILED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 297UX 120297 NR 1 DPU FAILED. INITIALIZED AHARS COMPUTER, OPS CHECKED GOOD. 2 L 7 2 4T RT A31SO 2001083000972 20010830 00972 CE 2001 8 30 GLBA2001120 1 20010607 A 7333 12281301 TRANSMITTER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NR 2 ENGINE INOPERATIVE A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 01 118UX 168 UE118 NR 1 FUEL FLOW INDICATOR FAILED ON T/O ROLL. REPLACED FUEL FLOW TRANSMITTER. 2 L 7 2 4T 4 T RT A24CE E26NE 2001083000973 20010830 00973 NM 2001 8 30 AWXA0002193 1 20010731 A 5330 6545776 SKIN BOEING 737 73733A 1384673 NM BS 947 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 D: fastener head, pulling BS 947 STR 27LTC: Removed fastener, corrosion found. Removed corrosion, found to be out of lim its installed repair doubler IAW ER 03-5361-01232-BA1 2 L 7 2 4F RT A16WE 2001083000974 20010830 00974 NM 2001 8 30 AWXA0002194 1 20010814 A 5313 654541041 WEB BOEING 737 73733A 1384673 NM BS178 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 D: Ultrasonic crack indication RBL 4.8 WL 214 BS 178 Bulkhead web fwd side beneath strap.C: Repaired Bulkhead web IAW B7 37 SRM 53-11-8 pgs 286-298 2 L 7 2 4F RT A16WE 2001083000975 20010830 00975 NM 2001 8 30 AWXA0002195 1 20010801 A 5313 65163007 WEB BOEING 737 73733A 1384673 NM BS 178 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 D: Crack LBL 4.8 WL 214 BS 178 Blkhd web fwd side beneath strapC: cut-out damage & installed doubler IAW B757-300 SRM 53 -10-08 pgs 286-291 2 L 7 2 4F RT A16WE 2001083000976 20010830 00976 NM 2001 8 30 AWXA0002196 1 20010801 A 5313 65163007 WEB BOEING 737 73733A 1384673 NM BS 178 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 D: Crack RBL 1.5 WL 205 BS 178 Blkhd web fwd side beneath angleC: Cut out damaged area and installed doubler IAW B737-30 0 SRM 53-10-08 pgs 286-291 2 L 7 2 4F RT A16WE 2001083000977 20010830 00977 NM 2001 8 30 AWXA0002198 1 20010828 A 5311 6516308 FRAME BOEING 737 737277 1384570 NM BS243RT CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 D: Frame BS 243 RT WL 190 crackedC: Repaired per 737-200 SRM 51-40-4 fig 1 2 L 7 2 4F RT A16WE 2001083000978 20010830 00978 NM 2001 8 30 AWXA0002199 1 20010826 A 5311 6516309 FRAME BOEING 737 737277 1384570 NM BS 251RT CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 D: Frame BS 251 RT WL 180 crackedC: Repaired per SRM 51-40-4 fig 1 page 1-7 2 L 7 2 4F RT A16WE 2001083000979 20010830 00979 NM 2001 8 30 AWXA0002201 1 20010827 A 5310 6550531523 DOUBLER BOEING 737 737277 1384570 NM BS 227.8 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 D: Internal doubler cracked P/N 65-50531-523 STA 227.8 C: Internal doubler repaired IAW SRM 51-10-2 and DWG 65-50531 (RH side)Repaired damaged doubler, fabbed new doubler from 2024-T3 040. Treated and installed REF SRM 51-10-2 2 L 7 2 4F RT A16WE 2001083000980 20010830 00980 CE 2001 8 30 GLBA2001121 1 20010608 A 3233 11438004115 ACTUATOR BEECH 1900 1900D 1154162 CE RT MLG FAILED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 118UX 8208 1638 UE118 MAIN GEAR WOULD NOT RETRACT. REPLACED RIGHT ACTUATOR. 2 L 7 2 4T RT A24CE 2001083000981 20010830 00981 2001 8 30 GLBA2001122 4 20010609 A 2297 WIRE BEECH 1900 1900D 1154162 CE YAW DAMPER CHAFED A GLBA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CE 01 154GL UE154 AFTER T/O YAW DAMP/RUDDER BOOST ENGAGED. REPAIRED CHAFED WIRE AT YAW DAMP SWITCH RACK. 2 L 7 2 4T RT A24CE 2001083000982 20010830 00982 CE 2001 8 30 GLBA2001123 1 20010610 A 3260 1123640211 CIRCUIT BOARD BEECH 1900 1900D 1154162 CE COCKPIT FAULTY A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 01 195GL UE195 GEAR WARNING HORN WHEN GEAR IS RETRACTED. REPLACED RELAY BOARD. 2 L 7 2 4T RT A24CE 2001083000983 20010830 00983 CE 2001 8 30 GLBA2001124 1 20010611 A 7714 503890571 TACH GENERATOR BEECH 1900 1900D 1154162 CE LT ENGINE FAILED A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 01 211UX 517 UE211 LEFT N1 INDICATOR FAILED. REPLACED TACH GENERATOR, OPS CHECKED GOOD. 2 L 7 2 4T RT A24CE 2001083000984 20010830 00984 CE 2001 8 30 GLBA2001127 1 20010614 A 7931 CONNECTOR BEECH 1900 1900D 1154162 CE OIL PRESS SWITCH LOOSE A GLBA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 01 100UX UE100 NR 2 ENGINE OIL FLUX IN FLIGHT. RESECURED OIL PRESSURE SWITCH CANNON PLUG; ADDED 2 QTS OIL TO NR 2 ENGINE. OP'S CHECKE D GOOD. 2 L 7 2 4T RT A24CE 2001083000985 20010830 00985 CE 2001 8 30 GLBA2001128 1 20010615 A 3260 387 LIGHT BEECH 1900 1900D 1154162 CE COCKPIT INOPERATIVE A GLBA O OTHER P NO WARNING INDICATION AP APPROACH 1 CE 01 204GL UE204 RIGHT MAIN LANDING GEAR ANNUNCIATOR INOPERATIVE. REPLACED LIGHT BULB. 2 L 7 2 4T RT A24CE 2001083000986 20010830 00986 SO 2001 8 30 GLBA2001129 1 20010616 A 3350 GE327 LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A GLBA K NONE L NO TEST UK UNKNOWN 1 CE 01 299UX 120299 RED EMERGENCY FLOOR PATH LIGHT INOPERATIVE. REPLACED LIGHT BULB. 2 L 7 2 4T RT A31SO 2001083000987 20010830 00987 NE 2001 8 30 GLBA2001130 3 20010617 A 6110 PROPELLER BEECH 1900 1900D 1154162 CE HARTZL HCE4A HCE4A3A NE LT & RT NOISY A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 169GL UE169 PROPELLERS NOISY. INSPECTED AND CLEANED LOW PITCH SOLENOIDS, OPS CHECK SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 5 C P10NE 2001083000988 20010830 00988 NE 2001 8 30 GLBA2001134 2 20010626 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RIGHT OVERTEMP A GLBA C ABORTED TAKEOFF M OVER TEMP TO TAKEOFF 1 CE 01 219GL UE219 ABORTED T/O RIGHT ENGINE TEMP LIMITED. PERFORMED REDUCED POWER T/O. 2 L 7 2 4T 4 T RT A24CE E26NE 2001083000989 20010830 00989 CE 2001 8 30 GLBA2001136 1 20010628 A 5270 M88051008 SWITCH BEECH 1900 1900D 1154162 CE CARGO DOOR FAILED A GLBA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 01 94UX UE94 CARGO DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. REPLACED MICRO SWITCH ON CARGO DOOR, OPS CHECKED SATISFACTORY. 2 L 7 2 4T RT A24CE 2001083000990 20010830 00990 CE 2001 8 30 GLBA2001137 1 20010628 A 2570 FASTENER BEECH 1900 1900D 1154162 CE ACCESS BAY FAILED A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 211UX UE211 NOISE FROM NOSE COMPARTMENT ON GEAR RETRACTION, AVIONICS LOUVER NOT SECURED DUE TO HARDWARE FAILURE. REPLACED LOUVER, O PS CHECKED SATISFACTORY. 2 L 7 2 4T RT A24CE 2001083000991 20010830 00991 SO 2001 8 30 GLBA2001138 1 20010628 A 2133 OUTFLOW VALVE EMB 120 EMB120RT SO CABIN PRESSURE OBSTRUCTED A GLBA G O2 MASK DEPLOYED O OTHER CR CRUISE 1 CE 01 85GL 120085 CABIN ALTITUDE CLIMBED WHILE AT ALTITUDE (26000) DEPLOYED MASKS. FOUND DEBRIS STUCK IN THE OUTFLOW VALVE. CLEAN VALVE, OPS CHECKED SATISFACTORY. 2 L 7 2 4T RT A31SO 2001083000993 20010830 00993 CE 2001 8 30 GLBA2001140 1 20010701 A 2130 FILTER BEECH 1900 1900D 1154162 CE CABIN PRESSURE DIRTY A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 01 192GL UE192 CABIN WILL NOT HOLD PRESSURIZATION. CLEANED PNEUMATIC RELAY AND FILTER, OPS CHECKED SATISFACTORY. 2 L 7 2 4T RT A24CE 2001083000994 20010830 00994 CE 2001 8 30 GLBA2001141 1 20010703 A 7720 3034857 PROBE BEECH 1900 1900D 1154162 CE LT ENGINE FAILED A GLBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 01 195GL UE195 LEFT ENGINE OVERTEMP ON T/O. REPLACED TRIM PROBE. 2 L 7 2 4T RT A24CE 2001083000995 20010830 00995 SO 2001 8 30 GLBA2001142 1 20010703 A 5610 SEAL EMB 120 EMB120ER 3260203 SO COCKPIT DIRTY A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 297UX 120297 COCKPIT WINDOW NOT SEALED ON T/O. INSPECTED AND CLEANED SEAL, OPS CHECKED SATISFACTORY. 2 L 7 2 4T RT A31SO 2001083000996 20010830 00996 CE 2001 8 30 GLBA2001143 1 20010704 A 5270 SWITCH BEECH 1900 1900D 1154162 CE CARGO DOOR OUT OF ADJ A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 01 94UX UE94 CARGO DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. ADJUSTED CARGO DOOR SWITCH , OPS CHECKED SATISFACTORY. 2 L 7 2 4T RT A24CE 2001083000997 20010830 00997 SO 2001 8 30 GLBA2001144 1 20010704 A 2130 CONNECTOR EMB 120 EMB120RT SO CABIN PRESSURE LOOSE A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 85GL 120085 WOULD NOT PRESSURIZE. INSPECTED FOUND LOOSE CONNECTION ON MANUAL CONTROL. SECURED CONNECTOR, OPS CHECKED SATISFACTORY. 2 L 7 2 4T RT A31SO 2001083000998 20010830 00998 SO 2001 8 30 GLBA2001145 1 20010705 A 2131 22201T011400 CONTROLLER EMB 120 EMB120RT SO CABIN PRESSURE FAILED A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 85GL 9246 650 120085 PRESSURIZATION WOULD NOT REACH MAX DIFFERENTIAL. REPLACED ELECTRONIC CONTROLLER AND OUTFLOW VALVE, OPS CHECKED SYSTEM S ATISFACTORY. 2 L 7 2 4T RT A31SO 2001083000999 20010830 00999 NE 2001 8 30 GLBA2001147 2 20010706 A 7510 11438903921 ACTUATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ENGINE INOPERATIVE A GLBA C ABORTED TAKEOFF M OVER TEMP TO TAKEOFF 1 CE 01 94UX 114 UE94 RIGHT ENGINE WILL NOT MAKE T/O TORQUE, TEMP LIMITED. REPLACED ICE VANE ACTUATOR, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T 4 T RT A24CE E26NE 2001083001000 20010830 01000 SO 2001 8 30 GLBA2001148 1 20010707 A 3297 WIRE EMB 120 EMB120ER 3260203 SO LT MLG BROKEN A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 71GL 120071 LANDING GEAR WOULD NOT RETRACT ON T/O. INSPECTED FOUND BROKEN WIRE ON LEFT SQUAT SWITCH. REPAIRED, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A31SO 2001083001001 20010830 01001 CE 2001 8 30 GLBA2001149 1 20010707 A 2750 1015210577 CAM BEECH 1900 1900C 1154161 CE T/E FLAP WORN A GLBA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CE 01 122GL UC122 FLAPS WOULD NOT RETRACT ON T/O. REPLACED SAFETY SWITCH CAM. 2 L 7 2 4T RT A24CE 2001083001002 20010830 01002 CE 2001 8 30 GLBA2001151 1 20010710 A 2130 CONTROLLER BEECH 1900 1900D 1154162 CE CABIN PRESSURE MALFUNCTIONED A GLBA O OTHER O OTHER CL CLIMB 1 CE 01 254GL UE254 AIRCRAFT WOULD NOT PRESSURIZE. COULD NOT DUPLICATE, OPS CHECKED SATISFACTORY. 2 L 7 2 4T RT A24CE 2001083001003 20010830 01003 CE 2001 8 30 GLBA2001155 1 20010712 A 2497 WIRE BEECH 1900 1900D 1154162 CE ELECTRICAL SYS BROKEN A GLBA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 CE 01 253GL UE253 EADI FLICKERED, LEFT AC BUSS FAILED AND RIGHT INVERTER OUT PUT ERRATIC. INSPECTED, FOUND 3 BROKEN WIRES ON THE K107 REL AY. OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001083001004 20010830 01004 NE 2001 8 30 GLBA2001159 2 20010716 A 7532 BLEED VALVE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ENGINE DIRTY A GLBA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CE 01 251GL UE251 RIGHT ENGINE COMPRESSOR STALLING ON T/O. INSPECTED AND CLEANED BLEED VALVE, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T 4 T RT A24CE E26NE 2001083001006 20010830 01006 CE 2001 8 30 GLBA2001165 1 20010720 A 2612 FIRE LOOP BEECH 1900 1900D 1154162 CE LT ENGINE OUT OF POSITION A GLBA K NONE N FALSE WARNING AP APPROACH 1 CE 01 249GL UE249 LEFT FIRE LOOP WARNING LIGHT ILLUMINATED. FOUND FIRE LOOP SHORTING TO THE O/B EXHAUST STACK REPOSITIONED, OPS CHECKED S ATISFACTORY. 2 L 7 2 4T RT A24CE 2001083001007 20010830 01007 CE 2001 8 30 GLBA2001166 1 20010720 A 3260 327 LIGHT BEECH 1900 1900D 1154162 CE GEAR HANDLE INOPERATIVE A GLBA O OTHER N FALSE WARNING AP APPROACH 1 CE 01 211UX UE211 RIGHT MAIN GEAR HANDLE LIGHTS WOULD NOT ILLUMINATE. REPLACED LAMP. 2 L 7 2 4T RT A24CE 2001083001008 20010830 01008 CE 2001 8 30 GLBA2001167 1 20010722 A 7714 503890571 TACH GENERATOR BEECH 1900 1900D 1154162 CE LT ENGINE FAILED A GLBA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 01 97UX 548 UE97 LEFT PROP RPM WENT TO ZERO. REPLACED N2 TACH GENERATOR, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001083001009 20010830 01009 CE 2001 8 30 GLBA2001168 1 20010722 A 7722 305399CL08 PROBE BEECH 1900 1900D 1154162 CE LT ENGINE DEFECTIVE A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 01 122UX UE122 LEFT ENGINE WILL NOT MAKE TAKEOFF TORQUE. REPLACED TRIM PROBE, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001083001010 20010830 01010 CE 2001 8 30 GLBA2001171 1 20010725 A 2720 RUDDER PEDAL BEECH 1900 1900D 1154162 CE COCKPIT OUT OF ADJ A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 01 245GL UE245 RUDDER CONTROL STIFF. INSPECTED, ADJUSTED PEDALS, OPS CHECK SATISFACTORY. 2 L 7 2 4T RT A24CE 2001083001011 20010830 01011 CE 2001 8 30 GLBA2001174 1 20010806 A 7722 1303800415 INDICATOR BEECH 1900 1900D 1154162 CE COCKPIT FAILED A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 01 154GL 5079 UE154 LEFT ITT INDICATOR FAILED ON T/O. REPLACED INDICATOR. 2 L 7 2 4T RT A24CE 2001091800109 20010918 00109 2001 9 18 GLBA2001176 4 20010807 A 2210 6225734002 SERVO BEECH 1900 1900D 1154162 CE YAW DAMPER MALFUNCTIONED A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 01 255GL 10688 4316 UE255 UNCOMMANDED YAW DAMP ON T/O. REPLACED YAW DAMP SERVO, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001083001012 20010830 01012 NE 2001 8 30 GLBA2001177 2 20010808 A 7532 BLEED VALVE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ENGINE DIRTY A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 01 260GL UE260 RIGHT ENGINE SURGE ON POWER UP FOR T/O. CLEANED BLEED VALVE, OPS CHECKED SATISFACTORY. 2 L 7 2 4T 4 T RT A24CE E26NE 2001083001013 20010830 01013 NM 2001 8 30 MWEA011142 1 20010830 A 5710 9919379505 FRAME DOUG MD88 MD88 3023688 NM RIGHT WING BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 RIGHT WING SUPPORT FRAME OUTBOARD OF TAT TELESCOPING IS BENT. -- FABRICATED AND INSTALLED STIFFNER. 2 L 7 2 4F RT A6WE 2001083001014 20010830 01014 NE 2001 8 30 GLBA2001179 2 20010812 A 7320 LINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ENGINE LOOSE A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 226GL UE226 LEFT ENGINE NOT MAKING TORQUE. TIGHTENED LOOSE PY LINE, OPS CHECKED SATISFACTORY. 2 L 7 2 4T 4 T RT A24CE E26NE 2001083001015 20010830 01015 2001 8 30 GLBA2001180 4 20010814 A 3442 6222501001 ANTENNA BEECH 1900 1900D 1154162 CE WX RADAR FAILED A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 01 192GL 361 UE192 WEATHER RADAR FAILED. REPLACED ANTENNA, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001083001016 20010830 01016 NE 2001 8 30 GLBA2001182 3 20010818 A 6140 1143800663 INDICATOR BEECH 1900 1900D 1154162 CE HARTZL HCE4A HCE4A3A NE COCKPIT FAILED A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 01 251GL 6599 UE251 NR 2 PROP RPM INDICATOR FAILED. REPLACED, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 5 C P10NE 2001091800110 20010918 00110 SO 2001 9 18 GLBA2001183 1 20010819 A 3230 18190003 SOLENOID VALVE EMB 120 EMB120ER 3260203 SO LANDING GEAR INTERMITTENT A GLBA O OTHER O OTHER AP APPROACH 1 CE 01 96ZK 2609 120096 LANDING GEAR WOULD NOT EXTEND UNTIL CYCLED TWICE. REPLACED LANDING GEAR SOLENOID VALVE, OPS CHECKED SYSTEM SATISFACTORY . 2 L 7 2 4T RT A31SO 2001083001017 20010830 01017 CE 2001 8 30 GLBA2001184 1 20010820 A 3200 MS2417101 RELAY BEECH 1900 1900D 1154162 CE ELEC PANEL FAILED A GLBA O OTHER O OTHER AP APPROACH 1 CE 01 211GL UE211 LANDING GEAR CIRCUIT BREAKER POPPED. REPLACED K3 RELAY AND A316 PCB, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001083001018 20010830 01018 NE 2001 8 30 GLBA2001185 2 20010823 A 7230 COMPRESSOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ENGINE STALLED A GLBA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 CE 01 96UX UE96 RIGHT ENGINE COMPRESSOR STALL OR BIRD STRIKE. INSPECTED, NO DEFECTS FOUND. 2 L 7 2 4T 4 T RT A24CE E26NE 2001083001019 20010830 01019 CE 2001 8 30 GLBA2001186 1 20010824 A 7722 3034857 PROBE BEECH 1900 1900D 1154162 CE LT ENGINE INOPERATIVE A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 01 225GL 1669 UE225 LEFT ENGINE TEMP LIMITED ON T/O. REPLACED TRIM PROBE, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001083001020 20010830 01020 CE 2001 8 30 GLBA2001187 1 20010824 A 7722 PROBE BEECH 1900 1900D 1154162 CE LT ENGINE OUT OF ADJ A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 255GL UE255 LEFT ITT CLOSE TO RED LINE ON CLIMBOUT. ADJUSTED TRIM PROBE, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001083001021 20010830 01021 CE 2001 8 30 GLBA2001188 1 20010825 A 2844 CONNECTOR BEECH 1900 1900D 1154162 CE FUEL PRESSURE DIRTY A GLBA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 01 192GL UE192 RIGHT LOW FUEL PRESSURE ANNUNCIATOR ILLUMINATED. CLEANED CANNON PLUG, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001083001022 20010830 01022 2001 8 30 HNAA0100037 4 20010714 A 2330 508811 CONTROL PANEL DHAV DHC8 DHC8102 2809003 NM COCKPIT FAULTY A HNAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 908HA 015 COCKPIT PA AUDIO CONTROL SWITCH EMITTED SPARKS AND SMOKE WHEN SWITCH WAS DEPRESSED. REMOVED AND REPLACED PA AUDIO CONTR OL PANEL. 2 H 7 2 4T RT A13NM 2001083001023 20010830 01023 NM 2001 8 30 HNAA0100038 1 20010622 A 7931 CONNECTOR DHAV DHC8 DHC8201 2809001 NM NR 2 ENGINE DIRTY A HNAA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 EA 07 965HA 450 NR 2 ENGINE OIL PRESSURE INDICATION FLUXED FROM 0-20 PSI AND THEN WENT TO ZERO WITH NO ASSOCIATED WARNING LIGHT. CREW S HUT DOWN THE ENGINE. MAINTENANCE CLEANED THE NR 2 ENGINE OIL PRESSURE TRANSMITTER CONNECTOR. 2 H 7 2 4T RT A13NM 2001083001024 20010830 01024 NM 2001 8 30 HNAA0100039 1 20010712 A 7933 MS280343 BULB DHAV DHC8 DHC8102 2809003 NM NR 2 ENGINE FAILED A HNAA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 EA 07 931HA NR 2 OIL TEMP FLUCTUATED TO BETWEEN 100 DEGREES AND 115 DEGREES THEN REPEATED TWICE. INSPECTED ENGINE, REMOVED AND REPL ACED ENGINE OIL TEMP INDICATOR, NO FIX. REMOVED AND REPLACED ENGINE OIL TEMP BULB, LEAK AND OPERATIONAL CHECK GOOD. SE RVICED ENGINE WITH 2 QUARTS OF OIL. 2 H 7 2 4T RT A13NM 2001083001025 20010830 01025 2001 8 30 HNAA0100042 4 20010723 A 3442 071131900 TRANSCEIVER DHAV DHC8 DHC8102 2809003 NM WX RADAR FAILED A HNAA A UNSCHED LANDING O OTHER UK UNKNOWN 1 EA 07 928HA 24051 1755 120 AIRCRAFT RETURNED TO TPA DUE TO WEATHER RADAR INOP. REPLACED RADAR R/T. 2 H 7 2 4T RT A13NM 2001083001026 20010830 01026 NM 2001 8 30 HNAA0100045 1 20010807 A 6123 30005000034 TSCU DHAV DHC8 DHC8102 2809003 NM NR 1 & NR 2 FAILED A HNAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 07 921HA 28086 1888 089 AUTO FEATHER DID NOT ARM ON TAKEOFF. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE. REPLACED NR 1 AND NR 2 TSC U AND ADJUSTED POWER LEVER SWITCH 6121-S13. 2 H 7 2 4T RT A13NM 2001083001027 20010830 01027 EU 2001 8 30 YENA 1 20010828 A 2120 EVT345H FAN AIRBUS 320 A320232 3930326 EU 18HQ SEIZED A YENA D RETURN TO BLOCK O OTHER CL CLIMB 1 EA 15 506JB 4724 4724 1235 Flt #37, JFK to PBI, Burning smell in flight, no visible smoke. vent extract fault in flight, 2 min later, aircraft RTB to JFK, emergency declared, met fire department, JetBlue emergency procedures followed. Inspected and found the extract fan seized. removed and replaced the extract fan, fan worked. IPW 21-26-51-401, Ops check IPW 21-26-710-001, Ops check g ood, no defect noted. 2 L 7 2 4F RT A28NM 2001083001028 20010830 01028 EU 2001 8 30 01FDEA00785 1 20010828 A 2930 HYDRAULIC SYSTEM AIRBUS 300 A300F4605R 3930327 EU FAULTY A FDEA O OTHER K FLUID LOSS DE DESCENT 1 SO 25 651FE 728 01-288 LOST GREEN HYD SYS ON DECENT. COMPLIED WITH ECAM & QRH PROC. ** S/D ** COMING 2 L 7 2 4F RT A35EU 2001091900131 20010919 00131 NM 2001 9 19 01FDEA00788 1 20010824 A 5311 FRAME DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 619FE 48770 FUSELAGE TRANSVERSE FRAME CRACKED AT STA Y=1601 LEFT 3.0 INCH LENGTH, ALONG LONGERON 12L. REMOVED AND REPLACED FRAME PE R SRM 53-30-00 FIG 1 VOL 1. 2 L 7 3 4F RT A22WE 2001083001029 20010830 01029 NM 2001 8 30 01FDEA00789 1 20010824 A 5310 FRAME DOUG MD11 MD11F 3023600 NM MAIN DECK CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 619FE 48770 N 527 FUSELAGE TRANSVERSE FRAME CRACKED AT STA Y=1571 LEFT ALONG LONGERON 12L. ** S/D ** COMING 2 L 7 3 4F RT A22WE 2001101500170 20011015 00170 NM 2001 10 15 01FDEA00790 1 20010824 A 5311 FRAME DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 619FE 48770 FUSELAGE TRANSVERSE FRAME DENTED AT STA 1701 LEFT ALONG LONGERON 12L. R&R FRAME PER SRM 53-30-00 FIG 1 VOL 1. 2 L 7 3 4F RT A22WE 2001101500172 20011015 00172 NM 2001 10 15 01FDEA00791 1 20010824 A 5311 FRAME DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 619FE 48770 FUSELAGE TRANSVERSE FRAME DENTED AT STA 1661 RIGHT ALONG LONGERON 12R. R&R FRAME PER SRM 53-30-00 FIG 1 VOL 1. 2 L 7 3 4F RT A22WE 2001101500174 20011015 00174 NM 2001 10 15 01FDEA00792 1 20010824 A 5311 FRAME DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 619FE 48770 FUSELAGE TRANSVERSE FRAME DENTED AT STA 1701 RIGHT ALONG LONGERON 12R. R&R FRAME PER SRM53-30-00 FIG 1 VOL 1. 2 L 7 3 4F RT A22WE 2001083001030 20010830 01030 EU 2001 8 30 YENA200104 1 20010828 A 2120 EVT345H FAN AIRBUS 320 A320232 3930326 EU 18HQ SEIZED A YENA D RETURN TO BLOCK O OTHER CR CRUISE 1 EA 15 506JB 4724 4724 1235 Flt #37, JFK to PBI, Burning smell in flight, no visible smoke. vent extract fault in flight, 2 min later, aircraft RTB to JFK, emergency declared, met fire department, JetBlue emergency procedures followed.Inspected and found the extract f an seized. Removed and replaced the extract fan, fan worked. IPW 21-26-51-401, Ops check IPW 21-26-710-001, Ops check go od, no defect noted. 2 L 7 2 4F RT A28NM 2001083001031 20010830 01031 NM 2001 8 30 A6WA200100049 1 20010804 A 2133 2097H020900 OUTFLOW VALVE DORNER DO32 DO328100 2996000 NM AFT STUCK A A6WA A UNSCHED LANDING S AFFECT SYSTEMS TO TAKEOFF 1 GL 31 330PH 4739 4739 3008 **CLOSED**CABIN WILL NOT PRESSURIZE, CAN SEE DAYLIGHT THRU DOOR AT UPPER LEFT HAND CORNER. MAINTENANCE REMOVED AND REPL ACED REAR OUTFLOW VALVE. 2 H 7 2 4T RT A45NM 2001083001032 20010830 01032 NM 2001 8 30 HNAA0100047 1 20010810 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A HNAA K NONE L NO TEST NR NOT REPORTED 1 EA 07 916HA 072 FIRST TWO FLOOR LEVEL EMERGENCY LIGHTS WERE INOP. FOUND BROKEN WIRE UNDER FLOOR AT ROW 1. REPAIRED WIRE. 2 H 7 2 4T RT A13NM 2001083001033 20010830 01033 EA 2001 8 30 HNAA0100050 1 20010817 A 3350 BATTERY PACK DHAV DHC8 DHC8311 1386006 EA CABIN DISCHARGED A HNAA K NONE L NO TEST NR NOT REPORTED 1 EA 07 330EN 274 THIRD AND FOURTH RED FLOOR LEVEL EMERGENCY LIGHTS AT ROW 1 AND 4 WHITE FLOOR LEVEL EMERGENCY LIGHTS AT ROW 4 WERE INOP. REPLACED EMERGENCY LIGHT BATTERY PACKS 3351-PS2 & PS3 AND BATTERY PACK POWER SUPPLY 3351-PS2. 2 H 7 2 4T RT A13NM 2001083001034 20010830 01034 NM 2001 8 30 HNAA010046 1 20010807 A 6123 30005000047 TSCU DHAV DHC8 DHC8102 2809003 NM HAMSTD 14SF 14SF7 NE NR 1 & NR 2 INOPERATIVE A HNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 07 921HA 19510 089 AUTO FEATHER DID NOT ARM ON TAKEOFF. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO GATE. REPLACED NR 1 AND 2 TSCU AND A DJUSTED POWER LEVER SWITCH 6121-S13. 2 H 7 2 4T RT A13NM 6 C P7NE 2001083001035 20010830 01035 NM 2001 8 30 HNAA010049 1 20010815 A 2913 CONNECTOR DHAV DHC8 DHC8102 2809003 NM HYD PUMP CORRODED A HNAA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 EA 07 926HA 114 NR 2 ENGINE HYDRAULIC PUMP CAUTION LIGHT ILLUMINATED IN FLIGHT, PRESSURE INDICATION WAS NORMAL. AIRCRAFT RETURNED TO DE PARTURE AIRPORT. FOUND CORROSION ON CONNECTOR PINS. CLEANED CONNECTOR PINS OF CORROSION. 2 H 7 2 4T RT A13NM 2001083001037 20010830 01037 NE 2001 8 30 IXXA0100050O 2 20010804 A 7310 217415 FILTER DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE NR 3 ENGINE DIRTY A IXXA O OTHER X ENGINE FLAMEOUT CL CLIMB 1 SW 11 821BX 81275 1285 45811 693303 EN ROUTE FROM LAX TO PDX, THE NUMBER THREE ENGINE FLAMED OUT DURING CLIMB. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURE A ND PERFORMED A SUCCESSFUL RESTART AFTER TRANSFERRING TO AN ALTERNATE FUEL SOURCE. THE FLIGHT CONTINUED TO PDX FOR AN UN EVENTFUL LANDING. MAINTENANCE INSPECTED THE ENGINE IN ACCORDANCE WITH THE CFMI MAINTENANCE MANUAL WITH NO DISCREPANCY N OTED. MAINTENANCE REPLACED THE MAIN ENGINE FUEL FILTER AS PRECAUTIONARY, PERFORMED POWER ASSURANCE CHECKS IN ACCORDANCE WITH THE COMPANY ENGINE RUN HANDBOOK WITH NO DISCREPANCIES NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT 4A25 E2GL 2001083001038 20010830 01038 EA 2001 8 30 JBXA000288 1 20010605 A 2750 FLAP CNDAIR CL600 CL6002B19 EA WING MALFUNCTIONED A JBXA K NONE F FLT CONT AFFECTED AP APPROACH 1 SO 05 591ML 7388 FLAPS FAIL AT 30 DEGREES ON SHORT FINAL. PERFORMED OPERATIONAL CHECK OF FLAP SYSTEM PER AMM 27-54-00. SYSTEM OPERATION AL CHECKS NORMAL. OK FOR SERVICE. 2 L 7 2 4F RT A21EA 2001083001039 20010830 01039 EA 2001 8 30 JBXA000289 1 20010607 A 3010 SWITCH CNDAIR CL600 CL6002B19 EA LT WING INOPERATIVE A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 575ML 7256 ANTI-ICE DUCT MESSAGE DURING CLIMBOUT OF RDU. MSG AND AURAL ON THRU FL180 WITH ANTI-ICE IN OFF MSG AND AURAL INTERMITTEN T BACK TO RDU. AUTO-ICE SYNOPTIC PAGE SHOWED RED LEADING EDGE ON LEFT WING. REMOVED AND REPLACED LEFT WING 21 THERMAL SWITCHES AND OPS CK GOOD IAW C--65 AMM 36-21-07, OPS CK GOOD. 2 L 7 2 4F RT A21EA 2001083001040 20010830 01040 EA 2001 8 30 JBXA000290 1 20010609 A 2700 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTIONED A JBXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 05 592ML 7410 ABORTED TAKEOFF DUE CONFIG AILERON, CONFIG SPOILERS, CONFIG TRIM RED MSG. PERFORMED OPERATIONAL CHECK OF PSEU AND MDC I AW 32-61-00. NO FAULTS FOUND AT THIS TIME. 2 L 7 2 4F RT A21EA 2001083001041 20010830 01041 2001 8 30 JBXA000291 4 20010610 A 2230 AUTOTHRUST SYS FOKKER F28 F28MK0100 4990807 EU COCKPIT MALFUNCTIONED A JBXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 05 110ML 11486 FLT 555 RDU/LGA AUTOTHROTTLE NR 1 AND 2 FAULTED ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE. RESET FCC AND FAC NR 1 AND 2 AUTOTHROTTLE, OPS CHECK GOOD IAW F-100 MM 22-11-00. 2 L 7 2 4F RT 2001083001042 20010830 01042 NM 2001 8 30 CALA0100819 1 20010829 A 5320 ANGLE BOEING 737 7373T0 1384582 NM R-2 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION R-2 DOOR Z-ANGLE CORRODED. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001083001043 20010830 01043 NM 2001 8 30 CALA0100820 1 20010829 A 5320 ANGLE BOEING 737 7373T0 1384582 NM L-2 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001083001044 20010830 01044 NM 2001 8 30 CALA0100821 1 20010829 A 5320 STRAP BOEING 737 7373T0 1384582 NM AFT LAV CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND "H" STRAP IN AFT LAV AREA CORRODED. THE STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 51-10-0 2. 2 L 7 2 4F RT A16WE 2001083001045 20010830 01045 NM 2001 8 30 CALA0100822 1 20010829 A 5320 BRACE BOEING 737 7373T0 1384582 NM STA 1006-1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND L/H AND R/H DIAGONAL BRACES CORRODED AT STA 1006-1016. NEW DIAGONAL BRACES WERE INSTALLED IAW SRM 51-10 -02. 2 L 7 2 4F RT A16WE 2001083001046 20010830 01046 NM 2001 8 30 JBXA000293 1 20010612 A 5270 WARNING LIGHT BOEING 737 737* NM COCKPIT ILLUMINATED A JBXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 05 362ML 30737 FLT 377 MCO/RDU ABORTED TAKEOFF FOR RIGHT OVERWING EXIT LIGHT ILLUMINATED ON P5 PANEL. ISSUED MEL 52-3-1. 2 L 7 2 4F RT A16WE 2001083001047 20010830 01047 EU 2001 8 30 JBXA000296 1 20010621 A 3241 61042724 CONTROL BOX FOKKER F28 F28MK0100 4990807 EU ANTI-SKID SYS FAULTY A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 109ML 11485 IN FLIGHT THE ANTI-SKID FAULT LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH. REMOVED AND REPLACED ANTI-SKID CONTROL BOX IA W F100 AMM 32-45-01. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F RT 2001083001048 20010830 01048 GL 2001 8 30 2001F00245 2 20010623 A 7200 ENGINE BOLKMS 105 BO105LSA3 5626020 EU ALLSN 250C 250C28C 03013 GL NR 1 FAILED A BRMA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 07 93LF 2038 CAE280102 AIRCRAFT WAS ON WAY BACK FROM BURLEY IDAHO TO BRMS, WHEN RECEIVING A CAUTIONARY CHIP LIGHT FOR THE NR 1 ENGINE. THE CHI P WAS BURNED OFF USING THE FUZZ BUSTER. SHORTLY THERE AFTER THE NR 1 CHIP LIGHT CAME ON AGAIN. THE AIRCRAFT MAD A PREC AUTIONARY LANDING AT THE POCATELLO AIRPORT. WHEN INSPECTING THE INCIDENT THE ENGINE WAS DETERMINED TO BE UNSERVICEABLE AND THE ENGINE REPLACED. THE ENGINE WAS SENT TO AN OVERHAUL FACILITY. (M) 1 G 7 2 3U 3 U H3AU E1GL 2001083001049 20010830 01049 NM 2001 8 30 2001F00246 1 20010522 A 3234 4105DA SELECTOR VALVE BOEING 737 7372K5 138448X NM MLG WW DEFECTIVE A RJEF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 231TA 22596 SAP - FLT 220 - DURING CLIMB, LEFT AND RIGHT MLG DID NOT SECURE IN UPLOCK POSITION. THE AIRCRAFT RETURNED TO SAP FOR MX . A FERRY FLT PERMIT WAS GRANTED. AFTER LANDING AT EL SALVADOR, MX TECHS PERFORMED RETRACTION AND EXTENSION OF THE LAN DING GEARS AS PER AMM 32-32. FOUND INCORRECT OPERATION OF THE SELECTOR VALVE. THE UNIT WAS REPLACED AND TESTED AS PER AMM 32-31-51. ALSO, THE FILTER ELEMENTS OF THE MODULAR PACKAGES 'A' AND 'B' WERE REPLACED AS PER AMM 29-11-71 AND AMM 2 9-12-41. LANDING GEARS RETRACTION AND EXTENSION WERE PERFORMED ON GROUND AS PER AMM 32-32. NORMAL RESULTS WERE OBSERVE D. TEST FLIGHT WAS PERFORMED. THE LANDING GEAR RETRACTION AND EXTENSION SYSTEM SHOWED NORMAL. THE AIRCRAFT RETURNED T 2 L 7 2 4F RT A16WE 2001083001050 20010830 01050 SO 2001 8 30 2001F00247 1 20010801 A 4940 51989261 STARTER GULSTM G1159 GIV 3980115 SO APU FAILED A UG8A O OTHER O OTHER NR NOT REPORTED 1 GL 23 940DC 1052 PTK - FLT 2164 - APU INOPERATIVE. APU STARTER FAILURE. REMOVED AND REPLACED STARTER WITH OVERHAULED UNIT. (M) 2 L 7 2 4F RT A12EA 2001083001051 20010830 01051 NM 2001 8 30 AALA20011466 1 20010725 A 5730 SKIN BOEING 757 757223 1384957 NM WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 655AA 24613 TUL - FOUND UPPER WING SKIN CORRODED IN BLACK PAINTED AREA AT EMERGENCY EXIT PATH. BLENDED AREA. FLAPPER PEEN, REINSTAL LED FASTENERS. (M) 2 L 7 2 4F RT A2NM 2001083001052 20010830 01052 WP 2001 8 30 AALA20011472 1 20010712 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7522A 49899 TUL - FOUND CORROSION ON LEFT CUSP AT STATION 660. FABRICATED AND INSTALLED DOUBLER PER AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 2001083001053 20010830 01053 WP 2001 8 30 AALA20011473 1 20010712 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7522A 49899 TUL - FOUND CUSP CORROSION FROM STATION 509 TO 518 RIGHT. INSTALLED DOUBLER FROM STATION 505 TO 522 PER SRM 53-01 FIG 4 -3. (M) 2 L 7 2 4F A6WE 2001083001054 20010830 01054 WP 2001 8 30 AALA20011476 1 20010711 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7522A 49899 TUL - FOUND CORROSION ON LEFT CUSP STATION 580-610. INSTALLED CUSP DOUBLER SRM 53-01 FIG 4-3 WITH HI-LOCKS USED AT AFT END OF DOUBLER UNDER TRACK NR 1 AND ALONG INBOARD OF NR 2 TRACK. (M) 2 L 7 2 4F A6WE 2001083001055 20010830 01055 WP 2001 8 30 AALA20011477 1 20010711 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7522A 49899 TUL - FOUND CORROSION ON LEFT CUSP IN SEVERAL AREAS STATION 503-598. REPLACED SECTION OF CUSP WITH NEW PER SRM 52-01 FI G 4-3. (M) 2 L 7 2 4F A6WE 2001083001056 20010830 01056 WP 2001 8 30 AALA20011478 1 20010709 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7522A 49899 TUL - FOUND CORROSION ON TOP OF CUSP RIGHT. CUT OUT CORRODED AREA AND INSTALLED REPAIR DOUBLER SRM 53-01 FIG 4-3. (M) 2 L 7 2 4F A6WE 2001083001057 20010830 01057 WP 2001 8 30 AALA20011487 1 20010722 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 487AA 49680 DFW - DURING OVERNIGHT MAINTENANCE, LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LEFT OVERWING EMERGENCY EX IT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001083001058 20010830 01058 WP 2001 8 30 AALA20011492 1 20010723 A 3350 LIGHT DOUG DC9 DC982 3022082 WP AFT AIRSTAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 203AA 49145 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AS SEMBLY AT AFT AIRSTAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001083001059 20010830 01059 WP 2001 8 30 AALA20011497 1 20010725 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 491AA 49684 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHT SEAT 8D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001083001060 20010830 01060 NM 2001 8 30 AALA20011516 1 20010728 A 3350 LIGHT BOEING 777 777223 1385213 NM G3 GALLEY INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 792AN 30253 DFW - DURING OVERNIGHT MAINTENANCE, LEFT FORWARD EMERGENCY EXIT LIGHT AT G3 GALLEY INOPERATIVE. REPLACED LIGHT ASSEMBLY AT G3 GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001083001061 20010830 01061 NM 2001 8 30 AALA20011524 1 20010729 A 3350 SOCKET BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 631AA 24589 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHT AT SEAT 15D INOPERATIVE. REPLACED SOCKET ASSEMBLY AT SEAT 15D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001083001062 20010830 01062 NM 2001 8 30 AALA20011576 1 20010727 A 5330 SKIN BOEING 727 727227 1384078 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 720AA 20613 TUL - FOUND SKIN BULGING AFT OF 480 BUTT SPLICE STRINGER 28 LEFT, 14 INCHES BY 2 INCHES. REMOVED CORROSION AND INSTALLE D DOUBLER REPAIR AND FILLER PER SRM 53-30-03 FIG 3A. (M) 2 L 7 3 4F A3WE 2001083001063 20010830 01063 NM 2001 8 30 AALA20011578 1 20010729 A 5720 ANGLE BOEING 727 727227 1384078 NM WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 720AA 20613 TUL - FOUND LEADING EDGE WING SKIN BULGED AT UPPER SPAR ATTACH SCREWS 8 INCH - 9 INCH OUTBOARD OF FUSELAGE. REMOVED COR ROSION TREATED AND PRIMED AREA AND INSTALLED A STRAP AND ANGLES WITH DOUBLER REPAIR PER ESO 11697 DATED 7/27/2001. (M) 2 L 7 3 4F A3WE 2001083001064 20010830 01064 NM 2001 8 30 AALA20011583 1 20010731 A 5730 SKIN BOEING 727 727227 1384078 NM LT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 716AA 20608 TUL - FOUND CORROSION ON LOWER WING SKIN IN AREA OF PREVIOUS REPAIR ABOVE LEFT PRIMARY HEAT EXCHANGER. REPAIRED PER ESO 11697 DATED 7/31/2001 EXTERNAL DOUBLER. (M) 2 L 7 3 4F A3WE 2001083001065 20010830 01065 NM 2001 8 30 AALA20011584 1 20010731 A 5730 SKIN BOEING 727 727227 1384078 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 716AA 20608 TUL - FOUND CORROSION AROUND FASTENER HEAD LOWER SKIN OF WING CENTER SECTION LBL 24 STRINGER 6. REPAIRED PER ESO 11697 DATED 7/31/2001 EXTERNAL DOUBLER. (M) 2 L 7 3 4F A3WE 2001083001066 20010830 01066 NM 2001 8 30 AALA20011587 1 20010731 A 5330 SKIN BOEING 727 727227 1384078 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 716AA 20608 TUL - FOUND FUSELAGE SKIN BULGED STATION 992 STRINGER 29R. REMOVED CORRODED AREA OF SKIN AND INSTALLED DOUBLER PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 2001083001067 20010830 01067 NM 2001 8 30 P2EA01125 1 20010702 A 5312 BULKHEAD BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 128NJ 22892 DURING C-CHECK INSPECTION PER SB 737-53A1173, PRESSURE BULKHEAD BS 178 WEB CRACKED AT WL 234, LBL 10. PRESSURE BULKHEAD BS 178 WEB REPAIRED FROM LBL 6.75 TO 16.25 BETWEEN WL 237 AND 230.5 IAW SRM 53-10-11 FIG 1 DET II. (M) 2 L 7 2 4F A16WE 2001083001068 20010830 01068 NM 2001 8 30 USAA010930 1 20010725 A 5347 SEAT TRACK BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND SEAT TRACK CORRODED 1 INCH BY 1 INCH AREA, BS 660, RBL 45. REMOVED AND REPLACED SEAT TRACK SECTION PER SRM 5 3-00-52. (M) 2 L 7 2 4F RT A2NM 2001083001070 20010830 01070 NM 2001 8 30 USAA010946 1 20010725 A 5300 SKIN BOEING 757 757225 1384959 NM BS 1360-1380 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND FUSELAGE SKIN WITH PREVIOUSLY RECORDED LIGHTNING STRIKE, BS 1360 TO 1380, BETWEEN S26/S27R. TWENTY PREVIOUS LY INSTALLED NR 6 RIVETS PER SRM 53-00-01, FIG 207. (M) 2 L 7 2 4F RT A2NM 2001083001071 20010830 01071 NM 2001 8 30 USAA010945 1 20010725 A 5330 SKIN BOEING 757 757225 1384959 NM BS 712 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND FUSELAGE SKIN WITH PREVIOUSLY RECORDED LIGHTNING STRIKE, BS 712, BETWEEN S23 AND S24R. PREVIOUSLY INSTALLED .25 INCH RIVET PER SRM 53-00-01, FIG 207. (M) 2 L 7 2 4F RT A2NM 2001083001072 20010830 01072 NM 2001 8 30 USAA010944 1 20010725 A 5300 SKIN BOEING 757 757225 1384959 NM BS 693 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND FUSELAGE SKIN WITH PREVIOUSLY RECORDED LIGHTNING STRIKE, BS 693, BETWEEN S23R AND S24R. PREVIOUSLY INSTALLE D .25 INCH RIVET PER SRM 53-00-01, FIG 207. (M) 2 L 7 2 4F RT A2NM 2001083001073 20010830 01073 NM 2001 8 30 USAA010943 1 20010725 A 5330 SKIN BOEING 757 757225 1384959 NM BS 690 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND FUSELAGE SKIN WITH PREVIOUSLY RECORDED LIGHTENING STRIKE, BS 690, BETWEEN S26R AND S27R AND BETWEEN S23 AND S24R. PREVIOUSLY INSTALLED .25 INCH RIVET PER SRM 53-00-01, FIG 207. (M) 2 L 7 2 4F RT A2NM 2001083001074 20010830 01074 NM 2001 8 30 USAA010942 1 20010725 A 5300 SKIN BOEING 757 757225 1384959 NM BS 685 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND FUSELAGE SKIN WITH PREVIOUSLY RECORDED LIGHTNING STRIKE, BS 685 BETWEEN S26R AND S27R. PREVIOUSLY INSTALLED .25 INCH RIVET PER SRM 53-00-01, FIG 207. (M) 2 L 7 2 4F RT A2NM 2001083001075 20010830 01075 NM 2001 8 30 USAA010941 1 20010725 A 5300 SKIN BOEING 757 757225 1384959 NM BS 644 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND FUSELAGE SKIN WITH PREVIOUSLY RECORDED LIGHTNING STRIKE, BS 644 BETWEEN S23R AND S24R. PREVIOUSLY INSTALLED .25 INCH RIVET PER SRM 53-00-01, FIG 207. (M) 2 L 7 2 4F RT A2NM 2001083001076 20010830 01076 NM 2001 8 30 USAA010940 1 20010725 A 5300 SKIN BOEING 757 757225 1384959 NM BS 625 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND FUSELAGE SKIN WITH PREVIOUSLY RECORDED LIGHTNING STRIKE, BS 625 BETWEEN S26R AND S27R. PREVIOUSLY INSTALLED .25 INCH RIVET PER SRM 53-00-01, FIG 207. (M) 2 L 7 2 4F RT A2NM 2001083001077 20010830 01077 NM 2001 8 30 USAA010993 1 20010806 A 5300 CLIP BOEING 757 757225 1384959 NM BS 1480 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND FRAME CLIP CORRODED 1 INCH BY 2.5 INCHES, BS 1480 BETWEEN STRINGER 26R AND 27R. LOWER FRAME SECTION REPLACE D AND BRACKETS ADDED PER SRM 51-40-02. (M) 2 L 7 2 4F RT A2NM 2001083001078 20010830 01078 NM 2001 8 30 USAA010965 1 20010723 A 5300 INTERCOSTAL BOEING 757 7572B7 1384964 NM BS 1661-1681 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 632AU 22219 27810 CLT - FOUND INTERCOSTAL CRACKED .5 INCH, BS 1661 TO 1681. REMOVED AND REPLACED PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 2001083001079 20010830 01079 NM 2001 8 30 USAA010971 1 20010731 A 5320 INTERCOSTAL BOEING 757 7572B7 1384964 NM BS 365.23-377.7 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 632AU 27810 CLT - FOUND INTERCOSTAL CORRODED 12 INCHES BY 3 INCHES, BS 365.23 TO 377.77, LBL 50. CORROSION LEVEL 1, TASK NR C53-221 -03. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 2001083001080 20010830 01080 NM 2001 8 30 USAA010967 1 20010731 A 5300 SKIN BOEING 757 7572B7 1384964 NM BS 686 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 632AU 22219 27810 CLT - FOUND SKIN HAS HOLE WITH DENT .250 INCH, BS 686, BETWEEN S21R AND 22R. DAMAGED REMOVED, INSTALLED DOUBLER AND FIL LER PER SRM 53-00-01 FIG 203, AND 51-40-02. (M) 2 L 7 2 4F RT A2NM 2001083001081 20010830 01081 NM 2001 8 30 USAA010968 1 20010731 A 5300 SKIN BOEING 757 7572B7 1384964 NM BS 438 PUNCTURED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 632AU 27810 CLT - FOUND SKIN PUNCTURED 1 INCH, STATION 438, BETWEEN STRINGER 19R AND 20R. PREVIOUSLY INSTALLED DOUBLER PER RM 53-00 -01 FIG 208. (M) 2 L 7 2 4F RT A2NM 2001083001082 20010830 01082 NM 2001 8 30 USAA010962 1 20010801 A 5300 SEAT TRACK BOEING 757 7572B7 1384964 NM BS 376.7-440 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 631AU 22441 27809 CLT - FOUND SEAT TRACK CORRODED APPROXIMATELY 4 SQUARE INCH AREA, BS 376.7 TO 440 AT LBL 24.75 AND LBL 45.5. CORROSION LEVEL 1, TASK NR C53-221-03. REMOVED AND ERPLACED SEAT TRACK SECTIONS PER SRM 51-10-02. (M) 2 L 7 2 4F RT A2NM 2001083001083 20010830 01083 NM 2001 8 30 USAA010972 1 20010731 A 5300 SEAT TRACK BOEING 757 7572B7 1384964 NM BS 377.7 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 632AU 22218 27810 CLT - FOUND SEAT TRACK CORRODED 2 INCH BY 2 INCH AREA, STATION 377.7 LBL 45.5. CORROSON LEVEL 1, TASK NR C53-221-03. R EMOVED AND REPLACED SEAT TRACK PER SRM 51-10-00 AND 51-40-02. (M) 2 L 7 2 4F RT A2NM 2001083001084 20010830 01084 NM 2001 8 30 USAA010973 1 20010731 A 5300 SEAT TRACK BOEING 757 7572B7 1384964 NM BS 377.7 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 632AU 22218 27810 CLT - FOUND SEAT TRACK CORRODED 2 INCHES BY 2 INCHES, STATION 377.7 LBL 24.75. CORROSION LEVEL 1, TASK NR C53-221-03. REPLACED SEAT TRACK PER SRM 51-30-01. (M) 2 L 7 2 4F RT A2NM 2001083001085 20010830 01085 NM 2001 8 30 USAA010978 1 20010806 A 5300 FRAME BOEING 757 757225 1384959 NM BS 1420 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 54141 22198 CLT - FOUND FRAME CORRODED .5 INCH HOLE AND .5 INCH CORRODED AREA, STATION 1420 BETWEEN STRINGER 26L AND 27L. DOUBLER I NSTALLED PER EA 69860. (M) 2 L 7 2 4F RT A2NM 2001083001086 20010830 01086 NM 2001 8 30 USAA010995 1 20010806 A 5300 FRAME BOEING 757 757225 1384959 NM BS 1500 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 54141 22198 CLT - FOUND FRAME DENT .5 INCH IN DIAMETER, BS 1500 ABOVE S26L. DAMAGED REMOVED, REPAIR DOUBLER INSTALLED PER EA 69860. (M) 2 L 7 2 4F RT A2NM 2001083001087 20010830 01087 NM 2001 8 30 ASAA0110319 1 20010607 A 3350 90052 BATTERY PACK BOEING 737 737210C 1384459 NM DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING PREFLIGHT CHECK, TRACK LIGHTING BATTERY PACK AT SEAT PALLET 5-1 WAS DETERMINED TO BE DISCHARGED. REPLACED BATTERY PACK WITH SERVICEABLE PACK. ASSOCIATED LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2001083001088 20010830 01088 NM 2001 8 30 ASA0110318 1 20010603 A 3350 86210144 BATTERY BOEING 737 737290C 138448V NM MID CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 ANC - DURING SCHEDULED MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT SEAT PALLETS 902 AND 10-8 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2001083001089 20010830 01089 NM 2001 8 30 ASAA0110313 1 20010530 A 3350 883200312 RECEIVER BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT SEAT PALLETS 6-9 INOPERATIVE. REMOVED AND REPLACED REMOT E ASSEMBLY BATTERY AND RECEIVER THEN LIGHTS OPERATED NORMAL. (M) 2 L 7 2 4F A16WE 2001083001090 20010830 01090 NM 2001 8 30 ASAA0110354 1 20010612 A 3350 86210144 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS FAILED RECON TEST. REMOVED AND REPLACED REMOTE ASSEMBLY BAT TERY THEN EXIT LIGHTS OPERATED NORMAL. (M) 2 L 7 2 4F RT A16WE 2001083001091 20010830 01091 WP 2001 8 30 ASAA0180201 1 20010611 A 3350 6011779 POWER SUPPLY DOUG DC9 DC982 3022082 WP INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 933AS 36455 7603 49234 PHX - DURING A-CHECK, EXTERIOR OVERWING EMERGENCY EXIT LIGHTS ON BOTH SIDES OF AIRCRAFT WERE DETERMINED TO BE INOPERATIV E. REPLACED ASSOCIATED BATTERY PACK. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 2001083001092 20010830 01092 NM 2001 8 30 ASAA0110364 1 20010614 A 3350 8821004 BATTERY PACK BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT SEAT PALLETS 7-4, 9-2, 7-5, 6-2 AND 5-6 WOULD NOT TEST. REMOVED AND REPLACED BATTERY PACKS THEN LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2001083001093 20010830 01093 NM 2001 8 30 ASAA0110365 1 20010615 A 3350 8821004 BATTERY PACK BOEING 737 7372Q8C 138448S NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS ON SEAT PALLET 10-3 AND SMOKE BARRIER WOULD NOT TEST. REMOV ED AND REPLACED BATTERY PACK AND REMOTE ASSEMBLY BATTERY, THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F A16WE 2001083001094 20010830 01094 WP 2001 8 30 ASAA0180204 1 20010620 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 953AS 49386 ANC - DURING PREFLIGHT, OVERWING EMERGENCY LIGHTS WERE DETERMINED TO BE INOPERATIVE. REPLACED BATTERY PACK. LIGHTS THE N OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 2001083001095 20010830 01095 NM 2001 8 30 ASAA0110427 1 20010625 A 3350 86210144 BATTERY BOEING 737 737210C 1384459 NM INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS ON SEAT PALLET 3 INOPERATIVE. REMOVED AND REPLACED REMOTE A SSEMBLY BATTERY AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2001083100001 20010831 00001 SO 2001 8 31 C2XA01IA347 1 20010828 A 2100 22045402 ACM EMB 120 EMB120ER 3260203 SO FUSELAGE FROZEN A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 58733 120197 IAH - FLIGHT 3518, THE CREW REPORTED THAT AFTER ENGINE START THE CABIN FILLED WITH SMOKE. MAINTENANCE INSPECTED THE AIRC RAFT AND PLACED THE NUMBER TWO ACM ON MEL 21-50-2/C CONTROL NUMBER 015282, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO S ERVICE. THE AIRCRAFT RETURNED TO IAH ON 08/30/01 WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ACM, REMOVED THE MEL, AND APPROVED THE AIRCRAFT FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001083100002 20010831 00002 SO 2001 8 31 C2XA01IA348 1 20010827 A 5713 12004363002 STRINGER EMB 120 EMB120ER 3260203 SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27716 120128 IAH - DURING MAINTENANCE INSPECTION, STRINGER 8 OF THE RIGHT WING WAS FOUND TO BE CRACKED AFT OF ACCESS PANEL 622EB. MAI NTENANCE PERFORMED A SPLICE REPAIR TO THE AFFECTED STRINGER IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHANGE EC 5710-01010, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001083100003 20010831 00003 EU 2001 8 31 C2XA01IA350 1 20010824 A 3230 D227010002 HARNESS AEROSP ATR42 ATR42320 8680930 EU NOSE GEAR INOPERATIVE A C2XA O OTHER J WARNING INDICATION UK UNKNOWN 1 SW 27 15818 153 LIT - FLIGHT 3595, THE CREW REPORTED THAT THE LANDING GEAR RETRACTION SYSTEM WAS INOPERATIVE. THE LANDING GEAR WAS PINNE D IN THE DOWN POSITION, AND PLACED ON MEL. THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE NOSE LA NDING GEAR UPPER HARNESS, OPERATIONALLY CHECKED GOOD, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI CE. 2 H 7 2 4T RT A53EU 2001083100004 20010831 00004 NM 2001 8 31 SABA010045 1 20010828 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A SABA K NONE O OTHER IN INSP/MAINT 1 SO 33 813PH 032 Aircraft 813 prior to flight 5099 CLT to PGV. During preflight the aft overhead emergency lights were inoperative. No emergency procedures were used. Maintenance removed and replaced the aft emergency light power supply. System ops chec ked good. Aircraft returned to service. 2 H 7 2 4T RT A13NM 2001083100006 20010831 00006 NM 2001 8 31 01FDEA00779 1 20010829 A 3520 GASPER FAN BOEING 727 727233 138408A NM OXYGEN SYS FAILED A FDEA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 25 282FE 22349 FOLLOWING DESCENT DUE TO PRESS PROBLEMS. CREW NOTICED SMELL ASSOCIATED WITH ELECTRICAL FIRE, NO SMOKE. R&R GASPER FAN P ER MM 21-23-011-4. OK FOR SERVICE. 2 L 7 3 4F RT A3WE 2001083100007 20010831 00007 SO 2001 8 31 GLBA2001181 1 20010815 A 3230 LANDING GEAR EMB 120 EMB120ER 3260203 SO NLG & MLG MALFUNCTIONED A GLBA K NONE J WARNING INDICATION LD LANDING 1 CE 01 96ZK 120096 LANDING GEAR HANDLE CYCLED TWICE BEFORE GEAR EXTENDED. COULD NOT DUPLICATE SYSTEM, OPS CHECKED SATISFACTORY. 2 L 7 2 4T RT A31SO 2001083100008 20010831 00008 NE 2001 8 31 JBXA000292 2 20010612 A 7261 SCREEN CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RT ENGINE COKED A JBXA K NONE J WARNING INDICATION AP APPROACH 1 SO 05 577ML 7269 FLIGHT 215 RDU TO PVD ON APPROACH HAD RIGHT ENG OIL PRESSURE LOW MASTER WARNING. DRAINED ADG OIL, INSPECTED CHIP DETEC TOR FOUND C SUMP FWD SCAVENGE DRAIN SCREEN COKED UP. REMOVED COKED UP OIL RESIDUE IAW ALERT SVC BULLETIN 79-00-12. C-SU MP SCAVENGE SCREEN CHECK, GROUND RAN ENGINE FOR COMSUMPTION CHECK IAW 71-00-00. NO FURTHER CONSUMPTION NOTED AT THIS TIM E. RE-EXAMINED CHIP DETECTOR IAW 72-00-00, NO CHIPS FOUND. 2 L 7 2 4F 4 F RT A21EA E15NE 2001083100009 20010831 00009 EA 2001 8 31 JBXA000294 1 20010613 A 3620 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA BLEED AIR SYS MALFUNCTIONED A JBXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 05 584 7330 ON TAKEOFF ROLL IN BLD WITH POWER GOING THROUGH 80PERCENT N1 AT ABOUT 40 KTS CREW GOT A MASTER WARNING, TRIPLE CHIME, R 14TH DUCT MESSAGE AND BLEED AIR DUCT MESSAGE. ABORTED TAKEOFF AND RETURNED TO THE GATE. OPS CHECK OF BLEED AIR SYSTEM A ND WARNING SYSTEM. OPS CHECK GOOD AT THIS TIME. RAN ENGINES TO 85 PERCENT N1 TEST BLEED AIR SYSTEM, NO DEFECT NOTED AT THIS TIME IAW 36-21-00. 2 L 7 2 4F RT A21EA 2001083100010 20010831 00010 EA 2001 8 31 JBXA000295 1 20010618 A 3620 SENSING ELEMENT CNDAIR CL600 CL6002B19 EA BLEED AIR SYS FAULTY A JBXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 05 584 9330 CLIMBING OUT OF 10,000 FT MSL R/T 14TH STAGE OVERHEAT WARNING CAME ON. A/C RETURNED TO RDU. REMOVED AND REPLACED RT SE NSING ELEMENT A58WK IAW 36-21-04. PERFORMED OPS CHECK. NO FAULTS NOTED AT THIS TIME. 2 L 7 2 4F RT A21EA 2001083100011 20010831 00011 NE 2001 8 31 JBXA000297 2 20010622 A 7200 ENGINE FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAY65015 54557 NE NR 1 MALFUNCTIONED A JBXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 05 110ML 11486 HIGH EGT APPROACHING REDLINE DURING TOGA TAKEOFF RDU. PEAK TGT 850 FOR 1 SECOND. PERFORMED OPS CHECK OF NR 1 ENGINE TO GA EGT IAW AMM 71-00-00, NO FAULTS NOTED EGT WITHIN LIMITS. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT E25NE 2001083100012 20010831 00012 EA 2001 8 31 JBXA000299 1 20010702 A 4970 SENSOR CNDAIR CL600 CL6002B19 EA APU FAILED A JBXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 05 576ML 7257 IN FLIGHT APU OIL TEMP CAUTION MESSAGE ON EICAS. DUE TO NR 2 GENERATOR MEL HAD TO RETURN TO RDU. REMOVED AND REPLACED APU OIL TEMP SENSOR IAW CRJ AMM 49-91-25. PERFORMED OPS AND LEAK CHECKS IAW CRJ AMM 49-10-00. ALL OPS AND LEAK CHECKS GOOD. 2 L 7 2 4F RT A21EA 2001083100013 20010831 00013 NM 2001 8 31 ASAA0110447 1 20010630 A 3350 8821004 BATTERY PACK BOEING 737 7372X6C 1384552 NM FWD CABIN DISCHARGED A ASAA K NONE L NO TEST CR CRUISE 1 NM 01 746AS 23123 SEA - DURING FLIGHT EMERGENCY EXIT LIGHTS ON THE FORWARD SEAT PALLET ILLUMINATED. REMOVED AND REPLACED BATTERY PACK, TH EN LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 2001083100014 20010831 00014 WP 2001 8 31 ASAA0180226 1 20010722 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 974AS 53450 PDX - DURING PRE-FLIGHT CHECK, FUOND THE FIRST CALSS EMERGENCY FLOOR TRACK ILGHTS ILLUMINATED WITH LIGHT SWITCH AND BATT ERY ON AND OFF. COACH LIGHTS DID NOT ILLUMINATE. REPLACED BATTERY PACK AT B5-24. ALL LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001083100015 20010831 00015 NM 2001 8 31 USAA010939 1 20010725 A 5300 SKIN BOEING 757 757225 1384959 NM BS 605 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND FUSELAGE SKIN WITH PREVIOUSLY RECORDED LIGHTNING STRIKE, BS 605, BETWEEN S27R AND S28R. PREVIOUSLY INSTALLE D .25 INCH RIVET PER SRM 53-00-01, FIG 207. (M) 2 L 7 2 4F RT A2NM 2001083100016 20010831 00016 NM 2001 8 31 USAA010938 1 20010725 A 5330 SKIN BOEING 757 757225 1384959 NM BS 452 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND PREVIOUSLY RECORDED LIGHTNING STRIKE, BS 452, BETWEEN S24R AND S25R. PREVIOUSLY INSTALLED .25 INCH RIVET PE R SRM 53-00-01, FIG 207. (M) 2 L 7 2 4F RT A2NM 2001083100017 20010831 00017 NM 2001 8 31 USAA010937 1 20010725 A 5300 SKIN BOEING 757 757225 1384959 NM BS 430 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND PREVIOUSLY RECORDED LIGHTNING STRIKE, BS 430 BETWEEN S24R AND S25R. PREVIOUSLY INSTALLED .21875 INCH RIVET PER SRM 53-00-01, FIG 207. (M) 2 L 7 2 4F RT A2NM 2001083100018 20010831 00018 NM 2001 8 31 USAA010936 1 20010725 A 5330 SKIN BOEING 757 757225 1384959 NM BS 400 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND PREVIOUSLY RECORDED LIGHTNING STRIKE, BS 400 BETWEEN S25R AND S26R. PREVIOUSLY INSTALLED .21875 INCH RIVET PER SRM 53-00-01, FIG 207. (M) 2 L 7 2 4F RT A2NM 2001083100019 20010831 00019 WP 2001 8 31 AALA20011486 1 20010717 A 2100 ACM DOUG DC9 DC982 3022082 WP ACM BAY INOPERATIVE A AALA K O NONE OTHER J O WARNING INDICATION OTHER CR CRUISE 1 SW 21 225AA 49175 DFW - FLT 1318 - EN ROUTE DFW-DEN, WITH PACKS 'ON' SMOKE AND FUMES ENTERED CABIN WHEN TAKEOFF POWER APPLIED. SMOKE AND FUMES DISAPPEARED JUST PRIOR TO CRUISE ALTITUDE. LANDED DEN WITHOUT INCIDENT. EN ROUTE DEN-DFW WITH PACKS 'OFF', SMOKE AND FUMES ENTERED CABIN WHEN PACKS SELECTED 'ON'. SMOKE AND FUMES DISAPPEARED PRIOR TO REACHING CRUISE ALTITUDE. LAND ED DFW WITHOUT INCIDENT. REPLACED ACM AND LEFT AND RIGHT WATER SEPARATORS. ACCOMPLISHED PACK BURNOUT. NO ODOR, FUMES, SMOKE PRESENT. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001083100020 20010831 00020 WP 2001 8 31 AALA20011533 1 20010716 A 5300 LONGERON DOUG DC9 DC983 3022083 WP A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 438AA 49456 TUL - FOUND LONGERON 17 LEFT BENT AT BLIND FASTENER REPAIR AREA STATION 250 SKIN ALSO DENTED SAME AREA. CUT OUT DAMAGED SECTION OF LONGERON SPLICED IN NEW SECTION OF LONGERON WITH 2 SPLICES PER SRM 53-02 FIG 18 SHEET 1. SKIN REPAIRED ON E -58-3 9069497. (M) 2 L 7 2 4F RT A6WE 2001083100021 20010831 00021 WP 2001 8 31 AALA20011534 1 20010724 A 5300 FRAME DOUG DC9 DC983 3022083 WP FS 522 A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 438AA 49456 TUL - FOUND TWO WEAR MARKS IN FRAME STATION 522 BETWEEN LONGERON 23L AND 24L 5 INCH APART. TRIMMED OUT DAMAGED AREAS TW O OUT OF LIMITS, J-ANGLE .010 INCH 17.7 CRS HEAT TREAT TO TH1050 ATTACH WITH HI-LOCKS, INSTALLED DOUBLER PER ESO 80554 D ATED 7/19/2001. (M) 2 L 7 2 4F RT A6WE 2001083100022 20010831 00022 WP 2001 8 31 AALA20011535 1 20010713 A 5300 LONGERON DOUG DC9 DC983 3022083 WP FS 160 A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 438AA 49456 TUL - FOUND LONGERON 3L CRACKED AT OUTBOARD LEG AT FASTENER AFT SIDE OF STATION 160. INSTALLED SECTION OF LONGERON AND SPLICE PER SRM 53-02. (M) 2 L 7 2 4F RT A6WE 2001083100023 20010831 00023 WP 2001 8 31 AALA20011536 1 20010712 A 5300 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 1200-1210 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 438AA 49456 TUL - FOUND NR 1 SEAT TRACK CORRODED STATION 1200-1210. REMOVED DAMAGED AREA ON NR 1 SEAT TRACK AT STATION 1200-1210. INSTALLED SEAT TRACK PLUG, TREATED AND PRIMED PER SRM 51-10-3 AND 53-05 PAGE 4A. (M) 2 L 7 2 4F RT A6WE 2001083100024 20010831 00024 WP 2001 8 31 AALA20011537 1 20010712 A 5300 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 200-216 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 438AA 49456 TUL - FOUND CORROSION ON SEAT TRACKS NR 5 AT BS 200-216. INSTALLED STRAP PER AARD 53-20-00-13 AFTER REMOVAL OF CORROSIO N THEN TREATED, PRIMED AND PAINTED. (M) 2 L 7 2 4F RT A6WE 2001083100025 20010831 00025 WP 2001 8 31 AALA20011538 1 20010712 A 5300 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1190-1201 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 488AA 49681 TUL - FOUND NR 2 SEAT TRACK CORRODED STATION 1190-1201. REMOVED DAMAGED AREA OF NR 2 SEAT TRACK AT BS 1190-1201. INSTA LLED SEAT TRACK PLUG, TREATED AND PRIMED PER SRM 53-05 FIG 4A. (M) 2 L 7 2 4F A6WE 2001083100026 20010831 00026 WP 2001 8 31 AALA20011539 1 20010715 A 5300 SEAT TRACK DOUG DC9 DC983 3022083 WP FS 256 A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 438AA 49456 TUL - FOUND STATION 256 LEFT LOOSE HARDWARE UNDER SEAT TRACK FLANGE, FLANGE BENT/CRACKED, NR 1 SEAT TRACK. REPAIRED NR 1 SEAT TRACK AT STATION 256 LEFT WITH SPLICE REPAIR PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2001083100027 20010831 00027 WP 2001 8 31 AALA20011540 1 20010716 A 5300 SKIN DOUG DC9 DC983 3022083 WP FS 252 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 438AA 49456 TUL - FOUND LEFT FUSELAGE HAS DENT 1.5 INCHE BY 1.5 INCHE BY .0555 INCH ABOVE LAV SERVICE PANEL WITH POSSIBLE CRACK .8 I NCH LONGERON. CUT OUT DAMAGED AREA OF SKIN, CUT TITANIUM DOUBLER, INSTALLED INTERNAL FINGER DOUBLER PER SRM 53-04 FIG 3 8. (M) 2 L 7 2 4F RT A6WE 2001083100028 20010831 00028 2001 8 31 JBXA000300 4 20010704 A 3442 RADAR CNDAIR CL600 CL6002B19 EA NOSE CONTAMINATED A JBXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 05 587ML RADAR STOPPED PAINTING RETURNS MOMENTARY (RADAR FAULT MSG) THEN PAINTED FULL SCREEN PURPLE IN ALL MODES. INSPECTED RADA R COMPONENTS SOME WATER FOUND AROUND RADAR ANTENNA. OPERATIONAL CHECK GOOD IAW AMM 34-41-00. 2 L 7 2 4F RT A21EA 2001083100029 20010831 00029 EA 2001 8 31 JBXA000301 1 20010708 A 2760 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTIONED A JBXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 05 572ML 7224 ON TAKEOFF ROLL IN RDU GOT SPOILERON FAULT ON EICAS. REJECTED TAKEOFF. PULLED AND RESET C/B'S FOR SECU NR 1 AND 2 IAW CRJ FIM. PERFORMED OPERATIONAL CHECK OF SECU'S AND SPOILER SYSTEM IAW CRJ AMM 27-61-00 WITH DEFECTS NOTED AT THIS TIME. 2 L 7 2 4F RT A21EA 2001083100030 20010831 00030 EA 2001 8 31 JBXA000302 1 20010708 A 3610 CHECK VALVE CNDAIR CL600 CL6002B19 EA BLEED AIR SYS LEAKING A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 581ML 7303 LEFT 14TH STAGE DUCT OVERHEAT WARNING MESSAGE ON EICAS CLIMBING THROUGH 14,000. CLOSED LEFT 14TH STAGE VALVE AND OPENED ISOLATION VALVE IAW QRH PROCEDURES. FOUND 10TH STAGE LEAK SETTING OFF 14TH STAGE DUCT MESSAGE. REMOVED AND REPLACED 1 0TH STAGE GROUND AIR CONNECTION CHECK VALVE AND CLAMP IAW CRJ AMM 36-11-27. ALL OPS AND LEAK CHECKS GOOD IAW CRJ AMM 36 -12-00. 2 L 7 2 4F RT A21EA 2001083100031 20010831 00031 SO 2001 8 31 GLBA2001191 1 20010829 A 2800 5905587 FILTER EMB 120 EMB120ER 3260203 SO DIRTY A GLBA O OTHER O OTHER CR CRUISE 1 CE 01 299UX 279 120299 RIGHT FUEL FILTER ANNUCIATOR ILLUMINATED, REPLACED FUEL FILTER OPS CHECKED SYSTEM SATISFACTORY 2 L 7 2 4T RT A31SO 2001083100032 20010831 00032 NE 2001 8 31 JBXA000303 2 20010709 A 7261 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE LEFT LACK OF LUBE A JBXA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 SO 05 583ML 7327 LEFT ENGINE OIL TEMP WAS 168 DEGREES. AFTER RETARDING THROTTLE THE TEMP FELL TO 164 DEGREES. WITH THE THROTTLE AT FLIG HT IDLE THE OIL TEMP DROPPED TO 153 DEGREES. SERVICED NR 1 ENGINE OIL TO PROPER LEVEL IAW CRJ AMM 12-13-00. PERFORMED VISUAL INSPECTION FOR ANY VISUAL LEAKS. NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A21EA E15NE 2001083100033 20010831 00033 EA 2001 8 31 JBXA000304 1 20010709 A 3620 SENSING ELEMENT CNDAIR CL600 CL6002B19 EA BLEED AIR SYS DAMAGED A JBXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 05 581ML 7303 LEFT HAND 14TH STAGE DUCT WARNING CAME ON AFTER T/O. FERRIED AIRCRAFT BACK TO RDU. INSPECTED AND TROUBLESHOT 14TH STAG E SYSTEM AND FOUND PYLON SENSING ELEMENT DAMAGED. REMOVED AND REPLACED PYLON SENSING ELEMENT IAW CRJ AMM 36-21-04. PER FORMED ALL OPS CHECKS IAW CRJ AMM 36-21-00. ALL OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2001083100034 20010831 00034 EA 2001 8 31 JBXA000305 1 20010710 A 5270 WIRE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DAMAGED A JBXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 05 571ML 7209 INTERMITTENT PASSENGER DOOR HANDLE CAUTION IN FLIGHT AND ON LANDING. REPAIRED WIRE PS4MB-RED IAW CRJ AMM 52-70-00. PER FORMED OPERATIONAL CHECK IAW 52-70-04. ALL OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2001083100035 20010831 00035 EU 2001 8 31 JBXA000306 1 20010711 A 7931 APTE173RT1756 TRANSMITTER FOKKER F28 F28MK0100 4990807 EU NR 2 ENGINE FAULTY A JBXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 05 108ML 11484 AT 500 FT AFTER T/O AT TPA OIL PRESS LIMIT ENG NR 2 FAULTED. REMOVED AND REPLACED NR 2 ENG OIL PRESSURE TRANSMITTER IAW AMM 77-47-01. LEAK AND OPS CHECK GOOD. GROUND RAN NR 1 & 2 ENGINES TO TOGA (1171 EPR) POWER IAW AMM 71-00-00. NO FAU LTS NOTED. 2 L 7 2 4F RT 2001083100036 20010831 00036 EA 2001 8 31 JBXA000309 1 20010715 A 2810 PANEL CNDAIR CL600 CL6002B19 EA RT WING DEFECTIVE A JBXA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 05 587ML 7346 RIGHT & LEFT CROSSFLOW SHUTOFF VALVE CAUTION MESSAGE. REMOVED AND REPLACED REFUEL/DEFUEL PANEL IAW CL-65 AMM 28-25-16, OPS CHECKED GOOD. PERFORMED SATISFACTORY OPS TEST OF THE LEFT AND RIGHT CROSSFLOW SHUTOFF VALVES IAW CL-65 AMM 28-13-45 . 2 L 7 2 4F RT A21EA 2001083100037 20010831 00037 EA 2001 8 31 JBXA000310 1 20010720 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT ACTIVATED A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 577ML 7269 EN ROUTE TO ATLANTA, PASSENGER DOOR MESSAGE CAME ON, RAN CHECKLIST-MESSAGE PERSISTED. GROUND OPERATIONAL CHECK IAW CRJ AIRCRAFT MAINTENANCE MANUAL 52-11-00, GROUND OPERATIONAL CHECKED GOOD, NO DEFECT NOTED AT THIS TIME. 2 L 7 2 4F RT A21EA 2001083100038 20010831 00038 NE 2001 8 31 JBXA000311 2 20010720 A 7200 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE NR 2 FAILED A JBXA C ABORTED TAKEOFF J M WARNING INDICATION OVER TEMP TO TAKEOFF 1 SO 05 578ML 7270 GEE872224 NR 2 ENGINE OVERTEMPED BEFORE REACHING RATED TAKEOFF POWER. PERFORMED BORESCOPE INSP OF ENGINE IAW 72-00-00-290-02, 72- 00-00-290-03, 72-00-00-290-04, 72-00-00-290-05. FAILED INSPECTION, REMOVED AND REPLACED ENGINE IAW 71-00-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2001083100039 20010831 00039 EA 2001 8 31 JBXA000314 1 20010810 A 3620 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA BLEED AIR SYS ACTIVATED A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 573ML 7227 ON TRANSFER OF BLEEDS FROM APU TO ENGINE CAUTION MESSAGE, L-PACK HI PRESSURE FOLLOWED. QUICK REFERENCE MANUAL CAUTION S TILL PERSISTED AIRCRAFT COMPLETELY DEPRESSURIZED. PERFORMED OPERATIONAL CHECK OF AIR CONDITIONING SYSTEM WITH 2 PACKS; OPS CHECK NORMAL IAW CRJ AMM CH 21-51-00. 2 L 7 2 4F RT A21EA 2001083100040 20010831 00040 EA 2001 8 31 JBXA000316 1 20010819 A 4990 APU CNDAIR CL600 CL6002B19 EA APU BAY LACK OF LUBE A JBXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 05 574NL 7242 APU OIL PRESS MESSAGE IN FLIGHT. LANDED AT KDCA IAW QRH; T/S PER FIM 49-60-00. FOUND OIL QUANTITY LOW. FILLED TANK AS REQUIRED, CKECKS OK. 2 L 7 2 4F RT A21EA 2001083100041 20010831 00041 NM 2001 8 31 CALA0100823 1 20010829 A 5330 SKIN BOEING 737 737524 1384721 NM STA 990 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19634 26319 INSPECTION FOUND FUSELAGE SKIN DENTED AND GOUGED AFT OF R-2 DOOR AT STA 990 BETWEEN S14R AND 15R. A DOUBLER WAS INSTALLE D IAW SRM 53-00-01. 2 L 7 2 4F RT A16WE 2001083100042 20010831 00042 WP 2001 8 31 CALA0100824 1 20010831 A 5313 LONGERON DOUG DC9 DC982 3022082 WP STA 1231 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND LONGERON 23R CORRODED IN AFT CARGO COMPARTMENT AT STA 1231. THE LONGERON WAS REPAIRED IAW SRM 53-02, FI GURE 18. 2 L 7 2 4F A6WE 2001083100043 20010831 00043 WP 2001 8 31 CALA0100825 1 20010831 A 5320 PAN DOUG DC9 DC982 3022082 WP FWD CARGO DR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND FORWARD CARGO DOOR FRAME PAN CORRODED AROUND 10 EACH NUTS. THE PAN AND SPLICES WERE REMOVED IAW SRM 53- 05, FIGURE 44. A NEW PAN AND SPLICE WERE INSTALLED IAW SRM 53-05, FIGURE 44. 2 L 7 2 4F A6WE 2001083100044 20010831 00044 SO 2001 8 31 LR7A01058 1 20010805 A 5330 SKIN LKHEED 382 382G 526414U SO FUSELAGE DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2167 4763 DURING SCHEDULED C2 INSPECTION PER JOB CARD HC5303 FOUND RT FS 869 - 935 FUSELAGE SKIN WITH A HIGH DENSITY OF PREVIOUS REPAIRS AT RBL 61, WL 194-254. REPAIRED IAW LAC MEA 382-53-01-048. 2 H 7 4 4T A1SO 2001083100045 20010831 00045 EU 2001 8 31 MALA010603 1 20010801 A 2432 40787 BATTERY SAAB SF340 SF340A 7850100 EU LT & RT DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 110XJ 340A110 DURING FLIGHT 2831, CREW REPORTED NO BATTERY START LIGHT WAS ON. AIR TURNBACK TO MSP. MAINTENANCE REMOVED AND REPLACED LT & RT BATTERY LT P/N 4078-7 SN/ON GO2561, RT P/N 4078-7 SN/ON EO2584 IAW TASK CARD 243401. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2001083100046 20010831 00046 2001 8 31 MALA010604 4 20010801 A 3425 6226190113 COMPUTER SAAB SF340 340B 7860101 EU E/E BAY FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 403XJ 340B403 DURING FLIGHT NR 2820, RT AHARS COMPUTER FAILED. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED NR 2 AHRS COMPUTE R P/N 622-6190-113, S/N ON 2247, S/N OFF 2788, SYSTEM OPS CHECK GOOD IAW SF340 MM CHAPTER 34. 2 L 7 2 4T RT A52EU 2001083100047 20010831 00047 NE 2001 8 31 MALA010606 2 20010731 A 7210 GEARBOX SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE MAKING METAL A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 447XJ 340B447 DURING FLIGHT 2759, LT CHIP DETECT LIGHT ILLUMINATED IN FLIGHT. AIR RETURN TO MSP. MAINTENANCE POWER UNIT AND PGB WAS REMOVED AND REPLACED REF WORK PACKAGE DATED 7-31-01 AND COMPLETED WORK PACKAGE JOB CARD 7910-303.. 2 L 7 2 4T 4 T RT A52EU E8NE 2001083100048 20010831 00048 EU 2001 8 31 MALA010609 1 20010802 A 7921 4504473 OIL COOLER BAC 146 AVRO146RJ85A 1500097 EU ENGINE DAMAGED A MALA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 508XJ E2318 DURING ENGINE SHUTDOWN ON AC 508, WITH APU OPERATING, PAX , F/A'S REPORTED SMOKE IN CABIN. SHUTDOWN ENGINE. MAINTENANC E REMOVED AND REPLACED DAMAGED OIL COOLER INTAKE DUCT P/N OFF 4501709, P/N ON 4504473 REF NR 409 116560. FOUND APU OIL OVER-SERVICED BY 1 QUART, BROUGHT OIL TO PROPER LEVEL. OPS AND CABIN SMELL CHECKS GOOD AT THIS TIME. REMOVED FROM DMR- MXC NOTIFIED. 2 H 7 4 4F RT A49EU 2001083100049 20010831 00049 EU 2001 8 31 MALA010611 1 20010526 A 7603 AS103 PULLEY BAC 146 AVRO146RJ85A 1500097 EU NR 3 ENGINE BROKEN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 506XJ E2314 FOUND DURING C-CHECK IN CVG, NR 3 ENGINE THRUST CONTROL CABLE PULLEY BROKEN IN PYLON. MAINTENANCE REPLACED PULLEY P/N A S103, RE-RIGGED THRUST CONTROL COMPENSATOR IAW AMM 76-11-00. 2 H 7 4 4F RT A49EU 2001083100050 20010831 00050 EU 2001 8 31 MALA010612 1 20010508 A 5330 SKIN BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 506XJ E2314 DURING C-CHECK IN CVG, NOTED DENTS ON LT FUSELAGE SKIN BETWEEN FRAMES 19 & 20, BELOW CABIN WINDOW. REQUIRES RE-INSPECT AND RE-PLOT EVERY 300 CYCLES PER MSP QC 2916. MAINTENANCE REPAIRED SKIN DAMAGE. PERMANENT REPAIR AT NEXT C-CHECK, REF E A01-99194. MAINTENANCE REPAIRED SKIN DAMAGE IAW EO A53045. 2 H 7 4 4F RT A49EU 2001083100051 20010831 00051 EU 2001 8 31 MALA010613 1 20010511 A 7110 HC716H9025000 STIFFENER BAC 146 AVRO146RJ85A 1500097 EU NR 1 COWLING CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 506XJ E2314 FOUND DURING C-CHECK IN CVG, NR 1 ENGINE NOSE COWL FWD BULKHEAD HAS FOUR CRACKED STIFFENERS (4, 16, 17, 32). MAINTENANC E REPLACED STIFFENERS IAW SRM 51-42-00 AND INSTALLED NEW FASTENERS P/N HC716H9025-000, IAW SRM 51-43-00. 2 H 7 4 4F RT A49EU 2001083100052 20010831 00052 EU 2001 8 31 MALA010614 1 20010511 A 7110 STIFFENER BAC 146 AVRO146RJ85A 1500097 EU NR 2 COWLING CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 506XJ FOUND DURING C-CHECK IN CVG, NR 2 ENGINE NOSE COWL FWD BULKHEAD HAS NINE CRACKED STIFFENERS (3, 4, 7, 10, 19, 27, 28, 32 , 33). MAINTENANCE INSTALLED NEW STIFFENERS IAW SRM 54-10-11 201. 2 H 7 4 4F RT A49EU 2001083100053 20010831 00053 EU 2001 8 31 MALA010615 1 20010511 A 7110 HC716H9025000 STIFFENER BAC 146 AVRO146RJ85A 1500097 EU NR 3 COWLING CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 506XJ E2314 FOUND DURING C-CHECK IN CVG, NR 3 ENGINE NOSE COWL FWD BULKHEAD HAS FOURTEEN CRACKED STIFFENERS. (4, 5, 6, 7, 10, 12, 16 , 19, 26, 27, 28, 29, 31, 33). MAINTENANCE REPAIRED STIFFENERS IAW SRM 51-42-00, AND INSTALLED FASTENERS P/N HC716H9025 -000 IAW SRM 51-43-00. 2 H 7 4 4F RT A49EU 2001083100054 20010831 00054 EU 2001 8 31 MALA010616 1 20010511 A 7110 BAEREF000025461 STIFFENER BAC 146 AVRO146RJ85A 1500097 EU NR 4 COWLING CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 506XJ E2314 FOUND DURING C-CHECK IN CVG, NR 4 ENGINE NOSE COWL FWD BULKHEAD HAS THREE STIFFENERS CRACKED (3, 27, 32). MAINTENANCE R EPLACED 3 STIFFENERS P/N BAEREF-000025461 IAW BAB SRM 54-10-11 201 IAW SRM 51-42-00. 2 H 7 4 4F RT A49EU 2001083100055 20010831 00055 EU 2001 8 31 MALA010617 1 20010616 A 5730 SKIN BAC 146 AVRO146RJ85A 1500097 EU LT WING CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 505XJ E2313 DURING C-CHECK IN CVG, WHILE REMOVING LT I/B LEADING EDGE NOTICED CRACK ON INNER SKIN INBOARD SIDE APPROXIMATELY 13.8 IN CH FROM EDGE AND APPROXIMATELY 1 INCH LONG. MAINTENANCE REPAIRED CRACK IN LT I/B LEADING EDGE IAW RICHC579H9114 PER BAE SYSTEMS. 2 H 7 4 4F RT A49EU 2001083100056 20010831 00056 2001 8 31 COMA0110137 4 20010829 A 3420 62261902004 COMPUTER EMB 120 EMB120RT SO AVIONICS BAY FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 463CA 19503 1267 FLIGHT #5005. DURING TAXI OUT RECEIVED A HEADING COMPUTER WARNING, AIRCRAFT RETURNED TO THE GATE.REPLACED THE AHC-85. 2 L 7 2 4T RT A31SO 2001083100057 20010831 00057 EU 2001 8 31 MALA010620 1 20010531 A 7110 HC716H9025000 STIFFENER BAC 146 AVRO146RJ85A 1500097 EU NR 3 COWLING CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 505XJ E2313 FOUND DURING C-CHECK IN CVG, NR 3 NOSE COWL HAS FWD BULKHEAD STIFFENERS CRACKED FIVE TOTAL (4, 6, 17, 22, 33). MAINTENA NCE REMOVED STIFFENER'S 4, 6, 17, 22, 33, IAW SRM 54-10-11. FABRICATED STIFFENER'S 4, 6, 17, 22, 33 AND REPLACED STIFFE NERS 4, 6, 17, 22, 33 P/N HC716H9025-000. 2 H 7 4 4F RT A49EU 2001083100058 20010831 00058 EU 2001 8 31 MALA010621 1 20010531 A 7110 HC716H9025000 STIFFENER BAC 146 AVRO146RJ85A 1500097 EU NR 2 COWLING CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 505XJ E2313 DURING C-CHECK IN CVG, NR 2 COWL FWD BULKHEAD HAS ELEVEN CRACKED STIFFENERS, (3, 12, 13, 14, 16, 17, 19, 27, 28, 29, 32) . MAINTENANCE REMOVED AND REPLACED 11 CRACKED STIFFENERS IN NR 2 NOSE COWL FWD BULKHEAD NR 3, 12, 13, 14, 16, 17, 19, 2 7, 28, 29, 32 WITH BULK STIFFENERS P/N HC716H9025-000 AND P/N HC716H0022-210 IAE BAE SRM 54-10-11-201 AND BAE SRM 51-41- 00-1. 2 H 7 4 4F RT A49EU 2001083100059 20010831 00059 EA 2001 8 31 COMA0160656 1 20010829 A 5346 601350061 WEB CNDAIR NA CNDAIR CL600 CL6002B19 EA ENGINE SUPPORT B CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 926CA 18356 NA 7027 ENGINE SUPPORT BEAM CRACKED ON TOP CENTER SKIN 1 1/2" LONG.REPAIRED ENGINE SUPPORT BEAM I/A/W REO 601R-53-61-345B. 2 L 7 2 4F RT A21EA 2001083100060 20010831 00060 EA 2001 8 31 COMA0110138 1 20010830 A 5210 DOOR CNDAIR CL600 CL6002B19 EA A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 259CA 1252 FLIGHT #5017. DURING TAXI OUT FLIGHT ATTENDANT NOTICED LIGHT SHOWING THROUGH BETWEEN CABIN DOOR AND DOOR FRAME, AIRCRAF T RETURNED TO THE GATE.RE-SHIMMED CABIN DOOR SEAL. 2 L 7 2 4F RT A21EA 2001083100061 20010831 00061 EU 2001 8 31 MALA010623 1 20010531 A 7110 HC716H9025000 STIFFENER BAC 146 AVRO146RJ85A 1500097 EU NR 4 COWLING CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 505XJ E2313 FOUND DURING C-CHECK IN CVG, NR 4 ENGINE NOSE COWL FWD BULKHEAD HAS FOUR STIFFENERS CRACKED (3, 19, 32, 33). MAINTENANC E REMOVED AND REPLACED 4 EACH 3, 9, 32, 33 STIFFENERS P/N HC716H9025-000 IAW SRM 54-10-11. 2 H 7 4 4F RT A49EU 2001083100062 20010831 00062 EA 2001 8 31 COMA0160657 1 20010829 A 2510 DOOR CNDAIR CL600 CL6002B19 EA A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 710CA 7241 FLIGHT #5967. DURING TAXI OUT DISCOVERED THAT THE COCKPIT DOOR WOULD NOT LATCH, AIRCRAFT RETURNED TO THE GATE.REPLACED THE COCKPIT DOOR ASSEMBLY. 2 L 7 2 4F RT A21EA 2001083100063 20010831 00063 EU 2001 8 31 MALA010624 1 20010610 A 5330 SKIN BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 505XJ E2313 DURING C-CHECK IN CVG, REPAIR FUSELAGE SKIN DAMAGE AT FRAME 20 AT STRINGER 18. MAINTENANCE PERFORMED REPAIRS IAW BAE SR M 53-00-12/201. 2 H 7 4 4F RT A49EU 2001083100064 20010831 00064 EU 2001 8 31 MALA010625 1 20010610 A 5330 SKIN BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 505XJ E2313 DURING C-CHECK IN CVG, REPAIR FUSELAGE SKIN DAMAGE AT FRAME 20, STRINGER 21. MAINTENANCE PERFORMED REPAIRS IAW BAE SRM 53-00-12/201. 2 H 7 4 4F RT A49EU 2001083100065 20010831 00065 EU 2001 8 31 MALA010626 1 20010615 A 3520 17408543 LINE BAC 146 AVRO146RJ85A 1500097 EU OXYGEN SYS BROKEN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 505XJ E2313 DURING C-CHECK IN CVG, WHILE STOWING OXYGEN MASKS FOUND LINE BROKEN AT CHECK VALVE AT SEAT 2A/B. MAINTENANCE REPLACED M ASK AND LINE ASSEMBLY P/N 174085-43 AT SEAT 2A/B IAW AMM 35-20-31. 2 H 7 4 4F RT A49EU 2001083100066 20010831 00066 EU 2001 8 31 MALA010627 1 20010615 A 3520 17408543 LINE BAC 146 AVRO146RJ85A 1500097 EU OXYGEN SYS BROKEN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 505XJ E2313 DURING C-CHECK IN CVG, WHILE STOWING OXYGEN MASK, FOUND LINE BROKEN AT CHECK VALVE AT SEAT 8 D/E/F. MAINTENANCE REPLACE D MASK ASSEMBLY P/N 174085-43, AMM 35-20-31 AT SEAT 8 D/E/F. 2 H 7 4 4F RT A49EU 2001083100067 20010831 00067 EA 2001 8 31 COMA0160659 1 20010829 A 3260 16600101 UPLOCK CNDAIR CL600 CL6002B19 EA NOSE ALNDING GEA FAULTY A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 918CA 19503 7018 FLIGHT #5266. SHORTLY AFTER TAKE OFF RECEIVED A NOSE LANDING GEAR DISAGREE LIGHT, AIRCRAFT RETURNED TO THE FIELD.REPLAC ED THE NOSE LANDING GEAR UPLOCK ASSEMBLY. 2 L 7 2 4F RT A21EA 2001083100068 20010831 00068 NM 2001 8 31 AWXA0002206 1 20010729 A 5313 65163007 WEB BOEING 737 73733A 1384673 NM BS 178 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 D: BS 178 Blkhd web fwd side RBL 4.8 WL 197 crack emenating from beneath strap.C: Cut out damaged area and installed dou bler IAW B737-300 SRM 53-10-08 pgs 286-291 2 L 7 2 4F RT A16WE 2001083100069 20010831 00069 EU 2001 8 31 MALA010628 1 20010621 A 5512 SKIN BAC 146 AVRO146RJ85A 1500097 EU HORIZ STAB DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 505XJ E2313 DURING C-CHECK IN CVG, PERFORM REPAIR TO RT STAB LOWER SKIN IAW BAE RIC HC551H9052. MAINTENANCE REMOVED DAMAGE TO RT ST AB LOWER SKIN; MANUFACTURED, ALODINE, PRIMED, PAINTED AND INSTALLED REPAIR PARTS FOR RT STAB IAW BAE RIL HC551H9052; SRM 'S 51-20-11, 51-42-00, 51-43-00. 2 H 7 4 4F RT A49EU 2001083100070 20010831 00070 EU 2001 8 31 MALA010629 1 20010720 A 2730 7227105712 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 436XJ 340B436 DURING 4K-CHECK IN CWA, LT O/B ELEVATOR CABLE IS CHAFED. MAINTENANCE REMOVED AND REPLACED LT O/B FWD FUSELAGE ELEVATOR CABLE P/N 7227105-712/711, SN/PEG2SFEX. 2 L 7 2 4T RT A52EU 2001083100071 20010831 00071 EU 2001 8 31 MALA010630 1 20010720 A 2730 7227105644 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 436XJ 340B436 FOUND DURING 4K-CHECK IN CWA, LT I/B ELEVATOR CABLE CHAFED. MAINTENANCE REPLACED LT I/B FWD FUSELAGE ELEVATOR CABLE P/N 7227105-644, S/N PEG2SFEX, IAW SAAB AMM 27-31-15-4. 2 L 7 2 4T RT A52EU 2001083100072 20010831 00072 EU 2001 8 31 MALA010631 1 20010720 A 2730 7227105712 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 436XJ 340B436 FOUND DURING 4K-CHECK IN CWA, RT O/B FWD FUSELAGE ELEVATOR CABLE CHAFED. MAINTENANCE INSTALLED RT O/B FWD ELEVATOR CABL E P/N 7227105-712, IAW SF3 AMM 27-31-15. 2 L 7 2 4T RT A52EU 2001083100073 20010831 00073 EU 2001 8 31 MALA010632 1 20010720 A 2730 7227105644 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 436XJ 340B436 FOUND DURING 4K-CHECK IN CWA, RT I/B FWD FUSELAGE ELEVATOR CABLE CHAFED. MAINTENANCE INSTALLED RT I/B FWD FUSELAGE ELE VATOR CABLE P/N 7227105-644, S/N PEG2SFEX IAW SF3 AMM 27-31-15. 2 L 7 2 4T RT A52EU 2001083100074 20010831 00074 EU 2001 8 31 MALA010633 1 20010721 A 2710 7227105624 CONTROL CABLE SAAB SF340 340B 7860101 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 436XJ 340B436 FOUND DURING 4K-CHECK IN CWA, RT O/B FWD AILERON CABLE CHAFED. MAINTENANCE REPLACED RT O/B FWD AILERON CABLE P/N 722710 5-624, S/N PEG3SFEX, IAW SAAB AMM 27-11-25. 2 L 7 2 4T RT A52EU 2001083100075 20010831 00075 EU 2001 8 31 MALA010634 1 20010721 A 2710 7227105614 CONTROL CABLE SAAB SF340 340B 7860101 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 436XJ 340B436 FOUND DURING 4K-CHECK IN CWA, RT I/B FWD AILERON CABLE CHAFED. MAINTENANCE REPLACED RT I/B FWD AILERON CABLE P/N 722710 5-614, S/N PEG2SFEX IAW SAAB AMM 27-11-25. 2 L 7 2 4T RT A52EU 2001083100076 20010831 00076 EU 2001 8 31 MALA010635 1 20010721 A 2710 7227105611 CONTROL CABLE SAAB SF340 340B 7860101 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 436XJ 340B436 FOUND DURING 4K-CHECK IN CWA, LT O/B FWD FUSELAGE AILERON CABLE CHAFED. MAINTENANCE REPLACED LT O/B FWD FUSELAGE AILERO N CABLE P/N 7227105-611, S/N PEG2SFEX IAW SF3 AMM 27-11-25. 2 L 7 2 4T RT A52EU 2001083100077 20010831 00077 EU 2001 8 31 MALA010636 1 20010721 A 2710 7227105623 CONTROL CABLE SAAB SF340 340B 7860101 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 436XJ 340B436 FOUND DURING 4K-CHECK IN CWA, LT I/B FWD AILERON CABLE CHAFED. MAINTENANCE REPLACED LT I/B FWD FUSELAGE AILERON CABLE P /N 7227105-623, S/N PEG2SFEX, IAW SF3 AMM 27-11-25. 2 L 7 2 4T RT A52EU 2001083100078 20010831 00078 EU 2001 8 31 MALA010638 1 20010725 A 2720 7227105562 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 436XJ 340B436 FOUND DURING 4K-CHECK IN CWA, RT O/B CIRCUIT 1 RUDDER CABLE DUAL CHAFED. MAINTENANCE INSTALLED SERVICEABLE RT O/B CIRCU IT 1 RUDDER CABLE P/N 7227105-562 IAW SF340 AMM 27-21-25. 2 L 7 2 4T RT A52EU 2001083100079 20010831 00079 EU 2001 8 31 MALA010639 1 20010723 A 2720 7227105571 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 436XJ 340B436 FOUND DURING 4K-CHECK IN CWA, RT I/B FWD FUSELAGE CIRCUIT 1 RUDDER CABLE CHAFED. MAINTENANCE REMOVED AND INSTALLED RT I /B FWD FUSELAGE CIRCUIT 1 DUAL RUDDER CABLE P/N 7227105-571 IAW SAAB AMM 27-21-25-4. 2 L 7 2 4T RT A52EU 2001083100080 20010831 00080 EU 2001 8 31 MALA010640 1 20010723 A 2720 7227105571 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 436XJ 340B436 FOUND DURING 4K-CHECK IN CWA, LT I/B FWD FUSELAGE CIRCUIT 1 DUAL RUDDER CABLE CHAFED. MAINTENANCE REMOVED AND INSTALLED LT I/B FWD FUSELAGE CIRCUIT 1 DUAL RUDDER CABLE P/N 7227105-571 IAW SAAB AMM 27-21-25-4. 2 L 7 2 4T RT A52EU 2001083100081 20010831 00081 EU 2001 8 31 MALA010641 1 20010723 A 2720 7227105562 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 436XJ 340B436 FOUND DURING 4K-CHECK IN CWA, LT O/B FWD FUSELAGE CIRCUIT 1 DUAL RUDDER CABLE CHAFED. MAINTENANCE REMOVED AND INSTALLED LT O/B FWD FUSELAGE CIRCUIT 1 DUAL RUDDER CABLE P/N 7227105-562 IAW SAAB AMM 27-21-25-4. 2 L 7 2 4T RT A52EU 2001083100082 20010831 00082 EU 2001 8 31 MALA010642 1 20010723 A 2720 7227105582 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 436XJ 340B436 FOUND DURING 4K-CHECK IN CWA, AFT FUSELAGE CIRCUIT 1 SINGLE LT RUDDER CABLE CHAFED. MAINTENANCE AND INSTALLED AFT FUSEL AGE CIRCUIT 1 SINGLE LT RUDDER CABLE P/N 7227105-582 IAW SAAB AMM 27-21-25-4. 2 L 7 2 4T RT A52EU 2001083100083 20010831 00083 EA 2001 8 31 COMA0160660 1 20010829 A 3040 WINDOW CNDAIR CL600 CL6002B19 EA A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 946CA 7072 FLIGHT #6015. DURING TAXI OUT RECEIVED A LEFT WINDOW AND LEFT WINDSHIELD OVERHEAT CAUTION MESSAGE, AIRCRAFT RETURNED TO THE GATE.COOLED SUN HEATED WINDOWS WITH COLD WATER. 2 L 7 2 4F RT A21EA 2001083100084 20010831 00084 EU 2001 8 31 MALA010644 1 20010809 A 2613 WARNING SYSTEM SAAB SF340 340B 7860101 EU COCKPIT MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 451XJ 340B451 ON FLIGHT 3219 OUT OF SUX, LEFT TAILPIPE HOT LIGHT ILLUMINATED AFTER TAKEOFF. MEMORY ITEMS COMPLETED. QRH'D AND LIGHT WENT OUT ON RETURN TO SUX. AIR TURNBACK TO SUX. MAINTENANCE INSPECTED LT AFT TAILPIPE ASSEMBLY. NO DEFECT NOTED. CLE ANED AND REST CANNON PLUGS AND PERFORMED GROUND RUN WITH NO DISCREPANCIES. AIRCRAFT OK FOR CONTINUED SERVICE. 2 L 7 2 4T RT A52EU 2001083100085 20010831 00085 EA 2001 8 31 COMA0160661 1 20010829 A 5270 ROD CNDAIR CL600 CL6002B19 EA A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 973CA 7146 FLIGHT #5219. DURING CLIMB-OUT OF CVG RECEIVED A CABIN DOOR OUTER HANDLE CAUTION MESSAGE, AIRCRAFT RETURNED TO THE FIEL D.PERFORMED RIGGING OF THE CABIN DOOR OUTER HANDLE PUSH-PULL-ROD. 2 L 7 2 4F RT A21EA 2001083100086 20010831 00086 EU 2001 8 31 MALA010646 1 20010812 A 3230 CONTROL VALVE SAAB SF340 340B 7860101 EU LANDING GEAR FAILED A MALA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 453XJ 340B453 DURING FLIGHT 3089, ON APPROACH INTO LEX, LANDING GEAR WOULD NOT COME DOWN. COMPLETED QRH, GEAR WOULD NOT COME DOWN WIT H GEAR EXTENSION HANDLE. HAD TO USE EMERGENCY GEAR EXTENSION T-HANDLE, THEN THREE GREEN DOWN AND LOCKED INDICATION. AC DIVERTED TO CVG. MAINTENANCE INSTALLED SERVICEABLE LANDING GEAR CONTROL VALVE AND SEPARATION BOLTS. SEE 409, 116601 FO R FURTHER DETAIL. 2 L 7 2 4T RT A52EU 2001083100087 20010831 00087 2001 8 31 MALA010647 4 20010814 A 3425 6226190113 COMPUTER SAAB SF340 SF340A 7850100 EU E/E BAY FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 110XJ 340A110 DURING FLIGHT 3372 AFTER TAKEOFF, YD OR AUTO-PILOT WOULD NOT STAY ENGAGED. F/O'S ADI SHOWED 8 DEGREE BANK TO LEFT IN ST RAIGHT AND LEVEL. AIR RETURN TO MSP. MAINTENANCE REPLACED NR 2 AHRS COMPUTER P/N 622-6190-113, S/N OFF 9285, S/N ON 24 8. NR 2 AHRS, OPS CHECKS GOOD IAW SF340 MM CHAP 34. 2 L 7 2 4T RT A52EU 2001083100088 20010831 00088 EA 2001 8 31 COMA0160662 1 20010829 A 7331 73664310 COMPUTER CNDAIR CL600 CL6002B19 EA AVIONICS BAY FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 927CA 13279 96 7031 FLIGHT #5553. DURING TAXI OUT RECEIVED A FUEL CHANNEL #2 FAIL STATUS MESSAGE, AIRCRAFT RETURNED TO THE GATE.REPLACED TH E FUEL COMPUTER. 2 L 7 2 4F RT A21EA 2001083100089 20010831 00089 EU 2001 8 31 MALA010650 1 20010818 A 3320 6524001 BALLAST SAAB SF340 340B 7860101 EU CABIN DEFECTIVE A MALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 15 410XJ 340B410 DURING FLIGHT 3004 AFTER DEPARTURE F/A CALLED TO NOTIFY MX OF SMOKE SMELL LIKE BURNING PLASTIC RETURNED TO RHI. NO VISI BLE SMOKE BUT SMELL NOTICED. AIR TURNBACK TO RHI. MAINTENANCE FOUND BALLAST 130LHF INOP. NOTED BURNT SMELL REMOVED AN D REPLACED P/N 65-24-001. OPS CHECK GOOD. RAN AVIONICS LIGHTS RECIRCULATION FAN FOR 30 MINUTES. NO SMOKE OR SMELL NOT ED BORESCOPED INLETS NO DEBRIS NOTED. CHECKED BLEED LINES ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2001083100090 20010831 00090 EU 2001 8 31 MALA010651 1 20010818 A 3234 D49412001 CONTROL HANDLE SAAB SF340 SF340A 7850100 EU COCKPIT DEFECTIVE A MALA O OTHER J WARNING INDICATION DE DESCENT 1 GL 15 102XJ 340A102 IN FLIGHT FROM ROA TO DTW, ON FLIGHT 2736, OVER CLE ON DESCENT THE GEAR UNSAFE LIGHT CAME ON, FOLLOWING QRH THE SITUATIO N DID NOT CHANGE, AFTER RECYCLING BREAKERS THE GEAR WENT DOWN, LEFT GEAR DOWN FOR REST OF FLIGHT. MAINTENANCE REPLACED LANDING GEAR CONTROL HANDLE PER SAAB MM PERFORMED SEVERAL GEAR SWINGS. ALL CHECKS GOOD. S/N ON 627/01-97, S/N OFF 632/ 03-97, P/N D494-12-001. 2 L 7 2 4T RT A52EU 2001083100091 20010831 00091 EU 2001 8 31 MALA010652 1 20010819 A 3260 LIGHT SAAB SF340 SF340A 7850100 EU COCKPIT INOPERATIVE A MALA K NONE N FALSE WARNING LD LANDING 1 GL 15 115XJ DURING FLIGHT 2745 INTO GRB, NOSE WHEEL INDICATOR (DOWN GREEN INDICATOR) NOT ILLUMINATED WHEN GEAR IS SELECTED DOWN. EX CHANGED BULBS, CYCLED GEAR, ETC. TOWER CONFIRMED GEAR DOWN, LANDED NORMALLY APPEARS TO BE INDICATOR PROBLEM. MAINTENAN CE RELAMPED NOSE LANDING GEAR INDICATOR AS NEEDED. 2 L 7 2 4T RT A52EU 2001083100092 20010831 00092 2001 8 31 MALA010653 4 20010819 A 3425 6226190113 COMPUTER SAAB SF340 340B 7860101 EU E/E BAY MALFUNCTIONED A MALA K NONE J WARNING INDICATION CL CLIMB 1 GL 15 444XJ 340B444 DURING FLIGHT 2730 CAPT AHRS COMPUTER FAILED AFTER DEPARTURE FROM DTW. HDG RED FLAG ON LT AND RT EFIS, IN FLIGHT. XSID E DATA CLEARED FLAG, BUT EFIS/COMPASS OFF 15 DEGREES. ALSO FLAG ON RIGHT RMI. MAINTENANCE CND ON GROUND. REPLACED NR 1 AHRS COMPUTER FOR PRECAUTION. P/N 622-6190-113, S/N OFF 933, S/N ON 277. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2001083100093 20010831 00093 2001 8 31 MALA010654 4 20010819 A 2565 D31050105 SLIDE BAC 146 AVRO146RJ85A 1500097 EU CABIN DEPLOYED A MALA K NONE O OTHER NR NOT REPORTED 1 GL 15 503XJ E2310 ON FLIGHT NR 3544, FWD LT SLIDE DEPLOYED. MAINTENANCE REPLACED FWD PAX DOOR EVAC SLIDE P/N D31050-105, S/N ON 1419 IAW AMM 25-60-11, OPS AND SECURITY CHECK GOOD. 2 H 7 4 4F RT A49EU 2001083100094 20010831 00094 EU 2001 8 31 MALA010655 1 20010821 A 7933 4053T73P01 PROBE SAAB SF340 SF340A 7850100 EU LT ENGINE DEFECTIVE A MALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 15 110XJ 340A110 DURING FLIGHT NR 3354, LT PROP OIL TEMP FLUCTUATES. AIR RETURN TO DTW. MAINTENANCE REPLACED LT ENGINE OIL TEMP PROBE I AW GE MM CHAP 79. REPLACED LT ENGINE OIL TEMP/PRESS INDICATOR IAW SAAB AMM CH 77. PERFORMED GROUND RUNS. ALL INDICATI ONS NORMAL OIL QUANTITY CHECK GOOD. ENG OIL TEMP PROBE P/N 4053T73P01, S/N ON EGNAB451. ENG OIL INDICATOR P/N 522794, S/N ON 06871426. 2 L 7 2 4T RT A52EU 2001083100095 20010831 00095 EU 2001 8 31 MALA010656 1 20010813 A 2910 HYDRAULIC LINE BAC 146 AVRO146RJ85A 1500097 EU HYDRAULIC SYS LEAKING A MALA K NONE B P SMOKE/FUMES/ODORS/SPARKS NO WARNING INDICATION NR NOT REPORTED 1 GL 15 501XJ E2208 STRONG GAS/OIL SMELL IN CABIN. MAINTENANCE FOUND HYDRAULICS BAY HAD A HYDRAULIC LEAK. MAINTENANCE INSPECTED AC AND FOUN D SAFE FOR DSM TO DTW. DTW MAINTENANCE REPLACED LEAKING LINE AT ANTI-SKID VALVE IAW 32/20 ALL CHECKS GOOD. SERVICED AS REQUIRED. 2 H 7 4 4F RT A49EU 2001083100096 20010831 00096 NE 2001 8 31 MALA010657 2 20010819 A 7200 ENGINE SAAB SF340 340B 7860101 EU LYC LF507 LF5071F NE NR 2 FAILED A MALA E ENGINE SHUTDOWN J M WARNING INDICATION OVER TEMP CL CLIMB 1 GL 15 456XJ 340B456 RT ENGINE INFLIGHT SHUTDOWN. CREW HEARD LOUD POPPING SOUND FROM RT ENGINE DURING CLIMBOUT. REDUCED POWER TO 20-30 PERC ENT ITT CONTINUED TO INCREASE, BUT OVERTEMP LIGHT PROCEEDED TO ACCOMPLISH ENGINE SHUTDOWN. MAINTENANCE COMPLETED WORK P ACKAGE DATED 8/18/01. REMOVED AND REPLACED NR 2 ENGINE. OPS AND LEAK CHECK GOOD. 2 L 7 2 4T 4 F RT A52EU E6NE 2001083100097 20010831 00097 EU 2001 8 31 MALA010659 1 20010827 A 7931 522794 INDICATOR SAAB SF340 340B 7860101 EU COCKPIT FAULTY A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 413XJ 340B413 DURING FLIGHT 2745, LT ENGINE OIL PRESSURE FLUCTUATES AT HIGH POWER SETTING BETWEEN 25-70 PSI. AIR TURNBACK TO MSP. MA INTENANCE REPLACED LT ENGINE OIL TEMP AND PRESSURE INDICATOR P/N 522794, S/N OFF 9701615A, S/N ON 970632A. 2 L 7 2 4T RT A52EU 2001083100098 20010831 00098 NM 2001 8 31 2001F00249 1 20010530 A 3350 86210144 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT SEAT PALLETS 6-9 INOPERATIVE. REMOVED AND REPLACED REMOT E ASSEMBLY BATTERY AND RECEIVER THEN LIGHTS OPERATED NORMAL. REF ASAA0110313. (M) 2 L 7 2 4F A16WE 2001083100099 20010831 00099 NM 2001 8 31 2001F00250 1 20010615 A 3350 86210144 BATTERY BOEING 737 7372Q8C 138448S NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS ON SEAT PALLET 10-3 AND SMOKE BARRIER WOULD NOT TEST. REMOV ED AND REPLACED BATTERY PACK AND REMOTE ASSEMBLY BATTERY, THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F A16WE 2001083100100 20010831 00100 EA 2001 8 31 2001F00244 1 20010630 A 7931 C6SC10891 INDICATOR DHAV DHC6 DHC6 2802606 EA COCKPIT FAILED A OEZA O OTHER P NO WARNING INDICATION DE DESCENT 1 WP 19 227SA 517 APPROXIMATELY 5 MINUTES FROM LANDING NR 1 OIL PRESSURE WAS NOTED AT 15 PSI WITH NO CAUTION LIGHT. HOWEVER, THE ENGINE W AS SECURED AND SINGLE ENGINE LANDING PERFORMED. (M) 1 H 7 2 3T RT A9EA 2001083100101 20010831 00101 SO 2001 8 31 COMA0110139 1 20010826 A 7710 SEDLOC29J INDICATOR EMB 120 EMB120RT SO COCKPIT FAULTY A COMA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 SO 01 264CA 19166 1256 FLIGHT #5053. DURING APPLICATION OF POWER FOR TAKE OFF AT MCO THE #2 NH ANALOG INDICATION FAILED, AIRCRAFT RETURNED TO THE GATE.REPLACED THE NH/NL INDICATOR. 2 L 7 2 4T RT A31SO 2001083100102 20010831 00102 WP 2001 8 31 AALA20011541 1 20010725 A 5310 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 438AA 49456 TUL - FOUND CORROSION AND TWO CRACKS ON AFT CARGO DOOR JAMB BEAM AND WEB STATION 1155 TO 1220. INSTALLED DOUBLER ON DOO R BEAM. REPLACED WEB WITH NEW WEB AND INSTALLED NEW STRAP PER AARD 53-10-00-3. (M) 2 L 7 2 4F RT A6WE 2001083100103 20010831 00103 NM 2001 8 31 ASAA0110100 1 20010220 A 5311 6545829505 FRAME BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND CHORD AT BS 294-366, STRINGER 27L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2002010400127 20020104 00127 NM 2002 1 4 ASAA0110101 1 20010220 A 5311 65465438 FRAME BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 597, STRINGER 13L-18R CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2002010400129 20020104 00129 NM 2002 1 4 ASAA0110102 1 20010220 A 5311 651630086 FRAME BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND CHORD AT BODY STATION 178, STRINGER 20L CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001083100104 20010831 00104 NM 2001 8 31 ASAA0110111 1 20010226 A 5312 6516300 BULKHEAD BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND BULKHEAD AT BS 178, LBL 7 CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001083100105 20010831 00105 NM 2001 8 31 ASAA0110112 1 20010226 A 5312 6516300 BULKHEAD BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND BULKHEAD AT BS 178, WL 200, LBL 7 CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001083100106 20010831 00106 NM 2001 8 31 ASAA0110114 1 20010305 A 5313 BAC1498158 STRINGER BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING D-CHECK FOUND STRINGER 27R, BS 360-430 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001083100107 20010831 00107 NM 2001 8 31 ASAA0110117 1 20010305 A 5320 6562110 INTERCOSTAL BOEING 737 737290C 138448V NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL BS 342-350, LBL 42.5 HAS ELONGATED HOLES. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001083100108 20010831 00108 NM 2001 8 31 ASAA0110136 1 20010320 A 5320 BAC15201397 FLOOR SUPPORT BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 720AS 22577 PHX - DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT ANGLE AT BS 893, STRINGER 27R CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001083100109 20010831 00109 NM 2001 8 31 ASAA0110220 1 20010418 A 5310 652072355 DOOR FRAME BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PAE - DURING MAINTENANCE, FOUND FRAME AROUND MAIN CARGO DOOR CUTOUT AT BS 472.4, STRINGER 24R CRACKED. REPAIRED PER EA. (M) 2 L 7 2 4F A16WE 2001083100110 20010831 00110 NM 2001 8 31 ASAA0110428 1 20010625 A 5330 6545775 SKIN PANEL BOEING 737 7372X6C 1384552 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND SKIN PANEL AT BODY STATION 897, STRINGER 18R DENTED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001083100111 20010831 00111 NM 2001 8 31 ASAA0110429 1 20010625 A 5310 6554956503 SHEAR TIE BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 480, LBL 69 CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001083100112 20010831 00112 NM 2001 8 31 ASAA0110430 1 20010625 A 5320 654796027 INTERCOSTAL BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL AT BODY STATION 847-867, STRINGER 26R CORRODED. REPAIRED PER SRM. (M ) 2 L 7 2 4F RT A16WE 2001083100113 20010831 00113 NM 2001 8 31 ASAA0110431 1 20010625 A 5320 65549707 SUPPORT BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND SEAT TRACK SUPPORT BEAM AT BS 663-685, LEFT BUTTOCK LINE 64 CORRODED. REPAIRED PE R SRM. (M) 2 L 7 2 4F RT A16WE 2001083100114 20010831 00114 NM 2001 8 31 ASAA0110432 1 20010625 A 5320 69514763 SUPPORT BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND SEAT TRACK SUPPORT BEAM AT BS 520, RBL 46 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001083100115 20010831 00115 NM 2001 8 31 ASAA0110433 1 20010625 A 5330 654577655 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND SKIN PANEL AT BS 927, STRINGER 27L-27R CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001083100116 20010831 00116 NM 2001 8 31 ASAA0110434 1 20010625 A 5320 69387803 ATTACH ANGLE BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND ATTACH ANGLE BS 380, STRINGER 25L-26L CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001083100117 20010831 00117 NM 2001 8 31 ASAA0110435 1 20010625 A 5310 6446526 SHEAR TIE BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 440, LBL 69 CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001083100118 20010831 00118 NM 2001 8 31 ASAA0110436 1 20010625 A 5320 694147372 INTERCOSTAL BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL SUPPORT AT BS 400-420, LBL 22 CRACKED. REPAIRED PER BOEING DRAWING. (M) 2 L 7 2 4F RT A16WE 2001083100119 20010831 00119 WP 2001 8 31 RRXA11091 1 20010411 A 5753 5642960 RIB DOUG DC8 DC862F 3021972 WP LT IB FLAP CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LT I/B FLAP O/B RIB AT STA. XW122, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-2-0FIG2A, 51-1-21 A ND EO# QC-069 REV. 7/98. 2 L 7 4 4F 4A25 2001083100120 20010831 00120 NM 2001 8 31 ASAA0110448 1 20010630 A 3350 8731002 SIGN BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 ANC - DURING SCHEDULED MAINTENANCE CHECK, FOUND OVERHEAD EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED OVERHEAD EMERGENCY EXIT SIGN AND SIGN OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2001083100121 20010831 00121 WP 2001 8 31 RRXA11095 1 20010424 A 5230 3757794 STRUCTURE DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO B-PIT DOOR FRAME TRIANGLE AT STA.500, DAMAGE EXCEEDED LIMITATION IA W DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F 4A25 2001083100122 20010831 00122 NM 2001 8 31 ASAA0110482 1 20010707 A 5320 656210038 ANGLE BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND SUPPORT ANGLE AT BS 300-344, LEFT BUTTOCK LINE 38 CORRODED. REPAIRED PER SRM. (M ) 2 L 7 2 4F RT A16WE 2001083100123 20010831 00123 NM 2001 8 31 ASAA0110484 1 20010707 A 5320 693535216 TIE CLIP BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER TIE AT BS 540, STRINGER 23L-24L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001083100124 20010831 00124 NM 2001 8 31 ASAA0110485 1 20010707 A 5320 654880147 GUSSET BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND BULKHEAD GUSSET AT BS 227, LBL 3 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001083100125 20010831 00125 NM 2001 8 31 ASAA0110486 1 20010707 A 5347 6554966 SEAT TRACK BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND SEAT TRACK AT BS 344-520, LBL 62.5 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001083100126 20010831 00126 NM 2001 8 31 ASAA0110487 1 20010707 A 5230 65549352 STRUCTURE BOEING 737 7372X6C 1384552 NM CARGO DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND MAIN CARGO DOOR AT BS 380-480, STRINGER 16L HAS CRACKED AND BROKEN RIVET HEADS WIT H CRACKS EMANATING FROM RIVETS. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001083100127 20010831 00127 NM 2001 8 31 ASAA0110488 1 20010707 A 5330 654577762 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND SKIN PANEL AT BS 967-977, STRINGER 19L-22L GOUGED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001083100128 20010831 00128 NM 2001 8 31 ASAA0110489 1 20010707 A 5320 66221622 TIE CLIP BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND FRAME TIE CLIP AT BS 380, LBL 64 CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001083100129 20010831 00129 NM 2001 8 31 ASAA0140088 1 20010607 A 3397 8100022607 WIRE BOEING 737 7374Q8 NM CABIN DAMAGED A K NONE L NO TEST IN INSP/MAINT 1 NM 01 769AS 25103 SEA - DURING A LINE CHECK, FOUND TWO BANKS OF EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE STARTING AT ROW 18. REPAIRED WIR ES AT ROW 18. FLOOR TRACK LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 2001083100130 20010831 00130 WP 2001 8 31 ASAA0180188 1 20010603 A 3350 HPD54053858 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 982AS 53473 PDX - DURING SERVICE CHECK, THE EMERGENCY CEILING LIGHT AT ROW 17 WAS FOUND TO BE INOPERATIVE. REPLACED THE LAMP ASSEMB LY AT ROW 17. THE LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001083100131 20010831 00131 WP 2001 8 31 ASAA0180202 1 20010615 A 3350 0105606003 MODULE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 SEA - DURING PRE-FLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN 1ST CLASS. RECONNECTED LIGHT MODULE SO CKET. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001083100132 20010831 00132 WP 2001 8 31 ASAA0180209 1 20010625 A 3350 0105606003 MODULE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SEA - DURING PRE-FLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS DISCONNECTED AT ROW 7. RECONNECTED LIGHT MODULE SOCKE T. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001083100133 20010831 00133 WP 2001 8 31 ASAA0180210 1 20010626 A 3397 0105606003 WIRE DOUG DC9 DC983 3022083 WP CABIN DAMAGED A K NONE L NO TEST IN INSP/MAINT 1 NM 01 948AS 53021 SEA - DURING PRE-FLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN FIRST CLASS CABIN AT ROW 3. REPLACED S ECTION OF TRACK LIGHT WIRING. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001083100134 20010831 00134 WP 2001 8 31 ASAA0180211 1 20010627 A 3350 0105606003 MODULE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 SEA - DURING PRE-FLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS DISCONNECTED AT ROW 8. RECONNECTED LIGHT MODULE. LIG HTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001083100135 20010831 00135 WP 2001 8 31 ASAA0180212 1 20010628 A 3350 0105606003 MODULE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SEA - DURING PRE-FLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS DISCONNECTED AT ROW 7. RECONNECTED LIGHT MODULE SOCKE T. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001083100136 20010831 00136 NM 2001 8 31 ZW0A0107801 1 20010830 A 3350 LP7265001 BULB BOEING 717 717200 1383700 NM SEAT 3E A ZW0A K NONE O OTHER NR NOT REPORTED 1 CE 13 406TW 55073 THE EGRESS LIGHT AT SEAT 3E WAS INOPERATIVE. REPLACED THE BULB. NO CHECK-C. --CLOSED-- 2 L 7 2 4F TR A6WE 2001083100137 20010831 00137 WP 2001 8 31 RRXA11096 1 20010424 A 5510 5714837 FAIRING DOUG DC8 DC862F 3021972 WP HORIZONTAL STAB CHAFED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CHAFING DAMAGE TO LT HORIZONTAL STAB LOWER FAIRING, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0 FIG#6 AND DHSK 996-102. 2 L 7 4 4F 4A25 2001083100138 20010831 00138 WP 2001 8 31 RRXA11098 1 20010426 A 5315 5759332 FLOORBEAM DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FLOORBEAM AT STA.1540 AND RBL44, DAMAGE EXCEEDED LIMITATION IAW DC-8 SR M. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21 AND DHK 996-34S. 2 L 7 4 4F 4A25 2001083100139 20010831 00139 NM 2001 8 31 USAA010961 1 20010801 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 631AU 27809 CLT - FOUND FLOORBEAM CORRODED APPROXIMATELY 6 SQUARE INCHES, BS 377.7, LBL 22 TO LBL 47.5. DAMAGE REMOVED, INSTALLED T- CAP REPAIR PER SRM 53-00-51, FIG 201. (M) 2 L 7 2 4F RT A2NM 2001083100140 20010831 00140 NM 2001 8 31 USAA010969 1 20010731 A 5330 SKIN BOEING 757 7572B7 1384964 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 632AU 27810 CLT - FOUND SKIN WITH PREVIOUSLY INSTALLED DOUBLER, BS 650 AT STRINGER 21R. PREVIOUSLY INSTALLED DOUBLER PER SRM 53-00- 01 FIG 204. (M) 2 L 7 2 4F RT A2NM 2001083100141 20010831 00141 NM 2001 8 31 USAA010974 1 20010731 A 5320 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 632AU 22219 27810 CLT - FOUND INTERCOSTAL CORRODED 7 INCHES BY 2 INCHES, STATION 324-331 AT RBL 60. INSTALLED NEW INTERCOSTAL PER SRM 51-4 0-02. (M) 2 L 7 2 4F RT A2NM 2001083100142 20010831 00142 NM 2001 8 31 USAA010975 1 20010731 A 5320 THRESHOLD BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 632AU 27810 CLT - FOUND THRESHOLD WEB CORRODED .300 INCH BY .300 INCH AND .031 DEEP, FORWARD CARGO FUSELAGE CUTOUT LOWER THRESHOLD O UTBOARD FACE. REPAIRED AND REPLACED RIVET PER SRM 53-30-15. (M) 2 L 7 2 4F RT A2NM 2001083100143 20010831 00143 NM 2001 8 31 USAA010994 1 20010806 A 5320 CHANNEL BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND STRINGER TIE CHANNEL CORRODED 1 INCH BY 2 INCHES, BS 1488 S26R. REPLACED STRAP PER SRM 51-10-02. (M) 2 L 7 2 4F RT A2NM 2001083100144 20010831 00144 NE 2001 8 31 USAABA01007 2 20010629 A 7520 52G070 COOLER AIRBUS 330 A330323 EU PWA 4168 PW4168A NE NR 3 ENGINE FAILED A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 674UW 342 733476 PIT - DURING TROUBLESHOOTING OF A TCC (TURBINE CLEARANCE CONTROL) ACTUATOR FUEL LEAK, SIGNIFICANT DAMAGE TO THE INTERMED IATE CASE HEAT SHIELDS AND THERMAL BLANKETS WAS NOTED FORWARD OF THE NR 3 BEARING BUFFER AIR COOLER. A MASSIVE AIR LEAK WAS DISCOVERED EMANATING FROM THE FORWARD FACE OF THE COOLER. IT WAS DETERMINED THAT THE DAMAGE TO THE THERMAL BLANKET S AND HEAT SHIELD WAS TOO EXTENSIVE TO REPAIR ON-WING. THE A/C WAS FERRIED TO PHL AND THE ENGINE WAS REPLACED. THE COO LER WAS REMOVED, AND IT WAS DETERMINED THAT THE FAILURE OF A WELD IN THE COOLER CASING WAS THE CAUSE OF THE AIR LEAK. ( M) 2 L 7 2 4F 4 F RT A46NM 2001083100145 20010831 00145 NM 2001 8 31 USAABB01074 1 20010729 A 3610 79275513 CONTROLLER BOEING 767 7672B7 1385107 NM LT ENGINE LEAKING A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 651US 4656 24764 PHL - FLT 12 - APPROXIMATELY THIRTY MINUTES AFTER DEPARTURE, THE LEFT ENGINE BLEED LIGHT ILLUMINATED, THE DUCT PRESSURE WENT TO ZERO, AND THE LEFT PACK 'INOP' LIGHT ILLUMINATED. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A LEAKING FITTING ON THE LEFT ENGINE PRV CONTROLLER AND REPLACED IT. (M) 2 L 7 2 4F RT A1NM 2001083100146 20010831 00146 WP 2001 8 31 RRXA11102 1 20010427 A 5210 5615403 INTERCOSTAL DOUG DC8 DC862F 3021972 WP FWD ENTRY DOOR DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND OPEN HOLE DAMAGE TO FWD ENTRY DOOR INNER SKIN WEB JUST ABOVE WING, DAMAGE EXCEEDED LIMI TATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1 -21, 52-3-2 FIG 3, DWG 5615403. 2 L 7 4 4F 4A25 2001083100147 20010831 00147 WP 2001 8 31 RRXA11103 1 20010427 A 5320 42514704117 SPLICE DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND MISSDRILLED DAMAGE TO FWD CARGO PIT FRAME AT STA.380 AND L32L, DAMAGE EXCEEDED LIMITATI ON IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21, 53-2-0 FIG 2. 2 L 7 4 4F 4A25 2001083100148 20010831 00148 NM 2001 8 31 USAASB01226 1 20010808 A 3397 WIRE BOEING 737 737201 1384454 NM CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 EA 19 254AU 22796 BDL - MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY LIGHT AT ROW 1 INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRING. OPE RATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A16WE 2001083100149 20010831 00149 NM 2001 8 31 USAA010970 1 20010731 A 5320 141N516152 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 632AU 22219 27810 CLT - FOUND INTERCOSTAL CORRODED 2 INCHES BY 2 INCHES, BS 363.23 TO 377.7 RBL 10.5. REMOVED AND REPLACED PER SRM 51-40-0 2 AND 51-10-00. (M) 2 L 7 2 4F RT A2NM 2001083100152 20010831 00152 WP 2001 8 31 RRXA11104 1 20010427 A 5320 5615762 INTERCOSTAL DOUG DC8 DC862F 3021972 WP RT FWD SERV DOOR MISDRILLED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND MISSDRILLED DAMAGE TO R/H FWD SERVICE DOOR LWR CENTER INTERCOASTAL, DAMAGE EXCEEDED LIM ITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 52- 2-0 FIG#2, 51-1-21, 51-1-20D, DWG 5615762. 2 L 7 4 4F 4A25 2001083100153 20010831 00153 WP 2001 8 31 RRXA11107 1 20010427 A 5340 3750757U503 FITTING DOUG DC8 DC862F 3021972 WP STA605-615 L31L CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO L/H SPLICE FITTING AT STA.605-615 AND L31L, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-3-0, 51- 1-20D. 2 L 7 4 4F 4A25 2001083100154 20010831 00154 WP 2001 8 31 RRXA11108 1 20010427 A 5310 5888367 SEAT TRACK DOUG DC8 DC862F 3021972 WP COCKPIT CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SEAT TRACK AT 2ND OBSERVERS SEAT, DAMAGE EXCEEDED LIMITATION IAW DC -8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 51-3-0 AND DWG#5888367. 2 L 7 4 4F 4A25 2001083100156 20010831 00156 WP 2001 8 31 RRXA11110 1 20010428 A 5347 5888367 SEAT TRACK DOUG DC8 DC862F 3021972 WP COCKPIT WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND WEAR DAMAGE TO SEAT TRACK AT PILOTS AFT LEFT SEAT TRACK, DAMAGE EXCEEDED LIMITATION IA W DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8 FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0. 2 L 7 4 4F 4A25 2001083100162 20010831 00162 NM 2001 8 31 01FDEA00784 1 20010824 A 2170 COALESCER BAG BOEING 727 7272S2F 1384O81 NM A/C BAY DIRTY A FDEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 217FE 13395 TWO HR INTO FLT, CREW NOTICED ELECTRICAL SMELL IN COCKPIT. REMOVED AND REPLACED BOTH COALESCER BAGS PRECAUTIONARY PER M M 21-55-051-4. CND. 2 L 7 3 4F A3WE 2001083100163 20010831 00163 NM 2001 8 31 01FDEA00786 1 20010828 A 2400 ELECTRICAL SYS DOUG MD11 MD11F 3023600 NM AC SYS FAILED A FDEA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 25 618FE 48754 GOT LEVEL ONE ALERT BUS R EMERGENCY AC OFF LOST ALL ASSOC DISPLAYS & RADIUS. REMOVED AND REPLACED R2-5157 PER SMP. 2 L 7 3 4F RT A22WE 2001083100164 20010831 00164 WP 2001 8 31 01FDEA00793 1 20010829 A 2910 HYDRAULIC LINE DOUG DC10 DC1010CF 3023502 WP HYDRAULIC SYS LEAKING A FDEA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 321FE 47836 HYD NR 1 QUANTITY DECREASED TO ZERO & PRESS LESS THAN 1000. REMOVED AND REPLACED HYD LINES. LEAK CHECK OK. 2 L 7 3 4F RT A22WE 2001083100165 20010831 00165 NM 2001 8 31 01FDEA00794 1 20010831 A 2613 WARNING LIGHT BOEING 727 727225 1384077 NM COCKPIT ILLUMINATED A FDEA O OTHER J WARNING INDICATION CR CRUISE 1 SO 25 466FE 21292 USING NR 2 ENG RT BLEED TO PROVIDE AIR TO RT PACK, LWR AFT BODY OVERHEAD LIGHT ILLUM. RED TABS FOLLOWED. 2 L 7 3 4F A3WE 2001083100166 20010831 00166 WP 2001 8 31 200100165 1 20010830 A 2740 591096229 JACKSCREW DOUG DC9 DC915 3022036 WP HORIZ STAB OUT OF TOLERANCE B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 915 7359 47061 HORIZONTAL STABILIZER JACKSCREW ENDPLAY AND FREEPLAY CHECK FOUND THAT THE ENDPLAY WAS OUT OF LIMITS. REMOVED AND REPLAC ED THE HORIZONTAL STABILIZER JACKSCREW. 2 L 7 2 4F A6WE 2001083100185 20010831 00185 CE 2001 8 31 AIOA288236 1 20010530 A 2841 10038000647 INDICATOR BEECH 90 C90A 1152911 CE PWA PT6 PT6* 52043 EA COCKPIT FAILED E AIOA K NONE O OTHER NR NOT REPORTED 1 GL 11 819MH LJ735 PILOT NOTED LEFT FUEL QUANTITY INDICATOR WAS UNRELIABLE AND REPORTING LOWER THAN NORMAL. GAUGE SN 1089 WAS REMOVED AND OVERHAULED, GAUGE SN 4739M WAS INSTALLED AND CALIBRATED TO THE A/C PER MM. GAUGE LASTED ONE TRIP BEFORE RESULTING A LIK E PROBLEM. GAUGE WAS SWAPPED LEFT TO RIGHT, IT WAS FOUND TO BE A PROBLEM WITH GAUGE. IT WAS SWAPPED BACK AND MEL`D. G AUGE SN 4739M WAS REMOVED AND GAUGE SN 2570M WAS INSTALLED. GAUGE LASTED 1 TRIP AND FAILED. THE AC WAS MEL`D FOR FLIGH T WITH THE INOPERATIVE GAUGE. SEVERAL CORRODED GROUNDS WERE FOUND TO PLAY A FACTOR. GROUND POINTS AT PROBES WERE CLEANE D, AND GAUGE RECALIBRATED TO THE AC AND WORKED. GAUGE FAILED AFTER SECOND FLIGHT AFTER INSPECTION. MAINTENANCE LOOKED A 1 L 7 2 3T 3 T RT 3A20 E2NE 2001083100186 20010831 00186 CE 2001 8 31 BSY2001F00007 1 20010806 A 3260 62 LIGHT LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP COCKPIT INOPERATIVE E BSYA O OTHER N FALSE WARNING AP APPROACH 1 GL 07 39DK 480 LTP74301 HAD NO LEFT MAIN GEAR DOWN AND LOCK INTO AIRPORT. REMOVED AND REPLACED BULB OPS OK. 2 L 7 2 4F 4 F A10CE E6WE 2001083100187 20010831 00187 CE 2001 8 31 BSY2001F00008 1 20010806 A 2432 BATTERY LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP RT MAIN OVERHEATED E BSYA O OTHER M J OVER TEMP WARNING INDICATION NR NOT REPORTED 1 GL 07 118DA 081 RT4423 RIGHT MAIN SHIP BATTERY GOT HOT TURNING ON 160 DEGREE LIGHT AND INDICATION READ HIGH. REMOVED LOANER BATTERIES AND REPL ACED WITH SERVICEABLE SET. OPS CHECK, OK. 2 L 7 2 4F 4 F A10CE E6WE 2001083100188 20010831 00188 CE 2001 8 31 BSY2001F00009 1 20010806 A 2432 BATTERY LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP RT MAIN OVERHEATED E BSYA O OTHER M J OVER TEMP WARNING INDICATION NR NOT REPORTED 1 GL 07 118DA 081 RP89303 RIGHT MAIN SHIP BATTERIES GOT HOT TURNING ON 160 DEGREE LIGHT AND INDICATION READ HIGH. REMOVED LOANER BATTERIES AND RE PLACED WITH SERVICEABLE SET. OPS CHECK OK. 2 L 7 2 4F 4 F A10CE E6WE 2001083100191 20010831 00191 CE 2001 8 31 FFS2001F00000 1 20010711 A 3250 11438801817 SERVO VALVE BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA NLG STEERING FAILED A FFSA O OTHER J WARNING INDICATION NR NOT REPORTED 1 AL 01 575D 1018 1018 UE24 POWER STEERING INOPERATIVE. FAILURE CODE C: ACTUATOR SERVO VALVE FAILURE: COMPUTER DETECTS A DECREASE IN SERVO CURREN T. 2 L 7 2 4T 3 T RT A24CE E2NE 2001083100192 20010831 00192 EA 2001 8 31 FFS2001F00001 2 20010502 A 7414 BL68256013 GEAR PIPER PA32 PA32R300 7103213 SO LYC O540 IO540K1A5 41532 EA MAGNETO DAMAGED B FFSA K NONE O OTHER IN INSP/MAINT 1 SO 05 38305 400 32R7780413 WHEN TROUBLE SHOOTING AN EXCESSIVE LEFT MAGNETO DROP, THE LEFT MAGNETO PLASTIC GEARS WERE FOUND TO BE MISSING SIX TEETH. ONE WAS MISSING ON THE RIGHT SIDE AS WELL. REMOVED AND REPLACED MAGNETO WITH SERVICEABLE PART. 1 L 7 1 3O 3 O A3SO 1E4 2001083100193 20010831 00193 CE 2001 8 31 FFSAFL92048 1 20010711 A 3250 SERVO VALVE BEECH 1900 1900D 1154162 CE NLG STEERING FAILED D FFSA O OTHER J WARNING INDICATION NR NOT REPORTED 1 AL 01 575D UE24 POWER STEERING INOPERATIVE. FAILURE CODE C. ACTUATOR SERVO VALVE FAILURE. COMPUTER DETECTS A DECREASE IN SERVO CURREN T. SERVO VALVE MAY BE DAMAGED. 2 L 7 2 4T RT A24CE 2001083100194 20010831 00194 CE 2001 8 31 GNB2001F00000 1 20010710 A 8120 47090813 WASTEGATE VALVE CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO TURBOCHARGER FAILED D GNBA O OTHER O OTHER NR NOT REPORTED 1 SW 01 525RH 1959 402C0525 823318R UNABLE TO CONTROL MAIN PRESSURE. 1 L 7 2 3O 3 O A7CE E8CE 2001083100195 20010831 00195 SO 2001 8 31 GNB2001F00001 2 20010710 A 7314 6462108 PUMP CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO ENGINE ERRATIC D GNBA O OTHER O OTHER NR NOT REPORTED 1 SO 01 525RH 11 402C0525 823315R ENGINE DRIVEN FUEL PUMP - FUEL PUMP ERRATIC ON UNMETERED FUEL PRESSURES. 1 L 7 2 3O 3 O A7CE E8CE 2001083100196 20010831 00196 NE 2001 8 31 HCM2001F00000 2 20010613 A 7421 SC2036 ELECTRODE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE IGNITER MISSING E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 312B 737 2243 DURING A ROUTINE 100 HOUR INSPECTION IT WAS NOTED THAT THE ELECTRODE WAS MISSING FROM THE IGNITER PLUG. FURTHER INVESTI GATION REVEALED THAT IT HAD CAUSED DAMAGE TO THE NG NR 1 BLADE WHEN IT BROKE LOOSE AND SEPARATED FROM THE IGNITER. FURT HER ANALYSIS IS REQUIRED TO DETERMINE ACTUAL CAUSE OF THE FAILURE. 1 G 7 1 3U 3 U NC H9EU E19EU 2001083100197 20010831 00197 NE 2001 8 31 HCM2001F00001 2 20010719 A 7421 SC2036 ELECTRODE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE IGNITER MISSING E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 532BH 380 2494 DURING A ROUTINE 100 HOUR INSPECTION IT WAS NOTED THAT THE ELECTRODE WAS MISSING FROM THE IGNITER PLUG. FURTHER INVESTI GATION REVEALED THAT IT HAD CAUSED DAMAGE TO THE NG NR 1 BLADE WHEN IT BROKE LOOSE AND SEPARATED FROM THE IGNITER. FURT HER ANALYSIS IS REQUIRED TO DETERMINE ACTUAL CAUSE OF THE FAILURE. 1 G 7 1 3U 3 U NC H9EU E19EU 2001083100198 20010831 00198 SW 2001 8 31 J8O2001F00000 1 20010727 A 6320 206040032105 BEARING BELL 206 206L3 1182108 SW ALLSN 250C 250C30 03013 GL M/R TRANSMISSION DAMAGED A J8OR K NONE O OTHER IN INSP/MAINT 1 WP 07 303MP 841 51202 TRANSMISSION REMOVED FOR METAL ON CHIP DETECTORS. ON DISASSEMBLY IT WAS DISCOVERED THE DUPLEX BEARING PN 206-040-032-10 5 OUTER RACE WAS SPALLING AND 3 BALL BEARINGS HAD COME APART. 1 G 7 1 3U 3 U H2SW E1GL 2001090300001 20010903 00001 SO 2001 9 3 C2XA01BT157 1 20010826 A 2100 UNK ACM EMB 145 EMB145LR SO FAULTY A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 15912 145439 EWR---CO4190, CREW REPORTED, "STRONG ELECTRICAL BURNING SMELL WITH SOME SMOKE IN AIRCRAFT" MAINTENANCE REMOVED AND REPLA CED #1 AIR CYCLE MACHINE IAW EMB 145 MM 21-51-03. OPS. CHECKED AND LEAKED CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2001091000385 20010910 00385 EU 2001 9 10 C2XA01BT159 1 20010814 A 5710 S5751052800204 STRUT AEROSP ATR42 ATR42320 8680930 EU RT WING WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14828 179 YUL---DURING 4C INSPECTION YUL MAINTENANCE FOUND RT WING REAR SPAR FITTING AT RIB 16, TRAILING EDGE STRUT HOLE TO BE ELO NGATED. MAINTENANCE REMOVED AND REPLACED RT WING REAR SPAR FITTING AT RIB 16, TRAILING EDGE STRUT IAW ATR42 STANDARD PR ACTICE 20-21-12. OK FOR SERVICE. 2 H 7 2 4T RT A53EU 2001090300002 20010903 00002 NM 2001 9 3 2001748001 1 20010903 A 7720 JT8D15 ENGINE BOEING 727 727225 1384077 NM A DHLA K NONE O OTHER CL CLIMB 1 SO 01 748DH 22440 During drop in-to keep from exceeding E.G.T. had to reduce thrust, on #1 engine during take-off. Unable to maintain take -off thrust.1) Checked #1 engine E.G.T. indicator and total resistance, all checked good I.A.W. B-727 M.M. 77-21-00.2) C hecked #1 E.P.R. , no leaks found, but indication was out of tolerance at 1.5 (1.47) + at 2.0 (1.96) I.A.W. B-727 M.M. 7 7-11-00.3) #1 engine bullet removed and stored in AV shops cage.4) Found #1 engine E.P.R indicator out of tolerance I.A. W. B-727 M.M. 77-11-00 page 5075) Removed and replaced #1 engine E.P.R. indicator I.A.W. B-727 M.M. 77-11-00.6) Leak and calibration check is good I.A.W. B-727 M.M. 77-11-10. #1 EPR7) Checked PRBC screens and tubing-PS3 strain 2 L 7 3 4F A3WE 2001090400001 20010904 00001 SO 2001 9 4 C2XA01IA353 1 20010901 A 3610 24540150 CLAMP EMB 120 EMB120ER 3260203 SO FUSELAGE LOOSE A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 16724 120171 ACT - FLIGHT 3420, THE CREW REPORTED A NUMBER TWO DUCT LEAK LIGHT. THE CREW SHUTDOWN THE NUMBER TWO ENGINE AS A PRECAUTI ON AND THE AIRCRAFT DIVERTED TO ACT WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A LOO SE CLAMP ON THE ON THE NUMBER TWO TEMPERATURE CONTROL VALVE. MAINTENANCE TIGHTENED THE AFFECTED CLAMP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001090400002 20010904 00002 WP 2001 9 4 RRXA11099 1 20010426 A 5320 5645357 PAN DOUG DC8 DC862F 3021972 WP CARGO DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FWD CARGO PIT DOOR PAN AT A-PIT, DAMAGE EXCEEDED LIMITATION IAW DC-8 SR M. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0, 51-1-21, 52-2-0 FIG 1F. 2 L 7 4 4F 4A25 2001090400003 20010904 00003 WP 2001 9 4 RRXA11126 1 20010430 A 5340 58942822 FITTING DOUG DC8 DC862F 3021972 WP CARGO DOORWAY CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FWD CARGO PIT CROSS SLIDE DOOR JAMB BACK UP FITTING NR 1 LWR TEE BO LT, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INST ALLED IAW DC-8 SRM 53-2-0 FIG2D, 51-1-21. 2 L 7 4 4F 4A25 2001090400004 20010904 00004 WP 2001 9 4 RRXA11131 1 20010427 A 5320 2773378 ANGLE DOUG DC8 DC862F 3021972 WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND DAMAGE TO TORQUE BOX ATTACH ANGLE AT STA.375 AND L6L, DAMAGE EXCEEDED LIMITATION IAW D C-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND DWG 2 773378. 2 L 7 4 4F 4A25 2001090400005 20010904 00005 WP 2001 9 4 RRXA11136 1 20010504 A 5310 57727873 DOOR FRAME DOUG DC8 DC862F 3021972 WP STA330 L17L-L21L TOOL DAMAGE A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND DRILL DAMAGE TO MCD JAMB DOOR FRAME AT STA330 AND L17L-L21L, DAMAGE EXCEEDED LIMITATIO N IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DHSK 996-743. 2 L 7 4 4F 4A25 2001090400006 20010904 00006 WP 2001 9 4 RRXA11140 1 20010410 A 5340 4646250 FITTING DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON END FITTING AT STA.1525 AND L33L, DAMAGE EXCEEDED LIMITAT ION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-5 FIG8C-1. 2 L 7 4 4F 4A25 2001090400007 20010904 00007 WP 2001 9 4 RRXA11144 1 20010501 A 5330 5644981 SKIN DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO EXTERIOR SKIN AT STA.203 AND L16L, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DHSK 996-493. 2 L 7 4 4F 4A25 2001090400008 20010904 00008 WP 2001 9 4 RRXA11147 1 20010424 A 5320 4616814 ANGLE DOUG DC8 DC862F 3021972 WP FUSELAGE TOOL DAMAGE A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING AS MAINTENANCE VISIT FOUND DRILLED DAMAGE TO ANGLE AND WEB AT STA.350 BETWEEN L19R-L22R, DAMAGE EXCEEDED LIMITAT ION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DHSK996-730. 2 L 7 4 4F 4A25 2001090400009 20010904 00009 WP 2001 9 4 RRXA11148 1 20010505 A 5730 5758387 SKIN DOUG DC8 DC862F 3021972 WP LT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LT WING LOWER SKIN FAST HOLES IN THE AREA SURROUNDING THE 3 O/B FASTNER S OF STRINGER 64L END FITTING AT STA. XRS543.2 AND STR 64, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TRE ATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW EO AM5732-05. 2 L 7 4 4F 4A25 2001090400010 20010904 00010 WP 2001 9 4 RRXA11151 1 20010509 A 5720 57698571 RUB STRIP DOUG DC8 DC862F 3021972 WP RT WING WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO RT WING L/E O/B SLOT VANE ATTACH FITTING, DAMAGE EXCEEDED LIMITATION IA W DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND DW G 5769857-1. 2 L 7 4 4F 4A25 2001090400011 20010904 00011 WP 2001 9 4 RRXA11152 1 20010509 A 5340 3755822503N FITTING DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING AT STA.540 AND L34L-L35L, DAMAGE EXCEEDED LIMITATI ON IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0 FIG 2D, 51-1-20D. 2 L 7 4 4F 4A25 2001090400012 20010904 00012 WP 2001 9 4 RRXA11162 1 20010406 A 5730 56434111 PANEL DOUG DC8 DC862F 3021972 WP LT WING CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO L/H WING UPPER T/E PANEL ABOVE MLG TRUNNION AT STA. XW60-70, DAMAG E EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0, 51-1-20D, 57-1-0. 2 L 7 4 4F 4A25 2001090400013 20010904 00013 WP 2001 9 4 RRXA11166 1 20010526 A 5330 97532901 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO AFT ACCY COMP. CUSP MEMBRANCE AT STA.158-1600 AND RBL48, DAMAGE EXCEEDE D LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 53-2-0 FIG.1D. 2 L 7 4 4F RT 4A25 2001090400014 20010904 00014 WP 2001 9 4 RRXA11167 1 20010527 A 5753 5655752 SKIN DOUG DC8 DC873F 302199F WP LT WING TE FLAP SCRATCHED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND SCRATCH DAMAGE TO LT WING O/B FLAP LOWER SKIN AT STA. XRS410, DAMAGE EXCEEDED LIMITATIO NS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-2-0, 51 -1-26, 51-1-21A, 57-2-0 FIG.2A. 2 L 7 4 4F RT 4A25 2001090400015 20010904 00015 WP 2001 9 4 RRXA11179 1 20010528 A 5730 576960035 DOUBLER DOUG DC8 DC873F 302199F WP LT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO L/H WING O/B L/E LWR INTERNAL DOUBLER AT STA.XFS597.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 5 1-1-21, 51-1-20D AND DWG 5769600. 2 L 7 4 4F RT 4A25 2001090400016 20010904 00016 WP 2001 9 4 RRXA11184 1 20010528 A 5712 576946919 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LT WING O/B L/E LOWER RIB AT STA. XFS622.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21, 5 1-3-0, 57-2-0 FIG.2. 2 L 7 4 4F RT 4A25 2001090400017 20010904 00017 WP 2001 9 4 RRXA11187 1 20010529 A 5712 425435101 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACKED DAMAGE TO LT WING L/E UPPER RIB AT STA. XFS 610, DAMAGE EXCEEDED LIMITATIONS IA W DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-2-0 FIG.2, 51-1-21. 2 L 7 4 4F RT 4A25 2001090400018 20010904 00018 WP 2001 9 4 MWEA011207 1 20010830 A 5230 39140251 FITTING DOUG DC9 DC932 3022066 WP AFT CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 AFT CARGO DOOR BEAM #4 AFT END FITTING IS CRACKED. -- REMOVED AND REPLACED FITTING. 2 L 7 2 4F A6WE 2001090400019 20010904 00019 WP 2001 9 4 MWEA011208 1 20010830 A 5230 39140252 FITTING DOUG DC9 DC932 3022066 WP AFT CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 AFT CARGO DOOR BEAM #5 FORWARD END FITTING IS CRACKED. -- REMOVED AND REPLACED FITTING. 2 L 7 2 4F A6WE 2001090400020 20010904 00020 WP 2001 9 4 MWEA011209 1 20010830 A 5260 99155709 WEB DOUG DC9 DC932 3022066 WP AFT STAIRS WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 AFT STAIR, LEFT SIDE WEB WORN AT JAMB MATING SURFACE BETWEEN #5 AND #6 STEP FROM BOTTOM. -- FABRICATED AND INSTALLED W EB. 2 L 7 2 4F A6WE 2001090400021 20010904 00021 WP 2001 9 4 MWEA011210 1 20010830 A 5310 99115243 SHEAR TIE DOUG DC9 DC932 3022066 WP STATION 832 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 STATION 832 SHEAR TIE JUST ABOVE THE CUSP LINE IS CRACKED. -- FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F A6WE 2001090400022 20010904 00022 WP 2001 9 4 MWEA011211 1 20010830 A 5310 99115233 SHEAR TIE DOUG DC9 DC932 3022066 WP STATION 275 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 1/4TH INCH IN THE BOTTOM OF A SHEAR CLIP IN THE CABIN AT STATION 275 LONGERON 17 LEFT, JUST ABOVE. -- FABRICATED AND I NSTALLED SHEAR TIE SPLICE. 2 L 7 2 4F A6WE 2001090400023 20010904 00023 WP 2001 9 4 MWEA011213 1 20010830 A 5310 995789923 FITTING DOUG DC9 DC932 3022066 WP STATION 69 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 FRAME ATTACH FITTING AT STATION 69, 12 INCHES LEFT OF CENTER TOP SECTION OF FORWARD ACCESORY IS CRACKED. -- FABRICATED AND INSTALLED FRAME ATTACH FITTING. 2 L 7 2 4F A6WE 2001090400024 20010904 00024 WP 2001 9 4 MWEA011214 1 20010830 A 5310 59114279 LONGERON DOUG DC9 DC932 3022066 WP STATION 945 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 LONGERON 17 LEFT AT STATION 945 CRACKED IN 2 PLACES. -- FABRICATED AND INSTALLED LONGERON SECTION. 2 L 7 2 4F A6WE 2001090400025 20010904 00025 WP 2001 9 4 MWEA011215 1 20010830 A 5310 59114277 LONGERON DOUG DC9 DC932 3022066 WP STATION 965 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 LONGERON 16 LEFT AT STATION 965 CRACKED. -- FABRICATED INSTALLED LONGERON SECTION AND SPLICES. 2 L 7 2 4F A6WE 2001090400026 20010904 00026 WP 2001 9 4 MWEA011216 1 20010830 A 5310 59114267 LONGERON DOUG DC9 DC932 3022066 WP STATION 965 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 LONGERON 13 LEFT AT STATION 965 CRACKED. -- FABRICATED AND INSTALLED LONGERON SECTION AND STRINGER SPLICE SECTIONS. 2 L 7 2 4F A6WE 2001090400027 20010904 00027 WP 2001 9 4 MWEA011217 1 20010830 A 5310 59114279 LONGERON DOUG DC9 DC932 3022066 WP STATION 965 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 LONGERON 17 RIGHT AT STATION 965 CRACKED AT TOP BOLT. -- FABRICATED AND INSTALLED LONGERON SECTION AND STRINGER SPLICE SECTIONS. 2 L 7 2 4F A6WE 2001090400028 20010904 00028 WP 2001 9 4 RRXA11188 1 20010529 A 5330 5644130 SKIN DOUG DC8 DC873F 302199F WP HORIZONTAL STAB CHAFED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CHAFFING DAMAGE TO LT HORIZ STAB FIXED LOWER FAIRING AT AFT END, DAMAGE EXCEEDED LIMITA TIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DHSK 606-648. 2 L 7 4 4F RT 4A25 2001090400029 20010904 00029 WP 2001 9 4 RRXA11189 1 20010529 A 5311 9751098 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE MISDRILLED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND MISSDRILLED HOLE DAMAGE TO MAIN CABIN LT LOWER SIDE OF FRAME AT STA.1560, DAMAGE EXCEED ED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-0 FIG.1F, 51-1-21. 2 L 7 4 4F RT 4A25 2001090400030 20010904 00030 WP 2001 9 4 RRXA11194 1 20010529 A 5710 57696001 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LT WING O/B L/E LOWER RIBS AT STA. XFS660-641.25-653.75, DAMAGE EXCEEDE D LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D, 51-3-0. 2 L 7 4 4F RT 4A25 2001090400031 20010904 00031 WP 2001 9 4 RRXA11195 1 20010530 A 5730 5769600 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LT WING O/B L/E LOWER SKIN AT STA.XFS597.5 AND DRAIN HOLE, DAMAGE EXCEE DED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 S RM 57-2-0 FIG.2A. 2 L 7 4 4F RT 4A25 2001090400032 20010904 00032 WP 2001 9 4 RRXA11196 1 20010530 A 5330 2892072 PANEL DOUG DC8 DC873F 302199F WP FUSELAGE PUNCTURED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND PUNCTURE DAMAGE TO FLOOR PANEL AT STA.1760, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. R EMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-3, 51-1-21. 2 L 7 4 4F RT 4A25 2001090400033 20010904 00033 WP 2001 9 4 RRXA11198 1 20010530 A 7160 D51B1181016 ANGLE DOUG DC8 DC873F 302199F WP NR 2 NACELLE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO NR 2 ENGINE INLET COWL I/B STRAKE ON LOWER LATCH, DAMAGE EXCEEDED LIMIT ATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0 , 51-1-21 AND DWG D51B11810. 2 L 7 4 4F RT 4A25 2001090400034 20010904 00034 WP 2001 9 4 RRXA11200 1 20010530 A 5522 56444001 DOUBLER DOUG DC8 DC873F 302199F WP RT ELEVATOR BROKEN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND BROKEN DAMAGE TO RT ELEVATOR O/B TIP CORNER BROKEN OFF, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 55-2-0, 51-3-0, 51-1-21. 2 L 7 4 4F RT 4A25 2001090400035 20010904 00035 WP 2001 9 4 RRXA11201 1 20010530 A 5710 576947012108 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H WING O/B L/E UPPER RIBS AT STA. XFS716.25, 728.75, 735, 741.25, DAM AGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED I AW DC-8 SRM 51-1-20D, 57-2-0 FIG.2. 2 L 7 4 4F RT 4A25 2001090400036 20010904 00036 WP 2001 9 4 RRXA11204 1 20010531 A 5720 5710351 BRACKET DOUG DC8 DC873F 302199F WP RT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO RT AFT WING TO BODY FAIRING SUPPORT BRACKET LOWER FORWARD ANGLE BRACKET AT STA.910, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-11, 51-3-0 AND DWG#5710351. 2 L 7 4 4F RT 4A25 2001090400037 20010904 00037 WP 2001 9 4 RRXA11205 1 20010531 A 5315 5758876 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO AFT ACCY. COMPARTMENT FLOOR BEAM AT STA.1660 AND RBL31, DAMAGE EXCE EDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC -8 SRM 51-1-11 AND DHSK 600-456. 2 L 7 4 4F RT 4A25 2001090400038 20010904 00038 WP 2001 9 4 RRXA11211 1 20010601 A 5347 54932154 SPLICE DOUG DC8 DC873F 302199F WP FUSELAGE BROKEN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND BROKEN DAMAGE TO MAIN CABIN SEAT TRACK SCALLOPS AT STA.540 AND RBL60, DAMAGE EXCEEDED L IMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 53 -2-3. 2 L 7 4 4F RT 4A25 2001090400039 20010904 00039 WP 2001 9 4 RRXA11215 1 20010603 A 5280 5616307 DOUBLER DOUG DC8 DC873F 302199F WP LT MLG DOOR CHAFED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CHAFFED DAMAGE TO L/H MLG DOOR LOWER AFT STMP AND CORNER OF DOOR, DAMAGE EXCEEDED LIMIT ATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-2 1, 52-2-0, 51-1-20A AND DWG 5616307. 2 L 7 4 4F RT 4A25 2001090400040 20010904 00040 WP 2001 9 4 RRXA11221 1 20010604 A 5720 570174539 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO RT O/B FLAP PANEL, LT HINGE ANGLE AT STA.410, DAMAGE EXCEEDED LIMITATI ONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21 A ND DWG 5761745-39. 2 L 7 4 4F RT 4A25 2001090400041 20010904 00041 WP 2001 9 4 RRXA11226 1 20010605 A 7110 42543208 DOUBLER DOUG DC8 DC873F 302199F WP NR 4 ENGINE COWL PUNCTURED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND PUNCTURE DAMAGE TO NR 4 ENGINE O/B T/R COWL INNER HEAT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND DC- 8 MM 78-31-10 FIG.806. 2 L 7 4 4F RT 4A25 2001090400042 20010904 00042 WP 2001 9 4 RRXA11229 1 20010605 A 5340 3755847502N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FITTING AT STA.1230 AND L33R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001090400043 20010904 00043 WP 2001 9 4 RRXA11231 1 20010606 A 5730 42543310 DOUBLER DOUG DC8 DC873F 302199F WP LT WING CHAFED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CHAFED DAMAGE TO LT I/B SLOT UPPER DOOR AT STA. XS250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 57-2-0 FIG.6. 2 L 7 4 4F RT 4A25 2001090400044 20010904 00044 WP 2001 9 4 RRXA11236 1 20010607 A 5210 5597646 INTERCOSTAL DOUG DC8 DC873F 302199F WP PAX DOOR TOOL DAMAGE A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND DRILL DAMAGE TO FWD ENTRY DOOR TORQUE BOX, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RE MOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-21D AND DWG 5 597646. 2 L 7 4 4F RT 4A25 2001090400045 20010904 00045 WP 2001 9 4 RRXA11237 1 20010607 A 5320 4614662 STRUCTURE DOUG DC8 DC873F 302199F WP TORQUE BOX DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND DRILL DAMAGE TO FWD ENTRY DOOR TORQUE BOX TEE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM . REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-1-20, AND DW G 4614602. 2 L 7 4 4F RT 4A25 2001090400046 20010904 00046 WP 2001 9 4 RRXA11239 1 20010608 A 5330 5801531 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DENTED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND DENT DAMAGE TO SKIN AT STA.165 AND L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMO VED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0 FIG.2. 2 L 7 4 4F RT 4A25 2001090400047 20010904 00047 WP 2001 9 4 RRXA11246 1 20010609 A 5330 4645290 PANEL DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND HOLE DAMAGE TO FUSELAGE PANEL BETWEEN MLG WW DOORS AT STA.857-980, DAMAGE EXCEEDED LIMI TATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM51-1-2 1, 51-20D. 2 L 7 4 4F RT 4A25 2001090400048 20010904 00048 WP 2001 9 4 RRXA11247 1 20010609 A 5320 4645535503 CLIP DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO CTR KEEL LOWER DOOR FRAME ATTACH CLIP AT STA.958, DAMAGE EXCEEDED LIMIT ATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-2 1, 51-1-20D. 2 L 7 4 4F RT 4A25 2001090400049 20010904 00049 WP 2001 9 4 RRXA11249 1 20010610 A 5320 5597646 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE TOOL DAMAGE A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND DRILL DAMAGE TO FWD ENTRY DOOR TORQUE BOX DOOR JAMB AT STA.70 AND L18L-L19L, DAMAGE EXC EEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D AND DSK606-944. 2 L 7 4 4F RT 4A25 2001090400050 20010904 00050 WP 2001 9 4 RRXA11258 1 20010610 A 5210 435434632 DOUBLER DOUG DC8 DC873F 302199F WP PAX DOOR TOOL DAMAGE A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND DRILL DAMAGE TO FWD ENTRY DOOR FWD LOWER CORNER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-3 FIG.1, 52-2-2 FIG.7, 51-1-21. 2 L 7 4 4F RT 4A25 2001090400051 20010904 00051 WP 2001 9 4 RRXA11274 1 20010612 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE TOOL DAMAGE A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND DRILL DAMAGE TO D-PIT TORQUE BOX WEB INTERCOSTAL AT STA.1440 AND L32R-L34R, DAMAGE EXC EEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0 FIG.1F AND DWG 5640231 AND DWG 5616674. 2 L 7 4 4F RT 4A25 2001090400052 20010904 00052 WP 2001 9 4 RRXA11276 1 20010613 A 5320 5597646111 WEB DOUG DC8 DC873F 302199F WP STA70 L11L-L12L TOOL DAMAGE A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND DRILLED DAMAGE TO FWD ENTRY DOOR TORQUE BOX WEB AT STA.70 AND L11L-L22L, DAMAGE EXCEED ED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SR M 51-1-21, 51-1-20D AND DWG 5597646-111. 2 L 7 4 4F RT 4A25 2001090400053 20010904 00053 WP 2001 9 4 RRXA11282 1 20010614 A 5210 9754002206 TRACK DOUG DC8 DC873F 302199F WP DOOR FRAME CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO C-PIT CROSS SLIDE AFT JAMB TRACK GUIDE AT STA.1220 AND L32L, DAMAGE EXC EEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D, 51-3-0 AND DHSK606-070-1. 2 L 7 4 4F RT 4A25 2001090400054 20010904 00054 WP 2001 9 4 RRXA11291 1 20010615 A 5712 5769857 RIB DOUG DC8 DC873F 302199F WP LT WING CHAFED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CHAFF DAMAGE TO LT WING CENTER L/E RIB AT STA. XS510, DAMAGE EXCEEDED LIMITATIONS IAW D C-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0 FIG2A. 2 L 7 4 4F RT 4A25 2001090400055 20010904 00055 WP 2001 9 4 RRXA11292 1 20010615 A 5712 5769859 RIB DOUG DC8 DC873F 302199F WP LT WING CHAFED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CHAFF DAMAGE TO LT WING L/E RIB AT STA. XS250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM . REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0 FIG2. 2 L 7 4 4F RT 4A25 2001090400056 20010904 00056 WP 2001 9 4 RRXA11293 1 20010615 A 5753 5642970 STRUCTURE DOUG DC8 DC873F 302199F WP RT WING TE FLAP CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO RTO/B FLAP I/B TEE ANGLE AT STA. XF164, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0 FIG2. 2 L 7 4 4F RT 4A25 2001090400057 20010904 00057 WP 2001 9 4 RRXA11308 1 20010618 A 5311 97540020205 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO A-PIT CROSS SLIDE DOOR JAMB FLOOR SUPPORT AT STA.280 AND L32L, DAMA GE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IA W DC-8 SRM 51-3-0, 51-1-21. 2 L 7 4 4F RT 4A25 2001090400058 20010904 00058 WP 2001 9 4 RRXA11309 1 20010620 A 5320 564091514 STIFFENER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO HORIZONTAL STIFFNERS IN RT MLG W/W AT STA.980, DAMAGE EXCEEDED LIMI TATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1- 20D AND DWG 5640915. 2 L 7 4 4F RT 4A25 2001090400059 20010904 00059 WP 2001 9 4 RRXA11310 1 20010620 A 5320 564091512 STIFFENER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO HORIZONTAL STIFFNERS IN RT MLG W/W AT STA.980, DAMAGE EXCEEDED LIMI TATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1- 20D AND DWG 5640915. 2 L 7 4 4F RT 4A25 2001090400060 20010904 00060 NM 2001 9 4 CALA0100829 1 20010902 A 5320 ANGLE BOEING 737 7373T0 1384582 NM R/H W/W CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND ATTACH ANGLE FOR R/H AFT I/B WHEEL WELL FAIRING CORRODED ON FORWARD CURVED ATTACH POINTS. THE ATTACH AN GLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001090400061 20010904 00061 EU 2001 9 4 01FDEA00799 1 20010903 A 5400 PYLON AIRBUS 310 A310222 3930315 EU LOWER SPAR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 421FE 342 NR 102 CRACK ON LH PYLON LWR SPAR BETWEEN RIB 9 & 10. ** S/D ** COMING 2 L 7 2 4F RT A35EU 2001090400062 20010904 00062 EU 2001 9 4 01FDEA00787 1 20010903 A 5400 PYLON AIRBUS 310 A310222 3930315 EU LOWER SPAR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 421FE 342 NR 100 CRACK ON RH PYLON LWR SPAR BETWEEN RIB 9 & 10. ** S/D ** COMING 2 L 7 2 4F RT A35EU 2001090400063 20010904 00063 EU 2001 9 4 01FDEA00800 1 20010903 A 5400 PYLON AIRBUS 310 A310222 3930315 EU LOWER SPAR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 421FE 342 NR 103 CRACK ON LH PYLON LWR SPAR BETWEEN RIB 6 & 7. ** S/D ** COMING 2 L 7 2 4F RT A35EU 2001090400064 20010904 00064 WP 2001 9 4 RRXA11311 1 20010610 A 5230 37540511N FITTING DOUG DC8 DC873F 302199F WP CARGO DOOR CHAFED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CHAFF DAMAGE A-PIT CROSS SLIDE LOWER LATCHES, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PARTS AND INSTALLED IAW DC-8 SRM 53-20-0 FIG1F, 51-1-21. 2 L 7 4 4F RT 4A25 2001090400065 20010904 00065 WP 2001 9 4 RRXA11317 1 20010621 A 5340 3755822503N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND ELONGATION DAMAGE TO A-PIT CROSS SLIDE TORQUE BOX BATH TUB FITTING HOLES AT STA.320 AND L29L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND I NSTALLED IAW DC-8 SRM 53-20-0FIG2D. 2 L 7 4 4F RT 4A25 2001090400066 20010904 00066 WP 2001 9 4 RRXA11318 1 20010623 A 5753 565228505 VANE DOUG DC8 DC873F 302199F WP LT WING TE FLAP CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LT WING NR 1 FLAP VANE FITTING, DAMAGE EXCEEDED LIMITATIONS IAW DC- 8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTAKLLED IAW DC-8 MM 27-51-10. 2 L 7 4 4F RT 4A25 2001090400067 20010904 00067 WP 2001 9 4 RRXA11319 1 20010623 A 7110 42543097001 DOUBLER DOUG DC8 DC873F 302199F WP NR 3 ENG COWL CHAFED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CHAFF DAMAGE TO NR 3 ENGINE I/B FAN COWL INNER DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC -8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 71-2-8 PAR.5C. 2 L 7 4 4F RT 4A25 2001090400068 20010904 00068 WP 2001 9 4 RRXA11321 1 20010624 A 5320 3770379 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO INTERCOSTAL AT STA.355, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOV ED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 57-3-3, 51-1-20D. 2 L 7 4 4F RT 4A25 2001090400069 20010904 00069 WP 2001 9 4 RRXA11326 1 20010702 A 5330 5779936 SKIN DOUG DC8 DC873F 302199F WP STA1400 L33-34R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO D-PIT LOWER R/H FUSELAGE SKIN AT STA.1400 AND L34R-L33R, DAMAGE EXC EEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DH SK 606-616. 2 L 7 4 4F RT 4A25 2001090400070 20010904 00070 WP 2001 9 4 RRXA11327 1 20010702 A 5730 010529002 SKIN DOUG DC8 DC873F 302199F WP WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LOWER WING SKIN STRINGER 64L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DMSK606-470. 2 L 7 4 4F RT 4A25 2001090400071 20010904 00071 WP 2001 9 4 RRXA11330 1 20010703 A 5730 576960039 DOUBLER DOUG DC8 DC873F 302199F WP LT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LT WING L/E INTERNAL DOUBLER AT STA. XFS572.51, DAMAGE EXCEEDED LIMITAT IONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 2001090400072 20010904 00072 WP 2001 9 4 RRXA11331 1 20010708 A 5311 5597646 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FRAME AT STA.55 AND L24L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REM OVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-0 FIG.2. 2 L 7 4 4F RT 4A25 2001090400073 20010904 00073 WP 2001 9 4 RRXA11350 1 20010610 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND D PIT DOOR FRAME AT FUSELAGE SKIN CRACKED, GOUGED AND A PIECE MISSING. TRIMMED OUT DAM AGE, NDT NO FURTHER CRACKS EXIST. FABRICATED DOUBLER AND 2 FILLERS PER SK 873-052. INSTALLED FILLERS AND DOUBLER IAW S K 873-052, SRM 51-1-2, 51-1-26. 2 L 7 4 4F RT 4A25 2001090400074 20010904 00074 WP 2001 9 4 RRXA11351 1 20010611 A 5240 5755530 SKIN DOUG DC8 DC873F 302199F WP SERVICE DOOR CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND SKIN ON RT FWD SERVICE DOOR, CORROSION OUT OF LIMITS. CUT OUT DAMAGE AREA IAW SRM 52-2 -0 FIG 4, FABRICATED& INSTALLED REPLACEMENT PART IAW SRM 52-2-0 FIG 4 & 52-3-1 FIG 3 AND 51-1-21, 2 L 7 4 4F RT 4A25 2001090400075 20010904 00075 WP 2001 9 4 RRXA11354 1 20010617 A 5330 5779936 SKIN DOUG DC8 DC873F 302199F WP L21L STA 1500 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND WHILE REMOVING CORROSION AT STA 1500 L21L, FOUND AREA OUT OF LIMITS IAW SRM 51-1-8, 53- 2-0 FIG 1F. FABRICATED REPLACEMENT PART AND REPAIR PER DHSK 873-702 2 L 7 4 4F RT 4A25 2001090400076 20010904 00076 WP 2001 9 4 RRXA11355 1 20010617 A 5330 5779936 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND WHILE REMOVING CORROSION N/R 85131 FOUND AREA OUT OF LIMIT IAW SRM51-1-8, 53-2-0 FIG 1F . FABRICATED REPLACEMENT PART AND INSTALLED IAW DHSK 873-702. 2 L 7 4 4F RT 4A25 2001090400077 20010904 00077 WP 2001 9 4 RRXA11356 1 20010618 A 5730 5763353 SKIN DOUG DC8 DC873F 302199F WP RT WING CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND RT WING UPPER SURFACE CORROSION FWD O/B AILERON O/B END. XRS 763 TO XRS 764. REPAIR D OUBLER PER SRM 57-2-0 FIG 2A AND DWG 5763353 2 L 7 4 4F RT 4A25 2001090400078 20010904 00078 WP 2001 9 4 RRXA11361 1 20010620 A 5330 5779936 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND FUSELAGE EXT SKIN STA 1690 L18L GOUGED. REPAIRED SKIN IAW 8110-3 APPROVED DH S/L 873-1 33 2 L 7 4 4F RT 4A25 2001090400079 20010904 00079 WP 2001 9 4 RRXA11366 1 20010622 A 5730 5803916 DOUBLER DOUG DC8 DC873F 302199F WP RT WING SEPARATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND RT WING L/E OB L/E HAS FASTENER PULLING THROUGH SKIN STA XW485. REPAIR DAMAGE AREA IAW DC8 SRM 51-1-21, 51-1-20 AND DHSK 873-917 2 L 7 4 4F RT 4A25 2001090400080 20010904 00080 WP 2001 9 4 RRXA11370 1 20010623 A 5340 37558401 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND C PIT BATH TUB FITTING AT STA 1160 L33R I/B TO 33R O/B HAS HEAVY CORROSION. REMOVED BA TH TUB FITTING PER SRM 51-1-20D, REMOVED CORROSION ON BATH TUB FITTING MOUNT POINT. THICKNESS PER NDI SPM 04.00.06 FOUN D TO BE WITHIN LIMITS PER SRM 53-2-0 FIG 1F. TREATED AND PRIMED AREA PER SRM 51-1-8. FABRICATED SPLICES PER SRM 53-2-0 FIG 2D. INSTALLED REPLACEMENT BATH TUB FITTING PER SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001090400081 20010904 00081 WP 2001 9 4 RRXA11376 1 20010626 A 5340 3755842 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND C PI BATH TUB FITTING STA 1180 L33R - L34R HAS LITE CORROSION. REMOVED BATH TUB IAW SR M 51-1-20D. REMOVED CORROSION, TREATED AND PRIMED IAW SRM 51-1-8 AND 53-2-0 FIG 1F. INSTALLED REPLACEMENT PARTS IAW SR M51-1-20 AND DWG 3755841 2 L 7 4 4F RT 4A25 2001090400082 20010904 00082 WP 2001 9 4 RRXA11389 1 20010701 A 5512 5644310 SKIN DOUG DC8 DC873F 302199F WP HORIZONTAL STAB CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND CORROSION ON LT HORIZ STAB L/E. REPAIRED PER DHSK 873-337 AT XFS 176. 2 L 7 4 4F RT 4A25 2001090400083 20010904 00083 WP 2001 9 4 RRXA11391 1 20010702 A 5340 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE MISDRILLED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND C-PIT FITTING FWD SIDE OF FRAME 1160 L35L IS MISDRILLED IN AFT UPPER RADIUS. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001090400084 20010904 00084 WP 2001 9 4 RRXA11398 1 20010704 A 5510 5652086 PAN DOUG DC8 DC873F 302199F WP HORIZONTAL STAB CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND LT HORIZ STAB O/B MOUNT PAN CRACKED AT STA XE195 REMOVED MOUNT PAN, REPAIRED AND INSTA LLED IAW SRM 51-1-21, DWG 5652086-D, PS 10-301 AND SRM 51-3-0 2 L 7 4 4F RT 4A25 2001090400085 20010904 00085 WP 2001 9 4 RRXA11402 1 20010707 A 5347 54755395 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND CORROSION ON SEAT TRACK FS STA 600 LBL 48. REMOVED DAMAGED AREA, FABRICATED REPLACEMEN T SECTION AND INSTALLED IAW 53-2-3 FIG 14 AND SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001090400086 20010904 00086 WP 2001 9 4 RRXA11404 1 20010709 A 5313 5773863111 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND L23L STA 8 HAS CORROSION OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPLACEMENT PART IAW DC8 SRM 51-1-20D DHSK 873-387 2 L 7 4 4F RT 4A25 2001090400087 20010904 00087 WP 2001 9 4 RRXA11405 1 20010710 A 5340 3754930IN FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND C-PIT BACK UP FITTING HAS CORROSION OUT OF LIMITS AT STA 1206 L33R. REMOVED AND REPLAC ED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001090400088 20010904 00088 WP 2001 9 4 RRXA11406 1 20010712 A 5347 2772666 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND CORROSION ON SEAT TRACK STA 1240 RBL 48. REMOVED DAMGED AREA AND FABRICATED REPLACEMEN T PART AND INSTALLED IAW SRM 53-2-3 FIG 14 AND SRM 51-3-00. 2 L 7 4 4F RT 4A25 2001090400089 20010904 00089 WP 2001 9 4 RRXA11407 1 20010713 A 5340 3754930 FITTING DOUG DC8 DC873F 302199F WP CARGO BAY CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND C-PIT BACK UP FITTING FOR NR 4 LWR T LATCH CORRODED AROUND FASTENERS STA 1215 BETWEEN L 33R I/B AND L33R O/B. REMOVED CORROSION FOUND TO BE OUT OF LIMITSA. SRM 51-1-8 AND 53-2-01F. RECEIVED BACK UP FITTING AND CLIP PER SRM 51-1-20D. INSTALLED FITTING AND CLIP IAW DC8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001090400090 20010904 00090 WP 2001 9 4 RRXA11409 1 20010713 A 5340 3754930IN FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND C PIT BACK UP FITTING FOR #6 LWR T LATCH CORRODED STA 1232 BETWEEN L33R I/B AND L33R O/ B. REMOVED CORROSION IAW DC8 SRM 51-1-8 MATERIAL LOSS OUT OF LIMITS IAW SRM 53-20 FIG F. REMOVED AND REPLACED BACK UP FITTING AND CLIS REF SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001090400091 20010904 00091 WP 2001 9 4 RRXA11410 1 20010714 A 5755 57075314 FITTING DOUG DC8 DC873F 302199F WP RT WING SPOILER CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND RT WING I/B GROUND SPOILER FITTING CRACKED. REMOVED FITTING PER SRM 51-1-21, REPAIRED BY WELDING PER DPS 10.225 AND ENGINEERING SUPPORT. ACCOMPLISHED PENETRENT INSP PER OPS 10.225 NO CRACKS. REINSTALLED PART IAW DC8 SRM 51-1-21 AND 51-1-21D. 2 L 7 4 4F RT 4A25 2001090400092 20010904 00092 WP 2001 9 4 RRXA11414 1 20010715 A 5340 37576001 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND STA 70 RBL 55 L27R HAS TIE FITTING CORRODED I/B FLANG BROKEN OFF. REMOVED DAMAGED PART FABRICATED REPLACEMENT PART AND INSTALLED ON NR 85752 IAW SRM 51-1-21 AND 51-1-20D AND DWG G37571.00 2 L 7 4 4F RT 4A25 2001090400093 20010904 00093 WP 2001 9 4 RRXA11421 1 20010724 A 7160 D51B118101 STRUCTURE DOUG DC8 DC873F 302199F WP NR 3 ENGINE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND NR 3 ENGINE RT INLET STRAKE LWR MOUNTBRACKET CRACKED. REMOVED DAMAGED BRACKET, FABRICA TED AND INSTALLED NEW BRACKET IAW DWG D51B11810 AND SRM 51-1-21 2 L 7 4 4F RT 4A25 2001090400094 20010904 00094 WP 2001 9 4 RRXA11422 1 20010726 A 5313 3648667 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND LONGERON 30R CRACKED AND CORRODED BETWEEN STA 8-70. REPLACED LONGERON 30R DUE TO CRACK AND CORROSION FROM STA 8 - 70 PER DC8 SRM 51-1-21, 51-1-20D AND DWG 3648667 2 L 7 4 4F RT 4A25 2001090400095 20010904 00095 WP 2001 9 4 RRXA11423 1 20010726 A 5330 5649028U DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND CORROSION ON INTERNAL DOUBLER STA 35-55 L26R TO L30R. REPLACED INTERNAL DOUBLER STA 35 -55 L26R TO L30R DUE TO CORROSION. REF DC8 SRM 51-1-21,51-1-20D, 53-1-0 AND DWG5649028 2 L 7 4 4F RT 4A25 2001090400096 20010904 00096 WP 2001 9 4 RRXA11424 1 20010729 A 5320 5753157 PLATE DOUG DC8 DC873F 302199F WP STA 574 L24R CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND LONGERON AND SKIN CORRODED AT L24 R TO L22R AT STA 574 AT APU BLANKING PLATE. MADE REP AIR BY BLENDING OUT AREA, FABRICATING REPAIR PART AND INSTALLING IAW DHSK 873-536 2 L 7 4 4F RT 4A25 2001090400097 20010904 00097 WP 2001 9 4 RRXA11431 1 20010729 A 5311 55976415 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND FRAME AT STA 70 CORRODED SEVERAL SPOTS FROM L21L TO L21R. REPLACED PER DC8 SRM 53-2-0 FIG 2 2 L 7 4 4F RT 4A25 2001090400098 20010904 00098 WP 2001 9 4 RRXA11432 1 20010729 A 5313 3750257 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND L31L CORRODED BEYOND LIMITS AT STA 450-520. REPLACED SECTION PER DHSK 873-508 2 L 7 4 4F RT 4A25 2001090400099 20010904 00099 WP 2001 9 4 RRXA11434 1 20010731 A 5520 56556943 PANEL DOUG DC8 DC873F 302199F WP LT ELEVATOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND LT ELEVATOR LEADING EDGE PANEL 73 CRACKED. REPLACED PANEL REF DC8 MM 20-15-0 2 L 7 4 4F RT 4A25 2001090400100 20010904 00100 WP 2001 9 4 RRXA11435 1 20010709 A 5330 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND FWD ACCESSARY COMPARTMENT INTERNAL DOUBLER CORRODED BEYOND LIMITS. REPAIRED PER DHSK 8 73-314. PART WAS AN OLD REPAIR DOUBLER NOT A DAC PART. 2 L 7 4 4F RT 4A25 2001090400101 20010904 00101 WP 2001 9 4 RRXA11437 1 20010730 A 5340 5750092505 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND LT W/W TRAPAZOID FITTING CRACKED. REPLACED PER DAC DWG 5750127, DC8 SRM 51-1-21, 51-1- 20D AND OHM 13-1-6 2 L 7 4 4F RT 4A25 2001090400102 20010904 00102 WP 2001 9 4 RRXA11443 1 20010730 A 5753 37511591 LINK DOUG DC8 DC873F 302199F WP FUSELAGE CHAFED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND RT FLAP FWD LINK HINGE WITH EXCESSIVE CHAFED DAMAGE AT STA 340. REPLACED RH FLAP FWD L INK HINGE AT STA 340. 2 L 7 4 4F RT 4A25 2001090400103 20010904 00103 WP 2001 9 4 RRXA11445 1 20010801 A 5753 5642060 ANGLE DOUG DC8 DC873F 302199F WP LT WING TE FLAP CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND LT I/B FLAP I/B END AT T/E RT MAIN ANGLE CRACKED. REMOVED CRACKED DOUBLER, FABRICATED AND INSTALLED RT MAIN ANGLE IAW SRM 57-2-0 FIG 2, SRM 51-1-21 AND DWG 5642060 2 L 7 4 4F RT 4A25 2001090400104 20010904 00104 WP 2001 9 4 RRXA11448 1 20010804 A 5320 5753893 WEB DOUG DC8 DC873F 302199F WP FUSELAGE MISDRILLED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND C PIT TORQUE BOX FS 1180 WEB FRAME MISDRILLED L29R L30R. REMOVED WEB, FABRICATED REPLA CEMENT WEB AND INSTALLED IAW DWG 5753893 AND SRM 51-1-8, 51-1-21, 51-1-20D AND 51-9-01. 2 L 7 4 4F RT 4A25 2001090400105 20010904 00105 WP 2001 9 4 RRXA11454 1 20010807 A 5730 5769857 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND RT WING L/E SKIN CRACKED AT STA XFS300. REPAIRED SKIN IAW 8110-3 APPROVED DHSK 873-883 2 L 7 4 4F RT 4A25 2001090400106 20010904 00106 WP 2001 9 4 RRXA11455 1 20010807 A 5347 54755395 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND CABIN SEAT TRACK HAS CORROSION AT STA FS 610 AT RBL 48. REPAIRED SEAT TRACK IAW DC8 SR M 53-23 FIG 8A. 2 L 7 4 4F RT 4A25 2001090400107 20010904 00107 WP 2001 9 4 RRXA11459 1 20010808 A 5750 56429704 WEDGE DOUG DC8 DC873F 302199F WP LT WING TE FLAP DENTED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND LT WING O/B FLAP I/B TRAILING EDGE WEDGE DENTED AND HOLE, STA XRS 351 TO 380. REMOVED WEDGE, FABRICATED AND INSTALLED IAW SRM 51-1-21,51-1-21D AND DWG 56429704 2 L 7 4 4F RT 4A25 2001090400108 20010904 00108 NM 2001 9 4 SPAA0100046 1 20010826 A 3350 1000679 LIGHT BOEING 737 7372Y5 1384554 NM INOPERATIVE A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 712S 23038 L-1 DOOR PORTABLE EMERGENCY EXIT LIGHT DIM, DISCOVERED DURING ACCOMPLISHMENT OF PREFLIGHT CHECK. REPLACED EXIT LIGHT IAW B737MM 33-51-101, OPERATIONAL CHECKS GOOD. 2 L 7 2 4U RT A16WE 2001090400109 20010904 00109 WP 2001 9 4 RRXA11460 1 20010811 A 5330 5779934 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 DURING A MAINTENANCE VISIT FOUND FUSELAGE SKIN DAMAGED AT APPROX STA 240 BELOW L32L. REMOVED DAMAGE/HFEC INSP NO CRACKS NOTED. FABRICATED REPAIR PARTS AND INSTALLED IAW DC8 SRM 53-2-1 FIG 7 2 L 7 4 4F RT 4A25 2001090400110 20010904 00110 WP 2001 9 4 AALA20011518 1 20010723 A 5100 SPAR DOUG DC9 DC982 3022082 WP A AALA K NONE O OTHER IN INSP/MAINT 1 NM 01 428AA 49340 TUL - FOUND INTERIM REPAIR ACCOMPLISHED ON RIB AFT FLANGE FRONT SPAR BETWEEN SLAT TRACKS NR 5 AND NR 6 RIGHT WING. REPL CED REAR HALF WITH NEW, FRONT SPAR, BETWEEN SLAT TRACKS 5 AND 6, SRM 51-01. (M) 2 L 7 2 4F A6WE 2001090400111 20010904 00111 WP 2001 9 4 AALA20011529 1 20010718 A 5300 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 219 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 438AA 49456 TUL - FOUND NR 2 SEAT TRACK HAS CORROSION IN CHANNEL, BS 219. CUT OUT DAMAGED SEAT TRACK FROM BS 200-246 PER SRM 53-05 FIG 4F. (M) 2 L 7 2 4F RT A6WE 2001090400112 20010904 00112 WP 2001 9 4 AALA20011532 1 20010713 A 5300 SKIN DOUG DC9 DC983 3022083 WP BS 1305 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 438AA 49456 TUL - FOUND DEEP GOUGE IN FUSELAGE SKIN AT STATION 1305 ABOVE LONGERON 19R. INSTALLED SCUFF PLATE PER AARD 53-30-00-8. (M) 2 L 7 2 4F RT A6WE 2001090400113 20010904 00113 WP 2001 9 4 AALA20011552 1 20010801 A 5600 59515841 WINDOW DOUG DC9 DC982 3022082 WP CABIN CRACKED A AALA A UNSCHED LANDING J O WARNING INDICATION OTHER CR CRUISE 1 SW 21 7538A 49992 TUL - FLT 1318 - EN ROUTE DFW-IND, AIR INTERRUPTED TO TUL DUE TO CRACKED WINDOW AT 12A. LANDED TUL WITHOUT INCIDENT. R EPLACED CRACKED WINDOW AT 12A. PRESSURIZATION AND LEAK CHECK OK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002120200077 20021202 00077 NM 2002 12 2 AALA20011514 1 20010725 A 2597 WIRE BOEING 767 767323 1385205 NM GALLEY SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 359AA 24040 MXP - DURING OVERNIGHT MAINTENANCE, BUSINESS CLASS GALLEY STORAGE AREA (503) HAS ELECTRICAL SHORT TO RIGHT SIDE METAL ST RIP. PULLED AND COLLARED OPTIONAL CIRCUIT BREAKER AT GALLEY ELECTRICAL PANEL. NO FURTHER ELECTRICAL FAULTS. SYSTEM GR OUND CHECKED NORMAL OPERATION. TECH SERVICE PROVIDING FOLLOW-UP ACTION. (M) 2 L 7 2 4F RT A1NM 2001090400114 20010904 00114 NM 2001 9 4 AALA20011545 1 20010731 A 3350 HARNESS BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 392AN 29429 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT ON SEAT 31B INOPERATIVE. RECONNECTED HARNESS TO SEAT. SYSTEM GROUN D CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001090400115 20010904 00115 NM 2001 9 4 AALA20011550 1 20010802 A 3350 P402005111 MODULE BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 686AA 25343 AUS - DURING OVERNIGHT MAINTENANCE, CABIN EMERGENCY EXIT ESCAPE PATH LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT MODULE AND BATTERY PACKS. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001090400116 20010904 00116 NM 2001 9 4 TSAA0133104 1 20010804 A 3300 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN INOPERATIVE A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED NR 2 FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2001090400117 20010904 00117 NM 2001 9 4 TSAA0133103 1 20010803 A 3350 86210066 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN INOPERATIVE A K NONE L NO TEST IN INSP/MAINT 1 WP 13 804AL 21719 REPLACED NR 2 AND NR 3 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4F A16WE 2001090400118 20010904 00118 NM 2001 9 4 TSAA0133105 1 20010803 A 3350 86210066 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN INOPERATIVE A K NONE L NO TEST IN INSP/MAINT 1 WP 13 809AL 21720 REPLACED NR 3 EMERGENCY FLOOR BATTERY PACKS DUE TO INOPERATIVE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2001090400119 20010904 00119 EA 2001 9 4 REXA01010 1 20010607 A 3500 380270260 HOSE CNDAIR CL600 CL6002B19 EA RUPTURED A REXA K NONE O OTHER TX TAXI/GRND HDL 1 SO 25 8409N 2220 7409 OBSERVER SEAT POSITION OXYGEN MASK SUPPLY HOSE RUPTURED AND SEPARATED FROM FITTING. REMOVED AND REPLACED HOSE. THIS WA S FOUND WHILE INVESTIGATING A DEPLETED CREW OXYGEN SYSTEM. (M) 2 L 7 2 4F RT A21EA 2001090400120 20010904 00120 EA 2001 9 4 REXA01011 1 20010717 A 3500 380270260 HOSE CNDAIR CL600 CL6002B19 EA RUPTURED A REXA K NONE O OTHER TX TAXI/GRND HDL 1 SO 25 8492C 609 7492 OBSERVER SEAT POSITION OXYGEN MASK SUPPLY HOSE RUPTURED AND SEPARATED FROM FITTING. REMOVED AND REPLACED HOSE. THIS WA S FOUND WHILE INVESTIGATING A DEPLETED CREW OXYGEN SYSTEM. (M) 2 L 7 2 4F RT A21EA 2001090400121 20010904 00121 EA 2001 9 4 REXA01013 1 20010717 A 3500 380270260 HOSE CNDAIR CL600 CL6002B19 EA RUPTURED A REXA K NONE O OTHER TX TAXI/GRND HDL 1 SO 25 8477R 53 7477 OBSERVER SEAT POSITION OXYGEN MASK SUPPLY HOSE RUPTURED AND SEPARATED FROM FITTING. REMOVED AND REPLACED HOSE. THIS WA S FOUND WHILE INVESTIGATING A DEPLETED CREW OXYGEN SYSTEM. (M) 2 L 7 2 4F RT A21EA 2001090400122 20010904 00122 NM 2001 9 4 GAIA01296ST 1 20010813 A 5300 FRAME BOEING 727 727223 1384074 NM BS 600 DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 858AA 21085 DURING ROUTINE MAINTENANCE AT DFW, IT WAS DISCOVERED THAT THE BS 600 FRAME WAS DAMAGED AT STRINGER S17R. REPAIRED IAW B OEING 727 SRM 51-40-3, FIGURE 1 PAGE 3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001090400124 20010904 00124 NM 2001 9 4 SWAA012432 1 20010830 A 2731 DAS414A1508 BEARING BOEING 737 7373H4 1384600 NM RH ELEVATOR. WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 611SW 27697 DURING SCHEDULED C4 CHECK, RH ELEVATOR FAILED FREE PLAY CHECK. R&R RH ELEVATOR BEARING PER M M. 2 L 7 2 4F RT A16WE 2001090400125 20010904 00125 NM 2001 9 4 SWAA012433 1 20010830 A 2731 65C26384 TAB BOEING 737 7373H4 1384600 NM LH ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 611SW 27697 DURING SCHEDULED C4 CHECK, LH ELEVATOR TAB FAILED FREE PLAY CHECK. R&R LH ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2001090400126 20010904 00126 NM 2001 9 4 SWAA012434 1 20010825 A 5310 6546529 TIE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 500A, LBL 25. R&R SHEAR TIE P ER SRM. 2 L 7 2 4F A16WE 2001090400127 20010904 00127 NM 2001 9 4 SWAA012435 1 20010824 A 5310 BAC1498 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED D CHECK, FOUND STR CRACKED AT BS 807, STR 16L. REPAIRED STR PER SRM. 2 L 7 2 4F A16WE 2001090400128 20010904 00128 NM 2001 9 4 SWAA012436 1 20010829 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 630WN 27705 FWD ENTRY EMERGENCY EXIT LIGHT COVER LOOSE. R&R EXIT LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001090400129 20010904 00129 NM 2001 9 4 SWAA012438 1 20010829 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 10L. REPAIRED SKIN PER SR M. 2 L 7 2 4F RT A16WE 2001090400130 20010904 00130 NM 2001 9 4 SWAA012439 1 20010829 A 2781 W19000 WIRE BOEING 737 7373A4 1384585 NM COCKPIT BROKEN A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 679AA 23291 ( AIR TURNBACK ) .L/E FLAPS TRANSIT LIGHT ILLUMINATED DURING TAKE OFF. REPAIRED BROKEN GRD WIRE FOR UPL OCK POSITION SENSOR PER MM. 2 L 7 2 4F RT A16WE 2001090400131 20010904 00131 2001 9 4 SWAA012426 4 20010826 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 607SW 27927 FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001090400132 20010904 00132 NM 2001 9 4 SWAA012427 1 20010802 A 5313 6551698 SPLICE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED SPECIAL VISIT, FOUND STR SPLICE CRACKED ( 2 EA ) AT BS 908, STR'S 4L & 4R. R&R STR SPLICE PER SRM. 2 L 7 2 4F A16WE 2001090400133 20010904 00133 NM 2001 9 4 SWAA012428 1 20010824 A 5313 65C27314 CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED D CHECK, FOUND STR CLIPS CRACKED ( 2 EA ) AT STR 16L, BS 767 & BS 787. R&R STR CLIPS PER SRM. 2 L 7 2 4F A16WE 2001090400134 20010904 00134 NM 2001 9 4 SWAA012429 1 20010820 A 5313 65C27314 CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED D CHECK, FOUND STR CLIP CRACKED AT BS 1138, STR 13L. R&R STR CLIP PER SRM. 2 L 7 2 4F A16WE 2001090400135 20010904 00135 NM 2001 9 4 SWAA012430 1 20010829 A 2910 251A12105 ACTUATOR BOEING 737 7373H4 1384600 NM # 3 SPOILER LEAKING A SWAA D RETURN TO BLOCK K FLUID LOSS CL CLIMB 1 SW 07 318SW 23339 ( DIVERSION, DECLARED EMERGENCY )…………………………LOSS OF A SYSTEM HYDRAULIC FLUID. FOUND # 3 SPOILER ACTUA TOR LEAKING, R&R 'O' RINGS PER MM. 2 L 7 2 4F RT A16WE 2001090400136 20010904 00136 NM 2001 9 4 SWAA012417 1 20010828 A 5310 6558280 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 519SW 25318 DURING SCHEDULED D CHECK AT DALFORT, FOUND FUSELAGE FRAME SHEAR TIE CRACKED, BS 360, BETWEEEN STRINGERS 14R-15R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2001090400137 20010904 00137 NM 2001 9 4 SWAA012418 1 20010828 A 5310 BAC5602 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 519SW 25318 DURING SCHEDULED D CHECK AT DALFORT, FOUND FUSELAGE Z-FRAME CRACKED, BS 787, STRINGER 8R. R&R Z- FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2001090400138 20010904 00138 NM 2001 9 4 SWAA012419 1 20010827 A 5753 6546435278 FLAP BOEING 737 7373Q8 1384670 NM RH WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED C4 CHECK, FOUND RH WING OUTBD AFT T/E FLAP DELAMINATED AT LOWER SURFACE NEAR OUTBD END. R &R FLAP ASSY PER MM. 2 L 7 2 4F RT A16WE 2001090400139 20010904 00139 NM 2001 9 4 SWAA012420 1 20010828 A 5310 65C27314 CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED, BS 663, STRINGER 10R. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F A16WE 2001090400140 20010904 00140 NM 2001 9 4 SWAA012424 1 20010828 A 2560 65C33828 PANEL BOEING 737 7377H4 NM COCKPIT DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 762SW 27876 COCKPIT DOOR EGRESS PANELS WOULD NOT LATCH IN PLACE. SECURED EGRESS PANELS PER MM. 2 L 7 2 4F RT A16WE 2001090400141 20010904 00141 NM 2001 9 4 SWAA012425 1 20010828 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED (3 INCHES LONG) AT BS 727C, STRINGER 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001090400142 20010904 00142 NM 2001 9 4 SWAA012397 1 20010826 A 2560 P2070021 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN WEAK A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 608SW 27928 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY FLASHLIGHT BATTERY WEAK AT FWD CABIN. R&R FLA SHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2001090400143 20010904 00143 2001 9 4 SWAA012399 4 20010826 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 607SW 27927 FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001090400144 20010904 00144 NM 2001 9 4 SWAA012401 1 20010827 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED ( 5 LONG ) AT BS 947.6, STR 26L. REPAIR ED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001090400145 20010904 00145 NM 2001 9 4 SWAA012402 1 20010818 A 5330 6545768 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 380, BETWEEN STR 28R & 28L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001090400146 20010904 00146 NM 2001 9 4 SWAA012404 1 20010826 A 2731 BACB28AK04 BUSHING BOEING 737 7377H4 NM RH ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 705SW 27839 DURING SCHEDULED SERVICE CHECK, RH ELEVATOR TAB FAILED FREE PLAY CHECK. R&R HINGE BUSHINGS # 1 - # 4 PER MM. 2 L 7 2 4F RT A16WE 2001090400147 20010904 00147 NM 2001 9 4 SWAA012406 1 20010826 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED ( 2 EA ) AT STR 10R, BS 500, BS 524. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001090400148 20010904 00148 NM 2001 9 4 SWAA012407 1 20010826 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED ( 6 EA ) AT STR 10L, BS 374 - 500 D. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001090400149 20010904 00149 NM 2001 9 4 SWAA012408 1 20010816 A 5310 65C27314 CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED D CHECK, FOUND STR CLIPS CRACKED ( 3 EA ) AT BS 420, STR 10L, BS 747, STR 16L, BS 520, STR 19L. R&R STR CLIPS PER SRM. 2 L 7 2 4F A16WE 2001090400150 20010904 00150 NM 2001 9 4 SWAA012410 1 20010825 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 23R. REPAIRED SKIN PER S RM. 2 L 7 2 4F A16WE 2001090400151 20010904 00151 NM 2001 9 4 SWAA012411 1 20010826 A 5753 654643089 FLAP BOEING 737 7372H4 138448C NM LH WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED A2 CHECK, FOUND LH INBD T/E FORE FLAP DELAMINATED ON UPPER SURFACE. R&R FORE FLAP PER MM. 2 L 7 2 4F A16WE 2001090400152 20010904 00152 NM 2001 9 4 SWAA012412 1 20010826 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B, STR 18L. REPAIRED SKIN PER SR M. 2 L 7 2 4F A16WE 2001090400153 20010904 00153 NM 2001 9 4 SWAA012413 1 20010826 A 5314 6551656 STRINGER BOEING 737 7372H4 138448C NM LH MLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED A2 CHECK, FOUND STR 18A CRACKED ( 3/16 LONG ) AT LH MLG W/W. REPAIRED STR P ER SWA ACO. 2 L 7 2 4F A16WE 2001090400154 20010904 00154 NM 2001 9 4 SWAA012414 1 20010819 A 5310 6517583 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 376SW 26584 DURING SCHEDULED 1/4D CHECK AT DALFORT, FOUND BULKHEAD WEB CRACKED ( 4 EA ) AT BS 178, LBL 5, WL198.5, WL 183.5, WL 201 , & RBL 5, WL 201. 2 L 7 2 4F RT A16WE 2001090400155 20010904 00155 NM 2001 9 4 SWAA012383 1 20010825 A 3350 07912 COVER BOEING 737 7377H4 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 792SW 27887 EEPLS COVER LOOSE. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2001090400156 20010904 00156 NM 2001 9 4 SWAA012387 1 20010824 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED 1/2D CHECK, FOUND FWD CARGO DOOR CUTOUT FRAME CRACKED AT BS 440, STR 23R. REPAIRED FRAME PER SWA T1-653-044. 2 L 7 2 4F RT A16WE 2001090400157 20010904 00157 NM 2001 9 4 SWAA012388 1 20010824 A 5310 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL BEAM WEBS CRACKED ( 2 EA ) AT BS 180, WL 224, RBL 17.1 & BS 185, WL 227, LB L 17.1. R&R WEBS PER SRM. 2 L 7 2 4F RT A16WE 2001090400158 20010904 00158 NM 2001 9 4 SWAA012390 1 20010823 A 5310 65C27314 CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED D CHECK, FOUND STR CLIP CRACKED AT BS 616, STR 7L. R&R STR CLIP PER SRM. 2 L 7 2 4F A16WE 2001090400159 20010904 00159 NM 2001 9 4 SWAA012391 1 20010822 A 5310 6546543 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 616, STR 7L. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2001090400160 20010904 00160 NM 2001 9 4 SWAA012392 1 20010825 A 2731 BACB28AK04 BUSHING BOEING 737 7377H4 NM LH ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 750SA 29802 DURING SCHEDULED SERVICE CHECK, FOUND LH ELEVATOR TAB HINGE # 2, # 3, & # 4 BUSHINGS WORN. R&R TAB BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2001090400161 20010904 00161 NM 2001 9 4 SWAA012393 1 20010825 A 2731 BACB28AK04 BUSHING BOEING 737 7377H4 NM RH ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 750SA 29802 DURING SCHEDULED RON, FOUND RH ELEVATOR TAB # 4 HINGE BUSHING WORN. R&R TAB BUSHING PER MM. 2 L 7 2 4F RT A16WE 2001090400162 20010904 00162 NM 2001 9 4 SWAA012394 1 20010820 A 5310 65C27314 CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED D CHECK, FOUND ( 2 EA ) STR CLIPS CRACKED AT BS 747, STR 6R, & 7R. R&R STR CLIPS PER SRM. 2 L 7 2 4F A16WE 2001090400163 20010904 00163 NM 2001 9 4 SWAA012395 1 20010817 A 5510 65C27314 CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED D CHECK, FOUND ( 4 EA ) STR CLIPS CRACKED AT BS 727, STR 5R, 4R, 7L, 5L. R&R ST R CLIPS PER SRM. 2 L 7 2 4F A16WE 2001090400164 20010904 00164 NM 2001 9 4 SWAA012396 1 20010820 A 5310 65C27314 CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED D CHECK, FOUND STR CLIPS CRACKED AT BS 787, STR 7R, BS 807, STR 10L, BS 847, STR 4L. R&R STR CLIPS PER SRM. 2 L 7 2 4F A16WE 2001090400165 20010904 00165 NM 2001 9 4 AWXA0002208 1 20010822 A 5311 6546540550 WEB BOEING 737 737277 1384570 NM CENTER FUSE CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 D: Frame web cracked 3 ea places at fastener holes, BS 639, RBL 65, WL 206C: Removed cracked web, drilled and installed new web IAW B737 200 SRM 51-40-2 at BS 639, RBL 65, wl 206 2 L 7 2 4F RT A16WE 2001090400166 20010904 00166 NM 2001 9 4 AWXA0002210 1 20010830 A 3230 1030875 SOLENOID BOEING 737 7373B7 1384580 NM COCKPIT P-2PANEL FAILED A AWXA O OTHER O OTHER TO TAKEOFF 1 WP 28 332AW 23384 D: PHX - Air turnback/Emergency landing- Flt 344 - after take off from PHX to PVR the landing gear lever would not move to the gear up position. PHX tower informed AWA operations that tire debris was found on runway 25R. The flight crew req uested a flyby of the tower to see if the condition of the aircraft tires could be determined. 2 flybys were made and to wer personnel thought the L/H nose tire tread may have separated. The aircraft was put into a holding pattern to burn of f fuel. after suffecient fuel was burnt off the aircraft landed without incident. C: Inspection of the aircraft tires de terminded they were all good. After troubleshooting it was determined the landing gear lever latch solenoid had failed 2 L 7 2 4F RT A16WE 2001090400167 20010904 00167 NM 2001 9 4 SWAA012374 1 20010823 A 3350 612825 BATTERY BOEING 737 737317 138447P NM CABIN ERRATIC A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 EEPLS ILLUMINATING ERRATICALLY AFT OF ROW # 10. R&R BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2001090400168 20010904 00168 NM 2001 9 4 SWAA012375 1 20010822 A 5330 6545774 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 19R. REPAIRED SK IN PER SRM. 2 L 7 2 4F RT A16WE 2001090400169 20010904 00169 NM 2001 9 4 SWAA012376 1 20010818 A 5310 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 376SW 26584 DURING SCHEDULED 1/4D CHECK AT DALFORT, FOUND VERTICAL BEAM WEBS CRACKED ( 3 EA ) AT BS 178, LBL 17.1, WL 227, WL 232, WL 233. REPAIRED WEBS PER SRM. 2 L 7 2 4F RT A16WE 2001090400170 20010904 00170 NM 2001 9 4 SWAA012377 1 20010822 A 2731 BACB28AK04 BUSHING BOEING 737 7373H4 1384600 NM RH ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED BC4 CHECK, RH ELEVATOR TAB FAILED FREE PLAY INSPECTION. R&R # 1 TAB HINGE BUSHING PER MM. 2 L 7 2 4F RT A16WE 2001090400171 20010904 00171 NM 2001 9 4 SWAA012378 1 20010823 A 2751 6546435 FLAP BOEING 737 7373H4 1384600 NM LH WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 610WN 27696 DURING SCHEDULED C4 CHECK, FOUND LH OTBD AFT FLAP DELAMINATED AT INBD CORNER. R&R AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2001090400172 20010904 00172 NM 2001 9 4 SWAA012379 1 20010822 A 2731 654516618 ROD BOEING 737 7377H4 NM RH ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 725SW 27857 DURING SCHEDULED SERVICE CHECK, RH ELEVATOR TAB FAILED FREE PLAY CHECK. R&R ELEVATOR TAB CO NTROL ROD END & # 1 HINGE BUSHING PER MM. 2 L 7 2 4F RT A16WE 2001090400173 20010904 00173 NM 2001 9 4 SWAA012380 1 20010822 A 5310 BAC1498 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED D CHECK, FOUND STR 5R LWR CHORD CRACKED BETWEEN BS 1138-1145, . R&R STR SECTION PER SRM. 2 L 7 2 4F A16WE 2001090400174 20010904 00174 NM 2001 9 4 SWAA012381 1 20010822 A 5330 6550570 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED SERVICE CHECK, FOUND 4 INCH CRACK AT AFT SVC DOOR LWR FWD CORNER OF FUSELAGE SKIN CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001090400175 20010904 00175 NM 2001 9 4 MWEA011226 1 20010904 A 5310 9930612 WEB DOUG MD88 MD88 3023688 NM STATION 1287 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 AFT CARGO COMPARTMENT FLOOR WEB CRACKED BETWEEN STATION 1287 AND 1309 AT LONGERON 18 RIGHT. -- FABRICATED AND INSTALLE D NEW WEB. 2 L 7 2 4F RT A6WE 2001090400176 20010904 00176 NM 2001 9 4 MWEA011231 1 20010904 A 5320 9936600503 FLOORBOARD DOUG MD88 MD88 3023688 NM STATION 465 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 FORWARD PIT CENTER FLOOR PANEL STATION 465-522 IS DENTED AND DELAMINATING AROUND 3 FASTENER HOLES. -- FABRICATED AND I NSTALLED FLOOR BOARD. 2 L 7 2 4F RT A6WE 2001090400177 20010904 00177 NM 2001 9 4 MWEA011233 1 20010904 A 5320 99365981 FLOORBOARD DOUG MD88 MD88 3023688 NM STATION 218 DELAMINATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 FORWARD PIT CENTER FLOORBOARD STATION 218-332 DELAMINATED AROUND EDGES, MISSING LOWER SURFACE MATERIAL AND CORRODED AROU ND FASTENER HOLES. -- FABRICATED AND INSTALLED FLOOR BOARD. 2 L 7 2 4F RT A6WE 2001090400178 20010904 00178 NM 2001 9 4 MWEA011234 1 20010904 A 5320 99365991 FLOORBOARD DOUG MD88 MD88 3023688 NM STATION 370 DELAMINATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 FORWARD PIT CENTER FLOORBOARD STATION 370-427 IS DELAMINATED AROUND EDGES. -- REMOVED DAMAGED CORE MATERIAL AND EDGE F ILLED PER DAC DRAWING S4932106. 2 L 7 2 4F RT A6WE 2001090400179 20010904 00179 NM 2001 9 4 MWEA011236 1 20010904 A 5320 9936599503 FLOORBOARD DOUG MD88 MD88 3023688 NM STATION 332 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 FORWARD PIT CENTER FLOORBOARD STATION 332-370 CORRODED AROUND FASTENER HOLES. -- FABRICATED AND INSTALLED FLOORBOARD. 2 L 7 2 4F RT A6WE 2001090400180 20010904 00180 NM 2001 9 4 VNAA0108020 1 20010830 A 3600 406B000002 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LH FAILED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 438JS 9952 240 3056 DURING CLIMB THE LEFT BLEED VALVE NEVER OPENED. AFTER TROUBLESHOOTING WITH MAINTENANCE CONTROL THE CREW WAS ASKED TO RE TURN TO PIT. UPON ARRIVAL AT PIT, MAINTENANCE INSPECTED AND REPLACED THE FLOW CONTROL SHUT OFF VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 36-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASEDFOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001090400181 20010904 00181 NM 2001 9 4 VNAA0108014 1 20010823 A 2400 8160121 GENERATOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RH FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 427JS 10952 326 3039 AFTER BRINGING THE POWER UP FOR TAKE OFF, THE CREW RECEIVED A RIGHT HAND DC GENERATOR FAILED AND ABORTED TAKE OFF. AFTE R RETURNING TO THE GATE, MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND STARTER GENERATOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPARATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001090400182 20010904 00182 NM 2001 9 4 UPS01236754 1 20010827 A 5330 SKIN BOEING 727 727172C 1384058 NM BS800 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 916UP 19808 INSPECTION TYPE:C EVIDENCE OF CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE BS 300 BET WEEN S23R AND S24R CUT OUT MA DE IAW SRM, CORROSION REMOVED AND REPROTECTED, HFEC CARRIE D OUT NDF, REPAIRED IAW SMRO EO 2001-039-003 CAT B REPAIR SSI D REPOR T INITIATED. 2 L 7 3 4F A3WE 2001090400183 20010904 00183 NM 2001 9 4 UPS01236755 1 20010830 A 7810 06453010041 BRACKET BOEING 727 727172C 1384058 NM #1 ENGINE\ CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 916UP 19808 INSPECTION TYPE:C #1 ENGINE 1: O/B T/R AFT PANEL ATTACH BRACKET IS CRACKED, 2: FWD BRA CKET IS DISPLACED. REPLACED A FT BRACKET ND RESECURED FWD BRACKET IAW MM PROCEDURES. 2 L 7 3 4F A3WE 2001090400184 20010904 00184 NM 2001 9 4 UPS01236756 1 20010827 A 5310 WEB BOEING 727 727172C 1384058 NM BS293.5RBL23 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 916UP 19808 INSPECTION TYPE:C SUSPECT CRACK R/H NLG PRESSURE WEB RBL 23 BS 293.5 NDT TO LOCATE CRACK ENDS, STOP DRILLED AND REPA IRED IAW SRM 51-40-2 2 L 7 3 4F A3WE 2001091800200 20010918 00200 NM 2001 9 18 UPS01236763 1 20010831 A 3230 SUPPORT BRACKET BOEING 727 727247 138408F NM NLG ACTUATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE:PFLT NOSE GEAR LOCK ACTUATOR SUPPORT BRACKET IS CRACKED. SUPPORT BRACKET IS LOCATED ON AFT BULKHEAD WAL L. REMOVED NOSE GEAR LOCK ACTUATOR SUPPORT BRACKET. DRILLED UP NEW SUPPORT BRACKET AS REQUIRED. INSTALLED BRACKET IAW 727 SRM 51-30-02 2 L 7 3 4F A3WE 2001090500001 20010905 00001 SO 2001 9 5 COMA0110140 1 20010901 A 5330 12027875001 SKIN EMB 120 EMB120RT SO FUSELAGE CTR SEC DENTED A COMA K NONE C F.O.D. IN INSP/MAINT 1 SO 01 259CA 23056 1252 CREW REPORTS DENT ON RIGHT SIDE OF FUSELAGE BETWEEN FRAME 18 AND FRAME 19 AFTER DEBRIS STRUCK RIGHT PROPELLER.DAMAGED AR EA WAS CUT OUT. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED. WORK DONE IN ACCORDANCE WITH EMBRAER STRUCTURES REPAIR MANUAL CHAPTER 53-00-01. 2 L 7 2 4T RT A31SO 2001090500002 20010905 00002 NM 2001 9 5 2001F00251 1 20010810 A 5320 65B073887 DOUBLER BOEING 747 747230B 1384889 NM LAVATORY CORRODED A Q2SA K NONE O OTHER IN INSP/MAINT 1 GL 23 742SA 22669 DURING COMPLIANCE OF AD 99-08-10 FOUND EVIDENCE OF CORROSION ON UPPER SIDE, FORWARD LAVATORY, SERVICE DRAIN BOX. AFTER FURTHER INVESTIGATION AND REMOVING THE DRAIN VALVE BOX DOUBLER. IT WAS FOUND THAT THE DRAIN BOX DOUBLER ITSELF WAS CORR ODED. REMOVED FORWARD LAVATORY DRAIN BOX AND REPLACED WITH NEW IAW SRM 51-20-02 FIG 2 AND BOEING DWG NR 65B07388. (M) 2 L 7 4 4F A20WE 2001090500003 20010905 00003 NM 2001 9 5 2001F00252 1 20010809 A 3350 90053A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 804MA 22435 ON PREFLIGHT TRANSIT, FOUND RIGHT OVERWING INTERIOR EXT SIGN BLINKING ON/OFF. REMOVED AND REPLACED EMERGENCY LIGHT HOUS ING AND BATTERY PACK. OPS CHECKED IAW 33-50-01. RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 3 4F A3WE 2001090500004 20010905 00004 EA 2001 9 5 COMA0160663 1 20010901 A 2751 855D1009 SENSOR CNDAIR CL600 CL6002B19 EA LEFT WIGN FAULTY A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 785CA 4674 7326 FLIGHT #5725. DURING CRUISE FLIGHT RECEIVED A FLAP SYSTEM FAIL CAUTION WITH FLAP AT ZERO DEGREE POSITION, CREW DECLARED AN EMERGENCY AND LANDED AT DESTINATION CITY ATW SAFELY.REPLACED THE LEFT BRAKE AND POSITION SENSING UNIT. 2 L 7 2 4F RT A21EA 2001090500005 20010905 00005 NM 2001 9 5 2001F00253 1 20010809 A 2560 PA35319 FLASHLIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 804MA 22435 ON PREFLIGHT TRANSIT, FOUND BOTH AFT PORTABLE FLASHLIGHTS INOPERATIVE. REMOVED AND REPLACED AFT FLIGHT ATTENDANT PORTAB LE FLASHLIGHTS. OPS CHECKED IAW 25-60-00. RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 3 4F A3WE 2001090500006 20010905 00006 EA 2001 9 5 COMA0160664 1 20010903 A 3350 64643 LIGHT CNDAIR CL600 CL6002B19 EA A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 959CA 7116 FLIGHT #5527. DURING TAXI OUT FROM CVG CREW MEMBER NOTICED THE FLOOR EMERGENCY FLIGHT LIGHTING BETWEEN ROWS 2 AND 5 INO PERATIVE.REPLACED DAMAGED EMERGENCY FLOOR LIGHTING STRIP. 2 L 7 2 4F RT A21EA 2001090500007 20010905 00007 NM 2001 9 5 0103055503 1 20010820 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 503US 23192 DURING "H" CHECK FOUND CRACK IN FLOORBEAM UPPER CAP AT BS 700 LBL 45. REPAIRED PER EA 55-185931. 2 L 7 2 4F RT A2NM 2001090500008 20010905 00008 EA 2001 9 5 COMA0160665 1 20010903 A 3350 M8171417D35 LIGHT CNDAIR CL600 CL6002B19 EA A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 982CA 7168 FLIGHT #5558. DURING PRE-FLIGHT INSPECTION DISCOVERED THE ORANGE EMERGENCY LIGHT AND THE LEFT AND RIGHT FLUSH EXIT LIGH TED SIGNS INOPERATIVE.REPALCED TERMINAL BLOCK FOR AFFECTED EMERGENCY LIGHTING. 2 L 7 2 4F RT A21EA 2001090500009 20010905 00009 EA 2001 9 5 COMA0160666 1 20010902 A 2751 852D100MD91 ACTUATOR CNDAIR CL600 CL6002B19 EA RT WING FAULTY A COMA K NONE J WARNING INDICATION DE DESCENT 1 SO 01 967CA 12263 7134 FLIGHT #5837. DURING DESCENT INTO GSO RECEIVED A FLAP SYSTEM FAIL CAUTION AT 17 DEGREE FLAP POSITION.REPLACED THE RIGHT INBOARD FLAP, INBOARD ACTUATOR. 2 L 7 2 4F RT A21EA 2001090500010 20010905 00010 EA 2001 9 5 COMA0160667 1 20010902 A 2751 852D100MD91 ACTUATOR CNDAIR CL600 CL6002B19 EA RT WING FAULTY A COMA K NONE J WARNING INDICATION DE DESCENT 1 SO 01 967CA 12263 7134 FLIGHT #5837. DUIRNG DESCENT INTO GSO RECEIVED A FLAP SYSTEM FAIL CAUTION AT 17 DEGREE FLAP POSITION.REPLACED THE RIGHT INBOARD FLAP, OUTBOARD ACTUATOR. 2 L 7 2 4F RT A21EA 2001090500011 20010905 00011 EA 2001 9 5 COMA0160668 1 20010902 A 2751 854D100MD91 ACTUATOR CNDAIR CL600 CL6002B19 EA LT WING FAULTY A COMA K NONE J WARNING INDICATION DE DESCENT 1 SO 01 967CA 12263 7134 FLIGHT #5837. DURING DESCENT INTO GSO RECEIVED A FLAP SYSTEM FAIL CAUTION AT 17 DEGREE FLAP POSITON.REPLACED THE LEFT O UTBOARD FLAP, OUTBAORD FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2001090500012 20010905 00012 2001 9 5 2001F00254 4 20010731 A 3422 25883024 GYRO BOEING 727 727225 1384077 NM COCKPIT FAILED A MYWA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 886MA 21855 ON DEPARTURE TAKEOFF OUT OF MIA, NR 1 COMPASS SYSTEM FAILED. RETURNED TO MIAMI. TROUBLE SHOT SYSTEM. FOUND NR 1 DIREC TIONAL GYRO INOPERATIVE. REMOVED AND REPLACED NR 1 DIRECTIONAL GYRO. OPERATIONAL CHECKED IAW 34-21-0. AIRCRAFT RETURN ED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001090500013 20010905 00013 EA 2001 9 5 COMA0160669 1 20010830 A 2120 AEO804AA1 COOLING FAN CNDAIR CL600 CL6002B19 EA NOSE FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 914CA 10698 7012 FLIGHT #5575. DURING TAXI OUT RECEIVED A DISPLAY COOL CAUTION MESSAGE, AIRCRAFT RETURNED TO THE GATE.DEFERRED PER MEL 2 1-24-02. 2 L 7 2 4F RT A21EA 2001090500014 20010905 00014 NM 2001 9 5 2001F00255 1 20010802 A 5610 PR1422 SEAL BOEING 727 72722C 138400F NM WINDSHIELD DETERIORATED A RRXA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 07 428EX 19097 DURING CLIMB-OUT FROM IND, CREW NOTED RIGHT WINDSHIELD NOISE. DESCENDED AIRCRAFT. NOISE CONTINUED UNTIL 12,000. AIRCR AFT RETURNED TO IND AND LANDED WITHOUT INCIDENT. RESEALED R1 WINDSHIELD LOWER EDGE THAT WAS DETERIORATED AND MISSING. P RESSURIZED AIRCRAFT. LEAK CHECK OF WINDSHIELD GOOD. (M) 2 L 7 3 4F A3WE 2001090500015 20010905 00015 2001 9 5 2001F00256 4 20010725 A 3444 5223698014 INDICATOR DOUG DC10 DC1010 3022110 WP COCKPIT FAILED A RYNA J A DUMP FUEL UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 07 571RY 46645 WHILE IN CRUISE BETWEEN HNL AND SFO, AIRCRAFT DEVELOPED SMOKE ODOR IN COCKPIT. AIR TURN BACK TO HNL. FUEL WAS DUMPED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED RADIO ALTIMETER INDICATOR. OPERATIONAL CHECK OF SYSTEM GOOD. (M) 2 L 7 3 4F A22WE 2001090500016 20010905 00016 2001 9 5 2001F00257 4 20010725 A 3444 5224825001 INDICATOR DOUG DC10 DC1010 3022110 WP COCKPIT FAILED A RYNA J A DUMP FUEL UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 07 571RY 46645 WHILE IN CRUISE BETWEEN HNL AND SFO, AIRCRAFT DEVELOPED SMOKE ODOR IN COCKPIT. AIR TURN BACK TO HNL. FUEL WAS DUMPED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED RADIO ALTIMETER INDICATOR. OPERATIONAL CHECK OF SYSTEM GOOD. (M) 2 L 7 3 4F A22WE 2001090500017 20010905 00017 EA 2001 9 5 COMA0160671 1 20010902 A 2720 6229958001 DAMPER CNDAIR CL600 CL6002B19 EA EMPENNAGE FAULTY A COMA D RETURN TO BLOCK O OTHER CR CRUISE 1 SO 01 932CA 18460 7038 FLIGHT #5889. DURING CRUISE FLIGHT AT 20,000 FEET, AIRSPEED 250 KNOTS AIRCRAFT ACQUIRED A RYTHMIC YAW, AIRCRAFT RETURNE D TO ORIGINATION CITY CVG.REPLACED THE #2 SVL-4000 YAW DAMPER. 2 L 7 2 4F RT A21EA 2001090500018 20010905 00018 WP 2001 9 5 2001F00258 1 20010729 A 7931 VT0306D TRANSMITTER DOUG DC10 DC1010 3022110 WP NR 2 ENGINE FAILED A RYNA J A DUMP FUEL UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 07 571RY 46645 NR 2 OIL PRESSURE GAUGE WENT TO FULL SCALE HIGH IN FLIGHT. PULLED AND RESET OIL PRESSURE CIRCUIT BREAKER. DUMPED FUEL AND RETURNED TO HONOLULU. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 OIL PRESSURE TRANSMITTER. OPERA TIONAL CHECK OF SYSTEM GOOD. (M) 2 L 7 3 4F A22WE 2001090500019 20010905 00019 NM 2001 9 5 2001F00259 1 20010729 A 8012 WIRE BOEING 727 72721 1384003 NM PWA JT8 JT8D7B 52053 NE START VALVE DAMAGED A E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 07 359QS 19007 654715 NR 1 ENGINE START VALVE LIGHT ILLUMINATED IN FLIGHT. EMERGENCY DECLARED. COMPLIED WITH ENGINE SHUTDOWN CHECK LIST. DI VERTED TO MCI. AIRCRAFT LANDED WITHOUT INCIDENT. REPAIRED WIRE TO START VALVE AT CANNON PLUG. OPERATIONAL CHECK OF SY STEM GOOD. (M) 2 L 7 3 4F 4 F A3WE E2EA 2001090500020 20010905 00020 EA 2001 9 5 COMA0160672 1 20010903 A 5600 NP1393222 WINDSHIELD CNDAIR CL600 CL6002B19 EA NOSE FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SO 01 960CA 9555 7117 FLIGHT #5697. DURING CLIMB OUT OF CVG RECEIVED A RIGHT WINDOW HEAT CAUTION MESSAGE, AIRCRAFT RETURNED TO THE FIELD.REPL ACED THE RIGHT WINDSHIELD. 2 L 7 2 4F RT A21EA 2001090500021 20010905 00021 WP 2001 9 5 ZW0A0107903 1 20010903 A 3350 58543 CABLE DOUG DC9 DC982 3022082 WP FWD CABIN A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 901TW 49166 THE EGRESS LIGHTS BACK TO ROW 14 WERE INOPERATIVE. REPLACED THE FLEX CABLE. CHECK-C 6-16-01 STL. --CLOSED-- 2 L 7 2 4F A6WE 2001090500022 20010905 00022 NE 2001 9 5 2001F00260 2 20010803 A 7200 ENGINE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D1A 30020 NE NR 2 FAILED A RYNA J A DUMP FUEL UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CE 07 571RY 46645 451529 DURING CLIMB-OUT FROM HNL, CREW NOTED AIRCRAFT VIBRATION FOLLOWED BY NR 2 ENGINE FAILURE. COMPLIED WITH EMERGENCY PROCE DURES CHECK LIST FOR ENGINE SHUT DOWN. JETTISONED FUEL. RETURNED TO HNL AND LANDED WITHOUT INCIDENT. EMERGENCY WAS DE CLARED AND EQUIPMENT WAS CALLED OUT. REMOVED AND REPLACED NR 2 ENGINE. (M) 2 L 7 3 4F 4 F A22WE E23EA 2001090500023 20010905 00023 WP 2001 9 5 AALA20011521 1 20010725 A 5320 PAN DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 438AA 49456 TUL - FOUND CRACK EMITTING FROM AND CORROSION FROM 373-377 ON LOWER CARGO DOOR PAN AREA. STOP DRILLED CRACK. REMOVED C ORROSION AND INSTALLED DOUBLER PER ESO 80559 DATED 7/24/2001. (M) 2 L 7 2 4F RT A6WE 2001090500024 20010905 00024 WP 2001 9 5 AALA20011523 1 20010725 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 438AA 49456 TUL - FOUND CORROSION UNDER CARGO TRACK RIGHT CLIP NUT HOLES BETWEEN STATION 1231-1250. REPLACED RIGHT AFT CARGO TRACK STATION 1212 TO 1327 WITH NEW TRACK PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2001090500025 20010905 00025 WP 2001 9 5 AALA20011527 1 20010720 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 438AA 49456 TUL - FOUND RIGHT CUSP CRACKED AT STATION 1270 AND STATION 1293. REMOVED AND REINSTALLED NEW CUSP RIGHT SIDE STATION 12 50 TO STATION 1309 PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2001090500026 20010905 00026 WP 2001 9 5 AALA20011528 1 20010718 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 438AA 49456 TUL - FOUND RIGHT CUSP CORRODED AT STATION 640-653. INSTALLED DOUBLER ON CUSP PER AARD 53-00-00-2. (M) 2 L 7 2 4F RT A6WE 2001090500027 20010905 00027 WP 2001 9 5 AALA20011530 1 20010717 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 438AA 49456 TUL - FOUND RIGHT CUSP CORRODED BOTTOM SIDE STATION 560-572 OUTBOARD SIDE OF LIGHTENING HOLES OUTBOARD OF NR 6 SEAT TRAC K. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-00-00-021 SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2001090500028 20010905 00028 WP 2001 9 5 AALA20011531 1 20010713 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 438AA 49456 TUL - FOUND RIGHT CUSP CORRODED AT STATION 674-693. CUT OUT CORROSION AND INSTALLED DOUBLER STATION 684-687 PER AARD 53 -00-02. (M) 2 L 7 2 4F RT A6WE 2001090500029 20010905 00029 WP 2001 9 5 AALA20011543 1 20010723 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG LOW A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 577AA 53154 DFW - FLT 865 - EN ROUTE DFW-SJD - DURING GEAR RETRACTION AFTER TAKEOFF NOSE GEAR RED LIGHT REMAINED ON AND AMBER DOOR O PEN LIGHT REMAINED ILLUMINATED. RECYCLED GEAR WITH NO RESULT. RETURNED DFW LANDED WITHOUT INCIDENT. SERVICED NOSE LAN DING GEAR WITH HYDRAULIC FLUID AND NITROGEN. PERFORMED RETRACTION AND EXTENSION CHECK. ALL CHECKS NORMAL WITH NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001090500030 20010905 00030 WP 2001 9 5 ASAA0180190 1 20010607 A 3350 0105606003 MODULE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 SEA - DURING PREFLIGHT CHECK, FOUND 1ST CLASS EMERGENCY TRACK LIGHTING TO BE INOPERATIVE. RECONNECTED LIGHT MODULE. LI GHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001090500031 20010905 00031 WP 2001 9 5 ASAA0180192 1 20010607 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 16353 728 53063 OAK - DURING C-CHECK, THE LEFT FORWARD ENTRY PORTABLE EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE PO RTABLE EMERGENCY LIGHT ASSEMBLY WITH A SERVICEABLE UNIT. (M) 2 L 7 2 4F RT A6WE 2001090500032 20010905 00032 NM 2001 9 5 GAIA01291OP 1 20010807 A 2170 22010 COALESCER BAG BOEING 727 727223 1384074 NM A/C BAY DIRTY A GAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 6827 20180 FLT 2031 - RNO-DEN - AFTER TAKEOFF, THERE WAS A STRONG ODOR OF JET FUEL IN THE COCKPIT. THIS AIRCRAFT MADE AN UNEVENTFU L RETURN TO RNO. REMOVED AND REPLACED BOTH CONDENSER BAGS. INSPECTED AND CHECKED FOR LEAKS. RAN APU AND ENGINES WITH NO LEAKS OR SMELL NOTED. OPERATIONAL CHECKS GOOD ON GROUND. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001090500033 20010905 00033 NE 2001 9 5 GAIA01293OP 2 20010808 A 7510 320115 SHUTOFF VALVE BOEING 727 727223 1384074 NM PWA JT8 JT8D9 52048 NE NR 1 ENGINE STUCK A GAIA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 6810 19485 FLT 2015 - BIL-DEN - DURING CLIMB-OUT FROM BIL, THE FLIGHT CREW NOTICED THE NR 1 ENGINE OIL TEMPERATURE SLOWLY RISING. A EMERGENCY WAS DECLARED AND THE ENGINE WAS SHUTDOWN. THE AIRCRAFT RETURNED TO BIL AND AN UNEVENTFUL LANDING WAS MADE. INVESTIGATION REVEALED THAT THE NR 1 ENGINE FUEL DE-ICE VALVE WAS STUCK IN THE OPEN POSITION. THE VALVE WAS REPLACED A ND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F 4 F A3WE E2EA 2001090500034 20010905 00034 NM 2001 9 5 GAIA01294 1 20010809 A 3350 1000679 LIGHT BOEING 737 737* NM L1 DOOR INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 281KH 21105 DURING ROUTINE MAINTENANCE AT PHX, IT WAS DISCOVERED THAT THE L1 DOOR POSITION EMERGENCY EXIT LIGHT WAS INOPERATIVE. RE MOVED AND REPLACED THE L1 DOOR POSITION EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONALLY CHECKS GOOD. THE AIRCRAFT WAS RET URNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001090500035 20010905 00035 NM 2001 9 5 GAIA01295OP 1 20010810 A 2613 WARNING SYSTEM BOEING 727 727223 1384074 NM COCKPIT MALFUNCTIONED A GAIA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 6809 19484 FLT 202 - SEA-GEG - DURING CRUISE, THE NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. THE CREW ACCOMPLISHED ABNORMAL PRO CEDURES AND THE LIGHT EXTINGUISHED. AIRCRAFT MADE AN UNEVENTFUL LANDING IN GEG. INSPECTED AIR DUCTS FOR LEAKS IN PYLON AREA. NO LEAKS WERE NOTED. INSPECTED OVERHEAT DETECTION LOOPS WITH NO DEFECTS NOTED. OVERHEAT DETECTION SYSTEM OPS C HECK NORMAL DURING ENGINE RUN. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001090500036 20010905 00036 NM 2001 9 5 GAIA01297OP 1 20010813 A 3350 1000677 LIGHT BOEING 727 727223 1384074 NM L1 DOOR INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 858AA 21085 DURING ROUTINE MAINTENANCE AT DFW, IT WAS DISCOVERED THAT THE L1 DOOR POSITION EMERGENCY EXIT LIGHT WAS INOPERATIVE. RE MOVED AND REPLACED THE L1 DOOR POSITION EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONALLY CHECKS GOOD. THE AIRCRAFT WAS RET URNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001090500037 20010905 00037 NM 2001 9 5 GAIA01300OP 1 20010820 A 3350 1000679 LIGHT BOEING 727 727251 138408H NM COCKPIT INOPERATIVE A GAIA K NONE O OTHER CR CRUISE 1 SW 07 255US 19974 FLT 1705 - IAH-FWA - DURING CRUISE, THE COCKPIT EMERGENCY EXIT LIGHT ILLUMINATED AND THEN DISCHARGED. THE AIRCRAFT CONT INUED TO FWA AND LANDED WITHOUT ANY FURTHER DIFFICULTIES. REMOVED AND REPLACED THE COCKPIT EMERGENCY EXIT LIGHT. OPERA TIONALLY CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001090500038 20010905 00038 NE 2001 9 5 HALA0100204 2 20010808 A 7321 MEC DOUG DC10 DC1010 3022110 WP GE CF6 CF66K 30020 NE NR 2 ENGINE FAILED A HALA O OTHER X ENGINE FLAMEOUT DE DESCENT 1 WP 13 135AA 47830 FLT 938 - INBOUND TO ANC, HAD NR 2 ENGINE QUIT AT 15,000 FT, ATTEMPTED RESTART, NO SUCCESS. DECLARED EMERGENCY. REMOVE D AND REPLACED MEC AND FUEL PUMP. TRIM RUN CHECKS OK. (M) 2 L 7 3 4F 4 F A22WE E23EA 2001090500039 20010905 00039 EA 2001 9 5 REXA01012 1 20010709 A 3510 380270260 HOSE CNDAIR CL600 CL6002B19 EA COCKPIT RUPTURED A REXA K NONE O OTHER TX TAXI/GRND HDL 1 SO 25 8477R 1072 7477 OBSERVER SEAT POSITION OXYGEN MASK SUPPLY HOSE RUPTURED AND SEPARATED FROM FITTING. REMOVED AND REPLACED HOSE. THIS WA S FOUND WHILE INVESTIGATING A DEPLETED CREW OXYGEN SYSTEM. (M) 2 L 7 2 4F RT A21EA 2001090500040 20010905 00040 NM 2001 9 5 UHLA003698 1 20010801 A 2910 82920010169 HYDRAULIC LINE DHAV DHC8 DHC8* NM RT WING BROKEN A UHLA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NE 03 804SA 17394 375 FLT 219 - BUF-BED - AFTER TAKEOFF, WHEN GEAR SELECTED UP NR 2 HYD QUANTITY WENT TO 1 QUART AND GEAR REMAINED DOWN AND LO CKED. RETURN TO BUF. MAINTENANCE FOUND BROKEN LINE AT BYPASS VALVE. INSTALLED FLEX LINE AND RETURNED AIRCRAFT TO SERV ICE. (M) 2 H 7 2 4T RT A13NM 2001090500041 20010905 00041 NM 2001 9 5 USAASB01202 1 20010716 A 5230 694173069 BUNGEE CORD BOEING 737 737301 1384611 NM CARGO DOOR DAMAGED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 334US 23231 IND - FLT 461 - EN ROUTE FROM CLT-ORD, AT FL240, THE CABIN ALTITUDE WARNING HORN ACTIVATED AS CABIN ALTITUDE WAS AT 10,0 00 FT AND CLIMBING. STANDBY PRESSURIZATION WOULD NOT CONTROL CABIN AND SELECTING MANUAL SHOWED OUTFLOW VALVE FULL CLOSE D. CREW SELECTED BOTH PACKS WITH ISOLATION VALVE OPEN AND CABIN STOPPED CLIMBING. FLIGHT DIVERTED TO IND AND LANDED WIT HOUT INCIDENT. NO EMERGENCY WAS DECLARED AND NO OXYGEN MASKS WERE DEPLOYED. MAINTENANCE FOUND THE AFT CARGO DOOR RELE ASE BUNGEE LANYARD CAUGHT IN THE DOOR SEAL. REPAIRED BUNGEE LANYARD AND CHECKED DOOR AND SEAL FOR DAMAGE. NO DAMAGE FO UND. PERFORMED SINGLE PACK CONFIDENCE CHECK PER MM 21-00-05. CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2001090500042 20010905 00042 WP 2001 9 5 WX0A01004 1 20010725 A 5230 SKIN DOUG DC9 DC921 302205A WP CARGO DOOR CRACKED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 LCQ - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND FORWARD CARGO DOOR INNER SKIN CRACKED IN THE RADIUS BELOW AFT LATCH COVER. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC9 SRM 51-10-4, 52-05 FIGURE 26A , 51-30-5, 51-30-2, AND 51-10-3. (M) 2 L 7 2 4F A6WE 2001090500043 20010905 00043 WP 2001 9 5 WX0A01005 1 20010725 A 5330 991556173 SKIN DOUG DC9 DC921 302205A WP FUSELAGE CORRODED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 LCQ - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, LEVEL 1 CORROSION WAS FOUND IN LOWER AFT FUSELAGE SKIN AT AFT JACK PAD AREA. CORROSION DAMAGE TO FASTENERS IN AREA ALSO DETECTED. REMOVED INTERNAL AND EXTERNAL STRUCTURE IN LOW ER FUSELAGE JACK PAD AREA FOR ACCESS. REPAIRED CORRODED SKIN IAW DC9 SRM 53-04 FIGURE 9 AND REPLACED CORRODED ANGLE IAW DC9 SRM 51-10-4, 51-30-5, 51-30-2 AND 51-10-3. REINSTALLED PARTS PREVIOUSLY REMOVED FOR ACCESS. (M) 2 L 7 2 4F A6WE 2001090500044 20010905 00044 WP 2001 9 5 WX0A01006 1 20010725 A 2740 591096237 JACKSCREW DOUG DC9 DC921 302205A WP HORIZ STAB WORN A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 44339 7106 47361 LCQ - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, HORIZONTAL STABILIZER JACKSCREW FAILED END PLAY CHECK PER WORK CARD 0855, SB 27A362 AND AD 2000-15-15. JACKSCREW END PLAY REPORTED AT .041 INCHES. REMOVED AND REPLACED HORIZONT AL STABILIZER JACKSCREW ASSEMBLY WITH OVERHAULED UNIT IAW DC9 MM 27-40-1. (M) 2 L 7 2 4F A6WE 2001090500045 20010905 00045 NE 2001 9 5 WX0A01007 2 20010725 A 7310 AE7000642 FUEL LINE DOUG DC9 DC921 302205A WP PWA JT8 JT8D11 52044 NE LT/RT ENGINE LEAKING A WXOA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 07 127NK 47361 LCQ - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, MAIN FUEL SUPPLY HOSE ASSEMBLIES ON RIGHT AND LEFT ENGINES TO FUEL CONTROL UNITS REPORTED LEAKING. FUEL LEAKAGE DETECTED DURING POST INSPECTION ENGINE RUNS. MAINTENANCE REMOVED AND REPLACED LEFT AND RIGHT FUEL HOSE ASSEMBLIES. LEAK CHECK NORMAL. NOTE, BOTH HOSE ASSEMBLIES MFG 2Q88. (M) 2 L 7 2 4F 4 F A6WE E2EA 2001090500046 20010905 00046 WP 2001 9 5 WX0A01008 1 20010725 A 2425 WIRE DOUG DC9 DC921 302205A WP COCKPIT CHAFED A K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 LCQ - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND RIGHT ENGINE AC LOAD METER IN COCKPIT OVERHEAD PANEL TO HAVE CHAFED WIRES AT CONNECTOR MAINTENANCE REPAIRED AND DETERMINED AC LOAD METER WIRING AIW DPS 1.834-2.1. SYSTEM OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A6WE 2001090500066 20010905 00066 NM 2001 9 5 AUS20010824 1 20010802 A 5241 18187323 ROD BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM565A1 NE DOOR GATE DAMAGED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT REAR GALLEY DOOR (R2) LOWER GATE ACTUATING ROD BROKEN WHEN THE DOOR WAS IMPACTED BY A CATERING TRUCK. MINOR SU PERFICIAL DAMAGE TO DOOR TRIM. 2 L 7 2 4F 4 F RT A16WE E29NE 2001090500075 20010905 00075 NM 2001 9 5 AUS20010849 1 20010806 A 5246 65454877 DOOR BOEING 737 737476 NM CFMINT CFM56 CFM563C 13802 EU PUMP ACCESS MISSING W O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 AU S (AUS) CENTRE FUEL BOOST PUMP ACCESS DOOR MISSING. 2 L 7 2 4F 4 F RT A16WE E21EU 2001090500076 20010905 00076 NM 2001 9 5 AUS20010853 1 20010806 A 2760 654645262A ATTACH FITTING BOEING 737 737376 NM CFMINT CFM56 CFM563C 13802 EU SPOILER CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S 42725 MA2670 (AUS) NR 6 GROUND SPOILER HINGE BOSS LUG CRACKED. 2 L 7 2 4F 4 F RT A16WE E21EU 2001090500080 20010905 00080 NM 2001 9 5 AUS20010870 1 20010803 A 2761 65448517 ATTACH FITTING BOEING 737 737376 NM CFMINT CFM56 CFM563C 13802 EU SPOILER ACTUATOR SHEARED W K NONE O OTHER IN INSP/MAINT 1 AU S 42109 4892 (AUS) NR 4 GROUND SPOILER OUTBOARD ACTUATOR LUGS SHEARED. 2 L 7 2 4F 4 F RT A16WE E21EU 2001090500085 20010905 00085 EU 2001 9 5 AUS20010879 1 20010807 A 3260 A78722001 SPRING FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAY62015 04564 NE MLG BROKEN W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 AU S (AUS) LT MAIN LANDING GEAR DOOR FORWARD UPLOCK ASSEMBLY RETURN SPRING BROKEN. 2 L 7 2 4F 4 F RT E25NE 2001090500086 20010905 00086 SO 2001 9 5 AUS20010881 1 20010808 A 5753 ROLLER EMB 120 EMB120 3260201 SO PWA 118 PW118A NE HAMSTD 14SF 14SF9 NE TE FLAP TRACK WORN W O OTHER F FLT CONT AFFECTED LD LANDING 1 AU S (AUS) RT OUTBOARD FLAP JAMMED. INVESTIGATION FOUND ALL FOUR ROLLERS WORN AND FLAP TRACK SCORED WITH RAISED METAL AREAS. 2 L 7 2 4T 4 T RT A31SO E20NE 6 N P11NE 2001090500095 20010905 00095 EU 2001 9 5 AUS20010909 1 20010821 A 2910 LINE BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE HYDRAULIC SYSTEM LEAKING W O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 AU S (AUS) HYDRAULIC PIPE LEAKING. LOSS OF HYDRAULIC FLUID. 2 H 7 4 4F 4 F A49EU E6NE 2001090500096 20010905 00096 SO 2001 9 5 AUS20010913 1 20010816 A 2751 3069001017L POWER SUPPLY EMB 120 EMB120 3260201 SO PWA 118 PW118A NE HAMSTD 14SF 14SF9 NE TE FLAP ANNUC FAULTY W O OTHER N FALSE WARNING CR CRUISE 1 AU S 0230 (AUS) FLAP ANNUNCIATOR UNIT FAULTY. SUSPECT POWER SUPPLY PROBLEM. 2 L 7 2 4T 4 T RT A31SO E20NE 6 N P11NE 2001090500102 20010905 00102 NM 2001 9 5 AUS20010922 1 20010823 A 2820 82820083003 TUBE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE FUEL SYSTEM CHAFED W K NONE K FLUID LOSS IN INSP/MAINT 1 AU S (AUS) LT ENGINE FUEL FEED MOTIVE FLOW TUBE CHAFED AND LEAKING IN AREA OF O-RING SEAL CONTACT POINT. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001090500104 20010905 00104 2001 9 5 AUS20010929 4 20010823 A 3418 36058 COMPUTER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE STALL WARNING FAULTY W O OTHER F FLT CONT AFFECTED CL CLIMB 1 AU S 291 (AUS) STALL COMPUTER FAULTY. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001090500113 20010905 00113 CE 2001 9 5 AKG2001F00000 1 20010815 A 3240 5100106159 LINE CESSNA 414 414A 2075907 CE BRAKE SYSTEM CHAFED A AKGA O OTHER K FLUID LOSS NR NOT REPORTED 1 CE 05 36887 4094 414A0835 RIGHT BRAKE LINE HAD A HOLE CHAFFED IN IT FROM BEING IN CONTACT WITH THE HEATER DUCT LINE UNDER THE COPILOTS SEAT. THE LINE RUNS UNDER THE HEATER DUCT AND IS VERY HARD TO SEE. 1 L 7 2 3O A7CE 2001090500114 20010905 00114 EU 2001 9 5 RAIA00108027 1 20010824 A 7500 PW124B ENGINE AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW124B NE RIGHT ENGINE FAILED A RAIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 722TE 16623 5022 220 124172 7400-STL-FLIGHT ATTENDANT OBSERVED SMOKE IN THE CABIN. AIRCRAFT RETURNED TO THE GATE WITHOUT INCEDENT. MAINTENANCE INSPE CTED AND REMOVED AND REPLACED THE RIGHT ENGINE DUE TO OIL INGRESS INTO THE BLEED AIR SYSTEM. 2 H 7 2 4T 4 T RT A53EU E2ONE 2001090500115 20010905 00115 EU 2001 9 5 RAIA00109003 1 20010904 A 7712 MT938T11F35S CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 556HK 13945 41073 75107 7067-STL-RIGHT ENGINE IEC FAILED DURING TAXI, RIGHT ENGINE TORQUE INDICATES -20%. MAINTENANCE INSPECTED AND REPLACED THE RIGHT ENGINE TORQUE RING CANNON PLUG. 2 L 7 2 4T 4 T RT A41NM E18NE 2001090500116 20010905 00116 EU 2001 9 5 AVS2001F00000 1 20010706 A 3244 TIRE STBROS SD3 SD330 8100602 EU PWA PT6 PT6* 52043 EA MLG SEPARATED A AVSA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 13 76NF SH3044 AT 100 KTS AS AIRCRAFT WAS BECOMING AIRBORNE, A LOUD BANG FOLLOWED BY A STRONG SHUDDER WAS HEARD AND FELT. AFTER LANDIN G IT WAS FOUND THAT THE ENTIRE RECAP OFF THE MAIN WHEEL HAD SEPARATED FROM THE TIRE. INSPECTION REVEALED THAT THERE WAS NO BOND BETWEEN THE RECAP RUBBER AND THE TIRE CASE. PROBABLE CAUSE: IMPROPER RECAPPING PROCESS BY MANUFACTURER. 2 H 7 2 4T 3 T A41EU E2NE 2001090500117 20010905 00117 NE 2001 9 5 CX72001F00000 3 20010623 A 6114 7901996P4 YOKE SAAB SF340 340B 7860101 EU GE CT7TS CT71 30030 NE ROTOL R354 R3544123F13 NE PROP HUB BROKEN A CX7A E ENGINE SHUTDOWN E VIBRATION/BUFFET AP APPROACH 1 GL 03 302CE 15756 1788 340B193 ON LANDING, 6 MILES OUT APPROX. THE AC STARTED SHAKING VIOLENTLY. AFTER A COUPLE SECONDS THE RIGHT TORQUE GAUGE STARTED TO FLUCTUATED BETWEEN 60 PERCENT AND 20 PERCENT TORQUE. SHUT DOWN RIGHT ENGINE AND VIOLENT SHAKING STOPPED. LANDED WI THOUT INCIDENT. SHUTDOWN THE RIGHT HAND ENGINE FOR VIBRATION. FOUND THE FORWARD YOKE EAR HAD BROKEN OFF ON THE PROPELLER HUB. VISUAL INSPECTION INDICATES THAT A PREVIOUS MANUFACTURING DEFECT OR CRACK EXISTED IN THE HUB. 2 L 7 2 4T 4 U RT A52EU E8NE 6 C P61GL 2001091800202 20010918 00202 NM 2001 9 18 UPS01236767 1 20010905 A 5610 WINDOW BOEING 727 7272A1 138407F NM COCKPIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE:PFLT CAPTAIN'S L1 WINDOW INNER PANE CRACKED AND ARCHING. REPLACED L1 WINDOW PER MM 56-11-11. 2 L 7 3 4F A3WE 2001092400194 20010924 00194 NM 2001 9 24 UPS01436765 1 20010902 A 5410 TEE CHORD BOEING 747 747212B 1384886 NM NR 4 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:W/E NR 4 PYLON TEE CHORD CRACKED BELOW L/E. FABBED CHORD, INSTALLED TEE CHORD IAW 51-40-04 SRM . 2 L 7 4 4F A20WE 2001090500118 20010905 00118 CE 2001 9 5 DGC2001F00000 1 20010709 A 3250 727425 CIRCUIT BREAKER RKWELL NA265 NA26565 7630107 CE COCKPIT FAILED E DGCA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 03 570R 46575 NOSE WHEEL STEERING CIRCUIT BREAKER PN 727425, FAILED, CAUSING THE AIRCRAFT TO LOSE NOSE WHEEL STEERING CONTROL. AS A RESULT OF LOSING NOSE WHEEL STEERING, AIRCRAFT VEERED OFF TAXI WAY DURING TAXI FOR TAKEOFF. 2 L 7 2 4J A2WE 2001090500119 20010905 00119 EA 2001 9 5 GAJ2001F00000 2 20010604 A 8520 THRU BOLT PIPER PA31 PA31350 7103110 SO LYC O541 TIO541* 41536 EA NR 2 CYLINDER CRACKED A GAJA K NONE O OTHER IN INSP/MAINT 1 NM 11 4237D 6000 1500 317305055 NR 2 CYLINDER THRU STUD STARTED TO CRACK ALLOWING CYLINDER TO ROCK, ENGINE REMOVED FOR INSPECTION AND CHANGE. 1 L 7 2 3O 3 O A20SO E10EA 2001090500120 20010905 00120 EA 2001 9 5 J192001F00000 2 20010815 A 8530 BAFFLE PIPER PA32 PA32R301T 7103220 SO LYC O540 TIO540* 41532 EA ENGINE OUT OF POSITION A J19Y O OTHER O OTHER CR CRUISE 1 EA 35 4178W 197 3257178 L1065861A PILOT REPORTED PROPELLER RPM LEVER NOT MOVEABLE IN CRUISE FLIGHT, BUT BECAME MOVEABLE AS SPEED DECREASED FOR LANDING AND NO FAULT APPARENT ON GROUND. ENGINE CYLINDER BAFFLE (PART NUMBER 85565-019) FOUND TO BE FOWLING ON GOVERNOR CONTROL AR M DUE TO FORWARD MOVEMENT OF BAFFLE IN FLIGHT. PIPER KIT 766-684 EMBODIED IAW SB1049. IT IS CONSIDERED THAT THIS DEFEC T SHOULD BE MADE THE SUBJECT OF AN AD AS IT COULD HAVE LED TO LOSS OF PROPELLER RPM CONTROL IN FLIGHT. 1 L 7 1 3O 3 O A3SO E14EA 2001090500121 20010905 00121 EU 2001 9 5 JGV2001F00010 1 20010726 A 5620 18360001 WINDOW ISRAEL 1125 ASTRASPX 4500205 EU GARRTT TFE731 TFE731* 01518 WP CABIN CHIPPED B JGVR K NONE O OTHER IN INSP/MAINT 1 CE 09 1125S 26 134 NR 2 RIGHT CABIN WINDOW WITH LOOSE CHIP ON EDGE. EDGE OF WINDOW WAS CHAFING ON A FUSELAGE RIVET. WINDOW IS CHIPPED BEY OND LIMITS. 2 L 7 2 4F 4 F RT A16NM E6WE 2001090500122 20010905 00122 CE 2001 9 5 JJB2001F00002 1 20010726 A 2701 NAS1738B4 RIVET BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA CONTROL COLUMN BACKED OUT E JJBA K NONE F FLT CONT AFFECTED LD LANDING 1 EA 01 836CA 1233 UE407 PILOT REPORTED EXCESSIVE CONTROL COLUMN MOVEMENT BEFORE ACHIEVING ANY PITCH CONTROL. NOTE: CONTROL COLUMN LOWER BEARI NG LOOSE, RIVETS BACKED OUT. BOTH SIDES OF COLUMN. MS 20218-2 BEARING (2 EA) 100-524119 WELD ASSY COLUMN. 2 L 7 2 4T 3 T RT A24CE E2NE 2001090500123 20010905 00123 EA 2001 9 5 COMA0160673 1 20010902 A 3620 355924400 SENSING ELEMENT CNDAIR CL600 CL6002B19 EA LT ENGINE PYLON FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SO 01 778CA 7297 FLIGHT #5934. DURING CLIMB OUT OF TRI RECEIVED A LEFT 14TH STAGE DUCT FAIL MESSAGE, AIRCRAFT RETURNED TO THE FIELD.REPL ACED THE LEFT 14TH STAGE PYLON SENSING ELEMENT. 2 L 7 2 4F RT A21EA 2001090500124 20010905 00124 NE 2001 9 5 JPB2001F00000 2 20010727 A 7310 955147560 SOLENOID VALVE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE ENGINE DAMAGED E JPBA O OTHER B R SMOKE/FUMES/ODORS/SPARKS PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 SO 25 353HW 2792 184 2741 9510 PILOT AND CREW SMELLED JET FUEL, SOON AFTER THE AIRCRAFT LOST PARTIAL POWER. MAINTENANCE FOUND THAT THE THREADS ON THE IGNITION SOLENOID VALVE/PURGE VALVE WERE DISTORTED AND LETTING FUEL PASS AROUND THE PACKING. UNIT WAS REPLACED WITH NEW PART. 1 G 7 1 3U 3 U H9EU E19EU 2001090500125 20010905 00125 2001 9 5 KBMA88659 4 20010713 A 3413 206070278005 INDICATOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL COCKPIT INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 73DP 2513 VSI REPORTED INOPERATIVE. REMOVED AND REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U H2SW E4CE 2001090500126 20010905 00126 EU 2001 9 5 KBMA88660 1 20010713 A 2150 060018 BELT SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE AIR CONDITIONING BROKEN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 115SH 2491 3141 AIR CONDITIONER BELT - A/C BELT IS BROKEN. REMOVED AND REPLACED WITH NEW BELT. 1 G 7 1 3U 3 U NC H9EU E19EU 2001090500127 20010905 00127 EU 2001 9 5 KBMA88661 1 20010714 A 2150 451400003 BELT SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE AIR CONDITIONING BROKEN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 270SH 205 1864 AIR CONDITIONER BLOWING HOT AIR. REMOVED AND REPLACED AIR CONDITIONER BELT WITH NEW. 1 G 7 1 3U 3 U NC H9EU E19EU 2001090500128 20010905 00128 NE 2001 9 5 COMA0160674 2 20010904 A 7270 6018T30P06 FAN BLADE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT ENGINE DAMAGED A COMA D RETURN TO BLOCK E VIBRATION/BUFFET CL CLIMB 1 SO 01 937CA 10237 7044 807261 FLIGHT #5775. DURING CLIMB OUT OF CVG AIRCRAFT ENCOUNTERED MULTIPLE BIRD STRIKES ON #1 ENGINE, CREW DECLARED AN EMERGEN CY AIRCRAFT RETURNED TO THE FIELD AND LANDED SAFELY.REPLACED DAMAGED FAN BLADE ON THE LEFT ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 2001090500129 20010905 00129 EU 2001 9 5 KBMA88662 1 20010715 A 2150 AS35034 COMPRESSOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE AIR CONDITIONER FAILED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 270SH 8030 1864 AIR CONDITIONER IS INOPERATIVE. REMOVED AND REPLACED COMPRESSOR WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U NC H9EU E19EU 2001090500130 20010905 00130 EU 2001 9 5 KBMA88663 1 20010729 A 6410 355A09103601 BEARING SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 350SH 537 2957 BEARINGS ARE WORN. REMOVED AND REPLACED WITH NEW BEARING SET. 1 G 7 1 3U 3 U NC H9EU E19EU 2001090500131 20010905 00131 EU 2001 9 5 KBMA88664 1 20010712 A 6520 350A33215300 BEARING SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 350SH 2957 TEETER BEARINGS WORN. REMOVED AND REPLACED WITH NEW BEARINGS. 1 G 7 1 3U 3 U NC H9EU E19EU 2001090500133 20010905 00133 EU 2001 9 5 KBMA88667 1 20010708 A 7921 95092 MOTOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE OIL COOLER SEIZED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 37SH 182 2300 MOTOR SEIZED. REMOVED AND REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U NC H9EU E19EU 2001090500134 20010905 00134 EU 2001 9 5 KBMA88668 1 20010706 A 7931 APTE17651506 TRANSMITTER SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE OIL SYSTEM INTERMITTENT E KBMA O OTHER O OTHER CR CRUISE 1 WP 19 350SH 2957 TRANSMITTER - GAUGE INTERMITTENT IN FLIGHT. INSTALLED NEW TRANSMITTER. 1 G 7 1 3U 3 U NC H9EU E19EU 2001090500135 20010905 00135 EU 2001 9 5 KBMA88669 1 20010711 A 2121 420800006 MOTOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE CABIN INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 270SH 90 1864 FORWARD FAN IS INOPERATIVE. REMOVED AND REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U NC H9EU E19EU 2001090500136 20010905 00136 NE 2001 9 5 COMA0160675 2 20010904 A 7270 6018T30P06 FAN BLADE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT ENGINE DAMAGED A COMA D RETURN TO BLOCK E VIBRATION/BUFFET CL CLIMB 1 SO 01 937CA 10237 7044 807261 FLIGHT #5775. DURING CLIMB OUT OF CVG AIRCRAFT ENCOUNTERED MULTIPLE BIRD STRIKES ON #1 ENGINE, CREW DELCARED AN EMERGEN CY AIRCRAFT RETURNED TO THE FIELD AND LANDED SAFETY.REPLACED DAMAGED FAN BLADE ON THE LEFT ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 2001090500137 20010905 00137 EU 2001 9 5 KBMA88670 1 20010711 A 6710 704A44831113 SERVO SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE MAIN ROTOR LEAKING E KBMA O OTHER K FLUID LOSS NR NOT REPORTED 1 WP 19 37SH 1533 2300 SERVO LEAKING. REMOVED AND REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U NC H9EU E19EU 2001090500138 20010905 00138 EU 2001 9 5 KBMA88671 1 20010710 A 2121 95092 MOTOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE CABIN INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 37SH 7 2300 FAN MOTOR REPORTED TO BE INOPERATIVE. REMOVED AND REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U NC H9EU E19EU 2001090500139 20010905 00139 2001 9 5 KBMA88672 4 20010707 A 3413 206070278005 INDICATOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL COCKPIT INOPERATIVE E KBMA O OTHER O OTHER CR CRUISE 1 WP 19 73DP 2513 SHOWING 20 PERCENT BANK ANGLE AFTER FIVE MINUTES IN FLIGHT. REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U H2SW E4CE 2001090500140 20010905 00140 NE 2001 9 5 COMA0160676 2 20010904 A 7270 6018T30P06 FAN BLADE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT ENGINE DAMAGED A COMA D RETURN TO BLOCK E VIBRATION/BUFFET CL CLIMB 1 SO 01 937CA 10237 7044 807261 FLIGHT #5775. DURING CLIMB OUT OF CVG AIRCRAFT ENCOUNTERD MULTIPLE BIRD STRIKES ON #1 ENIGNE, CREW DECLARED AN EMERGENC Y AIRCRAFT RETURNED TO THE FIELD AND LANDED SAFELY.REPLACED DAMAGED FAN BLADE ON THE LEFT ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 2001090500141 20010905 00141 EU 2001 9 5 KBMA88673 1 20010716 A 6410 355A12004008 BLADE SNIAS 350 AS350BA 8680817 EU TAIL ROTOR CRACKED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 1188P 691 2347 BLADE APPEARS TO HAVE A CRACKED SPAR. INSTALLED SERVICEABLE BLADE. TT1138.4 1 G 7 1 3U NC H9EU 2001090500142 20010905 00142 NE 2001 9 5 COMA0160677 2 20010904 A 7270 6018T30P06 FAN BLADE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT ENGINE DAMAGED A COMA D RETURN TO BLOCK E VIBRATION/BUFFET CL CLIMB 1 SO 01 937CA 10237 7044 807261 FLIGHT #5575. DURING CLIMB OUT OF CVG AIRCRAFT ENCOUNTERED MULTIPLE BIRD STRIKES ON #1 ENGINE, CREW DECLARED AN EMERGEN CY AIRCRAFT RETURNED TO THE FIELD AND LANDED SAFELY.REPLACED DAMAGED FAN BLADE ON THE LEFT ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 2001090500143 20010905 00143 WP 2001 9 5 KBMA88674 2 20010716 A 7421 9550168760 IGNITER MTSBSI MU2 MU2B35 5780411 CE GARRTT TPE331 TPE331* 01514 WP ENGINE INTERMITTENT E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 118P 10351 646 IGNITER - REPORTED TO BE INTERMITTENT. REMOVED AND REPLACED WITH NEW IGNITER. 1 H 7 2 3T 3 T RT A10SW E2WE 2001090500144 20010905 00144 EU 2001 9 5 QXEA0100905 1 20010604 A 3350 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 498US 11181 PDX- FORWARD FACING EXIT SIGN AT ROW 9 HAS 3 LIGHTS BURNED OUT. REMOVED AND REPLACED EXIT SIGN AS REQUIRED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001090500145 20010905 00145 EU 2001 9 5 QXEA0100906 1 20010606 A 3350 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 BOI- FORWARD CABIN EMERGENCY EXIT LIGHT OUT. REMOVED AND REPLACED EXIT SIGN ASSY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETU RNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001090500146 20010905 00146 EU 2001 9 5 KBMA88677 1 20010729 A 2121 050142 BLOWER MOTOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE CABIN INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 350SH 339 2957 BLOWER MOTOR - MOTOR NOT WORKING PROPERLY. REMOVED AND REPLACED WITH SERVICEABLE MOTOR AS REQUIRED. 1 G 7 1 3U 3 U NC H9EU E19EU 2001090500147 20010905 00147 NM 2001 9 5 QXEA0100907 1 20010530 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX - LOWER FUSELAGE SKIN BELOW CARGO DOOR HAS A AREA OF DAMAGE DUE TO CARGO NET SUPPORT ROD IMPACTING FUSELAGE. REPAIRE D IAW DHC-8 SRM 51-20-51. 2 H 7 2 4T RT A13NM 2001090500148 20010905 00148 NM 2001 9 5 QXEA0100908 1 20010602 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX - FUSELAGE SKIN SCRATCHED AROUND PERIMETER OF MOUNTING BASES FOR NR 1 RAD ALT SYSTEM, FORWARD AND AFT ANTENNAS. REPA IRED IAW DHC-8 SRM 53-10-11 AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2001090500149 20010905 00149 NM 2001 9 5 QXEA0100909 1 20010530 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX - NR 1 SEAT TRACK HAS LIGHT CORROSION ON TOP OF INBOARD AND OUTBOARD LUGS AT STATION X278.00. REPAIRED IAW DHC-8 CPM CHAPTER 5. 2 H 7 2 4T RT A13NM 2001090500150 20010905 00150 2001 9 5 KBMA88764 4 20010730 A 3452 066106200 TRANSPONDER SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 350SH 78 2957 TRANSPONDER REPORTED NO SIGNAL. REPLACED WITH 3V UNIT. 1 G 7 1 3U 3 U NC H9EU E19EU 2001090500151 20010905 00151 EU 2001 9 5 KBMA88765 1 20010730 A 2150 060018 BELT SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE AIR CONDITIONING BROKEN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 115SH 82 3141 AIR CONDITIONER BELT - BELT SNAPPED, REPLACED WITH NEW. 1 G 7 1 3U 3 U H9EU E19EU 2001090500152 20010905 00152 EU 2001 9 5 KBMA88766 1 20010731 A 3610 31921001ND02 BLEED VALVE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE BLEED AIR STUCK E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 350SH 2957 BLEED VALVE IS STICKING. REMOVED AND REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U NC H9EU E19EU 2001090500153 20010905 00153 2001 9 5 KBMA88767 4 20010726 A 2312 069102434 DISPLAY BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL VHF RADIO INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 73DP 2513 LED DISPLAY UNREADABLE. REMOVED AND REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U H2SW E4CE 2001090500154 20010905 00154 EU 2001 9 5 KBMA88770 1 20010804 A 2121 420800001 BLOWER SNIAS 350 AS350BA 8680817 EU CABIN INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 1188P 317 2347 AIR CONDITIONER NOT BLOWING IN REAR. REMOVED AND REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U NC H9EU 2001090500155 20010905 00155 EU 2001 9 5 KBMA88771 1 20010803 A 6510 770441 MAGNETIC SEAL SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR LEAKING E KBMA K NONE K FLUID LOSS NR NOT REPORTED 1 WP 19 350SH 2957 MAG SEAL IS LEAKING. REMOVED AND REPLACED WITH NEW. 1 G 7 1 3U 3 U NC H9EU E19EU 2001090500156 20010905 00156 EU 2001 9 5 KBMA88772 1 20010803 A 6510 704A33651181 BEARING SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 350SH 1678 2957 TAILROTOR DRIVE SHAFT BEARINGS WORN, REMOVED AND REPLACED WITH NEW BEARINGS. 1 G 7 1 3U 3 U NC H9EU E19EU 2001090500157 20010905 00157 NE 2001 9 5 COMA0160678 2 20010904 A 7270 6018T30P06 FAN BLADE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT ENGINE DAMAGED A COMA D RETURN TO BLOCK E VIBRATION/BUFFET CL CLIMB 1 SO 01 937CA 10237 7044 807261 FLIGHT #5575. DURING CLIMB OUT OF CVG AIRCRAFT ENCOUNTERED MULTIPLE BIRD STRIKES ON #1 ENGINE, CREW DECLARED AN EMERGEN CY AIRCRAFT RETURNED TO THE FIELD AND LANDED SAFELY.REPLACED DAMAGED FAN BLADE ON THE LEFT ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 2001090500158 20010905 00158 EU 2001 9 5 KBMA88815 1 20010728 A 2913 704A33635002 SLEEVE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE HYDRAULIC PUMP STRIPPED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 230SH 4036 2337 COUPLING SLEEVE - SPLINES STRIPPED OUT. REMOVED AND REPLACED WITH NEW HYDRAULIC PUMP/ BEARING AND SERVICEABLE COUPLING SLEEVE. 1 G 7 1 3U 3 U NC H9EU E19EU 2001090500159 20010905 00159 NM 2001 9 5 DL72S011351 1 20010816 A 5330 SKIN BOEING 727 727225A 1384077 NM S-7L CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 FUSELAGE / SKIN / L1 DOOR CUTOUT / FWD EDGE / STRG. 7L : CRACK REPAIR A SMALL CRACK WAS FOUND IN THE SKIN AT THE FWD EDGE OF THE L1 DOOR CUTOUT AT STRINGER 7L BELOW THE UPPER FWD CORNER. THE CRACK WAS REMOVED WITH A 1" ROUTE OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 381552-14, REV A. 2 L 7 3 4F RT A3WE 2001090500160 20010905 00160 NM 2001 9 5 DLM88011360 1 20010818 A 2410 JT8D219 ENGINE 696233B976J DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE #2 ENGINE FAILED A DALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 27 910DL 690MJ6162 49541 725835 T.O ABORTED FOR RT GEN FAILURE/ RESET ON GND SEEMED OK FOR 3 MIN THEN FAILED AGAIN TRIED NEW GCU RT SIDE NO HELPP GCU FAULTS GEN. REPLACED CSD AND GEN PER M/M OPS AND LK CKS GOOD 2 L 7 2 4F 4 F RT A6WE E9NE 2001090500161 20010905 00161 NM 2001 9 5 DL72W011370 1 20010818 A 5330 6518217189 SKIN BOEING 727 727247 138408F NM FS 360, S-4L GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 297WA 22534 FUSELAGE / SKIN / FS 360 / STRG. 4L : GOUGE REPAIR THE FUSELAGE SKIN WAS GOUGED OVER A 6" LENGTH AT FS 360, BELOW STRINGER 4L. THE SKIN WAS CUTOUT TO REMOVE THE GOUGED AREA. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 381559-14, REV. A. 2 L 7 3 4F A3WE 2001090500162 20010905 00162 NM 2001 9 5 DL738011371 1 20010817 A 5330 141A35214 SKIN BOEING 737 737832 13844CF NM FS 320, S-28R DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 373DA 29621 FUSELAGE / SKIN / FS 312-323 / STRG. 28R : DENT AND GOUGE REPAIR THE FUSELAGE BELLY SKIN WAS STRUCK BY TIRE DEBREE RESULTING IN A DEEP DENT AND GOUGES JUST FWD OF THE E&E DOOR CUTOUT BETWEEN FS 312 & 323 AT STRINGER 28R. THE DAMAGE WAS REMOVED WITH A 3.5" X 5.5" CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 381532-14, REV A. 2 L 7 2 4F RT A16WE 2001090500163 20010905 00163 NM 2001 9 5 DL757011373 1 20010817 A 5330 146N351111 SKIN BOEING 757 757232 1384965 NM FS 1422, S-30 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 638DL 23761 FUSELAGE / SKIN / FS 1422 / STRG. 30-29R : DENT REPAIR THE FUSELAGE SKIN WAS FOUND DENTED NEAR FS 1422 BETWEEN STRINGERS 30 AND 29R. THE DENT WAS COMPLETELY REMOVED WITH A CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 381455-14, REV A. 2 L 7 2 4F RT A2NM 2001090500164 20010905 00164 NM 2001 9 5 DLM88011376 1 20010820 A 3350 RPS1 POWER SUPPLY DOUG MD88 MD88 3023688 NM B5-211 UNSERVICEABLE A DALA O OTHER L NO TEST IN INSP/MAINT 1 SO 27 968DL 53161 ALL INTERIOR EMERGENCY LIGHTS INOP. REPLACED BATTERY RACK FOR OUTPUT LOGIC BEING INCORRECT. ALL OPS NOW NORMAL 2 L 7 2 4F RT A6WE 2001090500165 20010905 00165 NM 2001 9 5 DL73K011381 1 20010822 A 5310 654587547 WEB BOEING 737 737232 1384475 NM DOOR SILL CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 325DL 23097 THE R1 DOOR SILL WEB WAS FOUND CRACKED AT FS 297. THE DAMAGED SECTION OF WEB WAS CUT OUT AND A NEW SECTION SPLICED IN. THE DAMAGE WAS FOUND DURING HMV. 2 L 7 2 4F RT A16WE 2001090500166 20010905 00166 NM 2001 9 5 DL73K011382 1 20010822 A 5310 6546561508 FRAME BOEING 737 737232 1384475 NM FRAME CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 325DL 23097 CORROSION WAS FOUND ON THE FS 947.5 FRAME AT STR 17R. THE CORROSION WAS CUT OUT AND A REPAIR ANGLE INSTALLED. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001090500167 20010905 00167 NM 2001 9 5 DLM88011386 1 20010822 A 2400 1032200 SWITCH DOUG MD88 MD88 3023688 NM COCKPIT UNSERVICEABLE A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 915DE 53420 EMERGENCY POWER SW ON,A/C EMERGENCY BUSS OFF WARNING LIGHT ILLUMINATED//REPLACED EMERGENCY POWER SWITCH __DAL P/N 249201504 2 L 7 2 4F RT A6WE 2001090500168 20010905 00168 NM 2001 9 5 DL73K011387 1 20010823 A 5330 SKIN BOEING 737 737232 1384475 NM FS 951 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 322DL 23094 FUSELAGE / SKIN / AFT GALLEY DOOR (R2) OPENING / UPPER HINGECUTOUT : CRACK REPAIR A TYPICAL CRACK WAS FOUND IN THE SKIN AT THE UPPER HINGE CUTOUT OF THE AFT GALLEY DOOR OPENING. THE CRACK WAS ROUTED OUT AND REPAIRED WITH AN EXTERNAL STEEL DOUBLER PER B737 SRM 53-30-3, FIG 21A AND ER/A 381595-14, REV A. 2 L 7 2 4F RT A16WE 2001090500169 20010905 00169 NM 2001 9 5 DLM88011390 1 20010822 A 5330 593600419 SKIN DOUG MD88 MD88 3023688 NM FS 650, S-29R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 987DL 53338 FUSELAGE / SKIN / FS 650 / STRG. 29R-30 : CORROSION CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND WITH AN AREA OF CORROSION AT FS 650 BETWEEN STRINGERS 30 AND 29R. THE CORROSION WAS REMOVED WITH A 7.5" X 9.5" CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN ESTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 381586-14, REV A. 2 L 7 2 4F RT A6WE 2001090500170 20010905 00170 NM 2001 9 5 DL757011391 1 20010822 A 5330 146N37506 SKIN BOEING 757 757232 1384965 NM FS 1715, S-19R GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 639DL 23993 FUSELAGE / SKIN / FS 1715 / STRG. 19R : GOUGE REPAIR THE FUSELAGE SKIN WAS FOUND GOUGED AND FS 1715 AND STRINGER 19R. THE GOUGE WAS REMOVED WITH AN 8" X 3" CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 381362-14, REV A. 2 L 7 2 4F RT A2NM 2001090500171 20010905 00171 NM 2001 9 5 DL757011393 1 20010823 A 5330 146N35318 SKIN BOEING 757 757232 1384965 NM FS 1473, RBL 3.2 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 639DL 23993 FUSELAGE / SKIN / FS 1473 / RBL 3.2 / LOWER AFT VHF ANTENNA:CORROSION REPAIR THE FUSELAGE SKIN WAS FOUND CORRODED AT THE VHF ANTENNA MOUNT AT FS 1473 AND RBL 3.2. THE CORROSION WAS REMOVED WITH A 20" X 12" CUTOUT. THE CUTOUT WAS REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS INSTALLED PER ER/A 381450-14, REV A. 2 L 7 2 4F RT A2NM 2001090500172 20010905 00172 NM 2001 9 5 DL757011394 1 20010820 A 5330 143N34714 SKIN BOEING 757 757232 1384965 NM FS 445, S-28 MISDRILLED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 617DL 22907 FUSELAGE / SKIN / FS 440-456 / STRG. 28L-28R : TOOLING DAMAGE REPAIR THE FUSELAGE SKIN WAS GOUGED AND MISDRILLED DURING REPLACEMENT OF A TCAS ANTENNA BETWEEN FS 440 & 456 AND BETWEEN STRINGERS 28L & 28R. THE DAMAGE WAS REMOVED WITH A 15" X 13" CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS PER ER/A 381547-14, REV A. 2 L 7 2 4F RT A2NM 2001090500173 20010905 00173 NM 2001 9 5 DLM88011403 1 20010825 A 2710 K3LR48 BEARING DOUG MD88 MD88 3023688 NM RT SPOILER MIXER UNSERVICEABLE A DALA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 SO 27 963DL 49982 AILERON IN RIGHT ROLL HANGS UP. RPLD PIVOT BEARING AT RT SPOILER MIXER. NOW OPS NML 2 L 7 2 4F RT A6WE 2001090500174 20010905 00174 NM 2001 9 5 DLM11011415 1 20010826 A 5240 ACA31451 DOOR DOUG MD11 MD11 3023602 NM EXTERNAL MISSING A DALA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 SO 27 810DE 48565 FOUND BY MTC EXTERNAL ELECTRICAL CONNECTION DOOR MISSING - REPLACED SAME 2 L 7 3 4F RT A22WE 2001090500175 20010905 00175 NM 2001 9 5 DL767011418 1 20010827 A 2900 142012112E COUPLING BOEING 767 767232 1385132 NM ADP PRESS LINE BROKEN A DALA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 SO 27 108DL 22220 LNDG IN JAX "CTR HYD QTY" EICAS MSG ILLUMINATED. TURNING ONTO TAXIWAY, QTY WENT FROM 4.0 TO 0.0 AND LOST NOSEWHEEL STEERING. TOWED INTO GATE. LEFT AND RIGHT HYD SYSTEMS NORMAL. CA FD COUPLING BETWEEN ADP ASSY AND PRESS LINE BROKEN. REPLACED COUPLING PER MM. 2 L 7 2 4F RT A1NM 2001090500176 20010905 00176 NM 2001 9 5 DL73K011421 1 20010828 A 5311 6546541504 FRAME BOEING 737 737232 1384475 NM CABIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 325DL 23097 CRACKS WERE FOUND IN THE FS 663.75 FRAME AT STR. 3R, 2R, 2L,AND 3L. THE FRAME WAS REPAIRED PER B737 SRM 53-10-4, FIG 14 IN ORDER TO ACCOMMODATE THE FRAME REPAIR THE FUSELAGE SKIN WAS CUT AT EACH STRINGER LOCATION. AN EXTERNAL REPAIR DOUBLER AND TRIPLER WAS INSTALLED PER ERA 397877-14. THE DAMAGE WAS FOUND DURING HMV. 2 L 7 2 4F RT A16WE 2001090500177 20010905 00177 NM 2001 9 5 DL72S011444 1 20010831 A 5330 65C139132 SKIN BOEING 727 727232 1384082 NM FS 1080, S-28R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 524DA 21584 FUSELAGE / SKIN / FS 1070-1090 / STRG. 27R-29R : CORROSION CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND CORRODED BETWEEN FS 1070 & 1090 AND BETWEEN STRINGERS 27R & 29R. THE CORROSION WAS REMOVED WITH A 11.75" X 8" CUTOUT. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM DOUBLERS PER ER/A 381582-14, REV A. 2 L 7 3 4F A3WE 2001090500178 20010905 00178 NM 2001 9 5 DL72S011446 1 20010831 A 5330 65C139132 SKIN BOEING 727 727232 1384082 NM FS 1150, S-29R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 524DA 21584 FUSELAGE / SKIN / FS 1150 / STRG. 29R : CORROSION REPAIR THE FUSELAGE SKIN WAS FOUND WITH A SMALL AREA OF CORROSION JUST AFT OF THE FS 1150 FRAME AND JUST OUTBD OF STRINGER 29R. THE CORROSION WAS REMOVED WITH A CUTOUT AND REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS PER ER/A 381550-14, REV A. 2 L 7 3 4F A3WE 2001090500179 20010905 00179 NM 2001 9 5 DL738011448 1 20010829 A 5330 143A3250 SKIN BOEING 737 737832 13844CF NM FS 380, S-20R PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3750D 32375 FUSELAGE / SKIN / FS 380 / STRG. 19R-20R : GROUND DAMAGE CUTOUT REPAIR THE FUSELAGE SKIN WAS DAMAGED BY GROUND EQUIPMENT AT FS 380 BETWEEN STRINGERS 19R AND 20R. THE PUNCTURES AND GOUGES WERE REMOVED WITH A 14" X 4" CUTOUT IN THE SKIN. THE SKIN CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER INSTALLED PER ER/A 381650-14. 2 L 7 2 4F RT A16WE 2001090500180 20010905 00180 NM 2001 9 5 DL733011450 1 20010831 A 5330 654577683 SKIN BOEING 737 737347 1384647 NM FS 1000, S-25L/R GOUGED A DALA D RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 27 308WA 23441 FUSELAGE / SKIN / FS 907-1156 / STRG. 25L-25R : TAIL STRIKE REPAIR THE FUSELAGE SKIN SUFFERED A TAIL STRIKE ON TAKEOFF WHICH RESULTED IN MULTIPLE GOUGES, SCRAPES, AND HOLES IN THE FUSELAGE SKIN FROM FS 907 TO 1156 AND BETWEEN STRINGERS 25L & 25R. AN UNDERLYING SECTION OF DOUBLER WAS ALSO DAMAGED. A NEW SECTION OF DOUBLER WAS INSTALLED WITH AN ALUMINUM DOUBLER SPLICE REPAIR AND THE TWO DAMAGED SKIN PANELS REPLACED PER ER/A 381560-14, REV A. 2 L 7 2 4F RT A16WE 2001090500181 20010905 00181 NM 2001 9 5 DL767011464 1 20010902 A 3200 HYDRAULIC LINE BOEING 767 767232 1385132 NM RT PYLON BLOWN A DALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 27 106DA 22218 RT HYD SYSTEM PRESSURE LOST DUE TO LEAK. FLUID DECREASES RAPIDLY WHEN DEMAND PUMP IS ON. - REPLACED EDP DISCHARGE LINE 2 L 7 2 4F RT A1NM 2001090500182 20010905 00182 NM 2001 9 5 DL767011467 1 20010903 A 2560 PANEL BOEING 767 767232 1385132 NM COCKPIT FAULTY A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 113DA 22225 DURING TROUBLESHOOTING OF OVERWING SLIDE DOOR SQUIB TEST, SQUIBS WERE INADVERTANTLY FIRED. REPLACED SQUIB PANEL 2 L 7 2 4F RT A1NM 2001090500183 20010905 00183 NM 2001 9 5 QXEA0100910 1 20010531 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX - NR 10 SEAT TRACK HAS LIGHT CORROSION IN BOTTOM OF CHANNEL AT STATION X343.00 - 345.00. REPAIRED IAW DHC-8 CPM CHA PTER 5. 2 H 7 2 4T RT A13NM 2001090500184 20010905 00184 NE 2001 9 5 COMA0160679 2 20010904 A 7270 6018R30P06 FAN BLADE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT ENGINE DAMAGED A COMA D RETURN TO BLOCK E VIBRATION/BUFFET CL CLIMB 1 SO 01 937CA 10237 7044 807261 FLIGHT #5775. DURING CLIMB OUT OF CVG AIRCRAFT ENCOUNTERED MULTIPLE BIRD STRIKES ON #1 ENGINE, CREW DECLARED AN EMERGEN CY AIRCRAFT RETURNED TO THE FIELD AND LANDED SAFELY.REPLACED DAMAGED FAN BLADE ONT HE LEFT ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 2001090500185 20010905 00185 SW 2001 9 5 ALG2001F00016 1 20010714 A 6510 407340340101 DISC PACK BELL 407 407 SW ALLSN 250B 250B* GL TAIL ROTOR CRACKED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 547AL 53240 DURING 25 HOUR AD INSPECTION FOUND DISC PACK CRACKED. RECOMMENDATION TO PREVENT RECURRENCE: ALLOW TAIL ROTOR DRIVE TO FLOAT SO DISC PACKS DO NOT FLEX AS MUCH OR AS OFTEN. 1 G 7 1 3U 3 T O H2SW E10CE 2001120500079 20011205 00079 SW 2001 12 5 ALG2001F00018 1 20010910 A 6510 407340339101 BEARING BELL 407 407 1182206 SW ALLSN 250C 250C47B GL T/R DRIVESHAFT DAMAGED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 577AL 53247 CAE847167 TAILROTOR DRIVESHAFT BEARINGS, DURING DAILY INSPECTION, GREY GREASE FROM BEARINGS. 1 G 7 1 3U 3 U O H2SW E1GL 2001090500187 20010905 00187 SO 2001 9 5 LD22001F00000 1 20010117 A 3242 1159SC15043 ROTOR GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE BRAKE CRACKED A LD2R K NONE O OTHER IN INSP/MAINT 1 GL 15 73M 547 11203 SMALL CRACKS WERE FOUND IN THE NR 1 ROTOR DURING PREFLIGHT INSPECTION. BRAKE WAS REPLACED WITH NEW UNIT. WHILE REPLACI NG UNIT WE NOTICED THAT THE BOLT HOLES APPEAR LARGER THAN NEEDED, MEASURED HOLES, ALL ARE WITHIN SPECS. 2 L 7 2 4F 4 F RT A12EA E00057EN 2001090500188 20010905 00188 SO 2001 9 5 LD22001F00001 1 20010717 A 3242 1159SC15043 ROTOR GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE BRAKE CRACKED A LD2R K NONE O OTHER IN INSP/MAINT 1 GL 15 73M 547 11203 SMALL CRACKS WERE FOUND IN THE NR 1 ROTOR DURING PREFLIGHT INSPECTION. BRAKE WAS REPLACED WITH NEW UNIT. WHILE REPLACI NG UNIT WE NOTICED THAT THE BOLT HOLES APPEAR LARGER THAN NEEDED. MEASURED HOLES, ALL ARE WITHIN SPECS. 2 L 7 2 4F 4 F RT A12EA E00057EN 2001090500189 20010905 00189 SO 2001 9 5 LD22001F00003 1 20010710 A 3242 1159SC15043 ROTOR GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE NR 1 BRAKE CRACKED A LD2R K NONE O OTHER IN INSP/MAINT 1 GL 15 73M 547 11203 NR 1 BRAKE ASSEMBLY - TO SMALL CRACKS WERE FOUND IN NR 1 ROTOR DURING PREFLIGHT. BRAKE WAS REMOVED AND OVERHAULED UNIT INSTALLED. 2 L 7 2 4F 4 F RT A12EA E00057EN 2001090500190 20010905 00190 SO 2001 9 5 LD22001F00004 1 20010710 A 3242 159SC15043 ROTOR DUNLOP AHA2163 GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE NR 2 BRAKE CRACKED A LD2R K NONE O OTHER IN INSP/MAINT 1 GL 15 73M YK053 547 11203 BRAKE ASSEMBLY NR 2 - SMALL CRACKS WERE FOUND IN THE NR 1 ROTOR DURING PREFLIGHT INSPECTION. BRAKE WAS REPLACED WITH AN OVERHAULED UNIT. 2 L 7 2 4F 4 F RT A12EA E00057EN 2001090500191 20010905 00191 SO 2001 9 5 LD22001F00005 1 20010706 A 3242 1159SC15043 ROTOR GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE NR 1 BRAKE CRACKED A LD2R K NONE O OTHER IN INSP/MAINT 1 GL 15 83M 468 557 1122511226 NR 1 BRAKE ASSEMBLY - SMALL CRACKS WERE FOUND IN THE NR 1 ROTOR DURING PREFLIGHT INSPECTION. BRAKE WAS REPLACED WITH AN OVERHAULED UNIT. 2 L 7 2 4F 4 F RT A12EA E00057EN 2001090500192 20010905 00192 SO 2001 9 5 LD22001F00006 1 20010706 A 3242 1159SC15043 ROTOR DUNLOP GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE NR 2 BRAKE CRACKED A LD2R K NONE O OTHER IN INSP/MAINT 1 GL 15 83M 468 XW010 557 1122511226 NR 2 BRAKE ASSEMBLY - SMALL CRACKS WERE FOUND IN THE NR 1 ROTOR DURING PREFLIGHT INSPECTION. BRAKE WAS REPLACED WITH AN OVERHAULED UNIT. 2 L 7 2 4F 4 F RT A12EA E00057EN 2001090500193 20010905 00193 SO 2001 9 5 LD22001F00007 1 20010706 A 3242 1159SC15043 ROTOR GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE NR 3 BRAKE CRACKED A LD2R K NONE O OTHER IN INSP/MAINT 1 GL 15 83M 1081 557 11225 BRAKE ASSEMBLY NR 3 - SMALL CRACKS WERE FOUND IN THE NR 1 ROTOR DURING PREFLIGHT INSPECTION. BRAKE WAS REPLACED WITH AN OVERHAULED UNIT. 2 L 7 2 4F 4 F RT A12EA E00057EN 2001090500194 20010905 00194 SO 2001 9 5 LD22001F00008 1 20010706 A 3242 1159SC1504 ROTOR DUNLOP GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE NR 4 BRAKE CRACKED A LD2R K NONE O OTHER IN INSP/MAINT 1 GL 15 83M 1081 WN057 557 11225 BRAKE ASSEMBLY NR 4 - SMALL CRACKS WERE FOUND IN THE NR 1 ROTOR DURING PREFLIGHT INSPECTION. BRAKE WAS REPLACED WITH AN OVERHAULED UNIT. 2 L 7 2 4F 4 F RT A12EA E00057EN 2001090500198 20010905 00198 EU 2001 9 5 MALA010676 1 20010825 A 5310 SEAT TRACK SAAB SF340 340B 7860101 EU A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 437XJ 340B437 During 4K-check in CWA, LH Center Aisle seat track LBL 18.3 has heavy corrosion at Sta 297. Maintnenance repaired Seat Track IAW SR 53-70-60-2.Completed MAL EO S53060. 2 L 7 2 4T RT A52EU 2001090500199 20010905 00199 EU 2001 9 5 MALA010660 1 20010818 A 5310 7253799459 SEAT TRACK SAAB SF340 340B 7860101 EU CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 437XJ 340B437 During 4K-check in CWA, LH Center Aisle Seat Track LBL18.3 has corrosion that is out of limits from approximatelyu Sta 6 80 to 649 IAW Saab SR 53-70-60. Maintenance replaced Seat Track Section in Aft end of Left Center Aisle IAW S53060. Se at Track PN 7253799-459. 2 L 7 2 4T RT A52EU 2001090500200 20010905 00200 EU 2001 9 5 MALA010661 1 20010818 A 5310 SEAT TRACK SAAB SF340 340B 7860101 EU CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 437XJ 340B437 During 4K-check in CWA, LH Center Aisle Seat Track LBL18.3 has out of limits of pitting corrosion approximately Sta 649- 686.88. Maintenance replaced Seat Track section between Sta 618.88 to 686.88 IAW EO#S53060. 2 L 7 2 4T RT A52EU 2001090500201 20010905 00201 EU 2001 9 5 MALA010670 1 20010821 A 5310 7253721471 ANGLE SAAB SF340 340B 7860101 EU CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 437XJ 340B437 During 4K-check in CWA, Angle on Frame 272 is corroded between RH Galley Seat Track and RH Fwd Emergency Exit. Maintena nce replaced Angle PN 7253721-471 on Frame 272 RH Galley Seat Track and RH Fwd Emergency Exit IAW Saab SRM 51. 2 L 7 2 4T RT A52EU 2001090500202 20010905 00202 EU 2001 9 5 MALA010671 1 20010821 A 5310 7253720325 BEAM SAAB SF340 340B 7860101 EU CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 437XJ 340B437 During 4K-check in CWA, LH Beam between Frame Sta 272 and 288 has heavy corrosion. Maintenance replaced LH Beam PN 7253 720-325 between Frame Sta 272 and 288 IAW Saab SRM 51. 2 L 7 2 4T RT A52EU 2001090500203 20010905 00203 EU 2001 9 5 MALA010675 1 20010825 A 5310 7253722001 ANGLE SAAB SF340 340B 7860101 EU CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 437XJ 340B437 Found during 4K-check in CWA, Frame and Angle at Sta 258 has heavy corrosion. Maintenance installed new Angle PN 725372 2-001 and completed Frame repair IAW SRM 53-70-30-5. 2 L 7 2 4T RT A52EU 2001090500205 20010905 00205 NM 2001 9 5 2001UALA01838 1 20010823 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 187UA 26876 EMERGENCY LIGHT INOP, CEILING 51G SUPPLEMENTAL DATA UPDATE CEILING EMERGENCY LIGHT INOP. REPLACED BULB. 2 L 7 4 4F 4 F RT A20WE E24NE 2001090500206 20010905 00206 NM 2001 9 5 2001UALA01839 1 20010826 A 5313 STRINGER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BODY STATION 180 A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 647UA 25284 APPROXIMATELY BODY STATION 180 STRINGER 25R HAS 2 EACH BLIND FASTENERS. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISH ED. REPALCED 2 EACH BLIND FASTENERS WITH SOLID FASTENERS. 2 L 7 2 4F 4 F RT A1NM E24NE 2001090500207 20010905 00207 NM 2001 9 5 2001UALA01841 1 20010824 A 5315 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 519UA 24872 FORWARD CABIN FLOOR CREASE BEAM CORROSION ON INNER CHORD. BS 367 & RBL 65 SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLI SHED.REMOVED AND REPLACED CREASE BEAM INNER CHORD AT BODY STATION 367 & RBL 65" TREATED, PRIMED & PAINTED. 2 L 7 2 4F 4 F RT A2NM E17NE 2001090500208 20010905 00208 NM 2001 9 5 2001UALA01842 1 20010825 A 5313 CLIP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 519UA 24872 STRINGER CLIP 16L REPLACED DUE TO STRINGER SPLICE STATION 600. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.NEW CL IP INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2001090500209 20010905 00209 NM 2001 9 5 2001UALA01843 1 20010825 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 519UA 24872 STRINGER 16 LH DAMAGED AT STA 605 FORWARD OF 2 LH DOOR. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.STRINGER SPLI CE INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2001090500210 20010905 00210 NM 2001 9 5 2001UALA01844 1 20010825 A 5313 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 519UA 24872 SHEAR WEB CORRODED BETWEEN STATION 996 TO STATION 1020. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED SHEAR WEB OR CREASE BEAM WEB BETWEEN STATION 996 TO 1020. 2 L 7 2 4F 4 F RT A2NM E17NE 2001090500211 20010905 00211 NM 2001 9 5 2001UALA01862 1 20010828 A 5313 STRAP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 STATION 654-648 STRINGER 39L STRAP CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLE D STRINGER STRAP REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090500212 20010905 00212 NM 2001 9 5 2001UALA01863 1 20010828 A 5320 CLIP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 STATION 1087 STRINGER 36L ATTACH CLIP CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REPLACED STRINGER CLI P. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090500213 20010905 00213 NM 2001 9 5 2001UALA01872 1 20010828 A 5311 CLIP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE ELONGATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 STATION 368 STRINGER 38R CLIP HAS ELONGATED HOLE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INS TALLED CLIP REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090500214 20010905 00214 NM 2001 9 5 2001UALA01879 1 20010830 A 5315 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 323UA 23955 CABIN CREASE BEAM WEB IS CRACKED STATION 617 TO STATION 620 STRINGER 17R. MAJOR REPAIR ACCOMPLISHEDCREASE BEAM WEB REP LACED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001090500215 20010905 00215 NM 2001 9 5 2001UALA01883 1 20010829 A 5313 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 519UA 24872 CABIN CREASE BEAM STATION 1170 RBL 65 CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001090500216 20010905 00216 NM 2001 9 5 2001UALA01884 1 20010829 A 5313 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 519UA 24872 CABIN CREASE BEAM STATION 1040 RBL 70 EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001090500217 20010905 00217 NM 2001 9 5 2001UALA01885 1 20010830 A 5313 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 519UA 24872 CABIN CREASE BEAM INBOARD CORD ANGLE AT BODY STATION 730-734 LBL72 CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED INBOAR D CREASE BEAM CORD ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001090500218 20010905 00218 NM 2001 9 5 2001UALA01888 1 20010830 A 5313 STRINGER BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 998UA 22741 STRINGER 6-L CRACKED AT BODY STATION 787. MAJOR REPAIR ACCOMPLISHEDINSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F A16WE E2EA 2001090500219 20010905 00219 NM 2001 9 5 2001UALA01890 1 20010830 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 323UA 23955 CABIN BODY STATION 480, 1 INCH ABOVE STRINGER CLIP AT STRINGER 9R, FRAME WEB IS CRACKED AT STANDOFF FASTENER. MAJOR RE PAIR ACCOMPLISHEDREAMED HOLE TO REMOVE CRACK. INSTALLED HIGHLOCK. 2 L 7 2 4F 4 F RT A16WE E2GL 2001090500220 20010905 00220 NM 2001 9 5 2001UALA01891 1 20010831 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 323UA 23955 FUSELAGE FRAME AT BODY STATION 188 CRACKED AT WL 207 RIGHT HAND. MAJOR REPAIR ACCOMPLISHEDSTOP DRILLED CRACK. INSTALLE D REPAIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2001090500221 20010905 00221 NM 2001 9 5 2001UALA01892 1 20010831 A 5313 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 323UA 23955 RIGHT HAND FUSELAGE CREASE BEAM WEB IS CRACKED AT BODY STATION 196. MAJOR REPAIR ACCOMPLISHEDREMOVED DAMAGED WEB. MANU FACTURED NEW WEB AND INSTALLED 2 L 7 2 4F 4 F RT A16WE E2GL 2001090500222 20010905 00222 NM 2001 9 5 2001UALA01893 1 20010830 A 5311 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 324UA 23956 AFT PIT FUSELAGE FRAME AT STATION 807 HAS BENT SHEAR TIE AT SKIN ATTACH FLANGE LBL4 TO RBL4. MAJOR REPAIR ACCOMPLISHEDR EMOVED SHEAR TIE AND INSTALLED REPAIR ANGLE AT STATION 807. 2 L 7 2 4F 4 F RT A16WE E2GL 2001090500223 20010905 00223 NM 2001 9 5 2001UALA01896 1 20010831 A 5313 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 519UA 24872 CABIN CREASE BEAM STATION 680-740 CORRODED. MAJOR REPAIR ACCOMPLISHED. CABIN CREASE BEAM REPLACED STATION 680-740. 2 L 7 2 4F 4 F RT A2NM E17NE 2001090500224 20010905 00224 NM 2001 9 5 2001UALA01898 1 20010830 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1065-1087 STRINGER 25L CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090500225 20010905 00225 NM 2001 9 5 2001UALA01900 1 20010830 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 766 STRINGER 39L CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090500226 20010905 00226 NM 2001 9 5 2001UALA01902 1 20010830 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1065-1087 STRINGER 22R CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090500228 20010905 00228 NM 2001 9 5 2001UALA01905 1 20010830 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 434 STRINGER 36R SPLICE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SPLICE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090500229 20010905 00229 NM 2001 9 5 2001UALA01908 1 20010830 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1065-1087 STRINGER 25R CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090500230 20010905 00230 NM 2001 9 5 2001UALA01912 1 20010830 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1065-1087 STRINGER 26R CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090500233 20010905 00233 WP 2001 9 5 MWEA011076 1 20010727 A 2720 59141381 BRACKET DOUG DC9 DC982 3022082 WP RUDDER CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 AFT FUSELAGE RUDDER CONTROL BRACKET BETWEEN RUDDER BELLOWS TO RUDDER PACK IS CORRODED. REMOVED BRACKET BETWEEN RUDDER BE LLOW TO RUDDER POWERPACK, INSTALLED BRACKET BETWEEN RUDDER BELLOWS TO RUDDER. 2 L 7 2 4F A6WE 2001090500234 20010905 00234 WP 2001 9 5 MWEA011077 1 20010727 A 5311 9911842129 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 TWO CRACKS AROUND FASTENER ON CANTED FRAME AT STATION 1485 LEFT SIDE AFT AIDE OF CANTED FRAME ABOUT 10 O'CLOCK POSITION. -- STOP DRILLED CRACKS, FABRICATED AND INSTALLED REPAIR PARTS. 2 L 7 2 4F A6WE 2001090500235 20010905 00235 WP 2001 9 5 MWEA011080 1 20010730 A 5320 39258121 SUPPORT FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 NR 1 SEAT TRACK SUPPORT FITTING AT STATION 927 IS CRACKED. REMOVED BRACKET , DRILLED UP NEW PART, INSTALLED PART. 2 L 7 2 4F A6WE 2001090500236 20010905 00236 WP 2001 9 5 MWEA011081 1 20010730 A 5210 49559481 STRUCTURE DOUG DC9 DC982 3022082 WP PAX DOOR CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 PASSENGER DOOR HOLD OPEN HOOK CUP IS CHAFFED ON THE BOTTOM. REMOVED HOOK CUP, DRILLED NEW CUP, PLATE ASSEMBLY, INSTALLED HOOK CUP, NEW PLATE. 2 L 7 2 4F A6WE 2001090500237 20010905 00237 WP 2001 9 5 MWEA011082 1 20010730 A 5347 5936594527 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 GILL LINER SUPPORT BRACKET CORRODED BETWEEN LONGERONS 28 RIGHT TO 27 RIGHT FROM STATION 522-636 IN MID PIT AREA. BLENDED CORROSION, REMOVED CARGO TIE RAIL, FABRICATED NEW TRACK, INSTALLED GILL LINER SUPPORT AND NEW ANGLES. 2 L 7 2 4F A6WE 2001090500238 20010905 00238 WP 2001 9 5 MWEA011083 1 20010730 A 5310 9957906503 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 CENTER CARGO DOOR JAMB WEB CORRODED, EXFOLIATED, AT STATION 630 BETWEEN LONGERONS 28 RIGHT AND 27 RIGHT. REMOVED CORROSI ON, CUT OUT DAMAGED WEB, FABRICATED REPAIR WEB, DOUBLER RING, SPLICE PLATE, LOCATED AND DRILLED PARTS FOR REPAIR, INSTA LLED REPAIR. 2 L 7 2 4F A6WE 2001090500239 20010905 00239 WP 2001 9 5 MWEA011084 1 20010730 A 5311 995823959 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FRAME STATION 1322 HAS TWO CRACKS AT LONGERON 17 LEFT. REMOVED FRAME, FABRICATED FRAME SEGMENT, LOCATED AND DRILLED ANGL E, SPLICE, AND FRAME SECTION, INSTALLED FRAME AND SPLICE. 2 L 7 2 4F A6WE 2001090500240 20010905 00240 2001 9 5 MWEA011085 4 20010728 A 3443 4068048912 COMPUTER DOUG DC9 DC914 3022034 WP E&E BAY MALFUNCTIONED A MWEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 31 500ME 45711 WINDSHEAR LIGHT CAME ON WITH AUTO WARNING. FIRST MAINTENANCE DEFERRED, THEN COLLARD CIRCUIT BREAKER, AND REPLACED THE WI NDSHEAR COMPUTER. 2 L 7 2 4F A6WE 2001090500241 20010905 00241 WP 2001 9 5 MWEA011086 1 20010731 A 5320 39373781 FITTING DOUG DC9 DC982 3022082 WP RT MLG WW CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 RIGHT WHEEL WELL FORWARD WALL INBOARD SIDE 16 INCHES UP FROM BOTTOM T FITTING IS CRACKED AT OUTBOARD END. REMOVED CRACKE D ANGLE, DRILLED UP AND INSTALLED NEW ANGLE. 2 L 7 2 4F A6WE 2001090500242 20010905 00242 WP 2001 9 5 MWEA011087 1 20010718 A 5313 27779221 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 LONGERON 6 RIGHT DAMAGED BETWEEN STATION 503 AND 522. BLENDED DAMAGED AND ATTACHED SPLICE PLATE OVER DAMAGE. 2 L 7 2 4F A6WE 2001090500243 20010905 00243 WP 2001 9 5 MWEA011089 1 20010718 A 5754 99193742 SKIN DOUG DC9 DC932 3022066 WP L/E SLAT CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 RIGHT WING SLAT DOOR CUT OUT BETWEEN NR 4 AND NR 5 SLAT SKIN IS CRACKED. TRIMMED OUT CRACK, INSTALLED FILLER AND DOUBLER . 2 L 7 2 4F A6WE 2001090500244 20010905 00244 WP 2001 9 5 MWEA011090 1 20010718 A 5712 9919313502 RIB DOUG DC9 DC932 3022066 WP WING GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 GOUGE ON INBOARD SLAT SUPPORT TRACK STATION 480.871. REMOVED AND REPLACED RIB. 2 L 7 2 4F A6WE 2001090500245 20010905 00245 WP 2001 9 5 MWEA011095 1 20010802 A 5320 9936535103 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 SUB FLOOR AT STATION 210 APPROXIMATELY 12 INCHES TO THE RIGHT OF THE CENTER LINE IS CORRODED AROUND A FASTENER HOLE. REM OVED CORROSION, REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER, INSTALLED FILLER AND DOUBLER AND ANGLE CLIP. 2 L 7 2 4F A6WE 2001090500246 20010905 00246 2001 9 5 MWEA011097 4 20010803 A 3418 80098717 TRANSDUCER DOUG DC9 DC932 3022066 WP WING FAILED A MWEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 401ME 47133 WINDSHEAR AND STALL INDICATION FAILURE ANNUNCIATOR LIGHTS CAME ON WHEN AIRCRAFT WAS IN FLIGHT MODE. BOTH LIGHTS EXTINGUI SHED AT GROUND SHIFT MODE. REMOVED AND REPLACE RIGHT, AND LATER LEFT, ANGLE OF ATTACK TRANSDUCERS. 2 L 7 2 4F A6WE 2001090500247 20010905 00247 WP 2001 9 5 MWEA011098 1 20010808 A 5313 592480225 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 CABIN LONGERON 17 RIGHT HAS A CRACK AT FRAME ATTACH POINT AT FUSELAGE STATION 389. REMOVED DAMAGED SECTION OF LONGERON, DRILLED UP SECTION, INSTALLED SECTION. 2 L 7 2 4F A6WE 2001090500248 20010905 00248 WP 2001 9 5 MWEA011099 1 20010808 A 5313 592480219 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 CABIN LONGERON 17 RIGHT HAS CRACKS AT FRAME ATTACH POINTS FROM FUSELAGE STATION 237, 268 AND 275. REMOVED DAMAGED SECTIO N OF LONGERON, DRILLED AND INSTALLED SECTION. 2 L 7 2 4F A6WE 2001090500249 20010905 00249 WP 2001 9 5 MWEA011100 1 20010808 A 5311 FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 AFT CARGO COMPARTMENT FRAME SECTION AT STATION 1220 HAS LIGHT CORROSION BOTTOM SIDE INBOARD OF LONGERON 29 RIGHT. FABRIC ATED, LOCATED AND INSTALLED FRAME SECTION AND SHEAR TIE. 2 L 7 2 4F A6WE 2001090500250 20010905 00250 WP 2001 9 5 MWEA011101 1 20010808 A 5320 4912583501 SPLICE DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 STATION 229 LONGERON 29 LEFT SPLICE IS CRACKED. REMOVED, DRILLED AND INSTALLED NEW SPLICE. 2 L 7 2 4F A6WE 2001090500251 20010905 00251 WP 2001 9 5 MWEA011102 1 20010808 A 5313 591140139 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 E & E BAY LONGERON 30 HAS SEVERAL AREAS OF LIGHT CORROSION FROM STATION 218 TO 187. REMOVED LONGERON SECTION, DRILLED AN D INSTALLED NEW SPLICE. 2 L 7 2 4F A6WE 2001090500252 20010905 00252 WP 2001 9 5 MWEA011103 1 20010808 A 5320 99579103 INTERCOSTAL DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 FORWARD CARGO BAY INTERCOSTAL THAT ATTACHED TO LONGERON 29 RIGHT HAS LIGHT CORROSION ON FORWARD SIDE AND ATTACH T STATIO N 435. REMOVED CORROSION, FABRICATED AND INSTALLED NEW INTERCOSTAL. 2 L 7 2 4F A6WE 2001090500253 20010905 00253 WP 2001 9 5 MWEA011104 1 20010808 A 5313 591141277 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 FORWARD CARGO BAY LONGERON 29 RIGHT HAS LIGHT CORROSION AROUND SPLICE STATION 234. REMOVED SPLICE, BLENDED CORROSION, DR ILLED UP NEW SECTION OF LONGERON AND SPLICE, INSTALLED LONGERON SECTION AND SPLICE REPAIR. 2 L 7 2 4F A6WE 2001090500254 20010905 00254 WP 2001 9 5 MWEA011105 1 20010808 A 5320 47122611 SPLICE DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 FORWARD CARGO BAY LONGERON 25 LEFT SPLICE HAS LIGHT CORROSION AND IS CRACKED BETWEEN STATION 225-236. REMOVED, DRILLED A ND INSTALLED NEW SPLICE. 2 L 7 2 4F A6WE 2001090500255 20010905 00255 WP 2001 9 5 MWEA011106 1 20010808 A 5313 592480215 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 CABIN LONGERON 17 LEFT HAS CRACKS AT FRAME ATTACH POINTS FROM FUSELAGE STATION 229 TO 436. REMOVED LONGERON SECTION, DRI LLED UP NEW EXTRUSION, INSTALLED NEW LONGERON. 2 L 7 2 4F A6WE 2001090500256 20010905 00256 WP 2001 9 5 MWEA011107 1 20010808 A 5313 591140143N LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 E&E BAY LONGERON 30 HAS LIGHT CORROSION BETWEEN STATION 157-180. REMOVED LONGERON SECTION, DRILLED AND INSTALLED NEW LON GERON SECTION. 2 L 7 2 4F A6WE 2001090500257 20010905 00257 WP 2001 9 5 MWEA011108 1 20010808 A 5313 591140143N LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 E&E BAY LONGERON 29 LEFT HAS LIGHT CORROSION BETWEEN STATION 178-157. REMOVED LONGERON SECTION, DRILLED AND INSTALLED NE W SECTION OF LONGERON. 2 L 7 2 4F A6WE 2001090500258 20010905 00258 WP 2001 9 5 MWEA011109 1 20010809 A 5347 59108205 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 NR 4 SEAT TRACK IS CORRODED AND HAS SOME TOOL MARKS STATION 218-237. REMOVED CORROSION, FABRICATED, LOCATED, DRILLED AND INSTALLED NEW SECTION OF SEAT TRACK. 2 L 7 2 4F A6WE 2001090500259 20010905 00259 WP 2001 9 5 MWEA011110 1 20010809 A 5347 59108203 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 NR 3 SEAT TRACK CORRODED STATION 200-206. REMOVED CORROSION, FABRICATED AND INSTALLED NEW SECTION OF SEAT TRACK. 2 L 7 2 4F A6WE 2001090500260 20010905 00260 WP 2001 9 5 MWEA011111 1 20010809 A 5230 3914025502N FITTING DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 AFT CARGO DOOR BEAM NR 4 AFT END FITTING IS CRACKED. REMOVED CRACKED BRACKET, LOCATED, DRILLED AND INSTALLED NEW BRACKET AND SHIM. 2 L 7 2 4F A6WE 2001090500261 20010905 00261 WP 2001 9 5 MWEA011112 1 20010809 A 5320 991960327 SPLICE DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 AFT CARGO STATION 899 FRAME SPLICE TOP PLATE HAS LIGHT CORROSION IN TWO SPOTS. FABRICATED AND INSTALLED NEW FRAME SPLICE . 2 L 7 2 4F A6WE 2001090500262 20010905 00262 WP 2001 9 5 MWEA011113 1 20010809 A 5320 99579081 SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FORWARD CARGO COMPARTMENT DOOR JAMB SUPPORT BELOW LOWER WEB AT STATION 408 IS BUCKLED ON TOP END. REMOVED, FABRICATED AN D INSTALLED NEW SUPPORT. 2 L 7 2 4F A6WE 2001090500263 20010905 00263 WP 2001 9 5 MWEA011118 1 20010810 A 5312 59148653 BULKHEAD DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 STATION 604 BULKHEAD CRACKED AT TOP AND TWO INCHES LEFT OF CENTER. FABRICATED AND INSTALLED BULKHEAD REPAIR AND FINGER D OUBLERS. 2 L 7 2 4F A6WE 2001090500264 20010905 00264 WP 2001 9 5 MWEA011119 1 20010810 A 5730 591214426 SKIN DOUG DC9 DC932 3022066 WP RT WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 SKIN CRACKED RIGHT WING FORWARD OF INBOARD BUTE DOOR. REMOVED DAMAGED SKIN, FABRICATED, LOCATED AND INSTALLED NEW SKIN. 2 L 7 2 4F A6WE 2001090500265 20010905 00265 WP 2001 9 5 MWEA011120 1 20010810 A 5312 591486511 FINGER DOUBLER DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 MID PRESSURE BULKHEAD FINGER DOUBLER CRACKED AT MIDDLE. REMOVED, LOCATED, DRILLED AND INSTALLED FINGER DOUBLER. 2 L 7 2 4F A6WE 2001090500266 20010905 00266 WP 2001 9 5 MWEA011114 1 20010809 A 5320 99579081 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FORWARD CARGO COMPARTMENT DOOR JAMB SUPPORT BELOW LOWER WEB AT STATION 398 IS BUCKLED ON TOP END. REMOVED, FABRICATED AN D INSTALLED NEW SUPPORT. 2 L 7 2 4F A6WE 2001090500267 20010905 00267 WP 2001 9 5 MWEA011115 1 20010809 A 5320 9957908501 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FORWARD CARGO COMPARTMENT DOOR JAMB SUPPORT BELOW LOWER WEB AT STATION 379 IS BUCKLED AT SIDE. REMOVED, FABRICATED, LOCA TED, DRILLED AND INSTALLED NEW SUPPORT. 2 L 7 2 4F A6WE 2001090500268 20010905 00268 WP 2001 9 5 MWEA011116 1 20010809 A 5320 591014249N1 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 CRACK APPROXIMATELY 3/4 INCH LONG FOUND ON FORWARD CARGO DOOR JAMB JUST AFT OF AFT BOTTOM STOP SCREW HOLE. REMOVED, LOCA TED AND INSTALLED NEW JAMB. 2 L 7 2 4F A6WE 2001090500269 20010905 00269 WP 2001 9 5 MWEA011122 1 20010810 A 5330 5910072 DOUBLER DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 DOUBLER CORRODED IN THE E&E AT STATION 210 JUST AFT OF GALLEY DRAIN. REMOVED CORROSION, FABRICATED, LOCATED, DRILLED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001090500270 20010905 00270 WP 2001 9 5 MWEA011123 1 20010810 A 5320 9957908501 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FORWARD CARGO COMPARTMENT DOOR JAMB SUPPORT BELOW LOWER WEB AT STATION 418 IS BUCKLED ON TOP END. REMOVED, FABRICATED AN D INSTALLED NEW SUPPORT. 2 L 7 2 4F A6WE 2001090500271 20010905 00271 EU 2001 9 5 USAAF01064 1 20010815 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU PAX CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 868US 11313 RIC - THE FIRST CLASS EMERGENCY EXIT FLOOR LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE GROUND/FLIGHT SWITC H. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT 2001090500272 20010905 00272 WP 2001 9 5 WX0A01001 1 20010725 A 5500 59201031 ATTACH FITTING DOUG DC9 DC921 302205A WP FS 1096 CRACKED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 LCQ - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, CRACKED DETECTED BY VISUAL INSPECTION AT VERTICAL STABILIZ ER LEFT DORSAL FIN ATTACH FITTING. HFEC INSPECTION CONFIRMED CRACKS EMANATING FROM EIGHT FASTENERS HOLES. REMOVED AND REPLACED DORSAL FIN ATTACH FITTING IAW DC9 SRM 51-10-2, 51-10-3, 51-10-4, 51-30-1, 51-30-2, 51-30-5. (M) 2 L 7 2 4F A6WE 2001090500273 20010905 00273 EU 2001 9 5 ASOA01125 1 20010801 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72 EU FUSELAGE INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 636AS 375 DURING HANGAR MAINTENANCE IN MCN, EMERGENCY LIGHT ON PASSENGER DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED E MERGENCY LIGHT BATTERY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2001090500274 20010905 00274 SO 2001 9 5 ASOA01127 1 20010803 A 3350 D36604001 BATTERY PACK EMB 120 EMB120 3260201 SO CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 260AS 22695 120132 FLT 4935 - DURING GROUND INSPECTION IN DFW, CREW OBSERVED MID SECTION OF EMERGENCY FLOOR LIGHTS WERE INOPERATIVE. MAINT ENANCE REMOVED AND REPLACED MID SECTION EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS NORMAL. AIRCRAFT OK FOR SERVI CE. (M) 2 L 7 2 4T RT A31SO 2001090500275 20010905 00275 SO 2001 9 5 ASOA01131 1 20010808 A 3350 F02A250V1A FUSE EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 503AS 120275 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY LIGHTS AT ROWS 5-7 WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED F USELAGE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001090500276 20010905 00276 SO 2001 9 5 ASOA01132 1 20010811 A 3350 D36604001 BATTERY PACK EMB 120 EMB120 3260201 SO CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 245AS 120075 FLT 4011 - DURING DAILY INSPECTION IN ABY, MAINTENANCE FOUND THE FORWARD MOST SET OF EMERGENCY LIGHTS WENT OUT AFTER 30 SECONDS. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR S ERVICE. (M) 2 L 7 2 4T RT A31SO 2001090500277 20010905 00277 SO 2001 9 5 ASOA01135 1 20010811 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO CABIN WEAK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 638AS 120282 DURNIG SCHEDULED MAINTENANCE IN MCN, EMERGENCY LIGHTS ON FLOOR AT ROWS 3 AND 4 HAD WEAK ILLUMINATION. MAINTENANCE REMOV ED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001090500278 20010905 00278 SO 2001 9 5 ASOA01137 1 20010811 A 3350 3071BPE BULB EMB 120 EMB120ER 3260203 SO CABIN BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 500AS 120272 FLT 4817 - DURING GROUND INSPECTION IN DFW, ONE LIGHT BURNED OUT ON EMERGENCY EVACUATION LIGHTS. MAINTNANCE REMOVED AND REPLACED THE BURNED OUT BULB IN FRONT OF GALLEY AREA. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001090600001 20010906 00001 NM 2001 9 6 QXEA0100911 1 20010531 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX - NR 10 SEAT TRACK HAS LIGHT CORROSION IN BOTTOM OF CHANNEL AND TOP OF OUTBOARD LUG AT STATION X375.950. REPAIRED IA W CPM CHAPTER 5. 2 H 7 2 4T RT A13NM 2001090600002 20010906 00002 NM 2001 9 6 QXEA0100912 1 20010531 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX - LIGHT CORROSION IN BOTTOM OF SEAT PEG CHANNEL OF NR 11 SEAT TRACK, AT STATION X387.35. REPAIRED IAW DHC-8 CPM, CHA PTER 5. 2 H 7 2 4T RT A13NM 2001090600003 20010906 00003 NM 2001 9 6 QXEA0100913 1 20010606 A 7110 COWLING DHAV DHC8 DHC8202 2809007 NM RT PYLON CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX - RIGHT-HAND LOWER COWL, INBOARD DOOR 423AL FORWARD APERTURE FLANGE ON LOWER COWL STRUCTURE IS CHAFED .625 INCHES LE NGTH, .187 INCHES WIDE AND .025 DEEP, LOCATED APPROXIMATELY 3.5" BELOW UPPER LATCH CUT-OUT. REPAIRED IAW DHC-8 SRM 51-40 -00 AND HORIZON AIR EA 2-71-140. 2 H 7 2 4T RT A13NM 2001090600004 20010906 00004 NM 2001 9 6 QXEA0100914 1 20010604 A 7110 PAN DHAV DHC8 DHC8202 2809007 NM RT COWL CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX - RIGHT-HAND LOWER COWL, FORWARD LEFT-HAND CORNER OF SUMP PAN IS CRACKED. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001090600005 20010906 00005 NM 2001 9 6 QXEA0100915 1 20010605 A 2450 HARNESS DHAV DHC8 DHC8202 2809007 NM LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX - WIRE BUNDLE CHAFING AGAINST LEFT-HAND WING LEADING EDGE SPAR, YW199.4, APPROXIMATELY .003" DEEP, 1/2 INCH LONG, .1 INCH WIDE. REPAIRED IAW HORIZON AIR EA 2-57-110. 2 H 7 2 4T RT A13NM 2001090600006 20010906 00006 NM 2001 9 6 QXEA0100916 1 20010606 A 5210 STOP DHAV DHC8 DHC8202 2809007 NM PAX DOOR SCORED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX - TOP FORWARD AIRSTAIR STOP BOLT BRACKET IS SCORED ON LOWER SIDE. REPAIRED IAW HORIZON AIR EA 2-52-97. 2 H 7 2 4T RT A13NM 2001090600007 20010906 00007 NM 2001 9 6 QXEA0100917 1 20010604 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX - CORROSION ON TOP SURFACE OF INBOARD AND OUTBOARD LUGS OF NR 11 SEAT TRACK AT STATION X486.50. REPAIRED IAW DHC-8 S RM 51-20-36. 2 H 7 2 4T RT A13NM 2001090600008 20010906 00008 NM 2001 9 6 QXEA0100918 1 20010606 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX - NR 9 SEAT TRACK HAS LIGHT FRETTING IN BOTTOM OF CHANNEL FROM BULKHEAD ANCHOR AT STATION 539.00. REPAIRED IAW HORIZ ON AIR EA 2-53-283. 2 H 7 2 4T RT A13NM 2001090600009 20010906 00009 NM 2001 9 6 QXEA0100919 1 20010531 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX - NR 3 SEAT TRACK HAS LIGHT FRETTING IN BOTTOM OF CHANNEL FROM BULKHEAD ANCHOR AT STATION X539.00. REPAIRED IAW DHC- 8 CPM, CHAPTER 5. 2 H 7 2 4T RT A13NM 2001090600010 20010906 00010 NM 2001 9 6 QXEA0100920 1 20010606 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX - NR 6 SEAT TRACK HAS LIGHT FRETTING IN BOTTOM OF CHANNEL FROM BULKHEAD ANCHOR AT STATION X539.00. REPAIRED IAW HORI ZON AIR EA 2-53-282. 2 H 7 2 4T RT A13NM 2001090600011 20010906 00011 NM 2001 9 6 QXEA0100921 1 20010603 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX - NR 7 SEAT TRACK HAS SEVERAL DEEP PITS IN TOP FLAT SURFACE BETWEEN STATION X201.300 AND X252.300. REPAIRED IAW DHC- 8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001090600012 20010906 00012 NM 2001 9 6 QXEA0100922 1 20010603 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX - NR 4 SEAT TRACK HAS SEVERAL DEEP PITS IN TOP FLAT SURFACE BETWEEN STATIONS X201.300 AND X252.300. REPAIRED IAW DHC -8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001090600013 20010906 00013 NM 2001 9 6 QXEA0100923 1 20010601 A 5320 NUT PLATE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX - NUTPLATES UNDER AIRSTAIR DOOR THRESHOLD ARE CORRODED. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001090600014 20010906 00014 NM 2001 9 6 QXEA0100924 1 20010608 A 7110 COWLING DHAV DHC8 DHC8202 2809007 NM LEFT CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX - LEFT-HAND LOWER COWL LEFT-HAND CENTER CHAFE PAD CHAGED. REPAIRED IAW HORIZON AIR EA 2-71-142. AND RD 8-71-018. 2 H 7 2 4T RT A13NM 2001090600015 20010906 00015 NM 2001 9 6 QXEA0100925 1 20010608 A 7110 COWLING DHAV DHC8 DHC8202 2809007 NM RIGHT CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX - LEFT-HAND LOWER COWL RIGHT-HAND CENTER CHAFE PAD CHAFED. REPAIRED IAW HORIZON AIR EA 2-71-142 AND RD 8-71-018. 2 H 7 2 4T RT A13NM 2001090600016 20010906 00016 NM 2001 9 6 QXEA0100926 1 20010602 A 7810 TRUNNION DHAV DHC8 DHC8202 2809007 NM NR 2 EXHAUST DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX - NR 2 EXHAUST INBOARD TRUNNION TRACK IS GROOVED .050 . REMOVED AND REPLACED TRUNNION TRACK. INSTALLED 4 BOLTS AND S AFETY WIRED. 2 H 7 2 4T RT A13NM 2001090600017 20010906 00017 NM 2001 9 6 QXEA0100927 1 20010602 A 5720 ANGLE DHAV DHC8 DHC8202 2809007 NM RT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX - TRAILING WING ANGLE AT RIGHT-HAND YW171.4 HAS BEEN BENT BY CONTACTING SOMETHING. REPAIRED IAW HORIZON AIR EA 2-57- 109. 2 H 7 2 4T RT A13NM 2001090600018 20010906 00018 NM 2001 9 6 QXEA0100928 1 20010602 A 5720 ANGLE DHAV DHC8 DHC8202 2809007 NM LT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX - TRAILING WING ANGLE AT LEFT-HAND WING AT YW171.4 IS CHAFED. REPAIRED IAW HORIZON AIR EA 2-57-109. 2 H 7 2 4T RT A13NM 2001090600019 20010906 00019 NM 2001 9 6 QXEA0100929 1 20010602 A 5753 STRUCTURE DHAV DHC8 DHC8202 2809007 NM LT WING TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX - TOP SURFACE OF LEFT-HAND OUTBOARD FLAP, CHAFING, YW174.0, APPROXIMATELY .003 DEEP, 1.4 LONG, WIDE. REPAIRED IAW RD 8-57-1022. 2 H 7 2 4T RT A13NM 2001090600020 20010906 00020 NM 2001 9 6 QXEA0100930 1 20010603 A 5711 SPAR CAP DHAV DHC8 DHC8202 2809007 NM WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX - LOWER, LEADING EDGE SPAR CAP CHAFED AT YW57-60, AT LEADING EDGE PANEL 611AR, INBOARD ATTACH POINT. REPAIRED IAW RD 8-57-811, STEP 4, PAGE 3. 2 H 7 2 4T RT A13NM 2001090600021 20010906 00021 NM 2001 9 6 QXEA0100931 1 20010604 A 5753 STRUCTURE DHAV DHC8 DHC8202 2809007 NM RT WING TE FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX - RIGHT-HAND WING, OUTBOARD FLAP, UPPER SURFACE IS CHAFED APPROXIMATELY .015. REPAIRED IAW HORIZON AIR EA 2-57-109 A ND RD 8-57-1022, STEP 12. 2 H 7 2 4T RT A13NM 2001090600022 20010906 00022 NM 2001 9 6 QXEA0100932 1 20010609 A 5230 DOOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY OUT OF RIG A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX - BAGGAGE DOOR LOWER PORTION IS UNDER FLUSH WITH AIRCRAFT PRESSURIZED. REPAIRED IAW HORIZON AIR EA 2-52-101. 2 H 7 2 4T RT A13NM 2001090600023 20010906 00023 NM 2001 9 6 QXEA0100933 1 20010606 A 3231 DOOR DHAV DHC8 DHC8201 2809001 NM MLG MALFUNCTIONED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 828PH 287 PDX- RIGHT MAIN GEAR DOOR DID NOT CLOSE AFTER GEAR SELECTED UP. CLOSED AFTER RECYCLE. PERFORMED FUNCTIONAL CHECKS AND G EAR SWINGS. NO DEFECTS NOTED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001090600024 20010906 00024 NM 2001 9 6 QXEA0100934 1 20010607 A 5210 DOOR DHAV DHC8 DHC8202 2809007 NM MAIN PAX DIRTY A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 357PH 504 SEA- FLIGHT ATTENDANT REPORTS THAT THE MAIN CABIN DOOR IS DIFFICULT TO OPEN AND CLOSE WITH THE HANDLE. CLEANED AND LUBED HANDRAIL HINGE POINTS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001090600025 20010906 00025 NM 2001 9 6 QXEA0100935 1 20010607 A 5210 MECHANISM DHAV DHC8 DHC8202 2809007 NM PAX DOOR DIRTY A QXEA K NONE O OTHER NR NOT REPORTED 1 NM 09 830PH 526 PDX-MAIN CABIN DOOR DIFFICULT TO OPEN. DOOR STICKS. CLEANED AND LUBED MAIN CABIN DOOR STOPS AND SLIDE MECHANISM. OPERATI ONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001090600026 20010906 00026 EU 2001 9 6 QXEA0100936 1 20010609 A 2530 RECEPTACLE FOKKER F28 F28MK4000 4990810 EU CABIN ODOR A QXEA K NONE O OTHER NR NOT REPORTED 1 NM 09 486US 11237 PDX- FLIGHT ATTENDANT REPORTS ELECTRICAL SMELL IN CABIN. REMOVED AND REPLACED BEVERAGE HEATING RECEPTICLE. OPERATIONAL C HECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001090600027 20010906 00027 EU 2001 9 6 QXEA0100937 1 20010605 A 3350 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 11234 PDX- FORWARD FACING CABIN OVERHEAD EXIT SIGN HAS BULBS INOP. REMOVED AND REPLACED EXIT SIGN WITH SERVICEABLE SIGN. OPERA TIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001090600028 20010906 00028 EU 2001 9 6 QXEA0100938 1 20010608 A 3350 XB864041 LIGHT FOKKER F28 F28MK4000 4990810 EU CABIN MALFUNCTIONED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 492US 11159 SEA- EMERGENCY LIGHT ON SIDE OF SEAT 6B CAME OFF. REMOVED AND REPLACED EVACUATION LIGHT ASSEMBLY. OPERATIONAL CHECKS GOO D. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001090600029 20010906 00029 EU 2001 9 6 QXEA0100940 1 20010610 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN MALFUNCTIONED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 477AU 11226 PDX- EMERGENCY EXIT SIGNS NR 1, 3, 4 HAVE BURNED OUT LIGHTS. REMOVED AND REPLACED EMERGENCY EXIT SIGNS. OPERATIONAL CHEC KS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001090600030 20010906 00030 NM 2001 9 6 QXEA0100942 1 20010610 A 5210 MECHANISM DHAV DHC8 DHC8102 2809003 NM PAX DOOR DIRTY A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 830PH 314 PDX - MAIN CABIN DOOR DIFFICULT TO OPEN. ADJUSTED OVER CENTER STOP BOLT TO CORRECT LOADING. NO PARTS REPLACED. OPERATION AL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001090600031 20010906 00031 NM 2001 9 6 QXEA0100943 1 20010610 A 3350 CONTROLLER DHAV DHC8 DHC8202 2809007 NM EMER LIGHTS FAILED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - OVERHEAD EMERGENCY LIGHTS FOUND INOPERATIVE. REMOVED AND REPLACED NR 3 AND 6 EMERGENCY LIGHT CONTROLLERS. OPERATIO NAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001090600032 20010906 00032 EU 2001 9 6 QXEA0100944 1 20010612 A 3350 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 488US 11240 BOI - EXIT SIGN OVER MAIN CABIN DOOR WAS FOUND INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIR CRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001090600033 20010906 00033 EU 2001 9 6 QXEA0100945 1 20010607 A 5710 STRUCTURE FOKKER F28 F28MK4000 4990810 EU RT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - RIGHT-HAND STUBWING TRAILING EDGE HAS PLAY. REPAIED IAW HORIZON AIR EA 4-54-130 AND FOKKER MM 54-10-02, PAGE 3. 2 L 7 2 4F RT A20EU 2001090600034 20010906 00034 EU 2001 9 6 QXEA0100946 1 20010527 A 7110 COWLING FOKKER F28 F28MK4000 4990810 EU LEFT DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - LEFT-HAND UPPER FIXED COWL HAS PROTRUSION ON FRAME 2948. REPAIRED IAW HORIZON AIR EA 4-71-234 AND FOKKER SRM 51-70 -01, PAGE 1. 2 L 7 2 4F RT A20EU 2001090600035 20010906 00035 EU 2001 9 6 QXEA0100947 1 20010607 A 5720 GUIDE FOKKER F28 F28MK4000 4990810 EU LT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - LEFT-HAND STUBWING REAR GUIDE BLOCK IS WORN. REPLACED IAW HORIZON AIR EA 4-54-130, FOKKER FAX TS04.55321 AND FOKKE R MM 54-10-02, PAGE 3. 2 L 7 2 4F RT A20EU 2001090600036 20010906 00036 EU 2001 9 6 QXEA0100948 1 20010526 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - DENT 5 INCHES FORWARD OF FRAME 3450 AT STRINGER 19, LEFT-HAND FUSELAGE FORWARD OF MAIN CABIN DOOR. REPAIRED IAW FO KKER FAX TS01.55105 AND HORIZON AIR EA 4-53-1488. 2 L 7 2 4F RT A20EU 2001090600037 20010906 00037 EU 2001 9 6 QXEA0100949 1 20010526 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - DENT 3 INCHES FORWARD OF FRAME 3450 AT STRINGER 19, LEFT-HAND SIDE OF FUSELAGE FORWARD OF MAIN CABIN DOOR. REPAIRE D IAW FOKKER FAX TS 04.55105 AND HORIZON AIR EA 4-53-1488. 2 L 7 2 4F RT A20EU 2001090600038 20010906 00038 EU 2001 9 6 QXEA0100950 1 20010526 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - DENT FORWARD OF FRAME 3450 AND AT STRINGER 20, LEFT-HAND FUSELAGE FORWARD OF MAIN CABIN DOOR. REPAIRED IAW FOKKER SRM 53-02-05, FIGURE 1 AND HORIZON AIR EA 4-53-1488. 2 L 7 2 4F RT A20EU 2001090600039 20010906 00039 EU 2001 9 6 QXEA0100951 1 20010526 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - STRINGER 21A FOUND TO BE CRACKED FORWARD OF FRAME 3450. REPAIRED IAW FOKKER SRM 53-02-05, FIGURE 1, PAGE 3, ITEM F . 2 L 7 2 4F RT A20EU 2001090600040 20010906 00040 EU 2001 9 6 QXEA0100952 1 20010521 A 5300 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - OUTWARD DENT FOUND BETWEEN FRAME 9305 AND 9305A AT STRINGER 3. REPAIRED IAW FOKKER SRM 53-02-01, FIGURE 1, PAGE 3. 2 L 7 2 4F RT A20EU 2001090600041 20010906 00041 EU 2001 9 6 QXEA0100953 1 20010530 A 5312 BULKHEAD FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - REAR PRESSURE BULKHEAD, FORWARD SIDE, BEAM III, CRACKED IN UPPER ATTACH FLANGE RADIUS, BETWEEN BL425L AND BL425R. REPAIRED. 2 L 7 2 4F RT A20EU 2001090600042 20010906 00042 EU 2001 9 6 QXEA0100954 1 20010530 A 5300 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - CRACKED CASTELLATION ON FRAME 16660 REAR CARGO PIT BETWEEN STRINGERS 1 AND 2. REPAIRED IAW FOKKER SRM 53-02-13, FI GURE 2. 2 L 7 2 4F RT A20EU 2001090600043 20010906 00043 EU 2001 9 6 QXEA0100956 1 20010530 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - CRACKED CASTELLATION ON FRAME 16660 REAR CARGO PIT, BETWEEN STRINGER 2 AND 3. REPAIRED IAW FOKKER SRM 53-02-13, FI GURE 2. 2 L 7 2 4F RT A20EU 2001090600044 20010906 00044 EU 2001 9 6 QXEA0100957 1 20010603 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - FUSELAGE SKIN CHAFED BY TRAILING EDGE OF PANEL 91BC. REPAIRED AIW HORIZON AIR EA 4-53-1495. 2 L 7 2 4F RT A20EU 2001090600045 20010906 00045 EU 2001 9 6 QXEA0100958 1 20010524 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - CRACKED CLIP AT FRAME 6805 ABD STRINGER 6. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 53-165-04, PAGE 39, FIGURE 12. 2 L 7 2 4F RT A20EU 2001090600046 20010906 00046 EU 2001 9 6 QXEA0100959 1 20010524 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - CRACKED CLIP AT FRAME 5805 AND STRINGER 6. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 53-15-04, PA GE 20, FIGURE 7. 2 L 7 2 4F RT A20EU 2001090600047 20010906 00047 EU 2001 9 6 QXEA0100960 1 20010524 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - CRACKED CLIP AT FRAME 5805 AND STRINGER 5. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 53-15-04, PA GE 20, FIGURE 7. 2 L 7 2 4F RT A20EU 2001090600048 20010906 00048 EU 2001 9 6 QXEA0100961 1 20010528 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - FUSELAGE CORROSION FOUND UNDER AFT DME ANTENNA SKIN. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6, AND SRM 51-10-04, P ARAGRAPH 4, PAGE 9. 2 L 7 2 4F RT A20EU 2001090600049 20010906 00049 EU 2001 9 6 QXEA0100962 1 20010528 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - FUSELAGE CORROSION FOUND UNDER LOWER ATC ANTENNA ON SKIN. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6 AND SRM 51-10-0 4, PARAGRAPH 4, PAGE 9. 2 L 7 2 4F RT A20EU 2001090600050 20010906 00050 EU 2001 9 6 QXEA0100963 1 20010528 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - FUSELAGE CORROSION FOUND UNDER LOWER VHF COMM ANTENNA ON SKIN. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6 AND SRM 51 -10-4, PARAGRAPH 4, PAGE 9. 2 L 7 2 4F RT A20EU 2001090600051 20010906 00051 EU 2001 9 6 QXEA0100964 1 20010528 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - FUSELAGE CORROSION FOUND UNDER FORWARD DME ANTENNA ON SKIN. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6 AND SRM 51-10 -4, PARAGRAPH 4, PAGE 9. 2 L 7 2 4F RT A20EU 2001090600052 20010906 00052 EU 2001 9 6 QXEA0100965 1 20010603 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - ANTENNA MOUNT CORROSION FOUND ON MOUNTING PLATE FUSELAGE REBATE FOR THIS FORWARD RADIO ALTIMETER ANTENNA. REPAIED IAW HORIZON AIR EA 4-53-1491 AND FOKKER SRM 51-10-4, PARAGRAPH 4, PAGE 9. 2 L 7 2 4F RT A20EU 2001090600053 20010906 00053 2001 9 6 2001F00262 4 20010814 A 3418 9654020007 SENSOR AIRBUS 300 A300B4203 3930306 EU SENSOR FAILED A J A DUMP FUEL UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 05 821SC 211 AFTER DEPARTING BQN, SLATS WOULD NOT RETRACT, STALL WARNING AND STICK SHAKER ACTIVATED AT 175 KNOTS. DUMPED APPROXIMATE LY 38,000 LBS OF FUEL AND RETURNED TO BQN. AIRCRAFT LANDED NORMAL. CHECKED AND FOUND CODE 71 AND NR 1 PITCH TRIM AND N R 1 AOA SENSOR FAILED. REMOVED AND REPLACED NR 1 AOA SENSOR IAW MM 27-36-15. OPS CHECK GOOD. AIRCRAFT RETURNED TO SER VICE. (M) 2 L 7 2 4F RT A35EU 2001090600054 20010906 00054 EU 2001 9 6 QXEA0100966 1 20010528 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - FUSELAGE CORROSION FOUND ON AFT RADIO ALTIMETER MOUNTING REBATE AND SCORED. REPAIRED IAW FOKKER SRM 51-10-4, PARAG RAPH 4, PAGE 9 AND SRM 53-01-01, PAGE 6. 2 L 7 2 4F RT A20EU 2001090600055 20010906 00055 EU 2001 9 6 QXEA0100967 1 20010603 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - FUSELAGE CORROSION UNDER FORWARD RADIO ALTIMETER BLANKING PLATE REBATES. REPAIRED IAW HORIZON AIR EA 4-53-1491 AND SRM 51-20-00, PARAGRAPH 3. 2 L 7 2 4F RT A20EU 2001090600056 20010906 00056 EU 2001 9 6 QXEA0100968 1 20010528 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - FUSELAGE CORROSION FOUND UNDER MARKER BEACON ON SKIN. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6 AND SRM 51-10-4, PA RAGRAPH 4, PAGE 9. 2 L 7 2 4F RT A20EU 2001090600057 20010906 00057 EU 2001 9 6 QXEA0100969 1 20010530 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - FUSELAGE UPPER TCAS ANTENNA CORROSION FOUND ON SKIN. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6 AND SRM 51-10-4, PAR AGRAPH 4, PAGE 9. 2 L 7 2 4F RT A20EU 2001090600058 20010906 00058 EU 2001 9 6 QXEA0100970 1 20010528 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - FUSELAGE LOWER TCAS ANTENNA CORROSION FOUND ON SKIN. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6, AND SRM 51-10-4, PA RAGRAPH 4, PAGE 9. 2 L 7 2 4F RT A20EU 2001090600059 20010906 00059 WP 2001 9 6 WX0A01002 1 20010725 A 5700 AILERON DOUG DC9 DC921 302205A WP LT AILERON DELAMINATED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 LCQ - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, LEFT AILERON INBOARD TAB DELAMINATION DETECTED ON LOWER OU TBOARD SIDE. DELAMINATION REPORTED TO BE AN AREA OF APPROXIMTELY 5 SQUARE INCHES. CUTOUT DELAMINATED AREA (APPROX 10 I NCHES BY 3 INCHES). FABRICATED FILLER AND DOUBLER, HEAT TREATED, CLEANED AND PREPPED AREA, AND BONDED IAW DC9 SRM 51-70 -2, TIMCO TIPS 1003 AND DC9 SRM 57-50-1. (M) 2 L 7 2 4F A6WE 2001090600060 20010906 00060 EU 2001 9 6 SIMA200118801 1 20010707 A 3350 LP1670 BULB AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 424MQ 045 MIA - FLT 5239 - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHT AT SEAT 3AB TO BE INOPERATIVE. PUT ON MEL. MAINTENA NCE REPLACED THE BULB AT SEAT 3AB FLOOR LIGHT. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001090600061 20010906 00061 EU 2001 9 6 SIMA200121102 1 20010730 A 3350 CM85 BULB SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 392AE 340B392 DFW - FLT 3824 - CREW REPORTED THE FLIGHT ATTENDANTS EMERGENCY LIGHT ARM SWITCH LIGHT IS INOPERATIVE. MAINTENANCE REPLA CED THE BULB IN THE ARM SWITCH. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001090600062 20010906 00062 EU 2001 9 6 SIMA200121101 1 20010730 A 3350 6013211 BATTERY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 329AE 340B329 SAN - FLT 3212 - CREW REPORTED THE EMERGENCY OVERHEAD LIGHTS AT SEATS 9A, AND 11A, EMERGENCY EXIT LIGHT OVER SEAT 8A, AN D FLOOR PROXIMITY LIGHTS AT 8BC AND 10BC TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT BATTERY AT POSITION 8BC. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001090600063 20010906 00063 EU 2001 9 6 SIMA200120301 1 20010722 A 3350 G110881 SOCKET SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AE 340B348 JFK - FLT 5023 - CREW REPORTED AN EMERGENCY LIGHT TO BE INOPERATIVE IN THE CABIN. MAINTENANCE REPLACED THE SOCKET FOR T HE LIGHT OVER THE PASSENGER DOOR. OPERATIONAL HECK AS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001090600064 20010906 00064 EU 2001 9 6 SIMA200120204 1 20010721 A 2600 72111211000 DETECTOR SAAB SF340 340B 7860101 EU INOPERATIVE A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 236AE 340B236 ROC - FLT 5192 - CREW REPORTED THE AVIONICS SMOKE LIGHT ILLUMINATED AND A LOUD NOISE FROM THE AVIONIC RACK FAN IN FLIGHT . AIRCRAFT WAS RETURNED TO ROC. AVIONIC FAN WAS PUT ON MEL AT THIS TIME. MAINTENANCE REMOVED AND REPLACED THE AVIONIC SMOKE DETECTOR IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. NO DEFECTS WERE FOUND IN THE AVIONIC RACK FAN SYSTEM. (M) 2 L 7 2 4T RT A52EU 2001090600065 20010906 00065 EU 2001 9 6 SIMA200120102 1 20010720 A 3350 GE1317 BULB SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 256AE 340B256 JFK - FLT 5165 - CREW REPORTED THE EMERGENCY LIGHT ABOVE SEAT 5BC TO BE INOPERATIVE. LIGHT AS PUT ON MEL AT THIS TIME. MAINTENANCE REPLACED THE BULB AT SEAT 5BC EMERGENCY LIGHT. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SER VICE. (M) 2 L 7 2 4T RT A52EU 2001090600066 20010906 00066 EU 2001 9 6 SIMA200119707 1 20010716 A 3350 192412A FUSE SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 352SB 340B352 BOS - FLT 4620 - CREW REPORTED THE EMERGENCY LIGHTS AT SEATS 8BC AND 10BC TO BE INOPERATIVE. MAINTENANCE REPLACED THE F USE AT 27LN. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001090600067 20010906 00067 EU 2001 9 6 SIMA200118902 1 20010708 A 3350 7239050506 CONTROL PANEL SAAB SF340 340B 7860101 EU COCKPIT INOPERATIVE A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 232AE 340B232 ALB - FLT 4891 - CREW REPORTED ALL OF THE EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGE NCY LIGHT CONTROL PANEL IN THE COCKPIT IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCFAFT WAS RETURNED TO SERVICE. ( M) 2 L 7 2 4T RT A52EU 2001090600068 20010906 00068 EU 2001 9 6 SIMA200118901 1 20010708 A 3350 GE1317 BULB SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 309AE 340B309 JFK - FLT 5128 - CREW REPORTED THE OVERHEAD EMERGENCY LIGHT AT SEAT 5BC. PUT ON MEL AT THIS TIME. MAINTENANCE REPLACED THE BULB FOR SEAT 5BC EMEREGNCY LIGHT. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001090600069 20010906 00069 NM 2001 9 6 TSAA0152111 1 20010816 A 5310 65479602K DOOR FRAME BOEING 737 737209 13844AE NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 827AL 23913 DURING HEAVY CHECK INSPECTION FOUND A CRACK ON THE AFT LOWER CARGO DOORWAY FRAME. THE CRACK EXTENDS FROM A FASTENER HOL E DOWN INTO A FRAME FLANGE. THE REPAIR INVOLVED TRIMMING OUT THE DAMAGE, PERFORMING A HFEC INSPECTION TO ENSURE THE CRA CK AND ANY CORROSION WAS REMOVED. FABRICATED AND INSTALLED A FILLER AND ANGLE. COLD WORK ALUMINUM PARTS COMMON TO THE LAST ROW OF ANGLE PER SRM 51-40-9. INSTALLED COUNTERSUNK REPAIR WASHERS, INSTALLED REPAIR PARTS WITH BMS 5-95 SEALANT B ETWEEN FAYING SURFACES, FINISH ALL BARE SURFACES WITH ALODINE AND TWO COATS OF BMS 10-11, TYPE 1 PRIMER IAW 3241. AIRCR AFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001090600070 20010906 00070 NM 2001 9 6 TSAA0132110 1 20010815 A 3200 65465431 SUPPORT FITTING BOEING 737 7372S2C 138448G NM LT MLG STRUT GOUGED A TSAA O OTHER O OTHER NR NOT REPORTED 1 WP 13 806AL 21927 GOUGE LOCATED AT BS LT MLG STRUT SUPPORT FITTING. REMOVED ALL SHARP EDGES AND BLENDED SMOOTH. PERFORMED HFEC INSPECTIO N TO ENSURE TOTAL DAMAGE REMOVAL. FLAP PEEN AREA PE SRM 51-10-8. APPLIED AND BMS 10-11 TYPE 1 PRIMER. RESTORED AIRCRA FT TO NORMAL CONDITION, PERFORMED OPS AND FUNCTIONAL TESTS OF MLG SYSTEM. OPS CHECK OK IAW ECO 3242. RECEIVED 8110-3 A PPROVAL. THIS IS CONSIDERED AN INTERIM REPAIR, PERMANENT REPAIR DUE NEXT C-CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2001090600071 20010906 00071 NM 2001 9 6 TSAA0133109 1 20010815 A 3300 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM PAX CABIN INOPERATIVE A TSAA O OTHER O OTHER NR NOT REPORTED 1 WP 13 806AL 21927 REPLACED NR 1 FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2001090600072 20010906 00072 EU 2001 9 6 QXEA0100971 1 20010530 A 5312 BULKHEAD FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - BEAM II REAR PRESSURE BULKHEAD RBL425 UPPER AND LOWER CONSOLES DAMAGED AND BEAM II LBL425 LOWER CONSOLE CRACKED. R EPAIRED IAW FOKKER SRM 53-24-04, FIGURE 7, ITEMS 280. 2 L 7 2 4F RT A20EU 2001090600073 20010906 00073 EU 2001 9 6 QXEA0100972 1 20010606 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - CORROSION ON UNDERSIDE OF FRAME 13815B ABOVE STRINGER 74. REPAIRED IAW HORIZON AIR EA 4-53-1496. 2 L 7 2 4F RT A20EU 2001090600074 20010906 00074 EU 2001 9 6 QXEA0100973 1 20010531 A 5310 DOOR FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - LIGHT CORROSION AROUND MAIN CABIN DOOR HINGE FLANGE AREA ON AIRFRAME AROUND BOLT HOLES. REPAIED IAW FOKKER SRM 53- 01-01, PARAGRAPH 4, AND SRM 51-10-4, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 2001090600075 20010906 00075 EU 2001 9 6 QXEA0100974 1 20010527 A 5310 STRUCTURE FOKKER F28 F28MK4000 4990810 EU NLG WW CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - NOSE LANDING GEAR BAY LEFT-HAND WALL CRACK ABOVE LOWER RIVET LINE AT STATION 3050. REPAIRED IAW FOKKER SRM 53-02-1 8, FIGURE 12. 2 L 7 2 4F RT A20EU 2001090600076 20010906 00076 EU 2001 9 6 QXEA0100975 1 20010527 A 5321 FLOOR PANEL FOKKER F28 F28MK4000 4990810 EU COCKPIT DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - COCKPIT FLOOR LEFT-HAND SIDE NUMEROUS DENTS JUST AFT OF CONTROL COLUMN. REPAIRED IAW FOKKER SRM 53-02-01, PAGE 11, FIGURE 9, SRM 53-11-05, FIGURE 6 AND SRM 51-31-01, PARAGRAPH 7, PAGES 13 AND 14 2 L 7 2 4F RT A20EU 2001090600077 20010906 00077 EU 2001 9 6 QXEA0100976 1 20010527 A 5321 FLOOR PANEL FOKKER F28 F28MK4000 4990810 EU COCKPIT DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - COCKPIT FLOOR RIGHT-HAND SIDE NUMEROUS DENTS JUST AFT OF CONTROL COLUMN. REPAIED IAW FOKKER SRM 53-02-01, PAGE 11, FIGURE 9, SRM 53-11-05, FIGURE 6 AND SRM 51-31-01, PARAGRAPH 7, FIGURE 13 AND 14. 2 L 7 2 4F RT A20EU 2001090600078 20010906 00078 EU 2001 9 6 QXEA0100977 1 20010528 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - FUSELAGE CORROSION FOUND UNDER AFT RADIO ALTIMETER BLANKING PLATE REBATE. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6 AND SRM 51-10-04, PARAGRAPH 4, PAGE 9. 2 L 7 2 4F RT A20EU 2001090600079 20010906 00079 EU 2001 9 6 QXEA0100978 1 20010527 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - FUSELAGE STRINGER DAMAGED AT STATION 6805 WL-560. REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3, FIGURE 1 AND SRM 53-02 -06, FIGURE 1. 2 L 7 2 4F RT A20EU 2001090600080 20010906 00080 EU 2001 9 6 QXEA0100979 1 20010527 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - FUSELAGE SKIN STATION 6805, STRINGER 17 NON STANDARD REPAIR. REPAIRED IAW FOKKER SRM 53-02-05, PAGE 3, FIGURE 1 AN D SRM 53-15-02, FIGURE 03, ITEM 122. 2 L 7 2 4F RT A20EU 2001090600081 20010906 00081 EU 2001 9 6 QXEA0100980 1 20010529 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - FUSELAGE LEFT-HAND FRAME 6805, STRINGER 18, FRAME CASTELLATION CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 53-16-04, FIGURE 05, ITEM 35J. 2 L 7 2 4F RT A20EU 2001090600082 20010906 00082 EU 2001 9 6 QXEA0100981 1 20010529 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - FUSELAGE LEFT-HAND FRAME 5805, STRINGER 18, FRAME CASTELLATION CRACKED. REPAIRED IAW FOKKER SRM 53-16-04, FIGURE 0 4, ITEM 16AN. 2 L 7 2 4F RT A20EU 2001090600083 20010906 00083 EU 2001 9 6 QXEA0100982 1 20010529 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - FUSELAGE LEFT-HAND, FRAME 5805, STRINGER 16, FRAME CASTELLATION CRACKED. REPAIRED IAW FOKKER SRM 53-15-04, FIGURE 07, ITEM 240. 2 L 7 2 4F RT A20EU 2001090600084 20010906 00084 EU 2001 9 6 QXEA0100983 1 20010531 A 5210 HINGE FOKKER F28 F28MK4000 4990810 EU PAX DOOR WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - MAIN CABIN DOOR HINGE WORN. REPAIRED IAW MM 52-00-1, TABLE 803 ANDREPALCED IAW FOKKER SRM 52-02-02, FIGURE A. 2 L 7 2 4F RT A20EU 2001090600085 20010906 00085 EU 2001 9 6 QXEA0100984 1 20010531 A 5312 BULKHEAD FOKKER F28 F28MK4000 4990810 EU FUSELAGE CANNING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - REAR PRESSURE BULKHEAD FRONT SIDE AT BUTT LINE 1050L AND HORIZONTAL BEAM XI, SKIN IN OIL CANNED INWARDS. REPAIRED IAW HORIZON AIR EA 4-53-1492. 2 L 7 2 4F RT A20EU 2001090600086 20010906 00086 EU 2001 9 6 QXEA0100985 1 20010525 A 5311 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - CRACKED FRAME CLIP AT FRAME 16060 AND STRINGER 26. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 2001090600087 20010906 00087 EU 2001 9 6 QXEA0100986 1 20010525 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - CRACKED FRAME CLIP AT FRAME 16660 AND STRINGER 27. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. PAGE 4. 2 L 7 2 4F RT A20EU 2001090600089 20010906 00089 EU 2001 9 6 QXEA0100987 1 20010525 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - CRACKED FRAME CLIP AT FRAME 16660 AND STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2, PAGE 4. 2 L 7 2 4F RT A20EU 2001090600090 20010906 00090 EU 2001 9 6 QXEA0100988 1 20010527 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE DETACHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - FIRST BONDED STRINGER FROM THE TOP, BETWEEN 425L AND 425R ON THE REAR PRESSURE BULKHEAD AFT SIDE HAS BECOME DETATC HED ON THE LEFTHAND SIDE. REPAIRED IAW FOKKER SRM 51-20-00, PARAGRAPH 3. 2 L 7 2 4F RT A20EU 2001090600091 20010906 00091 EU 2001 9 6 QXEA0100989 1 20010525 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - CRACKED FRAME CLIP AT FRAME 16060 AND STRINGER 44. REPAIRED IAW FOKKER SRM 553-02-13, FIGURE 2, PAGE 4. 2 L 7 2 4F RT A20EU 2001090600092 20010906 00092 EU 2001 9 6 QXEA0100990 1 20010525 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - CRACKED FRAME CLIP AT FRAME 16660 AND STRINGER 51. REPAIRED IAW FOKEKR SRM 53-02-13, FIGURE 2, PAGE 4. 2 L 7 2 4F RT A20EU 2001090600093 20010906 00093 EU 2001 9 6 QXEA0100991 1 20010525 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - CRACKED FRAME CLIP AT FRAME 16660 AND STRINGER 54. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2, PAGE 4. 2 L 7 2 4F RT A20EU 2001090600094 20010906 00094 EU 2001 9 6 QXEA0100992 1 20010530 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - FUSELAGE CORROSION FOUND UNDER UPPER ATC ANTENNA ON SKIN. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6 AND SRM 51-10-4 , PARAGRAPH 4, PAGE 9. 2 L 7 2 4F RT A20EU 2001090600095 20010906 00095 EU 2001 9 6 QXEA0100993 1 20010530 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - FUSELAGE CORROSION FOUND UNDER UPPER NAV/COMM ANTENNA BASE ON SKIN. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6 AND S RM 51-10-04, PARAGRAPH 4, PAGE 9. 2 L 7 2 4F RT A20EU 2001090600096 20010906 00096 EU 2001 9 6 QXEA0100994 1 20010529 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - SEAT TRACK BL600L SUPPORT ANGLE CRACKED AT STATION 4175, OUTBOARD SIDE. REPAIRED IAW FOKKER SRM 51-31-01, PARAGRAP H 7, PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001090600097 20010906 00097 EU 2001 9 6 QXEA0100995 1 20010530 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - SEAT TRACK BL600L SUPPORT ANGLE CRACKED AT STATION 4610 INBOARD SIDE. REPAIRED IAW FOKKER SRM 51-31-01, PARAGRAPH 7, PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001090600098 20010906 00098 EU 2001 9 6 QXEA0100996 1 20010531 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - SURFACE CORROSION FOUND ON SEAT TRACK BL600L BETWEEN STATIONS 3870 TO STATION 4900. REPAIRED IAW FOKKER SRM 51-31- 01, PARAGRAPH 7, PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001090600099 20010906 00099 EU 2001 9 6 QXEA0100997 1 20010528 A 5310 STRUCTURE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - SURFACE CORROSION FOUND ON SUPPORT BLO BETWEEN STATION 3870 TO STATION 4610. REPAIRED IAW FOKKER SRM 51-10-04, PAR AGRAPH 4, PAGE 7. 2 L 7 2 4F RT A20EU 2001090600100 20010906 00100 EU 2001 9 6 QXEA0100998 1 20010528 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - SURFACE CORROSION FOUND ON SEAT TRACK BL600R BETWEEN STATION 3820 AND STATION 4610. REPAIRED IAW FOKKER SRM 51-10- 04, PARAGRAPH 4, PAGE 7. 2 L 7 2 4F RT A20EU 2001090600101 20010906 00101 EU 2001 9 6 QXEA0100999 1 20010531 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - SURFACE CORROSION FOUND ON SEAT TRACK BL1127R BETWEEN STATION 4175 AND 4900. REPAIRED IAW FOKKER SRM 51-31-01, PAR AGRAPH 7, PAGE 13 AND 14. 2 L 7 2 4F RT A20EU 2001090600102 20010906 00102 EU 2001 9 6 QXEA0101000 1 20010529 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - LEFT-HAND FUSELAGE FRAME 6305 AND STRINGER 18 CASTELLATION CRACKED. REPAIRED IAW FOKKER SRM 53-16-04, FIGURE 04, I TEM 200N. 2 L 7 2 4F RT A20EU 2001090600103 20010906 00103 EU 2001 9 6 QXEA0101001 1 20010529 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - LEFT-HAND FUSELAGE FRAME 5805 AND STRINGER 15 CASTELLATION CRACKED. REPAIRED IAW FOKKER SRM 53-15-04, FIGURE 07, I TEM 240. 2 L 7 2 4F RT A20EU 2001090600104 20010906 00104 EU 2001 9 6 QXEA0101002 1 20010529 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE MISREPAIRED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 481US 11230 YYC - NON STANDARD REPAIR ON CASTELLATION FRAME 6805 AND STRINGERS 16 AND 17. REPAIRED IAW HORIZON AIR EA 4-53-1490 AND FOKKER SRM 53-15-04, FIGURE 11, ITEM 6SM. 2 L 7 2 4F RT A20EU 2001090600105 20010906 00105 EU 2001 9 6 QXEA0101003 1 20010530 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - SEAT TRACK BL600L SUPPORT ANGLE CRACKED AT STATION 4610 OUTBOARD SIDE. REPAIRED IAW FOKKER SRM 51-31-01, PARAGRAPH 7, PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001090600106 20010906 00106 NM 2001 9 6 2001F00264 1 20010818 A 3150 285T003219 MODULE BOEING 757 75723A 1384967 NM E/E BAY MALFUNCTIONED A N8TA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 19 541NA 24291 MASTER CAUTION/WARNING LIGHT SWITCH ILLUMINATED AFTER TAKEOFF WITHOUT ANY ASSOCIATED EICAS MESSAGE OR ANNUNCIATOR LIGHT. MASTER CAUTION COULD NOT BE RESET. REMOVED AND REPLACED MASTER WARNING MODULE, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2001090600107 20010906 00107 EU 2001 9 6 QXEA0101004 1 20010529 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - SEAT TRACK BL600L SUPPORT ANGLE CRACKED AT STATION 4175, INBOARD SIDE. REPAIRED IAW FOKKER SRM 51-31-01, PARAGRAPH 7, PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001090600108 20010906 00108 EU 2001 9 6 QXEA0101005 1 20010531 A 5210 HINGE FOKKER F28 F28MK4000 4990810 EU PAX DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - MAIN CABIN DOOR DIAPHRAGM INBOARD OF HINGE CORRODED. REPAIRED IAW FOKKER SRM 52-02-02 FIGURE 1, SHEET1, PAGES 2 A ND 3. 2 L 7 2 4F RT A20EU 2001090600109 20010906 00109 EU 2001 9 6 QXEA0101006 1 20010525 A 5310 STRUCTURE FOKKER F28 F28MK4000 4990810 EU TAIL SECTION DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - FUSELAGE TAIL SECTION SKIN/STRINGERS BUCKLED AT RIGHT-HAND STATION 20285, STRINGERS 53, 54, 55. REPAIRED IAW HORIZ ON AIR EA 4-55-291. 2 L 7 2 4F RT A20EU 2001090600110 20010906 00110 EU 2001 9 6 QXEA0101007 1 20010530 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - CRACK PROGRESSING BEYOND STOP DRILL HOLE ON CASTELLATION AT FRAME 32-2 AND STRINGER 48. REPAIRED IAW FOKKER SRM 51 -31-02, PAGES 9 AND 10, SRM 53-02-13, PAGE 5, FIGURE 3 AND SRM 51-31-01, PARAGRAPH 7, PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001090600111 20010906 00111 EU 2001 9 6 QXEA0101008 1 20010530 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - CASTELLATION ON OBLIQUE FRAME 50-2 HAS CRACK PROGRESSING BEYOND STOP DRILL HOLE AT STRINGER 25. REPAIRED IAW FOKKE R SRM 53-02-13, PAGE 5, FIGURE 3, SRM 51-31-02, PAGES 9 AND 10 AND SRM 51-31-01, PARAGRAPH 7, PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001090600112 20010906 00112 EU 2001 9 6 QXEA0101009 1 20010603 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - CRACK ON CASTELLATION PROGRESSING BEYOND STOP DRILL HOLE AT FRAME 50-2 BETWEEN STRINGER 48 AND 49. REPAIRED IAW FO KKER SRM 53-02-13, PAGE 5, FIGURE 3, SRM 51-31-01, PARAGRAPH 7, PAGES 13 AND 14 AND SRM 51-30-02, PAGES 9 AND 10. 2 L 7 2 4F RT A20EU 2001090600113 20010906 00113 EU 2001 9 6 QXEA0101010 1 20010530 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - CATEGORY B CRACK BEYOND LIMITS ON CASTELLATION AT FRAME 32-2 AND STRINGER 27. REPAIED IAW FOKKER SRM 53-02-13, PAG E 5, FIGURE 3, SRM 51-31-02, PAGES 9 AND 10, AND SRM 51-31-01, PARAGRAPH 7, PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001090600114 20010906 00114 EU 2001 9 6 QXEA0101011 1 20010530 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - CRACK PROGRESSING BEYOND STOP DRILL HOLE AT FRAME 32-2 AND STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3, SRM 51-31-02, PAGES 9 AND 10 AND SRM 51-31-01, PARAGRAPH 7, PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001090600115 20010906 00115 EU 2001 9 6 QXEA0101012 1 20010530 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - CRACK PROGRESSING BEYOND STOP DRILL HOLE AT FRAME 50-2 AND STRINGER 53. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3, SRM 51-31-02, PAGE 9 AND 10, AND SRM 51-31-01, PARAGRAPH 7, PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001090600116 20010906 00116 EU 2001 9 6 QXEA0101013 1 20010530 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - CRACKED CASTELLATION AT FRAME 16-2 AND STRINGER 25. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3, SRM 51-31- 02, PAGE 9 AND 10, SRM 51-31-01, PARAGRAPH 7, PAGE 13 AND 14. 2 L 7 2 4F RT A20EU 2001090600117 20010906 00117 EU 2001 9 6 QXEA0101014 1 20010528 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - CRACK AT FRAME 24-2 AND STRINGER 11. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 2, PARAGRAPH 3(A), SRM 53-02-13, PAGE 5, FIGURE 3, SRM 51-31-01, PARAGRAPH 7, PAGE 13 AND 14 AND SRM 51-30-02, PAGE 9 AND 10. 2 L 7 2 4F RT A20EU 2001090600118 20010906 00118 EA 2001 9 6 ASOA01122 1 20010730 A 3350 362624 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 853AS 7374 FLT 4519 - DURING GROUND INSPECTION IN ATL, CREW OBSERVED SEVERAL FLOOR EMERGENCY LIGHTS WERE BURNED OUT. MAINTENANCE R EMOVED AND REPLACED SEVERAL FLOOR LIGHTS STRIPS WITH BURNED OUT BULBS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVIC E. (M) 2 L 7 2 4F RT A21EA 2001090600119 20010906 00119 EA 2001 9 6 ASOA01123 1 20010731 A 3350 362624 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 833AS 7246 DURING GROUND INSPECTION IN ATL, CREW FOUND GREEN FLOOR EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE FORWARD GREEN EMERGENCY TRACK LIGHTING SECTION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2001090600120 20010906 00120 EA 2001 9 6 ASOA01124 1 20010801 A 3397 64643 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN DEFECTIVE A K NONE L NO TEST IN INSP/MAINT 1 SO 11 837AS 7271 DURING GROUND INSPECTION IN ATL, CREW REPORTED PORTIONS OF THE EMERGENCY FLOOR LIGHTING ARE INOPERATIVE. MAINTENANCE RE MOVED AND REPLACED THE CENTER FLOOR SECTION CABLE ASSEMBLY AT ROWS 2-5. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVI CE. (M) 2 L 7 2 4F RT A21EA 2001090600121 20010906 00121 EA 2001 9 6 ASOA01126 1 20010803 A 3397 59465 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN DEFECTIVE A K NONE L NO TEST IN INSP/MAINT 1 SO 11 860AS 7433 DURING GROUND INSPECTION IN ATL, CREW REPORTED EMERGENCY LIGHT ON DECK FROM ROW 6 AND FORWARD WERE INOPERATIVE. MAINTEN ANCE REMOVED AND REPLACED POWER STRIP CABLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2001090600122 20010906 00122 SO 2001 9 6 ASOA01128 1 20010805 A 5311 FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 503AS 120275 DURING SCHEDULED MAINTENANCE IN MCN, CORROSION WAS DISCOVERED AT FRAME 23, STRINGERS 20 LEFT TO 19 RIGHT. MAINTENANCE R EPAIRED AIRCRAFT IAW ASA EO 120-53-0165. THIS EO CONTAINS REPAIR SPECIFICATIONS FOR CORROSION REPAIR AT FRAME 23, STRIN GERS 20 LEFT TO 19 RIGHT. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001090600123 20010906 00123 EU 2001 9 6 QXEA0101015 1 20010530 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - CASTELLATION CRACK AT FRAME 17565 AND STRINGER 23. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3, SRM 51-31-0 2, PAGES 9 AND 10, SRM 51-31-01, PARAGRAPH 7, PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001090600124 20010906 00124 SO 2001 9 6 ASOA01129 1 20010806 A 3350 31880 TERMINAL EMB 120 EMB120 3260201 SO CABIN BROKEN A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 264AS 120185 DURING HANGAR MAINTENANCE IN TXK, THE AFT EXIT SIGN ON THE RIGHT HAD A BROKEN WIRE. MAINTENANCE REMOVED AND REPLACED TH E BROKEN WIRE TERMINAL ON THE RIGHT AFT EMERGENCY EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001090600125 20010906 00125 EU 2001 9 6 QXEA0101016 1 20010530 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - CRACKED CASTELLATION AT FRAME 16-2 AND STRINGER 26. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3, SRM 51-31- 02, PAGES 9 AND 10 AND SRM 51-31-01, PARAGRAPH 7, PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001090600126 20010906 00126 EU 2001 9 6 ASOA01130 1 20010806 A 5311 FRAME AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 630AS 336 DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND AT FRAMES 36, 38, 39, 40 AND 41. CORROSION WAS ALSO FOUND ON THE FORWARD RADAR ALTIMETER CUT OUT BETWEEN FRAMES 15 AND 16. THIS AIRCRAFT IS STILL IN C-CHECK. ASA ENGINEERING IS CURREN TLY WRITING AN EO. (M) 2 H 7 2 4T RT 2001090600127 20010906 00127 EU 2001 9 6 QXEA0101017 1 20010529 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU BULKHEAD OUT OF POSITION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - STIFFENING ANGLE, AFT SIDE REAR PRESSURE BULKHEAD AT BUTT LINE 1050L AND HORIZONTAL BEAM INCORRECTLY POSITION BETW EEN BEAM 11 AND 10. REPOSITIONING OF ANGLE CARRIED OUT. 2 L 7 2 4F RT A20EU 2001090600128 20010906 00128 EU 2001 9 6 QXEA0101018 1 20010531 A 5310 STRUCTURE FOKKER F28 F28MK4000 4990810 EU TAIL SECTION DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - FUSELAGE, TAIL SECTION, OBLIQUE FRAME 16-2 AT STRINGER 59-61, WEB, OIL CANNING. REPAIRED IAW FOKKER SRM 53-02-01, PAGE 4, FIGURE 2, SRM 51-31-01, PARAGRAPH 7, PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001090600129 20010906 00129 EA 2001 9 6 ASOA01133 1 20010811 A 3350 362624 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 853AS 7374 FLT 4632 - DURING GROUND INSPECTION IN ATL, EMERGENCY FLOOR LIGHTING WAS INOPERATIVE FROM ROW 8 AFT. MAINTENANCE REMOVE D AND REPLACED THE EMERGENCY LIGHTING CABLE ASSEMBLY AND THE FLOOR LIGHTING STRIPS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2001090600130 20010906 00130 EU 2001 9 6 QXEA0101019 1 20010603 A 5320 WEB FOKKER F28 F28MK4000 4990810 EU TAIL SECTION CANNING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - FUSELAGE, TAIL SECTION, OBLIQUE FRAME 16-2 AT STRINGER 58-59 WEB OIL CANNING. REPAIRED IAW FOKKER SRM 53-02-01, PA GE 11, FIGURE 9. 2 L 7 2 4F RT A20EU 2001090600131 20010906 00131 EU 2001 9 6 QXEA0101020 1 20010531 A 5551 FITTING FOKKER F28 F28MK4000 4990810 EU HORIZONTAL STAB GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - HORIZONTAL STAB DRIVE FITTING LEFT-HAND ARM GOUGED. REPAIRED IAW HORIZON AIR EA 4-55-293. 2 L 7 2 4F RT A20EU 2001090600132 20010906 00132 EU 2001 9 6 QXEA0101021 1 20010529 A 5551 FITTING FOKKER F28 F28MK4000 4990810 EU HORIZONTAL STAB CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - HORIZONTAL STAB DRIVE FITTING RIGHT-HAND AND LEFT-HAND LOWER LUGS HAVE MINOR CORROSION. REPAIRED IAW HORIZON AIR E A 4-55-292 AND FOKKER SRM 51-10-04, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 2001090600133 20010906 00133 EA 2001 9 6 ASOA01134 1 20010811 A 2750 CONTROL UNIT CNDAIR CL600 CL6002B19 EA T/E FLAP MALFUNCTIONED A ASOA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION IN INSP/MAINT 1 SO 11 845AS 7324 DURING FLIGHT FROM YOW TO ATL, FLAPS FAILED AT 8 DEGREES. THE CAPTAIN DECLARED AN EMERGENCY. AIRCRAFT DIVERTED AND LAN DED SAFELY IN SYR. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT BRAKE AND POSITION SENSING UNIT. MAINTENANCE AL SO REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT AND THE LEFT FLAP ACTUATOR. (M) 2 L 7 2 4F RT A21EA 2001090600134 20010906 00134 EU 2001 9 6 ASOA01136 1 20010811 A 2913 4019501 PUMP AEROSP ATR72 ATR72 EU EQUIPT BAY LEAKING A ASOA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 11 641AS 2233 387 FLT 4288 - DURING FLIGHT FROM CHA TO ATL, THE BLUE HYDRAULIC SYSTEM FAILED. AN EMERGENCY WAS DECLARED. AIRCRAFT CONTIN UED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE BLUE AC HYDRAULIC PUMP. OPERATIONAL CHECK S GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT 2001090600135 20010906 00135 EU 2001 9 6 QXEA0101023 1 20010529 A 5542 SKIN FOKKER F28 F28MK4000 4990810 EU RUDDER CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - CHAFE DAMAGE ON NOSE OF RUDDER 8 INCHES BELOW MID HINGE OPENING. REPAIRED IAW FOKKER SRM 55-02-07, FIGURE 1. 2 L 7 2 4F RT A20EU 2001090600136 20010906 00136 EU 2001 9 6 QXEA0101024 1 20010531 A 5510 STRUCTURE FOKKER F28 F28MK4000 4990810 EU HORIZONTAL STAB DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - STRUCTURE CRACKED AT RIVET ON RIGHT HAND SIDE. REPAIRED IAW FOKKER SRM 55-02-07, FIGURE 2 AND CHAPTER 51. 2 L 7 2 4F RT A20EU 2001090600137 20010906 00137 NM 2001 9 6 P2EA01145 1 20010806 A 5330 SKIN BOEING 737 7372T5 NM FUSELAGE DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 120NJ 22979 DURING Q-CHECK, FOUND TWO DENTS RIGHT SIDE OF AFT OUT FLOW VALVE. REPAIRED FUSELAGE SKIN SECTION FROM BS 907 TO BS 922 BETWEEN STRINGER 21 RIGHT AND 23 RIGHT DUE TO DENTS IAW SRM 53-30-3, FIG 28. (M) 2 L 7 2 4F RT A16WE 2001090600138 20010906 00138 EU 2001 9 6 QXEA0101025 1 20010606 A 5511 RIB FOKKER F28 F28MK4000 4990810 EU HORIZONTAL STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - RIB 3.2 CRACKED ALONG AFT LEFT-HAND RADIUS. REPAIRED IAW HORIZON AIR EA 4-55-294. 2 L 7 2 4F RT A20EU 2001090600139 20010906 00139 EU 2001 9 6 QXEA0101026 1 20010603 A 2710 GUIDE FOKKER F28 F28MK4000 4990810 EU ALERON SYSTEM WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - AILERON ANTI-UP FLOAT CABLE GUIDE A STATION 7306 WORN. REPAIRED IAW FOKKER SRM 51-31-01, PARAGRAPH 7, PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001090600140 20010906 00140 EU 2001 9 6 QXEA0101027 1 20010523 A 5753 FLAP TRACK FOKKER F28 F28MK4000 4990810 EU TE FLAPS DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - LEFT-HAND OUTBOARD 5280 FLAP TRACK DENTED AT AFT END. REPAIRED IAW HORIZON AIR EA 4-53-1488. 2 L 7 2 4F RT A20EU 2001090600141 20010906 00141 EU 2001 9 6 QXEA0101028 1 20010531 A 5330 PANEL FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - 16 FASTENERS PULLING THOURGH PANEL 91J. REPAIRED IAW HORIZON AIR EA 4-53-1493. 2 L 7 2 4F RT A20EU 2001090600142 20010906 00142 NM 2001 9 6 P2EA01146 1 20010806 A 5330 SKIN BOEING 737 7372T5 NM FUSELAGE DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 120NJ 22979 DURING Q-CHECK, EXTERNAL FUSELAGE SKIN WITH DENT AT BS 1051, BETWEEN STRINGER 16 LEFT AND 17 LEFT. REPAIRED FUSELAGE SK IN SECTION FROM BS 1047.5 TO BS 1055.5 BETWEEN STRINGER 16 LEFT AND 17 LEFT DUE TO DENT IAW SRM 53-30-3, FIG 19. (M) 2 L 7 2 4F RT A16WE 2001090600143 20010906 00143 EU 2001 9 6 QXEA0101029 1 20010527 A 5320 STRINGER CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - Z STRINGER 2.20 TIE CLIP CRACKED ON RIGHT-HAND BOTTOM SIDE OF CENTER WING SECTION. REPAIRED IAW FOKKER SRM 53-02-1 7, PAGE 11, FIGURE 6, SRM 51-30-02, PAGES 9 AND 10 AND SRM 51-31-01, PARAGRAPH 7, PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001090600144 20010906 00144 EU 2001 9 6 QXEA0101030 1 20010530 A 5315 FLOORBEAM FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 YYC - CRACKED STIFFNER ON CENTER FLOORBEAM AT FRAME 12405 BELOW FLOOR PANEL 94AD. REPAIRED IAW FOKKER SRM 51-31-01, PARA GRAPH 7, PAGES 13 AND 14. 2 L 7 2 4F RT A20EU 2001090600145 20010906 00145 NM 2001 9 6 P2EA01148 1 20010803 A 5330 SKIN BOEING 737 7372T5 NM FUSELAGE DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 120NJ 22979 SJO - DURING Q-CHECK, EXTERNAL FUSELAGE SKIN WITH DENT AT BS 807, BETWEEN STRINGER 26 LEFT AND 27 RIGHT. REPAIRED FUSEL AGE SKIN SECTION FROM BS 789.5 TO BS 815 BETWEEN STRINGER 25 LEFT TO STRINGER 26 RT DUE TO DENT IAW SRM 53-30-3, FIG 06. (M) 2 L 7 2 4F RT A16WE 2001090600146 20010906 00146 EU 2001 9 6 QXEA0101031 1 20010611 A 3350 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487US 11238 PDX - CREW REPORTED MID CABIN OVER HEAD EXIT SIGN INOPERATIVE. REMOVED AND REPLACED MID CABIN EXIT SIGN. OPERATIONAL CHE CKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001090600147 20010906 00147 NM 2001 9 6 P2EA01149 1 20010804 A 5313 STRINGER BOEING 737 7372T5 NM FUSELAGE CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 120NJ 22979 DURING Q-CHECK, FOUND LOWER FUSELAGE AFT CARGO COMPARTMENT AT BS 968, STRINGER 27 RIGHT WITH CORROSION. S/D - REPAIRED STRINGER 27 RIGHT FROM BS 958.5 TO BS 976 DUE TO CORROSION IAW SRM 53-10-3, FIG 01. (M) 2 L 7 2 4F RT A16WE 2001090600148 20010906 00148 NM 2001 9 6 QXEA0101032 1 20010613 A 3310 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 360PH 515 EAT - CREW REPROTED STRONG ELECTRICAL SMELL EMINATING FROM THE LAV. REMOVED AND LAMP. STOWED ELECTRICAL CABLES. PLACED O N DEFERED MAINTENANCE LIST. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001090600149 20010906 00149 NM 2001 9 6 P2EA01150 1 20010806 A 5330 SKIN BOEING 737 7372T5 NM FUSELAGE DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 120NJ 22979 DURING Q-CHECK, FOUND EXTERNAL FUSELAGE SKIN WITH DENT AT BS 1040, BETWEEN STRINGER 27 LEFT AND 27 RIGHT. S/D - REPAIRE D FUSELAGE SKIN SECTION FROM BS 1030 TO BS 1057 BETWEEN STRINGER 27 RIGHT AND STRINGER 24 LEFT DUE TO DENT IAW SRM 53-30 -3, FIG 06. (M) 2 L 7 2 4F RT A16WE 2001090600150 20010906 00150 NM 2001 9 6 QXEA0101035 1 20010615 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 350PH 488 SEA- FLIGHT ATTENTANT ADVISES THAT HALF OF EMERGENCY LIGHTS ARE INOP. MAINTENANCE REPLACED POWER SUPPLY PS6. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001090600151 20010906 00151 NM 2001 9 6 P2EA01151 1 20010809 A 5311 FRAME BOEING 737 7372T5 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 120NJ 22979 DURING Q-CHECK, FUSELAGE AFT CARGO COMPARTMENT AT FRAME BS 807, BETWEEN STRINGER 27 LEFT AND 27 RIGHT, LOWER SECTION WIT H CRACK. S/D - REPAIRED FRAME SECTION AT BS 807 BETWEEN STRINGER 27 RIGHT AND STRINGER LEFT DUE TO CRACK IAW SRM 53-10- 4, FIG 06. (M) 2 L 7 2 4F RT A16WE 2001090600152 20010906 00152 NM 2001 9 6 P2EA01152 1 20010805 A 5315 FLOORBEAM BOEING 737 7372T5 NM FUSELAGE CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 120NJ 22979 SJO - DURING Q-CHECK, FOUND PAX CABIN AT BS 294, BETWEEN BL 0 AND RBL 40 INCHES, WL 208, UPPER SECTION AND BS 294.5 BETW EEN BL 0 AND LBL 30, FLOORBEAM WITH CORROSION. (M) 2 L 7 2 4F RT A16WE 2001090600153 20010906 00153 NM 2001 9 6 P2EA01153 1 20010808 A 5330 SKIN BOEING 737 7372T5 NM FUSELAGE DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 120NJ 22979 DURING Q-CHECK, FOUND EXTERNAL FUSELAGE SKIN WITH DENT AT BS 590, STRINGER 1. S/D - REPAIRED FUSELAGE SKIN SECTION FROM BS 590 TO BS 599 BETWEEN STRINGER 2 LEFT AND 2 RIGHT DUE TO DENT IAW SRM 53-30-3, FIG 7. (M) 2 L 7 2 4F RT A16WE 2001090600154 20010906 00154 NM 2001 9 6 P2EA01154 1 20010808 A 5330 SKIN BOEING 737 7372T5 NM FUSELAGE DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 120NJ 22979 DURING Q-CHECK, FOUND EXTERNAL SKIN WITH DENT AT BS 500A PLUS 12 INCHES, BETWEEN STRINGER 1 AND 2 LEFT. (M) 2 L 7 2 4F RT A16WE 2001090600155 20010906 00155 2001 9 6 P2EA01155 4 20010810 A 2230 AUTOTHRUST SYS DOUG DC9 DC987 3022087 WP COCKPIT MALFUNCTIONED A P2EA K NONE O OTHER NR NOT REPORTED 1 CE 05 132NJ 49780 FLT 945 - MCI - WITH AUTO THROTTLES ON AND ENGINE SYNC OFF OR N1, THE RIGHT THROTTLE RETARDS OVERTIME 10 PERCENT TO 20 P ERCENT. PERFORMED TROUBLE SHOOTING AND 'RETURN TO SERVICE TEST' IAW MM 22-31-00, NO FAULTS NOTED. (M) 2 L 7 2 4F RT A6WE 2001090600156 20010906 00156 NM 2001 9 6 P2EA01156 1 20010814 A 5330 DOUBLER BOEING 737 7372T5 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 120NJ 22979 SJO - DURING Q-CHECK, EXTERNAL FUSELAGE DOUBLER WITH CRACK AT BS 1138, WL 266 LEFT SIDE. (M) 2 L 7 2 4F RT A16WE 2001090600157 20010906 00157 NM 2001 9 6 P2EA01157 1 20010810 A 5312 BULKHEAD BOEING 737 7372T5 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 120NJ 22979 DURING Q-CHECK INSPECTION PER S/B 737-53A1173, FOUND PRESSURE BULKHEAD BS 178, WEB CRACKED AT RBL 11.5-WL 213, PRESSURE BULKHEAD BS 178 FLOOR WEB SECTION CRACKED AT SL 207, PRESSURE BULKHEAD BS 178 LEFT SIDE LATERAL CHORD CRACKED AT WL 207, PRESSURE BULKHEAD BS 178 LEFT AND RIGHT INTERCOSTALS CRACKED AT WL 195. (M) 2 L 7 2 4F RT A16WE 2001090600158 20010906 00158 NM 2001 9 6 P2EA01158 1 20010812 A 5313 STRINGER BOEING 737 7372T5 NM FUSELAGE DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 120NJ 22979 SJO - DURING Q-CHECK, LOWER FUSELAGE TAIL CONE STRINGER 27 LEFT WITH DENT AT BS 1035. REPAIRED STRINGER 27 LEFT FROM BS 1032 TO BS 1045 DUE TO DENT IAW SRM 53-10-3, FIG 01. (M) 2 L 7 2 4F RT A16WE 2001090600159 20010906 00159 NM 2001 9 6 P2EA01159 1 20010813 A 5330 SKIN BOEING 737 7372T5 NM FUSELAGE CANNING A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 120NJ 22979 DURING Q-CHECK, FOUND EXTERNAL FUSELAGE WITH OIL CAN AT BS 901, BETWEEN STRINGER 21 AND 22 RIGHT. REPAIRED FUSELAGE SKI N SECTION FROM BS 898.5 TO BS 902.5 BETWEEN STRINGER 21 AND 22 RT DUE TO OIL CAN IAW SRM 53-30-3, FIG 05. (M) 2 L 7 2 4F RT A16WE 2001090600160 20010906 00160 2001 9 6 P2EA01160 4 20010815 A 2210 AUTOPILOT SYS BOEING 737 737230 NM COCKPIT MALFUNCTIONED A P2EA O OTHER O OTHER CL CLIMB 1 CE 05 124NJ 22122 FLT 350 - MCI - AUTO PILOT A CHANNEL WOULD NOT STAY ENGAGED DURING CLIMB-OUT OR CRUISE. DEFERRED AUTO PILOT A CHANNEL I AW MEL 22-1, CI NR M124864 PER MAINTENANCE CONTROL. (M) 2 L 7 2 4F RT A16WE 2001090600161 20010906 00161 NM 2001 9 6 QXEA0101036 1 20010615 A 5210 MECHANISM DHAV DHC8 DHC8202 2809007 NM PAX DOOR DIRTY A QXEA K NONE O OTHER NR NOT REPORTED 1 NM 09 353PH 496 SEA- MAIN CABIN DOOR DOES NOT OPEN FREELY. MAINTENANCE LUBRICATED CABLE DRUM. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2001090600162 20010906 00162 NM 2001 9 6 P2EA01162 1 20010818 A 5330 SKIN BOEING 737 7372T5 NM FUSELAGE DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 120NJ 22979 SJO - DURING Q-CHECK, FOUND EXTERNAL FUSELAGE SKIN WITH DENT AT BS 500A PLUS 12, BETWEEN STRINGER 1 AND STRINGER 2L. RE PAIRED FUSELAGE SKIN SECTION FROM BS 500A PLUS 7 INCHES TO 500B, BETWEEN STRINGER 2 LEFT AND STRINGER 2 RIGHT DUE TO DEN T IAW SRM 53-30-3 FIG 07. (M) 2 L 7 2 4F RT A16WE 2001090600163 20010906 00163 NM 2001 9 6 QXEA0101037 1 20010614 A 5210 MECHANISM DHAV DHC8 DHC8102 2809003 NM PAX DOOR DIRTY A QXEA K NONE O OTHER NR NOT REPORTED 1 NM 09 830PH 314 SEA- MAIN CABIN DOOR DIFFICULT TO OPEN. MAINTENANCE CLEANED AND LUBRICATED DOOR MECHANISM. OPERATIONAL CHECKS GOOD. AIRC RAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2001090600164 20010906 00164 NM 2001 9 6 QXEA0101038 1 20010616 A 5210 MECHANISM DHAV DHC8 DHC8102 2809003 NM PAX DOOR DIRTY A QXEA K NONE O OTHER NR NOT REPORTED 1 NM 09 830PH 314 PDX- MAIN CABIN DOOR VERY HARD TO OPEN. MAINTENANCE CLEANED AND LUBRICATED DOOR STOPS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2001090600165 20010906 00165 EU 2001 9 6 QXEA0101039 1 20010615 A 2530 CA16707 RECEPTACLE FOKKER F28 F28MK4000 4990810 EU GALLEY ARCED A QXEA K NONE O OTHER NR NOT REPORTED 1 NM 09 476US 11224 SEA- ELECTRICAL SMELL COMING FROM COFFEE POT. SMELL WENT AWAY WHEN TURNED OFF. MAINTENANCE INSPECTED AIRCRAFT AND FOUND TOP COFFEE RECPTICLE SHOWING SIGNS OF ARCING. REPLACED RECPTICLE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001090600166 20010906 00166 NM 2001 9 6 P2EA01163 1 20010815 A 5347 CARGO TRACK BOEING 737 7372T5 NM FUSELAGE CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 120NJ 22979 DURING Q-CHECK, FOUND FORWARD CARGO COMPARTMENT FROM BS 380 TO BS 520 LBL 18.5, CARGO TRACK WITH CORROSION. (M) 2 L 7 2 4F RT A16WE 2001090600167 20010906 00167 EU 2001 9 6 QXEA0101042 1 20010608 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PDX - AT FRAME 3820/3870 AND MAIN ENTRANCE DOOR TORSION BOX CONNECTION ANGLE HAS CORROSION AT A RIVE TAIL. REPAIRED IAW FOKKER SRM 51-30-02. 2 L 7 2 4F RT A20EU 2001090600168 20010906 00168 EU 2001 9 6 QXEA0101043 1 20010608 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PDX - AT FRAME 4900 AND MAIN ENTRANCE DOOR TORSION BOX CONNECTION ANGLE IS CORRODED AT A HILOCK AND AT AN ADJACENT BOLT HEAT. REPAIRED IAW FOKKER SRM 51-30-02. 2 L 7 2 4F RT A20EU 2001090600169 20010906 00169 NM 2001 9 6 QXEA0101045 1 20010615 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - LEFT-HAND OUTBOARD SEAT TRACK AT X333.300 HAS PITTING CORROSION. REPAIRED IAW DHC-8 CPM CHAPTER 5, PAGES 5-4 AND 5 -5 AND HORIZON AIR EA 2-53-285. 2 H 7 2 4T RT A13NM 2001090600170 20010906 00170 NM 2001 9 6 QXEA0101046 1 20010615 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - LEFT-HAND OUTBOARD SEAT TRACK AT X312.350 HAS PITTING CORROSION. REPAIRED IAW DHC-8 CPM CHAPTER 5, PAGES 5-4 AND 5 5, HORIZON AIR EA 2-53-285. 2 H 7 2 4T RT A13NM 2001090600171 20010906 00171 NM 2001 9 6 QXEA0101047 1 20010615 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - LEFT-HAND OUTBOARD SEAT TRACK AT X290.000 HAS PITTING CORROSION. REPAIRED IAW DHC-8 CPM CHAPTER 5, PAGES 5-4 AND 5 .5, AND HORIZON AIR EA 2-53-285. 2 H 7 2 4T RT A13NM 2001090600172 20010906 00172 NM 2001 9 6 QXEA0101048 1 20010616 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - LEFT-HAND OUTBOARD SEAT TRACK AT X260.000 HAS PITTING CORROSION. REPAIRED IAW DHC-8 CPM CHAPTER 5, PAGES 5-4 AND 5 -5 AND HORIZON AIR EA 2-53-285. 2 H 7 2 4T RT A13NM 2001090600173 20010906 00173 NM 2001 9 6 QXEA0101049 1 20010616 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND OUTBOARD SEAT TRACK AT X436.500 HAS PITTING CORROSION. REPAIRED IAW DHC-8 CPM CHAPTER 5, PAGES 5-4 AND 5-5 AND HORIZON AIR EA 2-53-286. 2 H 7 2 4T RT A13NM 2001090600174 20010906 00174 NM 2001 9 6 QXEA0101050 1 20010615 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND OUTBOARD SEAT TRACK AT X445.500 HAS A GOUGE. REPAIRED IAW DHC-8 CPM CHAPTER 5, PAGES 5-4 AND 5-5, AND H ORIZON AIR EA 2-53-286. 2 H 7 2 4T RT A13NM 2001090600175 20010906 00175 NM 2001 9 6 QXEA0101051 1 20010615 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND OUTBOARD SEAT TRACK AT 456.500 HAS SURFACE CORROSION. REPAIRED IAW DHC-8 CPM CHAPTER 5, PAGES 5-4 AND 5 -5, AND HORIZON AIR EA 2-53-286. 2 H 7 2 4T RT A13NM 2001090600176 20010906 00176 NM 2001 9 6 QXEA0101052 1 20010616 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSEAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND OUTBOARD SEAT TRACK AT X488.500 HAS SURFACE CORROSION. REPAIRED IAW DHC-8 CPM CHAPTER 5, PAGES 5-4 AND 5-5, AND HORIZON AIR EA 2-53-286. 2 H 7 2 4T RT A13NM 2001090600177 20010906 00177 NM 2001 9 6 P2EA01164 1 20010815 A 5320 FLOOR SUPPORT BOEING 737 7372T5 NM FUSELAGE CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 120NJ 22979 DURING Q-CHECK, AFT CARGO COMPARTMENT BETWEEN BS 767 AND BS 847 AT STRINGER 25 RIGHT FLOOR SUPPORT WITH CORROSION. (M) 2 L 7 2 4F RT A16WE 2001090600178 20010906 00178 NM 2001 9 6 QXEA0101053 1 20010616 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND OUTBOARD SEAT TRACK AT APPROXIMATELY X505.000 CHAFE DAMAGE. REPAIRED IAW DHC-8 CPM CHAPTER 5, PAGE 5-4 AND 5-5, AND HORIZON AIR EA 2-53-286. 2 H 7 2 4T RT A13NM 2001090600179 20010906 00179 EU 2001 9 6 QXEA0101058 1 20010618 A 3350 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 479AU 11228 GEG - EXIT SIGN ABOVE FLIGHT COMPARTMENT DOOR INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001090600180 20010906 00180 NM 2001 9 6 USAABB01031 1 20010524 A 2121 FAN BOEING 767 7672B7 1385107 NM CABIN ODOR A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 653US 24894 LGW - FLT 49 EN ROUTE CDG-PIT, PASSENGER NOTED AN UNUSUAL ODOR IN THE VICINITY OF ROW 19. FLIGHT DIVERTED TO LGW AND LA NDED WITHOUT FURTHER INCIDENT. MAINTENANCE WAS ABLE TO ASSOCIATE THE ODOR WITH THE RECIRCULATION FANS. (M) 2 L 7 2 4F RT A1NM 2001090600181 20010906 00181 NM 2001 9 6 QXEA0101059 1 20010621 A 2120 UNKNOWN DHAV DHC8 DHC8202 2809007 NM CABIN ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 350PH 488 PDX - DURING PREFLIGHT INSPECTION, FLIGHT CREW NOTED ACRID ODOR IN BOTH THE FLIGHT COMPARTMENT AND THE CABIN. INSPECTED RADIO RACK, FLIGHT COMPARTMENT INSTURMENTS, AND CIRCUIT BREAKERS. NO DEFECTS NOTED. COULD NOT DUPLICATE. AIRCRAFT OPERAT IONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001090600182 20010906 00182 NM 2001 9 6 QXEA0101061 1 20010621 A 2430 RECEPTACLE DHAV DHC8 DHC8* NM GALLEY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX- FOUND THE GROUND POWER RECEPTICAL DAMAGED. REPAIRED GOUND POWER RECEPTICAL IN ACCORDENCE WITH ENGINEERING AUTHORIZA TION 6-53-16. OPERATIONAL CHECKS GOOD. REQUIRED INSPECTION COMPLIED WITH. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001090600183 20010906 00183 NM 2001 9 6 QXEA0101062 1 20010623 A 5540 RUDDER DHAV DHC8 DHC8202 2809007 NM VERTICAL STAB DAMAGED A QXEA K NONE O OTHER NR NOT REPORTED 1 NM 09 374PH 528 SEA - DENT IN VERTICAL STABILIZER SECTION OF RUDDER. DENT DETERMEND TO BE OUT OF LIMITS. AFFECTED DAMAGED AREA REMOVED A ND REPAIRED IN ACCORDENCE WITH STRUCTERAL REPAIR MANUAL 55-40-28. THIS DEEMED A REQUIRED INSPECTION ITEM. INSPECTION COM PLIED WITH. MAJOR REPAIR FOUND TO BE AIRWORTHY. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001090600184 20010906 00184 EU 2001 9 6 QXEA0101063 1 20010623 A 5240 STRUCTURE FOKKER F28 F28MK4000 4990810 EU SERVICE DOOR CRACKED A QXEA K NONE O OTHER NR NOT REPORTED 1 NM 09 480AU 11229 PDX - DURING INSPECTION, FOUND SERVICE DOOR CRACKED. REPAIRED VIA THE INSTALLATION OF DOUBLER AND FILLER IN ACCORDENCE W ITH STRUCTURAL REPAIR MANUAL 51-31-01. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001090600185 20010906 00185 NM 2001 9 6 QXEA0101065 1 20010625 A 2120 ODOR DHAV DHC8 DHC8102 2809003 NM CABIN DETECTED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 828PH 287 MFR - FLIGHT CREW REPORTED A STRONG HYDRAULIC SMELL IN THE CABIN AND FLIGHT COMPARTMENT DURING START UP. UPON INSPECTION , SMELL COULD NOT BE DUPLICATED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001090600186 20010906 00186 NM 2001 9 6 QXEA0101066 1 20010625 A 2150 ACM DHAV DHC8 DHC8102 2809003 NM ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 828PH 287 PDX - CREW REPORTED OILY ODOR IN FLIGHT COMPARTMENT AT START UP. REMOVED AND REPLACED AIR CYCLE MACHINE. INSPECTED P2/P3 VALVE ASSEMBLY. ENGINE AND PRESSURIZATION CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001090600187 20010906 00187 NM 2001 9 6 QXEA0101067 1 20010623 A 5210 MECHANISM DHAV DHC8 DHC8102 2809003 NM PAX DOOR LACK OF LUBE A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 830PH 314 PDX - MAIN CABIN DOOR REPORTED DIFFICULT TO OPEN. CLEANED AND LUBED DOOR STOPS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURN ED TO SERVICE. 2 H 7 2 4T RT A13NM 2001090600188 20010906 00188 EU 2001 9 6 QXEA0101068 1 20010627 A 3350 5515400009 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 482US 11231 GEG - MID CABIN OVERHEAD EMERGENCY EXIT LIGHTS REPORTED INOPERATIVE. REMOVED AND REPLACED EXIT SIGN CIRCUIT CARD. OPERAT IIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001090600189 20010906 00189 EU 2001 9 6 QXEA0101069 1 20010626 A 3350 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 488US 11240 PDX - OVERHEAD EXIT SIGNS REPORTED INOPERATIVE. REMOVED AND REPLACED EXIT SIGNS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETUR NED TO SERVICE. 2 L 7 2 4F RT A20EU 2001090600190 20010906 00190 EU 2001 9 6 QXEA0101070 1 20010626 A 3350 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 491US 11156 BOI - MID CABIN OVERHEAD EXIT SIGN REPORTED INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECK GOOD. AIRCRAF T RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001090600191 20010906 00191 EU 2001 9 6 QXEA0101073 1 20010630 A 2740 SWITCH FOKKER F28 F28MK4000 4990810 EU HORIZONTAL STAB STUCK A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 497US 11173 LAX - DURING CLIMB, FLIGHT CREW NOTED HORIZONTAL STABILIZER CHANNEL WARNING LIGHTS ILLUMINATED. FOUND SPRING BOX STICKIN G SWITCH OUT OF ADJUSTMENT. MADE PROPER ADJUSTMENTS, NO PARTS REPLACED. FUNCTIONALLY CHECKED STABILIZER MOVEMENT. OPERAT IONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001090600192 20010906 00192 GL 2001 9 6 ALG2001F00019 2 20010629 A 7260 6893673 PINION GEAR ALLSN 250C47 BELL 407 407 SW ALLSN 250C 250C* GL GEARBOX GALLED A ALGA O OTHER J WARNING INDICATION CR CRUISE 1 SW 03 58236 163 CAG47047 53069 CAE847085 IN FLIGHT, CHIP LIGHT ILLUMINATED. UPON DISASSEMLBLY OF GEARBOX, FOUND EXCESSIVE GALLING ON GEAR TEETH OF PINION GEAR, GEAR TEETH. PINION GEAR EXCESSIVE GALLING DUE TO IMPROPER GEAR TEETH MESHING AND EXCESSIVE LOAD TO TORQUE AREA. INSURE GEAR HARDNESS AND MESHING OF GEAR TEETH BY VENDOR. 1 G 7 1 3U 3 U O H2SW E4CE 2001090600193 20010906 00193 EU 2001 9 6 QXEA0101074 1 20010630 A 3350 LIGHT FOKKER F28 F28MK4000 4990810 EU CABIN FALSE ACTIVATION A QXEA K NONE O OTHER NR NOT REPORTED 1 NM 09 477AU 11226 SEA - FLIGHT CREW REPORTED THAT EMERGENCY LIGHTS ILLUMINATED WITH THE SWITCH IN ARM POSITION. FOUND CORROSION AND BREAKA GE OF WIRES AT ROW 9. REPAIRED AS REQUIRED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001090600194 20010906 00194 NM 2001 9 6 QXEA0101075 1 20010629 A 3230 PROXIMITY SENSOR DHAV DHC8 DHC8* NM MLG FAILED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 400QX 4030 SUN - DURING CRUISE, LANDING GEAR DOORS OPENED, FOLLOWED BY IN-TRANSIT LIGHTS IN FLIGHT COMPARTMENT. REMOVED AND REPLACE D RH MAIN LANDING GEAR UPLOCK ACTUATOR PROXIMITY SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001090600195 20010906 00195 SW 2001 9 6 ALG2001F00020 1 20010714 A 6510 406040340101 DISC PACK BELL 407 BELL 407 407 SW ALLSN 250C 250C* GL T/R DRIVE CRACKED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 58236 RNFS1826 53069 DURING 25 HOUR AD INSPECTION. DISC COUPLING CRACKED. 1 G 7 1 3U 3 U O H2SW E4CE 2001090600196 20010906 00196 SW 2001 9 6 ALG2001F00021 1 20010714 A 6510 407340340101 DISC PACK BELL 407 407 SW ALLSN 250C 250C* GL T/R DRIVE CRACKED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 1116H A195 53046 DURING 25 HOUR INSPECTION, DISC PACK IS CRACKED. 1 G 7 1 3U 3 U O H2SW E4CE 2001090600197 20010906 00197 GL 2001 9 6 ALG2001F00023 2 20010808 A 7200 ENGINE BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL ENGINE MAKING METAL A ALGA O OTHER J WARNING INDICATION LD LANDING 1 SW 03 139H 3216 CAE833257 ENGINE CHIP LIGHT ILLUMINATED ON LANDING. FOUND LARGE FLAKE ON BOTTOM CHIP PLUG. REPLACED ENGINE ASSEMBLY. 1 G 7 1 3U 3 U H2SW E4CE 2001090600198 20010906 00198 2001 9 6 KBMA88665 4 20010712 A 3120 1U569001 GAUGE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT INTERMITTENT E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 350SH 4953 2957 GAUGE IS READING INTERMITTENTLY. REMOVED AND REPLACED WITH SV GAUGE. 1 G 7 1 3U 3 U NC H9EU E19EU 2001090600199 20010906 00199 EU 2001 9 6 KBMA88675 1 20010717 A 7714 56337078012 INDICATOR SNIAS 350 AS350B1 8680811 EU COCKPIT INTERMITTENT E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 53SH 183 2009 NG GAUGE - GAUGE IS INTERMITTENT. REPLACED WITH LOANER UNIT WHILE OUT FOR REPAIR. 1 G 7 1 3U H9EU 2001090600200 20010906 00200 EA 2001 9 6 MJQ2001F00000 1 20010806 A 2820 600628567 FITTING CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF34* NE FUEL SYSTEM LEAKING A MJQR O OTHER K FLUID LOSS NR NOT REPORTED 1 GL 13 604PM 575 5354 FITTING DEVELOPED A CUT IN THE RUBBER ALLOWING FUEL TO LEAK INTO SHROUD, DRAINING OVERBOARD, THRU DRAIN. 2 L 7 2 4F 4 F RT A21EA E15NE 2001090600201 20010906 00201 NM 2001 9 6 QXEA0101076 1 20010621 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - SCRATCH IN FUSELAGE SKIN MEASURING .5 LONG, .031 WIDE AND APPROXIMATELY .005 DEEP, LOCATED AT STATION X119, JUST A FT OF NOSE LANDING GEAR. REPAIRED IAW DHC-8 SRM 51-20-16, PAGE 4. 2 H 7 2 4T RT A13NM 2001090600202 20010906 00202 NM 2001 9 6 QXEA0101077 1 20010620 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - FRAME STATION 167.000, CASTELLATION IS CORRODED BETWEEN STRINGERS 29 AND 30L. REPAIRED IAW HORIZON AIR EA 2-53-293 , STEPS 1 THROUGH 7. 2 H 7 2 4T RT A13NM 2001090600203 20010906 00203 NM 2001 9 6 QXEA0101078 1 20010620 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - FRAME STATION 167.000, CASTELLATION IS CORRODED BETWEEN STRINGERS 30 AND 31L. REPAIRED IAW DHC PSM, CHAPTER 4 AND HORIZON AIR EA 2-53-293, STEPS 1 THROUGHT 7. 2 H 7 2 4T RT A13NM 2001090600204 20010906 00204 NM 2001 9 6 QXEA0101079 1 20010620 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - FRAME STATION 151.600, CASTELLATION BETWEEN STRINGER 30 AND 31L IS CORRODED AT BUCKTAIL REPAIRED IAW DHC-8 SRM 51- 20-16, PAGES 2 THROUGH 4, PARAGRAPH 4 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001090600205 20010906 00205 NE 2001 9 6 MWEA011074 2 20010723 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE RIGHT VIBRATION A MWEA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 GL 31 601ME 49762 725366 FLIGHT ATTENDANT REPORTED A LOUD VIBRATION FROM THE LAVATORYS UP TO ROW 11 ON TAKE OFF AND AT CRUISE. MAINTENANCE PERFOR MED, VIBRATION CHECK ALL WITHIN LIMITS. 2 L 7 2 4F 4 F RT A6WE E9NE 2001090600206 20010906 00206 NM 2001 9 6 QXEA0101080 1 20010619 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - FRAME STATION 151.600 CASTELLATION IS CORRODED BETWEEN STRINGERS 30 AND 31R. REPAIRED IAW DHC-8 PSM CHAPTER 4 AND SRM 51-20-16, PAGES 2 THROUGH 4, PARAGRAPH 4. 2 H 7 2 4T RT A13NM 2001090600207 20010906 00207 NM 2001 9 6 QXEA0101081 1 20010617 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - FRAME STATION 167.000 CASTELLATION IS CORRODED BETWEEN STRINGERS 30 AND 31R. REPAIRED IAW DHC-8 CPM CHAPTER 4 AND CHAPTER 5. 2 H 7 2 4T RT A13NM 2001090600208 20010906 00208 NM 2001 9 6 QXEA0101082 1 20010625 A 5311 STRINGER DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND STRINGER 31 CORRODED AT RIVETS BETWEEN FRAME STATION 151.600 AND 167.000. REPAIRED IAW RD 8-53-925 AND HORIZON AIR EA 2-53-298. 2 H 7 2 4T RT A13NM 2001090600209 20010906 00209 NM 2001 9 6 QXEA0101083 1 20010616 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - FRAME STATION 467.000, CASTELLATION BETWEEN STRINGER 22L AND 23L IS CORRODED. REPAIRED IAW DHC-8 PSM 1-GEN-5, CHAP TER 5. 2 H 7 2 4T RT A13NM 2001090600210 20010906 00210 NM 2001 9 6 QXEA0101084 1 20010616 A 5100 STRUCTURE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - CORROSION AROUND NUT PLATE, UNDER RIGHT-HAND 144HZ, INBOARD AFT CORNER. REPAIRED IAW DHC-8 1-GEN-5, CHAPTER 4, SRM 51-20-11 AND MM 20-32-02. 2 H 7 2 4T RT A13NM 2001090600211 20010906 00211 WP 2001 9 6 MWEA011124 1 20010810 A 5320 991175111 ANGLE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 BULKHEAD PANEL ATTACH ANGLE TO CENTER TANK HAS A CRACK LOCATED JUST FORWARD OF KEEL BEAM AT STATION 604. -- REMOVED AT TACH ANGLE, LOCATED, DRILLED AND INSTALLED ANGLE. 2 L 7 2 4F A6WE 2001090600212 20010906 00212 NM 2001 9 6 QXEA0101085 1 20010621 A 5310 STRUCTURE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - 261NT HAS MINOR FRETTING CORROSION. REPAIRED IAW RD 8-53-3366. 2 H 7 2 4T RT A13NM 2001090600213 20010906 00213 NM 2001 9 6 QXEA0101086 1 20010621 A 5330 PANEL DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - LEADING EDGE OF PANEL 262AT HAS FRETTING CORROSION. REPAIRED IAW RD8-53-3366. 2 H 7 2 4T RT A13NM 2001090600214 20010906 00214 NM 2001 9 6 QXEA0101087 1 20010625 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - AT STATION 302 AND STRINGER 3L THERE ARE 3 SKIN DENTS MEASURING .015" DEEP, .035" DEEPT AND .030" DEEP. REPAIRED I AW HORIZON AIR EA 2-53-300 AND RD 8-53-5947. 2 H 7 2 4T RT A13NM 2001090600215 20010906 00215 NM 2001 9 6 QXEA0101088 1 20010614 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND INBOARD SEAT TRACK AT X234.400 HAD PITTING CORROSION. REPAIRED IAW RD 8-53-1339. 2 H 7 2 4T RT A13NM 2001090600216 20010906 00216 NM 2001 9 6 QXEA0101089 1 20010614 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND INBOARD SEAT TRACK AT X252.700 HAS CHAFE DAMAGE. REPAIRED IAW RD 8-53-1339. 2 H 7 2 4T RT A13NM 2001090600217 20010906 00217 NM 2001 9 6 QXEA0101090 1 20010614 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND INBOARD SEAT TRACK AT STATION 252.700 HAS PITTING CORROSION. REPAIRED IAW RD 8-53-1339. 2 H 7 2 4T RT A13NM 2001090600218 20010906 00218 NM 2001 9 6 QXEA0101091 1 20010614 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND INBOARD SEAT TRACK AT STATION 270.500 HAS PITTING CORROSION. REPAIRED IAW RD 8-53-1339. 2 H 7 2 4T RT A13NM 2001090600219 20010906 00219 WP 2001 9 6 MWEA011125 1 20010810 A 5311 9957740 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 KEEL BEAM AREA LEFT SIDE FRAME STATION 658 HAS A CRACK ON OUTBOARD END. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001090600220 20010906 00220 NM 2001 9 6 QXEA0101092 1 20010615 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND INBOARD SEAT TRACK AT STATION 570.000 HAS PITTING AT CREW HOLES. REPAIRED IAW DHC-8 SRM 51-20-16 AND RD 8-53-784. 2 H 7 2 4T RT A13NM 2001090600221 20010906 00221 NM 2001 9 6 QXEA0101093 1 20010616 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND INBOARD SEAT TRACK AT STATION 580.500 HAS SURFACE CORROSION AROUND SCREW HOLES. REPAIRED IAW DHC-8 PSM 1-GEN-5, CHAPTER 5 AND RD 8-53-784. 2 H 7 2 4T RT A13NM 2001090600222 20010906 00222 WP 2001 9 6 MWEA011126 1 20010810 A 5311 9957740 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 KEEL BEAM AREA LEFT SIDE, FRAME STATION 622 HAS A CRACK ON OUTBOARD END. FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 2001090600223 20010906 00223 NM 2001 9 6 QXEA0101094 1 20010616 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND INBOARD SEAT TRACK AT STATION 597.500 HAS SEVERAL SCRATCHES. REPAIRED IAW DHC-8 PSM 1-GEN-5, CHAPTER 5 AND HORIZON AIR EA 2-53-287. 2 H 7 2 4T RT A13NM 2001090600224 20010906 00224 NM 2001 9 6 QXEA0101095 1 20010616 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND INBOARD SEAT TRACK AT STATION 597.500 HAS PITTING CORROSION AROUND SCREW HOLES. REPAIRED IAW DHC-8 PSM 1-GEN-5, CHAPTER 5 AND HORIZON AIR EA 2-53-287. 2 H 7 2 4T RT A13NM 2001090600225 20010906 00225 NM 2001 9 6 QXEA0101096 1 20010614 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND INBOARD SEAT TRACK HAS TWO GOUGES AT STATION 215. REPAIRED IAW RD 8-53-1339. 2 H 7 2 4T RT A13NM 2001090600226 20010906 00226 NM 2001 9 6 QXEA0101097 1 20010620 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - NR 7 SEAT TRACK REQUIRES REPLACEMENT FOR NUMEROUS DISPCREPANCIES. REPLACED NR 7 SEAT TRACK IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001090600227 20010906 00227 2001 9 6 MWEA011130 4 20010819 A 3421 258733513 GYRO DOUG DC9 DC932 3022066 WP E/E BAY FAILED A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 207ME 47794 ON CLIMB OUT WX RADAR ATT FAILURE DISPLAYED INTERMITTENTLY (MOSTLY ON) IN ALL RANGES. VERIFIED BAD NR 1 VG REMOVED AND R EPLACED SAME, RETURNED ANTENNA CONNECTOR BACK TO J1 SYSTEM. OPERATION CHECK OK. REF DC9 MM 34-27-0 AND 34-41-0. 2 L 7 2 4F A6WE 2001090600228 20010906 00228 NM 2001 9 6 QXEA0101098 1 20010618 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - NR 4 SEAT TRACK REQUIRES REPLACEMENT FOR NUMEROUS DISCREPANCIES. REPLACED NR 4 SEAT TRACK IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001090600229 20010906 00229 NM 2001 9 6 QXEA0101099 1 20010620 A 5320 ANGLE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - CRACKED STRINGER CONNECTION ANGLE AT STATION 240 AND Z100.032 AT BOTTOM OF MAIN PASSENGER DOOR OPENING UNDER THRES HOLD. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001090600230 20010906 00230 NM 2001 9 6 QXEA0101100 1 20010616 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM LT WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - LEFT-HAND WING FORWARD SPAR, UPPER FLANGE AT STATION 285 THROUGH STATION 325 HAS SEVERAL GOUGES IN FLANGE SURFACE. REPAIRED IAW RD 8-57-1119. 2 H 7 2 4T RT A13NM 2001090600231 20010906 00231 NM 2001 9 6 QXEA0101101 1 20010614 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND NR 4 FLAP TRACK OUTBOARD SIDE ROLLER TRACK HAS ONE SPOT SURFACE CORROSION AND ONE SPOT PITTING NEAR FOR WARD END ROLLER TRAVEL. REPAIRED IAW HORIZON AIR EA 2-57-113 AND RD 8-57-988, STEP 2. 2 H 7 2 4T RT A13NM 2001090600232 20010906 00232 WP 2001 9 6 MWEA011131 1 20010822 A 5310 59174637 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 AFT VENTRAL DOOR JAMB PAN HAS A CRACK NEAR TOP RIGHT CORNER. REMOVED AND REPLACED DOOR JAMB SECTION. MAINTENANCE FOUND S TRICKER PAN DAMAGED BEYOND LIMITS. REMOVED AND REPLACED NEW STRICKER PAN. FABRICATED AND INSTALLED REPAIR SPLICE. 2 L 7 2 4F A6WE 2001090600233 20010906 00233 NM 2001 9 6 QXEA0101102 1 20010614 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND NR 4 FLAP TRACK OUTBOARD, LOWER ROLLER FLANGE HAS TWO SPOTS OF PITTING NEAR FORWARD END OF ROLLER TRACK /TRAVEL. REPAIRED IAW HORIZON AIR E A2-57-113 AND RD 8-57-988. 2 H 7 2 4T RT A13NM 2001090600234 20010906 00234 NM 2001 9 6 QXEA0101103 1 20010616 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND NR 5 FLAP TRACK OUTBOARD, LOWER ROLLER FLANGE PITTED AT FORWARD END OF ROLLER TRAVEL. REPAIRED IAW HORI ZON AIR EA 2-57-112 AND RD 8-57-989, STEP 2. 2 H 7 2 4T RT A13NM 2001090600235 20010906 00235 WP 2001 9 6 MWEA011133 1 20010822 A 5311 39122253 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FORWARD CARGO COMPARTMENT FRAME STATION 351 HAS LIGHT CORROSION ON AFT SIDE FROM LONGERON 29 LEFT TO 29 RIGHT. FABRICATE D AND INSTALLED SPLICE REPAIR. 2 L 7 2 4F A6WE 2001090600236 20010906 00236 NM 2001 9 6 QXEA0101104 1 20010616 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND NR 5 FLAP TRACK OUTBOARD SIDE ROLLER TRACK HAS PITTING AT FORWARD END OF ROLLER TRAVEL. REPAIRED IAW HO RIZON AIR EA 2-57-112. 2 H 7 2 4T RT A13NM 2001090600237 20010906 00237 NM 2001 9 6 QXEA0101105 1 20010616 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND NR 5 FLAP TRACK LOWER, INBOARD ROLLER FLANGE HAS TWO SPOTS OF PITTING NEAR FORWARD END OF ROLLER TRAVEL . REPAIRED IAW HORIZON AIR EA 2-57-112 AND RD 8-57-989, STEP 2. 2 H 7 2 4T RT A13NM 2001090600238 20010906 00238 NM 2001 9 6 QXEA0101106 1 20010613 A 5210 STRUCTURE DHAV DHC8 DHC8202 2809007 NM PAX DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - VERY LIGHT SURFACE CORROSION AT SHIM LOCATIONS ON MAIN CABIN DOOR SHELL. REPAIRED IAW DHC-8 SRM 51-20-11 AND SRM 5 2-00-16. 2 H 7 2 4T RT A13NM 2001090600239 20010906 00239 WP 2001 9 6 MWEA011134 1 20010822 A 5320 99236893 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FORWARD CARGO COMPARTMENT INTERCOSTAL BETWEEN LONGERON 27 RIGHT AND 28 RIGHT FROM STATION 484 TO 503 HAS LIGHT CORROSION AROUND NUT PLATES. FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001090600240 20010906 00240 NM 2001 9 6 QXEA0101107 1 20010616 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - BAGGAGE DOOR EXTERNAL SKIN DAMAGE - SCRATCH/GOUGE UPPER SECTION. REPAIRED IAW DHC-8 SRM 52-00-16. 2 H 7 2 4T RT A13NM 2001090600241 20010906 00241 NM 2001 9 6 QXEA0101108 1 20010619 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - BAGGAGE DOOR, EXTERNAL SKIN DAMAGE, SCRATCH AND DENT LOWER MID SECTION. REPAIRED IAW RD 8-52-230, PAGE 5, STEP 7. 2 H 7 2 4T RT A13NM 2001090600242 20010906 00242 NM 2001 9 6 QXEA0101109 1 20010621 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - SCRATCH IN FUSELAGE SKIN APPROXIMATELY .5 LONG, .031 WIDE AT STATION X597 AND STRINGER Y30. REPAIRED IAW DHC-8 SRM 51-20-16, PAGE 4 AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2001090600243 20010906 00243 NM 2001 9 6 QXEA0101110 1 20010626 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - IMPACT DAMAGE TO FUSELAGE SKIN BELOW CARGO DOOR STATION X547 AND STRINGER Y25. DAMAGED AREA APPROXIMATELY 18" LONG BY 14" WIDE. REPAIRED IAW DHC-8 SRM 53-00-16, SRM 51-20-11 AND HORIZON AIR EA 2-53-296. 2 H 7 2 4T RT A13NM 2001090600244 20010906 00244 NM 2001 9 6 QXEA0101111 1 20010626 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - SCRATCH IN FUSELAGE SKIN JUST AFT OF FORWARD DRAIN BELOW CARGO DOOR SILL MEASURES 1 1/8 INCH LONG, 1.8 INCH WIDE A ND APPROXIMATELYS .003 DEEP. REPAIRED IAW HORIZON AIR EA 2-53-296. 2 H 7 2 4T RT A13NM 2001090600245 20010906 00245 NM 2001 9 6 QXEA0101112 1 20010615 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - LEFT HAND OUTBOARD SEAT TRACK AT X531.000 HAS SURFACE CORROSION. REPAIRED IAW RD 8-53-3644 AND DHC-8 CPM, CHAPTER 5, PAGES 5-4 AND 5-5. 2 H 7 2 4T RT A13NM 2001090600246 20010906 00246 NM 2001 9 6 QXEA0101113 1 20010615 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - LEFT HAND OUTBOARD SEAT TRACK AT X521.050 HAS GOUGE. REPAIRED IAW DHC-8 CPM CHAPTER 5, PAGES 5-4 AND 5-5. 2 H 7 2 4T RT A13NM 2001090600247 20010906 00247 NM 2001 9 6 QXEA0101114 1 20010615 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - LEFT-HAND OUTBOARD SEAT TRACK AT X366.050 HAS PITTING CORROSION. REPAIRED IAW HORIZON AIR EA 2-53-285 AND DHC-8 CP M CHAPTER 5, PAGES 4-5 AND 5-5. 2 H 7 2 4T RT A13NM 2001090600248 20010906 00248 NM 2001 9 6 QXEA0101115 1 20010615 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - REPLACED NR 10 SEAT TRACK DUE TO CORROSION OUT OF LIMITS. REPLACED SEAT TRACK IAW DHC-8 SRM 51-40-11 AND RD 8-51-1 02. 2 H 7 2 4T RT A13NM 2001090600249 20010906 00249 NM 2001 9 6 QXEA0101116 1 20010615 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND INBOARD SEAT TRACK AT X234.500 NUT PLATE FLANGE HAS PITTING CORROSION. BLENDED CORROSION WITHOUT EXCEED ING LIMITS. 2 H 7 2 4T RT A13NM 2001090600250 20010906 00250 NM 2001 9 6 QXEA0101117 1 20010618 A 5410 STRUT DHAV DHC8 DHC8202 2809007 NM NR 1 NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - NR 1 ENGINE NACELLE LOWER OUTBOARD FORWARD STRUT CHAFED .002 DEEP, 1 1/2 TO 3 INCHES AFT OF FORWARD FIREWALL. REPA IRED IAW HORIZON AIR EA 2-54-77. 2 H 7 2 4T RT A13NM 2001090600251 20010906 00251 NM 2001 9 6 QXEA0101118 1 20010621 A 5412 FIREWALL DHAV DHC8 DHC8202 2809007 NM RT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND NACELLE FIREWALL CRACKED OUTBOARD OF EXHAUST DUCT APPROXIMATELY 10 O'CLOCK POSITION. REPAIRED IAW DHC-8 RD 8-54-806. 2 H 7 2 4T RT A13NM 2001090600252 20010906 00252 NM 2001 9 6 QXEA0101119 1 20010615 A 5330 PANEL DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - LIGHT FRETTING CORROSION AT MATING SURFACE ON BOTH ENDS OF FUEL PANEL 524 AT. REPLACED FUEL PANEL 524AT WITH NEW P ANEL IAW PANEL CARD P22 FOR INSTALLATION. 2 H 7 2 4T RT A13NM 2001090600253 20010906 00253 NM 2001 9 6 QXEA0101120 1 20010620 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - LEFT-HAND WING FORWARD SPAR, LOWER FLANGE WHERE LEADING EDGE ATTACHES HAS MILD FRETTING CORROSION BETWEEN STATION 178 THROUGH 225. REPAIRED IAW HORIZON AIR EA 2-57-114. 2 H 7 2 4T RT A13NM 2001090600254 20010906 00254 NM 2001 9 6 QXEA0101121 1 20010622 A 5751 BEARING DHAV DHC8 DHC8202 2809007 NM AILERON TAB LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND AILERON TAB OUTBOARD BEARING HAS RADIAL PLAY. REPAIRED IAW DHC-8-200 MM, PAGE 403 AND 404, TASK 27-13-1 1-400-801, PARAGRAPH 3(A), STEP 7 AND PARAGRAPH 4(A). 2 H 7 2 4T RT A13NM 2001090600255 20010906 00255 NM 2001 9 6 QXEA0101122 1 20010616 A 5751 BEARING DHAV DHC8 DHC8202 2809007 NM AILERON HINGE LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND AILERON INBOARD HINGE BEARING HAS RADIAL PLAY. REPLACED IAW DHC-8 MM 20-21-52 AND TASK CARD 9200001, 1- 4. 2 H 7 2 4T RT A13NM 2001090600256 20010906 00256 WP 2001 9 6 MWEA011135 1 20010822 A 5313 591140129 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 LONGERON 27 RIGHT AT STATION 195 CORRODED IN THE E&E BAY. FABRICATED AND INSTALLED LONGERON SECTION AND SPLICE. 2 L 7 2 4F A6WE 2001090600257 20010906 00257 NM 2001 9 6 QXEA0101123 1 20010614 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND NR 4 FLAP TRACK OUTBOARD, LOWER ROLLER FLANGE PITTED, TWO SPOTS ON UPPER SURFACE AT FORWARD END OF ROLL ER TRAVE. REPAIRED IAW HORIZON AIR EA 2-57-113 2 H 7 2 4T RT A13NM 2001090600258 20010906 00258 NM 2001 9 6 QXEA0101124 1 20010614 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND NR 4 FLAP TRACK OUTBOARD SIDE ROLLER TRACK HAS PITTING AT FORWARD END OF ROLLER TRAVEL. REPAIRED IAW HO RIZON AIR EA 2-57-113. 2 H 7 2 4T RT A13NM 2001090600259 20010906 00259 WP 2001 9 6 MWEA011136 1 20010822 A 5311 991151551 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 CAP LOCATED AT STATION 160 FROM APPROXIMATELY LONGERON 5 LEFT TO LONGERON 17 LEFT JUST FORWARD OF PAX DOOR JAMB IS CORRO DED OUT OF LIMITS. REMOVED AND REPLACED CAP. 2 L 7 2 4F A6WE 2001090600260 20010906 00260 WP 2001 9 6 MWEA011137 1 20010822 A 5521 99185433 RIB DOUG DC9 DC932 3022066 WP RT ELEVATOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 RIGHT ELEVATOR OUTBOARD RIB THAT ATTACHES TO THE COUNTERBALANCE HORN HAS EXCESSIVE CORROSION. FABRICATED AND INSTALLED R H ELEVATOR RIB. 2 L 7 2 4F A6WE 2001090600261 20010906 00261 WP 2001 9 6 MWEA011138 1 20010822 A 5311 9957740 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 KEEL BEAM AREA RIGHT SIDE, FRAME STATION 637 IS CRACKED AND HAS LIGHT CORROSION ON OUTBOARD END. -- FABRICATED AND INS TALLED REPAIR ANGLE. 2 L 7 2 4F A6WE 2001090600262 20010906 00262 NM 2001 9 6 MWEA011139 1 20010830 A 5313 593666713 LONGERON DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 AFT CARGO COMP LIGHT CORROSION ON LONGERON 30 JUST FORWARD OF STATION 1271. FABRICATED AND INSTALLED LONGERON SECTION AN D REPAIR SPLICE. 2 L 7 2 4F RT A6WE 2001090600263 20010906 00263 NM 2001 9 6 MWEA011140 1 20010830 A 5330 5911412309 DOUBLER DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 CENTER CARGO COMPARTMENT HAS HEAVY CORROSION ON THE ANTENNA DOUBLER BETWEEN STATION 674 AND 693. FABRICATED AND INSTALLE D DOUBLER. 2 L 7 2 4F RT A6WE 2001090600264 20010906 00264 NM 2001 9 6 MWEA011141 1 20010830 A 5347 1D0026B CARGO TRACK DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 BARE METAL AND LIGHT CORROSION ON LEFT TIE DOWN RAIL STATION 370 -446 UPPER AND LOWER SURFACE. FABRICATED AND INSTALLED TIE DOWN RAIL AND SPLICES. 2 L 7 2 4F RT A6WE 2001090600265 20010906 00265 WP 2001 9 6 MWEA011143 1 20010822 A 5320 995791761 SPLICE DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 AFT CARGO STATION 937 FRAME SPLICE PLATE ON TOP SIDE HAS LIGHT CORROSION ABOVE LONGERON 27 - 28 LEFT AB35. MAINTENANCE F OUND NUMEROUS MISDRILLED HOLES ON SPLICE PLATE AND REQUIRES REPLACEMENT.FABRICATED AND INSTALLED SPLICE PLATE. 2 L 7 2 4F A6WE 2001090600266 20010906 00266 NE 2001 9 6 MWEA011144 2 20010822 A 7200 JT8D9A ENGINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE LEFT OVERTEMP A MWEA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 GL 31 209ME 47730 667163 ON TAKE OFF LEFT ENGINE REACHED 605-610 DEGREES CELSIUS AFTER V1, ABOUT 40 SECONDS AFTER TAKE OFF POWER WAS REDUCED TO B RING TEMP BACK TO 590 DEGREES CELSIUS AT A NORMAL CLIMB, POWER SETTING ENGINE TEMP WAS 545 DEGREES CELSIUS MCI TEMP 37 D EGREES CELSIUS EPR 1.91 AT TAKE OFF TIME. AT 10,000 FEET 250 KNOTS OUTSIDE AIR TEMPERATURE PLUS 20 DEGREES LEFT ENGINE T EMP 300 DEGREES CELSIUS RIGHT ENGINE 220 DEGREES CELSIUS. REMOVED AND REPLACED THE ENGINE 2 L 7 2 4F 4 F A6WE E2EA 2001090600267 20010906 00267 WP 2001 9 6 MWEA011145 1 20010827 A 5753 4701562509 FITTING DOUG DC9 DC932 3022066 WP T/E FLAP WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 LEFT FLAP, INBOARD FIXED VANE, INBOARD FITTINGS, FORWARD AND AFT ARE WORN. FABRICATED AND INSTALLED FITTINGS. 2 L 7 2 4F A6WE 2001090600268 20010906 00268 WP 2001 9 6 MWEA011146 1 20010827 A 5260 991038111 FRAME DOUG DC9 DC932 3022066 WP VENTRAL STAIRS CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 AFT VENTRAL STAIR FRAME HAS MODERATE CORROSION ON THE STEP LEFT SIDE JUST FORWARD OF THE APU FIRE HORN. -- FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001090600269 20010906 00269 WP 2001 9 6 MWEA011147 1 20010827 A 5320 99196285 BRACKET DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 AFT CARGO DOOR AFT HINGE ATTACH BRACKETS HAVE ELONGATED HOLES AT STATION 926. FABRICATED AND INSTALLED BRACKETS. 2 L 7 2 4F A6WE 2001090600270 20010906 00270 WP 2001 9 6 MWEA011148 1 20010827 A 5320 99196289 BRACKET DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 AFT CARGO DOOR FORWARD HINGE ATTACH BRACKETS HAVE ELONGATED HOLES AT STATION 906. FABRICATED AND INSTALLED HINGE BRACKET S. 2 L 7 2 4F A6WE 2001090600271 20010906 00271 WP 2001 9 6 MWEA011152 1 20010827 A 5320 99367184 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 AFT CARGO INTERCOSTAL AT LONGERON 28 RIGHT HAS LIGHT CORROSION ON TOP SIDE BETWEEN STATION 980-996 AB63. FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001090600272 20010906 00272 WP 2001 9 6 MWEA011153 1 20010827 A 5311 995821519 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 AFT CARGO STATION 918 FRAME HAS LIGHT CORROSION ON FORWARD SIDE BETWEEN LONGERON 30-29 RIGHT AB68. FABRICATED AND INSTAL LED FRAME SECTION, FRAME SPLICES, AND PLATES. 2 L 7 2 4F A6WE 2001090600273 20010906 00273 WP 2001 9 6 MWEA011154 1 20010827 A 5320 99576621 ANGLE DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 AFT CARGO DOOR AFT HINGE BRACKET ATTACH ANGLE AT STATION 926 HAS CORROSION ON UPPER FLANGE. -- FABRICATED AND INSTALLE D ANGLE. 2 L 7 2 4F A6WE 2001090600274 20010906 00274 WP 2001 9 6 MWEA011155 1 20010827 A 5311 5911448517 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 AFT CARGO BAY FRAME AT STATION 851 HAS LIGHT CORROSION FROM LONGERON 29 RIGHT TO 28 LEFT. REMOVED AND REPLACED FRAME SEC TION. FABRICATED AND INSTALLED SHIMS. 2 L 7 2 4F A6WE 2001090600275 20010906 00275 WP 2001 9 6 MWEA011158 1 20010827 A 5320 99155534 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FORWARD CARGO COMPARTMENT INTERCOSTAL BETWEEN LONGERON 28 LEFT AND 27 LEFT FROM STATION 484 TO 503 HAS LIGHT CORROSION O N TOP SIDE AND AROUND NUT PLATES. FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001090600276 20010906 00276 WP 2001 9 6 MWEA011162 1 20010827 A 5311 9911501 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FRAME AT STATION 47 HAS AN AREA OF CORROSION ON AFT SIDE LOWER RADIUS AND FORWARD SIDE APPROXIMATELY 8 INCHES OUTBOARD O F RIGHT FORWARD CORNER OF DOOR JAMB. REMOVED AND REPLACED FRAME. FABRICATED AND INSTALLED CLIP FOR INTERCOSTAL. 2 L 7 2 4F A6WE 2001090600277 20010906 00277 WP 2001 9 6 MWEA011164 1 20010827 A 5310 5917579159 STRAP DOUG DC9 DC932 3022066 WP FUSELAGE MISALIGNED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 VENTRAL DOOR JAMB UPPER STRAP HAS MISALIGNED HOLES. FABRICATED AND INSTALLED STRIKER STRAP. 2 L 7 2 4F A6WE 2001090600278 20010906 00278 WP 2001 9 6 MWEA011170 1 20010827 A 5230 95200207 PAN DOUG DC9 DC932 3022066 WP CARGO DOOR CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FORWARD CARGO DOOR INNER PAN HAS CHAFES IN RADIUS AT THREE STOP PADS. THIRD STOP FROM TOP ON AFT SIDE AND TOP STOP AND T HIRD FROM TOP ON FORWARD SIDE. FABRICATED AND INSTALLED DOUBLERS. 2 L 7 2 4F A6WE 2001090600279 20010906 00279 WP 2001 9 6 MWEA011172 1 20010827 A 5320 99101516 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 OVERWING AREA SUBFLOOR IS CRACKED AND CORRODED AT STATION 614 APPROXIMATELY 9 INCHES OUTBOARD OF NR 4 SEAT TRACK. FABRIC ATED AND INSTALLED SUBFLOOR REPAIR. 2 L 7 2 4F A6WE 2001090600280 20010906 00280 WP 2001 9 6 MWEA011173 1 20010827 A 5321 995791820 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 CABIN FLOORBOARD E1 HAS CORROSION ON FORWARD EDGE AT STATION 237 BETWEEN NR 3 AND NR 4 SEAT TRACKS. FABRICATED AND INSTA LLED FLOORBOARD SKIN SECTION, HAT CHANNEL, AND INSULATION. 2 L 7 2 4F A6WE 2001090600281 20010906 00281 WP 2001 9 6 MWEA011175 1 20010827 A 5320 99100785 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FLOOR WEB HAS CHAFE MARKS BETWEEN CENTER LINE AND FORWARD SERVICE DOOR STATION 160-200. MAINTENANCE FOUND CRACK ON FLOOR WEB LOWER RIGHT OF CENTER LINE. FABRICATED REPAIR DOUBLER AND FILLER. 2 L 7 2 4F A6WE 2001090600282 20010906 00282 2001 9 6 MWEA011181 4 20010827 A 3160 4055900906 SYMBOL GENERATOR DOUG DC9 DC981 3022081 WP E/E BAY FAILED A MWEA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 812ME 48006 CAPTAIN AND FIRST OFFICER PRIMARY FLIGHT DISPLAY ARE BLANK. REPLACED NR 2 SYMBOL GENERATOR 2 L 7 2 4F A6WE 2001090600283 20010906 00283 WP 2001 9 6 MWEA011186 1 20010829 A 5311 3912237513 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 AFT CARGO BAY FRAME AT STATION 870 HAS MODERATE CORROSION FROM LONGERON 29 RIGHT TO 28 LEFT. REMOVED AND REPLACED FRAME SECTION. FABRICATED ADN INSTALLED SPLICE REPAIR. 2 L 7 2 4F A6WE 2001090600284 20010906 00284 WP 2001 9 6 MWEA011189 1 20010829 A 5312 99115468 BULKHEAD DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 AFT CARGO BAY STATION 996 BULKHEAD HAS CORROSION ON AFT SIDE AT LONGERON 23 TO 29 RIGHT NEAR BOTTOM. FABRICATED AND INST ALLED WEB. 2 L 7 2 4F A6WE 2001090600285 20010906 00285 WP 2001 9 6 MWEA011191 1 20010829 A 5320 991015393 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 CABIN SUBFLOOR IS CRACKED AT STATION 598 RIGHT SIDE. FABRICATED AND INSTALLED WEB SECTION. 2 L 7 2 4F A6WE 2001090600286 20010906 00286 WP 2001 9 6 MWEA011192 1 20010829 A 5320 59203472 FITTING DOUG DC9 DC932 3022066 WP FUSELAGE CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FRAME FITTING AT STATION 579 RIGHT SIDE, AFT SIDE OF FRAME HAS A CHAFE MARK. REMOVED AND REPLACED FRAME FITTING. 2 L 7 2 4F A6WE 2001090600287 20010906 00287 WP 2001 9 6 MWEA011194 1 20010829 A 5310 5912528501 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 AFT CARGO DOOR JAMB IS CHAFED ALONG FORWARD SIDE BETWEEN LONGERONS 24 TO 25 AT STATION 898. FABRICATED AND INSTALLED DOO R JAMB REPAIR. 2 L 7 2 4F A6WE 2001090600288 20010906 00288 WP 2001 9 6 MWEA011195 1 20010829 A 5330 5911426507 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 2 EA DENTS IN FUSELAGE SKIN AT STATION 965 AND LONGERON 11 LEFT. ONE IS 2.5 INCHES ABOVE LONGERON 11 LEFT AND ONE IS 2 I NCHES BELOW LONGERON 11 LEFT. FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 2001090600289 20010906 00289 WP 2001 9 6 MWEA011198 1 20010829 A 5330 99581561 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 WINDOW BELT HAS A CHAFE MARK IN FWD LOWER CORNER OF WINDOW CUTOUT ON LEFT SIDE AT WINDOW #12 STATION 452. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001090600290 20010906 00290 WP 2001 9 6 MWEA011199 1 20010829 A 5412 99122434 BULKHEAD DOUG DC9 DC932 3022066 WP RT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 RIGHT SIDE PYLON BULKHEAD WALL HAS A CRACK IN WEB AT STATION 965 AROUND RIVET FOR SNAP NEAR CENTER OF WALL. FABRICATED A ND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001090600291 20010906 00291 NM 2001 9 6 QXEA0101125 1 20010614 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND NR 4 FLAP TRACK, TOP FLANGE, LOWER SIDE HAS PITTING AT FORWARD END OF ROLLER TRAVEL. REPAIRED IAW HORIZ ON AIR EA 2-57-113. 2 H 7 2 4T RT A13NM 2001090600292 20010906 00292 NM 2001 9 6 QXEA0101126 1 20010614 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND NR 4 FLAP TRACK, LOWER FLANGE, LOWER SURFACE HAS PITTING AT FORWARD END OF ROLLER TRAVEL. REPAIRED IAW HORIZON AIR EA 2-57-113. 2 H 7 2 4T RT A13NM 2001090600293 20010906 00293 NM 2001 9 6 QXEA0101127 1 20010614 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND NR 4 FLAP TRACK INBOARD TOP FLANGE LOWER SURFACE HAS PITTING AT FORWARD END OF ROLLER TRAVEL. REPAIRED IAW HORIZON AIR EA 2-57-113. 2 H 7 2 4T RT A13NM 2001090600294 20010906 00294 WP 2001 9 6 MWEA011203 1 20010829 A 5347 59105234 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 NR 4 SEAT TRACK CHAFFED AT STATION 590. REMOVED AND REPLACED WITH SEAT TRACK SPLICE REPAIR. 2 L 7 2 4F A6WE 2001090600295 20010906 00295 WP 2001 9 6 MWEA011204 1 20010829 A 5743 5919289522 TRUNNION DOUG DC9 DC932 3022066 WP RT MLG CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 RIGHT MAIN LANDING GEAR TRUNNION FITTING HAS CORROSION ON FORWARD AND AFT FACE OF SIDE BRACE ATTACH LUG. FABRICATED AND INSTALLED SHOT PEENING AND SHIM. 2 L 7 2 4F A6WE 2001090600296 20010906 00296 WP 2001 9 6 MWEA011205 1 20010829 A 5751 995757112 SKIN DOUG DC9 DC932 3022066 WP AILERON DELAMINATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 RIGHT AILERON HAS CORROSION UNDER RUB STRIP AT FORWARD INBOARD END. SKIN IS DELAMINATED AT SAME AREA. FABRICATED AND INS TALLED FILLER AND DOUBLER. 2 L 7 2 4F A6WE 2001090600297 20010906 00297 WP 2001 9 6 MWEA011206 1 20010829 A 2760 3923253503 FITTING DOUG DC9 DC932 3022066 WP SPOILER DRIVE CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 RIGHT INBOARD SPOILER DRIVE FITTING ON SPOILER PANEL IS RUBBING ON WITH FITTING OR INBOARD SIDE. INSTALLED T-243 FIXTURE . REMOVED AND REPLACED FITTING . 2 L 7 2 4F A6WE 2001090600298 20010906 00298 WP 2001 9 6 MWEA011212 1 20010830 A 5220 59131951 PAN DOUG DC9 DC932 3022066 WP EMERGENCY DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 LEFT FORWARD EMERGENCY EXIT DOOR PAN IS CRACKED BY THE UPPER FORWARD SUPPORT. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001090600299 20010906 00299 WP 2001 9 6 MWEA011218 1 20010830 A 5313 3924050501 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 LONGERON 28 LEFT HAS 2 EACH CRACKS AT SPLICE STATION 550-560, CRACKS ARE ON EITHER SIDE OF VERTICAL LEGS AND INBOARD CRA CK RUNS 1 INCH BEYOND SPLICE. REMOVED AND REPLACED LONGERON SECTION. 2 L 7 2 4F A6WE 2001090600300 20010906 00300 WP 2001 9 6 MWEA011219 1 20010830 A 5312 59101307 BULKHEAD DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 AFT CARGO COMPARTMENT AFT PRESSURE BULKHEAD HAS SEVERAL AREAS OF LIGHT SURFACE CORROSION. FABRICATED AND INSTALLED DOUBL ERS. 2 L 7 2 4F A6WE 2001090600301 20010906 00301 WP 2001 9 6 MWEA011221 1 20010830 A 5330 5919707501 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 CORROSION ON INNER SURFACE OF SKIN, RIGHT SIDE OF LONGERON 30 AT STATION 988. FABRICATED AND INSTALLED REPAIR DOUBLER AN D FILLER. 2 L 7 2 4F A6WE 2001090600302 20010906 00302 WP 2001 9 6 MWEA011222 1 20010830 A 5711 5911300502 SPAR DOUG DC9 DC932 3022066 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 RIGHT WING AFT SPAR UPPER VERTICAL LEG HAS CORROSION AT STATION XRS 267.0, INBOARD OF UPPER FLAP HINGE BOLT. (XW 251.6) REMOVED CORROSION, INSPECTED, AND BLENDED AREA. ACCEPTABLE PER MWX-ORD-01-004-51H DATED 24 AUGUST 2001. 2 L 7 2 4F A6WE 2001090600303 20010906 00303 WP 2001 9 6 MWEA011223 1 20010830 A 5712 99193074 RIB DOUG DC9 DC932 3022066 WP RT WING CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 RIGHT WING NR 3 SLAT INBOARD IDLER TRACK BOLT CHAFING INTO OUTBOARD RIB. BLENDED AND REPAIRED DAMAGED HI LOCK AREA. 2 L 7 2 4F A6WE 2001090600304 20010906 00304 NM 2001 9 6 MWEA011224 1 20010904 A 5320 59560409 SUPPORT DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 AFT CARGO COMPARTMENT AFT WALL CENTER VERTICAL SUPPORT HAS LIGHT CORROSION AT LOWER RIGHT END. FABRICATED AND INSTALLED ANGLE REPAIR DOUBLERS. 2 L 7 2 4F RT A6WE 2001090600305 20010906 00305 NM 2001 9 6 MWEA011225 1 20010904 A 5320 99367184 INTERCOSTAL DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 AFT CARGO COMPARTMENT, MODERATE CORROSION ON INTERCOSTAL BETWEEN STATION 1309 AND 1322 AND LONGERON 28 AND 27 RIGHT. FA BRICATED AND INSTALLED REPAIR ANGLE. 2 L 7 2 4F RT A6WE 2001090600306 20010906 00306 NM 2001 9 6 MWEA011227 1 20010904 A 5330 591140159 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 E&E BAY CORROSION AROUND ANTENNA MOUNT AND SKIN BETWEEN STATION 178 AND 197 AT LONGERON 29 LEFT AND 30. FABRICATED AND I NSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 2001090600307 20010906 00307 NM 2001 9 6 MWEA011228 1 20010904 A 5330 5911412309 DOUBLER DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 ANTENNA DOUBLER AT STATION 605, LONGERON 29 LEFT AND 30 HAS EXTENSIVE SURFACE CORROSION AROUND FINGER DOUBLERS. ALSO, CO RROSION PRESENT BETWEEN EXTERIOR SKIN AND MOUNTING DOUBLER. REMOVED CORROSION FROM SKIN AND DOUBLERS. BLENDOUTS ARE ACCE PTABLE AS IS IAW MWX-ORD-01-00446G, 20 AUGUST 2001. 2 L 7 2 4F RT A6WE 2001090600308 20010906 00308 NM 2001 9 6 MWEA011229 1 20010904 A 5320 95300827 FLOOR SUPPORT DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 CENTER CARGO COMPARTMENT FLOORING SUPPORT RAILS HAVE SEVERAL AREAS OF LIGHT CORROSION AROUND NUT CLIPS. FABRICATED AND I NSTALLED FLOORING SUPPORT RAIL REPAIR PARTS. 2 L 7 2 4F RT A6WE 2001090600309 20010906 00309 NM 2001 9 6 MWEA011230 1 20010904 A 5320 39364451 ANGLE DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 AFT CARGO COMPARTMENT, LIGHT CORROSION AROUND FASTENERS ATTACHING STATION 1117 TO LONGERON 30. REMOVED AND REPLACED ANGL E. 2 L 7 2 4F RT A6WE 2001090600310 20010906 00310 NM 2001 9 6 MWEA011232 1 20010904 A 5321 9936599501 FLOORBOARD DOUG MD88 MD88 3023688 NM CARGO BAY DELAMINATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 FORWARD PIT CENTER FLOORBOARD STATION 427 - 465 DELAMINATING AROUND EDGES. FABRICATED AND INSTALLED FLOOR BOARD. 2 L 7 2 4F RT A6WE 2001090600311 20010906 00311 NM 2001 9 6 MWEA011235 1 20010904 A 5321 9936600501 FLOORBOARD DOUG MD88 MD88 3023688 NM CARGO BAY DELAMINATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 MID PIT CENTER FLOORBOARD STATION 731-788 DELAMINATING AND CORRODED. FABRICATED AND INSTALLED NEW FLOOR BOARD. 2 L 7 2 4F RT A6WE 2001090600312 20010906 00312 NM 2001 9 6 01FDEA00801 1 20010905 A 2780 40173 SWITCH BOEING 727 727233 138408A NM FAILED A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 SO 25 279FE 22346 01-299 DUR DEPART #2 L/E DEVICE FAILED TO RETRACT. R&R #2 LED SWITCH PER MM 27-82-001. OPS CK OK. 2 L 7 3 4F RT A3WE 2001092600058 20010926 00058 NM 2001 9 26 01FDEA00804 1 20010904 A 5712 RIB BOEING 727 727233 138408A NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 280FE 22347 LT WING LEAD EDGE RIB CRACKED FOR ACTUATOR ROD END CUTOUTS FOR NR 2 SLAT WS 640, WBL 540. REMOVED AND REPLACED RIBS PER SRM 57-30-4. 2 L 7 3 4F RT A3WE 2001092600059 20010926 00059 NM 2001 9 26 01FDEA00805 1 20010904 A 5341 69139017 PIN BOEING 727 727233 138408A NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 280FE 22347 CORROSION ON LT AFT TERMINAL PIN BS 870. REMOVED AND REPLACED TERMINAL PIN PER 57-41-001-4. 2 L 7 3 4F RT A3WE 2001092500095 20010925 00095 NM 2001 9 25 01FDEA00806 1 20010904 A 5312 PRESSURE PANEL BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 280FE 22347 RT NOSE WHEEL WELL SHELF WEB CRACKED AT LIGHTENING HOLE BS 291, WL 156, RBL 18. REMOVED AND REPLACED WEB PER SRM 51-20-1 . 2 L 7 3 4F RT A3WE 2001092500098 20010925 00098 NM 2001 9 25 01FDEA00807 1 20010904 A 5347 CARGO TRACK BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 280FE 22347 CORROSION ON CARGO TRACK NR 6 AT BS 420 TO 440. REMOVED AND REPLACED TRACK PER SRM 53-10-5. 2 L 7 3 4F RT A3WE 2001092500100 20010925 00100 NM 2001 9 25 01FDEA00808 1 20010904 A 5414 SKIN PANEL BOEING 727 727233 138408A NM NR 3 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 280FE 22347 UPPER O/B SKIN PANEL CRACKED ON NR 3 PYLON BS 1203 AT WL 240. REMOVED AND REPLACED PANEL PER SRM 51-20-1. 2 L 7 3 4F RT A3WE 2001092500105 20010925 00105 NM 2001 9 25 01FDEA00809 1 20010904 A 5754 RIB BOEING 727 727233 138408A NM L/E SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 280FE 22347 RT WING NR 5 SLAT ACTUATOR ATTACH RIBS CRACKED WS 408 AND 411, WBL 320 AND 322. ROUTED OUT CRACKS PER SRM 57-50-1. 2 L 7 3 4F RT A3WE 2001090600313 20010906 00313 WP 2001 9 6 MWEA011238 1 20010831 A 3230 29162281 UPLOCK ROLLER DOUG DC9 DC932 3022066 WP LT MLG OUT OF POSITION A MWEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 502ME 48132 LEFT MAIN GEAR RED UNSAFE LIGHT ILLUMINATED AFTER RETRACTION WITH GEAR DOOR OPEN LIGHT OUT. CORRECTLY REPOSITIONED LEFT GEAR DOOR UPLATCH ROLLER AND REPLACED STRIKER BUSHING, BEARING AND ASSOCIATED HARDWARE. 2 L 7 2 4F A6WE 2001090600314 20010906 00314 2001 9 6 COMA0110141 4 20010904 A 3420 6226190204 COMPUTER EMB 120 EMB120RT SO AVIONICS BAY FAULTY A COMA D RETURN TO BLOCK I FLT. ATTITUDE INST. CL CLIMB 1 SO 01 267CA 57980 1259 FLIGHT #5027. DURING CLIMB-OUT OF MCO RECEIVED HEADING AND PITCH CAPTIONS, RE-SETTING THE HEADING MONITOR CLEARED THE P ITCH CAPTION, BUT HEADING CAPTION REMAINED.REPLACED THE AHC-85. 2 L 7 2 4T RT A31SO 2001090600315 20010906 00315 WP 2001 9 6 MWEA011240 1 20010901 A 3340 LIGHT DOUG DC9 DC932 3022066 WP RT WING DEPARTED A MWEA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 GL 31 212ME 47701 AFTER TAKEOFF, PAX REPORTED RIGHT LOGO LIGHT BULB AND LOVER ASSY DEPARTED AIRCRAFT. CREW VERIFIED STRAY WIRES VISIBLE FR OM CABIN AT WING TIP. REPLACED LOGO LIGHT BULB AND LOVER ASSY. REPLACED BROKEN RIGHT AFT NAV LIGHT LENS. 2 L 7 2 4F A6WE 2001090600316 20010906 00316 NM 2001 9 6 MWEA011237 1 20010904 A 5321 99365991 FLOORBOARD DOUG MD88 MD88 3023688 NM CARGO BAY CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 MID PIT FLOORBOARD STATION 630-693 HAD NUMEROUS DENTS AND IS CORRODED AROUND FASTENER HOLES. FABRICATED AND INSTALLED NE W FLOORBOARD. 2 L 7 2 4F RT A6WE 2001090600317 20010906 00317 WP 2001 9 6 MWEA011121 1 20010810 A 5343 5936706506 FITTING DOUG DC9 DC932 3022066 WP NLG CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 NOSE LANDING GEAR RIGHT FORWARD DOOR STOP LINK ATTACH FITTING IS BEING CHAFED BY LINK. LOCATED, DRILLED AND INSTALLED NE W ATTACH FITTING. 2 L 7 2 4F A6WE 2001090600318 20010906 00318 SO 2001 9 6 LR7A01077 1 20010906 A 5312 INTERCOSTAL LKHEED 382 382G 526414U SO FS 607 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 911 4590 DURING INSPECTION PER JOB CARD HSP53127 FOUND LH PRESSURE FAIRING PANEL LBL 61 INTERCOSTAL CRACKED AT FS 603 - 611, WL 2 56.REPLACED INTERCOSTAL IAW SRM SMP 583-51-10, PG 4, PARA G. 2 H 7 4 4T A1SO 2001090600319 20010906 00319 EA 2001 9 6 COMA0160681 1 20010902 A 5100 601R1430353 VANE CNDAIR CL600 CL6002B19 EA INBD FLAP INBD WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 767CA 5665 7285 L/H AND R/H INBD FLAP VANES CHAFFED ON INBD LEADING EDGES.REMOVED AND REPLACED L/H AND R/H INBD INBD FLAP VANE, INBD LEA DING EDGES I/A/W AERODESIGN REPORT #1266-1 REV IR DATED 9/27/94. 2 L 7 2 4F RT A21EA 2001090600321 20010906 00321 EA 2001 9 6 COMA0160682 1 20010904 A 2820 2920030103 CHECK VALVE CNDAIR CL600 CL6002B19 EA CTR FUEL TANK FROZEN A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 767CA 5666 7285 FUEL TRANSFERRING FROM RT TANK TO LT TANK WITH POWER OFF AND A/C SITTING ON LEVEL GROUND.REMOVED APU XFEED CHECK VALVE W HICH WAS STUCK OPEN BY A PIECE OF FOREIGN MATERIAL. INSTALLED NEW VALVE. 2 L 7 2 4F RT A21EA 2001090600322 20010906 00322 NM 2001 9 6 EIA2001233 1 20010817 A 3040 GROUND WIRE BOEING 747 747273C 1384896 NM R1 WINDOW LOOSE A EIAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 471EV 20651 LCK - R1 WINDOW WIRES SMOKING IN FLIGHT. CREW PULLED CIRCUIT BREAKER AND CONTINUED FLIGHT WITHOUT FURTHER INCIDENT. SY STEM REMAINS DEACTIVATED PER MEL 30-11-1. MAINTENANCE TECHNICIANS FOUND AND SECURED A LOOSE GROUND WIRE. INSPECTED AND OPERATED SYSTEM ON GROUND. NO SMOKE OR SMELL. WIRING HARNESS COOL TO THE TOUCH. REACTIVATED AND REMOVED DMI. (M) 2 L 7 4 4F A20WE 2001090600323 20010906 00323 WP 2001 9 6 EIA2001234 1 20010730 A 5311 FRAME DOUG DC9 DC915F 3022037 WP FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 916F 47044 MZJ - FOUND STATION 897 LEFT L17 FRAME CRACKED. REPAIRED PER SRM 51-30-05, 53-03, FIGURE 32, SHT 5, AND 51-10-2, 51-10- 3. (M) 2 L 7 2 4F A6WE 2001090600324 20010906 00324 WP 2001 9 6 EIA2001237 1 20010720 A 5313 LONGERON DOUG DC9 DC915F 3022037 WP FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 916F 47044 MZJ - FOUND CORROSION ON LONGERON 30 NEAR STATION 290. FABRICATED AND INSTALLED REPAIR STRAP ON LONGERON 30 AT STATION 290 PER ECRA 916-53-033-2. (M) 2 L 7 2 4F A6WE 2001090600325 20010906 00325 WP 2001 9 6 EIA2001238 1 20010801 A 5310 DOUBLER DOUG DC9 DC915F 3022037 WP FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 916F 47044 FOUND LEFT FORWARD ENTRANCE DOOR FORWARD UPPER CORNER INNER DOUBLER HAS TWO CRACKS FROM EDGE GOING FORWARD. REMOVED DAM AGE AND INSTALLED REPAIR DOUBLERS AND FILLERS PER ECRA 916-53-030-2. (M) 2 L 7 2 4F A6WE 2001090600326 20010906 00326 NE 2001 9 6 EIA2001240 2 20010821 A 7320 1081679 LINE BOEING 747 747132 1384882 NM PWA JT9 JT9D7J 52054 NE NR 1 ENGINE FAILED A EIAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 NM 09 479EV 19898 685635 SUU - WHEN CLIMBING THROUGH FL300 TO FL380 NR 1 ENGINE HAD AN UNRECOVERABLE COMPRESSOR STALL, EPR WAS APPROX 1.49, WHEN STALL OCCURRED N1 AND N2 DECREASED EGT INCREASED THEN DECREASED PEAKING AT 850 DEGREE SHUTDOWN, RESTARTED ENGINE. PARAM ETERS NORMAL AFTER RESTART. AIRCRAFT RETURNED TO SUU FOR MAINTENANCE. TROUBLESHOT ENGINE, TECHNICIANS FOUND EVIDENCE O F FAILURE (PS2 LINE). REPLACED PS2 LINE. PERFORMED ENGINE RUN, CHECKED NORMAL DURING GROUND RUN. (M) 2 L 7 4 4F 4 F A20WE E20EA 2001090600327 20010906 00327 WP 2001 9 6 GTIA010812 1 20010813 A 2611 WIRE DOUG DC9 DC982 3022082 WP SMOKE DETECTION BROKEN A K NONE L NO TEST IN INSP/MAINT 1 GL 23 812NK 48021 DTW - BARFIELD SMOKE DETECTOR FAILS TEST. REPAIRED BROKEN WIRE AND OPS CHECKED IAW MD80 MM 26-30. (M) 2 L 7 2 4F A6WE 2001090600328 20010906 00328 EA 2001 9 6 COMA0160683 1 20010902 A 5300 S61444 ANGLE CNDAIR CL600 CL6002B19 EA FS 484.00 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 966CA 12036 7132 THE INTERCOSTAL FLANGE AT RBL36 AND ANGLES AT BL 27LH AND RH ARE CRACKED.REMOVED AND REPLACED CRACKED ANGLES I/A/W WVAC E.O. 601R-53-2675A. 2 L 7 2 4F RT A21EA 2001090600329 20010906 00329 EU 2001 9 6 SIMA200118001 1 20010629 A 3350 LIGHT AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 282AT 282 MIA - FLT 5318 - CREW REPORTED A FLOOR PROXIMITY EMERGENCY LIGHT AT SEAT 7AB TO BE INOPERATIVE. PUT ON MEL AT THIS TIME . MAINTENANCE REPLACED THE BULB. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001090600330 20010906 00330 EU 2001 9 6 SIMA200118501 1 20010704 A 3350 301210 LIGHT AEROSP ATR42 ATR42300 8680920 EU PAX DOOR INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 319AM 319 MIA - MAINTENANCE REPORTED THE PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE L IGHT ASSEMBLY IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001090600331 20010906 00331 EU 2001 9 6 SIMA200119101 1 20010710 A 3350 66362 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 396AE 340B396 ILE - FLT 9733 - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS FROM ROW 3 TO ROW 5 TO BE INOPERATIVE. PUT ON MEL A T THIS TIME. MAINTENANCE REPLACED THE FLOOR STRIP FOR THE EMERGENCY LIGHTS AT ROW 3 TO 5. OPS CHECK WAS GOOD AND AIRCR AFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001090600332 20010906 00332 EU 2001 9 6 SIMA200119201 1 20010711 A 3350 66362 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 375AE 340B375 DFW - FLT 3315 - FOUND EMERGENCY FLOOR PROXIMITY LIGHTING 4A-5A INOPERATIVE. REMOVED AND REPLACED LIGHT STRIP. (M) 2 L 7 2 4T RT A52EU 2001090600333 20010906 00333 EU 2001 9 6 SIMA200119912 1 20010718 A 3397 WIRE AEROSP ATR42 ATR42300 8680920 EU CABIN CHAFED A K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 135MQ 135 MIA - FLT 5364 - FOUND EMERGENCY LIGHT IN MAIN DOOR INOPERATIVE. REPAIRED CHAFED WIRE IAW AMM. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 2001090600334 20010906 00334 EU 2001 9 6 SIMA200120025 1 20010719 A 3350 LIGHT AEROSP ATR72 ATR72212 EU CABIN LOOSE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 420AT 420 MIA - FLT 5317 - CREW REPORTED THE FLOOR PROXIMITY ESCAPE PATH LIGHT TO BE INOPERATIVE. PUT ON MEL AT THIS TIME. MAINT ENANCE FOUND A LOOSE BULB IN SOCKET. BULB WAS REINSTALLED CORRECTLY, OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURN ED TO SERVICE. NO PARTS WERE REPLACED. (M) 2 H 7 2 4T RT A53EU 2001090600335 20010906 00335 EU 2001 9 6 SIMA200120101 1 20010720 A 7712 TORQUE SENSOR SAAB SF340 340B 7860101 EU NR 2 ENGINE DIRTY A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 244AE 340B244 BUF - FLT 5194 - DURING CLIMB-OUT, NR 2 ENGINE TORQUE SURGING PLUS/MINUS 7 PERCENT. CLEANED TORQUE SENSOR IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001090600336 20010906 00336 EU 2001 9 6 SIMA200120103 1 20010720 A 3350 LIGHT AEROSP ATR72 ATR72212A 8680902 EU GALLEY INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 533AT 533 DFW - FLT 3910 - CREW REPORTED A FLOOR PROXIMITY EMERGENCY LIGHT IN THE GALLEY TO BE INOPERATIVE. LIGHT WAS PUT ON MEL AT THIS TIME. (M) 2 H 7 2 4T RT A53EU 2001090600337 20010906 00337 EU 2001 9 6 SIMA200120202 1 20010721 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 324AE 340B324 LAX - FLT 3105 - EMERGENCY LIGHT AT SEAT 3C IN INOPERATIVE. LIGHT PUT ON MEL AT THIS TIME. (M) 2 L 7 2 4T RT A52EU 2001090600338 20010906 00338 EU 2001 9 6 SIMA200120203 1 20010721 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 319AM 319 MIA - FLT 5247 - CREW REPORTED THE PASSENGER DOOR EXTERNAL EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REMOVED AND REPL ACED THE BATTERY IN POWER SUPPLY UNIT 15WL IAW AMERICAN EAGLE WORK CARD. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RE TURNED SERVICE. (M) 2 H 7 2 4T RT A53EU 2001090600339 20010906 00339 EU 2001 9 6 SIMA200120501 1 20010724 A 3350 7239410802 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 180AE 340B180 SGF - FLT 3688 - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHT AT SEAT 9A TO BE INOPERATIVE. MAINTENANCE REPLACED T HE FLOOR LIGHT IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001090600340 20010906 00340 EA 2001 9 6 COMA0160684 1 20010905 A 5346 60135006119 ANGLE CNDAIR CL600 CL6002B19 EA FS640 CUT A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 926CA 18356 7027 WHILE ACCOMPLISHING THE REPAIR TO THE ENGINE SUPPORT BEAM UPPER WEB, THE HORIZONTAL SUPPORT ANGLE (P/N 601-35006-119) WA S CUT THROUGH AT BL0 BETWEEN FS640 AND FS625.3 AND THE WEB AT THE SAME LOCATION IS ALSO DAMAGED.PERFORMED A MAJOR REPAIR BE FABRICATING/INSTALLING SUPPORT ANGLE AND TRIMMING DAMAGED WEB I/A/W WVAC EO 601R-53-2682. 2 L 7 2 4F RT A21EA 2001090600341 20010906 00341 EU 2001 9 6 SIMA200120502 1 20010724 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 350SB 340B350 LAX - FLT 3211 - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS AT ROWS 8, 9, AND 10 TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY UNIT 24LN IAW AE WORK CARD 1283. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001090600342 20010906 00342 EU 2001 9 6 SIMA200120802 1 20010727 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 348AE 349 MAINTENANCE REPORTED AN EMERGENCY LIGHT BY THE FORWARD CABIN DOOR TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED P OWER SUPPLY UNIT 62WL. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001090600343 20010906 00343 EU 2001 9 6 SIMA200120803 1 20010727 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 253AE 340B253 BOS - FLT 4933 - CREW REPORTED INTERIOR EMERGENCY LIGHTS AT SEATS 12BC AND 14AB TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY UNIT 24LN. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001090600344 20010906 00344 EU 2001 9 6 SIMA200120901 1 20010728 A 3350 723941002 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 180AE 340B180 SGF - MAINTENANCE REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LI GHT. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001090600345 20010906 00345 EU 2001 9 6 SIMA200120902 1 20010728 A 3350 2LA00430500 LIGHT SAAB SF340 340B 7860101 EU EXTERIOR INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 335AE 340B335 CREW REPORTED THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT A SSEMBLY AND RECRIMPED ONE WIRE IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001090600346 20010906 00346 EA 2001 9 6 COMA0160685 1 20010903 A 5753 601R1430353 VANE CNDAIR CL600 CL6002B19 EA INBD FLAP VANE CHAFED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 767CA 5666 7285 L/H AND R/H INBD FLAP VANES CHAFED ON INBD L/E'S.REMOVED AND REPLACED L/H AND R/H INBD FLAP VANES IND L/E SKINS I/A/W WV AC EO 601R-57-2691. 2 L 7 2 4F RT A21EA 2001090600347 20010906 00347 EA 2001 9 6 COMA0160686 1 20010902 A 5346 WEB CNDAIR CL600 CL6002B19 EA FS 625.00 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 966CA 12036 7132 ENGINE SUPPORT BEAM IS CRACKED ON LOWER WEB AFT OF F.S. 625.00 AT LBL 36.REMOVED DAMAGED AREA, FABED REPAIR PARTS AND IN STALLED I/A/W CANADAIR REO 601-53-61-366. 2 L 7 2 4F RT A21EA 2001090600348 20010906 00348 EA 2001 9 6 COMA0160687 1 20010901 A 5346 WEB CNDAIR CL600 CL6002B19 EA FUSELAGE AFT EQP CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 926CA 18356 7027 THE TOP WEB OF THE ENGINE SUPPORT BEAM WAS CRACKED.REPAIRED WEB I/A/W BOMBARDIER REO 601R-53-61-345 REV. B TEMPORARY REP AIR. 2 L 7 2 4F RT A21EA 2001090600349 20010906 00349 NM 2001 9 6 ZW0A0108101 1 20010904 A 3350 8039251 POWER SUPPLY BOEING 717 717200 1383700 NM B5-235 A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 2410W 55077 THE FWD EMERGENCY EXIT SIGN ABOVE THE L-1 FLT ATTENDANT SEAT WAS INOPERATIVE. REPLACED THE POWER SUPPLY. NO CHECK-C. --CLOSED-- 2 L 7 2 4F TR A6WE 2001090600350 20010906 00350 NM 2001 9 6 ZW0A0108102 1 20010905 A 3350 20121 POWER SUPPLY BOEING 757 7572Q8 1384972 NM WDM M-734 A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 713TW 28173 WHEN ELECTRICAL POWER WAS LOST THE FLOOR AND CEILING EMERGENCY LIGHTS IN THE MID AND AFT CABIN STAYED ON AND WOULD NOT R ESET. REPLACED THE POWER SUPPLY. CHECK-C 7-22-00 LAX. --CLOSED-- 2 L 7 2 4F RT A2NM 2001090600351 20010906 00351 EU 2001 9 6 SIMA200121001 1 20010729 A 3397 WIRE AEROSP ATR42 ATR42300 8680920 EU CABIN BROKEN A K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 971NA 017 MIA - FLT 5248 - CREW REPORTED THE EMERGENCY EXIT SIGN AT THE SERVICE DOOR TO BE INOPERATIVE. MAINTENANCE REPAIRED A BR OKEN WIRE AT THE LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001090600352 20010906 00352 EU 2001 9 6 SIMA200121301 1 20010801 A 3350 6013211 BATTERY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 286AE 340B286 JFK - FLT 5018 - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS BY ROW 4 AND 5 ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY AT POSITION 20LN IAW SAAB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001090600353 20010906 00353 EU 2001 9 6 SIMA200121302 1 20010801 A 3350 LIGHT AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 213AT 211 MIA - MAINTENANCE REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHT AT SEAT 6AB TO BE INOPERATIVE. PUT ON MEL AT THIS TIME. (M) 2 H 7 2 4T RT A53EU 2001090600354 20010906 00354 EU 2001 9 6 SIMA200121601 1 20010804 A 3350 2LA00499300 LIGHT SAAB SF340 340B 7860101 EU PAX DOOR INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 905AE 340B319 DFW - FLT 3802 - CREW REPORTED THE PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED T HE LIGHT ASSEMBLY IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001090600355 20010906 00355 SO 2001 9 6 SIMA200122401 1 20010802 A 5315 FLOORBEAM EMB 135 EMB135LR SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 709GB 145211 ABI - DURING MBV INSPECTION, MAINTENANCE FOUND CORROSION ON THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25. CORROSION W AS REMOVED AND DAMAGE WAS REPAIRED IAW EMB REPAIR STATEMENT GST 2636/01. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001090600356 20010906 00356 SO 2001 9 6 SIMA200122402 1 20010731 A 5320 BEAM EMB 135 EMB135LR SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 706RG 145194 ABI - DURING AN MBV INSPECTION, FOUND CORROSION ON THE GALLEY CENTER BEAM. CORROSION WAS REMOVED AND DAMAGE WAS REPAIRE D IAW EMB REPAIR STATEMENT GST 2592/01. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001090600357 20010906 00357 SO 2001 9 6 SIMA200122403 1 20010731 A 5315 FLOORBEAM EMB 135 EMB135LR SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 706RG 145194 ABI - DURING AN MBV INSPECTION, MAINTENANCE FOUND CORROSION ON THE OMEGA BEAM AT FRAME 20. CORROSION WAS REMOVED AND DA MAGE WAS REPAIRED IAW EMB SRM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001090600358 20010906 00358 NM 2001 9 6 USAASB01175 1 20010615 A 2810 FUEL CELL BOEING 737 7373B7 1384580 NM LT WING LEAKING A USAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 EA 19 373US 22952 CLT - FLT 1290 - AFTER TAKEOFF, FUEL WAS REPORTED STREAMING OUT OF THE LEFT WING BY AN AMERICAN FLIGHT BEHIND AND WAS AL SO CONFIRMED BY THE CLT TOWER. AN EMERGENCY WAS DECLARED AND THE FLIGHT RETURNED TO FIELD AT CLT. FLIGHT LANDED WITHOU T FURTHER INCIDENT. (M) 2 L 7 2 4F RT A16WE 2001090600359 20010906 00359 WP 2001 9 6 WX0A01003 1 20010725 A 5230 PAN DOUG DC9 DC921 302205A WP CARGO DOOR CRACKED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 LCQ - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND AFT CARGO DOOR CRACKED AROUND RIVNUT FASTENER AT LOW ER FORWARD CORNER. ROUTED OUT CRACK ON AFT CARGO DOOR, FORWARD LOWER JAMB. FORMED DOUBLER REPAIR AND INSTALLED IAW DC9 SRM 51-10-2, 51-10-3, 51-10-4, 52-01 FIGURE 2, 51-20-0 AND 51-30-8. (M) 2 L 7 2 4F A6WE 2001090600360 20010906 00360 SO 2001 9 6 SWIA200110025 1 20010608 A 5311 FRAME EMB 120 EMB120RT SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 1117H 120117 CARGO FLOOR, BEAM AND FRAME AND SECTION CRACKED AT STATION 16080.0 LEFT SIDE LOWER PER SRM 53-30-04. REMOVED DAMAGED ARE A OF FRAME FABRICATED DOUBLER AND FILLER PARTS AND INSTALLED PER SRM 51-70-05. PN 120-27718 FRAME PN 120-22636-001. 2 L 7 2 4T RT A31SO 2001090600361 20010906 00361 EA 2001 9 6 SWIA200110026 1 20010715 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA T/E FLAP DEFECTIVE A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 903SW 7425 FLAPS FAIL CAUTION MESSAGE WHEN SELECTING FLAPS OUT OF ZERO. LEFT SIDE FAILED AT 4 DEGREES, RIGHT SIDE FAILED AT 3 DEGR EES.REPLACED RIGHT BRAKE POSITION SENSING UNIT IAW 27-51-10. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2001090600362 20010906 00362 EA 2001 9 6 SWIA200110027 1 20010715 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA T/E FLAP DEFECTIVE A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 903SW 7425 ON FINAL APPROACH WHILE SELECTING FLAPS FROM 20 TO 30 DEGREES "FLAPS HALF SPEED" STATUS MESSAGE ILLUMINATED.PULLED CB F4 ON CB PANEL 1 AND 2, RESET AND CYCLED FLAPS SEVERAL TIMES. OPS CHECKS GOOD. "FLAPS HALF SPEED" STATUS MESSAGE ILLUMINA TED AGAIN ON FINAL APPROACH. REPLACED RIGHT BPSU IAW 27-51-10. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2001090600363 20010906 00363 EA 2001 9 6 SWIA200110028 1 20010713 A 2750 FLAP CNDAIR CL600 CL6002B19 EA WINGS FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 497SW 7482 FLAPS FAILED AT 0 DEGREES ON APPROACH TO BUTTE, MT.COMPLIED WITH MAINTENANCE PROCEDURE, FLAPS RESET IN ACCORDANCE WITH A D 98-20-01. SYSTEM CHECKS OK. 2 L 7 2 4F RT A21EA 2001090600364 20010906 00364 EA 2001 9 6 SWIA200110029 1 20010713 A 5610 PC2511C WINDSHIELD CNDAIR CL600 CL6002B19 EA COCKPIT CRACKED A SWIA K NONE O OTHER CR CRUISE 1 NM 07 412SW 7101 AT 26,000 FEET THE CAPTAINS WINDSHIELD CRACKED.REMOVED AND REPLACED CAPTAIN'S WINDSHIELD. PN ON NP139321-5 SN ON 01113H 6149. REF MM 56-11-01. PERFORMED PRESSURIZATION LEAK CHECKS AND OPS CHECKS OF WINDOW HEAT, NO FAULTS NOTED. 2 L 7 2 4F RT A21EA 2001090600365 20010906 00365 WP 2001 9 6 MWEA011242 1 20010905 A 5310 FITTING FITTING DOUG DC9 DC932 3022066 WP CENTER FUEL TANK CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 FITTING CRACKED AT CENTER FUEL TANK FORWARD BULKHEAD ABOVE LONGERON 24 LEFT. -- FABRICATED AND INSTALLED FITTING. 2 L 7 2 4F A6WE 2001090600366 20010906 00366 WP 2001 9 6 MWEA011243 1 20010905 A 5310 3913577501 INTERCOSTAL DOUG DC9 DC932 3022066 WP STATION 446 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 CABIN FLOOR, CENTERLINE INTERCOSTAL CRACKED AT STATION 446. -- REMOVED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001090600367 20010906 00367 WP 2001 9 6 MWEA011245 1 20010905 A 5230 59101575 DOUBLER DOUG DC9 DC932 3022066 WP AFT CARGO DOOR TORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 THE AFT CARGO DOOR HAS A PREVIOUS REPAIR IN THE DOOR JAMB THAT IS TORN IN THE BOTTOM AFT EDGE NEAR THE DOOR ROTATING LOC K LATCH. -- FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001090600368 20010906 00368 2001 9 6 SWIA200110030 4 20010712 A 3425 6226190204 COMPUTER EMB 120 EMB120ER 3260203 SO E/E BAY FAULTY A SWIA A UNSCHED LANDING I FLT. ATTITUDE INST. CR CRUISE 1 NM 07 213SW 85 85 120277 COPILOT'S FLIGHT DIRECTOR WENT INTO A BANK AND HEADING WAS OFF 60 DEGREES IN LEVEL FLIGHT. RETURNED TO SLC.REMOVE AND REPLACE RIGHT AHC85 AHRS. REINITIALIZED SYSTEM. NOTE NEW AHRS RIGHTED COPILOT'S ATTITUDE INDICATION. 2 L 7 2 4T RT A31SO 2001090600372 20010906 00372 NE 2001 9 6 2001UALA01505 2 20010726 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 SHUTDOWN A UALA K NONE X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 WP 29 546UA 25367 727194 NR 1 ENGINE UNCOMMANDED SHUTDOWN AT GATE. SUPPLEMENTAL DATA UPDATE ALL CONNECTORS ON FMU, EEC AND PMA, WERE CHECKED AND ALL WERE FOUND SECURE. PERFORMED POWER ASSURANCE CHECK, ENGINE RAN NORMAL. REPLACED NR 1 ENGINE MASTER FUEL CONTROL SWI TCH PRECAUTIONARY. NO HARD FAULTS FOUND. ENGINE HAS NOT EXPERIENCED ANY SUBSEQUENT FAULTS. 2 L 7 2 4F 4 F RT A2NM E17NE 2001090600376 20010906 00376 2001 9 6 2001UALA01641 4 20010805 A 2565 SLIDE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE R4 DOOR DEPLOYED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 171UA 24322 MAIN ENTRY DOOR NR 4 RIGHT SLIDE IRREGULAR DEPLOYED DOOR CYLINDER DISCHARGED. DOOR NOT FULLY DISARMED PRIOR OPENING. REP LACED SLIDE. 2 L 7 4 4F 4 F RT A20WE E24NE 2001090600379 20010906 00379 NM 2001 9 6 2001UALA01722 1 20010810 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 121UA 10765 29167 FUSE SKIN WAS PUNCTURED AND GOUGED AT STA 460 STRINGER 46L. MAJOR REPAIR ACCOMPLISHED. FUSELAGE SKIN DOUBLER REPAIR INS TALLED PER BOEING STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2001090600380 20010906 00380 NM 2001 9 6 2001UALA01729 1 20010816 A 2421 734284F IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 ENGINE FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 579UA 26697 NR 2 IDG FAILED. REPLACED NUMBER 2 INTEGRATED DRIVE GENERATOR (IDG). 2 L 7 2 4F 4 F RT A2NM E17NE 2001090600400 20010906 00400 EU 2001 9 6 AWXA0002213 1 20010818 A 2820 NSA8203228 PACKING AIRBUS AIRBUS 320 A320231 3930325 EU L/HWING STA4067 BROKEN A AWXA F ACTIVATE FIRE EXT. A B FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 28 629AW 076 D: Las - L/H plyon /engine fire - Flt 69 - while taxing in to the gate personnel observed smoke and flame at the top of the #1 ENG. and pylon area. Ground crew advised the pilots who followed QRH procedures. Maintenance opened the thrust re versers / core cowls on the # 1 ENG. and extingished the flames using fire extinguisher located at the gate, ramp level. C: Maintenance inspected the pylon, engine and fixed structure per AWA engineering instructions. The #1 engine and #1 ou tboard thrust reverser Assy. were replaced as a result of the inspection. In addition several pylon seals and a hydrauli c line were replaced. The cause of the fire was determined to be from a fuel leak in the wing leading edge above the e 2 L 7 2 4F RT A28NM 2001090600401 20010906 00401 NM 2001 9 6 01EVA005 1 20010905 A 7500 CF680C2D1FG13 ENGINE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE FIRE WARNING W QOCF K NONE J O WARNING INDICATION OTHER CL CLIMB 1 WP 03 14894 14894 48786 704743 1.AIRCRAFT REG. NO.B-16110, "ENG 1 FIRE"WARNING ON CLIMB PASSING ABOUT 3000 FT. PROBLEM CLEAREDWHEN THROTTLE REDUCED. PR OBLEM RECURRED WITH CLIMB POWER RESELECTED. RETURNED TPE WITH REDUCED POWER ON NO.1 ENGINE WITHOUT SHUTTING DOWN ENGINE. 2.ON GROUND, MAINTENANCE FOUND THE 11TH STAGE LOWER COOLING TUBE LOOSEN OFF FROM THE CLAMP. REPLACED THE ENGINE AND COND ITION CHECK NORMAL.3.SENT THE REMOVED ENGINE TO SHOP FOR DETAIL INSPECTION AND MAINTENANCE. 2 L 7 3 4F 4 F RT A22WE E31N3 2001090700001 20010907 00001 NM 2001 9 7 QXEA0101128 1 20010614 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM RT WING TE FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND NR 4 FLAP TRACK INBOARD, LOWER ROLLER FLANGE TRACK HAS TWO SPOTS OF PITTING AT FORWARD END ROLLER TRAVE L. REPAIRED IAW HORIZON AIR EA 2-57-113. 2 H 7 2 4T RT A13NM 2001090700002 20010907 00002 NM 2001 9 7 QXEA0101129 1 20010614 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND NR 4 FLAP TRACK INBOARD SIDE ROLLER TRACK PITTED APPROXIMATELY 6 INCHES LONG. REPAIRED IAW HORIZON AIR EA 2-57-113. 2 H 7 2 4T RT A13NM 2001090700003 20010907 00003 NM 2001 9 7 QXEA0101130 1 20010516 A 5753 STRUCTURE DHAV DHC8 DHC8202 2809007 NM TE FLAP GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT-HAND OUTBOARD FLAP CHAFED/GOUGED ON PREVIOUS REPAIR PATCH UPPER SURFACE INBOARD END. REPAIRED IAW DHC-8 SRM 51-20-51 AND 51-40-00. 2 H 7 2 4T RT A13NM 2001090700004 20010907 00004 EU 2001 9 7 QXEA0101132 1 20010629 A 3350 SIGN AIRBUS 320 A320232 3930326 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 475UA 1495 SEA - FORWARD EXIT DOOR EXIT LIGHT FOUND INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2001090700005 20010907 00005 EU 2001 9 7 QXEA0101133 1 20010702 A 3350 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 482US 11231 BOI - MID CABIN EXIT SIGN REPORTED INOPERATIVE. REMOVED AND REPLACED EXIT SIGNS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETUR NED TO SERVICE. 2 L 7 2 4F RT A20EU 2001090700006 20010907 00006 NM 2001 9 7 QXEA0101134 1 20010620 A 3200 ARM DHAV DHC8 DHC8202 2809007 NM NLG DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - NOSE LANDING GEAR TRAILING ARM HAS IMPACT DAMAGE ON FORWARD FACE BETWEEN 4 INCHES TO 5 1/2 INCH FROM UPPER PIVOT P OINT. REPAIRED IAW RD 8-32-289. 2 H 7 2 4T RT A13NM 2001090700007 20010907 00007 EU 2001 9 7 QXEA0101135 1 20010703 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 PDX - LARGE DENT AFT OF MAIN CABIN DOOR FOUND DURING INSPECTION. REPAIRED DAMAGE IN ACCORDENCE WITH FOKKER STRUCTERAL RE PAIR MANUAL. CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001090700008 20010907 00008 NM 2001 9 7 QXEA0101136 1 20010621 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - THERE IS A SMALL SMOOTH DENT LOCATED BENEATH THE LEFT-HAND ICE SHIELD. REPAIRED IAW HORIZON AIR EA 2-53-295. 2 H 7 2 4T RT A13NM 2001090700009 20010907 00009 NM 2001 9 7 QXEA0101137 1 20010704 A 2610 ANNUNCIATOR DHAV DHC8 DHC8202 2809007 NM COCKPIT MALFUNCTIONED A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 364PH 524 SEA - CREW REPORTED THAT DURING CLIMB, THE MASTER AND SMOKE WARNING ANNUNCIATORS ILLUMINATED INTERMITTENTLY. PERFORMED I NSPECTION OF SMOKE DETECTORS, NO DEFECTS NOTED. NO INDICATION OF FIRE OR SMOKE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETUR NED TO SERVICE. 2 H 7 2 4T RT A13NM 2001090700010 20010907 00010 NM 2001 9 7 QXEA0101139 1 20010707 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE MISDRILLED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 348PH 484 PDX - TWO NR 40 DRILL HOLES IN FUSELAGE SKIN APPROXIMATELY STATION 312.350. REPAIRED IAW HORIZON AIR EA 2-53-305. DHC-8 SRM 51-40-11 AND DHC-8 200 MM 20-21-21, PARAGRAPH 34, FIGURE 209, PAGES 206 AND 217. 2 H 7 2 4T RT A13NM 2001090700011 20010907 00011 NM 2001 9 7 QXEA0101140 1 20010706 A 5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - LIGHT CORROSION ON UPPER SURFACE OF NUT PLATE FLANGE, FORWARD CARGO BAY FLOOR PANEL SUPPORT STRUCTURE, STATION X60 0, Y21.5. REPAIRED IAW DHC-8 SRM 51-20-11, 53-00-16 AND PSM 1-GEN-5, CHAPTER 4. 2 H 7 2 4T RT A13NM 2001090700012 20010907 00012 NM 2001 9 7 QXEA0101141 1 20010703 A 5530 STRUCTURE DHAV DHC8 DHC8202 2809007 NM VERTICAL STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - SMALL CRACK FOUND IN SHEET METAL ON RIGHT SIDE OF FORE RUDDER CENTER HINGE AREA. REPAIRED IAW DHC-8 SRM 51-40-11, PAGE 1. 2 H 7 2 4T RT A13NM 2001090700013 20010907 00013 NM 2001 9 7 QXEA0101142 1 20010701 A 5753 SHAFT DHAV DHC8 DHC8202 2809007 NM FLAP TRACK GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - LEFT-HAND NR 5 FLAP TRACK CARRIAGE ROLLER SHAFT GOUGED. REPLACED WITH NEW ROLLER SHAFT FROM STOCK. 2 H 7 2 4T RT A13NM 2001090700014 20010907 00014 NM 2001 9 7 QXEA0101143 1 20010701 A 5753 SHAFT DHAV DHC8 DHC8202 2809007 NM FLAP TRACK GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - LEFT-HAND FLAP TRACK CARRIAGE HOOK ROLLER SHAFT GOUGED. REPALCED WITH NEW ROLLE SHAFT FROM STOCK. 2 H 7 2 4T RT A13NM 2001090700015 20010907 00015 NM 2001 9 7 QXEA0101144 1 20010701 A 5753 ROLLER DHAV DHC8 DHC8202 2809007 NM TE FLAP SEIZED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - LEFT-HAND NR 4 FLAP TRACK CARRIAGE HOOK ROLLER SEIZED. REPALCED WITH NEW ROLLER FROM STOCK. 2 H 7 2 4T RT A13NM 2001090700016 20010907 00016 NM 2001 9 7 QXEA0101145 1 20010701 A 5753 ROLLER DHAV DHC8 DHC8202 2809007 NM FLAP TRACK SEIZED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - RIGHT-HAND NR 5 FLAP TRACK CARRIAGE HOOK ROLLER SEIZED. REPLACED WITH NEW ROLLER FROM STOCK. 2 H 7 2 4T RT A13NM 2001090700017 20010907 00017 NM 2001 9 7 QXEA0101146 1 20010701 A 5753 ROLLER DHAV DHC8 DHC8202 2809007 NM FLAP TRACK SEIZED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - RIGHT-HAND NR 4 FLAP TRACK CARRIAGE HOOK ROLLER SHAFT GOUGED. REPLACED WITH NEW ROLLER SHAFT FROM STOCK. 2 H 7 2 4T RT A13NM 2001090700018 20010907 00018 NM 2001 9 7 QXEA0101147 1 20010701 A 5753 SHAFT DHAV DHC8 DHC8202 2809007 NM FLAP TRACK GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - RIGHT-HAND NR 5 FLAP CARRIAGE HOOK ROLLER SHAFT GOUGED. REPLACED WITH NEW ROLLER SHAFT FROM STOCK. 2 H 7 2 4T RT A13NM 2001090700019 20010907 00019 NM 2001 9 7 QXEA0101148 1 20010706 A 2760 CONTROL CABLE DHAV DHC8 DHC8202 2809007 NM RT WING SPOILER WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - RIGHT WING LOWER SPOILER CABLE WORN AT AFT WING SPAR THROUGH STEEL PULLYS. REPAIRED IAW DASH 8 MM 200, 27-14-00, P AGE 507, STEPS 4A AND 4B. 2 H 7 2 4T RT A13NM 2001090700020 20010907 00020 NM 2001 9 7 QXEA0101149 1 20010706 A 2760 CONTROL CABLE DHAV DHC8 DHC8202 2809007 NM RT WING WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - RIGHT WING UPPER SPOILER CABLE WORN AT AFT WING SPAR THROUGH STEEL PULLEYS. REPAIRED IAW DASH 8 M/M 200, 27-14-00, PAGE 507. 2 H 7 2 4T RT A13NM 2001090700021 20010907 00021 NM 2001 9 7 QXEA0101150 1 20010703 A 3213 STRUT DHAV DHC8 DHC8202 2809007 NM MLG GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - NOSE LANDING GEAR LOWER STRUT IS GOUGED ON FORWARD SIDE. REPAIRED IAW RD 8-32-289. 2 H 7 2 4T RT A13NM 2001090700022 20010907 00022 NM 2001 9 7 QXEA0101151 1 20010710 A 3222 STRUT DHAV DHC8 DHC8202 2809007 NM NLG GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - NOSE LANDING GEAR LOWER STRUT IS GOUGED ON FORWARD SIDE, STEP NR 3 FROM RD 8-32-289, PAGE 4 HAS NOT BEEN COMPLIED WITH. COMPLIED WITH STEP NR 3 AND DHC-8 SRM 51-20-26. 2 H 7 2 4T RT A13NM 2001090700023 20010907 00023 NM 2001 9 7 QXEA0101152 1 20010706 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - FORWARD LEFT-HAND CENTER SEAT TRACK NR 4 HAS CORROSION ON OUTBOARD FLANGE AT APPROXIMATELY STATION X234.500. REPAI RED IAW HORIZON AIR EA 2-53-304. 2 H 7 2 4T RT A13NM 2001090700024 20010907 00024 NM 2001 9 7 QXEA0101153 1 20010706 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - FORWARD LEFT-HAND CENTER SEAT TRACK NR 4 HAS CORROSION ON TOP OF TRACK AT FORWARD END OF TRACK AT APPROIMATELY STA TION X262.400. REPAIRED IAW HORIZON AIR EA 2-53-304. 2 H 7 2 4T RT A13NM 2001090700025 20010907 00025 NM 2001 9 7 QXEA0101154 1 20010705 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - FORWARD RIGHT-HAND OUTBOARD SEAT TRACK NR 10 HAS GOUGES AT APPROXIMATELY STATION X436.500. REPAIRED IAW HORIZON AI R EA 2-53-305, STEP 3. 2 H 7 2 4T RT A13NM 2001090700026 20010907 00026 NM 2001 9 7 QXEA0101155 1 20010702 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - FORWARD RIGHT-HAND OUTBOARD SEAT TRACK NR 10 HAS CORROSION ON TOP OF SEAT TRACK RAIL AT APPROXIMATELY STATION X376 .110. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001090700027 20010907 00027 NM 2001 9 7 QXEA0101156 1 20010702 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - FORWARD RIGHT-HAND OUTBOARD SEAT TRACK NR 10 HAS CORROSION INSIDE TRACK CHANNEL AT APPROXIMATELY X302.400. REPAIRE D IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001090700028 20010907 00028 NM 2001 9 7 QXEA0101157 1 20010702 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - FORWARD OUTBOARD SEAT TRACK NR 10 HAS CORROSION INSIDE TRACK CHANNEL AT CUTOUT. LOCATED AT APPROXIMATELY STATION X 252.700. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001090700029 20010907 00029 NM 2001 9 7 QXEA0101158 1 20010706 A 5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - LIGHT CORROSION ON UPPER SURFACE OF NUTPLATE FLANGE, FORWARD CARGO BAY FLOOR PANEL SUPPORT STRUCTURE, STATION X600 , Y6.00, LEFT-HAND SIDE. REPAIRED IAW DHC-8 SRM 53-00-16. 51-20-11 AND PSM 1-GEN-5, CHAPTER 4. 2 H 7 2 4T RT A13NM 2001090700030 20010907 00030 NM 2001 9 7 QXEA0101159 1 20010706 A 5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - LIGHT CORROSION ON UPPER SURFACE OF NUTPLATE FLANGE, FORWARD CARGO BAY FLOOR PANEL SUPPORT STRUCTURE, STATION X600 , Y27. REPAIRED IAW DHC-8 SRM 53-00-16, 51-20-11 AND CPM CHAPTER 4, OF PSM 1-GEN-5. 2 H 7 2 4T RT A13NM 2001090700031 20010907 00031 NM 2001 9 7 QXEA0101160 1 20010701 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - FUSELAGE SKIN AT UPPER FORWARD CORNER OF LAST WINDOW ON RIGHT-HAND SIDE HAS SCRAPING DAMAGE. REPAIRED IAW DHC-8 SR M 51-20-16, AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2001090700032 20010907 00032 NM 2001 9 7 QXEA0101161 1 20010705 A 5412 FIREWALL DHAV DHC8 DHC8202 2809007 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - LEFT-HAND NACELLE STAINLESS EXHAUST FIREWALL IS CRACKED ON UPPER RIGHT-HAND SIDE BY UPLOCK ACTUATOR BRACKET MOUNT BOLTS. REPAIRED IAW RD 8-54-806. 2 H 7 2 4T RT A13NM 2001090700033 20010907 00033 NM 2001 9 7 QXEA0101162 1 20010704 A 5310 THRESHOLD DHAV DHC8 DHC8202 2809007 NM PAX DOORWAY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - THE DOOR THRESHOLD OF MAIN CABIN DOOR, PLATE IS PITTED AND CORRODED. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001091000356 20010910 00356 NE 2001 9 10 ARWA0010811 2 20010830 A 7230 COMPRESSOR DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 4 ENGINE STALLED A ARWA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 19 661AV 52042 4203 45969 NR 4 ENGINE SHUT DOWN DUE TO COMPRESSOR STALL. AIRCRAFT RETURNED TO SAL AND LANDED WITHOUT INCIDENT. C1 HARD TO ROTATE BY HAND. PREPARE NR 4 ENGINE FOR FERRY FLIGHT ONE ENGINE INOPERATIVE IAW ARROW AIR GMM 6-3-1 THRU 6-3-5. LOG PAGE 105029 ITEM 12 M, REMOVED AND REPLACED NR 4 ENGINE IAW ARROW AIR ENGINE REMOVAL/INSTALLATION PAPERWORK PAGES 5-46-1 THRU 5-46- 29 ACCOMPLISHED ENGINE ADJUSTMENT AND TEST IAW MM 71-00. 2 L 7 4 4F 4 F 4A25 1E8 2001090700034 20010907 00034 NM 2001 9 7 QXEA0101163 1 20010711 A 5230 RETAINER DHAV DHC8 DHC8202 2809007 NM CARGO DOOR SEAL BENT A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - BAG DOOR SEAL RETAINER AND FLANGE BENT AT LOWER AFT CORNER NEXT TO PROP ROD SWIVEL. REPAIRED IAW HORIZON AIR EA 2- 52-105 AND DHC-8-200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001090700035 20010907 00035 NM 2001 9 7 QXEA0101164 1 20010712 A 5230 STRUCTURE DHAV DHC8 DHC8202 2809007 NM CARGO DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - DENT IN AFT CARGO DOOR. 18 INCHES AFT OF LEADING EDGE, 4 1/2 INCHES ABOVE BOTTOM OF DOOR. REPAIRED IAW DHC 8 SRM 5 1-40-11, PAGE 1, PARAGRAPH A-G AND RD 8-52-230, PAGE 5, STEP 7-10. 2 H 7 2 4T RT A13NM 2001090700036 20010907 00036 NM 2001 9 7 QXEA0101165 1 20010706 A 5230 STRUCTURE DHAV DHC8 DHC8202 2809007 NM CARGO DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - TWO GOUGES, 34 1/2 INCHES FROM LEADING EDGE, 6 INCHES BELOW TOP EDGE OF CARGO DOOR. REPAIRED IAW RD 8-82-029. 2 H 7 2 4T RT A13NM 2001090700037 20010907 00037 NM 2001 9 7 QXEA0101166 1 20010706 A 5210 STRUCTURE DHAV DHC8 DHC8202 2809007 NM PAX DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - INSPECTED DENT ON MAIN CABIN DOOR, 6 INCHES BELOW UPPER EDGE OF SKIN AND 4 INCHES AFT OF FORWARD EDGE OF SKIN. REP AIRED IAW HORIZON AIR EA 2-52-103. 2 H 7 2 4T RT A13NM 2001090700039 20010907 00039 NM 2001 9 7 CALA0100830 1 20010904 A 5320 ANGLE BOEING 737 7373T0 1384582 NM STA 1014 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND R/H LAV WALL & L/H LAV WALL ANGLES CORRODED AT STA 1014 RBL 4 AND LBL 4. THE ANGLES WERE REMOVED AND RE PLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001090700040 20010907 00040 NM 2001 9 7 CALA0100831 1 20010904 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM STA 332 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND A 4" CRACK IN INTERCOSTAL AT STA 332, STRINGER 10R. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW BOEING DRAWING 65C33288 AND EA 5363-01014. 2 L 7 2 4F RT A16WE 2001090700041 20010907 00041 NM 2001 9 7 CALA0100832 1 20010904 A 5313 STRINGER BOEING 737 7373T0 1384582 NM STA 332 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND A 4" CRACK IN STRINGER 10R AT STA 332. THE STRINGER WAS REMOVED AND REPLACED IAW EA 5363-01014. 2 L 7 2 4F RT A16WE 2001090700042 20010907 00042 NM 2001 9 7 CALA0100833 1 20010905 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM STA 727B CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND A 1/4" CRACK IN UPPER FLANGE OF L/H O/B SEAT TRACK AT HI-LOCK ATTACH POINT, STA 727B. A STRAP WAS INSTA LLED IAW ECRA 5310-04183. 2 L 7 2 4F RT A16WE 2001090700043 20010907 00043 NM 2001 9 7 CALA0100834 1 20010905 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM STA 727B CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND A 1/2" CRACK IN L/H I/B SEAT TRACK AT AFT HI-LOCK, STA 727B. STRAP AND FILLER WERE INSTALLED IAW ECRA 5 310-04183. 2 L 7 2 4F RT A16WE 2001090700044 20010907 00044 WP 2001 9 7 CALA0100835 1 20010906 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP STA 1174-1193 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15820 49480 INSPECTION FOUND L/H O/B SEAT TRACK AT GALLEY MOUNT STA 1174 AND L/H CENTER SEAT TRACK AT GALLEY MOUNT STA 1193 CORRODED . THE SEAT TRACKS WERE REMOVED AND REPLACED IAW SRM 51-30-01. 2 L 7 2 4F A6WE 2001090700045 20010907 00045 NM 2001 9 7 CALA0100836 1 20010906 A 5320 PLATE BOEING 737 7373T0 1384582 NM STA 847 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND A 3" CRACK ON UPPER WEB OF DOOR THRESHOLD PLATE AT STA 847. A NEW THRESHOLD PLATE WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001090700048 20010907 00048 NM 2001 9 7 QXEA0101167 1 20010712 A 5230 STRUCTURE DHAV DHC8 DHC8202 2809007 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - 2 GOUGES, IN CARGO DOOR 1 1/2 INCHES LONG X 5.8 INCH WIDE AND APPROXIMATELY .019 DEEP. REPAIED IAW RD 8-52-029. 2 H 7 2 4T RT A13NM 2001090700049 20010907 00049 NM 2001 9 7 QXEA0101168 1 20010711 A 5210 STRUCTURE DHAV DHC8 DHC8202 2809007 NM CARGO DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - DENT FOUND ON LOWER CLOSURE OF AFT CARGO DOOR, BEHIND SEAL RETAINER FLANGE. REPAIRED IAW HORIZON AIR EA 2-52-105. 2 H 7 2 4T RT A13NM 2001090700050 20010907 00050 NM 2001 9 7 QXEA0101169 1 20010711 A 5230 DOOR FRAME DHAV DHC8 DHC8202 2809007 NM CARGO BAY SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - BAG DOOR LOWER FRAME, AFT CORNER OF DAMAGED AREA HAS SEVERAL SCRATCHES. REPAIRED IAW HORIZON AIR EA 2-52-105. 2 H 7 2 4T RT A13NM 2001090700052 20010907 00052 NM 2001 9 7 QXEA0101170 1 20010712 A 7110 COWLING DHAV DHC8 DHC8102 2809003 NM NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 314 PDX - SHEET METAL DAMAGED ON INBOARD LOWER NACELLE JUST AFT OF LOWER COWL. REPAIRED IAW RD 8-54-003. 2 H 7 2 4T RT A13NM 2001090700053 20010907 00053 EU 2001 9 7 QXEA0101171 1 20010713 A 5753 SKIN FOKKER F28 F28MK4000 4990810 EU LT WING TE FLAP GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - GOUGE ON TOP OF LEFT-HAND INBOARD FLAP AT STATION 183. REPAIRED IAW F-28 SRM 57-01-01, PAGE 3. 2 L 7 2 4F RT A20EU 2001090700054 20010907 00054 EU 2001 9 7 QXEA0101174 1 20010712 A 3350 5515800106 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU EXIT SIGN INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 GEG- FORWARD FACING EMERGENCY EXIT SIGN AT ROW 8 HAS BULBS OUT. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHE CKS GOOD. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F RT A20EU 2001090700056 20010907 00056 EU 2001 9 7 QXEA0101175 1 20010711 A 3350 XB864041 LAMP FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 476US 11224 PDX- ESCAPE PATH "ARROW" LIGHT AT ROW 12 INOP. MAINTENANCE REPLACED LAMP ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RET URNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001090700057 20010907 00057 EU 2001 9 7 QXEA0101176 1 20010711 A 3350 5515800106 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 11234 GEG- EXIT SIGN AT ROW 8 INOP. MAINTENANCE REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001090700058 20010907 00058 EU 2001 9 7 QXEA0101177 1 20010713 A 3350 5515800106 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 492US 11159 BOI- FORWARD EXIT SIGN HAS 28 VOLT LIGHTS INOP. MAINTENANCE REPLACED CIRCUIT CARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RET URNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001090700059 20010907 00059 EU 2001 9 7 QXEA0101178 1 20010712 A 3350 5515800106 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 496US 11169 SEA- FORWARD EMERGENCY EXIT SIGN HAS MANY BULBS INOP. MAINTENANCE REPLACED CIRCUIT CARD FOR EXIT SIGN. OPERATIONAL CHECK S GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001090700060 20010907 00060 EU 2001 9 7 QXEA0101179 1 20010708 A 3350 5515800106 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 497US 11173 PDX- EXIT SIGN AT CABIN ENTRY DIM. MAINTENANCE REPLACED SIGN ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SER VICE. 2 L 7 2 4F RT A20EU 2001090700061 20010907 00061 EU 2001 9 7 QXEA0101180 1 20010629 A 5330 PANEL FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - CHAFING DAMAGE AT PANEL 21A APERTURE. REPAIRED IAW FOKKER SRM 53-01-01. 2 L 7 2 4F RT A20EU 2001090700062 20010907 00062 EU 2001 9 7 QXEA0101181 1 20010630 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU GRAVEL GUARD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - NOSE LANDING GEAR BAY FORWARD CEILING GRAVEL GUARD SUPPORT FLANGE ATTACHED TO FORWARD FACE OF FRAME 2650 IS CRACKE D. REPAIRED IAW HORIZON AIR EA 4-53-1500. 2 L 7 2 4F RT A20EU 2001090700064 20010907 00064 EU 2001 9 7 QXEA0101182 1 20010722 A 5320 INTERCOSTAL FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - INTERCOSTAL AT FRAME 6305 AND STRINGER 18 HAS A 3/8 INCH CRACK EMITTING FROM RIVET HOLE. REPAIRED IAW FOKKER SRM 5 3-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 2001090700070 20010907 00070 EU 2001 9 7 QXEA0101183 1 20010722 A 5300 STRUCTURE FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - DENT IN SIDE OF FUSELAGE APT APPROXIMATELY 40 INCHES AFT OF MAIN CABIN DOOR WL 22.047 AND FS 238.779. REPAIRED IAW HORIZON AIR EA 4-53-1513 AND FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001090700072 20010907 00072 NM 2001 9 7 2001UALA01827 1 20010824 A 5311 FAILSAFE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 322UA 23954 AFT PIT STATION 727A LEFT HAND SIDE UNDER Z ANGLE FRAME FAIL SAFE STRAP BROKEN OFF AT LBL 18. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001090700073 20010907 00073 NM 2001 9 7 2001UALA01828 1 20010824 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 324UA 23956 CABIN FLOOR BEAM STATION 947 LBL 5 HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. REPLACE T CAP AT STA 947 LBL 10 TO RBL 60. 2 L 7 2 4F 4 F RT A16WE E2GL 2001090700074 20010907 00074 EU 2001 9 7 QXEA0101184 1 20010722 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - LEFT-HAND SIDE FUSELAGE EXTERIOR SKIN HAS A DENT MEASURING .500 X .200 X 0.11 DEEP. LOCATED 1.5 INCHES AFT OF FRAM E 6805 AND 1.5 INCHES BELOW SKIN LAP JOINT AT 560WL. REPAIRED IAW FOKKER SRM 53-02-07 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001090700075 20010907 00075 NM 2001 9 7 2001UALA01829 1 20010824 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 324UA 23956 CABIN FLOOR BEAM STATION 947 LBL 5 HAS EXCESSIVE MATERIAL LOSS DUE TO CORROSION. MAJOR REPAIR ACCOMPLISHED. REPLACED T CAP AT STATION 947 LBL 10 TO RBL 60. 2 L 7 2 4F 4 F RT A16WE E2GL 2001090700076 20010907 00076 NM 2001 9 7 2001UALA01830 1 20010825 A 5241 CHANNEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE GALLEY DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 324UA 23956 AFT GALLEY DOOR Z CHANNEL FROM STATION 942 TO 996, HAS CORROSION AT RBL 50. MAJOR REPAIR ACCOMPLISHED.REPLACED Z ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2001090700077 20010907 00077 NM 2001 9 7 2001UALA01831 1 20010825 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 324UA 23956 FUSELAGE EXT SKIN ABOVE STRINGER 14L, AT STATION 1006 HAS BLIND FASTENER INSTALLED, AND AT STATION 1001 HAS DENT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR TO SKIN. INSTALLED FRAME SHEAR TIE REPAIR, AND STRINGER SPLICE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001090700078 20010907 00078 NM 2001 9 7 2001UALA01832 1 20010826 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 323UA 23955 RIGHT FUSELAGE SKIN HAS SHARP DENT BETWEEN STRINGER 22 STRINGER 23 AND JUST FWD OF STATION 294.5. MAJOR REPAIR ACCOMPLIS HED. DAMAGE AREA CUTOUT AND DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001090700079 20010907 00079 NM 2001 9 7 2001UALA01833 1 20010822 A 5315 141W85191 FLOORBEAM BOEING 777 777222 1385219 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 795UA 17174 26927 STATION 246 FLOOR BEAM MID-CHORD CRACKED AT LBL 38.5 NOTED CRACKING OF THE 141W8519-1 MID CHORD IS DUE TO THERMAL CONTR ACTION THAT RESULTS IN HIGHER THAN EXPECTED IN-SERVICE LOADING OF THE DOUBLE DEPTH STATION 246 FLOOR BEAM. PART IS BEIN G REPAIRED. 2 L 7 2 4F RT T0001SE 2001090700081 20010907 00081 NM 2001 9 7 2001UALA01835 1 20010826 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 330UA 24191 LEFT FRAME AFT CHORD CRACKED AT BS 188 WL 206. MAJOR REPAIR ACCOMPLISHED.INSTALLED REPAIR ANGLE ON OUTBOARD CHORD. 2 L 7 2 4F 4 F RT A16WE E2GL 2001101800003 20011018 00003 NM 2001 10 18 2001UALA01836 1 20010825 A 2997 BACC63BP18A14P9L CONNECTOR BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE HYDRAULIC SYS FAULTY A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 617UA 21877 PASSING 15,000 FT EICAS C-HYD QTY MSG STATUS PAGE SHOWED ZERO QUANTITY, CENTER QUANTITY LIGHT CAME ON, OPERATED NORMALLY . POSSIBLE LOOSE CONNECTOR PIN AND LOOSE SHIELD TERMINAL. REPLACED CONNECTOR D4946P AND SHIELD GROUND RE-TERMINATED AT CONNECTOR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090700082 20010907 00082 NM 2001 9 7 2001UALA01837 1 20010821 A 3350 362624 LIGHT BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 106UA 26474 EMERGENCY LIGHT INOP 55C EEL. IN-SEAT EEL LAMP INOP. REPLACED LAMP ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 2001090700083 20010907 00083 NM 2001 9 7 2001UALA01840 1 20010827 A 5320 WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 519UA 24872 CABIN STATION 984 SHEAR WEB CORRODED AT RBL 70. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2001090700084 20010907 00084 EU 2001 9 7 QXEA0101185 1 20010722 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - LEFT-HAND SIDE FUSELAGE EXTERIOR SKIN HAS A DENT MEASURING 3 INCHE X 2 X .029 DEEP. LOCATED 3 INCHES AFT OF FRAME 6805 AND 2 INCHES BELOW SKIN LAP JOINT AT -560WL. 2 L 7 2 4F RT A20EU 2001090700085 20010907 00085 EU 2001 9 7 QXEA0101186 1 20010722 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSEAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - LEFT-HAND SIDE FUSELAGE SKIN EXTERIOR HAS A VERTICAL CREASE MARK THAT MEASURES 2 INCHES X .100 X .021 DEEP. LOCATE D 8 INCHES AFT OF FRAME 6805 AND 6 INCHES BELOW SKIN LAP JOINT AT -560WL. REPAIRED IAW FOKKER SRM 53-02-07 AND SRM 51-31 -01. 2 L 7 2 4F RT A20EU 2001090700087 20010907 00087 EU 2001 9 7 QXEA0101187 1 20010721 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - LEFT-HAND SIDE FORWARD FUSELAGE SKIN EXTERIOR HAS A SHARP DENT THAT MEASURES 1.4" X 1.0" X .035" DEEP. LOCATED 1.5 " ABOVE SKIN LAP JOINT AT -560WL AND 8.5" AFT OF FRAME 3050. REPAIRED IAW FOKKER SRM 53-02-01, PAGE 3, FIGURE 1. 2 L 7 2 4F RT A20EU 2001090700088 20010907 00088 NM 2001 9 7 2001UALA01846 1 20010827 A 2910 HYDRAULIC SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEFT LEAKING A UALA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION DE DESCENT 1 WP 29 504UA 24625 EICAS MESSAGE 'L HYD SYS PRESS' DISPLAYED. LEFT HYDRAULIC QUANTITY DECREASED TO 0.02, QUANTITY STABLE WITH PUMPS OFF. 2 L 7 2 4F 4 F RT A2NM E17NE 2001090700089 20010907 00089 EU 2001 9 7 QXEA0101188 1 20010722 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - LEFT-HAND SIDE FUSELAGE SKIN EXTERIOR HAS A DENT THAT MEASURES 3 INCHES X 1.2 X .025 DEEP. LOCATED 6 INCHES AFT O F FRAME 6805 AND 8 INCHES BELOW SKIN LAP JOINT AT -560WL. REPAIRED IAW FOKKER SRM 53-02-07 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001090700090 20010907 00090 EU 2001 9 7 QXEA0101189 1 20010721 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - LEFT-HAND SIDE FORWARD FUSELAGE SKIN EXTERIOR HAS A DENT THAT MEASURES 1.2 INCHES X .400 X 0.37 DEEP. LOCATED 1.2 INCHES FORWARD OF FRAME 3050 AND 10 INCHES ABOVE SKIN LAP JOINT AT -560WL. REPAIRED IAW FOKKER SRM 53-02-02, PAGE 2, FIG URE 1. 2 L 7 2 4F RT A20EU 2001090700091 20010907 00091 NM 2001 9 7 2001UALA01848 1 20010827 A 5312 PRESSURE PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 323UA 23955 BODY STATION 178 WEB HAS CRACK IND OUT OF FASTENER WL 234 RBL 11 AND 12. MAJOR REPAIR ACCOMPLISHED. DOUBLER INSTALLED ON WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2001090700092 20010907 00092 EU 2001 9 7 QXEA0101197 1 20010717 A 2612 FIRE LOOP FOKKER F28 F28MK4000 4990810 EU APU SHORTED A QXEA F ACTIVATE FIRE EXT. N FALSE WARNING NR NOT REPORTED 1 NM 09 494US 11167 SEA-APU FIRE WARNING. APU AUTO SHUT DOWN AND AGENT DISCHARGED. FOUND WE1-114 AND WE14-114 CONNECTION TO APU FIRE LOOP SH ORTED. REPLACED. REPLACED BOTTLE.APU FIRE EXT SYS OPS CHECKS AS PER F-28 MM 26-13-01. PAGE 202, ITEM 2. AIRCRAFT RETURNE D TO SERVICE. 2 L 7 2 4F RT A20EU 2001090700093 20010907 00093 NM 2001 9 7 2001UALA01849 1 20010827 A 2933 WARNING SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 514UA 24839 CENTER EICAS "C HYD LOW QTY" RSVR LIGHT ON OVERHEAD. TURNED OFF CENTER HYD PUMPS, LOW PRESSURE LIGHTS CAME ON AT THAT TI ME. LOWER EICAS STATUS CENTER QUANTITY ZERO 2 L 7 2 4F 4 F RT A2NM E17NE 2001090700094 20010907 00094 EU 2001 9 7 QXEA0101198 1 20010723 A 5330 BUTT JOINT FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PDX - CRACK ON THE BUTT JOINT ON NR 8 STRINGER, 17 INCHES FORWARD OF FRAME 4850. REPAIRED IAW FOKKER SRM 51-31-01 AND H ORIZON AIR EA 4-53-1517. 2 L 7 2 4F RT A20EU 2001090700095 20010907 00095 NM 2001 9 7 2001UALA01850 1 20010827 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 324UA 23956 LEFT SIDE FUSELAGE 2 FEET BELOW AFT ENTRY DOOR SHARP DENT. MAJOR REPAIR ACCOMPLISHED.DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001090700096 20010907 00096 NM 2001 9 7 2001UALA01851 1 20010827 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 324UA 23956 RIGHT HAND VERTICAL CHORD CRACKED AT BS 188. MAJOR REPAIR ACCOMPLISHED. REPAIR AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001090700097 20010907 00097 EU 2001 9 7 2001UALA01852 1 20010824 A 3320 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN SMOKE A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 414UA 472 SMOKE FROM FORWARD ENTRY LIGHTS. CIRCUIT BREAKER PULLED AND SMOKE APPEARS TO BE DISSIPATING. 2 L 7 2 4F 4 F RT A28NM E40NE 2001091400116 20010914 00116 2001 9 14 2001UALA01853 4 20010827 A 2213 K217ABM11 CONTROL UNIT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE AUTOPILOT SYS FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 446UA 834 INTERMITTENT MASTER CAUTION CHIME LIGHT. INTERMITTENT BLINKING OF FEATURES DISPLAYED ON CAPTAINS PRIMARY FLIGHT DISPLAY AND NAVIGATION DISPLAY. FLIGHT CONTROL UNIT LIGHTS FLASHING ALSO. THE FCU WAS REPLACED AND GROUND CHECK WAS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2001090700098 20010907 00098 EU 2001 9 7 2001UALA01854 1 20010827 A 5210 DOOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L1 VIBRATION A UALA A UNSCHED LANDING E VIBRATION/BUFFET NR NOT REPORTED 1 WP 29 443UA 820 LOUD BUZZING NOISE AND VIBRATION COMING FROM DOOR 1 LEFT. 2 L 7 2 4F 4 F RT A28NM E40NE 2001090700099 20010907 00099 NM 2001 9 7 2001UALA01855 1 20010826 A 3620 WARNING SYSTEM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT ACTIVATED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 364UA 24533 UNSCHEDULED LANDING DUE TO LT BLEED AIR INDICATIONS. 2 L 7 2 4F 4 F RT A16WE E2GL 2001090700100 20010907 00100 NM 2001 9 7 2001UALA01857 1 20010829 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 323UA 23955 FUSELAGE BULKHEAD WEB HAS 17 PERCENT MATERIAL LOSS AFTER GOUGE BLEND OUT BS 1028, LBL 30, WL 211. MAJOR REPAIR ACCOMPLIS HED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001090700101 20010907 00101 NM 2001 9 7 2001UALA01858 1 20010828 A 5320 CHANNEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 519UA 24872 CABIN FLOOR CHANNEL CORRODED, BODY STATION 401 RBL 56. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR CHANNEL STATION 395 TO STATION 415. 2 L 7 2 4F 4 F RT A2NM E17NE 2001090700102 20010907 00102 NM 2001 9 7 2001UALA01859 1 20010828 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 742 STRINGER 34L-33L SHEAR TIE CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090700103 20010907 00103 NM 2001 9 7 2001UALA01860 1 20010828 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 478 LBL 12-22 T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CAP REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090700104 20010907 00104 NM 2001 9 7 2001UALA01861 1 20010828 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 STATION 1175 STRINGER 38L-39L SHEARTIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEARTIE REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090700105 20010907 00105 NM 2001 9 7 2001UALA01864 1 20010828 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 STATION 1285 STRINGER 38L-39L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090700106 20010907 00106 NM 2001 9 7 2001UALA01865 1 20010828 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 STATION 1219 STRINGER 36L-37L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090700107 20010907 00107 NM 2001 9 7 2001UALA01866 1 20010828 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE L NO TEST UK UNKNOWN 1 WP 29 771UA 26932 SEAT 3E AFT EEL LIGHT INOP. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001090700108 20010907 00108 NM 2001 9 7 2001UALA01867 1 20010825 A 3350 LIGHT BOEING 777 777222 1385219 NM CABIN INOPERATIVE A UALA K NONE L NO TEST UK UNKNOWN 1 WP 29 796UA 26931 AFT EEL LIGHT ON SEAT 1F INOP. 2 L 7 2 4F RT T0001SE 2001090700109 20010907 00109 NM 2001 9 7 2001UALA01868 1 20010828 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 STATION 1219 STRINGER 36L-37L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090700110 20010907 00110 NM 2001 9 7 2001UALA01869 1 20010828 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 STATION 1351 STRINGER 33R-34R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090700111 20010907 00111 NM 2001 9 7 2001UALA01870 1 20010828 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 STATION 1153 LBL 10-RBL 28 T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CAP REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090700114 20010907 00114 NM 2001 9 7 2001UALA01875 1 20010828 A 3260 WARNING LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 328UA 24148 UNSCHEDULED LANDING UNDER AMBER ALERT DUE TO IN-TRANSIT LIGHT WOULD NOT EXTINGUISH WITH GEAR SELECTED UP. 2 L 7 2 4F 4 F RT A16WE E2GL 2001090700115 20010907 00115 EU 2001 9 7 QXEA0101199 1 20010728 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PDX - 1/4 INCH CRACK IN FUSELAGE SKIN. LOCATED UNDER MAIN CABIN DOOR FORWARD OF FRAME 4175. REPAIRED IAW FOKKER SRM 53-0 2-05, FIGURE 4 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001090700116 20010907 00116 NM 2001 9 7 QXEA0101200 1 20010723 A 5730 PANEL DHAV DHC8 DHC8202 2809007 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX - NUMEROUS COUNTER SUNK HOLES ON PANEL 623AT HAVE PITTING CORROSION. REPAIRED IAW RD-8-57-1715. 2 H 7 2 4T RT A13NM 2001090700117 20010907 00117 NM 2001 9 7 QXEA0101201 1 20010719 A 5730 SKIN DHAV DHC8 DHC8202 2809007 NM RT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX - RIGHT-HAND WING UPPER SURFACE HAS LIGHT CHAFING AROUND SCREW HOLES IN AFT ROW OF PANEL 422ET. REPAIRED IAW MM 20-3 2-02, 20-34-11, PAGES 201-203 2 H 7 2 4T RT A13NM 2001090700118 20010907 00118 NM 2001 9 7 QXEA0101202 1 20010723 A 7110 COWLING DHAV DHC8 DHC8202 2809007 NM RT NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX - RIGHT-HAND LOWER COWL INTAKE FLANGE HAS A SCREW HEAD CHAFE AT THE OUTBOARD SIDE OF THE RING. CHAFE MEASURES .375 W IDE AND IS APPROXIMATELY .008" DEEP. REPAIRED IAW HORIZON AIR EA 2-71-152 AND RD 8-71-74. 2 H 7 2 4T RT A13NM 2001090700119 20010907 00119 NM 2001 9 7 QXEA0101203 1 20010723 A 7110 COWLING DHAV DHC8 DHC8202 2809007 NM RT NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX - RIGHT-HAND LOWER COWL STIFFNER ON TOP DECK HAS CHAGE APPROXIMATELY 27" FORWARD OF AFT END OUTBOARD SIDE. REPAIRED IAW HORIZON AIR EA 2-71-151. 2 H 7 2 4T RT A13NM 2001090700120 20010907 00120 NM 2001 9 7 QXEA0101204 1 20010719 A 5410 STRUCTURE DHAV DHC8 DHC8202 2809007 NM RT PYLON CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX-RIGHT SIDE MAIN LANDING GEAR "H" MEMBER ACTUATOR ATTACH POINT HAS SURFACE CORROSION. REPAIRED IAW HORIZON AIR EA 2-5 4-88. 2 H 7 2 4T RT A13NM 2001090700121 20010907 00121 NM 2001 9 7 QXEA0101205 1 20010717 A 5530 FLANGE DHAV DHC8 DHC8202 2809007 NM VERTICAL STAB TOOL DAMAGE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX-SEVERAL TOOLING GOUGES AND SCRATCHES ON LEFT HAND VERTICAL STABILIZER LEADING EDGE MOUNT FLANGE. REPAIRED IAW DHC-8 RD8-55-584. 2 H 7 2 4T RT A13NM 2001090700122 20010907 00122 NM 2001 9 7 QXEA0101206 1 20010719 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX-SEAT TRACK NR 7 HAS CORROSION AND A SCRATCH AT STATION 244. REPAIRED IAW DHC-8 SRM 51-40-11 AND SRM 51-40-00. 2 H 7 2 4T RT A13NM 2001090700123 20010907 00123 NM 2001 9 7 QXEA0101207 1 20010719 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX-SEAT TRACK NR 7 HAS CORROSION ON OUTBOARD FLANGE BY ZUES FASTENER HOLE AT STATION 245. REPAIRED IAW DHC-8 SRM 51/40/ 11 AND SRM 51/40/00. 2 H 7 2 4T RT A13NM 2001090700124 20010907 00124 NM 2001 9 7 QXEA0101208 1 20010718 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX-SEAT TRACK NR 8 HAS CORROSION INSIDE TRACK AT STATION 435. REPAIRED IAW DHC-8 SRM 51-20-26 AND RD8-53-1339. 2 H 7 2 4T RT A13NM 2001101200067 20011012 00067 NM 2001 10 12 2001UALA01876 1 20010830 A 7603 208071 LINKAGE BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE NR 1 THROTTLE DAMAGED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING W INADEQUATE Q C DE DESCENT 1 WP 29 995UA 22399 708819 NR 1 ENGINE SHUTDOWN DUE TO THROTTLE CONTROL PROBLEM. *S/D* FOUND THE THROTTLE LINKAGE DISCONNECTED. REINSTALLED THE LINKAGE AND TRIMMED THE FUEL CONTROL. 2 L 7 2 4F 4 F A16WE E2EA 2001090700125 20010907 00125 NM 2001 9 7 QXEA0101209 1 20010718 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX-SEAT TRACK NR 8 HAS CORROSION INSIDE TRACK AT STATION 500. REPAIRED IAW DHC-8 SRM 51-20-26 AND RD8-53-1339. 2 H 7 2 4T RT A13NM 2001090700126 20010907 00126 NM 2001 9 7 QXEA0101210 1 20010722 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX-SEAT TRACK NR 9 HAS GOUGE JUST FORWARD OF STATION 545. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD8-53-784. 2 H 7 2 4T RT A13NM 2001090700127 20010907 00127 NM 2001 9 7 QXEA0101211 1 20010722 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX-SEAT TRACK NR 9 HAS SPOTS OF CORROSION ON INSIDE OF TRACK AT FRAME 597.5. REPAIRED IAW DHC-8 RD8-53-784. 2 H 7 2 4T RT A13NM 2001090700128 20010907 00128 NM 2001 9 7 2001UALA01877 1 20010828 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 STATION 743 STRINGER 37R-38R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090700129 20010907 00129 NM 2001 9 7 QXEA0101212 1 20010719 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX-SEAT TRACK NR 4 HAS CORROSION ON OUTBOARD FLANGE AT STATION 234.5. REPAIRED IAW DHC-8 RD8-53-1539. 2 H 7 2 4T RT A13NM 2001090700130 20010907 00130 NM 2001 9 7 QXEA0101213 1 20010719 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX-SEAT TRACK NR 4 HAS CORROSION ON OUTBOARD FLANGE AT ZUES FASTENER FRAME 252.7. REPAIRED IAW DHC-8 SRM 51-40-11 AND S RM 51-40-00. 2 H 7 2 4T RT A13NM 2001090700131 20010907 00131 NM 2001 9 7 2001UALA01878 1 20010828 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 MAJOR BODY STATION 743 STRINGER 37R-38R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TI E. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090700132 20010907 00132 NM 2001 9 7 QXEA0101214 1 20010718 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX- SEAT TRACK NR 6 HAS SPOTS OF CORROSION ON INSIDE OF TRACK AT STATION 547.5. REPAIRED IAW DHC-8 RD8-53-1339. 2 H 7 2 4T RT A13NM 2001090700133 20010907 00133 NM 2001 9 7 QXEA0101215 1 20010719 A 3110 STRUCTURE DHAV DHC8 DHC8202 2809007 NM INSTRUMENT PANEL DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX-DENT AT STATION X136.800, 5 INCHES OUT OF RADIO ALTIMETER ON RIGHT SIDE. REPAIRED IAW DHC-8 RD8-53-2181. 2 H 7 2 4T RT A13NM 2001090700134 20010907 00134 NM 2001 9 7 2001UALA01880 1 20010830 A 5320 FLOOR SUPPORT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 323UA 23955 AFT CABIN FLOOR, RIGHT HAND DOOR SILL AREA INBOARD OF CREASE BEAM WEB FLOOR SUPPORT ANGLE CORRODED FROM STATION 937 TO S TATION 990. MAJOR REPAIR ACCOMPLISHED, CORRODED CORD ANGLE REMOVED. REPLACED CORD. 2 L 7 2 4F 4 F RT A16WE E2GL 2001090700135 20010907 00135 NM 2001 9 7 QXEA0101216 1 20010718 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX-SEAT TRACK NR 3 HAS GOUGE ON INSIDE OF TRACK AT FRAME 531.5. REPAIRED IAW DHC-8 RD8-53-3644. 2 H 7 2 4T RT A13NM 2001091900133 20010919 00133 NM 2001 9 19 2001UALA01881 1 20010828 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 199UA 28717 UPPER DECK EMERGENCY CEILING LIGHTS ROW 12, 14, 16, 18 AND JUST AFT OF ROW 19 ARE INOP. LAMPS BURNED OUT (5 PLACES). RE PLACED ALL 5 BULBS. 2 L 7 4 4F 4 F RT A20WE E24NE 2001090700136 20010907 00136 NM 2001 9 7 QXEA0101217 1 20010718 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX-SEAT TRACK NR 6 HAS SEVERAL SPOTS OF CORROSION AT STATION 597.5. REPAIRED IAW DHC-8 RD8-53-1339. AND RD8-53-4936. 2 H 7 2 4T RT A13NM 2001090700137 20010907 00137 NM 2001 9 7 QXEA0101218 1 20010723 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX-REPLACE NR 7 SEAT TRACK DUE TO CORROSION. REPLACED IAW DHC-8 SRM 51-40-11 AND SRM 51-40-00. 2 H 7 2 4T RT A13NM 2001090700138 20010907 00138 NM 2001 9 7 2001UALA01886 1 20010830 A 5522 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ELEVATOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 RIGHT ELEVATOR UPPER LEADING EDGE SKIN DAMAGED BY ELECTRO STATIC DISCHARGE 6 INCHES FROM TIP, HOLE DIA .25 INCH. MAJOR R EPAIR ACCOMPLISHED. SEAL AND POT HOLE, OVERLAYED FIBERGLASS PLY, DRILLED FASTENER HOLE AND RESTORED FINISH. 2 L 7 2 4F 4 F RT A2NM E17NE 2001090700139 20010907 00139 NM 2001 9 7 QXEA0101219 1 20010723 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX-REPLACE RIGHT HAND INBOARD AFT SEAT TRACK STATION 551.5 - 600.0 NR 9 DUE TO CORROSION. REPLACED IAW DHC-8 RD8-53-44 72 AND SRM 51-40-00. 2 H 7 2 4T RT A13NM 2001090700140 20010907 00140 NM 2001 9 7 2001UALA01887 1 20010830 A 5330 DOUBLER BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 998UA 22741 FOUND GOUGE ON INTERNAL DOUBLER OF SKIN AT BODY STATION 787 STRINGER 6L. MAJOR REPAIR ACCOMPLISHED INSTALLED DOUBLER RE PAIR. 2 L 7 2 4F 4 F A16WE E2EA 2001090700141 20010907 00141 NM 2001 9 7 QXEA0101221 1 20010719 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX-CARGO DOOR HAS SCRATCH IN DOOR SKIN LOCATED ON LOWER SIDE. REPAIRED IAW DHC-8 RD8-52-230. 2 H 7 2 4T RT A13NM 2001090700142 20010907 00142 NM 2001 9 7 QXEA0101222 1 20010717 A 5530 STRUCTURE DHAV DHC8 DHC8202 2809007 NM VERTICAL STAB GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX-THREE TOOLING GOUGES ON LOWER RIGHT HAND VERTICAL STABILIZER LEADING EDGE MOUNTING FLANGE. REPAIRED IAW DHC-8 RD8-55 -584. 2 H 7 2 4T RT A13NM 2001090700143 20010907 00143 NM 2001 9 7 2001UALA01889 1 20010830 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CANNING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 322UA 23954 STATION 1016 PRESSURE DOME 11:30 POSITION HAS AREA OF OIL CANING AND TOOLING MARK. MAJOR REPAIR ACCOMPLISHED DAMAGED ARE A CUT OUT. INSTALLED DOUBLER 2 L 7 2 4F 4 F RT A16WE E2GL 2001090700144 20010907 00144 NM 2001 9 7 2001UALA01894 1 20010830 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 519UA 24872 CABIN FLOOR BEAM T-CAP CORRODED AT STATION 324 RBL 59. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2001090700145 20010907 00145 NM 2001 9 7 2001UALA01897 1 20010830 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1329 STRINGER 39L-39R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090700146 20010907 00146 NM 2001 9 7 2001UALA01899 1 20010830 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1329 STRINGER 36L-37L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090700147 20010907 00147 NM 2001 9 7 2001UALA01901 1 20010830 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1439 STRINGER 39R-39L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090700148 20010907 00148 NM 2001 9 7 2001UALA01904 1 20010830 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1333 STRINGER 35R-36R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090700149 20010907 00149 NM 2001 9 7 2001UALA01906 1 20010830 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1263 STRINGER 36L-37L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090700150 20010907 00150 NM 2001 9 7 2001UALA01907 1 20010830 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1263 STRINGER 38L-39L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090700151 20010907 00151 NM 2001 9 7 2001UALA01909 1 20010830 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1241 RBL 22-LBL24 T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CAP. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090700152 20010907 00152 NM 2001 9 7 QXEA0101223 1 20010717 A 5530 FLANGE DHAV DHC8 DHC8202 2809007 NM STABILIZER SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX-LEFT HAND STABILIZER FORWARD SPAR UPPER FLANGE HAS TOOL SCRATCH NEAR RIB 8, STATION YH77.500. REPAIRED IAW DHC-8 RD8 -55-626. 2 H 7 2 4T RT A13NM 2001090700153 20010907 00153 NM 2001 9 7 2001UALA01910 1 20010830 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1197 STRINGER 35L-36L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090700154 20010907 00154 NM 2001 9 7 2001UALA01911 1 20010830 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1241 STRINGER 38R TO 39R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090700155 20010907 00155 NM 2001 9 7 2001UALA01913 1 20010830 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1562 STRINGER 38R-38L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001090700156 20010907 00156 NM 2001 9 7 2001UALA01914 1 20010831 A 5230 6546921528 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 324UA 41456 23956 FWD CARGO DOOR SKIN DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED SKIN DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001090700157 20010907 00157 NM 2001 9 7 QXEA0101224 1 20010717 A 5530 FLANGE DHAV DHC8 DHC8202 2809007 NM VERTICAL STAB SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX-RIGHT HAND STABILIZER FORWARD SPAR LOWER EDGE FLANGE HAS SMALL SCRATCH NEAR RIB 8 STATION YH77.500. REPAIRED IAW DHC -8 RD8-55-626. 2 H 7 2 4T RT A13NM 2001090700158 20010907 00158 NM 2001 9 7 QXEA0101225 1 20010717 A 5530 FLANGE DHAV DHC8 DHC8202 2809007 NM VERTICAL STAB DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX-TOOL SCRATCH ON RIGHT HAND SIDE OF VERTICAL STABILIZER TOP RIB MOUNT FLANGE STATION AT 325AT. REPAIRED IAW DHC-8 SR M 51-20-16 AND SRM 55-30-16. 2 H 7 2 4T RT A13NM 2001090700159 20010907 00159 NM 2001 9 7 QXEA0101226 1 20010717 A 5530 FLANGE DHAV DHC8 DHC8202 2809007 NM VERTICAL STAB GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX-NUMEROUS TOOL GOUGES/SRATCHES ON UPPER HALF OF VERTICAL STABILIZER FORWARD SPAR RIGHT HAND LEADING EDGE MOUNT FLANGE . REPAIRED IAW DHC-8 RD8-55-584. 2 H 7 2 4T RT A13NM 2001090700160 20010907 00160 NM 2001 9 7 QXEA0101227 1 20010717 A 5530 FLANGE DHAV DHC8 DHC8202 2809007 NM VERTICAL STAB GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX-FOUR TOOLING GOUGES ON UPPER HALF OF VERTICAL STABILIZER FORWARD LEADING EDGE MOUNT FLANGE. REPAIRED IAW DHC-8 RD8-5 5-584. 2 H 7 2 4T RT A13NM 2001090700161 20010907 00161 WP 2001 9 7 0103069962 1 20010901 A 3010 093000400012 DUCT DOUG DC9 DC931 3022065 WP LT & RT WING STUCK A NWAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 01 914RW 47362 DURING SLAT EXTENSION, AIRCRAFT ROLLED TO THE RIGHT FOR APPROXIMATELY 2-3 SECONDS THEN ABRUPTLY STOPPED ROLL. CONSULTED MAINTENANCE CONTROL AND COM AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED EXCESSIVE AMOUNT OF GREASE AND SOLID FILM LUBRICANT FROM TELESCOPING DUCTS FROM BOTH LEFT AND RIGHT SIDES. CYCLED SLATS SEVERAL TIMES. OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 2001090700162 20010907 00162 NM 2001 9 7 QXEA0101228 1 20010720 A 5753 SKIN DHAV DHC8 DHC8202 2809007 NM TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX-AT STATION YW 204.00 TO YW 261.00 TOP OF FLAP THERE IS CHAFING A LONG LINE. REPAIRED IAW DHC-8 RD8-57-1022. 2 H 7 2 4T RT A13NM 2001090700163 20010907 00163 NM 2001 9 7 QXEA0101229 1 20010723 A 5730 ACCESS PANEL DHAV DHC8 DHC8202 2809007 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX-ACCESS PANEL 523AT COUNTERSINK HOLES HAVE PITTING CORROSION. REPAIRED IAW DHC-8 RD8-57-1715. 2 H 7 2 4T RT A13NM 2001090700164 20010907 00164 NM 2001 9 7 0103076624 1 20010823 A 3350 CONNECTOR BOEING 747 747251B 1384892 NM CABIN DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 624US 21706 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING IN 'A' ZONE INOPERATIVE. RECONNECTED ELECTRICAL CONNECTORS. OP ERATIONAL CHECK NORMAL. 2 L 7 4 4F A20WE 2001090700165 20010907 00165 NM 2001 9 7 QXEA0101230 1 20010722 A 5753 SKIN DHAV DHC8 DHC8202 2809007 NM TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX-RIGHT HAND WING INBOARD FLAP UPPER SURFACE NEAR LEADING EDGE IS LIGHTLY CHAFED DUE TO CONTACT WITH WING TRAILING EDG E SHROUD. REPAIRED IAW DHC-8 RD8-57-1241. 2 H 7 2 4T RT A13NM 2001090700166 20010907 00166 NM 2001 9 7 QXEA0101231 1 20010726 A 5754 SKIN DHAV DHC8 DHC8202 2809007 NM LE FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX-RIGHT HAND WING LEADING EDGE 612AR HAS A FASTENER HOLE TORN OUT 9.5 INCHES FROM INBOARD END IN BOTTOM ROW. REPAIRED IAW HORIZON AIR EA 2-57-124 AND RD8-57-2030. 2 H 7 2 4T RT A13NM 2001090700167 20010907 00167 EU 2001 9 7 QXEA0101232 1 20010705 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-DENT IN FUSELAGE SKIN FORWARD OF RIGHT HAND AR INLET. REPAIRED IAW FOKKER SRM 53-02-02. 2 L 7 2 4F RT A20EU 2001090700168 20010907 00168 NM 2001 9 7 0103082203 1 20010827 A 3210 651765752 BRACE BOEING 727 727251 138408H NM RT MLG SHEARED A NWAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 01 203US 35076 8393 22543 DURING PUSHBACK, THE RIGHT MAIN GEAR WAS TRACKING UNUSUALLY. AIRCRAFT RETURNED TO GATE FOR INSPECTION. MAINTENANCE FOU ND RIGHT MAIN SIDE BRACE ATTACHMENT SHEARED AT GEAR. DTW MAINTENANCE AWAITING SIDE BRACE PARTS AND WILL BE REPLACED UPO N ARRIVAL. ALL OPERATIONAL CHECKS PENDING JOB COMPLETION. 2 L 7 3 4F A3WE 2001090700169 20010907 00169 EU 2001 9 7 QXEA0101233 1 20010709 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-DENT IN FUSELAGE SKIN AT STATION 1750. DENT IS CREASED AND BEYOND LIMITS. REPAIRED IAW FOKKER SRM 53-01-01, SRM 53-0 2-02, PAGE 2, AND SRM 51-31-01, PAGE 13 & 14. 2 L 7 2 4F RT A20EU 2001090700170 20010907 00170 EU 2001 9 7 QXEA0101234 1 20010709 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-SHARP DENT ON LEFT HAND SIDE OF FUSELAGE AT FRAME 5305. REPAIRED IAW FOKKER SRM 53-01-01. 2 L 7 2 4F RT A20EU 2001090700171 20010907 00171 EU 2001 9 7 QXEA0101235 1 20010702 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-SHARP DENT ON LEFT HAND SIDE OF FUSELAGE BELOW AFT WINDOW AT STATION 659.252. REPAIRED IAW FOKKER SRM 53-02-02. 2 L 7 2 4F RT A20EU 2001090700172 20010907 00172 EU 2001 9 7 QXEA0101236 1 20010707 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-SKIN DENTED AROUND FRAME 6305 ON LEFT HAND SIDE OF FUSELAGE. REPAIRED IAW FOKKER SRM 53-02-02 AND SRM 53-01-01, PAGE 9. 2 L 7 2 4F RT A20EU 2001090700173 20010907 00173 EU 2001 9 7 QXEA0101237 1 20010705 A 5330 PANEL FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-SHARP DENT ON BOTTOM OF AIRCRAFT AFT OF PANEL 91BC, STATION 16745, WL-1650 BETWEEN STRINGER 74-1.REPAIRED IAW FOKKER SRM 53-02-02. 2 L 7 2 4F RT A20EU 2001090700174 20010907 00174 SO 2001 9 7 SWIA200110031 1 20010711 A 6123 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO COCKPIT ACTIVATED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 187SW 120037 AUTO FEATHER WARNING ON TAKE OFF ROLL.RAN BOTH ENGINES W/AUTO FEATHER ARMED. APPLIED 60% TORQUE. NO AUTO FEATHER WARNI NGS. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001090700175 20010907 00175 EU 2001 9 7 QXEA0101238 1 20010705 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-MARKER BEACON ANTENNA, CORROSION FOUND ON FUSELAGE SKIN UNDER ANTENNA.REPAIRED IAW FOKKER SRM 53-01-01 AND SRM 51-10 -04, PAGE 9. 2 L 7 2 4F RT A20EU 2001090700176 20010907 00176 EU 2001 9 7 QXEA0101239 1 20010705 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-AFT RADIO ALTIMETER ANTENNA, CORROSION FOUND ON FUSELAGE SKIN UNDER ANTENNA. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9 AND SRM 53-01-01. 2 L 7 2 4F RT A20EU 2001090700177 20010907 00177 EU 2001 9 7 QXEA0101240 1 20010705 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-FORWARD RADIO ALTIMETER ANTENNA, CORROSION FOUND ON FUSELAGE SKIN UNDER ANTENNA. REPAIRED IAW FOKKER SRM 51-10-04, P AGE 9 AND SRM 53-01-01. 2 L 7 2 4F RT A20EU 2001090700178 20010907 00178 EU 2001 9 7 QXEA0101241 1 20010705 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-LOWER FORWARD COMM ANTENNA, CORROSION FOUND ON FUSELAGE SKIN UNDER ANTENNA. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9 AND SRM 53-01-01. 2 L 7 2 4F RT A20EU 2001090700179 20010907 00179 EA 2001 9 7 SWIA200110032 1 20010716 A 5246 LATCH CNDAIR CL600 CL6002B19 EA FUEL DOOR DEFECTIVE A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 586SW 7028 'DOORS' LIGHT ON MAP ON TAKEOFF ROLL. 7/17/2001 - 'SERVICE' DOOR LIGHT ILLUMINATED DURING TAKEOFF. ABORTED AND RETURNE D TO GATE. FOUND FORWARD FUEL DOOR UNLATCHED. INSPECTED LATCH FOR CONDITION AND SECURITY. OPS CHECK GOOD AT THIS TIME. 7/17/2001 - FOUND FUEL DOOR FASTENER UNLATCHED. RE-SECURED LATCH. OK TO CONTINUE. UPDATE REPLACED BOTH OUTBOARD DOO R LATCHES. OPS CHECK GOOD ON FUEL SERVICES DOOR. 2 L 7 2 4F RT A21EA 2001090700180 20010907 00180 EU 2001 9 7 QXEA0101242 1 20010712 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-WEAR ON FUSELAGE SKIN FROM AFT FAIRING CONTACT AT STATION 16965 AND STRINGER 69. REPAIRED IAW FOKKER SRM 53-01-00, P AGE 6 AND SRM 51-10-04, PAGE 9. 2 L 7 2 4F RT A20EU 2001090700181 20010907 00181 EU 2001 9 7 QXEA0101243 1 20010713 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-CLIP CRACKED IN AFT PIT AT STATION 13815B, STRINGER 2. REPAIRED IAW FOKKER SRM 53-22-04, SRM 51-31-01, PAGE 13 & 14, AND HORIZON AIR EA 4-53-1507. 2 L 7 2 4F RT A20EU 2001090700182 20010907 00182 EU 2001 9 7 QXEA0101244 1 20010715 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-CLIP CRACKED IN AFT PIT AT STATION 13815A, STRINGER 73. REPAIRED IAW FOKKER SRM 53-22-04, SRM 51-31-01, PAGE 13 & 14 , AND HORIZON AIR EA 4-53-1507. 2 L 7 2 4F RT A20EU 2001090700183 20010907 00183 EU 2001 9 7 QXEA0101245 1 20010713 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-CLIP CRACKED IN AFT PIT AT STATION 13815A, STRINGER 2. REPAIRED IAW FOKKER SRM 51-31-01, PAGES 13 & 14, SRM 53-22-04 , AND HORIZON AIR EA 4-53-1507. 2 L 7 2 4F RT A20EU 2001090700184 20010907 00184 EU 2001 9 7 QXEA0101246 1 20010711 A 5310 STRUCTURE FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-RIGHT HAND SIDE FUSELAGE BETWEEN STATION 18870 AND 19275 HAS 3 SHARP DENTS. REPAIRED IAW FOKKER SRM 53-01-01. 2 L 7 2 4F RT A20EU 2001090700185 20010907 00185 EU 2001 9 7 QXEA0101247 1 20010707 A 5310 STRUCTURE FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-RIGHT HAND SIDE AFT FUSELAGE HAS AN OUTWARD DENT AT FRAME 21805. REPAIRED IAW FOKKER SRM 53-02-02. 2 L 7 2 4F RT A20EU 2001090700186 20010907 00186 EU 2001 9 7 QXEA0101248 1 20010711 A 5310 STRUCTURE FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-SHARP DENT ON RIGHT HAND AFT FUSELAGE BETWEEN STATION 19775 AND 20285. REPAIRED IAW FOKKER SRM 53-01-01. 2 L 7 2 4F RT A20EU 2001090700187 20010907 00187 SO 2001 9 7 SWIA200110033 1 20010714 A 3350 SIGN EMB 120 EMB120ER 3260203 SO CABIN BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 566SW 120341 6BC EMERGENCY EXIT LIGHT SIGN BROKEN. REPLACED AND SECURED EMERGENCY EXIT SIGN AT 6BC. OPS CHECK GOOD. PN 10-1301-15. 2 L 7 2 4T RT A31SO 2001090700188 20010907 00188 EU 2001 9 7 QXEA0101249 1 20010705 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-UPPER TCAS ANTENNA, NICKS FOUND IN FUSELAGE SKIN UNDER ANTENNA. REPAIRED IAW FOKKER SRM 53-01-01. 2 L 7 2 4F RT A20EU 2001090700189 20010907 00189 EU 2001 9 7 QXEA0101250 1 20010709 A 5210 DOOR FRAME FOKKER F28 F28MK4000 4990810 EU PAX DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-MAIN CABIN DOOR TOP OUTSIDE FRAME HAS SURFACE CORROSION ON FORWARD PORTION OF FRAME IN SECONDARY SEAL AREA AT STATIO N 4175, WL615, BL800. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9. 2 L 7 2 4F RT A20EU 2001090700190 20010907 00190 EU 2001 9 7 QXEA0101251 1 20010712 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-LEFT HAND LOWER FUSELAGE EXTERIOR BETWEEN FRAME 15205 AND 15635 AT STRINGER 7 AND 9 HAS SKIN CHAFING. REPAIRED IAW F OKKER SRM 53-01-00, SRM 53-01-01 AND SRM 51-10-04. 2 L 7 2 4F RT A20EU 2001090700191 20010907 00191 EU 2001 9 7 QXEA0101252 1 20010705 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-UPPER NAV/COMM ANTENNA, CORROSION FOUND ON FUSELAGE SKIN UNDER ANTENNA. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9. 2 L 7 2 4F RT A20EU 2001090700192 20010907 00192 EA 2001 9 7 SWIA200110034 1 20010715 A 2760 4916405 ECU CNDAIR CL600 CL6002B19 EA SPOILER FAILED A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 417SW 1525 1525 7400 SPOILERON FAULT MESSAGE ON EICAS DURING TAXI WITH SPOILERON OUTLINED IN WHITE. RESET SECU SPOILER FAULT STATUS MESSAGE I N ACCORDANCE WITH CRJ AMM 27-61-00. INSTALLED SERVICEABLE SECU ON NR 1 SIDE. TEST GOOD IAW 27-60-00. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2001090700193 20010907 00193 EU 2001 9 7 QXEA0101253 1 20010709 A 5260 SCREW FOKKER F28 F28MK4000 4990810 EU AIRSTAIR BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-MAIN CABIN DOOR STAIRS ATTACHMENT HAS BROKEN SCREW IN 9TH ANCHOR NUT AT UPPER MOUNTING. REPAIRED IAW FOKKER SRM 51-3 1-01, PAGE 10 & 11. 2 L 7 2 4F RT A20EU 2001090700194 20010907 00194 EU 2001 9 7 QXEA0101254 1 20010705 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-CORROSION ON LEFT HAND INBOARD SEAT TRACK AT FRAME 10966. REPAIRED IAW FOKKER SRM 53-10-4, PAGE 9. 2 L 7 2 4F RT A20EU 2001090700195 20010907 00195 SO 2001 9 7 SWIA200110035 1 20010718 A 5220 SEAL EMB 120 EMB120ER 3260203 SO EMERGENCY EXIT LEAKING A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 289YV 120289 FLIGHT ATTENDANT REPORTS LOUD AIR NOISE AT EXIT AT SEAT 9B/9C. INSTALLED RTV ON E-EXIT 9BC HANDLE SEAL AS REQUIRED. NO N OISE NOTED AT THIS TIME DURING PRESSURIZATION CHECK. 2 L 7 2 4T RT A31SO 2001090700196 20010907 00196 SO 2001 9 7 SWIA200110036 1 20010717 A 5753 FLAP EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 199SW 120237 RIGHT NACELLE FLAP HAS A CRACK IN UPPER SURFACE. REMOVED AND REPLACED RIGHT NACELLE FLAP IAW MM 27-50-02. P/N: 120-403 27-001 2 L 7 2 4T RT A31SO 2001090700197 20010907 00197 EA 2001 9 7 SWIA200110037 1 20010716 A 3040 WINDOW CNDAIR CL600 CL6002B19 EA COCKPIT FAULTY A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 416SW 7089 RT WINDOW HEAT CAUTION MESSAGE 30 SECONDS AFTER TAKE OFF. REMOVED AND REPLACED RT SIDE WINDOW WITH SERVICEABLE WINDOW IA W CRJ MM 56-12-01. PN ON 328 2 L 7 2 4F RT A21EA 2001090700198 20010907 00198 EA 2001 9 7 SWIA200110038 1 20010719 A 2760 270007 PCU CNDAIR CL600 CL6002B19 EA SPOILER FAULTY A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 417SW 7400 RIGHT SPOILERON WHITE MESSAGE ON MID FLIGHT TO LANDING. REMOVED RIGHT INBOARD SPOILERON PCU, REPLACED WITH SERVICEABLE P CU IAW MM 27-62-01. LEAK CHECK OK. 2 L 7 2 4F RT A21EA 2001090700199 20010907 00199 EA 2001 9 7 SWIA200110039 1 20010719 A 2120 SMOKE CNDAIR CL600 CL6002B19 EA CABIN DETECTED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 NM 07 906SW 7510 STRONG SMELL OF SMOKE ON LANDING. AFTER STOWING THRUST REVERSERS SMELL SEEMED TO SUBSIDE. PERFORMED RUN CHECK ON BOTH PA CKS. NO SMOKE SMELL NOTED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2001090700200 20010907 00200 SO 2001 9 7 SWIA200110040 1 20010718 A 2751 3069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203 SO COCKPIT FAULTY A SWIA O OTHER N FALSE WARNING CR CRUISE 1 NM 07 190SW 120050 FLAP ASYMMETRY, CONTROL FAULT, DISAGREEMENT LIGHTS AND MAP FLAP AND ADVANCED SWS LIGHTS ILLUMINATED BRIEFLY INFLIGHT AS AIRCRAFT LEVELED IN CRUISE FLIGHT. REMOVED AND REPLACED FLAP ANNUNCIATOR IAW 27-50-00. OPERATED FLAPS THROUGH RANGE OF T RAVEL SEVERAL TIMES. OPS CHECK GOOD. S/N OFF: 0200 2 L 7 2 4T RT A31SO 2001090700201 20010907 00201 SO 2001 9 7 SWIA200110041 1 20010720 A 2622 FIRE BOTTLE EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 293SW 120320 FIRE EXTINGUISHER UNDER THE FLIGHT ATTENDANT SEAT IS SHOWING EMPTY. REPLACED FIRE EXTINGUISHER UNDER THE FA'S SEAT WITH SERVICEABLE UNIT. P/N ON: 1211 S/N ON: W070425 S/N OFF: V-877583 2 L 7 2 4T RT A31SO 2001090700202 20010907 00202 SO 2001 9 7 SWIA200110043 1 20010723 A 6120 78249046 PCU EMB 120 EMB120ER 3260203 SO LT ENGINE DEFECTIVE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 215SW 120281 LEFT ENGINE TORQUE FLUCTUATION AT +30 TO -30 PERCENT ON CLIMBOUT. RETURNED TO SLC FOR NORMAL LANDING. ATTEMPTED TO FLY WITH EEC'S OFF, NO CHANGE. REMOVED AND REPLACED PCU ON LEFT ENGINE. OPS CHECKS, LEAK CHECKS GOOD. P/N: 782490-46 S/N ON : 900528 S/N OFF: 851019. 2 L 7 2 4T RT A31SO 2001090700203 20010907 00203 SO 2001 9 7 SWIA200110044 1 20010722 A 2721 6225734002 SERVO EMB 120 EMB120ER 3260203 SO RUDDER DEFECTIVE A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 582SW 120350 RUDDER HAS CLICK IN TRAVEL AS IT IS MOVED THROUGH FULL TRAVEL. INSPECTED AND DETERMINED RUDDER TRIM SERVO TO BE CAUSE OF CLICKING. INSTALLED SERVICEABLE SERVO FOR RUDDER TRIM IAW MM 27-00-00. RUDDER OPS CHECK GOOD. SMOOTH THROUGH FULL TRAVE L. P/N: 622-5734-002 S/N ON: 6060 S/N OFF: 10359 2 L 7 2 4T RT A31SO 2001090700204 20010907 00204 EU 2001 9 7 QXEA0101255 1 20010705 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-CORROSION ON RIGHT HAND INBOARD SEAT TRACK BETWEEN FRAMES 12405 AND 12875. REPAIRED IAW FOKKER SRM 53-10-4, PAGE 9. 2 L 7 2 4F RT A20EU 2001090700205 20010907 00205 EU 2001 9 7 QXEA0101256 1 20010705 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-CORROSION ON LEFT HAND INBOARD SEAT TRACK AT FRAME 13345. REPAIRED IAW FOKKER SRM 53-10-4, PAGE 9. 2 L 7 2 4F RT A20EU 2001090700206 20010907 00206 EU 2001 9 7 QXEA0101257 1 20010705 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-CORROSION ON LEFT HAND INBOARD SEAT TRACK BETWEEN FRAMES 15205 AND 15635. REPAIRED IAW FOKKER SRM 53-10-4, PAGE 9. 2 L 7 2 4F RT A20EU 2001090700207 20010907 00207 EU 2001 9 7 QXEA0101258 1 20010705 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-CORROSION ON RIGHT HAND INBOARD SEAT TRACK AT FRAME 13815B. REPAIRED IAW FOKKER SRM 53-10-4, PAGE 9. 2 L 7 2 4F RT A20EU 2001090700208 20010907 00208 EU 2001 9 7 QXEA0101259 1 20010705 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-CORROSION ON RIGHT HAND INBOARD SEAT TRACK BETWEEN FRAMES 14285 AND 14755. REPAIRED IAW FOKKER SRM 53-10-4, PAGE 9. 2 L 7 2 4F RT A20EU 2001090700209 20010907 00209 EU 2001 9 7 QXEA0101260 1 20010705 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-CORROSION ON RIGHT HAND OUTBOARD SEAT TRACK AT FRAME 4610. REPAIRED IAW FOKKER SRM 53-10-4, PAGE 9. 2 L 7 2 4F RT A20EU 2001090700210 20010907 00210 EU 2001 9 7 QXEA0101261 1 20010705 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-LEFT HAND INBOARD SEAT TRACK BETWEEN FRAMES 8305 AND 8805 IS CORRODED. REPAIRED IAW FOKKER SRM 53-10-4, PAGE 9. 2 L 7 2 4F RT A20EU 2001090700211 20010907 00211 WP 2001 9 7 UPS01036707 1 20010813 A 5244 DOOR DOUG DC8 DC873F 302199F WP ACCESSORY BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 815UP 46002 INSPECTION TYPE:C2 AFT ACC COMPT FS 1560 BULKHEAD DOOR CORRODED ALONG BOTTOM FWD SIDE. REMOVED DOOR, REMOVED CORROSION A ND FOUND OUT OF LIMITS. FABRICATE REPAIR DOUBLER & FILLER DC8 MM 52-30-00. INSTALL FILLER & DOUBLER IAW DC8 SRM 51-1-21 AND REINSTALL DOOR IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001090700212 20010907 00212 WP 2001 9 7 UPS01036708 1 20010818 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 815UP 46002 INSPECTION TYPE:C2 CABIN SEAT TRACK G BETWEEN PALLET POSITION 7 & 8 SEVERAL SCALLOPS HAVE ELONGATED HOLES. SEAT TRACK OU T OF LIMITS IAW DC8 SRM 53-2-3 FIG 12. REMOVED DAMAGED SCALLOP SECTIONS IAW DC8 SRM 53-2-3 FIG 6D. INSTALLED PLUGS AND CHANNELS IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001091000424 20010910 00424 EU 2001 9 10 UPS01136751 1 20010901 A 3350 BATTERY AIRBUS A300 A300F4622R 3930360 EU CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 122UP 0807 INSPECTION TYPE:PFLT EMERGENCY LIGHTS INOP. R&R NR 1 AND NR 2 BATTERIES AND PERFORMED CAPACITY TEST M AUTO. STANDBY POWE R SUPPLY UNIT PER MTC 52-300-03-1-4 PASS TEST. 2 L 7 2 4F RT A35EU 2001090700214 20010907 00214 NM 2001 9 7 DL72E011479 1 20010904 A 3350 387 SIGN BOEING 727 727247 138408F NM L1 DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 830WA 21482 EMERGENCY EXIT SIGN OVER L1 INOP. RELAMPED. 2 L 7 3 4F A3WE 2001090700215 20010907 00215 NM 2001 9 7 DL72E011480 1 20010904 A 3350 387 SIGN BOEING 727 727247 138408F NM COCKPIT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 830WA 21482 EMERGENCY EXIT SIGN OVER WINDOW EXIT, CAPTS SIDE, AFT EXIT INOP. RELAMPED. 2 L 7 3 4F A3WE 2001090700216 20010907 00216 NM 2001 9 7 DL72L011345 1 20010805 A 2761 65C163002 ACTUATOR BOEING 727 727232 1384082 NM LT SPOILER FAILED A DALA O OTHER F E FLT CONT AFFECTED VIBRATION/BUFFET CR CRUISE 1 SO 27 502DA 21304 LEFT MOST INBOARD B SYS FLIGHT SPOILER FLOATS IN FLIGHT, CAUSES VIBRATIONS IN LEFT TURNS (POM SPOILER FLOAT C/W)SPOILER FLOAT OBSERVED INFLIGHT BY SECOND OFFICER. REMOVED AND REPLACED NR 5 LEFT INBD FLT SPOILER ACTUATOR PER OPN 7052. 2 L 7 3 4F A3WE 2001090700217 20010907 00217 NM 2001 9 7 DL72L011417 1 20010826 A 2710 69667411 BEARING BOEING 727 727232 1384082 NM AILERON SCORED A DALA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 27 502DA 21304 YOKE BINDING IN ROLL AXIS. CHECKS OK ON GROUND. FOUND CAPTS AILERON DISCONNECT CAM AND BEARING PLATE RATCHETING. REPLACE D SAME. RIGGED SYS. CHKS NORMAL. REF IPC 27-10-00-07 ITEMS 445-420-410 2 L 7 3 4F A3WE 2001090700218 20010907 00218 NM 2001 9 7 DL72S011353 1 20010817 A 3350 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 546DA 22677 FWD EMER PATH/OVERHEAD LIGHTS INOP. CA REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 2001090700219 20010907 00219 NM 2001 9 7 DL72S011400 1 20010824 A 7931 WARNING SYSTEM BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE COCKPIT MALFUNCTIONED A DALA E ENGINE SHUTDOWN N FALSE WARNING TO TAKEOFF 1 SO 27 538DA 62229 22076 700202 DURING CLIMBOUT NR 1 ENGINE LOW OIL PRESSURE OR FILTER BYPASS LIGHT ILLUMINATED. RAN POM PROCEDURE ACCOMPLISHED INFLIGHT SHUTDOWN DUE TO SUSPECTED FILTER BYPASS. ALL OTHER OIL INDICATIONS NORMAL. CA REPLACED AND INSPECTED OIL FILTER. NO TRO UBLE FOUND. LEAK CKS NORMAL. RAN NR 1 ENG TO TAKE OFF POWER, LIGHT DID NOT COME ON. ALL OTHER OIL INDICATIONS NORMAL. CL EANED BYPASS SWITCH CONN. 2 L 7 3 4F 4 F A3WE E2EA 2001090700220 20010907 00220 NM 2001 9 7 DL72S011404 1 20010825 A 7931 1163P005201 PRESSURE SWITCH BOEING 727 727232 1384082 NM NR 1 ENGINE INTERMITTENT A DALA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SO 27 538DA 22076 LOW OIL PRESSURE/FILTER BYPASS LIGHT ILLUM IN FLIGHT. OIL PRESSURE WAS NORMAL AND PRECAUTIONARY ENG SHUTDOWN WAS ACCOMPL ISHED. REPLACED DIFF PRESS SWITCH AND LOP/FILTER BYPASS LIGHT MODULE ALONG WITH MASTER DIM AND TEST DIODE CARD. RAN ENGS AT HIGH POWER AND INSPECTED CHIP DETECTOR AND REPLACED MAIN OIL FILTER. OPS CHECK NORMAL AND RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2001090700221 20010907 00221 NM 2001 9 7 DL72S011416 1 20010824 A 5311 FRAME BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 524DA 21584 FUSELAGE FRAME AT FS 970 STR 26L-27L. THE FS 970 FRAME INNER CHORD WAS FOUND CRACKED AT A FLOOR ATTACH LOCATION BETWEEN STRINGERS 26L AND 27L. THE CRACK IS TYPICAL OF BAC S/B 727-53A0195 AND AD 92-12-03. 2 L 7 3 4F A3WE 2001090700222 20010907 00222 NM 2001 9 7 DL72S011419 1 20010827 A 3350 LIGHT BOEING 727 727225A 1384077 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 805EA 22436 PAX SEAT 15 & 29 EMERGENCY LIGHTS INOP. RE-ATTACHED CONNECTOR AT SEAT ROW 15 AND RELAMPED SEAT ROW 29. 2 L 7 3 4F RT A3WE 2001090700223 20010907 00223 NM 2001 9 7 DL72S011422 1 20010827 A 3233 ACTUATOR BOEING 727 727232 1384082 NM NLG WW LEAKING A DALA K NONE K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 27 516DA 21432 ON LANDING COMPLETE A SYSTEM HYD FAILURE. FOUND OVER CENTER ACTUATOR BULKHEAD FITTING BROKEN AND ACTUATOR LEAKING. CA RE PLACED SAME. 2 L 7 3 4F A3WE 2001090700224 20010907 00224 NM 2001 9 7 UPS01236782 1 20010830 A 7830 064530100 BRACKET BOEING 727 727172C 1384058 NM #3 ENGINE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 916UP 19808 INSPECTION TYPE:C #3 R/H T/R ACTUATOR AFT PANEL ATTACH BRACKET IS CRACKED BRACKET REPLACED IAW 70-30-31 2 L 7 3 4F A3WE 2001090700225 20010907 00225 NM 2001 9 7 UPS01236783 1 20010829 A 5330 SKIN BOEING 727 727172C 1384058 NM BS441 S18-19R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 916UP 19808 INSPECTION TYPE:C CARRY OUT PERMENANT REPAIR IAW UPS INSTRUCTIONS AT BS 441 BETWEEN S1 8 AND S19 R/H TEMP REPAIR REM OVED, AREA INSPECTED NO DEFECTS FOUND, HFEC PERFORMED ON AREA AND NDF, REPAIR CARRIED OUT IAW SMRO EO 2001-039-001 2 L 7 3 4F A3WE 2001090700226 20010907 00226 EU 2001 9 7 QXEA0101262 1 20010707 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-CRACKED CASTELLATION AT FRAME 15205 AND STRINGER 58. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 2001090700227 20010907 00227 EU 2001 9 7 QXEA0101263 1 20010707 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-CRACKED CASTELLATION AT FRAME 15205 AND STRINGER 59. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 2001090700228 20010907 00228 EU 2001 9 7 QXEA0101264 1 20010707 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-CRACKED CASTELLATION AT FRAME 13815B AND STRINGER 46. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 2001090700229 20010907 00229 EU 2001 9 7 QXEA0101265 1 20010707 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-CRACKED CASTELLATION AT FRAME 13815A AND STRINGER 33. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 2001090700230 20010907 00230 EU 2001 9 7 QXEA0101266 1 20010707 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-CRACKED CASTELLATION AT FRAME 12875 AND STRINGER 42. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 2001090700231 20010907 00231 EU 2001 9 7 QXEA0101267 1 20010707 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-CRACKED CASTELLATION AT FRAME 12875 AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 2001090700232 20010907 00232 EU 2001 9 7 QXEA0101268 1 20010708 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-CRACKED CASTELLATION AT FRAME 16060 BETWEEN STRINGER 57 AND 58. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 2001090700233 20010907 00233 NM 2001 9 7 DL72S011441 1 20010831 A 2916 RESERVOIR BOEING 727 727232 1384082 NM HYDRAULIC SYS LOW A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 532DA 22045 RETURNED TO DFW FOR LOW HYDRAULICS FLUID IN SYSTEM A. SERVICED A SYSTEM TO 4.4 GALLONS. INSPECTED ACFT FOR LEAKS, NONE F OUND. 2 L 7 3 4F A3WE 2001090700234 20010907 00234 EU 2001 9 7 QXEA0101269 1 20010707 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-CRACKED CASTELLATION AT FRAME 15205 AND STRINGER 55. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 2001090700235 20010907 00235 EU 2001 9 7 QXEA0101270 1 20010713 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-SCRATCH ON INTERNAL FUSELAGE SKIN BETWEEN FRAME 16660 - 16060 AND STRINGER 31 - 32. REPAIRED IAW FOKKER SRM 51-10-04 AND SRM 53-01-01. 2 L 7 2 4F RT A20EU 2001090700236 20010907 00236 EU 2001 9 7 QXEA0101271 1 20010712 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-DENT IN FUSELAGE AND SKIN TAIL SECTION FORWARD OF STATION 19775, ABOVE HYDRAULIC SERVICE PANEL RIGHT HAND SIDE OF AI RCRAFT. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 8. 2 L 7 2 4F RT A20EU 2001090700237 20010907 00237 EU 2001 9 7 QXEA0101272 1 20010705 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-CORROSION FOUND ON FUSELAGE SKIN UNDER NR 3 COMM BLANKING PLATE. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9. 2 L 7 2 4F RT A20EU 2001090700238 20010907 00238 EU 2001 9 7 QXEA0101273 1 20010705 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-AFT DME ANTENNA, CORROSION FOUND ON FUSELAGE SKIN UNDER ANTENNA.REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9. 2 L 7 2 4F RT A20EU 2001090700239 20010907 00239 EU 2001 9 7 QXEA0101274 1 20010717 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-CASTELLATION CRACKED BEYOND STOP DRILL AT FRAME 67-2 AND STRINGER 29. REPAIRED IAW HORIZON AIR EA 4-53-1505. 2 L 7 2 4F RT A20EU 2001090700240 20010907 00240 EU 2001 9 7 QXEA0101275 1 20010717 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-CASTELLATION CRACKED BEYOND STOP DRILL AT FRAME 50-2 AND STRINGER 25. REPAIRED IAW HORIZON AIR EA 4-53-1506. 2 L 7 2 4F RT A20EU 2001090700241 20010907 00241 EU 2001 9 7 QXEA0101276 1 20010717 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-CASTELLATION CRACKED BEYOND STOP DRILL AT FRAME 32-2 AND STRINGER 28 AND 29. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13 AND 14 AND SRM 51-30-02, PAGE 9 & 10. 2 L 7 2 4F RT A20EU 2001090700242 20010907 00242 NM 2001 9 7 DL72S011445 1 20010831 A 5320 655612910 SILL BOEING 727 727232 1384082 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 524DA 21584 FUSELAGE C2 DOOR OPENING LOWER SILL OUTER CHORD WAS FOUND WITH AN AREA OF CORROSION ON THE OUTBD SKIN FLANGE NEAR FS 950 E+10. THE CORROSION WAS MACHINED AWAY AND REPAIRED WITH AN ALUMINUM REPAIR ANGLE AND STRAP PER ER/A 381581-14, REV A. 2 L 7 3 4F A3WE 2001090700243 20010907 00243 EU 2001 9 7 QXEA0101277 1 20010717 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-CASTELLATION CRACKED BEYOND STOP DRILL AT FRAME 16-2 AND STRINGER 33. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001090700244 20010907 00244 EU 2001 9 7 QXEA0101278 1 20010717 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-CRACKED CASTELLATION AT FRAME 17565 AND STRINGER 23. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5. 2 L 7 2 4F RT A20EU 2001090700245 20010907 00245 EU 2001 9 7 QXEA0101279 1 20010717 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-CRACKED CASTELLATION AT FRAME 16-2 BETWEEN STRINGER 10 AND 11 FORWARD SIDE. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5 . 2 L 7 2 4F RT A20EU 2001090700246 20010907 00246 EU 2001 9 7 QXEA0101280 1 20010702 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU WING DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-TAIL LEADING EDGE 51F HAS SMALL DENT. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 7 AND SRM 51-70-10. 2 L 7 2 4F RT A20EU 2001090700247 20010907 00247 NM 2001 9 7 DL72S011451 1 20010829 A 3350 900542 CHARGER BOEING 727 727225A 1384077 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8882Z 21579 L-1 WING EMERGENCY EXIT LIGHT INOP, REPLACED CHARGER. 2 L 7 3 4F RT A3WE 2001090700248 20010907 00248 EU 2001 9 7 QXEA0101281 1 20010711 A 5511 RIB FOKKER F28 F28MK4000 4990810 EU HORIZONTAL STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-HORIZONAL STABILIZER LEADING EDGE 51B INTERNAL RIBS 3, 5. AND 7 CRACKED. REPAIRED IAW FOKKER SRM 55-02-02, PAGE 4 AN D HORIZON AIR EA 4-55-295. 2 L 7 2 4F RT A20EU 2001090700249 20010907 00249 EU 2001 9 7 QXEA0101282 1 20010713 A 5541 RIB FOKKER F28 F28MK4000 4990810 EU RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-RIB 5 ON RUDDER IS CRACKED IN 2 PLACES. REPAIRED IAW FOKKER SRM 55-31-01, PAGE 2. 2 L 7 2 4F RT A20EU 2001090700250 20010907 00250 EU 2001 9 7 QXEA0101283 1 20010707 A 5530 STRUCTURE FOKKER F28 F28MK4000 4990810 EU VERTICAL STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-RUDDER COVE CRACKED ON VERTICAL STABILIZER AT RIB 3.4. REPAIRED IAW FOKKER SRM 51-00-03, PAGE 17, SRM 55-31-01, PAGE 2, AND SRM 51-31-01, PAGE 7. 2 L 7 2 4F RT A20EU 2001090700251 20010907 00251 EU 2001 9 7 QXEA0101284 1 20010716 A 5520 STRUCTURE FOKKER F28 F28MK4000 4990810 EU ELEVATOR PUNCTURED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-RIGHT HAND ELEVATOR INBOARD LEADING EDGE PUNCTURED. REPAIRED IAW FOKKER SRM 55-01-01, PAGE 8, SRM 55-02-04, PAGE 1-4 , AND SRM 51-31-05. 2 L 7 2 4F RT A20EU 2001090700252 20010907 00252 EU 2001 9 7 QXEA0101285 1 20010712 A 5532 SKIN FOKKER F28 F28MK4000 4990810 EU VERTICAL STAB DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-VERTICAL STABILIZER SKIN PANEL HAS 2 MINOR DENTS. REPAIRED IAW FOKKER SRM 51-00-00, PAGE 1B AND HORIZON AIR EA 4-55- 297. 2 L 7 2 4F RT A20EU 2001090700253 20010907 00253 NM 2001 9 7 DL72W011348 1 20010817 A 5330 65562312 BEAR STRAP BOEING 727 727247 138408F NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2820W 21058 THE UPPER HINGE CUTOUT OF THE R1 DOOR OPENING WAS FOUND WITH A 2.5 INCH CRACK IN THE BEARSTRAP. THE SKIN WAS CUTOUT TO ACCESS THE BEARSTRAP AND THE CRACK IN THE BEARSTRAP STOP DRILLED. THE AREA WAS REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS PER ER/A 381555-14. 2 L 7 3 4F A3WE 2001090700254 20010907 00254 EU 2001 9 7 QXEA0101286 1 20010706 A 5320 COLLAR FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-CORROSION FOUND ON BASE OF INBOARD FORWARD SPIGOT COLLAR ON LEFT HAND FLAP STATION 1700. REPAIRED IAW FOKKER SRM 51- 10-4, PAGE 9. 2 L 7 2 4F RT A20EU 2001090700255 20010907 00255 EU 2001 9 7 QXEA0101287 1 20010710 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-FORWARD DME ANTENNA, CORROSION FOUND ON FUSELAGE SKIN UNDER ANTENNA. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9. 2 L 7 2 4F RT A20EU 2001090700256 20010907 00256 EU 2001 9 7 QXEA0101288 1 20010712 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CANNING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 YYC-OIL CANNING IN FUSELAGE SKIN AT RIGHT HAND KEEL BETWEEN FRAME 11905 - 11805. REPAIRED IAW FOKKER SRM 53-02-01, PAGE 4 AND SRM 53-02-02, PAGE 2. 2 L 7 2 4F RT A20EU 2001090700257 20010907 00257 NM 2001 9 7 DL72W011413 1 20010826 A 3397 WIRE BOEING 727 727247 138408F NM CABIN DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2819W 21057 PAX SEATS 23, 24, 25, 26 EMERGENCY LIGHTS INOPERATIVE, REPAIRED PINCHED WIRING. ALL CHECKED OK. 2 L 7 3 4F A3WE 2001090700258 20010907 00258 EA 2001 9 7 COMA0160689 1 20010906 A 5320 60034017351 ANGLE CNDAIR CL600 CL6002B19 EA FS280 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 966CA 12036 7132 THE FORWARD J-ANGLE AT FS80 BETWEEN LBL9.0 AND RBL9.0 IS CORRODED.PERFORMED A MAJOR REPAIR BY REPLACING CORRODED FORWARD J-ANGLE AT FS 280 BETWEEN LBL9.0 AND RBL9.0 I/A/W WVAC 601R-53-2676. 2 L 7 2 4F RT A21EA 2001090700259 20010907 00259 EA 2001 9 7 COMA0160690 1 20010904 A 2710 6009118610 ARM CNDAIR CL600 CL6002B19 EA WHEEL WELL FROZEN A COMA O OTHER S AFFECT SYSTEMS CR CRUISE 1 SO 01 917CA 7017 FLIGHT #5338. DURING CRUISE FLIGHT THE AILERON CONTROLS FELT HARD OR STIFF TO OPERATE, AFTER DISCONNECTING INTERCONNECT FOUND CO-PILOTS SYSTEM TO BE AT FAULT. FLIGHT CONTINUED TO CVG AND LANDED SAFELY.REPLACED RIGHT AILERON CONTROL ARM ASS EMBLY. 2 L 7 2 4F RT A21EA 2001090700260 20010907 00260 NM 2001 9 7 DL72W011420 1 20010827 A 3350 900835A BATTERY PACK BOEING 727 7272Q8 138407W NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 831L 21826 FOUND RT OVERWING EMERGENCY DOOR LIGHTS INOP. CA REPLACED BATTERY PACK, CKS GOOD. 2 L 7 3 4F A3WE 2001090700261 20010907 00261 2001 9 7 COMA0160691 4 20010904 A 3140 INDICATOR CNDAIR CL600 CL6002B19 EA A COMA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 914CA 7012 FLIGHT #5536. DURING TAKE-OFF ROLL RECEIVED AN INTERMITTENT AILERON AND SPOILER CONFIGURATION MESSAGE, ABORTED TAKE OFF AND RETURNED TO THE GATE.SET AIRCRAFT IN TAKE-OFF CONFIGURATION, PERFORMED OPERATIONAL CHECK, DISCREPANCY COULD NOT BE DUPLICATED BY MAINTENANCE. 2 L 7 2 4F RT A21EA 2001090700262 20010907 00262 NM 2001 9 7 DL733011409 1 20010826 A 3244 TIRE BOEING 737 737347 1384647 NM LT MLG SEPARATED A DALA O OTHER O OTHER TO TAKEOFF 1 SO 27 3301 23181 NR 1 MAIN TIRE TREAD SEPARATED FROM TIRE ON TAKE OFF. DAMAGING LEFT I/B FLAPS AND LEFT GEAR DOOR. CA REPLACED TIRE, GEAR DOOR AND REPAIRED FLAP DAMAGE. 2 L 7 2 4F RT A16WE 2001090700263 20010907 00263 NM 2001 9 7 DL733011477 1 20010904 A 2560 MV10S MEGAPHONE BOEING 737 73735B NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 221DL 23970 AFT MEGAPHONE INOP. REPLACED AFT MEGAPHONE. 2 L 7 2 4F RT A16WE 2001091200084 20010912 00084 EA 2001 9 12 COMA0160670 1 20010903 A 3040 NP1393222 CONTROLLER CNDAIR CL600 CL6002B19 EA WINDOW HEAT FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 960CA 13131 7117 FLIGHT 5697. DURING CLIMBOUT OF CVG RECEIVED A RIGHT WINDOW HEAT CAUTION MESSAGE, AIRCRAFT RETURNED TO THE FIELD. REPL ACED THE WINDSHIELD HEAT CONTROLLER. 2 L 7 2 4F RT A21EA 2001091200086 20010912 00086 EA 2001 9 12 COMA0160688 1 20010906 A 5320 601R3103077 SPLICE CNDAIR CL600 CL6002B19 EA FUSELAGE MISMANUFACTURED A COMA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 966CA 7132 DURING INCORPORATION OF SB 601R-53-037 REV B THE SPLICE PLATE(S) WAS FABRICATED INCORRECTLY BY THE MANUFACTURE. FABRICA TED/INSTALLED NEW SPLICE PLATES IAW WVAC EO 601R-53-2679. 2 L 7 2 4F RT A21EA 2001090700264 20010907 00264 NE 2001 9 7 DL738011423 2 20010827 A 7200 CFM567 ENGINE BOEING 737 737832 13844CF NM GE CFM56 CFM56* 13802 NE NR 1 FAILED A DALA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 SO 27 380DA 7044 3136 30266 875386 LEFT ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED ON FINAL APPROACH. THROTTLE WAS PULLED TO IDLE, LIGHT DID NOT GO OUT, EN GINE WAS SHUT DOWN. OIL QUANTITY WAS 0, PRESS WAS 1 PSI. NR 1 ENGINE CHANGED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001090700265 20010907 00265 2001 9 7 DL738011427 4 20010829 A 2350 5145142 PANEL BOEING 737 737832 13844CF NM COCKPIT DEFECTIVE A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 379DA 30349 LOST COMMUNICATIONS. FD OBS MIC SELECT PANEL PTT SW BAD. REPLACED PANEL PER MM. 2 L 7 2 4F RT A16WE 2001090700266 20010907 00266 NM 2001 9 7 DL738011433 1 20010830 A 2520 CONDUIT BOEING 737 737832 13844CF NM CABIN OUT OF POSITION A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 382DA 30345 BURNING SMELL IN THE OVERHEAD AREA AROUND SEAT ROW 21-ABC. FOUND PROTECTIVE NYLON BRAIDED WIRE CONDUIT LAYING ON R EADING LIGHT. NO OTHER DAMAGE FOUND. REPOSITIONED WIRE BUNDLE. 2 L 7 2 4F RT A16WE 2001090700267 20010907 00267 NM 2001 9 7 DL738011462 1 20010901 A 3350 LIGHT BOEING 737 737832 13844CF NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 383DN 30346 EMERGENCY AISLE LIGHTS OUT AT 25 AND 27 DEF. RELAMPED SAME, CHECKS OK. 2 L 7 2 4F RT A16WE 2001090700268 20010907 00268 NM 2001 9 7 DL73K011361 1 20010819 A 2560 P20700030 FLASHLIGHT BOEING 737 737232 1384475 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 304DL 23076 DURING L/O FOUND EMERGENCY FLASHLIGHT AT AFT-LOWER STATION INOP. 2 L 7 2 4F RT A16WE 2001090700269 20010907 00269 NM 2001 9 7 DL73K011364 1 20010819 A 3350 SOCKET BOEING 737 737232 1384475 NM CABIN DEFECTIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 321DL 23093 EMERGENCY LIGHT AT ROW 19DEF INOP. REPLACED LIGHT SOCKET IN SEAT ROW. 2 L 7 2 4F RT A16WE 2001090700270 20010907 00270 NM 2001 9 7 DL73K011369 1 20010818 A 5330 SKIN BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 237WA 23185 THE UPPER HINGE CUTOUT OF THE AFT ENTRY DOOR (L2) SURROUND SKIN WAS FOUND WITH A .375 INCH TYPICAL CRACK. THE CRACK WAS ROUTED OUT OF THE SKIN AND REPAIRED WITH AN EXTERNAL STEEL DOUBLER PER B737 SRM 53-30-3 FIG. 21A AND ER/A 381563-14, REV A. 2 L 7 2 4F A16WE 2001090700271 20010907 00271 NM 2001 9 7 DL73K011383 1 20010822 A 5553 FITTING BOEING 737 737232 1384475 NM VERTICAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 325DL 23097 CORROSION WAS FOUND ON THE VERTICAL STABILIZER ATTACH LUGS AND CLEVIS. THE LUG FACES WERE BLENDED AND THE BORES OVE RSIZED TO REMOVE CORROSION. OVERSIZED BUSHINGS WERE THEN INSTALLED. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001090700272 20010907 00272 NE 2001 9 7 DL73K011385 2 20010822 A 7311 749001307 COOLER BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE UNSERVICEABLE A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 328DL 23100 717148 ENGINE OIL SYSTEM CONTAMINATED WITH FUEL. REPLACED FUEL OIL COOLER DL P/N 794001307 S/N 398 2 L 7 2 4F 4 F RT A16WE E2EA 2001090700273 20010907 00273 2001 9 7 DL73K011458 4 20010901 A 2230 AUTOTHRUST SYS BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE COCKPIT MALFUNCTIONED A DALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 27 316DL 23088 709139 T/O ROLL NOTICED ENGINE PARAMETERS FLUCTUATING. T/O ABORTED AUTOTHROTTLES WERE ENGAGED. MAINT OPERATED ENGS AT T/O PWR P ER PFHB WITH OUT AUTOTHROTTLES ALL PARAMETERS CK NML. RAN ENGS AT T/O PWR AGAIN WITH AUTOTHROTTLES ENGAGED PER PFHB - NT F 2 L 7 2 4F 4 F RT A16WE E2EA 2001090700274 20010907 00274 NM 2001 9 7 DL757011352 1 20010817 A 3350 0201991007 LIGHT BOEING 757 757232 1384965 NM CABIN DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 625DL 22915 PASSENGER SEAT 26D EMERGENCY LIGHT DAMAGED, INSTALLED NEW SEAT MOUNTED LIGHT. 2 L 7 2 4F RT A2NM 2001090700275 20010907 00275 NM 2001 9 7 DL757011372 1 20010817 A 5330 143N35211 SKIN BOEING 757 757232 1384965 NM FUSELAGE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 638DL 23761 THE FUSELAGE SKIN WAS FOUND WITH A LIGHTNING STRIKE AT FS 680 AT STRINGER 27R AND A GOUGE AT FS 665 BELOW STRINGER 27R. BOTH DAMAGES WERE REMOVED WITH 2 INCH CUTOUTS. 2 L 7 2 4F RT A2NM 2001090700276 20010907 00276 NM 2001 9 7 DL757011380 1 20010821 A 2530 COFFEEMAKER BOEING 757 757232 1384965 NM AFT GALLEY DIRTY A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 6715C 30486 FLIGHT ATTENDANT REPORTED HAZE AND SMELL IN REAR OF AIRCRAFT. TURNED OFF UTILITY BUSSES. HAZE AND SMELL IMPROVED. INSPECTED UNDER OVERHEAD PANEL IN REAR GALLEY AND ABOVE BOTH LAVS. ALL SHOW NO SIGNS OF OVERHEATING. CHECKED EQUIP COOLI NG FANS AND RECIRC FANS. NTF. RAN ENGINES AND APU WITH PACKS ON. NO SMOKE OR HAZE. FOUND COFFEE GROUNDS BURNED AND STUCK IN BOTTOM OF COFFEMAKER IN REAR GALLEY. REMOVED SAME. F/A REPORT OVENS WERE OFF 2 L 7 2 4F RT A2NM 2001090700277 20010907 00277 NM 2001 9 7 DL757011389 1 20010823 A 5330 143N34001 SKIN BOEING 757 757232 1384965 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 639DL 23993 THE FUSELAGE SKIN WAS FOUND DENTED AT FS 454 AND STRINGER 27R NEAR THE E&E DOOR OPENING. THE DAMAGE WAS REMOVED IN THE S KIN AND IN THE UNDERLYING BEARSTRAP. REPAIRED PER ER/A 381521-14, REV A. 2 L 7 2 4F RT A2NM 2001090700278 20010907 00278 NE 2001 9 7 ZW0A0106101 2 20010729 A 7200 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D217A 52053 NE NR 2 FAILED A ZW0A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 13 9406W 53126 3227 DURING CLIMB OUT NUMBER 2 ENGINE FAILED. CAUSE-UNKNOWN. CHANGED NUMBER 2 ENGINE. LAST CHECK C 012201 JFK ---OPEN--- 2 L 7 2 4F 4 F RT A6WE E9NE 2001090700279 20010907 00279 NM 2001 9 7 ZW0A0106102 1 20010726 A 3397 WIRE BOEING 757 7572Q8 1384972 NM CABIN WORN A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 701TW 28160 DURING PRE FLIGHT EGRESS LIGHT STRIP NEXT TO LAV C WERE INOP DUE TO WEAR. INSTALLED NEW CABLE. 2 L 7 2 4F RT A2NM 2001090700280 20010907 00280 NM 2001 9 7 ZW0A0106203 1 20010802 A 3350 80741 LIGHT BOEING 767 7673Y0 NM CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 639TW 26208 DURING PREFLIGHT THE EGRESS LIGHT STRIP AT SEAT 40 AB WAS INOP. DUE TO WEAR. REPLACED EGRESS LIGHT STRIP AT SEAT 40 AB W ITH P/N 8074-1. 2 L 7 2 4F RT A1NM 2001090700281 20010907 00281 NM 2001 9 7 ZW0A0106204 1 20010802 A 3350 S417N5092SMI LIGHT BOEING 767 7673Y0 NM CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 632TW 24953 DURING MAINTENANCE EGRESS LIGHTS INOP DUE TO WEAR. REPLACED EGRESS LIGHT AND LENS P/N S417N509-2SMI AND P/N 81000-22703 . 2 L 7 2 4F RT A1NM 2001090700282 20010907 00282 WP 2001 9 7 ZW0A0106301 1 20010806 A 5230 STRUCTURE DOUG DC9 DC982 3022082 WP CARGO DOOR DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 922TW 48013 DURING MAINTENANCE A DEEP GROOVE WAS FOUND IN THE CUT OUT FOR THE MID CARGO DOOR HANDLE DUE TO WEAR. REPLACED DOOR HANDL E CUTOUT PER SPM 6-70-01. 2 L 7 2 4F A6WE 2001090700283 20010907 00283 WP 2001 9 7 ZW0A0106303 1 20010804 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 9305N 49395 DURING MAINTENANCE THE AFT FLOOR EGRESS LIGHTS WERE INOP DUE TO WEAR. REPLACED BATTERY PACK P/N5822-2 AND FEEDER JUMPER CABLE PER MM 33-51-01. 2 L 7 2 4F RT A6WE 2001090700284 20010907 00284 NM 2001 9 7 ZW0A0106402 1 20010806 A 3350 LIGHT BOEING 767 7673Q8 NM CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 636TW 30301 THE EMERGENCY EXIT LIGHTS WERE INOPERATIVE JUST AFT OF THE LT INBD T/E FLAP AND RT INBD T/E FLAP, THE FLOOR EGRESS LIGHT S WERE INOPERATIVE AT ROWS 37J AND 37H TO 44JH, AND THE EGRESS LIGHTS WERE INOPERATIVE AT SEATS 5A 5C 16A AND 16C. REPL ACED THE LAMP PN 767 FOR EACH OF THE EXIT LIGHTS, RECONNECTED THE POWER LEAD AT ROW 37 FOR THE EGRESS LIGHTS AT 37H TO 4 4JH, AND REPLACED THE BATTERY CHARGER FOR LIGHTS AT SEATS 5A 5C 16A AND 16C. 2 L 7 2 4F RT A1NM 2001090700285 20010907 00285 WP 2001 9 7 ZW0A0106502 1 20010808 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INTERMITTENT A ZW0A K NONE O OTHER CR CRUISE 1 CE 13 925TW 49357 THE EGRESS LIGHTS ROWS 7 TO 14 CAME ON INTERMITTENTLY. OPERATIONAL TEST NORMAL. 2 L 7 2 4F A6WE 2001090700286 20010907 00286 NE 2001 9 7 ZW0A0106504 2 20010809 A 7200 ENGINE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE RIGHT MAKING METAL A ZW0A E ENGINE SHUTDOWN E B VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CE 13 406TW 55073 2213 AT 600 FEET IN DESCENT THE RT ENGINE PRODUCED SMOKE IN THE CABIN AND A PHYSICAL VIBRATION. ENGINE WAS SHUT DOWN. FOUND M ETAL IN THE TAIL PIPE. CHANGED THE ENGINE. 2 L 7 2 4F 4 F TR A6WE E00061EN 2001090700287 20010907 00287 NM 2001 9 7 ZW0A0106601 1 20010809 A 3230 LANDING GEAR BOEING 717 717200 1383700 NM NLG FAILED A ZW0A A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 CE 13 2417F 55084 THE NOSE LANDING GEAR FAILED TO EXTEND SO THE FLIGHT DIVERTED TO AND LANDED AT BLV. PASSENGERS DEPLANED FROM THE LT AND RT FWD SLIDES. 2 L 7 2 4F TR A6WE 2001090700288 20010907 00288 WP 2001 9 7 ZW0A0106801 1 20010813 A 2612 FIRE DETECTOR DOUG DC9 DC983 3022083 WP CARGO BAY MALFUNCTIONED A ZW0A F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 13 968TW 53618 THE AFT CARGO FIRE DETECTOR WARNING SOUNDED. FIRED BOTTLE AND MADE UNSCHEDULED LANDING AT PIT. PLACARDED FIRE DETECTION SYSTEM INOPERATIVE PER MEL AND OPERATED TO STL. REPLACED THE AFT CARGO FIRE PROTECTION CEU CONNECTOR ACCOUNT CONTAMINAT ED. 2 L 7 2 4F RT A6WE 2001090900001 20010909 00001 EU 2001 9 9 DHL2001363021 1 20010908 A 7500 DUCT AIRBUS 300 A300B4203 3930306 EU A DHLA O OTHER O OTHER IN INSP/MAINT 1 SO 01 363DH 85 On A-5 check---Discrepancy #2 engine inboard reverser cowling cooling duct rear flange worn out matting surface cracked. 1) Welded #2 engine inboard reverser cowling cooling duct per G.E. CF6-50 Engine Shop Mannual 70-41-00.Note: Flange was welded on aircraft. 2 L 7 2 4F RT A35EU 2001090900002 20010909 00002 SO 2001 9 9 C2XA01IA356 1 20010905 A 3350 J1482 CONNECTOR EMB 120 EMB120ER 3260203 SO CABIN LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15725 120173 IAH- DURING PERFLIGHT THE CREW NOTED THAT THE LAST ROW OF EMERGENCY LIGHTING ON THE FLOOR DID NOT ILLUMINATE. IAH- MAIN TENANCE RESECURED THE EMERGENCY LIGHT CONNECTOR, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFE CTS NOTED,AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001091000001 20010910 00001 SO 2001 9 10 C2XA01IA357 1 20010905 A 3397 W220192424 WIRE EMB 120 EMB120ER 3260203 SO CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16724 120171 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT A SECTION OF AISLE PATH LIGHTING WAS INOP. MAINTENANCE REPAIRE D A BROKEN WIRE ON THE AFFECTED LIGHT STRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001091000002 20010910 00002 SO 2001 9 10 C2XA01IA358 1 20010906 A 5280 12036136001 BRACKET EMB 120 EMB120ER 3260203 SO LEFT NACELLE BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 22727 120177 IAH - DURING MAINTENANCE INSPECTION, THE LEFT HAND OUTBOARD AFT MAIN GEAR DOOR WAS FOUND TO HAVE A BROKEN BRACKET. MAINT ENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001091000003 20010910 00003 NM 2001 9 10 QXEA0101289 1 20010731 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION AND SOME RAISED METAL AT STATION 542 TO 545. REPAIRED IAW DHC-8 RD 8-53-3644, SRM 51-20-11, SRM 51-20-16 AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2001091000004 20010910 00004 NM 2001 9 10 QXEA0101290 1 20010731 A 5340 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - RIGHT-HAND INBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION AND SOME RAISED METAL AT STATION 541 TO 548. REPAIRED IA W RD 8-53-784 , DHC-8 SRM 51-20-11, SRM 51-20-16 AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2001091000005 20010910 00005 NM 2001 9 10 QXEA0101291 1 20010801 A 5320 WEB DHAV DHC8 DHC8202 2809007 NM LT MLG WW CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - LEFT-HAND NACELLE DECK INBOARD WHEEL PAN CHAFED THROUGH IN TWO PLACED. REMOVED AND REPLACED DAMAGED PAN IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001091000006 20010910 00006 NM 2001 9 10 QXEA0101292 1 20010801 A 5310 STRUCTURE DHAV DHC8 DHC8202 2809007 NM CARGO DOORWAY CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX-DOPPLER ABOVE CARGO DOOR INCLOSURE IS CHAFED IN 2 SPOTS. REPAIRED IAW DHC-8 RD8-53-5461. 2 H 7 2 4T RT A13NM 2001091000007 20010910 00007 NM 2001 9 10 QXEA0101302 1 20010805 A 5412 FIREWALL DHAV DHC8 DHC8202 2809007 NM NR 2 NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX-NACELLE NR 2 HAS A 3/4 INCH CRACK IN FIREWALL ON OUTBOARD SIDE NEXT TO TOP AFT CORNER OF IGNITOR DOOR. REPAIRED IAW RD8-54-806 2 H 7 2 4T RT A13NM 2001091000008 20010910 00008 NM 2001 9 10 QXEA0101303 1 20010806 A 7921 VALVE DHAV DHC8 DHC8* NM NR 1 ENGINE FAILED A QXEA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 NM 09 401QX 4031 GEG - DIVERTED TO GEG ON FLIGHT FROM SEA TO BTM FOR NR 1 ENGINE OIL TEMPERATURE HIGH. REPLACED OIL COOLER BYPASS VALVE. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091000009 20010910 00009 NM 2001 9 10 QXEA0101304 1 20010802 A 5230 STRUCTURE DHAV DHC8 DHC8* NM CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - CARGO DOOR DAMAGED AT FORWARD STRUCTURE CABLE FEED-THROUGH BY CABLE CHAFING.REPAIRED IAW HORIZON AIR EA 9-52-122. 2 H 7 2 4T RT A13NM 2001091000010 20010910 00010 NM 2001 9 10 QXEA0101305 1 20010802 A 5230 STRUCTURE DHAV DHC8 DHC8* NM CARGO DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - BAGGAGE DOOR INNER STRUCTURE DENTED WITH CRACK ON VERTICAL MEMBER ABOVE FORWARD COUNTERBALANCE ASSEMBLY. REPAIRED DAMAGE IAW E.A. 9-52-123. 2 H 7 2 4T RT A13NM 2001091000011 20010910 00011 NM 2001 9 10 QXEA0101306 1 20010801 A 7110 COWLING DHAV DHC8 DHC8202 2809007 NM NR 1 ENGINE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX- NR 1 ENGINE LOWER COWL, FORWARD OUTBOARD LATCH BUTTPLATE IS CHAFED. REPAIRED IAW DHC-8 RD8-71-18 AND HORIZON AIR EA 2-71-155. 2 H 7 2 4T RT A13NM 2001091000012 20010910 00012 NM 2001 9 10 QXEA0101307 1 20010802 A 5720 FLANGE DHAV DHC8 DHC8202 2809007 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX-CORROSION AROUND FASTENER HOLES ON FLANGE FOR PANEL 624BT FORWARD INBOARD CORNER. REPAIRED IAW DHC-8 SRM 51-00-06, R D8-57-529, AND RD8-57-633. 2 H 7 2 4T RT A13NM 2001091000013 20010910 00013 NM 2001 9 10 QXEA0101308 1 20010803 A 5740 FLANGE DHAV DHC8 DHC8202 2809007 NM RT WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX-GOUGES ON TOP SURFACE OF LEADING EDGE FLANGE AT RIGHT WING STATION YW376. REPAIRED IAW DHC-8 RD8-57-1675 AND SRM 51- 20-36. 2 H 7 2 4T RT A13NM 2001091000014 20010910 00014 NM 2001 9 10 QXEA0101309 1 20010801 A 5320 ATTACH FITTING DHAV DHC8 DHC8202 2809007 NM MLG ACTUATOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX-LEFT HAND MAIN LANDING GEAR RETRACTION ACTUATOR ATTACHMENT FITTING HAS MINOR CORROSION JUST OUTBOARD OF BUSHING. REP AIRED IAW DHC-8 RD8-54-1178. 2 H 7 2 4T RT A13NM 2001091000015 20010910 00015 NM 2001 9 10 QXEA0101310 1 20010803 A 5740 FLANGE DHAV DHC8 DHC8202 2809007 NM RT WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX-GOUGES ON TOP SURFACE OF RIGHT WING LEADING EDGE FLANGE FROM YW321 TO YW326. REPAIRED IAW DHC-8 RD8-57-1675 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2001091000016 20010910 00016 NM 2001 9 10 QXEA0101311 1 20010803 A 5740 FLANGE DHAV DHC8 DHC8202 2809007 NM RT WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX-GOUGES ON TOP SURFACEOF RIGHT WING LEADING EDGE FLANGE AT YW297. REPAIRED IAW DHC-8 RD8-57-1675 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2001091000017 20010910 00017 NM 2001 9 10 QXEA0101312 1 20010803 A 5740 FLANGE DHAV DHC8 DHC8202 2809007 NM RT WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX-GOUGES ON TOP SURFACE RIGHT WING LEADING EDGE FLANGE AT YW315. REPAIRED IAW DHC-8 RD8-57-1675 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2001091000018 20010910 00018 NM 2001 9 10 QXEA0101313 1 20010803 A 5740 FLANGE DHAV DHC8 DHC8202 2809007 NM RT WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX-GOUGES ON TOP SURFACES OF RIGHT WING LEADING EDGE FLANGE AT YW202. REPAIRED IAW DHC-8 RD8-57-1675 AND SRM 51-20-16 A ND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2001091000019 20010910 00019 NM 2001 9 10 QXEA0101314 1 20010803 A 5740 FLANGE DHAV DHC8 DHC8202 2809007 NM RT WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX-GOUGES ON TOP SURFACE OF RIGHT WING LEADING EDGE FLANGE AT YW288. REPAIRED IAW DHC-8 RD8-57-1675, SRM 51-20-36, AND SRM 51-20-16. 2 H 7 2 4T RT A13NM 2001091000020 20010910 00020 NM 2001 9 10 QXEA0101315 1 20010803 A 5740 FLANGE DHAV DHC8 DHC8202 2809007 NM RT WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX-GOUGES ON TOP SURFACE OF RIGHT WING LEADING EDGE FLANGE AT YW195. REPAIRED IAW DHC-8 RD8-57-1675, RM 51-20-16, AND S RM 51-20-36. 2 H 7 2 4T RT A13NM 2001091000021 20010910 00021 NM 2001 9 10 QXEA0101316 1 20010806 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - RIGHT HAND INBOARD SEAT TRACK TOP FLANGE HAS NICKS WITH RAISED METAL AT STATION 352 Y9.25 RIGHT. REPAIRED IAW DHC- 8 SRM 51-40-11, RD 8-53-3403 AND HORIZON AIR EA 2-53-314. 2 H 7 2 4T RT A13NM 2001091000022 20010910 00022 NM 2001 9 10 QXEA0101317 1 20010802 A 5410 STIFFENER DHAV DHC8 DHC8202 2809007 NM NR 1 NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - NR 1 NACELLE PANEL 413AL , OIL SERVICE DOOR, CENTER STIFFENER CRACKED. REPAIRED IAW DHC-8 RD 8-71-213. 2 H 7 2 4T RT A13NM 2001091000023 20010910 00023 NM 2001 9 10 QXEA0101318 1 20010802 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - PITTING CORROSION IN CENTER OF LEFT-HAND SEAT TRACK FORWARD OF STATION X545.0., REPAIRED IAW DHC-8 SRM 51-20-16, S ECTION C 1-9 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2001091000024 20010910 00024 NM 2001 9 10 QXEA0101319 1 20010802 A 5210 STRUCTURE DHAV DHC8 DHC8202 2809007 NM PAX DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - CORROSION ON AND UNDER NUT PLATE ON BOTTOM PERIPHERY OF MAIN CABIN DOOR. REPAIRED IAW DHC-8 CPM CHAPTER 4, PAGE 4- 25 AND SRM 51-40-00. 2 H 7 2 4T RT A13NM 2001091000025 20010910 00025 NM 2001 9 10 QXEA0101320 1 20010804 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - CORROSION IN AND AROUND NUT PLATES ON LEFT-HAND INBOARD SEAT TRACK AT STATION X182.0 TO X190.9. REPAIRED IAW DHC-8 CPM 5-2 THROUGH 5-7 AND CPM 5-47. 2 H 7 2 4T RT A13NM 2001091000026 20010910 00026 NM 2001 9 10 QXEA0101321 1 20010802 A 5530 STRUCTURE DHAV DHC8 DHC8202 2809007 NM VERTICAL STAB CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - LIGHT CORROSION BELOW VERTICAL STABILIZER LEADING EDGE, RIGHT-HAND FASTENER HOL AT X813.823, Z335.5. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2001091000027 20010910 00027 NM 2001 9 10 QXEA0101322 1 20010803 A 5730 FLANGE DHAV DHC8 DHC8202 2809007 NM RT WING SKIN SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - SCRATCHES ON TOP SURFACE OF RIGHT WING LEADING EDGE FLANGE AT YW230. REPAIRED IAW DHC-8 SRM 51-20-16, SRM 51-20-26 AND RD 8-57-1675. 2 H 7 2 4T RT A13NM 2001091000028 20010910 00028 NM 2001 9 10 QXEA0101323 1 20010803 A 5210 SKIN DHAV DHC8 DHC8202 2809007 NM PAX DOOR SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - MAIN CABIN DOOR SHELL FORWARD EDGE KNICKED, 18" FROM OUTBORD END. REPAIRED IAW DHC-8 SRM 51-20-11 AND SRM 51-20-51 . 2 H 7 2 4T RT A13NM 2001091000029 20010910 00029 EU 2001 9 10 QXEA0101324 1 20010808 A 3350 LIGHT FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 482US 11231 PDX - EVACUATION LIGHTS AT SEAT 8AB IS MISSING LENS COVER AND IS INOPERABLE. INSTALLED LENS COVER AND AND RECONNECTED W IRE AS REQUIRED. OPERATIONAL CHECK IS GOOD. 2 L 7 2 4F RT A20EU 2001091000030 20010910 00030 EU 2001 9 10 QXEA0101325 1 20010809 A 3350 6008903 BATTERY PACK FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 475AU 8402 1131 11222 PDX - FORWARD LEFT HAND AND RIGHT HAND LOWER FAIRING EMERGENCY LIGHTS DID NOT ILLUMINATE. REPLACED BATTERY POWER SUPPLY FOR THE FORWARD LEFT HAND AND RIGHT HAND LOWER FAIRING EMERGENCY LIGHTS. OPERATIONAL CHECK IS GOOD. 2 L 7 2 4F RT A20EU 2001091000031 20010910 00031 EU 2001 9 10 QXEA0101326 1 20010808 A 3350 6008903 BATTERY PACK FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 488US 11064 2312 11240 PDX - AFT LEFT HAND AND RIGHT HAND LOWER FAIRING EMERGENCY LIGHTS DID NOT ILLUMINATE. REMOVED AND REPLACED THE AFT CARG O BAY EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001091000032 20010910 00032 NM 2001 9 10 QXEA0101327 1 20010807 A 5730 SKIN DHAV DHC8 DHC8202 2809007 NM WING TOOL DAMAGE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX-TOOL MARKS AROUND FASTENER HOLE ON TRAILING EDGE OF PANEL 624AT 14 INCHES FROM INBOARD AFT CORNER. REPAIRED IAW DHC- 8 SRM 51-20-16, SRM 51-20-36, SRM 51-20-26, AND HORIZON AIR EA 2-57-129. 2 H 7 2 4T RT A13NM 2001091000033 20010910 00033 NM 2001 9 10 QXEA0101328 1 20010807 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX-LEFT HAND WING TOP INBOARD FLAP TRACK NEXT TO FUSELAGE HAS EDGE CHAFING. REPAIRED IAW HORIZON AIR EA 2-57-128. 2 H 7 2 4T RT A13NM 2001091000034 20010910 00034 NM 2001 9 10 QXEA0101329 1 20010808 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - TOP CAP OF FRAME IS CHAFED AT STATION X222.000 WHERE LAVATORY SITS. REPAIRED IAW HORIZON AIR EA 2-53-321. 2 H 7 2 4T RT A13NM 2001091000035 20010910 00035 NM 2001 9 10 QXEA0101330 1 20010802 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION AND RAISED METAL AT STATION 265 TO 268. REPAIRED IAW DHC-8 RD 8 -53-1342, SRM 51-20-16 AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2001091000036 20010910 00036 NM 2001 9 10 QXEA0101331 1 20010808 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - DENT 0.37 INCH DEEP X 1.350: HIGH X 1.050 WIDE IN LEFT-HAND OUTER FUSELAGE SKIN UNDER LEFT-HAND ICE SHIELD AT STAT ION X298.4, Z163 AND EDGE OF STRINGER 10L. REPAIRED IAW HORIZON AIR EA 2-53-322. 2 H 7 2 4T RT A13NM 2001091000037 20010910 00037 NM 2001 9 10 QXEA0101332 1 20010808 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - DENT .043 INCH DEEP X 1.00 INCH HIGH X 1.15 INCH WIDE IN LEFT-HAND OUTER FUSELAGE SKIN UNDER LEFT-HAND ICE SHIELD AT STATION X305.5, Z176.5 AND EDGE OF STRINGER 6L. REPAIRED IAW HORIZON AIR EA 2-53-322. 2 H 7 2 4T RT A13NM 2001091000038 20010910 00038 NM 2001 9 10 QXEA0101333 1 20010806 A 5410 STRUCTURE DHAV DHC8 DHC8202 2809007 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - LEFT-HAND NACELLE DECK IS CRACKED AT STATION XN249.00. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001091000039 20010910 00039 NM 2001 9 10 QXEA0101334 1 20010807 A 5413 STRINGER DHAV DHC8 DHC8202 2809007 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - LEFT-HAND NACELLE DECK STRINGER CRACKED AT STATION XN258.00. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2001091000040 20010910 00040 NM 2001 9 10 QXEA0101335 1 20010803 A 5400 STRINGER DHAV DHC8 DHC8202 2809007 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - LEFT-HAND NACELLE DECK STRINGER CRACKED IN TWO PLACES AT STATION XN264.5. REPAIRED IAW HORIZON AIR EA 2-54-95. 2 H 7 2 4T RT A13NM 2001091000041 20010910 00041 NM 2001 9 10 QXEA0101336 1 20010807 A 5413 STRINGER DHAV DHC8 DHC8202 2809007 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - LEFT-HAND NACELLE DECK STRINGER CRACKED AT STATION XN272.00. REPAIRED IAW HORIZON AIR EA 2-54-95, DHC-8 SRM 51-20- 16 AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2001091000042 20010910 00042 NM 2001 9 10 QXEA0101337 1 20010807 A 5413 STRINGER DHAV DHC8 DHC8202 2809007 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - LEFT-HAND NACELLE DECK LOWER SURFACE STRINGER IS CRACKED AT STATION XN258.00. REPAIRED IAW HORIZON AIR EA 2-54-93, DHC-8 SRM 51-20-16 AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2001091000043 20010910 00043 NM 2001 9 10 QXEA0101338 1 20010807 A 5413 STRINGER DHAV DHC8 DHC8202 2809007 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - LEFT-HAND NACELLE DECK LOWER SURFACE STRINGER IS CRACKED AT STATION XN247.00. REPAIRED IAW HORIZON AIR EA 2-54-95, DHC-8 SRM 51-20-16 AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2001091000044 20010910 00044 NM 2001 9 10 QXEA0101339 1 20010807 A 5413 STRINGER DHAV DHC8 DHC8202 2809007 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - LEFT-HAND NACELLE DECK LOWER SURFACE STRINGER IS CRACKED AT STATION XN247.00. REPAIRED IAW HORIZON AIR EA 2-54-95 AND DHC-8 SRM 51-20-16 AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2001091000045 20010910 00045 NM 2001 9 10 QXEA0101340 1 20010807 A 5413 STRINGER DHAV DHC8 DHC8202 2809007 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - LEFT-HAND NACELLE DECK LOWER SURFACE STRINGER IS CRACKED AT STATION XN258.00. REPAIRED IAW HORIZON AIR EA 2-54-94, DHC-8 SRM 51-20-16 AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2001091000046 20010910 00046 NM 2001 9 10 QXEA0101341 1 20010807 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - AIRCRAFT SURFACE UNDER BOTTOM TCAS ANTENNA NEEDS TO BLEANED DUE TO CORROSION. REPAIRED IAW HORIZON AIR EA 2-53-320 , DHC-8 SRM 51-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001091000047 20010910 00047 NM 2001 9 10 QXEA0101342 1 20010810 A 2700 3985001003 CONTROL UNIT DHAV DHC8 DHC8* NM FLIGHT CONTROL MALFUNCTIONED A QXEA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 NM 09 400QX 1082 4030 GEG - VIBRATION LEFT SIDE OF FUSELAGE. PITCH TRIM FAIL. REMOVED AND REPLACED FLIGHT CONTROL ELECTRONIC CONTROL UNIT. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091000048 20010910 00048 NM 2001 9 10 QXEA0101343 1 20010811 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 9888 484 SEA - AFT RIGHT HAND AND LEFT HAND EMERGENCY EXIT LIGHTS AND RIGHT EGRESS LIGHT INOPERABLE. REMOVED AND REPLACED EMERGE NCY POWER SUPPLY 3351-P5-4. PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTS IAW-8 MAINTENANCE MANUAL 33-51-01, PAGES 50 1-503. AIRCRAFT RETURNED TO SERVCICE. 2 H 7 2 4T RT A13NM 2001091000049 20010910 00049 NM 2001 9 10 QXEA0101344 1 20010811 A 2120 ODOR DHAV DHC8 DHC8202 2809007 NM CABIN DETECTED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 09 354PH 498 SEA - FIRST TWO ROWS OF PASSENGERS, AND FLIGHT ATTENDANT, SMELLED AN ODOR OF "BURNING ELECTRICAL" ON DESCENT INTO SEATTL E. NO SMOKE PRESENT. GROUND RAN BOTH ENGINES WITH BLEEDS ON. INSPECTED THOROUGHLY FOR SOURCE OF REPORTED SMELL/ODOR. COULD NOT DUPLICATE. NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091000050 20010910 00050 NM 2001 9 10 QXEA0101345 1 20010811 A 5414 SKIN DHAV DHC8 DHC8202 2809007 NM NR 1 NACELLE MISSING A QXEA O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 NM 09 358PH 506 PDX - NUMBER ONE ENGINE NACELLE HAS SKIN MISSING ON LOWER NACELLE, OUTBOARD, JUST AFT OF LOWER COWL. INSTALLED REPAIR D OUBLER AND FILLER AND PAINTED, IAW DASH 8 RD8-54-063 2 H 7 2 4T RT A13NM 2001091000051 20010910 00051 NM 2001 9 10 QXEA0101346 1 20010813 A 3260 UPLOCK SENSOR DHAV DHC8 DHC8* NM MLG OUT OF ADJ A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 401QX 4031 SEA - ALL GEAR DOORS CYCLED DURING MODERATE TURBULANCE AND RIGHT MAIN LANDING GEAR WENT UNSAFE. ADJUSTED RIGHT MAIN LAN DING GEAR UPLOCK SENSOR. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091000052 20010910 00052 EU 2001 9 10 QXEA0101348 1 20010814 A 5415 ANGLE FOKKER F28 F28MK4000 4990810 EU NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PDX - CRACK IN ANGLE ATTACHED TO FRAME 2948, ADJACENT TO FIREWALL, AND AT THE TOP OF THE STUB WING. REPAIRED IAW THE F- 28 STRUCTURAL REPAIR MANUAL 54-02-02, PAGES 12 AND 13, FIGURE 7. 2 L 7 2 4F RT A20EU 2001091000053 20010910 00053 NM 2001 9 10 QXEA0101349 1 20010813 A 5310 STRUCTURE DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX-TWO INCH DENT AT STATION 700.409 LEFT HAND SIDE, TAIL. FABRICATED AND INSTALLED DOUBLER REPAIR IAW THE DASH 8 STRUC TURAL REPAIR MANUAL 53-30-24, FIGURE 1, SHEET 2. 2 H 7 2 4T RT A13NM 2001091000054 20010910 00054 NM 2001 9 10 QXEA0101350 1 20010809 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - PITTING ON THE TOPSIDE OF THE LOWER TRACK ON THE RIGHT-HAND NR 3 FLAP TRACK. REPAIRED IAW DHC-8 RD 8-57-987. 2 H 7 2 4T RT A13NM 2001091000055 20010910 00055 NM 2001 9 10 QXEA0101351 1 20010810 A 5410 STRUCTURE DHAV DHC8 DHC8202 2809007 NM RT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - RIGHT NACELLE FINGNAIL ATTACHMENT TAP CRACKED AT NUPLATE RIVET, INBOARD OF STATION XN236.20. REPAIRED IAW DHC-8 RD 8-54-163. 2 H 7 2 4T RT A13NM 2001091000056 20010910 00056 NM 2001 9 10 QXEA0101352 1 20010809 A 5414 PANEL DHAV DHC8 DHC8202 2809007 NM NR 1 NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - NR 1 NACELLE PANEL 414AR IS CHAFED APPROXIMATELY .014 INCH DEEP. REPAIRED IAW HORIZON AIR EA 2-71-157. 2 H 7 2 4T RT A13NM 2001091000057 20010910 00057 NM 2001 9 10 QXEA0101353 1 20010808 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - DENT .067 INCH DEEP X 1.70 INCH HIGH X 1.60 INCH WIDE IN LEFT-HAND OUTER FUSELAGE SKIN UNDER LEFT-HAND ICE SHIELD. REPAIRED IAW HORIZON AIR EA 2-53-322. 2 H 7 2 4T RT A13NM 2001091000058 20010910 00058 NM 2001 9 10 QXEA0101354 1 20010816 A 5230 DOOR DHAV DHC8 DHC8* NM CARGO BAY OPEN A QXEA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CR CRUISE 1 NM 09 404QX 4046 GEG - ON FLIGHT FROM SEA TO BTM DIVERTED TO GEG FOR RIGHT FORWARD FUSELAGE CARGO DOOR WARNING LIGHT IN FLIGHT. FOUND RIG HT FORWARD CARGO DOOR NOT PROPERLY CLOSED AND MANY BAGS UP AGAINST DOOR. MOVED BAGS TO AFT PIT. DOOR WIRE HARNESS OK. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091000059 20010910 00059 NM 2001 9 10 QXEA0101355 1 20010811 A 5414 SKIN DHAV DHC8 DHC8102 2809003 NM NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 826PH 214 PDX - SEVERAL CRACKS IN AFT CONNECTION ANGLE FOR HORSE COLLAR TO UPPER SKIN AT TOP CENTER OF HORSE COLLAR STRUCTURE (MAR KED). REPAIRED IAW EA 9-54-306. 2 H 7 2 4T RT A13NM 2001091000060 20010910 00060 EU 2001 9 10 QXEA0101356 1 20010817 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 475AU 11222 PDX - EMERGENCY EXIT SIGN OVER COCKPIT DOOR DOES NOT ILLUMINATE IN EMERGENCY. REMOVED AND REPLACED EXIT SIGN ASSEMBLY. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001091000061 20010910 00061 EU 2001 9 10 QXEA0101357 1 20010820 A 3350 LIGHT FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 494US 11167 SEA - EMERGENCY EGRESS LIGHT INOPERABLE AT ROW 3B. REPLACED BUTT SPLICE. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001091000062 20010910 00062 NM 2001 9 10 QXEA0101358 1 20010806 A 2120 ODOR DHAV DHC8 DHC8202 2809007 NM CABIN AIR DETECTED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 NM 09 356PH 502 BOI - ODOR COMING FROM BLEED AIR SMELLS LIKE SKUNK OR BURNED OIL. MOST NOTICEABLE WHEN BLEED FLOW IS TURNED ON AFTER TA KE OFF, THEN DISSIPATES. STARTED AND GROUND RAN NR 1 AND NR 2 ENGINES AT LOW POWER SETTINGS. NO OIL SMELL OR DEFECTS N OTED. AIRCRAFT OKAY FOR CONTINUED SERVICE. 2 H 7 2 4T RT A13NM 2001091000063 20010910 00063 EU 2001 9 10 QXEA0101359 1 20010819 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 GEG - ROW EIGHT EMERGENCY EXIT SIGNS HAVE INOPERABLE BULBS. REMOVED AND REPLACED CIRCUIT BOARDS. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001091000064 20010910 00064 NM 2001 9 10 QXEA0101360 1 20010818 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX-SEAT TRACK NR 1 CORRODED ON TOP INBOARD AND OUTBOARD AT STATION 275. REPAIRED IAW DHC-8 RD8-53-1342, SRM 51-20-16 AN D SRM 51-20-41. 2 H 7 2 4T RT A13NM 2001091000065 20010910 00065 NM 2001 9 10 QXEA0101361 1 20010818 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX-SEAT TRACK NR 1 CORRODED ON TOP INBOARD AT STATION 282. REPAIRED IAW DHC-8 RD8-53-1342, SRM 51-20-16 AND SRM 51-20-4 1. 2 H 7 2 4T RT A13NM 2001091000066 20010910 00066 NM 2001 9 10 QXEA0101362 1 20010818 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX-SEAT TRACK NR 1 CORRODED ON TOP INBOARD AT STATION 328. REPAIRED IAW DHC-8 RD8-53-1342, SRM 51-20-16 AND SRM 51-20-4 1. 2 H 7 2 4T RT A13NM 2001091000067 20010910 00067 NM 2001 9 10 QXEA0101363 1 20010818 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX-SEAT TRACK NR 1 CORRODED ON TOP INBOARD AT STATION 361. REPAIRED IAW DHC-8 RD8-53-1342, SRM 51-20-16 AND SRM 51-20-4 1. 2 H 7 2 4T RT A13NM 2001091000068 20010910 00068 NM 2001 9 10 QXEA0101364 1 20010818 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX-SEAT TRACK NR 1 CORRODED ON TOP INBOARD AND OUTBOARD AT STATION 392. REPAIRED IAW DHC-8 RD8-53-1342, SRM 51-20-16 A ND SRM 51-20-41. 2 H 7 2 4T RT A13NM 2001091000069 20010910 00069 NM 2001 9 10 QXEA0101365 1 20010818 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX-SEAT TRACK NR 1 CORRODED ON INSIDE CENTER AT STATION 407. REPAIRED IAW DHC-8 RD8-53-1342, SRM 51-20-16 AND SRM 51-20 -41. 2 H 7 2 4T RT A13NM 2001091000070 20010910 00070 NM 2001 9 10 QXEA0101366 1 20010818 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX-SEAT TRACK NR 1 CORRODED ON TOP INBOARD AT STATION 422. REPAIRED IAW DHC-8 RD8-53-1342, SRM 51-20-16 AND SRM 51-20-4 1. 2 H 7 2 4T RT A13NM 2001091000071 20010910 00071 NM 2001 9 10 QXEA0101367 1 20010818 A 5310 THRESHOLD DHAV DHC8 DHC8202 2809007 NM PAX DOORWAY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX-MAIN CABIN DOOR THRESHOLD HAS CORROSION AROUND NUTPLATES.REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001091000072 20010910 00072 NM 2001 9 10 QXEA0101368 1 20010818 A 5310 THRESHOLD DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX-MAIN CABIN DOOR THRESHOLD HAS CORROSION BETWEEN NUTPLATES AND STRUCTURE. REPAIRED IAW DHC-8 SRM 51-00-06, SRM 51-20- 11 AND SRM 53-00-16. 2 H 7 2 4T RT A13NM 2001091000073 20010910 00073 NM 2001 9 10 QXEA0101369 1 20010807 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX-AIRCRAFT SURFACE UNDER BOTTOM TCAS ANTENNA NEEDS TO BE CLEANED DUE TO CORROSION. REPAIRED IAW DHC-8 SRM 51-40-11 AND HORIZON AIR EA 2-53-320. 2 H 7 2 4T RT A13NM 2001091000074 20010910 00074 NM 2001 9 10 QXEA0101370 1 20010802 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX-PITTING CORROSION IN CENTER OF SEAT TRACK LEFT HAND INBOARD FORWARD OF STATION X545.0. REPAIRED IAW DHC-8 RD8-53-133 9, SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2001091000075 20010910 00075 NM 2001 9 10 QXEA0101371 1 20010802 A 5310 STRUCTURE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX-CORROSION UNDER AND ON NUTPLATES JUST ABOVE CABIN DOOR. REPAIRED IAW DHC-8 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2001091000076 20010910 00076 NM 2001 9 10 QXEA0101372 1 20010804 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX-CORROSION IN AND AROUND NUTPLATES ON LEFT HAND INBOARD SEAT TRACK AT STATION X182.0-X190.9. REPAIRED IAW DHC-8 SRM 5 1-00-06. 2 H 7 2 4T RT A13NM 2001091000077 20010910 00077 NM 2001 9 10 QXEA0101373 1 20010802 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX-RIGHT HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION AND RAISED METAL AT STATION X265-268. REPAIRED IAW DHC-8 RD8-53-1 342, SRM 51-20-16 AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2001091000078 20010910 00078 NM 2001 9 10 QXEA0101374 1 20010801 A 5310 DOOR FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX-DOPPLER ABOVE CARGO DOOR INCLOSURE IS CHAFED IN TWO SPOTS. REPAIRED IAW DHC-8 RD8-53-5461, SRM 51-00-06. 2 H 7 2 4T RT A13NM 2001091000079 20010910 00079 EU 2001 9 10 QXEA0101375 1 20010819 A 3350 55159004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 498US 11181 BOI - FORWARD CABIN EXIT SIGN HAS BULBS BURNED OUT. REPLACED EXIT SIGN CIRCUIT BOARD IAW F-28 MAINTENANCE MANUAL, 33-50- 00, PAGE 412 AND 413. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001091000080 20010910 00080 NM 2001 9 10 USAASB01221 1 20010804 A 2700 189929 SENSOR BOEING 737 7373B7 1384580 NM A USAA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CR CRUISE 1 EA 19 384US 22957 PIT - FLT 283 - EN ROUTE FROM PHL-PIT, AT FL200 AND 300 KNOTS, THE CAPTAIN REPORTED THE NR 3 AND NR 4 LEADING EDGE DEVIC ES HAD DEPLOYED IN FLIGHT WITH FLAP HANDLE IN UP POSITION. THIS CAUSED A SLIGHT ROLL IN THE AIRCRAFT. CREW DECLARED AN EMERGENCY AND SLOWED THE AIRCRAFT TO 230 KNOTS TO DEAL WITH THE PROBLEM. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PR OCEDURES AND LANDED WITH FLAPS AT 15 UNITS. FLIGHT LANDED WITHOUT INCDIENT AT PIT AND EMERGENCY EQUIPMENT FOLLOWED THE AIRCRAFT TO THE GATE. CREW REPORTED THAT WITH FLAPS AT 15 UNITS AND 230 KNOTS THE NR 3 AND NR 4 LEADING EDGE DEVICES CY CLED INTERMITTENTLY. MX ACCOMPLISHED UNCOMMANDED LEADING EDGE EXTENSION TEST. FOUND A HIGH RESISTANCE ON THE NR 4 LEAD 2 L 7 2 4F RT A16WE 2001091000081 20010910 00081 NM 2001 9 10 USAASB01231 1 20010814 A 3350 20131A BATTERY PACK BOEING 737 737401 1384701 NM AFT CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 CLT - MAINTENANCE FOUND THE AFT SECTION OF CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EME RGENCY LIGHT BATTERY PACK. ALL EMERGENCY LIGHTS OPERATIONALLY CHECKED GOOD. (M) 2 L 7 2 4F RT A16WE 2001091000082 20010910 00082 NM 2001 9 10 USAA011060 1 20010813 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND TOP SURFACE OF T-CAP CORRODED, BS 947 RBL 22 THROUGH LBL 9. REPLACED T-CAP, INSTALLED PER EA 85177. (M) 2 L 7 2 4F A16WE 2001091000083 20010910 00083 NM 2001 9 10 USAA011050 1 20010809 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 70 INCHES, BS 986.5 RBL 40 TO LBL 30. REPLACED T-CAP PER SRM 53-10-9. (M) 2 L 7 2 4F A16WE 2001091000084 20010910 00084 NM 2001 9 10 USAA011048 1 20010809 A 5300 FLOOR SUPPORT BOEING 737 737201 1384454 NM BS 986.5-S1006 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND FLOOR SUPPORT CORRODED 1 INCH, BS 986.5 TO S 1006 BL 0 FLOOR LEVEL. REPLACED FLOOR SUPPORT PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2001091000085 20010910 00085 NM 2001 9 10 USAA011029 1 20010807 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 47570 22756 CLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 3.5 INCHES, BS 294.5 LBL 1.5 TO RBL 1.5. CORROSION LEVEL 1, TASK NR C53-107- 01. UPPER T-CHORD REPAIRED PER TR 53-10-04 B. (M) 2 L 7 2 4F A16WE 2001091000086 20010910 00086 NM 2001 9 10 USAA011044 1 20010808 A 5300 ANGLE BOEING 737 737201 1384454 NM BS 303 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND ANGLE CORRODED 1 INCH BY 27 INCHES, BS 303 TO RBL 55. CORROSION LEVEL 1, TASK NR C53-107-02. REMOVED AND R EPLACED WITH PART NR 1123138 PER SRM 50-10-1. (M) 2 L 7 2 4F A16WE 2001091000087 20010910 00087 NM 2001 9 10 USAA011023 1 20010807 A 5300 WEB BOEING 737 737201 1384454 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 22961 CLT - FOUND WEB CRACKED .125 INCH, BS 178 BULKHEAD AT WL 234 AT LBL 10. INSTALLED EXTERNAL DOUBLER PER SRM 53-10-11 FIG 1. (M) 2 L 7 2 4F A16WE 2001091000088 20010910 00088 NM 2001 9 10 USAA011024 1 20010807 A 5300 CLIP BOEING 737 737201 1384454 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47520 22961 CLT - FOUND CLIP CRACKED 1 INCH, BS 520 STRINGER 19L. REMOVED AND REPLACED CLIP PER SRM 51-10-02. (M) 2 L 7 2 4F A16WE 2001091000089 20010910 00089 NM 2001 9 10 USAA011025 1 20010807 A 5310 TIE CLIP BOEING 737 737201 1384454 NM BS 706 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 22961 CLT - FOUND TIE CLIP CRACKED .250 INCH, BS 706 STRINGER 10L. REMOVED AND REPLACED TIE CLIP PER PCI JOB CARD J253-10-10R . (M) 2 L 7 2 4F A16WE 2001091000090 20010910 00090 NM 2001 9 10 USAA011030 1 20010807 A 5300 TIE CLIP BOEING 737 737201 1384454 NM BS 685 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND TIE CLIP CRACKED .125 INCH, BS 685 S2L. REMOVED AND REPLACED TIE CLIP PER EO 5393L-227. (M) 2 L 7 2 4F A16WE 2001091000091 20010910 00091 NM 2001 9 10 USAA011031 1 20010807 A 5300 TIE CLIP BOEING 737 737201 1384454 NM BS 597 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND TIE CLIP CRACKED .125 INCH, BS 597 S9L. REMOVED AND REPLACED THE TIE CLIP CCN 1122006 PER SRM 737-200 51-30 -2. (M) 2 L 7 2 4F A16WE 2001091000092 20010910 00092 NM 2001 9 10 USAA011032 1 20010807 A 5300 TIE CLIP BOEING 737 737201 1384454 NM BS 706 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND TIE CLIP CRACKED .125 INCH, BS 706 S2L. REMOVED AND REPLACED TIE CLIP PER EO 5393G-227. (M) 2 L 7 2 4F A16WE 2001091000093 20010910 00093 NM 2001 9 10 USAA011033 1 20010807 A 5300 FRAME BOEING 737 737201 1384454 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47520 22961 CLT - FOUND FRAME CRACKED .25 INCH, BS 747, STRINGER 13L. REMOVED DAMAGED AREA, INSTALLED CHANNEL AND FILLER PER SRM 53 -10-4. (M) 2 L 7 2 4F A16WE 2001091000094 20010910 00094 NM 2001 9 10 USAA011034 1 20010807 A 5300 FRAME BOEING 737 737201 1384454 NM BS 807 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47520 22961 CLT - FOUND FRAME CRACKED .5 INCH, BS 807, S13L. REMOVED DAMAGE, INSTALLED CHANNEL AND FILLER PER SRM 53-10-4. (M) 2 L 7 2 4F A16WE 2001091000095 20010910 00095 NM 2001 9 10 USAA011035 1 20010807 A 5310 FRAME BOEING 737 737201 1384454 NM BS 767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47520 22961 CLT - FOUND FRAME CRACKED .5 INCH, BS 767 AT S13L. REMOVED DAMAGE, INSTALL CHANNEL AND FILLER PER SRM 53-10-4. (M) 2 L 7 2 4F A16WE 2001091000096 20010910 00096 NM 2001 9 10 USAA011036 1 20010807 A 5310 SUPPORT FITTING BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47520 22961 CLT - FOUND SUPPORT FITTING CRACKED 5 INCHES, BS 727 BL 0 WL 203. REMOVED AND REPLACED SUPPORT FITTING PER EO 5394G176. (M) 2 L 7 2 4F A16WE 2001091000097 20010910 00097 NM 2001 9 10 USAA011037 1 20010807 A 5300 FRAME BOEING 737 737201 1384454 NM BS 1006 GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 22961 CLT - FOUND FRAME GOUGED AND DENTED .040 INCH, BS 1006 LBL 41 WL 207. FASTENER INSTALLED PER SRM 53-10-1 FIG 1 SRM 51-3 0-02. (M) 2 L 7 2 4F A16WE 2001091000098 20010910 00098 NM 2001 9 10 USAA011038 1 20010807 A 5310 TIE CLIP BOEING 737 737201 1384454 NM BS 727A GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47520 22961 CLT - FOUND TIE CLIP GOUGED .5 INCH, BS 727A AT 518R. INSTALLED NEW TIE CLIP PER SRM 51-10-101. (M) 2 L 7 2 4F A16WE 2001091000099 20010910 00099 NM 2001 9 10 USAA011040 1 20010808 A 5300 ANGLE BOEING 737 737201 1384454 NM BS 290 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47520 22961 CLT - FOUND ANGLE WITH TWO CRACKS .750 INCH EACH, STR 11R AND STR 13R, BS 290. INSTALLED NEW ANGLE PER SRM 51-30-2 AND 51-10-1. (M) 2 L 7 2 4F A16WE 2001091000100 20010910 00100 NM 2001 9 10 USAA011041 1 20010808 A 5300 WEB BOEING 737 737201 1384454 NM BS 328 GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND WEB GOUGED .750 INCH, RBL 60 BS 328 BETWEEN BS 17R AND 18R. INSTALLED WEB REPAIR, FILLER SHIM, AND REPAIR P LATE PER SRM 51-40-2 FIG 1, AND SRM 51-30-3, 5300V153. (M) 2 L 7 2 4F A16WE 2001091000101 20010910 00101 NM 2001 9 10 USAA011046 1 20010809 A 5300 TIE CLIP BOEING 737 737201 1384454 NM BS 706 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47520 22961 CLT - FOUND TIE CLIP CRACKED .125 INCH, BS 706 S3L. REPLACED WITH MOD CLIP PER EO 5393G227. (M) 2 L 7 2 4F A16WE 2001091000102 20010910 00102 NM 2001 9 10 USAA011047 1 20010809 A 5300 STRINGER BOEING 737 737201 1384454 NM BS 787/807 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND STRINGER WITH 1.5 INCH INDENTIONS CAUSED BY DRILLING TOO DEEP, ON STRINGER 16R CHANNEL LEG BETWEEN BS 787 AN D 807. INSTALLED FILLER AND CHANNEL DOUBLER PER SRM 53-10-3 DETAIL V REPAIR. (M) 2 L 7 2 4F A16WE 2001091000103 20010910 00103 NM 2001 9 10 USAA011054 1 20010810 A 5300 SKIN BOEING 737 737201 1384454 NM BS 827 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND SKIN DENTED 2 INCHES BY 8 INCHES BY .250 INCH, BS 827 STRINGER 27L. PREVIOUS REPAIR, FOUND AT S27L, REPORT STATES S27R, PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 2001091000104 20010910 00104 NM 2001 9 10 USAA011055 1 20010813 A 5300 FRAME BOEING 737 737201 1384454 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND FRAME CRACKED .250 INCH, BS 380 STRINGER 26L. FABRICATED REPLACEMENT PART PER SRM 53-10-04. (M) 2 L 7 2 4F A16WE 2001091000105 20010910 00105 NM 2001 9 10 USAA011057 1 20010813 A 5300 STRINGER BOEING 737 737201 1384454 NM BS 359 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND STRINGER CRACKED .5 INCH, BS 359 S14L. REMOVED AND REPLACED WITH PART NR 1131272 PER SRM 51-10-01. (M) 2 L 7 2 4F A16WE 2001091000106 20010910 00106 NM 2001 9 10 USAA011058 1 20010813 A 5300 FRAME BOEING 737 737201 1384454 NM BS 827 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND FRAME DENTED .25 INCH, BS 827 AT S24L UPPER CHORD. INSTALLED FRAME DOUBLER PER SRM 53-10-4. (M) 2 L 7 2 4F A16WE 2001091000107 20010910 00107 NM 2001 9 10 USAA011059 1 20010813 A 5300 WEB BOEING 737 737201 1384454 NM CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND WEB CRACKED TWO PLACES .060 INCH, BULKHEAD WEB AT ATTACH TO 1016 Y CHORD. INSTALLED DOUBLER PER SRM 53-10-4 AND SRM 51-30-5. (M) 2 L 7 2 4F A16WE 2001091000108 20010910 00108 NM 2001 9 10 USAA01061 1 20010813 A 5300 INTERCOSTAL BOEING 737 737201 1384454 NM BS 300.5-301.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47520 22961 CLT - FOUND INTERCOSTAL CRACKED .75 INCH, BS 300.5 TO BS 301.5 S10L. INSTALLED NEW ANGLE PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2001091000109 20010910 00109 NM 2001 9 10 USAA011026 1 20010807 A 5300 WEB BOEING 737 737201 1384454 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 47570 22756 CLT - FOUND WEB CRACKED .125 INCH, BS 178 BULKHEAD AT WL 234 AT RBL 10. INSTALLED DOUBLER PER SRM 53-10-11 FIG 1, 53-10 -1. (M) 2 L 7 2 4F A16WE 2001091000110 20010910 00110 NM 2001 9 10 USAA011027 1 20010807 A 5300 CREASE BEAM BOEING 737 737201 1384454 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 47570 22756 CLT - FOUND CREASE BEAM CRACKED .750 INCH, BS 520 LBL 64. EXTRUDED SECTION REPAIR, SPLICE REPLACEMENT PER SRM 51-40-4 F IG 1. (M) 2 L 7 2 4F A16WE 2001091000111 20010910 00111 NM 2001 9 10 QXEA0101376 1 20010822 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 824PH 157 PDX - ONE LAMP INOPERABLE ON FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING, AT ROW ONE. RESPLICED ENVIRONMENTAL SPLICES AND REATTACHED LIGHT SOCKET. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091000112 20010910 00112 NM 2001 9 10 QXEA0101377 1 20010824 A 5542 CAP DHAV DHC8 DHC8* NM RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 PDX - CRACK ON RUDDER TOP CAP. REMOVED TOP CAP. FABRICATED NEW TOP CAM FROM 2024T3 .040 AND INSTALLED IAW E.A. # 6-55-02 2 H 7 2 4T RT A13NM 2001091000113 20010910 00113 EU 2001 9 10 QXEA0101378 1 20010819 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 497US 11173 PDX - NUMBER 3 EMERGENCY EXIT LIGHT IS BURNED OUT. REMOVED AND REPLACED EXIT LIGHT PANEL IAW F-28 MAINTENANCE MANUAL CH APTER 33-24-00 PAGE 205-206, SECTION 6, PARAGRAPH A AND B. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001091000114 20010910 00114 EU 2001 9 10 QXEA0101379 1 20010827 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481US 11230 BOI - EXIT SIGN AT CABIN ENTRANCE HAS BURNED OUT BULBS. REPLACED EXIT SIGN IAW F-28 MAINTENANCE MANUAL 33-50-00, PAGES 4 12-413. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001091000115 20010910 00115 EU 2001 9 10 QXEA0101380 1 20010822 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 496US 11169 SEA - EXIT SIGN ABOVE GALLEY HAS INOPERABLE BULBS. REPLACED EXIT SIGN LAMP BOARD. OPERATIONAL CHECK IS GOOD. AIRCRAFT RE TURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001091000116 20010910 00116 NM 2001 9 10 QXEA0101382 1 20010822 A 5330 DOUBLER DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX - DOUBLER AT FRAME X264.100 AND STRINGER 11 RT CHAFED. REPAIRED IAW DHX-8 SRM 51-40-11 AND HORIZON AIR EA 2-53-329. 2 H 7 2 4T RT A13NM 2001091000117 20010910 00117 NM 2001 9 10 QXEA0101383 1 20010821 A 5730 PANEL DHAV DHC8 DHC8202 2809007 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX - PANEL 522AT HAS FRETTING CORROSION IN COUTERSUNK SCREW HOLES. REPAIRED IAW RD 8-57-1715. 2 H 7 2 4T RT A13NM 2001091000118 20010910 00118 NM 2001 9 10 QXEA0101384 1 20010820 A 5730 PANEL DHAV DHC8 DHC8202 2809007 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX - PANEL 261GT, AFT MATING FLANGE HAS FRETTING CORROSION. REPAIRED IAW RD 8-57-1441. 2 H 7 2 4T RT A13NM 2001091000119 20010910 00119 NM 2001 9 10 QXEA0101385 1 20010820 A 5730 PANEL DHAV DHC8 DHC8202 2809007 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX - PANEL 261JT, AFT MATING FLANGE HAS FRETTING CORROSION. REPAIRED IAW RD 8-57-1441. 2 H 7 2 4T RT A13NM 2001091000120 20010910 00120 NM 2001 9 10 QXEA0101386 1 20010820 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX - SEAT TRACK NR 2 CORRODED IN CENTER AT STATION 453. REPAIRED IAW DHC-8/200 SRM 51-20-41. 2 H 7 2 4T RT A13NM 2001091000121 20010910 00121 NM 2001 9 10 QXEA0101387 1 20010820 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX - SEAT TRACK NR 2 CORRODED ON TOP OUTBOARD AT STATION 451. REPAIRED IAW DHC8/200 SRM 51-20-41. 2 H 7 2 4T RT A13NM 2001091000122 20010910 00122 NM 2001 9 10 QXEA0101388 1 20010820 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX - SEAT TRACK NR 2 CORRODED ON TOP INBOARD AND OUTBOARD AT STATION 456. REPAIRED IAW DHC8/200 SRM 51-20-41. 2 H 7 2 4T RT A13NM 2001091000123 20010910 00123 NM 2001 9 10 QXEA0101389 1 20010820 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX - SEAT TRACK NR 2 CORRODED ON TOP OUTBOARD AT STATION 470. REPAIRED IAW DHC8/202 SRM 51-20-41. 2 H 7 2 4T RT A13NM 2001091000124 20010910 00124 NM 2001 9 10 QXEA0101390 1 20010820 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX - SEAT TRACK NR 2 CORRODED ON TOP INBOARD AND OUTBOARD AT STATION 491. REPAIRED IAW DHC8/202 SRM 51-20-41. 2 H 7 2 4T RT A13NM 2001091000125 20010910 00125 NM 2001 9 10 QXEA0101391 1 20010820 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX - SEAT TRACK NR 3 CHAFED ON TOP OUTBOARD AT STATION 519. REPAIRED IAW DHC8/202 SRM 51-20-16 AND SRM 51-20-41. 2 H 7 2 4T RT A13NM 2001091000126 20010910 00126 NM 2001 9 10 QXEA0101392 1 20010816 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX - SEAT TRACK NR 3 CHAFED ON TOP CENTER AT STATION 542. REPAIRED IAW DHC8/202 SRM 51-20-16 AND SRM 51-20-41. 2 H 7 2 4T RT A13NM 2001091000127 20010910 00127 NM 2001 9 10 QXEA0101393 1 20010820 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX - SEAT TRACK NR 10 CORRODED ON TOP INBOARD AND OUTBOARD AT STATION 391. REPAIRED IAW DHC8/202 SRM 51-20-16 AND SRM 5 1-20-41. 2 H 7 2 4T RT A13NM 2001091000128 20010910 00128 NM 2001 9 10 QXEA0101394 1 20010820 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX - SEAT TRACK NR 10 CORRODED IN TO CENTER AT STATION 370. REPAIRED IAW DHC8/202 SRM 51-20-16 AND SRM 51-20-41. 2 H 7 2 4T RT A13NM 2001091000129 20010910 00129 NM 2001 9 10 QXEA0101395 1 20010820 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX - SEAT TRACK NR 10 CORRODED TOP CENTER AT STATION 312. REPAIRED IAW DHC8/202 SRM 51-20-16 AND SRM 51-20-41. 2 H 7 2 4T RT A13NM 2001091000130 20010910 00130 NM 2001 9 10 QXEA0101396 1 20010820 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX - SEAT TRACK NR 10 CORRODED IN TOP CENTER AT STATION 280. REPAIRED IAW DHC8/202 SRM 51-20-16 AND SRM 51-20-41. 2 H 7 2 4T RT A13NM 2001091000131 20010910 00131 NM 2001 9 10 QXEA0101397 1 20010820 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX - SEAT TRACK NR 10 CORRODED ON TOP INBOARD AND OUTBOARD AT STATION 266. REPAIRED IAW DHC8/202 SRM 51-20-16 AND SRM 5 1-20-41. 2 H 7 2 4T RT A13NM 2001091000132 20010910 00132 NM 2001 9 10 QXEA0101398 1 20010816 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX - SEAT TRACK NR 8 CORRODED ON TOP INBOARD AND OUTBOARD AT STATION 518. REPAIRED IAW DHC8 RD 8-53-1339. 2 H 7 2 4T RT A13NM 2001091000133 20010910 00133 NM 2001 9 10 QXEA0101399 1 20010822 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX - SEAT TRACK NR 9 REQUIRES REPLACEMENT DUE TO SEVERAL OUT OF LIMIT WRITE UPS. REPLACED SEAT TRACK IAW DHC-8 SRM 51-4 0-00, SRM 51-40-11 AND RD 8-53-4472. 2 H 7 2 4T RT A13NM 2001091000134 20010910 00134 NM 2001 9 10 QXEA0101400 1 20010821 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX - NR 4 SEAT TRACK NEEDS TO BE REPLACED DUE TO SEVERE CORROSION. REPLACED SEAT TRACK IAW DHC8 RD 8-53-1102 RD 8-53-44 73 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001091000135 20010910 00135 NM 2001 9 10 QXEA0101401 1 20010821 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX - NR 7 SEAT TRACK REQUIRES REPLACEMENT DUE TO NUMEROUS CORROSION DISCREPANCIES. REPLACED SEAT TRACK IAW HORIZON AIR EA 2-53-325 AND DHC 8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001091000136 20010910 00136 NM 2001 9 10 QXEA0101402 1 20010824 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX - GOUGE IN OUTER SKIN OF CARGO DOOR. REPAIRED IAW DHC-8 SRM 51-40-00, SRM 51-40-11 AND HORIZON AIR EA 2-52-108. 2 H 7 2 4T RT A13NM 2001091000137 20010910 00137 NM 2001 9 10 QXEA0101403 1 20010816 A 5210 SKIN DHAV DHC8 DHC8202 2809007 NM PAX DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX - MAIN CABIN DOOR SHELL HAS FRETTING AROUND FASTENER HOLE FOR FORWARD UPPER CORNER OF AIRSTAIRS. REPAIRED IAW DHC8/2 00 SRM 51-20-16, PAGE 2, TABLE 1. 2 H 7 2 4T RT A13NM 2001091000138 20010910 00138 NM 2001 9 10 QXEA0101404 1 20010822 A 5315 FLOORBEAM DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX - CABIN FLOOR SUPPORT BEAM IS CHAFED BELOW GALLEY AT X242.2, Y9.5-14R. REPAIRED IAW HORIZON AIR EA 2-53-327. 2 H 7 2 4T RT A13NM 2001091000139 20010910 00139 NM 2001 9 10 QXEA0101405 1 20010822 A 5315 FLOORBEAM DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX - CABIN FLOOR SUPPORT BEAM IS CHAFED BELOW GALLEY AT X227.7, Y95-14R. REPAIRED IAW HORIZON AIR EA 2-53-328. 2 H 7 2 4T RT A13NM 2001091000140 20010910 00140 NM 2001 9 10 QXEA0101406 1 20010822 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX - NR 7 SEAT TRACK AFT SPLICE PIECES HAVE UNSERVICEABLE FASTENER HOLES. REPAIRED IAW DHC-8 RD 8-53-4473. 2 H 7 2 4T RT A13NM 2001091000141 20010910 00141 NM 2001 9 10 QXEA0101407 1 20010820 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX - NR 8 SEAT TRACK FORWARD SPLICE HAS UNSERVICEABLE FASTENER HOLES. REPAIRED IAW DHC-8 SRM 51-40-11, RD 8-52-1102 AND RD 8-53-4472. 2 H 7 2 4T RT A13NM 2001091000142 20010910 00142 NM 2001 9 10 QXEA0101408 1 20010824 A 5753 SKIN DHAV DHC8 DHC8202 2809007 NM TE FLAP CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX - LEFT-HAND OUTBOARD FLAP CRACKED AND SKIN DELAMINATED UNDER PREVIOUS REPAIR PATCH AT APPROXIMATELY STATION YW174.00 0. REPAIRED IAW HORIZON AIR EA 2-57-133. 2 H 7 2 4T RT A13NM 2001091000143 20010910 00143 NM 2001 9 10 QXEA0101409 1 20010824 A 5310 DOOR FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE TOOL DAMAGE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX - TOOL MARKS ON UPPER AFT CORNER OF AFT CARGO DOOR FRAME 597.0. APPROXIMATELY 6 INCHES DOWN FROM TOP OF DOOR. REPAIR ED IAW HORIZON AIR EA 2-52-108. 2 H 7 2 4T RT A13NM 2001091000144 20010910 00144 NM 2001 9 10 QXEA0101410 1 20010823 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE MISINSTALLED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 379PH 530 PDX - INCORRECT HARDWARE INSTALLED IN TOP FLANGE OF SPLICE BETWEEN SEAT TRACK NR 7 AND 8. REPAIRED IAW DHC-8 RD 8-53-447 3. 2 H 7 2 4T RT A13NM 2001091000145 20010910 00145 NM 2001 9 10 QXEA0101411 1 20010824 A 2710 7002260923 SERVO DHAV DHC8 DHC8102 2809003 NM AILERONS MALFUNCTIONED A QXEA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 09 827PH 20082 1844 275 PDR - AIRCRAFT HARD TO ROLL LEFT AND HARD TO RETURN WINGS LEVEL AT 200-220 KNOTS. REPLACED AUTO PILOT AILERON SERVO MOTO R. INSPECTED AILERONS AND SPOILER CONTROL, NO DISCREPANCIES NOTED. OPERATIONAL CHECK FLIGHT IS GOOD. AIRCRAFT RETURNED T O SERVICE. 2 H 7 2 4T RT A13NM 2001091000146 20010910 00146 EU 2001 9 10 QXEA0101412 1 20010824 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 PDX - EMERGENCY EXIT SIGN ABOVE THE FOREWARD GALLEY LINTEL HAS SEVERAL BULBS THAT DID NOT ILLUMINATE. REPLACED LIGHT CAR D ON EXIT SIGN ABOVE FORWARD GALLEY LINTEL. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001091000147 20010910 00147 EU 2001 9 10 QXEA0101413 1 20010826 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 480AU 11229 GEG - EXIT LIGHT ROW 8 INOPERABLE. REMOVED AND REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001091000148 20010910 00148 EU 2001 9 10 01FDEA00812 1 20010903 A 5400 PYLON AIRBUS 310 A310222 3930315 EU LOWER SPAR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 421FE 342 NR 100 CRACK ON RH PYLON LWR SPAR BETWEEN RIB 9 & 10. R&R PER EO 6-5450-7-3320B PART 6.` 2 L 7 2 4F RT A35EU 2001091000149 20010910 00149 EU 2001 9 10 01FDEA00813 1 20010903 A 5400 PYLON AIRBUS 310 A310222 3930315 EU LOWER SPAR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 421FE 342 NR 102 CRACK ON LH PYLON LWR SPAR BETWEEN RIB 9 & 10. R&R PER EO 6-5450-7-3302B PART 5. 2 L 7 2 4F RT A35EU 2001091000150 20010910 00150 EU 2001 9 10 01FDEA00814 1 20010903 A 5400 PYLON AIRBUS 310 A310222 3930315 EU LOWER SPAR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 421FE 342 NR 103 CRACK ON LH PYLON LWR SPAR BETWEEN RIB 6&7. R&R PER EO 6-5410-7-3000 A3 PART 3. 2 L 7 2 4F RT A35EU 2001091000151 20010910 00151 NM 2001 9 10 01FDEA00817 1 20010904 A 5744 RIB BOEING 727 727233 138408A NM LEFT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 280FE 22347 N 1494 LH WING L/E RIB CRACKED FOR ACTUATOR ROD END CUT-OUTS FOR #2 SLAT AT WS 640, WBL 540. R&R RIBS PER SRM 57-30-4. 2 L 7 3 4F RT A3WE 2001091000152 20010910 00152 NM 2001 9 10 01FDEA00819 1 20010904 A 5320 WEB BOEING 727 727233 138408A NM FUSELAGE TOP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 280FE 22347 N 1481 RH NOSE WHEEL WELL SHELF WEB CRACKED AT LIGHTNING HOLE BS 291, WL 156, RBL 18. R&R WEB PER SRM 51-20-1. 2 L 7 3 4F RT A3WE 2001102500259 20011025 00259 NM 2001 10 25 01FDEA00820 1 20011004 A 5311 FRAME BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 281FE 22348 MAIN CARGO 4 HOLES IN FRAME BS 700 R10. REMOVED AND REPLACED FRAME PER EA 7-5310-60521. 2 L 7 3 4F RT A3WE 2001091000153 20010910 00153 NM 2001 9 10 01FDEA00821 1 20010904 A 5414 SKIN PANEL BOEING 727 727233 138408A NM NACELLES/PYLONS CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 280FE 22347 N 925 UPR O/B SKIN PANEL CRACKED ON #3 PYLON BS 1203 AT WL 240. R&R PNL PER SRM 51-20-1. 2 L 7 3 4F RT A3WE 2001100900155 20011009 00155 NM 2001 10 9 01FDEA00822 1 20011005 A 2750 65249661 SUPPORT BOEING 727 727233 138408A NM SPOILER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 N 1137 L/W I/B SPOILER SUPPORT BEAM CRACKED OF I/B END. ** S/D ** COMING 2 L 7 3 4F RT A3WE 2001091000154 20010910 00154 NM 2001 9 10 QXEA0101414 1 20010824 A 3320 LIGHT DHAV DHC8 DHC8202 2809007 NM LAVATORY INTERMITTENT A QXEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 360PH 515 SEA - LAVATORY LIGHT IS INTERMITTENT WITH A SLIGHT SMELL OF BURNING ELECTRICAL WIRING. PULLED AND INSTALLED COLLAR ON CI RCUIT BREAKER TO LAVATORY LIGHT. REMOVED BULB FROM SOCKET ASSEMBLY, LOCKED AND PLACARDED LAVATORY DOOR. FOUND BROKEN PIN CONNECTOR. REPINNED THE CONNECTOR. OPERATIONAL CHECK IS GOOD. NO SMELL OF BURNING. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091000155 20010910 00155 WP 2001 9 10 0103119922 1 20010712 A 5311 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 945N 47664 DURING AN M1-CHECK IN ATL, STATION 579 FRAME REINFORCEMENT STRAPS 2800206-8 AND -9 WERE CUT FOR ACCESS AT LOCATION BETWE EN L-28 LT AND L-29 RT. ADDITIONAL DAMAGE WAS FOUND AT L-24 RT ON STRAP 2800206-8. THE EA 99-181344 (LOG PAGE 1640709) PROVIDES A SPLICE REPAIR AT TWO LOCATIONS. 2 L 7 2 4F A6WE 2001091000156 20010910 00156 WP 2001 9 10 0103129922 1 20010716 A 5310 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 945N 47664 DURING M-CHECK AT ATL AND WHILE ACCOMPLISHING A DOORJAMB PAN SPLICE REPAIR PER SRM 53-05, FIG 44, EIGHT .1875 INCH DIA H OLES WERE FOUND WITH SHORT ON-CENTER DISTANCE IN THE VERTICAL FLANGE OF FRAME STA 896 P/N 9958214-29 AS SHOWN IN FIGURE 1. THE FASTENER HOLES ARE FROM A PREVIOUS AFT CARGO DOORJAMB PAN SPLICE REPAIR AT LN27R SHOWN IN FIGURE 1. 2 L 7 2 4F A6WE 2001091000157 20010910 00157 NM 2001 9 10 QXEA0101415 1 20010822 A 2610 WARNING SYSTEM DHAV DHC8 DHC8202 2809007 NM COCKPIT FALSE ACTIVATION A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 359PH 514 RDM - ON TAXI INTO RDM, NR 2 FAULT B LIGHT ILLUMINATED. REMOVED AND REPLACED SWITCHING VALVE TO REAR INLET GATE SEALING AIR TUBE ASSEMBLY IAW 72-01-31, PAGE 411-415. COMPLIED WITH OPERATIONAL TEST OF ENGINE FIRE/OVERHEAT DETECTION SYSTEM. C HECK IS GOOD, AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091000158 20010910 00158 WP 2001 9 10 0103139922 1 20010718 A 5521 SPAR DOUG DC9 DC932 3022066 WP ELEVATOR DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 945N 47664 DURING AN M-CHECK SHOP VISIT AT ATL MAINTENANCE BASE WHILE REMOVING THE FRONT SPAR FOR REPLACEMENT, SEVERAL FASTENER HOL ES ON THE UPPER AND LOWER SKIN ASSEMBLY WERE FOUND TO BE DAMAGED (TOOLING DAMAGE). REPAIR TO DAMAGED SKIN ASSEMBLY WAS ACCOMPLISHED PER SECTION 1 AND 2 OF EA 99-181293 PG PAGE 1628105. 2 L 7 2 4F A6WE 2001091000159 20010910 00159 NM 2001 9 10 QXEA0101416 1 20010827 A 3350 362624 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 365PH 526 PDX - FLOOR TRACK LIGHTING AT ROW 8 IS INOPERABLE. REMOVED AND REPLACED TRACK LIGHT ASSEMBLY AT ROW 8. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091000160 20010910 00160 NM 2001 9 10 0103146308 1 20010830 A 2121 FAN BOEING 747 747451 1384940 NM CABIN MALFUNCTIONED A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 668US 24223 (PEK) DURING CRUISE, SMOKE EMITTED IN THE FLIGHT DECK. TURNED OFF ALL FANS AND SMOKE DISSIPATED. RESET LOWER RECIRCULA TION FAN AND LEFT THE UPPER RECIRCULATION FANS OFF. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. OPE RATIONAL CHECK OF ALL FANS WAS GOOD. SYSTEM IS ON DEFERRAL FOR PRECAUTIONARY REPLACEMENT OF THE RECIRCULATION FAN AND F ILTER. 2 L 7 4 4F RT A20WE 2001091000161 20010910 00161 NM 2001 9 10 QXEA0101418 1 20010827 A 3350 6104781 BATTERY DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 367PH 22185 238 511 PDX - LEFT HAND AFT EMERGENCY LIGHT INOPERABLE. REMOVED AND REPLACED PS3 EMERGENCY POWER SUPPLY BATTERY. OPERATIONAL CHE CK IS O.K. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091000162 20010910 00162 EU 2001 9 10 QXEA0101419 1 20010829 A 2612 2WB19042 FIRE LOOP FOKKER F28 F28MK4000 4990810 EU RROYCE SPEY SPEY55515P 54521 EU NR 2 ENGINE SHORTED A QXEA F E A ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 479AU 11228 9633 BIL - ENROUTE FROM BIL TO SEA THE NR 2 FIRE WARNING SOUNDED AND LIGHT UP. PERFORMED ENGINE FIRE CHECK LIST, SHUTING DOWN NR 2 ENGINE. AFTER PULLING THE FIRE CONTROL GUARD THE FIRE LIGHT WENT OUT. FIRED NR 2 FIRE BOTTLE. DIVERTED TO GEG AND LANDED WITHOUT INCIDENT. CHECKED NR 2 ENGINE FOR FIRE DAMAGE OR LEAKING FLUIDS. NON NOTED. REPLACED FIRE LOOP SECTION. O PERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A20EU E2EU 2001091000163 20010910 00163 WP 2001 9 10 0103151225 1 20010830 A 3222 TORQUE LINK DOUG DC10 DC1030 3023501 WP NLG DISCONNECTED A NWAA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 01 225NW 46582 ABORTED TAKEOFF AT 100 KNOTS DUE TO VIBRATION AND LOSS OF NOSE GEAR STEERING. FOUND NOSE LANDING GEAR TORQUE LINKS DISC ONNECTED. AIRCRAFT WAS TOWED TO THE GATE. FOUND CEILING PANELS DOWN, CENTER OVERHEAD BIN DAMAGED, AND E/E SHELVING DAM AGED. AFTER INSPECTION AND EVALUATION, AIRCRAFT MAINTENANCE FERRIED TO MSP FOR PERMANENT REPAIR. 2 L 7 3 4F A22WE 2001091000164 20010910 00164 NM 2001 9 10 QXEA0101420 1 20010827 A 5210 DOOR DHAV DHC8 DHC8* NM MAIN PAX STUCK A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 HLN - AFT PASSENGER DOOR WILL NOT OPEN. REPAIRED AND APPLIED FAST WELD TO DOOR STOP IAW EA 6-52-71. 2 H 7 2 4T RT A13NM 2001091000165 20010910 00165 NM 2001 9 10 QXEA0101421 1 20010831 A 5412 BULKHEAD DHAV DHC8 DHC8202 2809007 NM NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX - 1 INCH CRACK ON NACELLE BULKHEAD AT STATION XN125.5, ZN1.0, AND YW 143.0 (VIEWED LOOKING IN THROUGH 416AR). REPAIR ED DAMAGE IAW DASH-8 RD 8-54-611 2 H 7 2 4T RT A13NM 2001091000166 20010910 00166 WP 2001 9 10 0103161156 1 20010903 A 3610 DUCT DOUG DC10 DC1040 3023508 WP PNEUMATIC SYS BROKEN A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 156US 46765 ON CLIMBOUT AT MSP, NR 1 AND NR 2 MANIFOLD FAIL LIGHTS ILLUMINATED, ACCOMPANIED BY A LOUD BANG AFT OF NR 2 DOOR. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PNEUMATIC DUCT BROKEN AT FLANGE. REPLACED DUCT, OPERAT IONAL CHECK OK. 2 L 7 3 4F A22WE 2001091000167 20010910 00167 NM 2001 9 10 QXEA0101422 1 20010829 A 5412 BULKHEAD DHAV DHC8 DHC8202 2809007 NM NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX - 3/4 INCH CRACK ON CLOSING MEMBER 85410449. REMOVED DAMAGED ANGLE AND FABRICATED NEW ANGLE OUT OF .016 TITANIUM AND INSTALLED IAW E.A. 2-54-98 AND RD 8-54-611. 2 H 7 2 4T RT A13NM 2001091000168 20010910 00168 EU 2001 9 10 QXEA0101423 1 20010830 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478US 11227 GEG - FORWARD, MIDDLE, AND AFT EXIT SIGNS INOPERABLE. REMOVED AND REPLACED THE FORWARD, MIDDLE, AND AFT EXIT SIGNS. OPER ATIONAL CHECK IS GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001091000169 20010910 00169 NM 2001 9 10 0103176626 1 20010904 A 2530 SMOKE BOEING 747 747251B 1384892 NM GALLEY DETECTED A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 626US 21708 DURING CRUISE, NOTICED SMOKE BEHIND OVEN IN E-ZONE GALLEY. INSPECTED AND OPERATED OVENS AND PASSENGER ENTERTAINMENT EQU IPMENT. NO TROUBLE FOUND. ALL EQUIPMENT OPERATED NORMALLY AND NO EVIDENCE OF SMOKE. 2 L 7 4 4F A20WE 2001091000170 20010910 00170 NM 2001 9 10 QXEA0101424 1 20010831 A 3350 LENS DHAV DHC8 DHC8202 2809007 NM CABIN MISSING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 SEA-LENS MISSING FROM EMERGENCY LIGHT BY THE MAIN CABIN DOOR. REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK IS GOOD. AIRCRA FT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091000171 20010910 00171 NM 2001 9 10 QXEA0101425 1 20010829 A 2120 ODOR DHAV DHC8 DHC8202 2809007 NM CABIN DETECTED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 354PH 498 SEA - VERY PUNGENT STENCH FROM BLEED SYSTEM WHEN POWER IS BACK, ON DESCENT, BLEED AIR ON. GROUND RAN ENGINES, ISOLATING BLEED AIR BY OPERATING ONE BLEED AT A TIME. NO SIGN OF ENGINE INGESTION. CLEANED AIR CYCLE MACHINE INLET SCREEN. AIRCRAF T RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091000172 20010910 00172 NM 2001 9 10 QXEA0101426 1 20010830 A 5540 STRUCTURE DHAV DHC8 DHC8* NM RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - FORE RUDDER CRACKED WITH PIECE MISSING AT TOP CLOSING RIB, PIECE OVERLAPPING AFT RUDDER. FABRICATED NEW RIB FROM . 040 2024T3. ALODINED, PRIMED, PAINTED AND INSTALLED END CAP IAW E.A. 6-55-03. 2 H 7 2 4T RT A13NM 2001091000173 20010910 00173 NM 2001 9 10 01FDEA00796 1 20010831 A 2620 NOZZLE BOEING 727 727233 138408A NM NR 1& 3 ENGINE MISSING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 223FE 20935 01-296 NR 3 ENG FIRE AGENT DISPERSE NOZZLE MISSING AND CAPPED OFF. REMOVED AND REPLACED FIRE NOZZLE ON ENG 1 & 3 PER MM 26-21-00. 2 L 7 3 4F RT A3WE 2001091000174 20010910 00174 EU 2001 9 10 QXEA0101431 1 20010902 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 477AU 11226 BOI - EXIT SIGN ABOVE COCKPIT DOOR HAS BURNED OUT BULBS. REPLACED EXIT SIGN IAW F-28 MAINTENANCE MNANUAL, 33-50-00, PAGE S 413-415. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001091000175 20010910 00175 EU 2001 9 10 QXEA0101432 1 20010902 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 477AU 11226 BOI - EXIT SIGN AT CABIN ENTRANCE HAS BURNED OUT BULBS. REPLACED EXIT SIGN IAW F-28 MAINTENANCE MANUAL 33-50-00, PAGES 4 12-413. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001091000176 20010910 00176 EU 2001 9 10 QXEA0101433 1 20010902 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 477AU 11226 BOI - BOTH EXIT SIGNS AT MID CABIN HAVE BURNED OUT BULBS. REPLACED EXIT SIGN IAW F-28 MAINTENANCE MANUAL 33-50-00, PAGE 422. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001091000177 20010910 00177 NM 2001 9 10 QXEA0101434 1 20010903 A 2120 ODOR DHAV DHC8 DHC8202 2809007 NM CABIN DETECTED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 345PH 476 BOI - FLIGHT ATTENDANT REPORTS A "BURNING SMELL" UPON ENGINE START THAT CLEARS UP AFTER TAKE-OFF. AIRCRAFT DOWN FOR MAIN TENANCE. 2 H 7 2 4T RT A13NM 2001091000178 20010910 00178 NM 2001 9 10 QXEA0101435 1 20010830 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 8 SEAT TRACK HAS CORROSION AT 517.12. REPAIRED IAW DASH-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2001091000179 20010910 00179 NM 2001 9 10 QXEA0101436 1 20010830 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 9 SEAT TRACK HAS CORROSION AT 568.50. REPAIRED IAW DASH-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2001091000180 20010910 00180 NM 2001 9 10 QXEA0101437 1 20010830 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 9 SEAT TRACK IS GOUGED AT CAMLOCK RECETPACLE AT 622.50. REPAIRED IAW DASH-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2001091000181 20010910 00181 NM 2001 9 10 QXEA0101438 1 20010830 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 7 SEAT TRACK HAS TWO GOUGES AT 311.00. REPAIRED IAW DASH-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2001091000182 20010910 00182 NM 2001 9 10 QXEA0101439 1 20010830 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 7 SEAT TRACK HAS CORROSION BETWEEN 322.0 AND 323.0. REPAIRED IAW DASH-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2001091000183 20010910 00183 NM 2001 9 10 01FDEA00797 1 20010831 A 2410 BULB BOEING 727 727227 1384078 NM NR 2 CSD FAULTY A FDEA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 SO 25 489FE 21492 01-297 NR 2 CSD TEMP ROSE TO 140 DEG AND STAB AFT THROTTLE RETARD IDLE TEMP DOWN 100 DEG. REMOVED AND REPLACED CSD OIL TEMP BULB, COOLER AND FILTER. 2 L 7 3 4F A3WE 2001091000184 20010910 00184 NM 2001 9 10 QXEA0101440 1 20010830 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 7 SEAT TRACK HAS CORROSION BETWEEN 357.00 AND 358.00. REPAIRED IAW DASH-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2001091000185 20010910 00185 NM 2001 9 10 QXEA0101441 1 20010830 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 7 SEAT TRACK CAMLOCK RECEPTACLE CUTOUT HAS CORROSION AT 371.00. REPARIED IAW DASH-8 SRM 51-20-16 AND SRM 51-20- 36. 2 H 7 2 4T RT A13NM 2001091000186 20010910 00186 NM 2001 9 10 01FDEA00802 1 20010906 A 2613 WARNING LIGHT BOEING 727 7272D4 138407U NM COCKPIT ILLUMINATED A FDEA K NONE J WARNING INDICATION CR CRUISE 1 SO 25 287FE 21849 01-300 LWR AFT BODY HEAT LIGHT CAME ON. CK DUCTS IN AIR CONDITION COMP & AFT AIRSTAIR AREA. NO DEFECTS NOTED. OPS CK PER MM 26-14-00-1. 2 L 7 3 4F A3WE 2001091000187 20010910 00187 NM 2001 9 10 QXEA0101442 1 20010830 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 7 SEAT TRACK HAS CORROSION BETWEEN 396.00 AND 398.00. REPAIRED IAW DASH-8 SRM 61-20-16 AND SRM 61-20-36. 2 H 7 2 4T RT A13NM 2001091000188 20010910 00188 NM 2001 9 10 QXEA0101443 1 20010830 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 8 SEAT TRACK HAS CORROSION AT 424.25. REPAIRED IAW DASH-8 SRM 51-20-16 AND SRM 51-2-36. 2 H 7 2 4T RT A13NM 2001091000189 20010910 00189 NM 2001 9 10 01FDEA00803 1 20010901 A 2550 WIRE DOUG MD11 MD11 3023602 NM CARGO BAY BURNED A FDEA H DEACTIVATE SYST/CIRCUITS P NO WARNING INDICATION CR CRUISE 1 SO 25 589FE 48491 DURING UPLOAD CTR CARGO LATERAL PWR ROLLER POPPED E/B (09-01-01). FOUND BURNED WIRES. 2 L 7 3 4F RT A22WE 2001091000190 20010910 00190 NM 2001 9 10 QXEA0101444 1 20010830 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 8 SEAT TRACK IS CHAFED AT BOTTOM OF TRACK GROOVE BETWEEN 438.00 AND 460.00. REPAIRED IAW DASH-8 SRM 51-20-16 AN D SRM 51-20-36. 2 H 7 2 4T RT A13NM 2001091000191 20010910 00191 NM 2001 9 10 QXEA0101445 1 20010830 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 11 SEAT TRACK HAS CORROSION BETWEEN 435.45 AND 439.45. REPAIRED IAW DASH-8 SRM 51-20-16 AND 51-20-36. 2 H 7 2 4T RT A13NM 2001091000192 20010910 00192 NM 2001 9 10 QXEA0101446 1 20010829 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 11 SEAT TRACK HAS CORROSION BETWEEN 455.00 AND 461.00. REPAIRED IAW RD 8-53-1432. 2 H 7 2 4T RT A13NM 2001091000193 20010910 00193 NM 2001 9 10 QXEA0101447 1 20010829 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 11 SEAT TRACK HAS CORROSION BETWEEN 467.00 AND 470.50. REPAIRED IAW RD 8-53-1432. 2 H 7 2 4T RT A13NM 2001091000194 20010910 00194 EU 2001 9 10 16824 1 20010827 A 5710 FITTING AEROSP ATR42 ATR42320 8680930 EU RT WING DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16824 166 YUL---DURING 4C INSPECTION YUL MAINTENANCE, AS PER COEX 5710-01025, INSPECTED AND REWORKED THE RT REAR WING SPAR FITTING S BETWEEN WING RIBS 7/8 AND RIB 12. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001091000195 20010910 00195 NM 2001 9 10 QXEA0101448 1 20010829 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 11 SEAT TRACK HAS CORROSION BETWEEN 484.45 AND 486.00. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001091000196 20010910 00196 NM 2001 9 10 QXEA0101449 1 20010829 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 11 SEAT TRACK HAS CORROSION BETWEEN 500.50 AND 501.50. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001091000197 20010910 00197 NM 2001 9 10 QXEA0101450 1 20010829 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 12 SEAT TRACK HAS CORROSION BETWEEN 515.00 AND 517.00. REPAIRED IAW RD 8-53-3644. 2 H 7 2 4T RT A13NM 2001091000198 20010910 00198 NM 2001 9 10 2001727500 1 20010820 A 5320 ANGLE BOEING 727 727228 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C-CHECK, MAIN CABIN FLOORBEAM REINFORCEMENT ANGLE DAMAGED AT STA 782 LBL 60. REMOVED ANGLE REINFORCEMENT AT CABIN FL OOR STA 782 LBL 60 AS PER B-727 SRM 51-30-2. FABRICATED AS PER B727 SRM 53-10-2 FIG 5 AND INSTALLED ANGLE REINFORCEMENT AT MAIN CABIN FLOORBEAM STA 782 LBL 60 PER BOING 727 SRM 51-302. 2 L 7 3 4F A3WE 2001091000199 20010910 00199 NM 2001 9 10 QXEA0101451 1 20010829 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 12 SEAT TRACK IS GOUGED BETWEEN 530.000 AND 532.50. REPAIRED IAW RD 8-53-3644. 2 H 7 2 4T RT A13NM 2001091000200 20010910 00200 NM 2001 9 10 QXEA0101452 1 20010829 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 12 SEAT TRACK HAS CORROSION BETWEEN 540.50 AND 541.00. REPAIRED IAW RD 8-53-3644. 2 H 7 2 4T RT A13NM 2001091000201 20010910 00201 NM 2001 9 10 QXEA0101453 1 20010830 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 7 SEAT TRACK HAS CORROSION AT 207.00. REPAIRED IAW DASH-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2001091000202 20010910 00202 NM 2001 9 10 QXEA0101454 1 20010830 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 7 SEAT TRACK IS CHAFED BETWEEN 213.00 AND 214.00. REPAIRED IAW DASH-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2001091000203 20010910 00203 NM 2001 9 10 QXEA0101456 1 20010828 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 10 SEAT TRACK HAS CORROSION BETWEEN 423.00 AND 425.00. REPAIRED IAW RD 8-53-1432. 2 H 7 2 4T RT A13NM 2001091000204 20010910 00204 NM 2001 9 10 QXEA0101457 1 20010828 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - BOTTOM TCAS ANTENNA AIRCRAFT SURFACE HAS CORROSION. REPAIRED IAW DASH-8 SRM 51-20-11 AND SRM 51-20-16. 2 H 7 2 4T RT A13NM 2001091000205 20010910 00205 NM 2001 9 10 2001727501 1 20010819 A 5755 CHANNEL BOEING 727 727228 NM SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C-CHECK, NR 10 SPOILER, OUTBD STOP CASTING, LWR ATTACH STRUCTURE TO LWR REAR SPAR CHORD, STRUCTURE IS LOSE AND WORKIN G. REMOVED FASTENERS AT HAT CHANNEL SUPPORT FOUND LARGE CRACKS. REMOVED CHANNEL AS PER B727 SRM 51-30-2. INSTALLED NE W HAT CHANNEL SUPPORT AS PER B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2001091000206 20010910 00206 NM 2001 9 10 QXEA0101458 1 20010829 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 10 SEAT TRACK HAS CORROSION BETWEEN 262.40 AND 267.00. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001091000207 20010910 00207 NM 2001 9 10 QXEA0101459 1 20010829 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 10 SEAT TRACK HAS CORROSION BETWEEN 296.50 AND 298.0. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001091000208 20010910 00208 NM 2001 9 10 QXEA0101460 1 20010829 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 10 SEAT TRACK HAS CORROSION BETWEEN 328.00 AND 328.50. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001091000209 20010910 00209 NM 2001 9 10 QXEA0101461 1 20010829 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 10 SEAT TRACK HAS CORROSION BETWEEN 341.40 AND 344.40. REPAIRED IAW RD 8-53-1432. 2 H 7 2 4T RT A13NM 2001091000211 20010910 00211 NM 2001 9 10 QXEA0101462 1 20010829 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 10 SEAT TRACK HAS CORROSION AT 356.40. REPAIRED IAW RD 8-53-1432. 2 H 7 2 4T RT A13NM 2001091000212 20010910 00212 NM 2001 9 10 QXEA0101463 1 20010829 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDFX - NR 10 SEAT TRACK HAS CORROSION BETWEEN 361 AND 365.40. REPAIRED IAW RD 8-53-1432. 2 H 7 2 4T RT A13NM 2001091000213 20010910 00213 NM 2001 9 10 QXEA0101464 1 20010829 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 10 SEAT TRACK HAS CORROSION BETWEEN 368.40 AND 369.40. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001091000214 20010910 00214 NM 2001 9 10 QXEA0101465 1 20010829 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 10 SEAT TRACK HAS CORROSION BETWEEN 374.40 AND 378.40. REPAIRED IAW RD 8-53-1432. 2 H 7 2 4T RT A13NM 2001091000215 20010910 00215 NM 2001 9 10 QXEA0101466 1 20010829 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 10 SEAT TRACK HAS CORROSION BETWEEN 391.40 AND 394.0.REPAIRED IAW RD 8-53-1432. 2 H 7 2 4T RT A13NM 2001091000216 20010910 00216 NM 2001 9 10 QXEA0101467 1 20010829 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 10 SEAT TRACK HAS CORROSION BETWEEN 404.40 AND 409.40. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001091000217 20010910 00217 NM 2001 9 10 QXEA011204 1 20010719 A 5340 ATTACH FITTING DHAV DHC8 DHC8202 2809007 NM MLG ACTUATOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX-RIGHT SIDE MAIN LANDING GEAR "H" MEMBER ACTUATOR ATTACH POINT HAS SURFACE CORROSION. REPAIRED IAW HORIZON AIR EA 2-5 4-88. 2 H 7 2 4T RT A13NM 2001091000218 20010910 00218 NM 2001 9 10 QXEA011205 1 20010717 A 5530 FLANGE DHAV DHC8 DHC8202 2809007 NM VERTICAL STAB GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX-SEVERAL TOOLING GOUGES AND SCRATCHES ON LEFT HAND VERTICAL STABILIZER LEAD EDGE MOUNT FLANGE. REPAIRED IAW DHC-8 RD8 -55-584. 2 H 7 2 4T RT A13NM 2001091000219 20010910 00219 NM 2001 9 10 QXEA011206 1 20010719 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX-SEAT TRACK NR 7 HAS CORROSION AND A SCRATCH AT STATION 244. REPAIRED IAW DHC-8 SRM 51-40-11 AND SRM 51-40-00. 2 H 7 2 4T RT A13NM 2001091000220 20010910 00220 NM 2001 9 10 XEA0101381 1 20010821 A 5413 PANEL DHAV DHC8 DHC8202 2809007 NM NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX - PANEL 422AT AT OUTBOARD FORWARD LATCH HAS CRACKED HORSE COLLAR SKIN AT .350 AND .300 INCH. REPAIRED IAW HORIZON AI R EA 2-71-159. 2 H 7 2 4T RT A13NM 2001091000221 20010910 00221 EA 2001 9 10 A6WA200100047 2 20010810 A 7323 230305204 CONTROL BOX BAC 146 146300A 1500267 EU LYC ALF502 ALF502* 41580 EA NR 1 ENGINE FAILED A A6WA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 GL 31 612AW 19929 1792 E3122 LF05428A NR 1 ENGINE FAILED IN FLIGHT, NO LEAKS NOTED OR DAMAGE NOTED. MAINTENANCE REMOVED AND REPLACED THE HIGH AND LOW PRESSUR E FUEL FILTERS, FUEL CONTROL AND PRIMARY OVERSPEED CONTROL BOX. 2 H 7 4 4F 4 F RT A49EU E6NE 2001091000222 20010910 00222 NM 2001 9 10 A6WA200100048 1 20010803 A 5245 LATCH DORNER DO32 DO328100 2996000 NM GROUND AIR DOOR OUT OF ADJ A A6WA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 GL 31 329PH 3007 GROUND AIR DOOR INDICATOR INDICATION AFTER TAKEOFF. MAINTENANCE INSPECTED AND ADJUSTED BOTH GROUND AIR DOOR LATCHES, DO OR CLOSED SECURELY. 2 H 7 2 4T RT A45NM 2001091000223 20010910 00223 EU 2001 9 10 A6WA200100050 1 20010803 A 2120 ODOR BAC 146 146300A 1500267 EU FWD GALLEY DETECTED A A6WA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 31 611AW E3120 AFTER TAKEOFF, FLIGHT ATTENDANT REPORTED SMELL IN FWD GALLEY AREA, GALLEY LOAD SHED, SMELL DISSIPATED. MAINTENANCE INSP ECTED FWD CABIN AND GALLEY AREA, RAN ENGINES, USED ENGINE AIR WITH GALLEY POWER ON, NO SMELL NOTED. 2 H 7 4 4F RT A49EU 2001091000224 20010910 00224 EU 2001 9 10 A6WA200100051 1 20010819 A 3610 6303250 PERISEAL BAC 146 146200A 1500266 EU PNEUMATIC SYS LEAKING A A6WA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 31 156TR E2156 RIGHT ZONE HIGH TEMP. MAINTENANCE REMOVED AND REPLACED PERI SEAL AT PNEUMATIC COUPLING FWD OF PRECOOLER. 2 H 7 4 4F A49EU 2001091000225 20010910 00225 NM 2001 9 10 USAA011028 1 20010807 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 2 INCHES, BS 294.5 LGL 709. CORROSION LEVEL 1, TASK NR C53-107-01. UPPER T- CHORD REPAIRED PER TR 53-10-04 B. (M) 2 L 7 2 4F A16WE 2001091000226 20010910 00226 NM 2001 9 10 USAA011042 1 20010808 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND FLOORBEAM UPPER CHORD 2 INCHES BY 31 INCHES, BS 344, FLOORBEAM LBL 11-42. SPLICED IN NEW SECTION OF T-CAP BE TWEEN LBL 30 TO RBL 17 PER TR 737-200, 53-10-13. (M) 2 L 7 2 4F A16WE 2001091000228 20010910 00228 NM 2001 9 10 USAA011043 1 20010808 A 5320 ANGLE BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND Z-ANGLE CORRODED 1 INCH BY 30 INCHES, FORWARD SERVICE DOOR Z-ANGLE BS 300. REMOVED AND REPLACED WITH PART NR 1138222 PER SRM 51-10-01. (M) 2 L 7 2 4F A16WE 2001091000229 20010910 00229 NM 2001 9 10 USAA011138 1 20010821 A 5300 SKIN BOEING 737 737401 1384701 NM BS 787 CRACKED A K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 36045 23984 CLT - FOUND SKIN CRACKED 4 INCHES, BS 787 BS 25L. INSTALLED DOUBLER AND FILLER PER SRM 53-00-01 FIG 217. (M) 2 L 7 2 4F RT A16WE 2001091000230 20010910 00230 NM 2001 9 10 USAASB01242 1 20010827 A 2500 15611175 SLIDE BOEING 737 737201 1384454 NM SERVICE DOOR INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 260AU 20220 3116 22866 BOS - THE AFT RIGHT SERVICE DOOR EVACUATION SLIDE FAILED TO REMAIN INFLATED DURING TEST. MAINTENANCE REPLACED THE EVACU ATION SLIDE. (M) 2 L 7 2 4F A16WE 2001091000231 20010910 00231 NM 2001 9 10 USAA011142 1 20010822 A 5300 BULKHEAD BOEING 737 737201 1384454 NM BS 1016 GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND PRESSURE AFT BULKHEAD WITH 3 GOUGES APPROXIMATELY .125 INCH, LBL 3 BS 1016. INSTALLED DOUBLER, TRIPLER, FIL LER OF REPAIR PER EA 85254. (M) 2 L 7 2 4F A16WE 2001091000232 20010910 00232 WP 2001 9 10 ASAA0180232 1 20010801 A 5600 59644202 WINDOW DOUG DC9 DC983 3022083 WP COCKPIT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 977AS 22899 53453 SEA - DURING PREFLIGHT CHECK, FIRST OFFICERS SLIDING CLEARVIEW WINDOW COULD NOT BE OPENED. REPOSITIONED UPPER GUIDE PIN . WINDOW THEN OPERATED PROPERLY AND EASILY. (M) 2 L 7 2 4F RT A6WE 2001091000233 20010910 00233 WP 2001 9 10 ASAA0180228 1 20010725 A 5600 5613217520 WINDOW DOUG DC9 DC982 3022082 WP COCKPIT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 935AS 49236 SEA - DURING PREFLIGHT CHECK, FIRST OFFICERS SLIDING CLEARVIEW WINDOW WAS DIFFICULT TO OPEN. TIGHTENED LOOSE SLIDE AT U PPE AFT LOCATION. WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001091000234 20010910 00234 WP 2001 9 10 ASAA0180222 1 20010712 A 5600 5613217520 WINDOW DOUG DC9 DC983 3022083 WP COCKPIT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 960AS 31672 53074 PDX - DURING PREFLIGHT CHECK, FIRST OFFICERS SLIDING CLEARVIEW WINDOW WAS DIFFICULT TO OPEN. LUBRICATED WINDOW TRACKS. WINDOW THEN OPERATED PROPERLY AND EASILY. (M) 2 L 7 2 4F RT A6WE 2001091000235 20010910 00235 WP 2001 9 10 ASAA0180213 1 20010628 A 5600 59644201 WINDOW DOUG DC9 DC982 3022082 WP COCKPIT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 954AS 43955 49387 SEA - DURING PREFLIGHT CHECK, CAPTAINS SLIDING CLEARVIEW WINDOW COULD NOT BE OPENED. REPLACED LOWER OUTBOARD HOOK ARM S PRING. WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001091000236 20010910 00236 WP 2001 9 10 ASAA0180206 1 20010621 A 5600 5613217519 WINDOW DOUG DC9 DC983 3022083 WP COCKPIT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 25725 53448 SEA - DURING PREFLIGHT CHECK, CAPTAINS SLIDING CLEARVIEW WINDOW WAS DETERMINED TO BE DIFFICULT TO OPEN. CLEANED AND LUB RICATED WINDOW SLIDING MECHANISM. WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001091000237 20010910 00237 WP 2001 9 10 ASAA0180191 1 20010607 A 5600 5613217519 WINDOW DOUG DC9 DC983 3022083 WP COCKPIT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 34229 53024 SEA - DURING PREFLIGHT CHECK, IT WAS DETERMINED THAT THE CAPTAINS SLIDING CLEARVIEW WINDOW COULD NOT BE OPENED. RESET A CTUATOR CAM UPPER LOCK BAR IN CHANNEL. WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001091000238 20010910 00238 WP 2001 9 10 ASAA0180187 1 20010601 A 5600 5613217520 WINDOW DOUG DC9 DC983 3022083 WP COCKPIT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 25574 53451 ANC - DURING PREFLIGHT CHECK, IT WAS DETERMINED THAT THE FIRST OFFICERS SLIDING CLEARVIEW WINDOW COULD NOT BE OPENED. A DJUSTED SLIDER MECHANISM. WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001091000239 20010910 00239 WP 2001 9 10 ASAA0180182 1 20010526 A 5600 5613217520 WINDOW DOUG DC9 DC982 3022082 WP COCKPIT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 967AS 49103 SEA - DURING PREFLIGHT CHECK, IT WAS DETERMINED THAT THE FIRST OFFICERS SLIDING CLEARVIEW WINDOW JAMS WHEN ATTEMPTING TO OPEN. ADJUSTED LOOSE PIECE OF TRIM. WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001091000240 20010910 00240 WP 2001 9 10 ASAA0180179 1 20010523 A 5600 5613217519 WINDOW DOUG DC9 DC982 3022082 WP LT SIDE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 954AS 43566 49387 SEA - DURING PREFLIGHT CHECK, IT WAS DETERMINED THAT THE CAPTAINS SLIDING CLEARVIEW WINDOW COULD NOT BE OPENED. RE-SITU ATED LOWER ECCENTRIC ADJUSTMENT ROLL PIN. WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001091000241 20010910 00241 WP 2001 9 10 ASAA0180172 1 20010517 A 5610 5613217519 WINDOW DOUG DC9 DC983 3022083 WP COCKPIT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 25725 53448 SEA - DURING PREFLIGHT CHECK, CAPTAINS SLIDING CLEARVIEW WINDOW WAS DETERMINED TO BE DIFFICULT TO OPEN. LUBRICATED WIND OW SLIDING MECHANISM. WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001091000242 20010910 00242 NM 2001 9 10 ASAA0110559 1 20010819 A 3350 883200312 RECEIVER BOEING 737 7372X6C 1384552 NM INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROWS 8 AND 12 FLASHING ON AND OFF. REMOVED AND REPLACED REMOTE ASSEMBLY RECEIVERS AND BATTERIES. LIGHTS THEN TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2001091000243 20010910 00243 NM 2001 9 10 GAIA01304OP 1 20010829 A 2611 302842 SMOKE DETECTOR BOEING 727 727251 138408H NM MAIN CARGO BAY MALFUNCTIONED A GAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 278US 21157 FLT 1278 - DFW-FWA - AFTER TAKEOFF, THE UPPER CARGO COMPARTMENT SMOKE DETECTOR ILLUMINATED. VISUAL INSPECTION DID NOT D ETECT ANY SMOKE IN CARGO AREA. THE FLIGHT CREW ELECTED TO RETURN TO DFW. AN UNEVENTFUL LANDING WAS MADE AT DFW. INSPE CTION FOUND THE NR 3 AND NR 6 SMOKE DETECTORS FAILED TO TEST. THE SMOKE DETECTORS WERE REPLACED AND THE SYSTEM OPERATIO NALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001091000244 20010910 00244 NM 2001 9 10 GAIA01303OP 1 20010828 A 2611 302842 SMOKE DETECTOR BOEING 727 727251 138408H NM CARGO BAY MALFUNCTIONED A GAIA K NONE N FALSE WARNING CR CRUISE 1 SW 07 278US 21157 KHA - FLT 278 - PHX-DFW - DURING CRUISE, THE UPPER CARGO COMPARTMENT SMOKE DETECTOR ILLUMINATED. VISUAL INSPECTION DID NOT DETECT ANY SMOKE IN CARGO AREA. AN UNEVENTFUL LANDING WAS MADE AT DFW. INSPECTION FOUND THE NR 6 SMOKE DETETECTOR FAILED TO TEST. THE SMOKE DETECTOR WAS REPLACED AND THE SYSTEM OPERATIONLLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001091000246 20010910 00246 NM 2001 9 10 USAA011049 1 20010809 A 5320 BRACE BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 41570 22961 CLT - FOUND DIAGONAL FLOOR BRACE CORRODED 1 INCH, BS 986.5 TO 1006, LBL 10 TO LBL 19. REPLACED BRACE PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2001091000247 20010910 00247 NM 2001 9 10 USAA011051 1 20010809 A 5320 SUPPORT BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47520 22961 CLT - FOUND FRAME SUPPORT HAS .25 INCH CRACK, S19R BS 520. REMOVED AND REPLACED FRAME SUPPORT PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2001091000249 20010910 00249 NM 2001 9 10 USAA011053 1 20010810 A 5312 PRESSURE PANEL BOEING 737 737201 1384454 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND BEADS MISSING IN PRESSURE WEB, BS 662 TO BS 673 WL 203. INSTALLED ANGLE STIFFENERS PER EA 85189 REF SB 737- 57-1234. (M) 2 L 7 2 4F A16WE 2001091000252 20010910 00252 NM 2001 9 10 USAA011056 1 20010813 A 5320 ANGLE BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND Z-CHORD CORRODED 2 INCHES BY 10 INCHES, BS 947 TO BS 996. REMOVED AND REPLACED WITH NEW PART NR 1124774 PER SRM 51-10-1 AND SRM 51-30-02. (M) 2 L 7 2 4F A16WE 2001091000253 20010910 00253 NM 2001 9 10 USAA011064 1 20010813 A 5320 ANGLE BOEING 737 737201 1384454 NM FUSELAGE BENT A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND DRAG ANGLE BENT, RIGHT AFT VERTICAL STABILIZER MOUNT AREA. FABRICATED AND INSTALLED REPAIR STRAPS AND FILLE RS PER EA 85186. (M) 2 L 7 2 4F A16WE 2001091000273 20010910 00273 WP 2001 9 10 USAAD01148 1 20010810 A 3230 CONTROL VALVE DOUG DC9 DC981 3022081 WP LANDING GEAR OUT OF RIG A USAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 19 807US 48039 PIT-BOS - FLT 564 - DURING APPROACH, RECEIVED LANDING GEAR UNSAFE INDICATIONS WHEN THE LANDING GEAR WAS SELECTED DOWN. RECYCLED THE LANDING GEAR AND RECEIVED NORMAL GEAR DOWN INDICATIONS. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINT ENANCE CHECKED AND ADJUSTED THE RIGGING OF THE LANDING GEAR CONTROL VALVE. A GEAR SWING WAS ALSO ACCOMPLISHED. OPERATI ONALLY CHECKED OK. (M) 2 L 7 2 4F A6WE 2001091000274 20010910 00274 WP 2001 9 10 USAAD01149 1 20010811 A 2560 CLIP DOUG DC9 DC981 3022081 WP ESCAPE SLIDE DISCONNECTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 828US 48028 PHL - THE FORWARD ENTRY DOOR EMERGENCY ESCAPE SLIDE PACK TO GIRT BAR RETENTION CLIP WAS FOUND DISCONNECTED. MAINTENANCE REATTACHED THE GIRT BAR RETENTION CLIP. OK FOR SERVICE. (M) 2 L 7 2 4F A6WE 2001091000275 20010910 00275 EU 2001 9 10 USAASA01042 1 20010813 A 2120 ODOR AIRBUS A321 A321211 EU CABIN DETECTED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 178US 1519 PHL - FLT 8 - EN ROUTE LAX-PHL, THE CABIN CREW REPORTED AN ODOR DURING FLIGHT. THE ODOR DISSIPATED AND THE FLIGHT LANDE D WITHOUT INCIDENT IN PHL. MAINTENANCE INSPECTED THE GALLEYS AND RAN THE AIR CONDITIONING PACKS. NO ODORS WERE DETECTE D. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2001091000276 20010910 00276 EU 2001 9 10 USAASA01045 1 20010816 A 3350 WARNING SYSTEM AIRBUS A321 A321211 EU COCKPIT MALFUNCTIONED A USAA K NONE N FALSE WARNING IN INSP/MAINT 1 EA 19 166US 1436 SFO - DURING THE TEST OF THE EMERGENCY LIGHTING SYSTEM, RECEIVED AN 'EPSU ARMED' MESSAGE ON THE CABIN INTERCOMMUNICATION DATA SYSTEM. MAINTENANCE DID A BITE TEST OF THE CABIN INTERCOMMUNICATION DATA SYSTEM AND PERFORMED AN EMERGENCY LIGHTS TEST. NO FAULTS WERE FOUND. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2001091000277 20010910 00277 NM 2001 9 10 USAASB01219 1 20010802 A 2133 322684003 OUTFLOW VALVE BOEING 737 7374B7 1384702 NM CABIN PRESSURE STUCK A USAA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 EA 19 780AU 56527 24997 BWI - FLT 282 - ON CLIMB-OUT, THROUGH FL230, THE AIRCRAFT EXPERIENCED A RISE IN CABIN PRESSURE FOLLOWED BY THE ALTITUDE WARNING HORN. CREW WAS UNABLE TO CONTROL CABIN PRESSURE IN AUTO OR STANDBY MODE. CREW DESCENDED FLIGHT TO FL120 AND WAS ABLE TO CONTROL ALTITUDE IN MANUAL MODE. REMAINED AT FL120 AND CONTINUED TO BWI WHERE IT LANDED WITHOUT INCIDENT. NO EME RGENCY WAS DECLARED. MAINT FOUND THE FWD OUTFLOW VALVE STICKING DURING PRESSURIZATION CHECK. REMOVED AND REPLACED THE FW D OUTFLOW VALVE PER MM. SYSTEM OPERATIONAL CHECK NORMAL. ALSO, REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER (P/N 763810-1) AND AFT OUTFLOW VALVE (P/N 711003-3) PER MM. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001091000278 20010910 00278 NM 2001 9 10 USAASB01235 1 20010819 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 441US 24812 BDL - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT ROWS 6, 7, 8 AND 9ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D THE BATTERY CHARGER ASSEMBLY. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2001091000279 20010910 00279 NM 2001 9 10 USAASB01236 1 20010819 A 3350 1010428 LIGHT BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 780AU 24997 PIT - PILOT REPORTED THAT THE EMERGENCY LIGHT AT OVERHEAD BIN 25D WAS BROKEN/INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001091000280 20010910 00280 NM 2001 9 10 USAASB01238 1 20010820 A 3350 1012721 LIGHT BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 441US 24812 TPA - MAINTENANCE FOUND A SEGMENT OF SEAT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPAIRED THE LIGHT ASSEMBLY ON SEAT ROW 9ABC. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001091000281 20010910 00281 NM 2001 9 10 USAASB01239 1 20010820 A 3350 1012721 LIGHT BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 442US 24841 TPA - MAINTENANCE FOUND THE EMERGENCY LIGHTS IN SEAT ROWS 6 THROUGH 9 AND 12 THROUGH 19 INOPERATIVE. ALSO, FOUND LEFT E MERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE FOUND A WIRE SHORTED UNDER SEAT ROW 9, LEFT SIDE. REMOVED AND REPLACED LIG HT ASSEMBLY AT SEAT ROW 9, LEFT SIDE. ALSO, REMOVED AND REPLACED BATTERY PACK (P/N 2013-1A) AT SEAT ROW 11, LEFT SIDE, FOR TROUBLESHOOTING. OPERATIONAL CHECK OF ALL LIGHTS GOOD. (M) 2 L 7 2 4F RT A16WE 2001091000282 20010910 00282 NM 2001 9 10 2001F00265 1 20010819 A 3350 86210144 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROWS 8 AND 12 FLASHING ON AND OFF. REMOVED AND REPLACED REMOTE ASSEMBLY RECEIVERS AND BATTERIES. LIGHTS THEN TESTED NORMAL. REF ASAA0110559. (M) 2 L 7 2 4F RT A16WE 2001091000283 20010910 00283 WP 2001 9 10 ASAA0180173 1 20010517 A 5610 5613217519 WINDOW DOUG DC9 DC982 3022082 WP COCKPIT LACK OF LUBE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 954AS 43516 49387 SEA - DURING TAXI IN, IT WAS DETERMINED THAT THE CAPTAINS SLIDING CLEARVIEW WINDOW COULD NOT BE OPENED. LUBRICATED WIND OW SLIDING MECHANISM. WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001091000284 20010910 00284 WP 2001 9 10 ASAA0180181 1 20010525 A 2560 3753213 LANYARD DOUG DC9 DC983 3022083 WP ENTRY DOOR DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 948AS 53021 SEA - DURING PREFLIGHT CHECK, FOUND GIRT BAR LANYARD DETACHED FROM EMERGENCY SLIDE COVER. REATTACHED LANYARD TO SLIDE C OVER PER MM 25-62-00. (M) 2 L 7 2 4F RT A6WE 2001091000285 20010910 00285 WP 2001 9 10 ASAA0180193 1 20010607 A 2560 3961899501 LANYARD DOUG DC9 DC983 3022083 WP R1 DOOR DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 SEA - DURING PREFLIGHT CHECK, R1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED FROM DOOR. REATTACHED LANYARD BE TWEEN GIRT BAR AND DOOR SLIDE COVER. (M) 2 L 7 2 4F RT A6WE 2001091000286 20010910 00286 WP 2001 9 10 ASAA0180194 1 20010605 A 5730 SKIN DOUG DC9 DC983 3022083 WP RT WING DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 969AS 53063 SEA - DURING LINE CHECK, FOUND RIGHT LOWER WING DAMAGE AT XRS 509.5 FROM FRONT TO REAR REAR. INITIATED PERIODIC INSPECT ION PER EA 5720-01193, WITH FINAL RESOLUTION TO BE ACCOMPLISHED AT NEXT C-CHECK. OAK - DURING C-CHECK, INSTALLED EXTERN AL DOUBLER FROM FRONT SPAR TO REAR SPAR PER EA 5730-01086. (M) 2 L 7 2 4F RT A6WE 2001091000287 20010910 00287 WP 2001 9 10 ASAA0180197 1 20010611 A 5210 5910081167 DOOR DOUG DC9 DC983 3022083 WP L1 OUT OF RIG A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 969AS 33095 53063 JUN - AFTER TAXI UP TO GATE, L1 DOOR FORWARD LEFT CREW/PAX DOOR WAS FOUND TO BE DIFFICULT TO OPEN. RIGGED L1 DOOR. THE DOOR THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001091000289 20010910 00289 WP 2001 9 10 ASAA0180200 1 20010613 A 2150 20495054 ACM DOUG DC9 DC983 3022083 WP A/C BAY FAILED A ASAA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 NM 01 960AS 31597 53074 SEA - JUST AFTER TAKEOFF, BURNED RUBBER/INSULATION SMELL WAS NOTED IN COCKPIT. REOCCURRED DURING BEGINNING OF DESCENT. REPLACED LEFT COOLING TURBINE ASSY AND BOTH LEFT AND RIGHT COALESCER. PERFORMED AIR QUALITY CHECK AND NO ODOR WAS EVIDE NT. (M) 2 L 7 2 4F RT A6WE 2001091000290 20010910 00290 WP 2001 9 10 ASAA0180203 1 20010617 A 2560 3961899501 LANYARD DOUG DC9 DC983 3022083 WP R1 DOOR DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 969AS 53063 SEA - DURING PREFLIGHT CHECK, R1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED FROM DOOR. REATTACHED LANYARD BE TWEEN GIRT BAR AND DOOR SLIDE COVER. (M) 2 L 7 2 4F RT A6WE 2001091000291 20010910 00291 2001 9 10 ASAA0180214 4 20010701 A 2565 3961899501 LANYARD DOUG DC9 DC983 3022083 WP R1 DOOR DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 SFO - DURING PREFLIGHT CHECK, R1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED FROM DOOR. REATTACHED LANYARD BE TWEEN GIRT BAR AND DOOR SLIDE COVER. (M) 2 L 7 2 4F RT A6WE 2001091000292 20010910 00292 WP 2001 9 10 ASAA0180223 1 20010714 A 5610 59644201 WINDOW DOUG DC9 DC983 3022083 WP COCKPIT OUT OF ADJ A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 26287 53448 SEA - DURING PREFLIGHT CHECK, CAPTAINS SLIDING CLEARVIEW WINDOW COULD NOT BE OPENED. ADJUSTED WINDOW CAM FOLLOWER PER M M 56-10-03. WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001091000293 20010910 00293 2001 9 10 ASAA0180225 4 20010721 A 2565 3961899501 LANYARD DOUG DC9 DC983 3022083 WP GALLEY DOOR DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 SEA - DURING PRE-FLIGHT CHECK, GALLEY SERVICE DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED FROM THE SLIDE COVER . REATTACHED LANYARD BETWEEN GIRT BAR AND DOOR SLIDE COVER. (M) 2 L 7 2 4F RT A6WE 2001091000294 20010910 00294 WP 2001 9 10 ASAA0180235 1 20010808 A 5210 5914730 HOOK DOUG DC9 DC983 3022083 WP L1 DOOR OUT OF ADJ A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 947AS 53020 SEA - DURING PREFLIGHT CHECK, IT WAS DETERMINED THAT THE DOOR HOLD OPEN LATCH DOES NOT ALWAYS LINE UP WITH PIN. ADJUSTE D HOLD-OPEN HOOK PER MM 52-11-00, PP 511-512A, STEPS 1-6. MECHANISM THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001091000295 20010910 00295 WP 2001 9 10 ASAA0180242 1 20010812 A 2170 COALESCER BAG DOUG DC9 DC983 3022083 WP A/C BAY DIRTY A ASAA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 01 969AS 53063 ZIH - DURING CLIMB AT 10K FEET ALTITUDE, BURNING RUBBER/ELECTRICAL FIRE SMELL WAS DETECTED IN VICINITY OF ROW 15. REMOV ED OVERHEAD PANELS AT ROWS 13-17 AND INSPECTED LIGHTS, BALLASTS, AND EMERGENCY BATTERIES. REPLACED LEFT AIR CONDITIONIN G SYSTEM COALESCER BAG. RAN ENGINE AND LEFT AC PACK FOR 45 MINUTES. COULD NOT DUPLICATE ODOR. RELEASED AIRCRAFT FOR S ERVICE. (M) 2 L 7 2 4F RT A6WE 2001091000296 20010910 00296 2001 9 10 ASAA0180243 4 20010816 A 2565 3961899501 LANYARD DOUG DC9 DC982 3022082 WP L1 DOOR DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 931AS 49232 SEA - DURING PRE-FLIGHT CHECK, L-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED FROM SLIDE COVER LATCH. REATTA CHED LANYARD BETWEEN GIRT BAR AND DOOR SLIDE COVER LATCH. (M) 2 L 7 2 4F A6WE 2001091000297 20010910 00297 WP 2001 9 10 ASAA0180244 1 20010818 A 3350 0105606 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 LAX - DURING PREFLIGHT CHECK, FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING WAS DETERMINED TO BE INOPERATIVE. RECON NECTED LIGHT MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001091000298 20010910 00298 2001 9 10 ASAA0180245 4 20010818 A 2565 3961896501 LANYARD DOUG DC9 DC983 3022083 WP SERVICE DOOR DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 SEA - DURING PRE-FLIGHT CHECK, R1 DOOR EMERGENCY SLIDE LANYARD ASSEMBLY LATCH WAS FOUND TO BE DETACHED FROM SLIDE COVER. REINSTALLED LATCH ON COVER. (M) 2 L 7 2 4F RT A6WE 2001091000299 20010910 00299 NM 2001 9 10 G60A057 1 20010727 A 5711 NRB67052 SPAR CAP DOUG MD11 MD11 3023602 NM RT WING CRACKED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 703GC 93088 48411 FOUND RIGHT WING REAR SPAR LOWER CAP HAS 3 INCH LONG CRACK IN RADIUS FROM RS 1046.2 TO RS 1049.9. (M) 2 L 7 3 4F RT A22WE 2001091000300 20010910 00300 NM 2001 9 10 GAIA01301OP 1 20010824 A 3350 1000679 LIGHT BOEING 727 727251 138408H NM COCKPIT INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 255US 19974 DURING MAINTENANCE AT PHL, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACE D THE COCKPIT EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001091000301 20010910 00301 NM 2001 9 10 GAIA01302OP 1 20010828 A 3350 1000679 CONNECTOR BOEING 727 727225 1384077 NM COCKPIT DIRTY A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 936PG 22441 DURING MAINTENANCE AT TOL, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT WAS INOPERATIVE. INSPECTION FOUND TH E EMERGENCY EXIT LIGHT CONNECTIONS DIRTY THE CONNECTORS WERE CLEANED AND THE LIGHT WAS REINSTALLED. THE SYSTEM OPERATI ONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001091000302 20010910 00302 NM 2001 9 10 TSAA0179112 1 20010823 A 7933 INDICATOR BOEING 737 737230 NM COCKPIT FALSE INDICATION A TSAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 13 821AL 23155 FLT 246 - HNL-ITO - DIVERT TO OGG, DURING CLIMB AT APPROX 200 FT PILOT NOTICED THE NR 1 ENGINE OIL TEMPERATURE GAUGE IN THE YELLOW BAND, 140 DEGREES. CONTINUED TO FL250 FT, POWER WAS REDUCED AND OIL TEMP INCREASED TO 150 DEGREES THEN WENT OFF SCALE MOMENTARILY. THE FUEL HEAT VALVE WAS CHECK, OIL TEMP BULB CANNON PLUG CLEANED, AND NR 1 AND NR 2 OIL TEMP GAU GED WERE SWAPPED FOR FURTHER TROUBLESHOOTING. THE ENGINE WAS THEN OPERATIONAL CHECKED AT TAKEOFF AND CRUISE POWER FOR S EVERAL MINUTES. ALL ENGINE PARAMETERS REPORTED NORMAL AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001091000303 20010910 00303 NM 2001 9 10 USAA011139 1 20010822 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND CHORD ANGLE CRACKED 1 INCH, BS 178 SIDE CHORD AT WL 207, LEFT SIDE. INSTALLED REPAIR SIDE CHORD PER EO 5300 V157. (M) 2 L 7 2 4F A16WE 2001091000304 20010910 00304 NM 2001 9 10 USAA011140 1 20010822 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND CHORD ANGLE CRACKED 1 INCH, RIGHT SIDE CHORD BS 178 AT WL 207. INSTALLED REPAIR, SIDE CHORD, PER EO 5300V15 7. (M) 2 L 7 2 4F A16WE 2001091000305 20010910 00305 NM 2001 9 10 USAA011141 1 20010822 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND INTERCOSTAL CORRODED 2 INCHES BY 2.5 INCHES, BS 312, FLOORBEAM LBL 8.5 TO RBL 11 UPPER SURFACE. CORROSION T ASK NR C53-107-01. REMOVED AND REPLACED FLOORBEAM UPPER CHORD WITH PART NR 65-45834-523 PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2001091000306 20010910 00306 2001 9 10 USAABB01084 4 20010818 A 3417 4040800906 ADC BOEING 767 767201 1385125 NM E/E BAY FAULTY A USAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 19 650US 56840 23902 PHL - FLT 1854 - AFTER TAKEOFF FROM PHL, CREW NOTED A SPLIT BETWEEN THE CAPTAINS AND FIRST OFFICERS ALTITUDE AND AIRSPEE D, AND THE E/M'S 'RUDDER RATION' AND 'AILERON LOCKOUT.' FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MA INTENANCE REPLACED THE NR 2 AIR DATA COMPUTER. (M) 2 L 7 2 4F RT A1NM 2001091000310 20010910 00310 NM 2001 9 10 HNAA0100053 1 20010717 A 5310 85320686101 STRAP DHAV DHC8 DHC8102 2809003 NM CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 906HA 43437 9 THRESHOLD STRAP AT AIRSTAIR DOOR CUTOUT HAS CORROSION .020" DEEP IN SEVERAL AREAS. REPLACED STRAP. 2 H 7 2 4T RT A13NM 2001091000312 20010910 00312 NM 2001 9 10 HNAA0100054 1 20010720 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 906HA 43437 9 FUSELAGE SKIN CORRODED ON STRINGER 31P BETWEEN STATIONS 202 AND 240. REPAIRED PER EO8-53-01-312. 2 H 7 2 4T RT A13NM 2001091000315 20010910 00315 CE 2001 9 10 AHE0101 1 20010606 A 2750 12527Y6331 CONTROL CABLE BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO T/E FLAP SHEARED A O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 EA 35 GJUST LE1165 THE LEFT FLAP DRIVE CABLE WAS FOUND TO HAVE A SUSPECT D.O.M. A NEW ITEM PN 12527Y6331 WAS ORDERED AND RECEIVED WITH A 03 -2001 D.O.M. THE NEW ITEM WAS IAW MM AND ON FIRST OPERATION OF THE FLAPS THE LEFT FLAP FAILED TO MOVE. ON INVESTIGATIO N IT WAS DISCOVERED THAT THE NEW FLAP DRIVE CABLE HAD SHEARED AT THE DRIVE END TO THE ACTUATOR. CABLE WAS RETURNED TO M FG. 1 L 7 1 3O 3 O 3A15 E5CE 2001091000316 20010910 00316 NM 2001 9 10 HNAA0100055 1 20010725 A 5311 85320318 FRAME DHAV DHC8 DHC8102 2809003 NM CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 906HA 43437 9 FRAME AT STATION 201 IS CORRODED AT STRINGER 31S. REPAIRED PER EO8-53-01-325. 2 H 7 2 4T RT A13NM 2001091000317 20010910 00317 SW 2001 9 10 ALG2001F00022 1 20010614 A 6210 206015001107 SKIN BELL 206 206L3 1182108 SW M/R BLADE CORRODED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 187AL 2612 51135 DISCOVERED DURING ROUTINE AIRFRAME INSPECTION, FOUND CORROSION BENEATH OUTBOARD TRIM TAB, T/E EXTRUSION AND BLADE SKIN C ORRODED BEYOND REPAIRABLE LIMITS. 1 G 7 1 3U H2SW 2001091000319 20010910 00319 SO 2001 9 10 KKY2001F00000 1 20010726 A 3246 AHA2063 WHEEL GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU MLG FIRE E KKYA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 NE 03 777SA 7507 14 1081 AFTER THREE LANDINGS WITH FULL STOPS (CHECK AIRMEN RIDE), ON TAXI IT WAS OBSERVED BY ANOTHER AIRCRAFT THAT FLAMES WERE C OMING FROM THE NR 1 MAIN WHEEL. GROUND WAS NOTIFIED AND ALERTED THE CREW WHO IMMEDIATELY STOPPED. THE CREW OBSERVED A SMALL BLUISH FLAME EMANATING FROM A LIGHTNING HOLE OF THE WHEEL. AN AIRCRAFT FIRE EXTINGUISHER WAS USED TO EXTINGUISH T HE FLAME. LOCAL MAINTENANCE DETERMINED THE AIRCRAFT SAFE TO MOVE FOR FURTHER INVESTIGATION. INVESTIGATION REVEALED NO CONCLUSIVE INFORMATION AS TO THE CAUSE OF IGNITION AND THE COMBUSTION SOURCE FOR SUSTAINING THE FIRE. THE LANDING GEAR, BRAKE, WHEEL WELL AND SURROUNDING STRUCTURE WERE INSPECTED WITH NO CONCLUSIVE EVIDENCE. THE WHEEL/TIRE ASSY WAS REMOVE 2 L 7 2 4F 4 F RT A12EA E25NE 2001091000320 20010910 00320 CE 2001 9 10 NSVA0104 1 20010623 A 5210 1145140309106 CABLE BEECH 1900 1900C 1154161 CE PAX DOOR BROKEN A K NONE O OTHER TX TAXI/GRND HDL 1 EA 27 119CJ UC19 BOSTON, CREW WAS UNABLE TO OPEN THE FORWARD CABIN DOOR. AIRCRAFT WAS RELEASED UNDER SPECIAL FLIGHT PERMIT TO HYA FOR RE PAIRS. MAINTENANCE REPLACED AIRSTAIR DOOR CABLE, OPERATIONAL CHECK WAS SATISFACTORY. 2 L 7 2 4T RT A24CE 2001091000322 20010910 00322 SO 2001 9 10 OG52001F00000 1 20010612 A 3260 36742014 SWITCH PIPER PA28 PA28R201 7102816 SO LYC O360 O360* 41514 EA RT MLG FAILED B OG5R O OTHER N FALSE WARNING AP APPROACH 1 GL 21 286ND 471 471 2844035 CREW DID NOT RECEIVE A GREEN DOWN AND LOCKED INDICATION ON THE RIGHT MAIN LANDING GEAR UPON GEAR EXTENSION. AN UNEVENTF UL LANDING WAS MADE AFTER TOWER CONFIRMED THAT THE GEAR WAS DOWN. INITIAL INSPECTION BY PERSONNEL FOUND THE RIGHT DOWN LIMIT SWITCH WAS OUT OF RIG. THE SWITCH WAS ADJUSTED AND A GEAR RETRACTION TEST WAS PERFORMED. UPON THE EMERGENCY EXTE NSION CHECK, THE SWITCH IN QUESTION ACTUATING ARMS HINGE PIN BECAME DISLODGED AND ALLOWED THE SWITCH TO DEACTIVATE. SWI TCH WAS REPLACED AND SYSTEM CHECKED GOOD. UPON COMPARISON WITH A NEW SWITCH, THE HINGE PIN HOLES WERE LARGER AND ALLOWE D THE MOVEMENT OF THE PIN UNTIL THE SWITCH FAILED. 1 L 7 1 3O 3 O 2A13 E286 2001091000326 20010910 00326 SO 2001 9 10 OG52001F00001 1 20010719 A 8011 711092252 SOLENOID PIPER PA28 PA28161 7102803 SO LYC O320 O320* 41508 EA STARTER INCORRECT A OG5R K NONE O OTHER IN INSP/MAINT 1 GL 21 241ND 2108 2842051 PILOT REPORTED THAT STARTER CONTINUED TO CRANK AFTER KEY WAS REMOVED AND ANYTIME BATTERY POWER WAS PRESENT. TROUBLESHOO TING BY MAINTENANCE PERSONNEL. FOUND WRONG PN STARTER SOLENOID INSTALLED. RESEARCH OF AIRCRAFT RECORDS FOUND THAT THIS PART HAD NEVER BEEN REPLACED AND MUST HAVE BEEN INSTALLED AT MANUFACTURE. 1 L 7 1 3O 3 O 2A13 E274 2001091000330 20010910 00330 EU 2001 9 10 OU1R01003 1 20010813 A 2932 704A37721034 PRESSURE SWITCH AEROSP SA365 SA365N1 8680668 EU TMECA ARRIEL ARRIEL1C 60030 NE HYDRAULIC SYS FAILED A OU1R A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 13 65CW 2439 6262 AUX HYDRAULIC LIGHT ILLUMINATED INFLIGHT. AIRCRAFT MADE PRECAUTIONARY UNSCHEDULED LANDING TO VACANT PARKING LOT. CAUSED BY UNIT FAILURE. 1 G 7 2 3U 3 U H10EU E19EU 2001091000332 20010910 00332 NM 2001 9 10 P7U2001F00000 1 20010628 A 2612 0881031007 SWITCH BOEING 737 737* NM FIREBELL CUTOUT INOPERATIVE E P7UR K NONE O OTHER NR NOT REPORTED 1 EA 17 VPGHN 7 32438 SWITCHES 2 EA SHORTED INTERNALLY, SHOULD RETURN TO N/O CONDITION. LOOKS LIKE MICRO SWITCH FAILED INTERNALLY IN ASSEMBLY . REMOVED AND REPLACED WITH NEW SWITCHES. RETESTED SYSTEM NO MALFUNCTIONS OR DEFECTS NOTED. FIRE BELL CUTOUT S/W OPS CHECKED GOOD. 2 L 7 2 4F RT A16WE 2001091000333 20010910 00333 EU 2001 9 10 QML2001F00000 1 20010601 A 2752 ACTUATOR PILATS PC12 PC1245 EU PWA PT6 PT6A66 52043 NE T/E FLAP FAILED D QMLA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 03 299AM 236 FLAP SYSTEM MALFUNCTION. FLAPS FROZE AT APPROXIMATELY 15 DEGREES, WHILE BEING RETRACTED IMMEDIATELY FOLLOWING TAKEOFF. D EFECTIVE FLAP ACTUATOR. FAULTY FLAP ACTUATOR REMOVED AND REPLACED. 1 L 7 1 3T 4 T RT A78EU E26NE 2001091000334 20010910 00334 EA 2001 9 10 SH52001F00001 1 20010713 A 2750 6009300065 FLAP CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF34* NE RT WING FAILED D SH5R K NONE F J FLT CONT AFFECTED WARNING INDICATION IN INSP/MAINT 1 NE 03 315FX 3275 5377 DURING OPS CHECK OF FLAPS, A FLAP FAIL MESSAGE APPEARED ON THE EICAS. PHYSICAL INSPECTION FOUND RIGHT OUTBOARD FLAP IN 45 DEGREE DOWN POSITION AND OTHER FLAP SEGMENTS APPROACHING 30 DEGREES DETENT. INVESTIGATION FOUND RIGHT FLAP DRIVE NR 8 SWAGED END PULLED OUT OF THE FLEX DRIVE HOUSING CAUSING DRIVE CABLE TO MOVE OUT OF FLAP ACTUATOR. FERRULE END DOES NO T APPEAR TO HAVE BEEN CRIMPED. 2 L 7 2 4F 4 F RT A21EA E15NE 2001091000335 20010910 00335 EU 2001 9 10 SW032001B0055 1 20010711 A 6310 350A35105901 COUPLING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE ENG/TRANS DEFORMED A B3OR K NONE O OTHER IN INSP/MAINT 1 SW 03 5204J 672 3118 COUPLING FOUND EXCESSIVELY DEFORMED AT 100 HR INSPECTION. NO OTHER PROBLEMS FOUND AT THIS TIME. 1 G 7 1 3U 3 U H9EU E19EU 2001091000337 20010910 00337 2001 9 10 TI1R001411 4 20010110 A 3422 40205773 GYRO BOLKMS 117 BK117A3 5626015 EU COCKPIT DEFECTIVE B TI1R O OTHER O OTHER NR NOT REPORTED 1 SW 05 4493X S7038 DIRECTIONAL GYRO, 20 DEGREES OFF ON READING, BETWEEN POLES. REMOVED AND REPLACED. 1 G 7 2 3U H13EU 2001091000338 20010910 00338 EU 2001 9 10 TI1R001414 1 20010104 A 3340 356H2801 LIGHT SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE ANTICOLLISION INOPERATIVE B TI1R O OTHER O OTHER NR NOT REPORTED 1 SW 05 40751 3154 LAMP, DOES NOT ILLUMINATE. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2001091000339 20010910 00339 SW 2001 9 10 TI1R001415 1 20010107 A 2510 222320823123 RESTRAINT BELL 230 230 1182149 SW ALLSN 250C 250C30 03013 GL COCKPIT FRAYED B TI1R O OTHER O OTHER NR NOT REPORTED 1 SW 05 4UV 3232 23019 RESTRAINT ASSEMBLY FRAYED. REMOVE AND REPLACE. 1 G 7 2 3U 3 U NC H9SW E1GL 2001091200085 20010912 00085 EA 2001 9 12 COMA0160680 1 20010904 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 809CA 7366 FLIGHT 5420. DURING CLIMBOUT OF CVG RECEIVED A CABIN DOOR OUTER HANDLE CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. PERFORMED AN OPERATIONAL CHECK OF THE CABIN DOOR OUTER HANDLE WARNING SYSTEM, DISCREPANCY COULD NOT BE DUPLICATED BY MAINTENANCE, RELEASED AIRCRAFT BACK TO SERVICE. 2 L 7 2 4F RT A21EA 2001091000340 20010910 00340 EU 2001 9 10 TI1R001419 1 20010205 A 5210 1172429117 LATCH BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE DOOR FAILED B TI1R O OTHER O OTHER NR NOT REPORTED 1 SW 05 317MC 7505 LATCH, LEFT HAND- FAILED , SCRAPPED ON SITE. REMOVED AND REPLACED. 1 G 7 2 3U 3 U NC H13EU E19EU 2001091000341 20010910 00341 EA 2001 9 10 A6WA200100052 1 20010816 A 7931 601509197 TRANSDUCER CNDAIR CL600 CL6002B19 EA RT ENGINE FAILED A A6WA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 405AW 4343 4343 7362 ZERO OIL PRESSURE ON RT ENGINE DURING FLIGHT. NO ASSOCIATED MESSAGES. ALL OTHER ENGINE INDICATIONS WERE NORMAL. NO LO W OIL PRESSURE LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED RT ENGINE OIL PRESSURE TRANSDUCER. 2 L 7 2 4F RT A21EA 2001091000342 20010910 00342 EU 2001 9 10 A6WA200100053 1 20010816 A 2910 HC324B0017000 HYDRAULIC LINE BAC 146 146200A 1500266 EU HYDRAULIC SYS CRACKED A A6WA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 GL 31 291UE E2084 AIRCRAFT EVACUATED DUE TO FUMES IN CABIN. AIRCRAFT SHUTDOWN, FIRE HANDLES PULLED BUT NOT ROTATED. BLEW 3 OF 4 SLIDES, BOTH FRONT AND LT AFT ENGINES SHUTDOWN BEFORE T-HANDLE PULLED. MAINTENANCE REMOVED AND REPLACED YELLOW SYSTEM TUBE ASSE MBLY AND 3 EVAC SLIDES. 2 H 7 4 4F A49EU 2001091000343 20010910 00343 EA 2001 9 10 A6WA200100054 1 20010802 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 EA COCKPIT ILLUMINATED A A6WA K NONE J WARNING INDICATION CR CRUISE 1 GL 31 403AW 7288 EN ROUTE THE PAX DOOR HANDLE CAUTION ILLUMINATED. PRESSURIZATION WAS NORMAL. WHILE C/W CHECKLIST THE PAX DOOR WARNING ILLUMINATED AS PRESSURIZATION WAS MANUALLY REDUCED, WARNING CHANGED BACK TO CAUTION. MAINTENANCE INSPECTED DOOR AND LOC KING MECHANISMS. NO DEFECTS NOTED. OPERATED DOOR 5 TIMES IAW MM 52-11-00, OK FOR SERVICE. 2 L 7 2 4F RT A21EA 2001091000344 20010910 00344 NM 2001 9 10 ABAX010461 1 20010831 A 5280 DOOR BOEING 767 767281 1385109 NM NLG OUT OF ADJ A ABXA K NONE E VIBRATION/BUFFET CR CRUISE 1 GL 23 787AX 23020 DURING CLIMB, THERE WAS A LOUD NOISE AND AIRFRAME VIBRATION AT SPEEDS ABOVE 280 KTS BETWEEN 15,000 TO 20,000 FEET. NO L OUD NOISE OR VIBRATION DURING CRUISE OR DESCENT. VISUALLY INSPECTED UPPER AND LOWER FUSELAGE AND ALL CONTROL SURFACES. NO DEFECTS NOTED. FOUND THE LEFT AFT NLG DOOR LEADING EDGE OUT OF TOLERANCE. ADJUSTED IAW 767 AMM 32-22-04-4. OPS CH ECKED GOOD ON GEAR SWING. FUNCTIONAL CHECK FLIGHT EVALUATION WAS SATISFACTORY. 2 L 7 2 4F RT A1NM 2001091000345 20010910 00345 WP 2001 9 10 ABXA010456 1 20010829 A 3260 1864 LIGHT DOUG DC9 DC932 3022066 WP COCKPIT INOPERATIVE A ABXA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 23 982AX 47317 CREW REPORTED ON APPROACH DOOR OPEN LIGHT WOULD NOT PRESS TO TEST. DID FLY BY, TOWER REPORTED DOORS CLOSED. RELAMPED G EAR DOOR OPEN LIGHT PRESS TO TEST INDICATOR. OPS CHECKED GOOD IAW DC-9 MM. 2 L 7 2 4F A6WE 2001091000346 20010910 00346 WP 2001 9 10 ABXA010457 1 20010829 A 3350 60030451 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 989AX 47314 EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW DC-9 MM 33-53-02-4-0001. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2001091000347 20010910 00347 EA 2001 9 10 COMA0160692 1 20010906 A 2720 6229815704 CARD CNDAIR CL600 CL6002B19 EA AVIONICS BASY FAULTY A COMA K NONE O OTHER CR CRUISE 1 SO 01 431CA 293 7472 FLIGHT #5247. DURING CRUISE FLIGHT THE AIRCRAFT DEMONSTRATED YAW CHARACTERISTICS, ESPECIALLY DURING CLIMB.REPLACED THE #2 FCC CARD. (FCC-4000) 2 L 7 2 4F RT A21EA 2001091000348 20010910 00348 NM 2001 9 10 UPS01236809 1 20010827 A 5330 STRINGER BOEING 727 727172C 1384058 NM BS 947 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 916UP 19808 INSPECTION TYPE:C CRACK FOUND ON S18 L/H AT BS 947 REPAIR CARRIED OUT IAW IAW SMRO EO 2001-039-002 UPS ENGINEERING F ILE NO. 727-53-20028 2 L 7 3 4F A3WE 2001091000349 20010910 00349 NM 2001 9 10 UPS01236810 1 20010830 A 5100 SKIN BOEING 727 727172C 1384058 NM FWD MCD CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 916UP 19808 INSPECTION TYPE:C ON REMOVAL OF FWD FUSELAGE HINGE FROM MAIN CARGO DOOR, CORROSION FOU ND ON FUSELAGE SKIN REPAIRED IAW SMRO EO 2001-039-004 2 L 7 3 4F A3WE 2001091000350 20010910 00350 WP 2001 9 10 ABXA010458 1 20010830 A 5270 SWITCH DOUG DC8 DC861 3021952 WP CARGO DOOR MALFUNCTIONED A ABXA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 849AX 45891 MAIN CARGO DOOR, NON-DOUGLAS, SYSTEM A-LIGHT CAME ON IN FLIGHT WITH PRESSURIZATION HOLDING. PER ABNORMALS, CREW DESCEND ED TO 10,000 FEET. DEPRESSURIZED AIRCRAFT AND INSPECTED DOOR. LIGHT WENT OUT BELOW 6.0 PSID. DOOR INSPECTION, ALL LAT CHED APPEARED LOCKED. REPRESSURIZED AIRCRAFT, LIGHT CAME BACK ON ABOVE 8.0 PSID. REPLACED HARDWARE ON S1-388 IAW DC-8 MM 20-16-0. PRESSURIZED CABIN TO 8.2 PSID, LIGHT REMAINED OFF IAW DC-8 MM 52-36-10-2-0001. 2 L 7 4 4F 4A25 2001091000351 20010910 00351 WP 2001 9 10 ABXA010459 1 20010830 A 2170 COALESCER BAG DOUG DC9 DC931 3022065 WP A/C BAY DIRTY A ABXA K NONE O OTHER CR CRUISE 1 GL 23 924AX 47403 OIL SMELL WAS COMING FROM THE AIR CONDITIONING OUTLETS. UNABLE TO DETERMINE FROM WHICH PACK. DUCT TEMPERATURES WERE NO RMAL. REPLACED THE LEFT AND RIGHT COALESCER BAGS IAW DC-9 MM 21-20-00. 2 L 7 2 4F A6WE 2001091000352 20010910 00352 2001 9 10 ABXA010462 4 20010828 A 2211 25866865 COMPUTER DOUG DC9 DC941 302207N WP E/E BAY DEFECTIVE A ABXA K NONE E VIBRATION/BUFFET CR CRUISE 1 GL 23 966AX 1474 47510 AUTOPILOT EVALUATION REQUESTED PER M1A 028521-64/2. AUTOPILOT EVALUATION WAS UNSATISFACTORY. HEADING BUG DID NOT OVERS HOOT AND THERE WASN'T EXCESSIVE BANK BUT THERE WAS RESISTANT VIBRATION IN THE ELEVATOR WITH AUTOPILOT ENGAGED. REPLACED THE AUTOPILOT PITCH COMPUTER IAW DC9 AMM 22-13-01. 2 L 7 2 4F A6WE 2001091000353 20010910 00353 WP 2001 9 10 ABXA010463 1 20010901 A 5610 WINDOW DOUG DC9 DC933F 302207A WP COCKPIT LACK OF LUBE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 CREW REPORTED THAT THE FIRST OFFICER'S CLEAR VIEW WINDOW WOULD NOT OPEN. LUBRICATED THE UPPER LOCK BAR. OPERATIONAL CH ECKED GOOD. 2 L 7 2 4F A6WE 2001091000354 20010910 00354 WP 2001 9 10 ABXA010464 1 20010905 A 5610 WINDOW DOUG DC9 DC941 302207N WP COCKPIT OPEN A ABXA K NONE O OTHER CL CLIMB 1 GL 23 952AX 47615 OUT OF 2500 FT AGL, THE CAPTAIN'S CLEAR VIEW WINDOW OPENED AND DUMPED PRESSURIZATION. CHECKED AND INSPECTED CAPTAIN'S C LEAR VIEW WINDOW PER DC9 AMM 56-10-03. PRESSURIZED AIRCRAFT TO 3 PSI. NO LEAKS NOTED. CHECKED CLEARANCES OF THE LOWER AFT HOOK AND FITTING, AFT LOCK BAR, FORWARD LOCK BAR STOP AND FORWARD LOCK HOOK & FITTING. ALL FOUND WITHIN LIMITS. C HECKED THE WINDOW FRAME AND SEALS. NO DEFECTS FOUND. LUBRICATED THE LOWER AFT LINKAGE ROD IAW DC9 AMM 56-10. 2 L 7 2 4F A6WE 2001091000355 20010910 00355 EA 2001 9 10 COMA0160693 1 20010906 A 2720 6229815704 CARD CNDAIR CL600 CL6002B19 EA AVIONICS BAY FAULTY A COMA K NONE O OTHER CR CRUISE 1 SO 01 431CA 328 7472 FLIGHT #5247. DURING CRUISE FLIGHT THE AIRCRAFT DEMONSTRATED YAW CHARACTERISTICS, ESPECIALLY DURING CLIMB.REPLACED THE # 1 FCC CARD. (FCC-4000) 2 L 7 2 4F RT A21EA 2001091000357 20010910 00357 EA 2001 9 10 COMA0160694 1 20010906 A 2720 6229968001 DAMPER CNDAIR CL600 CL6002B19 EA AVIONICS BAY FAULTY A COMA K NONE O OTHER CR CRUISE 1 SO 01 431CA 5659 7472 FLIGHT #5247. DURING CRUISE FLIGHT THE AIRCRAFT DEMONSTRATED YAW CHARACTERISTICS, ESPECIALLY DURING CLIMB.REPLACED THE #1 YAW DAMPER ACTUATOR. (SVL-4000). 2 L 7 2 4F RT A21EA 2001091000358 20010910 00358 EA 2001 9 10 COMA0160695 1 20010906 A 2720 6229968001 DAMPER CNDAIR CL600 CL6002B19 EA AVIONICS BAY FAULTY A COMA K NONE O OTHER CR CRUISE 1 SO 01 431CA 602 7472 FLIGHT #5247. DURING CRUISE FLIGHT THE AIRCRAFT DEMONSTRATED YAW CHARACTERISTICS, ESPECIALLY DURING CLIMB.REPLACED THE #2 YAW DAMPER ACTUATOR. (SVL-4000). 2 L 7 2 4F RT A21EA 2001091000359 20010910 00359 NM 2001 9 10 AT0100226 1 20010828 A 3350 CONNECTOR BOEING 717 717200 1383700 NM TAIL COMPARTMENT LOOSE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 952AT 55014 TAIL COMPARTMENT AFT THREE EMERGENCY LIGHTS ON LEFT SIDE DO NOT ILLUMINATE. FOUND CONNECTOR P1-116 LOOSE AT BATTERY PAC K. RESECURED CONNECTOR IAW B717 WDW 33-51-13. 2 L 7 2 4F TR A6WE 2001091000360 20010910 00360 NE 2001 9 10 AWXA0002166 2 20010816 A 7200 V2524A5 ENGINE AIRBUS A319 A319132 NM IAE V2524 V2524A5 NE NR 1 FAILED A AWXA E A ENGINE SHUTDOWN UNSCHED LANDING J R WARNING INDICATION PARTIAL RPM/PWR LOSS CR CRUISE 1 WP 28 818AW 1375 V10845 DEN - IN FLIGHT SHUTDOWN / UNSCHEDULED LANDING - FLT 534 - ORIG OPEN - EN ROUTE FROM PHX TO CLE THE NR 1 ENGINE EXPERIEN CED A COMPRESSOR STALL AND WENT TO IDLE, UPPER ECAM DISPLAYED ENG OIL FILTER (1) AND WAS SHUT DOWN. THE FLIGHT WAS DIVE RTED TO DEN AND ON DESCENT ENGINE RELIGHT WAS INITIATED BY FADEC THEN SHUT DOWN AGAIN. THE CREW FOLLOWED ECAM PROCEDURE S AND LANDED IN DEN WITHOUT INCIDENT. IN DEN MAINTENANCE INSPECTED THE MAIN OIL FILTER AND FOUND IT CLOGGED WITH METALL IC DEBRIS. THE ENGINE WAS REPLACED AND ALL FUNCTIONAL CHECKS WERE GOOD. AWAITING VENDOR REPORTS TO DETERMINE CAUSE OF FAILURE. 2 L 7 2 4F 4 F RT A28NM E40NE 2001091000361 20010910 00361 EA 2001 9 10 COMA0160696 1 20010908 A 5300 6003401737337 ANGLE CNDAIR CL600 CL6002B19 EA FS280 BL9.0 L/H CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 948CA 13697 7079 PERFORMED A MAJOR REPAIR TO THE L/H AND R/H VERTICAL J-ANGLES AT F.S. 280, BL 9.0 L/H AND R/H BY REMOVING THE CRACKED AN GLES AND INSTALLING FABRICATED ANGLES I/A/W WVAC EO 601R-53-2705. 2 L 7 2 4F RT A21EA 2001091000362 20010910 00362 EA 2001 9 10 COMA0160697 1 20010908 A 5346 601R31171 ANGLE CNDAIR CL600 CL6002B19 EA FS484 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 948CA 13967 7079 INTERCOSTAL FLANGES AT BL36 AND ANGLES AT BL27 LEFT AND RIGHT SIDES ARE CRACKED.REPAIRED ANGLE AND INTERCOSTAL AT FS484 I/A/W WVAC EO 601R-53-2701. 2 L 7 2 4F RT A21EA 2001091000363 20010910 00363 NM 2001 9 10 AWXA0002197 1 20010824 A 5315 6546568107 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 CORROSION ON FLOORBEAM UPPER FLANGE BS 1016. REMOVED CORROSION FOUND WITHIN LIMITS IAW B737-300 SRM 53-60-51 PG 105-114. REMOVED AND REPLACED ENTIRE 1016 FLOORBEAM UPPER CAP. DUE TO SEVERAL AREAS ON BEAM AFFECTED, PER ER 03-5365-01234-DL1 . 2 L 7 2 4F RT A16WE 2001091000364 20010910 00364 EA 2001 9 10 COMA0160698 1 20010908 A 3350 64641 LIGHT CNDAIR CL600 CL6002B19 EA A COMA K NONE S AFFECT SYSTEMS IN INSP/MAINT 1 SO 01 957CA 7109 FLIGHT #5067. DURING PRE-FLIGHT NOTICED THE FORWARD FLOOR EMERGENCY LIGHTING INOPERATIVE.REPLACED THE AFFECTED FLOOR EM ERGENCY LIGHT STRIP CABLE ASSEMBLY. 2 L 7 2 4F RT A21EA 2001091000365 20010910 00365 2001 9 10 AWXA0002202 4 20010824 A 2213 K217ABM11 CONTROLLER AIRBUS 320 A320231 3930325 EU AUTOPILOT SYS FAILED A AWXA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 28 628AW 29945 5553 67 PHX- ABORTED TAKEOFF - FLT 239 - ON TAKEOFF ROLL CREW HAD NO INDICATION OF TOGA AND ABORTED THE TAKEOFF AT 70 KTS AND RE TURNED TO THE GATE. MAINTENANCE TROUBLESHOT AND REPLACED THE FLIGHT CONTROL UNIT PER AMM 22-81-12-401, SYSTEM CHECKS WE RE GOOD. NO FURTHER DISCREPANCIES HAVE BEEN REPORTED. 2 L 7 2 4F RT A28NM 2001091000366 20010910 00366 EA 2001 9 10 COMA0160699 1 20010907 A 7931 INDICATOR CNDAIR CL600 CL6002B19 EA A COMA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SO 01 957CA 7109 FLIGHT #5067. DURING CLIMB OUT OF MCO THE RIGHT ENGINE LOST OIL PRESSURE ASSOCIATED WITH AN AURAL WARNING MESSAGE, AIRC RAFT RETURNED TO THE FIELD.FLUSHED AND RESERVICED THE RIGHT ENGINE OIL SYSTEM, PERFORMED 30 MINUTES GROUND RUN WITH NO N EGATIVE RESULTS. 2 L 7 2 4F RT A21EA 2001091000367 20010910 00367 NM 2001 9 10 AWXA0002203 1 20010822 A 2920 65178229 MODULE BOEING 737 7372E3 NM HYDRAULIC SYS FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 138AW 25182 22792 AIR TURNBACK - FLT 704 - DURING CLIMBOUT OF PHX THE AUTO PILOT DISCONNECTED, YAW DAMPER DISENGAGED AND B-SYSTEM HYDRAULI C PRESSURE WENT TO ZERO. AT THE TIME OF OCCURRENCE THE NR 2 B-SYSTEM ELEC HYD PUMP WAS INOPERATIVE ON MEL 29-2 COND 1 D UE TO LOW PRESSURE. THE AIRCRAFT WAS RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. IN PHX MAINTENANCE REPLACED THE N R 2 B-SYS HYD PUMP WHICH WAS NO HELP. FURTHER TROUBLESHOOTING DETERMINED THE B-SYSTEM HYDRAULIC MODULAR PACKAGE ASSY TO BE THE CAUSE FOR LOSING PRESSURE. THE B-SYS HYD MOD ASSY WAS REPLACED PER AMM 29-12-31 AND OPERATIONAL AND FUNCTION CH ECKS WERE GOOD. MEL 29-2 WAS CLEARED. NO FURTHER DISCREPANCIES HAVE BEEN REPORTED. 2 L 7 2 4F RT A16WE 2001091000368 20010910 00368 EA 2001 9 10 COMA0160700 1 20010907 A 5100 DOOR CNDAIR CL600 CL6002B19 EA A COMA D RETURN TO BLOCK E VIBRATION/BUFFET CR CRUISE 1 SO 01 807CA 7364 FLIGHT #5512. DURING CRUISE FLIGHT EXPERIENCED INTERMITTENT LOW FREQUENCY VIBRATION FROM COCKPIT FLOOR, AIRCRAFT RETURN ED TO ORIGINATION CITY CVG AND LANDED SAFELY.PERFORMED STATIC GEAR SWING, INSPECTED GEAR DOORS AND PERFORMED FLIGHT CHEC K, DISCREPANCY COULD NOT BE DUPLICATED. 2 L 7 2 4F RT A21EA 2001091000369 20010910 00369 EA 2001 9 10 COMA0160701 1 20010907 A 2751 CONNECTOR CNDAIR CL600 CL6002B19 EA A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 783CA 7315 FLIGHT #5741. DURING APPROACH INTO TRI RECEIVED A FLAP FAIL CAUTION MESSAGE AT 22 DEGREES FLAP POSITION.REMOVED CONNECTO R B2CE ON FLAP POWER DDRIVE UNTI, CLEANED AND REINSTALLED. 2 L 7 2 4F RT A21EA 2001091000370 20010910 00370 EU 2001 9 10 AWXA0002204 1 20010808 A 2433 X0052 TRANSFORMER AIRBUS 320 A320231 3930325 EU NR 1 FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 627AW 38541 66 BOS- AIR TURNBACK - FLT 442 - AFTER TAKEOFF FROM BOS EN ROUTE TO PHX THE CREW GOT A TRANSFORMER RECTIFIER 1 (TR1) FAILUR E INDICATION AND RETURNED TO BOS. IN BOS MAINTENANCE TROUBLESHOT AND REPLACED TR1 PER AMM 24-32-51-401. THE SYSTEM OPE RATIONALLY CHECKED NORMAL PER AMM 24-23-00-501. NO FURTHER DISCREPANCIES HAVE BEEN REPORTED. 2 L 7 2 4F RT A28NM 2001091000371 20010910 00371 NM 2001 9 10 AWXA0002205 1 20010808 A 2810 L95F50603 RELIEF VALVE AIRBUS A319 A319132 NM CENTER FUEL TANK RUPTURED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 822AW 2301 1410 MCI- UNSCHEDULED LANDING - FLT 77 - ON CLIMBOUT FROM BOS EN ROUTE TO PHX ECAM MESSAGE FOR FUEL AUTO FEED FAULT APPEARED, CREW DESELECTED AUTO AND MONITORED THE FUEL PAGE. ALL FUEL WAS BEING USED FROM LT MAIN TANK WITH X-FEED CLOSED. WITH LEFT PUMPS OFF FUEL WAS STILL BEING USED FROM LEFT SIDE. WITH LEFT AND CENTER PUMPS OFF FUEL WAS BEING USED FROM RIGHT TANK. ONCE FUEL WAS BALANCED FUEL STARTED FEEDING FROM THE LEFT TANK AGAIN, THE AIRCRAFT DIVERTED TO MCI. IN MCI MAINT ENANCE TROUBLESHOT AND FOUND OVER PRESSURE PROTECTOR 96QM RUPTURED. REPLACED SAME, OPERATIONAL AND LEAK CHECKED PER AMM 28-12-4-1, ALL CHECKS WERE GOOD. 2 L 7 2 4F RT A28NM 2001091000372 20010910 00372 NM 2001 9 10 AWXA0002207 1 20010824 A 3260 189915 SENSOR BOEING 737 7373G7 1384595 NM LT MLG OUT OF ADJ A AWXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 302AW 24009 AIR TURNBACK - FLT 271 - LT MAIN LANDING GEAR RED LIGHT REMAINED ILLUMINATED AFTER TAKEOFF AND GEAR SELECTED UP. WHEN L ANDING GEAR SELECTED DOWN ALL GEAR GREEN LIGHTS ILLUMINATED AND THE AIRCRAFT RETURNED TO PHX MAKING AN UNEVENTFUL LANDIN G. MAINTENANCE TROUBLESHOT AND FOUND THE LT MLG UPLOCK SENSOR TO TARGET GAP TO BE OUT OF ADJUSTMENT (TO FAR). THE SENS OR WAS ADJUSTED PER AMM 32-61-21, THE GEAR WAS CYCLED SEVERAL TIMES AND ALL INDICATIONS WERE NORMAL. NO FURTHER DISCREP ANCIES HAVE BEEN REPORTED. 2 L 7 2 4F RT A16WE 2001091000373 20010910 00373 NM 2001 9 10 AWXA0002209 1 20010827 A 2782 654465115 ACTUATOR BOEING 737 737277 1384570 NM L/E SLAT FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 185AW 47146 20894 22652 LAX - AIR TURNBACK - FLT 115 - DURING DEPARTURE CLIMB THE NR 6 LEADING EDGE SLAT WAS EXTENDED WITH FLAPS SELECTED UP. T HE AIRCRAFT ENCOUNTERED A ROLL TO THE LEFT, MAX SPEED WAS 250 KTS. THE AIRCRAFT RETURNED TO LAX AND MADE AN UNEVENTFUL LANDING. IN LAX MAINTENANCE TROUBLESHOT AND REPLACED THE NR 6 LEADING EDGE SLAT ACTUATOR PER AWA TASK CARD R3M27020. O PERATIONAL CHECKS WERE NORMAL. NO FURTHER DISCREPANCIES HAVE BEEN REPORTED. 2 L 7 2 4F RT A16WE 2001091000374 20010910 00374 NM 2001 9 10 AWXA0002211 1 20010901 A 2130 87292325V04 COMPUTER AIRBUS A319 A319132 NM E/E BAY FAILED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 828AW 351 1552 PHX - ABORTED TAKEOFF - FLT 79 - ON TAKE ROLL ECAM MESSAGE FOR AVIONICS VENT SKIN FAULT APPEARED AND THE TAKEOFF WAS ABO RTED UNDER 80 KTS. MAINTENANCE TROUBLESHOT AND REPLACED THE AVIONICS EQUIPMENT VENTILATION COMPUTER (AEVC), FUNCTIONAL CHECKS WERE GOOD. NO FURTHER DISCREPANCIES HAVE BEEN REPORTED. 2 L 7 2 4F RT A28NM 2001091000375 20010910 00375 EU 2001 9 10 AWXA0002212 1 20010904 A 2913 974540 PUMP AIRBUS 320 A320233 EU HYDRAULIC SYS LEAKING A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 28 825AW 689 0953 PHX - AIR TURNBACK - FLT 536 - ABOUT 10 MIN AFTER DEPARTURE FROM PHX EN ROUTE TO CLE THE BLUE HYD SYS PRESS AND QUANTITY DROPPED TO ZERO AND ASSOCIATED WARNING INDICATIONS WERE DISPLAYED. THE AIRCRAFT RETURNED TO PHX MAKING AN UNEVENTFUL L ANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE BLUE HYD SYS ELEC MOTOR DRIVEN HYD PUMP LEAKING FLUID AT THE P ARTING SURFACE BETWEEN THE MOTOR AND PUMP. THE MOTOR/PUMP ASSY WAS REPLACED, THE SYSTEM SERVICED AND ALL FUNCTIONAL AND LEAK CHECKS WERE GOOD. 2 L 7 2 4F RT A28NM 2001091000376 20010910 00376 NM 2001 9 10 ABXA010460 1 20010830 A 5300 STRUCTURE BOEING 767 767281 1385109 NM FUSELAGE VIBRATION A ABXA K NONE E VIBRATION/BUFFET CR CRUISE 1 GL 23 787AX 23020 THERE WAS A LOUD NOISE ON BOTH SIDES OF THE COCKPIT AND AIRFRAME VIBRATION AT AIRSPEEDS ABOVE 310 AT 10,000 TO 20,000 FO OT ALTITUDES. INSPECTED FLAPS, GEAR WELL AREAS, FLIGHT CONTROLS. RAN FLIGHT CONTROLS THRU. PRESSURIZED AIRCRAFT TO 6 PSI. INSPECTED MEC AREA AND DOOR SEAL. INSPECTED FORWARD EQUIPMENT AREA DOOR SEAL. NO DEFECTS FOUND. 2 L 7 2 4F RT A1NM 2001091000377 20010910 00377 EU 2001 9 10 AWXA0002214 1 20010904 A 3230 S4340131004 VALVE AIRBUS 320 A320232 3930326 EU RT MLG WW MALFUNCTIONED A AWXA O OTHER J WARNING INDICATION AP APPROACH 1 WP 28 652AW 11006 16 0953 BOS - USED ALTERNATE GEAR EXTENSION - ON APPROACH THE LANDING GEAR FAILED TO EXTEND WITH THE GEAR SELECTOR IN THE DOWN P OSITION, (NO GEAR OR DOOR MOTION SENSED). THE CREW USED ALTERNATE EXTENSION AND GEAR EXTENDED. AN UNEVENTFUL LANDING W AS MADE. IN BOS MX PERFORMED CHECKS PER THE TSM, NO FAULTS WERE NOTED ON LGCIU NR 1/2 BITE CHECKS. NO INDICATIONS OF A NY PROBLEMS. PER AWA TECHNICAL SUPPORT THE FOLLOWING COMPONENTS WERE REPLACED, AND ALL FUNCTIONAL CHECKS WERE GOOD. LA NDING GEAR CONTROL LEVER - P/N: 210TS07Y01, S/N: 1470, TT: 10356 - TC: 3950. LGCIU DOWTY ELEC CONMT LTD - P/N: 66470050 04D, S/N: 2243, TT:8110 - TC:3376 - TSR: 1530. LGCIU - DOWTY ELEC CONT LTD - P/N: 6647005004D - S/N: 2212 - LOC: NR 2 - 2 L 7 2 4F RT A28NM 2001091000378 20010910 00378 EU 2001 9 10 C2AX01CL200 1 20010831 A 3260 D22924014 SWITCH AEROSP ATR42 ATR42320 8680930 EU NR 2 SYSTEM DEFECTIVE A C2XA K NONE N FALSE WARNING AP APPROACH 1 SW 27 15827 175 CLE FLT NR 3294 THE CREW REPORTED LANDING GEAR UNSAFE LIGHT ILLUMINATED ON SYSTEM NR 2. MAINTENANCE REPLACED SECONDARY DOWNLOCK INDICATOR SWITCH. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001091000379 20010910 00379 EU 2001 9 10 C2XA01BT158 1 20010831 A 3234 CONTROL HANDLE AEROSP ATR42 ATR42320 8680930 EU COCKPIT DEFECTIVE A C2XA O OTHER O OTHER UK UNKNOWN 1 SW 27 14830 184 EWR---CO3578, CREW REPORTED, GEAR HANDLE GETS STUCK IN DOWN POSITION, VERY DIFFICULT TO MOVE GEAR INTO THE UP POSITION. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER IAW ATR42 JIC 32-31-81. OPS CHECKED GOOD. AIRCRAFT RET URNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001091000380 20010910 00380 NM 2001 9 10 CALA0100840 1 20010907 A 5230 SKIN BOEING 737 7373T0 1384582 NM C-1 DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND C-1 DOOR SKIN DENTED 13 INCHES AFT OF FORWARD EDGE AND 12 INCHES FROM TOP. A DOUBLER WAS INSTALLED IAW SRM 52-00-01. 2 L 7 2 4F RT A16WE 2001091000381 20010910 00381 WP 2001 9 10 CALA0100843 1 20010908 A 5330 SKIN DOUG DC9 DC982 3022082 WP FS 1183 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND EXTERNAL FUSELAGE SKIN HAD TWO SHEARED FASTENERS AT FS 1183 WITH CORROSION ON INSIDE. THE DOUBLER WAS R EMOVED AND REPLACED IAW SRM 51-10-4, 51-30-5, 51-30-2, ECRA 5330-03100, AND EA 9-5332-2-A924. 2 L 7 2 4F A6WE 2001091000382 20010910 00382 WP 2001 9 10 CALA0100848 1 20010909 A 5311 BELTFRAME DOUG DC9 DC982 3022082 WP STA 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15820 49480 INSPECTION FOUND A 1" CRACK IN BELTFRAME AT STA 1418, LONGERON 2R. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW DRAWING SRO9530003. 2 L 7 2 4F A6WE 2001091000383 20010910 00383 NM 2001 9 10 CALA0100849 1 20010909 A 5754 SLAT BOEING 737 7373T0 1384582 NM #3 POSN. DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND #3 SLAT LEADING EDGE DENTED APPROXIMATELY 30" FROM O/B END. REPAIRED SLAT IAW SRM 57-43-01. 2 L 7 2 4F RT A16WE 2001091000384 20010910 00384 WP 2001 9 10 CALA0100850 1 20010909 A 5330 SKIN DOUG DC9 DC982 3022082 WP STA 218 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND L/H FUSELAGE SKIN GOUGED AFT OF L-1 DOOR AT STA 218. THE GOUGED SKIN SECTION WAS REMOVED AND A NEW SECT ION OF SKIN WAS INSTALLED IAW SRM 51-30-2, 51-10-3, AND ECRA 5330-02445. 2 L 7 2 4F A6WE 2001091000386 20010910 00386 EU 2001 9 10 C2XA01BT160 1 20010814 A 5330 SKIN AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14828 179 YUL- DURING 4C INSPECTION YUL MAINTENANCE FOUND CRACK LOCATED ON THE RT SIDE OF THE RT HYDRAULIC CUTOUT IN THE FUSELAGE AT FRAME 25. MAINTENANCE REPAIRED CRACK ON RT SIDE OF RT HYDRAULIC CUTOUT AT FRAME 25 IAW COEX EC 5310-01200. OK FOR S ERVICE. 2 H 7 2 4T RT A53EU 2001091000387 20010910 00387 EU 2001 9 10 C2XA01BT161 1 20010814 A 5330 SKIN AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14828 179 YUL- DURING 4C INSPECTION MAINTENANCE FOUND CRACK ON THE LT SIDE OF THE LT HYDRAULIC CUTOUT. MAINTENANCE REPAIRED CRACK AT FRAME 25 IAW COEX EC 5310-01200. LT INBOARD CUTOUT REWORKED IAW COEX EC 5310-01201. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001091000388 20010910 00388 EU 2001 9 10 C2XA01BT162 1 20010830 A 3320 E036601 SOCKET AEROSP ATR42 ATR42320 8680930 EU CABIN BURNED A C2XA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 11835 194 EWR---CO3384, CREW REPORTED, NOTICED ELECTRICAL BURNING SMELL IN AFT CABIN AREA, COULD NOT ISOLATE. TURNED OFF ALL CABI N LIGHTS, STILL SMELLED. TURNED OFF RECIRCULATION FANS NR 1 AND 2, STILL SMELLED. MAINTENANCE TROUBLESHOT AIRCRAFT, FO UND BURNT LIGHT SOCKET IN SEAT ROW 7A/B OF SIDEWALL LIGHTS. INSTALLED NEW SOCKET. OPS CHECKED GOOD OF SIDEWALL LIGHTS IAW ATR42 MM 33-20-00. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001091000389 20010910 00389 EU 2001 9 10 C2XA01BT163 1 20010905 A 3234 F96GA0102 CONTROL HANDLE AEROSP ATR42 ATR42320 8680930 EU COCKPIT FAULTY A C2XA K NONE O OTHER UK UNKNOWN 1 SW 27 14830 184 EWR- 3064, CREW REPORTED, GEAR HANDLE DIFFICULT TO RETRACT THE GEAR. MAINTENANCE TROUBLESHOT SYSTEM AND REMOVED AND REP LACED LANDING GEAR CONTROL HANDLE IAW ATR42 JIC 32-31-81. OPS CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001091000390 20010910 00390 EU 2001 9 10 C2XA01BT164 1 20010827 A 5720 FITTING AEROSP ATR42 ATR42320 8680930 EU RT WING DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16824 166 YUL- DURING 4C INSPECTION YUL MAINTENANCE, AS PER COEX 5710-01025, INSPECTED AND REWORKED THE RT REAR WING SPAR FITTINGS BETWEEN WING RIBS 7/8 AND RIB 12. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2001091000391 20010910 00391 EU 2001 9 10 C2XA01BT165 1 20010825 A 5320 SPLICE AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16824 166 YUL- DURING 4C INSPECTION YUL MAINTENANCE FOUND HEAVY CORROSION AT FR9 ON EACH SIDE OF THE SPLICE AT BL 0. RT SIDE OF F R9 REPAIRED IAW ATR42 SRM 53-11-40 FIGURE 403. LT SIDE REPAIRED AS PER COEX EC5310-01204. AIRCRAFT RETURNED TO SERVICE . 2 H 7 2 4T RT A53EU 2001091000392 20010910 00392 SO 2001 9 10 C2XA01CL199 1 20010828 A 2530 1095A COFFEEMAKER EMB 145 EMB145LR SO GALLEY BURNED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 17984 145246 CLE FLIGHT 3062, THE CREW REPORTED A BURNING SMELL COMING FROM GALLEY HOT JUG. MAINTENANCE INSPECTED AND REPLACED THE G ALLEY HOT JUG. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001091000393 20010910 00393 SO 2001 9 10 C2XA01IA349 1 20010827 A 5713 12004367002 STRINGER EMB 120 EMB120ER 3260203 SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27716 120128 IAH - DURING MAINTENANCE INSPECTION, STRINGER 10 OF THE RIGHT WING WAS FOUND TO BE CRACKED AFT OF ACCESS PANEL 622EB. M AINTENANCE PERFORMED A SPLICE REPAIR OF THE AFFECTED STRINGER IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHANGE EC5710-01010, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001091000394 20010910 00394 SO 2001 9 10 C2XA01IA351 1 20010830 A 2750 3631101007 CONTROL HANDLE EMB 145 EMB145LR SO COCKPIT DIRTY A C2XA A UNSCHED LANDING N FALSE WARNING UK UNKNOWN 1 SW 27 13908 145465 IAH - FLIGHT 3745, THE CREW REPORTED A LANDING GEAR AURAL WARNING IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LAND ED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND CLEANED THE FLAP CONTROL LEVER. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE AFTER SATISFACTORY COMPLETION OF OPERATIONAL CHECKS. 2 L 7 2 4T RT T00011AT 2001091000395 20010910 00395 SO 2001 9 10 C2XA01IA352 1 20010831 A 3350 7287580509 LIGHT EMB 145 EMB145LR SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13979 145181 IAH - FLIGHT 4256, DURING PREFLIGHT INSPECTION, THE CREW REPORTED AN AISLE PATH EMERGENCY EXIT LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF LIGHT STRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI CE. 2 L 7 2 4T RT T00011AT 2001091000396 20010910 00396 SO 2001 9 10 C2XA01IA354 1 20010903 A 5610 163500110 WINDSHIELD EMB 145 EMB145ER SO COCKPIT CRACKED A C2XA B EMER. DESCENT O OTHER AP APPROACH 1 SW 27 14943 5704 5704 145040 IAH - FLIGHT 3712, THE CREW REPORTED THAT THE FIRST OFFICERS WINDSHIELD SHATTERED ON APPROACH. THE CREW DECLARED AN EME RGENCY, PERFORMED AN EMERGENCY DESCENT, AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AFFECT ED WINDSHIELD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001091000397 20010910 00397 EU 2001 9 10 C2XA01IA355 1 20010904 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14815 104 IAH - DURING A-CHECK INSPECTION, THE FORWARD SECTION OF EMERGENCY AISLE PATH LIGHTING WAS FOUND TO BE INOPERATIVE. MAIN TENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. 2 H 7 2 4T RT A53EU 2001091000398 20010910 00398 SO 2001 9 10 C2XA01IA359 1 20010908 A 3260 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A C2XA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 27 22727 120177 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED A LEFT MAIN LANDING GEAR UNSAFE LIGHT. MAINTENANCE PERFORMED SEVER AL GEAR SWINGS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001091000399 20010910 00399 SO 2001 9 10 C2XA01TY103 1 20010905 A 5320 BRF24AD4 PLATE EMB 145 EMB145 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13990 145277 TYS DURING A SCHEDULED INSPECTION THE FORWARD DIGITAL PLATE LOCATED AT COCKPIT ENTRANCE WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION ON AND AROUND THE RIVETS. MAINTENANCE CLEANED AND TREATED THE CORRODED AREAS, ALSO THE RIVETS WERE REPLAC ED IAW EMB-145 SRM 51-40-02 AND CPM 51-21-04, 05, &06. REPAIR WAS SATISFACTORY, AIRCRAFT WILL BE RELEASED FOR SERVICE U PON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001091000400 20010910 00400 SO 2001 9 10 C2XA01TY104 1 20010905 A 2612 3601133500230 FIRE LOOP EMB 145 EMB145 SO LT ENGINE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13990 3447 3447 145277 TYS DURING A SCHEDULED INSPECTION, THE LEFT HAND ENGINE FIRE LOOP WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPL ACED THE FIRE LOOP IAW EMB-145 26-11-01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THE INSPECTION. 2 L 7 2 4F RT T00011AT 2001091000401 20010910 00401 SO 2001 9 10 C2XA01TY105 1 20010905 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13990 145277 TYS DURING A SCHEDULED INSPECTION THE CENTER OMEGA BEAM TOP CAP BETWEEN FRAMES 19 & 23 WAS FOUND TO BE CORRODED. MAINT ENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB-145 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE REL EASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001091000402 20010910 00402 SO 2001 9 10 C2XA01TY106 1 20010905 A 5320 14522459003 SUPPORT EMB 145 EMB145 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13990 145277 TYS DURING A SCHEDULED INSPECTION THE RAMP SUPPORT ON THE CENTER OMEGA BEAM BETWEEN FRAMES 19 & 21 WAS FOUND TO BE CORR ODED. MAINTENANCE REMOVED AND REPLACED THE RAMP SUPPORT IAW EMB-145 SRM 51-40-02, REPAIR WAS SATISFACTORY. THE AIRCRAF T WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001091000403 20010910 00403 SO 2001 9 10 C2XA01TY107 1 20010906 A 7110 14575065001 FLANGE EMB 145 EMB145 SO RT ENGINE SCRATCHED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13990 145277 TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND ENGINE INLET UPPER COWL MOUNT FLANGE AT THE 12 O'CLOCK POSITION WAS FO UND TO BE SCRATCHED. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW EMB GST-3097/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001091000404 20010910 00404 SO 2001 9 10 C2XA01TY108 1 20010906 A 5260 STEP EMB 145 EMB145 SO ENTRY DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13990 145277 TYS DURING A SCHEDULED INSPECTION THE FLOOR GUSSET LOCATED AFT OF THE COCKPIT ENTRANCE STEP WAS FOUND TO HAVE SEVERAL A REAS OF CORROSION AROUND THE RIVETS. MAINTENANCE TREATED THE CORRODED AREAS AND REMOVED AND REPLACED THE RIVETS IAW EMB -145 SRM 51-40-02 AND CPM 51-21-04, 05 & 06. THE REPAIR WAS SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001091000405 20010910 00405 NM 2001 9 10 CALA0100817 1 20010829 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 947 - 967, RBL 30 AND STA 967-987, RBL 16. THE FLOOR SUPPORTS WERE REMO VED AND REPLACED IAW ECRA 5310-03585. 2 L 7 2 4F RT A16WE 2001091000406 20010910 00406 NM 2001 9 10 CALA0100818 1 20010829 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND THREE FLOOR SUPPORTS CORRODED AT STA 950 FROM RBL 24 TO RBL 53. THE FLOOR SUPPORTS WERE REMOVED AND RE PLACED IAW ECRA 5310-03585. 2 L 7 2 4F RT A16WE 2001091000407 20010910 00407 WP 2001 9 10 CALA0100826 1 20010831 A 3230 RESTRICTOR VALVE DOUG DC10 DC1030 3023501 WP DOWNLOCK CYL FAILED A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 39081 47861 THE LT MLG WOULD NOT RETRACT AFTER TAKEOFF FROM NRT. A VISUAL CHECK CONFIRMED THE GEAR WAS DOWN. THE AIRCRAFT WAS RETU RNED TO NRT WHERE IT LANDED WITHOUT INCIDENT. THE LT MLG RETRACT CYLINDER WAS REMOVED AND REPLACED, BUT THE PROBLEM REM AINED. MAINTENANCE FOUND THE LT MLG DOWNLOCK CYLINDER RESTRICTOR AT FAULT. THE DOWNLOCK CYLINDER RESTRICTOR WAS REPLAC ED. THE LT MLG WAS SWUNG IAW MM 32-30-00, PAGE 501 AND OPERATION CHECKED GOOD. 2 L 7 3 4F A22WE 2001091000408 20010910 00408 NM 2001 9 10 ZW0A0106302 1 20010803 A 5330 SKIN BOEING 757 7572Q8 1384972 NM FUSELAGE DENTED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 707TW 27625 DURING MAINTENANCE SMALL DENTS WERE DISCOVERED AT FLIGHT STATION 640 AND WL 200. REMOVED OLD EXTERNAL DOUBLER ALSO REMO VED DOUBLER FROM NEW DAMAGED AREA AND INSTALLED NEW EXTERNAL DOUBLER PER SRM BETWEEN STN. 640 TO 196 AND BETWEEN STN. 19 6 AND 216. 2 L 7 2 4F RT A2NM 2001091000409 20010910 00409 WP 2001 9 10 ZW0A0107002 1 20010816 A 2410 696233B CSD DOUG DC9 DC983 3022083 WP RT ENGINE OVERTEMP A ZW0A A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 CE 13 9406W 53126 THE RH CSD OIL TEMP INCREASED. THE CSD WAS DISCONNECTED AND APU STARTED. SEVERAL MINUTES LATER THE FREQUENCY STARTED TO FLUCTUATE AND APU SPEED DROPPED. MADE UNSCHEDULED LANDING AT TPA. CHANGED THE RT CSD AND ADJUSTED THE APU LOAD STAT. 2 L 7 2 4F RT A6WE 2001091000410 20010910 00410 WP 2001 9 10 ZW0A0107102 1 20010818 A 2170 VALVE DOUG DC9 DC982 3022082 WP A/C BAY CONTAMINATED A ZW0A D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 13 918TW 49367 DURING TAXI SMOKE WAS NOTED IN THE CABIN DUE TO INTERNAL CONTAMINATION. REMOVED AND REPLACED WATER SEPARATOR VALVE P/N 179460-8-1. PREFORMED BORESCOPE E2 AND PACK BURN PER MD94906 AND M-SHEET M97207. 2 L 7 2 4F A6WE 2001091000411 20010910 00411 WP 2001 9 10 ZW0A0107202 1 20010821 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 959U 49704 THE EGRESS LIGHTS WERE INOPERATIVE FROM ROWS 21 TO 26. REPLACED BROKEN CONTACT ON POWER STRIP AT THE LIGHT TRACK. 2 L 7 2 4F A6WE 2001091000412 20010910 00412 NM 2001 9 10 ZW0A0107203 1 20010821 A 3350 CONNECTOR BOEING 767 76733AER 1385230 NM CABIN LOOSE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 637TW 25403 THE EGRESS LIGHT WAS INOPERATIVE AT THE LEFT REAR LAVATORY. SECURED FEEDER CABLE CONNECTOR FOR THE EGRESS LIGHT AT THE L EFT LAV. 2 L 7 2 4F RT A1NM 2001091000413 20010910 00413 WP 2001 9 10 ZW0A0107204 1 20010817 A 5320 DOUBLER DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT THE LT MAIN WHEEL WELL REPAIR DOUBLER WAS CRACKING, ONE INCH LONG AFT EDGE OF THE WHEEL WELL. REMO VED CRACKED DOUBLER AND REPLACED WITH NEW PER SPM 6-70-01 AND SRM 51-30-05. 2 L 7 2 4F RT A6WE 2001091000414 20010910 00414 WP 2001 9 10 ZW0A0107205 1 20010817 A 5320 CHANNEL DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 922TW 48013 DURING CHECK-C MAINT FOUND L-2 HAT SECTION CRACKED AT STA 1418, LT SIDE. REPAIRED PER 53-02 FIG 18. PRIMED AND PAINTED PER SRM 51-10-03. INSTALLED FASTENERS PER SRM 51-30-05. 2 L 7 2 4F A6WE 2001091000415 20010910 00415 NE 2001 9 10 ZW0A0107303 2 20010822 A 7261 STUD DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE NR 1 ENGINE BACKED OUT A ZW0A E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 13 926TW 49356 1409 EXPERIENCED AN OIL LOSS ON THE NUMBER 1 ENGINE. SHUT DOWN THE ENGINE AND LANDED AT IND. FOUND OIL FILTER HOUSING STUDS HAD PULLED OUT. WAS NECESSARY TO REPLACE THE ENGINE DUE TO THE TIME THE ENGINE HAD RUN WITH NO OIL. CHECK-C 8-29-00 STL . 2 L 7 2 4F 4 F A6WE E9NE 2001091000416 20010910 00416 WP 2001 9 10 ZW0A0107401 1 20010822 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT FOUND CORROSION ON RH TIE DOWN TRACK, OTBD FLANGE, STA 1212 TO 1322. REMOVED CORRODED TRACK. FABR ICATED NEW TRACK AND PAINTED TRACK. INSTALLED NEW TRACK PER SPM 6-70-01, PAGE 2 AND 3. FASTENER INSTALLATION PER 51-30 AND 51-10-4. 2 L 7 2 4F RT A6WE 2001091000417 20010910 00417 WP 2001 9 10 ZW0A0107402 1 20010822 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND LT TIE DOWN TRACK WITH CORROSION, OTBD FLANGE, STA 1220 TO 1322. REMO VED AND REPLACED CORRODED TRACK PER SRM 6-70-01, USING PROPER FASTENERS PER SRM 51-30-1 AND SRM 51-10-3. 2 L 7 2 4F RT A6WE 2001091000418 20010910 00418 WP 2001 9 10 ZW0A0107403 1 20010822 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT ON RH FLOOR/SIDEWALL, FOUND MEMBRANE CRACKED AT STA 220, LONGERON 18R. INSTALLED DOUBLER OVER CRAC K PER SRM 53-01, FIG 4, SHEET 3. 2 L 7 2 4F RT A6WE 2001091000419 20010910 00419 WP 2001 9 10 ZW0A0107404 1 20010823 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT FOUND IN MID CABIN, LT SIDE, CORROSION ON MEMBRANE AT STA 712, LONGERON 18L. CUT OUT CORROSION ON MEMBRANE. INSTALLED DOUBLER PER SRM 51-70-4. 2 L 7 2 4F RT A6WE 2001091000420 20010910 00420 WP 2001 9 10 ZW0A0107405 1 20010823 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT IN RH CABIN SIDEWALL, FOUND CORROSION ON MEMBRANE AT STA 522 TO 541, LONGERON 18R. CUT OUT CORROSI ON ON MEMBRANE. INSTALLED DOUBLER PER SRM 51-70-4. 2 L 7 2 4F RT A6WE 2001091000421 20010910 00421 WP 2001 9 10 ZW0A0107501 1 20010824 A 2160 60714621 AMPLIFIER DOUG DC9 DC932 3022066 WP CABIN TEMP DEFECTIVE A ZW0A H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 13 931L 47173 TWO TIMES IN FLIGHT THE RH TEMPERATURE CONTROL VALVE WENT FULL HOT IN AUTO. WAS OK IN MANUAL CONTROL. CHANGED THE RH TE MPERATURE CONTROL AMPLIFIER, PN 607146-2-1. CHANGED BOTH WATER SEPARATORS ACCOUNT SMOKE CONTAMINATION, PN 1794608-1. CH ECK-C 7-4-00 MCI. 2 L 7 2 4F A6WE 2001091000422 20010910 00422 NM 2001 9 10 ZW0A0107503 1 20010826 A 3350 6100928 LIGHT BOEING 767 7673Y0 NM L2 DOOR INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 632TW 24953 THE EGRESS RED LIGHT AT THE LEFT SIDE NUMBER 2 CABIN DOOR WAS INOPERATIVE. REPLACED THE LAMP. 2 L 7 2 4F RT A1NM 2001091000423 20010910 00423 NM 2001 9 10 ZW0A0107504 1 20010826 A 3350 767 LIGHT BOEING 767 767* NM EXTERIOR INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 632TW 24953 THE OUTSIDE EMERGENCY LIGHT AT THE RH SIDE NUMBER 2 CABIN DOOR WAS INOPERATIVE. REPLACED THE LAMP. 2 L 7 2 4F RT A1NM 2001091000425 20010910 00425 NM 2001 9 10 UPS01236727 1 20010828 A 2611 SMOKE DETECTOR BOEING 727 727247 138408F NM MAIN CARGO BAY MALFUNCTIONED A IPXA A UNSCHED LANDING N FALSE WARNING UK UNKNOWN 1 SO 01 211UP 21700 INSPECTION TYPE:IN MAIN CARGO SMOKE DETECTION SYSTEM (RT SIDE) WARNING LIGHT ILLUMINATED IN FLIGHT. AC DIVERTED TO IND. LIGHT EXTINGUISHED WHEN MAIN CARGO DOOR OPENED. NO EVIDENCE OF SMOKE FOUND. WHILE TESTING SYSTEMS, NR 3 SYSTEM RIGHT DET ECTOR LIGHT STAYED ILLUMINATED. R&R NR 3 R SMOKE DETECTOR PER MM 26-17-00 OPS CK GOOD. 2 L 7 3 4F A3WE 2001091100019 20010911 00019 EA 2001 9 11 COMA0160702 1 20010909 A 2760 270003 PCU CNDAIR CL600 CL6002B19 EA WING FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 927CA 17846 7031 FLIGHT #5285. DURING TAXI OUT RECEIVED A LEFT SPOILER CAUTION MESSAGE, AIRCRAFT RETURNED TO THE GATE.REPLACED THE LEFT INBOARD FLIGHT SPOILER POWER CONTROL UNIT. 2 L 7 2 4F RT A21EA 2001091100020 20010911 00020 EA 2001 9 11 COMA0160703 1 20010908 A 2741 83963 ACTUATOR CNDAIR CL600 CL6002B19 EA EMPENNAGE FAULTY A COMA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 929CA 3377 7035 FLIGHT #5531. WHILE PARKED AT THE GATE PRIOR TO DEPARTURE RECEIVED A STAB. CH #2 TRIM INOPERATIVE MESSAGE.REPLACED THE HORIZONTAL STABILIZER TRIM ACTUATOR. 2 L 7 2 4F RT A21EA 2001091100021 20010911 00021 EA 2001 9 11 COMA0160704 1 20010908 A 2741 70623 MOTOR CNDAIR CL600 CL6002B19 EA EMPENNAGE FAULTY A COMA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 929CA 14594 7035 FLIGHT #5531. WHILE PARKED AT THE GATE PRIOR TO DEPARTURE RECEIVED A STAB CH #2 TRIM INOPERATIVE MESSAGE.REPLACED THE H ORIZONTAL STABILIZER TRIM MOTOR CONTROL UNIT. 2 L 7 2 4F RT A21EA 2001091100022 20010911 00022 EA 2001 9 11 COMA0160705 1 20010909 A 5270 DOOR CNDAIR CL600 CL6002B19 EA A COMA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SO 01 937CA 7044 FLIGHT #5300. DURING CLIMB OUT OF CAE THE CARGO DOOR CAUTION MESSAGE ACTIVATED, AIRCRAFT RETURNED TO THE FIELD AND LANDE D SAFELY.DEFERRED THE CARGO DOOR INDICATION IN ACCORDANCE WITH MEL 52-70-04. 2 L 7 2 4F RT A21EA 2001091100023 20010911 00023 EA 2001 9 11 COMA0160706 1 20010910 A 5553 60021061 BUSHING CNDAIR CL600 CL6002B19 EA VERTICAL STAB WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 949CA 14350 7080 HORIZONTAL STABILIZER RHS VERTICLE BUSHING WORN.REMOVED R/H VERTICAL STAB BUSHING P/N 600-21061 INSTALLED NEW BUSHING AL T P/N 600-21061-7/SB I/A/W CRJ MM 20-26-00-910-803 FINAL REAMED BUSHING 1.50 I/A/W CANADAIR REO 601R-55-11-022 MACHINED BUSHING HAT I/A/W WVAC EO 601R-55-2707. 2 L 7 2 4F RT A21EA 2001091100024 20010911 00024 WP 2001 9 11 ABXA010465 1 20010814 A 5300 992341931 PANEL DOUG DC9 DC933F 302207A WP CABIN CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 RIGHT SLANT PANEL WAS CORRODED AROUND NUTPLATES ON THE LOWER EDGE OF PANEL. LEVEL II CORROSION. INSTALLED NEW SLANT PANE L IAW DC-9 SRM. 2 L 7 2 4F A6WE 2001091100025 20010911 00025 WP 2001 9 11 ABXA010466 1 20010814 A 5300 992341929 PANEL DOUG DC9 DC933F 302207A WP CABIN CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 LEFT SLANT PANEL WAS CORRODED AROUND THE LOWER NUTPLATES. LEVEL II CORROSION. INSTALLED NEW SLANT PANEL IAW DC-9 SRM 51- 30-1. 2 L 7 2 4F A6WE 2001091100026 20010911 00026 WP 2001 9 11 ABXA010467 1 20010816 A 5300 39248461 FITTING DOUG DC9 DC933F 302207A WP LEFT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 LEFT SLANT PANEL, OUTBOARD ATTACH FITTING WAS CORRODED. REPLACED FITTING IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2001091100027 20010911 00027 EU 2001 9 11 AWXA0002216 1 20010911 A 5315 D533726130040 FITTING AIRBUS 320 A320232 3930326 EU STRG 42R FR43 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 639AW 471 Discrepancy/Corrective Action: RH MLG Door Actuator Fitting PN# D533-72613-60400, Fastener Hole Has Corrosion.Corrective Action: Repaired As Per AWA ER 26-5315-01250-JS2 2 L 7 2 4F RT A28NM 2001091100028 20010911 00028 NM 2001 9 11 USAA011021 1 20010807 A 5330 SKIN BOEING 737 7374B7 1384702 NM BS 1074 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 24893 CLT - FOUND SKIN WITH PREVIOUSLY INSTALLED REPAIR 1 INCH BY 4 INCH, STATION 1074 BETWEEN S17R AND S14R. PREVIOUSLY INST ALLED DOUBLER AND TRIPLER PER SRM 53-00-01 FIG 210 SHEET 3. (M) 2 L 7 2 4F RT A16WE 2001091100029 20010911 00029 NM 2001 9 11 USAA011004 1 20010807 A 5300 SKIN BOEING 737 7374B7 1384702 NM DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 24893 CLT - FOUND SKIN DENTED 12.5 INCH BY 5 INCH, LEFT SIDE AT STATION 420 STRINGERS 15 THROUGH 17. INSTALLED DOUBLER PER SR M 53-00-01. (M) 2 L 7 2 4F RT A16WE 2001091100030 20010911 00030 NM 2001 9 11 USAA011092 1 20010814 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND FLOORBEAM CRACKED .5 INCHES, BS 520 TO RBL 24 AND LBL 24. INSTALLED DOUBLER PER EA 85215. (M) 2 L 7 2 4F A16WE 2001091100031 20010911 00031 NM 2001 9 11 USAA011093 1 20010814 A 5300 WEB BOEING 737 737201 1384454 NM BS 927-947 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND CREASE BEAM WEB CORRODED 10 SQUARE INCHES, LEFT SIDE BS 927-947. FABRICATED NEW WEB PER DRAWING 65-52878 AN D INSTALLED PER SRM 51-30-2. (M) 2 L 7 2 4F A16WE 2001091100032 20010911 00032 NM 2001 9 11 USAA011085 1 20010814 A 5300 STRINGER BOEING 737 737201 1384454 NM BS 359 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND STRINGER CRACKED .5 INCH, BS 359 S11L. REMOVED AND REPLACED PART WITH PART NR 1126212 PER 51-10-1. (M) 2 L 7 2 4F A16WE 2001091100033 20010911 00033 NM 2001 9 11 USAA011086 1 20010814 A 5300 ANGLE BOEING 737 737201 1384454 NM BS 328 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND ANGLE CRACKED .5 INCH, BS 328 FLOORBEAM RBL 31.5 TO INTERCOSTAL. FABRICATED REPAIR DOUBLER PER SRM 53-10-02 . (M) 2 L 7 2 4F A16WE 2001091100034 20010911 00034 NM 2001 9 11 USAA011087 1 20010814 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND FLOORBEAM CRACKED 1.5 INCH, BS 520 LBL 45. INSTALLED DOUBLER PER EA 85214. (M) 2 L 7 2 4F A16WE 2001091100035 20010911 00035 NM 2001 9 11 USAA011088 1 20010814 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND FLOORBEAM CORRODED 3 SQUARE INCHES, BS 1006 LBL 10. CORROSION LEVEL 1. REPLACED T-CAP PER SRM 53-10-9. (M ) 2 L 7 2 4F A16WE 2001091100036 20010911 00036 NM 2001 9 11 USAA011089 1 20010814 A 5300 SKIN BOEING 737 737201 1384454 NM BS 309 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND SKIN DENTED AND GOUGED 1 INCH BY .070 INCH, BS 309 JUST BELOW BS 24R. FABRICATED AND INSTALLED FILLERS AND REPAIR DOUBLERS PER SRM 53-30-3 FIG 42. (M) 2 L 7 2 4F A16WE 2001091200005 20010912 00005 NM 2001 9 12 USAA011100 1 20010820 A 5300 WEB BOEING 737 737201 1384454 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND FLOORBEAM WEB CORRODED, BS 344 FLOORBEAM, LBL 14.5 TO 21.5. CORROSION LEVEL 1, TASK NR C53-107-01. BLENDED OUT CORROSION, INSTALLED DOUBLER AND TRIPLER PER EA 85198. (M) 2 L 7 2 4F A16WE 2001091200006 20010912 00006 NM 2001 9 12 USA011101 1 20010820 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE UNKNOWN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND FLOORBEAM NO CRACKS PER NDT, BS 520 RBL 45. INSTALLED DOUBLER PER EA 85214. (M) 2 L 7 2 4F A16WE 2001091200007 20010912 00007 NM 2001 9 12 USAA011103 1 20010820 A 5300 TIE CLIP BOEING 737 737201 1384454 NM BS 596 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND TIE CLIP WITH WRONG TYPE CLIP INSTALLED, BS 596-S9L. INSTALLED NEW TIE CLIP PER EO NR 5393G227. (M) 2 L 7 2 4F A16WE 2001091200008 20010912 00008 NM 2001 9 12 USA011106 1 20010820 A 5330 SKIN BOEING 737 737201 1384454 NM CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND SKIN CRACKED, AFT ENTRY DOOR LOWER HINGE CUTOUT. INSTALLED DOUBLER AND TRIPLER PER SRM 53-30-3 FIG 34. (M) 2 L 7 2 4F A16WE 2001091200009 20010912 00009 NM 2001 9 12 USAA011129 1 20010821 A 5700 WEB BOEING 737 7373B7 1384580 NM BS 685 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 385US 46895 22958 CLT - FOUND ON WALKAROUND, WEB CRACKED .5 INCH AND .125 INCH, WHEEL WELL CEILING AT LBL 30 BS 685. INSTALLED DOUBLER PER TR 53-60-04. (M) 2 L 7 2 4F RT A16WE 2001091200010 20010912 00010 NM 2001 9 12 USAA011113 1 20010820 A 5300 FRAME BOEING 737 7374B7 1384702 NM BS 827 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 28481 24893 CLT - FOUND FRAME DENTED .5 INCH BY .5 INCH BY .035 INCH, BS 827 STRINGER 24-251. INSTALLED FRAME DOUBLER PER TR 53-60- 07. (M) 2 L 7 2 4F RT A16WE 2001091200011 20010912 00011 NM 2001 9 12 USAA011112 1 20010820 A 5300 STIFFENER BOEING 737 7374B7 1384702 NM BS 900 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 28481 24893 CLT - FOUND STIFFENER CRACKED .5 INCH, BS 900 STRINGER 11L. INSTALLED NEW PART PER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 2001091200012 20010912 00012 NM 2001 9 12 USAA011111 1 20010820 A 5300 WEB BOEING 737 7374B7 1384702 NM BS 297 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 28481 24893 CLT - FOUND WEB CRACKED .5 INCH, BS 297 BS 9R CUTOUT STRUCTURE. INSTALLED REPAIR AND REPAIR PARTS PER SRM 51-40-02. (M ) 2 L 7 2 4F RT A16WE 2001091200013 20010912 00013 NM 2001 9 12 USAA011110 1 20010820 A 5310 FRAME BOEING 737 7374B7 1384702 NM BS 907L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 28481 24893 CLT - FOUND FRAME CRACKED .75 INCH, INBOARD RIVET BETWEEN STRINGER 8-9 AT BS 907L. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001091200014 20010912 00014 NM 2001 9 12 USAA011109 1 20010820 A 5330 SKIN BOEING 737 7374B7 1384702 NM BS 400 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 31027 24893 CLT - FOUND SKIN DENTED .063 INCH BY 4.125 INCH, BS 400 BETWEEN S16L ND S17L. REPLACED DOUBLER AND FILLERS PER SRM 53-0 0-01 FIG 227 DETAIL X11. (M) 2 L 7 2 4F RT A16WE 2001091200015 20010912 00015 NM 2001 9 12 USAA011108 1 20010820 A 5300 SKIN BOEING 737 737401 1384701 NM BS 727D CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 36713 23886 CLT - FOUND SKIN CRACKED 2 INCHES, BS 727D PLUS 17 INCHES STRINGER 24R. INSTALLED DOUBLER PER SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2001091200016 20010912 00016 NM 2001 9 12 USAA011107 1 20010820 A 5300 SKIN BOEING 737 737401 1384701 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 36713 23886 CLT - FOUND SKIN CRACKED 1 INCH, BS 727 D AND 3 INCHES AT STRINGER 23L. INSTALLED DOUBLER PER TR 53-60-03. (M) 2 L 7 2 4F RT A16WE 2001091200017 20010912 00017 NM 2001 9 12 USAA011096 1 20010815 A 5300 SKIN BOEING 737 737401 1384701 NM BS 1016 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 411US 37994 23880 CLT - FOUND SKIN OIL CAN IN AFT PRESSURE BULKHEAD, BS 1016. INSTALLED DOUBLER PER SRM 53-80-08 FIG 201. (M) 2 L 7 2 4F RT A16WE 2001091200051 20010912 00051 NM 2001 9 12 01FDEA00810 1 20010907 A 3244 TIRE BOEING 727 7272S2F 1384O81 NM NR 3 FAILED A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 217FE 22938 WHEEL WELL FIRE LIGHT CAME ON WITH GLARESHIELD. REMOVED AND REPLACED NR 3 & 4 TIRE ASSY AND NR 3 WHEEL TRANSDUCER PER M M 32-45-001-4, 32-2-001-4. 2 L 7 3 4F A3WE 2001091200052 20010912 00052 WP 2001 9 12 01FDEA00811 1 20010905 A 5312 PRESSURE PANEL DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 310FE 48299 CTR WHEEL WELL, LT SIDEWALL, LWR FWD CORNER, CORROSION UNDER SEALANT, AROUND ACCESS PNL. 2 L 7 3 4F RT A22WE 2001091200053 20010912 00053 NM 2001 9 12 01FDEA00815 1 20010908 A 2613 CONNECTOR BOEING 727 727232 1384082 NM OVERHEAT LOOP DIRTY A FDEA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CL CLIMB 1 SO 25 497FE 20866 ON DEPARTURE NR 3 STRUT O/H LIGHT CAME ON. REMOVED, CLEANED NR 3 ENG LOOP CONNECTOR PER MM REF ATA 20. RESECURED STRUT PANELS. 2 L 7 3 4F A3WE 2001091200054 20010912 00054 NM 2001 9 12 01FDEA00816 1 20010908 A 2750 FLAP DOUG MD11 MD11F 3023600 NM WING VIBRATION A FDEA O OTHER E VIBRATION/BUFFET AP APPROACH 1 SO 25 605FE 48514 VIBRATION ON SELECTING FLAPS TO 50 DEG. NO PROBLEMS FOUND ON FLT CONTROL INSP. AC OK FOR SERVICE. 2 L 7 3 4F RT A22WE 2001100900152 20011009 00152 NM 2001 10 9 01FDEA00818 1 20011002 A 3230 69139017 SEQUENCE VALVE BOEING 727 727232 1384082 NM LEFT WING CORRODED A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 498FE 20867 01-327 AFT GEAR IN UP POSITION L/G DOOR LIGHT REMAIN ON. R/R NR 1 & 2 ENGINE DRIVEN HYD PUMPS PER MM 29-11-000-2. & LG LOCK OPERATING SEQ VALVE. 2 L 7 3 4F A3WE 2001092100026 20010921 00026 NM 2001 9 21 01FDEA00823 1 20010907 A 5521 RIB BOEING 727 727247 138408F NM ELEVATOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 RT HORIZ NR1 ELEVATOR HINGE RIB O/B LUG, O/B FACE HAS CORROSION (C55-391-20-3). REMOVED AND REPLACED PER EA 7-550-59272. 2 L 7 3 4F A3WE 2001091200055 20010912 00055 EU 2001 9 12 2001F00266 1 20010910 A 2150 9599020111 A/C PACK PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL ENGINE BAY INOPERATIVE A S4WA K NONE O OTHER TX TAXI/GRND HDL 1 WP 07 317NA 2567 2567 223 0294 HJ736 ECS SYSTEM WOULD NOT COOL BELOW AMBIENT TEMPERATURE NO MATTER WHAT POSITION THE CONTROL WAS IN, AUTO OR MANUAL. AFTER T ROUBLESHOOTING SYSTEM AND TALKING TO TECH REPS, CHANGED COOLING TURBINE AND HEAT EXCHANGER. OPERATIONAL AND FUNCTIONAL CHECKED OK. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001091200056 20010912 00056 NM 2001 9 12 CALA0100827 1 20010903 A 3230 CONTROL CABLE BOEING 737 7373T0 1384582 NM RT MLG OUT OF RIG A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 70352 23590 THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM DTW. THE AIRCRAFT WAS DIVERTED TO CLE WHERE IT LANDED WITHOUT INC IDENT. TROUBLESHOOTING FOUND THE RT MLG TELEFLEX CABLE OUT OF RIG. THE TELEFLEX CABLE WAS RIGGED AND AN ADJUSTMENT/TES T WAS PERFORMED IAW MM 32-09-01. THE GEAR WAS SWUNG AND OPERATION CHECKED GOOD. 2 L 7 2 4F RT A16WE 2001091200057 20010912 00057 NE 2001 9 12 CALA0100828 2 20010831 A 7510 777793 DUCT DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE NR 2 ENGINE BLOWN A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 14889 49118 THE CREW RECEIVED A FIRE WARNING INDICATION FROM THE RT ENGINE DURING CLIMBOUT OF IAH. THE THROTTLE WAS RETARDED AND TH E FIRE WARNING INDICATION WENT OUT. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOU ND THE NR 2 ENGINE 8TH STAGE ANTI-ICE DUCT BLOWN AND WIRING HARNESS DAMAGE. THE ANTI-ICE DUCT WAS REPLACED IAW MM 75-10 -02 AND THE WIRING WAS REPAIRED. THE ENGINE WAS RUN WITH NO LEAKS NOTED AND OPERATION CHECKED GOOD. 2 L 7 2 4F 4 F A6WE E9NE 2001091200058 20010912 00058 WP 2001 9 12 CALA0100837 1 20010907 A 3350 AD4002P BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16808 49262 INSPECTION FOUND PORTABLE EMERGENCY EXIT LIGHT AT MAIN CABIN DOOR INOPERATIVE. THE BATTERIES FOR THE PORTABLE EMERGENCY EXIT LIGHT WERE REMOVED AND REPLACED IAW MM 33-53-00. 2 L 7 2 4F A6WE 2001091200059 20010912 00059 NM 2001 9 12 CALA0100838 1 20010907 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND FLOOR SUPPORT CORRODED AT FASTENER HOLE AFT OF STA 787, BL 0. A REPAIR WAS INSTALLED IAW SRM 53-00-53. 2 L 7 2 4F RT A16WE 2001091200060 20010912 00060 WP 2001 9 12 CALA0100839 1 20010907 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND CUSP ANGLE CORRODED AT FS 207, LBL 54. THE CUSP ANGLE WAS REMOVED AND A NEW CUSP ANGLE WAS INSTALLED I AW SRM 51-30-1 AND EA 9-5310-2-A0917. 2 L 7 2 4F A6WE 2001091200061 20010912 00061 WP 2001 9 12 CALA0100841 1 20010907 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND AFT LT LAV FLOOR SUPPORT CORRODED AT STA 1309-1338, L18L. THE CORROSION WAS REMOVED IAW SRM 51-10-3 AN D THE SUPPORT WAS REPAIRED IAW EA 9-5314-2-A0919 AND ECRA 5310-04182. 2 L 7 2 4F A6WE 2001091200063 20010912 00063 WP 2001 9 12 CALA0100842 1 20010907 A 5320 SPLICE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15820 49480 INSPECTION FOUND A .75 INCH CRACK ON LONGERON SPLICE AT L28L BETWEEN STA 218 AND 229. THE LONGERON SPLICE WAS REMOVED A ND A NEW SPLICE WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2001091200065 20010912 00065 WP 2001 9 12 CALA0100844 1 20010907 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15820 49480 INSPECTION FOUND UPPER SURFACE OF CENTER FLOOR SUPPORT CORRODED AT STA 1287-1307. THE CENTER FLOOR SUPPORT WAS REPAIRED IAW SRM 53-01, FIGURE 2. 2 L 7 2 4F A6WE 2001091200067 20010912 00067 WP 2001 9 12 CALA0100845 1 20010908 A 5320 STRAP DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15820 49480 INSPECTION FOUND A 6 INCH CRACK IN TAIL COMPARTMENT STRAP CAP AT STA 1446, LONGERONS 2R/2L. THE STRAP CAP WAS REMOVED A ND REPLACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 2001091200068 20010912 00068 WP 2001 9 12 CALA0100846 1 20010908 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15820 49480 INSPECTION FOUND A 1 INCH CRACK IN SUPPORT ANGLE ATTACHED TO AFT CROSSBEAM IN TAIL COMPARTMENT AT TORQUE TUBE, RT SIDE. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-02. 2 L 7 2 4F A6WE 2001091200069 20010912 00069 WP 2001 9 12 CALA0100847 1 20010909 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15820 49480 INSPECTION FOUND LT TRACK TIE DOWN FLANGES IN AFT PIT CORRODED AT STA 1212. THE LT TRACK TIE DOWN FLANGES WERE REPAIRED IAW SRM 51-30-0. 2 L 7 2 4F A6WE 2001091200070 20010912 00070 SO 2001 9 12 CHQ00021 1 20010830 A 7830 PANEL EMB 145 EMB145 SO THRUST REVERSER DEPARTED A CHQA O OTHER O OTHER CR CRUISE 1 GL 11 CHQ 145344 THRUST REVERSER PANEL FELL OFF. 2 L 7 2 4F RT T00011AT 2001091200071 20010912 00071 EU 2001 9 12 CHQ00022 1 20010821 A 5220 DOOR SAAB SF340 340B 7860101 EU EMERGENCY EXIT UNSECURE A CHQA K NONE O OTHER LD LANDING 1 GL 11 CHQ 035 RT OVERWING EMERGENCY EXIT FELL OPEN ON LANDING. 2 L 7 2 4T RT A52EU 2001091200072 20010912 00072 SO 2001 9 12 CHQOOO23 1 20010902 A 3230 LANDING GEAR EMB 145 EMB145 SO NLG & MLG MALFUNCTIONED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 CHQ 145345 LANDING GEAR NOT RETRACTING LEVER DISAGREE MESSAGE. 2 L 7 2 4F RT T00011AT 2001091200073 20010912 00073 WP 2001 9 12 CALA0100851 1 20010909 A 5320 WEB DOUG DC9 DC982 3022082 WP FS 1430 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND A 4" CRACK IN FRAME TO LONGERON ATTACH WEB IN AFT ACCESSORY AREA AT FS 1430, R/H SIDE. THE CRACK WAS ST OP DRILLED IAW SRM 53-01, FIGURE 2. A DOUBLER WAS INSTALLED IAW SRM 53-14-4, 51-10-4, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 2001091200074 20010912 00074 WP 2001 9 12 CALA0100852 1 20010909 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FS 200-218 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND SEAT TRACK CORRODED AT FS 200-218, LBL 45. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SEA T TRACK, SPLICE, AND TAB WERE INSTALLED IAW SRM 53-03, FIGURE 4B, 51-30-2, 51-10-4, 51-10-3, AND 53-05-4. 2 L 7 2 4F A6WE 2001091200075 20010912 00075 WP 2001 9 12 CALA0100853 1 20010909 A 5320 SHEAR TIE DOUG DC9 DC982 3022082 WP STA 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND A 1" CRACK IN SHEAR TIE AT STA 1418 BETWEEN LONGERON 1R AND 2R. THE SHEAR TIE WAS REMOVED AND A NEW SHE AR TIE WAS INSTALLED IAW SRM 53-03, 51-30-02, 51-10-3, AND 51-30-5. 2 L 7 2 4F A6WE 2001091200076 20010912 00076 WP 2001 9 12 CALA0100854 1 20010909 A 5280 WEB DOUG DC9 DC982 3022082 WP R/H MLG DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND A 1" CRACK IN R/H MLG WHEEL WELL DOOR LOWER WEB. A REPAIR WAS INSTALLED IAW EA 9-5281-2-A0920 AND ECRA 5281-01017. 2 L 7 2 4F A6WE 2001091200077 20010912 00077 WP 2001 9 12 CALA0100856 1 20010909 A 5320 WEB DOUG DC9 DC982 3022082 WP BY RUDDER SEC CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15820 49480 INSPECTION FOUND A 3/4" CRACK IN UPPER WEB IN TAIL COMPARTMENT ON L/H SIDE BY RUDDER SECTOR. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-01, PAGE 9. 2 L 7 2 4F A6WE 2001091200078 20010912 00078 WP 2001 9 12 CALA0100857 1 20010909 A 5320 BRACKET DOUG DC9 DC982 3022082 WP NWW FWD WALL CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15820 49480 INSPECTION FOUND ONE EACH 3/4" CRACK IN GUSSET ATTACH BRACKETS AT RIVET ATTACH ON L/H AND R/H SIDE OF NWW FWD WALL. A NE W STIFFENER WAS INSTALLED AT EACH LOCATION IAW SRM 53-14-1, FIGURE 4 AND 51-30-0. 2 L 7 2 4F A6WE 2001091200079 20010912 00079 NM 2001 9 12 CALA0100859 1 20010910 A 5754 PANEL BOEING 737 7373T0 1384582 NM #5 SLAT DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND O/B TRAILING EDGE OF #5 SLAT PANEL DELAMINATED. THE #5 SLAT ASSY WAS REMOVED AND REPLACED IAW MM 27-81- 21. 2 L 7 2 4F RT A16WE 2001091200080 20010912 00080 NM 2001 9 12 CALA0100861 1 20010911 A 5754 SLAT BOEING 737 7373T0 1384582 NM R/W #6 POSN. DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND R/H WING #6 L/E SLAT DELAMINATED AT UPPER SURFACE I/B END. THE SLAT WAS REPAIRED IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 2001091200081 20010912 00081 WP 2001 9 12 CALA0100862 1 20010912 A 5753 SKIN PANEL DOUG DC9 DC982 3022082 WP L/H I/B FLAP DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15820 49480 INSPECTION FOUND L/H I/B FLAP SKIN PANEL DENTED AFT OF MLG. A NEW SKIN PANEL WAS INSTALLED IAW SRM 51-30-1. 2 L 7 2 4F A6WE 2001091200082 20010912 00082 NM 2001 9 12 CALA0100863 1 20010912 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 843 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND L/H FUSELAGE SKIN DENTED AT STA 843 BETWEEN S22L AND S23L. THE DENTED AREA OF SKIN WAS CUT OUT AND A RE PAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 202. 2 L 7 2 4F RT A16WE 2001091200083 20010912 00083 NM 2001 9 12 CALA0100864 1 20010912 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 727E DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND R/H FUSELAGE SKIN DENTED AT STA 727E BETWEEN S21R AND S22R. THE DENTED AREA OF SKIN WAS CUT OUT AND A R EPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 208. 2 L 7 2 4F RT A16WE 2001091200087 20010912 00087 EU 2001 9 12 DHL2001362032 1 20010901 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU AFT DUCT INOPERATIVE A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 362DH 84 AFT DUCT SMOKE DETECTOR INOP. RESET ELECTRONIC SMOKE DETECTOR BOX, OPS CHECK IS GOOD IAW M/M 26-11-11. 2 L 7 2 4F RT A35EU 2001091200089 20010912 00089 NE 2001 9 12 DHL2001363020 2 20010908 A 7520 MANIFOLD AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650* 30018 NE NR 2 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 ON A-5 CHECK, NR 2 ENGINE LP TURBINE UPPER COOLING MANIFOLD CRACKED AT 10 O'CLOCK POSITION. REMOVED UPPER COOLING MANIF OLD NR 2 ENGINE ROUTED FOR REPAIR PER A-300 AMM 75-30-00. REINSTALLED SERVICEABLE UPPER COOLING MANIFOLD ON NR 2 ENGINE PER A-300 MM 75-30-00. OPS CHECK GOOD IAW AMM 75-30-00. 2 L 7 2 4F 4 F RT A35EU E23EA 2001091200090 20010912 00090 EU 2001 9 12 DHL2001364024 1 20010905 A 3610 LINE AIRBUS 300 A300B4203 3930306 EU PNEUMATIC SYS CHAFED A DHLA J B A DUMP FUEL EMER. DESCENT UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 01 364DH 141 DURING CLIMBOUT, SMOKE ANNUN ILLUMINATED. SHORTLY AFTER THE FLIGHT DECK SMOKE ILLUMINATED. RECEIVED A REGUL FAULT LIGH T, TEMP HI LIGHT, PACK FAULT ALL ON THE NR 1 SIDE. AFTER RUNNING THE APPROPRIATE CHECK LIST, AND SHUTTING OFF THE NR 1 PACK, THE LIGHTS EVENTUALLY EXTINGUISHED. FOUND NR 1 ENG AFT B-SUMP VENT AND PNEU SUPPLY TUBE HAD CHAFED THRU EACH- OTH ER. REMOVED AND REPLACED BOTH THE AFT VENT B-SUMP VENT AND PNEUMATIC SUPPLY LINE. AS FOR THE TEMP HI FAULT. REMOVED A ND REPLACED THE FAN AIR VALVE. OPS & LEAK CK'D OK IAW M/M 36-11-16, 36-11-00, 21-00-00, JRH CHAPT 18, & M/M 26-12-0. O K FOR CONTINUED SERVICE. 2 L 7 2 4F RT A35EU 2001091200091 20010912 00091 CE 2001 9 12 GLBA2001156 1 20010714 A 2150 A/C PACK BEECH 1900 1900D 1154162 CE A/C BAY MALFUNCTIONED A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 01 251GL UE251 LEFT ENVIRONMENTAL FAILURE ON T/O. COULD NOT DUPLICATE FAULT, RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 2001091200092 20010912 00092 NM 2001 9 12 2001F00267 1 20010801 A 3242 BRAKE DHAV DHC8 DHC8201 2809001 NM RT MLG SMOKE A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 17 986HA 421 ON LANDING ROLLOUT ATC REPORTED HEAVY SMOKE OFF RIGHT MLG. INSPECTED AND CLEANED RIGHT MAIN LANDING BRAKES, LEAK CHECKE D WITH PARKING BRAKE APPLIED AND DURING TAXI. NO DEFECT FOUND ALL OPERATION NORMAL IAW AIRCRAFT MM 32-40-00. (M) 2 H 7 2 4T RT A13NM 2001091200095 20010912 00095 NE 2001 9 12 2001F00268 2 20010826 A 7200 ENGINE BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE NR 2 FAILED A UIEA A UNSCHED LANDING B J Y SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION ENGINE STOPPAGE CR CRUISE 1 EA 15 512MC 21220 517938 AT FLT 310, NR 2 ENGINE FAILED. PROCEEDING FAILURE CREW COULD SMELL OIL SMELL, THEN ENGINE QUIT. N2 WENT TO ZERO ALSO ZERO OIL PRESSURE. N1 APPROXIMATELY 22 PERCENT. A/C DIVERTED TO BKK. (M) 2 L 7 4 4F 4 F A20WE E23EA 2001091200097 20010912 00097 NM 2001 9 12 BJNA010801 1 20010811 A 3350 LIGHT BOEING 737 737282 13844AT NM CABIN LOOSE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 233TM 23043 L3 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND RESEATED L3 DOOR LIGHT ASSEMBLY IAW 33-51-01, OPS CHECK GOOD. (M ) 2 L 7 2 4F RT A16WE 2001091200098 20010912 00098 NM 2001 9 12 BJNA010802 1 20010822 A 3350 62474 LIGHT BOEING 737 737282 13844AT NM CABIN INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 233TM 23043 ON WALK AROUND, DISCOVERED LUMINESCENT STRIP ON EMERGENCY TRACK LIGHTING INOPERATIVE. REMOVED AND REPLACED LUMINESCENT STRIP IAW LOETITE LUMINESCENT SYSTEMS, BMM 33-51-01, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001091200104 20010912 00104 WP 2001 9 12 WXOA01012B 1 20010821 A 5300 2777948 STRINGER DOUG DC9 DC951 3022051 WP FS 1022L CRACKED A WXOA K NONE O OTHER TX TAXI/GRND HDL 1 WP 17 411EA 47732 LAS - AIRCRAFT FUSELAGE DAMAGED BY GROUND SERVICE EQUIPMENT WITH AIRCRAFT POSITIONED AT GATE. DAMAGE IDENTIFIED AS PUNC TURED FUSELAGE SKIN AT FUSELAGE STATION 1022 LEFT BETWEEN LONGERON 24L AND 26L, AND CRACKED STRINGER AT FUSELAGE STATION 1022L LONGERON 26L. TEMP REPAIRS ACCOMPLISHED. AIRCRAFT FERRIED TO LCQ FOR REPAIRS. REPAIR STATION MAINTENANCE CUT O UT PUNCTURED AREA OF FUSELAGE SKIN AT FUSELAGE STATION 1022L. FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 53-04, FIGURE 12C. REMOVED AND REPLACED CRACKED STRINGER SECTION AT LONGERON 26L, FUSELAGE STATION 1022L IAW DC9 SRM 53-02, FIGURE 1 8. (M) 2 L 7 2 4F RT A6WE 2001091200105 20010912 00105 EU 2001 9 12 USAAF01066 1 20010822 A 3350 F0N96118D4L RELAY FOKKER F28 F28MK0100 4990807 EU PAX CABIN FAULTY A USAA K NONE O OTHER AP APPROACH 1 EA 19 850US 11276 PHL - FLT 2249 - EN-ROUTE MHT-PHL, THE EMERGENCY EXIT LIGHTS WOULDN'T ILLUMINATE WHEN THE LANDING GEAR WAS EXTENDED. MA INTENANCE REPLACED EXIT LIGHTING RELAY K2618A. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT 2001091200106 20010912 00106 NM 2001 9 12 USAA011083 1 20010810 A 5300 BEAM BOEING 737 7373B7 1384580 NM BS 957-986 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 588US 41171 23933 PIT - FOUND BEAM CORRODED 4 SQUARE INCHES, AFT SERVICE DOOR THRESHOLD STATION 957-986 RT. (M) 2 L 7 2 4F RT A16WE 2001091200107 20010912 00107 NM 2001 9 12 USAA011082 1 20010809 A 5300 FRAME BOEING 737 7373B7 1384580 NM BS 663.75 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 588US 41171 23933 PIT - FOUND FRAME WITH THREE CRACKS .25 INCH EACH, STRINGER CUT OUTS AT 5-2L, S-1, 5-2R STATION 663.75. (M) 2 L 7 2 4F RT A16WE 2001091200108 20010912 00108 NM 2001 9 12 USAA011081 1 20010810 A 5300 CREASE BEAM BOEING 737 7373B7 1384580 NM BS 727A CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 588US 41171 23933 PIT - FOUND CREASE BEAM CORROED 4 INCHES BY 1 INCH AROUND RIVETS, 10 INCHES AFT OF STATION 727A TOP SIDE CREASE BEAM, RI GHT SIDE. (M) 2 L 7 2 4F RT A16WE 2001091200109 20010912 00109 NM 2001 9 12 USAA011078 1 20010810 A 5300 FRAME BOEING 737 7373B7 1384580 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 588US 41171 23933 PIT - FOUND FRAME CRACKED .5 INCH, STATION 827 LEFT BETWEEN STRINGER 8/9. (M) 2 L 7 2 4F RT A16WE 2001091200110 20010912 00110 NM 2001 9 12 USAA011077 1 20010810 A 5300 FRAME BOEING 737 7373B7 1384580 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 588US 41171 23933 PIT - FOUND FRAME CRACKED .5 INCH, STATION 867 LEFT BETWEEN STRINGER 8/9. (M) 2 L 7 2 4F RT A16WE 2001091200111 20010912 00111 NM 2001 9 12 USAA011076 1 20010810 A 5300 FRAME BOEING 737 7373B7 1384580 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 588US 41171 23933 PIT - FOUND FRAME CRACKED .5 INCH, STATION 867 RIGHT BETWEEN STRINGER 8/9. (M) 2 L 7 2 4F RT A16WE 2001091200112 20010912 00112 NM 2001 9 12 USAA011075 1 20010810 A 5300 FRAME BOEING 737 7373B7 1384580 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 588US 41171 23933 PIT - FOUND FRAME CRACKED .5 INCH, STATION 787 LEFT BETWEEN STRINGER 8/9. (M) 2 L 7 2 4F RT A16WE 2001091200113 20010912 00113 NM 2001 9 12 USAA011074 1 20010810 A 5300 FRAME BOEING 737 7373B7 1384580 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 588US 41171 23933 PIT - FOUND FRAME CRACKED .5 INCH, STATION 787 RIGHT BETWEEN STRINGER 8/9. (M) 2 L 7 2 4F RT A16WE 2001091200114 20010912 00114 NM 2001 9 12 USAA011073 1 20010810 A 5300 FRAME BOEING 737 7373B7 1384580 NM CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 588US 41171 23933 PIT - FOUND FRAME CRACKED .5 INCH, BOTTOM OF VERTICAL FRAME ATTACH AREA AT WING BOX. (M) 2 L 7 2 4F RT A16WE 2001091200115 20010912 00115 NM 2001 9 12 USAA011072 1 20010812 A 5300 BEAM BOEING 737 737301 1384611 NM BS 328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 590US 43359 23935 PIT - FOUND BEAM CORRODED LBL 60 INCHES - RBL 60 INCHES, STATION 328 CABIN FLOOR LBL 60 INCHES, RBL 60 INCHES. REMOVED CORROSION, TREATED AND PRIMED PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2001091200116 20010912 00116 NM 2001 9 12 USAA011071 1 20010812 A 5300 BEAM BOEING 737 737301 1384611 NM BS 986.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 590US 43359 23935 PIT - FOUND BEAM CORRODED, LBL 48 INCHES-RBL 48 INCHES, STATION 986.5 CABIN FLOOR LBL 48 INCHES RBL 48 INCHES. REPLACED UPPER CHORD PER TYPICAL REPAIR 53-10-05. (M) 2 L 7 2 4F RT A16WE 2001091200117 20010912 00117 NM 2001 9 12 USAA011069 1 20010801 A 5300 FRAME BOEING 737 7374B7 1384702 NM BS 794 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 441US 30772 24812 PIT - FOUND FRAME CORRODED 4 INCHES BY .500 INCHES CORRODED, FORWARD FUSELAGE DOOR FRAME BS 794 ABOVE S25R. CORROSION L EVEL 1, TASK NR C53-100-01. INSTALLED DOUBLER PER SRM 53-60-15 AND EA 71737. (M) 2 L 7 2 4F RT A16WE 2001091200118 20010912 00118 NM 2001 9 12 USAA011068 1 20010810 A 5300 WEB BOEING 737 7373B7 1384580 NM BS 887 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 588US 41171 23933 PIT - FOUND WEB CORRODED 8 INCH BY 4 INCH AREA OF CORROSION, STATION 887 LEFT CREASE BEAM WEB. CORROSION LEVEL 1, TASK NR C53-107-01. BURNISHED, TREATED, PRIMED AND PAINTED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001091200119 20010912 00119 NM 2001 9 12 USAA011067 1 20010810 A 5300 WEB BOEING 737 7373B7 1384580 NM BS 867 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 588US 41171 23933 PIT - FOUND WEB CORRODED 4 INCHES BY 2 INCHES, STATION 867 RIGHT CREASE BEAM WEB. CORROSION LEVEL 1, TASK NR C53-107-01 . BURNISHED, TREATED AND PRIMED AND PAINTED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001091200120 20010912 00120 NM 2001 9 12 USAA011063 1 20010813 A 5300 STRAP BOEING 737 7374B7 1384702 NM BS 493 DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 24893 CLT - FOUND FRAME AND STRAP HAS DRILL DAMAGE .25 INCH, AFT FLANGE OF FRAME AND STRAP, BS 493 ABOVE BS 25R. INSTALLED DO UBLER AT FRAME AND STRAP PER SRM 53-00-07, SRM 51-70-11. (M) 2 L 7 2 4F RT A16WE 2001091200121 20010912 00121 NM 2001 9 12 USAA011062 1 20010813 A 5300 STRINGER BOEING 737 7374B7 1384702 NM BS 400 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 31027 24893 CLT - FOUND STRINGER DENTED .5 INCH, STRINGER 16L STATION 400. FABRICATED REPAIR CHANNEL, STRINGER TIE CLIP PER EA 8517 8. (M) 2 L 7 2 4F RT A16WE 2001091200122 20010912 00122 NM 2001 9 12 USAA011052 1 20010809 A 5300 SKIN BOEING 737 737301 1384611 NM BS 380 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 339US 43435 23236 CLT - FOUND SKIN DAMAGED 1 INCH, BETWEEN BS 28L AND BS 28R BS 380. INSTALLED .100 INCH THICK 2024 T3 DOUBLER PER TR 53- 30-07, SB 737-53-1117 REV 1. (M) 2 L 7 2 4F RT A16WE 2001091200123 20010912 00123 NM 2001 9 12 USAA011039 1 20010808 A 5300 WEB BOEING 737 7374B7 1384702 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 444US 31528 24862 CLT - FOUND WEB WITH SEVERAL CRACKED .75 TO .5 INCH, BS 178 WL 201 TO WL 213, LBL 5 TO LBL 6. INSTALLED DOUBLER PER EO 5300V153. (M) 2 L 7 2 4F RT A16WE 2001091200124 20010912 00124 NM 2001 9 12 USAA011022 1 20010807 A 5300 SKIN BOEING 737 7374B7 1384702 NM BS 500B A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 31027 24893 CLT - FOUND SKIN WITH 1 INCH CUTOUT, PREVIOUSLY INSTALLED DOUBLER, 7 INCHES BY 10 INCHES, BS 500B-500C, AT S22L 23L. PR EVIOUSLY INSTALLED DOUBLER PER SRM 53-00-01 FIG 202. (M) 2 L 7 2 4F RT A16WE 2001091200125 20010912 00125 NM 2001 9 12 USAA011019 1 20010807 A 5300 FRAME BOEING 737 7374B7 1384702 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 31027 24893 CLT - FOUND FRAME CRACKED .75 INCH, INBOARD RIVET BETWEEN STRINGER 8-9L AT BS 827. REPAIR DOUBLER INSTALLED PER TR 53-1 0-14. (M) 2 L 7 2 4F RT A16WE 2001091200126 20010912 00126 NM 2001 9 12 USAA011018 1 20010807 A 5300 FRAME BOEING 737 7374B7 1384702 NM BS 947.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 28481 24893 CLT - FOUND FRAME CRACKED .75 INCH, INBOARD RIVET BETWEEN STRINGER 8-9R AT BS 947.5. INTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001091200127 20010912 00127 NM 2001 9 12 USAA011015 1 20010807 A 5300 SKIN BOEING 737 7374B7 1384702 NM BS 927 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 31027 24893 CLT - FOUND SKIN DENTED 2.5 INCH BY 1.5 INCH BY .080 INCH, BS 927 STRINGER 18L. INSTALLED DOUBLER PER SRM 53-00-01 SRM 53-60-01 EA NR 69903. (M) 2 L 7 2 4F RT A16WE 2001091200128 20010912 00128 NM 2001 9 12 USAA011014 1 20010807 A 5300 FRAME BOEING 737 7374B7 1384702 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 31027 24893 CLT - FOUND FRAME CRACKED .5 INCH, BS 616, RBL 64 INCHES, 8 INCHES BELOW FLOOR. INSTALLED FILLER AND STIFFENER ANGLE PE R TR 53-62-01, HT J020-37-22. (M) 2 L 7 2 4F RT A16WE 2001091200129 20010912 00129 NM 2001 9 12 USAA011013 1 20010807 A 5300 SKIN BOEING 737 7374B7 1384702 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 28481 24893 CLT - FOUND SKIN CRACKED .75 INCH, INBOARD RIVET BETWEEN STRINGERS 8-9 AT BS 867L. REPAIR DOUBLER INSTALLED PER TR 53-1 0-14. (M) 2 L 7 2 4F RT A16WE 2001091200130 20010912 00130 NM 2001 9 12 2001UALA01513 1 20010729 A 3350 S106 BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7448U 21902 AFT AIRSTAIR OVERHEAD EMERGENCY EXIT LIGHT IS INOPERABLE. SUPPLEMENTAL DATA UPDATE BATTERY FAILED. REPLACED BATTERY. OPE RATIONS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001091200131 20010912 00131 NM 2001 9 12 2001UALA01720 1 20010815 A 2700 65503245 TRANSMISSION BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE WING FAILED A UALA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 989UA 21751 LANDED UNDER AMBER ALERT DUE TO STUCK TE FLAPS. SUPPLEMENTAL DATA UPDATE REPLACED THE #4 TRAILING EDGE FLAP TRANSMISSION . 2 L 7 2 4F 4 F A16WE E2EA 2001091200132 20010912 00132 NM 2001 9 12 2001UALA01723 1 20010815 A 2700 6AL1618 BEARING BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FEEL MECH SEIZED A UALA O OTHER F FLT CONT AFFECTED LD LANDING 1 WP 29 615UA 0 0 21876 RUDDER PEDALS EXTREMELY STIFF DURING APPROACH AND LANDING AFTER FIVE AND A HALF HOUR FLIGHT. SUPPLEMENTAL DATA UPDATE CA USE: A SEIZED CAM BEARING IN THE RUDDER FEEL AND CENTERING MECHANISM CAUSED THE HEAVY FORCE CONDITION IN THE RUDDER PED ALS.CORR ECTION: SUBJECT CAM BEARING WAS REMOVED AND REPLACED WITH NEW BEARING. RUDDER SYSTEM WAS OPS CHECKED PER APPL ICABLE MAINTENANCE MANUAL AND ALL CHECKED NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091200133 20010912 00133 NM 2001 9 12 2001UALA01726 1 20010810 A 3350 S106 BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7257U 21404 AFT AIRSTAIRS EMERGENCY LIGHT IS INOPERABLE. SUPPLEMENTAL DATA UPDATE THE BATTERY FAILED. REPLACED BATTERY. OPERATIONS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001091900138 20010919 00138 NM 2001 9 19 2001UALA01932 1 20010831 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST UK UNKNOWN 1 WP 29 188UA 26877 EMERGENCY LIGHT INOP 48C CEILING. EMERGENCY CEILING LIGHT BURNED OUT. RELAMPED LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2001091200135 20010912 00135 NM 2001 9 12 2001UALA01942 1 20010831 A 5311 CLIP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE BODY STATION 720 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 720-722 STRINGER 34L CLIP CRACKED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTA LLED CLIP. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091200136 20010912 00136 NM 2001 9 12 2001UALA01946 1 20010831 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE BODY STATION 418 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 418-478 STRINGER 38L CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091200137 20010912 00137 NM 2001 9 12 2001UALA01948 1 20010831 A 5313 DOUBLER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE BODY STATION 170 GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1709-1809 STRINGER 12L DOUBLER GOUGED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPLACED AND INS TALLED DOUBLER. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091200138 20010912 00138 NM 2001 9 12 2001UALA01949 1 20010831 A 5300 INTERCOSTAL BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE BODY STATION 317 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 317 LBL 12 WL 110 INTERCOSTAL CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091200139 20010912 00139 NM 2001 9 12 2001UALA01950 1 20010831 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE BODY STATION 325 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 325-434 STRINGER 38L CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER AND SPLICES. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091200140 20010912 00140 NM 2001 9 12 2001UALA01966 1 20010904 A 5313 STRINGER CLIP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE BODY STATION 368 ELONGATED A UALA J DUMP FUEL O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 368 STRINGER 36L STRINGER CLIP HAS ELONGATED HOLES. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FAB RICATED AND INSTALLED STRINGER CLIP. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091200141 20010912 00141 NM 2001 9 12 2001UALA01969 1 20010903 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE BODY STATION 584 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 584-592 STRINGER 36L CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091200142 20010912 00142 NM 2001 9 12 2001UALA01970 1 20010903 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE BODY STATION 478 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 478 STRINGER 39L CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STR INGER. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091200143 20010912 00143 NM 2001 9 12 2001UALA01971 1 20010903 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE BODY STATION 141 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 410 STRINGER 36R CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STR INGER. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091200144 20010912 00144 NM 2001 9 12 2001UALA01972 1 20010903 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE BODY STATION 106 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1065-1087 STRINGER 28R IS CRACKED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPLACED AND INSTALL ED STRINGER. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091200145 20010912 00145 NM 2001 9 12 2001UALA01973 1 20010903 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE BODY STATION 325 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 325-434 STRINGER 39R CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPLACED AND INSTALLED S TRINGER. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091200146 20010912 00146 NM 2001 9 12 2001UALA01974 1 20010903 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE BODY STATION 500 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 500 STRINGER 36R CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STR INGER. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091200163 20010912 00163 NM 2001 9 12 USAA010956 1 20010727 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 37039 23882 CLT - FOUND SIDE CHORDS .5 INCH, BS 178 WL 207 LEFT AND RIGHT SIDE. DAMAGE SECTION REMOVED, INSTALLED CHORD SPLICE REPA IR AND EXT SKIN STRAP PER EO 5300V157. (M) 2 L 7 2 4F RT A16WE 2001091200164 20010912 00164 NM 2001 9 12 USAA010957 1 20010727 A 5320 STRAP BOEING 737 737401 1384701 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 37040 23882 CLT - FOUND VERTICAL STRAP .125 INCH, BS 178, WL 208, LBL 25. DAMAGE SECTION REMOVED, REPLACEMENT SECTION SPLICED IN WI TH DOUBLER PER EA 85114. (M) 2 L 7 2 4F RT A16WE 2001091200165 20010912 00165 NM 2001 9 12 USAA010963 1 20010802 A 5511 SKIN BOEING 737 737301 1384611 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 573US 44887 23560 CLT - FOUND STAB LOWER SKIN CRACKED 1.5 INCH, RIGHT STAB, STAB STATION 66.5 TO 110. DAMAGE REMOVED, FILLER AND DOUBLER INSTALLED PER TYPICAL REPAIR 55-10-07 REV A. (M) 2 L 7 2 4F RT A16WE 2001091200166 20010912 00166 NM 2001 9 12 USAA011008 1 20010807 A 5320 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 31027 24893 CLT - FOUND WEB ANGLE CRACKED 2 INCHES, BS 291.5 AND 9R. WEB ANGLE PART NR 65-45807-31 INSTALLED PER SRM 51-40-05. (M) 2 L 7 2 4F RT A16WE 2001091200167 20010912 00167 NM 2001 9 12 USAA011009 1 20010807 A 5320 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 31027 24893 CLT - FOUND WEB ANGLE CRACKED 2 INCHES, BS 291.5 AND 10R. REPLACED WITH ANGLE PART NR 65-45807-33 PER SRM 51-40-05. (M ) 2 L 7 2 4F RT A16WE 2001091200168 20010912 00168 NM 2001 9 12 USAA011097 1 20010820 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 22961 CLT - FOUND CHORD CRACKED 1 INCH, BS 178, LBL 5.8, WL 184. INSTALLED REPAIR ANGLES PER EO 5300V155 PER M2-90-93857. (M ) 2 L 7 2 4F A16WE 2001091200169 20010912 00169 NM 2001 9 12 USAA011098 1 20010820 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND FRAME OUTER CHORD 1 INCH, BS 597, 6 INCHES BELOW 17L ON AFT SIDE OF FRAME. REMOVED AND REPLACED PART WITH P ART NR 1126923 PER SRM 51-30-2. (M) 2 L 7 2 4F A16WE 2001091200170 20010912 00170 NM 2001 9 12 USAA011099 1 20010820 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND CHORD CRACKED .250 INCH, BS 178, LBL 5.6, RBL 5.7, WL 184. INSTALLED REPAIR ANGLES PER EO 5300 US155 PER JC MC-90-93857. (M) 2 L 7 2 4F A16WE 2001091200171 20010912 00171 NM 2001 9 12 USAA011102 1 20010820 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND FRAME OUTER CHORD CRACKED 1 INCH, BS 597, 6 INCHES BELOW S17L ON FORWARD SIDE OF FRAME. REMOVED AND REPLACE D WITH PART NR 65-46538-33 PER SRM 51-30-2. (M) 2 L 7 2 4F A16WE 2001091200172 20010912 00172 NM 2001 9 12 USAA011104 1 20010820 A 5313 STRINGER BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 22961 CLT - FOUND STRINGER AND TIE CLIP CORRODED 1 INCH, BS 538, S26R. REMOVED AND REPLACED PART PER SRM 53-10-03. (M) 2 L 7 2 4F A16WE 2001091200173 20010912 00173 NM 2001 9 12 USAA011136 1 20010821 A 5314 KEELBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 42760 23237 CLT - FOUND 2 INCHES OF CORROSION, LEFT KEEL BEAM, VERTICAL LEG, INBOARD SURFACE BS 530. CORROSION LEVEL 2. CLEANED CO RROSION, VERIFIED REMOVAL AND RESTORED FINISH, PER EA 85288 SRM 53-60-12. (M) 2 L 7 2 4F RT A16WE 2001091200176 20010912 00176 WP 2001 9 12 WXOA01009 1 20010801 A 3350 1315 LIGHT DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A WXOA K NONE L NO TEST IN INSP/MAINT 1 WP 17 411EA 47732 FAT - DURING AIRCRAFT SCHEDULED INSPECTION, FOUND CABIN EMERGENCY LIGHTS INOPERATIVE AT STATION 1167 (AFT CABIN EXIT DOO R AREA). MAINTENANCE FOUND LOOSE WIRE CONNECTION AND INOPERATIVE BULBS. RESECURED WIRING AND RELAMPED LIGHTS. EMERGENC Y LIGHTING SYSTEM OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 2001091200178 20010912 00178 EA 2001 9 12 COMA0160707 1 20010911 A 2780 601R1430310 CAP CNDAIR CL600 CL6002B19 EA FLAP LEADING EDG CHAFED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 949CA 14351 7080 THE R/H INBOARD FLAP LEADING EDGE VANE CAP MIDDLE SKIN IS CHAFED WHERE THE FLAP CONTACTS THE TEFLON BUMPER PAD.REMOVED T HE CHAFED MIDDLE VANE CAP. INSTALLED A NEW CAP (P/N 601R14303-10) IAW AERODESIGN ENGINEERING REPORT NO. 1286-1. 2 L 7 2 4F RT A21EA 2001091200181 20010912 00181 WP 2001 9 12 WXOA01010 1 20010807 A 3350 1315 LIGHT DOUG DC9 DC951 3022051 WP TAILCONE INOPERATIVE A WXOA K NONE L NO TEST IN INSP/MAINT 1 WP 17 411EA 47732 FAT - DURING AIRCRAFT SCHEDULED INSPECTION, FOUND EMERGENCY LIGHTS INOPERATIVE IN TAILCONE COMPARTMENT. MAINTENANCE FOU ND INOPERATIVE BULBS. RELAMPED LIGHTS. EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 2001091200183 20010912 00183 EA 2001 9 12 COMA0160708 1 20010911 A 2780 601R14303 CAP CNDAIR CL600 CL6002B19 EA FLAP LEADING EDG CHAFED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 949CA 14351 7080 THE L/H AND R/H INBOARD FLAP LEADING EDGE INBOARD VANE CAPS ARE CHAFED WHERE THEY CONTACT THE TEFLON BUMPER PADS.REMOVED THE CHAFED INBOARD VANE CAPS. INSTALLED NEW VANE CAPS L/H (601R14303-53S) AND R/H (601R14303-54) IAW WVAC EO 601R-57-2 706. 2 L 7 2 4F RT A21EA 2001091200184 20010912 00184 EA 2001 9 12 COMA0160709 1 20010910 A 5300 RADOME CNDAIR CL600 CL6002B19 EA A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 952CA 7092 FLIGHT #5420. DURING TAKE OFF AT CVG AIRCRAFT ENCOUNTERED MULTIPLE BIRD STRIKES ON RADOME, TAKE OFF WAS ABORTED AND RET URNED TO THE GATE.PERFORMED BIRD STRIKE AND HIGH ENERGY STOP INSPECTION, NO DEFECTS NOTES. 2 L 7 2 4F RT A21EA 2001091200186 20010912 00186 EA 2001 9 12 COMA0160710 1 20010910 A 3350 64641 LIGHT CNDAIR CL600 CL6002B19 EA A COMA O OTHER S AFFECT SYSTEMS IN INSP/MAINT 1 SO 01 818CA 7408 FLIGHT #5646. WHILE AT THE GATE CREW NOTICED A SECTION OF FLOOR EMERGENCY LIGHTING INOPERATIVE.REPLACED AFFECTED SECTIO N OF FLOOR EMERGENCY LIGHT STRIP. 2 L 7 2 4F RT A21EA 2001091200187 20010912 00187 WP 2001 9 12 2001F00269 2 20010819 A 7320 1390136 DIAPHRAGM SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP RT ENGINE LEAKING A C9UA E ENGINE SHUTDOWN O OTHER DE DESCENT 1 WP 23 200PT TC211EEEE P54199 PILOT DID A PRECAUTIONARY RIGHT ENGINE SHUTDOWN BECAUSE THE ENGINE WAS NOT RESPONDING TO HIS INPUTS. FOUND THE P3 DIAPH RAGM ON THE FUEL CONTROL UNIT WAS LEAKING. (M) 2 L 7 2 4T 4 T RT A8SW E4WE 2001091200188 20010912 00188 WP 2001 9 12 2001F00270 2 20010819 A 7320 1390136 DIAPHRAGM SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP RT ENGINE LEAKING A C9UA E ENGINE SHUTDOWN O OTHER DE DESCENT 1 WP 23 200PT 3282 TC211EEEE P54199 PILOT DID A PRECAUTIONARY RIGHT ENGINE SHUTDOWN BECAUSE THE ENGINE WAS NOT RESPONDING TO HIS INPUTS. FOUND THE P3 DIAPH RAGM ON THE FUEL CONTROL UNIT WAS LEAKING. (M) 2 L 7 2 4T 4 T RT A8SW E4WE 2001091700100 20010917 00100 EA 2001 9 17 COMA0160711 1 20010910 A 2760 4916405 ECU CNDAIR CL600 CL6002B19 EA E/E BAY FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 927CA 14217 12006 7031 FLIGHT 5356. DURING TAXI OUT OF MHT RECEIVED A RIGHT SPOILERON CAUTION MESSAGE. AIRCRAFT RETURNED TO THE GATE. REPLAC ED THE NR 1 SPOILER ELECTRONIC CONTROL UNIT. 2 L 7 2 4F RT A21EA 2001091200189 20010912 00189 NM 2001 9 12 USAA011016 1 20010807 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 31027 24893 CLT - FOUND BULKHEAD WEB CRACKED .35 INCH, BS 178, LBL 6.5, WL 212. DOUBLER INSTALLED PER EO 5300V153. (M) 2 L 7 2 4F RT A16WE 2001091200191 20010912 00191 EA 2001 9 12 COMA0160712 1 20010910 A 2741 83963 ACTUATOR CNDAIR CL600 CL6002B19 EA HORIZONTAL STABI FAULTY A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 814CA 2906 7387 FLIGHT #5517. CREW REPORTED HORIZONTAL STABILIZER TRIM INDICATION BEING ERRATIC.REPLACED THE HORIZONTAL STABILIZER TRIM ACTUATOR. 2 L 7 2 4F RT A21EA 2001091200193 20010912 00193 NM 2001 9 12 USAA011017 1 20010807 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 31027 24893 CLT - FOUND PRESSURE WEB WITH NUMEROUS CRACKS RANGING FROM .250 INCH TO .600 INCH, BS 178 WL 188 TO 206, RBL 6.5 TO LBL 5. DAMAGED REMOVED, REPAIR DOUBLER INSTALLED PER EO 5300V153. (M) 2 L 7 2 4F RT A16WE 2001091200195 20010912 00195 EA 2001 9 12 COMA0160713 1 20010910 A 2741 70623 MOTOR CNDAIR CL600 CL6002B19 EA HORIZONTAL STABI FAULTY A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 814CA 2906 7387 FLIGHT #5517. CREW REPORTED HORIZONTAL STABILIZER TRIM INDICATION BEING ERRATIC.REPLACED THE HORIZONTAL STABILIZER MOTO R CONTROL UNIT. 2 L 7 2 4F RT A21EA 2001091200196 20010912 00196 NM 2001 9 12 USAA011020 1 20010807 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 31027 24893 CLT - FOUND FLOORBEAM T-CAP CORRODED APPROX 10 SQUARE INCHES, BS 947 RBL 5 TO LBL 14. DAMAGE REMOVED AND T-CAP REPLACED PER TR 53-60-02. (M) 2 L 7 2 4F RT A16WE 2001091200198 20010912 00198 NM 2001 9 12 USAA011045 1 20010808 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 444US 31528 24862 CLT - FOUND LEFT/RIGHT SIDE CHORD WITH APPROXIMATELY 1 INCH CRACK, BS 178, WL 207, RBL 27 AND LBL 27. SPLICED IN NEW CH ORD SECTION PER EO 5300V157. (M) 2 L 7 2 4F RT A16WE 2001091200199 20010912 00199 NM 2001 9 12 USAA011066 1 20010806 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 339US 23236 TPA - FOUND 1 INCH CRACK IN SKIN AFT OF EQUIPMENT COOLING EXH, LOWER LOBE SKIN BETWEEN S28L AND 28R STATION 380. INSTAL LED DOUBLER PER TYPICAL REPAIR 53-30-07, SB 737-53-1117 REV 1. (M) 2 L 7 2 4F RT A16WE 2001091200200 20010912 00200 NM 2001 9 12 USAA011070 1 20010812 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 590US 43359 23935 PIT - FOUND BEAM CORRODED LBL 60 - RBL 18, STATION 344 CABIN FLOOR LBL 60 RBL 18. REPLACED UPPER CHORD PER SRM 53-10-51, FIG 205 AND EA 71720. (M) 2 L 7 2 4F RT A16WE 2001091200201 20010912 00201 NM 2001 9 12 USAA011079 1 20010810 A 5320 SUPPORT BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 588US 41171 23933 PIT - FOUND OVER 15 FEET OF SPOTTY CORROSION ON SUPPORT ZEE, STATION 727 TO 787 ABOVE STRINGER 26R AFT CARGO. (M) 2 L 7 2 4F RT A16WE 2001091200202 20010912 00202 NM 2001 9 12 USAA011080 1 20010810 A 5320 SUPPORT BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 588US 41171 23933 PIT - FOUND OVER 15 FEET OF SPOTTY CORROSION ON SUPPORT ZEE, STATION 727-787 ABOVE STRINGER 26L AFT CARGO. (M) 2 L 7 2 4F RT A16WE 2001091200205 20010912 00205 NM 2001 9 12 USAA011084 1 20010810 A 5240 GATE BOEING 737 737301 1384611 NM SERVICE DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 588US 41171 23933 PIT - FOUND GATE CORRODED .125 INCH BY 4 INCH, BOTTOM GATE OF AFT SERVICE DOOR. (M) 2 L 7 2 4F RT A16WE 2001091200206 20010912 00206 EU 2001 9 12 USAABA01008 1 20010822 A 3230 D31AB4431 VALVE AIRBUS 330 A330323 EU MLG MALFUNCTIONED A USAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 19 675US 3530 370 FRA - FLT 894 - EN ROUTE PHL-FRA - DURING APPROACH, THE LANDING GEAR DID NOT EXTEND WHEN SELECTED DOWN. THE LANDING GEA R WAS RECYCLED TWICE, BUT STILL WOULD NOT EXTEND. FLIGHT EXECUTED A MISSED APPROACH. WHEN THE LANDING GEAR GRAVITY EXT ENSION CHECKLIST WAS STARTED, THE LANDING GEAR MOVED TO THE DOWN AND LOCKED POSITION AFTER THE LANDING GEAR LEVER WAS SE LECTED DOWN. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR SAFETY VALVE. PERFORMED GE AR SWING. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A46NM 2001091200207 20010912 00207 WP 2001 9 12 WXOA01011 1 20010813 A 3350 TERMINAL DOUG DC9 DC951 3022051 WP TAILCONE CORRODED A WXOA K NONE L NO TEST IN INSP/MAINT 1 WP 17 411EA 47732 FAT - DURING AIRCRAFT SCHEDULED INSPECTION, FOUND EMERGENCY LIGHTS INOPERATIVE IN TAILCONE COMPARTMENT. MAINTENANCE FOU ND CORRODED TERMINAL CONNECTION. CLEANED TERMINALS. EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 2001091200210 20010912 00210 WP 2001 9 12 MWEA011251 1 20010908 A 5310 5911415161 SKIN DOUG DC9 DC932 3022066 WP STATION 718 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FUSELAGE SKIN WAS CRACKED AT STATION 718 BELOW LONGERON 10 RIGHT. -- REMOVED DAMAGE, INSTALLED DOUBLERS. 2 L 7 2 4F A6WE 2001091200211 20010912 00211 WP 2001 9 12 Y2PA01024 1 20010830 A 3297 WIRE DOUG DC9 DC915F 3022037 WP MLG LOOSE A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 197US 47154 YIP - AFTER TAKEOFF PRIOR TO GEAR RETRACTION NOTICED THE RT MLG DOWN LIGHT WAS NOT LIT. THE GEAR WAS LEFT IN THE DOWN P OSITION AND AIRCRAFT RETURNED TO POINT OF DEPARTURE AT YIP. CREW TROUBLESHOT SYSTEM AND DETERMINED GEAR WAS DOWN AND LOC KED. TOWER NOTIFIED, FLY BY TO CONFIRM GEAR DOWN. CREW MAINTAINED SYS PRESSURE TO KEEP GEARS DOORS RETRACTED. NO WARNIN GS SOUNDED WHEN FLAPS EXTENDED AND THROTTLES REDUCED. CREW DECLARED AN EMERGENCY AND THEN LANDED WITHOUT INCIDENT. AFTER LANDING AIRCRAFT WAS STOPPED ON THE RUNWAY AND GEAR PINS WERE INSTALLED PRIOR TO FURTHER TAXI. MAINT AT FOUND LOOSE WI RE ON TERMINAL STRIP S3-66. WIRE WAS TIGHTENED. LANDING GEAR SYS WAS CHECKED IAW DC9 MM 32-60-0 NO DEFECTS NOTED. 2 L 7 2 4F A6WE 2001091200215 20010912 00215 SO 2001 9 12 SWIA200110045 1 20010718 A 5310 WINDOW POST EMB 120 EMB120RT SO COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 196CA 120196 CRACK FOUND IN RIGHT POST BETWEEN DIRECT VIEW WINDOW AND WINDSHIELD.FABRICATED AND INSTALLED DOUBLER IAW SB120-053-0010/ 3-18-88. 2 L 7 2 4T RT A31SO 2001091200216 20010912 00216 SO 2001 9 12 SWIA200110046 1 20010715 A 6123 RELAY EMB 120 EMB120ER 3260203 SO AUTOFEATHER SYS FAILED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 189SW 120048 ON TAKEOFF IN JAC, RECEIVED TRIPLE CHIME TAKEOFF AURAL AUTOFX AT ABOUT 100 KTS. ABORTED TAKEOFF WAS INITIATED AND WE CO NTACTED MX CONTROL. PERFORMED AUTOFX TEST. OPS CHECK GOOD (DELAY WITH POWER LEVERS POSITIVE CULPRIT).REPLACED AUTO FEA THER ARM RELAY K0161. AUTO FEATHER TEST CHECKS GOOD. NO AUTO FEATHER WARNING IN TAKEOFF CONFIGURATION. 2 L 7 2 4T RT A31SO 2001091200217 20010912 00217 SO 2001 9 12 SWIA200110047 1 20010718 A 6123 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO COCKPIT ACTIVATED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 295UX 120295 ON TAKEOFF ROLL AURAL WARNING ''AUTO FEATHER''. SWITCH WAS ON AND TESTED ON TAXI CHECK.COULD NOT DUPLICATE DURING RUNU P. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001091200218 20010912 00218 2001 9 12 SWIA200110048 4 20010720 A 3425 6229336400 COMPUTER CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 903SW 7425 WITH AUTOPILOT ENGAGED (INFLIGHT OPERATIONS) BOTH CONTROL COLUMNS JERK FORWARD AND BACK INTERMITTENTLY DURING FLIGHT. T HE FO'S INCLINOMETER WOULD ALSO DEFLECT QUICKLY LEFT AND RIGHT THEN RETURN TO CENTER POSITION. THEN IT WOULD REPEAT. RE MOVED AND REPLACED NR 1 AHC-85E. AP SYSTEM OPS CHECK GOOD IAW MM 22-10-00 AND AHC OPS CHECK GOOD IAW 34-21-00. COMPLIED WITH CAT II AS REQUIRED. P/N: 622-9336-402 S/N ON: 5GNX P/N OFF: 622-9336-400 S/N OFF: 468L 2 L 7 2 4F RT A21EA 2001091200219 20010912 00219 WP 2001 9 12 ZW0A0107701 1 20010824 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT FOUND CORROSION FROM STA 1180 TO 1188, LONGERON 18R MEMBRANE. CUT OUT CORRODED AREA. INSTALLED DOU BLER PER SRM 53-01 PAGE 18. 2 L 7 2 4F RT A6WE 2001091200220 20010912 00220 WP 2001 9 12 ZW0A0107702 1 20010827 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT IN THE AFT CABIN THE LT SIDEWALL CUSP MEMBRANE HAD CORROSION AT STA 1306 TO 1287, AT WATER LINE 200 , LONGERON 18L. REMOVED CORROSION PER SPM 6-80-01. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 51-70-4. 2 L 7 2 4F RT A6WE 2001091200221 20010912 00221 WP 2001 9 12 ZW0A0107703 1 20010827 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT FOUND CORROSION ON MEMBRANE AND CRACK BETWEEN STA 655 AND 674, AT CUSP ANGLE WATER LINE 200, LONGER ON 18L. INSTALLED DOUBLER PER SRM 51-70-4. 2 L 7 2 4F RT A6WE 2001091200222 20010912 00222 2001 9 12 ZW0A0107802 4 20010830 A 3422 25883024 GYRO DOUG DC9 DC931 3022065 WP COCKPIT FAILED A ZW0A A UNSCHED LANDING O OTHER CL CLIMB 1 CE 13 979Z 47343 ON TAKEOFF BOTH COMPASS CARDS SPUN RAPIDLY. NO FLAGS PRESENT. BOTH SYSTEMS DISAGREED WITH THE STANDBY/WET COMPASS. RETUR NED TO STL. REPLACED THE NR 1 DG PN 2588302-4, THE NR 2 FLUX VALVE PN 2587794, AND THE NR 2 COMPASS RACK PN 614937-101. CHECK-C 12-3-00 STL. 2 L 7 2 4F A6WE 2001091200223 20010912 00223 NM 2001 9 12 ZW0A0107901 1 20010903 A 3350 80741 LIGHT BOEING 767 7673Y0 NM CABIN MISSING A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 639TW 26208 THE EGRESS LAMPS WERE MISSING AT ROWS 34 AND 40 ON LEFT SIDE OF THE CABIN, AND ROW 20 ON RT SIDE. REPLACED THE LAMP STRI P AT EACH LOCATION. 2 L 7 2 4F RT A1NM 2001091200224 20010912 00224 WP 2001 9 12 ZW0A0107902 1 20010901 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 902TW 49153 THE EMERGENCY LIGHT IN THE TAIL CONE AND WALKWAY, AND THE CABIN EMERGENCY LIGHT IN THE CEILING AT THE AFT FLIGHT ATTENDA NT SEAT AREA, WERE INOPERATIVE. REPLACED THE BATTERY PACK PN 408822-101 FOR THE TAIL CONE AND WALKWAY, AND REPLACED THE BATTERY POWER SUPPLY PN 5822-2 FOR THE AFT CABIN CEILING EMERGENCY LIGHT. CHECK-C 2-5-01 STL. 2 L 7 2 4F A6WE 2001091200225 20010912 00225 WP 2001 9 12 ZW0A0108001 1 20010904 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 963TW 53613 THE FORWARD OVERWING EMERGENCY EXIT LIGHTS WERE INOPERATIVE. REPLACED THE POWER SUPPLY PN 60-0304-51LB, AND LAMPS PN 13 15. 2 L 7 2 4F RT A6WE 2001091200226 20010912 00226 WP 2001 9 12 ZW0A0108002 1 20010828 A 5320 ATTACH ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 911TW 49182 DURING CHECK-C MAINT THE L1 DOOR SILL PLATE ATTACH ANGLE HAD CORROSION ON UPPER AND LOWER EDGE APPROXIMATELY STA 170 TO 190, LBL 57. FABRICATED NEW FLOOR SUPPORT PER SPM 6-70-01, PAGE 2 AND 3, AND SRM 53-14-11. INSTALLED PER SRM 51-30-5, SRM 51-30-2, AND SRM 51-60-0. INSTALLED NEW ANGLE FROM STOCK. 2 L 7 2 4F A6WE 2001091200227 20010912 00227 WP 2001 9 12 ZW0A0108003 1 20010829 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 911TW 49182 DURING CHECK-C MAINT FOUND CRACK IN LONGERON 4L AT ATTACH POINT OF LONGERON TO STA 160 FORMER, OTBD FASTENER. REPLACED L ONGERON PER SPM 6-70-01. 2 L 7 2 4F A6WE 2001091200228 20010912 00228 NM 2001 9 12 ZW0A0108004 1 20010830 A 5753 FLAP BOEING 757 757231 1384950 NM RT WING DELAMINATED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 708TW 28480 DURING CHECK-C MAINT FOUND RT WING OTBD T/E FLAP, INBD END, HAD A DELAMINATED AREA. REPAIRED DELAMINATION PER SRM 51-70 -05. 2 L 7 2 4F RT A2NM 2001091200229 20010912 00229 NM 2001 9 12 ZW0A0108005 1 20010831 A 5730 SKIN BOEING 757 757231 1384950 NM LT WING CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 708TW 28480 DURING CHECK-C MAINT ON LT WING L/E FOUND 2 EACH CRACKS AND DELAMINATION ON THE UPPER SURFACE OF THE FIXED PANE L/E, WIN G STA 428 TO 436. REPAIRED WING PANEL PER SERVICE BULLETIN 757-57-0052, NUMBER 1, FIGURE 3. 2 L 7 2 4F RT A2NM 2001091200230 20010912 00230 WP 2001 9 12 ZW0A0108006 1 20010829 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT FOUND RT MEMBRANE AT LONGERON 18R CRACKED FROM STA 1283 TO 1301. REPAIRED CRACKED MEMBRANE PER SRM 53-05, FIG 96. 2 L 7 2 4F RT A6WE 2001091200231 20010912 00231 WP 2001 9 12 ZW0A0108007 1 20010829 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT FOUND CABIN MEMBRANE CRACKED AT STA 1277, LONGERON 18R. REPAIRED CRACKED MEMBRANE PER SRM 53-05, F IG 96. 2 L 7 2 4F RT A6WE 2001091200232 20010912 00232 WP 2001 9 12 ZW0A0108008 1 20010829 A 5320 BRACKET DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT IN THE AFT ACCESSORY COMPARTMENT, FOUND CRACK IN BRACKET, STA 1491, 6 IN AFT AND 3 IN BELOW THE LEF T REAR PIVOT OF THE AIRSTAIRS. FABRICATED MANUFACTURED PART 4967110-503 PER SPM 6-70-01 AND PRINT GMC86623 FROM MANUFAC TURER. INSTALLED MANUFACTURED PART PER SPM 6-70-01. 2 L 7 2 4F RT A6WE 2001091200233 20010912 00233 WP 2001 9 12 ZW0A0108009 1 20010830 A 5320 ATTACH ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT IN THE MID CARGO COMPT FOUND ATTACH ANGLE CRACKED AT AFT END OF INTERCOSTAL, STA 789, BETWEEN LONGE RON 28L AND 27L. REPLACED INTERCOSTAL ATTACH ANGLE PER SPM 6-70-01. 2 L 7 2 4F RT A6WE 2001091200234 20010912 00234 WP 2001 9 12 ZW0A0108010 1 20010830 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT FOUND CORROSION ON CUSP MEMBRANE AT LONGERON 18R, BETWEEN STA 655 AND 674, BETWEEN STA 693 AND 712, AND BETWEEN STA 674 AND 693. REPAIRED ALL AREAS PER SRM 51-70-4, FIG 2. 2 L 7 2 4F RT A6WE 2001091200235 20010912 00235 WP 2001 9 12 ZW0A0108011 1 20010831 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT FOUND CORROSION IN LOWER CABIN MEMBRANE PANEL, WHERE MEMBRANE OVERLAPS AT STA 180, RBL 48 INCHES. REMOVED CORROSION PER SPM 6-80-01. REPAIRED MEMBRANE PER SRM 51-70-4. 2 L 7 2 4F RT A6WE 2001091200236 20010912 00236 WP 2001 9 12 ZW0A0108012 1 20010831 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT FOUND ANGLE IN CABIN WITH CORROSION AT STA 200, LBL 14 TO 19. REMOVED AND REPLACED CORRODED FLOOR SUPPORT. 2 L 7 2 4F RT A6WE 2001091200237 20010912 00237 WP 2001 9 12 ZW0A0108013 1 20010831 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT CORRODED AT STA 1155, BETWEEN NUMBER 2 AND 3 TRACKS. REMOVED AND REPLACE D CORRODED FLOOR SUPPORT. 2 L 7 2 4F RT A6WE 2001091200238 20010912 00238 WP 2001 9 12 ZW0A0108014 1 20010831 A 5320 BRACKET DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT FOUND CORROSION ON BRACKET AT STA 200 RBL 9 INCHES TO LBL 9 IN. FABRICATED NEW BRACKET PER SPM 6-7 0-01. 2 L 7 2 4F RT A6WE 2001091200239 20010912 00239 NM 2001 9 12 ZW0A0108201 1 20010907 A 3350 LIGHT BOEING 757 757231 1384950 NM CABIN LOOSE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 714P 28482 THE EGRESS LIGHT WAS INOPERATIVE AT SEAT 14D. SECURED LIGHT STRIP. 2 L 7 2 4F RT A2NM 2001091200240 20010912 00240 NM 2001 9 12 ZW0A0108202 1 20010910 A 3350 CONNECTOR BOEING 767 76733AER 1385230 NM CABIN CONTAMINATED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 637TW 25403 THE EGRESS LIGHT AT SEAT ROW 1 AND 3, RT SIDE OF CABIN, AND THE RT FORWARD CLOSET, WERE INOPERATIVE. CLEARED AND DRIED THE CONNECTOR AT THE CLOSET LAMP. 2 L 7 2 4F RT A1NM 2001091200241 20010912 00241 WP 2001 9 12 ZW0A0108203 1 20010902 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 956U 49701 DURING CHECK-C MAINT FOUND .375 INCH VERTICAL CRACK IN END OF LONGERON 2R, STA 1418. REPAIR ON NUMBER 2R LONGERON AT ST A 1418 COMPLETED PER SRM 53-02. 2 L 7 2 4F A6WE 2001091200242 20010912 00242 WP 2001 9 12 ZW0A0108205 1 20010907 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9403W 53139 DURING CHECK-C MAINT THE NUMBER 2L LONGERON WAS CRACKED ABOVE THE Y DUCT ALONG LONGERON END. REPLACED LONGERON SECTION P ER SRM 53-02. 2 L 7 2 4F RT A6WE 2001091200243 20010912 00243 WP 2001 9 12 ZW0A0108206 1 20010905 A 5320 FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 926TW 49356 DURING CHECK-C MAINT THE T FITTING BELOW KEEL BEAM, STA 875, WAS CRACKED. REMOVED FITTING. FABRICATED NEW FITTING AND IN STALLED PER SRM 51-10-4. 2 L 7 2 4F A6WE 2001091200244 20010912 00244 WP 2001 9 12 ZW0A0108207 1 20010906 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 926TW 49356 DURING CHECK-C MAINT IN THE AFT CARGO COMPT THE FLOOR SUPPORT HAD CORROSION AT STA 1212, LBL 14 TO RBL 6. REPLACED SUPP ORT WITH NEW PART PER SPM 6-70-01 AND DOUGLAS DRAWING 5936597. 2 L 7 2 4F A6WE 2001091200245 20010912 00245 WP 2001 9 12 ZW0A0108208 1 20010906 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 926TW 49356 DURING CHECK-C MAINT FOUND FLOOR MEMBRANE CRACKED OTBD OF RT OTBD CHAIR TRACK, STA 1271-1287. REPAIRED PER SRM 53-05, PA GE 345. 2 L 7 2 4F A6WE 2001091200246 20010912 00246 WP 2001 9 12 ZW0A0108209 1 20010906 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 911TW 49182 DURING CHECK-C MAINT FOUND CORROSION ON AFT TOP OF FORMER, 9 INCHES LBL TO 21 IN LBL. REMOVED CORROSION FROM FORMER STA 1322, LBL 9 IN TO LBL 21 IN. SPLICED NEW SECTION AT STA 1322 LONGERON 29L TO 29R PER SRM 53-03, FIG 2A. CORROSION REM OVED PER SPM 6-80-01 AND TREATED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001091200247 20010912 00247 WP 2001 9 12 ZW0A0108301 1 20010903 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT FOUND CORROSION ON CABIN CHAIR TRACK NUMBER 2, FROM STA 1136 TO 1174. REPLACED TRACK PER SPM 6-70- 1, AND SRM 53-05 PAGE 10G. 2 L 7 2 4F RT A6WE 2001091200248 20010912 00248 WP 2001 9 12 ZW0A0108302 1 20010903 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR SUPPORT AT STA 200, RBL 10 TO RBL 31. MADE NEW FLOOR SUPPORT FROM ST OCK. INSTALLED PER SRM 51-30-15 AND 51-30-7. 2 L 7 2 4F RT A6WE 2001091200249 20010912 00249 WP 2001 9 12 ZW0A0108303 1 20010905 A 5320 BRACKET DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR MOUNTING BRACKET AT STA 210, RBL 10. MADE NEW FLOOR MOUNTING BRACKE T FROM STOCK. INSTALLED IN AIRCRAFT PER SRM 51-30-5. 2 L 7 2 4F RT A6WE 2001091200250 20010912 00250 WP 2001 9 12 ZW0A0108305 1 20010905 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT FOUND CORROSION IN CABIN ON NUMBER 3 FLOOR TRACK, FROM STA 205 TO 225. REPLACED SECTION OF TRACK P ER SPM 6-70-1 AND SRM 53-05 FIG 4. 2 L 7 2 4F RT A6WE 2001091300028 20010913 00028 NM 2001 9 13 SWAA012443 1 20010903 A 3350 07912 COVER BOEING 737 7377H4 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 774SW 27882 DURING SCHEDULED C4 CHECK, FOUND SEVERAL EEPLS COVERS CRACKED. R&R EEPLS COVERS PER MM. 2 L 7 2 4F RT A16WE 2001091300029 20010913 00029 NM 2001 9 13 SWAA012446 1 20010902 A 5310 6551698 SPLICE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED D CHECK, FOUND STR SPLICE CRACKED AT BS 365, STR 5L. R&R STR SPLICE PER SRM. 2 L 7 2 4F A16WE 2001091300030 20010913 00030 NM 2001 9 13 SWAA012447 1 20010901 A 5310 65C27314 CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED 1/2D CHECK, FOUND STR CLIP CRACKED AT BS 1137, LH APU TORQUE BOX. R&R STR CL IP PER SRM. 2 L 7 2 4F RT A16WE 2001091300031 20010913 00031 NM 2001 9 13 SWAA012448 1 20010827 A 5310 65C27314 CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 524SW 26566 DURING SCHEDULED D CHECK, FOUND STR CLIPS CRACKED ( 2 EA ) AT BS 727, STR 2L & 2R. R&R S TR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001091300032 20010913 00032 NM 2001 9 13 SWAA012449 1 20010831 A 2731 6545190 MECHANISM BOEING 737 7373H4 1384600 NM RH ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 653SW 28398 DURING SCHEDULED C4 CHECK, RH ELEVATOR TAB FAILED FREE PLAY CHECK. R&R RH ELEVATOR LOCK MECHA NISM PER MM. 2 L 7 2 4F RT A16WE 2001091300033 20010913 00033 NM 2001 9 13 SWAA012450 1 20010831 A 3350 07912 COVER BOEING 737 7373G7 1384595 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED C4 CHECK, FOUND SEVERAL EEPLS COVERS CRACKED BETWEEN ROW 12 & ROW 18. R& R COVERS PER MM. 2 L 7 2 4F RT A16WE 2001091300034 20010913 00034 2001 9 13 SWAA012452 4 20010901 A 2565 D31591 SLIDE BOEING 737 7375H4 138449D NM FWD SVC DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 510SW 24187 DURING SCHEDULED RON, FWD SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. R&R EVAC SL IDE PER MM. 2 L 7 2 4F RT A16WE 2001091300035 20010913 00035 NM 2001 9 13 SWAA012453 1 20010901 A 5310 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL BEAM WEBS CRACKED ( 2 EA ) AT BS 178, WL 230, RBL 17.1 & LBL 17.1. R&R VERTICAL BEAM WEBS PER SRM. 2 L 7 2 4F RT A16WE 2001091300036 20010913 00036 NM 2001 9 13 SWAA012454 1 20010822 A 5511 6507991 RIB BOEING 737 7375H4 138449D NM RH HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 519SW 25318 DURING SCHEDULED D CHECK AT DALFORT, FOUND RH HORIZ STAB L/E PANEL RIB CRACKED AT STA 203.1. R& R RIB PER SRM. 2 L 7 2 4F RT A16WE 2001091300037 20010913 00037 NM 2001 9 13 SWAA012455 1 20010822 A 5511 6547994 RIB BOEING 737 7375H4 138449D NM LH HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 519SW 25318 DURING SCHEDULED D CHECK AT DALFORT, FOUND LH HORIZ STAB L/E PANEL RIBS CRACKED ( 2 EA ) AT STA 258.3 & STA 249.1. R&R RIBS PER SRM. 2 L 7 2 4F RT A16WE 2001091300038 20010913 00038 NM 2001 9 13 SWAA012456 1 20010827 A 5310 65C77314 CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 524SW 26566 DURING SCHEDULED D CHECK, FOUND STR CLIPS CRACKED ( 4 EA ) AT BS 887, STR 4L & 4R, BS 328, STR 24R, BS 663, STR 10R. R&R STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001091300039 20010913 00039 NM 2001 9 13 SWAA012457 1 20010902 A 5310 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 350SW 24409 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEBS CRACKED ( 9 EA ) AT BS 178, LBL 20-RBL 28. R EPAIRED WEBS PER SRM. 2 L 7 2 4F RT A16WE 2001091300040 20010913 00040 NM 2001 9 13 SWAA012458 1 20010828 A 5754 65C26686 WEDGE BOEING 737 7372H4 138448C NM # 2 SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED D CHECK, FOUND # 2 SLAT T/E WEDGE DELAMINATED. R&R SLAT ASSY PER MM. 2 L 7 2 4F A16WE 2001091300041 20010913 00041 NM 2001 9 13 SWAA012459 1 20010824 A 5754 65C26686 WEDGE BOEING 737 7372H4 138448C NM # 3 SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED D CHECK, FOUND # 3 SLAT T/E WEDGE DELAMINATED. R&R SLAT ASSY PER MM. 2 L 7 2 4F A16WE 2001091300042 20010913 00042 NM 2001 9 13 SWAA012460 1 20010828 A 5310 6546564 SHEAR TIE BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 986.5, BETWEEN STR 21R & 22R. R&R S HEAR TIE PER SRM. 2 L 7 2 4F A16WE 2001091300043 20010913 00043 NM 2001 9 13 SWAA012461 1 20010828 A 5310 6546546 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, BETWEEN STR 8R & 9R. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2001091300044 20010913 00044 NM 2001 9 13 SWAA012462 1 20010828 A 5310 6516301 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17L. REPAIRED FRAME PER SR M. 2 L 7 2 4F A16WE 2001091300045 20010913 00045 NM 2001 9 13 SWAA012468 1 20010901 A 5313 6551698 SPLICE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 524SW 26566 DURING SCHEDULED D CHECK, FOUND STR SPLICE CRACKED AT BS 907, STR 4R. R&R STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2001091300046 20010913 00046 2001 9 13 SWAA012469 4 20010831 A 2565 6557463 FITTING BOEING 737 7373A4 1384585 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 DURING SCHEDULED 1/4D CHECK, FOUND BOTH ENTRY DOOR EVAC SLIDE GIRT BAR FLOOR ATTACH FITTINGS LOOSE. R&R ATTACH FITTING FASTENERS PER SRM. 2 L 7 2 4F RT A16WE 2001091300047 20010913 00047 NM 2001 9 13 SWAA012472 1 20010822 A 3210 6959886 FITTING BOEING 737 7375H4 138449D NM LH WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 519SW 25318 DURING SCHEDULED D CHECK AT DALFORT, FOUND LH MLG BEAM STABILIZER FITTING CORRODED. R&R FITTING PER MM. 2 L 7 2 4F RT A16WE 2001091300048 20010913 00048 2001 9 13 SWAA012473 4 20010825 A 2565 6557463 BRACKET BOEING 737 7375H4 138449D NM CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 524SW 26566 DURING SCHEDULED D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE FLOOR BRACKET CORRODED. R& R EVAC SLIDE FLOOR BRACKET PER SRM. 2 L 7 2 4F RT A16WE 2001091300049 20010913 00049 NM 2001 9 13 SWAA012474 1 20010904 A 5310 65C27314 CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 524SW 26566 DURING SCHEDULED D CHECK, FOUND STR CLIPS CRACKED ( 4 EA ) AT BS 312, STR 24R, BS 663, STR 10L, BS 683, STR 4L, BS 1088, STR 17L. R&R STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001091300050 20010913 00050 NM 2001 9 13 SWAA012479 1 20010905 A 3350 100031 LIGHT BOEING 737 737301 1384611 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 OVERHEAD EMERGENCY LIGHT BROKEN AT ROW 22 R&R LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001091300051 20010913 00051 2001 9 13 SWAA012480 4 20010903 A 2565 D31354 SLIDE BOEING 737 7373G7 1384595 NM AFT ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PARTIALLY PULLED FROM CONTAINER. REINSTALLED EVAC S LIDE PER MM. 2 L 7 2 4F RT A16WE 2001091300052 20010913 00052 NM 2001 9 13 SWAA012482 1 20010905 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 327SW 23691 DURING SCHEDULED C3 CHECK, FOUND LH EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2001091300053 20010913 00053 NM 2001 9 13 SWAA012483 1 20010905 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740, STR 17R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001091300054 20010913 00054 NM 2001 9 13 SWAA012484 1 20010801 A 5310 6546529 SHEAR TIE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED SPECIAL VISIT, FOUND FRAME SHEAR TIE CRACKED AT BS 360, STR 14L. R&R SHEAR TIE PER SRM. 2 L 7 2 4F A16WE 2001091300055 20010913 00055 NM 2001 9 13 SWAA012485 1 20010904 A 5310 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 524SW 26566 DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 312, STR 24R. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2001091300056 20010913 00056 NM 2001 9 13 SWAA012486 1 20010906 A 2731 65C35943 BEARING BOEING 737 7373Y0 1384671 NM RH ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED C2 CHECK, RH ELEVATOR FAILED FREE PLAY CHECK. R&R RH ELEVATOR CONTROL BEARIN G PER MM. 2 L 7 2 4F RT A16WE 2001091300057 20010913 00057 NM 2001 9 13 SWAA012487 1 20010906 A 2731 6573782 TAB BOEING 737 7373Y0 1384671 NM RH ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED C2 CHECK, RH ELEVATOR TAB FAILED FREE PLAY CHECK. R&R RH ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2001091300058 20010913 00058 NM 2001 9 13 SWAA012488 1 20010906 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 1.7 INCH LONG AT BS 523-524, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001091300059 20010913 00059 NM 2001 9 13 SWAA012490 1 20010908 A 2560 6556633 SIGN BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 376SW 26584 EMERGENCY EXIT SIGN LH OVERWING FELL OUT. SECURED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2001091300060 20010913 00060 NM 2001 9 13 SWAA012492 1 20010907 A 3350 300432 LIGHT BOEING 737 7372T4 1384492 NM FUSELAGE BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED 1/4D CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT AFT BULB INOP. RELAMPED EXIT LI GHT PER MM. 2 L 7 2 4F A16WE 2001091300061 20010913 00061 2001 9 13 SWAA012496 4 20010908 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 063SW 22061 DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE P ER MM. 2 L 7 2 4F A16WE 2001091300062 20010913 00062 NM 2001 9 13 SWAA012497 1 20010901 A 3350 07912 COVER BOEING 737 7372T4 1384492 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED 1/4D CHECK, FOUND EEPLS COVERS LOOSE AT ROWS 20 & 21. SECURED COVERS PER MM. 2 L 7 2 4F A16WE 2001091300063 20010913 00063 NM 2001 9 13 SWAA012498 1 20010908 A 5310 6517582 WEB BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17.1 & WL 230. R&R WEB PER SRM. 2 L 7 2 4F A16WE 2001091300064 20010913 00064 NM 2001 9 13 SWAA012500 1 20010906 A 5753 6546435 FLAP BOEING 737 7373T5 NM RH WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED C3 CHECK, FOUND RH WING OTBD AFT FLAP DELAMINATED. R&R AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2001091300065 20010913 00065 NM 2001 9 13 SWAA012501 1 20010906 A 5310 6517583 WEB BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL WEB CRACKED AT BS 180, LBL 5.7 & WL 183. REPAI RED WEB PER SWA RA 1-253-263 REV.1. 2 L 7 2 4F A16WE 2001091300066 20010913 00066 NM 2001 9 13 SWAA012502 1 20010908 A 5754 6573714 SLAT BOEING 737 7373H4 1384600 NM LH WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 331SW 23695 DURING SCHEDULED C3 CHECK, FOUND # 2 L/E SLAT CRACKED 6 INCHES LONG ON LOWER SKIN, OTBD OF INBD AUX TRACK. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2001091300067 20010913 00067 NM 2001 9 13 SWAA012503 1 20010904 A 5751 6973066 FITTING BOEING 737 7375H4 138449D NM LH WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 519SW 25318 DURING SCHEDULED D CHECK AT DALFORT, FOUND LH AILERON INBD ATTACH FITTING CRACKED. R&R AILERON FI TTING PER SRM. 2 L 7 2 4F RT A16WE 2001091300068 20010913 00068 NM 2001 9 13 SWAA012504 1 20010907 A 5330 6545765 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED BC4 CHECK, FOUND FUSELAGE SKIN CRACKED 4.4 INCHES LONG AT BS 498, STR 10R. REPAIRED SKIN PER SWA RA 1-353-2641. 2 L 7 2 4F RT A16WE 2001091300069 20010913 00069 NM 2001 9 13 SWAA012505 1 20010906 A 5315 BAC1509 BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO BIN FLOOR BEAMS CORRODED ( 3 EA ) AT BS'S 795, 813 & 826, LBL3. REPAIRED FLOOR BEAMS PER SWA RA 1-A53-2021. 2 L 7 2 4F RT A16WE 2001091300070 20010913 00070 NM 2001 9 13 SWAA012506 1 20010906 A 5315 BAC1509 BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO BIN FLOOR BEAMS CORRODED ( 2 EA ) AT BS 859, LBL 12 & LBL 8. REPAIRED FLOOR BEAMS PER SWA RA 1-A53-2021. 2 L 7 2 4F RT A16WE 2001091300071 20010913 00071 NM 2001 9 13 SWAA012507 1 20010909 A 2731 6565310 TORQUE TUBE BOEING 737 7373A4 1384585 NM LH ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED C4 CHECK, LH ELEVATOR FAILED FREE PLAY CHECK. R&R ELEVATOR BUSS ASSY OUTPUT T ORQUE TUBE PER MM. 2 L 7 2 4F RT A16WE 2001091300072 20010913 00072 NM 2001 9 13 SWAA012509 1 20010908 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 931, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001091300073 20010913 00073 NM 2001 9 13 SWAA012511 1 20010906 A 5310 6516301 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 524SW 26566 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17L. REPAIRED FRAME PER SR M. 2 L 7 2 4F RT A16WE 2001091300074 20010913 00074 NM 2001 9 13 SWAA012512 1 20010909 A 2731 65C26384 TAB BOEING 737 7373K2 13844BA NM LH ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 340LV 23738 DURING SCHEDULED C2 CHECK, FOUND LH ELEVATOR TAB WORN AT HINGE POINTS. R&R LH ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2001091300075 20010913 00075 NM 2001 9 13 SWAA012513 1 20010910 A 5330 6545776 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR FUSELAGE SKIN CRACKED AT UPPER DOOR HINGE CUT OUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001091300076 20010913 00076 NM 2001 9 13 SWAA012514 1 20010910 A 5330 6545768 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR FUSELAGE SKIN CRACKED AT BS 297, STR 17R. RE PAIRED SKIN PER SWA RA 1-253-2638. 2 L 7 2 4F A16WE 2001091300077 20010913 00077 NM 2001 9 13 SWAA012515 1 20010909 A 5610 5893543130 WINDOW BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA A UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 SW 07 312SW 23334 ( DIVERSION )…………………………..R1 COCKPIT WINDOW ARCED & SHATTERED. R&R WINDOW & WINDOW HEAT CONTROL LER PER MM. 2 L 7 2 4F RT A16WE 2001091300078 20010913 00078 2001 9 13 SWAA012518 4 20010906 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM AFT ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 DURING SCHEDULED 1/4D CHECK AT DALFORT, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE. R &R EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001091300079 20010913 00079 NM 2001 9 13 SWAA012519 1 20010907 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 DURING SCHEDULED 1/4D CHECK AT DALFORT, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR, FWD LOWER CORNER CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001091300080 20010913 00080 NM 2001 9 13 SWAA012522 1 20010910 A 5310 6517582 WEB BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17.1 & WL 230. R&R WEB PER SRM. 2 L 7 2 4F A16WE 2001091300081 20010913 00081 NM 2001 9 13 SWAA012523 1 20010910 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING WALKAROUND INSPECTION FOUND ( 2 EA ) FUSELAGE SKIN CRACKS AT BS 420 & 500B, STR 10R. REPAIRED SKINS PER SWA RA 1-A53-2545 & SWA RA 1-353-2645. 2 L 7 2 4F RT A16WE 2001091300092 20010913 00092 NM 2001 9 13 DL733011356 1 20010818 A 3260 SAFETY SWITCH BOEING 737 737347 1384647 NM LANDING GEAR OUT OF ADJ A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 302WA 23182 UPON DEPARTURE ATL LDG WOULD NOT RETRACT. GEAR HANDLE WOULD ONLY RAISE TO THE OFF POSITION. ADJUSTED AND TESTED GROUND S POILER INTERLOCK AND SAFETY SWITCHES. REF MM 27-62-51-5 AND E2-09-01-5. ALL CHECKS OK. 2 L 7 2 4F RT A16WE 2001091300094 20010913 00094 NM 2001 9 13 DL738011401 1 20010824 A 2120 ODOR BOEING 737 737832 13844CF NM CABIN DETECTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 3743H 30836 DURING CRUISE FLIGHT ATTENDANT REPORTED AN ELECTRICAL ODOR IN CABIN AT SEAT ROWS 17&18. FLIGHT ATTENDANT TURNED OFF CABIN LIGHTS AND RECIRCULATION FANS WERE TURNED OFF. SMELL DISAPPEARED AND NO VISIBLE SMOKE WAS NOTED IN THE CABIN D URING THIS PERIOD. EXAMINED WIRING UNDER PASS SERVICE UNITS AND CEILING PANELS FROM ROWS 16-19. NO TROUBLE FOUND. C HECKED AIR CONDITIONING BAYS AND RECIRCULATION FANS AREA. NO OVERHEATING OR SMELL NOTED. RAN BOTH ENGINES TO POWER W ITH BOTH PACKS RUNNING, ALL CABIN LIGHTS ON, VIDEO SYS ON, AND OVEN/COFFEEMAKERS ON. NO TROUBLE FOUND. 2 L 7 2 4F RT A16WE 2001091300095 20010913 00095 NM 2001 9 13 DL73K011465 1 20010901 A 3240 WARNING SYSTEM BOEING 737 737232 1384475 NM COCKPIT MALFUNCTIONED A DALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 27 316DL 23088 UPON INITIAL T/O ROLL EWR, AUTOBRAKE DISARM LIGHT ILLUMINATED. CYCLED RTO SWITCH AND THE AUTOBRAKE LIGHT ILLUMINATED AGA IN. PERFORMED AUTOBRAKE TEST PER M/M. UNABLE TO DUPLICATE. 2 L 7 2 4F RT A16WE 2001091300098 20010913 00098 NM 2001 9 13 DL757011402 1 20010825 A 2931 TC125UK00ZY1 INDICATOR BOEING 757 757232 1384965 NM HYD PRESSURE LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 631DL 23612 IR - LT HYDRAULIC SYSTEM DROPPED TO .41 FOLLOWED POM PROCEDURES. FOUND LT PRESSURE DIFFERENTIAL INDICATOR LEAKING AT PRESSURE MODULE. REPLACED INDICATOR AND LEAK CHECK OK. 2 L 7 2 4F RT A2NM 2001091300101 20010913 00101 NM 2001 9 13 DL757011412 1 20010826 A 3350 BPS73 CHARGER BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 664DN 25012 ON LAYOVER FOUND R2 DOOR EXTERIOR EMERGENCY LIGHT INOP. REPLACED BATTERY CHARGER. LIGHT OPS CKECKS GOOD 2 L 7 2 4F RT A2NM 2001091300106 20010913 00106 NM 2001 9 13 DL757011426 1 20010829 A 2131 211738813 CONTROLLER BOEING 757 757232 1384965 NM NR 1 MALFUNCTIONED A DALA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 27 618DL 22908 CRUISE ALT 370 -DISCRETE CABIN ALT LIGHT ILLUM AND ASSOCIATED EICAS MSG CBN ALT APPEARED. CABIN ALT REACHED 11500 AND SL OWLY INCREASING BY TIME WE WERE EMERG DESCENDING. CABIN REMAINED ABOVE 10000 DURING DESCENT UNTIL APPROX 140 MSL. AFTER LEVELING AT 100 MSL CABIN ALT CONTINUED TO DESCEND TO LOW THOUSANDS 1000-2000 FT. THIS OCCURRED WHILE IN AUTO 1 ON CABIN PRESS PANEL. BITE CHECKED NR 1 AND NR 2 AUTOPRESS CONTROLLERS, NOFAULTS. REPLACED NR 1 AUTO PRESS. CONTROLLER AND SEL P NL PER M/M. REPLACED NR 1 PRESS. CONTROLLER C/B. PRESS A/C CKS OK. CKED IXT 2 L 7 2 4F RT A2NM 2001091300108 20010913 00108 NM 2001 9 13 DL757011435 1 20010830 A 3350 0201991008 LIGHT BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 645DL 24216 EMERGENCY LIGHT INOP. AT SEAT 20DEF. REPLACED EMERGENCY LIGHT ASSY. AT 20DEF; OPS CHECK GOOD. DELTA PART NUMBER 33320153 2 INSTALLED. 2 L 7 2 4F RT A2NM 2001091300111 20010913 00111 NM 2001 9 13 DL757011466 1 20010902 A 3242 AHA1884 BRAKE BOEING 757 757232 1384965 NM MLG DAMAGED A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 603DL 22810 NR FIVE BRAKE TWISTED AND PADS COMING APART, REPLACED BRAKE. 2 L 7 2 4F RT A2NM 2001091300112 20010913 00112 NM 2001 9 13 DL757011473 1 20010904 A 3350 GE3171 LIGHT BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 656DL 24396 EMERG LIGHT ABOVE SEAT 24 DEF INOP, RELAMPED. 2 L 7 2 4F RT A2NM 2001091300115 20010913 00115 NM 2001 9 13 DL757011474 1 20010904 A 3242 AHA1884 BRAKE BOEING 757 757232 1384965 NM MLG FIRE A DALA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 SO 27 636DL 23763 RAMP WORKER NOTICED SMALL GREASE FIRE ON NR 7 BRAKE UPON ARRIVAL. NO ABNORMAL BRAKE TEMPS NOTED BY CREW VIA COCKPIT INDI CATIONS. REPLACED BRAKE ASSY. NO DAMAGE FOUND. 2 L 7 2 4F RT A2NM 2001091300116 20010913 00116 NM 2001 9 13 DL757011478 1 20010904 A 3350 LIGHT BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 612DL 22819 R2 EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A2NM 2001091300117 20010913 00117 NM 2001 9 13 DL757011481 1 20010904 A 3350 767 LIGHT BOEING 757 757232 1384965 NM L3 DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 6706Q 30422 L3 DOOR EMERGENCY LIGHT BURNED OUT. RELAMPED. 2 L 7 2 4F RT A2NM 2001091300118 20010913 00118 2001 9 13 SWAA012372 4 20010822 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE PER MM. 2 L 7 2 4F A16WE 2001091300119 20010913 00119 2001 9 13 SWAA012373 4 20010822 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE PER MM. 2 L 7 2 4F A16WE 2001091300120 20010913 00120 NM 2001 9 13 SWAA012382 1 20010823 A 2782 3818001001 ACTUATOR BOEING 737 7377H4 NM L/E SLAT FAILED A SWAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 07 731SA 27863 (AIR TURNBACK) AFTER TAKEOFF, L/E TRANSIT LIGHT STAYED ILLUMINATED. REMOVED AND REPLACED NR 4 & 7 L/E SLAT ACTUATORS PE R MM. 2 L 7 2 4F RT A16WE 2001091300121 20010913 00121 NM 2001 9 13 SWAA012384 1 20010824 A 3350 6104789 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED SERVICE CHECK, FOUND RT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2001091300122 20010913 00122 NM 2001 9 13 SWAA012385 1 20010824 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM COCKPIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 396SW 27690 DURING SCHEDULED C3 CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001091300123 20010913 00123 NM 2001 9 13 SWAA012386 1 20010823 A 3350 2013 BATTERY BOEING 737 7377H4 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 724SW 27856 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT MID CABIN. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001091300124 20010913 00124 NM 2001 9 13 SWAA012389 1 20010820 A 5311 BAC1506 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED D-CHECK, FOUND HORIZONTAL CHORD CORRODED AT LWR APU AIR INLET BETWEEN BS 1167-1177. REMOVED AND REPLAC ED CHORD PER SRM. 2 L 7 2 4F A16WE 2001091300126 20010913 00126 2001 9 13 SWAA012398 4 20010826 A 2565 61621469 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 364SW 26575 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001091300128 20010913 00128 NM 2001 9 13 SWAA012400 1 20010826 A 3350 BR2013 COVER BOEING 737 7372T4 1384492 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVER LOOSE IN CABIN. SECURED EEPLS TRACK COVER PER MM. 2 L 7 2 4F A16WE 2001091300129 20010913 00129 2001 9 13 SWAA012403 4 20010825 A 2565 D31354 SLIDE BOEING 737 7377H4 NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 742SW 29278 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001091300130 20010913 00130 NM 2001 9 13 SWAA012405 1 20010826 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 060SW 21812 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGH T PER MM. 2 L 7 2 4F A16WE 2001091300132 20010913 00132 NM 2001 9 13 SWAA012409 1 20010826 A 3350 610478 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2001091300135 20010913 00135 NM 2001 9 13 SWAA012415 1 20010826 A 2612 100012701 CONTROL UNIT BOEING 737 7373L9 1384470 NM CARGO BAY ERRATIC A SWAA K NONE N FALSE WARNING CR CRUISE 1 SW 07 657SW 23331 CARGO COMP FIRE INDICATION DURING FLIGHT LASTED ONLY 2 TO 3 SECONDS, REMAINDER OF FLIGHT NORMAL. REMOVED AND REPLACED C CU PER MM. 2 L 7 2 4F RT A16WE 2001091300137 20010913 00137 NM 2001 9 13 SWAA012416 1 20010826 A 2782 654465116 ACTUATOR BOEING 737 7372H4 138448C NM L/E SLAT FAILED A SWAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 07 071SW 22358 (AIR TURNBACK) NR 4 L/E SLAT WOULD NOT RETRACT. REMOVED AND REPLACED NR 4 SLAT ACTUATOR PER MM. 2 L 7 2 4F A16WE 2001091300138 20010913 00138 2001 9 13 SWAA012421 4 20010827 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 373SW 26581 DURING SCHEDULED C4 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001091300141 20010913 00141 NM 2001 9 13 SWAA012422 1 20010828 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED 1/4D CHECK, FOUND BOTH AFT DOOR EVACUATION SLIDE GIRT BAR FLOOR ATTACH BRACKETS CORRODED. REMOVED AND REPLACED ATTACH BRACKETS PER MM. 2 L 7 2 4F RT A16WE 2001091300145 20010913 00145 NM 2001 9 13 SWAA012423 1 20010827 A 5411 BAC1503 FRAME BOEING 737 7373H4 1384600 NM RT PYLON CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED A1 CHECK, FOUND NR 2 ENG PYLON STRUT AFT INBOARD CHORD CRACKED, NAC STA 354. REPAIRED CHORD PER SWA RA 1-354-0388. 2 L 7 2 4F RT A16WE 2001091300147 20010913 00147 NE 2001 9 13 SWAA012431 2 20010827 A 7230 CFN563 COMPRESSOR BOEING 737 7373Y0 1384671 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE STALLED A SWAA A UNSCHED LANDING R X PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT CL CLIMB 1 SW 07 308SA 23498 720778 (AIR TURNBACK) INFLIGHT ENGINE SHUT DOWN, DECLARED EMERGENCY. AT 13,000 FT NR 1 ENG COMPRESSOR STALLED, EGT INDICATED 9 30 DEGS, ENG VIBRATION FELT, AS POWER WAS REDUCED ENG FLAMED OUT. REMOVED AND REPLACED NR 1 ENG PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091300148 20010913 00148 NM 2001 9 13 SWAA012437 1 20010830 A 3350 6104789 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 090SW 22905 DURING SCHEDULED C1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2001091300149 20010913 00149 NM 2001 9 13 SWAA012440 1 20010901 A 3350 20131A BATTERY BOEING 737 7377H4 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 724SW 27856 DURING SCHEDULED RON, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001091300150 20010913 00150 NM 2001 9 13 SWAA012441 1 20010903 A 3350 610478 BATTERY BOEING 737 7373Y0 1384671 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 665WN 23497 DURING SCHEDULED SERVICE CHECK, FOUND LT LOWER FWD EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001091300151 20010913 00151 2001 9 13 SWAA012442 4 20010903 A 2565 D31354 SLIDE BOEING 737 7377H4 NM GALLEY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 774SW 27882 DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EVAC SLIDES OUT OF ADJUST AT BOTH GALLEY DOORS. ADJUSTED EVAC SLIDES PER MM. 2 L 7 2 4F RT A16WE 2001091300152 20010913 00152 NM 2001 9 13 SWAA012444 1 20010827 A 3350 65C34691 LIGHT BOEING 737 7373A4 1384585 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 674AA 23252 DURING SCHEDULED 1/4D CHECK, FOUND OVERHEAD EMERGENCY EXIT BULL NOSE LIGHT INOP AT ROW 18 ABC. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001091300153 20010913 00153 NM 2001 9 13 SWAA012445 1 20010827 A 3350 65C27093 LIGHT BOEING 737 7373A4 1384585 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 674AA 23252 DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001091300154 20010913 00154 NM 2001 9 13 SWAA012451 1 20010831 A 3350 20121 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 653SW 28398 DURING SCHEDULED C4 CHECK, FOUND EEPLS INOP BETWEEN ROW 11 & 17. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001091300155 20010913 00155 2001 9 13 SWAA012463 4 20010902 A 2565 D31354 SLIDE BOEING 737 737317 138447P NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001091300156 20010913 00156 2001 9 13 SWAA012464 4 20010903 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 074SW 22674 DURING SCHEDULED C4 CHECK, FOUND BOTH AFT DOOR EMERGENCY EVAC SLIDES PRESS IND OUT OF VIEW. REPOSITIONED SLIDES PER MM. 2 L 7 2 4F A16WE 2001091300157 20010913 00157 2001 9 13 SWAA012465 4 20010901 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 BOTH AFT DOOR EMERGENCY EVAC SLIDES PRESS IND OUT OF VIEW. REPOSITIONED SLIDES PER MM. 2 L 7 2 4F A16WE 2001091300158 20010913 00158 NM 2001 9 13 SWAA012466 1 20010901 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN EXPOSED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 638SW 27711 EEPLS WIRING EXPOSED AT ROW 12. SECURED EEPLS WIRING PER MM. 2 L 7 2 4F RT A16WE 2001091300159 20010913 00159 NM 2001 9 13 SWAA012467 1 20010904 A 3350 BR2013 TRACK BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 362SW 26573 EEPLS LENS MISSING AT MID CABIN AND FLOOR TRACK BROKEN. REMOVED AND REPLACED EEPLS LENS AND FLOOR TRACK SEGMENT. 2 L 7 2 4F RT A16WE 2001091300160 20010913 00160 NM 2001 9 13 SWAA012470 1 20010905 A 3350 100885 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED RON, FOUND EEPLS INOP AT AFT SECTION OF CABIN. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001091300162 20010913 00162 NM 2001 9 13 SWAA012471 1 20010905 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 654SW 28399 DURING SCHEDULED C4 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 14. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001091300163 20010913 00163 2001 9 13 SWAA012475 4 20010906 A 2565 22D22901151 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001091300164 20010913 00164 2001 9 13 SWAA012476 4 20010905 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001091300165 20010913 00165 2001 9 13 SWAA012477 4 20010906 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 611SW 27697 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001091300166 20010913 00166 2001 9 13 SWAA012478 4 20010906 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 632SW 27707 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001091300167 20010913 00167 NM 2001 9 13 SWAA012481 1 20010901 A 3350 300432 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 327SW 23691 DURING SCHEDULED BC3 CHECK, FOUND RT AFT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001091300168 20010913 00168 2001 9 13 SWAA012489 4 20010906 A 2565 D31354 SLIDE BOEING 737 7377H4 NM AFT ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 725SW 27857 AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001091300169 20010913 00169 NM 2001 9 13 SWAA012491 1 20010909 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 388SW 26591 EEPLS INOP AT SEVERAL LOCATIONS IN CABIN. RELAMPED AND SECURED WIRING PER MM. 2 L 7 2 4F RT A16WE 2001091300170 20010913 00170 NM 2001 9 13 SWAA012493 1 20010906 A 3350 20131A BATTERY BOEING 737 7377H4 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 724SW 27856 DURING SCHEDULED RON, FOUND EEPLS INOP AT MID CABIN. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001091300171 20010913 00171 NM 2001 9 13 SWAA012494 1 20010906 A 3350 20121 BATTERY BOEING 737 7377H4 NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 724SW 27856 DURING SCHEDULED RON, FOUND FWD CABIN EEPLS BATTERY PIN CONNECTOR BENT. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001091300172 20010913 00172 NM 2001 9 13 SWAA012495 1 20010907 A 3350 100885 BATTERY BOEING 737 7377H4 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 798SW 28436 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT AFT CABIN. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001091300173 20010913 00173 NM 2001 9 13 SWAA012499 1 20010907 A 3350 57771 CAP BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 331SW 23695 DURING SCHEDULED C3 CHECK, FOUND EEPLS END CAP MISSING AT AFT CABIN. INSTALLED END CAP PER MM. 2 L 7 2 4F RT A16WE 2001091300174 20010913 00174 NM 2001 9 13 SWAA012508 1 20010908 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 362SW 26573 DURING SCHEDULED C4 CHECK, FOUND TWO EEPLS INOP AT OVERWING EXIT. SECURED WIRES PER MM. 2 L 7 2 4F RT A16WE 2001091300175 20010913 00175 2001 9 13 SWAA012510 4 20010910 A 2565 D31354 SLIDE BOEING 737 737317 138447P NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001091300176 20010913 00176 NM 2001 9 13 SWAA012516 1 20010909 A 3411 0851CM2 PROBE BOEING 737 7375H4 138449D NM PITOT/STATIC SYS LEAKING A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 519SW 25318 (AIR TURNBACK) FEEL DIFF PRESSURE LIGHT ILLUMINATED AFTER TAKEOFF. FOUND LT AND RT PITOT PROBES LEAKING. REMOVED AND R EPLACED BOTH PITOT PROBES PER MM. 2 L 7 2 4F RT A16WE 2001091300177 20010913 00177 NM 2001 9 13 SWAA012517 1 20010911 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 640SW 27713 DURING SCHEDULED C3 CHECK, FOUND EEPLS LOOSE AT FWD ENTRY. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001091300180 20010913 00180 NM 2001 9 13 SWAA012520 1 20010911 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 640SW 27713 DURING SCHEDULED C3 CHECK, FOUND RT EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001091300184 20010913 00184 NM 2001 9 13 SWAA012521 1 20010910 A 5315 6545410 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED 1/2D CHECK, FOUND 2 FLOORBEAMS CORRODED AT BS 859, LBL 3 & RBL 14. REPAIRED FLOORBEAMS PER SWA 1-A53-2 021. 2 L 7 2 4F RT A16WE 2001091300201 20010913 00201 NM 2001 9 13 AWXA0002217 1 20010903 A 5310 140N200283 SHEAR TIE BOEING 757 757225 1384959 NM FS840 BL0 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 915AW 22209 D: Fwd Cargo Compt. F/S 840 BL0 Fame Shear tie corroded.C: Removed Fwd Shear tie SRM 51-40-02, Fabricated new Shear tie in DRW. 140 N 2002 - 813 Sht. 7075-0-71 R 7028, install Shear tie IAW SRM 51-40-02 2 L 7 2 4F RT A2NM 2001091700064 20010917 00064 NM 2001 9 17 AWXA0002218 1 20010801 A 5330 6573741219 DOUBLER BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 R1 DOOR LOWER AFT CORNER REPAIR DOUBLER FWD EDGE CRACKED .25 INCH AT TAPERED FILLER, FUSELAGE CUTOUT BS 318. REMOVED AN D REPLACED TAPED FILLER PER SRM 53-10-01 PG 205 & 206. 2 L 7 2 4F RT A16WE 2001091700068 20010917 00068 NM 2001 9 17 AWXA0002222 1 20010812 A 5313 6552988607 STRINGER BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 STRINGER 25 LT AT BS 967 CORRODED. REMOVED STRINGER AND REPLACED WITH NEW STRINGER SECTION FROM BS 967 TO 1016, IAW B73 7-300 SRM 51-40-02 PG 10 & 11. 2 L 7 2 4F RT A16WE 2001091300202 20010913 00202 NM 2001 9 13 AWXA0002223 1 20010803 A 5313 655162829 STRINGER BOEING 737 73733A 1384673 NM STR 26L BS 947 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 D: BS 947 STR 26L corrodedC: Removed stringer, repaired & reinstalled stringer 26L @ BS 907-1016 IAW Boeing 737 SRM 53-0 0-03 pg 201-207, 51-40-02 pg 3-4, 51-20-01 pg 10 & 47 & 51-21-00 pg 1 2 L 7 2 4F RT A16WE 2001091300203 20010913 00203 NM 2001 9 13 AWXA0002224 1 20010803 A 5313 655162812 STRINGER BOEING 737 73733A 1384673 NM STR 27R BS 965 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 D: Stringer 27R corroded at BS 965C: Removed, repaired & reinstalled stringer 27R @ BS 907-1016 IAW boeing 737 SRM 53-00 -03 pg 101-102, 53-00-03 pg 201-207, 51-20-01-pgs. 1,10 & 47 & 51-40-02 pg 3-4 2 L 7 2 4F RT A16WE 2001091300204 20010913 00204 NM 2001 9 13 AWXA0002225 1 20010803 A 5313 65457768 STRINGER BOEING 737 73733A 1384673 NM STR 26R BS1006 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 D: Stringer 26R BS 1006-1016 corrodedC: Removed and replaced stringer IAW 737-300 SRM 51-40-60 pgs 10&11 2 L 7 2 4F RT A16WE 2001091300205 20010913 00205 NM 2001 9 13 AWXA0002226 1 20010801 A 5315 65C33940 BEAM BOEING 737 73733A 1384673 NM BS 294 LBL 19 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 D: Corrosion on top of floor beam BS 294 LBL 19C: Repaired floor beam IAW B737-300 SRM 53-10-51 pgs 220-223 2 L 7 2 4F RT A16WE 2001091300206 20010913 00206 NM 2001 9 13 AWXA0002227 1 20010803 A 5313 655162829 STRINGER BOEING 737 73733A 1384673 NM STR 27L BS 948 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 D: Stringer 27L corroded at BS 948 and 1003.5C: removed, repaired and reinstalled stringer IAW B737-300 SRM 51-40-02 pgs 3-4 & 38 SRM 53-00-03 pgs 201-207 2 L 7 2 4F RT A16WE 2001091700075 20010917 00075 NM 2001 9 17 AWXA0002228 1 20010811 A 5312 654658571 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 AFT PRESSURE BULKHEAD INNER SKIN GOUGED 1 INCH OUTBOARD OF STRINGER 22R. REPAIRED AFT PRESSURE BULKHEAD IAW AWA ER 03-5 312-01242-DL2. 2 L 7 2 4F RT A16WE 2001091300207 20010913 00207 NM 2001 9 13 AWXA0002229 1 20010805 A 5310 6552988 SKIN BOEING 737 73733A 1384673 NM BS 948 STR 11L CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 D: L2 door fuselage upper hinge cut out cracked BS 948C: Removed damaged area and installed repair IAW 737 SRM 53-60-01 fig 205 pgs 210-212 2 L 7 2 4F RT A16WE 2001091700076 20010917 00076 NM 2001 9 17 AWXA0002230 1 20010801 A 5312 6545833640 PRESSURE PANEL BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 COCKPIT FLOOR WEB CRACKED LBL 24, WL 207, BS 180. REMOVED AND REPLACED FLOOR WEB IAW ER 03-5311-01218-DD1. 2 L 7 2 4F RT A16WE 2001091300208 20010913 00208 NM 2001 9 13 AWXA0002231 1 20010801 A 5313 6516300512 WEB BOEING 737 73733A 1384673 NM BS 178 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 D: Cracks at 5 EA fastener holes BS 178 BLKHD web Fwd side, WL 234, RBL8,9,10,11,& 12C: Repaired damaged area IAW 737-30 0 SRM 53-10-08 pg 269-278 2 L 7 2 4F RT A16WE 2001091700082 20010917 00082 NM 2001 9 17 AWXA0002235 1 20010801 A 5312 65163007 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 CRACK RBL,1.5 WL 205 BS 178 BLKHD WEB FWD SIDE BENEATH ANGLE. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER IAW B737-300 S RM 53-10-08 PG 286-291. 2 L 7 2 4F RT A16WE 2001091300209 20010913 00209 NM 2001 9 13 AWXA0002236 1 20010729 A 5330 65C35778 SKIN BOEING 737 73733A 1384673 NM BS 908 STR 27R CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 D: Fastener heads pulling BS 967 STR 27RTC: Removed skin BS 908 to 1016 Removed corrosion, removal of material within li mits, treat & primed and reinstalled skin IAW B737-300 SRM 51-40-02 pg 38 SRM 53-00-01 pg 104, SRM 51-20-01 pg 1 & SRM 5 1-40-02 pg 2 & 3 2 L 7 2 4F RT A16WE 2001091300210 20010913 00210 NM 2001 9 13 AWXA0002238 1 20010827 A 5310 65729032 SHEAR TIE BOEING 737 73733A 1384673 NM BS 967 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 D: Clip corroded at BS 967 between STR 27R and 26RC: Repaired shear tie at BS 967 STR 27-26R IAW B737 SRM 53-00-07 pgs 2 19-221 2 L 7 2 4F RT A16WE 2001091300211 20010913 00211 NM 2001 9 13 AWXA0002239 1 20010827 A 5330 65184201 SKIN BOEING 737 73733A 1384673 NM BS 338 STR 17 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 D: L1 Door fuselage cutout lower aft corner cracked 1/4" out of fastener hole BS 338C: Repaired skin at L1 door cutout l ower aft corner IAW AWA ER 03-5330-01234-DD1 2 L 7 2 4F RT A16WE 2001091300212 20010913 00212 NM 2001 9 13 AWXA0002240 1 20010803 A 5310 65516242 STRAP BOEING 737 73733A 1384673 NM BS 967 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 D: Aft LAV service door frame inner doubler corroded at BS 967, 986.5 & 1006C: Aft LAV service door inner doubler was co rroded beyond limits, repaired inner doubler IAW ER 03-5313-01234-DL2 2 L 7 2 4F RT A16WE 2001091300213 20010913 00213 NM 2001 9 13 AWXA0002241 1 20010801 A 5311 651630007 WEB BOEING 737 73733A 1384673 NM BS 178 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 D: Crack RBL 15, WL 221, BS 178 Blkhd web Fwd side beneath strapC: Cutout damaged area & installed doubler IAW B737-300 SRM 53-10-08 pg 291 2 L 7 2 4F RT A16WE 2001091700084 20010917 00084 NM 2001 9 17 AWXA0002242 1 20010729 A 5312 65163007 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 BLKHD 178 WEB FWD SIDE LBL 4.8 WL 193 AND 197 2 EA CRACKS EMANATING FROM BENEATH STRAP. CUT OUT DAMAGE, INSTALLED DOUBL ER IAW B737-300 SRM 53-10-8 PG 287-291. 2 L 7 2 4F RT A16WE 2001091700085 20010917 00085 NM 2001 9 17 AWXA0002243 1 20010801 A 5312 65163007 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 AFT SIDE BS 178 BLKHD WEB 2 CRACKS LBL 7 AND RBL 7 WL 184. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW B737-300 SRM 53-10- 08 PG 287-291. 2 L 7 2 4F RT A16WE 2001091300214 20010913 00214 NM 2001 9 13 AWXA0002244 1 20010801 A 5311 65163007 WEB BOEING 737 73733A 1384673 NM BS 178 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 D: Crack LBL 4.8 WL 214 BS 178 Blkhd web Fwd side beneath strapC: Cutout damaged & installed doubler IAW B737-300 SRM 53 -10-08 pgs 286-291 2 L 7 2 4F RT A16WE 2001091300215 20010913 00215 NM 2001 9 13 AWXA0002245 1 20010729 A 5311 65163007 WEB BOEING 737 73733A 1384673 NM BS 178 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 D: BS 178 Blkhd web Fwd side RBL 4.8 WL 197 crack emanating from beneath strap.C: Cutout damaged area and installed doub ler IAW B737-300 SRM 53-10-08 pgs 286-291 2 L 7 2 4F RT A16WE 2001091700086 20010917 00086 NM 2001 9 17 AWXA0002246 1 20010731 A 5330 6545776 SKIN BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 FASTENER HEADS PULLING BS 947 STR 27 LT. CORROSION OUT OF LIMITS. INSTALLED REPAIR DOUBLER IAW ER 03-5361-01232-BA1. 2 L 7 2 4F RT A16WE 2001091300216 20010913 00216 NM 2001 9 13 AWXA0002247 1 20010814 A 5313 654541041 WEB BOEING 737 73733A 1384673 NM BS 178 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 D: Ultrasonic crack indication RBL 4.8 WL 214 BS 178 Bulkhead web fwd side beneath strapC: Repaired Bulkhead web IAW B73 7 SRM 53-10-8 pgs 286-298 2 L 7 2 4F RT A16WE 2001091700087 20010917 00087 NM 2001 9 17 AWXA0002248 1 20010803 A 5310 654656445 SHEAR TIE BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 SHEAR TIE CORRODED AT BS 986.5 BETWEEN STR 26R-25R. REMOVED AND REPLACED SHEAR TIE IAW B737-300 SRM 51-40-02 FIG 8 & 51 -40-02 PG 3. 2 L 7 2 4F RT A16WE 2001091300217 20010913 00217 NM 2001 9 13 AWXA0002249 1 20010803 A 5330 6551625502 SKIN BOEING 737 73733A 1384673 NM BS 947 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 D: Inner skin for potable water pan cutout BS 947-967 corrodedC: Removed & replaced inner skin IAW B737-300 SRM 51-40-02 pg 3 2 L 7 2 4F RT A16WE 2001091700088 20010917 00088 NM 2001 9 17 AWXA0002250 1 20010801 A 5312 6545833U40 PRESSURE PANEL BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 COCKPIT FLOOR WEB CRACKED RBL 24, WL 207, BS 180. REMOVED AND REPLACED WEB P/N 65-45833U40 IAW B737 SRM 51-40-02 PG 38 AN E/R 03-5316-01218-DD1. 2 L 7 2 4F RT A16WE 2001091300227 20010913 00227 NM 2001 9 13 VNAA0109003 1 20010906 A 3200 INDICATOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 460PS 3061 DURING THE TAKE OFF ROLL, THE CREW RECEIVED A LEFT HAND INBOARD BRAKE TEMPERATURE MESSAGE AND ABORTEDTAKE OFF. THE CRE W RETURNED TO THE GATE AND MAINTENANCE PERFORMED A MAINTENANCE FUNCTION AND MEL'D THE INDICATOR. THE ACTUAL BRAKE TEMP ERATURE WAS 32C. FLIGHT 4055 CONTINUED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001091300233 20010913 00233 NM 2001 9 13 VNAA0109006 1 20010910 A 5600 SPSD0328121A WINDSHIELD DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RH FAILED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 460PS 8071 3061 AFTER DEPARTING TYS, THE CREW RECEIVED A RIGHT HAND WINDSHIELD HEAT FAIL CAS MESSAGE. THE CREW FOLLOWED THE QUICK REFER ENCE HANDBOOK AND THEN CALLED DISPATCH. DUE TO WEATHER SURROUNDING PHL THE CREW DIVERTED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND FORWARD WINSHIELD IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 56-00-00.OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001110700109 20011107 00109 WP 2001 11 7 01FDEA00833 1 20010911 A 5311 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 CTR CARGO LT BS 1701 CRACK IN FRAME AT L27. REMOVED AND REPLACED FRAME PER SRM & IAW. 2 L 7 3 4F A22WE 2001110600050 20011106 00050 WP 2001 11 6 01FDEA00827 1 20010911 A 5310 DOOR FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 F/S 960 LONG 40R TO 41R FWD CARGO DOOR AFT FRAME WORN. R&R PER IAW & SRM. 2 L 7 3 4F A22WE 2001091300235 20010913 00235 NM 2001 9 13 01FDEA00828 1 20010911 A 3260 189915 SENSOR BOEING 727 727227 1384078 NM UPLOCK FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 496FE 21670 01-304 RED L/GEAR LIGHT ON. R&R LMG UPLOCK SENSOR PER MM 32-61-081-4. 2 L 7 3 4F A3WE 2001101500177 20011015 00177 EU 2001 10 15 01FDEA00832 1 20010911 A 5312 A53610030242 DOUBLER AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 LT & RT EXTERNAL DOUBLERS AT FWD PRESSURE BULKHEAD 6 O'CLOCK POS CORRODED. R&R BULKHEAD PER EA 6-5310-59382. 2 L 7 2 4F RT A35EU 2001091300237 20010913 00237 NM 2001 9 13 COOSDR010083 1 20010814 A 5753 RIB BOEING 737 737230 NM PWA JT8 JT8D15 52051 NE T/E FLAP CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 737TW 20257 RIGHT WING, INBOARD MID FLAP RIB CRACKED AT WBL 86.74. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091300238 20010913 00238 NM 2001 9 13 COOSDR010084 1 20010814 A 5753 RIB BOEING 737 737230 NM PWA JT8 JT8D15 52051 NE T/E FLAP CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 737TW 20257 LEFT WING, INBOARD MID FLAP RIB CRACKED AT WBL 86.74. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091300239 20010913 00239 NM 2001 9 13 COOSDR010086 1 20010814 A 5751 65464542 SKIN BOEING 737 737230 NM PWA JT8 JT8D15 52051 NE AILERON DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 737TW 20257 RIGHT WING, AILERON PN 65-46454-2, SN 306 UPPER SKIN WITH DELAMINATIONS. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091300240 20010913 00240 NM 2001 9 13 COOSDR010087 1 20010814 A 5755 65799527 SKIN BOEING 737 737230 NM PWA JT8 JT8D15 52051 NE RT SPOILER DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 737TW 20257 RIGHT WING, FLIGHT SPOILER NR 6, PN 65-79952-7 UPPER AND LOWER SKIN WITH DELAMINATIONS. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091300241 20010913 00241 NM 2001 9 13 COOSDR010088 1 20010814 A 5753 6571950 SKIN BOEING 737 737230 NM PWA JT8 JT8D15 52051 NE T/E FLAP DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 13 737TW 20257 RIGHT WING, OUTBOARD FLIPPER FLAP, PN 6571950, SN BN-137 SKIN DELAMINATED. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091300242 20010913 00242 NM 2001 9 13 COOSDR010100 1 20010814 A 5330 SKIN BOEING 737 737230 NM PWA JT8 JT8D17 52049 NE FUSELAGE DELAMINATED E EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 767TW 20258 FUSELAGE SKIN FROM BS 847 TO BS 867 BETWEEN STR 22R AND STR 23R WITH DELAMINATION. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091300243 20010913 00243 NM 2001 9 13 COOSDR010101 1 20010814 A 5330 SKIN BOEING 737 737230 NM PWA JT8 JT8D17 52049 NE FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 767TW 20258 FUSELAGE SKIN FROM BS 500B+6 TO BS 500B+10 AT STR 19R UPPER SKIN WITH CRACK INDICATION. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091300246 20010913 00246 NM 2001 9 13 COOSDR010102 1 20010814 A 5330 DOUBLER BOEING 737 737230 NM PWA JT8 JT8D17 52049 NE FUSELAGE DEBONDED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 767TW 20258 FUSELAGE SKIN FROM BS 335 TO BS 350 BETWEEN STR 24L AND STR 25L WITH DOUBLER DEBONDED. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091300247 20010913 00247 NM 2001 9 13 COOSDR010103 1 20010814 A 5330 SKIN BOEING 737 737230 NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 767TW 20258 FUSELAGE SKIN AT BS 340 AT STR 24L WITH CORROSION. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091300250 20010913 00250 NM 2001 9 13 COOSDR010104 1 20010814 A 5330 SKIN BOEING 737 737230 NM PWA JT8 JT8D17 52049 NE FUSELAGE DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 767TW 20258 FUSELAGE SKIN FROM BS 950 TO BS 955 BETWEEN STR 5R AND STR 6R DELAMINATED. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091300253 20010913 00253 NM 2001 9 13 COOSDR010105 1 20010814 A 5312 BULKHEAD BOEING 737 737230 NM PWA JT8 JT8D17 52049 NE FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 767TW 20258 BULKHEAD WEB SECTION CRACKED, AT LBL 10, BETWEEN WL 237.25 AND WL 230.5. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091300254 20010913 00254 NM 2001 9 13 COOSDR010106 1 20010814 A 5312 BULKHEAD BOEING 737 737230 NM PWA JT8 JT8D17 52049 NE FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 767TW 20258 BULKHEAD WEB SECTION CRACKED, RBL 10, BETWEEN WL 237.25 AND WL 230.5 2 L 7 2 4F 4 F RT A16WE E2EA 2001091300256 20010913 00256 NM 2001 9 13 COOSDR010107 1 20010814 A 5330 DOUBLER BOEING 737 737230 NM PWA JT8 JT8D17 52049 NE FUSELAGE DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 767TW 20258 FUSELAGE SKIN DOUBLER FROM BS 639 TO BS 663 BETWEEN STR 9L AND 10L WITH DELAMINATION. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091300257 20010913 00257 NM 2001 9 13 COOSDR010108 1 20010814 A 5330 SKIN BOEING 737 737230 NM PWA JT8 JT8D17 52049 NE FUSELAGE DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 767TW 20258 FUSELAGE SKIN SECTION FROM BS 635 TO BS 663 BETWEEN STR 14R AND 15R WITH DELAMINATION. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091300258 20010913 00258 NM 2001 9 13 COOSDR010109 1 20010814 A 5712 RIB BOEING 737 737230 NM PWA JT8 JT8D17 52049 NE LT WING CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 767TW 20258 LEFT WING LEADING EDGE RIB CRACKED, LOCATED AT FSS 267, NR3 SLAT INBOARD MAIN TRACK SUPPORT. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091300259 20010913 00259 NM 2001 9 13 COOSDR010110 1 20010814 A 5712 RIB BOEING 737 737230 NM PWA JT8 JT8D17 52049 NE LT WING CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 767TW 20258 LEFT WING LEADING EDGE RIB CRACKED, LOCATED AT FSS 394, NR2 SLAT OUTBOARD MAIN TRACK SUPPORT. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091300260 20010913 00260 NM 2001 9 13 COOSDR010111 1 20010814 A 5330 SKIN BOEING 737 737230 NM PWA JT8 JT8D17 52049 NE FUSELAGE DEBONDED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 767TW 20258 FUSELAGE SKIN SECTION FROM BS 330 TO BS 350 BETWEEN STR 21L AND 23L WITH DISBONDING. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091300262 20010913 00262 NE 2001 9 13 LD22001F00002 2 20010720 A 7230 BRR19248 DISK GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE RT ENGINE CRACKED A LD2R K NONE O OTHER IN INSP/MAINT 1 GL 15 23M 724 579 11261 WHILE COMPLETING THE RECURRING NDT INSPECTION OF THE FAN DISC, A CRACK WAS FOUND. THERE WERE NO VISUAL INDICATIONS OF A CRACK. (ATTACHED SHEET FOR LOCATION OF CRACK ON FAN DISC.) THE FAN DISC HAD BEEN NDT 117 CYCLES PREVIOUS TO THIS NDT T HAT REVEALED A CRACK. A NEW FAN MODULE HAS BEEN INSTALLED AND THE AIRCRAFT HAS BEEN RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A12EA E00057EN 2001091300263 20010913 00263 WP 2001 9 13 MXI2001F00000 2 20010808 A 7261 30743723 VALVE LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP LT OIL PUMP DEFECTIVE A MXIA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 21 431AS 9317 999 431 P89194 OIL PRESSURE GAUGE INDICATES IN THE RED ZONE (HIGH) AT TAKE OFF POWER. OIL PRESSURE FOLLOWS THE POWER LEVER. 2 L 7 2 4F 4 F A10CE E6WE 2001091300264 20010913 00264 CE 2001 9 13 QTV2001F00000 1 20010814 A 2750 50000083CR CONTROL CABLE CESSNA 402 402B 207590P CE CONT O520 TSIO520* 17040 SO T/E FLAP BROKEN B QTVR O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 11 7947Q 12101 402B0397 ON SHORT FINAL THE CABLE BROKE AND THE LEFT FLAP RETRACTED WHICH CAUSED A SPLIT FLAP CONDITION. REPLACED CABLE . INSPE CTED THE OTHER FLAP CABLES, NO DEFECTS NOTED. 1 L 7 2 3O 3 O A7CE E8CE 2001091300265 20010913 00265 EU 2001 9 13 TI1R001420 1 20010309 A 5210 350A25136600 ROD SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE DOOR DISCHARGED B TI1R O OTHER O OTHER NR NOT REPORTED 1 SW 05 350AZ 3127 GAS ROD, LOST GAS CHARGE. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2001091300266 20010913 00266 NE 2001 9 13 TI1R001430 2 20010421 A 7200 ENGINE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE MAKING METAL B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 350AZ 1185 3127 ENGINE ASSEMBLY - REMOVED FOR HIGH IRON IN OIL ANALYSIS (19.4). REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2001091300274 20010913 00274 NE 2001 9 13 TI1R001443 2 20010427 A 7200 ENGINE SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE MAKING METAL B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 40751 986 3154 ENGINE CHECKED, HIGH IRON CONTENT IN OIL ANALYSIS. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2001091300276 20010913 00276 2001 9 13 TI1R001451 4 20010420 A 3416 1042011968E ALTIMETER BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT FAILED B TI1R O OTHER O OTHER NR NOT REPORTED 1 SW 05 317MC 7505 ALTIMETER, ENCO- FAILS TO SEND SIGNAL TO AUTOPILOT AND TRANSPONDER - REPORTS RISE IN ALTITUDE WHEN DESCENDING. REMOVED AND REPLACED. 1 G 7 2 3U 3 U NC H13EU E19EU 2001091300277 20010913 00277 EU 2001 9 13 TI1R001453 1 20010508 A 2822 1176415103 PUMP BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE FUEL SYS INOPERATIVE B TI1R O OTHER O OTHER NR NOT REPORTED 1 SW 05 317MC 7505 BOOST PUMP, INOPERATIVE PUMP, WILL NOT RUN. REMOVED AND REPLACED. 1 G 7 2 3U 3 U NC H13EU E19EU 2001091300278 20010913 00278 2001 9 13 TI1R001454 4 20010501 A 3424 55508340N5L INDICATOR SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT ERRATIC B TI1R O OTHER O OTHER NR NOT REPORTED 1 SW 05 5230J 3256 TURN AND BANK INDICATOR, RATE OF TURN NEEDLE IS ERRATIC. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2001091300279 20010913 00279 EU 2001 9 13 TI1R001455 1 20010427 A 7931 642790041 TRANSMITTER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE OIL SYSTEM INOPERATIVE B TI1R O OTHER O OTHER NR NOT REPORTED 1 SW 05 40751 986 3154 OIL PRESSURE TRANSMITTER - INOPERATIVE- REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2001091300280 20010913 00280 EU 2001 9 13 TI1R001456 1 20010420 A 6520 350A33215300 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR CRACKED B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 350AZ 3127 BEARING - CRACKED/SPLIT. REMOVED AND REPLACED 1 G 7 1 3U 3 U H9EU E19EU 2001091300281 20010913 00281 2001 9 13 TI1R001459 4 20010508 A 3417 7002353913 SENSOR BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE AIR DATA MALFUNCTIONED B TI1R O OTHER O OTHER NR NOT REPORTED 1 SW 05 317MC 7505 AIR DATA SENSOR- WILL NOT CAPTURE ALTITUDE IN ANY MODE. REMOVED AND REPLACED. 1 G 7 2 3U 3 U NC H13EU E19EU 2001091300282 20010913 00282 EU 2001 9 13 TI1R001460 1 20010514 A 2140 HTE920018 VALVE BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE HEAT SYSTEM INOPERATIVE B TI1R O OTHER O OTHER NR NOT REPORTED 1 SW 05 317MC 7505 ALT NR HTE200016 - WILL NOT CLEAR COCKPIT LIGHT, VALVE FUNCTIONS NORMALLY. REMOVED AND REPLACED. 1 G 7 2 3U 3 U NC H13EU E19EU 2001091300284 20010913 00284 2001 9 13 TI1R001470 4 20010522 A 3120 B1894522282A CLOCK SNIAS 350 AS350B2 8680813 EU INSTRUMENT PNL INOPERATIVE B TI1R O OTHER O OTHER NR NOT REPORTED 1 SW 05 911GF 3140 CLOCK - WILL NOT OPERATE. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2001091300288 20010913 00288 2001 9 13 TI1R001474 4 20010601 A 3424 55508340N5L INDICATOR SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE TURN & BANK FAILED B TI1R O OTHER O OTHER NR NOT REPORTED 1 SW 05 5230J 3256 TURN AND BANK INDICATOR, CORE RETURN-WARRANTY FAILURE - INSTRUMENT LIGHT INOPERATIVE. 1 G 7 1 3U 3 U H9EU E19EU 2001091300289 20010913 00289 EU 2001 9 13 TI1R001475 1 20010530 A 6420 350A33214501 BEARING SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE PITCH LINK WORN B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 5230J 3256 TAIL ROTOR PITCH LINK, PARTS SUPPORT- ELASTOMER BEARING BUSHING AND SPERICALS, WORN. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2001091300290 20010913 00290 EU 2001 9 13 TI1R001476 1 20010530 A 6420 350A33214501 BUSHING SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE PITCH LINK WORN B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 5230J 677 3256 TAIL ROTOR PITCH LINK, ELASTOMER BUSHINGS AND SPHERICALS, WORN. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2001091300291 20010913 00291 2001 9 13 TI1R001477 4 20010313 A 3120 NAB017ES CLOCK BOLKMS 117 BK117A3 5626015 EU INSTRUMENT PNL DEFECTIVE B TI1R O OTHER O OTHER NR NOT REPORTED 1 SW 05 911MZ 7098 CLOCK 8 DAY - CLOCK WORKS FOR 30 TO 90 MINUTES AND THEN STOPS. REMOVED AND REPLACED. 1 G 7 2 3U H13EU 2001091300292 20010913 00292 EU 2001 9 13 TI1R001478 1 20010606 A 6710 SC5083 SERVO SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE MAIN ROTOR LEAKING B TI1R O OTHER O OTHER NR NOT REPORTED 1 SW 05 350AZ 1250 3127 MAIN ROTOR SERVO - SERVO LEAKING EXCESSIVELY. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2001091300293 20010913 00293 2001 9 13 TI1R001479 4 20010608 A 3422 060001500 GYRO SNIAS 350 AS350B2 8680813 EU COCKPIT DEFECTIVE B TI1R O OTHER O OTHER NR NOT REPORTED 1 SW 05 911GF 3140 KG102A DIRECTIONAL GYRO - HDG FLAG WILL NOT PULL OUT OF VIEW INTERMITTENTLY. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2001091300294 20010913 00294 EU 2001 9 13 TI1R001480 1 20010104 A 6321 350A32501000 BRAKE SNIAS 350 AS350B2 8680813 EU MAIN ROTOR WORN B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 350AZ 3127 BRAKE LINING SU - LININGS WORN TO LIMITS. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2001091300298 20010913 00298 2001 9 13 TI1R001484 4 20010604 A 3416 1042011968E ALTIMETER BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT INOPERATIVE B TI1R O OTHER O OTHER NR NOT REPORTED 1 SW 05 317MC ALTIMETER, ENCO - BARROW POT KNOB DOES NOT ENGAGE BARROW POT ON OCCASION. REMOVED AND REPLACED. 1 G 7 2 3U 3 U NC H13EU E19EU 2001091300299 20010913 00299 EU 2001 9 13 TI1R001485 1 20010601 A 7714 1179405603 INDICATOR BOLKMS 117 BK117A3 5626015 EU COCKPIT INOPERATIVE B TI1R O OTHER O OTHER NR NOT REPORTED 1 SW 05 527MB 7103 INDICATOR NG - NEEDLE DOES NOT MOVE. REMOVED AND REPLACED. 1 G 7 2 3U H13EU 2001091300300 20010913 00300 EU 2001 9 13 TI1R001487 1 20010622 A 6520 350A33215300 BEARING SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR DETERIORATED B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 5230J 3256 BEARING, BUSHINGS DETERIORATED AND WORN. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2001091300303 20010913 00303 NE 2001 9 13 TI1R001490 2 20010617 A 7313 0283317500 INJECTOR BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE OBSTRUCTED B TI1R O OTHER R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 SW 05 317MC 7505 INJECTOR, COMPL - INTERRUPTED START. ENGINE HANGS AT 20 PERCENT N1 - SPRAY PATTERN APPEARS INCORRECT. REMOVED AND REPL ACED. 1 G 7 2 3U 3 U NC H13EU E19EU 2001091300304 20010913 00304 NE 2001 9 13 TI1R001491 2 20010617 A 7313 0283317500 INJECTOR BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE OBSTRUCTED B TI1R O OTHER R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 SW 05 317MC 7505 INJECTOR COMPL - INTERRUPTED ENGINE START, HANGS AT 20 PERCENT NI, FUEL INJECTOR SPRAY PATTERN APPEARS INCORRECT. REMOVE D AND REPLACED. 1 G 7 2 3U 3 U NC H13EU E19EU 2001091300305 20010913 00305 NE 2001 9 13 TI1R001492 2 20010603 A 7200 9560137520 MAGNETIC SEAL SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE LEAKING B TI1R O OTHER O OTHER NR NOT REPORTED 1 SW 05 40751 543 3154 SEAL, LEAK AT NR 5 MODULE. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2001091300306 20010913 00306 EU 2001 9 13 TI1R001495 1 20010618 A 7714 1179405603 INDICATOR BOLKMS 117 BK117B1 5626012 EU COCKPIT FLUCTUATES B TI1R O OTHER O OTHER NR NOT REPORTED 1 SO 05 460H 6257 7142 NEEDLE FLUCTUATES BETWEEN 0-10 PERCENT. WILL NOT INDICATE ABOVE 10 PERCENT. 1 G 7 2 3U H13EU 2001091300307 20010913 00307 CE 2001 9 13 TIM2001F00005 1 20010718 A 3260 WARNING LIGHT BEECH 99 99A 1154003 CE COCKPIT ILLUMINATED A TIMA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 99GH U112 GEAR INTRANSIT LIGHT STAYED ON, AFTER GEAR RERACK. 1 L 7 2 3T A14CE 2001091300308 20010913 00308 CE 2001 9 13 UG82001F00001 1 20010802 A 2932 99145242 TRANSDUCER CESSNA 750 750 2076810 CE ALLSN AE300 AE3007A GL HYDRAULIC SYS DEFECTIVE A UG8A O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 23 5113 2549 7500013 NO A SYSTEM HYDRAULIC PRESSURE INDICATION. INDICATION SYSTEM FAULT. REMOVED AND REPLACED TRANSDUCER, INDICATION NORMAL 2 L 7 2 4J 4 F RT T00007WI TE6CH 2001091300309 20010913 00309 CE 2001 9 13 UG82001F00002 1 20010809 A 2752 99146152 POWER UNIT CESSNA 750 750 2076810 CE ALLSN AE300 AE3007A GL T/E FLAP FAILED A UG8A O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 GL 23 5115 1747 7500018 PROBLEM ENCOUNTERED: FLAPS FAILED. FLAP SYSTEM COMPONENT FAILURE. REPLACED FLAP POWER DRIVE UNIT, OPS CHECKED NORMAL. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2001091300310 20010913 00310 CE 2001 9 13 UG82001F00004 1 20010808 A 8011 S29431 RELAY CESSNA 650 650 2076802 CE GARRTT TFE731 TFE731* 01518 WP ENGINE STARTER STUCK A UG8A O OTHER O OTHER TX TAXI/GRND HDL 1 GL 23 5117 6507064 RIGHT ENGINE STARTER WOULD NOT DISENGAGE. STUCK START RELAY. REMOVED AND REPLACED START RELAY. 2 L 7 2 4F 4 F A9NM E6WE 2001091300312 20010913 00312 NM 2001 9 13 COOSDR010090 1 20010816 A 5753 RIB BOEING 737 737230 NM PWA JT8 JT8D15 52051 NE T/E FLAP CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 737TW 20257 RIGHT WING, INBOARD MID FLAP RIB CRACKED AT WBL 120.24. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091300313 20010913 00313 NM 2001 9 13 COOSDR010091 1 20010816 A 5320 ANGLE BOEING 737 737230 NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 737TW 20257 ELECTRONIC EQUIPMENT COMPARTMENT AT STA 352, STR 27R ANGLE WITH CORROSION. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091300314 20010913 00314 NM 2001 9 13 COOSDR010092 1 20010816 A 5280 6552201 SKIN BOEING 737 737230 NM PWA JT8 JT8D15 52051 NE RT MLG DOOR DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 737TW 20257 RIGHT WING, MAIN LANDING GEAR INNER DOOR PN 6552201, SN BN 325 INNER SKIN DELAMINATED. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091300316 20010913 00316 NM 2001 9 13 COOSDR010095 1 20010816 A 5312 BULKHEAD BOEING 737 737230 NM PWA JT8 JT8D15 52051 NE FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 737TW 20257 BS 1016, BULKHEAD WEB CRACKED. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091300317 20010913 00317 NM 2001 9 13 COOSDR010097 1 20010816 A 5330 SKIN BOEING 737 737230 NM PWA JT8 JT8D15 52051 NE FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 737TW 20257 FUSELAGE SKIN, HOLES CRACKED AND MISSING MATERIAL AT UPPER SKIN, LAP JOINT AREA. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091300318 20010913 00318 NM 2001 9 13 COOSDR010098 1 20010816 A 5330 DOUBLER BOEING 737 737230 NM PWA JT8 JT8D15 52051 NE FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 737TW 20257 MAIN CARGO CABIN, FORWARD ENTRY DOOR UPPER HINGE CUTOUT INTERNAL DOUBLER WITH CRACK. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091300319 20010913 00319 NM 2001 9 13 COOSDR010112 1 20010816 A 5312 BULKHEAD BOEING 737 737230 NM PWA JT8 JT8D15 52051 NE FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 737TW 20257 FUSELAGE, PRESSURE BULKHEAD WEB WITH CRACK AT BS 178, WL 233.5 BETWEEN RBL 10 AND RBL 13. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091300320 20010913 00320 NM 2001 9 13 COOSDR010114 1 20010816 A 5312 BULKHEAD BOEING 737 737230 NM PWA JT8 JT8D15 52051 NE FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 737TW 20257 UPPER FUSELAGE AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6L, AT AFT FASTENER ROWS ATTACHMENT TO THE Y CHORD. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091300322 20010913 00322 NM 2001 9 13 COOSDR010116 1 20010816 A 5311 FRAME BOEING 737 737230 NM PWA JT8 JT8D15 52051 NE FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 737TW 20257 MAIN CARGO CABIN FRAME CRACKED AT BS 277, BETWEEN S9L, AND S10L. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091300323 20010913 00323 NM 2001 9 13 COOSDR010117 1 20010816 A 5313 STRINGER BOEING 737 737230 NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 737TW 20257 FORWARD CARGO COMPARTMENT STRINGER 19R CORRODED, AT BS 500A+14. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091300324 20010913 00324 NM 2001 9 13 COOSDR010118 1 20010816 A 5311 FRAME BOEING 737 737230 NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 737TW 20257 LOWER NOSE COMPARTMENT, AT BS 222, WL 168, LBL 18 FRAME WITH CORROSION. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091300325 20010913 00325 NM 2001 9 13 COOSDR010119 1 20010816 A 5330 DOUBLER BOEING 737 737230 NM PWA JT8 JT8D15 52051 NE FUSELAGE DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 737TW 20257 LOWER NOSE COMPARTMENT, BONDED DOUBLER WITH DELAMINATION, FROM BS 211 TO BS 203, BETWEEN LBL 16 AND LBL 20. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091300326 20010913 00326 NM 2001 9 13 UPS01236729 1 20010829 A 3350 LIGHT BOEING 727 72722C 138400F NM COCKPIT DEFECTIVE A IPXA K NONE O OTHER CR CRUISE 1 SO 01 929UP 19092 INSPECTION TYPE:IN COCKPIT EMERGENCY LIGHT ILLUMINATED DURING FLIGHT THEN FELL OUT OF ITS CONTAINER. UNABLE TO REINSTALL . REINSTALLED EMERGENCY EXIT LIGHT ASSY TEST OK LENS SECURED. 2 L 7 3 4F A3WE 2001091300327 20010913 00327 NM 2001 9 13 UPS01236732 1 20010829 A 3350 GUARD BOEING 727 72730C 1384009 NM COCKPIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:IN EMERGENCY EXIT LIGHTS SWITCH GUARD IS INOP; WHEN LIGHTS ARE TURNED ON TO TEST & GUARD IS CLOSED, LIGH TS REMAIN ON INSTEAD OF MOVING TO ARMED POSITION. R&R EMERGENCY EXIT LIGHT SWITCH GUARD. OPS CHECKS NORMAL. PERFORMED EM ERGENCY EXIT LIGHT OPS. CHECKS PER MM 33-50-01 CHECKS NORMAL. 2 L 7 3 4F A3WE 2001091300328 20010913 00328 WP 2001 9 13 NACA20010032 1 20010806 A 2610 TERMINAL DOUG DC6 DC6B 3021712 WP FORWARD DETECTOR BROKEN A NACA A UNSCHED LANDING J N WARNING INDICATION FALSE WARNING CL CLIMB 1 AL 03 867TA 111897 45202 DISCRPANCEY: Zone 2 fire waring, forward baggage.CORRECTIVE ACTION: Repaired broken terminal on the fwd baggage, fwd L/H detector. 2 L 7 4 4R 6A4 2001091700094 20010917 00094 SO 2001 9 17 C2XA01TY109 1 20010913 A 5230 14522493003 SKIN EMB 145 EMB145LR SO CARGO DOOR CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13990 145277 TYS DURING A SCHEDULED INSPECTION, THE CARGO DOOR SKIN AROUND THE EXTERIOR HANDLE WAS FOUND CHAFED. MAINTENANCE REMOVE D THE DAMAGED AREA, PERFORMED DYE-PENETRENT INSPECTION, ALODINED, PRIMED AND PAINTED AREA IAW-EMB-145-GST-3098/01. THE REPAIR WAS SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2001091400001 20010914 00001 SO 2001 9 14 C2XA01TY110 1 20010913 A 2620 14523355403 TUBE EMB 145 EMB145LR SO LEFT ENGINE BENT A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13990 145277 TYS During a scheduled inspection. The left engine fire extingisher line was found bent. Maintenance removed and replac ed the fire extingisher line I.A.W.-EMB-145-MM-26-21-06 and SB # 145-26-0008 page 12 & 13. The repair was satisfactory a nd the aircraft will be released upon completion of inspection. 2 L 7 2 4T RT T00011AT 2001091400002 20010914 00002 SO 2001 9 14 C2XA01TY112 1 20010913 A 5315 14521700007 BEAM EMB 145 EMB145LR SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13990 145277 TYS During a scheduled inspection, The left omega beam was found corroded at frame 20. Maintenance removed damaged are a, fabricated repair filler, shims & external angle. Alodined, primed and installed repair parts. I.A.W.-EMB-135/145-SRM -51-40-02, 53-21-10 and CMP-51-21-04 & 05. The repair was satisfactory and the aircraft will be released upon complectio n of inspection. 2 L 7 2 4T RT T00011AT 2001091400003 20010914 00003 SO 2001 9 14 C2XA01TY114 1 20010913 A 5313 14533805021 STRINGER EMB 145 EMB145LR SO CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13990 145277 TYS During a scheduled inspection, Stringer 19L was found chafed at frame 53. Maintenance blended chafed area, performe d dye-penetrant inspection, alodined, primed and restored top coat I.A.W.-EMB-GST-2979/01. The repair was satisfactory a nd the aircraft will be released upon complection of inspection. 2 L 7 2 4T RT T00011AT 2001091400004 20010914 00004 SO 2001 9 14 C2XA01TY115 1 20010913 A 5313 14533805022 STRINGER EMB 145 EMB145LR SO CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13990 145277 TYS During a scheduled inspection, Stringer 19R was found chafed at frame 53, Maintenance blended chafed area, performe d dye-penetrant inspection, alodined, primed and restored top coat, I.A.W.-EMB-145-GST-2979/01. The repair was satisfact ory and the aircraft will be released upon complection of inspection. 2 L 7 2 4T RT T00011AT 2001091400005 20010914 00005 2001 9 14 SWIA200110050 4 20010712 A 2210 DAMPENER CNDAIR CL600 CL6002B19 EA NR 1 YAW MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 496SW 7473 YAW DAMPER NR 1 WILL NOT ENGAGE. NOTIFIED SGU MAINTENANCE CONTROL.TROUBLESHOOT SYSTEM, YAW DAMPER ACTUATOR CHECKS GOOD. FCC 1 COMPUTER CHECKS GOOD. REMOVED AND REPLACED YAW DAMPER NR 1 POWER RELAY (1K2CA) IAW CRJ WMM 20-18-00. OPS CHECK GOOD IAW CRJ MM 22-22-01. AIRCRAFT OK FOR CAT II OPERATIONS.PN ON MS27400-31X. 2 L 7 2 4F RT A21EA 2001091400006 20010914 00006 EA 2001 9 14 SWIA200110051 1 20010713 A 2913 PV304448 PUMP CNDAIR CL600 CL6002B19 EA HYD SYSTEM INOPERATIVE A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 408SW 7055 HYDRAULIC EDP 1A CAUTION MESSAGE ON EICAS , NO HYDRAULIC FLUID QUANTITY IN SYSTEM NR 1. FOUND LEAKING HYDRAULIC LINE IN PYLON, REMOVED AND REPLACED HYDRAULIC LINE AND ENGINE DRAIN PUMP IAW MM 29-11-01. OPS CHECK GOOD. LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2001091400007 20010914 00007 SO 2001 9 14 SWIA200110053 1 20010715 A 3150 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO COCKPIT FALSE ACTIVATION A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 578SW 120346 AURAL WARNING TRIM ON TAKEOFF; ABORTED. AURAL BREAKER POPPED.RESET CB. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001091400008 20010914 00008 EA 2001 9 14 SWIA200110054 1 20010717 A 2121 AE0607AA2 FAN CNDAIR CL600 CL6002B19 EA AIR DIST FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 906SW 7510 ON CLIMBOUT RECEIVED ARINC COOL CAUTION MESSAGE. USED QRH PROCEDURE, MESSAGE WOULD NOT CLEAR. ON RETURN TO FAT DESCEND ING THROUGH 25,000 FT MESSAGE WENT AWAY AFTER APPROXIMATELY 20 MINUTES.REPLACED ARINC FAN NR 1 AND REPLACED LOW FLOW ARI NC DETECTOR. PERFORMED OPS TEST IAW 21-24-25. GROUND CHECK GRD ALT NORMAL/FLT ALT CHECK NORMAL. 2 L 7 2 4F RT A21EA 2001091400009 20010914 00009 SO 2001 9 14 SWIA200110055 1 20010720 A 2121 AE1711AA0 FAN EMB 120 EMB120ER 3260203 SO AIR DIST SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 209SW 132 132 120269 IMMEDIATELY AFTER ENGINE START WHEN PACKS WERE SWITCHED ON, SMOKE BECAME VISIBLE IN CABIN.REMOVED AND REPLACED LEFT GROU ND COOLING FAN WITH A SERVICEABLE UNIT IAW MM 21-51-03. 2 L 7 2 4T RT A31SO 2001091400010 20010914 00010 SO 2001 9 14 SWIA200110056 1 20010720 A 2750 CONTROL UNIT EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 07 188SW 120039 FLAP DISAGREEMENT WHEN SELECTING 45 DEGREES. CLEANED MOISTURE FROM RIGHT OUTBOARD CANNON PLUG (INSTALLED FLAP ACTUATOR T EST BOX). NO FAULTS NOTED ON ALL FLAP ACTUATORS. REINSTALLED FECU. SECURED DOORS. OPERATED FLAPS SEVERAL TIMES. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001091400011 20010914 00011 SO 2001 9 14 SWIA200110057 1 20010723 A 3231 SEQUENCE VALVE EMB 120 EMB120ER 3260203 SO MLG FAILED A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 293SW 120320 LEFT MAIN GEAR WOULD NOT RETRACT AFTER TAKEOFF. ADJUSTED LEFT INBOARD FORWARD GEAR DOOR SEQUENCE VALVE IAW MM 32-32-04. SWING GEAR OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001091400012 20010914 00012 EA 2001 9 14 SWIA200110058 1 20010721 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 407SW 7034 THREE STRIPS OF EMERGENCY FLOOR LIGHTING INOP.EMERGENCY TRACK LIGHTING COVER REMOVED. LOOSE CONNECTION PUT TOGETHER AND EMERGENCY TRACK COVER REINSTALLED. EMERGENCY TRACK LIGHTING TESTED SERVICEABLE. 2 L 7 2 4F RT A21EA 2001091400013 20010914 00013 SO 2001 9 14 SWIA200110059 1 20010720 A 2752 3430001001 ACTUATOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 215SW 120281 ON DEPARTURE, FLAP DISAGREEMENT - INBOARD. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR IAW MM 27-50-02. LEAK AND O PS CHECK SATISFACTORY. 2 L 7 2 4T RT A31SO 2001091400014 20010914 00014 SO 2001 9 14 SWIA200110060 1 20010723 A 3150 WARNING HORN EMB 120 EMB120ER 3260203 SO COCKPIT FALSE ACTIVATION A SWIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 564SW 120339 INTERMITTENT FIRE BELL DURING GOUND OPERATIONS. NO LIGHTS SUPPORTING INDICATION. REPLACED AURAL WARNING UNIT. OPS CHEC K GOOD. 2 L 7 2 4T RT A31SO 2001091400015 20010914 00015 SO 2001 9 14 SWIA200110061 1 20010725 A 5220 SEAL EMB 120 EMB120ER 3260203 SO EMERGENCY EXIT LEAKING A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 221SW 120290 DOOR SQUEAL AT EMERGENCY EXIT 9BC. UPDATE 7/26/2001 - LOUD SQUEAL AT EXIT DOOR 9BC, SQUEALS AT ALTITUDE.RESEALED DOOR G ASKET AT EMERGENCY EXIT 9BC. PRESSURIZED TO 6 PSI, NO SQUEAL. UPDATE 7/26/2001 - CLEANED SEAL AND REPLACED EXIT TAPE O N LOWER PART OF DOOR. REMOVED EXCESS SILICON FROM AROUND EXIT DOOR SEAL CUTOUT. REMOVED INSULATION TAPE FROM AROUND LO WER HANDLE SEAL. AIRCRAFT PRESSURIZED ON GROUND, NO LEAKS NOTED. 2 L 7 2 4T RT A31SO 2001091400016 20010914 00016 SO 2001 9 14 SWIA200110062 1 20010726 A 3010 DUCT EMB 120 EMB120ER 3260203 SO RT ENGINE LEAKING A SWIA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 NM 07 218SW 120287 RIGHT ENGINE DUCT LEAK IN FLIGHT. SHUT ENGINE DOWN AS PER QRH.RESECURED DRAIN TUBING CUP AT RIGHT ENGINE DEICER PRESSU RE REGULATING VALVE. PERFORMED RUN UP. OPS CHECK GOOD IAW MM 30-10-06. 2 L 7 2 4T RT A31SO 2001091400017 20010914 00017 EA 2001 9 14 SWIA200110063 1 20010720 A 2760 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE SPOILERS ACTIVATED A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 417SW 7400 WHITE SPOILERON FAULT MESSAGE ON EICAS. RETURN TO GATE AS PER QRH.DEFERRED AS PER MEL 27-65-3. COMPLIED WITH MAINTENAN CE PROCEDURE PER MEL. SUPPLEMENTAL REPORT FORTHCOMING. UPDATE 7/26/2001: REMOVED AND REPLACED NR 2 SECU IAW MM 27-60 -01. SPOILERS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2001091400018 20010914 00018 SO 2001 9 14 SWIA200110065 1 20010725 A 3350 D36604001 BATTERY EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE CABIN DISCHARGED A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 292UX 1451 1451 120292 EMERGENCY LIGHTS WOULD NOT TEST PROPERLY. REMOVED AND REPLACED FORWARD, MID AND AFT ELBP'S IAW 33-50-02. OPS CHECK GOOD . 2 L 7 2 4T 4 T RT A31SO E20NE 2001091400019 20010914 00019 SO 2001 9 14 SWIA200110066 1 20010717 A 2750 CONTROL UNIT EMB 120 EMB120RT SO PWA 118 PW118 NE TE FLAPS FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 162CA 120150 DURING CRUISE, ASWS & FLAP LIGHTS ON MAP & ASYMMETRY DISSAGREEMENT, CONTROL FAULT LIGHTS ON OVERHEAD. PANEL FLAP INDICA TOR FLUCTUATING 0 DEGREES - 45 DEGREES SEVERAL TIMES INTERMITTENTLY. INSTALLED SERVICEABLE FCU. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091400020 20010914 00020 SO 2001 9 14 SWIA200110067 1 20010724 A 3150 WARNING SYSTEM EMB 120 EMB120RT SO COCKPIT ACTIVATED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 162CA 120150 ABORTED TAKEOFF - TRIPLE CHIME - AURAL WARNING - BRAKES, FLAPS, AUTO FEATHER OCCURRED DURING TAKEOFF ROLL. REPLACED AND SECURED AURAL WARNING UNIT. PERFORMED OPS CHECK OF AUTO FEATHER SYSTEM. OPS CHECK GOOD. SN ON 0419 SN OFF 0224. 2 L 7 2 4T RT A31SO 2001091400021 20010914 00021 SO 2001 9 14 SWIA200110068 1 20010726 A 2750 12042642507 SWITCH EMB 120 EMB120RT SO PWA 118 PW118 NE FLAP SELECTOR FAILED A SWIA D RETURN TO BLOCK J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 162CA 1247 1247 120150 ON TAXI, FLAPS SELECTED 15 DEGREES. FLAP INDICATOR GOES FROM 15 DEGREES TO 0 DEGREES EVERY MINUTE. GREEN BARS DISAPPEA R WHEN FLAPS ARE AT 0 DEGREES. THEY REAPPEAR AT FLAP 15. NO MAP INDICATION, JUST ONE CHIME ALERT. AS WE TAXIED BACK, ADVANCED SWS/FLAP ON MAP.REPLACED FLAP SELECTOR AND ALSO REPLACED FLAP ANNUNCIATOR ASSEMBLY. CYCLED FLAPS SEVERAL TIMES . OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091400022 20010914 00022 EA 2001 9 14 SWIA200110069 1 20010729 A 7722 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT ACTIVATED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 405SW 7029 TAKEOFF ABORTED DUE TO HIGH ITT WARNING. OBSERVED 902 DEGREES CENT. BEFORE TRIPLE CHIME AND WARNING MESSAGE APPEARED. B TMS WENT TO 8 ON LEFT SIDE. OPERATED ENGINES AS REQUIRED IAW GE MM 72-00-00. ENGINE PARAMETERS WITHIN LIMITS. NO DISCR EPANCIES NOTED AT THIS TIME. 2 L 7 2 4F RT A21EA 2001091400023 20010914 00023 SO 2001 9 14 SWIA200110070 1 20010726 A 2752 CONNECTOR EMB 120 EMB120ER 3260203 SO RT FLAP ACTUATOR CONTAMINATED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 NM 07 284YV 120284 FLAP DISAGREEMENT WARNING AFTER SELECTION OF FLAPS 45. OUTBOARD FLAP PAIR INDICATES 2 BAR DISAGREEMENT. COMPUTER FAULT CODES SHOWING RIGHT OUTBOARD FLAP NOT RESPONDING. FOUND MOISTURE IN RIGHT OUTBOARD FLAP ACTUATOR CANNON PLUG, CLEANED MO ISTURE. OPS CHECKED GOOD OF FLAP SEVERAL TIMES. 2 L 7 2 4T RT A31SO 2001091400024 20010914 00024 SO 2001 9 14 SWIA200110078 1 20010803 A 3350 FUSE EMB 120 EMB120ER 3260203 SO EMERG LIGHTING FAILED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 220SW 120288 FOUR FLOOR EMERGENCY LIGHTS OUT BY ROW 8.INSTALLED SERVICEABLE FUSE. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001091400025 20010914 00025 SO 2001 9 14 SWIA200110079 1 20010803 A 3010 FLOW VALVE EMB 120 EMB120ER 3260203 SO DEICE BOOTS INOPERATIVE A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 215SW 120281 LEFT AND RIGHT INBOARD STABILIZER DEICE BOOTS INOP INFLIGHT AT FL 200.REMOVED AND REPLACED FLOW CONTROL VALVE FOR HORIZO NTAL STABILIZER IAW MM 32-20-04. OPS CHECK SATISFACTORY. 2 L 7 2 4T RT A31SO 2001091400026 20010914 00026 EA 2001 9 14 SWIA200110080 1 20010802 A 3030 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT ACTIVATED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 499SW 7398 AFTER LEAVING SLC RECEIVED ON EICAS NR 1 (4 MESSAGES): 1. PITOT BASE HEAT; 2. LEFT AOA HEAT; 3. LEFT STATIC HEAT; 4. LE FT PITOT HEAT.REMOVED AND REPLACED LEFT PROBE HEATERS SENSOR CONTROLLER IAW MM 30-31-15. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2001091400027 20010914 00027 NE 2001 9 14 SWIA200110082 2 20010804 A 7321 RELAY EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE FUEL CONTROL FAILED A SWIA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 NM 07 308SW 120326 RIGHT ENGINE TORQUE LOSS AT 14,000 FEET. PERFORMED OPS CHECK OF EEC 14,000 FT SWITCH PER MM 73-23-01. NO DEFECTS NOTED . REMOVED AND REPLACED REVERSION RELAY. PERFORMED OPS CHECK GOOD IAW MM 73-23-00. P/N: M83536/6-022 2 L 7 2 4T 4 T RT A31SO E20NE 2001091400028 20010914 00028 2001 9 14 SWIA200110083 4 20010804 A 3425 6226190204 COMPUTER EMB 120 EMB120ER 3260203 SO AHRS MALFUNCTIONED A SWIA A UNSCHED LANDING I FLT. ATTITUDE INST. CL CLIMB 1 NM 07 215SW 1075 1075 120281 DURING CLIMBOUT FOS ADI ERRATIC + - 5 DEGREES OF PITCH WITH NO ASSOCIATED FAILURE FLAGS. FOLLOW UP: AFTER TAKEOFF FOS ADI ROLLED TO 50 DEGREES BANK, 30 DEGREES NOSE UP. ATTITUDE DISPLAY LIGHT ON MAP. FOLLOWED QRH PROCEDURE AND RETURNED F OR LANDING.REMOVE AND REPLACE NR 2 AHRS COMPUTER IAW 34-21-00. OPS CHECK GOOD. FOLLOW UP: REMOVE AND REPLACE NR 2 A HRS COMPUTER (SUSPECT PREVIOUS UNIT WAS BAD OFF THE SHELF) IAW 34-21-00. OPS CHECK GOOD. PN ON 622-6190-204, SN ON 210 0, SN OFF 2662. 2 L 7 2 4T RT A31SO 2001091400029 20010914 00029 EA 2001 9 14 SWIA200110084 1 20010802 A 2760 CONTROL UNIT CNDAIR CL600 CL6002B19 EA SPOILERS MALFUNCTIONED A SWIA D RETURN TO BLOCK F FLT CONT AFFECTED TO TAKEOFF 1 NM 07 413SW 7102 GLDS DEPLOY UNCOMMANDED DURING TAXI.RESET SPOILER SYSTEM. PERFORMED LGD TEST, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2001091400030 20010914 00030 EA 2001 9 14 SWIA200110085 1 20010802 A 2612 WIRE CNDAIR CL600 CL6002B19 1900309 EA EXHAUST PIPE CHAFED A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 413SW 7102 LEFT JET PIPE LOOP A FIRE DETECTION IS INOP. FOUND AND REPAIRED CHAFFED WIRE LEFT JET PIPE. TEST NORMAL. 2 L 7 2 4F RT A21EA 2001091400031 20010914 00031 SO 2001 9 14 SWIA200110086 1 20010803 A 2810 ACCESS PANEL EMB 120 EMB120ER 3260203 SO WING LOOSE A SWIA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 232SW 120306 STRONG FUEL SMELL IN AIRCRAFT WITH AIR CONDITIONER TURNED ON DURING ENGINE OPERATION.FOUND LOOSE SCREWS ON LEFT INBOARD WING FUEL CELL ACCESS PANEL CAUSING FUEL TO ENTER PACK AREA DURING ENGINE OPERATIONS. SECURED ACCESS PANEL AND RAN ENGIN ES WITH PACKS OPERATING. NO FURTHER SMELL NOTED. OPS AND LEAK CHECK GOOD. 2 L 7 2 4T RT A31SO 2001091400032 20010914 00032 2001 9 14 SWIA200110087 4 20010729 A 3414 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT ACTIVATED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 405SW 7029 AFTER TAKEOFF, HIGH SPEED CHECKER BOARD CAME DOWN TO 230 KIAS AND LATER FILLED ENTIRE SPEED TAPE. DUE TO FLAP SYSTEM DEF ERRAL AIR DATA SYSTEM AND EICAS BELIEVED FLAPS WERE IN A POSITION OTHER THAN ZERO, THUS CAUSING HIGH SPEED TAPE TO BE LO WER. FLAP DEFERRAL HAS BEEN CLEARED AND HIGH SPEED TAPE INDICATION IS NOW NORMAL. 2 L 7 2 4F RT A21EA 2001091400033 20010914 00033 EA 2001 9 14 SWIA200110088 1 20010807 A 3150 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT ACTIVATED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 417SW 7400 CLIMBING THROUGH 10,000 MSL - DISPLAY COOL CAUTION MESSAGE. FOLLOWED QRH PROCEDURE AND SWITCHED TO FLT ALT. MESSAGE BR IEFLY WENT AWAY THEN RETURNED. SWITCHED TO STANDBY POSITION - MESSAGE EXTINGUISHED. RETURNED TO SLC. REPLACED P196325 DISPLAY COOL INLET FILTER. OPS CHECK OK. 2 L 7 2 4F RT A21EA 2001091400034 20010914 00034 SO 2001 9 14 SWIA200110089 1 20010802 A 7120 TORQUE TUBE EMB 120 EMB120ER 3260203 SO RIGHT ENGINE DELAMINATED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 251YV 120251 RIGHT ENGINE TORQUE TUBE DELAMINATED. REPLACED RIGHT ENGINE TORQUE TUBE WITH SERVICEABLE UNIT, IAW MM 71-20-00.PN LM430- 32V 2 L 7 2 4T RT A31SO 2001091400035 20010914 00035 SO 2001 9 14 SWIA200110094 1 20010813 A 2450 RELAY EMB 120 EMB120ER 3260203 SO NR 1 FAILED A SWIA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 NM 07 578SW 120346 INVERTER NR 1 FAILED IN FLIGHT, WOULD NOT RESET.INVERTER OPS CHECK OK, 115 VAC ESS BUS LIGHT ILLUMINATED. FOUND K0005 R ELAY BAD. REPLACED K0005 115 ESS BUS SENSOR RELAY IAW MM 20-00-00. INVERTER OPS CHECK NORMAL. 2 L 7 2 4T RT A31SO 2001091400036 20010914 00036 NE 2001 9 14 SWIA200110095 2 20010813 A 7320 3035659 HMU EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE LEFT ENGINE MALFUNCTIONED A SWIA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 NM 07 215SW 1109 1109 120281 LEFT ENGINE WOULD NOT PRODUCE OVER 40 PERCENT TORQUE BEFORE T/O AURAL WARNING SOUNDED. THIS HAPPENED TWICE. T/O WAS AB ORTED TWICE.REMOVED THE LEFT ENGINE HMU AND INSTALLED A SERVICEABLE HMU. GROUND OPS CHECK AND LEAK CHECK GOOD IAW EMB M M 73-21-00. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091400037 20010914 00037 SO 2001 9 14 SWIA200110096 1 20010815 A 2752 3203001005 ACTUATOR EMB 120 EMB120ER 3260203 SO RT WING TE FLAPS MALFUNCTIONED A SWIA L ABORTED APPROACH F FLT CONT AFFECTED DE DESCENT 1 NM 07 268UE 120207 AFTER SELECTING FLAPS TO 15 DEGREES ON DOWNWIND, RECEIVED ''FLAP ASYMMETRY'' WARNING. RIGHT INBOARD FLAP INDICATED 2 SE GMENTS BEYOND 15 DEGREES. INITIATED GO-AROUND. COMPLETED QRH PROCEDURE. SUBSEQUENT LANDING UNEVENTFUL. REMOVED AIRCRA FT FCU AND BENCH CHECKED IN AVIONICS. COMPUTER CHECKS GOOD ON BENCH. FOUND RIGHT INBOARD FLAP ACTUATOR POTS READING ER RATIC. REMOVED RIGHT INBOARD FLAP ACTUATOR AND REPLACED IT WITH A SERVICEABLE ONE IAW EMB MM 27-50-07. OPS AND LEAK CH ECKS GOOD. FCU REINSTALLED. 2 L 7 2 4T RT A31SO 2001091400038 20010914 00038 SO 2001 9 14 SWIA200110097 1 20010815 A 2750 3472001001 CONTROL UNIT EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE TE FLAPS MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 NM 07 268UE 943 943 120207 FLAP CONTROL FAULT (NACELLE PAIR) AFTER SELECTING FLAPS 25. RESET OK BUT ALSO HAPPENED WHEN SITTING ON GROUND WITH FLAP S UP.REPLACED FLAP CONTROL UNIT PER MM 27-50-06. OPS CHECK GOOD AND INDICATION CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091400039 20010914 00039 SO 2001 9 14 SWIA200110098 1 20010816 A 2460 BUSS EMB 120 EMB120RT SO DC SYSTEM FAILED A SWIA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION AP APPROACH 1 NM 07 1105G 120105 ON APPROACH TO SEA THE ''EMERGENCY BUS OFF" LIGHT ON OVERHEAD PANEL LIGHT CAME ON, AND ON THE MAP PANEL THE AMBER APU, E LECTRIC, POWER OFF, DEICE AND BRAKES LIGHTS CAME ON. FOLLOWED QRH PROCEDURE TO AFM 3-8 PROCEDURE - EMERGENCY DC BUS FAI LED.RESET EMERGENCY DC BUS 2 CB 0470. ALL SYSTEMS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001091400040 20010914 00040 SO 2001 9 14 SWIA200110099 1 20010816 A 2460 CIRCUIT BREAKER EMB 120 EMB120RT SO DC BUSS TRIPPED A SWIA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION AP APPROACH 1 NM 07 1105G 120105 ON APPROACH TO PDX, EMERGENCY DC BUS 2 FAILED WHEN FLAPS WERE SELECTED 15 DEGREES.REMOVED AND REPLACED EMERGENCY DC BUS 2 CIRCUIT BREAKER IAW WM 20-00-07. NO DEFECTS NOTED. 2 L 7 2 4T RT A31SO 2001091400041 20010914 00041 EA 2001 9 14 SWIA200110100 1 20010812 A 7330 CONNECTOR CNDAIR CL600 CL6002B19 EA FUEL FLOW TRANSM DIRTY A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 427SW 7497 RIGHT FUEL FLOW READOUT FAILED ON TAKEOFF. CLEANED CANNON PLUG ON RIGHT ENGINE FUEL FLOW TRANSMITTER FOR TROUBLESHOOTING . RAN ENGINES, COULD NOT DUPLICATE FUEL FLOW FAIL. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2001091400042 20010914 00042 SO 2001 9 14 SWIA200110101 1 20010810 A 3350 D36604001 BATTERY EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 188SW 902 902 120039 EMERGENCY EXIT SIGN WILL NOT ILLUMINATE ROW 9.REMOVED AND REPLACED NR 3 EMERGENCY BATTERY PACK. 2 L 7 2 4T RT A31SO 2001091400043 20010914 00043 SO 2001 9 14 SWIA200110102 1 20010810 A 3234 HANDLE EMB 120 EMB120ER 3260203 SO MLG STUCK A SWIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 07 566SW 120341 GEAR HANDLE WOULD NOT GO TO UP POSITION AFTER TAKEOFF. USED DOWNLOCK RELEASE TO RAISE GEAR. INSPECTED LANDING GEAR FOR DEFECTS; NONE NOTED. INSPECTED AIR GROUND SWITCHES AND HARNESS. ALL FOUND GOOD. PERFORMED SEVERAL GEAR SWINGS. ALL C HECKS FOUND GOOD. 2 L 7 2 4T RT A31SO 2001091400044 20010914 00044 SO 2001 9 14 SWIA200110103 1 20010814 A 2750 3472001001 CONTROL UNIT EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 250YV 120250 ON TAXI OUT FLAP ASYMMETRY RIGHT INBOARD FLAP. FLAP BARS ILLUMINATED.INSPECTED FLAPS. PULLED MX CODES AND CLEARED FAUL TS. REPLACED FLAP CONTROL UNIT. GROUND CHECK NORMAL. ALL PANELS CLOSED. 2 L 7 2 4T RT A31SO 2001091400045 20010914 00045 SO 2001 9 14 SWIA200110104 1 20010815 A 3260 CONNECTOR EMB 120 EMB120ER 3260203 SO UPLOCK SENSOR LOOSE A SWIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 07 250YV 120250 AFTER TAKEOFF RIGHT GEAR A & B RED LIGHTS REMAINED ON AND IT FELT LIKE GEAR WAS STILL DOWN. WHILE READING QRH, LEFT MAI N A & B RED LIGHTS CAME ON AND AIRPLANE YAWED TO THE LEFT, THEN TO THE RIGHT, FOLLOWED BY ALL LIGHTS OUT.TIGHTENED CONNE CTOR AT LEFT AND RIGHT MAIN UPLOCK SENSORS. CYCLED GEAR 20 TIMES. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001091400046 20010914 00046 WP 2001 9 14 0103189922 1 20010628 A 5312 BULKHEAD DOUG DC9 DC932 3022066 WP FUSELAGE GOUGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 945N 47664 DURING AN M-CHECK IN ATL, A GOUGE WAS FOUND IN THE STATION 604 BULKHEAD TEE AT LONGERON 27L. THE GOUGE WAS LOCATED IN T HE AFT FACE OF THE WEB FLANGE AND WAS BLENDED OUT TO A MATERIAL THICKNESS OF 0.058 INCH. 2 L 7 2 4F A6WE 2001091400047 20010914 00047 SO 2001 9 14 SWIA200110106 1 20010818 A 2752 3082001007 ACTUATOR EMB 120 EMB120RT SO TE FLAPS ERRATIC A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 1110J 120110 RT NACELLE FLAP POT IS ERRATIC.REMOVED AND REPLACED RIGHT NACELLE FLAP ACTUATOR. OPS CHECKS GOOD IAW MM 27-50-08. 2 L 7 2 4T RT A31SO 2001091400048 20010914 00048 NE 2001 9 14 SWIA200110107 2 20010816 A 7200 ENGINE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RIGHT MALFUNCTIONED A SWIA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 NM 07 215SW 120281 RIGHT ENGINE WOULD NOT POWER UP FOR TAKEOFF. RAN BOTH ENGINES THROUGH ALL PARAMETERS WITH EEC'S ON AND ALSO WITH EEC'S O FF. NO FAULTS NOTED. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091400049 20010914 00049 WP 2001 9 14 0103199922 1 20010727 A 5414 SKIN DOUG DC9 DC932 3022066 WP LT & RT PYLON DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 945N 47664 DURING AN M-CHECK IN ATL, CORROSION WAS FOUND IN THE LEFT AND RIGHT UPPER BEAVER TAILS, P/N 5923937-501/502. THE BEAVER TAILS WERE REMOVED TO ACCOMPLISH CORROSION REMOVAL. AFTER THE BEAVER TAIL REMOVAL, IT WAS NOTED THAT 11 FASTENER HOLES COMMON TO THE PYLON FRONT SPAR WERE ELONGATED ON EACH SIDE OF THE AIRCRAFT. REPAIR WAS ACCOMPLISHED PER EA 99-181347 O N HOLES NR 78, 79, 81, 82, 84, 85, 88, 90, 91, 92 AND 93 PER LOG PAGE 1644536. 2 L 7 2 4F A6WE 2001091400050 20010914 00050 2001 9 14 SWIA200110108 4 20010817 A 2211 6228315402 COMPUTER EMB 120 EMB120RT SO PWA 118 PW118 NE RIGHT AUTOPILOT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 1117H 120117 UNCOMMANDED PITCH UP WITH AP ENGAGED, AP DISCONNECTED. PERFORMED QRH, RE-ENGAGED AP, AND EXPERIENCED UNCOMMANDED PTICH ROLL. AP DEFERRED ON FO SIDE. MEL 22-11-1 REPLACED NR 2 AUTOPILOT COMPUTER IAW MM 22-10-00. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091400052 20010914 00052 SO 2001 9 14 SWIA200110109 1 20010820 A 2752 3203001005 ACTUATOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA K NONE F FLT CONT AFFECTED CL CLIMB 1 NM 07 196SW 120151 ON DEPARTURE DURING FLAP RETRACTION, FLAP DISAGREEMENT INBOARD PAIR.FOUND LEFT INBOARD FLAP ACTUATOR WITH BAD WIPER. RE MOVED AND REPLACED FLAP ACTUATOR IAW AMM 27-50-00. OPS GOOD. 2 L 7 2 4T RT A31SO 2001110600046 20011106 00046 WP 2001 11 6 01FDEA00824 1 20010911 A 5312 PRESSURE PANEL DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 CORROSION ON CAPT & F/O'S SIDE COCKPIT FLOOR BETWEEN BS 295-322. R&R COCKPIT FLOOR PER SRM & EA. 2 L 7 3 4F A22WE 2001091400053 20010914 00053 2001 9 14 SWIA200110110 4 20010819 A 6122 GOVERNOR EMB 120 EMB120ER 3260203 SO PROPELLER LEAKING A SWIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 393SW 120330 OIL PRESSURE DROPPED IN FLIGHT. ALTERNATE LANDING IN SNA.FOUND OIL LEAKING FROM OVERSPEED GOVERNOR. REPLACED OVERSPEED GOVERNOR. PERFORMED OPS AND LEAK CHECK. OPS CHECK GOOD. NO LEAKS NOTED. 2 L 7 2 4T RT A31SO 2001091400054 20010914 00054 2001 9 14 SWIA200110111 4 20010816 A 3130 WARNING LIGHT EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE COCKPIT ILLUMINATED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 295SW 120322 ''TRIM FAIL'' LIGHT ON MAP ILLUMINATED ON TAKEOFF ROLL. MEL 22-10-1A, MC 021OPERATED TRIM SEVERAL TIMES FULL RANGE. OP S CHECK GOOD ON GROUND. 2 L 7 2 4T 4 T RT A31SO E20NE 2001110600048 20011106 00048 WP 2001 11 6 01FDEA00825 1 20010911 A 5310 DOOR FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 F/S 963 LONG 39R TO 40R AFT FRAME FWD CARGO DOOR FRAME WORN THRU BOTH LAYERS OF SKIN. R&R FRAME PER SRM & EA. 2 L 7 3 4F A22WE 2001091400055 20010914 00055 SO 2001 9 14 SWIA200110112 1 20010819 A 3010 38E966A VALVE EMB 120 EMB120ER 3260203 SO RT ENGINE LEAKING A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 NM 07 296SW 36 36 120325 AFTER TAKE OFF, RIGHT DUCT LEAK LIGHT CAME ON. FOLLOWED QRH PROCEDURE AND AFTER 3 MINUTES WE SHUT DOWN THE RIGHT ENGINE IN FLIGHT. RETURNED TO FAT REPLACED RIGHT PRESSURE REGULATING VALVE. OPS CHECK GOOD. PERFORMED EXTENSIVE GROUND RUN S, NO DUCT LEAK LIGHT NOTED. 2 L 7 2 4T RT A31SO 2001110600049 20011106 00049 WP 2001 11 6 01FDEA00826 1 20010911 A 5230 SKIN DOUG DC10 DC1010 3022110 WP CARGO DOOR DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 F/S 559 LONG 39R TO 40R 6 EA DENTS AFT OF FWD CARGO DOOR. R&R DOOR PER EA & SRM. 2 L 7 3 4F A22WE 2001091400056 20010914 00056 NE 2001 9 14 SWIA200110113 2 20010815 A 7200 ENGINE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LEFT MALFUNCTIONED A SWIA L ABORTED APPROACH R J PARTIAL RPM/PWR LOSS WARNING INDICATION AP APPROACH 1 NM 07 209SW 120269 ON APPROACH, LEFT ENGINE EXPERIENCED A SEVERE POWER LOSS. TRIPLE CHIME ''ENGINE CONTROL'' AND WHITE ''MANUAL'' LIGHT IL LUMINATED. INITIATED A GO-AROUND TO AVOID TERRAIN CONTACT. ON GO-AROUND, REGAINED SOME POWER ON LEFT ENGINE. BROUGHT POWER BACK TO LEVEL OFF AND LEFT ENGINE AUTO-FEATHERED. POSSIBLE OVER-TORQUE OF LEFT ENGINE. BROUGHT LEFT POWER LEVER TO FLT-IDLE. ENGINE APPEARED HEALTHY. RESET AUTO-FEATHER; LANDED NORMALLY. DOWNLOADED FDAU. RIGHT ENGINE RECORDED EX CEEDANCE. RIGHT TORQUE MAX 112 PERCENT EXCEEDANCE (AVERAGE 111.5 PERCENT) FOR 007 SECONDS. MAX T6 TEMP 769 DEGREES. RA N BOTH ENGINES ON GROUND PER EMB MM 71-00-00. ALL PROCEDURES REF. MM 61-00-00. RIGHT ENGINE EXCEEDANCES WITHIN LIMITS 2 L 7 2 4T 4 T RT A31SO E20NE 2001100900156 20011009 00156 NM 2001 10 9 01FDEA00829 1 20010911 A 2170 ACM BOEING 727 72722C 138400F NM LEFT HAND FAILED A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 104FE 19198 01-305 IN CLIMB CREW NOTICED ODOR IN COCKPIT. R&R LT ACM PER MM 21-51-001-4. 2 L 7 3 4F A3WE 2001091400057 20010914 00057 SO 2001 9 14 SWIA200110114 1 20010817 A 2121 FAN EMB 120 EMB120ER 3260203 SO CABIN COOLING INTERMITTENT A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 290SW 120317 AFTER SHUTDOWN, WITH APU ON AND SET TO AUTO-NORM, CABIN FILLED WITH SMOKE. NO COCKPIT INDICATIONS AND PACKS STILL BLOWI NG COOL AIR. PER CONVERSATION WITH THE CAPTAIN, SMOKE WAS NOTICED ON LANDING ROLL. WHILE INVESTIGATING CAUSE, RIGHT GRO UND COOLING FAN SHUT DOWN AND THEN RESTARTED AFTER TEN TO FIFTEEN SECONDS. SUSPECT GROUND COOLING FAN ON RIGHT SIDE INT ERMITTENT. INSTALLED SERVICEABLE UNIT. OPS CHECK GOOD ON DECK. SN ON 179 SN OFF 164. 2 L 7 2 4T RT A31SO 2001092700062 20010927 00062 NM 2001 9 27 01FDEA00830 1 20010911 A 3610 652245320 DUCT BOEING 727 72725C 138400H NM NR 3 ENGINE CRACKED A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 136FE 19855 PASSING 1500 FT ABOVE GROUND LEVEL NR 3 ENG FIRE LIGHT ILLUM WHEN THROTTLE RETARD. REMOVED AND REPLACED 8TH STAGE BLEED DUCT PER MM 36-00-001-2. 2 L 7 3 4F A3WE 2001091400058 20010914 00058 SO 2001 9 14 SWIA200110115 1 20010818 A 2750 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE TE FLAPS CONTAMINATED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 188SW 120039 FLAP DISAGREEMENT WHEN FLAPS BROUGHT UP FROM 15 DEGREES ON TAKEOFF (HAPPENED REPEATEDLY) THEN GOES AWAY. CLEANED OUTBOA RD FLAP ACTUATOR CANNON PLUGS. TESTED FLAP. NO FAULTS. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091400059 20010914 00059 NM 2001 9 14 01FDEA00831 1 20010908 A 7830 LINE BOEING 727 727232 1384082 NM NR 3 T/R LOOSE A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 497FE 20866 NR 3 ENG STRUT O/H LIGHT ILLUM DURING CLIMBOUT. RAN ENG WITH BOTH PACKS AT HIG 5 MIN, NO O/H LIGHT. TIGHTENED LEAKING THRUST REVERSER FLEX LINE. OK FOR SERVICE. 2 L 7 3 4F A3WE 2001091400060 20010914 00060 SO 2001 9 14 SWIA200110116 1 20010812 A 6120 ROD END EMB 120 EMB120ER 3260203 SO HAMSTD 14RF 14RF19 NE RIGHT PCU WORN A SWIA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 NM 07 308SW 120326 ABORTED TAKEOFF DUE TO RIGHT ENGINE TORQUE FLUCTUATIONS. DEFERRED PER MEL 73-21-1. TROUBLESHOT SYSTEM. FOUND A WORN RO D END ON THE RIGHT ENGINE PCU. REPLACED THE ROD END AND PERFORMED AN OPS CHECK OF ENGINE. ALL CHECKS GOOD. 2 L 7 2 4T RT A31SO 6 C P11NE 2001091400062 20010914 00062 SO 2001 9 14 SWIA200110117 1 20010817 A 6123 30005000053 SIGNAL COND UNIT EMB 120 EMB120ER 3260203 SO HAMSTD 14RF 14RF19 NE LEFT ENGINE MALFUNCTIONED A SWIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 227SW 390 390 120305 DURING AUTOFEATHER SYSTEM TEST, NO GREEN ''ARMED'' LIGHT ALTHOUGH THE TORQUE DOES RISE 75 PERCENT AND THE PROPS WILL FEA THER.REPLACED LEFT SCU. REPLACED XK0161 AND K0161. REPLACED SOCKET FOR RELAY K0161. OPS CHECKED AUTOFEATHER ARM LIGHT . ALL CHECKS GOOD PER MM 61-23-00. 2 L 7 2 4T RT A31SO 6 C P11NE 2001091400063 20010914 00063 SO 2001 9 14 SWIA200110118 1 20010820 A 2120 SMOKE EMB 120 EMB120ER 3260203 SO CABIN DETECTED A SWIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 188SW 120039 SMELL OF SMOKE IN COCKPIT WHILE AIRCRAFT ON THE GROUND.CHECKED AVIONIC COMPARTMENT, BATTERY COMPARTMENT AND HYDRAULIC CO MPARTMENT AND FOUND NO DISCREPANCIES. SMELLED NO SMOKE OR BURNED MATERIALS. 2 L 7 2 4T RT A31SO 2001091400064 20010914 00064 NM 2001 9 14 USAA011012 1 20010807 A 5300 SKIN BOEING 737 7374B7 1384702 NM BS 727D CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 28481 24893 CLT - FOUND SKIN CRACKED .75 INCH, INBOARD RIVET BETWEEN STRINGERS 8-9R AT BS 727D. REPAIR DOUBLER INSTALLED PER TR 53- 10-14. (M) 2 L 7 2 4F RT A16WE 2001091400065 20010914 00065 NM 2001 9 14 USAA011006 1 20010807 A 5300 SKIN BOEING 737 7374B7 1384702 NM BS 927 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 31027 24893 CLT - FUOND SKIN DENTED 1 INCH BY 1.25 INCH BY .030 INCH, BS 927 STRINGER 21L. FILLERS AND DOUBLER INSTALLED PER SRM 51 -20-01 SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2001091400066 20010914 00066 NM 2001 9 14 USAA011005 1 20010807 A 5300 FRAME BOEING 737 7374B7 1384702 NM BS 907R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 28481 24893 CLT - FOUND FRAME CRACKED .75 INCH, INBOARD RIVET BETWEEN STRINGERS 8-9 AT BS 907R. FRAME DOUBLER INSTALLED PER TR 53-1 0-14. (M) 2 L 7 2 4F RT A16WE 2001091400067 20010914 00067 NM 2001 9 14 USAA011002 1 20010807 A 5300 SKIN BOEING 737 7374B7 1384702 NM BS 440 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 31027 24893 CLT - FOUND SKIN WITH BLENDED AREA 1.5 INCH BY .200 INCH BY .180 INCH, BS 440 FORWARD CARGO DOOR CUTOUT STRUCTURE. REWO RK BLENDED AREA PER SRM 53-30-15. (M) 2 L 7 2 4F RT A16WE 2001091400068 20010914 00068 NM 2001 9 14 USAA011000 1 20010807 A 5300 SKIN BOEING 737 7374B7 1384702 NM BS 867R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 28481 24893 CLT - FOUND SKIN CRACKED .75 INCH, INBOARD RIVET BETWEEN STRINGERS 8-9 AT BS 867R. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001091400069 20010914 00069 NM 2001 9 14 USAA010997 1 20010807 A 5300 FRAME BOEING 737 7374B7 1384702 NM BS 727D CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 31027 24893 CLT - FOUND FRAME CRACKED .5 INCH, BS 727D BETWEEN STRINGER 8/9L. REPAIR DOUBLER INSTALLED PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001091400070 20010914 00070 NM 2001 9 14 USAA010996 1 20010807 A 5300 FRAME BOEING 737 7374B7 1384702 NM BS 867 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 31027 24893 CLT - FOUND FRAME DENTED .5 INCH BY 1 INCH, BS 867 S24L. REPAIR DOUBLER INSTALLED PER TR 53-60-07. (M) 2 L 7 2 4F RT A16WE 2001091400071 20010914 00071 EU 2001 9 14 DKAA01017 1 20010718 A 5300 MY2023711052 PANEL AMD FALC20 FALCON 2720302 EU CENTER TANK A DKAA K NONE O OTHER IN INSP/MAINT 1 GL 23 560RA 20724 56 DURING 12 YEAR CORROSION INSPECTION OF CENTER WING FUEL TANK, REMOVABLE PANEL STIFFENER WAS FOUND CRACKED AT THE END OF THE STIFFENER. DASSAULT ENGINEERING WAS CONTACTED AND PROVIDED CHANGE APPROVAL SHEET R245. STIFFENER WAS TRIMMED AND R E-INSPECTED TO ENSURE COMPLETER CRACK REMOVAL. (M) 2 L 7 2 4F A7EU 2001091400072 20010914 00072 CE 2001 9 14 KKFA62201N72C 1 20010626 A 3200 178K235 TIRE LEAR 35 35A 5170602 CE MLG FAILED A KKFA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 23 72CK 165 LEFT MAIN GEAR TIRES BLEW ON LANDING ROLL OUT. REPLACED TIRES WITH SERVICEABLE UNITS. TIRES SHIPPED TO MFG FOR ANALYSI S, THE FOLLOWING IS THEIR CONCLUSION BASED ON INSPECTION AND OBSERVATION FROM MFG REPORT NR NA010707: SUBMITTER STATES, PROBABLE CAUSE OF THIS DOUBLE TIRE FAILURE WAS FOREIGN OBJECT DAMAGE. TIRE S/N 02920527, THE TIRE MOST WORN WAS PUNCTUR ED AND OPERATED OVER DEFLECTED. THIS IN TURN OVERLOADED THE MATE, WHICH FAILED, FOLLOWED SHORTLY AFTER BY THE TIRE WITH THE FOD. CONTROL NR KKFA62201N72CK. (M) 2 L 7 2 4F A10CE 2001091400075 20010914 00075 SO 2001 9 14 SWIA200110119 1 20010820 A 5220 SEAL EMB 120 EMB120RT SO EMERGENCY EXIT LEAKING A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 1117H 120117 ON DEPARTURE FA REPORTED A LOUD SQUEAL COMING FROM FLOOR LEVEL EXIT AT ROW 9.REPAIRED EMERGENCY EXIT DOOR SEAL AS REQUIR ED. PRESSURIZATION CHECK TO 4 PSI. ALL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2001091400077 20010914 00077 SO 2001 9 14 SWIA200110120 1 20010811 A 2750 3069001005 ANNUNCIATOR EMB 120 EMB120RT SO COCKPIT MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 156CA 580 580 120156 RECEIVED FLAP CONTROL FAULT WARNING WHEN SELECTING FLAPS TO 15 DEGREES. RESET WAS SUCCESSFUL AFTER PRESSING RESET TWICE .REPLACED FLAP ANNUNCIATOR IAW MM 27-50-05. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001091400079 20010914 00079 SO 2001 9 14 SWIA200110121 1 20010820 A 2750 12042642507 SELECTOR SWITCH EMB 120 EMB120RT SO TE FLAPS MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 1110J 393 393 120110 FLAP CONTROL FAULT DURING FLAP RETRACTION AND AGAIN WHEN SETTING FLAPS TO 25 DEGREES FOR LANDING. ALL LIGHT BARS FLASHI NG. QRH RESET PROCEDURE WORKED BOTH TIMES.REMOVED AND REPLACED FLAP SELECTOR IAW MM 27-51-00. OPS CHECK GOOD ON GROUND . 2 L 7 2 4T RT A31SO 2001091400080 20010914 00080 NM 2001 9 14 2001UALA01411 1 20010715 A 2710 65263194 PCU BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE AILERON FAILED A UALA K NONE F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 7298U 21893 CREW REPORTS AILERONS EXPERIENCED AN UNCOMMANDED JERKING MOVEMENT WHEN MAKING TURNS TO THE RIGHT. REPLACED AILERON PCU. SYSTEM CHECKS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001091400081 20010914 00081 NE 2001 9 14 SWIA200110122 2 20010820 A 7320 78639010 HMU EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LEFT ENGINE MALFUNCTIONED A SWIA A UNSCHED LANDING F R FLT CONT AFFECTED PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 NM 07 216SW 120285 LEFT ENGINE TORQUE SURGE FROM 71% TO 100% WITH ASSOCIATED YAW ON TAKEOFF.REMOVED AND REPLACED HMU AND FUEL PUMP PER EMB1 20 MM 73-21-00, 73-13-00. RAN LEFT ENGINE PER 71-00-00. OPS CHECK GOOD. NO LEAKS NOTED. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091400083 20010914 00083 NM 2001 9 14 AWXA0002253 1 20010830 A 5310 654N02438 TRACK BOEING 757 757225 1384959 NM CABIN FLOOR CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 D: Seat track flange has corrosion at RBL 25 station 405 to C: Removed and replaced seat track from STA 377 to 410 IAW S RM 51-10-02,53-00-52 Pg 101-102 2 L 7 2 4F RT A2NM 2001091400084 20010914 00084 NM 2001 9 14 AWXA0002255 1 20010829 A 5300 7075T6050 SUPPORT BOEING 757 757225 1384959 NM FLOOR CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 D: Corrosion on floor support Hat section at station 405 between RBL 25 to RBL 45.C: Removed and fabricated and installe d floor support Hat section at STA 405 between RBL 25 to 45 IAW SRM 51-10-2 pg 12, 51-40-02 pg 1 SRM 51-20-01 pg 1 2 L 7 2 4F RT A2NM 2001091400085 20010914 00085 NM 2001 9 14 AWXA0002256 1 20010829 A 5310 654N02438 TRACK BOEING 757 757225 1384959 NM STA 405 RBL 45.0 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 D: Seat track corroded at STA 405 RBL 45.0 beyond allowable limitsC: Removed and replaced seat track IAW SRM 51-10-02, 5 3-00-52 pg 101,102,12 2 L 7 2 4F RT A2NM 2001091400086 20010914 00086 NE 2001 9 14 2001UALA01452 2 20010720 A 7321 FCU BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE NR 2 ENGINE OUT OF ADJ A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 620UA 21880 709617 NR 2 ENGINE REPORT POWER FLUCTUATES SYMPTOMS OR PATTERN ALONG WITH FAULT CODES. FRM CODE 73 21 XD RT ENG EPR+EGT FLUCTU ATES AFTER POWER CHANGE IN CLRWX COND DURING CLIMB EPR+--. THIS IS CAUSED BY THE FUEL CONTROL (FCU) DECELERATION (DECEL) SCHEDULE BEING TO CLOSE TO THE ENGINE'S STEADY STATE OPERATING LINE. THE FCU WILL CYCLE THE 3.0 AND 3.5 BLEEDS TRYING TO KEEP UP WITH THE FCU DECEL SCHEDULE AND THE ENGINE OPERATING LINE, WHICH CAUSES POWER FLUCTUATIONS. THIS IS ESPECIA LLY THE CASE ON ENGINES NEW OUT OF THE SHOP. THIS POWER FLUCTUATION IS CORRECTED BY ADJUSTING THE FCU DECEL SCHEDULE AW AY FROM THE STEADY STATE OPERATING LINE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091400090 20010914 00090 SO 2001 9 14 SWIA200110123 1 20010823 A 2150 VENTURI EMB 120 EMB120ER 3260203 SO LEFT CRACKED A SWIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 291SW 120318 LEFT DUCT LEAK LIGHT ILLUMINATED PRIOR TO ADDING TAKEOFF POWER; TAXI BACK TO GATE. REPLACED LEFT VENTURI WITH SERVICEABL E UNIT. OPS CHECK AND LEAK CHECK GOOD. 2 L 7 2 4T RT A31SO 2001091400091 20010914 00091 NM 2001 9 14 0103206623 1 20010909 A 3040 BOEING 6584609930 BOEING 747 747251B 1384892 NM A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 01 623US D00326 21705 DURING FLIGHT, THE SMELL OF ELECTRICAL SMOKE WAS NOTICED BY THE FLIGHT CREW. PULLED CIRCUIT BREAKERS FOR THE LOWER LEFT HEAT CONTROLLER ON WINDOW L1. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED WINDOW L1 AND WI NDOW HEAT CONTROL MODULE. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2001091400092 20010914 00092 WP 2001 9 14 0103249988 1 20010907 A 2450 CIRCUIT BREAKER DOUG DC9 DC931 3022065 WP FAULTY A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 8944E 47167 ELECTRIC SMOKE IN COCKPIT DURING CLIMB. CAPTAIN TURNED OFF "ENG GEN" AND TURNED ON EMERGENCY POWER. STILL SMELLED SMOKE WITH EMERGENCY POWER ON. PERFORMED COM PROCEDURES, DECLARED AN EMERGENCY, AND RETURNED TO STL AND LANDED WITHOUT INCIDEN T. FOUND AUTO GROUND SPOILER ACTUATOR TO BE THE CAUSE OF SMOKE AND FOUND CIRCUIT BREAKER B1-243 FAULTY. REPLACED CIRC UIT BREAKER. OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 2001091400098 20010914 00098 SO 2001 9 14 SWIA200110124 1 20010820 A 5270 SWITCH EMB 120 EMB120ER 3260203 SO CARGO DOOR MISALIGNED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 578SW 120346 ON TAKEOFF ROLL RECEIVED TRIPLE CHIME AND CARGO LIGHT. ADJUSTED CARGO DOOR MICROSWITCHES FOR WARNING LIGHT. CHECKS GOOD . 2 L 7 2 4T RT A31SO 2001091400103 20010914 00103 SO 2001 9 14 SWIA200110125 1 20010823 A 2751 3471001001 ANNUNCIATOR EMB 120 EMB120RT SO TE FLAPS MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 156CA 120156 FLAPS SET 45 DEGREES ON FINAL, CONTINUITY FAULT ILLUMINATED FOR OUTBOARD PAIR OF FLAPS.REPLACED ANNUNCIATOR/I WITH VERSI ON II PER MM 27-50-00. OPS CHECK OK ON GROUND TESTS. 2 L 7 2 4T RT A31SO 2001091400104 20010914 00104 SO 2001 9 14 SWIA200110126 1 20010820 A 2750 CONTROL UNIT EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 213SW 120277 FLAP ASYMMETRY THEN DISAGREEMENT ON THE GROUND AFTER APU START. NO HYDRAULIC PUMPS ON.INSTALLED A SERVICEABLE FCU. OPE RATED FLAPS SEVERAL TIMES. OPS CHECK GOOD. NO FAULTS NOTED. S/N ON: 0028 S/N OFF: 0221 2 L 7 2 4T RT A31SO 2001091400105 20010914 00105 EA 2001 9 14 SWIA200110127 1 20010826 A 2751 SENSOR CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 423SW 7456 DURING APPROACH TO LANDING (SLC) FLAPS FAILED IN THE DOWN POSITION - LEFT 42 DEGREES AND RIGHT 43 DEGREES.REMOVED AND RE PLACED LEFT BPSU WITH SERVICEABLE UNIT IAW 27-51-10. FLAPS OPS CHECK GOOD. COMPLIED WITH AD 98-20-01. 2 L 7 2 4F RT A21EA 2001091400106 20010914 00106 EA 2001 9 14 SWIA200110128 1 20010825 A 2121 SWITCH CNDAIR CL600 CL6002B19 EA COOLING FAN MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 412SW 7101 ''DISPLAY COOL'' CAUTION MESSAGE IN FLIGHT WITH FAN SWITCH ''NORM'' AND ''FLT ALTN'' EXTINGUISHED IN STBY MODE. MOVED DI SPLAY FAN SWITCH FROM NORMAL TO GND ALT POSITION AND COLLARED CB 1D2. 2 L 7 2 4F RT A21EA 2001091400107 20010914 00107 SO 2001 9 14 SWIA200110129 1 20010822 A 5270 SWITCH EMB 120 EMB120RT SO PASSENGER DOOR MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 269UE 120194 FORWARD DOOR ACTUATOR LT ON IN FLIGHT. LIGHT EXTINGUISHES ON THE GROUND. COULD NOT GET MAIN CABIN DOOR OPEN NORMALLY O N GROUND. USED EMERGENCY OVERRIDE. REMOVED AND REPLACED PASSENGER DOOR SWITCH AT FLIGHT ATTENDANT'S STATION. SYSTEM OP S CHECK GOOD. 2 L 7 2 4T RT A31SO 2001091400108 20010914 00108 SO 2001 9 14 SWIA200110130 1 20010825 A 4920 TURBINE EMB 120 EMB120ER 3260203 SO APU FAILED A SWIA O OTHER A P FLAME/FIRE NO WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 297SW 120327 APU FIRE ON GROUND AFTER APPARENTLY NORMAL STARTUP - NO FIRE INDICATION OBSERVED ON FIRE DETECTION SYSTEM. FIRE WAS OBS ERVED EXTERNALLY. FIRE EXTINGUISHER WAS DISCHARGED FOLLOWING QRH PROCEDURE.INSPECTED APU AND SURROUNDING AREA. FOUND T URBINE FAILURE. NO OTHER DAMAGE NOTED. INSPECTED RUDDER AND SKIN SURFACES. NO DAMAGE NOTED. MEL APU PER 49-00-1. PU LLED APU CONTROL CB & SECURED. 2 L 7 2 4T RT A31SO 2001091400109 20010914 00109 SO 2001 9 14 SWIA200110131 1 20010824 A 3241 WARNING LIGHT EMB 120 EMB120ER 3260203 SO COCKPIT ILLUMINATED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 235SW 120310 ON TAKEOFF ROLL AT APPROXIMATELY 80 KTS, ANTI-SKID ON OUTBOARD LIGHT ILLUMINATED AND BRAKES ON MAP ILLUMINATED WITH SING LE CHIME.POWERED DOWN AIRCRAFT AND POWERED UP, ANTI-SKID INOP LIGHT EXTINGUISHED. TAXI AIRCRAFT TO 80 KTS. ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2001091400110 20010914 00110 EA 2001 9 14 SWIA200110132 1 20010816 A 2621 8978892 EXTINGUISHER CNDAIR CL600 CL6002B19 EA APU DISCHARGED A SWIA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 496SW 7473 APU FIRE BOTTLE IS EMPTY.REMOVED AND REPLACED APU FIRE BOTTLE. OPS CHECKS GOOD. SN OFF 864DEC. 2 L 7 2 4F RT A21EA 2001091400111 20010914 00111 SO 2001 9 14 SWIA200110133 1 20010818 A 3231 SEQUENCE VALVE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE MLG OUT OF ADJ A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 250YV 120250 UPON GEAR RETRACTION, LEFT MAIN GEAR REMAINED DOWN WITH BOTH A AND B RED AND GREEN LIGHTS ILLUMINATED. RECYCLED GEAR DO WN WITH NORMAL INDICATIONS. CYCLED GEAR UP AND LEFT MAIN AGAIN REMAINED DOWN, THIS TIME WITH RIGHT RED A AND B LIGHTS I LLUMINATED AND THEN EXTINGUISHED. RETURNED TO PSP.LEFT MLG-ADJUSTED FORWARD OUTBOARD DOOR SEQUENCE VALVE PLUNGER. OPS C HECK GOOD. RIGHT MLG ADJUSTED FORWARD OUTBOARD INBOARD DOOR SEQUENCE VALVE PLUNGER. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091400112 20010914 00112 NM 2001 9 14 2001UALA01672 1 20010811 A 2121 VF4957EVT3454G BLOWER AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE E/E BAY DEFECTIVE A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 809UA 825 UNUSUAL SMELL IN THE COCKPIT. REPLACED AVIONICS BLOWER FAN. NO FURTHER DISCREPANCIES REPORTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2001091400113 20010914 00113 NM 2001 9 14 2001UALA01725 1 20010813 A 2751 9660022001 INDICATOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE COCKPIT MALFUNCTIONED A UALA O OTHER N FALSE WARNING AP APPROACH 1 WP 29 7445U 21899 AIRCRAFT HAD SPLIT FLAP INDICATION ON APPROACH. OUTBOARD FLAP POSITION INDICATOR FAILED. REPLACED OUTBOARD FLAP POSITIO N INDICATOR. SYSTEM TESTS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001091400117 20010914 00117 WP 2001 9 14 ABXA010471 1 20010912 A 3230 38881571 TIRE DOUG DC8 DC861 3021952 WP NOSE W/W DEFECTIVE A ABXA O OTHER O OTHER CL CLIMB 1 GL 23 849AX 36 45891 DURING DEPARTURE FROM ILN, UPON GEAR RETRACTION, WHEN THE NOSE GEAR ENTERED THE WELL, A VIBRATION WAS FELT IN THE THROTT LE QUADRANT AREA. CREW RECYCLED GEAR AND DID A TOWER FLYBY THEN CONTINUED ON TO LAX. FOUND THE LEFT NOSE TIRE DEFORMED A ND OUT OF ROUND. REPLACED THE LEFT NOSE WHEEL/TIRE ASSEMBLY. REPLACED THE RIGHT NOSE WHEEL/TIRE ASSEMBLY AS PRECAUTIONAR Y IAW DC-8 MM 32-40-01-2. 2 L 7 4 4F 4A25 2001091400118 20010914 00118 WP 2001 9 14 ABXA010472 1 20010912 A 2933 B7127W INDICATOR DOUG DC8 DC861 3021952 WP COCKPIT DEFECTIVE A ABXA B EMER. DESCENT K FLUID LOSS CL CLIMB 1 GL 23 849AX 784 45891 DURING GEAR DOWN EXTENTION INTO LAX, THE HYDRAULIC QUANTITY BEGAN TO RAPIDLY DECREASE. CREW DECLARED AN EMERGENCY INTO L AX. FOUND THE HYDRAULIC INDICATOR INTERMITTENTLY INOPERATIVE. REPLACED THE INDICATOR. BLED THE HYRDRAULIC SYSTEM AND CYC LED ALL FLIGHT CONTROLS. HYDRAULICS OPS CHECKED GOOD IAW DC-8 MM 29-30-00. 2 L 7 4 4F 4A25 2001091400119 20010914 00119 NM 2001 9 14 2001UALA01915 1 20010831 A 5312 BULKHEAD BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 998UA 22741 BULKHEAD BODY STATION 178, RBL 7, WL 224 CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F A16WE E2EA 2001091400120 20010914 00120 SO 2001 9 14 SWIA200110134 1 20010827 A 5753 FLAP TRACK EMB 120 EMB120RT SO PWA 118 PW118 NE TE FLAPS DIRTY A SWIA A UNSCHED LANDING F FLT CONT AFFECTED AP APPROACH 1 NM 07 156CA 120156 ON APPROACH TO OXR, HAD FLAP DISAGREEMENT (INBOARD FLAPS TWO BARS). RETURNED TO LAX.CLEANED FLAP TRACKS. CYCLED FLAPS, COULD NOT DUPLICATE. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091400121 20010914 00121 NM 2001 9 14 2001UALA01916 1 20010831 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 323UA 23955 CABIN STATION 312 FLOORBEAM UPPER SURFACE LBL 5 TO RBL 8 CORROSION REMOVAL MATERIAL LOSS IS BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. REMOVED ORIGINAL REPAIR AND FABRICATED NEW REPAIR PARTS FOR UPPER CAP DOUBLE FLANGE REPAIR. INSTALLED D OUBLER FLANGE REPAIR ANGLES WITH NEW T-CAP. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091400122 20010914 00122 SO 2001 9 14 SWIA200110135 1 20010827 A 7714 ENGINE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LEFT FLUCTUATES A SWIA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 NM 07 216SW 120285 LEFT ENGINE TORQUE FLUCTUATED 20 PERCENT DURING TAKEOFF RUN.FOUND LT ENGINE NH AND NP SENSORS BAD BY USING EEC BREAKOUT BOX. REMOVED AND REPLACED LH ENIGNE NH AND NP SENSORS. TRIMMED ENGINE AS REQUIRED. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091400123 20010914 00123 NM 2001 9 14 2001UALA01917 1 20010831 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 324UA 23956 178 BULKHEAD WL 188, BL 0 RIGHT HAND SIDE WEB CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091400124 20010914 00124 NM 2001 9 14 2001UALA01918 1 20010901 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 323UA 23955 CABIN BODY STATION 827 1-INCH ABOVE STRINGER CLIP STRINGER 9R FRAME WEB CRACKED AT STANDOFF. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091400125 20010914 00125 EA 2001 9 14 COMA0160714 1 20010913 A 2710 601R9002073 CABLE CNDAIR CL600 CL6002B19 EA RT WING FRAYED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 917CA 7017 DURING SCHEDULED MAINTENANCE INSPECTION FOUND THE RIGHT WING LOWER AILERON CABLE TO BE FRAYED WITH BROKEN STRANDS.REPLAC ED AILERON CABLE. 2 L 7 2 4F RT A21EA 2001091400126 20010914 00126 SO 2001 9 14 SWIA200110136 1 20010828 A 2750 CONTROL UNIT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS MALFUNCTIONED A SWIA K NONE F FLT CONT AFFECTED CL CLIMB 1 NM 07 215SW 120281 AFTER FLAP RETRACTION AFTER TAKEOFF INBOARD FLAP DISAGREEMENT. ATTEMPTED CONTROL WITH FLAP HANDLE PER QRH TO NO EFFECT. TROUBLESHOT FLAP SYSTEM IAW MM 27-50-01 AND IAW FIM 27-50-01. COULD NOT GET A FAILURE. ALSO REPLACED FLAP CONTROL UNIT. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091400127 20010914 00127 NM 2001 9 14 2001UALA01919 1 20010901 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 323UA 23955 CABIN BODY STATION 847 1-INCH ABOVE STRINGER CLIP STRINGER 9, FRAME WEB IS CRACKED AT STANDOFF FASTENER. MAJOR REPAIR A CCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091400128 20010914 00128 2001 9 14 SWIA200110137 4 20010820 A 3425 CONNECTOR EMB 120 EMB120RT SO NR 2 DPU MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 07 1117H 120117 ON DESCENT WITH A/P SELECTED TO FIRST OFFICER AND ENGAGED, AIRCRAFT PITCHED OVER. NO AURAL WARNING, NO LIGHTS ON MAP. NOTED CAPTAIN'S RMI FLAGGED AT THE TIME OF HARD OVER. REMOVED AND REPLACED NR 2 DPU CONNECTOR V1 AND V2. DPU SYSTEM OP S CHECK GOOD IAW MM 34-23-00 AND AD. SYSTEM OPS CHECK GOOD AT THIS TIME IAW 22-10-00. 2 L 7 2 4T RT A31SO 2001091400129 20010914 00129 NM 2001 9 14 2001UALA01920 1 20010901 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 324UA 23956 AFT PIT FRAME PUNCTURED AT STATION 887 BETWEEN STRINGER 23 AND 22 RIGHT. MAJOR REPAIR ACCOMPLISHED. FRAME REPAIR ACCOM PLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091400130 20010914 00130 NM 2001 9 14 2001UALA01922 1 20010902 A 5312 BULKHEAD BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 998UA 22741 STATION 178 WEB CRACKED AT LBL 5, 7 AND WL 200. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F A16WE E2EA 2001091400131 20010914 00131 SO 2001 9 14 SWIA200110138 1 20010821 A 2912 FILTER EMB 120 EMB120ER 3260203 SO HYD SYSTEM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 07 216SW 120285 NR 2 HYDRAULIC FILTER LIGHT AFTER DEPARTURE. RETURNED TO SLC. REMOVED AND REPLACED BLUE SYSTEM RETURN FILTERS IAW 29-10 -06. OPS CHECK AND LEAK CHECK SATISFACTORY. 2 L 7 2 4T RT A31SO 2001091400132 20010914 00132 NM 2001 9 14 2001UALA01923 1 20010902 A 5320 SPLICE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 324UA 23956 AFT CARGO PIT SPLICE ANGLE CORRODED, GOUGED. MAJOR REPAIR ACCOMPLISHED. REPLACED SPLICE ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091400133 20010914 00133 2001 9 14 SWIA200110139 4 20010830 A 3442 6225941002 INDICATOR EMB 120 EMB120ER 3260203 SO RADAR SYSTEM INOPERATIVE A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 190SW 120050 RADAR DISPLAY + TCAS DISPLAY WXR-270 MADE A BRIGHT FLASH AND WENT INOP. REMOVED & REPLACED RADAR TRANSCEIVER WTX-250B, RADAR/TCAS INDICATOR IND-270, AND RADAR ANTENNA ANT-318 IAW AMM 34-41-00. OPS CHECK GOOD. ANT-318 PN ON 622-2504-001 2 L 7 2 4T RT A31SO 2001091400134 20010914 00134 EA 2001 9 14 SWIA200110140 1 20010830 A 2760 3G5209C LEVER CNDAIR CL600 CL6002B19 EA SPOILER CONTROL MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 07 499SW 7398 ON A TEN MILE FINAL, WHILE RETRACTING FLIGHT SPOILERS, AIRCRAFT ROLLED LEFT AT 1/4 DETENT. FULLY RETRACTING SPOILERS CO RRECTED THE PROBLEM.NO FAULTS LOGGED IN MDC OR SECU'S. SPOILER RIGGING CHECKS GOOD. REMOVE AND REPLACE FLIGHT SPOILER CONTROL LEVER IAW CRJ MM 27-61-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2001091400135 20010914 00135 EA 2001 9 14 SWIA200110141 1 20010829 A 2750 CONTROL UNIT CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 07 497SW 7482 ''FLAPS FAIL'' MESSAGE APPEARED WHEN SELECTING FLAPS TO ''30''.FLAPS FAIL MESSAGE CLEARED AFTER POWER CYCLE. COMPLIED W ITH AD 98-20-01. FECU FAULT CODE 311/5/A. FLAPS VISUAL INSPECTION CHECKS GOOD, FUNCTIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2001091400136 20010914 00136 EA 2001 9 14 COMA0160715 1 20010913 A 2710 601R9002087 CONTROL CABLE CNDAIR CL600 CL6002B19 1900309 EA RT WING FRAYED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 917CA 7017 DURING SCHEDULED MAINTENANCE INSPECTION FOUND THE RIGHT WING UPPER INBOARD AILERON CABLE TO BE FRAYED WITH BROKEN STRAND S.REPLACED AILERON CABLE. 2 L 7 2 4F RT A21EA 2001091400137 20010914 00137 EA 2001 9 14 SWIA200110142 1 20010828 A 2760 4916405 CONTROL UNIT CNDAIR CL600 CL6002B19 EA NR 2 SPOILERS MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 NM 07 497SW 7482 SPOILER (GROUND) RED MESSAGE ON TAKE OFF. REMOVE AND REPLACE NR 2 SECU IAW CRJ MM 27-61-05. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2001091400138 20010914 00138 NM 2001 9 14 2001UALA01924 1 20010828 A 2760 B435407 PCU BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE SPOILER LEAKING A UALA A UNSCHED LANDING K FLUID LOSS NR NOT REPORTED 1 WP 29 798UA 15733 26928 ACFT RETURNED TO FIELD DUE TO HYDRAULIC LEAK. FOUND NR 6 SPOILER, LEFT WING SECOND SPOILER FROM FUSELAGE LEAKING. THIS IS PART OF THE RIGHT HYDRAULIC SYSTEM JUST INBOARD OF LEFT PYLON. PANEL 552FB REMOVED AND HARDWARE IS BAGGED. MAINT RE PLACED LEAKING NR 6 INBOARD SPOILER PCU. SHOP INSPECTION FOUND FLUID LOSS WAS FROM LOOSE SARD PLUG AN814-8TL ON PCU, RE F CMM 27-60-08 ITEM 377. INSPECTION AND CORRECTION OF LOOSE SARD PLUGS IS BEING ACCOMPLISHED PER BOEING SERVICE LETTER 777-SL-27-021 AND MOOG SERVICE BULLETIN B43540-27-04. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001091400139 20010914 00139 SO 2001 9 14 SWIA200110143 1 20010903 A 2750 CONNECTOR EMB 120 EMB120ER 3260203 SO TE FLAPS DIRTY A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 213SW 120277 AFTER TAKEOFF ON RETRACTION FLAP DISAGREEMENT WITH ASSOCIATED AIRCRAFT ROLL TO THE RIGHT. INSPECTED FLAP SYSTEM WITH BRE AKOUT BOX AND THE MAINTENANCE MODE. FOUND NO FAULTS. CLEANED CANNON PLUGS. FOUND MOISTURE AND GREASE. OPS CHECK GOOD . 2 L 7 2 4T RT A31SO 2001091400140 20010914 00140 NM 2001 9 14 2001UALA01925 1 20010903 A 2120 ODOR BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN DETECTED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 924UA 26645 UNSCHEDULED LANDING DUE TO A BURNING ODOR IN THE CABIN. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091400141 20010914 00141 SO 2001 9 14 SWIA200110144 1 20010902 A 2752 3431001001 SOLENOID EMB 120 EMB120ER 3260203 SO FLAP ACTUATOR BROKEN A SWIA O OTHER J K F WARNING INDICATION FLUID LOSS FLT CONT AFFECTED AP APPROACH 1 NM 07 297SW 120327 DURING APPROACH AFTER NORMAL GEAR EXTENSION FLAPS WERE SELECTED TO 15 DEGREES. A FLAP DISAGREEMENT WITH WARNINGS WAS O BSERVED FOLLOWED BY A HYDRAULIC WARNING AND COMPLETE LOSS OF BLUE SYSTEM HYDRAULICS. APPROXIMATE 10 MINUTES AFTER INITI AL FAILURE A LEFT ANTI-SKID INOP WARNING WAS OBSERVED.FOUND RIGHT NACELLE FLAP ACTUATOR TO HAVE A BROKEN SOLENOID. REPL ACED ACTUATOR IAW MM 27-50-00. REPLACED RIGHT ENGINE DRIVEN HYDRAULIC PUMP ALL HYDRAULIC FILTERS. RAN ENGINE AND NO LE AKS NOTED. FLAPS OPS CHECK GOOD AND NO ANTI-SKID WARNINGS NOTED 2 L 7 2 4T RT A31SO 2001101200071 20011012 00071 NM 2001 10 12 2001UALA01927 1 20010831 A 2910 FITTING BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE HYD SYSTEM LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 907UA 25007 UNSCHEDULED LANDING DUE TO A-SYSTEM HYDRAULIC PROBLEM. *S/D* TIGHTENED LOOSE FITTING ON A-SYS MODULE (TO A-SYS ELEC PU MP). REFILLED A SYS RESERVIOR. LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091900135 20010919 00135 NM 2001 9 19 2001UALA01930 1 20010902 A 5315 FLOORBEAM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 179UA 25158 UPPER DECK FLOORBEAM STATION 1060 RBL 46 CORRODED. MAJOR REPAIR ACCOMPLISHED, TO FLOORBEAM STATION 1060 RBL 46. 2 L 7 4 4F 4 F RT A20WE E24NE 2001091900137 20010919 00137 NM 2001 9 19 2001UALA01931 1 20010902 A 3350 582240 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN FAULTY A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 188UA 26877 EMERGENCY EXIT PATH LIGHTS CAME ON UNCOMMANDED IN CABIN FROM ROW 55ABC THRU 60BC. FAULTY EEL BATTERY PACK AT DOOR 5L. R EPLACED BATTERY PACK. 2 L 7 4 4F 4 F RT A20WE E24NE 2001091900140 20010919 00140 NM 2001 9 19 2001UALA01933 1 20010830 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST UK UNKNOWN 1 WP 29 107UA 26900 EEL AISLE LIGHT INOP 1ST CLASS CROSS AISLE. EEL LIGHT BURNED OUT. REPLACED EEL LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2001091400142 20010914 00142 NM 2001 9 14 2001UALA01934 1 20010903 A 2910 HYDRAULIC SYSTEM AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE YELLOW SYS FAILED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 816UA 871 LANDED UNDER AMBER ALERT DUE TO LOSS OF YELLOW HYDRAULIC SYSTEM. 2 L 7 2 4F 4 F RT A28NM E40NE 2001110800026 20011108 00026 NM 2001 11 8 2001UALA01936 1 20010901 A 7334 42D395 SWITCH BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT ENGINE FAULTY A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 771UA 26932 777049 ENG FUEL FILTER R EICAS MSG DURING CLIMB. POWER (CLIMB) STABLE. ACFT ATTITUDE 8 DEGREES NOSE-UP. RTF. 2 FAULT MESSAGE S: 73-60912 SWITCH POSITION SIGNAL FROM FUEL PUMP FILTER DIFF PRESS SW (R ENG) CHANNEL A AND B DO NOT AGREE AND 73-6092 2 FUEL PUMP FILTER DIFF PRESS SWITCH (R ENG) SIGNAL IS OUT OF RANGE. REPLACED FILTER, NO CONTAMINANTS FOUND, POINTING T O A WARNING SYSTEM PROBLEM. REPLACED DIFFERENTIAL PRESSURE SWITCH. NO RECURRENCE OF FAULT MESSAGES SINCE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001091400143 20010914 00143 NM 2001 9 14 2001UALA01937 1 20010829 A 2530 2676 CHILLER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE GALLEY MALFUNCTIONED A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 779UA 26941 CHILLER IN BUSINESS CLASS CAUSING BURNING SMELL, CREW TURNED OFF CHILLER AND SMELL DISSIPATED. REPLACED FWD CHILLER, RAN BOTH CHILLERS 5 MINUTES AND NOTED NO SMELL. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001091400144 20010914 00144 NM 2001 9 14 2001UALA01939 1 20010902 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 519UA 24872 RT FUSELAGE FRAME AT BS 1682, CABIN FLOOR LEVEL, DAMAGED ON THE TOP OF THE INBD CAP. MAJOR REPAIR ACCOMPLISHED. BLENDED AREA. INSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001091400145 20010914 00145 NM 2001 9 14 2001UALA01940 1 20010831 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1197 STRINGER 37R-36R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091400146 20010914 00146 NM 2001 9 14 2001UALA01941 1 20010831 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1175 STRINGER 37R-36R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091800208 20010918 00208 WP 2001 9 18 ZW0A0107301 1 20010822 A 2133 20219741 ACTUATOR DOUG DC9 DC982 3022082 WP OUTFLOW VALVE FAILED A ZW0A G B A O2 MASK DEPLOYED EMER. DESCENT UNSCHED LANDING O OTHER CR CRUISE 1 CE 13 917TW 49366 IN CRUISE LOST CONTROL OF CABIN PRESSURIZATION. PASSENGER OXYGEN MASKS DEPLOYED AUTOMATICALLY. ACCOMPLISHED EMERGENCY D ESCENT AND PRESSURIZATION CONTROL WAS REGAINED. MADE AN UNSCHEDULED LANDING AT PIT BECAUSE OF THE ADDITIONAL FUEL BURNED AT LOWER ALTITUDE. CHECK-C 6-29-01 STL. REPLACED THE AC OUTFLOW VALVE ACTUATOR BECAUSE ONE MOTOR ON THE ACTUATOR HAD A FAILED SIGNAL GENERATOR. ALSO REPLACED BOTH PRESSURIZATION CONTROLLERS PRECAUTIONARY 2 L 7 2 4F A6WE 2001091400147 20010914 00147 NM 2001 9 14 2001UALA01943 1 20010831 A 5320 FITTING BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 368 STRINGER 38R END FITTING CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FITTING. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091400148 20010914 00148 NM 2001 9 14 2001UALA01944 1 20010831 A 5320 FITTING BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 325 STRINGER 39L END FITTING CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FITTING. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091400149 20010914 00149 SO 2001 9 14 SWIA200110145 1 20010903 A 2750 CONTROL UNIT EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 215SW 120281 FLAP CONTROL FAULT IN CRUISE FLIGHT. DID NOT RESET AS PER QRH PROCEDURE. OUTBOARD FLAPS REMAINED IN UP POSITION THROUG HOUT APPROACH AND LANDING.REMOVED AND REPLACED ANNUNCIATOR. REMOVED LEFT INBOARD FLAP AND REPLACED ALL BEARINGS AND LEF T INBOARD MOVEABLE TRACK IAW 27-50-00. FLAP SYSTEM OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001091400150 20010914 00150 NM 2001 9 14 2001UALA01945 1 20010831 A 5320 FITTING BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 325 STRINGER 39R END FITTING CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FITTING. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091400151 20010914 00151 SO 2001 9 14 SWIA200110146 1 20010903 A 2422 RELAY EMB 120 EMB120ER 3260203 SO ELECTRICAL SYS OVERHEATED A SWIA O OTHER J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 07 581SW 120349 DURING CRUISE INVERTER NR 2 FAILED, ACCOMPANIED BY SMELL OF ELECT SMOKE.FOUND RELAY SOCKET K002 FRIED. REPLACED SOCKET AND RELAY IAW 24-00-00. GROUND OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001091400152 20010914 00152 NM 2001 9 14 2001UALA01947 1 20010831 A 5320 FITTING BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1087-1080 STRINGER 37R END FITTING CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW FITTING. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091400153 20010914 00153 SO 2001 9 14 SWIA200110147 1 20010828 A 5753 FLAP TRACK EMB 120 EMB120ER 3260203 SO TE FLAPS DIRTY A SWIA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 NM 07 224SW 120294 WHEN SELECTING FLAPS 25 DEGREES THE COMMAND BARS WENT TO 25 DEGREES, BUT ALL THREE PAIRS OF FLAPS STAYED AT 15 DEGREES. WE GOT A CONTROL FAULT WHICH RESET AFTER RUNNING THE QRH.CLEANED FLAP TRACKS. PERFORMED OPS CHECK OF FLAP SYSTEM. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001091400154 20010914 00154 NM 2001 9 14 2001UALA01951 1 20010831 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1518 STRINGER 35R-36R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091400155 20010914 00155 SO 2001 9 14 SWIA200110148 1 20010902 A 2751 SELECTOR SWITCH EMB 120 EMB120RT SO TE FLAPS MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 161CA 120143 ON TAXI CHECK, WHEN FLAPS 15 DEGREES WERE SELECTED THE MAP LIGHT ''FLAPS'' AND ''ADV SWS'' ILLUMINATED WITH AN ASSOCIATE D CONTROL FAULT ON FLAP WARNING PANEL WITH FLASHING NACELLE BARS.RESET FLAP SYSTEM. RE-RACKED FCU. REPLACED FLAP SELEC TOR. OPERATED FLAP SYSTEM SEVERAL TIMES. OPS CHECK GOOD. S/N ON: 244495 S/N OFF: 120090. 2 L 7 2 4T RT A31SO 2001091400156 20010914 00156 SO 2001 9 14 SWIA200110149 1 20010901 A 5280 STRUCTURE EMB 120 EMB120ER 3260203 SO MLG DOOR DAMAGED A SWIA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 07 585SW 120353 AFTER TAKEOFF, SELECTED ''GEAR UP''. RIGHT MAIN GEAR RED LIGHTS REMAINED ILLUMINATED ''A" & "B''.FOUND INBOARD RIGHT GE AR DOOR UNLATCHED AND PIN BENT. REPLACED LATCH PIN AND CYCLE GEAR MULTIPLE TIMES. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001091400157 20010914 00157 SO 2001 9 14 SWIA200110152 1 20010907 A 2722 3081401003 ACTUATOR EMB 120 EMB120ER 3260203 SO RUDDER FAILED A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 196SW 120151 RUDDER LOCKED UP ON CLIMBOUT, LOSS OF AUTHORITY OF THE RIGHT RUDDER. RETURNED TO SLC.TESTED RUDDER SYSTEM IAW EMB120 MM 27-22-00. FOUND ACTUATORS THAT FAILED DIFFERENTIAL PRESSURE FUNCTIONAL TESTS. REMOVED AND REPLACED BOTH RUDDER ACTU ATORS IAW EMB120 MM 27-22-02. OPS AND LEAK CHECKS GOOD. GREEN SN OFF 0374. BLUE SN OFF 0551. 2 L 7 2 4T RT A31SO 2001091400158 20010914 00158 NM 2001 9 14 2001UALA01952 1 20010831 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1395 STRINGER 37L-38L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091400159 20010914 00159 NM 2001 9 14 2001UALA01953 1 20010831 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 698 STRINGER 39R-39L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091400161 20010914 00161 NM 2001 9 14 2001UALA01955 1 20010831 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1395 STRINGER 37R-38R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091400162 20010914 00162 NM 2001 9 14 2001UALA01956 1 20010831 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1197 STRINGER 37L-38L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091400163 20010914 00163 NM 2001 9 14 2001UALA01957 1 20010831 A 3260 WARNING SYSTEM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COCKPIT ACTIVATED A UALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 WP 29 108UA 26903 DURING APPROACH, UPON GEAR EXTENSION, THE CREW GOT A GEAR DISAGREE INDICATION. A MISSED APPROACH WAS EXECUTED. ACFT TU RNED FOR NORMAL LANDING. 2 L 7 4 4F 4 F RT A20WE E24NE 2001091400164 20010914 00164 NM 2001 9 14 2001UALA01958 1 20010904 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 323UA 23955 CABIN OVERWING EXIT FRAME BODY STATION 616L FRAME CHORD WEB IS CRACKED TO 2ND FASTENER HOLE APPROXIMATELY 6 INCHES BELOW FLOOR LEVEL. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091400165 20010914 00165 NM 2001 9 14 2001UALA01959 1 20010904 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 323UA 23955 CABIN BODY STATION 727E 1 INCH ABOVE STRINGER CLIP AT STRINGER 9L, FRAME WEB IS CRACKED AT STANDOFF FASTENER. MAJOR R EPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091400166 20010914 00166 NM 2001 9 14 2001UALA01960 1 20010905 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 323UA 23955 CABIN BODY STATION 847 1 INCH ABOVE STRINGER CLIP STRINGER 9L, FRAME WEB IS CRACKED STANDOFF FASTENER. MAJOR REPAIR ACC OMPLISHED. TRIM OUT DAMAGE AREA. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091400167 20010914 00167 NM 2001 9 14 2001UALA01961 1 20010905 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 323UA 23955 AFT CABIN FLOOR STATION 967 FLOORBEAM CAP HAS NICKS, GOUGES AND AN ELONGATED HOLE AT LBL 5 TO LBL 14. MAJOR REPAIR ACCO MPLISHED. CUT OUT DAMAGE AND INSTALLED REINFORCEMENT REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091400168 20010914 00168 NM 2001 9 14 2001UALA01962 1 20010904 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 323UA 23955 EXCESSIVE MATERIAL LOSS ON CABIN FLOORBEAM AT BODY STATION 294.5 LBL 27. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOORBEAM . 2 L 7 2 4F 4 F RT A16WE E2GL 2001091400169 20010914 00169 NM 2001 9 14 2001UALA01963 1 20010903 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 330UA 24191 STATION 178 CENTER WEB FOUND CRACKED AT 12 EA LOCATIONS. MAJOR REPAIR ACCOMPLISHED. INSTALLED SINGLE DOUBLER REPAIR EN COMPASSING ALL CRACKS. 2 L 7 2 4F 4 F RT A16WE E2GL 2001101200088 20011012 00088 NE 2001 10 12 2001UALA01964 2 20010904 A 7230 BLADE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ENGINE DEBONDED A UALA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 WP 29 436UA 25082 8476 638 V10042 UNSCHEDULED LANDING DUE TO NR 1 ENGINE COMPRESSOR STALL. *S/D* BORESCOPE INSPECTION REVEALED DAMAGED HIGH PRESSURE COM PRESSOR SIXTH STAGE BLADES AND DISBONDED RUBSTRIP, WITH ASSOCIATED DOWNSTREAM DAMAGE. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A28NM E40NE 2001091400170 20010914 00170 NM 2001 9 14 2001UALA01965 1 20010904 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1131 STRINGER 39L-39R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091400172 20010914 00172 NM 2001 9 14 2001UALA01968 1 20010903 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 830-860 RBL 59 FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM SECTION A ND SPLICES. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091400173 20010914 00173 NM 2001 9 14 2001UALA01975 1 20010903 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1197 STRINGER 33L T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CAP. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091600001 20010916 00001 NM 2001 9 16 PCAA0109108 1 20010909 A 7921 28E997 OIL COOLER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RIGHT LEAKING A PCAA D RETURN TO BLOCK K FLUID LOSS CL CLIMB 1 EA 13 829EX 12083 146 121071 LGA-MDT FLIGHT#3996. CREW REPORTED #2 ENGINE SHUT DOWN DUE TO LOW OIL PRESSURE. OIL PRESSURE INDICATING BETWEEN 0 AND 35 PSI DURING CLIMBOUT.#2 ENGINE OIL PRESSURE ANNUNCIATOR ILLUMINATED. EMERGENCY DECLARED, PLANE LANDED SAFELY WITHOUT INC IDENT. MAINTENANCE REPLACED #2 OIL COOLER AND REPLENISHED LOST OIL IN ACCORDANCE WITH DASH 8 MAINTENANCE MANUAL. OPERATI ONAL AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2001091700001 20010917 00001 SO 2001 9 17 C2XA01CL202 1 20010914 A 3350 110049 CHARGER EMB 145 EMB145LR SO INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 16963 145116 BNA MAINTENANCE DURING A SERVICE CHECK DISCOVERED LEFT FORWARD EXTERIOR EMERGENCY LIGHT INOPERTIVE.MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY CHARGING UNIT. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001091700002 20010917 00002 EA 2001 9 17 SWIA200110153 1 20010906 A 2750 CONTROL UNIT CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 417SW 7400 FLAP FAIL MESSAGE ON EICAS WHEN FLAPS SELECTED TO 30 DEGREES.COMPLIED WITH AD 98-20-01 BY COMPLYING WITH PARAGRAPH (B)(1 ) 1-4. NO DISCREPANCIES NOTED. 2 L 7 2 4F RT A21EA 2001091700003 20010917 00003 SO 2001 9 17 SWIA200110154 1 20010909 A 5753 FLAP TRACK EMB 120 EMB120ER 3260203 SO RIGHT OUTBOARD WORN A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 198SW 120227 FLAP DISAGREEMENT AFTER TO. QRH PROCEDURE CORRECTED PROBLEM.REPLACED OUTBOARD RIGHT FLAP OUTBOARD FIXED FLAP TRACK IAW EMB MM 57-53-04. OPS CHECK OK. NEW UNIT INSTALLED. P/N: 120-33047-004 2 L 7 2 4T RT A31SO 2001091700004 20010917 00004 2001 9 17 SWIA200110155 4 20010908 A 2210 AUTOPILOT SYS EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 198SW 120227 AUTOPILOT JERKS TO THE LEFT (ROLLS) IN HDG MODE, FIRST OFFICER'S SIDE. PERFORMED OPS CHECK OF AUTOPILOT SYSTEM IAW AMM 2 2-10-00. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001091700005 20010917 00005 SO 2001 9 17 SWIA200110156 1 20010901 A 2751 INDICATOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 07 214SW 120280 WHEN RETRACTING FLAPS AFTER DEPARTURE FROM EKO GOT A FLAP DISAGREEMENT. THE PROBLEM CORRECTED ITSELF BUT TOOK ABOUT TWO MINUTES.CLEANED TRACKS. OPERATED FLAPS SEVERAL TIMES. ALL INDICATIONS NORMAL. FLAPS OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001091700006 20010917 00006 NE 2001 9 17 SWIA200110157 2 20010903 A 7321 EEC EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT ENGINE MALFUNCTIONED A SWIA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 NM 07 214SW 120280 ABORTED TAKEOFF IN WYS DUE TO LEFT ENGINE SURGE +/- 45 PERCENT. PERFORMED ENGINE RUNS. DEFERRED LEFT EEC.RAN LEFT ENGI NE TO TAKEOFF POWER WITH NO FLUCTUATIONS NOTED. ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091700007 20010917 00007 NE 2001 9 17 SWIA200110158 3 20010910 A 6140 PROBE EMB 120 EMB120ER 3260203 SO HAMSTD 14RF 14RF19 NE RIGHT ENGINE INOPERATIVE A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 308SW 120326 ABORTED TAKEOFF IN COD DUE TO ERRATIC NP GAUGE. TAXIED BACK TO GATE AND OBTAINED SPECIAL FLIGHT PERMIT. FERRIED AIRCRA FT TO SLC.INSTALLED SERVICEABLE NP PROBE ON RIGHT ENGINE. P/N: 01R3033515 S/N OFF: CH17235. 2 L 7 2 4T RT A31SO 6 C P11NE 2001091700008 20010917 00008 SO 2001 9 17 SWIA200110159 1 20010908 A 3260 UPLOCK SENSOR EMB 120 EMB120RT SO RIGHT MLG DIRTY A SWIA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 07 196CA 120196 RIGHT 'A' RED GEAR LIGHT DID NOT EXTINGUISH AFTER TAKEOFF. ALL GEAR DOORS REMAINED OPEN WITH GEAR SELECTED IN UP POSITI ON. CYCLED AS PER QRH.CLEANED AND INSPECTED RIGHT MAIN UPLOCK SENSORS AND SWUNG GEAR 20+ TIMES. NO FAULTS FOUND. 2 L 7 2 4T RT A31SO 2001091700009 20010917 00009 2001 9 17 SWIA200110160 4 20010910 A 2215 6225734002 CONTROL SERVO EMB 120 EMB120ER 3260203 SO AILERON MALFUNCTIONED A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 216SW 120285 EXCESSIVE AILERON FORCE REQUIRED ONCE AIRBORNE ALONG THE LONGITUDINAL AXIS. AIRCRAFT ROLLED LEFT ON TAKEOFF AND REQUIRE D 3 3/4 UNITS OF AILERON TRIM WITH A CENTERED INCLINOMETER (BALL). ALMOST FELT AS IF THE AUTOPILOT WAS ENGAGED.REMOVE A ND REPLACE AUTOPILOT SERVO FOR AILERONS. OPS CHECKS GOOD. AILERON CONTROL FELT NORMAL THROUGH FULL TRAVEL. 2 L 7 2 4T RT A31SO 2001091700010 20010917 00010 SO 2001 9 17 SWIA20019996 1 20010702 A 3243 BRAKE ASSY EMB 120 EMB120RT SO PWA 118 PW118 NE HAMSTD 14RF 14RF19 NE MLG FAILED A SWIA O OTHER O OTHER LD LANDING 1 NM 07 137H 120137 NR 2 BRAKE LOCKED UPON LANDING. REPLACED NR 2 BRAKE ASSEMBLY, ALSO BRAKE CONTROL VALVE. AIRCRAFT RESTORED TO NORMAL. AL L CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 6 C P11NE 2001091700011 20010917 00011 2001 9 17 SWIA20019997 4 20010702 A 3418 3995100208 CONTROL UNIT CNDAIR CL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 408SW 7055 30 SECONDS AFTER T/O, ''STALL WARNING'' CAUTION MESSAGE. COMPLIED WITH QRH & RETURNED TO SLC.REPLACED STALL PROTECTION UNIT. STALL PROBLEM OPS CHECKS GOOD IAW MM 27-35-01. 2 L 7 2 4F RT A21EA 2001091700012 20010917 00012 SO 2001 9 17 SWIA20019998 1 20010704 A 5270 WARNING LIGHT EMB 120 EMB120ER 3260203 SO PAX DOOR ILLUMINATED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 197SW 120186 ON TAKEOFF, THE FORWARD DOOR LIGHT ILLUMINATED WITH ASSOCIATED AURAL WARNINGS, THE TAKEOFF WAS ABORTED. THE DOOR WAS CH ECKED CLOSED AND THE FORWARD DOOR WARNING INDICATION WAS DEFERRED PER MX CONTROL 52-70-1C, MC 021.INSPECTED WIRING & MIC RO SWITCHES FOR SECURITY. NO FAULTS FOUND. CLEANED AND LUBED FORWARD DOOR MICRO SWITCHES AS NEEDED. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2001091700013 20010917 00013 2001 9 17 SWIA972617 4 20010528 A 3414 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT ACTIVATED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 234SW 120308 ABORTED TAKEOFF AT 90 KNOTS DUE TO TRIPLE CHIME AND AURAL WARNING HIGH SPEED. VERIFIED NR 2 ASI HAS INTERMITTENT (DIRTY) OVERSPEED SWITCH. REPLACED NR 2 ASI. LEAK TESTED PITOT STATIC SYSTEM IAW MM CHAPTER 34 AND FAR 43 APPENDIX E. TEST G OOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091700014 20010917 00014 SO 2001 9 17 SWIA972618 1 20010605 A 3260 SENSOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE MLG UNSERVICEABLE A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 07 579SW 120347 ON DEPARTURE LANDING GEAR WOULD NOT RETRACT NORMALLY. USED OVERRIDE BUTTON FOR RETRACTION. AFTER GEAR EXTENSION ''IDLE 1 UNLK'' AND ''IDLE 2 UNLK'' ILLUMINATED. CONTINUED PER QRH WITH NO REVERSE ON LANDING. UPON LANDING ''ELEC'' LIGHT IL LUMINATED. NO NOSEWHEEL STEERING WAS AVAILABLE. TAXIED TO THE GATE USING DIFFERENTIAL BRAKING AND POWER. INSTALLED SER VICEABLE WEIGHT ON WHEELS PROXIMITY SENSOR ON RIGHT MAIN GEAR. SYSTEM OPS CHECK GOOD.P/N: 20505-001 2 L 7 2 4T 4 T RT A31SO E20NE 2001091700015 20010917 00015 SO 2001 9 17 SWIA972619 1 20010605 A 2750 POTENTIOMETER EMB 120 EMB120RT SO PWA 118 PW118 NE TE FLAPS FAILED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 07 156CA 120156 FLAP DISAGREEMENT LIGHT MOMENTARILY ILLUMINATED AFTER TAKEOFF. FAULT CODE STORED IN MEMORY BANK INDICATED FLAP SELECTOR POTENTIOMETER FAILED. REPLACED FLAP SELECTOR. OPS CHECK GOOD ON GROUND CHECK. P/N: 120-42642-507 S/N ON: 120028R 2 L 7 2 4T 4 T RT A31SO E20NE 2001091700016 20010917 00016 2001 9 17 SWIA972620 4 20010601 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA GE CF34 CF34* NE STALL WARNING MALFUNCTIONED A SWIA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED TO TAKEOFF 1 NM 07 498SW 7483 AFTER TAKE OFF, DURING FLAP RETRACTION, THE STALL FAIL CAUTION MESSAGE CAME ON. POWERED DOWN A/C, POWERED UP A/C. PERFO RMED SELF TEST OF FLAP CONTROL, PASSED TESTS. RESET STALL COMPUTER. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F 4 F RT A21EA E15NE 2001091700017 20010917 00017 SO 2001 9 17 SWIA972621 1 20010606 A 2752 ACTUATOR EMB 120 EMB120RT SO PWA 118 PW118 NE TE FLAPS MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 1110J 120110 ON FINAL AFTER SELECTING FLAPS 25, FLAP ASYMMETRY WARNING, FOUR SEGMENTS SHOWING ON RIGHT INBOARD AND ONE SEGMENT ON LEF T INBOARD FLAP INDICATOR. AIRCRAFT WAS CONTROLLABLE. LEFT INBOARD FLAP ACTUATOR FEEDBACK POT FAILED INSULATION RESISTAN CE CHECK PER PARKER TROUBLESHOOTING GUIDE. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR IAW MM 27-50-07. OPS CHECK GOOD. NO LEAKS FOUND. P/N: 320300-1005 S/N ON: 1029 S/N OFF: 0059 2 L 7 2 4T 4 T RT A31SO E20NE 2001091700018 20010917 00018 SO 2001 9 17 SWIA972622 1 20010607 A 5610 WINDSHIELD EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT CRACKED A SWIA O OTHER O OTHER DE DESCENT 1 NM 07 585SW 120353 DESCENDING THROUGH 19,500 FT THE CAPTAIN'S WINDSHIELD CRACKED. COMPLIED WITH QRH PROCEDURE AND LANDED WITHOUT INCIDENT. REPLACED CAPTAIN'S WINDSHIELD IAW EMB120 MM 56-10-01. P/N: NP-151311-1 S/N ON: 01131H7722 S/N OFF: 98342H4748 2 L 7 2 4T 4 T RT A31SO E20NE 2001091700020 20010917 00020 2001 9 17 SWIA972624 4 20010604 A 3414 INDICATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 224SW 120294 ABORTED TAKEOFF DUE TO ''HIGH SPEED WARNING''. REMOVE AND REPLACE CAPTAIN'S AIRSPEED INDICATOR. OPS CHECK GOOD. DONE I AW MM 34-12-01. SN ON AH485 SN OFF AH790 2 L 7 2 4T 4 T RT A31SO E20NE 2001091700021 20010917 00021 EA 2001 9 17 SWIA972625 1 20010608 A 2913 PUMP CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE RT ENG HYD SYS FAILED A SWIA O OTHER J WARNING INDICATION LD LANDING 1 NM 07 903SW 7425 30 SECONDS AFTER GEAR WAS SELECTED DOWN, NR 2 HYDRAULIC PRESSURE MESSAGE HYDRAULIC LEVEL IN NR 2 INDICATED 0 PERCENT FLU ID. AFTER SHUTDOWN LEVEL ROSE TO 15 PERCENT. EDP RUNNING DRY FOR 5 MINUTES. REPLACED RIGHT ENGINE HYDRAULIC PUMP IAW MM 29-11-01. PN ON 887055 SN ON MX625954 SN OFF MX555746. SERVICED WITH 4 QTS SKYDROL. RAN RIGHT ENGINE AND CYCLED H YDRAULIC COMPONENTS. NO LEAKS NOTED. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2001091700022 20010917 00022 2001 9 17 SWIA972626 4 20010610 A 2297 WIRE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE AUTOPILOT FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 195SW 120127 AUTOPILOT ENGAGED DURING CLIMB AND WOULD NOT DISENGAGE UNTIL CIRCUIT BREAKER PULLED. FOUND WIRE W201-1153-24 BETWEEN AUT OPILOT TRANSFER BOX P1122 PIN 2 AND COPILOTS FCP-65 P0178 PIN 47 BAD AND NEEDS REPAIRED. AMBER ''DIS'' FOR YAW DOES NO T ILLUMINATE WHEN COPILOTS AUTOPILOT SELECTED ON APP-65 PANEL. DEFERRED RIGHT AUTOPILOT. UPDATE 6/17/2001: REMOVED AN D INSTALLED A SERVICEABLE WIRE W201-1153-24 BETWEEN RIGHT FCP AND TRANSFER BOX IAW WM 20-20-00. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091700023 20010917 00023 SO 2001 9 17 SWIA972627 1 20010611 A 3010 BOOT EMB 120 EMB120RT SO PWA 118 PW118 NE DEICE SYSTEM DAMAGED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 161CA 120143 DURING FLIGHT IN ICING CONDITIONS RIGHT OUTBOARD DEICE BOOT FAILED TO INFLATE AFTER ASSOCIATED INOP LIGHT. INSTALLED BOO T PATCH ON RIGHT OUTBOARD WING IAW BF 74-451-AA. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091700024 20010917 00024 SO 2001 9 17 SWIA972628 1 20010611 A 2752 ACTUATOR EMB 120 EMB120RT SO PWA 118 PW118 NE TE FLAPS FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 162CA 120150 CONTROL FAULT WHEN SELECTING FLAPS 15, RESET AS PER QRH. CONTROL FAULT AGAIN WHEN SELECTING FLAPS 25. PERFORMED ACTUATO R TEST ON BOTH OUTBOARD ACTUATORS. FOUND LEFT OUTBOARD ACTUATOR TO BE BAD. REMOVED AND REPLACED LEFT OUTBOARD ACTUATOR IAW MM 27-50-09. RAN FLAPS NUMEROUS TIMES. NO FAULTS. OPS CHECKS GOOD. PN ON 322300-007 SN ON 0971 SN OFF 0779. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091700025 20010917 00025 EA 2001 9 17 SWIA972629 1 20010611 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 EA GE CF34 CF34* NE TE FLAPS ILLUMINATED A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 499SW 7398 FLAPS FAIL CAUTION MESSAGE ENROUTE AT FL 310. ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURE H 8-8. COMPLIED WITH MAIN TENANCE PROCEDURE OF AD 98-20-01. FLAPS OPERATED NORMAL AT THIS TIME AND NO DISCREPANCIES NOTED. 2 L 7 2 4F 4 F RT A21EA E15NE 2001091700026 20010917 00026 SO 2001 9 17 SWIA972631 1 20010614 A 3260 HARNESS EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE MLG FAILED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 213SW 120277 AFTER DEPARTING, GEAR WOULD NOT RETRACT. GEAR LEVER MOVED FREELY WITH NO GEAR MOVEMENT. LEFT MAIN SYSTEM ''A'' TRANSIT ION LIGHT (RED) DID NOT ILLUMINATE. FOUND LEFT ''A'' UP LOCK HARNESS BAD. REMOVED AND REPLACED WITH SERVICEABLE HARNESS IAW AMM 32-61-01. OHMED OLD HARNESS AND FOUND BAD. OPERATIONAL CHECK IS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091700028 20010917 00028 NM 2001 9 17 DHL2001748001 1 20010903 A 7720 JT8D15 ENGINE BOEING 727 727225 1384077 NM A DHLA K NONE O OTHER CL CLIMB 1 SO 01 748DH 22440 During drop in-to keep from exceeding E.G.T. had to reduce thrust, on #1 engine during take-off. Unable to maintain take -off thrust.1) Checked #1 engine E.G.T. indicator and total resistance, all checked good I.A.W. B-727 M.M. 77-21-00.2) C hecked #1 E.P.R. , no leaks found, but indication was out of tolerance at 1.5 (1.47) + at 2.0 (1.96) I.A.W. B-727 M.M. 7 7-11-00.3) #1 engine bullet removed and stored in AV shops cage.4) Found #1 engine E.P.R indicator out of tolerance I.A. W. B-727 M.M. 77-11-00 page 5075) Removed and replaced #1 engine E.P.R. indicator I.A.W. B-727 M.M. 77-11-00.6) Leak and calibration check is good I.A.W. B-727 M.M. 77-11-10. #1 EPR7) Checked PRBC screens and tubing-PS3 strain 2 L 7 3 4F A3WE 2001091700029 20010917 00029 EA 2001 9 17 SWIA972633 1 20010616 A 2741 CONNECTOR CNDAIR CL600 CL6002B19 EA GE CF34 CF34* NE STAB INDICATOR DAMAGED A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 496SW 7473 ''FLUTTER DAMPER'' ADVISORY APPEARS INTERMITTANTLY INFLIGHT. INSPECTED CANNON PLUG, J1CR PIN 2 TO GROUND CHECK GOOD. C HECK PIN NR 1 ON J1CR TO PIN 19 ON CANNON PLUG P212 JB8 CHECK GOOD. PHYSICALLY CHECKED CANNON PLUG J1CR AND P212 2 L 7 2 4F 4 F RT A21EA E15NE 2001091700031 20010917 00031 NM 2001 9 17 CA010905007 1 20010815 A 3260 MODULE BOEING BOEING 737 737275 1384485 NM PWA JT8 JT8D17 52049 NE MLG SHORTED W O OTHER N FALSE WARNING LD LANDING 1 CA (CAN) ON LANDING IN YHZ LOWER PANEL CAUTION LIGHTS CAME ON & WOULD NOT EXTINGUISH. FOUND SCREW SHORTING TERMINAL OF LAN DING GEAR WARNING INDICATION MODULE SOCKET. REMOVED SCREW AND CHECKED INDICATION SYSTEM & ASSOCIATED SYSTEMS. ALL INDICA TIONS & OPEATIONS NORMAL. A/C RETURNED TO SERVICE. 2 L 7 2 4F 4 F A16WE E2EA 2001091700032 20010917 00032 EU 2001 9 17 CA010906018 1 20010808 A 2722 SC47003 ACTUATOR AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE YAW DAMPER FAILED W H DEACTIVATE SYST/CIRCUITS F I FLT CONT AFFECTED FLT. ATTITUDE INST. CR CRUISE 1 CA (CAN) IN ROUTE TO MIAMI THE AIRCRAFT EXPERIENCED AN UNCOMMANDED YAW, SEVERAL ATTEMPTS FROM THE CREW TO ISOLATE THE PRO BLEM FAILED, THE AIRCRAFT DIVERTD TO RALEIGH FOR REPAIR. FOUND TO BE THE YAW DAMPER ACTUATOR, ALSO AS A PRECAUTION THE Y CHANGED BOTH (FAC) FLIGHT AUGMENTATION COMPUTER. REPLACED NR 1 & 2 FLIGHT AUGMENTATION COMPUTER AND REPLACEDD THE YAW DAMPER ACTUATOR. 2 L 7 2 4F 4 F RT A28NM E29NE 2001091700034 20010917 00034 SO 2001 9 17 SWIA972634 1 20010614 A 2750 HANDLE EMB 120 EMB120RT SO PWA 118 PW118 NE TE FLAPS MALFUNCTIONED A SWIA O OTHER N FALSE WARNING CL CLIMB 1 NM 07 137H 120137 DURING CLIMB WITH FLAPS UP, WE GOT A FLAP/ADVANCED SWS ON MAP, WITH ASSYMETRY AND CONTROL FAULT, ALL LIGHT BARS INDICATI NG FULL FLAPS AND NOT FLASHING. FOLLOWED QRH PROCEDURES AND RESET. INSTALLED SERVICEABLE FLAP SELECT HANDLE, FLAPS CHEC K GOOD 27-50-00. SN ON 120334, SN OFF 120289. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091700035 20010917 00035 EA 2001 9 17 SWIA972635 1 20010615 A 3610 BLEED VALVE CNDAIR CL600 CL6002B19 EA GE CF34 CF34* NE APU FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 413SW 7102 WHEN CONDUCTING THE SINGLE PACK SWITCH OVER FROM THE APU TO THE RIGHT 10TH STAGE AS PER THE PROCEDURE IN THE MEL, THE RI GHT 10TH STAGE BLEED VALVE WOULD NOT OPEN. RETURNED TO THE FIELD DUE TO LEFT A/C PACK BEING DEFERRED. C/W OPS CHECK OF 10TH STAGE BLEED VALVES, APU BLEED VALVES AND 10TH STAGE ISOLATION VALVES. ALL CHECK GOOD AT THIS TIME. LEFT PACK REPL ACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2001091700036 20010917 00036 SO 2001 9 17 SWIA972636 1 20010616 A 5270 LATCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FUEL DOOR MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 586SW 120354 SERVICE DOOR WARNING LIGHT ILLUMINATED ON TAKEOFF ROLL. ABORTED TAKEOFF. RETURNED TO GATE. RE-SECURED LATCH ON OUTBOAR D FUEL DOOR. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091700037 20010917 00037 SO 2001 9 17 SWIA972637 1 20010615 A 7712 INDICATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ENG TORQUE MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 569SW 120344 TORQUE FLUCTUATIONS RIGHT ENGINE ON TAKEOFF ROLL. ABORTED AND RETURNED TO GATE. REPLACED RIGHT ENGINE TORQUE GAUGE. OP S CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091700038 20010917 00038 SO 2001 9 17 SWIA972638 1 20010615 A 2750 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS DIRTY A SWIA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 07 295SW 120322 WHILE RETRACTING FLAPS AFTER TAKEOFF THE INBOARD FLAPS STOP RETRACTING AT APPROXIMATELY 12 DEGREES, WHILE THE OUTBOARD A ND NACELLE FLAPS STOP AT APPROXIMATELY 6 DEGREES. PERFORMED QRH PROCEDURE FOR A FLAP DISAGREEMENT. THE PROBLEM DID NOT CORRECT ITSELF. RETURNED TO LAX FOR LANDING. ENABLED MX MODE OF ANN PNL. ALL HISTORIES REPORTED NO FAILURES. CLEANED ALL CANNON PLUGS. RESTORED A/C TO NORMAL. CYCLED FLAPS 50+ TIMES. NO DISCREPANCIES NOTED. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091700039 20010917 00039 2001 9 17 SWIA972639 4 20010615 A 2210 CONTROL PANEL EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE AUTOPILOT SYS FAILED A SWIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 07 212SW 120276 AIRCRAFT NOSE PITCHES DOWN ABNORMALLY FAST AND STEEP WHEN USING THE A/P ROCKER SWITCH TO NOSE DOWN. NORMAL PITCH CHANGE WHEN ROCKING UP. DEFERRED PER MEL 22-11-1, MC 021. REMOVED AND REPLACED APP-65A CONTROL PANEL. SYSTEM OPS CHECK GOOD IAW EMB120 MM CHAPTER 22-10-04.P/N: 622-6684-006 S/N ON: 2255 S/N OFF: 1689. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091700040 20010917 00040 SO 2001 9 17 SWIA972640 1 20010613 A 3020 BOOT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 212SW 120276 LEFT ENGINE INTAKE BOOT FAILED ON CLIMB OUT. RETURNED TO SLC. REMOVED LEFT ENGINE INLET AND INSTALLED UNIVERSAL COWL ON LEFT ENGINE IAW BR124B-71. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091700041 20010917 00041 EA 2001 9 17 SWIA972641 1 20010609 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT FAILED A SWIA O OTHER O OTHER DE DESCENT 1 NM 07 417SW 7400 PASSING THROUGH 10000 FT AT 150 KIAS AND NORMAL RATE OF DESCENT THE CAPTAIN'S FORWARD WINDSHIELD SHATTERED. IT SHATTER ED WITH A VERY LOUD BANG. REMOVED AND REPLACED PILOT'S WINDSHIELD WITH SERVICEABLE WINDSHIELD IAW CRJ MM 56-00-00. PN O N NP-13921-9 SN ON 01130H7681. 2 L 7 2 4F 4 F RT A21EA E15NE 2001091700042 20010917 00042 2001 9 17 SWIA972642 4 20010618 A 2215 SERVO EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RUDDER TRIM FAILED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 289YV 120289 RUDDER TRIM DELAYED EXCESSIVELY AND THEN WILL KICK TO PROPER DIRECTION AFTER AUTOPILOT ENGAGED, W/O AUTOPILOT ALSO. SER VO PREVIOUSLY NOTED AS NEEDING ADJUSTMENT. REPLACED RUDDER SERVO IAW MM 22-10-05, OPS CHECK GOOD. PN ON 622-5734-002 S N ON 8341 SN OFF 7387. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091700043 20010917 00043 2001 9 17 SWIA972643 4 20010618 A 3414 INDICATOR EMB 120 EMB120RT SO PWA 118 PW118 NE COCKPIT FAILED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 1110J 120110 ''HIGH SPEED'' AURAL WARNING/TRIPLE CHIME SOUNDED ON TAKEOFF ROLL - IAS APPROXIMATELY 40 KNOTS. TAKEOFF ABORTED. REMOVE D AND REPLACED PILOT'S AIRSPEED INDICATOR IAW MM 34-14-00 TO START HISTORY. COULD NOT DUPLICATE BEFORE REPLACEMENT. OP S AND LEAK CHECK GOOD. P/N: 320AS1 S/N ON: AH789 S/N OFF: AH752 2 L 7 2 4T 4 T RT A31SO E20NE 2001091700045 20010917 00045 SO 2001 9 17 SWIA972645 1 20010618 A 2751 ANNUNCIATOR EMB 120 EMB120RT SO PWA 118 PW118 NE TE FLAPS FAILED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 137H 120137 ON CLIMB OUT FLAP ASYMMETRY AND CONTROL FAULT. FLAP HANDLE WAS IN UP POSITION. ALL PAIRS SHOWED IN DOWN POSITION. COM MAND BAR SHOWED DOWN. RETURNED TO FIELD. REPLACED FLAP ANNUNCIATOR IAW MM 27-50-05. OPS CHECK GOOD ON GROUND. P/N: 3 06900-1005 S/N ON: 0155 S/N OFF: 0010 2 L 7 2 4T 4 T RT A31SO E20NE 2001091700046 20010917 00046 EA 2001 9 17 SWIA972649 1 20010624 A 3040 CONTROLLER CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE DEICE SYSTEM INOPERATIVE A SWIA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 NM 07 906SW 7510 SHORTLY AFTER TAKE OFF GOT LEFT WINDOW HEAT CAUTION MESSAGE. RETURNED TO FAT. AFTER TROUBLESHOOTING SYSTEM FOUND FORWAR D TEMP CONTROLLER INOP AND CANNON PLUGS SWAPPED. PUT CANNON PLUGS IN CORRECT POSITION AND REPLACED FORWARD TEMP CONTROL LER IAW CRJ MM 30-41-00. ALL OPS CHECKS GOOD AT THIS TIME. SN ON FORWARD 2454 SN OFF 2464 SN ON AFT 609, PN ON 1659-1. 2 L 7 2 4F 4 F RT A21EA E15NE 2001091700047 20010917 00047 SO 2001 9 17 SWIA972650 1 20010620 A 2750 CONTROL UNIT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 NM 07 194SW 120120 ON DESCENT THROUGH 13,000 FT CONTROL FAULT/SWS WARNING CAUTIONS ILLUMINATE WITH NO MOVEMENT OF FLAP HANDLE. AFTER PUSHI NG RESET, CAUTIONS DISAPPEAR AND THEN REAPPEAR AFTER 2-3 SECONDS. WAS ABLE TO RESET AND USE FLAPS NORMALLY ON 3RD ATTEM PT. REMOVED AND REPLACED FLAP CONTROL UNIT. OPERATED FLAPS NORMALLY. REF. MM 27-50-06. OPS CHECK GOOD. SECURED DOOR. P/N: 307500-1017 S/N ON: 0193 S/N OFF: 0278. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091900141 20010919 00141 NM 2001 9 19 2001UALA01976 1 20010831 A 2721 CONTROL UNIT BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE COCKPIT FAULTY A UALA A UNSCHED LANDING F FLT CONT AFFECTED UK UNKNOWN 1 WP 29 615UA 21876 RETURNED TO SFO DUE RUDDER TRIM ANOMALY. REPLACED AILERON AND RUDDER TRIM CONTROL. OPERATIONALLY CHECKED RUDDER SYSTEM PER APPLICABLE MAINTENANCE MANUAL. ALL OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 2001101800004 20011018 00004 NM 2001 10 18 2001UALA01977 1 20010831 A 2120 CONTROLLER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE E/E BAY FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 618UA 21878 FWD EQUIPMENT NO COOLING LIGHT ON FOR 3 MINUTES. REPLACED CONTROLLER AND CLEANED EQUIPMENT COOLING AIR CLEANER. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091700049 20010917 00049 EA 2001 9 17 SWIA972652 1 20010624 A 3610 CONTROL UNIT CNDAIR CL600 CL6002B19 EA GE CF34 CF34* NE BLEED AIR SYS FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 496SW 7473 ''ANTI ICE DUCT'' MESSAGE INTERMITTANT IN FLIGHT. QRH PROCEDURE COMPLIED WITH. REMOVED PANELS, RAN ENGINES TO CHECK LEFT FUSELAGE DUCTING. NO LEAKS FOUND. INSPECTED SENSORS WITH NO PROBLEMS FOUND. REINSTALLED PANELS. REMOVED AND REPLACE D LEFT BLEED AIR CONTROL UNIT WITH SERVICEABLE UNIT IAW 36-21-10 FOR TROUBLESHOOTING. BLEED AIR CONTROL INDICATING OPS CHECK GOOD. PN ON 20-035008-067 SN ON A0322 SN OFF A1542. 2 L 7 2 4F 4 F RT A21EA E15NE 2001091700050 20010917 00050 NE 2001 9 17 SWIA972653 2 20010615 A 7261 CARBON SEAL EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE LEAKING A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 190SW 120050 LEFT ENGINE INBOARD NACELLE HAS LEAK (APPEARS TO BE FUEL). PERFORMED NECESSARY SHUT DOWN AND RETURNED TO SLC. REMOVE AN D REPLACE LEFT ENGINE BREATHER CARBON SEAL IAW 72-30-00. LEAK CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091900143 20010919 00143 NM 2001 9 19 2001UALA01978 1 20010904 A 3350 BATTERY PACK BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN INTERMITTENT A UALA K NONE O OTHER CR CRUISE 1 WP 29 617UA 21877 EEL IN RIGHT HAND FLASHING INTERMITTENTLY IN FLIGHT. REPLACED EEL BATTERY PACK. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091700051 20010917 00051 SO 2001 9 17 SWIA972654 1 20010611 A 3150 WARNING SYSTEM EMB 120 EMB120RT SO PWA 118 PW118 NE COCKPIT ACTIVATED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 200CD 120200 AURAL WARNING AND MAP LIGHT ILLUMINATED ON TAKEOFF WITH ABORT BELOW 80 KTS. RESET AURAL WARNING SYSTEM. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091700053 20010917 00053 SO 2001 9 17 SWIA972655 1 20010624 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS FAILED A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 194SW 120120 CONTROL FAULT OCCURS IN FLIGHT, WILL NOT RESET. OUTBOARD FLAPS FLASHING. REMOVED AND REPLACED BOTH OUTBOARD FLAP ACTUA TORS IAW 27-50-04. RAN FLAPS NUMEROUS TIMES, OPS AND LEAK CHECK GOOD ON BOTH SIDES. PN ON 320300-1007 SN ON RT 1148, LT 0026A SN OFF RT 1143, LT 0953 2 L 7 2 4T 4 T RT A31SO E20NE 2001101200089 20011012 00089 NE 2001 10 12 2001UALA01981 2 20010824 A 7200 CHECK VALVE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE LEAKING A UALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 WP 29 7286U 21564 ACARS DISPLAYED A STRUT OVERHEAT LIGHT ON NUMBER 1 ENGINE. *S/D* FOUND SENSE LINE LEAKAGE AT 6TH STAGE CHECK VALVE. R EPLACED AND WRENCHED CHECKED LINES. OPERATIONS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001091700054 20010917 00054 SO 2001 9 17 SWIA972656 1 20010625 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS FAILED A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 194SW 120120 OUTBOARD FLAPS DO NOT EXTEND FOR LANDING. PERFORMED TEST WITH BREAKOUT BOX AND LEFT OUTBOARD ACTUATOR FAILED WIPER TEST. INSTALLED SERVICEABLE UNIT IAW MM 27-50-09 AND CYCLED WITH BREAKOUT BOX AND WITH AIRCRAFT SYSTEM. ALL OPS AND LEAK CH ECKS GOOD. PN ON 320300-1001 SN ON 0019 SN OFF 026A. 2 L 7 2 4T 4 T RT A31SO E20NE 2001101200091 20011012 00091 NM 2001 10 12 2001UALA01982 1 20010903 A 3350 S106 BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7275U 21422 OVERHEAD EMERGENCY LIGHTS IN CABIN AT ROW 9 AND 20 ARE NOT OPERATING. *S/D* BATTERY FAILED. FOUND LIGHTS AT ROW 9 NOR MAL, REPLACED BATTERY AT ROW 20. OPERATION CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001101200092 20011012 00092 NM 2001 10 12 2001UALA01983 1 20010828 A 3350 LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE OVERWING INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7293U 21571 RIGHT HAND FORWARD OVERWING EMERGENCY LIGHT IS INOPERABLE. *S/D* DURING OPERATIONAL CHECK ALL EMERGENCY LIGHTS ARE FUN CTIONING NORMALLY. 2 L 7 3 4F 4 F A3WE E2EA 2001091700055 20010917 00055 SO 2001 9 17 SWIA972657 1 20010625 A 2710 TRANSMITTER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE AILERON CONTROL FAILED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 563SW 120338 DURING TAXI CHECK , TAXIING OUT AILERON CONTROL ONLY MOVES 1/2 WAY TO RIGHT - ''SPRINGY'' FEELING. FOUND LEFT AILERON FD R INPUT SHAFT UNSECURED AND BENT UNSERVICEABLE. REPLACED ROTARY VARIABLE INTENSITY TRANSMITTER (RVIT) ARM AND BELLCRANK INPUT SHAFT WITH SERVICEABLE UNITS. ADJUSTED RVIT AS REQD IAW MM 31-30-00. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091900148 20010919 00148 NM 2001 9 19 2001UALA01984 1 20010907 A 5330 SKIN BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 997UA 22457 AIRCRAFT HAS 32 INCH CREASE IN RIGHT SIDE OF FUSELAGE WITH CENTER 18 INCH PUNCTURE BETWEEN STATIONS 907R-947R CROSSING S TRINGERS 22R AND 23R. MAJOR REPAIR ACCOMPLISHED. SPLICED SECTIONS OF S22R AND S23R. REPAIRED SHEAR TIE STA 927. REPAI R SKIN WITH TRIPLER - DOUBLER. 2 L 7 2 4F 4 F A16WE E2EA 2001091900149 20010919 00149 NM 2001 9 19 2001UALA01985 1 20010906 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 915UA 25382 EXISTING REPAIR AT FLOORBEAM AT BS 910 RBL 23 THRU RBL 45 IS CORRODED, OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. REPLAC ED TEE CHORD. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091900150 20010919 00150 NM 2001 9 19 2001UALA01986 1 20010906 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 323UA 23955 FUSELAGE FORWARD BULKHEAD LONGITUDINAL CHORD CRACKED AT BODY STATION 179, WL 207 RIGHT SIDE OF AIRCRAFT. MAJOR REPAIR AC COMPLISHED. INSTALLED STRAP DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091900151 20010919 00151 NM 2001 9 19 2001UALA01987 1 20010906 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 323UA 23955 CABIN BODY STATION 867 1-INCH ABOVE STRINGER CLIP STRINGER 9L FRAME WEB IS CRACKED FASTENER STANDOFF. MAJOR REPAIR ACCOM PLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091900156 20010919 00156 NM 2001 9 19 2001UALA01988 1 20010906 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 323UA 23955 CABIN 1L DOOR CUT UPPER AUXILIARY SILL WEB IS CRACKED AT BODY STATION 306 STRINGER 4L. MAJOR REPAIR ACCOMPLISHED. REPLA CED WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091900157 20010919 00157 NM 2001 9 19 2001UALA01989 1 20010907 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 324UA 23956 STATION 877 FRAME GOUGED CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SPLICE REPAIR, BLENDED DAMAGE ON FRAME. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091900160 20010919 00160 NM 2001 9 19 2001UALA01992 1 20010905 A 3350 POWER SUPPLY BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN DISCHARGED A UALA K NONE O OTHER CR CRUISE 1 WP 29 617UA 21877 RIGHT AISLE OF ECONOMY EMERGENCY FLOOR LIGHTING ILLUMINATED IN FLIGHT. REPLACED EEL LIGHT POWER SUPPLIES. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091900162 20010919 00162 NM 2001 9 19 2001UALA01993 1 20010906 A 3350 7945243 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST UK UNKNOWN 1 WP 29 117UA 28810 EEL STRIP LIGHT INOP AT RT CLOSET ON BOTTOM FWD OF LAV 102. LOOSE CONNECTOR BEHIND SEAT. SECURED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2001091700056 20010917 00056 NM 2001 9 17 ABXA010468 1 20010910 A 2910 HYDRAULIC LINE BOEING 767 767200 1385120 NM NR 1 ENGINE LEAKING A ABXA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 785AX 23018 NR 1 HYDRAULIC QUANTITY DECREASED TO 0.44 IN FLIGHT. QUANTITY STABLE WITH EDP DEPRESSURIZED AND ACMP OFF. INSPECTED NR 1 ENGINE FOUND ENGINE PUMP PRESSURE HOSE LEAKING. REPLACED THE NR 1 ENGINE PRESSURE HOSE. LEAK CHECKED GOOD IAW B767 AMM. 2 L 7 2 4F RT A1NM 2001091700057 20010917 00057 NM 2001 9 17 ABXA010469 1 20010909 A 5330 SKIN BOEING 767 767231 1385131 NM FUSELAGE DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 702AX 22566 GOUGE/DENT IN RIGHT AFT FUSELAGE, TEN FEET AFT OF PIT APPROXIMATELY 11 INCHES IN LENGTH. REPAIRED DAMAGED SKIN BELOW RI GHT SERVICE DOOR, AFT LOWER CARGO DOOR AS REQUIRED IAW REA B653-42263-MR AND B767 SRM 53-00-01. 2 L 7 2 4F RT A1NM 2001091700058 20010917 00058 SO 2001 9 17 SWIA972660 1 20010601 A 7330 HARNESS EMB 120 EMB120RT SO PWA 118 PW118 NE FUEL CELL DAMAGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 1105G 120105 FOUND BADLY DAMAGED WIRES IN LEFT WING TANK NEAR LAST UNDERWING PANEL. REMOVED WIRE HARNESS AND INSTALLED SERVICEABLE AS SEMBLY IAW EMB 120 MM 20-20-00. PN ON 50040-000-01. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091700059 20010917 00059 WP 2001 9 17 ABXA010470 1 20010907 A 2916 A602035509 ASPIRATOR DOUG DC8 DC863 302198A WP HYD RESERVOIR LEAKING A ABXA K NONE K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 23 818AX 46075 THERE WAS A SLOW HYDRAULIC LEAK DURING CLIMB AND CRUISE. LOST APPROXIMATELY 2 GALLONS IN 15 MINUTES. FOUND THE HYDRAUL IC RESERVOIR ASPIRATOR LEAKING WHEN ENGINE WAS RUNNING. REPLACED THE ASPIRATOR IAW DC-8 MM 29-10-05-02-0001. RAN ENGIN E, OPS AND LEAK CHECKED GOOD. 2 L 7 4 4F 4A25 2001091700060 20010917 00060 SO 2001 9 17 SWIA972661 1 20010629 A 3010 VALVE EMB 120 EMB120RT SO PWA 118 PW118 NE DEICE SYSTEM LEAKING A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 269UE 120194 DURING CLIMB OUT, DUCT LEAK LIGHT ILLUMINATED FOR RIGHT ENGINE. COMPLIED WITH QRH, NO CHANGE. CLOSED BLEEDS, ALSO THE PACKS. THE LIGHT DID NOT EXTINGUISH UNTIL POWER ON THE RIGHT ENGINE WAS PULLED TO FLIGHT IDLE. RETURNED TO MEDFORD. GAI NED ACCESS TO ALL DUCT WORK ASSOCIATED WITH RIGHT DUCT LEAK INDICATION SYSTEM. FOUND RIGHT DE-ICE PRESSURE REGULATING V ALVE TO BE LEAKING. REPLACED VALVE IAW MM 30-10-06. OPS CHECKS GOOD. PN ON 38E96-6A SN ON RF1918. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091700061 20010917 00061 NM 2001 9 17 AWXA0002215 1 20010906 A 5330 14803213 SKIN BOEING 757 757225 1384959 NM FUSELAGE DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 915AW 22209 AT FS 1768 BETWEEN STR 19R & STR 20R HAS A DENT. AREA FOUND OUT OF LIMITS, CUT OUT DAMAGE PER SRM 53-00-01 FIG 205. HF EC INSP PER B757 NTM PT6 57-00-19 NO CRACKS NOTED. INSTALLED REPAIR PARTS PER SRM 53-00-01. 2 L 7 2 4F RT A2NM 2001091700062 20010917 00062 EA 2001 9 17 SWIA972662 1 20010630 A 2930 CONNECTOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE HYD SYSTEM LOOSE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 417SW 7400 DURING CLIMB OUT THROUGH 18,000 FT LEFT ENGINE HAD UNCOMMANDED ACCELERATION. N1 WENT INTO RED. REDUCED THRUST LEVERS O N LEFT ENGINE SUCESSFULLY AND RETURNED TO SLC. PERFORMED FAN ROTOR N1 OVERSPEED INSPECTION PER RJ MM 71-00-00 PG 504 TAB LE 503. NO DEFECTS FOUND OF INLET AND TAILPIPE AREAS. PERFORMED UNCOMMANDED ACCELERATION FAULT ISOLATION PER GE MM 72 -00-00 FAULT ISOLATION 12, FOUND YELLOW HARNESS CONNECTOR W8P1 TO AMPLIFIER E5 WAS NOT FULLY SECURED. ALL OTHER HARNESS CONNECTORS CHECKED AND FOUND SECURED. N1 AMPLIFIER DISABLE CHECK, ACCEL/DECEL CHECKS PERFORMED IAW RJ MM 71-00-00. AL L ENGINE PARAMETERS FOUND TO BE WITHIN LIMITS. 2 L 7 2 4F 4 F RT A21EA E15NE 2001091700063 20010917 00063 SO 2001 9 17 SWIA972663 1 20010628 A 2450 RECEPTACLE EMB 120 EMB120RT SO PWA 118 PW118 NE COFFEEMAKER MELTED A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 269UE 120194 ON CLIMB OUT FROM EUGENE, NOTICED BURNING SMELL LIKE BURNING RUBBER IN FLIGHT DECK. SMELL CONTINUED, COULD NOT ISOLATE. NO VISABLE SMOKE. DIVERTED TO PDX. RAN AIRCRAFT FOR 30 MINUTES, COULD NOT DUPLICATE. FOUND FORWARD COFFEE POT ELECTR ICAL RECEPTACLE MELTED. SUSPECT THIS IS ORIGIN. REMOVED AND REPLACED RECEPTACLE IAW CMM 25-00-00. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091700065 20010917 00065 NM 2001 9 17 AWXA0002219 1 20010728 A 5754 65C26794 SKIN BOEING 737 73733A 1384673 NM NR 2 SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 NR 2 SLAT HAS CRACKS PROTRUDING FROM UNDER 2 RIVETS AT BOTTOM ROW UNDER O/B AUX ARM. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR IAW B737-300 SRM 57-43-01 PG 216-219. 2 L 7 2 4F RT A16WE 2001091700066 20010917 00066 NM 2001 9 17 AWXA0002220 1 20010731 A 5315 6546811 FLOORBEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 CORROSION ON FLOORBEAM BS 986.5 RBL 18 TO LBL 18. REMOVED AND REPLACED T-CHORD IAW B737-300 SRM 53-60-51 PG 105-114. 2 L 7 2 4F RT A16WE 2001091700067 20010917 00067 NM 2001 9 17 AWXA0002221 1 20010802 A 5320 672038U2 INTERCOSTAL BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 RT INTERCOSTAL CRACKED BS 178 BLKHD, RBL 24 WL 195 CONFIRMED HFEC. REMOVED AND REPLACED INTERCOSTAL IAW B737-300 SRM 51 -40-02. 2 L 7 2 4F RT A16WE 2001091700069 20010917 00069 WP 2001 9 17 MWEA011256 1 20010914 A 5315 49246791 FLOORBEAM DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 FLOORBEAM CRACKED APPROXIMATELY 8 INCHES FORWARD OF AFT PRESSURE BULKHEAD AT LOWER LEFT CORNER OF VENTRAL DOOR BELOW FLO ORBOARD. CRACK INDICATION FOUND ON RADIOGRAPH LLB. -- REMOVED AND REPLACED FITTING. 2 L 7 2 4F A6WE 2001091700070 20010917 00070 WP 2001 9 17 MWEA011262 1 20010915 A 5310 5911401107 LONGERON DOUG DC9 DC932 3022066 WP STATION 200 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 E&E COMPARTMENT, LONGERON 24 LEFT IS CRACKED AT FRAME STATION 200. -- REMOVED AND REPLACED LONGERON AND SPLICE. 2 L 7 2 4F A6WE 2001091700071 20010917 00071 WP 2001 9 17 MWEA011263 1 20010915 A 5310 591140199 LONGERON DOUG DC9 DC932 3022066 WP STATION 200 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 E&E COMPARTMENT, LONGERON 23 LEFT IS CRACKED AT FRAME STATION 200. -- REMOVED AND REPLACED LONGERON AND SPLICE. 2 L 7 2 4F A6WE 2001091700072 20010917 00072 WP 2001 9 17 MWEA011266 1 20010915 A 5320 59175643 CASTING DOUG DC9 DC932 3022066 WP AFT STAIRS CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 AFT STAIR, LEFT AFT JAMB CORNER FITTING HAS DEEP CHAFE DAMAGE. -- REMOVED AND REPLACED CASTING. 2 L 7 2 4F A6WE 2001091700073 20010917 00073 WP 2001 9 17 MWEA011267 1 20010915 A 5320 591013045 SHEAR TIE DOUG DC9 DC932 3022066 WP STATION 995 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 AFT CARGO PIT, STATION 995, LEFT SHEAR TIE CRACKED AT 28 LEFT. -- REMOVED AND REPLACED SHEAR TIE. 2 L 7 2 4F A6WE 2001091700074 20010917 00074 SO 2001 9 17 SWIA972664 1 20010628 A 3040 TERMINAL EMB 120 EMB120RT SO PWA 118 PW118 NE WINDSHIELD FAILED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 07 269UE 120194 RIGHT WINDSHIELD REPORTED NOT FUNCTIONING & BURN SMELL NOTED IN COCKPIT. FOUND BURNED POWER TERMINAL ON RIGHT WINDSHIEL D. REMOVED AND REPLACED RIGHT WINDSHIELD PER MM 56-10-01. REMOVED & REPLACED POWER WIRE PER WM 30-41-00. WINDSHIELD HE AT OPS CHECK GOOD. NP151311-2 SN ON 9914H3022 SN OFF 97219H2979. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091700077 20010917 00077 EA 2001 9 17 SWIA972665 1 20010628 A 2820 PRESSURE SWITCH CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE FUEL SYSTEM FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 427SW 7497 INFLIGHT LEFT SCAVENGER EJECTOR CAUTION MESSAGE REPEATELLY ILLUMINATES, INCREASES FREQUENCY WITH VERTICAL SPEED GREATER THAN 1,000 FPM. INSTALLED SCAVENGE EJECTOR PRESSURE SWITCH IAW 28-42-07. 2 L 7 2 4F 4 F RT A21EA E15NE 2001091700078 20010917 00078 SO 2001 9 17 SWIA972666 1 20010628 A 5246 SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FUEL DOOR OUT OF ADJ A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 209SW 120269 SERVICE DOOR LIGHT CAME ON JUST AFTER ROTATION. RETURNED TO FIELD. ADJUSTED OUTBOARD FUEL PANEL MICRO SWITCH IAW 52-73- 03. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091700079 20010917 00079 NM 2001 9 17 AWXA0002232 1 20010802 A 5320 651758348 STIFFENER BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 AFT SIDE 178 BLKHD LBL 5.7 VERTICAL TEE CRACKED 1.5 INCH INBOARD SIDE. REMOVED DAMAGE FROM VERTICAL TEE AND INSTALLED R EPAIR IAW 737-300 SRM 53-10-08 PG 221-240. 2 L 7 2 4F RT A16WE 2001091700080 20010917 00080 NM 2001 9 17 AWXA0002233 1 20010802 A 5311 651630087 FRAME BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 RT BS 178 MAIN FRAME CHORD CRACKED AFT SIDE CENTER OF RADIUS WL 206. REMOVED CHORD P/N 65-16300-87 AND INSTALLED CHORD P/N 65-16300-302 IAW ER 03-5311-01232-JS2. 2 L 7 2 4F RT A16WE 2001091700081 20010917 00081 NM 2001 9 17 AWXA0002234 1 20010802 A 5311 651630087 FRAME BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 LT BS 178 MAIN FRAME CHORD CRACKED AFT SIDE CENTER OF RADIUS WL 206. REMOVED CHORD P/N 65-16300-87 AND INSTALL CHORD P/ N 65-16300-301. 2 L 7 2 4F RT A16WE 2001091700083 20010917 00083 NM 2001 9 17 AWXA0002261 1 20010908 A 5310 141N131515 SHEAR TIE BOEING 757 757225 1384959 NM FS 324 DAMAGED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 915AW 22209 D: Shear tie at F.S. 324 between STR 1 & STR 2 left side damaged.C: Removed shear tie, fabricated shear tie filler & shi m IAW DWG # 141N1315 & SRM 51-40-02. Installed shear tie, filler & shim IAW DRG 141N1315 & SRM 51-40-02 2 L 7 2 4F RT A2NM 2001091700089 20010917 00089 NM 2001 9 17 AWXA0002251 1 20010813 A 5330 146N8730 SKIN BOEING 757 757225 1384959 NM FUSELAGE DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 DENT AT APPROX STA 1681.8 STR 18R FOUND TO BE OUT OF LIMITS REF SRM 53-00-01. REPAIRED PER ER 19-5331-01252-DL1. 2 L 7 2 4F RT A2NM 2001091700090 20010917 00090 NM 2001 9 17 AWXA0002252 1 20010910 A 5330 148N321516 SKIN BOEING 757 757225 1384959 NM FUSELAGE DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 DENT IN FUSELAGE SKIN AT STA 1862 BETWEEN STR 23L-25L. TRIMMED CUT DAMAGE AND REPAIRED PER ER 19-5381-01248-TB2. 2 L 7 2 4F RT A2NM 2001091700091 20010917 00091 SO 2001 9 17 SWIA972667 1 20010623 A 3020 HOSE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENG DEICE SYS FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 190SW 120050 LEFT ENGINE AIR INLET FAILED. RETURNED TO THE FIELD. REPLACED HOSE TO LEFT ENG INLET DEICE. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091700092 20010917 00092 NM 2001 9 17 AWXA0002254 1 20010830 A 5415 311N52171 PIN BOEING 757 757225 1384959 NM RT PYLON CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 RIGHT PYLON MIS SPAR O/B FUSE PIN HAS EDDY CURRENT CRACK INDICATION. REMOVED AND REPLACED I/B AND O/B FUSE PINS IAW EO 54-51-03 MM 54-51-02 PG 401-403. 2 L 7 2 4F RT A2NM 2001091700093 20010917 00093 NM 2001 9 17 AWXA0002259 1 20010821 A 5330 146N3711 SKIN BOEING 757 757225 1384959 NM FUSELAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 FUSELAGE SKIN CREASED BETWEEN STA 1681 TO STA 1701 FROM STR 17L TO 14L. REMOVED DAMAGED SKIN AND INSTALLED REPAIR DOUBLE R TRIPLER & FILLERS AT STA 1681 TO 1701, S14L TO S17L PER AWA ER 19-5361-01249-TB2, DATED 9/6/01. REPAIR PERFORMANCE IN ACCORDANCE WITH FAA FORM 8110-3, DATED 9/5/01. 2 L 7 2 4F RT A2NM 2001091700095 20010917 00095 SO 2001 9 17 C2XA01TY111 1 20010913 A 5751 14569009407 ATTACH FITTING EMB 145 EMB145LR SO AILERON GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13990 145277 TYS DURING A SCHEDULED INSPECTION, THE LEFT AILERON CENTER INBOARD ATTACH FITTING WAS FOUND GOUGED. MAINTENANCE BLENDE D OUT THE DAMAGED AREA, PERFORMED DYE-PENETRANT INSPECTION, ALODINED, PRIMED AND PAINTED THE AILERON FITTING IAW-EMB-145 -GST-3059/01. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2001091700096 20010917 00096 SO 2001 9 17 C2XA01TY113 1 20010913 A 3350 20131A BATTERY EMB 145 EMB145LR SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13990 145277 TYS DURING A SCHEDULED INSPECTION, THE EMERGENCY AISLE LIGHTING SYSTEM BATTERY SUPPLY NUMBER 4 WAS FOUND DEAD. MAINTEN ANCE REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY, IAW EMB-145-MM-33-50-04. OPERATIONAL CHECKS WERE GOOD. THE REP AIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2001091700097 20010917 00097 WP 2001 9 17 CALA0100855 1 20010909 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15820 49480 INSPECTION FOUND A 1.5 INCH CRACK IN VENT BOX WEB AT UPPER AFT CORNER AT STA 1485, RT SIDE. AN ANGLE BRACKET WAS INSTAL LED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 2001091700098 20010917 00098 NM 2001 9 17 CALA0100858 1 20010910 A 5343 FITTING BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND RT MLG SIDE STRUT FITTING LUG CORRODED AT STA 685. THE LUG WAS REPAIRED IAW ECRA 5340-01354. 2 L 7 2 4F RT A16WE 2001091700099 20010917 00099 NM 2001 9 17 CALA0100860 1 20010911 A 5210 PAN BOEING 737 7373T0 1384582 NM L1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND A 0.20 INCH CRACK IN L-1 DOOR PAN AT AFT SIDE OF DOOR AT STOP SCREW BELOW CENTERING GUIDE. A DOUBLER W AS INSTALLED IAW ECRA 5210-01398. 2 L 7 2 4F RT A16WE 2001091700101 20010917 00101 EU 2001 9 17 SIMA200124201 1 20010829 A 5315 S5367240620802 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 242AT 242 SAW - DURING CPCP2 INSPECTION, FOUND CORROSION WAS FOUND ON FLOORBEAM 36 AND FLOORBEAM 38. THE FLOORBEAMS WERE REMOVED AND REPLACED IAW WITH ATR42 SRM 51-25-02 AND 51-25-02. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001091700102 20010917 00102 EU 2001 9 17 SIMA200120702 1 20010718 A 5315 S53672409218 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 308AE 309 SAW - DURING CPCP2 INSPECTION, FOUND CORROSION ON FLOORBEAM 40. THE FLOORBEAM WAS REMOVED AND REPLACED IAW ATR72 SRM 51 -25-02. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001091700103 20010917 00103 EU 2001 9 17 SIMA200117801 1 20010614 A 5300 S53671217372 SILL AEROSP ATR72 ATR72212 EU PAX DOOR AREA CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 426AT 426 SAW - DURING CPCP2 INSPECTION, MAINTENANCE FOUND THE PASSENGER DOOR SILL CORRODED. SILL AS REMOVED AND REPLACED IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001091700104 20010917 00104 EU 2001 9 17 NSVA0108 1 20010816 A 2500 006WS00 WEU SAAB SF340 340B 7860101 EU AVIONICS RACK A NSVA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 27 237CJ 237 IAD - LAVATORY SMOKE CWP. MAINTNANCE REMOVED AND REPLACED THE WEU. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001091700105 20010917 00105 SO 2001 9 17 ASOA01138 1 20010816 A 3350 D36604001 BATTERY PACK EMB 120 EMB120 3260201 SO CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 239AS 120057 FLT 4158 - DURING GROUND INSPECTION IN ATL, CREW REPORTED AFT SECTION OF EMERGENCY FLOOR LIGHTS INOPERATIVE. MAINTENANC E REMOVED AND REPLACED AFT EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001091700106 20010917 00106 SO 2001 9 17 ASOA01140 1 20010818 A 3350 D36604001 BATTERY PACK EMB 120 EMB120 3260201 SO CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 232AS 120036 DURING GROUND INSPECTION IN ATL, MAINTENANCE FOUND THE RIGHT FUSELAGE FORWARD EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001091700107 20010917 00107 EU 2001 9 17 DHL2001363022 1 20010808 A 7500 SUPPORT AIRBUS 300 A300B4203 3930306 EU NR 2 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 ON A-5 CHECK, NR 2 ENGINE 14TH STAGE PNEUMATIC DUCT SUPPORT ROD (ARM) AT 9:00 O`CLOCK POSITION IS CRACKED. REMOVED AND REPLACED NR 2 ENGINE 14TH STAGE PNEUMATIC DUCT SUPPORT ROD (ARM) AT 7:00 O`CLOCK POSITION IAW A-300 MM 75-00. 2 L 7 2 4F RT A35EU 2001091700108 20010917 00108 EU 2001 9 17 DHL2001365036 1 20010906 A 2612 CONNECTOR AIRBUS 300 A300B4203 3930306 EU FIRE DETECTION DIRTY A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 365DH 149 NR 2 ENG B-LOOP WILL NOT TEST. DEFERRED PER MEL 26-12-01 MX CTL AUTH 7005 PLACARD INSTALLED. CLEANED AND INSPECTED NR 2 ENG FIRE DETECTION CONTROL UNIT ELECTRICAL PLUG. PERFORMED OPERATIONAL CHECK IAW A300 M/M 26-12-11, OPS CHECK SERVICE ABLE. 2 L 7 2 4F RT A35EU 2001091700109 20010917 00109 SW 2001 9 17 PNSA010402 1 20010410 A 7722 8974697 LEAD SWRNGN SA227 SA227AC 8780603 SW EGT INDICATOR DEFECTIVE A PNSA A UNSCHED LANDING O OTHER CL CLIMB 1 AL 03 640PA AC759B EGT INDICATION ERRATIC DURING CLIMB. RETURNED TO BASE. REPLACED EGT LEAD. OPS CHECK OK. 2 L 7 2 4T RT A8SW 2001091700111 20010917 00111 SW 2001 9 17 PNSA010502 1 20010524 A 3250 MLB2041WO1LJ SWITCH SWRNGN SA227 SA227AC 8780603 SW COCKPIT STUCK A PNSA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 AL 03 41NE AC741B DURING TAXI FOR TAKEOFF PARKING AUTHORITY SWITCH STUCK IN THE PARK POSITION. RETURNED TO BLOCK. REPLACED AUTHORITY SWI TCH. OPS CHECK OK. 2 L 7 2 4T RT A8SW 2001091700113 20010917 00113 SW 2001 9 17 PNSA010503 1 20010508 A 8011 CONNECTOR SWRNGN SA227 SA227AC 8780603 SW RT STARTER LOOSE A PNSA K NONE O OTHER TX TAXI/GRND HDL 1 AL 03 640PA AC759B RT ENGINE WOULD NOT START. REPLACED LOOSE WIRE CONNECTOR FOR STARTER. OPS CHECK OK. 2 L 7 2 4T RT A8SW 2001091700114 20010917 00114 WP 2001 9 17 PNSA010504 2 20010501 A 7321 89778014 FCU SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP RT ENGINE FAILED A PNSA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 AL 03 41NE AC741B P44601C RT ENGINE WOULD NOT DEVELOP TORQUE DURING TAKEOFF RUN. ABORTED TAKEOFF. RETURNED FOR MAINTENANCE. REPLACED FUEL CONTR OL. 2 L 7 2 4T 4 T RT A8SW E4WE 2001091700115 20010917 00115 SO 2001 9 17 PNSA010505 1 20010504 A 2823 SELECTOR VALVE PIPER PA32 PA32301 7103207 SO ENGINE OUT OF ADJ E PNSA D RETURN TO BLOCK X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 AL 03 8429N 328106089 DURING TAXI TO RUNWAY ENGINE QUIT RUNNING. RE-STARTED ENGINE, RETURNED TO BLOCK FOR MAINTENANCE. ADJUSTED FUEL SELECTO R VALVE. 1 L 7 1 3O A3SO 2001091700116 20010917 00116 EA 2001 9 17 PNSA010601 2 20010601 A 7322 252427312 SERVO PIPER PA32 PA32301 7103207 SO LYC O540 IO540K1G5 41532 EA ENGINE FAULTY E PNSA K NONE R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 8327S 328106039 ENGINE WAS RUNNING A LITTLE ROUGH DURING CRUISE. AFTER LANDING AT DESTINATION ENGINE RPM WENT TO IDLE AFTER ADVANCING T HROTTLE. RETURNED TO BLOCK. REPLACED FUEL SERVO. OPERATIONAL CHECK OK. 1 L 7 1 3O 3 O A3SO 1E4 2001091700117 20010917 00117 SO 2001 9 17 PNSA010602 1 20010603 A 2434 ALU8521R ALTERNATOR PIPER PA31 PA31350 7103110 SO LT ENGINE FAILED E PNSA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 28KE 318152049 CLIMBING THROUGH 8000 FEET LT ALTERNATOR LIGHT ILLUMINATED. RETURNED TO BASE. REPLACED ALTERNATOR. OPERATIONAL CHECK OK. 1 L 7 2 3O A20SO 2001091700118 20010917 00118 SW 2001 9 17 PNSA010603 1 20010612 A 7712 CONNECTOR SWRNGN SA227 SA227AC 8780603 SW RT ENGINE DIRTY A PNSA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 AL 03 41NE AC741B RT ENGINE INDICATED LOW TORQUE DURING TAKEOFF. ABORTED TAKEOFF. RETURNED TO BLOCK. CLEANED AND SECURED TORQUE BRIDGE CANNON PLUG AT ENGINE. NO FURTHER PROBLEMS NOTED. 2 L 7 2 4T RT A8SW 2001091700119 20010917 00119 SW 2001 9 17 PNSA010604 1 20010618 A 2930 INDICATOR SWRNGN SA227 SA227AC 8780603 SW COCKPIT ERRATIC A PNSA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 AL 03 650PA AC775B AFTER TAKEOFF HYDRAULIC PRESSURE INDICATION WAS ERRATIC. RETURNED TO BASE. NO FAULT FOUND. 2 L 7 2 4T RT A8SW 2001091700121 20010917 00121 NM 2001 9 17 CALA0100866 1 20010912 A 5320 INTERCOSTAL BOEING 737 737524 1384721 NM BS 482B-520 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19634 26319 INSPECTION FOUND A 1/2" CRACK IN INTERCOSTAL AT BS 482B-520, BL 0. A NEW ANGLE WAS INSTALLED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001091700122 20010917 00122 NM 2001 9 17 CALA0100868 1 20010913 A 5230 SKIN BOEING 737 7373T0 1384582 NM FWD CARGO DR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND FORWARD CARGO DOOR SKIN DENTED IN TWO PLACES. A DOUBLER WAS INSTALLED A EACH LOCATION IAW SRM 52-30-1. 2 L 7 2 4F RT A16WE 2001091700123 20010917 00123 NM 2001 9 17 CALA0100869 1 20010913 A 5754 RIB BOEING 737 7373T0 1384582 NM #4 SLAT GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND R/H WING L/E RIB GOUGED AROUND SCREW HOLE AT #4 SLAT(SLAT STA 30). THE SLAT RIB WAS REPAIRED IAW ECRA 5 750-03584. 2 L 7 2 4F RT A16WE 2001091700124 20010917 00124 NM 2001 9 17 CALA0100871 1 20010913 A 5320 ATTACH ANGLE BOEING 737 7373T0 1384582 NM STA 460 BENT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND FRAME 460 ATTACH ANGLE BENT AT BELLY OF AIRCRAFT. NEW ATTACH ANGLES WERE INSTALLED IAW SRM 53-00-07. 2 L 7 2 4F RT A16WE 2001091700125 20010917 00125 NM 2001 9 17 CALA0100872 1 20010913 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 1040 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND FUSELAGE BELLY SKIN DENTED AT STA 1040, BL 0. A DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 202. 2 L 7 2 4F RT A16WE 2001091700126 20010917 00126 NM 2001 9 17 CALA0100874 1 20010914 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 460 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND EXTERIOR FUSELAGE SKIN DENTED AT STA 460, S22L. THE SKIN WAS REPAIRED IAW SRM 53-00-01. 2 L 7 2 4F RT A16WE 2001091700127 20010917 00127 NM 2001 9 17 CALA0100875 1 20010914 A 5230 SKIN BOEING 737 7373T0 1384582 NM AFT CARGO DR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND AFT CARGO DOOR SKIN DENTED 5 INCHES FROM UPPER EDGE AND 29 INCHES FROM LEADING EDGE. A REPAIR WAS INSTA LLED IAW SRM 53-00-01, FIGURE 219. 2 L 7 2 4F RT A16WE 2001091700128 20010917 00128 NM 2001 9 17 CALA0100876 1 20010914 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM STA 947.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND FLOORBEAM CORRODED AT STA 947.5, RBL 4 TO LBL 24. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-04187 AND SR M 53-00-51, FIGURE 202. 2 L 7 2 4F RT A16WE 2001091700129 20010917 00129 NM 2001 9 17 CALA0100878 1 20010916 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 360-368 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND EXTERIOR FUSELAGE SKIN DENTED AT STA 360-368, S17L. THE DENTED AREA WAS CUT OUT AND A DOUBLER WAS INSTA LLED IAW SRM 53-30-01. 2 L 7 2 4F RT A16WE 2001091700130 20010917 00130 SW 2001 9 17 PNSA010605 1 20010619 A 2931 2719154003 TRANSDUCER SWRNGN SA227 SA227AC 8780603 SW HYD PRESSURE FAULTY A PNSA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 AL 03 650PA AC775B JUST AFTER TAKEOFF HYDRAULIC PRESSURE INDICATION WAS ERRATIC. RETURNED TO BASE. REPLACED HYDRAULIC PRESSURE TRANSDUCER . OPERATIONAL CHECK OK. 2 L 7 2 4T RT A8SW 2001091700131 20010917 00131 SW 2001 9 17 PNSA010607 1 20010628 A 3230 LANDING GEAR SWRNGN SA227 SA227AC 8780603 SW NLG MALFUNCTIONED A PNSA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 640PA AC759B AFTER TAKEOFF NOSE GEAR WOULD NOT LOCK UP. SELECTED DOWN AND RETURNED TO BASE. MAINTENANCE COULD NOT DUPLICATE PROBLEM ON JACKS. NO FURTHER PROBLEMS NOTED. 2 L 7 2 4T RT A8SW 2001091700132 20010917 00132 SO 2001 9 17 PNSA010701 1 20010713 A 2400 SMOKE PIPER PA31 PA31350 7103110 SO COCKPIT DETECTED E PNSA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 AL 03 27663 317852094 DURING CLIMB PILOT NOTICED AN ELECTRICAL BURNING SMELL AND SLIGHT SMOKE IN COCKPIT. AIRCRAFT RETURNED TO AIRPORT. SUBS EQUENT INVESTIGATION INTO THE ELECTRICAL SYSTEM REVEALED NO DISCREPANCIES. AIRCRAFT FLIGHT CHECKED OK AND SUBSEQUENT OP ERATION OF 5.7 HOURS HAS REVEALED NO PROBLEMS. 1 L 7 2 3O A20SO 2001091700134 20010917 00134 SW 2001 9 17 PNSA010703 1 20010705 A 2750 WIRE SWRNGN SA227 SA227AC 8780603 SW FLAP CONTROL BROKEN A PNSA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 AL 03 640PA AC759B WHILE TAXING FOR DEPARTURE FLAPS WOULD EXTEND BUT WOULD NOT RETRACT. AIRCRAFT RETURNED TO GATE AND MAINTENANCE REPAIRED BROKEN WIRE AT FLAP CONTROL VALVE. 2 L 7 2 4T RT A8SW 2001091700137 20010917 00137 WP 2001 9 17 PNSA010704 2 20010708 A 7323 GOVERNOR FRCHLD SA227 SA227DC 3377521 SW GARRTT TPE331 TPE331* 01514 WP RT ENGINE OUT OF ADJ A PNSA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 AL 03 30135 DC890B ABORTED TAKEOFF DUE TO LOW RPM ON RT ENGINE WITH SPEED LEVERS FULL FORWARD. MAINTENANCE ADJUSTED UNDERSPEED GOVERNOR HI GH SETTING AND GROUND RUNUP NORMAL. 2 L 7 2 4T 3 T RT A18SW E2WE 2001091700138 20010917 00138 2001 9 17 VNAA0108015 4 20010824 A 3425 FLIGHT DIR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 423JS 3032 AFTER TAKE OFF, THE CREW WAS GIVEN A HEADING AND DISCOVERED THAT THE FLIGHT DIRECTOR WAS GIVING IMPROPER INDICATIONS. T HE CREW DECIDED TO RETURN TO YOW AND CALL MAINTENANCE. MAINTENANCE HAD THE CREW RECYCLE AIRCRAFT POWER. OPERATIONAL CH ECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. FLIGHT 4190 DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001091700141 20010917 00141 NM 2001 9 17 VNAA0108016 1 20010824 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 437JS 13789 195 3055 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT THE FLIGHT ATTENDANTS SEATING WAS NOT ILLUMINATING. MAINTENANCE INSPEC TED AND REPLACED THE EMERGENCY BATTERY AT THE 5LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPER ATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001091700143 20010917 00143 NM 2001 9 17 VNAA0108017 1 20010826 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN INTERMITTENT A VNAA K NONE O OTHER TX TAXI/GRND HDL 1 GL 07 439JS 13719 80 3057 THE CREW REPORTED THAT THE EMERGENCY LIGHTING STRIP AT ROWS 1 TO 3 WAS WORKING INTERMITTENTLY. THE AIRCRAFT WAS FERRIED TO PIT WHERE MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 4LK POSITION IN ACCORDANCE WITH DORNIER MA INTENANCE MANUAL 33-00- 00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001091700144 20010917 00144 NM 2001 9 17 VNAA0108018 1 20010827 A 2121 011389502 FAN DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE A/C BAY FAILED A VNAA H D DEACTIVATE SYST/CIRCUITS RETURN TO BLOCK J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 442JS 3060 DURING THE TAXI FROM THE GATE, THE CREW NOTICED A LEFT HAND PACK OVERHEAT LIGHT. THE FLIGHT ATTENDANT THEN REPORTED THE RE WAS SMOKE IN THE CABIN. THE CREW RETURNED TO THE GATE AFTER TURNING OFF THE PACKS. MAINTENANCE INSPECTED, CONFIRMED , AND MEL'D THE LEFT HAND HX FAN. FLIGHT 4015 TOOK A THIRTY MINUTE DELAY. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001091700147 20010917 00147 NM 2001 9 17 VNAA0109005 1 20010908 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 432JS 12868 95 3045 THE CREW REPORTED THAT THE EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY B ATTERY AT THE 6LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AN D THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001091700151 20010917 00151 NM 2001 9 17 AWXA0002237 1 20010824 A 5315 6546568107 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 CORROSION ON FLOORBEAM UPPER FLANGE BS 1016 AT SEVERAL LOCATIONS ACROSS THE BEAM. REMOVED CORROSION, FOUND WITHIN LIMIT S IAW B737-300 SRM 53-60-51 P 105-114. REMOVED AND REPLACED ENTIRE 1016 FLOORBEAM UPPER CAP IAW ER 03-5365-01234-DL1. 2 L 7 2 4F RT A16WE 2001091700159 20010917 00159 NM 2001 9 17 PCAA0107073 1 20010717 A 2910 HYDRAULIC SYSTEM DHAV DHC8 DHC8102 2809003 NM NR 1 LOW A PCAA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 EA 13 828EX 392 SYR FLIGHT 3800. CREW REPORTED A MOMENTARY LOSS OF NORMAL BRAKING AFTER LANDING. ALSO NR 1 HYDRAULIC ISOLATION CAUTION LIGHT ILLUMINATED FOR 2 TO 3 SECONDS. MAINTENANCE INSPECTED NR 1 HYDRAULIC SYSTEM, TAXIED AIRCRAFT AND FOUND BRAKING O PERATES NORMALLY. DETERMINED TO BE LOW HYDRAULIC FLUID LEVEL. HYDRAULIC SYSTEM SERVICED. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091700160 20010917 00160 NM 2001 9 17 PCAA0107074 1 20010728 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 819EX 016 MDT- DURING ROUTINE MAINTENANCE VISIT FORWARD RIGHT FLOOR SECTION EMERGENCY LIGHT AFT BULB IN MID LEFT EXIT AND FORWARD LEFT EXTERIOR EGRESS LIGHT FOUND INOPERATIVE. JUMPER REPLACED BETWEEN LIGHT STRIPS AT ROW 7 FOR INTERIOR LIGHT DISCREPA NCY. RELAMPED EMERGENCY EGRESS LIGHT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091700161 20010917 00161 NM 2001 9 17 PCAA0107075 1 20010727 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 811AW 201 BGM- DURING ROUTINE MAINTENANCE VISIT EMERGENCY PATH LIGHTS AT FORWARD EXIT FOUND INOPERATIVE. WIRING FOUND BROKEN AND SPLICES LOOSE. REPLACED LIGHT ASSEMBLY AND REPAIRED WIRES IN ACCORDANCE WITH MAINTENANCE MANUAL. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091700162 20010917 00162 NM 2001 9 17 PCAA0107076 1 20010731 A 3222 88303 NUT DHAV DHC8 DHC8102 2809003 NM NLG STRUT BROKEN A PCAA K NONE O OTHER TX TAXI/GRND HDL 1 EA 13 831EX 160 BWI- FLIGHT 3806. CREW REPORTED NOSE LANDING GEAR SHOCK STRUT GLAND NUT TIGHTENING RING BROKEN OFF. MAINTENANCE REPLAC ED NOSE LANDING GEAR SHOCK STRUT GLANDNUT IN ACCORDANCE WITH COMPONENT MAINTENANCE MANUAL 32-20-01 AND SERVICED STRUT. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091700163 20010917 00163 NM 2001 9 17 PCAA0108077 1 20010801 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 849EX 337 BGM- DURING ROUTINE MAINTENANCE VISIT 1 SECTION OF EMERGENCY PATHWAY LIGHTS FOUND INOPERATIVE. OPEN CIRCUIT REPAIRED UN DER CENTER AISLE FLOOR. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091700164 20010917 00164 NM 2001 9 17 PCAA0108080 1 20010806 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN DISCONNECTED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 819EX 016 MDT- DURING ROUTINE MAINTENANCE VISIT FOUND FORWARD HALF OF RIGHT FLOOR PATH LIGHTS AND FORWARD ARROW EXIT SIGN INOPERAT IVE. PLUGS BETWEEN LIGHTING STRIPS FOUND DISCONNECTED. RECONNECTED PLUGS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091700165 20010917 00165 NM 2001 9 17 PCAA0108081 1 20010717 A 5520 RIVET DHAV DHC8 DHC8102 2809003 NM ELEVATOR LOOSE A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 832EX 280 DURING ROUTINE MAINTENANCE VISIT SEVERAL RIVETS WERE FOUND TO BE WORKING ON RIGHT ELEVATOR AT STATION Y139.5 AND Y 145.8 . RIVETS WERE REPLACED IN ACCORDANCE WITH DEHAVILLAND REPAIR DRAWING RD8-55-324 AND 8110-3 ID CAS-AAL02 FROM CALLAHAN A IRCRAFT SERVICES. ELEVATOR RE-BALANCED PER STRUCTURAL REPAIR MANUAL. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091700166 20010917 00166 NM 2001 9 17 PCAA0108082 1 20010811 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN DISCONNECTED A PCAA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 13 819EX 016 BTV-FLIGHT 3691. CREW REPORTED FLOOR STRIP EMERGENCY LIGHT FROM SEAT 4D FORWARD ARE INOPERATIVE. MAINTENANCE FOUND PLU G DISCONNECTED AT 4D. PLUG RECONNECTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091700167 20010917 00167 NM 2001 9 17 PCAA0108085 1 20010729 A 5520 RIVET DHAV DHC8 DHC8102 2809003 NM ELEVATOR LOOSE A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 833EX 282 DURING ROUTINE MAINTENANCE VISIT LEFT ELEVATOR FOUND TO HAVE ONE NR 4 RIVET WORKING AND ONE TIGHT NR 6 FASTENER. FASTEN ERS REPLACED IN ACCORDANCE WITH DEHAVILLAND REPAIR DRAWING RD8-55-324 AND 8110-3 FORM FROM CALLAHAN REPAIR SERVICES CAS- AAL-03. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091700168 20010917 00168 NM 2001 9 17 PCAA0108086 1 20010722 A 5520 RIVET DHAV DHC8 DHC8102 2809003 NM ELEVATOR LOOSE A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 804EX 27676 227 DURING ROUTINE MAINTENANCE VISIT RIGHT ELEVATOR FOUND TO HAVE LOOSE NR 4 FASTENERS AND A TIGHT NR 6 FASTENER ON TOP OUTB OARD SKIN. LOOSE FASTENERS REMOVED AND REPLACED AS NEEDED IN ACCORDANCE WITH DEHAVILLAND REPAIR DRAWING RD8-55-324, FOU ND NR 6 FASTENER INSTALLED CORRECTLY PER 8110-3 FORM FROM CALLAHAN REPAIR SERVICES ID CAS-AAL-03. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091700169 20010917 00169 NM 2001 9 17 PCAA0108087 1 20010807 A 5520 RIVET DHAV DHC8 DHC8102 2809003 NM ELEVATOR LOOSE A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 847EX 333 DURING ROUTINE MAINTENANCE VISIT LEFT ELEVATOR TOP SKIN AT STATION 145.8 FOUND TO HAVE 1 LOOSE NR 6 FASTENER, 1 LOOSE NR 5 FASTENER, 4 TIGHT NR 6 FASTENERS BUT FLUSH WITH SKIN, AND 2 TIGHT NR 5 FASTENERS BUT FLUSH WITH SKIN. LOOSE FASTENER S REPLACED, AND TIGHT FASTENERS INSPECTED ALL IN ACCORDANCE WITH 8110-3 FORM ID CAS-AAL-02 FROM CALLAHAN AIRCRAFT SERVIC ES. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091700170 20010917 00170 NM 2001 9 17 PCAA0108088 1 20010807 A 5520 RIVET DHAV DHC8 DHC8102 2809003 NM ELEVATOR LOOSE A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 805EX 26694 228 BGM- DURING A CHECK INSPECTION FOUND LEFT ELEVATOR TOP SKIN STATION Y145.8 HAS 1 NR 5 FASTENER TIGHT, BUT FLUSH WITH SKI N AND 14 NR 6 FASTENERS THAT ARE TIGHT BUT FLUSH WITH SKIN. RIGHT ELEVATOR TOP SKIN AT STATION 145.8 HAS 4 NR 5 FASTEN ERS TIGHT BUT FLUSH WITH SKIN, AND STATION 139.5 HAS 4 NR 5 FASTENERS TIGHT BUT FLUSH. FASTENERS INSPECTED AND FOUND TO BE INSTALLED IN ACCORDANCE WITH 8110-3 FORM ID CAS-AAL-02 REV A FROM CALLAHAN AIRCRAFT SERVICES AS A INTERIM INSTALLATI ON. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091700171 20010917 00171 NM 2001 9 17 PCAA0108091 1 20010817 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 818EX 235 BGM-DURING ROUTINE MAINTENANCE VISIT TWO FORWARD EMERGENCY LIGHTS ON FLOOR WERE FOUND INOPERATIVE. BROKEN WIRES REPAIRE D ON TWO FORWARD EMERGENCY LIGHTS. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091700172 20010917 00172 NM 2001 9 17 PCAA0108092 1 20010728 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 820EX 019 MDT- DURING C-INSPECTION FUSELAGE FRAME FOUND CRACKED AT STATION 354.250 JUST ABOVE OUTBOARD RIGHT SEAT RAIL AND JUST FO RWARD OF RIGHT MID EMERGENCY EXIT. DEHAVILLAND ISSUED REPAIR DRAWING RD8-53-6050 AS AN INTERIM REPAIR. REPAIR TO BE IN SPECTED AT 500 HOUR INTERVALS UNTIL PERMANENT REPAIR INSTALLED. 2 H 7 2 4T RT A13NM 2001091700173 20010917 00173 NM 2001 9 17 PCAA0108093 1 20010823 A 5210 85210240007 HAND RAIL DHAV DHC8 DHC8102 2809003 NM AIRSTAIR DOOR BROKEN A PCAA K NONE O OTHER TX TAXI/GRND HDL 1 EA 13 843EX 335 BWI - FLIGHT 3803. CREW REPORTED LEFT HANDRAIL STRUT BROKEN ON AIRSTAIR DOOR. MAINTENANCE REPLACED AIRSTAIR DOOR HANDR AIL. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091700174 20010917 00174 NM 2001 9 17 PCAA0108097 1 20010829 A 5410 RIVET DHAV DHC8 DHC8102 2809003 NM RT NACELLE MISSING A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 818EX 26073 235 BGM- DURING FLEET INSPECTION OF NACELLES FOR LOOSE AND MISSING FASTENERS FOUND 4 RIVETS MISSING FROM OUTBOARD RIGHT NACE LLE AFT OF FLAP TRACK TRAILING EDGE. MAINTENANCE REPLACED RIVETS ON RIGHT OUTBOARD NACELLE AFT OF FLAP TRACK TRAILING E DGE. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091700175 20010917 00175 NM 2001 9 17 PCAA0108098 1 20010728 A 5347 85320490127 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 820EX 019 MDT- DURING C-CHECK INSPECTION INBOARD LEFT FORWARD SEAT RAIL FOUND CORRODED. REPLACED WORN LT INBOARD CABIN SEAT RAIL SECTION, P/N 85320490-127, BETWEEN STATION X182.0 AND X424.0 IN ACCORDANCE WITH DHC ASSEMBLY DRAWING 85320019 AND DHC RE PAIR DRAWINGS 8-53-6057, 8-53-6055, 8-53-4473 AND CAS-AAL08 PAGE 3.1 REVISION DATED 20AUG01 AS APPROVED ON FAA FORM 8110 -3. 2 H 7 2 4T RT A13NM 2001091700176 20010917 00176 NM 2001 9 17 PCAA0108099 1 20010829 A 7110 RIVET DHAV DHC8 DHC8102 2809003 NM LT COWL LOOSE A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 839EX 27817 226 DURING FLEET INSPECTION SEVERAL RIVETS FOUND LOOSE ON LEFT COWLING OUTBOARD END JUST BELOW FLAP TRACK. RIVETS REPLACED IN ACCORDANCE WITH CALLAHAN REPAIR SERVICES DER AUTHORIZATION CAS-AAL-09. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091700177 20010917 00177 NM 2001 9 17 PCAA0108100 1 20010831 A 5410 RIVET DHAV DHC8 DHC8102 2809003 NM LT NACELLE LOOSE A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 809EX 25522 302 DURING FLEET INSPECTION FOR NACELLE RIVETS BEING LOOSE AND MISSING, ONE RIVET FOUND MISSING AND ONE FOUND PULLING THROUG H ON LEFT NACELLE OUTBOARD END PLATE JUST BELOW FLAP TRACK. THREE RIVETS REPLACED ON OUTBOARD LEFT NACELLE JUST BELOW F LAP TRACK IN ACCORDANCE CALLAHAN REPAIR SERVICES DER 8110 FORM CAS-AAL09. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091700178 20010917 00178 NM 2001 9 17 PCAA0108102 1 20010831 A 5410 RIVET DHAV DHC8 DHC8102 2809003 NM RT NACELLE LOOSE A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 817EX 27105 191 DURING FLEET INSPECTION FOR NACELLE RIVETS BEING LOOSE AND MISSING, FOUR LOOSE RIVETS WERE FOUND ON OUTBOARD RIGHT COWLI NG BELOW FLAP TRACK. FOUR RIVETS WERE REPLACED ON COWLING. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091700179 20010917 00179 NM 2001 9 17 PCAA0108103 1 20010108 A 5410 RIVET DHAV DHC8 DHC8102 2809003 NM RT NACELLE LOOSE A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 821EX 26957 173 DURING FLEET INSPECTION FOR NACELLE RIVETS BEING LOOSE AND MISSING, 2 RIVETS ON RIGHT NACELLE OUTBOARD END FOUND LOOSE J UST BELOW FLAP TRACK. LOOSE RIVETS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091700180 20010917 00180 NM 2001 9 17 PCAA0108104 1 20010831 A 5410 RIVET DHAV DHC8 DHC8102 2809003 NM RT NACELLE MISSING A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 848EX 21590 331 DURING FLEET INSPECTION FOR NACELLE RIVETS BEING LOOSE AND MISSING, ONE RIVET WAS FOUND MISSING ON INSPECTION PANEL ON R EAR OF RIGHT NACELLE. LOOSE AND MISSING RIVETS ON INSPECTION PANEL REPLACED IN ACCORDANCE WITH DER CALLAHAN REPAIR SERV ICES 8110 FORM CASAAL09. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091700181 20010917 00181 NM 2001 9 17 PCAA0108107 1 20010831 A 5410 RIVET DHAV DHC8 DHC8102 2809003 NM RT NACELLE MISSING A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 822EX 27038 187 DURING FLEET INSPECTION OF NACELLES FOR LOOSE AND MISSING RIVETS, FOUND 2 MISSING AND 5 LOOSE RIVETS ON RIGHT OUTBOARD N ACELLE FORWARD OF FINGERNAIL (PANEL 15). RIVETS REPLACED IN ACCORDANCE WITH CALLAHAN REPAIR SERVICES DER REPAIR REFEREN CE NUMBER CAS-AAL-09 REVISION B. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091700182 20010917 00182 NM 2001 9 17 PCAA0109101 1 20010903 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN DAMAGED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 811EX 201 DURING ROUTINE MAINTENANCE VISIT FOUND FIRST RED FLOOR PATH EMERGENCY LIGHT INOPERATIVE. WIRING REPAIRED IN FLOOR EMERG ENCY LIGHT TRACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091700183 20010917 00183 NM 2001 9 17 PCAA0109105 1 20010904 A 2701 YOKE DHAV DHC8 DHC8102 2809003 NM COCKPIT MALFUNCTIONED A PCAA O OTHER O OTHER LD LANDING 1 EA 13 829EX 146 ROC- FLIGHT 3555. CREW REPORTED UPON LANDING CAPTAINS YOKE ROLLED 90 DEGREES TO THE LEFT, FIRST OFFICERS YOKE REMAINED CENTERED. MAINTENANCE INSPECTED AREA, CYCLED DISCONNECT HANDLE. CABLE TENSIONS FOUND TO BE WITHIN SERVICE BULLETIN LIM ITS. CLUTCH ENGAGEMENT AT .063 IN. GREASE AND OIL CLEANED FROM CLUTCH PLATES. RETURN SPRING REPLACED. ALL WORK PERFO RMED IN ACCORDANCE WITH DEHAVILLAND SERVICE BULLETIN 8-27-79 AND DASH 8 MAINTENANCE MANUAL 27-16-00. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091700184 20010917 00184 NM 2001 9 17 PCAA0109106 1 20010829 A 7110 RIVET DHAV DHC8 DHC8102 2809003 NM RT COWL LOOSE A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 806EX 26259 263 DURING FLEET INSPECTION FOR NACELLE RIVETS BEING LOOSE AND MISSING, RIGHT OUTBOARD ENGINE COWL JUST BELOW FLAP TRACKS FO UND TO HAVE LOOSE RIVETS. RIVETS REPLACED IN ACCORDANCE WITH DER CALLAHAN REPAIR SERVICES 8110 FORM CAS-AAL09-REV B. A IRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091700186 20010917 00186 NM 2001 9 17 PCAA0109109 1 20010906 A 7110 RIVET DHAV DHC8 DHC8102 2809003 NM RT COWL LOOSE A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 816EX 24075 329 DURING FLEET INSPECTION OF NACELLES FOR LOOSE AND MISSING RIVETS SEVERAL RIVETS FOUND LOOSE ON RIGHT COWLING OUTBOARD EN D UNDER FLAP TRACK. RIVETS REPLACED ON RIGHT ENGINE COWL IN ACCORDANCE WITH DER CALLAHAN REPAIR SERVICES 8110 FORM CAS- AAL-09 REVISION B. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091700188 20010917 00188 SW 2001 9 17 PNSA010507 1 20010530 A 7712 CONNECTOR SWRNGN SA227 SA227AC 8780603 SW TORQUE INDICATOR DIRTY A PNSA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 AL 03 640PA AC759B TORQUE INDICATION ERRATIC ON TAKEOFF RUN. ABORTED TAKEOFF. RETURNED TO BLOCK. CLEANED CANNON PLUG FOR TORQUE INDICATI ON SYSTEM. OPERATIONAL CHECK OK. 2 L 7 2 4T RT A8SW 2001091700189 20010917 00189 NM 2001 9 17 AUS20010822 1 20010802 A 3244 7824 TIRE BOEING 737 7373Q8 1384670 NM CFMINT CFM56 CFM563C 13802 EU MLG SEPARATED W C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 AU S 373 (AUS) LT MAIN LANDING GEAR OUTBOARD TIRE (NR 1) TREAD SEPARATED. SECONDARY DAMAGE CAUSED TO TRAILING EDGE FLAPS, WING TR AILING EDGE PANELS AND LT UNDERCARRIAGE DOOR WHICH WAS PARTIALLY MISSING. AIRCRAFT WAS OPERATED BY AIR VANUATU AND WAS R EGISTEREDYJAV18. 2 L 7 2 4F 4 F RT A16WE E21EU 2001091700190 20010917 00190 SW 2001 9 17 PNSA010705 1 20010722 A 5230 ROD SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR OUT OF ADJ A PNSA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 2708D AC709B BOTH CARGO DOOR LIGHTS ILLUMINATED AFTER TAKEOFF CLIMBING THROUGH 500 FEET. CIRCLED AND DUMPED FUEL AND RETURNED TO ANC . MAINTENANCE FOUND UNSECURED BAG SHIFTED DURING TAKEOFF AND MOVED INSIDE DOOR HANDLE SLIGHTLY, ALSO FOUND UPPER AFT CL ICK CLACK ROD NOT ADJUSTED PROPERLY. ADJUSTED PER MAINTENANCE MANUAL AND OP CHECKED DOOR WARNING SYSTEM OK. 2 L 7 2 4T RT A8SW 2001091700194 20010917 00194 SW 2001 9 17 PNSA010706 1 20010725 A 2821 FUEL FILTER SWRNGN SA227 SA227AC 8780603 SW FUEL SYS OBSTRUCTED A PNSA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 AL 03 650PA AC775B ON PRE-START CHECK LIST FOUND NO FUEL PRESSURE INDICATION WITH RT MAIN OR AUX FUEL BOOST PUMP ON. MAINTENANCE REMOVED D EBRIS FROM FUEL FILTER ORIFICE TO FUEL PRESSURE LINE AND OP CHECK OK. 2 L 7 2 4T RT A8SW 2001091700196 20010917 00196 EU 2001 9 17 AUS20010835 1 20010801 A 5311 FASTENER BAG BAE146 BAE146100A 1500260 EU LYC ALF502 ALF502R3A 41580 NE FUSELAGE CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) DURING INSPECTION FOR LOCATION OF CENTRE FUEL TANK LEAK THE FOLLOWING DEFECTS WERE FOUND: 1. FRAME 29 LT HAND UPPE R SIDE (AFT WING ATTACHMENTS) FASTENER IN POSITION NR 11 FOUND WITH SHEARED HEAD 2. FRAME 29 RIGHT HAND UPPER SIDE (AFT WING ATTACHMENT) FASTENER IN POSITION NR 11 FOUND CORRODED 2 H 7 4 4F 4 F RT A49EU E6NE 2001091700198 20010917 00198 2001 9 17 PNSA010708 4 20010727 A 6122 GOVERNOR SWRNGN SA227 SA227AC 8780603 SW LT ENGINE OUT OF ADJ A PNSA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 AL 03 2719H AC709B LT ENGINE PROP GOVERNOR WOULD NOT RESET BELOW 95.5 PERCENT DURING TAXI TEST. MAINTENANCE ADJUSTED PROP GOVERNOR LOW STO P AND CLEANED GOVERNOR SHAFT GROUND CHECK OK. 2 L 7 2 4T RT A8SW 2001091700200 20010917 00200 WP 2001 9 17 PNSA010709 2 20010715 A 7250 8964943 SEAL SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP LT ENGINE LEAKING A PNSA K NONE K FLUID LOSS LD LANDING 1 AL 03 2719H AC713B P44311 ON LANDING IN CDB WHEN REVERSE SELECTED LT ENGINE OIL PRESSURE FLUCTUATED. CDB MAINTENANCE FOUND OIL LEVEL LOW AND SERV ICED. GROUND RAN ENGINE WITH NO APPARENT OIL LEAKAGE. AIRCRAFT WAS FERRIED TO ANC FOR FURTHER INVESTIGATION. ANC MAIN TENANCE FOUND OIL LOW AND OIL SEAL TO REAR TURBINE BEARING LEAKING AND OIL BEING BURNT IN TAIL PIPE. ENGINE WAS REMOVED DUE TO REAR TURBINE BEARING OIL STARVATION. 2 L 7 2 4T 4 T RT A8SW E4WE 2001091700201 20010917 00201 SW 2001 9 17 PNSA010801 1 20010810 A 2432 WARNING LIGHT SWRNGN SA227 SA227AC 8780603 SW COCKPIT ILLUMINATED A PNSA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 AL 03 640PA AC759B BATTERY FAULT LIGHT ON TAKEOFF ROLL. ABORTED TAKEOFF, RESET BATTERIES, DEPARTED. 2 L 7 2 4T RT A8SW 2001091700203 20010917 00203 SW 2001 9 17 PNSA010802 1 20010828 A 3244 TIRE SWRNGN SA227 SA227AC 8780603 SW LT MLG SEPARATED A PNSA A UNSCHED LANDING E VIBRATION/BUFFET TO TAKEOFF 1 AL 03 41NE AC741B DURING DEPARTURE OUT OF DILLINGHAM FELT A SHUDDER AFTER V1 CONTINUED CLIMB, COMPANY CALLED TO INFORM US OF TIRE PARTS ON THE RUNWAY. DETERMINED THAT THE AIRCRAFT TIRE WAS DAMAGED. RETURNED TO ANCHORAGE, DECLARED AN EMERGENCY LANDING IN AN C. LEFT INBOARD MAIN TIRE LOST IT'S TREAD AND BRAKES WERE INOP. 2 L 7 2 4T RT A8SW 2001091700204 20010917 00204 EA 2001 9 17 COMA0160716 1 20010915 A 2611 473052 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY FAULTY A COMA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 719CA 13351 5968 7253 FLIGHT 5068. DURING CRUISE FLIGHT RECEIVED A CARGO SMOKE CAUTION MESSAGE, CREW DECLARED AN EMERGENCY, DISCHARGED THE CA RGO FIRE EXTINGUISHING BOTTLE AND RETURNED TO THE FIELD SAFELY. REPLACED DEFECTIVE CARGO SMOKE DETECTOR. 2 L 7 2 4F RT A21EA 2001091700205 20010917 00205 NM 2001 9 17 AUS20010841 1 20010803 A 2530 3510004403 COFFEEMAKER BOEING 767 767330 NM RROYCE RB211 RB211524* NE GALLEY SHORTED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AU S (AUS) CENTRE GALLEY NR 3 BEVERAGE MAKER TEMPERATURE SENSOR SHORT CIRCUIT 2 L 7 2 4F 4 F RT A1NM E12EU 2001091700206 20010917 00206 EA 2001 9 17 COMA0160717 1 20010915 A 2760 270003 PCU CNDAIR CL600 CL6002B19 EA RT WING FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 981CA 19077 7163 FLIGHT #5323. DURING TAXI OUT WHILE PERFORMING FLIGHT CONTROL CHECK RECEIVED A SPOILERON FAULT STATUS MESSAGE, AIRCRAFT RETURNED TO THE GATE.REPLACED THE RIGHT OUTBOARD SPOILER POWER CONTROL UNIT. 2 L 7 2 4F RT A21EA 2001091700209 20010917 00209 EA 2001 9 17 COMA0160718 1 20010914 A 2760 270003 PCU CNDAIR CL600 CL6002B19 EA LEFT WING FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 933CA 16955 7040 FLIGHT #5395. DURING TAXI OUT WHILE PERFORMING FLIGHT CONTROL CHECK RECEIVED A FLIGHT SPOILER FAULT STATUS MESSAGE, AIRC RAFT RETURNED TO THE GATE.REPLACED THE LEFT OUTBOARD POWER CONTROL UNIT. 2 L 7 2 4F RT A21EA 2001091700211 20010917 00211 EA 2001 9 17 COMA0160719 1 20010913 A 2410 755469D IDG CNDAIR CL600 CL6002B19 EA LEFT ENGINE FAULTY A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 815CA 2557 7397 FLIGHT #5098. ABORTED TAKE OFF AT 50KTS DUE TO #1 IDG CAUTION MESSAGE, AIRCRAFT RETURNED TO THE GATE.REPLACED THE #1 IT EGRATED DRIVE GENERATOR. 2 L 7 2 4F RT A21EA 2001091700212 20010917 00212 2001 9 17 AUS20010847 4 20010805 A 2210 SC47003AMDTD ACTUATOR AIRBUS 320 A320* EU CFMINT CFM56 CFM565A1 NE AUTOPILOT SYSTEM LEAKING W O OTHER K FLUID LOSS DE DESCENT 1 AU S 34 (AUS) LT YAW DAMPER ACTUATOR LEAKING. 2 L 7 2 4F 4 F RT A46NM E29NE 2001091700213 20010917 00213 EU 2001 9 17 PNSA010803 1 20010802 A 7722 4078T09P02 ITT TRIMMER SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE FAILED A PNSA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 AL 03 675PA 340B206 785539 ABORTED T/O AT AKN DUE TO ERRATIC ITT INDICATION ON LT ENGINE. NO FAULT FOUND AT LINE STATION AIRCRAFT FERRIED BACK TO ANC MAIN MAINTENANCE STATION. ITT TRIMMER WAS FOUND BAD WHEN HEAT AND VIBRATION APPLIED. 2 L 7 2 4T 4 T RT A52EU E8NE 2001091700216 20010917 00216 2001 9 17 COMA0160721 4 20010913 A 3418 PITOT LINE CNDAIR CL600 CL6002B19 EA A COMA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SO 01 959CA 7116 FLIGHT #5680. DURING CLIMB OUT OF CVG RECEIVED A STALL FAIL CAUTION MESSAGE ACCOMPANIED WITH STICK SHAKER AND LOW AIRSP EED INDICATION ON CO-PILOTS SIDE, AIRCRAFT RETUREND TO THE FIELD.PURGED WATER FROM THE #1 AND #2 STANDBY PITOT STATIC SY STEM. 2 L 7 2 4F RT A21EA 2001091700218 20010917 00218 EA 2001 9 17 PNSA010804 2 20010821 A 8530 ROCKER BOSS PIPER PA32 PA32301 7103207 SO LYC O540 IO540K1G5 41532 EA NR 2 CYLINDER CRACKED E PNSA K NONE O OTHER TX TAXI/GRND HDL 1 AL 03 8470Y 328206012 L1743548A DURING ENGINE START UNUSUAL SOUND WAS HEARD. MAINTENANCE CONTACTED AND FOUND NR 2 CYLINDER ROCKER ARM SHAFT BOSS CRACKE D. CYLINDER REPLACED AND ENGINE OP CHECK GOOD. 1 L 7 1 3O 3 O A3SO 1E4 2001091700220 20010917 00220 SO 2001 9 17 AUS20010854 1 20010806 A 2750 CONTROL UNIT EMB 120 EMB120 3260201 SO PWA 118 PW118A NE HAMSTD 14SF 14SF9 NE TE FLAPS FAULTY W C ABORTED TAKEOFF F N FLT CONT AFFECTED FALSE WARNING TO TAKEOFF 1 AU S (AUS) FLAP DISAGEEMENT ON RETRACTION. FLAP OPERATING SYSTEM INSPECTED AND NIL FAULT FOUND. 2 L 7 2 4T 4 T RT A31SO E20NE 6 N P11NE 2001091700221 20010917 00221 SW 2001 9 17 PNSA070102 1 20010725 A 2611 CONNECTOR FRCHLD SA227 SA227DC 3377521 SW SMOKE DETECTOR DIRTY A PNSA O OTHER N FALSE WARNING CL CLIMB 1 AL 03 30135 DC890B LAV SMOKE DETECTOR LIGHT CAME ON PASSING THRU 14,000 FEET, COPILOT VISUALLY CHECKED LAV NO SMOKE DETECTED. MAINTENANCE CONTACTED AND SYSTEM DEFERRED PER MEL 26-4. SMOKE DETECTOR CANNON PLUG CLEANED AND RESECURED AT RETURN OF FLIGHT DAY. O P CHECK OK. 2 L 7 2 4T RT A18SW 2001091800090 20010918 00090 EA 2001 9 18 COMA0160720 1 20010913 A 2760 4916405 ECU CNDAIR CL600 CL6002B19 EA E/E BAY FAULTY A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 912CA 7787 470 7011 FLIGHT 5241. DURING TAKEOFF ROLL RECEIVED A CONFIGURATION SPOILER MESSAGE. TAKEOFF WAS ABORTED AT 50 KTS AND RETURNED TO THE GATE. REPLACED THE SPOILER ELECTRONIC CONTROL UNIT. 2 L 7 2 4F RT A21EA 2001091700225 20010917 00225 NM 2001 9 17 SCNA01341 1 20010804 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 282SC 22558 DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON THE MAIN CABIN FLOORBEAM TEE CAP AT STA 1030 BL 0 TO LBL 10. REMOVED CORROSION IAW B727 SRM 511006. REMOVED DAMAGED AREA IAW B727 SRM 531008. FABRICATED 1 EACH TEE CAP, 1 EACH ANGLE, 1 EACH STRAP AND 1 EACH STRAP IAW B727 SRM 531008. INSTALLED IAW B727 SRM 531008 AND 513002. 2 L 7 3 4F A3WE 2001091700227 20010917 00227 NM 2001 9 17 SCNA01342 1 20010807 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 282SC 22558 DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON FLOORBEAM AT STA 1110 LBL 12 THROUGH RBL 24. R EMOVED CORROSION IAW B727 SRM 511006. REMOVED DAMAGED AREA, FABRICATED 1 EACH TEE CAP, 1 EACH ANGLE, 1 EACH ANGLE, 1 EA CH STRAP AND 1 EACH STRAP IAW B727 SRM 531008. INSTALLED IAW B727 SRM 531008 AND 513002. 2 L 7 3 4F A3WE 2001091700230 20010917 00230 EU 2001 9 17 QXEA0101511 1 20010913 A 3350 6008905 POWER SUPPLY FOKKER F28 F28MK4000 4990810 EU DISCHARGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 2918 11156 PDX - NUMBER 4 CABIN EMERGENCY BATTERY PACK IS WEAK. REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECK IS GOOD. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001091700231 20010917 00231 NM 2001 9 17 SCNA01344 1 20010807 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM FUSELAGE CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 282SC 22558 DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON THE SEAT TRACK AT STA 1090 THROUGH 1110 RBL 24. REMOVED CORROSION IAW B727 SRM 511006. REMOVED DAMAGED AREA IAW B727 SRM 513002. FABRICATED NEW SEAT TRACK PER SAMPL E. INSTALLED IAW B727 SRM 513002. 2 L 7 3 4F A3WE 2001091700233 20010917 00233 NM 2001 9 17 SCNA01345 1 20010807 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM FUSELAGE CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 282SC 22558 DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON THE SEAT TRACK AT STA 1070 THROUGH 1110 LBL 24. REMOVED CORROSION IAW B727 SRM 511006. REMOVED DAMAGED AREA IAW B727 SRM 513002. FABRICATED NEW SEAT TRACK PER SAMPL E. INSTALLED IAW B727 SRM 513002. 2 L 7 3 4F A3WE 2001091700234 20010917 00234 NM 2001 9 17 SCNA01346 1 20010807 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM FUSELAGE CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 282SC 22558 DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON THE SEAT TRACK AT STA 1070 THOUGH 1090 LBL 48. REMOVED CORROSION IAW B727 SRM 511006. REMOVED DAMAGED SECTION IAW B727 SRM 513002. FABRICATED NEW SEAT TRACK SECTION PER SAMPLE. INSTALLED IAW B727 SRM 513002. 2 L 7 3 4F A3WE 2001091700235 20010917 00235 NM 2001 9 17 SCNA01347 1 20010807 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM FUSELAGE CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 282SC 22558 DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON THE SEAT TRACK AT STA 4380 TO 480 RBL 24. REMO VED CORROSION IAW B727 SRM 511006. REMOVED DAMAGED AREA IAW B727 513002. FABRICATED NEW SEAT TRACK PER SAMPLE. INSTAL LED IAW B727 SRM 513002. 2 L 7 3 4F A3WE 2001091700236 20010917 00236 NM 2001 9 17 SCNA01348 1 20010807 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM FUSELAGE CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 282SC 22558 DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON THE SEAT TRACK AT STA 344 TO 480 RBL 42. REMOV ED CORROSION IAW B727 SRM 511006. REMOVED DAMAGED AREA IAW B727 SRM 513002. FABRICATED NEW SEAT TRACK PER SAMPLE. INST ALLED IAW B727 SRM 513002. 2 L 7 3 4F A3WE 2001091700237 20010917 00237 NM 2001 9 17 SCNA01349 1 20010809 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM FUSELAGE CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 282SC 22558 DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON THE SEAT TRACK AT STA 1020 TO 1060 LBL 36. REM OVED CORROSION IAW B727 SRM 511006. REMOVED DAMAGED AREA IAW B727 SRM 513002. FABRICATED NEW SEAT TRACK PER SAMPLE. I NSTALLED IAW B727 SRM 513002. 2 L 7 3 4F A3WE 2001091700238 20010917 00238 NM 2001 9 17 SCNA01350 1 20010809 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 282SC 22558 DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON THE FLOORBEAM UPPER TEE CAP AT STA 1060 LBL 66. REMOVED CORROSION IAW B727SRM 511006. REMOVED DAMAGED AREA IAW B727 SRM 531008. FABRICATED 1 EACH ANGLE, 1 EACH ANGL E AND 1 EACH FILLER IAW B727 SRM 531008. INSTALLED IAW B727 SRM 531008 AND 513002. 2 L 7 3 4F A3WE 2001091700239 20010917 00239 NM 2001 9 17 SCNA01351 1 20010808 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 282SC 22558 DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON THE FLOORBEAM TEE CAP AT BS 360 LBL 18 TO RBL 1 8. REMOVED CORROSION IAW B727 SRM 511006. REMOVED DAMAGED AREA IAW B727 SRM 531008. FABRICATED TEE CAP, ANGLE AND STR AP REPAIR IAW B727 SRM 531008. INSTALLED IAW B727 SRM 513002 AND 531008. 2 L 7 3 4F A3WE 2001091700240 20010917 00240 NM 2001 9 17 SCNA01352 1 20010809 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM FUSELAGE CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 282SC 22558 DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON THE SEAT TRACK AT STA 1020 TO 1028 LBL 56. REM OVED CORROSION IAW B727 SRM 511006. REMOVED DAMAGED AREA IAW B727 SRM 513002. FABRICATED NEW SEAT TRACK PER SAMPLE. I NSTALLED IAW B727 SRM 513002. 2 L 7 3 4F A3WE 2001091700241 20010917 00241 NM 2001 9 17 SCNA01708 1 20010821 A 2612 WARNING HORN BOEING 727 7272K3 138400D NM NLG WW INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 291SC 22770 NOSE WHEEL WELL APU FIRE WARNING HORN INOPERATIVE. REPLACEMENT OF THE NOSE WHEEL WELL APU FIRE WARNING HORN. 2 L 7 3 4F RT A3WE 2001091700242 20010917 00242 NM 2001 9 17 SCNA01709 1 20010812 A 2612 WARNING SYSTEM BOEING 727 7272J4 1384006 NM COCKPIT MALFUNCTIONED A SCNA E ENGINE SHUTDOWN N FALSE WARNING TX TAXI/GRND HDL 1 GL 15 290SC 20764 NR 1 ENGINE FIRE LIGHT AND WARNING BELL COME ON AT THE BEGINNING OF TAXI, AND REMAINED ILLUMINATED AFTER ENGINE SHUTDOWN . PROBLEM COULD NOT BE DUPLICATED BY MAINTENANCE. 2 L 7 3 4F RT A3WE 2001091700243 20010917 00243 NM 2001 9 17 SCNA01710 1 20010816 A 2611 SMOKE DETECTOR BOEING 727 727259 138408J NM LAVATORY INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 LEFT HAND AFT LAVATORY SMOKE DETECTOR INOPERATIVE. REMOVED AND REPLACED SMOKE DETECTOR. 2 L 7 3 4F A3WE 2001091700244 20010917 00244 EU 2001 9 17 XN0A01021 1 20010906 A 3150 WARNING SYSTEM AIRBUS 300 A300B4203 3930306 EU COCKPIT MALFUNCTIONED A TC8A C ABORTED TAKEOFF N FALSE WARNING TX TAXI/GRND HDL 1 GL 23 371PC 157 ON TAKEOFF ROLL, CONFIGURATION LIGHT CAME ON MWP, ABORTED TAKE OFF. PERFORM OPS ON KRUEGER AND NOTCH POSITION UNIT. NO DEFECTS NOTED. OPS GOOD ON LOW SPEED AILERON IAW A300 AMM 27-84-00. 2 L 7 2 4F RT A35EU 2001091700245 20010917 00245 EU 2001 9 17 XNA01010 1 20010516 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU MAIN CARGO BAY MALFUNCTIONED A TC8A D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 23 371PC 157 MAIN DECK CARGO SMOKE INDICATIONS AND WARNING DURING TAXI. NO SMOKE NOTED. PERFORMED GROUND OPERATIONS CHECK OF SMOKE DETECTION SYSTEM IAW A300 MM 26-04-00. NO DEFECTS NOTED. 2 L 7 2 4F RT A35EU 2001091700246 20010917 00246 EU 2001 9 17 XNA01011 1 20010608 A 2433 TRANSFORMER AIRBUS 300 A300B4203 3930306 EU E/E BAY FAILED A TC8A H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 23 370PC 134 DURING PREFLIGHT SMOKE STARTED COMING FROM AVIONICS BAY. VERIFIED NR TR2 AT FAULT. DEACTIVATED NR TR2 IAW A300 MEL 24- 25-03 CAT-B. SP 24-25-03 COMPLIED WITH. TRANSFERRED TO DMI 1319. 2 L 7 2 4F RT A35EU 2001091700247 20010917 00247 EU 2001 9 17 XNA01011A 1 20010608 A 2710 INDICATOR AIRBUS 300 A300B4203 3930306 EU COCKPIT FAULTY A TC8A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 473AS 203 DURING CONTROL CHECK, LT&RT AIL INDICATORS SHOWED LESS THAN FULL THROW. MEASURED LT & RT LS & AS AILERONS FOR PROPER DE FLECTION UP AND DOWN. CHECKED NORMAL IAW A300 MM 27-11-00. REMOVED BIRD NESTS FROM LT AND RT LS AILERON ACCESS PANEL. REMOVED AND REPLACED CONTROL SURFACE INDICATOR. OPS CHECK NORMAL IAW A300 MM 27-15-00. 2 L 7 2 4F RT A35EU 2001091700248 20010917 00248 EU 2001 9 17 XNA01012A 1 20010612 A 2910 HYDRAULIC SYSTEM AIRBUS 300 A300B4203 3930306 EU YELLOW SYS LOW A TC8A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 370PC 134 DURING TAXI YELLOW SYSTEM HYDRAULICS DROP TO CAUTION ZONE. SERVICED YELLOW SYSTEM HYDRAULICS AS REQUIRED. OPS CHECK NO RMAL IAW AMM CHAPTER 12. 2 L 7 2 4F RT A35EU 2001091700249 20010917 00249 EU 2001 9 17 XNA01012B 1 20010621 A 2781 WARNING LIGHT AIRBUS 300 A300B4203 3930306 EU COCKPIT ILLUMINATED A TC8A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 472AS 125 KRUEGER LIGHT FLASHING AND CONFIGURATION HORN/FLAPS O-SLATS 16. TRANSFERRED TO DMI LIST PER ENA A300 MEL 27-84-02. DMI 1352 PLACARDS INSTALLED. SP 27-84-02 COMPLIED WITH IAW A300 MM 27-00-00. RIGHT WING KRUEGER AND NOTCH FLAP DEACTIVATE D. 2 L 7 2 4F RT A35EU 2001091700250 20010917 00250 EU 2001 9 17 XNA01012C 1 20010626 A 3411 PITOT TUBE AIRBUS 300 A300B4203 3930306 EU PITOT/STATIC SYS OBSTRUCTED A TC8A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 474AS 219 NO AIRSPEED INDICATION ON F/O SIDE ON 100 KT CHECK. REMOVED DEBRIS FROM F/O PITOT TUBE. OPS CHECK GOOD IAW 34-11-40. 2 L 7 2 4F RT A35EU 2001091700251 20010917 00251 NM 2001 9 17 XNA01012D 1 20010629 A 8012 START VALVE BOEING 727 727227 1384078 NM NR 3 ENGINE FAILED A TC8A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 793A 20774 ENGINE NR 3 STARTER SW STARTER VALVE FAILED TO OPEN. TESTER IN MANUAL. VALVE NR 3 ENGINE DEFERRED AS PER MEL 80-3. TR ANSFERRED TO DMI 1373. 2 L 7 3 4F A3WE 2001091700252 20010917 00252 NM 2001 9 17 XNA01012E 1 20010703 A 2751 CONTROL PANEL BOEING 727 727227 1384078 NM T/E FLAP CONTAMINATED A TC8A A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 23 793A 20774 DURING CLIMB AFTER DEPARTURE, DEVELOPED ASYMMETRICAL INBOARD FLAPS. FOUND EXCESSIVE WATER CONTENT IN INBOARD AND OUTBOA RD TRAILING EDGE FLAP POSITION TRANSMITTER C/P. CLEANED AND RESECURED TRANSMITTER C/P'S. REACTIVATED FLAPS AFTER CREW LOCK OUT. SYSTEM OPS CHECK NORMAL IAW B727 MM 27-51-00. 2 L 7 3 4F A3WE 2001091700253 20010917 00253 NM 2001 9 17 XNA01012F 1 20010708 A 2751 INDICATOR BOEING 727 727227 1384078 NM COCKPIT FAULTY A TC8A D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 23 793A 20774 ON TAXI OUT FLAPS INDICATED SPLIT AND ASYMMETRICAL SETTING. REMOVED AND REPLACED I/B FLAP POSITION INDICATOR. OPS CHEC KS GOOD IAW 27-52-0 B727 MM. 2 L 7 3 4F A3WE 2001091700254 20010917 00254 EU 2001 9 17 XNA01012G 1 20010711 A 5270 WARNING SYSTEM AIRBUS 300 A300B4203 3930306 EU COCKPIT MALFUNCTIONED A TC8A D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 23 474AS 219 BULK LIGHT DOOR LIGHT ILLUMINATED AFTER TAXI. CYCLED BULK PIT DOOR SEVERAL TIMES. OPS CHECK NORMAL IAW A300 MM 52-71-0 0. 2 L 7 2 4F RT A35EU 2001091700255 20010917 00255 EU 2001 9 17 XNA01013 1 20010717 A 5270 WARNING LIGHT AIRBUS 300 A300B4203 3930306 EU COCKPIT ILLUMINATED A TC8A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 473AS 203 CLIMBING THRU 13,000 FEET HEARD LOUD BANGING NOISE FROM CARGO SECTION FOLLOWED BY FLAPPING NOISE COMING FROM AIR CONDITI ONING DUCTS. DOORS LIGHT CAME ON, ON MASTER WARNING PANEL ONLY. INSPECTED FREIGHT IN MAIN CARGO COMPARTMENT, FWD, MID AND BULK CARGO COMPARTMENTS. NO SHIFTED LOADS NOTED, ALL CARGO SECURED. INSPECTED NR 1 & 2 AIR CONDITIONING DUCTING, N O DEFECTS NOTED. INSPECTED NR 1 & NR 2 PACKS FOR ICING, FOUND NR 1 HAD WATER, DRAINED AND CHANGED BAG. OPS CHECK NORMA L IAW A300 MM 21-51-00. CYCLED FWD, MID, AFT CARGO DOORS. OPS CHECK NORMAL IAW A300 MM 52-71-00. 2 L 7 2 4F RT A35EU 2001091700256 20010917 00256 EU 2001 9 17 XNA01014 1 20010725 A 2781 WARNING LIGHT AIRBUS 300 A300B4203 3930306 EU COCKPIT ILLUMINATED A TC8A D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 472AS 125 ON TAXI, KRUEGER LIGHT FLASHING AND CONFIG LIGHT ON MWP. TRANSFERRED TO DMI 1421 IAW 27-84-01. DEACTIVATED LEFT NOTCH AND KRUEGER IAW SP 27-84-02. PLACARDS INSTALLED. 2 L 7 2 4F RT A35EU 2001091700257 20010917 00257 EU 2001 9 17 XNA01015 1 20010728 A 2782 JACKSCREW AIRBUS 300 A300B4203 3930306 EU L/E SLAT LACK OF LUBE A TC8A D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 GL 23 473AS 203 DURING TAXI, NO SLATS INDICATION ON THE FCPI. SERVICED SLAT JACKSCREW AT LEFT WING ROOT. OPS CHECK GOOD IAW A300 MM 27 -80. 2 L 7 2 4F RT A35EU 2001091700258 20010917 00258 NE 2001 9 17 XNA01016 2 20010801 A 7200 ENGINE BOEING 727 727227 1384078 NM PWA JT8 JT8D7B 52053 NE NR 2 OVERTEMP A TC8A E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 23 793A 20774 657736 NR 2 OIL TEMP GAUGE INDICATED 130 DEGREES. PERFORMED PRECAUTIONARY ENGINE SHUT DOWN AS PER CHECK LIST. 2 L 7 3 4F 4 F A3WE E2EA 2001091700259 20010917 00259 2001 9 17 XNA01018 4 20010821 A 2210 DAMPER BOEING 727 72722C 138400F NM AUTOPILOT SYS DEFECTIVE A TC8A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 792A 19195 LOWER YAW DAMPER POPS C/B. TRANSFERRED TO DMI 1462 IAW EWA B727 MEL 22-6 CAT-C. A/P CONSIDERED INOP. 2 L 7 3 4F A3WE 2001091700260 20010917 00260 EU 2001 9 17 XNA01020 1 20010824 A 7722 CONNECTOR AIRBUS 300 A300B4203 3930306 EU EGT INDICATOR DISCONNECTED A TC8A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 373PC 218 RTB DUE NR 1 EGT INDICATOR FELL TO ZERO DURING TAXI (BOTH ANALOG & DIGITAL INDICATORS). RESET CANNON PLUG ON NR 1 EGT I NDICATOR. SYSTEM OPS CHECKS GOOD IAW AMM 77-21-00. 2 L 7 2 4F RT A35EU 2001091700263 20010917 00263 NM 2001 9 17 OZIA013125002 1 20010310 A 3350 321430 BATTERY DORNER DO32 DO328300 NM CABIN WILL NOT TEST A OZIA K NONE L NO TEST IN INSP/MAINT 1 CE 05 410Z 686 3125 EMERGENCY LIGHTS WOULD NOT TEST. REPOSITIONED 7LK BATTERY TO 6LK AND 6LK BATTERY TO 7LK FOR TROUBLESHOOTING. OPS CHECK GOOD. LEFT COMPONENTS INSTALLED AS REPOSITIONED. 2 H 7 2 4T RT A55NM 2001091700264 20010917 00264 NM 2001 9 17 2001F00271 1 20010723 A 7110 83014H39643 LATCH BOEING 727 7272J7 138400E NM NR 2 ENGINE BROKEN A ULHF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 553NA 20707 FLT 1 - FLL - ON DEPARTURE CLIMB-OUT, NR 2 ENGINE ACCESS DOOR ILLUMINATED. AIRCRAFT RETURNED TO FLL. INSPECTED AND FOU ND BROKEN LATCH ON NR 2 ENGINE ACCESS DOOR. REMOVED AND REPLACED LATCH ASSEMBLY PER MM 71-10-00. OPERATION CHECKED NOR MAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001091700265 20010917 00265 NE 2001 9 17 2001F00272 2 20010723 A 7532 658385 CONTROL VALVE BOEING 727 7272J7 138400E NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE FAILED A ULHF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 23 553NA 20707 ON FLT 748 - FPO-CVG - TAKEOFF ROLL, NR 2 ENGINE STALLED DURING ACCELERATION THROUGH 70 KTS. PARAMETERS WERE OBSERVED T O RECOVER TO NORMAL. HOWEVER, NR 2 ENGINE ACCESS DOOR LIGHT ILLUMINATED, TAKEOFF ABORTED. REMOVED AND REPLACED NR 2 PR BC VALVE, OPERATION CHECKED NORMAL IAW MM 75-31-11. AIRCRAFT RETURNED TO NORMAL SERVICE. (M) 2 L 7 3 4F 4 F A3WE E2EA 2001091700266 20010917 00266 NE 2001 9 17 2001F00273 3 20010614 A 6112 SFA13M1ROAD BOOT DHAV DHC8 DHC8103 1386005 NM HAMSTD 14SF 14SF7 NE LT PROP TORN A IQJA K NONE O OTHER IN INSP/MAINT 1 NM 01 807WP 16069 1430 023 NR 1 PROP NR 2 BLADE HEATING BOOT RIPPED. REMOVED AND REPLACED NR 2 PROP BLADE IAW HAMSTD CMM CH 61-10-00 PAGE 707-711, LEAK AND OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 6 C P7NE 2001091700267 20010917 00267 CE 2001 9 17 2001F00274 1 20010328 A 2612 47790008 CONTROLLER CESSNA 208 208B 2073701 CE FIRE DETECTION DEFECTIVE A HSYA O OTHER N FALSE WARNING CR CRUISE 1 NM 05 751FE 208B0245 FLT 7769 - GTF - PILOT REPORTED 'ENGINE FIRE LIGHT CAME ON DIMLY IN FLIGHT'. NO AURAL WARNING, ONLY PARTIAL DIM LIGHT I NDICATION. INTERNAL MALFUNCTION OF THE FIRE DETECTION CONTROLLER. REMOVED AND REPLACED THE FIRE DETECTION CONTROLLER. PERFORMED FUNCTIONAL CHECK WITH ENGINE RUNNING. OPERATIONAL CHECKED GOOD PER THE C208 MAINTENANCE MANUAL. (M) 1 H 7 1 3T A37CE 2001091700268 20010917 00268 EU 2001 9 17 2001F00275 1 20010514 A 3260 200918206 DOWNLOCK SWITCH STBROS SD3 SD360 8100606 EU RT MLG FAILED A HSYA O OTHER N FALSE WARNING DE DESCENT 1 NM 05 701A SH3627 FLT 7562 - GFK - LEFT CIRCUIT BREAKER NR 38 GEAR WARNING POPPED. RESET CIRCUIT BREAKER, RECEIVED 3 GREEN, DOWN AND LOCK ED INDICATION. AT 500 FT AGL TO LOW GEAR WARNING. DID GO AROUND AND LANDED. RIGHT MAIN LANDING GEAR DOWN LIMIT SWITCH MALFUNCTIONED INTERNAL SHORT CIRCUIT. REMOVED AND REPLACED THE SWITCH, PLACED LANDING GEAR ON DEFERRED MAINTENANCE ITE M LIST PER MEL 32-1-3 CATEGORY 'C' FOR RETRACTION CHECK. (M) 2 H 7 2 4T A41EU 2001091700269 20010917 00269 CE 2001 9 17 2001F00276 1 20010605 A 2613 WARNING LIGHT CESSNA 402 402B 207590P CE COCKPIT ILLUMINATED A X07R E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 03 306 402B0435 RIGHT ENGINE TAIL PIPE ILLUMINATED. ENGINE SHUTDOWN, RETURN TO MKE. (M) 1 L 7 2 3O A7CE 2001091700270 20010917 00270 2001 9 17 2001F00277 4 20010905 A 3442 6225130021 CONTROL UNIT AIRBUS A319 A319132 NM WEATHER RADAR INOPERATIVE A RJEF A UNSCHED LANDING O OTHER CL CLIMB 1 SO 23 474TA 1159 SAL - DURING FLIGHT TA582 - THE CAPTAIN REPORTED WX RADAR INOPERATIVE. THE AIRCRAFT RETURNED TO SAL STATION FOR MAINTEN ANCE. AFTER LANDING MAINTENANCE TECHNICIANS PERFORMED THE FAULT ANALYSIS TO FIND THE CAUSE OF THE REPORT. SEVERAL TASK S WERE PERFORMED IAW AMM 34-41-00-740-002/34-41-00-001-321. THE WX RADAR CONTROL UNIT WAS FOUND INOPERATIVE, AND IT WAS REPLACED ACCORDING TO AMM 34-41-12-00. THE WX'D RADAR SYSTEM WAS TESTED WITH SATISFACTORY RESULTS. THE AIRCRAFT RETUR NED TO NORMAL OPERATION. (M) 2 L 7 2 4F RT A28NM 2001091700271 20010917 00271 SO 2001 9 17 ASOA01139 1 20010818 A 3350 F02A250V1A FUSE EMB 120 EMB120 3260201 SO CABIN BLOWN A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 237AS 120051 DURING GROUND INSPECTION IN ATL, MAINTENANCE FOUND THE RIGHT FUSELAGE FORWARD EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A FUSE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001091700272 20010917 00272 WP 2001 9 17 ZW0A0108603 1 20010915 A 3350 58222 BATTERY PACK DOUG DC9 DC983 3022083 WP AFT CABIN A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9616G 53563 THE AFT CABIN EMERGENCY CEILING LIGHT AT THE AFT AIRSTAIR DOOR WAS INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 8-12 -01 MCI. --CLOSED-- 2 L 7 2 4F RT A6WE 2001091700273 20010917 00273 NM 2001 9 17 AWXA0002263 1 20010910 A 5330 148N321516 SKIN BOEING 757 757225 1384959 NM A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 D: Dent in fuselage skin from STA 1844 to 1862 between STR 23L & 25LC: Trimed out damage and repaired per ER 19-5381-012 48-TB2 2 L 7 2 4F RT A2NM 2001091700274 20010917 00274 EU 2001 9 17 RAIA00109005 1 20010916 A 7931 81071100010 SWITCH AEROSP ATR72 ATR72202 8680940 EU RT ENGINE FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 721TE 803 217 7118-STL-RIGHT ENGINE OIL PRESSURE GAUGE AND LIGHT FLICKERED INTERMITTENTLY. MAINTENANCE INSPECTED AND REPLACED THE RIGH T ENGINE OIL PRESSURE SWITCH. 2 H 7 2 4T RT A53EU 2001091800003 20010918 00003 WP 2001 9 18 AUS20010866 2 20010812 A 7250 TURBINE BLADES GARRTT TPE33112UA SWRNGN SA227 SA227* SW GARRTT TPE331 TPE33112UA 01514 WP MCAULY 4HFR34 4HFR34C652 NE TURBINE SECTION DAMAGED W C ABORTED TAKEOFF E B VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 AU S 3067 (AUS) LT ENGINE INTERNAL FAILURE. TURBINE BLADES AND EXHAUST NOZZLE DAMAGED. 2 L 7 2 4T 4 T RT A5SW E4WE 6 C 3PNE 2001091800011 20010918 00011 NE 2001 9 18 AUS20010883 2 20010814 A 7230 RB211524D19 ENGINE BOEING 747 747338 NM RROYCE RB211 RB211524D419 54555 NE NR 2 VIBRATES W O OTHER E F VIBRATION/BUFFET FLT CONT AFFECTED CR CRUISE 1 AU S 603 (AUS) NR 2 ENGINE VIBRATION EXCESSIVE. 2 L 7 2 4F 4 F RT A20WE E12EU 2001091800012 20010918 00012 GL 2001 9 18 AUS20010884 2 20010813 A 7321 8061865 MEC BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL RT ENGINE FAULTY W O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 AU S (AUS) RT ENGINE MAIN ENGINE CONTROL (MEC) FAULTY. 2 L 7 2 4F 4 F RT A1NM E23EA 2001091800016 20010918 00016 EU 2001 9 18 AUS20010891 1 20010809 A 2910 S4340092002 VALVE AIRBUS 320 A320* EU CFMINT CFM56 CFM565A1 NE HYDRAULIC SYSTEM FRACTURED W O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 AU S 11542 (AUS) YELLOW HYDRAULIC SYSTEM TWO WAY VALVE MOUNTING FLANGE FRACTURED AND VALVE COCKED. LOSS OF HYDRAULIC FLUID. 2 L 7 2 4F 4 F RT A46NM E29NE 2001091800021 20010918 00021 EU 2001 9 18 AUS20010900 1 20010802 A 7722 54285538010 INDICATOR AMD FALC50 FALCON900 2700160 EU GARRTT TFE731 TFE7315R 01518 WP NR 1 ENGINE FAILED W O OTHER E M VIBRATION/BUFFET OVER TEMP NR NOT REPORTED 1 AU S 3068 (AUS) NR 1 ENGINE ITT INDICATOR INTERNAL FAILURE. 2 L 7 3 4F 4 F RT A46EU E6WE 2001091800022 20010918 00022 NM 2001 9 18 AUS20010901 1 20010820 A 3230 69355005 ACTUATOR BOEING 737 7374Y0 1384705 NM CFMINT CFM56 CFM563C 13802 EU MLG FAULTY W O OTHER N FALSE WARNING CL CLIMB 1 AU S (AUS) RT MAIN LANDING GEAR UPLOCK ACTUATOR FAULTY. 2 L 7 2 4F 4 F RT A16WE E21EU 2001091800024 20010918 00024 GL 2001 9 18 ASOA01108S 2 20010713 A 7200 ENGINE AEROSP ATR72 ATR72 EU ALLSN AE300 AE3007A GL RIGHT MAKING METAL A ASOA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 11 643AS 14734 413 FLT 4171 - DURING FLIGHT FROM ATL-GNV - PILOT RECEIVED AN INTERMITTENT OIL PRESSURE LIGHT . PILOT DECLARED AN EMERGENCY AND DIVERTED THE AIRCRAFT TO AYS. AIRCRAFT LANDED IN AYS WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RIGHT ENG INE. THE NR 2 SCAVENGE OIL FILTER WAS FULL OF METAL. THE TEAR DOWN REPORT DID NOT REVEAL THE SOURCE OF THE METAL CONTAM INATION. THE DAMAGE TO THE NR 14 BEARING AND PROPELLER BRAKE COUPLING APPEARS TO BE SECONDARY MECHANICAL DAMAGE AND IND ICATE THAT THE METAL FOUND ON THE CHIP DETECTOR MOST LIKELY ENTERED THE REDUCTION GEAR BOX AT THIS POINT WHERE THE MAJOR ITY OF MECHANICAL DAMAGE WAS FOUND. (M) 2 H 7 2 4T 4 F RT TE6CH 2001091800025 20010918 00025 EU 2001 9 18 ASOA01141 1 20010819 A 3412 102EH2EB PROBE AEROSP ATR72 ATR72 EU TAT SYSTEM FAILED A ASOA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 11 531AS 454 FLT 4171 - DURING CLIMB FROM ATL-GNV, CREW REPORTED A STRONG ELECTRICAL SMELL IN THE COCKPIT. THEN THE F/O'S TAT AND AL PHA PROBE LIGHTS ILLUMINATED WITH ANTI-ICE ON CAP. AIRCRAFT RETURNED AND LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE RIGHT TAT PROBE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT 2001091800026 20010918 00026 EU 2001 9 18 DKAA01018 1 20010718 A 2810 SKIN AMD FALC20 FALCON 2720302 EU CTR FUEL TANK CORRODED A DKAA K NONE O OTHER IN INSP/MAINT 1 GL 23 560RA 20724 56 DURING 12 YEAR CORROSION INSPECTION OF CENTER WING FUEL TANK, CORROSION WAS DISCOVERED WHICH REQUIRED EXCESSIVE REMOVAL OF MATERIAL FROM CENTER TANK LOWER SKIN. DASSAULT ENGINEERING WAS CONTACTED AND PROVIDED CHANGE APPROVAL SHEET R247. T HINNED AREA WAS REPAIRED BY INSTALLING AN EXTERNAL DOUBLER PER ABOVE MENTIONED DOCUMENT. (M) 2 L 7 2 4F A7EU 2001091800027 20010918 00027 WP 2001 9 18 GTIA010816 1 20010815 A 3350 60030431 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 808NK 49504 FLL - EMERGENCY EXIT LIGHT AT LEFT AFT SERVICE DOOR INOPERATIVE, EMERGENCY LIGHTING SYSTEM. FOUND BATTERIES DEAD IN BAT TERY POWER SUPPLY. REMOVED AND REPLACED POWER SUPPLY REF MM 33-53-00 AND WDM 33-51-14. OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 2001091800028 20010918 00028 2001 9 18 GTIA010818 4 20010821 A 2230 CLUTCH DOUG DC9 DC982 3022082 WP AUTOTHRUST SYS LACK OF LUBE A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 812NK 48021 FLT 678 - DTW - AUTOTHROTTLES, LEFT THROTTLE DID NOT RETARD FROM CLIMB POWER SETTING TO CRUISE POWER SETTING TWICE DURIN G CLIMB-OUT. WORKED FINE DURING REST OF FLIGHT. SERVICED AUTO THROTTLE CLUTCH ASSY IAW MD80 MM CH 76-11-04, SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2001091800029 20010918 00029 WP 2001 9 18 GTIA010819 1 20010823 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 809NK 49503 FTW - AFT CARGO COMPARTMENT HAS CORROSION UNDER THE LONGERON LIP AT FS 1231 AT 29L IN TWO PLACES. REMOVED CORROSION IAW MD-80 SRM 51-10-3. FOUND CORROSION OUT OF LIMITS IAW MC-80 SRM 51-10-3. REMOVED LONGERON 29L STATION 1202 STATION 124 0. LONGERON 29L FROM STATION 1202-1240 TO BE INSTALLED BY 05N00176. (M) 2 L 7 2 4F RT A6WE 2001091800030 20010918 00030 WP 2001 9 18 GTIA010820 1 20010626 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 809NK 49503 FTW - AFT CARGO COMPARTMENT HAS CORROSION AT FS 1211 AT 29L UNDER THE CHANNEL. REMOVED CORROSION IAW MD-80 MM SRM 51-10 -3. FOUND OUT CORROSION OUT OF LIMITS. REMOVED LONGERON 29L STATION 1202-1240. LONGERON 29L FROM STATION 1202-1240 TO BE INSTALL BY 05N00176. (M) 2 L 7 2 4F RT A6WE 2001091800031 20010918 00031 WP 2001 9 18 GTIA010821 1 20010626 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 809NK 49503 FTW - AFT CARGO COMP STATION 1003-1022 LONGERON HAS CORROSION 29 LEFT. REMOVED CORROSION IAW MD-80 SRM 51-10-03. CORRO SION REMOVAL FOUND TO OUT OF LIMITS. REMOVED SECTION OF LONGERON 1003 TO 1032 IAW MD-80 SRM. LOCATED AND DRILLED THE N EW LONGERON FABRICATED THE LONGERON SPLICE. INSTALLED LONGERON 29L FROM STATION Y1003 TO STA Y1032 SPLICE AT STATION Y 1030 IAW MD-80 SRM 53-02. (M) 2 L 7 2 4F RT A6WE 2001091800032 20010918 00032 WP 2001 9 18 GTIA010822 1 20010617 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 809NK 49503 FTW - AFT CARGO COMPARTMENT LONGERON NR 29 LEFT SIDE BETWEEN STATION 1193 AND 1212 CORRODED. REMOVED CORROSION AREA VER IFIED OUT OF LIMITS. REMOVED LONGERON 29L FROM STATION Y1183 TO STA Y 1240 AND SPLICE AT STATION 1202 IAW MD-80 SRM 53- 02 AND 51-30. FABRICATED LONGERON 29L FROM STA Y1240 TO STA 1202 IAW DAC DWG 5930627. LOCATED AND DRILLED LONGERON 29L . (M) 2 L 7 2 4F RT A6WE 2001091800033 20010918 00033 SO 2001 9 18 LR7A01078 1 20010915 A 2613 WIRE LKHEED 382 382G 526414U SO FS 486 CORRODED A LR7A E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 AL 03 405LC 5025 DURING DESCENT INTO OKO NR. 4 ENGINE NACELLE OVERHEAT LIGHT ILLUMINATED. NR. 4 ENGINE SHUTDOWN IAW ENGINE SHUTDOWN PROC EDURES (QRH), FIRE EXTINGUISHER DISCHARGED. REPLACED 3 EA. OVERHEAT DETECTORS IAW SMP 581 26-10 PG 206 PARA. 3. (PRECAU TIONARY). FOUND OVERHEAT DETECTOR WIRE CORRODED AT AFT SIDE OF FS 486 FIREWALL CONNECTOR. REPAIRED WIRE. SYSTEM OPS C HECK NORMAL IAW SMP 581 26-10 PG. 202. REPLACED NORMAL FIRE EXTINGUISHER AGENT BOTTLE AND DISCHARGE SQUIB IAW SMP 581 2 6-20 PG 204, 206A - 207. 2 H 7 4 4T A1SO 2001091800034 20010918 00034 WP 2001 9 18 GTIA010824 1 20010626 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 809NK 49503 FTW - AFT CARGO COMP HAS BLENDED AREAS THAT ARE OUT OF LIMITS AT FS 1003-1022, AT LONGERON. MATERIAL LOSS OUT OF LIMITS AT NR 30 LONGERON. REMOVED LONGERON AT STATION 1003 TO 1050 IAW SRM MD-80 51-30-2. INSTALLED NEW SPLICE. (M) 2 L 7 2 4F RT A6WE 2001091800035 20010918 00035 WP 2001 9 18 GTIA010825 1 20010821 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST NR NOT REPORTED 1 GL 23 801NK 48048 DTW - FLT 872 - FLIGHT ATTENDANT STATION C EMERGENCY LIGHT RED LIGHTS INOPERATIVE EXPOSED WIRE. INSTALLED NEW LIGHT BUL B IAW MD80 MM 33-53-01. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2001091800036 20010918 00036 WP 2001 9 18 GTIA010826 1 20010622 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 809NK 49503 FTW - AFT CARGO BAY, HAS CORROSION UNDER THE LONGERON LIP AT FS 1255 AT 29R. REMOVED CORROSION, FOUND TO BE OUT OF LIMI TS. REMOVED CORRODED LONGERON FROM 1231 TO FS 1291. FABRICATED NEW LONGERON SECTION MATERIAL. (M) 2 L 7 2 4F RT A6WE 2001091800037 20010918 00037 WP 2001 9 18 GTIA010827 1 20010625 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 809NK 49503 FTW - AFT LOWER CARGO COMPARTMENT, CORRODED AT STRINGER 29R, STATION 1136 TO STATION 1098. REMOVED CORROSION AT STRINGE R 29R, STATION 1136 TO 1098 CORRODED AREAS FOUND TO BE OUT OF LIMITS. REMOVED LONGERON 29R FROM STATION Y1089 TO STA Y1 136. FABRICATED LONGERON SECTION. (M) 2 L 7 2 4F RT A6WE 2001091800038 20010918 00038 WP 2001 9 18 GTIA010828 1 20010626 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 809NK 49503 FTW - AFT CARGO COMPT HAS CORROSION UNDER THE CHANNEL AT FS 1231-1250 AT 30L. REMOVED CORROSION OF LONGERON CHANNEL AT AFT CARGO COMPARTMENT MATERIAL LOSS FOUND TO BE OUT OF LIMITS. REMOVED LONGERON FROM STATION 1231 TO 1309. SPLICE FOUND CORRODED. LOCATED AND DRILLED LONGERON NR 30 FROM STATION 1231 TO 1309 IAW MD-80 MM 53-02. (M) 2 L 7 2 4F RT A6WE 2001091800039 20010918 00039 WP 2001 9 18 GTIA010829 1 20010624 A 5312 FITTING DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 809NK 49503 FTW - AFT CARGO COMPARTMENT HAS CORROSION ON THE BULKHEAD FITTING AT FS 1336 AT LONGERON NR 30 IN 4 PLACES. REMOVED COR ROSION ON THE BULKHEAD FITTING AT FS 1336 AT LONGERON NR 30 IAW MD-80 SRM 51-10-0. DRILLED AND LOCATED NEW BULKHEAD FIT TING IAW MD-80 MM. INSTALLED NEW BULKHEAD AND FRAME SUPPORT. (M) 2 L 7 2 4F RT A6WE 2001091800040 20010918 00040 WP 2001 9 18 GTIA010830 1 20010621 A 5320 ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 809NK 49503 FTW - AFT CARGO BAY DOOR JAMB BEHIND VERTICAL GILLLINER WALL HAS SEVERE CORROSION AT FS 1121, 4 INCHES ABOVE 23R. FOUND CORROSION TO BE OUT OF LIMITS IAW DC-9. REMOVED ANGLE FROM AFT CARGO DOOR JAMB THAT HAD EXCESSIVE CORROSION IAW DC-9 M D-80 SRM 51-10-03. INSTALLED NEW PART IAW MD-80 SRM 51-30-02. (M) 2 L 7 2 4F RT A6WE 2001091800041 20010918 00041 WP 2001 9 18 GTIA010831 1 20010626 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 809NK 49503 FTW - AFT CARGO COMPARTMENT STATION 1003 TO 1022 LONGERON 29 RIGHT HAS CORROSION. REMOVED CORROSION IAW MD-80 SRM 51-10 -03 CORROSION REMOVAL FOUND TO BE OUT OF LIMITS. REMOVED SECTION OF LONGERON 29R. LOCATED AND DRILLED THE NEW LONGERON . (M) 2 L 7 2 4F RT A6WE 2001091800042 20010918 00042 2001 9 18 GTIA010834 4 20010823 A 3460 4034241972 COMPUTER DOUG DC9 DC982 3022082 WP COCKPIT FAULTY A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 817NK 49141 FLT 1572 - NR 2 DFGC ALT PRE-SELECT BLANK. REMOVED AND REPLACED NR 2 DFGC IAW MD80 MM 22-01-01 RAN RTS TEST MD MM 22-01 -05, ALL OPS CHECK OK. (M) 2 L 7 2 4F A6WE 2001091800043 20010918 00043 WP 2001 9 18 GTIA010837 1 20010828 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 GL 23 800NK 49144 DTW - FOUND EMERGENCY PATH LIGHTING NOT WORKING SEAT ROW 16-30. FOUND BROKEN WIRE AT SEAT 18 DEF. RESECURED BROKEN WIR E, OPS CHECK GOOD IAW MD-80 MM 20-50-01. (M) 2 L 7 2 4F A6WE 2001091800044 20010918 00044 2001 9 18 GTIA010841 4 20010829 A 3460 COMPUTER DOUG DC9 DC982 3022082 WP COCKPIT MALFUNCTIONED A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 812NK 48021 ACY - FLT 138 - SELECTING CLIMB POWER ON TRP AFTER TAKEOFF CAUSED RIGHT THROTTLE TO MOVE BACK TO CORRECT POSITION MANUAL LY WORKED OK REST OF FLIGHT DFGC NR 1. REMOVED NR 1 DFGC CLEANED CONTACTS AND REINSTALLED SAME UNIT PERFORMED RTS CHECK OF NR 1 DFGC IAW MM 22-05-1. GROUND OPS CHECKS GOOD AT THIS TIME. (M) 2 L 7 2 4F A6WE 2001091800045 20010918 00045 EU 2001 9 18 MTNA200111 1 20010914 A 7931 CV3450KT245SNK CONNECTOR FOKKER F27 F27MK500 4990629 EU LOOSE A MTNA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 33 718FE 10470 During climb out from SGF. The left oil pressure gauge dropped to zero then fluctuated between zero and five PSI. The cr ew performed the emergency shut dowm check list, declared an emergency. The crew returned the aircraft to SGF. and lande d with out incident. After checking the connection on the cannon plug and reinstalling the plug the system checked good IAW. The Fokker Maintenance Manual Chapter 77. 2 H 7 2 4T A817 2001091800046 20010918 00046 WP 2001 9 18 GTIA010844 1 20010830 A 3230 HANDLE DOUG DC9 DC983 3022083 WP MLG WW UNSECURE A GTIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 808NK 49504 FLL - FLT 1780 - GEAR WOULD NOT RETRACT AFTER TAKEOFF. BURNED FUEL DOWN, LANDED AT 138,400 TURNED OFF R/W. GEAR DOOR L IGHT CAME ON STOPPED AIRCRAFT CALLED MAINTENANCE. INSPECTED MLG DOOR, FOUND BYPASS HANDLE IN UNSECURED POSITION. WITH HYDRAULICS ON, CYCLED GEAR DOOR (RT) CLOSED, RELEASED HANDLE (GEAR BYPASS) DROPPED DOOR. RESECURED BYPASS HANDLE, RIGHT DOOR CLOSED AND LOCKED NO DAMAGE TO HINGE OR ACTUATOR OR BUMPER FOUND ON VISUAL INSPECTION IAW MD80 MM 32-10-00/32-31/0 0. (M) 2 L 7 2 4F RT A6WE 2001091800047 20010918 00047 WP 2001 9 18 GTIA0823 1 20010624 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 809NK 49503 FOUND MID LOWER CARGO COMPARTMENT CORRODED AT STRINGER 30 STATION 684 DOT 01. REMOVED CORROSION ON STRINGER 30 STATION 674 IAW MD-80 SRM 51-10-3. STRINGER IS OUT OF LIMITS AT STATION 674 IAW MD-80 SRM 51-01-00. REMOVED DAMAGED SECTION OF LONGERON 30 FROM STATION 684 TO 744. FABRICATED LONGERON SPLICE. INSTALLED LONGERON AND LONGERON SPLICE. (M) 2 L 7 2 4F RT A6WE 2001091800048 20010918 00048 EA 2001 9 18 MASA01065 1 20010711 A 2913 887055 PUMP CNDAIR CL600 CL6002B19 EA NR 2 ENGINE FAILED A MASA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 17358 7358 FLT 6334 - BFL-PHX - DECLARED AN INFLIGHT EMERGENCY, THE NR 2 HYDRAULIC SYSTEM LOST QUANTITY. INDICATED 4 PERCENT DURIN G FLIGHT. THE ENGINE PUMP OPERATED AT LOW FLUID FOR 15 MINUTES DURING FLIGHT. MAINTENANCE REPLACED THE NR 2 ENGINE HYD PUMP. OPS CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001091800049 20010918 00049 EA 2001 9 18 NSVA0109 2 20010820 A 7321 FCU BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA LT ENGINE MALFUNCTIONED A NSVA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 EA 27 207CJ UC107 32447 EN ROUTE FROM BOS-BHB, CREW NOTED THE FOLLOWING DISCREPANCY IN FIGHT LOG; LEFT ENGINE PARAMETERS DID NOT CHANGE WITH POW ER LEVER CHANGES. AT THAT TIME THE CREW DECLARED AN IN FLIGHT EMERGENCY AND PRECEDED TO BHB. UPON LANDING ROLL OUT AT BHB, THE CREW NOTICED LEFT ENGINE N1 WAS AT 20 PERCENT. LEFT ENGINE WAS SHUT DOWN BY CREW AS A PRECAUTION. MAINTENANCE REMOVED AND REPLACED THE FUEL LINE, FUEL PUMP AND FUEL CONTROL. OPS CHECK GOOD. (M) 2 L 7 2 4T 4 T RT A24CE E4EA 2001091800050 20010918 00050 EU 2001 9 18 NSVA0110 1 20010901 A 7334 8346 PRESSURE SWITCH SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE NR 1 ENGINE LEAKING A NSVA O OTHER K FLUID LOSS NR NOT REPORTED 1 EA 27 242CJ 340B242 293 PILOT REPORTED FUEL LEAKING OUT OF NR 1 ENGINE DRAIN. MAINTENANCE OPENED COWLING AS NECESSARY OBSERVE FOR LEAKS, DISCON NECTED COMPONENT DRAIN LINES AT OV FUEL FILTER AND PRESSURE DIFFERENTIAL SWITCH WHILE RUNNING BOOST PUMP. ISOLATED LEAK TO FUEL PRESSURE DIFFERENTIAL PRESSURE SWITCH. REMOVED AND REPLACED SWITCH IAW SAAB MM 73-31-05-02. OPERATED BOOST PU MP WITH NO LEAKS. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 2001091800051 20010918 00051 NE 2001 9 18 SIMA200117406 2 20010623 A 7200 ENGINE AEROSP ATR72 ATR72212 EU PWA PW120 PW127 NE NR 2 MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 322AC 320 MIA - FLT 5420 - ON TAKEOFF, ITT ON NR 2 DURING ROLL WAS 765 DEGREES AND CLIMBING. PULLED NR 2 POWER LEVER BACK 6 DEGRE ES TORQUE BEFORE IT STOPPED CLIMBING AT 769. APPLIED POWER MANAGEMENT AT 700 FT AND ITT STARTED DOWN. DIVERTED TO MIA. PERFORMED ENGINE T6 IND SYSTEM INSPECTION AND CHECK IAW 72-01-60. NO DEFECTS NOTED. PERFORMED ENGINE PERFORMANCE REC OVERY WASH IAW JIC 72-00-00. GROUND RUNS CHECKED AND WITH LIMIT IAW 72-00-00. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 2001091800052 20010918 00052 EU 2001 9 18 SIMA200117504 1 20010624 A 5320 S53678008216 ANGLE AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 426AT 426 SAW - DURING CPCP-2 INSPECTION, FOUND RIGHT ZEE MEMBER CORRODED BEYOND LIMITS. REMOVED AND REPLACED ZEE MEMBER IAW SRM 51-25-02 AND 51-25-05. (M) 2 H 7 2 4T RT A53EU 2001091800053 20010918 00053 EU 2001 9 18 SIMA200117802 1 20010614 A 5320 S53671217372 SILL AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AT 499 DURING CPCP2 INSPECTION, MAINTENANCE FOUND THE PASSENGER DOOR SILL PLATE WAS CORRODED. SILL PLATE WAS REMOVED AND REPLA CED IAW ATR SRM. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001091800054 20010918 00054 EU 2001 9 18 SIMA200120703 1 20010718 A 5347 S5367800122402 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 308AE 309 DURING CPCP2 INSPECTION, FOUND CORROSION ON SEAT TRACKS, LEFT AFT OUTBOARD AND RIGHT AFT INBOARD. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW AMERICAN EAGLE AIRLINES ENGINEERING ORDER E2-53MR-115. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001091800055 20010918 00055 EU 2001 9 18 SIMA200120704 1 20010726 A 3240 BRAKE AEROSP ATR72 ATR72212A 8680902 EU PILOT SIDE MALFUNCTIONED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 541AT 541 DFW - FLT 3726 - CREW REPORTED NO TOE BRAKES ON CAPTAINS SIDE. AIRCRAFT WAS STOPPED WITH EMERGENCY BRAKES. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001091800056 20010918 00056 EU 2001 9 18 SIMA200121103 1 20010730 A 3234 100538400 SELECTOR VALVE AEROSP ATR42 ATR42300 8680920 EU HYD BAY FAILED A SIMA O OTHER O OTHER DE DESCENT 1 SW 21 282AT 282 MIA - FLT 5252 - DURING DESCENT, THE LANDING GEAR WOULD NOT EXTEND WHEN SELECTED DOWN. CREW USED EMERGENCY EXTENSION TO LOWER GEAR. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR SELECTOR VALVE IAW MM 32-31-51. OPERATIONAL CHECK WAS G OOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001091800057 20010918 00057 EU 2001 9 18 SIMA200121201 1 20010718 A 5347 S5367800122402 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 308AE 309 SAW - DURING CPCP2 INSPECTION, FOUND CORROSION ON SEAT TRACKS, LEFT AFT OUTBOARD AND RIGHT AFT INBOARD. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW AMERICAN EAGLE AIRLINES ENGINEERING ORDER E2-53MR-115. THE AIRCRAFT WAS RETURNED TO SERV ICE. (M) 2 H 7 2 4T RT A53EU 2001091800058 20010918 00058 EU 2001 9 18 SIMA200124202 1 20010829 A 5347 EPNE95300013009 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 242AT 242 SAW - DURING CPCP2 INSPECTION, FOUND CORROSION WAS FOUND ON 5 SEAT TRACKS, RIGHT AFT INBOARD, RIGHT AFT OUTBOARD, RIGHT AFT CARGO, RT F/A AND LT F/A. ALL SEAT TRACKS WERE REMOVED AND REPLACED IAW AMERICAN EAGLE ENGINEERING ORDER E9-5300-01 3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001091800059 20010918 00059 NM 2001 9 18 USAA010958 1 20010727 A 5312 BULKHEAD BOEING 737 737401 1384701 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 37040 23882 CLT - FOUND PRESSURE WEB WITH ELONGATED HOLES, .281 INCH TO .321 INCH, BS 178, WL 207. DAMAGE REMOVED, INSTALLED ACCESS HOLE DOUBLER PER EA 85146. (M) 2 L 7 2 4F RT A16WE 2001091800060 20010918 00060 NM 2001 9 18 USAA010959 1 20010727 A 5312 BULKHEAD BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 37040 23882 CLT - FOUND PRESSURE WEB CRACKED .5 INCH, BS 178 WL 217 AT LBL 6. DAMAGE REMOVED, REPAIR DOUBLER INSTALLED PER EO 5300V 153. (M) 2 L 7 2 4F RT A16WE 2001091800061 20010918 00061 NM 2001 9 18 USAA010960 1 20010727 A 5320 STIFFENER BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 37040 23882 CLT - FOUND VERTICAL CHORD CRACKED IN TWO PLACES .25 INCH EACH, BS 178, WL 184 AND 195 AT LBL 5.7. DOUBLER INSTALLED PE R EO 5300V155. (M) 2 L 7 2 4F RT A16WE 2001091800062 20010918 00062 NM 2001 9 18 USAA010998 1 20010807 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 31027 24893 CLT - FOUND T-CAP CORRODED .5 INCH BY .5 INCH, BS 986 RBL 16 RBL 40. T-CAP REPLACED PER TR 53-60-01. (M) 2 L 7 2 4F RT A16WE 2001091800063 20010918 00063 NM 2001 9 18 USAA010999 1 20010807 A 5320 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 31027 24893 CLT - FOUND Z-ANGLE CORRODED 1 INCH BY 30 INCHES, BS 312 AND BS 344. INSTALLED Z-ANGLE PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001091800064 20010918 00064 NM 2001 9 18 USAA011001 1 20010807 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 24893 CLT - FOUND T-CAP CORRODED 2 INCHES, BS 344 LBL 6 TO RBL 6. INSTALLED T-CAP PER SRM 53-10-51 SRM 51-40-02 SRM 51-40-00. (M) 2 L 7 2 4F RT A16WE 2001091800065 20010918 00065 NM 2001 9 18 USAA011003 1 20010807 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 31027 24893 CLT - FOUND FLOORBEAM CORRODED 1 INCH BY 40 INCH, BS 312 LBL 28 TO RBL 22. REMOVED DAMAGED T-CAP AND INSTALLED A NEW SE CTION PER BOEING 737-400 SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2001091800066 20010918 00066 NM 2001 9 18 USAA011007 1 20010807 A 5320 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 31027 24893 CLT - FOUND Z-ANGLE CORRODED .5 INCH BY .5 INCH, BS 960 BS 993 LBL 65. REPAIR AND REPLACE Z-ANGLE PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001091800067 20010918 00067 NM 2001 9 18 USAA011010 1 20010807 A 5320 654580734 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 31027 24893 CLT - FOUND SUPPORT ANGLE CRACKED .5 INCH, BS 291 AND S12R. REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51-40-05. (M) 2 L 7 2 4F RT A16WE 2001091800068 20010918 00068 NM 2001 9 18 USAA011011 1 20010807 A 5320 654580730 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 31027 24893 CLT - FOUND SUPPORT ANGLE CRACKED .5 INCH, BS 291 AND S12R. REMOVED AND REPLACED SUPPORT ANGLE PER 51-40-05. (M) 2 L 7 2 4F RT A16WE 2001091800069 20010918 00069 NM 2001 9 18 USAASB01243 1 20010827 A 3350 20121 POWER SUPPLY BOEING 737 737401 1384701 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 412US 23881 CT - MAINTENANCE FOUND THE LEFT LOWER AFT EMERGENCY PATHWAY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE M11 36 POWER SUPPLY. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2001091800070 20010918 00070 WP 2001 9 18 0103099917 1 20010719 A 5320 ANGLE DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 967N DURING AN H CHECK IN ATLANTA, CORROSION WAS FOUND ON THE HORIZONTAL FLANGE OF THE FUSELAGE CUSP ANGLE AT STATION 120 (RT ). DUE TO DEPTH OF CORROSION, IT WAS ELECTED TO TRIM THE FLANGE TO REMOVE THE DAMAGED AREA AND REPAIR ACCOMPLISHED PER EA 99-181362 LOG PAGE 1640717. TE 9910078-3 SUBFLOOR DIAPHRAGM WAS TRIMMED AT A SINGLE ATTACHMENT LOCATION TO REMOVE A C RACK. 2 L 7 2 4F A6WE 2001091800071 20010918 00071 NM 2001 9 18 0103213105 1 20010910 A 2910 HYDRAULIC LINE AIRBUS A319 A319113 NM RT ENGINE LEAKING A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 305NB 1090 IN FLIGHT IN CLIMB THROUGH FL330, THE ECAM SHOWED AN IMMEDIATE LOSS OF YELLOW SYSTEM HYDRAULIC FLUID. AIRCRAFT RETURNED TO DTW. MAINTENANCE FOUND HYDRAULIC LINE LEAKING IN RIGHT ENGINE PYLON. INSTALLED TEMPORARY LINE. PERMANENT LINE REP LACEMENT IS ON DEFERRAL. 2 L 7 2 4F RT A28NM 2001091800072 20010918 00072 WP 2001 9 18 0103229150 1 20010909 A 2131 CONTROLLER DOUG DC9 DC914 3022034 WP CABIN PRESSURE FAILED A NWAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 01 8908E 45749 LOSS OF CABIN PRESSURIZATION DURING CRUISE. CABIN CLIMBED TO 10,500 FEET AT FL290 WITH ANTI-ICE ON AND STEADY CRUISE PO WER. FLIGHT DIVERTED TO GRB, REQUESTED CFR BECAUSE OF EXPECTED OVERWEIGHT LANDING CONDITION AND LANDED WITHOUT INCIDENT . MAINTENANCE REPLACED THE CABIN PRESSURE CONTROLLER, SECURED A CLAMP AT THE DIVERTER VALVE, AND ONE AT THE RIGHT DUCT BOOT. ALL CHECKS WERE GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001091800073 20010918 00073 NM 2001 9 18 0103236302 1 20010910 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 662US 23720 DURING LINE CHECK, FOUND CABIN EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE IN C AND D ZONE. RECONNECTED NUMEROUS LOOSE E LECTRICAL CONNECTORS AT LIGHT FIXTURES. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001091800074 20010918 00074 WP 2001 9 18 0103259927 1 20010605 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8920E 45835 DURING AN H-CHECK AT ATLANTA THE FUSELAGE BELLY SKIN AT STA 332 AND BL 0 WAS DISCOVERED TO HAVE HOLES FOR FASTENERS COMM ON TO SKIN AND SHEAR CLIP HAVE BEEN ELONGATED. THE SHEAR CLIP IS REPLACED AND THE SKIN IS REPAIRED BY TRIMMING OUT THE DAMAGE AND REINFORCING WITH AN EXTERNAL DOUBLER PER EA 99-181262 LOG PAGE1622091. 2 L 7 2 4F A6WE 2001091800075 20010918 00075 WP 2001 9 18 0103269927 1 20010604 A 5314 KEELBEAM DOUG DC9 DC931 3022065 WP FUSELAGE GOUGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8920E 45835 DURING AN H-CHECK AT ATLANTA BASE A DEEP GOUGE WAS FOUND IN THE KEEL FORMER AT STATION 737 (RT) JUST BELOW THE BRAKE CON TROL VALVE. THE GOUGE WAS AT THE TOP OF THE FORMER. THE REPAIR TO FORMER WAS ACCOMPLISHED PER EA 99-181256 LOG PAGE 16 17459. 2 L 7 2 4F A6WE 2001091800076 20010918 00076 NM 2001 9 18 01FDEA00834 1 20010914 A 2781 40173 SWITCH BOEING 727 7272S2F 1384O81 NM L/E FLAP INOPERATIVE A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 201FE 22924 NR 4 LEADING EDGE DEVICE MALFUNCTION DURING FLAP RETRACTION. REMOVED AND REPLACED FLAP SWITCH PER MM 27-82-001-4. 2 L 7 3 4F A3WE 2001092100028 20010921 00028 NM 2001 9 21 01FDEA00835 1 20010914 A 2782 ACTUATOR BOEING 727 72722 1384002 NM L/E FLAP FAILED A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 189FE 19082 LEADING EDGE FLAP LIGHT CAME ON AT 10L FT WITH FLAPS UP. REMOVED AND REPLACED NR 2 & 6 SLAT ACTUATORS PER MM 27-81-032-4 . 2 L 7 3 4F A3WE 2001091800077 20010918 00077 WP 2001 9 18 ABXA010473 1 20010917 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 901AX 47381 EMERGENCY EXIT LIGHTS WERE INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERIES IAW DC9 AMM 33-53-02-04. 2 L 7 2 4F A6WE 2001091800078 20010918 00078 EU 2001 9 18 AWXA0002260 1 20010913 A 2120 ODOR AIRBUS 320 A320231 3930325 EU COCKPIT DETECTED A AWXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 28 620AW 052 PHX - AIR TURNBACK - FLT 751 - AFTER TAKEOFF THE FLIGHT DECK CREW SMELLED AN ELECTRICAL ODOR IN THE COCKPIT AND RETURNED TO PHX MAKING AN UNEVENTFUL LANDING. EMERGENCY EQUIPMENT HAD BEEN CALLED OUT. BY THE TIME THE AIRCRAFT LANDED THE ODO R HAD DISSIPATED. PRIOR TO THIS FLIGHT SEVERAL MAJOR ASSEMBLIES HAD BEEN REPLACED AS PART OF ROUTINE MAINTENANCE, THESE INCLUDE THE NR 1 ENGINE AND THE LT AIR CONDITIONING SYSTEM AIR CYCLE MACHINE. DURING THE EVENT NO WARNING INDICATIONS WERE DISPLAYED IN THE COCKPIT. MAINTENANCE RAN BOTH ENGINES AT HIGH POWER SETTINGS, OPERATED ALL SYSTEMS TURNING THEM O N AND OFF SEVERAL TIMES WITH NO DISCREPANCIES NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2001091800079 20010918 00079 NM 2001 9 18 AWXA0002262 1 20010903 A 5312 65C375903 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 CRACK ON AFT SIDE OF BULKHEAD BS 178 RBL 0.5 WL 187.5. CUT OUT DAMAGED AREA OF CENTER WEB AT FS 178 WL 186.5 TO 188.5 I AW B737-300 SRM 53-10-08 PG 210-215 FIG 203. INSTALLED REPAIR DOUBLER FILLERS AND SHIMS IAW B737-300 SRM 53-10-08 PGS 21 0-215 FIG 203. 2 L 7 2 4F RT A16WE 2001091900158 20010919 00158 NM 2001 9 19 2001UALA01990 1 20010909 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 AFT CARGO PIT AT BODY STATION 1373-1395 STRINGER 24L IS CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091900163 20010919 00163 NM 2001 9 19 2001UALA01995 1 20010901 A 5330 SKIN AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 843UA 1573 FUSELAGE SKIN DAMAGED FWD OF APU COMPARTMENT AFT OF FRAME 76, STRINGER 30. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER . 2 L 7 2 4F 4 F RT A28NM E40NE 2001091900193 20010919 00193 NM 2001 9 19 2001UALA02008 1 20010907 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1421 STRINGER 35L CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER AND SPLICES. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091900195 20010919 00195 NM 2001 9 19 2001UALA02009 1 20010907 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1417 STRINGER 33R IS CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091900196 20010919 00196 NM 2001 9 19 2001UALA02010 1 20010907 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 456 STRINGER 34L CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER AND SPLICE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091900198 20010919 00198 NM 2001 9 19 2001UALA02011 1 20010907 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1329-1351 STRINGER 34L CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091900199 20010919 00199 NM 2001 9 19 2001UALA02012 1 20010907 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1395-1404 STRINGER 34L CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091900200 20010919 00200 NM 2001 9 19 2001UALA02013 1 20010907 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 325-434 STRINGER 38L CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER AND SPLICES. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091900201 20010919 00201 NM 2001 9 19 2001UALA02014 1 20010907 A 5330 SKIN BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1395-1417 STRINGER 34L-35L FUSELAGE SKIN CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DO UBLER REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091900205 20010919 00205 NM 2001 9 19 2001UALA02015 1 20010907 A 5330 SKIN BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1351-1373 STRINGER 37L-39L FUSELAGE SKIN CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DO UBLER REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091900207 20010919 00207 NM 2001 9 19 2001UALA02017 1 20010907 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1329-1351 STRINGER 35L CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091900209 20010919 00209 NM 2001 9 19 2001UALA02018 1 20010907 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1329-1351 STRINGER 36R CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091900238 20010919 00238 NM 2001 9 19 2001UALA02020 1 20010907 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 412-434 STRINGER 38R CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER AND SPLICES. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091900244 20010919 00244 NM 2001 9 19 2001UALA02026 1 20010910 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 412-434 STRINGER 38L CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW STRINGER. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091900245 20010919 00245 NM 2001 9 19 2001UALA02027 1 20010912 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 647UA 25284 FUSELAGE SKIN HOLE ELONGATED LOCATED BETWEEN STRINGER 19L-20L BODY STATION 1473. MAJOR REPAIR ACCOMPLISHED PER SRM 51-20 -07. 2 L 7 2 4F 4 F RT A1NM E24NE 2001091800080 20010918 00080 NM 2001 9 18 2001UALA02036 1 20010913 A 5315 BEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE MISDRILLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 916UA 25383 STATION 360 BL 0 FLOOR BEAM UPPER CAP WAS DRILLED INTO. MAJOR REPAIR ACCOMPLISHEDINSTALLED ANGLE AND STRAP REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091900258 20010919 00258 NM 2001 9 19 2001UALA02038 1 20010913 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 606UA 21867 A .5 INCH LONG CRACK WITH CORROSION BUBBLE AT STA 593 + STRINGER 38L. MAJOR REPAIR ACCOMPLISHED. REPLACE BOTH THE EXIST ING REPAIR DOUBLER AND NEW REPAIR DOUBLER WITH A ONE PIECE REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091800081 20010918 00081 NM 2001 9 18 AWXA0002264 1 20010912 A 5311 144N7130 FRAME BOEING 757 757225 1384959 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 915AW 22209 CORROSION ON FRAME OF WING TO BODY SUPPORT STRUCTURE LOWER TEE CHORD STA 900 RBL 2 TO LBL 9. FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGED SECTION OF TEE CHORD ON BOTH SIDES OF FRAME. FABRICATED TEE CHORD AND REPAIR PARTS AND INSTALLED IAW S RM 51-20-01 PAGE 6, SRM 51-70-12 PAGE 1. 2 L 7 2 4F RT A2NM 2001091800082 20010918 00082 NM 2001 9 18 AWXA0002266 1 20010906 A 5315 141N5112 FLOORBEAM BOEING 757 757225 1384959 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 915AW 22209 FS 366 FLOORBEAM UPPER CHORD CORRODED FROM RBL 8 TO RBL 50. REMOVED UPPER CHORD FROM RBL 8 TO RBL 50 IAW SRM 51-40-02, FABBED UPPER CHORD AND INSTALLED PER SRM 53-10-51 & 53-00-51 FIG 203. 2 L 7 2 4F RT A2NM 2001091800083 20010918 00083 SO 2001 9 18 C2XA01CL203 1 20010916 A 2120 ODOR EMB 135 EMB135LR SO COCKPIT DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 14514 145303 CLE FLIGHT 4169 THE CREW REPORTED A MODERATE SMOKE SMELL AFTER TAKEOFF WHEN THE ENGINE BLEEDS WERE SELECTED. MAINTENANC E INSPECTED AND PERFORMED ENGINE GROUND RUNS AND FOUND NO DEFECTS WITH THE ENGINE BLEED SYSTEM OR THE AIR CONDITIONING S YSTEM. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT TOOO11AT 2001091800084 20010918 00084 NM 2001 9 18 CALA0100865 1 20010912 A 5320 FLOOR SUPPORT BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19634 26319 INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT BS 540, LBL 2. THE FLOOR SUPPORT WAS REMOVED AND REPLACED 51-10-02. 2 L 7 2 4F RT A16WE 2001091800085 20010918 00085 NM 2001 9 18 CALA0100867 1 20010912 A 5320 FLOOR SUPPORT BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19634 26319 INSPECTION FOUND A .5 INCH CRACK IN FLOOR SUPPORTS AT STA 540, BL 0 ON RT AND LT SIDES. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001091800086 20010918 00086 NM 2001 9 18 CALA0100870 1 20010913 A 5330 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CANNING A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND FUSELAGE BELLY SKIN OIL CANNING AROUND ANTENNA BETWEEN STA 460-480, S26R/L. THE DAMAGED SKIN WAS REMOV ED AND A DOUBLER WAS INSTALLED IAW SRM 53-00-01. 2 L 7 2 4F RT A16WE 2001091800087 20010918 00087 NM 2001 9 18 CALA0100873 1 20010913 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND A NOTCH CUT INTO FLOORBEAM WEB AT STA 328, LOCATED JUST FORWARD OF RT HORIZONTAL STABILIZER PULLEY CABL E. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5320-01694. 2 L 7 2 4F RT A16WE 2001091800088 20010918 00088 WP 2001 9 18 CALA0100877 1 20010915 A 5410 SUPPORT DOUG DC9 DC982 3022082 WP NR 1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13891 49102 INSPECTION FOUND A 1.52 INCH CRACK IN NR 1 PYLON UPPER SUPPORT ANGLE AT CANTED FRAME 1463, L17L. A REPAIR ANGLE WAS INS TALLED IAW ECRA 5410-01555. 2 L 7 2 4F A6WE 2001091800089 20010918 00089 2001 9 18 CNMA200100033 4 20010901 A 2330 RDAX5321 DECODER DOUG DC10 DC1010 3022110 WP CABIN FAILED A CNMA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 450AX 46942 ELECTRICAL BURNING SMELL NOTICED IN COCKPIT, SOURCE UNKNOWN. SHUTOFF RECIRC FANS AND SMELL DISSIPATED. UPON INSPECTION CABIN, SMELL WAS VERY STRONG BETWEEN ROWS 30-34 ON RT SIDE. PULLED MUX C/B'S AND SMELL CONTINUED. FURTHER INVESTIGATI ON DISCOVERED HEAVY SMELL AT OVERHEAD LIGHT PANEL ABOVE SEAT 34K. FOUND OVERHEAD DECODER BURNT AT SEAT 34HJK. REMOVED AND REPLACED DECODER. OP CKED GOOD, RESET ALL CB'S, NO SMELL/SMOKE NOTED. 2 L 7 3 4F A22WE 2001091800091 20010918 00091 2001 9 18 DL757011406 4 20010825 A 2330 ODOR BOEING 757 757232 1384965 NM CABIN DETECTED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 612DL 22819 HEAVY ELECTRICAL SMELL IN ROWS 43-45 CO-PILOTS SIDE. TURNED OFF PASSENGER ENTERTAINMENT SYSTEM, SMELL WENT AWAY. TURNE D ON PASSENGER ENTERTAINMENT SYSTEM. NO SMELL PRESENT. INSPECTED PSU'S AND BALLASTS FROM ADJACENT SIDEWALL LIGHTS. NO TROUBLE/SMELL FOUND. A/C OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2001091800092 20010918 00092 NM 2001 9 18 DL764011346 1 20010815 A 2120 ODOR BOEING 767 767432ER NM CABIN DETECTED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 830MH 29701 ELECTRICAL SMELL IN MID CABIN AREA EN ROUTE ATL. CREW SECURED UTILITY BUSSES AND PERFORMED CHECKLIST. MAINTENANCE WAS UNABLE TO DUPLICATE OR DETERMINE SOURCE. CEILING PANELS OPENED AND ALL EQUIPMENT WAS POWERED. A/C WAS RELEASED FOR SER VICE. 2 L 7 2 4F RT A1NM 2001091800093 20010918 00093 2001 9 18 DL764011434 4 20010829 A 2210 6224717004 CONTROL PANEL BOEING 767 767432ER NM AUTOPILOT SYS FAULTY A DALA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 27 830MH 29701 STATUS MSG NO LAND 3, NOTE: SMELLED A SLIGHT ODOR OF BURNT WIRE INSULATION JUST PRIOR TO THE MSG. IN ADDITION F/O`S AD I LOST THE RT FLT DIR AND DATA FROM THE MCP DOES NOT DISPLAY ON F/O`S ADI. REPLACED MCP. 2 L 7 2 4F RT A1NM 2001091800094 20010918 00094 NM 2001 9 18 DL764011453 1 20010831 A 2120 ODOR BOEING 767 767432ER NM CABIN DETECTED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 830MH 29701 ELECTRICAL SMELL NOTED BETWEEN ROWS 22 AND 36 RT SIDE. TURNED OFF UTILITY BUSSES AND SMELL DISSIPATED. INSPECTED AIRCR AFT NTF. 2 L 7 2 4F RT A1NM 2001091800095 20010918 00095 NE 2001 9 18 DL767011350 2 20010817 A 7310 FUEL LINE BOEING 767 767232 1385132 NM GE CF680 CF680A2 NE NR 2 ENGINE CRACKED A DALA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 SO 27 103DA 22215 580390 FLUID LEAKING FROM RIGHT ENGINE ON PUSHBACK AFTER START. T/S LEAK PER M/M FOUND FUEL TUBE ON FUEL NOZZLE FEEDER MANIFO LD AT 5'OCLOCK POSITION CRACKED. REPLACED SAME, RAN ENG PERPFHB, LEAK CKS GOOD. 2 L 7 2 4F 4 F RT A1NM E13NE 2001091800096 20010918 00096 NM 2001 9 18 DL767011384 1 20010822 A 2560 P2070003001 FLASHLIGHT BOEING 767 767232 1385132 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 108DL 22220 AFT RT CABIN FLASHLIGHT INOP. REPLACED FLASHLIGHT ASSY AND BATTERY CHECK GOOD. 2 L 7 2 4F RT A1NM 2001091800097 20010918 00097 NM 2001 9 18 DL767011392 1 20010823 A 2912 271T00422 MODULE BOEING 767 767232 1385132 NM HYDRAULIC SYS CRACKED A DALA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 106DA 22218 ON HYD START UP LOST ALL CENTER SYSTEM FLUID. FOUND PRESS FILTER BOWL CRACKED AND SEPARATED FROM C1 ACMP PRESSURE/CASE DRAIN FILTER MODULE. REPLACED SAME MODULE PER M/M, CHECKS NORMAL, NO LEAKS. 2 L 7 2 4F RT A1NM 2001091800098 20010918 00098 NM 2001 9 18 DL767011407 1 20010825 A 3350 LIGHT BOEING 767 767232 1385132 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 105DA 22217 ON L/O FOUND EMERGENCY LIGHTS INOP AT RT OVERWING EXIT SIGN, 2L DOOR EXIT SIGN AND AFT RT LAV RED FLOOR LIGHT. RELAMPED RT OVERWING EXIT AND 2L DOOR EXIT. REPAIRED BROKEN WIRE AT 3R LAV FLOOR LIGHT. 2 L 7 2 4F RT A1NM 2001091800099 20010918 00099 EU 2001 9 18 QXEA0101514 1 20010914 A 3350 6008903 POWER SUPPLY FOKKER F28 F28MK4000 4990810 EU WEAK A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 14059 4095 11227 PDX - AFT LEFT CABIN EMERGENCY BATTERY PACK IS WEAK. REMOVED AND REPLACED AFT LEFT BATTERY PACK. OPERATIONAL CHECK IS GO OD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001091800100 20010918 00100 NE 2001 9 18 DL767011455 2 20010901 A 7321 MEC BOEING 767 767232 1385132 NM GE CF680 CF680A2 NE NR 2 ENGINE DEFECTIVE A DALA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 SO 27 113DA 51502 22225 580157 NR 2 ENGINE SHUT DOWN BY CREW ON APPROACH TO PBI. DURING CRUISE NOTICED RT THROTTLE/ENGINE WAS NOT RESPONDING TO MOVEME NT, COMMAND BAR WAS PRESENT. DURING DESCENT GOT EICAS R ENG SPEED CARD. REPLACED ENGINE MEC. 2 L 7 2 4F 4 F RT A1NM E13NE 2001091800101 20010918 00101 NM 2001 9 18 DL76L011354 1 20010817 A 2560 P20700030 CONNECTOR BOEING 767 767332 1382001 NM FLASHLIGHT DISCONNECTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 171DN 24759 JUMP SEAT LT FWD CTR FLASH LIGHT RED CHARGE INDICATOR LIGHT NOT FLASHING. FOUND SECURITY SEAL BROKEN AND BATTERY CONNEC TOR NOT CONNECTED. RECONNECTED BATTERY AND INSTALLED NEW SEAL. BATTERY RED LIGHT INDICATES CHARGED. 2 L 7 2 4F RT A1NM 2001091800102 20010918 00102 NM 2001 9 18 DL76L011375 1 20010820 A 3350 LIGHT BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 181DN 25986 EMERGENCY LIGHT ESCAPE PATH INOP AT SEAT 22F AND 32B. TROUBLE SHOT SYSTEM FOUND BOTH ROWS FROM 30 AFT INOP. ISOLATED M ALFUNCTION TO SEAT 32B. SEAT 22F WAS RELAMPED, NO HELP SO SEAT 32B AND 22F WERE TRANSFERRED TO MCO. PER MEL 33- 51-03D . 2 L 7 2 4F RT A1NM 2001091800103 20010918 00103 NM 2001 9 18 DL76L011378 1 20010820 A 2120 ODOR BOEING 767 767332 1382001 NM COCKPIT DETECTED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 182DN 25987 TWENTY MINUTES OUT OF ATL CREW BECAME AWARE OF SULFUR SMELL IN COCKPIT. MTC T/S FOUND NO DISCREPANCIES. A/C WAS RELEAS ED FOR FLIGHT. 2 L 7 2 4F RT A1NM 2001091800104 20010918 00104 NM 2001 9 18 F3LA200100104 1 20010831 A 3350 58781 LIGHT BOEING 737 7372Y5 1384554 NM CABIN INOPERATIVE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 118RW 40 23040 DURING SERVICE CHECK, MAINTENANCE REPORTED EMERGENCY EXIT FLOOR PATH LIGHTING BETWEEN ROWS 6 AND 11 INOPERATIVE. FERRIE D AIRCRAFT TO DEN FOR REPAIR. REPLACED EMERGENCY FLOOR PATH LIGHTING STRIP BETWEEN ROWS 6 AND 11 AND SYSTEM CHECKED OKA Y. 2 L 7 2 4U RT A16WE 2001091800105 20010918 00105 2001 9 18 F3LA200100105 4 20010910 A 2565 22D22900139 SLIDE BOEING 737 7372Y5 1384554 NM R1 DOOR DISCHARGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 10 23040 DURING SERVICE CHECK, MAINTENANCE REPORTED R-1 DOOR SLIDE PRESSURE LOW. AIRCRAFT WILL BE FERRIED TO DEN FOR REPLACEMENT OF SLIDE. 2 L 7 2 4U RT A16WE 2001091800106 20010918 00106 NM 2001 9 18 F3LA200100106 1 20010915 A 5330 SKIN BOEING 737 7372Y5 1384554 NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 921WA 2755 23039 DURING C-3 CHECK, INSPECTION REPORTED CRACK IN L-2 DOOR CUTOUT, LOWER FWD CORNER, BS 947.5, S-18L, APPROXIMATELY 3.5 INC HES LONG. REPAIRED CRACK PER SRM 53-30-3, FIGURE 24. 2 L 7 2 4U RT A16WE 2001091800107 20010918 00107 NM 2001 9 18 01FDEA00837 1 20010917 A 5310 FRAME BOEING 727 727233 138408A NM AFT CARGO DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 N 450 AFT CARGO FRAME DENT AT BS 970, LBL 33. ** S/D ** COMING 2 L 7 3 4F RT A3WE 2001092600060 20010926 00060 NM 2001 9 26 01FDEA00838 1 20010917 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 CORROSION (C53-224-1-, 1) ON FLOORBEAM BS 620 LBL 25 TO 45, WL 208. REMOVED AND REPLACED CORROSION ON FLOORBEAM PER SRM 53-10-8. 2 L 7 3 4F RT A3WE 2001092600061 20010926 00061 NM 2001 9 26 01FDEA00839 1 20010917 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 CORROSION (C53-024-02) ON FLOORBEAM TOP CHORD UPPER AND LOWER FLANGE BS 680, RBL 3 - 25, WL 208. REMOVED AND REPLACED FL OORBEAM PER SRM 53-10-8 FIG 3. 2 L 7 3 4F RT A3WE 2001092600062 20010926 00062 NM 2001 9 26 01FDEA00840 1 20010917 A 5310 SHEAR TIE BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 CORRODED SHEAR TIE BS 1110, RBL 10 - 14. REMOVED AND REPLACED SHEAR TIE PER SRM 51-20-1, 51-10-2 & 51-30-2. 2 L 7 3 4F RT A3WE 2001091800108 20010918 00108 CE 2001 9 18 GLBA2001113 1 20010528 A 7722 3053995CL08 PROBE BEECH 1900 1900D 1154162 CE RT ENGINE OUT OF TOLERANCE A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 01 118UX UE118 RT ENGINE ITT OVER 800 DEG ON TAKEOFF. ABORTED TAKEOFF. ADJUSTED TRIM STICK, OPS CHECKED GOOD. 2 L 7 2 4T RT A24CE 2001091800111 20010918 00111 CE 2001 9 18 GLBA2001190 1 20010829 A 3297 WIRE BEECH 1900 1900D 1154162 CE LANDING GEAR CHAFED A GLBA O OTHER O OTHER AP APPROACH 1 CE 01 192GL UE192 LANDING GEAR C/B POPPED, MANUALLY EXTENDED GEAR. INSPECTED FOUND CHAFED WIRE. REPAIRED, OPS CHECKED SYSTEM SATISFACTOR Y. 2 L 7 2 4T RT A24CE 2001091800112 20010918 00112 CE 2001 9 18 GLBA2001192 1 20010830 A 3230 1013880083 VALVE BEECH 1900 1900D 1154162 CE LANDING GEAR FAILED A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 192GL 13588 UE192 LANDING GEAR WOULD NOT RETRACT AFTER T/O. REPLACED HYDRAULIC SERVICE VALVE, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001091800113 20010918 00113 CE 2001 9 18 GLBA2001193 1 20010901 A 7333 12281301 TRANSMITTER BEECH 1900 1900D 1154162 CE LT ENGINE FAULTY A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 01 201YQ 3796 718 UE201 LEFT FUEL FLOW FLUX ON T/O. REPLACED FUEL FLOW TRANSMITTER, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001092800068 20010928 00068 SO 2001 9 28 GLBA2001195 1 20010902 A 3260 32138 SWITCH EMB 120 EMB120 3260201 SO LANDING GEAR FAILED A GLBA K NONE N FALSE WARNING AP APPROACH 1 CE 01 92GL 120092 LANDING GEAR WARNING AND MAP LIGHTS. REPLACED PRESSURE SWITCH, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A31SO 2001091800114 20010918 00114 CE 2001 9 18 GLBA2001196 1 20010902 A 7722 305399SCL08 PROBE BEECH 1900 1900D 1154162 CE RT ENGINE DEFECTIVE A GLBA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 CE 01 261GL UE261 RIGHT ENGINE TEMP LIMITED ON T/O. REPLACED TRIM PROBE, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001100100052 20011001 00052 SO 2001 10 1 GLBA2001197 1 20010903 A 3260 SWITCH EMB 120 EMB120 3260201 SO COCKPIT OUT OF ADJ A GLBA K NONE N FALSE WARNING CL CLIMB 1 CE 01 92GL 120092 LANDING GEAR WARNING AND MAP LIGHTS. ADJUSTED RIGHT POWER LEVER SWITCH, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A31SO 2001091800115 20010918 00115 SO 2001 9 18 GLBA2001198 1 20010905 A 2897 WIRE EMB 120 EMB120ER 3260203 SO FUEL QUANTITY CHAFED A GLBA K NONE O OTHER IN INSP/MAINT 1 CE 01 96ZK 120096 FUEL QUANTITY WIRES CHAFING ON LINE (TUBE) BY LEFT VENT VALVE BETWEEN RIBS NR 24 & 25. 2 L 7 2 4T RT A31SO 2001091800116 20010918 00116 SO 2001 9 18 GLBA2001199 1 20010905 A 2810 VENT LINE EMB 120 EMB120ER 3260203 SO RT WING CHAFED A GLBA K NONE O OTHER IN INSP/MAINT 1 CE 01 96ZK 120096 FUEL QUANTITY WIRING RIGHT WING CHAFED ON LINE (TUBE) GOING TO VENT VALVE, LINE ALSO DAMAGE FROM CHAFING BETWEEN RIBS NR 24 & 25. 2 L 7 2 4T RT A31SO 2001091800117 20010918 00117 SO 2001 9 18 GLBA2001200 1 20010905 A 2897 WIRE EMB 120 EMB120ER 3260203 SO RT WING CHAFED A GLBA K NONE O OTHER IN INSP/MAINT 1 CE 01 96ZK 120096 RIGHT WING FUEL QUANTITY WIRING CHAFED ON LIGHTENING HOLE OUTBOARD OF NR 4 FUEL STICK AND RIB NR 20. 2 L 7 2 4T RT A31SO 2001091800118 20010918 00118 SO 2001 9 18 GLBA2001201 1 20010905 A 2897 WIRE EMB 120 EMB120ER 3260203 SO RT WING CHAFED A GLBA K NONE O OTHER IN INSP/MAINT 1 CE 01 96ZK 120096 RIGHT WING FUEL QUANTITY WIRES CHAFED ON FUEL VENT LINE (TUBE) AT RIB NR 20. 2 L 7 2 4T RT A31SO 2001091800119 20010918 00119 CE 2001 9 18 GLBA2001202 1 20010904 A 2460 1293800161 CONTROL PANEL BEECH 1900 1900D 1154162 CE COCKPIT DEFECTIVE A GLBA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 01 192GL 5579 2044 UE192 LEFT GENERATOR FALLS OF LINE. REPLACED DC PWR PANEL, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001092800070 20010928 00070 CE 2001 9 28 GLBA2001203 1 20010904 A 5610 10138402521 WINDSHIELD BEECH 1900 1900D 1154162 CE COCKPIT CRACKED A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 01 151GL UE151 CAPTAINS WINDSHIELD CRACKED IN FLIGHT. REPLACED WINDSHIELD, SYSTEM CHECK SATISFACTORY. 2 L 7 2 4T RT A24CE 2001092800076 20010928 00076 CE 2001 9 28 GLBA2001205 1 20010915 A 2460 1293640797 FUSE BEECH 1900 1900D 1154162 CE CIRCUIT BOARD LOOSE A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 01 97UX UE97 ANNUNCIATOR POWER SOURCE ILLUMINATED ON T/O. INSPECTED FOUND LOOSE CONNECTION ON PICO FUSE ON PCB A141. REPLACED BOARD , OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001091800120 20010918 00120 EA 2001 9 18 JBXA000317 1 20010828 A 3620 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT ACTIVATED A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 570ML 7206 RIGHT 14TH STAGE DUCT WARNING MESSAGE CAME ON CLIMBOUT OF RDU. PERFORMED GROUND RUN OF RIGHT ENGINE, CHECKED PYLON BLEE D DUCTS FOR LEAKS, NO LEAKS NOTED AT THIS TIME. INSTALLED BOOT ON COWL ANTI-ICE DUCTING IAW 36-12-09. 2 L 7 2 4F RT A21EA 2001091800121 20010918 00121 EA 2001 9 18 JBXA000318 1 20010828 A 3610 ISOLATION VALVE CNDAIR CL600 CL6002B19 EA NR 2 ENGINE LEAKING A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 570ML 7206 RIGHT 14TH STAGE DUCT WARNING MESSAGE CAM ON IN CLIMB OUT OF RDU. PERFORMED GROUND ENGINE RUN OF NR 2 ENGINE. FOUND 14 TH STAGE ISOL VALVE LEAKING. REMOVED AND REINSTALLED ISOL VALVE, LEAK CHECK GOOD AT THIS TIME IAW AMM 36-12-01. 2 L 7 2 4F RT A21EA 2001091800122 20010918 00122 NE 2001 9 18 NACA20010027 2 20010709 A 8530 404482 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 3 ENGINE DAMAGED A NACA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 AL 03 43872 591 591 533294 P32304 FEATHERED NR 3 ENGINE AT 2311Z DUE TO LOSS OF OIL. REMOVED AND REPLACED ENGINE ASSY. 2 L 7 4 4R 4 R A781 5E8 2001091800123 20010918 00123 NE 2001 9 18 NACA20010028 2 20010728 A 8520 76570F CAM DOUG DC6 DC6B 3021712 WP PWA R2800 R2800CB3 52026 NE NR 2 ENGINE FAILED A NACA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 867TA 1491 1491 45202 NK510177 NR 2 ENGINE NR 16 CYLINDER DOUBLE SHORTED SECONDARY, (FRONT CAM FAILURE). REPLACED NR 2 ENGINE. 2 L 7 4 4R 4 R 6A4 5E8 2001091800124 20010918 00124 WP 2001 9 18 NACA20010031 1 20010831 A 7921 319721 ACTUATOR DOUG DC6 DC6 3021702 WP PWA R2800 R2800* 52026 NE NR 2 ENGINE STUCK A NACA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 AL 03 2907F 3124 2976 533265 NK51771 NR 2 ENGINE PRECAUTIONARY SHUT DOWN IN CRUISE DUE TO HIGH OIL TEMP (105 DEGREES), LOW OIL PRESS (55 PSI), UNABLE TO CONT ROL RPM (STUCK AT 2400), OIL COOLER CONTROL HAS NO EFFECT. REPLACED NR 2 OIL COOLER ACTUATOR, PERFORMED GROUND MAINT RU N, OIL PRESS AND OIL TEMP WITHIN LIMITS, BMEP, F/F, MAG CHECK OK. PROP OPERATION AND FEATHER CHECK NORMAL. REF NAC DC- 6 MM SECT IV EC01.1 AND 2 AND PURDUE MM 11-1-6. 2 L 7 4 4R 4 R A781 5E8 2001091800126 20010918 00126 NM 2001 9 18 OZIA013125004 1 20010527 A 7732 30B370102 SENSOR DORNER DO32 DO328300 NM PWA 306 PW306B NE LT ENGINE MALFUNCTIONED A OZIA O OTHER N FALSE WARNING CL CLIMB 1 CE 05 410Z 3125 CD0019 RECEIVED LEFT ENGINE VIBRATION INDICATION ON CLIMBOUT. THE INDICATION VARIED BETWEEN INTERMITTENT TO FULL INDICATION AT 3.6 IPS. ONCE IN FLIGHT, INDICATION WOULD RETURN TO NORMAL AFTER BETWEEN 2 AND 3 MINUTES UP TO 5 MINUTES. PER MANUFAC TURER'S REQUEST, REPOSITIONED BOTH VIBRATION SENSOR AND VIBRATION MONITORING UNIT FROM LEFT TO RIGHT ENGINE AND RIGHT TO LEFT ENGINE. INDICATION FOLLOWED TO RIGHT ENGINE. INDICATION DIFFICULTY RESOLVED BY REPLACING BOTH VIBRATION SENSOR A ND MONITORING UNIT WITH KNOWN COMPATIBLE UNITS. VIBRATION SENSOR P/N 30B3701-02, S/N 1071, ENGINE VIBRATION MONITORING UNIT P/N 241-277-000-011, SN 2511, LT ENGINE S,N CD0019, RT ENGINE S/N CD0022. 2 H 7 2 4T 4 F RT A55NM E35NE 2001091800127 20010918 00127 NE 2001 9 18 OZIA200141005 2 20010726 A 7250 30B428501 TURBINE BLADES DORNER DO32 DO328300 NM PWA 306 PW306B NE ENGINE DAMAGED A OZIA K NONE O OTHER IN INSP/MAINT 1 CE 05 410Z 2334 540 3125 CD0019 ENGINE S/N CD0019 HAD A BURNT HOLE EXPOSING INNER CAVITY AT LEADING EDGE OF ONE BLADE. BORESCOPES ON OTHER ENGINES IN F LEET HAVE REVEALED SINGLE CRACKS AT CENTER OF VARIOUS BLADE TIPS; 2 CRACKS (NON-CONVERGING) AT CENTER OF BLADE TIP; MINO R COATING LOSS AT LEADING EDGE OF ALL TURBINE BLADES. DAMAGE NOTED IS WITHIN LIMITS PER DORNIER 328J JIC TR 72-087. EN GINE S/N`S CD0019 AND CD0022 WERE REMOVED TO BE SENT TO REPAIR FACILITY. 2 H 7 2 4T 4 F RT A55NM E35NE 2001091800128 20010918 00128 NM 2001 9 18 P5CA0100568 1 20010601 A 3520 80080201 CONTROL UNIT BOEING 747 747122 1384872 NM CABIN FAILED A P5CA K NONE L NO TEST IN INSP/MAINT 1 WP 23 850FT 19755 WHEN COMPLYING WITH FCD 35-10, O2 DOOR AND MASK FAILED TO DEPLOY. REMOVED AND REPLACED FLOW CONTROL UNIT SYSTEM OPS CHE CK NORMAL P/N ON 800802-01 ON 0444, P/N OFF 800802-01 S/N OFF 761. 2 L 7 4 4F A20WE 2001091800129 20010918 00129 2001 9 18 P5CA0100569 4 20010612 A 2565 7A124836 SLIDE BOEING 747 747249F 1384849 NM CABIN DEFECTIVE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 RT UPPER DECK SLIDE BLOWN BY MAINTENANCE AND ONLY HALF INFLATED. REPLACED U/D RIGHT SLIDE ASSIST BOTTLE. REMOVED AND R EPLACED U/D RIGHT SLIDE FOUND SHEARED CABLE. P/N ON 7A1248-36 S/N ON G476. 2 L 7 4 4F A20WE 2001091800130 20010918 00130 NM 2001 9 18 P5CA0100584 1 20010625 A 5320 INTERCOSTAL BOEING 747 747249F 1384849 NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION - BULK CARGO FLOOR INTERCOSTAL AT STA 2040 LBL 23 FOUND CORRODED. CORROSION REMOVED AND INSPECTED. F OUND WITHIN LIMITS AS PER SRM 51-010-01 & SRM 53-10-01. BLENDED SURFACES, RE-PROTECTED AND REPLACED ANCHOR NUT AS PER S RM 51-10-02 & SRM 51-30-02. 2 L 7 4 4F A20WE 2001091800131 20010918 00131 NM 2001 9 18 P5CA0100585 1 20010625 A 5320 INTERCOSTAL BOEING 747 747249F 1384849 NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION - BULK CARGO FLOOR INTERCOSTAL AT STA 2040 RBL 23 FOUND CORRODED. CORROSION REMOVED AND INSPECTED. F OUND WITHIN LIMITS AS PER SRM 51-10-01 & SRM 53-10-01. BLENDED SURFACES, REPROTECTED AND REPLACED ANCHOR NUT AS PER SRM 51-10-02 & SRM 51-30-02. 2 L 7 4 4F A20WE 2001091800132 20010918 00132 NM 2001 9 18 P5CA0100587 1 20010717 A 7931 WARNING LIGHT BOEING 747 747123 1384873 NM NR 1 ENGINE ILLUMINATED A P5CA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 WP 23 859FT 20326 NR 1 OIL PRESSURE FLUCTUATING BETWEEN 40 AND 42 PSI, OIL QTY NORMAL, NO LIGHTS. ON POWER REDUCTION AT TOP OF DESCENT NR 1 OIL PRESSURE LIGHT AND FILTER BYPASS LIGHT CAME ON. ENG SHUTDOWN AS PRECAUTIONARY. OIL TEMP AND QTY STILL NORMAL. 2 L 7 4 4F A20WE 2001091800133 20010918 00133 NE 2001 9 18 P5CA0100590 2 20010729 A 7200 ENGINE BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 3 MALFUNCTIONED A P5CA F E A ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 23 850FT 19755 662326 DURING CLIMBOUT NR 3 ENGINE FIRE LIGHT CAME ON WITH FIRE LOOPS BOTH AT 9 ALSO STARTER VALVE OPEN LIGHT. ZERO OIL QTY CS D OIL AND RISE IN TEMP READING. ZERO N2 RPM AND N1 14 PERCENT. RAN ENG FIRE CHECK LIST BOTH LIGHTS STAYED ON. ENGINE REMOVED AND REPLACED PER POLAR WORK CARD M7100-002. REMOVED AND REPLACED FIRE BOTTLE AND SQUIB. ENG S/N ON 695757. 2 L 7 4 4F 4 F A20WE E20EA 2001091800134 20010918 00134 NM 2001 9 18 P5CA0100591 1 20010914 A 5270 WARNING SYSTEM BOEING 747 7472U3B NM CARGO DOOR MALFUNCTIONED A P5CA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 23 923FT 22769 MAIN DECK SIDE CARGO DOOR WARNING LIGHT ILLUMINATED DURING ROTATION AT TAKEOFF. AIRCRAFT RETURNED TO AIRPORT. CYCLED D OOR OPEN AND INSPECTED LATCHES. DOOR CLOSED OK AND LOCKING LEVER CLOSED DOWN. OK FOR SERVICE PER MM 52-32-00. 2 L 7 4 4F RT A20WE 2001091800137 20010918 00137 EU 2001 9 18 RAIA00106003 1 20010608 A 7722 30738461 TERMINAL JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE DEFECTIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 557HK 41074 5402-EWR-RIGHT IEC FAILURE ASSOCIATED WITH RIGHT EGT RISE. MAINTENANCE INSPECTED AND REPLACED RIGHT ENGINE EGT HARNESS TERMINAL END. 2 L 7 2 4T RT A41NM 2001091800138 20010918 00138 EU 2001 9 18 RAIA00106004 1 20010610 A 2160 5326C000 CONTROL VALVE JETAIR JETSTM JETSTM4101 1500501 EU A/C BAY FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 566HK 10110 3490 41084 7071-STL-CREW REPORTED LEFT ECS IS BLOWING HOT THEN COLD AIR. MAINTENANCE INSPECTED AND REPLACED LEFT TEMPERATURE CONTR OL VALVE. 2 L 7 2 4T RT A41NM 2001091800139 20010918 00139 EU 2001 9 18 RAIA00106005 1 20010610 A 3230 1005383Y00 CONTROL VALVE AEROSP ATR72 ATR72202 8680940 EU HYDRUALIC BAY FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 722TE 23574 220 7116-STL-LANDING GEAR WOULD NOT RETRACT. MAINTENANCE INSPECTED AND REPLACED LANDING GEAR CONTROL VALVE. PERFORMED GEAR SWING, SYSTEM CHECKED GOOD. 2 H 7 2 4T RT A53EU 2001091800140 20010918 00140 EU 2001 9 18 RAIA00106006 1 20010611 A 7722 102090 SENSOR JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE LT ENGINE FAILED A RAIA D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 CE 03 552HK 11698 41057 75091 7325-BMI-LEFT ENGINE ACHIEVED 87 PERCENT TORQUE, TARGET TORQUE WAS 99 PERCENT. MAINTENANCE INSPECTED AND REPLACED LEFT ENGINE INLET TEMPERATURE SENSOR. PERFORMED GROUND RUN, TARGET TORQUE ACHIEVED. 2 L 7 2 4T 4 T RT A41NM E18NE 2001091800141 20010918 00141 SO 2001 9 18 RAIA00107017 1 20010706 A 5311 FRAME EMB 145 EMB145ER SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 801HK 145053 MX-STL-DURING BLOCK INSPECTION MAINTENANCE FOUND CORROSION AFT OF FUSELAGE FRAME 18 AT RIGHT BL 18. MAINTENANCE REMOVED CORROSION FROM AFT OF FUSELAGE FRAME 18 AT RIGHT BL 18 IAW EMB 145 CPM. 2 L 7 2 4F RT T00011AT 2001091800142 20010918 00142 SO 2001 9 18 RAIA00107018 1 20010706 A 5311 FRAME EMB 145 EMB145ER SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 801HK 145053 MX-STL-DURING MAINTENANCE CHECK FOUND CORROSION AFT OF FUSELAGE FRAME 19A ON BL. MAINTENANCE INSPECTED AND REMOVED CORR OSION AT INBOARD AFT OF FUSELAGE FRAME 19A ON BL IAW EMB 145 CPM. 2 L 7 2 4F RT T00011AT 2001091800143 20010918 00143 SO 2001 9 18 RAIA00107019 1 20010706 A 5311 FRAME EMB 145 EMB145ER SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 801HK 145053 MX-STL-DURING MAINTENANCE CHECK FOUND CORROSION AFT OF FUSELAGE FRAME 19A AT LEFT BL 18. MAINTENANCE REMOVED CORROSION AND REPAIRED FUSELAGE FRAME 19A AT LEFT BL 18 IAW EMB 145 SRM. 2 L 7 2 4F RT T00011AT 2001091800144 20010918 00144 SO 2001 9 18 RAIA00107020 1 20010707 A 5311 FRAME EMB 145 EMB145ER SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 801HK 145053 MX-STL-DURING MAINTENANCE CHECK FOUND CORROSION FORWARD OF FUSELAGE FRAME 18 ON BL. MAINTENANCE REPAIRED DIGITAL FORWAR D OF FUSELAGE FRAME 18 AT BL IAW EMBRAER ENGINEERING ORDER GST-2322/01. 2 L 7 2 4F RT T00011AT 2001091800145 20010918 00145 SO 2001 9 18 RAIA00107021 1 20010706 A 5311 FRAME EMB 145 EMB145ER SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 801HK 145053 MX-STL-DURING MAINTENANCE CHECK FOUND CORROSION AFT OF FUSELAGE FRAME 15 AT LEFT BL 18. MAINTENANCE REMOVED CORROSION F ROM AFT FUSELAGE FRAME 15 AT LEFT BL 18 IAW EMB145 CPM. 2 L 7 2 4F RT T00011AT 2001091800146 20010918 00146 SO 2001 9 18 RAIA00107022 1 20010707 A 5311 FRAME EMB 145 EMB145ER SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 801HK 145053 MX-STL-DURING MAINTENANCE CHECK FOUND CORROSION FORWARD OF FUSELAGE FRAME 17 AT LEFT BL 18. MAINTENANCE REPAIRED DIGITA L FORWARD OF FUSELAGE FRAME 17 AT LEFT BL 18 IAW EMBRAER ENGINEERING ORDER GST-2322/01. 2 L 7 2 4F RT T00011AT 2001091800147 20010918 00147 SO 2001 9 18 RAIA00107026 1 20010706 A 5311 FRAME EMB 145 EMB145ER SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 801HK 145053 MX-STL-DURING MAINTENANCE CHECK FOUND CORROSION AT FUSELAGE FRAME 19A ON SIDE OF LEFT BL 18. MAINTENANCE REPAIRED FUSEL AGE GRAME 19A ON SIDE OF LEFT BL 18 IAW EMB145 SRM. 2 L 7 2 4F RT T00011AT 2001091800148 20010918 00148 SO 2001 9 18 RAIA00107027 1 20010706 A 5320 STRUCTURE EMB 145 EMB145ER SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 801HK 145053 MX-STL-DURING MAINTENANCE CHECK FOUND CORROSION FROM 10 INCHES FORWARD AND 12 INCHES AFT OF FUSELAGE FRAME 22A ON BL. M AINTENANCE REMOVED CORROSION FROM 10 INCHES FORWARD AND 12 INCHES AFT OF FUSELAGE FRAME 22A ON BL IAW EMB145 CPM. 2 L 7 2 4F RT T00011AT 2001091800149 20010918 00149 SO 2001 9 18 RAIA00107029 1 20010706 A 5311 FRAME EMB 145 EMB145ER SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 801HK 145053 MX-STL-DURING MAINTENANCE CHECK FOUND CORROSION AT FUSELAGE FRAME 18 BETWEEN BL AND RIGHT BL 31. MAINTENANCE REMOVED CO RROSION FROM FUSELAGE FRAME 18 BETWEEN BL AND RIGHT BL 31 IAW EMB145 CPM. 2 L 7 2 4F RT T00011AT 2001091800150 20010918 00150 SO 2001 9 18 RAIA00107030 1 20010707 A 5320 STRUCTURE EMB 145 EMB145ER SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 801HK 145053 MX-STL-DURING MAINTENANCE CHECK FOUND CORROSION BETWEEN FUSELAGE FRAMES 15 AND 18 ON THE BL. MAINTENANCE REPAIRED DIGIT AL FORWARD BETWEEN FUSELAGE FRAMES 15 AND 18 IAW EMBRAER ENGINEERING ORDER GST-2322/01. 2 L 7 2 4F RT T00011AT 2001091800151 20010918 00151 SO 2001 9 18 RAIA00107031 1 20010709 A 5320 SILL EMB 145 EMB145ER SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 801HK 145053 MX-STL-DURING MAINTENANCE CHECK FOUND CORROSION AT THE RIGHT FORWARD SILL, FORWARD OF SERVICE DOOR. MAINTENANCE REMOVED CORROSION FROM RIGHT FORWARD SILL, FORWARD OF SERVICE DOOR IAW EMB145 CPM. 2 L 7 2 4F RT T00011AT 2001091800152 20010918 00152 SO 2001 9 18 RAIA00107032 1 20010709 A 5320 GUSSET EMB 145 EMB145ER SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 801HK 145053 MX-STL-DURING MAINTENANCE CHECK FOUND CORROSION AT CENTER GUSSET AFT OF FORWARD DIGITAL. MAINTENANCE REMOVED CORROSION FROM CENTER GUSSET FORWARD OF DIGITAL IAW EMB145 CPM. 2 L 7 2 4F RT T00011AT 2001091800153 20010918 00153 EU 2001 9 18 RAIA00108014 1 20010814 A 5610 14156002409 WINDSHIELD JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT CRACKED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 568HK 11876 41086 7416-STL-CAPTAINS (LEFT) OUTER PANEL WINDSCREEN CRACKED IN FLIGHT, AIRCRAFT RETURNED FROM FLIGHT AND LANDED WITHOUT INCI DENT. MAINTENANCE INSPECTED AND REPLACED THE LEFT (CAPTAINS) WINDSCREEN. 2 L 7 2 4T RT A41NM 2001091800154 20010918 00154 EU 2001 9 18 RAIA00108019 1 20010820 A 7714 31055863 TRANSDUCER JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE MCAULY 5JFR36 B5JFR36C1103 GL LEFT ENGINE FAILED A RAIA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 CE 03 550HK 14457 41039 75018 941684 5372-BWI-LEFT ENGINE RPM OVERSPEED ON APPROACH JUST AFTER PUSHING CONDITION LEVERS FORWARD. CREW PERFORMED ENGINE SHUTD OWN, AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE SPEED TRANSDUCER AND THE LEFT PROPELLER PIT CH CONTROL. PERFORMED MAINTENANCE CHECK FLIGHT, CHECK FLIGHT RESULTS SATISFACTORY. 2 L 7 2 4T 4 T RT A41NM E18NE 6 C P15NE 2001091800155 20010918 00155 NE 2001 9 18 RAIA00108028 2 20010827 A 7261 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE LEFT LACK OF LUBE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 554HK 41067 76019 5417-PVD-LEFT ENGINE OIL PRESSURE LIGHT CAME ON AFTER ENGINE START, CREW SHUT DOWN ENGINE. MAINTENANCE INSPECTED ENGIN E AND SERVICED OIL, PERFORMED GROUND RUN, ALL INDICATIONS NORMAL. 2 L 7 2 4T 4 T RT A41NM E18NE 2001091800156 20010918 00156 EU 2001 9 18 RAIA00109001 1 20010903 A 2435 23095002 SEAL JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RT STARTER GEN LEAKING A RAIA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 03 564HK 2864 555 41081 76092 5388-RIC-RIGHT ENGINE OIL PRESSURE FELL TO ZERO, RIGHT OIL PRESSURE CAPTION ILLUMINATED, CREW PERFORMED ENGINE SHUTDOWN. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE RIGHT STARTER GENERATOR SEAL DAMAGED. MAINTENA NCE SERVICED THE ENGINE OIL AND REPLACED THE RIGHT ENGINE STARTER GENERATOR. MAINTENANCE PERFORMED GROUND RUN AND LEAK CHECK. SYSTEMS CHECKED GOOD. 2 L 7 2 4T 4 T RT A41NM E18NE 2001091800157 20010918 00157 NE 2001 9 18 RAIA00109002 2 20010904 A 7321 FCU JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RT ENGINE OUT OF ADJ A RAIA O OTHER X ENGINE FLAMEOUT LD LANDING 1 CE 03 566HK 41084 76082 7136-EVV-ON LANDING RIGHT ENGINE FLAMED OUT. MAINTENANCE ADJUSTED RIGHT ENGINE FUEL CONTROL DECELERATION SCHEDULE. 2 L 7 2 4T 4 T RT A41NM E18NE 2001091800158 20010918 00158 GL 2001 9 18 RAIA00109004 2 20010908 A 7200 AE3007A1 ENGINE EMB 145 EMB145LR SO ALLSN AE300 AE3007A GL RIGHT FAILED A RAIA C E ABORTED TAKEOFF ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CE 03 811HK 1978 145256 311611 5298-LIT-RIGHT ENGINE FAILED AS THRUST LEVERS ADVANCED FOR TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE RIGHT ENGINE . 2 L 7 2 4T 4 F RT T00011AT TE6CH 2001091800159 20010918 00159 NM 2001 9 18 SCNA01707 1 20010809 A 7700 WARNING SYSTEM BOEING 727 727200 138407E NM COCKPIT ACTIVATED A SCNA O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 15 211DB 20766 ENGINE FAILURE INDICATION ON TAKEOFF. NR 3 GENERATOR BREAKER TRIP AND AUTO PACK TRIP OFF LEFT AND RIGHT PACK. PLACED O N MEL. 2 L 7 3 4F RT A3WE 2001091800160 20010918 00160 NM 2001 9 18 DL76L011410 1 20010826 A 2120 ODOR BOEING 767 767332 1382001 NM CABIN DETECTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 182DN 25987 ACFT DIVERTED TO BOS WITH FUMES IN CABIN. CHECKED COMPLETE CABIN, NO TROUBLES FOUND. CKD FOR POPPED C/BS IN COCKPIT AN D E/E. NO DISCREPANCIES. RAN BOTH ENGINES AND LOADED SYSTEMS. NO TROUBLE FOUND. 2 L 7 2 4F RT A1NM 2001091800161 20010918 00161 NM 2001 9 18 DL76L011411 1 20010826 A 2120 ODOR BOEING 767 767332 1382001 NM CABIN DETECTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 182DN 25987 ACRID SMELL IN BUSINESS CLASS, NO SMOKE OR BURNING WAS OBSERVED BY PASSENGERS OR CREW. OCCURRED 20 MINS AFTER T/O SMELL DECREASED AFTER 5 MINS AND GONE UPON LANDING. CHECKED SIDEWALL AND OVERHEAD LIGHTS AND SURROUNDING AREAS, CHECKED UNDE R SEATS AND OPERATION OF SAME. CKD FOR POPPED C/B'S IN COCKPIT AND E/E AREA NONE POPPED RAN ENGS AND LOADED SYSTEMS. N O TROUBLE FOUND, A/C OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2001091800162 20010918 00162 NM 2001 9 18 DL76L011428 1 20010829 A 2913 PUMP BOEING 767 767332 1382001 NM HYDRAULIC SYS FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 188DN 27583 C-HYD PRESS LIGHT ON EICAS AND OVERHEAD PANEL AT GEAR RETRACTION AND REMAINED ON. ALSO ADP PRESS LIGHT REMAINED ON TILL ADP TURNED ON. ADP SWITCH IN AUTO LIGHT CAME ON AGAIN. REPLACED C-HYD SYS PRESS SWITCH S35, REPLACED HYD CONTROL OVER HEAD PANEL, REPLACED AIR DRIVEN HYDRAULIC PUMP AND ALL SYSTEMS OP OK. LEAK CHECKS GOOD. 2 L 7 2 4F RT A1NM 2001091800163 20010918 00163 NM 2001 9 18 DL76P011469 1 20010903 A 7930 CHIP DETECTOR BOEING 767 767332 1382001 NM PWA 4090 PW4090 52119 NE NR 1 ENGINE LEAKING A DALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 143DA 41387 724139 25991 724139 ON CLIMB HAD LOSS OF OIL QTY NR 1 ENG OIL PRESS TO 60 PSI SHUT DOWN ENG. NR 3 BEARING COMP CHIP DETECTOR LEAKING. REPL ACED CHIP DET AND HOUSING. PERFORMED WINDMILL INSP PER M/M, REPLD OIL FILTER. LEAK CHECKS GOOD, NO FURTHER DEFECTS NOT ED, OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E46NE 2001092800066 20010928 00066 CE 2001 9 28 GLBA2001194 1 20010901 A 2120 SEAL BEECH 1900 1900D 1154162 CE RT WING DETERIORATED A GLBA D RETURN TO BLOCK O OTHER CL CLIMB 1 CE 01 211GL UE211 CABIN PRESSURIZATION INOPERATIVE. REPLACED SEAL IN RIGHT WING ROOT, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001091800164 20010918 00164 NE 2001 9 18 RAIA00108009 2 20010809 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE MCAULY 5JFR36 B5JFR36C1103 GL LEFT MALFUNCTIONED A RAIA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 CE 03 550HK 41039 75018 951478 5422-EWR-CREW PERFORMED LEFT ENGINE SHUTDOWN ON SHORT FINAL, RPM ROSE TO 104.9 AND WAS CLIMBING UPON SHUTDOWN. MAINTENA NCE INSPECTED AND PERFORMED FULL POWER RUN IAW ALLIED SIGNAL MM. 2 L 7 2 4T 4 T RT A41NM E18NE 6 C P15NE 2001091800165 20010918 00165 NM 2001 9 18 QXEA0101455 1 20010830 A 5320 STRUCTURE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - DRIP THROUGH, ATTACHED TO NR 7 SEAT TRACK IS CORRODED BETWEEN 187.00 AND 257.00. REPAIRED IAW DASH-8 SRM 51-20-16, PAGE 3, TABLE 1, SHEET 2. 2 H 7 2 4T RT A13NM 2001091800166 20010918 00166 NM 2001 9 18 QXEA0101468 1 20010907 A 5243 ACCESS DOOR DHAV DHC8 DHC8* NM HYDRAULIC BAY DEPARTED A QXEA A UNSCHED LANDING D INFLIGHT SEPARATION CR CRUISE 1 NM 09 405QX 4047 SEA - LEFT HYDRAULIC ACCESS DOOR CAME OFF IN FLIGHT. INSTALLED NEW LEFT HYDRAULIC ACCESS DOOR IAW EA 6-54-06, DATED 9-7- 01. 2 H 7 2 4T RT A13NM 2001091800167 20010918 00167 NM 2001 9 18 QXEA0101469 1 20010908 A 3350 82520977001 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN OUT OF POSITION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 SEA - EMERGENCY FLOOR LIGHTS BY ROW ONE ARE FALLING OUT OF TRACK. REMOVED AND REPLACED FORWARD EMERGENCY FLOOR LIGHT STR IP. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001091800168 20010918 00168 NM 2001 9 18 QXEA0101470 1 20010904 A 3234 860TS09Y00 CONTROL PANEL DHAV DHC8 DHC8* NM COCKPIT MALFUNCTIONED A QXEA K NONE O OTHER CL CLIMB 1 NM 09 402QX 999 999 4032 SEA - AFTER RAISING GEAR ON TAKE OFF, GEAR BEGAN TO CYCLE UP AND DOWN. PUT GEAR DOWN THEN BACK UP. THEY STAYED IN THE WH EEL WELLS UP AND LOCKED, THEN NORMAL GEAR OPERATIONS. REMOVED AND REPLACED LANDING GEAR CONTROL PANEL. OPERATIONAL CHECK IS GOOD IAW 32-31-00-710-801. 2 H 7 2 4T RT A13NM 2001091800169 20010918 00169 EA 2001 9 18 QXEA0101471 1 20010906 A 5754 RETAINER CNDAIR CL600 CL600* EA L/E SLAT CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX - CRACK ON SLAT SEAL RETAINER OUTBOARD SEGMENT WING STATION 180.00 TO APPROXIMATELY 0.00 CHORD. STOP DRILLED CRACK I AW EA R-57-01. 2 L 7 2 4F RT A21EA 2001091800170 20010918 00170 EU 2001 9 18 QXEA0101473 1 20010827 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - FRAME 2220 LEFT BETWEEN STRINGERS 53 AND 57 HAS A TEMPORARY REPAIR. REPLACED SKIN AND STRINGER ASSEMBLY IAW F28 SR M 51-31-01 2 L 7 2 4F RT A20EU 2001091800171 20010918 00171 EU 2001 9 18 QXEA0101474 1 20010828 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - THE REPAIR DOUBLER FOR THE REPAIR AT FRAME 2220 AND STRINGER 18 EXCEEDS 20 PERCENT OF SKIN PANEL. REPLACED SKIN PA NEL AND STRINGER ASSEMBLY IAW F-28 SRM 51-31-01 2 L 7 2 4F RT A20EU 2001091800172 20010918 00172 EU 2001 9 18 QXEA0101475 1 20010828 A 5710 STRUCTURE FOKKER F28 F28MK4000 4990810 EU LT WING LEAKING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX -FUEL LEAKING FROM HI LOCK, BOTTOM OF LEFT WING 13 INCHES FORWARD OF LEFT LANDING GEAR FORWARD TRUNNION. REMOVED AND REPLACED HI LOCKS AND SEALED SAME IAW F28 SRM 51-30-02. SEALED HI LOCK COLLARS IAW F28 MANUAL 28-11-00 PARAGRAPHS 4A,5A ,B,C AND D. 2 L 7 2 4F RT A20EU 2001091800173 20010918 00173 EU 2001 9 18 QXEA0101476 1 20010831 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PCDX - STRINGER 20 AT FRAME 2220 HAS DAMAGE AT END OF STRINGER. REPAIRED DAMAGE IAW F28 SRM 53-02-08 PAGE 6. 2 L 7 2 4F RT A20EU 2001091800174 20010918 00174 EU 2001 9 18 QXEA0101477 1 20010831 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE BENT A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - STRINGER 17 IS BENT ON FORWARD SIDE OF FRAME 2220 STRINGER TIE AND STRINGER. REPAIRED IAW SRM 53-02-01 AND SRM 51- 30-02. 2 L 7 2 4F RT A20EU 2001091800175 20010918 00175 EU 2001 9 18 QXEA0101478 1 20010829 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - STRINGER 20 IS DAMAGED BETWEEN FRAME 1600 AND FRAME 1890. REMOVED DAMAGED PORTION OF STRINGER AND REPAIRED IAW F28 SRM 53-02-05. 2 L 7 2 4F RT A20EU 2001091800176 20010918 00176 EU 2001 9 18 QXEA0101479 1 20010829 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - STRINGER 21A IS DAMAGED BETWEEN FRAME 1890 AND 2220. REPAIRED STRINGER 21A IAW F-28 SRM 53-02-05. 2 L 7 2 4F RT A20EU 2001091800177 20010918 00177 WP 2001 9 18 MWEA011272 1 20010915 A 5310 99115993 WEB DOUG DC9 DC932 3022066 WP NOSE WHEEL WELL CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 FOUND MINOR CHAFE ON WEB IN NOSE WELL. -- BLENDED CHAFE AND REPAIRED WITH DOUBLER REPAIR. 2 L 7 2 4F A6WE 2001091800178 20010918 00178 EU 2001 9 18 QXEA0101480 1 20010829 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - SKIN DAMAGE BETWEEN FRAME 1600 AND 2200 AND STRINGERS 18 AND 21A. REPAIRED IAW F28 SRM 53-02-08, 51-31-01, AND 53- 12-02. 2 L 7 2 4F RT A20EU 2001091800179 20010918 00179 EU 2001 9 18 QXEA0101482 1 20010829 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - STRINGER TIE AT FRAME 2220 AND STRINGER 18 IS DAMAGED. REMOVED AND REPLACED STRINGER TIES IAW F28 SRM 53-02-05. 2 L 7 2 4F RT A20EU 2001091800180 20010918 00180 EU 2001 9 18 QXEA0101483 1 20010829 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - STRINGER 19 DAMAGED BETWEEN FRAME 1600 AND FRAME 1890. REMOVED DAMAGED SECTION OF STRINGER AND REPAIRED IAW F28 SR M 53-02-05. 2 L 7 2 4F RT A20EU 2001091800181 20010918 00181 EU 2001 9 18 QXEA0101484 1 20010829 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - FRAME CASTELLATION CRACKED ON FRAME 1285 BETWEEN STRINGERS 17 AND 18. REMOVED DAMAGED AREA AND REPAIRED PER F28 SR M 53-02-13. 2 L 7 2 4F RT A20EU 2001091800182 20010918 00182 EU 2001 9 18 QXEA0101485 1 20010903 A 5720 CLIP FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX- CORROSION FOUND ON CLIPS AT LOWER END OF NR 2, NR 3 NR 4 RIBS ON INBOARD WALL OF LEFT SIDE OF COLLECTOR FUEL TANK. REMOVED CORROSION AND REPLACED HI LOCKS AND TREATED AREA IAW F28 SRM 51-01-01 AND SRM 51-10-04. 2 L 7 2 4F RT A20EU 2001091800183 20010918 00183 NM 2001 9 18 QXEA0101486 1 20010908 A 5512 SKIN DHAV DHC8 DHC8202 2809007 NM HORIZ STAB DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - DENT IN LOWER SKIN OF HORIZONTAL STAB JUST AFT OF FORWARD SPAR AND JUST OUTBOARD OF RIB 11. REPAIRED IAW HORIZON A IR EA 2-55-59. 2 H 7 2 4T RT A13NM 2001091800184 20010918 00184 NM 2001 9 18 QXEA0101487 1 20010901 A 2730 PUSHROD DHAV DHC8 DHC8202 2809007 NM ELEVATOR EXCESS PLAY A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - RIGHT-HAND ELEVATOR TRIM PUSH ROD HAS APPROXIMATELY .020 INCH RADIAL PLAY ON ROD BEARING AT IDLER ARM END. REPAIRE D IAW DASH-8 MM 27-36-00. 2 H 7 2 4T RT A13NM 2001091800185 20010918 00185 NM 2001 9 18 QXEA0101488 1 20010903 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NR 4 SEAT TRACK HAS NUMEROUS DISCREPANCIES. REPLACED IAW DASH-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001091800186 20010918 00186 NM 2001 9 18 QXEA0101489 1 20010901 A 5320 ANGLE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - WING SPAR TO FUSELAGE RIGHT-HAND FORWARD CLOSING ANGLE HAS CRACK IN ANGLE RADIUS. REPAIRED IAW HORIZON AIR EA 2-53 -332, STEP 1. 2 H 7 2 4T RT A13NM 2001091800187 20010918 00187 NM 2001 9 18 QXEA0101490 1 20010904 A 5414 PLATE DHAV DHC8 DHC8202 2809007 NM LT NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - BOTTOM METAL PIECE IN AFT HOT SECTION OF NACELLE HAS HOLE CHAFE THROUGH JUST BELOW LEFT-HAND BOTTOM NACELLE BOTTOM STRUT. REPAIRED IAW DAHS-8 SRM 51-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001091800188 20010918 00188 NM 2001 9 18 QXEA0101491 1 20010904 A 5414 PLATE DHAV DHC8 DHC8202 2809007 NM NR 1 NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - BOTTOM OF NR 1 NACELLE HOT SECTION FORWARD BOTTOM LIP IS CRACKED AND MISSING RIVETS. REPAIRED IAW DASH-8 SRM 51-40 -00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001091800189 20010918 00189 NM 2001 9 18 QXEA0101492 1 20010830 A 5320 STIFFENER DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - NOSE LANDING GEAR DOOR MECHANISM INBOARD TOGGLE LINK AT OUTBOARD TOGGLE LINK PIVOT BOLT, COTTER PIN CHAFING BULKHE AD STIFFENER. REPAIRED IAW DAHS-8 SRM 51-20-11, PAGE 7. 2 H 7 2 4T RT A13NM 2001091800190 20010918 00190 NM 2001 9 18 QXEA0101493 1 20010905 A 5522 SKIN DHAV DHC8 DHC8202 2809007 NM ELEVATOR SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - 3 SCRATCHES ON LEFT-HAND ELEVATOR LEADING EDGE AT YH45.0. REPAIRED IAW DASH-8 SRM 51-20-26. 2 H 7 2 4T RT A13NM 2001091800191 20010918 00191 NM 2001 9 18 QXEA0101494 1 20010902 A 5720 BRACKET DHAV DHC8 DHC8202 2809007 NM LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - LEFT WING ISOLATION VALVE LOWER ATTACH BRACKET HAS A CRACK. REPLACED IAW DASH-8 200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001091800192 20010918 00192 NM 2001 9 18 QXEA0101495 1 20010902 A 5320 BRACKET DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - RIGHT ISOLATION CHECK VALVE DUCT LOWER ATTACH BRACKET HAS A CRACK. REPAIRED IAW DASH-8 200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001091800193 20010918 00193 EU 2001 9 18 DHL2001363023 1 20010914 A 5270 WARNING SYSTEM AIRBUS 300 A300B4203 3930306 EU COCKPIT MALFUNCTIONED A DHLA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 363DH 85 ON TAXI OUT THE DOORS LIGHT ON THE MWP ILLUMINATED AND WOULD NOT TEST. CYCLED MAIN CARGO DOOR PERFORMED DOOR SYS TEST IA W M/M 52-71-00 OPS CHECKED OK. 2 L 7 2 4F RT A35EU 2001091800194 20010918 00194 EU 2001 9 18 DHL2001364025 1 20010915 A 7830 THRUST REVERSER AIRBUS 300 A300B4203 3930306 EU NR 2 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 ON WEEKLY CHECK - NR 2 ENGINE I/B REVERSER, AFT FIN AREA HAS A CRACK. REMOVED AFT FIN FROM NR 2 ENGINE I/B REVERSER FOR REPAIR IAW A-300 SRM 51-30-29 SENT FOR WELDING. REINSTALLED SERVICEABLE AFT FIN FAIRING ON NR 2 ENGINE I/B REVERSER IAW A-300 SRM 51-30-29. 2 L 7 2 4F RT A35EU 2001091800195 20010918 00195 EU 2001 9 18 DHL2001366026 1 20010829 A 2612 CONNECTOR AIRBUS 300 A300B4203 3930306 EU NR 1 ENGINE DIRTY A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 366DH 249 NR 1 ENG A FIRE LOOP TEST. CLEANED A LOOP CONNECTIONS AT PYLON SYSTEM OPS CKS GOOD IAW A300 MM 26-12-00. 2 L 7 2 4F RT A35EU 2001091800196 20010918 00196 EU 2001 9 18 DHL2001366028 1 20010915 A 2560 SMOKE BARRIER AIRBUS 300 A300B4203 3930306 EU CABIN TORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 366DH 249 SMOKE CURTAIN IS TORN AWAY FROM 6 CAMLOCKS ON BOTTOM OF THE CURTAIN. INSTALLED SMOKE BARRIER IAW A300 CMM 25-50-02. 2 L 7 2 4F RT A35EU 2001091800197 20010918 00197 NM 2001 9 18 UPS01236733 1 20010830 A 5320 STIFFENER BOEING 727 72751C 1384015 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:N/A RT MLG ACT BEAM SUPPORT PANEL. FWD STIFFENER CRACKED AT INBD HINGE. REPAIRED CRACKED STIFFENER RT ML G ACT BEAM SUPPORT PANEL PER B727 SRM 51-40-3 2 L 7 3 4F A3WE 2001091800198 20010918 00198 NM 2001 9 18 UPS01236752 1 20010831 A 5753 FLAP BOEING 727 72725C 138400H NM RT WING DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE:W/E RIGHT WING I/B T/E MID-FLAP HAS 3 X 15 INCH DELAMINATION. REMOVED AND REPLACED FLAP IAW MM27-51-03 A ND TASK CARD 1 259 2 L 7 3 4F A3WE 2001091800199 20010918 00199 NM 2001 9 18 UPS01236753 1 20010830 A 5311 FRAME BOEING 727 727172C 1384058 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 916UP 19808 INSPECTION TYPE:C CRACK ON FRAME WEB BS 807 RBL 48 APPROX BETWEEN JIG HOLE AND LIGHTNING HOLE. REPAIR CARRIED OUT IAW SR M 51-40-2 2 L 7 3 4F A3WE 2001091800201 20010918 00201 NM 2001 9 18 UPS01236766 1 20010830 A 3350 1000679 LIGHT BOEING 727 72721C 138400M NM CABIN DEFECTIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 INSPECTION TYPE:PFLT EXIT LIGHTS STAY ON IN ARMED POSITION. REPLACED LIGHT ASSEMBLY 2 L 7 3 4F A3WE 2001091800203 20010918 00203 NM 2001 9 18 UPS01236772 1 20010905 A 3350 1000679 LIGHT BOEING 727 72722C 138400F NM COCKPIT DOOR WILL NOT TEST A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHT AT COCKPIT DOOR WILL NOT TEST. R&R LIGHT ASSY WITH NEW BATTERIES, OPS CHECK K PER MM 33-50-01. 2 L 7 3 4F A3WE 2001091800204 20010918 00204 NM 2001 9 18 UPS01236778 1 20010825 A 5230 65196701 STOP FITTING BOEING 727 72722C 138400F NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C CRACK FOUND ON DOOR STOP AT LWR AFT CORNER OF FWD PIT DOOR. REPLACED CRACKED FITTING IAW B727-5230-003 2. 2 L 7 3 4F A3WE 2001091800205 20010918 00205 NM 2001 9 18 UPS01236779 1 20010827 A 5753 652163230 FLAP BOEING 727 72722C 138400F NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:AD SUSPECT CORROSION BETWEEN SKIN MIDSPAR OF RT INBD MIDFLAP WBL130 APPROX. CORROSION FOUND TO BE OUT OF LIMITS, FLAP REPLACED IAW TC 1259 2 L 7 3 4F A3WE 2001091800206 20010918 00206 NM 2001 9 18 UPS01236780 1 20010828 A 5315 FLOORBEAM BOEING 727 727172C 1384058 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 916UP 19808 INSPECTION TYPE:C ON INSPECTION OF TOILET AREA, CORROSION FOUND ON FLOORBEAM TOP CAP BS 344 LBL 0. FLOORBEAM REPAIRED IA W SRM 53-10-08 2 L 7 3 4F A3WE 2001091800207 20010918 00207 NM 2001 9 18 UPS01236781 1 20010823 A 5753 6521795U284 FAIRING BOEING 727 727172C 1384058 NM T/E FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 916UP 19808 INSPECTION TYPE:C D-203210, RT I/B FLAP TRACK FAIRING CRACKED, INTERIM REPAIR PER B727-5720-13399A, PERM REPAIR AT NEXT C CHECK. CRACKED RIB REPLACED IAW DWG 65-21795 2 L 7 3 4F A3WE 2001091800209 20010918 00209 WP 2001 9 18 ZW0A0108306 1 20010905 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT FOUND FLOOR SUPPORT ON FLOOR FRAME 1309, LBL 18 INCHES TO RBL 18 IN, HAD CORROSION. FABRICATED NEW PART PER SPM 6-70-01. 2 L 7 2 4F RT A6WE 2001091800210 20010918 00210 WP 2001 9 18 ZW0A0108307 1 20010905 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT THE LT FLOOR TRACK FLANGE HAD CORROSION BETWEEN STA 1079 AND 1220. REMOVED AND REPLACED CORRODED T RACK PER SRM 51-01, PAGE 1 ITEM C. REMOVED AND REPLACED AFT SPLICE PER SRM 51-01 PAGE 1 ITEM C. INSTALLED FWD SPLICE P ER SRM 53-05, FIG 4G. 2 L 7 2 4F RT A6WE 2001091800211 20010918 00211 WP 2001 9 18 ZW0A0108308 1 20010905 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT FOUND CORROSION IN FLOOR SUPPORT AT STA 180, RBL 10 INCHES TO RBL 31 IN. FABRICATED NEW FLOOR SUPP ORT PER SPM 6-70-01. INSTALLED PER SRM 51-30-0. 2 L 7 2 4F RT A6WE 2001091800212 20010918 00212 WP 2001 9 18 ZW0A0108309 1 20010906 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT FOUND FWD CABIN SERVICE DOOR THRESHOLD SILL AND MEMBRANE HAD CORROSION, STA 160 AND LONGERON 18R, T O STA STA 200. REPLACED MEMBRANE AND THRESHOLD SILL. INSTALLED FASTENERS PER SRM 51-30-2 AND SRM 51-30-5. 2 L 7 2 4F RT A6WE 2001091800213 20010918 00213 WP 2001 9 18 ZW0A0108310 1 20010906 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT FOUND MAIN CABIN FLOOR SUPPORT CORRODED AT LBL 18, STA 1309 TO 1352. REPLACED FLOOR SUPPORT PER SR M 51-30-1. 2 L 7 2 4F RT A6WE 2001091800214 20010918 00214 WP 2001 9 18 ZW0A0108311 1 20010906 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT FOUND NUMBER 3 CABIN FLOOR TRACK WITH SEVERAL AREAS OF CORROSION FROM STA 1070 TO 1308. REPLACED F LOOR TRACK PER SRM 53-05, FIG 4F, SHEET 1. 2 L 7 2 4F RT A6WE 2001091800215 20010918 00215 WP 2001 9 18 ZW0A0108312 1 20010907 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT ON LT SIDE OF CABIN FOUND CUSP MEMBRANE WITH CORROSION BETWEEN STA 1174 AND 1193, WATER LINE 200, L ONGERON 18L. REMOVED CORROSION PER SPM 6-80-01. REPLACED MEMBRANE PER SRM 51-70-4. 2 L 7 2 4F RT A6WE 2001091800216 20010918 00216 WP 2001 9 18 ZW0A0108313 1 20010907 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR SUPPORT FROM STA 170 TO 200, RBL 44. REPLACED FLOOR SUPPORT PER SPM 6-70-01. 2 L 7 2 4F RT A6WE 2001091800217 20010918 00217 WP 2001 9 18 ZW0A0108314 1 20010907 A 5320 SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT ON FWD CABIN FLOOR, THE DOOR ANGLE AT STA 160 TO 200, LBL 54, HAD CORROSION IN NUT PLATE HOLES, AND AT TWO RIVNUTS INSTALLED. FABRICATED NEW SUPPORT. 2 L 7 2 4F RT A6WE 2001091800218 20010918 00218 WP 2001 9 18 ZW0A0108315 1 20010906 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 911TW 49182 DURING CHECK-C MAINT FOUND CORROSION ON AFT TOP OF FORMER LOCATED 9 INCHES LBL TO 21 IN LBL. REMOVED CORROSION FROM FOR MER STA 1322, LBL 9 IN TO LBL 21 IN AND SPLICED NEW SECTION LONGERON 29L TO 29R, PER SRM 53-03 FIG 2A. 2 L 7 2 4F A6WE 2001091800219 20010918 00219 WP 2001 9 18 ZW0A0108316 1 20010910 A 5210 BEAM DOUG DC9 DC982 3022082 WP L1 DOOR CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 911TW 49182 DURING CHECK-C MAINT ON THE FWD LT PASSENGER DOOR, THE NR 6 DOOR BEAM WAS CRACKED 4 INCHES BELOW BAYONET FITTING. REPLA CED THE NR 6 BEAM PER MM AND SRM 51-00, PAGE 27 ITEM B. 2 L 7 2 4F A6WE 2001091800220 20010918 00220 WP 2001 9 18 ZW0A0108317 1 20010907 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 911TW 49182 DURING CHECK-C MAINT FOUND CORROSION ON RT FLOOR MEMBRANE AT STA 1297 TO 1309, BETWEEN RBL 44 IN AND RBL 54 IN TRACKS. INSTALLED REPAIRED WEB PER SRM 53-05, FIG 96. 2 L 7 2 4F A6WE 2001091800221 20010918 00221 WP 2001 9 18 ZW0A0108318 1 20010908 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 911TW 49182 DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT RBL 44, STA 180 TO 200. INSTALLED NEW FLOOR SUPPORT PER SRM 51 -30-7 AND SPM 6-70-01. 2 L 7 2 4F A6WE 2001091800222 20010918 00222 WP 2001 9 18 ZW0A0108401 1 20010910 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 926TW 49356 DURING CHECK-C MAINT A FWD CABIN FLOOR ANGLE HAD CORROSION AT RBL 5 INCHES TO LBL 5, STA 200. FOUND CORRODED BEYOND LIM ITS AND FABRICATED NEW SUPPORT. INSTALLED SUPPORT PER SRM 51-30-2 PAGE 2, FABRICATED PARTS PER SPM 6-70-01, PAGE 1 TO 3. 2 L 7 2 4F A6WE 2001091800223 20010918 00223 WP 2001 9 18 ZW0A0108501 1 20010911 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT FOUND FLOOR TRACK RBL 54 CORRODED AT STA 229 TO 796. REPLACED AND SPLICED IN NEW TRACK PER SRM 51- 10-3, 51-10-4, 51-30-2, 51-30-5, AND SPM 6-70-01. 2 L 7 2 4F RT A6WE 2001091800224 20010918 00224 WP 2001 9 18 ZW0A0108601 1 20010914 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 905TW 49157 THE EMERGENCY EXIT SIGN AT THE LT OVERWING EXIT, AND THE EMERGENCY CEILING LIGHT BETWEEN NUMBER 4 GALLEY AND THE AFT AIR STAIR DOOR, WERE INOPERATIVE. REPLACED THE LAMP PN 1315 FOR THE OVERWING EXIT, AND REPLACED THE POWER SUPPLY PN 5822-2 FOR THE CEILING LIGHT. 2 L 7 2 4F A6WE 2001091800225 20010918 00225 SO 2001 9 18 ASOA01144 1 20010821 A 3350 D36604001 BATTERY PACK EMB 120 EMB120 3260201 SO CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 241AS 19230 120065 DURING GROUND INSPECTION MAINTENANCE, FOUND THE FORWARD SECTION OF EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED EMERGENCY BATTERY PACK. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001091800226 20010918 00226 SO 2001 9 18 SIMA200123002 1 20010818 A 5600 163500109 WINDSHIELD EMB 145 EMB145LR SO COCKPIT BROKEN A SIMA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 630AE 145132 MTY - FLT 3494 - DURING FLIGHT, THE CAPTAINS WINDSHIELD SHATTERED. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSH IELD IAW EMB MM 56-10-01. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001091800227 20010918 00227 EU 2001 9 18 SIMA200124209 1 20010829 A 5300 EPNE95300013020 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 538AT 538 SAW - DURING CPCP4 INSPECTION, FOUND CORROSION ON THE LEFT AFT INBOARD, LEFT AFT OUTBOARD AND RIGHT FLIGHT ATTENDANT SEA T TRACKS. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW EO E2-53-115R1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001091800228 20010918 00228 EU 2001 9 18 USAAF01068 1 20010828 A 3350 59257 INVERTER FOKKER F28 F28MK0100 4990807 EU PAX CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 885US 11345 CLT - THE EMERGENCY FLOOR TRACK LIGHTING BETWEEN ROWS 9-16 WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE FLOOR LIGHTI NG OVERWING EXIT MARKER STATIC INVERTER. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT 2001091800229 20010918 00229 EU 2001 9 18 USAAF01070 1 20010831 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU PAX CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 891US 11366 IND - THE EMERGENCY LIGHTS WERE OUT IN THE MID-CABIN AREA MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT 2001091800230 20010918 00230 EU 2001 9 18 USAABA01009 1 20010828 A 3350 321430 BATTERY AIRBUS 330 A330323 EU R2 DOOR INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 671UW 323 PHL - FOUND THE BATTERY AT EPSU 2 SHOWING A FAULT. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A46NM 2001091800231 20010918 00231 NM 2001 9 18 USAASB01244 1 20010829 A 3200 189929 SENSOR BOEING 737 7374B7 1384702 NM RT MLG W/W FAILED A USAA B A EMER. DESCENT UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 449US 24893 IND - FLT 338 - ON CLIMB-OUT FROM ORD, EN ROUTE TO CLT, WHEN AIRCRAFT WAS CLEARED TO CLIMB TO FL290 FROM FL250, THE CABI N PRESSURIZATION ROSE TO 9,500 FEET. AIRCRAFT LOST INFLIGHT SENSING AND PRESSURIZATION COULD NOT BE CONTROLLED IN AUTO MODE. FLIGHT ALSO LOST AUTO THROTTLE, TRANSPONDER, ACARS INFLIGHT FUNCTION AND HAD AN ENGINE LOW IDLE LIGHT. FLIGHT DE SCENDED TO FL100 AND DIVERTED TO IND. FLIGHT LANDED WITHOUT FURTHER INCIDENT WITH NO EMERGENCY BEING DECLARED. MX CHEC KED AIR/GRD SAFETY SWITCHES FOR SECURITY. PERFORMED SATISFACTORY CIRCUIT CARD TEST FOR THE M990 AND M991 CIRCUIT CARDS PER MM 32-09-20. REPLACED R280 REALY (P/N BACR13CG2AB). AIRCRAFT RETURNED TO NORMAL AIR/GRD CONFIGURATION. AIRCRAFT O 2 L 7 2 4F RT A16WE 2001091800232 20010918 00232 NM 2001 9 18 USAASB01229 1 20010812 A 3200 189929 SENSOR BOEING 737 7374B7 1384702 NM MLG FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 782AU 25021 CLT - FLT 1919 - AFTER TAKEOFF FROM CLT, EN ROUTE TO SJU, THE CAPTAIN REPORTED THE AIRCRAFT ACTED AS THOUGH THE FLIGHT/G ROUND SWITCH WAS STUCK IN THE GROUND MODE. THE AIRCRAFT WOULD NOT PRESSURIZE AND THE TRANSPONDER AND AUTO THROTTLE WAS INOPERATIVE. NO CIRCUIT BREAKERS WERE TRIPPED SO THE CAPTAIN ELECTED TO RETURN TO FIELD AT CLT WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND THE S105 GROUND SAFETY S ENSOR INOPERATIVE. REMOVED AND REPLACED SENSOR PER MM 32-09-01. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001091800233 20010918 00233 WP 2001 9 18 USAA011179 1 20010816 A 5200 SKIN DOUG DC9 DC981 3022081 WP CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 809US 53825 48041 TPA - FOUND SKIN CRACKED 3 INCHES, AFT END OF DOOR HOLD OPEN HOOK OPENING DOOR SKIN. INSTALLED DOUBLER PER SRM 52-05 FI G 20A. (M) 2 L 7 2 4F A6WE 2001091800234 20010918 00234 WP 2001 9 18 USAA011128 1 20010821 A 5200 SKIN DOUG DC9 DC981 3022081 WP CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 811US 54397 48043 CLT - FOUND SKIN CRACKED, SKIN ON AFT ENTRANCE DOOR L2 AROUND HOLE OPEN HOOK CUTOUT. INSTALLED DOUBLER PER E NR 72317. (M) 2 L 7 2 4F A6WE 2001091800235 20010918 00235 SO 2001 9 18 ASOA01142 1 20010820 A 3350 1317 BULB EMB 120 EMB120 3260201 SO CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 243AS 120072 DURING SCHEDULED MAINTENANCE IN TXK, THE RIGHT OVERWING FORWARD EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED RIGHT OVERWING FORWARD EMERGENCY EXIT LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. ( M) 2 L 7 2 4T RT A31SO 2001091800236 20010918 00236 EA 2001 9 18 ASOA01143 1 20010820 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 870AS 7530 DURING GROUND INSPECTION AT ATL, CRWE REPORTED OVERHEAD EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED B URNED OUT BULB IN THE CEILING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2001091800237 20010918 00237 EU 2001 9 18 SIMA200124208 1 20010829 A 5300 S536780090002 FLOOR SUPPORT AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 536AT 536 SAW - DURING CPCP4 INSPECTION, FOUND CORROSION ON THE LT FLOOR SUPPORT BETWEEN FRAMES 36 AND 38. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-25-02. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001091800238 20010918 00238 EU 2001 9 18 SIMA200124207 1 20010829 A 5300 EPNE95300013025 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 536AT 536 SAW - DURING CPCP4 INSPECTION, FOUND CORROSION ON THE LEFT AFT OUTBOARD, RIGHT AFT OUTBOARD, LEFT F/A, RT F/A AND LT AFT CARGO SEAT TRACKS. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW EO E2-53MR-115. THE AIRCRAFT WAS RETURNED TO SERVICE . (M) 2 H 7 2 4T RT A53EU 2001091800239 20010918 00239 EU 2001 9 18 SIMA200124206 1 20010829 A 5315 S53672408254 FLOORBEAM AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 536AT 536 SAW - DURING CPCP4 INSPECTION, FOUND CORROSION ON FLOORBEAMS 36, 38 AND 39. THE FLOORBEAMS WERE REMOVED AND REPLACED IA W ATR72 SRM 51-25-01, 51-25-04 AND 51-25-02. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001091800240 20010918 00240 EU 2001 9 18 SIMA200124205 1 20010829 A 5300 S5367131831801 SILL AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 536AT 536 SAW - DURING CPCP4 INSPECTION, FOUND CORROSION ON PASSENGER ENTRY SILL AND THE SERVICE DOOR SILL PLATES. THE SILLS WERE REMOVED AND REPLACED IAW ATR72 SRM 51-25-01 AND 51-25-02. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001091800241 20010918 00241 EU 2001 9 18 SIMA200124204 1 20010829 A 5300 S536780092002 FLOOR SUPPORT AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 242AT 242 SAW - DURING CPCP2 INSPECTION, FOUND CORROSION ON THE LEFT AND RIGHT FLOOR SUPPORTS FROM FRAME 36 TO FRAME 38. THE FLOO R SUPPORTS WERE REMOVED AND REPLACED IAW ATR SRM 51-25-01 AND 51-25-02. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001091900018 20010919 00018 EA 2001 9 19 COMA0160722 1 20010917 A 5300 601R3866949 DOUBLER CNDAIR CL600 CL6002B19 EA F.S.310.00 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 696CA 11964 7141 THE DOUBLER FORWARD OF THE SERVICE DOOR IS CORRODED P/N 601R38669-49.REMOVED AND REPLACED DOUBLER FORWARD OF SERVICE DOO R WITH NEW P/N 601R38669-49 I/A/W WVAC EO 601R-53-2719. 2 L 7 2 4F RT A21EA 2001091900024 20010919 00024 NM 2001 9 19 ZW0A0108701 1 20010914 A 3350 251005 FUSE BOEING 767 7673Q8 NM ROW 11 RH A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 634TW 28132 THE EGRESS LIGHT WAS INOPERATIVE AT CABIN ROW 11, RH SIDE OF AIRCRAFT. REPLACED THE FUSE ON BATTERY CHARGER. CHECK-C 10 -25-00 LAX. --CLOSED-- 2 L 7 2 4F RT A1NM 2001091900033 20010919 00033 EA 2001 9 19 COMA0110142 1 20010917 A 3260 TQD120205401 PROXIMITY SWITCH CNDAIR CL600 CL6002B19 EA NOSE GEAR FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SO 01 269CA 1263 FLIGHT #5041. DURING CLIMB OUT OF MCO THE GEAR HANDLE RELEASE BUTTON HAD TO BE USED TO RETRACT THE GEAR, IN ADDITION WH EN THE FLAPS WERE RETRACTED RECEIVED A T/O AURAL WARNING.REPLACED THE NOSE LANDING GEAR PROXIMITY SWITCH AND ADJUSTED TH E CENTERING CAM. 2 L 7 2 4F RT A21EA 2001091900040 20010919 00040 EA 2001 9 19 COMA0160723 1 20010917 A 5300 60034017373 ANGLE CNDAIR CL600 CL6002B19 EA FS 280.00 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 969CA 11964 7141 THE VERTICAL J ANGLE CLIP LOCATED INSIDE OF CBP1 AT LBL 9 L/H SIDE WAS FOUND CRACKED.REMOVED AND REPLACED VERTICAL J ANG LE CLIP INSIDE OF CBP1 WITH NEW ANGLE P/N 600-34017-723S I/A/W WVAC E.O. 601R-53-2720. 2 L 7 2 4F RT A21EA 2001091900042 20010919 00042 EA 2001 9 19 COMA0160724 1 20010917 A 5300 60034017351 ANGLE CNDAIR CL600 CL6002B19 EA FS 280.00 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 969CA 11964 7141 THE FORWARD J ANGLE AT F.S. 280.00 BETWEEN LBL9 AND RBL9 IS CORRODED.REMOVED AND REPLACED FORWARD J ANGLE AT F.S. 280.00 BETWEEN LBL9 AND RBL9 WITH NEW P/N 6000-34017-351 ANGLE I/A/W WVAC EO 601R-53-2718. 2 L 7 2 4F RT A21EA 2001091900043 20010919 00043 EA 2001 9 19 COMA0160725 1 20010917 A 5300 601R31527221 ANGLE CNDAIR CL600 CL6002B19 EA FS 310.00 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 969CA 11964 7141 THE THRESHOLD SUPPORT ANGLE AT THE PASSENGER DOOR IS CORRODED.REMOVED CORRODED THRESHOLD SUPPORT ANGLE. FABED NEW THRESH OLD SUPPORT ANGLE AND INSTALLED I/A/W WVAC EO 601R-53-2717. 2 L 7 2 4F RT A21EA 2001091900044 20010919 00044 EA 2001 9 19 COMA0160726 1 20010917 A 5300 601R3114879 THRESHOLD CNDAIR CL600 CL6002B19 EA FS 310.00 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 969CA 11964 7141 THE THRESHOLD/SILL PANEL FORWARD OF THE SERVICE DOOR IS CORRODED.REMOVED CORRODED THRESHOLD AND REPLACED WITH FABED THRE SHOLD I/A/W WVAC EO 601R-53-2716. 2 L 7 2 4F RT A21EA 2001091900045 20010919 00045 EA 2001 9 19 COMA0160727 1 20010914 A 5315 601R3117115 ANGLE CNDAIR CL600 CL6002B19 EA FS 484.0 RBL 36 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 949CA 14350 7080 RIGHT SIDE ELEVATER AND RUDDER PULLEY SUPPORT BRACKET AT F.S. 484.0 UNDER FLOOR PANEL 262DRF IS CRACKED.REPAIRED THE RIG HT SIDE ELEVATER AND RUDDER SUPPORT BRACKET AT F.S. 484.0 I/A/W WVAC EO 601R-53-2711A. 2 L 7 2 4F RT A21EA 2001091900046 20010919 00046 WP 2001 9 19 ABXA010481 1 20010830 A 5312 9915558109 ANGLE DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 UPPER OUTBOARD ATTACH ANGLE ON RADIAL 5A, FWD SIDE, WAS FOUND TO BE CRACKED. MAINTENANCE REPLACED THE ATTACH ANGLE IAW A BX EA 53120037-006. 2 L 7 2 4F A6WE 2001091900047 20010919 00047 WP 2001 9 19 ABXA010480 1 20010901 A 5315 995773713 SUPPORT DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 FLOOR SUPPORT AT FUSELAGE STATION 945 WAS FOUND TO BE CORRODED ABOVE LONGERON 30. MAINTENANCE MANUFACTURED AND INSTALLED A SUPPORT SPLICE IAW DRAWING 99577 AND DC-9 SRM. 2 L 7 2 4F A6WE 2001091900048 20010919 00048 WP 2001 9 19 ABXA010477 1 20010830 A 5347 2492584877075T6 TRACK DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 THE CENTER SEAT TRACK AT STATION 237-275 WAS FOUND TO BE CORRODED. MAINTENANCE REPLACED THE AFFECTED SECTION OF SEAT TRA CK IAW DC-9 SRM. 2 L 7 2 4F A6WE 2001091900049 20010919 00049 EA 2001 9 19 COMA0160728 1 20010914 A 5315 601R3117127 ANGLE CNDAIR CL600 CL6002B19 EA FS 484.0 LBL27 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 949CA 14350 7080 LEFT SIDE INBOARD ANGLE AT F.S. 484.0 LBL 27 UNDER FLOOR PANEL 261DLF IS CRACKED.REPAIRED THE ANGLE AT F.S. 484.0 LBL27 I/A/W WVAC EO 601R-53-2711A. 2 L 7 2 4F RT A21EA 2001091900051 20010919 00051 NM 2001 9 19 DL76S011343 1 20010815 A 3230 273T63008 ACTUATOR BOEING 767 767332 1382001 NM RT MLG DEFECTIVE A DALA O OTHER J WARNING INDICATION TO TAKEOFF 1 SO 27 116DL 23275 ON TAKEOFF AFTER GEAR HANDLE RAISED DOOR GEAR LIGHTS REMAINED ILLUMINATED EICS MESSAGE GEAR DISAGREE AND GEAR DOORS WITH HANDLE IN OFF POSITION GREEN RT MAIN LIGHT ON. MAINTENANCE IN PROGRESS. REMOVED AND REPLACED DRAG BRACE ACTUATOR ON T HE RIGHT GEAR. C/W LEAK AND OPERATIONAL CK ALL OK PER MM 32-32-02--4-01. 2 L 7 2 4F RT A1NM 2001091900052 20010919 00052 NM 2001 9 19 DL76S011436 1 20010830 A 2560 20131A BATTERY PACK BOEING 767 767332 1382001 NM CABIN RT SIDE DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 123DN 23437 RT EMERGENCY ESCAPE SQUIB WILL NOT TEST. REPLACED RT BATTERY PACK TEST OK. 2 L 7 2 4F RT A1NM 2001091900053 20010919 00053 EA 2001 9 19 COMA0160729 1 20010914 A 5315 601R3117117 ANGLE CNDAIR CL600 CL6002B19 EA FS 484.0 LBL9 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 949CA 14350 7080 LEFT SIDE INBOARD ANGLE AT F.S. 484.0 LBL 9 UNDER FLOOR PANEL 261CLF IS CRACKED.REPAIRED THE ANGLE AT FS 484.0 LBL9 I/A/ W WVAC EO 601R-53-2711A. 2 L 7 2 4F RT A21EA 2001091900054 20010919 00054 NM 2001 9 19 DL76S011452 1 20010901 A 2560 PT0700300 FLASHLIGHT BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 136DL 23146 FLASHLIGHT INOP FWD AC. REPLACED SAME. 2 L 7 2 4F RT A1NM 2001091900055 20010919 00055 NM 2001 9 19 CALA0100879 1 20010917 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 420 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT STA 420, S24R. THE SKIN WAS REPAIRED IAW SRM 53-00-01, PAGE 18, FIGURE 8. 2 L 7 2 4F RT A16WE 2001091900056 20010919 00056 NM 2001 9 19 CALA0100880 1 20010918 A 5753 SKIN BOEING 737 7373T0 1384582 NM #1 MID FLAP GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND #1 MID FLAP SKIN GOUGED ON L/E AT O/B END. THE GOUGED AREA WAS REMOVED AND FILLER AND DOUBLER WERE INST ALLED IAW SRM 57-53-01. 2 L 7 2 4F RT A16WE 2001091900057 20010919 00057 NM 2001 9 19 CALA0100881 1 20010918 A 5754 SKIN BOEING 737 7373T0 1384582 NM #3 SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND A 4" CRACK IN #3 SLAT SKIN AT I/B L/E. THE CRACKED AREA WAS CUT OUT AND FILLER AND SPLICE PLATE WERE IN STALLED IAW SRM 57-43-01, FIGURE 206. 2 L 7 2 4F RT A16WE 2001091900058 20010919 00058 NM 2001 9 19 CALA0100882 1 20010918 A 5230 SKIN BOEING 737 7373T0 1384582 NM FWD CARGO DR GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND FORWARD CARGO DOOR EXTERNAL SKIN GOUGED AT AFT END OF HANDLE CUTOUT. A DOUBLER WAS INSTALLED IAW SRM 52 -00-01, FIGURE 203. 2 L 7 2 4F RT A16WE 2001091900059 20010919 00059 NM 2001 9 19 CALA0100883 1 20010918 A 5230 SKIN BOEING 737 7373T0 1384582 NM C-1 DOOR GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND C-1 DOOR SKIN GOUGED 11 INCHES FROM BOTTOM AND 21 INCHES FROM FORWARD EDGE. A DOUBLER WAS INSTALLED IAW SRM 52-00-01, FIGURE 203. 2 L 7 2 4F RT A16WE 2001091900060 20010919 00060 NM 2001 9 19 DL777011355 1 20010818 A 2560 257204896 BATTERY BOEING 777 777232 1385232 NM FLASHLIGHT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 860DA 29951 REPLACED FLASHLIGHT BATTERY AT 4L DOOR FOUND BY CREW DURING EMERGENCY EQUIPMENT CHECK. 2 L 7 2 4F RT T00001SE 2001091900061 20010919 00061 NM 2001 9 19 DL777011374 1 20010819 A 2530 72077500 OVEN BOEING 777 777232 1385232 NM R2 GALLEY OVERHEATED A DALA H DEACTIVATE SYST/CIRCUITS M OVER TEMP CR CRUISE 1 SO 27 862DA 29734 FRC-253-13809 LOCATION CABIN 2R OVEN OVERHEATS. FWD TO MCO AND PLACARD PER MEL 25-20-01. PULLED AND COLLARED CBS. OVE N OVERHEATS. THE F/A HAD TO PULL BREAKERS TO SHUTOFF. OVEN LOC 809 NR 2 OVEN. 2 L 7 2 4F RT T00001SE 2001091900062 20010919 00062 NM 2001 9 19 DLM11011357 1 20010818 A 2150 3965202 FLOW VALVE DOUG MD11 MD11 3023602 NM A/C BAY FAILED A DALA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 810DE 48565 ON CLIMBOUT OF ATL NR 1 PACK RUNNING ABOUT 40 DEGREES C HOTTER THAN PACKS 2 AND 3. NR 1 PACK WAS CYCLING ON AND OFF WIT H A FLOW LIGHT. WENT TO MANUAL AND SECURED NR 1 PACK. CFDS FAULTS NR 1 PACK FLOW CONTROL VALVE. REPLACED SAME. LEAK AND OPS CHECK OK. RAN ACC1 RTS. RTS PASSED. 2 L 7 3 4F RT A22WE 2001091900063 20010919 00063 2001 9 19 DLM11011358 4 20010816 A 2210 4059002903 CONTROL PANEL DOUG MD11 MD11 3023602 NM COCKPIT FAILED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 807DE 48478 AFTER T/O, A/P & A/T WOULD NOT ENGAGE. REPLACED GCP PER MM. 2 L 7 3 4F RT A22WE 2001091900065 20010919 00065 NM 2001 9 19 DLM11011359 1 20010818 A 2530 831610405 OVEN DOUG MD11 MD11 3023602 NM AFT GALLEY MALFUNCTIONED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 806DE 48477 AFT GALLEY FWD OVEN GIVING OFF BURNING SMELL. REPLACED OVEN. 2 L 7 3 4F RT A22WE 2001091900066 20010919 00066 WP 2001 9 19 MWEA010768 1 20010517 A 5730 99194701 SKIN DOUG DC9 DC932 3022066 WP STATION XRS 540 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 .067" DENT ON LEFT WING TRAILING EDGE PANEL, DUE TO HAIL. -- FABRICATED TWO ROW ROUND DOUBLER AND INSTALLED. 2 L 7 2 4F A6WE 2001091900067 20010919 00067 NM 2001 9 19 DLM11011362 1 20010819 A 2611 SA308C SMOKE DETECTOR DOUG MD11 MD11 3023602 NM LAVATORY MALFUNCTIONED A DALA K NONE B P SMOKE/FUMES/ODORS/SPARKS NO WARNING INDICATION CR CRUISE 1 SO 27 812DE 48601 LAV F - SMELLED OF CIGARETTE SMOKE BUT NO ALARM. FOUND USED DISCARDED CIGARETTE IN LAV-F WASTE BASKET. NO EVIDENCE OF BURNING GARBAGE. WASTE CONTAINER FIRE BOTTLES CHECK OKAY AND HEAT SENSE INDICATORS ARE NORMAL. AREA UNDER LAV SINK OKA Y. REPLACED OVERHEAD SMOKE DETECTOR AND TESTS OKAY. PERFORMED LAV SMOKE TEST FROM FLT ATTN FWD PANEL AND LAV SMOKE TES T OKAY. 2 L 7 3 4F RT A22WE 2001091900068 20010919 00068 NM 2001 9 19 ABXA010475 1 20010916 A 2910 AE70577778 LINE BOEING 767 767200 1385120 NM DEFECTIVE A ABXA O OTHER K FLUID LOSS CR CRUISE 1 GL 23 783AX 23016 THE RIGHT HYDRAULIC QUANTITY DECREASED TO .35 QT. THEN STABILIZED WITH THE ENGINE DRIVIN PUMP DEPRESSURIZED AND THE ALTE RNATING CURRENT MOTOR PUMP OFF. MAINTENANCE INSPECTED AND FOUND A HOLE IN P/N AE705777-78 HYDRAULIC LINE. THE LINE WAS R EPLACED IAW B767 MM. LEAK CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A1NM 2001091900069 20010919 00069 NM 2001 9 19 ABXA010476 1 20010916 A 2910 AS11510K0324 LINE BOEING 767 767231 1385131 NM RUPTURED A ABXA O OTHER K FLUID LOSS CR CRUISE 1 GL 23 702AX 22566 "C" HYDRAULIC SYSTEM QUANTITY DECREASED TO ZERO, AND THE SYSTEM PRESSURE AND QUANTITY LIGHTS ILLUMINATED. MAINTENANCE IN SPECTED AND REPLACED HYDRAULIC LINE P/N AS115-10K0324. THE SYSTEM WAS SERVICED AND ALL FLIGHT CONTROLS WERE CYCLED SEVER AL TIMES. OPERATION AND LEAK CHECKS WERE SATISFACTORY. 2 L 7 2 4F RT A1NM 2001091900070 20010919 00070 NM 2001 9 19 DLM11011405 1 20010825 A 2120 ODOR DOUG MD11 MD11 3023602 NM CABIN DETECTED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 807DE 48478 ODOR OF BURNING RUBBER IN CABIN DURING CRUISE. UNABLE TO LOCATE OR DUPLICATE. 2 L 7 3 4F RT A22WE 2001091900071 20010919 00071 NM 2001 9 19 DLM11011424 1 20010828 A 2530 72077500 OVEN DOUG MD11 MD11 3023602 NM GALLEY DIRTY A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 804DE 48475 AFT MOST OVEN ON F/O SIDE OF A/C HAD BURNING SMELL WHEN ON. TURNED OFF, SMELL WENT AWAY. FOUND REMNANTS OF MELTED PLAS TIC BAG IN AFT RT OVEN. CLEANED OVEN. INSPECTED OVEN HARNESS AND CONNECTOR. REINSTALLED, OPS OK. NO ABNORMAL SMELL N OTED. HARNESS AND CONNECTOR OK. 2 L 7 3 4F RT A22WE 2001091900072 20010919 00072 NM 2001 9 19 DLM11011425 1 20010828 A 2611 SAAU308C SMOKE DETECTOR DOUG MD11 MD11 3023602 NM LAVATORY DAMAGED A DALA K NONE O OTHER CR CRUISE 1 SO 27 804DE 48475 SMOKE ALARM AFT TOILET CAPT SIDE BATT LOW. DETECTOR DAMAGED. REMOVED AND REPLACED SAME. OPS OK. 2 L 7 3 4F RT A22WE 2001091900073 20010919 00073 NM 2001 9 19 DLM11011439 1 20010831 A 3080 11501281 SENSOR DOUG MD11 MD11 3023602 NM E/E BAY FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 810DE 11C174 48565 AIR RETURN NRT DUE A ICE SENSOR FAIL. REPLACED NR PSC, CHECKS GOOD. 2 L 7 3 4F RT A22WE 2001091900074 20010919 00074 NM 2001 9 19 DLM11011459 1 20010901 A 2530 4110001137 COFFEEMAKER DOUG MD11 MD11 3023602 NM GALLEY DAMAGED A DALA H DEACTIVATE SYST/CIRCUITS M OVER TEMP CR CRUISE 1 SO 27 809DE 48480 TRANSFER FROM CMI - MID GALLEY COFFEEMAKER NR 4 HANDLE INOP. FOUND COFFEEMAKER BAG/POUCH TRAY BOTTOM BURNED/MELTED. RE PLACED SAME. 2 L 7 3 4F RT A22WE 2001091900075 20010919 00075 NM 2001 9 19 DLM11011482 1 20010904 A 3520 80138682 GENERATOR DOUG MD11 MD11 3023602 NM CABIN ACTIVATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 805DE 48476 OXYGEN GENERATOR ACCIDENTLY DEPLOYED AT SEAT 11 C. REPLACED SAME. 2 L 7 3 4F RT A22WE 2001091900076 20010919 00076 NM 2001 9 19 DLM11011483 1 20010904 A 3520 80138682 GENERATOR DOUG MD11 MD11 3023602 NM CABIN ACTIVATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 805DE 48476 OXYGEN GENERATOR ACCIDENTLY DEPLOYED AT SEAT 11 G. REPLACED SAME. 2 L 7 3 4F RT A22WE 2001091900077 20010919 00077 NM 2001 9 19 DLM11011484 1 20010904 A 3520 80138682 GENERATOR DOUG MD11 MD11 3023602 NM CABIN ACTIVATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 805DE 48476 OXYGEN GENERATOR ACCIDENTLY DEPLOYED AT SEATS 55AB. REPLACED SAME. 2 L 7 3 4F RT A22WE 2001091900078 20010919 00078 NM 2001 9 19 DLM11011485 1 20010904 A 3520 80138682 GENERATOR DOUG MD11 MD11 3023602 NM CABIN ACTIVATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 805DE 48476 OXYGEN GENERATOR ACCIDENTLY DEPLOYED AT SEATS 48JH. REPLACED SAME. 2 L 7 3 4F RT A22WE 2001091900079 20010919 00079 NM 2001 9 19 DLM88011347 1 20010816 A 2170 COALESCER BAG DOUG MD88 MD88 3023688 NM A/C BAY DIRTY A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 914DE 49957 BURNING SMELL WHEN ENGINE ANTI-ICE USED. INSPECTED A/C - NTF. PERFORMED DUCT BURNOUT. 2 L 7 2 4F RT A6WE 2001091900080 20010919 00080 NM 2001 9 19 DLM88011363 1 20010819 A 3350 LIGHT DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 984DL 53311 EMERGENCY LIGHT ON SEAT ROW 21DE INOP. RELAMPED, OPS NORMAL. 2 L 7 2 4F RT A6WE 2001091900081 20010919 00081 NE 2001 9 19 DLM88011368 2 20010820 A 7314 PUMP DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE DEFECTIVE A DALA A UNSCHED LANDING R X PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT CL CLIMB 1 SO 27 907DL 33670 49538 718176 ON T/O FROM PWM DURING CLIMBOUT NR 2 ENG ROLLED BACK TO IDLE MOMENTARILY THEN WENT BACK TO CLIMB POWER THEN SHUTDOWN AT APPROX 10,000 FT. DIVERTED TO BGR. REPLACED FUEL PUMP AND CONTROL. 2 L 7 2 4F 4 F RT A6WE E9NE 2001091900082 20010919 00082 NM 2001 9 19 DLM88011379 1 20010821 A 3260 833703 SENSOR DOUG MD88 MD88 3023688 NM NLG MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 920DL 49644 NOSE GEAR UNSAFE LIGHT CAME ON AFTER T/O. LIGHT WENT OUT AFTER AUX PUMPS TURNED ON. REPLACED D-132 LOCK SENSOR PER M/M . SWUNG GEAR SEVERAL TIMES, OPS CHECKS NORMAL. 2 L 7 2 4F RT A6WE 2001091900083 20010919 00083 NM 2001 9 19 DLM88011396 1 20010823 A 2560 FLASHLIGHT DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 975DL 53243 FLT ATTENDANT FLASHLIGHT MID-CABIN INOP. REPLACED FLASHLIGHT. 2 L 7 2 4F RT A6WE 2001091900084 20010919 00084 NM 2001 9 19 DLM88011397 1 20010823 A 3350 RPS1 POWER SUPPLY DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 920DE 53423 SEAT ROW 31-38 EMERGENCY TRACK LIGHTING INOP. REPLACED POWER SUPPLY. 2 L 7 2 4F RT A6WE 2001091900086 20010919 00086 NM 2001 9 19 DLM88011398 1 20010824 A 2150 SCREEN DOUG MD88 MD88 3023688 NM LT ACM CLOGGED A DALA O OTHER O OTHER CR CRUISE 1 SO 27 912DL 49543 UNABLE TO PRESSURIZE A/C WITH LEFT PACK. CLEARED CLOGGED SCREEN FROM ACM TO ACM ANTI ICE VALVE. 2 L 7 2 4F RT A6WE 2001091900104 20010919 00104 NM 2001 9 19 EISA20010114 1 20010820 A 2761 652460821 ANGLE BOEING 727 7272M7 138407S NM REAR SPAR CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 721RW 62932 21200 LT. WING SPOILER #4 ACTUATOR MOUNT O/B LWR. MOUNT LOBE IS BROKENFOUND DURING 'B' CHECK.CORRECTIVE ACTION:R/R #4 SPOILER ACTUATOR MOUNT BRACKET IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2001091900105 20010919 00105 NM 2001 9 19 EISA20010115 1 20010820 A 2761 65C8067822 FITTING BOEING 727 7272M7 138407S NM TRAILING EDGE CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 721RW 21200 #9 SPOILER R/H ACTUATOR SUPPORT FITTING CRACKED SEVERAL PLACES.FOUND DURING 'B' CHECK.CORRECTIVE ACTION:R/R #9 ACTUATOR SUPPORT FITTING IAW B727 SRM 51-30-1, 51-30-2 & 51-30-5. 2 L 7 3 4F A3WE 2001091900106 20010919 00106 NM 2001 9 19 EISA20010120 1 20010830 A 2760 651734781A SPOILER PANEL BOEING 727 727200 138407E NM #12 SPOILER DAMAGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 702NE 22460 ON POSTFLIGHT, FOUND RIGHT WING INFLIGHT SPOILER DAMAGED (#12)CORRECTIVE ACTION:R/R #12 FLIGHT SPOILER ON R/H WING IAW B 727 MM 27-61-1. OPS CK NORMAL ON GROUND. 2 L 7 3 4F RT A3WE 2001091900107 20010919 00107 NM 2001 9 19 EISA20010116 1 20010820 A 2761 NPN WEB BOEING 727 7272M7 138407S NM AUX SPAR CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 721RW 21200 R/H SPOILER R/H ACTUATOR ATTACH WEB CRACKED 2 PLACES.CORRECTIVE ACTION:REMOVED DAMAGED SECTION OF WEB BY CUT-OUT IAW B72 7 SRM 51-10-1. VERIFIED DAMAGED AREA REMOVED BY NDT IAW B727 NDT MANUAL PART 6. FABRICATED WEB REPAIR IAW B727 SRM 51-4 0-2. TREATED, PRIMED & INSTALLED WEB REPAIR IAW B727 SRM 51-10-2 & 51-30-2. 2 L 7 3 4F A3WE 2001091900108 20010919 00108 NM 2001 9 19 EISA20010118 1 20010829 A 5297 NPN WIRE AEI BOEING 727 7272M7 138407S NM MCD SWITCH LOOSE A EISA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 07 742RW 21952 TAKEOFF DISCONTINUED AT 100 KTS DUE TO MAIN CARGO DOOR LIGHT ON STEADY, RETURNED TO RAMP, LIGHT REMAINS ON.CORRECTIVE AC TION:TROUBLESHOT MAIN CARGO DOOR IAW AERO. M/M, FOUND WIRING FROM SWITCH PULLED LOOSE. REPAIRED WIRING. OPS CK OK. 2 L 7 3 4F A3WE 2001091900109 20010919 00109 NM 2001 9 19 EISA20010111 1 20010814 A 2751 NPN BOLT HONEYWELL BOEING 727 727225 1384077 NM WORN A EISA O OTHER O OTHER AP APPROACH 1 SW 07 356PA 20626 ON APPROACH AND LANDING INBOARD FLAPS TRIPPED DUE TO AN ASYMMETRY. TRIPPED AT LESS THAN 2DEG. ACC. APPROPRIATE EMERGENC Y CHECKLIST AND OPERATED ACCORDINGLY.CORRECTIVE ACTION:REPLACED WORN BOLT IN L/H INBD FLAP POSITION TRANSMITTER ADJUSTED TRANSMITTER AND OPS CHECKED OK IAW 727 MM CH 27-51-00 2 L 7 3 4F A3WE 2001091900110 20010919 00110 NM 2001 9 19 DLM88011408 1 20010825 A 2150 20495062 ACM DOUG MD88 MD88 3023688 NM A/C BAY LEAKING A DALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 914DE 49957 F/A REPORTED SMOKE IN CABIN IMMEDIATELY AFTER T/O. SMOKE DISAPPEARED AFTER POWER WAS REDUCED. RTN TO CVG FOR IMMEDIATE LANDING. BOTH REAR LAV SMOKE DETECTORS ACTIVATED. REMOVED LT ACM DUCTING AND FOUND OIL RESIDUE. SUSPECT LT ACM LEAKI NG. ACM P/N219001545. REINSTALLED ACM DUCTING. FWD LT A/C PACK TO MCO AND PLAC PER MEL 21-00-01A. SENSE LINE DISCO NNECTED AT FLOW CONTROL VLV. REPLACED COALESCER BAGS AFTER DUCT BURNOUT PER MM. OK FOR SERVICE. 2 L 7 2 4F RT A6WE 2001091900111 20010919 00111 NM 2001 9 19 DLM88011429 1 20010830 A 2910 B-NUT DOUG MD88 MD88 3023688 NM HYDRAULIC SYS LOOSE A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 942DL 49815 LT HYD QTY W/HYD QTY LOW IND. FOLLOWED CK LIST PROCEDURES AND LOST LT HYD PRESSURE W/GOOD QTY. ZERO LEFT HYD PRESSURE W/GOOD RIGHT HYD PRESSURE AND GOOD QUANTITIES. WHEN XFER PUMP TURNED ON PER MCC. QTY RETURNED TO 19 QTS WITHOUT PRESSU RE. FWD B-NUT LOOSE AT LT THRUST RVSR CONTROL VALVE. REPLACED HYD PRESS LINE THAT RUNS FROM ACCUMULATOR TO CONTROL VAL VE. CHECK OF EDP CKS GOOD, LEAK CKS GOOD. 2 L 7 2 4F RT A6WE 2001091900112 20010919 00112 NM 2001 9 19 DLM88011430 1 20010830 A 4990 TANK DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE APU LEAKING A DALA O OTHER K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 908DL 9876 P80347 49539 P80347 AFT LAV SMOKE DETECTORS ACTIVATED DURING CLIMB AND SMOKE WAS APPARENT. NATURE OF PROBLEM, SMOKE IN CABIN. CAUSE OF SMO KE DETERMINED TO BE OIL LEAKING FROM APU OIL TANK AND INGESTED IN APU INLET. RENDERED APU INOP AND PERFORMED OPER 5088 FOR DUCT BURN OUT PROCEDURE. APU WILL NEED REPLACEMENT DUE TO LOCATION OF OIL LEAK. 2 L 7 2 4F 4 F RT A6WE E9NE 2001091900113 20010919 00113 NM 2001 9 19 DLM88011432 1 20010830 A 2120 ODOR DOUG MD88 MD88 3023688 NM CABIN DETECTED A DALA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 SO 27 920DL 49644 ON APPROACH INTO DAB RT AFT LAVATORY SMOKE DETECTOR SOUNDED WITH A HOT BURNING SMELL IN CABIN. UNABLE TO DUPLICATE. PE RFORMED DUCT BURNOUT AS PRECAUTION. 2 L 7 2 4F RT A6WE 2001091900114 20010919 00114 NM 2001 9 19 DLM88011460 1 20010901 A 3397 WIRE DOUG MD88 MD88 3023688 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 931DL 49718 PAX SEAT 35 D/E EMERGENCY LIGHT INOP. FOUND BROKEN WIRE. REPLACED SEAT HARNESS EMERGENCY LIGHT, NOW NORMAL. 2 L 7 2 4F RT A6WE 2001091900115 20010919 00115 NE 2001 9 19 DLM88011461 2 20010831 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 MAKING METAL A DALA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 27 955DL 29017 49886 725548 LEFT OIL STRAINER CLOGGED MESSAGE CAME ON 1 HR INTO FLT. ENGINE SHUTDOWN. FOUND METAL ON CHIP DETECTOR AND MAIN OIL FI LTER. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A6WE E9NE 2001091900116 20010919 00116 NM 2001 9 19 DLM88011463 1 20010902 A 2120 ODOR DOUG MD88 MD88 3023688 NM CABIN DETECTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 931DL 49718 AFTER TAKEOFF SMELLED ODOR IN CABIN. FIRST IN THE BACK THEN UP FRONT AND IN COCKPIT, PASSENGERS SAID IT SMELLED LIKE OI L. CREW THOUGHT IT SMELLED ELECTRICAL. PERFORMED DUCT BURNOUT. 2 L 7 2 4F RT A6WE 2001091900117 20010919 00117 NM 2001 9 19 DLM88011468 1 20010903 A 3510 MC1004101 OXYGEN MASK DOUG MD88 MD88 3023688 NM COCKPIT WILL NOT TEST A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 975DL 53243 CAPT'S O2 MASK WON'T TEST. REPLACED CAPT'S O2 MASK. 2 L 7 2 4F RT A6WE 2001091900118 20010919 00118 NE 2001 9 19 DLM88011472 2 20010904 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 MAKING METAL A DALA E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 27 943DL 25692 49816 726087 LEFT ENG OIL STRAINER CLOG MSG IN FLIGHT PROCEEDED BY VIBRATION IN AIRCRAFT. SHUTDOWN ENGINE PER POM. ALL ENGINE INDIC ATIONS WERE NORMAL FOR CLIMB POWER. FOUND METAL IN ENG OIL FILTER. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A6WE E9NE 2001091900119 20010919 00119 NE 2001 9 19 DLM88011475 2 20010904 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 FAILED A DALA E ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 27 943DL 25692 49816 726087 AT 10 - 15 MIN AFTER T/O AT 14,000 FT HAD AN AIRFRAME VIB. CLIMBED TO 20,000 FT AND THE OIL CLOG LIGHT CAME ON WITH HAR D KNOCKING ON THE FLOORBOARD OF COCKPIT. PULLED POWER BACK BUT CLOG LIGHT STAYED ON. SHUTDOWN THE ENG, HAD POSITIVE O IL PRESSURE THROUGHOUT WINDMILL PROCESS. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A6WE E9NE 2001091900120 20010919 00120 NM 2001 9 19 DLM90011395 1 20010823 A 3241 60060791R MANIFOLD DOUG MD90 MD9030 3023690 NM ANTI SKID SYS DAMAGED A DALA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 903DA 53383 DURING TAXI RIGHT HYD QUANTITY DROPPED TO 3 RAPIDLY. VISIBLE FLUID SEEN ON TAXIWAY. FOUND DUAL ANTI-SKID CONTROL MANIF OLD ASSY TO HAVE A HYD FUSE BLOWN OFF MANIFOLD ASSY. REPLACED ANTI-SKID MANIFOLD PER AMM. LEAK CHECKS GOOD. 2 L 7 2 4F RT A6WE 2001091900121 20010919 00121 2001 9 19 DLM90011431 4 20010830 A 3442 20412222456 INDICATOR DOUG MD90 MD9030 3023690 NM COCKPIT FAULTY A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 27 907DA 53387 AIRCRAFT DIVERTED TO LUBBOCK TX WITH PUNGENT ELECTRICAL/PLASTIC SMELL IN COCKPIT. REPLACED WX RADAR INDICATOR FOR PRODU CING SMELL. 2 L 7 2 4F RT A6WE 2001091900122 20010919 00122 NM 2001 9 19 DLM90011476 1 20010904 A 3244 M90N TIRE DOUG MD90 MD9030 3023690 NM NLG SEPARATED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 908DA 53388 AFTER TAKEOFF AND RAISING LANDING GEAR, UNSAFE NOSE GEAR INDICATION WITH LANDING GEAR HANDLE UP. CONFIRMED BY AIRPORT O PERATIONS RUBBER/GLASS ON THE RUNWAY. AIRCRAFT RECONFIGURED FUEL BURNED DOWN, LANDING ACCOMPLISHED AT 142,200 GROSS WT. RT NOSE TIRE CAP SEPARATED, TIRE NOT BLOWN, TIRE PSI 190 PSI ON ARRIVAL PER TRANS CK LIMITS. REPLACED RT NOSE TIRE, N OSE GEAR SWING CKD OK. 2 L 7 2 4F RT A6WE 2001091900123 20010919 00123 NE 2001 9 19 OZIA013127001 2 20010219 A 7200 ENGINE DORNER DO32 DO328300 NM PWA 306 PW306B NE ENGINE OVERTEMP A OZIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 05 430Z 3127 CD0022 HIGH ITT ON TAKEOFF ROLL. REJECTED TAKEOFF. ENGINE EXCEEDANCE PAGE INDICATED 930 DEGREES. NO FURTHER ACTION NEEDED PE R 328 MANUAL. 2 H 7 2 4T 4 F RT A55NM E35NE 2001091900145 20010919 00145 NM 2001 9 19 2001UALA01979 1 20010907 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 916UA 25383 CABIN FLOORBEAM UPPER FLANGE IS CORRODED AT BS 986 FORWARD, RBL 24, WL 208. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091900164 20010919 00164 NM 2001 9 19 2001UALA01996 1 20010907 A 5312 PRESSURE PANEL BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7265U 21412 NOSE LANDING GEAR WHEEL WELL TOP PRESSURE PANEL CRACKED AT FASTENER HOLES AT BODY STATION 284. REPAIRED PRESSURE PANEL WEB. MAJOR REPAIR ACCOMPLISHED. 2 L 7 3 4F 4 F A3WE E2EA 2001091900165 20010919 00165 EA 2001 9 19 COMA0160730 1 20010917 A 2460 BKAE2400301 CONNECTOR CNDAIR CNDAIR CL600 CL6002B19 EA JUNCTION BOX JB- BURNED A COMA H DEACTIVATE SYST/CIRCUITS G MULTIPLE FAILURE IN INSP/MAINT 1 SO 01 916CA 19212 7014 UPON APPLYING ELECTRICAL POWER TO AIRCRAFT FOR MAINTENANCE SEVERAL AVIONICS COOLING SYSTEM AND FLIGHT RECORDER SYSTEM CI RCUIT BREAKERS POPPED, ACCOMPANIED BY VARIOUS FAILURES OF COCKPIT PANEL BACKLIGHTING. INVESTIGATION FOUND THE JUNCTION BOX (JB-2) ELECTRICAL CONNECTOR (J130/P130) TO SHOW SIGNS OF SEVERE OVERHEATING, WITH SEVERAL PINS SHORTED AND BURNED. REPLACED BOTH HALVES OF CONNECTOR WITH NEW PARTS. 2 L 7 2 4F RT A21EA 2001091900167 20010919 00167 2001 9 19 AUS20010905 4 20010813 A 3442 20704090104 ANTENNA BOEING 747 747238B 1384828 NM RROYCE RB211 RB211524D419 54555 NE WEATHER RADAR SY FAULTY W O OTHER O OTHER CR CRUISE 1 AU S 2330 3697 (AUS) WEATHER RADAR ANTENNA FAULTY. 2 L 7 4 4F 4 F A20WE E12EU 2001091900168 20010919 00168 2001 9 19 AUS20010906 4 20010816 A 3140 COMPUTER BOEING 747 747438 NM RROYCE RB211 RB211524G19 NE EICAS FAILED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) UPPER EICAS DISPLAY FAILED. 2 L 7 4 4F 4 F RT A20WE E30NE 2001091900169 20010919 00169 SW 2001 9 19 AUS20010907 1 20010814 A 2730 2744062005 CONTROL CABLE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TFE33112UHR WP ROTOL R321 R321482F8 GL ELEVATOR CONTROL FRAYED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) ELEVATOR DOWN CONTROL CABLE FRAYED. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P61GL 2001091900170 20010919 00170 NM 2001 9 19 AUS20010910 1 20010821 A 3232 ACTUATOR BOEING 747 747238B 1384828 NM RROYCE RB211 RB211524D419 54555 NE MLG DOOR SHEARED W O OTHER E K VIBRATION/BUFFET FLUID LOSS CL CLIMB 1 AU S (AUS) NOSE LANDING GEAR DOOR ACTUATOR SHEARED. LOSS OF HYDRAULIC FLUID. 2 L 7 4 4F 4 F A20WE E12EU 2001091900171 20010919 00171 NM 2001 9 19 AUS20010911 1 20010819 A 2782 126344211 PDU BOEING 747 747SP38 1384817 NM RROYCE RB211 RB211524D419 54555 NE LE SLATS FAULTY W O OTHER F FLT CONT AFFECTED CL CLIMB 1 AU S 7736 114P2597 (AUS) NR 3 LT LEADING EDGE FLAP PNEUMATIC DRIVE UNIT FAULTY. 2 L 7 4 4F 4 F RT A20WE E12EU 2001091900172 20010919 00172 EA 2001 9 19 COMA0160731 1 20010915 A 2910 848847 PUMP CNDAIR CL600 CL6002B19 EA MLG BAY FAULTY A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 718CA 5088 7312 FLIGHT #5034. DURING RDU APPROACH RECEIVED A HYDRAULIC 3A FAIL CAUTION MESSAGE.REPLACED THE ALTERNATING CURRENT MOTOR H YDRAULIC PUMP 3A. 2 L 7 2 4F RT A21EA 2001091900173 20010919 00173 NM 2001 9 19 AUS20010912 1 20010821 A 3230 162T30332 SPRING BOEING 767 767* NM RROYCE RB211 RB211524* NE NLG MISSING W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NOSE LANDING GEAR OVERCENTRE LOCK SPRING MISSING. 2 L 7 2 4F 4 F RT A1NM E12EU 2001110800027 20011108 00027 NM 2001 11 8 2001UALA01998 1 20010907 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 916UA 25383 CABIN FLOORBEAM UPPER FLANGE IS CORRODED BODY STATION 986 FORWARD, RBL 24, WL 208. MAJOR REPAIR ACCOMPLISHED. ACCOMPLIS HED STRAP REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091900174 20010919 00174 EU 2001 9 19 AUS20010916 1 20010821 A 3246 AHA1490 BEARING BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE MLG FAILED W O OTHER O OTHER TX TAXI/GRND HDL 1 AU S 1272 (AUS) NR 2 MAIN WHEEL INNER BEARING DISINTEGRATED CAUSING THE INNER RACE TO FUSE TO THE AXLE. 2 H 7 4 4F 4 F RT A49EU E6NE 2001091900175 20010919 00175 NM 2001 9 19 AUS20010918 1 20010813 A 2730 2827001009 ACTUATOR BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL ELEVATOR CONTROL LEAKING W O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 AU S 51821 1424 (AUS) RT ELEVATOR CENTRE ACTUATOR LEAKING. 2 L 7 2 4F 4 F RT A1NM E23EA 2001091900176 20010919 00176 NM 2001 9 19 2001UALA01999 1 20010907 A 5320 WEB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 323UA 23955 FUSELAGE FLOOR STRUCTURE WEB CRACKED AT BS 179, WL 207, LBL 27 ON AFT SIDE OF BODY STATION 178 BULKHEAD. MAJOR REPAIR A CCOMPLISHED. FLOOR STRUCTURE WEB REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091900177 20010919 00177 NM 2001 9 19 2001UALA02000 1 20010908 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 323UA 23955 CABIN BODY STATION 887 1-INCH ABOVE STRINGER CLIP STRINGER 9L FRAME WEB CRACKED FASTENER STANDOFF. MAJOR REPAIR ACCOMPL ISHED. REMOVED DAMAGE. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091900178 20010919 00178 EA 2001 9 19 COMA0160732 1 20010917 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA R/H MALFUNCTIONED A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 981CA 833 7163 FLIGHT #5589. FLAPS FAIL CAUTION MESSAGE DURING TAXI. DISCREPANCY DID NOT DUPLICATE BUT COMPUTER INDICATED R/H BPSU AS MOST LIKELY SUSPECT.REPLACED THE R/H BPSU. 2 L 7 2 4F RT A21EA 2001091900179 20010919 00179 NM 2001 9 19 2001UALA02001 1 20010908 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 323UA 23955 CABIN BODY STATION 807 1-INCH ABOVE STRINGER CLIP STRINGER 9L FRAME WEB IS CRACKED STANDOFF. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091900181 20010919 00181 NM 2001 9 19 2001UALA02002 1 20010908 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 323UA 23955 CABIN BODY STATION 907 1-INCH ABOVE STRINGER CLIP STRINGER 9R FRAME WEB IS CRACKED STANDOFF FASTENER. MAJOR REPAIR ACCO MPLISHED. REMOVED DAMAGE. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091900182 20010919 00182 2001 9 19 AUS20010924 4 20010823 A 2565 616591 TUBE AIRBUS 320 A320* EU CFMINT CFM56 CFM565A1 NE ESCAPE SLIDE CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S C008030888 (AUS) OFF WING ESCAPE SLIDERAFT PNEUMATIC BALL LOCK TUBE CONNECTOR CORRODED AND END SEPARATED FROM THE BALL LOCK. 2 L 7 2 4F 4 F RT A46NM E29NE 2001091900183 20010919 00183 NM 2001 9 19 AUS20010926 1 20010824 A 3233 65C329561 ACTUATOR BOEING 737 7374Y0 1384705 NM CFMINT CFM56 CFM563C 13802 EU MLG FAULTY W O OTHER J WARNING INDICATION CL CLIMB 1 AU S (AUS) RT MAIN LANDING GEAR ACTUATOR FAULTY. 2 L 7 2 4F 4 F RT A16WE E21EU 2001091900184 20010919 00184 NM 2001 9 19 2001UALA02003 1 20010908 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 323UA 23955 CABIN BODY STATION 827 1-INCH ABOVE STRINGER CLIP 9L FRAME WEB IS CRACKED STANDOFF FASTENER. MAJOR REPAIR ACCOMPLISHED .REMOVED DAMAGE. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091900186 20010919 00186 NM 2001 9 19 AUS20010928 1 20010823 A 7603 65B8280125 COVER RROYCE RB211524D4 BOEING 747 747338 NM RROYCE RB211 RB211524D419 54555 NE POWER LEVER CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LT AND RT ENGINE THRUST CABLE GUARD COVERS LOCATED IN AREABETWEEN BS960 TO BS1000 DETERIORATED AND CRACKED. FOUND DURING INSPECTION IAW EI 743-076-0002R02. 2 L 7 2 4F 4 F RT A20WE E12EU 2001091900187 20010919 00187 EU 2001 9 19 2001UALA02004 1 20010909 A 2810 L95F50603 RELIEF VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CENTER TANK BROKEN A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 478UA 1533 FUEL AUTO FEED FAULT ECAM MESSAGE. FUEL IMBALANCE BETWEEN LEFT AND RIGHT WING TANKS OF 1500 POUNDS. FOUND FUEL TANK PRO TECTOR-OVERPRESSURE DISC BROKEN BETWEEN THE LEFT WING AND CENTER FUEL TANKS. THIS ALLOWED FUEL TO MIGRATE FROM THE LEFT WING TANK INTO THE CENTER TANK. REPLACED DISC. 2 L 7 2 4F 4 F RT A28NM E40NE 2001091900188 20010919 00188 NM 2001 9 19 2001UALA02006 1 20010907 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1263 STRINGER 27L-28L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091900189 20010919 00189 2001 9 19 AUS20010931 4 20010826 A 3460 WIRE BOEING 737 73733A 1384673 NM GE CFM56 CFM563B1 13802 NE F/M COMPUTER TRANSPOSED W O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 AU S (AUS) FLIGHT CONTROL COMPUTER TO STABILISER POSITION SENSOR WIRES TOPIN 22 AND PIN 23ON CONNECTOR D4079 CROSSED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091900190 20010919 00190 NM 2001 9 19 2001UALA02007 1 20010907 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1351 STRINGER 33L-34L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091900191 20010919 00191 SW 2001 9 19 AUS20010933 1 20010820 A 2150 20475546 ACM SWRNGN SA227 SA227* SW GARRTT TPE331 TPE33112UA 01514 WP MCAULY 4HFR34 4HFR34C652 NE CABIN COOLING SEIZED W O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 AU S 1892 (AUS) RT AIR CYCLE MACHINE (ACM) SEIZED. 2 L 7 2 4T 4 T RT A5SW E4WE 6 C 3PNE 2001091900192 20010919 00192 NM 2001 9 19 AUS20010937 1 20010824 A 5610 5893543109 WINDSHIELD BOEING 737 73733A 1384673 NM GE CFM56 CFM563B1 13802 NE COCKPIT CRACKED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AU S (AUS) NR 1 WINDSHIELD LT SIDE OUTER PANE CRACKED FOLLOWING ARCING. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091900202 20010919 00202 EU 2001 9 19 AUS20010940 1 20010828 A 7603 POWER LEVER LYC ALF502R5 BAG BAE146 BAE146300A 1500267 EU LYC ALF502 ALF502R5 41580 NE POWER LEVER SEIZED W O OTHER O OTHER CR CRUISE 1 AU S (AUS) NR 3 ENGINE THRUST LEVER SEIZED. THRUST LEVER WORKED NORMALLYLATER IN THE FLIGHT. INVESTIGATION COULD FIND NO REAS ON FOR LEVER STICKING. 2 H 7 4 4F 4 F RT A49EU E6NE 2001091900206 20010919 00206 NM 2001 9 19 2001UALA02016 1 20010907 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1417-1461 STRINGER 33L CHORD CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED AND INSTALLED CHORD. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091900208 20010919 00208 2001 9 19 SWAA012530 4 20010911 A 2565 65C19901 CABLE BOEING 737 7373Q8 1384670 NM AFT SVC DOOR FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 663SW 23256 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. R&R CAB LE PER MM. 2 L 7 2 4F RT A16WE 2001091900210 20010919 00210 NM 2001 9 19 SWAA012536 1 20010912 A 3350 100031 LIGHT BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 502SW 24179 DURING SCHEDULED C1 CHECK, FOUND CENTER EMERGENCY OVERHEAD EXIT LIGHT WIRES BROKEN. REPAIRED BROKEN WIRES PER MM. 2 L 7 2 4F RT A16WE 2001091900211 20010919 00211 NM 2001 9 19 SWAA012537 1 20010907 A 5755 6573730 SPOILER BOEING 737 7373A4 1384585 NM LH WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 DURING SCHEDULED 1/4D CHECK AT DALFORT, FOUND # 3 SPOILER DELAMINATED. R&R SPOILER PER MM. 2 L 7 2 4F RT A16WE 2001091900212 20010919 00212 NM 2001 9 19 SWAA012538 1 20010906 A 5755 6573730 SPOILER BOEING 737 7373A4 1384585 NM RH WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 DURING SCHEDULED 1/4D CHECK AT DALFORT, FOUND # 7 SPOILER DELAMINATED. R&R SPOILER PER MM. 2 L 7 2 4F RT A16WE 2001091900213 20010919 00213 NM 2001 9 19 SWAA012539 1 20010913 A 5230 6547952 SKIN BOEING 737 7373H4 1384600 NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 604SW 27955 DURING SCHEDULED C2 CHECK, FOUND AFT CARGO DOOR SKIN CRACKED 3/8 INCH LONG AT BS 817. REPAIRED DO OR PER SRM. 2 L 7 2 4F RT A16WE 2001091900214 20010919 00214 2001 9 19 SWAA012541 4 20010912 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED 1/2D CHECK, FOUND AFT ENTRY DOOR EVAC SLIDE CABLE FRAYED. R&R EVAC SLIDE CABLE P ER MM. 2 L 7 2 4F RT A16WE 2001091900215 20010919 00215 NM 2001 9 19 SWAA012542 1 20010913 A 5310 6517582 WEB BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 504SW 24181 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL WEBS CRACKED ( 2 EA ) AT BS 183, WL 233, LBL 17.1 & RBL 17.1. R&R WEBS PER SRM. 2 L 7 2 4F RT A16WE 2001091900216 20010919 00216 NM 2001 9 19 SWAA012543 1 20010912 A 5310 6516300 WEB BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 504SW 24181 DURING SCHEDULED SPECIAL VISIT, FOUND HORIZONTAL WEBS CRACKED ( 2 EA ) AT BS 180, WL 207, LBL 26.5 & RBL 26.5. R&R WEBS PER SRM. 2 L 7 2 4F RT A16WE 2001091900217 20010919 00217 NM 2001 9 19 SWAA012544 1 20010913 A 5310 6517582 WEB BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 504SW 24181 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL WEB CRACKED AT BS 179, WL 227 & LBL 17.1. R&R W EB PER SRM. 2 L 7 2 4F RT A16WE 2001091900218 20010919 00218 EA 2001 9 19 COMA0160733 1 20010918 A 5210 DOOR CNDAIR CL600 CL6002B19 EA A COMA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SO 01 809CA 7366 FLIGHT #5506. DURING CLIMB OUT OF CHO RECEIVED A CABIN DOOR OUTER HANDLE CAUTION MESSAGE, AIRCRAFT RETURNED TO THE FIEL D.CLEANED AND LUBRICATED THE CABIN DOOR OUTER HANDLE LOCKING MECHANISM. 2 L 7 2 4F RT A21EA 2001091900219 20010919 00219 NM 2001 9 19 SWAA012546 1 20010914 A 5753 6546435 FLAP BOEING 737 7373H4 1384600 NM RH WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 656SW 28401 DURING SCHEDULED C4 CHECK, FOUND OTBD T/E FLAP DELAMINATED AT INBD CORNER. R&R FLAP PER MM. 2 L 7 2 4F RT A16WE 2001091900220 20010919 00220 NM 2001 9 19 SWAA012550 1 20010914 A 5330 6545768 SKIN BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 345SA 23786 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT END OF E&E EQUIPTMENT COOLING CUT OUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001091900221 20010919 00221 NM 2001 9 19 SWAA012551 1 20010904 A 5310 6547978 CREASE BEAM BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED D CHECK, FOUND CREASE BEAM CRACKED AT BS 189, STR 17L, WL 207. REPAIR ED CREASE BEAM PER BFG ER. 2 L 7 2 4F A16WE 2001091900222 20010919 00222 NM 2001 9 19 SWAA012552 1 20010913 A 5314 6545866 SKIN BOEING 737 7373H4 1384600 NM MLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 604SW 27955 DURING SCHEDULED C2 CHECK, FOUND KEEL BEAM SKIN CRACKED 2 INCHES LONG, LH SIDE AT BS 682. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001091900223 20010919 00223 NM 2001 9 19 SWAA012553 1 20010913 A 5330 654577886 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR LOWER FWD CUT OUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001091900224 20010919 00224 NM 2001 9 19 SWAA012554 1 20010915 A 5310 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL WEBS CRACKED ( 4 EA ) AT BS 178, RBL 17.1 & LBL 17.1, WL 176 TO WL 230. REPAIRED WEBS PER SRM. 2 L 7 2 4F RT A16WE 2001091900225 20010919 00225 NM 2001 9 19 SWAA012555 1 20010914 A 5310 6517583 BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM CRACKED AT BS 178, LBL 17.1 & WL 220. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 2001091900226 20010919 00226 NM 2001 9 19 SWAA012560 1 20010915 A 3350 07912 COVER BOEING 737 7377H4 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 745SW 29491 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER CRACKED AT ROW 2. R&R COVER PER MM. 2 L 7 2 4F RT A16WE 2001091900227 20010919 00227 NM 2001 9 19 SWAA012564 1 20010917 A 3411 6568558 PITOT TUBE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 646SW 28331 UPPER LH PITOT TUBE CRACKED. R&R PITOT TUBE PER MM. 2 L 7 2 4F RT A16WE 2001091900228 20010919 00228 NM 2001 9 19 SWAA012566 1 20010917 A 5310 6517582 WEB BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED D CHECK, FOUND VERTICAL BEAM WEBS CRACKED ( 2 EA ) AT BS 178, WL 175 & WL 177, RBL 17.1. R&R WEBS PER BFG ER 01-0781. 2 L 7 2 4F A16WE 2001091900229 20010919 00229 NM 2001 9 19 SWAA012567 1 20010914 A 5754 65C26602 SLAT BOEING 737 7373H4 1384600 NM LH WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 630WN 27705 DURING SCHEDULED C1 CHECK, FOUND # 2 L/E SLAT OTBD T/E WEDGE DELAMINATED AT UPPER SURFACE. R&R SLAT PER MM. 2 L 7 2 4F RT A16WE 2001091900230 20010919 00230 NM 2001 9 19 SWAA012569 1 20010917 A 5310 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 27L. R&R STR CLIP PER S RM. 2 L 7 2 4F RT A16WE 2001091900231 20010919 00231 NM 2001 9 19 SWAA012570 1 20010917 A 5310 6546546 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED ( 2 EA ) AT BS 767 & BS 807, BETWEEN STR 8L & 9L. REPAIRED FRAMES PER BFG ER 01-0788. 2 L 7 2 4F A16WE 2001091900232 20010919 00232 NM 2001 9 19 SWAA012571 1 20010917 A 5310 6546546 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, BETWEEN STR 8R & 9R. R EPAIRED FRAME PER BFG ER 01-0788 2 L 7 2 4F A16WE 2001091900233 20010919 00233 NM 2001 9 19 SWAA012573 1 20010915 A 5330 6545778 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT CARGO DOOR FWD LOWER CORNER CUTOUT. REPAIRED SKIN PER SRM & ER 01-0796. 2 L 7 2 4F A16WE 2001091900234 20010919 00234 EA 2001 9 19 COMA0160734 1 20010918 A 3610 9799981 BLEED VALVE CNDAIR CL600 CL6002B19 EA AFT EQUIPMENT BA FAULTY A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 957CA 12219 7109 FLIGHT #5237. DURING TAXI OUT THE RIGHT ENGINE FAILED TO START, AIRCRAFT RETURNED TO THE GATE.REPLACED THE RIGHT ENGINE 10TH STAGE BLEED VALVE. 2 L 7 2 4F RT A21EA 2001091900236 20010919 00236 NM 2001 9 19 2001UALA02019 1 20010907 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1263 STRINGER 38R-39R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091900239 20010919 00239 NM 2001 9 19 2001UALA02021 1 20010908 A 5311 FRAME BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 TWO INCHES ABOVE CABIN FLOOR BODY STATION 1270 RIGHT HAND FUSE FRAME STRAP REWORK ON INBOARD OF FRAME. MAJOR REPAIR ACC OMPLISHED. C9, APPROVED SPECIFICATION FOR THIS REPAIR IS EVA G95 7758. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091900240 20010919 00240 NE 2001 9 19 AUS20010945 2 20010824 A 7310 30611912 PIPE GARRTT TFE73140R ISRAEL 1125 ASTRASPX 4500205 EU GARRTT TFE731 TFE73140 29001 NE FUEL SYSTEM WORN W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LT ENGINE FUEL LINE CHAFED. FOUND DURING INSPECTION IAW ALERT SBTFE731-A73-5126. 2 L 7 2 4F 4 F RT A16NM E1NM 2001091900241 20010919 00241 NM 2001 9 19 2001UALA02022 1 20010909 A 5330 SKIN BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 FORWARD PIT STATION 412 TO STATION 434 FUSELAGE SKIN CORRODED AT STRINGER 39R. MAJOR REPAIR ACCOMPLISHED IN ACCORDANCE WITH BAC DWG 141T3220-20 AND 141T3221-3 AND SRM 53-00-03. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091900242 20010919 00242 NM 2001 9 19 2001UALA02024 1 20010911 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 323UA 23955 BODY STATION 178 WEB CRACK AT WL 186, RBL 1 AND LBL 1 AFT OF LOC ANT 2 EACH AREAS AFT SIDE OF WEB. MAJOR REPAIR ACCOMPL ISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091900243 20010919 00243 NM 2001 9 19 2001UALA02025 1 20010911 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 AFT PIT STATION 1395 SHEAR TIE BETWEEN STRINGER 38L AND 39R IS CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INST ALLED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091900247 20010919 00247 NM 2001 9 19 2001UALA02029 1 20010907 A 5230 6546921528 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 323UA 23955 FWD CARGO DOOR SKIN DAMAGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED SKIN DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091900248 20010919 00248 NM 2001 9 19 2001UALA02031 1 20010907 A 5210 6545871114 STOP FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE ENTRY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 323UA 23955 FWD RT ENTRY DOOR, AFT NUMBER 3 STOP FITTING FROM BOTTOM CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091900249 20010919 00249 NM 2001 9 19 2001UALA02032 1 20010913 A 5312 PRESSURE PANEL BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7266U 21413 NOSE WHEEL WELL PRESSURE DECK WEB CRACKED AT BODY STATION 282, RBL 4. 2 L 7 3 4F 4 F A3WE E2EA 2001110800028 20011108 00028 NM 2001 11 8 2001UALA02033 1 20010913 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 915UA 25382 EXTERNAL FUSELAGE SKIN AT BODY STATION 1006 STRINGER 4L IS GOUGED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. INSTALLED D OUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091900250 20010919 00250 GL 2001 9 19 01FDEA00841 2 20010914 A 7200 ENGINE DOUG DC10 DC1010F 3022111 WP GE CF6 CF66D 30020 GL NR 1 DAMAGED A FDEA A UNSCHED LANDING D INFLIGHT SEPARATION NR NOT REPORTED 1 SO 25 058FE 46705 PER ATC'S NOTIFICATION NR 1 ENGINE LOSING PARTS AND LOSS OF NR 1 EGT. 2 L 7 3 4F 4 F A22WE E23EA 2001091900252 20010919 00252 NM 2001 9 19 01FDEA00842 1 20010914 A 3310 2632 CONTROLLER DOUG MD11 MD11 3023602 NM COCKPIT DEFECTIVE A FDEA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 25 589FE 48491 LOUD PUMPING SOUND AND SOME SMOKE FROM OVHD C/B PNL. REMOVED AND REPLACED DIMMER CONTROLLER PER MM 33-11-03-2. 2 L 7 3 4F RT A22WE 2001091900254 20010919 00254 NM 2001 9 19 01FDEA00843 1 20010914 A 3260 SWITCH BOEING 727 727225 1384077 NM NLG FAILED A FDEA K NONE J WARNING INDICATION CL CLIMB 1 SO 25 469FE 21581 AFT T/O GEAR WAS RETRACT NORMAL WHEN HANDLE IN OFF POS. REMOVED AND REPLACED RIGHT AND LEFT NOSE LAND GEAR DOOR SWITCH PER MM 32-33-00-5. 2 L 7 3 4F A3WE 2001091900255 20010919 00255 EU 2001 9 19 01FDEA00844 1 20010918 A 5270 WARNING SYSTEM AIRBUS 310 A310200 3930310 EU COCKPIT ACTIVATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 426FE 245 ON CLIMBOUT FWD BELLY CARGO DOOR WARNING CAME ON. 2 L 7 2 4F RT A35EU 2001091900257 20010919 00257 NM 2001 9 19 2001UALA02037 1 20010913 A 5313 STRINGER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 172UA 24363 DENT IN STRINGER 27R 41 INCH FWD OF NR 2 RIGHT HAND MAIN ENTRY DOOR (UNDERNEATH THE FLOOR). 2 L 7 4 4F 4 F RT A20WE E24NE 2001091900259 20010919 00259 WP 2001 9 19 ABXA010474 1 20010918 A 3310 LIGHT DOUG DC9 DC932 3022066 WP COCKPIT SHORTED A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 901AX 47381 THE FIRST OFFICERS OVERHEAD MAP LIGHT WENT OUT AND CAME BACK ON. A BURNING ELECTRICAL SMELL WAS NOTED. THE ASSOCIATED MAP LIGHT CIRCUIT BREAKER OPENED, NO FURTHER PROBLEMS WERE NOTED. MAINTENANCE INSPECTED AND FOUND EVIDENCE OF THE LIGHT ASSY TOUCHING A CAM LOCK RECEPTACLE WHEN TURNED EXCESSIVELY. MAINTENANCE REPOSITIONED THE LIGHT ASSY AS REQUIRED TO PR EVENT CONTACT AND RETURNED THE AIRCRAFT TO SERVICE. 2 L 7 2 4F A6WE 2001091900260 20010919 00260 WP 2001 9 19 ABXA010478 1 20010906 A 5320 5910130391 FITTING DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 A CRACK WAS INDICATED ON THE AFT PRESSURE BULKHEAD TEE FITTING NR 6, L14L. MAINTENANCE INSPECTED AND REPLACED THE TEE FITTING IAW ABX EA 53120037-006. 2 L 7 2 4F A6WE 2001091900261 20010919 00261 WP 2001 9 19 ABXA010479 1 20010905 A 5311 59135953 FRAME DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 FUSELAGE FRAME AT STATION 1076 WAS FOUND TO HAVE THREE CRACKS AT FASTENERS L13L AND L14L. MAINTENANCE INSPECTED AND REP LACED THE AFFECTED SECTION OF THE FRAME FROM LONGERON 10L TO 17L IAW DC-9 SRM 53-03. 2 L 7 2 4F A6WE 2001091900262 20010919 00262 WP 2001 9 19 ABXA010482 1 20010901 A 5320 9915558243 STIFFENER DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 RADIAL 5A ON AFT PRESSURE BULKHEAD WAS FOUND TO BE CRACKED. REPAIRED THE RADIAL IAW SERVICE BULLETIN 53-166-W. 2 L 7 2 4F A6WE 2001091900263 20010919 00263 EU 2001 9 19 AWXA200100447 1 20010917 A 4930 36163641 FUEL LINE AIRBUS 320 A320231 3930325 EU APU DAMAGED A AWXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 28 636AW 098 PHX-FLT 299-FUEL SMELL IN CABIN-C-WHILE THE AIRCRAFT WAS SITTING AT THE GATE WITH THE APU RUNNING AND AIR CONDITIONING P ACKS ON THERE WAS A SMELL OF FUEL IN THE CABIN, STRONGEST OVERWING. WITH THE PACKS TURNED OFF THE SMELL DISSIPATED. MA INTENANCE TROUBLESHOT AND FOUND A FUEL LINE ON THE APU MISROUTED AND HAD A HOLE WORN IN IT CAUSING FUEL TO LEAK. THE FU EL SMELL WAS BEING DRAWN INTO THE CABIN BY THE PACKS. MAINTENANCE REPLACED THE LINE. FUNCTIONAL AND LEAKS CHECKS WERE GOOD AND NO FURTHER SMELL OF FUEL IN THE CABIN WITH PACKS ON. 2 L 7 2 4F RT A28NM 2001101800038 20011018 00038 EU 2001 10 18 AWXA200100448 1 20010914 A 4920 38832203 ACTUATOR AIRBUS 320 A320231 3930325 EU APU LEAKING A AWXA H DEACTIVATE SYST/CIRCUITS K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 28 643AW 2953 315 LAS-FLT 238-FUEL SMELL IN CABIN- C -WHILE APPROACHING THE GATE AFTER LANDING THE CABIN CREW AND SOME PASSENGERS NOTED A FUEL SMELL. THE FLIGHT DECK CREW STARTED THE APU AFTER LANDING, NO FUEL ODOR WAS NOTICED PRIOR TO STARTING THE APU. AT T HE GATE THE CREW TURNED THE APU OFF. MAINTENANCE PERFORMED INITIAL TROUBLESHOOTING AND INSPECTED THE AIRCRAFT FOR SIGNS OF FUEL LEAKAGE, NONE WERE NOTED. THE APU WAS PLACED ON MEL 49-10-01, COND 1. AWAITING FURTHER TROUBLESHOOTING. MAINTENA NCE FOUND THE APU IGV ACTUATOR LEAKING AND REPLACED IT. OPERATIONAL AND LEAK CHECKS WERE GOOD. NO FURTHER DISCREPANCIES HAVE BEEN REPORTED. 2 L 7 2 4F RT A28NM 2001091900264 20010919 00264 NM 2001 9 19 SWAA012524 1 20010912 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 642WN 27715 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT FWD CABIN. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001091900265 20010919 00265 NM 2001 9 19 SWAA012525 1 20010912 A 3350 6104781 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 365SW 26576 DURING SCHEDULED SERVICE CHECK, FOUND LT EXTERNAL AND RT INTERNAL WING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATT ERY PER MM. 2 L 7 2 4F RT A16WE 2001091900266 20010919 00266 NM 2001 9 19 SWAA012526 1 20010912 A 2560 65C168209 HOOK BOEING 737 7373T5 NM SERVICE DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EVAC SLIDE GIRT BAR HOOKS LOOSE. SECURED GIRT BAR HOOKS PER MM. 2 L 7 2 4F RT A16WE 2001091900267 20010919 00267 2001 9 19 SWAA012527 4 20010911 A 2565 D31354 SLIDE BOEING 737 7373T5 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED BC3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PE R MM. 2 L 7 2 4F RT A16WE 2001091900268 20010919 00268 NM 2001 9 19 SWAA012528 1 20010911 A 3350 20131A BATTERY BOEING 737 7373Y0 1384671 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 682SW 23496 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY AND SVC DOORS EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PER M M. 2 L 7 2 4F RT A16WE 2001091900269 20010919 00269 NM 2001 9 19 SWAA012529 1 20010910 A 3350 20131A BATTERY BOEING 737 7373A4 1384585 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 674AA 23252 DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001091900270 20010919 00270 NM 2001 9 19 SWAA012531 1 20010911 A 3350 BR2013 LIGHT BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED C1 CHECK, FOUND EEPLS LOOSE AT AFT CABIN. SECURED EEPLS PER MM. 2 L 7 2 4F A16WE 2001091900271 20010919 00271 NM 2001 9 19 SWAA012532 1 20010911 A 5320 65C27314 TIE CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED 1/2D CHECK, FOUND TIE CLIPS CRACKED (2 EA) AT BS 663, STR 10R & 10L. REMOVED AND REPLACED TIE CLIPS PE R SRM. 2 L 7 2 4F RT A16WE 2001091900272 20010919 00272 NM 2001 9 19 SWAA012540 1 20010912 A 5753 6546435 FLAP BOEING 737 7373H4 1384600 NM LT WING DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED BC4 CHECK, FOUND LT WING OTBD AFT FLAP DISBONDED 4.0 INCH AT LOWER SURFACE INBD END. REMOVED AND REPLA CED FLAP PER MM. 2 L 7 2 4F RT A16WE 2001091900273 20010919 00273 NM 2001 9 19 SWAA012545 1 20010913 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 986, BL 0 TO RBL 15. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2001091900274 20010919 00274 NM 2001 9 19 SWAA012547 1 20010914 A 5520 6976419 BUSHING BOEING 737 7373H4 1384600 NM ELEVATOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 656SW 28401 DURING SCHEDULED C4 CHECK, FOUND RT ELEVATOR NR 6 HINGE BEARING PLATE BUSHINGS MIGRATED. REMOVED AND REPLACED BEARING P LATE PER MM. 2 L 7 2 4F RT A16WE 2001091900275 20010919 00275 2001 9 19 SWAA012548 4 20010915 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 520SW 25319 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001091900276 20010919 00276 NM 2001 9 19 SWAA012549 1 20010915 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CRACKED 1 INCH LONG AT BS 665, LBL 25. REPAIRED BEAM PER SWA RA 1-353-2650 . 2 L 7 2 4F RT A16WE 2001091900277 20010919 00277 2001 9 19 SWAA012556 4 20010915 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 324SW 23414 DURING SCHEDULED RON, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001091900278 20010919 00278 NM 2001 9 19 SWAA012557 1 20010916 A 3350 20131A BATTERY BOEING 737 7377H4 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 724SW 27856 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP, ROW 6 TO ROW 10. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001091900279 20010919 00279 NM 2001 9 19 SWAA012558 1 20010916 A 3350 6104791 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED SERVICE CHECK, FOUND RT AFT EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY AND SOCKET ASS Y PER MM. 2 L 7 2 4F A16WE 2001091900280 20010919 00280 NM 2001 9 19 SWAA012559 1 20010917 A 2560 P2070001 FLASHLIGHT BOEING 737 7377H4 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 403WN 29815 AFT LT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2001091900281 20010919 00281 2001 9 19 SWAA012561 4 20010916 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001091900282 20010919 00282 2001 9 19 SWAA012562 4 20010916 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 641SW 27714 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001091900283 20010919 00283 2001 9 19 SWAA012563 4 20010917 A 2565 D31354 SLIDE BOEING 737 7373G7 1384595 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001091900284 20010919 00284 NM 2001 9 19 SWAA012565 1 20010917 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 30 TO RBL 60. REPAIRED FLOORBEAM PER SWA T1-553-00 5. 2 L 7 2 4F RT A16WE 2001091900285 20010919 00285 2001 9 19 SWAA012568 4 20010915 A 2565 6557463 BRACKET BOEING 737 7373H4 1384600 NM ENTRY DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR GIRT BAR, FWD AND AFT FLOOR ATTACH BRACKETS CORRODED. REMOVED AND REP LACED ATTACH BRACKETS PER SRM. 2 L 7 2 4F RT A16WE 2001091900286 20010919 00286 NM 2001 9 19 SWAA012572 1 20010916 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 294, RBL 40 TO RBL 46. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2001091900287 20010919 00287 NM 2001 9 19 SWAA012574 1 20010917 A 5751 69600833 ROD END BOEING 737 7373H4 1384600 NM AILERON WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED 1/4D CHECK, FOUND RT AILERON HINGES NR 1, 3 & 4 WORN. REMOVED AND REPLACED AILERON HINGE BUSHINGS AND ROD END ASSY'S PER SWA ACO 7197-27. 2 L 7 2 4F RT A16WE 2001091900288 20010919 00288 2001 9 19 SWAA012575 4 20010917 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 680AA 23505 FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. INSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001091900289 20010919 00289 EU 2001 9 19 2001F00278 1 20010829 A 5347 EPNE95300013019 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 538AT 538 SAW - DURING CPCP4 INSPECTION, FOUND CORROSION ON THE LEFT AFT INBOARD, LEFT AFT OUTBOARD AND RIGHT FLIGHT ATTENDANT SEA T TRACKS. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW EO E2-53-115R1. THE AIRCRAFT WAS RETURNED TO SERVICE. REF SIM A200124209. (M) 2 H 7 2 4T RT A53EU 2001091900290 20010919 00290 EU 2001 9 19 2001F00279 1 20010829 A 5347 EPNE95300013022 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 538AT 538 SAW - DURING CPCP4 INSPECTION, FOUND CORROSION ON THE LEFT AFT INBOARD, LEFT AFT OUTBOARD AND RIGHT FLIGHT ATTENDANT SEA T TRACKS. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW EO E2-53-115R1. THE AIRCRAFT WAS RETURNED TO SERVICE. REF SIM A200124209. (M) 2 H 7 2 4T RT A53EU 2001091900291 20010919 00291 NM 2001 9 19 2001F00280 1 20010908 A 7921 6A4700 OIL COOLER BOEING 737 737232 1384475 NM NR 1 ENGINE DEFECTIVE A SOKF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 261LR 22402 SJO - FLT LR-610 - DURING CLIMB OF THE FLIGHT LR610, THE CAPTAIN REPORTED NR 1 ENGINE, HIGH OIL TEMP CSD, AND NR 2 ENGIN E, HIGH OIL TEMP CSD, THE AIRCRAFT RETURN TO SJO STATION FOR MAINTENANCE. AFTER LANDING, TECHNICIANS PERFORMED THE FAUL T ANALYSIS, THE CSD NR 1 AND OIL COOLER NR 1 WERE REMOVED AND REPLACED, AND NR 2 OIL COOLER CSD WAS CHANGE IAW MM 24-11- 11 AND 24-11-21. AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2001091900292 20010919 00292 NM 2001 9 19 2001F00281 1 20010908 A 2410 731753 CSD BOEING 737 737232 1384475 NM NR 1 ENGINE OVERTEMP A SOKF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 261LR 22402 SJO - FLT LR-610 - DURING CLIMB OF THE FLIGHT LR610, THE CAPTAIN REPORTED NR 1 ENGINE, HIGH OIL TEMP CSD, AND NR 2 ENGIN E, HIGH OIL TEMP CSD, THE AIRCRAFT RETURN TO SJO STATION FOR MAINTENANCE. AFTER LANDING, TECHNICIANS PERFORMED THE FAUL T ANALYSIS, THE CSD NR 1 AND OIL COOLER NR 1 WERE REMOVED AND REPLACED, AND NR 2 OIL COOLER CSD WAS CHANGE IAW MM 24-11- 11 AND 24-11-21. AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2001091900293 20010919 00293 NM 2001 9 19 2001F00282 1 20010908 A 7921 6A4700 OIL COOLER BOEING 737 737232 1384475 NM NR 2 ENGINE DEFECTIVE A SOKF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 261LR 22402 SJO - FLT LR-610 - DURING CLIMB OF THE FLIGHT LR610, THE CAPTAIN REPORTED NR 1 ENGINE, HIGH OIL TEMP CSD, AND NR 2 ENGIN E, HIGH OIL TEMP CSD, THE AIRCRAFT RETURN TO SJO STATION FOR MAINTENANCE. AFTER LANDING, TECHNICIANS PERFORMED THE FAUL T ANALYSIS, THE CSD NR 1 AND OIL COOLER NR 1 WERE REMOVED AND REPLACED, AND NR 2 OIL COOLER CSD WAS CHANGE IAW MM 24-11- 11 AND 24-11-21. AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2001091900294 20010919 00294 NE 2001 9 19 2001F00283 2 20010809 A 7200 ENGINE AMD FALC20 FALCON 2720302 EU GE CF700 CF700* 30010 NE NR 1 MALFUNCTIONED A CEDA O OTHER R PARTIAL RPM/PWR LOSS DE DESCENT 1 SW 05 209CA 71 WHILE ON DESCENT TO KLRD FROM MMQT, WHILE PASSING FL180 A SMALL REDUCTION IN POWER WAS MADE. THE NR 1 ENGINE ROLLED BAC K. AFTER 15-30 SECONDS THE NR 1 ENGINE SPOOLED BACK UP. THE AIRCRAFT CONTINUED ON TO KLRD WITH NO OTHER PROBLEMS AND M ADE A NORMAL LANDING. (M) 2 L 7 2 4F 4 F A7EU E7EA 2001121400007 20011214 00007 NM 2001 12 14 AWXA200100450 1 20010918 A 2782 654465116 ACTUATOR BOEING 737 7372U9 1384498 NM L/E SLAT FAILED A AWXA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 28 149AW 30494 18252 22575 PHX - AIR TURNBACK - FLT 416 - "C" - DURING CLIMB OUT OF PHX ENROUTE TO COS, WHEN THE FLAPS WERE RETRACTED THE NR 2 L/E SLAT TRANSIT LIGHT STAYED ILLUMINATED. PERFORMED THE QRH PROCEDURES AND LIGHTS REMAINED ON, VISUALLY CONFIRMED THE NR 2 SLAT NOT COMPLETELY FAIRED, NO ROLL WAS NOTICED. RETURNED TO PHX MAKING AN UNEVENTFUL LANDING. MX TROUBLESHOT AND REPLAC ED THE NR 2 L/E SLAT ACTUATOR. OPERATIONAL CHECKS AND INDICATIONS WERE NORMAL. TEARDOWN REPORT INDICATES THE FOLLOWING P ARTS WERE WORN AND REPLACED; STRAP, PACKINGS, SCRAPERS, SEALS, TUBING, CAP RINGS, BACK UP RINGS, O-RINGS, SLEEVES, CAD P LATE, AND RETAINER. ALSO REPLACED WAS A DEFECTIVE SWITCH. 2 L 7 2 4F RT A16WE 2001092000001 20010920 00001 2001 9 20 C2XA01TY118 4 20010919 A 3445 DMNI5042 ANTENNA EMB 145 EMB145LR SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13989 145271 TYS During a schedule inspection, corrosion was found on the lower TCAS 2 antenna. Maintenance removed and replaced the TCAS antenna I.A.W.-EMB-145-AMM-34-43-03, operational checked good. The repair was satisfactory and the aircraft will b e released upon complection of the inspection. 2 L 7 2 4T RT T00011AT 2001092000004 20010920 00004 EU 2001 9 20 C2XA01CL201 1 20010906 A 3350 3011180 POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU CABIN DEFECTIVE A C2XA O OTHER L NO TEST IN INSP/MAINT 1 SW 27 25811 094 BTV MAINTENANCE DURING A LINE CHECK MAINTENANCE DISCOVERED THE AFT FLOOR STRIP EMERGENCY LIGHTS WOULD NOT EXTINGUISH WHE N POWER WAS REMOVED.MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY 30WL. OPERATIONAL CHECKS WERE GOOD.THE AIRCRAF T WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A53EU 2001092000005 20010920 00005 WP 2001 9 20 MWEA011273 1 20010917 A 5523 5930497501 TAB DOUG DC9 DC981 3022081 WP LEFT ELEVATOR DAMAGED A MWEA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 GL 31 803ME 48029 LEFT ELEVATOR STUCK BY TAIL OF 812ME DURING PUSH BACK. -- OUTBOARD TRAILING EDGE OF TAB WAS CHIPPED. REPAIRED IAW SRM ( HOT BOND). 2 L 7 2 4F A6WE 2001092000008 20010920 00008 CE 2001 9 20 2001F00286 1 20010803 A 5330 SKIN BEECH 1900 1900D 1154162 CE FUSELAGE DENTED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 69548 UE193 AT FAR 121 ACCEPTANCE INSPECTION, DETERMINED LEFT FUSELAGE TO HAVE LARGE FLAT DENT AT FUSELAGE STATION 198.6 AND STRINGE R 6L. REPAIRED WITH FLUSH PATCH IAW MANUFACTURER'S STRUCTURAL REPAIR MANUAL. (M) 2 L 7 2 4T RT A24CE 2001092000009 20010920 00009 CE 2001 9 20 2001F00287 1 20010809 A 2620 SQUIB BEECH 1900 1900D 1154162 CE LT FIRE BOTTLE DIRTY A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 19 53545 UE185 FLT 9242 - FPO-FLL - DURING FLIGHT, LEFT FIRE EXTINGUISHER DISCHARGE LIGHT ILLUMINATED. INSPECTED AND CLEANED LEFT FIRE BOTTLE SQUIB. OPS CHECK NORMAL. (M) 2 L 7 2 4T RT A24CE 2001092000010 20010920 00010 CE 2001 9 20 2001F00288 1 20010809 A 2620 SQUIB BEECH 1900 1900D 1154162 CE LT FIRE BOTTLE DIRTY A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 19 53545 UE185 FLT 9242 - FPO-FLL - DURING FLIGHT, LEFT FIRE EXTINGUISHER DISCHARGE LIGHT ILLUMINATED. INSPECTED AND CLEANED LEFT FIRE BOTTLE SQUIB. OPS CHECK NORMAL. (M) 2 L 7 2 4T RT A24CE 2001092000011 20010920 00011 CE 2001 9 20 2001F00289 1 20010808 A 2620 SWITCH BEECH 1900 1900C 1154161 CE EXTINGUISH SYS DIRTY A GUUA O OTHER N FALSE WARNING LD LANDING 1 SO 19 137GA UC105 FLT 9437 - TLH-TPA - DURING LANDING, RIGHT FIRE EXTINGUISHER DISCHARGE LIGHT ILLUMINATED. CLEANED RIGHT FIRE EXTINGUISH ER TEST SWITCH. OPERATIONAL TEST NORMAL ON THE GROUND. (M) 2 L 7 2 4T RT A24CE 2001092000013 20010920 00013 CE 2001 9 20 2001F00290 1 20010809 A 2897 WIRE BEECH 1900 1900C 1154161 CE FUEL VENT CHAFED A H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 19 151GA UC171 FLT - 9262 - FPO-PBI - ON LANDING, LEFT FUEL VENT CIRCUIT BREAKER BEGAN TO EMIT SMOKE. MANUALLY PULLED CIRCUIT BREAKER. SMOKE STOPPED. CONTINUED TO LAND WITHOUT INCIDENT. DETERMINED WIRING ON LEFT FUEL VENT ASSEMBLY TO BE CHAFED. REPLA CED LEFT FUEL VENT ASSEMBLY AND WIRING, AND LEFT FUEL VENT CIRCUIT BREAKER, PART NR 7277-2-5. (M) 2 L 7 2 4T RT A24CE 2001092000014 20010920 00014 EA 2001 9 20 2001F00291 2 20010821 A 7321 8061328B FCU BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA RT ENGINE FAILED A GUUA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 19 130GA UC96 FLT 9139 - RSW/TPA - EN ROUTE FROM RSW TO TPA, THE RIGHT ENGINE LOST POWER. ADVANCED POWER LEVER AND THE RIGHT ENGINE C ONTINUED TO LOSE POWER. FLIGHT CREW SECURED THE ENGINE. EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLAC ED RIGHT FUEL CONTROL UNIT. (M) 2 L 7 2 4T 4 T RT A24CE E4EA 2001092000015 20010920 00015 EU 2001 9 20 2001F00292 1 20010829 A 5347 EPNE95300013019 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 536AT 536 SAW - DURING CPCP4 INSPECTION, FOUND CORROSION ON THE LEFT AFT OUTBOARD, RT AFT OUTBOARD, LEFT F/A, RT F/A AND LT AFT CA RGO SEAT TRACKS. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW EO E2-53MR-115. THE AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200124207. (M) 2 H 7 2 4T RT A53EU 2001092000016 20010920 00016 EU 2001 9 20 2001F00293 1 20010829 A 5347 S53678001210 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 536AT 536 SAW - DURING CPCP4 INSPECTION, FOUND CORROSION ON THE LEFT AFT OUTBOARD, RIGHT AFT OUTBOARD, LT F/A, RT F/A AND LEFT AFT CARGO SEAT TRACKS. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW EO E2-53MR-115. THE AIRCRAFT WAS RETURNED TO SERVICE . REF SIMA200124207 (M) 2 H 7 2 4T RT A53EU 2001092000017 20010920 00017 EU 2001 9 20 2001F00294 1 20010829 A 5347 S53678001246 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 536AT 536 SAW - DURING CPCP4 INSPECTION, FOUND CORROSION ON THE LEFT AFT OUTBOARD, RT AFT OUTBOARD, LEFT F/A, RT F/A AND LT AFT CA RGO SEAT TRACKS. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW EO E2-53MR-115. THE AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200124207. (M) 2 H 7 2 4T RT A53EU 2001092000018 20010920 00018 EU 2001 9 20 2001F00295 1 20010829 A 5347 EPNE95300013020 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 536AT 536 SAW - DURING CPCP4 INSPECTION, FOUND CORROSION ON THE LEFT AFT OUTBOARD, RT AFT OUTBOARD, LEFT F/A, RT F/A AND LT AFT CA RGO SEAT TRACKS. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW EO E2-53MR-115. THE AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200124207. (M) 2 H 7 2 4T RT A53EU 2001092000019 20010920 00019 EU 2001 9 20 2001F00296 1 20010829 A 5315 S5367240725202 FLOORBEAM AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 536AT 536 SAW - DURING CPCP4 INSPECTION, FOUND CORROSION ON FLOORBEAMS 36, 38 AND 39. THE FLOORBEAMS WERE REMOVED AND REPLACED IA W ATR72 SRM 51-25-01, 51-25-04 AND 51-25-02. THE AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200124206. (M) 2 H 7 2 4T RT A53EU 2001092000020 20010920 00020 EU 2001 9 20 2001F00297 1 20010829 A 5315 S5367240725202 FLOORBEAM AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 536AT 536 SAW - DURING CPCP4 INSPECTION, FOUND CORROSION ON FLOORBEAMS 36, 38 AND 39. THE FLOORBEAMS WERE REMOVED AND REPLACED IA W ATR72 SRM 51-25-01, 51-25-04 AND 51-25-02. THE AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200124206. (M) 2 H 7 2 4T RT A53EU 2001092000021 20010920 00021 EU 2001 9 20 2001F00298 1 20010829 A 5320 S53671217294 SILL AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 536AT 536 SAW - DURING CPCP4 INSPECTION, FOUND CORROSION ON PASSENGER ENTRY SILL AND THE SERVICE DOOR SILL PLATES. THE SILLS WERE REMOVED AND REPLACED IAW ATR72 SRM 51-25-01 AND 51-25-02. THE AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200124205. ( M) 2 H 7 2 4T RT A53EU 2001092000022 20010920 00022 EU 2001 9 20 2001F00299 1 20010829 A 5320 S5367800920102 FLOOR SUPPORT AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 242AT 242 SAW - DURING CPCP2 INSPECTION, FOUND CORROSION ON THE LEFT AND RIGHT FLOOR SUPPORTS FROM FRAME 36 TO FRAME 38. THE FLOO R SUPPORTS WERE REMOVED AND REPLACED IAW ATR SRM 51-25-01 AND 51-25-02. THE AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA 200124204. (M) 2 H 7 2 4T RT A53EU 2001092000023 20010920 00023 EU 2001 9 20 2001F00300 1 20010829 A 5320 S5367121729401 SILL AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 242AT 242 SAW - DURING CPCP2 INSPECTION, FOUND CORROSION ON PASSENGER ENTRY SILL PLATE AND THE SERVICE DOOR SILL PLATE. THE PASSE NGER AND SERVICE DOOR SILLS WERE REMOVED AND REPLACED IAW ATR SRM 51-25-02, AND 51-25-03. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001092000024 20010920 00024 WP 2001 9 20 2001F00301 1 20010919 A 8011 492651AF STARTER DOUG DC4 C54BDC 3021516 WP ENGINE INOPERATIVE A B2OB O OTHER O OTHER NR NOT REPORTED 1 AL 03 44911 10461 BURNS AND BRUSHES DON'T WORK. (M) 2 L 7 4 4R A762 2001092000025 20010920 00025 2001 9 20 2001F00302 4 20010919 A 3452 KT76 LIGHT DOUG DC4 C54BDC 3021516 WP TRANSPONDER INOPERATIVE A B2OB K NONE L NO TEST NR NOT REPORTED 1 AL 03 44911 10461 TEST BUTTON QUIT WORKING, NO LIGHT. (M) 2 L 7 4 4R A762 2001092000026 20010920 00026 NE 2001 9 20 2001F00303 2 20010806 A 7411 COIL DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE ENGINE FAULTY A B2OB K NONE O OTHER IN INSP/MAINT 1 AL 03 44911 10461 LEFT MAG NR 4 ROUGH ON PARKING CHECK. COIL WAS BAD AND IT WAS REPLACED. (M) 2 L 7 4 4R 4 R A762 5E5 2001092000028 20010920 00028 SO 2001 9 20 ACSA020A 2 20010607 A 8500 649134 CRANKSHAFT CESSNA 207 207A 2073604 CE CONT O520 IO520F 17032 SO ENGINE BROKEN E ACSA K NONE O OTHER IN INSP/MAINT 1 AL 01 917AC 346 20700517 814871R ENGINE WAS NOT MAKING FULL RPM. PROP GOV WAS REPLACED, GROUND RUN WAS NORMAL. SHORTLY AFTER TAKEOFF OIL PRESSURE FELL BELOW GREEN ARC. PILOT WAS SHUTTING THE ENGINE DOWN, OIL APPEARED ON THE WINDSHIELD, LOUD BANG WAS HEARD, AND PROPELLER DEPARTED THE AIRCRAFT. PILOT LANDED WITHOUT ANY FURTHER DAMAGE TO AIRCRAFT. CRANKSHAFT BROKE AT CRANKCASE NOSE SEAL. ENGINE HAD 346.9 HOURS TIME SINCE REBUILD BY MFG. AT 252.6 HOURS TIME SINCE REBUILD, THIS CRANKSHAFT WAS INSTALLED BY MFG IN COMPLIANCE WITH AD99-09-17, CSB99-3A. CRANKSHAFT WAS OF INFERIOR COMPOSITION? AD 2000-23-21 ADDRESSES THIS. 1 H 7 1 3O 3 O A16CE E5CE 2001092000031 20010920 00031 WP 2001 9 20 ABXA010483 1 20010830 A 5400 591326243 ANGLE DOUG DC9 DC932 3022066 WP L PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 THE UPPER PYLON ATTACH ANGLE WAS FOUND TO BE CRACKED AT THE FORWARD END. MAINTENANCE REPAIRED THE ANGLE IAW DC-9 SRM 54- 04 FIG. 10. 2 L 7 2 4F A6WE 2001092000032 20010920 00032 WP 2001 9 20 ABXA010484 1 20010830 A 5320 49125401 FITTING DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 THE CABIN FLOOR LH VERTICAL SUPPORT UPPER FITTING WAS FOUND TO BE CRACKED AT STA 965. MAINTENANCE REPLACED THE CABIN FLO OR LH VERTICAL SUPPORT UPPER FITTING IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2001092000033 20010920 00033 WP 2001 9 20 ABXA010485 1 20010831 A 5320 591359611 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 SHEAR TIE WAS FOUND CRACKED AT FUSELAGE STATION 1059 L17L. MAINTENANCE REPLACED THE SHEAR TIE SECTION IAW DC-9 SRM. 2 L 7 2 4F A6WE 2001092000034 20010920 00034 WP 2001 9 20 ABXA010486 1 20010820 A 5310 99196181 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 MAIN FRAME AT STATION 718L WAS CRACKED BETWEEN "Z" ANGLE FASTENERS. MAINTENANCE REPAIRED THE FRAME IAW ABX EA 53400210-0 01-1. 2 L 7 2 4F A6WE 2001092000035 20010920 00035 WP 2001 9 20 ABXA010487 1 20010831 A 5310 99196192 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 MAIN FRAME AT STATION 737R WAS CRACKED BETWEEN "Z" ANGLE FASTENERS. MAINTENANCE REPAIRED THE FRAME IAW ABX EA 53400320-0 01-1. 2 L 7 2 4F A6WE 2001092000036 20010920 00036 WP 2001 9 20 ABXA010488 1 20010831 A 5311 99582387 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 FRAME WAS FOUND CRACKED AT FUSELAGE STATION 980,L16L. MAINTENANCE REPAIRED THE FRAME IAW DC-9 SRM. 2 L 7 2 4F A6WE 2001092000037 20010920 00037 WP 2001 9 20 ABXA010489 1 20010831 A 5320 99577397 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 SHEAR TIE REPAIR WAS FOUND TO BE CRACKED AT FUSELAGE STATION 945 L14R. MAINTENANCE REPLACED THE SHEAR TIE IAW DC-0 SRM 5 1-30-2. 2 L 7 2 4F A6WE 2001092000038 20010920 00038 WP 2001 9 20 ABXA010490 1 20010831 A 5320 995823870 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 SHEAR TIE REPAIR WAS FOUND TO BE CRACKED AT FUSELAGE STATION 980, L16R. MAINTENANCE REPLACED THE SHEAR TIE IAW DC-9 SRM AND ABX DRAWING N07080. 2 L 7 2 4F A6WE 2001092000039 20010920 00039 WP 2001 9 20 ABXA010492 1 20010904 A 5320 991150985 RIB DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 CORROSION FOUND ON RIB LOCATED IN THE RIGHT NOSE WHEEL TUNNEL STATION 100, BELOW PRESSURE WEB. MAINTENANCE INSTALLED A D OUBLER IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 2001092000040 20010920 00040 WP 2001 9 20 ABXA010494 1 20010904 A 5330 5911407503 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT THE AFT LOWER CORNER OF SERVICE DOOR CUT OUT. MAINTEANCE REPAIRED THE AREA IAW ABX EA 53100123-001. 2 L 7 2 4F A6WE 2001092000041 20010920 00041 WP 2001 9 20 2001F00304 1 20010730 A 7100 CAP SEAL DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE ENGINE LEAKING A B2OB O OTHER K FLUID LOSS NR NOT REPORTED 1 AL 03 44911 10461 PIN CAP SEAL WAS LEAKING. PIN CAP SEAL WAS CHANGED. 2 L 7 4 4R 4 R A762 5E5 2001092000042 20010920 00042 CE 2001 9 20 B4O2001F00000 1 20010725 A 2810 SEALANT CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO FUEL CELL DETERIORATED E B4OA K NONE O OTHER IN INSP/MAINT 1 WP 07 510NE 402C1001 THE WINGS WERE OPENED TO COMPLY WITH A 1200 HOUR INSPECTION AND THE FOLLOWING SITUATION WAS FOUND: 1) SEALANT: TURNING BROWN/TAN, TEXTURE: SOFTER THAN NORMAL WITH FUEL DRAINED AND TANK PLATES OPEN, AFTER 4 DAYS EXPOSED TO AIR, SEALANT TEXT URE WAS RETURNING TO NORMAL. 2) OB END OF TANK, ABOVE FULL FUEL LEVEL LINE, SEALANT SURFACE WAS CRACKING ACROSS FACE A ND ALONG EDGES, SEPARATEING FROM TANK SURFACE AT EDGE OF CRACKS. SEALANT WAS THIN AT EDGES, NO RUBBER CONSISTENCY LEFT, IT SCRAPED OFF LIKE DRY DIRT. WHERE SEALANT WAS THICK, TEXTURE WAS GUMMY AND WAS GRAYER IN COLOR AS WITH SEALANT AFTER AIR EXPOSURE. BEGAN TO STIFFEN BUT WAS TOO FAR GONE TO SAVE. GRAY POWDER WAS FOUND INSIDE TANK, SUSPECT DETERIORATING 1 L 7 2 3O 3 O A7CE E8CE 2001092000043 20010920 00043 WP 2001 9 20 2001F00305 1 20010531 A 2913 PF171911 PUMP DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE ENGINE FAILED A B2OB O OTHER O OTHER NR NOT REPORTED 1 AL 03 44911 1400 10461 HYD PUMP HAD SEAL FAILURE. SHAFT SEAL FAILED. (M) 2 L 7 4 4R 4 R A762 5E5 2001092000044 20010920 00044 SO 2001 9 20 BSY2001F00010 1 20010909 A 2913 1213HBG310A PUMP PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540* 41533 EA HYD SYSTEM INOPERATIVE E BSYA K NONE O OTHER IN INSP/MAINT 1 GL 07 35871 318052123 996661A PHL M.I.R. GEAR WOULD NOT RETRACT, GEAR UNSAFE LIGHT ON AND HANDLE WOULD NOT RETURN TO NEUTRAL. FOUND LEFT ENGINE DRIVEN HYDRAULIC PUMP, INOPERATIVE. REMOVED AND REPLACED, PUMP OPS CHECK GOOD. 1 L 7 2 3O 3 O A20SO E14EA 2001092000045 20010920 00045 CE 2001 9 20 BSY2001F00011 1 20010909 A 7603 50389012 THROTTLE CABLE BEECH 58 58 1152740 CE CONT O520 IO520* 17032 SO RT ENGINE BROKEN E BSYA O OTHER O OTHER NR NOT REPORTED 1 GL 07 6573K TH1369 299411R (TFB) M.I.R. RIGHT ENGINE THROTTLE STUCK AT FULL THROTTLE. REMOVED AND REPLACED BROKEN THROTTLE CABLE. 1 L 7 2 3O 3 O 3A16 E5CE 2001092000051 20010920 00051 WP 2001 9 20 2001F00307 1 20010705 A 2432 688601752024 CELL DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE BATTERY DISCHARGED A B2OB O OTHER O OTHER NR NOT REPORTED 1 AL 03 44911 10461 BATTERY HAS DEAD CELL. (M) 2 L 7 4 4R 4 R A762 5E5 2001092000052 20010920 00052 NE 2001 9 20 2001F00308 2 20010728 A 7420 LEAD DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE NR 3 ENGINE WORN A B2OB O OTHER O OTHER NR NOT REPORTED 1 AL 03 44911 1100 10461 HIGH TENSION LEAD WORN. (M) 2 L 7 4 4R 4 R A762 5E5 2001092000054 20010920 00054 WP 2001 9 20 2001F00309 1 20010725 A 7714 PIN DOUG DC4 C54BDC 3021516 WP TACHOMETER LOOSE A B2OB O OTHER O OTHER NR NOT REPORTED 1 AL 03 44911 10461 THE PIN ON THE TACH NEEDED RESOLDERD. OPS CHECK GOOD. (M) 2 L 7 4 4R A762 2001092000056 20010920 00056 NE 2001 9 20 2001F00310 2 20010808 A 8500 ENGINE DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE ENGINE MAKING METAL A B2OB O OTHER O OTHER NR NOT REPORTED 1 AL 03 44911 10461 P108336 FOUND METAL CONTAMINATION. (M) 2 L 7 4 4R 4 R A762 5E5 2001092000058 20010920 00058 WP 2001 9 20 2001F00311 1 20010919 A 7714 AN55311 WIRE DOUG DC4 C54BDC 3021516 WP TACH GENERATOR BROKEN A O OTHER O OTHER NR NOT REPORTED 1 AL 03 44911 10461 BROKE WIRE ON CANNON PLUG. (M) 2 L 7 4 4R A762 2001092000060 20010920 00060 WP 2001 9 20 2001F00312 1 20010919 A 3244 TIRE DOUG DC4 C54BDC 3021516 WP MLG DAMAGED A B2OB O OTHER O OTHER NR NOT REPORTED 1 AL 03 44911 1500 10461 TIRE HAS MISSING CHUNK OF RUBBER IN CENTER ABOUT 10 INCHES LONG, NR 4 MAIN. (M) 2 L 7 4 4R A762 2001092000062 20010920 00062 WP 2001 9 20 2001F00313 1 20010919 A 3242 1511831 PAD DOUG DC4 C54BDC 3021516 WP NR 1 BRAKE WORN A B2OB O OTHER O OTHER NR NOT REPORTED 1 AL 03 44911 1400 10461 PADS WORN ON BRAKE, NEEDS OVH, NR 1 BRAKE. (M) 2 L 7 4 4R A762 2001092000063 20010920 00063 NE 2001 9 20 2001F00314 2 20010919 A 7421 ELECTRODE DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE SPARK PLUG MISSING A B2OB O OTHER O OTHER NR NOT REPORTED 1 AL 03 44911 350 10461 FOUND CENTER ELECTRODE MISSING FROM PLUG. (M) 2 L 7 4 4R 4 R A762 5E5 2001092000064 20010920 00064 WP 2001 9 20 2001F00315 1 20010705 A 7923 2E6013 VALVE DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE OIL SYSTEM LEAKING A B2OB O OTHER K FLUID LOSS NR NOT REPORTED 1 AL 03 44911 10461 LEAK AT SURGE PROTECTION VALVE. (M) 2 L 7 4 4R 4 R A762 5E5 2001092000065 20010920 00065 WP 2001 9 20 2001F00316 1 20010705 A 7930 AN57652 TRANSMITTER DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE NR 4 ENGINE RUPTURED A B2OB O OTHER O OTHER NR NOT REPORTED 1 AL 03 44911 10461 NR 4 ENGINE RUPTURED DIAPHRAM. (M) 2 L 7 4 4R 4 R A762 5E5 2001092000066 20010920 00066 WP 2001 9 20 2001F00317 1 20010705 A 3244 TIRE DOUG DC4 C54BDC 3021516 WP MLG WORN A B2OB O OTHER O OTHER NR NOT REPORTED 1 AL 03 44911 10461 FOUND TIRE OUT OF LIMITS. (M) 2 L 7 4 4R A762 2001092000067 20010920 00067 WP 2001 9 20 2001F00318 1 20010705 A 3242 1511831 BRAKE DOUG DC4 C54BDC 3021516 WP MLG WORN A B2OB O OTHER O OTHER NR NOT REPORTED 1 AL 03 44911 1000 10461 FOUND BRAKE WORN, NEED OVH. NO MORE ADJUSTMENT. (M) 2 L 7 4 4R A762 2001092000069 20010920 00069 NE 2001 9 20 2001F00320 2 20010705 A 8530 88962 GASKET DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE ENGINE LEAKING A B2OB O OTHER K FLUID LOSS NR NOT REPORTED 1 AL 03 44911 10461 CHANGED A FEW ROCKER GASKETS ON ALL ENGINES FOR LEAKING. (M) 2 L 7 4 4R 4 R A762 5E5 2001092000070 20010920 00070 WP 2001 9 20 2001F00321 1 20010702 A 7100 77688 CAP SEAL DOUG DC4 C54BDC 3021516 WP ENGINE LEAKING A B2OB O OTHER K FLUID LOSS NR NOT REPORTED 1 AL 03 44911 10461 CHANGED A FEW PIN CAP SEALS ON ALL ENGINES FOR LEAKING. (M) 2 L 7 4 4R A762 2001092000071 20010920 00071 NE 2001 9 20 2001F00322 2 20010713 A 8520 STUD DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE NR 4 ENGINE BROKEN A B2OB O OTHER O OTHER NR NOT REPORTED 1 AL 03 44911 10461 107886 CYLINDER STUDS BROKE. CHANGED CYLINDER AND ALL STUDS ON THAT CYLINDER. (M) 2 L 7 4 4R 4 R A762 5E5 2001092000072 20010920 00072 NE 2001 9 20 2001F00323 2 20010716 A 7411 COIL DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE NR 3 ENGINE DAMAGED A B2OB O OTHER O OTHER NR NOT REPORTED 1 AL 03 44911 1200 10461 107886 MATTER FROM INSIDE THE COIL WAS LEAKING OUT CAUSING ELECTRICITY TO RUN ELSEWHERE, NOT THROUGH COIL. (M) 2 L 7 4 4R 4 R A762 5E5 2001092000074 20010920 00074 CE 2001 9 20 2001F00284 1 20010818 A 2620 30100023 EXTINGUISHER BEECH 1900 1900D 1154162 CE LT ENGINE MALFUNCTIONED A GUUA O OTHER N FALSE WARNING CL CLIMB 1 SO 19 53545 UE185 FLT 9317 - FLL/ELH - AFTER TAKEOFF, THE LEFT FIRE EXTINGUISHER DISCHARGE LIGHT ILLUMINATED, THEN WENT OUT. AIRCRAFT RET URNED TO FLL AND LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINE FIRE EXTINGUISHER ASSEMBLY. (M) 2 L 7 2 4T RT A24CE 2001092000078 20010920 00078 EU 2001 9 20 ASOA01130S 1 20010806 A 5311 FRAME AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 630AS 336 DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND AT FRAMES 36, 38, 39, 40, AND 41. CORROSION WAS ALSO FOUND ON THE FORWARD RADAR ALTIMETER CUTOUT BETWEEN FRAMES 15 AND 16. MAINTENANCE REPAIRED CORROSION TO THE FUSELAGE IAW ASA EO 72- 53-0114. THIS EO INCLUDES REPAIR SPECIFICATIONS FOR AIRCRAFT CORROSION. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT 2001092000080 20010920 00080 EU 2001 9 20 ASOA01145 1 20010815 A 3350 SM400D41 CONTACTOR AEROSP ATR72 ATR72 EU COCKPIT FAILED A ASOA K NONE O OTHER TX TAXI/GRND HDL 1 SO 11 536AS 465 FLT 4085 - DURING TAXI IN ATL, CREW REPORTED EMERGENCY LIGHTS IN CABIN CAME ON WHEN THE COCKPIT SWITCH WAS IN THE ARM PO SITION DURING HOTEL MODE AND SINGLE TAXI. THE EMERGENCY LIGHTS WENT OUT WHEN NR 1 GENERATOR CAME ONLINE. MAINTENANCE R EMOVED AND REPLACED CONTACTOR 12PU. OPERATIONAL CHECKS NORMAL. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2001092000082 20010920 00082 NM 2001 9 20 0103295503 1 20010827 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 503US 23192 DURING "H" CHECK FOUND CORROSION ON FLOORBEAM UPPER SURFACE AT BS 1280 LBL 24 TO RBL 24. REPAIRED PER EA 55-185615. 2 L 7 2 4F RT A2NM 2001092000083 20010920 00083 EU 2001 9 20 ASOA01146 1 20010822 A 3350 3011210 LIGHT AEROSP ATR72 ATR72 EU CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 642AS 395 DURING HANGAR MAINTENANCE IN MCN, PASSENGER DOOR EMERGENCY LIGHTS WERE REPORTED INOPERATIVE. MAINTENANCE REMOVED AND RE PLACED PASSENGER DOOR EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2001092000084 20010920 00084 EU 2001 9 20 ASOA01147 1 20010823 A 3350 3011210 LIGHT AEROSP ATR72 ATR72 EU CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 536AS 2915 465 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D TEH PASSENGER DOOR EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2001092000085 20010920 00085 EU 2001 9 20 ASOA01148 1 20010823 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72 EU CABIN DISCHARGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 630AS 336 DURING GROUND INSPECTION IN ATL, THE FIRST FEW EMERGENCY LIGHTS STAYED ON. MAINTENANCE REMOVED AND REPLACED THE EMERGEN CY POWER SUPPLY AT THE 43WL POSITION. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2001092000088 20010920 00088 NM 2001 9 20 GAIA01305OP 1 20010831 A 2782 1U109592 ACTUATOR BOEING 727 727223 1384074 NM NR 8 SLAT FAILED A GAIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 07 6827 20180 FLT - 1843 - PHL-FWA - ON APPROACH TO FWA, THE FLIGHT CREW NOTICED THAT THE NR 8 SLAT DID NOT INDICATE EXTENDED WHEN THE FLAP HANDLE WAS MOVED FROM 2 DEGREES TO THE 5 DEGREE POSITION. AN EMERGENCY WAS DECLARED AND A UNEVENTFUL LANDING WAS MADE AT FWA. REMOVED AND REPLACED THE NR 8 SLAT ACTUATOR AND NR 8 SLAT POSITION SWITCH. THE SYSTEM OPERATIONALLY CHECK ED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001092000089 20010920 00089 SO 2001 9 20 SIMA200122405 1 20010812 A 3350 7287580509 LIGHT EMB 145 EMB145LR SO CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 620AE 145102 ORD - FLT 4382 - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS AT ROWS 10 AND 11 TO BE INOPERATIVE. MAINTENANCE RE MOVED AND REPLACED THE LIGHT STRIP IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001092000090 20010920 00090 EU 2001 9 20 SIMA200124203 1 20010829 A 5320 S5367131830402 SILL AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 242AT 242 SAW - DURING CPCP2 INSPECTION, FOUND CORROSION ON PASSENGER ENTRY SILL PLATE AND THE SERVICE DOOR SILL PLATE. THE PASSE NGER AND SERVICE DOOR SILLS WERE REMOVED AND REPLACED IAW ATR SRM 51-25-01, 51-25-02 AND 51-25-03. THE AIRCRAFT WAS RET URNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001092000092 20010920 00092 NM 2001 9 20 TSAA0130036 1 20010905 A 3040 HARNESS BOEING 737 737209 NM COCKPIT BURNED A TSAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 13 827AL 23913 FLT - 41 - ITO-HNL - INBOUND FROM HILO, HAD STRONG ELECTRICAL SMOKE SMELL IN COCKPIT AND SOME SMOKE SMELL IN CABIN AROUN D ROW 5. DECLARED EMERGENCY. LANDED SAFELY IN HNL. FOUND WINDOW HARNESS AT THE RIGHT SIDE WINDOW BURNED AT THE QUICK DISCONNECT. WINDOW HEAT DEFERRED PER MEL 30-11, CONTROL NR 2428C04. REPAIRED WIRE ON RIGHT SIDE WINDOW HARNESS. OPS C HECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001092000095 20010920 00095 NM 2001 9 20 TSAA0133114 1 20010831 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 39735 REPLACED NR 1 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001092000097 20010920 00097 2001 9 20 UIEA01096 4 20010904 A 2565 7A14124 SLIDE BOEING 747 747400 NM UPPER DECK FAILED A UIEA K NONE L NO TEST IN INSP/MAINT 1 EA 15 498MC 29260 DURING C-CHECK IN FRA, THE UPPER DECK SLIDE WOULD NOT DEPLOY DURING TEST. FOUND 2 RELEASE PINS ON THE PACK BOARD LOWER HORIZONTAL BAR NOT PULLED. THE RELEASE PINS WERE ROTATED AND CAUGHT ON THE EDGE OF THE RELEASE PIN CAUSING THEM TO GET CAUGHT IN THE OPENING OF THE HOLE. REMOVED SLIDE AND INSTALLED NEW SLIDE IAW MM. (M) 2 L 7 4 4F RT A20WE 2001092000099 20010920 00099 WP 2001 9 20 USAA011137 1 20010821 A 5210 SKIN DOUG DC9 DC981 3022081 WP DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 809US 53852 48041 CLT - FOUND DOOR SKIN CRACKED 3 INCHES, AFT END OF DOOR HOLD OPEN HOOK/DOOR SKIN. INSTALLED DOUBLER PER SRM 52-05 FIG 2 0A. (M) 2 L 7 2 4F A6WE 2001092000101 20010920 00101 EU 2001 9 20 USAASA01047 1 20010829 A 3397 WIRE AIRBUS 330 A330202 3930316 EU CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 EA 19 112US 1134 LGA - THE FORWARD CLOSET EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRES IN THE WIRE HARNESS ASSEMBL Y FOR THE FORWARD CLOSET. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A46NM 2001092000102 20010920 00102 EU 2001 9 20 USAASA01048 1 20010830 A 3350 32145510 POWER SUPPLY AIRBUS A321 A321211 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 166US 1436 PHL - THE LEFT MID-CABIN EMERGENCY LIGHT WILL NOT ILLUMINATE. MAINTENANCE REPLACED THE LEFT EMERGENCY POWER SUPPLY UNIT . OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2001092000103 20010920 00103 NM 2001 9 20 USAASB01230 1 20010812 A 2131 7612608 CONTROLLER BOEING 737 737301 1384611 NM CABIN PRESSURE FAILED A USAA G B O2 MASK DEPLOYED EMER. DESCENT O OTHER CR CRUISE 1 EA 19 584US 75 23743 PBI - FLT 431 - EN ROUTE FROM DCA TO PBI, AT FL350 AND 100 TO 120 MILES OUT FROM PBI, THE AIRCRAFT DEPRESSURIZED, CABIN ALTITUDE WENT TO 15,000 FEET AND THE OXYGEN MASKS AUTO DEPLOYED. CREW DECLARED AN EMERGENCY, DESCENDED AIRCRAFT TO 10,0 00 FEET AND SWITCHED TO MANUAL DC TO STABILIZE THE CABIN PRESSURE. FLIGHT LANDED AT PBI WITHOUT FURTHER INCIDENT. MX RE MOVED AND REPLACED THE CABIN PRESSURE CONTROLLER PER MM 21-31-00. OPERATIONAL CHECK GOOD. REMOVED AND REPLACED THE DELT A P A/C MODULE (P/N 65-45314-53) PER MM 21-31-22 AND TESTED BOTH SAFETY RELIEF VALVES PER MM 21-32-21. CABIN PRESSURIZAT ION CHECKS NORMAL PER MM 21-31-00. REPLACED O2 GENERATORS, REPLACED OXYGEN MASKS AND STOWED. (M) 2 L 7 2 4F RT A16WE 2001092000109 20010920 00109 NM 2001 9 20 USAASB01245 1 20010829 A 2160 32902062 CONTROL VALVE BOEING 737 7374B7 1384702 NM A/C BAY DEFECTIVE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 432US 24554 PBI - FLT 002 - CLIMBING-OUT OF MIA TO FL290, EN ROUTE TO PHL, THE LT WING-T0-BODY OVERHEAT LIGHT ILLUMINATED. CREW ACCO M QRH PROCEDURES BUT COULD NOT MAINTAIN CABIN ALTITUDE, CABIN PRESSURE ROSE TO 11,000 FT. CREW COULD NOT GET THE CABIN P RESSURE TO LOWER AND WITH THE WING-TO-BODY OVERHEAT LIGHT NOT EXTINGUISHING. DIVERTED TO NEAREST AIRPORT. FLT LANDED WI THOUT INCIDENT. EMERGENCY WAS DECLARED. MX R&R THE LT ACM, REMAINED RUNNING HOT. FOUND LT STANDBY TEMP CONTROL VALVE TO BE CREEPING OPEN CAUSING PACK TO RUN HOT. R&R STANDBY TEMP CONTROL VALVE. OPS AND LEAK CHECK GOOD. R&R OVERHEAT MODULE ( P/N 65-52808-7). OPS CHECK GOOD WITH LT PACK AND LT ENGINE BLEED SUPPLYING SYSTEM. AS FOR PRESSURIZATION PROBLEM, INSPE 2 L 7 2 4F RT A16WE 2001092000111 20010920 00111 WP 2001 9 20 CA010817001 2 20010817 A 7321 89778015 FUEL CONTROL SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE RT ENGINE MALFUNCTIONED W E ENGINE SHUTDOWN W E J INADEQUATE Q C VIBRATION/BUFFET WARNING INDICATION AP APPROACH 1 CA 7557 2658 (CAN) AIRCRAFT WAS ON APPROACH AND THE RIGHT HAND ENGINE WENT TO FULL POWER AND WENT INTO BY-PASS. THE PILOT TRIED TO R ETARD POWER BUT THERE WAS NO EFFECT. PILOT SHUT THE RIGHT HAND ENGINE DOWN AND LANDED WITHOUT INCIDENT. FCU AN DUMP WE RE REPLACED AS AN ASSEMBLY. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 2001092000122 20010920 00122 SW 2001 9 20 CA010822001 1 20010807 A 6120 HCE4N5D CONTROLLER SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP HARTZL HCB3T HCB3TN5 GL LT PROPELLER FLUCTUATES W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 401 (CAN) DURING TAKEOFF ROLL THE POWER ON THE LT ENGINE WOULD FLUCTUATE BETWEEN 80 AND 100 PERCENT. THE LT PROPELLER WAS R EPLACED, RESOLVING THE PROBLEM. THE REMOVED PROPELLER WAS SENT TO A REPAIR FACILITY FOR FURTHER INSPECTION. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P15EA 2001092000123 20010920 00123 WP 2001 9 20 0103279933 1 20010330 A 5330 29536591 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1334U 47280 DURING AN L-CHECK. THE LOWER AFT CORNER OF THE SERVICE DOOR SKIN WAS FOUND WITH CRACKS. THE SUBJECT SKIN PANEL WAS TRIM MED AND RESTORED USING A SPLICE AFT OF THE DOOR CUT OUT USING EA 99-169344 LOG PAGE 1577098. THE EXISTING SKIN ASSEMBLY 5911407-33 IS MANUFACTURE PART NUMBER 2953659-1. 2 L 7 2 4F A6WE 2001092000124 20010920 00124 NM 2001 9 20 AWXA200100449 1 20010918 A 2612 350F51000 CIRCUIT BOARD AIRBUS A319 A319132 NM COCKPIT FAULTY A AWXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 814AW 1281 PHX - AIR TURNBACK - FLT 803 - C - DURING CLIMBOUT OF PHX TO SFO, THE NR 1 ENG FIRE LIGHT AT THE START SWITCH AND OVERHE AD INDICATION CAME ON TWICE, (NO ECAM INDICATION OR CRC). THE AIRCRAFT WAS RETURNED TO PHX MAKING AN UNEVENTFUL LANDING . MAINTENANCE TROUBLESHOT PER TSM 26-12-00-810 AND REPLACED ANNUNCIATOR LIGHT INTERFACE BOARDS 5LP & 18LP PER AMM 33-14 -33. INDICATIONS AND OPERATIONAL TESTS WERE NORMAL. (NOTE: 2 BOARDS WERE REPLACED, SAME P/N). 2 L 7 2 4F RT A28NM 2001092000125 20010920 00125 SO 2001 9 20 C2XA01BT166 1 20010915 A 3350 LIGHT EMB 145 EMB145ER SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15941 145035 EWR---CO2951, CREW REPORTED GALLEY DOOR EMERGENCY EXIT LIGHT BURNED OUT. MAINTENANCE REMOVED AND REPLACED GALLEY EMERGE NCY DOOR EMERGENCY EXIT LIGHT. OPS CHECKED GOOD IAW EMB145 AMM 33-50-00. 2 L 7 2 4F RT T00011AT 2001092000126 20010920 00126 SO 2001 9 20 C2XA01CL204 1 20010917 A 4990 OIL CAP EMB 135 EMB135ER 3260203 SO APU OUT OF POSITION A C2XA D RETURN TO BLOCK K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 SW 27 16511 145267 CLE FLIGHT 3864 THE CREW REPORTED A LAV SMOKE WARNING INDICATION ON TAXI OUT WITH A SMELL OF SMOKE IN LAV. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND THE APU OIL SERVICE CAP WAS OFF AND OIL LEAKING OUT OF RESERVOIR. THE APU WAS SERVICED TO PROPER LEVEL AND THE CAP WAS INSTALLED. THE SPILLED OIL WAS CLEANED UP. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001092000127 20010920 00127 SO 2001 9 20 C2XA01IA360 1 20010919 A 5315 14521699001 FLOORBEAM EMB 145 EMB145LR SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14950 145060 IAH - DURING C-CHECK INSPECTION, THE LEFT HAND DIGITAL AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE A FFECTED DIGITAL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001092000128 20010920 00128 SO 2001 9 20 C2XA01IA361 1 20010919 A 2150 A/C PACK EMB 120 EMB120ER 3260203 SO A/C BAY MALFUNCTIONED A C2XA H B DEACTIVATE SYST/CIRCUITS EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 16724 120171 LFK - FLIGHT 3442, THE CREW REPORTED HEAVY SMOKE IN THE COCKPIT WITH AN ELECTRICAL SMELL. THE CREW DE-SELECTED PACKS AN D PERFORMED AN EMERGENCY DESCENT. THE AIRCRAFT LANDED AT JFK WITHOUT INCIDENT WHERE MAINTENANCE PLACED THE NUMBER TWO P ACK ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001092000129 20010920 00129 NM 2001 9 20 01FDEA00848 1 20010919 A 2780 BUSHING BOEING 727 727233 138408A NM WORN A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 286FE 22623 01-317 ON CLIMB GOT AN AMBER LEAD EDGE FLAP LIGHT. R&R WORN BUSHING & ADJ PER MM 27-82-001-4. 2 L 7 3 4F RT A3WE 2001100900157 20011009 00157 NM 2001 10 9 01FDEA00850 1 20010918 A 5330 SKIN BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 N 490 CORROSION ON FUSELAGE SKIN INNER SIDE BS 498, RBL 7, WL 148. R&R SKIN PER EA 7-5330-59857. 2 L 7 3 4F RT A3WE 2001100900158 20011009 00158 NM 2001 10 9 01FDEA00851 1 20010918 A 5310 STRINGER BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 N 489 STRINGER 28R CORRODED AT BS 498. R&R STRINGER PER SRM 53-10-1 FIG 1. 2 L 7 3 4F RT A3WE 2001092000130 20010920 00130 NM 2001 9 20 CALA0100885 1 20010919 A 5754 SKIN BOEING 737 7373T0 1384582 NM #3 SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND A 2" CRACK IN #3 SLAT LOWER BULLNOSE SKIN AT TWO RIVETS BELOW STOP O/B OF THE ACTUATOR. THE CRACKED ARE A WAS CUT OUT AND FILLER AND SPLICE PLATE WERE INSTALLED IAW SRM 57-43-01, FIGURE 206. 2 L 7 2 4F RT A16WE 2001092000131 20010920 00131 NM 2001 9 20 CALA0100888 1 20010919 A 5230 SKIN BOEING 737 7373T0 1384582 NM AFT CARGO DR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND THE AFT CARGO DOOR SKIN DENTED AT TWO LOCATIONS. A DOUBLER REPAIR WAS INSTALLED AT EACH LOCATION IAW SR M 52-00-01. 2 L 7 2 4F RT A16WE 2001092000132 20010920 00132 SO 2001 9 20 C2XA01TY116 1 20010918 A 2134 214C40183 SWITCH EMB 145 EMB145LR SO CABIN FAILED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13989 3417 3417 145271 TYS DURING A SCHEDULED INSPECTION, THE ALTITUDE SENSING SWITCH FOR PASSENGER OXYGEN FAILED OPS CHECK. MAINTENANCE REMO VED AND REPLACED THE ALTITUDE SENSING SWITCH IAW-EMB-145-AMM-35-20-03, OPERATIONAL CHECKED GOOD. THE REPAIR WAS SATISFA CTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2001092000133 20010920 00133 SO 2001 9 20 C2XA01TY117 1 20010918 A 3222 14521680003 CAP EMB 145 EMB145ER SO NLG GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13989 145271 TYS DURING A SCHEDULED INSPECTION, A GOUGE WAS FOUND ON THE BEARING CAP SURFACE OF THE LEFT HAND TOP BEARING CAP OF THE NOSE GEAR. MAINTENANCE REWORKED THE LEFT UPPER HALF TOP BEARING CAP SURFACE OF NOSE LANDING GEAR IAW-EMB-GST-3164/01. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THE INSPECTION. 2 L 7 2 4F RT T00011AT 2001092000134 20010920 00134 NM 2001 9 20 C8GA2001017 1 20010916 A 3411 PROBE BOEING 727 7272A1 138407F NM PITOT SYS CLOGGED A C8GA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 15 287SC 21345 FLT 287 FROM MCO TO MCO PART 91 TRAINING FLIGHT. ON TAKEOFF ROLL NO AIRSPEED INDICATION ON FIRST OFFICER'S INSTRUMENT. DISCONTINUED TAKEOFF AND RETURNED TO BLOCK WITHOUT INCIDENT. PERFORMED PITOT LEAK TEST AND FOUND FOD ON FIRST OFFICER PITOT PROBE. REMOVED FOD AND PERFORMED PITOT LEAK TEST IAW MM 34-11-00. SYSTEM OPS CHECKED GOOD AND AIRCRAFT RETURN TO SERVICE. 2 L 7 3 4F A3WE 2001092000135 20010920 00135 NM 2001 9 20 CALA0100884 1 20010918 A 5753 6546431279 FLAP BOEING 737 7373T0 1384582 NM WING GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND NR 1 FOREFLAP GOUGED ON O/B END. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-37. 2 L 7 2 4F RT A16WE 2001092000136 20010920 00136 2001 9 20 DHL2001365037 4 20010906 A 2230 COUPLING AIRBUS 300 A300B4203 3930306 EU AUTOTHROTTLE SYS FAULTY A DHLA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 01 365DH 149 AUTOTHROTTLE SYSTEM DISENGAGED CONTINUOUSLY DURING FLIGHT AND HAD TO BE RESET. DUE TO NO FAULT SHOWN FOR AUTOTHROTTLE PROBLEM. REMOVED AND REPLACED AFCS TEST CONTROL PANEL. PLACED AUTOTHROTTLE SYSTEM ON DMI 7014, MEL 22-31-01 CAT B. DE FERRED BY WKERTZ 9101. REMOVED AND REPLACED AFCS TEST CONTROL PANEL AS PER MM 22-42-21. OPS CHECKED GOOD. COMPLIED WI TH S/P 22-31-01. NORMAL OPS CONFIRMED. DMI 7014 REMAINS OPEN AND IN EFFECT. REMOVED AND REPLACED NR 2 ENGINE AUTOTHRO TTLE COUPLING UNIT IAW AMM 22-31-00, OPS CHECKS SERVICEABLE THIS CLEARS DMI 7014 PLACARD REMOVED. 2 L 7 2 4F RT A35EU 2001092000137 20010920 00137 EU 2001 9 20 DHL2001366027 1 20010909 A 4960 RELAY AIRBUS 300 A300B4203 3930306 EU APU FAILED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 366DH 249 APU AUTOMATIC FIRE SHUTDOWN SYSTEM WILL NOT TEST. REF DMI 7050. APU AUTO FIRE SHUTDOWN SYS WILL NOT TEST. TRANSFERRED TO DMI 7050 IAW MEL 26-13-02, CAT C. MXC NOTIFIED. PLACARD INSTALLED. WILL COMPLY SP 26-13-02. ON T/S FOUND 32WF RE LAY (APU S/D CONT) AT FAULT. REMOVED AND REPLACED APU S/D CONT. 2 L 7 2 4F RT A35EU 2001092000138 20010920 00138 NM 2001 9 20 DHL2001707011 1 20010901 A 5312 BULKHEAD BOEING 727 72722 1384002 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 ON DROP IN CHECK, FWD CARGO COMPT, WING CENTER SECTION FWD BULKHEAD WEB CRACKED (APPROX 1 INCH) RBL 29 APPROX 14 INCHES ABOVE PRESS SPAL BETWEEN VERTICAL ROW OF FASTENERS. STOP DRILLED CRACK 2 PLACES IN FWD CARGO COMPL, WING CENTER SECTION FWD BULKHEAD WEB AT RBL 29 APPROX 14 INCHES ABOVE PRESS SEAL BETWEEN VERTICAL FASTENER ROWS. INSTALLED INTERIM REPAIR DOUBLER AS PER S/B 727-57-0101. 2 L 7 3 4F A3WE 2001092000139 20010920 00139 NM 2001 9 20 DHL2001707012 1 20010915 A 3350 BATTERY BOEING 727 72722 1384002 NM CABIN DISCHARGED A DHLA K NONE L NO TEST NR NOT REPORTED 1 SO 01 707DH 18321 EMERGENCY EXIT LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERIES IN EMERGENCY EXIT LIGHTS IAW B-M/M 33-50-71. 2 L 7 3 4F A3WE 2001092000140 20010920 00140 NM 2001 9 20 DHL2001708012 1 20010830 A 3241 CONTROL VALVE BOEING 727 72725 1384006 NM ANTI SKID SYS FAILED A DHLA D RETURN TO BLOCK A FLAME/FIRE TX TAXI/GRND HDL 1 SO 01 708DH 18275 LT MAIN GEAR BRAKE DRAGGING ON TAXI OUT. TAXI BACK TO GATE PER PHONE PATCH. MX FLT CONT CVG LT MAIN BRAKE FIRE THERMAL DISCHARGED TIRE 1 TIRE 2 FIRE LAST OVER 45 MIN, FIRE REFLARED UP 3 TIMES IN 45 MIN. CHECKED/INSP SERVICE OF LT MAIN SH OCK STRUT / STRUT IS NOT FLAT, NO 5606 FLUID LEAKAGE IAW MM 12-15-21. LEAK IS AT LT NR 1 BRAKE SHUTTLE VALVE. INSPECT ED LT MAIN STRUT FOR FIRE DAMAGE IAW MM 5-51-121. LEFT MAIN STRUT FLAT HYD FLUID LEAKING. FIRE DAMAGE TO STRUT. REMOV ED AND REPLACED LT ANTI-SKID CONTROL VALVE IAW MM 32-42-21 / VALVE LEAK CHECK GOOD. REMOVED AND REPLACED NR 1 & 2 MAIN WHEEL/TIRE ASSY IAW MM 32-45-1. 2 L 7 3 4F A3WE 2001092000141 20010920 00141 NM 2001 9 20 DHL2001709012 1 20010911 A 3260 SWITCH BOEING 727 72782C 1384026 NM NLG MALFUNCTIONED A DHLA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 709DH 19968 ON FINAL NOSE GEAR INDICATION WENT FROM DOWN AND LOCKED 3 GREEN TO UNSAFE. VISUALLY CONFIRMED GEAR DOWN AND LOCKED. ON FINAL GEAR WENT FROM UNSAFE TO DOWN AND LOCKED. INSTALLED NEW NOSE GEAR LOCK AND POSITION CONTROL SWITCH IAW B-MM 32-6 1-01, OPS CHECK GOOD. 2 L 7 3 4F A3WE 2001092000142 20010920 00142 NM 2001 9 20 DHL2001709013 1 20010915 A 2612 FIRE LOOP BOEING 727 72782C 1384026 NM FIRE DETECTION OUT OF POSITION A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 709DH 19968 NR 1 FIRE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED ON P6-3 GROUND FAULT. DEFERRED PER MEL 26-9 CAT-C CONTROL 7094. RE POSITIONED FIRE LOOP AND TESTED IAW 727 MM 26-11-0, OPS CHECK NORMAL AT THIS TIME. THIS CLEARS DMI 7094 PLACARD REMOVED . 2 L 7 3 4F A3WE 2001092000143 20010920 00143 NM 2001 9 20 DHL2001712011 1 20010904 A 3350 BATTERY BOEING 727 72729 1384007 NM CABIN DISCHARGED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 712DH 19401 DURING STANDBY POWER CHECK EMERGENCY EXIT LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS BATTER IES PER B727 MM 24-54-0. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2001092000144 20010920 00144 NM 2001 9 20 DHL2001712012 1 20010905 A 5755 SPOILER BOEING 727 72729 1384007 NM WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 NR 4 J-SCREW GEARBOX REQ CLEAN AND LEAK CK NR 10 SPOILER CRACK AT ACTUATION ROD ATTACH POINT. THRU BOLT EXCESSIVELY LOO SE 4" 6" DELAMINATION LOCATED UPPER SURFACE NR 4 SPOILER OUTBD FWD EDGE NR 2 SPOILER ACT HAS HYD FLUID ON BOTTOM NR 6 SP OILER CENTER HINGE PIN HAS ROTATED AND SHEARED OFF LOCK CLIP. CLEANED AND SERVICED AS REQUIRED IAW MM 27-51-22 31217 SY STEM LEAK CHECKED GOOD. REPLACED NR 4 SPOILER PANEL IAW B727 MM 27-61-1. TO BE OPS CHECKED 33794 09/05/2001. SYSTEM OP S CHECKS GOOD, FOUND LEAK AT LOWER B-NUT TO ACTUATOR FITTING. INSTALLED NEW O-RING LEAK AND OPS CHECK DUE 3524 9/05/200 1 SYSTEM LEAK CHECKED GOOD. 2 L 7 3 4F A3WE 2001092000145 20010920 00145 NM 2001 9 20 DHL2001712013 1 20010912 A 2612 FIRE LOOP BOEING 727 72729 1384007 NM NR 3 ENGINE OUT OF POSITION A DHLA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 712DH 19401 NR 3 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED NR 1 ENG REQ OIL SVS. TRANSFERRED TO DMI 7080 MEL REF 26-7 CAT-C PLACARD INSTALLED SERVICED NR 1 ENG OIL IAW B727 MM 12-13-01. INSPECTED AND REPOSITIONED NR 3 ENG FIRE LOOP AND TESTED IAW 727 MM 26-11GROUND CHECKS NORMAL AT THIS TIME. 2 L 7 3 4F A3WE 2001092000146 20010920 00146 NM 2001 9 20 DHL2001712014 1 20010915 A 2612 FIRE LOOP BOEING 727 72729 1384007 NM NR 3 ENGINE OUT OF POSITION A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 712DH 19401 NR 3 ENGINE FIRE DETECTOR CIRCUIT ARMED LIGHT ILLUMINATED FROM INITIAL CLIMB TO TOP OF DESCENT. OPEN COWLING FOUND FIRE LOOP DETECTOR LINE RUBBING COWLING. RE-ROUTED IAW B727 MM 26-11-000. 2 L 7 3 4F A3WE 2001092000147 20010920 00147 NM 2001 9 20 DHL2001717021 1 20010905 A 2612 FIRE DETECTOR BOEING 727 72723 1384004 NM NR 2 ENGINE MALFUNCTIONED A DHLA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 717DH 19389 NR 2 ENGINE FIRE WARNING GROUND FAULT DETECTOR SYSTEM LIGHT ILLUMINATED DURING TAXI THEN SELF EXTINGUISHED AFTER TAKEOFF DEFERRED PER MEL 26-9-1 LM. REMOVED AND REPLACED NR 2 ENG FIRE DETECTOR, OPS CK NORMAL IAW M/M 26-11-001. 2 L 7 3 4F A3WE 2001092000148 20010920 00148 2001 9 20 DHL2001721006 4 20010829 A 3418 STALL WARNING BOEING 727 727228 NM COCKPIT MALFUNCTIONED A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 721DH 19545 OVERSPEED WARNING SOUNDED ON CLIMBOUT APPROX 10 KTS BEFORE BARBER POLE AND STICK SHAKER SOUNDED ON DESCENT AT 210 KTS CL EAN CONFIGURATION. PERF ADJ/ TEST STALL WARNING SYS PER MM 34-18-01. OPS CKS NORMAL. PLACED BOTH MACH METERS (CAPT & F/O ) TO MODE B. PERF PITOT STATIC CK. OPS CHECKS NORMAL. 2 L 7 3 4F A3WE 2001092000149 20010920 00149 NM 2001 9 20 DHL2001721007 1 20010908 A 2612 POWER UNIT BOEING 727 7272Q9 138448M NM APU FAULTY A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 721DH 21931 DURING APU FIRE TEST FIRE BOTTLE C/B POPS APPROX 35 SEC AND FIRE TEST IS INOP. TRIED NEW SENSOR DET, NO HELP. REPLACED O/H DET POWER UNIT, SYS OPS CHECK NORMAL IAW MM 26-15-0. 2 L 7 3 4F RT A3WE 2001092000150 20010920 00150 NM 2001 9 20 DHL2001727500 1 20010816 A 5280 BUSHING BOEING 727 727200 138407E NM RT MLG DOOR WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C-CK; RT MAIN LANDING GEAR STRUT DOOR HAS EXCESS PLAY. REMOVED AND REPLACED BUSHINGS ON FWD HINGE HANGER ON FLAP TRA CK PER B727 M/M 20-10-7. REMOVED AND REPLACED GIMBAL, BOLT, NUT & BUSHINGS ON STRUT DOOR B727 M/M 32-10-1, OPS CK PER B 727 M/M 32-11-0. 2 L 7 3 4F RT A3WE 2001092100001 20010921 00001 SO 2001 9 21 C2XA01IA362 1 20010911 A 3350 AD3127 BATTERY PACK EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 22727 120177 IAH - DURING MAINTENANCE INSPECTION, THE FORWARD SET OF EMERGENCY AISLE PATH LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTE NANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC E. 2 L 7 2 4T RT A31SO 2001092100009 20010921 00009 GL 2001 9 21 CA010822021 2 20010817 A 7320 FUEL CONTROL CVAC 580 580 2422806 WP ALLSN 501D 501D13D 03004 GL ALLSN A6441 A6441FN606 GL NR 1 ENGINE MALFUNCTIONED W E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION DE DESCENT 1 CA (CAN) LOW ENGINE FUEL BOOST PRESS LITE NR 1 ILLUMINATED IN FLIGHT.ALL ENGINE PARAMETERS NORMAL WITH CRUISE POWER SET. P OWER WAS REDUCED FOR ANTICIPATION OF ROUGH AIR ON DESCENT.WHEN POWER WAS CALLED FOR AGAIN NONE WAS AVAILABLE. ENGINE SH UT DOWN FOR REST OF DESCENT AND LANDING.ATC WAS NOTIFIED OF PRECAUTIONARY SHUTDOWN. MAINTENANCE T/S AIRCRAFT AND REPLAC ED THE NR 1 FCU. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT E282 6 C P898 2001092100010 20010921 00010 WP 2001 9 21 CA010823002 1 20010819 A 2150 7339347 ACM LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE NR 2 CONTAMINATED W H D DEACTIVATE SYST/CIRCUITS RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA 28063 28063 (CAN) DURING TAXI NR 2 AIR CONDITIONING SYSTEM BECAME NOISY. LOUD GRINDING NOISE WAS NOTICED IN THE FLIGHT DECK. SMOKE A ND ODOUR WERE NOTICED IN THE CABIN. NR 2 PACK WAS TURN OFF. SMOKE AND ODOUR WAS STILL COMING INTO THE CABIN. CREW PROCEE D WITH AN EMERGENCY EVACUATION. AIRCRAFT WAS DEPLANNED THRU ALL 8 SLIDES. INVESTIGATION HAS CONFIRMED NR 2 AIR CYCLE MAC HINE FAILURE. OIL SYSTEM WAS CONTAMINATED WITH METAL OIL SEEPING INTO COMPRESSOR HAD CAUSED THE FUMES AND ODOURS IN THE CABIN. THE ACM ASSEMBLY WAS REPLACED WITH THE COMPRESSOR DISCHARGE OVER TEMP SWITCH CAUSING THE PACK. FLOW CONTROL VALVE CIRCUIT BREAKER TO TRIP. 2 L 7 3 4F 4 F A23WE E12EU 2001092100012 20010921 00012 EU 2001 9 21 CA010823005 1 20010822 A 3244 TIRE AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NLG DEFLATED W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA (CAN) L/H NOSE WHEEL ASSEMBLY DEFLATED DURING TAXI TO GATE. MECHANICS ON SITE NOTED, OVER PRESSURE VALVE WAS LOOSE WHICH CONTRIBUTED TO THE LOSS OF PRESSURE IN THE TIRE. L/H AND R/H NOSE WHEEL ASSEMBLIES WERE CHANGED. 2 L 7 2 4F 4 F RT A28NM E311NE 2001092100013 20010921 00013 EU 2001 9 21 CA010823006 1 20010822 A 3411 INDICATOR AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE PITOT/STATIC SYS CONTAMINATED W C ABORTED TAKEOFF H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 CA (CAN) AIRCRAFT ABORTED TAKEOFF FOR NO AIRSPEED INDICATION ON CAPTAIN'S SIDE. DEBRIS FOUND IN CAPTAIN'S PITOT TUBE. D EBRIS REMOVED AND PITPT CHECK AND AIR DATA COMPUTER CHECK CARRIED OUT. NO FAULTS FOUND AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A35EU E23EA 2001092100014 20010921 00014 WP 2001 9 21 CA010823007 1 20010819 A 2160 7244251 SWITCH LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE ACM OVERTEMP SHORTED W H D DEACTIVATE SYST/CIRCUITS RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN) DURING TAXI, NR 2 AIR CONDITIONING SYSTEM BECAME NOISY AND PRODUCING SMOKE AND ODOUR IN THE CABIN. NR 2 PACK WAS S HUT DOWN. EMERGENCY EVACUATION WAS EXECUTED DUE TO SMOKE AND ODOUR STILL COMING FROM NR 2 PACK AFTER SHUT DOWN. DURING I NVESTIGATION FOUND THAT NR 2 PACK CONTROL VALVE CIRCUIT BREAKER HAD TRIPPED. DURING TROUBLE SHOOTING, IT WAS CONFIRMED T HAT THE ACM OVERTEMP SWITCH WAS SHORTED AND CAUSING C/B TO TRIP FOR NR 2 PACK VALVE. OVERTEMP SWITCH WAS REPLACED AND SY STEM TESTED SERVICEABLE AS PER MAINTENANCE MANUAL. 2 L 7 3 4F 4 F A23WE E12EU 2001092100015 20010921 00015 EU 2001 9 21 CA010823008 1 20010810 A 2810 FUEL CELL AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE RT WING LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 33869 (CAN) DURING THE PREFLIGHT INSPECTION, A HEAVY FUEL LEAK WAS NOTICED ON THE RT LOWER WING SURFACE OUTBOARD OF THE PYLON. THE FUEL WAS LEAKING ON TO THE TAIL CONE OF THE EXHAUST AREA OF NR 2 ENGINE. THE NR 2 FUEL TANK WAS DEFUELED AND A NE GATIVE PRESSURE CHECK IDENTIFIED 4 LEAKS BETWEEN SEALANT AND THE WING INTERNAL STRUCTURE. THE AREAS WERE CLEANED UP AND RESEALED. ANOTHER LEAK WAS FOUND ON THE SKIN SEAM AREA WHICH WAS ALSO RESEALED. THE TANK WAS REFUELED AND A LEAK CHECK CONFIRMED THE AREA HAD BEEN FIXED. 2 L 7 2 4F 4 F RT A35EU E23EA 2001092100020 20010921 00020 NM 2001 9 21 CA010910008 1 20010809 A 2436 A41905533505 RELAY BOEING 737 7372T7 1384482 NM PWA JT8 JT8D17A 52049 NE BATTERY CHARGER FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING SRVICE CHECK, WITH NO A/C POWER & BATTERY SELECTED TO DC, THE AMP METER WENT TO 40 AMPS, AFTER APU START , THE D.C. AMPS METER STOCKED AT 100 AMPS. FOUND HIGH RESISTANCE BETWEEN TERMINAL B2 AND A2 OF R1 BATTERY BUS RELAY, W HEN RESISTANCE SHOULD HAVE BEEN INFINITE. REPLACED RELAY ALSO AS A RECAUTIONARY MEASURE, THE BATTERY AND BATTERY CHARGER WERE REPLACED. SYSTEM FUNCTIONALLY TESTED AND FOUND SERVICEABLE. 2 L 7 2 4F 4 F RT A16WE E2EA 2001092100022 20010921 00022 2001 9 21 CA010828008 4 20010823 A 3418 861CA40001 SENSOR AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE AOA FAILED W H DEACTIVATE SYST/CIRCUITS N FALSE WARNING AP APPROACH 1 CA (CAN) ON 3 OCCASIONS AUGUST 24, 2000, SEPT 13 2000, AND SEPT 20 2000 "ALPHA FLOOR" (MAX AUTO THROTTLE) WAS ENGAGED ON AP PROACH AND DEPARTURE. PROBLEM WAS INTERMITTANT AND TROUBLESHOOTING LEAD TO AOA SENSOR. SENSOR REPLACED, PROBLEM CLEARED. 2 L 7 2 4F 4 F RT A35EU E23EA 2001092100023 20010921 00023 EU 2001 9 21 CA010828016 1 20010827 A 2530 3510004409 COFFEEMAKER AIRBUS 320 A320212 3930322 EU CFMINT CFM56 CFM565A3 NE AFT GALLERY OVERHEATED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) FLIGHT ATTENDANT REPORTED SMOKE IN REAR GALLEY. AIRCRAFT WAS DIVERTED, UPON INSPECTION, A SHORT CIRCUIT WAS DET ECTED ON THE COFFEE HEATER SYSTEM. COFFEEMAKER WAS DISCONNECTED AND REMOVED. 2 L 7 2 4F 4 F RT A28NM E29NE 2001092100024 20010921 00024 WP 2001 9 21 0103289945 1 20010329 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE WRINKLED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8925E 45840 DURING AN H-CHECK AT ATLANTA, WAVINESS AND SKIN MISMATCH WERE FOUND IN THE AREA OF THE ALTERNATE STATIC PORT. IN ORDER TO CORRECT THE DISCREPANCY, THE FUSELAGE SKIN WAS TRIMMED OUT. HOWEVER, THE FLUSH SKIN REPAIR PER THE DC-9 SRM, CHAPTER 53-04, FIGURE 12C COULD NOT BE ACCOMPLISHED DUE TO THE CLOSE PROXIMITY WITH OTHER REPAIRS. THE SUBJECT SKIN PANEL HAD BEEN PREVIOUSLY REPLACED. THE EA 99-181020 LOG PAGE 1583873 PROVIDES AUTHORIZATION TO ACCOMPLISH AN ALTERNATE FLUSH SKI N REPAIR. HOWEVER, DUE TO THE IMPENDING REPAIR ASSESSMENT PROGRAM, IT WAS DECIDED TO CONSIDER THIS REPAIR A INTERIM. 2 L 7 2 4F A6WE 2001092100027 20010921 00027 EU 2001 9 21 CA010828022 1 20010825 A 2610 D826 FIRE LOOP BRAERO 748 HS7482A 4231001 EU RROYCE DART DART5342 EU ROTOL R4304 R2124304 EU NR 1 ENGINE WORN W F E A ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CA (CAN) WHILE IN CRUISE THE CREW OBSERVRD A FIRE INDICATION ON NR 1 ENGINE. FIRE DRILL WAS PRFORMED AND BOTH BOTTLES DISCH ARGED. THE INDICATION REMAINED ON, THE F/A CONFIRMED NO VISIBLE INDICATION OF FIRE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO BASE, LANDING WITHOUT INCIDENT. MAINTENANCE DETERMINED A COUPLING IN THE FIRE WIRE WAS AT FAULT. BOTH FIRE BOTTLES AND FIRE WIRE WERE REPLACED AND SYSTEM CHECKED SERVICEABLE. 2 L 7 2 3T 4 T A24EU A196 6 C P899 2001092100029 20010921 00029 NM 2001 9 21 01FDEA00845 1 20010918 A 2780 SLAT BOEING 727 72725C 138400H NM WING FAILED A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 135FE 19853 UPON FLAP RETRACTION NR 6 SLAT FAILED TO RETRACT. 2 L 7 3 4F A3WE 2001092100030 20010921 00030 EU 2001 9 21 01FDEA00846 1 20010918 A 2611 SMOKE WARNING AIRBUS 300 A300F4605R 3930327 EU COCKPIT ILLUMINATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 665FE 769 CARGO SMOKE WARNING CAME ON. RELEASE PER MEL, NO CARGO TO BE CARRIED IN MAIN DECK. 2 L 7 2 4F RT A35EU 2001092100031 20010921 00031 NM 2001 9 21 01FDEA00847 1 20010919 A 3610 MANIFOLD DOUG MD11 MD11F 3023600 NM PNEUMATIC SYS FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 602FE 48402 AIR MANF NR 2 FAIL ALERT NR 2 PACK OFF. REMOVED AND REPLACED MFC & RTS PER MM 36-23-01-4. CLOSED NR 2 COWLING & PLATFO RM PER 71-00-00. 2 L 7 3 4F RT A22WE 2001092100032 20010921 00032 GL 2001 9 21 01FDEA00849 2 20010919 A 7200 ENGINE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 1 MALFUNCTIONED A FDEA E ENGINE SHUTDOWN O OTHER DE DESCENT 1 SO 25 373FE 46611 451228 NR 1 ENGINE FAILED AFT THROTTLES REDUCTION. SHUT DOWN. REMOVED AND REPLACED CIT SENSOR AND PERF BORESCOPE PER STALL RE Q. RAN ENG OK FOR SERVICE. 2 L 7 3 4F 4 F A22WE E23EA 2001092100036 20010921 00036 WP 2001 9 21 ABXA010491 1 20010904 A 5220 5912995503 DOOR FRAME DOUG DC9 DC932 3022066 WP EMERGENCY EXIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 THE LEFT AFT EMERGENCY EXIT DOOR INNER JAMB WAS CRACKED ON UPPER INTERIOR AFT CORNER ADJACENT TO HANDLE. MAINTENANCE RE PAIRED THE AREA IAW DC-9 SRM 52-05. 2 L 7 2 4F A6WE 2001092100037 20010921 00037 WP 2001 9 21 ABXA010493 1 20010904 A 5320 49127722 SPLICE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 SPLICE FITTING AT FUSELAGE STATION 229, L18R WAS FOUND TO BE CRACKED. MAINTENANCE REPLACED THE FITTING IAW DC-9 SRM 51- 30-1. 2 L 7 2 4F A6WE 2001092100038 20010921 00038 WP 2001 9 21 ANCF200100014 1 20010918 A 2150 39613011 FLOW VALVE DOUG DC9 DC983 3022083 WP A/C BAY FAILED B ANCF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 632CT 16760 1540 49632 AFTER TAKEOFF WITH LT PACK INOPERATIVE, THE FLOW LIGHT CAME ON. CHECK LIST WAS PERFORMED UNSUCCESSFULLY, OUT FLOW VALVE WAS FULLY CLOSE ALL THE TIME. CABIN AUTOMATIC PRESSURE CONTROLLER DEFERRED TO CARRY OVER 090 MEL 21-24 CAT-C. FLOW CO NTROL VALVE WAS CHANGED IAW AMM 21-31-02 PAGES 202 & 207. TEST OK. 2 L 7 2 4F RT A6WE 2001092100039 20010921 00039 WP 2001 9 21 AT0100227 1 20010913 A 3350 60030451 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 801AT 47275 FOUND EMERGENCY LIGHTS AT FORWARD GALLEY AND FORWARD ENTRY INOPERATIVE. REMOVED AND REPLACED B5-23 EMERGENCY LIGHT POWE R SUPPLY IAW DC9 MM 33-53-0. 2 L 7 2 4F A6WE 2001092100040 20010921 00040 WP 2001 9 21 AT0100228 1 20010914 A 3350 6011779 BATTERY PACK DOUG DC9 DC932 3022066 WP CARGO BAY DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 801AT 47275 FOUND STARBOARD NACELLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE STARBOARD NACELLE EMERGENCY LIGHT BATTERY PACK IAW DC9 MM 33-50. 2 L 7 2 4F A6WE 2001092100041 20010921 00041 SO 2001 9 21 C2XA01CL205 1 20010919 A 3350 78812 LIGHT EMB 145 EMB145LR SO CABIN INOPERATIVE A C2XA K NONE L NO TEST NR NOT REPORTED 1 SW 27 16918 145397 CLE FLIGHT 3675 THE CREW REPORTED THE FORWARD EMERGENCY AISLE PATH LIGHTING STRIP WAS INOPERATIVE. MAINTENANCE REPLACED THE FORWARD EMERGENCY AISLE PATH LIGHTING STRIP. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2001092100042 20010921 00042 EU 2001 9 21 WRNA200100016 1 20010918 A 2100 3809441 APU AIRBUS A300B4 AIRBUS 300 A300B4203 3930306 EU TAIL ACTIVE A WRNA A D UNSCHED LANDING RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 05 502TA 59426 1392 075 075 Just after takeoff, strong odor of wood smoke was smelled in the cockpit. Aircraft returned to station. landing was norm al.Corrective Action: Investigation found wood smell to be residue of accomplished APU rice hull wash C/W I/A/W MM 49-00 -00. Aircraft returned to service and cleared for departure. 2 L 7 2 4F RT A35EU 2001092100043 20010921 00043 WP 2001 9 21 CALA0100886 1 20010919 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35836 49441 INSPECTION FOUND AFT BAGGAGE BIN LOWER DOOR JAMB CORRODED BETWEEN STA 1155-1211. A Z-ANGLE BEAM REPAIR WAS INSTALLED IA W SRM 53-05, FIGURE 63. 2 L 7 2 4F A6WE 2001092100044 20010921 00044 WP 2001 9 21 CALA0100887 1 20010919 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35836 49441 INSPECTION FOUND MID BAGGAGE BIN LOWER DOOR JAMB CORRODED AROUND H-SHEAR AT STA 636-693. A REPAIR DOUBLER AND SPACER WE RE INSTALLED IAW SRM 53-05, FIGURE 63. 2 L 7 2 4F A6WE 2001092100045 20010921 00045 NM 2001 9 21 CALA0100889 1 20010919 A 5230 STOP FITTING BOEING 737 7373T0 1384582 NM CARGO DOOR WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND AFT CARGO DOOR FORWARD LOWER, FORWARD SECOND FROM BOTTOM, AND AFT UPPER STOP FITTINGS WORN. NEW STOP F ITTINGS WERE INSTALLED IAW SRM 51-10-02, 51-10-01, AND 51-40-00. 2 L 7 2 4F RT A16WE 2001092100046 20010921 00046 EU 2001 9 21 CA010829012 1 20010816 A 8200 SERVO A702AC BRAERO 748 HS7482A 4231001 EU RROYCE DART DART5342 EU ROTOL R4304 R2124304 EU WATER METH PUMP SEIZED W C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CA MU7373 (CAN) DURING TAKEOFF THE CREW OBSERVED THAT NR 1 ENGINE WAS NOT DEVELOPING "WET" POWER. THE TAKEOFF WAS REJECTED AND TH E AIRCRAFT RETURNED TO THE GATE. MAINTENANCE FOUND THE SHUTOFF VALVE UNSERVICEABLE. THE MOTOR WAS REPLACED AND THE SYS TEM CHECKED SERVICEABLE. 2 L 7 2 3T 4 T A24EU A196 6 C P899 2001092100050 20010921 00050 NM 2001 9 21 DHL2001707013 1 20010919 A 3260 SWITCH BOEING 727 72722 1384002 NM NLG INOPERATIVE A DHLA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 SO 01 707DH 18321 NOSE GEAR UNSAFE LIGHT DOES NOT ILLUMINATE DURING GEAR RETRACTION OR EXTENSION, LIGHT TEST OK. REMOVED NLG POSITION SWI TCH AND LINKAGE PER M/M 32-61-71. INSTALLED NLG POSITION SWITCH IAW B727 MM 32-61-71. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2001092100051 20010921 00051 NM 2001 9 21 DHL2001727501 1 20010828 A 5320 STRAP BOEING 727 727200 138407E NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C-CK; AFT CARGO FLOOR SUPPORT STRAP AT BS 991 LT TO RT HAS NUMEROUS ELONGATED HOLES AND DENTED. REMOVED OLD STRAP, C LEANED,TREATED AND PRIMED AREA IAW B727 SRM 51-10-2, FABRICATED AND INSTALLED NEW STRAP IAW B727 SRM 51-30-2 PG 1. 2 L 7 3 4F RT A3WE 2001092100052 20010921 00052 NM 2001 9 21 DHL2001727502 1 20010819 A 2710 CONTROL CABLE BOEING 727 727228 NM AILERON DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 INBOARD AILERON LWR CABLE HAS LOST IDENTITY AT W/S 290 APPROX AS VIEWED THRU ACCESS 8505, AT INBOARD SIDE OF FAIR LEAD J UST FWD OF MLG BEAM. FABRICATED AND INSTALLED I/B AILERON LWR CABLE AT WS 290 JUST FWD OF MLG BEAM PER M/M 27-10-71. T ENSION AND RIGGED PER M/M 27-10-71. OPS CHECK NORMAL PER M/M 27-10-0. 2 L 7 3 4F A3WE 2001092100053 20010921 00053 NM 2001 9 21 DHL2001727503 1 20010816 A 2711 CONTROL ROD BOEING 727 727228 NM AILERON TAB WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 RT WING, I/B AILERON TAB HAS EXCESSIVE PLAY WITH POWER ON. REMOVED RT WING I/B AILERON TAB AFT CONTROL ROD FOR ACCESS P ER B 727-M/M 27-10-0. REMOVED AND REPLACED RT INBOARD CONTROL ROD, ROD END PER M/M 51-30-2. INSTALLED RT WING I/B CONT ROL ROD PER M/M 27-10-0. OPS CHECK OK PER M/M 27-10-0. 2 L 7 3 4F A3WE 2001092100054 20010921 00054 NM 2001 9 21 DHL2001727504 1 20010816 A 2710 BOLT BOEING 727 727228 NM AILERON WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH RT WING INBOARD AILERON HAS EXCESS PLAY WITH POWER ON. REMOVED AND REPLACED AILERON CONTROL ROD BOLTS AT RT WING I/B SI DE PER M/M 27-10-1. OPS CHECK OK PER M/M 27-10-0. 2 L 7 3 4F A3WE 2001092100056 20010921 00056 NM 2001 9 21 DHL2001727505 1 20010816 A 2710 ROD END BOEING 727 727228 NM AILERON WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH RT WING O/B AILERON HAS EXCESS PLAY WITH POWER ON. REMOVED AND REPLACED O/B ROD END AND BOLT PER M/M 27-10-01. OPS CK OK PER M/M 27-10-01. 2 L 7 3 4F A3WE 2001092100057 20010921 00057 NM 2001 9 21 DHL2001727506 1 20010816 A 2711 CONTROL ROD BOEING 727 727228 NM AILERON TAB WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH LEFT WING I/B AILERON TAB HAS EXCESS PLAY WITH POWER ON. REMOVED FWD CONTROL ROD PER M/M 27-10-0. REMOVED AND REPLACED ROD END PER SRM 51-30-2. REINSTALLED FWD CONTL ROD PER M/M 27-10-0. OPS CHECK GOOD PER M/M 27-10-01. 2 L 7 3 4F A3WE 2001092100058 20010921 00058 CE 2001 9 21 CA010831003 1 20010815 A 3213 1148100217 TORQUE LINK BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 12664 3969 (CAN) DURING BRAKE REMOVAL THE AME FOUND A CRACK ON THE TORQUE LINK LUG. AFTER INSPECTION WE FOUND BOTH SIDES CRACKED. THE PARTS WERE REPLACED. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2001092100060 20010921 00060 NM 2001 9 21 DHL2001727507 1 20010816 A 2710 ROD END BOEING 727 727228 NM AILERON WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH LT WING I/B AILERON HAS EXCESS PLAY WITH POWER ON. REMOVED LT WING I/B AILERON CONTROL ROD PER M/M 27-10-0. REMOVED AN D REPLACED ROD END PER SRM 51-30-2. REINSTALLED CONTROL ROD PER M/M 27-10-0. OPS CHECK OK PER M/M 27-10-01. 2 L 7 3 4F A3WE 2001092100061 20010921 00061 NM 2001 9 21 DHL2001727508 1 20010816 A 2710 ROD END BOEING 727 727228 NM AILERON WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH LT WING O/B AILERON HAS EXCESS PLAY WITH POWER ON. REMOVED AND REPLACED LEFT WING O/B CONTROL ROD END AND BOLT PER M/M 27-10-01. OPS CHECK OK PER M/M 27-10-01. 2 L 7 3 4F A3WE 2001092100063 20010921 00063 NM 2001 9 21 DHL2001727509 1 20010823 A 5720 652414677 RETAINER BOEING 727 727228 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH REAR SPAR PRESSURE SEAL RETAINER CRACKED AT STA 849L WL 208. REMOVED AND INSTALLED NEW SEAL RETAINER PER SRM 51-30-2. 2 L 7 3 4F A3WE 2001092100064 20010921 00064 NM 2001 9 21 DHL2001727510 1 20010823 A 5330 SKIN BOEING 727 727228 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH NR 1 LWR CARGO LWR SILL CUT OUT SHOWS CRACK, BS 610 26R CRACK GOES THRU ALL 3 LAYERS. NDT VERIFIED CRACK GOES THRU ALL 3 LAYERS FROM EDGE OF DOOR CUTOUT TO FIRST FASTENER PER NDT MAN PART 6 51-00-00 FIG 4. CLEANED OUT DAMAGED MATERIAL INS IDE THE GOUGE AND DOOR JAMB SURFACE PER HVHM 253B0-1. APPLIED ALODINE AND PRIMED AREA SRM 51-10-2. 2 L 7 3 4F A3WE 2001092100066 20010921 00066 NM 2001 9 21 DHL2001727511 1 20010817 A 5532 6517561183 SKIN PANEL BOEING 727 727228 NM VERTICAL STAB DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH REPLACE TEMP REPAIR LT VERT FIN BELOW RUDDER. REMOVED ACCESS PANEL BETWEEN FWD ENG MOUNT FOR SHEET METAL ACCESS PER SRM 51-30-2. REMOVED SKIN PANEL AT LT OF HORIZ STABILIZER PER SRM 51-30-2. SENT TO COMPOSITE SHOP FOR REPAIR. INSTALLED NEW SKIN PANEL PER SRM 51-30-2. INSTALLED ALL PARTS REMOVED FOR ACCESS PER SRM 51-30-2. 2 L 7 3 4F A3WE 2001092100067 20010921 00067 NM 2001 9 21 DHL2001727512 1 20010821 A 5347 BAC1520792 SEAT TRACK BOEING 727 727228 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH CABIN SEAT TRACK HEAVY CORRODED AT STA 360 TO 460 LBL 55. REMOVED CABIN SEAT TRACK STA 360 TO 460 LBL 55 PER SRM 51-30- 2. INSTALLED NEW SEAT TRACK PER SRM 51-30-2 AND 53-10-5 FIG 7. 2 L 7 3 4F A3WE 2001092100069 20010921 00069 NM 2001 9 21 DHL2001727513 1 20010828 A 5347 BAC1520792 SEAT TRACK BOEING 727 727228 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH CORROSION ON SEAT TRACK AT RBL 46 & STA 1020 TO 1030. REMOVED CABIN SEAT TRACK FROM STA 1020 TO 1070, CORROSION OUT OF LIMITS PER SRM 51-30-2 AND 53-10-5. INSTALLED NEW SEAT TRACK PER SRM 53-10-5 FIG 1. ALODINE AND PRIMED PER SRM 51-10-2 . 2 L 7 3 4F A3WE 2001092100070 20010921 00070 NM 2001 9 21 DHL2001727514 1 20010821 A 5320 WEB BOEING 727 727228 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH AFT AIR STAIRS RT SIDE BS 1203 LOWER WEB PREVIOUS REPAIR, WEB HAS CRACK, SEEMS INTERNAL AREA OIL CANNING. REMOVED FASTE NERS AND CUT OUT DAMAGED SECTION OF WEB BS 1203 RT SIDE 24 X 9.25 INCH PER SRM 51-30-2 AND 51-4-02. INSTALLED WEB REPAI R PER SRM 51-40-2 FIG 1. TREATED AND PRIMED PER SRM 51-10-2. 2 L 7 3 4F A3WE 2001092100071 20010921 00071 NM 2001 9 21 DHL2001727515 1 20010816 A 5321 FLOOR PANEL BOEING 727 727228 NM CABIN DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH MAIN CABIN BS 380 LBL 52 FLOOR PANEL PREVIOUS REPAIR METAL ROLLED BACK. REMOVED FLOOR PANELS PER SRM 51-30-2. FABRICAT ED NEW FLOOR PANEL PER SRM 53-20-1. ALODINED AND PRIMED AREA PER SRM 51-10-2. INSTALLED NEW FLOOR PANELS PER SRM 51-30 -2. 2 L 7 3 4F A3WE 2001092100072 20010921 00072 WP 2001 9 21 CA010831008 1 20010827 A 2820 67154101 INDICATOR LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE COCKPIT FAILED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA (CAN) THE AIRCRAFT RETURNED TO THE STATION AFTER 2 HOURS OF FLIGHT DUE TO FLIGHT CREW EXPERIENCED DIFFICULTY TO USE FUEL FROM TANK NR 2 RT. DURING INITIAL INVESTIGATION AN ACTUAL UNBALANCE WAS FOUND BETWEEN TANK NR 2R AND TANK NR 2 LT. ENGI NES GROUND RUN CONFIRMED THE ABLITY OF FUEL TO BE TRANSFERRED FROM TANK NR 2 RT. FUEL FLOW EQUALIZER WAS ISOLATED AS PER M.E.L. AT NEXT LAYOVER THE FUEL FLOW EQUALIZER WAS REPLACED WITH 3 FUEL QUANTITY PROBES. THE FUEL PUMP FILTERS WERE CLE ANED AND THE FUEL QUANTITY SYSTEM CALIBRATED. 2 L 7 3 4F 4 F A23WE E12EU 2001092100073 20010921 00073 SW 2001 9 21 CA010831009 1 20010827 A 2742 ACTUATOR DL5040M6 SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP PITCH TRIM SLIPPED W O OTHER F FLT CONT AFFECTED CR CRUISE 1 CA 5447 (CAN) DURING A TRAINING FLIGHT, THE PITCH TRIM FAILED TO MOVE WHEN SELECTED BY EITHER PILOTS OR CO-PILOTS CONTROL FOR A PPROXIMATELY 2 MINUTES DURING THE FLIGHT. ONCE PITCH TRIM CONTROL WAS RESTORED, THE AIRCRAFT LANDED WITHOUT INCIDENT. A SUBSEQUENT INSPECTION REVEALED THAT INITIALY THE HORIZONTAL STAB WOULD NOT MOVE WHEN SELECTED, BUT AFTER APPLYING FORCE TO THE STAB TO ASSIST IT, IT BEGAN TO FUNCTION. ONCE MOVING, VERY LITTLE FORCE APPLIED TO THE HORIZONZONTAL STAB WOULD CAUSE THE ACTUATOR TO SLIP, ON EITHER THE PILOTS OR CO-PILOTS SYSTEM. THE ACTUATOR WAS REPLACED AND THE AIRCRAFT RETURNE D TO SERVICE. 2 L 7 2 4T 4 T RT A8SW E4WE 2001092100081 20010921 00081 CE 2001 9 21 CA010905005 1 20010831 A 2435 23085001 STARTER GEN BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA ENGINE OVERHEATED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA 1112 (CAN) A/C DEPARTED AIRPORT, 5 MINUTES AFTER TAKEOFF THE LT GENERATOR ANNUNCIATOR ILLUMINATED & CREW REPORTED SMELLING A STRANGE BURNING ODOUR. THEY TURNED A ROUND RETURNED TO AIRPORT. AN UNEVENTFUL LANDING WAS MADE & A/C SENT TO HANGAR. THE FLOOR BOARDS WERE LIFTED & THE ODOUR INCREASED. THE LT GENERATOR CONTROL UNIT WAS FOUND TO BE THE CAUSE, IT WAS REPLACE D. THE LT START/GEN WAS ALSO FOUND TO BE OVERHEATED & REPLACED. THE CIRCUIT BREAKER FOR THE SYSTEM WAS FOUND POPPED BUT OBVIOUSLY TOO LATE. IT WAS RESET & THE SYSTEM TESTED WITH NO FURTHER FAULTS. 2 L 7 2 4T 4 T RT A24CE E4EA 2001092100084 20010921 00084 NM 2001 9 21 DHL2001727516 1 20010824 A 5347 SEAT TRACK BOEING 727 727228 NM FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH CABIN FLOOR SEAT TRACK BETWEEN BS 595 TO 600, RBL 25 HAS WORN AREAS MARKED. REMOVED FLOOR PANELS TO GAIN ACCESS TO SEAT TRACK. REMOVED DAMAGED SEAT TRACK SECTION PER SRM 51-30-2. INSTALLED NEW SEAT TRACK PER SRM 53-10-5 FIG 7. (P/N BAC 1520-729) 2 L 7 3 4F A3WE 2001092100086 20010921 00086 NM 2001 9 21 CA010906008 1 20010814 A 2530 6253190003 CONTROLLER BOEING 767 767375 1385217 NM GE CF6 CF680C2B6F 30025 NE OVEN FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) SMELL AND SMOKE COMING OUT NR 2 GALLEY OVEN. OVEN CONTROLLER REPLACED. OPERATION CHECKED FOR ONE HOUR. NO SIGN OF VERHEATING, CONSIDER SERVICEABLE. 2 L 7 2 4F 4 F RT A1NM E13NE 2001092100087 20010921 00087 EA 2001 9 21 COMA0160735 1 20010920 A 5320 DOOR FRAME CNDAIR CL600 CL6002B19 EA A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 796CA 7338 PREVIOUS REPAIR ON PAX DOOR SEAL STRIKER AT F.S. 349.00 UPPER CORNER DAMAGED.REPAIRED UPPER CORNER ON PAX DOOR STRIKER A T F.S. 349.00 I/A/W REE 601R-52-11-008 REPAIR (A) 2 L 7 2 4F RT A21EA 2001092100088 20010921 00088 EA 2001 9 21 COMA0160736 1 20010918 A 2760 SPOILER CNDAIR CL600 CL6002B19 EA A COMA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 01 929CA 7035 FLIGHT 6082. FLIGHT SPOILER AND OUTBOARD GROUND SPOILER FAULT MESSAGE DURING T/O. T/O ABORTEDRESET SYSTEM AND C/W OPERAT IONAL CHECKS. NO FAULTS FOUND. 2 L 7 2 4F RT A21EA 2001092100089 20010921 00089 NM 2001 9 21 DHL2001727517 1 20010821 A 5410 ANGLE BOEING 727 727228 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH NR 2 ENG LEFT TOP PANEL OF PYLON ANGLE SUPPORT IS CORRODED AND CRACK AT STA 1380. REMOVED CORRODED ANGLE AT TOP OF PYLO N NR 2 ENG LEFT SIDE BS 1381.5 TO 1455 PER SRM 51-30-2. FABRICATED NEW ANGLE PER SRM 54-10-2 FIG 3. INSTALLED ANGLE PER SRM 51-30-2. 2 L 7 3 4F A3WE 2001092100090 20010921 00090 NM 2001 9 21 DHL2001727518 1 20010819 A 2752 BELLCRANK BOEING 727 727228 NM T/E FLAP GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH INBOARD FLAP, O/B AFT FLAP ACTUATOR BELL CRANK, HAS SPRING GOUGING. CLEANED AND PAINTED RIGHT O/B FLAP AFT FLAP ACTUATO R DRUM PER M/M 12-10-00. REPLACED BOLT AND 2 SPACERS AND CONICAL WASHER AT AFT END OF FOLLOW UP DRUM. RESHIMMED FWD EN D OF FOLLOW UP DRUM PER M/M 27-51-0. OPS CHECK OK PER M/M 27-51-0. 2 L 7 3 4F A3WE 2001092100091 20010921 00091 NM 2001 9 21 DHL2001727519 1 20010819 A 7830 658822710 FAIRING BOEING 727 727228 NM THRUST REVERSER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH NR 3 ENGINE, THRUST REVERSER CASCADE VANE ASSY LOWER HALF FED FAIRING O/B END CRACKED. REMOVED PANEL FOR WELDER PER M/M 78-10-0. INSTALLED FAIRING PER M/M 78-10-0. 2 L 7 3 4F A3WE 2001092100092 20010921 00092 NM 2001 9 21 DHL2001727520 1 20010819 A 5753 6920303862 FITTING BOEING 727 727228 NM T/E FLAP WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH INBOARD FLAP O/B GIMBAL FITTING LOOSE BEARING, PLAY IN SHAFT. REMOVED AND REPLACED I/B FLAP O/B GIMBAL AND FABROID BUSH ING PER M/M 57-53-0. 2 L 7 3 4F A3WE 2001092100093 20010921 00093 NM 2001 9 21 DHL2001727521 1 20010815 A 5730 FAIRING BOEING 727 727228 NM LT WING LOOSE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH LEFT O/B FLAP O/B JACKSCREW FAIRING LOOSE. TIGHTENED FAIRING MOUNTING BOLTS PER M/M 57-30-2. 2 L 7 3 4F A3WE 2001092100094 20010921 00094 NM 2001 9 21 DHL2001727522 1 20010823 A 5530 65282235 BRACKET BOEING 727 727228 NM VERTICAL STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH VERTICAL STABILIZER TOP SIDE SUPPORT BRACKET FOR HORIZONTAL STAB POSITION INDICATOR IS CRACKED AT LT AND RT ATTACH POINT . REMOVED SUPPORT BRACKET PER SRM 51-30-2. INSTALLED NEW SUPPORT BRACKET PER SRM 51-30-2. 2 L 7 3 4F A3WE 2001092100095 20010921 00095 NM 2001 9 21 DHL2001727523 1 20010824 A 5347 SEAT TRACK BOEING 727 727228 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C-CHECK, CABIN SEAT TRACK BETWEEN BS 756 TO 765, LBL 46 HAS WORN AREAS. REMOVED CORROSION, FOUND OUT OF LIMITS AS PE R SRM 51-10-61, 53-10-1. REMOVED AND REPLACED THE CABIN SEAT TRACK PER B-727 SRM 51-10-1 PARA 4 AND 51-30-2. 2 L 7 3 4F A3WE 2001092100096 20010921 00096 NM 2001 9 21 DHL2001727524 1 20010623 A 5321 FLOOR PANEL BOEING 727 727228 NM CABIN DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH CABIN FLOOR PANEL BETWEEN STA 380 TO 440, LBL 24 TO 42 HAS DELAMINATION. REMOVED FLOOR PANEL PER SRM 51-30-2. FABRICAT ED NEW FLOOR PANEL AS PER SRM 53-20-1. TREATED AND PRIMED PER SRM 51-10-2. INSTALLED NEW FLOOR PANEL PER SRM 51-30-2. 2 L 7 3 4F A3WE 2001092100097 20010921 00097 NM 2001 9 21 CA010906010 1 20010814 A 2530 1435 OVEN BOEING 737 737217 1384464 NM PWA JT8 JT8D17A 52049 NE GALLEY FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) FORWARD GALLEY OVEN BURNING SMELL. OVEN REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 2001092100098 20010921 00098 NM 2001 9 21 DHL2001727525 1 20010820 A 5730 PLENUM BOEING 727 727228 NM RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH CENTER WING RT UPPER WALL OF RAM AIR PLENUM CHAMBER HAS SPOTS OF CORROSION APPROX BS 800. REMOVED CORROSION PER SRM 51- 10-6. (MATERIAL LOSS 0.055 FOUND TO BE OUT OF LIMITS PER SRM 57-30-1 FIG 4. FLAP PEENED AREAS OF BLEND OUT PER SOP M-2 0-10-03. ACCOMP SHOT PEEN PER SRM 57-30-03. INSTALLED EXTERNAL REPAIR AT LOWER SKIN OF PLENUM PER SRM 57-30-03 FIG 8. 2 L 7 3 4F A3WE 2001092100099 20010921 00099 WP 2001 9 21 CA010906013 1 20010810 A 2131 21011403 CONTROLLER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE CABIN PRESSURE FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) SHORTLY AFTER TAKEOFF THE FLIGHT CREW LOST CONTROL OF THE CABIN PRESSURE. THE CREW WAS UNABLE TO CONTROL THE CABIN IN MANUAL MODE. AIRCRAFT RETURNED TO MONTREAL. ERS CALLED OUT DUE TO OVERWEIGHT LANDING. BOTH CABIN PRESSURE CONTROLLER S REPLACED. PRESSURIZATION CONTROL SYSTEM CERTIFICATION CARRIED OUT. AIRCRAFT SERVICEABLE. 2 L 7 2 4F 4 F A6WE E2EA 2001092100101 20010921 00101 NM 2001 9 21 DHL2001727526 1 20010623 A 5347 SEAT TRACK BOEING 727 727228 NM FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH CABIN FLOOR SEAT TRACK HAS WORN AREAS BETWEEN BS 504 TO 51B LBL 46. REMOVED SEAT TRACK AT CABIN FLOOR BETWEEN BS 480-56 0 LBL 46 PER SRM 51-30-2. FABRICATED NEW SEAT TRACK PER SRM 53-10-5. INSTALLED NEW SEAT TRACK PER SRM 53-10-5 FIG 7. 2 L 7 3 4F A3WE 2001092100102 20010921 00102 WP 2001 9 21 CA010906016 1 20010801 A 2131 70210 CONTROLLER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE CABIN PRESSURE FAILED W O OTHER J WARNING INDICATION CR CRUISE 1 CA (CAN) AT FL 330 "CABIN PRESURE" WARNING LIGHT ILLUMINATED. CABIN UNCONTROLLABLE, RAPID CABIN DESCENT CARRIED OUT. CABIN LIGHT WENT OUT THROUGH FL 200 BUT CABIN ALT SHOWING FL 300. ALSO, BOTH LAVATORIES DETECTORS CAME ON WITH NO VISIBLE SMOK E. CABIN RESSURE CONTROLLER REPLACED AND SYSTEM CHECKED SERVICEABLE AS PER MM 21-32-00. BATTERIES REPLACED IN BOTH LAVAT ORY SMOKE DETECTORS. 2 L 7 2 4F 4 F A6WE E2EA 2001092100106 20010921 00106 NM 2001 9 21 DHL2001727527 1 20010827 A 5315 FLOORBEAM BOEING 727 727228 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH MAIN CABIN FLOORBEAM AT STA 961 RBL 46 TO 50 HAS CORROSION. REMOVED CORROSION TO EVALUATE AREA PER SRM 51-30-2 AND 51-1 0-2. CORROSION OUT OF LIMITS PER SRM 53-10-1. FABRICATED NEW WEB FOR MAIN CABIN FLOORBEAM SUPPORT STA 761 RBL 46-50 PER SRM 53-10-2 FIG 7. BONDED MAIN CABIN FLOORBEAM AT STA 761 RBL 46 -50 PER SRM 57-40-6. INSTALLED FLOORBEAM AND WEB PER SRM 51-30-2. 2 L 7 3 4F A3WE 2001092100108 20010921 00108 NM 2001 9 21 DHL2001727528 1 20010820 A 5410 BRACKET BOEING 727 727228 NM NR 3 PYLON CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH CRACKED BRACKET AT NR 3 ENGINE PYLON AFT OF PRECOOLER SHROUD. REMOVED AND REPLACED BRACKET PER SRM 54-10-3. 2 L 7 3 4F A3WE 2001092100110 20010921 00110 NM 2001 9 21 DL72W011490 1 20010905 A 5300 651751737 ANGLE BOEING 727 727247 138408F NM STA 1263 R/H CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 296WA 22533 1 IN. CRACK GUSSET ANGLE AFT SIDE STA 1263 R/H TORQUE BOX REPAIRED PER M/M 53-11-000-8 2 L 7 3 4F A3WE 2001092100111 20010921 00111 NM 2001 9 21 DL73K011492 1 20010906 A 5330 SKIN BOEING 737 737232 1384475 NM SKIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 307DL 23079 THE FUSELAGE SKIN AND BEAR STRAP OF THE R2 DOOR WERE FOUND CRACKED AT THE LOWER HINGE CUTOUT. THE DAMAGE WAS REPAIRED PER SRM 53-30-3, FIG. 45 AT HMV. 2 L 7 2 4F RT A16WE 2001092100112 20010921 00112 NM 2001 9 21 DL733011494 1 20010905 A 5330 65458001140 SKIN BOEING 737 737347 1384647 NM FS 178, S-19R MISDRILLED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 311WA 23597 FUSELAGE / SKIN / FS 178 / STRG. 19R : REPAIR OF MISDRILLED HOLES SEVERAL MISSDRILLED HOLES WERE FOUND IN THE FUSELAGE SKIN AT FS 178 NEAR STRINGER 19R DURING ACCOMLISHMENT OF THE FS 178 BULKHEAD MODIFICATION. THE SECTION OF SKIN WITH THE BAD HOLES WAS TRIMMED OFF AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 381604-14, REV A. 2 L 7 2 4F RT A16WE 2001092100113 20010921 00113 NM 2001 9 21 DL72W011495 1 20010906 A 5311 65175061 FRAME BOEING 727 727247 138408F NM FS 1303 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 296WA 22533 FUSELAGE / FRAME / FS 1303 / RH : CRACKED FLANGE REPAIR THE FS 1303 RH FRAME WAS FOUND WITH A CRACK IN THE INNER FLANGE OF THE FRAME AT A HYDRAULIC LINE CLAMP ATTACH LOCATION JUST ABOVE THE RH VENTRAL STAIRWELL TORQUE BOX STRUCTURE. THE CRACK WAS ROUTED OUT OF THE FLANGE AND REPAIRED WITH AN ALUMINUM EXTRUDED ANGLE PER ER/A 381707-14,REV A. 2 L 7 3 4F A3WE 2001092100114 20010921 00114 NM 2001 9 21 DL72S011499 1 20010906 A 5500 STRINGER BOEING 727 727225A 1384077 NM STR 6R STA 6.372 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 805EA 22436 VERT STAB STR 6R CRACKED @ STA 6.372 REPAIRED PER M/M 55-30-000-8 FIG 803 2 L 7 3 4F RT A3WE 2001092100115 20010921 00115 NM 2001 9 21 DL72S011500 1 20010906 A 5500 STRINGER BOEING 727 727225A 1384077 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 805EA 22436 VERT STAB STRINGER 6R CRACKED AT STA 6.372 REPAIRED PER MM 55-30-000-8 FIG 803 2 L 7 3 4F RT A3WE 2001092100116 20010921 00116 NM 2001 9 21 DL72S011501 1 20010827 A 3230 69181946 SUPPORT BOEING 727 727232 1384082 NM STA.351.5BULKHD CRACKED A DALA O OTHER K FLUID LOSS LD LANDING 1 SO 27 516DA 21432 ON FINAL WHEN LDG GEAR EXTENDED -A-SYS HYD FAILURE-COMPLETE-GEAR DOWN AND LOCKED FLAPS 30DGS-RAISED FLAP ELEC. TO 15DGS AND LANDED A/C- FOUND NOSEGEAR UPLCKACT.BRACKET CRACKED AND ACT.LINES DAMAGED-RPLCD BRACKET ACTUATOR LINES AND C/W ERA R EPAIR TO STA351.5 WEB. AND CORD-RPLCD WATER SEPERATOR BAGS EDPPOS.1/2AND FILTERS. 2 L 7 3 4F A3WE 2001092100117 20010921 00117 NM 2001 9 21 DL72S011506 1 20010908 A 3260 H1010153 SWITCH BOEING 727 727225A 1384077 NM NOSE CONTAMINATED A DALA O OTHER J WARNING INDICATION LD LANDING 1 SO 27 805EA 22436 NOSE GEAR RED UNSAFE LIGHT ILLUM IN FLT ON GEAR EXTENSION RED AND GREEN NOSE GEAR IND LIGHT ILLUM. MTC FOUND THE NOSE GEAR RED LIGHT ILLUM AT THE GATE CLEANED THE CANNON PLUG FOR THE NOSE GEAR LOCK SWITCH AND OPS CHECK NORMAL PER THE MTC MANUAL. 2 L 7 3 4F RT A3WE 2001092100118 20010921 00118 NE 2001 9 21 DL76S011516 2 20010910 A 7200 CF680A2 ENGINE BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE #2 ENGINE UNSERVICEABLE A DALA D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 27 124DE 49701 531 23438 580125 ON CLIMB OUT RIGHT ENGINE STALLED. ACCOMPLISHED POM "ENGINE SURGE OR STALL" PROCEDURE. THROTTLE REDUCED TO IDLE. ENGINE SHUT DOWN AFTER LANDING. EGT MAX 895 FOR 1.4 SECONDS. FOUND METAL IN EXHAUST. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E13NE 2001092100119 20010921 00119 NM 2001 9 21 DL72S011518 1 20010906 A 5312 6516317215 BULKHEAD BOEING 727 727232 1384082 NM FS 351.2, LBL 5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 516DA 21432 FUSELAGE / BULKHEAD / FS 351.2 / LBL 5 : WEB CRACK REPAIR THE FS 351.2 BULKHEAD WEB WAS FOUND CRACKED AT LBL 5 AT A DAMAGED NLG UPLOCK FITTING ATTACH POINT. THE WEB AND LOCAL BULKHEAD CHORD WERE CUT TO REMOVE THE DAMAGE. THE WEB WAS REPAIRED WITH TWO ALUMINUM DOUBLERS AND THE CHORD WITH AN ALUMINUM REPAIR ANGLE PER ER/A 381651-14, REV A. 2 L 7 3 4F A3WE 2001092100120 20010921 00120 NM 2001 9 21 DL767011519 1 20010909 A 5312 148T27405003 BULKHEAD BOEING 767 767232 1385132 NM FS 1809.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 105DA 22217 FUSELAGE / BULKHEAD / FS 1809.5 / RH / OUTER FWD CHORD : CRACK REPAIR INSPECTION OF THE FS 1809.5 BULKHEAD PER AD 2001-09-13 REVEALED A CRACK IN THE RH FWD OUTER CHORD TYPICAL OF THE AD AND BAC S/B 767-53-0078. THE FWD CHORD WAS CUT AND A NEW SECTION SPLICED PER THE S/B. INSPECTION OF THE LOCAL SPLICE FITTING AND SKIN IN THE AREA REVEALED A CRACK AT A FASTENER HOLE. THE HOLE WAS OVERSIZED AND BUSHED IN THE CRACKED MEMBERS. THE REPAIRS WERE PER ER/A 381714-14AD,REV A 2 L 7 2 4F RT A1NM 2001092100121 20010921 00121 NM 2001 9 21 DL757011520 1 20010910 A 2560 D30655133 SLIDE BOEING 757 757232 1384965 NM 2L DOOR UNSERVICEABLE A DALA I CABIN DEPRESSURIZATION O OTHER IN INSP/MAINT 1 SO 27 670DN 25331 AT DEPARTURE THE STEWARDESS WHO CLOSED THE 2L DOOR NOTICED SOMETHING DROPPED ON THE FLOOR. IT WAS A PRESSURE RELIEF VALVE FOR THE SLIDE/RAFT. WE REMOVED AND REPLACED THE SLIDE.LOG SHEET D622305 ITEM 1. 2 L 7 2 4F RT A2NM 2001092100122 20010921 00122 NM 2001 9 21 DL72S011531 1 20010914 A 5300 WEB BOEING 727 727232 1384082 NM TAIL CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 517DA 21433 CRACK AT UPPER FASTNER VERTICAL WEB L/H SIDE STA 1223 REPAIRED PER M/M 57-11-000-8 2 L 7 3 4F A3WE 2001092100123 20010921 00123 NM 2001 9 21 DLM88011536 1 20010916 A 4900 499201431 OIL CAP DOUG MD88 MD88 3023688 NM APU DAMAGED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 956DL 11387 49887 APU AFTER T/O SMOKE ALARM WENT OFF AT 6500 FT SMOKE WASN'T EVIDENT IN COCKPIT FUMES WERE EVIDENT IN CABIN - FOUND APU O IL CAP O-RING CUT - REPLACED SAME - CLEANED AREA - PERFORMED DUCT BURNOUT 2 L 7 2 4F RT A6WE 2001092100124 20010921 00124 NM 2001 9 21 DLM88011543 1 20010916 A 2560 MV10 MEGAPHONE DOUG MD88 MD88 3023688 NM MID CABIN DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 991DL 53343 MID CABIN MEGAPHONE HANDLE DAMAGED._REPLACED MEGAPHONE WITH SERVICABLE UNIT. 2 L 7 2 4F RT A6WE 2001092100125 20010921 00125 NM 2001 9 21 DLM88011545 1 20010916 A 3350 HARNESS DOUG MD88 MD88 3023688 NM 10DE OPEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 994DL 53346 EMERGENCY PATH LIGHT AT SEAT 10DE INOP. FOUND WIRE AT SEAT HARNESS BROKEN. RPLD PATH LIGHT SEAT WIRE HARNESS. LIGHT CKS OK. 2 L 7 2 4F RT A6WE 2001092100126 20010921 00126 NM 2001 9 21 DLM11011550 1 20010915 A 5711 ARB71781 SPAR CAP DOUG MD11 MD11 3023602 NM XORS 725 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 801DE 48472 LH WING / REAR SPAR / UPPER CAP / XORS 725, 745, 790 : CORROSION REPAIR THE LH WING REAR SPAR WAS FOUND CORRODED ON THE UPPER SURFACE OF THE UPPER CHORD AT XORS 725, 745, & 790 COMMON TO TRAILING EDGE PANEL ATTACH FASTENER LOCATIONS. AT THE XORS 725 LOCATION, THE CORROSION EXTENDED UNDER THE UPPER WING SKIN. THE SKIN WAS TRIMMED AWAY OVER A 2" X 2.5" AREA TO ACCESS THE CORROSION. ALL CORROSION AREAS WERE BLENDED AWAY AND THE SKIN REPAIRE WITH 2 ALUM DOUBLERS PER ER/A. 2 L 7 3 4F RT A22WE 2001092100127 20010921 00127 NM 2001 9 21 DL757011554 1 20010918 A 3397 WIRE BOEING 757 757232 1384965 NM CABIN DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 684DA 27104 ON L/O FOUND E+PATH LITE ON 2R FLIGHT ATTENDENT SEAT INOPERATIVE. FOUND WIREING TO BE DAMAGED UNDER SEAT. REPAIRED WIRE ING OPS CHECK NORMAL. 2 L 7 2 4F RT A2NM 2001092100128 20010921 00128 NM 2001 9 21 DL733011558 1 20010918 A 3350 20131A BATTERY BOEING 737 73735B NM RTAFT OVER DOOR DISCHARGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 222DZ 23971 AFT RT OVER DOOR EMER LIGHT REPLCD PWR SUPPLY AND BATT. OPS CKS GOOD 2 L 7 2 4F RT A16WE 2001092100129 20010921 00129 NM 2001 9 21 DL733011559 1 20010918 A 3350 20131A BATTERY BOEING 737 73735B NM LT AFT DOOR EXT DISCHARGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 222DZ 23971 LT AFT DOOR EXT EMER LIGHT INOP REPLCED BATT. OP CKS GOOD 2 L 7 2 4F RT A16WE 2001092100130 20010921 00130 NM 2001 9 21 DL75A011563 1 20010919 A 5330 141N38513 SKIN BOEING 757 757212 NM FS 278, WL 208 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 750AT 23126 FUSELAGE / SKIN / FS 278 / WL 208 : DENT CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND DENTED NEAR FS 278 AT WL 208. THE DENT WAS REMOVED WITH A 5" X 4" CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PERER/A 381653-14. 2 L 7 2 4F RT A2NM 2001092100132 20010921 00132 WP 2001 9 21 CA010907008 1 20010905 A 7120 5072936 MOUNT DOUG DC3 DC3G202A 3021424 WP WRIGHT R1820 R1820G2 67020 EA ENGINE CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 81363 (CAN) ENGINE MOUNT INSPECTED IN ACCORDANCE WITH DC3 SUPPLEMENTAL INSPECTION DOCUMENT 71.03.01E RADIOGRAPHY PROCEDURE. LT MOUNT WAS FOUND TO BE SATISFACTORY, HOWEVER, THE RT MOUNT WAS THOROUGHLY CONTAMINATED WITH CORROSION. THIS CORROSION IS ONLY VISIBLE USING RADIOGRAPHY. MOUNT REPLACED WITH AN AIRWORTHY REPLACEMENT. 2 L 7 2 4R 4 R A618 TC157 2001092100133 20010921 00133 WP 2001 9 21 CA010907009 1 20010905 A 5530 5118022 SUPPORT BRACKET DOUG DC3 DC3G202A 3021424 WP WRIGHT R1820 R1820G2 67020 EA VERTICAL STAB BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 81363 (CAN) BRACKET INSPECTED IN ACCORDANCE WITH THE DC3 SUPPLEMENTAL INSPECTION DOCUMENT 53.03.01. BASE FLANGE BROKEN AS DESC RIBED IN THE SID. REPLACEMENT BRACKET FABRICATED AND INSTALLED AS ORIGINAL. TO BE INSPECTED IN ACCORDANCE WITH THE SID O N A CONTINUING BASIS. 2 L 7 2 4R 4 R A618 TC157 2001092100135 20010921 00135 NM 2001 9 21 CA010907014 1 20010831 A 3244 404F42T2 TIRE BENDIX 26015711 BOEING 737 737281 138448P NM PWA JT8 JT8D17 52049 NE MLG SEPARATED W K NONE O OTHER IN INSP/MAINT 1 CA BH3441BH226 (CAN) RECAP SEPARATED FROM TIRE ON TAKEOFF FROM YVR WAS NOT NOTICED UNTIL AIRCRAFT ARRIVED IN YLW. NO OTHER REPORTABLE D AMAGE AS A RESULT OF THIS INCIDENT. 2 L 7 2 4F 4 F A16WE E2EA 2001092100136 20010921 00136 NM 2001 9 21 DHL2001727529 1 20010819 A 7110 GUSSET BOEING 727 727228 NM NR 3 COWL CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH NR 3 ENG COWLING O/B SIDE INTERNAL GUSSET CRACKED AT 4TH U-BOLT CUTOUT. REMOVED AND REPLACED NR 3 ENG LWR COWLING O/B S IDE INTERNAL GUSSET AT NR 4 U-BOLT CUTOUT . 2 L 7 3 4F A3WE 2001092100137 20010921 00137 NM 2001 9 21 DHL2001727530 1 20010821 A 2120 DUCT BOEING 727 727228 NM A/C BAY BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH FWD CARGO A/C DISTRIBUTION BAY FIBERGLASS DUCT FROM GASPER FAN O/B HAS SEVERAL CRACKS AND BROKEN SPOTS. REMOVED DUCT AS SY AND ROUTED TO FIBERGLASS SHOP PER M/M 21-20-5. INSTALLED FIBERGLASS OVERLAY REPAIR TO DISTRIBUTION BAY PER SRM 51-40 -8 FIG 1. REINSTALLED DUCT PER M/M 21-20-5. 2 L 7 3 4F A3WE 2001092100138 20010921 00138 NM 2001 9 21 DHL2001727531 1 20010823 A 5320 ANGLE BOEING 727 727228 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH FUS LWR EXT BS 720/730 STR 29R/29L FUS TO BODY FAIRING ANGLES SUPPORT 3 CRACKED AT I/B END AT ANCHOR NUT. CUT OUT CRACK ED AREAS PER SRM 51-40-3. FABRICATED REPAIR ANGLES PER SRM 51-40-3. INSTALLED ANGLE REPAIR 3 PER SRM 51-40-3. 2 L 7 3 4F A3WE 2001092100139 20010921 00139 NM 2001 9 21 DHL2001727532 1 20010820 A 5753 FAIRING BOEING 727 727228 NM RT FLAP CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH RT ELEPHANT EAR FLAP FAIRING HAS CHAFING MARKS AT INNER FACE, L/E TORN. REMOVED AND REPLACED INNER SKIN AT RT ELEPHANT EAR FAIRING. 2 L 7 3 4F A3WE 2001092100140 20010921 00140 NM 2001 9 21 DHL2001727534 1 20010819 A 5720 RETAINER BOEING 727 727228 NM LT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH NR 1 SPOILER DOWN STOP O/B BRACKET AT WING T/E HAS ATTACHED RETAINER WITH NICK AND DENTS. REPLACED RETAINER ON NR 1 SPO ILER DOWN STOP O/B BRACKET AT WING LT TRAILING EDGE. 2 L 7 3 4F A3WE 2001092100141 20010921 00141 SO 2001 9 21 CA010907019 1 20010825 A 5610 1159SCV51022 WINDSHIELD GULSTM G1159 G1159A 3970109 SO RROYCE SPEY SPEY5118 54523 EU COCKPIT CRACKED W O OTHER O OTHER CR CRUISE 1 CA (CAN) DURING CRUISE AT FL410 PILOT HEARD A "BANG" AT WHICH POINT HE NOTICED THE LEFT SIDE FORWARD WIND SCREEN WAS CRACK ED. AIRCRAFT SPEED, ALTITUDE AND PRESSURE DIFFERENTIAL WAS REDUCED AS PER THE AFM AND AN UNEVENTFUL LANDING WAS COMPLET ED. SUSPECT CRACKING IS BELIEVED TO HAVE STARTED FROM LOCALIZED SHORTING / BURNING OF THE INTEGRAL ANTI-ICE ELEMENT. 2 L 7 2 4F 4 F A12EA E2EU 2001092100142 20010921 00142 NM 2001 9 21 DHL2001727535 1 20010818 A 5720 GUSSET BOEING 727 727228 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH LEFT WING I/B END, COVE PNL TO NR 7 SPOILER ACTUATOR CASTING, I/B GUSSET CRACKED AT LOWER BOLT HOLE. REMOVED AND REPLAC ED I/B GUSSETS AT NR 7 SPOILER PER SRM 51-30-2. 2 L 7 3 4F A3WE 2001092100144 20010921 00144 NM 2001 9 21 0103306642 1 20010916 A 3350 6042225 POWER SUPPLY BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 642NW 21942 DURING LINE CHECK, FOUND "C" ZONE EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 2001092100145 20010921 00145 NM 2001 9 21 0103315507 1 20010908 A 3350 POWER SUPPLY BOEING 757 757251 1384970 NM MAIN CABIN A NWAA O OTHER O OTHER IN INSP/MAINT 1 GL 01 507US 23169 DURING SCHEDULED MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING SECTION AFT OF ROW 23 INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A2NM 2001092100146 20010921 00146 NE 2001 9 21 EGR2001F00001 1 20010709 A 2910 7665103003053 LINE SKRSKY S76 S76A 8143006 NE HYD SYSTEM DAMAGED A EGRA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 17 911LV 5550 760281 NR 2 HYDRAULIC FAILURE. HYDRAULIC LINE THAT CONNECTS THE NR 2 HYDRAULIC MODULE TO THE YALL PEDAL DAMPNER HAD A LEAK. P N 7665103003053 THIS IS THE SECOND LINE FAILURE IN THE SAME AREA WITHIN ONE WEEK. PIN HOLE IN HYDRAULIC LINE. REPLACE D AFFECTED LINE, REPLACED HYDRAULIC PUMP NR 2 DUE TO DRY RUN CONDITIONS. REPLACED SUPPLY AND RETURN FILTERS. SERVICED AND LEAK CHECKED SYSTEM. 1 G 7 2 3U H1NE 2001092100147 20010921 00147 WP 2001 9 21 CALA0100890 1 20010920 A 5755 FITTING DOUG DC9 DC982 3022082 WP GRD SPOILER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35836 49441 INSPECTION FOUND A 2.25" CRACK IN L/H WING LEFT I/B GROUND SPOILER ACTUATOR SUPPORT FITTING. REPAIRED IAW ECRA 5740-0131 7 AND DRAWING SR09570010. 2 L 7 2 4F A6WE 2001092100148 20010921 00148 WP 2001 9 21 CALA0100891 1 20010920 A 5755 FITTING DOUG DC9 DC982 3022082 WP GRD SPOILER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35836 49441 INSPECTION FOUND A 2.5" CRACK IN R/H WING GROUND SPOILER ACTUATOR FITTING. A DOUBLER WAS INSTALLED IAW ECRA 5740-01317 A ND DRAWING SRO9570010. 2 L 7 2 4F A6WE 2001092100149 20010921 00149 NM 2001 9 21 CALA0100892 1 20010920 A 5415 FITTING BOEING 737 7373T0 1384582 NM #2 PYLON TORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND #2 PYLON AFT FITTING TORN. THE TORN AREA WAS REMOVED AND FILLER AND DOUBLER WERE INSTALLED IAW ECRA 575 0-03588. 2 L 7 2 4F RT A16WE 2001092100150 20010921 00150 2001 9 21 DHL2001727537 4 20010820 A 2310 ANTENNA BOEING 727 727228 NM HF COMM ERODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH HF ANTENNA MAST TIP IS ERODED. REPAIRED HF ANTENNA TIP PER SRM 51-40-8 FIG 1. 2 L 7 3 4F A3WE 2001092100151 20010921 00151 NM 2001 9 21 DHL2001727538 1 20010821 A 5220 SKIN BOEING 727 727228 NM EMERGENCY EXIT DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH RT AFT EMERGENCY EXIT DOOR OUTER SKIN HAS SOME DENTS AROUND. REWORKED DENTS AT RT AFT EMERGENCY EXIT DOOR SKIN PER SRM 51-40-1. 2 L 7 3 4F A3WE 2001092100152 20010921 00152 NM 2001 9 21 DHL2001727539 1 20010818 A 5730 PANEL BOEING 727 727228 NM LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH LEFT WING UPPER PANEL ABOVE I/B AILORON BALANCE PANEL BAY HAS CORROSION BULGES ALONG AFT AND I/B EDGE. REMOVED FASTENER S AT LT PANEL ABOVE I/B AILERON BALANCE PANEL BAY IN ORDER TO ROUT TO FIBERGLASS SHOP PER SRM 51-30-2. REINSTALLED PANE L PER SRM 51-30-2. 2 L 7 3 4F A3WE 2001092100153 20010921 00153 NM 2001 9 21 DHL2001727540 1 20010821 A 5320 CHANNEL BOEING 727 727228 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH MAIN CABIN FLOOR SUPPORT CHANNEL HAS CRACK AT ATTACHMENT BOLT WL STA 850 LBL 1. REMOVED FASTENERS AND REMOVED FLOOR CHAN NEL SUPPORT AT MAIN CABIN STA 850 LBL 1 PER SRM 51-30-2. INSTALLED DOUBLER REPAIR AT CHANNEL AS PER 51-40-2. INSTALLED CHANNEL SUPPORT PER SRM 51-30-2 2 L 7 3 4F A3WE 2001092100154 20010921 00154 NM 2001 9 21 DHL2001727541 1 20010823 A 5512 PANEL BOEING 727 727228 NM HORIZ STAB DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH RT HORIZ STAB UPPER COVER PANEL FOR THE PDU IS DAMAGED AROUND FASTENER. INSTALLED BOND REPAIR TO RT HORIZ STAB COVER PE R SRM 51-40-5. 2 L 7 3 4F A3WE 2001092100156 20010921 00156 NM 2001 9 21 DHL2001727542 1 20010823 A 5347 SEAT TRACK BOEING 727 727228 NM FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH CABIN FLOOR SEAT TRACK WORN BETWEEN BS 405 TO 409 LBL 23. REMOVED DAMAGED SECTION OF SEAT TRACK PER SRM 53-10-5 FIG 7. INSTALLED NEW SEAT TRACK PER SRM 53-10-5 FIG 7. 2 L 7 3 4F A3WE 2001092100158 20010921 00158 NM 2001 9 21 DHL2001727543 1 20010817 A 3231 ROD END BOEING 727 727200 138407E NM LT MLG DOOR WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, LEFT MLG DOOR HAS PLAY AT ACTUATING ARM LINK ATTACHED TO DOOR. REMOVED LINK ROD END AT LEFT MLG WING DOOR A ND REPLACED IAW B-727 MM 32-12-11, OPS CHECKED LEFT MLG NORMAL IAW B-727 MM 32-11-0. 2 L 7 3 4F RT A3WE 2001092100159 20010921 00159 NM 2001 9 21 DHL2001727544 1 20010817 A 5280 BUSHING BOEING 727 727200 138407E NM LT MLG DOOR WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, LEFT MLG WING DOOR HAS PLAY AT FWD AND AFT HINGES. REMOVED BUSHING AT LEFT MLG WING DOOR FWD HINGES AND REP LACED IAW B-727 MM 32-12-11. FOUND GEAR, OPS CHECK NORMAL IAW B-727 MM 32-11-00. 2 L 7 3 4F RT A3WE 2001092100160 20010921 00160 NM 2001 9 21 DHL2001727545 1 20010816 A 5280 BUSHING BOEING 727 727200 138407E NM LT MLG DOOR WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, LEFT MAIN LANDING GEAR STRUT DOOR HAS EXCESS PLAY. REMOVED AND REPLACED BUSHING IN LEFT MAIN LANDING GEAR S TRUT DOOR IAW B-727 MM 32-11-12 BOTH FWD AND AFT HINGES. REMOVED AND REPLACED GIMBALS ASSY BUSHING AND DOOR LINK ROD EN D IAW B-727 MM 32-12-11 FOUND GEAR SWING NORMAL IAW B-727 MM 32-11-00. 2 L 7 3 4F RT A3WE 2001092100164 20010921 00164 NM 2001 9 21 DHL2001727546 1 20010819 A 7110 SKIN BOEING 727 727200 138407E NM NR 1 COWL CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH DURING C-CHECK, NR 1 ENGINE LWR COWLING, O/B SIDE, FIRST U-BOLT CUTOUT, PREVIOUS REPAIR CRACKED. REMOVED PREVIOUS REPAI R PER B-727 SRM 51-30-2 FROM THE NR 1 ENGINE LOWER COWLING O/B SIDE FIRST U-BOLT CUTOUT. MADE NEW DOUBLER PER B-727 SRM 54-10-3 INSTALLED DOUBLER TO NR 1 ENGINE LOWER COWLING O/B SIDE 1ST CUTOUT IAW B-727 SRM 54-30-3. 2 L 7 3 4F RT A3WE 2001092100166 20010921 00166 NM 2001 9 21 DHL2001727547 1 20010817 A 3210 GIMBAL JOINT BOEING 727 727200 138407E NM LT MLG DOOR WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH DURING C-CHECK, LEFT MLG DOOR HAS PLAY AT ACTUATING ARM SWIVEL ATTACH TO GEAR. REMOVED GIMBAL FROM LEFT MLG WING DOOR A CTUATING LINK AND REPLACED IAW B-727 MM 32-12-11. OPS CHECKED LEFT MLG NORMAL IAW B-727 MM 32-11-0. 2 L 7 3 4F RT A3WE 2001092100169 20010921 00169 WP 2001 9 21 ARWA0010902 1 20010918 A 7931 JT3D7 ENGINE DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE A ARWA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 810BN 53068 3690 45905 671358 LOG PAGE 106168. DISCREPANCY: ON CLIMB OUT OF KMIA NBR-3 ENG OIL PRESS LIGHT CAME ON AND OIL PRESS ERRATIC. PERFORMED PR ECAUTIONARY SHUT DOWN. TOTAL WINDMILLING TIME 25 MIN. LANDING WT 240.0 LBS ENG SHUT DOWN AT 0536Z.AIRCRAFT LANDED WITHOU T INCIDENT. CORRECTIVE ACTION: REMOVED AND REPLACED #3 ENGINE IN ACCORDANCE WITH ARROW AIR J/C 6519-6528. PERFORMED ENGI NE TRIN AND RUN IAW ARROW AIR J/C 6527-6528. ENGINE RUN NORMAL. 2 L 7 4 4F 4 F 4A25 1E8 2001092100170 20010921 00170 NM 2001 9 21 DHL2001727548 1 20010817 A 2150 656190311 HEAT EXCHANGER BOEING 727 727200 138407E NM A/C BAY WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH DURING C-CHECK, LEFT SECONDARY H/E EXHAUST LOUVERS HAVE PLAY. REMOVED LT EXHAUST LOUVERS PER B-727 IAW MM 21-55-0. REP LACED LT SECONDARY H/E EXHAUST LOUVERS IN ACCORDANCE WITH B-727 MM 21-55-0. REINSTALLED LT SECONDARY H/E EXHAUST LOUVER S PANEL IN ACCORDANCE WITH B-727 MM 21-55-0. OPS CHECKED LT SECONDARY HEAT EXCHANGER EXHAUST LOUVERS PER B-727 MM 21-55 -0, OPS CHECK OK. 2 L 7 3 4F RT A3WE 2001092100171 20010921 00171 NM 2001 9 21 DHL2001727549 1 20010817 A 2150 65619033 HEAT EXCHANGER BOEING 727 727200 138407E NM A/C BAY WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, LEFT PRIMARY H/E EXHAUST LOUVERS HAVE PLAY. REMOVED LT PRIMARY H/E EXHAUST LOUVERS PER B-727 IAW MM 21-55-0 0. REPLACED LT PRIMARY HEAT EXCHANGER EXHAUST LOUVERS IN ACCORDANCE WITHB-727 MM 21-55-00. REINSTALLED LT PRIMARY HEAT EXCHANGER EXHAUST LOUVER PANEL IN ACCORDANCE WITH B-727 MM 21-55-00. OPS CHECKED LT PRIMARY HEAT EXCHANGER EXHAUST LOU VERS PER B-727 MM 21-55-00, OPS CHECK OK. 2 L 7 3 4F RT A3WE 2001092100172 20010921 00172 NM 2001 9 21 DHL2001727550 1 20010817 A 2150 656190312 HEAT EXCHANGER BOEING 727 727200 138407E NM A/C BAY WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, RIGHT SECONDARY H/E EXHAUST LOUVERS HAVE PLAY. REMOVED RT SECONDARY H/E EXHAUST LOUVERS PER B-727 IAW MM 21 -55-00. REPLACED RT SECONDARY H/E EXHAUST LOUVERS IN ACCORDANCE WITH B-727 MM 21-55-00. OPS CHECKED RT SECONDARY HEAT EXCHANGER EXHAUST LOUVERS PER B-727 MM 21-55-00, OPS CHECK OK. 2 L 7 3 4F RT A3WE 2001092100173 20010921 00173 NM 2001 9 21 DHL2001727551 1 20010817 A 2150 65619034 HEAT EXCHANGER BOEING 727 727200 138407E NM A/C BAY WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, RIGHT PRIMARY H/E EXHAUST LOUVERS HAVE PLAY. REMOVED RT PRIMARY H/E EXHAUST LOUVERS PER B-727 IAW MM 21055- 00. REPLACED RT PRIMARY H/E EXHAUST LOUVERS PER B-727 MM 21-55-00. OPS CHECK RT PRIMARY HEAT EXCHANGER EXHAUST LOUVER S PER B-727 MM 21-55-01, OPS CHECK OK. 2 L 7 3 4F RT A3WE 2001092100174 20010921 00174 NM 2001 9 21 DHL2001727552 1 20010817 A 2150 65602411 DUCT BOEING 727 727200 138407E NM HEAT EXCHANGER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON C-CHECK LEFT PRIMARY H/E U-DUCT HAS CRACKED FLANGE. REMOVED LT PRIMARY H/E DUCT FOR SEND OUT TO REPAIR PER B-727 IAW MM 21-55-11. INSTALLED LT PRIMARY H/E DUCT PER B-727 MM 21-55-11. LEAK CHECKED GOOD LT PRIMARY H/E DUCT IAW MM 21-55- 11. OPS CHECK LT PRIMARY H/E DUCT PER B-727 MM 21-55-21. 2 L 7 3 4F RT A3WE 2001092100175 20010921 00175 NM 2001 9 21 DHL2001727553 1 20010817 A 2150 65602412 DUCT BOEING 727 727200 138407E NM EAT EXCHANGER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, RIGHT PRIMARY H/E U-DUCT HAS CRACKED FLANGE. REMOVED RT PRIMARY H/E DUCT FOR SEND OUT TO REPAIR PER B-727 I AW MM 21-55-11. INSTALLED RT PRIMARY H/E DUCT PER B-727 IAW MM 21-55-11. LEAK CHECK RT PRIMARY H/E DUCT GOOD B-727 IAW 21-55-11. OPS CHECK RT PRIMARY H/E DUCT B-727 IAW MM 21-55-11. 2 L 7 3 4F RT A3WE 2001092100176 20010921 00176 NM 2001 9 21 DHL2001727554 1 20010828 A 2120 656024221 DUCT BOEING 727 727200 138407E NM RT A/C BAY CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, RT A/C BAY, DUCT INBD OF FLOW MULTIPLIER HAS A DEEP WEAR MARK (DUCT MARKED). REMOVED RT A/C BAY DUCT T/B OF FLOW MULTIPLIER AND SEND OUT TO WELDING B-727 IAW MM 21-55-00. REINSTALLED RT A/E BAY DUCT I/B OF FLOW MULTIPLIER B-72 7 IAW MM 21-55-11. LEAK CHECK RT A/C BAY DUCT I/B OF FLOW MULTIPLIER B-727 IAW MM 21-55-11. 2 L 7 3 4F RT A3WE 2001092100177 20010921 00177 NM 2001 9 21 DHL2001727555 1 20010818 A 2612 7C311AA BRACKET BOEING 727 727200 138407E NM NR 3 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, NR 3 ENGINE PYLON I/B FIRE SUPPORT BRACKET IS CRACKED. REMOVED BRACKET SUPPORT AT NR 3 ENGINE PYLON I/B FIR E CLIP CRACK THE BRACKET IS OK FOR SERVICE AS PER B-727 SRM 51-30-2. INSTALLED BRACKET AND NEW CLIP FIRE DETECTOR AS PE R B-727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2001092100178 20010921 00178 NM 2001 9 21 DHL2001727556 1 20010816 A 2120 69162941 SELECTOR VALVE BOEING 727 727200 138407E NM A/C BAY BROKEN A DHLA O OTHER O OTHER IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, FWD CARGO, A/C DISTRIBUTION BAY, THE SELECTOR VALVE AT THE MANIFOLD Y-DUCT IS BROKEN AT LOWER PIVOT BUSHING. REMOVED AND REPLACED VALVE ASSY SHAFT AND DAMPER ASSY, AT MANIFOLD Y-DUCT IAW MM CHP 21-20-3. SYSTEM NEEDS OPS AND LE AK CHECK AND A/C DISTRIBUTION BAY THE SELECTOR VALVE B-727 IAW MM 21-20-3. 2 L 7 3 4F RT A3WE 2001092100179 20010921 00179 NM 2001 9 21 DHL2001727557 1 20010816 A 2120 DUCT BOEING 727 727200 138407E NM A/C BAY LEAKING A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, FWD CARGO, A/C DISTRIBUTION BAY HAS SEVERAL A/C DUCTS JOINED TOGETHER WITH TAPE. AIR LEAKING FROM THESE ARE AS. REPLACED RUBBER BOOST AT Y-DUCT ASSY AREA CLAMPS AT TOP SIDE, IAW MM OPS 21-20-4. SYSTEM REQUIRES OPS AND LEAK CHE CK FOR COMPLETION OF WORK AND DUCT INSTALLATION IAW B-727 MM 21-20-4. 2 L 7 3 4F RT A3WE 2001092100180 20010921 00180 NM 2001 9 21 DHL2001727558 1 20010818 A 5753 MOUNT BOEING 727 727200 138407E NM T/E FLAP CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, REMOVE NR 4 FLAP TRACK FOR INSPECTION AND REINSTALL AFTER INSPECTION C/W. REMOVED LT I/B TRAILING EDGE FLAP IAW B-727 MM 27-51-1. REMOVED NR 4 FLAP TRACK IAW B-727 MM 27-51-31. ACCOMPLISHED VISUAL INSPECTION OF THE NR 4 FLAP TRACK IAW S/B 727-57-0178 FIG 1 REV 3 FOUND MOUNT PAD CORRODED. REMOVED .020 FROM PAD A & B ORIGINAL 0.400 TO 0.380 PER S/B 727-57-0178. REMOVED INSTALLED MACHINED 3 BUSHINGS. INSTALLED NR 4 FLAP TRACK IAW B-727 MM 27-51-31 AS PER S/B 727 -57-0178. INSTALLED LT I/B TRAILING EDGE FLAP ASSEMBLY PER B-727 MM 27-51-1. OPS CHECK OK PER B-727 MM 27-51-0. 2 L 7 3 4F RT A3WE 2001092100181 20010921 00181 NM 2001 9 21 DHL2001727559 1 20010818 A 5753 MOUNT BOEING 727 727200 138407E NM T/E FLAP CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, REMOVE NR 5 FLAP TRACK FOR INSPECTION AND REINSTALL AFTER INSPECTION IS C/W. REMOVED RIGHT I/B TRAILING EDG E FLAP IAW B-727 MM 27-51-31. REMOVED NR 5 FLAP TRACK IAW B-727 MM 27-51-31. ACCOMPLISHED VISUAL INSPECTION OF THE NR 5 FLAP TRACK IAW S/B 727-57-0178 FIG 1 REV 3, FOUND MOUNT PAD CORRODED. REMOVED 0.020 FROM A PAD SAME PAD B ORIGINAL PA D .400 TO .380. REMOVED MACHINED AND INSTALLED 3 BUSHINGS AS PER O/M 57-40-01. INSTALLED NR 5 FLAP TRACK IAW B-727 MM 2 7-51-31 AS PER S/B 727-57-0178. INSTALLED RT INBOARD TRAILING EDGE FLAP ASSEMBLY AS PER B-727 MM 27-51-1. OPS CHECK OK PER B-727 MM 27-51-0. 2 L 7 3 4F RT A3WE 2001092100182 20010921 00182 NM 2001 9 21 DHL2001727560 1 20010816 A 5755 651734748 SPOILER BOEING 727 727200 138407E NM WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, REMOVED NR 3 SPOILER PANEL AND ROUTED TO S/R FOR REPAIR PER B-727 MM 27-61-1. INSTALLED NEW NR 3 SPOILER PA NEL AS B-727 MM 27-61-1. PERFORMED OPS CHECK FOR FAIRING AND FITTING PER MM 27-61-1. OPS CHECK FOR OPERATION OK PER SP OILER NR 3 B-727 MM 27-30-61. 2 L 7 3 4F RT A3WE 2001092100183 20010921 00183 NM 2001 9 21 DHL2001727561 1 20010829 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, MAIN CABIN FLOORBEAM UPPER CHORD CORRODED AT STA 1030 RBL 46. REMOVED CORROSION FROM MAIN CABIN FLOORBEAM U PPER CHORD STA 1030 RBL 46 AS PER 51-10-6 FOUND OUT OF LIMITS AS PER 53-10-1 FIG 4 B-727. CUT OUT CORROSION AREA AS PER B-727 SRM 51-30-2. INSTALLED FLOORBEAM CHORD REPAIR AT MAIN CABIN FLOORBEAM UPPER CHORD IAW B-727 SRM 53-10-3-FIG 3. 2 L 7 3 4F RT A3WE 2001092100184 20010921 00184 NM 2001 9 21 DHL2001727562 1 20010823 A 2842 391041021 PROBE BOEING 727 727200 138407E NM FUEL SYS OUT OF TOLERANCE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH C-CHECK COMP W/DHL REPEATER ALERT FOR NR 2 QTY FUEL INDICATOR REAL CODE 6 IN CRUISE & TANK QTY INTERMITTENTLY INOP. T/S NR 2 FUEL QTY INDICATING SYS TO A BAD FUEL HARNESS PLUS FUEL PROBE F-14, F-13, F-30 READ OUT-OF-TOLERANCE ALONG WITH CO MPENSATOR PROBE F-12. R & R COMP FUEL PROBE F-12, F-14, F-13, F-30 NR 2 FUEL TANK. R & R FUEL QTY HARNESS. TORQUED FU EL TANK BULKHEAD RECEPTACLE WIRE HARNESS. TORQUED CONNECTOR PLUG ATTACH BOLTS. PERF CAPACITANCE & RESISTANCE CHECK NR 2 FUEL TANK HARNESS & PROBES, FOUND GOOD. PERF NR 2 TANK DRY & FULL CALIBRATION OF INDICATORS. INSPECTED FWD LT WING S PAR CONNECTOR NR 2 FUEL TANK HARNESS FOR LEAKS & EVIDENCE OF SEEPAGE THRU WING SPAR CONN SUMMATION UNIT (NO LEAKS). 2 L 7 3 4F RT A3WE 2001092100185 20010921 00185 2001 9 21 2001F00325 4 20010724 A 2300 7510764902 TRANSCEIVER CESSNA 650 650 2076802 CE NR 2 MALFUNCTIONED A UG8A A UNSCHED LANDING O OTHER CR CRUISE 1 GL 23 5117 6507064 NR 2 COMM RADIO FAILED EN ROUTE, WILL NOT HOLD A FREQUENCY. UNABLE TO DUPLICATE AFTER SIX HOURS OF GROUND OPERATION. P ERFORMED BIT AND SELF TEST. CHECKED POWER INPUTS AND GROUNDS AT PT538 AND SECURITY OF PA502. (M) 2 L 7 2 4F A9NM 2001092100186 20010921 00186 CE 2001 9 21 2001F00326 1 20010724 A 2432 991405811 BATTERY CESSNA 750 750 2076810 CE RIGHT OVERTEMP A UG8A A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 GL 23 5114 7500017 FOUND RIGHT BATTERY OVERTEMPED 75 DEGREES CELSIUS, SHUT OFF BATTERY AND RETURNED TO DTW. REPLACED BATTERY, CLEANED TEMP SENSOR CONNECTOR. (M) 2 L 7 2 4J RT T00007WI 2001092100187 20010921 00187 NM 2001 9 21 2001F00328 1 20010905 A 5330 SKIN BOEING 737 737400 NM FUSELAGE DENTED B WT9M K NONE O OTHER NR NOT REPORTED 1 EA 27 933NU 25226 DENT IN SKIN OUT OF LIMITS. REPAIRED PER SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2001092100188 20010921 00188 NM 2001 9 21 2001F00329 1 20010905 A 5311 FRAME BOEING 737 737400 NM FUSELAGE GOUGED B SBEF K NONE O OTHER NR NOT REPORTED 1 EA 27 933NU 25226 FRAME GOUGED OUT OF LIMITS, BS 1064, STRINGER 24L. REPAIRED PER SRM 51-70-11. (M) 2 L 7 2 4F RT A16WE 2001092300001 20010923 00001 SO 2001 9 23 RAIA00109006 1 20010919 A 3260 23092900001 UPLOCK EMB 145 EMB145ER SO Zone 600 FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 8O5HK 5586 145096 5265-MEM-RIGHT MAIN LANDING GEAR DID NOT INDICATE UP AND LOCKED WHEN GEAR RETRACTED AFTER TAKE-OFF. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR UP-LOCK BOX. 2 L 7 2 4F RT T00011AT 2001092300002 20010923 00002 2001 9 23 RAIA00109007 4 20010920 A 3442 MI5853505 TRANSCEIVER AEROSP ATR42 ATR42300 8680920 EU INOPERATIVE A RAIA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 CE 03 422TE 18916 3330 106 7282-STL-WEATHER RADAR WILL NOT TEST.MAINTENANCE REMOVED AND REPLACED WEATHER RADAR TRANSCEIVER. 2 H 7 2 4T RT A53EU 2001092400001 20010924 00001 NE 2001 9 24 2001F00332 2 20010921 A 7200 PT6A67B ENGINE PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL NACELLE MAKING METAL E K NONE O OTHER IN INSP/MAINT 1 WP 07 317NA 2556 223 PR0079 HJ736 ENGINE OIL ANALYSIS SHOWED A CLIMBING TREND IN THE MAGNESIUM AND IRON AMOUNTS. AFTER THREE SAMPLES, IN ACCORDANCE WITH THE MANUFACTURER, REMOVED AND ENGINE AND SENT TO MANUFACTURER FOR INSPECTION AND REPAIR. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001092400013 20010924 00013 WP 2001 9 24 CA010910012 1 20010822 A 3310 BA17011 BALLAST DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE COCKPIT FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) STRONG ELECTRICAL BURNING SMELL IN COCKPIT AFTER TAKEOFF. THUNDERSTORM WHITE FLOODLIGHT SUSPECTED DUE TO LOCALIZAT ION OF SMELL. SMELL DISSIPATED WHEN THUNDERSTORM LIGHT TURNED OFF. REPLACED THUNDERSTORM LIGHT BALLAST ASSEMBLY. 2 L 7 2 4F 4 F A6WE E2EA 2001092400018 20010924 00018 NE 2001 9 24 2001F00333 2 20010921 A 7200 PT6A67B ENGINE PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL FRONT MAKING METAL E S4WA K NONE O OTHER IN INSP/MAINT 1 WP 07 317NA 2556 223 PR0079 HJ736 ENGINE OIL ANALYSIS SHOWED A CLIMBING TREND IN THE MAGNESIUM AND IRON AMOUNTS. AFTER THREE SAMPLES, IN ACCORDANCE WITH THE MANUFACTURER, REMOVED ENGINE AND SENT TO MANUFACTURER FOR INSPECTION AND REPAIR. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001092400019 20010924 00019 EA 2001 9 24 CA010912009 1 20010906 A 2912 MPRV30123 PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE HYD SYSTEM LEAKING W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA 14815 (CAN) SHORTLY AFTER TAKEOFF, THE FLT CREW REPORTED LOSS OF NR 3 HYDRAULIC PRESSURE. ALTRNATE LANDING GEAR EXTENSION CARR IED OUT IN ACCORDANCE WITH THE QRH. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT FURTHER INCIDENT. UPON FURTHER INVES TIGATION, A LEAK WAS FOUND AT THE 3A PUMP/ACOUSTIC FILTER ASSY. BOTH 3A AND 3B PUMPS WERE REPLACED. THE NR 3 HYD SYSTEM WAS RESERVICED AND OPS CHECKED IN ACCORDANCE WITH THE AMM AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2001092400021 20010924 00021 EA 2001 9 24 CA010912011 1 20010906 A 5241 HA6761 HANDLE BOMBDR CC670381001 CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SERVICE DOOR CRACKED W K NONE O OTHER TX TAXI/GRND HDL 1 CA (CAN) GALLEY/SERVICE DOOR OUTER HANDLE CRACKED WHILE DOOR WAS BEING CLOSED BY CATERING PERSONNEL. 2 L 7 2 4F 4 F RT A21EA E15NE 2001092400022 20010924 00022 EA 2001 9 24 CA010912012 1 20010909 A 2760 3G5209C LEVER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SPOILERS FAILED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 767 (CAN) THE CREW REPORTED THAT ON FINAL, WHILE RETRACTING THE FLIGHT SPOILERS, THE AIRCRAFT ROLLED LEFT 1/4 DETENT. FULL R ETRACTION OF THE FLIGHT SPOILER CORRECTED THE CONDITION.THE MAINTENANCE FOUND NO FAULTS LOGGED IN THE MDC OR SECUS. THE SPOILER RIGGING CHECKED GOOD. THEY REMOVED AND REPLACED THE FLIGHT SPOILER CONTROL LEVER IAW AMM 27-61-01, SYSTEM CHECKE D SERVICEABLE AFTER THAT. 2 L 7 2 4F 4 F RT A21EA E15NE 2001092400023 20010924 00023 EA 2001 9 24 CA010912013 1 20010909 A 3230 530507 SWIVEL VALVE CNDAIR CL600 CL600* EA GE CF34 CF34* NE NLG STEERING SEIZED W D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 CA 481 (CAN) THE MAINTENANCE FOUND THE NL HYDRAULIC SWIVEL VALVE ANTI-ROTATION PIN SHEARED. THE SWIVEL VALVE P/N 53050-7, S/N M AL-0079, WAS REMOVED FROM AIRCRAFT 10008, IT WOULD APPEAR THAT THE VALVE WOULD HAVE SEIZED RESULTING IN THE LT ANTI-ROTA TION PIN P/N 52119-1 SHEARING ALLOWING THE BOTTOM PART OF THE SWIVEL VALVE TO ROTATE BACK AND FORTH FOLLOWING THE MOVEME NT OF THE ACTUATOR, SUBSEQUENTLY BREAKING THE HYDRAULIC LINE P/N 52404-3. 2 L 7 2 4F 4 F RT A21EA E15NE 2001092400024 20010924 00024 EA 2001 9 24 CA010912014 1 20010909 A 5240 HA6761 HANDLE CNDAIR CL600 CL6002A12 1900304 EA GE CF34 CF34* NE SERVICE DOOR BROKEN W K NONE O OTHER TX TAXI/GRND HDL 1 CA 63 (CAN) THE RAMP PERSONNEL BROKE THE OUTER HANDLE OF THE SERVICE DOOR DURING NORMAL OPERATION. THE PERSON WORKING REPORT ED THAT HE DID NOT USED ANY EXCESSIVE FORCE TO OPEN THE DOOR. THE MAINTENANCE REPLACED THE OUTER HANDLE ON THE SERVICE D OOR. 2 L 7 2 4F 4 F RT A21EA E15NE 2001092400025 20010924 00025 EA 2001 9 24 CA010912015 1 20010911 A 5410 601350061 WEB BOMBDR 60135006 CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE UPPER WEB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 20129 (CAN) TWO CRACKS FOUND ON ENGINE SUPPORT BEAM UPPER WEB AT FS 640 NEAR L & R BL 9.0 (1.25 AND 1.5 INCHES LONG). ONE CRAC K FOUND ON LHS OF ACCESS PANEL LANDING CORNER ON LOWER WEB NEAR LBL 36.2 (0.5 INCHES LONG). REPAIRED IN ACCORDANCE WITH REO'S 601R-53-61-366 (BOTH SIDES). 2 L 7 2 4F 4 F RT A21EA E15NE 2001092400033 20010924 00033 NE 2001 9 24 2001F00331 2 20010921 A 7200 PT6A67B ENGINE PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL ENGINE MAKING METAL E S4WA K NONE O OTHER IN INSP/MAINT 1 WP 07 317NA 2556 223 PR0079 HJ736 ENGINE OIL ANALYSIS SHOWED A CLIMBING TREND IN THE MAGNESIUM AND IRON AMOUNTS. AFTER THREE SAMPLES, IN ACCORDANCE WITH THE MANUFACTURER, REMOVED ENGINE AND SENT TO MANUFACTURER FOR INSPECTION AND REPAIR. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001092400034 20010924 00034 WP 2001 9 24 ARWA0010901 1 20010907 A 3030 3377 CONTROL PANEL LKHEED 1011 1011385115 5265015 WP COCKPIT FAILED A ARWA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SO 19 308GB 193U1133 F/O'S RIGHT PITOT HEAT LIGHT ON WITH SWITCH IN. F/O AIRSPEED INDICATION FAILED 5' LATER, THEN NR 2 MACH FEEL CHANNEL AN D NR 2 MACH TRIM FAILED, RUDDER HYDRAULIC LIMITER LIGHT ON PILOT'S C&W PANEL ON 34-14-61-02. REMOVED AND REPLACED AIR D ATA SENSOR HEAT PANEL IAW MM 30-31-00, OPS CK NORMAL. 2 L 7 3 4F A23WE 2001092400035 20010924 00035 EU 2001 9 24 AWXA200100451 2 20010917 A 7321 9368M57P19 MEC BOEING 737 73733A 1384673 NM CFMINT CFM56 CFM562BFR 13802 EU NR 2 ENGINE OUT OF RIG A AWXA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 28 173AW 39711 539 23632 722294 PHX - ABORTED TAKEOFF - FLT 436 - C - DURING TAKEOFF ROLL THE NR 2 ENGINE WAS SLOW TO SPOOL UP, ABOUT 6 SEC SLOWER THAN NR 1 ENGINE. PMC'S AND BLEEDS WERE ON. ALL OTHER PARAMETERS WERE NORMAL. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE TROUBLESHOT AND FOUND THE NR 2 ENGINE MAIN ENGINE CONTROL HI AND LOW IDLE'S WERE OUT OF TRIM. T HE HI AND LOW IDLE'S WERE TRIMMED PER AMM 71-00-01 PG 234. PERFORMED TEST 4 ACCELERATION / DECELERATION TEST, ALL CHEC KS GOOD. NO FURTHER DISCREPANCIES REPORTED. 2 L 7 2 4F 4 F RT A16WE E21EU 2001092400036 20010924 00036 NM 2001 9 24 AWXA200100452 1 20010918 A 2750 FLAP BOEING 737 73733A 1384673 NM WING MALFUNCTIONED A AWXA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 WP 28 509DC 23636 SFO - FLAP LOCKOUT - FLT 815 - C - ON APPROACH TO SFO FLAPS 5 WAS SELECTED AND THE FLAP POSITION INDICATOR NEEDLES SPLIT AT FLAPS 1 AND THE FLAPS STOPPED AT FLAPS 1. THE AIRCRAFT LANDED AT FLAPS 1 AND UPON TOUCHDOWN THE FLAPS MOVED TO FLAP S 5 AS WAS SELECTED. IN SFO MAINTENANCE CHECKED THE TRAILING EDGE FLAP ASYMMETRY PER AWA TASK CARD F1B27016. NO DISCRE PANCIES WERE FOUND, THE FLAPS WERE CYCLED SEVERAL TIMES WITH NO FAULTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE AND NO DISCREPANCIES HAVE BEEN REPORTED SINCE. 2 L 7 2 4F RT A16WE 2001092400037 20010924 00037 SO 2001 9 24 C2XA01TY119 1 20010916 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13989 145271 TYS DURING A SCHEDULED INSPECTION THE FORWARD TOP CAP BETWEEN FRAMES 19 AND 23 WAS FOUND TO HAVE AREAS OF MINOR CORROSI ON AND GOUGED. MAINTENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB-145 SRM 51-40-01, REPAIR WAS SATISFACTORY. AIRCRAF T WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001092400038 20010924 00038 SO 2001 9 24 C2XA01TY120 1 20010921 A 5315 14522459001 FLOORBEAM EMB 145 EMB145 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13989 145271 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RAMP ANGLE BETWEEN FRAMES 19 AND 20. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW EMB-145 SRM 51-40-02, REPAIR WAS SATISFACTORY. AIRCRAFT WILL BE RELEASED UPON COMPLETIO N OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001092400039 20010924 00039 SO 2001 9 24 C2XA01TY121 1 20010921 A 2612 3601133500 FIRE LOOP EMB 145 EMB145 SO RT ENGINE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13989 3417 3417 145271 TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND ENGINE FIRE DETECTION LOOP WAS FOUND CHAFED BEYOND LIMITS. MAINTENANC E REMOVED AND REPLACED THE FIRE DETECTION LOOP IAW EMB-145 MM 26-11-01, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001092400040 20010924 00040 SO 2001 9 24 C2XA01TY122 1 20010921 A 7160 14575001405 INLET EMB 145 EMB145 SO RT ENGINE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13989 145271 TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND ENGINE INLET GUIDE PIN HOLE FOR COWLING WAS FOUND TO BE GOUGED. MAINT ENANCE ACCOMPLISHED THE BLEND OUT REPAIR IAW EMB GST 3178/01, REPAIR WAS SATISFACTORY. AIRCRAFT WILL BE RELEASED UPON C OMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001092400041 20010924 00041 NM 2001 9 24 DHL2001717022 1 20010921 A 3350 BATTERY PACK BOEING 727 72723 1384004 NM CABIN DISCHARGED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 717DH 19389 DURING STBY POWER CHECK EMERGENCY EXIT LIGHTS WOULD NOT STAY ILLUMINATED. REMOVED AND REPLACED BATTERY PACK IAW B-727 M /M 33/50/71. 2 L 7 3 4F A3WE 2001092400043 20010924 00043 NM 2001 9 24 DHL2001727533 1 20010815 A 5720 ANGLE BOEING 727 727228 NM WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH APU EXHAUST TOP COVE PANEL AT T/E FOR APU EXHAUST LOUVERS, FWD O/B SUPPORT ANGLE IS CRACKED JUST AFT OF SPAR. REMOVED A ND REPLACED THE APU EXHAUST TOP COVE PANEL AT T/E FWD O/B SUPPORT ANGLE PER SRM 51-30-2 AND 57-10-2. HEAT TREATED AND AG ED PART PER GPS988MSI.247. 2 L 7 3 4F A3WE 2001092400044 20010924 00044 CE 2001 9 24 CA010914007 1 20010907 A 2612 MS250832DE5 BONDING JUMPER KIDDE 896H16 LEAR 35 35LEAR 5170600 CE GARRTT TFE731 TFE73122B 01518 WP OTBD CONNECTOR FAILED W B EMER. DESCENT N FALSE WARNING DE DESCENT 1 CA (CAN) DUING CRUISE PILOTS NOTICED RT ENGINE FIRE INDICTION, FIRED BOTH BOTTLES AND DID EMERGENCY LANDING IN JFK AIRPORT. AFTER VISUAL INSPECTION OF RT ENGINE FIRE DETECTION SYSTEM, THE OUTBOARD CONNECTOR ON THE GEARBOX FIRE LOOP WAS FOUND T O BE IN LOOSE. CONNECTOR RE-SECURED AND FIRE DETECTION SYSTEM FUNCTION CHECK C/O, NO FAULT.REF: LEAR 35/36 IPC 26-10-30 2 L 7 2 4F 4 F A10CE E6WE 2001092400045 20010924 00045 NM 2001 9 24 DHL2001727536 1 20010816 A 2782 MOUNT BOEING 727 727228 NM SLAT ACTUATOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH LT WING NR 3 SLAT ACTUATOR FWD MOUNT INSP HOLE HAS 2 CRACKS AT I/B SIDE OF ACCESS PANEL. STOP DRILLED CRACKS PER SRM 51 -10-1. INSTALLED DOUBLER REPAIR PER SRM 51-30-2. 2 L 7 3 4F A3WE 2001092400046 20010924 00046 NM 2001 9 24 DHL2001727563 1 20010829 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, MAIN CABIN FLOORBEAM UPPER CHORD CORRODED AT STA 1070 RBL 46. FOUND CORROSION OUT OF LIMITS AS PER B-727 SR M 53-10-1. CUT OUT CORRODED AREA AS PER B-727 SRM 51-30-2 AND 53-10-8. INSTALLED FLOORBEAM CHORD REPAIR IAW B-727 SRM 53-10-8 FIG 3. 2 L 7 3 4F RT A3WE 2001092400047 20010924 00047 NM 2001 9 24 DHL2001727564 1 20010819 A 5312 BULKHEAD BOEING 727 727200 138407E NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH C-CHECK, RT W/WELL FWD BULKHEAD, LWR CENTER WEB SKIN AROUND ELECT CONNECTOR HAS 2 BROKEN RIVETS AND SKIN CRACKED AND COR RODED. REMOVED CORROSION AT RT W/W FWD BULKHEAD LWR CENTER WEB STA 870. FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA AT S TA 870 RT W/W FWD BULKHEAD LWR CENTER WEB AND CUT OUT PREVIOUS DOUBLER IAW B-727 SRM 53-10-9. INSTALLED WEB REPAIR AT BL KD STA 870 RT SIDE AS PER AVITAS EO= AVHM-255RO-1. 2 L 7 3 4F RT A3WE 2001092400048 20010924 00048 NM 2001 9 24 DHL2001727565 1 20010823 A 5347 SEAT TRACK BOEING 727 727200 138407E NM FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, CABIN FLOOR SEAT TRACK BETWEEN BS 570 TO BS 600, LBL 25 HAS WORN AREA. REMOVED MAIN CABIN SEAT TRACK LBL 25 FROM BS 500 TO 680 AS PER B-727 SRM 51-30-2. INSTALLED NEW SEAT TRACK ON BS 500 TO 680 LRL 25 AT FLOOR CABIN B-727 SRM 52-30-2. 2 L 7 3 4F RT A3WE 2001092400049 20010924 00049 NM 2001 9 24 DHL2001727566 1 20010824 A 5347 SEAT TRACK BOEING 727 727200 138407E NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, CABIN FLOOR SEAT TRACK BETWEEN BS 650 TO 660, LBL 25 HAS NICKS AND DENTS. REMOVED MAIN CABIN SEAT TRACK LBL 25 FROM BS 500 TO BS 680 AS PER B-727 SRM 51-30-2. INSTALLED NEW SEAT TRACK ON BS 500 TO 680 LBL 25 AT FLOOR CABIN B-72 7 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2001092400050 20010924 00050 NM 2001 9 24 DHL2001727567 1 20010817 A 5244 69467531 DOOR BOEING 727 727200 138407E NM LT PACK EXCESS PLAY A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, LEFT PACK GROUND COOLING FAN DOOR EXCESSIVE. REMOVED LT PACK GROUND COOLING FAN DOOR PER B-727 IAW MM 21-11 -0. INSTALLED BUSHING AND BEARING AND BRAKE RT PACK GROUND FAN COOLING DOOR PER B-727 IAW MM 21-11-0. OPS CHECK GOOD L T PACK GROUND COOLING FAN DOOR B-727-IAW MM 21-11-0. 2 L 7 3 4F RT A3WE 2001092400051 20010924 00051 NM 2001 9 24 DHL2001727568 1 20010821 A 3610 656329529 DUCT BOEING 727 727200 138407E NM BLEED AIR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, FOUND A CRACK AND GOUGES ON DUCT FROM BLEED AIR TO FLOW MULTIPLIER. REMOVED RT DUCT BLEED AIR TO FLOW MULTI PLIER TO SEND OUT TO WELDING B-727 IAW MM 21-55-11. INSTALLED RT DUCT BLEED AIR FLOW MULTIPLIER B-727 IAW MM 21-55-11. LEAK CHECK GOOD RT DUCT BLEED AIR TO FLOW MULTIPLIER B-727 IAW MM 21-55-11. 2 L 7 3 4F RT A3WE 2001092400052 20010924 00052 NM 2001 9 24 DHL2001727569 1 20010828 A 5320 STIFFENER BOEING 727 727200 138407E NM FUSELAGE BENT A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, WEB BS 970 TO 991 OVER STR 29 RT STIFFENER BENT (AFT CARGO COMPARTMENT). STRAIGHTENED DAMAGED AREA ON VERTI CAL STIFFENER AS PER BOEING A/C 727 SRM 51-40-1. 2 L 7 3 4F RT A3WE 2001092400053 20010924 00053 NM 2001 9 24 DHL2001727570 1 20010820 A 2810 STRUCTURE BOEING 727 727200 138407E NM RT TANK LEAKING A DHLA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, FUEL LEAK AT 2 FASTENERS ON STIFFENER LOWER FWD SPAR WS 224, RT CENTER TANK. OPENED TANK AND PURGED IAW MM 28-10-0. REMOVED SEALANT FROM STIFFENER, TIGHTENED FASTENER AND RESEALED IAW MM 28-11-0. LEAK CHECK IAW 727 MM 25-11-0. NO LEAKS NOTED. 2 L 7 3 4F RT A3WE 2001092400054 20010924 00054 NM 2001 9 24 DHL2001727571 1 20010820 A 2420 651893122 CONDUIT BOEING 727 727200 138407E NM AC GEN SYSTEM BENT A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, MAIN CABIN UNDER FLOOR CONDUIT LINE BENT AND CHAFING WITH SKIN AT STA 770 LBL 30. REMOVED NR 1 GENERATOR CA BLE CONDUIT AND ROUTED FOR REPAIR 24-20-81 IAW B-727 MM 24-20-81. INSTALLED NR 1 GENERATOR CABLE AND CONDUIT IAW B727 M M 24-20-81. OPS CHECK NR 1 GENERATOR AS PER JRH06, NO DEFECTS NOTED. 2 L 7 3 4F RT A3WE 2001092400055 20010924 00055 NM 2001 9 24 DHL2001727572 1 20010820 A 2810 STRUCTURE BOEING 727 727200 138407E NM NR 3 MAIN TANK LEAKING A DHLA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, FUEL LEAKS AT 2 BOTTOM BOLTS AT RT MLG TRUNNION NR 3 MAIN TANK. OPENED TANK AND PURGED IAW MM 28-10-0. REM OVED SEALANT FROM LOWER REAR SPAR AT GEAR TRUNNION AND RESEALED IAW MM 28-11-0. OK TO CLOSE TANK. CLOSED ACCESS PLATES 7602 IAW MM 28-11-21. LEAK CHECK GOOD IAW B727 MM 28-11-0. 2 L 7 3 4F RT A3WE 2001092400056 20010924 00056 NM 2001 9 24 DHL2001727573 1 20010821 A 4910 38067811 APU BOEING 727 727200 138407E NM APU BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, APU BORESCOPE INSPECTION REVEAL VISIBLE CRACK AT CONTAINMENT RINGS. ALSO CONVERGING MULTIPLES CRACKS FROM I NTERIOR. REMOVED AND REPLACED APU ASSY ACCOMPLISHED ON NR 6856 PER B-727 MM 49-11-00. 2 L 7 3 4F RT A3WE 2001092400057 20010924 00057 NM 2001 9 24 DHL2001727574 1 20010911 A 5280 DOOR BOEING 727 727200 138407E NM LT MLG CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, LT SIDE MLG STRUT DOOR HAS A CRACK BETWEEN LOWER PORTION AND TOP PORTION FWD TOP SKIN ON REPAIR. REMOVED PR EVIOUS REPAIR AND MAKE NEW REPAIR IAW B-727 SRM 51-10-3. 2 L 7 3 4F RT A3WE 2001092400058 20010924 00058 NM 2001 9 24 DHL2001727575 1 20010820 A 2810 STRUCTURE BOEING 727 727200 138407E NM NR 3 MAIN TANK LEAKING A DHLA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, FUEL LEAK AT FWD BOTTOM SKIN PLANK SEAM AT CURVE TO FWD SPAR TO NR 8 FLAP TRACK, NR 3 MAIN TANK. REMOVED LO OSE SEALANT FROM PLANK SEAM AND RESEALED IAW MM 28-11-0. LEAK CHECK GOOD IAW B-727 MM 28-1-0. 2 L 7 3 4F RT A3WE 2001092400060 20010924 00060 NM 2001 9 24 DHL2001727576 1 20010820 A 2810 STRUCTURE BOEING 727 727200 138407E NM NR 3 MAIN TANK LEAKING A DHLA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, FUEL LEAK AT UPPER SPAR DOUBLER FWD SPAR AT WS 7604 NR 3 MAIN TANK. OPENED TANK AND PURGED IAW MM 28-10-0. REMOVED SEALANT FROM UPPER SPAR DOUBLER AND TIGHTENED FASTENERS, RESEALED IAW 28-11-0. LEAK CHECK GOOD IAW B-727 MM 28- 11-0. 2 L 7 3 4F RT A3WE 2001092400061 20010924 00061 NM 2001 9 24 DHL2001727577 1 20010820 A 2810 STRUCTURE BOEING 727 727200 138407E NM NR 3 MAIN TANK LEAKING A DHLA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, FUEL LEAKS AT APPROX 15 EACH FASTENERS TOP SKIN FWD SPAR APPROX WS 410 AND ADJACENT PLANK SEAM NR 3 MAIN. O PENED TANK AND PURGED IAW 28-10-0. REMOVED SEALANT FROM FASTENERS, TIGHTENED AND RESEALED IAW 28-11-0. LEAK CHECK GOOD I AW B-727 MM 28-11-00. 2 L 7 3 4F RT A3WE 2001092400062 20010924 00062 NM 2001 9 24 DHL2001727578 1 20010820 A 2810 STRUCTURE BOEING 727 727200 138407E NM NR 3 MAIN TANK LEAKING A DHLA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, FUEL LEAKS AT 4 FASTENERS TOP SKIN FROM WS 304 TO INBOARD END OF NR 3 MAIN TANK. OPENED TANK AND PURGED IAW MM 28-10-0. REMOVED SEALANT FROM FASTENERS, TIGHTENED, AND RESEALED IAW MM 28-11-0. LEAK CHECK GOOD IAW B-727 MM 28-11 -0. 2 L 7 3 4F RT A3WE 2001092400063 20010924 00063 NM 2001 9 24 DHL2001727579 1 20010820 A 2810 STRUCTURE BOEING 727 727200 138407E NM NR 3 MAIN TANK LEAKING A DHLA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, FUEL LEAKS AT TOP AND BOTTOM OF STIFFENER FWD SPAR JUST OUTBOARD OF PRESSURE SWITCHES, NR 3 MAIN TANK. OPEN ED TANK AND PURGED IAW MM 28-10-0. REMOVED SEALANT FROM STIFFENER, TIGHTENED AND RESEALED IAW MM 28-11-0. LEAK CHECK GO OD IAW B-727 MM 28-11-0. 2 L 7 3 4F RT A3WE 2001092400064 20010924 00064 NM 2001 9 24 DHL2001727580 1 20010820 A 2810 STRUCTURE BOEING 727 727200 138407E NM NR 3 MAIN TANK LEAKING A DHLA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, FUEL LEAK AT FASTENERS AT BOTTOM OF STIFFENER JUST INBOARD OF PRESSURE SWITCHES NR 3 MAIN TANK. OPENED TANK AND PURGED IAW MM 28-10-0. REMOVED SEALANT FROM STIFFENER, TIGHTENED FASTENERS AND RESEALED IAW MM 28-11-0. LEAK CHECK GOOD IAW B-727 MM 28-11-0. 2 L 7 3 4F RT A3WE 2001092400065 20010924 00065 NM 2001 9 24 DHL2001727581 1 20010820 A 2810 STRUCTURE BOEING 727 727200 138407E NM NR 2 MAIN TANK LEAKING A DHLA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, FUEL LEAK AT LOWER 2 BOLTS RT GEAR TRUNNION, NR 2 MAIN TANK. OPENED TANK AND PURGED IAW MM 28-10-0. REMOVE D SEALANT FROM LOWER REAR SPAR AT GEAR TRUNNION AND RESEALED IAW MM 28-11-0. LEAK CHECK GOOD IAW B-727 MM 28-11-0. 2 L 7 3 4F RT A3WE 2001092400066 20010924 00066 NM 2001 9 24 DHL2001727582 1 20010911 A 5280 69148161 HINGE BOEING 727 727200 138407E NM LT MLG DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, LT MLG I/B DOOR HAS FWD HINGE WITH CRACK. REMOVED AND REPLACED LT MLG I/B DOOR FWD HINGE IAW B-727 MM 32-2- 1. 2 L 7 3 4F RT A3WE 2001092400067 20010924 00067 NM 2001 9 24 2001F00335 1 20010905 A 5330 SKIN BOEING 737 737400 NM FUSELAGE DENTED B WT9M K NONE O OTHER IN INSP/MAINT 1 EA 27 933NU 25226 FOUND DENT IN SKIN OUT OF LIMITS, BS 360 STRINGER 22R. REMOVED DAMAGE AND REPAIRED PER SRM 53-00-03 FIG 204. (M) 2 L 7 2 4F RT A16WE 2001092400068 20010924 00068 CE 2001 9 24 2001F00336 1 20010722 A 3260 67420292 SQUAT SWITCH CESSNA 750 750 2076810 CE NLG OUT OF ADJ B UG8A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 5116 2268 7500019 DTW - NOSE GEAR WOULD NOT RETRACT. ADJUSTED NOSE GEAR SQUAT SWITCH RAMP. (M) 2 L 7 2 4J RT T00007WI 2001092400069 20010924 00069 NM 2001 9 24 2001F00337 1 20010905 A 5311 FRAME BOEING 737 737400 NM FUSELAGE CORRODED B WT9M K NONE O OTHER IN INSP/MAINT 1 EA 27 933NU 25226 FOUND CORROSION ON FRAME OUT OF LIMITS, BS 7270 STRINGER 25L. REPAIRED PER SRM 51-70-11. (M) 2 L 7 2 4F RT A16WE 2001092400070 20010924 00070 NM 2001 9 24 2001F00339 1 20010905 A 5311 FRAME BOEING 737 737400 NM FUSELAGE CRACKED A WT9M K NONE O OTHER IN INSP/MAINT 1 EA 27 933NU 25266 FRAME CRACKED. REPAIRED PER SRM 53-00-07 FIG 202, AT BS 400 BETWEEN STRINGER 8L AND 9L. (M) 2 L 7 2 4F RT A16WE 2001092400071 20010924 00071 NM 2001 9 24 2001F00340 1 20010905 A 5313 STRINGER BOEING 737 737400 NM FUSELAGE CORRODED B WT9M K NONE O OTHER IN INSP/MAINT 1 EA 27 933NU 25226 FOUND CORROSION ON STRINGER 17L AT BS 637. REPAIRED PER ER 01-0753. (M) 2 L 7 2 4F RT A16WE 2001092400072 20010924 00072 NM 2001 9 24 2001F00341 1 20010905 A 5311 FRAME BOEING 737 737400 NM FUSELAGE CRACKED B WT9M K NONE O OTHER IN INSP/MAINT 1 EA 27 933NU 25226 FRAME CRACKED AT BS 727D BETWEEN STRINGER 8 AND 9L. REPAIRED PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 2001092400073 20010924 00073 NM 2001 9 24 2001F00342 1 20010905 A 5311 FRAME BOEING 737 737400 NM FUSELAGE CRACKED B WT9M K NONE O OTHER IN INSP/MAINT 1 EA 27 933NU 25226 FOUND FRAME CRACKED AT BS 727D BETWEEN STRINGER 8R AND 9L. REPAIRED PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 2001092400074 20010924 00074 NM 2001 9 24 2001F00343 1 20010905 A 5311 FRAME BOEING 737 737400 NM FUSELAGE CRACKED A WT9M K NONE O OTHER IN INSP/MAINT 1 EA 27 933NU 25226 FOUND FRAME CRACKED AT BS 747 BETWEEN STRINGER 8/9L. REPAIRED PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 2001092400075 20010924 00075 NM 2001 9 24 2001F00344 1 20010905 A 5311 FRAME BOEING 737 737400 NM FUSELAGE CRACKED B WT9M K NONE O OTHER IN INSP/MAINT 1 EA 27 933NU 25226 FOUND FRAME CRACKED AT BS 727 BETWEEN STRINGER 8 AND 9L. REPAIRED PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 2001092400076 20010924 00076 NM 2001 9 24 2001F00345 1 20010905 A 5311 FRAME BOEING 737 737400 NM FUSELAGE CRACKED B WT9M K NONE O OTHER IN INSP/MAINT 1 EA 27 933NU 25226 FOUND FRAME CRACKED AT BS 727D BETWEEN STRINGER 8/9R. REPAIRED PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 2001092400077 20010924 00077 NM 2001 9 24 2001F00346 1 20010905 A 5311 FRAME BOEING 737 737400 NM FUSELAGE CRACKED B WT9M K NONE O OTHER IN INSP/MAINT 1 EA 27 933NU 25226 FOUND FRAME CRACKED AT BS 747 BETWEEN STRINGER 8/9R. REPAIRED PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 2001092400078 20010924 00078 NM 2001 9 24 2001F00347 1 20010905 A 5311 FRAME BOEING 737 737400 NM FUSELAGE CRACKED B WT9M K NONE O OTHER IN INSP/MAINT 1 EA 27 933NU 25226 FOUND FRAME CRACKED AT BS 787 BETWEEN STRINGER 8/9R. REPAIRED PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 2001092400079 20010924 00079 NM 2001 9 24 2001F00348 1 20010905 A 5311 FRAME BOEING 737 737400 NM FUSELAGE CRACKED A WT9M K NONE O OTHER IN INSP/MAINT 1 EA 27 933NU 25226 FOUND FRAME CRACKED AT BS 827 BETWEEN STRINGER 8/9R. REPAIRED PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 2001092400080 20010924 00080 NM 2001 9 24 CA010917005 1 20010908 A 2910 82950010237 TUBE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM LEAKING W K NONE K FLUID LOSS TX TAXI/GRND HDL 1 CA 30038 (CAN) CREW REPORTED FLUID LEAK UNDER RIGHT HAND WING AND FALLING ON THE #4 MAIN WHEEL ASSEMBLY. AFTER MAINTENANCE INVEST IGATION IT WAS FOUND THAT THE LIFT DUMP PRESSURE LINE HAD A PIN HOLE LEAK IN A BEND 14 INCHES FROM OUTBOARD END OF THE R IGID HYDRAULIC TUBE.RIGID HYDRAULIC TUBE WAS REPLACED, LEAK CHECKS CARRIED OUT AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001092400081 20010924 00081 NM 2001 9 24 2001F00349 1 20010905 A 5311 FRAME BOEING 737 737400 NM FUSELAGE CRACKED B WT9M K NONE O OTHER IN INSP/MAINT 1 EA 27 933NU 25226 FOUND FRAME CRACKED AT BS 867 BETWEEN STRINGER 8/9R. REPAIRED PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 2001092400082 20010924 00082 NM 2001 9 24 2001F00350 1 20010905 A 5315 FLOORBEAM BOEING 737 737400 NM FUSELAGE CORRODED B WT9M K NONE O OTHER IN INSP/MAINT 1 EA 27 933NU 25226 FOUND CORROSION ON FLOORBEAM AT BS 344 LBL 55. REPAIRED PER ER 01-0730. (M) 2 L 7 2 4F RT A16WE 2001092400084 20010924 00084 NM 2001 9 24 2001F00351 1 20010905 A 5315 FLOORBEAM BOEING 737 737400 NM FUSELAGE CORRODED B WT9M K NONE O OTHER IN INSP/MAINT 1 EA 27 933NU 25226 FOUND CORROSION ON FLOORBEAM AT BS 312 RBL 38 TO LBL 37. REPAIRED PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2001092400085 20010924 00085 NM 2001 9 24 CA010917007 1 20010906 A 2910 82970410115 TUBE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM CHAFED W O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 CA 7832 (CAN) AFTER TAXIING THE AIRCRAFT TO THE GATE FOR THE MORNING DEPARTURE, MAINTENANCE DISCOVERED A HYDRAULIC LEAK IN THE R IGHT WHEEL. UPON FURTHER INVESTIGATION, IT WAS DETERMINED THAT THE LEAK WAS COMING FROM TWO CHAFED HYDRAULIC LINES ROUTE D TOGETHER ALONG THE EXHAUST SHROUD. (THE RIGHT ENGINE HYDRAULIC PUMP CASE DRAIN LINE DEVELOPED A PIN HOLE LEAK DUE TO B EING CHAFED AGAINST THE PUMP PRESSURE LINE AFT OF THE FIRWALL.) BOTH HYDRAULIC LINES WERE REPLACED AND ALL FURTHER CHECK S WERE COMPLETED PRIOR TO RETURNING THE AIRCRAFT TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001092400086 20010924 00086 NM 2001 9 24 CA010917008 1 20010909 A 2910 92940010103 TUBE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM CRACKED W K NONE K FLUID LOSS TX TAXI/GRND HDL 1 CA 35125 (CAN) DURING A WALK AROUND, THE FLIGHT CREW NOTICED HYDRAULIC FLUID LEAKING FROM THE RIGHT HAND WING ROOT AREA. UPON MAI NTENANCE INVESTIGATION IT WAS FOUND THAT THE NR 2 SYSTEM SPOILER LIFT DUMP PRESSURE LINE WAS LEAKING FROM A CRACK IN THE TUBE.THE RIGID HYDRAULIC TUBE WAS REPLACED AND LEAK CHECKS CARRIED OUT. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001092400087 20010924 00087 NM 2001 9 24 2001F00352 1 20010905 A 5315 FLOORBEAM BOEING 737 737400 NM FUSELAGE CORRODED B WT9M K NONE O OTHER IN INSP/MAINT 1 EA 27 933NU 25226 FOUND CORROSION ON FLOORBEAM AT BS 328 LBL 15 TO RBL 56. REPAIRED PER EO 01-0731. (M) 2 L 7 2 4F RT A16WE 2001092400088 20010924 00088 CE 2001 9 24 CDH2001F00000 1 20010514 A 7921 636900 OIL COOLER CESSNA 340 340A 2076405 CE CONT O520 TSIO520* 17040 SO OIL SYSTEM CRACKED E CDHA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 05 151GS 2 340A0545 2187352 OVERHAULED OIL COOLER CRACKED AT LOWER MOUNTING FLANGE. REPLACEMENT OVERHAULED OIL FAILED (ONE OF THE CENTER TUBES BURS T) INFLIGHT AFTER 1.5 HOURS. ENGINE LOST 4 QUARTS IN 10 MINUTES. 1 L 7 2 3O 3 O 3A25 E8CE 2001092400089 20010924 00089 NM 2001 9 24 2001F00353 1 20010905 A 5315 FLOORBEAM BOEING 737 737400 NM FUSELAGE CORRODED B WT9M K NONE O OTHER IN INSP/MAINT 1 EA 27 933NU 25226 FOUND CORROSION ON FLOORBEAM AT BS 344 LBL 35. REPAIRED PER ER 01-0730. (M) 2 L 7 2 4F RT A16WE 2001092400090 20010924 00090 NM 2001 9 24 2001F00354 1 20010905 A 5315 FLOORBEAM BOEING 737 737400 NM FUSELAGE CORRODED A WT9M K NONE O OTHER IN INSP/MAINT 1 EA 27 933NU 25226 FOUND CORROSION ON FLOORBEAM AT BS 328 LBL 28. REPAIRED PER EO 01-0731. (M) 2 L 7 2 4F RT A16WE 2001092400091 20010924 00091 NM 2001 9 24 2001F00355 1 20010905 A 5320 STRINGER CLIP BOEING 737 737400 NM FUSELAGE CRACKED B WT9M K NONE O OTHER IN INSP/MAINT 1 EA 27 933NU 25226 FOUND CRACKED STRINGER CLIP AT BS 663.75 STRINGER 10R. REPAIRED PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2001092400092 20010924 00092 NM 2001 9 24 2001F00356 1 20010905 A 5320 SILL BOEING 737 737400 NM FUSELAGE CORRODED B WT9M K NONE O OTHER IN INSP/MAINT 1 EA 27 933NU 25229 FOUND CORROSION ON MOPSILL AT BS 960 RBL 50. REPLACED PER SRM 51-40-2. (M) 2 L 7 2 4F RT A16WE 2001092400094 20010924 00094 NM 2001 9 24 2001F00357 1 20010905 A 5311 FRAME BOEING 737 737400 NM FUSELAGE CRACKED A WT9M K NONE O OTHER IN INSP/MAINT 1 EA 27 933NU 25226 FOUND FRAME CRACKED AT BS 867 BETWEEN STRINGER 8L AND 9L. REPAIRED PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 2001092400096 20010924 00096 NM 2001 9 24 2001F00358 1 20010905 A 5311 FRAME BOEING 737 737400 NM FUSELAGE CRACKED B WT9M K NONE O OTHER IN INSP/MAINT 1 EA 27 933NU 25226 FOUND FRAME CRACKED AT BS 400 BETWEEN STRINGER 8R/9R. REPAIRED PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 2001092400097 20010924 00097 NM 2001 9 24 2001F00359 1 20010905 A 5311 FRAME BOEING 737 737400 NM FUSELAGE CRACKED B WT9M K NONE O OTHER IN INSP/MAINT 1 EA 27 933NU 25226 FOUND FRAME CRACKED AT BS 480 BETWEEN STRINGER 8L AND 9L. REPAIRED PER SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 2001092400098 20010924 00098 2001 9 24 GXPA0117 4 20010814 A 3421 CONNECTOR PIPER PA60 PA60601 7106010 NM LYC O540 TIO540* 41532 EA ARTIFICAL HORIZ MALFUNCTIONED E GXPA O OTHER O OTHER NR NOT REPORTED 1 GL 23 160GA 61002150 ARTIFICIAL HORIZON TUMBLED AND SHOWED 10 DEGREES LEFT BANK IN STRAIGHT LEVEL FLIGHT. CLEANED CANNON PLUG AND CLEARED FO R TEST FLIGHT. OPS CHECKED GOOD. TEST FLIGHT COMPLETED, FOUND OK. 1 M 7 2 3O 3 O RT A17WE E14EA 2001092400099 20010924 00099 EU 2001 9 24 HDN2001F00000 1 20010830 A 7930 L792M2002102 VALVE UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE THERMOSTAT VALVE INOPERATIVE E HDNA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 SW 03 313MS 1427 0095 BB0032 CRUSE FLIGHT, ENGINE OIL TEMPERATURE EXCEEDED RED LINE. ENGINE THROTTLE ROLLED TO 20 TO 30 PERCENT TORQUE. TEMPERATURE REMAINED ABOVE RED LINE. ENGINE SHUT DOWN (NR 1) AND PROCEEDED TO NEAREST AIRPORT. DECLARED AND EMERGENCY, LANDING OK , NO DAMAGE. 1 G 7 2 3U 3 U O H88EU E42NE 2001092400100 20010924 00100 SO 2001 9 24 2001F00360 1 20010815 A 5270 1159F501403 SWITCH GULSTM GV GULFSTREAMGV 3980116 SO DOOR OUT OF ADJ A UG8A A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 23 5102 1453 551 KLAS - AFTER LEAVING KLAS AT APPRO FL450, THE RED DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO KLAS, PASSING TH OUGHT 8000 FEET ON DESCENT. THE LIGHT EXTINGUISHED. AIRCRAFT INSPECTED AND DEFERRED PER MEL 52-1 FOR RETURN TO DTW. A DJUSTED AFT UPPER SWITCH PER GULFSTREAM MM. (M) 2 L 7 2 4F RT A12EA 2001092400102 20010924 00102 CE 2001 9 24 2001F00361 1 20010808 A 3222 67940701 STRUT CESSNA 750 750 2076810 CE NLG LOW A UG8A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 5113 1855 494 7500013 DTW - AFTER TAKEOFF AND UPON LANDING GEAR RETRACTION THE NOSE GAR FAILED TO RETRACT. NLG STRUT LOWER CHAMBER NITROGEN P RESSURE LOW. SERVICED STRUT PER CESSNA MM. (M) 2 L 7 2 4J RT T00007WI 2001092400106 20010924 00106 SW 2001 9 24 2001F00362 1 20010828 A 3710 COUPLING MOONEY M20 M20J 5870219 SW LYC O360 IO360A3D6D 41514 EA DRY AIR PUMP SHEARED B BUWA O OTHER O OTHER NR NOT REPORTED 1 EA 07 4128H 31 240642 L1935251A DRIVE COUPLING SHEARED AFTER 30.52 HOURS OPERATION SINCE NEW. THIS IS THE FOURTH COUPLING (PUMP) FAILURE OF PUMPS INSTA LLED ON THIS AIRCRAFT ENGINE. OTHERS FAILED AFTER 30.95, 63.35, 73.17 HOURS OF OPERATION. VACUUM SYSTEM TESTED FOR LEA KS AND VACUUM LINES CLEANED. NEW FILTERS INSTALLED. (M) 1 L 7 1 3O 3 O 2A3 1E10 2001092400109 20010924 00109 NE 2001 9 24 IY22001F00002 2 20010730 A 7230 BLADE CESSNA 500 500CESSNA 2076602 CE PWA JD15 JT15D1A NE HP TURBINE SEPARATED A IY2R K NONE O OTHER IN INSP/MAINT 1 SW 99 15AW 5000139 PCE7630 PCE 76307, SUSTAINED HPT BLADE SEPARATION AND RESULTED IN DOWN STREAM HOT SECTION DAMAGE. THIS SEPARATION OCCURS AT 580 .5 HOURS AFTER HOT SECTION, WHICH IS COMMON TO THE PREVIOUS FAILURES/MDRS SUBMITTED. THE GROWTH (NECKING) IS FROM .007 INCHES TO .012 INCHES. RECOMMENDATIONS: A) PERFORM GROWTH CHECK FOR THE 3028601 TURBINE BLADES AT 1750 HOURS (HSI) AND REJECT IF GROWTH IS OVER .004 INCHES. B) PLACE LIFE LIMIT OF 1750 ON 3028601 BLADES. 1 L 7 2 4F 4 F A22CE E25EA 2001092400110 20010924 00110 2001 9 24 2001F00363 4 20010816 A 2312 ANTENNA BEECH 33 35C33 1151408 CE VHF COMM CRACKED B MGOR O OTHER O OTHER NR NOT REPORTED 1 CE 09 6124V CD856 AIRCRAFT ARRIVED WITH AN ANTENNA 'FLUTTERS' SQUAWK. UPON INSPECTION OF VHF COMM ANTENNA, IT WAS NOTED THAT THE ANTENNA WAS INSTALLED WITH NO SUPPORTING DOUBLER. UPON ANTENNA REMOVAL, A 5.5 INCH RADIAL CRACK WAS DISCOVERED AROUND THE ANTEN NA BASE. THE ADJOINING STRINGER IS ALSO CRACKED. THE SKIN UNDER THE ANTENNA WAS CORRODED DUE TO NO SEALANT BEING APPLI ED TO THE ANTENNA BASE AFTER INSTALLATION. (M) 1 L 7 1 3O 3A15 2001092400112 20010924 00112 CE 2001 9 24 JUK2001F00000 1 20010823 A 3213 NAS464623 BOLT HELIO H295 H295 4300802 CE LYC O480 GO480* 41527 EA MLG SHOCK STRUT SHEARED E JUKA K NONE O OTHER IN INSP/MAINT 1 SO 33 269L 1286 NAS 464623 BOLT WHICH SECURES THE UPPER (PISTON) END OF THE 391-040-401 SHOCK STRUT TO THE MAIN LANDING GEAR LEG, FAILED . THE BOLT SHEARED ON BOTH SIDES OF THE SPHERICAL BEARING IN THE SHOCK STRUT. MECHANICS DISASSEMBLING THE LANDING GEAR NOTED THAT THE BOTH ENDS OF THE BOLT WERE STUCK IN THE MAIN LANDING GEAR AND THE SHANK PORTION OF THE BOLT WAS STUCK IN THE SPHERICAL BEARING. CAUSE OF THE FAILURE IS STILL BEING ANALYZED. 1 H 7 1 3O 3 O 1A8 E275 2001092400114 20010924 00114 SW 2001 9 24 KBMA88769 1 20010728 A 3310 76547 SWITCH BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL LIGHTS INOPERATIVE B KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 667JM 187 3444 LIGHT STAYS OFF WITH BREAKER PULLED. REMOVED AND REPLACED WITH NEW SWITCH. 1 G 7 1 3U 3 U H2SW E4CE 2001092400125 20010924 00125 SW 2001 9 24 2001F00324 1 20010823 A 2823 54009533 CONTROL CABLE GULSTM 690TP 690A 0141722 SW GARRTT TPE331 TPE3315251K NM LT ENGINE FAILED B MV5R O OTHER O OTHER NR NOT REPORTED 1 GL 11 744JD 6875 11135 P06054 LEFT ENGINE CONTROL CABLE FAILED TO THE PORTION THAT CONTROLLED THE MANUAL FUEL SHUTOFF VALVE. FAILURE WAS LOCATED AT T HE AREA THAT THE FUEL AND PROPELLER MANUAL STOP AND FEATHER CABLE ARE COMBINED INTO ONE CONTROL. (M) 1 H 7 2 3T 4 T 2A4 E2WE 2001092400129 20010924 00129 CE 2001 9 24 2001F00330 1 20010727 A 2910 NAS16124 O-RING CESSNA 750 750 2076810 CE HYDRAULIC SYS DAMAGED A UG8A K NONE K FLUID LOSS IN INSP/MAINT 1 GL 23 5116 7500019 IND - PILOT WALKAROUND PRIOR TO DEPARTURE, TWO HYD PUDDLES UNDER TAIL OF A/C. 'A' HYD SYSTEM INDICATES 25 PERCENT. APP EARS TO BE COMING FROM ELEVATOR. REPLACED O-RING UNDER HYD FITTING (PRESSURE) ON RIGHT INBOARD PCU. (M) 2 L 7 2 4J RT T00007WI 2001092400133 20010924 00133 NM 2001 9 24 PCAA0109113 1 20010920 A 2430 23088002B GENERATOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LEFT FAILED A PCAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 13 845EX 34166 220 344 121152 PWM-LGA FLIGHT#3738. CREW REPORTED WHILE AT 6,000 FT OVER HVN AIRPORT #2 ENGINE D.C. GENERATOR HOT LIGHT ILLUMINATED. #2 GENERATOR TURNED OFF, THEN NUMBER TWO ENGINE EXPERIENCED TORQUE AND PROP VIBRATION. THE NUMBER TWO ENGINE SHUT DOWN AND SECURED. FLIGHT DIVERTED TO HVN, SINGLE ENGINE LANDED WITHOUT FURTHER INCIDENCE. MAINTENANCE INSPECTED #2 STARTER/GENER ATOR #2 A.C. GENERATOR.ALSO CHECKED #2 ENGINE COMPRESSOR AND PROPELLER FOR FREEDOM OF MOVEMENT. MAINTENANCE ALSO CHECKED THE #1 STARTER/GENERATOR AND FOUND IT INOPERATIVE. #1 STARTER GENERATOR REPLACED. DURING GROUND RUN OPERATIONAL CHECK G OOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2001092400135 20010924 00135 NM 2001 9 24 2001F00334 1 20010905 A 5311 FRAME BOEING 737 737400 NM FUSELAGE CORRODED B WT9M K NONE O OTHER IN INSP/MAINT 1 EA 27 933NU 25226 FOUND CORROSION ON FRAME OUT OF LIMITS, B 7270 STRINGER 25L. REPAIRED PER SRM 51-40-02, 51-00-07, 51-70-11. (M) 2 L 7 2 4F RT A16WE 2001092400137 20010924 00137 WP 2001 9 24 IXXA0100051O 1 20010920 A 3210 57712063216 LINE DOUG DC8 DC862 3021970 WP LT GEAR DEFECTIVE A IXXA O OTHER K FLUID LOSS CR CRUISE 1 SW 11 31CX 73365 40 45911 DURING CRUISE FROM AVB TO RMS, THE FLIGHT CREW NOTICED THAT THE MAIN HYDRAULIC QUANTITY SYSTEM WAS DECLINEING. THE FLIGH T CREW FOLLOWED COMPANY PROCEDURES AND CONTINUED TO RMS FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT LO CATE A DEFECTIVE SUPPLY LINE ON THE LEFT MAIN GEAR BOGIE TRIM CYCLINER. MAINTENANCE REPLACED THE SUPPLY AND PERFORM AND OPERATIONAL CHECK IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2001092400139 20010924 00139 SO 2001 9 24 COMA0110143 1 20010922 A 7710 SEDL0C2R INDICATOR EMB 120 EMB120RT SO COCKPIT FAULTY A COMA D RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 463CA 22508 120267 FLIGHT #5017. DURING TAKE OFF AT MCO THE LEFT ENGINE DIGITAL TORQUE INDICATION WAS INTERMITTENT, TAKE OFF WAS ABORTED AN D REUTRNED TO THE GATE.REPLACED THE LEFT ENGINE TORQUE GAUGE. 2 L 7 2 4T RT A31SO 2001092400146 20010924 00146 NM 2001 9 24 UPS01236808 1 20010828 A 5320 WEB BOEING 727 727172C 1384058 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 916UP 19808 INSPECTION TYPE:C SUSPECT CRACK IN VERTICAL WEB UPPER LIGHTNING HOLE IN THE RT LWR TORQUE BOX AT BS 1268 APPROX. AREA R EPAIRED IAW SRM 51-40-02. 2 L 7 3 4F A3WE 2001092400149 20010924 00149 NM 2001 9 24 UPS01236811 1 20010828 A 5711 SPAR CAP BOEING 727 727172C 1384058 NM LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 916UP 19808 INSPECTION TYPE:C LT WING ON INSPECTION OF LEADING EDGE TO FRONT SPAR JOINT, CORROSION FOUND IN UPPER CAP OF SPAR AT FR ONT SPAR STN189. CORROSION REMOVED IAW SRM , HFEC AREA AND NO DEFECTS FOUND, CORROSION BLEND FOUND TO BE OUTSIDE LIMITS , UPPER FRONT SPAR REPAIRED IAW SRM 57-10-6 FIG2 AREA LEAK CHECKED SATIS. 2 L 7 3 4F A3WE 2001092400152 20010924 00152 EA 2001 9 24 COMA0160737 1 20010923 A 2751 860D10018ABC FCU CNDAIR CL600 CL6002B19 EA AVIONICS BAY FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 965CA 10272 7131 FLIGHT #5073. DURING APPROACH INTO TLH RECEIVED A FLAP FAIL CAUTION MESSAGE WITH FLAPS AT ZERO DEGREES.REPLACED THE FLAP ELECTRONIC CONTROL UNIT. 2 L 7 2 4F RT A21EA 2001092400154 20010924 00154 NM 2001 9 24 UPS01236812 1 20010829 A 5230 HINGE BOEING 727 727172C 1384058 NM CARGO DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 916UP 19808 INSPECTION TYPE:C CORRODED HINGES ON MAIN CARGO DOOR. CORRODED HINGE SECTIONS REPLACED AS REQUIRED IAW OHM 20-50-01 & SM RO EO 2001-039-004 & UPS ENGINEERING FILE NO B727-5330-15313-A. 2 L 7 3 4F A3WE 2001092400156 20010924 00156 NM 2001 9 24 UPS01236823 1 20010915 A 3350 LIGHT BOEING 727 72751C 1384015 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:IN CABIN ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT IAW B727 MM 33- 50-101 OPS CHECKS GOOD. 2 L 7 3 4F A3WE 2001092400158 20010924 00158 EA 2001 9 24 COMA0160738 1 20010923 A 2751 865D1007 PCU CNDAIR CL600 CL6002B19 EA CENTER WING FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 965CA 12280 7131 FLIGHT #5073. DURING APPROACH INTO TLH RECEIVED A FLAP FAIL CAUTION MESSAGE WITH FLAPS AT ZERO DEGREES.REPLACED THE POW ER DRIVE UNIT. 2 L 7 2 4F RT A21EA 2001092400161 20010924 00161 NM 2001 9 24 UPS01236824 1 20010916 A 3230 CONTROL CABLE BOEING 727 72727C 138400J NM NLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 REF SEG CHECK NR 7 NOSE GEAR MANUAL EXTENSION CABLES DRY WITH EVIDENCE OF SURFACE CORROSION. CLEANED AND LUBRICATED AS R EQUIRED. OK FOR SERVICE PER MM 12-20-01. 2 L 7 3 4F A3WE 2001092400164 20010924 00164 NM 2001 9 24 UPS01236825 1 20010916 A 3231 CONTROL CABLE BOEING 727 72727C 138400J NM NLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE:IN REF SEG CHECK NR 7 NWW DOOR ACTUATION CABLES DRY WITH EVIDENCE OF SURFACE CORROSION. CLEANED & LUBRIC ATED AS REQUIRED PER MM 12-20-01. 2 L 7 3 4F A3WE 2001092400165 20010924 00165 EU 2001 9 24 MALA010719 1 20010914 A 5310 7253722001 ANGLE SAAB SF340 340B 7860101 EU CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438XJ 340B438 During 4K-Inspcection found frome Top Flange and Angle corroded on bottom Frame at Sta 258. Maintenance replaced corrod ed Angle PN 7253722-001 and performed repair to Top Flange IAW EO S53102. 2 L 7 2 4T RT A52EU 2001092400166 20010924 00166 EU 2001 9 24 MALA010720 1 20010914 A 5310 7253799383 SEAT TRACK SAAB SF340 340B 7860101 EU CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438XJ 340B438 During 4K-check in CWA, found LH Center Aisle seat LBL 18.3 corroded. Mx Performed Repair from Sta 297 to 349 IAW EO S53 060. Seat Track PN 7253799-383, Slice joint PN 7253799-379. 2 L 7 2 4T RT A52EU 2001092400167 20010924 00167 EU 2001 9 24 MALA010721 1 20010918 A 3020 44730501 CONTROL BOX SAAB SF340 340B 7860101 EU DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 422XJ 340B422 During Flight #3398 out of DTW, RH Engine Intake light cycles. Air Turnback to DTW. Maintenance T/S Intake Heat system , found De-ice Controller bad. Removed and replaced De-ice Controller box PN 44730-501, SN/off A00581, SN/on A00561. A ll check good IAW SF340 MM 30-20-00. 2 L 7 2 4T RT A52EU 2001092400170 20010924 00170 NM 2001 9 24 UPS01236826 1 20010916 A 5510 HINGE PIN BOEING 727 7271A7C 13840X2 NM HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE:IN FOUND SURFACE CORROSION ON BOTH LT AND RT HORIZONTAL STAB HINGE PIN NUTS. PER EO B7275105166 APPX D M UST BE COMPLIED WITH PER EO B727-5510-1566-B, CORROSION SHOULD ONLY BE NOTED ON PIN THREADED END AND REMOVED SURFACE COR ROSION WITH MECHANICAL NON ABRASIVE INSTRUMENT. OK FOR SERVICE. 2 L 7 3 4F A3WE 2001092400176 20010924 00176 SO 2001 9 24 MHJ2001F00000 2 20010820 A 8500 TSIO520E ENGINE CESSNA 401 401 207590C CE CONT O520 TSIO520E 17040 SO LEFT MALFUNCTIONED A MHJA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SW 05 4021Q 1322 4010121 275311 LEFT ENGINE HAD A FUEL FLOW PROBLEM. ENGINE QUIT ON TAKE-OFF WITHOUT INCIDENT. MORE INFORMATION TO FOLLOW. WHEN ACTUA L PROBLEM IS FOUND. 1 L 7 2 3O 3 O A7CE E8CE 2001092400177 20010924 00177 SW 2001 9 24 MV52001F00000 1 20010810 A 3210 73005821 ANGLE GULSTM 690TP 690B 7630516 SW LEFT GEAR CRACKED E MV5R K NONE O OTHER IN INSP/MAINT 1 GL 11 690SM 7278 11337 ANGLE LOCATED AT LEFT MAIN LANDING GEAR TO WING ATTACH AREA CRACKED AT INBOARD SIDE. CRACK EXTENDED ONE INCH FROM AFT P ORTION OF WING AREA FORWARD. 1 H 7 2 3T 2A4 2001092400181 20010924 00181 NM 2001 9 24 UPS01436711 1 20010826 A 3350 S1356B37 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:N/A EMERGENCY LIGHT INOP AT STA 600 MAIN DECK RT SIDE. REPLACED EMERGENCY LIGHT ASSY AT STA 600 RH MAIN DECK, CKS GOOD. 2 L 7 4 4F A20WE 2001092400182 20010924 00182 NM 2001 9 24 UPS01436716 1 20010826 A 3350 S1356837 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:N/A EMERGENCY LIGHT AT STAIR WELL IS INOP. R&R EMERG LT ASSY AT TOP OF STAIRWELL TO UPPER DECK. 2 L 7 4 4F A20WE 2001092400183 20010924 00183 EA 2001 9 24 COMA0160739 1 20010921 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 786CA 7333 FLIGHT #5474. DURING INSPECTION FOUND THE FORWARD SECTION OF THE FLOOR EMERGENCY LIGHTING TO BE INOPERATIVE.DISCONNECTE D, CLEANED AND RE-CONNECTED THE ELECTRICAL CONNECTOR FOR THE FORWARD SECTION OF FLOOR EMERGENCY LIGHTING. 2 L 7 2 4F RT A21EA 2001092400185 20010924 00185 NM 2001 9 24 UPS01436718 1 20010826 A 3350 S1356B37 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:N/A EMERG LIGHT INOP STA 2350 RT SIDE MAIN DECK. REPLACED EMERG LIGHT ASSY. 2 L 7 4 4F A20WE 2001092400186 20010924 00186 EA 2001 9 24 COMA0160740 1 20010920 A 2760 4916405 COMPUTER CNDAIR CL600 CL6002B19 EA AVIONICS BAY FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 815CA 2577 7397 FLIGHT #5449. DURING TAXI OUT RECEIVED A SPOILERON FAULT MESSAGE, AIRCRAFT RETURNED TO THE GATE.REPLACED THE SPOILERON ELECTRONIC CONTROL UNIT. 2 L 7 2 4F RT A21EA 2001092400187 20010924 00187 NM 2001 9 24 UPS01436719 1 20010825 A 3350 S3156B37 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:N/A EMERG LIGHT INOP STA 2350 RT SIDE MAIN DECK. REPLACED EMERG LIGHT ASSY. 2 L 7 4 4F A20WE 2001092400188 20010924 00188 NM 2001 9 24 UPS01436734 1 20010828 A 3350 BATTERY BOEING 747 747200 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:N/A PAX CABIN AFT EMERGENCY LIGHTS INOP. R&R PAX AFT CABIN EMERGENCY LIGHT BATTERY. GROUND CK GOOD REF 3 3-51-04. 2 L 7 4 4F RT A20WE 2001092400189 20010924 00189 NM 2001 9 24 UPS01436735 1 20010828 A 3350 S135837 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:IN EMERGENCY LIGHT AT STAIR WELL IS INOP. REPLACED EMERGENCY LIGHT ASSY AT TOP OF STAIRWELL TO UPPER DEC K. CKS GOOD. 2 L 7 4 4F A20WE 2001092400190 20010924 00190 NM 2001 9 24 UPS01436736 1 20010827 A 3350 S1356837 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:IN UPPER DECK RT CENTER EMERGENCY LIGHT IS INOP. REPLACED EMERGENCY LIGHT ASSY UPPER DECK RT CENTER CKS GOOD. 2 L 7 4 4F A20WE 2001092400191 20010924 00191 NM 2001 9 24 UPS01436737 1 20010827 A 3350 S1356B37 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:N/A EMERGENCY LIGHT INOP AT STA 600 MAIN DECK RT SIDE. REPLACED EMERGENCY LIGHT ASSY AT STA 600 RT MAIN DECK. CKS GOOD. 2 L 7 4 4F A20WE 2001092400192 20010924 00192 NM 2001 9 24 UPS01436738 1 20010827 A 3350 S1356B37 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:IN EMERGENCY LIGHT INOP AT STA 2650 ON RT SIDE MAIN DECK. REPLACED EMERGENCY LIGHT ASSY AT STA 2350 RT C KS GOOD. 2 L 7 4 4F A20WE 2001092400193 20010924 00193 NM 2001 9 24 UPS01436739 1 20010827 A 3350 S1356B37 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:IN EMERGENCY LIGHT INOP AT STA 350 ON RT SIDE MAIN DECK. REPLACED EMERGENCY LIGHT ASSY AT STA 2350 RT. 2 L 7 4 4F A20WE 2001092400195 20010924 00195 NM 2001 9 24 UPS01436776 1 20010904 A 3397 WIRE BOEING 747 747200 1384847 NM CABIN LOOSE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:PFLT LIGHTED EMERGENCY EXIT SIGN, LOCATED ON BACK SIDE OF P6 ENST TO UPPER DECK EMERGENCY SLIDE, HAS WIR ES PULLED FROM CONNECTOR. SYSTEM DEACTIVATED, WIRE AND CONNECTORS CAPPED AND STOWED, "DEACT" PLACARD INSTALLED PER EO B7 47-3350-15296. 2 L 7 4 4F RT A20WE 2001092400196 20010924 00196 NM 2001 9 24 UPS01436834 1 20010907 A 2520 PANEL BOEING 747 747121 1384871 NM CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C RT BS 2230 FIVE CRACKS FOUND AT REVEAL PANEL BETWEEN S24R TO FLOOR LEVEL AS MARKED. REVEAL PANEL REPAI RED AT CABIN BS 2231 STR 24 TO 26R PER HX RS R53-62-34682. 2 L 7 4 4F A20WE 2001092400197 20010924 00197 NM 2001 9 24 UPS01436835 1 20010906 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C RT SIDE BS 2231, ONE EA FASTENER HOLE CRACK REVEALED AT STR 25R ON CHORD AREA RUNNING FWD LOWER THRU T HICKNESS DETAIL PLEASE REFER ATT DRAWING. THE CHORD AREA REPAIRED AS PER RS R53-62-34682. 2 L 7 4 4F A20WE 2001092400198 20010924 00198 NM 2001 9 24 UPS01436836 1 20010908 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C FWD CARGO, BS 600 STR 37L STR 38L FUSELAGE FRAME FOUND CRACKED. FRAME REPAIRED PER HX RS R53-22-34683 . 2 L 7 4 4F A20WE 2001092400199 20010924 00199 NM 2001 9 24 UPS01436840 1 20010908 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C AFT CARGO, BS 1540 RT STR 39 - STR 40 FUSELAGE FRAME FOUND CRACKED. AFT CARGO COMPT BS 1540 RH S39R - S40R CRACKED FRAME REPAIRED AS PER SRM 53-10-04 FIG 69. 2 L 7 4 4F A20WE 2001100200078 20011002 00078 NM 2001 10 2 UPS01436842 1 20010921 A 5753 FITTING BOEING 747 747SR46 NM T/E FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:A LT INBOARD FORE FLAP CENTER SUPPORT FITTING HAS A CRACK AROUND IT. REPLACED LT INBOARD FORE FLAP PER M M 27-51-02. 2 L 7 4 4F A20WE 2001092400200 20010924 00200 NM 2001 9 24 UPS01536829 1 20010913 A 5347 SEAT TRACK BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 403UP 23725 INSPECTION TYPE:C CORROSION ON SEAT TRACK FLANGES STA-1080-1180. RBL 45, WL 208. REMOVED CORROSION FROM SEAT TRACK FLANG ES, FROM BS-1080 TO 1180 RBL 45 WL 208, WITH MATERIAL LOSS OUT OF LIMITS IAW UPS SRM 53-00-52. REMOVED SEAT TRACK FROM B S 1080-1180 RBL 45 WL 208 AND INSTALLED NEW FABRICATED TRACK PER SRM 51-40-08 AND SRM 51-40-02. 2 L 7 2 4F RT A2NM 2001092400201 20010924 00201 NM 2001 9 24 UPS01536841 1 20010924 A 3350 487190 CONNECTOR BOEING 757 75724APF 1384969 NM CABIN DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 469UP 25485 INSPECTION TYPE:N/A ELECTRICAL CONNECTOR ON EMERGENCY LIGHT POWER SUPPLY CAME APART. REPLACED SPLICE AND PIN. 2 L 7 2 4F RT A2NM 2001092400202 20010924 00202 NM 2001 9 24 UPS01636828 1 20010918 A 3610 VALVE BOEING 767 767300 1385204 NM BLEED AIR MALFUNCTIONED A IPXA H DEACTIVATE SYST/CIRCUITS O OTHER TX TAXI/GRND HDL 1 SO 01 306UP 27759 INSPECTION TYPE:ETOP LEFT DUCT PRESSURE FLUCTUATES W/ENGINE RUNNING AND BLEED SWITCH ON. AFTER TAKEOFF PRESSURE DROPPED BELOW 20 PSI & ROSE ABOVE 60 PSI. TURNED LEFT PACK OFF AND LEFT ENG BLEED SWITCH OFF. DEF LEFT ENG PRSOV PER MEL 36-11-1 -1. C/W DMP 36-11-1. PER FIM 36-10-00 FIG 109 FAN AIR MODULATING VALVE DEF. R&R FAV PER 36-11-16. PERFORMED AIR SUPPLY BITE CHECK & NO FAULTS. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2001092500229 20010925 00229 NE 2001 9 25 RAIA00109008 2 20010920 A 7421 CH34406 IGNITER AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE LT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 423TE 119 121372 STL-LEFT ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE IGNITORS. 2 H 7 2 4T 4 T RT A53EU E20NE 2001092400204 20010924 00204 WP 2001 9 24 UPS01836700 1 20010819 A 5320 STIFFENER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 STA -99 LT CUSP STIFFENER IS CORRODED BEYOND LIMITS. REPAIRED STIFFENER IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001092400205 20010924 00205 WP 2001 9 24 UPS01836701 1 20010808 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 LEFT WING L/E SKIN IS CRACKED AT XW 485. REPAIRED SKIN IAW SRM 57-2-1 FIG 2H. 2 L 7 4 4F RT 4A25 2001092400206 20010924 00206 WP 2001 9 24 UPS01836702 1 20010808 A 5720 97532937 ANGLE DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 LEFT WING L/E VERTICAL ATTACH ANGLE IS CRACKED AT XS 250. REMOVED,FABRICATED,AND REPLACED ANGLE IAW DWG 9753293,AND SRM 51-3-0,51-1-20D. 2 L 7 4 4F RT 4A25 2001092400207 20010924 00207 WP 2001 9 24 UPS01836703 1 20010809 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 STA 1600 AT LONG 20L-21L FUSELAGE SKIN AT FWD LOWER CORNER. REPAIRED SKIN IAW SRM 53-2-0 FIG 18. 2 L 7 4 4F RT 4A25 2001092400208 20010924 00208 WP 2001 9 24 UPS01836704 1 20010808 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 LEFT WING L/E RIB IS CRACKED AT XFS 224. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001092400209 20010924 00209 WP 2001 9 24 UPS01836705 1 20010811 A 5320 37558451N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 STA 1200 LONG 35R-36 BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DW G 3755845, AND SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 2001092400210 20010924 00210 WP 2001 9 24 UPS01836706 1 20010807 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 LEFT IB SLOT VANE HAS SCREWS PULLING THRU SKIN AT XILD 7095. REPAIRED SKIN IAW SRM 57-2-1 FIG 2H. 2 L 7 4 4F RT 4A25 2001092400211 20010924 00211 WP 2001 9 24 UPS01836712 1 20010808 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 RIGHT WING L/E RIB IS CRACKED AT XFS 335.25. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001092400212 20010924 00212 WP 2001 9 24 UPS01836713 1 20010810 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 STA 1030-1080 SEAT TRACK IS CORRODED BEYOND LIMITS. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A. 2 L 7 4 4F RT 4A25 2001092400213 20010924 00213 2001 9 24 RAIA00109009 4 20010921 A 2300 VF10347 ANTENNA JETAIR JETSTM JETSTM4101 1500501 EU BROKEN A RAIA K NONE O OTHER CL CLIMB 1 CE 03 557HK 12620 41074 5388-RIC-#1 COMMUNICATIONS SYSTEM INOPERATIVE AFTER BIRD STRIKE. MAINTENANCE REMOVED AND REPLACED #1 COM ANTENNA AND FOU ND NO DAMAGE TO FUSELAGE. 2 L 7 2 4T RT A41NM 2001092400214 20010924 00214 NM 2001 9 24 AWXA200100453 1 20010813 A 5320 65465318 SHEAR TIE BOEING 737 737277 1384570 NM BS 965, RBL 20 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 MCN - C-21 CK - "C" - FUSELAGE SKIN BULGE AND CUPPED FASTENERS IN SKIN AT BS 977, BETWEEN STR 23R TO 24R. MAINTENANCE RE MOVER FASTENERS IN SKIN, NO CORROSION FOUND ON FUSELAGE SKIN, HOWEVER FOUND SHEAR TIE CORRODED BS 965, RBL 20. REMOVED A ND REPLACED SHEAR TIE BS 965, RBL 20 IAW B737 SRM 51-30-2. 2 L 7 2 4F RT A16WE 2001092400215 20010924 00215 NM 2001 9 24 AWXA200100455 1 20010824 A 5313 6545866600 STRINGER BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 MCN - C21 CK - "C" - WHILE INVESTIGATING POSSIBLE CORROSION AROUND FASTENERS AT BS 727 + 17, STR 27L TO 27R, FOUND A 3" CRACK IN STR 27R. NOTE; NO CORROSION WAS FOUND. MAINTENANCE REMOVED CRACKED SECTION OF STR 27R AND INSTALLED REPAIR IAW B737 SRM 53-10-6. 2 L 7 2 4F RT A16WE 2001092500005 20010925 00005 EA 2001 9 25 CEC2001F00000 2 20010802 A 7322 30804 FLOAT PRECISION PIPER PA28 PA28140 7102802 SO LYC O320 O320* 41508 EA CARBURATOR FAILED A CECA K NONE O OTHER IN INSP/MAINT 1 EA 05 6139J 1000 BL73881 287625222 FLOAT SUNK. 1000HRS PN30804 -AIRCRAFT WOULD QUIT ON ROLL OUT. THESE ARE MADE OF PLASTIC. THE FLOAT FILLS WITH FUEL D UE TO THE GLUE FAILURE. 1 L 7 1 3O 3 O 2A13 E274 2001092500006 20010925 00006 EU 2001 9 25 KBM2001F00000 1 20010916 A 7921 100FU01050 FUSE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE OIL COOLER FAN INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 115SH 299 3141 OIL COOLER FAN INOPERATIVE. INSTALLED SERVICEABLE CIRCUIT BREAKER. 1 G 7 1 3U 3 U H9EU E19EU 2001092500007 20010925 00007 NE 2001 9 25 KBMA88787 2 20010916 A 7200 ENGINE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE NACELLE MAKING METAL E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 115SH 2619 3141 HIGH IRON COUNT RECEIVED FROM OIL ANALYSIS. REMOVED AND REPLACED WITH RENTAL ENGINE. 1 G 7 1 3U 3 U H9EU E19EU 2001092500008 20010925 00008 SW 2001 9 25 KBMA88794 1 20010907 A 2436 VOLT REGULATOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ELECTRICAL MALFUNCTIONED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 667JM 3444 VOLTAGE REGULATOR MAX ADJUSTMENT IS 27.5 VOLTS. REMOVED AND REPLACED SERVICEABLE VOLTAGE REGULATOR. 1 G 7 1 3U 3 U H2SW E4CE 2001092500009 20010925 00009 EU 2001 9 25 KBMA88795 1 20010916 A 7921 100FU01050 FUSE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE OIL COOLER FAN INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 115SH 2998 3141 OIL COOLER FAN INOPERATIVE, INSTALLED SERVICEABLE CIRCUIT BREAKER. 1 G 7 1 3U 3 U H9EU E19EU 2001092500010 20010925 00010 2001 9 25 KBMA88796 4 20010914 A 2312 KX155 SWITCH BELL 206 206B 1181511 SW LYC O320 O320* 41508 EA VHF COMM FAILED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 73DP 11654 2513 RADIO SWITCH DOES NOT WORK. INSTALLED SERVICEABLE UNIT. 1 G 7 1 3U 3 O H2SW E274 2001092500011 20010925 00011 EU 2001 9 25 KBMA88797 1 20010917 A 7931 350A67402301 HARNESS SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE OIL PRESS IND BROKEN E KBMA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 19 115SH 3002 3141 OIL PRESSURE GUAGE READS HIGH AND LOW. REPAIRED BROKEN WIRE ON OIL PRESSURE HARNESS. 1 G 7 1 3U 3 U H9EU E19EU 2001092500012 20010925 00012 EU 2001 9 25 KBMA88798 1 20010917 A 6520 350A33215300 BEARING SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 230SH 714 2337 TEETER BEARINGS WORN, INSTALLED NEW TEETER BEARINGS. 1 G 7 1 3U 3 U NC H9EU E19EU 2001092500013 20010925 00013 EU 2001 9 25 KBMA88800 1 20010916 A 7921 95092 MOTOR SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE OIL COOLER FAN INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 115SH 2998 3141 OIL COOLER FAN INOPERATIVE, INSTALLED SERVICEABLE FAN MOTOR. 1 G 7 1 3U 3 U H9EU E19EU 2001092500014 20010925 00014 EU 2001 9 25 OLJ2001F00002 1 20010828 A 2560 E428K PUMP AEROSP AS365 AS365N2 8680815 EU TMECA ARRIEL ARRIEL1C 60030 NE MEDICAL SYSTEM MALFUNCTIONED A OLJA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 13 291LL 6402 12088 PILOT DETECTED AN ODOR OF SMOKE IN CABIN OF AIRCRAFT AND PERFORMED A PRECAUTIONARY LANDING. MAINTENANCE WAS DISPATCHED TO AIRCRAFT. A MEDICAL PUMP WAS FOUND TO BE THE ORIGIN OF THE SMOKE. THE SYSTEM WAS DE-ACTIVATED AND THE DISCREPANCY W AS DEFERED TOTHE MEL. PUMP WAS REMOVED AND REPLACED AFTER RETURN TO HOME BASE OF OPERATION. 1 G 7 2 3U 3 U RT H10EU E19EU 2001092500016 20010925 00016 SW 2001 9 25 QJ5R20017 1 20010716 A 5302 VTF030800 SPAR BELL BELL 204 UH1E 1181401 SW LYC T53 T53* 41549 NE TAILBOOM MISINSTALLED B QJ5R K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 05 137US 151874 DURING MODIFICATION OF THE TAIL BOOM VERTICAL FIN SPAR USING SPAR KIT, THE INSTALLER IMPROPERLY INSTALLED THE HI LOC FAS TNERS WHERE THE 90 DEGREE GEARBOX CASTING ATTACHES TO SIDE RAILS OF SPAR CAPS. OPPOSITE OF STC INSTALLATION INSTRUCTION S, THE HI LOC COLLARS WERE INSTALLED IB AND HAD MADE CONTACT WITH TAIL ROTOR PITCH CHANGE CHAIN. THE PITCH CHANGE CHAIN WAS WORN WHICH ALLOWED IT TO MAKE CONTACT WITH END OF ONE HI LOC PIN AND COLLAR. A NEW CHAIN WAS INSTALLED AND CLEARA NCE EXISTED BETWEEN THE PIN AND CHAIN AGAIN. AS THE NEW CHAIN WEARS IT MAY CONTACT AGAIN. GHT WAS NOTIFIED OF PROBLEM AND STATED THEY WILL ISSUE BULLETIN. 1 G 7 1 4U 4 U EXPA1G71 E1EA 2001092500018 20010925 00018 EU 2001 9 25 R7MR33349 1 20010610 A 7600 70BMB01010 ECU SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL2B NE ENGINE SURGES E R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 52281 728 3249 22103 ENGINE SURGING 1 PERCENT TO 5 PERCENT DURING NORMAL CRUISE FLIGHT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E00054EN 2001092500019 20010925 00019 NE 2001 9 25 R7MR33363 2 20010602 A 7230 0292005340 COMPRESSOR SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE ENGINE SEIZED E R7MR K NONE O OTHER TX TAXI/GRND HDL 1 NM 07 52281 762 3249 22103 AFTER ENGINE SHUT DOWN, THEN 10 MINUTES LATER NR 1 COMPRESSOR WOULD NOT TURN. SUSPECT COMPRESSOR SIEZED DUE TO EXCESS C ARBON BUILD-UP. REPLACED WITH RENTAL ENGINE CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E00054EN 2001092500020 20010925 00020 EU 2001 9 25 R7MR33364 1 20010109 A 7712 0177987030 CONTROL UNIT SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE TORQUE INOPERATIVE E R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 52281 541 3249 22093 UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E00054EN 2001092500021 20010925 00021 2001 9 25 COMA0160741 4 20010920 A 3420 6229336400 COMPUTER CNDAIR CL600 CL6002B19 EA AVIONICS BAY FAULTY A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 962CA 9149 7123 FLIGHT #5510. DURING CLIMB-OUT OF CVG THE #2 ATTITUDE AND HEADING REFERENCE INDICATION FAILED, AIRCRAFT RETURNED TO THE FIELD.REPLACED THE #2 ATTITUDE AND HEADING REFERENCE SYSTEM (AHC-85E). 2 L 7 2 4F RT A21EA 2001092500022 20010925 00022 EA 2001 9 25 COMA0160742 1 20010920 A 7930 4059T40P02 SEAL CNDAIR CL600 CL6002B19 EA A COMA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SO 01 957CA 7109 FLIGHT #6080. DURING CLIMB-OUT OF JAX RECEIVED A RIGHT ENGINE OIL PRESSURE INDICATION WARNING, AIRCRAFT RETURNED TO THE FIELD.REPLACED THE RIGHT ENGINE #7 CARBON SEAL. 2 L 7 2 4F RT A21EA 2001092500024 20010925 00024 EA 2001 9 25 COMA0160743 1 20010917 A 5300 60034017351 ANGLE CNDAIR CL600 CL6002B19 EA F.S.280.00 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 969CA 11964 7141 THE FORWARD J ANGLE AT F.S. 280.00 BETWEEN LBL9 AND RBL9 IS CORRODED.REMOVED AND REPLACED FORWARD J ANGLE AT F.S.280.00 BETWEEN LBL9 AND RBL9 WITH NEW P/N 6000-34017-351 ANGLE I/A/W WVAC EO 601R-53-2718. 2 L 7 2 4F RT A21EA 2001092500025 20010925 00025 CE 2001 9 25 RJW2001F00000 1 20010731 A 5753 12210107 FLAP TRACK CESSNA 206 U206G 2073356 CE CONT O520 IO520* 17032 SO TE FLAPS LOOSE B RJWR K NONE O OTHER IN INSP/MAINT 1 GL 15 932DB 4604 U20605397 FLAP TRACK HAS WORKED LOOSE. INDICATIONS ARE: CRACKED FLAP COVER SKIN AND COVE SKIN AND COVE SKIN ATTACH BRACKETS. BO TH OF THESE ARE INDICATION OF LOOSE FLAP TRACK. REPAIRS WERE NOTED IN BOTH OF THESE AREAS BUT FLAP TRACKS WERE NOT REPA IRED. CRACKED FLAP COVE SKINS AND ATTACH BRACKEST IS CAUSED BY LOOSE FLAP TRACKS. 1 H 7 1 3O 3 O A4CE E5CE 2001092500026 20010925 00026 EA 2001 9 25 COMA0160744 1 20010917 A 5300 60034017373 ANGLE CNDAIR CL600 CL6002B19 EA F.S.280.00 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 969CA 11964 7141 THE VERTICAL J ANGLE CLIP LOCATED INSIDE OF CBP1 AT LBL9 L/II SIDE WAS FOUND CRACKED.REMOVED AND REPLACED VERTICAL J ANG LE CLIP INSIDE OF DBPJ WITH NEW ANGLE P/N 600-34017-723S I/A/W WVAC EO 601R-53-2720. 2 L 7 2 4F RT A21EA 2001092500027 20010925 00027 WP 2001 9 25 ABXA010495 1 20010915 A 5330 SKIN DOUG DC8 DC861 3021952 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 850AX 45894 CORROSION WAS FOUND AT FUSELAGE STATION 300, LONGERON 33R THRU 34R ON WALK AROUND INSPECTION. MAINTENANCE REPAIRED THE A REA IAW ABX REA D853-36700MR. OPEN: CORRECTIVE ACTION IS NOT COMPLETE. 2 L 7 4 4F 4A25 2001092500028 20010925 00028 WP 2001 9 25 ABXA010496 1 20010919 A 3260 7000010101 SWITCH DOUG DC9 DC932 3022066 WP NG WELL DEFECTIVE A ABXA K NONE O OTHER CL CLIMB 1 GL 23 980AX 47176 DURING DEPARTURE WHEN LANDING GEAR WAS RETRACTED, A RED NOSE GEAR UNSAFE LIGHT ILLUMINATED. THE LANDING GEAR WAS RECYCLE D AND THE GEAR RETRACTED NORMALLY. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR UPLOCK AND DOWN LOCK SWITCHES. OPERA TIONAL CHECKS WERE COMPLETED IAW DC-9 MM 32-60-01, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001092500029 20010925 00029 WP 2001 9 25 ABXA010497 1 20010920 A 3260 7000010101 SWITCH DOUG DC9 DC931 3022065 WP NG WELL DEFECTIVE A ABXA K NONE O OTHER CR CRUISE 1 GL 23 941AX 47419 A NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE INSPECTED AND ADJUSTED THE NOSE LANDING GEAR DOWN LO CK SENSOR AND REPLACED THE LEFT FORWARD NOSE GEAR DOOR ACTUATOR DUE TO A NONE ADJUSTABLE EYEBOLT. ADJUSTMENT AND TEST PR OCEDURES WERE COMPLETED IAW DC-9 MM 32-60-01 AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001092500030 20010925 00030 EA 2001 9 25 COMA0160745 1 20010923 A 2780 601R1430353S VANE CNDAIR CL600 CL6002B19 EA R/H INBOARD FLAP CHAFED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 969CA 11965 7141 R/H INBOARD FLAP INBOARD VANE CAP IS CHAFED BEYOND LIMITS PER S/B 601R-57-022.REMOVED R/H INBOARD FLAP VANE CAP AND INST ALLED NEW SERVICEABLE CAP P/N 601R4303S-54S I/A/W AERODESIGN ENGINEERING REPORT NUMBER 1286-1 REV A. 2 L 7 2 4F RT A21EA 2001092500031 20010925 00031 EA 2001 9 25 COMA0160746 1 20010917 A 5300 601R3866949 DOUBLER CNDAIR CL600 CL6002B19 EA F.S.310.00 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 969CA 11964 7141 THE DOUBLER FORWARD OF THE SERVICE DOOR IS CORRODED P/N 601R38669-49.REMOVED AND REPLACED DOUBLER FORWARD OF SERVICE DOO R WITH NEW P/N 601R38669-49 I/A/W WVAC EO 601R-53-2719. 2 L 7 2 4F RT A21EA 2001092500033 20010925 00033 EA 2001 9 25 COMA0160747 1 20010917 A 5300 601R31527221 ANGLE CNDAIR CL600 CL6002B19 EA F.S. 310.00 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 969CA 11964 7141 THE THRESHOLD SUPPORT ANGLE AT THE PASSENGER DOOR IS CORRODED.REMOVED CORRODED THRESHOLD SUPPORT ANGLE. FABED NEW THRES HOLD SUPPORT ANGLE AND INSTALLED I/A/W WVAC EO 601R-53-2717. 2 L 7 2 4F RT A21EA 2001092500038 20010925 00038 NM 2001 9 25 AALA20011564 1 20010804 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN DISCONNECTED A K NONE L NO TEST IN INSP/MAINT 1 SW 21 353AA 24034 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING ON SEATS 23B AND 21H INOPERATIVE. RECONNECTED ELECTRICAL WI RING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001092500039 20010925 00039 NM 2001 9 25 AALA20011609 1 20010806 A 5322 SHEAR TIE BOEING 727 727223 1384074 NM FS 520 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 870AA 21382 TUL - FOUND SHEAR TIE CORRODED AT STATION 520 STRINGER 26 TOP SIDE. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1, TRE ATED, PRIMED PAINTED IAW MM 51-20-0. (M) 2 L 7 3 4F A3WE 2001092500040 20010925 00040 NM 2001 9 25 AALA20011608 1 20010806 A 5330 SKIN BOEING 727 727223 1384074 NM FS 936 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 870AA 21382 TUL - FOUND GOUGE IN SKIN AT STATION 936 BETWEEN STRINGER 3R AND 4R. INSTALLED DOUBLER REPAIR AT STATION 936 BETWEEN ST RINGER 3R AND 4R PER SRM 53-30-3 PART 1. (M) 2 L 7 3 4F A3WE 2001092500041 20010925 00041 NM 2001 9 25 AALA20011606 1 20010726 A 5100 STIFFENER BOEING 727 727227 1384078 NM FS 870 CORRODED A AALA O OTHER O OTHER IN INSP/MAINT 1 SW 21 716AA 20608 TUL - FOUND STIFFENER CORRODED ON 870 BULKHEAD 1ST STIFFENER OUTBOARD OF KEEL BEAM, ON OUTBOARD SIDE APPROX MIDDLE OF ST IFFENER. DAMAGE, REMOVED HFEC INDICATED NO CRACK AROUND ELONGATED BLENDED HOLE, DOUBLER INSTALLED PER ESO11697 DATED 7- 24-01. (M) 2 L 7 3 4F A3WE 2001092500042 20010925 00042 NM 2001 9 25 AALA20011663 1 20010816 A 2700 SKIN BOEING 727 727223 1384074 NM BS 115 CORRODED A AALA O OTHER O OTHER IN INSP/MAINT 1 SW 21 885AA 21524 TUL - FOUND CORROSION UPPER RIGHT HORIZONTAL STAB SKIN T/E BEAM 4 HINGE IN FROM STAB TIP AT ABOUT STAB STATION 115. REP AIRED CORROSION AREA AS PER ESO 11697 DATED 8-16-2001. (M) 2 L 7 3 4F A3WE 2001092500043 20010925 00043 NM 2001 9 25 AALA20011665 1 20010817 A 5330 SKIN BOEING 727 727223 1384074 NM A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 885AA 21524 TUL - FOUND BULGE ABOVE LEFT RAM AIR DOOR MIDWAY ALONG LEFT EDGE OF CUTOUT. REMOVED CORROSION AND INSTALLED .080 17-7 P H DOUBLER PER ESO 11697 DATED 8/15/2001. (M) 2 L 7 3 4F A3WE 2001092500044 20010925 00044 NM 2001 9 25 AALA20011659 1 20010820 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 191AN 32385 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT OVER SEAT INOPERATIVE. RECONNECTED QUICK DISCONNECT AT EMERGENCY LI GHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001092500045 20010925 00045 NM 2001 9 25 AALA20011656 1 20010819 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN DAMAGED A K NONE L NO TEST IN INSP/MAINT 1 SW 21 382AN 25451 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT SEAT 34B INOPERATIVE. REPAIRED WIRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001092500046 20010925 00046 NM 2001 9 25 AALA20011703 1 20010827 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7375A 25202 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 31H INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT CONNECTOR A T SEAT 31H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001092500047 20010925 00047 NM 2001 9 25 AALA20011683 1 20010823 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 370AA 25197 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 9B INOPERATIVE. REPAIRED CONNECTOR. SYSTEM GROUND CHE CKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001092500048 20010925 00048 NM 2001 9 25 AALA20011650 1 20010819 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 373AA 25200 ORD - DURING OVERNIGHT MAINTENANCE, EMEREGNCY LIGHTS AT SEAT 25B INOPERATIVE. RE-SECURED CONNECTOR. SYTEM GROUND CHECK ED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001092500049 20010925 00049 NM 2001 9 25 AALA20011719 1 20010824 A 5300 STRINGER BOEING 727 727223 1384074 NM FS 460 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 880AA 21519 TUL - FOUND STRINGER 24L DENTED AT STATION 460. CUT AND REMOVED DAMAGED SECTION OF STRINGER. SPLICED IN NEW SECTION OF STRINGER PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 2001092500050 20010925 00050 NM 2001 9 25 USAA011149 1 20010824 A 5310 WEB BOEING 737 737201 1384454 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND WEB CRACKED 1 INCH, BS 178 BULKHEAD AT WL 207.5 AT RBL 1 TO 2. INSTALLED DOUBLER DAMAGE. REMOVED HFEC DONE . PER EO 5300V153 EA 69902, SRM 53-10-08 FIG 211. (M) 2 L 7 2 4F A16WE 2001092500051 20010925 00051 NM 2001 9 25 USAA011156 1 20010828 A 5310 FRAME BOEING 737 737201 1384454 NM BS 500 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND FRAME CORRODED 2 INCHES BY 5 INCHES, BS 500 BL0. CORROSION LEVEL 1, TASK NR 90-25-01. CUT OUT DAMAGE ON FR M, HFEC INSPECTION FMD PARTS, HT TREAT/INSTALLED PER SRM 53-10-4/51-10-6/53-30-1. (M) 2 L 7 2 4F A16WE 2001092500052 20010925 00052 NM 2001 9 25 USAA011159 1 20010829 A 5300 WEB BOEING 737 7372B7 1384560 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 52062 22885 CLT - FOUND WEB CRACKED .6 INCHES, BS 178, WL 188 AT RBL .5 AND LBL .5 INCH. INSTALLED WEB REPAIR PER EA 85310, EO 5300 V152. (M) 2 L 7 2 4F A16WE 2001092500053 20010925 00053 NM 2001 9 25 USAA011161 1 20010829 A 5300 WEB BOEING 737 7372B7 1384560 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 52062 22885 CLT - FOUND WEB CRACKED .5 INCH, BS 178 BULKHEAD WL 2.8, LBL 11.7. CUT OUT DAMAGE FABRICATED FILLER AND DOUBLER PER EA 85310 AND SRM 53-10-08 FIG 211. (M) 2 L 7 2 4F A16WE 2001092500054 20010925 00054 NM 2001 9 25 USAA011164 1 20010829 A 5310 WEB BOEING 737 7372B7 1384560 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 52062 22885 CLT - FOUND WEB CRACKED FIVE PLACES .25 INCH EACH, BS 178, WL 234, LBL 10. INSTALLED DOUBLER ON WEB, CRACK CUT OUT OF W EB PER EO 5300V153 AND SRM 53-10-08 FIG 209. (M) 2 L 7 2 4F A16WE 2001092500055 20010925 00055 NM 2001 9 25 USAA011165 1 20010829 A 5330 WEB BOEING 737 7372B7 1384560 NM BS 179 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 52062 22885 CLT - FOUND WEB CRACKED 1 INCH, BS 179, WL 207, RBL 24. REMOVED AND REPLACED PART WITH NR 65-45833U40. (M) 2 L 7 2 4F A16WE 2001092500056 20010925 00056 NM 2001 9 25 USAA011169 1 20010829 A 5300 FRAME BOEING 737 737201 1384454 NM BS 807 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND FRAME CORRODED, BS 807 STRINGER 17R TO STRINGER 27R, CORROSION LEVEL 1 TASK NR C53-100-01. (M) 2 L 7 2 4F A16WE 2001092500057 20010925 00057 SO 2001 9 25 STZ2001F00001 1 20010828 A 2750 451813 TRANSMISSION PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA RIGHT FLAP INOPERATIVE A STZA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 AL 03 509FS 317952162 ON TAXI AFTER LANDING, PILOT SELECTED FLAPS UP, HEARD A LOUD POPPING SOUND, FLAPS STOPPED RETRACTING, AND FLAP FAULT LI GHT ILLUMINATED. MAINTENANCE FOUND RIGHT HAND FLAP HANGING LOOSE IN FULL DOWN POSITION. FLAP JACKSCREW BECAME SEPARATE D FROM FLAP TRANSMISSION, WITH JACKSCREW STILL ATTACHED TO FLAP. DISASSEMBLY OF FLAP TRANSMISSION BODY HAD BACKED ALL O F THE WAY OFF, ALLOWING JACKSCREW SHAFT TO SEPARATE FROM TRANSMISSION. CASTELLATED NUT IS SAFETIED IN POSITION AFTER TI GHTENING BY BENDING A TANG OF THE LOCK WASHER BENEATH IT INTO ONE OF CASTELLATED NUT GROOVES. NO TANGS OF THIS LOCK WAS HER SHOWED ANY SIGNS OF HAVING BEEN BENT. WITH NO SAFETY, NUT EVENTUALLY VIBRATED LOOSE. LEAD SEALS ON COMPONENT EXTER 1 L 7 2 3O 3 O A20SO E14EA 2001092700144 20010927 00144 NM 2001 9 27 P2EA2001M0001 1 20010923 A 4950 CONNECTOR BOEING 737 73725A 1384481 NM APU BLEED AIR DIRTY A P2EA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 05 239TA 23789 AIR-CONDITION AND MASTER CAUTION ON PRE-TAKEOFF RECALL WITH NO ASSOCIATED PANEL INDICATION. RETURNED TO GATE. SUSPECTED APU BLEED VALVE. OP'S CHECKED, GOT DUAL BLEED LIGHTS WITH APU BLEED SHUT OFF, PSI HELD, DUAL BLEED LIGHTS STAYED ON. BLEED VALVE OP'S NORMAL WITH BAD INDICATION. FOUND APU BLEED VALVE CONNECTOR DIRTY. CLEANED CONNECTOR, SYSTEM OP'S CHE CKED NORMAL. 2 L 7 2 4F RT A16WE 2001092500059 20010925 00059 NM 2001 9 25 SWAA012611 1 20010920 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED 1/4D CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 11 ABC. R&R LENS PER MM. 2 L 7 2 4F RT A16WE 2001092500060 20010925 00060 NM 2001 9 25 SWAA012612 1 20010920 A 5313 65C27314 CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294.5, STR 8L. R&R S TR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001092500061 20010925 00061 NM 2001 9 25 SWAA012616 1 20010919 A 5310 65C10300 FITTING BOEING 737 7372H4 138448C NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 068SW 22357 DURING SCHEDULED RON, FOUND NLG UPPER ACTUATOR SUPPORT T FITTING CRACKED. R&R SUPPORT T FITTING PER MM. 2 L 7 2 4F A16WE 2001092500062 20010925 00062 NM 2001 9 25 SWAA012617 1 20010919 A 5330 141A880 WINDOW POST BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 091SW 22963 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED 1/4 INCH LONG ON FIRST OFFICER'S CD WINDOW POST AT LOWER END. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001092500063 20010925 00063 NM 2001 9 25 SWAA012621 1 20010921 A 3350 07912 COVER BOEING 737 7377H4 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 785SW 30602 DURING SCHEDULED C3 CHECK, FOUND SEVERAL EEPLS COVERS CRACKED. R&R COVERS PER MM. 2 L 7 2 4F RT A16WE 2001092500064 20010925 00064 NM 2001 9 25 SWAA012622 1 20010922 A 3350 07912 COVER BOEING 737 7377H4 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 711HK 27845 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS CRACKED ( 19 EA ) IN CABIN. R&R EEPLS COVERS PER MM. 2 L 7 2 4F RT A16WE 2001092500065 20010925 00065 2001 9 25 SWAA012597 4 20010919 A 2565 65574639 BRACKET BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 091SW 22963 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR AFT FLOOR GIRT BAR BRACKET LOOSE. TIGHTENE D AFT GIRT BAR BRACKET PER MM. 2 L 7 2 4F A16WE 2001092500066 20010925 00066 NM 2001 9 25 SWAA012598 1 20010920 A 5250 656134263SP DOOR BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 COCKPIT DOOR TOP PANEL LOOSE. R & R COCKPIT DOOR ASSY. 2 L 7 2 4F A16WE 2001092500067 20010925 00067 NM 2001 9 25 SWAA012600 1 20010919 A 2910 651782121 MODULE BOEING 737 7373H4 1384600 NM WHEEL WELL FAILED A SWAA K NONE S AFFECT SYSTEMS LD LANDING 1 SW 07 371SW 26598 B SYSTEM HYDRAULIC FAILURE DURING LANDING. R & R B HYDRAULIC SYS MODULE PER MM. 2 L 7 2 4F RT A16WE 2001092500068 20010925 00068 NM 2001 9 25 SWAA012601 1 20010919 A 5752 6546434370 FLAP BOEING 737 7373H4 1384600 NM WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED C3 CHECK, FOUND RT INBD T/E AFTFLAP OUTBD LWR SURFACE DELAMINATED. R & R RT INBD AFTFLAP PER MM. 2 L 7 2 4F RT A16WE 2001092500069 20010925 00069 NM 2001 9 25 SWAA012602 1 20010919 A 5754 65C26602258A SLAT BOEING 737 7373H4 1384600 NM WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED 1/2D CHECK, FOUND #5 L/E SLAT DOUBLER PATCH CRACKED ON THE OUTBD END. R & R DOUBLER PER SRM. 2 L 7 2 4F RT A16WE 2001092500070 20010925 00070 NM 2001 9 25 SWAA012604 1 20010920 A 3350 BR9442910 SIGN BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED 1/4D CHECK, FOUND LH OVERWING EMER EXIT SIGN LOOSE. SECURED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2001092500071 20010925 00071 NM 2001 9 25 SWAA012605 1 20010920 A 5241 696985411 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR AFT LWR FRAME CRACKED AT STOP FITTING. REPAIR ED PER BAC DWG 69-69854. 2 L 7 2 4F RT A16WE 2001092500072 20010925 00072 NM 2001 9 25 SWAA012606 1 20010920 A 3350 1010425 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED 1/4D CHECK, FOUND OVHD BIN EMER EXIT LT LENS ROW 8 DEF LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2001092500073 20010925 00073 NM 2001 9 25 SWAA012607 1 20010920 A 5310 6546546 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 524SW 26566 DURING SCHEDULED D CHECK, FOUND FRAME FASTENER HOLES CRACKED ( 2 EA ) AT BS 827, BETWEEN STR 8R & 9R, AND BS 867, BETWEE N STR 8R & 9R. REPAIRED FRAMES PER SRM. 2 L 7 2 4F RT A16WE 2001092500074 20010925 00074 NM 2001 9 25 SWAA012608 1 20010919 A 5310 6546529 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 524SW 26566 DURING SCHEDULED D CHECK, FOUND FRAME FASTENER HOLES CRACKED ( 2 EA ) AT BS 400, STR 8 L, AND BS 360, STR 8 L. REPAIRED FRAMES PER SRM. 2 L 7 2 4F RT A16WE 2001092500075 20010925 00075 NM 2001 9 25 SWAA012609 1 20010919 A 5310 6546529 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 524SW 26566 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 360, BETWEEN STR 7L & 8L. REPAIR ED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001092500076 20010925 00076 NM 2001 9 25 SWAA012586 1 20010917 A 5310 6546529 FRAME BOEING 737 7375H4 138449D NM FWD CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 524SW 26566 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294.5, WL 209 & RBL 55. REPA IRED FRAME PER BFG ER 01-0838. 2 L 7 2 4F RT A16WE 2001092500077 20010925 00077 NM 2001 9 25 SWAA012589 1 20010918 A 5751 65C25922 BEARING BOEING 737 7373H4 1384600 NM LH WING WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED C2 CHECK, FOUND PLAY AT LH AILERON HINGES. R&R B EARINGS AT # 1, 2 & 4 HINGES PER MM. 2 L 7 2 4F RT A16WE 2001092500078 20010925 00078 NM 2001 9 25 SWAA012593 1 20010918 A 5310 6517582 BEAM BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAMS CRACKED ( 2 EA ) AT BS 183, WL 183 & RBL 5.7, WL 223 & RBL 17.1. R&R VERTICAL BEAMS PER SWA RA 1-353-2655. 2 L 7 2 4F RT A16WE 2001092500079 20010925 00079 NM 2001 9 25 SWAA012594 1 20010918 A 5310 6516300 WEB BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL WEBS CRACKED ( 2 EA ) AT BS 180, WL 207 & RBL 26, BS 178, WL 219 & LBL 12 . REPAIRED WEBS PER SRM. 2 L 7 2 4F RT A16WE 2001092500080 20010925 00080 NM 2001 9 25 SWAA012595 1 20010919 A 5230 6545871 FRAME BOEING 737 7373H4 1384600 NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR FRAME CRACKED AT FWD LWR CORNER. REPAIRE D DOOR FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001092500081 20010925 00081 2001 9 25 SWAA012596 4 20010918 A 2565 BACR12BU9B RING BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR DETERIORATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE RELEASE LATCH ASSY SPLIT RING SOLDER DETERIORATED. RESOLDERED SPLIT RING PER MM. 2 L 7 2 4F RT A16WE 2001092500082 20010925 00082 NM 2001 9 25 SWAA012577 1 20010917 A 3350 07912 COVER BOEING 737 7377H4 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 776WN 30591 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED ( 23 EA ) THROUGH OUT CABIN. R&R CO VERS PER MM. 2 L 7 2 4F RT A16WE 2001092500083 20010925 00083 NM 2001 9 25 SWAA012578 1 20010917 A 3350 07912 COVER BOEING 737 7377H4 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 763SW 27877 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS CRACKED IN FWD CABIN. R&R COVERS PER MM . 2 L 7 2 4F RT A16WE 2001092500084 20010925 00084 2001 9 25 SWAA012579 4 20010917 A 2565 6556685 BRACKET BOEING 737 7377H4 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 732SW 27864 DURING SCHEDULED BC4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET LOOSE ON CONTAINER. SECURED EVAC SLIDE BRACKET PER MM. 2 L 7 2 4F RT A16WE 2001092500085 20010925 00085 NM 2001 9 25 SWAA012580 1 20010918 A 2750 6573732 FLAP BOEING 737 7373H4 1384600 NM LH WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 639SW 27712 DURING SCHEDULED 1/4D CHECK AT DALFORT, FOUND LH T/E OTBD FLAP DELAMINATED AT UPPER INBD SURFACE. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2001092500086 20010925 00086 NM 2001 9 25 SWAA012582 1 20010918 A 3350 90083 BATTERY BOEING 737 7372H4 138448C NM FWD SVC DOOR ERRATIC A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 087SW 22903 DURING SCHEDULED RON, FWD SVC DOOR EMERGENCY EXIT LIGHT VOLTAGE IND. LOW. . R&R BATTERY PER M M. 2 L 7 2 4F A16WE 2001092500087 20010925 00087 NM 2001 9 25 SWAA012583 1 20010918 A 3350 610478 BATTERY BOEING 737 7372T4 1384492 NM CABIN ERRATIC A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 CEILING EMERGENCY EXIT LIGHT AT ROW 3 ILLUMINATED. R&R BATTERY PER MM. 2 L 7 2 4F A16WE 2001092500088 20010925 00088 NM 2001 9 25 SWAA012584 1 20010918 A 5310 6546543 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT LH OVERWING EMERGENCY EXIT, BS 616, WL 202. REPAIRED FRAME PER SWA T1-153-018. 2 L 7 2 4F RT A16WE 2001092500089 20010925 00089 NM 2001 9 25 SWAA012585 1 20010918 A 5310 6516300 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL WEB CRACKED AT BS 178, LBL 5 & WL199. REPAIRED WEB P ER SRM. 2 L 7 2 4F RT A16WE 2001092500091 20010925 00091 NM 2001 9 25 CA010924004 1 20010824 A 2612 207248 CONNECTOR BOEING 737 7372T7 1384482 NM PWA JT8 JT8D17A 52049 NE NR 2 ENGINE FAILED W F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 CA (CAN) ON APPROACH TO YVR NR 2 ENGINE FIRE WARNING INDICATED. BOTH FIRE BOTTLE FIRE DISCHARGED. FIRE WARNING REMAINED ILL UMINATED. NO EXTERNAL EVIDENCE OF FIRE ON LANDING YVR. FOUND CONNECTOR D1098 SHORTING INTERNALLY. REPLACED CONNECTOR 525 6. 2 L 7 2 4F 4 F RT A16WE E2EA 2001092700146 20010927 00146 2001 9 27 P2EA2001M0003 4 20010921 A 3421 2588733511 GYRO BOEING 737 7372T5 NM COCKPIT FAULTY A P2EA K NONE F FLT CONT AFFECTED CR CRUISE 1 CE 05 120NJ 22979 AUTO PILOT ON HDG2 HOLD WILL NOT MAINTAIN BANK AND ROLL LEVEL AND OCCASIONALLY JERKS ABRUPTLY. REPLACED NR 1 VERTICAL G YRO PER MM 34-22-11, OPERATIONAL CHECK OKAY. 2 L 7 2 4F RT A16WE 2001092500092 20010925 00092 2001 9 25 P2EA2001M0004 4 20010923 A 2210 2588810903 COMPUTER BOEING 737 7372T5 NM A P2EA K NONE F FLT CONT AFFECTED CR CRUISE 1 CE 05 120NJ 22979 Auto Pilot twitches in pitch on VG1. Auto Pilot pulls back on controls continuiously when operated on system "A". Correc tive action: Removed and replaced Pitch Computer IAW MM 22-11-151A, operatoinal check normal. See A/C 120 Log pages 9274 3 and 92744. This report is filed closed. 2 L 7 2 4F RT A16WE 2001092500094 20010925 00094 EU 2001 9 25 TI1R001437 1 20010405 A 3240 432B124 LINER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE BRAKES DAMAGED B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 911GF 3140 BRAKE LINING - LININGS WORN TO LIMITS. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2001092500096 20010925 00096 EU 2001 9 25 TI1R001438 1 20010411 A 6720 350A33214501 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE T/R PITCH LINK WORN B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 40751 491 3154 TAIL ROTOR PITCH CHANGE, BEARINGS WORN. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2001092500097 20010925 00097 EU 2001 9 25 TI1R001439 1 20010411 A 6720 350A33214501 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR WORN B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 40751 953 3154 TAIL ROTOR PITCH CHANGE, BEARING WORN. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2001092500099 20010925 00099 EU 2001 9 25 TI1R001440 1 20010418 A 3300 1179203103 CONTROL UNIT BOLKMS 117 BK117A3 5626015 EU LIGHTS BURNED B TI1R O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 05 1140H 7078 CONTROL UNIT, LIGHTS EXTINGUISHED, HEAVY BURNING SMELL. REMOVED AND REPLACED. 1 G 7 2 3U H13EU 2001092500107 20010925 00107 EU 2001 9 25 TI1R001450 1 20010420 A 7714 117902101 LIGHT BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE RPM INDICATOR INOPERATIVE B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 317MC 7505 RPM INDICATOR, BACK LIGHTS INOPERATIVE. REMOVED AND REPLACED. 1 G 7 2 3U 3 U NC H13EU E19EU 2001092500110 20010925 00110 EU 2001 9 25 TI1R001461 1 20010511 A 7712 117902131 CONTROL UNIT BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE RPM INOPERATIVE B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 317MC 7505 RMP CONTROL UNIT - PARTS SUPPORT AGREEMENT. REMOVED AND REPLACED. 1 G 7 2 3U 3 U NC H13EU E19EU 2001092500111 20010925 00111 EU 2001 9 25 TI1R001462 1 20010515 A 6240 117945641 INDICATOR BOLKMS 117 BK117A1 5626010 EU MAST MOMENT SHORTED B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 117M S7023 MAST MOMENT INDICATOR - POPS CIRCUIT BREAKER. REMOVED AND REPLACED. 1 G 7 2 3U H13EU 2001092500112 20010925 00112 EU 2001 9 25 TI1R001463 1 20010515 A 6240 10594575 TRANSMITTER BOLKMS 117 BK117A1 5626010 EU ROTOR TORQUE SHORTED B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 117M S7023 TORQUE TRANSMITTER - POPS CIRCUIT BREAKER. REMOVED AND REPLACED. 1 G 7 2 3U H13EU 2001092500114 20010925 00114 EU 2001 9 25 TI1R001465 1 20010511 A 6320 SL100153B PIN SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE M/R GEARBOX WORN B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 40751 1003 3154 PIN, WORN AT BOLT HEAD SIDE. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2001092500115 20010925 00115 EU 2001 9 25 TI1R001466 1 20010511 A 6410 355A09103601 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR WORN B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 40751 1003 BEARING SET, WORN. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2001092500116 20010925 00116 WP 2001 9 25 257207 2 20010920 A 7200 ENGINE HAWKER BAE125 BAE125700B 7450007 EU GARRTT TFE731 TFE7313R1H 29001 WP NR 2 MALFUNCTIONED E ERYA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 07 913V 257207 P84464 DURING TAKEOFF ROLL, HEARD LOUD NOISE FROM OUTSIDE AIRCRAFT. AIRCRAFT YAWED TO RIGHT. ABORTED TAKEOFF AND APPLIED BRAK ES. TAXIED BACK TO FBO WHERE NR 2 ENGINE DID NOT APPEAR NORMAL AND NR 3 MAIN TIRE WAS DEFLATED. POSSIBLE FAILURE 1 OR MORE COMPONENTS ON RT ENGINE AND BRAKING ACTION HEAT CAUSED DEFLATION OF TIRE. 2 L 7 2 4F 4 F RT A3EU E6WE 2001092500117 20010925 00117 EU 2001 9 25 TI1R001468 1 20010520 A 7931 646600251 PROBE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE OIL TEMP ERRATIC B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 40751 1019 3154 TEMPERATURE PROBE, OIL TEMPERATURE, ERRATIC. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2001092500118 20010925 00118 WP 2001 9 25 AT0100229 1 20010915 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN BROKEN A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 810AT 47277 FOUND FORWARD RED LIGHTS OF THE PASSENGER EMERGENCY EGRESS PATH LIGHTING SYSTEM INOPERATIVE. REPAIRED BROKEN WIRE AT FO RWARD LEFT PORTION OF TRACK IAW DC9 MM 33-50. 2 L 7 2 4F A6WE 2001092500119 20010925 00119 2001 9 25 TI1R001469 4 20010522 A 3443 066011530101 RADAR SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT ERRATIC B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 911GF 3140 KRA 405B RAD. A - VERY ERRATIC - SWINGS AND HAS UNRELIABLE READINGS. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2001092500120 20010925 00120 NM 2001 9 25 AWXA200100454 1 20010815 A 5330 6545800 SKIN BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 C-21 CK - C - L-1 DOOR CUTOUT FUSELAGE SKIN LOWER EDGE BS 338.5 CRACKED .0625 INCH AT SILL PLATE ATTACH HOLE. MAINTENAN CE REAMED CRACKED FASTENER HOLE, DRILLED AND INSTALLED REPAIR DOUBLER AT L-1 DOOR CUTOUT LOWER EDGE, BS 338.5 PER AWA ER 15-5300-01234-DD1. 2 L 7 2 4F RT A16WE 2001092500121 20010925 00121 2001 9 25 TI1R001496 4 20010629 A 3422 109290 GYRO BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101600A 41560 NE TAIL ROTOR DEFECTIVE A TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 217MC 6488 7195 SEVERE TAIL ROTOR OSCILLATION. REMOVED AND REPLACED 1 G 7 2 3U 3 U H13EU E5NE 2001092500122 20010925 00122 EU 2001 9 25 TI1R97330 1 20010420 A 7714 1179405303 TACHOMETER BOLKMS 117 BK117B1 5626012 EU COCKPIT INOPERATIVE B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 460H 7142 NR 2 NEEDLE INOPERATIVE. 1 G 7 2 3U H13EU 2001092500123 20010925 00123 EU 2001 9 25 TI1R97331 1 20010529 A 7714 1179405303 TACHOMETER BOLKMS 117 BK117B1 5626012 EU NR 1 ENGINE STUCK B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 117VU 7211 NUMBER 1 ENGINE STUCK AT 90 PERCENT. 1 G 7 2 3U H13EU 2001092500124 20010925 00124 NM 2001 9 25 AWXA200100456 1 20010824 A 5311 6545409602 FRAME BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 MCN - C21 CK - C - MAIN CABIN SUB FLOOR PRESSURE DECK FWD CHORD BS 663.75, LBL 24, WL 202 CRACKED 3.5 INCH. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED IAW AWA ER 15-5312-01238-GF1. 2 L 7 2 4F RT A16WE 2001092500125 20010925 00125 NM 2001 9 25 AWXA200100457 1 20010818 A 5312 65163007 BULKHEAD BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 C21 CK - C - AFT SIDE OF BS 178 PRESS BULKHEAD CENTER WEB HAS A .5 INCH CRACK AT LBL .7, WL 203 TO 203.5, CONFIRMED WITH HFEC. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLERS AND INSTALLED REPAIR IAW B737 SRM 53-10- 11, PG 83 & 84 AND TEMP REV 53-52. 2 L 7 2 4F RT A16WE 2001092500126 20010925 00126 NM 2001 9 25 AWXA200100458 1 20010826 A 5312 65163007 BULKHEAD BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 MCN - C21 CK - C - BS 178 PRESS BULKHEAD CENTER WEB, LBL 4.8, WL 187.2 TO 188 HAS A .8 INCH CRACK CONFIRMED WITH HFEC. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLERS AND INSTALLED IAW B737 SRM 53-10-11 AND TEMP REV 53-52. 2 L 7 2 4F RT A16WE 2001092500127 20010925 00127 CE 2001 9 25 UKW2001F00000 1 20010806 A 3210 BUSHING CESSNA 172 172S 2072439 CE LYC IO360 IO360L2A EA MLG WORN A UKWT K NONE O OTHER IN INSP/MAINT 1 SW 19 208SP 1344 172S8208 L2862151A PILOT REPORTED POPPING NOISE COMING FROM LEFT MAIN GEAR WHEN BRAKES WERE APPLIED. BOLT AND BOLT HOLE IN THE LANDING GEA R SPRING ASSEMBLE WAS FOUND TO BE WORN BEYOND LIMITS. AIRCRAFT HAS BEEN USED AS A FLIGHT SCHOOL AIRCRAFT SINCE NEW. CA USE IS NOT KNOWN AT THIS TIME. PART WAS RETURNED TO MANFACTURER FOR EVALUATION. 1 H 7 1 3O 3 O NT 3A12 1E10 2001092500128 20010925 00128 CE 2001 9 25 VG42001F00000 1 20010830 A 5321 431130 FASTENER BEECH 90 C90A 1152911 CE CABIN FLOOR BROKEN B VG4R K NONE O OTHER IN INSP/MAINT 1 SO 35 588SA LJ1588 THE ADJUSTABLE GRIP LATCH FASTENER THAT HOLDS DOWN THE CENTER ISLE FLOORBOARD IN THE CABIN FALLS APART AND CONDUCTIVE PI ECES FALL INTO THE ELECTRICAL EQUIPMENT BELOW THE FLOORBOARDS. A PIECE WAS FOUND ON THE FLAP RELAY DURING REGULAR MAINT ENANCE. 1 L 7 2 3T RT 3A20 2001092500129 20010925 00129 NM 2001 9 25 AWXA200100459 1 20010815 A 5312 65163007 BULKHEAD BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 MCN - C21 CK - C - BS 178 PRESS BULKHEAD CENTER WEB HAS A .8 INCH CRACK AT LBL 9.2 TO LBL 10, WL 218, UNDER REINFORCEMEN T AS DETERMINED WITH ULTRASONIC INSPECTION. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLERS AND INSTALLED REPAIR IAW AWA ER 15-5312-01249-DL3. 2 L 7 2 4F RT A16WE 2001092500130 20010925 00130 CE 2001 9 25 VG42001F00001 1 20010814 A 5522 50610000432 SKIN BEECH 90 C90 1152913 CE ELEVATOR CRACKED B VG4R K NONE O OTHER IN INSP/MAINT 1 SO 35 34CE 4384 88 LJ932 THE LEFT ELEVATOR LOWER SKIN AT THE OUTBOARD HINGE POINT HAD TWO CRACKS EXTENDING FROM THE HINGE CUTOUT AREA ACROSS SPAR CAP. 1 L 7 2 3T 3A20 2001092500131 20010925 00131 GL 2001 9 25 VGY2001F00000 2 20010821 A 7321 23065104 FUEL CONTROL BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL NR 2 ENGINE FAULTY A VGYA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 EA 21 200VB 1763 4070 270457 AFTER INSTILLATION OF O/H ENG, HELICOPTER WAS GROUND RUN AND ALL ENG INSTRUMENTS AND OPERATION WAS NORMAL. A HOVER TEST FLIGHT WAS PERFORMED AND EVERYTHING STILL NORMAL. A SERIES OF 2 OR 3 HOVERING AUTOS WERE PERFORMED. DURING SPOOL UP O N LAST AUTO, NR 2 WOULD NOT GO PAST 90 PERCENT. MECHANIC CHECKED THROTTLE LINKAGE AND NO PROBLEM WAS FOUND. THROTTLE W AS RETURNED TO GROUND IDLE OF 62 PERCENT. UPON TRYING TO RETURN THROTTLE TO 100 PERCENT, ENGINE RPM WOULD ONLY DECREASE , TO THE POINT THAT ENGINE OUT HORN WOULD COME ON. INSTALLED ANOTHER FUEL CONTROL AND PROBLEM WAS ELIMINATED. FAULTY F UEL CONTROL WAS SENT FOR REPAIR. 1 G 7 1 3U 3 U H2SW E4CE 2001092500132 20010925 00132 EA 2001 9 25 WVBA2001040 2 20010719 A 7314 RG8090J4AM PUMP PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540* 41533 EA FUEL SYSTEM STUCK A WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 300ED 449 317852008 DURING PREINSPECTION RUN, IT WAS NOTED THAT THE ENGINE DRIVEN FUEL PUMP PRESSURE WAS LOW AFTER ADJUSTMENTS WERE MADE THE DESIRED PRESSURE SETTING WAS NOT OBTAINABLE. TROUBLESHOOTING, IT APPEARS THE RELIEF VALVE IS HUNG UP PUMP WAS REMOVED FROM SERVICE AND SENT OUT FOR REPAIR. 1 L 7 2 3O 3 O A20SO E14EA 2001092500133 20010925 00133 NM 2001 9 25 AWXA200100460 1 20010815 A 5312 65163007 BULKHEAD BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 MCN - C21 CK - C - BS 178 PRESS BULKHEAD CENTER WEB HAS A 1 INCH CRACK AT LBL 6.6, WL 221.5 TO WL 222.5 BELOW REINFORCE MENT AS DETERMINED WITH ULTRASONIC INSPECTION. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLERS AND INSTALLED REPAIR IAW AWA ER 15-5312-01249-DL3. 2 L 7 2 4F RT A16WE 2001092500134 20010925 00134 EA 2001 9 25 WVBA2001041 2 20010719 A 7314 RG8090J4AM PUMP PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540* 41533 EA FUEL SYSTEM LEAKING A WVBA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 01 59829 59 317652081 DURING INSPECTION IT WAS FOUND THAT FUEL WAS LEAKING FROM THE SET SCREW FOR THE DRIVE COUPLING LOCK NUT REFERENCE THE RG 9080 SERIES COMPONENT MM FOR PARTS BREAKDOWN. PUMP WAS REMOVED FROM SERVICE. 1 L 7 2 3O 3 O A20SO E14EA 2001092500135 20010925 00135 NM 2001 9 25 AWXA200100461 1 20010814 A 5312 65163007 BULKHEAD BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 MCN - C21 CK - C - BS 178 PRESS BULKHEAD CENTER WEB HAS A .5 INCH CRACK, WL 234, LBL 10 AT A FASTENER HOLE AS DETERMINED WITH HFEC. MAINTENANCE CUT OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED REPAIR PARTS IAW AW A ER 15-5312-01249-DL3. 2 L 7 2 4F RT A16WE 2001092500136 20010925 00136 NM 2001 9 25 AWXA200100462 1 20010813 A 5312 65163007 BULKHEAD BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 MCN - C21 CK - C - BS 178 PRESS BULKHEAD CENTER WEB, AFT SIDE HAS A 1 INCH CRACK, LBL .7, WL 185 FOUND VISUALLY AND CONF IRMED WITH HFEC. MAINTENANCE CUT OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED REPAIR PARTS I AW B737 SRM 53-10-11 PG 83 & 84 AND TEMP REV 53-52. 2 L 7 2 4F RT A16WE 2001092500137 20010925 00137 NM 2001 9 25 AWXA200100463 1 20010814 A 5312 65163007 BULKHEAD BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 MCN - C21 CK - C - BS 178 PRESS BULKHEAD CENTER WEB HAS A .75 INCH CRACK, WL 234, RBL 10, FWD SIDE AT A FASTENER HOLE, A S DETERMINED WITH HFEC. MAINTENANCE CUT OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED IAW B73 7 SRM 53-10-11, PG 1 - 8. 2 L 7 2 4F RT A16WE 2001092500138 20010925 00138 NM 2001 9 25 AWXA200100464 1 20010818 A 5320 65163009 STIFFENER BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 MCN - C21 - C - BS 178 PRESS BULKHEAD WEB, AFT SIDE, VERT TEE CRACKED 1 INCH ON I/B SIDE, WL 184 TO 185, LBL 5.7, FOUND VISUALLY AND CONFIRMED BY HFEC. MAINTENANCE CUT OUT DAMAGED AREA OF VERT TEE AND FORMED REPAIR ANGLES, STRAPS AND FILLE RS AND INSTALLED REPAIR PARTS IAW B737 SRM 53-10-11 PG 57 & 58. 2 L 7 2 4F RT A16WE 2001092500139 20010925 00139 NM 2001 9 25 AWXA200100465 1 20010815 A 5312 65163007 BULKHEAD BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 MCN - C21 CK - C - BS 178 PRESS BULKHEAD CENTER WEB .7 INCH CRACK, WL 218, RBL 11.7 TO RBL 12.7, BELOW REINFORCEMENT DET ECTED BY ULTRASONIC INSPECTION. MAINTENANCE CUT OUT DAMAGED AREA OF WEB AND FABRICATED REPAIR DOUBLER AND FILLER AND IN STALLED IAW B737 SRM 53-10-11 FIG 1 PG 1 - 8. 2 L 7 2 4F RT A16WE 2001092500140 20010925 00140 NM 2001 9 25 AWXA200100466 1 20010815 A 5312 65163007 BULKHEAD BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 MCN - C21 CK - C - BS 178 PRESS BULKHEAD CENTER WEB HAS A 1 INCH CRACK, WL 227.7 TO 228.7, RBL 6.4, BELOW REINFORCEMENT, FOUND WHILE PERFORMING ULTRASONIC INSPECTION. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLER A ND INSTALLED REPAIR PARTS IAW B737 SRM 53-10-11 PG 1 - 8. 2 L 7 2 4F RT A16WE 2001092500141 20010925 00141 NM 2001 9 25 AWXA200100467 1 20010817 A 5315 65468111 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 MCN - C21 CK - C - FLOORBEAM BS 986.5, LBL 44 TO RBL 49 HAS CORROSION IN SEVERAL PLACES ON UPPER FLANGE. MAINTENANCE RE MOVED THE FLOORBEAM UPPER CAP FROM LBL 44 TO RBL 49 AND FABRICATED NEW UPPER CAP SECTION AND INSTALLED IAW B737 SRM 53-1 0-9 FIG 2 PG 7 - 11. 2 L 7 2 4F RT A16WE 2001092500142 20010925 00142 NM 2001 9 25 AWXA200100468 1 20010818 A 5753 657192665 SKIN BOEING 737 737277 1384570 NM T/E FLAP CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 MCN - C21 CK - C - LT WING, I/B FLIPPER FLAP LOWER O/B SKIN CHAFED BEYOND LIMITS. MAINTENANCE REMOVED THE LOWER SKIN PA NEL, FABRICATED AND INSTALLED NEW LOWER SKIN PANEL IAW AWA ER 15-5752-01249-DL4. 2 L 7 2 4F RT A16WE 2001092500143 20010925 00143 EA 2001 9 25 WVBA2001042 2 20010731 A 8500 LTIO540J2BD ENGINE PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA RIGHT SEIZED E WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 3582P 883 883 318052103 RL248368A PILOT REPORTED THAT IN CRUISE THE RIGHT ENGINE MANIFOLD PRESSURE DROPPED 2 INCHES, THE OIL TEMPERATURE STARTED TO RISE W ITH THE OIL PRESSURE REMAINING IN THE GREEN. CHART WAS WITHIN LIMITS, AT THIS POINT HE DECIDE TO DO A PRECAUTIONARY SHU T DOWN OF THE ENGINE. HE ATTEMPTED TO FEATHER, THE ENGINE APPARENTLY SEIZED AND THE PROP FEATHERED. THE A/C LANDED WIT HOUT INCIDENT. IT APPEARS THAT EITHER NR 5 CYLINDER CONNECT ROD OR POSSIBLY THE CRANKSHAFT BROKE CAUSING THE ENGINE TO SEIZE. THE CYLINDER HAD STARTED TO SEPARATE FROM THE CASE, CRACKING IT THROUGH THE INTAKE/OIL SUMP ASSEMBLY AND THE ACC ESSORY SECTION CASE WAS ALSO CRACKED . CAUSE OF THE FAILURE: TO BE DETERMINED AT BREAKDOWN BY THE MANUFACTURER. 1 L 7 2 3O 3 O A20SO E14EA 2001092500144 20010925 00144 EA 2001 9 25 WVBA2001043 2 20010731 A 7314 RG9080J4AM PUMP PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA FUEL SYSTEM LEAKING A WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 4434D 921 317552020 DURING INSPECTION, FUEL WAS OBSERVED LEAKING FROM THE SET SCREW THAT HOLDS THE DRIVE SHAFT LOCK NOT IN CHECK IN THE PUMP BODY. THE PUMP WAS REMOVED AND REPLACED. THE LOCK NUT WAS REMOVED FOR INSPECTION AND IT WAS NOTED THAT A BACK UP PACK ING BEHIND THE ORING WOULD INSURE THAT FUEL COULD NOT FIND ITS WAY OUT OF THE ORING GROVE AND UP THE OUTER PORTION OF TH E LOCK NUT TO THE SET SCREW PORT. 1 L 7 2 3O 3 O A20SO E14EA 2001092500145 20010925 00145 EA 2001 9 25 WVBA2001044 2 20010802 A 7314 RG8090J4AM PUMP PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540* 41533 EA FUEL SYSTEM INOPERATIVE E WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 59829 59 59 317652081 DURING INSPECTION, FUEL STAIN WAS OBSERVED FROM THE DISCHARGE FITTING ON THE PUMP BODY FUEL STAIN WAS ALSO NOTED ON THE PUMP BODY HOUSING PARTING FLANGE. PUMP WAS REMOVED FROM SERVICE. NOTE: THIS IS A (M) STYLE PUMP THAT IS RE-DESIGNED TO RELIEVE LEAKS ON THE PARTING FLANGE. 1 L 7 2 3O 3 O A20SO E14EA 2001092500146 20010925 00146 EA 2001 9 25 WVBA2001045 2 20010821 A 7314 RG8090J4AM PUMP PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540* 41533 EA FUEL SYSTEM LEAKING A WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 59829 34 317652081 DURING INSPECTION IT WAS NOTICED THAT THE FUEL PUMP WAS LEAKING FROM THE PARTING SURFACE AND THE PUMP BODY. THIS IS THE SIDE WITH THE LADDER SEAL TO THE PUMP BODY. THE PUMP WAS REMOVED FROM SERVICE. THIS IS A (M) STYLE PUMP. 1 L 7 2 3O 3 O A20SO E14EA 2001092500147 20010925 00147 SO 2001 9 25 WVBA2001047 1 20010910 A 3234 5541602 CONTROL CABLE PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540* 41533 EA MLG MISINSTALLED E WVBA O OTHER J WARNING INDICATION NR NOT REPORTED 1 AL 01 42WP 318252038 PILOT REPORTED GEAR WOULD NOT EXTEND. ATTEMPTS WERE MADE TO TROUBLESHOOT SYSTEM FROM GROUND BUT GEAR FAILED TO EXTEND. A GEAR UP LANDING WAS MADE AND ALL PASSENGERS AND PILOT EXITED THE AIRCRAFT. INVESTIGATION DETERMINED THAT THE END OF THE GEAR SELECTOR CABLE HAD BEEN INSTALLED IMPROPERLY AND HAD WALKED OFF THE PIN THAT SECURES IT TO THE HYDRAULIC POWER- PAK ACTUATOR ARM. THE AREA THIS CABLE END IS LOCATED ON THE POWER-PAK IS AN EXTREMELY CLOSE QUARTERED AREA A CONTRIBUTI NG FACTOR. TO PREVENT FURTHER OCCURANCE A REQUIRED INSPECTION ITEM (RII) PROGRAM WILL BE IMPLEMENTED. 1 L 7 2 3O 3 O A20SO E14EA 2001092500148 20010925 00148 EA 2001 9 25 WVBA200146 2 20010906 A 8520 LW19340 CAMSHAFT PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA ENGINE DAMAGED E WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 59829 1027 317652081 L966361A DURING INSPECTION, METAL CONTAMINATION WAS OBSERVED IN THE OIL FILTER. A CHECK WAS MADE OF VALVE LIFT AND IT WAS DETER MINED THAT THE NR 1 AND NR 2 INTAKE LOBES ON THE CAMSHAFT WERE EXCESSIVE. NR 2 CYLINDER WAS REMOVED AND DAMAGE ON THE CAM LOBES AND TAPPET FOLLLOWERS WERE OBSERVED. ENGINE WAS REMOVED FROM SERVICE. 1 L 7 2 3O 3 O A20SO E14EA 2001092500149 20010925 00149 CE 2001 9 25 X762001F00000 1 20010130 A 2140 HEATER BEECH 95 95B55 1152729 CE CONT O470 IO470* 17026 SO COMBUSTION HEAD DAMAGED E X76R K NONE O OTHER IN INSP/MAINT 1 CE 03 303RM 1739 TC1219 AIRCRAFT WAS BROUGHT INTO SHOP WITH THE HEATER INOPERATIVE. INSPECTION REVEALED A .500 INCH DIAMETER HOLE IN THE COMBUS TION HEAD JUST BELOW AND TO THE RIGHT OF THE IGNITOR, NEAR THE FUEL SUPPLY LINE. RECOMMEND VISUAL INSPECTION AND/OR PRE SSURE TEST EACH 100 HOURS OF HEATER OPERATION. 1 L 7 2 3O 3 O RT 3A16 E1CE 2001092500150 20010925 00150 SO 2001 9 25 XGN2001F00001 2 20010802 A 8530 SA629340 ROD BOLT BEECH 36 36BEECH 1151602 CE CONT O520 IO520BB 17032 SO NR 6 CYLINDER BROKEN A XGNA K NONE O OTHER IN INSP/MAINT 1 SW 05 361BC E1331 285689R ROD BOLT BROKE ON NR 6 CYLINDER, WHILE AIRCRAFT WAS ON FINAL APPROACH. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE ENGIN E WAS DESTROYED. 1 L 7 1 3O 3 O 3A15 E5CE 2001092500151 20010925 00151 EU 2001 9 25 ZWYA100157 1 20010315 A 3210 17988 HARNESS AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE MLG INOPERATIVE A ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365SJ 3561 6018 HARNESS ASSEMBLY. NO CONTAVITY THROUGH SWITCH. REMOVED AND REPLACED HARNESS ASSEMBLY. 1 G 7 2 3U 3 U H10EU E19EU 2001092500152 20010925 00152 EU 2001 9 25 ZYWA100155 1 20010312 A 3230 1934500002 CONTACTOR AEROSP SA365 SA365N 8680669 EU MLG INOPERATIVE A ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365SJ 3559 6018 CONTACTOR ASSEMBLY INOPERATIVE. REMOVED AND REPLACED CONTACTOR. 1 G 7 2 3U H10EU 2001092500153 20010925 00153 WP 2001 9 25 ABXA010498 1 20010924 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP COCKPIT DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 968AX 47499 EMERGENCY LIGHTS FAILED TO TEST. MAINTENANCE INSPECTED AND REPLACED THE COCKPIT EMERGENCY LIGHT BATTERIES IAW DC-9 MM 3 3-53-02. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001092500154 20010925 00154 NM 2001 9 25 AWXA200100469 1 20010817 A 5315 65468101 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 MCN - C21 CK - C - BS 967 FLOORBEAM UPPER FLANGE CORRODED IN 4 PLACES BETWEEN LBL 22 AND RBL 49, BEYOND SRM LIMITS. MAI NTENANCE REMOVED THE FLOORBEAM UPPER CAP AND FABRICATED AND INSTALLED NEW UPPER CAP IAW B737 SRM 53-10-9, FIG 2, PG 7 - 11. 2 L 7 2 4F RT A16WE 2001092500155 20010925 00155 EU 2001 9 25 DHL2001363024 1 20010922 A 2560 SMOKE BARRIER AIRBUS 300 A300B4203 3930306 EU CABIN DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 SMOKE CURTAIN HAS DAMAGE TO BOTTOM AROUND CAMLOCS. REMOVED AND REPLACED SMOKE CURTAIN IAW B/E AEROSPACE CM/M 25-50-02, OP'S CHECK SERVICEABLE. 2 L 7 2 4F RT A35EU 2001092500156 20010925 00156 EU 2001 9 25 DHL2001366029 1 20010922 A 2560 SMOKE BARRIER AIRBUS 300 A300B4203 3930306 EU CABIN DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 SMOKE CURTAIN HAS DAMAGE TO BOTTOM AROUND CAMLOCS. REMOVED AND REPLACED SMOKE CURTAIN IAW B/E AEROSPACE CM/M 25-50-02, OP'S CHECK SERVICEABLE. 2 L 7 2 4F RT A35EU 2001092500157 20010925 00157 EU 2001 9 25 DHL2001367014 1 20010909 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU CARGO BAY MALFUNCTIONED A DHLA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 367DH 265 PRIOR TO ENGINE START CARGO SMOKE DETECTOR ILLUMINATED. FOUND ZONE TEMPS HIGH. COOLED A/C. PERFORMED SYSTEM TEST OF C ABIN SMOKE DETECTORS, NO FAULTS NOTED. DONE IAW A300 M/M REF 26-14-00. 2 L 7 2 4F RT A35EU 2001092500158 20010925 00158 NM 2001 9 25 DHL2001727585 1 20010828 A 5320 FLOOR SUPPORT BOEING 727 727200 138407E NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C-CK; AFT CARGO COMPT FLOOR SUPPORT BRACKET CRACKED STA 970 OVER STR 27R. REMOVED OLD BRACKET IAW B727 SRM 53-10-1, CLEANED, TREATED AND PRIMED AREA PER B727 SRM 51-30-2, PG 2. FABRICATED AND INSTALLED NEW BRACKET PER B727 SRM 53-10-1 AND 51-30-2. 2 L 7 3 4F RT A3WE 2001092500159 20010925 00159 NM 2001 9 25 DHL2001727586 1 20010818 A 3213 STRUT BOEING 727 727200 138407E NM MLG WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C-CK; LEFT MLG SIDE STRUT LOWER SEGMENT SWIVEL WORN OUT OF LIMITS. REMOVED AND REPLACED LT MLG SIDE STRUT LOWER SEGM ENT ASSY PER B727 M/M 32-11-41. GEAR SWING AND OPS CHECK FOUND GOOD, NO PLAY NOTED PER M/M 32-11-00. 2 L 7 3 4F RT A3WE 2001092500160 20010925 00160 NM 2001 9 25 DHL2001727587 1 20010818 A 2750 652661453 JACKSCREW BOEING 727 727200 138407E NM TE FLAPS WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH LT WING, INBOARD FLAP, INBOARD JACKSCREW (N04) HAS EXCESSIVE PLAY AT UNIVERSAL BUSHING AND AT JACKSCREW TO YOLK ATTACH B OLT. REMOVED INBOARD FLAP JACKSCREW NR 4 IAW B-727-200 PER MM 27-51-41. REINSTALLED INBOARD FLAP JACKSCREW NR 4 AS PER DHL 727 MM 27-51-1. RIGGED AND ADJUSTED FLAPS PER B-727 MM 27-51-1. OPS CHECK OK PER B-727 MM 27-51-0. 2 L 7 3 4F RT A3WE 2001092500161 20010925 00161 NM 2001 9 25 DHL2001727588 1 20010816 A 5753 FLAP TRACK BOEING 727 727200 138407E NM TE FLAPS LOOSE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, LEFT WING OUTBOARD FLAP HAS EXCESS PLAY WITH POWER ON FLAPS UP. REMOVED NEW INSTALLED BUSHINGS AS PER O/H 5 7-40-01. INSTALLED NEW BOLT AT FWD FLAP TRACK ATTACH POINT AND FLAP FAIRING ATTACH BRACKET FOR NR 2 FLAP TRACK PER B-72 7 MM 27-51-31. OPS CHECK OK PER B-727 MM 27-51-0. NO EXCESS PLAY NOTED. 2 L 7 3 4F RT A3WE 2001092500162 20010925 00162 NM 2001 9 25 DHL2001727589 1 20010817 A 3213 STRUT BOEING 727 727200 138407E NM MLG WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, LEFT MLG OUTER CYLINDER SIDE STRUT LOWER SEGMENT SPINDLE ATTACH WORN OUT OF LIMITS. REMOVED, MACHINED NEW B USHINGS AND INSTALLED AS PER O/M 32-12-01. NO PLAY NOTED PER B-727 MM 32-12-01. OPS CHECK GOOD ON GEAR RUN PER B-727 M M 32-11-0. 2 L 7 3 4F RT A3WE 2001092500163 20010925 00163 NM 2001 9 25 DHL2001727590 1 20010817 A 3213 BUSHING BOEING 727 727200 138407E NM MLG STRUT WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, RIGHT MLG OUTER CYLINDER SIDE STRUT LOWER SEGMENT SPINDLE ATTACH WORN OUT OF LIMITS. REMOVED MACHINED NEW B USHINGS AND INSTALLED PER O/M 32-12-01. NO PLAY NOTED PER B-727 MM 32012-01. OPS CHECK GOOD ON GEAR RUN PER B-727 M/M 32-11-0. 2 L 7 3 4F RT A3WE 2001092500164 20010925 00164 NM 2001 9 25 DHL2001727591 1 20010824 A 5340 SEAT TRACK BOEING 727 727200 138407E NM FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON C-CHECK, CABIN SEAT TRACK BETWEEN BS 756 TO 765, LBL 46 HAS WORN AREAS, MKD. REMOVED CORROSION, FOUND TO BE OUT OF L IMITS AS PER SRM 51-10-6/53-10-1. REMOVED AND REPLACED THE CABIN SEAT TRACK PER B-727 SRM 51-10-1 PARA 4 AND 51-30-2. 2 L 7 3 4F RT A3WE 2001092500165 20010925 00165 NM 2001 9 25 DHL2001727592 1 20010817 A 3231 10605459 BEARING BOEING 727 727200 138407E NM RT MLG WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON "C" CHECK DISCREPANCY------ R.M.L.G. FWD. UPPER SEGMENT BEARING WORN BEYOND LIMITS.1) REMOVED R.M.L.G. UPPER SEGMENT PER B-727 M.M. 32-11-41.2) REMOVED AND REPLACED R.M.L.G. UPPER SEGMENTS AFT. BEARING, FWD. FABROID BUSHING AND FWD. BEAR ING PER B-727 M.M. 32-11-41.3) REMOVED AND REPLACED R.M.L.G. UPPER SEGMENT LINK ASSY PER B-727 M.M. 32-11-41.4) GEAR SWI NG AND OPS CHECK FOUND GOOD NO PLAY NOTED PER B-727 M.M. 32-11-00. 2 L 7 3 4F RT A3WE 2001092500166 20010925 00166 NM 2001 9 25 DHL2001727593 1 20010817 A 3231 651952026 SWIVEL BOEING 727 727200 138407E NM MLG STRUT WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON "C" CHECK DISCREPANCY--------- RIGHT M.L.G. LOWERSEGMENT SWIVEL WORN BEYOND LIMITS.1) REMOVED AND REPLACED R/H M.L.G. SIDE STRUT LOWER SEGMENT ASSY. PER B-727 M.M. 32-11-41.2) GEAR SWING AND OPS CHECK FOUND GOOD NO PLAY NOTED PER 32-11-0 0. 2 L 7 3 4F RT A3WE 2001092500167 20010925 00167 NM 2001 9 25 AWXA200100470 1 20010816 A 5320 6545833440 WEB BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 MCN - C21 CK - C - RT COCKPIT FLOOR WEB CRACKED 1 INCH AT CUTOUT, BS 180, WL 207, RBL 24. MAINTENANCE REMOVED THE FLOOR WEB, FABRICATED AND INSTALLED NEW FLOOR WEB IAW AWA ER 15-5311-01234-TR1. 2 L 7 2 4F RT A16WE 2001092500168 20010925 00168 NM 2001 9 25 DHL2001727594 1 20010827 A 5714 SPAR BOEING 727 727200 138407E NM CENTER WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON "C" CHECK DISCREPANCY. WING CENTER SECTION AFT. SPAR LOWER CHORD APPROX. 15 RBL. RIVET HEAD BROKEN ON VERTICAL LEG OF CHORD. 2 L 7 3 4F RT A3WE 2001092500169 20010925 00169 NM 2001 9 25 DHL2001727595 1 20010824 A 5347 SEAT TRACK BOEING 727 727200 138407E NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON "C" CHECK DISCREPANCY. MAIN CABIN FLOOR SEAT TRACK AT BS 990 RBL 46 HAS 46 DENTS AND CHAFING MARKS, MKD. 2 L 7 3 4F RT A3WE 2001092500170 20010925 00170 NM 2001 9 25 DHL2001727596 1 20010817 A 5280 FITTING BOEING 727 727200 138407E NM RT MLG DOOR LOOSE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON "C" CHECK DISCREPANCY, RIGHT M.L.G. WING DOOR ACTUATING ARM HAS PLAY AT GIMBALL FITTING. 2 L 7 3 4F RT A3WE 2001092500171 20010925 00171 NM 2001 9 25 DHL2001727598 1 20010819 A 7110 COWLING BOEING 727 727200 138407E NM NR 3 NACELLE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON "C" CHECK DISCREPANCY-------NR 3 ENGINE, LOWER. COWLING, O/B SIDE, CLOSING ASSIST HALE, SKIN CRACKED. 2 L 7 3 4F RT A3WE 2001092500172 20010925 00172 NM 2001 9 25 USAA011171 1 20010830 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND FLOORBEAM CRACKED 3 INCH, BS 663 BL 0. INSTALLED DOUBLER, SPLICE PLATES AND STIFFENERS, PER T/R 57-10-04 AN D EA 69909. (M) 2 L 7 2 4F A16WE 2001092500173 20010925 00173 EU 2001 9 25 USAAF01071 1 20010904 A 3350 6104789 BATTERY FOKKER F28 F28MK0100 4990807 EU PAX CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 861US 11297 RDU - THE FLOOR STRIP EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK. (M) 2 L 7 2 4F RT 2001092500174 20010925 00174 WP 2001 9 25 AALA20011620 1 20010806 A 5300 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 215 CORRODED A AALA O OTHER O OTHER IN INSP/MAINT 1 SW 21 7518A 49895 TUL - FOUND CORROSION ON SEAT TRACK 6 AT STATION 215-216. INSTALLED NEW SECTION OF SEAT TRACK FROM STATION 215-304 IAW SRM 53-05. (M) 2 L 7 2 4F A6WE 2001092500175 20010925 00175 WP 2001 9 25 AALA20011621 1 20010807 A 5100 INTERCOSTAL DOUG DC9 DC982 3022082 WP BS 1291 CRACKED A AALA O OTHER O OTHER IN INSP/MAINT 1 SW 21 7518A 49895 TUL - FOUND INTERCOSTAL STATION 1291 BL0 CRACKED. REPLACED INTERCOSTAL PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2001092500176 20010925 00176 WP 2001 9 25 AALA20011623 1 20010807 A 5300 SKIN DOUG DC9 DC982 3022082 WP FS 235 DENTED A AALA O OTHER O OTHER IN INSP/MAINT 1 SW 21 7518A 49895 TUL - FOUND DENT IN FUSELAGE SKIN STATION 235 BETWEEN LONGERON 18L AND LONGERON 19L. INSTALLED .063 INCH 2024T3 DOUBLER PER SRM 53-04 FIG 12B. (M) 2 L 7 2 4F A6WE 2001092500177 20010925 00177 WP 2001 9 25 AALA20011624 1 20010807 A 5300 SKIN DOUG DC9 DC982 3022082 WP FS 232 DENTED A AALA O OTHER O OTHER IN INSP/MAINT 1 SW 21 7518A 49895 TUL - FOUND DENT IN FUSELAGE SKIN AT STATION 232 BETWEEN LONGERON 20L AND LONGERON 21L. CUT 1 INCH HOLE TO REMOVE DAMAG E INSTALLED .063 INCH 2024-T3 DOUBLER PER SRM 53-04 FIG 12B. (M) 2 L 7 2 4F A6WE 2001092500178 20010925 00178 WP 2001 9 25 AALA20011625 1 20010807 A 5300 SKIN DOUG DC9 DC982 3022082 WP FS 1318 DENTED A AALA O OTHER O OTHER IN INSP/MAINT 1 SW 21 7518A 49895 TUL - FOUND SMALL DENT ON FUSE BELOW RIGHT ENGINE ENGINE AT STATION 1318 BETWEEN LONGERON 19 AND 20R ADL NR 5180005. CU TOUT DAMAGE AREA, INSTALLED DOUBLER PER SRM 53-04-00 FIGURE 38 SHEET 23. (M) 2 L 7 2 4F A6WE 2001092500179 20010925 00179 WP 2001 9 25 AALA20011626 1 20010807 A 5300 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 205-237 CORRODED A AALA O OTHER O OTHER IN INSP/MAINT 1 SW 21 7518A 49895 TUL - FOUND CORROSION ON SEAT TRACK NR 5 SEVERAL AREAS STATION 205-237. INSTALLED NEW TRACK NR 5 STATION 200-240 PER SR M 53-05. (M) 2 L 7 2 4F A6WE 2001092500180 20010925 00180 WP 2001 9 25 AALA20011628 1 20010808 A 5300 SEAT TRACK DOUG DC9 DC982 3022082 WP FS 1200-1202 CORRODED A AALA O OTHER O OTHER IN INSP/MAINT 1 SW 21 7518A 49895 TUL - FOUND CORROSION ON NR 2 SEAT TRACK STATION 1200-1202. REPAIRED SEAT TRACK STATION 1182-1260 BY SPLICING NEW SEAT TRACK SECTION PER SRM 53-05 FIG 4. (M) 2 L 7 2 4F A6WE 2001092500181 20010925 00181 WP 2001 9 25 AALA20011629 1 20010808 A 5300 LONGERON DOUG DC9 DC982 3022082 WP FS 160 CRACKED A AALA O OTHER O OTHER IN INSP/MAINT 1 SW 21 7518A 49895 TUL - FOUND LONGERON 4L CRACKED AROUND FASTENERS AT STATION 160. REMOVED SECTION OF DAMAGED LONGERON. INSTALLED NEW SE CTION OF LONGERON AND DOUBLER PER SRM 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 2001092500182 20010925 00182 WP 2001 9 25 AALA20011631 1 20010804 A 5300 LONGERON DOUG DC9 DC983 3022083 WP FS 237 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 435AA 49453 TUL - FOUND LONGERON 17 LEFT CRACKED AT STATION 237 BEHIND FRAME. CUT OUT DAMAGED SECTION AND INSTALLED REPAIR PER SRM 53-02 FIGURE 18. (M) 2 L 7 2 4F RT A6WE 2001092500183 20010925 00183 WP 2001 9 25 AALA20011632 1 20010806 A 5300 LONGERON DOUG DC9 DC983 3022083 WP BS 160 CRACKED A AALA O OTHER O OTHER IN INSP/MAINT 1 SW 21 435AA 49453 TUL - FOUND CRACK AT FASTENER INBOARD FLANGE OF L4L AT STATION 160. CUT OUT CRACK, INSTALLED LONGERON SPLICE PER AARD 5 3-00-005 AND NEW END FITTING ON LONGERON. (M) 2 L 7 2 4F RT A6WE 2001092500184 20010925 00184 WP 2001 9 25 AALA20011633 1 20010806 A 5300 SEAT TRACK DOUG DC9 DC983 3022083 WP FS 1304 CORRODED A AALA O OTHER O OTHER IN INSP/MAINT 1 SW 21 435AA 49453 TUL - FOUND NR 1 SEAT TRACK CORRODED AT STATION 1304. REMOVED DAMAGED AREA OF NR 3 SEAT TRACK, ALODINED AND PRIMED AND INSTALLED SEAT TRACK PLUG PER SRM 53-05 FIG 4A. (M) 2 L 7 2 4F RT A6WE 2001092500185 20010925 00185 NM 2001 9 25 DHL2001727599 1 20010820 A 2150 65662451 DEFLECTOR BOEING 727 727200 138407E NM HEAT EXCHANGER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON "C" CHECK DISCREPANCY------PRIMARY HEAT EXCHANGER FAN DEFLECTOR FOR LT SIDE HAS NUMEROUS CRACKS. 2 L 7 3 4F RT A3WE 2001092500186 20010925 00186 NM 2001 9 25 DHL2001727600 1 20010820 A 2150 65662452 DEFLECTOR BOEING 727 727200 138407E NM HEAT EXCHANGER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON "C" CHECK DISCREPANCY-------- PRIMARY HEAT EXCHANGER FAN DEFLECTOR FOR RT SIDE HAS NUMEROUS CRACKS. 2 L 7 3 4F RT A3WE 2001092500187 20010925 00187 NM 2001 9 25 DHL2001727601 1 20010817 A 2150 DOOR BOEING 727 727200 138407E NM GROUND FAN LOOSE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON "C" CHECK DISCREPANCY------RIGHT PACK GROUND FAN COOLING DOOR HAS EXCESSIVE PLAY. 2 L 7 3 4F RT A3WE 2001092500188 20010925 00188 NM 2001 9 25 DHL2001727602 1 20010822 A 5310 65C330231 STRINGER BOEING 727 727200 138407E NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON "C" CHECK DISCREPANCY----- AFT. CARGO COMPARTMENT HAS CORROSION AT STRINGER L29 AND F/STATION 990 TO 1010. 2 L 7 3 4F RT A3WE 2001092500189 20010925 00189 NM 2001 9 25 DHL2001727603 1 20010818 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH ON "C" CHECK DISCREPANCY------- AFT. CARGO COMPARTMENT HALF FRAME STA. 980 P/H HAS CORROSION AT LWR. FLANGES. 2 L 7 3 4F RT A3WE 2001092500190 20010925 00190 NM 2001 9 25 DHL2001727610 1 20010821 A 2750 652661453 JACKSCREW BOEING 727 727200 138407E NM TE FLAPS LOOSE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK; LT WING INBD FLAP INBD JACKSCREW (NO.4)HAS EXCESSIVE PLAY AT UNIVERSAL BUSHINGS AND AT JACKSCREW TO YOKE ATT ACH BOLT. REMOVED AND REPLACED INBD FLAP JACKSCREW NR 4 AS PER DHL 727 M/M 27-51-41, RIGGED AND ADJUSTED FLAPS PER B727 M/M 27-51-1, OPS CHECK PER B727 M/M 27-51-0. REF: N/R 1682. 2 L 7 3 4F RT A3WE 2001092500191 20010925 00191 NM 2001 9 25 DHL2001727611 1 20010818 A 5753 BUSHING BOEING 727 727200 138407E NM TE FLAPS LOOSE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK; LT WING O/B FLAP HAS EXCESS PLAY WITH PWR ON, FLAPS UP. REMOVED AND REPLACED BUSHINGS AND BOLT AT FWD FLAP T RACK ATTACH POINT PER B727 M/M 27-51-31, OPS CK OK PER B727 M/M 27-51-0, NO EXCESS PLAY NOTED. REF: N/R 1660. 2 L 7 3 4F RT A3WE 2001092500192 20010925 00192 NM 2001 9 25 DHL2001727612 1 20010817 A 3213 STRUT BOEING 727 727200 138407E NM MLG WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CK; LEFT MLG OUTER CYLINDER SIDE STRUT LOWER SEGMENT SPINDLE ATTACH WORN OUT OF LIMITS. REMOVED AND REPLACED BUSHIN GS PER O/M 32-12-01, OPS CK GOOD ON GEAR RUN PER B727 M/M 32-11-0. REF: N/R 7158. 2 L 7 3 4F RT A3WE 2001092500193 20010925 00193 NM 2001 9 25 DHL2001727613 1 20010817 A 3213 STRUT BOEING 727 727200 138407E NM MLG WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CK; RIGHT MLG OUTER CYLINDER SIDE STRUT LOWER SEGMENT SPINDLE ATTACH WORN OUT OF LIMITS. REMOVED AND REPLACED BUSHI NGS PER O/M 32-12-01, OPS CK GOOD ON GEAR RUN PER B727 M/M 32-11-0. REF: N/R 7162. 2 L 7 3 4F RT A3WE 2001092500194 20010925 00194 NM 2001 9 25 DHL2001727614 1 20010824 A 5347 SEAT TRACK BOEING 727 727200 138407E NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CK; CABIN SEAT TRACK BETWEEN BS 756 TO 765, LBL 46 HAS WORN AREAS. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 51-10-6, REMOVED AND REPLACED THE CABIN SEAT TRACK PER B727 SRM 51-10-1 PARA.4 AND 51-30-2. REF: N/R 5187. 2 L 7 3 4F RT A3WE 2001092500195 20010925 00195 NM 2001 9 25 DHL2001727615 1 20010817 A 3213 BEARING BOEING 727 727200 138407E NM MLG STRUT WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK; RT MLG UPPER SEGMENT BEARING WORN BEYOND LIMITS. REMOVED RT MLG UPPER SEGMENT PER B727 M/M 32-11-41, REMOVED AND REPLACED UPPER AFT BEARING, FWD BUSHING, AND FWD BEARING PER B727 M/M 32-11-41, REMOVED AND REPLACED UPPER SEGMENT LINK ASSY. PER B727 M/M 32-11-41, GEAR SWING AND OPS CK FOUND GOOD, NO PLAY NOTED PER B727 M/M 32-11-00. REF: N/R 7150. 2 L 7 3 4F RT A3WE 2001092500196 20010925 00196 NM 2001 9 25 DHL2001727616 1 20010817 A 3213 SWIVEL BOEING 727 727200 138407E NM MLG STRUT WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CK; RIGHT MLG LOWER SEGMENT SWIVEL WORN BEYOND LIMITS. REMOVED AND REPLACED R/H MLG SIDE STRUT LOWER SEGMENT ASSY P ER B727 M/M 32-11-41, GEAR SWING AND OPS CHECK FOUND GOOD NO PLAY NOTED, PER 32-11-00. REF: N/R 7151. 2 L 7 3 4F RT A3WE 2001092500197 20010925 00197 NM 2001 9 25 DHL2001727617 1 20010820 A 2910 680005003 PCU BOEING 727 727200 138407E NM LT ELEVATOR LEAKING A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 2020204 ON "C" CHECK-----DISCREPANCY LT ELEVATOR HAS EVIDENCE OF HYDRAULIC LEAK BELOW THE PCU. 2 L 7 3 4F RT A3WE 2001092500198 20010925 00198 NM 2001 9 25 DHL2001727618 1 20010824 A 5347 SEAT TRACK BOEING 727 727200 138407E NM FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 ON "C" CHECK DISCREPANCY------- CABIN FLOOR TRACK BETWEEN BS 740 TO 762, BLOHAS WORN AREAS, MKD. 2 L 7 3 4F RT A3WE 2001092500199 20010925 00199 NM 2001 9 25 AWXA200100471 1 20010816 A 5311 6516300302 FRAME BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 MCN - C21 CK - C - BS 178 PRESS BULKHEAD 1.7 INCH CRACK CENTER OF RADIUS, RT CHORD, WL 207, RBL 24. MAINTENANCE REMOVED AND REPLACED THE RT SIDE CHORD IAW AWA ER 15-5311-01242-TB2. 2 L 7 2 4F RT A16WE 2001092500200 20010925 00200 SO 2001 9 25 C2XA01CL206 1 20010923 A 2530 CBC16707 RECEPTACLE EMB 145 EMB145LR SO GALLEY DEFECTIVE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 14916 145415 IAH FLIGHT 3740 THE CREW REPORTED A BURNING SMELL COMING FROM THE COFFEEMAKER. MAINTENANCE INSPECTED AND REPLACED THE H OT JUG RECEPTACLE. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2001092500201 20010925 00201 NM 2001 9 25 DL72S011513 1 20010909 A 2912 FILTER BOEING 727 727232 1384082 NM HYDRAULIC SYS DIRTY A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 531DA 21814 SYSTEM A O-HEAT LIGHT CAME ON JUST PRIOR TO CRUISE. REPLACED A-SYSTEM RETURN FILTER MODULE. 2 L 7 3 4F A3WE 2001092500202 20010925 00202 NM 2001 9 25 AWXA200100472 1 20010903 A 5320 143N5352 SHEAR TIE BOEING 757 757225 1384959 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 915AW 22209 SAT - C7 CK - "C" - FWD CARGO COMPARTMENT, BS 800, BL 0, FRAME SHEAR TIE CORRODED BEYOND SRM LIMITS. MAINTENANCE REMOVE D THE CORRODED SHEAR TIE AND FABRICATED A NEW SHEAR TIE IAW BOEING DRAWING 140N2002 AND INSTALLED IAW B757 SRM 51-40-02, FIG 3, PG 405. 2 L 7 2 4F RT A2NM 2001092500203 20010925 00203 NM 2001 9 25 AWXA200100473 1 20010901 A 5230 146N6603 SKIN BOEING 757 757225 1384959 NM #2 CARGO DOOR GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 915AW 22209 SAT - C7 CK - "C" - #2 CARGO DOOR INNER SKIN GOUGED ON AFT LOWER SIDE 10.5" FROM AFT EDGE AND 3.2" UP FROM LOWER EDGE, B EYOND SRM LIMITS. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER IAW B757 SRM 51-70-13, FIG 1, PG 1 &2. 2 L 7 2 4F RT A2NM 2001092500204 20010925 00204 NM 2001 9 25 DL72S011522 1 20010909 A 2730 65178234 MODULE BOEING 727 727232 1384082 NM ELEVATOR DAMAGED A DALA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 27 531DA 21814 ON LANDING ROLLOUT HYD SYS -A- PRESS AND QTY WENT TO ZERO. FOUND -A- SYS ELEV CONTROL MODULE DAMAGED. SOLENOID BLEW OU T OF THE TOP OF MODULE. REPLACED MODULE. 2 L 7 3 4F A3WE 2001092500205 20010925 00205 NM 2001 9 25 DL72S011546 1 20010917 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 542DA 22391 LT AND RT AFT SVC DOORS EXTERIOR EMERGENCY SLIDE LIGHTS INOP. RELAMPED, NO HELP. REPLACED BATTERY PACK. LIGHTS CK OK. 2 L 7 3 4F A3WE 2001092500206 20010925 00206 NM 2001 9 25 DL72S011547 1 20010917 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 542DA 22391 RT WING EXT OVERWING MID EMERGENCY LIGHT INOP. RELAMPED, NO HELP. REPLACED BATTERY PACK. LIGHTS CK OK. 2 L 7 3 4F A3WE 2001092500207 20010925 00207 NM 2001 9 25 DL72S011548 1 20010917 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 542DA 22391 RT OVERWING EXTERIOR AFT EMERGENCY LIGHT INOP. RELAMPED, NO HELP. REPLACED BATTERY PACK. LIGHT CKS OK. 2 L 7 3 4F A3WE 2001092500208 20010925 00208 NM 2001 9 25 DL72S011555 1 20010918 A 3350 BATTERY BOEING 727 727225A 1384077 NM AIRSTAIRS DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8890Z 21859 AIRSTAIRS EMERGENCY LIGHT INOP. REPLACED BATTERIES, OPS NORMAL NOW. 2 L 7 3 4F RT A3WE 2001092500209 20010925 00209 NM 2001 9 25 DL72W011512 1 20010907 A 5730 570206003 PANEL BOEING 727 727247 138408F NM RT WING MISSING A DALA K NONE D INFLIGHT SEPARATION TO TAKEOFF 1 SO 27 2820W 21058 PANEL ON TOP OF RT WING TIP NAV LIGHT IS MISSING. REPLACED SAME. 2 L 7 3 4F A3WE 2001092500210 20010925 00210 NM 2001 9 25 DHL2001727619 1 20010818 A 5523 BEARING BOEING 727 727200 138407E NM LT ELEVATOR TAB WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 ON "C" CHECK DISCREPANCY------ LT ELEVATOR TAB HINGE BEARING WORN, FITTINGS CORRODED. 2 L 7 3 4F RT A3WE 2001092500211 20010925 00211 NM 2001 9 25 DL733011509 1 20010908 A 2560 61020 BATTERY BOEING 737 737347 1384647 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 313WA 23599 LWR EMERGENCY FLASHLIGHT AT AFT JUMPSEAT INOP. REPLACED BATTERY AND BRACKET. 2 L 7 2 4F RT A16WE 2001092500212 20010925 00212 EU 2001 9 25 01FDEA00854 1 20010921 A 3230 DETECTOR AIRBUS 310 A310222 3930315 EU PROXIMITY FAILED A FDEA B EMER. DESCENT S AFFECT SYSTEMS TO TAKEOFF 1 SO 25 422FE 346 01-320 SYS 1 LAND GEAR FAIL TO RETRACT. R&R PROXIMITY DETECTOR PER 32-00-00. 2 L 7 2 4F RT A35EU 2001092500213 20010925 00213 NM 2001 9 25 DHL2001727620 1 20010818 A 5523 BEARING BOEING 727 727200 138407E NM RT ELEVATOR TAB WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 ON "C" CHECK DISCREPANCY------- RT ELEVATOR TAB HINGE BEARINGS WORN, FITTINGS CORRODED. 2 L 7 3 4F RT A3WE 2001092500214 20010925 00214 NM 2001 9 25 DL733011557 1 20010918 A 2560 BPS73 POWER SUPPLY BOEING 737 73735B NM CABIN DEFECTIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 222DZ 23971 AFT CABIN EMERGENCY LIGHT INOP. RELAMPED, NO HELP. REPLACED PWR SUPPLY AND BATTERY, OP CKS GOOD. 2 L 7 2 4F RT A16WE 2001092500215 20010925 00215 NM 2001 9 25 DL738011549 1 20010917 A 3350 387 LIGHT BOEING 737 737832 13844CF NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 3757D LEFT AFT LOWER EXTERIOR EMERGENCY LIGHT AFT OF WING IS INOP. RELAMPED, CHECKS OK. 2 L 7 2 4F RT A16WE 2001092500216 20010925 00216 NM 2001 9 25 DHL2001727621 1 20010818 A 5523 SKIN BOEING 727 727200 138407E NM RT ELEVATOR TAB DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 ON "C" CHECK DISCREPANCY------ RT ELEVATOR TAB T/E DELAMITED. 2 L 7 3 4F RT A3WE 2001092500217 20010925 00217 NM 2001 9 25 DL73K011487 1 20010905 A 7120 FITTING BOEING 737 737232 1384475 NM PYLON WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 318DL 23090 SUBJECT FWD ENGINE MOUNT SUPPORT FITTING ASSY WAS FOUND WITH OVERSIZED MOUNT HOLES. REPAIR PER ER/A 410315-14AD. 2 L 7 2 4F RT A16WE 2001092500218 20010925 00218 NM 2001 9 25 DL73K011510 1 20010908 A 3397 WIRE BOEING 737 737247 138448D NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 239WA 23187 EMERGENCY LIGHT INOP AT 16D. REPAIRED BROKEN WIRE. 2 L 7 2 4F A16WE 2001092500219 20010925 00219 NM 2001 9 25 DL73K011515 1 20010909 A 2611 WIRE BOEING 737 737247 138448D NM LAVATORY BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 238WA 23186 FWD LAV UNDERSINK COUNTER SMOKE DETECTOR UNIT WOULD NOT TEST. REPAIRED BROKEN WIRE CONNECTOR AT TEST SWITCH. 2 L 7 2 4F A16WE 2001092500220 20010925 00220 NM 2001 9 25 DL73K011534 1 20010915 A 3320 61482 BALLAST BOEING 737 737232 1384475 NM LAVATORY DEFECTIVE A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 328DL 23100 WHILE AT GATE WAITING FOR MTC ON A/C BLACK/GRAY SMOKE POURED OUT OF P18-1 PANEL. FLT CREW SHUT DOWN A/C POWER. FOUND B ALLAST FOR FWD LAV MIRROR TO BE SOURCE OF SMOKE. REPLACED BALLAST. 2 L 7 2 4F RT A16WE 2001092500221 20010925 00221 NM 2001 9 25 DL757011471 1 20010904 A 2822 PUMP BOEING 757 757232 1384965 NM CTR FUEL TANK FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 656DL 24396 APPROXIMATELY 25 MINUTES INTO FLIGHT WITH 5,100 LBS IN CENTER FUEL TANK, RIGHT CENTER LOW PRESSURE LIGHT ILLUMINATED. T WO MINUTES LATER LEFT CENTER LOW PRESSURE LIGHT ILLUMINATED. ACCOMPLISHED POM, TURNED OFF PUMPS. INSPECTED INLET LINES AND PRESSURE LINES. NO CRACKS OR OBSTRUCTIONS FOUND. NO TRASH FOUND IN TANK REPLACED CNTR/LEFT PUMP MOTOR AND PRESS S WITCH. REPLACED CTR RT FUEL PUMP MOTOR AND PRESSURE SWITCH. 2 L 7 2 4F RT A2NM 2001092500222 20010925 00222 NM 2001 9 25 DHL2001727622 1 20010818 A 5523 SKIN BOEING 727 727200 138407E NM LT ELEVATOR TAB DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 ON "C" CHECK DISCREPANCY----- LT ELEVATOR TAB T/E DELAMINATED. 2 L 7 3 4F RT A3WE 2001092500223 20010925 00223 NM 2001 9 25 DL757011493 1 20010906 A 2910 SWITCH BOEING 757 757232 1384965 NM COCKPIT ARCED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 6713Y 30777 ON PUSHBACK HAD ELECTRICAL MALFUNCTION. ELECTRICAL SMOKE INDICATOR LIGHT C/B POPPED AND CENTER NR 2 HYDRAULIC C/B POPPE D. FOUND C2 HYD PUMP SWITCHLIGHT STUCK IN. UPON PANEL REMOVAL FOUND EVIDENCE OF ARCING/BURNING ON SWITCH HOUSING. REP LACED HYD PUMP SWITCHES PANEL M10050 AND ALL OK. 2 L 7 2 4F RT A2NM 2001092500224 20010925 00224 NM 2001 9 25 DL757011503 1 20010907 A 3320 1142691B LENS BOEING 757 757232 1384965 NM GALLEY MELTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 661DN 24972 DURING CRUISE A BURNING ODOR WAS NOTICED IN MID GALLEY. A/C DIVERTED TO MEM. CONTRACT MTC UNABLE TO LOCATE SOURCE OF O DOR. ATL MTC WENT TO MEM AND FOUND THE BEZEL ASSY ON THE MID GALLEY OVERHEAD WORK LIGHT BURNT/MELTED. REPLACED SAME. A/C OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2001092500225 20010925 00225 NM 2001 9 25 DL757011505 1 20010907 A 3350 SIGN BOEING 757 757232 1384965 NM R1 DOOR DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 627DL 22917 R1 DOOR EMERGENCY LIGHTING EXIT SIGN IS DAMAGED. REPLACED LIGHT ASSY, CHECKS OK. 2 L 7 2 4F RT A2NM 2001092500226 20010925 00226 WP 2001 9 25 ERKR200100165 1 20010830 A 2740 591096229 JACKSCREW DOUG DC9 DC915 3022036 WP HORIZ STAB OUT OF TOLERANCE B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 915 7359 47061 HORIZONTAL STABILIZER JACKSCREW ENDPLAY AND FREEPLAY CHECK FOUND THAT THE ENDPLAY WAS OUT OF LIMITS. REMOVED AND REPLAC ED THE HORIZONTAL STABILIZER JACKSCREW. 2 L 7 2 4F A6WE 2001092500227 20010925 00227 CE 2001 9 25 GLBA2001206 1 20010920 A 2422 SPC10 INVERTER BEECH 1900 1900D 1154162 CE LEFT MALFUNCTIONED A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 01 204GL 139 UE204 CAPTAINS EADI FLICKERS. REPLACED INVERTER, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001092500228 20010925 00228 2001 9 25 GLBA2001207 4 20010920 A 3418 VANE BEECH 1900 1900D 1154162 CE STALL WARNING DIRTY A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 01 247GL UE247 STALL WARNING WOULD NOT SILENCE. CLEANED STALL VANE, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001092500230 20010925 00230 NM 2001 9 25 SCNA01711 1 20010821 A 2612 WARNING HORN BOEING 727 7272K3 138400D NM NLG WW INOPERATIVE A SCNA K NONE L NO TEST UK UNKNOWN 1 GL 15 291SC 22770 NOSE WHEEL WELL APU FIRE WARNING HORN INOPERATIVE. CORRECTED BY THE REMOVAL AND REPLACEMENT OF THE APU FIRE WARNING HOR N. 2 L 7 3 4F RT A3WE 2001092500231 20010925 00231 NM 2001 9 25 SWAA012576 1 20010917 A 3350 610478 BATTERY BOEING 737 7377H4 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 776WN 30591 DURING SCHEDULED C4 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001092500232 20010925 00232 NM 2001 9 25 SWAA012581 1 20010917 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIPS CRACKED (4 EACH) AT BS 827, STR 23L, 24L, 26L & 27L. REMOVED AND REPL ACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001092500233 20010925 00233 NM 2001 9 25 SWAA012587 1 20010919 A 5315 6545669 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 524SW 26566 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 21 & WL 208. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2001092500234 20010925 00234 NM 2001 9 25 SWAA012588 1 20010919 A 5520 6976419 HINGE BOEING 737 7373H4 1384600 NM LT & RT ELEVATOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 652SW 27722 DURING SCHEDULED C4 CHECK, FOUND LT & RT ELEVATORS OUTBOARD HINGES LOOSE. REMOVED AND REPLACED ELEVATOR HINGE PLATE ASS Y'S PER MM. 2 L 7 2 4F RT A16WE 2001092500235 20010925 00235 NM 2001 9 25 SWAA012590 1 20010919 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001092500236 20010925 00236 2001 9 25 SWAA012591 4 20010918 A 2565 22022900131 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001092500237 20010925 00237 2001 9 25 SWAA012592 4 20010918 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT DOORS OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 063SW 22061 DURING SCHEDULED C1 CHECK, FOUND BOTH AFT DOORS EMERGENCY EVAC SLIDES PRESS IND OUT OF VIEW. REPOSITIONED SLIDES PER MM . 2 L 7 2 4F A16WE 2001092500238 20010925 00238 2001 9 25 SWAA012599 4 20010919 A 2565 61620468 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001092500239 20010925 00239 NM 2001 9 25 SWAA012603 1 20010920 A 3213 65461083 BEAM BOEING 737 7373H4 1384600 NM LT MLG WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED A2 CHECK, FOUND LT MLG WALKING BEAM I/B BEARING MIGRATED 3/16. REMOVED AND REPLACED WALKING BEAM PER M M. 2 L 7 2 4F RT A16WE 2001092500240 20010925 00240 NM 2001 9 25 SWAA012610 1 20010921 A 3350 300432 LIGHT BOEING 737 7377H4 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 761RR 27875 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR LOWER EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT AS SY PER MM. 2 L 7 2 4F RT A16WE 2001092500241 20010925 00241 NM 2001 9 25 SWAA012613 1 20010922 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 384SW 26590 EEPLS LOOSE AT SEVERAL LOCATIONS IN CABIN. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001092500242 20010925 00242 2001 9 25 SWAA012614 4 20010921 A 2565 22022901 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED E VAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001092500243 20010925 00243 NM 2001 9 25 SWAA012615 1 20010923 A 5250 65C33828 PANEL BOEING 737 7375H4 138449D NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 528SW 26570 COCKPIT DOOR EMERGENCY BLOW-OUT PANEL FELL OUT. INSTALLED PANEL PER MM. 2 L 7 2 4F RT A16WE 2001092500244 20010925 00244 NM 2001 9 25 SWAA012618 1 20010920 A 5753 6546481 CARRIAGE BOEING 737 7372H4 138448C NM RT WING BROKEN A SWAA K NONE F FLT CONT AFFECTED CR CRUISE 1 SW 07 083SW 22732 WITH AIRCRAFT TRIMMED AT 280 KTS 13 DEGREES OF AILERON TRAVEL WAS NEEDED. FOUND RT WING OTBD FLAP CARRIAGE SPINDLE SHEA RED. REMOVED AND REPLACED RT WING OTBD CARRIAGE ASSY PER MM. 2 L 7 2 4F A16WE 2001092500245 20010925 00245 NM 2001 9 25 SWAA012619 1 20010920 A 2760 6546360 CONTROLLER BOEING 737 7373H4 1384600 NM MLG W/W FAULTY A SWAA K NONE F FLT CONT AFFECTED CR CRUISE 1 SW 07 362SW 26573 AILERONS HEAVY AND WOULD NOT RETURN TO NORMAL. REMOVED AND REPLACED SPOILER MIXER AND AILERON CENTERING CAM BEARING PER MM. 2 L 7 2 4F RT A16WE 2001092500246 20010925 00246 NM 2001 9 25 SWAA012623 1 20010922 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM SERVICE DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F A16WE 2001092500247 20010925 00247 NM 2001 9 25 SWAA012624 1 20010922 A 3350 BR2013 LIGHT BOEING 737 7377H4 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 708SW 27842 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT ROW 8. RELAMPED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001092500248 20010925 00248 NM 2001 9 25 SWAA012625 1 20010921 A 3350 6104789 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001092500249 20010925 00249 2001 9 25 SWAA012626 4 20010922 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 511SW 24188 DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED E VAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001092500250 20010925 00250 2001 9 25 XN0A01022 4 20010919 A 2311 UHF COMM AIRBUS 300 A300B4203 3930306 EU COCKPIT INOPERATIVE A TC8A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 472AS 125 NUMBER 2 RADIO DOES NOT TRANSMIT. TRANSFERRED NR 2 UHF COMM TRANSMIT TO DMI LOG IAW ENA MEL 23-10-01. 2 L 7 2 4F RT A35EU 2001092500251 20010925 00251 NM 2001 9 25 DL757011507 1 20010907 A 2120 ODOR BOEING 757 757232 1384965 NM CABIN DETECTED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 661DN 24972 ABOUT 3 HRS INTO FLT THE PASSENGERS AND FLT ATTENDANTS REPORTED AN ODOR IN THE AFT CABIN. ODOR STRONGEST AROUND ROWS 30 AND 31. SHUT OFF THE UTILITY BUSES AND RT RECIRC FAN AND CREW REPORTED THE ODOR BEGAN TO DISSIPATE. ODOR WAS REPORTE D AS SMELLING LIKE A PLASTIC SMELL. NEVER SMELLED ODOR FROM OR IN THE COCKPIT. POWERED UTILITY BUSES. TURNED ALL CABI N LIGHTS ON, RAN RECIRC FANS FOR SEVERAL MINUTES. NO ODOR AND NO HISTORY. 2 L 7 2 4F RT A2NM 2001092500252 20010925 00252 WP 2001 9 25 ABXA010499 1 20010914 A 3241 42241 CONTROL UNIT DOUG DC8 DC863 302198A WP FUSELAGE DEFECTIVE A ABXA K NONE O OTHER LD LANDING 1 GL 23 826AX 84207 2032 46061 ANTI-SKID CONTROL PANEL RIGHT AND LEFT INBOARD LIGHTS ILLUMINATED ON LANDING. REDUCED BRAKING WAS EXPERIENCED ON LANDING ROLL OUT. MAINTENANCE INSPECTED AND DEFERRED THE ANTI-SKID SYSTEM IAW DC-8 MEL 32-1. LATER ON 09/15/01 THE ANTI-SKID CO NTROL UNIT WAS REPLACED AND THE DEFERRAL WAS REMOVED. 2 L 7 4 4F 4A25 2001092500253 20010925 00253 NM 2001 9 25 DL757011542 1 20010916 A 3397 WIRE BOEING 757 757232 1384965 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 693DL 29725 EMERGENCY LIGHT 2CD INOPERATIVE. REPAIRED BROKEN WIRE. 2 L 7 2 4F RT A2NM 2001092500254 20010925 00254 WP 2001 9 25 MWEA011275 1 20010920 A 5310 49122621 LONGERON DOUG DC9 DC932 3022066 WP STATION 794 GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 AFT CARGO BAY LONGERON 26 LEFT IS GOUGED AT STATION 794 -- FABRICATED AND INSTALLED LONGERON AND SPLICES. 2 L 7 2 4F A6WE 2001092500255 20010925 00255 WP 2001 9 25 MWEA011277 1 20010920 A 5310 99582387 FRAME DOUG DC9 DC932 3022066 WP STATION 980 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 FRAME CRACKED AT STATION 980 LONGERON RIGHT -- FABRICATED AND INSTALLED FRAME SPLICE, LONGERON ANGLE AND FILLER FRAME MATERIALS. 2 L 7 2 4F A6WE 2001092500256 20010925 00256 WP 2001 9 25 MWEA011278 1 20010920 A 5310 3924050501 LONGERON DOUG DC9 DC932 3022066 WP STATION 560 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 LONGERON 28 LEFT CRACKED STATION 560 -- REMOVED AND REPLACED LONGERON. 2 L 7 2 4F A6WE 2001092500257 20010925 00257 NM 2001 9 25 2001F00364 1 20010814 A 7830 DEFLECTOR BOEING 757 757* NM THRUST REVERSER DEPARTED A N8TA K NONE O OTHER CL CLIMB 1 WP 19 508NA 26244 AFTER DEPARTURE OF AIRCRAFT A PORTION OF THE THRUST REVERSER DEFLECTOR BOX ASSEMBLY WAS FOUND ON RUNWAY. INVESTIGATION UPON ARRIVAL OF AIRCRAFT AT NEXT STATION REVEALED CENTER PORTION OF THE NR 1 DEFLECTOR BOX ASSEMBLY MISSING, THERE WERE NO UNUSUAL INDICATIONS ON THE PREVIOUS OR SUBSEQUENT LANDING. (M) 2 L 7 2 4F RT A2NM 2001092500258 20010925 00258 NE 2001 9 25 2001F00365 2 20010823 A 7421 9550168760 IGNITER SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE FAILED A KBMA K NONE O OTHER NR NOT REPORTED 1 WP 19 37SH 2300 FOUND ENGINE IGNITER HAS INSUFFICIENT SPARK. REPLACED WITH NEW IGNITER. (M) 1 G 7 1 3U 3 U NC H9EU E19EU 2001092500259 20010925 00259 SW 2001 9 25 2001F00366 1 20010826 A 2841 INDICATOR BELL 206 206B 1181511 SW INSTRUMENT PNL DEFECTIVE A KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 667JM 3444 FUEL GAUGE REPORTED TO BE STICKING. NEW FACTORY INSTALLED. (M) 1 G 7 1 3U H2SW 2001092500260 20010925 00260 EU 2001 9 25 2001F00367 1 20010824 A 2150 BELT SNIAS 350 AS350B2 8680813 EU AIR CONDITIONER BROKEN A KBMA O OTHER O OTHER CR CRUISE 1 WP 19 345SH 3345 AIR CONDITIONER BELT BROKE IN FLIGHT. REPLACED WITH NEW BELT. (M) 1 G 7 1 3U H9EU 2001092500261 20010925 00261 EU 2001 9 25 2001F00368 1 20010822 A 2150 420800022 MOTOR SNIAS 350 AS350BA 8680817 EU CABIN FAILED A KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 270SH 8236 1864 AIR CONDITIONING BLEW WARM AIR. REPLACED WITH SERVICEABLE UNIT. (M) 1 G 7 1 3U NC H9EU 2001092500262 20010925 00262 NM 2001 9 25 DHL2001727623 1 20010819 A 7110 SKIN BOEING 727 727200 138407E NM NR 3 COWLING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 ON "C" CHECK DISCREPANCY------- NR 3 ENGINE LOWER COWLING , O/B SIDE, OUTER SKIN CRACKED/ BENT AROUND 3RD U-BOLT CUT-OUT . 2 L 7 3 4F RT A3WE 2001092500263 20010925 00263 EU 2001 9 25 MALA010723 1 20010918 A 2420 51634002 GCU SAAB SF340 SF340A 7850100 EU CT7TP CT75A 30030 NE DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 068XJ 068 During Flight # 2806, RH AC Gen Inop. Maitenance cleaned contaminated connector at RH AC Gen GCU and replaced RH AC GCU PN 51634-002, SN/off 97018, SN/on 98023. IAE Saab SF340 AMM 24-21-10-2. Ops check good. 2 L 7 2 4T 4 T RT A52EU E8NE 2001092500264 20010925 00264 SO 2001 9 25 COMA0110144 1 20010924 A 6123 SEDLOC2R GAUGE EMB 120 EMB120RT SO COCKPIT FAULTY A COMA D RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 259CA 13630 1252 FLIGHT #5062. DURING TAKE OFF FROM NAS THE RIGHT ENGINE PROPELLER AUTO FEATHERED AT 80 KNOTS, ABORTED TAKE OFF AND RETU RNED TO THE GATE.REPLACED THE RIGHT ENGINE TORQUE GAUGE. 2 L 7 2 4T RT A31SO 2001092500265 20010925 00265 EA 2001 9 25 COMA0160748 1 20010917 A 5300 601R3114879 THRESHOLD CNDAIR CL600 CL6002B19 EA 310.00 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 969CA 11964 7141 THE THRESHOLD/SILL PANEL FORWARD OF THE SERVICE DOOR IS CORRODED.REMOVED CORRODED THRESHOLD AND REPLACED WITH FABED THRE SHOLD I/A/W WVAC EO 601R-53-2716. 2 L 7 2 4F RT A21EA 2001092500266 20010925 00266 EA 2001 9 25 COMA0160749 1 20010924 A 2751 855D1009 BPSU CNDAIR CL600 CL6002B19 EA RIGHT WING FAULTY A COMA K NONE J WARNING INDICATION DE DESCENT 1 SO 01 965CA 11920 7131 FLIGHT #5650. DURING DESCENT INTO SRQ RECEIVED A FLAP FAIL CAUTION MESSAGE WITH FLAPS AT 20 DEGREES.REPLACED THE BRAKE AND POSITIONING SENSING UNIT. 2 L 7 2 4F RT A21EA 2001092500267 20010925 00267 EU 2001 9 25 2001F00370 1 20010824 A 2150 AM7017 MOTOR SNIAS 350 AS350* EU A/C CONDENSER INOPERATIVE A KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 115SH 3141 AIR CONDITIONING CONDENSER MOTOR DID NOT OPERATE. INSTALLED SERVICEABLE MOTOR. (M) 1 G 7 1 3U H9EU 2001092500268 20010925 00268 EU 2001 9 25 2001F00371 1 20010730 A 2121 050021 MOTOR SNIAS 350 AS350BA 8680817 EU CABIN NOISY A KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 37SH 2300 FOUND MOTOR REPORTED TO BE MAKING NOISE. REMOVED AND REPLACED WITH NEW MOTOR. (M) 1 G 7 1 3U NC H9EU 2001092500269 20010925 00269 2001 9 25 2001F00372 4 20010807 A 2312 064105430 VHF COMM SNIAS 350 AS350BA 8680817 EU COCKPIT FAULTY A KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 350SH 2957 RADIO HAS STATIC AND NO DISPLAY. REPLACED WITH SERVICEABLE UNIT. (M) 1 G 7 1 3U NC H9EU 2001092500270 20010925 00270 EA 2001 9 25 COMA0160750 1 20010923 A 2410 IDG CNDAIR CL600 CL6002B19 EA A COMA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 988CA 7204 FLIGHT #5594. DURING TAKE OFF ROLL AT MKE GENERATOR #1 DROPPED OFF LINE ACCOMPANIED BY AN IDG CAUTION MESSAGE, ABORTED TAKE OFF AT 60 KNOTS AND RETURNED TO THE GATE.SERVICED THE #1 INTEGRATED DRIVE GENERATOR WITH OIL. 2 L 7 2 4F RT A21EA 2001092500271 20010925 00271 NM 2001 9 25 AALA20011563 1 20010803 A 3350 S479W2302 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 771AN 29579 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY LIGHT ON G3 GALLEY INOPERATIVE. REPLACED LAMP ASSEMBLY. SYSTEM G ROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001092500272 20010925 00272 EU 2001 9 25 AALA20011568 1 20010804 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 41063 506 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT AT FIRST CLASS BULKHEAD LEFT SIDE INOPERATIVE. SECURED LIGHT ASSEMB LY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2001092500273 20010925 00273 WP 2001 9 25 AALA20011589 1 20010805 A 2611 SWITCH DOUG DC9 DC982 3022082 WP SMOKE DETECTOR DIRTY A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 491AA 49684 ORD - DURING OVERNIGHT MAINTENANCE, AFT LAVATORY SMOKE ALARM RINGS CONTINUOUSLY. CLEANED TEST SWITCH. SYSTEM GROUND CH ECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001092500274 20010925 00274 EU 2001 9 25 AALA20011598 1 20010806 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 41063 506 JFK - DURING OVERNIGHT MAINTENANCE, INTERIM REPAIR PREVIOUSLY ACCOMPLISHED ON FIRST CLASS EMERGENCY LIGHT. REPLACED LIG HT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2001092500275 20010925 00275 NM 2001 9 25 AALA20011605 1 20010724 A 5511 SPAR CAP BOEING 727 727227 1384078 NM HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 716AA 20608 TUL - FOUND LEFT HORIZONTAL STAB, REAR SPAR CAP EXTENSION, ON AFT END, HAD CORROSION ABOVE NR 1 ELEVATOR HINGE. INSTALL ED DOUBLER AND FILLER REPAIR PER ESO 11697 DATED 7-23-2001. (M) 2 L 7 3 4F A3WE 2001092500276 20010925 00276 NM 2001 9 25 AALA20011607 1 20010727 A 5310 DOOR FRAME BOEING 727 727227 1384078 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 716AA 20608 TUL - FOUND LEFT AFT GALLEY DOOR FORWARD JAMB CRACKED AT TOP FORWARD SIDE. STOP DRILLED CRACK INSTALLED DOUBLER PER ES O 11697 DATED 7-26-2001. (M) 2 L 7 3 4F A3WE 2001092500277 20010925 00277 EA 2001 9 25 COMA0160751 1 20010924 A 3150 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 810CA 7370 FLIGHT 5420. DURING TAKE OFF AT YYZ RECEIVED MULTIPLE AURAL WARNINGS, ABORTED TAKE OFF AT 65 KNOTS AND RETURNED TO THE GATE. RESET CIRCUIT BREAKER H7 ON CBP-1. 2 L 7 2 4F RT A21EA 2001092500278 20010925 00278 NM 2001 9 25 AALA20011610 1 20010808 A 5330 BEAR STRAP BOEING 727 727223 1384074 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 870AA 21382 TUL - FOUND LOW FREQUENCY EDDY CURRENT INDICATES CRACK PROGRESSING FROM FASTENER ON AFT LWR FORWARD GALLEY DOOR CUTOUT. TRIMMED OUT DAMAGE AT BARE STRAP AND INSTALLED DOUBLER/TRIPLER PER SB 727-53-188 FIG 3. (M) 2 L 7 3 4F A3WE 2001092500279 20010925 00279 WP 2001 9 25 AALA20011616 1 20010802 A 5310 RING DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7518A 49895 TUL - FOUND WINDOW RING PAN CRACKED STATION 599 RIGHT SIDE LOWER FORWARD CORNER. TRIMMED OUT CRACK AND INSTALLED DOUBLE R PER AARD 53-10-00-25. (M) 2 L 7 2 4F A6WE 2001092500280 20010925 00280 WP 2001 9 25 AALA20011617 1 20010802 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7518A 49895 TUL - FOUND CORROSION ON SEAT TRACK NR 3 AT 1302-1303. FABRICATED AND INSTALLED NEW TRACK STATION 1260-1309 PER SRM 53- 05. (M) 2 L 7 2 4F A6WE 2001092500281 20010925 00281 WP 2001 9 25 AALA20011618 1 20010803 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE PUNCTURED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7518A 49895 TUL - FOUND LEFT CUSP PUNCTURED BELOW GALLEY TIE DOWN NR 1 SEAT TRACK STATION 1236. INSTALLED DOUBLER PER SRM 53-01 FIG 4-3. ROUTED OUT NR 1 SEAT TRACK FOM (CUSP REPAIR). INSTALLED SEAT TRACK PLUG REPAIR PER SRM 53-05 FIG 4A. (M) 2 L 7 2 4F A6WE 2001092500282 20010925 00282 WP 2001 9 25 AALA20011619 1 20010803 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7518A 49895 TUL - FOUND AFT CARGO DOOR JAMB BEAM IS CORRODED FROM STATION 1159 TO STATION 1208, ONE SMALL AREA BEYOND LIMITS AFTER C ORROSION REMOVAL. INSTALLED SRO9520008-15 DOUBLER PER AARD 53-10-00-3. (M) 2 L 7 2 4F A6WE 2001092500283 20010925 00283 WP 2001 9 25 AALA20011622 1 20010807 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7518A 49895 TUL - FOUND SLIGHT CREASE IN LEFT SIDE OF FUSELAGE SKIN 36 INCHES AFT AND 18 INCHES DOWN FROM FORWARD ENTRY DOOR. INSTA LLED DOUBLER PER SRM 53-04 FIG 12B. (M) 2 L 7 2 4F A6WE 2001092500284 20010925 00284 WP 2001 9 25 AALA20011627 1 20010808 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7518A 49895 TUL - FOUND DENT IN LEFT CUSP OUTBOARD OF LIGHTENING HOLE STATION 1244. INSTALLED DOUBLER PER SRM 53-04. (M) 2 L 7 2 4F A6WE 2001092500285 20010925 00285 WP 2001 9 25 AALA20011634 1 20010807 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 435AA 49453 TUL - FOUND STATION 446-448, LEFT CUSP CORRODED, TOP SIDE ALSO 1 INCH CRACK IN LEFT CUSP STATION 446-448. INSTALLED DOU BLER PER SRM 53-01 FIG 4. (M) 2 L 7 2 4F RT A6WE 2001092500286 20010925 00286 WP 2001 9 25 AALA20011644 1 20010808 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7518A 49895 TUL - FOUND RIGHT CUSP CORRODED BETWEEN LIGHTENING HOLES STATION 1236-1238. INSTALLED DOUBLER ON CUSP PER SRM 53-01. ( M) 2 L 7 2 4F A6WE 2001092500287 20010925 00287 WP 2001 9 25 AALA20011645 1 20010808 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE PUNCTURED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7518A 49895 TUL - FOUND LEFT CUSP HAS PUNCTURE BELOW GALLEY TIE DOWN STATION 1207 BELOW NR 1 SEAT TRACK. INSTALLED DOUBLER PER SRM 53-01 FIG 4-3. ROUTED SEAT TRACK FOM NR 1 STATION 1207. INSTALLED SEAT TRACK PLUG PER SRM 53-05 FIG 4A. (M) 2 L 7 2 4F A6WE 2001092500288 20010925 00288 NM 2001 9 25 AALA20011647 1 20010817 A 3350 LIGHT BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 322AA 22323 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR LIGHT AFT OF MID GALLEY ON RIGHT SIDE INOPERATIVE. REPLACED LI GHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001092500289 20010925 00289 WP 2001 9 25 AALA20011657 1 20010820 A 2170 22D10 COALESCER BAG DOUG DC9 DC982 3022082 WP A/C BAY CONTAMINATED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 426AA 49338 SJC - FLT 1549 - SJC-SAN, AIR INTERRUPTED DUE TO SMOKE IN CABIN. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED CONICAL CO NDENSER, CLEAN DUCTS, AND ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001092500290 20010925 00290 WP 2001 9 25 AALA20011658 1 20010820 A 2910 HYDRAULIC SYSTEM DOUG DC9 DC982 3022082 WP TAIL LEAKING A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 462AA 49592 DFW - FLT 692 - SIX MINUTES AFTER LANDING AIR CONDITIONING PACK BEGAN EMITTING AN ACRID ODOR AND SMOKE APPEARED SHORTLY AFTERWARDS. PACKS WERE SHUTDOWN. REPAIRED HYDRAULIC LEAK AT TAIL. REPLACED WATER FILTER BAGS AND ACCOMPLISHED PACK BU RNOUT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001092500291 20010925 00291 WP 2001 9 25 AALA20011661 1 20010807 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 435AA 49453 TUL - FOUND CORROSION ON LEFT CUSP AT CLIP STATION 640. INSTALLED DOUBLER PER AARD 53-00-00-02. (M) 2 L 7 2 4F RT A6WE 2001092500292 20010925 00292 NM 2001 9 25 AALA20011662 1 20010816 A 5510 BEAM BOEING 727 727223 1384074 NM HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 885AA 21524 TUL - FOUND CORROSION UPPER RIGHT HORIZONTAL T/E BEAM 3RD ELEVATOR HINGE IN FROM TIP. REPAIRED CORROSION AREA AS PER ES O 11697, 8-16-2001. (M) 2 L 7 3 4F A3WE 2001092600001 20010926 00001 NM 2001 9 26 DHL2001727624 1 20010817 A 3230 SWIVEL BOEING 727 727200 138407E NM MLG WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 ON "C" CHECK DISCREPANCY---------- LEFT MLG SIDESTRUT LOWER SEGMENT SWIVEL WORN OUT OF LIMITS. 2 L 7 3 4F RT A3WE 2001092600002 20010926 00002 NM 2001 9 26 DHL2001727625 1 20010828 A 5320 FLOOR SUPPORT BOEING 727 727200 138407E NM COCKPIT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 ON "C" CHECK DISCREPANCY AFT. CARGO COCKPIT FLOOR SUPPORT BLKT CRACKED STA. 970 OVER 27R. 2 L 7 3 4F RT A3WE 2001092600003 20010926 00003 NM 2001 9 26 DHL2001727626 1 20010828 A 5320 FLOOR SUPPORT BOEING 727 727200 138407E NM CARGO BAY DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 ON "C" CHECK DISCREPANCY------ AFT. CARGO FLOOR SUPPORT STRAP AT BS 991 LT TO RT HAS NUMEROUS ELONGATED HOLES AND DENTED . 2 L 7 3 4F RT A3WE 2001092600004 20010926 00004 NM 2001 9 26 VNAA0109001 1 20010903 A 2400 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE #1 FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 439JS 3057 DURING THE TAKE OFF ROLL, THE CREW RECEIVED A #1 BATTERY FAIL MESSAGE AND ABORTED THE TAKE OFF. MAINTENANCE INSPECTED A ND CLEANED CORROSION THAT WAS ON THE CANNON PLUG IN ACCORDANCEWITH DORNIER MAITENANCE MANUAL 24-00-00. OPERATIONAL CHEC KS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001092600005 20010926 00005 NM 2001 9 26 VNAA0109007 1 20010911 A 2400 DTSP400L BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RH FAILED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 458PS 12598 3068 WHILE CLIMBING THROUGH5000 FEET THE CREW RECEIVED A RIGHT HAND BATTERY OVERHEAT CAS MESSAGE AND THE FLIGHT RETURNED TO C AK. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND BATTERYIN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. O PERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001092600006 20010926 00006 NM 2001 9 26 VNAA0109009 1 20010915 A 2400 DTSP400L BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LH FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 439JS 11839 3057 DURING FLIGHT, THE CREW RECEIVED A BATTERY FAIL CAS MESSAGE AND DIVERTED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001092600007 20010926 00007 NM 2001 9 26 VNAA0109011 1 20010916 A 3397 WIRE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN FAILED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 427JS 3039 THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING STRIP WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPAIRED A W IRE IN THE LIGHTING STRIP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-50-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001092600008 20010926 00008 NM 2001 9 26 DHL2001727627 1 20010816 A 3213 STRUT BOEING 727 727200 138407E NM MLG LOOSE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 ON "C" CHECK DISCREPANCY---- RT MAIN LANDING GEAR STRUT DOOR HAS EXCESS PLAY. 2 L 7 3 4F RT A3WE 2001092600009 20010926 00009 NM 2001 9 26 DHL2001727755 1 20010820 A 2810 FUEL CELL BOEING 727 727200 138407E NM WING LEAKING A DHLA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 727DH ON "C" CHECK DISCREPANCY------- FUEL LEAK AT FWD. BOTTOM SKIN PLANK SEAM AT CURVE TO FWD. SPAR TO NR 8 FLAP TRACK, NR 3 MAIN TANK. 2 L 7 3 4F RT A3WE 2001092600010 20010926 00010 NM 2001 9 26 DHL2001727756 1 20010820 A 2810 FUEL CELL BOEING 727 727200 138407E NM WING LEAKING A DHLA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 727DH ON "C" CHECK DISCREPANCY------- FUEL LEAK AT UPPER SPAR DOUBLER FWD. SPAR AT WS 7604 NR 3 MAINTANK. 2 L 7 3 4F RT A3WE 2001092600011 20010926 00011 NM 2001 9 26 DHL2001741015 1 20010830 A 2781 SWITCH BOEING 727 7272Q9 138448M NM LE FLAPS MALFUNCTIONED A DHLA B EMER. DESCENT J E F WARNING INDICATION VIBRATION/BUFFET FLT CONT AFFECTED DE DESCENT 1 SO 01 741DH 21931 1) LE FLAP AND NR 2 KREUGER FLAP LIGHT WENT AMBER AT FL 250.ROLL FORCE CONFIRMED ASSYMETRICALLY SLOWED TO230 AND DESCE NDED TO FL200. CYCLED FLAPS TO 5 DEGREES AND BACK TO UP. ALL AMBER LIGHTS WENT OUT AND AIRPLANE FELT SYMETRICAL. CONTIN UED TO MCI AT 230 KTSAND FL 200 AS PRECAUTION.SEE WRITE-UPPREVIOUS PAGE ON S.O. FLAP PANEL, AMBER LIGHTS DO NOT COME ON FOR NR 1 FLAP AND NR 8 SLAT 2) R&R'D NR 2 FLAP INDICATING POSITION SWITCH PER MM. OPSCKS NORMAL DEFERRED PER MEL 27 -6 DMI 6928 3) REPOSITIONED POSITION SWITCH AND CLEANED CANNON PLUG ON NR 1 FLAP. T/S FOUND LOOSE WIRE AND SEC URED AND CLEANED CANNON PLUG ON # 8 SLAT. OPS CK GOOD. THIS CLEARS DMI 6928. STATUS: CLOSED 2 L 7 3 4F RT A3WE 2001092600012 20010926 00012 NM 2001 9 26 DHL2001741016 1 20010830 A 2780 CONTROL UNIT BOEING 727 7272Q9 138448M NM LE FLAPS MALFUNCTIONED A DHLA B EMER. DESCENT J E F WARNING INDICATION VIBRATION/BUFFET FLT CONT AFFECTED CR CRUISE 1 SO 01 741DH 21931 1) AT FL 250 LEADING EDGE AMBER LIGHT ILLUMINATED.S/O FLAP INDICATOR SHOW LEFT NR 2 KLUEGER FLAP EXTENDED (A/C FLYS NO RMAL ) DESCENDED TO FL 200 AND SLOWED TO 230 KTS.RECYCLED FLAPS, ALL INDICATIONS WERE NORMAL. 2) INSPECTED & CLEANE D CONNECTOR ON NR 2 KRUEGER FLAP SWITCH. NO DEFECTS NOTED. PERFORMED OPERATIONAL TEST OF LEADING EDGE FLAPS & CHECKS GOO D AT THIS TIME IAW B-727 M/M 27-82-0. STATUS: CLOSED 2 L 7 3 4F RT A3WE 2001092600013 20010926 00013 NM 2001 9 26 DHL2001741017 1 20010908 A 2751 CONTROLLER BOEING 727 727 UTILSYS NM TE FLAPS LACK OF LUBE A DHLA O OTHER O OTHER AP APPROACH 1 SO 01 741DH 21931 1) DURING FLAP EXTENSION LEFT INBOARD FLAP WOULD NOT EXTEND TO FLAPS 30. APPROX. 1 NEEDLE WIDTH OUT OF BOX DURING APPR OACH AND 2ND ATTEMPT WAS MADE AFTER LANDING. 2) LUBRICATED FLAP MECHANISM AND ADJUSTED LEFT INBOARD FLAP TRANSMITER CHECK OPS. IS GOOD PER MM 2780 STATUS: CLOSED 2 L 7 3 4J RT A3WE 2001092600014 20010926 00014 2001 9 26 DHL2001743012 4 20010830 A 3414 INDICATOR BOEING 727 727225 1384077 NM COCKPIT MALFUNCTIONED A DHLA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 743DH 22438 1) REJECTED T/O DUE TO 30KT DISCREPENCY BETWEEN CAPTAIN & F/O AIRSPEED INDICATOR. REJECTED WHEN: F/O AIRSPEED INDICAT ED 110KTS,CAPTAINS INDICATED 80KTS. 2) FOUND INSECT IN CAPTAINS AIRSPEED PITOT TUBE. REMOVED BUG AND PERFORMED PITO T STATIC TEST PER MM 34-11-0. CAPT AND F/O AIRSPEED CKS GD. STATUS: CLOSED 2 L 7 3 4F A3WE 2001092600015 20010926 00015 NM 2001 9 26 DHL2001745013 1 20010905 A 2510 LATCH BOEING 727 727224 1384076 NM COCKPIT SEAT STUCK A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 1) F/O'S SEAT WILL NOT LOCK IN RELEASE POSITION 2) FOUND STICKING LATCH , LUBED SAME . OPS CHK'D GOOD IAW MM 25-10 -41 STATUS: CLOSED 2 L 7 3 4F A3WE 2001092600016 20010926 00016 NM 2001 9 26 DHL2001747006 1 20010920 A 2612 FIRE LOOP BOEING 727 727224 1384076 NM NR 1 ENGINE OUT OF POSITION A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 747DH 22253 1) NR 1 ENGINE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED 2) FOUND 1 EA LOOSE CLAMP ON NR 1 ENGINE FIRE LOOP, RE POSITIONED LOOP. SECURED CLAMP & INSULATOR OPS CK GOOD PER MM 26-11-1 STATUS: CLOSED 2 L 7 3 4F A3WE 2001092600017 20010926 00017 NM 2001 9 26 SCNA01353 1 20010917 A 3350 900542 BATTERY PACK BOEING 727 727259 138408J NM FWD OVERWING INOPERATIVE A SCNA O OTHER O OTHER IN INSP/MAINT 1 GL 15 289SC 22475 DURING HEAVY MAINTENANCE INSPECTION THE CENTER ISLE EMERGENCY EXIT LIGHT IN FORWARD OVERWING BULLNOSE WILL NOT STAY ILLU MINATED. REMOVED AND REPLACED BATTERY PACK CHARGER IAW B727 MM 335022. OPS CHECK GOOD IAW B727 MM 335022. 2 L 7 3 4F A3WE 2001092600018 20010926 00018 NM 2001 9 26 DHL2001748002 1 20010826 A 3110 B070710025 SWITCH BOEING 727 727225 1384077 NM MACH OVERSPEED MALFUNCTIONED A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 748DH 22440 DURING TEST FLIGHT (DISCREPANCY)-------- MACH OVERSPEED ACTUATED AT .84 MACH AT 278 KNOTS AT 37000.1) ONT/S FOUND 300 FE ET PER MINUTE LEAK ON AUX STATIC SYS, OUT OF LIMITS PER B-727 M.M. 34-11-00.2)FOUND CRACKED TEE-FITTING ON AUX STATIC LI NE AT E AND E COMPARTMENT AND LEAK CHECKED GOOD ON AUX STATIC SYSTEM PER B-727 M.M. 34-11-0.3) NR 2 MACH WARNING SYS OPS CHECK GOOD PER B-727-200 AFM DOC D6-8728, STC ST00116SE " ALTAIR HOLDINGS, LTD, MAXIMUM AIRSPEED LIMITATIONS TABLE 1,4 ) REPLACED NR 3 OVERSPEED WARNING SWITCH OPERATIONAL CHECK OF WARNING SWITCH GOOD.-I.A.W. B-727-200 AFM DOR # D6-8788 ST C ST0016SE LIMITATIONS TABLE 1 DWG 4502 REV. B. I.A.W. B-727 M.M. 34-18-0. 2 L 7 3 4F A3WE 2001092600019 20010926 00019 NM 2001 9 26 DHL2001748003 1 20010826 A 3110 ANNUNCIATOR BOEING 727 727225 1384077 NM COCKPIT FALSE ACTIVATION A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 748DH 22440 ON TEST FLIGHT DISCREPANCY------- WINDSHEAR ANNUNCIATION INTERMITTENT OPERATION ROUTINE FAIL IN FLIGHT. 2 L 7 3 4F A3WE 2001092600020 20010926 00020 NM 2001 9 26 DHL2001748004 1 20010827 A 2810 FUEL CELL BOEING 727 727225 1384077 NM RT WING LEAKING A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 DURING "DROP IN INSPECTION" DISCREPANCY---------- SUSPECT FUEL LEAK IN THE AREA OF THE RIGHT WING REAR SPAR JUST OUTBD. OF THE RIGHT MAIN GEAR. 2 L 7 3 4F A3WE 2001092600021 20010926 00021 NM 2001 9 26 DHL2001748005 1 20010830 A 2611 ENGINE BOEING 727 727225 1384077 NM NR 1 MALFUNCTIONED A DHLA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 748DH 22440 DURING TEST FLIGHT DISCREPANCY----------- NR 1 ENGINE GROUND FAULT INDICATOR ILLUMINATED. 2 L 7 3 4F A3WE 2001092600022 20010926 00022 WP 2001 9 26 DHL2001801010 1 20010901 A 2510 SEAT DOUG DC8 DC873F 302199F WP COCKPIT LACK OF LUBE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 1) FO'S SEAT WILL NOT STAY LOCKED IN THE MOST FORWARD 3 POSITIONS.2) LUBED FO'S SEAT LOCKING MECHANISM , OPS CHECKED GOOD, IAW DC8 MM # 25-11-1.STATUS: CLOSED 2 L 7 4 4F RT 4A25 2001092600023 20010926 00023 EU 2001 9 26 2001F00369 1 20010823 A 7920 1742510 FILTER ELEMENT SNIAS 350 AS350B2 8680813 EU ENGINE DIRTY A KBMA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 19 115SH 3141 CLOGGING INDICATOR BUTTON FOR FACET FILTER ELEMENT POPS UP. INSTALLED NEW FACET FILTER ELEMENT. APPEARS MAGNET IN FILT ER HOUSING MAYBE WEAK, WILL MONITOR. THIS IS A NEW EXT FILTERING SYSTEM. (M) 1 G 7 1 3U H9EU 2001092600024 20010926 00024 NM 2001 9 26 AALA20011664 1 20010814 A 5730 SKIN BOEING 727 727223 1384074 NM WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 885AA 21524 TUL - FOUND LOWER WING LEADING EDGE SKIN CORRODED AFT OF INBOARD FUEL CAP. INSTALLED DOUBLER PER ESO NR 11697 DATED 8-1 3-2001. (M) 2 L 7 3 4F A3WE 2001092600025 20010926 00025 NM 2001 9 26 AALA20011666 1 20010818 A 5712 RIB BOEING 727 727223 1384074 NM WING CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 885AA 21524 TUL - FOUND STATION 760 RIB CHORD CRACKED BEHIND 760 RIGHT FRAME. STOP DRILLED CRACK. INSTALLED REPAIR DOUBLERS 760 RB L 70.5 IAW SB 727-57-0112 AS EPR CARD 4258 PAGE 2 ITEM 9. (M) 2 L 7 3 4F A3WE 2001092600026 20010926 00026 WP 2001 9 26 DHL2001801011 1 20010904 A 2611 SMOKE DETECTOR DOUG DC8 DC873F 302199F WP CARGO BAY MALFUNCTIONED A DHLA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 801DH 46033 1) ON PRE-DEPT CHECK,FOUND LWR CARGO SMOKE DET. SYS.OK "GREEN"LIGHT WOULD NOT ILLUMINATE W/NO TEST BUTTONS PUSHED OR W HEN PUSHING MX TEST BUTTON; BUT YOU GET A SYS.OK MESSEGE ON MX. DISPLAY & SYS. OK "GREEN" LIGHT OPS NORMAL IN LAMP TEST. 2) CYCLED PWR & C/B'S TO LWR CARGO SMOKE DET. SYS. NO HELP; RECONFIGURED SYS, GOT MESSEGE "FA1689". R & R (2) EA. B ATTERIES TO SDU FA1689 & RECONFIGURED SYS. OPS CKS. NORMAL I.A.W. DC-8 SMM 26-15-05 & 26-15-00. STATUS: CLOSED 2 L 7 4 4F RT 4A25 2001092600027 20010926 00027 NM 2001 9 26 AALA20011667 1 20010819 A 5320 WEB BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 885AA 21524 TUL - FOUND CORROSION ALONG LINE STATION 1140 FROM APPROX 24 INCHES RBL TO 36 INCHES RBL SEVERAL AREAS. CUTOUT DAMAGED AREA AND INSTALLED WEB REPAIR PER SRM 51-40-2 PAGES 1-6. (M) 2 L 7 3 4F A3WE 2001092600028 20010926 00028 NM 2001 9 26 AALA20011682 1 20010823 A 3350 LIGHT BOEING 767 767223 1385123 NM CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 302AA 22308 LAX - DURING OVERNIGHT MAINTENANCE, AFT 'IN SEAT' EMERGENCY LIGHT AT SEAT 11H INOPERATIVE. CLEANED LIGHT ASSEMBLY. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001092600029 20010926 00029 NM 2001 9 26 AALA20011718 1 20010822 A 5320 WEB BOEING 727 727223 1384074 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 880AA 21519 TUL - FOUND VERTICAL WEB OF RIGHT LOWER TORQUE BOX CRACKED APPROX STATION 1233 UPPER LIGHTENING HOLE. INSTALLED DOUBLER OVER DAMAGED AREA (AFTER ROUTING OUT CRACK) PER SRM 51-40-2. (M) 2 L 7 3 4F A3WE 2001092600030 20010926 00030 NM 2001 9 26 AALA20011720 1 20010824 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 880AA 21519 TUL - FOUND GOUGE IN SKIN STATION 460 STRINGER 24L. CUTOUT DAMAGED AREA OF SKIN AND INSTALLED DOUBLER REPAIR PER SRM 53 -30-3. (M) 2 L 7 3 4F A3WE 2001092600031 20010926 00031 WP 2001 9 26 DHL2001801012 1 20010906 A 2612 CONNECTOR DOUG DC8 DC873F 302199F WP FIRE LOOP DAMAGED A DHLA K NONE N L FALSE WARNING NO TEST IN INSP/MAINT 1 SO 01 801DH 46033 1) SHORT TEST FOR NR 1 B INOPERATIVE. 2) R&R WIRE CONNECTOR PI-8058 ON LT UPPER CORE FIRE DETECTOR LOOP, TESTED O PERATION OK. THIS CLEARS DMI 7008 STATUS: CLOSED 2 L 7 4 4F RT 4A25 2001092600032 20010926 00032 WP 2001 9 26 DHL2001801013 1 20010919 A 2510 SMOKE BARRIER DOUG DC8 DC873F 302199F WP CABIN BROKEN A DHLA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 801DH 46033 1) SMOKE BARRIER LT SIDE HAS 8 EA HOLD FASTENERS BROKEN 2) REPLACED 8 EA HOLD FASTENERS LT SIDE SMOKE BARRIER IAW DC-8 SRM 51-1-8 P/N 560168 ON/OFF STATUS: CLOSED 2 L 7 4 4F RT 4A25 2001092600033 20010926 00033 WP 2001 9 26 DHL2001802011 1 20010917 A 2611 SMOKE DETECTOR DOUG DC8 DC873 302199C WP NR 6 AND 7 WILL NOT TEST A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 802DH 46076 1) NR 6 SMOKE DETECTOR LIGHT WILL NOT COME ON FOR TEST. NR 7 SMOKE DETECTOR LIGHT WILL NOT GO OUT AFTER TEST. 2) RELAMPED NR 6 SMOKE DETECTOR PER SMM 26-15-00.OPS CHECK OK. RELAMPED NR 7 SMOKE DETECTOR PER SMM 26-15-00.OPS CHECK OK. STATUS: CLOSED 2 L 7 4 4F RT 4A25 2001092600034 20010926 00034 WP 2001 9 26 DHL2001802012 1 20010923 A 2612 FIRE LOOP DOUG DC8 DC873 302199C WP CARGO BAY INTERMITTENT A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 802DH 46076 1) NR 3 FIRE WARNING LOOP GIVES SHORT CIRCUIT LIGHT IN FIRE POSITION INTERMITTANTLY. 2) DEFERRED NR 3 ENG B LOOP FIRE DETECTION IAW MEL 26-2-3 DMI 7170, SPEC PROC C/W, PLACARD INSTALLED. 3) REMOVED & REPLACED FAN,FIRE DETECTOR LOOP. OPS CK GOOD AS PER MM 26-10-0. CLEARED DMI 7170. AC OK FOR SERVICE. STATUS: CLOSED 2 L 7 4 4F RT 4A25 2001092600035 20010926 00035 NM 2001 9 26 AALA20011722 1 20010830 A 3350 3015646 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 393AN 29430 LAX - DURING OVERNIGHT MAINTENANCE, AFT LOWER LEFT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY. SYSTEM G ROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001092600036 20010926 00036 WP 2001 9 26 DHL2001802013 1 20010923 A 2612 FIRE LOOP DOUG DC8 DC873 302199C WP NR 3 ENGINE SHORTED A DHLA F E J A ACTIVATE FIRE EXT. ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 802DH 46076 1) FIRE WARNING NR 3 ENGINE COMPLETED ENGINE FIRE SHUTDOWN CHECK LIST. LOOP B WOULD NOT SHORT TEST. 2) INSPECTED INLET AND EXHAUST OF NR 3 ENGINE. NO EVIDENCE OF FIRE. INSPECTED AND CHECKED FOR PNEUMATIC LEAKS IAW 71-00-00,NONE NOTED . PERFORMED NR 3 ENGINE B LOOP FIRE TEST, GAVE SHORT CIRCUIT LITE IN FIRE POS. RAN NR 3 ENG PER J. STATUS: CLOSED 2 L 7 4 4F RT 4A25 2001092600037 20010926 00037 NM 2001 9 26 AALA20011725 1 20010905 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN PINCHED A A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 372AA 25199 LHR - FLT 121 - CDG-JFK - APPROXIMATELY 30 MINUTES INTO FLIGHT PASSENGERS AND FLIGHT ATTENDANT REPORTED ELECTRICAL ARCIN G AND SPARKING ORIGINATING FROM PSU OVERHEAD BIN AT SEAT 28H-J. ALL READING LIGHTS ON RIGHT CABIN SIDE BECAME INOPERATI VE. ALL REMAINING CABIN READING LIGHTS ALSO BECAME INOPERATIVE. AIRCRAFT DIVERTED TO LHR AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PINCHED. CHAFFED WIRE AND ACCOMPLISHED INTERIM REPAIR PRIOR TO AIRCRAFT DEPARTURE. PERMANENT REPAIR ACCOMPLISHED AT ORD. TWO SUBSEQUENT FLIGHTS REVEALED NO REPEAT WRITE-UPS. (M) 2 L 7 2 4F RT A1NM 2001092600038 20010926 00038 NM 2001 9 26 USAA011150 1 20010824 A 5312 BULKHEAD BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 22961 CLT - FOUND WEB SKIN CRACKED .500 INCH, BS 178 BULKHEAD, RBL 1, WL 206. REMOVED DAMAGED HFEC INSPECTION, CUT .100 MORE, INSTALLED DOUBLER PER EO 5300V153 EA 69902, SRM 53-10-08. (M) 2 L 7 2 4F A16WE 2001092600039 20010926 00039 NM 2001 9 26 USAA011152 1 20010824 A 5312 BULKHEAD BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND WEB SKIN CRACKED .500 INCH, BS 178 BULKHEAD, LBL 1,WL 206. REMOVED DAMAGE, HFEC INSPECTION. CUT .100 MORE, INSTALLED DOUBLER PER EO 5300V153, EA 69902, SRM 53-10-08. (M) 2 L 7 2 4F A16WE 2001092600040 20010926 00040 WP 2001 9 26 DHL2001804015 1 20010918 A 2510 VAPOR BARRIER DOUG DC8 DC873F 302199F WP CABIN DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 1) VAPOR BARRIER HAS TWO BROKE FASTNERS AT 10 OCLOCK POSITION. 2) R&R FASTENERS PER DC8 SUPPLEMENTARY M/M REF 25- 50-03. STATUS: CLOSED 2 L 7 4 4F RT 4A25 2001092600041 20010926 00041 NM 2001 9 26 USAA011157 1 20010828 A 5313 6546B77144 STRINGER BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND SHELF WEB CRACKED 3 INCHES, RIGHT 18A SHELF. REPLACED WITH NEW PART PER SRM 51-10-1 AND EO 85230. (M) 2 L 7 2 4F A16WE 2001092600042 20010926 00042 WP 2001 9 26 DHL2001804016 1 20010918 A 5610 WINDOW DOUG DC8 DC873F 302199F WP COCKPIT LACK OF LUBE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 1) CAPT SLIDING WINDOW WILL NOT OPEN. 2) ADJUSTED AND LUBED CAPTAINS SLIDING WINDOW IAW 56-10-3. WINDOW OPS GO OD. STATUS: CLOSED 2 L 7 4 4F RT 4A25 2001092600043 20010926 00043 NM 2001 9 26 USAA011160 1 20010829 A 5312 BULKHEAD BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 52062 22885 CLT - FOUND WEB PRESSURE CRACKED .06 AND .08 INCH, BS 178 BULKHEAD WEB, LBL .5 AND RBL .5, WL 188. CUT OUT CRACKS AND I NSTALLED DOUBLER PER EA 85310. (M) 2 L 7 2 4F A16WE 2001092600044 20010926 00044 NM 2001 9 26 USAA011162 1 20010829 A 5320 STIFFENER BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 52062 22885 CLT - FOUND VERTICAL CHORD CRACKED .5 INCH AND .9 INCH, BS 178 BULKHEAD LBL 5-7 VERTICAL CHORD, WL 184. INSTALLED REPAI R DOUBLER PER EO NR 5300V155. (M) 2 L 7 2 4F A16WE 2001092600045 20010926 00045 NM 2001 9 26 USAA011163 1 20010829 A 5311 FRAME BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 52062 22885 CLT - FOUND SIDE CHORD CRACKED .5 INCH, BS 178 BULKHEAD, WL 207 AND WL 196, LEFT SIDE CHORD. INSTALLED NEW CHORD SECTIO N AND SPLICE PARTS. (M) 2 L 7 2 4F A16WE 2001092600046 20010926 00046 NM 2001 9 26 USAA011166 1 20010829 A 5311 FRAME BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 52062 22885 CLT - FOUND CHORD CRACKED .5 INCH, IN RADIUS OF LEFT SIDE CHORD BS 178 AT WL 196 AND WL 207. SPLICED IN ANGLE AND DOUBL ER STRAP PER EO 5300V157. (M) 2 L 7 2 4F A16WE 2001092600047 20010926 00047 NM 2001 9 26 USAA011170 1 20010830 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND FLOORBEAM WEB CRACKED .5 INCH, BS 663 BL0. INSTALLED DOUBLER SPLICE PLATES AND STIFFENERS, PER TT 57-10-04 AND EA 69909. (M) 2 L 7 2 4F A16WE 2001092600048 20010926 00048 NM 2001 9 26 USAA011188 1 20010831 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND CHORD ANGLE CRACKED 1 INCH, BS 178 BULKHEAD RIGHT SIDE RADIUS WL 195. REMOVED AND REPLACED CHORD SECTION, I NSTALLED INT DOUBLER ANGLE AND EX DOUBLER STRAP PER EO 5300V157AND EA 85332. (M) 2 L 7 2 4F A16WE 2001092600049 20010926 00049 NM 2001 9 26 USAA011189 1 20010831 A 5330 BEAR STRAP BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND DOOR C/O BEARSTRAP CORRODED 3 INCHES BY 5 INCHES, BS 485 AND BS 440 AND BS 420. INSTALLED FILLER AND DOUBLE R AND 2 TRIPLERS PER EA NR 85292. (M) 2 L 7 2 4F A16WE 2001092600050 20010926 00050 NM 2001 9 26 USAABB01091 1 20010831 A 3350 8731002511REV14 SIGN BOEING 757 757225 1384959 NM R4 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 609AU 22205 CLT - FOUND THE R4 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001092600051 20010926 00051 2001 9 26 USAAD01155 4 20010831 A 2565 D29985103 SLIDE DOUG DC9 DC982 3022082 WP SERVICE DOOR FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 822US 6601 49139 PIT - THE AFT SERVICE DOOR EVACUATION SLIDE FAILED TO DEPLOY DURING A FUNCTIONAL TEST. MAINTENANCE REPLACED THE EVACUAT ION SLIDE. (M) 2 L 7 2 4F A6WE 2001092600052 20010926 00052 2001 9 26 USAAD01156 4 20010831 A 2565 100503111 SLIDE DOUG DC9 DC982 3022082 WP TAIL CONE FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 822US 28803 49139 PIT - THE TAIL CONE EVACUATION SLIDE FAILED TO DEPLOY DURING A FUNCTIONAL TEST. MAINTENANCE REPLACED THE EVACUATION SLI DE. (M) 2 L 7 2 4F A6WE 2001092600053 20010926 00053 2001 9 26 DHL2001804017 4 20010921 A 2210 SWITCH DOUG DC8 DC873F 302199F WP TORQUE LIMITING OUT OF RIG A DHLA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 804DH 46124 1) IN ALTITUDE HOLD, AUTO PILOT WILL DECEND AND CLIMB AIRCRAFT UNCOMMANDED. RII AND AIRWORTHINESS REQUIRED. 2) FO UND SERVO TORQUE LIMITING SWITCH OUT OF RIG. ADJUSTED PER DC-8 MM, CHAPTER 27-50-0 ITEM (17A). R&R AIR DATA COMPUTER, P REFORMED PITOT/ STATIC TEST, AND PREFORMED FUNCTIONAL TEST OF AUTOPILOT. OPS CHECK. STATUS: CLOSED 2 L 7 4 4F RT 4A25 2001092600054 20010926 00054 2001 9 26 P2EA2001M0005 4 20010924 A 2220 2590650901 COUPLER BOEING 737 737297 1384480 NM A P2EA K NONE F FLT CONT AFFECTED CR CRUISE 1 CE 05 005WM 22629 Mach Trim "fail" light illumimnates intermitently. Corrective action: Defferred Mach Trim system per MEL 22-5, CI#M00508 9 per MX CNTL Mic. Removed and replaces Mach Trim Coupler IAW MM 22-21-31, operational check normal. This clears MEL CI# M005089. See 005 Log pages 92956 and 92957. This report filed closed. 2 L 7 2 4F A16WE 2001092600055 20010926 00055 2001 9 26 USAAD01157 4 20010903 A 2565 LANYARD DOUG DC9 DC981 3022081 WP TAIL CONE OUT OF POSITION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 819US 48099 IND - THE TAIL CONE EVACUATION SLIDE COVER WAS NOT ATTACHED AT THE AFT HINGE POINTS AND THE MANUAL DEPLOY LANYARD WAS NO T ROUTED PROPERLY. MAINTENANCE ATTACHED THE TAIL CONE EVACUATION SLIDE COVER AND ROUTED THE MANUAL DEPLOY LANYARD PROPE RLY. (M) 2 L 7 2 4F A6WE 2001092600063 20010926 00063 EU 2001 9 26 01FDEA00855 1 20010924 A 2750 CONTROL UNIT AIRBUS 310 A310222 3930315 EU T/E FLAP MALFUNCTIONED A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 446FE 224 AFT T/O FLAP RETRACT AND ECAM ALERT FLAP 1 & 2 FAULT. SFCC 1 & 2 RESET. SLAT AND FLAP CYCLE CK NORMAL. 2 L 7 2 4F RT A35EU 2001092600064 20010926 00064 EU 2001 9 26 2001F00373 1 20010908 A 2150 5613C000002 A/C PACK PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL ENGINE BAY INOPERATIVE E K NONE O OTHER IN INSP/MAINT 1 WP 07 317NA 2567 223 PR0294 HJ736 ECS SYSTEM BLOWS WARM AIR IN EITHER MANUAL OR AUTO MODES. REMOVED AND REPLACED REFRIGERATION PACK AND OPS CHECK OK. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001092600065 20010926 00065 WP 2001 9 26 ABXA010500 1 20010923 A 2133 VALVE DOUG DC8 DC863 302198A WP CABIN PRESSURE OBSTRUCTED A ABXA K NONE O OTHER CR CRUISE 1 GL 23 819AX 45927 AUTO PRESSURIZATION WAS INOPERATIVE AND CABIN PRESSURIZATION COULD NOT BE CONTROLLED MANUALLY WITH ALL BLEEDS ON HIGH AN D ALL CTC'S OPERATING. THE CREW DONNED OXYGEN MASKS AND DESCENDED TO FL 10. MAINTENANCE INSPECTED AND REMOVED A PIECE OF INSULATION FROM THE RIGHT SAFETY VALVE. OPERATION CHECKS WERE COMPLETED IAW DC-8 MM, AND THE AIRCRAFT WAS RETURNED T O SERVICE. 2 L 7 4 4F 4A25 2001092600066 20010926 00066 WP 2001 9 26 AT0100230 1 20010924 A 3350 41B004AD073 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 828AT 47274 FOUND SEVERAL EMERGENCY CEILING LIGHTS OUT. REMOVED AND REPLACED EMERGENCY LIGHT NICAD BATTERIES IN CABIN CEILING AT RO W 18 IAW DC9 MM 33-50. 2 L 7 2 4F A6WE 2001092600067 20010926 00067 EU 2001 9 26 C2XA01IA363 1 20010923 A 6123 100300311 SENSOR AEROSP ATR42 ATR42320 8680930 EU COCKPIT FAULTY A C2XA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SW 27 42836 24005 24005 200 FLT 2937, CREW REPORTED THAT THE AUTOFEATHER LIGHT DID NOT ILLUMINATE AND NUMBER 2 ENGINE WAS LOSING POWER DURING TAKEOF F ROLL. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE INSPECTED AND FOUND THE NR 2 GCU MAGNETIC INDIC ATOR TO BE POPPED. FURTHER TROUBLESHOOTING INDICATED THAT THE NR 2 DC GENERATOR HALL EFFECTS SENSOR TO BE FAULTY. THE AFFECTED HALL EFFECTS SENSOR WAS REMOVED AND REPLACED. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001092600068 20010926 00068 WP 2001 9 26 CALA0100893 1 20010921 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35836 49441 INSPECTION FOUND A CRACK IN TAIL COMPARTMENT CANTED FRAME AT STA 1446, L3R AN L26L. THE CRACKED FRAME CAP WAS REMOVED A ND REPLACED IAW SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2001092600069 20010926 00069 WP 2001 9 26 CALA0100894 1 20010923 A 5350 CLIP DOUG DC9 DC982 3022082 WP TAILCONE OUT OF ADJ A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35836 49441 THE TAILCONE EXTERIOR RELEASE HANDLE PULL FROM CLIPS WAS LOW. THE CLIPS WERE ADJUSTED IAW MM 53-53-00. 2 L 7 2 4F A6WE 2001092600070 20010926 00070 NM 2001 9 26 CALA0100895 1 20010924 A 5320 SPLICE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 INSPECTION FOUND A 2 INCH CRACK IN STRINGER SPLICE AT STA 907, S4R. A NEW SPLICE WAS INSTALLED IAW SRM 53-40-3. 2 L 7 2 4F RT A16WE 2001110900033 20011109 00033 2001 11 9 CALA0100896 4 20010924 A 2330 7430315003 CAPACITOR BOEING 737 737724 NM VIDEO SYS FAILED A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 09 16709 10454 28779 FLIGHT ATTENDANT'S REPORTED SMOKE IN THE FORWARD GALLEY AREA WHILE EN ROUTE FROM EWR TO MEX. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE IDENTIFIED THE SOURCE OF SMOKE TO BE FROM THE VIDEO SYSTEM CONTROL UNIT (SCU) BASED ON THE BURN SMELL NOTED INSIDE THE UNIT. THE SCU WAS REMOVED AND REPLACED. SCU BITE TEST CHECKED GOO D. NO OTHER FAULTS WERE FOUND. TEARDOWN REVEALED THAT THE HEAT DAMAGE AND RESULTANT SMOKE WAS DUE TO FAILURE OF A CAPA CITOR IN THE SCU. 2 L 7 2 4F RT A16WE 2001092600071 20010926 00071 NM 2001 9 26 DL757011551 1 20010915 A 5330 146N351111 SKIN BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 611DL 22818 THE FUSELAGE SKIN WAS FOUND WITH AN AREA OF CORROSION AFT OF THE FS 1380 FRAME AT STRINGER 30. THE CORROSION WAS REMOVE D AND THE SKIN WAS REPAIRED WITH AN EXTERNAL DOUBLER. THE REPAIR WAS ACCOMPLISHED PER B757 SRM 53-00-01 AND ER/A 381769 -14. 2 L 7 2 4F RT A2NM 2001092600072 20010926 00072 NM 2001 9 26 DL757011561 1 20010917 A 5754 114N4005164 SKIN BOEING 757 757232 1384965 NM L/E SLAT DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 640DL 23994 NR 7 SLAT HAS OVERSIZED HOLES COMMON TO THE TRAILING EDGE WEDGE, SKIN, AND RIB. REPAIR PER ER/A 401937-14AD. 2 L 7 2 4F RT A2NM 2001092600073 20010926 00073 NM 2001 9 26 F3LA200100108 1 20010924 A 2750 COUPLING BOEING 737 7372L9 1384497 NM DISCONNECTED A F3LA A UNSCHED LANDING F FLT CONT AFFECTED TO TAKEOFF 1 NM 03 271FL 309 22734 AIR TURN BACK. FLIGHT CREW REPORTED FLAPS DID NOT RETRACT AFTER TAKEOFF. LT. TORQUE TUBE COUPLING AT NO. 4 FLAP TRANSM ISSION WAS DISCONNECTED. RECONNECTED COUPLING PER MM 27-51-251. ADJUSTED TRAILING EDGE FLAPS PER MM 27-51-01 AND PERFO RMED OPERATIONAL TEST. 2 L 7 2 4F RT A16WE 2001092600074 20010926 00074 NM 2001 9 26 DL764011504 1 20010907 A 2752 PIN BOEING 767 767432ER NM ROTARY ACTUATOR OUT OF ADJ A DALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 27 835MH 29708 ON DEPARTURE, RECEIVED T/E FLAP DISAGREE UPON RETRACTION, RETURNED TO HNL FOR AN OVERWEIGHT LANDING 376,000 LBS. T/S PE R FIM 27-51-00. RESET NR 1 ROTARY ACTUATOR PIN. RAN FLAPS SEVERAL TIMES WITH NO DISCREPANCIES. RETURNED A/C TO SERVIC E. 2 L 7 2 4F RT A1NM 2001092600075 20010926 00075 NM 2001 9 26 HNAA0100057 1 20010814 A 5341 85300016113 ANGLE DHAV DHC8 DHC8102 2809003 NM CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 934HA 34184 139 WING FRONT SPAR TO FUSELAGE L/H CLOSING ANGLE CRACKED. REPLACED CLOSING ANGLE. 2 H 7 2 4T RT A13NM 2001092600076 20010926 00076 NM 2001 9 26 HNAA0100058 1 20010814 A 5400 85410149103 ANGLE DHAV DHAV DHC8 DHC8102 2809003 NM CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 934HA 34184 S2BHC0290 139 R/H NACELLE HORSECOLLAR FRAME AFT FLANGE ANGLE CRACKED. REPLACED ANGLE. 2 H 7 2 4T RT A13NM 2001092600077 20010926 00077 2001 9 26 P2EA2001M0006 4 20010922 A 2210 2588809901 CONTROL PANEL BOEING 737 7372T5 NM A P2EA K NONE F FLT CONT AFFECTED CR CRUISE 1 CE 05 120NJ 22979 Heading Hold will not hold heading with Auto Pilot in B channnel. Corrective action: Deffered Heading Hold per MEL 22-1, CI#M120076 per MX CNTL Mic. Replaced Mode Control Panel, operational check normal IAW MM 22-11-191, This clears CI#M120 079. See A/C 120 Log pages 92740 and 92653. This report filed closed. 2 L 7 2 4F RT A16WE 2001092600078 20010926 00078 NM 2001 9 26 HNAA0100059 1 20010814 A 5400 85410149103 ANGLE DHAV DHAV DHC8 DHC8102 2809003 NM CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 934HA 34184 S2BHC0297 139 L/H NACALLE HORSECOLLAR AFT FLANGE ANGLE CRACKED. REPLACED ANGLE. 2 H 7 2 4T RT A13NM 2001092600079 20010926 00079 NM 2001 9 26 DL764011535 1 20010915 A 2430 CM74818 RELAY BOEING 767 767432ER NM ELECTRICAL SYS FAILED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 837MH 29710 ON CLIMBOUT, STBY BUS C/B POPPED. T/S FOUND BAD K106 RELAY NASI. REMOVED ACCESS PNL P6 C/B PANEL AND REMOVED K105 A/C STBY PW RELAY DPN 241202153. REMOVED AND REPLACED RELAY K105, OPS CKS NORMAL PER M/M 24-33-00-6-02. INSTALLED ACCESS P ANEL. 2 L 7 2 4F RT A1NM 2001092600080 20010926 00080 NM 2001 9 26 DL767011538 1 20010915 A 3350 LIGHT BOEING 767 767232 1385132 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 108DL 22220 EMERGENCY LIGHT INOP 5L POS. REPLACED LIGHT. 2 L 7 2 4F RT A1NM 2001092600081 20010926 00081 NM 2001 9 26 DL767011539 1 20010915 A 3350 20131A BATTERY PACK BOEING 767 767232 1385132 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 108DL 22220 OVERHEAD EMERGENCY LIGHTS IN F/C INOP. REPLACED BATTERY PACK IN FIRST CLASS LEFT SIDEWALL, CHECK GOOD. 2 L 7 2 4F RT A1NM 2001092600082 20010926 00082 NM 2001 9 26 HNAA0100060 1 20010901 A 5744 85780189101 TRACK DHAV DHC8 DHC8102 2809003 NM CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 934HA 34184 139 L/H WING #3 FLAP TRACK HAS AREA OF CORROSION ON BACK FACE OF TRACK. BLENDED CORROSION IAW EO8-57-01-396. 2 H 7 2 4T RT A13NM 2001092600083 20010926 00083 NM 2001 9 26 DL767011564 1 20010920 A 3350 767 LIGHT BOEING 767 767232 1385132 NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 107DL 22219 RELAMPED R2 EXTERIOR EMERGENCY LIGHT. 2 L 7 2 4F RT A1NM 2001092600084 20010926 00084 NM 2001 9 26 DL76G011511 1 20010908 A 3350 BPS73 POWER SUPPLY BOEING 767 7673P6 1385105 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 152DL 24984 OVERHEAD EMERGENCY LIGHT INOP AFT CABIN. REPLACED POWER SUPPLY. 2 L 7 2 4F RT A1NM 2001092600085 20010926 00085 NM 2001 9 26 HNAA010061 1 20010826 A 5744 85780189102 TRACK DHAV DHC8 DHC8102 2809003 NM CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 934HA 34184 139 R/H WING #3 FLAP TRACK HAS CORROSION ON BACK SURFACE. BLECDED CORROSION IAW EO8-57-01-396. 2 H 7 2 4T RT A13NM 2001092600086 20010926 00086 NM 2001 9 26 DL76G011523 1 20010910 A 2121 732591F FAN BOEING 767 7673P6 1385105 NM E/E BAY FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 153DL 24985 IN CRUISE AT FL 370 A STRONG ODOR OF BURNING PLASTIC. FOLLOWED BY FWD EQUIPMENT EXHAUST FAN C/B POPPING AND FWD EQUIPME NT EXIT FAN STATUS MSG. REPLACED FWD EQUIPMENT EXHAUST FAN PER MM. OPS CHECK NORMAL. S/N OFF 1529, S/N ON 5586A, P/N 211002542. 2 L 7 2 4F RT A1NM 2001092600087 20010926 00087 WP 2001 9 26 IXXA0100052S 1 20010518 A 5313 LONGERON DOUG DC8 DC871F 302199D WP LOWER FUSELAGE CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 822BX 84173 2919 45813 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON LONGERON 36 AT FUSELAGE STATION 621. REPAIR ACCOMPLISHED REM OVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION NEW LONGERON SPLICE FITTING IN ACCORDANCE WITH DOUGLAS STRUCTURAL REP AIR MANUAL AND ENGINEERING ORDER 53-DC8-3023. 2 L 7 4 4F RT 4A25 2001092600088 20010926 00088 WP 2001 9 26 IXXA0100054S 1 20010503 A 5511 RIB DOUG DC8 DC871F 302199D WP HORIZONTAL STAB CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 822BX 84173 2919 45813 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED AT THE LEFT HAND LEADING EDGE HORIZONTAL STABILIZER INBOARD SIDE INTERIOR PANEL 2ND RIB. REPAIR ACCOMPLISHED STOP DRILLED CRACK, FABRICATION AND INSTALLATION REPAIR ANGLE IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING ORDER 55-DC8-3025. 2 L 7 4 4F RT 4A25 2001092600089 20010926 00089 WP 2001 9 26 IXXA0100053S 1 20010503 A 5511 RIB DOUG DC8 DC871F 302199D WP HORIZONTAL STAB CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 822BX 84173 2919 45813 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED AT THE LEFT HAND LEADING EDGE HORIZONTAL STABILIZER INBOARD SIDE INTERIOR PANEL 16TH RIB. REPAIR ACCOMPLISHED STOP DRILLED CRACK, FABRICATION AND INSTALLATION REPAIR ANGLE IN ACCORDANC E WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING ORDER 55-DC8-3024. 2 L 7 4 4F RT 4A25 2001092600090 20010926 00090 WP 2001 9 26 IXXA0100055S 1 20010517 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 822BX 84173 2919 45813 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON FORWARD PIT LONGERON 36 BETWEEN FUSELAGE STATION 590 AND 61 0. REPAIR ACCOMPLISHED REMOVAL OF LONGERON SECTION, FABRICATION AND INSTALLATION OF A NEW LONGERON SECTION AND SPLICE I N ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING ORDER 51-DC8-3030. 2 L 7 4 4F RT 4A25 2001092600091 20010926 00091 WP 2001 9 26 IXXA0100057S 1 20010504 A 5712 RIB DOUG DC8 DC871F 302199D WP RIGHT WING MISDRILLED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 822BX 84173 2919 45813 DURING ROUTINE C-CHECK INSPECTION, MISDRILLED HOLES WERE DETECTED IN THE RIGHT WING LEADING EDGE RIB AT WING STATION 763 , ACCESS PANEL 517B. REPAIR ACCOMPLISHED REMOVAL OF DEFECTIVE DOUBLER, FABRICATION AND INSTALLATION OF NEW REPAIR DOUBLE R IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING ORDER 57-DC8-3038. 2 L 7 4 4F RT 4A25 2001092600092 20010926 00092 WP 2001 9 26 IXXA0100058S 1 20010508 A 5710 DOUBLER DOUG DC8 DC871F 302199D WP R/H WING L/E CORRODED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 822BX 84173 2919 45813 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE RIGHT WING LEADING EDGE INTERIOR DOUBLER AT THE LIFT TR ANSDUCER, STATION 380. REPAIR ACCOMPLISHED REMOVAL OF DEFECTIVE DOUBLER, FABRICATION AND INSTALLATION OF NEW DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING ORDER 57-DC8-3040. 2 L 7 4 4F RT 4A25 2001092600093 20010926 00093 WP 2001 9 26 IXXA0100059S 1 20010511 A 5740 HINGE FITTING DOUG DC8 DC871F 302199D WP R/H WING CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 822BX 84173 2919 45813 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE RIGHT WING AILERON MECHANISM AREA LOWER SUPPORT HINGE FIT TING "L" ANGLE. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED ANGLE, FABRICATION AND INSTALLATION OF NEW REPAIR ANGLE IN ACCOR DANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL, DRAWING 5705518 AND ENGINEERING ORDER 57-DC8-3043. 2 L 7 4 4F RT 4A25 2001092600094 20010926 00094 WP 2001 9 26 IXXA0100061S 1 20010503 A 5531 SPAR CAP DOUG DC8 DC871F 302199D WP VERTICAL STAB CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 822BX 84173 2919 45813 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED AT THE VERTICAL STABILIZER REAR SPAR LEFT HAND CAP AT STATION ZR 265. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED CAP. FABRICATION AND INSTALLATION OF NEW CAP IN ACCORDANCE WITH DOUGLAS STR UCTURAL REPAIR MANUAL, DAC DRAWING 5611409 AND ENGINEERING ORDER 55-DC8-3048. 2 L 7 4 4F RT 4A25 2001092600095 20010926 00095 WP 2001 9 26 IXXA0100063S 1 20010512 A 5311 FRAME DOUG DC8 DC871F 302199D WP TAIL CONE CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 822BX 84173 2919 45813 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED IN THE TAIL CONE FRAME AT FUSELAGE STATION 1992 LEFT SIDE BEHIND THE CROSS BRACE. REPAIR ACCOMPLISHED FABRICATION AND INSTALLATION OF REPAIR ANGLES IN ACCORDANCE WITH DOUGLAS STRUCTURA L REPAIR MANUAL AND ENGINEERING ORDER 53-DC8-3051. 2 L 7 4 4F RT 4A25 2001092600096 20010926 00096 WP 2001 9 26 IXXA0100065S 1 20010502 A 5313 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DENTED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 822BX 84173 2919 45813 DURING ROUTINE C-CHECK INSPECTION, A DENT WAS FOUND AT FUSELAGE STATION Y+1400.000 BETWEEN LONGERONS 26R AND 27R. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF DOUBLER AND FILLER IN ACCORDANCE WITH DOUGLAS STR UCTURAL REPAIR MANUAL AND ENGINEERING ORDER 53-DC8-3053. 2 L 7 4 4F RT 4A25 2001092600097 20010926 00097 NM 2001 9 26 HNAA0100062 1 20010827 A 5300 85322331139 STRAP DHAV DHC8 DHC8102 2809003 NM CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 934HA 34184 139 SKIN JOINT STRAP BETWEEN STRINGERS 20S AND 22S AT STATION X370.80 IS CORRODED. REPAIRED STRAP IAW EO8-53-01-399. 2 H 7 2 4T RT A13NM 2001092600098 20010926 00098 NM 2001 9 26 DL76G011532 1 20010914 A 3350 FUSE BOEING 767 767332 1382001 NM BATTERY CHARGER BLOWN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1608 30573 FOUND FUSE BLOWN ON EMERGENCY LIGHT BATTERY CHARGER. REPLACED FUSE, OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 2001092600099 20010926 00099 2001 9 26 DL76G011556 4 20010918 A 2561 COVER BOEING 767 7673P6 1385105 NM LIFE VEST TORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 156DL 25354 FOUND 65 LIFE VEST PROTECTIVE COVERS TORN THROUGH OUT THE CABIN. REPLACED 65 LIFE VESTS THROUGH OUT THE CABIN AS REQUIR ED. 2 L 7 2 4F RT A1NM 2001092600100 20010926 00100 NM 2001 9 26 DL76K011553 1 20010917 A 2560 BATTERY BOEING 767 767332 1382001 NM FLASHLIGHT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 176DZ 29697 EMERGENCY FLASHLIGHT HAS LOW BATTERY. REPLACED BATTERY. 2 L 7 2 4F RT A1NM 2001092600101 20010926 00101 2001 9 26 DL76L011497 4 20010906 A 2330 1301851100 VIDEO DISPLAY BOEING 767 767332 1382001 NM CABIN FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 186DN 27962 SMOKE SMELLED IN CABIN NEAR 20AB. DETERMINED PROBLEM WITH VIDEO MONITOR AT 20AB BULKHEAD. C/B C9095 NOW PULLED AND COLL ARED. PART 1301851-100 NOT AVAIL. VIDEO SYS FROM 10AB THRU 10FG BACK TO 32AB THRU 32FG NOW DEACTIVATED DUE TO C/B C9095 PULLED AND COLLARED. 2 L 7 2 4F RT A1NM 2001092600102 20010926 00102 WP 2001 9 26 DHL2001804555 1 20010824 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 D-CHECK; LT WING LWR SKIN- FASTENER HOLE (3/16 INCH DIA) IDENTIFIED WITH CODE "A" SHOWS CRACK (0.375 LENGTH) AT XCW 69.5 00.CORR ACTION; REMOVED FASTENERS IAW SRM 51-3-0 PG 1. TRIMMED OUT DAMAGED AREA IAW S/B 57-88 PG 21 COND I ITEM 3( DRWG SR 08570004, SHEET 3) EO 2001350 FABRICATED A FILLER FROM ORIGINAL SECTION THICKNESS (7075-T6) IAW S/B 57-88 PG 21 COND I ITEM 3 (DRWG SR 08570004, SHEET 3)EO 2001350.TREATED & PRIMED IAW SRM 51-1-8B. APPLIED (PRC) SEALANT TO FAYING SURFACE IAW SRM 51-1-11 PG 1. INSTALLED FILLER IAW SRM 51-3-0 PG 1, S/B 57-88 PG 21 COND I ITEM 3 (DWG SR 08570004 SHEET 3) SRM 51-1-15 PG 1 EO 2001350. REFER N/R 1289.ACTION CLOSED. 2 L 7 4 4F RT 4A25 2001092600103 20010926 00103 WP 2001 9 26 DHL2001804556 1 20010823 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 D-CHECK; RT WING LWR SKIN- FASTENER HOLE (3/16 INCH DIA) IDENTIFIED WITH CODE "A" SHOWS CRACK (0.375 LENGTH)AT XCW 69.50 0.CORR ACTION; REMOVED FASTENERS IAW SRM 51-3-0 PG 1. TRIMMED OUT DAMAGED AREA IAW S/B 57-88 PG 21 COND I ITEM 3( DRWG S R 08570004, SHEET 3) EO 2001350 FABRICATED A FILLER FROM ORIGINAL SECTION THICKNESS (7075-T6) IAW S/B 57-88 PG 21 COND I ITEM 3 (DRWG SR 08570004, SHEET 3)EO 2001350.TREATED & PRIMED IAW SRM 51-1-8B. APPLIED (PRC) SEALANT TO FAYING SURFACE IAW SRM 51-1-11 PG 1. INSTALLED FILLER IAW SRM 51-3-0 PG 1, S/B 57-88 PG 21 COND I ITEM 3 (DWG SR 08570004 SHEET 3) SRM 51-1-15 PG 1 EO 2001350. REFER N/R 1290.ACTION CLOSED. 2 L 7 4 4F RT 4A25 2001092600104 20010926 00104 WP 2001 9 26 DHL2001804557 1 20010823 A 5753 SPRING DOUG DC8 DC873F 302199F WP LT TE FLAPS CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 D-CHECK; LT FLAP FOLDING HINGE COVER SPRING AT STA 330 CRACKED. CORR ACTION; REMOVED & REPLACED LT FLAP FOLDING HINGE CO VER SPRING AT STA 330 IAW OHM 27-27-2 PG 2, 7, 15, 16, & SRM 51-1-21 PG 1-2 REF N/R 1727 FOR OPS CHECK. REFER N/R 1700 . ACTION CLOSED. 2 L 7 4 4F RT 4A25 2001092600105 20010926 00105 WP 2001 9 26 DHL2001804558 1 20010828 A 5751 SKIN DOUG DC8 DC873F 302199F WP AILERON CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 D-CHECK; RT OTBD AILERON LWR SKIN CRACKED 2 INCH AT XW 546.000.CORR ACTION;REMOVED FASTENERS FROM RT OTBD AILERON LWR SK IN IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED AREA IAW EO DHL 010821, EO-2596, & EO-2001298. CLEANED, TREATED, & PRIMED IAW S RM 51-1-8B. APPLIED SEALANT (PRC) TO FAYING SURFACE IAW SRM 51-1-11 PG 1. INSTALLED FILLER & DOUBLER IAW EO DHL 010821, EO-2001298, SRM 51-1-21 PG 7 & 51-1-15 PG1. REF N/R 0896. ACTION CLOSED. 2 L 7 4 4F RT 4A25 2001092600106 20010926 00106 WP 2001 9 26 DHL2001806009 1 20010831 A 2612 FIRE DETECTOR DOUG DC8 DC873F 302199F WP CARGO BAY MALFUNCTIONED A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 806DH 46002 1) LOWER CARGO FIRE DETECTION DISPLAYS FAULT "AD7031" 2) INSPECTED DETECTOR, RESET CDU OP CK GOOD. IAW DACO S/M/M 26-15-1 STATUS: CLOSED 2 L 7 4 4F RT 4A25 2001092600107 20010926 00107 2001 9 26 DL76L011502 4 20010907 A 2330 HARNESS BOEING 767 767332 1382001 NM CABIN DEFECTIVE A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 199DN 28456 FLIGHT ATTENDANTS REPORTED ELECTRICAL SMELL FROM VIDEO MONITOR AT SEAT 10 F AND G. PER MCC LT AND RT UTILITY BUSSES TUR NED OFF. REPLACED MONITOR. STILL N/G. FOUND BAD HARNESS FROM VDU TO 14 INCH MONITOR. DISCONNECTED PLUGS BOTH SIDE VD U AND MONITOR. NEEDS HARNESS P/N 1303319-001. 2 L 7 2 4F RT A1NM 2001092600108 20010926 00108 NM 2001 9 26 DL76L011533 1 20010914 A 3350 POWER SUPPLY BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 178DN 25143 EMERGENCY PATH LIGHTS INOP FROM ROWS 6A/B TO 20A/B. REPLACED BATTERY POWER SUPPLY UNIT. 2 L 7 2 4F RT A1NM 2001092600109 20010926 00109 EU 2001 9 26 C2XA01BT167 1 20010924 A 3350 AD3127 BATTERY AEROSP ATR42 ATR42320 8680930 EU FAULTY A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 18814 103 BTV---CO3014, DURING LINE CHECK MAINTENANCE FOUND AFT LOWER EMERGENCY EXIT LIGHTS BY SERVICE DOOR AND PASSENGER DOOR ARE INOPERATIVE.....REMOVED AND REPLACED EMERGENCY LIGHT BATTERY IAW ATR42 MM 33-53-21. OPS.CHECKED GOOD. 2 H 7 2 4T RT A53EU 2001092600110 20010926 00110 WP 2001 9 26 DHL2001806010 1 20010901 A 2612 FIRE DETECTOR DOUG DC8 DC873F 302199F WP CARGO BAY FAILED A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 806DH 46002 1) LOWER CARGO FIRE DETECT FAILURE INDICATES AC6772 FALSE ALARM. 2) R&R LOWER SMOKE DETECTOR BATTERIES NO HELP. I TEM XFER TO DMI LOG PER MELB 26-10-1A1 DMI #6960 PLACARD IJNSTALLED. 3) LOWER CARGO FIRE DETECT FAILURE INDIACTOR " AC6772" FALSE ALARM REF DMI 6960. 4) REPLACED SMOKE DETECTOR OPS CK GOOD IAW DC-8 SMM 26-15-05 THIS CLEARS DMI 6960 PLACARDS REMOVED. STATUS: CLOSED 2 L 7 4 4F RT 4A25 2001092600111 20010926 00111 WP 2001 9 26 DHL2001806011 1 20010908 A 2510 SEAT DOUG DC8 DC873F 302199F WP COCKPIT LACK OF LUBE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 1) F/O'S SEAT VERTICAL ADJUSTMENT FAILS TO LOCK PROPERLY. 2) LUBRICATED F/O'S SEAT TRACK AND SLIDE ASSY. LUBRICATE D VERTICAL PIN LOCK. OPS CHECK NORMAL IAW DC-8 MM 25-11-1. STATUS: CLOSED 2 L 7 4 4F RT 4A25 2001092600112 20010926 00112 NE 2001 9 26 DL76L011544 2 20010917 A 7230 COMPRESSOR BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE STALLED A DALA A UNSCHED LANDING R M PARTIAL RPM/PWR LOSS OVER TEMP CL CLIMB 1 SO 27 193DN 20117 28450 727708 NR 2 ENGINE HAD COMPRESSOR STALL AT ROTATION OF 170 KTS. ENGINE TEMP WENT TO 673. ENGINE EXPERIENCED MULTIPLE STALLS. REPLACED NR 2 ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 2001092600113 20010926 00113 WP 2001 9 26 DHL2001806012 1 20010915 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 806DH 46002 1) EMERGENCY LIGHTS STAY ON DIM WITH SWITCH DISARMED. 2) REPLACED EMERGENCY LITE BATTERY PACK SYS OPS CHECK GOOD IAW DC-8 M/M 33-50-1STATUS: CLOSED 2 L 7 4 4F RT 4A25 2001092600114 20010926 00114 NM 2001 9 26 DL76P011541 1 20010916 A 3397 WIRE BOEING 767 767332 1382001 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1402A 25989 ON L/O FOUND SEAT ROWS 12 AND 17 FG EMERGENCY LIGHTS INOP. FOUND WIRES BROKEN. REPLACED LIGHT ASSEMBLIES, OPN CKS GOOD . 2 L 7 2 4F RT A1NM 2001092600115 20010926 00115 NM 2001 9 26 DL76S011514 1 20010909 A 3350 1000677 LIGHT BOEING 767 767332 1382001 NM COCKPIT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 116DL 23275 COCKPIT EMERGENCY LIGHT FAILS TO TEST. REPLACED LIGHT ASSEMBLY AND BATTERIES, EMERGENCY LIGHTS NORMAL NOW. 2 L 7 2 4F RT A1NM 2001092600116 20010926 00116 2001 9 26 DHL2001807022 4 20010525 A 2210 AUTOPILOT SYS DOUG DC8 DC873F 302199F WP COCKPIT MALFUNCTIONED A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 807DH 45990 1) STEADY WARNING HORN DURING CLIMBOUT WITH GEAR UP AND FLAPS RETRACTED. AIR TURNBACKED TO ORD. 2) TROUBLESHOOTI NG FOUND ITEM RELATED TO AUTOPILOT DMI 5739. SEE ITEM 2D FOR AUTOPILOT CORRECTIVE ACTION. AT THIS TIME AUTOPILOT WARNIN G HORN OPERATES NORMALLY PER 22-8-10. 3) ITEM 2D) REF DMI 5739 A/P OFF LIGHT WILL NOT EXTINGUISH. 4) CLEANED B OTH CAPTAINS AND FIRST OFFICER'S AUTOPILOT DISCONNECT SWITCHES. BOTH SWITCHES AND LIGHT WORK NORMALLY PER 22-10-8. THIS CLEARS DMI 5739. NOTE PREVIOUS HISTORY FROM 5/25: AUTOPILOT OFF ANNUNCIATOR LIGHT REMAINS ILLUMINATED. UNABLE TO CA NCEL THE LIGHT. AUTOPILOT APPEARS TO FUNCTION NORMALLY. PLACARDED AUTOPILOT 'INOP' PER 22-1 ASSIGNED DMI NBR 5739. S 2 L 7 4 4F RT 4A25 2001092600117 20010926 00117 NM 2001 9 26 DL76S011527 1 20010906 A 5330 146T32311 SKIN BOEING 767 767332 1382001 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 129DL 24079 THE LOWER FORWARD CORNER OF THE BULK CARGO DOOR CUTOUT WAS FOUND TO BE CRACKED IN THE SKIN ONLY. AT THE SAME LOCATION, THE SKIN AND BEARSTRAP HAD BEEN PREVIOUSLY REWORKED PER SRM ALLOWABLE EDGE DAMAGE LIMITS. ER/A 397956-14 2 L 7 2 4F RT A1NM 2001092600118 20010926 00118 WP 2001 9 26 DHL2001807023 1 20010908 A 2510 SEAT DOUG DC8 DC873F 302199F WP COCKPIT LACK OF LUBE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 1) CAPT'S SEAT BACK WILL NOT LOCK IN POSITION. 2) CLEANED AND LUBED SEAT RECLINE CABLE IAW MM 25-00-00 OP CK OK. STATUS: CLOSED 2 L 7 4 4F RT 4A25 2001092600119 20010926 00119 NM 2001 9 26 DLM11011486 1 20010905 A 5220 HANDLE DOUG MD11 MD11 3023602 NM EMERGENCY EXIT OUT OF POSITION A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 809DE 48480 R1 DOOR EMERGENCY EXIT HANDLE OUT OF POSITION. SERVICED ASSIST BOTTLE, RESET HANDLE. 2 L 7 3 4F RT A22WE 2001092600120 20010926 00120 SO 2001 9 26 SWIA200110161 1 20010818 A 3232 SWIVEL EMB 120 EMB120RT SO MLG DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 200CD 120200 NOSE GEAR AFT DOORS RODS AND SWIVELS WORN AND CORRODED.REMOVED AND REPLACED NOSE LANDING GEAR AFT DOORS RODS AND SWIVELS WITH SERVICEABLE PARTS AS REQUIRED. 2 L 7 2 4T RT A31SO 2001092600121 20010926 00121 NM 2001 9 26 DLM11011524 1 20010910 A 2120 ODOR DOUG MD11 MD11 3023602 NM CABIN DETECTED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 802DE 48473 ACRID ODOR COMING FROM AIR COND SYS, RAN PACKS AND INSPECTED AIRCRAFT. 2 L 7 3 4F RT A22WE 2001092600122 20010926 00122 SO 2001 9 26 SWIA200110162 1 20010818 A 5753 BEARING EMB 120 EMB120RT SO RT WING TE FLAP CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 200CD 120200 RIGHT NACELLE FLAP HINGE BEARINGS 2 EA. CORRODED AND WORN.REPLACED NACELLE FLAP WITH SERVICEABLE FLAP ASSEMBLY AS NEEDED .P/N: 120-40327-002 S/N OFF: 120212 2 L 7 2 4T RT A31SO 2001092600123 20010926 00123 SO 2001 9 26 SWIA200110163 1 20010818 A 5713 STRINGER EMB 120 EMB120RT SO FUEL PANEL CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 200CD 120200 RIGHT MOST INBOARD FUEL PANEL FORWARD STRINGER CRACKED. REPAIRED IAW EMB120 SRM 57-20-03 AS OUTLINED. 2 L 7 2 4T RT A31SO 2001092600124 20010926 00124 SO 2001 9 26 SWIA200110164 1 20010818 A 5713 STRINGER EMB 120 EMB120RT SO FUEL BAY CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 200CD 120200 CRACKED LOWER STRINGER IN FUEL BAY LEFT WING AT NR 2 FUEL ACCESS PANEL BAY AFT.REPAIRED IAW EMB120 SRM 57-20-03. 2 L 7 2 4T RT A31SO 2001092600125 20010926 00125 NM 2001 9 26 DLM11011560 1 20010918 A 7920 ADAPTER DOUG MD11 MD11 3023602 NM PWA 4060 PW4060 52119 NE NR 3 ENGINE BROKEN A DALA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 808DE 39372 48479 723842 OIL QTY ON ENG 3 DROPPED RAPIDLY TO 1 QT AFTER ABOUT 20 MINUTES IN FLIGHT . INITIALLY OIL PRESSURE WAS GOOD, SLOWLY DRO PPED TO THE BOTTOM OF THE GREEN BAND 90 PSI. THE ENGINE WAS OPERATED AT IDLE UNTIL LANDING WITH THIS OIL PRESSURE. ON DECEL DURING ROLLOUT PRESSURE WENT RED IT WAS THEN SHUT DOWN. FOUND OIL COOLER BYPASS VALVE SERVO OIL RETURN LINE ADAPT ER BROKEN. REPLACED AND CKD CHIP DETS, ALL OK. REPLACED MAIN OIL FILTER, NO METAL. RAN ENG T/O POWER, ALL CKS OK. 2 L 7 3 4F 4 F RT A22WE E24NE 2001092600126 20010926 00126 NM 2001 9 26 DLM88011488 1 20010905 A 3260 387 LIGHT DOUG MD88 MD88 3023688 NM COCKPIT INOPERATIVE A DALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 27 968DL 53161 ON APPROACH INTO BDL RIGHT MAIN GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER LOWERING GEAR. PERFORMED PUSH-TO-TEST LIGHT D ID NOT ILLUMINATE. PERFORMED FLY-BY OF TOWER TO VERIFY GEAR DOWN AND VISUALLY CONFIRMED GEAR WAS DOWN. CONFIRMED BULBS WERE BURNT OUT ON RIGHT GEAR LIGHT ASSY. RELAMPED SAME. 2 L 7 2 4F RT A6WE 2001092600127 20010926 00127 NM 2001 9 26 DLM88011489 1 20010905 A 2131 21184904S CONTROLLER DOUG MD88 MD88 3023688 NM CABIN PRESSURE STUCK A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 967DL 53116 AUTO PRESSURIZATION 1 AND 2 INP ON T/O. MANUAL PRESSURE CONTROLLER JAMMED IN MIDWAY POSITION. REPLACED PRESSURIZATION CONTROLLER. 2 L 7 2 4F RT A6WE 2001092600128 20010926 00128 NM 2001 9 26 EISA20010112 1 20010819 A 7931 ST104Z TRANSMITTER BOEING 727 7272M7 138407S NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE FAILED A EISA E ENGINE SHUTDOWN N FALSE WARNING TX TAXI/GRND HDL 1 SW 07 725RW 21502 685552 DURING NR 1 ENG START OIL PRESS STABILIZED AT 25 PSI, BELOW RED RADIAL. ENGINE SHUT DOWN ACCOMPLISHED. REMOVED AND REP LACED OIL PRESSURE TRANSMITTER, OPS CK OK PER MM REF 79-32. 2 L 7 3 4F 4 F A3WE E2EA 2001092600129 20010926 00129 SO 2001 9 26 SWIA200110165 1 20010818 A 5713 STRINGER EMB 120 EMB120RT SO LT WING FUEL BAY CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 200CD 120200 CRACKED LOWER STRINGER IN FUEL BAY LEFT WING AT NR 2 FUEL ACCESS PANEL BAY FWD.REPAIRED IAW EMB120 SRM 57-20-03. 2 L 7 2 4T RT A31SO 2001092600130 20010926 00130 NM 2001 9 26 EISA20010113 1 20010823 A 2910 HYDRAULIC LINE BOEING 727 727223 1384074 NM PWA JT8 JT8D7B 52053 NE NR 1 ENGINE LOOSE A EISA K NONE K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 07 311NE 19703 657422 ON HEADING TO JOIN THE FINAL APPROACH COURSE TO 31R AT JFK, SYSTEM 1 LOW LEVEL LIGHT ILLUMINATED. OBSERVED SYSTEM A HYD RAULIC QUANTITY DECREASING RAPIDLY PAST 2 TO LESS THAN 1 GALLON. REQUESTED A VECTOR OFF THE FINAL APPROACH COURSE TO CO MPLETE THE SYSTEM A LEAK AND SYSTEM A LOSS CHECKLIST. NOTIFIED ATC OF THE HYDRAULIC LOSS AND RETURN FOR A LANDING AT JF K. EMERGENCY EQUIPMENT WAS PRESENT, CLEARED THE RUNWAY AT THE HIGH SPEED TURNOFF. FOUND LOOSE HYD LINE ON NR 1 ENG HYD RAULIC PUMP. RETORQUED B-NUT. RAN ENG PER MM 29-13-01, NO LKS NOTED. A/C OK FOR SRC. 2 L 7 3 4F 4 F A3WE E2EA 2001092600131 20010926 00131 SO 2001 9 26 SWIA200110166 1 20010818 A 5411 FRAME EMB 120 EMB120RT SO RIGHT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 200CD 120200 RIGHT NACELLE FRAME 1 CRACKED AT OUTBOARD TORSION MOUNT.REPLACED RIGHT NACELLE FRAME 1 IAW SB120-54-0036 PART 2. 2 L 7 2 4T RT A31SO 2001092600132 20010926 00132 SO 2001 9 26 SWIA200110167 1 20010818 A 5411 FRAME EMB 120 EMB120RT SO LEFT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 200CD 120200 LEFT NACELLE FRAME 1 CRACKED AT INBOARD TORSION MOUNT.REPLACED LEFT NACELLE FRAME 1 IAW SB120-54-0036 PART 2. 2 L 7 2 4T RT A31SO 2001092600133 20010926 00133 SO 2001 9 26 SWIA200110168 1 20010913 A 7931 TRANSDUCER EMB 120 EMB120ER 3260203 SO RTENG OIL PRESS MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 581SW 120349 RIGHT ENGINE OIL PRESSURE DROPPED BELOW 55 PSI IN FLIGHT BUT REMAINED ABOVE 50 PSI.REPLACED RT ENGINE OIL PRESSURE TRANS DUCER WITH SERVICEABLE UNIT. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001092600134 20010926 00134 NM 2001 9 26 EISA20010117 1 20010828 A 2910 HYDRAULIC SYSTEM BOEING 727 727223 1384074 NM A SYSTEM LOW A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 312NE 20193 AFTER TAKEOFF WITH GEAR UP AND FLAPS AT 2 DEGREES HYD SYS A QTY DROPPED TO 1.6 GALLONS. SERVICED A-SYSTEM HYDRAULICS, R AN ALL FLT CONTROLS, SYS OPS OK AND A-SYS QTY IND FALL. 2 L 7 3 4F A3WE 2001092600135 20010926 00135 NM 2001 9 26 EISA20010119 1 20010829 A 5510 STRUCTURE BOEING 727 727243 138408D NM HORIZ STAB CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 17410 21663 RT HORIZONTAL STAB O/B T/E CORNER IS CRACKED, TOP SIDE. FOUND DURING B-CHECK. ROUTED OUT CRACK IAW B727 SRM 55-10-1. ND T VERIFIED CRACK BEING REMOVED. FABRICATED DOUBLER AND FILLER PER EO NR 01-236. INSTALLED REPAIR PER EO 01-236 & B727 S RM 57-30-2 WITH APPROVED 8110-3 DATED 08-27-01. 2 L 7 3 4F RT A3WE 2001092600136 20010926 00136 NM 2001 9 26 UPS01236814 1 20010515 A 5330 SKIN BOEING 727 727247 138408F NM B.S. 848 STR 7L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE:C CORROSION ON CROWN SKIN B.S. 848 4" BELOW STR 7L BLENDED CORROSION AT B.S. 848 4" BELOW STR 7L IN AN AREA OF 1"X2" REMOVED .032" FROM ORIGINAL THICKNESS OF .090", FOUND TO BE OUT LIMITS IAW SRM 53-30-1 PG 1 - 2B REPAIR ED AREA IAW SRM 53-30-3 2 L 7 3 4F A3WE 2001092600137 20010926 00137 NM 2001 9 26 EISA20010121 1 20010907 A 3350 BATTERY BOEING 727 7272M7 138407S NM CABIN DISCHARGED A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 725RW 21502 EMERGENCY EXIT LIGHTING SYSTEM DOES NOT TEST OR FUNCTION. NOTED ON PREFLIGHT AT AUS. REMOVED AND REPLACED BATTERIES PE R MM CH 33-50, OPS CK NORMAL. 2 L 7 3 4F A3WE 2001092600138 20010926 00138 NM 2001 9 26 ERKR200100144 1 20010703 A 3350 LIGHT BOEING 737 7372K9 1384494 NM CABIN MISSING B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 714A 23405 EMERGENCY LIGHTING MISSING, EXIT SIGNS AT L-1, 2, R-1, 2 AND OVERWING EXITS. EMERGENCY PATH LIGHTING MISSING. INSTALLI NG NEW SYSTEM. 2 L 7 2 4F A16WE 2001092600139 20010926 00139 NM 2001 9 26 ERKR200100166 1 20010830 A 7830 E5033515 THRUST REVERSER DOUG MD90 MD9030 3023690 NM NR 1&2 ENGINE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 901TR 53578 NR 1 ENGINE AND NR 2 ENGINE THRUST REVERSER INNER SLEEVES HAVE AREAS OF CORROSION. REPAIRED PER ECRA'S P4-MDF-78-120 (1 21, 122, 123)-EAC. 2 L 7 2 4F RT A6WE 2001092600140 20010926 00140 EA 2001 9 26 SWIA200110169 1 20010905 A 7120 SUPPORT CNDAIR CL600 CL6002B19 EA ENGINE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 406SW 7030 DURING INSPECTION PER SB 53-058 FOUND ENGINE SUPPORT BEAM IS CRACKED. COMPLIED WITH REO 601R-53-61-345 AND REO 601R-5 3-61-366. REMOVED BOTH ENGINES FOR REPAIR OF ENGINE SUPPORT BEAM. 2 L 7 2 4F RT A21EA 2001092600142 20010926 00142 SO 2001 9 26 SWIA200110171 1 20010916 A 3230 LANDING GEAR EMB 120 EMB120ER 3260203 SO MAINS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 NM 07 250YV 120250 LANDING GEAR WOULD NOT EXTEND UNTIL THE FOURTH CYCLE OF THE HANDLE, AT WHICH POINT THE GEAR EXTENDED NORMALLY, WITH THRE E GREEN A & B LIGHTS ILLUMINATED. AIRCRAFT WAS FERRIED FROM RDD TO SFO. PERFORMED GEAR SWING. OPS CHECK GOOD THROUGH C YCLING OF THE LANDING GEAR SELECTOR MANY TIMES. UNABLE TO DUPLICATE DISCREPANCY. CLEARED FERRY FLIGHT. GEAR PINS REMO VED AND STOWED. 2 L 7 2 4T RT A31SO 2001092600143 20010926 00143 NM 2001 9 26 HNAA0100052 1 20010830 A 5410 85410012001 ANGLE DHAV DHC8 DHC8102 2809003 NM NR 2 NACELLE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 925HA 35114 111 NR 2 NACELLE HORSE COLLAR WAS FOUND CRACKED IN RADIUS OF FWD UPPER CLOSING ANGLE JUST ABOVE ENGINE HOIST ATTACH BRACKET. REPAIRED PER EO8-54-01-799. 2 H 7 2 4T RT A13NM 2001092600144 20010926 00144 SO 2001 9 26 LR7A01076 1 20010906 A 2170 1858486 COALESCER BAG LKHEED 382 382G 526414U SO A/C BAY DIRTY A LR7A H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AL 03 405LC 133 5025 FLIGHT CREW REPORTED FLIGHT DECK AIR CONDITIONING SYSTEM PRODUCES MODERATE SMOKE IN COCKPIT DURING NORMAL OPERATION. RE PLACED FLIGHT DECK AIR CONDITIONING WATER SEPARATOR COALESCER ASSY, OPS CK GOOD PER SMP 581 21A-50 PAGE 17 AND 201. 2 H 7 4 4T A1SO 2001092600145 20010926 00145 SO 2001 9 26 SWIA200110172 1 20010915 A 3241 140043 TRANSDUCER EMB 120 EMB120ER 3260203 SO ANTI-SKID SYS MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 308SW 120326 ABORTED TAKEOFF DUE TO ANTI-SKID LIGHT ON OVERHEAD. ANTI-SKID DISENGAGES (ON RIGHT SIDE) THROUGH 60 KTS ON TAKEOFF ROLL UNTIL AIRBORNE, THEN NORMAL IN AIR. UPON LANDING DISENGAGES UPON TOUCHDOWN THROUGH 20KTS, THEN NORMAL AT LOW SPEEDS.RE MOVED AND REPLACED LEFT INBOARD WHEEL SPEED TRANSDUCER. OPS CHECK GOOD, REF. 32-42-04. P/N: 140-043 S/N OFF: 81982 2 L 7 2 4T RT A31SO 2001092600146 20010926 00146 EU 2001 9 26 MALA010662 1 20010820 A 2730 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 437XJ 340B437 DURING 4K-CHECK IN CWA, LT ELEVATOR FWD O/B FUSELAGE CABLE IS CHAFED. MAINTENANCE REPLACED LT ELEVATOR FWD FUSELAGE CAB LE REPLACED IAW SF340 AMM 27-31-15. 2 L 7 2 4T RT A52EU 2001092600147 20010926 00147 EU 2001 9 26 MALA010663 1 20010820 A 2710 7227105613 CONTROL CABLE SAAB SF340 340B 7860101 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 437XJ 340B437 DURING 4K-CHECK, FOUND LT AILERON FWD O/B FUSELAGE CABLE IS CHAFED. MAINTENANCE REPLACED LT O/B AILERON FWD FUSELAGE CA BLE IS CHAFED. MAINTENANCE REPLACED LT AILERON FWD O/B FUSELAGE CABLE WITH NEW CABLE P/N 7227105-613. 2 L 7 2 4T RT A52EU 2001092600148 20010926 00148 EU 2001 9 26 MALA010664 1 20010820 A 2730 7227705643 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 437XJ 340B437 DURING 4K-CHECK, FOUND LT ELEVATOR FWD I/B FUSELAGE CABLE IS CHAFED. MAINTENANCE REPLACED LT I/B FUSELAGE CABLE IS CHAF ED. MAINTENANCE REPLACED LT I/B FWD 7227705-643 P/N 7227705-643 IAW SF340 MM 27-31-15. 2 L 7 2 4T RT A52EU 2001092600149 20010926 00149 EU 2001 9 26 MALA010665 1 20010820 A 2710 7227105621 CONTROL CABLE SAAB SF340 340B 7860101 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 437XJ 340B437 DURING 4K-CHECK IN CWA, LT I/B AILERON FWD FUSELAGE CABLE IS CHAFED. MAINTENANCE REPLACED LT I/B AILERON FWD FUSELAGE C ABLE P/N 7227105-621/623 IAW SF340 AMM 27-11-25. 2 L 7 2 4T RT A52EU 2001092600150 20010926 00150 EU 2001 9 26 MALA010666 1 20010820 A 2710 7227105614 CONTROL CABLE SAAB SF340 340B 7860101 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 437XJ 340B437 DURING 4K-CHECK IN CWA, RT I/B AILERON FWD FUSELAGE CABLE IS CHAFED. MAINTENANCE REPLACED RT I/B AILERON FWD FUSELAGE C ABLE WITH NEW CABLE P/N 7227105-614 IAW SF340 AMM 27-11-25-4. 2 L 7 2 4T RT A52EU 2001092600151 20010926 00151 EU 2001 9 26 MALA010667 1 20010820 A 2710 7227105624 CONTROL CABLE SAAB SF340 340B 7860101 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 437XJ 340B437 DURING 4K-CHECK IN CWA, RT O/B AILERON FWD FUSELAGE CABLE IS CHAFED. MAINTENANCE REPLACED RT O/B FWD FUSELAGE CABLE WIT H NEW CABLE P/N 7227105-624 IAW SF 340 AMM 27-11-25-4. 2 L 7 2 4T RT A52EU 2001092600152 20010926 00152 EU 2001 9 26 MALA010668 1 20010820 A 2730 7227705643 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 437XJ 340B437 DURING 4K-CHECK IN CWA, FOUND RT I/B ELEVATOR FWD FUSELAGE CABLE IS CHAFED. MAINTENANCE REPLACED RT I/B FWD FUSELAGE CA BLE P/N 7227705-643, IAW SF340 AMM 27-31-15. 2 L 7 2 4T RT A52EU 2001092600153 20010926 00153 EA 2001 9 26 SWIA200110173 1 20010914 A 7732 ANALYZER CNDAIR CL600 CL6002B19 EA ENGINE MALFUNCTIONED A SWIA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 NM 07 416SW 7089 N1 VIB AND ITT 899 DEGREES SHORTLY AFTER DEPARTURE (RIGHT SIDE). HAD TO CONTINUE AND REDUCE RIGHT POWER TO MAINTAIN CON TROL OF POWER SETTING. VIB ON LEFT .6, RIGHT WAS 1.6. RETURNED TO FIELD.MM 71-00-00 FIGURE 505 PAGE 521, ITT C DEGREE TABLE INDICATED NO MAINTENANCE ACTION REQUIRED FOR N1 VIB & 899 DEGREES ITT. GE OPERATION LIMITS TABLE 3-1 SHOWS WITHIN LIMITS. 2 L 7 2 4F RT A21EA 2001092600154 20010926 00154 SO 2001 9 26 SWIA200110174 1 20010915 A 2750 12042642507 SELECTOR SWITCH EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 07 207SW 120266 FLAPS WILL NOT MOVE WHEN 45 DEGREES IS SELECTED.REMOVED AND REPLACED FLAP SELECTOR LEVER IAW MM 27-50-01. OPS CHECK GOO D IAW 27-50-00. 2 L 7 2 4T RT A31SO 2001092600155 20010926 00155 EA 2001 9 26 SWIA200110175 1 20010916 A 2760 CONTROL UNIT CNDAIR CL600 CL6002B19 EA GROUND SPOILERS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 906SW 7510 INBOARD GROUND SPOILER FAULT MESSAGE.REPLACED SECU. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2001092600156 20010926 00156 SO 2001 9 26 SWIA200110176 1 20010905 A 2910 LINE EMB 120 EMB120ER 3260203 SO HYD SYSTEM LEAKING A SWIA O OTHER K F FLUID LOSS FLT CONT AFFECTED AP APPROACH 1 NM 07 190SW 120050 BLUE HYDRAULIC FILTER LIGHT ILLUMINATED , THEN MAIN PUMP LOW PRESSURE LIGHT ILLUMINATED WHEN TRIED FLAPS 15 DEGREES LOST ALL BLUE HYDRAULIC LEVEL AND PRESSURE. HYD FLUID LEAKING FROM R MAIN GEAR BAY.REPAIRED BROKEN HYDRAULIC LINE, CHANGED E NGINE DRIVEN PUMP, PERFORMED HYDRUALIC FLUSH AND CHANGED ALL FILTERS IAW MM 29-00-00 OPS AND LEAK CHECK GOOD PN ON PV3-0 22-29 SN MX-490588 SN MX-523017 2 L 7 2 4T RT A31SO 2001092600157 20010926 00157 EU 2001 9 26 MALA010669 1 20010820 A 2730 7227105712 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 437XJ 340B437 FOUND DURING 4K-CHECK IN CWA, RT O/B ELEVATOR FWD FUSELAGE CABLE IS CHAFED. MAINTENANCE REPLACED RT O/B FWD ELEVATOR CA BLE P/N 7227105-712 IAW SF340 AMM 27-31-15. 2 L 7 2 4T RT A52EU 2001092600158 20010926 00158 EU 2001 9 26 MALA010672 1 20010821 A 2720 7227105582 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 437XJ 340B437 DURING 4K-CHECK IN CWA, RT RUDDER AFT SINGLE CABLE OF CIRCUIT I IS CHAFED. MAINTENANCE REPLACED RT RUDDER AFT SINGLE CA BLE P/N 7227105-582 OF CIRCUIT I IAW SF340 AMM 27-21-25. 2 L 7 2 4T RT A52EU 2001092600159 20010926 00159 SO 2001 9 26 COMA0110145 1 20010925 A 2431 CIRCUIT BREAKER EMB 120 EMB120RT SO A COMA O OTHER L NO TEST IN INSP/MAINT 1 SO 01 463CA 120267 FLIGHT #5057. DURING PRE-FLIGHT CREW DISCOVERED THE CIRCUIT BREAKER FOR THE FLIGHT IDLE STOP SOLENOID TRIPPED.PERFOMRED RESET AND OPERATIONAL CHECK OF THE FLIGHT IDLE STOP CIRCUIT BREAKER. 2 L 7 2 4T RT A31SO 2001092600160 20010926 00160 EA 2001 9 26 COMA0160752 1 20010925 A 5300 STRUCTURE CNDAIR CL600 CL6002B19 EA A COMA D RETURN TO BLOCK O OTHER CL CLIMB 1 SO 01 995CA 7229 FLIGHT #5574. DURING CLIMB OUT OF GRB AIRCRAFT ENCOUNTERED MULTIPLE BIRD STRIKES, RETURNED TO THE FIELD.PERFORMED BIRD S TRIKE INSPECTION, NO DAMAGE NOTED. 2 L 7 2 4F RT A21EA 2001092600161 20010926 00161 EA 2001 9 26 COMA0160753 1 20010924 A 2751 860D10018ABC FCU CNDAIR CL600 CL6002B19 EA AVIONICS BAY FAULTY A COMA K NONE J WARNING INDICATION DE DESCENT 1 SO 01 958CA 14177 7111 DUIRNG DESCENT INTO CVG RECEIVED A FLAP FAIL CAUTION MESSAGE, LANDED WITH ZERO DEGREE FLAPS.REPLACED THE FLAP ELECTRONIC CONTROL UNIT. 2 L 7 2 4F RT A21EA 2001092600162 20010926 00162 EU 2001 9 26 MALA010673 1 20010823 A 2720 7227105562 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 437XJ 340B437 FOUND DURING 4K-CHECK IN CWA, LT O/B RUDDER CABLE OF DUAL CIRCUIT I IS CHAFED. MAINTENANCE REPLACED LT O/B RUDDER CABLE IN DUAL CIRCUIT I IAW SAAB AMM 27-21-25-4 P/N 7227105-562. 2 L 7 2 4T RT A52EU 2001092600163 20010926 00163 EU 2001 9 26 MALA010674 1 20010824 A 2720 7227105562 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 437XJ 340B437 DURING 4K-CHECK IN CWA, RT O/B RUDDER CABLE OF DUAL CIRCUIT I IS CHAFED. MAINTENANCE INSTALLED RT O/B RUDDER CABLE P/N 7227105-562, IAW SF3 AMM 27-21-25. 2 L 7 2 4T RT A52EU 2001092600164 20010926 00164 EU 2001 9 26 MALA010677 1 20010828 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 437XJ 340B437 DURING 4K-CHECK IN CWA, FRAME AND ANGLE AT STA 258 HAS HEAVY CORROSION. COMPLETED REPAIR TO FRAME IAW EO S53102. 2 L 7 2 4T RT A52EU 2001092600165 20010926 00165 EU 2001 9 26 MALA010678 1 20010831 A 3297 85106RC84SNB WIRE SAAB SF340 340B 7860101 EU RT MLG BROKEN A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 435XJ 340B435 DURING EMERGENCY EXTENSION CHECK MAINTENANCE NOTED INFINITE RESISTANCE TO RT MLG SEPARATION BOLT. MAINTENANCE FOUND ALL WIRES CORRODED AND BROKEN IN CANNON PLUG. MAINTENANCE REPLACED CANNON PLUGS 4GBP1 PN 851-06RC8-4SNB. OPS CHECK GOOD I AW MAL TASK CARD 323108. 2 L 7 2 4T RT A52EU 2001092600166 20010926 00166 EU 2001 9 26 MALA010679 1 20010908 A 2150 MOTOR SAAB SF340 340B 7860101 EU A/C BAY FAILED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 15 450XJ 340B450 AFTER DEPLANING FLIGHT 3180 GROUND OPS HOOKED UP EXTERNAL POWER. SHORTLY AFTER, VISIBLE SMOKE WAS SMELLED IN CABIN. MAIN TENANCE VISUALLY INSPECTED CABIN AREA, FOUND SIDEWALL LIGHTS AT ROW 1-5 AND OVERHEAD LIGHTS AT ROWS 9A AND 10, SUSPECT B AD LIGHT SOCKET AND/OR BALLAST. DEFERRED ALL SIDEWALL LIGHTS AS A PRECAUTIONARY MEASURE DUE TO SMOKE IN CABIN SMELL. MA INTENANCE RESET BREAKERS, RELAMPED LIGHTS. MAINTENANCE PERFORMED FURTHER INVESTIGATION AND TROUBLESHOOTING FOUND SUPPLEM ENTAL A/C MOTOR BURNED AND MELTED. MAINTENANCE REPLACED MOTOR. 2 L 7 2 4T RT A52EU 2001092600167 20010926 00167 EU 2001 9 26 MALA010681 1 20010909 A 7930 523525 INDICATOR SAAB SF340 340B 7860101 EU COCKPIT FAULTY A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 408XJ 340B408 ON CLIMBOUT NOTICED RT PROP OIL TEMP IN YELLOW ARC (>77 DEGREE, MAX LIMIT) AT 40 PERCENT TG IT WAS RIGHT AT THE MAX LIMI T OF 77 DEGREES. EVEN AT GROUND IDLE IT WAS AT MAX LIMIT. MAINTENANCE REMOVED AND REPLACED RT OIL PRESS/TEMP GAUGE WIT H SERVICEABLE UNIT P/N 523525 IAW SF340 MM, ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2001092600168 20010926 00168 EU 2001 9 26 MALA010682 1 20010829 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 439XJ 340B439 DURING 4K-CHECK IN CWA, DENTS ON LT FUSELAGE APPROX STA 354 ARE OUT OF LIMITS. MAINTENANCE REPAIRED DENTS IAW MAL EO530 09 AND SRM 53-70-10-2, NR 5. 2 L 7 2 4T RT A52EU 2001092600169 20010926 00169 EU 2001 9 26 MALA010683 1 20010829 A 2710 7227151521 CONTROL CABLE SAAB SF340 340B 7860101 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 439XJ 340B439 DURING 4K-CHECK IN CWA, RT O/B AILERON FWD WING CABLE IS CHAFED. MAINTENANCE REPLACED RT O/B WING AILERON CABLE WITH NE W P/N 7227151-521, IAW AMM 27-11-25. 2 L 7 2 4T RT A52EU 2001092600170 20010926 00170 EU 2001 9 26 MALA010684 1 20010829 A 2710 7227151522 CONTROL CABLE SAAB SF340 340B 7860101 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 439XJ 340B439 DURING 4K-CHECK IN CWA, LT O/B AILERON FWD WING CABLE IS CHAFED. MAINTENANCE REMOVED AND REPLACED LT O/B AILERON FWD WI NG CABLE WITH A NEW CABLE P/N 7227151-522 IAW SF3 AMM 27-11-25 AND 27-11-00 AND 27-11-45. 2 L 7 2 4T RT A52EU 2001092600171 20010926 00171 WP 2001 9 26 ARWA0010903 1 20010922 A 3260 H146 SWITCH DOUG DC8 DC863F 302198F WP A ARWA O OTHER J WARNING INDICATION LD LANDING 1 SO 19 441J 45988 LOG PAGE 106071. DISCREPANCY: L/H MAIN LANDING GEAR DOWN INDICATOR INOP DURING LANDING ROLL. CHECKLIST ACCOMPLISHED. AIR CRAFT LANDED WITHOUT INCIDENT. CORRECTIVE ACTION: REPLACED L/H MAIN LANDING GEAR DOWN LOCK SWITCH AND CONNECTOR AND ACCO MPLISHED ALL REQUIRED TESTS ON LANDING GEAR INDICATION SYSTEM IAW MM 32-60-0 TEST GOOD. 2 L 7 4 4F 4A25 2001092600172 20010926 00172 EU 2001 9 26 MALA010685 1 20010830 A 2730 7227105711 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 439XJ CT79B DURING 4K-CHECK IN CWA, LT O/B FWD ELEVATOR FUSELAGE CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED LT O/B FWD ELEVATOR FUSELAGE CABLE P/N 7227105-711 IAW SF340 AMM 27-31-15. 2 L 7 2 4T RT A52EU 2001092600173 20010926 00173 EU 2001 9 26 MALA010686 1 20010830 A 2720 7227105582 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 439XJ CT79B DURING 4K-CHECK IN CWA, LT CIRCUIT I AFT SINGLE RUDDER CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED LT CIRCUIT 1 AFT SINGLE RUDDER CABLE P/N 7227105-582 IAW SF340 AMM 27-21-25. 2 L 7 2 4T RT A52EU 2001092600174 20010926 00174 EU 2001 9 26 MALA010687 1 20010903 A 2720 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 439XJ 340B439 DURING 4K-CHECK IN CWA, LT O/B DUAL CIRCUIT I FUSELAGE RUDDER CABLE IS CHAFED. MAINTENANCE REMOVED AND REPLACED LT O/B DUAL CIRCUIT 1 FUSELAGE RUDDER CABLE P/N 7227105-562 IAW SF340 AMM 27-21-25. 2 L 7 2 4T RT A52EU 2001092600175 20010926 00175 EU 2001 9 26 MALA010688 1 20010903 A 2720 7227105562 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 439XJ 340B439 DURING 4K-CHECK IN CWA, RT O/B DUAL CIRCUIT 1 FUSELAGE RUDDER CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED RT O/B DUA L CIRCUIT 1 FUSELAGE RUDDER CABLE P/N 7227105-562 IAW SF340 AMM 27-21-25. 2 L 7 2 4T RT A52EU 2001092600176 20010926 00176 EU 2001 9 26 MALA010689 1 20010903 A 2730 7227105712 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 439XJ 340B439 DURING 4K-CHECK IN CWA, RT O/B FWD ELEVATOR FUSELAGE CABLE CHAFED. MAINTENANCE REPLACED RT O/B FWD ELEVATOR FUSELAGE CA BLE P/N 7227105-712 IAW SF340 AMM 27-31-15. 2 L 7 2 4T RT A52EU 2001092600177 20010926 00177 EU 2001 9 26 MALA010690 1 20010903 A 2710 7227105613 CONTROL CABLE SAAB SF340 340B 7860101 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 439XJ 340B439 DURING 4K-CHECK IN CWA, LT O/B FWD AILERON FUSELAGE CABLE CHAFED. MAINTENANCE REPLACED LT O/B FWD AILERON CABLE IN FUSE LAGE WITH NEW CABLE P/N 7227105-613 IAW SF340AMM 27-11-25-4. 2 L 7 2 4T RT A52EU 2001092600178 20010926 00178 EU 2001 9 26 MALA010691 1 20010903 A 2710 7227105623 CONTROL CABLE SAAB SF340 340B 7860101 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 439XJ 340B439 DURING 4K-CHECK IN CWA, LT I/B FWD AILERON FUSELAGE CABLE CHAFED. MAINTENANCE REPLACED LT I/B FWD AILERON CABLE IN FUSE LAGE WITH NEW CABLE P/N 7227105-623 IAW SF340 AMM 27-11-25-4. 2 L 7 2 4T RT A52EU 2001092600179 20010926 00179 EU 2001 9 26 MALA010692 1 20010903 A 2710 7227105624 CONTROL CABLE SAAB SF340 340B 7860101 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 439XJ 340B439 DURING 4K-CHECK IN CWA, RT O/B FWD AILERON CABLE IN FUSELAGE IS CHAFED. MAINTENANCE REPLACED RT O/B FWD AILERON CABLE I N FUSELAGE WITH NEW CABLE P/N 7227105-624 SF340 AMM 27-11-25-4. 2 L 7 2 4T RT A52EU 2001092600180 20010926 00180 EU 2001 9 26 MALA010693 1 20010903 A 2730 7227705643 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 439XJ 340B439 DURING 4K-CHECK IN CWA, RT I/B ELEVATOR FUSELAGE CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED RT I/B ELEVATOR FUSELAG E CABLE P/N 7227705-643 IAW SF340AMM 27-31-15. 2 L 7 2 4T RT A52EU 2001092600181 20010926 00181 EU 2001 9 26 MALA010694 1 20010903 A 2730 7227705643 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 439XJ 340B439 DURING 4K-CHECK IN CWA, LT I/B ELEVATOR FUSELAGE CABLE IS CHAFED. MAINTENANCE REMOVED AND REPLACED LT I/B ELEVATOR FUSE LAGE CABLE P/N 7227705-643 IAW SF340 AMM 27-31-15. 2 L 7 2 4T RT A52EU 2001092600182 20010926 00182 EU 2001 9 26 MALA010695 1 20010906 A 5347 7253721495 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 439XJ 340B439 DURING 4K-CHECK IN CWA, RT GALLEY SEAT TRACK PROFILE HAS HEAVY CORROSION. MAINTENANCE REMOVED AND INSTALLED NEW PROFILE P/N 7253721-495 AND RAIL P/N 7253721-459 IAW SRM CHAPTER 51. 2 L 7 2 4T RT A52EU 2001092600183 20010926 00183 EU 2001 9 26 MALA010696 1 20010906 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 439XJ 340B439 DURING 4K-CHECK IN CWA, AFT PORTION OF LT CENTER IS SEAT TRACK LBL 18.3 HAS HEAVY CORROSION FROM APPROXIMATELY STA 686.5 TO 633 ON FLOORBOARD FLANGE. MAINTENANCE TREATED CORROSION AND REPAIRED SEAT TRACK IAW SRM 53-70-60, MAL EO S53078. 2 L 7 2 4T RT A52EU 2001092600184 20010926 00184 NE 2001 9 26 MALA010698 3 20010914 A 6140 522742 INDICATOR SAAB SF340 340B 7860101 EU ROTOL R354 R3544123F13 NE COCKPIT ERRATIC A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 452XJ 340B452 DURING FLIGHT 2933, LT PROP RPM INDICATION ERRATIC. INDICATION VARIES FROM ACTUAL RPM AND ZERO INTERMITTENTLY. AIR TUR NBACK TO MSP. MAINTENANCE REMOVED AND REPLACED LT PROP INDICATOR P/N 522742, S/N ON 0387128, S/N OFF 9802872 IAW AMM 61 -40-05-2. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 6 C P61GL 2001092600185 20010926 00185 NM 2001 9 26 01FDEA00857 1 20010926 A 5210 SKIN BOEING 727 72722 1384002 NM DOORS CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 150FE 19141 N 418 EXTERIOR SKIN CRACKED AT LWR HINGE CUTOUT. R/R SKIN PER SRM 52-00-03. 2 L 7 3 4F A3WE 2001092600186 20010926 00186 NM 2001 9 26 01FDEA00859 1 20010926 A 5752 SKIN BOEING 727 72722 1384002 NM RIGHT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 150FE 19141 N 457 RIGHT OUTBOARD AILERON TAB LEAD EDGE CRACKED. R/R TAB PER MM 27-10-041-4. 2 L 7 3 4F A3WE 2001092600187 20010926 00187 EU 2001 9 26 MALA010700 1 20010909 A 3080 465465240 PRINTED CKT BOAR BAC 146 AVRO146RJ85A 1500097 EU ICE PROTECTION FAULTY A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 520XJ E2345 DURING FLIGHT 3681 ICE PROTECTION LOOK-UP LIGHT ILLUMINATED ON CWP WITH NO OVERHEAD INDICATION. CREW WAS HEADING INTO W EATHER. AIR TURNBACK TO MEM. MAINTENANCE REPLACED PCB WQ7 P/N 46546-524-0, S/N ON 3211, S/N OFF 3204, REPLACED WQ1 P/N 46546-514, S/N ON 3739, S/N OFF 3566. TESTED OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 2001092600188 20010926 00188 EU 2001 9 26 MALA010703 1 20010806 A 5330 SKIN BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 526XJ E2351 IN CVG, 2 DENTS STRADDLING FRAME 20 ON LT FUSELAGE INITIALED PLANNING WATCH TO ACCOMPLISH A CLOSE VISUAL INSPECTION OF D ENTED AREA EVERY 300 FLIGHTS PER EA01-00142 UNTIL PERMANENT REPAIR IS COMPLETED. MAINTENANCE REPAIRED IAW EO A53053 ON LT SIDE FUSELAGE FRAME 20. 2 H 7 4 4F RT A49EU 2001092600189 20010926 00189 EU 2001 9 26 MALA010705 1 20010917 A 2910 L387105A SWIVEL SAAB SF340 SF340A 7850100 EU RT MLG WW LEAKING A MALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 15 991XJ 340A091 DURING GEAR RETRACTION ON FLIGHT 3236, LEAK SOMEWHERE IN RT WHEEL WELL CAUSED MAIN ACCUMULATOR AND RESERVOIR TO DECREASE TO ZERO. GEAR WAS EXTENDED BY T-HANDLE. PERFORMED A ZERO FLAP LANDING. AIR TURNBACK TO RST. MAINTENANCE REPLACED H YDRAULIC SWIVEL AT TOP OF DRAG LINK (GOING TO DOWN LOCK ACTUATOR) P/N L387105A. PERFORMED LEAK AND OPS CHECKS OF GEAR A ND EMERGENCY EXTENT ION TEST PER AMM 32-30-00. REPLACED LT AND RT SEPARATION BOLTS 32-34-15, PERFORMED TEST OF SEPARATI ON BOLTS ELECT SYS 32-34-20. 2 L 7 2 4T RT A52EU 2001101000013 20011010 00013 NM 2001 10 10 F3LA200100109 1 20010924 A 5310 DOOR FRAME BOEING 737 7372Y5 1384554 NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 921WA 2755 23039 DURING C-3 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT DOOR FRAME CRACKED AT LOWER SET OF BACK FASTENERS. REPAIRED PER SRM 51-40-04. 2 L 7 2 4U RT A16WE 2001092600190 20010926 00190 EU 2001 9 26 MALA010706 1 20010911 A 2730 7227105712 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438XJ 340B438 DURING 4K-CHECK IN CWA, RT O/B ELEVATOR FWD FUSELAGE CABLE IS CHAFED. MX REPLACED RT O/B FWD FUSELAGE ELEVATOR CABLE P/ N 7227105-712. 2 L 7 2 4T RT A52EU 2001092700001 20010927 00001 SO 2001 9 27 SWIA200110178 1 20010919 A 2750 CONTROL UNIT EMB 120 EMB120RT SO TE FLAPS MALFUNCTIONED A SWIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 1105G 120105 TAXI OUT RECEIVED FLAP CONTROL FAULT ANNUNCIATION ON OUTBOARD PAIR, ONE ROW OF LIGHTS. RETURNED TO GATE.REPLACED FLAP C ONTROL UNIT. OPS CHECK GOOD.S/N ON: 0016 S/N OFF: 156 2 L 7 2 4T RT A31SO 2001092700003 20010927 00003 SO 2001 9 27 SWIA200110180 1 20010803 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO LEFT SIDEWALL CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 189SW 120048 LEFT REAR SIDEWALL SEAT TRACK IS CORRODED.REMOVED AND REPLACED LEFT REAR SIDEWALL SEAT TRACK WITH NEW PART IAW 53-01-05 .P/N: 120-26865-005 2 L 7 2 4T RT A31SO 2001092700004 20010927 00004 SO 2001 9 27 SWIA200110181 1 20010803 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO LEFT REAR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 189SW 120048 LEFT REAR FLOOR TRACK IS CORRODED.REMOVED AND REPLACED LEFT REAR FLOOR SEAT TRACK WITH NEW PART IAW 53-01-05.P/N: 120-2 6863-605 2 L 7 2 4T RT A31SO 2001092700005 20010927 00005 SO 2001 9 27 SWIA200110182 1 20010803 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO RIGHT REAR FLOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 189SW 120048 RIGHT REAR FLOOR TRACK IS CORRODED.REMOVED AND REPLACED RIGHT REAR FLOOR SEAT TRACK WITH NEW PART IAW 53-01-05.P/N: 120 -26865-005 2 L 7 2 4T RT A31SO 2001092700006 20010927 00006 SO 2001 9 27 SWIA200110183 1 20010803 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO RIGHT REAR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 189SW 120048 RIGHT REAR SIDEWALL TRACK IS CORRODED.REMOVED AND REPLACED RIGHT REAR SIDEWALL SEAT TRACK WITH NEW PART IAW 53-01-05.P/N : 120-15996-005. 2 L 7 2 4T RT A31SO 2001092700007 20010927 00007 SO 2001 9 27 SWIA200110184 1 20010803 A 7120 DOUBLER EMB 120 EMB120ER 3260203 SO LEFT ENGINE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 189SW 120048 LEFT ENGINE CRADLE AFT INBOARD DOUBLER CRACKED.REMOVED CRACKED DOUBLER. FABRICATED AND INSTALLED SERVICEABLE DOUBLER IA W EMB SRM 51-40-02. 2 L 7 2 4T RT A31SO 2001092700008 20010927 00008 SO 2001 9 27 SWIA200110185 1 20010803 A 5520 HINGE EMB 120 EMB120ER 3260203 SO RIGHT ELEVATOR LOOSE A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 189SW 120048 RIGHT ELEVATOR OUTBOARD AND MIDDLE HINGE POINTS ARE LOOSE.REPLACED RIGHT ELEVATOR HINGE ARM ASSEMBLY AND MIDDLE HINGE PO INT IAW MM SRM 51-40-02. 2 L 7 2 4T RT A31SO 2001092700009 20010927 00009 SO 2001 9 27 SWIA200110186 1 20010803 A 5520 BEARING EMB 120 EMB120ER 3260203 SO LEFT ELEVATOR WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 189SW 120048 LEFT ELEVATOR OUTBOARD HINGE POINT BEARINGS AND BUSHINGS WORN.REMOVED AND REPLACED LEFT ELEVATOR OUTBOARD HINGE POINT BE ARINGS AND BUSHINGS WITH A SERVICEABLE BEARINGS AND BUSHINGS IAW MM 20. 2 L 7 2 4T RT A31SO 2001092700010 20010927 00010 SO 2001 9 27 SWIA200110187 1 20010803 A 5520 BEARING EMB 120 EMB120ER 3260203 SO ELEVATOR WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 189SW 120048 LEFT AND RIGHT ELEVATOR BELLCRANK/TORQUE TUBE BEARINGS WORN AND RATCHET.REPLACED BEARINGS IAW 27-31-00. 2 L 7 2 4T RT A31SO 2001092700011 20010927 00011 SO 2001 9 27 SWIA200110188 1 20010803 A 5411 FRAME EMB 120 EMB120ER 3260203 SO LEFT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 189SW 120048 LEFT ENGINE NACELLE MOST FORWARD FRAME IS CRACKED AT OUTBOARD PREVIOUS REPAIR.REMOVED AND REPLACED MOST FORWARD NACELLE FRAME, INCLUDING THE ATTACHED CHIN COWL ATTACHING FRAME SECTIONS IAW EMB120 SRM 51-40-02 AND 54-10-02. 2 L 7 2 4T RT A31SO 2001092700012 20010927 00012 SO 2001 9 27 SWIA200110189 1 20010803 A 5411 FRAME EMB 120 EMB120ER 3260203 SO RIGHT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 189SW 120048 RIGHT ENGINE NACELLE MOST FORWARD FRAME WORN AND CRACKED - INCLUDING CHIN COWL NUT PLATE FLANGES - OB, FROM TOP, EXTENDI NG DOWN TO LOWER CHIN COWL NUT PLATE FLANGE.REMOVED AND REPLACED RIGHT ENGINE NACELLE MOST FORWARD FRAME, INCLUDING CHIN COWL NUT PLATE FLANGES, AND ALL NEW NUT PLATES, IAW EMB120 SRM 51-40-02 AND 54-10-02. 2 L 7 2 4T RT A31SO 2001092700013 20010927 00013 SO 2001 9 27 SWIA200110190 1 20010803 A 5410 CLIP EMB 120 EMB120ER 3260203 SO RIGHT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 189SW 120048 RIB NR 19 RIGHT WING INNER SKIN CLIPS CRACKED AT 3 PLACES ONE LOWER, THREE UPPER.REMOVED, FABRICATED AND INSTALLED SKIN CLIPS IAW SRM 51-40-02 AND 51-70-06. 2 L 7 2 4T RT A31SO 2001092700014 20010927 00014 SO 2001 9 27 SWIA200110191 1 20010803 A 5310 WINDOW POST EMB 120 EMB120ER 3260203 SO LEFT SIDE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 189SW 120048 LEFT SIDE WINDOW POST CRACKED ON AFT SKIN ATTACH FLANGE AT BOTTOM.REMOVED AND REPLACED THE LEFT SIDE WINDOW POST IAW EMB SRM 51-00-00 AND 51-40-02. P/N: 120-03029-003, 120-03067-001 2 L 7 2 4T RT A31SO 2001092700015 20010927 00015 SO 2001 9 27 SWIA200110192 1 20010803 A 5320 STRAP EMB 120 EMB120ER 3260203 SO PILOTS WINDOW CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 189SW 120048 CONNECTING STRAP ON FRAME AFT OF PILOT'S SIDE WINDOW ON LONGITUDINAL FRAME AT PREVIOUS REPAIR IS CRACKED THROUGH AT 1ST RIVET.FABRICATED AND INSTALLED AN ALUMINUM DOUBLER FOR THE CRACKED FRAME IAW EMB SRM 51-40-02 AND 51-00-00. 2 L 7 2 4T RT A31SO 2001092700016 20010927 00016 NE 2001 9 27 SWIA200110193 2 20010920 A 7321 EEC EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE LEFT ENGINE MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 190SW 120050 LEFT EEC WENT TO MANUAL ON TAKEOFF POWER UP. ABORTED TAKEOFF.RESET LEFT EEC. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001092700017 20010927 00017 SO 2001 9 27 SWIA200110194 1 20010920 A 3350 D36604001 BATTERY EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 567SW 1142 1142 120342 MIDDLE EMERGENCY LIGHT STRIP INOP.REPLACED BATTERY. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001092700018 20010927 00018 EU 2001 9 27 QXEA0101481 1 20010828 A 2810 FASTENER FOKKER F28 F28MK4000 4990810 EU FUEL CELL DAMAGED A QXEA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 09 491US 11156 PDX - SUSPECTED FUEL LEAK FROM TWO HI-LOKS BY COLLECTOR TANK. REMOVED AND REPLACED TWO HI-LOKS AND REPAIRED IAW F28 SRM 51-30-02. 2 L 7 2 4F RT A20EU 2001092700019 20010927 00019 NM 2001 9 27 QXEA0101496 1 20010908 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - LEFT-HAND WING FRONT SPAR TO INBOARD NACELLE CONNECTION ANGLE IS CRACKED IN 2 SPOTS NEAR TOP. REPAIRED IAW DASH-8 SRM 51-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001092700020 20010927 00020 NM 2001 9 27 QXEA0101497 1 20010906 A 5510 STRUCTURE DHAV DHC8 DHC8202 2809007 NM HORIZONTAL STAB TOOL DAMAGE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - 3 TOOL MARKS IN H-STAB, RIGHT-HAND UPPER LEADING EDGE ATTACH LIP AT RBL 12. REPAIRED IAW HORIZON AIR EA 2-55-57. 2 H 7 2 4T RT A13NM 2001092700021 20010927 00021 NM 2001 9 27 QXEA0101498 1 20010904 A 5320 MOUNT DHAV DHC8 DHC8202 2809007 NM ANTENNA SPINNING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - THE AFT LEFT-HAND SIDE MOUNTING NUTPLATE FOR THE NR 1 VHF ANTENNA IS SPINNING. REPAIRED IAW DASH-8 200 SRM 51-40- 11. 2 H 7 2 4T RT A13NM 2001092700022 20010927 00022 EU 2001 9 27 QXEA0101499 1 20010909 A 3350 6008905 BATTERY FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 475AU 8081 11222 BOI - EMERGENCY EVACUATION LIGHT ON AFT WING FAIRING REMAINS ON WHEN AIRCRAFT ELECTRICAL POWER IS TURNED OFF. INSTALLED SERVICEABLE BATTERY IAW F28 MANUAL, 33-50-01. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001092700023 20010927 00023 WP 2001 9 27 0103439620 1 20010515 A 5330 SKIN DOUG DC9 DC932 3022066 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 620NW 47533 During H-check found corrosion damage on external side of fuselage skin. Corrosion is in area of a chem-milled pocket of .113" thickness. Repaired per EA. 96-183986 2 L 7 2 4F A6WE 2001092700024 20010927 00024 WP 2001 9 27 0103329957 1 20010223 A 5330 SKIN DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 915RW 47139 During an H-check found a 3" long skin crack at shear clip attach under dorsal attach front fairings. Repaired per EA. 9 9-180941 2 L 7 2 4F A6WE 2001092700025 20010927 00025 WP 2001 9 27 0103339969 1 20010730 A 5330 CHANNEL DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9333 47246 During H-check of the APB found a 1 1/8" crack in the upper inboard bend radius of the 5910130-9 channel running downwar d along the radius. Repaired per EA 99-181359 2 L 7 2 4F A6WE 2001092700026 20010927 00026 WP 2001 9 27 0103349971 1 20010531 A 5220 PAN DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9335 47337 During H-check found crack on RH aft emergency exit door lower pan. Repaired per EA. 99-181208. 2 L 7 2 4F A6WE 2001092700027 20010927 00027 WP 2001 9 27 0103359988 1 20010508 A 5330 SKIN DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8944E 47167 During H-check found a 1" crack on the fuselage skin panel. Repaired per EA. 99-181165. 2 L 7 2 4F A6WE 2001092700028 20010927 00028 WP 2001 9 27 0103369992 1 20010214 A 5312 BULKHEAD DOUG DC9 DC931 3022065 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8960E 45869 During H-check found corrosion on the horizontal flange of the floor support tee on RHS of the aft pressure bulkhead. Re paired per EA. 99-180937. 2 L 7 2 4F A6WE 2001092700029 20010927 00029 WP 2001 9 27 0103379992 1 20010216 A 5320 FLOOR SUPPORT DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8960E 45869 DURING H-CHECK FOUND CRACK IN THE RADIUS OF THE CABIN FLOOR SUPPORT. THE CRACK IS LOCATED IN THE VERTICAL WEB OF THE T- CAP, BELOW THE RADIUS. REPAIRED PER EA. 99-180963. 2 L 7 2 4F A6WE 2001092700030 20010927 00030 NM 2001 9 27 USAABB01087 1 20010825 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM ROW 4 INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 624AU 27245 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 4 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2001092700031 20010927 00031 NM 2001 9 27 USAABB01088 1 20010826 A 3350 9221009 BATTERY BOEING 757 757225 1384959 NM R4 DOOR FAULTY A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND THE EXIT IDENTIFIERS AT THE L4 AND R4 DOORS BLINKING. MAINTENANCE REPLACED THE R4 DOOR BATTERY AND RESET TH E L4 DOOR LIGHT. (M) 2 L 7 2 4F RT A2NM 2001092700032 20010927 00032 NM 2001 9 27 USAASB01240 1 20010823 A 3350 6104789 BATTERY BOEING 737 7372B7 1384560 NM PAX CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 288AU 23135 BWI - THE AFT ENTRY/SERVICE DOOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A16WE 2001092700033 20010927 00033 WP 2001 9 27 USAAD01150 1 20010816 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 828US 48028 IND - THE TAILCONE REMOTE RECEIVER FOR THE EMERGENCY LIGHTS WILL NOT TEST. MAINTENANCE REPLACED THE BATTERY PACK. OK F OR SERVICE. (M) 2 L 7 2 4F A6WE 2001092700034 20010927 00034 WP 2001 9 27 USAAD01151 1 20010817 A 3350 AD4002P BATTERY DOUG DC9 DC931 3022065 WP PAX CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 926VJ 48146 PIT - THE LEFT AND RIGHT AFT OVERWING EXIT EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED BATTERIES. OP ERATIONALLY CHECKED OK. (M) 2 L 7 2 4F A6WE 2001092700035 20010927 00035 WP 2001 9 27 USAAD01153 1 20010824 A 3350 873100191 RECEIVER DOUG DC9 DC982 3022082 WP AFT FUSELAGE FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 815US 48095 IND - THE TAILCONE EMERGENCY LIGHT RECEIVER, SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS, AND THE CEILING EMERGENCY LIGHTS F OR SEAT ROWS 1 THROUGH 8 WERE INOPERATIVE. MAINTENANCE REPLACED THE TAILCONE EMERGENCY LIGHT REMOTE RECEIVER, AND THE L OW LEVEL AND CEILING EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001092700036 20010927 00036 WP 2001 9 27 AALA20011636 1 20010807 A 5300 ATTACH ANGLE DOUG DC9 DC983 3022083 WP BS 1474 CRACKED A AALA O OTHER O OTHER IN INSP/MAINT 1 SW 21 435AA 49453 TUL - FOUND CRACK IN EXTERNAL SURFACE ATTACH ANGLE (LEFT SIDE AT CANTED STATION 1474) FUSELAGE TO VERTICAL STAB JOINER. REPAIRED PER AARD 53-10-00-2 FIG 1 PAGES 1 AND 2. (M) 2 L 7 2 4F RT A6WE 2001092700037 20010927 00037 WP 2001 9 27 AALA20011639 1 20010808 A 5300 SKIN DOUG DC9 DC983 3022083 WP FS 1383 CRACKED A AALA O OTHER O OTHER IN INSP/MAINT 1 SW 21 435AA 49453 TUL - FOUND CRACK IN SKIN AT FASTENER STATION 1383 JUST ABOVE L14R. STOP DRILLED CRACK AND INSTALLED DOUBLER AT STATION 1383 AOVER 14R IAW SRM 53-01 FIG 2. (M) 2 L 7 2 4F RT A6WE 2001092700038 20010927 00038 WP 2001 9 27 AALA20011640 1 20010809 A 5300 SKIN DOUG DC9 DC983 3022083 WP FS 1304 DENTED A AALA O OTHER O OTHER IN INSP/MAINT 1 SW 21 435AA 49453 TUL - FOUND DENT IN SKIN AT STATION 1304 LONGERON 19R. INSTALLED DOUBLER PER SRM 53-04 FIG 38 AND INSTALLED SCUFF PLATE PER AARD 53-00-8 FIG 1. (M) 2 L 7 2 4F RT A6WE 2001092700039 20010927 00039 WP 2001 9 27 AALA20011641 1 20010809 A 5300 SKIN DOUG DC9 DC983 3022083 WP BS 1474 CRACKED A AALA O OTHER O OTHER IN INSP/MAINT 1 SW 21 435AA 49453 TUL - FOUND .5 INCH CRACK ON THE RIGHT SIDE OF FUSELAGE AT STATION 1474. INSTALLED DOUBLER REPAIR PER AARP 53-30-00-02. (M) 2 L 7 2 4F RT A6WE 2001092700040 20010927 00040 WP 2001 9 27 AALA20011642 1 20010813 A 5300 FRAME DOUG DC9 DC983 3022083 WP FS 313 A AALA O OTHER O OTHER IN INSP/MAINT 1 SW 21 435AA 49453 TUL - FOUND DENT IN TOP FLANGE OF FRAME STATION 313 BETWEEN LONGERON 24L-25L. REPAIRED FRAME PER AARD 53-10-00-17. (M) 2 L 7 2 4F RT A6WE 2001092700041 20010927 00041 NM 2001 9 27 AALA20011542 1 20010728 A 3350 SOCKET BOEING 767 767223 1385123 NM INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 301AA 22307 LAX - DURING OVERNIGHT MAINTENANCE, EXTERIOR EMERGENCY LIGHT AT 1L DOOR INOPERATIVE. REPLACED BAD SOCKET BEHIND CLOSET AT 1L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001092700042 20010927 00042 NM 2001 9 27 AALA20011709 1 20010829 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 374AA 25201 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 25B INOPERATIVE. SECURED LOOSE CONNECTOR. SYSTEM GROUND CH ECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001092700043 20010927 00043 NM 2001 9 27 AALA20011558 1 20010803 A 3350 1721651 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 387AM 27184 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT SEAT 23H IS INTERMITTENT. RE-SECURED CONNECTO R AT FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001092700044 20010927 00044 NM 2001 9 27 AALA20011566 1 20010804 A 3350 P4010049 BATTERY PACK BOEING 767 767323 1385205 NM TAIL CONE INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39356 24037 ORD - DURING OVERNIGHT MAINTENANCE, TAILCONE ACCESS WALKWAY EMEREGNCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. SYSTE M GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001092700045 20010927 00045 EA 2001 9 27 MASA01044 1 20010506 A 7700 SHAFT SEAL CNDAIR CL600 CL6002B19 EA NR 2 ENGINE A MASA E ENGINE SHUTDOWN K FLUID LOSS DE DESCENT 1 SW 07 27318 7318 FLT 6151 - SBA-PHX - AFTER BEGINNING THEIR INITIAL DESCENT THE OIL PRESSURE ON THE RIGHT ENGINE DROPPED TO 23 PSI. AFTE R SECURING THE NR 2 ENGINE, THE PLANE LANDED UNEVENTFULLY. MAINTENANCE FOUND A OIL SHAFT SEAL WHICH WAS INSTALLED TO CO MPLY WITH A PREVIOUS MEL HAD BECOME DISLOGGED. MAINTENANCE REPLACED THE HYD PUMP SIGNING OFF THE MEL. (M) 2 L 7 2 4F RT A21EA 2001092700046 20010927 00046 EU 2001 9 27 FJT01018751 1 20010130 A 7700 KPT06P84S CONNECTOR BAG JETSTM JETSTM3201 1500217 EU ENG COMPT A FJTA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 03 875JX 875 TBN - FLT 7842 - AIRCRAFT WAS EN-ROUTE FROM TBN TO STL, WHEN THE RIGHT ENGINE STARTED TO HAVE TORQUE AND TEMP FLUCTUATIO NS. NORMAL PROCEDURES WERE FOLLOWED AND THE ENGINE WAS SHUTDOWN. THE AIRCRAFT LANDED SAFELY AT STL WITHOUT FURTHER INC IDENTS. ENGINE GROUND RUNS CONFIRMED THE FLUCTUATING TORQUE AND TEMP. THE TTL COMPUTER WAS TURNED OFF AND THE ENGINE T HEN MAINTAINED A CONSTANT TORQUE AND TEMP. THE AIRCRAFT WAS FERRIED FROM STL TO MQY WITH THE TTL OFF FOR REPAIR. ON AR RIVAL AT MQY, SEVERAL ENGINE RUN WERE PERFORMED WAS UNABLE TO DUPLICATE THE FLUCTUATIONS WITH OR WITHOUT THE TTL COMPUTE R ON LINE. FURTHER INSPECTION REVEALED THAT THE CANNON PLUG TO THE TTL VALVE DID NOT HAVE A BACKSHELL INSTALLED THIS EX 2 L 7 2 4T RT A56EU 2001092700047 20010927 00047 WP 2001 9 27 MWEA011298 1 20010925 A 5310 591235040 GUSSET DOUG DC9 DC981 3022081 WP COCKPIT WINDOW CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 FO'S CLEARVIEW WINDOW SILL LOWER AFT CORNER HAS A CORRODED GUSSET. -- BLENDED AREA UNDER GUSSET FOR CORROSION. 2 L 7 2 4F A6WE 2001092700048 20010927 00048 WP 2001 9 27 MWEA011300 1 20010925 A 5310 9911840165 SHEAR TIE DOUG DC9 DC981 3022081 WP STATION 1437 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 SHEAR TIE CRACKED, STATION 1437, LONGERON 3 LEFT. -- REMOVED AND REPLACED SHEAR TIE. 2 L 7 2 4F A6WE 2001092700049 20010927 00049 WP 2001 9 27 MWEA011301 1 20010925 A 5310 9911840166 SHEAR TIE DOUG DC9 DC981 3022081 WP STATION 1437 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 SHEAR TIE CRACKED, STATION 1437, LONGERON 3 RIGHT. -- REMOVED AND REPLACED SHEAR TIE. 2 L 7 2 4F A6WE 2001092700050 20010927 00050 NM 2001 9 27 QXEA0101500 1 20010910 A 3350 82520977001 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 363PH 520 PDX - FORWARD EMERGENCY ESCAPE PATH TRACK DAMAGED. REMOVED AND REPLACED FORWARD EMERGENCY ESCAPE PATH TRACK IAW TASK 33 -51-11-000-801 AND 33-51-11-400-801. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001092700051 20010927 00051 EU 2001 9 27 QXEA0101501 1 20010911 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 480AU 11229 GEG - EMERGENCY EXIT SIGN AT ROW 9 INOPERABLE. REPLACED SIGN. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE . 2 L 7 2 4F RT A20EU 2001092700052 20010927 00052 EU 2001 9 27 QXEA0101502 1 20010911 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US 11161 SEA - EXIT SIGN ABOVE COCKPIT DOOR HAS SEVERAL LIGHTS INOPERABLE. REMOVED AND REPLACED SIGN ABOVE COCKPIT DOOR. OPERAT IONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001092700053 20010927 00053 EU 2001 9 27 MALA010707 1 20010911 A 2730 7227705644 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438XJ 340B438 DURING 4K-CHECK IN CWA, RT I/B FWD ELEVATOR FUSELAGE CABLE IS CHAFED. MX REPLACED RT I/B FWD FUSELAGE CABLE IAW SF340 A MM 27-31-15-4. P/N 7227705-644. 2 L 7 2 4T RT A52EU 2001092700054 20010927 00054 NM 2001 9 27 QXEA0101503 1 20010901 A 5330 PANEL DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX- TOOL MARK WITH SURFACE CORROSION ON AFT SPAR AS VIEWED THROUGH PANEL 521AT. REPAIRED IAW DHC-8 SRM 51-20-16 AND 51 -20-36. 2 H 7 2 4T RT A13NM 2001092700055 20010927 00055 EU 2001 9 27 MALA010708 1 20010911 A 2710 7227105624 CONTROL CABLE SAAB SF340 340B 7860101 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438XJ 340B438 DURING 4-K CHECK IN CWA, RT O/B FWD AILERON FUSELAGE CABLE IS CHAFED. MX REPLACED RT O/B FWD FUSELAGE AILERON CABLE P/N 7227105-624. 2 L 7 2 4T RT A52EU 2001092700056 20010927 00056 EU 2001 9 27 MALA010709 1 20010911 A 2710 7227105614 CONTROL CABLE SAAB SF340 340B 7860101 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438XJ 340B438 DURING 4K-CHECK IN CWA, RT I/B AILERON FUSELAGE CABLE IS CHAFED. MX REPLACED RT I/B AILERON FWD FUSELAGE CABLE WITH NEW CABLE P/N 7227105-614 IAW SF340 AMM 27-11-25-4. 2 L 7 2 4T RT A52EU 2001092700057 20010927 00057 WP 2001 9 27 0103399992 1 20010213 A 5712 RIB DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8960E 45869 During H-check found LH wing leading edge ribs cracked. Repaired per EA. 99-180959. 2 L 7 2 4F A6WE 2001092700058 20010927 00058 WP 2001 9 27 0103389992 1 20010213 A 5712 RIB DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8960E 45869 During H-check found LH wing leading edge ribs cracked. Repaired per EA. 99-180959. 2 L 7 2 4F A6WE 2001092700059 20010927 00059 WP 2001 9 27 0103409604 1 20010418 A 5312 BULKHEAD DOUG DC9 DC932 3022066 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 604NW 47222 During H-check found extensive corrosion on the aft pressure bulkhead web, doubler, and tripler. Repaired per EA. 99-172 626. 2 L 7 2 4F A6WE 2001092700060 20010927 00060 NM 2001 9 27 P5CA0100593 1 20010922 A 2700 BSBO85003 LINK BOEING 747 747123 1384873 NM BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 R.H. O/B FORE FLAP, MOST O/B SUPPORT LINK BROKEN. REMOVED & REPLACED LINK ASSY. OPS CHECK O.K. 2 L 7 4 4F A20WE 2001092700063 20010927 00063 NM 2001 9 27 01FDEA00856 1 20010924 A 3620 COMPUTER DOUG MD11 MD11F 3023600 NM BLEED AIR SYS FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 602FE 48402 ON CLIMBOUT LEVEL 3 EMERGENCY ALERT AIR MANIFOLD NR 2 FAIL. REMOVED AND REPLACED MFC & ALL SENSORS IN ZONE 15. 2 L 7 3 4F RT A22WE 2001092700064 20010927 00064 NM 2001 9 27 01FDEA00858 1 20010926 A 3350 BATTERY BOEING 727 72722 1384002 NM CABIN DISCHARGED A FDEA K NONE L NO TEST IN INSP/MAINT 1 SO 25 150FE 19141 FWD ENTRY DOOR ESCAPE SLIDE LIGHT INOP. REMOVED AND REPLACED LIGHT BATTERY ASSY PER MM 33-50-121-2. 2 L 7 3 4F A3WE 2001102400082 20011024 00082 NM 2001 10 24 DHL2001720012 1 20010925 A 2750 FLAP BOEING 727 727228 1384083 NM WING MALFUNCTIONED A DHLA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 720DH 19544 ON TAXI OUT ELP, INBOARD FLAPS WOULD NOT EXTEND TO THE SELECTED POSITION OF 15 DEGREES. MX ADVISED TO RESET INBOARD T/E FLAP POSITION CB. RESET INDICATOR WENT FROM 0 DEGREES TO 20 DEGREES. TAXI BACK TO GATE. WENT TO APU AND FLAPS THEN I NDICATED 15 DEGREES. T/S FLAP POSITION INDICATION SYSTEM FOR I/B TRAILING AFT FLAPS. FOUND TERMINALS ON FLAP C/B REPLA CED I/B FLAP C/B FOUND PIN B2 RECESSED ON R 187 RELAY REPOSITIONED PIN B2. REPLACED R187 RELAY SWAPPED BUS PROTECT ION PANEL, NO HELP. REINSTALLED ORIGINAL BUS PROT PANEL. REMOVED AND REPLACED I/B FLAP BY-PASS VALVE IAW B727 MM 27-51-151 . REMOVED CONNECTOR SHELLS ON I/B FLAP INDICATOR, LEFT AND RIGHT FLAP POSITION XMITTER, I/B FLAP BYPASS VALVE. 2 L 7 3 4F RT A3WE 2001092700065 20010927 00065 2001 9 27 DHL2001721008 4 20010925 A 2212 AUTOPILOT SYS BOEING 727 727228 NM COCKPIT MALFUNCTIONED A DHLA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 01 721DH 19545 EACH TIME ALTITUDE HOLD IS DISENGAGED, A/C ABRUPTLY PITCHES UP AND CLIMB AT 500-100 FPM, STAB OUT OF TRIM LIGHT IS NOT I LLUMINATED. COULD NOT DUPLICATE ON GROUND. AUTO PILOT ALTITUDE HOLD CHECKS GOOD IAW B727 M/M 22-11-01. NO HISTORY. 2 L 7 3 4F A3WE 2001092700066 20010927 00066 WP 2001 9 27 DHL2001807024 1 20010925 A 2510 LOCKPIN DOUG DC8 DC873F 302199F WP COCKPIT LACK OF LUBE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 CAPTS SEAT FORE AND AFT TRACKING DOES NOT LOCK SECURELY. LUBED CAPTAINS SEAT FORE AND AFT LOCK PINS OPS CHECKS GOOD IAW MM 25-11-1. 2 L 7 4 4F RT 4A25 2001092700067 20010927 00067 NM 2001 9 27 QXEA0101504 1 20010906 A 3211 FITTING DHAV DHC8 DHC8202 2809007 NM MLG ACTUATOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX- LEFT HAND MAIN LANDING GEAR RETRACTION ACTUATOR FITTING MOUNTING AREA ON H-MEMBER HAS FRETTING CORROSION AROUND TOP MOUNTING HOLE AND BOTTOM OUTBOARD MOUNTING HOLE. REPAIRED IAW DHC-8 RD 8-54-1178. 2 H 7 2 4T RT A13NM 2001092700068 20010927 00068 NM 2001 9 27 QXEA0101505 1 20010906 A 5310 STRUCTURE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX- CORROSION 4.5 INCHES BEHIND FRAME 445.500 INBOARD OF STRINGER 31 RT. REPAIRED IAW DHC-8 SRM 53-00-16 PAGE 13, 53-1 0-11 PAGES 3 AND 5, 51-20-16 PAGE 4 AND 51-20-36 PAGE 7. 2 H 7 2 4T RT A13NM 2001092700069 20010927 00069 NM 2001 9 27 QXEA0101506 1 20010903 A 5711 SPAR CAP DHAV DHC8 DHC8202 2809007 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX- FRETTING CORROSION AT 15 FASTENER HOLES LOWER SPAR CAP BELOW LEADING EDGE 611AR. REPAIRED IAW DHC-8 RD 8-57-811, 8 -57-1150 AND DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001092700070 20010927 00070 NM 2001 9 27 QXEA0101507 1 20010905 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX- LEFT HAND WING FRONT SPAR FLANGE FROM YW57 TO YW72 IS CHAFED. REPAIRED IAW DHC-8 RD 8-57-811 AND 8-57-1150. 2 H 7 2 4T RT A13NM 2001092700071 20010927 00071 NM 2001 9 27 QXEA0101508 1 20010905 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX- LEFT HAND WING FRONT SPAR BOTTOM FLANGE YW135 TO YW139 IS CHAFED. REPAIRED IAW DHC-8 RD 8-57-1150 AND DHC-8 SRM 51 -20-26. 2 H 7 2 4T RT A13NM 2001092700072 20010927 00072 NM 2001 9 27 QXEA0101509 1 20010906 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX- CRACK .65 INCHES LONG IN FRAME 4 WHERE IT ATTACHES TO STRINGER 4R IN TAIL SECTION FORWARD OF VERTICAL STAB FORWARD SPAR AT STATION X712 AND Z174. REPAIRED IAW DHC-8 RD 8-55-199 AND DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001092700073 20010927 00073 EU 2001 9 27 MALA010710 1 20010911 A 2720 7227105582 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438XJ 340B438 DURING 4K-CHECK IN CWA, RT RUDDER AFT SINGLE CABLE OF CIRCUIT I IS CHAFED. MX REPLACED RT RUDDER SINGLE CABLE P/N 72271 05-582 OF CIRCUIT I IAW SF340 AMM 27-21-25-4. 2 L 7 2 4T RT A52EU 2001092700074 20010927 00074 EU 2001 9 27 MALA010711 1 20010911 A 2720 7227105562 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438XJ 340B438 DURING 4K-CHECK IN CWA, RT O/B RUDDER CABLE OF DUAL CIRCUIT I IS CHAFED. MX REPLACED RT O/B RUDDER CABLE P/N 7227105-56 2 OF DUAL CIRCUIT I IAW SF340 AMM 27-21-25-4. 2 L 7 2 4T RT A52EU 2001092700075 20010927 00075 EU 2001 9 27 MALA010712 1 20010911 A 2720 7227105571 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438XJ 340B438 DURING 4K-CHECK IN CWA, RT I/B RUDDER CABLE OF DUAL CIRCUIT I IS CHAFED. MX REPLACED RT I/B RUDDER CABLE P/N 7227105-57 1 IAW SF340 AMM 27-21-25-4. 2 L 7 2 4T RT A52EU 2001092700076 20010927 00076 EU 2001 9 27 MALA010713 1 20010911 A 2720 7227105582 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438XJ 340B438 DURING 4K-CHECK IN CWA, LT RUDDER AFT SINGLE CABLE OF DUAL CIRCUIT I IS CHAFFED. MX REPLACED LT RUDDER AFT SINGLE CABLE CIRCUIT I P/N 7227105-582 IAW SF340 AMM 27-21-25-4. 2 L 7 2 4T RT A52EU 2001092700077 20010927 00077 EU 2001 9 27 MALA010714 1 20010911 A 2720 7227105562 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438XJ 340B438 DURING 4K-CHECK IN CWA, LT O/B RUDDER CABLE OF DUAL CIRCUIT I IS CHAFED. MX REPLACED LT O/B RUDDER CABLE P/N 7227105-56 2 OF DUAL CIRCUIT I IAW SF340 AMM 27-21-25-4. 2 L 7 2 4T RT A52EU 2001092700078 20010927 00078 EU 2001 9 27 MALA010715 1 20010911 A 2710 7227105623 CONTROL CABLE SAAB SF340 340B 7860101 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438XJ 340B438 DURING 4K-CHECK IN CWA, LT I/B FWD AILERON FUSELAGE CABLE IS CHAFED. MX REMOVED AND REPLACED LT I/B AILERON CABLE, P/N 7227105-623 IAW SF 340 AMM 27-11-15-4. 2 L 7 2 4T RT A52EU 2001092700079 20010927 00079 EU 2001 9 27 MALA010716 1 20010911 A 2710 7227105623 CONTROL CABLE SAAB SF340 340B 7860101 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438XJ 340B438 DURING 4K-CHECK IN CWA, LT O/B AILERON FWD FUSELAGE CABLE CHAFED. MX REPLACED LT O/B AILERON FUSELAGE CABLE P/N 7227105 -623 IAW SF340 AMM 27-11-25-4. 2 L 7 2 4T RT A52EU 2001092700080 20010927 00080 EU 2001 9 27 MALA010717 1 20010911 A 2730 7227705644 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438XJ 340B438 DURING 4K-CHECK IN CWA, LT I/B ELEVATOR FWD FUSELAGE CABLE IS CHAFED. MX REPLACED LT I/B FWD ELEVATOR CABLE P/N 7227705 -644 IAW SF340 AMM 27-31-15. 2 L 7 2 4T RT A52EU 2001092700081 20010927 00081 EU 2001 9 27 MALA010718 1 20010911 A 2730 7227105712 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438XJ 340B438 DURING 4K-CHECK IN CWA, LT O/B ELEVATOR FWD FUSELAGE CABLE IS CHAFED. MX REPLACED LT O/B ELEVATOR FWD FUSELAGE CABLE P/ N 7227105-712. 2 L 7 2 4T RT A52EU 2001092700082 20010927 00082 NE 2001 9 27 MALA010722 2 20010907 A 7261 LF07643 ENGINE BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 3 ENGINE LACK OF LUBE A MALA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 GL 15 522XJ E2347 DURING DESCENT ON FLIGHT 3611, RECEIVED A OIL NR 3 LO PRESS LIGHT AT 7000 FT AND 250 KTS ON DESCENT INTO MSP. OIL PRESS URE WAS FLUCTUATING BETWEEN 20 AND 40 PSI AND OIL QUANTITY READ ZERO. ENGINE WAS SHUTDOWN PER QRH. N1 INDICATED ABOUT 15 PERCENT AFTER SHUTDOWN. ENGINE WINDMILLED ABOUT 10 MINUTES BEFORE LANDING. MAINTENANCE REPLACED THE ENGINE ASSEMBLY P/N LF07643, S/N OFF LF07643, S/N ON P07688. CHECKED AND ADDED 6.25 QTS OF OIL TO NR 3 ENGINE. 2 H 7 4 4F 4 F RT A49EU E6NE 2001092700083 20010927 00083 2001 9 27 MALA010724 4 20010903 A 2210 AUTOPILOT SYS BAC 146 AVRO146RJ85A 1500097 EU COCKPIT MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 511XJ E2325 CLIMBING OUT OF DTW ON FLIGHT 3481, ABOVE 10,000 FT SPEED 280 KNOTS, AUTOPILOT ENGAGED, WHEN AP DISCONNECTED AND THE YD ADVISORY LIGHT ILLUMINATED. AFTER A FEW MINUTES IN FGC ADVISORY LIGHT ILLUMINATED, ALSO ALONG WITH THE WINDSHEAR INOP L IGHT. AP WOULD NOT RE-ENGAGE, LOST THE FLIGHT DIRECTORS. MAINTENANCE CLEARED FAULTS, AND LOGGED IN FGC. PERFORMED, RT S ON DFGS AND CHECKS GOOD. 2 H 7 4 4F RT A49EU 2001092700084 20010927 00084 EU 2001 9 27 MALA010725 1 20010902 A 2150 11341041 MOTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE CABIN FAILED A MALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 15 418XJ 340B418 DURING WALK-AROUND AFTER FLIGHT 2742, NOTICED SUPPLEMENTAL AIR CONDITIONING INOP. NOTICED UNUSUAL SMELL FROM SUPP A/C V ENT. MAINTENANCE DEFERRING SUPP A/C IAW 1-16-125-60-5-12 AFT AIR CONDITIONING, AUX HEAT BLOWN CONTROL CIRCUIT BREAKERS PULLED AND COLLARED. MAINTENANCE REPLACED COMPRESSOR MOTOR P/N 1134104-1, S/N ON 762 IAW AMM, ALL CHECK GOOD. REMOVED FROM DMR, MXC NOTIFIED. 2 L 7 2 4T 4 T RT A52EU E8NE 2001092700085 20010927 00085 2001 9 27 MALAL010680 4 20010908 A 3460 4068300904 COMPUTER BAC 146 AVRO146RJ85A 1500097 EU E/E BAY FAULTY A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 527XJ E2352 DURING ROTATION RECEIVED FTC, EL TRIM WITH LOUD BUZZING NOISE OVER OVERHEAD SPEAKER, WINDSHR AMBER AND RED FLASHED ON AN D OFF, YD ALSO FAILED AND ASSOCIATED YD WHITE LIGHT. FGC 1 WHITE ILLUMINATED, TRP FAILED, FD FAILED, CONTINUOUSLY REC'D WDSHR WARNING LIGHT LOST ALT SEL FUNCTION ON MCP ON GND HEARD BEEPING AND CLICKING NOISE FROM AUTO THROTTLE CONTROL SER VO. MAINTENANCE VERIFIED FGC FAULTS INDICATE FGC IS THE PROBLEM, REPLACED FGC P/N 4068300-904, S/N ON 96120264, S/N OFF 99090362, TEST GOOD IAW AVRO MM CHAPTER 22 AND 34. 2 H 7 4 4F RT A49EU 2001092700086 20010927 00086 EU 2001 9 27 QXEA0101512 1 20010913 A 3350 6008905 POWER SUPPLY FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 2668 11156 PDX - NUMBER 5 CABIN BATTERY PACK IS WEAK. REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECK IS GOOD. AIRCRAFT RET URNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001092700087 20010927 00087 EU 2001 9 27 QXEA0101513 1 20010913 A 3350 6008905 POWER SUPPLY FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 2668 11156 PDX - NUMBER 6 CABIN BATTERY PACK IS WEAK. REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECK IS GOOD. AIRCRAFT RET URNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001092700088 20010927 00088 NM 2001 9 27 QXEA0101515 1 20010914 A 3350 8252097701 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 SEA - FORWARD RED PROXIMITY EMERGENCY ESCAPE PATH LIGHTS DO NOT ILLUMINATE. REPLACED SECTION OF FLOOR TRACK LIGHTING. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001092700089 20010927 00089 WP 2001 9 27 MWEA011244 1 20010905 A 5730 9937581501 DOUBLER DOUG DC9 DC932 3022066 WP RT WING CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 RIGHT WING FUELING PANEL MIDDLE LATCHES CHAFING INTO LEFT STRAP. FABRICATED AND INSTALLED DOUBLERS, FILLERS, AND SHIMS. 2 L 7 2 4F A6WE 2001092700090 20010927 00090 NM 2001 9 27 QXEA0101516 1 20010905 A 5230 SKIN DHAV DHC8 DHC8* NM CARGO DOOR NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - TWO SMALL NICKS IN FUSELAGE ON THE LEFT SIDE OF AFT BAGGAGE DOOR ABOVE THE N-NUMBER. COMPLIED WITH EA 6-53-24. 2 H 7 2 4T RT A13NM 2001092700091 20010927 00091 EU 2001 9 27 QXEA0101517 1 20010919 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - EMERGENCY EXIT SIGN ABOVE THE COCKPIT DOOR IN GALLEY AREA HAS MULTIPLE LAMPS BUNED OUT. REPLACED CURCUIT BOARD IN EMERGENCY EXIT SIGN. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001092700092 20010927 00092 NM 2001 9 27 QXEA0101518 1 20010919 A 5330 SKIN DHAV DHC8 DHC8* NM FUSELAGE DAMAGED A QXEA O OTHER O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 GEG - AIRCRAFT ROTATED TO 6 DEGREES PITCH UP WHILE IN GATE. WHEN AIRCRAFT SETTLED, FOUND ELECTROCART HAD PASSED UNDER A IRCRAFT FROM FRONT TO BACK WITH FUSELAGE AND ANTENNAE DAMAGE. AIRCRAFT DOWN FOR REPAIRS. 2 H 7 2 4T RT A13NM 2001092700093 20010927 00093 NM 2001 9 27 MWEA011246 1 20010905 A 2130 CONTROL VALVE DOUG MD88 MD88 3023688 NM CABIN PRESSURE OBSTRUCTED A MWEA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 701ME 49760 LOST NR 1 AND 2 PRESSURIZATION CONTROLLER. WENT TO MANUAL, CABIN CLIMBED TO 1,500 FEET CABIN ALTITUDE. THEN MANUAL OUT FLOW FULL CLOSED. CABIN QUICKLY BEGAN TO PRESSURIZE TO BELOW CABIN ALTITUDE. FOUND BOTH A/C MOTOR FAULT LIGHT ILLUMINA TED ON BOTH CONTROLLERS. NOTED INSULATION CLIP INTERFERING WITH CONTROL VALVE MOVEMENT. REPOSITIONED CLIP AND INSULATI ON. 2 L 7 2 4F RT A6WE 2001092700094 20010927 00094 NM 2001 9 27 QXEA0101519 1 20010918 A 5753 STRUCTURE DHAV DHC8 DHC8* NM TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 PDX - RIGHT INBOARD FLAP IS CHAFED ON UPPER SURFACE WHERE IT MEETS WING SHROUD. SHIMMED RIGHT FLAP IAW EA 6-57-05, PRIME D AND PAINTED. 2 H 7 2 4T RT A13NM 2001092700095 20010927 00095 NM 2001 9 27 MWEA011247 1 20010905 A 2133 5653731503 OUTFLOW VALVE DOUG MD88 MD88 3023688 NM CABIN PRESSURE FAILED A MWEA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 701ME 49760 LOST BOTH NR 1 AND 2 AUTO PRESSURIZATION CONTROLLERS AT 8,000 FEET. WITH THE CABIN OUTFLOW VALVE FULLY CLOSED CABIN CLI MBED AT 400 FEET. UNABLE TO CONTROL IN MANUAL. REMOVED AND REPLACED OUTFLOW VALVE ASSEMBLY. 2 L 7 2 4F RT A6WE 2001092700096 20010927 00096 NM 2001 9 27 QXEA0101520 1 20010918 A 5753 STRUCTURE DHAV DHC8 DHC8* NM TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 PDX - LEFT INBOARD FLAP IS CHAFED ON UPPER SURFACE WHERE IT MEETS WING SHROUD. SHIMMED LEFT INBOARD FLAP SHROUD IAW EA 6 -57-05. PRIMED AND PAINTED CHAFFED AREA. 2 H 7 2 4T RT A13NM 2001092700097 20010927 00097 EU 2001 9 27 QXEA0101521 1 20010922 A 3350 83320 LIGHT FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 BOI - EMERGENCY EXIT LIGHT PANEL ABOVE ROW 8 IS INOPERABLE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PANEL. OPERATIONAL CHECK IS GOOD AND AIRCRAFT RETURNED FOR SERVICE. 2 L 7 2 4F RT A20EU 2001092700098 20010927 00098 EU 2001 9 27 QXEA0101522 1 20010921 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 SEA - COCKPIT DOORWAY EMERGENCY EXIT SIGN HAS INOPERABLE BULBS. REMOVED AND REPLACED CIRCUIT BOARD. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001092700099 20010927 00099 NM 2001 9 27 QXEA0101523 1 20010915 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - AIRCRAFT SKIN SURFACE, ADJACENT TO LOWER TCAS ANTENNA HAS CORROSION AT ANTENNA ATTACH HOLE AREA. REPAIRED IAW DHC- 8 SRM 53-00-16, PAGE 3. 2 H 7 2 4T RT A13NM 2001092700100 20010927 00100 NE 2001 9 27 MWEA011248 2 20010906 A 7200 JT8D9A ENGINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE RIGHT OVERTEMP A MWEA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 GL 31 204ME 47680 665555 ON TAKEOFF IN OMA AT A REDUCED POWER TAKEOFF OF 1.94 EPR THE RIGHT ENGINE EGT ROSE TO 600 DEGREES FOR 5 SECONDS BEFORE P OWER COULD BE REDUCED. AIRCRAFT TO REMAIN IN MKE FOR REPAIR. REMOVED AND REPLACED ENGINE. 2 L 7 2 4F 4 F A6WE E2EA 2001092700101 20010927 00101 NM 2001 9 27 QXEA0101524 1 20010917 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - SEAT TRACK NR 12 AT STATION 539 HAS CHAFING INSIDE SEAT TRACK. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2001092700102 20010927 00102 NM 2001 9 27 QXEA0101525 1 20010919 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - LEFT-HAND OUTBOARD SEAT TRACK IS GOUGED AT STATION 490.00. REPAIRED IAW DHC-8-200 SRM 51-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001092700103 20010927 00103 WP 2001 9 27 MWEA011249 1 20010908 A 2720 CONTROL VALVE DOUG DC9 DC932 3022066 WP RUDDER OUT OF ADJ A MWEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 31 501ME 47132 ON TAXI OUT, FLAP/RUDDER STOP INOP LIGHT ILLUMINATED, RETURNED TO GATE. SHIMMED AUX RUDDER THROW LIMITER CONTROL VALVE PER MM 27-20-0. OPERATIONS CHECK GOOD. 2 L 7 2 4F A6WE 2001092700104 20010927 00104 2001 9 27 MWEA011250 4 20010909 A 3160 4055900906 SYMBOL GENERATOR DOUG DC9 DC981 3022081 WP E/E BAY FAULTY A MWEA A UNSCHED LANDING I FLT. ATTITUDE INST. CL CLIMB 1 GL 31 812ME 48006 FIRST OFFICER SIDE EFIS TUBES WENT BLANK ON CLIMBOUT. NR 2 SYMBOL GENERATOR WENT OFF AND ON FOR ENTIRE FLIGHT. REMOVED AND REPLACED NR 2 SYMBOL GENERATOR. 2 L 7 2 4F A6WE 2001092700105 20010927 00105 NM 2001 9 27 QXEA0101526 1 20010917 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - RIGHT-HAND INBOARD SEAT TRACK HAS LIGHT CORROSION AT STATION 291.400. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-2 0-36. 2 H 7 2 4T RT A13NM 2001092700106 20010927 00106 NM 2001 9 27 QXEA0101527 1 20010917 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - RIGHT-HAND INBOARD SEAT TRACK HAS LIGHT GOUGES IN CENTER AT STATION 312.350. REPAIRED IAW DHC-8 SRM 51-20-16 AND S RM 51-20-36. 2 H 7 2 4T RT A13NM 2001092700107 20010927 00107 NM 2001 9 27 QXEA0101528 1 20010917 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - RIGHT-HAND INBOARD SEAT TRACK HAS LIGHT GOUGES IN CENTER AT STATION 354.250. REPAIRED IAW DHC-8 SRM 51-20-16 AND S RM 51-20-36. 2 H 7 2 4T RT A13NM 2001092700108 20010927 00108 NM 2001 9 27 QXEA0101529 1 20010917 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - RIGHT-HAND INBOARD SEAT TRACK HAS LIGHT GOUGES IN CENTER AT STATION 377.850. REPAIRED IAW DHC-8 SRM 51-20-16 AND S RM 51-20-36. 2 H 7 2 4T RT A13NM 2001092700109 20010927 00109 WP 2001 9 27 MWEA011252 1 20010910 A 5350 591335505 WARNING SYSTEM DOUG DC9 DC981 3022081 WP TAILCONE MALFUNCTIONED A MWEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 31 806ME 48032 THE TAIL CONE WARNING LIGHT ILLUMINATED. EXECUTED A LOW SPEED ABORT. NR 3 AND 4 BRAKES WERE SMOKING AFTER RTO. BRAKE TEMPS NEVER EXCEED 400 DEGREES AND OVERHEAT LIGHT NEVER CAME ON. DEFERRED TAIL CONE ANNUNCIATOR SYSTEM PER MEL 53-1B T- FUNCTION C/W. REINSTALLED LOCKING CABLE INTO AFT TAIL CONE DEPLOYMENT HANDLE BRACKET AND SWITCH ASSEMBLY PER MM 53-53-0 0. OPS CHECK GOOD. PERFORMED LIGHT ENERGY STOP INSPECTION PER MM 5-57-00. NO ABNORMALITIES NOTED. 2 L 7 2 4F A6WE 2001092700110 20010927 00110 NM 2001 9 27 QXEA0101530 1 20010917 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - RIGHT-HAND INBOARD SEAT TRACK APPROXIMATELY STATION 420.00 HAD LIGHT GOUGES IN CENTER. REPAIRED IAW DHC-8 SRM 51-2 0-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2001092700111 20010927 00111 WP 2001 9 27 MWEA011254 1 20010914 A 5230 59101575 SKIN DOUG DC9 DC932 3022066 WP CARGO DOOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 AFT CARGO DOOR BOTTOM INNER SKIN CORRODED UNDER STOP FITTING. FABRICATED AND INSTALLED DOUBLER AND FILLER. 2 L 7 2 4F A6WE 2001092700112 20010927 00112 WP 2001 9 27 MWEA011255 1 20010914 A 5240 591008417 WEB DOUG DC9 DC932 3022066 WP SERVICE DOOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 FORWARD SERVICE DOOR, LIGHT CORROSION AND MISDRILLED HOLE ON LOWER WEB OF DOORS. FABRICATED AND INSTALLED REPAIR DOUBLE R. 2 L 7 2 4F A6WE 2001092700113 20010927 00113 NM 2001 9 27 QXEA0101531 1 20010917 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - RIGHT-HAND INBOARD SEAT TRACK AT APPROXIMATELY STATION 445.500 HAS LIGHT GOUGES IN CENTER. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2001092700114 20010927 00114 NM 2001 9 27 QXEA0101532 1 20010917 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - RIGHT-HAND INBOARD SEAT TRACK AT APPROXIMATELY STATION 488.500 HAS LIGHT GOUGES IN CENTER. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2001092700115 20010927 00115 NM 2001 9 27 QXEA0101533 1 20010917 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - RIGHT-HAND INBOARD SEAT TRACK AT APPROXIMATELY STATION 510.000 HAS LIGHT GOUGES IN CENTER. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2001092700116 20010927 00116 NM 2001 9 27 QXEA0101534 1 20010917 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - RIGHT-HAND INBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION BETWEEN STATION 262.00 AND 182.00. REPAIRED IAW DHC-8 SR M 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2001092700117 20010927 00117 NM 2001 9 27 CALA0100900 1 20010925 A 5313 STRINGER BOEING 737 7373T0 1384582 NM STA 500C-500D CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 INSPECTION FOUND A 1/2" CRACK IN STRINGER 16L BETWEEN STA 500C AND 500D. REPAIRED IAW SRM 53-00-03, FIGURE 201, SHEET 6. 2 L 7 2 4F RT A16WE 2001092700118 20010927 00118 WP 2001 9 27 MWEA011257 1 20010915 A 5313 4912583501 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 BARE METAL AND LIGHT CORROSION, LONGERON 29 LEFT, STATION 218 TO 237. REMOVED AND REPLACED LONGERON AND SPLICE. 2 L 7 2 4F A6WE 2001092700119 20010927 00119 NM 2001 9 27 QXEA0101537 1 20010920 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM TE FLAPS CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - RIGHT-HAND FLAP TRACK NR 4 HAS PITTING ON OTH SIDE OF TRACK. REPAIRED IAW RD 8-57-988 AND HORIZON AIR EA 2-57-138. 2 H 7 2 4T RT A13NM 2001092700120 20010927 00120 WP 2001 9 27 MWEA011258 1 20010915 A 5310 59129951 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 LEFT AFT EMERGENCY EXIT DOOR JAMB AT THE UPPER LATCH IS GOUGED. REMOVED AND REPLACED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001092700121 20010927 00121 NM 2001 9 27 QXEA0101538 1 20010920 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM TE FLAPS CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - RIGHT-HAND NR 5 FLAP INBOARD SIDE OF TRACK HAS PITTING. REPAIRED IAW RD 8-57-989 AND HORIZON AIR EA 2-57-136. 2 H 7 2 4T RT A13NM 2001092700122 20010927 00122 WP 2001 9 27 MWEA011259 1 20010915 A 5313 591140141 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 E&E COMPARTMENT, LONGERON 30 HAS AREAS OF LIGHT CORROSION AND BARE METAL BETWEEN STATION 160 & 180. REMOVED AND REPLACE D LONGERON. 2 L 7 2 4F A6WE 2001092700123 20010927 00123 NM 2001 9 27 QXEA0101539 1 20010920 A 5753 BEAM DHAV DHC8 DHC8202 2809007 NM TE FLAPS CHIPPED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - LEFT-HAND NR 4 FLAP BEAM FAIL SAFE HOOK UPPER SURFACE METALIC PLATING CHIPPED IN THREE SMALL SPOTS WITHIN AN AREA OF .25 X 1.25. REPAIRED IAW HORIZON AIR EA 2-57-137. 2 H 7 2 4T RT A13NM 2001092700124 20010927 00124 NM 2001 9 27 QXEA0101540 1 20010920 A 5753 BEAM DHAV DHC8 DHC8202 2809007 NM TE FLAPS DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - LEFT-HAND WING NR 4 FLAP BEAM OUTBOARD SURFACE "E" HAS PITS IN METALIC PLATING ALONG ENTIRE ROLLER WEAR MARK. REPA IRED IAW HORIZON AIR EA 2-57-137. 2 H 7 2 4T RT A13NM 2001092700125 20010927 00125 NM 2001 9 27 QXEA0101541 1 20010920 A 5753 BEAM DHAV DHC8 DHC8202 2809007 NM TE FLAPS CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - LEFT-HAND WING NR 4 FLAP BEAM INBOARD SURFACE "E" HAS A PIT THROUGH METALIC PLATING, .070 IN DIAMETER. REPAIRED IA W HORIZON AIR EA 2-57-137. 2 H 7 2 4T RT A13NM 2001092700126 20010927 00126 WP 2001 9 27 MWEA011260 1 20010915 A 5320 5911401105N SPLICE DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 E&E COMPARTMENT, LONGERON 29 LEFT HAS AREAS OF LIGHT CORROSION BETWEEN STATION 160 AND 170. REMOVED AND REPLACED SPLICE . 2 L 7 2 4F A6WE 2001092700127 20010927 00127 NM 2001 9 27 QXEA0101542 1 20010920 A 5753 BEAM DHAV DHC8 DHC8202 2809007 NM TE FLAPS CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - LEFT-HAND WING NR 4 FLAP BEAM INBOARD SURFACE "B" HAS SMALL PITS IN METALIC COATING ALONG ENTIRE ROLLER WEAR MARK. REPAIRED IAW HORIZON AIE EA 2-57-1373. 2 H 7 2 4T RT A13NM 2001092700128 20010927 00128 NM 2001 9 27 QXEA0101543 1 20010920 A 5753 BEAM DHAV DHC8 DHC8202 2809007 NM TE FLAPS CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - LEFT-HAND WING NR 4 FLAP BEAM OUTBOARD SURFACE "B" METALIC PLATING PITTED ALONG ENTIRE ROLLER WEAR MARK. REPAIRED IAW HORIZON AIR EA 2-57-137. 2 H 7 2 4T RT A13NM 2001092700129 20010927 00129 WP 2001 9 27 MWEA011261 1 20010915 A 5313 591140141 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 E&E COMPARTMENT LONGERON 29 RIGHT HAS SPOTS OF LIGHT CORROSION AFT OF STATION 180. REMOVED AND REPLACED LONGERON. 2 L 7 2 4F A6WE 2001092700130 20010927 00130 NM 2001 9 27 QXEA0101544 1 20010920 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM TE FLAPS CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - LEFT-HAND WING OUTBOARD FLAP NR 3 LOWER TRACK SURFACE "Y" HAS TWO WEAR PITS THROUGH METALIC PLATING ABOUT 10 INCH FROM AFT END OF TRACK. REPAIRED IAW RD 8-57-987. 2 H 7 2 4T RT A13NM 2001092700131 20010927 00131 NM 2001 9 27 QXEA0101545 1 20010920 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM TE FLAPS CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - LEFT-HAND WING OUTBOARD FLAP NR 3 TRACK LOWER RAIL UPPER SURFACE "Y" HAS A WEAR PIT THROUGH METALIC PLATING. REPAI RED IAW RD 8-57-987. 2 H 7 2 4T RT A13NM 2001092700132 20010927 00132 WP 2001 9 27 MWEA011264 1 20010915 A 5312 59101303 BULKHEAD DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 AFT PRESSURE BULKHEAD SKINS 5910130-3 /-5 ARE CRACKED ON THE LOWER INBOARD TABS. TRIMMED INBOARD TABS OF SKINS AND FABR ICATED AND INSTALLED NEW SPACER. 2 L 7 2 4F A6WE 2001092700133 20010927 00133 NM 2001 9 27 QXEA0101546 1 20010920 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM TE FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - LEFT-HAND WING OUTBOARD FLAP NR 3 TRACK LOWER RAIL UPPER SURFACE "Y" HAS TWO WEAR PITS ON OF THEM THROUGH METALIC PLATING, LOCATED 7" FROM FORWARD END. REPAIRED IAW RD 8-57-987. 2 H 7 2 4T RT A13NM 2001092700134 20010927 00134 NM 2001 9 27 QXEA0101547 1 20010922 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - SEAT TRACK #11, STATION 500, CORRODED INSIDE SEAT TRACK. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001092700135 20010927 00135 WP 2001 9 27 MWEA011268 1 20010915 A 5312 991556173 DOUBLER DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 FORWARD FACE OF AFT PRESSURE BULKHEAD, CORROSION ON VERTICAL LEG OF AFT PRESSURE BULKHEAD TEE, AT LONGERON 30 AREA. REM OVED AND REPLACED DOUBLER. 2 L 7 2 4F A6WE 2001092700136 20010927 00136 WP 2001 9 27 MWEA011269 1 20010915 A 5320 99155613 DOUBLER DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 STATION 996 VENTRAL STAIR WAY LOWER WEB CORRODED BETWEEN WEB SKINS BETWEEN 28 LEFT AND 28 RIGHT. FABRICATED AND INSTALL ED WEB SECTIONS AND DOUBLERS. 2 L 7 2 4F A6WE 2001092700137 20010927 00137 WP 2001 9 27 MWEA011271 1 20010915 A 5311 99115075 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 NOSE WHEEL WELL LEFT TUNNEL AREA, FRAME STATION 94 HAS A CRACK, LOCATED FORWARD OF EXTERNAL POWER RECEPTACLE. REMOVED A ND REPLACED FRAME SECTION. 2 L 7 2 4F A6WE 2001092700138 20010927 00138 WP 2001 9 27 MWEA011274 1 20010920 A 5320 99196287 SUPPORT BRACKET DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 AFT CARGO DOOR FUSELAGE SUPPORT BRACKET (AFT HINGE FORWARD BRACKET) HAS VERY ELONGATED FASTENER HOLES. FABRICATED AND I NSTALLED SUPPORT BRACKET. 2 L 7 2 4F A6WE 2001092700139 20010927 00139 WP 2001 9 27 MWEA011276 1 20010920 A 5310 99577193 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 SHEAR TIE CRACKED IN 2 PLACES AT STATION 945 LONGERON 15 RIGHT. FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F A6WE 2001092700140 20010927 00140 WP 2001 9 27 MWEA011338 1 20010925 A 5754 99225134 SLAT DOUG DC9 DC981 3022081 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 805ME 48031 HEAVY SPOT OF CORROSION INSIDE RIGHT SLAT NR 2 JUST INBOARD OF THE SLAT DRIVE TRACK, APPROXIMATELY STATION XOS 240. FAB RICATED AND INSTALLED END BRACKET AND REMOVED AND REPLACED NEW SPAR INBOARD SECTION. 2 L 7 2 4F A6WE 2001092700141 20010927 00141 NE 2001 9 27 NAFA20010001 2 20010709 A 8530 356994 CYLINDER DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE NR 3 ENGINE DAMAGED I N32B E ENGINE SHUTDOWN O OTHER CR CRUISE 1 AL 01 7780B 689 689 45372 NK510101 NR 3 ENGINE NR 13 CYLINDER LT & RT NO COMBUSTION PATTERN ON ANALYZER. REMOVED AND REPLACED THE NR 13 CYLINDER. 2 L 7 4 4R 4 R 6A3 5E8 2001092700142 20010927 00142 NE 2001 9 27 NAFA20010002 2 20010723 A 8530 356994 CYLINDER DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE NR 4 ENGINE CRACKED I N32B E A ENGINE SHUTDOWN UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS TO TAKEOFF 1 AL 01 7780B 381 381 45372 P31966 NR 4 ENGINE RUNS ROUGH AND ANALYZER SHOWED LOW COMPRESSION. REPLACED NR 3 CYLINDER. 2 L 7 4 4R 4 R 6A3 5E8 2001092700143 20010927 00143 WP 2001 9 27 NAFA20010003 1 20010910 A 5713 STRINGER DOUG DC6 DC6A 3021706 WP LT WING CRACKED I N32B K NONE O OTHER IN INSP/MAINT 1 AL 01 7780B 21494 45372 STRINGER 17 CRACKED AT WING STA L40. REPAIRED STRINGER 17 AT WING STA L40 IAW NAC 2001-05. 2 L 7 4 4R 6A3 2001092700145 20010927 00145 NE 2001 9 27 P2EA2001M0002 2 20010920 A 7200 SMOKE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 2 ENGINE DETECTED A P2EA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 05 130NJ 49222 717399 WHILE TAXIING TO GATE AFTER FLIGHT NR 2 ENGINE SHUT DOWN, GROUND PERSONAL REPORTED BLACK SMOKE, NO ABNORMAL INDICATIONS IN COCKPIT. OPERATED ENGINES UP TO TAKEOFF POWER ALL PARAMETERS NORMAL. SUSPECTED FUEL ICE PROBLEM. OPS CHECK FUEL AN TI-ICE PER MM 73-14-00, NO DEFECTS NOTED. 2 L 7 2 4F 4 F A6WE E9NE 2001092700147 20010927 00147 NM 2001 9 27 PCAA0109110 1 20010915 A 5210 STOP DHAV DHC8 DHC8102 2809003 NM PAX DOOR OUT OF ADJ A PCAA K NONE O OTHER TX TAXI/GRND HDL 1 EA 13 807EX 292 PHL- FLIGHT 1369. CREW REPORTED PASSENGER DOOR WOULD NOT OPEN FROM OUTSIDE. MAINTENANCE INSPECTED PASSENGER DOOR, AND ADJUSTED STOPPER ON EXTERIOR RELEASE HANDLE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001092700148 20010927 00148 NM 2001 9 27 PCAA0109111 1 20010906 A 5347 85320490 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 851EX 343 MDT- DURING C-CHECK INSPECTION INBOARD LEFT FORWARD SEATRAIL FOUND CORRODED. INBOARD LEFT FORWARD SEATRAIL SECTION, P/N 8532490 REPLACED IN ACCORDANCE WITH DEHAVILLAND AIRCRAFT DRAWING 85320019, BOMBARDIER AEROSPACE REPAIR DRAWING 8-53-307 4 AND DEHAVILLAND PSM 1-8-3 STRUCTURAL REPAIR MANUAL 51-20-16, 51-20-36, AND 51-40-11. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001092700149 20010927 00149 NM 2001 9 27 PCAA0109112 1 20010918 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN DISCONNECTED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 820EX 019 MDT- DURING ROUTINE MAINTENANCE VISIT FLOOR LEVEL EMERGENCY LIGHTS ON LEFT AFT SIDE FOUND INOPERATIVE. AFT LEAD TO FLOO R LEVEL EMERGENCY LIGHTING FOUND DISCONNECTED. REROUTED AND RECONNECTED LEAD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURN ED TO SERVICE. 2 H 7 2 4T RT A13NM 2001092700150 20010927 00150 SW 2001 9 27 PNSA010901 1 20010919 A 2150 20475546 ACM SWRNGN SA227 SA227AC 8780603 SW A/C BAY SEIZED A PNSA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 AL 03 640PA 8803 AC759B AFTER LANDING IN CDB PILOT NOTICED SMOKE IN CABIN. MAINTENANCE FOUND LT COOLING TURBINE SEIZED, BLEED AIR SYSTEM DEFERR ED PER MEL 21-3. 2 L 7 2 4T RT A8SW 2001092700151 20010927 00151 NE 2001 9 27 NACA20010033 2 20010914 A 8530 356993 CYLINDER DOUG DC6 DC6A 3021706 WP PWA R2800 R2800* 52026 NE NR 2 ENGINE CRACKED A NACA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS DE DESCENT 1 AL 03 2907F 1242 1242 533265 NK510771 NR 2 ENGINE RUNNING ROUGH, SUSPECT NR 4 CYLINDER. REMOVED AND REPLACED THE NR 4 CYLINDER ASSY. 2 L 7 4 4R 4 R 6A3 5E8 2001092700152 20010927 00152 NM 2001 9 27 P5A0100592 1 20010920 A 3350 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A P5CA K NONE L NO TEST IN INSP/MAINT 1 WP 23 858FT 20109 EMERGENCY LIGHTS IN UPPER DECK DO NOT TEST. REMOVED AND REPLACED U/D DOME EMERGENCY LIGHT PER MM 33-51-00. ALL OPS OK. 2 L 7 4 4F A20WE 2001092700153 20010927 00153 NE 2001 9 27 P5CA0100594 2 20010920 A 7200 ENGINE BOEING 747 7472U3B NM PWA JT9 JT9D7F 52054 NE NR 2 MALFUNCTIONED A P5CA E ENGINE SHUTDOWN E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS DE DESCENT 1 WP 23 922FT 22768 662991 WHEN THROTTLES WERE RETARDED FOR DESCENT, NR 2 ENG HAD EXCESSIVE VIBRATION FOLLOWED BY UNCLEARABLE STALL CONDITION. ENG SHUTDOWN WAS ACCOMPLISHED NORMALLY. LUBRICATED BLEED FEEDBACK PUSH PULL CABLE SYSTEM. INSPECTED ENG INLET EXHAUST BLE EDS. OPS CHECKED OK ON ENG GROUND RUN. 2 L 7 4 4F 4 F RT A20WE E20EA 2001092700154 20010927 00154 NM 2001 9 27 P5CA0100595 1 20010925 A 2710 AILERON BOEING 747 747123 1384873 NM WING HUNG UP A P5CA K NONE F FLT CONT AFFECTED CR CRUISE 1 WP 23 858FT 20109 WITH FLAPS UP, AILERON LOCKED UP WHILE TRYING TO MAKE A RIGHT TURN. WITH FLAPS 5 DEGREES, AILERON LOCKED AT LEFT BANK + /- 20 DEGREES (IAS 250 KNOTS). CLEANED LEFT AND RIGHT AILERON PROGRAMMERS AND LUBRICATED PER 12-21-16. FLIGHT CONTROL CHECK OF AILERONS OPERATION OK. 2 L 7 4 4F A20WE 2001092700155 20010927 00155 NE 2001 9 27 SABA010018 3 20010606 A 6110 4HFR34C653EFHJK PROPELLER BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE331* 01514 WP MCAULY 4HFR34 4HFR34C653 NE RT ENGINE DEFECTIVE A SABA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 33 963AE 963 P66264 901594 AIRCRAFT 963 ON FLIGHT 5123 FROM RDU TO ORF. AFTER ENTERING CRUISE FLIGHT THE RIGHT ENGINE PROPELLER FLUCTUATED UP TO T WO PERCENT. ALSO THE BETA CAP LIGHT ILLUMINATED. AIRCRAFT RETURNED TO RDU AND LANDED WITH NO OTHER PROBLEMS. NO INFLI GHT EMERGENCY WAS DECLARED. AIRCRAFT WAS FERRIED TO CLT FOR REPAIRS. MAINTENANCE REMOVED AND REPLACED THE RIGHT PROPEL LER. OPS CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 3 T RT A56EU E2WE 6 C 3PNE 2001092700156 20010927 00156 WP 2001 9 27 ZW0A0108304 1 20010905 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 DURING CHECK-C MAINT FOUND 2 HOLES OUTBOARD OF CABIN FLOOR SUPPORT, LONGERON 18R, STA 180, MEMBRANE. REPAIRED MEMBRANE PER SRM 51-70-4. 2 L 7 2 4F RT A6WE 2001092700157 20010927 00157 WP 2001 9 27 ZW0A0108402 1 20010910 A 5320 FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 926TW 49356 DURING CHECK-C MAINT FOUND IN LT WHEEL WELL POSSIBLE CRACK AT STA 946, KEEL BEAM AREA BETWEEN GEAR DOORS AT RBL 5 INCHES , 3 INCHES ABOVE FAIRING SUPPORTS. ACCOMPLISHED NDT HIGH FREQ EDDY CURRENT PER 51-00-03, PART 6 AND CONFIRMED CRACK. R EPLACED FITTING PER SPM 6-70-01. 2 L 7 2 4F A6WE 2001092700158 20010927 00158 WP 2001 9 27 ZW0A0108403 1 20010910 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 926TW 49356 DURING CHECK-C MAINT FOUND CORROSION ON FORMER FOOT AT LONGERON 29R TO LONGERON 29L, STA 1287. REMOVED CORROSION PER SP M 6-80-01. TREATED AND PAINTED PER SRM 51-10-03. FABRICATED AND INSTALLED FORMER SPLICE PER SRM 53-03, FIG 3 AND SRM 5 1-30-02. 2 L 7 2 4F A6WE 2001092700159 20010927 00159 WP 2001 9 27 ZW0A0108602 1 20010914 A 3350 LIGHT DOUG DC9 DC982 3022082 WP EMPENNAGE INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 905TW 49157 THE AFT TAIL CONE AREA EMERGENCY CAT WALK LIGHT, AND THE AFT TAIL CONE AREA EMERGENCY LIGHT, WERE INOPERATIVE. REPLACED THE LIGHT ASSEMBLY P/N 0200335-001 FOR THE CAT WALK LIGHT, AND REPLACED THE LIGHT ASSEMBLIES P/N 0200333-002 AND 020033 3-001 FOR THE EMERGENCY LIGHT. CHECK-C 4-12-01 MCI. 2 L 7 2 4F A6WE 2001092700160 20010927 00160 WP 2001 9 27 ZW0A0108604 1 20010911 A 2750 PULLEY BRACKET DOUG DC9 DC982 3022082 WP RT MLG WW CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 926TW 49356 DURING CHECK-C MAINT IN RT WHEEL WELL FOUND CRACK IN MOUNT BRACKET FOR FLAP BUS CABLE PULLEY MOUNT AT STA 994 TO 1003, B ETWEEN LONGERON 20R AND 21R. ACCOMPLISHED NDT HIGH FREQ EDDY CURRENT PER 51-00-03 PART 6 AND CONFIRMED CRACK. REMOVED CRACKED PART. INSTALLED NEW PART PER SPM 6-70-01 AND SRM 51-30-00. 2 L 7 2 4F A6WE 2001092700161 20010927 00161 WP 2001 9 27 ZW0A0108605 1 20010912 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 926TW 49356 DURING CHECK-C MAINT FOUND CHAIR TRACK DAMAGED AT LBL 44 INCHES, STA 200 INSIDE TRACK. REMOVED CORROSION AND REPLACED C HAIR TRACK PER SPM 6-80-01 PAGE 2, AND SRM 51-30-02. 2 L 7 2 4F A6WE 2001092700162 20010927 00162 WP 2001 9 27 ZW0A0108606 1 20010912 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 926TW 49356 DURING CHECK-C MAINT FOUND ANGLE WITH CORROSION AT STA 200, LBL 45. REPLACED CORRODED ANGLE PER SRM 51-30-02. 2 L 7 2 4F A6WE 2001092700163 20010927 00163 WP 2001 9 27 ZW0A0108607 1 20010912 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 926TW 49356 DURING CHECK-C MAINT FOUND A CLASS III REPAIR ON THE FUSELAGE AT STA 237, BETWEEN LONGERON 17L AND 18L. SKIN INSTALLED WITH CHERRY MAX RIVETS AT LONGERON 18 TO 17, STA 235. REMOVED REPAIR AND CUT OUT DAMAGED AREA UNDER REPAIR. INSTALLED FLUSH PATCH PER SSRM 53-10-107. 2 L 7 2 4F A6WE 2001092700164 20010927 00164 WP 2001 9 27 ZW0A0108608 1 20010911 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 911TW 49182 DURING CHECK-C MAINT IN AFT CARGO COMPT FOUND CORROSION ON STA 1309 FORMER, FROM RT LONGERON TO LT LONGERON 25. ACCOMPL ISHED SERVICE REWORK PER DRAWING SRO9530057, PARTS 5, 9, 12, AND 25, FOR FORMER SPLICE REPAIR PER SRM 53-03 PAGE 4J, AND TURNOVER CARDS. 2 L 7 2 4F A6WE 2001092700165 20010927 00165 WP 2001 9 27 ZW0A0108609 1 20010912 A 5320 PAN DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 911TW 49182 DURING CHECK-C MAINT FOUND AREA UNDER FWD CABIN GALLEY DRAIN CORRODED ALL AROUND PAN AS VIEWED FROM THE E&E COMPARTMENT. INSTALLED REPAIR DOUBLER PER SRM 53-01, AND INSTALLED NEW FLOOR SUPPORTS PER SPM 6-70-01. 2 L 7 2 4F A6WE 2001092700166 20010927 00166 NE 2001 9 27 DHL2001742013 2 20010924 A 7520 DUCT BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE DISLODGED A DHLA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 742DH 21290 NR 3 ENG GROUND FAULT LIGHT ILLUMINATED. FOUND GENERATOR COOLING DUCT DISLODGED AND RESTING ON FIRE LOOP. RESECURED CO OLING DUCT, CLEANED AND RE SEATED FIRE LOOP C/P. OPS NORMAL IAW MM CH 26-11-0. 2 L 7 3 4F 4 F A3WE E2EA 2001092800001 20010928 00001 WP 2001 9 28 ABXA010512 1 20010815 A 5310 36471172 FITTING DOUG DC8 DC863 302198A WP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 815AX 21291 LEFT WHEEL WELL LONGERON 24, FUSALAGE STATION 960, SUPPORT FITTING WAS CRACKED AND CORRODED AT UPPER FORWARD AND AFT HOR IZONTAL FLANGES. MAINTENANCE REPLACED THE FITTING AT STATION 960 IAW REA D853-41938MR. 2 L 7 4 4F 4A25 2001092800002 20010928 00002 WP 2001 9 28 ABXA010511 1 20010925 A 5310 DOUBLER DOUG DC8 DC863 302198A WP CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 815AX 21291 CORROSION FOUND AT FUSELAGE STATION 960 LEFT AT FLOOR LINE FINGER DOUBLER. MAINTENANCE INSTALLED DOUBLER REPAIR IAW REA D853-41935MR. 2 L 7 4 4F 4A25 2001092800003 20010928 00003 WP 2001 9 28 ABXA010510 1 20010925 A 5320 4751625U1 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 815AX 21291 FUSELAGE INTERIOR LONGERON SPLICE FITTING CRACKED AT FS 680.5, RIGHT LONGERON 10 AT UPPER NUT ANGLE. MAINTENANCE REPLACE D THE SPLICE FITTING IAW SRM 51-1-20D. 2 L 7 4 4F 4A25 2001092800004 20010928 00004 WP 2001 9 28 ABXA010509 1 20010925 A 5320 580267721N FITTING DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 815AX 21291 L24L SUPPORT FITTING AT STATION 960 WAS CRACKED AT UPPER FORWARD SIDE. MAINTENANCE REPLACED THE STUB FITTING IAW REA D 8 53-41938MR. 2 L 7 4 4F 4A25 2001092800005 20010928 00005 WP 2001 9 28 ABXA010508 1 20010925 A 5310 SKIN DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 815AX 21291 FUSELAGE EXTERIOR SKIN AT LEFT MID SERVICE DOOR CUTOUT FS 1287, CRACKED AT DOOR STRUT ATTACH POINT. MAINTENANCE INSTALLE D A DOUBLER REPAIR AT FUSELAGE IAW REA D853-41936MR. 2 L 7 4 4F 4A25 2001092800006 20010928 00006 WP 2001 9 28 ABXA010507 1 20010925 A 5710 SKIN DOUG DC8 DC863 302198A WP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 815AX 21291 RIGHT WING AT STATION XW 253 OUTBD OF #3 PYLON AT LEADING EDGE, WAS CRACKED. MAINTENANCE REPAIRED THE AREA IAW DC-8 SRM 57-2-1 FIG 2H. 2 L 7 4 4F 4A25 2001092800007 20010928 00007 WP 2001 9 28 ABXA010506 1 20010925 A 5210 DOOR DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 815AX 21291 MAIN CARGO DOOR LOWER FORWARD CORNER SKIN AND FRAME CRACKED. MAINTENANCE REPAIRED THE AREA IAW REA D852-41939MR AND REA 852-41940MR. 2 L 7 4 4F 4A25 2001092800008 20010928 00008 WP 2001 9 28 ABXA010505 1 20010925 A 5310 5750198 LONGERON DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 815AX 21291 L24L FOUND CRACKED AT FORWARD MAIN ATTACH BOLT HOLE. MAINTENANCE REPLACED L24L IAW REA D853-41938MR. 2 L 7 4 4F 4A25 2001092800009 20010928 00009 WP 2001 9 28 ABXA010513 1 20010827 A 5340 FITTING DOUG DC8 DC861 3021952 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 848AX 46032 MAIN CABIN TIE FITTING AT STA 682 L11R WAS CRACKED. MAINTENANCE REPLACED THE FITTING IAW DC-8 SRM. 2 L 7 4 4F 4A25 2001092800010 20010928 00010 WP 2001 9 28 ABXA010503 1 20010925 A 5210 ANGLE DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 815AX 21291 MAIN CARGO DOOR BOTTOM Z- ANGLE CRACKED AT FASTENER BS 140 AND BS 160. MAINTENANCE REPLACED THE Z-ANGLE AT BS 140 AND 16 0 IAW DC-8 SRM 53-01-0 AND 51-01-20. 2 L 7 4 4F 4A25 2001092800011 20010928 00011 WP 2001 9 28 ABXA010504 1 20010925 A 5310 RIB DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 815AX 21291 FUSELAGE RIB AT FS 880 LEFT WAS CRACKED. MAINTENANCE REPLACED THE RIB AT FS 880 LEFT, IAW DC-8 SRM 51-1-21. 2 L 7 4 4F 4A25 2001101500180 20011015 00180 NM 2001 10 15 01FDEA00861 1 20010926 A 2710 ARH7057515 ACTUATOR DOUG MD11 MD11F 3023600 NM AILERON FAILED A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 607FE 48547 AFTER T/O AILERON DEFLECT DISAGREE ALERT DISPLAYED. CYCLED FLAPS NO HELP. R&R LT O/B DEF AILERON ACT ASSY. 2 L 7 3 4F RT A22WE 2001092800012 20010928 00012 NM 2001 9 28 QXEA0101548 1 20010922 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - SEAT TRACK NR 11 CORRODED INSIDE AT STATION 437. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001092800013 20010928 00013 NM 2001 9 28 QXEA0101549 1 20010922 A 5340 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - SEAT TRACK NR 11 CHAFED ON TOP FLANGES AT STATION 437. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001092800014 20010928 00014 EA 2001 9 28 COMA0160754 1 20010926 A 2610 TERMINAL CNDAIR CL600 CL6002B19 EA A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 956CA 7105 FLIGHT #5332. WHEN THRUST LEVERS WERE ADVANCED FOR TAKE-OFF; RECEIVED A LEFT JET OVERHEAT MESSAGE, AIRCRAFT RETUREND TO THE GATE.REPOSITIONED CHAFING DETECTION LOOP TERMINAL ON LEFT ENGINE FROM LOWER CORE COWL. 2 L 7 2 4F RT A21EA 2001092800015 20010928 00015 NM 2001 9 28 QXEA0101550 1 20010922 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - SEAT TRACK NR 11 CHAFED ON INSIDE OF TRACK AT STATION 433. REPAIRED IAW RD 8-53-1432. 2 H 7 2 4T RT A13NM 2001092800016 20010928 00016 NM 2001 9 28 QXEA0101551 1 20010922 A 5340 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - SEAT TRACK NR 10 CORRODED ON TOP INBOARD AND OUTBOARD TIPS AT STATION 425. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001092800017 20010928 00017 NM 2001 9 28 QXEA0101552 1 20010922 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - SEAT TRACK NR 10 CHAFED INSIDE VALLEY OF SEAT TRACK AT STATION 405. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001092800018 20010928 00018 NM 2001 9 28 QXEA0101553 1 20010922 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - SEAT TRACK NR 10 CHAFED ON OUTSIDE LIP AT STATION 393. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001092800019 20010928 00019 NM 2001 9 28 QXEA0101554 1 20010922 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - SEAT TRACK NR 10 CORRODED INSIDE VALLEY AT STATION 374. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001092800020 20010928 00020 NM 2001 9 28 QXEA0101555 1 20010920 A 5753 ROLLER DHAV DHC8 DHC8202 2809007 NM FLAP TRACK STUCK A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - NR 5 FLAP SIDE TRACK ROLLER NOT ROLLING CAUSING PITS ON SIDE OF TRACKS. REPAIRED IAW HORIZON AIR EA 2-57-136. 2 H 7 2 4T RT A13NM 2001092800021 20010928 00021 NM 2001 9 28 QXEA0101556 1 20010922 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - SEAT TRACK NR 10 CHAFED ON TOP LIPS AT STATION 371. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001092800022 20010928 00022 WP 2001 9 28 0103419616 1 20010105 A 5342 ATTACH ANGLE DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 616NW 47229 DURING H-CHECK FOUND CORROSION ON THE HORIZONTAL FLANGE OF THE VERTICAL STABILIZER-FUSELAGE ATTACH ANGLE. REPAIRED PER EA 99-177558. 2 L 7 2 4F A6WE 2001092800023 20010928 00023 WP 2001 9 28 USAAD01152 1 20010817 A 3350 AD4002P BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805US 48053 PIT - THE AFT CABIN EMERGENCY EXIT LIGHTS WERE FLASHING WITH THE EMERGENCY LIGHT SWITCH IN THE ARMED POSITION. MAINTENA NCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001092800024 20010928 00024 NM 2001 9 28 USAABB01085 1 20010823 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 620AU 27199 BWI - FOUND THE EMERGENCY LIGHT AT ROW 9 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2001092800025 20010928 00025 WP 2001 9 28 USAAD01154 1 20010828 A 2400 696233B CSD DOUG DC9 DC982 3022082 WP LT ENGINE FAILED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 EA 19 821US 39337 49138 PIT - BWI -FLT 1458 - AFTER TAKEOFF, THE LEFT CSD LOW OIL PRESSURE LIGHT ILLUMINATED AND THE CSD WAS DISCONNECTED. SINC E THE APU WAS ON MEL THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT CSD, CSD OIL COOLER, AND LEFT GENERATOR. (M) 2 L 7 2 4F A6WE 2001092800026 20010928 00026 WP 2001 9 28 USAAD01158 1 20010903 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 819US 48099 IND - THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS, LEFT AND RIGHT AFT OVERWING EXIT EMERGENCY LIGHTS, AND THE AFT FUSELA GE REMOTE RECEIVER WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES AND THE REMOTE RECEIVER. (M) 2 L 7 2 4F A6WE 2001092800027 20010928 00027 WP 2001 9 28 USAAD01159 1 20010904 A 3350 9721055 BATTERY DOUG DC9 DC982 3022082 WP PAX CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 821US 49138 IND - THE SEAT MOUNTED EMEREGNCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMEREGNCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001092800028 20010928 00028 NM 2001 9 28 USAASB01246 1 20010902 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM FWD/AFT CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 385US 22958 LGA- MAINTENANCE FOUND THE AISLE EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT POWER SUPPLY (P /N 11-0049) AND BATTERY PACK ALONG WITH THE FORWARD AND RIGHT FORWARCD BATTERY PACKS. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001092800029 20010928 00029 WP 2001 9 28 HALA010022 1 20010902 A 3200 VALVE DOUG DC9 DC951 3022051 WP A HALA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 WP 13 699HA 47763 ATB - NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. NOSE GEAR UNSAFE LIGHT ILLUMINATED, NOSE GEAR GREEN LIGHT ILLUMINATED RECYCLED GEAR WNO CHANGE. RETURNED TO OGG - LANDING NORMAL. FOUND NOSE STRUT UNDER SERVICED. SERVICED PER MM 32-21-2 METHOD 'B'. REPLACED SHRADER VALVE AND PACKING, GEAR, GEAR SWING. OPS CHECK, LEAK CHECK GOOD. AIRCRAFT FERRIED TO HNL . (M) 2 L 7 2 4F RT A6WE 2001092800030 20010928 00030 WP 2001 9 28 GTIA010850 1 20010904 A 2150 20495053 ACM DOUG DC9 DC982 3022082 WP RIGHT LEAKING A GTIA O OTHER K FLUID LOSS CL CLIMB 1 GL 23 823NK 48020 DTW - FLT 941 - ON INITIAL CLIMB THROUGH APPROX 4000 'A' FLIGHT ATTENDANT REPORTED THICK OILY SMOKE IN AFT CABIN COMPLIE D WITH QRH PROCEDURE RETURNED TO DTW BOTH AC PACKS OFF SMOKE DISIPATED. FOUND ACM (RT) SHAFT LEAKING OIL INTO AIR CONDI TIONING SYSTEM. REMOVED AND REPLACED RIGHT ACM IAW MD 80 MM 21-51-01 LEAK AND FUNCTIONAL CHECK GOOD. NO SMOKE NOTED IN CABIN. (M) 2 L 7 2 4F A6WE 2001092800031 20010928 00031 WP 2001 9 28 GTIA010865 1 20010904 A 2700 591096253AB2 JACKSCREW DOUG DC9 DC981 3022081 WP A GTIA O OTHER O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 DTW - FOUND JACKSCREW FAILED PHASE 2 INPSECTION, REF W/C 00115 END PLAY AT .1875 INCH. REMOVED AND REPLACED JACKSCREW I AW MD80 MM 27-40-01. OPS CHECK GOOD END PLAY .003 FREE PLAY .006. (M) 2 L 7 2 4F A6WE 2001092800032 20010928 00032 WP 2001 9 28 0103429617 1 20010320 A 5312 BULKHEAD DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 617NW 47235 DURING H-CHECK FOUND CORROSION IN THE BULKHEAD WEB. REPAIRED PER EA 96-181030. 2 L 7 2 4F A6WE 2001092800033 20010928 00033 NM 2001 9 28 QXEA0101557 1 20010922 A 5340 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - SEAT TRACK NR 10 CORRODED ON TOP LIPS AT STATION 350. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001092800034 20010928 00034 WP 2001 9 28 ABXA010501 1 20010924 A 3350 41B004AD0763 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 948AX 47065 THE COCKPIT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE ON PRE-DEPARTURE CHECK. MAINTENANCE INSPECTED AND REPLACED TH E EMERGENCY LIGHT BATTERIES IAW DC-9 MM 33-53-02. OPERATION CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERV ICE. 2 L 7 2 4F A6WE 2001092800035 20010928 00035 NM 2001 9 28 QXEA0101558 1 20010922 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - SEAT TRACK NR 10 CORRODED ON TOP LIPS AT STATION 342. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001092800036 20010928 00036 WP 2001 9 28 ABXA010502 1 20010926 A 3350 60030451 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 957AX 80474 270 47759 EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK IAW DC-9 MM 33-5 0-00. 2 L 7 2 4F A6WE 2001092800037 20010928 00037 WP 2001 9 28 ABXA010514 1 20010925 A 2760 3719596501 DRIVE LINK DOUG DC8 DC863 302198A WP LT SPOILER BROKEN A ABXA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 GL 23 820AX 69470 46155 THE LEFT MID FLIGHT SPOILER INBOARD DRIVE LINK FOUND BROKEN DURING SERVICE CHECK INSPECTION. MAINTENANCE INSPECTED AND REPLACED THE INBOARD DRIVE LINK CRANK ASSY AND COMPLETED OPERATIONAL CHECKS IAW DC-8 MM 27-61-01-2. 2 L 7 4 4F 4A25 2001092800038 20010928 00038 WP 2001 9 28 ABXA010515 1 20010927 A 3231 39567851 DRIVE LINK DOUG DC9 DC941 302207N WP NLG DOOR BINDING A ABXA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 23 957AX 47759 AFTER TAKEOFF WHEN THE LANDING GEAR WAS RAISED, A LOUD NOISE AND VIBRATIONS WERE NOTED FROM THE NOSE LANDING GEAR AREA. MAINTENANCE INSPECTED AND FOUND THE RIGHT NOSE LANDING GEAR OPEN ON THE TAXI IN. THE RIGHT FORWARD NOSE LANDING GEAR D OOR WAS FOUND TO BE BINDING. MAINTENANCE LUBRICATED THE DOOR DRIVE LINK AND COMPLETED OPERATIONAL CHECKS IAW DC-9 MM 32 -20-00. 2 L 7 2 4F A6WE 2001092800039 20010928 00039 CE 2001 9 28 BSY2001F00012 1 20010909 A 2910 HYDRAULIC LINE LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP HYDRAULIC SYS LEAKING E BSYA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 07 684HA 113 P74404 (CMH) LOST HYDRAULIC PRESSURE COMING INTO AIRPORT, BLEW GEAR DOWN LANDED OK. REPAIRED HYDRAULIC LINE. NOSE WHEEL WELL, SERVICED RES. CHANGED BOTH PUMPS AS PRECAUTIONARY MEASURES, OPS CHECK GOOD. 2 L 7 2 4F 4 F A10CE E6WE 2001092800041 20010928 00041 NE 2001 9 28 BSY2001F00014 2 20010719 A 7200 CJ6106 ENGINE LEAR 25 25 5170506 CE GE CJ610 CJ6106 30006 NE RIGHT FLAMED OUT E BSYA O OTHER X ENGINE FLAMEOUT CL CLIMB 1 GL 07 121EL 12563 1611 010 251287 AIRCRAFT WAS AT FL 440 CLIMBING ABOVE SOME STORMS, RIGHT ENGINE FLAMED OUT DUE TO HEAVY TURBULENCE WHICH CAUSED INTERRUP TION OF AIR INTO INLET. AIRCRAFT DESCENDED TO LOWER ALTITUDE, RELIGHT OF ENGINE ACCOMPLISHED. THIS ENGINE HAS HAD NO F LAME-OUT PROBLEMS, OPERATED NORMALLY ON INSPECTION GROUND CHECK, NO REPAIRS REQUIRED. 2 L 7 2 4J 4 J A10CE 1E16 2001092800043 20010928 00043 EU 2001 9 28 AWXA200100476 1 20010925 A 2910 NAS1611224 PACKING AEROQUIP AIRBUS 320 A320231 3930325 EU ZONE 198 BROKEN A AWXA L ABORTED APPROACH K FLUID LOSS AP APPROACH 1 WP 28 627AW 66 LAX - ABORTED APPROACH - FLT 37 - "C" - ON FINAL APPROACH ECAM INDICATED YELLOW HYDRAULIC SYSTEM LOW PRESSURE, SYSTEM FL UID DEPLETED AND THE CREW PERFORMED A GO AROUND. THE SUBSEQUENT APPROACH AND LANDING WAS UNEVENTFUL. MAINTENANCE INSPEC TED THE AIRCRAFT AND FOUND A PACKING FROM THE QUICK DISCONNECT FITTING FROM THE PTU BROKEN AND THE FITTING LEAKING FLUID . MAINTENANCE REPLACED THE PACKING, SERVICED THE HYD SYSTEM AND PERFORMED LEAK CHECKS, ALL CHECKS WERE GOOD. 2 L 7 2 4F RT A28NM 2001092800044 20010928 00044 EU 2001 9 28 C2XA01BT168 1 20010926 A 3234 F96GA0102 CONTROL HANDLE AEROSP ATR42 ATR42320 8680930 EU COCKPIT INTERMITTENT A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 19812 099 SYR/BTV---CO3185, CREW REPORTED, THE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. MAINTENANCE DISPATCHED TO SYR, INSPE CTED AIRCRAFT AND RELEASED AIRCRAFT IAW MEL 32-31-03 PLACARD NUMBER 015983. AIRCRAFT RETURNED TO SERVICE. DUE TO WEATH ER RESTRICTIONS TOWARD INTENDED DESTINATION AIRCRAFT REPOSITIONED TO BTV TO CLEAR THE MEL. BTV MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL SELECTOR LEVER IAW ATR42 AMM 32-31-81. SYSTEM OPS CHECKED GOOD. MEL CLEARED. 2 H 7 2 4T RT A53EU 2001092800045 20010928 00045 EU 2001 9 28 C2XA01CL207 1 20010925 A 3230 C245890002 UPLOCK AEROSP ATR42 ATR42320 8680930 EU RT MLG FAILED A C2XA K NONE J WARNING INDICATION CR CRUISE 1 SW 27 14821 1935 160 CLE FLT 3189 CREW REPORTED A LANDING GEAR UNSAFE INDICATION (RIGHT MAIN GEAR) DURING FLIGHT. AIRCRAFT LANDED WITHOUT I NCIDENT. MAINTENANCE REMOVED AND REPLACED UNLOCK BOX ASSEMBLY. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS RELEASED BACK T O SERVICE. 2 H 7 2 4T RT A53EU 2001092800046 20010928 00046 SO 2001 9 28 C2XA01TY123 1 20010925 A 3350 5113 LIGHT EMB 145 EMB145 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12921 145354 TYS DURING A SCHEDULED INSPECTION THE AISLE PATH LIGHTING AT SEATS 8A,14A,15A,16A, AND 19A WERE FOUND TO BE INOPERATIVE . MAINTENANCE REMOVED AND REPLACED THE LIGHT BULBS, OPERATIONAL CHECK WAS SATISFACTORY IAW EMB-145 MM 33-21-06. AIRCRA FT RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001092800047 20010928 00047 NM 2001 9 28 QXEA0101559 1 20010922 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - SEAT TRACK NR 10 CORRODED ON INSIDE AND ON INSIDE LIP AT STATION 329. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001092800048 20010928 00048 NE 2001 9 28 DLM88011496 2 20010906 A 7510 DUCT DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE BLOWN A DALA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 SO 27 939DL 49812 718045 DURING CLIMB LT ENG OIL PRESS LOW MESSAGE ALONG WITH LT ENG OIL PRESS WENT TO DASHES. AT THE SAME TIME THE LT FF BLANKE D MTC FOUND LT ENG LT FRONT FRAME A/I VALVE AFT DUCTING BLOWN WHERE IT COMES OUT OF THE ENG CASE AT THE 8 TH STAGE WIRIN G WAS CUT AND MELTED. REPLACED DUCT AND REPAIRED HARNESS. 2 L 7 2 4F 4 F RT A6WE E9NE 2001092800049 20010928 00049 NM 2001 9 28 QXEA0101560 1 20010922 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - SEAT TRACK NR 10 CORRODED ON INBOARD AND OUTBOARD LIPS AT STATION 298. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001092800050 20010928 00050 NM 2001 9 28 QXEA0101561 1 20010922 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - SEAT TRACK NR 10 CORRODED ON OUTBOARD LIP AT STATION 296. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001092800051 20010928 00051 NM 2001 9 28 QXEA0101562 1 20010922 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - SEAT TRACK NR 10 CORRODED INSIDE VALLEY AT STATION 280. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001092800052 20010928 00052 NM 2001 9 28 QXEA0101563 1 20010922 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - SEAT TRACK NR 10 CORRODED ON INSIDE VALLEY AT STATION 278. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001092800053 20010928 00053 NM 2001 9 28 QXEA0101564 1 20010922 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - SEAT TRACK NR 10 CORRODED ON TOP LIPS AT STATION 265. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001092800054 20010928 00054 NM 2001 9 28 QXEA0101565 1 20010922 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - SEAT TRACK NR 10 CORRODED ON INBOARD AND OUTBOARD LIPS AT STATION 291. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001092800055 20010928 00055 NE 2001 9 28 DLM88011508 2 20010908 A 7261 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 LEAKING A DALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 912DL 21925 49543 AT 1000 FT AGL CREW EXPERIENCED SMOKE/HAZE IN CABIN. ANTI ICE SYSTEM NOT IN USE. REPLACED NR 1 ENGINE FOR INTERNAL OIL LEAK. 2 L 7 2 4F 4 F RT A6WE E9NE 2001092800056 20010928 00056 NM 2001 9 28 QXEA0101566 1 20010920 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - LEFT-HAND INBOARD SEAT TRACK AT APPROXIMATELY STATION 291.400 HAS LIGHT GOUGES IN CENTER. REPAIRED IAW RD 8-53-133 9, RD 8-53-1102 ABD DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001092800057 20010928 00057 2001 9 28 DLM88011529 4 20010911 A 2565 D29984213 SLIDE DOUG MD88 MD88 3023688 NM TAIL CONE FAILED A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 976DL 53257 ATC ORDERED AIRCRAFT TO LAND ASAP FOR SECURITY CONCERNS. RAMP PERSONNEL PULLED OUTSIDE EMERGENCY HANDLE AND DEPLOYED TH E TAIL CONE. HOWEVER THE EMERGENCY SLIDE DID NOT DEPLOY. MTC INSTALLED TAIL CONE AND AIRCRAFT WAS FERRIED TO ATL. SLI DE WAS REPLACED IN ATL DPN 259001305. 2 L 7 2 4F RT A6WE 2001092800058 20010928 00058 NM 2001 9 28 QXEA0101567 1 20010920 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - LEFT-HAND INBOARD SEAT TRACK AT APPROXIMATELY STATION 445.500 HAS LIGHT GOUGES IN CENTER. REPAIRED IAW RD 8-53-133 9 AND DHC-8 SRM 51-20-36. 2 H 7 2 4T RT A13NM 2001092800059 20010928 00059 GL 2001 9 28 C2XA01IA364 2 20010925 A 7200 23072309 SEAL EMB 135 EMB135LR SO ALLSN AE300 AE3007A GL LEFT ENGINE LEAKING A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 14514 2654 2654 145303 CAE311500 ICT FLT#4151 - CREW REPORTED A "PACK 2 FAIL" MESSAGE AFTER TAKEOFF AND RETURNED TO ICT. THE #2 PACK WAS PLACED ON MEL AN D THE AIRCRAFT DISPATCHED. UPON THE NEXT TAKEOFF WITH THE #2 PACK MEL, A LAV SMOKE INDICATION WAS DISPLAYED AND THE AIRC RAFT RETURNED AGAIN TO ICT WHERE MAINTENANCE PLACED THE NUMBER ONE BLEED SYSTEM ON MEL. THE AIRCRAFT WAS RETURNED TO SER VICE. AT IAH, DURING FURTHER TROUBLESHOOTING OF THE #1 BLEED SYSTEM MEL, MAINETANNCE FOUND THE #1 ENGINE FAN SEAL TO BE LEAKING OIL. THE AFFECTED SEAL WAS REMOVED AND REPLACED, THE AIRCRAFT WAS OPERATIONALLY AND LEAK CHECKED, AND THEN RETUR NED TO SERVICE. 2 L 7 2 4F 4 F RT TOOO11AT TE6CH 2001092800060 20010928 00060 NM 2001 9 28 AWXA200100477 1 20010911 A 5311 654796039 FRAME BOEING 737 7373G7 1384595 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 MCN-C17 CK - "C" - CORROSION FOUND ON AFT PIT FRAME BS 848 NEAR CARGO DOOR OPENING, BEYOND SRM LIMITS. ALSO, UPPER LEG A NGLE FOR FRAME WEB AND FILLER STRAP CORRODED, FOUND IN LIMITS. MAINTENANCE INSTALLED REPAIR ANGLE ON FRAME BS 848 IAW B737 SRM 51-70-11 PG 1-6. REMOVED CORROSION FROM UPPER LEG ANGLE FOR FRAME WEB AND FILLER STRAP, TREATED, PRIMED AND PA INTED. 2 L 7 2 4F RT A16WE 2001092800061 20010928 00061 NM 2001 9 28 AWXA200100478 1 20010911 A 5320 65677757 FRAME BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 MCN-C17 CK - "C" - CRACK FOUND STA 616 LEFT HAND, INBOARD ANGLE BELOW FLOOR WEB. MAINTENANCE REPAIRED ANGLE IAW AWA ER 03-5311-01143-DD1. 2 L 7 2 4F RT A16WE 2001092800062 20010928 00062 NM 2001 9 28 DLM88011530 1 20010914 A 3260 833703 SENSOR DOUG MD88 MD88 3023688 NM NLG FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 962DL 49981 ON DEPARTURE THE NOSE GEAR DID NOT RETRACT. RED LIGHT WAS ON AND BOTH MAIN LIGHTS WERE EXTINGUISHED. REPLACED LOCK SEN SOR. 2 L 7 2 4F RT A6WE 2001092800063 20010928 00063 NM 2001 9 28 QXEA0101568 1 20010920 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - LEFT-HAND INBOARD SEAT TRACK AT APPROXIMATELY STATION 488.500 HAS LGIHT GOUGES IN CENTER. REPAIRED IAW RD 8-53-133 9 AND DHC-8 SRM 51-20-36. 2 H 7 2 4T RT A13NM 2001092800064 20010928 00064 NM 2001 9 28 DLM88011562 1 20010919 A 3350 20131A BATTERY PACK DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 926DL 49713 F/C EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F RT A6WE 2001092800065 20010928 00065 NM 2001 9 28 DLM90011517 1 20010909 A 2420 3101363901 TRANSFORMER DOUG MD90 MD9030 3023690 NM COCKPIT FAILED A DALA O OTHER M OVER TEMP DE DESCENT 1 SO 27 914DN 53394 L9 CIRCUIT BREAKER POPPING. T1-20 RIGHT INSTRUMENT TRANSFORMER REPLACED. 2 L 7 2 4F RT A6WE 2001092800067 20010928 00067 NM 2001 9 28 QXEA0101569 1 20010920 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - LEFT-HAND INBOARD SEAT TRACK AT APPROXIMATELY STATION 510.00 HAS LIGHT GOUGES IN CENTER. REPAIRED IAW RD 8-53-1339 AND DHC-8 SRM 51-20-36. 2 H 7 2 4T RT A13NM 2001092800069 20010928 00069 NM 2001 9 28 QXEA0101570 1 20010920 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - RIGHT-HAND INBOARD SEAT TRACK AT APPROXIMATELY 467.00 HAS TWO GOUGES IN CENTER. REPAIRED IAW RD 8-53-1339, DHC-8 S RM 51-20-16 AND SRM SRM 51-20-41. 2 H 7 2 4T RT A13NM 2001092800071 20010928 00071 NM 2001 9 28 QXEA0101571 1 20010922 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - LEFT-HAND INBOARD SEAT TRACK AT APPROXIMATELY STATION 540.00 IS GOUGED IN CENTER. REPAIRED IAW DHC-8 SRM 51-20-36. 2 H 7 2 4T RT A13NM 2001092800072 20010928 00072 CE 2001 9 28 GLBA2001204 1 20010909 A 3610 DUCT BEECH 1900 1900D 1154162 CE BLEED AIR DAMAGED A GLBA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 01 170GL UE170 RIGHT BLEED AIR FAILURE AND LOSS OF PRESSURIZATION. REPAIRED EVA TUBING, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001092800073 20010928 00073 NM 2001 9 28 QXEA0101572 1 20010920 A 5320 STRUCTURE DHAV DHC8 DHC8202 2809007 NM FLOOR DRIP TRAY CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - CENTER FLOOR BOARD DRIP TRAY IS CRACKED IN TWO SPOTS AT STATION 430.00. REPAIRED IAW RD 51-40-11. 2 H 7 2 4T RT A13NM 2001092800074 20010928 00074 NM 2001 9 28 QXEA0101573 1 20010919 A 5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - CABIN WARDROBE FLOOR SUPPORT IS CORRODED AT NUTPLATE AT STATION 210.00 AND 2100.052. REPAIRED IAW RD 8-53-1339. 2 H 7 2 4T RT A13NM 2001092800075 20010928 00075 NM 2001 9 28 QXEA0101574 1 20010920 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - LEFT-HAND INBOARD SEAT TRACK BETWEEN STATION 182 AND 262.40 HAS LIGHT SURFACE CORROSION. REPAIRED IAW 8-53-1342. 2 H 7 2 4T RT A13NM 2001092800077 20010928 00077 NM 2001 9 28 QXEA0101575 1 20010922 A 5410 STRUT DHAV DHC8 DHC8202 2809007 NM NR 1 NACELLE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - NR 1 ENGINE INBOARD AFT NACELLE STRUT JUST ABOVE INBOARD IGNITOR DOOR HAS CORROSION FROM ENGINE EXHAUST. REPAIRED IAW DHC-8 SRM 51-20-36 AND HORIZON AIR EA 2-54-102. 2 H 7 2 4T RT A13NM 2001092800078 20010928 00078 CE 2001 9 28 GLBA2001208 1 20010925 A 3260 H111541 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE LT MLG FAILED A GLBA K NONE N FALSE WARNING CR CRUISE 1 CE 01 228GL UE228 LANDING GEAR INTRANSIT LIGHT ILLUMINATED WITH GEAR UP. INSPECTED, REPLACED UPLOCK SWITCH, OPS CHECKED SYSTEM SATISFACTO RY. 2 L 7 2 4T RT A24CE 2001092800079 20010928 00079 NM 2001 9 28 F3LA200100111 1 20010926 A 5230 DOOR FRAME BOEING BOEING 737 7372Y5 1384554 NM CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 921WA 2755 753 23039 DURING C-3 CHECK, INSPECTION REPORTED CRACK IN LOWER AFT CORNER OF C1 DOOR. DOOR WAS REPAIRED AT VENDOR AND RETURNED IN SERVICEABLE CONDITION. 2 L 7 2 4U RT A16WE 2001092800080 20010928 00080 WP 2001 9 28 IXXA0100056S 1 20010504 A 5220 DOOR FRAME DOUG DC8 DC871F 302199D WP EMERGENCY EXIT DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 84173 2919 45813 DURING ROUTINE C-CHECK INSPECTION, ON THE LEFT HAND AFT OVERWING EMERGENCY EXIT DOOR FRAME BOTTOM SIDE FORWARD DOOR KEEP ER STOP WAS FOUND DAMAGED. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED KEEPER, FABRICATION AND INSTALLATION OF NEW CLIP IN A CCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL, DACO DRAWING 2779323 AND ENGINEERING ORDER 52-DC8-3037. 2 L 7 4 4F RT 4A25 2001092800081 20010928 00081 WP 2001 9 28 IXXA0100060S 1 20010503 A 5522 SKIN DOUG DC8 DC871F 302199D WP ELEVATOR GOUGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 84173 2919 45813 DURING ROUTINE C-CHECK INSPECTION, A GOUGE WAS DETECTED ON THE LEFT ELEVATOR UPPER SKIN AT STATION XE 176. REPAIR ACCOM PLISHED FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERI NG ORDER 55-DC8-3046. 2 L 7 4 4F RT 4A25 2001092800082 20010928 00082 WP 2001 9 28 IXXA0100062S 1 20010503 A 5230 SKIN DOUG DC8 DC871F 302199D WP CARGO DOOR GOUGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 84173 2919 45813 DURING ROUTINE C-CHECK INSPECTION, A GOUGE WAS DETECTED IN THE A-PIT BASKET EXTERNAL DOOR PLATING RIGHT HAND AFT CORNER. REPAIR ACCOMPLISHED FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING ORDER 52-DC8-3054. 2 L 7 4 4F RT 4A25 2001092800083 20010928 00083 WP 2001 9 28 IXXA0100064S 1 20010503 A 5230 DOOR FRAME DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 84173 2919 45813 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE C-PIT BASKET DOOR FORWARD CENTER DOOR PAN FRAME. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA. FABRICATION AND INSTALLATION OF DOOR PAN AND SPLICE IN ACCORDANCE WITH DOUGLAS ST RUCTURAL REPAIR MANUAL, DAC DRAWING 5704349 AND ENGINEERING ORDER 52-DC8-3052. 2 L 7 4 4F RT 4A25 2001092800084 20010928 00084 NM 2001 9 28 QXEA0101576 1 20010920 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM TE FLAPS CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - LEFT-HAND WING OUTBOARD FLAP TRACK NR 3 UPPER RAIL, LOWER SURFACE HAS TWO WEAR PITS THROUGH METALIC PLATING. REPAI RED IAW RD 8-57-987. 2 H 7 2 4T RT A13NM 2001092800085 20010928 00085 NM 2001 9 28 QXEA0101577 1 20010920 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM TE FLAPS CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - LEFT-HAND WING FLAP NR 3 TRACK UPPER RAIL, LOWER SURFACE HAS TWO WEAR PITS THROUGH METALIC PLATING, LOCATED 7 INCH ES FROM FORWARD END. REPAIRED IAW RD 8-57-987. 2 H 7 2 4T RT A13NM 2001092800086 20010928 00086 NM 2001 9 28 QXEA0101578 1 20010920 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM LT WING TE FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - LEFT-HAND WING OUTBOARD FLAP NR 4 TRACK, OUTBOARD SURFACE "D" HAS A WEAR PIT THROUGH METALIC PLATING IN FORWARD EN D OF ROLLER WEAR MARK. REPAIRED IAW HORIZON AIR EA 2-57-137. 2 H 7 2 4T RT A13NM 2001092800087 20010928 00087 NM 2001 9 28 QXEA0101579 1 20010921 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM LT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - LEFT-HAND WING INBOARD LEADING EDGE 511AL, LOWER ATTACH FLANGE ON FRONT SPAR, INBOARD NUTPLATE HAS DAMAGED BUSHING S. REPAIRED IAW HORIZON AIR EA 2-57-139. 2 H 7 2 4T RT A13NM 2001092800088 20010928 00088 WP 2001 9 28 MWEA011281 1 20010925 A 5320 49176501 CLIP DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 AFT CARGO COMPARTMENT LONGERON 29 LEFT END CLIP FORWARD OF FRAME STATION 1338 HAS LIGHT CORROSION AROUND A FASTENER. RE MOVED AND REPLACED SHOVEL CLIP. 2 L 7 2 4F A6WE 2001092800089 20010928 00089 NM 2001 9 28 QXEA0101580 1 20010922 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM LT WING TE FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - LEFT-HAND WING INBOARD FLAP NR 1 TRACK UPPER RAIL, UPPER SURFACE HAS TWO WEAR PITS THROUGH METALIC PLATING, LOCATE D 9 INCHES FROM FRONT END. REPAIRED IAW RD 8-57-985. 2 H 7 2 4T RT A13NM 2001092800090 20010928 00090 NM 2001 9 28 QXEA0101581 1 20010922 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM LT WING TE FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - LEFT-HAND WING INBOARD FLAP NR 1 TRACK LOWER RAIL, UPPER SURFACE HAS THREE WEAR PITS THROUGH METALIC PLATING, ONE LOCATED AT FORWARD END AND 2 LOCATED 6 INCH AFT OF FORWARD PIT. REPAIRED IAW RD 8-57-985. 2 H 7 2 4T RT A13NM 2001092800091 20010928 00091 NM 2001 9 28 QXEA0101582 1 20010922 A 5412 FIREWALL DHAV DHC8 DHC8202 2809007 NM RT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - RIGHT-HAND NACELLE OUTBOARD SIDE AFT FIRE WALL HAS A 2 INCH CRACK BETWEEN THE FIRE LOOP BRACKET AND SUPPORT. REPAI RED IAW RD 8-54-806. 2 H 7 2 4T RT A13NM 2001092800092 20010928 00092 NM 2001 9 28 QXEA0101583 1 20010922 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - LIGHT SURFACE CORROSION AT FRAME FLANGE AND LOWER FUSELAGE SKIN AT STATION 467.00, RIGHT-HAND BETWEEN STRINGER 30 AND 31. REPAIRED IAW DHC-8 SRM 51-20-16 2 H 7 2 4T RT A13NM 2001092800093 20010928 00093 WP 2001 9 28 MWEA011283 1 20010925 A 5320 991556173 STIFFENER DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 STATION 1338 JACK PAD ANGLE STIFFENER THAT ATTACHES TO APB TEE HAS CORROSION. REMOVED AND REPLACED JACK PAD ANGLE STIFF ENER. 2 L 7 2 4F A6WE 2001092800094 20010928 00094 WP 2001 9 28 MWEA011284 1 20010925 A 5310 591013045 SHEAR TIE DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 AFT CARGO COMPARTMENT SHEAR TIE STATION 1338 HAS LIGHT CORROSION ON FORWARD SIDE AT LONGERON 23 LEFT. REMOVED AND REPLA CED SHEAR TIE. 2 L 7 2 4F A6WE 2001092800095 20010928 00095 WP 2001 9 28 MWEA011285 1 20010925 A 5313 5936051501 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 MID CARGO BAY LONGERON 28 LEFT HAD AREA OF LIGHT CORROSION BETWEEN STATION 598 THROUGH STATION 629. REMOVED AND REPLACE D LONGERON SECTION AND REPAIR SPLICE. 2 L 7 2 4F A6WE 2001092800096 20010928 00096 WP 2001 9 28 MWEA011286 1 20010925 A 5313 5936053 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 MID CARGO BAY LONGERON 29 LEFT HAS AREAS OF LIGHT CORROSION BETWEEN STATION 636. REMOVED AND REPLACED LONGERON SECTION AND SPLICE SECTION. 2 L 7 2 4F A6WE 2001092800097 20010928 00097 WP 2001 9 28 MWEA011287 1 20010925 A 5313 59360531 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 MID CARGO BAY LONGERON 30 HAS AREAS OF LIGHT CORROSION BETWEEN STATION 647 - STATION 676. REMOVED AND REPLACED LONGERON SECTION AND SPLICE SECTION. 2 L 7 2 4F A6WE 2001092800098 20010928 00098 WP 2001 9 28 MWEA011288 1 20010925 A 5313 59360511 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 MID CARGO BAY LONGERON 26 LEFT HAS AREAS OF LIGHT CORROSION BETWEEN STATION 634 THROUGH 637.5. REMOVED AND REPLACED LON GERON SECTION AND REPAIR SPLICE. 2 L 7 2 4F A6WE 2001092800099 20010928 00099 WP 2001 9 28 MWEA011289 1 20010925 A 5311 59101633 FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 FRAME STATION 1338 HAS LIGHT CORROSION ON FORWARD SIDE ABOVE LEFT CUSP. FABRICATED AND INSTALLED -5 SPLICE AND -3 FRAME . 2 L 7 2 4F A6WE 2001092800100 20010928 00100 WP 2001 9 28 MWEA011290 1 20010925 A 5313 593666713 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 AFT CARGO COMPARTMENT LONGERON 30 HAS LIGHT CORROSION AND CORRODED FASTENERS AFT OF STATION 1231. FABRICATED LONGERON A ND SPLICE. 2 L 7 2 4F A6WE 2001092800101 20010928 00101 NM 2001 9 28 QXEA0101584 1 20010920 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - ACCESS 311AB FORWARD ABOUT 11 O'CLOCK FRAME NR 4 IS CRACKED. REPAIRED IAW RD 8-55-199. 2 H 7 2 4T RT A13NM 2001092800102 20010928 00102 NM 2001 9 28 QXEA0101585 1 20010920 A 5230 BRACKET DHAV DHC8 DHC8202 2809007 NM CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - CARGO DOOR TOP STOP BRACKETS HAVE BEEN STRIKING DOOR APERTURE STRUCTURE. REPAIRED IAW RD 8-53-5461, SECTION 1, PAG E 2 THROUGH 4. 2 H 7 2 4T RT A13NM 2001092800103 20010928 00103 WP 2001 9 28 MWEA011291 1 20010925 A 5320 995790554 CLIP DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 SHEAR CLIP AT STATION 769 HAS A DAMAGED HOLE BETWEEN LONGERON 26 RIGHT THROUGH 25 RIGHT. FABRICATED AND INSTALLED SHEAR CLIP AND REPAIR SPLICE SECTION. 2 L 7 2 4F A6WE 2001092800104 20010928 00104 WP 2001 9 28 MWEA011292 1 20010925 A 5310 993644817 SHEAR TIE DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 MID CARGO BAY SHEAR TIE AND FUSELAGE SKIN AT STATION 807 HAVE AREAS OF LIGHT CORROSION BETWEEN LONGERON 28 THROUGH LONGE RON 29 RIGHT. FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F A6WE 2001092800105 20010928 00105 WP 2001 9 28 MWEA011293 1 20010925 A 5320 99373875 STIFFENER DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 MID CARGO BAY BULKHEAD TEE STATION 826 HAS MODERATE CORROSION BETWEEN LONGERON 28 THROUGH LONGERON 29 RIGHT. FABRICATED AND INSTALLED TEE. 2 L 7 2 4F A6WE 2001092800106 20010928 00106 WP 2001 9 28 MWEA011294 1 20010925 A 5311 99364483 FRAME DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 REMOVED FORMER FROM FRAME ASSEMBLY STATION 807, LONGERON 26 LEFT THROUGH 26 RIGHT TO FACILITATE OTHER MAINTENANCE. FOUN D DAMAGE ON FORMER. FABRICATED AND INSTALLED FORMER. 2 L 7 2 4F A6WE 2001092800107 20010928 00107 NM 2001 9 28 UPS01236903 1 20010917 A 7830 0645301004059 BRACKET BOEING 727 72762C 138402C NM #3 T/R FAIRING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 912UP 19244 INSPECTION TYPE:C #3 THRUST REVERSER O/B LATCH FAIRING MID ANF AFT BRACKETS ARE CRACKE D. BRACKETS REPLACED IAW MM 7 8-30-01 2 L 7 3 4F A3WE 2001092800108 20010928 00108 NM 2001 9 28 UPS01236937 1 20010828 A 5330 NA WEB BOEING 727 72725C 138400H NM STA 277 R/SIDE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:C NOSE WHEEL WELL R/T AT STA 277 RIGHT SIDE WALL SHOW CRACK BETWEEN RIVET, CRACK ALREADY VERIFIED IAW P6 -51-00-00 FIG 2. REMOVED NOSE LANDING GEAR ACCESS PANEL #3125 RIGHT SIDE FOR REPAIR AS PER 727 SRM 51-30-02, CUT OUT DAMAGE AREA APPROX 2"X1" AND 4"X1" AT RIGHT SIDE WEB STA 274 AS PER B727 SRM 51-40-02. PERFORMED NDT INSP AFTER CUT OU T DAMAGE AREA, NO CRACK FOUND AS PER PART#6 51-00-0 0 FIG 4 INSTALLED DOUBLER REPAIR AT R/SIDE WEB IAW SRM 51-40-02. 2 L 7 3 4F A3WE 2001092800109 20010928 00109 NM 2001 9 28 UPS01236938 1 20010904 A 5330 NA SKIN BOEING 727 72725C 138400H NM STA 1080 S14R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:C FUSELAGE SKIN SHOW CRACK INDICATION BS 1080 STR 14R NDT FINDING MARKED RUNNING FORM FASTENER HOLE. VERIFICATION SKIN CRACK AT BS 1080 S14R IAW B727 NDT MANUAL PART 6 51-00-00 FIG 4, CUT OUT DAMAGE AREA AT BS 1080 STR 1 4R IAW B727 SRM 53-30-3 PERFORMED HFEC AROUND CUT OUT, FOUND NO CRACK NDT INSPECTION AS PER B727 PART 6 51-00-00 FIG 4. INSTALLED DOUBLER AND FILLER RE PAIR AT STA 1080 STR14 IAW SRM B727 53-30-3 FIG 14. 2 L 7 3 4F A3WE 2001092800110 20010928 00110 NM 2001 9 28 UPS01236939 1 20010824 A 5330 NA DOUBLER BOEING 727 72725C 138400H NM BS 1040-1080 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:C AFT CARGO CUT OUT UPER SILL INTERNAL DOUBLER, HAS CORROSION FROM BS 1080. REMOVED CORROSION, FOUNF OUT OF LIMITS AT STA 1040-1080 AS PER B727- SRM 51-10-6 CUT OUT DAMAGE AREA AS PER 53-10-01 UPPER SILL INTERNAL DOUBLER BS 1080 AS PER TELEX #B2-9430 BOEING DROWING #65-18385. TREATED, PRIMED AND INSTALED DOUBLER IAW B727-SRM 51-10-02. 2 L 7 3 4F A3WE 2001092800111 20010928 00111 NM 2001 9 28 UPS01236940 1 20010821 A 5330 NA SKIN BOEING 727 72725C 138400H NM BS1080-1130 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:C FUSELAGE SKIN BULGING AROUND FASTENERS ABOVE UPPER AFT CORNER OF AFT CARGO DOOR BS 1080 TO BS 1130 ST R 17R TO STR 20R. REMOVED AND REPLACED FUSELAGE SKIN FROM BS 1080 TO BS 1185 FORM STR 17R TO STR 20R AS PER BOEING D RAWING # 6518385 AND AVITA REPAIR ORDER AVHM 259120-1 AND UPS EO B727-5310-15416-A. 2 L 7 3 4F A3WE 2001092800112 20010928 00112 WP 2001 9 28 MWEA011295 1 20010925 A 5313 59365631 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 STATION 775 TO STATION 826 LONGERON 30 REQUIRES REMOVAL TO FACILITATE OTHER MAINTENANCE. FOUND CORROSION ON LONGERON. REMOVED AND REPLACED LONGERON. 2 L 7 2 4F A6WE 2001092800113 20010928 00113 WP 2001 9 28 MWEA011296 1 20010925 A 5313 59365642 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 LONGERON 29 RIGHT, STATION 826 THROUGH 798 END FITTING HAS TOOL MARKS AND CORROSION IN THE UPPER CENTER CHANNEL. REMOVE D CORROSION AND BLENDED TOOL MARKS. 2 L 7 2 4F A6WE 2001092800115 20010928 00115 WP 2001 9 28 MWEA011299 1 20010925 A 5320 56137301 SILL DOUG DC9 DC981 3022081 WP COCKPIT CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 CAPTAINS CLEAR VIEW WINDOW SILL HAS EXFOLIATION CORROSION AT LOWER AFT CORNER STATION 117. BLENDED AREA UNDER GUSSET FO R CORROSION. 2 L 7 2 4F A6WE 2001092800116 20010928 00116 WP 2001 9 28 MWEA011302 1 20010925 A 5311 94115195 FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 LIGHT CORROSION ON FUSELAGE FRAME FORMER AT STATION 207 BETWEEN LONGERON 8 AND 10 RIGHT. FABRICATED AND INSTALLED SHEAR CLIP. 2 L 7 2 4F A6WE 2001092800117 20010928 00117 WP 2001 9 28 MWEA011303 1 20010925 A 5313 591142923 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 MODERATE CORROSION ON LONGERON 24 LEFT FROM AFT PRESSURE BULKHEAD AFT TO STATION 1380. FABRICATED AND INSTALLED LONGERO N SECTION. 2 L 7 2 4F A6WE 2001092800118 20010928 00118 CE 2001 9 28 RK287 1 20010830 A 2720 ICC4008 COMPUTER BEECH MU300 400A 1155402 CE E/E BAY FAILED E ERYA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 07 361AS 446 RK287 RUDDER BOOST FAIL ON TAKEOFF ROLL. MASTER CAUTION FOLLOWED BY RUDDER BOOST FAIL ANNUNCIATOR. 2 H 7 2 4F RT A16SW 2001092800119 20010928 00119 WP 2001 9 28 SABA010019 2 20010602 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE331* 01514 WP LEFT POWER LOSS A SABA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 33 952AE 952 P66261 AIRCRAFT 952 ON FLIGHT 5045 AGS TO CLT. DURING TAKEOFF ROLL THE LEFT ENGINE EGT DROPPED AS IF THE ENGINE WAS BYPASSING FUEL. THE TAKEOFF WAS ABORTED. AIRCRAFT RETURNED TO THE GATE WITH NO OTHER PROBLEMS. NO EMERGENCY WAS DECLARED AND NO EMERGENCY PROCEDURES WERE USED. MAINTENANCE PERFORMED A GROUND RUN AND COULD NOT DUPLICATE THE PROBLEM. AIRCRAFT RETU RNED TO SERVICE. 2 L 7 2 4T 3 T RT A56EU E2WE 2001092800120 20010928 00120 NM 2001 9 28 SABA010022 1 20010613 A 3620 7506593 SWITCH DHAV DHC8 DHC8102 2809003 NM BLEED AIR FAULTY A SABA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 33 883CC 162 AIRCRAFT 883 ON FLIGHT 5222 CLT TO LEX. DURING TAKEOFF ROLL THE NUMBER ONE BLEED HOT LIGHT ILLUMINATED. TAKEOFF WAS AB ORTED. NO EMERGENCY WAS DECLARED AND NO EMERGENCY PROCEDURES WERE USED. AIRCRAFT RETURNED TO THE GATE WITH NO OTHER PR OBLEMS. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE BLEED OVERTEMP SWITCH. OPS CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001092800121 20010928 00121 WP 2001 9 28 ZW0A0108610 1 20010912 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 911TW 49182 DURING CHECK-C MAINT FOUND CORROSION ON NUMBER 3 CABIN FLOOR TRACK AT LBL 22 INCHES, STA 1096 TO 1309. REPLACED CHAIR T RACK PER SRM 53-05 AND DRAWING CO3580. INSTALLED SPLICE PER SRM 53-05, FIG 4F. 2 L 7 2 4F A6WE 2001092800122 20010928 00122 WP 2001 9 28 2001F00379 1 20010824 A 3350 AD4002P BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 815US 48095 IND - THE TAILCONE EMERGENCY LIGHT RECEIVER, SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS, AND THE CEILING EMERGENCY LIGHTS F OR SEAT ROWS 1 THROUGH 8 WERE INOPERATIVE. MAINTENANCE REPLACED THE TAILCONE EMERGENCY LIGHT REMOTE RECEIVER, AND THE L OW LEVEL AND CEILING EMERGENCY LIGHT BATTERIES. REF USAAD01153. (M) 2 L 7 2 4F A6WE 2001092800123 20010928 00123 EU 2001 9 28 2001F00382 1 20010907 A 5553 22201BC060016L BOLT SNIAS 350 AS350B2 8680813 EU VERTICAL STAB SHEARED A KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 115SH 2985 3141 RIGHT SIDE UPPER FORWARD VERTICAL ATTACHMENT BOLT SHEARED OFF. INSTALLED NEW BOLT. (M) 1 G 7 1 3U H9EU 2001092800124 20010928 00124 EU 2001 9 28 2001F00383 1 20010907 A 7920 1742510 FILTER SNIAS 350 AS350B2 8680813 EU ENGINE DEFECTIVE A KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 115SH 3141 OIL FILTER HAS A WEAK MAGNET, SHOWS BYPASS CONDITION WHEN NOT IN BYPASS. INSTALLED A NEW OIL FILTER. (M) 1 G 7 1 3U H9EU 2001092800125 20010928 00125 EU 2001 9 28 2001F00385 1 20010903 A 2435 150SG1229 BRUSHES SNIAS 350 AS350BA 8680817 EU STARTER GEN WORN A KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 270SH 378 1864 STARTER/GENERATOR BRUSHES WORN. INSTALLED SERVICEABLE STARTER. (M) 1 G 7 1 3U NC H9EU 2001092800126 20010928 00126 2001 9 28 2001F00388 4 20010809 A 3120 AT420000 CLOCK SNIAS 350 AS350B2 8680813 EU COCKPIT INTERMITTENT A KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 313LV 3296 CLOCK KEPT INTERMITTENT TIME. INSTALLED SERVICEABLE CLOCK. (M) 1 G 7 1 3U H9EU 2001092800127 20010928 00127 WP 2001 9 28 2001F00389 1 20010903 A 3350 9721050 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 819US 48099 IND - THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS, LEFT AND RIGHT AFT OVERWING EXIT EMERGENCY LIGHTS, AND THE AFT FUSELA GE REMOTE RECEIVER WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES AND THE REMOTE RECEIVER. REF U SAAD01158. (M) 2 L 7 2 4F A6WE 2001092800128 20010928 00128 WP 2001 9 28 2001F00390 1 20010903 A 3350 873100191 RECEIVER DOUG DC9 DC981 3022081 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 819US 48099 IND - THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS, LEFT AND RIGHT AFT OVERWING EXIT EMERGENCY LIGHTS, AND THE AFT FUSELA GE REMOTE RECEIVER WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES AND THE REMOTE RECEIVER. REF U SAAD01158. (M) 2 L 7 2 4F A6WE 2001092800129 20010928 00129 NM 2001 9 28 2001F00391 1 20010805 A 5311 6519886220 FRAME BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 357QS 19259 RIGHT NOSE WHEEL WELL, MID CHORD EXFOLIATED AT INTERSECTION OF RIGHT WEB AND FLOOR WEB AS VIEWED FROM DOG HOUSE. ACCOMP LISHED RIGHT NOSE WHEEL WELL MID CHORD REPLACEMENT IAW B727 SRM 51-30-2 AND 51-20-4. (M) 2 L 7 3 4F A3WE 2001092800130 20010928 00130 NM 2001 9 28 2001F00392 1 20010712 A 5311 FRAME BOEING 727 72721 1384003 NM FUSELAGE DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 355QS 19257 LEFT CABIN FRAME BS 380 HAS DENT AT INBOARD FLANGE JUST ABOVE FLOOR. INSTALLED DOUBLER REPAIR AT LEFT CABIN FRAME BS 38 0 INBOARD FLANGE JUST ABOVE FLOOR IAW WITH SRM 51-40-3. (M) 2 L 7 3 4F A3WE 2001092800131 20010928 00131 NM 2001 9 28 2001F00393 1 20010603 A 5310 STRUCTURE BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 355QS 19257 FOUND COCKPIT BS 259 BETWEEN STRINGER 6L AND 7L HAS WHITE POWER AROUND DOUBLER EDGE. INSTALLED DOUBLER REPAIR IAW B727 SB 727-53-0084 AND DRAWING NR 69-62161 AT BS 259 BTW STRINGER 6L AND 7L BTW STRINGER 6L AND 7L. (M) 2 L 7 3 4F A3WE 2001092800132 20010928 00132 NM 2001 9 28 2001F00395 1 20010603 A 5230 FRAME BOEING 727 72721 1384003 NM CARGO DOOR CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 355QS 19257 MAIN CARGO DOOR UPPER FRAME LOWER CHORD BS 581 SHOWS CRACK AT FRAME END, VIEW FROM LIGHTING HOLE. INSTALLED ANGLE REPAI R AT MAIN CARGO DOOR FRAME LOWER CHORD BS 584 IAW AVBORNE DWG N355QS-2 AND SIE 8110-3. (M) 2 L 7 3 4F A3WE 2001092800133 20010928 00133 SO 2001 9 28 2001F00396 1 20010906 A 5711 SPAR PIPER PA31T PA31T1 7103126 SO RT WING CRACKED B BUER K NONE O OTHER IN INSP/MAINT 1 GL 23 398SP 31T8104027 WHILE PERFORMING THE MANUFACTURERS EVENT 1 INSPECTION, A CRACK WAS DISCOVERED IN THE RIGHT WING MAIN SPAR 9FS 137) JUST INBOARD OF WING STATION 87.50. THE CRACK WAS APPROXIMATELY .875 INCH LONG AND EXTENDS FROM THE CENTER OF THE SPAR AFT T HROUGH A RIVET HOLE. (M) 1 L 7 2 3T A8EA 2001092800134 20010928 00134 WP 2001 9 28 2001F00375 1 20010824 A 3350 873100191 RECEIVER DOUG DC9 DC982 3022082 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 815US 48095 IND - THE TAILCONE EMERGENCY LIGHT RECEIVER, SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS, AND THE CEILING EMERGENCY LIGHTS F OR SEAT ROWS 1 THROUGH 8 WERE INOPERATIVE. MAINTENANCE REPLACED THE TAILCONE EMERGENCY LIGHT REMOTE RECEIVER, AND THE L OW LEVEL AND CEILING EMERGENCY LIGHT BATTERIES. REF USAAD01153. (M) 2 L 7 2 4F A6WE 2001092800135 20010928 00135 NM 2001 9 28 2001F00377 1 20010910 A 3350 10005511 LIGHT DHAV DHC8 DHC8103 1386005 NM COCKPIT INOPERATIVE A IQJA K NONE L NO TEST IN INSP/MAINT 1 NM 01 808WP 182 026 HNL - FLIGHT COMPARTMENT PORTABLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED PORTABLE EMERGENCY LIGHT ASSEMBLY, OPERATIONAL CHECK OF SYSTEM COMPLIED WITH, AND CHECKED GOOD. (M) 2 H 7 2 4T RT A13NM 2001092800136 20010928 00136 2001 9 28 2001F00378 4 20010908 A 3421 5040017901 GYRO SNIAS 350 AS350BA 8680817 EU COCKPIT FAULTY A KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 2273A 2273 ART HORIZON INDICATING A TURN OR DIVE IN STRAIGHT AND LEVEL FLIGHT THREE MINUTES AFTER BEING CAGED. INSTALLED OVERHAULE D ATTITUDE GYRO. (M) 1 G 7 1 3U NC H9EU 2001092800137 20010928 00137 NM 2001 9 28 AALA20011559 1 20010803 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN LOOSE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 634AA 24592 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING WIRE AT SEAT 23D IS PULLED LOOSE. REPLACED SEAT MOUNTED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001092800138 20010928 00138 NM 2001 9 28 AALA20011570 1 20010804 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN MALFUNCTIONED A AALA K NONE O OTHER CR CRUISE 1 SW 21 772AN 29580 ORD - FLT 47 - EN ROUTE LHR-ORD, EMEREGNCY EXIT LIGHTS ILLUMINATED FOR 2 MINUTES IN FLIGHT 2 HOURS AND 35 MINUTES AFTER TAKEOFF. COULD NOT DUPLICATE FAULT. NO PREVIOUS HISTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001092800139 20010928 00139 WP 2001 9 28 AALA20011635 1 20010807 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 435AA 49453 TUL - FOUND CORROSION ON RIGHT CUSP STATION 558. INSTALLED REPAIR DOUBLER PER SRM 53-01 FIG 4. (M) 2 L 7 2 4F RT A6WE 2001092900001 20010929 00001 NM 2001 9 29 PCAA0109115 1 20010923 A 3230 CO3600491750S ACTUATOR DHAV DHC8 DHC8102 2809003 NM LEFT BROKEN A PCAA K NONE S AFFECT SYSTEMS IN INSP/MAINT 1 EA 13 830EX 155 DURING A CHECK INSPECTION LEFT UPLOCK ACTUATOR INBOARD SPRING FOUND BROKEN. BROKEN SPRING REPLACED IN ACCORDANCE WITH DO WTY COMPONENT MAINTENANCE MANUAL 32-30-21. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001093000001 20010930 00001 NE 2001 9 30 RAIA00109010 2 20010925 A 7200 TPE33114 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE FOD A RAIA O OTHER C F.O.D. DE DESCENT 1 CE 03 566HK 11660 2849 41084 76100 7200-STL-BIRD STRIKE LEFT ENGINE. MAINTENANCE REMOVED AND REPLACED LEFT HAND ENGINE 2 L 7 2 4T 4 T RT A41NM E18NE 2001100100001 20011001 00001 NM 2001 10 1 QXEA0101586 1 20010917 A 5230 STOP DHAV DHC8 DHC8202 2809007 NM CARGO DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - CARGO DOOR PRESSURE STOP LANDING HAVE LIGHT FRETTING PITTING IN CENTER. REPAIRED IAW RD 8-53-104. 2 H 7 2 4T RT A13NM 2001100100002 20011001 00002 NM 2001 10 1 QXEA0101587 1 20010919 A 5753 ROLLER DHAV DHC8 DHC8202 2809007 NM FLAP TRACK CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - NR 4 UPPER DEAD WEIGHT ROLLER HAS PITTED FLAP TRACK ON UPPER HORIZONTAL TRACK. REPAIRED IAW DHC-8 MM 27-51-11. 2 H 7 2 4T RT A13NM 2001100100003 20011001 00003 NM 2001 10 1 QXEA0101588 1 20010920 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM TE FLAPS CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - RIGHT-HAND FLAP TRACK NR 4 HAS PITTING ON BOTH SIDES OF TRACK. REPAIRED IAW HORIZON AIR EA 2-57-138. 2 H 7 2 4T RT A13NM 2001100100004 20011001 00004 NM 2001 10 1 QXEA0101589 1 20010920 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE MISINSTALLED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 352PH 494 PDX - RIGHT-HAND FORWARD OUTBOARD SEAT TRACK FROM STATION 262.40 TO 420.00 HAS TEN HILOCK TO LONG ON GAUGE. REPAIRED IAW DHC-8 SRM 51-40-00, PAGE 4, TABLE 4. 2 H 7 2 4T RT A13NM 2001100100005 20011001 00005 EU 2001 10 1 QXEA0101590 1 20010922 A 3350 5515800106 LIGHT FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 491US 11156 BOI - EMERGENCY EXIT LIGHT PANEL ABOVE ROW 8 IS INOPERABLE. REMOVED AND REPLACED EXIT LIGHT PANEL. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001100100006 20011001 00006 EA 2001 10 1 QXEA0101591 1 20010925 A 5210 SEAL CNDAIR CL600 CL6002A12 1900304 EA PAX DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 606QX 10023 PDX - MAIN CABIN DOOR SEAL MATING SURFACE IS DENTED MIDWAY ALONG THE FORWARD LENGTH OF DOOR APERATURE. REPAIRED IAW EA R -53-03. 2 L 7 2 4F RT A21EA 2001100100007 20011001 00007 EA 2001 10 1 QXEA0101592 1 20010925 A 5300 SEAL CNDAIR CL600 CL600* EA PAX DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 606QX 10023 PDX - MAIN CABIN DOOR SEAL MATING SURFACE DENTED MIDWAY ALONG THE AFT LENGH OF DOOR APERTURE. REPAIRED IAW EA R-53-03 2 L 7 2 4F RT A21EA 2001100100008 20011001 00008 EU 2001 10 1 QXEA0101593 1 20010923 A 3350 6008903 POWER SUPPLY FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 496US 11169 BOI - EMERGENCY LIGHTING ON SEATS 1B,2B,3B, AND 4B ARE INOPERABLE. REPLACED BATTERY PACK UNDER SEAT 1A. OPERATIONAL CHEC K IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001100100009 20011001 00009 EU 2001 10 1 QXEA0101594 1 20010927 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 492US 11159 PDX - BOTH CENTER EMERGENCY EXIT SIGNS HAVE NUMEROUS BULBS BURNED OUT. REMOVED AND REPLACED EXIT SIGNS. OPERATIONAL CHEC K IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001100100010 20011001 00010 EA 2001 10 1 QXEA0101595 1 20010924 A 5210 SEAL CNDAIR CL600 CL600* EA PAX DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX - MAIN CABIN DOOR MATING FACE IS DENTED MIDWAY ALONG THE FORWARD LENGTH. REPAIRED IAW EA-53-02. 2 L 7 2 4F RT A21EA 2001100100011 20011001 00011 EA 2001 10 1 QXEA0101596 1 20010925 A 5300 SEAL CNDAIR CL600 CL600* EA PAX DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX - MAIN CABIN DOOR MATING FACE IS DENTED MIDWAY ALONG THE AFT LENGTH OF DOOR APERATURE. REPAIRED IAW EA R-53-02 2 L 7 2 4F RT A21EA 2001100100012 20011001 00012 SO 2001 10 1 145450 1 20010727 A 3610 54722250 CLAMP EMB 135 EMB135ER 3260203 SO ALLSN AE300 AE3007A GL BLEED AIR SYS LOOSE E CWQA K NONE O OTHER IN INSP/MAINT 1 GL 05 948AL 145450 DURING ACCEPTANCE INSPECTION IT WAS NOTED THAT THE V-BAND CLAMPS ON THE BLEED AIR CHECK VALVE WERE LOOSE DURING PHYSICAL CHECK OF THE CLAMP. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001100100013 20011001 00013 SO 2001 10 1 145450A 1 20010727 A 3610 54722250 CLAMP EMB 135 EMB135ER 3260203 SO ALLSN AE300 AE3007A GL BLEED AIR SYS LOOSE E CWQA K NONE O OTHER IN INSP/MAINT 1 GL 05 829RN 145360 DURING ACCEPTANCE INSPECTION IT WAS NOTED THAT THE V-BAND CLAMPS ON THE BLEED AIR CHECK VALVE WERE LOOSE DURING PHYSICAL CHECK OF THE CLAMP. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001100100014 20011001 00014 EU 2001 10 1 2001F00374 1 20010615 A 6321 704A34130044 SLEEVE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE ROTOR BRAKE FROZEN E LV6A K NONE O OTHER IN INSP/MAINT 1 WP 19 313LV 447 3296 ROTOR BRAKE CABLE IS FROZEN. CANNOT ACTUATE CABLE, SUSPECT SILICA SAND BUILD UP FROM FORWARD END. MFG DOES NOT INSTALL BRASS END CAP ON THE CABLE END WHICH IS INSTALLED UNDER BELLY PANS. 1 G 7 1 3U 3 U H9EU E19EU 2001100100021 20011001 00021 EU 2001 10 1 2001F00381 1 20010907 A 2433 CONVERTER SNIAS 350 AS350B2 8680813 EU CD PLAYER FAILED A KBMA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 19 115SH 3141 BURNING SMELL NOTED FOLLOWED BY BOTH CD PLAYERS LOSING POWER. AFTER LOSS OF POWER NO BURNING SMELL NOTED. INSTALLED SE RVICEABLE AC TO DC POWER CONVERTER FOR CD PLAYERS. (M) 1 G 7 1 3U H9EU 2001100100022 20011001 00022 EU 2001 10 1 2001F00384 1 20010903 A 2400 371GC01Y021 ELECTRICAL BOX SNIAS 350 AS350BA 8680817 EU ELECTRICAL SYS FAILED A KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 270SH 1864 GENERATOR WILL NOT COME ON LINE, NO POWER TO PIN 10 K2 RELAY. INSTALLED NEW ECE BOX. (M) 1 G 7 1 3U NC H9EU 2001100100023 20011001 00023 EU 2001 10 1 2001F00386 1 20010809 A 6520 350A33215321 BEARING SNIAS 350 AS350B2 8680813 EU TAIL ROTOR WORN A KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 313LV 3296 T/R LAMINATED TEETER BEARINGS WORN. REPLACED WITH NEW BEARINGS. (M) 1 G 7 1 3U H9EU 2001100100024 20011001 00024 EU 2001 10 1 2001F00387 1 20010809 A 6410 355A09103601 BEARING SNIAS 350 AS350B2 8680813 EU TAIL ROTOR WORN A KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 313LV 3296 T/R LAMINATED FLAPPING BEARINGS WORN. REPLACED WITH NEW BEARINGS. (M) 1 G 7 1 3U H9EU 2001100100025 20011001 00025 NM 2001 10 1 2001F00394 1 20010603 A 5310 STRUCTURE BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 355QS 19257 SNOW WHITE POWDER AND CORROSION AT BS 481 FROM STRINGER 4L TO 4R. REPAIRED BS 481 FROM STRINGER 4L AND 4R IAW AVBORNE DW G NR 355QS AND SIE 8110-3. (M) 2 L 7 3 4F A3WE 2001100100026 20011001 00026 2001 10 1 AALA20011615 4 20010813 A 3460 COMPUTER BOEING 767 767223 1385123 NM COCKPIT FAULTY A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 321AA 22322 JFK - FLT 52 - NO CAPTAIN FLT DIR, NO AIRSPEED SALMON BUG ON LEFT AUTO PILOT. ACCOMPLISHED MCDP FAUCT FLIGHT REVIEW FAU LTED LFCC COMPUTER REPLACED L FCC COMPUTER ACCOMPLISHED ALL REQUIRED TESTS PER MM ALSO ACCOMPLISHED LAND TEST 40 AN CKS NORMAL PER MM. (M) 2 L 7 2 4F RT A1NM 2001100100027 20011001 00027 WP 2001 10 1 AALA20011637 1 20010807 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 435AA 49453 TUL - FOUND CRACK IN FUSELAGE SKIN STATION 1383 AT FAST ABOVE LONGERON 14L. STOP DRILLED CRACKED INSTALLED DOUBLER REPA IR PER AARD 53-30-00-02. (M) 2 L 7 2 4F RT A6WE 2001100100028 20011001 00028 WP 2001 10 1 AALA20011638 1 20010808 A 5310 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 435AA 49453 TUL - FOUND MID CARGO DOOR CUTOUT LOWER BEAM CORRODED STATION 636-693. REMOVED CORROSION, INSTALLED 2 ANGLE DOUBLER PER AARD 53-10-00-3 FIG 2 PAGE 18. (M) 2 L 7 2 4F RT A6WE 2001100100029 20011001 00029 WP 2001 10 1 AALA20011643 1 20010813 A 5310 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 435AA 49453 TUL - FOUND DOUBLER IN FORWARD CARGO DOOR CUTOUT AT LOWER FORWARD CORNER NOT PER SRM. REMOVED OLD DOUBLER. INSTALLED D OUBLER PER ESO 80559 DATED 8-13-01. (M) 2 L 7 2 4F RT A6WE 2001100100030 20011001 00030 NM 2001 10 1 AALA20011707 1 20010829 A 3350 60030451 BATTERY PACK BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 361AA 24042 ORD - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT AT ROWS 18 THROUGH 21 INOPERATIVE. REPLACED BATTERY P ACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001100100031 20011001 00031 2001 10 1 GTIA010835 4 20010826 A 2210 PIN DOUG DC9 DC982 3022082 WP AUTOPILOT SYS GROUNDED A GTIA O OTHER O OTHER CL CLIMB 1 GL 23 817NK 49141 DTW - FLT 520 - CAN NOT SELECT MACH FOR CLIMB/DESCENT. FOUND BURNITY PIN AT STATION 110 GROUNDED TO ACTIVATE MACH HOLD ON COMP IAW MM 22-10-00. NO DEFECTS NOTED. (M) 2 L 7 2 4F A6WE 2001100100032 20011001 00032 WP 2001 10 1 GTIA010849 1 20010904 A 3350 60030431 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FLL - FOUND FORWARD BATTERY POWER SUPPLY INOPERATIVE, REQUIRES REMOVED AND REPLACED WITH NO POWER ON A/C FORWARD OVERHEA D LIGHTS CAME ON. REMOVED AND REPLACED BATTERY AND POWER PACK TO FORWARD OVERHEAD EMERGENCY LIGHTS IAW 33-53-00. (M) 2 L 7 2 4F A6WE 2001100100033 20011001 00033 WP 2001 10 1 GTIA010851 1 20010904 A 2751 TERMINAL DOUG DC9 DC982 3022082 WP COCKPIT LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 823NK 48020 DTW - WHILE CHECK TAKEOFF WARNING SYSTEM. UNABLE TO GET A FLAP WARNING. ALL OTHER WARNINGS OK. FOUND LOOSE TERMINAL O N FLAP SWITCH IN PEDESTAL, RESECURED IAW MM 20-00-00. NO DEFECTS NOTED. (M) 2 L 7 2 4F A6WE 2001100100034 20011001 00034 WP 2001 10 1 GTIA010853 1 20010906 A 3350 60117799 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 823NK 48020 FLL - THE EXTERIOR EMERGENCY LIGHTS ASSEMBLIES ILLUMINATED WHEN EMERGENCY LIGHT SWITCH IS PLACED FROM ARM TO OFF. REMOV ED AND REPLACED BATTERY POWER SUPPLY ASSEMBLY. OPS CHECKED IAW MD 80 MM 33-53-00 NORMAL. (M) 2 L 7 2 4F A6WE 2001100100035 20011001 00035 WP 2001 10 1 GTIA010854 1 20010901 A 2611 SMOKE DETECTOR DOUG DC9 DC982 3022082 WP LAVATORY INTERMITTENT A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 823NK 48020 FLL - RIGHT AFT LAV SMOKE ALARM OPERATES INTERMITTENTLY. MUST GO TO L2 DOOR (CEILING) TO CANCEL HORN AND LIGHT. REMOVE D AND REPLACED RIGHT AFT SMOKE DETECTOR IAW 25-31-08. (M) 2 L 7 2 4F A6WE 2001100100037 20011001 00037 NE 2001 10 1 GTIA010864 2 20010905 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE NR 2 LEAKING A GTIA H DEACTIVATE SYST/CIRCUITS K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 823NK 48020 DTW - FLT 1691 - F/A'S REPORTED SMOKE IN CABIN, FOLLOWED QRH, LANDED AT 128,000 NR TURNED OFF L PACK. SMOKE PERSISTED. TURNED LEFT AND RETURNED OFF LATER TURNED OFF NI SMOKE. FOUND OIL IN 13TH STAGE DUCT REPLACED NR 2 ENGINE. (M) 2 L 7 2 4F 4 F A6WE E2EA 2001100100040 20011001 00040 WP 2001 10 1 GTIA010866 1 20010910 A 5753 FLAP DOUG DC9 DC981 3022081 WP LT WING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 DTW - LEFT TRAILING EDGE DAMAGED BETWEEN TABS. REPAIRED CRACK ON TRAILING EDGE IAW MD80 SRM 51-70-1A MATERIAL REMOVED . 03 OUNCES. REPLACED .01 FIBERGLASS .01 RESIN, .01 PAINT MATERIAL REMOVED IS EQUAL TO MATERIAL REPLACED. NO CHANGE IN W EIGHT TOTAL WEIGHT 255.86. (M) 2 L 7 2 4F A6WE 2001100100041 20011001 00041 WP 2001 10 1 HALA0100222 1 20010902 A 3222 VALVE DOUG DC9 DC951 3022051 WP NLG STRUT LEAKING A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 699HA 47763 ATB - NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. NOSE GAR UNSAFE LIGHT ILLUMINATED, NOSE GEAR GREEN LIGHT ILLUMINATED R ECYCLED GEAR WITH NO CHANGE. RETURNED TO OGG-LANDING NORMAL. FOUND NOSE STRUT UNDER SERVICED. SERVICED PER MM 32-21-2 METHOD 'B'. REPLACED SHRADER VALVE AND PACKING, GEAR SWING, OPS CHECK, LEAK CHECK GOOD. AIRCRAFT FERRIED TO HNL. (M) 2 L 7 2 4F RT A6WE 2001100100042 20011001 00042 WP 2001 10 1 HALA0100223 1 20010902 A 2910 HYDRAULIC LINE DOUG DC10 DC1010 3022110 WP HYD CASE DRAIN CRACKED A HALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 13 132AA 47827 ATB - DURING CLIMB-OUT AFTER DEPARTING LAX, HYD SYSTEM NR 3 ELEV OFF LIGHT ILLUMINATED WITH RAPID LOSS OF NR 3 HYDRAULIC FLUID FLUID. DUMPED FUEL AND RETURNED TO LAX FOR LANDING. ACCOMPLISHED APPROPRIATE ABNORMAL CHECK LIST AND ALTERNATE GEAR EXTENSION. FOUND NR 3 HYD CASE DRAIN LINE ON RIGHT SIDE CRACKED. WAITING FOR NEW LINE. (M) 2 L 7 3 4F A22WE 2001100100043 20011001 00043 NM 2001 10 1 USAABB01086 1 20010823 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 620AU 27199 BWI - FOUND THE LIGHT ASSEMBLY AT ROW 1 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2001100100044 20011001 00044 NM 2001 10 1 USAABB01090 1 20010831 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 609AU 22205 CLT - FOUND THE FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE AT ROWS 1, 4, 9, 18, 23, 26 AND 29. MAINTENANCE REPLACED THE A SSOCIATED BATTERIES. (M) 2 L 7 2 4F RT A2NM 2001100100045 20011001 00045 NM 2001 10 1 USAABB01092 1 20010904 A 3350 873100151REV12 LIGHT BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 609AU 22205 CLT - FOUND LOW LEVEL EMERGENCY LIGHT AT ROW 4 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001100100046 20011001 00046 NM 2001 10 1 USAABB01093 1 20010905 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 615AU 27146 BDL - FOUND LOW LEVEL EMERGENCY LIGHT AT ROW 6 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001100100047 20011001 00047 NM 2001 10 1 USAABB01094 1 20010906 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 625VJ 27246 BDL - FOUND LOW LEVEL EMERGENCY LIGHTS AT ROWS 4 AND 13 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLIES. (M) 2 L 7 2 4F RT A2NM 2001100100048 20011001 00048 NM 2001 10 1 USAASB01232 1 20010816 A 3350 1000679 LIGHT BOEING 737 737201 1384454 NM COCKPIT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 244US 22752 ALB - PILOT REPORTED THAT THE COCKPIT EVACUATION LIGHT WOULD NOT ILLUMINATE WITH COCKPIT SWITCH IN THE ON POSITION. MAI NTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 2001100100049 20011001 00049 NM 2001 10 1 USAASB01233 1 20010815 A 3350 1000679 LIGHT BOEING 737 737201 1384454 NM ENTRY DOOR NOT SEATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 22757 BWI - PILOT REPORTED THE THE EMERGENCY EXIT LIGHT AT THE FORWARD ENTRY DOOR WAS ILLUMINATED. MAINTENANCE RESEATED THE L IGHT ASSEMBLY. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A16WE 2001100100050 20011001 00050 NM 2001 10 1 USAASB01247 1 20010905 A 3350 SOCKET BOEING 737 7372B7 1384560 NM CABIN DAMAGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 279AU 22891 BWI - THE LEFT AFT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT REFLECTOR AN D LAMP SOCKET ASSEMBLY. (M) 2 L 7 2 4F A16WE 2001100100051 20011001 00051 WP 2001 10 1 DHL2001805020 1 20010926 A 2710 AILERON DOUG DC8 DC873F 302199F WP WING MALFUNCTIONED A DHLA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 01 805DH 46125 AILERON TRIM FROZEN DURING FLIGHT. INSPECTED AND OPERATED AILERON TRIM, NO DEFECTS NOTED IAW DC-8 MM 27-13-0. 2 L 7 4 4F RT 4A25 2001100100053 20011001 00053 NM 2001 10 1 SABA010020 1 20010610 A 3231 LINKAGE DHAV DHC8 DHC8102 2809003 NM LT MLG DOOR OUT OF ADJ A SABA K NONE J WARNING INDICATION CR CRUISE 1 SO 33 883CC 162 AIRCRAFT 883 ON FLIGHT 5054 FROM CLT TO PGV. DURING CRUISE THE LEFT FORWARD MAIN GEAR DOOR SHOWED NOT RETRACTED. AIRCR AFT CONTINUED FLIGHT TO PGV AND LANDED WITH NO OTHER PROBLEMS. NO EMERGENCY WAS DECLARED AND NO EMERGENCY PROCEDURES WE RE USED. AIRCRAFT WAS FERRIED TO CLT GEAR DOWN FOR MAINTENANCE. MAINTENANCE ADJUSTED THE LEFT FORWARD MAIN GEAR DOOR L INKAGE. OPS CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001100100058 20011001 00058 NM 2001 10 1 SABA010021 1 20010610 A 3231 54C546247 SEQUENCE VALVE DHAV DHC8 DHC8102 2809003 NM RT MLG WW LEAKING A SABA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 841PH 82 AIRCRAFT 841 ON FLIGHT 5157 CVG TO CLT. AFTER TAKEOFF THE RIGHT SYSTEM FAILED WITH A NR 2 ISOLATION LIGHT ILLUMINATED. ALSO THE RIGHT MAIN GEAR DOOR FAILED TO CLOSE. LANDING GEAR WAS EXTENDED AND AIRCRAFT RETURNED TO CVG AND LANDED WITH NO OTHER PROBLEMS. NO INFLIGHT EMERGENCY WAS DECLARED AND NO EMERGENCY PROCEDURES WERE USED. MAINTENANCE REMOVED AND R EPLACED THE RIGHT GEAR DOOR SEQUENCING VALVE AND SERVICED THE RIGHT HYDRAULIC SYSTEM. SYSTEM LEAK AND OPS CHECK WERE GO OD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001100100060 20011001 00060 WP 2001 10 1 SABA010024 2 20010614 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE331* 01514 WP RIGHT MALFUNCTIONED A SABA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 33 961AE 961 P66314C AIRCRAFT 961 ON FLIGHT 5200 RDU TO CLT. DURING TAKEOFF ROLL THE RIGHT SHOWED 80 PERCENT TORQUE. TAKEOFF WAS ABORTED AN D AIRCRAFT RETURNED TO THE GATE WITH NO OTHER PROBLEMS. MAINTENANCE PERFORMED A GROUND RUN. THE ENGINE SHOWED 100 PERC ENT TORQUE. ALL SYSTEMS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 3 T RT A56EU E2WE 2001100100061 20011001 00061 NE 2001 10 1 ALG2001F00024 1 20010617 A 6220 7610608004102 ROD END SKRSKY SKRSKY S76 S76 8143010 NE M/R DAMPER CRACKED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 705AL 1832 A06101802 760267 DURING FIELD INSPECTION, FOUND ROD END CRACKED AT BARREL NUT SEAT. 1 G 7 2 3U H1NE 2001100100062 20011001 00062 EU 2001 10 1 SABA010025 1 20010613 A 7722 COMPENSATOR BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE331* 01514 WP RT ENGINE OUT OF ADJ A SABA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 33 961AE 961 P066314C AIRCRAFT 961 ON FLIGHT 7178 FROM CLT TO SOP. DURING TAKEOFF ROLL THE RIGHT ENGINE TORQUE WAS 80 PERCENT. TAKEOFF WAS A BORTED. AIRCRAFT RETURNED TO THE GATE WITH NO OTHER PROBLEMS. NO EMERGENCY WAS DECLARED AND NO EMERGENCY PROCEDURES WE RE USED. MAINTENANCE ADJUSTED THE RIGHT ENGINE EGT COMPENSATOR. GROUND RUN WAS PERFORMED. ALL SYSTEMS OPS CHECKED NOR MAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 3 T RT A56EU E2WE 2001100100064 20011001 00064 CE 2001 10 1 B4O2001F00001 1 20010813 A 2810 SEALANT CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO WING TANK DETERIORATED A B4OA K NONE O OTHER IN INSP/MAINT 1 WP 07 500NE 402C0808 WING TANK SEALANT DETERIORATION. 1 L 7 2 3O 3 O A7CE E8CE 2001100100065 20011001 00065 SW 2001 10 1 BH1R708876 1 20010125 A 6420 406012102109 YOKE BELL 407 407 SW ALLSN 250C 250C47B GL TAIL ROTOR OUT OF TOLERANCE B BH1R K NONE O OTHER IN INSP/MAINT 1 SW 19 407LR 1854 53279 DURING FIRST OVERHAUL OF TAIL ROTOR HUB, YOKE ASSEMBLY WAS FOUND TO HAVE BOTHE INBOARD BEARING RACES WORN OUT OF LIMITS. REMOVED AND REPLACED YOKE. 1 G 7 1 3U 3 U O H2SW E1GL 2001100100066 20011001 00066 NE 2001 10 1 SABA010027 2 20010628 A 7260 TOWERSHAFT DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RT ENGINE FAILED A SABA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 SO 33 841PH 082 121097 ACFT 841 ON FLIGHT 5028 FROM TLH TO CLT. DURING CLIMBOUT FROM TLH THE RIGHT ENGINE SHUTDOWN. AN INFLIGHT EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO TLH AND LANDED WITH NO FURTHER PROBLEMS. MAINTENANCE FROM CLT SENT TO TLH TO REMOV E AND REPLACE RIGHT ENGINE. THIS REPORT TO BE SUPPLEMENTED WHEN ENGINE TEARDOWN REPORT IS AVAILABLE. SUPPLEMENTAL INFO RMATION: VENDOR REPORTED THE TOWER SHAFT FAILED CAUSING FAILURE OF DRIVE TO THE FUEL CONTROL UNIT. 2 H 7 2 4T 4 T RT A13NM E20NE 2001100100067 20011001 00067 SO 2001 10 1 BTVR194756 1 20010608 A 5320 1159B31267 CLIP GULSTM GULSTM G1159 G1159A 3970109 SO RROYCE SPEY SPEY5118 54523 EU ANTENNA ATTACH CRACKED B BTVR K NONE O OTHER IN INSP/MAINT 1 GL 23 599DA 7324 445 VHF ANTENNA WAS FOUND LOOSE ON THE LOWER FUSELAGE FAIRING, JUST FWD OF THE WING. AFTER DISASSEMBLY, IT WAS DETERMINED T HAT THE ANTENNA ATTACHMENT STRUCTURE TO THE FUSELAGE WAS CRACKED IN SEVERAL AREAS. FATIGUE/ VIBRATION MAY HAVE BEEN THE CAUSE. 2 L 7 2 4F 4 F A12EA E2EU 2001100100068 20011001 00068 NM 2001 10 1 COOSDR010120 1 20010816 A 5330 DOUBLER BOEING 737 737230 NM PWA JT8 JT8D15 52051 NE FUSELAGE DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 737TW 20257 LOWER NOSE COMPARTMENT, BONDED DOUBLER WITH DELAMINATION, FROM BS 241 TO BS 247, BETWEEN RBL 17 AND RBL 20. 2 L 7 2 4F 4 F RT A16WE E2EA 2001100100070 20011001 00070 NM 2001 10 1 COOSDR010122 1 20010816 A 5330 DOUBLER BOEING 737 737230 NM PWA JT8 JT8D15 52051 NE FUSELAGE DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 737TW 20257 CARGO CABIN BONDED DOUBLER WITH DELAMINATION, FROM BS 995 TO BS 1006 AND BETWEEN STR 8L AND STR 10L. 2 L 7 2 4F 4 F RT A16WE E2EA 2001100100071 20011001 00071 NM 2001 10 1 COOSDR010123 1 20010816 A 5330 DOUBLER BOEING 737 737230 NM PWA JT8 JT8D15 52051 NE FUSELAGE DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 737TW 20257 CARGO CABIN BONDED DOUBLER WITH DELAMINATION, FROM BS 927 TO BS 947 AND BETWEEN STR 14L AND STR 15L. 2 L 7 2 4F 4 F RT A16WE E2EA 2001100100072 20011001 00072 NM 2001 10 1 COOSDR010124 1 20010816 A 5330 DOUBLER BOEING 737 737230 NM PWA JT8 JT8D15 52051 NE FUSELAGE DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 737TW 20257 CARGO CABIN BONDED DOUBLER WITH DELAMINATION, FROM BS 500 TO BS 500A AND BETWEEN STR 3L AND STR 6L. 2 L 7 2 4F 4 F RT A16WE E2EA 2001100100073 20011001 00073 NM 2001 10 1 COOSDR010125 1 20010816 A 5330 DOUBLER BOEING 737 737230 NM PWA JT8 JT8D15 52051 NE FUSELAGE DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 737TW 20257 CARGO CABIN BONDED DOUBLER WITH DELAMINATION, FROM BS 639 TO BS 655 AND BETWEEN STR 9L AND STR 8L. 2 L 7 2 4F 4 F RT A16WE E2EA 2001100100074 20011001 00074 EU 2001 10 1 SABA010028 1 20010703 A 7712 TRANSMITTER BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE331* 01514 WP LT ENGINE MALFUNCTIONED A SABA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 33 913AE 913 66346 AIRCRAFT 913 ON FLIGHT 5109 CLT TO HKY. DURING CLIMBOUT FROM CLT THE LEFT ENGINE TORQUE INDICATION WENT TO ZERO. ALL E NGINE INDICATIONS WERE NORMAL. NO INFLIGHT EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO CLT AND LANDED WITH NO OTHER P ROBLEMS. MAINTENANCE CHANGED THE SIGNAL CONDITIONER HOOKUP FROM BRIDGE NR 2 TO BRIDGE NR 1. GROUND RUN WAS PERFORMED. ALL SYSTEMS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 3 T RT A56EU E2WE 2001100100075 20011001 00075 EU 2001 10 1 SABA010031 1 20010720 A 3244 AH52688 TIRE BAG JETSTM JETSTM3201 1500217 EU NLG OUT OF BALANCE A SABA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 SO 33 963AE 963 ACFT 963 ON FLIGHT 5067 FROM CLT TO AHN. DURING TAKEOFF ROLL AT 120 KTS THE CREW FELT A SEVERE NOSE WHEEL SHIMMY. NO E MERGENCY WAS DECLARED. AIRCRAFT RETURNED TO THE GATE WITH NO OTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED BOTH NOS E WHEEL/TIRE ASSEMBLIES. TAXI CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A56EU 2001100100076 20011001 00076 NM 2001 10 1 COOSDR010126 1 20010816 A 5330 DOUBLER BOEING 737 737230 NM PWA JT8 JT8D15 52051 NE FUSELAGE DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 737TW 20257 CARGO CABIN BONDED DOUBLER WITH DELAMINATION AT BS 937 AND BETWEEN STR 6R AND STR 7R. 2 L 7 2 4F 4 F RT A16WE E2EA 2001100100077 20011001 00077 NM 2001 10 1 SABA010032 1 20010724 A 3350 6104789 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 841PH 082 AIRCRAFT 841 ON FLIGHT 5025 TLH TO CLT. AFTER ARRIVING AT CLT THE FLOOR EMERGENCY LIGHTING WAS FOUND TO BE INOPERATIVE. NO EMERGENCY WAS DECLARED AND NO EMERGENCY PROCEDURES WERE USED. MAINTENANCE REPLACED THE FLOOR EMERGENCY LIGHT BATTE RY PACK. SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001100100078 20011001 00078 EU 2001 10 1 CX72001F00001 1 20010309 A 6120 7901996X4 ACTUATOR SAAB SF340 340B 7860101 EU RT PROPELLER BROKEN A CX7A O OTHER O OTHER NR NOT REPORTED 1 GL 03 306CE 340B203 RIGHT ACTUATOR PROPELLER BROKEN. ENGINE SHUT DOWN. 2 L 7 2 4T RT A52EU 2001100100079 20011001 00079 EU 2001 10 1 SABA010035 1 20010727 A 3350 311701 BATTERY BAG JETSTM JETSTM3201 1500217 EU CABIN DISCHARGED A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 957AE 957 AIRCRAFT 957 PRIOR TO FLIGHT 5141 CLT TO LYH. DURING PREFLIGHT THE LEFT EMERGENCY EXIT AND THE MAIN CABIN DOOR EXIT SIG NS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT EMERGENCY LIGHT BATTERIES. NO EMERGENCY PRO CEDURES WERE USED. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT A56EU 2001100100080 20011001 00080 CE 2001 10 1 DVP2001F00000 1 20010727 A 2822 6467664A1 SEAL BEECH 36 A36 1151604 CE CONT O550 IO550* SO FUEL PUMP FAILED A DVPR A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION DE DESCENT 1 SO 03 1849L 607 E848 249144R DURING DESCENT, PILOT HAD TO OPERATE ELECTRIC FUEL BOOST PUMP IN ORDER TO MAINTAIN ENGINE POWER. ON LANDING, FUEL WAS F OUND TO BE LEAKING FROM SEAL DRAIN LINE OF ENGINE DRIVEN FUEL PUMP. FUEL STAINS WERE EVIDENT ALONG ENGINE SIDE OF NOSE GEAR BAY AND ONTO LOWER FUSELAGE SKIN IN VACINITY OF RIGHT EXHAUST. NO FIRE HAD OCCCURED. HAD FUEL IGNITED IT WOULD H AVE LED TO A CATASTROPHE. THERE WAS NOT WARNING OF IMMINENT FAILURE. MFG SB ADDRESSES THIS PARTICULAR PROBLEM ON FUEL PUMPS MANUFACTURED DURING A 2.5 YEAR TIME FRAME. THIS PUMP FALLS WITHIN THAT PERIOD, BUT IS NOT INCLUDED BECAUSE IT HA D MORE THAN STIPULATED 300 HOURS TIME IN SERVICE. RECOMMEND MFG REVISE THIS SB OF ANY PUMP THAT FALLS WITHIN THE DATE 1 L 7 1 3O 3 O 3A15 E3SO 2001100100081 20011001 00081 EU 2001 10 1 ECA2001F00000 1 20010816 A 3110 365A67907101 CIRCUIT BOARD AEROSP AS365 AS365N2 8680815 EU TMECA ARRIEL ARRIEL1 60030 NE CAUTION PANEL FAULTY E ECAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 11 886TW 1691 6413 WHILE IN CRUISE FLIGHT, THE PILOT NOTED SEVERAL CAUTION PANEL WARNING LIGHTS HAD ILLUMINATED AND THE TRIM RELEASE SYSTEM HAD FAILED. THE PILOT ELECTED TO MAKE A PRECAUTIONARY LANDING AT THE CLOSEST AIRPORT. WHEN THE LANDING GEAR WAS SELEC TED DOWN, NO INDICATIONS OF GEAR POSITION WERE VISIBLE. THE PILOT MADE A PASS BY THE TOWER TO VERIFY GEAR DOWN AND MADE AN UNEVENTFUL LANDING. COMPANY MAINTENANCE PERSONNEL WERE DISPATCHED TO THE AIRCRAFT TO MAKE REPAIRS. WITH THE ASSIS TANCE OF THE AIRCRAFT MFG, THE PROBLEM WAS TROUBLE SHOT TO A CIRCUIT CARD IN THE A36 PANEL. THE CARD WAS REPLACED AND T HE AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 2 3U 3 U RT H10EU E19EU 2001100100082 20011001 00082 NM 2001 10 1 SABA010036 1 20010729 A 3350 61D4789 BATTERY DHAV DHC8 DHC8103 1386005 NM CABIN DISCHARGED A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 801WP 086 AIRCRAFT 801 PRIOR TO FLIGHT 5089 CLT TO SOP. DURING PREFLIGHT THE CABIN EMERGENCY LIGHTS WERE FOUND INOPERATIVE. NO E MERGENCY WAS DECLARED AND NO EMERGENCY PROCEDURES USED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERIES. SYSTEM OP CHECKED GOOD. 2 H 7 2 4T RT A13NM 2001100100083 20011001 00083 EU 2001 10 1 SABA010038 1 20010815 A 7933 696219 INDICATOR BAG JETSTM JETSTM3201 1500217 EU COCKPIT INACCURATE A SABA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 33 957AE 957 ACFT 957 ON FLIGHT 5144 CLT TO GTSP. 7 AFTER DEPARTING CLT THE NR 1 OIL TEMPERATURE WAS INDICATING 105 DEGREES. NO INF LGHT EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO CLT WITH NO OTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED THE NR 1 OIL TEMPERATURE INDICATOR. OPS CHECK WAS GOOD. 2 L 7 2 4T RT A56EU 2001100100084 20011001 00084 EU 2001 10 1 SABA010039 1 20010815 A 7922 L8523427 BYPASS VALVE BAG JETSTM JETSTM3201 1500217 EU OIL COOLER FAILED A SABA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 957AE 957 ACFT 957 ON FLIGHT 9475 CLT TO RDU. ON CLIMBOUT NR 1 OIL TEMPERATURE WENT INTO RED. PILOT PULLED POWER BACK TO 60 PERCE NT AND TEMP WENT INTO THE YELLOW. NO INFLIGHT EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO CLT AND LANDED WITH NO OTHE R PROBLEMS. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE OIL COOLER THERMAL BYPASS VALVE. OPS CHECK WAS GOOD. 2 L 7 2 4T RT A56EU 2001100100085 20011001 00085 EU 2001 10 1 SABA010040 1 20010815 A 3230 PIN BAG JETSTM JETSTM3201 1500217 EU MLG MALFUNCTIONED A SABA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 961AE 961 GEAR WOULD NOT RETRACT AFTER TAKEOFF. NO EMERGENCY DECLARED RETURN TO FIELD. JACKED AIRCRAFT RESET MAIN LANDING GEAR B YPASS PIN OPERATIONALLY CHECKED LANDING GEAR. NO FURTHER ACTION REQUIRED. 2 L 7 2 4T RT A56EU 2001100100086 20011001 00086 WP 2001 10 1 SABA010041 2 20010818 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE331* 01514 WP LEFT MALFUNCTIONED A SABA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 33 961AE 961 66248 AIRCRAFT 961 ON FLIGHT 5121 CLT TO HKY. DURING TAKEOFF ROLL THE LEFT ENGINE WOULD NOT DEVELOP MORE THAN 60 PERCENT TORQ UE. TAKEOFF WAS ABORTED. NO EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO THE GATE WITH NO OTHER PROBLEMS. MAINTENANC E PERFORMED GROUND RUN OF THE ENGINE, WERE UNABLE TO DUPLICATE PROBLEM. NO TROUBLE FOUND. AIRCRAFT RETURNED TO SERVICE . 2 L 7 2 4T 3 T RT A56EU E2WE 2001100100087 20011001 00087 SW 2001 10 1 GXPA0114 1 20010619 A 2120 UNKNOWN SWRNGN SA226 SA226TC 8780404 SW COCKPIT ODOR E GXPA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 164GA TC281 AIRCRAFT MADE A PRECAUTIONARY LANDING, DUE TO ELECTRICAL ODOR IN THE COCKPIT. INSPECTED PILOT AND CO-PILOT SWITCH CUB P ANEL AND FOUND NO DISCREPANCIES. GROUND RUN ENGINE AND CHECKED GENERATOR OUTPUTS AND FOUND. OK 2 L 7 2 4T RT A8SW 2001100100088 20011001 00088 EU 2001 10 1 HSY2001F00000 1 20010509 A 3260 200918206 LIMIT SWITCH STBROS SD3 SD360 8100606 EU RT MLG SHORTED A HSYA O OTHER O OTHER NR NOT REPORTED 1 NM 05 701A SH3627 LEFT CIRCUIT BREAKER NR 38 GEAR WARNING POPPED. RESET CIRCUIT BREAKER, RECEIVED 3 GREEN, DOWN AND LOCKED INDICATION. A T 500 FEET AFL (TOO LOW GEAR) WARNING. DID GO AROUND AND LANDED. RIGHT MAIN LANDING GEAR DOWN LIMIT SWITCH MALFUNCTION ED, INTERNAL SHORT CIRCUIT. REMOVED AND REPLACED THE SWITCH, PLACED LANDING GEAR ON DEFERRED MAINTENANCE ITEM LIST PER MEL FOR RETRACTION CHECK. 2 H 7 2 4T A41EU 2001100100090 20011001 00090 2001 10 1 SABA010046 4 20010901 A 3425 700182906 INDICATOR BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A SABA A UNSCHED LANDING I FLT. ATTITUDE INST. CR CRUISE 1 SO 33 961AE 961 AIRCRAFT 961 ON FLIGHT 5196 FROM CLT TO LYH. WHILE IN CRUISE FLIGHT AFTER DEPARTING CLT THE CAPTAINS ATTITUDE INDICATOR BECAME INOPERATIVE. THE CIRCUIT BREAKER WAS CYCLED WITH NO RESULTS. SNO INFLIGHT EMERGENCY WAS DECLARED. AIRCRAFT RE TURNED TO CLT AND LANDED WITH NO OTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED THE NUMBER ADI. SYSTEM OPS CHECKED G OOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A56EU 2001100100091 20011001 00091 NM 2001 10 1 SABA010047 1 20010907 A 3350 8245110001SP LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 841PH 082 ACFT 841 ON FLIGHT 5057 TLH TO CLT. AFTER THE AIRCRAFT WAS PARKED AT THE GATE IN CLT THE FLOOR EMERGENCY LIGHTS WERE FO UND TO BE INOPERATIVE. NO EMERGENCY PROCEDURES WERE USED. MAINTENANCE REPAIRED THE WIRING HARNESS AND REPLACED TWO LIG HT ASSEMBLYS. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001100100092 20011001 00092 EU 2001 10 1 SABA010048 1 20010914 A 3350 311701 BATTERY BAG JETSTM JETSTM3201 1500217 EU CABIN DISCHARGED A SABA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 33 965AE 965 ACFT 965 ON FLIGHT 5100 FROM CLT AND HTS. BEFORE DEPARTURE FROM THE GATE THE RIGHT EMERGENCY EXIT DOOR EMERGENCY EXIT L IGHT WAS INOPERATIVE. NO EMERGENCY PROCEDURES WERE USED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERIE S. SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A56EU 2001100100094 20011001 00094 WP 2001 10 1 MWEA011355 1 20010927 A 5310 99579113 INTERCOSTAL DOUG DC9 DC932 3022066 WP STATION 351 BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 FORWARD PIT INTERCOSTAL IS BENT BETWEEN FRAMES 351 AND 370 AT LONGERON 29 LEFT. -- FABRICATED AND INSTALLED INTERCOSTA L. 2 L 7 2 4F A6WE 2001100100095 20011001 00095 WP 2001 10 1 MWEA011339 1 20010927 A 5310 99124533 ANGLE DOUG DC9 DC932 3022066 WP A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 TOOL DAMAGE, CORROSION AROUND BN NUT, ONE ELONGATED FASTENER HOLE AND THREE EMPTY FASTENER HOLES, FORWARD CARGO DOOR JAM B BAY, STATION 427 TO 435, LONGERON 28 RIGHT TO 26 RIGHT -- REMOVED, FABRICATED AND INSTALLED REPAIR ANGLE. 2 L 7 2 4F A6WE 2001100100096 20011001 00096 WP 2001 10 1 MWEA011340 1 20010927 A 5310 5956034501 FITTING DOUG DC9 DC932 3022066 WP STATION 427 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 FRAME FITTING CRACKED, STATION 427, LONGERON 28 LEFT -- FABRICATED AND INSTALLED FITTING 2 L 7 2 4F A6WE 2001100100097 20011001 00097 WP 2001 10 1 MWEA011357 1 20010927 A 5310 99236893 INTERCOSTAL DOUG DC9 DC932 3022066 WP STATION 484 BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 FORWARD PIT INTERCOASTAL IS BENT LOCATED BETWEEN FRAMES 484 AND 503 BEWEEN LONGERONS 28 LEFT AND 27 LEFT. -- FABRICATE D AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001100100098 20011001 00098 WP 2001 10 1 MWEA011364 1 20010927 A 5330 99582391 DOUBLER DOUG DC9 DC932 3022066 WP STATION 1019 CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 AFT ACCESSORY COMPARTMENT FRAME STATION 1019 HAS CHAFFE MARKS BETWEEN LONGERON 14 LEFT AND 15 LEFT WITH TWO BROKEN CLAMP S FOR INSTRUMENT AIR LINES. -- FABRICATED AND INSTALLED REPAIR ANGLE, DOUBLER, AND FILLER AND REMOVED AND REPLACED CLA MPS. 2 L 7 2 4F A6WE 2001100100099 20011001 00099 WP 2001 10 1 MWEA011365 1 20010927 A 5330 595602617 DOUBLER DOUG DC9 DC932 3022066 WP STATION 360 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 FORWARD CARGO INTERIOR SKIN HAS A CUT BETWEEN STAITON 360 THROUGH 364 AND LONGERON 27 LEFT THROUGH 28 LEFT. -- FABRICA TED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001100100100 20011001 00100 WP 2001 10 1 MWEA011366 1 20010927 A 5520 591804611 DOUBLER DOUG DC9 DC932 3022066 WP LEFT ELEVATOR MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 LEFT ELEVATOR, UPPER OUTBOARD SKIN AT FORWARD SPAR HAS A FINGER DOUBLER MISDRILLED. -- FABRICATED AND INSTALLED REPLAC EMENT DOUBLER. 2 L 7 2 4F A6WE 2001100100101 20011001 00101 WP 2001 10 1 MWEA011348 1 20010927 A 5330 99124534 DOUBLER DOUG DC9 DC932 3022066 WP STATION 370 MISSING A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 SIX EMPTY FASTNER HOLES, FORWARD CARGO DOOR JAMB BAY, STATION 370 TO 362, LONGERON 29 RIGHT TO 28 RIGHT. -- FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLER. 2 L 7 2 4F A6WE 2001100100102 20011001 00102 WP 2001 10 1 MWEA011361 1 20010927 A 5310 DOUBLER DOUG DC9 DC932 3022066 WP STATION 330 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 SKIN DENTED AT STATION 330, LONGERON 26 APPROXIMATELY 1 1/4 INCH BY .046 DEEP RIGHT HAND SIDE. -- REMOVED DAMAGE, INST ALLED INTERNAL DOUBLER AND FLUSH PLUG. 2 L 7 2 4F A6WE 2001100100103 20011001 00103 EU 2001 10 1 SABA010049 1 20010919 A 2910 137930A159 HYDRAULIC LINE BAG JETSTM JETSTM3201 1500217 EU RT MLG WW LEAKING A SABA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 33 965AE 965 ACFT 965 ON FLIGHT 5156 FROM AVL TO CLT. WHILE IN FLIGHT THE AIRCRAFT LOST ALL MAIN HYDRAULIC PRESSURE. AN INFLIGHT EM ERGENCY WAS DECLARED. LANDING GEAR WAS LOWERED WITH THE ALTERNATE SYSTEM. AIRCRAFT LANDED AT RDU AND TAXIED TO THE GAT E WITH NO OTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR RADIUS ROD UP LINE. SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A56EU 2001100100104 20011001 00104 NM 2001 10 1 SABA01023 1 20010614 A 3350 LIGHT DHAV DHC8 DHC8103 1386005 NM COCKPIT INOPERATIVE A SABA K NONE O OTHER CR CRUISE 1 SO 33 801WP 086 AIRCRAFT 801 ON FLIGHT 5138 CVG TO CLT. DURING CRUISE FLIGHT THE FORWARD OVERHEAD EMERGENCY LIGHT WENT OUT. THE FLIGHT WAS CONTINUED TO AND LANDED CLT WITH NO OTHER PROBLEMS. NO INFLIGHT EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND R EPLACED BULBS. OPS CHECK WAS GOOD. 2 H 7 2 4T RT A13NM 2001100100105 20011001 00105 NM 2001 10 1 SCNA01354 1 20010907 A 3350 LIGHT BOEING 727 727259 138408J NM L1 DOOR INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 DURING HEAVY MAINTENANCE INSPECTION THE L1 DOOR EMERGENCY SLIDE LIGHT WAS FOUND TO BE INOPERATIVE. RELAMPED IAW B727 MM 335041, OPS CHECK GOOD IAW B727 MM 335041. 2 L 7 3 4F A3WE 2001100100106 20011001 00106 NM 2001 10 1 SCNA01355 1 20010917 A 3350 LIGHT BOEING 727 727259 138408J NM EXTERIOR INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 DURING HEAVY MAINTENANCE INSPECTION THE EXTERIOR EMERGENCY LIGHT ADJACENT TO L1 DOOR WAS INOPERATIVE. RELAMPED IAW B727 MM 335041, OPS CHECK GOOD IAW B727 MM 335041. 2 L 7 3 4F A3WE 2001100100107 20011001 00107 EU 2001 10 1 YENA200101 1 20010508 A 3530 9700C1ABF23A OXYGEN BOTTLE AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A YENA K NONE O OTHER CR CRUISE 1 EA 15 509JB 2650 115 1270 IN FLIGHT, FLT NR 20, TPA TO JFK, F/A'S ADMINISTERED OXYGEN TO PAX FROM POB IN AFT GALLEY. FWD A/C RIGHT POB WOULD NOT FLOW WHEN ATTEMPT WAS MADE TO USE IT, APPEARS TO BE EMPTY. REMOVED AND REPLACED 1 POB IAW MM 35-32-42, BOTTLE SECURED I N FWD BIN. 2 L 7 2 4F RT A28NM 2001100100108 20011001 00108 WP 2001 10 1 ZW0A0108204 1 20010908 A 5311 BELTFRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9403W 53139 DURING CHECK-C MAINT THE BELT RING AT STATION, 1418 LONGERON 2L, HAD A .5 INCH CRACK. BELT RING REPAIRED PER ARA 17916, AND SRM 53-20. 2 L 7 2 4F RT A6WE 2001100100109 20011001 00109 NM 2001 10 1 CALA0100903 1 20010928 A 5414 SKIN BOEING 737 7373T0 1384582 NM #2 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17306 23357 INSPECTION FOUND A 5/8" CRACK IN #2 ENGINE PYLON SKIN ACCESS PANEL #5827R CUTOUT. REPAIRED IAW ECRA 5430-01230. 2 L 7 2 4F RT A16WE 2001100100110 20011001 00110 NM 2001 10 1 CALA0100905 1 20010928 A 5313 STRINGER BOEING 737 7373T0 1384582 NM STA 338 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 INSPECTION FOUND A 6" CRACK IN STRINGER 10R AT STA 338. A NEW STRINGER WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001100100111 20011001 00111 NM 2001 10 1 CALA0100906 1 20010928 A 5320 ANGLE BOEING 737 7373T0 1384582 NM STA 380-400 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 INSPECTION FOUND A 2" CRACK IN INTERCOSTAL UPPER ANGLE AT STA 380-400, BL 0. A NEW ANGLE WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001100100112 20011001 00112 NM 2001 10 1 CALA0100908 1 20010930 A 5330 SKIN BOEING 737 7373T0 1384582 NM WINDOW POST CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 INSPECTION FOUND A 1.125" CRACK AT UPPER R/H CORNER I/B SIDE OF CO-PILOT'S R/H WINDOW POST SKIN AND GUSSET. THE CRACKED AREA WAS ROUTED OUT AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-10-1, FIGURE 210. 2 L 7 2 4F RT A16WE 2001100100113 20011001 00113 NM 2001 10 1 CALA0100910 1 20010930 A 5320 WEB BOEING 737 7373T0 1384582 NM C-2 THRESHOLD CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10323 23374 INSPECTION FOUND WEB CORRODED AROUND FASTENERS AT LOWER SIDE OF C-2 DOOR UPPER THRESHOLD. A NEW WEB WAS INSTALLED IAW SR M 51-10-2. 2 L 7 2 4F RT A16WE 2001100100114 20011001 00114 NM 2001 10 1 ZW0A0108613 1 20010914 A 5753 FLAP BOEING 757 7572Q8 1384972 NM LT WING PUNCTURED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 709TW 28168 DURING CHECK-C MAINT ON LT WING THE LOWER SURFACE OF THE INBD FOREFLAP, MIDDLE SECTION, HAD .25 INCH WIDE PUNCTURE AND 1 INCH LONG DENT, LOCATED JUST OTBD AND AFT OF THE INBD CANOE FAIRING. INSTALLED HOT BOND REPAIR AND PRIMED AND PAINTED PER SRM 51-70-10. 2 L 7 2 4F RT A2NM 2001100100115 20011001 00115 NM 2001 10 1 ZW0A0108703 1 20010911 A 5330 SKIN BOEING 757 7572Q8 1384972 NM FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 709TW 28168 DURING CHECK-C MAINT FOUND AT STA 1365 AND STRINGER 23L, 2 DAMAGE AREAS WITHIN 6 INCHES OF STATIC PORT. GOUGE AND DENT ABOVE PORT. SHOWS EDDY CURRENT CRACK. INSTALLED 1 INCH ROUND REPAIR, FLUSH TYPE, PER SRM 53-00-01, FIG 208 PAGE 225. 2 L 7 2 4F RT A2NM 2001100100116 20011001 00116 NM 2001 10 1 ZW0A0108704 1 20010912 A 5512 DOUBLER BOEING 757 7572Q8 1384972 NM HORIZ STAB DELAMINATED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 709TW 28168 DURING CHECK-C MAINT THE TOP SURFACE JUST AFT OF L/E AND 6 FT OTBD OF FUSELAGE, FOUND PATCH DELAMINATED WITH RAGGED EXPO SED EDGE. INSTALLED 4 .5 INCH DIAMETER METAL TO METAL HOT BOND REPAIR ON UPPER LEFT HORIZONTAL STABILIZER PANEL PER SRM 55-10-01, PAGE 1, AND 51-70-10 PAGE 52. PRIMER, SANDED, AND MATCHED PAINT. 2 L 7 2 4F RT A2NM 2001100100117 20011001 00117 WP 2001 10 1 ZW0A0108705 1 20010913 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 911TW 49182 DURING CHECK-C MAINT FOUND CORROSION ON LT CHAIR TRACK AT LBL 54, STA 1282 AND 1174. REMOVED CORROSION BY REPLACING CHA IR TRACK FROM STA 1174 TO 1309, LBL 54 INCHES, PER SPM 6-70-01 AND SRM 51-30-1. 2 L 7 2 4F A6WE 2001100100118 20011001 00118 WP 2001 10 1 ZW0A0108706 1 20010913 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 911TW 49182 DURING CHECK-C MAINT FOUND CHAIR TRACK AT LBL 44 INCHES, STA 1088 TO 1309, WAS CORRODED BEYOND LIMITS. REMOVED CORRODED TRACK AND INSTALLED NEW TRACK WITH TRACK SPLICE PER SRM 53-05, FIG 4F, AND BOLTED TRACK DOWN PER SRM 51-30-1. 2 L 7 2 4F A6WE 2001100100119 20011001 00119 WP 2001 10 1 ZW0A0108801 1 20010918 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN CONTAMINATED A ZW0A K NONE L NO TEST NR NOT REPORTED 1 CE 13 959U 49704 THE EGRESS LIGHTS IN THE FIRST CLASS CABIN WERE INOPERATIVE. CLEANED AND DRIED OUT THE LIGHT STRIP. CHECK-C 6-28-01 ST L. 2 L 7 2 4F A6WE 2001100100120 20011001 00120 NM 2001 10 1 AWXA200100481 1 20010829 A 5311 656220815 FRAME BOEING 737 737301 1384611 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 MCN - C16 CK - "C" - FRAME CRACKED AT BS 663, STR 2R. MAINTENANCE PERFORMED REPAIR TO FRAME IAW B737 SRM 53-00-07 PG 22 6, FIG 209. 2 L 7 2 4F RT A16WE 2001100100121 20011001 00121 NM 2001 10 1 AWXA200100482 1 20010829 A 5311 656220815 FRAME BOEING 737 737301 1384611 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 MCN - C16 CK - "C" - FRAME FOUND CRACKED AT BS 663, STR 2L. MAINTENANCE REPAIRED FRAME IAW B737 SRM 53-00-07, PG 226, F IG 209. 2 L 7 2 4F RT A16WE 2001100100122 20011001 00122 NM 2001 10 1 AWXA200100483 1 20010913 A 5313 6545769 STRINGER BOEING 737 737301 1384611 NM GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 MCN - C16 CK - "C" - GOUGE IN STR 27R AT BS 480, FOUND TO BE BEYOND SRM LIMITS AFTER BLEND OUT. MAINTENANCE CUT OUT DAMA GED AREA, FABRICATED STRINGER SECTION AND FILLERS, AND INSTALLED REPAIR PARTS IAW B737 SRM 53-00-03, PG 201 - 206. 2 L 7 2 4F RT A16WE 2001100100123 20011001 00123 NM 2001 10 1 AWXA200100488 1 20010827 A 5311 6546547624 FRAME BOEING 737 737301 1384611 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 MCN - C16 CK - "C" - .625" CRACK IN FRAME AT BS 727, STR 14L. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED REPAIR ANGLE & DOUBLER AND INSTALLED REPAIR PARTS IAW AWA ER 03-5300-01271-TB1. 2 L 7 2 4F RT A16WE 2001100100124 20011001 00124 WP 2001 10 1 ZW0A0108802 1 20010913 A 5320 SILL DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 911TW 49182 DURING CHECK-C MAINT FOUND THE AFT CARGO COMPT DOOR SILL OTBD FLANGE HAD MATERIAL REMOVED BEYOND LIMITS, STA 1155 THRU 1 212. REPAIRED TWO OUT OF LIMITS AREAS PER SRM 53-05, FIG 63, SHEETS 1 THRU 8. 2 L 7 2 4F A6WE 2001100100125 20011001 00125 WP 2001 10 1 ZW0A0108803 1 20010913 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 926TW 49356 DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT BRACKET AT RBL 10 TO RBL 42, STA 180. REPLACED FLOOR SUPPORT PER SPM 6-70-01. 2 L 7 2 4F A6WE 2001100100126 20011001 00126 WP 2001 10 1 ZW0A0108804 1 20010913 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 926TW 49356 DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 1155, LBL 23 INCHES TO LBL 44 INCHES. REPLACED WITH NEW PA RT PER SAMPLE AND SPM 6-70-1 AND DOUGLAS DRAWING 5930544. INSTALLED PER SRM 51-30. 2 L 7 2 4F A6WE 2001100100127 20011001 00127 WP 2001 10 1 ZW0A0108805 1 20010914 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 911TW 49182 DURING CHECK-C MAINT FOUND APPROX 2 INCH CRACK IN FWD LEFT CABIN OUTER DOOR FRAME, LOWER FWD CORNER BELOW THE DOOR HINGE ASSEMBLY. REPLACED LOWER FWD CORNER OF PAN ASSY PER SRM 51-00 P27 ITEM B. 2 L 7 2 4F A6WE 2001100100128 20011001 00128 WP 2001 10 1 ZW0A0108806 1 20010914 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 911TW 49182 DURING CHECK-C MAINT FOUND IN THE AFT CARGO COMPT, STA 1212 TO 1219, BETWEEN LONGERON 27R AND 28R, CORROSION ON BOTTOM S IDE OF UPPER WEB SKIN AND STRUCTURE AFT OF BOTTOM AFT CORNER OF THE C3 CARGO COMPARTMENT. INSTALLED NEW SECTION OF WEB PER SPM 6-70-1. SPLICE INSTALLED PER SRM 51-70-4, PAGE 2, AND FASTENERS AND WEB INSTALLED PER DOUGLAS PRINT 5936442. 2 L 7 2 4F A6WE 2001100100129 20011001 00129 WP 2001 10 1 ZW0A0108807 1 20010918 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 911TW 49182 DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND LT FLOOR TRACK CORRODED AT CLIP NUT HOLES AT STA 1222 THRU 1322, TIE D OWN TRACK. REMOVED CORRODED TRACK AND INSTALLED NEW PER SRM 51-30-5 AND SRM 51-30-0. REPLACED TRACK FROM STA 1222 TO 1 322. 2 L 7 2 4F A6WE 2001100100130 20011001 00130 WP 2001 10 1 ZW0A0108808 1 20010918 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 911TW 49182 DURING CHECK-C MAINT IN THE AFT CARGO COMPT THE RT TIE DOWN TRACK FROM STA 1212 TO 1322 WAS CORRODED. INSTALLED FABRICA TED TRACK FROM STOCK. TRACK INSTALLED PER SRM 51-30-00. REPLACED FROM STA 1212 TO 1322. 2 L 7 2 4F A6WE 2001100100131 20011001 00131 WP 2001 10 1 ZW0A0108809 1 20010914 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 926TW 49356 DURING CHECK-C MAINT THE AFT CABIN UPPER SURFACE OF MEMBRANE HAD CORROSION AT STA 1249 FROM LBL 47 INCHES TO LBL 56 IN, THE FLOOR MEMBRANE WAS CRACKED AT STA 1246, LBL 55. THREE BLIND FASTENERS WERE INSTALLED AT MEMBRANE AT STA 1249 LBL 56 IN. UPPER SIDE OF MEMBRANE HAD CORROSION AT STA 1251 LBL 55 INCHES, BACK TAIL MISSING FROM RIVET IN MEMBRANE AT STA 12 51 LBL 53 INCHES. REMOVED AND REPLACED RIVET PER SRM 51-30-6. CUT OUT CORRODED AREA OF MEMBRANE AND INSTALLED DOUBLER PER SRM 53-01 FIG 4. REMOVED BLIND FASTENERS AND INSTALLED SOLID RIVETS PER SRM 51-30-00. STOP DRILLED CRACK IN MEMBRA NE AND INSTALLED DOUBLER PER SRM 53-01 FIG 4. 2 L 7 2 4F A6WE 2001100100132 20011001 00132 WP 2001 10 1 ZW0A0108810 1 20010917 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 926TW 49356 DURING CHECK-C MAINT FOUND FLOOR MEMBRANE WAS TORN OUT AND ELONGATED HOLES FOR FASTENERS AT LBL 44 INCHES, STA 1175 TO 1 191. INSTALLED MEMBRANE REPAIR PER SRM 53-05, FIG 96. 2 L 7 2 4F A6WE 2001100100133 20011001 00133 WP 2001 10 1 ZW0A0108901 1 20010917 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 926TW 49356 DURING CHECK-C MAINT FOUND CORROSION AT UPPER SURFACE OF MEMBRANE LBL 54 INCHES, STA 1231. REMOVED CORROSION AND CUT OU T DAMAGED AREA. MADE DOUBLER AND INSTALLED PER SRM 51-30-4. 2 L 7 2 4F A6WE 2001100100134 20011001 00134 WP 2001 10 1 ZW0A0108902 1 20010914 A 5730 SKIN DOUG DC9 DC983 3022083 WP LT WING CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9617R 53564 DURING CHECK-C MAINT ON THE LT WING L/E, A CRACK WAS FOUND AT DOUBLER AT LOWER L/E OPENING BETWEEN NUMBER 5 AND 6 L/E SL AT TRACK. ACCOMP EDDY CURRENT INSPECTION PER NDT 51-00-03 AND FOUND CRACK CONTAINED. FABRICATED DOUBLER REPAIR PER SRM 57-01, PAGE 9, AND SRM 51-10-3, PAGE 16. INSTALLED PER SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F RT A6WE 2001100900161 20011009 00161 NM 2001 10 9 01FDEA00862 1 20010928 A 5311 6516316 FRAME BOEING 727 727233 138408A NM PAX DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 281FE 22348 N 700 FRAME AT BS 344 IS CRACKED ABOVE FWD ENTRY DOOR. R/R FRAME PER SRM 53-10-4. 2 L 7 3 4F RT A3WE 2001102500260 20011025 00260 NM 2001 10 25 01FDEA00864 1 20010930 A 5311 FRAME BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 281FE 22348 BS 1090, LBL 20, WL 154 FRAME CRACKED UNDER FLOOR TO SIDEWALL SUPPORT. REMOVED AND REPLACED FRAME PER SRM 51-40-3 FIG 1. 2 L 7 3 4F RT A3WE 2001102500261 20011025 00261 NM 2001 10 25 01FDEA00865 1 20010929 A 5313 STRINGER BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 281FE 22348 CRACK ON STR 27L AT BS 480. REMOVED AND REPLACED STRINGER PER SRM 53-10-3 FIG 1. 2 L 7 3 4F RT A3WE 2001102500263 20011025 00263 NM 2001 10 25 01FDEA00867 1 20010929 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 281FE 22348 CORROSION (C53-224-01,1) ON FLOORBEAM BS 344, LBL 40 TO RBL 5, WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8, 5 3-10-1, 51-30-2 & 51-10-6. 2 L 7 3 4F RT A3WE 2001100200011 20011002 00011 NM 2001 10 2 HNAA0100064 1 20011001 A 3232 82970018011 ACTUATOR DHAV DHC8 DHC8102 2809003 NM INOPERATIVE A HNAA K NONE O OTHER CL CLIMB 1 EA 07 923HA 23390 2270 099 #1 MLG FWD DOOR REMAINS OPEN AFTER GEAR IS SELECTED UP. REPLACED #1 MLG FWD GEAR DOOR ACTUATOR. 2 H 7 2 4T RT A13NM 2001100200014 20011002 00014 NM 2001 10 2 ZW0A0108611 1 20010911 A 5414 SKIN BOEING 757 7572Q8 1384972 NM NR 1 PYLON WORN A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 709TW 28168 DURING CHECK-C MAINT ON THE NUMBER 1 PYLON, THE AFT REVERSER EQUALIZER BAR HAD WEAR SPOT AT CONTACT POINT WITH INBOARD S KIN. CLEANED UP AND SMOOTHED OUT AREA PER SRM 54-51-01. 2 L 7 2 4F RT A2NM 2001100200015 20011002 00015 NM 2001 10 2 ZW0A0108612 1 20010911 A 5410 BAR BOEING 757 7572Q8 1384972 NM NR 1 PYLON WORN A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 709TW 28168 DURING CHECK-C MAINT ON THE NUMBER 1 INBD PYLON, THE EQUALIZER BAR HOLE IN THE PYLON FWD OF AFT REVERSER MOUNT, THE FWD EDGE OF THE HOLE WAS WORN. CLEANED AND SMOOTHED OUT AREA PER SRM 54-5-01. 2 L 7 2 4F RT A2NM 2001100200016 20011002 00016 EU 2001 10 2 2001UALA02040 1 20010914 A 3620 THERMOSTAT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 412UA MR3621023 465 #1 ENGINE BLEED FAULT LIGHT ILLUMINATED, HAD BLEED 1OVERHEAT. UNABLE TO RESET SYSTEM. SUPPLEMENTAL DATA UPDATE REPLACED FAN AIR THERMOSTAT, RAN ENGINES, BLEED PARAMETERS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2001100200017 20011002 00017 NM 2001 10 2 2001UALA02055 1 20010917 A 5315 141W85189 STIFFENER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RBL 38 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 775UA 24250 0 26947 STATION 246 RBL 38 FLOOR BEAM VERTICAL STIFFENER CRACKED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHEDFABRICATED A ND INSTALLED NEW STIFFENER.NOTED CRACKING OF THE STIFFENER IS DUE TO THERMAL CONTRACTION THAT RESULTS IN HIGHER THAN EXP ECTED IN-SERVICE LOADING OF THE DOUBLE DEPTH STATION 246 FLOOR BEAM. PART IS BEING REPAIRED. REPLACED STIFFENER. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001100200018 20011002 00018 NM 2001 10 2 2001UALA02056 1 20010917 A 5315 141W851815 STIFFENER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RBL 40 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 775UA 24250 0 26947 STATION 246 RBL 40 FLOOR BEAM VERTICAL STIFFENER CRACKED SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHEDFABRICATED AN D INSTALLED NEW STIFFENERNOTED CRACKING OF THE STIFFENER IS DUE TO THERMAL CONTRACTION THAT RESULTS IN HIGHER THAN EXPEC TED IN-SERVICE LOADING OF THE DOUBLE DEPTH STATION 246 FLOOR BEAM. PART IS BEING REPAIRED. REPLACED STIFFENER. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001100200019 20011002 00019 NM 2001 10 2 2001UALA02071 1 20010921 A 2700 SEAL BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 924UA 26645 UNSCHEDULED LANDING DUE TO A LOOSE #2 FLAP SEAL. SUPPLEMENTAL DATA UPDATE REMOVED AND REPLACED THE #2 LEADING EDGE FLAP AERODYNAMIC SEAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2001100200020 20011002 00020 NM 2001 10 2 2001UALA02086 1 20010927 A 2530 OVEN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 592UA 28143 CREW REPORTS LIGHT SMOKE COMING FROM FWD GALLEY AREA. FOUND CHEESE IN FWD GALLEY OVEN. CLEANED OVEN. 2 L 7 2 4F 4 F RT A2NM E17NE 2001100200026 20011002 00026 WP 2001 10 2 ZW0A0108903 1 20010914 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9617R 53564 DURING CHECK-C MAINT ON THE LT MAIN GEAR WHEEL WELL, APPROX STA 946, LBL 7, THE FWD INBD CORNER OF THE GEAR WELL WAS CRA CKED AND BUSTED. ACCOMP EDDY CURRENT INSP PER NDT 51-00-03 AND FOUND CRACK CONTAINED. REPAIRED PER SRM 53-01, PAGE 10, TWO REPAIR ANGLES. 2 L 7 2 4F RT A6WE 2001100200029 20011002 00029 EA 2001 10 2 BTH2001F00000 2 20010914 A 7414 DISTRIBUTOR GEAR PIPER PA32 PA32R300 7103213 SO LYC O540 IO540K1A5 41532 EA MAGNETO DAMAGED E BTHA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION TX TAXI/GRND HDL 1 AL 01 75387 342 32R7680298 L2512448A MAGNETO DEAD ON LEFT SIDE DURING RUNUP MAG CHECK. FOUND SEVERAL TEETH BROKEN ON BOTH DISTRIBUTOR GEARS. 1 L 7 1 3O 3 O A3SO 1E4 2001100200030 20011002 00030 WP 2001 10 2 ZW0A0109001 1 20010919 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 981Z 47345 THE FUSELAGE SKIN WAS CRACKED AT STA 168 AND LONGERON 29R, 1.625 INCHES AFT OF AREA CUT OUT FOR CORROSION, VERIFIED BY E DDY CURRENT. ACCOMPLISHED SKIN REPAIR AT STA 168 AND LONGERON 29R PER SRM 53-04 AND ARA 17918. 2 L 7 2 4F A6WE 2001100200031 20011002 00031 NM 2001 10 2 AWXA200100490 1 20010904 A 5230 6546921528 CROSSBEAM BOEING BOEING 737 737277 1384570 NM LOWER CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 0617 22651 YVR - C19 CK - "C" - FWD CARGO DOOR LOWER CROSSBEAM WEB, TWO CRACKS FOUND, ONE ON FWD END AND ONE ON THE AFT END. BOTH C RACKS ARE .5 INCH. MAINTENANCE REPAIRED THE CARGO DOOR IAW AWA E.O.52-31-04, SHEETS 1 - 18. 2 L 7 2 4F RT A16WE 2001100200032 20011002 00032 NM 2001 10 2 ZW0A0109101 1 20010924 A 3350 363674 LIGHT BOEING 757 757231 1384950 NM L2 DOOR BROKEN A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 726TW 30339 THE EGRESS LIGHT WAS BROKEN AT THE LEFT SIDE NUMBER 2 CABIN DOOR. REPLACED THE FLEX LAMP. 2 L 7 2 4F RT A2NM 2001100200034 20011002 00034 WP 2001 10 2 ZW0A0109102 1 20010921 A 5342 ATTACH ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9617R 53564 DURING CHECK-C MAINT ON THE AFT FUSELAGE EXTERIOR, LT SIDE 3 INCHES FWD OF VERTICAL FIN REAR SPAR, A CRACK WAS FOUND BET WEEN FASTENERS IN THE ATTACH ANGLE. CONFIRMED BY EDDY CURRENT. ACCOMP HIGH FREQ EDDY CURRENT AND FOUND CRACK CONTAINME NT PER NDT MANUAL 51-00-03, PART 6. REPAIRED PER SRM 53-05, PAGE 49. 2 L 7 2 4F RT A6WE 2001100200035 20011002 00035 WP 2001 10 2 ZW0A0109103 1 20010919 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 926TW 49356 DURING CHECK-C MAINT FOUND CORROSION ON THE NUMBER 2 SEAT TRACK, STA 1041 TO 1309, AT UPPER AND LOWER SURFACES OF FLOOR PANEL BOLT HOLES. REPLACED TRACK PER SRM 53-24-0, FIG 6 WITH TRACK FROM STOCK. REINSTALLED BOLTS AND NUTS PER SRM 51-3 0-1. INSTALLED TRACK SPLICE PER SRM 53-05, FIG 4F. 2 L 7 2 4F A6WE 2001100200036 20011002 00036 WP 2001 10 2 ZW0A0109104 1 20010921 A 5230 FLANGE DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 926TW 49356 DURING CHECK-C MAINT THE AFT CARGO DOOR AFT MID FLANGE WAS CRACKED AT FASTENER HOLES. REPAIRED CARGO DOOR CRACK PER SRM 52-05, PAGE 110A. INSTALLED RIVETS PER SRM 51-30-1. 2 L 7 2 4F A6WE 2001100200037 20011002 00037 WP 2001 10 2 ZW0A0109105 1 20010922 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 926TW 49356 DURING CHECK-C MAINT ON THE UPPER FUSELAGE, THE SKIN AT STA 226, LONGERON 5L, WAS OUT OF LIMITS AFTER REMOVAL OF CORROSI ON. INSTALLED EXTERNAL DOUBLER PER SRM 53-04, PAGE 60F. 2 L 7 2 4F A6WE 2001100200038 20011002 00038 WP 2001 10 2 ZW0A0109106 1 20010921 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 926TW 49356 DURING CHECK-C MAINT THE NUMBER 1 SEAT TRACK AT LBL 44.5 INCHES HAD CORROSION FROM STA 1218 TO 1302. SPLICED IN NEW SEC TION OF TRACK PER SRM 53-05, FIG 4F. 2 L 7 2 4F A6WE 2001100200039 20011002 00039 WP 2001 10 2 ZW0A0109201 1 20010924 A 5320 ATTACH FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 926TW 49356 DURING CHECK-C MAINT THE AFT SERVICE DOOR SILL PLATE ATTACH FITTINGS, FWD AND AFT, WERE CORRODED. REMOVED CORRODED FITT INGS AND INSTALLED NEW FITTINGS PER SPM 6-70-01. 2 L 7 2 4F A6WE 2001100200040 20011002 00040 WP 2001 10 2 ZW0A0109202 1 20010924 A 5320 SILL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 926TW 49356 DURING CHECK-C MAINT FOUND CORROSION ON DOOR SILL MEMBRANE AT AFT SERVICE DOOR, STA 1138 TO 1179. REMOVED CORROSION PER SPM 6-80-01. INSTALLED SMALL DOUBLER REPAIR AT STA 1140 PER SRM 53-01, FIG 2. 2 L 7 2 4F A6WE 2001100200041 20011002 00041 WP 2001 10 2 ZW0A0109203 1 20010924 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 926TW 49356 DURING CHECK-C MAINT THE FLOOR SEAT TRACK NUMBER 1 FROM STA 1136 TO 1218 HAD CORROSION. REPLACED SEAT TRACK SECTION FRO M STA 1136 TO 1218 WITH NEW TRACK PER SRM 53-05, FIG 4F. 2 L 7 2 4F A6WE 2001100200042 20011002 00042 NM 2001 10 2 ZWOA0106103 1 20010730 A 3350 S417N5092SMI LIGHT BOEING 767 7673Y0 NM R2 DOOR INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 632TW 24953 DURING PREFLIGHT EGRESS LIGHT WERE INOP AT DOOR R 2 DUE TO WEAR. REPLACED EGRESS LIGHT ASSY AT DOOR R2 P/N S417N509-2SM I. 2 L 7 2 4F RT A1NM 2001100200043 20011002 00043 WP 2001 10 2 AT0100231 1 20010823 A 2610 FIRE BOTTLE DOUG DC9 DC932 3022066 WP FWD CARGO DISCHARGED A ZZDA O OTHER J WARNING INDICATION CR CRUISE 1 SO 15 824AT 47278 FOUND FORWARD CARGO FIRE INDICATION ILLUMINATED. CORRECTIVE ACTION: CHECKED FORWARD CARGO AREA, COULD N OT DUPLICATE PROBLEM, AICRAFT WAS FERRIED TO AVBORNE FOR REPAIRS. 2 L 7 2 4F A6WE 2001100200044 20011002 00044 NM 2001 10 2 UPS01236815 1 20010521 A 5315 FLOORBEAM BOEING 727 727247 138408F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE:C WHILE WORKING FUSELAGE, DISCOVERED CORROSION ON BS 328 FLOORBEAM, LBL 18, WL 208. REMOVED CORROSION FR OM THE FLOORBEAM UPPER CHORD. FLAP PEENED AREA. FABRICATED AND INSTALLED REPAIR PARTS. ALL WORK ACCOMPLISHED IAW ER 01- 0537. 2 L 7 3 4F A3WE 2001100200046 20011002 00046 NM 2001 10 2 UPS01236816 1 20010606 A 5320 SILL BOEING 727 727247 138408F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE:C FOUND CORROSION ON AFT CARGO DOOR CUTOUT SILL CHORD AT BS 950E+19. REPAIRED CHORD IAW SRM 51-40-4, 53- 10-1, 51-10-1, 51-30-2. 2 L 7 3 4F A3WE 2001100200047 20011002 00047 NM 2001 10 2 UPS01236817 1 20010619 A 5310 SHEAR TIE BOEING 727 727247 138408F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE:C WHILE WORKING FUSELAGE, DISCOVERED SHEAR TIE CORRODED BS 970, RBL 8 OUTBOARD OF STR 29R. CORROSION FOU ND TO BE OUT OF LIMITS. CUT OUT DAMAGED SHEAR TIE, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-4. 2 L 7 3 4F A3WE 2001100200048 20011002 00048 NE 2001 10 2 CA010921007 2 20010816 A 7200 ENGINE BOEING 737 737281 138448P NM PWA JT8 JT8D17 52049 NE NR 1 FAILED W A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 CA (CAN) ENROUTE FROM YVR TO YYC EXPERIENCED COMPRESSOR STALL ON NR 1 ENGINE. UPON ESTABLISHING CRUISE POWER SETTNG, CREW HEARD LOUD POP, FOLLOWED 20 SEC LATER BY ANOTHER POP (SEVERE COMPRESSOR STALL) & ASSOCIATED NR 1 ENGINE PRESSURE RATIO (EPR), N1 POWER SURGES AS WELL AS LARGE THROTTLE STAGGER. THRUST REDUCED & ENGINE STABILIZED - AFTER SLOWLY INCREASING THRUST, ANOTHER STALL. QUICK REACTION CHECK (QRC) CARRIED OUT & NO FURTHER SYMPTOMS NOTED BELOW 80 PERCENT N1. MAINT C ONTROL NOTIFIED & CREW ADVISED TO CARRY ON TO YYC AT IDLE THRUST. A/C LANDED IN YYC WITH NO FURTHER INCIDENTS TO REPORT. (THERE NO INFLIGHT SHUTDOWN ON ENGINE). 2 L 7 2 4F 4 F A16WE E2EA 2001100200049 20011002 00049 NM 2001 10 2 UPS01236865 1 20010926 A 2611 LIGHT BOEING 727 727247 138408F NM CARGO BAY INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:PFLT NR 6R CARGO SMOKE LIGHT WOULD NOT ILLUMINATE PRIOR TO FLIGHT. R&R BULB IN NR 6R MAIN CARGO SMOKE DE TECTOR OPS CK OK. 2 L 7 3 4F A3WE 2001100200050 20011002 00050 EU 2001 10 2 CA010921008 1 20010919 A 7933 S483117 INDICATOR FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU OIL TEMP FALSE INDICATION W E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 CA 45267 (CAN) AIRCRAFT WAS INVOLVED IN AN INFLIGHT PRECAUTIONARY SHUTDOWN OF ONE ENGINE DUE TO AN INDICATION OF OIL TEMP INDICAT ION TO RED LINE ENROUTE TO SANDSPIT. THE TROUBLESHOOTING PROVED THAT IT WAS AN INDICATION PROBLEMM ONLY.THE AIRCRAFT WAS RETURNED TO SERVICE UNDER M.E.L FOR THE OIL TEMP INDICATOR. INDICATOR TO BE REPLACED AT A LATER DATE. 2 L 7 2 4F 4 F RT A20EU E2EU 2001100200051 20011002 00051 NM 2001 10 2 CA010921024 1 20010910 A 4997 976J5981 GENERATOR BOEING 737 737201 1384454 NM PWA JT8 JT8D9A 52048 NE APU FAILED W O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION LD LANDING 1 CA (CAN) ON LANDING INTO YYZ, PILOT STARTED THE APU BUT COULD NOT GET APU GENERATOR ON LINE. MAINTENANCE NOTIFIED AND APU G ENERATOR AND WIRING INSPECTED. IT WAS THEN DETERMINED THE WIRING AT THE FIREWALL DISCONNECT WAS BURNED AND CONNECTOR DAM AGED. AIRCRAFT WAS RELEASED UNDER M.E.L. 24-2 AND PARTS ORDERED FOR REPAIR. 2 L 7 2 4F 4 F A16WE E2EA 2001100200052 20011002 00052 NE 2001 10 2 CA010924001 2 20010818 A 7250 RB211BTRENT772 BLADE AIRBUS 330 A330323 3930335 EU RROYCE RB211 RB211TRENT77 NE RT ENGINE DAMAGED W D RETURN TO BLOCK R J PARTIAL RPM/PWR LOSS WARNING INDICATION TX TAXI/GRND HDL 1 CA R16 (CAN) AIRCRAFT RETURNED TO GATE BEFORE TAKEOFF DUE TO COMPRESSOR STALL ON THE RIGHT ENGINE. IP TURBINE BLADE FOUND DAMAG ED DURING BORESCOPE.REPLACED ENGINE, (ENGINE ROUTED TO SHOP FOR REPAIR.) 2 L 7 2 4F 4 F RT A46NM E39NE 2001100200053 20011002 00053 NM 2001 10 2 UPS01236876 1 20010917 A 3230 DRUM BOEING 727 72762C 138402C NM NLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 912UP 19244 INSPECTION TYPE:C NLG MANUAL EXTENSION AFT DRUM CORRODED. DRUM ASSY REPLACED IAW OHM 32-34-03. 2 L 7 3 4F A3WE 2001100200055 20011002 00055 2001 10 2 CA010924005 4 20010908 A 3170 HG480B13 COMPUTER BOEING 737 7372L9 1384497 NM PWA JT8 JT8D17A 52049 NE CENTRAL AIR DATA FAILED W A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 CA (CAN) ON CLIMB OUT AUTO PILOT DISENGAGED, TCAS, GROUND PROXIMITY, MACH TRIM, ALTITUDE ALERT, TOTAL AIR TEMPERATURE AND E NGINE PRESSURE RATIO GAUGES FAILED. CENTRAL AIR DATA COMPUTER (CADC) RESET BUT DID NOT FIX PROBLEM AIRCRAFT RETURNED TO YYZ. CADC REPLACED AS PRE AIRCRAFT MAINTENANCE MANUAL 34-12-00 & 34-12-11. 2 L 7 2 4F 4 F RT A16WE E2EA 2001100200056 20011002 00056 NM 2001 10 2 CA010924006 1 20010909 A 2742 R1631 ACTUATOR BOEING 737 7372T7 1384482 NM PWA JT8 JT8D17A 52049 NE STAB TRIM FAILED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA (CAN) ON DEPARTURE YYZ ATTEMPTED FORWARD HORIZONTAL STAB TRIM USING CONTROL WHEEL SWITCHES. NO FORWARD TRIM AVAILABLE, F ULL AFT TRIM OK. AUTO PILOT SEEMED ABLE TO TRIM FORWARD. STABILIZER TRIM MAIN ACTUATOR REPLACED AS PER AIRCRFT MAINTENAN CE MANUAL 27-41-71. TRIM FUNCTION CHECKED SERVICEABLE. 2 L 7 2 4F 4 F RT A16WE E2EA 2001100200057 20011002 00057 NM 2001 10 2 CA010924008 1 20010822 A 5230 SCREW BOEING 767209 BOEING 767 767209 1385127 NM PWA JT9 JT9D7R4D 52054 NE DOOR HANDLE LOOSE W O OTHER J WARNING INDICATION LD LANDING 1 CA 22681 (CAN) UPON LANDING IN TORONTO THE BULK CARGO DOOR OPENED. AFTER INVESTIGATION, FOUND TO BE 2 SCREWS LOOSE INSIDE THE DOO R HANDLE MECHANISM. SCREWS TIGHTENED SECURED. DOOR CYCLED AND FOUND OPERATIONAL. 2 L 7 2 4F 4 F RT A1NM E3NE 2001100200058 20011002 00058 NM 2001 10 2 UPS01236877 1 20010917 A 3221 TRUNNION BOEING 727 72762C 138402C NM NLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 912UP 19244 INSPECTION TYPE:C ON REMOVAL OF TRUNNION CAPS ON NLG TRUNNION AREA WHERE BUSHINGS WERE INSTALLED HAS EVIDENCE OF CORROSI ON. REPAIR CARRIED OUT IAW SRM 53-40-1, 20-20-02, & SMRO EO 2001-044-001. 2 L 7 3 4F A3WE 2001100200059 20011002 00059 WP 2001 10 2 DHL2001806015 1 20010929 A 5750 FAIRING DOUG DC8 DC873F 302199F WP A DHLA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 806DH 46002 On take off from Mexico City aborted----discrepancy R/H T/E Inboard flap, inboard actuator fairing FWD section is damage d on inboard side at mating edge, also not flush with wing surface when flaps in up position.1) Removed previous repair at actuator fairing and re-installed new doubler repair at actuator fairing R/H T/E I/B flap per DC-8 S.R.M. 51-1-21 mat erials used 2024T3 .050 P.O. 83113272 Lot # 50086/01 doubler, filler 2024T3 .040 P.O. 83113272 Lot# 50050/01.2) Check fa iring fit with T/E flaps upDC-8 M/M 27-61-0. 2 L 7 4 4F RT 4A25 2001100200060 20011002 00060 NM 2001 10 2 UPS01236890 1 20010914 A 5320 SUPPORT FITTING BOEING 727 72762C 138402C NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 912UP 19244 INSPECTION TYPE:C SUSPECT CRACKS ON LT AND RT 940 SUPPORT FRAME FITTING AT FLOOR BEAM ATTACH FLANGES. HFEC CARRIED OUT L T NDF RT CRACK CONFIRMED ON FWD I/B UPPER FLANGE. REPAIRED IAW UPS EO B727-5310-2954 A. 2 L 7 3 4F A3WE 2001100200061 20011002 00061 NM 2001 10 2 UPS01236901 1 20010917 A 3221 TRUNNION BOEING 727 72762C 138402C NM NLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 912UP 19244 INSPECTION TYPE:C ON REMOVAL OF NLG TRUNNION CAPS CORROSION WAS FOUND IN ALL FOUR BOLT HOLES FOR CLAMPING OF TRUNNION CA PS. REPAIRED IAW SMRO EO 2001-044-001 UPS 727-53-200032. 2 L 7 3 4F A3WE 2001100200062 20011002 00062 NM 2001 10 2 UPS01236902 1 20010917 A 5330 STRAP BOEING 727 72762C 138402C NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 912UP 19244 INSPECTION TYPE:C NDI INSP OF MID GALLEY DOOR CUTOUT INDICATES REINFORCING STRAP CRACK AT UPPER FWD CUTOUT. REPAIRED I AW UPS EO B727-5330-2685. 2 L 7 3 4F A3WE 2001101000006 20011010 00006 SO 2001 10 10 COMA0110147 1 20010930 A 3397 WIRE EMB 120 EMB120RT SO CABIN BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 268CA 1262 FLIGHT 5025. OVERHEAD EMERGENCY LIGHT AT ROW 8 IS INOP. REPAIRED BROKEN WIRE AT LIGHT FIXTURE. OPERATIONAL CHECK SATI SFACTORY. 2 L 7 2 4T RT A31SO 2001100200064 20011002 00064 SO 2001 10 2 COMA0110148 1 20010928 A 2750 KRP138112VT ROLLER EMB 120 EMB120RT SO R/H OUTBD WORN A COMA A UNSCHED LANDING O OTHER DE DESCENT 1 SO 01 264CA 1256 FLIGHT 5070 FLAP SELECTION BEYOND 25 DEGREES RESULTS IN FLAP DISAGREEMENT WARNING.REPLACED THE R/H OUTBD FLAP ROLLERS. SYSTEM CHECK SATISFACTORY. 2 L 7 2 4T RT A31SO 2001100200065 20011002 00065 NM 2001 10 2 UPS01236904 1 20010915 A 5312 PRESSURE PANEL BOEING 727 72762C 138402C NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 912UP 19244 INSPECTION TYPE:C NDT INSPECTION FOUND CRACK INDICATION AT BS 880 LBL18-19. STOP DRILLED AND HFEC, CRACK CONTAINED. REPA IRED IAW EO B727-5310-04 60. 2 L 7 3 4F A3WE 2001100200067 20011002 00067 SO 2001 10 2 COMA0110149 1 20010926 A 3350 LIGHT EMB 120 EMB120RT SO A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 268CA 120262 FLIGHT #5057. DURING INSPECTION; FOUND THE EMERGENCY EXIT SIGN ON OVERHEAD BIN INOPERATIVE.REPAIRED WIRING AT THE EMERG ENCY EXIT SIGN ASSEMBLY. 2 L 7 2 4T RT A31SO 2001100200070 20011002 00070 NM 2001 10 2 UPS01236905 1 20010913 A 5711 SPAR BOEING 727 72762C 138402C NM CENTER WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 912UP 19244 INSPECTION TYPE:C EVIDENCE OF CORROSION ON CENTER TANK FRONT SPAR UPPER CHORD VERTICAL FLANGE AT BS 740 RBL 25. REPAIRE D IAW SRM 51-30-02 RBL 19 TO 31. 2 L 7 3 4F A3WE 2001100200073 20011002 00073 NM 2001 10 2 UPS01236934 1 20010828 A 5312 PRESSURE PANEL BOEING 727 72725C 138400H NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:C NLG WW, BEHIND NOSE LANDING GEAR RT SIDE WALL SHOWS CRACK BETWEEN RIVETS. CUT OUT DAMAGE SECTION AS PE R B727 SRM 51-40-2. ACCOMPLISHED NDT AROUND CUT OUT AREAS, NO CRACK AS PER 727 NDT PART 6 53-00-00. INSTALLED REPAIR DO UBLER AS PER B727 SRM 51-40-2. 2 L 7 3 4F A3WE 2001100200074 20011002 00074 NM 2001 10 2 UPS01236936 1 20010829 A 5330 SKIN BOEING 727 72725C 138400H NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:C FUSELAGE INNER SKIN AT STA 1148-1166 STR 20R CRACKED AND CORRODED OUT OF LIMITS. REMOVE CORROSION FOUN D OUT OF LIMITS AS PER SRM 51-10-2, CUT OUT DAMAGED AREA AT STA 1148-1166 STR 20R AND NDT INSPECTION AS PER PART 6 51-00 -00 FIGURE 4, NO CRACK FOUND. INSTALLED REPAIR AT FUSELAGE INNER SKIN STA 1148-1166 STR 20R AS PER B727 SRM 53-30-3. 2 L 7 3 4F A3WE 2001100200079 20011002 00079 EA 2001 10 2 COMA0160758 1 20010929 A 5320 60034017351 ANGLE CNDAIR CL600 CL6002B19 EA FLOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 979CA 10406 7159 FWD/AFT J-ANGLE AT FS280 HAS CORROSION, FLOOR BEAM WEB AT FS280 HAS CORROSION.REPAIRED FWD/AFT J-ANGLES AND FLOOR BEAM W EB I/A/W WVAC EO 601R-53-2731, 601R-53-2733, 601R-53-2734. 2 L 7 2 4F RT A21EA 2001100200080 20011002 00080 NE 2001 10 2 UPS01436854 2 20010925 A 7310 FUEL LINE BOEING 747 747259B NM PWA JT9 JT9D7Q 52054 NE NR 4 ENGINE CHAFED A IPXA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 527UP 21730 INSPECTION TYPE:N/A NR 4 ENGINE HAS FUEL LEAK - TUBES TAGGED - CHAFED WITH ANOTHER TUBE. REMOVED TWO CHAFED LINES KLS 82 050 INSTALLED SERVICEABLE FUEL SIGNAL TUBE ASSY AND INSTALLED SERVICEABLE DRAIN TUBE ASSY PER AMM 30-10-10 LEAK CHECK GO OD. 2 L 7 4 4F 4 F RT A20WE E3NE 2001100200081 20011002 00081 EA 2001 10 2 COMA0160759 1 20010929 A 5320 601R3866949 DOUBLER CNDAIR CL600 CL6002B19 EA 310.00 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 979CA 10406 7159 THE DOUBLER PANEL FORWARD OF THE SERVICE DOOR IS CORRODED.REMOVED CORRODED DOUBLER AND REPLACED I/A/W WVAC E.O. 601R-53- 2732. 2 L 7 2 4F RT A21EA 2001100200082 20011002 00082 NM 2001 10 2 UPS01436857 1 20010914 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C M/D STA 1940 - 1960 STRINGER 4R FOUND CRACKED. REPAIRED FUSELAGE STRINGER BETWEEN BS 1940 TO BS 1960, S-4R AS PER RS R53-61-34689. 2 L 7 4 4F A20WE 2001100200083 20011002 00083 EA 2001 10 2 COMA0160760 1 20011001 A 5320 60034017373 ANGLE CNDAIR CL600 CL6002B19 EA FLOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 917CA 18741 7017 THE VERTICAL J ANGLE CLIP INSIDE OF CBP1 AT LBL9 WAS FOUND CRACKED.REMOVED AND REPLACED VERTICAL J ANGLE CLIP I/A/W WVAC E.O. 601R-53-2729. 2 L 7 2 4F RT A21EA 2001100200084 20011002 00084 NM 2001 10 2 UPS01436858 1 20010908 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C AFT CARGO BAY BS 1500 LT STR 39 FRAME WEB FOUND CRACKED. AFT CARGO COMPT BS 1500 LT FRAME S33L - S39L AREA REPAIRED AS PER SRM 5310-04 FIG 66. 2 L 7 4 4F A20WE 2001100200085 20011002 00085 NM 2001 10 2 UPS01436859 1 20010917 A 5310 SHEAR TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C M/D, SHEAR TIE CRACKED, BETWEEN S-3R AND S-4R STA 1960. SHEAR TIE REPLACED PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001100200086 20011002 00086 EA 2001 10 2 COMA0160761 1 20011001 A 5720 601R10045 SKIN CNDAIR CL600 CL6002B19 EA WS95.950 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 979CA 10406 7159 R/H LOWER WING FUEL TANK ACCESS HOLE (640DB) HAS CORROSION ON FORWARD AND AFT CUT-OUT AREAS.REPAIRED R/H LOWER WING FUEL TANK ACCESS HOLE (640DB) I/A/W CANADAIR R.E.O. 601R-57-21-148 AND 601R-57-21-030 REV A. 2 L 7 2 4F RT A21EA 2001100200087 20011002 00087 EA 2001 10 2 COMA0160762 1 20011001 A 2120 APU CNDAIR CL600 CL6002B19 EA A COMA O OTHER O OTHER DE DESCENT 1 SO 01 927CA 7031 FLIGHT 5296. DURING DESCENT INTO CVG AND AFTER THE APU WAS STARTED; STRONG ODOR OF FUEL THROUGHOUT THE ENTIRE AIRCRAFT. INSPECTED FUEL SYSTEM FOR POSSIBLE LEAKS, OPERATED APU AND AIR CONDITIONING SYSTEM, DISCREPANCY COULD NOT BE DUPLCIATED BY MAINTENANCE, NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2001100200088 20011002 00088 EA 2001 10 2 COMA0160763 1 20011001 A 2120 COMPRESSOR CNDAIR CL600 CL6002B19 EA A COMA K NONE O OTHER DE DESCENT 1 SO 01 796CA 7338 FLIGHT 5654. DURING DESCENT INTO CVG STRONG SMELL OF ENGINE OIL AND VISIBLE LIGHT ENGINE OIL SMOKE. AFTER TRANSFERRING TO ENGINE BLEED AIR, SMOKE AND SMELL DISAPPEARED.PERFORMED COMPRESSOR WASH OF THE RIGHT ENGINE. 2 L 7 2 4F RT A21EA 2001100200092 20011002 00092 EA 2001 10 2 COMA0160764 1 20011001 A 5270 SHAFT CNDAIR CL600 CL6002B19 EA A COMA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SO 01 798CA 7348 FLIGHT 5891. DURING CLIMB-OUT OF CVG; RECEIVED A CABIN DOOR OUTER HANDLE CAUTION MESSAGE, AIRCRAFT RETURNED TO THE FIEL D.REMOVED EXCESSIVE GREASE FROMT HE DOOR HANDLE SHAFT MECHANISM. 2 L 7 2 4F RT A21EA 2001100200096 20011002 00096 EA 2001 10 2 COMA0160765 1 20011001 A 2751 FLAP CNDAIR CL600 CL6002B19 EA A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 420CA 7451 FLIGHT 5489. RECEIVED FLAP FAIL CAUTION WITH FLAPS AT 28 DEGREES DURING TAXI AFTER LANDING. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 1,2,3, (A,B,C AND E). FLAP SYSTEM WAS RESET WITH NO FURHTER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2001100200101 20011002 00101 NM 2001 10 2 UPS01436860 1 20010910 A 5411 654116662413 FRAME BOEING 747 747121 1384871 NM NR 2 PYLON WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C NR 2 ENG FWD BHD FOR ENG FRONT MOUNT ATTACH, THE I/B CHORD LOWER SECTION HAS A MINOR DENT MARK WHICH W AS PREVIOUSLY SMOOTHED OUT. NDT INSP FOUND THE THICKNESS OF THE CHORD WORN OUT 25% APPROX IT'S OUT OF SRM LIMIT 54-10-01 FIG 1. THE FWD ENGINE MOUNT ATTACHED BHD CHORD WAS REPLACED IAW SRM 51-10-01 PG 8. THE ENGINE FWD MOUNT FTGS ( I/B AND O/B ) WERE REFITTED PER MM 20-51-01 AND THE ANTI-ICING DUCT WAS REFITTED AND LEAK CHK CARRIED OUT PER MM 30-21-06. 2 L 7 4 4F A20WE 2001100200108 20011002 00108 EA 2001 10 2 COMA0160766 1 20010930 A 2751 FLAP CNDAIR CL600 CL6002B19 EA A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 420CA 7451 FLIGHT 5489. FLAP FAIL CAUTION AFTER LANDING AT CAK.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTE NANCE ACTION, PARAGRAPH (B) 1,2,3, (A,B,C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2001100200109 20011002 00109 NM 2001 10 2 UPS01436862 1 20010910 A 5280 SKIN BOEING 747 747121 1384871 NM LT MLG DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C LT BLG I/B W/W DOOR I/B REAR FACE NEAR MID END AREA FOUND CRACK AND BULGE UP AS MARKED. LT BLG I/B W/W DOOR I/B REAR FACE SKIN PNL REPAIRED PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 2001100200113 20011002 00113 2001 10 2 COMA0160767 4 20010930 A 3418 607300001 TRANSDUCER CNDAIR CL600 CL6002B19 EA COCKPIT FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SO 01 735CA 6470 7267 FLIGHT #5078. STALL FAIL CAUTION MESSAGE DUIRNG CLIMB OUT OF MCO, AIRCRAFT RETURNED TO THE FIELD.REPALCED THE # MACH. T RANSDUCER. 2 L 7 2 4F RT A21EA 2001100200116 20011002 00116 NM 2001 10 2 UPS01436863 1 20010911 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C AFT CARGO BAY STR 51R FOUND CORROSION AT STA 1880. AFT CARGO COMPT STR 51R AT BS 1870 - 1890 REPAIR PE R SRM 53-10-03 FIG 8. 2 L 7 4 4F A20WE 2001100200119 20011002 00119 NM 2001 10 2 UPS01436864 1 20010907 A 5320 INTERCOSTAL BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C M/D, NLG W/W TOP PANEL INTERCOSTAL AT BS 290 LBL 21 1EA STAND OFF HOLE CRACKED. INTERCOSTAL REPLACED P ER SRM 51-10-01. 2 L 7 4 4F A20WE 2001100200120 20011002 00120 EA 2001 10 2 COMA0160768 1 20010928 A 2410 IDG CNDAIR CL600 CL6002B19 EA A COMA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 958CA 7111 FLIGHT 5673. DURING TAKE OFF ROLL, RECEIVED AN INTEGRATED DRIVE GENERATOR #1 CAUTION MESSAGE, TAKE OFF WAS ABORTED AT 7 0 KNOTS AND RETURNED TO THE GATE.#1 IDG MESSGE CLEARED, IDG DID NOT AUTO DISCONNECT, NO FAULTS FOUND, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2001100200121 20011002 00121 EA 2001 10 2 COMA0160769 1 20010930 A 3350 BR9279232 LIGHT CNDAIR CL600 CL6002B19 EA A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 918CA 7018 FLIGHT 5362. DURING INSPECTION FOUND THE FLOOR EMERGENCY EXIT FLOOR LIGHT BY THE CABIN DOOR INOPERATIVE.REPLACED FAULTY LIGHT ASSEMBLY. 2 L 7 2 4F RT A21EA 2001100200122 20011002 00122 NM 2001 10 2 UPS01436885 1 20010910 A 5310 DOOR FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C M/D, MED NR 1L CUTOUT FWD FRAME BS 434 1EA HOLE CRACK AT FRAME WEB. REPAIRED FRAME WEB AT LT BS 434 S- 21L TO S-26L AS PER SRM 53-10-04 FIG 99. 2 L 7 4 4F A20WE 2001100200123 20011002 00123 NM 2001 10 2 UPS01436886 1 20010911 A 5230 SKIN BOEING 747 747121 1384871 NM CARGO DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C REF EO B747-5330-13494, REMOVE EXISTING REPAIR AND ACCOMPLISH SRM REPAIR AT BS 662 670 STR 30R - 33R D UE EXISTING REPAIR FOUND STRUCTURALLY UNSATISFACTORY. FWD CARGO COMPT DOOR OUTER SKIN AT BS 662 - BS 670 STRINGER 30R - S34R AREA REPAIRED AS PER SRM 52-00-03 FIG 4. 2 L 7 4 4F A20WE 2001100200124 20011002 00124 EA 2001 10 2 COMA0160770 1 20010930 A 5300 SKIN CNDAIR CL600 CL6002B19 EA A COMA C ABORTED TAKEOFF C F.O.D. TO TAKEOFF 1 SO 01 784CA 7319 FLIGHT 5774. BIRDSTRIKE DURING T/O. T/O ABORTED.C/W BIRDSTRIKE INSPECTION. NO DAMAGE FOUND. C/W REJECTED T/O INSPECTI ON NO DAMAGE FOUND. 2 L 7 2 4F RT A21EA 2001100200125 20011002 00125 NM 2001 10 2 UPS01436887 1 20010912 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C REFER EO B747-5330-13494, REMOVE EXISTING REPAIR AND ACCOMPLISH SRM REPAIR AT BS 1950 - 1960, STR 3R - 4R, DUE EXISTING REPAIR FOUND STRUCTURALLY UNSATISFACTORY. FUSELAGE SKIN AT BS 1946 TO BS 1960 STRINGER 3R - 4R AREA RE PAIRED AS PER SRM 53-30-03 FIG 48. 2 L 7 4 4F A20WE 2001100200126 20011002 00126 NM 2001 10 2 UPS01436888 1 20010911 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C REFER EO B747-5330-13494, REMOVE EXISTING REPAIRS AND ACCOMPLISH SRM REPAIR AT BS 1605 STR 44L - 45L AND BS 1610 STR 44L - 45L, DUE EXISTING REPAIR FOUND STRUCTURALLY UNSATISFACTORY. 2 L 7 4 4F A20WE 2001100200127 20011002 00127 NM 2001 10 2 UPS01436889 1 20010911 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C REFER EO B747-5330-13494, REMOVE EXISTING REPAIR AND ACCOMPLISH SRM REPAIR AT BS 920 - 940, STR 39L, D UE EXISTING REPAIR FOUND STRUCTURALLY UNSATISFACTORY. FUSELAGE SKIN AT BS 920 - 940 STRINGER 39L AREA REPAIRED AS PER SR M 53-30-03 FIG 11. 2 L 7 4 4F A20WE 2001101000007 20011010 00007 EA 2001 10 10 COMA0160755 1 20010923 A 5346 BEAM CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 931CA 17257 7037 CRACKS FOUND ON LT AND RT SIDES OF ENGINE SUPPORT BEAM. REPAIRED LT AND RT SIDES OF ENGINE SUPPORT BEAM IAW CANADAIR RE O 601R-53-61-366 REV C. 2 L 7 2 4F RT A21EA 2001101000010 20011010 00010 EA 2001 10 10 COMA0160756 1 20010929 A 5320 WEB CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 931CA 17257 7037 CRACK FOUND ON UPPER WEB FS 630, LBL 9. PERFORMED TEMPORARY REPAIR TO UPPER AND LOWER WEBS FS 630, LBL 9 IAW CANADAIR R EO 601R-53-61-345. 2 L 7 2 4F RT A21EA 2001101000011 20011010 00011 EA 2001 10 10 COMA0160757 1 20010929 A 5320 WEB CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 931CA 17257 7037 CRACK FOUND ON UPPER WEB FS 640, RBL 18. CUT OUT DAMAGED WEB, LP1 AND RESTORED FINISH IAW CANADAIR REO 601R-53-61-439. (TEMPORARY REPAIR). 2 L 7 2 4F RT A21EA 2001100200128 20011002 00128 NM 2001 10 2 UPS01436891 1 20010911 A 5230 SKIN BOEING 747 747121 1384871 NM CARGO DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C REFER EO B747-5330-13494, REMOVE EXISTING REPAIR AND ACCOMPLISH SRM REPAIR AT BS 670 STR 33R - 34R, DU E EXISTING REPAIR FOUND STRUCTURALLY UNSATISFACTORY. FWD CARGO COMPT DOOR OUTER SKIN AT BS 662 - 670 STRINGER 30R - 34R AREA REPAIRED AS PER SRM 52-00-03 FIG 4. 2 L 7 4 4F A20WE 2001100200129 20011002 00129 NM 2001 10 2 UPS01436892 1 20010911 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C REFER EO B747-5330-13494, REMOVE EXISTING REPAIR AND ACCOMPLISH SRM REPAIR AT BS 740 - 750, STR 34R DU E EXISTING REPAIR FOUND STRUCTURALLY UNSATISFACTORY. FUSELAGE SKIN AT BS 740 - 750 STRINGER 34R AREA REPAIRED AS PER SRM 53-30-03 FIG 48. 2 L 7 4 4F A20WE 2001100200130 20011002 00130 NM 2001 10 2 UPS01436893 1 20010910 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C REFER EO B747-5330-13494, REMOVE EXISTING REPAIR AND ACCOMPLISH SRM REPAIR AT BS 140 - 150, STR 15L - 19L, DUE TO EXISTING REPAIR FOUND STRUCTURALLY UNSATISFACTORY. FUSELAGE SKIN AT BS 140 - BS 150 S15L - 19L AREA REPAIRED AS PER SRM 5303 FIG 1. 2 L 7 4 4F A20WE 2001100200131 20011002 00131 NM 2001 10 2 UPS01436894 1 20010908 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C - EXTERIOR SKIN FOUND A NON STANDARD REPAIR PATCH AT BS 140 - 150 S15L - 19L AREA. FUSELAGE SKIN AT BS 140 - 150 STRINGER 15L - 19L. AREA REPAIRED AS PER SRM 53-30-03 FIG 1. 2 L 7 4 4F A20WE 2001100200132 20011002 00132 NM 2001 10 2 UPS01436895 1 20010910 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C REFER EO B747-5330-13494, REMOVE EXISTING REPAIR AND ACCOMPLISH SRM REPAIR AT BS825 - 835 STR 47L - 47 R DUE TO EXISTING REPAIR FOUND STRUCTURALLY UNSATISFACTORY. FUSELAGE SKIN AT BS 825 - 835 S47L - 47R AREA REPAIRED AS PE R SRM 53-30-03 FIG 1. 2 L 7 4 4F A20WE 2001100200133 20011002 00133 NM 2001 10 2 UPS01436896 1 20010910 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C REFER EO B747-5330-13494, REMOVE EXISTING REPAIR AND ACCOMPLISH SRM REPAIR AT BS 140 - 150 STR 30R - 3 4R DUE EXISTING REPAIR FOUND STRUCTURALLY UNSATISFACTORY. FUSELAGE SKIN AT BS 140 - BS 150 STRINGER 30R TO S40R AREA REP AIRED AS PER SRM 53-30-03 FIG 1 2 L 7 4 4F A20WE 2001100200134 20011002 00134 NM 2001 10 2 CALA0100911 1 20011001 A 5720 SPLICE BOEING 737 7373T0 1384582 NM #3 FLAP TRK CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 INSPECTION FOUND A 5" CRACK IN #3 FLAP TRACK FAIRING SPLICE. THE #3 FAIRING SPLICE WAS REMOVED AND REPLACED IAW SRM 51-1 0-02. 2 L 7 2 4F RT A16WE 2001100200135 20011002 00135 NM 2001 10 2 CALA0100912 1 20011001 A 5720 STIFFENER BOEING 737 7373T0 1384582 NM #3 FLAP TRK CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 INSPECTION FOUND A 5" CRACK IN ANGLE STIFFENER INSIDE #3 FLAP TRACK FAIRING. THE ANGLE STIFFENER WAS REMOVED AND REPLACE D IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 2001100200136 20011002 00136 NM 2001 10 2 CALA0100913 1 20011001 A 5320 ANGLE BOEING 737 7373T0 1384582 NM STA 312-344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 INSPECTION FOUND L-1 DOORWAY ANGLE CORRODED AT STA 312-344, LBL 60. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001100200137 20011002 00137 NM 2001 10 2 CALA0100914 1 20011001 A 5720 STIFFENER BOEING 737 7373T0 1384582 NM #6 FLAP TRK CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 INSPECTION FOUND AN 8" CRACK IN STIFFENER LOCATED JUST FORWARD OF HORSE COLLAR IN #6 FLAP TRACK FAIRING. THE STIFFENER W AS REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001100200138 20011002 00138 NM 2001 10 2 CALA0100915 1 20011001 A 5320 ANGLE BOEING 737 7373T0 1384582 NM STA 298-328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 INSPECTION FOUND ANGLE BELOW SCUFF PLATE AREA OF R-1 DOOR JAMB CORRODED AT STA 298-328. THE ANGLE WAS REMOVED AND REPLAC ED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001100200139 20011002 00139 NM 2001 10 2 CALA0100916 1 20011001 A 5320 FITTING BOEING 737 7373T0 1384582 NM STA 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 INSPECTION FOUND L-1 DOOR GIRT BAR LATCH ATTACH FITTING CORRODED AT STA 344. THE ATTACH FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001100200140 20011002 00140 NM 2001 10 2 CALA0100917 1 20011001 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM STA 360-380 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 INSPECTION FOUND L/H O/B SEAT TRACK CORRODED AT STA 360-380. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52. 2 L 7 2 4F RT A16WE 2001100200141 20011002 00141 NM 2001 10 2 CALA0100918 1 20011001 A 5320 CHANNEL BOEING 737 7373T0 1384582 NM STA 312-344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 INSPECTION FOUND U-CHANNEL UNDER L-1 DOOR THRESHOLD CORRODED AT STA 312-344. THE CHANNEL WAS REPLACED IAW SRM 51-40-00. 2 L 7 2 4F RT A16WE 2001100200142 20011002 00142 NM 2001 10 2 UPS01436897 1 20010912 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C REFER EO B747-5330-13494, REMOVE EXISTING REPAIR AND ACCOMPLISH SRM REPAIR AT BS 220 STR 15R - 17R DUE EXISTING REPAIR FOUND STRUCTURALLY UNSATISFACTORY. REPAIRED FUSELAGE SKIN AS PER SRM 53-30-03 FIG 47. 2 L 7 4 4F A20WE 2001100200143 20011002 00143 WP 2001 10 2 MWEA011324 1 20011001 A 2730 9918450505 FLANGE DOUG DC9 DC981 3022081 WP RIGHT ELEVATOR BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 RIGHT ELEVATOR FORWARD SPAR LOWER VERTICAL FLANGE IS BENT AND CRACKED AT SECOND FROM OUTBOARD HINGE POINT. -- FABRICAT ED AND INSTALLED ANGLE REPAIRS, RIB, AND FILLER. 2 L 7 2 4F A6WE 2001100200144 20011002 00144 WP 2001 10 2 MWEA011330 1 20011001 A 5330 59114153 SKIN DOUG DC9 DC981 3022081 WP STATION 551 GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 CABIN FUSELAGE SKIN AT STATION 551 ABOVE LONGERON 7 RIGHT HAS A DEEP GOUGE. -- FABRICATED AND INSTALLED REPAIR DOUBLER . 2 L 7 2 4F A6WE 2001100200145 20011002 00145 WP 2001 10 2 MWEA011333 1 20011001 A 5340 593056675 SEAT TRACK DOUG DC9 DC981 3022081 WP STATION 1134 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 CABIN NUMBER 2 SEAT TRACK AT STATION 1134 IS DAMAGED BEYOND LIMITS DUE TO REMOVAL OF G.3 GALLEY MOUNT. -- FABRICATED A ND INSTALLED SEAT TRACK AND SPLICE. 2 L 7 2 4F A6WE 2001100200146 20011002 00146 WP 2001 10 2 MWEA011336 1 20011001 A 5710 5911301505 SPAR DOUG DC9 DC981 3022081 WP STATION 164 UNSERVICEABLE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 PREVIOUS REPAIR AT LEFT WING STATION 164 THAT STRADDLES #3 FLAP HINGE, AND ON THE AFT WING SPAR IN THE SAME AREA. -- R EMOVED AND REPLACED SPAR TEE SECTION AND SPLICE. FABRICATED AND INSTALLED WEB SPLICE REPAIR. 2 L 7 2 4F A6WE 2001100200147 20011002 00147 NM 2001 10 2 UPS01436927 1 20010912 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C REFER EO B747-5330-13494, REMOVE EXISTING REPAIR AND ACCOMPLISH SRM REPAIR AT BS 1898 - 1906, STR 41R - 42R, DUE EXISTING REPAIR FOUND STRUCTURALLY UNSATISFACTORY. BS 1898 - 1920 STR 39R - 42R SKIN CRACKED AREA TRIMMED OFF AND CRACK FREE CHECKED BY NDT, SKIN REPAIR CARRIED OUT AS PER SRM 52-00-03 FIG 4. 2 L 7 4 4F A20WE 2001100200148 20011002 00148 NM 2001 10 2 UPS01436928 1 20010912 A 5230 SKIN BOEING 747 747121 1384871 NM CARGO DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C REFER EO B747-5330-13494, REMOVE EXISTING REPAIR AND ACCOMPLISH SRM REPAIR AT BS 1906 - 1920, STR 39R - 42R DUE EXISTING REPAIR FOUND STRUCTURALLY UNSATISFACTORY. AFT CARGO COMPT DOOR OUTER SKIN AT BS 1886 - BS 1920 STRING ER 39R - S42R AREA REPAIRED AS PER SRM 52-00-03 FIG 4. 2 L 7 4 4F A20WE 2001100200149 20011002 00149 NM 2001 10 2 UPS01436929 1 20010926 A 3350 SIGN BOEING 747 747200 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT SIGN DOES NOT ILLUMINATE WHEN SELECTED ON. 2 L 7 4 4F RT A20WE 2001100200150 20011002 00150 NM 2001 10 2 UPS01436945 1 20010911 A 5310 SHEAR TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C FWD CARGO COMPARTMENT STA 980 RT STR 45 - 46 FRAME SHEAR TIE CORROSION AND CRACK FOUND AS MARKED. THE CORRODED SHEAR TIE WAS TRIMMED OFF, AND WAS REPAIRED AS PER SRM 53-10-04 FIG 3 HFEC INSP CONFIRMED CRACK FREE AS PER NTM PT6, 51-00-00 FIG 4. 2 L 7 4 4F A20WE 2001100200151 20011002 00151 NM 2001 10 2 UPS01436946 1 20010913 A 5320 65B0794232 STIFFENER BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C NOSE TUNNEL BTN BS 280 - 300 RT VERT BEAM NR 1 LONG STIFFENER FOUND CRACKED. STIFFENER REPLACED IAW SR M 51-10-01. 2 L 7 4 4F A20WE 2001101500139 20011015 00139 NE 2001 10 15 UPS01536933 2 20010928 A 7200 COMPRESSOR BOEING 757 75724APF 1384969 NM PWA 2037 PW2040 NE LT ENGINE STALLED A IPXA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 01 432UP 25463 LT ENGINE SHUTDOWN DUE TO COMPRESSOR STALLS, A/C DIVERTED TO BIL. R AND R NR 1 ENGINE PER TASK CARD 5001 PW OK FOR SERVICE 2 L 7 2 4F 4 F RT A2NM E17NE 2001100200152 20011002 00152 WP 2001 10 2 UPS01836714 1 20010810 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 STA 1030-1080 LBL 24 SEAT TRACK IS CORRODED BEYOND LIMITS. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8 A. 2 L 7 4 4F RT 4A25 2001100200153 20011002 00153 WP 2001 10 2 UPS01836715 1 20010815 A 5320 57510403 PAN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 L-2 DOOR LOWER PAN IS CRACKED AT STA 1630 LONG 21L. REPAIRED PAN IAW SRM 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 2001100200154 20011002 00154 WP 2001 10 2 UPS01836721 1 20010828 A 3350 6012235 RELAY DOUG DC8 DC871F 302199D WP CABIN FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:ASE DURING MX INSPECTION FOUND EMERGENCY LIGHTS FAILING OPERATIONAL TEST. CAUSE FOUND TO BE A STICKING E MERGENCY LIGHT CONTROL RELAY. REMOVED AND REPLACED THE EMERGENCY LIGHTING BATTERY AND RELAY UNIT 2 L 7 4 4F RT 4A25 2001100200155 20011002 00155 WP 2001 10 2 UPS01836722 1 20010806 A 5730 5769859U164 PAN DOUG DC8 DC873F 302199F WP RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 RT WING IB SLOT PAN HAS INTERGRANULAR CORROSION AT XS 250. REMOVED AND REPLACED PAN IAW DWG 5769859 , AND SRM 51-1-21, 51-3-0. 2 L 7 4 4F RT 4A25 2001100200156 20011002 00156 WP 2001 10 2 UPS01836726 1 20010828 A 3350 RELAY DOUG DC8 DC871F 302199D WP COCKPIT FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:IN EMERGENCY LIGHTS FAILED OPS CHECK, FOUND EMERGENCY LIGHT CONT RELAY STICKING. R&R EMERGENCY LIGHTING BATTERY AND RELAY UNIT AND PERFORMED OPS CK PER MM 33-50-01 PARA 2 & 4 OPS CKS NORMAL. 2 L 7 4 4F RT 4A25 2001100200157 20011002 00157 WP 2001 10 2 UPS01836730 1 20010805 A 5712 5769857 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 RT WING L/E UPPER RIB CAP IS CRACKED AT XS 467. REMOVED,FABRICATED,AND REPLACED RIB CAP IAW SRM 57- 3-3 FIG 4, 51-1-21, 51-1-20D, 57-1-0. 2 L 7 4 4F RT 4A25 2001100200158 20011002 00158 WP 2001 10 2 UPS01836731 1 20010806 A 5320 3642974501 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 STA 680 WING BOX TO FRAME SUPPORT FITTING IS CRACKED BELOW LONG 21L. REMOVED AND REPLACED FITTING I AW DWG 3642974, AND SRM 51-1-20D, 51-3-0. 2 L 7 4 4F RT 4A25 2001100200159 20011002 00159 WP 2001 10 2 UPS01836740 1 20010830 A 5310 SHEAR TIE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 STA 640 SHEAR TIE IS CRACKED BETWEEN LONG 26L-27L. REPAIRED SHEAR TIE IAW SRM 53-2-0 FIG 2A AND 2B. 2 L 7 4 4F RT 4A25 2001100200160 20011002 00160 WP 2001 10 2 UPS01836742 1 20010807 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 STA 798 FLOORBEAM IS CORRODED BEYOND LIMITS AT LBL 60. REPAIRED FLOORBEAM IAW 8110-3 APPROVED DH SK 809-212. 2 L 7 4 4F RT 4A25 2001100200161 20011002 00161 WP 2001 10 2 UPS01836743 1 20010813 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 FITTING CORRODED AT FASTENER HOLE FWD SIDE AT STA 1480R IN CUSP AREA. REMOVED & REPLACED FITTING IAW DAC DWG 4640162. 2 L 7 4 4F RT 4A25 2001100200162 20011002 00162 WP 2001 10 2 UPS01836749 1 20010813 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 CUSP FITTING BTW STA 1080R & 1100R SUSPECTED CRACK. REPAIRED AREA IAW DC8 SRM 53-2-5. 2 L 7 4 4F RT 4A25 2001100200163 20011002 00163 WP 2001 10 2 UPS01836757 1 20010814 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 FWD CARGO PIT FS 300 BETWEEN LONG 34R-35R ZEE FITTING IS CORRODED. REMOVED & REPLACED ZEE FITTING FAB BED SPLICES IAW DC8 SRM 53-2-2. 2 L 7 4 4F RT 4A25 2001100200164 20011002 00164 WP 2001 10 2 UPS01836760 1 20010816 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 FWD PIT STA 280-300 L35R HAS AREA OF CORROSION. REMOVED DAMAGED SECTION OF LONGERON SPLICED NEW SECTI ON IAW SRM 53-2 -2. 2 L 7 4 4F RT 4A25 2001100200165 20011002 00165 WP 2001 10 2 UPS01836762 1 20010816 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 FWD PIT STA 320 L35L INBD FWD CORNER OF Z FITTING HAS CORROSION & CRACK. RMVD ZEE FITTING IAW DC8 SRM 51-1-20D FABRICATE SPLICES IAW DC8 SRM 53-2-0, INSTALLED ZEE FITTING/SPLICES IAW DC8 SRM 53-2-0 & 51-1-20D 2 L 7 4 4F RT 4A25 2001100200166 20011002 00166 WP 2001 10 2 UPS01836773 1 20010806 A 5320 4750521U1 SPLICE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 STA 680-700 LONG 1 SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG4750521, AND SRM 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 2001100200167 20011002 00167 WP 2001 10 2 UPS01836786 1 20010810 A 5320 4772397U1 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 STA 1766 LONG 17R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397U1. 2 L 7 4 4F RT 4A25 2001100200168 20011002 00168 NM 2001 10 2 AWXA200100491 1 20010906 A 5344 6573748 SKIN BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 22651 YVR - C19 CK - "C" - L2 DOOR, FUSELAGE TORQUE BOX INNER SKIN 2" CRACK BS 952, BETWEEN STR 11R & 12R. MAINTENANCE FABRIC ATED REINFORCEMENT STRAP AND INSTALLED IAW AWA ER 15-5345-01264-TB4, REFERENCING PROCEDURES IN BOEING SB 737-53-1094. 2 L 7 2 4F RT A16WE 2001100300007 20011003 00007 WP 2001 10 3 ABXA010517 1 20010927 A 3350 60030451 POWER SUPPLY DOUG DC9 DC932 3022066 WP FUSELAGE DEFECTIVE A ABXA K NONE O OTHER CR CRUISE 1 GL 23 985AX 1024 47522 EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE IN THE ON POSITION. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY IAW DC-9 MM. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001100300013 20011003 00013 WP 2001 10 3 UPS01836741 1 20010829 A 5753 SKIN DOUG DC8 DC873F 302199F WP T/E FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 RT EXHAUST GATE IS CRACKED AT IB T/E. REPAIRED SKIN IAW DC8-5720-7767-A. 2 L 7 4 4F RT 4A25 2001100300014 20011003 00014 WP 2001 10 3 UPS01836744 1 20010813 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 AFT PIT STA 1200-1220 L34L-L35L SKIN & FITTING CORRODED. REMOVED CORROSION, OUT OF LIMITS. REMOVED FI TTING. RECEIVED NEW FITTING P/N 3755845-1N. FAB REPAIR ANGLE IAW DC8 SR M 53-2-0. INSTALLED FITTING IAW DC8 SRM 51-1-8 & 51-1-20D 2 L 7 4 4F RT 4A25 2001100300015 20011003 00015 WP 2001 10 3 UPS01836745 1 20010814 A 5510 STIFFENER DOUG DC8 DC873F 302199F WP HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 RT HORIZ STAB LE INBD END AT FUSELAGE CRACKED. REMOVED STIFFENER, TRACK & TRACK BEARING & SHIMS IAW D C8 51. FABBED & INSTALLED NEW STIFFENER P/N 5654501 IAW DC8 SRM 51-1-20D. REINSTALLED TRACK SHIMS AND NEW TRACK BEARING IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001100300020 20011003 00020 WP 2001 10 3 UPS01836747 1 20010814 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 MAIN CABIN LT CUSP AT STA 1260 HAS CORROSION ON FRAME FITTING AROUND FASTENERS. REMOVED CORROSION, NO T OUT OF LIMITS. REMOVED FITTING AND INSTALLED NEW PART. 2 L 7 4 4F RT 4A25 2001100300021 20011003 00021 NM 2001 10 3 DHL2001712015 1 20010928 A 2797 BACC13AP6E538 WIRE BOEING 727 72729 1384007 NM FLIGHT CONTROLS BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 ON WALK AROUND FOUND LT AILERON BUSS CABLE BROKEN, LT MLG W/W.R&R LT AILERON BUSS CABLE (CORRODED)R&R RT AILERON BUSS CA BLE AS PRECUTION. 2 L 7 3 4F A3WE 2001100300024 20011003 00024 WP 2001 10 3 UPS01836748 1 20010814 A 5730 PANEL DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 LT UPPER DINEDRAL CRACKED. REMOVED FILLET ATTACH ANGLE IAW DC8 SRM 51-1-20D & 51-1-21. REMOVED DAMAGE D AREA. FABBED REPAIR FILLER IAW REO G08337. FABBED REPAIR DOUBLERS IAW TIMCO REO G08337. CUT OUT AREA IAW DC8 SRM 51-1- 8. INSTALLED ALL REPAIR PARTS IAW REO G0 8337. 2 L 7 4 4F RT 4A25 2001100300026 20011003 00026 WP 2001 10 3 UPS01836758 1 20010814 A 5320 ATTACH ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 FWD CARGO PIT AT FS 280 AT L31R-33R DOORWAY FWD TORQUE BOX WEB LWR ATTACH ANGLE IS CORRODED. REMOVED & REPLACED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001100300027 20011003 00027 NM 2001 10 3 C1HA200192007 1 20010905 A 3350 900542 BATTERY BOEING 727 727212 138407G NM A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 Row 8 Overhead Emergency Exit Light Inoperative. Action Taken: Replaced Battery Power Supply Illumination. 2 L 7 3 4F A3WE 2001100300028 20011003 00028 WP 2001 10 3 UPS01836759 1 20010815 A 5320 STRUCTURE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 FLC AT STA 612-620 AT L36 CORRODED. REPAIRED IAW REO G08340. 2 L 7 4 4F RT 4A25 2001100300029 20011003 00029 NM 2001 10 3 C1HA200192006 1 20010904 A 3350 900542 BATTERY BOEING 727 727212 138407G NM A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 Left Hand Forward and Aft Overwing Emergency Exit Lights Inoperative. Action Taken: Removed and replaced emergency lig ht power supply. Ops Checks good In accordance with 33-50-22. 2 L 7 3 4F A3WE 2001100300030 20011003 00030 NM 2001 10 3 C1HA200182012 1 20010924 A 3350 1000677 LIGHT BOEING 727 7272S7 138407Z NM A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 682CA 22019 Forward Emergency Ceiling light inop. Action Taken: Removed and replaced battery pack chg in accordance with MM 33-50- 01. Ops checks good. 2 L 7 3 4F A3WE 2001100300031 20011003 00031 2001 10 3 C1HA200183006 4 20010925 A 2564 6013211 BATTERY BOEING 727 7272S7 138407Z NM A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 683CA 22490 L2 and R2 slide lights inop. Action Taken: Removed and replaced power supply for L2 and R2 slide lights. Ops checks g ood per MM. 2 L 7 3 4F A3WE 2001100300032 20011003 00032 NM 2001 10 3 C1HA200184010 1 20010916 A 3350 900542 BATTERY BOEING 727 7272S7 138407Z NM A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 684CA 22491 #2 FWD O/H EMERGENCY EXIT LIGHT INOP. ACTION TAKEN: REMOVED AND REPLACED O/H EMERGENCY EXIT LIGHT CHARGER AND BATTERY IAW MM 33-50-71. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2001100300033 20011003 00033 NM 2001 10 3 C1HA200184011 1 20010916 A 3350 900542 BATTERY BOEING 727 7272S7 138407Z NM A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 684CA 22491 FWD O/H EMERGENCY EXIT LIGHT INOP. ACTION TAKEN: REMVOED AND REPLACED OVERHEAD EMERGENCY EXIT LIGHT CHARGER AND BATTER Y IAW MM 33-50-71. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2001100300034 20011003 00034 NM 2001 10 3 C1HA200185011 1 20010919 A 3350 900542 BATTERY BOEING 727 7272S7 138407Z NM A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 685CA 22492 R2 EMERGENCY EXIT SIGN INOP. ACTION TAKEN: REMOVED AND REPLACED BATTERY PACK AND CHARGER PER MM 33-50-1. 2 L 7 3 4F A3WE 2001100300035 20011003 00035 2001 10 3 UPS01836761 4 20010904 A 2565 BAR DOUG DC8 DC873F 302199F WP EVAC SLIDE STUCK A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:PFLT EVACUATION SLIDE BAR STUCK IN THE EVAC SLIDE, UNABLE TO ARM SLIDE. REPLACED EVAC SLIDE. 2 L 7 4 4F RT 4A25 2001100300036 20011003 00036 WP 2001 10 3 UPS01836764 1 20010904 A 5414 PANEL DOUG DC8 DC873F 302199F WP NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:PFLT NR 1 ENGINE PYLON RT SIDE AT FORWARD EDGE OF REMOVED PANEL. STRUCTURE UNDERNEATH HAS A CRACK ON LOW ER FORWARD CORNER. PANEL HAS PREVIOUS DOUBLER INSTALLED AND SECURED, REFERENCE EO DC8-5430-0461C TRANSFERRED TO FERRY P ERMIT FOR PERMANENT REPAIR. 2 L 7 4 4F RT 4A25 2001100300037 20011003 00037 WP 2001 10 3 UPS01836774 1 20010806 A 5730 DOUBLER DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C1,3 LT WING FUEL PANEL 505F INTERNAL DOUBLER IS CRACKED AT XRS 12 AT STRINGER 5-6 AREA ON WING. REPAIRE D DOUBLER IAW SRM 57-2-1 FIG 36. 2 L 7 4 4F RT 4A25 2001100300038 20011003 00038 WP 2001 10 3 UPS01836787 1 20010811 A 5320 3755847501N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 STA 1152 LONG 33R BANANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755847, AND SRM 51-1-20D, 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 2001100300039 20011003 00039 WP 2001 10 3 UPS01836788 1 20010811 A 5320 47585141N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 STA 1140 AFT SIDE LONG 33R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IA W DWG 4758514, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001100300040 20011003 00040 WP 2001 10 3 UPS01836789 1 20010811 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 STA 1620 FRAME IS CRACKED ABOVE LONG 21L. REPAIRED FRAME IAW SRM 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 2001100300041 20011003 00041 WP 2001 10 3 UPS01836790 1 20010809 A 5320 5753113502N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 RT WHEEL WELL LONG 24R SUPPORT FITTING IS CRACKED AT STA 920. REMOVED AND REPLACED FITTING IAW DWG 5753113, AND SRM 51-1-20D, 53-2-0 FIG 8. 2 L 7 4 4F RT 4A25 2001100300043 20011003 00043 WP 2001 10 3 UPS01836791 1 20010807 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 FUSELAGE SKIN CRACKED STA 25 LONG 10L FWD UPPER CORNER L-1 DOOR. REPAIRED SKIN IAW SRM 53-2-1 FIG 1 5. 2 L 7 4 4F RT 4A25 2001100300044 20011003 00044 WP 2001 10 3 UPS01836792 1 20010811 A 5320 3755847U2 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 STA 1225 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG 31R-32R. REMOVED AND REPLACED FITTI NG IAW DWG 3755847, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001100300045 20011003 00045 WP 2001 10 3 UPS01836793 1 20010811 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 STA 160 FLOORBEAM IS CORRODED BEYOND LIMITS AT RBL 38. REPAIRED FLOORBEAM IAW 8110-3 APPROVED DH SK 866-956. 2 L 7 4 4F RT 4A25 2001100300046 20011003 00046 WP 2001 10 3 UPS01836795 1 20010813 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 CORROSION ON INNER SKIN IN AFT PIT FS 1080 LONG 36. REMOVED CORROSION IAW DC8 SRM 51-1-8 FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED DAMAGED SECTION OF SKIN IAW DC SRM 51-1-20D. INSTALLED NEW SECTION OF BELLY S KIN IAW DC SRM 51-1-20D 51-1-21 & 51-3-0. 2 L 7 4 4F RT 4A25 2001100300047 20011003 00047 WP 2001 10 3 UPS01836797 1 20010816 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 FWD PIT STA 272 L33R INSIDE TQ BOX LWR FITTING CORRODED. R&R ZEE FITTING. 2 L 7 4 4F RT 4A25 2001100300048 20011003 00048 WP 2001 10 3 UPS01836804 1 20010813 A 5244 DOOR DOUG DC8 DC873F 302199F WP AFT ACCY DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 AFT ACC COMPT FS 1540 BULKHEAD DOOR CORRODED ALONG BOTTOM FWD SIDE. REMOVED DOOR, REMOVED CORROSION A ND FOUND OUT OF LIMITS. FABRICATE REPAIR DOUBLER & FILLER MM 52-30-00. INSTALL FILLER & DOUBLER IAW DC SRM 51-1-21 AND R EINSTALLED DOOR IAW DC SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001100300049 20011003 00049 WP 2001 10 3 UPS01836806 1 20010816 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 FWD PIT STA 272 L33R INSIDE TRQ BOX LWR FITTING CORRODED. REMOVED & REPLACED ZEE FITTING. 2 L 7 4 4F RT 4A25 2001100300050 20011003 00050 WP 2001 10 3 UPS01836813 1 20010809 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 STA 17 FRAME IS CRACKED AT LONG 16L-17L. REPAIRED FRAME IAW SRM 53-2-0 FIG 23. 2 L 7 4 4F RT 4A25 2001100300051 20011003 00051 WP 2001 10 3 UPS01836820 1 20010809 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 R-2 DOOR UPPER AFT CORNER SKIN IS CRACKED AT STA 1660 LONG 11R. REPAIRED SKIN IAW SRM 53-2-0 FIG 17 . 2 L 7 4 4F RT 4A25 2001100300052 20011003 00052 WP 2001 10 3 UPS01836821 1 20010811 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C2,3 STA 60 FLOORBEAM AT RBL 12 UPPER FLANGE IS CRACKED. REPAIRED FLOORBEAM IAW 8110-3 APPROVED DH SK 86 6-019. 2 L 7 4 4F RT 4A25 2001100300058 20011003 00058 2001 10 3 UPS01836827 4 20010914 A 2565 COVER DOUG DC8 DC871F 302199D WP EVAC SLIDE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:IN EVAC SLIDE COVER IS DAMAGED. SLIDE CASE WILL NOT STAY CLOSED. GAPS OPEN AT THE BOTTOM. SLIDE COVER RE MOVED AND ROUTED TO SHEETMETAL REPLACED SHEARED RIVETS ON COVER LATCH IAW 51-1-21 DC8 SRM 79657 9-15-01 INSTALLED SLIDE PER 25-60-01. 2 L 7 4 4F RT 4A25 2001100300064 20011003 00064 NM 2001 10 3 AWXA200100499 1 20010904 A 5343 654581951 ANGLE BOEING 737 737277 1384570 NM NOSE WHEEL WELL CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 22651 YVR - C19 CK - "C" - NOSE LANDING GEAR ACTUATOR UPPER ATTACH SUPPORT FITTING VERTICAL WEB CRACKS EMINATING FROM 3 RIVIT HOLES, EACH CRACK ABOUT .25". MAINTENANCE REMOVED DAMAGED FITTING, FABRICATED A NEW ANGLE (FITTING) AND INSTALLED IAW BOEING INSTALLATION DRAWING 65-45819. 2 L 7 2 4F RT A16WE 2001100300065 20011003 00065 WP 2001 10 3 UPS01836830 1 20010919 A 2612 FIRE DETECTOR DOUG DC8 DC873F 302199F WP CARGO BAY MALFUNCTIONED A IPXA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING DE DESCENT 1 SO 01 804UP 46004 INSPECTION TYPE:N/A AT TOP OF DESCENT, LWR CARGO FIRE LIGHT ILLUMINATED. MX DISPLAY READ "AFT D FIRE". ACCOPM CKLIST PRO CEDURE, FIRE LIGHT EXTINGUISHED AND MX DISPLAY READ "AFT D INOP". MX LIGHT ALSO ILLUMINATED WHEN AFT D INOP MSG APPEARE D. FOUND MX FAULT AD2318 AND AD3411 AFT CARGO PIT. AFT D INOP MSG ON CONTROL. GREEN SYST OK LIGHT ON. DEFER AFT CARGO CO MP PER 26-10 FIRE DET INOP AFT PIT D. 2 L 7 4 4F RT 4A25 2001100300066 20011003 00066 WP 2001 10 3 UPS01836833 1 20010920 A 3350 570845803 BATTERY PACK DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. R&R BATTERY PACK. OPS CHECKS GOOD PER DC8 MM 33-50-00. 2 L 7 4 4F RT 4A25 2001100300067 20011003 00067 WP 2001 10 3 UPS01836837 1 20010917 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 AFT PIT FS 1185 T LATCH BACKUP FITTING REPAIR ANGLE CRACKED. R&R T BOLT BACK UP FITTING SPLICE. 2 L 7 4 4F RT 4A25 2001100300068 20011003 00068 2001 10 3 GLBA2001210 4 20011002 A 2300 890018 SWITCH BEECH 1900 1900D 1154162 CE CAPTAINS STUCK A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 01 260GL UE206 CAPTAINS PTT SWITCH STUCK, REPLACED OPS CHECKED SATISFACTORY 2 L 7 2 4T RT A24CE 2001100300069 20011003 00069 2001 10 3 GLBA2001211 4 20011002 A 3400 066306200 ALTIMETER BEECH 1900 1900D 1154162 CE CAPTAINS INACCURATE A GLBA D RETURN TO BLOCK I FLT. ATTITUDE INST. CR CRUISE 1 CE 01 195GL 85 UE195 400 FOOT SPLIT CAPTAINS ALTIMETER, REPLACED OPS CHECKED SYSTEM SATISFACTORY 2 L 7 2 4T RT A24CE 2001100300071 20011003 00071 WP 2001 10 3 ABXA010521 1 20010918 A 5330 99234343 DOUBLER DOUG DC9 DC941 302207N WP CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 CORROSION SPOTS WERE NOTED BELOW FRAME AT FUSELAGE STATION 617L AND LONGERON 29L. MAINTENANCE REPLACED THE INTERNAL DOUB LER IAW DC-9 SRM 51-30-5 AND 51-30-1. 2 L 7 2 4F A6WE 2001100300072 20011003 00072 2001 10 3 ABXA010522 4 20010914 A 3444 9510868060 CAPACITOR COLLINS F1 DOUG DC8 DC863 302198A WP BLOWN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 820AX 11043 46155 #1 RADIO ALTEMETER CIRCUIT BREAKER OPENED. THE BREAKER WAS RESET ONCE AND OPENED AGAIN. MAINTENANCE REPLACED THE #1 RADI O ALTIMETER IAW DC8 MAINTENANCE MANUAL 34. INSPECTION OF THE RADIO ALTIMETER INDICATED THAT THE POWER SUPPLY INPUT CAPAC ITOR A6C1A EXPLODED, CAUSING POWER SUPPLY DAMAGE AND POSSIBLE FLAME. ADJACENT COMPONENTS WITHIN THE RADIO ALTIMETER WERE DAMAGED OR BURNT, AND THE UNIT WAS CONTAMINATED WITH CAPACITOR CHEMICALS. RADIO ALTIMETER S/N 11043 WAS SCRAPPED. 2 L 7 4 4F 4A25 2001100300075 20011003 00075 WP 2001 10 3 UPS01836838 1 20010908 A 5320 PAN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 AFT CARGO PIT AT FS 1150-1160 AT LONG 33R X SLIDE DOOR TORQUE BOX PAN IS CRACKED. LOCATED AND DRILLED EXISTING HOLES IN NEW TORQUE BOX PAN IAW DC8 SRM 51-3-2. PAN TO BE INSTALLED ON UPS TASK CARD. 2 L 7 4 4F RT 4A25 2001100300077 20011003 00077 WP 2001 10 3 UPS01836839 1 20010907 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 FLC STA 300-444 SEAT TRACK A CORRODED AT FASTENER HOLES I/B LWR SIDE. REMOVED CORROSION ON TRACK STA 300-444. FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0 AND 53-1-0. REPLACED TRACK IAW DC8 SRM 53-2-0 AND 51-3-0. INSTALLE D SPLICES IAW DC8 SRM 53-2-0. 2 L 7 4 4F RT 4A25 2001100300080 20011003 00080 WP 2001 10 3 UPS01836843 1 20010914 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 RIGHT WING LOWER SKIN IS CRACKED AT FRONT SPAR AT LONG 64 END. REPAIRED SKIN IAW EO DC8-5730-9004 APP X E. 2 L 7 4 4F RT 4A25 2001100300082 20011003 00082 WP 2001 10 3 UPS01836845 1 20010915 A 5540 570125141 WEB DOUG DC8 DC873F 302199F WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 RUDDER LOWER CLOSURE WEB IS CRACKED FWD OF ACCESS PLATE 81. REMOVED, FABRICATED, AND REPLACED WEB IAW DWG 5701251, AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001100300088 20011003 00088 WP 2001 10 3 UPS01836846 1 20010914 A 5320 4772397U1 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 STA 1770 LONG 17R AND 17R END FITTING ARE CRACKED. REMOVED, FABRICATED, AND REPLACED LONGERON IAW DWG 5649327, AND REPLACED FITTING IAW DWG 4772397, AND SRM 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 2001100300091 20011003 00091 WP 2001 10 3 UPS01836847 1 20010909 A 5414 SKIN DOUG DC8 DC873F 302199F WP NR 4 PYLON DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 NR 4 PYLON OUTBOARD SKIN HAS FOUR DENTS BEYOND LIMITS BETWEEN YN335 TO YN353. REPAIRED SKIN IAW 8110- 3 APPROVED DH SK 852-534. 2 L 7 4 4F RT 4A25 2001100300093 20011003 00093 WP 2001 10 3 UPS01836853 1 20010915 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 STA 1020 LBL 60 SEAT TRACK IS CORRODED BEYOND LIMITS. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 14. 2 L 7 4 4F RT 4A25 2001100300096 20011003 00096 WP 2001 10 3 UPS01836855 1 20010925 A 2497 WIRE DOUG DC8 DC871F 302199D WP ELECTRICAL SYS LOOSE A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:N/A NR 1 BUS OFF LIGHT ILLUMINATED AND SMOKE IN COCKPIT. RESECURED WIRE TO TERMINAL X2 OF LMR R2-25 OF N R 1 AC BUS OPS CHECKS NORMAL OF NR 1 AC BUS. 2 L 7 4 4F RT 4A25 2001100300103 20011003 00103 WP 2001 10 3 UPS01836866 1 20010908 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 CORROSION AROUND FASTENERS ON SEAT TRACK FROM 1060 TO 1160 BUTTLINE 0 AFT CARGO COMPT. REMOVED AND RE PLACED SEAT TRACK IAW UPS EO DC8-5320-5167. 2 L 7 4 4F RT 4A25 2001100300104 20011003 00104 NM 2001 10 3 UPS01236970 1 20010827 A 5330 DOUBLER BOEING 727 72725C 138400H NM BS1030-1130 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:C CORROSION AFT CARGO DOOR CUT OUT INNER DOUBLER STRAP BETWEEN BS1030 AND BS1130 AND BETWEEN STR 17R AND 20R. REMOVED INNER DOUBLER STRAP BETWEEN BS1030 AND BS1130 STR17 AND STR 20 IAW SRM B727-51-30-02. FABRICATED INNE R DOUBLER STRAP IAW UPS DI-00011H AND DRAWING# 65-18622. INSTALL INNER DOUBLER STRAP AT AFT CARGO DOOR CUT OUT AT STA 1 030 TO 1130 BETWEEN STR 17R AND STR 20R AS PER DRAWING# 65-18622. 2 L 7 3 4F A3WE 2001100300105 20011003 00105 WP 2001 10 3 UPS01836867 1 20010913 A 5720 ATTACH FITTING DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 STGR 64 TO FRONT SPAR ATTACH FTG CRACKED ON I/B SIDE OF NR 4 PYLON NR 4 ALT. REMOVED AND REPLACED W/N EWLY MANUFACTURED PART IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001100300106 20011003 00106 WP 2001 10 3 UPS01836869 1 20010925 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:AS UPON BLOCK IN, CHECKED EMERGENCY EXIT LIGHTS. EMERGENCY EXIT LIGHTS INOP. R&R EMERGENCY BATTERY PACK ASSY. OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2001100300107 20011003 00107 WP 2001 10 3 UPS01836870 1 20010920 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 FLC BETWEEN STA 80 TO 100 AT STA 100 FRAME CORRODED AT FASTENER AT LONG 36. REMOVED CORROSION FOUND O UT OF LIMITS. HEAT TREATED AND FABBED IAW DC8 EO 5310-11728A. INSTALLED FRAME IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001100300108 20011003 00108 WP 2001 10 3 UPS01836871 1 20010909 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 AFT CARGO COMP FWD DOOR STA 1220 INSIDE TORQUE BOX CLIP CRACKED UNDER GUSSET BY STRINGER 33R. REMOVED STIFFENER NO CRACK FOUND. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 51-1-8 AND 53-2-0. INSTALLED NEW ANG LE IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001100300109 20011003 00109 WP 2001 10 3 UPS01836872 1 20010908 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 AFT CARGO PIT AT FS 1160 Z FITTING IS CORRODED BETWEEN LONG 33R-34R. R&R FITTING IAW DC8 SRM 51-1-20D . 2 L 7 4 4F RT 4A25 2001100300110 20011003 00110 WP 2001 10 3 UPS01836873 1 20010908 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 AFT CARGO PIT AT FS 1170 AT LONG 33R T BOLT LATCH FITTING ATTACH FITTING IS CRACKED THROUGH FASTENER HOLES. REMOVED & REPLACED FWD & AFT SPLICE FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001100300111 20011003 00111 WP 2001 10 3 UPS01836874 1 20010908 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 AFT CARGO PIT AT FS 1120-1140 AT RBL 20 MAIN CABIN SEAT TRACK IS CORRODED AROUND ATTACH FASTENERS. RE MOVED & REPLACED SECTION OF SEAT TRACK IAW UPS EO DC8-5320-5167-C. 2 L 7 4 4F RT 4A25 2001100300112 20011003 00112 WP 2001 10 3 UPS01836875 1 20010908 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 SEAT TRACK CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK IAW DC8 SRM 53-2-3 AND UPS EO DC8- 53 20-5167-C. 2 L 7 4 4F RT 4A25 2001100300113 20011003 00113 WP 2001 10 3 UPS01836878 1 20010823 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 C/W PERMANENT REPAIR TO LEFT OUTBOARD SEAT TRACK B/TW POSITIONS 2 & 3. REMOVED AND REPLACED DAMAGED S ECTION OF TRACK IAW DC8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 2001100300114 20011003 00114 WP 2001 10 3 UPS01836879 1 20010906 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 EXT AFT FUSELAGE BULGE IN SKIN AT STA 1834 ABOVE RT LWR SEAM. REPAIRED AREA IAW DC8 SRM 53-2-1. 2 L 7 4 4F RT 4A25 2001100300115 20011003 00115 WP 2001 10 3 UPS01836882 1 20010908 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 R1 DOOR UPPER FWD CORNER HAS A CRACK INDICATION APPROX .500 IN LENGTH. PERFORMED HFEC IAW DC8 SRM 06- 10-001. REMOVED DAMAGE IAW DC8 SRM 53-2-0. FABBED DOUBLER, TRIPLER & FLR IAW DC8 SRM 53-2-0. INSTALLED IAW DC8 SRM 53-2 -0 & 51-1-20D. 2 L 7 4 4F RT 4A25 2001100300116 20011003 00116 WP 2001 10 3 UPS01836906 1 20010914 A 5313 564932743 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 STA 1770 LONG 17L AND END FITTING ARE CRACKED. REMOVED, FABRICATED, AND REPLACED LONGERON AND FITTING IAW DWG 4772397, AND DWG 5649327 AND SRM 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 2001100300117 20011003 00117 WP 2001 10 3 UPS01836907 1 20010915 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 SEAT TRACK IS WORN BEYOND LIMITS AT STA 300 AT RBL 63. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A. 2 L 7 4 4F RT 4A25 2001100300118 20011003 00118 WP 2001 10 3 UPS01836909 1 20010825 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 ACCOMPLISH PERMANENT REPAIR TO DOUBLE SEAT TRACK AT RBL 45.50-49.50 PER SRM. INSTALLED NEW SEAT TRACK IAW DC8 SRM 51-1-24 & 51-3-0. 2 L 7 4 4F RT 4A25 2001100300119 20011003 00119 WP 2001 10 3 UPS01836910 1 20010908 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 FS 444 TO 590 SEAT TRACK A IS CORRODED AT FASTENERS HOLES. REMOVED CORROSION ON TRACK STA 444-590. FO UND OUT OF LIMITS IAW DC8 SRM 53-2- 0 & 53-1-0. REPLACED TRACK IAW DC8 SRM 53-2-3 & 51-3-0. INSTALLED SPLICE IAW DC8 SRM 53-2-0. 2 L 7 4 4F RT 4A25 2001100300120 20011003 00120 WP 2001 10 3 UPS01836911 1 20010919 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 FLC L27L STA 70 LONGERON END FITTING CRACKED. R&R FITTING IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001100300121 20011003 00121 WP 2001 10 3 UPS01836912 1 20010925 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 FLOORBEAM AT STA 160 CORRODED. REPLACED SECTION OF FLOORBEAM & SPLICED. 2 L 7 4 4F RT 4A25 2001100300122 20011003 00122 WP 2001 10 3 UPS01836913 1 20010910 A 5540 FITTING DOUG DC8 DC873F 302199F WP RUDDER WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 RUDDER BASE ATTACH POINT RT AFT BUSHING FALLING OUT. REAMED HOLE AND INSTALLED OVERSIZE BUSHING IAW R EO G08406. 2 L 7 4 4F RT 4A25 2001100300123 20011003 00123 WP 2001 10 3 UPS01836914 1 20010911 A 5320 SPLICE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 FWD CARGO PIT FS 440-460 LONG 31L SPLICE FITTING IS CRACKED. R&R SPLICE. 2 L 7 4 4F RT 4A25 2001100300124 20011003 00124 WP 2001 10 3 UPS01836916 1 20010913 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 AFT PIT FS 1220 FITTING INSIDE TORQUE BOX AT L27R IS CRACKED. R&R FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001100300125 20011003 00125 WP 2001 10 3 UPS01836918 1 20010915 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 RT WING LOWER SKIN IS CORRODED BEYOND LIMITS AT XRS795 BETWEEN STRINGER 52 AND 53. REPAIRED SKIN IAW 8110-3 DH SK 852-762. 2 L 7 4 4F RT 4A25 2001100300126 20011003 00126 WP 2001 10 3 UPS01836919 1 20010911 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 FUSELAGE SKIN IS CORRODED BEYOND LIMITS AT STA 1260 LONG 35R. REPAIRED SKIN IAW 8110-3 APPROVED DH SK 852-822. FABRICATED DOUBLER PER SRM 51-2-1 FIG 7, INSTALLED FILLER PER SRM 51-126. 2 L 7 4 4F RT 4A25 2001100300127 20011003 00127 WP 2001 10 3 UPS01836920 1 20010915 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 SEAT TRACK AT STA 65 LBL 50 HAS LUGS BROKEN. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 14. 2 L 7 4 4F RT 4A25 2001100300128 20011003 00128 WP 2001 10 3 UPS01836921 1 20010915 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 SEAT TRACK WORN BEYOND LIMITS AT STA 860-875 RBL 45-51. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 14. 2 L 7 4 4F RT 4A25 2001100300129 20011003 00129 NM 2001 10 3 CALA0100919 1 20011002 A 5320 ANGLE BOEING 737 7373T0 1384582 NM STA 302-306 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 INSPECTION FOUND FWD LAV WALL MOUNT L-ANGLES ON HAT SECTION CORRODED AT STA 302, LBL 36-56 AND AT STA 306, LBL12-43. NEW ANGLES WERE INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001100300130 20011003 00130 NM 2001 10 3 CALA0100922 1 20011002 A 5230 FRAME BOEING 737 7373T0 1384582 NM C-1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17306 23357 INSPECTION FOUND A 4" CRACK IN C-1 DOOR AFT LOWER FRAME. A NEW FRAME WAS INSTALLED IAW W/C JA 5230-0103007001. 2 L 7 2 4F RT A16WE 2001100300131 20011003 00131 NM 2001 10 3 CALA0100923 1 20011002 A 5230 WEB BOEING 737 7373T0 1384582 NM C-1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17306 23357 INSPECTION FOUND A 3" CRACK IN C-1 DOOR FWD AND AFT LOWER WEBS. A REPAIR WAS INSTALLED AT EACH LOCATION IAW W/C JA 5230- 0103006001. 2 L 7 2 4F RT A16WE 2001100300132 20011003 00132 NM 2001 10 3 CALA0100924 1 20011002 A 5247 ANGLE BOEING 737 7373T0 1384582 NM APU DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10323 23374 INSPECTION FOUND APU DOOR ANGLE DENTED ON AFT EDGE. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-70-13. 2 L 7 2 4F RT A16WE 2001100300133 20011003 00133 NM 2001 10 3 CALA0100925 1 20011003 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM STA 294 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 INSPECTION FOUND FLOORBEAM CORRODED ON UPPER SURFACE AT STA 294, RBL 53. THE FLOORBEAM UPPER SURFACE WAS REPAIRED IAW SR M 53-10-51. 2 L 7 2 4F RT A16WE 2001100300134 20011003 00134 WP 2001 10 3 UPS01836922 1 20010915 A 5330 5645332113 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 FINGER DOUBLER IS CORRODED BEYOND LIMITS STA 940-960 RBL 60-65. REMOVED FABRICATED AND REPLACED DOUBL ER IAW DWG 5645332, AND SRM 53-1-0, 51-1-21. 2 L 7 4 4F RT 4A25 2001100300135 20011003 00135 WP 2001 10 3 UPS01836923 1 20010914 A 5320 5751966503N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 STA 940 FRAME TO FLOORBEAM FITTING IS CRACKED AT LONG 21L. REMOVED AND REPLACED FITTING IAW DWG 57519 66, AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001100300136 20011003 00136 WP 2001 10 3 UPS01836924 1 20010911 A 5320 4641324N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 STA 1690 LONG 36 END FITTING IS CORRODED BEYOND LIMITS AND LONG 36 IS CRACKED. R&R FITTING, AND REPAI RED LONGERON IAW DWG 4641324, AND SRM 53-2-2 FIG 8, AND 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 2001100300138 20011003 00138 WP 2001 10 3 UPS01836925 1 20010914 A 5330 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 INTERNAL DOUBLER IS CORRODED BEYOND LIMITS AT STA 1214 BETWEEN LONG 34R-35R. REPAIRED DOUBLER IAW 811 0-3 APPROVED DH SK 852-409. 2 L 7 4 4F RT 4A25 2001100300139 20011003 00139 WP 2001 10 3 UPS01836926 1 20010915 A 5530 36480113 FITTING DOUG DC8 DC873F 302199F WP VERTICAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 VERTICAL STAB REAR SPAR FWD SIDE FITTING IN 4TH LIGHTENING HOLE FROM THE TOP IS CORRODED BEYOND LIMIT S. REMOVED AND REPLACED FITTING IAW DWG 36480113, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001100300140 20011003 00140 WP 2001 10 3 UPS01836930 1 20010921 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 STA 160 LONG 10R IS CRACKED. REPAIRED LONGERON IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2001100300141 20011003 00141 WP 2001 10 3 UPS01836931 1 20010915 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 SEAT TRACK IS CORRODED BEYOND LIMITS STA 740-840 LBL 65. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A. 2 L 7 4 4F RT 4A25 2001100300142 20011003 00142 WP 2001 10 3 UPS01836932 1 20010911 A 5330 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 STA 1640 LONG 32R INTERNAL DOUBLER IS CORRODED BEYOND LIMITS. REPAIRED DOUBLER IAW 8110-3 APPROVED DH SK 852-817. 2 L 7 4 4F RT 4A25 2001100300143 20011003 00143 WP 2001 10 3 UPS01836935 1 20010916 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 FLOORBEAM IS CORRODED BEYOND LIMITS AT STA 1360 AT LBL 48. REPAIRED FLOORBEAM IAW 8110-3 APPROVED DH SK 852-652. 2 L 7 4 4F RT 4A25 2001100300144 20011003 00144 NM 2001 10 3 AWXA200100501 1 20010904 A 5311 6546554 FRAME BOEING 737 7373G7 1384595 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 MCN - C17 CK - "C" - FRAME AT BS 867, BETWEEN STR 27L & 27R HAS AREA OF CORROSION. MAINTENANCE REMOVED CORROSION AND FAB RICATED AND INSTALLED SHEAR TIE IAW B737 SRM 53-00-01, FIG 208, PG 222 TO 224. 2 L 7 2 4F RT A16WE 2001100300145 20011003 00145 NM 2001 10 3 AWXA200100502 1 20010905 A 5330 65457778 SKIN BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 MCN - C17 CK - "C" - .5" EXTERNAL FUSELAGE SKIN CRACK AT BS 985.5, UPPER AFT CORNER OF L2 DOOR FUSELAGE CUTOUT. MAINTEN ANCE STOP DRILLED THE CRACK AND INSTALLED REPAIR IAW B737 SRM 53-60-01, PG 1 TO 3, FIG 203, SHT 1 TO 3. 2 L 7 2 4F RT A16WE 2001100300146 20011003 00146 NM 2001 10 3 AWXA200100503 1 20010904 A 5330 6545765200 SKIN BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 MCN - C17 CK - "C" - EXTERNAL FUSELAGE SKIN, 4" CRACK ABOVE STR 10R LAP SPLICE, BS 512 - 516. MAINTENANCE CUT OUT DAMAGE D AREA, FABRICATED DOUBLER AND FILLERS AND INSTALLED REPAIR IAW AWA ER 03-5330-01263-KB1. 2 L 7 2 4F RT A16WE 2001100300147 20011003 00147 NM 2001 10 3 AWXA200100504 1 20010911 A 5320 65C3453719 WEB BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 MCN - C17 CK - "C" - 2 EA 1" CRACKS FOUND IN VERTICAL WEB BETWEEN BS 708 & 714, BL 0 BELOW THE FLOOR PANELS. MAINTENANC E REMOVED DAMAGED AREA, FABRICATED WEB REPAIR AND DOUBLER AND INSTALLED IAW AWA ER 03-5315-01257-TB2. 2 L 7 2 4F RT A16WE 2001100300148 20011003 00148 NM 2001 10 3 AWXA200100505 1 20010911 A 5311 65677758 FRAME BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 MCN - C17 CK - "C" - 1.25" CRACK IN FRAME ANGLE AT BS 616, WL 203, RBL 65. MAINTENANCE ACCOMPLISHED REPAIR TO FRAME ANGL E IAW AWA ER 03-5311-01143-DD1. 2 L 7 2 4F RT A16WE 2001100300149 20011003 00149 NM 2001 10 3 AWXA200100506 1 20010911 A 5315 65C3454719 WEB BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 MCN - C17 CK - "C" - 3 EA. CRACKS ABOUT 1" EA. FOUND ON FLOOR BAEAM WEB BS 706 TO 714, RBL 24, BELOW FLOOR PANELS. MAIN TENANCE REMOVED DAMAGED AREA OF WEB AND FABRICATED REPAIR PARTS AND INSTALLED IAW AWA ER 03-5715-01267-DL1. 2 L 7 2 4F RT A16WE 2001100300150 20011003 00150 NM 2001 10 3 AWXA200100508 1 20010911 A 5310 654541039 WEB BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 MCN - C17 CK - "C" - 5 EA CRACKS (TOTAL OF 3") ON VERTICAL WEB BS 706 TO 718, WL 200, LBL24, BELOW FLOOR PANELS. MAINTE NANCE REMOVED DAMAGED SECTION OF VERTICAL WEB, FABRICATED REPAIR PARTS AND INSTALLED IAW AWA ER 03-5700-01270-JS3. 2 L 7 2 4F RT A16WE 2001100300151 20011003 00151 NM 2001 10 3 AWXA200100510 1 20010912 A 5312 6546568524 WEB BOEING 737 7373G7 1384595 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 MCN - C17 CK - "C" - AREA OF CORROSION FOUND ON FWD SIDE OF AFT PRESS. BULKHEAD, BS 1016, FROM LBL 7 TO RBL 7, WL 190. MAINTENANCE REMOVED CORROSION AND ACCOMPLISHED AFT PRESS. BULKHEAD REPAIR IAW AWA ER 03-5312-01269-DL1. 2 L 7 2 4F RT A16WE 2001100300152 20011003 00152 NM 2001 10 3 AWXA200100511 1 20010912 A 5312 6546568519520 STIFFENER BOEING 737 7373G7 1384595 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 MCN - C17 CK - "C" - 3" AREA OF CORROSION FOUND ON LOWER CENTER STIFFENER ON FWD SIDE OF AFT PRESS. BULKHEAD, BS 1016, W L 190 TO 193, BL 0. MAINTENANCE REMOVED CORRODED AREA OF LOWER CENTER STIFFENER, FABRICATED AND INSTALLED REPAIR PARTS IAW AWA ER 03-5312-01269-DL2. 2 L 7 2 4F RT A16WE 2001100400004 20011004 00004 EA 2001 10 4 BTH2001F00001 2 20010914 A 7414 BL682560B MAGNETO PIPER PA32 PA32R300 7103213 SO LYC O540 IO540K1A5 41532 EA LEFT INOPERATIVE A BTHA O OTHER O OTHER NR NOT REPORTED 1 AL 01 75387 342 32R7680298 MAGNETO DEAD ON LEFT SIDE DURING RUNUP MAG-CHECK. FOUND SEVERAL TEETH BROKEN ON BOTH DISTRIBUTOR GEARS. 1 L 7 1 3O 3 O A3SO 1E4 2001100400018 20011004 00018 WP 2001 10 4 MWEA011314 1 20011001 A 5310 991556135 WEB DOUG DC9 DC981 3022081 WP STATION 1338 TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 STATION 1338 LONGERON 18 THROUGH LONGERON 30 LEFT WEB SUPPORT ANGLE HAS TOOL DAMAGE. -- REMOVED AND REPLACED WEB SUPPO RT ANGLE. 2 L 7 2 4F A6WE 2001100400019 20011004 00019 WP 2001 10 4 MWEA011317 1 20011001 A 5310 591143315 LONGERON DOUG DC9 DC981 3022081 WP STATION 1361 CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 LONGERON 13 RIGHT HAS VERY DEEP CHAFE MARKS BETWEEN AFT PRESSURE BULKHEAD AND STATION 1361. -- FABRICATED AND INSTALLE D LONGERON REPAIR SECTION AND SPLICE PLATE. 2 L 7 2 4F A6WE 2001100400020 20011004 00020 WP 2001 10 4 MWEA011318 1 20011001 A 5310 59114335 LONGERON DOUG DC9 DC981 3022081 WP STATION 1418 CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 LONGERON 8 LEFT CHAFED BETWEEN STATION 1418 AND 1401. -- FABRICATED AND INSTALLED LONGERON REPAIR PARTS. 2 L 7 2 4F A6WE 2001100400021 20011004 00021 WP 2001 10 4 MWEA011319 1 20011001 A 5310 591143317 LONGERON DOUG DC9 DC981 3022081 WP STATION 1401 CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 LONGERON 14 RIGHT HAS SEVERE CHAFE DAMAGE ON UPPER LEG BETWEEN STATION 1401 AND 1418. -- FABRICATED AND INSTALLED LONG ERON SECTION AND SPLICE. 2 L 7 2 4F A6WE 2001100400023 20011004 00023 WP 2001 10 4 MWEA011312 1 20011001 A 5310 591013044 SHEAR TIE DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 STATION 1338 LONGERON 18 THROUGH LONGERON 22 RIGHT SHEAR TIE HAS CORROSION. FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F A6WE 2001100400024 20011004 00024 WP 2001 10 4 MWEA011313 1 20011001 A 5310 591013043 SHEAR TIE DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 STATION 1338 LONGERON 18 THROUGH LONGERON 22 LEFT SHEAR TIE HAS CORROSION. FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F A6WE 2001100400025 20011004 00025 WP 2001 10 4 MWEA011315 1 20011001 A 5320 991556153 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 STATION 1338 RIGHT, LONGERON 18 RIGHT THROUGH LONGERON 30 WEB REQUIRES REMOVAL TO FOM. FOUND CORROSION. MAINTENANCE FABR ICATED AND INSTALLED WEB. 2 L 7 2 4F A6WE 2001100400026 20011004 00026 WP 2001 10 4 MWEA011316 1 20011001 A 5320 99155613 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 STATION 1338 LONGERON 18 LEFT THROUGH LONGERON 30 WEB REQUIRES REMOVAL TO FOM. FOUND CORROSION. MAINTENANCE FABRICATED A ND INSTALLED WEB. 2 L 7 2 4F A6WE 2001100400027 20011004 00027 WP 2001 10 4 MWEA011322 1 20011001 A 5310 5936038501 DOOR FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 AFT CARGO COMPARTMENT DOOR JAMB BOTTOM FRAME HAS NUMEROUS AREAS OF LIGHT CORROSION FROM STATION 1155 TO 1212 ON OUTBOARD SIDE. REMOVED AND REPLACED DOOR JAMB FRAME. 2 L 7 2 4F A6WE 2001100400028 20011004 00028 WP 2001 10 4 MWEA011323 1 20011001 A 5311 59135961 FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 MODERATE CORROSION ON FORWARD FACE OF FUSELAGE FRAME 1361 ABOVE LONGERON 24 LEFT. FABRICATED AND INSTALLED DOUBLERS. 2 L 7 2 4F A6WE 2001100400032 20011004 00032 WP 2001 10 4 MWEA011325 1 20011001 A 5540 FITTING DOUG DC9 DC981 3022081 WP RUDDER CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 LEFT AND RIGHT ELEVATOR CONTROL TAB PUSHROD INBOARD CRANK ARM ATTACH BOLT NUT IS CHAFING STRUCTURE WHEN YOKE IS POSITION ED TO FULL AIRCRAFT NOSE DOWN. TRIMMED FITTING IAW MWX-ORD-01-00467H. 2 L 7 2 4F A6WE 2001100400033 20011004 00033 WP 2001 10 4 MWEA011326 1 20011001 A 5753 BUSHING DOUG DC9 DC981 3022081 WP T/E FLAP WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 LEFT OUTBOARD FLAP MOST INBOARD HINGE LOWER INBOARD ATTACH POINT BUSHING AND OR HINGE WORN. FABRICATED AND INSTALLED BUS HINGS. 2 L 7 2 4F A6WE 2001100400034 20011004 00034 WP 2001 10 4 MWEA011327 1 20011001 A 5320 591015176 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 CABIN SUBFLOOR RIGHT SIDE BETWEEN STATION 845 AND 864 HAS LIGHT CORROSION ON TOP SIDE ALONG OUTBOARD END. REMOVED AND RE PLACED MEMBRANE. 2 L 7 2 4F A6WE 2001100400035 20011004 00035 WP 2001 10 4 MWEA011328 1 20011001 A 5320 9910151102 WEB DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 CABIN SUBFLOOR RIGHT SIDE CUSP MEMBRANE HAS PREVIOUS REPAIRS FROM STATION 905-946. FABRICATED AND INSTALLED CUSP MEMBRAN E. 2 L 7 2 4F A6WE 2001100400036 20011004 00036 WP 2001 10 4 MWEA011329 1 20011001 A 5320 591015194 WEB DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 CABIN SUBFLOOR RIGHT SIDE CUSP MEMBRANE HAS PREVIOUS REPAIRS FROM STATION 805-845. REMOVED AND REPLACED CUSP MEMBRANE. 2 L 7 2 4F A6WE 2001100400037 20011004 00037 WP 2001 10 4 MWEA011368 1 20010930 A 3220 591498564 SKIN DOUG DC9 DC932 3022066 WP NLG DOOR INOPERATIVE A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 202ME 47672 WHEN GEAR RETRACTED, FORWARD RIGHT NOSE GEAR DOOR WOULD NOT CLOSE. 4 FOOT CABLE PULLED OUT OF SWAGGED END FOR DOOR. -- REMOVED AND REPLACED UPPER STRANDED WIRE DOOR STOP CABLE ASSY. MAINTENANCE FOUND GOUGE LOCATED ON RIGHT FORWARD NOSE LA NDING GEAR DOOR INNER SKIN (PAN) ADJACENT TO AFT HINGE BRACKET. GOUGE WAS REMOVED AND EXTERNAL DOUBLER WAS INSTALLED. 2 L 7 2 4F A6WE 2001100400039 20011004 00039 WP 2001 10 4 MWEA011331 1 20011001 A 5312 591013061 DOUBLER DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 AFT PRESSURE BULKHEAD DOUBLER NEAR LONGERON 30 HAS CORROSION AT STATION 1338. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001100400040 20011004 00040 WP 2001 10 4 MWEA011332 1 20011001 A 5320 591142917 STIFFENER DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 MODERATE SPOTS OF CORROSION ON TEE CORD LEFT OF APU OPENING ON OUTBOARD SURFACE FROM AFT PRESSURE BULKHEAD AFT TO STATIO N 1380. FABRICATED AND INSTALLED TEE SECTION. 2 L 7 2 4F A6WE 2001100400041 20011004 00041 WP 2001 10 4 MWEA011334 1 20011001 A 5347 593054763 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 STATION 230, SEAT TRACK NR 2 INBOARD FLOOR BOARD HOLE HAS CORROSION. REMOVED AND REPLACED SEAT TRACK SECTION, SPLICE SEC TION, AND DOUBLER. 2 L 7 2 4F A6WE 2001100400042 20011004 00042 NM 2001 10 4 AALA20011329 1 20010630 A 3397 WIRE BOEING 727 727227 1384078 NM CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 21 723AA 20731 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT DIM. REPLACED EMERGENCY EXIT LIGHT JUMPER WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001100400043 20011004 00043 WP 2001 10 4 MWEA011335 1 20011001 A 5320 9930582 ATTACH ANGLE DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 STATION 826 FORWARD KEEL VERTICAL ATTACH ANGLE REQUIRES REMOVAL TO FACILITATE OTHER MAINTENANCE AT LONGERON 30. FOUND EL ONGATED HOLES. MAINTENANCE FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F A6WE 2001100400044 20011004 00044 WP 2001 10 4 MWEA011337 1 20011001 A 5730 5937533 SKIN DOUG DC9 DC981 3022081 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 RIGHT WING LEADING EDGE LOWER SKIN HAS MODERATE CORROSION ON LOWER AND UPPER SURFACE, AROUND AND UNDER NUT PLATES, STATI ON XOS 592-604. FABRICATED AND INSTALLED REPAIR TITANIUM STRAP. 2 L 7 2 4F A6WE 2001100400045 20011004 00045 WP 2001 10 4 MWEA011341 1 20010927 A 5311 59114481 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 E&E COMPARTMENT FRAME STATION 180 HAS LIGHT CORROSION ON FORWARD SIDE FROM LONGERON 28 RIGHT TO 30. FABRICATED AND INSTA LLED FRAME REPAIR. 2 L 7 2 4F A6WE 2001100400046 20011004 00046 WP 2001 10 4 MWEA011342 1 20010927 A 5311 9911520389 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 CORROSION ON BOTTOM FACE OF FRAME, STATION 218, BETWEEN AND EXTENDING UNDER LONGERONS 30 AND 29 LEFT. FABRICATED AND INS TALLED REPAIR ANGLES AND PLATES. 2 L 7 2 4F A6WE 2001100400047 20011004 00047 SO 2001 10 4 C2XA01IA366 1 20011001 A 3350 BS2197 BATTERY EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16723 14754 254 120169 DURING SCHEDULED MAINTENANCE THE CENTER SECTION OF CABIN EMERGENCY LIGHTS WERE FOUND TO TURN ON AND OFF INTERMITTANTLY. MAINTENANCE REMOVED AND REPLACED THE CENTER SECTION EMERGENCY LIGHT BATTERY PACK. THE EMERGENCY LIGHTING SYSTEM WAS OPER ATIONALLY CHECKED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001100400048 20011004 00048 SO 2001 10 4 C2XA01IA365 1 20011001 A 3350 AD2047 BATTERY EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16723 4654 706 120169 DURING SCHEDULED MAINTENANCE, THE FORWARD CABIN EMERGENCY LIGHTS WERE FOUND TO TURN ON AND OFF INTERMITTANTLY. MAINTENAN CE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT BATTERY PACK. THE SYSTEM WAS OPERATIONALLY CHECKED AND THE AIRCRAFT APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001100400049 20011004 00049 WP 2001 10 4 MWEA011343 1 20010927 A 5310 5917579237 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 VENTRAL DOOR JAMB HAS 4 EACH HOLES THAT ARE ELONGATED. HOLES ARE UNDER SILL PLATE. FABRICATED AND INSTALLED SCUFF PLATE AND REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001100400050 20011004 00050 WP 2001 10 4 MWEA011345 1 20010927 A 5311 59114481 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 CORROSION ON LOWER CHANNEL OF FRAME, STATION 332, LONGERON 30. REMOVED AND REPLACED SECTION OF FRAME AND SPLICE DOUBLERS . 2 L 7 2 4F A6WE 2001100400052 20011004 00052 WP 2001 10 4 MWEA011346 1 20010927 A 5311 59114481 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 CORROSION ON LOWER CHANNEL OF FRAME, STATION 313, LONGERON 30. FABRICATED AND INSTALLED REPAIR DOUBLERS AND PLATES. 2 L 7 2 4F A6WE 2001100400053 20011004 00053 WP 2001 10 4 MWEA011347 1 20010927 A 5330 591142485 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 FUSELAGE SKIN BETWEEN STATION 813-832 HAS AREAS OF LIGHT CORROSION UNDER CHAFE STRIP AROUND NUT PLATE HOLES FROM LONGERO N 21 THROUGH LONGERON 26 RIGHT. FABRICATED AND INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F A6WE 2001100400055 20011004 00055 WP 2001 10 4 MWEA011350 1 20010927 A 5530 591214159 ANGLE DOUG DC9 DC932 3022066 WP VERTICAL STAB CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 EXFOLIATION CORROSION ON AFT END OF VERTICAL STABILIZER ATTACH ANGLE LEFT SIDE, STATION 1121. FABRICATED AND INSTALLED A NGLE REPAIR. 2 L 7 2 4F A6WE 2001100400057 20011004 00057 WP 2001 10 4 MWEA011352 1 20010924 A 3260 0080004003 CONTROL BOX DOUG DC9 DC932 3022066 WP E/E BAY FAULTY A MWEA L ABORTED APPROACH N FALSE WARNING CR CRUISE 1 GL 31 212ME 47701 IN CRUISE NOSE GEAR UNSAFE LIGHT CAME ON, RIGHT GEAR HANDLE UP, RED LIGHT ON IN CRUISE AND APPROACH, LOWERED GEARS, NOSE GEAR RED STAYED ON. QRH PERFORMED, CONFIRMED VISUALLY NOSE GEAR DOWN AND LOCKED. INSPECTED NOSE GEAR SYSTEM, REMOVED A ND REPLACED PROXIMITY SWITCH CONTROL BOX AND TESTED CIRCUIT. OPS CHECK GOOD, NO DEFECTS. 2 L 7 2 4F A6WE 2001100400058 20011004 00058 WP 2001 10 4 MWEA011353 1 20010927 A 5522 591041234 SKIN DOUG DC9 DC932 3022066 WP ELEVATOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 TOPSIDE OF LEFT ELEVATOR HAS AN AREA OF CORROSION 36 INCHES INBOARD FROM OUTBOARD TIP. FABRICATED AND INSTALLED SKIN/PAN EL. 2 L 7 2 4F A6WE 2001100400059 20011004 00059 WP 2001 10 4 MWEA011354 1 20010927 A 5320 591015835 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 AFT CARGO BAY JAMB WEB BETWEEN STATION 889 THROUGH STATION 897 HAS SEVERAL AREAS OF LIGHT CORROSION AROUND FASTENER HOLE S (INTERNAL AND EXTERNAL) BETWEEN LONGERON 24 RIGHT THROUGH LONGERON 28 RIGHT. REMOVED CORROSION FROM STIFFENERS AND FAB RICATED AND INSTALLED WEB SECTION. 2 L 7 2 4F A6WE 2001100400060 20011004 00060 WP 2001 10 4 MWEA011359 1 20010927 A 5313 527779225 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 LONGERON 23 RIGHT HAS LIGHT CORROSION AT STATION 579-580. FABRICATED AND INSTALLED LONGERON AND REPAIR SPLICE. 2 L 7 2 4F A6WE 2001100400061 20011004 00061 WP 2001 10 4 MWEA011360 1 20010927 A 5320 5912528501 PAN DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 AFT CARGO BAY FORWARD JAMB PAN HAS AREAS OF LIGHT CORROSION BETWEEN LONGERON 25 THROUGH LONGERON 26 RIGHT. FABRICATED AN D INSTALLED REPLACEMENT SECTION OF PAN, DOUBLERS, AND SHIM. 2 L 7 2 4F A6WE 2001100400062 20011004 00062 WP 2001 10 4 MWEA011362 1 20010927 A 5230 591014167 PAN DOUG DC9 DC932 3022066 WP CARGO DOOR GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 FORWARD CARGO DOOR HAS A DEEP GOUGE IN THE PAN RADIUS JUST OUTBOARD OF THE DOOR FORWARD ROTATING CAM LOCK. FABRICATED AN D INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 2001100400063 20011004 00063 NM 2001 10 4 AALA20011291 1 20010625 A 3397 WIRE BOEING 727 727223 1384074 NM AIRSTAIRS BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 864AA 21369 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WI RE AT AFT AIRSTAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001100400064 20011004 00064 NM 2001 10 4 AALA20011295 1 20010619 A 3350 LIGR013 LIGHT BOEING 727 727227 1384078 NM SERVICE DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 725AA 20732 TUL - FOUND AFT SERVICE AND GALLEY DOORS AFT LIGHT ASSEMBLY FOR EACH HAS LAMP OUT IN LIGHT ASSEMBLIES FOR EMERGENCY EXIT . INSTALLED NEW LAMP ASSEMBLY AT AFT SIDE EACH DOOR. OPS CHECKED OK. (M) 2 L 7 3 4F A3WE 2001100400065 20011004 00065 NM 2001 10 4 AALA20011318 1 20010628 A 3350 1001141 LIGHT BOEING 727 727223 1384074 NM AIRSTAIR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 848AA 20989 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASS EMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001100400066 20011004 00066 NM 2001 10 4 AALA20011328 1 20010630 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 723AA 20731 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT AT SEAT 8 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001100400067 20011004 00067 NM 2001 10 4 AALA20011338 1 20010702 A 3350 1000679 LIGHT BOEING 727 727227 1384078 NM AFT AIRSTAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 718AA 20611 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AS SEMBLY AT AFT AIRSTAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001100400068 20011004 00068 NM 2001 10 4 AALA20011414 1 20010719 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 883AA 21522 TUL - LIGHT FLICKERS. REPLACED LIGHT OPS CHECKS GOOD. (M) 2 L 7 3 4F A3WE 2001100400069 20011004 00069 NM 2001 10 4 AALA20011496 1 20010725 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 717AA 20610 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTING FORWARD SECTION INOPERATIVE. REPLACED EMERGENCY EXIT ESCAPE PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001100400070 20011004 00070 NM 2001 10 4 AALA20011513 1 20010727 A 3397 CONNECTOR BOEING 727 727223 1384074 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 848AA 20989 MIA - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY SIGN BETWEEN L1 AND R1 INOPERATIVE. RECONNECTED EMERGENCY EXIT S IGN CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001100400071 20011004 00071 NM 2001 10 4 AALA20011522 1 20010728 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 873AA 21385 MIA - DURING OVERNIGHT MAINTENANCE, AFT ENTRY DOOR EMERGENCY EXIT ESCAPE PATH LIGHT INOPERATIVE. REPAIRED WIRE TO EMERG ENCY EXIT ESCAPE PATH LIGHT AT AFT ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001100400072 20011004 00072 NM 2001 10 4 AALA20011525 1 20010727 A 3350 1001141 LIGHT BOEING 727 727223 1384074 NM AFT AIRSTAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 860AA 21087 DTW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT STAIRWAY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASS EMBLY AT AFT STAIRWAY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001100400073 20011004 00073 NE 2001 10 4 AWXA200100512 2 20011001 A 7250 2A2175 NIPPLE IAE AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE #2 ENG LOOSE A AWXA E ENGINE SHUTDOWN J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 28 626AW V0340 65 V0340 PHX - ENG FIRE/SMOKE - FLT 14 - "C" - AFTER LANDING, WHEN TAXING OFF RUNWAY, ECAM MESSAGE APPEARED, NO. 2 ENG. FIRE AND CREW SHUTDOWN #2 ENG. OVERHEAD #2 FIRE PUSHBUTTON DID NOT ILLUMINATE. ALL ENG PARAMETERS WERE NORMAL, SMOKE WAS OBSERVED BY THE FIRE DEPT FROM THE TAILPIPE. MAINTENANCE INSPECTED AND FOUND #5 BEARING OIL PRESS. LINE FITTING LOOSE BEHIND REA R COVER, SAFETY WIRE STILL INTACT, BUT LOOSE. MAINTENANCE REPLACED THE PACKING AND TORQUED THE FITTING. ALSO REPLACED TH E REAR COVER SEAL AND SCAVANGE LINE SEALS DUE TO SIGNS OF LEAKAGE/SEEPAGE. REPLACED SCAVANGE LINE BRACKET DUE TO CRACK F OUND. PERFORMED ENG RUN AND NO FURTHER LEAKAGE NOTED. REF AMM 71-00-02 & 72-51-41 FOR WORK PERFORMED. 2 L 7 2 4F 4 F RT A28NM E311NE 2001100400074 20011004 00074 NM 2001 10 4 AALA20011548 1 20010730 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 886AA 21525 DFW - DURING OVERNIGHT MAINTENANCE CEILING EMERGENCY LIGHT AT SEAT ROW 8 DIM. REPLACED CEILING EMERGENCY LIGHT ASSEMBLY AT SEAT ROW 8. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001100400075 20011004 00075 NM 2001 10 4 AALA20011549 1 20010730 A 3350 LIGHT BOEING 727 727223 1384074 NM R1 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 879AA 21391 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT R1 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001100400076 20011004 00076 NM 2001 10 4 AALA20011678 1 20010821 A 3397 HARNESS BOEING 757 757223 1384957 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 676AN 29426 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT ROWS 1 AND 2 INOPERATIVE. RECONNECTED WIRING HARNES S. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001100400077 20011004 00077 NM 2001 10 4 AALA20011687 1 20010822 A 3397 CONNECTOR BOEING 757 757223 1384957 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 612AA 24488 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT ROWS 9 THROUGH 16 INOPERATIVE. RECONNECTED TR ACK LIGHTING CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001100400078 20011004 00078 NM 2001 10 4 AALA20011688 1 20010824 A 3350 LIGHT DOUG MD11 MD11 3023602 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1765B 48596 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT L4 DOOR INOPERATIVE. REPLACED LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 2001100400079 20011004 00079 NM 2001 10 4 AALA20011694 1 20010824 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 182AN 29592 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT INOPERATIVE AT CLASS DIVIDER. REPLACED LIGHT STRIP. SYST EM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001100400080 20011004 00080 NM 2001 10 4 AALA20011724 1 20010830 A 3350 P4010051112 MODULE BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 621AM 24579 DFW - DURING OVERNIGHT MAINTENANCE, AFT EMERGENCY EXIT SEAT LIGHTS INOPERATIVE. REPLACED MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001100400081 20011004 00081 WP 2001 10 4 AALA20011731 1 20010911 A 3397 WIRE DOUG DC9 DC983 3022083 WP AIRSTAIRS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 438AA 49456 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT STAIRS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT WIRE AT AFT AIRSTAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001100400082 20011004 00082 NM 2001 10 4 AALA20011733 1 20010910 A 2530 OVEN BOEING 767 767223 1385123 NM GALLEY DIRTY A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 323AA 22324 GLA - FLT 53 - EN ROUTE GLA-ORD, DETECTED ELECTRICAL SMELL AT FIRST CLASS OVEN. TURNED OFF OVEN. LANDED ORD WITHOUT FU RTHER INCIDENT. CLEANED FIRST CLASS OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001100400090 20011004 00090 NM 2001 10 4 AALA20011734 1 20010827 A 2421 GEN3014 IDG BOEING 777 777223 1385213 NM RT ENGINE MALFUNCTIONED A AALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SW 21 770AN 29578 FLT 128 - FOUND RIGHT GEN IDG DISCONNECTED INFLIGHT. REPLACED RIGHT IDG LEAK AND OPS OK PER MM. (M) 2 L 7 2 4F RT T00001SE 2001100400092 20011004 00092 NE 2001 10 4 IY22001F00003 2 20010524 A 7250 3028601 BLADE CESSNA 500 500CESSNA 2076602 CE PWA JD15 JT15D1A NE TURBINE WHEEL BROKEN A IY2R K NONE O OTHER IN INSP/MAINT 1 SW 15 8DE 2717 166 HIGH TURBINE BLADE BROKE OFF APPROXIMATELY .500 INCH FROM THE BLADE TIP. ONE OTHER BLADE IS CRACKED ABOUT MID-CENTER OF THE BLADE. THESE BLADES HAVE A LIFE LIMIT OF 3500 HOURS. 1 L 7 2 4F 4 F A22CE E25EA 2001100400093 20011004 00093 2001 10 4 SWAA012627 4 20010924 A 2565 65574632 BRACKET BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED C CHECK, FOUND AFT SVC DOOR AFT FLOOR GIRT BAR BRACKET LOOSE. TIGHTENED AFT GI RT BAR BRACKET PER MM. 2 L 7 2 4F A16WE 2001100400094 20011004 00094 NM 2001 10 4 SWAA012629 1 20010924 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 316SW 23338 DURING SCHEDULED PM CHECK, FOUND STRINGER CRACKED AT BS 747,STR 19L. REPAIRED STR PER SRM. 2 L 7 2 4F RT A16WE 2001100400095 20011004 00095 NM 2001 10 4 SWAA012630 1 20010924 A 3350 07912 COVER BOEING 737 7377H4 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 733SA 27865 DURING SCHEDULED C4 CHECK, FOUND EEPLS TRACK COVERS CRACKED AT SEVERAL LOCATIONS IN CABIN. R & R TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 2001100400096 20011004 00096 NM 2001 10 4 SWAA012631 1 20010924 A 3350 07912 COVER BOEING 737 7377H4 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 765SW 29805 DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK COVERS CRACKED AT SEVERAL LOCATIONS IN CABIN. R & R TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 2001100400097 20011004 00097 NM 2001 10 4 SWAA012634 1 20010923 A 5330 6545774 SKIN BOEING 737 7372K6 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 757 BELOW LH EXTERIOR EMERGENCY EXIT LIGHT. R EPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001100400098 20011004 00098 NM 2001 10 4 SWAA012635 1 20010923 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING WALK AROUND INSPECTION FOUND FUSELAGE SKIN CRACKED 4 INCHES LONG BETWEEN BS 500A & BS 500C, STR 14R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001100400099 20011004 00099 NM 2001 10 4 SWAA012640 1 20010924 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 640SW 27713 EEPLS MISSING COVER AT ROW # 6. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2001100400100 20011004 00100 NM 2001 10 4 SWAA012641 1 20010923 A 5330 141A880 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED ON CAPTIAN'S # 1 WINDOW POST UPPER AFT CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001100400101 20011004 00101 NM 2001 10 4 SWAA012644 1 20010924 A 5330 6545409245 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED 1/2D CHECK, FOUND BEADED FLOOR WEB CRACKED ( 2 EA ) AT BS 665, RBL 39.5 & LBL 39. REPAIRED WEB PER SWA RA 1-353-2644. 2 L 7 2 4F RT A16WE 2001100400102 20011004 00102 NM 2001 10 4 SWAA012646 1 20010925 A 2731 BACB28AK04 BUSHING BOEING 737 7373H4 1384600 NM LH ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 639SW 27712 DURING SCHEDULED 1/2D CHECK AT DALFORT, FOUND LH ELEVATOR TAB # 2 HINGE WORN. R&R TAB BUSHING P ER MM. 2 L 7 2 4F RT A16WE 2001100400103 20011004 00103 NM 2001 10 4 SWAA012647 1 20010925 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 612SW 27930 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001100400104 20011004 00104 NM 2001 10 4 SWAA012648 1 20010924 A 5754 6573714 SLAT BOEING 737 7373H4 1384600 NM LH WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 371SW 26598 DURING SCHEDULED C1 CHECK, FOUND # 1 L/E SLAT CRACKED ( 2 EA ) AT AFT ROW OF FASTENERS NEAR CENTER AUX TRACK. REPAIRED SLAT PER SWA RA 1-357-1107. 2 L 7 2 4F RT A16WE 2001100400105 20011004 00105 NM 2001 10 4 SWAA012649 1 20010923 A 5310 6516300 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED ( 2 EA ) AT BS 178,WL 234, LBL 12 & RBL 9. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001100400106 20011004 00106 NM 2001 10 4 SWAA012650 1 20010923 A 5310 6517582 BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEBS CRACKED ( 3 EA ) AT BS 178, LBL 17.1 & WL 229, BS 185, RBL 17.1 & WL 232, BS 178, RBL 17.1 & WL 220. R&R VERTICAL BEAMS PER SRM. 2 L 7 2 4F RT A16WE 2001100400107 20011004 00107 NM 2001 10 4 SWAA012656 1 20010925 A 5753 6546434 FLAP BOEING 737 737301 1384611 NM LH WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING WALKAROUND INSPECTION FOUND LH INBD T/E FLAP DELAMINATED. R&R FLAP PER MM. 2 L 7 2 4F RT A16WE 2001100400108 20011004 00108 NM 2001 10 4 SWAA012657 1 20010924 A 2560 A170033 COVER BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 EMERGENCY FLASHLIGHT COVER MISSING. INSTALLED COVER PER MM. 2 L 7 2 4F A16WE 2001100400109 20011004 00109 NM 2001 10 4 SWAA012658 1 20010923 A 3350 07912 COVER BOEING 737 7377H4 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 733SA 27865 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED AT ROW 1 & ROW 11. R&R COVERS PER MM. 2 L 7 2 4F RT A16WE 2001100400110 20011004 00110 NM 2001 10 4 SWAA012659 1 20010923 A 2730 251A2345 TORQUE TUBE BOEING 737 7377H4 NM TAIL WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 733SA 27865 DURING SCHEDULED C4 CHECK, BOTH ELEVATORS FAILED FREE PLAY CHECK. R&R ELEVATOR CONTROL BUS TOR QUE TUBE PER MM. 2 L 7 2 4F RT A16WE 2001100400111 20011004 00111 NM 2001 10 4 SWAA012660 1 20010924 A 5753 6546035 FLAP BOEING 737 7373H4 1384600 NM RH WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 612SW 27930 DURING SCHEDULED C4 CHECK, FOUND RH OTBD AFT T/E FLAP DELAMINATED AT INBD END. R&R FLA P PER MM. 2 L 7 2 4F RT A16WE 2001100400112 20011004 00112 NM 2001 10 4 SWAA012661 1 20010926 A 5220 65C35004 HANDLE BOEING 737 7373H4 1384600 NM O/W EXIT DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 639SW 27712 LH OVER WING EMERGENCY EXIT DOOR HANDLE BROKEN. R&R HANDLE PER MM. 2 L 7 2 4F RT A16WE 2001100400113 20011004 00113 NM 2001 10 4 SWAA012663 1 20010925 A 5310 6545819 WEB BOEING 737 7373H4 1384600 NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED 1/2D CHECK, FOUND CEILING PRESS PANEL CUTOUT CRACKED (1 INCH ) IN NOSE W/W AFT INBD CORNER. REPAIRED PANEL CUTOUT PER SWA T1-235-001. 2 L 7 2 4F RT A16WE 2001100400114 20011004 00114 NM 2001 10 4 SWAA012664 1 20010925 A 5330 6545776 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED ( 2 INCHES ) AT BS 830, STR 10R. REPAIR ED SKIN PER SWA RA 1-A53-2545 2 L 7 2 4F A16WE 2001100400115 20011004 00115 NM 2001 10 4 SWAA012666 1 20010924 A 5310 65C27314 TIE CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER TIE CLIPS CRACKED ( 2 EA ) AT BS 400, STR 4R, BS 767, STR 11L. R&R TIE CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001100400116 20011004 00116 NM 2001 10 4 SWAA012668 1 20010920 A 5310 6545629 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAMES CRACKED ( 2 EA ) AT BS 500A & BS 500B, STR 14R. REPAIRED FRAMES PER SRM. 2 L 7 2 4F RT A16WE 2001100400117 20011004 00117 2001 10 4 SWAA012680 4 20010928 A 2565 6943448 BRACKET BOEING 737 7373H4 1384600 NM AFT SVC DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 387SW 26602 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE MOUNT BRACKET CRACKED. R&R MOUNT BRACKET PER MM. 2 L 7 2 4F RT A16WE 2001100400118 20011004 00118 NM 2001 10 4 SWAA012681 1 20010929 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 387SW 26602 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER CRACKED AT ROW 8. R&R EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2001100400119 20011004 00119 NM 2001 10 4 SWAA012682 1 20010929 A 3350 07912 COVER BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 501SW 24178 EEPLS COVER LOOSE AT ROW 1. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2001100400120 20011004 00120 NM 2001 10 4 SWAA012684 1 20010929 A 5310 684568 INTERCOSTAL BOEING 737 7373T5 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED SPECIAL VISIT, FOUND INTERCOSTAL CRACKED AT BS 178, LBL 24 & WL 207. REPAIRED INTERCOSTAL PER SRM. 2 L 7 2 4F RT A16WE 2001100400121 20011004 00121 NM 2001 10 4 SWAA012685 1 20011001 A 5310 BAC5602 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 522SW 26564 DURING SCHEDULED D CHECK AT DALFORT, FOUND Z FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRA ME PER SRM. 2 L 7 2 4F RT A16WE 2001100400122 20011004 00122 NM 2001 10 4 SWAA012687 1 20010927 A 5610 5893543130 WINDOW BOEING 737 7373H4 1384600 NM COCKPIT CRACKED A SWAA O OTHER O OTHER AP APPROACH 1 SW 07 605SW 27956 R1 WINDOW BEGAN ARCING, WINDOW HEAT TURNED OFF, R1 CONTINUED TO PROPAGATE CRACKS IN THE OUTER PANE. PRESSURIZATION NORMA L. R&R R1 WINDOW PER MM. 2 L 7 2 4F RT A16WE 2001100400123 20011004 00123 NM 2001 10 4 SWAA012689 1 20010928 A 5310 BAC1490 ANGLE BOEING 737 7373T5 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED SPECIAL VISIT, FOUND L ANGLES CRACKED ( 2 EA ) AT BS 178, WL 207, LBL 24 & RBL 24. R&R ANGLES PER SRM. 2 L 7 2 4F RT A16WE 2001100400124 20011004 00124 NM 2001 10 4 SWAA012692 1 20010923 A 5310 6546559 FRAME BOEING 737 7373H4 1384600 NM AFT CARGO CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 927, BBL 0. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001100400125 20011004 00125 NM 2001 10 4 SWAA012670 1 20010924 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 FWD OVERHEAD AISLE EXIT LENS COVER FELL OFF. REINSTALLED LENS COVER PER MM. 2 L 7 2 4F RT A16WE 2001100400126 20011004 00126 NM 2001 10 4 SWAA012672 1 20010926 A 3350 07912 COVER BOEING 737 7377H4 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 717SA 27851 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED BETWEEN ROW 1 & ROW 23. R&R COVERS P ER MM. 2 L 7 2 4F RT A16WE 2001100400127 20011004 00127 NM 2001 10 4 SWAA012673 1 20010926 A 2731 6545166 ROD END BOEING 737 7373H4 1384600 NM LH ELEVATOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 342SW 24133 DURING SCHEDULED 1/4D CHECK, FOUND BOTH LH ELEVATOR TRIM TAB ACTUATING ROD ENDS CORRODED AT FWD END. R&R ROD ENDS PER MM. 2 L 7 2 4F RT A16WE 2001100400128 20011004 00128 NM 2001 10 4 SWAA012675 1 20010926 A 5310 6516300 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED ( 2 EA ) AT BS 178, LBL 5, WL 198 & WL 201. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001100400129 20011004 00129 NM 2001 10 4 SWAA012717 1 20011002 A 2731 BACB28AK04 BUSHING BOEING 737 7377H4 NM RH ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 730SW 27862 DURING SCHEDULED RON SI # 11038-55, FOUND RH ELEVATOR TAB BUSHINGS WORN AT # 1 & # 4 HINGES. R&R BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2001100400130 20011004 00130 NM 2001 10 4 SWAA012718 1 20011002 A 5310 6516300 WEB BOEING 737 7373T5 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED SPECIAL VISIT, FOUND WEB CRACKED AT BS 178, WL 187 & RBL 1.0. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001100400131 20011004 00131 NM 2001 10 4 SWAA012719 1 20011002 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 342SW 24133 DURING SCHEDULED 1/4D CHECK, FOUND OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LOOSE & LENS MISSING AT ROW 3 ABC. SECURED LIGHT & INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2001100400132 20011004 00132 NM 2001 10 4 SWAA012720 1 20011002 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED C3 CHECK, FOUND EEPLS COVER BROKEN AT ROW 3 & COVER MISSING AT ROW 17. R EPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2001100400133 20011004 00133 NM 2001 10 4 SWAA012721 1 20010929 A 5310 65C27314 TIE CLIP BOEING 737 7373H4 1384600 NM MID CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED 1/2D CHECK AT DALFORT, FOUND TIE CLIP CRACKED AT BS 663, STR 10R. R&R TIE CLI P PER SRM. 2 L 7 2 4F RT A16WE 2001100400134 20011004 00134 NM 2001 10 4 SWAA012722 1 20011002 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 331SW 23695 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 2.25 INCHES LONG AT BS 747, BETWEEN STR 18R & 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001100400135 20011004 00135 NM 2001 10 4 SWAA012723 1 20011001 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED C1 CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 3B. I NSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2001100400136 20011004 00136 NM 2001 10 4 SWAA012724 1 20011001 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 073SW 22673 DURING WALK AROUND INSPECTION FOUND FUSELAGE SKIN CRACKED 1.5 INCHES LONG AT BS 945, STR 24R. R EPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001100400137 20011004 00137 NM 2001 10 4 SWAA012725 1 20011002 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 060SW 21812 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 831, STR 18L. REPAIRE D SKIN PER SRM. 2 L 7 2 4F A16WE 2001100400139 20011004 00139 NM 2001 10 4 VNAA0110001 1 20011003 A 2697 WIRE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CARGO BAY CHAFED A VNAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 424JS 3033 DURING TAXI, THE CREW RECEIVED AN INTERMITTENT CARGO FIRE CAS MESSAGE AND FIRE WARNING ON THE RED WARNING PANEL. FLIGHT 4019 RETURNED TO THE GATE. MAINTENANCE INSPECTED AND FOUND A CHAFED WIRE. MAINTENANCE REPAIRED THE CHAFED WIRE IN ACC ORDANCE WITH 26-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001100400141 20011004 00141 2001 10 4 VNAA0109018 4 20010926 A 3140 7013348937 DAU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RIGHT FAILED A VNAA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 07 424JS 604 3033 THE CREW REPORTED THAT THE CARGO SMOKE AND FIRE DETECT LIGHTS WERE INTERMITTENTLY COMING ON. MAINTENANCE INSPECTED AND REPLACED THE NUMBER 2 DATA ACQUISITION UNIT IN ACCORDANCE WITH 31-00-00. OPERATION CHECKS WERE PERFORMED AND THE AIRCR AFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001100400146 20011004 00146 SW 2001 10 4 O9I2001F00000 1 20010906 A 7603 8935701 CONTROL ARM GULSTM 690TP 690A 0141722 SW GARRTT TPE331 TPE3315251K NM RT ENGINE DISCONNECTED E O9IA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 09 290PF 4618 11290 P06575 THE RIGHT ENGINE WAS SHUT DOWN AFTER DISCOVERING A NON-RESPONSIVE POWER LEVER DUE TO THE AIRCRAFT POWER LEVER CABLE BECO MING DISCONNECTED FROM THE RIGHT ENGINE PROPELLER PITCH CONTROL (PPC). THE AFFECTED POWER LEVER ARM THAT BECAME DISCONN ECTED IS SPLINED TO A SHAFT ON THE PPC, AND SECURED BY A SAFETY WIRED SCREW. THE SAFETY WIRE ON THE SCREW WAS INTACT. WHEN THE PILOTS RECOGNIZED THE POWER LEVER WAS NON RESPONSIVE, THE AFFECTED ENGINE WAS SHUT DOWN AND THE PROPELLER FEATH ERED. THE AIRPLANE MADE AN UNEVENTFUL LANDING. 1 H 7 2 3T 4 T 2A4 E2WE 2001100400147 20011004 00147 2001 10 4 R7MR33513 4 20010608 A 3160 B19030MC02 DISPLAY SNIAS 350 AS350B3 8680954 EU COCKPIT MALFUNCTIONED A R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 52285 229 3251 VEMD, UNIT HAS INTERMITTENT FAULT CODE FOR THE SAME NON-EXISTENT PROBLEM. ERRORS IN ANALOG DISPLAY. INTERMITTENT AC ST ART PROBLEM. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 2001100400149 20011004 00149 SO 2001 10 4 SAE06011 2 20010625 A 8520 654084A1 CAMSHAFT CESSNA 414 414 2075908 CE CONT O520 TSIO520NB 17040 SO ENGINE DAMAGED A E5ZR K NONE O OTHER IN INSP/MAINT 1 GL 05 414FZ 4140175 519277 THIS ENGINE WAS RECEIVED FOR REPAIR OF METAL IN THE OIL FILTER. ENGINE WAS RECEIVED WITHOUT THE EXHAUST AND TURBOCHARGE R SYSTEMS, AS THESE ARE MAINLY AIRFRAME MOUNTED. THE EXCEPTION IS THAT THE RAM CONVERSION OF THIS ENGINE INCREASES BOTH THE MAXIMUM POWER OUTPUT AND AUW OF THE AIRCRAFT CAUSED BY FITTING OF THE RAM CAMSHAFT. TO PREVENT RECURRENCE OF THIS MISTAKE, ALL FUTURE ENGINE RECEIVED FOR OVERHAUL OR REPAIR WILL BE VETTED FOR ANY INFORMATION REGARDING POSSIBLE RAM CON VERSION PRIOR TO PROCEEDING WITH THE REQUIRED WORK. 1 L 7 2 3O 3 O RT A7CE E8CE 2001100400150 20011004 00150 SO 2001 10 4 SAE06012 2 20010625 A 8520 654837A1 CAMSHAFT CESSNA 414 414 2075908 CE CONT O520 TSIO520NB 17040 SO ENGINE DAMAGED A E5ZR K NONE O OTHER IN INSP/MAINT 1 GL 05 414FZ 4140175 516413H THIS ENGINE WAS RECEIVED FOR REPAIR OF METAL IN THE OIL FILTER. NO REFERENCE ON THE ORDER AS BEING RAM CONVERSION. THE ENGINE WAS RECEIVED WITHOUT THE EXHAUST AND TURBOCHARGER SYSTEMS. THESE ARE MAINLY AIRFRAME MOUNTED. THE RAM CONVERSI ON OF THIS ENGINE INCREASES BOTH THE MAXIMUM POWER OUTPUT AND AUW OF THE AIRCRAFT CAUSED BY FITTING OF THE RAM CAMSHAFT. 1 L 7 2 3O 3 O RT A7CE E8CE 2001100400151 20011004 00151 NM 2001 10 4 AALA20011739 1 20010910 A 2421 GEN3014 IDG BOEING 777 777223 1385213 NM LT ENGINE FAILED A AALA K NONE J WARNING INDICATION CR CRUISE 1 SW 21 777AN 29585 DFW - FLT 158 - AFTER TAKEOFF, AT 15,000 FEET, LEFT ENGINE GEN OFF LIGHT CAME ON. RESET ONCE DUE TO CHECKLIST. OFF LIG HT REMAINED. IDG TEMP NORMAL. REMOVED AND REPLACED LEFT ENGINE IDG. OPS AND LEAK CHECKS GOOD. (M) 2 L 7 2 4F RT T00001SE 2001100400152 20011004 00152 WP 2001 10 4 AALA20011744 1 20010905 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7519A 49896 TUL - FOUND 1485 CANT FRAME IS CRACKED AT STAIR ACTUATOR CASTING. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-33. (M) 2 L 7 2 4F A6WE 2001100400153 20011004 00153 WP 2001 10 4 AALA20011745 1 20010831 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7519A 49896 TUL - FOUND VERY DEEP WORN AREA BL '0' STATION 148 TOP OF FUSELAGE. REMOVED DAMAGED AREA. INSTALLED DOUBLER PER ESO 80 559. (M) 2 L 7 2 4F A6WE 2001100400154 20011004 00154 WP 2001 10 4 AALA20011746 1 20010910 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7519A 49896 TUL - FOUND DENT IN FUSELAGE SKIN AT OUTFLOW VALVE, STATION 1263 BETWEEN LONGERONS 21 AND 22 LEFT. DENTED UP TO 0.115 I NCH DEEP. INSTALLED REPAIR DOUBLER PER ESO 80559. (M) 2 L 7 2 4F A6WE 2001100400155 20011004 00155 WP 2001 10 4 AALA20011747 1 20010830 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7519A 49896 FOUND NR 6 SEAT TRACK CORRODED STATION 609-610. REMOVED DAMAGE AND INSTALLED SEAT TRACK PLUG REPAIR PER SRM 53-05 FIG 4 . (M) 2 L 7 2 4F A6WE 2001100400156 20011004 00156 WP 2001 10 4 AALA20011748 1 20010828 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7519A 49896 TUL - FOUND NR 3 SEAT TRACK CORRODED STATION 1304. INSTALLED PLUG REPAIR PER SRM 53-05 FIG 4A. (M) 2 L 7 2 4F A6WE 2001100400157 20011004 00157 WP 2001 10 4 AALA20011749 1 20010828 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7519A 49896 TUL - FOUND CRACK LEFT SIDE OF L4L AT STATION 160. SPLICED IN NEW SECTION OF LONGERON L4L FROM STATION 147 TO 170 PER S RM 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 2001100400158 20011004 00158 WP 2001 10 4 AALA20011750 1 20010831 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7519A 49896 TUL - FOUND SHEAR TIE CRACKED AT STATION 1451 JUST INBOARD OF LONGERON 2L. REPLACED SHEAR TIE AT STATION 1451 INBOARD O F LONGERON 2L SRM 51-01. (M) 2 L 7 2 4F A6WE 2001100400159 20011004 00159 WP 2001 10 4 AALA20011751 1 20010825 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7519A 49896 TUL - FOUND DENT AT STATION 218 BETWEEN L22R AND 23R ADL 0001. CUT OUT DAMAGE AND INSTALLED FLUSH PATCH PER SRM 53-04-0 0 PERMANENT REPAIR. (M) 2 L 7 2 4F A6WE 2001100400160 20011004 00160 WP 2001 10 4 AALA20011752 1 20010828 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7519A 49896 TUL - FOUND RIGHT CUSP CORRODED BETWEEN STATION 1155 TO STATION 1170. INSTALLED DOUBLER ON RIGHT CUSP STATION 1155 TO 1 170 PER AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 2001100400161 20011004 00161 WP 2001 10 4 AALA20011753 1 20010829 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7519A 49896 TUL - FOUND NR 1 SEAT TRACK CORRODED OUT OF LIMITS AT STATION 1237. INSTALLED SEAT TRACK PLUG REPAIR PER SRM 53-05 FIG 40. (M) 2 L 7 2 4F A6WE 2001100400162 20011004 00162 WP 2001 10 4 AALA20011754 1 20010828 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7519A 49896 TUL - FOUND NR 1 SEAT TRACK HAS CORROSION AT AFT G-4 GALLEY MOUNT. INSTALLED SEAT TRACK PLUG REPAIR PER SRM 53-05 FIG 4 A. (M) 2 L 7 2 4F A6WE 2001100400163 20011004 00163 WP 2001 10 4 AALA20011755 1 20010830 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7519A 49896 TUL - FOUND RIGHT TUNNEL (MID CARGO) STATION 625, CUSP HAS HOLE IN IT. REAMED HOLE AND INSTALLED HI-LOCK PER ESO NR 805 59, DATED 8-30-01. (M) 2 L 7 2 4F A6WE 2001100400164 20011004 00164 WP 2001 10 4 AALA20011756 1 20010828 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7519A 49896 TUL - FOUND WINDOW PANEL CRACKED AT AFT UPPER CORNER BETWEEN STRINGER 1041-1060. CUT OUT CRACK PORTION. INSTALLED DOUB LER ON WINDOW PANEL AT STATION 1041-1060 SRM 53-10-00-25. (M) 2 L 7 2 4F A6WE 2001100400165 20011004 00165 WP 2001 10 4 AALA20011758 1 20010904 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 437AA 49455 TUL - FOUND SKIN CRACKED AT RIVET STATION 1380 BELOW LONGERON 13L. INSTALLED DOUBLER AT STATION 1380 LONGERON 13L IAW A ARD 53-30-00-00 AND SRM 53-01 FIG 2 SHEET 3. (M) 2 L 7 2 4F RT A6WE 2001100400166 20011004 00166 WP 2001 10 4 AALA20011759 1 20010904 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 437AA 49455 TUL - FOUND DENT AT STATION 256 BETWEEN L18 AND L19 LEFT OUT OF LIMITS. INSTALLED REPAIR DOUBLER PER SRM 53-04-01 FIG 1 2B AND AARD 53-30-00-9. (M) 2 L 7 2 4F RT A6WE 2001100400167 20011004 00167 WP 2001 10 4 AALA20011760 1 20010831 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 437AA 49455 TUL - FOUND CORROSION AROUND ATTACHMENT HOLES IN LEFT CUSP, UNDER GIRT BAR SUPPORT FOR LEFT AFT GALLEY DOOR SLIDE. CORR OSION REMOVED, REMOVAL MADE CUSP OUT OF LIMITS, REPAIR DOUBLER INSTALLED PER SRM 53-02. (M) 2 L 7 2 4F RT A6WE 2001100400168 20011004 00168 WP 2001 10 4 AALA20011761 1 20010902 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 437AA 49455 TUL - FOUND DEEP GOUGES ON TOP OF FUSELAGE 4 INCHES AFT OF VERTICAL STAB REAR SPAR 8 RBL. BLENDED GOUGES AND INSTALLED REPAIR DOUBLER PER AARD 53-30-00-2 AND AARD 53-00-00-11. (M) 2 L 7 2 4F RT A6WE 2001100400169 20011004 00169 WP 2001 10 4 AALA20011762 1 20010907 A 5320 ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 437AA 49455 TUL - FOUND ANGLE CRACKED AT FASTENER ON VERTICAL STABILIZER TOO FUSELAGE ATTACH, AT CANT FRAME STATION 1474 LEFT SIDE. INSTALLED DOUBLER REPAIR PER AARD 53-10-00-2. (M) 2 L 7 2 4F RT A6WE 2001100400170 20011004 00170 WP 2001 10 4 AALA20011763 1 20010831 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 437AA 49455 TUL - FOUND CORROSION ON RIGHT CUSP STATION 486-598. REMOVED SECTION OF CUSP AT FACTORY LENGTH AND REPLACED WITH NEW AN D INSTALLED ONE DOUBLER PER 53-01 FIG 4. (M) 2 L 7 2 4F RT A6WE 2001100400171 20011004 00171 WP 2001 10 4 AALA20011764 1 20010904 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 437AA 49455 TUL - FOUND SKIN CRACKED AT RIVET, STATION 1380 BELOW LONGERON 13R. INSTALLED DOUBLER AFTER STOP DRILLING CRACK PER SRM 53-01 FIG NR 2. (M) 2 L 7 2 4F RT A6WE 2001100400172 20011004 00172 WP 2001 10 4 AALA20011765 1 20010830 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 437AA 49455 TUL - FOUND RIGHT CUSP, STATION 598 IS DAMAGED OUTBOARD OF NR 6 SEAT TRACK, FORWARD OF FRAME FITTING. INSTALLED REPAIR DOUBLER IAW SRM 53-01 FIG 4. (M) 2 L 7 2 4F RT A6WE 2001100400173 20011004 00173 NM 2001 10 4 AALA10011743 1 20010831 A 5330 SKIN BOEING 727 727223 1384074 NM FS 1013 A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 884AA 21523 TUL - FOUND BUBBLE IN FUSELAGE SKIN STATION 1013 ABOVE STRINGER 28 LEFT. CUT AND REMOVED DAMAGED SECTION OF SKIN, FABRI CATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-3A. (M) 2 L 7 3 4F A3WE 2001100400174 20011004 00174 SO 2001 10 4 C2XA01TY128 1 20011003 A 5330 14520553001 SKIN EMB 145 EMB145LR SO A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16981 145208 TYS During a scheduled inspection the main cabin door frame skin was found gouged and rubbing on the forward upper cut out. Maintenance blended the gouged and rubbed areas I.A.W.-EMB-GST-3272/01. The repair is satisfactory and the aircraft will be released upon completion of inspection. 2 L 7 2 4T RT T00011AT 2001100500001 20011005 00001 EU 2001 10 5 RAIA00109011 1 20010924 A 3350 6134051 POWER SUPPLY JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA O OTHER L NO TEST IN INSP/MAINT 1 CE 03 560HK 9927 552 41076 7434-STL-FLOOR EMERGENCY PATH LIGHTS OUT BETWEEN ROW 6&7. MAINTENANCE REMOVED AND REPLACED #3 EMERGENCY LIGHT POWER SUPP LY. 2 L 7 2 4T RT A41NM 2001100500002 20011005 00002 EU 2001 10 5 RAIA00109012 1 20010923 A 7800 14178007805 EXHAUST PIPE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 559HK 41075 75093 5409-STR-FIRE WARNING INDICATION,LEFT HAND ENGINE. MAINTENANCE INSPECTED AND FOUND NO EVIDENCE OF FIRE.IDENTIFIED JET PI PE INSULATION DETERIORATED. REMOVED AND REPLACED LEFT HAND JET PIPE. 2 L 7 2 4T 4 T RT A41NM E18NE 2001100500003 20011005 00003 EU 2001 10 5 RAIA00109013 1 20010924 A 2612 51228532 FIRE LOOP JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE DEFECTIVE A RAIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 03 559HK 41075 75093 9547-SYR-LEFT HAND ENGINE FIRE LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED LEFT HAND ENGINE FIRE LOOP. 2 L 7 2 4T 4 T RT A41NM E18NE 2001100500004 20011005 00004 EU 2001 10 5 RAIA00109014 1 20010927 A 7600 30005000044 TORQUE SENSOR AEROSP ATR42 ATR42300 8680920 EU INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 423TE 10223 119 7408-STL-AUTO TRIM POWER CONTROL SYSTEM INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LEFT HAND ENGINE TORQUE SIGNAL CON DITIONER 2 H 7 2 4T RT A53EU 2001100500005 20011005 00005 WP 2001 10 5 AALA20011671 1 20010822 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 400AA 49311 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY EXIT PATH LIGHTS DIM. REPLACED BATTERY PACK. SYSTEM GROUND CHECK ED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100500006 20011005 00006 WP 2001 10 5 AALA20011668 1 20010820 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 77421 49333 BDL - FOUND DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING FROM ROW 20 THROUGH 31 INOPERATIVE. REPLACED BAT TERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100500007 20011005 00007 WP 2001 10 5 AALA20011697 1 20010826 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 587AA 53250 DEN - DURING OVERNIGHT MAINTENANCE, EMERGENCY CABIN LIGHTING IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100500008 20011005 00008 WP 2001 10 5 AALA20011698 1 20010826 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 556AA 53086 DEN - DURING OVERNIGHT MAINTENANCE, EMERGENCY CABIN LIGHTING IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100500009 20011005 00009 WP 2001 10 5 AALA20011692 1 20010824 A 3350 60030541 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 457AA 49562 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS OVER AFT STAIRS DIMS. REPLACED BATTERY PACK. SYSTEM GROUND CHECKE D NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100500010 20011005 00010 WP 2001 10 5 AALA20011693 1 20010824 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 416AA 49327 TUL - DURING OVERNIGHT MAINTENANCE, EMERGENCY CABIN LIGHTS AT ROWS 28 AND 29 INOPERATIVE. REPLACED BATTERY PACK. SYSTE M GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100500011 20011005 00011 WP 2001 10 5 AALA20011551 1 20010731 A 3350 8034001 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 294AA 49306 DFW - DURING OVERNIGHT MAINTENANCE, AFT CABIN SEAT MOUNTED EMERGENCY EXIT ESCAPE PATH LIGHTS DIM. REPLACED AFT CABIN EM ERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100500012 20011005 00012 WP 2001 10 5 AALA20011565 1 20010804 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP TAILCONE DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7536A 49990 ORD - DURING OVERNIGHT MAINTENANCE, 2 TAILCONE GROUND ILLUMINATION EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100500013 20011005 00013 WP 2001 10 5 AALA20011569 1 20010804 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 432AA 49350 RDU - DURING OVERNIGHT MAINTENANCE, VENTRAL STAIRS OVERHEAD EMERGENCY PATH LIGHTING INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100500014 20011005 00014 WP 2001 10 5 AALA20011590 1 20010805 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7521A 49898 BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT OATH LIGHTS OF BOTH AFT OVERWING DOORS INOPERATIVE. REPLACED BATTERY . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100500015 20011005 00015 WP 2001 10 5 AALA20011592 1 20010805 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 228AA 49178 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY PATH LIGHTING IN LOWER TAIL CONE INOPERATIVE. REPLACED BATTERY PACK. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100500016 20011005 00016 WP 2001 10 5 AALA20011594 1 20010805 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 412AA 49323 TPA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT SEAT 9 INOPERATIVE. REPAIRED BROKEN WIRE. SYSTEM G ROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100500017 20011005 00017 SO 2001 10 5 COMA0110150 1 20011001 A 3150 ATG120TR SENSOR EMB 120 EMB120RT SO L/H MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 267CA 120259 FLIGHT 5038. T/O TRIM AURAL WARNING WHEN POWER LEVERS ADVANCED. COULD NOT DUPLICATE DISCREPANCY AND A/C RETURNED TO SE RVICE. DURING CALLBACK MAINTENANCE THE LEFT ELEVATOR TRIM PROXIMITY SENSOR WAS DETERMINED TO BE DEFECTIVE AND WAS REPLA CED. 2 L 7 2 4T RT A31SO 2001100500018 20011005 00018 WP 2001 10 5 AALA20011595 1 20010805 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 434AA 49452 RDU - DURING OVERNIGHT MAINTENANCE, STAIRWAY MOUNTED EMERGENCY EXIT PATH LIGHT INOPERATIVE. CLEANED CONTACTS ON LIGHT A SSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001100500019 20011005 00019 WP 2001 10 5 AALA20011597 1 20010806 A 3397 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 59523 49915 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L1 DOOR DIM. TIGHTENED LOOSE CONNECTOR. GROUND CHECKED NOR MAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100500020 20011005 00020 WP 2001 10 5 AALA20011599 1 20010806 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 588AA 53251 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT 20F INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001100500021 20011005 00021 WP 2001 10 5 AALA20011649 1 20010818 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 498AA 49736 RDU - DURING OVERNIGHT MAINTENANCE, FLIGHT ATTENDANT EMERGENCY FLASH INOPERATIVE. REPLACED BATTERY. SYSTEM GROUND CHEC KED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100500022 20011005 00022 EU 2001 10 5 RAIA00109015 1 20010924 A 2150 1718D000 HEAT EXCHANGER JETAIR JETSTM JETSTM4101 1500501 EU DEFECTIVE A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 03 554HK 1647 1589 41067 5403-RIC-SMOKE AND HOT AIR IN CABIN DURING CLIMB OUT. MAINTENANCE REMOVED AND REPLACED #1 ECS COLD AIR UNIT. 2 L 7 2 4T RT A41NM 2001100500023 20011005 00023 EA 2001 10 5 COMA0160771 1 20011003 A 5300 6003603024 FRAME CNDAIR CL600 CL6002B19 EA F.S.718.00 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 708CA 7937 7235 R/H 718.00 FRAME UPPER AND LOWER FLANGE IS CRACKED BETWEEN STRINGER 11 AND 12.REMOVED CRACKED SECTION OF R/H 718.00 FRAM E AND REPAIRED USING NEW SECTION OF FRAME I/A/W CANADAIR R.E.O. 601R-53-61-193 REV. A. 2 L 7 2 4F RT A21EA 2001100500024 20011005 00024 WP 2001 10 5 AALA20011651 1 20010818 A 3350 P4010049 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 589AA 53252 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS DIM AT ROW 13 THROUGH 16. REPLACED BATTERY PACK. SY STEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001100500025 20011005 00025 EA 2001 10 5 COMA0160772 1 20011003 A 5300 6003603031 DOUBLER CNDAIR CL600 CL6002B19 EA F.S.718.00 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 708CA 7937 7235 L/H AFT DOUBLER AT F.S. 718.00 BETWEEN STRINGER 11 AND 12 IS CRACKED.REMOVED CRACKED L/H AFT DOUBLER AT F.S. 718.00 AND INSTALLED NEW DOUBLER I/A/W CANADAIR R.E.O. 601R-53-61-193 REV A. 2 L 7 2 4F RT A21EA 2001100500026 20011005 00026 EA 2001 10 5 COMA0160773 1 20011003 A 5300 6003603032 DOUBLER CNDAIR CL600 CL6002B19 EA F.S.718.00 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 708CA 7937 7235 R/H AFT DOUBLER AT F.S. 718.00 BETWEEN STRINGER 11 AND 12 IS CRACKED.REMOVED CRACKED R/H AFT DOUBLER AT F.S. 718.00 AND INSTALLED NEW DOUBLER I/A/W CANADAIR R.E.O. 601R-53-61-193 REV A. 2 L 7 2 4F RT A21EA 2001100500027 20011005 00027 WP 2001 10 5 AALA20011655 1 20010819 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 437AA 49455 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT AT 21D INOPERATIVE. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001100500028 20011005 00028 WP 2001 10 5 AALA20011660 1 20010820 A 3350 SIGN DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 484AA 49677 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT EXIT SIGN OVER R2 DOOR INOPERATIVE. REPLACED R2 DOOR EMER GENCY EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100500029 20011005 00029 WP 2001 10 5 AALA20011670 1 20010820 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 408AA 49319 PHX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT OVERWING EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GRO UND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100900057 20011009 00057 WP 2001 10 9 ABXA010526 1 20011003 A 2750 4913810AS29514 CONTROL CABLE DOUG DC9 DC941 302207N WP T/E FLAP BROKEN A ABXA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 23 966AX 47510 A FLAP RUDDER STOP INOP LIGHT ILLUMINATED WHEN FLAPS WERE SET TO FIVE DEGREES. THE LIGHT EXTINGUISHED AT 15 DEGREES FLAP SETTING AND REMAINED EXTINGUISHED. MAINTENANCE INSPECTED AND REPLACED FLAP CONTROL UP CABLE 75B IAW DC9 MM 27-52-00-02, DUE TO IT BEING BROKEN. 2 L 7 2 4F A6WE 2001100500030 20011005 00030 NM 2001 10 5 ABXA010525 1 20010928 A 5280 141T69205 SEAL BOEING 767 767281 1385109 NM NLG WHEEL WELL WORN A ABXA K NONE E VIBRATION/BUFFET CL CLIMB 1 GL 23 787AX 23020 A MEDIUM FREQUENCY LOUD TONE ACCOMPANIED BY AIRFRAME VIBRATION WAS FELT IN THE YOKE AND RUDDER PEDALS, WHILE CLIMBING TH ROUGH 12000 ACCELERATING TO 280 KNOTS. THE TONE CONTINUED UNTIL FL310. THE TONE CEASED UPON LEVAL OFF AT FL350. MAINTENA NCE INSPECTED THE LEFT AND RIGHT FORWARD GEAR DOORS AND LINKAGES. THE DOORS WERE DEFERRED PER ABX REA B652-42367. LATER, THE NOSE LANDING GEAR SEALS WERE REPLACED, IAW B767 MM32-22-02 AND THE DEFERRAL WAS REMOVED. 2 L 7 2 4F RT A1NM 2001100500031 20011005 00031 WP 2001 10 5 ABXA010523 1 20010920 A 5311 99196182 FRAME DOUG DC9 DC931 3022065 WP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 929AX 45874 MULTIPULE CRACKS WERE FOUND ON FRAME 718 AFT INBOARD FLANGE. THE FIRST CRACK IS LOCATED IN THE MACHINED RADIOUS AND EXTE NDS SIX INCHES FROM THE BASE. THE SECOND CRACK IS 2.5 INCHES LONG AND ORIGINATES AT THE LOWER THROUGH BOLT, EXTENDING TO WARD THE AFT EDGE OF THE FLANGE. MAINTENACE INSPECTED AND FOUND THE DAMAGE TO BE WITHIN LIMITS IAW DC9 SERVICE BULLETIN 53-100 AND ABX REA D953-42388. 2 L 7 2 4F A6WE 2001100500032 20011005 00032 WP 2001 10 5 AALA20011674 1 20010822 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 400AA 49311 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING IN MID CABIN INOPERATIVE. REPLACED BATTERY PACK. SYST EM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100500033 20011005 00033 WP 2001 10 5 AALA20011675 1 20010821 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 400AA 49311 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTS AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED BATTERY PACK . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100500034 20011005 00034 WP 2001 10 5 AALA20011676 1 20010821 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 400AA 49311 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT CEILING LIGHTS AT ROWS 13 THROUGH 16 INOPERATIVE. REPLACED BATTERY P ACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100500035 20011005 00035 WP 2001 10 5 AALA20011679 1 20010821 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 410AA 49321 RDU - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AFT OF OVERWING EXITS INOPERATIVE. REPLACED BATTERY PA CK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100500036 20011005 00036 WP 2001 10 5 AALA20011680 1 20010821 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 246AA 49258 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT ROWS 28 THROUGH 31 INOPERATIVE. REPLACED BATTERY PA CK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100500037 20011005 00037 EA 2001 10 5 COMA0160775 1 20011002 A 2751 7455001 CONTROL BOX CNDAIR CL600 CL6002B19 EA COCKPIT FAULTY A COMA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 868CA 1880 7427 FLIGHT #5593. WHILE PARKED AT THE GATE RECEIVED A FLAP FAIL CAUTION MESSAGE.REPLACED THE FLAP POSITION CONTROL LEVER. 2 L 7 2 4F RT A21EA 2001100500038 20011005 00038 EA 2001 10 5 COMA0160776 1 20011002 A 2750 601R930303 TRANSMITTER CNDAIR CL600 CL6002B19 EA WING FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SO 01 929CA 7035 FLIGHT #5697. DURING CLIMB OUT OF CVG RECEIVED A FLAP CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FI ELD WITH FLAPS OSCILLATING BETWEEN 2 AND 5 ABOVE SELECTED POSITION.REPLACED THE FLAP POSITION TRANSMITTER. 2 L 7 2 4F RT A21EA 2001100500039 20011005 00039 EA 2001 10 5 COMA0160777 1 20011002 A 5415 601370102 PYLON CNDAIR CL600 CL6002B19 EA EMPENNAGE CORRODED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 940CA 16365 7048 DURING REMOVAL OF THE RIGHT ENGINE ASSEMBLY, DISCOVERED PITTING CORROSION ON THE AFT ENGINE PYLON THRUST FITTING MOUNTIN G RIB.REPAIRED IN ACCORDANCE WITH REO 601R-54-50-026. 2 L 7 2 4F RT A21EA 2001101000012 20011010 00012 EA 2001 10 10 COMA0160774 1 20011002 A 2760 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTIONED A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 915CA 7013 FLIGHT 5212. DURING TAXI OUT FROM DTW RECEIVED A FLIGHT SPOILER STATUS MESSAGE, AIRCRAFT RETURNED TO THE GATE. PERFORM ED RESET OF THE FLIGHT SPOILER SYSTEM. 2 L 7 2 4F RT A21EA 2001100500040 20011005 00040 WP 2001 10 5 AALA20011689 1 20010824 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 481AA 49656 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY SEAT LIGHTING INOPERATIVE. REPLACED FORWARD AND MID BATTERY PACKS. SYSTE M GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100500041 20011005 00041 WP 2001 10 5 AALA20011690 1 20010824 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 457AA 49562 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY CEILING LIGHTS OVER ROW 14 DIM. REPLACED BATTERY PACK. SYSTEM GROUND CHE CKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100500042 20011005 00042 WP 2001 10 5 AALA20011701 1 20010828 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 482AA 49675 LAX - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY CABIN LIGHTS AT ROWS 4 THROUGH ROW 6 INOPERATIVE. REPLACED BATTE RY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100500043 20011005 00043 WP 2001 10 5 AALA20011702 1 20010826 A 3350 TERMINAL DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7508 49802 ORD - DURING OVERNIGHT MAINTENANCE, AFT EMERGENCY CEILING LIGHT ABOVE AFT STAIRS DIM. REWIRED BATTERY PACK TERMINALS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100500044 20011005 00044 WP 2001 10 5 AALA20011704 1 20010827 A 3350 AB51 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 439AA 49457 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN AFT CABIN AND STAIRWELL AREA INOPERATIVE. REPLACED EMERGENC Y EXIT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001100500045 20011005 00045 WP 2001 10 5 AALA20011706 1 20010829 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 413AA 49324 ORD - DURING OVERNIGHT MAINTENANCE, OVERWING EMERGENCY EXIT LIGHTS DIM. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED N ORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100500046 20011005 00046 WP 2001 10 5 AALA20011708 1 20010829 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 291AA 49303 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY LIGHTS AT ROWS 16 THROUGH 18 INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100500047 20011005 00047 WP 2001 10 5 AALA20011713 1 20010830 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 297AA 49309 DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIRWELL OVERHEAD EMERGENCY LIGHT DIM. REPLACED BATTERY PACK. SYSTEM GROUND C HECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100500048 20011005 00048 WP 2001 10 5 AALA20011716 1 20010829 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7547A 53029 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT R1 AND R2 DOOR INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100500049 20011005 00049 WP 2001 10 5 AALA20011717 1 20010829 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 488AA 49681 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT FORWARD ENTRY DOOR AND GALLEY SERVICE DOOR VERY DIM. REPLA CED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100500050 20011005 00050 WP 2001 10 5 AALA20011723 1 20010830 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 480AA 49655 DFW - DURING OVERNIGHT MAINTENANCE, OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND C HECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001100500051 20011005 00051 NM 2001 10 5 AALA20011741 1 20010906 A 5510 BEAM BOEING 727 727223 1384074 NM HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 884AA 21523 TUL - FOUND CORROSION ON RIGHT HORIZONTAL STAB UPPER T/E BEAM INBOARD OF NR 7 ELEV HINGE. INSTALLED DOUBLER PER ESO 116 97. (M) 2 L 7 3 4F A3WE 2001100500052 20011005 00052 NM 2001 10 5 AALA20011742 1 20010905 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 884AA 21523 TUL - FOUND DENT WITH CREASE IN FUSELAGE SKIN. CUT OUT DAMAGE AND INSTALLED FILLER AND DOUBLER PER 53-30-3 FIG 3 PAGE 1 3 AND 53-30-3 PART 1 DETAIL 1. (M) 2 L 7 3 4F A3WE 2001100500053 20011005 00053 WP 2001 10 5 AALA20011767 1 20010830 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 437AA 49455 TUL - FOUND NR 5 SEAT TRACK CORRODED AT STATION 234. INSTALLED PLUG REPAIR PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2001100500054 20011005 00054 WP 2001 10 5 AALA20011768 1 20010830 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 437AA 49455 TUL - FOUND CUSP CRACKED OUTBOARD OF NR 5 SEAT TRACK. INSTALLED DOUBLER PER AARD 53-00-00-02. (M) 2 L 7 2 4F RT A6WE 2001100500055 20011005 00055 WP 2001 10 5 AALA20011769 1 20010830 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 437AA 49455 TUL - FOUND RIGHT CUSP CORRODED STATION 1097. INSTALLED DOUBLER PER AARD 53-00-00-02. (M) 2 L 7 2 4F RT A6WE 2001100500056 20011005 00056 WP 2001 10 5 AALA20011770 1 20010830 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 437AA 49455 TUL - FOUND RIGHT CUSP CORRODED STATION 1156-1158. INSTALLED DOUBLER PER AARD 53-00-00-02. (M) 2 L 7 2 4F RT A6WE 2001100500057 20011005 00057 WP 2001 10 5 AALA20011771 1 20010830 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 437AA 49455 TUL - FOUND DEEP GOUGES IN SKIN STATION 589 LONGERON 23 RIGHT. INSTALLED REPAIR PER SRM 53-04 FIG 38. (M) 2 L 7 2 4F RT A6WE 2001100500058 20011005 00058 WP 2001 10 5 AALA20011772 1 20010829 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 437AA 49455 TUL - FOUND CORROSION ON SEAT TRACK NR 1. REMOVED DAMAGED AREA OF NR 1 SEAT TRACK STATION 1235 TO 1238. INSTALLED SEAT TRACK PLUG PER 53-05 FIG 4A. (M) 2 L 7 2 4F RT A6WE 2001100500059 20011005 00059 WP 2001 10 5 AALA20011773 1 20010829 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 437AA 49455 TUL - FOUND SKIN DENTED AND GOUGED AT STATION 1309, BETWEEN L18 AND L19 RIGHT. BLENDED GOUGE. INSTALLED REPAIR DOUBLER AND SCUFF PLATE PER SRM 53-40, FIG 38, SHEET 20 PAGE 18H. (M) 2 L 7 2 4F RT A6WE 2001100500060 20011005 00060 WP 2001 10 5 AALA20011774 1 20010829 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 437AA 49455 TUL - FOUND CORROSION ON LEFT CUSP STATION 674. INSTALLED DOUBLER PER SRM 53-01, AARD 53-00-00-02. (M) 2 L 7 2 4F RT A6WE 2001100500061 20011005 00061 WP 2001 10 5 AALA20011775 1 20010829 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 437AA 49455 TUL - FOUND LONGERON 4L CRACKED STATION 160 BOTH SIDES. REMOVED DAMAGED SECTION OF LONGERON. INSTALLED NEW LONGERON SE CTION AND SPLICE 53-02 FIG 18. (M) 2 L 7 2 4F RT A6WE 2001100500062 20011005 00062 WP 2001 10 5 AALA20011776 1 20010928 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 437AA 49455 TUL - FOUND RIGHT CUSP STATION 290 CORRODED. INSTALLED DOUBLER PER SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2001100500063 20011005 00063 WP 2001 10 5 AALA20011777 1 20010831 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 437AA 49455 TUL - FOUND CORROSION ON LEFT CUSP STATION 1270 AND 1285 BETWEEN NR 1 AND NR 2 SEAT TRACKS. REMOVED CUSP PANEL STATION 1250 TO 1309 PER SRM. REINSTALLED NEW CUSP PANEL STATION 1250 TO 1309 PER SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2001100500064 20011005 00064 NM 2001 10 5 CALA0100897 1 20010925 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 INSPECTION FOUND A .5 INCH CRACK IN FLOOR SUPPORT AT STA 540 BETWEEN RT I/B AND O/B SEAT TRACKS. THE FLOOR SUPPORT WAS R EMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001100500065 20011005 00065 NM 2001 10 5 CALA0100898 1 20010925 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 INSPECTION FOUND A .5 INCH CRACK IN FLOOR SUPPORT AT STA 540, LEFT OF BL 0 FLEX JOINT. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001100500066 20011005 00066 NM 2001 10 5 CALA0100899 1 20010925 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 INSPECTION FOUND UPPER SURFACE OF FLOOR SUPPORT CORRODED AT STA 294-312, LBL 12. THE FLOOR SUPPORT WAS REMOVED AND REPLA CED IAW SRM 51-40-02 AND 51-10-02. 2 L 7 2 4F RT A16WE 2001100500067 20011005 00067 NM 2001 10 5 CALA0100901 1 20010926 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 INSPECTION FOUND UPPER SURFACE OF FLOORBEAM CORRODED AT STA 312, LBL 20 - RBL 20. THE FLOORBEAM CHORD WAS REMOVED AND RE PLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001100500068 20011005 00068 NM 2001 10 5 CALA0100902 1 20010927 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 INSPECTION FOUND FLOOR SUPPORT CORRODED AROUND FASTENER HOLES AT STA 312-328. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001100500069 20011005 00069 NM 2001 10 5 CALA0100904 1 20010928 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 967-986.5, LBL 18. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IA W SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001100500070 20011005 00070 NM 2001 10 5 CALA0100907 1 20010929 A 5314 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10323 23374 INSPECTION FOUND KEEL BEAM CORRODED ON LOWER SURFACE AT STA 705-727, LT SIDE. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5310-03740. 2 L 7 2 4F RT A16WE 2001100500071 20011005 00071 NM 2001 10 5 CALA0100909 1 20010930 A 5320 CLIP BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17306 23357 INSPECTION FOUND SKIN CLIP CORRODED AT STA 500D BETWEEN STRINGER 27L AND 28L. A REPAIR CLIP WAS INSTALLED IAW SRM 53-00- 07, FIGURE 210. 2 L 7 2 4F RT A16WE 2001100500072 20011005 00072 NM 2001 10 5 CALA0100920 1 20011001 A 5320 CHANNEL BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 INSPECTION FOUND FWD LAV WALL HAT SECTION CORRODED AT STA 306, LBL 36-56. THE HAT SECTION WAS REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001100500073 20011005 00073 NM 2001 10 5 CALA0100927 1 20011003 A 5512 SKIN BOEING 737 7373T0 1384582 NM L/H HOR STAB DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10323 23374 INSPECTION FOUND THE L/H HORIZONTAL STABILIZER FIXED L/E SKIN DENTED AT SECOND RIB FROM I/B. A REPAIR WAS INSTALLED IAW SRM 55-10-01, PAGE 202. 2 L 7 2 4F RT A16WE 2001100500074 20011005 00074 NM 2001 10 5 CALA0100928 1 20011003 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM STA 947.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 INSPECTION FOUND FLOORBEAM UPPER CAP CORRODED AT STA 947.5, LBL 6 TO RBL 6. THE FLOORBEAM UPPER CAP WAS REMOVED AND REPL ACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001100500075 20011005 00075 NM 2001 10 5 CALA0100929 1 20011004 A 5512 SKIN BOEING 737 7373T0 1384582 NM RSS 129 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17306 23357 INSPECTION FOUND A 1.25" CRACK IN R/H HORIZONTAL STABILIZER SKIN FORWARD OF I/B BALANCE PANEL AT REAR SPAR STA 129. AN I NTERIM AIRWORTHY REPAIR WAS INSTALLED IAW ECRA 5510-01601. A DIP WAS ISSUED TO REINSPECT THE AREA AT INTERVALS NOT TO EX CEED 3000 FLIGHT HOURS UNTIL A PERMANENT REPAIR IS COMPLETED PRIOR TO THE ACCUMULATION OF 15,000 FLIGHT HOURS. 2 L 7 2 4F RT A16WE 2001100500076 20011005 00076 NM 2001 10 5 CALA0100930 1 20011004 A 5344 FITTING BOEING 737 7373T0 1384582 NM L2 DR HINGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17306 23357 INSPECTION FOUND A 2" CRACK IN L-2 DOOR LOWER HINGE FITTING. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001100500077 20011005 00077 NM 2001 10 5 CALA0100931 1 20011004 A 5542 SKIN BOEING 737 7373T0 1384582 NM R/H RUDDER GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10323 23374 INSPECTION FOUND R/H RUDDER L/E SKIN GOUGED BELOW ACCESS PANEL 9559. REPAIRED IAW SRM 51-70-17 AND ECRA 5543-01017. 2 L 7 2 4F RT A16WE 2001100500078 20011005 00078 NM 2001 10 5 CALA0100932 1 20011004 A 5230 SKIN BOEING 737 7373T0 1384582 NM C-2 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17306 23357 INSPECTION FOUND A 1/2" CRACK AT LIGHTENING HOLE IN C-2 DOOR INNER SKIN. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5230-01 627. 2 L 7 2 4F RT A16WE 2001100500079 20011005 00079 NM 2001 10 5 CALA0100933 1 20011005 A 5230 SKIN BOEING 737 7373T0 1384582 NM C-2 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17306 23357 INSPECTION FOUND A 1/4" CRACK AT LIGHTENING HOLE OF C-2 DOOR INNER SKIN. A REPAIR WAS INSTALLED IAW ECRA 5230-01629. 2 L 7 2 4F RT A16WE 2001100500080 20011005 00080 NM 2001 10 5 CALA0100921 1 20011002 A 5320 FITTING BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 INSPECTION FOUND GALLEY MOUNT FITTINGS ON FLOORBEAM CORRODED AT STA 270-294, RBL 43 AND AT STA 294, RBL 12. THE TWO GALL EY MOUNT FITTINGS WERE REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001100500081 20011005 00081 WP 2001 10 5 CALA0100926 1 20010929 A 2612 WARNING SYSTEM DOUG DC10 DC1030 3023501 WP COCKPIT MALFUNCTIONED A CALA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SW 09 12064 47862 A FORWARD CARGO FIRE WARNING WAS INDICATED AT 10,000 FEET ON APPROACH TO HNL. BOTH FIRE BOTTLES WERE DISCHARGED AND THE AIRCRAFT LANDED AT HNL WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE FIRE WARNING SYSTEM WAS TROUBLESHOT AND NO FAULTS WERE FOUND. THE FAILURE COULD NOT BE DUPLICATED. BOTH FIRE BOTTLES WERE REPLACED IAW MM 26-22-02. 2 L 7 3 4F A22WE 2001100500082 20011005 00082 NE 2001 10 5 AWXA200100475 2 20010925 A 7320 UL16688 SENSE LINE BOEING 757 7572G7 1384963 NM RROYCE RB211 RB211535E4 54555 NE NR 2 ENGINE SEVERED A AWXA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 WP 28 908AW 719 24233 MCI - DIVERTED FLT - FLT 807 - ENROUTE FROM BWI TO PHX, FL 390, THE NR 2 ENGINE WOULD NOT PRODUCE COMMANDED POWER AND TH E AIRCRAFT DIVERTED TO MCI MAKING AN UNEVENTFUL LANDING. MAINTENANCE TROUBLESHOT AND FOUND THE NR 2 ENG P-1 AIR SENSE LI NE, PN UL16688 CHAFFED THROUGH AND SEVERED BY A CLAMP. THE SAME LINE AND CLAMPS HAD BEEN REPLACED ON 7/9/01 DUE TO WEAR FOUND DURING A-7 CHECK. 2 L 7 2 4F 4 F RT A2NM E12EU 2001100500083 20011005 00083 NM 2001 10 5 AWXA200100480 1 20010823 A 5512 65C27494 SKIN BOEING 737 737301 1384611 NM HORIZ STAB DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 MCN - C16 CK - DENT IN RT HORIZONTAL STABILIZER SKIN 2.5 INCH WIDE X .065 DEEP, STA 239 INTER SPAR AREA, BEYOND SRM LIMI TS. MAINTENANCE CUT OUT DAMAGED AREA, FORMED DOUBLER, FILLERS, AND ANGLES AND INSTALLED REPAIR PARTS IAW B737 SRM 55-10- 01, PG 225, 228. 2 L 7 2 4F RT A16WE 2001100500084 20011005 00084 NM 2001 10 5 AWXA200100484 1 20010830 A 5330 6545769 SKIN BOEING 737 737301 1384611 NM FUSELAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 MCN - C16 CK - NON STANDARD REPAIR INSTALLED AT BS 440 TO 490, STR 26R TO 28R BELOW FWD CARGO DOOR. MAINTENANCE REMOVED NON STANDARD REPAIR, TRIMMED OUT DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED IAW AWA ER 03-5300-01264-BA1. 2 L 7 2 4F RT A16WE 2001100500085 20011005 00085 NM 2001 10 5 AWXA200100486 1 20010823 A 5512 65737943 SKIN BOEING 737 737301 1384611 NM HORIZ STAB DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 MCN - C16 CK - PERMANENT REPAIR TO DENT IN RT HORIZONTAL STABILIZER LOWER SKIN, STA 111.10, THAT HAD PREVIOUSLY BEEN PLA CED ON A DEFERRED MAINTENANCE ITEM UNTIL C CHECK. MAINTENANCE REMOVED DAMAGED SKIN SECTION (STA 89 TO 116), FABRICATED N EW SKIN SECTION, INTERNAL & EXTERNAL REPAIR PLATES AND INSTALLED REPAIR PARTS IAW AWA ER 03-5513-01264-TB2. 2 L 7 2 4F RT A16WE 2001101200141 20011012 00141 WP 2001 10 12 SABA011051 2 20011005 A 7200 310440001 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UAR 01514 WP LEFT POWER LOSS A SABA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 33 965AE 965 66261C FLIGHT 5214 FROM LEX TO CLT; THE LEFT ENGINE WOULD MAKE ONLY 10 PERCENT TORQUE. TAKEOFF WAS ABORTED. AIRCRAFT RETURNED TO GATE. GROUND RUN OF THE NUMBER ONE ENGINE, IN ALL RANGES WAS PERFORMED. ENGINE RUN AND OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A56EU E4WE 2001100500086 20011005 00086 NM 2001 10 5 AWXA200100487 1 20010823 A 5330 6546881150 SKIN BOEING 737 737301 1384611 NM FUSELAGE DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 MCN - C16 CK - DENT IN FUSELAGE SKIN BS 1017, BETWEEN STR 15R & 16R, .5 INCH LONG X .5 INCH WIDE X .060 DEEP, BEYOND SRM LIMITS. MAINTENANCE CUT OUT DAMAGED AREA AND FABRICATED REPAIR PARTS AND INSTALLED IAW AWA ER 03-5331-01269-DL1. 2 L 7 2 4F RT A16WE 2001100500087 20011005 00087 NM 2001 10 5 AWXA200100489 1 20011001 A 3246 314395 WHEEL BOEING 737 737277 1384570 NM LT MLG FRACTURED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 26014 235 22646 LAX - WHEEL HUB FAILURE - DURING OVERNIGHT MAINTENANCE IN LAX, TECHNICIAN NOTICED THE NR 1 TIRE AND WHEEL ASSY APPEARED TO BE CANTED SLIGHTLY. MAINTENANCE REMOVED THE WHEEL ASSY FOR FURTHER INSPECTION AND FOUND THE INNER WHEEL HUB HAD CRACK ED AND FRACTURED AROUND THE WHEEL BEARING AREA. THE BRAKE WAS ALSO REMOVED AND AXLE INSPECTED. NO DEFECTS WERE FOUND ON THE AXLE. THE BRAKE WAS REPLACED DUE TO METALLIC PARTICLES FROM THE WHEEL WERE FOUND IN THE BRAKE ASSY. THE WHEEL ASSY W AS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2001100500088 20011005 00088 NM 2001 10 5 AWXA200100492 1 20010909 A 5330 6573746 SKIN BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 22651 YVR - C19 CK - L2 DOOR CUTOUT, LOWER FWD CORNER, FUSELAGE SKIN CRACKED IN 3 PLACES (1 INCH). MAINTENANCE ROUTED OUT THE CRACK IN THE FUSELAGE SKIN, DOUBLER AND BEARSTRAP. FABRICATED AND INSTALLED REPAIR IAW B737 SRM 53-30-3, FIG 24, PG 83. 2 L 7 2 4F RT A16WE 2001100500089 20011005 00089 NM 2001 10 5 AWXA200100493 1 20010904 A 5312 65163000 BULKHEAD BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 22651 YVR - C19 CK - BS 178 PRESS. BULKHEAD FWD FACE, .050 CRACK EMANATING FROM FASTENER HOLE, WL 234, RBL 5.7. MAINTENANCE R EPAIRED IAW B737 SRM 53-10-11, FIG 1, DETAIL II, PG 5. 2 L 7 2 4F RT A16WE 2001100500090 20011005 00090 NM 2001 10 5 AWXA200100496 1 20010907 A 5315 65468101 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 22651 YVR - C19 CK - FLOORBEAM AT BS 967 HAS CORROSION BETWEEN BL 0 AND RBL 30 ON TOP SURFACE. AFTER CORROSION REMOVAL, MATERI AL LOSS BEYOND SRM LIMITS. MAINTENANCE REMOVED DAMAGED SECTION OF FLOORBEAM TOP CAP AND REPLACED IAW B737 SRM 53-10-9, F IG 2, PG 7. 2 L 7 2 4F RT A16WE 2001100500091 20011005 00091 NM 2001 10 5 AWXA200100497 1 20010907 A 5315 65468111 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 22651 YVR - C19 CK - FLOORBEAM AT BS 987 TOP SURFACE HAS CORROSION BETWEEN LBL 30 AND RBL 12. MAINTENANCE REMOVED PREVIOUS BEA M CAP REPAIR, FABRICATED NEW BEAM CAP AND INSTALLED IAW B737 SRM 53-10-9, FIG 2, PG 7. 2 L 7 2 4F RT A16WE 2001100500092 20011005 00092 EU 2001 10 5 MALA010730 1 20010919 A 2710 7227151522 CONTROL CABLE SAAB SF340 SF340A 7850100 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 110XJ 340A110 DURING 4K-CHECK IN CWA, RT O/B FWD AILERON WING CABLE IS CHAFED. MAINTENANCE REPLACED RT O/B FWD AILERON CABLE ASSEMBLY PN 7227151-522 IAW SAAB AMM 27-11-00-2. 2 L 7 2 4T RT A52EU 2001100500093 20011005 00093 EU 2001 10 5 MALA010731 1 20010921 A 2710 7227151522 CONTROL CABLE SAAB SF340 SF340A 7850100 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 110XJ 340A110 DURING 4K-CHECK IN CWA, LT O/B AILERON FWD WING CABLE IS CHAFFED. MAINTENANCE REMOVED AND REPLACED FWD LT O/B WING CABL E PN 7227151-522 IAW SAAB 340 AMM 27-11-25. 2 L 7 2 4T RT A52EU 2001100500094 20011005 00094 EU 2001 10 5 MALA010732 1 20010921 A 2720 7227105582 CONTROL CABLE SAAB SF340 SF340A 7850100 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 110XJ 340A110 DURING 4K-CHECK IN CWA, FWD RT FUSELAGE RUDDER CIRCUIT AFT SINGLE CABLE IS CHAFFED. MAINTENANCE INSTALLED SERVICEABLE RT SINGLE AFT RUDDER CABLE PN 7227105-582 IAW SF340 AMM 27-21-25. 2 L 7 2 4T RT A52EU 2001100500095 20011005 00095 EU 2001 10 5 MALA010733 1 20010921 A 2720 7227105562 CONTROL CABLE SAAB SF340 SF340A 7850100 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 110XJ 340A110 DURING 4K-CHECK IN CWA, RT O/B RUDDER SYSTEM CABLE OF DUAL CIRCUIT IS CHAFFED. MAINTENANCE INSTALLED SERVICEABLE RT O/B DUAL CIRCUIT CABLE PN 7227105-562 IAW SF340 AMM 27-21-25. 2 L 7 2 4T RT A52EU 2001100500096 20011005 00096 EU 2001 10 5 MALA010734 1 20010922 A 2720 7227105571 CONTROL CABLE SAAB SF340 SF340A 7850100 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 110XJ 340A110 DURING 4K-CHECK IN CWA, FOUND LT I/B FWD FUSELAGE RUDDER CIRCUIT 1 CABLE CHAFFED. MAINTENANCE REMOVED AND REPLACED LT I /B FWD FUSELAGE RUDDER PN 7227105-571 CIRCUIT 1 CABLE IAW SF3 AMM 27-21-25. 2 L 7 2 4T RT A52EU 2001100500097 20011005 00097 EU 2001 10 5 MALA010735 1 20010923 A 2730 7227705644 CONTROL CABLE SAAB SF340 SF340A 7850100 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 110XJ 340A110 DURING 4K-CHECK IN CWA, LT I/B ELEVATOR FWD FUSELAGE CABLE IS CHAFFED. MAINTENANCE REMOVED AND REPLACED LT I/B FWD FUSE LAGE ELEVATOR CABLE PN7227705-644 IAW SF3 AMM 27-31-15. 2 L 7 2 4T RT A52EU 2001100600001 20011006 00001 EU 2001 10 6 C2XA01IA367 1 20011004 A 3397 212 WIRE AEROSP ATR42 ATR42320 8680930 EU CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14822 163 IAH- DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR DID NOT ILLUMINATE. IAH- MAINT ENANCE REPAIRED A BROKEN WIRE, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM,NO DEFECTS NOTED,AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001100800001 20011008 00001 EU 2001 10 8 QXEA0101610 1 20011007 A 3350 6008905 POWER SUPPLY FOKKER F28 F28MK4000 4990810 EU INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 7684 3607 11167 PDX - EMERGENCY EVACUATION LIGHTS BY ROWS 13 AND 14 ARE WEAK AND INTERMITTENT. REMOVED AND REPLACED AFT EMERGENCY BATTER Y POWER SUPPLY, OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001100800002 20011008 00002 NM 2001 10 8 01FDEA00870 1 20011007 A 5400 FAIRING DOUG MD11 MD11 3023602 NM AFT LOWER MISSING A FDEA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 SO 25 590FE 48505 01-329 #3 ENG INBD WING PYLON AFT LOWER FAIRING MISSING. ** S/D ** COMING 2 L 7 3 4F RT A22WE 2001100800003 20011008 00003 EA 2001 10 8 COMA0160778 1 20011004 A 2740 70623 ACTUATOR CNDAIR CL600 CL6002B19 EA EMPENAGE FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 969CA 9381 7141 FLIGHT #5871. DURING TAXI OUT RECEIVED A STABILIZER CHANNEL #1 INOPERATIVE MESSAGE, AIRCRAFT RETURNED TO THE GATE.REPLA CED THE HORIZONTAL STABILIZER TRIM ACTUATOR. 2 L 7 2 4F RT A21EA 2001100800004 20011008 00004 EA 2001 10 8 COMA0160779 1 20011004 A 2740 83963 MOTOR CNDAIR CL600 CL6002B19 EA EMPENAGE FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 969CA 643 7141 FLIGHT #5871. DURING TAXI OUT RECEIVED A STABILIZER CHANNEL #1 INOPERATIVE MESSAGE, AIRCRAFT RETURNED TO THE GATE.REPLA CED THE HORIZONTAL STABILIZER MOTOR CONTROL UNIT. 2 L 7 2 4F RT A21EA 2001100800005 20011008 00005 EA 2001 10 8 COMA0160780 1 20011005 A 7810 NAS6303U4 BOLT CNDAIR CL600 CL6002B19 EA RIGHT ENGINE MISSING A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 940CA 7048 DURING REMOVAL OF EXHAUST FAIRING THREE EXHAUST NOZZLE BOLTS WERE FOUND MISSING.INSTALLED NEW HARDWARE. 2 L 7 2 4F RT A21EA 2001100800006 20011008 00006 EA 2001 10 8 COMA0160781 1 20011005 A 7810 NAS6303U9 BOLT CNDAIR CL600 CL6002B19 EA RIGHT ENGINE MISSING A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 940CA 7048 DURING REMOVAL OF EXHAUST FAIRING ONE EXHAUST NOZZLE BOLT WAS FOUND MISSING.INSTALLED NEW HARDWARD. 2 L 7 2 4F RT A21EA 2001100800008 20011008 00008 EA 2001 10 8 COMA0160782 1 20011004 A 3350 20131A BATTERY CNDAIR CL600 CL6002B19 EA CABIN WEAK A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 979CA 8945 7159 FLIGHT #5423. PRIOR TO DEPARTURE FROM CVG DISCOVERED THE EMERGENCY LIGHTING INOPERATIVE.REPLACED DRAINED BATTERY FOR THE EMERGENCY LIGHTING. 2 L 7 2 4F RT A21EA 2001100800009 20011008 00009 EA 2001 10 8 COMA0160783 1 20011004 A 3350 20131A BATTERY CNDAIR CL600 CL6002B19 EA CABIN WEAK A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 979CA 8021 7159 FLIGHT #5423. PRIOR TO DEPARTURE FROM CVG DISCOVERED THE EMERGENCY LIGHTING INOPERATIVE.REPLACED DRAINED BATTERY FOR TH E EMERGENCY LIGHTING. 2 L 7 2 4F RT A21EA 2001100800010 20011008 00010 EA 2001 10 8 COMA0160784 1 20011004 A 3350 20131A BATTERY CNDAIR CL600 CL6002B19 EA CABIN WEAK A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 979CA 7063 7159 FLIGHT #5423. PRIOR TO DEPARTURE FROM CVG DISCOVERED THE EMERGENCY LIGHTING INOPERATIVE.REPLACED DRAINED BATTERY FOR TH E EMERGENCY LIGHTING. 2 L 7 2 4F RT A21EA 2001100800011 20011008 00011 EA 2001 10 8 COMA0160785 1 20011004 A 3350 20131A BATTERY CNDAIR CL600 CL6002B19 EA CABIN WEAK A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 979CA 9694 7159 FLIGHT #5423. PRIOR TO DEPARTURE FROM CVG DISCOVERED THE EMERGENCY LIGHTING INOPERATIVE.REPLACED DRAINED BATTERY FOR TH E EMERGENCY LIGHTING. 2 L 7 2 4F RT A21EA 2001100800012 20011008 00012 SW 2001 10 8 PNSA010903 1 20010919 A 2432 RG390E BATTERY SWRNGN SA227 SA227AC 8780603 SW WEAK A PNSA K NONE O OTHER TX TAXI/GRND HDL 1 AL 03 2708D 1819 AC709B Aircraft would not start on batteries at SNP. ANC maintenance flew to line station and replaced batteries. 2 L 7 2 4T RT A8SW 2001100800013 20011008 00013 EU 2001 10 8 RAIA00109016 1 20010901 A 2150 1250104 MOTOR JETAIR JETSTM JETSTM4101 1500501 EU BINDING A RAIA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CE 03 565HK 2305 41082 7099-SPI-SMOKE COMING FROM VENT AT VAPOR CYCLE COOLING SYSTEM BAY. MAINTENANCE REMOVED AND REPLACED FREON COOLING SYSTEM MOTOR. 2 L 7 2 4T RT A41NM 2001100800014 20011008 00014 SW 2001 10 8 PNSA010927 1 20010927 A 2931 SS10127 PRESSURE SWITCH SWRNGN SA227 SA227AC 8780603 SW BLOCKED A PNSA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 AL 03 2719H 199 AC713B During cruise RH low hydraulic warning light came on with normal pressure indication. Maintenance found hydraulic pressu re switch bad for indicator light. 2 L 7 2 4T RT A8SW 2001100800015 20011008 00015 NM 2001 10 8 PCAA0110117 1 20011008 A 5610 17180003 WINDSHIELD DHAV DHC8 DHC8102 2809003 NM LEFT CRACKED A PCAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 13 809EX 4284 302 BOS-ABE FLIGHT#3898. WHILE ENROUTE TO ABE @ 14,000 FT CAPTAIN SIDE WINDOW CRACKED. FLIGHT DIVERTED TO BGM AND LANDED WIT HOUT INCIDENT. MAINTENANCE REPLACED CAPTAINS SIDE WINDOW IN ACCORDANCE WITH DASH 8 MAINTENANCE MANUAL 56-10-16. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001100800016 20011008 00016 SO 2001 10 8 C2XAA01TY130 1 20011007 A 5330 DMN15042 ANTENNA EMB 145 EMB145LR SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS Durind a scheduled inspection the lower TCAS antenna mating surface to fuselage was corroded. Maintenance removed a ntenna, cleaned corrosion I.A.W.-EMB-135/145-CPM-51-14-00 and reinstalled antenna I.A.W.-EMB-145-AMM-34-43-03. Repairs w ere satisfactory and aircraft will be released upon completion of inspection. 2 L 7 2 4T RT T00011AT 2001100800017 20011008 00017 SO 2001 10 8 C2XAA01TY131 1 20011007 A 5330 14526436401 SUPPORT EMB 145 EMB145LR SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS Durind a scheduled inspection the lavatory sink drain line support at stringer 19L was found corroded around rivits . Maintenance removed and replaced the support. I.A.W.-EMB-145-SRM-51-40-02. Repairs were satisfactory and aircraft will be released upon completion of inspection. 2 L 7 2 4T RT T00011AT 2001100800018 20011008 00018 SO 2001 10 8 C2XAA01TY132 1 20011007 A 5315 14521700007 BEAM EMB 145 EMB145LR SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS Durind a scheduled inspection corrosion was found under and around the forward carbon fiber omega beam. Maintenance removed and replaced the top cap, ramp angle, L-profile angle, cross fiber beam and installed shim, filler, plate and e xternal angle. I.A.W.-EMB-135/145-SRM-51-40-02, 53-21-02 and CMP-52-21-04 & 05. Repairs were satisfactory and aircraft w ill be released upon completion of inspection. 2 L 7 2 4T RT T00011AT 2001100900001 20011009 00001 SO 2001 10 9 C2XAA01TY133 1 20011007 A 3230 14571028001 SPRING EMB 145 EMB145LR SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS Durind a scheduled inspection the left and right springs for the MLG uplock box was found corroded. Maintenance rem oved and replaced the left and right springs. I.A.W.-EMB-145-MM-32-33-10. Repairs were satisfactory and aircraft will be released upon completion of inspection. 2 L 7 2 4T RT T00011AT 2001100900002 20011009 00002 SO 2001 10 9 C2XAA01TY134 1 20011007 A 5320 14521721007 PLATE EMB 145 EMB145LR SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS Durind a scheduled inspection, several areas of corrosion was found on the forward and aft. floor beam digital plat es.. Maintenance removed and replaced the aft floor digital plate, and removed and replaced corroded rivits in the forwa rd digital plate I.A.W.-EMB-145-SRM-51-40-02. Repairs were satisfactory and aircraft will be released upon completion of inspection. 2 L 7 2 4T RT T00011AT 2001100900003 20011009 00003 SO 2001 10 9 C2XAA01TY135 1 20011007 A 3210 14525545401 CABLE EMB 145 EMB145LR 3260212 SO MLG WW CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS DURING A SCHEDULED INSPECTION, THE EMERGENCY EXTENTION CONTROL CABLE IN THE RIGHT WHEEL-WELL WAS FOUND BENT AT THE TURNBUCKEL. MAINTENANCE REMOVED AND REPLACED THE FREE FALL CABLES IN RIGHT WHEEL-WELL. I.A.W.-EMB-145-AMM-32-34-03. REPA IRS WERE SATISFACTORY AND AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2001100900004 20011009 00004 SO 2001 10 9 C2XAA01TY136 1 20011007 A 5753 14568004005 TRACK EMB 145 EMB145LR SO GROOVED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS Durind a scheduled inspection, the right inbd. flap, inbd. track was found to have grooves worn into track. Mainten ance blended grooved areas I.A.W.-EMB-145-GST-3350/01. Repairs were satisfactory and aircraft will be released upon comp letion of inspection. 2 L 7 2 4T RT T00011AT 2001100900005 20011009 00005 SO 2001 10 9 C2XAA01TY137 1 20011007 A 5753 14568003003 TRACK EMB 145 EMB145LR SO GROOVED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS Durind a scheduled inspection, the right inbd. flap, outbd. track was found to have grooves worn into track. Mainte nance blended grooved areas I.A.W.-EMB-145-GST-3350/01. Repairs were satisfactory and aircraft will be released upon com pletion of inspection. 2 L 7 2 4T RT T00011AT 2001101000084 20011010 00084 SO 2001 10 10 C2XA01TY137 1 20011007 A 5753 14568003003 FLAP TRACK EMB 145 EMB145LR SO T/E FLAP GROOVED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS DURING A SCHEDULED INSPECTION, THE RIGHT INBD FLAP, OUTBD TRACK WAS FOUND TO HAVE GROOVES WORN INTO TRACK. MAINTENA NCE BLENDED GROOVED AREAS IAW EMB 145 GST 3350/01. REPAIRS WERE SATISFACTORY AND AIRCRAFT WILL BE RELEASED UPON COMPLETI ON OF INSPECTION. 2 L 7 2 4T RT T00011AT 2001101000083 20011010 00083 SO 2001 10 10 C2XA01TY136 1 20011007 A 5753 14568004005 FLAP TRACK EMB 145 EMB145LR SO T/E FLAP GROOVED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS DURING A SCHEDULED INSPECTION, THE RIGHT INBD FLAP, INBD TRACK WAS FOUND TO HAVE GROOVES WORN INTO TRACK. MAINTENAN CE BLENDED GROOVED AREAS IAW EMB 145 GST 3350/01. REPAIRS WERE SATISFACTORY AND AIRCRAFT WILL BE RELEASED UPON COMPLETIO N OF INSPECTION. 2 L 7 2 4T RT T00011AT 2001100900006 20011009 00006 SO 2001 10 9 C2XA01TY134 1 20011007 A 5320 14521721007 PLATE EMB 145 EMB145LR SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS Durind a scheduled inspection, several areas of corrosion was found on the forward and aft. floor beam digital plat es.. Maintenance removed and replaced the aft floor digital plate, and removed and replaced corroded rivits in the forwa rd digital plate I.A.W.-EMB-145-SRM-51-40-02. Repairs were satisfactory and aircraft will be released upon completion of inspection. 2 L 7 2 4T RT T00011AT 2001100900007 20011009 00007 SO 2001 10 9 C2XA01TY133 1 20011007 A 3230 14571028001 SPRING EMB 145 EMB145LR SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS Durind a scheduled inspection the left and right springs for the MLG uplock box was found corroded. Maintenance rem oved and replaced the left and right springs. I.A.W.-EMB-145-MM-32-33-10. Repairs were satisfactory and aircraft will be released upon completion of inspection. 2 L 7 2 4T RT T00011AT 2001100900008 20011009 00008 SO 2001 10 9 C2XA01TY132 1 20011007 A 5315 14521700007 BEAM EMB 145 EMB145LR SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS Durind a scheduled inspection corrosion was found under and around the forward carbon fiber omega beam. Maintenance removed and replaced the top cap, ramp angle, L-profile angle, cross fiber beam and installed shim, filler, plate and e xternal angle. I.A.W.-EMB-135/145-SRM-51-40-02, 53-21-02 and CMP-52-21-04 & 05. Repairs were satisfactory and aircraft w ill be released upon completion of inspection. 2 L 7 2 4T RT T00011AT 2001100900009 20011009 00009 SO 2001 10 9 C2XA01TY131 1 20011007 A 5330 14526436401 SUPPORT EMB 145 EMB145LR SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS Durind a scheduled inspection the lavatory sink drain line support at stringer 19L was found corroded around rivits . Maintenance removed and replaced the support. I.A.W.-EMB-145-SRM-51-40-02. Repairs were satisfactory and aircraft will be released upon completion of inspection. 2 L 7 2 4T RT T00011AT 2001100900010 20011009 00010 SO 2001 10 9 C2XA01TY130 1 20011007 A 5330 DMN15042 ANTENNA EMB 145 EMB145LR SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS Durind a scheduled inspection the lower TCAS antenna mating surface to fuselage was corroded. Maintenance removed a ntenna, cleaned corrosion I.A.W.-EMB-135/145-CPM-51-14-00 and reinstalled antenna I.A.W.-EMB-145-AMM-34-43-03. Repairs w ere satisfactory and aircraft will be released upon completion of inspection. 2 L 7 2 4T RT T00011AT 2001100900011 20011009 00011 SO 2001 10 9 C2XA01TY138 1 20011007 A 5753 14568254003 TRACK EMB 145 EMB145LR SO GROOVED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS During a scheduled inspection, the right outbd. flap, inbd. track was found to have grooves worn into track. Mainte nance blended grooved areas I.A.W.-EMB-145-GST-3350/01. Repairs were satisfactory and aircraft will be released upon com pletion of inspection. 2 L 7 2 4T RT T00011AT 2001100900012 20011009 00012 SO 2001 10 9 C2XA01TY139 1 20011007 A 5753 14566415004 TRACK EMB 145 EMB145LR SO GROOVED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS During a scheduled inspection, the right outbd. flap, outbd. track was found to have grooves worn into track. Maint enance blended grooved areas I.A.W.-EMB-145-GST-3350/01. Repairs were satisfactory and aircraft will be released upon co mpletion of inspection. 2 L 7 2 4T RT T00011AT 2001100900013 20011009 00013 SO 2001 10 9 C2XA01TY140 1 20011007 A 5753 14568003003 TRACK EMB 145 EMB145LR SO GROOVED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS During a scheduled inspection, the right inbd. flap, inbd. wing mounted track was found to have grooves worn into t rack. Maintenance blended grooved areas I.A.W.-EMB-145-GST-3350/01. Repairs were satisfactory and aircraft will be relea sed upon completion of inspection. 2 L 7 2 4T RT T00011AT 2001100900014 20011009 00014 SO 2001 10 9 C2XA01TY141 1 20011007 A 5753 14568253003 TRACK EMB 145 EMB145LR SO GROOVED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS During a scheduled inspection, the right outbd. flap, outbd. wing mounted track was found to have grooves worn into track. Maintenance blended grooved areas I.A.W.-EMB-145-GST-3350/01. Repairs were satisfactory and aircraft will be rel eased upon completion of inspection. 2 L 7 2 4T RT T00011AT 2001100900015 20011009 00015 SO 2001 10 9 C2XA01TY142 1 20011007 A 5753 14568254003 TRACK EMB 145 EMB145LR SO GROOVED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS During a scheduled inspection, the right outbd. flap, inbd wing mounted track was found to have grooves worn into t rack. Maintenance blended grooved areas I.A.W.-EMB-145-GST-3350/01. Repairs were satisfactory and the aircraft will be r eleased upon complection of inspection. 2 L 7 2 4T RT T00011AT 2001100900016 20011009 00016 SO 2001 10 9 C2XA01TY143 1 20011007 A 5753 14566911003 TRACK EMB 145 EMB145LR SO GROOVED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS During a scheduled inspection, the left inbd. flap, inbd flap track was found to have grooves worn into track. Main tenance blended grooved areas I.A.W.-EMB-145-GST-3350/01. Repairs were satisfactory and the aircraft will be released up on complection of inspection. 2 L 7 2 4T RT T00011AT 2001100900017 20011009 00017 SO 2001 10 9 C2XA01TY144 1 20011007 A 5753 14566412003 TRACK EMB 145 EMB145LR SO GROOVED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS During a scheduled inspection, the left inbd. flap, outbd flap track was found to have grooves worn into track. Mai ntenance blended grooved areas I.A.W.-EMB-145-GST-3350/01. Repairs were satisfactory and the aircraft will be released u pon complection of inspection. 2 L 7 2 4T RT T00011AT 2001100900018 20011009 00018 SO 2001 10 9 C2XA01TY145 1 20011007 A 5753 14566415004 TRACK EMB 145 EMB145LR SO GROOVED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS During a scheduled inspection, the left outbd. flap, outbd flap track was found to have grooves worn into track. Ma intenance blended grooved areas I.A.W.-EMB-145-GST-3350/01. Repairs were satisfactory and the aircraft will be released upon complection of inspection. 2 L 7 2 4T RT T00011AT 2001100900019 20011009 00019 SO 2001 10 9 C2XA01TY146 1 20011007 A 5753 14566413003 TRACK EMB 145 EMB145LR SO GROOVED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS During a scheduled inspection, the left outbd. flap, inbd flap track was found to have grooves worn into track. Mai ntenance blended grooved areas I.A.W.-EMB-145-GST-3350/01. Repairs were satisfactory and the aircraft will be released u pon complection of inspection. 2 L 7 2 4T RT T00011AT 2001100900020 20011009 00020 SO 2001 10 9 C2XA01TY147 1 20011007 A 5753 14568003003 TRACK EMB 145 EMB145LR SO GROOVED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS During a scheduled inspection, the left inbd. flap, inbd wing mounted flap track was found to have grooves worn int o track. Maintenance blended grooved areas I.A.W.-EMB-145-GST-3350/01. Repairs were satisfactory and the aircraft will b e released upon complection of inspection. 2 L 7 2 4T RT T00011AT 2001100900021 20011009 00021 SO 2001 10 9 C2XA01TY148 1 20011007 A 5753 14568254003 TRACK EMB 145 EMB145LR SO GROOVED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS During a scheduled inspection, the left outbd. flap, inbd wing mounted flap track was found to have grooves worn in to track. Maintenance blended grooved areas I.A.W.-EMB-145-GST-3350/01. Repairs were satisfactory and the aircraft will be released upon complection of inspection. 2 L 7 2 4T RT T00011AT 2001100900022 20011009 00022 SO 2001 10 9 C2XA01TY149 1 20011007 A 5753 14568253003 TRACK EMB 145 EMB145LR SO GROOVED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS During a scheduled inspection, the left outbd. flap, outbd wing mounted flap track was found to have grooves worn i nto track. Maintenance blended grooved areas I.A.W.-EMB-145-GST-3350/01. Repairs were satisfactory and the aircraft will be released upon complection of inspection. 2 L 7 2 4T RT T00011AT 2001100900028 20011009 00028 2001 10 9 AWT2001F00000 4 20010926 A 2562 100HM ELT BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL CABIN MALFUNCTIONED A AWTA K NONE O OTHER IN INSP/MAINT 1 WP 25 67PJ 3966 ELT WOULD ACTIVATE ON ITS OWN, RETURNED TO MANUFACTURE. REPLACED G SWITCH, RECERTIFY AND FOUND TO BE OK. 1 G 7 1 3U 3 U H2SW E4CE 2001100900029 20011009 00029 CE 2001 10 9 GON2001F00000 1 20010905 A 3232 508202085 ACTUATOR BEECH 90 E90 1152914 CE PWA PT6 PT6A27 52043 EA NLG INTERMITTENT A GONR K NONE O OTHER IN INSP/MAINT 1 SW 01 5NM LW237 AC TOOK OFF, PILOT RETRACTED GEAR, GEAR WENT UP 1/3 WAY AND STOPPED, POPPED LANDING GEAR C/B AND RED HANDLE LIGHT ON PIL OT ATTEMPTED TO EXTEND GEAR MANUALLY. GOT 3 PUMPS OF HANDLE AND IT STOPPED. COULD NOT MOVE, PILOT THEN FLEW FOR APPROX 1.5 HOURS TO BURN OFF FUEL, PRIOR TO BELLY LANDING OF AIRCRAFT, PILOT PUT LARGE HANDLE UP AND RESET ALL C/B, GEAR THEN WENT FULL UP, THEN PUT HANDLE DOWN, GEAR WENT DOWN AND LOCK. PILOT LANDED. AFTER AC LANDED, PUT AC ON JACKS AND SWUNG GEAR. HEARD NLG ACTUATOR SCREAMING, REMOVED NLG ACTUATOR, IT FELT VERY HARD TO TURN AND RACHETY, POSSIBLE GEAR TOOTH O N 90 DEGREE GEAR MISSING. RETURNED NLG ACTUATOR TO MFG FOR WARRANTY. 1 L 7 2 3T 4 T 3A20 E4EA 2001100900030 20011009 00030 NE 2001 10 9 KBMA111940 2 20010926 A 8550 1742510 FILTER ELEMENT SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE OIL INOPERATIVE A KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 115SH 40 3141 EXTERIOR OIL FILTER BYPASS INDICATOR POPPED. INDICATOR HAS BEEN REPLACED-CALL IN TO MFG ABOUT FACET FOR TROUBLESHOOTING . INSTALLED NEW OIL FILTER. 1 G 7 1 3U 3 U H9EU E19EU 2001100900031 20011009 00031 EU 2001 10 9 KBMA111941 1 20010927 A 7712 305734363 TORQUEMETER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT INTERMITTENT A KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 313LV 518 3296 TORQUE METER INDICATOR, INTERMITTANT. INSTALLED SERVICEABLE UNIT. 1 G 7 1 3U 3 U H9EU E19EU 2001100900032 20011009 00032 2001 10 9 KBMA111943 4 20010927 A 2312 064105430 RADIO SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE VHF SYSTEM INOPERATIVE A KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 230SH 4268 2337 VHF RADIO, INOPERATIVE. REMOVED AND REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U NC H9EU E19EU 2001100900033 20011009 00033 SW 2001 10 9 KBMA88793 1 20010917 A 6510 206040339103 BEARING BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL COOLER HANGER WORN A K NONE O OTHER IN INSP/MAINT 1 WP 19 667JM 10078 3444 TAIL ROTOR OIL COOLER HANGER BEARING, WORN, ROUGH, AND EXCESSIVE PLAY. INSTALLED NEW BEARINGS. 1 G 7 1 3U 3 U H2SW E4CE 2001100900034 20011009 00034 EU 2001 10 9 KBMA88799 1 20010917 A 7921 47750 MOTOR SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1 60030 NE COOLER FAN INOPERATIVE A KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 53SH 238 2009 ENGINE OIL COOLER, FAN, INOPERATIVE. REMOVED AND REPLACED WITH SERIVCEABLE UNIT. 1 G 7 1 3U 3 U H9EU E19EU 2001100900037 20011009 00037 2001 10 9 WVBA2001048 4 20010926 A 2200 011033T COMPUTER STEC PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540* 41533 EA PITCH INOPERATIVE A WVBA O OTHER O OTHER NR NOT REPORTED 1 AL 01 59829 2243 4848 317652081 PILOT REPORTED AIRCRAFT PORPOISES 5 DEGREES UP AND DOWN IN CRUISE. AUTOPILOT PITCH COMPUTER REMOVED AND REPLACED WITH L OANER UNIT. THIS PROBLEM HAS OCCURRED IN THE PAST IT IS SUSPECTED THAT THE SERVO DRIVE SPEED IS TOO SLOW. SUGEST ADJUS TING THE SPEED AND PERHAPS MOVE THE MOUNT LOCATION CLOSER TO THE ELEVATOR BELLCRANK TO LESSEN VECHANICAL DELAY IN PITCH FROM COMPUTER TO SERVO. 1 L 7 2 3O 3 O A20SO E14EA 2001100900038 20011009 00038 NM 2001 10 9 SWAA012727 1 20011003 A 3350 207377 LENS BOEING 737 7372T4 1384492 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 EEPLS MISSING LENS AT ROW 18. INSTALLED LENS PER MM. 2 L 7 2 4F A16WE 2001100900039 20011009 00039 NM 2001 10 9 SWAA012728 1 20011003 A 3350 207377 LENS BOEING 737 7372T4 1384492 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 EEPLS MISSING LENS AT ROWS 4 & 6. INSTALLED LENSES PER MM.. 2 L 7 2 4F A16WE 2001100900040 20011009 00040 NM 2001 10 9 SWAA012729 1 20011002 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING WALK AROUND INSPECTION FOUND FUSELAGE SKIN CRACKED 2.5 INCHES LONG AT BS 470, BETWEEN STR 15L & 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001100900041 20011009 00041 NM 2001 10 9 SWAA012730 1 20011003 A 5315 6546568 WEB BOEING 737 7373H4 1384600 NM AFT CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED 1/2D CHECK AT DALFORT, FOUND WEB CORRODED AFT OF BS 1016 FLOOR BEAM, RBL 32 TO RBL 36. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001100900042 20011009 00042 NM 2001 10 9 SWAA012733 1 20011001 A 5310 6516300 WEB BOEING 737 7372K6 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA CRACKS AT BS 178, LBL 17.1 & WL 234, LBL 11 & WL 218. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001100900043 20011009 00043 SO 2001 10 9 WVBA2001049 1 20010926 A 8120 HOUSING ALIDSG PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA TURBOCHARGER LOOSE A WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 4434D 284 CBN00319 317552020 L832361A WHILE COWLING WAS OFF FOR A LINE SQUAWK THE TECHNICIAN NOTICED EXHAUST STAIN AROUND THE TURBOCHARGER WHICH UPON FURTHER INVESTIGATION REVEALED THE HOUSING TO BE LOOSE. THE SAFETY TABS ON THE BOLTS WERE ALL IN PLACE. THE UNIT WAS REMOVED F ROM SERVICE. 1 L 7 2 3O 3 O A20SO E14EA 2001100900046 20011009 00046 NM 2001 10 9 UPS01236956 1 20010927 A 3230 MECHANISM BOEING 727 7272A1 138407F NM MANUAL EXTEND OUT OF RIG A IPXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 213UP 21341 ON DEPARTUE FROM LAN AT GEAR RETRACT (GEAR HANDLE UP) RED DOOR LIGHT (FRONT) AND " LEFT GEAR DOOR" ILLUMINATED, PER CHE CKLIST RECYCLED O F GEAR (BACK DOWN) RED "LT GEAR AND RT GEAR" AND "LT GEAR DOOR AND R T GEAR DOOR ILLUMINATED. PER CHEC KLIST LEFT GEAR HANDLE DOWN REMAIND ER OF FLIGHT. FOUND LT MLG MANUAL EXTEND MECHAINISM IN THE GEAR EXTEND POSITION. R ESET AND PERFORMED GEAR SWING. 2 L 7 3 4F A3WE 2001100900047 20011009 00047 WP 2001 10 9 ABXA010516 1 20010926 A 3260 WARNING LIGHT DOUG DC9 DC931 3022065 WP COCKPIT ILLUMINATED A ABXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 946AX 47003 A LOUD NOISE WAS HEARD FROM THE NOSE LANDING GEAR AREA AFTER TAKEOFF. THE NOISE INCREASED WITH SPEED. THE CREW RECYCLED THE LANDING GEAR. PROBLEM REMAINED, AND THE NOSE GEAR RED IN TRANSIT LIGHT REMAINED ON DURING THE GEAR RECYCLE. THE AIRC RAFT RETURNED TO BUF FOR INSPECTION. AFTER LANDING, THE NOSE TAXI LIGHTS WERE FOUND TO BE INOPERATIVE. BUF MAINTENANCE I NSPECTED AND APPROVED THE AIRCRAFT FOR A FERRY FLIGHT TO ILN. ILN MAINTENANCE REPLACED THE NOSE TAXI LIGHTS. THE AIRCRAF T WAS JACKED AND THE NOSE LANDING GEAR WAS LUBRICATED AND OPERATIONALLY CHECKED IAW DC-9 MAINTENANCE MANUAL 32-30-00. NO DEFECTS WERE NOTED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001100900048 20011009 00048 NM 2001 10 9 UPS01236969 1 20010930 A 3350 LIGHT BOEING 727 727247 138408F NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 211UP 21700 EMERGENCY EXIT LIGHTS ABOVE ENTRY DOOR INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY AS PER MM 35-50-1 01. OPS CHECKS GOOD. 2 L 7 3 4F A3WE 2001100900049 20011009 00049 WP 2001 10 9 ABXA010518 1 20010926 A 5250 AR2529B1 LOCK DOUG DC8 DC863 302198A WP COCKPIT DOOR LACK OF LUBE A ABXA K NONE O OTHER UK UNKNOWN 1 GL 23 812AX 46126 THE COCKPIT DOOR STUCK INTERMITTENTLY AND WOULD NOT OPEN. MAINTENANCE INSPECTED AND LUBRICATED THE LOCK. OPERATIONAL CHE CKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2001100900050 20011009 00050 NM 2001 10 9 UPS01436958 1 20010908 A 5310 65B169522 FITTING BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: C, RT BATH TUB FITTING FOUND 1EA BOLT HOLE CRACK AT VERT CHORD ATTACH SURFACE AT 9 O'CLOCK POSITION ( LOOKING FWD ) APPROX 3/16 INCH IN LENGTH. RT BS 1000 S38R AREA BATH STUB FITTING REPLACED AS PER SRM 51-10-01 PAGE 8 . 2 L 7 4 4F A20WE 2001100900051 20011009 00051 NM 2001 10 9 UPS01436959 1 20010908 A 5320 65B169521 FITTING BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: C, LT BATH TUB FITTING 1EA BOLT HOLE CRACK AT AFT SURFACE AT 5 O'CLOCK POSITION ( LOOKING FWD ) APPROX 0.040 INCH IN LENGTH, LT BS 1000 BATH STUB FITTING REPLACED AND ATT BOLTS REINSTALLED. MM 20-51-01 AND SRM 51-10-01 PAGE 8. 2 L 7 4 4F A20WE 2001100900052 20011009 00052 NM 2001 10 9 UPS01436960 1 20010908 A 5320 65B105178 FITTING BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: C, RT DRAG SPLICE FITTING ( UPPER AND LOWER FITTING ) FOUND BOTH FITTING 1EA FASTENER HOLE CRACK, REFE R ATTACHED SKETCH FOR DETAIL. RT BS 980 - 1000, S38R AREA UPPER DRAG SPLICE FITTING REPAIRED AS PER RS R53-43-34686 AND LOWER DRAG SPLICE FITTING REPLACED AS PER RS R53-43-34686. 2 L 7 4 4F A20WE 2001100900053 20011009 00053 WP 2001 10 9 ABXA010519 1 20010927 A 5250 AR2529B1 LOCK DOUG DC8 DC863 302198A WP COCKPIT DOOR DEFECTIVE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AX 46126 THE COCKPIT DOOR WOULD NOT OPEN. MAINTENANCE REPLACED THE DOOR LOCK IAW DC-8 MM 52-51-01. OPERATIONAL CHECKS WERE COMPLE TED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2001100900054 20011009 00054 NM 2001 10 9 UPS01436961 1 20010908 A 5320 65B105173 FITTING BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: C, LT DRAG SPLICE FITTING ( LOWER FITTING ) FOUND 1EA HOLE CRACK, LT BS 980 - 1000 S38L AREA LWR D RAG SPLICE REPAIRED AS PER RS 53-43-34686. 2 L 7 4 4F A20WE 2001100900055 20011009 00055 NM 2001 10 9 ABXA010520 1 20010927 A 2120 ODOR BOEING 767 767200 1385120 NM COCKPIT DETECTED A ABXA K NONE O OTHER CL CLIMB 1 GL 23 769AX 22787 DURING INITIAL CLIMB AND ENROUTE CLIMB, THE AIR CONDITIONING SYSTEM HAD AN OILY ODOR AND TASTE IN THE COCKPIT AND MAIN C ABIN. MAINTENANCE RAN AIR CONDITIONING PACKS AND ENGINE PNEUMATICS AT TAKEOFF POWER. NO ODORS WERE NOTED. OPERATIONAL CH ECKS WERE COMPLETED IAW B767 FRM 21, FIG 25A. 2 L 7 2 4F RT A1NM 2001100900056 20011009 00056 2001 10 9 ABXA010524 4 20010926 A 3432 INDICATOR BOEING 767 767281 1385109 NM COCKPIT MALFUNCTIONED A ABXA L ABORTED APPROACH G MULTIPLE FAILURE AP APPROACH 1 GL 23 787AX 23020 BOTH LEFT AND RIGHT GLIDE SLOPES WERE FLAGGED. MAINTENANCE PERFORMED B767 FIM 22-00-02, FIG 113. A CAT III EVALUATION AP PROACH WAS COMPLETED WITH SATISFACTORY RESULTS. 2 L 7 2 4F RT A1NM 2001100900058 20011009 00058 WP 2001 10 9 ABXA010527 1 20011004 A 2612 WARNING SYSTEM DOUG DC9 DC933F 302207A WP COCKPIT MALFUNCTIONED A ABXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 23 931AX 47384 A LOWER CARGO FIRE WARNING ILLUMINATED IN FLIGHT. MAINTENANCE RESET THE FIRE WARNING CIRCUIT BREAKER AND COMPLETED ADJUS TMENT TEST AND OPERATIONAL TEST IAW DC-9 MM 26-15-00-5-0001. INSPECTED THE AFT CARGO PIT FOR EVIDENCE OF SMOKE. NO DEFEC TS WERE NOTED. 2 L 7 2 4F A6WE 2001100900059 20011009 00059 NM 2001 10 9 ABXA010528 1 20011004 A 3350 1000679 LIGHT BOEING 767 767200 1385120 NM COCKPIT INOPERATIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 768AX 22786 EMERGENCY EXIT LIGHT IN COCKPIT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY IAW B767 MM 33-5 1-00. OPERATIONAL CHECKS WERE COMPLETED AND WERE SATISFACTORY. 2 L 7 2 4F RT A1NM 2001100900060 20011009 00060 NM 2001 10 9 UPS01436962 1 20010908 A 5320 FITTING BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: C, RT BS 1000 BULKHEAD VERTICAL LOWER CHORD ( BATH TUB FITTING ATTACH AREA ) FOUND 1EA BOLT HOLE CRACK AT 5 O'CLOCK POSITION APPROX 0.060 INCH IN LENGTH. RT BS 1000 B/H VERTICAL LWR CHORD BATH STUB FITTING ATTACH AREA 5 O'CLOCK POSITION CRACKED BOTH HOLE REWORK AS PER RS 53-43-34686. 2 L 7 4 4F A20WE 2001100900061 20011009 00061 NM 2001 10 9 UPS01436963 1 20010912 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: C, FWD CARGO COMPT STA 980 RT STR 47R CORROSION FOUND AS MARKED. FWD CARGO BS 950 - 980 STR 47R ST RINGER REPAIR PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2001100900062 20011009 00062 EU 2001 10 9 AWXA200100518 1 20010927 A 5347 D531103962001 SEAT TRACK AIRBUS 320 A320232 3930326 EU CABIN CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 YWG - C6 CK - "C" - CORROSION FOUND ON #3 SEAT TRACK AT FR 20R, Y765. AFTER CORROSION REMOVAL, FOUND TO BE BEYOND SRM LI MITS. MAINTENANCE REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED REPAIR SECTION AND SPLICEDS AND INSTALLED IAW SRM 53 -00-15, FIG 201, PG 202 - 206 2 L 7 2 4F RT A28NM 2001100900063 20011009 00063 EU 2001 10 9 AWXA200100519 1 20010927 A 5347 D5311278220000 SEAT TRACK AIRBUS 320 A320232 3930326 EU CABIN CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 YWG - C6 CK - "C" - CORROSION FOUND ON #4 SEAT TRACK AT FR 20R, Y-1292. AFTER CORROSION REMOVAL FOUND TO BE BEYOND SRM L IMITS. MAINTENANCE REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED REPAIR SECTION AND SPLICES AND INSTALLED IAW A320 S RM 53-11-15, FIG 203, PG 217 - 218. 2 L 7 2 4F RT A28NM 2001100900064 20011009 00064 EU 2001 10 9 AWXA200100479 1 20010930 A 2130 VFT210A1 VALVE AIRBUS 320 A320231 3930325 EU CABIN PRESSURE FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 633AW 9571 7 82 PHX - AIR TURNBACK - FLT 77 - ON CLIMBOUT THE CREW GOT AN ECAM MESSAGE FOR INLET SKIN FAULT AND WERE UNABLE TO PRESSURIZ E THE AIRCRAFT. THE AIRCRAFT RETURNED TO PHX MAKING AN UNEVENTFUL LANDING. MAINTENANCE FOUND THE AVI VENT CONT C/B POPPE D. THEY RESET THE C/B WHICH POPPED AGAIN DURING SYSTEM TEST. THEY TROUBLESHOT PER TSM 21-26-00-810-829 AND REPLACED THE SKIN INLET AIR VALVE 15 HQ AND THE AVEC COMPUTER. AFTERWARDS FUNCTIONAL AND PRESSURIZATION CHECKS WERE GOOD.AVEC COMPUTE R, MFG SEXTANT, P/N:87292325V04 S/N 143 TT 34630 TC 16275 TSR 1922. 2 L 7 2 4F RT A28NM 2001100900065 20011009 00065 NM 2001 10 9 AWXA200100494 1 20010913 A 5315 654541027 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 22651 YVR - C19 CK - RT OVERWING PRESSURE DECK LOWER VERT CHORD AT BS 698, RBL 24.82 CRACKED .5 INCH. MAINTENANCE TRIMMED OUT DAMAGED AREA, FABRICATED REPAIR ANGLE AND INSTALLED IAW AWA ER 15-5702-01271-SS2. 2 L 7 2 4F RT A16WE 2001100900066 20011009 00066 NM 2001 10 9 AWXA200100495 1 20010913 A 5315 6545410555 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 22651 YVR - C19 CK -RT OVERWING SEAT TRACK AILERON CUTOUT STRUCTURE AT RT I/B SEAT TRACK BS 658 VERT FLANGE CRACKED .3125 INCH . VISIBLE THROUGH CUTOUT UNDER STRUCTURE OF CLOSED FLOOR PANEL. MAINTENANCE STOP DRILLED CRACK AND INSTALLED REPAIR IAW AWA ER 15-5710-01269-JS1, REFERENCING BOEING S/B 737-57-1139, REV 4, FIG 6. 2 L 7 2 4F RT A16WE 2001100900067 20011009 00067 NM 2001 10 9 AWXA200100498 1 20010927 A 5315 6545410555 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 22651 YVR - C19 CK -LONGITUDINAL SEAT TRACK SUPPORT BEAM, LBL 24.5 CRACKED AT BOLT RELIEF HOLE, BS 679. MAINTENANCE MADE REPA IRS IAW AWA ER 15-5710-01269-JS1, REFERENCING BOEING S/B 737-57-1139, REV 4, FIG6. 2 L 7 2 4F RT A16WE 2001100900068 20011009 00068 NM 2001 10 9 SWAA012746 1 20011005 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY LIGHT LENS CRACKED. R&R LENS PER MM. 2 L 7 2 4F RT A16WE 2001100900069 20011009 00069 2001 10 9 SWAA012749 4 20011005 A 2565 D31354 SLIDE BOEING 737 737317 138447P NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001100900070 20011009 00070 2001 10 9 SWAA012750 4 20011005 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR DRAGGING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 611SW 27697 FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. R&R SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001100900071 20011009 00071 NM 2001 10 9 SWAA012752 1 20011005 A 5250 65C33828 PANEL BOEING 737 7373Y0 1384671 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 308SA 23498 COCKPIT DOOR UPPER BREAKAWAY PANEL NOT SECURED. SECURED PANEL PER MM. 2 L 7 2 4F RT A16WE 2001100900072 20011009 00072 NM 2001 10 9 SWAA012753 1 20011005 A 5250 65C33828 PANEL BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 COCKPIT DOOR UPPER BREAKAWAY PANEL NOT SECURED. R&R BREAKAWAY PINS PER MM. 2 L 7 2 4F A16WE 2001100900073 20011009 00073 NM 2001 10 9 SWAA012754 1 20011004 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED .562 INCH AT AFT SVC DOOR LOWER HINGE CUT OUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001100900074 20011009 00074 NM 2001 10 9 SWAA012755 1 20011005 A 5310 6545409 WEB BOEING 737 7373H4 1384600 NM LH W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESS WEB CRACKED AT BS 663, LBL 32. REPAIRED WEB PER SWA TI-353-046. 2 L 7 2 4F RT A16WE 2001100900075 20011009 00075 NM 2001 10 9 SWAA012756 1 20011007 A 5320 BAC1503 STIFFENER BOEING 737 7373H4 1384600 NM RH W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL STIFFENER CRACKED .25 INCH AT BS 663, RBL 6.0. REPAIRED STIFFENER PER SWA RA 1-357-2673. 2 L 7 2 4F RT A16WE 2001100900076 20011009 00076 NM 2001 10 9 SWAA012757 1 20011006 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING WALKAROUND INSPECTION FOUND FUSELAGE SKIN CRACKED AT BS 940, STR 20R. REPAIRED SK IN PER SRM. 2 L 7 2 4F A16WE 2001100900077 20011009 00077 NM 2001 10 9 SWAA012758 1 20011006 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM LH FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727, WL 180. REPAIRED SK IN PER SRM. 2 L 7 2 4F A16WE 2001100900078 20011009 00078 NM 2001 10 9 SWAA012759 1 20011006 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 830, STR 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001100900079 20011009 00079 NM 2001 10 9 SWAA012760 1 20011007 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FWD CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CORRODED AT BS 500D, STR 28L. REPAIRED STR PER S RM. 2 L 7 2 4F RT A16WE 2001100900080 20011009 00080 NE 2001 10 9 SWAA012762 2 20011006 A 7261 3505716 STARTER BOEING 737 7373A4 1384585 NM CFM56 CFM56* 13802 NE # 1 ENGINE LEAKING A SWAA B EMER. DESCENT J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SW 07 669SW 23752 726161 ( ENGINE SHUTDOWN, DECLARED EMERGENCY )………………………SHUTDOWN # 1 ENGINE INFLIGHT DUE TO OIL PRESSURE LIGHT. OIL QUANITY ZE RO, NORMAL TEMP, VIBRATION & EGT. R&R STARTER & STARTER GARLOCK OUTER SEAL. PERFORMED FULL POWE R RUN, & LEAK CHECK PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2001100900081 20011009 00081 NM 2001 10 9 AWXA200100507 1 20010904 A 5522 65C25753 SKIN BOEING 737 7373G7 1384595 NM ELEVATOR DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 MCN - C17 CK -1 SQUARE INCH DISBOND AREA ON LT ELEV UPPER SURFACE, ELEV STA 91, 18 INCHES AFT OF LEADING EDGE. MAINTENA NCE REPAIRED ELEV DISBOND IAW B737 SRM 51-70-17, FIG 1, PG 3 - 45. CALCULATED ELEV BALANCE MOMENT IAW B737 SRM 51-60-04 PG 15 & 16. 2 L 7 2 4F RT A16WE 2001100900082 20011009 00082 NM 2001 10 9 SWAA012738 1 20011003 A 3350 07912 COVER BOEING 737 7375H4 138449D NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 503SW 24180 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER CRACKED AT ROW 1. R&R COVER PER MM. 2 L 7 2 4F RT A16WE 2001100900083 20011009 00083 NM 2001 10 9 SWAA012740 1 20011002 A 5310 65C27314 TIE CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED 1/2D CHECK AT DALFORT, FOUND STRINGER TIE CLIP CRACKED AT BS 663, STR 10L R&R TIE CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001100900084 20011009 00084 NM 2001 10 9 SWAA012741 1 20011004 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 270, BETWEEN STR 9L & 10L. R EPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001100900085 20011009 00085 NM 2001 10 9 SWAA012742 1 20011003 A 5753 6546435 FLAP BOEING 737 7373H4 1384600 NM LH WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 316SW 23338 DURING SCHEDULED C4 CHECK, FOUND LH OTBD AFT T/E FLAP DELAMINATED AT INBD END. R&R FLAP PER MM. 2 L 7 2 4F RT A16WE 2001100900086 20011009 00086 NM 2001 10 9 SWAA012744 1 20011003 A 5310 6516300 WEB BOEING 737 7373T5 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED SPECIAL VISIT, FOUND WEB CRACKED ( 3 EA )AT BS 178, BETWEEN LBL 1.0 & LBL 12.0, BETWEEN WL 187 & WL 218 . REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001100900087 20011009 00087 NM 2001 10 9 AWXA200100509 1 20010911 A 5347 654541027 SEAT TRACK BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 MCN - C17 CK -1 INCH CRACK ON SEAT TRACK VERTICAL FLANGE, BS 663, RBL 24, BELOW FLOOR PANELS.MAINTENANCE PERFORMED SEAT TRACK REPAIR IAW AWA ER 03-5700-01270-JS1. 2 L 7 2 4F RT A16WE 2001100900088 20011009 00088 EU 2001 10 9 AWXA200100513 1 20010925 A 5347 D53112091203 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 635AW 092 YWG - C1 CK -NR 3 SEAT TRACK AT FR 20R, Y-765, CORRODED. BEYOND SRM LIMITS AFTER CORROSION REMOVAL. MAINTENANCE REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED REPAIR SECTION AND SPLICES AND INSTALLED REPAIR IAW SRM 53-00-15, FIG 201. 2 L 7 2 4F RT A28NM 2001100900089 20011009 00089 EU 2001 10 9 AWXA200100514 1 20010925 A 5347 D53112092206 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 635AW 092 YWG - C1 CK -NR 4 SEAT TRACK CORRODED AT FR 20R, Y-1292. BEYOND LIMITS AFTER CORROSION REMOVAL. MAINTENANCE REMOVED DAM AGED SECTION OF TRACK, FABRICATED REPAIR SECTION AND SPLICES AND INSTALLED REPAIR PARTS IAW SRM 53-00-15, FIG 201. 2 L 7 2 4F RT A28NM 2001101800025 20011018 00025 NM 2001 10 18 AWXA200100515 1 20011002 A 7830 6573606149 ACCESSORY UNIT BOEING 737 73733A 1384673 NM NR 1 ENGINE WRONG PART A AWXA C ABORTED TAKEOFF W J INADEQUATE Q C WARNING INDICATION TO TAKEOFF 1 WP 28 174AW 31500 31 23633 PHX - ABORTED TAKEOFF - FLT 302 - C - ON TAKEOFF ROLL AT 110 KTS THE NR 1 THRUST REVERSER OVERHEAD LIGHT ILLUMINATED AND THE T/O WAS ABORTED. THE CREW DID USE BOTH T/R'S TO SLOW THE AIRCRAFT, FUNCTIONED NORMALLY. MAINTENANCE INSPECTED THE NR 1 T/R AND PLACED ON MEL 78-7 COND 1. MAINTENANCE REPLACED THE ENGINE ACCESSORY UNIT, FOUND P/N INSTALLED NOT COMPATI BLE WITH THIS AIRCRAFT. REMOVED 65-73606-149 AND INSTALLED P/N 65-73606-170 IAW AMM 78-34-06, PG 401 - 404, FUNCTIONAL CHECKS GOOD. 2 L 7 2 4F RT A16WE 2001100900090 20011009 00090 EU 2001 10 9 AWXA200100516 1 20011006 A 2910 NAS161212 O-RING AIRBUS 320 A320232 3930326 EU HYDRAULIC SYS FAILED A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 648AW 770 PHX - AIR TURNBACK - FLT 882 - 30 MIN INTO FLT. CREW RECEIVED CLASS 1 ECAM YELLOW HYD LOW LEVEL, WITH ASSOCIATED ECAM IN DICATION OF NO RESERVOIR FLUID IN YELLOW SYSTEM. CREW FOLLOWED ECAM PROCEDURES AND RETURNED TO PHX MAKING AN UNEVENTFUL LANDING. EMERGENCY EQUIP WAS CALLED OUT. MAINTENANCE TROUBLESHOT AND FOUND 2 O-RINGS FAILED ON THE QD AND CHECK VALVE ON THE PTU MANIFOLD ASSY. BOTH WERE REPLACED AND THE HYD SYS SERVICED AND LEAK CHECKS PERFORMED WITH NO FURTHER DISCREPANC IES NOTED. PACKING P/N NAS1612-20 2 L 7 2 4F RT A28NM 2001100900091 20011009 00091 EU 2001 10 9 AWXA200100517 1 20011006 A 3213 MS288892 VALVE AIRBUS 320 A320231 3930325 EU LT MLG STRUT LEAKING A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 645AW 238 PHX - AIR TURNBACK - FLT 27 - AFTER T/O THE LANDING GEAR WOULD NOT RETRACT. CREW RESET LGCIU 1 & 2 PER MAINTENANCE CONTR OL, NO HELP. THE AIRCRAFT APPEARED TO REMAIN IN GROUND MODE. THE AIRCRAFT RETURNED TO PHX, MAKING AN UNEVENTFUL LANDING. MAINTENANCE TROUBLESHOT AND FOUND THE PRESSURE IN THE UPPER CHAMBER OF THE LT MLG STRUT TO BE 480 PSI AND LOWER CHAMBER AT 1250 PSI. MAINTENANCE REPLACED THE UPPER SERVICING SCHRADER VALVE, SERVICED THE STRUT, LEAK CHECKED THE VALVE AND PE RFORMED GEAR SWING, ALL FUNCTIONAL CHECKS NORMAL. NO FURTHER FAULTS REPORTED. 2 L 7 2 4F RT A28NM 2001100900092 20011009 00092 NM 2001 10 9 UPS01436971 1 20010906 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: C, LT SIDE BS 800 BTN STR 16 - 17 FOUND TWO EACH FASTENER HOLES CRACKED AT STRAP RUNNING AFT FROM HOLE TO EDGE. REPAIRED FRAME STRAP AS PER RS R53-22-34680. 2 L 7 4 4F A20WE 2001100900093 20011009 00093 NM 2001 10 9 UPS01436972 1 20010906 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: C, RT SIDE BS 800, ONE EA FASTENER HOLE CRACK REVEALED AT STRAP AREA, RUNNING FWD APPROX 3/16 INCH IN L ENGTH AS MARKED PLEASE REFER DRAWING FOR DETAIL. REPAIRED FRAME STRAP AS PER RS NO. R53-22-34680. 2 L 7 4 4F A20WE 2001101500141 20011015 00141 NM 2001 10 15 UPS01636986 1 20011007 A 7930 O-RING BOEING 767 767300 1385204 NM RT ENGINE LEAKING A IPXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 309UP 27740 RT ENG OIL QTY DROPPING IN FLIGHT. CHIP DETECTOR "O" RING BAD R/R SAME. NR 2 ENG NR 6 BEARING CARBON SEAL REPLACED I AW MAINTENANCE MANUAL 72-53-03 C AOL FOR GROUND RUN. REPLACE CARBON SEAL P/N537L685003 GRN ILLEG. REPLACE STATIC SEAL P/ N 1664M10P22 GRN1541572 2 L 7 2 4F RT A1NM 2001100900094 20011009 00094 WP 2001 10 9 UPS01836725 1 20010828 A 3350 LIGHT DOUG DC8 DC871 302199A WP CABIN INOPERATIVE A IPXA O OTHER O OTHER CR CRUISE 1 SO 01 772UP 46072 EMERGENCY EXIT LIGHTS CIRCUIT BREAKER OPENED IN FLIGHT. PERFORMED EMERGENCY LIGHT BATTERY TEST PER MM REF 33-50-01 E MERGENCY LIGHTING CHECKS GOOD 2 L 7 4 4F 4A25 2001100900095 20011009 00095 NM 2001 10 9 C1AH200192008 1 20010918 A 2560 FLASHLIGHT BOEING 727 727212 138407G NM CABIN INOPERATIVE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 292AS 21458 FORWARD O/B EMERGENCY FLASHLIGHT INOPERATIVE. REINSTALLED FLASHLIGHT AND SAFETY STRAP CHARGING INDICATION NORMAL. 2 L 7 3 4F A3WE 2001100900096 20011009 00096 NM 2001 10 9 C1HA200182011 1 20010905 A 2560 BATTERY BOEING 727 7272S7 138407Z NM FLASHLIGHT DISCHARGED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 682CA 22019 AFT EMERGENCY FLASHLIGHTS WERE FOUND WITH SEAL BROKEN AND BATTERIES DRAINED. ACTION TAKEN: REMOVED AND REPLACED BATTER IES ON BOTH AFT EMERGENCY FLASH LIGHTS, INSTALLED SEAL, GROUND OPS CHECK GOOD. 2 L 7 3 4F A3WE 2001100900097 20011009 00097 WP 2001 10 9 UPS01836770 1 20010906 A 2421 NA GENERATOR DOUG DC8 DC871 302199A WP NR 2 SMOKE A IPXA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 730UP 46030 DURING TAXI OUT NR 2 BUS POWER FAIL LIGHT ILLUMINATED NR 2 GEN UNPAR'LD LIGHT ILLUMINATED AND LEFT EMERG AC BUS POWER FA IL LIGHT ILLUMINATED ATTEMPTED TO PERFORM BUS POWER FAIL LIGHT ILL CHECKLIST COCKPIT SMOKE CONTINUED, SECURED 1-4 GENS MOVED A/C TO ISOLATED AREA ACCOMP EMERGENCY EVAC PROCEDURES DUE TO SMOKE IN COCKPIT. INSPECTED RELAYS AND WIRES ON N R 2 GENERATOR SYSTEM IN FLIGHT DECK AND GALLEY AREA. RAN BOTH PACKS AND RECIRC FAN WITH NO EVIDENCE OF SMOKE NOTED. N R 2 BUS PWR FAIL LIGHT, REPLACED NR 2 GENERATOR RELAY BUT NO HELP, DEFERRED NR 2 GENERATOR SYSTEM PER MEL 24-1-1. 2 L 7 4 4F 4A25 2001100900098 20011009 00098 WP 2001 10 9 UPS01836941 1 20010910 A 5311 FRAME DOUG DC8 DC873 302199C WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 STA. 8 FRAME IS CORRODED BEYOND LIMITS BETWEEN LONG. 24R-29R REMOVED,FABRICATED AND REPLACED CHO RD I.A.W. 8110-3 APROVED DH SK 852-708 2 L 7 4 4F RT 4A25 2001100900099 20011009 00099 WP 2001 10 9 UPS01836942 1 20010914 A 5321 PRESSURE PANEL DOUG DC8 DC873 302199C WP COCKPIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE: C2, COCKPIT SUBFLOOR PRESSURE WEB IS CRACKED AT STA. -67 AT RBL. 60 REPAIRED WEB I.A.W. SRO 8520026 2 L 7 4 4F RT 4A25 2001100900100 20011009 00100 WP 2001 10 9 UPS01836943 1 20010916 A 5230 NA PAN DOUG DC8 DC873 302199C WP CARGO DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE: C2, AFT CROSS SLIDE DOOR UNDER AFT LIFT HANDLE DOOR FRAME. CUT & REMOVED SECTION OF DOOR PAN IAW R EO G08404 FAB NEW SECTION IAW RE O G08404 ALODINE & PRIME IAW DC8 SRM 51-1-8 INSTALLED IAW REO G08404 FAB REPAIR ANGLE IAW REO G08404 ALODINE & PRIMED IAW SRM 51 AND INS TALLED IAW REO G08404 2 L 7 4 4F RT 4A25 2001100900101 20011009 00101 NM 2001 10 9 C1HA200184008 1 20010906 A 2612 HANDLE BOEING 727 7272S7 138407Z NM COCKPIT DISCONNECTED A C1HA K NONE O OTHER UK UNKNOWN 1 GL 15 684CA 22491 NR 1 FIRE HANDLE FELL OFF. RE-INSTALLED NR 1 FIRE HANDLE OPS CHECK GOOD PER MM 26-10. 2 L 7 3 4F A3WE 2001100900102 20011009 00102 WP 2001 10 9 UPS01836944 1 20010908 A 5320 ATTACH ANGLE DOUG DC8 DC873 302199C WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 MAIN CABIN FLOOR PNL ATTACH ANGLE HAS CORROSION AROUND NP'S AND MISDRILLED HOLES AT STA 25 AND BW LBL 14-LBL23 IN FRONT L RADIO RACK BLEND AREA TO RMV CORROSION FOUND OUT OF LIMITS IAW 53-2-1 RMVD FLR SUPPORT IAW DC8 SRM 51-1-20D FABBED -17 & -7 ANGLES IAW DAC DWG 5645 828 & 5888479 ALODINED AND PRIMED IAW 51-1-8 INSTALLED ANGLES IAW D C 8 SRM 51-1-20D & 51-3-0 2 L 7 4 4F RT 4A25 2001100900103 20011009 00103 NM 2001 10 9 C1HA200184009 1 20010911 A 2897 WIRE BOEING 727 7272S7 138407Z NM FUEL SYSTEM BROKEN A C1HA J DUMP FUEL F FLT CONT AFFECTED LD LANDING 1 GL 15 684CA 22491 DURING FLAP ASSYM PROCEDURE, FUEL WAS PUMPED LEFT PUMP NOZZLE FAILED TO CLOSE. FOUND BROKEN WIRE REPAIRED BROKEN WIRE PE R STANDARD WIRING PRACTICES CHAPTER 28-31-01. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2001100900104 20011009 00104 WP 2001 10 9 UPS01836947 1 20010907 A 5311 FRAME DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE: C2, FRAME IS CRACKED REPAIR IAW DC8 SRM 53-2-0 FIG 2 2 L 7 4 4F RT 4A25 2001100900105 20011009 00105 WP 2001 10 9 UPS01836948 1 20010909 A 5315 FLOORBEAM DOUG DC8 DC873 302199C WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE: C2, FLOORBEAM CORRODED IN FWD UPPER FLANGE APPROX 10 INCHES FROM LT CUSP AT FS 1080. CUT OUT DAMAG ED FLOORBEAM SECTION. FABRICATED NEW SECTION & REPAIR A NGLES. REMOVED TAIL DEICE AIR LINE. INSTALLED NEW SECTION & REPA IR S PLICES IAW DC8 SRM 51-1-20D. INSTALLED TAIL ICE AIR LINE IAW MM 20-1 1-00 2 L 7 4 4F RT 4A25 2001100900106 20011009 00106 WP 2001 10 9 UPS01836949 1 20010909 A 5315 FLOORBEAM DOUG DC8 DC873 302199C WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE: C2, FLOORBEAM CORRODED IN FWD UPPER FLANGE APPROX 10 INCHES FROM LT CUSP AT FS 1080. CUT OUT DAMAG ED FLOORBEAM SECTION. FABRICATED NEW SECTION & REPAIR A NGLES. REMOVED TAIL DEICE AIR LINE. INSTALLED NEW SECTION & REPA IR S PLICES IAW DC8 SRM 51-1-20D. INSTALLED TAIL ICE AIRLINE IAW MM 20-11 -00 2 L 7 4 4F RT 4A25 2001100900107 20011009 00107 NE 2001 10 9 C1HA200185012 2 20010922 A 7260 BOLT BOEING 727 7272S7 138407Z NM PWA JT8 JT8D17R 52049 NE ENGINE GEARBOX LOOSE A C1HA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 GL 15 685CA 22492 ENGINE NR 1 LOST ALL OIL DURING LOSS OF PRESSURE PRECAUTIONARY ENGINE PROCEDURES WERE COMPLETED (AFTER 2 MIN COOL DOWN) AT 10 PSI OIL PRESSURE DROPPED TO 0 DURING WIND MILLING 17:05-18:00 OIL PRESSURE WAS AT 10 PSI AT SHUTDOWN AND DECREASE. INSPECTED ENGINE VISUALLY IAW TROUBLESHOOTING 02A OF PWA MM 72-00. FOUND SEVERAL GEARBOX CASE BOLTS LOOSE, TIGHTENED B OLTS PER PG 108B STEP 4 ACCOMPLISHED MAIN OIL SCREEN INSPECTION AND REPLACEMENT (NO ABNORMALITIES NOTED) ENG CHP DETECTO R INSPECTIONS. 2 L 7 3 4F 4 F A3WE E2EA 2001100900108 20011009 00108 2001 10 9 C1HA200193018 4 20010902 A 2565 LATCH BOEING 727 727212 138407G NM L1 SLIDE FAILED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 1L DOOR SLIDE NEEDS TO BE FIXED SO IT STAYS IN. BOX KEEPS FALLING OUT OF BOTTOM. REPLACED SLIDE LATCH ASSEMBLY. OPS CH ECKS GOOD. 2 L 7 3 4F A3WE 2001100900109 20011009 00109 2001 10 9 C1HA200193019 4 20010903 A 2565 LATCH BOEING 727 727212 138407G NM L1 SLIDE OUT OF ADJ A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 NR 1 LEFT SLIDE NOT INTACT. KEEPS FALLING OUT. ADJUSTED LATCH AND RESECURED SLIDE IN CONTAINER IN ACCORDANCE WITH 25-60 -15. 2 L 7 3 4F A3WE 2001100900110 20011009 00110 WP 2001 10 9 UPS01836950 1 20010910 A 5720 SPLICE DOUG DC8 DC873 302199C WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE: C2, REMOVE INTERCOSTAL AT LEFT WING STA 340 TO ACCESS FWD DRIVE LINK BOLT. REMOVED INTERCOSTAL & WE B IAW DC8 SRM 51-1-21. MAT ID FOR ANGLE DOUBLER DMS 1592 TITANIUM .040 PO 300420 IAW REO G08396 & SHIMS 7075-T6 .040 PO 362742 & 7075-T6 .063 PO 367060 IAW REO G08396. FABRICATED A NGLE IAW REO G08396. FAB SHIMS IAW REO G08396. TREAT & PRIM E IAW DC8 SRM 51-1-8. INSTALLED IAW SRM 51-1-21, 51-3-0 & 51-1-20D 2 L 7 4 4F RT 4A25 2001100900111 20011009 00111 NM 2001 10 9 C1HA200194016 1 20011001 A 3150 WARNING SYSTEM BOEING 727 727290 138408W NM COCKPIT MALFUNCTIONED A C1HA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 15 294AS 22146 ON TAKEOFF ROLL APPROXIMATELY 95 KTS THE MACH OVERSPEED WARNING HORN (CLACKER)CAME ON. PERFORMED LOW SPEED ABORT AND RE TURNED TO GATE. PERFORMED MACH AIRSPEED WARNING SYSTEM TEST, OPS CHECKS GOOD. 2 L 7 3 4F A3WE 2001100900112 20011009 00112 WP 2001 10 9 UPS01836951 1 20010910 A 5315 FLOORBEAM DOUG DC8 DC873 302199C WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE: C2, FLC FS 70 FLOORBEAM AT RBL 32 CORRODED FABBED REPAIR ANGLES IAW TIMCO SRM STD 5310-001 ALODINE D & PRIMED IA W DC8 SRM 51-1-8. INSTALLED REPAIR ANGLES IAW 51-1-20 INSTALLED 2 EA FLOOR PANELS IAW DC8 SRM 51-3-0 2 L 7 4 4F RT 4A25 2001100900113 20011009 00113 NM 2001 10 9 C1HA200194017 1 20011003 A 3150 WARNING SYSTEM BOEING 727 727290 138408W NM COCKPIT MALFUNCTIONED A C1HA O OTHER N FALSE WARNING CL CLIMB 1 GL 15 294AS 22146 HIGH SPEED WARNING SOUNDED AT ROTATION MOMENTARILY. IT SOUNDED AGAIN AT 600 AGL, 180 KTS. PERFORMED SYSTEM ELF TEST IAW MM 34-14-01. MACH AIRSPEED WARNING OPS CHECKS GOOD ON GROUND. 2 L 7 3 4F A3WE 2001100900114 20011009 00114 2001 10 9 C1HA200194018 4 20011004 A 3414 INDICATOR BOEING 727 727290 138408W NM COCKPIT FAULTY A C1HA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 15 294AS 22146 MACH AIRSPEED WARNING SOUNDED AT VR PULLED NR 1 CB TO SILENCE. REPLACED CAPTAINS MACH AIRSPEED INDICATOR. OPS CHECKS GO OD IAW MM 34-42-01. 2 L 7 3 4F A3WE 2001100900115 20011009 00115 WP 2001 10 9 UPS01836954 1 20010916 A 5320 STIFFENER DOUG DC8 DC873 302199C WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE: C2, LONGERON STIFFENER EXFOLIATED. REMOVED AND REPLACED STIFFENER IAW RFTS 801UP-19-21236 2 L 7 4 4F RT 4A25 2001100900116 20011009 00116 WP 2001 10 9 UPS01836957 1 20010928 A 5320 WEB DOUG DC8 DC873 302199C WP RT MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE: C2, WEB IN RT WW STA 870 ABOVE KEEL BEAM HAS CRACK IN RADIUS. REMOVED WEB AT STA 870 REMOVED HYD L INES TO GEAR ACTUATOR, FABBED AN GLE AND FILLER ALODINED & PRIMED REPAIR ANGLE AND FILLER, INSTALLED WEB REPAIR ANGLE AN D FILLER RECONNECTEDHYD LINES TO GEAR ACT PERFORMED LEAK & OPS CHECK REINSTALLED CLOSEOUT PANELS 2 L 7 4 4F RT 4A25 2001100900117 20011009 00117 NM 2001 10 9 C1HA200196014 1 20010902 A 3150 WARNING SYSTEM BOEING 727 7272J4 1384006 NM PWA JT8 JT8D17 52049 NE COCKPIT MALFUNCTIONED A C1HA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 15 696CA ON T/O ROLL AT 40 KNOTS APT ARMED FOLLOWED BY AUTO PACK TRIP AND ENG FAIL LIGHTS ILLUMINATED, ABORTED T/O RETURN TO GATE . INSPECTED AND CHECKED ENGINES RAN ENGINE AT TAKE-OFF EPR AND OPS CHECK NORMAL. 2 L 7 3 4F 4 F RT A3WE E2EA 2001100900118 20011009 00118 WP 2001 10 9 UPS01836965 1 20011002 A 3350 6012235 BATTERY PACK DOUG DC8 DC873 302199C WP CABIN FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 880UP 46080 EMERGENCY LIGHTS WILL NOT TEST. REPLACED EMERGENCY LIGHT BATTERY PACK IAW MM 33-50-01, TESTS GOOD. 2 L 7 4 4F RT 4A25 2001100900119 20011009 00119 WP 2001 10 9 UPS01836968 1 20011002 A 3350 BATTERY DOUG DC8 DC873 302199C WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 880UP 46080 EMERGENCY LIGHTS WILL NOT TEST. REPLACED BATTERY PACK TESTS GOOD. 2 L 7 4 4F RT 4A25 2001100900120 20011009 00120 NM 2001 10 9 C1HA200196015 1 20010929 A 3350 CAP BOEING 727 7272S7 138407Z NM CABIN MISSING A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 686CA 22021 EMERGENCY FLOOR TRACK LIGHTING FROM ROW 32 EXIT IS OFF. INSTALLED MISSING END CAP EMERGENCY FLOOR TRACK AT ROW 32 AS REQ UIRED. 2 L 7 3 4F A3WE 2001100900121 20011009 00121 WP 2001 10 9 UPS01836973 1 20011003 A 3397 LIGHT DOUG DC8 DC873 302199C WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 801UP 46101 EMERGENCY LIGHTS WILL NOT TEST. FOUND BAD CONNECTOR WIRE AND TERM STRIP GND WIRE BROKEN 2 L 7 4 4F RT 4A25 2001100900122 20011009 00122 NM 2001 10 9 C1HA200197006 1 20010917 A 2560 FLASHLIGHT BOEING 727 727270 138408P NM CABIN INOPERATIVE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 697CA 23052 AFT A/C RT EMERGENCY HAND HELD FLASHLIGHT RED CHARGING LIGHT INOP. REMOVED AND REPLACED EMERGENCY HAND HELD FLASHLIGHT A ND BATTERY PACK. 2 L 7 3 4F RT A3WE 2001100900123 20011009 00123 WP 2001 10 9 UPS01836974 1 20010917 A 5730 SKIN DOUG DC8 DC873 302199C WP RIGHT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE: SP, RIGHT WING UPPER SKIN BLENDOUT IS BEYOND LIMITS AT ACCESS PANEL 505B AT APPROX. STA. XRS489 AT STR INGER 7. REPAIRED SKIN I.A.W. SRM. 57-2-1 FIG. 36 2 L 7 4 4F RT 4A25 2001100900124 20011009 00124 WP 2001 10 9 UPS01836975 1 20010926 A 5710 3644046501 FITTING DOUG DC8 DC873 302199C WP LEFT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE: C1, LEFT WING STRINGER 64 END SPLICE FITTING IS CRACKED AT FRONT SPAR. REMOVED,FABRICATED,AND REPL ACED FITTING I.A.W. DWG. 3644046.AND SRM. 51-1-20D 2 L 7 4 4F RT 4A25 2001100900125 20011009 00125 WP 2001 10 9 UPS01836976 1 20010928 A 5710 3644046502 FITTING DOUG DC8 DC873 302199C WP RIGHT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE: C1, RIGHT WING STRINGER 64 END/SPLICE FITTING IS CRACKED AT FRONT SPAR. REMOVED,FABRICATED,AND REP LACED FITTING I.A.W. DWG. 3644046,AND SRM. 51-1-20D 2 L 7 4 4F RT 4A25 2001100900126 20011009 00126 WP 2001 10 9 UPS01836977 1 20010921 A 5310 LONGERON DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP INSPECTION TYPE: C1, STA. 965 LONG. 24R IS CRACKED ON BOTTOM SIDE. REPAIRED LONGERON I.A.W. SRM. 53-2-2 FIG. 5 2 L 7 4 4F RT 4A25 2001101800037 20011018 00037 GL 2001 10 18 C2XA01CL208 2 20010928 A 7230 23069629 TORQUE TUBE EMB 145 EMB145ER SO ALLSN AE300 AE3007A GL INLET GUIDE VANE FAILED A C2XA K NONE J WARNING INDICATION AP APPROACH 1 SW 27 14940 7245 1655 145033 311021 CLE-BNA FLIGHT NR 4045 CREW REPORTED THAT THE NR 2 ENGINE N2 WENT TO 102.5 PERCENT WITH N1 AT 67 PERCENT MAX. COULD NOT GET MORE THAN 67 PERCENT N1 AT ANY TIME. NR 2 ENGINE FAILED ON LANDING ROLLOUT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE AND OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. SUPPLEMENT: INTERNAL ENGINE INSPECTION AT THE REPAIR FACILITY REVEALED THE IGV TORQUE TUBE HAD FAILED. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001100900127 20011009 00127 WP 2001 10 9 UPS01836978 1 20010920 A 5320 47504201 FITTING DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE: C1, STA. 859 LONG. 18L INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED, FABRICATED, AND RE PLACED FITTING I.A.W. DWG. 4750420,AND SRM 51-1-20D 2 L 7 4 4F RT 4A25 2001100900128 20011009 00128 WP 2001 10 9 UPS01836979 1 20010921 A 5320 97540241 FITTING DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE: C1, STA. 280 ABOVE LONG. 27R FLOORBEAM SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING I. A.W. DWG. 9754024,AND SRM. 51-1-21, 51-3-0 2 L 7 4 4F RT 4A25 2001101900005 20011019 00005 SO 2001 10 19 C2XA01CL210 1 20011001 A 2612 WARNING SYSTEM EMB 145 EMB145LR SO COCKPIT FALSE INDICATION A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 16976 145171 CLE FLIGHT 3931 CREW REPORTED BAGGAGE FIRE EXTINGUISHER BUTTON ILLUMINATED DURING FLIGHT. NO EICAS MSG OR MASTER WARNIN G WAS ASSOCIATED. RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RESET SYSTEM. ALL OPERATIONA L CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001100900129 20011009 00129 WP 2001 10 9 UPS01836980 1 20010920 A 5320 3779498504 FITTING DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE: C1, STA. 902 LONG. 18L INTERCOSTAL TO FRAME FITTING IS CRACKED REMOVED,FABRICATED,AND REPLACED FIT TING I.A.W. DWG. 3779498,AND SRM. 51-1-20D 2 L 7 4 4F RT 4A25 2001100900130 20011009 00130 2001 10 9 C2XA01CL211 4 20011003 A 3452 7510700726 TRANSPONDER EMB 135 EMB135ER 3260203 SO COCKPIT FAILED A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 15509 3498 145238 CLE FLIGHT NR 3899 CREW REPORTED THAT THE NUMBER 1 TRANSPONDER NO MODE "C". NUMBER 2 TRANSPONDER ALREADY ON MEL. RETUR NED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, AND REMOVED AND REPLACED THE NUMBER 1 TRANSPONDER. SYSTE M OPERATIONAL CHECKS GOOD. AIRCRAFT WAS RELEASED TO SERVICE. 2 L 7 2 4F RT T00011AT 2001100900131 20011009 00131 WP 2001 10 9 UPS01836981 1 20010920 A 5320 47794961 FITTING DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE: C1, STA. 902 LONG. 18L INTERCOSTAL TO FRAME AFT FITTING IS CRACKED REMOVED,FABRICATED,AND REPLACED FITTING I.A.W. DWG. 4779496,AND SRM. 51-1-20D 2 L 7 4 4F RT 4A25 2001100900132 20011009 00132 WP 2001 10 9 AALA20011648 1 20010818 A 3350 P4010049 BATTERY PACK DOUG DC9 DC983 3022083 WP A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 595AA 53285 LAX - DURING OVERNIGHT MAINTENANCE, TAIL COMPARTMENT EMERGENCY EXIT LIGHTS FAILED TEST. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001100900133 20011009 00133 EU 2001 10 9 AALA20011445 1 20010719 A 3350 LAMP FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1412A 11370 ORD - DURING OVERNIGHT MAINTENANCE, EIGHT FORWARD CABIN EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. REPLACED EIGHT FORWAR D CABIN LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001100900134 20011009 00134 EU 2001 10 9 AALA20011446 1 20010719 A 3350 LAMP FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1412A 11370 ORD - DURING OVERNIGHT MAINTENANCE, THIRTEEN MID CABIN EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. REPLACED THIRTEEN MID CABIN LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001100900135 20011009 00135 EU 2001 10 9 AALA20011417 1 20010713 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A K NONE L NO TEST IN INSP/MAINT 1 SW 21 1401G 11352 DFW - DURING OVERNIGHT MAINTENANCE, NR 2 AISLE STANDBY LIGHT INOPERATIVE. REPAIRED WIRE TO AISLE STANDBY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001100900136 20011009 00136 NM 2001 10 9 USAA011224 1 20010910 A 5300 WEB BOEING 737 7372B7 1384560 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 275AU 51053 22887 CLT - FOUND WEB CRACKED .75 INCH, BS 178, LBL 10, WL 234. REPAIR DOUBLER INSTALLED PER EA 85403. (M) 2 L 7 2 4F A16WE 2001100900137 20011009 00137 NM 2001 10 9 USAA011225 1 20010910 A 5310 WEB BOEING 737 7372B7 1384560 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 275AU 51053 22887 CLT - FOUND WEB CRACKED .75 INCH, BS 178, RBL 10, WL 234. INSTALLED REPAIR DOUBLER PER EA 85403. (M) 2 L 7 2 4F A16WE 2001100900138 20011009 00138 NM 2001 10 9 USAA011234 1 20010912 A 5300 INTERCOSTAL BOEING 737 7372B7 1384560 NM BS 180 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 275AU 51053 22887 CLT - FOUND INTERCOSTAL 1.5 INCH, BS 180 WL 195 RBL 26. REMOVED AND REPLACED INTERCOSTAL PER EO 5300V157. (M) 2 L 7 2 4F A16WE 2001100900139 20011009 00139 NM 2001 10 9 USAA011202 1 20010904 A 5300 FRAME BOEING 737 737201 1384454 NM BS 415 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 22961 CLT - FOUND FRAME CORRODED 5 INCHES, BS 415 STRINGER 25R. REMOVED DAMAGED SECTION OF STRINGER 25R, ADD STRINGER SPLICE J CHANNEL DOUBLER AND CENTER U-CHANNEL EA 85157, SRM 53-10-3. (M) 2 L 7 2 4F A16WE 2001100900140 20011009 00140 SO 2001 10 9 SIMA200124701 1 20010904 A 5600 163500109 WINDSHIELD EMB 145 EMB145LR SO COCKPIT FAILED A SIMA O OTHER O OTHER CR CRUISE 1 SW 21 631AE 145139 DFW - FLT 3766 - CAPTAIN'S WINDSHIELD SHATTERED IN FLIGHT. EMERGENCY WAS DECLARED. CAPTAINS WINDSHIELD WAS REMOVED AND REPLACED. (M) 2 L 7 2 4T RT T00011AT 2001100900141 20011009 00141 WP 2001 10 9 UPS01836982 1 20010919 A 5320 3757794503 STIFFENER DOUG DC8 DC873 302199C WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE: C1, STA. 1215-1220 DIAGONAL STIFFENER IS CORRODED AT LONG. 33R. REMOVED AND REPLACED STIFFENER I.A .W. DWG. 375794,AND SRM. 51-1-20D 2 L 7 4 4F RT 4A25 2001100900142 20011009 00142 WP 2001 10 9 UPS01836983 1 20010926 A 5330 SKIN DOUG DC8 DC873 302199C WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE: C1, STA. 1690 LONG. 28L FUSELAGE SKIN IS CORRODED BEYOND LIMITS. REPAIRED SKIN I.A.W. SRM. 53-2-1 FIG . 7 2 L 7 4 4F RT 4A25 2001100900143 20011009 00143 WP 2001 10 9 UPS01836984 1 20010920 A 5311 FRAME DOUG DC8 DC873 302199C WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE: C1, STA. 1160 FRAME IS CORRODED BEYOND LIMITS BETWEEN LONG. 4L TO 5L. REPAIRED FRAME I.A.W. DC8-53A -011 2 L 7 4 4F RT 4A25 2001100900144 20011009 00144 WP 2001 10 9 UPS01836985 1 20010921 A 5320 5613861119 FITTING DOUG DC8 DC873 302199C WP COCKPIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE: C1, STA 127 FRAME ABOVE PRESSURE WEB IS CORRODED LH OB SIDE APPROX. LBL. 50. REMOVED, FABRICATED, AND RELACED FITTING I.A.W. DWG. 5613861,AND SRM. 51-1-20D,51-1-21 2 L 7 4 4F RT 4A25 2001100900145 20011009 00145 NM 2001 10 9 UPS01M36777 1 20010411 A 5347 S49291477075T6 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 250UP INSPECTION TYPE: C, MAIN DECK SEAT TRACK LBL 9 CORRODED AT BS 840 TO BS 898. CORROSION CLEANED FOUND OUT OF LIMIT A T STA 840 - 919. NEW SEAT TRAC K INSTALLED AS PER SRM 53-70-00 REV.28. 2 L 7 3 4F RT A22WE 2001100900146 20011009 00146 EU 2001 10 9 2001F00397 1 20010906 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY MALFUNCTIONED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 21 383AE 340B383 DFW - CARGO SMOKE WARNING LIGHT ILLUMINATED DURING CRUISE. NR 1 FIRE BOTTLE WAS ACTUATED. WARNING LIGHT WENT OUT WITHI N SEVERAL MINUTES AFTER BOTTLE WAS BLOWN. MAINTENANCE REMOVED AND REPLACED FORWARD AND AFT CARGO SMOKE DETECTORS IAW SA AB 340 AMM. OPS CHECK WAS SATISFACTORY. REF SIMA200124904. (M) 2 L 7 2 4T RT A52EU 2001100900147 20011009 00147 NM 2001 10 9 UPS01M36822 1 20010914 A 5312 NJC6040175 TEE CHORD DOUG MD11 MD11F 3023600 NM AFT BULKHEAD CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 252UP INSPECTION TYPE: C, AFT PRESSURE BULKHEAD LOWER 'T'-CHORD AT STA 2007 FOUND WITH CORROSION. "T" CHORD AT AFT PRESSU RE BULKHEAD STA 2007 REMOVED AS PER SRM 51-31-01 REV 29. PICK UP HOLES AND TRIMMED AS PER DWG NJC6040. INSTALLED NEW 'T' CHORD TREATED & PRIMED AS PER SRM 51-21-01 VOL 2 REV. 29. ITEM 27.* 2 L 7 3 4F RT A22WE 2001100900148 20011009 00148 EU 2001 10 9 AALA20011447 1 20010719 A 3350 BALLAST FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1412A 11370 ORD - DURING OVERNIGHT MAINTENANCE, CABIN EMERGENCY EXIT LIGHT BALLAST BAD. REPLACED EMERGENCY EXIT LIGHT FIXTURE. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001100900149 20011009 00149 SO 2001 10 9 SIMA200123419 1 20010814 A 5315 FLOORBEAM EMB 145 EMB145LR SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 642AE 145193 ABI - DURING MBV INSPECTION, MAINTENANCE FOUND CORROSION ON THE LEFT OMEGA BEAM AT FRAME 20. CORROSION WAS REMOVED AND AREA WAS REPAIRED IAW EMB SRM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001100900150 20011009 00150 SO 2001 10 9 SIMA200123420 1 20010820 A 5315 FLOORBEAM EMB 135 EMB135LR SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 708AE 145205 ABI - DURING MBV INSPECTION, MAINTENANCE FOUND THE LEFT OMEGA BEAM AT FRAME 20 TO BE CORRODED. CORROSION WAS REMOVED AN D AREA WAS REPAIRED IAW EMB SRM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001100900151 20011009 00151 SO 2001 10 9 SIMA200124301 1 20010831 A 4930 4503258 FUEL LINE EMB 145 EMB145LR SO APU CHAFED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 624AE 145111 XNA - MAINTENANCE REPORTED APU WOULD NOT START. MAINTENANCE TROUBLESHOT AND FOUND APU FUEL LINE WHICH RUNS TO THE START FUEL NOZZLES CHAFFED. REMOVED AND REPLACED APU FUEL LINE IAW HAMILTON SUNSTRAND CMM. (M) 2 L 7 2 4T RT T00011AT 2001100900153 20011009 00153 EU 2001 10 9 SIMA200124702 1 20010904 A 7603 C8222410 CONTROL CABLE SAAB SF340 340B 7860101 EU LT ENGINE FAILED A SIMA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 902AE 340B269 CLL - FLT 3902 - DURING CLIMB, LEFT ENGINE TORQUE DROPPED TO 30 PERCENT. CREW DECLARED INFLIGHT EMERGENCY, SHUT ENGINE DOWN, AND RETURNED TO FIELD. REMOVED AND REPLACED LEFT WING PUSHPULL POWER CABLE FROM HMU TO NACELLE WHEEL WELL IAW SAA B 340 AMM 76-10-00. (M) 2 L 7 2 4T RT A52EU 2001100900154 20011009 00154 EU 2001 10 9 SIMA200124803 1 20010905 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 235AE 340B235 ABI - DURING MBV INSPECTIONS, FOUND UPPER FLANGE OF BOTTOM FRAME 225 HAD CORROSION BEYOND SRM LIMITATIONS. REMOVED CORR OSION AND REPAIRED IAW SAAB 340 SRM. (M) 2 L 7 2 4T RT A52EU 2001100900159 20011009 00159 NM 2001 10 9 01FDEA00852 1 20010917 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE MISDRILLED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 258FE 20940 N 783 FLOORBEAM LWR FLANGE HAS DRILL HOLE IN RADIUS BS 460, RBL 45, WL 208. R&R FLOORBEAM PER SR 27-53-034E & SRM 51-30 -2. 2 L 7 3 4F RT A3WE 2001100900160 20011009 00160 NE 2001 10 9 01FDEA00860 2 20010927 A 7200 ENGINE AIRBUS 310 A310222 3930315 EU PWA JT9 JT9D* NE NR 2 MALFUNCTIONED A FDEA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 25 453FE 267 707728 01-324 ON T/O NR 2 ENGINE N1 STAGNATED & W/N ACCELERATE PAST 49 PERCENT, ALL PARAMETERS NORMAL AND PROCEEDED TO T/O. 2 L 7 2 4F 4 F RT A35EU E20EA 2001100900162 20011009 00162 WP 2001 10 9 01FDEA00863 1 20011001 A 5320 STRUCTURE DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 NR 491 AFT PIN RBL 22 AT BS 1967 VERTICAL CORROSION LVL 2 UNDER SEALANT AROUND ACCESS PNL. ** S/D ** COMING 2 L 7 3 4F RT A22WE 2001102500262 20011025 00262 NM 2001 10 25 01FDEA00866 1 20010929 A 5320 SPLICE BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 281FE 22348 STRINGER SPLICE CORRODED BEYOND LIMITS AT BS 690, STR 27L. REMOVED AND REPLACED SPLICE PER SRM 53-10-3, 51-30-2 & 51-10- 2. 2 L 7 3 4F RT A3WE 2001100900163 20011009 00163 NM 2001 10 9 01FDEA00868 1 20010929 A 5320 SPLICE BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 281FE 22348 N 463 STRINGER SPLICE CORRODED BEYOND LIMITS AT BS 690, STR 27R. R/R SPLICE PER SRM 53-10-8, 51-30-2, 51-10-6. 2 L 7 3 4F RT A3WE 2001100900164 20011009 00164 NM 2001 10 9 01FDEA00869 1 20011001 A 5310 BAC1512705 FRAME BOEING 727 727233 138408A NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 281FE 22348 N 703 BAD FASTENER HOLES AT BS 420 FRAME STR 8L. R&R DOUBLER PER EA 7-5310-60509. 2 L 7 3 4F RT A3WE 2001110700110 20011107 00110 WP 2001 11 7 01FDEA00871 1 20011008 A 5751 AILERON DOUG DC10 DC1010F 3022111 WP RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 364FE 46600 SIX SEPARATE AREAS ON RT OUTBOARD AILERON LWR CORRODED. REMOVED AND REPLACED AILERON PER IAW AMM 27-10-02-4. 2 L 7 3 4F A22WE 2001100900165 20011009 00165 EU 2001 10 9 DHL2001362033 1 20010927 A 3510 OXYGEN MASK AIRBUS 300 A300B4203 3930306 EU COCKPIT INTERMITTENT A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 362DH 84 1) F/OS OXYGEN MASK EMERGENCY OPERATION INTERMITTING 2) REPLACED F/O'S OXYGEN MASK EMERGENCY OPS CK NORMAL IAW 35-1 0-00 STATUS: CLOSED 2 L 7 2 4F RT A35EU 2001100900166 20011009 00166 EU 2001 10 9 SIMA200124902 1 20010906 A 3234 D49410001 CONTROL HANDLE SAAB SF340 340B 7860101 EU COCKPIT FAULTY A SIMA O OTHER N FALSE WARNING AP APPROACH 1 SW 21 286AE 340B286 BGR - FLT 4929 - CREW INITIATED EMERGENCY LANDING DUE TO THE LEFT MAIN LANDING GEAR INDICATION NOT SHOWING DOWN AND LOCK ED (GREEN) DURING APPROACH. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE IAW SAAB 340 AMM. LANDING GEA R OPERATIONALLY AND FUNCTIONALLY CHECKED GOOD. (M) 2 L 7 2 4T RT A52EU 2001100900167 20011009 00167 EU 2001 10 9 SIMA200124904 1 20010906 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY MALFUNCTIONED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 21 383AE 340B383 DFW - CARGO SMOKE WARNING LIGHT ILLUMINATED DURING CRUISE. NR 1 FIRE BOTTLE WAS ACTUATED. WARNING LIGHT WENT OUT WITHI N SEVERAL MINUTES AFTER BOTTLE WAS BLOWN. MAINTENANCE REMOVED AND REPLACED FORWARD AND AFT CARGO SMOKE DETECTORS IAW SA AB 340 AMM. OPS CHECK WAS SATISFACTORY. (M) 2 L 7 2 4T RT A52EU 2001100900168 20011009 00168 EU 2001 10 9 SIMA200124905 1 20010906 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 235AE 340B235 DURING MBV INSPECTION, FOUND FRAME 236.5 UNDER GALLEY AREA HAD CORROSION BEYOND SRM LIMITS. CORROSION WAS REMOVED FROM FRAME AND WAS REPAIRED IAW SAAB 340 SRM. (M) 2 L 7 2 4T RT A52EU 2001100900169 20011009 00169 EU 2001 10 9 SIMA200125001 1 20010907 A 2520 E152000161 CIRCUIT BOARD SAAB SF340 340B 7860101 EU PSU DEFECTIVE A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 320AE 340B320 LAX - FLT 3202 - DURING CRUISE, FLIGHT ATTENDANT REPORTED ODOR OF BURNED ELECTRICAL INSULATION FROM GALLEY AREA BY COFFE E JUG. CIRCUIT BOARD IN PSU AT SEAT 3A FOUND DEFECTIVE. REMOVED AND REPLACED SEAT 3A PSU IAW SAAB 340 AMM. NO FURTHER BURNED ODORS NOTED. (M) 2 L 7 2 4T RT A52EU 2001100900170 20011009 00170 NM 2001 10 9 USAA011196 1 20010904 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND SKIN CORRODED 1 INCH BY 2 INCH, BS 1016. CORROSION LEVEL 2. INSTALLED DOUBLER PER EA 85159 AND EA 85231. (M) 2 L 7 2 4F A16WE 2001100900171 20011009 00171 NM 2001 10 9 USAA011200 1 20010904 A 5510 FITTING BOEING 737 737201 1384454 NM HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 22961 CLT - FOUND CORROSION ON CLEVIS LUG .020 INCH BY 2 INCH, LEFT HORIZONTAL, STAB CENTER SECTION UP REAR SPAR FORWARD LUG. SPOT FACED AFFECTED AREA AND INSTALLED NEW BUSHINGS PER EA NR 85229. (M) 2 L 7 2 4F A16WE 2001100900172 20011009 00172 NM 2001 10 9 USAA011201 1 20010904 A 5510 FITTING BOEING 737 737201 1384454 NM HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 22961 CLT - FOUND CORROSION ON CLEVIS LUG .019 INCH BY 2 INCH, LEFT HORIZONTAL CENTER, UP REAR SPAR AFT LUG, AFT FACE. SPOT F ACED AFFECTED AREA AND INSTALLED NEW BUSHINGS PER EA NR 85229. (M) 2 L 7 2 4F A16WE 2001100900173 20011009 00173 NM 2001 10 9 USAA011203 1 20010904 A 5312 BULKHEAD BOEING 737 737201 1384454 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 22961 CLT - FOUND WEB SKIN DAMAGED 10 SQUARE INCHES, BS 178, WL 196 TO WL 205, LBL 10.5 TO RBL 10.5. C/O DAMAGE VERIF, NO DAM AGE AT PERIM INSU CUT .100 MORE, INSTALLED DOUBLER PER EO 5300V153, EA 69902, SRM 531008. (M) 2 L 7 2 4F A16WE 2001100900174 20011009 00174 NM 2001 10 9 USAA011204 1 20010905 A 5314 KEELBEAM BOEING 737 737201 1384454 NM FUSELAGE CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 22961 CLT - FOUND KEEL BEAM CHAFED 1 INCH BY 64 INCHES, RT KEEL BEAM, BS 663-727. INSTALLED REPAIR WASHERS AND REPAIR STRAP P ER EA 85306A. (M) 2 L 7 2 4F A16WE 2001100900175 20011009 00175 NM 2001 10 9 USAA011205 1 20010905 A 5314 KEELBEAM BOEING 737 737201 1384454 NM FUSELAGE CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 22961 CLT - FOUND KEEL BEAM CHAFED 1 INCH BY 27 INCHES, LEFT KEEL BEAM BS 700-727 LOWER CHORD. INSTALLED REPAIR WASHERS AND R EPAIR STRAP PER EA 85306A. (M) 2 L 7 2 4F A16WE 2001100900176 20011009 00176 NM 2001 10 9 USAA011206 1 20010905 A 5313 STRINGER BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 22961 CLT - FOUND STRINGER SHELF 18A CRACKED .375 INCH, BS 727 AT STRINGER 18R. INSTALLED NON SHELF PER EA 85230. INSTALLED NON SHELF PER EA 85230. (M) 2 L 7 2 4F A16WE 2001100900177 20011009 00177 NM 2001 10 9 USAA011207 1 20010905 A 5313 STRINGER BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 47570 22961 CLT - FOUND STRINGER CRACKED .5 INCH, BS 360 STRINGER 11L. INSTALLED REPAIR DOUBLER PER SRM 53-1-2. (M) 2 L 7 2 4F A16WE 2001100900178 20011009 00178 NM 2001 10 9 USAA011220 1 20010910 A 5311 FRAME BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 275AU 51053 22887 CLT - FOUND CHORD CRACKED .09 INCH, BS 178 BULKHEAD, WL 207, RIGHT SIDE CHORD. SPLICED IN NEW SECTION OF CHORD PER EO NR 5300V157. (M) 2 L 7 2 4F A16WE 2001100900179 20011009 00179 NM 2001 10 9 USAA011221 1 20010910 A 5311 FRAME BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 275AU 51053 22887 CLT - FOUND CHORD CRACKED 1.75 INCH, BS 178 BULKHEAD, WL 207, LEFT SIDE CHORD. SPLICED IN NEW SECTION OF CHORD. (M) 2 L 7 2 4F A16WE 2001100900180 20011009 00180 NM 2001 10 9 USAA011223 1 20010910 A 5312 BULKHEAD BOEING 727 727251 138408H NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 275US 21154 CLT - FOUND WEB CRACKED .75 INCH, BS 178, WL 207, LBL 14. INSTALLED DOUBLER PER EO 85408. (M) 2 L 7 3 4F A3WE 2001100900181 20011009 00181 NM 2001 10 9 USAA011226 1 20010910 A 5320 INTERCOSTAL BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 275AU 51053 22887 CLT - FOUND INTERCOSTAL CRACKED 1.5 INCH, BS 180 WL 195 LBL 26. INSTALLED DOUBLER PER EO NR 5300V157. (M) 2 L 7 2 4F A16WE 2001100900182 20011009 00182 NM 2001 10 9 USAA011233 1 20010912 A 5320 WEB BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 275AU 51053 22887 CLT - FOUND FLOOR WEB CRACKED .25 INCH, WL 207 BS 180 RBL 26. REMOVED AND REPLACED FLOOR WEB PER EO 5300V157. (M) 2 L 7 2 4F A16WE 2001100900183 20011009 00183 NM 2001 10 9 USAA011238 1 20010914 A 5320 CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 48384 22962 CLT - FOUND CLIP CRACKED .25 INCH, BS 663, S10L. NEW CLIP INSTALLED PER EO 53936227. (M) 2 L 7 2 4F A16WE 2001100900184 20011009 00184 NM 2001 10 9 USAA011239 1 20010914 A 5320 CLIP BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 48384 22962 CLT - FOUND CLIP CRACKED .25 INCH, BS 706 AT S10L. NEW CLIP INSTALLED PER EO 53936227. (M) 2 L 7 2 4F A16WE 2001100900185 20011009 00185 NM 2001 10 9 USAA011241 1 20010914 A 5553 BACB30FD9114 BOLT BOEING 737 737201 1384454 NM VERTICAL STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 227AU 57214 21816 PIT - FOUND FAIL SAFE BOLT SEVERELY CORRODED, VERTICAL STABILIZER BOTTOM LEFT ATTACH FITTING. DEFECTIVE PART REPLACED W ITH IDENTICAL PART NR DEFECTIVE BOLT FOUND IN YQB. (M) 2 L 7 2 4F A16WE 2001100900186 20011009 00186 NM 2001 10 9 USAABB01095 1 20010909 A 2530 5000387D4 COFFEEMAKER BOEING 757 7572B7 1384964 NM GALLEY FAULTY A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 19 626AU 23075 27303 PIT - FLT 36 - APPROXIMATELY FIVE MINUTES PRIOR TO LANDING, CREW NOTED AN ELECTRICAL SMELL IN THE AFT GALLEY. MAINTENAN CE REPLACED THE 4B-11 COFFEEMAKER. (M) 2 L 7 2 4F RT A2NM 2001100900187 20011009 00187 NM 2001 10 9 USAASB01222 1 20010804 A 2751 1817389 TRANSMITTER BOEING 737 737301 1384611 NM T/E FLAP FAULTY A USAA O OTHER N FALSE WARNING AP APPROACH 1 EA 19 351US 23554 ORD - FLT 537 - A TRAILING EDGE FLAP ASYMMETRY OCCURRED ON APPROACH TO ORD FROM CLT. LEFT FLAP INDICATED 1 UNIT WHILE R IGHT FLAP INDICATED 1.5 UNITS. CREW DECLARED AN EMERGENCY, ACCOMPLISHED QUICK REF HANDBOOK PROCEDURES AND COMPLETED A F LAPS 1 LANDING WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT FLAP POSITION TRANSMITTER PER MM 27-58-12. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001100900188 20011009 00188 NM 2001 10 9 USAASB01241 1 20010824 A 2910 65C268103024 HYDRAULIC LINE BOEING 737 7373B7 1384580 NM RT MLG W/W CRACKED A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 510AU 23385 DTW - FLT 1291 - ON CLIMB-OUT FROM DTW, EN ROUTE TO PHL, CAPTAIN REPORTED A FAILURE OF THE 'A' HYDRAULIC SYSTEM ALONG WI TH HYDRAULIC QUANTITY LOSS. CAPTAIN DECIDED IT WAS BEST TO RETURN TO FIELD TO DTW. FLIGHT LANDED WITHOUT FURTHER INCID ENT AND WAS TOWED TO THE GATE DUE TO NO NOSE WHEEL STEERING. AN EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE RIGHT ML G UP HYDRAULIC LINE CRACKED AND LEAKING. REMOVED ADN REPLACED LINE WITH TEMPORARY LINE, THEN LATER REPLACED WITH PERMAN ENT LINE. LEAK CHECKED GOOD PER MM 32-32-00. (M) 2 L 7 2 4F RT A16WE 2001100900189 20011009 00189 NM 2001 10 9 USAASB01250 1 20010913 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 504AU 23379 CLT - MAINTENANCE FOUND THE CABIN EMERGENCY LIGHTING AT SEAT ROWS 17 TO 22, LEFT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001100900190 20011009 00190 NM 2001 10 9 USAASB01251 1 20010911 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 376US 22955 ORD - MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE MID LEFT EM ERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001100900191 20011009 00191 NM 2001 10 9 USAASB01252 1 20010912 A 3350 20131A BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 435US 24557 GSO - MAINTENANCE FOUND THE EMERGENCY LIGHTS, ON THE LAST FEW SEATS IN COACH CLASS, INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001100900192 20011009 00192 NM 2001 10 9 USAASB01254 1 20010912 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 520AU 23706 LGA - MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT OVER WING EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001100900193 20011009 00193 NM 2001 10 9 SWAA012628 1 20010924 A 3350 1011133 LIGHT BOEING 737 7373H4 1384600 NM COCKPIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 313SW 23335 DURING SCHEDULED A2 CHECK, FOUND COCKPIT OVERHEAD EMERGENCY LIGHT INOP. RELAMPED OVERHEAD EMERGENCY LIGHT. 2 L 7 2 4F RT A16WE 2001101000001 20011010 00001 SO 2001 10 10 C2XA01TY150 1 20011009 A 3350 1317 BULB EMB 145 EMB145LR SO CABIN BLOWN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14960 145100 TYS During a scheduled inspection, the emergency light above seat 12A was found not working. Maintenance removed and re placed the light bulb, operational checks good I.A.W.-EMB-MM-33-50-09. Aircraft released to servive. 2 L 7 2 4T RT T00011AT 2001101000002 20011010 00002 SO 2001 10 10 C2XA01TY151 1 20011009 A 3350 1317 BULB EMB 145 EMB145LR SO CABIN BLOWN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14960 145100 TYS During a scheduled inspection, the emergency light in the service door was found not working. Maintenance removed a nd replaced the light bulb, operational checks good I.A.W.-EMB-MM-33-50-09. Aircraft released to servive. 2 L 7 2 4T RT T00011AT 2001101000003 20011010 00003 SO 2001 10 10 C2XA01TY152 1 20011009 A 5300 PE6402H4016 BUSHING EMB 145 EMB145LR SO WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS During a scheduled inspection, the passenger door airframe fitting for the hold open hook has a displaced & loose l ower pin bushing. Maintenance removed and replaced the bushing I.A.W.-EMB-GST-1682/01. Repair were satisfactory, Aircraf t will be released to servive upon complection of inspection 2 L 7 2 4T RT T00011AT 2001101000004 20011010 00004 NM 2001 10 10 2001UALA02067 1 20010919 A 2910 NAS1611014 PACKING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 659UA 27114 RIGHT HYDRAULIC SYSTEM MSG AND LOW QTY LIGHT ILLUMINATED, QTY DOWN TO 0.4, PUMPS TURNED OFF AND HYD FLUID LOSS MINIMIZED . RETURN TO FIELD OVERWEIGHT LANDING. SUPPLEMENTAL DATA UPDATE REPLACED PACKING OF CASE DRAIN FILTER DIFFERENTIAL PRESSU RE INDICATOR. OPS CHECK, NO MORE LEAKAGE FOUND.REFILLED RIGHT HYDRAULIC RESERVOIR. 2 L 7 2 4F 4 F RT A1NM E24NE 2001101000005 20011010 00005 NM 2001 10 10 2001UALA02082 1 20010924 A 2932 731414 ACTUATOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE A UALA K NONE J WARNING INDICATION LD LANDING 1 WP 29 7253U 21400 AIRCRAFT LOST SYSTEM "A" HYDRAULIC PRESSURE AND QUANTITY DURING LANDING. SUPPLEMENTAL DATA UPDATE FOUND RT MLG DOOR AC T BROKEN, LARGE LEAK. REPLACED ACTUATOR. SYSTEM CHECKS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001101000008 20011010 00008 NM 2001 10 10 CALA0100934 1 20011005 A 5512 SKIN BOEING 737 7373T0 1384582 NM STA 147.90 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10323 23374 INSPECTION FOUND L/H HORIZONTAL STABILIZER L/E SKIN DENTED AT STA 147.90. A REPAIR WAS INSTALLED IAW ECRA 5510-01602. 2 L 7 2 4F RT A16WE 2001101000009 20011010 00009 WP 2001 10 10 CALA0100936 1 20011009 A 5330 SKIN DOUG DC9 DC982 3022082 WP STA 1401 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69803 49229 INSPECTION FOUND A 1/2" CRACK IN R/H FUSELAGE SKIN JUST ABOVE ENGINE PYLON AT STA 1401. A DOUBLER WAS INSTALLED IAW SRM 53-04. 2 L 7 2 4F A6WE 2001101000014 20011010 00014 NM 2001 10 10 F3LA200100110 1 20010924 A 5310 DOOR FRAME BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 921WA 2755 23039 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON LT SIDE OF E&E DOOR CUTOUT BETWEEN CHORD AND SKIN. REMOVED DOOR FITT INGS, CORRODED WEBS, SKIN AND CHORDS. INSTALLED NEW CHORDS, WEBS AND STIFFENERS, NEW SKIN, FASTENERS, DOOR FITTINGS AND ALL RELATED HARDWARE AND STRUCTURE PER BOEING DRAWINGS 65-45800 AND SRM 53-10-2, 51-40-2 AND 53-10-1. 2 L 7 2 4U RT A16WE 2001101000016 20011010 00016 NM 2001 10 10 HNAA0100063 1 20010815 A 5313 STRINGER DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 934HA 139 STRINGER 31S CORRODED AT STATION X207. BLENDED CORROSION ON STRINGER. 2 H 7 2 4T RT A13NM 2001101000017 20011010 00017 NM 2001 10 10 SWAA012632 1 20010924 A 3350 D71702030 BATTERY BOEING 737 7377H4 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 799SW 28209 DURING SCHEDULED CHECK, FOUND EEPLS INOP AT FWD CABIN. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001101000018 20011010 00018 2001 10 10 SWAA012633 4 20010923 A 2565 D31354 SLIDE BOEING 737 7377H4 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 733SA 27865 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER M M. 2 L 7 2 4F RT A16WE 2001101000019 20011010 00019 2001 10 10 SWAA012636 4 20010923 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2001101000020 20011010 00020 NM 2001 10 10 SWAA012637 1 20010923 A 3350 57771 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED CHECK, FOUND EEPLS END CAP MISSING AT FWD CABIN. INSTALLED CAP PER MM. 2 L 7 2 4F A16WE 2001101000021 20011010 00021 2001 10 10 SWAA012639 4 20010923 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2001101000022 20011010 00022 NM 2001 10 10 SWAA012642 1 20010922 A 5312 6516300 BULKHEAD BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED SPECIAL VISIT, FOUND WEBS CRACKED (2 EA) AT BS 178, WL 207 & LBL 26.5, WL 234 & LBL 9.0. REMOVED AND R EPLACED WEBS PER SRM & SWA ACO 7338-53. 2 L 7 2 4F RT A16WE 2001101000023 20011010 00023 NM 2001 10 10 SWAA012643 1 20010921 A 5311 BAC1505 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 606SW 27926 DURING SCHEDULED SPECIAL VISIT, FOUND BOTH LT & RT SIDE CHORDS CRACKED AT BS 178, WL 207. REMOVED AND REPLACED CHORDS P ER SRM & SWA ACO 7395-53. 2 L 7 2 4F RT A16WE 2001101000024 20011010 00024 NM 2001 10 10 SWAA012645 1 20010925 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 388SW 26591 EEPLS LOOSE AT MID CABIN. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001101000025 20011010 00025 NM 2001 10 10 SWAA012651 1 20010924 A 3350 100885 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED SPECIAL VISIT, FOUND AFT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001101000026 20011010 00026 NM 2001 10 10 SWAA012652 1 20010924 A 3350 57771 CAP BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED C4 CHECK, FOUND EEPLS END CAP MISSING IN AFT CABIN. INSTALLED END CAP PER MM. 2 L 7 2 4F RT A16WE 2001101000027 20011010 00027 NM 2001 10 10 SWAA012653 1 20010924 A 3350 BR2013 SOCKET BOEING 737 7373H4 1384600 NM CABIN DEFECTIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED C4 CHECK, FOUND EEPLS LIGHT INOP (1 EA) AT AFT CABIN. REMOVED AND REPLACED LIGHT SOCKET PER MM. 2 L 7 2 4F RT A16WE 2001101000028 20011010 00028 NM 2001 10 10 SWAA012654 1 20010924 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT LT OVERWING EXIT. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001101000029 20011010 00029 NM 2001 10 10 SWAA012655 1 20010925 A 3350 6104781 BATTERY BOEING 737 7372K6 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED PM CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001101000030 20011010 00030 2001 10 10 SWAA012662 4 20010926 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 383SW 26589 DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED S LIDE PER MM. 2 L 7 2 4F RT A16WE 2001101000031 20011010 00031 NM 2001 10 10 SWAA012665 1 20010925 A 3221 1060545 BEARING BOEING 737 7373H4 1384600 NM NLG TRUNNION OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 632SW 27707 DURING SCHEDULED C1 CHECK, FOUND LEFT MAIN NOSE GEAR TRUNNION BEARING SHIMS MIGRATED .625 INCH TO .75 INCH FROM MOUNT FL ANGE. REMOVED AND REPLACED TRUNNION BEARING AND SHIMS PER MM. 2 L 7 2 4F RT A16WE 2001101000032 20011010 00032 NM 2001 10 10 SWAA012667 1 20010924 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2001101000033 20011010 00033 2001 10 10 SWAA012669 4 20010927 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2001101000034 20011010 00034 2001 10 10 SWAA012671 4 20010927 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001101000035 20011010 00035 NM 2001 10 10 SWAA012674 1 20010926 A 5320 65C27314 CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED 1/4D CHECK, FOUND TIE CLIP CRACKED AT BS 663, STR 4R. REMOVED AND REPLACED TIE CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001101000036 20011010 00036 NM 2001 10 10 SWAA012676 1 20010926 A 5311 963820 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED SPECIAL VISIT, FOUND RT OUTBOARD CHORD ANGLE CRACKED AT BS 178, WL 207. REMOVED AND REPLACED CHORD PER SWA ACO 7342-53. 2 L 7 2 4F RT A16WE 2001101000037 20011010 00037 2001 10 10 SWAA012677 4 20010925 A 3140 WARNING SYSTEM BOEING 737 7372H4 138448C NM GE CFM56 CFM56* 13802 NE COCKPIT FALSE ACTIVATION A SWAA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 082SW 22731 687808 ENGINE SHUT DOWN, DECLARED EMERGENCY, AIR TURNBACK. NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED AFTER T/O. REMOVED AND REPLACED OIL FILTER AND RAN ENGINE. CK'D FILTER, NO CONTAMINANTS FOUND. OPS CK GOOD PER MM. 2 L 7 2 4F 4 F A16WE E2GL 2001101000038 20011010 00038 2001 10 10 SWAA012679 4 20010929 A 2565 D31354 SLIDE BOEING 737 7373G7 1384595 NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691WN 23781 DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001101000039 20011010 00039 NM 2001 10 10 SWAA012683 1 20010928 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 623SW 27933 DURING SCHEDULED BC2 CHECK, FOUND KEEL BEAM CRACKED 1.5 INCH LONG RT MLG WW AFT SIDE. REPAIRED KEEL BEAM PER SWA TI-153 -009. 2 L 7 2 4F RT A16WE 2001101000040 20011010 00040 NM 2001 10 10 SWAA012686 1 20010926 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 342SW 24133 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 814, LBL 18 TO RBL 3. REPAIRED FLOORBEAM PER SWA RA 1-353-2 668. 2 L 7 2 4F RT A16WE 2001101000041 20011010 00041 NM 2001 10 10 SWAA012688 1 20010926 A 3260 189915 UPLOCK SENSOR BOEING 737 7372H4 138448C NM NLG OUT OF ADJ A SWAA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 068SW 22357 UNSAFE NOSE GEAR INDICATION LIGHT ILLUMINATED AT FL 350. LIGHT WENT OUT WITH LANDING GEARS DOWN. ADJUSTED NOSE GEAR UP LOCK SENSOR PER MM. 2 L 7 2 4F A16WE 2001101000042 20011010 00042 NM 2001 10 10 SWAA012690 1 20010928 A 5312 6517582 BULKHEAD BOEING 737 7373T5 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEBS CRACKED (2 EA) AT BS 178, RBL 17.1 & WL 235, LBL 17.1 & WL 227. REMOVED AND REPLACED WEBS PER SRM. 2 L 7 2 4F RT A16WE 2001101000043 20011010 00043 NM 2001 10 10 SWAA012691 1 20010927 A 3350 65C27093 LIGHT BOEING 737 7372T4 1384492 NM AFT ENTRY DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 2001101000044 20011010 00044 NM 2001 10 10 SWAA012726 1 20011001 A 3350 65C27093 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 091SW 22963 DURING SCHEDULED RON, FOUND FWD SVC DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2001101000045 20011010 00045 NM 2001 10 10 SWAA012731 1 20011002 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED C3 CHECK, FOUND EEPLS LOOSE AT FWD CABIN. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001101000046 20011010 00046 NM 2001 10 10 SWAA012732 1 20011001 A 3350 610478 BATTERY BOEING 737 7372K6 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED SPECIAL VISIT, FOUND EMERGENCY LIGHTS INOP AT AFT CABIN. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001101000047 20011010 00047 NM 2001 10 10 SWAA012734 1 20011003 A 5311 96380 FRAME BOEING 737 7372K6 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND RT SIDE CHORD CRACKED AT BS 178, WL 209. REMOVED AND REPLACED CHORD PER SW A ACO. 2 L 7 2 4F RT A16WE 2001101000048 20011010 00048 NM 2001 10 10 SWAA012735 1 20011001 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 334, BL 0.0 TO LBL 12.0. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2001101000049 20011010 00049 2001 10 10 SWAA012736 4 20011003 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 520SW 25319 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001101000050 20011010 00050 2001 10 10 SWAA012737 4 20011004 A 2565 22D22901 SLIDE BOEING 737 7372T4 1384492 NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001101000051 20011010 00051 NM 2001 10 10 SWAA012739 1 20011004 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 638SW 27711 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001101000052 20011010 00052 EA 2001 10 10 COMA0160786 1 20011006 A 3231 ROD CNDAIR CL600 CL6002B19 EA NLG MISRIGGED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 995CA 8057 7229 FLIGHT 5521 - NOSE L/G DOORS CYCLE CONSTANTLY AFTER GEAR RETRACTION.ADJUSTED THE L/H NLG DOOR LINKAGE. 2 L 7 2 4F RT A21EA 2001101000053 20011010 00053 NM 2001 10 10 SWAA012743 1 20011003 A 5753 6546431 FLAP BOEING 737 7373H4 1384600 NM LT WING DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 316SW 23338 DURING SCHEDULED C4 CHECK, FOUND LT OUTBOARD T/E FORE FLAP DISBONDED AT UPPER INBOARD END. REMOVED AND REPLACED FLAP PE R MM. 2 L 7 2 4F RT A16WE 2001103100018 20011031 00018 NM 2001 10 31 SWAA012745 1 20011002 A 5312 148A2232 BULKHEAD BOEING 737 7377H4 1384404 NM FUSELAGE CANNING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 743SW 29279 DURING SCHEDULED SERVICE CHECK, (SI 11152-53) FOUND AFT SIDE BS 1016 BULKHEAD HAS MULTIPLE DAMAGE, DENTS AND OIL CANNING BETWEEN LT & RT STRINGERS 1 & 4, ABOVE FIRST STRAP & BELOW 2ND STRAP. MX FERRY TO PAE FOR BAC EVALUATION. OCT 21, 200 1 REPAIRED BULKHEAD PER BOEING DOCUMENT 6-1171-RE-1013. 2 L 7 2 4F RT A16WE 2001101000054 20011010 00054 NM 2001 10 10 MASAM01101 1 20010910 A 7100 PWA DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE A MASA A UNSCHED LANDING B K SMOKE/FUMES/ODORS/SPARKS FLUID LOSS CR CRUISE 1 SO 07 455YV 455 IN FLIGHT, THE PILOT NOTICED AN OILY HAZE IN THE COCKPIT AND CABIN. THE PILOT SECURED THE NR 1 ENGINE BLEED WHICH SEEME D TO DISIPATE THE HAZE. THE AIRCRAFT RETURNED TO THE FIELD WITH AN UNEVENTFUL LANDING WHERE MAINTENANCE TROUBLESHOT THE PROBLEM. ON 8/13 MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE. 2 H 7 2 4T 4 T RT A13NM E20NE 2001101000055 20011010 00055 NM 2001 10 10 SWAA012747 1 20011005 A 3350 610479 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY & FWD SVC DOOR'S EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTE RY PER MM. 2 L 7 2 4F A16WE 2001101000056 20011010 00056 NM 2001 10 10 SWAA012748 1 20011007 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 639SW 27712 FWD INBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2001101000057 20011010 00057 2001 10 10 SWAA012751 4 20011007 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 612SW 27930 FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001101000058 20011010 00058 NM 2001 10 10 SWAA012761 1 20011007 A 5320 6551698 SPLICE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 522SW 26564 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2001101000059 20011010 00059 SO 2001 10 10 M01089 1 20010813 A 2500 HEATER EMB 145 EMB145LR SO ALLSN AE300 AE3007A GL BEVERAGE/GALLEY MALFUNCTIONED A MASA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 831MJ 145273 THE CREW FOUND THE OUTBOARD BEVERAGE HEATER GIVING OFF AN ELECTRICAL SMELL. MAINTENANCE FOUND THE PLUG IN THE BACK OF T HE HEATER SHORTING OUT. THE SYSTEM WAS DEACTIVATED AND DEFERRED. ON 8/15, MAINTENANCE REMOVED AND REPLACED THE INBOARD AND OUTBOARD BEVERAGE HEATER RECEPTACLES. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2001101200119 20011012 00119 EA 2001 10 12 COMA0160787 1 20011007 A 2750 FLAP CNDAIR CL600 CL6002B19 EA WINGS FAILED A COMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 SO 01 948CA 7079 FLIGHT 5234 - FLAPS FAILED AT 30 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. A/C CONTINUED SERVICE. 2 L 7 2 4F RT A21EA 2001101200120 20011012 00120 EA 2001 10 12 COMA0160788 1 20011007 A 2750 FLAP CNDAIR CL600 CL6002B19 EA WINGS FAILED A COMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 01 815CA 7397 FLIGHT 5671, FLAPS FAILED AT 30 DEGREES DURING LANDING APPROACH. RESET THE FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20- 01. A/C CONTINUED SERVICE. 2 L 7 2 4F RT A21EA 2001101000060 20011010 00060 EA 2001 10 10 M01111 1 20010921 A 3300 1317 LAMP CNDAIR CL600 CL6002B19 EA GE CF34 CF34* NE RT WNG LE INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37218 7218 DURING A MAINTENANCE PERFORMANCE CHECK, THE CREW FOUND A EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT AN D OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2001101000061 20011010 00061 2001 10 10 SWAA012763 4 20011007 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 074SW 22674 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2001101000062 20011010 00062 NM 2001 10 10 SWAA012764 1 20011007 A 2782 6544651 ACTUATOR BOEING 737 7372H4 138448C NM L/E SLAT FAILED A SWAA D RETURN TO BLOCK F FLT CONT AFFECTED CL CLIMB 1 SW 07 068SW 22357 AIR TURNBACK, NR 6 L/E SLAT WOULD NOT RETRACT, ALL FLAPS AND SLATS EXTENDED. REMOVED AND REPLACED NR 6 L/E SLAT ACTUATO R ASSY PER MM. 2 L 7 2 4F A16WE 2001101000063 20011010 00063 2001 10 10 VNAA0109002 4 20010905 A 3160 DISPLAY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 438JS 3056 DURING THE TAKEOFF ROLL, FLIGHT 4021 LOST REFERENCE DATA AND ABORTED TAKEOFF. WHILE DEPARTING THE RUNWAY AND ENTERING THE TAXI WAY THE REFERENCE DATA RE-APPEARED. FLIGHT 4021 WAS APPROVED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITHOUT ANY FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001101000064 20011010 00064 NM 2001 10 10 VNAA0109008 1 20010914 A 7712 311835602 SIGNAL COND UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA K NONE N FALSE WARNING DE DESCENT 1 GL 07 438JS 12598 3056 DURING DESCENT, THE LEFT HAND ENGINE TORQUE WAS 35 PERCENT THEN JUMPED TO AN INDICATED 85 PERCENT. FLIGHT 4012 CONTINUE D AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE TORQUE SIGNAL CONDITIONER IN ACCORDANCE W ITH DORNIER MAINTENANCE MANUAL 77-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001101000065 20011010 00065 2001 10 10 VNAA0109010 4 20010916 A 3460 COMPUTER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE E/E BAY MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 442JS 3060 DURING TAKEOFF, THE CREW RECEIVED A FLIGHT GUIDANCE COMPUTER FAIL MESSAGE AND ABORTED TAKEOFF. AS FLIGHT 4065 EXITED TH E RUNWAY THE MESSAGE CLEARED. THE CREW CONTACTED MAINTENANCE CONTROL AND CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4 065 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001101000066 20011010 00066 NM 2001 10 10 VNAA0109012 1 20010920 A 2435 8160121 STARTER GEN DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 426JS 11293 3038 AT APPROXIMATELY 60 KNOTS THE CREW RECEIVED A LEFT HAND GENERATOR FAIL MESSAGE AND ABORTED TAKEOFF. MAINTENANCE INSPECT ED AND REPLACED THE STARTER GENERATOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE P ERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001101000067 20011010 00067 EU 2001 10 10 SIMA200123404 1 20010814 A 5300 7253710459 TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 343SB 340B343 SBP - DURING MBV INSPECTION, MAINTENANCE FOUND THE RIGHT GALLEY TRACK IS CORRODED. REMOVED AND REPLACED GALLEY TRACK AN D PROFILE IAW SAAB SRM 51-40-40, 51-40-21, AND 51-40-22. (M) 2 L 7 2 4T RT A52EU 2001101000068 20011010 00068 EU 2001 10 10 SIMA200123405 1 20010814 A 5300 7253721427 BEAM SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 343SB 340B343 SBP - DURING MBV INSPECTION, MAINTENANCE FOUND THE LEFT GALLEY FLOOR FRAME AND INBOARD BRACKET CORRODED. REMOVED AND RE PLACED INTERCOSTAL AND L ANGLE IAW SAAB SRM 51-40-21. (M) 2 L 7 2 4T RT A52EU 2001101000069 20011010 00069 EU 2001 10 10 SIMA200123410 1 20010814 A 3200 725700067 LINK SAAB SF340 340B 7860101 EU RT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 343SB 340B343 DURING MBV INSPECTION, FOUND THE RIGHT MLG SUPPORT ASSEMBLY LINK IS CORRODED IN THE INBOARD HOLES. REMOVED AND REPLACED SUPPORT LINK IAW SAAB AMM 57-40-05. (M) 2 L 7 2 4T RT A52EU 2001101000070 20011010 00070 EU 2001 10 10 SIMA200123421 1 20010814 A 2700 7327200561 CARRIAGE SAAB SF340 340B 7860101 EU COCKPIT CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 343SB 340B343 SBP - DURING MBV INSPECTION MAINTENANCE, FOUND THE LEFT RUDDER PEDAL CONSOLE CARRIAGE CORRODED. MAINTENANCE REMOVED AND REPLACED THE LEFT CARRIAGE IAW SAAB MM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001101000071 20011010 00071 2001 10 10 SWIA200110228 4 20011006 A 2220 TRIM SWITCH CNDAIR CL600 CL6002B19 EA FIRST OFFICER MALFUNCTIONED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 413SW 7102 STAB TRIM AND MACH TRIM DISCONNECTED IN FLIGHT. FOLLOWED QRH. ABOUT 1 MINUTE LATER, DISCONNECTED AGAIN AND WOULD NOT R ESET. RETURNED TO SLC AND FOLLOWED QRH.FOUND BAD TRIM SWITCH ON FO'S YOKE. R&R SWITCH IAW 27-41-05. OPS CHECK GOOD. SELF TEST OF HSTCU OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2001101000072 20011010 00072 EA 2001 10 10 M01092 1 20010818 A 3300 1317 BULB BRUCE CNDAIR CL600 CL6002B19 EA GE CF34 CF34* NE LT BULB/FWD O/W2 FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SO 07 27172 7172 DURING ROUTINE MAINTENANCE, THE CREW FOUND THE RIGHT HAND FORWARD NR 2 OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANC E REPLACED THE LIGHT BULB AND OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2001101000073 20011010 00073 NM 2001 10 10 VNAA0109016 1 20010925 A 3150 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 422JS 3018 POWER WAS ADVANCED FOR TAKEOFF AND THE CREW RECEIVED A TAKEOFF CONFIGURATION WARNING ON THE RED WARNING PANEL. THE CREW ABORTED TAKEOFF AND WHEN TAXIING FROM THE RUNWAY THE LIGHT EXTINGUISHED AND FLIGHT 9407 RETURNED TO THE GATE FOR ANOTHE R DEPARTURE INFORMATION. FLIGHT 9407 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001101000074 20011010 00074 SO 2001 10 10 M01097 1 20010827 A 3300 3025101 FABRIC EMB 145 EMB145LR SO ALLSN AE3007 AE3007C GL RT RR EM FLD LT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SO 01 825MJ 145179 DURING A PREFLIGHT INSPECTION, THE CREW FOUND THE RIGHT AFT FUSELAGE EXTERNAL EMERGENCY FLOOD LIGHT INOPERATIVE. THIS I TEM WAS DEFERRED PER MEL. LATER MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOD LIGHT. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2001101000075 20011010 00075 NM 2001 10 10 VNAA0109017 1 20010926 A 3620 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 438JS 3056 AT 50 KNOTS THE CREW RECEIVED A BLEED VALVE SHUT OFF AND APU SHUT OFF VALVE CAS MESSAGE AND ABORTED TAKEOFF. AS THE CRE W CLEARED THE RUNWAY THE MESSAGE CLEARED AND FLIGHT 4177 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4177 THEN DEPA RTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001101000076 20011010 00076 NE 2001 10 10 C2XA01IA368 2 20011007 A 7200 PCW121TM ENGINE AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE NR 2 UNSERVICEABLE A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 26826 172 GPT- FLIGHT 3397, AFTER LEAVING THE GATE,THE CREW NOTED SMOKE IN THE CABIN, RETURNED TO THE GATE. THE AIRCRAFT WAS RELE ASED IAW MEL. THE AIRCRAFT WAS INSPECTED AND RELEASED FOR FERRY FLIGHT FROM GPT TO IAH. MAINTENANCE REMOVED AND REPLACED THE NUMBER 2 ENGINE, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI CE. 2 H 7 2 4T 4 T RT A53EU E20NE 2001101000077 20011010 00077 SO 2001 10 10 C2XA01TY124 1 20010930 A 2621 336000575 LENS EMB 145 EMB145LR SO FIRE BOTTLE MISSING A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 7362 7362 145103 TYS DURING A SCHEDULE INSPECTION THE LEFT ENGINE FIRE BOTTLE GAUGE, LENS IS MISSING. MAINTENANCE REMOVED AND REPLACED T HE FIRE BOTTLE IAW EMB 145 AMM 26-21-02. REPAIR WAS SATISFACTORY, AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTIO N. 2 L 7 2 4T RT T00011AT 2001101000078 20011010 00078 SO 2001 10 10 C2XA01TY125 1 20010930 A 2621 301000505 GAUGE EMB 145 EMB145LR SO FIRE BOTTLE UNSERVICEABLE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 7362 7362 145103 TYS DURING A SCHEDULE INSPECTION THE APU ENGINE FIRE BOTTLE GAUGE IS UNREADABLE. MAINTENANCE REMOVED AND REPLACED THE F IRE BOTTLE IAW EMB 145 AMM 26-22-01. REPAIR WAS SATISFACTORY, AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2001101000079 20011010 00079 SO 2001 10 10 C2XA01TY126 1 20011002 A 3350 1317 LIGHT EMB 145 EMB145 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15973 145159 TYS DURING A SCHEDULED INSPECTION THE LEFT HAND OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE LIGHT BULB IN THE LEFT HAND OVERWING EMERGENCY LIGHT ASSY IAW EMB-145 MM 33-50-10, OPERATIONAL CHEC KS WERE SATISFACTORY. 2 L 7 2 4F RT T00011AT 2001101000080 20011010 00080 EA 2001 10 10 M010195 1 20010817 A 3300 BC100200004 LIGHT CNDAIR CL600 CL6002B19 EA GE CF34 CF34* NE EM CABIN FLD LT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 01 17156 7156 ON A PREFLIGHT INSPECTION, THE CREW NOTED THAT THE NR1 AFT CABIN EMERGENCY LIGHT WAS OPERATIVE. THIS ITEM WAS DEFERRED PER MEL. ON 8/20, MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT. 2 L 7 2 4F 4 F RT A21EA E15NE 2001101000081 20011010 00081 SO 2001 10 10 C2XA01TY127 1 20011002 A 3350 7287580505 LIGHT EMB 145 EMB145 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15973 145159 TYS DURING A SCHEDULED INSPECTION THE MOST FORWARD SECTION OF THE CABIN EMERGENCY ISLE PATH LIGHTING STRIP WAS INOPERAT IVE. MAINTENANCE REMOVED AND REPLACE THE FORWARD EMERGENCY ISLE PATH LIGHT STRIP IAW EMB-145 MM 33-50-08, OPERATIONAL C HECKS WERE SATISFACTORY. 2 L 7 2 4F RT T00011AT 2001101000082 20011010 00082 SO 2001 10 10 C2XA01TY129 1 20011008 A 5330 14571620401 PANEL EMB 145 EMB145LR SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 16961 TYS DURING A SCHEDULED INSPECTION CORROSION WAS NOTED ON PANELS 192JR AND PANEL 192HL. MAINTENANCE REMOVED AND REFINIS HED 192JR AND 192HL IAW EMB 145 AMM 51-14-003 AND 51-20-00.THE WORK IS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UP ON COMPLETION OF THE SCHEDULED INSPECTION. 2 L 7 2 4T RT T00011AT 2001101000085 20011010 00085 SO 2001 10 10 C2XA01TY153 1 20011010 A 5312 14526850001 FIREWALL EMB 145 EMB145 SO APU GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS DURING A SCHEDULED INSPECTION A GOUGE WAS FOUND IN THE APU FIREWALL AFFECTING A PREVIOUS REPAIR. MAINTENANCE REMOV ED ORIGINAL REPAIR AND ACCOMPLISHED THE INSERT/DOUBLER REPAIR IAW EMBRAER GST-3315A/01 AND SRM 53-32-13. THE REPAIR WAS SATISFACTORY, AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001101000086 20011010 00086 NM 2001 10 10 QXEA0101597 1 20010927 A 5412 FIREWALL DHAV DHC8 DHC8202 2809007 NM LT PYLON CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - AFT FIREWALL IS CRACKED AT TOP INBOARD SIDE APPROXIMATELY 3" LONG ON NUMBER ONE SIDE. REPAIRED IAW RD8-54-806 2 H 7 2 4T RT A13NM 2001101000087 20011010 00087 NM 2001 10 10 QXEA0101598 1 20010928 A 5412 FIREWALL DHAV DHC8 DHC8202 2809007 NM PYLON CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - AFT FIRE WALL IS CRACKED AT CONNECTING CLIP ON TOP INBOARD SIDE. REPAIRED IAW RD8-54-109 2 H 7 2 4T RT A13NM 2001101000088 20011010 00088 EU 2001 10 10 QXEA0101599 1 20010928 A 3350 6008903 POWER SUPPLY FOKKER F28 F28MK4000 4990810 EU CARGO BAY DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US 10485 10485 11161 PDX - AFT EXTERIOR FAIRING EMERGENCY LIGHTS DID NOT ILLUMINATE. REMOVED AND REPLACED AFT CARGO BATTERY POWER SUPPLY UNIT FOR EVACUATION LIGHTS. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001101100001 20011011 00001 EU 2001 10 11 2001F00398 1 20010814 A 5347 7253721495 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 343SB 340B343 SBP - DURING MBV INSPECTION, MAINTENANCE FOUND THE RIGHT GALLEY TRACK IS CORRODED. REMOVED AND REPLACED GALLEY TRACK AN D PROFILE IAW SAAB SRM 51-40-40, 51-40-21, AND 51-40-22. REF SIMA200123404. (M) 2 L 7 2 4T RT A52EU 2001101100002 20011011 00002 EU 2001 10 11 2001F00399 1 20010814 A 5320 7253721447 INTERCOSTAL SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 343SB 340B343 SBP - DURING MBV INSPECTION, MAINTENANCE FOUND THE LEFT GALLEY FLOOR FRAME AND INBOARD BRACKET CORRODED. REMOVED AND RE PLACED INTERCOSTAL AND L ANGLE IAW SAAB SRM 51-40-21. REF SIMA200123405. (M) 2 L 7 2 4T RT A52EU 2001101100003 20011011 00003 CE 2001 10 11 2001F00400 1 20010915 A 7931 1013890235 TRANSDUCER BEECH 1900 1900D 1154162 CE LT ENGINE FAILED A GUUA K NONE P NO WARNING INDICATION CL CLIMB 1 SO 19 81533 UE137 FLT 9134 - FLL - AFTER TAKEOFF, LEFT ENGINE OIL PRESSURE DROPPED TO ZERO WITH NO ANNUNCIATOR INDICATION. REMOVED AND RE PLACED NR 1 ENGINE OIL PRESSURE TRANSDUCER. OPS AND LEAK CHECKS NORMAL. (M) 2 L 7 2 4T RT A24CE 2001101100004 20011011 00004 CE 2001 10 11 2001F00401 1 20010910 A 3230 PRINTED CKT BOAR BEECH 1900 1900D 1154162 CE E/E BAY UNSECURE A GUUA O OTHER J WARNING INDICATION CL CLIMB 1 SO 19 49543 UE181 FLT 9511 - MIA-FLL - AFTER TAKEOFF, LANDING GEAR FAILED TO STOW COMPLETELY. SECURED PCBA316. OPERATIONAL CHECK OF LAND ING GEAR EXTENSION AND RETRACTION NORMAL. (M) 2 L 7 2 4T RT A24CE 2001101100005 20011011 00005 NM 2001 10 11 NOCA0301 1 20010907 A 2500 5A30863 SLIDE BOEING 737 7378Q8 13844BX NM A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 800NA 28215 DOOR R1 SLIDE FOUND PARTIALLY UNRAVELED DURING INSPECTION. SLIDE REMAINED IN BUSTLE AND DID NOT DEPLOY. REPLACED DOOR R1 SLIDE. (M) 2 L 7 2 4F RT A16WE 2001101100006 20011011 00006 NM 2001 10 11 AALA20011596 1 20010805 A 3350 WIRE BOEING 727 727227 1384078 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 731AA 20738 RDU - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT SEAT 16 THROUGH 18 INOPERATIVE. REPAIRED BROKEN WIR E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001101100007 20011011 00007 CE 2001 10 11 2001F00402 1 20010830 A 2730 5052453421 INDICATOR BEECH 1900 1900D 1154162 CE COCKPIT WORN A GUUA O OTHER O OTHER CR CRUISE 1 SO 19 81533 UE137 FLT 9389 - MIA/FLL - DURING FLIGHT, ELEVATOR TRIM WHEEL POSITION INDEX MARKER DOES NOT CORRESPOND TO TRIM SETTINGS. REM OVED AND REPLACED ELEVATOR TRIM DIAL INDICATOR ASSEMBLY AND INDEXED. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4T RT A24CE 2001101100008 20011011 00008 NM 2001 10 11 2001F00403 1 20010812 A 7920 M832481011 LINE BOEING 727 727134C 138404H NM NR 1 ENGINE LOOSE A RYNA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 07 424EX 20042 DURING CRUISE FLIGHT, NR 1 ENGINE OIL QUANTITY WENT TO ZERO. LOW OIL PRESSURE LIGHT ILLUMINATED WITH LOSS OF OIL PRESSU RE. COMPLIED WITH ENGINE SHUTDOWN CHECKLIST. EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND NR 1 EN GINE OIL BYPASS LINE LOOSE. REPLACED O-RINGS AND RESECURED LINE. LEAK CHECK AND OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 2001101100009 20011011 00009 NM 2001 10 11 2001F00404 1 20010726 A 5711 SPAR BOEING 727 72721 1384003 NM CENTER WING CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 355QS 19257 WING CENTER SECTION INTERNAL AFT SPAR WEB BULGED IN AREA OF UPPER SPAR CHORD BL 22L DUE TO CORROSION. INSTALLED WING CE NTER SECTION AFT SPAR WEB REPAIR AT STATION 870 BETWEEN LBL 17.2 AND LBL 25.9 IAW AVITAS ENGINEERING REPAIR ORDER AVHM-2 37RO-1 REV 1R DATED 07/24/2001, 8110-3 DATED JULY 24, 2001 ISSUED. MATERIAL LOSS WAS WITHIN LIMITS. (M) 2 L 7 3 4F A3WE 2001101100010 20011011 00010 NM 2001 10 11 2001F00406 1 20010701 A 5320 ATTACH ANGLE BOEING 727 72721 1384003 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 355QS 19257 FUSELAGE AIRCRAFT BAY AREA FS 758 LBL 7 BELLY FAIRING SUPPORT BRACKET ATTACH ANGLE IS CRACKED. REPLACED BELLY FAIRING S UPPORT BRACKET ATTACH ANGLE AT FUSELAGE, AIRCRAFT BAY FS 758 LBL 7 PER AVIATS ENGINEERING DRAWING AVHM 232D-1. (M) 2 L 7 3 4F A3WE 2001101100011 20011011 00011 NM 2001 10 11 2001F00407 1 20010720 A 5210 DOOR FRAME BOEING 727 72721 1384003 NM ENTRY DOOR CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 355QS 19257 MAIN ENTRY DOOR INNER SURFACE AT UPPER TORQUE TUBE AFT AREA, FOUND FRAME AND WEB WITH HEAVY CRACK DAMAGES. INSTALLED RE PAIR ON MAIN ENTRY DOOR INNER SURFACE AT UPPER TORQUE TUBE AFT AREA OF FRAME IAW AVITAS ENGINEERING ORDER AVHS 241-R0-1 REV 1. (M) 2 L 7 3 4F A3WE 2001101100012 20011011 00012 NM 2001 10 11 2001F00408 1 20010725 A 5314 KEELBEAM BOEING 727 72721 1384003 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 355QS 19257 KEEL BEAM WEB CRACKED AT AFT HINGE ATTACH POINT OF SAFETY BAR NEAR BS 930, LEFT WHEEL WELL. INSTALLED KEEL BEAM WEB REP AIR AT AFT HINGE ATTACH POINT OF SAFETY BAR NEAR BS 930 LEFT WHEEL WELL IAW SRM 51-40-2. (M) 2 L 7 3 4F A3WE 2001101100013 20011011 00013 EA 2001 10 11 COMA0160789 1 20011008 A 2750 855D1005 BPSU CNDAIR CL600 CL6002B19 EA L/H MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS LD LANDING 1 SO 01 948CA 14114 7079 FLIGHT #5431. FLAPS FAILED AT 39 DEGREES.REPLACED THE L/H BPSU. 2 L 7 2 4F RT A21EA 2001101100014 20011011 00014 EA 2001 10 11 COMA0160790 1 20011008 A 3350 363782 LAMP CNDAIR CL600 CL6002B19 EA CABIN FLOOR INOPERATIVE A COMA O OTHER L NO TEST IN INSP/MAINT 1 SO 01 983CA 7169 FLIGHT #5832. EMERGENCY FLOOR PATH LIGHTING IS INOP ROWS 2 THRU 6.REPLACED THE #2 FLOOR LIGHT STRIP. 2 L 7 2 4F RT A21EA 2001101100015 20011011 00015 EA 2001 10 11 COMA0160791 1 20011008 A 2420 755469D IDG CNDAIR CL600 CL6002B19 EA L/H ENG FAILED A COMA C ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 SO 01 958CA 450 7111 FLIGHT #6080. IDG #1 AND GENERATOR #1 CAUTION DURING T/O. ABORTED T/O.REPLACED THE #1 IDG 2 L 7 2 4F RT A21EA 2001101100016 20011011 00016 NM 2001 10 11 2001F00411 1 20010817 A 5320 FLOOR SUPPORT BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND CORROSION ON COCKPIT FLOOR SUPPORT PANEL FROM BS 259.5 TO BS 282.5 AT LBL 8 INCHES. REMOVED FLOOR SUPPORT SECTION BETWEEN BS 259.5 TO 282.5. INSTALLED NEW SECTION IAW B727 SRM 51-30-2. (M) 2 L 7 3 4F A3WE 2001101100017 20011011 00017 NM 2001 10 11 2001F00412 1 20010731 A 5320 FLOOR SUPPORT BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND CORROSION ON COCKPIT FLOOR SUPPORT PANELS FROM BS 257.5 TO BS 312 AT LBL 13 INCHES. REMOVED CORROSION BETWEEN STA TION 259.5-278 AND STATION 294-312 IAW B727 SRM 51-10-5. MATERIAL LOSS WITHIN LIMITS AS PER B727 SRM 55-10-1. TREATED AND PRIMED PER B727 SRM 51-10-2. REPLACED SECTION AT STATION 278-294 LBL 13 INCHES. (M) 2 L 7 3 4F A3WE 2001102200060 20011022 00060 EU 2001 10 22 RAIA00110002 1 20011001 A 3010 3D354701 PRESSURE SWITCH JETAIR JETSTM JETSTM4101 1500501 EU DE-ICE SYS FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 562HK 12055 41078 5384-RIC-AIRFRAME DE-ICE FAULT CCT 2. REMOVED AND REPLACED THE CCT 2 DE-ICE PRESSURE SWITCH. 2 L 7 2 4T RT A41NM 2001101100018 20011011 00018 NM 2001 10 11 CALA0100939 1 20011010 A 5320 SILL BOEING 737 7373T0 1384582 NM STA 767-787 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 INSPECTION FOUND AFT BAGGAGE BIN FORWARD LOWER SILL CORRODED AT STA 767-787, S26R. THE SILL WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001101100019 20011011 00019 NM 2001 10 11 2001F00409 1 20010822 A 5714 CLIP BOEING 727 72721 1384003 NM WING CENTER BOX CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 WING CENTER SECTION INTERIOR REAR SPAR UPPER CHORD ATTACH CLIP (SMALL ANGLE) CRACKED AT BS 870 AND BBL 0. REMOVED AND R EPLACED ATTACH CLIP IN WING CENTER SECTION INTERIOR REAR SPAR UPPER CHORD BS 870 AND BBL 0 AS PER B727 SRM 51-30-2. (M) 2 L 7 3 4F A3WE 2001101100020 20011011 00020 NM 2001 10 11 2001F00410 1 20010817 A 5320 FLOOR SUPPORT BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 CORRODED COCKPIT FLOOR SUPPORT ANGLE AT BS 295 RBL 10 INCHES. REMOVED CORRODED FLOOR SUPPORT AT BS 295 RBL 10 INCHES IA W B727 SRM 51-30-2. REMOVED CORROSION AND TREATED IAW B727 SRM 51-10-2 AND B727 SRM 51-10-6. INSTALLED NEW FLOOR SUPPO RT IAW B727 SRM 51-30-2. (M) 2 L 7 3 4F A3WE 2001101100021 20011011 00021 EA 2001 10 11 COMA0160793 1 20011004 A 2750 854D10012 ACTUATOR CNDAIR CL600 CL6002B19 EA R/H OUTBD FAILED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 785CA 4877 7326 FLIGHT 5420. FLAPS FAILED AT 23 DEGREES DURING LANDING APPROACH. POST FLIGHT INSP. FOUND R/H OUTBD FLAP TWISTED.REPLACED THE R/H OUTBD FLAP, BOTH FLAP ACTUATORS AND THE FLEX DRIVE SHAFT. 2 L 7 2 4F RT A21EA 2001101100022 20011011 00022 NM 2001 10 11 AALA20011301 1 20010614 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 725AA 20732 TUL - FOUND EMERGENCY EXIT LIGHT INOPERATIVE. AFT VAULT DOOR OVERHEAD LIGHT. REPLACED EXIT LIGHT E58 NR 3934056, MM 33 -50-101-2. (M) 2 L 7 3 4F A3WE 2001101100023 20011011 00023 NM 2001 10 11 AALA20011335 1 20010702 A 3350 1001141 LIGHT BOEING 727 727223 1384074 NM AFT AIRSTAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 861AA 21088 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AS SEMBLY AT AFT AIRSTAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001101100024 20011011 00024 EU 2001 10 11 AALA20011439 1 20010718 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1400H 11340 ORD - DURING OVERNIGHT MAINTENANCE, TEN EMERGENCY EXIT AISLE LIGHTS IN FIRST CLASS CABIN INOPERATIVE. REPLACED EMERGENC Y EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001101100025 20011011 00025 EU 2001 10 11 AALA20011441 1 20010718 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1400H 11340 ORD - DURING OVERNIGHT MAINTENANCE, ELEVEN EMERGENCY EXIT AISLE LIGHTS IN MID CABIN INOPERATIVE. REPLACED EMERGENCY EXI T LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001101100026 20011011 00026 NM 2001 10 11 AALA20011469 1 20010723 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 882AA 21521 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD FLOOR EMERGENCY EXIT PATH LIGHTING INOPERATIVE. REATTACHED WIRE TO FLOOR EM ERGENCY EXIT PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001101100027 20011011 00027 NM 2001 10 11 AALA20011488 1 20010723 A 3350 SIGN BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 860AA 21087 DFW - DURING OVERNIGHT MAINTENANCE, LEFT AFT SERVICE DOOR EXIT SIGN INOPERATIVE. REPLACED LEFT AFT SERVICE DOOR EXIT SI GN ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001101100028 20011011 00028 EU 2001 10 11 AALA20011494 1 20010724 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1458H 11478 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT TRACK LIGHTING SEGMENT AT FORWARD ENTRY DOORS HAS SEVERAL LAMPS INOPE RATIVE. REPLACED EMERGENCY EXIT TRACK LIGHTING LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001101100029 20011011 00029 EU 2001 10 11 AALA20011499 1 20010723 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1402K 11353 DFW - DURING OVERNIGHT MAINTENANCE, SEVERAL LEFT WING AFT ESCAPE HATCH EXIT LIGHTS BURNED OUT. REPLACED FUSED LAMPS AT LEFT WING AFT ESCAPE HATCH EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001101100030 20011011 00030 EU 2001 10 11 AALA20011500 1 20010723 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1402K 11353 DFW - DURING OVERNIGHT MAINTENANCE, SEVERAL LEFT WING FORWARD ESCAPE HATCH EXIT LIGHTS BURNED OUT. REPLACED FUSED LAMPS AT LEFT WING FORWARD ESCAPE HATCH EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001101100031 20011011 00031 EU 2001 10 11 AALA20011501 1 20010723 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1402K 11353 DFW - DURING OVERNIGHT MAINTENANCE, SEVERAL RIGHT WING FORWARD ESCAPE HATCH EXIT LIGHTS BURNED OUT. REPLACED FUSED LAMP S AT RIGHT WING FORWARD ESCAPE HATCH EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001101100032 20011011 00032 EU 2001 10 11 AALA20011502 1 20010723 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1402K 11353 DFW - DURING OVERNIGHT MAINTENANCE, SEVERAL RIGHT WING AFT ESCAPE HATCH EXIT LIGHTS BURNED OUT. REPLACED FUSED LAMPS AT RIGHT WING AFT ESCAPE HATCH EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001101100033 20011011 00033 EU 2001 10 11 AALA20011503 1 20010723 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1402K 11353 DFW - DURING OVERNIGHT MAINTENANCE, SEVERAL MID CABIN CEILING MOUNTED EMERGENCY EXIT LIGHTS BURNED OUT. REPLACED FUSED LAMPS IN MID CABIN CEILING MOUNTED EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001101100034 20011011 00034 EU 2001 10 11 AALA20011504 1 20010723 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU COCKPIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1402K 11353 DFW - DURING OVERNIGHT MAINTENANCE, SEVERAL COCKPIT ENTRY EMERGENCY EXIT LIGHTS BURNED OUT. REPLACED FUSED LAMPS IN COC KPIT ENTRY EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001101100035 20011011 00035 EU 2001 10 11 AALA20011505 1 20010723 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1402K 11353 DFW - DURING OVERNIGHT MAINTENANCE, SEVERAL FORWARD ENTRY DOOR EMERGENCY EXIT LIGHTS BURNED OUT. REPLACED FUSED LAMPS A T FORWARD ENTRY DOOR EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001101100036 20011011 00036 SO 2001 10 11 LR7A01079 1 20011009 A 5311 3590913R CAP LKHEED 382 382G 526414U SO FS 924 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC5330 FOUND FS 924 FRAME CAP CRACKED AT RBL 61, WL 200.REPLACED FRAME CAP P ER DWG 359091 & SRM SMP 583-51-70. NR 0013. 2 H 7 4 4T A1SO 2001101100037 20011011 00037 SO 2001 10 11 LR7A01082 1 20011009 A 5343 3897271 FORGING LKHEED 382 382G 526414U SO FS 517 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC3208 FOUND FS 517 LMLG BEAM REINFORCING PLATE CRACKED AT LBL 65, WL 146.RE PLACED REINFORCING PLATE PER SRM SMP 583-51-70. NR 0171. 2 H 7 4 4T A1SO 2001101100038 20011011 00038 SO 2001 10 11 LR7A01083 1 20011009 A 5350 STRUT LKHEED 382 382G 526414U SO FS 523 ELONGATED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC3209 FOUND RMLG WL 200 LONGERON 2 EA. ELONGATED HOLES AT FS 523, RBL 75.RE PAIRED IAW LAC MEA 382-53-01-061. NR 0211. 2 H 7 4 4T A1SO 2001101100039 20011011 00039 SO 2001 10 11 LR7A01086 1 20011009 A 5312 WEB LKHEED 382 382G 526414U SO FS 518-528 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC3208 FOUND FS 518 - 528 WEB CORRODED AT LBL 62, WL 146.REPAIRED IAW SRM SM P 583-51-140-17. NR 0285. 2 H 7 4 4T A1SO 2001101100040 20011011 00040 SO 2001 10 11 LR7A01087 1 20011009 A 5343 3897311 CAP LKHEED 382 382G 526414U SO FS 517 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC3208 FOUND FS 517 BEAM ASSY CRACKED AT UPPER INBD SHELF BRACKET HOLE, LBL 62, WL 144.REPLACED FS 517 BEAM OUTER & INNER CAPS PER DWG 3312869 & SRM SMP 583-51-70. NR 0287. 2 H 7 4 4T A1SO 2001101100041 20011011 00041 SO 2001 10 11 LR7A01088 1 20011009 A 5311 WEB LKHEED 382 382G 526414U SO FS 924 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION PER JOB CARD HSP5330 FOUND FS 924 RH WEB CRACKED AT RBL 61, WL 250.REPLACED WEB PER DWG 3 59091 & SRM SMP 583-51-70. NR 0299. 2 H 7 4 4T A1SO 2001101100042 20011011 00042 SO 2001 10 11 LR7A01089 1 20011009 A 5343 38850411 CAP LKHEED 382 382G 526414U SO FS 528 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC3208 FOUND FS 528 LMLG BEAM OUTER CAP CRACKED AT LBL 66, WL 208.REPLACED O UTER CAP PER DWG 388504 & SRM SMP 583-51-70. NR 0306. 2 H 7 4 4T A1SO 2001101100043 20011011 00043 SO 2001 10 11 LR7A01090 1 20011009 A 5311 3590913L CAP LKHEED 382 382G 526414U SO FS 924 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION PER JOB CARD HSP5330 FOUND FS 924 FRAME CAP CRACKED AT LBL 61, WL 146.REPLACED CAP PER DW G 359091 & SRM SMP 583-51-70. NR 0310. 2 H 7 4 4T A1SO 2001101100044 20011011 00044 SO 2001 10 11 LR7A01091 1 20011009 A 5311 FRAME LKHEED 382 382G 526414U SO FS 330 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC05297 FOUND RH FS 330 FRAME CORRODED AT RBL 62, WL 146.REPAIRED IAW SRM SM P 583-51-140-21. NR 0313. 2 H 7 4 4T A1SO 2001101100045 20011011 00045 SO 2001 10 11 LR7A01092 1 20011009 A 5311 FRAME LKHEED 382 382G 526414U SO FS 425 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC05297 FOUND RH FS 425 FRAME CORRODED AT RBL 62, WL 146.REPAIRED IAW SRM SM P 583-51-140-21. NR 0314. 2 H 7 4 4T A1SO 2001101100046 20011011 00046 SO 2001 10 11 LR7A01093 1 20011009 A 5712 3338069 FITTING LKHEED 382 382G 526414U SO OWS 293 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION PER JOB CARD HSP57165 FOUND RH WING OWS 293 LOWER RIB FORMER FITTING CRACKED.REPLACED FIT TING PER DWG 371285, SRM SMP 583-51-70 & SB 382-57-75. NR 0381. 2 H 7 4 4T A1SO 2001101100047 20011011 00047 SO 2001 10 11 LR7A01094 1 20011009 A 5311 FRAME LKHEED 382 382G 526414U SO FS 410 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC05297 FOUND FS 410 RH FRAME CORRODED AT RBL 62, WL 146.REPAIRED IAW SRM SM P 583-51-140-21. NR 0382. 2 H 7 4 4T A1SO 2001101100048 20011011 00048 SO 2001 10 11 LR7A01095 1 20011009 A 5311 FRAME LKHEED 382 382G 526414U SO FS 320 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC05297 FOUND FS 320 RH FRAME CORRODED AT RBL 62, WL 146.REPAIRED IAW SRM SM P 583-51-140-21. NR 0383. 2 H 7 4 4T A1SO 2001101100049 20011011 00049 SO 2001 10 11 LR7A01096 1 20011009 A 5311 FRAME LKHEED 382 382G 526414U SO FS 380 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC05297 FOUND FS 380 RH FRAME CORRODED AT RBL 62, WL 146.REPAIRED IAW SRM SM P 583-51-140-21. NR 0384. 2 H 7 4 4T A1SO 2001101100050 20011011 00050 SO 2001 10 11 LR7A01097 1 20011009 A 5311 FRAME LKHEED 382 382G 526414U SO FS 340 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC05297 FOUND FS 340 RH FRAME CORRODED AT RBL 62, WL 146.REPAIRED IAW LAC ME A 382-53-01-062. NR 0398. 2 H 7 4 4T A1SO 2001101100051 20011011 00051 SO 2001 10 11 LR7A01098 1 20011009 A 5312 3761016L ANGLE LKHEED 382 382G 526414U SO FS 537 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION PER JOB CARD HSP5369 FOUND LMLG BAY FS 537 HORIZONTAL SHELF TO BOW BEAM ANGLE CORRODED AT LBL 68, WL 200.REPLACED ANGLE IAW SRM SMP 51-10. NR 0410. 2 H 7 4 4T A1SO 2001101100052 20011011 00052 SO 2001 10 11 LR7A01099 1 20011009 A 5312 3759441L SPLICE LKHEED 382 382G 526414U SO FS 617 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION PER JOB CARD HSP5335 FOUND FS 617 BULKHEAD SPLICE CRACKED AT LBL 20, WL 285.REPLACED SPLI CE PER DWG 375944 & SRM SMP 583-51-10. NR 0440. 2 H 7 4 4T A1SO 2001101100053 20011011 00053 SO 2001 10 11 LR7A01100 1 20011009 A 5712 3338069 FITTING LKHEED 382 382G 526414U SO OWS 293 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION PER JOB CARD HSP57165 FOUND LH WING OWS 293 LOWER RIB FORMER FITTING CRACKED.REPLACED FIT TING PER DWG 371285, SRM SMP 583-51-70 & SB 382-57-75. NR 0470. 2 H 7 4 4T A1SO 2001101100054 20011011 00054 SO 2001 10 11 LR7A01101 1 20011009 A 5312 37003264 SUPPORT LKHEED 382 382G 526414U SO FS 180.5 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC2560 FOUND FS 180.5 WEB AND SUPPORT CRACKED AT LBL 22, WL 168.REPLACED SUP PORT PER SB 382-53-51 AND REPAIRED WEB PER SB 382-53-51. NR 0479. 2 H 7 4 4T A1SO 2001101100055 20011011 00055 SO 2001 10 11 LR7A01102 1 20011009 A 5312 37003265 SUPPORT LKHEED 382 382G 526414U SO FS 180.5 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC2560 FOUND FS 180.5 WEB AND SUPPORT CRACKED AT RBL 22, WL 168.REPLACED SUP PORT PER SB 382-53-51 AND REPAIRED WEB PER SB 382-53-51. NR 0483. 2 H 7 4 4T A1SO 2001101100056 20011011 00056 SO 2001 10 11 LR7A01103 1 20011009 A 5330 SKIN LKHEED 382 382G 526414U SO FS 740E GOUGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC5303 FOUND FS 740E RH AFT SKIN GOUGED DUE ROCK DAMAGE AT RBL 67, WL 154.RE PAIRED IAW SRM SMP 583-51-140-12. NR 0531. 2 H 7 4 4T A1SO 2001101100057 20011011 00057 SO 2001 10 11 LR7A01104 1 20011009 A 5330 SKIN LKHEED 382 382G 526414U SO FS 745E GOUGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC5303 FOUND FS 745E RH AFT SKIN GOUGED DUE ROCK DAMAGE AT RBL 73, WL 163.RE PAIRED IAW SRM SMP 583-51-140-12. NR 0531. 2 H 7 4 4T A1SO 2001101100058 20011011 00058 SO 2001 10 11 LR7A01105 1 20011009 A 5330 SKIN LKHEED 382 382G 526414U SO FS 802E GOUGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC5303 FOUND FS 802E RH AFT SKIN GOUGED DUE ROCK DAMAGE AT RBL RBL 71, WL 16 0.REPAIRED IAW SRM SMP 583-51-140-12. NR 0531. 2 H 7 4 4T A1SO 2001101100059 20011011 00059 SO 2001 10 11 LR7A01106 1 20011009 A 5330 SKIN LKHEED 382 382G 526414U SO FS 924 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION PER JOB CARD HSP5303 FOUND FS 924 LH SKIN CRACKED AT PREVIOUS REPAIR AT LBL 61, WL 200.RE PAIRED IAW SRM SMP 583-51-140-12. NR 0543. 2 H 7 4 4T A1SO 2001101100060 20011011 00060 SO 2001 10 11 LR7A01107 1 20011009 A 5230 CAP LKHEED 382 382G 526414U SO FS 999 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC05297 FOUND FS 999 AFT CARGO DOOR LOWER BEAM CAP CRACKED AT RBL 60.REPAIRE D IAW LAC MEA 53-01-064. NR 0547. 2 H 7 4 4T A1SO 2001101100061 20011011 00061 SO 2001 10 11 LR7A01108 1 20011009 A 5230 CAP LKHEED 382 382G 526414U SO FS 999 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC05297 FOUND FS 999 AFT CARGO DOOR LOWER BEAM CAP CORRODED AT LBL 60.REPAIR ED IAW LAC MEA 53-01-064. NR 0548. 2 H 7 4 4T A1SO 2001101100062 20011011 00062 SO 2001 10 11 LR7A01109 1 20011009 A 5343 3914793 STRAP LKHEED 382 382G 526414U SO FS 517 MISALIGNED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION NR 0287 ACCOMPLISHMENT FOUND FS 517 BEAM REINFORCING STRAP DOES NOT ALIGN WITH NEW BEAM.R EPLACED STRAP PER DWG 3313869 & SRM SMP 583-51-70. NR 0569. 2 H 7 4 4T A1SO 2001101100063 20011011 00063 SO 2001 10 11 LR7A01110 1 20011009 A 5312 3724651L BRACKET LKHEED 382 382G 526414U SO FS 528 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC3208 FOUND FS 528 LMLG BEAM OUTER CAP ATTACH BRACKET CORRODED AT LBL 66, W L 200.REPLACED BRACKET IAW SRM SMP 51-70. NR 0572. 2 H 7 4 4T A1SO 2001101100064 20011011 00064 SO 2001 10 11 LR7A01111 1 20011009 A 5330 SKIN LKHEED 382 382G 526414U SO FS 477 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC3209 FOUND FS 477 RMLG WHEEL WELL UPPER FWD SKIN PANEL CRACKED AT RBL 78, WL 206.REPAIRED IAW SRM SMP 583-53-40-09. NR 0089. 2 H 7 4 4T A1SO 2001101100065 20011011 00065 NM 2001 10 11 AALA20011506 1 20010724 A 3350 CONTACTOR BOEING 727 727223 1384074 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 861AA 21088 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS AT 27D AND FORWARD DIM. REPLACED BROKEN CONDUCTOR AT R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001101100066 20011011 00066 EU 2001 10 11 AALA20011508 1 20010723 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1402K 11353 DFW - DURING OVERNIGHT MAINTENANCE, SEVERAL GALLEY DOOR EMERGENCY EXIT LIGHTS BURNED OUT. REPLACED FUSED LAMPS AT GALLE Y DOOR EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001101100067 20011011 00067 EU 2001 10 11 AALA20011544 1 20010731 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1444N 11447 ORD - FLT 31 - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT FORWARD CABIN INOPERATIVE. REPLACED FORWARD CABIN EMERGENCY EXIT FLOOR PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001101100068 20011011 00068 EU 2001 10 11 AALA20011547 1 20010730 A 3397 CONNECTOR FOKKER F28 F28MK0100 4990807 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1459A 11479 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS SEATS 12D THROUGH 14D DIM. RECONNECTED LOOSE CONN ECTION AT SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001101100069 20011011 00069 EU 2001 10 11 AALA20011554 1 20010801 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1444N 11447 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT MID CABIN INOPERATIVE. REPLACED MID CABIN EME RGENCY EXIT FLOOR PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001101100070 20011011 00070 NM 2001 10 11 AALA20011557 1 20010803 A 3397 SCN001 CONNECTOR BOEING 727 727227 1384078 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 730AA 20737 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY FLOOR PATH LIGHTING FROM AFT TO FORWARD OF CABIN DIMMING. REPLACED DAMAGE D CONNECTOR AT SEAT 3E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001101100071 20011011 00071 NM 2001 10 11 AALA20011560 1 20010803 A 3397 SCN001 CONNECTOR BOEING 727 727223 1384074 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 873AA 21385 MIA - DURING OVERNIGHT MAINTENANCE, AFT ENTRY DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED BAD CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001101100072 20011011 00072 NM 2001 10 11 AALA20011561 1 20010803 A 3397 SCN001 CONNECTOR BOEING 727 727223 1384074 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 848AA 20989 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIGN BETWEEN L1 AND R1 DOOR INOPERATIVE. RECONNECTED EMERGENCY SIGN CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001101100073 20011011 00073 NM 2001 10 11 AALA20011562 1 20010803 A 3350 1001141 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 879AA 21391 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT OVERHEAD LIGHTING INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY. S YSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2002071000157 20020710 00157 EU 2002 7 10 AALA20011567 1 20010804 A 3350 P4010049 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1416A 11395 ORD - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS AT ROW 12 AND 17 INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001101100074 20011011 00074 EU 2001 10 11 AALA20011572 1 20010804 A 3350 PR010049 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1416A 11395 ORD - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY PATH LIGHTING AT ROW 12 AND ROW 17 INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001101100075 20011011 00075 NM 2001 10 11 AALA20011573 1 20010807 A 3350 BAT5019 BATTERY PACK BOEING 727 727223 1384074 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 870AA 21382 TUL - FOUND LEFT AND RIGHT FORWARD DOOR SLIDE LIGHTS FAILED 10 MINUTE CHECK. REPLACED FORWARD DOOR SLIDE LIGHT BATTERY PACK. (M) 2 L 7 3 4F A3WE 2001101100076 20011011 00076 NM 2001 10 11 AALA20011574 1 20010807 A 3350 BAT5018 BATTERY PACK BOEING 727 727223 1384074 NM FS 800 DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 870AA 21382 TUL - FOUND RIGHT FORWARD AND AFT OVERWING EXIT EMERGENCY LIGHTS FAIL 10 MINUTE CHECK. REPLACED OVERWING EMERGENCY EXIT SIGN BATTERY PACK. (M) 2 L 7 3 4F A3WE 2001101100077 20011011 00077 NM 2001 10 11 AALA20011575 1 20010807 A 3350 BATTERY PACK BOEING 727 727223 1384074 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 870AA 21382 TUL - FOUND CENTER AISLE OVERHEAD FORWARD AND AFT OVERWING AREA EMERGENCY EXIT LIGHTS FAIL 10 MINUTE CHECK. REPLACED AI SLE SIGN EMERGENCY EXIT BATTERY PACK. (M) 2 L 7 3 4F A3WE 2001101100078 20011011 00078 NM 2001 10 11 AALA20011580 1 20010803 A 3350 6012211 BATTERY PACK BOEING 727 727223 1384074 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 848AA 20989 TUL - AFT SLIDE LIGHTS INOPERATIVE, STATION 1143 EQUIP NR M983. REPLACED BATTERY PACK M983. (M) 2 L 7 3 4F A3WE 2001101100079 20011011 00079 NM 2001 10 11 AALA20011581 1 20010803 A 3350 1001141 LIGHT BOEING 727 727223 1384074 NM AIRSTAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 848AA 20989 TUL - FOUND AIRSTAIRS EMERGENCY EXIT LIGHT INOPERATIVE, STATION 1398. REPLACED LIGHT ASSEMBLY. (M) 2 L 7 3 4F A3WE 2001101100080 20011011 00080 NM 2001 10 11 AALA20011582 1 20010724 A 3350 1000679 LIGHT BOEING 727 727227 1384078 NM COCKPIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 716AA 20608 TUL - FOUND LIGHT WOULD NOT OPERATE IN ARM POSITION. REPLACED LIGHT ASSEMBLY. OPS CHECKED GOOD. (M) 2 L 7 3 4F A3WE 2001101100081 20011011 00081 NM 2001 10 11 AALA20011593 1 20010805 A 3350 0200333001 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 890AA 22006 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING IN AFT STAIRWELL INOPERATIVE. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001101100082 20011011 00082 EU 2001 10 11 AALA20011600 1 20010806 A 3350 P4010049 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1442E 11437 DFW - DURING OVERNIGHT MAINTENANCE, NR 2 CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHE CKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001101100083 20011011 00083 NE 2001 10 11 GAIA01310OP 2 20010927 A 7250 JT8D15 ENGINE PWA JT8D BOEING 727 727251 138408H NM PWA JT8 JT8D15 52051 NE NR 1 POSITION FAILED A GAIA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 07 278US 76281 4984 657394 21157 DURING CLIMBOUT THROUGH 22,500 FEET, NR 1 ENGINE EPR DROPPED TO APPROXIMATELY 1.6 PROCEEDED BY A LOAD THUMP. ENGINE WAS SHUT DOWN AND EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO AIRPORT AND LANDED WITHOUT ANY FURTHER DIFFICULTIES. I NSPECTED THE AIRCRAFT AND FOUND THAT THE NR1 ENGINE HAD FAILED. MAINTENANCE FERRIED THE AIRCRAFT TO AIRPORT FOR AN ENGI NE CHANGE. 2 L 7 3 4F 4 F A3WE E2EA 2001101100084 20011011 00084 EU 2001 10 11 AALA20011601 1 20010806 A 3350 P4010049 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1442E 11437 DFW - DURING OVERNIGHT MAINTENANCE, NR 3 CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED MID CABIN BATTERY PACK. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001101100085 20011011 00085 NM 2001 10 11 AALA20011602 1 20010806 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 866AA 21371 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY FLOOR PATH LIGHTING AT ROW 6 DAMAGED. REPLACED TRACK AND LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001101100086 20011011 00086 NM 2001 10 11 AALA20011735 1 20010821 A 2120 ODOR BOEING 767 767323 1385205 NM CABIN DETECTED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 376AN 25445 FLT 111 - FCO - LEFT BUSINESS CLASS LAV HAS A STRONG ODOR EITHER PETROLEUM BASED OR DETERGENT BASED. LEFT BUS CLASS LAV CLEARED AND SERVICED BY CBN SERVICE. NO FUEL SMELL DETECTABLE INFOR NOTED A/C OK FOR SERVICE. (M) 2 L 7 2 4F RT A1NM 2001101100087 20011011 00087 NM 2001 10 11 AALA20011738 1 20010910 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN CHAFED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 372AA 25199 LHR - FLT 121 - ELEC ARC REPORTED ABOVE SEAT 28HJ ALL READING LIGHTS IN AREA INOPERATIVE. APPROXIMATELY 30 MIN INTO FLI GHT, CABIN ATTENDANT AND PASSENGER REPORTED AN ELECTRICAL ARC/SPARK ORIGINATING FROM PSU/OVERHEAD BIN AT SEAT 28HJ. ALL READING LIGHTS ON RT CABIN INOPERATIVE. TEN MINUTES LATER THE REMAINING COACH CABIN READING LIGHTS BECAME INOPERATIVE. CARRIED OUT T/S AND FOUND PSS WIRING CHAFED AT OVERHEAD DECODER AT SEATS 28HJ DUE INCORRECT ROUTING OF WIRES ACCOMPLIS HED AIRWORTHY REPAIR TO PSS WIRING AND CARRIED OUT ALL CHECKS OK. (M) 2 L 7 2 4F RT A1NM 2001101100088 20011011 00088 SO 2001 10 11 ASAOA01150 1 20010829 A 3350 10130115 LIGHT EMB 120 EMB120 3260201 SO CABIN DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 242AS 120069 DURING SCHEDULED MAINTENANCE IN TXK, THE EMERGENCY LIGHTS AT SEAT 5A WERE FOUND DAMAGED. MAINTENANCE REMOVED AND REPLAC ED EMERGENCY EXIT SIGN AT SEAT 5A. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001101100089 20011011 00089 2001 10 11 ASAOA01152 4 20010831 A 2350 509111 CONTROL PANEL EMB 120 EMB120 3260201 SO COCKPIT DEFECTIVE A ASOA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 265AS 19899 120170 FLT 4026 - DURING FLIGHT ATL TO ILM, CREW REPORTED SMOKE IN THE COCKPIT. AIRCRAFT DIVERTED AND LANDED SAFELY IN FLO. C REW ADVISED MAINTENANCE THAT THE SMOKE WAS COMING FROM THE FIRST OFFICERS COMM CONTROL PANEL. MAINTENANCE REMOVED AND R EPLACED THE NR 2 AUDIO CONTROL PANEL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001101100090 20011011 00090 SO 2001 10 11 ASOA01149 1 20010827 A 2752 3082001007 ACTUATOR EMB 120 EMB120 3260201 SO T/E FLAP FAILED A ASOA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 11 237AS 120051 FLT 4112 - DURING TAKEOFF FROM ATL, CREW RECEIVED A FLAP ASYMMETRY INDICATION. CREW DECLARED AN EMERGENCY AND AIRCRAFT RETURNED TO ATL FOR A ZERO FLAP LANDING. MAINTENANCE TESTED FLAP ACTUATORS WITH BRAKE OUT BOX CHECK. BOTH LEFT AND RIG HT ACTUATORS FAILED. MAINTENANCE REMOVED AND REPLACED BOTH LEFT AND RIGHT NACELLE FLAP ACTUATORS. LEAK AND OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001101100091 20011011 00091 SO 2001 10 11 ASOA01151 1 20010831 A 5311 FRAME EMB 120 EMB120 3260201 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SW 21 273AS 120222 DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND AT FRAME 21, STRINGERS 18 LEFT TO 18 RIGHT. MAINTENANCE WILL PERF ORM REPAIR IAW ASA EO120-53-0166. THIS AIRCRAFT IS CURRENTLY IN C-CHECK. (M) 2 L 7 2 4T RT A31SO 2001101100092 20011011 00092 EA 2001 10 11 ASOA01154 1 20010828 A 5610 NP1393216 WINDSHIELD CNDAIR CL600 CL600* EA COCKPIT CRACKED A ASOA K NONE O OTHER DE DESCENT 1 SO 11 824AS 1297 7203 DURING DESCENT INTO DFW AT 25,000 FEET, THE FIRST OFFICERS WINDSHIELD CRACKED. AIRCRAFT LANDED IN DFW WITHOUT FURTHER I NCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT WINDSHIELD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001101100093 20011011 00093 SO 2001 10 11 C2XA01CL212 1 20011007 A 3241 38793500 SHUTOFF VALVE EMB 135 EMB135LR SO DEFECTIVE A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 17524 1329 145399 CLE FLIGHT 3283 THE CREW REPORTED AT SLOW SPEEDS THE BRAKES WOULD STICK,JERK,AND VIBRATE.MAINTENANCE INSPECTED AND REPLA CED THE OUTBOARD BRAKE SHUT OFF VALVE.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT TOOO11AT 2001101100094 20011011 00094 SO 2001 10 11 ASOA01155 1 20010923 A 3350 1317 LIGHT EMB 120 EMB120 3260201 SO CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 229AS 120042 FLT 4252 - DURING GROUND INSPECTION IN ATL, THE RIGHT FORWARD OVERWING EMERGENCY LIGHT WAS BURNED OUT. MAINTENANCE REMO VED AND REPLACED THE BURNED OUT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001101100095 20011011 00095 SO 2001 10 11 ASOA01156 1 20010904 A 3350 3071BPE LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 504AS 120278 DURING SCHEDULED MAINTENANCE IN MCN, THE FLOOR LIGHT TRACK HAD ONE RED LIGHT INOPERATIVE AT THE OVERWING EXIT. MAINTENA NCE REMOVED AND REPLACED THE INOPERATIVE FLOOR LAMP AT THE OVERWING EXIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SER VICE. (M) 2 L 7 2 4T RT A31SO 2001101100096 20011011 00096 NM 2001 10 11 GAIA01309 1 20010914 A 3350 1315 LIGHT BOEING 727 727222 1384073 NM COCKPIT INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 90AX 20040 DURING ROUTINE MAINTENANCE AT FWA, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT HAD ONE EACH BULB BURNED OUT. MAINTENANCE RELAMPED THE LIGHT BULB IN THE COCKPIT EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WA S RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001101100097 20011011 00097 NM 2001 10 11 KPVA200118 1 20010914 A 3350 10005511 LIGHT DHAV DHC8 DHC8103 1386005 NM COCKPIT INOPERATIVE A KPVA K NONE L NO TEST IN INSP/MAINT 1 WP 13 807WP 023 HNL - FLT 1132 - COCKPIT EMERGENCY PORTABLE LIGHT INOPERATIVE. REMOVED AND REPLACED PORTABLE EMERGENCY LIGHT ASSEMBLY. OPS CHECK GOOD IAW PSM 1-8-2 CH 33-51-00 PAGE 201-202. (M) 2 H 7 2 4T RT A13NM 2001101100098 20011011 00098 EU 2001 10 11 RAIA00110003 1 20011009 A 7997 1241012 TRANSMITTER JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE INOPERATIVE A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 574HK 59 41093 75082 7228-STL-LEFT ENGINE HIGH OIL PRESSURE. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE OIL PRESSURE TRANSMITTER. 2 L 7 2 4T 4 T RT A41NM E18NE 2001101100099 20011011 00099 NM 2001 10 11 KPVA200119 1 20010915 A 3350 6104789 POWER SUPPLY DHAV DHC8 DHC8103 1386005 NM CABIN DISCHARGED A KPVA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806WP 357 HNL - LEFT SIDE WALL EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY. SYSTEM OPS C HECKED GOOD. (M) 2 H 7 2 4T RT A13NM 2001101100100 20011011 00100 EU 2001 10 11 REXA01014 1 20010829 A 2150 12501511 MOTOR SAAB SF340 340B 7860101 EU AIR CONDITIONING OVERHEATED A REXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 25 367PX 2263 340B271 SMOKE IN CABIN. REMOVED AND REPLACED AFT FREON COMPRESSOR MOTOR. (M) 2 L 7 2 4T RT A52EU 2001101100101 20011011 00101 EU 2001 10 11 SIMA200123402 1 20010814 A 3211 7257500181 TRUNNION SAAB SF340 340B 7860101 EU LT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 343SB 340B343 SBP - DURING MBV INSPECTION MAINTENANCE, FOUND THE LEFT MAIN LANDING GEAR TRUNNION SUPPORT IS CORRODED IN THE BEARING SU PPORT HOUSING. REMOVED AND REPLACED TRUNNION SUPPORT HOUSING IAW SAAB AMM 57-40-05. (M) 2 L 7 2 4T RT A52EU 2001101100102 20011011 00102 2001 10 11 RAIA00110004 4 20011010 A 3442 MI5853505 RECEIVER AEROSP ATR42 ATR42300 8680920 EU INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 424TE 29079 915 124 7125-PIA- WEATHER RADAR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED WEATHER RADAR RECEIVER/TRANSMITTER. 2 H 7 2 4T RT A53EU 2001101100103 20011011 00103 EU 2001 10 11 SIMA200123403 1 20010814 A 5260 7253710871 TRACK SAAB SF340 340B 7860101 EU AIRSTAIR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 343SB 340B343 DURING MBV INSPECTION MAINTENANCE FOUND THE AIRSTAIR TRACK CORRODED. REMOVED AND REPLACED AIRSTAIR TRACK AND SUPPORT AN GLES IAW SAAB SRM 5140-21. (M) 2 L 7 2 4T RT A52EU 2001101100104 20011011 00104 EU 2001 10 11 SIMA200123406 1 20010814 A 5320 7253721439 WEB SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 343SB 340B343 SBP - DURING MBV INSPECTION, MAINTENANCE FOUND THE WEB REINFORCEMENT CORRODED AT STATION 294. REMOVED AND REPLACED WEB REINFORCEMENT IAW SAAB SRM 51-40-21. (M) 2 L 7 2 4T RT A52EU 2001101100105 20011011 00105 EA 2001 10 11 SWIA200110241 1 20011009 A 5240 ACCESS PANEL CNDAIR CL600 CL6002B19 EA NOSE DOOR OPEN A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 405SW 7029 LOUD SQUEAL COMING FROM RIGHT SIDE OF NOSE ON TAKEOFF. DIVERTED TO SLC.INSPECTED FORWARD PORTION OF A/C. FOUND FORWARD RIGHT SIDE NOSE DOOR ACCESS PANEL OPEN. NO DAMAGE. CHECKS GOOD. 2 L 7 2 4F RT A21EA 2001101100106 20011011 00106 EU 2001 10 11 SIMA200123407 1 20010814 A 5311 7253722001 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 343SB 340B343 SBP - DURING MBV INSPECTION, MAINTENANCE FOUND A PREVIOUS REPAIR AT STATION 258 FRAMES CORRODED. REMOVED AND FABRICATED NEW FRAMES IAW SAAB REPAIR STATEMENT 340 SDS002169. (M) 2 L 7 2 4T RT A52EU 2001101100107 20011011 00107 SO 2001 10 11 M01053 1 20010620 A 4900 14521330401 APU EMB EMB 145 EMB145LR SO OIL LEAK/AFT EQP LEAKING A MASA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 828MJ 828 145218 THE CREW FOUND SMOKE IN THE CABIN WITH THE PACKS ON. MAINTENANCE WAS CALLED AND FOUND OIL IN THE BLEED LINES FROM THE A PU. THE APU WAS DEFERRED AND THE BLEED VALVE CLOSED. ON 07/01/2001 MAINTENANCE REMOVED AND REPLACED THE APU UNIT. 2 L 7 2 4T RT T00011AT 2001101100108 20011011 00108 EU 2001 10 11 SIMA200123408 1 20010814 A 5320 7253711245 PLATE SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 343SB 340B343 SBP - DURING MBV INSPECTION, MAINTENANCE FOUND THE SEAT TRACK KICK PLATE AT BL 18.3 IS CORRODED IN THE RADIUS. REMOVED AND REPLACED KICK PLATE IAW SAAB SRM 51-40-21, AND 51-40-40. (M) 2 L 7 2 4T RT A52EU 2001101100109 20011011 00109 EU 2001 10 11 SIMA200123409 1 20010814 A 3211 7257500182 TRUNNION SAAB SF340 340B 7860101 EU RT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 343SB 340B343 SBP - DURING MBV INSPECTION MAINTENANCE, FOUND THE RIGHT MAIN LANDING GEAR TRUNNION SUPPORT IS CORRODED IN THE BEARING S UPPORT HOUSINGS. REMOVED AND REPLACED TRUNNION SUPPORT HOUSING IAW SAAB AMM 57-40-05. (M) 2 L 7 2 4T RT A52EU 2001101100110 20011011 00110 EU 2001 10 11 SIMA200123417 1 20010813 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 261AE 340B261 ABI - DURING MBV INSPECTION MAINTENANCE, FOUND CORROSION WAS FOUND ON FLOOR FRAME 258. CORROSION WAS REMOVED AND AREA W AS REPAIRED IAW SAAB REPAIR STATEMENT 340SDS002195. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001101100111 20011011 00111 EU 2001 10 11 SIMA200123422 1 20010814 A 5260 7253710871 TRACK SAAB SF340 340B 7860101 EU AIRSTAIR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 343SB 340B343 SBP - DURING MBV INSPECTION, MAINTENANCE FOUND THE AIRSTAIR TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE TRACK IAW SAAB MM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001101900006 20011019 00006 SO 2001 10 19 C2XA01IA370 1 20011008 A 3260 W608011424BL WIRE EMB 120 EMB120ER 3260203 SO RT MLG BROKEN A C2XA K NONE O OTHER CL CLIMB 1 SW 27 40717 120133 IAH-UPON TAKEOFF THE CREW NOTED THAT THE GEAR WOULD NOT RETRACT WITHOUT OVERRIDE USAGE. THE AIRCRAFT RETURNED TO IAH WI THOUT INCIDENT WHERE MAINTENANCE REPAIRED A WIRE ON THE RIGHT HAND AIR/GROUND PROX SWITCH. PERFORMED AN OPERATIONAL CHE CK OF THE LANDING GEAR SYSTEM, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001101200001 20011012 00001 EU 2001 10 12 DHL2001363025 1 20011010 A 2130 SELECTOR VALVE AIRBUS 300 A300B4203 3930306 EU CABIN PRESSURE MALFUNCTIONED A DHLA B A EMER. DESCENT UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 363DH 85 1) NR 2 PRESS SYSTEM OVERPRESSURIZED ON TAKEOFF REACHING 8 PSI. MAIN CABIN SMOKE DETECTORS ILLUMINATED, EMERGENCY PROC EDURES COMPLETED.2) REPLACED NR 2 CABIN PRESSURE SELECTOR IAW 21-31-12. OPS CHECKS GOOD ON GROUND.STATUS: CLOSED 2 L 7 2 4F RT A35EU 2001101200002 20011012 00002 EU 2001 10 12 DHL2001364026 1 20010926 A 5320 SMOKE BARRIER AIRBUS 300 A300B4203 3930306 EU CABIN CUT A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 1) SMOKE BARRIER HAS SEVERAL CUTS.2) R & R SMOKE BARRIER PER CMM (B/E AEROSPACE) SMOKE BARRIER 5MA1705-1 OK FOR SERV ICE.STATUS: CLOSED 2 L 7 2 4F RT A35EU 2001101200003 20011012 00003 EU 2001 10 12 DHL2001365038 1 20011003 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU CARGO BAY MALFUNCTIONED A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 365DH 149 1) CARGO SMOKE DETECTOR LIGHT ON MAIN CARGO DOOR SECOND LIGHT LEFT SIDE STAYS ILLUMINATED WHEN TESTED.2) COOL A/C WIT H EXTERNAL UNIT , TEST SMOKE DETECTOR LIGHTS ALL DETECTORS STAY OUT MM21-60-00.STATUS: CLOSED 2 L 7 2 4F RT A35EU 2001101200004 20011012 00004 EU 2001 10 12 DHL2001365039 1 20011003 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU CABIN MALFUNCTIONED A DHLA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 365DH 149 1) TAXING OUT OF THE BLOCKS MAIN DECK SMOKE DETECTORS WENT OFF IN POSITI-ON MID AND AFT AS WELL AS MWP SMOKE INDICATION .2) RUN ENG WITH PACKS ON TO COOL OFF MAIN CARGO AREA AFTER IT COOL DOWN ACCOMP SMOKE DETECTOR TEST GROUND OPS NORMAL MM-21-60-00.STATUS: CLOSED 2 L 7 2 4F RT A35EU 2001102300076 20011023 00076 EU 2001 10 23 DHL2001367015 1 20011002 A 2120 ODOR AIRBUS 300 A300B4203 3930306 EU CABIN DETECTED A DHLA B A EMER. DESCENT UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 01 367DH 265 SUSPECT SMOKE OR OIL FUMES FROM APU AIR. VISUALLY INSPECTED INSIDE OF APU DUCT FOR OIL RESIDUE NEXT TO FDR & CVR AFT OF BULK PIT. NO EVIDENCE OF OIL IN SUPPLY DUCT. OPERATED APU IAW JRH 19.1. NO SMOKE OR OIL FUMES NOTED. 2 L 7 2 4F RT A35EU 2001101200005 20011012 00005 EU 2001 10 12 DHL2001367016 1 20011002 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU CABIN MALFUNCTIONED A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 367DH 265 1) SMOKE LIGHT ILLUMINATED IN FLT.2) UNABLE TO DUPLICATE CONDITION AT THIS TIME ON GROUND SYSTEM OPS CHECKED GOOD PE R MM 26-16-0.STATUS: CLOSED. 2 L 7 2 4F RT A35EU 2001101200006 20011012 00006 NM 2001 10 12 CALA0100942 1 20011011 A 5330 SKIN BOEING 737 7373T0 1384582 NM L-1 WINDOW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69333 23571 INSPECTION FOUND A 1/2" CRACK IN L-1 WINDOW POST SKIN. THE CRACKED AREA OF SKIN WAS REMOVED AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-10-01. 2 L 7 2 4F RT A16WE 2001101200007 20011012 00007 NM 2001 10 12 DHL2001705006 1 20010928 A 3350 BATTERY BOEING 727 72722C 138400F NM CABIN DISCHARGED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 705DH 19191 1) EMERGENCY EXIT LIGHTS ABOVE DOORS INOP.2) REPLACED BATTERIES IN EMERGENCY EXIT LIGHTS IAW B-M/M 33-50-101 OPS CHE CKED GOOD.STATUS: CLOSED 2 L 7 3 4F A3WE 2001101200008 20011012 00008 NM 2001 10 12 USAASB01255 1 20010910 A 3300 8412 BALLAST BOEING 737 737201 1384454 NM PAX CABIN FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 263AU 22869 BWI-MDW - FLT 2735 - DURING CRUISE, SMOKE WAS REPORTED IN THE AFT GALLEY. THE AFT GALLEY CIRCUIT BREAKER WAS PULLED AND THE SMOKE SUBSIDED. THE FLIGHT CREW DECIDED TO DIVERT TO PIT AND THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AFT GALLEY WORK LIGHT WAS PLACED ON MEL AND THE FLIGHT CONTINUED. DURING OVERNIGHT MAINTENANCE THE AFT GALLEY WORK LIGHT BALLAST WAS REPLACED. (M) 2 L 7 2 4F A16WE 2001101200009 20011012 00009 NM 2001 10 12 USAASB01261 1 20010919 A 3350 6013211 POWERPACK BOEING 737 737201 1384454 NM PAX CABIN FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 22961 BWI - THE FORWARD RIGHT EMERGENCY EVACUATION SLIDE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (M) 2 L 7 2 4F A16WE 2001101200010 20011012 00010 NM 2001 10 12 USAASB01260 1 20010915 A 3350 1012721 LIGHT BOEING 737 7372B7 1384560 NM PAX CABIN MISSING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 266AU 22878 LGA - THE LOW LEVEL EMERGENCY LIGHT AT SEAT ROW 16 WAS MISSING. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F A16WE 2001101200011 20011012 00011 EU 2001 10 12 USAASA01050 1 20010909 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319112 EU PAX CABIN FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 721UW 6723 1095 PIT - THE LEFT CENTER CABIN EMERGENCY POWER SUPPLY UNIT FAILED THE CABIN INTERCOMMUNICATION DATA SYSTEM TEST. MAINTENAN CE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. TESTS OK. (M) 2 L 7 2 4F RT A28NM 2001101200012 20011012 00012 NM 2001 10 12 USAASB01249 1 20010908 A 3200 189929 DOWNLOCK SENSOR BOEING 737 7374B7 1384702 NM RT MLG A USAA L ABORTED APPROACH O OTHER AP APPROACH 1 EA 19 429US 24551 SDF - FLT 1144 - IN PREPARATION FOR LANDING AT SDF, THE CREW RECEIVED A RIGHT MAIN LANDING GEAR UNSAFE LIGHT DURING GEAR EXTENSION. CAPTAIN ACCOMPLISHED A FLYBY AT SDF TOWER FOR VISUAL THAT GEAR WAS DOWN. TOWER CONFIRMED GEAR WAS DOWN. C APTAIN ALSO REPORTED THAT THE LANDING GEAR VIEWER SHOWS THE GEAR DOWN AND LOCKED. FLIGHT LANDED WITHOUT FURTHER INCIDEN T AND WAS TOWED TO THE GATE. AN EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE RIGHT MLG DOWNLOCK SENSOR TARGET DAMAGED . REMOVED AND REPLACED TARGET AND PERFORMED ADJUSTMENT AND OPERATIONAL CHECK PER MM 32-61-31. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2001101200013 20011012 00013 EU 2001 10 12 USAAF01072 1 20010909 A 3200 D11320422 DOOR FOKKER F28 F28MK0100 4990807 EU MLG BAY WORN A USAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 19 898US 11398 SDF - FLT 457 - EN ROUTE PIT-SDF, DURING APPROACH, RECEIVED A LEFT MAIN GEAR DOOR MESSAGE. PERFORMED THE QRH PROCEDURE WHILE EXECUTING A MISSED APPROACH. ACCOMPLISHED A FLY BY TO VERIFY THAT THE GEAR WAS DOWN. THE FLIGHT THEN LANDED WITH OUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT MLG DOOR AND THE DOOR SKID ON LEFT MAIN LANDING GEAR DOOR. ACCOMP LISHED A GEAR RETRACTION AND EXTENSION. ALL CHECKS OK. (M) 2 L 7 2 4F RT 2001101200014 20011012 00014 NM 2001 10 12 USAASB01234 1 20010818 A 5550 69633917 BOLT BOEING 737 737301 1384611 NM RT ELEV TRIM TAB WORN A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 351US 23554 DCA - FLT 360 - ON CLIMB-OUT FROM DCA, EN ROUTE TO ROC, CREW FELT A RUMBLE/AIRFRAME VIBRATION THROUGHOUT THE CABIN. DUE TO PREVIOUS FILGHT SEGMENT EXPERIENCING THE SAME PROBLEM, FLIGHT RETURNED TO FIELD AT DCA. FLIGHT LANDED WITHOUT FURTH ER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE RIGHT ELEVATOR TRIM TAB INBOARD ATTACH FITTING BOLT AND BUSHING WORN. REMOVED AND REPLACED INBOARD ATTACH FITTING BOLT AND BUSHING FOR RIGHT ELEVATOR TRIM TAB. OPERATIONAL CH ECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001101200015 20011012 00015 NM 2001 10 12 USAA011243 1 20010905 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 373 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 517AU 45622 23703 PIT - FOUND SKIN CRACKED 1.25 INCH LONG, AFT CORNER OF COOLING EXHAUST STATION 373 STRINGER 28L. INSTALLED DOUBLER PER EA 72400A. (M) 2 L 7 2 4F RT A16WE 2001101200016 20011012 00016 NM 2001 10 12 USAA011242 1 20010918 A 5300 SKIN BOEING 737 7373B7 1384580 NM BS 727D A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 531AU 24478 CLT - FOUND SKIN CRACKED 1.25 INCH, BS 727D STRINGER 23L. INSTALLED DOUBLER PER TR NR 53-60-03. (M) 2 L 7 2 4F RT A16WE 2001101200017 20011012 00017 WP 2001 10 12 2001F00413 1 20010910 A 3350 873100272 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 830US 49443 THE LOW LEVEL EMERGENCY LIGHTS AND THE RIGHT AFT EMERGENCY EXIT LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LE VEL EMERGENCY LIGHT BATTERIES AND THE RIGHT AFT EMERGENCY EXIT LIGHT ASSEMBLY. REF USAAD0160. (M) 2 L 7 2 4F A6WE 2001101200018 20011012 00018 WP 2001 10 12 AALA016078 1 20010906 A 2170 4090233 COALESCER BAG DOUG DC9 DC983 3022083 WP A/C BAY DIRTY A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 871RA 49788 BURNING OIL SMELL REPORTED BY FA AFT OF REAR GALLEY. NO VISIBLE SMOKE, JUST ODOR. PARTICULARLY NOTICEABLE AT HIGH POWE R SETTING. CLEANED APU INLET. REPLACED BOTH PACKS COALESCER BAGS. RAN BOTH ENGINES, OPS CHECK OF AIR CAN SYSTEM FOUND NO EVIDENCE OF OIL SMELL AT DIFFERENT POWER SETTINGS. (M) 2 L 7 2 4F RT A6WE 2001101200019 20011012 00019 NM 2001 10 12 DHL2001708013 1 20011004 A 2612 FIRE LOOP BOEING 727 72725 1384006 NM NR 1 ENGINE OUT OF POSITION A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 708DH 18275 1) NR 1 GROUND DETECTOR CIRCUIT ILLUMINATED IN FLIGHT.2) REPOSITIONED NR 1 ENGINE LOOP-NO FAULTS NOTED.OPS CK SATISFA CTORILY PER MM 26-11-000.THIS CLEARS DMI 7284.STATUS: CLOSED 2 L 7 3 4F A3WE 2001101200020 20011012 00020 WP 2001 10 12 AALA016079 1 20010831 A 2760 WARNING SYSTEM DOUG DC9 DC983 3022083 WP COCKPIT MALFUNCTIONED A AALA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 21 871RA 49788 AUTO SPOILER FAIL LIGHT CAME ON. PRIOR TO GATE DEPARTURE. RESET BREAKER AND RERACKED UNIT RESET MASTER WARNING LIGHT E XTINGUISHED. (M) 2 L 7 2 4F RT A6WE 2001101200021 20011012 00021 NM 2001 10 12 DHL2001720014 1 20010927 A 2611 SMOKE DETECTOR BOEING 727 727228 NM CARGO BAY MALFUNCTIONED A DHLA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 720DH 19544 1) LOWER CARGO FIR E LIGHT ILLUMINATED WITH FIRE BELL. DECLARED EMERGENCY PERFORMED MAIN/LOWER CARGO SMOKE OR FIRE EM ERGENCY CHECKLIST. AFTER LANDING IN KSGF PERFORMED EMRGENCY EVACUATION CHECKLIST.2) TRANSFERRED LOWER PIT SMOKE DETECT ION SYSTEM TO DMI 7193, MEL 26-19 CAT "C" DMI EXPIRES IN 10 DAYS.3) REMOVED & REPLACED RT FWD, FWD PIT SMOKE DETECTOR PER MM 26-16-01. CKS GOOD CLEAR DMI #7193 PLACARD REMOVED.STATUS: CLOSED 2 L 7 3 4F A3WE 2001101200022 20011012 00022 WP 2001 10 12 AALA016080 1 20010820 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 871RA 49788 CCI-RNO - EMERGENCY LIGHT INOPERATIVE AT SEAT 29D. CONNECTED A BROKEN WIRE, DID OPS CHECK. OPS CHECKED OK. (M) 2 L 7 2 4F RT A6WE 2001101200023 20011012 00023 2001 10 12 AALA016081 4 20010908 A 2565 CABLE DOUG DC9 DC983 3022083 WP SLIDE LOOSE A AALA K NONE O OTHER NR NOT REPORTED 1 SW 21 836RA 53046 FORWARD GALLEY EXIT DOOR EMERGENCY SLIDE HAS A CABLE LOOSE ON THE GIRT BAR. RECONNECTED CABLE WIRED TO SLIDE, GOOD FOR SERVICE. (M) 2 L 7 2 4F RT A6WE 2001101200024 20011012 00024 WP 2001 10 12 AALA016083 1 20010915 A 2170 4090233 COALESCER BAG DOUG DC9 DC983 3022083 WP A/C BAY DIRTY A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 836RA 53046 MAIN ENTRY CABIN SERVICE REPORTED SMOKE/FUMES IN CABIN. REMOVED AND REPLACED COALESCER BAGS. ACCOMPLISHED PACK BURN PE R 21-20-01-2. RAN BOTH ENGINES TO HIGH POWER. BOTH RIGHT AND LEFT PACKS OPS CHECKS NORMAL. (M) 2 L 7 2 4F RT A6WE 2001101200025 20011012 00025 2001 10 12 AALA016084 4 20010907 A 2565 CABLE DOUG DC9 DC983 3022083 WP SLIDE LOOSE A K NONE O OTHER NR NOT REPORTED 1 SW 21 836RA 53046 FORWARD GALLEY DOOR EMERGENCY SLIDE HAS A CABLE MECHANISM LOOSE AT BOTTOM OF SLIDE. RECONNECTED GIRT BAR CABLE ASSY TO DOOR SLIDE COVER. (M) 2 L 7 2 4F RT A6WE 2001101200026 20011012 00026 NM 2001 10 12 DHL2001745014 1 20010927 A 5270 WARNING SYSTEM BOEING 727 727224 1384076 NM MLG MALFUNCTIONED A DHLA B A EMER. DESCENT UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 745DH 20665 1) MAIN DOOR CARGO, LITE FL. 31.0 ILLUMINATED. MAIN CARGO DOOR NOT CLESELITE ON BULKHEAD WAS ALSO ILLUMINATED DEPRESS URIZED A/C AAT APPROX. 6.0 PSI DIFFERTIAL BOTH LIGHTS WENT OUT PERFORMED MAIN CARGO DOOR ILLUMINATED IN FLT. C`KLIST.2 ) CLEANED MCD SWITCH IAW WPM 20-60-1. TESTED MCD WARNING SYS. IAW AEI MM 52. PRESSURIZED A/C IAW 21-31-0. DOOR LIG HT & MCD WARNING SYS. OPS GOOD. NO DEFECTS NOTED. OK TO CONTINUE. 2 L 7 3 4F A3WE 2001101200027 20011012 00027 NM 2001 10 12 DHL2001745015 1 20010929 A 5270 SWITCH BOEING 727 727224 1384076 NM MLG OUT OF ADJ A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 745DH 20665 1) AT FL 330 "MAIN CARGO DOOR" LIGHT ILLUMINATED. DIFFERENTIAL WAS AT 8.4 PSI. COMPLETD EMERGENCY PROCEDURE. AT FL 300 AND 7.8 PSI DIFFERENTIAL THE LIGHT EXTINGUISHED.2) INSPECTED CARGO DOOR SYSTEM. NO MECHANICAL DEFECTS NOTED. ADJUSTED DOOR CLOSED MICROSWITCH IAW AEI MM, OPS CKS. GOOD.STATUS: CLOSED 2 L 7 3 4F A3WE 2001101200028 20011012 00028 NM 2001 10 12 DHL2001746002 1 20011005 A 3350 LIGHT BOEING 727 727224 1384076 NM CABIN INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 746DH 22252 1) FWD ENTRY EMERGENCY LT. WILL NOT COME ON WHEN ARMED & TESTED.2) R&R FWD ENTRY EMERGENCY LIGHT ASSY IAW B-727M/M 3 3-50-00.STATUS: CLOSED 2 L 7 3 4F A3WE 2001101200029 20011012 00029 WP 2001 10 12 DHL2001802014 1 20011009 A 2611 SMOKE DETECTOR DOUG DC8 DC873 302199C WP CABIN WILL NOT TEST A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 802DH 46076 1) MAIN CABIN NR 12 SMOKE DETECTOR FAILS TO TEST.2) RELAMPED NR 12 SMOKE DETECTOR IAW 26-10-5 OPS GOOD THIS CLEARS DMI #7340STATUS: CLOSED 2 L 7 4 4F RT 4A25 2001101200030 20011012 00030 NM 2001 10 12 AALA20011337 1 20010702 A 3397 SPLICE BOEING 727 727223 1384074 NM GALLEY DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 885AA 21524 DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT LIGHT AT GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT LIG HT WIRE SPLICE AT FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001101200031 20011012 00031 NM 2001 10 12 AALA20011367 1 20010705 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 875AA 21387 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 27 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STRIP AT ROW 27. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001101200032 20011012 00032 NM 2001 10 12 AALA20011400 1 20010711 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 726AA 20733 TUL - FOUND FLOOR EMERGENCY ESCAPE PATH LIGHTING STRIP WEAK, DIM, FROM FORWARD GALLEY TO AFT GALLEY. INSTALLED NEW PATH LIGHT AND CLEAR LENS. OPS CHECK OK. (M) 2 L 7 3 4F A3WE 2001101200033 20011012 00033 NM 2001 10 12 AALA20011493 1 20010723 A 3397 CONNECTOR BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 884AA 21523 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS VERY DIM. REPLACED EMERGENCY EXIT ESCAPE PATH LIG HT CONNECTORS AT FIRST CLASS FORWARD PARTITION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001101200034 20011012 00034 WP 2001 10 12 DHL2001803012 1 20011006 A 2611 SMOKE DETECTOR DOUG DC8 DC873 302199C WP NR 10 WILL NOT TEST A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 803DH 46123 1) NR 10 SMOKE DETECTOR WONT TEST.2) INSPECTED NO.10 SMOKE DETECTOR AND C/P NO DEFECTS NOTED. RELAMPED TEST AND FUNCTI ON BULBS OPS NORMAL PER MM 26-10-6. DMI 7323 CLRD. PLCD RMVD.STATUS: CLOSED 2 L 7 4 4F RT 4A25 2001101200035 20011012 00035 WP 2001 10 12 DHL2001804018 1 20010927 A 3350 LIGHT DOUG DC8 DC873F 302199F WP CABIN MALFUNCTIONED A DHLA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 804DH 46124 1) EMERGENCEY LIGHTS WILL NOT DISARM.2) RELAMPED EMERGENCY LIGHT ARM-DISARM SOCKET OPS CHKD SYS PER MM 33-50-2 NO DEF ECTS NOTEDSTATUS: CLOSED 2 L 7 4 4F RT 4A25 2001101200036 20011012 00036 WP 2001 10 12 DHL2001804019 1 20011009 A 5610 WINDOW DOUG DC8 DC873F 302199F WP COCKPIT MALFUNCTIONED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 1) CAPTAINS SLIDING WINDOW WILL NOT OPEN.2) LUBRICATED CAPTAIN'S SLIDING WINDOW I.A.W. MAINTENANCE MANUAL 56-20 OPS. CHECK O.K.STATUS: CLOSED 2 L 7 4 4F RT 4A25 2001101200037 20011012 00037 WP 2001 10 12 DHL2001804020 1 20011010 A 5610 WINDOW DOUG DC8 DC873F 302199F WP COCKPIT LACK OF LUBE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 1) CAPT'S SLIDING WINDOW WILL NOT OPEN.2) ADJUSTED SLIDING WINDOWS IAW MM 56-10-2 CHECKED OPERATION OKSTATUS: CLOSED 2 L 7 4 4F RT 4A25 2001101200038 20011012 00038 WP 2001 10 12 DHL2001805021 1 20010926 A 2710 CONTROL CABLE DOUG DC8 DC873F 302199F WP AILERON FROZEN A DHLA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 01 805DH 46125 1) AILERON TRIM FROZEN DURING CRUISE FLIGHT BECAME OPERATIVE AT -3C OAT.2) LUBED AILERON TRIM TABS AND CONTROL TABS PER DC-8 27-10-0. OPS CHKS NORMALSTATUS: CLOSED 2 L 7 4 4F RT 4A25 2001101200039 20011012 00039 WP 2001 10 12 DHL2001805022 1 20010927 A 2710 JACKSCREW DOUG DC8 DC873F 302199F WP AILERON FROZEN A DHLA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 01 805DH 46125 1) AILERON TRIM FROZEN IN FLIGHT BELOW -20DEG.2) LUBED LEFT & RIGHT AILERON TRIM JACKSCREWS. OPS CHECK OK IAW MM 27- 13-0.STATUS: CLOSED 2 L 7 4 4F RT 4A25 2001101200040 20011012 00040 2001 10 12 AALA20011736 4 20010910 A 3140 COMPUTER BOEING 767 767323 1385205 NM E/E BAY FALSE INDICATION A AALA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 SW 21 360AA 24041 ORD - FLT 42 - IN CRUISE FLIGHT AT FL330 FMC 2 CB POPPED AND THE FOLLOWING EICAS MESSAGE APPEARED, R FMC FAIL, EICAS CON TROL PNL, EICAS DISPLAY, R IRS ON DC ALSO AUTO THROTTLES WOULD NOT MATCH N1 POWER SETTINGS. RIGHT ENGINE NR 1 WAS 6 PER CENT HIGHER THAN LEFT ENGINE WITH MATCHED POWER LEVERS ALL OTHER PARAMETERS ALSO UNMATCHED FWD GALLEY CHILLER NAV F/O NA V RMDI INOPERATIVE AS WELL, ALSO NO LAND 3. REINSTATED C/B C307. INSPECTED RIGHT IDG AND RT ENGINE FEEDER HARNESS. NO FAULTS FOUND, CHECKED AND SERVICED RIGHT IDG OIL CHECKED OK. RAN BOTH ENGINES AT CRUISE POWER FOR TWENTY MINUTES. NO FAULTS FOUND. LOADED RIGHT MAIN BUS TO 75 PERCENT LOAD FOR APPROXIMATELY 10 MINUTES. NO FAULTS AND C/B C307 REMAINED I 2 L 7 2 4F RT A1NM 2001101200041 20011012 00041 WP 2001 10 12 DHL2001805023 1 20011001 A 2612 FIRE LOOP DOUG DC8 DC873F 302199F WP NR 4 ENGINE FAILED A DHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 805DH 46125 1) DURING CLIMOUT FM MDSD LOOP B, NR 4 SHORT CIRCUIT ILLUMINATED. LIGHT EXTINGUISHED AFTER CHANGING TO LOOP A. GOOD FIR E TEST IN LOOP A POSITION. 2) ENTERED ON DMI 7230 AS PER DHL MEL 26-2-3 C/W SP 26-2 PLACARD INSTALLED. 3) CHA NGED 2EA FIRE LOOP SENSORS ON CORE ENGINE. OPS CHECKED SYSTEM-NO DEFECTS NOTED. THIS CLEARS DMI#7230. PERFORMED IAW DC -8 MM 26-10-1STATUS: CLOSED 2 L 7 4 4F RT 4A25 2001101200042 20011012 00042 EU 2001 10 12 SIMA200123401 1 20010814 A 3830 7253680117 PAN SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 343SB 340B343 SBP - DURING MBV INSPECTION, MAINTENANCE FOUND THE LAVATORY SERVICE BOX IS CORRODED. REMOVED AND REPLACED LAVATORY SERV ICE BOX IAW SAAB SERVICE BULLETIN 340-53-050. (M) 2 L 7 2 4T RT A52EU 2001101200043 20011012 00043 WP 2001 10 12 DHL2001805024 1 20010929 A 3260 INDICATOR DOUG DC8 DC873F 302199F WP MLG MALFUNCTIONED A DHLA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 01 805DH 46125 1) GEAR NOT LATCHED LIGHT ILLUMINATED INTERMITTENLY STRONG VIBRATION IN RUDDER PEDALS, UPLATCH CHECK OK. 2) INSPEC TED NOSE & MLG IAW M/M 32-10-0 & 32-20-0, INSP LANDING GEAR IND IAW WDM 32-1-0 NO DEFECTS NOTED. AS PER M/M 32-60-0 GEAR NOT LATCHED IND WILL ILLUMINATE WITHIN 7 DEG FROM IDLE STOP WITH GEAR NOT DOWN.STATUS: CLOSED 2 L 7 4 4F RT 4A25 2001101200044 20011012 00044 WP 2001 10 12 DHL2001806013 1 20010930 A 3210 DOOR DOUG DC8 DC873F 302199F WP MLG CRACKED A DHLA O OTHER O OTHER TO TAKEOFF 1 SO 01 806DH 46002 DURING TAKEOFF IN MEXICO CITY ABORTED-- DISCREPANCY LEFT MAIN GEAR DOOR INSIDE SKIN HAS 2 INCH CRACK VERY LOWER CENTER A REA.1) REMOVED CRACKED EXISTING DOUBLER REPAIR ON LOWER CENTER AREA OF LEFT MAIN GEAR DOOR INSIDE SKIN I.A.W. DC-8 S.R.M . 51-1-21A.2) INSTALLED NEW DOUBLER REPAIR ON LOWER CENTER AREA OF LEFT MAIN GEAR DOOR INTERIOR SKIN I.A.W. DC-8 S.R.M. 51-1-21A. SIZE OF REPAIR 6 1/2" X 8 MATERIALS USED 2024-0 HEAT-TREATED TO 2024T-3 .050 2 L 7 4 4F RT 4A25 2001101200045 20011012 00045 WP 2001 10 12 DHL2001806014 1 20010929 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 806DH 46002 1) EMERGENCY EXIT LIGHTS VERY DIM.2) REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK I.A.W. DC-8 M.M. 33-50-2 OPS N ORMAL.STATUS: CLOSED 2 L 7 4 4F RT 4A25 2001101200046 20011012 00046 WP 2001 10 12 DHL2001806016 1 20010929 A 7830 DOOR DOUG DC8 DC873F 302199F WP THRUST REVERSER DAMAGED A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 806DH 46002 ON TAKE OFF FROM MEXICO CITY ABORTED-----DISCREPANCY NR 4 ENGINE I/B T/R DOOR LOWER FWD EDGE DAMAGED.1) ROUTED OUT DAMAG E AREA ON NR 4 ENGINE I/B T/R LOWER FORWARD ADGE AS PER CFM56 ESM FIG. NR 2 78-31-41.2) INSTALLED DOUBLER REPAIR I.A.W. CFM56 ESM 78-31-41 MATERIAL USED 7075-T6 .090 P.O.# 831892 LOT# 3L0XWS85 SIZE 3 1/2" X 10". 2 L 7 4 4F RT 4A25 2001101200047 20011012 00047 WP 2001 10 12 DHL2001807025 1 20010926 A 2500 SEAT BACK DOUG DC8 DC873F 302199F WP COCKPIT DAMAGED A DHLA K NONE O OTHER NR NOT REPORTED 1 SO 01 807DH 45990 1) CAPTS SEAT DOES NOT POSITIVELY LOCK IN FORE/AFT TRACK. SEVERAL INSTANCES OF UNCOMMANDED REARWARD MOVEMENT EG,. SETT ING OR RELEASING BRAKES PUSHING ON RUDDER PEDALS, ETC. ALSO, SEATBACK RELEASE WOULD NOT RE-ENGINE.2) ADJUSTED TRACK L OCK.CLEAN TRACK HOLES AND LUBED OK SEAT ON FWD&AFT MOVEMENT LOCKS OK.STATUS: CLOSED 2 L 7 4 4F RT 4A25 2001101200048 20011012 00048 SO 2001 10 12 SIMA200123418 1 20010814 A 5315 FLOORBEAM EMB 145 EMB145LR SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 642AE 145193 ABI - DURING MBV INSPECTION MAINTENANCE, FOUND CORROSION ON THE GALLEY FLOOR FORWARD DIGITAL. CORROSION WAS REMOVED AND AREA WAS REPAIRED IAW EMB GST-2713/01 AND SRM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001101200050 20011012 00050 EU 2001 10 12 SIMA200123423 1 20010814 A 2720 7327200561 CARRIAGE SAAB SF340 340B 7860101 EU COCKPIT CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 343SB 340B343 SBP - DURING MBV INSPECTION MAINTENANCE, FOUND THE RIGHT RUDDER PEDAL CONSOLE CARRIAGE CORRODED. MAINTENANCE REMOVED AN D REPLACED THE RIGHT CARRIAGE IAW SAAB MM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001101200052 20011012 00052 SO 2001 10 12 SIMA200123424 1 20010822 A 5315 FLOORBEAM EMB 145 EMB145LR SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 641AE 145191 ABI - DURING MBV INSPECTION, MAINTENANCE FOUND THE RIGHT OMEGA BEAM TO BE CORRODED. CORROSION WAS REMOVED AND AREA WAS REPAIRED IAW EMB REPAIR STATEMENT GST-2864/01, AND GST-2811/01, AND EMB SRM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M ) 2 L 7 2 4T RT T00011AT 2001101200053 20011012 00053 SO 2001 10 12 SIMA200123425 1 20010822 A 5315 FLOORBEAM EMB 145 EMB145LR SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 641AE 145191 ABI - DURING MBV INSPECTION, MAINTENANCE FOUND THE FORWARD DIGITAL TO BE CORRODED. CORROSION WAS REMOVED AND AREA WAS R EPAIRED IAW EMB REPAIR STATEMENT GST-2811/01 AND EMB SRM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001101200054 20011012 00054 SO 2001 10 12 SIMA200123426 1 20010822 A 5315 FLOORBEAM EMB 145 EMB145LR SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 641AE 145191 ABI - DURING MBV INSPECTION MAINTENANCE, FOUND THE LEFT OMEGA BEAM AT FRAME TO BE CORRODED. CORROSION WAS REMOVED AND A REA WAS REPAIRED IAW EMB SRM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001101200055 20011012 00055 SO 2001 10 12 SIMA200123427 1 20010822 A 5315 FLOORBEAM EMB 145 EMB145LR SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 641AE 145191 ABI - DURING MBV INSPECTION MAINTENANCE, FOUND THE CENTER OMEGA BEAM TO BE CORRODED. CORROSION WAS REMOVED AND AREA WAS REPAIRED IAW EMB REPAIR STATEMENT GST 2811/01 AND EMB SRM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001101200057 20011012 00057 SO 2001 10 12 SIMA200123428 1 20010822 A 5315 FLOORBEAM EMB 135 EMB135LR SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 708AE 145208 ABI - DURING MBV INSPECTION MAINTENANCE, FOUND THE RIGHT OMEGA BEAM LOWER FLANGE FORWARD OF FRAME 25 TO BE CORRODED. CO RROSION WAS REMOVED AND AREA WAS REPAIRED IAW EMB REPAIR STATEMENT GST 2830/01 AND EMB SRM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001101200058 20011012 00058 EA 2001 10 12 COMA0160792 1 20011008 A 5300 SKIN CNDAIR CL600 CL6002B19 EA A COMA O OTHER C F.O.D. DE DESCENT 1 SO 01 954CA 7100 FLIGHT #5572. CREW REPORTED A BIRD STRIKE, LEFT WING TIP.C/W BIRDSTRIKE INSPECTION AND NO DAMAGE WAS FOUND. 2 L 7 2 4F RT A21EA 2001101200059 20011012 00059 SO 2001 10 12 SIMA200124802 1 20010905 A 7930 WARNING SYSTEM EMB 145 EMB145LR SO COCKPIT ACTIVATED A SIMA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 SW 21 635AE 145158 DFW - FLT 3479 - AFTER TAKEOFF, CREW NOTED E2 OIL IMPENDING BYPASS MESSAGE ON EICAS. AFTER 10 MINUTES NOTED 200 DEGREE ITT INCREASE ACCOMPANIED BY VIBRATION. ENGINE POWER WAS REDUCED TO IDLE AND CREW RETURNED TO FIELD. (M) 2 L 7 2 4T RT T00011AT 2001101200060 20011012 00060 EU 2001 10 12 SIMA200125301 1 20010910 A 5414 SKIN SAAB SF340 340B 7860101 EU RT NACELLE CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 235AE 340B235 ABI - DURING MBV INSPECTION, FOUND OUTER SKIN OF RIGHT ENGINE NACELLE CRACKED ON OUTBOARD SIDE. REPAIRED NACELLE SKIN I AW SAAB 340 SRM AND REPAIR STATEMENT SDS002401. (M) 2 L 7 2 4T RT A52EU 2001101200061 20011012 00061 SO 2001 10 12 SIMA200125401 1 20010911 A 5320 BEAM EMB 145 EMB145LR SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 644AE 145204 ABI - DURING MBV INSPECTION, FOUND GALLEY CENTER BEAM AT FRAME 20 CORRODED. REMOVED CORROSION ON GALLEY CENTER BEAM AT FRAME 20 AND REPAIRED IAW EMB 145 SRM AND REPAIR STATEMENT GST 2977/01. (M) 2 L 7 2 4T RT T00011AT 2001101200064 20011012 00064 NE 2001 10 12 2001UALA01728 2 20010815 A 7321 546689 FERRULE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE LEAKING A UALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 WP 29 7276U 21423 700114 AIRCRAFT DIVERTED TO MIA DUE TO IDLE POWER CONDITION FROM NR 1 ENGINE. *S/D* THE CAUSE WAS A FUEL LEAK FROM THE FUEL L INE FROM THE FUEL/OIL COOLER TO THE P&D VALVE. THIS LINE WAS MISSING A FERRULE AT THE P&D VALVE CONNECTION. THIS ENGI NE HAD ONLY 370 HRS SINCE OVERHAUL. REPLACED P&D VALVE AND FERRULE ON FUEL LINE. 2 L 7 3 4F 4 F A3WE E2EA 2001101200068 20011012 00068 NM 2001 10 12 TSAA0126118 1 20010916 A 2612 FIRE WARNING BOEING 737 7372M6C 1384708 NM APU FALSE ACTIVATION A TSAA F ACTIVATE FIRE EXT. N FALSE WARNING LD LANDING 1 WP 13 805AL 21809 FLT - 117 - HNL-LIH - ON SHORT FINAL LANDING IN LIHUE, HI, THE APU WAS STARTED AND FOLLOWED BY AN ILLUMINATION OF THE AP U FIRE WARNING HANDLE, THE SOUNDING OF THE FIRE WARNING BELL, AND ILLUMINATION OF THE GLARE SHIELD FIRE WARNING LIGHTS. THE APU FIRE HANDLE WAS PULLED AND THE APU SWITCH WAS POSITIONED TO OFF. THE FIRE WARNING LIGHT REMAINED ILLUMINATED. THE APU FIRE BOTTLE WAS DISCHARGED. NO SMOKE OR FIRE DETECTED BY THE ATC TOWER. INSPECTED THE APU AREA FOR DAMAGE. N O DAMAGE FOUND. DEFERRED THE APU ASSEMBLY PER MEL 49-1 AND APU FIRE DETECTION SYSTEM PER MEL 26-8-1. (M) 2 L 7 2 4F RT A16WE 2001101200069 20011012 00069 NM 2001 10 12 USAA011231 1 20010910 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 45284 23380 CLT - FOUND CHORD CRACKED .75 INCH, BS 178 WL 184 LBL 5.5. INSTALLED REPAIR ANGLES PER EO NR 5300V155. (M) 2 L 7 2 4F RT A16WE 2001101200070 20011012 00070 NM 2001 10 12 USAA011244 1 20010909 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 44611 23232 TPA - FOUND SKIN WITH 6 INCH GOUGE, STATION 807 STRINGER 27R AND 28R. REPAIRED USING SAME DOUBLER PER SRM 53-00-01 FIG 201. (M) 2 L 7 2 4F RT A16WE 2001101200072 20011012 00072 NM 2001 10 12 USAA011245 1 20010918 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 23232 TPA - FOUND SKIN WITH 6 INCH CREASE, STATION 807 STRINGER 28 LEFT AND 28 RIGHT. REPAIRED BY INSTALLING DOUBLER, ONE DOU BLER INSTALLED FOR 2 DAMAGES PER SRM 53-00-01 FIG 201. (M) 2 L 7 2 4F RT A16WE 2001101200074 20011012 00074 EA 2001 10 12 COMA0160794 1 20011006 A 5311 600363031 DOUBLER CNDAIR CL600 CL6002B19 EA DOOR CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 709CA 7687 7238 F.S.718 FRAME DOUBLER CRACKED ON LEFT SIDE OF FUSELAGE.REPAIRED LEFT SIDE DOUBLER I/A/W REO 601R-53-61-193 REV A. 2 L 7 2 4F RT A21EA 2001101200075 20011012 00075 EA 2001 10 12 COMA0160795 1 20011003 A 5300 6003603031 DOUBLER CNDAIR CL600 CL6002B19 EA DOOR FRAME CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 708CA 7937 7235 L/H AFT DOUBLER AT F.S. 718.00 BETWEEN STRINGER 11 AND 12 IS CRACKED.REMOVED CRACKED L/H AFT DOUBLER AT F.S. 718.00 AND INSTALLED NEW DOUBLER I/A/W CANADAIR REO 601R-53-61-193 REV A. 2 L 7 2 4F RT A21EA 2001101200076 20011012 00076 EA 2001 10 12 COMA0160796 1 20011003 A 5300 6003603024 FRAME CNDAIR CL600 CL6002B19 EA DOOR FRAME CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 708CA 7937 7235 R/H 718.00 FRAME UPPER AND LOWER FLANGE IS CRACKED BETWEEN STRINGER 11 AND 12.REMOVED CRACKED SECTION OF R/H 718.00 FRAM E AND REPAIRED USING NEW SECITON OF FRAME I/A/W CANADAIR REO 601R-53-61-193 REV A. 2 L 7 2 4F RT A21EA 2001101200077 20011012 00077 EA 2001 10 12 COMA0160797 1 20011009 A 5346 WEB CNDAIR CL600 CL6002B19 EA BEAM CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 709CA 7687 7238 ENGINE SUPPORT BEAM LOWER WEB CRACKED BETWEEN FS 625.30 AND FS 640.00 AT WL 111.09, BL37 LT AND RT.PERFORMED TEMPORARY R EPAIR I/A/W BOMBARDIER REO 601R-53-61-366 REV. C. 2 L 7 2 4F RT A21EA 2001101200078 20011012 00078 NM 2001 10 12 USAA011246 1 20010910 A 5415 STRUT BOEING 737 737401 1384701 NM NACELLE WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 PIT - STRUT BEARING BORE REQUIRES RECHAMFERING, MAIN BEARING BORE. MACHINE BORE AND RECHAMFER. (M) 2 L 7 2 4F RT A16WE 2001101200079 20011012 00079 NM 2001 10 12 USAA011247 1 20010916 A 5320 STIFFENER BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 22959 PIT - FOUND STIFFENER WITH CORROSION 1.25 INCH IN DIAMETER, AFT CLIP NUT HOLE ON STIFFENER BS 312 AND 328. DEFECTIVE PAR T REPLACED WITH IDENT PART NR. (M) 2 L 7 2 4F RT A16WE 2001101200080 20011012 00080 EA 2001 10 12 COMA0160798 1 20011010 A 2760 SPOILER CNDAIR CL600 CL6002B19 EA A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 951CA 7091 FLIGHT #5648 - CONFIG SPOILER MESSAGE DURING T/O. SPOILERS OPERATED NORMAL, AIRCRAFT RETURNED TO THE GATE.RESET SPOILER SYSTEM, NO FAULTS WERE FOUND. 2 L 7 2 4F RT A21EA 2001101200081 20011012 00081 EU 2001 10 12 USAA011248 1 20010913 A 5330 SKIN FOKKER F28 F28MK0100 4990807 EU FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 855US 11283 PIT - FOUND SKIN DENTED 4 INCHES BY 2 INCHES BY .125 INCHES, STATION 930.5 AT STRINGER 72. FILLER AND DOUBLER INSTALLED PER SRM 53-00-02. (M) 2 L 7 2 4F RT 2001101200082 20011012 00082 EU 2001 10 12 USAABA01010 1 20010905 A 3350 32146220 POWER SUPPLY AIRBUS 330 A330323 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 675US 370 PHL - FOUND THE NR 3 EPSU FAILED. MAINTENANCE REPLACED THE NR 3 EPSU. (M) 2 L 7 2 4F RT A46NM 2001101200083 20011012 00083 NM 2001 10 12 USAABB01096 1 20010911 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 614AU 27145 CLT - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 1, 4, 6, 9, 13, 18, 23, 26 AND 29 INOPERATIVE. MAINTENANCE REPLACED TH E BATTERIES. (M) 2 L 7 2 4F RT A2NM 2001101200084 20011012 00084 NM 2001 10 12 USAABB01097 1 20010920 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 612AU 27124 PIT - FOUND FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE AT ROWS 1, 6 AND 25. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2001101200085 20011012 00085 WP 2001 10 12 USAAD01161 1 20010919 A 3350 873100272 LIGHT DOUG DC9 DC981 3022081 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 802US 48036 BOS - THE AFT RIGHT EXIT WINDOW EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F A6WE 2001101200086 20011012 00086 EU 2001 10 12 USAAF01073 1 20010916 A 3233 415005 ACTUATOR FOKKER F28 F28MK0100 4990807 EU LT MLG FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 864US 2304 11306 RDU - FLT 1286 - EN ROUTE - RDU-PHL, THE LEFT MLG WOULD NOT RETRACT AFTER TAKEOFF. THE LANDING GEAR WAS RECYCLED, BUT T HE LEFT MLG STILL DID NOT RETRACT. THE FLIGHT RETURNED TO THE FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE R EPLACED THE LT MLG RETRACTION ACTUATOR. OPS AND LEAK CHECKED OK. (M) 2 L 7 2 4F RT 2001101200087 20011012 00087 EU 2001 10 12 USAASA01049 1 20010830 A 3350 32145510 POWER SUPPLY AIRBUS A321 A321211 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 166US 1436 PHL - THE LEFT MID CABIN EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (M) 2 L 7 2 4F RT A28NM 2001101200090 20011012 00090 NM 2001 10 12 USAASB01224 1 20010807 A 2133 7110033 OUTFLOW VALVE BOEING 737 737301 1384611 NM CABIN PRESSURE FAILED A USAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 355US 23558 PIT - FLT 1146 - EN ROUTE FROM PHL TO CMH, AT FL350, THE CABIN ALTITUDE WARNING HORN SOUNDED. CREW NOTICED CABIN ALTITU DE AT 11,000 FEET. CREW WAS UNABLE TO CONTROL CABIN ALTITUDE, DESCENDED TO 10,000 FEET PER QUICK REF HANDBOOK PROCEDURE S. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE AC MO TOR HAD FAILED ON THE AFT OUTFLOW VALVE. REMOVED AND REPLACED AFT OUTFLOW VALVE PER MM 21-31-11. OPS CHECK NORMAL. CH ECKED FORWARD OUTFLOW VALVE PER MM 21-43-11. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2001101200093 20011012 00093 NM 2001 10 12 USAASB01248 1 20010907 A 2130 69291413 CHECK VALVE BOEING 737 7374B7 1384702 NM CABIN PRESSURE BROKEN A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 426US 24548 CLT - FLT 12 - EN ROUTE FROM MCO TO PHL, AT APPROXIMATELY FL190, THE CREW HAD DIFFICULTY MAINTAINING CABIN PRESSURIZATIO N. MAINTENANCE CONTROL WAS CONTACTED FOR TROUBLESHOOTING BUT THE PROBLEM CONTINUED. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE SWING CHECK VALVE, FOR THE EXTERNAL GROUND CONDITIONED AIR, BROKEN AND DISPLACED. REMOVED AND REPLACED CHECK VALVE ASSEMBLY. PRESSURIZATION CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001101200094 20011012 00094 EA 2001 10 12 COMA0160799 1 20011010 A 4950 APU CNDAIR CL600 CL6002B19 EA A COMA K NONE O OTHER CL CLIMB 1 SO 01 940CA 7048 FLIGHT #5790 - L/H AC PACK EMITS OILY SMELL WHEN APU BLEED SOURCE USED.COULD NOT DUPLICATE OPERATED L/H AND R/H AC PACKS ON APU AND NO SMOKE OR ODOR WAS NOTED. 2 L 7 2 4F RT A21EA 2001101200095 20011012 00095 NM 2001 10 12 USASB01255 1 20010910 A 3320 LIGHT BOEING 737 737201 1384454 NM GALLEY FAULTY A USAA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 263AU 22869 BWI-MDW - FLT 2735 - DURING CRUISE, SMOKE WAS REPORTED IN THE AFT GALLEY. THE AFT GALLEY CIRCUIT BREAKER WAS PULLED AND THE SMOKE SUBSIDED. THE FLIGHT CREW DECIDED TO DIVERT TO PIT AND THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AFT GALLEY WORK LIGHT WAS PLACED ON MEL AND THE FLIGHT CONTINUED. (M) 2 L 7 2 4F A16WE 2001101200096 20011012 00096 NM 2001 10 12 2001UALA01997 1 20010901 A 5310 PRESSURE PANEL BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7265U 21412 NOSE LANDING GEAR WHEEL WELL TOP PRESSURE PANEL IS CRACKED AT FASTENER HOLES BS 275, RBL 13, AND BS 284, RBL 6. REPAIRE D PRESSURE PANEL WEB. MAJOR REPAIR ACCOMPLISHED. 2 L 7 3 4F 4 F A3WE E2EA 2001101200097 20011012 00097 WP 2001 10 12 0103449991 1 20010922 A 2611 473925 CONTROL UNIT DOUG DC9 DC931 3022065 WP CARGO BAY MALFUNCTIONED A NWAA F L A ACTIVATE FIRE EXT. ABORTED APPROACH UNSCHED LANDING N G FALSE WARNING MULTIPLE FAILURE CL CLIMB 1 GL 01 8957E 47215 DURING CLIMB, THE FORWARD CARGO SMOKE DETECTOR INDICATION AND FAULT LIGHT ILLUMINATED. FOLLOWED COM PROCEDURES AND CREW DISCHARGED THE NR 1 FIRE BOTTLE. AN EMERGENCY WAS DECLARED AND FLIGHT DIVERTED TO MKE. WHILE DIVERTING, NUMEROUS ELEC TRICAL FAULTS OCCURRED. A GO-AROUND WAS PERFORMED TO ENABLE A VISUAL CHECK OF LANDING GEAR DOWN AND LOCKED. AIRCRAFT L ANDED UNEVENTFULLY AT MKE AND THE GEAR WAS PINNED PRIOR TO TAXIING. MAINTENANCE INSPECTED ALL CARGO AREAS AND FOUND NO EVIDENCE OF SMOKE OR FIRE. REPLACED THE LEFT AC BUS PHASE C-CIRCUIT BREAKER, LEFT GENERATOR AC POWER RELAY, BOTH FIRE B OTTLES, AND CARGO SMOKE DETECTOR. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001101200098 20011012 00098 NM 2001 10 12 2001UALA02049 1 20010916 A 2120 SMOKE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT DETECTED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 593UA 28144 SMOKE IN FLIGHT DECK AND MAIN CABIN. *S/D* UNABLE TO DUPLICATE PROBLEM. ALL SYSTEMS OPERATE NORMALLY. ACCOMPLISHED P ACK BURNOUT. 2 L 7 2 4F 4 F RT A2NM E17NE 2001101200099 20011012 00099 EA 2001 10 12 COMA0160800 1 20011009 A 5320 60034017374 ANGLE CNDAIR CL600 CL6002B19 EA COCKPIT CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 934CA 16859 7042 THE VERTICAL J ANGLE CLIP INSIDE OF CBP2 AT RBL9 WAS FOUND CRACKED.REMOVED AND REPLACED VERTICAL J ANGLE CLIP I/A/W WVAC EO 601R-53-2755. 2 L 7 2 4F RT A21EA 2001101200100 20011012 00100 NM 2001 10 12 2001UALA02072 1 20010921 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 323UA 23955 BODY STATION 706 FUSELAGE FRAME WEB CRACKED AT STRINGER 11 LEFT HAND. MAJOR REPAIR ACCOMPLISHED. DAMAGE REMOVED. DOUB LER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001101200101 20011012 00101 NM 2001 10 12 2001UALA02073 1 20010922 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 518UA 24871 FLOORBEAM TOP CAP CORRODED STA 680, RBL 9 TO LBL 9. MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW TOP CAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2001102600021 20011026 00021 2001 10 26 2001UALA02074 4 20010919 A 3460 B397BAM0513 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE E/E BAY MALFUNCTIONED A UALA A UNSCHED LANDING E F VIBRATION/BUFFET FLT CONT AFFECTED CL CLIMB 1 WP 29 404UA 450 ON CLIMBOUT FELT STRONG VIBRATION IN RUDDER PEDALS. STRONG VIBRATION WAS FELT IN THE REAR OF THE CABIN. THE VIBRATION WAS REPORTED AS BEING A SIDE-TO-SIDE MOTION. FAC (FLIGHT AUGMENTATION COMPUTER) WAS REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2001102600022 20011026 00022 NE 2001 10 26 2001UALA02075 2 20010921 A 7230 6A4904 BLADE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ENGINE CRACKED A UALA A UNSCHED LANDING Y ENGINE STOPPAGE NR NOT REPORTED 1 WP 29 435UA 10823 613 V10377 NR 1 ENGINE FAILURE. IN FLIGHT SHUT DOWN DUE TO ENGINE FAILURE CAUSED BY HIGH PRESSURE COMPRESSOR (HPC) 6TH STAGE BLADE CRACKING/LIBERATION AT ROOT. INSTALLATION OF NEW DESIGN OF C6 BLADES. 2 L 7 2 4F 4 F RT A28NM E40NE 2001101200102 20011012 00102 NE 2001 10 12 0103452289 2 20010926 A 7220 65196842 INLET BULLET BOEING 727 727251 138408H NM PWA JT8 JT8D15A 52051 NE LT ENGINE DISLODGED A NWAA E A ENGINE SHUTDOWN UNSCHED LANDING J R E WARNING INDICATION PARTIAL RPM/PWR LOSS VIBRATION/BUFFET CL CLIMB 1 GL 01 289US 21377 700027 DURING CLIMBOUT FROM LAN, THE LEFT ENGINE FAILURE LIGHT ILLUMINATED WITH ASSOCIATED LOSS OF THRUST AND VIBRATION FROM TH E LEFT ENGINE. CREW SHUT DOWN THE LEFT ENGINE AND AIRCRAFT RETURNED TO LAN. MAINTENANCE FOUND NOSE DOME DISLODGED IN N OSE COWL. REPLACED THE LEFT ENGINE INLET CASE, NOSE COWL, AND NOSE DOME. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO S ERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2001101200103 20011012 00103 NM 2001 10 12 2001UALA02076 1 20010918 A 5754 STRUCTURE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LE FLAP DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7266U 21413 DENT ON NR 8 LEADING EDGE KRUEGER FLAP FOUND APPROXIMATELY 5 INCHES LONG, 0.750 INCHES WIDE AND 0.250 INCHES DEEP. DENT REPAIRED. MAJOR REPAIR ACCOMPLISHED. 2 L 7 3 4F 4 F A3WE E2EA 2001101800006 20011018 00006 NM 2001 10 18 2001UALA02077 1 20010909 A 3350 900835A BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7461U 21915 RT FORWARD AND REAR OVERWING EMERGENCY EXIT LIGHTS ARE INOPERABLE. REPLACED BATTERY PACK. OPERATIONS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001101200104 20011012 00104 NM 2001 10 12 0103466302 1 20010930 A 3397 CONNECTOR BOEING 747 747451 1384940 NM CABIN DAMAGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 662US 23720 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE FROM ROWS 26ABC - 36ABC AND FROM ROW 11JK - DOOR 2R. REPAIRED ELECTRICAL CONNECTORS. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2001101800007 20011018 00007 NE 2001 10 18 2001UALA02079 2 20010921 A 7297 420437 HARNESS BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 1 ENGINE DEFECTIVE A UALA O OTHER S AFFECT SYSTEMS DE DESCENT 1 WP 29 668UA 8563 8563 30024 727869 AUTO THROTTLE DISCONNECTED ON DESCENT WITH LEFT ENGINE CONTROL ROLL EICAS MSG. RE-ENGAGED AUTO THROTTLE AND DISCONNECTE D AGAIN. INTERMITTENT HARNESS PROBLEM BETWEEN THE PERMANENT MAGNET ALTERNATOR (PMA) AND THE ELECTRONIC ENGINE CONTROL (E EC) CAUSED THE EEC A-CHANNEL TO SET THE A-CHANNEL POWER FAIL MESSAGE WITH ENGINE REVERSION TO ALTERNATE MODE OPERATION. AUTO THROTTLE IS NOT OPERABLE IN THE ALTERNATE (N1) MODE. ENGINE WAS REPLACED. ENGINE HARNESS BETWEEN THE PMA AND EEC WAS REPLACED ALONG WITH THE PMA AND EEC. TEST CELL RUN CONFIRMED NORMAL OPERATION. HARNESS IS UNDER INVESTIGATION. 2 L 7 2 4F 4 F RT A1NM E24NE 2001101200105 20011012 00105 NM 2001 10 12 0103475534 1 20011001 A 2120 SMOKE BOEING 757 757251 1384970 NM CABIN DETECTED A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 534US 24265 DURING CRUISE AT 41,000 FT, A BURNING SMELL WAS NOTICED IN THE FLIGHT DECK. LEAD FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. SMOKE IN THE AIRCRAFT DISSIPATED AFTER SMOKE CHECK LIST WAS COMPLIED WITH BUT RETURNED DURING APPROACH. MAINTE NANCE CHECKED OPERATION OF OVENS, COFFEEMAKERS, HOT PLATES, INTERIOR LIGHTS, LAV HOT WATER HEATERS, LAV FLUSH MOTORS, AN D RECIRCULATION FANS. CHECKED E/E COMPARTMENTS, AND CB PANELS. PERFORMED ENGINE HIGH POWER RUNUP AND OPERATED PACKS. APU CHECKED OK. NO TROUBLE FOUND. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2001101800008 20011018 00008 NM 2001 10 18 2001UALA02080 1 20010925 A 2710 252T1172 LINK BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE AILERON WORN A UALA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 WP 29 617UA 21877 WITH HYDRAULICS PRESSURIZED LEFT INBOARD AILERON CAN BE PHYSICALLY MOVED UPWARD APPROX 5 INCHES. EXCESSIVE WEAR IN THE S UPPORT BEARINGS OF THE INBOARD AND OUTBOARD ACTUATOR HANGER LINK ASSEMBLIES. SUBJECT HANGER LINK ASSEMBLIES ARE PART OF THE REACTION LINK ASSEMBLIES THAT DIRECTLY AFFECT THE MOVEMENT OF THE LT INBOARD AILERON. REPLACED BOTH SUBJECT HANGER LINK ASSEMBLIES PER APPLICABLE MAINTENANCE PROCEDURES. OPS CHECKED AILERON SYSTEM PER APPLICABLE MAINTENANCE PROCEDURE S AND ALL OPS CHECKS WERE NORMAL. BOTH LEFT AND RIGHT POWER CONTROL ACTUATORS OF THE LEFT INBOARD AILERON WERE REPLACED AS PRECAUTION. 2 L 7 2 4F 4 F RT A1NM E3NE 2001101200106 20011012 00106 EA 2001 10 12 COMA0160801 1 20011005 A 5300 6003603023 FRAME CNDAIR CL600 CL6002B19 EA DOOR FRAME CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 708CA 7937 7235 L/H FRAME AT F.S. 718.00 BETWEEN STRINGERS 11 AND 12 IS CRACKED.PERFORMED A REPAIR ON THE 718.00 FRAME BETWEEN STRINGERS 11 AND 12 I/A/W CANADAIR REO 601R-53-61-193 REV A. 2 L 7 2 4F RT A21EA 2001101200108 20011012 00108 NM 2001 10 12 UPS01537002 1 20011002 A 5340 BAC15061108 BEAM BOEING 757 75724APF 1384969 NM 131,100 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 404UP 23726 INSPECTION TYPE:C CORROSION (CP53-131-01.02-1I) ON SEAT TRACK LONGITUDINAL BEAM BETWEEN BS 900 & BS 1040 LBL 45, WL 208 REMOVED, FABRICATED AND INSTALLED FABRICATED BEAM FROM BS 900-1040. WORK DONE IAW SRM 53-00-51, 51-40-05, 51-20-01, 51-20-05. 2 L 7 2 4F RT A2NM 2001101900078 20011019 00078 SO 2001 10 19 C2XA01BT169 1 20011005 A 3260 PROXIMITY SWITCH EMB 145 EMB145ER SO LANDING GEAR DIRTY A C2XA O OTHER N FALSE WARNING UK UNKNOWN 1 SW 27 14939 145030 EWR---CO4143 CREW REPORTED LANDING GEAR INDICATION DISAGREEMENT. AFTER TROUBLESHOOTING PROBLEM, MAINTENANCE CLEANED LAN DING GEAR PROXIMITY SWITCHES IAW EMB145 MM CHAPTER 32-61-00. AIRCRAFT TEST FLOWN SATISFACTORY AND RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2001101200109 20011012 00109 SO 2001 10 12 C2XA01IA369 1 20011005 A 3260 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A C2XA K NONE N FALSE WARNING CL CLIMB 1 SW 27 22727 120177 FLIGHT 3447 - CREW REPORTED THAT THE LANDING GEAR SYSTEM DID NOT INDICATE THE RIGHT MAIN GEAR AS BEING RETRACTED. THE A IRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE PERFORMED A LANDING GEAR EXTENSION AND RETRACTION TEST IAW EMBR AER EMB-120 MAINTENANCE MANUAL. NO DEFECTS WERE NOTED DURING THE TEST AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI CE. 2 L 7 2 4T RT A31SO 2001101200110 20011012 00110 EA 2001 10 12 COMA0160802 1 20011003 A 5300 6003603032 DOUBLER CNDAIR CL600 CL6002B19 EA DOOR FRAME CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 708CA 7937 7235 R/H AFT DOUBLER AT F.S.718.00 BETWEEN STRIGER 11 AND 12 IS CRACKED.REMOVED CRACKED R/H AFT DOUBLER AT F.S. 718.00 AND IN STALLED NEW DOUBLER I/A/W CANADAIR REO 601R-53-61-193 REV A. 2 L 7 2 4F RT A21EA 2001101200111 20011012 00111 SO 2001 10 12 C2XA01TY154 1 20011010 A 3210 14567115403 HOUSING EMB 145 EMB145 SO RT MLG GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND LANDING GEAR SIDE BRACE, AFT UPPER HOLLOW PIN BEARING HOUSING WAS FOUN D TO BE GOUGED. MAINTENANCE ACCOMPLISHED THE BLEND OUT REPAIR IAW EMBRAER GST-3363/01 AND SRM 51-10-01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001101200112 20011012 00112 SO 2001 10 12 C2XA01TY155 1 20011010 A 2750 3634001019 SHAFT EMB 145 EMB145 SO T/E FLAP BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS DURING A SCHEDULED INSPECTION THE NR 1 FLAP FLEX SHAFT ON THE RIGHT HAND SIDE WAS FOUND BROKEN. MAINTENANCE REMOVE D AND REPLACED THE FLAP FLEX SHAFT IAW EMB-145 MM 27-51-06, OPERATIONAL CHECKS WERE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001101200113 20011012 00113 EA 2001 10 12 COMA0160803 1 20011010 A 5220 ESCAPE HATCH CNDAIR CL600 CL6002B19 EA A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 809CA 7366 FLIGHT #5354 - CREW ESCAPE HATCH EXTREMELY LOUD DURING T/O, AIRCRAFT RETURNED TO THE FIELD.REMOVED, INSPECTED AND REINST ALLED CREW ESCAPE HATCH. NO DEFECTS WERE FOUND. CABIN PRESSURE CHECK WAS NORMAL. 2 L 7 2 4F RT A21EA 2001101200114 20011012 00114 SO 2001 10 12 C2XA01TY156 1 20011010 A 2750 3634001019 SHAFT EMB 145 EMB145 SO LT WING BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS DURING A SCHEDULED INSPECTION THE NR 1 FLAP FLEX SHAFT ON THE LEFT HAND SIDE WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE FLAP FLEX SHAFT IAW EMB-145 MM 27-51-06, OPERATIONAL CHECKS WERE SATISFACTORY. THE AIRCRAFT WILL BE R ELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001101200115 20011012 00115 SO 2001 10 12 C2XA01TY157 1 20011010 A 5312 14521811403 BULKHEAD EMB 145 EMB145 SO FUSELAGE DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS DURING A SCHEDULED INSPECTION THE AFT PRESSURE BULKHEAD WAS FOUND TO BE DENTED BEYOND MANUFACTURES LIMITS. MAINTEN ANCE ACCOMPLISHED A DOUBLER REPAIR IAW EMRAER GST-3336/01, REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001101200116 20011012 00116 EA 2001 10 12 COMA0160804 1 20011010 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 916CA 7014 FLIGHT #5625. CARGO DOOR CAUTION MESSAGE AFTER T/O. AIRCRAFT RETURNED TO CVG.MAINTENANCE DEFERRED THE CARGO DOOR WARNI NG SYSTEM PER MEL. 2 L 7 2 4F RT A21EA 2001101200117 20011012 00117 EA 2001 10 12 M01110 1 20010920 A 3300 1317 BULB CNDAIR CL600 CL6002B19 EA GE CF34 CF34* NE LT AFT WING FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 97325 7325 DURING SCHEDULED MAINTENANCE, THE CREW FOUND THE LEFT HAND WING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE B ULB, OPS CHECKED GOOD AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2001101200118 20011012 00118 EA 2001 10 12 M01091 1 20010815 A 3300 363782 LIGHT CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE DIRTY CONNECTOR INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17175 7175 DURING A PREFLIGHT INSPECTION, THE CREW FOUND THE FIRST THREE SECTIONS OF THE FLOOR TRACK LIGHTING INOPERATIVE. MAINTEN ANCE CLEANED THE CONNECTIONS. OPS CHECKED GOOD AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2001101200121 20011012 00121 2001 10 12 GLBA2001209 4 20010928 A 3425 6229682002 COMPUTER BEECH 1900 1900D 1154162 CE COCKPIT FAILED A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 210GL 15620 UE210 COPILOTS EFIS DISPLAY FAILED INFLIGHT. REPLACED DPU, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001101200122 20011012 00122 SO 2001 10 12 GLBA2001212 1 20011003 A 3260 922A2YA6PZ722A DOWNLOCK SENSOR EMB 120 EMB120ER 3260203 SO RT MLG SHORTED A GLBA O OTHER O OTHER LD LANDING 1 CE 01 71GL 120071 LANDING GEAR WOULD NOT EXTEND, ELECTRIC OVERRIDE USED. REPLACED RIGHT (A) SYSTEM DOWNLOCK PROX SENSOR, OPS CHECKED SYST EM SATISFACTORY. 2 L 7 2 4T RT A31SO 2001101200124 20011012 00124 WP 2001 10 12 ARWA0011005 1 20011010 A 3233 4771392 PIN DOUG DC8 DC862 3021970 WP A ARWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 810BN 45905 LOG PAGE 105745. DISCREPANCY:GEAR NOT LATCHED LIGHT ON, DOOR NOT LATCHED LIGHT ON, AIRCRAFT DIVERTED TO SJU AND ACCOMPLI SHED AN UNEVENTFULL LANDING.AIRCRAFT PERFORMED AN OVERWEIGHT LANDING. CORRECTIVE ACTION:FOUND LEFT HAND MAIN GEAR RETRAC T ACTUATOR PIN BROKEN. REMOVED AND REPLACED LEFT MAIN GEAR RETRACT PIN IAW SB 32-102. OVERWEIGHT LANDING INSPECTION ACCO MPLISHED PER DC8 MM J/C 6372. 2 L 7 4 4F 4A25 2001101200125 20011012 00125 WP 2001 10 12 MWEA011381 1 20011011 A 5340 591140125 LONGERON DOUG DC9 DC981 3022081 WP STA 148 TO 180 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 E AND E BAY LONGERON 25 HAS MODERATE CORROSION FROM STATION 148 TO STATION 180 -- REMOVED AND INSTALLED LONGERON 25. 2 L 7 2 4F A6WE 2001101200126 20011012 00126 WP 2001 10 12 MWEA011385 1 20011011 A 5230 59101415 DOUBLER DOUG DC9 DC981 3022081 WP AFT CENTER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 SUSPECTED CRACK EMINATING OUT FROM UNDER AFT CENTER STOP FITTING ON FORWARD CARGO DOOR -- FABRICATED AND INSTALLED DOU BLER. 2 L 7 2 4F A6WE 2001101200127 20011012 00127 WP 2001 10 12 MWEA011386 1 20011011 A 5330 59360021 LONGERON DOUG DC9 DC981 3022081 WP STATION 769 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 FUSEALAGE SKIN (MID BAG C0MPARTMENT) HAS A DAMAGED HOLE AT STATION 769 BETWEEN LONGERON 26 RIGHT TO LONGERON 25 RIGHT. 2 L 7 2 4F A6WE 2001101200128 20011012 00128 WP 2001 10 12 MWEA011387 1 20011011 A 5330 59360041 DOUBLER DOUG DC9 DC981 3022081 WP STATION 758 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 REPAIR DOUBLER ON FUSELAGE SKIN AT STATION 758 TO 780 FROM LONGERON 27 RIGHT TO 28 RIGHT REMOVED TO FACILITATE OTHER MAI NTENANCE -- FABBED AND INSTALLED FILLER, REPLACE DOUBLER AND TRIPLER. 2 L 7 2 4F A6WE 2001101200129 20011012 00129 EA 2001 10 12 MASA01084 1 20010805 A 2700 SPOILER CNDAIR CL600 CL6002B19 EA GE CF34 CF34* NE OUTTER WING BROKEN A MASA K NONE F FLT CONT AFFECTED CR CRUISE 1 SW 07 17337 7337 RIGHT FLIGHT SPOILER DEPLOY IN FLIGHT. THE CREW WAS ABLE TO OVERCOME THE ACTION OF THE SPOILER AND CONTROL THE AIRCRAFT IN FLIGHT. THE SPOILER WOULD NOT RETRACT AND WHEN THE AIRCRAFT ARRIVED AT THE GATE THE SPOILER WAS STILL FULLLY DEPLOY ED AND THE ATTACHMENT BRACKET WAS BROKEN. MACHANIC WAS CALLED, REMOVED AND REPLACED THE SPOILER, OP CHECKS GOOD. THE A IRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2001101200130 20011012 00130 2001 10 12 MALA010726 4 20010921 A 3417 HC396H0485008 DAU BAC 146 AVRO146RJ85A 1500097 EU E/E BAY FAULTY A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 507XJ E2316 ON DEPARTURE OFF OF MSP RECEIVED A RUDDER LIMITER ANNUNCIATOR AT 200 KIAS, NOTIFIED MTX CONTROL, ADVISED TO RETURN TO MS P. AT DECELERATION BELOW 190 KIAS ANNUNCIATOR WENT OUT, AND REMAINED OUT FOR THE REST OF APP. ALSO ANYTIME FLT IDLE WA S SELECTED GEAR HORN WENT OFF, REGARDLESS OF SPEED. MAINTENANCE FOUND ADAU AT FAULT, WILL NOT TEST. REPLACED ADAU PN H C396-HO485-008, SN/ON ULT-0076-97, SN/OFF 559WDFD97. ADAU OPS CHECK GOOD AVRO MM CHAP 34-18-00. 2 H 7 4 4F RT A49EU 2001101200131 20011012 00131 EU 2001 10 12 MALA010727 1 20010927 A 2120 ODOR SAAB SF340 340B 7860101 EU CABIN DETECTED A MALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 438XJ 340B438 DURING FLIGHT 2745 THE F/A REPORTED A RUMBLE SOUND FROM FLOOR FOLLOWED BY AN ELECTRICAL SMELL. AC RETURNED TO GATE. MA INTENANCE RAN SUPPLEMENTAL AC FOR AWHILE, NO RUMBLING OR FUMES NOTED. OPS CHECK GOOD. RAN RECIRC FAN ON BOTH SETTINGS, NO DISCREPANCY, NO RUMBLING NOTED FOR THE DURATION OF ALL. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2001101200132 20011012 00132 EU 2001 10 12 MALA010728 1 20010930 A 2797 CONNECTOR SAAB SF340 SF340A 7850100 EU TRIM ACTUATOR DIRTY A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 112XJ 112 AFTER T/O ON FLIGHT 2904 MAIN PITCH TRIM FOUND TO BE INOP. MAIN PITCH TRIM FAILED ON CLIMBOUT, INOP FROM BOTH CAPTS AND F/O'S SIDE. STANDBY TRIM OPERATES NORMALLY AFTER ABOUT 10 MINUTES MAN TRIM STARTED WORKING MOMENTARILY. AIR TURNBACK TO DTW. MAINTENANCE CLEANED CANNON PLUG A MAIN PITCH TRIM ACTUATOR. 2 L 7 2 4T RT A52EU 2001101200133 20011012 00133 WP 2001 10 12 MWEA011369 1 20011004 A 3010 P2027 ANTI-ICE SYSTEM DOUG DC9 DC932 3022066 WP TAIL FAULTY A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 215ME 47744 LEFT ICE PROTECTION TEMP HIGH LIGHT CAME ON. PERFORMED QRH AND LEFT TEMP HIGH LIGHT WENT OUT BUT GOT A PRESSURE ABNORMA L LIGHT ON AND THE LEFT ICE PROTECTION TEMP LOW LIGHT CAME ON. REMOVED AND REPLACED ICE PROTECTION CONTROL ANTICIPATOR. 2 L 7 2 4F A6WE 2001101200134 20011012 00134 EU 2001 10 12 MALA010742 1 20011005 A 7720 CT79B ENGINE SAAB SF340 340B 7860101 EU CT7TP CT79B 30030 NE A MALA A E UNSCHED LANDING ENGINE SHUTDOWN Y ENGINE STOPPAGE CR CRUISE 1 GL 15 451XJ 340B451 During Flight #3071, RH Engine failed 600'AGL after Takeoff. ITT exceeded 1000 degressC. ORH performed. No fire. Maint enance replaced RH Engine with serviceable unit. See Engine Change Task Cards for details. PN CT7-9B, SN/off GE-E78575 0, SN/on GE-E785181. All checks good. 2 L 7 2 4T 4 T RT A52EU E8NE 2001101200135 20011012 00135 WP 2001 10 12 NACA20010034 1 20010927 A 2110 75372415507 SUPERCHARGER DOUG DC6 DC6 3021702 WP NR 1 MAKING METAL A NACA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AL 03 43872 2886 2195 533294 EN ROUTE, SMOKE IN COCKPIT. SHUTDOWN CABIN HEATERS, ELIMINATED SMOKE. SUSPECT NR 1 SUPERCHARGER SYSTEM. PULLED MAGNET IC PLUG ON THE NR 1 CSC, FOUND TO BE FULL OF METAL. SYSTEM DEFERRED PER MEL 21-1 AT 0800 ON 9-27-01Z. CSC TO BE REPLAC ED. 2 L 7 4 4R A781 2001101200136 20011012 00136 NE 2001 10 12 NACA20010035 2 20011004 A 8530 356994 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 4 ENGINE CRACKED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS AP APPROACH 1 AL 03 2907F 2765 2765 533265 CP450668 SHUTDOWN NR 4 ENGINE AT 2345Z DUE TO BACKFIRE AND LOW BMEP. REMOVED AND REPLACED THE NR 17 CYLINDER. 2 L 7 4 4R 4 R A781 5E8 2001101200137 20011012 00137 EU 2001 10 12 PNSA010902 1 20010916 A 7797 CONNECTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE DIRTY A PNSA A UNSCHED LANDING O OTHER CL CLIMB 1 AL 03 675PA 340B206 ON CLIMBOUT FROM ANC RT ENGINE ITT GAUGE STARTED FLUCTUATING NO OTHER UNUSUAL INDICATIONS. MAINTENANCE CONTACTED ON RAD IO AND AIRCRAFT RETURNED TO ANC. MAINTENANCE CLEANED ITT YELLOW HARNESS CANNON PLUG AT ENGINE AND GROUND RUN AIRCRAFT O K. 2 L 7 2 4T 4 T RT A52EU E8NE 2001101200138 20011012 00138 SW 2001 10 12 PNSA010904 1 20010920 A 3411 PITOT HEAD SWRNGN SA227 SA227AC 8780603 SW PITOT/STATIC SYS BLOCKED A PNSA A UNSCHED LANDING O OTHER CL CLIMB 1 AL 03 2719H AC713B DURING CLIMB FROM ANC CAPTAINS AIRSPEED INDICATOR WAS READING LOW COMPARED TO COPILOTS SIDE. AIRCRAFT RETURNED TO ANC W HERE MAINTENANCE FOUND PITOT HEAD PARTIALLY BLOCKED WITH FOREIGN OBJECT. 2 L 7 2 4T RT A8SW 2001101200140 20011012 00140 EU 2001 10 12 SABA011050 1 20011002 A 2820 1349305A73 FUEL LINE BAG JETSTM JETSTM3201 1500217 EU FUEL SYS KINKED A SABA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 33 966AE 966 FLIGHT 5018 CLT TO OAJ ABORTED TAKEOFF, LEFT FUEL CAPTION LIGHT ILLUMINATING AT 70 KNOTS. AIRCRAFT RETURNED TO GATE WIT H NO OTHER PROBLEMS. MAINTENANCE FOUND THE MAIN FUEL SUPPLY LINE KINKED. REMOVED AND REPLACED FUEL LINE, RUN, LEAK AND OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A56EU 2001101200142 20011012 00142 EU 2001 10 12 SABA011052 1 20011009 A 7712 31024766 SIGNAL COND UNIT BAG JETSTM JETSTM3201 1500217 EU NR 2 ENGINE OUT OF ADJ A SABA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 33 961AE 961 AIRCRAFT 961 ON FLIGHT 5093 FROM CHARLOTTE TO AUGUSTA; ON ARRIVAL TO THE AUGUSTA AREA THE NUMBER TWO-ENGINE TORQUE INDIC ATION WAS READING ERRATIC AND FLUCTUATING FROM 0 TO 20 PERCENT. THIS CAUSING THE AIRCRAFT TO START SURGING TO THE RIGHT . NUMBER TWO ENGINE WAS SHUTDOWN. AN IN-FLIGHT EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED AT AUGUSTA WITH NO OTHER P ROBLEMS. MAINTENANCE FROM CHARLOTTE MOVED THE TORQUE SIGNAL CONDITIONER FROM BRIDGE TWO TO BRIDGE ONE. MAINTENANCE GRO UND RUN THE AIRCRAFT AND MADE ADJUSTMENTS TO THE SIGNAL CONDITIONER. AIRCRAFT GROUND RUN AND OPS CHECKED GOOD. AIRCRAF T WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A56EU 2001101200143 20011012 00143 NM 2001 10 12 SCNA01712 1 20010922 A 2613 OVERHEAT LOOP BOEING 727 727282 138408T NM OVERHEAT DETECT DEFECTIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 281SC 21949 LOWER AFT BODY OVERHEAT LIGHT WILL NOT ILLUMINATE WHEN TEST BUTTON IS PUSHED, WILL ILLUMINATE IF LIGHT IS PUSHED DIRECTL Y. CORRECTED BY REMOVING AND REPLACING OVERHEAT DETECTOR. 2 L 7 3 4F RT A3WE 2001101200144 20011012 00144 NM 2001 10 12 SCNA01713 1 20010921 A 2612 FIRE LOOP BOEING 727 7272J4 1384006 NM NR 3 ENGINE FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 290SC 20764 NR 3 ENGINE B-LOOP FIRE WARNING TEST INOPERATIVE. MEL'D NR 3 ENGINE B-LOOP FIRE WARNING. 2 L 7 3 4F RT A3WE 2001101200145 20011012 00145 NM 2001 10 12 SCNA01715 1 20010924 A 3350 LIGHT BOEING 727 7272J4 1384006 NM EXTERIOR INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 284SC 21438 RIGHT AFT OVERWING EXTERIOR EMERGENCY LIGHT INOPERATIVE. CORRECTED BY CLEANING AND RESECURING WING FAIRING DISCONNECT L IGHT. 2 L 7 3 4F RT A3WE 2001110800029 20011108 00029 NM 2001 11 8 2001UALA02084 1 20010926 A 3233 654491012 ACTUATOR BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE RT MLG FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 976UA 21598 UNSCHEDULED LANDING UNDER AMBER ALERT DUE TO A RED GEAR LIGHT INDICATION. FLIGHT CREW REPORTED AFTER TAKEOFF, AT LANDIN G GEAR RETRACTION WITH GEAR HANDLE IN OFF POSITION HAD RIGHT MAIN GEAR RED UNSAFE LIGHT INDICATION. DURING TROUBLESHOOT ING FOUND RIGHT GEAR DID NOT FULLY RETRACT AND STOPS SEVERAL INCHES SHORT OF BEING FULLY UP, THEN MOVES SLOWLY UPWARD AN D MUST BE MANUALLY PUSHED TO FULL UP POSITION. WITH GEAR FULLY UP, ALL COCKPIT GEAR INDICATIONS WERE NORMAL. REMOVED A ND REPLACED RIGHT MAIN LANDING GEAR RETRACT ACTUATOR ASSEMBLY. ACTUATOR FAILED THE INTERNAL LEAKAGE TEST AND APPEARS TO BE BYPASSING THE PISTON SEALS. 2 L 7 2 4F 4 F A16WE E2EA 2001101500002 20011015 00002 NM 2001 10 15 2001UALA02085 1 20010926 A 3350 1315 LAMP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7288U 21566 EMERGENCY EXIT LIGHTING IN FIRST CLASS AISLE IS INOPERABLE. *S/D* LAMPS FAILED. REPLACED LAMPS. OPERATIONS CHECK NOR MAL. 2 L 7 3 4F 4 F A3WE E2EA 2001110800030 20011108 00030 NM 2001 11 8 2001UALA02088 1 20010928 A 3233 654491027 ACTUATOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RT MLG FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 321UA 23953 CREW REPORTS RT MAIN GEAR EXTENDED WHEN LANDING GEAR HANDLE PLACED TO OFF POSITION. CREW SAW NO TRANSIT LIGHT BUT ON DE SCENT THE RT GEAR INDICATED DOWN AND LOCKED WITH THE SELECTOR HANDLE STILL IN OFF. WHEN HANDLE SELECTED TO DOWN ALL GRE EN LIGHTS ILLUMINATED. INDICATING DOWN AND LOCKED. WHILE TROUBLESHOOTING LANDING GEAR PROBLEM, FOUND THAT RIGHT MAIN LA NDING GEAR WOULD NOT ALWAYS GO TO THE FULL UP AND LOCKED POSITION. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR RETRACT ACTUATOR ASSEMBLY. AFTER MLG RETRACT ACTUATOR REPLACEMENT, ACCOMPLISHED SEVERAL GEAR SWING WITH NO PROBLEMS NOTED. AL SO ACCOMPLISHED FREE FALL EXTENSION ON ALL 3 GEARS. SYS OP'S CHECKED GOOD, RETURNED ACFT TO REVENUE SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2001101800009 20011018 00009 NM 2001 10 18 2001UALA02089 1 20010928 A 1420 CONNECTOR BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN LOOSE A UALA K NONE O OTHER CR CRUISE 1 WP 29 603UA 21864 7EF TO BS GALLEY EMERGENCY LIGHTS COME ON INTERMITTENTLY THROUGHOUT FLIGHT. SECURED CONNECTION AT BATTERY PACK AT SEAT 1 EF SIDEWALL. ALL EEL STRIPS NOW TEST OK. 2 L 7 2 4F 4 F RT A1NM E3NE 2001121700098 20011217 00098 NE 2001 12 17 2001UALA02090 2 20011001 A 7230 8198021 ACTUATOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LT ENGINE SEIZED A UALA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 WP 29 779UA 717 26941 777006 LEFT ENGINE WOULD NOT COME OUT OF IDLE. DIVERTED TO CCS. LEFT ENGINE WENT INTO SUB-IDLE STALL ACCOMPANIED BY STATOR VA NE FAULT MSG. LATER DURING DESCENT TO DIVERSION STATION, ENG FAIL MSG ILLUMINATED & FLIGHT CREW SHUT THE ENGINE DOWN AN D MADE A SINGLE-ENGINE LANDING. MAINT REPLACED THE STATOR VANE ACTUATOR (SVA), ENGINE PASSED ALL INSPECTIONS & RUN-UPS AND WAS RETURNED TO SERVICE. THE REMOVED ACTUATOR, WHICH HAD BEEN PREVIOUSLY MODIFIED PER SERVICE BULL. 75-10, WAS SENT TO THE OEM HAMILTON-SUNDSTRAND FOR INVESTIGATION. HS RPTD THAT THE LINEAR VARIABLE DIFFERENTIAL TRANSDUCER (LVDT) WITH IN THE SVA WAS SEIZED & THE FLAT PIN FRACTURED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001102600024 20011026 00024 NM 2001 10 26 2001UALA02091 1 20010826 A 2120 213W31501 BEARING BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RAM AIR DOOR WORN A UALA J A DUMP FUEL UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 29 773UA 26929 VIBRATION REPORTED IN CLIMB STARTING AT FL200. VIBRATION COMING FROM COCKPIT FLOOR AND ROW 12 FWD IN PAX CABIN. UPON L EVEL OFF FL300, VIBRATION DID NOT GO AWAY, WITH CABIN CREW REPORTING IT WAS GETTING WORSE. DUMPED FUEL AND RETURN TO IA D. INSPECTED AIRFRAME AND FOUND WORN BEARING AT INBOARD END CAP OF RIGHT PACK RAM AIR INLET DOOR TORQUE TUBE. REPLACED END CAP. AIRCRAFT RETURNED TO REVENUE SERVICE WITHOUT FURTHER VIBRATION REPORT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001110800031 20011108 00031 NM 2001 11 8 2001UALA02092 1 20011001 A 2920 HYDRAULIC SYSTEM BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE B SYSTEM MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 7452U 21906 AIRCRAFT LOST B-SYSTEM HYDRAULIC PRESSURE IN FLIGHT. THE AIRCRAFT DIVERTED TO DTW. HYDRAULIC SYSTEM CHECKED PER THE 727 MAINTENANCE MANUAL. NO FAULTS FOUND. NO HYDRAULIC ISSUES IN AIRCRAFT HISTORY SINCE THIS INCIDENT. 2 L 7 3 4F 4 F A3WE E2EA 2001111400026 20011114 00026 NM 2001 11 14 2001UALA02093 1 20011003 A 2721 CONTROL UNIT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RUDDER MALFUNCTIONED A UALA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 565UA 26669 RUDDER REQUIRES 6 UNITS OF LEFT TRIM. ACCOMPLISHED TROUBLESHOOTING OF RUDDER TRIM AND RUDDER RATIO SYSTEMS AND EXAMINED RATIO CHANGER SHEAR PINS. NO DISCREPANCIES FOUND, AIRCRAFT RETURNED TO SERVICE WITHOUT FURTHER GRIPES ABOUT EXCESSIVE TRIM REQUIRED. 2 L 7 2 4F 4 F RT A2NM E17NE 2001101500003 20011015 00003 NM 2001 10 15 SWAA012765 1 20011008 A 5754 6573714 SLAT BOEING 737 7373Q8 1384670 NM LH WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED C4 CHECK, FOUND # 2 L/E SLAT CRACKED .75 INCH LONG AT INBD LOWER T/E. REPAIRED # 2 SLAT PER SWA RA 1-357-1114. 2 L 7 2 4F RT A16WE 2001101500004 20011015 00004 2001 10 15 SWAA012768 4 20011008 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 611SW 27697 FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001101500005 20011015 00005 NM 2001 10 15 SWAA012771 1 20011009 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACK ( 2 EA ) AT BS 932, STR 24L & BS 930, STR 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001101500006 20011015 00006 2001 10 15 SWAA012773 4 20011008 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 611SW 27697 FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001101500007 20011015 00007 2001 10 15 SWAA012774 4 20011009 A 2565 6556685 BRACKET BOEING 737 7377H4 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 718SW 27852 FWD ENTRY DOOR EMERGENCY EVAC SLIDE CONTAINER RH ATTACH BRACKET LOOSE. SECURED BRACKET PER MM. 2 L 7 2 4F RT A16WE 2001101500008 20011015 00008 2001 10 15 SWAA012775 4 20011008 A 2565 D31354 SLIDE BOEING 737 7377H4 NM AFT SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 785SW 30602 AFT SVC DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001101500009 20011015 00009 NM 2001 10 15 SWAA012776 1 20011009 A 3350 90083 BATTERY BOEING 737 7375H4 138449D NM CABIN ERRATIC A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED PM CHECK, FOUND AFT CABIN EMERGENCY LIGHTS ON WHEN SWITCH IS OFF. R&R BAT TERY PER MM. 2 L 7 2 4F RT A16WE 2001101500010 20011015 00010 NM 2001 10 15 SWAA012778 1 20011009 A 5310 6547978 WEB BOEING 737 7373Q8 1384670 NM MID CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 637, STR 17L. R&R WEB PER SR M. 2 L 7 2 4F RT A16WE 2001101500011 20011015 00011 NM 2001 10 15 SWAA012780 1 20011008 A 3350 BR2013 COVER BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVER MISSING AT ROW 14. INSTALLED COVER PER MM. 2 L 7 2 4F A16WE 2001101800010 20011018 00010 NE 2001 10 18 2001UALA02094 2 20010811 A 7530 SHUTOFF VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT ENGINE FAILED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 647UA 25284 LEFT ENG HPSOV EICAS DURING CLIMB AND CRUISE. REPLACED LT ENG HPSOV. FAULT WAS IN HPC. 2 L 7 2 4F 4 F RT A1NM E24NE 2001101500012 20011015 00012 NM 2001 10 15 SWAA012781 1 20011010 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED ( 3 EA ) AT BS 944, STR 25R, BS 931, STR 25R & BS 937, STR 2 1L. REPIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001101500013 20011015 00013 NM 2001 10 15 SWAA012783 1 20011009 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 394SW 27380 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVER CRACKED AT ROW 17. R&R EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2001101500014 20011015 00014 NM 2001 10 15 SWAA012784 1 20011009 A 5753 6546435 FLAP BOEING 737 7373H4 1384600 NM LH WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 344SW 24152 DURING SCHEDULED BC3 CHECK, FOUND OTBD T/E AFT FLAP DELAMINATED. R&R OTBD T/E AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2001101500015 20011015 00015 NM 2001 10 15 SWAA012785 1 20011009 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 1.7 INCH LONG AT BS 870, STR 23R. RE PAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001101500016 20011015 00016 NM 2001 10 15 SWAA012786 1 20011010 A 5320 6547977 WEB BOEING 737 7373Q8 1384670 NM CORRODED CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED D CHECK, FOUND WEB CORRODED AT BS 296, RBL 50 & WL 208. REPAIRED WEB PER MM. 2 L 7 2 4F RT A16WE 2001101500017 20011015 00017 NM 2001 10 15 SWAA012789 1 20011005 A 5310 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CORRODED BETWEEN BS 847 & BS 857, BETWEEN STR 27R & STR 27L. 2 L 7 2 4F RT A16WE 2001101500018 20011015 00018 NM 2001 10 15 SWAA012791 1 20011010 A 5523 65C26384 TAB BOEING 737 7373H4 1384600 NM RH ELEVATOR. DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED 1/4D CHECK, FOUND RH ELEVATOR TAB DELAMINATED NEAR OTBD HINGE ON LOWER SIDE. R&R TAB PER MM. 2 L 7 2 4F RT A16WE 2001101500019 20011015 00019 NM 2001 10 15 SWAA012793 1 20011011 A 5310 6547978 WEB BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 637, STR 17R. R&R WEB SECT ION PER SRM. 2 L 7 2 4F RT A16WE 2001101500020 20011015 00020 NM 2001 10 15 SWAA012795 1 20011010 A 5310 6546569 FRAME BOEING 737 7373Q8 1384670 NM CORRODED CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 967, LBL 2 & WL 171. REPAIRED F RAME PER SRM. 2 L 7 2 4F RT A16WE 2001101500021 20011015 00021 NM 2001 10 15 SWAA012796 1 20011011 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 089SW 22904 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED 2 INCHES LONG AT BS 872.5, STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001102600025 20011026 00025 NM 2001 10 26 2001UALA02095 1 20011004 A 2410 735511 CSD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 376UA 24641 UNSCHEDULED LANDING DUE TO NR 2 GENERATOR INOPERATIVE. SUBJECT AIRCRAFT RETURNED TO FIELD DUE TO REPORTS OF NR 2 ENGINE GENERATOR DROPPING OFF LINE. TROUBLESHOOTING ISOLATED CAUSE TO NR 2 CONSTANT SPEED DRIVE (CSD). NR 2 CSD AND NR 2 GEN ERATOR WERE REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001101500022 20011015 00022 NM 2001 10 15 VNAA0110006 1 20011010 A 2400 GENERATOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LH FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 458PS 3068 DURING TAKE OFF, THE CREW RECEIVED A LEFT HAND GENERATOR FAIL CAS MESSAGE AND ABORTED TAKE OFF. THE CREW COMPLIED WITH THE QUICK REFERENCE HANDBOKK AND RESET THE SYSTEM. FLIGHT 9408 WAS CLEARED FOR ANOTHER TAKE OFF ATTEMPT AND DEPARTED WI TH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001101500024 20011015 00024 NM 2001 10 15 CALA0100944 1 20011012 A 5320 6545808 ANGLE BOEING 737 7373T0 1384582 NM BS 294 R1 FWD CRACKED A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 69333 23571 BS 294 BOX ANGLE CRACKED AT R1 DOOR CUT OUT JUST ABOVE FLOOR BEAM. TRIMMED CRACKED FLANGE. APPLIED ALODINE ADN PRIMER AN D INSTALLED .050 FILLER PER EC/RA 5310-03895. 2 L 7 2 4F RT A16WE 2001101500025 20011015 00025 NM 2001 10 15 CALA0100945 1 20011014 A 5414 311A1450 DOUBLER BOEING 737 7373T0 1384582 NM #2 PYLON GOUGED A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 14335 23573 #2 ENGINE PYLON UPPER LEFT SIDE OF PYLON ACCESS PANEL 5827 SUPPORT FOR PANEL HAS DEEP GOUGES. BLENDED AREA. INSTALLED DO UBLER PER EC/RA 5430-01230. 2 L 7 2 4F RT A16WE 2001101500027 20011015 00027 NM 2001 10 15 ABXA010533 1 20011001 A 5510 BOLT BOEING 767 767231 1385131 NM EMPENNAGE SHEARED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 709AX 22572 THE RIGHT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD ATTACH FITTING HAD A DOME SEALED FASTENER BACKING OFF. MAINTENANCE REPLACED THE FASTENERS IAW B767 SRM 51-40-04. 2 L 7 2 4F RT A1NM 2001101500029 20011015 00029 NM 2001 10 15 AUS20010951 1 20010802 A 2824 737M28500011 VALVE BOEING 737 737376 NM CFMINT CFM56 CFM563C 13802 EU FUEL TRANSFER FAULTY W J DUMP FUEL J WARNING INDICATION CR CRUISE 1 AU S 17862 2563 (AUS) FUEL CROSSFEED VALVE FAULTY. 2 L 7 2 4F 4 F RT A16WE E21EU 2001101500032 20011015 00032 NM 2001 10 15 AUS20010959 1 20010831 A 2750 CONTROLLER BOEING 767 767216 1385121 NM GE CF6 CF680A 30025 NE TE FLAPS MALFUNCTIONED W O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 AU S (AUS) FLAP SYSTEM FAULTY. FLAP DRIVE SYSTEM INSPECTED AND NO FAULTS FOUND. FLAPS CYCLED AND FAULT DISAPPEARED. LIMITED INFORMATION PROVIDED 2 L 7 2 4F 4 F RT A2NM E13NE 2001101500039 20011015 00039 NM 2001 10 15 AUS20010976 1 20010905 A 2910 7972110529 LINE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE HYD SYSTEM WORN W O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 AU S 2236 (AUS) RT OUTBOARD SPOILER ACTUATOR HYDRAULIC PRESSURE PIPE WORN THROUGH BY THE RT WING AILERON CONTROL CABLE. 2 L 7 2 4F 4 F TR A6WE E00061EN 2001101500041 20011015 00041 EU 2001 10 15 AUS20010982 1 20010908 A 2497 M2275934109 WIRE HARNESS SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R320 R3204123F1 NE AC GENERATOR DAMAGED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LT AC GENERATOR WIRING HARNESS DAMAGED. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P5NE 2001101500043 20011015 00043 EU 2001 10 15 AUS20010987 1 20010826 A 4980 38002162 SEAL BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE APU EXHAUST DETERIORATED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 AU S P236AUC (AUS) APU EXHAUST DUCT SHROUD SEAL DETERIORATED. 2 H 7 4 4F 4 F A49EU E6NE 2001101500054 20011015 00054 NM 2001 10 15 AUS20011012 1 20010913 A 5230 6546921528 STRUCTURE BOEING 737 737376 NM CFMINT CFM56 CFM563C 13802 EU CARGO DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S 1026 (AUS) FORWARD CARGO DOOR CRACKED IN FORWARD AND AFT LOWER CORNERS. FOUND DURING EDDY CURRENT INSPECTION IAW AD/B737/142 . 2 L 7 2 4F 4 F RT A16WE E21EU 2001101500055 20011015 00055 SO 2001 10 15 AUS20011015 1 20010905 A 2422 PC2511C INVERTER MARATHON PC2511C EMB 120 EMB120 3260201 SO PWA 118 PW118A NE HAMSTD 14SF 14SF9 NE A/C ELECTRIC SYS FAILED W O OTHER H ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 AU S 961034523855 (AUS) NR 1 AND 2 MAIN INVERTERS FAILED. 2 L 7 2 4T 4 T RT A31SO E20NE 6 N P11NE 2001101500060 20011015 00060 NM 2001 10 15 AUS20011028 1 20010927 A 2824 ACTUATOR BOEING 737 737476 NM CFMINT CFM56 CFM563C 13802 EU FUEL TRANSFER FAULTY W O OTHER J WARNING INDICATION NR NOT REPORTED 1 AU S (AUS) FUEL VALVE WOULD NOT FULLY CLOSE. SUSPECT FAULTY ACTUATOR. 2 L 7 2 4F 4 F RT A16WE E21EU 2001101500061 20011015 00061 2001 10 15 AUS20011029 4 20010927 A 3421 4019700902 INDICATOR BAC 146 146100A 1500260 EU LYC ALF502 ALF502R3A 41580 NE ATTITUDE GYRO FAILED W O OTHER O OTHER CL CLIMB 1 AU S (AUS) FIRST OFFICERS ATTITUDE INDICATOR FAILED. 2 H 7 4 4F 4 F RT A49EU E6NE 2001101500062 20011015 00062 NM 2001 10 15 CA011001009 1 20010921 A 3040 KCD4N RELAY LEACH DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE WINDSHIELD FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) THE FLIGHT CREW REPORTED THE F/O'S WINDSHIELD "MISTING", WITH NO CURRENT DRAW INDICATED ON "C" PHASE OF THE LOADM ETER. MAINTENANCE REPLACED DEICE RELY 3041-K6 WHICH HAD FAILED INTERNALLY. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001101500066 20011015 00066 SO 2001 10 15 SWIA200110195 1 20010920 A 5270 SWITCH EMB 120 EMB120ER 3260203 SO REFUEL DOOR FAILED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 292UX 120292 SERVICE DOOR LIGHT WILL NOT EXTINGUISH. ABORTED TAKEOFF.REPLACED REFUELING RECEPTACLE DOOR MICROSWITCH WITH SERVICEABLE UNIT, OPS CHECKED GOOD. 2 L 7 2 4T RT A31SO 2001101500067 20011015 00067 NE 2001 10 15 SWIA200110196 2 20010921 A 7200 ENGINE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NR 2 MALFUNCTIONED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 393SW 120330 ON CLIMB OUT OF SEA, 100 PERCENT NP & 84 PERCENT TQ, NP FLUCTUATIONS NOTED ON NR 2 ENGINE. NP SWIFTLY OSCILLATED BETWEE N 96 PERCENT TO 100.5 PERCENT, ACCOMPANIED WITH YAWING. PROP SYNC DESELECTED HAD NO EFFECT. TORQUE FLUCTUATIONS WERE A PPROXIMATELY 2-3 PERCENT. APPEARED TO BE RESULT OF NP FLUCTUATION RATHER THAN CAUSE. RETURNED TO SEATTLE.INSPECTED ENGI NE AND PROPELLER CONTROL LINKAGES. PERFORMED ENGINE RUN UP. NP FLUCTUATION NOT OBSERVED DURING RUN UP. NP WITHIN LIMIT S. 2 L 7 2 4T 4 T RT A31SO E20NE 2001101500070 20011015 00070 SO 2001 10 15 SWIA200110197 1 20010919 A 3251 12037995001 CONTROL ARM EMB 120 EMB120RT SO NLG MALFUNCTIONED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 161CA 120143 NOSE WHEEL STEERING PULLS LEFT WITH OR WITHOUT TILLER ENGAGED. ABORTED TAKEOFF BELOW 80 KNOTS. CENTERED FEEDBACK POT AND REPLACED NOSE WHEEL STEERING TILLER. OPS CHECK GOOD ON TAXI. 2 L 7 2 4T RT A31SO 2001101500071 20011015 00071 2001 10 15 SWIA200110198 4 20010923 A 3425 INDICATOR EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING I FLT. ATTITUDE INST. CL CLIMB 1 NM 07 226SW 120296 LT ATTITUDE INDICATOR FAILED ON CLIMBOUT. ATTITUDE DISPLAY ON MAP ILLUMINATED. FIRST OFFICER INDICATED ERRONEOUS READI NGS ON THE FIS ON HIS SIDE.PERFORMED OPS CHECK OF CAPTAIN ADI AND COPILOT FIS. FOUND TO OPS CHECK GOOD AT THIS TIME. O K FOR SERVICES. 2 L 7 2 4T RT A31SO 2001101500072 20011015 00072 SO 2001 10 15 SWIA200110199 1 20010922 A 2730 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO ELEVATOR TRIM FAILED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 190SW 120050 ABORTED TAKEOFF WHEN WE BROUGHT THE POWER UP DUE TO TAKEOFF TRIM WARNING. TRIM CONFIRMED SET AT 4 IN THE GREEN BAND.REMO VED AND REPLACED LEFT TRIM PROXIMITY SENSOR. OPS CHECK GOOD. P/N: ATG120TR 2 L 7 2 4T RT A31SO 2001101500073 20011015 00073 EA 2001 10 15 SWIA200110200 1 20010923 A 5270 PROXIMITY SWITCH CNDAIR CL600 CL6002B19 EA CARGO DOOR OUT OF ADJ A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 410SW 7066 ON TAKEOFF, HAD A CARGO DOOR CAUTION MESSAGE. PERFORMED ADJUSTMENT/TEST OF CARGO DOOR PROX SWITCHES PER CRJ MM 52-70-02. OPS CHECK FOUND GOOD. 2 L 7 2 4F RT A21EA 2001101500074 20011015 00074 SO 2001 10 15 SWIA200110201 1 20010922 A 3251 2054000101 PROXIMITY SWITCH EMB 120 EMB120ER 3260203 SO NLG STRUT FAILED A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 564SW 120339 AIRCRAFT RUNS TO LEFT ON TAKEOFF ROLL WITH FULL RIGHT RUDDER. ABORTED TAKEOFF.REMOVED AND REPLACED THE NOSE STRUT PROXI MITY SWITCH. ALSO REMOVED AND REPLACED THE FEEDBACK POT HARNESS. P/N: 20540-001-01 2 L 7 2 4T RT A31SO 2001101500075 20011015 00075 2001 10 15 SWIA200110202 4 20010923 A 2210 CONTROL PANEL CNDAIR CL600 CL6002B19 EA COCKPIT FAULTY A SWIA K NONE F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 496SW 7473 YD1 FAILS TO ENGAGE ON ORIGINATING CHECK. REMOVED YAW DAMPER CONTROL PANEL AND REPLACED WITH SERVICEABLE CONTROL PANEL. OPS CHECKS GOOD. REMOVED, REPLACED AND TESTED NR 1 YD IAW CRJ MM . ALL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2001101500076 20011015 00076 EA 2001 10 15 SWIA200110203 1 20010923 A 5210 LATCH CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE PAX DOOR MALFUNCTIONED A SWIA K NONE O OTHER TX TAXI/GRND HDL 1 NM 07 412SW 7101 CABIN DOOR DIFFICULT TO OPEN FROM INSIDE OR OUT.REPLACED TRIGGER ON MAIN PASSENGER HANDLE LATCH IAW CMM 52-11-03. 2 L 7 2 4F 4 F RT A21EA E15NE 2001101500078 20011015 00078 SO 2001 10 15 SWIA200110204 1 20010921 A 2133 STRAP EMB 120 EMB120RT SO PNEUMATIC VALVE OUT OF POSITION A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 200CD 120200 CLIMBING THROUGH 22,000 CABIN ALT LIGHT ON MAP. CABIN WOULD NOT RESPOND IN AUTO. SWITCH TO MANUAL, WOULD NOT RESPOND. AFTER ABOUT 30 SECONDS CABIN STARTED DESCENDING. DIVERTED FROM STS TO SFO.SECURED INSULATION ON AFT PRESSURE BULKHEAD AND REPOSITIONED BONDING STRAPS ON PNEUMATIC AND ELECTROPNEUMATIC VALVES. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001101500080 20011015 00080 EA 2001 10 15 SWIA200110205 1 20010930 A 2910 601R752861 HYDRAULIC LINE CNDAIR CL600 CL6002B19 EA NR 1 SYSTEM LEAKING A SWIA A UNSCHED LANDING F K J FLT CONT AFFECTED FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 906SW 7510 HYD 1 LO PRESS MESSAGE ON INFLIGHT. QUANTITY AND PRESSURE AT 0. EXECUTED APPROPRIATE CHECK LISTS. DIVERTED TO GJT. EN GINE DRIVEN PUMP RAN DRY FOR 37 MINUTES. REMOVED AND REPLACED NR 1 HYDRAULIC ENGINE DRIVEN PUMP IAW 29-13-00 DUE TO BEI NG RAN DRY. REMOVED AND REPLACED NR 1 SYSTEM RETURN LINE DUE TO PIN HOLE IAW 29-11-00. C/W ENGINE RUN AND NR 1 ELECTRIC PUMP. OPS CHECK GOOD, NO LEAKS NOTED. S/N OFF: MX637287 LINE P/N: 601R75286-1 2 L 7 2 4F RT A21EA 2001101500081 20011015 00081 SO 2001 10 15 SWIA200110206 1 20010907 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 564SW 120339 LEFT AFT FLOOR SEAT TRACK CORRODED LAST SIX FEET.REMOVED AND REPLACED LEFT AFT FLOOR SEAT TRACK. 2 L 7 2 4T RT A31SO 2001101500082 20011015 00082 SO 2001 10 15 SWIA200110207 1 20010907 A 2720 CONTROL CABLE EMB 120 EMB120ER 3260203 SO RUDDER WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 564SW 120339 RIGHT MID INBOARD AND OUTBOARD RUDDER CABLES WORN. RIGHT AFT INBOARD AND OUTBOARD RUDDER CABLES WORN. REPLACED RIGHT MI D INBOARD, OUTBOARD AND AFT INBOARD, OUTBOARD RUDDER CABLES. 2 L 7 2 4T RT A31SO 2001101500083 20011015 00083 SO 2001 10 15 SWIA200110208 1 20010907 A 2731 CONTROL CABLE EMB 120 EMB120ER 3260203 SO ELEVATOR TRIM WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 564SW 120339 ELEVATOR TRIM OUTBOARD AND INBOARD CABLES WORN. REPLACED OUTBOARD AND INBOARD ELEVATOR TRIM CABLES. 2 L 7 2 4T RT A31SO 2001101500084 20011015 00084 SO 2001 10 15 SWIA200110209 1 20010907 A 2710 CONTROL CABLE EMB 120 EMB120ER 3260203 SO AILERON WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 564SW 120339 RIGHT AND LEFT UPPER AND LOWER AILERON CABLES WORN. REPLACED RIGHT AND LEFT UPPER AILERON AND LOWER CABLES. 2 L 7 2 4T RT A31SO 2001101500085 20011015 00085 SO 2001 10 15 SWIA200110210 1 20010907 A 2720 PULLEY EMB 120 EMB120ER 3260203 SO RUDDER NICKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 564SW 120339 AFT RUDDER RIGHT INBOARD CABLE PULLEY HAS NICK. REPLACED RIGHT AFT INBOARD CABLE AFT PULLEY. 2 L 7 2 4T RT A31SO 2001101500086 20011015 00086 SO 2001 10 15 SWIA200110211 1 20011001 A 2611 CONNECTOR EMB 120 EMB120ER 3260203 SO SMOKE DETECTOR DIRTY A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 569SW 120344 BAGGAGE SMOKE/FIRE EXTINGUISHER WILL NOT SOUND AURAL SMOKE WARNING WHEN TESTING. CLEANED CANNON PLUG ON CARGO COMPARTMEN T DETECTOR ASSEMBLY. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2001101500088 20011015 00088 SO 2001 10 15 SWIA200110212 1 20010920 A 2750 FCU EMB 120 EMB120ER 3260203 SO T/E FLAP MALFUNCTIONED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 214SW 120280 ON CLIMBOUT RECEIVED A FLAP DISAGREEMENT AND FLAPS WOULD NOT FULLY RETRACT. RETURNED TO FAT. AIRCRAFT IN FOR C CHECK INS PECTION. DETAILS FORTHCOMING. UPDATE: PULLED FCU, MEGGED WIRES TO BOTH INBOARD FLAP ACTUATORS. NO DEFECTS NOTED. CHE CKED ANNUNCIATORS FOR ANY FAULT CODES. RERACKED FCU. OPS CHECKED FLAP WITH NO FURTHER FAULTS NOTED AT THIS TIME. 2 L 7 2 4T RT A31SO 2001101500089 20011015 00089 NM 2001 10 15 USAA011255 1 20010916 A 5300 FRAME BOEING 737 7373B7 1384580 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 46526 22959 PIT - FOUND FRAME CRACKED .125 INCH CRACK, STATION 787 AT RIVET HOLD ABOVE S9R. CLEANED UP CRACK, INSTALLED .25 INCH RI VET PER TYPICAL REPAIR 53-14-01. (M) 2 L 7 2 4F RT A16WE 2001101500092 20011015 00092 SO 2001 10 15 SWIA200110213 1 20010930 A 3297 HARNESS EMB 120 EMB120ER 3260203 SO LANDING GEAR CRUSHED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 189SW 120048 LANDING GEAR WON'T RETRACT AFTER T/O. FOLLOWED EAP-34 FOR LANDING GEAR DISAGREEMENT AND WAS UNSUCCESSFUL, RETURNED TO J AC. CYCLED GEARS MANY TIMES ON JACKS. COULD NOT DUPLICATE PROBLEM. 10/1/2001 UPDATE: TROUBLESHOOTING FOUND LEFT B HAR NESS CRUSHED. REMOVED AND REPLACED LEFT B HARNESS IAW MM 32-61-01. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001101500095 20011015 00095 SO 2001 10 15 SWIA200110216 1 20010930 A 2131 22201T011400 CONTROLLER EMB 120 EMB120ER 3260203 SO CABIN PRESSURE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 308SW 120326 CABIN PRESSURE PEGGED AT 2000 FPM, SWITCHED TO MANUAL; THAT HAD NO EFFECT ON PRESSURE. RETURNED TO SLC. REMOVED AND REP LACED CABIN PRESSURE CONTROLLER IAW 21-30-00. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001101500097 20011015 00097 2001 10 15 SWIA200110217 4 20011005 A 2210 8220044001 CONTROL PANEL CNDAIR CL600 CL6002B19 EA COCKPIT FAULTY A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 597SW 7293 IAPS RIGHT AFCS BREAKER POPS GIVING A YD2 INOP AND IAPS DEGRADED MESSAGE. REMOVED AND REPLACED FLIGHT CONTROL PANEL IAW AMM 22-13-00. OPS CHECK GOOD. S/N ON: CYJL S/N OFF: 315 2 L 7 2 4F RT A21EA 2001101500099 20011015 00099 SO 2001 10 15 SWIA200110218 1 20011004 A 3213 STRUT EMB 120 EMB120ER 3260203 SO RT MLG OVERSERVICED A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 564SW 120339 AT 80 KTS AIRCRAFT VEERED HARD LEFT. ABORTED TAKEOFF.FOUND RIGHT MAIN LANDING GEAR OVERSERVICED. RETURNED RIGHT MAIN LA NDING GEAR TO PROPER POSITION. 2 L 7 2 4T RT A31SO 2001101500101 20011015 00101 EA 2001 10 15 SWIA200110219 1 20010928 A 2910 ADA686301 MANIFOLD CNDAIR CL600 CL6002B19 EA HYDRAULIC SYS LEAKING A SWIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 496SW 7473 HYDRAULIC SYSTEM NR 3 LOST ALL FLUID. FOUND NR 3 PRESSURE MANIFOLD ASSEMBLY LEAKING. REMOVED AND REPLACED NR 3 HYDRAULI C PRESSURE MANIFOLD ASSEMBLY IAW CRJ MM 29-11-05. OPS CHECK GOOD, LEAK CHECK GOOD. P/N OFF: ADA686-301 S/N OFF: 158 0 2 L 7 2 4F RT A21EA 2001101500104 20011015 00104 SO 2001 10 15 SWIA200110220 1 20011002 A 2750 FCU EMB 120 EMB120RT SO T/E FLAP MALFUNCTIONED A SWIA C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 NM 07 200CD 120200 ON TAKEOFF WE GOT THE FLAP AND ADVANCED SWS ON MAP AND CONTROL FAULT. ASYMMETRY AND DISAGREEMENT ON OVERHEAD FLAP PANEL AND FLAP DEG. INDICATOR WENT TO 0 DEGREES. ABORTED TAKEOFF. POWERED DOWN 5 MINUTES AND IT REPLICATED SAME PROBLEM AFT ER POWER UP. RE-RACKED FLAP CONTROL BOX. SYSTEM FUNCTIONS NORMALLY. ALL WORK PERFORMED IAW EMB AMM 27-50-06. 2 L 7 2 4T RT A31SO 2001101500108 20011015 00108 NE 2001 10 15 SWIA200110221 2 20011002 A 7230 ROTOR SHAFT CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT ENGINE BROKEN A SWIA K NONE O OTHER TX TAXI/GRND HDL 1 NM 07 406SW 7030 807353 LEFT ENGINE N2 GAUGE FLUCTUATES BETWEEN NORMAL INDICATIONS AND ZERO. LEFT ENGINE REMOVED DUE TO N2 ROTOR SHAFT BROKEN. INSTALLED LEFT ENGINE WITH SERVICEABLE UNIT PER RII 71-401. 2 L 7 2 4F 4 F RT A21EA E15NE 2001101500111 20011015 00111 SO 2001 10 15 SWIA200110222 1 20011003 A 2131 CONTROLLER EMB 120 EMB120ER 3260203 SO CABIN PRESSURE MALFUNCTIONED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 564SW 120339 PRESSURIZATION CABIN WOULD NOT PRESSURIZE IN AUTO. REFERRED TO QRH AND WENT TO MANUAL CONTROL. IN MANUAL CONTROL RATE SEEMED VERY SLOW, IT TOOK AROUND 2 MINUTES FOR THE CABIN TO START DOWN FROM 5000 FT TO 200 FT. RETURNED TO PSP. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER WITH A SERVICEABLE UNIT. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001101500112 20011015 00112 2001 10 15 E842001F00000 4 20010917 A 8300 646391 IDLER PULLEY BEECH 36 A36 1151604 CE CONT O520 IO520BB 17032 SO ENGINE FAILED B E84R K NONE O OTHER IN INSP/MAINT 1 SO 09 703KP E1975 285990R THE KIT CONDITIONER BELT IDLER PULLEY WHICH HOLDS TENSION ON THE COMPRESSOR TO CRANKSHAFT PULLEY BELT. THIS IS THE SECO ND OCCURANCE IN WHICH THE BEARINGS IN THIS PULLEY SIEZE AND CAUSE THE PULLEY TO FALL OFF INTO THE COWLING AND ENGINE COM PARTMENT. 1 L 7 1 3O 3 O 3A15 E5CE 2001101500113 20011015 00113 CE 2001 10 15 HUK2001F00000 1 20010903 A 7933 624600615 GAUGE CESSNA 207 T207 2073612 CE CONT O520 IO520F 17032 SO HARTZL HCC3Y HCC3YF1 GL OIL TEMP DAMAGED E HUKA K NONE O OTHER IN INSP/MAINT 1 NM 01 7405 51 20700147 818866 EC1374A OIL TEMPERATURE GUAGE (ROCHESTER SERVICE KIT) FAILED CAUSEING OVER VOLTAGE PROBLEM THROUGH-OUT. SHORTING OUT ALTERNATOR , VOLTAGE REGULATOR, OVER VOLTAGE SENSOR, ENTIRE RADIO STACK, LIGHTING, ELECTRIC SERVICE KIT OIL TEMP WAS REMOVED AND RE PLACED WITH ORIGINAL CAPILLARY STYLE TEMP PROBE AND REPLACEMENT OF ELECTRICAL COMPONENTS CARRIED OUT AS THIS WAS THE 3 G UAGE FAILED IN THE AIRCRAFT AND MANUFACTURE WAS NO SUPPORT FOR THIS UNIT. 1 H 7 1 3O 3 O A16CE E5CE 5 C P25EA 2001101500114 20011015 00114 EA 2001 10 15 SWIA200110223 1 20010930 A 2760 270005 PCU CNDAIR CL600 CL6002B19 EA SPOILER MALFUNCTIONED A SWIA D RETURN TO BLOCK J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 411SW 7067 LEFT OUTBOARD FLIGHT SPOILER TURNS WHITE WHILE PERFORMING GROUND TEST, ALSO SPOILERON FAULT MESSAGE. REMOVED AND REPLACE D LEFT INBOARD SPOILER PCU IAW CRJ MM 27-62-01. OPS AND LEAK CHECK GOOD. P/N: 27000-5 S/N OFF: MAL0566 2 L 7 2 4F RT A21EA 2001101500115 20011015 00115 SO 2001 10 15 SWIA200110224 1 20011005 A 2752 3431001001 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 250YV 120250 FLAP DISAGREEMENT DURING FLAP RETRACTION AFTER LANDING. REPLACED LEFT NACELLE FLAP ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-50-00. NO LEAKS NOTED. NO FLAP DISAGREEMENTS NOTED. FLAPS FUNCTIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2001101500116 20011015 00116 SO 2001 10 15 SWIA200110225 1 20010930 A 7330 SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE DEFECTIVE A SWIA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 07 308SW 120326 FUEL LOW TEMPERATURE LIGHT CAME ON DURING TAXI. INSTALLED SERVICEABLE FUEL TEMPERATURE SWITCH ON LEFT ENGINE. CHECKS OK . 2 L 7 2 4T 4 T RT A31SO E20NE 2001101500117 20011015 00117 SO 2001 10 15 HYI2001F00000 2 20010907 A 8500 CASE CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO ENGINE DAMAGED E HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 6879R 17 402C0611 823329R AIRCRAFT WAS AT CRUISE ALTITUDE, WHEN THE RIGHT ENGINE SHUTTERED, FOLLOWED BY A BANG AND LOSS OF POWER. CREW SECURED TH E ENGINE AND LANDED WITHOUT INCIDENT. MECHANIC DETERMINED THE ENGINE EXPERIENCED AN INTERNAL FAILURE, RESULTING IN 2 ON E INCH HOLES IN THE CASE HALVES OPPOSITE EACH OTHER IN THE AREA OF THE CAMSHAFT FOLLOWERS/LIFTERS AT THE NR 6 AND NR 5 C YLINDER POSITIONS. 1 L 7 2 3O 3 O A7CE E8CE 2001101500118 20011015 00118 SO 2001 10 15 SWIA200110227 1 20010928 A 5270 STRIKER EMB 120 EMB120ER 3260203 SO CARGO DOOR OUT OF ADJ A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 568SW 120343 CARGO DOOR LIGHT ILLUMINATED ON TAKEOFF ROLL. READJUSTED MICRO SWITCHES STRIKER PLATES IAW EMB 120 MM 52-70-02. OPS CHE CK GOOD. 2 L 7 2 4T RT A31SO 2001101500119 20011015 00119 CE 2001 10 15 TIMAP53 1 20010906 A 3230 995800663 POWERPACK BEECH 99 C99 1154006 CE PWA PT6 PT6A11 52043 NE MLG INOPERATIVE E TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 216CS U216 LANDING GEAR POWER PACK FAILED. INSPECTION OF THE POWER PACK REVELED MOTOR SHORTED, CAUSED BY INTERNAL LEAK IN THE POWE R PACK. CREW LOWERED GEAR MANUALLY. 1 L 7 2 3T 3 T A14CE E4EA 2001101500120 20011015 00120 EA 2001 10 15 SWIA200110229 1 20011006 A 2721 SWITCH CNDAIR CL600 CL6002B19 EA COCKPIT FAILED A SWIA C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 NM 07 413SW 7102 STAB TRIM CAUTION MESSAGE CAME ON AT ABOUT 110KTS ON TAKEOFF ROLL. ABORTED TAKEOFF. TROUBLESHOT SYSTEM AND FOUND COPILO T TRIM DISCONNECT SWITCH BAD. REPLACED SWITCH IAW 20-16-10 & 27-41-30. CHECKED SYSTEM IAW 27-41-15. NO FAULTS FOUND. PN ON 996-0013. 2 L 7 2 4F RT A21EA 2001101500121 20011015 00121 SO 2001 10 15 SWIA200110230 1 20011007 A 2751 3472001001 FCU EMB 120 EMB120ER 3260203 SO T/E FLAP FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 290SW 1315 1315 120317 UPON LEVELING AT FL 230 FLAP AND ADV SWS LIGHTS ON MAP WITH CONTROL FAULT ON FLAP WARNING INDICATION PANEL. INBOARD PAI R WAS FLASHING, WOULD NOT RESET PER QRH. REPLACED FCU IAW MM 27-50-00. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001101500122 20011015 00122 SO 2001 10 15 SWIA200110231 1 20011008 A 5230 DOOR SEAL EMB 120 EMB120ER 3260203 SO CARGO DOOR OUT OF POSITION A SWIA G O2 MASK DEPLOYED P NO WARNING INDICATION CR CRUISE 1 NM 07 209SW 120269 RAPID DEPRESSURIZATION AT FL 260. MASKS DEPLOYED.REINSTALLED CARGO DOOR SEAL IAW MM 52-30-01 AND STOWED O2 MASKS IAW MM 35-20-01. 2 L 7 2 4T RT A31SO 2001101500123 20011015 00123 SO 2001 10 15 SWIA200110232 1 20011001 A 2450 RELAY EMB 120 EMB120ER 3260203 SO ELECTRICAL SYS FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 583SW 120351 NR 2 INVERTER INOP LIGHT ILLUMINATED INFLIGHT, FAILED RESET. REPLACED AC DISABLE/TRANSFER RELAY K0002. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001101500124 20011015 00124 NE 2001 10 15 SWIA200110233 2 20011004 A 7321 SENSOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT ENGINE READS HIGH A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 301YV 120301 RIGHT EEC FAILED ON TAKEOFF. MANUAL AND RED EEC LIGHT ILLUMINATED. PERFORMED ENGINE RUNS FOR 20 MINUTES IN TAKEOFF AND CRUISE CONFIGURATIONS, NO DEFECTS NOTED. CLEANED AND OHMED ALL EEC CANNON PLUGS. FOUND NP SENSOR HIGH. REMOVED AND RE PLACED RT ENGINE NP SENSOR AS NEEDED. OPS CHECK GOOD ON RIGHT ENGINE NP SENSOR. EEC OPS CHECK GOOD IAW 71-00-00 120MM. 2 L 7 2 4T 4 T RT A31SO E20NE 2001101500125 20011015 00125 SO 2001 10 15 SWIA200110234 1 20011009 A 2131 CONTROLLER EMB 120 EMB120ER 3260203 SO CABIN PRESSURE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 580SW 120348 DURING CLIMB OUT CABIN PRESSURE BEGAN TO OSCILLATE +/- 2000 FPM. SELECTED MANUAL MODE IAW QRH AND PRESSURE HELD NORMALL Y. REPLACED ELECTRONIC PRESSURE CONTROLLER. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001101500126 20011015 00126 CE 2001 10 15 VOX2001F00000 1 20010919 A 3231 030A3842141 ROD MTSBSI MU2 MU2B60 5780460 CE GARRTT TPE331 TPE33110 01514 WP MLG DOOR FROZEN I VOXA K NONE O OTHER IN INSP/MAINT 1 NM 07 60FL 7124 1512SA 1512SA AIRCRAFT SUFFERED FORWARD DOOR MALIFUNCTION, THE SAFEGUARD SYSTEM FAILED (SHEAR PIN ROD) ASSEMBLY COULD NOT SEPARATE FRO ZE UP. FORWARD DOORS WERE OPEN PARTIALLY, TRIED TO EMERGENCY EXTEND. LEFT MAIN TIRE CAUGHT EDGE OF FORWARD DOOR AND J AMMED MAIN LANDING GEAR EXTENSION. AIRCRAFT HAD TO MAKE GEAR UP LANDING. 1 H 7 2 3T 4 T RT A10SW E4WE 2001101500128 20011015 00128 EU 2001 10 15 ZWYA100173 1 20010727 A 6420 360A33100300M HUB AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR CRACKED A ZWYA K NONE O OTHER IN INSP/MAINT 1 GL 09 365SJ 3644 6018 TAIL ROTOR HUB, HOLES ELONGATED, STRAP PACK CRACKED, SPIDER BROKEN. REMOVED AND REPLACED, TAIL ROTOR HUB. 1 G 7 2 3U 3 U H10EU E19EU 2001101500129 20011015 00129 EU 2001 10 15 ZYWA100162 1 20010403 A 7712 645500071 TACH GENERATOR AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE ROTOR LEAKING A ZYWA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 09 365SJ 3593 6018 TACH GENERATOR LEAKS AT BODY. REMOVED AND REPLACED TACH GENERATOR. 1 G 7 2 3U 3 U H10EU E19EU 2001101500130 20011015 00130 EU 2001 10 15 ZYWA100163 1 20010408 A 2422 SPC30B INVERTER AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE ELECTRICAL INOPERATIVE A ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365SJ 6018 INVERTER INOPERATIVE. REMOVED AND REPLACED INVERTER. 1 G 7 2 3U 3 U H10EU E19EU 2001101500131 20011015 00131 2001 10 15 ZYWA100164 4 20010501 A 2210 41800478034 ACTUATOR AEROSP AS365 AS365N2 8680815 EU TMECA ARRIEL ARRIEL1 60030 NE YAW CHANNEL INOPERATIVE A ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365WM 6429 UNUSED FREQ ADAPTER, MATERIAL. RETURNED FOR RESTOCK AND CREDIT. 1 G 7 2 3U 3 U RT H10EU E19EU 2001101500132 20011015 00132 EU 2001 10 15 ZYWA100166 1 20010324 A 6420 360A33107002 SPIDER AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR CRACKED A ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365SJ 1677 6018 SPIDER CRACKED AND PITCH LUG BROKEN OFF. REMOVED AND REPLACED SPIDER. 1 G 7 2 3U 3 U H10EU E19EU 2001101500133 20011015 00133 EU 2001 10 15 ZYWA100167 1 20010403 A 3340 4217212 LANDING LIGHT AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE FUSELAGE INTERMITTENT A ZYWA K NONE L NO TEST IN INSP/MAINT 1 GL 09 365SJ 453 6018 LANDING LIGHT INTERMITTENT 1 G 7 2 3U 3 U H10EU E19EU 2001101500134 20011015 00134 EU 2001 10 15 ZYWA100174 1 20010707 A 7932 53408 TRANSMISSION AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE NR 1 ENGINE FLUCTUATES A ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365SJ 982 6018 NR 1 ENGINE OIL PRESSURE FLUCTUATES. REMOVED AND REPLACED NR 1 ENGINE OIL PRESSURE TRANSMITTER. 1 G 7 2 3U 3 U H10EU E19EU 2001101500135 20011015 00135 EU 2001 10 15 ZYWA100175 1 20010913 A 2510 504305401 SEAT BELT AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT WORN A ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 07 365SJ 6018 HARNESS ASSEMBLY- REMOVED AND REPLACED BELTS DUE TIME CHANGE. 1 G 7 2 3U 3 U H10EU E19EU 2001101500136 20011015 00136 EU 2001 10 15 ZYWA100176 1 20010612 A 3242 5002566 WHEEL AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE BRAKE LUG CRACKED A ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365SJ 3648 6018 WHEEL ASSEMBLY CRACKED AT BRAKE LUG. REMOVED AND REPLACED WHEEL ASSEMBLY. 1 G 7 2 3U 3 U H10EU E19EU 2001101500137 20011015 00137 2001 10 15 SWIA200110235 4 20011008 A 2300 SWITCH EMB 120 EMB120ER 3260203 SO COCKPIT INOPERATIVE A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 190SW 120050 FIRST OFFICER'S PTT SWITCH INOP. RETURNED TO SLC. INSTALLED NEW SWITCH. FIRST OFFICER'S PTT OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001101500138 20011015 00138 SO 2001 10 15 SWIA200110236 1 20011009 A 2752 3203001005 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 NM 07 190SW 1211 1211 120050 CONTROL FAULT ON FLAPS ON TAKEOFF. REPLACED INBOARD FLAP ACTUATOR IAW MM 27-50-00. OPS AND LEAK CHECK GOOD. 2 L 7 2 4T RT A31SO 2001111400141 20011114 00141 NM 2001 11 14 UPS01237036 1 20010923 A 5330 LAP JOINT BOEING 727 72725C 138400H NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:IN CORROSION AT CREW OXYGEN SERVICE PORT LAP SEAM, STRINGER 19R, STATION 360 TO 344 HAS CORROSION AT LAP SEAM. REMOVED FASTENERS HS 86801 10501 / REMOVED CORROSION HS 86801. VERIFIED REMOVAL OF CORROSION. REINSTALLED FASTE NERS AS PER EO B727-533 0-15449-A AND EXTENDED CORRECTIVE ACTION FORM 05130. 2 L 7 3 4F A3WE 2001102200096 20011022 00096 NM 2001 10 22 UPS01537034 1 20011012 A 2120 SMOKE BOEING 757 75724APF 1384969 NM COCKPIT DETECTED A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SO 01 462UP 28266 INSPECTION TYPE:N/A PILOT REPORT SMOKE IN COCKPIT L-PACK OFF AND L-PACK TEMP EICAS MSGS. LEFT PACK DEFERRED. 2 L 7 2 4F RT A2NM 2001101500142 20011015 00142 WP 2001 10 15 UPS01836987 1 20010920 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 LONG. 36 IS CRACKED STA. 1260-1280 REPAIRED LONGERON I.A.W. 8110-3 APPROVED DH SK 867-681 2 L 7 4 4F RT 4A25 2001101500143 20011015 00143 WP 2001 10 15 UPS01836988 1 20010920 A 5320 5613430503 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE: C1, RIGHT CUSP LOWER FITTING IS CRACKED AT STA. 149 BELOW LONG. 21 RT. REMOVED,FABRICATED,AND REP LACED FITTING I.A.W. DWG. 5613430,AND SRM. 51-1-20D 2 L 7 4 4F RT 4A25 2001101500144 20011015 00144 WP 2001 10 15 UPS01836989 1 20010921 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE: C1, STA. 1727 LONG. 15R IS CRACKED. REPAIRED LONGERON I.A.W. SRM. 53-2-2 FIG. 10 2 L 7 4 4F RT 4A25 2001101500145 20011015 00145 WP 2001 10 15 UPS01836990 1 20010921 A 5330 DOUBLER DOUG DC8 DC873F 302199F WP AFT FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE: C1, R-2 DOOR UPPER AFT CORNER INTERNAL DOUBLER IS CRACKED AT STA. 1620 AT LONG. 10RT. REPAIRED DOU BLER I.A.W. SRM. 53-2-0 FIG. 16 2 L 7 4 4F RT 4A25 2001101500146 20011015 00146 WP 2001 10 15 UPS01836991 1 20010920 A 5320 37558451N FITTING DOUG DC8 DC873F 302199F WP CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE: C1, BATHTUB FITTING IS CORRODED BEYOND LIMITS AT STA. 1220 BETWEEN LONG. 35L-36 REMOVED AND REPLAC ED FITTING I.A.W. DWG.3755845,AND SRM.53-2-0 FIG. 2D, 51-1-20D 2 L 7 4 4F RT 4A25 2001101500147 20011015 00147 WP 2001 10 15 UPS01836992 1 20010921 A 5320 47723981 FITTING DOUG DC8 DC873F 302199F WP AFT CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE: C1, STA. 1768 LONG. 18R END FITTING IS CRACKED REMOVED AND REPLACED FITTING I.A.W. DWG. 4772398, AND SRM. 51-1-20D 2 L 7 4 4F RT 4A25 2001101500148 20011015 00148 WP 2001 10 15 UPS01836993 1 20010920 A 5314 KEELBEAM DOUG DC8 DC873F 302199F WP RT MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE: C1, RIGHT WHEEL WELL KEEL BEAM STA. 827 UPPER WEB AND ATTACH ANGLE ARE CRACKED. REPAIRED WEB AND A NGLE I.A.W. SRM. 53-2-0 FIG. 1B 2 L 7 4 4F RT 4A25 2001101500149 20011015 00149 WP 2001 10 15 UPS01836994 1 20010921 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP COCKPIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE: C1, STA. -80 LOWER FLOORBEAM CAP IS CORRODED BEYOND LIMITS AT LBL. 44 REPAIRED FLOORBEAM I.A.W. 8 110-3 APPROVED DH SK 867-840 2 L 7 4 4F RT 4A25 2001101500150 20011015 00150 WP 2001 10 15 UPS01836995 1 20010921 A 5313 LONGERON DOUG DC8 DC873F 302199F WP RT MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE: C1, STA. 890-900 LONG. 24R IS CRACKED FWD. OF MLG. TORQUE BOX BOTTOM SIDE REPAIRED LONGERON I.A.W . SRM. 53-2-2 FIG. 5 2 L 7 4 4F RT 4A25 2001101500151 20011015 00151 WP 2001 10 15 UPS01836997 1 20010920 A 5320 WEB DOUG DC8 DC873F 302199F WP COCKPIT SUBFLOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE: C1, COCKPIT SUBFLOOR IS CORRODED BEYOND LIMITS STA. -80 TO -130 LBL. 15 TO LBL. 20 REPAIRED WEB I .A.W. SRO8530026, SRM. 51-1-21,51-1-20D.51-3-0 2 L 7 4 4F RT 4A25 2001101500152 20011015 00152 EA 2001 10 15 SWIA200110238 1 20011006 A 4920 38004882 CASE CNDAIR CL600 CL6002B19 EA APU CRACKED A SWIA H DEACTIVATE SYST/CIRCUITS K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 905SW 7456 SMOKE APPEARED IN CABIN, PACKS WERE TURNED OFF. FIRST OFFICER NOTICED FLUID DRAINING THROUGH APU DRAIN VENTS, THEN APU AUTO SHUT DOWN. FOUND OIL LEAKING FROM APU. FOUND APU OIL CASE CRACKED. REMOVED AND REPLACED APU IAW CRJ MM 49-10-00. ALL OPS AND LEAK CHECKS GOOD. P/N ON: 3800488-3 S/N ON: P279C P/N OFF: 3800488-2 S/N OFF: P615 2 L 7 2 4F RT A21EA 2001101500153 20011015 00153 SO 2001 10 15 SWIA200110239 1 20010921 A 5411 FRAME EMB 120 EMB120ER 3260203 SO LT & RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 214SW 120277 RIGHT AND LEFT NACELLE NR 1 FRAMES CRACKED. REPLACED BOTH NACELLE NR 1 FRAMES IAW EMB120 SRM 51-10-02 AND SB 120-54-003 6. 2 L 7 2 4T RT A31SO 2001101500154 20011015 00154 WP 2001 10 15 UPS01836998 1 20010921 A 5330 564932975N2 SKIN DOUG DC8 DC873F 302199F WP AFT FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE: C1, STA. 1690 TO 1890 LONG. 31L TO 31R BELLY SKIN IS CORRODED BEYOND LIMITS REMOVED AND REPLACED SKIN I.A.W. SRM. 53-1-0,51-1-21,51-1-20D 2 L 7 4 4F RT 4A25 2001101500155 20011015 00155 WP 2001 10 15 UPS01836999 1 20010921 A 5330 DOUBLER DOUG DC8 DC873F 302199F WP AFT FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE: C1, INTERNAL DOUBLER IS CORRODED BEYOND LIMITS AT STAS. 1660 LONG. 30R REPAIRED DOUBLER I.A.W. 811 0-3 APPROVED DH SK 867-915 2 L 7 4 4F RT 4A25 2001101500156 20011015 00156 WP 2001 10 15 UPS01837000 1 20010924 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE: C1, L-1 DOOR UPPER FWD. CORNER DOUBLER/TRIPLER REPAIR DOES NOT CONFORM TO SRM. 53-2-0 FIG. 15 AND SRO8 530021 INSTALLED REPAIR I.A.W. SRM. 53-2-0 FIG. 15 2 L 7 4 4F RT 4A25 2001101500157 20011015 00157 SO 2001 10 15 SWIA200110240 1 20011009 A 2751 3472001001 FCU EMB 120 EMB120ER 3260203 SO T/E FLAP FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 213SW 293 293 120277 FLAP DISAGREEMENT REQUIRED ZERO FLAP LANDING. REMOVED AND REPLACED FLAP CONTROL UNIT IAW 27-50-00. RAN FLAPS THROUGH 20 CYCLES. NO DEFECTS NOTED. 2 L 7 2 4T RT A31SO 2001102200097 20011022 00097 WP 2001 10 22 UPS01837003 1 20011010 A 2910 CONTROL UNIT DOUG DC8 DC873F 302199F WP NR 2 ENGINE FAILED A IPXA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 SO 01 803UP 46073 INSPECTION TYPE:NA DEPLOYED REVERSERS IN FLIGHT (280 KIAS) TO MEET CROSSING RESTRICTION, NR 2 WOULD NOT STOW. RAN CHECK LISTS THROUGH INFLIGHT SHUTDOWN. SLOWING THROUGH 200 KIAS, REVERSER STOWED. THREE ENGINE LANDING. INFLIGHT WINDMILLIN G. REMOVED NR 2 ENGINE THRUST REVERSER HYDRAULIC CONTROL UNIT PER MM 78- 31-01. INSTALLED NR 2 T/R HCE IAW MM 78-31-01. OPS AND LEAK CHECKS GOOD. 2 L 7 4 4F RT 4A25 2001101500158 20011015 00158 WP 2001 10 15 UPS01837004 1 20011003 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING L/E CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE: C2,3, RIGHT WING L/E. UPPER RIB IS CRACKED AT XFS 766.25 REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2001101500159 20011015 00159 WP 2001 10 15 UPS01837005 1 20011003 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE: C23, RIGHT WING UPPER SKIN IS CRACKED AT XRS 74 AT STRINGER 9 REPAIRED SKIN I.A.W. SRM. 57-2-1 FI G. 10 2 L 7 4 4F RT 4A25 2001101500160 20011015 00160 SO 2001 10 15 SWIA200110242 1 20011009 A 7712 SEDLOC2R INDICATOR EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 194SW 120120 LEFT TORQUE GAUGE ROLLER BACK TO ZERO ON TAKEOFF. SYSTEM AUTO FEATHERED. ABORTED TAKEOFF. INSPECTED AND CLEANED LEFT ENGINE TORQUE PROBE CANNON PLUG. NO DEFECTS NOTED. REPLACED LEFT ENGINE TORQUE INDICATOR. RAN LEFT ENGINE. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001101500161 20011015 00161 WP 2001 10 15 UPS01837006 1 20011004 A 5730 576958927 DOUBLER DOUG DC8 DC873F 302199F WP LEFT WING L/E CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE: C23, LEFT WING L/E. LOWER INTERNAL DOUBLER IS CRACKED AT DRAIN HOLE AT XFS 335.25 REMOVED,FABRIC ATED,AND REPLACED DOUBLER I.A.W. DWG. 5769589,AND SRM. 51-1-21,51-1-20D 2 L 7 4 4F RT 4A25 2001101500162 20011015 00162 WP 2001 10 15 UPS01837007 1 20011004 A 5320 3750257U1 FITTING DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE: C23, STA. 440-460 LONG. 31R SPLICE FITTING IS CRACKED REMOVED AND REPLACED FITTING I.A.W. DWG. 375 0257,AND SRM. 51-1-20D 2 L 7 4 4F RT 4A25 2001101500163 20011015 00163 SO 2001 10 15 SWIA200110243 1 20011010 A 4930 MANIFOLD EMB 120 EMB120ER 3260203 SO APU CRACKED A SWIA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 293SW 120320 WITH APU BLEED AIR ON CABIN SMELLS OF FUEL. RAN LEFT AND RIGHT ENGINE BLEEDS, NO FUEL SMELL NOTED. FOUND LEAK IN SECON DARY FUEL MANIFOLD CRACK AT THE FLARE. REPLACED APU SECONDARY FUEL MANIFOLD WITH SERVICEABLE ASSEMBLY. OPS CHECK GOOD. NO LEAKS NOTED AT THIS TIME. 2 L 7 2 4T RT A31SO 2001101500164 20011015 00164 WP 2001 10 15 UPS01837008 1 20011003 A 5712 RIB DOUG DC8 DC873F 302199F WP LEFT WING L/E. CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE: C23, LEFT WING L/E. UPPER RIBS ARE CRACKED AT XFS 722.5 AND XFS 728.75 REPAIRED RIBS I.A.W. SRM. 57-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2001101500165 20011015 00165 WP 2001 10 15 UPS01837009 1 20011003 A 5712 RIB DOUG DC8 DC873F 302199F WP RIGHT WING L/E. CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE: C23, RIGHT WING L/E. LOWER RIBS ARE CRACKED AT XFS 653.75 AND XFS 660 REPAIRED RIBS I.A.W. SRM. 5 7-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2001101500166 20011015 00166 WP 2001 10 15 UPS01837010 1 20011004 A 5712 RIB DOUG DC8 DC873F 302199F WP RIGHT WING L/E CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE: C23, RIGHT WING L/E. UPPER RIB IS CRACKED AT XFS 297.5 REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2001101500167 20011015 00167 WP 2001 10 15 UPS01837011 1 20011004 A 5712 RIB DOUG DC8 DC873F 302199F WP LEFT WING L/E CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE: C23, LEFT WING L/E. UPPER RIBS ARE CRACKED AT XFS 354 AND XFS 379 REPAIRED RIBS I.A.W. SRM. 57-2 -0 FIG. 2 2 L 7 4 4F RT 4A25 2001101500168 20011015 00168 NE 2001 10 15 SWIA200110244 3 20011011 A 6110 PROPELLER EMB 120 EMB120ER 3260203 SO HAMSTD 14RF 14RF9 NE LT & RT ENGINE OUT OF BALANCE A SWIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 NM 07 213SW 120277 BAD VIBRATION INFLIGHT, POSSIBLY DUE TO PROP ICING. RETURNED TO SLC. FOUND PROPS OUT OF BALANCE. PERFORMED PROP BALANC E ON BOTH. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 6 C P11NE 2001101500169 20011015 00169 WP 2001 10 15 UPS01837012 1 20011003 A 5712 RIB DOUG DC8 DC873F 302199F WP LEFT WING L/E CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE: C23, LEFT WING L/E. LOWER RIBS ARE CRACKED AT XFS 616.25 AND XFS 622.5 REPAIRED RIBS I.A.W. SRM. 57-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2001101500171 20011015 00171 WP 2001 10 15 UPS01837013 1 20011004 A 5720 576958975 CLIP DOUG DC8 DC873F 302199F WP LEFT WING L/E CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE: C23, LEFT WING L/E. INTERCOSTAL ATTACH CLIP IS CRACKED AT XOLDI 6.225. REMOVED,FABRICATED,AND REP LACED CLIP I.A.W.DWG. 5769589,AND SRM. 51- 1-20D 2 L 7 4 4F RT 4A25 2001101500173 20011015 00173 WP 2001 10 15 UPS01837014 1 20011003 A 5712 RIB DOUG DC8 DC873F 302199F WP RIGHT WING L/E CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE: C23, RIGHT WING L/E. LOWER RIBS ARE CRACKED AT XFS 616.25 AND XFS 622.5 REPAIRED RIBS I.A.W. SRM . 57-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2001101500175 20011015 00175 WP 2001 10 15 UPS01837015 1 20011003 A 5712 RIB DOUG DC8 DC873F 302199F WP RIGHT WING L/E CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE: C23, RIGHT WING L/E. UPPER RIBS ARE CRACKED AT XFS 722.5,XFS 728.75, XFS 735. REPAIRED RIBS I.A.W . SRM. 57-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2001101500176 20011015 00176 WP 2001 10 15 UPS01837016 1 20011003 A 5712 RIB DOUG DC8 DC873F 302199F WP RIGHT WING L/E CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE: C23, RIGHT WING L/E. UPPER RIBS ARE CRACKED AT XFS 635 AND XFS 647.5. REPAIRED RIBS I.A.W. SRM. 57-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2001101500178 20011015 00178 WP 2001 10 15 UPS01837017 1 20011003 A 5712 RIB DOUG DC8 DC873F 302199F WP RIGHT WING L/E CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE: C23, RIGHT WING L/E. LOWER RIBS ARE CRACKED AT XFS 747.5 TO XFS 760 REPAIRED RIBS I.A.W. SRM. 57- 2-0 FIG. 2 2 L 7 4 4F RT 4A25 2001101500179 20011015 00179 WP 2001 10 15 UPS01837018 1 20011003 A 5712 RIB DOUG DC8 DC873F 302199F WP RIGHT WING L/E CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE: C23, RIGHT WING L/E. UPPER RIB IS CRACKED AT XFS 672.5 REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2001101500183 20011015 00183 EU 2001 10 15 QXEA0101621 1 20011011 A 2560 P4010021 BATTERY PACK FOKKER F28 F28MK4000 4990810 EU INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX-LED LIGHT NOT ILLUMINATED ON EMERGENCY FLASHLIGHT BEHIND F/O'S SEAT. LIGHT WAS INSTALLED BACKWARDS. REMOVED AND REPL ACED BATTERY PACK ON EMERGENCY FLASHLIGHT BEHIND F/O'S SEAT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001101500184 20011015 00184 NM 2001 10 15 01FDEA00872 1 20011008 A 3020 32138683 ANTI-ICE VALVE DOUG MD11 MD11F 3023600 NM NR 2 ENGINE FAILED A FDEA J E A DUMP FUEL ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 620FE 48791 DURING CLIMBOUT REC'D LEVEL 3 NR 2 ENG ANTI-ICE DUCT ALERT, SHUTDOWN ENG. R&R RELAYS R2-5229 & R2-5527. R&R NR 2 ENG MA NIFOLD FAILURE SENSING COMPONENTS. R&R ANTI-ICE & REGULATING VALVE PER MM 30-22-04. 2 L 7 3 4F RT A22WE 2001101500185 20011015 00185 NM 2001 10 15 01FDEA00874 1 20011009 A 3620 WARNING LIGHT BOEING 727 72722 1384002 NM COCKPIT ILLUMINATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 149FE 19087 NR 3 ENG BLEED AIR TRIP LIGHT ILLUMINATED AND WOULD NOT RESET. *S/D* COMING 2 L 7 3 4F A3WE 2001101500186 20011015 00186 WP 2001 10 15 01FDEA00875 1 20011010 A 5315 FLOORBEAM DOUG DC10 DC1010F 3022111 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 059FE 46907 AFT CARGO COMPARTMENT FLOORBEAM CORRODED BS 1841, LBL 50 - RBL 50. R&R FLOORBEAM. 2 L 7 3 4F A22WE 2001101500188 20011015 00188 WP 2001 10 15 01FDEA00877 1 20011009 A 5310 DOOR FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 059FE 46907 CENTER CARGO DOOR JAMB AREA LWR AFT OF OUTER BAIL CORRODED. *S/D* COMING 2 L 7 3 4F A22WE 2001101500189 20011015 00189 WP 2001 10 15 01FDEA00878 1 20011010 A 5320 2929169 FLOOR SUPPORT DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 BS 1741, X=71.5 TO X=103 FLOOR SUPPORT CORRODED. R&R FLOOR SUPPORT PER SRM 51-00-01 & 51-30-00. 2 L 7 3 4F RT A22WE 2001101500190 20011015 00190 NM 2001 10 15 01FDEA00879 1 20011011 A 3610 MANIFOLD DOUG MD11 MD11 3023602 NM BLEED AIR FAILED A FDEA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 585FE 48481 NR 2 MANIFOLD FAIL LEVEL 3 ALERT CAME ON. *S/D* COMING 2 L 7 3 4F RT A22WE 2001101500191 20011015 00191 GL 2001 10 15 01FDEA00880 2 20011011 A 7200 ENGINE AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2* GL NR 1 VIBRATION A FDEA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 25 650FE 726 705213 ON CLIMB OUT NR 1 ENG EXPERIENCED NOTICEABLE VIBRATION. *S/D* COMING 2 L 7 2 4F 4 F RT A35EU E23EA 2001101500192 20011015 00192 NM 2001 10 15 01FDEA00883 1 20011012 A 2913 887480 PUMP BOEING 727 7272S2F 1384O81 NM HYDRUALIC BAY LEAKING A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 203FE 22925 AFTER T/O HYD SYS B LOSS. R&R NR 1 B SYS PUMP & FILTERS PER MM 29-12-011-2. 2 L 7 3 4F A3WE 2001110700111 20011107 00111 WP 2001 11 7 01FDEA00884 1 20011011 A 5320 SPLICE DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 364FE 46600 CTR CARGO BILGE AREA LEFT LONGERON 46 BETWEEN BS 1744 & 1761 LONGERON SPLICE CRACKED. REMOVED AND REPLACED SPLICE PER SR M 51-21-01, 51-35-01. 2 L 7 3 4F A22WE 2001101500193 20011015 00193 NM 2001 10 15 UPS01237037 1 20010930 A 5310 STRINGER BOEING 727 72762C 138402C NM BS440 STR24L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 913UP 19245 INSPECTION TYPE:C EVIDENCE OF CORROSION ON STRINGER NESTING SECTION AT BS 440 STR24L STRINGER REPAIR CARRIED OUT IAW SRM 53-10-03 2 L 7 3 4F A3WE 2001101500194 20011015 00194 NM 2001 10 15 UPS01237038 1 20011001 A 5310 STRINGER BOEING 727 72762C 138402C NM BS680 STR15L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 913UP 19245 INSPECTION TYPE:C WHILE INVESTIGATING WING SCANNING LIGHT SUSPECT CRACK STRINGER 15L F OUND CRACKED AT BS 680. DAMAG E BLENDED OUT IAW SRM 53-10-3 2 L 7 3 4F A3WE 2001101500195 20011015 00195 NM 2001 10 15 UPS01237039 1 20011002 A 5310 STRINGER BOEING 727 72762C 138402C NM BS 344 RBL6 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 913UP 19245 INSPECTION TYPE:C ON REMOVAL OF FLOOR PANELS FOR CABLE INSPECTION, CORROSION FOUND ON FLOOR BEAM TOP CAP BS 344 RBL6. CORROSION REMOVED IAW SRM 51-10-06, DAMAGE OUT OF LIMITS, REPAIRED I AW SRM 53-10-08 2 L 7 3 4F A3WE 2001110700112 20011107 00112 WP 2001 11 7 01FDEA00885 1 20011011 A 5320 SPLICE DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 364FE 46600 CTR CARGO BILGE AREA L47 BETWEEN BS 1741 & 1761 LONGERON SPLICE CRACKED. REMOVED AND REPLACED SPLICE PER SRM 51-23-01, 5 1-00-00. 2 L 7 3 4F A22WE 2001110700113 20011107 00113 WP 2001 11 7 01FDEA00886 1 20011011 A 5320 SPLICE DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 364FE 46600 IN CTR CARGO BILGE AREA BETWEEN BS 1701 & 1721 CRACK ON LONGERON SPLICE 51L. REMOVED AND REPLACED LONGERON SPLICE PER SR M 51-23-01 & 51-00-00. 2 L 7 3 4F A22WE 2001110700114 20011107 00114 WP 2001 11 7 01FDEA00887 1 20011011 A 5320 AEA00181 ATTACH ANGLE DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 364FE 46600 IN CTR CARGO AT BS 1521 BILGE AREA BETWEEN LONGERONS R44 & R46 CRACK IN BULKHEAD ATTACH ANGLE. REMOVED AND REPLACED TEE CHORD PER SRM & AEA0453-1 & SRM 51-39-01. 2 L 7 3 4F A22WE 2001101500196 20011015 00196 EU 2001 10 15 QXEA0101600 1 20010929 A 3350 6008903 POWER SUPPLY FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 475AU 11222 PDX - EMERGENCY LIGHTS INOPERABLE ON ROWS ONE THROUGH FIVE. REMOVED AND REPLACED EMERGENCY BATTERY SUPPLY AT ROW 1. OPER ATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001101500197 20011015 00197 EU 2001 10 15 QXEA0101601 1 20010929 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 491US 11156 PDX - EXIT SIGN OVER COCKPIT DOOR HAS NUMEROUS BULBS BURNED OUT. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECK IS GO OD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001101500198 20011015 00198 NM 2001 10 15 QXEA0101602 1 20010922 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - NR 10 SEAT TRACK ON THE RT OUTBOARD TRACK FROM STATION 262.40 TO 420.00 IS DAMAGED. REPLACED NR 10 SEAT TRACK IAW DHC-8 SRM 51-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001101500199 20011015 00199 NM 2001 10 15 QXEA0101603 1 20010921 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX NR 11 SEAT TRACK DAMAGED AT RT OUTBOARD SEAT TRACK FROM STATION 420.000 TO 505.00. REPAIRED IAW DHC-8 SRM 51-40-00 A ND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001101500200 20011015 00200 NM 2001 10 15 QXEA0101604 1 20010926 A 5320 INTERCOSTAL DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - INTERCOSTAL AT X354 TO X370 AND STRINGER 23R IS CRACKED AT A TOOLING MARK. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001101500201 20011015 00201 NM 2001 10 15 QXEA0101606 1 20010928 A 5230 TRACK DHAV DHC8 DHC8202 2809007 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - CARGO DOOR FORWARD TRACK HAS A GOUGE .028 INCH X .750 INCH X .5 INCH LOCATED AT Z130, X547. REPAIRED IAW HORIZON A IR EA 2-52-109. 2 H 7 2 4T RT A13NM 2001101500202 20011015 00202 2001 10 15 QXEA0101607 4 20010926 A 3460 101741111 COMPUTER DHAV DHC8 DHC8202 2809007 NM COCKPIT FAULTY A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 353PH 7294 496 RDD- ELECTRICAL SMELL IN COCKPIT BELIEVED TO BE COMING FROM NR 2 FMS. WHEN FMS IS TURNED OFF THERE IS NO SMOKE. REMOVED AND REPLACED NR 2 FMS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001101600001 20011016 00001 SO 2001 10 16 C2XA01IA373 1 20011014 A 3350 276005 FUSE EMB 145 EMB145LR SO CABIN BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13908 145465 IAH- DURING PERFLIGHT THE CREW NOTED THAT THE COCKPITCEILING AND THE CABIN CEILING AFT OF GALLEY EMERGENCY LIGHTS FAILE D TO ILLUMINATE. IAH- MAINTENANCE REMOVED AND REPLACED THE FUSE IN THE FORWARD BATTERY PACK, PREFORMED A OPERATIONAL C HECK, NO DEFECTS NOTED,AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001101900012 20011019 00012 NM 2001 10 19 CALA0100950 1 20011015 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69333 23571 FLOOR SUPPORT CRACKED AT SCREW HOLES BETWEEN STATIONS 927 AND 947.5 AT BL 0.0. FABRICATED AND INSTALLED SUPPORT ASSEMBL Y PER SRM 51-10-2. 2 L 7 2 4F RT A16WE 2001101600002 20011016 00002 NM 2001 10 16 01FDEA00888 1 20011012 A 2750 CONNECTOR BOEING 727 727233 138408A NM FAULTY A FDEA A UNSCHED LANDING I FLT. ATTITUDE INST. CL CLIMB 1 SO 25 220FE 20934 01-337 ASSYMETRICAL INBD T/E FLAP BETWEEN 2 & 5 DEG AFT T/O. R&R RIGHT INBD FLAP POS TRANSMITTER ELECTRICAL CONNNECTOR. 2 L 7 3 4F RT A3WE 2001101600003 20011016 00003 EU 2001 10 16 ASOA01168 1 20010906 A 5300 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 632AS 338 DURING C-CHECK INSPECTION IN BNA, MAINTENANCE DISCOVERED CORROSION ON THE RIGHT OUTBOARD SEAT TRACK AND FLANGES (TOP AND BOTTOM) SURFACES BETWEEN FRAMES 29 AND 36. MAINTENANCE REPAIRED CORROSION IAW ASA EO 72-53-0115. (M) 2 H 7 2 4T RT 2001101600004 20011016 00004 NM 2001 10 16 NOCA0201 1 20010914 A 2500 5A30883 SLIDE BOEING 737 7378Q8 13844BX NM RT AFT INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 800NA 28215 JFK - SCHEDULED SLIDE DEPLOYMENT FOR SAMPLING PROGRAM. NR 2 RIGHT DOOR SLIDE FAILED TO DEPLOY CORRECTLY. SLIDE INFLATE D PRIOR TO DROPPING FROM DOOR. SLIDE DID NOT DEPLOY FULLY AND CONTACT GROUND. COMPLIANCE WITH AD 2001-15-01 WILL INCOR PORATED MODIFICATIONS TO SLIDE COMPARTMENT ASSEMBLIES. (M) 2 L 7 2 4F RT A16WE 2001101600005 20011016 00005 EU 2001 10 16 SIMA200125901 1 20010916 A 3200 AIR130902 SWITCH SAAB SF340 340B 7860101 EU LT MLG INOPERATIVE A SIMA A UNSCHED LANDING S AFFECT SYSTEMS LD LANDING 1 SW 21 376AE 340B376 LAX - FLT 3268 - AFTER LANDING GEAR WAS SELECTED DOWN THE LEFT DOWNLOCK LIGHT DID NOT ILLUMINATE. CREW DECLARED AN EMER GENCY. MAINTENANCE REMOVED AND REPLACED THE LEFT DOWNLOCK SWITCH IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001101600006 20011016 00006 NM 2001 10 16 USAA011172 1 20010830 A 5330 SKIN BOEING 767 767201 1385125 NM BS 456 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647US 58982 23899 CLT - FOUND SKIN DENTED .500 BY .150 INCH BS 456, STRINGER 25R. FOUND TO BE WITHIN LIMITS PER BOEING 767-200 SRM 53-00- 01 FIG 101. (M) 2 L 7 2 4F RT A1NM 2001101600007 20011016 00007 EU 2001 10 16 QXEA0101608 1 20011003 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN FAULTY A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 496US 11169 GEG- FORWARD AND AFT FACING EXIT SIGNS IN CEILING AND MID CABIN ARE INOPERATIVE. REMOVED AND REPLACED FORWARD AND AFT CI RCUIT BOARDS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001101600008 20011016 00008 EU 2001 10 16 QXEA0101609 1 20011003 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN FAULTY A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 496US 11169 GEG- EXIT SIGN ABOVE COCKPIT ENTRANCE HAS SEVERAL BULBS INOPERATIVE. REMOVED AND REPLACED CIRCUIT BOARD. OPERATIONAL CHE CKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001101600009 20011016 00009 EU 2001 10 16 QXEA0101611 1 20011007 A 3350 5515800106 LIGHT FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 494US 11167 BOI - FORWARD CENTER AISLE EXIT SIGN HAS SEVERAL LIGHTS INOPERABLE. REMOVED AND REPLACED CENTER AISLE EXIT LIGHT ASSEMBL Y. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001101600010 20011016 00010 EU 2001 10 16 QXEA0101612 1 20011006 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 488US 11240 PDX - OVERWING EXIT SIGNS AND COCKPIT ENTRANCE EXIT SIGN HAVE INOP LAMPS. REMOVED AND REPLACED EXIT SIGN ASSEMBLY'S. OPE RATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001101600011 20011016 00011 NM 2001 10 16 QXEA0101613 1 20011006 A 5210 COVER DHAV DHC8 DHC8* NM AFT PAX DOOR LOOSE A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 400QX 4030 SEA- AFT PASSENGER DOOR DIFFICULT TO OPEN. RESECURED TRIM PIECE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2001101600012 20011016 00012 NM 2001 10 16 QXEA0101614 1 20011006 A 5210 STOP DHAV DHC8 DHC8202 2809007 NM PAX DOOR DEFECTIVE A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 357PH 504 SEA- MAIN CABIN DOOR HANDLE RECESSED AND UNABLE TO OPEN. REMOVED AND REPLACED MAIN CABIN DOOR HANDLE UP STOP BUMPER. OPE RATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001101600013 20011016 00013 EU 2001 10 16 QXEA0101615 1 20011009 A 3397 WIRE FOKKER F28 F28MK4000 4990810 EU CABIN BROKEN A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478US 11227 BOI - EVACUATION LIGHT ON SEAT 12A,B IS INOPERABLE. REPAIRED BROKEN WIRE. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED T O SERVICE. 2 L 7 2 4F RT A20EU 2001101600014 20011016 00014 EU 2001 10 16 QXEA0101616 1 20011008 A 3350 5515800106 LIGHT FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 BOI - EMERGENCY EXIT LIGHT IN GALLEY DOOR DOES NOT LIGHT UP. REMOVED AND REPLACED EXIT LIGHT ASSEMBLY. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001101600015 20011016 00015 EU 2001 10 16 QXEA0101617 1 20011011 A 3397 PIN FOKKER F28 F28MK4000 4990810 EU CABIN DAMAGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 497US 11173 PDX - ESCAPE PATH LIGHTS ON ROWS 1 THROUGH 4 WILL NOT RESET. REMOVED AND REPLACED CONNECTOR PIN. OPERATIONAL CHECK IS GO OD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001101600016 20011016 00016 EU 2001 10 16 QXEA0101618 1 20011009 A 3397 SPLICE FOKKER F28 F28MK4000 4990810 EU CABIN BROKEN A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 497US 11173 PDX - ROWS 1, 2, AND 3 EVACUATION LIGHTS STAY ON WITH BATTERY SHUTDOWN. REPAIRED BROKEN SPLICE ON THE ARM WIRE FOR THE F ORWARD BATTERY PACK. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001101600017 20011016 00017 NM 2001 10 16 QXEA0101619 1 20011011 A 5210 LINK DHAV DHC8 DHC8202 2809007 NM PAX DOOR BINDING A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 356PH 502 PDX- MAIN CABIN DOOR VERY DIFFICULT TO OPEN. REMOVED AND REPLACED PIVOT LOWER LINK AND ASSOCIATED BUSHINGS ON FORWARD HA NDRAIL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001101600018 20011016 00018 NM 2001 10 16 QXEA0101620 1 20011006 A 5210 COVER DHAV DHC8 DHC8* NM AFT PAX DOOR LOOSE A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 400QX 4030 SEA- AFT PASSENGER DOOR DIFFICULT TO OPEN. RESECURED TRIM PIECE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2001101600019 20011016 00019 NM 2001 10 16 QXEA0101622 1 20011008 A 5410 BRACKET DHAV DHC8 DHC8* NM RT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX-RIGHT HAND FINGERNAIL DECK SUPPORT BRACKET AT AFT EXHAUST SHROUD ATTACHMENT POINT IS CRACKED. FABRICATED AND INSTALL ED DECK SUPPORT BRACKET IAW HORIZON AIR EA 6-54-21. 2 H 7 2 4T RT A13NM 2001101600020 20011016 00020 EA 2001 10 16 MAS2001F00000 1 20010726 A 3300 1317 LAMP CNDAIR CL600 CL6002B19 EA GE CF34 CF34* NE CABIN EMRG LTS BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37342 7342 DURING PREFLIGHT THE CREW NOTICED 2 FORWARD CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. MECHANIC REPLACED THE BULB IN BOTH UNITS. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2001101600021 20011016 00021 EA 2001 10 16 COMA0160806 1 20011012 A 3350 LAMP CNDAIR CL600 CL6002B19 EA A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 779CA 7306 FLIGHT #UNK-FWD CEILING EMERGENCY LIGHT IS INOP.DEFERRED MAINTENANCE PER MEL ACFT CONTINUED SERVICE. 2 L 7 2 4F RT A21EA 2001101600022 20011016 00022 EA 2001 10 16 COMA0160807 1 20011012 A 3350 363782 LAMP CNDAIR CL600 CL6002B19 EA FLOOR BURNED OUT A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 957CA 7109 FLIGHT 5442-FLOOR PATCH EMERGENCY LIGHTS ROWS 2 THRU 5 ARE INOP.REPLACED INOP SECTION OF FLOOR PATCH LIGHTING. 2 L 7 2 4F RT A21EA 2001101600023 20011016 00023 EA 2001 10 16 COMA0160808 1 20011013 A 3260 46193 VALVE CNDAIR CL600 CL6002B19 EA MLG BAY FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SO 01 708CA 7963 7235 FLIGHT 6040. DURING CLIMB-OUT OF IAD AND AFTER GEAR RETRACTION RECEIVED A GEAR DISAGREE MESSAGE WITH AURAL WARNING. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD.REPLACED THE LANDING GEAR PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2001101600024 20011016 00024 NM 2001 10 16 QXEA0101623 1 20011008 A 5410 STRUCTURE DHAV DHC8 DHC8* NM RT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX-DECK CRACKED UNDER RIGHT HAND FINGERNAIL AFT ATTACH POINT. FABRICATED AND INSTALLED DECK IAW HORIZON AIR EA 6-54-23. 2 H 7 2 4T RT A13NM 2001101600025 20011016 00025 2001 10 16 SWAA012766 4 20011008 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 074SW 22674 DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER M M. 2 L 7 2 4F A16WE 2001101600026 20011016 00026 EA 2001 10 16 COMA0160809 1 20011013 A 2751 852D100MD91 ACTUATOR CNDAIR CL600 CL6002B19 EA WING FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 948CA 14150 7079 FLIGHT 5555. DURING APPROACH INTO CRW, RECEIVED A FLAP FAIL CAUTION WITH FLAP POSITION AT 26 DEGREES. CREW DECLARED AN E MERGENCY AND LANDED SAFELY.REPLACED LEFT INBOARD FLAP, INBOARD ACTUATOR. 2 L 7 2 4F RT A21EA 2001101600027 20011016 00027 NM 2001 10 16 SWAA012767 1 20011007 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACK (2 EA) AT BS 727E, STR 18R & BS 747, STR 25R. REPAIRED SKIN PER SR M. 2 L 7 2 4F RT A16WE 2001101600028 20011016 00028 2001 10 16 SWAA012769 4 20011008 A 2565 D31354 SLIDE BOEING 737 7377H4 NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 785SW 30602 AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001101600029 20011016 00029 NM 2001 10 16 SWAA012770 1 20011008 A 3260 65C28034 TARGET BOEING 737 7373H4 1384600 NM NLG OUT OF ADJ A SWAA K NONE N FALSE WARNING DE DESCENT 1 SW 07 306SW 22946 WHEN GEAR LOWERED FOR LANDING, GREEN LIGHT FOR NOSE GEAR DID NOT ILLUMINATE. AFTER MANUAL EXTENSION ALL INDICATIONS OK. FOUND NOSE GEAR POSITION SENSOR TARGET GAP OUT OF TOLERANCE. ADJUSTED TARGET AND CLEANED SENSOR PER MM. 2 L 7 2 4F RT A16WE 2001101600030 20011016 00030 NE 2001 10 16 SWAA012772 2 20011004 A 7200 CFM563 ENGINE BOEING 737 7373TO 138447G NM GE CFM56 CFM56* 13802 NE NR 1 OVERHEATED A SWAA K NONE M J OVER TEMP WARNING INDICATION IN INSP/MAINT 1 SW 07 697SW 23838 721766 NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED DURING CRUISE. REDUCED THROTTLE TO IDLE AND LIGHT WENT OUT. ON THE GROUND EGT W AS 680 AND OIL PRESS WAS 18 - 20 PSI. SHUT NR 1 ENGINE DOWN. REMOVED AND REPLACED NR 1 ENGINE PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2001101600031 20011016 00031 NM 2001 10 16 SWAA012777 1 20011005 A 5315 6546804 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 1006, LBL 9 & WL 208. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2001101600032 20011016 00032 NM 2001 10 16 SWAA012779 1 20011008 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIPS CORRODED (2 EA) AT BS 767, STR 26R & BS 787, STR 26R. REMOVED AND REP LACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001101600033 20011016 00033 NM 2001 10 16 SWAA012782 1 20011009 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 394SW 27380 DURING SCHEDULED C4 CHECK, FOUND EEPLS INOP AT AFT CABIN. RELAMPED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001101600034 20011016 00034 NM 2001 10 16 SWAA012787 1 20011008 A 5320 6551698 SPLICE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER SPLICE AT BS 907, STR 4R. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2001101600035 20011016 00035 NM 2001 10 16 SWAA012788 1 20011010 A 5320 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 16L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001101600036 20011016 00036 EA 2001 10 16 COMA0160810 1 20011013 A 2751 852D100MD91 ACTUATOR CNDAIR CL600 CL6002B19 EA WING FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 948CA 14150 7079 FLIGHT 5555. DURING APPROACH INTO CRW, RECEIVED A FLAP FAIL CAUTION WITH FLAP POSITION AT 26 DEGREES. CREW DECLARED AN E MERGENCY AND LANDED SAFELY.REPLACED RIGHT INBOARD FLAP, INBOARD ACTUATOR. 2 L 7 2 4F RT A21EA 2001101600037 20011016 00037 EA 2001 10 16 COMA0160811 1 20011013 A 3310 LIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ODOR A COMA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SO 01 967CA 7134 FLIGHT 5651. ELECTRICAL BURNING SMELL COMING FROM THE COCKPIT DOME LIGHT.INSPECTED LIGHT ASSY, SECURED INSULATION AND WI RING-NO DEFECTS OR SMELL NOTED. 2 L 7 2 4F RT A21EA 2001101600038 20011016 00038 EA 2001 10 16 COMA0160812 1 20011013 A 7830 M8372395R10059 CONNECTOR CNDAIR CL600 CL6002B19 EA RIGHT ENGINE FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 916CA 19371 7014 FLIGHT 5280. DURING CRUISE FLIGHT, RECEIVED A RIGHT ENGINE REVERSER UNLOCK MESSAGE, AIRCRAFT DIVERTED TO PIT.REPLACED CO NNECTOR FOR THE RIGHT ENGINE RED WIRING HARNESS ATTACHING TO AIR GEAR BOX. 2 L 7 2 4F RT A21EA 2001101600039 20011016 00039 NM 2001 10 16 SWAA012790 1 20011010 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAMS CORRODED AT BS 770, LBL 3 TO LBL 12, BS 793, RBL 3 TO LBL 8 & BS 857, LBL 17. REPAIRED FLOORBEAMS PER SRM & SWA RA 1-A53-2021. 2 L 7 2 4F RT A16WE 2001101600040 20011016 00040 EA 2001 10 16 COMA0160813 1 20011014 A 5320 601R3110919 SKIN CNDAIR CL600 CL6002B19 EA DOOR FRAME DENTED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 932CA 7038 PREVIOUS REPAIR TO FUSELAGE SKIN AT FS 310.00 IS DAMAGED.REMOVED DAMAGED SKIN REPAIR AND INSTALLED NEW SKIN REPAIR AT FS 310.00 IAW CANADAIR REO 601R-53-21-180. 2 L 7 2 4F RT A21EA 2001101600041 20011016 00041 2001 10 16 SWAA012792 4 20011010 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001101600042 20011016 00042 NM 2001 10 16 SWAA012794 1 20011011 A 5320 6551698 SPLICE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 522SW 26564 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2001101600043 20011016 00043 NE 2001 10 16 SWAA012797 2 20011010 A 7230 3400018090 COMPRESSOR BOEING 737 7377H4 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE DAMAGED A SWAA A UNSCHED LANDING E J B VIBRATION/BUFFET WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 787SA 29812 877667 AIR TURNBACK, VIBRATION STARTED ON NR 1 ENGINE CLIMBING THROUGH 16,000 FEET, FOLLOWED BY AN ELECTRICAL ODOR. FOUND FWD FAN BLADE PLATFORM BROKEN BETWEEN FAN BLADES NR 19 & 20. REMOVED AND REPLACED ENGINE PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2001101600044 20011016 00044 EA 2001 10 16 COMA0160814 1 20011013 A 5270 DOOR CNDAIR CL600 CL6002B19 EA A COMA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SO 01 978CA 7158 FLIGHT 5836. DURING CLIMB-OUT OF MDT, RECEIVED A CABIN DOOR OUTER HANDLE CAUTION MESSAGE, AIRCRAFT RETURNED TO THE FIELD .INSPECTED THE CABIN DOOR OUTER HANDLE ASSEMBLY, PRESSURIZED AIRCRAFT AND OPERATIONAL CHECK WAS SATISFACTORY. 2 L 7 2 4F RT A21EA 2001101600045 20011016 00045 EA 2001 10 16 COMA0160815 1 20011014 A 2760 SPOILER CNDAIR CL600 CL6002B19 EA A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 988CA 7204 FLIGHT 5872. TAKE-OFF ABORTED BECAUSE OF SPOILERON FAULT MESSAGE.COULD NOT DUPLICATE. RESET THE S.E.C.U. AND OPERATIONAL CHECK OF SPOILERON SYSTEM WAS NORMAL. 2 L 7 2 4F RT A21EA 2001101600046 20011016 00046 NM 2001 10 16 2001F00415 1 20010611 A 5754 ARB1949504 RIB DOUG DC10 DC1040F 3023507 NM L/E SLAT CRACKED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 140WE 46920 DURING C-CHECK, THE RIGHT WING NR 8 SLAT RIB AT STATION XOS1158 WAS FOUND CRACKED, 12 INCHES LONG. THE CRACK WAS REPAIR ED IAW EA NR 10-5755-24-A0886. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 2001101600047 20011016 00047 NM 2001 10 16 2001F00416 1 20010611 A 5753 NRC6053501 RIB DOUG DC10 DC1040F 3023507 NM T/E FLAP CORRODED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 140WE 46920 DURING C-CHECK, THE LEFT OUTBOARD FLAP HAS CORROSION BETWEEN FRONT SPAR CAP STATION 538 THROUGH 554. SURFACE CORROSION O N RIBS AT STATION 538. LEFT OUTBOARD FLAP WAS REMOVED AND SENT TO OVERHAUL AT HONEYCOMB COMPOSITE SYSTEMS, WHERE THE CO RROSION WAS REMOVED AND THE FLAP WAS REPAIRED IAW AS ELEVEN INC EO, AS11277, WHICH WAS ISSUED DERT-510394-CE. THE OUTBO ARD LEFT FLAP WAS INSTALLED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 2001101600048 20011016 00048 NM 2001 10 16 2001F00417 1 20010611 A 5711 ARB30392 SPAR CAP DOUG DC10 DC1040F 3023507 NM RT WING CORRODED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 140WE 52849 46920 DURING C-CHECK, FOUND CORROSION IN THE NR 3 ENGINE WING SPAR FITTING BULKHEAD UPPER CAP NR 3 ATTACH HOLE. THE CORROSION WAS REMOVED AND THE UPPER CAP WAS REPAIRED IAW EA 10-5720-24-A0865. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 2001101600049 20011016 00049 NM 2001 10 16 USA2001F00006 1 20010531 A 5730 6591700194 PANEL BOEING 737 737301 1384611 NM GE CFM56 CFM56* 13802 NE TOP RT WING PANL DEPARTED A USAA A UNSCHED LANDING D K W INFLIGHT SEPARATION FLUID LOSS INADEQUATE Q C CL CLIMB 1 EA 19 585US 23930 AFTER TAKEOFF, FLIGHT ENCOUNTERED COMPLETE LOSS OF SYSTEM A HYDRAULICS AND PRESSURE. LOST LG TRIANGULAR PANEL OFF TOP O F RT WING. NOSE GEAR WOULD RETRACT BUT MAIN GEAR WOULD NOT. HYDRAULIC LINE HAD BROKEN. PANEL DEPARTED AIRCRAFT AT END OF RUNWAY. CAPTAIN DECLARED EMERGENCY AND RETURNED TO FIELD. MANUAL GEAR EXTENSION WAS PERFORMED AS WELL AS QUICK REF ERENCE HANDBOOK PROCEDURES. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND WAS TOWED FROM END OF RUNWAY. MAINT REMOVED AND REPLACED HYDRAULIC LINES DAMAGED BY DEPARTING WING PANEL. REPLACED RIGHT WING PANEL. SERVICED HYDRAULICS AND CYCLED L ANDING GEAR AND FLIGHT CONTROLS TO REMOVE ALL AIR FROM HYDRAULIC SYSTEM. OPERATIONAL CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2001101600050 20011016 00050 NM 2001 10 16 2001F00418 1 20010611 A 5753 NRC6053506 FLAP DOUG DC10 DC1040F 3023507 NM RT WING CORRODED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 140WE 52849 46920 DURING C-CHECK, THE RIGHT OUTBOARD FLAP OUTBOARD HINGE ATTACH POINTS HAVE HEAVY EXFOLIATION AT LOWER MOUNT BULKHEAD FITT ING (VIEWED INTERNALLY). RIGHT OUTBOARD FLAP WAS REMOVED AND SENT TO OVERHAUL AT HONEYCOMB COMPOSITE SYSTEMS, THE CORRO SION WAS REMOVED AND FLAP WAS REPAIRED IAW AS ELEVEN INC EO'S AS11276, AS 11277, AND AS11280. THE OUTBOARD RIGHT FLAP W AS INSTALLED AND THE AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (M) 2 L 7 3 4F RT A22WE 2001101600051 20011016 00051 NM 2001 10 16 2001F00419 1 20010611 A 5310 DOOR FRAME DOUG DC10 DC1040F 3023507 NM FUSELAGE CORRODED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 140WE 52849 46920 DURING C-CHECK, FOUND CORROSION ON THE LOWER FORWARD END OF THE FORWARD CARGO DOOR JAMB FRAME AT STATION 886. CORROSION WAS REMOVED AND REPAIRED IAW EA NR 10-5316-24-A0861. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 2001101600052 20011016 00052 NM 2001 10 16 2001F00420 1 20010611 A 7830 196000371 PANEL DOUG DC10 DC1040F 3023507 NM NR 3 T/R CORRODED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 140WE 46920 DURING C-CHECK, FOUND CORROSION ON THE NR 3 ENGINE OUTBOARD THRUST REVERSER INTERNAL SKIN ACOUSTICAL PANEL. CORROSION W AS REMOVED AND THE PANEL WAS REPAIRED IAW AIRBORNE NACELLE ENGINEERING REPAIR ORDER ANS-DC10-R0010. AIRCRAFT WAS RETURN ED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 2001101600053 20011016 00053 NM 2001 10 16 2001F00421 1 20010611 A 5753 SKIN DOUG DC10 DC1040F 3023507 NM T/E FLAP CHAFED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 140WE 46920 DURING C-CHECK, FOUND RIGHT OUTBOARD FLAP UPPER SKIN WAS FOUND CHAFED NEAR STATION XOF 759. REPAIRED CHAFED SKIN ON RIG HT OUTBOARD FLAP UPPER SKIN NEAR STATION XOF 759 IAW EA NR 10-5753-24-A0859. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 2001101600054 20011016 00054 NM 2001 10 16 2001F00422 1 20010711 A 5711 SPAR BOEING 727 72721 1384003 NM CENTER WING CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 355QS 19257 WING CENTER SECTION, INTERNAL, AFT SPAR WEB BULGED IN AREA OF UPPER SPAR CHORD BL 45 R. INSTALLED DOUBLER REPAIR AT AFT WEB, STATION BS 870, RBL 50.9 IAW AVHM-23RO-1 REVISION R1. (M) 2 L 7 3 4F A3WE 2001101600055 20011016 00055 NM 2001 10 16 2001F00423 1 20010711 A 5711 SPAR BOEING 727 72721 1384003 NM CENTER WING CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 355QS 19257 WING CENTER SECTION FRONT SPAR BS 740 LOWER CHORD OUTBOARD OF VERTICAL STRINGER F5 HAS TWO RIVETS POPPED OUT AND SKIN BU LGING. INSTALLED REPAIR ANGLES AND STRAPS WING CENTER SECTION FRONT SPAR LOWER CHORD AT STATION 740 RBL 42 THROUGH 48.4 3 IAW AVHM 238R0-1. (M) 2 L 7 3 4F A3WE 2001101600056 20011016 00056 NM 2001 10 16 2001F00424 1 20010802 A 5711 SPAR BOEING 727 72721 1384003 NM CENTER WING CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 355QS 19257 CENTER TANK UPPER SKIN AT REAR SPAR BS 870 HAS CORRODED AREAS FROM LBL 40 TO RBL 40. ACCOMPLISHED WING CENTER SECTION A FT SPAR UPPER CHORD AND SKIN REPAIR AT RBL 24 IAW AVHM-246RO-1 REV IR. (M) 2 L 7 3 4F A3WE 2001101600057 20011016 00057 NM 2001 10 16 2001F00425 1 20010807 A 5315 FLOORBEAM BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 355QS 19257 FOUND BS 620 FLOORBEAM CORRODED ON UPPER CAP AT RBL 50. INSTALLED FLOORBEAM REPAIR AT BS 620 UPPER CAP AT RBL 50 IAW SR M 53-10-8 FIG 3. (M) 2 L 7 3 4F A3WE 2001101600058 20011016 00058 WP 2001 10 16 ZW0A0109601 1 20011014 A 3350 58222 BATTERY PACK DOUG DC9 DC983 3022083 WP FWD CABIN A ZW0A K NONE O OTHER NR NOT REPORTED 1 CE 13 9622A 53593 THE EGRESS LIGHTING IN THE FIRST CLASS CABIN WAS INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 7-25-01 STL. --CLOSE D-- 2 L 7 2 4F RT A6WE 2001101600059 20011016 00059 NM 2001 10 16 2001F00426 1 20010901 A 5330 SKIN BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 355QS 19257 FOUND FUSELAGE UPPER LOBE INTERIOR WING CENTER SECTION UPPER SKIN HAS CORROSION AT RBL 24-45.5 BETWEEN STATION 740 AND 8 70. ACCOMPLISHED WING CENTER SECTION UPPER SKIN CORROSION REPAIR AT STATION 752 BETWEEN STRINGER 20C AND STRINGER 21C I AW AVHM-2430RO-1 REV IR. (M) 2 L 7 3 4F A3WE 2001101600060 20011016 00060 NM 2001 10 16 2001F00427 1 20010726 A 5315 FLOORBEAM BOEING 727 72721 1384003 NM FUSELAGE DAMAGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 355QS 19257 FOUND CABIN FLOORBEAM BS 344 HAS EXCESS OF OVERSIZE HOLES ON UPPER CAP FROM LBL 62 INCHES TO RBL 62 INCHES. REPLACED SE CTION OF CABIN FLOORBEAM UPPER T-CAP AT BS 344 IAW SRM 53-10-8. (M) 2 L 7 3 4F A3WE 2001101600061 20011016 00061 NM 2001 10 16 2001F00428 1 20010909 A 5310 DOOR FRAME BOEING 727 72721 1384003 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 MAIN CARGO DOOR CUTOUT, FORWARD FRAME SKIN HAS A CRACK APPROXIMATELY AT BS 502 ABOVE STRINGER 14L. (M) 2 L 7 3 4F A3WE 2001101600062 20011016 00062 NM 2001 10 16 2001F00429 1 20010821 A 5313 STRINGER BOEING 727 72721 1384003 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 LOWER FORWARD CARGO COMPARTMENT BETWEEN BS 680 AND BS 700 STRINGER 20L SHOWS CRACK TO CENTER. ALSO, BS 700 FRAME TIED T O FUSELAGE IS CRACKED FROM TOP FASTENER. INSTALLED STRINGER REPAIR AT LOWER FORWARD CARGO COMPARTMENT BETWEEN BS 680 AN D BS 700 AT STRINGER 20L PER B727 SRM 53-10-3 AND 53-10-2. (M) 2 L 7 3 4F A3WE 2001101600063 20011016 00063 NM 2001 10 16 2001F00430 1 20010816 A 5311 FRAME BOEING 727 72721 1384003 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FUSELAGE LOWER FORWARD CARGO, BS 700 STATION 20L, AT FRAME TO SKIN WEB, HAS A CRACK AT RIVET. CUT OUT DAMAGE AREA AND I NSTALLED FRAME REPAIR AT BS 700 STATION 20L IAW B727 SRM 53-10-4. (M) 2 L 7 3 4F A3WE 2001101600064 20011016 00064 NM 2001 10 16 2001F00431 1 20010802 A 5347 SEAT TRACK BOEING 727 72721 1384003 NM FUSELAGE DAMAGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 MAIN CABIN FLOOR SEAT TRACK DAMAGED AT BS 640, RBL 24. REMOVED AND REPLACED SECTION OF SEAT TRACK IN MAIN CABIN FROM BS 600 TO BS 740 RBL 24 IAW B727 SRM 53-10-8 AND 51-30-2. (M) 2 L 7 3 4F A3WE 2001101600065 20011016 00065 NE 2001 10 16 2001F00432 2 20010916 A 7200 ENGINE BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535* NE RIGHT VIBRATION A NOCA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 EA 15 750NA 26277 A/C AT FL330 EXPERIENCED RIGHT ENGINE VIBRATION. THROTTLE RETARDED AND VIBRATION REMAINED 1.2 AND 3.1 AT EPR 1.71. CRE W REPORTED LEFT ENGINE VIBRATION DURING DESCENT. A/C REQUESTED DIVERSION TO ORF. VIBRATION RETURNED TO NORMAL RANGE ON DESCENT AT FLIGHT LEVEL 170. CREW SUSPECTED ICING. ON GROUND FAULT ISOLATION MANUAL TASK 77-31-00 AVM BITE TEST PERFO RMED. NO FAULTS. BOTH LEFT AND RIGHT ENGINE CHIP DETECTORS INSPECTED. NO METAL FOUND. ENGINE TEST 6 VIBRATION SURVEY PERFORMED. ALL ENGINE PARAMETERS WITHIN LIMITS. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2001101600066 20011016 00066 NM 2001 10 16 P5CA0100597 1 20010929 A 5311 NONE WEB BOEING 747 747123 1384873 NM Zone 100 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 NOSE WHEEL WELL - BS300 INTERNAL VERTICAL BEAM WEB CRACKED BY INSULATION HOLES. FOUND BY H.F.E.C. (3) CRACKS TOTAL. R EPAIRED WITH DOUBLER INSTALLED PER BOEING FAX - PAO-LGB-01-00155H & SRM A5310-33-01. 2 L 7 4 4F A20WE 2001101600067 20011016 00067 NM 2001 10 16 P5CA0100598 1 20010929 A 5311 NONE WEB BOEING 747 747123 1384873 NM CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 NOSEWHEEL WELL - BS320 INTERNAL VERTICAL BEAM WEB WITH 2 INCH LONG CRACK FROM INSULATION HOLE FOUND BY E.F.E.C. REPAIRE D WITH DOUBLER INSTALLED WITH "T" ANGLE PER BOEING FAX - PAO-LGB-01-00155H & SRM A5310-33-01. 2 L 7 4 4F A20WE 2001101600068 20011016 00068 NM 2001 10 16 P5CAO100599 1 20010929 A 5311 NONE WEB BOEING 747 747123 1384873 NM CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 NOSE WHEEL WELL - BS300 INTERNAL VERTICAL BEAM WEB CRACKED BY INSULATION HOLE. FOUND BY H.F.E.C. REPAIRED BY HOLE OPENE D UP & DOUBLER INSTALLED PER BOEING FAX - PAO-LGB-01-00155H & SRM A5310-33-01. 2 L 7 4 4F A20WE 2001101600069 20011016 00069 NM 2001 10 16 P5CA0100600 1 20010929 A 5311 NONE WEB BOEING 747 747123 1384873 NM CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 NOSE WHEEL WELL - INTERNAL VERTICAL BEAM WEB CRACKED AT INSULATION HOLE - 2 INCHES LONG - FOUND BY H.F.E.C. REPAIRED BY REMOVING CRACKED SECTION. INSTALLED SPLICE & DOUBLER PER BOEING FAX - PAO-LGB-01-00155H & SRM A5310-33-01. 2 L 7 4 4F A20WE 2001101600070 20011016 00070 NM 2001 10 16 P5CA0100601 1 20011015 A 3310 16419 TRANSFORMER BOEING 747 747249F 1384849 NM COCKPIT MALFUNCTIONED A P5CA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 23 920FT 22237 SMELLED SMOKE IN COCKPIT. FOUND PILOT'S BACKGROUND LIGHT C/B OPEN & MAIN PANEL BACKGROUND LIGHT CONTROL KNOB VERY HOT. ( NEXT TO THUNDERSTORM LIGHT SWITCH). SMOKE WENT AWAY. REPLACED TRANSFORMER. OPS NORMAL. 2 L 7 4 4F RT A20WE 2001101600071 20011016 00071 SO 2001 10 16 C2XA01CL215 1 20011015 A 2611 FDS765A2 SMOKE DETECTOR EMB 135 EMB135ER 3260203 SO LAV DEFECTIVE A C2XA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 27 17507 3865 145215 CLE FLIGHT#3300 THE CREW REPORTED THE LAV SMOKE DETECTOR WARNING ILLUMINATED.MAINTENANCE INSPECTED AND FOUND NO SMOKE.TH EY REPLACED THE LAV SMOKE DETECTOR.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001101600072 20011016 00072 2001 10 16 2001F00434 4 20010929 A 2210 DAMPER AIRBUS 300 A300B4203 3930306 EU AUTOPILOT SYS MALFUNCTIONED A RJEF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 68142 142 MIA - FLT 841 - DURING TAKEOFF, PITCH TRIM 1 AND 2 DISENGAGED AND COULDN'T BE REENGAGED, YAW DAMPER NR 2 WAS INOPERATIVE AND APU AUTO SHUTDOWN AT FL220 COULDN'T BE RESTART. THE AIRCRAFT RETURNED TO MIA STATION FOR MAINTENANCE. AFTER LANDI NG AT MIA STATION, TECHNICIANS PERFORMED RESET OF THE PITCH TRIM COMPENSATION COMPUTER AND PERFORMED OPERATIONAL TEST OF THE SYSTEM, WITH NORMAL RESULTS AS PER AMM 27-41-00. THE YAW DAMPER SYSTEM WAS ENTER AS DEFERRED DEFECT ITEM AS PER ME L 22-21-01 AND THE APU WAS RE-STARTED AND FAILURE WAS NOT DUPLICATED. AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2001101600073 20011016 00073 EU 2001 10 16 2001F00435 1 20010929 A 4920 APU AIRBUS 300 A300B4203 3930306 EU APU BAY SHUTDOWN A RJEF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 68142 142 MIA - FLT 841 - DURING TAKEOFF, PITCH TRIM 1 AND 2 DISENGAGED AND COULDN'T BE REENGAGED, YAW DAMPER NR 2 WAS INOPERATIVE AND APU AUTO SHUTDOWN AT FL220 COULDN'T BE RESTART. THE AIRCRAFT RETURNED TO MIA STATION, AND THE AIRCRAFT REMAINS ON GROUND FOR MAINTENANCE. (M) 2 L 7 2 4F RT A35EU 2001101600074 20011016 00074 NM 2001 10 16 2001F00414 1 20010718 A 5530 RUB STRIP BOEING 727 72721 1384003 NM VERTICAL STAB BULGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 355QS 19257 VERTICAL STABILIZER, LEFT UPPER SIDE RUB STRIP, SHOWS BULGES IN SEVERAL AREAS. REPAIRED VERTICAL FIN TRACK OUTBOARD LEF T SIDE IAW SRM 51-30-2 AND AVHM-245RO-1 REVISION R1. (M) 2 L 7 3 4F A3WE 2001101600075 20011016 00075 WP 2001 10 16 AALA016082 1 20010909 A 3350 BR9194501 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST NR NOT REPORTED 1 SW 21 871RA 49788 CCI-LAX - RIGHT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. OPS CHECKS NORMAL. (M) 2 L 7 2 4F RT A6WE 2001101600076 20011016 00076 SO 2001 10 16 ASOA01150 1 20010829 A 3350 10130115 SIGN EMB 120 EMB120 3260201 SO CABIN DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 242AS 120069 DURING SCHEDULED MAINTENANCE IN TXK, THE EMERGENCY LIGHTS AT SEAT 5A WERE FOUND DAMAGED. MAINTENANCE REMOVED AND REPLAC ED EMERGENCY EXIT SIGN AT SEAT 5A. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001101600077 20011016 00077 2001 10 16 ASOA01152 4 20010831 A 2350 509111 CONTROL PANEL EMB 120 EMB120 3260201 SO COCKPIT SMOKE A ASOA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 265AS 120170 FLT 4026 - DURING FLIGHT FROM ATL TO ILM, CREW REPORTED SMOKE IN THE COCKPIT. AIRCRAFT DIVERTED AND LANDED SAFELY IN FL 0. CREW ADVISED MAINTENANCE THAT THE SMOKE WAS COMING FROM THE FIRST OFFICERS COMM CONTROL PANEL. MAINTENANCE REMOVED AND REPLACED THE NR 2 AUDIO CONTROL PANEL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001101600078 20011016 00078 SO 2001 10 16 ASOA01157 1 20010905 A 3350 D36604001 BATTERY EMB 120 EMB120 3260201 SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 232AS 120036 DURING HANGAR MAINTENANCE IN TXK, THE OVERWING EMERGENCY EXIT SIGNS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHTING BATTERY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001101600079 20011016 00079 EA 2001 10 16 ASOA01159 1 20010907 A 3350 64641 LIGHT CNDAIR CL600 CL600* EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 843AS 7310 DURING GROUND INSPECTION IN TOL, CREW REPORTED FLOOR LEVEL EMERGENCY TRACK LIGHTING INOPERATIVE AT ROWS 1-6. MAINTENANC E REMOVED AND REPLACED THE CABLE FLOOR TRACK LIGHTING ASSEMBLY AT ROWS 1-6. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR S ERVICE. (M) 2 L 7 2 4F RT A21EA 2001101600080 20011016 00080 EU 2001 10 16 ASOA01160 1 20010908 A 3350 E0062B1A4AC0A SWITCH AEROSP ATR72 ATR72 EU COCKPIT INTERMITTENT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 637AS 383 DURING GROUND INSPECTION IN ATL, THE EMERGENCY LIGHTS WERE OPERATING INTERMITTENTLY. HALF OF THE SWITCHES WERE IN THE AR M POSITION AND NONE WERE IN THE ON POSITION. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT SWITCH. OPERATIONAL CH ECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2001101600081 20011016 00081 SO 2001 10 16 ASOA01161 1 20010910 A 3350 D36604001 BATTERY PACK EMB 120 EMB120 3260201 SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 244AS 120073 DURING GROUND INSPECTION IN ATL, CREW REPORTED SEVERAL EXTERNAL EMERGENCY LIGHTS INOPERATIVE, ONE OVER THE RIGHT WING AN D BOTH OF THE AFT LIGHTS ON EACH ACM PANEL. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY PACK AT CEILING FRAM E 31. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001101600082 20011016 00082 SO 2001 10 16 ASOA01162 1 20010911 A 3350 D36604001 BATTERY EMB 120 EMB120 3260201 SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 230AS 120032 DURING SCHEDULED MAINTENANCE IN MCN, SEVERAL FLOOR TRACK LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY AT ROW 4BC. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001101600083 20011016 00083 SO 2001 10 16 ASOA01163 1 20010914 A 3350 D36604001 BATTERY PACK EMB 120 EMB120 3260201 SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 240AS 16022 120060 DURING GROUND INSPECTION IN ATL, EMERGENCY LIGHTS FROM ROW 6 AFT WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLAC ED THE NR 3 EMERGENCY LIGHTING BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001101600084 20011016 00084 NM 2001 10 16 P2EA2001M0008 1 20011016 A 5300 SKIN BOEING 737 737230 NM A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 124NJ 22122 During Inspection found Crack in fuselage skin at BS 847 and STR. 25R approx. 1.00" in length.See Vanguard Aircraft log page #92242 2 L 7 2 4F RT A16WE 2001101600085 20011016 00085 NM 2001 10 16 MWEA011389 1 20011014 A 7711 S001354196 SENSE LINE DOUG MD88 MD88 3023688 NM RH PYLON LEAKING A MWEA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 701ME 49760 RIGHT ENGINE, ENGINE PRESSURE RATIO INDICATOR KEEPS CLIMBING WITH ENGINE SPEEDS MATCHED -- FOUND PYLON PT2 LINE LEAK. REMOVED AND REPLACED PYLON PT2 LINE. 2 L 7 2 4F RT A6WE 2001101600086 20011016 00086 WP 2001 10 16 MWEA011392 1 20011016 A 5310 59327171 DOUBLER DOUG DC9 DC981 3022081 WP STATION 971 GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 CABIN FUSELAGE SKIN AT STATION 971 ABOVE LONGERON 7 RIGHT HAS DEEP GOUGE -- FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001101600087 20011016 00087 EU 2001 10 16 ASOA01164 1 20010914 A 3350 LP1670 LIGHT AEROSP ATR72 ATR72 EU CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 642AS 395 DURING GROUND INSPECTION IN ATL, FLIGHT ATTENDANT REPORTED THE EMERGENCY LIGHTS BETWEEN ROW 9 AND 11 WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BURNED OUT LIGHT BULBS IN EMERGENCY FLOOR STRIP LIGHT ASSEMBLIES AT ROWS 9-11. OPERATI ONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2001101600088 20011016 00088 EU 2001 10 16 ASOA01166 1 20010906 A 5315 FLOORBEAM AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 632AS 338 DURING C-CHECK INSPECTION IN BNA, MAINTENANCE DISCOVERED CORROSION ON THE FLOORBEAM AT FRAMES 36 AND 38. MAINTENANCE RE PAIRED CORROSION IAW ASA EO 72-53-0115. (M) 2 H 7 2 4T RT 2001101600089 20011016 00089 EU 2001 10 16 ASOA01167 1 20010906 A 5315 FLOORBEAM AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 632AS 338 DURING C-CHECK INSPECTION IN BNA, MAINTENANCE DISCOVERED CORROSION ON THE FLOORBEAM TOP FLANGE AT FRAMES 39, 40 AND 41. MAINTENANCE REPAIRED CORROSION IAW ASA EO 72-53-0115. (M) 2 H 7 2 4T RT 2001101600090 20011016 00090 EU 2001 10 16 ASOA01169 1 20010906 A 5311 FRAME AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 632AS 338 DURING C-CHECK INSPECTION IN BNA, MAINTENANCE DISCOVERED CORROSION AT FRAME 39 FROM STRINGER 21 LEFT TO STRINGER 21 RIGH T. MAINTENANCE REPAIRED CORROSION IAW ASA EO 72-53-0115. (M) 2 H 7 2 4T RT 2001101600091 20011016 00091 NM 2001 10 16 EISA20010124 1 20011005 A 5270 21EN93 SWITCH BOEING 727 727223 1384074 NM MAIN CARGO DOOR INOPERATIVE A EISA A I UNSCHED LANDING CABIN DEPRESSURIZATION J WARNING INDICATION CL CLIMB 1 SW 07 6813 19488 DURING CLIMB, RED MCD LIGHT ALONG WITH AMBER VENT DOOR NOT CLOSED ILLUM. ALONG WITH UNSCHEDULED CLIMB IN CABIN ALT. ACC. AERONAUTICAL MCD WARNING ILLUM. IN FLT. AFTER RAPID DEPRESS. CHECKLIST COMPLETED LAND AT NEAREST SUITABLE AIRPORT.CORRE CTIVE ACTION:DUPLICATED MALFUNCTION ON GROUND AND FOUND VENT DOOR SWITCH ITNERMITTENTLY DEFECTIVE ALLOWING THE VENT DOOR NOT TO CLOSE FULLY. REPLACED VENT DOOR SWITCH AND SYS CHECKED NORMAL WITH A/C PRESSURIZED. 2 L 7 3 4F A3WE 2001101600092 20011016 00092 EU 2001 10 16 ASOA01170 1 20010906 A 5246 ACCESS DOOR AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SO 11 632AS 338 DURING C-CHECK INSPECTION IN BNA, MAINTENANCE DISCOVERED CORROSION ON THE FUEL TANK ACCESS DOOR. MAINTENANCE APPLIED A TEMPORARY REPAIR IAW FAA FORM 810-3, REPORT NR 01-244. MAINTENANCE WILL REPLACE THE FUEL TANK ACCESS DOOR UPON AVAILABI LITY OR THE NEXT C-CHECK, WHICHEVER IS THE EARLIEST. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2001101600093 20011016 00093 SO 2001 10 16 ASOA01171 1 20010916 A 3350 1317 LIGHT EMB 120 EMB120 3260201 SO CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 236AS 120049 DURING SCHEDULED MAINTENANCE IN TXK, THE RIGHT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLAC ED THE RIGHT OVERWING EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001101600094 20011016 00094 2001 10 16 GTIA010875 4 20010910 A 2211 25866865 COMPUTER DOUG DC9 DC931 3022065 WP AUTOPILOT SYS FAULTY A GTIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 23 969ML 47268 FLT 273 - TPA - A/P PITCH SERVO IS ERRATIC, HUNTS UP AND DOWN FLT 273. REMOVED AND REPLACED PITCH AXIS COMPUTER IAW MM 22-13-0. OPS CHECK NORMAL. (M) 2 L 7 2 4F A6WE 2001101600095 20011016 00095 NM 2001 10 16 MWEA011399 1 20011016 A 5310 2912727 LONGERON DOUG MD88 MD88 3023688 NM STA 1306 &1313 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 AFT PIT LONGERON 22 RIGHT HAS TWO AREAS OF CORROSION PRESENT AT STATION 1306 AND 1313 -- REMOVED DAMAGED SECTION AND I NSTALLED REPAIR SPLICES AND LONGERON SECTION. 2 L 7 2 4F RT A6WE 2001101600096 20011016 00096 NE 2001 10 16 GTIA010902 2 20010915 A 7220 5930646505 NOSE BULLET DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE ENGINE DAMAGED A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 957AS 49126 AUTOTHROTTLES OFF AND EQUAL ERP, THE LEFT EPR VALUE DECREASES .11 AND THE RIGHT EPR INITIALLY INCREASES .02 THEN DECREAS ES .03 LEAVING AN EPR SPLIT OF .08 N1 AND N2 BOTH CHANGE BY APPROXIMATELY EQUAL AMOUNT. WITH AUTOTHROTTLES ON AND SYNC ON THE EPR SPLIT IS .16 (N1 AND N2 ARE MATCHED) WITH ENGINE ANTI-ICE ON FOR ABOVE CONDITIONS. CHANGED IN EPR NOTED ABOV E OCCUR WHEN ENGINE ANIT-ICE IS TURNED ON. CRUISE AUTOTHROTTLES/SYNC AND ENGINE ANTI-ICE ON THE RIGHT EPR IS AT MAXIMUM /BOTH N1'S MATCHED AUTHOTHROTTLES UNABLE TO MAINTAIN .76M (FL350) UNLESS AUTOTHROTTLES ARE TURNED OFF AND LEFT THROTTLE ADVANCED. FOUND HOLE IN NR 2 NOSE BULLET REMOVED AND REPLACED IAW MM CH 71-00-00. (M) 2 L 7 2 4F 4 F A6WE E9NE 2001101600097 20011016 00097 WP 2001 10 16 GTIA010903 1 20010916 A 2731 CONTROL CABLE DOUG DC9 DC981 3022081 WP ELEVATOR TAB OUT OF RIG A GTIA O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 818NK 48018 FLL - FLT 779 - ELEVATOR POWER ON LIGHT ILLUMINATES IN FLIGHT WITH 1 UNITS NOSE UP TRIM. FOUND RIGHT CONTROL TAB SECTOR SLIGHTLY OUT OF RIG ADJUSTED CABLE SECTORS 5C AND 6C RIG CHECK OK IAW MM 27-30-00, 27-30-07. (M) 2 L 7 2 4F A6WE 2001101600098 20011016 00098 WP 2001 10 16 GTIA010904 1 20010914 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DIRTY A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 602CA 49415 DTW - EMERGENCY FLOOR PATH LIGHT INOPERATIVE ROW 20 BACK. CLEANED AND RESEALED PACK BATTERY SYSTEM, OP CHECKS GOOD IAW MD80 MM 33-53-00. (M) 2 L 7 2 4F RT A6WE 2001101600099 20011016 00099 2001 10 16 GTIA010905 4 20010918 A 3421 258733511 GYRO DOUG DC9 DC983 3022083 WP COCKPIT FAILED A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 808NK 49504 FLT 923 - AUTO PILOT AND AUTO THROTTLE DISENGAGES AND FMA GO TO GO AROUND MODE. WHEN PERFORMING RTS FOUND AUX GYRO BAD. REMOVED AND REPLACED AUX GYRO IAW MD80 MM 34-23-01, PERFORMED RTS SYSTEMS OPS CHECK GOOD IAW MD80 MM 22-01-05. (M) 2 L 7 2 4F RT A6WE 2001101600100 20011016 00100 CE 2001 10 16 NSVA0112 1 20010925 A 2422 BPC38 INVERTER BEECH 1900 1900C 1154161 CE ELECTRICAL SYS FAILED A NSVA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 129CJ UC129 NR 1 INVERTER FAILED ON TAKEOFF ROLL, ABORTED TAKEOFF RETURNED. MAINTENANCE REMOVED AND REPLACED THE NR 1 INVERTER TEST RUN. OPS CHECK GOOD. AIRCRAFT RELEASE FROM MAINTENANCE. (M) 2 L 7 2 4T RT A24CE 2001101600101 20011016 00101 SO 2001 10 16 SIMA200124703 1 20010904 A 5315 FLOORBEAM EMB 145 EMB145LR SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 643AE 145200 ABI - DURING MBV INSPECTION, FOUND LEFT OMEGA BEAM AT FRAME 25 CORRODED. REMOVED CORROSION FROM LEFT OMEGA BEAM AT FRAM E 25 AND REPAIRED IAW EMB145 SRM AND EMB REPAIR STATEMENT GST-2930/01. (M) 2 L 7 2 4T RT T00011AT 2001101600102 20011016 00102 SO 2001 10 16 SIMA200124704 1 20010904 A 5315 FLOORBEAM EMB 145 EMB145LR SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 643AE 145200 DURING MBV INSPECTION, FOUND LEFT OMEGA BEAM AT FRAME 20 CORRODED. REMOVED CORROSION FROM OMEGA BEAM AT FRAME 20 AND RE PAIRED IAW EMB 145 SRM. (M) 2 L 7 2 4T RT T00011AT 2001101600103 20011016 00103 SO 2001 10 16 SIMA200124705 1 20010904 A 5315 FLOORBEAM EMB 145 EMB145LR SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 643AE 145200 ABI - DURING MBV INSPECTION, FOUND CENTER OMEGA BEAMS AT FRAMES 20 AND 22 CORRODED. REMOVED CORROSION FROM CENTER OMEGA BEAMS AT FRAMES 20 AND 22 AND REPAIRED IAW EMB145 SRM AND EMB REPAIR STATEMENT GST-2930/01. (M) 2 L 7 2 4T RT T00011AT 2001101600104 20011016 00104 SO 2001 10 16 SIMA200125002 1 20010907 A 5315 FLOORBEAM EMB 145 EMB145LR SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 644AE 145204 ABI - DURING MBV INSPECTION, FOUND CORROSION ON THE LEFT OMEGA BEAM AT FRAME 20. REMOVED CORROSION FROM LEFT OMEGA BEAM AT FRAME 20 AND REPAIRED IAW EMB 145 SRM. (M) 2 L 7 2 4T RT T00011AT 2001101600105 20011016 00105 EU 2001 10 16 SABA011053 1 20011014 A 3210 622800200 SWITCH BAG JETSTM JETSTM3201 1500217 EU A SABA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 959AE 959 Aircraft 959 on flight 5222from Charlotte to Lexington; after takeoff the left main gear intransit light illuminated and would not go out. Pilot had cycled the gear up. Gear was cycled down and indicated safe. Aircraft returned to Charlotte and made a safe landing. No emergency was declared. Maintenance trouble shot the system, jacked aircraft, adjusted up-l imit switch and cycled the gear numerous times. Could not get the gear to malfunction. Aircraft was returned to srevice 2 L 7 2 4T RT A56EU 2001101600106 20011016 00106 SO 2001 10 16 SIMA200125101 1 20010908 A 3234 8271013 PIN EMB 145 EMB145LR SO CONTROL HANDLE BENT A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 631AE 145139 DFW - FLT 3745 - AFTER TAKEOFF, CREW REPORTED A LANDING GEAR DISAGREE MESSAGE ON EICAS. LANDING GEAR HANDLE WAS CYCLED SEVERAL TIMES WITH NO SUCCESS. AIRCRAFT WAS RETURNED TO DFW. MAINTENANCE FOUND AN REPOSITIONED LANDING GEAR POSITION S WITCH FROM DOORS TO NORMAL. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. THE NEXT FLIGHT, DURING C LIMB-OUT THE LANDING GEAR HANDLE WOULD NOT MOVE. CREW DECLARED EMERGENCY AND RETURNED TO DFW. MAINTENANCE FOUND A BENT CONNECTOR PIN IN THE LANDING GEAR CONTROL HANDLE. LANDING GEAR CONTROL HANDLE WAS REMOVED AND REPLACED IAW EMB MM. OP ERATIONAL CHECK AS GOOD AND AIRCRAFT WAS RELEASED FOR A FUNCTIONAL CHECK FLIGHT. FCF WAS SATISFACTORY AND AIRCRAFT WAS 2 L 7 2 4T RT T00011AT 2001101600107 20011016 00107 SO 2001 10 16 SIMA200125402 1 20010911 A 3397 CONNECTOR EMB 145 EMB145LR SO CABIN DISCONNECTED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 606AE 145062 ORD - FLT 4221 - DURING TAXI, AFT OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND CANNON PLUG F OR AFT OVERHEAD EMERGENCY LIGHT TO BE DISCONNECTED. CANNON PLUG WAS RECONNECTED IAW EMB 145 AMM. LIGHT OPERATIONALLY C HECKED GOOD. (M) 2 L 7 2 4T RT T00011AT 2001101600108 20011016 00108 SO 2001 10 16 SIMA200126006 1 20010917 A 2760 14533022409 CONTROL UNIT EMB 135 EMB135LR SO SPOILER FAULTY A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 728AE 145328 LGA - FLT 4545 - RETURN TO FIELD DUE TO RUMBLING NOISE COMING FROM NOSE AREA. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE SPOILER CONTROL UNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RET URNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001101600109 20011016 00109 NM 2001 10 16 UIEA01097 1 20010907 A 5320 654U6075594 INTERCOSTAL BOEING 747 747230B 1384889 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 1979 DURING TVCI PER AD 90-06-14 REF SB 747-53-2293 AREA, FOUND VERTICAL CRACK IN INTERCOSTAL, STATION 290, APPROX LBL 26, UP PER NOSE WHEEL WELL BOX, INTERIOR. REMOVED INTERCOSTAL AT STATION 290. REPLACED INTERCOSTAL WITH P/N 654U6075-594 PER B747 SRM 51-30-02 PAGE 5. REMOVED AND REINSTALLED TWO INTERCOSTALS TO GAIN ACCESS PER SRM 51-30-02. (M) 2 L 7 4 4F A20WE 2001101600110 20011016 00110 NM 2001 10 16 USAA011146 1 20010823 A 5312 PRESSURE PANEL BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 385US 46895 22958 CLT - FOUND WEB CRACKED 1.5 INCH, MAIN W/W PRESSURE DECK AT 664 RBL 40. INSTALLED DOUBLER PER TR 53-60-04. (M) 2 L 7 2 4F RT A16WE 2001101600111 20011016 00111 NM 2001 10 16 USAA011154 1 20010827 A 5312 PRESSURE PANEL BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 23312 CLT - FOUND FLOOR SKIN CRACKED 1 INCH, PRESSURE FLOOR RIGHT WHEEL WELL. INSTALLED DOUBLER PER TR 53-60-4. (M) 2 L 7 2 4F RT A16WE 2001101600112 20011016 00112 NM 2001 10 16 USAA011155 1 20010827 A 5312 PRESSURE PANEL BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 46478 23312 CLT - FOUND PRESSURE FLOOR SKIN CRACKED 1 INCH, PRESSURE FLOOR LEFT WHEEL WELL. INSTALLED DOUBLER PER TR 53-60-4. (M) 2 L 7 2 4F RT A16WE 2001101600113 20011016 00113 NM 2001 10 16 USAA011181 1 20010829 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 40268 23559 TPA - FOUND SKIN CRACKED .125 INCH FROM FASTENERS THREE PLACES, STATION 787 AT STRINGER 7R. INSTALLED REPAIR DOUBLER PE R SRM 53-00-01 FIG 201. (M) 2 L 7 2 4F RT A16WE 2001101600114 20011016 00114 NM 2001 10 16 USAA011183 1 20010824 A 7120 310A10227 MOUNT BOEING 737 737301 1384611 NM FORWARD SCORED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 573US 23560 PIT - FOUND MOUNT BEARING BORE SCORED, FORWARD ENGINE MOUNT. MACHINED BORE PER TYPICAL REPAIR 54-50-08 REV A. (M) 2 L 7 2 4F RT A16WE 2001101600115 20011016 00115 NM 2001 10 16 USAA011184 1 20010830 A 5311 BELTFRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 588US 23933 PIT - FOUND BELTFRAME CRACKED .25 INCH, STATION 380 BETWEEN 7R AND 8R. INSTALLED DOUBLER PER TYPICAL REPAIR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001101700001 20011017 00001 NM 2001 10 17 SWAA012822 1 20011015 A 5314 6545409 WEB BOEING 737 7373H4 1384600 NM MAIN WHEEL WELL CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED 1/4 D CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663, LBL 32. REPAIRED WE B PER SWA T1-353-046. 2 L 7 2 4F RT A16WE 2001101700002 20011017 00002 NM 2001 10 17 SWAA012823 1 20011015 A 5311 6545871 FRAME BOEING 737 7373H4 1384600 NM FWD SVC DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR FWD CUTOUT FRAME CRACKED AT # 3 DOOR STOP. REPA IRED FRAME PER SWA T1-152-003. 2 L 7 2 4F RT A16WE 2001101700003 20011017 00003 NM 2001 10 17 SWAA012825 1 20011014 A 3350 07912 COVER BOEING 737 7372T4 1384492 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS CRACKED AT ROWS 7 & 19. R&R COVERS PER MM. 2 L 7 2 4F A16WE 2001101700004 20011017 00004 NM 2001 10 17 SWAA012828 1 20011015 A 2612 1061803 WARNING LIGHT BOEING 737 7375H4 138449D NM COCKPIT ERRATIC A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 522SW 26564 DURING FLIGHT FIRE WARNING LIGHT CAME ON FOR 2 SECONDS AT FLIGHT LEVEL 310 AND WENT OUT, NO OTHER INDICATIONS NOTED. INSPECTED CARGO COMP & ENGINE FOR DEFECTS, NONE NOTED. FIRE TEST OF CARGO COMP & ENGINES NORMA L. 2 L 7 2 4F RT A16WE 2001101700005 20011017 00005 2001 10 17 SWAA012798 4 20011013 A 2565 6557463 BRACKET BOEING 737 7372H4 138448C NM FWD SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 FWD SVC DOOR EMERGENCY EVAC SLIDE RETENTION BAR BRACKET LOOSE. R&R BRACKET PER MM. 2 L 7 2 4F A16WE 2001101700006 20011017 00006 2001 10 17 SWAA012801 4 20011011 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 312SW 23334 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE VEIWING WINDOW LOOSE. SECURED WINDOW PER MM. 2 L 7 2 4F RT A16WE 2001101700007 20011017 00007 2001 10 17 SWAA012808 4 20011011 A 2565 65C16820 HOOK BOEING 737 7373H4 1384600 NM FWD SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 372SW 26599 DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURE D HOOK PER MM. 2 L 7 2 4F RT A16WE 2001101700008 20011017 00008 NM 2001 10 17 SWAA012810 1 20011012 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING WALK AROUND INSPECTION FOUND FUSELAGE SKIN CRACKED 1.0 INCH LONG AT BS 727D + 6, BETWEEN STR 19L & 20L. REPAIRED SKIN PER SRM & SWA RA 1-353-2678. 2 L 7 2 4F RT A16WE 2001101700009 20011017 00009 NM 2001 10 17 SWAA012811 1 20011013 A 5755 6546451 SPOILER BOEING 737 7373H4 1384600 NM RH WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 330SW 23694 DURING SCHEDULED C4 CHECK, FOUND # 9 SPOILER DELAMINATED AT UPPER SIDE. R&R SPOILER PER M M. 2 L 7 2 4F RT A16WE 2001101700010 20011017 00010 NM 2001 10 17 SWAA012812 1 20011013 A 5310 6546569 SHEAR TIE BOEING 737 7373Q8 1384670 NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 987, RBL 51 & WL 199. R&R SHEAR TIE PER SRM . 2 L 7 2 4F RT A16WE 2001101700011 20011017 00011 NM 2001 10 17 SWAA012813 1 20011012 A 5753 6546435 FLAP BOEING 737 7375H4 138449D NM LH WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 507SW 24184 DURING WALK AROUND INSPECTION, FOUND # 1 T/E FLAP DELAMINATED 1 1/2 INCHES FROM AFT T/E. REPAIRE D FLAP PER SRM.. 2 L 7 2 4F RT A16WE 2001101700012 20011017 00012 2001 10 17 SWAA012814 4 20011013 A 2565 6567380 WINDOW BOEING 737 7375H4 138449D NM AFT SVC DOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 504SW 24181 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND VIEWING WINDOW MISSING. INSTALLED VIEWING WINDOW PER MM. 2 L 7 2 4F RT A16WE 2001101700013 20011017 00013 NM 2001 10 17 SWAA012816 1 20011010 A 5330 589337 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED 1/4D CHECK, FOUND BOTH LH & RH COCKPIT UPPER WINDOW POST SKIN CRACKED. RE PAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001101700014 20011017 00014 NM 2001 10 17 SWAA012817 1 20011014 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED 1.0 INCH LONG AT BS 486, STR 16R. REPAIR ED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001101700015 20011017 00015 NM 2001 10 17 SWAA012818 1 20011013 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED 4.0 INCHES AT BS 440, FWD UPPER CORNER CUTOUT FOR FWD CARGO DOOR. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001101700016 20011017 00016 NM 2001 10 17 SWAA012821 1 20011011 A 5311 6546569 FRAME BOEING 737 737317 138447P NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 1006, RBL 34 & WL 200. REPAIRE D FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001101700017 20011017 00017 NM 2001 10 17 USAA011090 1 20010814 A 5300 RIVET BOEING 767 7672B7 1385107 NM BS 889 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 652US 49920 24765 CLT - FOUND WORKING RIVET, BS 889 AND 12R. INSTALLED NEW RIVET PER SRM 51-40-00. (M) 2 L 7 2 4F RT A1NM 2001101700018 20011017 00018 NM 2001 10 17 USAA011125 1 20010821 A 5300 SKIN BOEING 757 7572B7 1384964 NM BS 620 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 30461 27122 CLT - FOUND SKIN WITH LIGHTNING STRIKE, BS 620 - 2.5 INCH, BETWEEN STRINGER 18L AND 19L. DRILLED OUT DAMAGE AND INSTALL ED RIVET PER SRM 53-00-01. (M) 2 L 7 2 4F RT A2NM 2001101700019 20011017 00019 NM 2001 10 17 USAA011227 1 20010910 A 5300 FRAME BOEING 757 7572B7 1384964 NM BS 1540 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 633AU 22292 27811 FOUND FRAME DENTED .75 INCH BY 1.25 INCH, AFT CARGO BS 1540. INSTALLED REPAIR DOUBLER PER EA NR 85390. (M) 2 L 7 2 4F RT A2NM 2001101700020 20011017 00020 NM 2001 10 17 2001UALA02107 1 20011009 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 520UA 24890 AFT PIT FRAME AT STATION 1420 DENTED BETWEEN STRINGER 25L AND 26L. MAJOR REPAIR ACCOMPLISHED.FORMED DOUBLER WAS INSTALL ED ON FRAME. 2 L 7 2 4F 4 F RT A2NM E17NE 2001101700021 20011017 00021 NM 2001 10 17 2001UALA02110 1 20011011 A 5311 CLIP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 520UA 24890 FRAME STATION 1400 STRINGER 25L CLIP REPLACE DUE TO FRAME SPLICE REPAIR. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER C LIP. 2 L 7 2 4F 4 F RT A2NM E17NE 2001101700022 20011017 00022 NM 2001 10 17 2001UALA02111 1 20011011 A 5311 CLIP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 520UA 24890 FRAME STATION 1400 STRINGER 26L CLIP REPLACE DUE TO FRAMESPLICE REPAIR. MAJOR REPAIR ACCOMPLISHED.REPLACED STRINGER 26L CLIP. 2 L 7 2 4F 4 F RT A2NM E17NE 2001102600030 20011026 00030 NM 2001 10 26 2001UALA02117 1 20011011 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 518UA 24871 AFT PIT FUSELAGE FRAME DENT IS OUT OF LIMITS STATION 1420 ABOVE STRINGER 26L LBL 35. MAJOR REPAIR ACCOMPLISHED. INSTAL LED NESTED ANGLE REPAIR ON FRAME. 2 L 7 2 4F 4 F RT A2NM E17NE 2001101700023 20011017 00023 CE 2001 10 17 0017 1 20010928 A 3040 322867003 SHUTOFF VALVE LEAR 35 35A 5170602 CE GARRTT TFE731 TFE7312B WP DEICE SYSTEM LEAKING E CIEA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 NM 03 222BE 489 AT CRUISE ALT 43,000 FT PILOT NOTICE CABIN ALT WARNING LIGHT ILLUMINATED. THE PILOT INITIATED A DESCENT TO 27,000 FT PRE SSURIZATION STARTED WORKING NORMAL. FLT CONTINUED AT 35,000 FT & WORKED NORMAL REST OF FLT. AFTER TROUBLESHOOTING SYS TH E WINDSHIELD DEICE SHUTOFF VALVE WAS FOUND LEAKING AT FLANGE OF THE VALVE. VALVE WAS REPLACED & SYS WAS CHECKED FOR OPER ATION, SYS CHECKED NORMAL. POSSIBLE FACTORS EFFECTING THE SYS, ACFT WAS IN A HEAVY RAIN STORM PRIOR TO TAKEOFF 3-4 HRS & WAS FLOWN IN HEAVY RAIN FOR ABOUT 45 MIN PRIOR TO OCCURRENCE. A LOT OF MOISTURE IN NOSE AVIONICS UPON LANDING. DRAINS WERE FOUND CLEAR. THE AVIONICS DOOR SEALS INSPECTED, NO DEFECTS NOTED. TIME ON VALVE UNKNOWN, ESTIMATED 5300 HRS. 2 L 7 2 4F 4 F A10CE E6WE 2001101700024 20011017 00024 NE 2001 10 17 0113 2 20010927 A 7532 ACTUATOR BOEING 757 757* NM PWA 2037 PW2037 NE LT ENGINE STUCK H UZAF K NONE Y J ENGINE STOPPAGE WARNING INDICATION AP APPROACH 1 EA 29 VPBUB 30060 P728715 DURING FINAL APPROACH AT ALTITUDE 1700 FEET THE LEFT ENGINE WAS AUTOMATICALLY SHUTDOWN. CREW PERFORMED QRH PROCEDURE. AT THE UPPER EICAS DISPLAY EGT OF LEFT ENGINE MAX EXCEEDANCE 652 DEGREES WAS SHOWN. THE SURGE SOUND WAS HEARD. TS IN A CCORDANCE WITH FIM 71-05-00 NO FAILURES FOUND. PW RECOMMENDATION THAT THE ACTUATOR OF 2,5 BLEED VALVE CHECKED. FOUND S TUCK NEAR TO CLOSED POSITION. LEFT ENGINE REPLACED DUE TO ENGINE SURGE AND OVERTEMP. 2 L 7 2 4F 4 F RT A2NM E17NE 2001101700025 20011017 00025 NM 2001 10 17 01FDEA00881 1 20011012 A 7931 ST104ZM1M2 TRANSMITTER BOEING 727 727232 1384082 NM NR 1 ENGINE FAULTY A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 498FE 20867 NR 1 ENG OIL PRESS GAUGE IND 20 PSI PRECAUTIONARY SHUTDOWN. REMOVED AND REPLACED NR 1 OIL PRESS TRANSMITTER PER MM 79-3 3-001-2. OPS & LEAK CHECK GOOD. 2 L 7 3 4F A3WE 2001101700026 20011017 00026 WP 2001 10 17 01FDEA00889 1 20011015 A 5347 SEAT TRACK DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 SEAT TRACK AT BS 1865 TO BS 1871 X=49Z=19 CORRODED. REMOVED AND REPLACED SEAT TRACK PER IAW SRM 53-10-00 FIG 1. 2 L 7 3 4F RT A22WE 2001101700027 20011017 00027 EU 2001 10 17 01FDEA00890 1 20011015 A 7830 WARNING LIGHT AIRBUS 310 A310222 3930315 EU COCKPIT ILLUMINATED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 446FE 224 DURING T/O, NR 1 REVERSER UNLOCK LIGHT ILLUM. RELEASE PER MEL. 2 L 7 2 4F RT A35EU 2001102300054 20011023 00054 GL 2001 10 23 01FDEA00891 2 20011014 A 7321 MEC DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 2 ENGINE FAILED A FDEA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 SO 25 365FE 46601 451448 ON DESCENT NR 2 ENG PWR LEVER FAILED TO CONTROL ENG PWR. SHUTDOWN ENG. REMOVED AND REPLACED NR 2 MAIN ENG CONTROL, FUEL PUMP, FUEL FILTER PER MM. 2 L 7 3 4F 4 F A22WE E23EA 2001101700028 20011017 00028 NM 2001 10 17 01FDEA00892 1 20011016 A 2133 10328051 OUTFLOW VALVE BOEING 727 72722 1384002 NM CABIN PRESSURE FAILED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 149FE 19087 AIRCRAFT FAILED TO PRESS. REMOVED AND REPLACED LEFT OUTFLOW VALVE PER MM 21-30-051-4. 2 L 7 3 4F A3WE 2001101700029 20011017 00029 CE 2001 10 17 A027SA 1 20011009 A 3231 UPLOCK MTSBSI MU300 MU300 5780602 CE RT MLG FAILED E ERYA K NONE O OTHER LD LANDING 1 CE 07 7PW A027SA RIGHT MAIN INBOARD GEAR DOOR (UPON LANDING) DID NOT LATCH IN UP POSITION, ALLOWING DOOR TO LOWER ITSELF TO PAVEMENT, CAU SING SKIN DAMAGE TO DOOR. 2 H 7 2 4F RT A14SW 2001101700030 20011017 00030 NE 2001 10 17 A083SA 2 20011009 A 7261 MS9388140 O-RING MTSBSI MU300 MU300 5780602 CE PWA JT15 JT15D4 52112 NE ENG OIL FILTER DAMAGED E ERYA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION DE DESCENT 1 CE 07 417KT 2 A083SA PCE71173 CREW OBSERVED OIL PRESSURE ON RIGHT ENGINE DROPPING FOLLOWED BY A MASTER WARNING. VERIFIED LOSS OF OIL PRESSURE OCCURRI NG. FLIGHT CREW SHUT RIGHT ENGINE DOWN PRECAUTIONARY AS CHECKLIST COMMANDS. 2 H 7 2 4F 4 F RT A14SW E1NE 2001101700031 20011017 00031 NM 2001 10 17 A6WA200100055 1 20010910 A 7931 TRANSDUCER DORNER DO32 DO328100 2996000 NM PWA 119 PW119C NE RT ENGINE FAULTY A A6WA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 31 337PH 3020 PCE116030 RIGHT OIL PRESSURE HIGH. MAINTENANCE REMOVED AND REPLACED ENG PSI TRANSDUCER, MAIN ENGINE SCAVENGE FILTERS, OIL PUMP RE GULATOR VALVE, AND NR 2 ENG KB HARNESS. 2 H 7 2 4T 4 T RT A45NM E20NE 2001101700032 20011017 00032 NE 2001 10 17 A6WA200100056 2 20010906 A 7532 9799981 SHUTOFF VALVE CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE RT ENGINE FAILED A A6WA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 31 401AW 7332 7332 7280 872590 IN-FLIGHT WITH RIGHT PACK SELECTED ON AND RIGHT 10TH STAGE BLEED SELECTED ON, RIGHT PACK INOP ECS PAGE SHOWED RT PACK AN D 10TH STAGE VALVE CLOSED. CABIN TEMP TOO HIGH, ACFT RETURNED TO DEN. MAINTENANCE REPLACED RIGHT 10TH STAGE BLEED VALV E. 2 L 7 2 4F 4 F RT A21EA E15NE 2001101700033 20011017 00033 WP 2001 10 17 ABXA010529 1 20011006 A 2910 HYDRAULIC SYSTEM DOUG DC8 DC861 3021952 WP MAIN LOW A ABXA K NONE K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 23 853AX 46037 THE GENERAL HYDRAULIC SYSTEM NEEDED SERVICED. THE SYSTEM INDICATED ZERO DURING APPROACH AND LANDING. MAINTENANCE SERVI CED THE GENERAL HYDRAULIC SYSTEM IAW DC-8 MAINTENANCE MANUAL. 2 L 7 4 4F 4A25 2001101700034 20011017 00034 NM 2001 10 17 ABXA010530 1 20011005 A 7732 CONNECTOR BOEING 767 767231 1385131 NM LT ENGINE DIRTY A ABXA K NONE N FALSE WARNING CR CRUISE 1 GL 23 708AX 22571 FRM CODE FOR LEFT ENGINE VIBRATION HIGH INDICATED. OTHER ENGINE INDICATIONS WERE NORMAL. VIBRATION INDICATION CHANGED WITH THRUST LEVER MOVEMENT. HIGHEST INDICATION WAS 1.5 IPS. FAN /LPT0.6 IPS N2. MAINTENANCE COMPLETED ABX767 FIM 71A 05.00 PROCEDURES. CLEANED MINOR OXIDATION FROM LEFT ENGINE FAN VIBRATION ACCELEROMETER CONNECTOR. COMPLETED LEFT ENGIN E RUN. THE ENGINE VIBRATION SYSTEM OPERATIONALLY CHECKED GOOD. 2 L 7 2 4F RT A1NM 2001101700035 20011017 00035 NM 2001 10 17 CALA0100952 1 20011016 A 5315 6546811 FLANGE BOEING 737 7373T0 1384582 NM 986.5 FLOOR BEAM CORRODED A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 70352 23590 AFT CARGO COMPARTMENT UNDER LEFT LAV FLOOR BEAM STATION STATION 986.5 CORRODED. REMOVED CORRODED REPAIR AND REINSTALLED NEW UPPER FLANGE DOUBLER PER SRM 5310-03139 ADN SRM 51-40-2. 2 L 7 2 4F RT A16WE 2001101700036 20011017 00036 NM 2001 10 17 CALA0100953 1 20011016 A 5315 6546811 FLANGE BOEING 737 7373T0 1384582 NM STA 986.5 RT CORRODED A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 70352 23590 AFT CARGO COMPARTMENT UNDER RIGHT LAV FLOOR BEAM STATION 986.5 HAS CORROSION ON THE OUTBOARD. REMOVED CORRODED PREVIOUS REPAIR AND INSTALLED NEW UPPER FLANGE DOUBLER PER SRM 5310-03139 AND SRM 51-40-2. 2 L 7 2 4F RT A16WE 2001101700037 20011017 00037 NM 2001 10 17 CALA0100954 1 20011016 A 5315 6546811 FLANGE BOEING 737 7373T0 1384582 NM STA 986.5 CORRODED A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 70352 23590 AFT CARGO COMPARTMENT UNDER LAV FLOOR BEAMS AT STATION 986.5 NUT CLIPS CORRODED ON UPPER BEAM. REMOVED DAMAGED UPPER BEA M AND CLIPS. INSTALLED REPAIR DOUBLER PER SRM 51-40-2. 2 L 7 2 4F RT A16WE 2001101700038 20011017 00038 NM 2001 10 17 CALA0100957 1 20011016 A 5230 6547952 SKIN BOEING 737 7373T0 1384582 NM INNER DOOR SKIN CRACKED A CALA O K OTHER NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 LIGHTING HOLES DAMAGED ABOVE COUNTER BALANCE CABLES AT A/B/B (1" CRACK). INSTALLED REPAIR AS PER EC/RA 5230-01632. 2 L 7 2 4F RT A16WE 2001101700039 20011017 00039 NM 2001 10 17 ABXA010531 1 20011001 A 2740 251T43101 JACKSCREW BOEING 767 767231 1385131 NM HORIZ STAB DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 709AX 22572 THE HORIZONTAL STABILIZER JACKSCREW LOWER GIMBLE STOPS WERE DAMAGED. MAINTENANCE REPLACED THE HORIZONTAL STABILIZER JAC KSCREW ASSEMBLY IAW B767 MM 27-41-10. OPERATION CHECKS WERE COMPLETED AND WERE SATISFACTORY. 2 L 7 2 4F RT A1NM 2001101700040 20011017 00040 WP 2001 10 17 ABXA010532 1 20011008 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 939AX 47201 THE EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES IAW DC-9 MM 33-53-00. THE EMER GENCY LIGHT BATTERY PACK WAS DEFERRED FOR REPLACEMENT. THE EMERGENCY LIGHT BATTERY PACK WAS REPLACED. 2 L 7 2 4F A6WE 2001101700041 20011017 00041 WP 2001 10 17 ANCF200100016 1 20011008 A 2121 FAN DOUG DC9 DC983 3022083 WP COCKPIT FAILED W ANCF A UNSCHED LANDING O OTHER CL CLIMB 1 SO 23 632CT 49632 DURING CLIMB STRONG NOISE WAS HEARD CLOSE TO THE RT AFT WINDOW IN THE COCKPIT AND BETWEEN 15 & 16 ROW CEILING IN THE CAB IN. WHEN LEVELED OFF AT FL310 THE AHRS NR 2 WAS LOST, CONTINUING THE FLIGHT WITH TRANSFER BOTH ON 1. RETURNED TO BOGOT A. CIRCUIT BREAKER B10-396 AND AHRS FAN NR 2 WERE REPLACED AHRS 1 & 2 WERE SWAPPED IN ACCORDANCE WITH AMM 34-21-10/201. TESTS OK. 2 L 7 2 4F RT A6WE 2001102400074 20011024 00074 WP 2001 10 24 ARWA0011003 1 20011009 A 3231 DOOR DOUG DC8 DC862 3021970 WP NLG OPEN A ARWA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 19 8969U 46070 AFTER GEAR RETRACTION LOUD NOISE AND VIBRATION COMING FROM NOSE WHEEL WELL. NOISE DISAPPEARED ON SHORT FINAL WITH GEAR DOWN. OVERWEIGHT LANDING AT PANC. UPON RETURN TO RAMP AFTER SPEAKING TO GROUND CREW FOUND NOSE GEAR DOORS WERE LEFT OP EN. RESET NOSE LANDING GEAR DOORS FOLLOW UP, INSPECT AREA FOR DAMAGE, NONE FOUND IAW MM 32-22-1. OVERWEIGHT LANDING IN SPECTION ACCOMPLISHED, NO DEFECTS FOUND AS PER ARROW AIR DC8-60 W/C 6372. 2 L 7 4 4F 4A25 2001101700042 20011017 00042 WP 2001 10 17 ARWA0011004 1 20011010 A 2612 894885 FIRE LOOP LKHEED 1011 1011385114 WP NR 2 ENGINE MALFUNCTIONED A ARWA E F A ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 19 260FA 193A1158 ENGINE NR 2 FIRE WARNING SHUTDOWN AT 1320Z, BOTH BOTTLES DISCHARGED WARNING CONTINUED (B-LOOP ON DMI), AIRCRAFT HAD AN U NEVENTFUL LANDING. REMOVED AND REPLACED ZONE 1 LOWER LOOPS CLEAR DMI 15678, GROUND OPERATIONAL NORMAL IAW 26-12-00. RE MOVED AND REPLACED BOTH FIRE BOTTLES AND CARTRIDGES IAW 26-21-02, OPS CK NORMAL. 2 L 7 3 4F A23WE 2001101700043 20011017 00043 NE 2001 10 17 ARWA0011006 2 20011012 A 7200 ENGINE LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B402 54555 NE NR 3 VIBRATION A ARWA E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SO 19 308GB 193U1133 ENGINE NR 3 SHUTDOWN AT 0535Z DUE TO VIBRATION A & B LOW POSITION 2.5 WARNING LIGHT ON OTHER PARAMETERS NORMAL. 2 L 7 3 4F 4 F A23WE E12EU 2001101700044 20011017 00044 NM 2001 10 17 AWXA200100154 1 20011004 A 5315 6546568157 FLOORBEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - C18 CK-C, CORROSION FOUND ON FLOORBEAM UPPER HORIZONTAL FLANGE AT BS 1016, LBL 6, WL 208.1, BEYOND SRM LIMITS AFTE R CORROSION CLEAN UP. MAINTENANCE REPAIRED THE FLOORBEAM UPPER HORIZONTAL FLANGE IAW SRM 53-00-51 FIG 203 PG 212 - 214. 2 L 7 2 4F RT A16WE 2001101700045 20011017 00045 NM 2001 10 17 AWXA200100500 1 20011001 A 7931 ST104Z TRANSMITTER BOEING 737 737277 1384570 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE INACCURATE A AWXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 28 182AW 28380 3941 22649 P708351B ICT - ABORTED TAKEOFF - FLT 620 - C - DURING T/O ROLL, THE CREW NOTED THE NR 2 ENG OIL PRESS WAS AT 23 PSI AND REJECTED THE T/O BETWEEN 100 & 110 KTS. SHUT THE ENG DOWN WHILE TAXIING. NOTE: OIL TEMP AND QUANTITY BOTH INDICATED GOOD. MAIN TENANCE TROUBLESHOT AND REPLACED THE NR 2 ENG OIL PRESS TRANSMITTER IAW B737 AMM 79-32-11. PERFORMED AN ENGINE RUN AT T /O POWER AND ALL CHECKS WERE GOOD. MAINTENANCE PERFORMED HIGH ENERGY STOP INSPECTION IAW AWA TASK CARD F8M32001. NO DI SCREPANCIES WERE NOTED. 2 L 7 2 4F 4 F RT A16WE E2EA 2001101700046 20011017 00046 EU 2001 10 17 AWXA200100520 1 20011009 A 2130 VFT300A1 VALVE AIRBUS 320 A320232 3930326 EU CABIN PRESSURE FAILED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 619AW 19077 5753 527 DEN - ABORTED TAKEOFF - C - ON T/O ROLL THE CREW GOT CLASS 1 ECAM MESSAGE FOR SKIN VALVE FAULT AND REJECTED THE T/O AT 9 0 KTS. MX PLACED THE SKIN AIR EXTRACT VALVE ON MEL 21-26-04, COND 1. IN PHX MX C/W BITE CHECK IAW AMM 21-26-55 AFTER R EACTIVATION, OP'S CHECKED GOOD AT THAT TIME AND THE MEL WAS CLEARED. ON 10/10/01 THE FAULT RETURNED. MX TROUBLESHOT AN D REPLACED AVEC (10HQ), EXHAUST VALVE PRESS SW (30HQ) AND PERFORMED WIRING CHECKS BETWEEN AEVC AND SAOV (22HQ). STILL F AILED TEST IAW 21-26-00-710-00-1. MX REPLACED THE SKIN AIR OUTLET VALVE (SAOV 22HQ) PER AWA TECH SUPPORT, AND FUNCTIONA L CHECKS WERE GOOD. NOTE: PREVIOUS FAULT SHOWS SKIN AIR VALVE. NO FURTHER DISCREPANCIES REPORTED. 2 L 7 2 4F RT A28NM 2001101700047 20011017 00047 2001 10 17 AWXA200100521 4 20011008 A 2330 RDAM699328 HARNESS BOEING 757 757225 1384959 NM CABIN BROKEN A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 907AW 22691 AFTER T/O LANDING GEAR REQUIRED LOCK OVERRIDE TO RETRACT LANDING GEAR, DIVERTED TO PHX. RECENT HISTORY OF INTERMITTENT RT MLG INDICATION PROBLEMS & GEAR LEVER LOCK SOLENOID CHATTERING PROBLEMS. TROUBLESHOT, REPLACED SEVERAL COMPONENTS, CA USED BY EMI FROM THE PASSENGER ENTERTAINMENT SYSTEM WIRE HARNESS RT SIDE OF THE ACFT (AWA HAS PREVIOUS EXPERIENCE WITH T HIS PHENOMENON). WIRE HARNESS PLACED ON ORDER, PRE-RECORDED PASSENGER ANNOUNCEMENT SYSTEM PLACED ON MEL 23-31-2, COND 1 . C/B'S E-2, C-6,C-7 & C-8 WERE PULLED & COLLARED. MX INSPECTED ALL SEAT WIRE HARNESS RT SIDE, REPLACED WIRE HARNESS S EAT 7D & 30D DUE TO CHAFING & BROKEN WIRES. ALL OTHER HARNESS FOUND TO BE SERVICEABLE. MEL CLEARED. 2 L 7 2 4F RT A2NM 2001101700048 20011017 00048 EU 2001 10 17 AWXA200100522 1 20011009 A 2913 693335 PUMP AIRBUS 320 A320231 3930325 EU HYDRAULIC SYS OVERHEATED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 635AW 6462 4951 092 PHX - AIR TURNBACK - FLT 794 - C - ON CLIMBOUT THE CREW GOT ECAM MESSAGE FOR BLUE HYD SYS ELECTRIC PUMP OVERHEAT. THE C REW FOLLOWED ECAM PROCEDURES AND RETURNED TO PHX. THE ECAM MESSAGE WAS DISPLAYED ENTIRE FLIGHT. MAINTENANCE TROUBLESHO T AND REPLACED THE BLUE SYSTEM ELECTRIC HYDRAULIC PUMP IAW AMM 29-12-51, OPERATIONAL AND LEAK CHECKS WERE GOOD. NO FURT HER DISCREPANCIES HAVE BEEN REPORTED. 2 L 7 2 4F RT A28NM 2001101700049 20011017 00049 NM 2001 10 17 AWXA200100523 1 20011001 A 5315 65C31392 FLOORBEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - C18 CK - C - CORROSION FOUND ON FLOORBEAM UPPER FLANGE AT BS 294.5, RBL 32, BEYOND SRM LIMITS AFTER CORROSION CLEA N UP. MAINTENANCE REMOVED DAMAGED FLOORBEAM UPPER CHORD, FABRICATED AND INSTALLED FLOORBEAM UPPER CHORD IAW B737 SRM 53 -10-51, FIG 205, PG 220 - 223. 2 L 7 2 4F RT A16WE 2001101700050 20011017 00050 NM 2001 10 17 AWXA200100524 1 20011004 A 5315 6546568157 FLOORBEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - C18 CK - C - CORROSION FOUND ON FLOORBEAM UPPER HORIZONTAL FLANGE AT BS 1016, LBL 6, WL 208.1, BEYOND SRM LIMITS A FTER CORROSION CLEAN UP. MAINTENANCE REPAIRED THE FLOORBEAM UPPER HORIZONTAL FLANGE IAW SRM 53-00-51 FIG 203 PG 212 - 2 14. 2 L 7 2 4F RT A16WE 2001101700051 20011017 00051 NM 2001 10 17 CALA0100935 1 20011006 A 5330 DOUBLER BOEING 737 7373T0 1384582 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 INSPECTION FOUND SKIN DOUBLER TORN IN TWO LOCATIONS AT EXHAUST DUCT ATTACH POINT IN E&E COMPARTMENT BELLY OF AIRCRAFT. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001101700052 20011017 00052 NM 2001 10 17 CALA0100937 1 20011010 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 INSPECTION FOUND A 2 INCH CRACK COMING FROM HI-LOC HOLE IN BOTH THE RT AND LT O/B FLOOR TRACKS AT STA 727B. BOTH FLOOR TRACKS WERE REPAIRED IAW ECRA 5310-04202. 2 L 7 2 4F RT A16WE 2001101700053 20011017 00053 NM 2001 10 17 CALA0100938 1 20011010 A 5347 CARGO TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 INSPECTION FOUND RT TIE DOWN CHANNEL CORRODED AROUND FASTENERS AT STA 500A-500D IN FORWARD BAGGAGE BIN. THE TIE DOWN CH ANNEL WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001101700054 20011017 00054 NM 2001 10 17 CALA0100940 1 20011011 A 5320 WEB BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70352 23590 INSPECTION FOUND A 1 INCH CRACK IN CABIN FLOOR WEB ON AFT SIDE OF FLOORBEAM AT BS 328. AN INTERCOSTAL WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001101700055 20011017 00055 NM 2001 10 17 CALA0100941 1 20011011 A 5320 WEB BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70352 23590 INSPECTION FOUND A 1 INCH CRACK IN CABIN FLOOR WEB ON FORWARD SIDE OF FLOORBEAM AT BS 328. AN INTERCOSTAL WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001101700056 20011017 00056 2001 10 17 CALA0100943 4 20011011 A 2562 416N222019 BOTTLE BOEING 757 757224 1384958 NM OVERWING SLIDE INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 67134 11031 29283 THE RT OVERWING SLIDE BOTTLE PRESSURE WOULD NOT TEST. THE SLIDE BOTTLE WAS REMOVED AND REPLACED IAW MM 25-65-02 AND OPE RATION CHECKED GOOD. 2 L 7 2 4F RT A2NM 2001101700057 20011017 00057 NM 2001 10 17 CALA0100946 1 20011013 A 2916 RESERVOIR BOEING 757 757224 1384958 NM HYDRAULIC SYS OVERSERVICED A CALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 14121 27563 VISIBLE SMOKE WITH ODOR OF BURNING RUBBER IN CABIN AT FL 390. TURNED OFF RECIRC FANS, ODOR AND SMOKE DISSIPATED, DURING DESCENT AND LANDING. FOUND RT HYD SYS RESERVOIR OVERFULL. DRAINED TO PROPER LEVEL. NO OTHER DISCREPANCIES FOUND. NO ODOR OR SMELL USING ACFT PACKS AT GATE. 2 L 7 2 4F RT A2NM 2001101700058 20011017 00058 NM 2001 10 17 CALA0100947 1 20011012 A 5315 6545818 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69333 23571 FLOORBEAM BS 360, RBL 0-60, CORROSION UNDER G-2 GALLEY. REPAIRED FLOORBEAM IN REF TO SRM 53-00-51. 2 L 7 2 4F RT A16WE 2001101700059 20011017 00059 NM 2001 10 17 CALA0100948 1 20011015 A 5320 6545783502 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70352 23590 FBB 3 INCH CRACK ON FLOOR SUPPORT STRUCTURE BETWEEN STA 500 AND 500A AND ABOUT 2 INCHES TO RT SIDE FROM CENTER LINE MARK ED. REMOVED AND REPLACED SUPPORT PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001101700060 20011017 00060 SO 2001 10 17 C2XA01CL216 1 20011016 A 3350 7287103507 MODULE EMB 135 EMB135LR SO CABIN DEFECTIVE A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 14514 244 28 145303 CLE FLIGHT# 3574 THE CREW REPORTED THE EMERGENCY LIGHTS CAME ON IN FLIGHT.THEY COULD ONLY BE TURNED OFF WITH THE COCKPIT SWITCH.CABIN SWITCH HAD NO CONTROL.MAINTENANCE REPLACED THE CABIN LIGHT CONTROL MODULE.OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT TOOO11AT 2001101700061 20011017 00061 NM 2001 10 17 CALA0100949 1 20011015 A 5230 6547952524 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 THIRD LIGHTENING HOLE FROM AFT END OF DOOR AND THIRD LIGHTENING HOLE FROM TOP OF DOOR HAS A CRACK. INSTALLED REPAIR PER EC/RA 5230-01630. 2 L 7 2 4F RT A16WE 2001101700062 20011017 00062 NM 2001 10 17 CALA0100951 1 20011015 A 5347 655548424 CARGO TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70352 23590 FORWARD BAG BIN CRACKED (10 INCHES) ON RIGHT TIE DOWN RAIL FROM STATION 480 - 500. INSTALLED NUT PLATES ON UPPER FLANGE OF TIE DOWN RAIL PER SRM 51-10-2. 2 L 7 2 4F RT A16WE 2001101700063 20011017 00063 EU 2001 10 17 DHL2001363026 1 20011012 A 2560 SMOKE BARRIER AIRBUS 300 A300B4203 3930306 EU COCKPIT TORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 SMOKE BARRIER HAS TEAR. REMOVED AND REPLACED SMOKE BARRIER IAW BE AEROSPACE A300B4 SMOKE BARRIER MANUAL. OK FOR SERVIC E. 2 L 7 2 4F RT A35EU 2001101700064 20011017 00064 NM 2001 10 17 UPS01237055 1 20010928 A 5330 STRINGER BOEING 727 72762C 138402C NM STR. 19R BS1120 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 913UP 19245 INSPECTION TYPE:C SUSPECT CORROSION AT BS 1120 STR 19R AREA PAINT STRIPPED, AREA OF SUSPECT CORROSION DERIVETED, SUR FACE CO RROSION AND SEALANT REMOVED BETWEEN BS1110-1130 STR19R, STRINGER 19R CUT AND REMOVED AT BS1115-1135, INTERCOSTA L BETWEEN 1110-1130 S19R REMOVED. CORROSION REMOVED FROM BETWEEN STRINGER AND STRUCTURE AND R EPROTECTED.STRINGER AND IN TERCOSTAL REPAIRED REPLACED 2 L 7 3 4F A3WE 2001101700065 20011017 00065 NM 2001 10 17 UPS01237058 1 20011005 A 2750 PANEL BOEING 727 72762C 138402C NM RH WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 913UP 19245 INSPECTION TYPE:C RH WING, WHILE BLENDING PAINT FROM A DENT ON PANEL 65-21655-470 IT W AS NOTED THAT THE UPPER SKIN WAS CRACKED REPAIRED IAW SRM 51-40-20 2 L 7 3 4F A3WE 2001101700066 20011017 00066 NM 2001 10 17 UPS01237064 1 20010921 A 5330 SKIN BOEING 727 727173C 1384059 NM NWW BS290-288 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C NOSE W/W PRESSURE CEILING IS CRACKED AT BL-0. BETWEEN BS 290-288, CONFIRMED BY NDT. CUT OUT CRACK AT NWW PRESSURE CEILING AT BL-0 STA 303 APPROX 3"X1" IAW B727 SRM 51-40-2. INSTALLED DOUBLER REPAIR ON NWW PRESSURE CE ILING IAW B727 SRM 51-40-2. 2 L 7 3 4F A3WE 2001101700067 20011017 00067 NM 2001 10 17 UPS01237065 1 20010921 A 5330 SKIN BOEING 727 727173C 1384059 NM NWW BS260-265 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C NWW R/H PRESSURE WEB IS CRACKED BETWEEN BS 260-265, JUST BELOW PANEL #3125, CONFIRMED BY NDT. CUT OUT CRACK AREA AT NWW R/H PERSURE WEB BS 260-365 AS PER B727 SRM 51-40-2 APPROX 2"X1". INSTALLED DOUBLER REPIAR AS PER B727 SRM 51-4 0-2. 2 L 7 3 4F A3WE 2001101700068 20011017 00068 NM 2001 10 17 UPS01237066 1 20010921 A 5330 NA SKIN BOEING 727 727173C 1384059 NM NWW BS277 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C NWW R/H PRESSURE WEB IS CRACKED EXTENDING FROM REPAIR DOUBLER AT BS 277, APPROX 8" FROM BOTOM OF WW, C ONFIRMED BY NDT. REMOVED OLD DOUBLER REPAIR IAW B727 SRM 51-40-2. CUT OUT CRACK AT N WW RH PRESSURE WEB BS 277 IAW B727 SRM 51-40-2. INSTALLED EXTENDED DOUBLER REPAIR AND FILLER IAW B727 SRM 51-40-2. 2 L 7 3 4F A3WE 2001101700069 20011017 00069 NM 2001 10 17 UPS01237068 1 20010921 A 5330 NA SKIN BOEING 727 727173C 1384059 NM NWW BS285 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C NWW PRESS CEILING IS CRACKED AT BS 285, BETWEEN RBL 3 AND RBL 6, CON FIRMED BY NDT. CUT OUT CRACK AT NWW PRESS CEILING RBL 3 APPROX 4"X1" AND AT LBL 6 APPROX 5"X1" IAW B727 SRM 51-40-2. INSTALLED DOUBLER REPAIR AT NWW PRESS CEILING BS 285 IAW B727 SRM 51-40-2. 2 L 7 3 4F A3WE 2001101700070 20011017 00070 NM 2001 10 17 UPS01237069 1 20011001 A 2760 651734742 SPOILER PANEL BOEING 727 72762C 138402C NM #1 SPOILER DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 913UP 19245 INSPECTION TYPE:C L/H WING DELAM ON #1 SPOILER PANEL PANEL REPLACED 2 L 7 3 4F A3WE 2001101700071 20011017 00071 NM 2001 10 17 UPS01237072 1 20010919 A 5740 NA SPLICE PLATE BOEING 727 727173C 1384059 NM STR18 ALT SIDE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C LEFT MAIN WHEEL WELL CENTER SPLICE PLATE, CRACK AT STR 18 ALT BS935 STOP DRILED END OF CRACK IAW B 727 SRM 51-10-10, INSTALLED REPAIR STR 18 ALT SIDE FUSELAGE SKIN IAW B727 EO B727-5330-3815A. 2 L 7 3 4F A3WE 2001101700072 20011017 00072 NM 2001 10 17 UPS01237075 1 20010919 A 5740 NA SPLICE PLATE BOEING 727 727173C 1384059 NM BS 935 STR 18A CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C RIGHT MAIN W/W CENTER SPLICE PLATE CRACKED AT STR 18A RT. STA 935 STOP DRILLED END OF CRACK IAW B7 27 SRM 51-10-1. INSTALLED REPAIR IAW EO B727-5330-3815A ON FUSELAGE SKIN BS 935 STR 18A R/H SIDE. 2 L 7 3 4F A3WE 2001101700073 20011017 00073 NM 2001 10 17 UPS01237076 1 20010919 A 5330 NA SKIN BOEING 727 727173C 1384059 NM BS300 STR25L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C LEFT NOSE SECTION EXTERIOR FUSELAGE SKIN SHOWS BULGE STR 25L AND BS 300. CUT OUT DAMAGED AREA AT E XTERIOR FUSELAGE SKIN L/H STR 25L BS 300, APROX 10"X3" IAW B727 53-30-3 FIG 3. REMOVED CORROSION ON SKIN STA 310 STR 25 L, MATERIAL LOST .003"; WITHIN LIMITS IAW B727 SRM 53-10-1 INSTALLED DOUBLER REPAIR IAW B727 SRM 53-30-3. 2 L 7 3 4F A3WE 2001101700074 20011017 00074 NM 2001 10 17 DHL2001712016 1 20011013 A 2612 FIRE LOOP BOEING 727 72729 1384007 NM NR 3 ENGINE BROKEN A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 712DH 19401 NR 3 FIRE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED INFLIGHT. NR 3 ENGINE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED DUR ING CLIMBOUT FROM MCI. IN CRUISE, LIGHT DIMMED BUT REMAINED ON. OPENED NR 3 ENGINE CHECKED ROUTING OF SENSOR LOOP SECU RE CLAMP AND REPOSITIONED LOOP SYSTEM CHECK GOOD IAW (REF 26-11-000) CLOSED COWLING. REPAIRED BROKEN WIRE ON NR 3 ENG F IRE LOOP IAW WPM 20-10-13 & 20-60-06. TESTED IAW MM 26-11-01. SYSTEM OPS CKECKS GOOD. 2 L 7 3 4F A3WE 2001113000100 20011130 00100 NE 2001 11 30 DHL2001720013 2 20011011 A 7200 JT8D7B ENGINE BOEING 727 727228 1384083 NM PWA JT8 JT8D7B 52053 NE NR 1 FAILED A DHLA O OTHER Y ENGINE STOPPAGE CR CRUISE 1 SO 01 720DH 19544 INFLIGHT ENGINE FAILURE NR 1 ENGINE. REMOVED AND REPLACED NR 1 ENGINE IAW DHL B727 MAINT TASK MANUAL NR 1 ENG CHANGE WO RKSHEET. RAN ENGINE PER JRH 7.9, OPS CHECKED GOOD. 2 L 7 3 4F 4 F RT A3WE E2EA 2001101700075 20011017 00075 NM 2001 10 17 DHL2001726006 1 20011006 A 5313 STRINGER BOEING 727 727228 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 FCD INSPECTION- AIR CONDITIONING BAY STR 26R SHOW BULGING AND CRACK CORROSION AT DIFFERENT SPOTS FROM 720 THRU 740. CUT OUT AND REMOVED CRACKED AND CORRODED SECTION OF STRINGER 26R FROM STA 740 TO STA 720 IAW B727 SRM 53-10-3 FIG 1. REMOV ED SURFACE CORROSION ON SKIN, FOUND TO BE WITHIN LIMITS. INSTALLED STRINGER REPAIR PER SRM B727 53-10-3 FIG 1 DETAIL 1. 2 L 7 3 4F A3WE 2001101700076 20011017 00076 NM 2001 10 17 DHL2001726007 1 20011006 A 5313 STRINGER BOEING 727 727228 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 FCD INSP - AIR COND DISTRIBUT BAY STRING 27R SHOW CRACK CORROSION AND BULGING FROM BS 720F THRU BS 740. CUT OUT AND REMO VED 8.5 SECTION OF CRACKED & CORRODED STR 27R STA 740 TO STA 720F IAW B727 SRM 53-10-3 FIG 1. REMOVED SURFACE CORROSION ON SKIN .001 FOUND TO BE WITHIN LIMITS. SPLICED IN A NEW SECTION OF STR 27R FROM STA 740 TO 720F 8.5 IAW B727 SRM 53-10 -3 FIG 1, 27R FROM STA 740 TO 720F. 2 L 7 3 4F A3WE 2001101700077 20011017 00077 NM 2001 10 17 DHL2001746003 1 20011011 A 2612 POWER UNIT BOEING 727 727224 1384076 NM APU FAILED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 746DH 22252 APU WILL NOT FIRE TEST. REMOVED AND REPLACED OPERATING POWER UNIT, OPS CKS NORMAL PER B727 MM 26-15-00. APU FIRE TEST NORMAL S/N 2402 OFF 1549 ON P/N 1014A. 2 L 7 3 4F A3WE 2001101700078 20011017 00078 WP 2001 10 17 DHL2001806017 1 20011013 A 2611 SMOKE DETECTOR DOUG DC8 DC873F 302199F WP CABIN INOPERATIVE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 NR 1 SMOKE DETECTOR NOT SECURE AND NR 5 SMOKE DETECTOR INOP. RESECURED SMOKE DETECTOR IAW 26-15-05, RELAMPED SMOKE DETE CTOR IAW 26-15-5. 2 L 7 4 4F RT 4A25 2001101700079 20011017 00079 WP 2001 10 17 DHL2001807026 1 20011016 A 2612 FIRE LOOP DOUG DC8 DC873F 302199F WP NR 4 ENGINE OUT OF POSITION A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 NR 4 ENG B-LOOP SHORT TEST LIGHT IN ON. FOUND GROUNDED LOOP REPOSITIONED, OPS CK'D OK IAW MM 26-10-0. 2 L 7 4 4F RT 4A25 2001101700080 20011017 00080 EU 2001 10 17 MALA010729 1 20011001 A 5330 SKIN SAAB SF340 SF340A 7850100 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 142XJ 142 LT FUSELAGE 55 INCHES AFT OF PAX DOOR, 14 INCHES UP FROM TOP WINDOW LINE IN THE R, DENT APPROXIMATELY 6 X 6 INCH DEEPEST .065. REPAIRED DENT IAW EO S53009. THIS EO IS A GENERIC REPAIR FOR DENTS IN CABIN SKIN BETWEEN STA 339 - 389 AND 487 - 608 ONLY. REFERENCE SAAB SRM 53-70-10. THIS DOUBLER/TRIPLER REPAIR IS USED WHEN THE REPAIR FASTENERS OVERLAP THE CEN TER CABIN .050 INCH WINDOW REINFORCEMENT DOUBLER THAT IS BONDED TO THE FUSELAGE SKIN. 2 L 7 2 4T RT A52EU 2001101700081 20011017 00081 EU 2001 10 17 MALA010736 1 20010923 A 2710 7227105623 CONTROL CABLE SAAB SF340 SF340A 7850100 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 110XJ 340A110 DURING 4K-CHECK IN CWAM LT INBOARD AILERON FWD FUSELAGE CABLE IS CHAFED. MAINTENANCE INSTALLED NEW LT I/B FWD AILERON F USELAGE CABLE P/N 7227105-623 IAW SAAB AMM 27-11-25. 2 L 7 2 4T RT A52EU 2001101700082 20011017 00082 EU 2001 10 17 MALA010737 1 20010923 A 2730 7227105712 CONTROL CABLE SAAB SF340 SF340A 7850100 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 110XJ 340A110 DURING 4K-CHECK IN CWA, LT OUTBOARD FWD FUSELAGE ELEVATOR CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED LT OUTBOARD FW D ELEVATOR CABLE P/N 7227105-712, IAW SF3 AMM 27-31-15. 2 L 7 2 4T RT A52EU 2001101700083 20011017 00083 EU 2001 10 17 MALA010738 1 20010925 A 2730 7227215841 CONTROL CABLE SAAB SF340 SF340A 7850100 EU ELEVATOR CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 110XJ 340A110 DURING 4K-CHECK IN CWA, LT OUTBOARD AFT ELEVATOR CABLE CORRODED. MAINTENANCE REPLACED LT OUTBOARD AFT ELEVATOR CABLE P/ N 7227215-841 IAW SF340 AMM 27-31-15-4. 2 L 7 2 4T RT A52EU 2001101700084 20011017 00084 EU 2001 10 17 MALA010739 1 20010925 A 2730 7227215946 CONTROL CABLE SAAB SF340 SF340A 7850100 EU ELEVATOR BROKEN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 110XJ 340A110 DURING 4K-CHECK IN CWA, LT INBOARD AFT ELEVATOR CABLE HAS A BROKEN WIRE. MAINTENANCE REPLACED LT INBOARD AFT ELEVATOR C ABLE P/N 7227215-946 IAW SF340 AMM 27-31-15-4. 2 L 7 2 4T RT A52EU 2001101700085 20011017 00085 EU 2001 10 17 MALA010740 1 20010926 A 5347 SEAT TRACK SAAB SF340 SF340A 7850100 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 110XJ 340A110 DURING 4K-CHECK IN CWA, LT CENTER AISLE SEAT TRACK LBL 18.3 FWD PORTION OF FLOOR BOARD FLANGE HAS CORROSION, STARTING AT APPROXIMATELY STA 297. MAINTENANCE INSTALLED NEW SECTION OF SEAT TRACK ON LT CENTER AISLE IAW EO S53060 DATED 11-07-20 00. 2 L 7 2 4T RT A52EU 2001101700086 20011017 00086 EU 2001 10 17 MALA010741 1 20011003 A 2140 HEATER SAAB SF340 SF340A 7850100 EU CABIN SPARKS A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 991XJ 340A091 PILOT ON FLIGHT 3009 REPORTED TO MAINTENANCE CONTROL THE MID CABIN DC AUX HEATER WAS EXPELLING SPARKS OUT VENT IN ROW 6, AND SMELLED HOT (ELECTRICAL SMELL). MAINTENANCE INSPECTED ROW 6 HEATER, NO ELECTRICAL SMELL NOTICED. REMOVED HEATER S HROUD, CLEANED SMALL PAPERS AND DEBRIS FROM HEATER. RAN HEATER FOR 1015 MINUTES. NO SMELL AND NORMAL OPERATION. 2 L 7 2 4T RT A52EU 2001101700087 20011017 00087 EU 2001 10 17 MALA010743 1 20011009 A 7931 IPTE551000200D TRANSDUCER SAAB SF340 SF340A 7850100 EU RT ENGINE FAULTY A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 68XJ 340A068 AFTER TAKEOFF OF FLIGHT 3236, R PROP GAUGE INDICATED MAX OIL PRESSURE. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPL ACED RT PGB OIL PRESSURE TRANSDUCER P/N IPTE55-1000-200D10 IAW SAAB AMM 79-30-05. REPLACED RT ENGINE WIRE HARNESS AND O HMED AND MEGGED WIRES BETWEEN RT PRESSURE TRANSDUCER. 2 L 7 2 4T RT A52EU 2001101700088 20011017 00088 WP 2001 10 17 MWEA001396 1 20011016 A 5310 591014249 DOOR FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 FORWARD CARGO BAY LOWER JAMB AREA HAS LIGHT CORROSION AND PREVIOUS BLENDS BETWEEN STATION 395 TO 400. FABRICATED AND IN STALLED FORWARD CARGO DOOR JAMB PLATE AND SEAL DEPRESSOR. 2 L 7 2 4F A6WE 2001101700089 20011017 00089 WP 2001 10 17 MWEA011370 1 20011011 A 5320 591016331 STIFFENER DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 APB, AFT SIDE, RADIAL STIFFENER NR 16 LT SIDE HAS A CRACK AT STANDOFF ATTACHMENT. FABRICATED AND INSTALLED REPAIR DOUBL ERS. 2 L 7 2 4F A6WE 2001101700090 20011017 00090 WP 2001 10 17 MWEA011371 1 20011011 A 5522 591041275 COVER DOUG DC9 DC981 3022081 WP ELEVATOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 RT ELEVATOR LEADING EDGE, OUTBOARD END COVER HAS A CRACK ON EDGE. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001101700091 20011017 00091 WP 2001 10 17 MWEA011372 1 20011011 A 5320 9910140102 FLOOR SUPPORT DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 FORWARD BAG PIT RIGHT HAND TUNNEL AT STATION 484 SUBFLOOR CRACKED. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001101700092 20011017 00092 WP 2001 10 17 MWEA011373 1 20011010 A 5350 NAS427K10 PIN DOUG DC9 DC914 3022034 WP TAILCONE WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 TAIL CONE REQUIRED EXCESSIVE FORCE DURING OPERATIONAL CHECK. REROUTED CABLE AND REPLACED WORN GUIDE PINS. 2 L 7 2 4F A6WE 2001101700093 20011017 00093 NM 2001 10 17 MWEA011374 1 20011011 A 5347 5936663521 CARGO TRACK DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 AFT PIT LEFT HAND SUPPORT/CARGO HOLD DOWN TRACK HAS LIGHT CORROSION AND BARE METAL FROM STATION 1220-1155 LOCATED ABOVE AND BETWEEN LONGERON 28 LEFT AND 27 LEFT. FABRICATED AND INSTALLED NEW TRACK. 2 L 7 2 4F RT A6WE 2001101700094 20011017 00094 NM 2001 10 17 MWEA011375 1 20011011 A 5320 3913291501 SPLICE DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 AFT PIT LONGERON 25 LEFT SPLICE IS CRACKED BETWEEN FASTENERS. SPLICE IS LOCATED BETWEEN FRAME 1287 AND 1309. CRACK VER IFIED WITH HFEC. FABRICATED AND INSTALLED SPLICE. 2 L 7 2 4F RT A6WE 2001101700095 20011017 00095 NM 2001 10 17 MWEA011376 1 20011011 A 5320 5936660168 FLOOR SUPPORT DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 FORWARD CARGO COMPARTMENT FLOOR SUPPORT CHANNEL JUST INBOARD OF RT TIE DOWN RAIL HAS AREAS OF LIGHT CORROSION AND BARE M ETAL ON TOP AND BOTTOM SIDE LOCATED FROM STATIONS 332 TO 370. FABRICATED AND INSTALLED NEW FLOOR SUPPORT CHANNEL. 2 L 7 2 4F RT A6WE 2001101700096 20011017 00096 NM 2001 10 17 MWEA011377 1 20011011 A 5347 5936594529 CARGO TRACK DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 CENTER CARGO COMPARTMENT LEFT HAND TIE DOWN CHANNEL HAS AREAS OF LIGHT CORROSION ON TOP SIDE FROM STATIONS 693 TO 788. REMOVED AND INSTALLED REPAIR SPLICE AND TRACK. 2 L 7 2 4F RT A6WE 2001101700097 20011017 00097 WP 2001 10 17 MWEA011379 1 20011011 A 5522 993780415 SKIN DOUG DC9 DC981 3022081 WP ELEVATOR DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 LEFT HAND ELEVATOR TOP SKIN HAS A DENT AT APPROXIMATELY XE14 8 INCHES FORWARD OF SKIN TEE. DENT IS 1.5 X 1.3 INCH AND .0 70 DEEP. FABRICATED AND INSTALLED EXTERNAL DOUBLER. 2 L 7 2 4F A6WE 2001101700098 20011017 00098 WP 2001 10 17 MWEA011382 1 20011011 A 5315 991556171 FLOORBEAM DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 CAP ON FLOORBEAM AT STATION 1338 FROM LEFT LAV TO RIGHT LAV REQUIRES REPLACEMENT. FABRICATED AND INSTALLED NEW FLOORBEA M CAP AND INSTALLED LEFT HAND AND RIGHT HAND LAV FLOOR SUPPORTS. 2 L 7 2 4F A6WE 2001101700099 20011017 00099 WP 2001 10 17 MWEA011384 1 20011011 A 5242 59127561N PAN DOUG DC9 DC981 3022081 WP E/E DOOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 E&E BAY DOOR PAN HAS LIGHT CORROSION FROM STATION 157 TO STATION 160 BETWEEN LONGERON 29 LEFT HAND TO LONGERON 29 RIGHT HAND. REMOVED E AND E DOOR PAN AND INSTALLED NEW E&E DOOR PAN. 2 L 7 2 4F A6WE 2001101700100 20011017 00100 WP 2001 10 17 MWEA011388 1 20011013 A 7910 OIL CAP DOUG DC9 DC981 3022081 WP RT ENGINE UNSECURE A MWEA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 GL 31 807ME 48033 RIGHT ENGINE LEAKING OIL. CONTRACTED PHX MAINTENANCE INSPECTED AND FOUND NR 2 OIL TANK FILLER CAP UNSECURED. SERVICE W ITH 2197 OIL. INSPECTED CAP AND SECURED. LEAK CHECK GOOD. 2 L 7 2 4F A6WE 2001101700101 20011017 00101 WP 2001 10 17 MWEA011391 1 20011016 A 5230 59101413 SKIN DOUG DC9 DC981 3022081 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 AFT CARGO DOOR HAS A CRACK ON THE TRAILING EDGE SKIN APPROXIMATELY IN THE MIDDLE OF THE OUTSIDE SKIN. FABRICATED AND IN STALLED REPAIR PIECES. 2 L 7 2 4F A6WE 2001101700102 20011017 00102 WP 2001 10 17 MWEA011393 1 20011016 A 5310 59364421 DOOR FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 AFT CARGO COMPARTMENT DOOR JAMB BOTTOM WEB HAS AREAS OF LIGHT CORROSION FROM STATION 1148 TO 1212. FABRICATED AND INSTA LLED 4 DOUBLER REPAIR. 2 L 7 2 4F A6WE 2001101700103 20011017 00103 WP 2001 10 17 MWEA011394 1 20011016 A 5522 99378041 SKIN DOUG DC9 DC981 3022081 WP ELEVATOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 RIGHT HAND ELEVATOR TOP SKIN, LIGHT CORROSION AROUND ELEVATOR HOIST MOUNT SCREWS AT APPROXIMATELY XE73. FABRICATED NEW SKIN SECTION AND FINGER DOUBLER. INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001101700104 20011017 00104 WP 2001 10 17 MWEA011395 1 20011016 A 5330 59103435 DOUBLER DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 E&E BAY SKIN DOUBLER BETWEEN LONGERON 29 LEFT HAND TO LONGERON 30 HAS LIGHT CORROSION STATION 193. FABRICATED AND INSTA LLED ANTENNA DOUBLER. 2 L 7 2 4F A6WE 2001101700105 20011017 00105 NM 2001 10 17 MWEA011397 1 20011016 A 5347 5936594531 CARGO TRACK DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 CENTER CARGO COMPARTMENT RIGHT HAND TIE DOWN CHANNEL HAS AREAS OF LIGHT CORROSION ON TOP SIDE FROM STATION 636 TO 598. FABRICATED AND INSTALLED CARGO TRACK SPLICE ANGLE. 2 L 7 2 4F RT A6WE 2001101700106 20011017 00106 NM 2001 10 17 MWEA011398 1 20011016 A 5347 5936594523 CARGO TRACK DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 FORWARD CARGO COMPARTMENT LEFT HAND TIE DOWN CHANNEL HAS AREAS OF LIGHT CORROSION TOP AND BOTTOM SIDE AROUND FASTENER HO LES FROM STATION 370 TO 446. FABRICATED, DRILLED AND INSTALLED SECTION OF TRACK AND SPLICES. 2 L 7 2 4F RT A6WE 2001101700107 20011017 00107 NM 2001 10 17 BJNA010901 1 20010921 A 2797 CONNECTOR BOEING 737 737214 138446R NM T/E FLAP DIRTY A BJNA K NONE N FALSE WARNING CR CRUISE 1 WP 11 457TM 20156 WING FLAP POSITION INDICATOR SHOWED FLAPS NOT RETRACTED THE LAST 5 DEGREES IN FLIGHT. FUNCTIONAL TEST OF FLAP RETRACTIO N AND EXTENSION SYSTEM BY MAINTENANCE OK. REMOVED FLAP POSITION INDICATOR TRANSMITTER ELECTRICAL CONNECTOR, CLEANED, IN SPECTED AND RECONNECTED. REMOVED FLAP POSITION INDICATOR ELECTRICAL CONNECTOR, CLEANED, INSPECTED AND RECONNECTED. GRO UND OPS CHECK NORMAL. (M) 2 L 7 2 4F A16WE 2001101700108 20011017 00108 NM 2001 10 17 BJNA010902 1 20010921 A 2131 7110033 CONTROLLER BOEING 737 737282 13844AT NM CABIN PRESSURE MALFUNCTIONED A BJNA K NONE O OTHER CL CLIMB 1 WP 11 233TM 23043 CABIN RATE OF CLIMB/DESCENT TEMPORARILY INTERMITTENT OPERATION DURING CLIMB IN BOTH 'STANDBY' AND 'MANUAL' MODE. OUTFLO W VALVE WOULD NOT MOVE IN 'MANUAL' MODE. REPLACED OUTFLOW VALVE P/N 763810-2 AND CABIN PRESSURIZATION CONTROLLER P/N 71 10033 AS REQUIRED BY MM 21-31. GROUND OPERATIONAL CHECKS AS PER BMM 21-31-0 NORMAL. (M) 2 L 7 2 4F RT A16WE 2001101700109 20011017 00109 NM 2001 10 17 USA011135 1 20010821 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 612AU 30204 27124 CLT - FOUND FLOORBEAM CORRODED .5 INCH, BS 365 RBL 60. (M) 2 L 7 2 4F RT A2NM 2001101700110 20011017 00110 NM 2001 10 17 USAA010966 1 20010731 A 5240 SKIN BOEING 757 7572B7 1384964 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 632AU 22219 27810 CLT - FOUND SKIN INTERIOR WITH CRACK .5 INCH, L4 DOOR, AT LIGHTENING HOLE ABOVE LOWER HINGE. INSTALLED DOUBLER PER EA 8 5161. (M) 2 L 7 2 4F RT A2NM 2001101700111 20011017 00111 NM 2001 10 17 USAA011091 1 20010814 A 5330 DOUBLER BOEING 767 7672B7 1385107 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 652US 24765 CLT - FOUND SKIN DOUBLER AND TRIPLER, 22 INCH BY 16.5 INCH DOUBLER AND 12.75 INCH BY 4 INCH TRIPLER, BS 380 S28R S30R. INSTALLED DOUBLER AND TRIPLER PER EA 40719A. (M) 2 L 7 2 4F RT A1NM 2001101700112 20011017 00112 NM 2001 10 17 USAA011094 1 20010815 A 5311 FRAME BOEING 767 7672B7 1385107 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 652US 49920 24765 CLT - FOUND OUTER CHORD CRACKED .25 INCH, BS 1807, JUST BELOW STRINGER 12A. STOPPED DRILLED HOLE AND DOUBLER REPAIR PER EO 5307T120. (M) 2 L 7 2 4F RT A1NM 2001101700113 20011017 00113 NM 2001 10 17 USAA011095 1 20010815 A 5320 INTERCOSTAL BOEING 767 7672B7 1385107 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 652US 49920 24765 CLT - FOUND INTERCOSTAL CRACKED .5 INCH, BS 764 LBL 73.8 AND RBL 73.8. FABRICATED NEW BRACKET AND WEB PER EO 5399T503 A ND SRM 51-10-00. (M) 2 L 7 2 4F RT A1NM 2001101700114 20011017 00114 NM 2001 10 17 USAA011131 1 20010821 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 612AU 30204 27124 CLT - FOUND FLOORBEAM WITH .5 INCH DAMAGE, BS 377 LBL 2. SPLICED IN NEW T-CAP SECTION PER TR 53-15-01. (M) 2 L 7 2 4F RT A2NM 2001101700115 20011017 00115 NM 2001 10 17 USAA011132 1 20010821 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 612AU 30204 27124 FOUND FLOORBEAM CORRODED .5 INCH, BS 377 RBL 9. SPLICED IN NEW T-CAP SECTION PER TR 53-15-01. (M) 2 L 7 2 4F RT A2NM 2001101700116 20011017 00116 NM 2001 10 17 USAA011133 1 20010821 A 5320 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 612AU 30204 27124 CLT - FOUND FLOOR SUPPORT CORRODED 1.5 INCH, BS 324 AND 6 INCHES INBOARD OF RIGHT FUSELAGE SKIN. (M) 2 L 7 2 4F RT A2NM 2001101700117 20011017 00117 NM 2001 10 17 S01232030 1 20010720 A 3250 LANDING GEAR BOEING 747 747209B NM PWA JT9 JT9D7Q 52054 NE W SAJF O OTHER O OTHER TX TAXI/GRND HDL 1 WP 03 2050RU 22446 B18753 DURING INITIAL T/O ROLLING, GEAR NOT CENTER IT & LH BODY GEAR UNLOCK IT ILLUM.INITAL ACTION:CHK LH BLG FND LH STR N ACT ROD END SEPARATED FROM ACT BODY, THIS ACT WAS RPLD AND FUNC CHK NML.C/A:1.ONE-TIME INSP:EON 742-32-634053-0005 & E ON 744-32-631014-0003 INSP FOR INTEGRITY & COND OF BLG STRN ACT ROD END & SEALANT WAS ACCOMPLISHED, THE ACT WITH DAMAGE SEALANT & POSSIBLE INTERIOR CORROSION WERE RPLD. 2.AMP REVISION EO 744-32-53-0001 & EO 742-32-53-0001 WERE ISSUED TO SPE CIFY THAT IN EVERY 4A & B CHK FOR 744 & 742 FLEETS, RESPECTIVELY, TO PERFORM A VISUAL INSP ON BLG STRN ACT ROD END TO RO D END JOINT & LOCK RING SEALANT. REPLACEMENT AS REQUIRED FOR BENCH CHK. 3.BENCH CHK:ATIPS 32-50-01-002 SW ASSY RPLD, 2 L 7 4 4F 4 F RT A20WE E3NE 2001101800001 20011018 00001 SO 2001 10 18 C2XA01TY160 1 20011017 A 3350 GE1317 BULB EMB EMB 135 EMB135ER 3260203 SO CABIN BURNED OUT A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14508 NA 145220 TYS During a scheduled inspection the overhead emergency light on right side was found out. Maintenance removed and re placed the bulb, operational checks good I.A.W.-EMB-135-AMM-33-50-07, Aircraft released for service. 2 L 7 2 4F RT T00011AT 2001101800002 20011018 00002 WP 2001 10 18 01FDEA00893 1 20011010 A 5320 SPLICE DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 375FE 46613 CLG W/W COMPT LT SIDEWALL SPLICE DOUBLER IS CRACKED LOC AFT OF AIL/SPOILER DETRIM ACT. 2 L 7 3 4F A22WE 2001101800005 20011018 00005 NM 2001 10 18 2001UALA02058 1 20010917 A 2797 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE T/E FLAP LOOSE A UALA C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 WP 29 179UA 46784 25158 STATUS MESSAGE ON TAKEOFF, FLAPS CONF WITH FLAPS IN POSITION 10 DEGREES. ABORTED TAKEOFF AT 100 KTS. FOUND LEFT OUTBOAR D TRAILING EDGE FLAP DRIVE CANNON PLUG NOT SECURED. SECURED CONNECTOR MESSAGE CLEARED. FLAPS OPS NORMAL NOW. 2 L 7 4 4F 4 F RT A20WE E24NE 2001101800011 20011018 00011 NM 2001 10 18 2001UALA02096 1 20011007 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 520UA 24890 CABIN FLOORBEAM AT STA 297, RBL 34 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED UPPER SURFACE STRAP REPAIR STA 297, RBL 41 TO RBL 47.5. 2 L 7 2 4F 4 F RT A2NM E17NE 2001101800012 20011018 00012 EA 2001 10 18 COMA0160816 1 20011014 A 7931 5018T49P01 SEAL CNDAIR CL600 CL6002B19 EA RIGHT ENGINE CRACKED A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 708CA 7235 FLIGHT 5369. DURING CRUISE FLIGHT, THE RIGHT ENGINE OIL PRESSURE SLOWLY DROPPED TO 23 PSI, THE RIGHT ENGINE WAS SHUT-DOW N AND AN EMERGENCY WAS DECLARED. AIRCRAFT LANDED SAFELY AT DESTINATION CITY MSP.REPLACED THE RIGHT ENGINE OIL PUMP CARBO N SEAL. 2 L 7 2 4F RT A21EA 2001101800013 20011018 00013 NM 2001 10 18 2001UALA02097 1 20011007 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 520UA 24890 AFT CABIN FLOORBEAM WEB CORRODED STA 1685, RBL 51. MAJOR REPAIR ACCOMPLISHED. INSTALLED UPPER SURFACE DOUBLER STA 1685, RBL 47.5 TO RBL 54. 2 L 7 2 4F 4 F RT A2NM E17NE 2001110800032 20011108 00032 NM 2001 11 8 2001UALA02098 1 20011005 A 5610 WINDOW BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE COCKPIT OPEN A UALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 29 609UA 21870 ABORTED TAKEOFF. CAPTAINS SLIDING WINDOW OPENED. WINDOW RIG OPS CHECKED OK. WINDOW SEAL, LOCK ASSEMBLY AND HANDLE INS PECTED AND FOUND SERVICEABLE. HULL WAS PRESSURIZED WITH NO LEAKS NOTED. SUSPECT WINDOW WAS NOT FULLY CLOSED AND LOCKED . 2 L 7 2 4F 4 F RT A1NM E3NE 2001110800033 20011108 00033 NM 2001 11 8 2001UALA02099 1 20011004 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 196UA 28715 EMERGENCY CEILING LIGHT AT SEAT 16 INOP. RELAMPED, CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2001101800014 20011018 00014 NM 2001 10 18 2001UALA02100 1 20011003 A 5315 FLOORBEAM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 181UA 25278 BS 520 FLOORBEAM UPPER CHORD EXCESSIVELY CORRODED. BLENDED BEYOND LIMITS. 2 L 7 4 4F 4 F RT A20WE E24NE 2001101800015 20011018 00015 NM 2001 10 18 2001UALA02101 1 20011008 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 STATION 178 BULKHEAD AT RBL 5.7, WL 212 IS CRACKED. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001101800016 20011018 00016 EA 2001 10 18 COMA0160817 1 20011015 A 2781 855D1009 BPSU CNDAIR CL600 CL6002B19 EA LEFT WING FAULTY A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 926CA 11446 7027 FLIGHT 5507. DURING DESCENT INTO CHO, RECEIVED A FLAP FAIL CAUTION MESSAGE AT 45 DEGREE FLAP POSITION.REPLACED THE LEFT BRAKE AND POSITION SENSING UNIT. 2 L 7 2 4F RT A21EA 2001101800017 20011018 00017 NM 2001 10 18 2001UALA02102 1 20011008 A 5310 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 327UA 24147 STRINGER 12R AT STA 344 SHEAR TIE CRACKED AFT OF DOOR R1 CENTER LINE. MAJOR REPAIR ACCOMPLISHED. REPLACED THE SHEAR TI E AT STRINGER 12R STA 344. 2 L 7 2 4F 4 F RT A16WE E2GL 2001101800018 20011018 00018 NM 2001 10 18 2001UALA02103 1 20011008 A 5230 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 327UA 24147 FORWARD PIT DOOR HAS EXTERIOR SKIN DAMAGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001101800019 20011018 00019 EA 2001 10 18 COMA0160818 1 20011015 A 5346 601350061 WEB CNDAIR CL600 CL6002B19 EA BEAM CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 934CA 16859 7042 FOUND CRACKS IN ENGINE SUPPORT BEAM AT FS 625.30, LBL37 AND RBL37, CENTER OF BEAM BL0,WL111.09.REPAIRED ENGINE SUPPORT B EAM IAW CANADAIR REOS 601R-53-61-366 REV C AND TEMPORARY REPAIR REO 601R-53-61-345 REV B IN CONJUNCTION WITH 601R-53-61- 445. 2 L 7 2 4F RT A21EA 2001101800020 20011018 00020 2001 10 18 2001UALA02104 4 20011008 A 2565 62771118 SLIDE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE R1 DOOR CUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 769UA 898 26921 DOOR 1 RT SLIDE/RAFT P/N 62771-118, S/N 0284 FOUND TO HAVE 5 CUTS IN INFLATABLE. CUTS FOUND DURING SHOP OVERHAUL OF THE UNIT. THERE WERE 3 CUTS IN TOP TUBE AND 2 IN BOTTOM TUBE ON RT SIDE OF SLIDE/RAFT ABOVE BOTTOM TUBE RELIEF VALVE. CUTS IN THE INFLATABLE APPEAR TO BE CAUSED BY A SNAP ON THE REBOARD LINE BEING PUSHED INTO THE BACK OF THE BOTTOM TUBE RELIE F VALVE CUTTING THE INFLATABLE MATERIAL. THIS HAPPENED WHEN THE UNIT WAS REPACKED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001101800021 20011018 00021 EA 2001 10 18 COMA0160819 1 20011016 A 3030 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 EA A COMA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SO 01 959CA 7116 FLIGHT 5662. DURING CLIMB-OUT OF CVG, RECEIVED MULTIPLE ANTI-ICE CAUTION MESSAGES, AIRCRAFT RETURNED TO THE FIELD.RESET THE HEAT CAUTION CONTROLLER CIRCUIT BREAKER. 2 L 7 2 4F RT A21EA 2001101800022 20011018 00022 NM 2001 10 18 2001UALA02105 1 20011009 A 5711 SPAR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RT WING DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 RIGHT HAND WING REAR SPAR WEB DAMAGED FROM WS 585 TO 605. MAJOR REPAIR ACCOMPLISHED. SPLICED AND REPAIRED WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2001101800023 20011018 00023 NM 2001 10 18 2001UALA02106 1 20011009 A 5711 SPAR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RT WING DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 RIGHT HAND WING REAR SPAR LOWER CHORD DAMAGED AT WS 590 TO WS 605. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE, MANUFACT URED CHORD ANGLE AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001110800034 20011108 00034 NM 2001 11 8 2001UALA02108 1 20011010 A 5310 STRUCTURE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7449U 21903 FUSELAGE DAMAGE FOUND DURING MAINTENANCE CHECK. MAJOR REPAIR ACCOMPLISHED. REPAIRED DAMAGE. OPERATIONS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001101800024 20011018 00024 NM 2001 10 18 CALA0100960 1 20011017 A 5347 6543813 SEAT TRACK BOEING 737 7373T0 1384582 NM STA 328-380 CRACKED A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 69333 23571 SEAT TRACK RBL 44 BS 328 - 380 CORRODED. CRACK (1/2") AT BS 380. REPAIRED PER SRM 53-00-02 AND 51-30-02. 2 L 7 2 4F RT A16WE 2001102600026 20011026 00026 NM 2001 10 26 2001UALA02109 1 20011010 A 2120 ODOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LAVATORY DETECTED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 367UA 24536 UNSCHEDULED LANDING DUE TO ELECTRICAL ODOR IN THE LAVATORY. NO ROOT CAUSE OF ODOR WAS FOUND. INSPECTED PRECOOLER INLET , ACM'S FOR OVER-SERVICING, PNEUMATIC DUCTS AND COALESCER BAGS FOR OIL CONTAMINATION, THEN OPERATED PACKS FOR 20 MINUTES WITH NO DEFECT NOTED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001102600027 20011026 00027 NM 2001 10 26 2001UALA02112 1 20011010 A 2121 4100941C COOLING FAN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE E/E BAY FAILED A UALA D RETURN TO BLOCK J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 777UA 26916 NR 2 EQUIP COOLING FAN EICAS MESSAGE WITH SMELL ON FLT DECK. RTN TO GATE. FOUND RT EQUIPMENT COOLING FAN INOP. REPLAC ED FAN. AIRCRAFT RETURNED TO REVENUE SERVICE WITHOUT FURTHER INCIDENT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001102600028 20011026 00028 NM 2001 10 26 2001UALA02113 1 20011011 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 918UA 25385 STATION 294.5 STUB FRAME AT FORWARD GALLEY DOOR CUTOUT CRACKED. MAJOR REPAIR ACCOMPLISHED. DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001102600029 20011026 00029 NM 2001 10 26 2001UALA02114 1 20011011 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 336UA 24240 CORROSION ON UPPER FORWARD FLANGE OF BODY STATION 986 FLOORBEAM AT RBL 41. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSIO N. INSTALLED REINFORCEMENT REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001110800035 20011108 00035 NM 2001 11 8 2001UALA02115 1 20011010 A 3350 LIGHT BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 105UA 26473 EMERGENCY LIGHT INOP AFT UPPER DECK CEILING BETWEEN SLIDE DOORS. REPLACED LAMP, CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2001110800036 20011108 00036 NM 2001 11 8 2001UALA02116 1 20011009 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN SHORTED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 194UA 26892 FOUND EEL FIRST CLASS AREA (1A-5A) AND (4E-5E) INOP. ALL EELS CHECKS GOOD. FOUND SHORT AT SEAT 1A EEL LIGHT ASSY WIRIN G. REPAIRED AND REPLACED LIGHT ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 2001102600031 20011026 00031 NM 2001 10 26 2001UALA02118 1 20011011 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 520UA 24890 AFT PIT STA 1400 JUST ABOVE STRINGER 25L, UPPER CHORD IS DENTED AND CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPA IR SPLICE ON FRAME. 2 L 7 2 4F 4 F RT A2NM E17NE 2001101800026 20011018 00026 EU 2001 10 18 CHQ00026 1 20010929 A 3260 WARNING LIGHT SAAB SF340 SF340A 7850100 EU COCKPIT ILLUMINATED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 123CQ 123 GEAR INTRANSIT LIGHT ON. 2 L 7 2 4T RT A52EU 2001101800027 20011018 00027 NE 2001 10 18 CHQ00027 2 20011004 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A1 30030 NE RIGHT MALFUNCTIONED A CHQA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 11 96CQ 96 367142 RIGHT HAND ENGINE PEGGED OUT AND RIGHT HAND ENGINE POL PRESSURE LIGHT CAME ON. 2 L 7 2 4T 4 T RT A52EU E8NE 2001101800028 20011018 00028 CE 2001 10 18 GLBA2001217 1 20011017 A 5400 1299100435 PANEL BEECH 1900 1900D 1154162 CE SEPARATED A GLBA K NONE O OTHER IN INSP/MAINT 1 CE 01 150GL UE150 POST FLIGHT INSPECTION FOUND LEFT O/B COWL PANEL MISSING, REPLACED PANEL 2 L 7 2 4T RT A24CE 2001101800029 20011018 00029 SO 2001 10 18 CHQ00028 1 20011008 A 5610 WINDOW EMB 145 EMB145 SO COCKPIT NOISY A CHQA O OTHER O OTHER UK UNKNOWN 1 GL 11 260SK 145128 FIRST OFFICER SIDE SQUEALS BADLY. 2 L 7 2 4F RT T00011AT 2001101800030 20011018 00030 2001 10 18 CHQ00029 4 20011012 A 3425 COMPUTER SAAB SF340 SF340A 7850100 EU COCKPIT FAULTY A CHQA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 11 CHQA N157CQ NR 1 CAPTAINS AHRS STARTED PITCHING AND ROLLING. 2 L 7 2 4T RT A52EU 2001101800031 20011018 00031 EA 2001 10 18 COMA0160822 1 20011017 A 5320 600360303132 DOUBLER CNDAIR CL600 CL6002B19 EA FS718.00 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 933CA * 7040 FS 718.00 L/H AND R/H AFT DOUBLERS CRACKED, FRAME SECTIONS L/H UPPER AND R/H UPPER AND LOWER ARE CRACKED.F.S.718.00 L/H AND R/H AFT DOUBLERS REMOVED AND REPLACED IAW CANADAIR REO 601R-53-61-193 REV A. FRAME SECTIONS L/H UPPER AND R/H UPPER AND LOWER REMOVED AND REPLACED IAW CANADAIR REO 601R-53-61-193 REV A. 2 L 7 2 4F RT A21EA 2001101800032 20011018 00032 NM 2001 10 18 USAA011211 1 20010905 A 5300 SKIN BOEING 757 757225 1384959 NM BS 475 A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 601AU 54736 22193 CLT - FOUND SKIN PLUG FLUCH PATCH 1 INCH, STATION 475 AT 30-29R E/E MAIN BAY DOOR. PREVIOUSLY INSTALLED REPAIR (FLUCH P ATCH) PER SRM 52-40-01 FIG 201. (M) 2 L 7 2 4F RT A2NM 2001101800033 20011018 00033 NM 2001 10 18 USAA011176 1 20010814 A 5300 STRINGER BOEING 737 7373B7 1384580 NM FS 967 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 395US 23317 TPA - FOUND STRINGER CORRODED 6 SQUARE INCH AREA, STRINGER 25L STATION 967 PLUS 10 INCHES. CORROSION LEVEL 2. SPLICED IN SECTION OF STRINGER PER SRM 53-00-03 PAGE 201-204. (M) 2 L 7 2 4F RT A16WE 2001101800034 20011018 00034 NM 2001 10 18 USAA011177 1 20010830 A 5300 SKIN BOEING 737 737301 1384611 NM BS 947.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 42760 23237 TPA - FOUND SKIN CRACKED 1.3 INCHES, STATION 947.5 LOWER FORWARD CORNER OF HINGE CUT OUT. INSTALLED DOUBLERS PER SRM 53 -60-01 FIG 208. (M) 2 L 7 2 4F RT A16WE 2001101800035 20011018 00035 NM 2001 10 18 USAA011178 1 20010816 A 5300 SKIN BOEING 737 737301 1384611 NM BS 947.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 42760 23237 TPA - FOUND SKIN CRACKED 1 INCH, STATION 947.5 UPPER FORWARD CORNER HINGE CUT OUT. INSTALLED DOUBLERS PER SRM 53-60-01 FIG 205. (M) 2 L 7 2 4F RT A16WE 2001101800036 20011018 00036 EU 2001 10 18 CHQ00030 1 20011012 A 7540 WARNING SYSTEM SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE COCKPIT ACTIVATED A CHQA O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 123 N123CQ 367421 ON FINAL APPROACH INTO STL, THE PILOT HAD A RT BLEED LEAK. PILOT DECLARED AN EMERGENCY. 2 L 7 2 4T 4 T RT A52EU E8NE 2001101800040 20011018 00040 NM 2001 10 18 AWXA200100525 1 20011008 A 2751 1817389 TRANSMITTER BOEING 737 73733A 1384673 NM T/E FLAP ARCED A AWXA L ABORTED APPROACH F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 WP 28 509DC 45264 23636 ON APPROACH T/E FLAPS LOCKED OUT AT 5 UNITS, APPROACH WAS ABORTED. CREW FOLLOWED QRH CHECKLIST. ON RETURN FLAP POS IND ICATOR NEEDLES MARRIED UP, CREW SELECTED FLAPS 10 & DOWN TO 30, PERFORMED NORMAL LANDING. MX PERFORMED T/E FLAP ASYMMET RY CHECK & T/E FLAP POSITION INDICATING SYSTEM ADJ TEST. NO DEFECTS NOTED. TECHNICAL SUPPORT REQUESTED ADDITIONAL TROU BLESHOOTING DUE TO INTERMITTENT HISTORY OF FLAP LOCKOUTS. MX INSPECTED ALL T/E FLAP TRANSMISSIONS AND JACKSCREWS, NO DI SCREPANCIES WERE NOTED. MX FOUND SIGNS OF ARCING ON LT T/E FLAP POSITION XMITTER CONNECTOR & PLUG. MX REPLACED XMITTER & PLUG, PERFORMED ADJ AND TEST. NO FURTHER DISCREPANCIES. PLUG P/N: BACC63BP16A24S7L, LOC: LT WING T/E, COND: ARCED. 2 L 7 2 4F RT A16WE 2001101800041 20011018 00041 NM 2001 10 18 AWXA200100526 1 20011016 A 7170 3352534030 DRAIN LINE BOEING 737 737317 138447P NM CFMINT CFM56 CFM563B2 13802 EU NR 1 ENGINE BLOCKED A AWXA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 28 331AW 23747 720701 AFTER TAKEOFF AT 500 FT TAKEOFF POWER WAS AT 93.4 PERCENT N1, THE NR 1 ENG RAPIDLY LOST PWR TO APPROX 60 PERCENT N1, FUE L FLOW REDUCED. AUTO THROTTLE REMAINED ON & POWER LEVERS REMAINED FORWARD IN TAKEOFF POSITION. AFTER LEVELING OFF & RE DUCING PWR ON BOTH ENGINES, POWER ON NR 1 ENG WAS NORMAL. RETURNED MAKING AN UNEVENTFUL LANDING. NR 1 ENG OPERATED NOR MAL ON LANDING. MX FOUND NR 1 ENG CDP TUBE DRAIN HOLE BLOCKED. CLEARED BLOCKAGE IN CDP TUBE DRAIN HOLE, RAN BOTH ENG'S & CHECKED ENG TRIM, TRIM TABLES & FOUND PARAMETERS WITHIN LIMITS. PERFORMED AUTO THROTTLE BITE CHECK, NO FAULTS NOTED & PERFORMED AUTO THROTTLE RANGE & RIG CHECK, CHECKED NORMAL. PERFORMED TAKEOFF POWER RUNS, ENG'S CHECKED NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2001101800042 20011018 00042 NM 2001 10 18 AWXA200100527 1 20011001 A 5315 6545810519 FLOORBEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - C18 CK - C - CORROSION FOUND ON FLOORBEAM UPPER FLANGE AT BS 312, RBL 6 TO RBL 13, WL 208, BEYOND SRM LIMITS AFTER CORROSION CLEAN UP. MAINTENANCE REMOVED DAMAGED FLOORBEAM UPPER FLANGE FROM LBL 18 TO RBL 22, FABRICATED REPAIR FLOORB EAM UPPER FLANGE AND INSTALLED IAW B737 SRM 53-10-51, FIG 205, PG 200 - 203. 2 L 7 2 4F RT A16WE 2001101800043 20011018 00043 SO 2001 10 18 C2XA01CL213 1 20011009 A 3350 7287580503 LIGHT EMB 135 EMB135ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 27506 145206 CLE FLIGHT NR 3683 THE CREW REPORTED THAT THE 2ND AND 3RD EMERGENCY LIGHT STRIPS WERE INOPERATIVE. MAINTENANCE INSPECTE D AND REPLACED THE 3RD LIGHT STRIP AND REPAIRED THE WIRING ON THE 2ND LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. THE A IRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001101800044 20011018 00044 SO 2001 10 18 C2XA01CL214 1 20011010 A 2120 ODOR EMB 135 EMB135ER 3260203 SO CABIN DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 14505 145192 CLE FLIGHT 3350 THE CREW REPORTED A BURNING SMELL FROM THE APU WHENEVER THE BLEED AIR WAS USED. MAINTENANCE INSPECTED A ND FOUND NO DEFECTS OR SMELLS. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001101800045 20011018 00045 NM 2001 10 18 2001F00439 1 20010915 A 3350 BATTERY PACK DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A MASA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 07 448YV 448 FLT 6329 - DURING TAXI-OUT, THE CREW FOUND 3 EMERGENCY LIGHTS INOPERATIVE. THE AIRCRAFT RETURNED TO THE GATE WHERE MAIN TENANCE REPLACED THE BATTERY PACKS. OPS CHECKED GOOD AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 2001101800046 20011018 00046 EA 2001 10 18 2001F00440 1 20010916 A 3350 1317 LIGHT CNDAIR CL600 CL600* EA CABIN INOPERATIVE A MASA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 07 97325 7325 FLT 6585 - CMH-BDL - DURING TAXI-OUT, THE CREW FOUND THE CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. THE AIRCRAFT RETURN ED TO THE GATE WHERE MAINTENANCE REPLACED THE FLOOD LIGHT. OPS CHECKED GOOD AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001101800047 20011018 00047 NM 2001 10 18 2001F00441 1 20010917 A 3350 6038443 BATTERY PACK DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A MASA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 07 446YV 446 FLT 6350 - DURING TAXI-OUT, THE CREW FOUND THE MAIN DOOR EMERGENCY EXIT SIGN, ROW 1D EMERGENCY EXIT SIGN AND OVERHEAD EM ERGENCY LIGHT INOPERATIVE. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE TROUBLESHOT AND REPLACED THE EMERGENCY L IGHT BATTERY PACKS. OPS CHECKED GOOD AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 2001101800048 20011018 00048 NM 2001 10 18 2001F00442 1 20010917 A 3350 6038443 BATTERY PACK DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 07 449YV 449 FLT 6330 - PHX-BFL - DURING TAXI-OUT, THE CREW HAD A MAIN DOOR EMERGENCY EXIT SIGN, ROW 1D EMERGENCY EXIT SIGN AND OVERH EAD EMERGENCY LIGHT INOPERATIVE. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE TROUBLESHOT AND REPLACED THE EMERG ENCY LIGHT BATTERY PACK. OPS CHECKED GOOD AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 2001101800049 20011018 00049 EA 2001 10 18 2001F00443 1 20010917 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A MASA K NONE O OTHER UK UNKNOWN 1 SW 07 77331 7331 FLT 5805 - PHL-MKE - THE CREW HAD AND OVERHEAD FLOOD LIGHT INOPERATIVE. MAINTENANCE TROUBLESHOT AND REPLACED THE LIGHT BULB. OPS CHECKED GOOD AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001101800050 20011018 00050 EA 2001 10 18 2001F00444 1 20010630 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A MASA K NONE L NO TEST UK UNKNOWN 1 SW 07 47239 7239 FLT 6718 - THE CREW NOTED THAT THE NR 4 CEILING EMERGENCY LIGHT WAS INOPERATIVE. SINCE THE LIGHT WAS NOT ADJACENT TO AN OTHER ROW OF EMERGENCY LIGHTS THE ITEM WAS DEFERRED PER MEL NR 35-51-01-1. THE EMERGENCY LIGHT WAS LATER REPLACED BY MX . (M) 2 L 7 2 4F RT A21EA 2001101800051 20011018 00051 SO 2001 10 18 2001F00445 1 20010709 A 2530 CONNECTOR EMB 145 EMB145 SO GALLEY DIRTY A MASA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 838MJ FLT 5882 - PHX-XNA - SHORTLY AFTER ARRIVING IN XNA, THE FLIGHT ATTENDANT REPORTED SMOKE COMING FROM THE COFFEE POTS. TH E CREW SECURED THE CB'S AND MAINTENANCE PERFORMED AND INSPECTION OF THE COFFEE POTS AND DEFERRED THE ITEM. LATER MAINTE NANCE CLEANED THE CONNECTOR PLUG AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT T00011AT 2001101800052 20011018 00052 EA 2001 10 18 2001F00446 1 20010709 A 3350 BC10020004 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17231 7231 FLT 6150 - ON PREFLIGHT, THE CAPTAIN REPORTED THE 3RD LIGHT FROM THE FRONT ROW CEILING FLOOD LIGHT WAS INOPERATIVE. THE ITEM WAS DEFERRED. LATER MAINTENANCE REPLACED THE EMERGENCY LIGHT. (M) 2 L 7 2 4F RT A21EA 2001101800053 20011018 00053 EA 2001 10 18 2001F00447 1 20010805 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77302 7302 DURING OVERNIGHT MAINTENANCE, IT WAS DISCOVERED THAT AN OVERHEAD EMERGENCY LIGHT WAS BURNED OUT. THIS ITEM WAS DEFERRED PER MEL NR 35-51-01-1. THIS LIGHT WAS LATER REPLACED BY MAINTENANCE. (M) 2 L 7 2 4F RT A21EA 2001101800054 20011018 00054 NM 2001 10 18 2001F00438 1 20010914 A 3350 6038443 BATTERY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A MASA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 07 437YV 437 FLT 6389 - PHX-YUM - DURING TAXI-OUT, THE CREW HAD AN OVERHEAD EMERGENCY LIGHT INOPERATIVE AND THE MAIN DOOR EMERGENCY E XIT SIGN INOPERATIVE. MAINTENANCE TROUBLESHOT TO THE EMERGENCY LIGHT BATTERIES. THE PARTS HAD TO BE SENT FROM GJT AND THE AIRCRAFT IS AOG FOR BATTERIES. (M) 2 H 7 2 4T RT A13NM 2001101800055 20011018 00055 EA 2001 10 18 MASA01087 1 20010811 A 2611 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT FALSE ACTIVATION A MASA K NONE N FALSE WARNING AP APPROACH 1 SW 07 77260 7260 FLT 6506 - DECLARED AN EMERGENCY DURING APPROACH TO CMH DUE TO THE CARGO SMOKE WARNING LIGHT ILLUMINATED. THE AIRCRAFT LANDED WITHOUT INCIDENT. NO FIRE EVIDENCE WAS FOUND. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001101800056 20011018 00056 EA 2001 10 18 MASA01088 1 20010811 A 3350 1317 LIGHT CNDAIR CL600 CL600* EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37218 7218 DURING OVERNIGHT MAINTENANCE IT WAS DISCOVERED THAT AN EMERGENCY LIGHT NR 8 AT FS 491.50R WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB. OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001101800057 20011018 00057 NM 2001 10 18 USAA010989 1 20010806 A 5320 WEB BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 54141 22198 CLT - FOUND WEB CRACKED 2 INCHES, BS 740-760 RBL 11. FABRICATED AND INSTALLED WEB PER EA 85162 SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 2001101800058 20011018 00058 NM 2001 10 18 USAA011130 1 20010821 A 5330 SKIN BOEING 757 7572B7 1384964 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 30461 27122 CLT - FOUND FUSELAGE SKIN WITH PREVIOUSLY INSTALLED DOUBLER 7 INCHES BY 7 INCHES, BS 1737 BETWEEN STRINGER 27L AND 29L. REMOVED DAMAGE, INSTALLED DOUBLER PER EA 66258A. (M) 2 L 7 2 4F RT A2NM 2001101800059 20011018 00059 NM 2001 10 18 USAA011134 1 20010821 A 5320 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 612AU 30204 27124 CLT - FOUND FLOOR SUPPORT CORRODED 20 INCHES BY 5 INCHES, BS 345 AND 365.25. (M) 2 L 7 2 4F RT A2NM 2001101800060 20011018 00060 NM 2001 10 18 USAA011143 1 20010822 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 631AU 22441 27809 CLT - FOUND CHORD CORRODED 2.5 INCH BY 53 INCHES, BS 1640 BL 0 TO RBL 53. INSTALLED NEW T-CAP AT BS 1640 BL 0 TO RBL 53. (M) 2 L 7 2 4F RT A2NM 2001101800061 20011018 00061 NM 2001 10 18 USAA011147 1 20010823 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 612AU 30304 27124 CLT - FOUND FLOORBEAM CORRODED, BS 310.5 BL 0. REPAIRED FLOORBEAM PER SRM T-CAP REPAIR PER SRM 51-70-12. (M) 2 L 7 2 4F RT A2NM 2001101800062 20011018 00062 NM 2001 10 18 USAA011153 1 20010827 A 5320 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 633AU 27811 CLT - FOUND INTERCOSTAL CRACKED IN THREE PLACES 1 INCH EACH, BS 1660/1680 AT RBL 11. INSTALLED NEW INTERCOSTAL ANGLE PE R DWG NR 14GN5191-39 SRM 51-40-05. (M) 2 L 7 2 4F RT A2NM 2001101800063 20011018 00063 NM 2001 10 18 USAA011158 1 20010828 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 633AU 30461 27811 CLT - FOUND FLOORBEAM CORRODED, BS 1640 RBL 22, 30, 36, 42, 49. REMOVED AND REPLACED T-CAP. (M) 2 L 7 2 4F RT A2NM 2001101800064 20011018 00064 NM 2001 10 18 USAA011167 1 20010829 A 5320 ANGLE BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 633AU 27811 CLT - FOUND ANGLE CORRODED 2 INCHES BY 8 INCHES, ANGLE AFT OF L1 DOOR BS 395 AT LBL 64. BLENDED CORROSION PER 757 SRM 5 3-00-51 FIG 101. (M) 2 L 7 2 4F RT A2NM 2001101800065 20011018 00065 NM 2001 10 18 USAA011168 1 20010829 A 5320 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 633AU 22292 27811 CLT - FOUND INTERCOSTAL CORRODED 2 INCHES BY 4 INCHES, L1 DOOR THRESHOLD INTERCOSTAL AT BS 345, LBL 64. REMOVED AND REPL ACED INTERCOSTAL PER SRM 51-40-02. (M) 2 L 7 2 4F RT A2NM 2001101800066 20011018 00066 NM 2001 10 18 USAA011180 1 20010817 A 5314 KEELBEAM BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 42760 23237 TPA - FOUND KEELBEAM CRACKED 2 INCHES, LEFT KEEL BEAM VERTICAL LEG INBOARD SURFACE STATION 530. CORROSION LEVEL 2. CLE ANED CORROSION, VERIFIED REMOVAL AND RESTORED FINISH PER EA 85288, SRM 53-60-12. (M) 2 L 7 2 4F RT A16WE 2001101800067 20011018 00067 NM 2001 10 18 USAA011185 1 20010830 A 5311 BELTFRAME BOEING 737 737* NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 588US * 23933 PIT - FOUND BELTFRAME CRACKED .25 INCH, STATION 727D BELOW S8R. ROUTED OUT CRACKS, INSTALLED REPAIR ANGLE PER TYPICAL R EPAIR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001101800068 20011018 00068 NM 2001 10 18 USAA011186 1 20010818 A 5311 BELTFRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 588US 41171 23933 PIT - FOUND BELTFRAME CRACKED .25 INCH, BELTFRAME AT STATION 747 BELOW STRINGER 8R. ROUTED OUT CRACK, INSTALLED REPAIR ANGLE PER TYPICAL REPAIR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001101800069 20011018 00069 NM 2001 10 18 USAA011187 1 20010831 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 633AU 22292 27811 CLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 2 INCHES, FS 377.7 AT LBL 49 AND LBL 21. REMOVED DAMAGED SECTION OF T-CAP AND INSTALLED NEW PER T/R 53-15-01 EA 69911. (M) 2 L 7 2 4F RT A2NM 2001101800070 20011018 00070 NM 2001 10 18 USAA011191 1 20010904 A 5311 FRAME BOEING 757 7572B7 1384964 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 30461 27122 CLT - FOUND FRAME DENTED 1 INCH BY 1 INCH, FORWARD CARGO, LEFT FRAME 10 INCHES ABOVE TRANSITION ANGLE. TRIM OUT DAMAGE, NDT AREA, INSTALL FILLER AND DOUBLER PER EA 85262. (M) 2 L 7 2 4F RT A2NM 2001101800071 20011018 00071 NM 2001 10 18 USAA011192 1 20010904 A 5320 STRUCTURE BOEING 757 7572B7 1384964 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 30461 27122 CLT - FOUND FLANGE CRACKED .5 INCH, BETWEEN BS 1620 AND BS 1640 BL 0. INSTALLED DOUBLER AND FILLER PER DRAWING 146N5180 . (M) 2 L 7 2 4F RT A2NM 2001101800072 20011018 00072 NM 2001 10 18 USAA011193 1 20010904 A 5347 SEAT TRACK BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 633AU 27811 CLT - FOUND SEAT TRACK CORRODED 3 INCHES BY 3 INCHES, BS 377.7 AT LBL 26. REMOVED AND REPLACED PART NR 141N5131-1 PER DW G NR 141N51311. (M) 2 L 7 2 4F RT A2NM 2001101800073 20011018 00073 NM 2001 10 18 USAA011194 1 20010904 A 5347 SEAT TRACK BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 633AU 22292 27811 CLT - FOUND SEAT TRACK CORRODED 3 INCHES BY 3 INCHES, BS 377.7 AT LBL 26. REMOVED AND REPLACED PART WITH PART NR 141N51 31-1 PER DWG NR 141N5131-1. (M) 2 L 7 2 4F RT A2NM 2001101800074 20011018 00074 NM 2001 10 18 USAA011195 1 20010904 A 5320 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 633AU 22292 27811 CLT - FOUND INTERCOSTAL CORRODED 3 INCHES BY 5 INCHES, BS 395 AT RBL 12. REMOVED AND REPLACED PART NR 1840009 PER DWG NR 1840009. (M) 2 L 7 2 4F RT A2NM 2001101800075 20011018 00075 NM 2001 10 18 USAA011208 1 20010905 A 5311 FRAME BOEING 757 7572B7 1384964 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 30461 27122 CLT - FOUND FUSELAGE FRAME DENTED APPROXIMATELY .25 INCH BY .125 INCH, BS 580, 10 INCHES ABOVE TRANSITION ANGLE LEFT SID E. CUT OUT DAMAGE, FABRICATE FILLER AND DOUBLER PER EA 85312. (M) 2 L 7 2 4F RT A2NM 2001101800076 20011018 00076 NM 2001 10 18 USAA011213 1 20010905 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 601AU 54736 22193 CLT - FOUND SKIN WITH EXTERNAL PATCH 11 INCHES BY 8 INCHES, STATION 538-549 29L. PREVIOUSLY INSTALLED EXTERNAL PATCH RE PAIR. (M) 2 L 7 2 4F RT A2NM 2001101800077 20011018 00077 NM 2001 10 18 USAA011214 1 20010905 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 601AU 54736 22193 CLT - FOUND SKIN WITH PLUG FLUSH REPAIR .5 INCH, STATION 503 27L TO 28L. PREVIOUSLY INSTALLED REPAIR PER SRM 53-00-01 F IG 208. (M) 2 L 7 2 4F RT A2NM 2001101800078 20011018 00078 NM 2001 10 18 USAA011216 1 20010906 A 5330 SKIN BOEING 767 767201 1385125 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647US 58982 23899 CLT - FOUND SKIN DENTED, STATION 1291 RBL 26. (M) 2 L 7 2 4F RT A1NM 2001101800079 20011018 00079 NM 2001 10 18 USAA011217 1 20010906 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 601AU 54736 22193 CLT - FOUND SKIN PLUG REPAIR, LEFT SIDE OF FUSELAGE, BS 255, 18 INCHES BL COCKPIT WINDOW. PREVIOUSLY INSTALLED FREEZE P LUG REPAIR PER SRM 51-20-07. (M) 2 L 7 2 4F RT A2NM 2001101800080 20011018 00080 NM 2001 10 18 USAA011218 1 20010906 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 601AU 54736 22193 CLT - FOUND SKIN WITH PLUG PATCH 1 INCH, STATION 524, 24L-25L FUSELAGE SKIN. PREVIOUSLY INSTALLED FLUSH PATCH REPAIR PE R SRM 53-00-01. (M) 2 L 7 2 4F RT A2NM 2001101800081 20011018 00081 NM 2001 10 18 USAA011219 1 20010906 A 5330 SKIN BOEING 767 767201 1385125 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647US 23899 CLT - FOUND SKIN DENTED 3 INCHES, STATION 1291 RBL 26. PREVIOUSLY INSTALLED FLUSH PLUG REPAIR PER SRM 53-00-01 DETAIL 3 PAGE 231-232. (M) 2 L 7 2 4F RT A1NM 2001101800082 20011018 00082 NM 2001 10 18 USAA011222 1 20010910 A 5330 SKIN BOEING 767 767201 1385125 NM FUSELAGE DEFORMED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647US 23899 CLT - FOUND SKIN WITH DEFORMED AREA 4 INCHES BY 4 INCHES, BETWEEN BS 1197 AND BS 1219, BETWEEN STRINGER 38R AND 39R. CU T OUT DAMAGE AND INSTALLED REPAIR DOUBLERS PER EA 85351 AND SRM 53-00-01 FIG 201. (M) 2 L 7 2 4F RT A1NM 2001101800083 20011018 00083 GL 2001 10 18 RAIA00110005 2 20011014 A 7200 AE3007A ENGINE EMB 145 EMB145ER SO ALLSN AE300 AE3007A GL RT ENGINE FAILED A RAIA E ENGINE SHUTDOWN X ENGINE FLAMEOUT LD LANDING 1 CE 03 804HK 3878 145119 311257 5292-ITH-RIGHT ENGINE FAILED AND AUTO SHUTDOWN ON LANDING ROLL-OUT AT 72% REVERSE THRUST. MAINTENANCE INSPECTED AND REMO VED AND REPLACED THE RIGHT ENGINE 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001101900001 20011019 00001 SO 2001 10 19 C2XA01IA376 1 20011015 A 2530 CBC16371 CONNECTOR EMB 145 EMB145LR SO CABIN BURNED A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 15985 145248 IAH- WHILE AT THE GATE THE CREW NOTED A BURNT RUBBER SMELL THROUGHOUT THE AIRCRAFT, WITHOUT PACKS OR APU OPERATING. IA H- MAINTENANCE REMOVED AND REPLACED THE COFFEE POT RECEPTACLE/CONNECTOR,PERFORMED A OPERATIONAL CHECK ,NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001101900003 20011019 00003 NE 2001 10 19 S00473057 2 20010711 A 7300 FUEL CONTROL BOEING 747 747400 NM PWA 4056 PW4056 NE #1 ENG W SAJF O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 WP 03 F27209 28710 B-18202 DURING ENG START #1 ENG TAIL PIPE FIRE. NO FIRE WARNING PRESENT, CREW SHUT DOWN ENG, BOTH FIRE EXTINGUISHERS DIS CHARGED.C/A:1.ENG INLET & EXHAUST VISUAL CK NML. 2.ENG REV. COWLING OPEN VISUAL CK NML. 3.EXCITER, CABLE, INGITOR PLUG R PLD. 4.ENG FIRE EXTINGUISHER AGENTS CONTAMINATION INSP. NML. 5.ENG FUEL FILTER INSP. NML. 6.RPLD 2 FIRE BTL AND 4 CARTRI DGE. 7.PERFORM BORESCOPE INSP. THE HPC NML. 8.RPLD #1 FMU. 9.#1 ENG R/U CK NML. 10.RPLD VOICE RECORDER FOR FUTURE READOU T. 2 L 7 4 4F 4 F RT A20WE E24NE 2001101900004 20011019 00004 WP 2001 10 19 ABXA010534 1 20011015 A 2910 FLUID DOUG DC8 DC863F 302198F WP HYDRAULIC SYS LOW A ABXA K NONE K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 23 812AX 46126 GEAR WOULD NOT RETRACT AFTER TAKEOFF. HYDRAULIC PRESSURE WAS 0 PSI. HYDRAULIC QUANTITY WAS NORMAL. ACCOMPLISHED LOSS OF HYDRAULICS CHECKLIST. SYSTEM OPERATED NORMALLY ON AUX PUMP. FOUND AIRCRAFT WAS BELOW STANDPIPE LEVEL. SUSPECT AIRC RAFT HYDRAULIC QUANTITY WAS SERVICED INCORRECTLY AFTER HYDRAULIC TEST STAND REMOVED. NO LEAKS NOTED ON AIRCRAFT. REPLA CED BOTH ENGINE DRIVEN HYDRAULIC PUMPS IAW DC-8 AMM 29-10-12-2 AND BOTH CASE DRAIN FILTERS IAW 29-10-15-2, DUE TO LACK O F HYDRAULIC FLUID. LEAK CHECKED GOOD. SERVICED HYDRAULIC QUANTITY IAW DC-8 AMM. 2 L 7 4 4F 4A25 2001101900007 20011019 00007 SO 2001 10 19 C2XA01IA371 1 20011008 A 4920 4501968D APU EMB 145 EMB145LR SO APU BAY DEFECTIVE A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 13992 145284 IAH- FLIGHT 3953 STRONG FUEL ODOR OBSERVED AFTER APU START, WHILE ON ENGINE BLEED SOURCE. IAH- MAINTENANCE INSPECTED THE AIRCRAFT AND THE AIRCRAFT WAS RELEASED IAW MEL. MAINTENANCE REMOVED AND REPLACED THE APU, PERFORMED AN OPERATIONAL CHECK OF THE APU. NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001101900008 20011019 00008 SO 2001 10 19 C2XA01IA372 1 20011012 A 3350 BS2197 BATTERY EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16724 120171 IAH- WHILE PERFORMING A SERVICE CHECK MAINTENANCE NOTED THAT THE MIDDLE SECTION OF EMERGENCY LIGHTING FAILED TO ILLUMINA TE. MAINTENANCE REMOVED AND REPLACED THE NR 2 (TWO) EMERGENCY BATTERY POWER SUPPLY, PERFORMED A OPERATIONAL CHECK OF TH E EMERGENCY LIGHTING SYSTEM. NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001101900009 20011019 00009 SO 2001 10 19 C2XA01IA374 1 20011013 A 3260 WARNING SYSTEM EMB 145 EMB145LR SO COCKPIT MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 13908 145465 IAH- FLIGHT 4185 DURING CLIMB THE CREW NOTED THAT THE LANDING GEAR WARNING SYSTEM, CONSTANT LANDING GEAR WARNING, ALL E ICAS INDICATIONS NORMAL. LANDING GEAR OPERATES NORMAL. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAIN TENANCE PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM, NO DEFECTS NOTED. COULD NOT DUPLICATE THE PROBLEM. T HE AIRCRAFT FLEW A TEST FLIGHT, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001101900010 20011019 00010 SO 2001 10 19 C2XA01TY158 1 20011016 A 5310 14532604001 LATCH EMB 145 EMB145 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS DURING A SCHEDULED INSPECTION THE FUSELAGE CUTOUT FOR LEFT HAND EMERGENCY EXIT HATCH WAS FOUND TO BE GOUGED ON THE UPPER RELEASE LATCH. MAINTENANCE REMOVED AND REPLACED THE LATCH IAW EMB-145 MM 20-10-01, ALL OPERATIONAL AND PRESSURE C HECKS WERE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001101900011 20011019 00011 SO 2001 10 19 C2XA01TY159 1 20011016 A 5523 14522358416 TAB EMB 145 EMB145 SO ELEVATOR DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND ELEVATOR SPRING TAB WAS FOUND TO BE DAMAGED ON THE TRAILING EDGE. MAI NTENANCE ACCOMPLISHED A COMPOSITE REPAIR IAW EMB-145 SRM 51-70-01 AND EMB-145 CPM 51-21-05, 51-21-06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001101900013 20011019 00013 NM 2001 10 19 CALA0100955 1 20011016 A 5230 WEB BOEING 737 7373T0 1384582 NM CARGO DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 FORWARD CARGO DOOR INNER SKIN LOWER CENTER DENT AT LIGHTENING HOLE. INSTALLED DOUBLER REPAIR PER EC/RA 5230-1631. 2 L 7 2 4F RT A16WE 2001101900014 20011019 00014 NM 2001 10 19 CALA0100956 1 20011016 A 5320 6517688U165 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69333 23571 CORROSION ON Z1 ANGLE AND ON L ANGLES BENEATH THE Z (BS 312-328 AND 328-344). REMOVED AND REPLACED ZEE ANGLES AND L-ANG LES PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001101900015 20011019 00015 WP 2001 10 19 CALA0100958 1 20011017 A 3350 6011777 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 33805 49249 BOTH LEFT AND RIGHT OVERWING EVACUATION LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY PER MM 33-53-00 PAGE 407. 2 L 7 2 4F A6WE 2001101900016 20011019 00016 NM 2001 10 19 CALA0100959 1 20011017 A 3397 WIRE BOEING 737 737524 1384721 NM CABIN BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17663 28924 ESCAPE PATH LIGHT INOP AT ROW 5. REMOVED AND REPLACED FLOOR SECTION WIRING AND LIGHT ASSEMBLY. 2 L 7 2 4F RT A16WE 2001101900017 20011019 00017 NM 2001 10 19 CALA0100961 1 20011017 A 5230 6546921528 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 FORWARD BAG BIN DOOR INNER SKIN PREVIOUS REPAIR DAMAGED / GOUGED. INSTALLED REPAIR DOUBLER PER EC/RA 5230-01633. 2 L 7 2 4F RT A16WE 2001101900018 20011019 00018 SO 2001 10 19 CHQ00032 1 20011015 A 3230 LANDING GEAR EMB 145 EMB145 SO NLG & MLG MALFUNCTIONED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 CHQ 145345 LANDING GEAR WOULD NOT RETRACT. 2 L 7 2 4F RT T00011AT 2001101900019 20011019 00019 EA 2001 10 19 COMA0160805 1 20011012 A 3397 6464 WIRE CNDAIR CL600 CL6002B19 EA CABIN FAULTY A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 964CA 7129 FLIGHT 5354, FLOOR PATCH EMERGENCY LIGHTING, ROWS 2 THROUGH 5, ARE INOPERATIVE. REPLACED POWER WIRES FOR INOP SECTION O F LIGHTING. 2 L 7 2 4F RT A21EA 2001101900020 20011019 00020 EA 2001 10 19 COMA0160820 1 20011016 A 5330 601R36008 SKIN CNDAIR CL600 CL6002B19 EA FUSELAGE CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 941CA 16196 7050 FLIGHT N/A, DURING REPAIR OF ENGINE BOX BEAM DISCOVERED A CHAFED AREA ABOVE THE BOX BEAM AT Z-MEMBER. REPAIRED IN ACCOR DANCE WITH REO 601R-53-61-448. 2 L 7 2 4F RT A21EA 2001102400083 20011024 00083 NM 2001 10 24 DHL2001742500 1 20011003 A 3211 BRACKET BOEING 727 727225 1384077 NM LT MLG CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, LT MLG DEBOOST CYLS ATTACH BRACKET CRACKED AT CENTER OF BACK PANEL. REMOVED LT MLG DEBOOST CYLS ATTACH BRAC KET AS PER B727 MM 32-41-21 FOR S/M ACCESS. FABRICATED NEW BRACKET SUPPORT PANEL FOR LML GEAR DEBOOST CYLS AS PER B727 SRM 53-10-2 FIG 5. INSTALLED LT MLG DEBOOST CYLS ATTACH BRACKET AS PER B727 MM 32-41-21. 2 L 7 3 4F A3WE 2001101900022 20011019 00022 NM 2001 10 19 EISA20010122 1 20010917 A 3350 1000679 LIGHT BOEING 727 727225 1384077 NM CABIN DEFECTIVE A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 354PA 20624 EMERGENCY EXIT LIGHT AT L1 DOOR VERY DIM. REMOVED AND REPLACED EXIT LIGHT IAW MM 33, OPS CHECKS NORMAL. 2 L 7 3 4F A3WE 2001101900023 20011019 00023 NM 2001 10 19 EISA20010125 1 20011011 A 5230 DOOR BOEING 727 727223 1384074 NM MAIN CARGO DOOR OUT OF ADJ A EISA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 6813 19488 F/E PANEL MAIN CARGO DOOR WARNING LIGHT ILLUMINATE, PRESSURIZATION NORMAL, ALT FL310 PSID 8.0. MAIN CARGO DOOR PANEL, D OOR WARNING LIGHT, VENT DOOR OPEN, AND MAIN CARGO DOOR NOT CLOSED. ADJUSTED MAIN CARGO DOOR, DOOR CLOSED, AND LATCH CLO SED SWITCHES AND OPS CHECKED GOOD IAW AEI MM. 2 L 7 3 4F A3WE 2001101900024 20011019 00024 NE 2001 10 19 HAEA200100001 2 20011005 A 7510 146401117 ANTI-ICE VALVE AMD FALC20 FALCON 2720302 EU GE CF700 CF7002D2 30010 NE LT ENGINE INTERMITTENT E HAEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 05 148TW 148 ICE VALVE LIGHT STAYED ILLUMINATED. 2 L 7 2 4F 4 F A7EU E7EA 2001101900025 20011019 00025 NE 2001 10 19 HAEA200100002 2 20011005 A 7321 FCU LEAR 24 24 5170302 CE GE CJ610 CJ6104 30006 NE RT ENGINE OUT OF ADJ E HAEA O OTHER X ENGINE FLAMEOUT CL CLIMB 1 SW 05 333TW 168 241267 AIRCRAFT WAS CLIMBING FROM 390 TO 410 AT 410 RIGHT ENGINE FLAMED OUT. DESCEND TO 240, PERFORMED SUCCESSFUL RELIGHT AND CLIMB BACK TO 390. DENSITY SETTING CHANGED ON FUEL CONTROL BY MAINTENANCE. ALL FLAME-OUT CKS PERFORMED IAW GE MM'S. 2 L 7 2 4J 4 J A10CE 1E16 2001101900026 20011019 00026 CE 2001 10 19 HAEA200100003 1 20011013 A 2612 FIRE WARNING LEAR 24 24D 5170311 CE GE CJ610 CJ6106 30006 NE COCKPIT ACTIVATED E HAEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 299TW 24299 241008A DURING CLIMB AT FLT LVL 390 RT ENGINE FIRE WARNING ILLUMINATED. REDUCED POWER, LIGHT WENT OUT. RETURNED TO DEPARTURE A IRPORT. 2 L 7 2 4J 4 J A10CE 1E16 2001101900027 20011019 00027 NE 2001 10 19 HAEA200100004 2 20011015 A 7200 ENGINE AMD FALC20 FALCON 2720302 EU GE CF700 CF7002D2 30010 NE LEFT FLAMED OUT E HAEA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 SW 05 232TW 32 304226B LT ENGINE FLAME-OUT AT FL390, RELIGHT AT FL260. 2 L 7 2 4F 4 F A7EU E7EA 2001101900028 20011019 00028 NM 2001 10 19 HNAA0100065 1 20011005 A 2710 AILERON DHAV DHC8 DHC8102 2809003 NM WING MALFUNCTIONED A HNAA K NONE F FLT CONT AFFECTED LD LANDING 1 EA 07 942HA 163 JUST BEFORE LANDING, ROLL CONTROL SYSTEM DISCONNECTED. INSPECTED DISCONNECT, ROLLED AILERONS SEVERAL TIMES, INSPECTED V ISUALLY AILERON CONTROL CABLES. COULD NOT DUPLICATE PROBLEM ON GROUND. PERFORMED EVALUATION FLIGHT WITH SATISFACTORY R ESULTS. 2 H 7 2 4T RT A13NM 2001101900029 20011019 00029 NM 2001 10 19 HNAA0100066 1 20011005 A 2611 CONNECTOR DHAV DHC8 DHC8201 2809001 NM SMOKE DETECTOR DIRTY A HNAA K NONE N FALSE WARNING NR NOT REPORTED 1 EA 07 983HA 478 SMOKE WARNING LIGHT ILLUMINATED IN FLIGHT 3 TIMES FOR APPROXIMATELY 10 SECONDS EACH TIME. CLEANED AND RESEATED CONNECTO R ON SMOKE DETECTOR. 2 H 7 2 4T RT A13NM 2001101900030 20011019 00030 SO 2001 10 19 LR7A01080 1 20011009 A 5320 BEAM LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION FOUND FS 497 LT UPPER BOW BEAM LOWER LUG CRACKED AT RBL 62, WL 200. REPAIRED IAW SRM SMP 583-53-40-14. 2 H 7 4 4T A1SO 2001101900031 20011019 00031 EU 2001 10 19 SIMA200126504 1 20010921 A 5300 7253710871 TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 305AE 340B305 SBP - AIRSTAIR TRACK CORRODED, REMOVED AND REPLACED AIRSTAIR TRACK IAW SAAB SRM 51-40-21 AND 51-40-22. (M) 2 L 7 2 4T RT A52EU 2001101900032 20011019 00032 EU 2001 10 19 SIMA200126506 1 20010921 A 5300 7253721429 TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 305AE 340B305 LAVATORY TRACK AND PROFILE ARE CORRODED. REMOVED AND REPLACED LAVATORY TRACK AND PROFILE IAW SAAB SRM 51-40-21. (M) 2 L 7 2 4T RT A52EU 2001101900033 20011019 00033 EU 2001 10 19 SIMA200126507 1 20010921 A 5300 7253795383 TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 305AE 340B305 SBP - FOUND SEAT TRACK AT STATION 18.3 LEFT SIDE IS CORRODED AT FRONT SPLICE. REMOVED AND REPLACED SEAT TRACK AND U-BEA M IAW SAAB SRM 53-70-60. (M) 2 L 7 2 4T RT A52EU 2001101900034 20011019 00034 EU 2001 10 19 SIMA200126508 1 20010921 A 5300 7253799459 TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 305AE 340B305 SBP - FOUND CARGO SEAT TRACK SECTION STATION 18.3 LEFT SIDE IS CORRODED ON THE FLANGE AND WEB, SPLICED IN NEW 67.75 INCH ES OF TRACK IAW SAAB SRM 53-70-60. (M) 2 L 7 2 4T RT A52EU 2001101900035 20011019 00035 EU 2001 10 19 SIMA200126509 1 20010921 A 5300 7253799457 TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 305AE 340B305 SBP - FOUND CARGO SEAT TRACK AT STATIONB BL 0.0 IS CORRODED ON THE FLANGE AND WEB, SPLICED IN NEW SECTION OF TRACK 67.75 INCHES IAW SAAB SRM 53-70-60. (M) 2 L 7 2 4T RT A52EU 2001101900036 20011019 00036 SO 2001 10 19 LR7A01081 1 20011009 A 5320 BEAM LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION FOUND FS 557 LT UPPER BOW BEAM LOWER LUG CRACKED AT RBL 62, WL 200. REPAIRED IAW SRM SMP 583-53-40-14. 2 H 7 4 4T A1SO 2001101900037 20011019 00037 SO 2001 10 19 LR7A01084 1 20011009 A 5520 35719125 BALANCE WEIGHT LKHEED 382 382G 526414U SO ELEVATOR CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION FOUND LT ELEVATOR MASS BALANCE WEIGHT CORRODED AT FS 1090, LT HSS 316, WL 278. REPLACED BALANCE WEIGHT PER DWG 357191 & SRM SMP 583-51-70. 2 H 7 4 4T A1SO 2001101900038 20011019 00038 SO 2001 10 19 LR7A01085 1 20011009 A 5343 3889971 TRACK LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2361 4698 DURING SCHEDULED C3 INSPECTION FOUND FS 517 LT MLG FWD SHOE TRACK CRACKED AT LOWER TANG, LBL 62. REPLACED TRACK ASSEMBL IES (FWD & AFT) IAW SRM SMP 583-53-40-02. 2 H 7 4 4T A1SO 2001101900039 20011019 00039 WP 2001 10 19 P2EA2001M0007 1 20010929 A 3260 TARGET DOUG DC9 DC981 3022081 WP LT MLG LOOSE A P2EA O OTHER N FALSE WARNING CR CRUISE 1 CE 05 814US 52851 48094 FLIGHT 150 FROM LAX TO MCI. GEAR DOOR OPEN LIGHT ILLUMINATED WHILE LEVELING OFF AT CRUSE. CYCLED ENGINE HYDRAULICS TO HI AND LIGHT WENT OUT. FOUND THE LEFT HAND GEAR DOOR PROX SENSOR TARGET LOOSE. RESECURED AND OP'S CHECKED GOOD PER MM 32-60-00. 2 L 7 2 4F A6WE 2001101900040 20011019 00040 NM 2001 10 19 PCAA0109114 1 20010922 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 833EX 282 DURING ROUTINE MAINTENANCE VISIT, FOUND FORWARD EMERGENCY EXIT PATH RED LIGHT INOPERATIVE. BROKEN WIRE REPAIRED IN PATH LIGHT TRACK. ALSO REPOSITIONED LAMP HOLDER LENS ASSEMBLY TO CORRECT POSITION. OPERATIONAL CHECK GOOD. AIRCRAFT RETUR NED TO SERVICE. 2 H 7 2 4T RT A13NM 2001101900041 20011019 00041 NM 2001 10 19 PCAA0110116 1 20011005 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN DISCONNECTED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 820EX 019 DURING ROUTINE MAINTENANCE VISIT EMERGENCY FLOOR LIGHTING FOUND INOPERATIVE. SYSTEM TROUBLESHOT AND FOUND SEVERAL LIGHT STRIPS DISCONNECTED. LIGHT STRIPS RECONNECTED AND SECURED WITH HARNESS TAPE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURN ED TO SERVICE. 2 H 7 2 4T RT A13NM 2001101900042 20011019 00042 NM 2001 10 19 PCAA0110118 1 20011010 A 3350 SWITCH DHAV DHC8 DHC8102 2809003 NM COCKPIT INTERMITTENT A PCAA K NONE O OTHER CR CRUISE 1 EA 13 832EX 280 PHL- FLIGHT 3748. CREW REPORTED CABIN EMERGENCY LIGHTS WERE FLASHING ON AND OFF ALONG WITH SEVERAL ADVISORY LIGHTS. MA INTENANCE INSPECTED CABIN EMERGENCY LIGHTS, RERACKED ADVISORY DIM AND TEST BOX. GROUND RAN AIRCRAFT AND FOUND NO DEFECT S. AIRCRAFT RETURNED TO SERVICE. PROBLEM REOCCURRED IN SYR FLIGHT 3800. EMERGENCY LIGHTS IN CABIN FLASH ON AND OFF. MAINTENANCE REPLACED S1 PILOTS EMERGENCY LIGHT SWITCH, S2 FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH, EMERGENCY LIGHT CONT ROL BOX, AND EMERGENCY LIGHT BATTERIES AT POSITIONS 300, 400, 500 & 600. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001101900043 20011019 00043 NM 2001 10 19 QXEA0101624 1 20011004 A 5753 FLAP DHAV DHC8 DHC8202 2809007 NM LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - LEFT-HAND OUTBOARD FLAP JUST OUTBOARD OF THE NACELLE AT WING STATION YW174.00 IS CHAFED. REPAIRED IAW RD 8-57-173 4. 2 H 7 2 4T RT A13NM 2001101900044 20011019 00044 NM 2001 10 19 QXEA0101625 1 20011011 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - SKIN BELOW FORWARD CORNER OF BAGGAGE DOOR HAS LARGE AREA OF DAMAGE FROM CARGO NET. REPAIRED IAW DHC-8 SRM 51-20-1 6 AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2001101900045 20011019 00045 NM 2001 10 19 QXEA0101626 1 20011005 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - RIGHT-HAND OUTBOARD SEAT TRACK AT STATION X405.737 BOTTOM FLANGE HAS PITTING. REPAIRED IAW DHC-8 SRM 51-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001101900046 20011019 00046 NM 2001 10 19 QXEA0101627 1 20011009 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - RIGHT-HAND OUTBOARD SEAT TRACK AT STATION X436.000 HAS SCRATCHES ON BOTTOM FLANGE. REPAIRED IAW RD 8-52-1342. 2 H 7 2 4T RT A13NM 2001101900047 20011019 00047 NM 2001 10 19 QXEA0101628 1 20011009 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - RIGHT-HAND OUTBOARD SEAT TRACK AT STATION X445.000 TOP FLANGE HAS PITTING CORROSION. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001101900048 20011019 00048 NM 2001 10 19 QXEA0101629 1 20011009 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - RIGHT-HAND OUTBOARD SEAT TRACK AT STATION X467.000 BOTTOM FLANGE HAS PITTING CORROSION. REPAIRED IAW RD 8-53-1342 . 2 H 7 2 4T RT A13NM 2001101900049 20011019 00049 NM 2001 10 19 QXEA0101630 1 20011009 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - RIGHT-HAND OUTBOARD SEAT TRACK AT STATION X469.000 HAS A NICK OUT OF THE HOLE CIRCUMFERENCE. REPAIRED IAW RD 8-53 -1342. 2 H 7 2 4T RT A13NM 2001102500265 20011025 00265 NM 2001 10 25 01FDEA00894 1 20011015 A 5321 ABA73423 SUPPORT DOUG MD11 MD11 3023602 NM FLOORBOARD CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 CORROSION ON FLOORBOARD HAT SECTION SUPPORT AT BS 457 X=+76 IN AT FWD CABIN. REMOVED AND REPLACED FLOORBOARD PER SRM 51- 31-01 VOL II. 2 L 7 3 4F RT A22WE 2001101900050 20011019 00050 NM 2001 10 19 01FDEA00897 1 20011016 A 3260 PLUG BOEING 727 727227 1384078 NM LOOSE A FDEA K NONE J WARNING INDICATION CL CLIMB 1 SO 25 479FE 21461 01-341 AFT T/O WHEN RETRACT GEAR S/O ANNUN PNL LIGHTS OUT. RECONNECTED LOOSE PLUG P4270. 2 L 7 3 4F A3WE 2001101900051 20011019 00051 NM 2001 10 19 QXEA0101631 1 20011009 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - RIGHT-HAND OUTBOARD SEAT TRACK AT STATION X488.000 HAS PITTING CORROSION AT TOP FLANGE. REPAIRED IAW RD 8-53-1342 . 2 H 7 2 4T RT A13NM 2001101900052 20011019 00052 NM 2001 10 19 QXEA0101632 1 20011009 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS CORROSION BETWEEN X390.0 AND X391.0 ON UPPER SURFACE. REPAIRED IAW RD 8-53-1342 . 2 H 7 2 4T RT A13NM 2001101900053 20011019 00053 NM 2001 10 19 QXEA0101633 1 20011008 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - LEFT-HAND INBOARD SEAT TRACK HAS CORROSION BETWEEN X390.0 AND X391.0 ON UPPER SURFACE. REPAIRED IAW RD 8-53-1339. 2 H 7 2 4T RT A13NM 2001101900054 20011019 00054 NM 2001 10 19 QXEA0101634 1 20011008 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - LEFT-HAND INBOARD SEAT TRACK HAS CORROSION BETWEEN STATIONS X361.0 AND 362.0. REPAIRED IAW RD 8-53-1339. 2 H 7 2 4T RT A13NM 2001101900055 20011019 00055 NM 2001 10 19 QXEA0101635 1 20011003 A 5720 BRACKET DHAV DHC8 DHC8202 2809007 NM WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - BRACKET CRACKED, FRONT WING SPAR UPPER SPAR CAP AT YW138. REPAIRED IAW DHC-8 SRM 51-40-00, PAGE 1 (2) AND PAGE 2. 2 H 7 2 4T RT A13NM 2001101900056 20011019 00056 NM 2001 10 19 QXEA0101636 1 20011003 A 5720 BRACKET DHAV DHC8 DHC8202 2809007 NM WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - BRACKET CRACKED, FRONT SPAR, RIGHT WING LOWER SPAR CAP AT YW138. REPAIRED IAW DHC-8 SRM 51-40-00, PAGE 1 (2) AND PAGE 2. 2 H 7 2 4T RT A13NM 2001101900057 20011019 00057 NM 2001 10 19 QXEA0101637 1 20011003 A 5720 BRACKET DHAV DHC8 DHC8202 2809007 NM WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - BRACKET CRACKED, FRONT SPAR LEFT WING LOWER SPAR CAP AT YW138. REPAIRED IAW DHC-8 SRM 51-40-00, PAGE 1 (2) AND PA GE 2. 2 H 7 2 4T RT A13NM 2001101900058 20011019 00058 NM 2001 10 19 QXEA0101638 1 20011003 A 5720 BRACKET DHAV DHC8 DHC8202 2809007 NM LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - BRACKET CRACKED, FRONT SPAR, LEFT WING UPPER SPAR CAP AT STATION YW138. REPAIRED IAW DHC-8 SRM 51-40-00, PAGE 1 ( 2) AND PAGE 2. 2 H 7 2 4T RT A13NM 2001101900059 20011019 00059 EU 2001 10 19 MALA010744 1 20011003 A 2710 7227151522 CONTROL CABLE SAAB SF340 SF340A 7850100 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 99XJ 340A099 DURING 4K-CHECK IN CWA, FOUND LT O/B LT AILERON FWD CABLE CHAFED. MAINTENANCE REPLACED LT O/B AILERON FWD CABLE P/N 722 7151-522 IAW SAAB 340 AMM 27-11-25. 2 L 7 2 4T RT A52EU 2001101900061 20011019 00061 EU 2001 10 19 MALA010746 1 20011004 A 2730 7227105711 CONTROL CABLE SAAB SF340 SF340A 7850100 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 99XJ 340A099 FOUND DURING 4K-CHECK IN CWA, LT O/B FWD FUSELAGE ELEVATOR CABLE CHAFED. MAINTENANCE REPLACED LT FWD O/B ELEVATOR FUSEL AGE CABLE IAW SF3 AMM 27-31-15 P/N 7227105-711. 2 L 7 2 4T RT A52EU 2001101900062 20011019 00062 EU 2001 10 19 MALA010747 1 20011004 A 2730 7227705644 CONTROL CABLE SAAB SF340 SF340A 7850100 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 99XJ 340A099 FOUND DURING 4K-CHECK IN CWA, LT I/B FWD FUSELAGE ELEVATOR CABLE CHAFED. MAINTENANCE REPLACED LT I/B FWD FUSELAGE ELEVA TOR CABLE IAW SR3 AMM 27-31-154 P/N ON 7227705-644. 2 L 7 2 4T RT A52EU 2001101900063 20011019 00063 EU 2001 10 19 MALA010748 1 20011004 A 2720 7227105582 CONTROL CABLE SAAB SF340 SF340A 7850100 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 99XJ 340A099 FOUND DURING 4K-CHECK IN CWA, LT FUSELAGE CIRCUIT I AFT RUDDER CABLE CHAFED. MAINTENANCE REPLACED LT CIRCUIT I AFT RUDD ER CABLE P/N 7227105-582 IAW SF340 AMM 27-21-25-4. 2 L 7 2 4T RT A52EU 2001101900064 20011019 00064 EU 2001 10 19 MALA010749 1 20011004 A 2720 7227105562 CONTROL CABLE SAAB SF340 SF340A 7850100 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 99XJ 340A099 DURING 4K-CHECK IN CWA, MAINTENANCE FOUND LT O/B CIRCUIT I DUAL FUSELAGE RUDDER CABLE CHAFED. MX REPLACED LT O/B CIRCUI T I DUAL RUDDER CABLE P/N 7227105-562 IAW SF340 AMM 27-21-25-4. 2 L 7 2 4T RT A52EU 2001101900065 20011019 00065 EU 2001 10 19 MALA010750 1 20011004 A 2720 7227105571 CONTROL CABLE SAAB SF340 SF340A 7850100 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 99XJ 340A099 LT I/B CIRCUIT I DUAL FUSELAGE RUDDER CABLE CHAFED. MAINTENANCE REPLACED LT I/B CIRCUIT I RUDDER CABLE P/N 7227105-571 IAW SF340 AMM 27-21-25-4. 2 L 7 2 4T RT A52EU 2001101900066 20011019 00066 EU 2001 10 19 MALA010751 1 20011004 A 2710 7227105614 CONTROL CABLE SAAB SF340 SF340A 7850100 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 99XJ 340A099 FOUND DURING 4K-CHECK, IN CWA, RT I/B FWD FUSELAGE AILERON CABLE CHAFED. MAINTENANCE REPLACED RT I/B FWD FUSELAGE AILER ON CABLE P/N 7227105-614 IAW SAAB AMM 27-11-25. 2 L 7 2 4T RT A52EU 2001101900067 20011019 00067 EU 2001 10 19 MALA010752 1 20011004 A 2710 7227105624 CONTROL CABLE SAAB SF340 SF340A 7850100 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 99XJ 340A099 DURING 4K-CHECK IN CWA, RT FWD FUSELAGE AILERON O/B CABLE CHAFED. MAINTENANCE REPLACED RT O/B FWD FUSELAGE AILERON CABL E IAW SF3AMM 27-11-25. P/N 7227105-624. 2 L 7 2 4T RT A52EU 2001101900068 20011019 00068 EU 2001 10 19 MALA010753 1 20011004 A 2720 7227105582 CONTROL CABLE SAAB SF340 SF340A 7850100 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 99XJ 340A099 DURING 4K- CHECK IN CWA, DISCOVED RT CIRCUIT I AFT SINGLE RUDDER CABLE CHAFED. MAINTENANCE REPLACED CIRCUIT I AFT SINGL E RUDDER CABLE REPLACED P/N 7227105-582, IAW SF340AMM 27-21-25-4. 2 L 7 2 4T RT A52EU 2001101900069 20011019 00069 EU 2001 10 19 MALA010754 1 20011004 A 2720 7227105571 CONTROL CABLE SAAB SF340 SF340A 7850100 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 99XJ 340A099 RT I/B CIRCUIT I DUAL FUSELAGE RUDDER CABLE CHAFED. MAINTENANCE INSTALLED RT I/B DUAL CIRCUIT I RUDDER CABLE P/N 722710 5-571 IAW SF340AMM 27-21-25-4. 2 L 7 2 4T RT A52EU 2001101900070 20011019 00070 EU 2001 10 19 MALA010755 1 20011004 A 2720 7227105562 CONTROL CABLE SAAB SF340 SF340A 7850100 EU RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 99XJ 340A099 RT O/B CIRCUIT I DUAL FUSELAGE RUDDER CABLE CHAFED. MAINTENANCE INSTALLED NEW RUDDER RT O/B CIRCUIT I FUSELAGE CABLE. P/N 7227105-562 IAW SR 340 AMM 27-21-25-4. 2 L 7 2 4T RT A52EU 2001101900071 20011019 00071 EU 2001 10 19 MALA010756 1 20011004 A 2730 7227105644 CONTROL CABLE SAAB SF340 SF340A 7850100 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 99XJ 340A099 DURING 4K-CHECK IN CWA, RT I/B FWD FUSELAGE ELEVATOR CABLE CHAFED. MAINTENANCE REPLACED RT I/B FWD FUSELAGE ELEVATOR CA BLE P/N 7227105-644 IAW SF3AMM 27-31-15. 2 L 7 2 4T RT A52EU 2001101900072 20011019 00072 EU 2001 10 19 MALA010757 1 20011006 A 2730 7227105712 CONTROL CABLE SAAB SF340 SF340A 7850100 EU ELEVATOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 99XJ 340A099 DURING 4K-CHECK IN CWA, RT O/B FWD FUSELAGE ELEVATOR CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED RT O/B FWD FUSELAGE ELEVATOR CABLE IAW SF3 AMM 27-31-15-4, P/N 7227105-712. 2 L 7 2 4T RT A52EU 2001101900073 20011019 00073 CE 2001 10 19 2001F00436 1 20011016 A 7810 NH100089770 CLAMP CESSNA 340 340A 2076405 CE CONT O520 TSIO520NB 17040 SO ENGINE CRACKED B BIGA K NONE O OTHER IN INSP/MAINT 1 NM 03 118BH 49 340A0003 NEW AEROQUIP EXHAUST CLAMPS ARE CRACKING AROUND OUTER PERIPHERY. FOUR CLAMPS IN 201 HOURS. ALL CLAMPS APPEAR TO BE MAN UFACTURING DEFECTS. NON LIFE LIMITED CLAMPS. 1 L 7 2 3O 3 O 3A25 E8CE 2001101900074 20011019 00074 CE 2001 10 19 2001F00448 1 20011016 A 7810 NH100089770 CLAMP CESSNA 340 340A 2076405 CE CONT O520 TSIO520NB 17040 SO ENGINE CRACKED B BIGA K NONE O OTHER IN INSP/MAINT 1 NM 03 114BH 100 340A1230 NEW AEROQUIP EXHAUST CLAMPS ARE CRACKING AROUND OUTER PERIPHERY. TWO CLAMPS IN LAST 200 HOURS. BOTH APPEAR TO BE MANUF ACTURING DEFECTS. NON LIFE LIMITED CLAMPS. 1 L 7 2 3O 3 O 3A25 E8CE 2001101900075 20011019 00075 EA 2001 10 19 COMA0160823 1 20011016 A 2751 855D1009 BPSU CNDAIR CL600 CL6002B19 EA LEFT WING FAULTY A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 920CA 4636 7022 FLIGHT 5362. DURING DESCENT, RECEIVED A FLAP CAUTION MESSAGE AT 8 DEGREE FLAP POSITION.REPLACED THE BRAKE AND POSITION S ENSING UNIT. 2 L 7 2 4F RT A21EA 2001101900076 20011019 00076 EA 2001 10 19 COMA0160824 1 20011018 A 2720 RUDDER CNDAIR CL600 CL6002B19 EA A COMA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 971CA 7145 FLIGHT 5412. DURING CRUISE FLIGHT ABOVE 280 KNOTS, THE AIRCRAFT ENCOUNTERED UNCOMMANDED RUDDER MOVEMENTS.PERFORMED ON OP ERATIONAL CHECK OF THE YAW DAMPER SYSTEM, INCLUDING SVL-4000 COMMAND AND FEED BACK TEST. DISCREPANCY COULD NOT BE DUPLIC ATED. 2 L 7 2 4F RT A21EA 2001101900077 20011019 00077 EA 2001 10 19 COMA0160825 1 20011016 A 5610 NP1393221 WINDOW CNDAIR CL600 CL6002B19 EA L/H FRACTURED A COMA K NONE Z SIGNIFICANT FAILURE REPORT CR CRUISE 1 SO 01 949CA 14536 7080 FLIGHT 5903. PILOT'S SIDE WINDOW SHATTERED AT 29,000 FT.REPLACED THE PILOT'S SIDE WINDOW. 2 L 7 2 4F RT A21EA 2001102900121 20011029 00121 SO 2001 10 29 C2XA01BT171 1 20011016 A 4920 4501968 APU EMB 145 EMB145LR SO APU BAY FAILED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 14974 145161 CREW REPORTED, APU AUTO SHUTDOWN ON TAXI TO GATE, FOLLOWED BY HEAVY SMOKE SMELL AND SMOKE HAZE IN REAR CABIN. YUL MAINT ENANCE INSPECTED AND DEFERRED APU IAW MEL 49-00-00, PLACARD CONTROL NUMBER 017287. AIRCRAFT RETURNED TO SERVICE. 10/19 /2001 RIC MAINTENANCE REMOVED AND REPLACED THE APU IAW EMB145 MM 49-10-00. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2001101900079 20011019 00079 SO 2001 10 19 C2XA01IA375 1 20011017 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN MALFUNCTIONED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 57734 120199 IAH- DURING PREFLIGHT THE CREW NOTED THAT FOUR EMERGENCY LIGHTS ON THE FLOOR FAILED TO ILLUMINATE. IAH- MAINTENANCE P ERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN T O SERVICE. 2 L 7 2 4T RT A31SO 2001101900080 20011019 00080 NM 2001 10 19 CALA0100962 1 20011018 A 5320 WEB BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69333 23571 AFT LEFT AREA STATION 996 FLOOR WEB CRACKED (1 INCH) UNDER L2 Z-ANGLE. INSTALLED SERVICEABLE WEB WITH FASTENERS PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001101900081 20011019 00081 EU 2001 10 19 CHQ00033 1 20011018 A 7931 WARNING LIGHT SAAB SF340 SF340A 7850100 EU COCKPIT ACTIVATED A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 146 146 LT PROP OIL PRESSURE LIGHT-0-PRESSURE. 2 L 7 2 4T RT A52EU 2001101900083 20011019 00083 NM 2001 10 19 PCAA0110119 1 20011015 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM POSITION 400 INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 834EX 285 DURING ROUTINE MAITENANCE VISIT TWO FLOOR EMERGENCY LIGHT BULBS FOUND INOPERATIVE AT ROW 1. POWER SUPPLY AND BATTERY AT POSITION 400 REPLACED. BULB SOCKETS ALSO REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001101900087 20011019 00087 NE 2001 10 19 GLBA2001214 2 20011012 A 7261 OIL SYSTEM BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ENGINE LOW A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 01 249GL UE249 RIGHT ENGINE OIL FLUX. INSPECTED FOUND OIL SYSTEM LOW. SERVICED, OPS CHECKED SATISFACTORY. 2 L 7 2 4T 4 T RT A24CE E26NE 2001101900088 20011019 00088 CE 2001 10 19 GLBA2001215 1 20011016 A 3244 50060285 TIRE BEECH 1900 1900D 1154162 CE NR 2 BLEW OUT A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 01 208GL 151 UE208 NR 2 TIRE BLEW OUT ON T/O. REPLACED WHEEL ASSEMBLY. 2 L 7 2 4T RT A24CE 2001101900089 20011019 00089 CE 2001 10 19 GLBA2001216 1 20011016 A 2421 WIRE BEECH 1900 1900D 1154162 CE GENERATOR SYS BROKEN A GLBA C ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 CE 01 101UX UE101 LEFT GENERATOR FELL OFF LINE ON T/O. INSPECTED, FOUND WIRE BROKEN. REPAIRED, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001101900090 20011019 00090 NM 2001 10 19 UPS01237093 1 20011018 A 5310 STRINGER BOEING 727 72725C 138400H NM STA 319 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:N/A STRINGER 20R CRACKED AT FRAME 294 FWD OF LAV WASTE CHUTE STRINGER REPAIRED AS PER SRM 53-10-03. STATION 319 TO 284.5 REPAIRED 2 L 7 3 4F A3WE 2001101900091 20011019 00091 NM 2001 10 19 P5CA0100602 1 20011017 A 5297 WIRE BOEING 747 747122 1384872 NM CARGO DOOR CHAFED A P5CA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 23 850FT 19755 FWD LOWER CARGO DOOR ANNUNCIATOR LIGHT ILLUMINATED WHEN LEVELING FL350. FWD ANNUNCIATOR CARGO DOOR LIGHT ON GLARESHIELD WAS ILLUMINATED. LIGHT EXTINGUISHED WHEN DESCENDING THROUGH FL270 AT 6.0 PSI DIFFERENTIAL CABIN. FOUND CHAFED WIRE AT FWD CARGO DOOR JUNCTION BOX. REPAIRED WITH SPLICE IAW MM 20-10-19. LIGHT NOW CK'S NORMAL. 2 L 7 4 4F A20WE 2001101900092 20011019 00092 NM 2001 10 19 QXEA0101639 1 20011008 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - LEFT-HAND INBOARD SEAT TRACK HAS PITTING CORROSION AT STATION X342 ON CENTER OF UPPER SURFACE. REPAIRED IAW RD 8- 53-1339. 2 H 7 2 4T RT A13NM 2001101900093 20011019 00093 NM 2001 10 19 QXEA0101640 1 20011008 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - LEFT-HAND INBOARD SEAT TRACK HAS CORROSION BETWEEN STATIONS X264.0 AND X266.0. REPAIRED IAW RD 8-53-1339. 2 H 7 2 4T RT A13NM 2001101900094 20011019 00094 NM 2001 10 19 QXEA0101641 1 20011008 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - LEFT-HAND INBOARD SEAT TRACK, OUTBOARD FLANGE HAS CORROSION AT STATION X302 ON UPPER SURFACE. REPLACED SEAT TRACK . 2 H 7 2 4T RT A13NM 2001101900095 20011019 00095 NM 2001 10 19 QXEA0101642 1 20011008 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - LEFT-HAND INBOARD SEAT TRACK HAS CORROSION BETWEEN STATIONS X280.0 AND X281.0 ON UPPER SURFACE. REPAIRED IAW RD 8 -53-1339. 2 H 7 2 4T RT A13NM 2001101900096 20011019 00096 NM 2001 10 19 QXEA0101643 1 20011008 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - LEFT-HAND INBOARD SEAT TRACK HAS CORROSION BETWEEN STATION X264.0 AND X270.0 ON UPPER SURFACE. REPAIRED IAW RD 8- 53-1339. 2 H 7 2 4T RT A13NM 2001101900097 20011019 00097 NM 2001 10 19 QXEA0101644 1 20011003 A 3210 YOKE DHAV DHC8 DHC8202 2809007 NM LT MLG CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - LEFT-HAND MAIN LANDING GEAR YOKE ASSEMBLY HAS A SMALL CHAFE DAMAGE ON INBOARD SIDE NEAR FLIGHT SPOILER SERVO VALVE . REPAIRED IAW DHC-8 SRM 51-20-16, SRM 51-20-36 AND SRM 51-20-57. 2 H 7 2 4T RT A13NM 2001101900098 20011019 00098 EU 2001 10 19 QXEA0101652 1 20011013 A 3350 6008905 POWER SUPPLY FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 498US 6808 6808 11181 PDX - LEFT AND RIGHT AFT EVACUATION LIGHTS ON FUSELAGE WING/BELLY ARE INOPERABLE. REMOVED AND REPLACED BATTERY POWER SU PPLY. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001101900099 20011019 00099 NM 2001 10 19 MWEA011401 1 20011017 A 2720 5910257 TAB DOUG MD88 MD88 3023688 NM RUDDER DEBONDED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 RUDDER TAB, FIXED TAB IS DEBONDED AT LEFT LOWER END. -- REMOVED AND REPAIRED FLAME SPRAY AND INSTALLED RUDDER CONTROL TAB. 2 L 7 2 4F RT A6WE 2001101900100 20011019 00100 NM 2001 10 19 QXEA0101653 1 20011009 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - RIGHT-HAND OUTBOARD SEAT TRACK AT STATION X513.000 HAS PITTING CORROSION ON TOP FLANGE. REPAIRED IAW RD 8-5.3-364 4. 2 H 7 2 4T RT A13NM 2001102100001 20011021 00001 SO 2001 10 21 C2XA01IA377 1 20011016 A 2150 24540150 CLAMP EMB 120 EMB120ER 3260203 SO FUSELAGE LOOSE A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 15725 17258 120173 IAH- FLIGHT 3442 NOTED SMOKE WARNING ON MAP, FOLLOWED BY #2 PACK FAIL IN FLIGHT. RAN QRH ON BOTHWARNINGS, AND, RETURNE D TO IAH. BOTH WARNINGS CLEARED ON RETURN TO IAH. IAH- MAINTENANCE TIGHTENED CLAMPS ON NUMBER 2 HEAT EXCHANGER,PERFOR MED A OPERATIONAL CHECK OF THE AIR CONDITIONING SYSTEM, NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SE RVICE. 2 L 7 2 4T RT A31SO 2001102100002 20011021 00002 SO 2001 10 21 C2XA01IA379 1 20011018 A 3350 20131A BATTERY EMB 145 EMB145LR SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13979 145181 IAH- DURING PERFLIGHT THE CREW NOTED THAT THE EMERGENCY ISLE PATH LIGHTING FAILED TO ILLUMINATE. IAH- MAINTENANCE REMO VED AND REPLACED THE BATTERY, PERFORMED A OPERTIONAL CHECK,NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN T O SERVICE. 2 L 7 2 4T RT T00011AT 2001102100003 20011021 00003 SO 2001 10 21 CX2A01IA380 1 20011020 A 3350 AD2047 BATTERY EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 57734 120199 IAH- DURING POST FLIGHT THE CREW NOTED THAT THE EMERGENCY ISLE PATH LIGHTS DID NOT ILLUMINATE. IAH- MAINTENANCE REMOVE D AND REPLACED THE #2 EMERGENCY BATTERY PACK,PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED,AND, THE AIRCRAFT WAS APPRO VED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001102200001 20011022 00001 2001 10 22 SWAA012859 4 20011017 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 611SW 27697 FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001102200002 20011022 00002 NM 2001 10 22 SWAA012861 1 20011018 A 5310 6545409 WEB BOEING 737 7373H4 1384600 NM RH W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESS WEB CRACKED AT BS 663, RBL 42. REPAIRED W EB PER SWA TI-353-032. 2 L 7 2 4F RT A16WE 2001102200003 20011022 00003 NM 2001 10 22 SWAA012862 1 20011018 A 5310 6516300 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND WEB CRACKED AT BS 178, RBL 5, WL 212. REPAIR ED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001102200004 20011022 00004 NM 2001 10 22 SWAA012863 1 20011018 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED 1.75 INCHES LONG AT BS 727D+6, ABOVE STR 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001102200005 20011022 00005 NM 2001 10 22 SWAA012864 1 20011018 A 5310 6969854 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED 142D CHECK, FOUND FWD SVC DOOR CUT OUT LWR STUB FRAME CRACKED AT BS 294.5. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001102200006 20011022 00006 NM 2001 10 22 SWAA012865 1 20011018 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED 1/2D CHECK AT DALFORT, FOUND STRINGER CORRODED AT BS 1006, STR 26R. RE PAIRED STR PER SRM. 2 L 7 2 4F RT A16WE 2001102200007 20011022 00007 NM 2001 10 22 SWAA012866 1 20011018 A 5315 6546804 BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED 1/2D CHECK AT DALFORT, FOUND FLOOR BEAM CRACKED AT BS 744A, RBL 43.5. REPAIR ED FLOOR BEAM PER DLF XEA. 2 L 7 2 4F RT A16WE 2001102200008 20011022 00008 NM 2001 10 22 SWAA012867 1 20011018 A 5755 6544960 SPOILER BOEING 737 7373H4 1384600 NM LH WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED 1/2D CHECK AT DALFORT, FOUND LH WING OUTBD SPOILER DELAMINATED. REPA IRED SPOILER PER SRM. 2 L 7 2 4F RT A16WE 2001102200009 20011022 00009 NM 2001 10 22 SWAA012868 1 20011018 A 5753 6546435 FLAP BOEING 737 7373H4 1384600 NM LH WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 370SW 26597 DURING SCHEDULED BC1 CHECK, FOUND LH WING OUTBD T/E AFT FLAP DELAMINATED AT INBD T/E. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2001102200010 20011022 00010 NM 2001 10 22 SWAA012869 1 20011017 A 5330 6518420 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 504SW 24181 DURING SCHEDULED A1 CHECK, FOUND CAPT'S FWD WINDOW POST SKIN CRACKED .5 INCHES. REPAIRED WINDOW POST SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001102200011 20011022 00011 NM 2001 10 22 SWAA012839 1 20011016 A 5314 6545866 WEB BOEING 737 7373H4 1384600 NM AFT CARGO CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM WEB CRACKED AT BS 727B. R&R WEB PER SRM. 2 L 7 2 4F RT A16WE 2001102200012 20011022 00012 NM 2001 10 22 SWAA012841 1 20011016 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 314SW 23336 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 533B, STR 10L. REPAIRED STR PER SRM. 2 L 7 2 4F RT A16WE 2001102200013 20011022 00013 NM 2001 10 22 SWAA012846 1 20011015 A 3350 07912 COVER BOEING 737 7373T5 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVER LOOSE AT ROW 1. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2001102200014 20011022 00014 2001 10 22 SWAA012847 4 20011017 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM AFT SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 700GS 27835 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR FLAP LOOSE. ADJUS TED GIRT BAR FLAP. 2 L 7 2 4F RT A16WE 2001102200015 20011022 00015 NM 2001 10 22 SWAA012849 1 20011017 A 3350 07912 COVER BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 501SW 24178 EEPLS COVER BROKEN AT ROW 15. R&R COVER PER MM. 2 L 7 2 4F RT A16WE 2001102200016 20011022 00016 NM 2001 10 22 SWAA012850 1 20011017 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 703SW 27837 EEPLS MISSING COVER AT ROW 14. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2001102200017 20011022 00017 NM 2001 10 22 SWAA012851 1 20011017 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 714CB 27848 EEPLS WIRES EXPOSED AT ROW 11. INSTALLED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2001102200018 20011022 00018 2001 10 22 SWAA012852 4 20011016 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM AFT ENTRY DOOR. LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 527SW 26569 AFT ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001102200019 20011022 00019 2001 10 22 SWAA012853 4 20011017 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 707SA 27841 FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE. SECURED GIRT BAR PER MM. 2 L 7 2 4F RT A16WE 2001102200020 20011022 00020 NM 2001 10 22 SWAA012855 1 20011016 A 5310 6546529 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED ( 4 EA ) BETWEEN STR 8R & 9R, BS 440, 480, 827 & 887. REPAIRED FRAMES PER BFG ER. 2 L 7 2 4F RT A16WE 2001102200022 20011022 00022 2001 10 22 SWAA012831 4 20011016 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM AFT ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 525SW 26567 AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR LANYARD LOOSE. SECURED LANYARD PER MM. 2 L 7 2 4F RT A16WE 2001102200023 20011022 00023 2001 10 22 SWAA012832 4 20011016 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001102200024 20011022 00024 NM 2001 10 22 SWAA012833 1 20011015 A 5311 6546568 FRAME BOEING 737 7373Q8 1384670 NM AFT FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 1018, LBL 1 & WL 191. REPAIR ED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001102200025 20011022 00025 NM 2001 10 22 SWAA012834 1 20011016 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED ( 2 EA ) AT BS 727E, STR 22R & 23R. REP AIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001102200026 20011022 00026 NM 2001 10 22 SWAA012835 1 20011015 A 5754 6573714 SLAT BOEING 737 7373Q8 1384670 NM LH WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED C1 CHECK, FOUND # 1 L/E SLAT CRACKED 3/8 INCH LONG AT AFT ROW OF FASTENERS, LOWER SKIN. REPAIRED # 1 L/E SLAT PER SWA RA 1-357-1118. 2 L 7 2 4F RT A16WE 2001102200027 20011022 00027 NM 2001 10 22 SWAA012837 1 20011015 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 312SW 23334 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED 2 1/2 INCH LONG AT BS 500C+ 6, ABOVE STR 15R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001102200028 20011022 00028 NM 2001 10 22 SWAA012838 1 20011015 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 312SW 23334 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED 1 1/4 INCH LONG AT BS 727, STR 20L. REPA IRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001102200029 20011022 00029 NM 2001 10 22 CALA0100963 1 20011022 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM STA 727-767 CORRODED A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 69333 23571 CABIN RIGHT SIDE INBOARD SEAT TRACK CORRODED FROM STATION 727E TO STATION 767. REMOVED AND REPLACED SEAT TRACK PER SRM 5 3-00-52, SOPM 20-41-04 AND AMM 51-21-00. 2 L 7 2 4F RT A16WE 2001102200030 20011022 00030 WP 2001 10 22 ABXA010535 1 20011014 A 7722 PROBE DOUG DC8 DC863F 302198F WP NR 1 ENGINE DAMAGED A ABXA O OTHER O OTHER TO TAKEOFF 1 GL 23 815AX 46097 NR 1 ENGINE EGT AT V1 WENT TO 575 DEGREES AND INCREASED, REDUCE POWER BY 1 KNOB. DURING INITIAL TAKEOFF ROLL ALL PARAME TERS WERE NORMAL. NR 4 ENGINE, SAME AS NR 1 ENGINE. FOUND THE NR 1 ENGINE EGT PROBES NR 2 AND NR 6 DAMAGED, FOUND THE N R 4 ENGINE EGT WIRE SHORTED TO GROUND, REPAIRED AS REQUIRED IAW DC-8 MM. 2 L 7 4 4F 4A25 2001102200031 20011022 00031 SO 2001 10 22 CHQ00031 1 20011014 A 7931 WARNING SYSTEM EMB 145 EMB145 SO COCKPIT ACTIVATED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 CHQ 145345 E1 LOW OIL PRESS SWITCH EICAS MSG INTERMITTENT. 2 L 7 2 4F RT T00011AT 2001102200032 20011022 00032 WP 2001 10 22 DHL2001803013 1 20011018 A 2612 FIRE LOOP DOUG DC8 DC873 302199C WP NR 4 ENGINE SHORTED A DHLA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 803DH 46123 ENG NR 4 SHORT CIRCUIT LIGHT ILLUMINATED MASTER FIRE AND FIRE HANDLE LIGHTS AFTER SHUT DOWN. DEFERRED NR 4 ENG B-LOOP F IRE WARNING. INSPECTED SYSTEM FOUND ELEMENT SHORTED OUT AND ONE CONNECTOR LOOSE. CORRECT PROBLEMS RING WIRES OPS CK NORM AL AS PER MM 26-10. 2 L 7 4 4F RT 4A25 2001102200033 20011022 00033 NM 2001 10 22 QXEA0101654 1 20011009 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - RIGHT-HAND OUTBOARD SEAT TRACK AT STATION X547.000 TOP AND BOTTOM FLANGES HAVE PITTING CORROSION. REPAIRED IAW RD 8-53-7644. 2 H 7 2 4T RT A13NM 2001102200034 20011022 00034 NM 2001 10 22 QXEA0101655 1 20011009 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - RIGHT-HAND INBOARD SEAT TRACK AT STATION X547.000 TO STATION X537.000 HAS PITTING CORROSION ON TOP AND BOTTOM FLAN GE. REPAIRED IAW RD 8-53-1339. 2 H 7 2 4T RT A13NM 2001102200035 20011022 00035 NM 2001 10 22 QXEA0101656 1 20011009 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - RIGHT-HAND INBOARD SEAT TRACK AT STATION 513.000 HAS PITTING CORROSION ON TOP FLANGE. REPAIRED IAW RD 8-53-1339. 2 H 7 2 4T RT A13NM 2001102200036 20011022 00036 NM 2001 10 22 QXEA0101657 1 20011009 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - RIGHT-HAND INBOARD SEAT TRACK AT STATION X501.000 HAS PITTING CORROSION ON TOP FLANGE. REPAIRED IAW RD 8-53-1339. 2 H 7 2 4T RT A13NM 2001102200037 20011022 00037 NM 2001 10 22 QXEA0101658 1 20011009 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - RIGHT-HAND INBOARD SEAT TRACK AT STATION X488.000 HAS PITTING CORROSION ON TOP FLANGE. REPAIRED IAW RD 8-53-1339. 2 H 7 2 4T RT A13NM 2001102200038 20011022 00038 NM 2001 10 22 QXEA0101659 1 20011009 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - LEFT-HAND INBOARD SEAT TRACK HAS CORROSION BETWEEN STATIONS X537.5 THROUGH X543.5 ON UPPER SURFACE. REPAIRED IAW RD 8-53-4936. 2 H 7 2 4T RT A13NM 2001102200039 20011022 00039 NM 2001 10 22 QXEA0101660 1 20011009 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - LEFT-HAND INBOARD SEAT TRACK HAS CORROSION AT STATION X515.0 THROUGH X517.0 ON UPPER SURFACE. REPAIRED IAW RD 8-5 3-1339. 2 H 7 2 4T RT A13NM 2001102200040 20011022 00040 NM 2001 10 22 QXEA0101661 1 20011009 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS CORROSION AT STATION X515.0 THROUGH X517.0 ON UPPER SURFACE. REPAIRED IAW RD 8- 53-3644. 2 H 7 2 4T RT A13NM 2001102200042 20011022 00042 NM 2001 10 22 QXEA0101663 1 20011009 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS CORROSION AT STATION X374.0 THROUGH X375.0 ON UPPER SURFACE. REPAIRED IAW RD 8- 53-1342. 2 H 7 2 4T RT A13NM 2001102200043 20011022 00043 NM 2001 10 22 QXEA0101664 1 20011009 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS CORROSION BETWEEN STATION X361.0 AND X362.0 ON UPPER SURFACE. REPAIRED IAW RD 8 -53-1342. 2 H 7 2 4T RT A13NM 2001102200044 20011022 00044 NM 2001 10 22 QXEA0101665 1 20011009 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS CORROSION BETWEEN STATION X327.3 AND X329.3 ON UPPER SURFACE. REPAIRED IAW RD 8 -53-1342. 2 H 7 2 4T RT A13NM 2001102200045 20011022 00045 NM 2001 10 22 QXEA0101666 1 20011008 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - LEFT-HAND INBOARD SEAT TRACK HAS CORROSION BETWEEN STATION 327.3 AND 329.3 ON UPPER SURFACE. REPAIRED IAW RD 8-53 -1339. 2 H 7 2 4T RT A13NM 2001102200046 20011022 00046 NM 2001 10 22 QXEA0101667 1 20011009 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS CORROSION BETWEEN STATION X279.0 AND X281.0 ON UPPER SURFACE. REPAIRED IAW RD 8 -53-1342. 2 H 7 2 4T RT A13NM 2001102200047 20011022 00047 NM 2001 10 22 QXEA0101668 1 20011009 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS CORROSION BETWEEN STATIONS X264.0 AND X266.0. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2001102200048 20011022 00048 NM 2001 10 22 QXEA0101669 1 20011002 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - LEFT-HAND INBOARD SEAT TRACK HAS CORROSION BETWEEN STATION X224.0 AND X262.0 ON UPPER SURFACE. REPAIRED IAW RD 8- 53-4698. 2 H 7 2 4T RT A13NM 2001102200049 20011022 00049 NM 2001 10 22 QXEA0101670 1 20011004 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM LT WING SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - LEFT-HAND WING AT STATION YW133.00 FORWARD SPAR TOWARD THE TOP THERE ARE 3 SMALL LIGHT SCRATCHES. REPAIRED IAW DH C-8 SRM 51-20-26, PAGES 4 AND 5, STEPS 3-A B AND C. 2 H 7 2 4T RT A13NM 2001102200051 20011022 00051 NM 2001 10 22 QXEA0101672 1 20011012 A 5230 FLANGE DHAV DHC8 DHC8202 2809007 NM CARGO DOOR BENT A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - AFT CARGO DOOR EXTERIOR TOP EDGE IS BENT AND HAS SEVERAL CHAFFD PLACES. REPAIRED IAW HORIZON AIR EA 2-52-112. 2 H 7 2 4T RT A13NM 2001102200052 20011022 00052 NM 2001 10 22 QXEA0101678 1 20011015 A 5412 FIREWALL DHAV DHC8 DHC8202 2809007 NM NR 2 NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - CHAFE IN NR 2 NACELLE FIREWALL FLANGE APPROXIMATELY 3 INCHES ABOVE LOWER SUPPORT STRUT 6 INCHES LONG AND APPROXIMA TELY .020 INCH DEEP. INSTALLED REPAIR DOUBLER IAW EA 2-54-106. 2 H 7 2 4T RT A13NM 2001102200053 20011022 00053 NM 2001 10 22 QXEA0101679 1 20011011 A 5415 BRACKET DHAV DHC8 DHC8* NM RT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - RIGHT HAND AFT NACELLE DECK AND EXHAUST SHROUD SUPPORT BRACKETS, CLIPS, AND ATTACH POINTS ARE CRACKED AND CHAFED. REPAIRED IAW RD 8/4-54-033, RD 8/54-044, RD 8/54-31, RD 8/54-016, EA 6-54-31, EA 6-54-27, AND EA 6-54-29. 2 H 7 2 4T RT A13NM 2001102200054 20011022 00054 NM 2001 10 22 QXEA0101680 1 20011011 A 5415 CLIP DHAV DHC8 DHC8* NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - LEFT HAND AFT NACELLE AND EXHAUST SHROUD SUPPORT BRACKETS, CLIPS, AND ATTACH POINTS ARE CRACKED AND CHAFED. REPAI RED IAW RD 8/4 54-033, RD 8/4 54-044, RD 8/4 54-019, RD 8/4 54-016, EA 6-54-30, EA 6-54-28, EA 6-54-42, EA 6-54-26, EA 6 -54-25. 2 H 7 2 4T RT A13NM 2001102200055 20011022 00055 NM 2001 10 22 QXEA0101681 1 20011012 A 7110 COWL DOOR DHAV DHC8 DHC8* NM NR 2 ENGINE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - NR 2 ENGINE FORWARD COWL DOOR ON THE OUTBOARD SIDE IS CHAFED AT RAIN GUTTER. REPAIRED IAW HORIZON AIR EA 6-71-16. 2 H 7 2 4T RT A13NM 2001102200056 20011022 00056 NM 2001 10 22 QXEA0101682 1 20011012 A 7110 COWL DOOR DHAV DHC8 DHC8* NM NR 1 ENGINE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - NR 1 ENGINE FORWARD COWL DOOR, 412AR, IS CHAFED ON THE COMPOSITE RAIN GUTTER. REPAIRED IAW HORIZON AIR EA 6-71-16 . 2 H 7 2 4T RT A13NM 2001102200057 20011022 00057 EU 2001 10 22 QXEA0101683 1 20011017 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 497US 8887 4487 11173 BOI - EMERGENCY EXIT SIGN IS INOPERABLE AT FORWARD ROW. REMOVED AND REPLACED EMERGENCY EXIT SIGN. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001102200058 20011022 00058 NM 2001 10 22 QXEA0101684 1 20011014 A 5412 FIREWALL DHAV DHC8 DHC8102 2809003 NM NR 2 NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 828PH 287 PDX - NR 2 ENGINE NACELLE FIREWALL HAS A CRACK ABOVE THE TWO ATTACH RIVETS THROUGH THE INBOARD WALL OF THE CLOSING MEMBE R. REPAIRED IAW RD 8-54-109. 2 H 7 2 4T RT A13NM 2001102200059 20011022 00059 NM 2001 10 22 QXEA0101685 1 20011013 A 1430 RIVET DHAV DHC8 DHC8102 2809003 NM NR 1 NACELLE LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 828PH 287 PDX - ONE LOOSE RIVET AT FORWARD NR 1 NACELLE, RIGHT-HAND SIDE, LOWER EDGE OF HORSE COLLAR COWL MATING FLANGE. REPAIRED IAW 51-40-00. 2 H 7 2 4T RT A13NM 2001102200061 20011022 00061 WP 2001 10 22 SABA011054 2 20011016 A 7320 SCREW BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UAR 01514 WP RT ENGINE OUT OF ADJ A SABA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 33 961AE 961 AIRCRAFT 961 ON FLIGHT 5067 FROM CHARLOTTE TO ATHENS GA, ABORTED TAKEOFF DUE TO RIGHT ENGINE MAKING ONLY 80 PERCENT TORQ UE. AIRCRAFT RETURNED TO GATE AND NO EMERGENCY PROCEDURE WAS USED. MAINTENANCE ADJUSTED THE RIGHT ENGINE X SCREW AND P ERFORMED A POWER RUN. GROUND RUN AND OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A56EU E4WE 2001102200062 20011022 00062 NM 2001 10 22 SCNA01716 1 20010928 A 3350 BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 275AF 22092 RIGHT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. CORRECTED BY REPLACING BATTERY PACK. 2 L 7 3 4F A3WE 2001102200063 20011022 00063 NM 2001 10 22 SCNA01717 1 20010917 A 3350 LIGHT BOEING 727 727259 138408J NM EXTERIOR INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 EXTERIOR EMERGENCY LIGHT ADJACENT TO L-1 DOOR DOES NOT WORK. CORRECTED BY RELAMPING LIGHT. 2 L 7 3 4F A3WE 2001102200064 20011022 00064 NM 2001 10 22 SCNA01718 1 20010917 A 3350 BATTERY PACK BOEING 727 727259 138408J NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 CENTER AISLE EMERGENCY EXIT LIGHT IN FWD OVERWING BULL NOSE WILL NOT STAY ILLUMINATED. CORRECTED BY REPLACING LIGHT BAT TERY PACK. 2 L 7 3 4F A3WE 2001102200065 20011022 00065 NM 2001 10 22 SCNA01719 1 20011006 A 5270 WARNING LIGHT BOEING 737 7378Q8 13844BX NM COCKPIT FALSE INDICATION A SCNA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 15 800SY 30627 ON TAKEOFF RIGHT FWD OVERWING AND RIGHT AFT OVERWING LIGHT ILLUMINATED ALONG WITH MASTER CAUTION. CORRECTED BY RESETTIN G CIRCUIT BREAKER, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2001102200066 20011022 00066 NM 2001 10 22 SCNA01721 1 20011016 A 3350 LIGHT BOEING 727 727259 138408J NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 AFT CABIN EMERGENCY LIGHT FLOOR TRACK INOPERATIVE. CORRECTED BY REPLACING DAMAGED POWER STRIP. 2 L 7 3 4F A3WE 2001102200067 20011022 00067 NM 2001 10 22 SCNA01722 1 20011008 A 3350 BATTERY BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 284SC 21438 OVERHEAD EMERGENCY LIGHT AT BOTTOM OF AIRSTAIR INOP. FOUND DURING LINE CHECK. CORRECTED BY REMOVING AND REPLACING BATT ERIES. 2 L 7 3 4F RT A3WE 2001102200068 20011022 00068 NM 2001 10 22 SROM200100024 1 20010606 A 3350 362624 LIGHT BOEING 737 737205 NM CABIN CONTAMINATED C SROM K NONE L NO TEST IN INSP/MAINT 1 AL 03 733PA 7 23466 DURING CABIN PREFLIGHT FOUND EMERGENCY TRACK LIGHTS IN FORWARD CABIN INOP. FOUND WATER PUDDLE IN TRACK LIGHT CHANNEL. DRIED AREA. EMERGENCY EXIT LIGHTS OPS CHECKED NORMAL. 2 L 7 2 4F A16WE 2001102200069 20011022 00069 NM 2001 10 22 SWAA012799 1 20011014 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 642WN 27715 EEPLS INOP FROM ROW 16 TO ROW 18. RECONNECTED WIRES PER MM. 2 L 7 2 4F RT A16WE 2001102200070 20011022 00070 NM 2001 10 22 SWAA012800 1 20011014 A 3244 2606671 TIRE BOEING 737 7373H4 1384600 NM RT MLG BLOWN A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 378SW 26585 DECLARED EMERGENCY NR 3 MLG TIRE BLEW ON T/O. FOUND DAMAGE TO RT INBOARD AFT FLAP AND NR 5 GROUND SPOILER. REMOVED AND REPLACED NR 3 & 4 MLG TIRE AND WHEEL ASSY'S. REMOVED AND REPLACED RT INBOARD AFT FLAP AND NR 5 GROUND SPOILER PER MM. 2 L 7 2 4F RT A16WE 2001102200071 20011022 00071 NM 2001 10 22 SWAA012802 1 20011013 A 3397 65C27093 WIRE BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 522SW 26564 DURING SCHEDULED D-CHECK, FOUND FWD SVC DOOR EMERGENCY EXIT LIGHT INOP. REPAIRED BROKEN WIRE PER MM. 2 L 7 2 4F RT A16WE 2001102200072 20011022 00072 NM 2001 10 22 SWAA012803 1 20011011 A 3350 1330122 BATTERY BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 724SW 27856 DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT MID CABIN LT SIDE. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001102200073 20011022 00073 NM 2001 10 22 SWAA012804 1 20011013 A 3350 65C27093 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 522SW 26564 DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001102200074 20011022 00074 NM 2001 10 22 SWAA012805 1 20011013 A 3350 300432 BALLAST BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 783SW 29809 DURING SCHEDULED C3 CHECK, FOUND LT OVERWING INTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BALLAST PER MM. 2 L 7 2 4F RT A16WE 2001102200075 20011022 00075 2001 10 22 SWAA012806 4 20011012 A 2565 D31354 SLIDE BOEING 737 737317 138447P NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001102200076 20011022 00076 2001 10 22 SWAA012807 4 20011010 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2001102200077 20011022 00077 2001 10 22 SWAA012809 4 20011013 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 779SW 27884 AFT ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001102200078 20011022 00078 NE 2001 10 22 SWAA012815 2 20011013 A 7320 8063208 PMC BOEING 737 7373TO 138447G NM GE CFM56 CFM563B1 13802 NE NR 1 ENGINE ERRATIC A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 697SW 23838 AIR TURNBACK, DURING CLIMBOUT PASSING 10,000 FT, NR 1 ENG SURGED TO 107.9 PERCENT N1, EGT CLIMBED TO 930 DEGREES, ENG ST ABILIZED AT RETARDED THROTTLE, PMC LIGHT ON. BORESCOPE ACCOMPLISHED, NO DEFECTS NOTED PER MM. REMOVED AND REPLACED NR 1 ENG PMC PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2001102200079 20011022 00079 NM 2001 10 22 SWAA012819 1 20011014 A 3230 LANDING GEAR BOEING 737 7373Q8 1384670 NM NLG & MLG MALFUNCTIONED A SWAA K NONE J WARNING INDICATION CL CLIMB 1 SW 07 662SW 23255 DURING CLIMB WHEN MOVING GEAR HANDLE FROM UP TO OFF, GEAR STARTED TO EXTEND. RECYCLED HANDLE TO UP. ON APPROACH MOVED HANDLE FROM UP TO OFF AND GEAR REMAINED UP. INSPECTED LANDING GEAR SELECTOR VALVE. LANDING GEAR EXTENSION AND RETRACTI ON SYSTEM CHECKS NORMAL PER MM. 2 L 7 2 4F RT A16WE 2001102200080 20011022 00080 NM 2001 10 22 SWAA012820 1 20011014 A 5320 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (4 EA) AT BS 597, STR 7L & STR 8R, BS 767, STR 10L, BS 706, STR 1 0L. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001102200081 20011022 00081 NM 2001 10 22 SWAA012824 1 20011014 A 3350 610478 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED SERVICE CHECK, FOUND AFT RT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2001102200082 20011022 00082 2001 10 22 SWAA012826 4 20011014 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 089SW 22904 DURING SCHEDULED A1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLID E PER MM. 2 L 7 2 4F A16WE 2001102200083 20011022 00083 NM 2001 10 22 SWAA012827 1 20011014 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 525SW 26567 EEPLS LOOSE IN CABIN. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001102200084 20011022 00084 NM 2001 10 22 SWAA012829 1 20011014 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM COCKPIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 073SW 22673 DURING SCHEDULED RON CHECK, FOUND FLIGHT DECK EMERGENCY CEILING LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 2001102200085 20011022 00085 WP 2001 10 22 MWEA011402 1 20011017 A 3260 LATCH DOUG DC9 DC914 3022034 WP RIGHT MLG OUT OF ADJ A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 600ME 45725 WHEN RETRACTING THE GEAR, RIGHT MAIN LANDING GEAR UNSAFE LIGHT WOULD NOT EXTINGUISH. EXTENDED GEAR FOR LANDING, ALL INDI CATIONS NORMAL. -- ADJUSTED LEFT AND RIGHT MAIN LANDING GEAR LATCH MECHANISMS. 2 L 7 2 4F A6WE 2001103100072 20011031 00072 EU 2001 10 31 UPS01237043 2 20011014 A 7220 BULLET BOEING 727 72751C 1384015 NM RROYCE TAY TAY65154 EU NR 3 ENGINE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:S-10 ENGINE 3 SPINNER CRACK FOUND DURING SEG-10 CHECK. HAS 1 INCH CRACK AT BOLT HOLE. REMOVED AND REPL ACED NR 3 ENG SPINNER FAIRING IAW MM 72-30-10. OPS NORMAL AT THIS TIME. 2 L 7 3 4F 4 F A3WE E25NE 2001102200086 20011022 00086 NM 2001 10 22 UPS01237044 1 20011012 A 2611 SMOKE DETECTOR BOEING 727 72751C 1384015 NM CARGO BAY FAULTY A IPXA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE: LOWER CARGO SMOKE DETECTOR SYS MX LIGHT ILLUMINATED. REMOVED AND REPLACED TWO SMOKE DETECTORS REF MM 2 6/18/00 S/N IN FWD 11363 S/N OUT FWD 3740 S/N IN AFT 2356 S/N OUT AFT 5107. 2 L 7 3 4F A3WE 2001102200087 20011022 00087 NM 2001 10 22 UPS01237045 1 20011013 A 2560 CLIP BOEING 727 72751C 1384015 NM ENTRY DOOR DEFECTIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 903UP 18945 INSPECTION TYPE: MAIN ENTRY SLIDE INOP. REPLACED BOTH BAR RETAINER CLIPS, P/N 65-64828-3, REINSTALLED SLIDE. 2 L 7 3 4F A3WE 2001102200088 20011022 00088 NM 2001 10 22 UPS01237046 1 20011002 A 5414 PANEL BOEING 727 72762C 138402C NM NR 3 PYLON DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 913UP 19245 INSPECTION TYPE:C NR 3 PYLON PANEL NR 5501 HAS DELAMINATION AT O/B FWD CORNER. REPAIRED IAW SRM. 2 L 7 3 4F A3WE 2001102200089 20011022 00089 NM 2001 10 22 UPS01237051 1 20011004 A 3221 BEAM BOEING 727 72762C 138402C NM NLG CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 913UP 19245 INSPECTION TYPE:C SUSPECT CRACK IN NLG DRAGBRACE ATTACH FITTING SUPPORT BEAM IN RT AFT CORNER. REPLACEMENT OF NLG DRAGB RACE SUPPORT BEAM CARRIED OUT IAW UPS EO B72 7-5310-0943 & BOEING DRAWING 65C15724. 2 L 7 3 4F A3WE 2001102200090 20011022 00090 NM 2001 10 22 UPS01237063 1 20011002 A 2720 STRUCTURE BOEING 727 72762C 138402C NM RUDDER CONTROL CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 913UP 19245 INSPECTION TYPE:C SUSPECT CORROSION ON AFT RUDDER CONTROL QUADRANT. REPAIR CARRIED OUT IAW MM 27-20-71, 27-20-00 & DRW 65-20879. 2 L 7 3 4F A3WE 2001102200091 20011022 00091 NM 2001 10 22 UPS01237067 1 20010921 A 5312 PRESSURE PANEL BOEING 727 727173C 1384059 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C NWW PRESSURE CEILING IS CRACKED BETWEEN BS 270 - 273 RBL 14, CONFIRMED BY NDT. CUT OUT CRACK APPROX 4 X 1 INCH AT NWW PRESS CEILING BS 270 - 273 RBL 14 IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR ON NWW PRESS CEILING IAW B727 SRM 51-40-2. 2 L 7 3 4F A3WE 2001102200092 20011022 00092 NM 2001 10 22 UPS01237070 1 20011001 A 5414 PANEL BOEING 727 72762C 138402C NM NR 3 PYLON DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 913UP 19245 INSPECTION TYPE:C NR 3 PYLON PANEL 5508 ON LOWER SURFACE HAS DELAMINATION ON LOWER SKIN. REPAIRED IAW SRM 51-40-20. 2 L 7 3 4F A3WE 2001102200093 20011022 00093 NM 2001 10 22 UPS01237071 1 20011017 A 5414 ACCESS PANEL BOEING 727 72762C 138402C NM NR 1 PYLON DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 913UP 19245 INSPECTION TYPE:C NR 1 PYLON PANEL LOWER SURFACE ACCESS PANEL 5408 HAS DELAMINATION ON UPPER SURFACE. REPAIRED IAW SRM 51-40-20. 2 L 7 3 4F A3WE 2001102200094 20011022 00094 NM 2001 10 22 UPS01237073 1 20010915 A 5743 BEAM BOEING 727 727173C 1384059 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C NUMBER 3 FUEL TANK CRACK ON L/G SUPPORT BEAM AT WS 304. REPLACED BUSHING RT LANDING GEAR O/B END OF B EAM IAW SB 727-57-167. REMOVED AND REPLACED FWD AND AFT FITTINGS AT WS 304 LEFT GEAR SUPPORT BEAM AS PER B727 SRM 51-10 -2. PERFORMED HFEC INSP PER BOEING NDT MANUAL PART 6-51-01-00 FIG 11, NO CRACK FOUND. 2 L 7 3 4F A3WE 2001102200095 20011022 00095 NM 2001 10 22 USAABB01103 1 20011002 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 27122 PHL - FOUND FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE AT ROW 29. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2001102900105 20011029 00105 NM 2001 10 29 UPS01537054 1 20011016 A 2612 LIGHT BOEING 757 75724APF 1384969 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 403UP 23725 INSPECTION TYPE:PFLT LEFT ENGINE FIRE HANDLE LIGHTS INOP. RELAMPED HANDLE, OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 2001102200098 20011022 00098 WP 2001 10 22 UPS01837019 1 20011003 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 772.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001102200099 20011022 00099 WP 2001 10 22 UPS01837020 1 20011003 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 RIGHT WING L/E LOWER RIB IS CRACKED AT XFS 772.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001102200100 20011022 00100 NE 2001 10 22 MYW2001F00000 2 20010924 A 7200 577957 TUBE PWA BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE ENGINE NR 1 DAMAGED A MYWA A E J UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL M H OVER TEMP ELECT. POWER LOSS-50 PC TO TAKEOFF 1 SO 19 803MA 700278 22434 AFTER TAKEOFF AT APPROXIMATELY 1500 FT. THE NR 1 ENGINE FIRE WARNING (BOTTLE AND BELL) ACTIVATED. AOM EMERGENCY PROCEDU RES PER 2-C-2 COMPLIED WITH. DUMPED APPROXIMATELY 12000 POUNDS OF FUEL PER AOM PROCEDURE 2-A-B-1. RETURNED TO AIRPORT. PREPARED FOR 2 ENGINE FERRY PER MAI FORM 14 B/C AND MM 71-00 224C AND SUBSEQUENT. ACTION TAKEN: INSPECTED ENGINE, FOU ND 13 STAGE AIR TUBE RUPTURED CAUSING MELTING OF WIRE HARNESS. REMOVED AND REPLACED NR ENGINE IAW 727-7101 ENGINE CHANG E SHEETS. RUNUP COMPLETED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2001102200101 20011022 00101 WP 2001 10 22 UPS01837021 1 20011004 A 5730 576958929 DOUBLER DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 LEFT WING L/E INBOARD WRAP-AROUND DOUBLER IS CRACKED AT XFS 304. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769589, AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001102200102 20011022 00102 WP 2001 10 22 UPS01837022 1 20011002 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 LEFT WING L/E UPPER SKIN IS CRACKED AT XFS 638. REPAIRED SKIN IAW SRM 57-2-1 FIG 38. 2 L 7 4 4F RT 4A25 2001102200103 20011022 00103 WP 2001 10 22 UPS01837026 1 20011004 A 5720 97532937 ANGLE DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 NR 2 STUB WING VERTICAL ATTACH ANGLE IS CRACKED AT XS 250. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 9753293, AND SRM 51-1-20D, 51-3-0. 2 L 7 4 4F RT 4A25 2001102200104 20011022 00104 WP 2001 10 22 UPS01837027 1 20011004 A 5320 3750257U1 SPLICE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 STA 600-620 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257, AND S RM 51-1-20D, 51-3-0. 2 L 7 4 4F RT 4A25 2001102200105 20011022 00105 WP 2001 10 22 UPS01837029 1 20011003 A 5320 ANGLE DOUG DC8 DC873F 302199F WP COCKPIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C2,3 STA -99 PILOTS WINDOW FRAME HAS A CRACKED ANGLE AT FWD LOWER CORNER AFT OF SPLICE. REMOVED, FABRIC ATED, AND REPLACED ANGLE IAW SRM 53-2-3 FIG 3, 53-1-0. 2 L 7 4 4F RT 4A25 2001102200106 20011022 00106 WP 2001 10 22 UPS01837030 1 20011003 A 5730 36412572 DOUBLER DOUG DC8 DC873F 302199F WP RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 RIGHT WING L/E LOWER INTERNAL DOUBLER IS CORRODED BEYOND LIMITS BETWEEN XFS 722.25 TO XFS 735 (PANEL 518C). REMOVED AND REPLACED DOUBLER IAW DWG 3641257, AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001102200107 20011022 00107 WP 2001 10 22 UPS01837031 1 20011003 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 LEFT WING L/E LOWER SKIN HAS INTERGRANULAR CORROSION AT XFS 341. CUT OUT CORRODED AREA, FABRICATED DOUBLER AND FILLER APPROX SIZE 6 X 2.5 INCH. REPAIRED SKIN IAW EO DC8-5720-7767-A. 2 L 7 4 4F RT 4A25 2001102200108 20011022 00108 WP 2001 10 22 UPS01837032 1 20011004 A 5730 576958989 DOUBLER DOUG DC8 DC873F 302199F WP RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 RIGHT WING L/E STALL WARNING DOUBLER IS CORRODED BEYOND LIMITS AT XFS 373. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769589, AND SRM 51-1-21 APPROX SIZE 5 X 7 INCHES. 2 L 7 4 4F RT 4A25 2001102200109 20011022 00109 WP 2001 10 22 UPS01837033 1 20011003 A 5320 5772638118 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 STA 1766 LONG 10R AFT SIDE OF AFT PRESSURE BULKHEAD HAS TWO SEAL ANGLES CORRODED BEYOND LIMITS. REM OVED, FABRICATED, AND REPLACED ANGLES IAW DWG 5772638, AND SRM 51-1-20D, 51-3-0. 2 L 7 4 4F RT 4A25 2001102200111 20011022 00111 WP 2001 10 22 UPS01837035 1 20011011 A 7830 HEAT SHIELD DOUG DC8 DC871F 302199D WP NR 3 T/R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:IN NR 3 ENG RT TRUST REVERSER HALF STAINLESS SHIELD ON FWD FACE 4 O`CLOCK CRACKED AND PIECE MISSING. AC COMPLISHED EO DC-8 7830-15530-B. 2 L 7 4 4F RT 4A25 2001102200113 20011022 00113 WP 2001 10 22 UPS01837042 1 20011013 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:N/A CRACKS RT WING INBOARD OF INBOARD FUELING CAP (MARKED LOWER WING) BETWEEN NR 3 & 4 PYLON LWR WING) 2 8 INCHES FROM L/E & 3 INCHES FROM ACCESS PNL 1206. HFEC VERIFIED CRACK-CRACK TERMINUS CENTER PUNCH MARKED EP QC 70100 1 0-13-01. COMPLIED WITH EO DC8-5720-4087-B PERFORMED INTERIM REPAIR. 2 L 7 4 4F RT 4A25 2001102200114 20011022 00114 WP 2001 10 22 UPS01837059 1 20010926 A 5720 FITTING DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:SV LT WING NR 2 ALT STRINGER 51 END FITTING ON O/B SIDE IS CRACKED. PERFORMED HFEC INSPECTION TO VERIFY CRACK IAW DAC NDT SPM 060101. REMOVED CRACKED FITTING. LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24 AND DAC DW G 5613423. INSTALLED IAW DC8 SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 2001102200116 20011022 00116 WP 2001 10 22 UPS01837060 1 20010926 A 5720 FITTING DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:SV LT WING NR 2 MAIN STRINGER 51 AFT I/B STRINGER END FITTING IS CRACKED. PERFORMED HFEC INSPECTION TO VERIFY CRACK IAW DAC NDT SPM 06-10-01-0 01. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 2001102200117 20011022 00117 NM 2001 10 22 AWXA200100528 1 20010928 A 5330 654577518 SKIN BOEING 737 73733A 1384673 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - C18 CK - "C" - CRACK FOUND AT L2 DOOR UPPER HINGE CUTOUT, .300 LONG AT BS 960, STR 11L, WL 252. MAINTENANCE PERFOR MED REPAIR IAW B737 SRM 53-60-01, FIG 205, PG 210 - 212. 2 L 7 2 4F RT A16WE 2001102200118 20011022 00118 NM 2001 10 22 AWXA200100531 1 20011002 A 5313 6545800122 STRINGER BOEING 737 73733A 1384673 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - C18 CK - "C" - CORROSION FOUND ON STR 28R, BS 320 TO 323, JUST FWD OF MAIN E&E COMPARTMENT DOOR, BEYOND SRM LIMITS AFTER CLEAN UP. MAINTENANCE REMOVED DAMAGED SECTION OF STRINGER, FABRICATED REPAIR PARTS AND INSTALLED. REFERENCE B737 SRM 51-40-02, PG 4 - 6, 53-00-07, FIG 201, PG 202 - 203, AND BOEING DWG's 65-45800-122, 65-45800, PG 58 AND 69-37258. 2 L 7 2 4F RT A16WE 2001102200119 20011022 00119 NM 2001 10 22 AWXA200100533 1 20011001 A 5312 65163007 WEB BOEING 737 73733A 1384673 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - C18 CK - "C" - CRACK FOUND ON FWD PRESS. BULKHEAD AT BS 178, RBL .7, WL 188, 1.375" LONG. MAINTENANCE CUT OUT DAMA GED AREA, FABRICATED REPAIR FILLER AND DOUBLER AND INSTALLED IAW B737 SRM 53-10-08, FIG 203, PG 210 - 215. 2 L 7 2 4F RT A16WE 2001102200120 20011022 00120 WP 2001 10 22 UPS01837061 1 20010926 A 5720 FITTING DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:SV LT WING NR 2 ALT STRINGER 51 END FITTING ON O/B SIDE IS CRACKED. PERFORMED HFEC INSPECTION TO VERIFY CRACK IAW DAC NDT SPM 06-10-01-0 01. REMOVED AND RPLACED FITTING IAW DC8 SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 2001102200121 20011022 00121 WP 2001 10 22 UPS01837062 1 20010926 A 5720 FITTING DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:SV LT WING NR 2 MAIN STRINGER 51 FWD I/B SIDE HAS A CRACKED STRINGER END FITTING. PERFORMED HFEC TO VER IFY CRACK IAW DAC NDT SPM 06-10-01-001. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 2001102200122 20011022 00122 NM 2001 10 22 VNAA0109014 1 20010924 A 3310 329630 CONTROL BOX DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FAILED A VNAA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 424JS 11097 3033 THE CARGO FAIL CAS MESSAGE AND THE RED CARGO FIRE BUTTON CAME ON INTERMITTENTLY. MAINTENANCE INSPECTED AND REPLACED THE DIMMER BOX IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001102200123 20011022 00123 NM 2001 10 22 VNAA0110002 1 20011005 A 7332 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT ACTIVATED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 431JS 3028 AFTER TAKEOFF, THE CREW WAS CROSS FEEDING THE FUEL SYSTEM AND RECEIVED A FUEL PRESSURE LOW CAS MESSAGE. THE CREW RECYCL ED THE FUEL CROSS FEED. AT THAT TIME THE CREW RECEIVED A FUEL PRESSURE LOW ON BOTH ENGINES AND VALVES INDICATED CLOSED. THE CAPTAIN SHUT OFF THE CROSS FEED AND CALLED MAINTENANCE CONTROL. MAINTENANCE CONTROL ADVISED THE CREW TO RETURN TO PIT. UPON RETURN TO PIT, MAINTENANCE EXTENSIVELY TROUBLESHOT AND GROUND RAN THE AIRCRAFT AND FOUND NO DISCREPANCIES. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001102200124 20011022 00124 NM 2001 10 22 VNAA0110003 1 20011006 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 429JS 13376 110 3043 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 4 THROUGH 7 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPL ACED THE EMERGENCY BATTERY AT THE 5LK POSITION IAW DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORM ED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001102200125 20011022 00125 NM 2001 10 22 VNAA0110004 1 20011007 A 2120 ODOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DETECTED A VNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 436JS 3052 THE APU WAS RUNNING AND THE FLIGHT ATTENDANT REPORTED SMELLING SMOKE. MAINTENANCE INSPECTED THE AIRCRAFT AND COULD NOT DUPLICATE OR FIND ANY DISCREPANCIES. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001102200126 20011022 00126 NM 2001 10 22 VNAA0110005 1 20011009 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 432JS 12324 3045 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS EIGHT AND NINE WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND R EPLACED THE EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001102200127 20011022 00127 NM 2001 10 22 VNAA0110007 1 20011010 A 2400 230GC02Y02 PANEL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 458PS 10214 3068 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND GENERATOR FAIL CAS MESSAGE AND ABORTED TAKEOFF. MAINTENANCE WAS SENT TO L EX AND FOUND NO DISCREPANCIES. THE AIRCRAFT WAS FERRIED TO PIT WHERE MAINTENANCE INSPECTED AND REPLACED THE 1VE PANEL I N ACCORDANCE WITH 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001102200128 20011022 00128 NM 2001 10 22 VNAA0110009 1 20011014 A 3010 001B574A1000006 BOOT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT WING FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 441JS 15457 3059 DURING CLIMBOUT, THE LEFT HAND INBOARD DE-ICE BOOT FAILED AND FLIGHT 4075 RETURNED TO PIT. MAINTENANCE INSPECTED AND RE PLACED THE LEADING EDGE ASSEMBLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-00-00. OPERATIONAL CHECKS WERE PERFOR MED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001102200129 20011022 00129 NM 2001 10 22 VNAA0110010 1 20011014 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 423JS 11154 3032 THE CREW REPORTED THAT THE EMERGENCY LIGHTING WAS NOT ILLUMINATING AT ROWS 6 THROUGH 9 ON ENGINE START UP. MAINTENANCE INSPECTED AND REPLACED THE 6LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CH ECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001102200130 20011022 00130 2001 10 22 VNAA0110011 4 20011016 A 3418 STALL WARNING DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 426JS 3038 DURING THE TAKEOFF ROLL, THE CREW RECEIVED AN ANGLE OF ATTACK CHIME AND FAILURE. ABORTED THE TAKEOFF. AS FLIGHT 4138 C LEARED THE RUNWAY THE MESSAGE CLEARED. THE CREW CONTACTED MAINTENANCE CONTROL AND WAS CLEARED FOR ANOTHER TAKEOFF ATTEM PT. FLIGHT 4138 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001102200131 20011022 00131 NM 2001 10 22 VNAA0110012 1 20011017 A 5270 PROXIMITY SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE PAX DOOR OUT OF ADJ A VNAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 07 427JS 3039 WHILE EN ROUTE FROM TYS TO PHL, THE CREW RECEIVED A MAIN CABIN DOOR LIGHT ON THE RED WARNING PANEL. THE CREW DECLARED A N EMERGENCY AND DIVERTED TO TRI. OUTSTATION DETERMINED THE PROBLEM WAS DUE TO THE MAIN CABIN DOOR OVER CENTER PROXI SE NSOR. THE AIRCRAFT WAS FERRIED TO PIT WHERE MAINTENANCE INSPECTED AND ADJUSTED THE MAIN CABIN DOOR OVER C ENTER PROXI S ENSOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RE LEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001102200132 20011022 00132 EU 2001 10 22 XN0A01024 1 20010920 A 3230 UPLOCK AIRBUS 300 A300B4203 3930306 EU NLG OUT OF ADJ A XN0A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 472AS 125 NOSE GEAR DOOR LIGHT ILLUMINATED AFTER TAKEOFF WHEN GEAR RETRACT. INSPECTED NOSE GEAR DOORS, FOUND NO DAMAGE. INSPECTE D NOSE GEAR DOOR UPLOCK ASSY AND MECHANISM, FOUND OUT OF ADJUSTMENT. ADJUSTED NOSE GEAR DOOR UPLOCK ASSY IAW A300 MM 32 -30-00 AND FREEFALL TEST IAW A300 MM 32-30-00. ALL TESTS FUNCTIONALLY AND OPERATIONALLY CHECK NORMAL. 2 L 7 2 4F RT A35EU 2001102200133 20011022 00133 SO 2001 10 22 COMA0110151 1 20010926 A 3350 LIGHT EMB 120 EMB120RT SO A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 268CA 120262 FLIGHT #5057. DURING INSPECTION; FOUND THE EMERGENCY EXIT SIGN ON OVERHEAD BIN INOPERATIVE.REPAIRED WIRING AT THE EMERG ENCY EXIT SIGN ASSEMBLY. 2 L 7 2 4T RT A31SO 2001102200134 20011022 00134 EA 2001 10 22 COMA0160826 1 20011020 A 5551 600210617 BUSHING CNDAIR CL600 CL6002B19 EA VERT STABILIZER WORN A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 933CA 17158 7040 L/H VERTICAL STABILIZER BUSHING P/N 600-21061-7 IS WORN.REMOVED THE WORN BUSHING I/A/W CRJ AMM CH 20-26-00-910-802, FABR ICATED NEW BUSHING P/N 601R55-31-033-1 I/A/W REO 601R-55-31-033 AND INSTALLED THE BUSHING I/A/W REO 601R-55-31-002. 2 L 7 2 4F RT A21EA 2001102200135 20011022 00135 EA 2001 10 22 COMA0160827 1 20011018 A 2720 9960013 TRIM SWITCH CNDAIR CL600 CL6002B19 EA COCKPIT FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 796CA 7338 FLIGHT #5280. DURING CRUSIE FLIGHT DESTINATION CVG, THE STABILIZER AND MACH. TRIM CAUTION MESSAGES ACTIVATED, CREW DECL ARED AN EMERGENCY AND DIVERTED TO PIT.REPLACED THE CAPTIANS PITCH TRIM SWITCH. 2 L 7 2 4F RT A21EA 2001102200136 20011022 00136 EU 2001 10 22 XN0A01025 1 20010921 A 3230 UPLOCK AIRBUS 300 A300B4203 3930306 EU NLG OUT OF ADJ A XN0A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 472AS 125 NOSE DOOR AMBER LIGHT REMAINED ON AFTER GEAR RETRACTION AND NOSE DOOR OPENED UP AT GEAR NEUTRAL. ADJUSTED NLG RT FWD DO OR UPLOCK ASSEMBLY IAW A300 MM 32-22-11 LANDING GEAR SWING C/W IAW A300 32-30-00, OPS CHECK GOOD. 2 L 7 2 4F RT A35EU 2001102200137 20011022 00137 EU 2001 10 22 XN0A01026 1 20011016 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU COCKPIT DIRTY A XN0A C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 23 372PC 196 ON TAKEOFF ROLL AT 80 KTS, FLT DECK SMOKE LIGHTS AND CHIME CAME ON. TAKEOFF ABORTED. CLEANED FLT DECK SMOKE DET C/P, O PS CHECK NORMAL IAW A300 MM 26-11-00. 2 L 7 2 4F RT A35EU 2001102200138 20011022 00138 EU 2001 10 22 YENA200102 1 20010607 A 5610 STA320171A WINDSHIELD AIRBUS 320 A320232 3930326 EU COCKPIT CRACKED A YENA K NONE O OTHER CR CRUISE 1 EA 15 517JB 2320 2320 1327 BEFORE DESCENT FLT 43, JFK TO MCO, AT 39,000 FT, FLIGHT CREW REPORTED CRACKED CAPTAIN'S FRONT WINDSHIELD. REMOVED AND R EPLACED CAPT WINDSHIELD PER AMM 56-11-11-000001 AND OPS CHECKED OK PER AMM 56-11-11-501. 2 L 7 2 4F RT A28NM 2001102200139 20011022 00139 EU 2001 10 22 YENA200103 1 20010709 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN FAULTY A YENA K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 15 517JB 1327 ON DAILY MAINTENANCE CHECK EPSU FWD LEFT FAULT. REMOVED AND REPLACED EPSU UNIT IAW AMM 33-51-38. OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 2001102200140 20011022 00140 WP 2001 10 22 ZW0A0109301 1 20011003 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP L1 DOOR DEFECTIVE A ZW0A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 13 971TW 53621 THE LEFT SIDE NUMBER 1 CABIN DOOR EMERGENCY EXIT LIGHT WOULD NOT EXTINGUISH AFTER ENGINE START. REPLACED THE LIGHT ASSE MBLY. CHECK-C 7-20-01 STL. 2 L 7 2 4F RT A6WE 2001102200141 20011022 00141 NM 2001 10 22 ZW0A0109402 1 20011004 A 3397 WIRE BOEING 767 7673Q8 NM CABIN DISCONNECTED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 634TW 28132 FOUND EGRESS LIGHT MALFUNCTIONS ON LT SIDE OF FIRST CLASS ONE LAMP, RT SIDE OF CABIN ROW 16 TO 22, AND RT SIDE OF CABIN ROW 24 TO 27. FOUND FIRST CLASS LAMP OK. RECONNECTED WIRING FOR ROW 16 TO 22 AND FOR ROW 24 TO 27. 2 L 7 2 4F RT A1NM 2001102200142 20011022 00142 WP 2001 10 22 ZW0A0109501 1 20011008 A 5320 BRACKET DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 905TW 49157 DURING CHECK-C MAINT FOUND BRACKET CRACKED AT STA 1485, 18 INCHES RBL, JUST FWD OF RUDDER TRIM CABLE SPOOL BRACKET. FAB RICATED AND INSTALLED REPLACEMENT BRACKET PER SRM 53-14-4. 2 L 7 2 4F A6WE 2001102200143 20011022 00143 WP 2001 10 22 ZW0A0109602 1 20011015 A 3350 408822101 BATTERY DOUG DC9 DC982 3022082 WP A/C BAY DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 923TW 49379 THE EMERGENCY LIGHTS IN THE TAIL COMPT FOR CHUTE AND CAT WALK WERE INOPERATIVE. REPLACED THE BATTERIES IN THE POWER PAC K. CHECK-C 8-10-01 MCI. 2 L 7 2 4F A6WE 2001102200144 20011022 00144 WP 2001 10 22 ZW0A0109701 1 20011016 A 3350 408822101 BATTERY DOUG DC9 DC983 3022083 WP COCKPIT DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 9627R 53597 BOTH COCKPIT EMERGENCY LIGHTS FAILED TO ILLUMINATE. TIGHTENED WIRE TERMINAL AT B5-23 AND REPLACED THE BATTERIES IN THE POWER SUPPLY. 2 L 7 2 4F RT A6WE 2001102200145 20011022 00145 WP 2001 10 22 ABXA010537 1 20011003 A 5313 LONGERON DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX 47494 LONGERON 17 RIGHT WAS CRACKED AT FASTENERS AT FS 389. REPLACED LONGERON AT STATION 380 - 430, IAW DC-9 SRM 5302. 2 L 7 2 4F A6WE 2001102300001 20011023 00001 WP 2001 10 23 DHL2001801500 1 20011001 A 5315 ANGLE DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 # 6 FLOOR PANEL REINFOCING ANGLE CRACKED 1 IN. FROM STA 1700.000 TO 1766.000STOP DRILLED CRACK PER SRM 53-2-0 FIG 1B.FAB RICATED REINFOCING ANGLE (2024 T3 0.040) PER SRM 53-2-0 FIG 1 B.CLEAND TREATED AND PRIMED PER SRM 51-1-8B.INSTALLED REIN FOCING ANGLE PER SRM 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 2001102300002 20011023 00002 WP 2001 10 23 DHL2001801505 1 20011003 A 5340 3750257U1 FITTING DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AFT CARGO COMPT-SPLICE FITTING 2 IN CRACKED , BETWEEN STA 1040.000 AND STA 1060 , L31R.REMOVED CRACKED FITTING PER SRM 5 1-120D PG 21.CLEANED, TREATED AND PRINED PER SRM 51-1-20B.INSTALLED NEW FITTING PER SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2001102300047 20011023 00047 NM 2001 10 23 CALA0100964 1 20011022 A 5320 BAC1496364 PANEL BOEING 737 7373T0 1384582 NM STA420-440 RT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69333 23571 TRANSITION PANEL CORRODED AT BS 420 - 440 RIGHT. FABRICATED AND INSTALLED TRANSITION PANEL PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001102300048 20011023 00048 NM 2001 10 23 CALA0100965 1 20011022 A 5340 2024T3 SKIN BOEING 737 7373T0 1384582 NM L2 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69333 23571 L2 DOOR SKIN CRACKED AT UPPER HINGE CUT OUT (5/16"). REPAIRED PER SRM 52-00-01. 2 L 7 2 4F RT A16WE 2001102300049 20011023 00049 WP 2001 10 23 AT0100232 1 20011016 A 3350 AD4002P BATTERY DOUG DC9 DC932 3022066 WP MID CABIN DISCHARGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 811AT 47285 FOUND PASSENGER CABIN EMERGENCY LIGHTS INOPERATIVE AT AT ROW 10-15. CORRECTIVE ACTION: REMOVED AND REPLA CED NICAD BATTERIES. IAW DC9 MM33-50 2 L 7 2 4F A6WE 2001102300050 20011023 00050 WP 2001 10 23 MWEA011404 1 20011022 A 5310 59203235 LONGERON DOUG DC9 DC981 3022081 WP STATION 298 UNSERVICEABLE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 FORWARD CARGO BAY LONGERON 21 RIGHT HAS PREVIOUS REPAIR ON UPPER FLANGE BETWEEN STATION 298 THROUGH 303. -- FABRICATED AND INSTALLED REPAIR SPLICE SECTIONS. 2 L 7 2 4F A6WE 2001102300051 20011023 00051 WP 2001 10 23 MWEA011405 1 20011022 A 5330 592480295 SKIN DOUG DC9 DC981 3022081 WP STATION 237 GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 FUSELAGE SKIN GOUGED AT APPROXIMATELY LONGERON 15 LEFT AND AT STATION 237. -- FABRICATED AND INSTALLED REPAIR DOUBLER AND SHIMS. REPAIR PUT ON WATCH ITEM #6274 FOR EXTERNAL VISUAL INSPECTION. 2 L 7 2 4F A6WE 2001102300053 20011023 00053 NM 2001 10 23 0103536743 1 20011010 A 3040 CONTROLLER BOEING 747 747249F 1384849 NM COCKPIT FAILED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 643NW 22245 DURING CLIMB, AN ELECTRICAL BURNING SMELL EMITTED IN THE COCKPIT. AIRCRAFT DIVERTED TO NRT AND LANDED WITHOUT INCIDENT. REPLACED THE R1 WINDOW HEAT CONTROLLER, R1 WINDOW, APU BATTERY CHARGER, AND CLEANED AN INSTRUMENT COOLING DUCT. OPERA TIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2001102300055 20011023 00055 WP 2001 10 23 01FDEA00895 1 20011017 A 5320 GUIDE DOUG DC10 DC1030 3023501 WP CARGO BAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 303FE 46802 N 56 LEVEL CORROSION IN FWD CARGO PIT ON LEFT HAND CARGO GUIDE RAIL. 2 L 7 3 4F A22WE 2001102300056 20011023 00056 EU 2001 10 23 01FDEA00896 1 20011018 A 3230 LANDING GEAR AIRBUS 310 A310203 EU LANDING GEAR MALFUNCTIONED A FDEA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 413FE 397 01-342 LANDING GEAR DID NOT LEAVE THE WELLS. 2 L 7 2 4F RT A35EU 2001102300057 20011023 00057 NM 2001 10 23 01FDEA00899 1 20011021 A 2780 S207 SWITCH BOEING 727 727 UTILSYS NM FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 205FE 22927 01-344 #6 L/E FLAP INDICATING IN TRANSIT AFTER RETRACTION. AIR RETURN. ** S/D ** COMING 2 L 7 3 4J RT A3WE 2001102300058 20011023 00058 NM 2001 10 23 01FDEA00901 1 20011022 A 2432 BATTERY DOUG MD11 MD11F 3023600 NM FAILED A FDEA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 25 614FE 48528 01-346 AFTER T/O 1 BAT CHARGING ANNUNCIATED. BATTERY DISCHARGED. VOLTAGE DROPPED. ** S/D ** COMING 2 L 7 3 4F RT A22WE 2001102300059 20011023 00059 NM 2001 10 23 01FDEA00903 1 20011021 A 5313 CLIP BOEING 727 727233 138408A NM FUSELAGE TOP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 282FE 22349 N 1043 STRINGER TIE CLIP CRACKED AT BS 680, STR 4L. R&R CLIP PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2001102300060 20011023 00060 NM 2001 10 23 01FDEA00904 1 20011021 A 5312 SEAL BOEING 727 727233 138408A NM FUSELAGE TOP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 282FE 22349 N 519 DITCHING SEAL CRACKED AT BS 1183, LBL 48, WL 208.1. R&R SEAL PER SRM 51-40-8. 2 L 7 3 4F RT A3WE 2001102300061 20011023 00061 NM 2001 10 23 01FDEA00905 1 20011021 A 5313 CLIP BOEING 727 727233 138408A NM FUSELAGE TOP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 282FE 22349 N 482 STRINGER TIE CLIP CRACKED AT BS 480, STR 2R. R&R CLIP PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2001102300062 20011023 00062 NM 2001 10 23 01FDEA00906 1 20011021 A 5720 CHANNEL BOEING 727 727233 138408A NM LEFT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 282FE 22349 N 345 CHANNEL CRACKED ON LEFT WING BS 425, WL 357. R&R CHANNEL PER SRM 51-30-2 2 L 7 3 4F RT A3WE 2001102300063 20011023 00063 NM 2001 10 23 01FDEA00908 1 20011021 A 5313 CLIP BOEING 727 727233 138408A NM FUSELAGE TOP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 282FE 22349 N 1042 STR TIE CLIP CRACKED BS 660 AT STR 6L. R&R CLIP PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2001102300065 20011023 00065 WP 2001 10 23 ABXA010540 1 20011019 A 3350 5708458503 BATTERY DOUG DC8 DC863 302198A WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 817AX 45928 DURING MAINTENANCE PRE-DEPARTURE INSPECTION, FOUND THE COCKPIT AND CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED THE RAC K ASSEMBLY BATTERY EMERGENCY LIGHT IAW AMM 33-50-02. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 2001102300066 20011023 00066 NM 2001 10 23 ANCF200100015 1 20010929 A 7711 TRANSMITTER BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE FAILED W ANCF A UNSCHED LANDING O OTHER CL CLIMB 1 SO 23 321LF 26269 30856 LT ENGINE PARAMETERS FLUCTUATED AT TAKEOFF AND CLIMB. CREW DECIDED TO RETURN TO EDR. THE EPR TRANSMITTER LT ENGINE WAS REPLACED IAW AMM 77-11-00, REPLACED LT ENGINE IAW EWO 75-72-43-77 TEST SATISFACTORY IAW AMM 71-00-00 PAGE 404. 2 L 7 2 4F 4 F RT A2NM E12EU 2001102300067 20011023 00067 NM 2001 10 23 ANCF200100017 1 20011006 A 2722 3800022105 ACTUATOR BOEING 757 757236 NM RROYCE RB211 RB211535C37 54555 NE RUDDER FAILED W ANCF A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 23 227AN 23227 RUDDER RATIO LIGHT ILLUMINATED IN FLIGHT. EICAS MESSAGE RUDDER RATIO DISPLAYED, CREW DECIDED TO RETURN TO EDR. ACCOMPL ISHED FIM 27-09-00, WAS REPLACED RUDDER RATIO CHANGER ACTUATOR IAW AMM 27-21-13 PAGE 209, TEST OK IAW AMM 27-21-00 PAGE 501. 2 L 7 2 4F 4 F RT A2NM E12EU 2001102300068 20011023 00068 WP 2001 10 23 ANCF200100018 1 20011011 A 3246 WHEEL DOUG DC9 DC983 3022083 WP LT MLG FAILED W ANCF O OTHER J WARNING INDICATION LD LANDING 1 SO 23 593AN 195 53093 LANDING AT CALI DURING TOUCH DOWN, THE WHEEL NOT TURNING LIGHT FLASHED. LANDING SEQUENCE WAS ACCOMPLISHED SMOOTHLY. AS PRECAUTIONARY MEASURE THE PLANE WAS BROUGHT TO FULL STOP AT THE END OF RUNWAY FINDING THAT THE LEFT OUTER MAIN WHEEL HA D BLOWN UP. THE RUNWAY WAS BLOCKED FOR FOUR HOURS DUE TO AIRCRAFT WHEEL DAMAGE. WHEEL HUB SHAFT COUPLING WAS FOUND BRO KEN AND BRAKE DISK DEFORMED 60 DEGREES IN THE BORDER. MAIN WHEELS AND BRAKES NR 1 AND 2 WERE REPLACED IAW AMM 32-40-01 PAGE 201 AND 32-42-01 PAGE 201. 2 L 7 2 4F RT A6WE 2001102300069 20011023 00069 NM 2001 10 23 ANCF200100020 1 20011018 A 5230 SEAL BOEING 757 757236 NM RROYCE RB211 RB211535C37 54555 NE CARGO DOOR OUT OF POSITION W ANCF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 951PG 22185 DURING TAKEOFF CARGO DOOR LIGHT CAME ON AFT CARGO DOOR NR 2. AIRPLANE DID NOT PRESSURIZE. CREW RETURNED TO CTG. REPOS ITIONED SEAL IN AFT CARGO DOOR FRAME IAW AMM 52-71-00. CHECKED ALL AFT DOOR FRAME, FOUND NORMAL. 2 L 7 2 4F 4 F RT A2NM E12EU 2001102300070 20011023 00070 WP 2001 10 23 ARWA0011007 1 20011012 A 7711 SENSE LINE DOUG DC8 DC862 3021970 WP NR 4 ENGINE BROKEN A ARWA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 19 8968U 46069 NR 4 ENGINE LOW N1, N2, FF, HIGH EGT. INSPECTED NR 4 ENGINE FOUND PT7 LINE BROKEN. REMOVED AND REPLACED PT7 LINE IAW MM 70-30-2, PERFORMED ENGINE RUN UP AND FOUND NORMAL IAW DC8 MM 71-00. 2 L 7 4 4F 4A25 2001102300072 20011023 00072 2001 10 23 ARWA0011008 4 20011016 A 3422 1783993304 INDICATOR DOUG DC8 DC862 3021970 WP COCKPIT INOPERATIVE A ARWA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 19 1804 45896 CAPTAIN COMPASS INOP, RETURNED TO KMIA. REMOVED AND REPLACED PICTORIAL DEVIATION INDICATOR IAW MM 34-00. PERFORMED OPE RATIONAL CHECK IAW 34-21-0, FOUND ALL SYSTEMS NORMAL. 2 L 7 4 4F 4A25 2001102300073 20011023 00073 SO 2001 10 23 C2XA01CL217 1 20011015 A 5240 LOCK EMB 145 EMB145LR SO SERVICE DOOR OUT OF ADJ A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 12967 145133 SDF FLIGHT 4072 THE CREW REPORTED THE SERVICE DOOR WAS JAMMED, WOULD NOT OPEN OR CLOSE. MAINTENANCE INSPECTED AND ADJUS TED THE SERVICE DOOR LOCKING MECHANISM. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001102300074 20011023 00074 SO 2001 10 23 C2XA01IA378 1 20011018 A 5540 12061385009 RUDDER EMB 145 EMB145LR SO TAIL DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14905 145476 ORF- DURING POSTFLIGHT THE CREW NOTED THAT RUDDER NR 2, AFT BOTTOM RIGHT SIDE HAS A 6 INCH BY 2 INCH HOLE. THE AIRCRAF T WAS RELEASED FOR FERRY FLIGHT FROM ORF TO IAH. MAINTENANCE REMOVED AND REPLACED RUDDER NR 2, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001102300077 20011023 00077 NM 2001 10 23 2001F00454 1 20010906 A 5210 DOOR BOEING 727 727231 1384079 NM L1 OUT OF ADJ A MYWA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 19 808MA 21988 ON TAKEOFF ROLL, FORWARD ENTRY L1 DOOR LIGHT CAME ON, HANDLE UNSEATED. ADJUSTED/TEST DOOR IAW MM 52-11-01. PRESSURIZED AIRCRAFT TO 1 PSI IAW MM 21-31-00. NO DOOR LIGHT, OPS CHECK SATISFACTORY. PERFORMED SPECIAL INSPECTION DUE HIGH SPEED ABORT 110 KNOTS, 150 LBS IAW MM 5-51-121, NO DISCREPANCIES NOTED. RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 3 4F A3WE 2001102300078 20011023 00078 NM 2001 10 23 2001F00455 1 20010822 A 3350 1102833 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 889MA 21854 DURING PREFLIGHT, TRANSIT EMERGENCY LIGHT ASSEMBLY AT SEAT ROW 28 CEILING INOPERATIVE. REMOVED AND REPLACED EMERGENCY L IGHT ASSEMBLY AT ROW 28. OPS CHECK OK IAW B727 33-50-1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001102300079 20011023 00079 2001 10 23 2001F00456 4 20010901 A 3460 FMC BOEING 737 737* NM COCKPIT MALFUNCTIONED A MYWA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SO 19 732MA 30618 RIGHT AFTER TAKEOFF IN A LEFT TURN EXPERIENCED A DUAL FMC FAILURE. BOTH SYSTEMS RETURNED TO NORMAL WHEN WINGS LEVEL. P ERFORMED BITE CHECK OF LEFT AND RIGHT FMC'S. NO FAULTS FOUND. SYSTEM OPS CHECK NORMAL ON GROUND. REF MM 34-61-00 AND FIM 34-61-00. RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001102300080 20011023 00080 NM 2001 10 23 2001F00457 1 20010819 A 2560 237702242 MEGAPHONE BOEING 727 727225 1384077 NM CABIN INOPERATIVE A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 804MA 22435 ON PREFLIGHT, TRANSIT FOUND AFT MEGAPHONE INOPERATIVE. REMOVED AND REPLACED AFT MEGAPHONE. OPS CHECKED IAW 25-60-00. RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 3 4F A3WE 2001102300081 20011023 00081 EU 2001 10 23 2001F00458 1 20010921 A 5347 7253721495 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 305AE 340B305 LAVATORY TRACK AND PROFILE ARE CORRODED. REMOVED AND REPLACED LAVATORY TRACK AND PROFILE IAW SAAB SRM 51-40-21. REF SI MA200126506. (M) 2 L 7 2 4T RT A52EU 2001102300082 20011023 00082 EU 2001 10 23 2001F00459 1 20010921 A 5347 7253799379 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 305AE 340B305 SBP - FOUND SEAT TRACK AT STATION 18.3 LEFT SIDE IS CORRODED AT FRONT SPLICE. REMOVED AND REPLACED SEAT TRACK AND U-BEA M IAW SAAB SRM 53-70-60. REF SIMA200126507. (M) 2 L 7 2 4T RT A52EU 2001102300083 20011023 00083 NM 2001 10 23 F3LA200100113 1 20011021 A 2120 DUCT BOEING 737 7372Y5 1384554 NM BROKEN A F3LA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 921WA 33 23039 ENROUTE FROM SAN TO DEN, FLIGHT CREW REPORTED CABIN SIDEWALL AT ROW 7 EXTREMELY HOT TO THE TOUCH AND AN OVERHEAT ODOR. AN EMERGENCY WAS DECLARED AND AIRCRAFT DIVERTED TO YUMA, AZ WITHOUT INCIDENT. AIRCRAFT WAS FERRIED TO PHX FOR REPAIR. MAINTENANCE REPLACED BROKEN BOOT IN MAIN DISTRIBUTION BAY. REPLACED BROKEN DUCT ON RT. SIDE OF CHRISTMAS TREE IN MAIN D ISTRIBUTION SYSTEM. INSTALLED NEW CLAMP ON RT. SIDE OF CONDENSER CAN, REPLACED WATER SEPARATOR BAG AND O-RINGS. REPLAC ED DAMAGED TUBING AT ROWS 7A AND 7F. RAN BOTH ENGINES AND PERFORMED PRESSURIZATION CHECK AND LEAK CHECK. SYSTEMS CHECK ED OKAY. 2 L 7 2 4U RT A16WE 2001102300084 20011023 00084 EU 2001 10 23 2001F00460 1 20010921 A 5347 7253799379 CARGO TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 305AE 340B305 SBP - FOUND CARGO SEAT TRACK AT STATION BL 0.0 IS CORRODED ON THE FLANGE AND WEB, SPLICED IN NEW SECTION OF TRACK 67.75 INCHES IAW SAAB SRM 53-70-60. REF SIMA200126509. (M) 2 L 7 2 4T RT A52EU 2001102300085 20011023 00085 NM 2001 10 23 2001F00461 1 20010821 A 3220 FITTING BOEING 727 72721 1384003 NM NLG CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 NOSE LANDING GEAR DRAG SUPPORT FITTING HAS CORROSION ON LOWER SURFACE. (M) 2 L 7 3 4F A3WE 2001102300086 20011023 00086 NM 2001 10 23 2001F00462 1 20010822 A 5311 FRAME BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FUSELAGE STATION 351 FRAME LOWER FLANGE INBOARD OF STRINGER 26R HAS CORROSION. (M) 2 L 7 3 4F A3WE 2001102300087 20011023 00087 NM 2001 10 23 2001F00463 1 20010822 A 5315 DOUBLER BOEING 727 72721 1384003 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 CABIN FUSELAGE STATION BS 480 STRINGER 17L LOWER FLOORBEAM ANGLE STRAP REPAIR CRACKED. (M) 2 L 7 3 4F A3WE 2001102300088 20011023 00088 NM 2001 10 23 2001F00464 1 20010911 A 5512 SKIN BOEING 727 72721 1384003 NM HORIZ STAB DAMAGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 RIGHT HORIZONTAL STABILIZER UPPER SURFACE SKIN DAMAGED AT INBOARD END AFT OF LEADING EDGE SKIN. (M) 2 L 7 3 4F A3WE 2001102300089 20011023 00089 NM 2001 10 23 2001F00465 1 20010825 A 5532 RUB STRIP BOEING 727 72721 1384003 NM VERTICAL STAB BULGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 VERTICAL STABILIZER UPPER FORWARD RUB STRIPS, FOR HORIZONTAL STABILIZER PATH, HAS BULGED AREAS ON BOTH RIGHT AND LEFT SI DES. (M) 2 L 7 3 4F A3WE 2001102300090 20011023 00090 NM 2001 10 23 2001F00466 1 20010726 A 5311 FRAME BOEING 727 72721 1384003 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 NOSE GEAR WHEEL SIDE PANEL LEFT SIDE FORWARD LOWER CHORD CRACKED AT WEB STATION 244.0. (M) 2 L 7 3 4F A3WE 2001102300091 20011023 00091 NM 2001 10 23 2001F00467 1 20010924 A 3350 10005511 LIGHT DHAV DHC8 DHC8103 1386005 NM COCKPIT INOPERATIVE A KPVA K NONE L NO TEST IN INSP/MAINT 1 NM 01 807WP 023 COCKPIT EMERGENCY PORTABLE LIGHT INOPERATIVE. REMOVED AND REPLACED PORTABLE EMERGENCY LIGHT ASSEMBLY. OPS CHECK GOOD I AW PSM 1-8-2 CH 33-51-00 PAGE 201-202. (M) 2 H 7 2 4T RT A13NM 2001102300092 20011023 00092 WP 2001 10 23 2001F00468 1 20011002 A 3350 60030451LB BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 819US 48099 IND - THE LOW LEVEL EMERGENCY LIGHTS AND THE AFT SECTION OF CEILING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPL ACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES AND THE AFT CEILING EMERGENCY LIGHT POWER SUPPLY. REF USAAD01165. (M) 2 L 7 2 4F A6WE 2001102300093 20011023 00093 NM 2001 10 23 2001F00469 1 20011005 A 3233 PA4207 ACTUATOR BOEING 737 7372L9 1384497 NM NLG DAMAGED A SOKF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 281LF 22071 DURING TAKEOFF OF FLIGHT, THE NOSE GEAR DIDN'T RETRACT, THE AIRCRAFT RETURNED TO SJO STATION. AFTER LANDING, TECHNICIAN S PERFORMED INSPECTION OF THE AIRCRAFT AND FOUND THE NOSE GEAR LOCK ACTUATOR DAMAGED, IT WAS REPLACED IAW AMM 32-33-21 A ND 32-33-00. ALSO, DURING CHECK ANTI-SKID TEST FOUND VALVE RI FAULT INDICATION. REPLACED ANTI-SKID CONTROL SHIELD AS P ER MM 32-42-21, AND MAIN WHEEL ASSY NR 1, 2, 3, AND 4 WAS REPLACED DUE TO DAMAGED AS PER MM 32-45-11. RESULTS WERE SATIS FACTORY. A/C RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2001102300094 20011023 00094 NM 2001 10 23 GAI2001F00000 1 20011011 A 2750 WIRE BOEING 727223 BOEING 727 727223 1384074 NM PWA JT8 JT8D9 52048 NE CONNECTOR PLUG DIRTY A C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 07 6806 19481 19481 AFTER TAKE OFF, THE FLIGHT CREW DISCOVERED THAT THE OUTBOARD FLAPS WERE STUCK AT THE 2 DEGREE POSITION. AN EMERGENCY WA S DECLARED AND THE AIRCRAFT RETURNED TO AIRPORT. THE AIRCRAFT MADE AN UNEVENTFUL LANDING. RESET ASYMMETRY CIRCUIT AND CLEANED CANNON PLUG OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2001102300095 20011023 00095 NM 2001 10 23 2001F00470 1 20011005 A 3241 101A SHIELD BOEING 737 7372L9 1384497 NM ANTI-SKID SYS FAULTY A SOKF K NONE O OTHER IN INSP/MAINT 1 SO 23 281LF 22071 DURING TAKEOFF OF FLIGHT, THE NOSE GEAR DIDN'T RETRACT, THE AIRCRAFT RETURNED TO SJO STATION. AFTER LANDING, TECHNICIAN S PERFORMED INSPECTION OF THE AIRCRAFT AND FOUND THE NOSE GEAR LOCK ACTUATOR DAMAGED, IT WAS REPLACED IAW AMM 32-33-21 A ND 32-33-00. ALSO, DURING CHECK ANTI-SKID TEST FOUND VALVE RI FAULT INDICATION. REPLACED ANTI-SKID CONTROL SHIELD AS P ER MM 32-42-21, AND MAIN WHEEL ASSY NR 1, 2, 3, AND 4 WAS REPLACED DUE TO DAMAGED AS PER MM 32-45-11. RESULTS WERE SATIS FACTORY. A/C RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2001102300096 20011023 00096 EA 2001 10 23 COMA0160828 1 20011022 A 5346 6013701912 WEB CNDAIR CL600 CL6002B19 EA BEAM CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 9666 7026 L/H AND R/H LOWER WEBS ARE CRACKED ON ENGINE SUPPORT BEAM AT F.S. 625.30 AND UPPER AND LOWER WEBS ARE CRACKED AT BL 0.00 CENTER OF BEAM F.S. 625.30.REPAIRED L/H AND R/H LOWER WEBS I/A/W CANADAIR R.E.O. 601R-53-61-366 REV C. PERFORMED TEMPOR ARY REPAIR TO UPPER AND LOWER WEBS AT BL 0.00 CENTER OF BEAM I/A/W CANADAIR R.E.O. 601R-53-61-345 REV B. 2 L 7 2 4F RT A21EA 2001102300097 20011023 00097 NM 2001 10 23 2001F00449 1 20010910 A 2421 727792L IDG BOEING 757 757236 NM NR 1 ENGINE DEFECTIVE A N8TA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 WP 19 506NA 24771 ON CLIMB-OUT, THE LEFT IDG LIGHT CAME ON. DISCONNECTED IDG AND RETURNED TO STATION. BPCU INTERROGATION INDICATED TRIP DUE TO LOW OIL PRESSURE. IDG REPLACED, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2001102300098 20011023 00098 WP 2001 10 23 DHL2001801537 1 20011004 A 5300 47723971 FITTING DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AFT BULK HEAD JOINT FITTING CRACKED 1 1/2 IN STA 1966.000 L17R.REMOVED CRACKED FITTING PER SRM 51-1-20D PG 21.CLEANED TR EATED AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-1-20 PG 9. 2 L 7 4 4F RT 4A25 2001102300099 20011023 00099 NM 2001 10 23 2001F00450 1 20010910 A 4970 38760354 SENSOR BOEING 757 75723A 1384967 NM APU FAILED A N8TA K NONE J WARNING INDICATION CR CRUISE 1 WP 19 541NA 24291 ON PUSH BACK, STARTING RIGHT ENGINE, APU FAULT CAUSING POWER LOSS. ECU BITE CHECK WAS ACCOMPLISHED WITH NO FAULTS FOUND. AIRCRAFT RELEASED. ABOUT 30 MINUTES AFTER DEPARTURE APU FAULTED, SINGLE ELECTRICAL SOURCE, AIRCRAFT RETURNED TO DEPAR TURE STATION. ON INBOUND APU WAS RESTATED AND RAN FOR ABOUT 10 MINUTES AND FAULTED AGAIN. A ECU BITE TEST REPORTED FAU LT CODE 16 (P2 SENSOR). P2 SENSOR REPLACED APU OPS CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2001102300100 20011023 00100 NM 2001 10 23 2001F00451 1 20010906 A 3610 312N53061 DUCT BOEING 757 757200 1384950 NM LT ENGINE LEAKING A N8TA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 19 512NA 26962 LEFT ENGINE OVERHEAT EICAS MESSAGE APPEARED OUT OF FL210. ACCOMPLISHED QRH PROCEDURES INDICATION WENT AWAY. AIRCRAFT R ETURNED TO STATION, AN UNEVENTFUL LANDING ACCOMPLISHED. INSPECTION REVEALED THE HP2 DUCT WAS WARN AND LEAKING. REPLACED HP2 DUCT, LEAK CHECKED GOOD. (M) 2 L 7 2 4F RT A2NM 2001102300101 20011023 00101 NM 2001 10 23 2001F00452 1 20010924 A 2432 S282T0026 CHARGER BOEING 757 757200 1384950 NM E/E BAY FAILED A N8TA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 19 512NA 26962 AFTER TAKEOFF, MAIN BATTERY CHARGER FAILED, ACCOMPANIED BY NUMEROUS MAINTENANCE STATUS MESSAGES FOLLOWED BY MASTER CAUTI ON AND AMBER EICAS MESSAGES. RETURNED TO STATION. REPLACED BATTERY CHARGER AND BATTERY, ALL SYSTEMS OPERATIONALLY CHEC KED GOOD. (M) 2 L 7 2 4F RT A2NM 2001102300102 20011023 00102 EA 2001 10 23 COMA0160829 1 20011022 A 5346 6013701912 WEB CNDAIR CL600 CL6002B19 EA BEAM CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 984CA 9666 7171 L/H AND R/H LOWER WEBS ARE CRACKED ON ENGINE SUPPORT BEAM AT F.S. 625.30.REPAIRED L/H AND R/H LOWER WEBS I/A/W CANADAIR R.E.O. 601R-53-61-366 REV. C. 2 L 7 2 4F RT A21EA 2001102300103 20011023 00103 NM 2001 10 23 2001F00453 1 20010813 A 2424 GCU BOEING 727 727259 138408J NM NR 1 ENGINE FAILED A FX7A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 203AV 22474 FLT 504 - DEPARTING CCS - WHILE CLIMBING OUT, NR 1 GENERATOR HAD DIFFERENT FAULT INDICATION ON F/E PANEL. NR 3 GENERATO R WAS PREVIOUSLY ON DMI. RETURNED TO DEPARTURE CITY. AIRCRAFT LANDED WITHOUT INCIDENT. NR 1 ENGINE GENERATOR SYSTEM T ROUBLESHOT AND VOLTAGE REGULATOR AND GCU REMOVED AND REPLACED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001102300104 20011023 00104 NM 2001 10 23 AALA20011603 1 20010806 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 907AN 29509 DEN - DURING OVERNIGHT MAINTENANCE, EMERGENCY FLOOR PATH LIGHTING AT 7D INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GRO UND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2001102300105 20011023 00105 NM 2001 10 23 AALA20011653 1 20010818 A 3397 CONNECTOR BOEING 727 727223 1384074 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 882AA 21521 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY FLOOR PATH LIGHTING IS INTERMITTENT. RESECURED LOOSE CONNECTOR. SYSTEM G ROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001102300106 20011023 00106 NM 2001 10 23 AALA20011669 1 20010820 A 3397 WIRE HARNESS BOEING 727 727227 1384078 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 721AA 20729 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING IN FORWARD PASSENGER CABIN INOPERATIVE. REPLACED WIR ING HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001102300107 20011023 00107 NM 2001 10 23 AALA20011677 1 20010821 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 890AA 22006 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING IN AFT STAIRWELL INOPERATIVE. REPLACED AFT STAIRWELL L IGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001102300108 20011023 00108 NM 2001 10 23 AALA20011684 1 20010823 A 3350 CONTACTOR BOEING 727 727227 1384078 NM CABIN WORN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 719AA 20612 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY PATH FLOOR LIGHT STRIP AFT OF FIRST CLASS DIM. REPLACED EMERGENCY PATH FL OOR LIGHT CONDUCTOR STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001102300109 20011023 00109 EA 2001 10 23 COMA0160830 1 20011021 A 2740 70607 CONTROL BOX CNDAIR CL600 CL6002B19 EA AVIONICS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 929CA 13282 7035 STAB CHANNEL 1 INOP MESSAGE DURING APPROACH.REPLACED THE HSTCU. 2 L 7 2 4F RT A21EA 2001102300110 20011023 00110 NM 2001 10 23 AALA20011685 1 20010824 A 3350 8100037801 LIGHT BOEING 737 737823 13844BZ NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 913AN 29514 SNA - DURING OVERNIGHT MAINTENANCE, EXTERIOR EMERGENCY LIGHT AT R1 DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY. SYSTEM G ROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2001102300111 20011023 00111 NM 2001 10 23 AALA20011686 1 20010822 A 3350 900542 BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 723AA 20731 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT AT R1 DOOR INOPERATIVE. REPLACED BATTERY PACK. SYSTE M GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001102300112 20011023 00112 NM 2001 10 23 AALA20011691 1 20010824 A 3350 P4010049 BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 725AA 20732 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN AFT SECTION DIM. REPLACED BATTERY PACK. SYST EM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001102300113 20011023 00113 NM 2001 10 23 AALA20011695 1 20010824 A 3350 900542 BATTERY PACK BOEING 727 727223 1384074 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 848AA 20989 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY AFT STAIRWELL LIGHTS INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND C HECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001102300114 20011023 00114 NM 2001 10 23 AALA20011699 1 20010826 A 3350 P4010049 BATTERY PACK BOEING 727 727223 1384074 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 848AA 20989 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHE CKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001102300115 20011023 00115 NM 2001 10 23 AALA20011710 1 20010829 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 867AA 21372 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING INOPERATIVE. REPLACED LIGHT STRIP. SYSTEM GROUND CHEC KED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001102300116 20011023 00116 EA 2001 10 23 COMA0160831 1 20011021 A 2701 CONTROL COLUMN CNDAIR CL600 CL6002B19 EA A COMA O OTHER F FLT CONT AFFECTED IN INSP/MAINT 1 SO 01 709CA 7238 FLIGHT #5260. WHILE MOVING AILERONS THRU FULL RANGE OF TRAVEL, A SLIGHT BINDING CAN BE FELT AT FULL TRAVEL AND AT NEUTRO L.RETROQUED THE NUT HOLDING YOKE TO CONTROL COLUMN. 2 L 7 2 4F RT A21EA 2001102300117 20011023 00117 NM 2001 10 23 AALA20011711 1 20010829 A 3350 P4010049 BATTERY PACK BOEING 727 727223 1384074 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 849AA 20990 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING DIM THROUGHOUT COACH. REPLACED FORWARD AND AFT BATTERY PACKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001102300118 20011023 00118 NM 2001 10 23 AALA20011712 1 20010829 A 3350 6013211 BATTERY PACK BOEING 727 727223 1384074 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 872AA 21384 DFW - DURING OVERNIGHT MAINTENANCE, L1 AND R1 EMERGENCY EXIT SLIDE LIGHT INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GR OUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001102300119 20011023 00119 NM 2001 10 23 AALA20011714 1 20010830 A 3350 900542 BATTERY PACK BOEING 727 727223 1384074 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 861AA 21088 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD GALLEY CEILING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK. SY STEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001102300120 20011023 00120 NM 2001 10 23 AALA20011715 1 20010830 A 3350 P4010051126 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 861AA 21088 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY LIGHT AT ROW 9 INOPERATIVE. REPLACED LIGHT ASSEMBLY. SYSTEM GRO UND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001102300121 20011023 00121 EA 2001 10 23 COMA0160832 1 20011021 A 2720 RUDDER CNDAIR CL600 CL6002B19 EA A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 954CA 7100 FLIGHT #5775 - CONFIG RUDDER WARNING DURING T/O.C.N.D. NO CONFIG WARNING WITH T/O POWER. 2 L 7 2 4F RT A21EA 2001102300122 20011023 00122 NM 2001 10 23 AALA20011778 1 20010912 A 3350 LIG5192 LIGHT BOEING 727 727223 1384074 NM COCKPIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 860AA 21087 TUL - FOUND PORTABLE EMERGENCY EXIT LIGHT OVER COCKPIT DOOR INOPERATIVE. INSTALLED SERVICEABLE LIGHT ASSEMBLY LIG5197 I PC 33-50-00-20. INSTALLED PER MM 33-50-101-2, OPS CHECK OK. WORK ACCOMPLISHED ON E-58 3862640. (M) 2 L 7 3 4F A3WE 2001102300123 20011023 00123 NM 2001 10 23 AALA20011779 1 20010911 A 3350 LIG5714 LIGHT BOEING 727 727223 1384074 NM AFT AIRSTAIR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 879AA 21391 TUL - FOUND VENTRAL AIRSTAIRS AFT OVERHEAD EMERGENCY LIGHT INOPERATIVE. (M) 2 L 7 3 4F A3WE 2001102300124 20011023 00124 NM 2001 10 23 AALA20011783 1 20010917 A 3350 LIGHT BOEING 727 727227 1384078 NM AFT AIRSTAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 731AA 20738 DTW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AS SEMBLY. SYSTEM GROUND CHECKED NOMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001102300125 20011023 00125 EA 2001 10 23 COMA0160833 1 20011019 A 2750 860D10018 FCU CNDAIR CL600 CL6002B19 EA AVIONICS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 431CA 831 7472 FLIGHT #5453. FLAPS FAILED AT 30 DEGREES DURING DESCENT.REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2001102300126 20011023 00126 NM 2001 10 23 AALA20011801 1 20010918 A 3310 5949155 RELAY BOEING 757 757223 1384957 NM COCKPIT FAILED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 191AN 32385 HNL - FLT 58 - EN ROUTE HNL-SJC - DETECTED FLICKERING OF COCKPIT LIGHTING SYSTEM. FLIGHT ATTENDANT REPORTED BURNING SME LL IN CABIN. ACCOMPLISHED CABIN FIRE SMOKE CHECKLIST. RETURNED HNL AND LANDED WITHOUT FURTHER INCIDENT. REPLACED P-37 RELAYS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001102300127 20011023 00127 EA 2001 10 23 COMA0160834 1 20011019 A 3350 363782 LAMP CNDAIR CL600 CL6002B19 EA CABIN FLOOR INOPERATIVE A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 934CA 7042 FLIGHT #5898 EMERGENCY FLOOR PATH LIGHTING FROM ROW 8 AFT IS INOP.REPLACED THE FLEXIBLE LAMP ASSY. 2 L 7 2 4F RT A21EA 2001103000012 20011030 00012 SO 2001 10 30 COMA0110152 1 20011023 A 3242 20563 PIN BFGOODRICH EMB 120 EMB120RT SO BRAKE ASSY BROKEN A COMA K NONE O OTHER NR NOT REPORTED 1 SO 01 267CA 3158 1132 1259 FLIGHT MECHANICS TAXIED A/C TO HANGAR FROM GATE AND FELT A BRAKE DRAGGING. A/C WAS JACKED AND THE LEFT INBD BRAKE WAS FO UND TO BE DRAGGING. AFTER THE BRAKE WAS REMOVED, IT WAS DISCOVERED THAT ONE OF THE RETURN SPRING ASSEMBLIES "PIN" WAS B ROKEN AT END THAT ATTACHES TO THE PRESSURE PLATE. REMOVED BRAKE ASSEMBLY AND INSTALLED SERVICEABLE BRAKE ASSEMBLY I/A/W EMB-120 MM 32-41-05 P401-404. 2 L 7 2 4T RT A31SO 2001102300128 20011023 00128 NM 2001 10 23 PCAA0110126 1 20011017 A 5311 85311420 FRAME DHAV DHC8 DHC8102 2809003 NM RIGHT CRACKED A PCAA O OTHER O OTHER IN INSP/MAINT 1 EA 13 817EX 191 DURING A LEVEL INSPECTION RIGHT NOSE GEARWELL Z MEMBER FOUND CRACKED AT STATION X97 & X109. REPAIRED BY INSTALLING REPAI R DOUBLER IN ACCORDANCE WITH DEHAVILLAND REPAIR DRAWING RD8-53-1676 AND DER CALLAHAN REPAIR SERVICES DRAWING #CAS AAL23. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001102300129 20011023 00129 NM 2001 10 23 PCAA0110121 1 20011019 A 7930 APT761000100DW TRANSMITTER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LEFT ENGINE INACCURATE A PCAA E ENGINE SHUTDOWN O OTHER DE DESCENT 1 EA 13 822EX 187 120773 BWI-GSO FLIGHT#3772. CREW REPORTED DURING DECENT NUMBER 1 ENGINE OIL PRESSURE INDICATED 15 PSI. ALL OTHER INDICATIONS NO RMAL, CAUTION LIGHT DID NOT ILLUMINATE.ENGINE WAS SHUT DOWN.MAINTENANCE REPLACED OIL PRESSURE TRANSMITTER. GROUND RUN AI RCRAFT, OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2001102300130 20011023 00130 NM 2001 10 23 PCAA0110125 1 20011021 A 5610 NP15790213 WINDOW DHAV DHC8 DHC8102 2809003 NM CAPTAINS SIDE CRACKED A PCAA K NONE O OTHER NR NOT REPORTED 1 EA 13 842EX 14720 341 LGA- FLIGHT# 3969. CREW REPORTED CAPTAINS SIDE WINDOW CRACKED. MAINTENANCE REPLACED CAPTAINS SIDE WINDOW IN ACCORDANCE W ITH MAINTENANCE MANUAL CHAPTER 56-10-16. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002032600077 20020326 00077 NM 2002 3 26 PCAA0110127 1 20011016 A 5315 85310380 FLOORBEAM DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 837EX 217 DURING A LEVEL INSPECTION NOSE GEAR DRAG STRUT ACTUATOR BRACKET FOUND CRACKED. THREE FASTENER HOLES FOUND TO HAVE SMALL CRACKS FORMING IN NOSE GEAR FLOORBEAM. CRACKED FLOORBEAM TEMRORARILY REPAIRED IAW DEHAVILLAND REPAIR DRAWING RD 8-53-6 246. ACTUATOR BRACKET REPLACED IAW DEHAVILLAND STRUCTURAL REPAIR MANUAL. 2 H 7 2 4T RT A13NM 2001102300137 20011023 00137 NM 2001 10 23 MAS2001F00001 1 20011009 A 5500 75540027 HINGE FITTING DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE AFT RUD CTR HNG WORN A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 446YV SSA0119 446 DURING AN AIRCRAFT INSPECTION, MAINTENANCE FOUND THE AFT RUDDER CENTER HINGE FITTING WORN. THE FITTING WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 2001102300138 20011023 00138 NM 2001 10 23 AALA20011828 1 20010928 A 3350 P4010049 BATTERY PACK BOEING 727 727223 1384074 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 843AA 20984 DTW - DURING OVERNIGHT MAINTENANCE, EMERGENCY FLOOR PATH LIGHTING INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CH ECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001102300141 20011023 00141 SO 2001 10 23 ASOA01183 1 20010924 A 5720 12017054 BRACKET EMB 120 EMB120 3260201 SO LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 241AS 120065 DURING SCHEDULED MAINTENANCE IN TXK, THE LEFT WING RIB NR 6 LOWER MID SKIN SUPPORT BRACKET WS FOUND TO BE CRACKED. MAIN TENANCE REMOVED AND REPLACED THE LEFT WING RIB NR 6 LOWER MID SKIN SUPPORT BRACKET. MAINTENANCE REINSTALLED THE LEFT WI NG DEFUEL PANEL IAW ASA EO120-51-0005. LEAK CHECK GOOD. INSPECTION WAS COMPLIED WITH. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001102300143 20011023 00143 SO 2001 10 23 ASOA01184 1 20010925 A 5711 12016806001 SPAR CAP EMB 120 EMB120 3260201 SO LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 245AS 120075 DURING SCHEDULED MAINTENANCE IN MCN, THE LEFT WING FORWARD SPAR CAP WAS FOUND TO BE CRACKED. MAINTENANCE IS REPAIRING C RACKED LEFT WING SPAR CAP IAW ASA EO120-57-0114. (M) 2 L 7 2 4T RT A31SO 2001102300144 20011023 00144 SO 2001 10 23 ASOA01185 1 20010925 A 5711 12016806002 SPAR CAP EMB 120 EMB120 3260201 SO RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 238AS 120053 DURING HANGAR MAINTENANCE MCN, THE RIGHT WING FORWARD SPAR CAP WAS FOUND TO BE CRACKED. MAINTENANCE IS REPAIRING THE RI GHT WING CRACKED SPAR CAP IAW ASA EO120-57-0115. (M) 2 L 7 2 4T RT A31SO 2001102300145 20011023 00145 2001 10 23 ASOA01186 4 20010925 A 2350 509111 AUDIO PANEL CESSNA 140 140 2071602 CE COCKPIT FAULTY A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 11 241S 968 9532 WHILE ON APPROACH INTO ATL FROM LYH, CAPTAIN REPORTED SMELLING AN ELECTRICAL ODOR FOLLOWED BY SEEING SMOKE COMING FROM F IRST OFFICERS AUDIO CONTROL PANEL. CAPTAIN REQUESTED PRIORITY HANDLING, BUT HE DID NOT DECLARE AN EMERGENCY. ON FINAL APPROACH THE SMOKE HAD CEASED. AIRCRAFT LANDED IN ATL WITHOUT FURTHER INCIDENT. (M) 1 H 7 1 3O NC A768 2001102300147 20011023 00147 SO 2001 10 23 ASOA01187 1 20010925 A 3350 1317 LIGHT EMB 120 EMB120 3260201 SO CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 229AS 120042 DURING GROUND INSPECTION IN ATL, EMERGENCY LIGHT ON RIGHT OVERWING WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TH E FORWARD RIGHT EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001102300150 20011023 00150 SO 2001 10 23 ASOA01188 1 20010925 A 3350 3071BPE LIGHT EMB 120 EMB120 3260201 SO CABIN MISSING A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 228AS 120025 FLT 4101 - DURING GROUND INSPECTION IN ATL, FLIGHT ATTENDANT REPORTED EMERGENCY FLOOR LEVEL LIGHTING WAS INOPERATIVE AT ROW 3. MAINTENANCE INSPECTED AND FOUND THAT THERE WAS NO LIGHT BULB INSTALLED AT ROW 3. MAINTENANCE REPLACED MISSING BU LB AT ROW 3. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001102300151 20011023 00151 EU 2001 10 23 ASOA01189 1 20010925 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72 EU CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 634AS 370 FLT 4100 - DURING GROUND INSPECTION IN ATL, CREW REPORTED THE FORWARD EMERGENCY EXIT SIGN LIGHT WAS INOPERATIVE. MAINTE NANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY AT POSITION 61WL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVI CE. (M) 2 H 7 2 4T RT 2001102300152 20011023 00152 WP 2001 10 23 GTIA010907 1 20010921 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 603CA 49508 FLL - FOUND EMERGENCY EXIT LIGHTS OVER LEFT AND RIGHT AFT OVERWING EXITS INOPERATIVE. REMOVED AND REPLACED BATTERIES FO R EMERGENCY EXITS LIGHTS OVER LEFT AND RIGHT AFT OVERWING EXITS. OPS CHECK NORMAL IAW MD80 MM 33-50-00. (M) 2 L 7 2 4F A6WE 2001102300153 20011023 00153 WP 2001 10 23 GTIA010910 1 20010930 A 5270 STRIKER DOUG DC9 DC983 3022083 WP CARGO DOOR OUT OF ADJ A GTIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 23 DALLO 53012 FLT 923 - DTW - ABORTED TAKEOFF DUE TO FORWARD CARGO DOOR LIGHT ON TAKEOFF ROLL. ADJUSTED FORWARD CARGO DOOR PROXIMITY STRIKER, OPS CHECK GOOD IAW MD-80 MM 57-70-02. (M) 2 L 7 2 4F RT A6WE 2001102300154 20011023 00154 WP 2001 10 23 GTIA010913 1 20010925 A 3350 AD4002P BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 818NK 48018 FLL - CENTER AISLE OVERHEAD EMERGENCY LIGHTS OUT FIRST 5 SEAT ROWS. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES FOR ROWS 1 THROUGH 5. OPS CHECK GOOD IAW MD80 MM 33-53-00. (M) 2 L 7 2 4F A6WE 2001102300155 20011023 00155 NM 2001 10 23 P2EA01161 1 20010813 A 5330 SKIN BOEING 737 737200A 1384416 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 120NJ 22979 SJO - DURING Q-CHECK, R1 DOOR, LOWER AFTER CORNER CUT OUT WITH CRACK. REPAIRED FUSELAGE SKIN FORWARD GALLEY DOOR CUT OU T FROM BS 314 TO BS 340, BETWEEN STRINGER 16 AND 18 RIGHT DUE TO CRACK IAW SRM 53-30-3, FIG 26. (M) 2 L 7 2 4F RT A16WE 2001102300156 20011023 00156 NM 2001 10 23 P2EA01166 1 20010818 A 5312 BULKHEAD BOEING 737 737200A 1384416 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 120NJ 22979 SJO - DURING Q-CHECK, INSPECTION PER S/B 737-53A1173, BS 178 FORWARD PRESSURE BULKHEAD WEB WITH CRACK AT WL 210 AND RBL 8.5. FORWARD PRESSURE BULKHEAD BS 178, VERTICAL CHORD CRACKED AT INBOARD FLANGE WL 184 AND LBL 5.7. REPAIRED FORWARD P RESSURE BULKHEAD WEB FROM WL 204.5 TO WL 234 AND RBL 1.250 TO RBL 18 IAW SRM 53-10-11, FIG 1. REPAIRED FORWARD PRESSURE BULKHEAD BS 178 VERTICAL CHORD FROM WL 176 TO WL 197 AND LBL 5.7 IAW SRM 53-10-11 FIG 68. (M) 2 L 7 2 4F RT A16WE 2001102300157 20011023 00157 NM 2001 10 23 P2EA01167 1 20010820 A 5753 SKIN BOEING 737 7372T5 1384474 NM T/E FLAP CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 120NJ 22979 SJO - DURING Q-CHECK, RIGHT WING OUTBOARD MID FLAP WBL 304.5, SKIN WITH CRACK. RIGHT WING OUTBOARD MID FLAP L/E OF CENT ER TRACK CAVITY SKIN SECTION REPAIRED IAW COOPESA EO NR COO-3-57-452-01. (M) 2 L 7 2 4F RT A16WE 2001102300158 20011023 00158 NM 2001 10 23 P2EA01168 1 20010814 A 5330 SKIN BOEING 737 737200A 1384416 NM FUSELAGE DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 120NJ 22979 DURING Q-CHECK, EXTERNAL FUSELAGE, SKIN WITH SCRATCH AND DENT FROM BS 306 TO BS 307, BETWEEN STRINGER 20 AND 21 RIGHT. REPAIRED FUSELAGE SKIN SECTION FROM BS 296.5 TO BS 318, BETWEEN STRINGER 20 AND 25 RT DUE TO DENT IAW COOPESA EO COO-3-5 3-430-01. (M) 2 L 7 2 4F RT A16WE 2001102300159 20011023 00159 NM 2001 10 23 P2EA01171 1 20010828 A 2750 FLAP BOEING 737 737230 1384401 NM WING MALFUNCTIONED A P2EA O OTHER F FLT CONT AFFECTED AP APPROACH 1 CE 05 124NJ 22122 FLT 451-MCI- ON APPROACH INTO MCI WHEN FLAPS SELECTED TO 1, FLAPS DID NOT EXTEND. RECYCLED AND FLAPS EXTENDED UP TO 15, BUT WOULD NOT GO TO 25. RECYCLED THE HANDLE A COUPLE OF MORE TIMES AND FLAPS FINALLY EXTENDED TO 25 AND THEN 30. AFTER L ANDING, FLAPS RETRACTED NORMALLY. VISUALLY INSPECTED THE TRAILING EDGE FLAPS AND CARRIAGES. NO STRUCTURAL INTERFERENCE N OTED. VISUALLY INSPECTED FLAP JACKSCREWS AND TRANSMISSIONS, NO DEFECTS OBSERVED. OPERATED FLAPS PER BOEING MM 27-51-0. ALL INDICATIONS NORMAL. REQUESTED THAT AN EVALUATIONS FLIGHT OF THE AIRCRAFT AND FLAPS BE PERFORMED. AFTER EVALUATION FL IGHT THE FLIGHT CREW REPORTED THAT SEVERAL APPLICATIONS OF FLAPS WAS PERFORMED WITHOUT ANY PROBLEMS. (M) 2 L 7 2 4F RT A16WE 2001102300160 20011023 00160 NM 2001 10 23 P2EA01173 1 20010907 A 5330 DOUBLER BOEING 737 737230 1384401 NM FUSELAGE DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 123NJ 22121 SJO - DURING C-CHECK, EXTERNAL FUSELAGE, FROM BS 867 TO BS 877, BETWEEN STRINGER 21 AND 24 LEFT EXISTING REPAIR WITH DEN TS. (M) 2 L 7 2 4F RT A16WE 2001102300161 20011023 00161 NM 2001 10 23 HNAA0100067 1 20011019 A 3222 8800129 STRUT DHAV DHC8 DHC8102 2809003 NM FLAT A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 911HA 33050 358 034 UPON GEAR RETRACTION, MAIN GEAR CAUTION LIGHTS REMAINED ON WITH W.O.W. CAUTION LIGHT. CYCLED GEAR, CAME DOWN AND LOCKED WITH THREE GREEN INDICATION. RETRACTED GEAR AGAIN, NOSE DOOR CAUTION LIGHT REMAINED ON WITH W.O.W. CAUTION LIGHT. EXTEND ED GEAR AND RETURNED TO DEPARTURE FIELD. FOUND NLG SHOCK STRUT FLAT. RESEALED NLG STRUT CHARGING VALVE AND SERVICED STRU T. 2 H 7 2 4T RT A13NM 2001102300162 20011023 00162 NM 2001 10 23 P2EA01176 1 20010908 A 5310 DOOR FRAME BOEING 737 737230 1384401 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 123NJ 22121 SJO - DURING C-CHECK, LOWER FUSELAGE AFT CARGO COMPARTMENT DOOR WAY SECTION BS 794, BETWEEN STRINGER 25 AND 24 RT WEB WI TH CRACK. REPAIRED AFT CARGO COMPARTMENT DOORWAY AT BS 794 BETWEEN STRINGERS 21 AND 25 RT, DUE TO CRACKS IAW COOPESA EO COO-3-53-503-01. (M) 2 L 7 2 4F RT A16WE 2001102300163 20011023 00163 NM 2001 10 23 P2EA01177 1 20010908 A 5311 FRAME BOEING 737 737230 1384401 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 123NJ 22121 SJO - DURING C-CHECK, LOWER FUSELAGE, FORWARD CARGO COMPARTMENT BS 500, STRINGER 26 RIGHT FRAME WITH CRACK. REPAIRED FU SELAGE FRAME SECTION AT BS 500, BETWEEN STRINGER 24 AND 28 RIGHT DUE TO CRACK IAW COOPESA EO NR COO-3-53-523-01. THIS R EPAIR HAS BEEN APPROVED AS AN ALTERNATIVE METHOD OF COMPLIANCE (AMOC) TO PARAGRAPH (A.1.B) OF AD 89-11-00 R1. (M) 2 L 7 2 4F RT A16WE 2001102300164 20011023 00164 NM 2001 10 23 P2EA01178 1 20010908 A 5311 FRAME BOEING 737 737230 1384401 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 123NJ 22121 SJO - DURING C-CHECK, LOWER FUSELAGE FORWARD CARGO COMPT BS 460, BETWEEN STRINGER 20 AND 21 LEFT FRAME WITH CRACK. REPA IRED FUSELAGE FRAME SECTION AT BS 460, BETWEEN STRINGER 19 AND 26 LEFT, DUE TO CRACKS IAW COOPESA EO NR COO-3-53-519-01. THIS REPAIR HAS BEEN APPROVED AS AN ALTERNATIVE METHOD OF COMPLIANCE (AMOC) TO PARAGRAPH (A.1.B) OF AD 89-11-06 R1. ( M) 2 L 7 2 4F RT A16WE 2001102300165 20011023 00165 2001 10 23 P2EA01179 4 20010910 A 2230 AUTOTHRUST SYS DOUG DC9 DC987 3022087 WP COCKPIT MALFUNCTIONED A P2EA O OTHER O OTHER CR CRUISE 1 CE 05 132NJ 49780 FLT 775 - MCI - AUTOTHROTTLE ON EPR SYNC FAILS TO MAINTAIN BETTER THAN .02 SPLIT, LEFT ENGINE HIGHER. WITH N1 SYNC ON E PR'S ARE TOGETHER. PERFORMED RETURN TO SERVICE TEST IAW MM 22-10-05, SYSTEM NORMAL. (M) 2 L 7 2 4F RT A6WE 2001102300166 20011023 00166 NM 2001 10 23 P2EA01180 1 20010907 A 5230 SKIN BOEING 737 737230 1384401 NM CARGO DOOR DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 123NJ 22121 SJO - DURING C-CHECK, AFT CARGO COMPARTMENT DOOR EXTERNAL SKIN WITH SEVERAL DENTS OUT OF LIMITS. AFT CARGO COMPARTMENT EXTERIOR SKIN REPLACED DUE TO SEVERAL DENTS OUT OF LIMITS IAW SRM 52-30-2, FIG 3. (M) 2 L 7 2 4F RT A16WE 2001102300172 20011023 00172 NM 2001 10 23 P2EA01182 1 20010907 A 5330 SKIN BOEING 737 737230 1384401 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 123NJ 22121 SJO - DURING C-CHECK, FUSELAGE SKIN STRINGER 14 RT, LAP JOINT LOWER ROW OF FASTENERS BETWEEN BS 727B PLUS 3 INCHES, AND BS 727B PLUS 9 INCHES, WITH CRACKS AROUND FASTENERS. REPAIRED FUSELAGE SKIN SECTION FROM BS 727A PLUS 19 INCHES TO BS 7 27B PLUS 12 INCHES, BETWEEN STRINGER 13 AND 15 RIGHT, DUE TO CRACK IAW SRM 53-30-3 FIG 9. (M) 2 L 7 2 4F RT A16WE 2001102300173 20011023 00173 NM 2001 10 23 P2EA01183 1 20010909 A 5753 SKIN BOEING 737 737230 1384401 NM T/E FLAP DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 123NJ 22121 SJO - DURING C-CHECK, FOUND LEFT WING INBOARD MID FLAP T/E PANEL CENTER AREA, WBL 135, LOWER SURFACE, DENT FILLING COMPO UND MIGRATED. REPAIRED LEFT WING INBOARD MID FLAP, P/N 65-46486, COOPESA CODE TMC-078, AT T/E SECTION, DUE TO DELAMINAT ION, FROM WBL 106.24 TO WBL 124.615, IAW COOPESA EO NR COO-CMP-3-57-497-01. (M) 2 L 7 2 4F RT A16WE 2001102300174 20011023 00174 SO 2001 10 23 COMA0110153 1 20011022 A 3231 12043270501 CONTROLLER EMB 120 EMB120RT SO COCKPIT FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SO 01 267CA 22091 1259 FLIGHT #5009. DURING CLIMB OUT OF MCO A LOUD AIR NOISE EMANATING FROM THE NOSE AREA, AIRCRAFT RETURNED TO THE FIELD.REP LACED THE LANDING GEAR RELAY BOX. 2 L 7 2 4T RT A31SO 2001102300192 20011023 00192 2001 10 23 P2EA01184 4 20010909 A 2210 AUTOPILOT SYS BOEING 737 737230 1384401 NM COCKPIT MALFUNCTIONED A P2EA K NONE F FLT CONT AFFECTED DE DESCENT 1 CE 05 124NJ 22122 A CHANNEL AUTO PILOT STARTED TO SHAKE IN THE DESCENT. PERFORMED ADJUSTMENT AND TEST PER MM 22-11-01, NO DEFECTS NOTED. (M) 2 L 7 2 4F RT A16WE 2001102300194 20011023 00194 WP 2001 10 23 ABXA010542 1 20011009 A 5300 5956034526 SUPPORT DOUG DC9 DC933F 302207A WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 90 DEGREE FITTING WAS CRACKED ON THE END OF LONGERON 28 RIGHT, BOTTOM OF FLOOR PANEL SUPPORT BOTTOM SIDE F.S. 756. REPLA CED SUPPORT IAW DC-9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 2001102300195 20011023 00195 WP 2001 10 23 ABXA010543 1 20011008 A 5300 49125402 FITTING DOUG DC9 DC933F 302207A WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 RIGHT UPPER CARGO FLOOR BEAM VERTICAL ATTACH FITTING WAS CRACKED. REPLACED THE ATTACH FITTING IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2001102300196 20011023 00196 WP 2001 10 23 ABXA010544 1 20011017 A 5200 99211662 FITTING DOUG DC9 DC933F 302207A WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 MAIN CARGO DOOR FITTING WAS CRACKED IN TWO PLACES, F.S. 313 LONGERON 15 - 16 LEFT. REPAIRED FRAME IAW REA D952-42464-MR. 2 L 7 2 4F A6WE 2001102300197 20011023 00197 WP 2001 10 23 ABXA010545 1 20011011 A 5300 9911840165 CLIP DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 SHEAR TIE WAS CRACKED BETWEEN LONGERON "0" AND "1" LEFT AT F.S. 1087, ON AFT SIDE. REPLACED CRACKED SHEAR TIE IAW DC-9 S RM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2001102300198 20011023 00198 WP 2001 10 23 ABXA010546 1 20011008 A 5300 9919619503 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 F.S. 737 WAS CRACKED ON THE FORWARD UPPER FLANGE BETWEEN THE OUTBOARD FASTENERS. FRAME WAS REPLACED ON JOB CARD E.A. 534 00326-001-3. 2 L 7 2 4F A6WE 2001102300199 20011023 00199 WP 2001 10 23 ABXA010547 1 20011010 A 5300 995773925 CLIP DOUG DC9 DC933F 302207A WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 LEFT FUSELAGE FRAME SHEAR TIE WAS CRACKED AT STATION 945 BETWEEN LONGERON 15 LEFT AND 16 LEFT. REPAIRED SHEAR TIE IAW DC -9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2001102300201 20011023 00201 NM 2001 10 23 P2EA01185 1 20010908 A 5311 FRAME BOEING 737 737230 1384401 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 123NJ 22121 SJO - DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT, BS 460, BETWEEN STRINGER 20 AND 21 LEFT FRAME WITH CRACK. REPAIR ED FUSELAGE FRAME SECTION AT BS 460, BETWEEN STRINGER 19 AND 26 LEFT DUE TO CRACKS IAW COOPESA EO NR COO-3-53-519-01. TH IS REPAIR HAS BEEN APPROVED AS AN ALTERNATIVE METHOD OF COMPLIANCE (AMOC) TO PARAGRAPH (A.1.B) OF AD 89-11-06 R1. (M) 2 L 7 2 4F RT A16WE 2001102300205 20011023 00205 NM 2001 10 23 P2EA01186 1 20010908 A 5311 FRAME BOEING 737 737230 1384401 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 123NJ 22121 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT, BS 500, STRINGER 26 RIGHT, FRAME WITH CRACK. REPAIRED FUSELAGE FRAME S ECTION AT BS 500, BETWEEN STRINGER 24 AND 28 RIGHT DUE TO CRACK IAW COOPESA EO NR COO-3-53-523-01. THIS REPAIR HAS BEEN APPROVED AS AN ALTERNATIVE METHOD OF COMPLIANCE (AMOC) TO PARAGRAPH (A.1.B) OF AD 89-11-06 R1. (M) 2 L 7 2 4F RT A16WE 2001102300207 20011023 00207 EA 2001 10 23 COMA0160835 1 20011022 A 2150 504175 SLEEVE CNDAIR CL600 CL6002B19 EA ACM BLEW OUT A COMA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 967CA 7134 FLIGHT #5001. L/H ACM UNCONTROLLABLE, AFT EQUIP BAY FILLED WITH SMOKE.REPLACED DEFECTIVE TURBINE INLET DUCT SLEEVE. 2 L 7 2 4F RT A21EA 2001102300208 20011023 00208 NM 2001 10 23 P2EA01187 1 20010908 A 5311 FRAME BOEING 737 737230 1384401 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 123NJ 22121 SJO - DURING C-CHECK, FORWARD CARGO COMPARTMENT, BS 500B, STRINGER 22 LEFT FRAME WITH DENT AND CRACK. REPAIRED FUSELAGE FRAME SECTION AT BS 500B, BETWEEN STRINGER 21 AND 23 LEFT, DUE TO DENT AND CRACK IAW SRM 51-40-3, FIG 1. THIS REPAIR H AD BEEN APPROVED AS AN ALTERNATE METHOD OF COMPLIANCE (AMOC) TO PARAGRAPH (A.1.B) OF AD 89-11-06 R1. (M) 2 L 7 2 4F RT A16WE 2001102300210 20011023 00210 NM 2001 10 23 P2EA01188 1 20010908 A 5311 FRAME BOEING 737 737230 1384401 NM FUSELAGE CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 123NJ 22121 SJO - DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT, BS 500A, BETWEEN STRINGER 25 AND 26 RT, FRAME END LOWER FLANGE WI TH CORROSION. REPAIRED FUSELAGE FRAME SECTION AT BS 500A, BETWEEN STRINGER 25 AND 26 RT, DUE TO CORROSION IAW SRM 53-10 -4, FIG 10. (M) 2 L 7 2 4F RT A16WE 2001102300212 20011023 00212 EA 2001 10 23 COMA0160836 1 20011022 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 EA EXTERIOR BURNED OUT A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 868CA 7427 R/H FWD EXTERIOR EMERGENCY LIGHT IS INOP.REPLACED LIGHT BULB. 2 L 7 2 4F RT A21EA 2001102300213 20011023 00213 NM 2001 10 23 P2EA01189 1 20010908 A 5311 FRAME BOEING 737 737230 1384401 NM FUSELAGE CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 123NJ 22121 SJO - DURING C-CHECK, FORWARD COMPARTMENT, BS 480, BETWEEN STRINGER 23 AND 24 LEFT, FRAME WITH CORROSION. REPAIRED FRAM E SECTION AT FORWARD CARGO COMPARTMENT, BS 480 BETWEEN STRINGER 23 AND 25 LEFT DUE TO CORROSION IAW SRM 51-40-3, FIG 1. (M) 2 L 7 2 4F RT A16WE 2001102300215 20011023 00215 2001 10 23 P2EA01190 4 20010916 A 2210 COUPLER BOEING 737 737230 1384401 NM YAW DAMPER FAILED A P2EA K NONE F FLT CONT AFFECTED CR CRUISE 1 CE 05 122NJ 22120 FLT 552 - MDW - YAW DAMPER INOPERATIVE. REMOVED AND REPLACED YAW DAMPER COUPLER OPERATIONAL CHECK NORMAL IAW MM 22-12-0 . (M) 2 L 7 2 4F RT A16WE 2001102300218 20011023 00218 EA 2001 10 23 COMA0160837 1 20011022 A 4990 APU CNDAIR CL600 CL6002B19 EA A COMA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CR CRUISE 1 SO 01 805CA 7354 FLIGHT #5635. APU OIL PRESSURE CAUTION MESSAGE. ACFT MADE UNSCHEDULED LANDING DUE TO IDG DEFERRAL.INSPECTED APU OIL LE VEL AND OIL PRESSURESWITCH. RAN APU FOR 30 MINUTES. NO DEFECTS FOUND. COULD NOT DUPLICATE. 2 L 7 2 4F RT A21EA 2001102300220 20011023 00220 2001 10 23 P2EA01191 4 20010917 A 2230 CONTROL UNIT DOUG DC9 DC987 3022087 WP AUTOTHROTTLE SYS MALFUNCTIONED A P2EA K NONE O OTHER TO TAKEOFF 1 CE 05 132NJ 49780 FLT 904 - MCI - WITH AUTO THROTTLES ENGAGED, RIGHT ENGINE SPOOLS UP SLOW AT TAKEOFF. THROTTLES SPLIT AS MUCH AS .3 EPR IN CRUISE. REMOVED AND REPLACED EPR SYNC-DRIVE SWITCHING UNIT, OPERATIONAL CHECK NORMAL IAW MM 22-01-05. (M) 2 L 7 2 4F RT A6WE 2001102300222 20011023 00222 EA 2001 10 23 COMA0160838 1 20011022 A 2741 3094334 SWITCH CNDAIR CL600 CL6002B19 EA COCKPIT FAULTY A COMA K NONE S AFFECT SYSTEMS IN INSP/MAINT 1 SO 01 708CA 7235 FLIGHT #5835. CREW REPORTED THE STAB/MACH TRIM NOT OPERATING NOSE UP DURING THEIR PREFLIGHT INSPECITON.REPLACED THE PIT CH TRIM SWITCH. 2 L 7 2 4F RT A21EA 2001102300223 20011023 00223 NM 2001 10 23 2001UALA02125 1 20011012 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 520UA 24890 FUSELAGE SKIN DENT STATION 1717 STRINGER 14L. MAJOR REPAIR ACCOMPLISHED. DAMAGED REMOVED DOUBLER AND FILLER INSTALLED, SKIN LAP AREA BEHIND DOOR 4L. 2 L 7 2 4F 4 F RT A2NM E17NE 2001102300224 20011023 00224 NM 2001 10 23 2001UALA02142 1 20011017 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 646UA 25283 FLOORBEAM CORRODED AT STATION 1197, RBL 15, AFT CARGO COMPARTMENT. MAJOR REPAIR ACCOMPLISHED. INSTALLED T-CAP AND DOUBL ER REPAIR ON FLOORBEAM. 2 L 7 2 4F 4 F RT A1NM E24NE 2001102300225 20011023 00225 NM 2001 10 23 2001UALA02143 1 20011017 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 646UA 25283 FORWARD PIT, FS 588, RBL 42, CARGO FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR ON FLOORBEAM . 2 L 7 2 4F 4 F RT A1NM E24NE 2001102300226 20011023 00226 NM 2001 10 23 2001UALA02144 1 20011017 A 4990 4950488 PRESSURE SWITCH AIRBUS A319 A319131 NM IAE V2527 V2527A5 NE A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 825UA 980 OIL SMELL IN CABIN. FOUND APU OIL PRESS SWITCH LEAKING INTO APU INLET. REPLACEDSWITCH AND RAN PACKS. NO LEAKS OR SME LL NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2001102300227 20011023 00227 EA 2001 10 23 COMA0160839 1 20011022 A 2741 601R517063 PANEL CNDAIR CL600 CL6002B19 EA COCKPIT FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 999CA 8234 7230 FLIGHT #6003. DURING TAXI OUT RECEIVED AMBER "MACH TRIM/STAB TRIM" CAUTION MESSAGE, AIRCRAFT RETURNED TO THE GATE.REPLA CED THE MACH/STAB TRIM PANEL. 2 L 7 2 4F RT A21EA 2001102300228 20011023 00228 EA 2001 10 23 COMA0160840 1 20011022 A 2751 855D1009 BPSU CNDAIR CL600 CL6002B19 EA LEFT WING FAULTY A COMA K NONE J WARNING INDICATION CL CLIMB 1 SO 01 958CA 641 7111 FLIGHT #5978. DURING CLIMB OUT OF BHM RECEIVED A FLAP INDICATION CAUTION MESSAGE WITH FLAPS AT ZERO DEGREES.REPLACED TH E LEFT BRAKE AND POSITION SENSING UNIT. 2 L 7 2 4F RT A21EA 2001102300229 20011023 00229 EA 2001 10 23 COMA0160841 1 20011023 A 3246 50105842 WHEEL CNDAIR CL600 CL6002B19 EA WHEEL CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 709CA 5550 187 7238 DURING N.D.T. INSPECTION OF THE MLG WHEEL INBOARD SUB ASSEMBLY, DISCOVERED A CRACK AT THE SPOKE AREA.WHEEL WAS REMOVED F ROM SERVICE AND SCRAPPED. 2 L 7 2 4F RT A21EA 2001102300230 20011023 00230 2001 10 23 P2EA01192 4 20010915 A 3421 GYRO BOEING 737 737230 1384401 NM COCKPIT FAILED A P2EA K NONE F FLT CONT AFFECTED DE DESCENT 1 CE 05 124NJ 22122 FLT 313 - MCI - WITH `A` AUTO PILOT ENGAGED, YOKE JERKS/PUMPS 3 OR 4 TIMES ABRUPTLY IN DESCENT. REMOVED AND REPLACED NR 1 VERTICAL GYRO AND OPERATIONAL CHECK NORMAL IAW MM 22-11-01. (M) 2 L 7 2 4F RT A16WE 2001102300231 20011023 00231 2001 10 23 P2EA01193 4 20010916 A 2211 COMPUTER BOEING 737 737297 1384480 NM AUTOPILOT SYS FAULTY A P2EA K NONE F FLT CONT AFFECTED CR CRUISE 1 CE 05 120NJ 22979 FLT 451 - MCI - WITH AUTOPILOT IN HGD HOLD AIRCRAFT ROLLS TO APPROXIMATELY WINGS LEVEL FROM AND BANK ANGLE AND TURNS AT ABOUT 1 DEGREE PER MINUTE TO THE LEFT. ALL OTHER AUTO PILOTS FUNCTIONS ARE NORMAL. REMOVED AND REPLACED ROLL COMPUTER AND OPERATIONAL CHECK IAW MM 22-11-16. (M) 2 L 7 2 4F A16WE 2001102300232 20011023 00232 NM 2001 10 23 P2EA01194 1 20010914 A 5313 STRINGER BOEING 737 737230 1384401 NM FUSELAGE CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 123NJ 22121 SJO - DURING C-CHECK, AFT CARGO COMPARTMENT BS 927 STRINGER 27 RIGHT WITH CORROSION. STRINGER 27 RIGHT REPAIRED, FROM BS 902 TO BS 962, DUE TO CORROSION IAW SRM 53-10-3 FIG 1. (M) 2 L 7 2 4F RT A16WE 2001102300233 20011023 00233 EA 2001 10 23 COMA0160843 1 20011022 A 5346 NA WEB CNDAIR CL600 CL6002B19 EA BEAM CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 941CA 16796 7050 DURING INSPECTION DISCOVERED A CRACK IN THE ENGINE SUPPORT BOX BEAM.PERFORMED TEMPORARY REPAIR TO UPPER AND LOWER WEBS F .S. 630 IN ACCORDANCE WITH CANADAIR REO 601R-53-61-345. 2 L 7 2 4F RT A21EA 2001102300234 20011023 00234 NM 2001 10 23 F3LA200100114 1 20011022 A 2761 65449617 ACTUATOR BOEING BOEING 737 7372L9 1384497 NM FAILED A F3LA K NONE K FLUID LOSS TX TAXI/GRND HDL 1 NM 03 271FL 489 MA21129 22734 UPON ARRIVAL, FLIGHT CREW REPORTED "A" SYSTEM HYDRAULIC QUANTITY AND PRESSURE FELL TO ZERO AFTER LANDING. REPLACED NO. 8 GROUND SPOILER ACTUATOR PER MM 27-62-101. PERFORMED OPERATIONAL CHECK, LEAK CHECK AND RIG CHECK. REPLACED NO. 1 AND NO. 2 ENGINE DRIVEN HYDRAULIC PUMPS PER MM 29-11-32 AND SERVICED HYDRAULIC SYSTEM. 2 L 7 2 4F RT A16WE 2001102300235 20011023 00235 NM 2001 10 23 P2EA01195 1 20010918 A 5210 SKIN BOEING 737 737230 1384401 NM AFT ENTRY DOOR DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 123NJ 22121 SJO - DURING C-CHECK, AFT ENTRY DOOR, EXTERIOR SKIN WITH TEMPORARY REPAIR AT LOWER HINGE. REPAIRED DOOR SKIN SECTION, B ETWEEN BEAMS 5 AND 6, FROM BS 959 TO BS 963.750, IAW SRM 52-00-3, FIG 3. (M) 2 L 7 2 4F RT A16WE 2001102300236 20011023 00236 NE 2001 10 23 P2EA01196 2 20010920 A 7200 SMOKE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE NR 2 ENGINE DETECTED A P2EA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 05 130NJ 49222 FLT 913 - MCI - WHEN TAXIING TO GATE, NR 2 ENGINE WAS SHUT DOWN 100 YARDS SHORT OF GATE. NR 2 ENGINE SPOOLED DOWN, PERS ONNEL ON GROUND REPORTED BLACK SMOKE FROM ENGINE. NO COCKPIT ABNORMAL INDICATIONS. OPERATED NR 2 ENGINE UP TAKEOFF POW ER, ALL PERIMETERS NORMAL. SUSPECTED FUEL ICE PROBLEM. OPS CHECKED ANTI-ICE SYSTEM. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4F 4 F A6WE E9NE 2001102300237 20011023 00237 EU 2001 10 23 SIMA200126401 1 20010921 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 241AE 340B241 ABI - DURING MBV INSPECTION, FOUND FRAME 272 CORRODED. REPAIRED FRAME 272 IAW SAAB SRM. (M) 2 L 7 2 4T RT A52EU 2001102300238 20011023 00238 EU 2001 10 23 SIMA200126505 1 20010921 A 5320 7253721439 STIFFENER SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 305AE 340B305 SBP - WEB REINFORCEMENT IS CORRODED AT STATION 294, REMOVED AND REPLACED WEB REINFORCEMENT IAW SAAB SRM 51-40-21. (M) 2 L 7 2 4T RT A52EU 2001102300239 20011023 00239 EU 2001 10 23 SIMA200126510 1 20010921 A 5320 7253720272 BRACKET SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 305AE 340B305 FUSELAGE BRACKET FOR WING LINK LEFT SIDE ATTACH POINT IS CORRODED. REMOVED AND REPLACED BRACKET IAW SAAB SRM 51-40-21, 51-40-22, 51-40-40 AND 51-20-50. (M) 2 L 7 2 4T RT A52EU 2001102300240 20011023 00240 NM 2001 10 23 TSAA0179120 1 20010928 A 7931 69726881 PRESSURE SWITCH BOEING 737 7372X6C 1384552 NM NR 1 ENGINE FAULTY A TSAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 13 817AL 23292 FLT 953 - ITO-HNL - DURING A NON-ETOPS QC CARGO FLIGHT, THE NR 1 ENGINE OIL FILTER BYPASS LIGHT CAME ON. SHUTDOWN THE N R 1 ENGINE AND DECLARED AN EMERGENCY. UNEVENTFUL LANDING AT HNL. REMOVED AND REPLACED THE OIL BYPASS SWITCH IAW MM 79- 35-011-4. INSPECTED AND REPLACED THE MAIN OIL FILTER. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001102300241 20011023 00241 NM 2001 10 23 USAA011228 1 20010910 A 5320 FLOOR SUPPORT BOEING 757 757225 1384959 NM FUSELAGE GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 601AU 54736 22193 CLT - FOUND FLOOR SUPPORT GOUGED 1 INCH, BS 640 RBL 16.10. BURNISHED AREA, ALODINE AND PRIME AREA PER SRM 51-10-06. (M ) 2 L 7 2 4F RT A2NM 2001102300242 20011023 00242 GL 2001 10 23 RAIA00110006 2 20011013 A 7320 14531128402B DUCT EMB 145 EMB145ER SO ALLSN AE300 AE3007A GL CRACKED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 809HK 145187 310166 5275-PIT-RIGHT ENGINE AUTO TAKEOFF THRUST CONTROL SYSTEM WARNING ON TAKE OFF ROLL. MAINTENANCE DEFERRED PER MEL 73-22-02 . CLEARED DMI - REMOVED AND REPLACED THE RIGHT HAND ANTI-ICE BLEED DUCT. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001102300243 20011023 00243 NM 2001 10 23 USAA011229 1 20010910 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 45284 23380 CLT - FOUND CHORD CRACKED 1.5 INCH, BS 178 WL 207 RBL 28. SPLICED IN NEW CHORD SECTION PER EO NR 5300V157 AND EA NR 853 95. (M) 2 L 7 2 4F RT A16WE 2001102300244 20011023 00244 NM 2001 10 23 USAA011230 1 20010910 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 45284 23380 CLT - CHORD CRACKED .75 INCH, BS 178 WL 184 LBL 5.9. INSTALLED REPAIR ANGLE PER EO NR 5300V155. (M) 2 L 7 2 4F RT A16WE 2001102300245 20011023 00245 NM 2001 10 23 USAA011232 1 20010910 A 5330 SKIN BOEING 767 767201 1385125 NM FUSELAGE DEFORMED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647US 23899 CLT - FOUND SKIN WITH DEFORMED AREA 3 INCHES BY 3 INCHES, BETWEEN BS 1197 AND BS 1219, BETWEEN BS 38L AND 39L. INSTALLE D DOUBLER PER EA NR 85351. (M) 2 L 7 2 4F RT A1NM 2001102300246 20011023 00246 NM 2001 10 23 USAA011235 1 20010912 A 5314 KEELBEAM BOEING 767 767201 1385125 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647US 58982 23899 CLT - FOUND KEEL CHORD CORRODED 6 INCHES, BS 1009 LBL 9. CUTOUT AND BLENDOUT CORROSION PER EA 85401. (M) 2 L 7 2 4F RT A1NM 2001102300247 20011023 00247 NM 2001 10 23 USAA011249 1 20010915 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 46526 22959 PIT - FRAME CRACKED .125 INCH, BS 767 ABOVE S9L TIE CLIP AT RIVET HOLE. INSTALLED DOUBLER PER TYPICAL REPAIR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001102400033 20011024 00033 WP 2001 10 24 CALA0100967 1 20011024 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP FWD CABIN INOPERATIVE A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 33817 49371 CABIN FORWARD SET OF EMERGENCY LIGHTS ON AFTER POWER TURNED OFF. EMERGENCY PACK BAD. REMOVED AND REPLACED BATTERY PACK A ND BATTERIES PER MM 33-53-00. OPS CHECK GOOD. 2 L 7 2 4F A6WE 2001102400072 20011024 00072 SO 2001 10 24 ASOA01179 1 20010920 A 5300 12019230003 SKIN PANEL EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 501AS 120273 DURING SCHEDULED MAINTENANCE IN MCN, CORROSION WAS FOUND ON THE SKIN AT FRAMES 22 AND 23, BETWEEN STRINGERS 20 LEFT AND 20 RIGHT. MAINTENANCE REPAIRED AIRCRAFT IAW ASA EO120-53-0167. THIS EO STATES REPAIR SPECIFICATIONS FOR FRAME 22 AND 2 3 SKIN CORROSION REPAIR ON AIRCRAFT N501AS. (M) 2 L 7 2 4T RT A31SO 2001102400073 20011024 00073 NM 2001 10 24 USAA011292 1 20010925 A 5300 SEAT TRACK BOEING 737 737201 1384454 NM BS 1013 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 48384 22962 CLT - FOUND SEAT TRACK CORRODED 1 INCH BY 1 INCH, RBL 45 BS 1013 FLOOR LEVEL. FABRICATED AND INSTALLED NEW SEAT TRACK P ER SRM 51-10-2. (M) 2 L 7 2 4F A16WE 2001102400075 20011024 00075 NM 2001 10 24 AWXA200100529 1 20011001 A 5315 6545810519 FLOORBEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - C18 CK -C- CORROSION FOUND ON FLOORBEAM UPPER FLANGE AT BS 312, LBL 2 TO RBL 3, BEYOND SRM LIMITS. MAINTENANCE RE MOVED FLOORBEAM UPPER FLANGE FROM LBL 18 TO RBL 22, FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 SRM 53-10-51, FIG 205, PG 220 - 223. 2 L 7 2 4F RT A16WE 2001102400076 20011024 00076 NM 2001 10 24 AWXA200100530 1 20011003 A 5315 6546810 FLOORBEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - C18 CK -C- CORROSION FOUND ON FLOORBEAM UPPER FLANGE AT BS 967, RBL 15 TO RBL 19, BEYOND SRM LIMITS. MAINTENANCE REMOVED DAMAGED SECTION, FABRICATED REPAIR PARTS AND INSTALLED IAW B737 SRM 53-00-51, FIG 202, PG 207 - 211. 2 L 7 2 4F RT A16WE 2001102400077 20011024 00077 NM 2001 10 24 AWXA200100532 1 20011001 A 5315 65C3139229 FLOORBEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - C18 CK -C- CORROSION FOUND ON FLOORBEAM UPPER FLANGE AT BS 294.5, RBL 45.5, BEYOND SRM LIMITS AFTER CORROSION CLEA N UP. MAINTENANCE REMOVED DAMAGED SECTION OF FLOORBEAM FROM RBL 32 TO RBL 66, FABRICATED REPAIR PARTS AND INSTALLED IAW B737 SRM 53-10-51, FIG 205, PG 220 - 223. 2 L 7 2 4F RT A16WE 2001102400078 20011024 00078 NM 2001 10 24 AWXA200100534 1 20011002 A 5311 65613295 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 25400 YVR - C11 CK -C- CRACK FOUND ON FUSELAGE FRAME WEB AT BS 794.3, STR 24R, WL 160, .50 INCH LONG, (FWD OF AFT CARGO DOOR, DOOR SURROUND STRUCTURE). MAINTENANCE REMOVED DAMAGED SECTION, FABRICATED REPAIR PARTS AND INSTALLED IAW B737 SRM 51-70 -13 AND BOEING DWG'S 65-61329-5 & 65-47959 SHT 5. 2 L 7 2 4F RT A16WE 2001102400080 20011024 00080 NM 2001 10 24 AWXA200100535 1 20011004 A 5520 65498731 HINGE BRACKET BOEING 737 7373G7 1384595 NM ELEVATOR CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 25400 YVR - C11 CK -C- FRETTING AND MOUNT BOLT HOLE ELONGATION FOUND ON NR 5 & 6 RT ELEVATOR HINGE ATTACH BRACKETS, ELEV STA 1 76.54 AND 213.32 RESPECTIVELY. MAINTENANCE REMOVED THE ELEVATOR AND HINGE ATTACH BRACKETS AND REPAIRED IAW AWA ER 03-55 20-01283-SS2 REFERENCING WORK PERFORMED PER INSTRUCTIONS IN BOEING SB 737-55-1054. 2 L 7 2 4F RT A16WE 2001102400081 20011024 00081 NM 2001 10 24 DHL2001712017 1 20011020 A 2612 GROMMET BOEING 727 72729 1384007 NM NR 3 ENGINE DEFECTIVE A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 712DH 19401 NR 3 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED ON S/O PANEL AUXILIARY. REMOVED NR 3 FIRE LOOP CLAMP GROMMETS IAW B727 M M 26-11-00. OPERATIONAL CHECK SERVICEABLE. 2 L 7 3 4F A3WE 2001102400084 20011024 00084 NM 2001 10 24 DHL2001742501 1 20011002 A 5330 SKIN BOEING 727 727225 1384077 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK-FUSELAGE, AFT AIRSTAIRS, LT SIDE AT TOP CUTOUT AREA FOR AIRSTAIRS FUSELAGE SKIN HAS CRACK AT CORNER OF CUTOUT BS 1222. ROUTED OUT CRACK AREA OF FUSELAGE AFT 1222 AS PER B727 SRM 51-10-01. PERFORMED HFEC IAW B727 NDT MANUAL 51-0 0-00, PART 6 FIG 4. NO CRACKS FOUND AT REWORKED AREA. 2 L 7 3 4F A3WE 2001103000047 20011030 00047 NM 2001 10 30 DHL2001742502 1 20011002 A 5320 ATTACH ANGLE BOEING 727 727225 1384077 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, RT FWD FUSE FAIRING ATTACH ANGLE CRACKED STA 720 RBL 6. STOP DRILLED CRACK AT RT FWD FUS FAIRING ATTACH ANG LE STA 720 RBL 6 AS PER B727 SRM 51-10-1. ACCOMPLISHED NDT INSPECTED AROUND STOP HOLE, NO CRACK NOTED. INSTALLED DOUBL ER REPAIR AT RT FWD FUS FAIRING ATTACH ANGLE PER B727 SRM 51-40-3. 2 L 7 3 4F A3WE 2001103000048 20011030 00048 NM 2001 10 30 DHL2001742503 1 20011003 A 5720 CHANNEL BOEING 727 727225 1384077 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, LEFT WING T/E AREA, UPPER FIXED PANEL TOP OF I/B FLAP O/B JACKSREW HAS SUPPORT ANGLE CRACKED ALONG RIVET. R EMOVED AND REPLACED U-CHANEL SUPPORT ON LEFT WING T/E FIXED PANEL TOP OF I/B FLAP O/B JACKSCREW, IAW B727-SRM 51-10-1. 2 L 7 3 4F A3WE 2001103000049 20011030 00049 NM 2001 10 30 DHL2001742504 1 20011003 A 5720 ANGLE BOEING 727 727225 1384077 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, RT WING L/E INTERIOR AT WS 130, FOUND CRACK DAMAGE TO UPPER ANGLE BETWEEN UPPER SKIN AND STA 130 RIB. REMOV ED UPPER ANGLE AT RT WING L/E INTERIOR AT WS 130 BETWEEN UPPER SKIN AND STA 130 RIB IAW B727 SRM 51-30-2. INSTALLED UPP ER ANGLE AT RT WING L/E INTERIOR IAW B727 SRM 51-03-2. 2 L 7 3 4F A3WE 2001110900041 20011109 00041 NM 2001 11 9 DHL2001742505 1 20011004 A 5320 PLATE BOEING 727 727225 1384077 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C CHECK- AFT CABIN HAS SHEAR WEB PLATE HAS CRACK AROUND BOLT, AND BOLT IMPROPERLY INSTALLED BS 1176 RBL 30. REMOVED FASTENER AND CUT OUT DAMAGE AREA FOR CRACK AT AFT CABIN STA 1187 RBL 30 CUT OUT SIZE .75 AND .5 INCH AS PER B727 SRM 51- 40-2. REMOVED AND REPLACED DOUBLER AT CABIN BS 1176 RBL 30 PER B727 SRM 51-40-2 FIG 1. 2 L 7 3 4F A3WE 2001103000050 20011030 00050 NM 2001 10 30 DHL2001742506 1 20011004 A 5320 WEB BOEING 727 727225 1384077 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, AFT CABIN HAS SHEAR WEB PLATE WITH CORROSION IN TWO PLACES BS 1166 & RBL 15. CUT OUT CORNER AREA OF SHEAR W EB AT BS 1148 & 1166 RBL 15 INCHES. INSTALLED DOUBLER REPAIR AT BS 1148 AND 1166 AS PER B727 SRM 51-40-2 FIG 1. 2 L 7 3 4F A3WE 2001102400085 20011024 00085 NM 2001 10 24 DHL2001742507 1 20011004 A 5711 SPAR BOEING 727 727225 1384077 NM WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, LIGHT CORROSION OF FWD SIDE OF FULSE SPAR ABOVE O/B FLAP POSITION TRANSMITTER MKD. 2 L 7 3 4F A3WE 2001102400088 20011024 00088 NM 2001 10 24 DHL2001742508 1 20011004 A 5711 SPAR BOEING 727 727225 1384077 NM RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK- RT WING REAR AUX SPAR AT WS 294. FOUND CORROSION TO FWD/UPPER ANGLE. 2 L 7 3 4F A3WE 2001102400089 20011024 00089 NM 2001 10 24 DHL2001742509 1 20011004 A 5350 SKIN BOEING 727 727225 1384077 NM TAIL CONE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, TAIL CONE UPPER SIDE RT AFT AREA. SKIN HAS THREE SMALL HOLES. (RED MARKED) 2 L 7 3 4F A3WE 2001102400090 20011024 00090 NM 2001 10 24 DHL2001742510 1 20011005 A 5532 SKIN BOEING 727 727225 1384077 NM VERTICAL STAB ERODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, VERTICAL STAB L/E PANEL NR 9502 AT LOWER SECTION HF ANTENNA IS ERODED. 2 L 7 3 4F A3WE 2001102400091 20011024 00091 NM 2001 10 24 DHL2001742511 1 20011005 A 5321 FLOOR PANEL BOEING 727 727225 1384077 NM LAVATORY CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK- FWD LAV FLOOR PANEL IS CORRODED, MARKED. 2 L 7 3 4F A3WE 2001102400092 20011024 00092 NM 2001 10 24 DHL2001742512 1 20011004 A 5753 SKIN BOEING 727 727225 1384077 NM T/E FLAP DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, RIGHT WING INBOARD FLAP AFT LOWER SKIN HAS PITTED AREA IN TWO PLACES INBOARD AND MID SECTION OF FLAP. 2 L 7 3 4F A3WE 2001102400093 20011024 00093 NM 2001 10 24 DHL2001742513 1 20011004 A 5711 SPAR BOEING 727 727225 1384077 NM WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, CRACK IN FULSE SPAR WEB NR 4 FLAP TRACK, MKD. 2 L 7 3 4F A3WE 2001102400094 20011024 00094 NM 2001 10 24 DHL2001742514 1 20011004 A 5522 SKIN BOEING 727 727225 1384077 NM ELEVATOR DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, RT ELEVATOR TOP SURFACE I/B (CLOSE TO TAB I/B AREA) SHOW A 2 X 4 INCHES. TEMPORARY REPAIR. 2 L 7 3 4F A3WE 2001102400095 20011024 00095 NM 2001 10 24 DHL2001742515 1 20011005 A 5730 DOUBLER BOEING 727 727225 1384077 NM LT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, LT WING ROOT T/E (FALSE SPAR) LWR PANEL ABOVE GEAR, OLD REPAIR IS COMING OFF AT TOP SIDE. 2 L 7 3 4F A3WE 2001102400096 20011024 00096 NM 2001 10 24 DHL2001742516 1 20011008 A 7110 SKIN BOEING 727 727225 1384077 NM NR 2 COWLING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, NR 2 ENG, FWD LT COWL FWD LOWER CORNER, SKIN EDGE AND INTERIOR ANGLE DOUBLER IS CORRODED. 2 L 7 3 4F A3WE 2001102400097 20011024 00097 NM 2001 10 24 DHL2001742517 1 20011010 A 5320 SUPPORT BOEING 727 727225 1384077 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, AFT BAG BIN, SIDE WALL TO FLOOR, SUB FLOOR ABOVE 55R 27L IS CRACKED AT STA 1148, MARKED. 2 L 7 3 4F A3WE 2001102400098 20011024 00098 NM 2001 10 24 DHL2001742518 1 20011012 A 5730 SKIN BOEING 727 727225 1384077 NM WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, PANEL ABOVE NR 1 FLAP TRANSMISSION HAS A TEMPORARY REPAIR. 2 L 7 3 4F A3WE 2001102400099 20011024 00099 NM 2001 10 24 DHL2001742519 1 20011016 A 7110 SKIN BOEING 727 727225 1384077 NM NR 3 COWLING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, ENG NR 3 UPPER COWL, UPPER LATCH CUTOUT AT STA 175.70 HAS SKIN CRACK. 2 L 7 3 4F A3WE 2001102400100 20011024 00100 NM 2001 10 24 DHL2001742520 1 20011009 A 5330 SKIN BOEING 727 727225 1384077 NM FUSELAGE BULGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, LOWER FUSELAGE HAS BULGING SKIN AT BS 1050 AND STRINGER L28. 2 L 7 3 4F A3WE 2001102400101 20011024 00101 NM 2001 10 24 DHL2001742521 1 20011010 A 5320 WEB BOEING 727 727225 1384077 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, AFT CABIN HAS CORROSION AT LWR WEB STA 1177 & RBL 17. 2 L 7 3 4F A3WE 2001102400102 20011024 00102 NM 2001 10 24 DHL2001742522 1 20011009 A 5330 SKIN BOEING 727 727225 1384077 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 DURING C-CHECK, LOWER FUSELAGE HAS BULGING SKIN AT BS 1050 AND STRINGER R28. CUT OUT DAMAGED STRINGER 35 IAW B-727 SRM 53-10-3. REMOVED CORROSION ON INNER SKIN AT STATION 1050, STRINGER 28R, FOUND TO BE OUT OF LIMITS AS PER B-727 SRM 51- 10-6. CUT OUT CORRODED AREA AT LOWER SKIN AT BS 1050 STRINGER R28 IAW B-727 SRM 53-30-3. INSTALLED STRINGER IAW B-727 SRM 53-10-3 AND FUSELAGE DOUBLER REPAIR AS PER B-727 SRM 53-30-3. 2 L 7 3 4F A3WE 2001102400104 20011024 00104 WP 2001 10 24 DHL2001801226 1 20010922 A 5320 PLATE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 MAIN CARGO COMPT BEAM UPPER PLATE CRACKED 1 INCH STA 580.000 LBL 39. STOP DRILLED CRACK PER SRM 53-2-0 FIG 1 B. FABRIC ATED DOUBLER PER SRM 53-2-0 FIG 1B. INSTALLED DOUBLER PER SRM 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 2001102400105 20011024 00105 WP 2001 10 24 DHL2001801501 1 20011003 A 5320 ATTACH ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AFT CARGO COMPT - FLOOR LINING ATTACH ANGLE CRACKED 1 INCH BETWEEN STA 1360.000 AND L-35R. STOP DRILLED CRACK PER SRM 5 3-2-0 PG 2E-2F. FABRICATED ANGLE PER SRM 53-2-0 PG 2E-2F. INSTALLED ANGLE PER SRM 53-2-0 PG 2E-2F. 2 L 7 4 4F RT 4A25 2001102400106 20011024 00106 WP 2001 10 24 DHL2001801502 1 20011004 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 FWD CARGO COMPT-FLOOR SUPPORT ANGLE CRACKED .5 INCH AT STA 350.000 L-33R. STOP DRILLED CRACK PER SRM 53-2-0 PG 2E-2F. FABRICATED SUPPORT ANGLE PER SRM 53-2-0 PG2E-2F. INSTALLED ANGLE PER SRM 53-2-0 PG 2E-2F. 2 L 7 4 4F RT 4A25 2001102400107 20011024 00107 WP 2001 10 24 DHL2001801503 1 20011004 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 FWD CARGO COMPT-FLOOR SUPPORT ANGLE CRACKED .5 INCH AT STA 272.000, L33R. STOP DRILLED CRACK PER SRM 53-2-0 PG 2E-2F. FABRICATED ANGLE PER SRM 53020-0 PG 2E-2F. INSTALLED ANGLE PER SRM 53-2-0 PG 2E-2F. 2 L 7 4 4F RT 4A25 2001102400108 20011024 00108 WP 2001 10 24 DHL2001801504 1 20011003 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 FWD CARGO COMPT-FRAME AT STA 220.000, L-35L SHOWS .5 INCH CRACK. STOP DRILLED CRACK PER SRM 53-2-0 FIG 2. FABRICATED D OUBLER PER SRM 53-2-0-FIG 2. INSTALLED DOUBLER PER SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001102400109 20011024 00109 WP 2001 10 24 DHL2001801506 1 20011003 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 MAIN CARGO SEAT TRACK LUG WORN BETWEEN STA 500.000 AND STA 580.000. CUT DAMAGED AREA PER SRM 53-2-3 PG 49-50. FABRICAT ED 3 SPLICES. CONDITIONED NEW TRACK PER SRM 53-2-3 PG 40-50. INSTALLED SPLICES AND NEW TRACK PER SRM 53-2-3 PG 49-50. 2 L 7 4 4F RT 4A25 2001102400110 20011024 00110 WP 2001 10 24 DHL2001801507 1 20011006 A 5320 RIB DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 FWD CARGO LWR COMPT TRACK SUPPORT RIB CRACKED 1 INCH AT STA 90 L-34 R. STOP DRILLED CRACK PER SRM 53-2-0 FIG 1B. FABRI CATED DOUBLER PER SRM 53-2-0 FIG 1B. INSTALLED DOUBLER PER SRM 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 2001102400111 20011024 00111 WP 2001 10 24 DHL2001801508 1 20011004 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 FLT CABIN - ANGLE BROKEN AT STA 8.000, RBL-10. REMOVED BROKEN ANGLE PER SRM 53-2-0 FIG 1B. FABRICATED ANGLE PER SRM 53 -2-0 FIG 1B. INSTALLED NEW ANGLE PER SRM 51-1-21 PG 7. 2 L 7 4 4F RT 4A25 2001102400112 20011024 00112 WP 2001 10 24 DHL2001801509 1 20011001 A 5753 RIB DOUG DC8 DC873F 302199F WP T/E FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 RIGHT I/B FLAP RIB STA XW. 130.000, CRACKED. STOP DRILLED CRACK PER SRM 57-2-5 FIG 2. FABRICATED REINFORCING ANGLE PER SRM 57-2-5 FIG 2. INSTALLED REINFORCING ANGLE PER SRM 57-2-5. 2 L 7 4 4F RT 4A25 2001102400113 20011024 00113 WP 2001 10 24 DHL2001801510 1 20010927 A 5347 PLUG DOUG DC8 DC873F 302199F WP SEAT TRACK DETERIORATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 MAIN CARGO SEAT TRACK NR 32 LT TRACK PLUG DETERIORATED STA 320.000. CUT OUT DAMAGED PLUG PER SRM 53-2-3 PG 17-18. INST ALLED NEW PLUG (P/N 7452952-3) PER SRM 53-2-3 PG 17-18. 2 L 7 4 4F RT 4A25 2001102400114 20011024 00114 WP 2001 10 24 0103609607 1 20011016 A 5311 PRESSURE PANEL DOUG DC9 DC932 3022066 WP CRACKED A NWAA O OTHER O OTHER IN INSP/MAINT 1 GL 01 607NW 47232 During H CK ATL base Maintenance while accomplishing APB inspections per ref F a 1/2 inch crack was found in the upper i nboard bend radius of the 5910130-9 channel running downward along the radius. Material is made from .125" 2014-t6 QQ-A- 250/3. 2 L 7 2 4F A6WE 2001102400115 20011024 00115 WP 2001 10 24 0103589607 1 20011002 A 5312 PRESSURE PANEL DOUG DC9 DC932 3022066 WP CRACKED A NWAA O OTHER O OTHER IN INSP/MAINT 1 GL 01 607NW 47232 During H-ck at ATL base, four cracks were found in the horizontal pressure panel at station 105, X=+-35. All cracks were less than 2 inches in length. material 9910073-313 web made from .040 2024-t3 aluminum clad sheet. 2 L 7 2 4F A6WE 2001102400116 20011024 00116 WP 2001 10 24 0103599607 1 20011002 A 5312 BULKHEAD DOUG DC9 DC932 3022066 WP CRACKED A NWAA O OTHER O OTHER IN INSP/MAINT 1 GL 01 607NW 47232 During H-ck at ATL base maintenance, two cracks were found in the station 756 bulkhead. The cracks are located in the up per ends of the verticle stiffeners at x=-11 (.070)"(p/n 9958212-10) and x=-22 (1.0) "(p/n 9958212-121). Material 2014-t 6511. 2 L 7 2 4F A6WE 2001102400117 20011024 00117 WP 2001 10 24 0103569607 1 20011008 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A NWAA O OTHER O OTHER IN INSP/MAINT 1 GL 01 607NW 47232 DURING M-CK IN ATL, CORROSION HAS BEEN FOUND ON STA 160 CABIN FLOOR BEAM CAP AFT FACING FLANGE WHERE THE OUTBOARD GALLEY MOUNT IS ATTACHED. IT WAS ELECTED TO TO TRIM THE AFT FACING FLANGE TO REMOVE THE DAMAGE. THE RADIUS OF THE CAP WAS NOT TRIMMED. 7075-T6511 2 L 7 2 4F A6WE 2001102400118 20011024 00118 WP 2001 10 24 DHL2001801511 1 20010927 A 5347 PLUG DOUG DC8 DC873F 302199F WP SEAT TRACK WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 MAIN CARGO SEAT TRACK NR 3 RT TRACK LUG WORN AT STA 740.000. CUT OUT DAMAGED PLUG PER SRM 53-2-3 PG 17-18. INSTALLED N EW PLUG (P/N 7452952-3) PER SRM 53-2-3 PG 17-18. 2 L 7 4 4F RT 4A25 2001102400119 20011024 00119 WP 2001 10 24 DHL2001801512 1 20010928 A 5320 WEB DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 MAIN CARGO SUB FLOOR CRACKED .5 INCH AT STA 1540.000 RBL 10. STOP DRILLED CRACK PER SRM 53-2-0 FIG 18. FABRICATED DOUB LER PER SRM 53-2-0 FIG 18. INSTALLED DOUBLER PER SRM 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 2001102400120 20011024 00120 WP 2001 10 24 DHL2001801513 1 20010929 A 5720 ANGLE DOUG DC8 DC873F 302199F WP WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 CENTER WING BEAM LOWER SUPPORT ANGLE CRACKED 1 INCH AT STA 683 XCW 23 RT. REMOVED CRACKED SUPPORT ANGLE PER SRM 51-1-20 D. FABRICATED NEW ANGLE PER SRM 53-20-0. INSTALLED NEW ANGLE PER SRM 51-1-20D PG 21. 2 L 7 4 4F RT 4A25 2001102400121 20011024 00121 WP 2001 10 24 DHL2001801514 1 20010927 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 MAIN CARGO COMPT SEAT TRACK NR 3 AT STA 320.00 LUG IS WORN. CUT OUT DAMAGED AREA PER SRM 53-2-3 PG 17 - 18. INSTALLED TRACK PLUG PER SRM 53-2-3 PG 17-18. 2 L 7 4 4F RT 4A25 2001102400122 20011024 00122 WP 2001 10 24 DHL2001801515 1 20010927 A 5347 PLUG DOUG DC8 DC873F 302199F WP SEAT TRACK WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 MAIN CARGO SEAT TRACK NR 1 RT LUG WORN AT AT STA 510.000. CUT OUT DAMAGED PLUG PER SRM 53-2-3 PG 17-18. INSTALLED NEW PLUG (P/N 745295-3) PER SRM 53-2-3 PG 12. 2 L 7 4 4F RT 4A25 2001102400123 20011024 00123 WP 2001 10 24 DHL2001801516 1 20010925 A 5347 PLUG DOUG DC8 DC873F 302199F WP SEAT TRACK DETERIORATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 MAIN CARGO NR 2 LT SEAT TRACK PLUG DETERIORATED STA 1140.000. CUT OUT DAMAGED PLUG PER SRM 53-2-3 PG 17-18. INSTALLED N EW PLUG (P/N 7452952-3) PER SRM 53-2-3 PG 17-18. 2 L 7 4 4F RT 4A25 2001102400124 20011024 00124 WP 2001 10 24 DHL2001801517 1 20010925 A 5210 INTERCOSTAL DOUG DC8 DC873F 302199F WP PAX DOOR BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AFT PASSENGER DOOR, VERTICAL INTERCOSTAL PLATE BROKEN. REMOVED BROKEN PLATE PER SRM 51-121 PG 1. FABRICATED NEW PLATE PER SRM 52-2-3 FIG 10. INSTALLED NEW PLATE PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001102400125 20011024 00125 WP 2001 10 24 DHL2001801518 1 20010101 A 5720 STRUCTURE DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 RT WING L/E INNER PART CRACKED 2 INCHES AT HOT AIR LINER XFS 716.000. STOP DRILLED CRACK PER SRM 57-2-0 FIG 2. FABRICA TED DOUBLER PER SRM 57-2-0 FIG 62. INSTALLED DOUBLER PER SRM 572-0 FIG 2. 2 L 7 4 4F RT 4A25 2001102400126 20011024 00126 WP 2001 10 24 DHL2001801519 1 20011005 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 RIGHT WING CENTER LEADING EDGE INTERIOR RIB CRACKED .5 INCH AT XFS 304. STOP DRILLED CRACK PER SRM 57-2-0 PG 1-2. FABR ICATED REINFORCING ANGLE PER SRM 57-2-0 PG 1-2. INSTALLED ANGLE PER SRM 57-2-0 PG 1-2. 2 L 7 4 4F RT 4A25 2001102400128 20011024 00128 WP 2001 10 24 DHL2001801520 1 20011003 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 RIGHT WING CENTER LEADING EDGE INTERIOR RIB CRACKED .5 INCH AT XFS 310. STOP DRILLED CRACK PER SRM 57-2-0 PG 1-2. FABR ICATED REINFORCING ANGLE PER SRM 57-2-0 PG 1-2. INSTALLED ANGLE PER SRM 57-2-0 PG 1-2. 2 L 7 4 4F RT 4A25 2001102400129 20011024 00129 WP 2001 10 24 DHL2001801521 1 20011002 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP FUSELAGE BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AFT ACCESSORY COMPT-FLOOR SUPPORT ANGLE BROKEN STA 1740.000 RBL 20. REMOVED BROKEN FLOOR SUPPORT SECTION PER SRM 53-2-0 . FABRICATED REINFORCING ANGLE PER SRM 53-2-0. INSTALLED ANGLE PER SRM 53-2-0 FIG 18. 2 L 7 4 4F RT 4A25 2001102400131 20011024 00131 WP 2001 10 24 DHL2001801522 1 20010925 A 5720 CHANNEL DOUG DC8 DC873F 302199F WP NR 4 MAIN TANK CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 NR 4 MAIN TANK CHANNEL ASSY CRACKED (REF 505D ACCESS DOOR). REMOVED AND REPLACED CHANNEL ASSY PER S/B 57-65 PG 1-5. LE AK CHECK COMPLIED WITH. 2 L 7 4 4F RT 4A25 2001102900075 20011029 00075 NM 2001 10 29 SABA011055 1 20011021 A 3350 6104789 BATTERY PACK DHAV DHC8 DHC8103 1386005 NM CABIN DISCHARGED A SABA O OTHER L NO TEST TX TAXI/GRND HDL 1 SO 33 801WP 086 AIRCRAFT 801 FLIGHT 5248, CHARLOTTE TO TALLAHASSEE; DURING PRE-FLIGHT INSPECTION THE AIRCREW FOUND THE CABIN EMERGENCY L IGHTS INOP. MAINTENANCE FOUND THE LIGHT SWITCH ON. REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACKS. SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001102400139 20011024 00139 WP 2001 10 24 DHL2001801523 1 20010929 A 5720 CHANNEL DOUG DC8 DC873F 302199F WP NR 4 MAIN TANK CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 NR 4 MAIN TANK-CHANNEL ASSY CRACKED (REF ACCESS DOOR 505C). REMOVED AND REPLACED CHANNEL ASSY PER S/B 57-65 PG 1-5. LE AK CHECK ACCOMPLISHED. 2 L 7 4 4F RT 4A25 2001102400140 20011024 00140 WP 2001 10 24 DHL2001801524 1 20010930 A 5720 CHANNEL DOUG DC8 DC873F 302199F WP NR 1 MAIN TANK CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 NR 1 MAIN TANK-CHANNEL ASSY CRACKED (REF ACCESS DOOR NR 505 C). REMOVED AND REPLACED CHANNEL ASSY PER S/B57-65 PG 1-5, LEAK CHECKED. 2 L 7 4 4F RT 4A25 2001102400141 20011024 00141 WP 2001 10 24 DHL2001801525 1 20010928 A 5320 WEB DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 MAIN CARGO LBL 32 SUBFLOOR CRACKED .5 INCH STA 640.000. STOP DRILLED CRACK PER SRM 53-2-0 FIG 1 B. FABRICATED DOUBLER PER SRM 53-2-0 FIG 1 B. INSTALLED DOUBLER PER SRM 53-2-0 FIG 1 B. 2 L 7 4 4F RT 4A25 2001103100008 20011031 00008 CE 2001 10 31 GLBA2001218 1 20011021 A 3260 404EN16 DOWNLOCK SWITCH BEECH 1900 1900D 1154162 CE RT MLG FAILED A GLBA K NONE N FALSE WARNING CR CRUISE 1 CE 01 204GL UE204 LANDING GEAR WARNING HORN SOUNDS CONTINUOUSLY. REPLACED RIGHT MAIN GEAR DOWNLOCK SWITCH, OPS CHECKED SYSTEM SATISFACTOR Y. 2 L 7 2 4T RT A24CE 2001102400142 20011024 00142 2001 10 24 MALA010758 4 20011015 A 3425 COMPUTER SAAB SF340 340B 7860101 EU COCKPIT MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 452XJ 340B452 DURING FLIGHT 3399, YELLOW HEADING ON EHSI COMING ON INTERMITTENTLY DURING FLIGHT. ATTEMPTED TO SAVE SEVERAL TIMES DURI NG STRAIGHT AND LEVEL, NO CORRECTIONS NOTICED. MAINTENANCE REINITIALIZED BOTH AHRS SYSTEMS. ALL CHECKS GOOD IAW SF-340 MM CHAP 34. 2 L 7 2 4T RT A52EU 2001102400143 20011024 00143 EU 2001 10 24 MALA010759 1 20011016 A 3020 44730501 MODULE SAAB SF340 340B 7860101 EU LT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 142XJ 142 SHORTLY AFTER T/O FROM FWA THE LT ENGINE INTAKE FAILED. CREW RAN QRH AND SYSTEM FAILED AGAIN (APPROXIMATELY EVERY 15 SE CONDS). AIR RETURN TO FWA. MAINTENANCE REPLACED LT DE-ICE MODULE P/N 44730-501, S/N ON A00122 IAW SF340 MM, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2001102400144 20011024 00144 SO 2001 10 24 COMA0110154 1 20011022 A 7931 3006084 CAP EMB 120 EMB120RT SO A COMA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 01 259CA 1252 FLIGHT #5057. DURING CRUISE FLIGHT THE RIGHT ENGINE OIL PRESSURE DROPPED BELOW 40 PSI, CREW DECLARED AN EMERGENCY AND P ERFORMED AN INFLIGHT SHUT DOWN OF THE RIGHT ENGINE.REPLACED THE RIGHT ENGINE OIL SERVICING FILLER CAP AND NECK. 2 L 7 2 4T RT A31SO 2001102900130 20011029 00130 EA 2001 10 29 COMA0160842 1 20011022 A 2751 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT ACTIVATED A COMA K NONE J WARNING INDICATION DE DESCENT 1 SO 01 420CA 7451 FLIGHT 5981 DURING DESCENT INTO BHM RECEIVED A FLAP INDICATION CAUTION MESSAGE AT 30 DEGREE FLAP POSITION. COMPLIED WIT H AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3, (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2001102400150 20011024 00150 EU 2001 10 24 MALA010760 1 20011018 A 2751 CIRCUIT BREAKER SAAB SF340 SF340A 7850100 EU COCKPIT TRIPPED A MALA L ABORTED APPROACH J WARNING INDICATION LD LANDING 1 GL 15 99XJ 340A099 DURING FLIGHT 2774 ON FINAL, THE FLAPS DID NOT COME DOWN ON THE MISSED APPROACH. NOTICED FLAP INDICATOR C/B POPPED. RE SET AND EVERYTHING WAS NORMAL. MAINTENANCE INSPECTED FLAPS FOR ANY OBVIOUS DEFECTS, NONE NOTED. PERFORMED OPERATIONAL CHECK OF FLAP SYSTEM. ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2001102400152 20011024 00152 WP 2001 10 24 MWEA011383 1 20011017 A 5313 5911410241 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 REMOVED AND REPLACED LONGERON 25 LEFT FROM STATION 237 - 400 DUE TO SEVERAL SPOTS OF DEEP CORROSION. REMOVED AND REPLAC ED SECTION OF LONGERON. 2 L 7 2 4F A6WE 2001102400155 20011024 00155 WP 2001 10 24 MWEA011400 1 20011017 A 5320 593607111 INTERCOSTAL DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 MID CARGO BAY INTERCOSTAL BETWEEN LONGERON 29 RIGHT THROUGH LONGERON 30 HAS LIGHT CORROSION AND DOUBLE DRILLED HOLES BET WEEN STATION 630-STATION 636. REMOVED AND REPLACED INTERCOSTAL AND FABRICATED AND INSTALLED CLIP. 2 L 7 2 4F A6WE 2001102400156 20011024 00156 WP 2001 10 24 MWEA011403 1 20011018 A 2120 5910244125 DUCT DOUG DC9 DC932 3022066 WP A/C BAY CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 LOUD (RUSHING AIR) SOUND FROM AFT CABIN AREA. ALSO RIGHT TEMP CONTROL VALVE WHEN FULL HOT, BUT CABIN TEMP SHOWS FULL CO LD. TEMP MODULATION (MANUAL MODE) HAS NO EFFECT. FOUND RIGHT TEMP CONTROL VALVE OUTLET DUCT CRACKED AND COUPLING HOSE DETERIORATED. INSTALLED NEW WELDED DUCT ASSEMBLY AND HOSE COUPLING. OPERATIONAL AND LEAK CHECK GOOD. 2 L 7 2 4F A6WE 2001102900076 20011029 00076 NM 2001 10 29 SABA011056 1 20011022 A 3350 6104789 BATTERY PACK DHAV DHC8 DHC8103 1386005 NM CABIN DISCHARGED A SABA O OTHER L NO TEST TX TAXI/GRND HDL 1 SO 33 801WP 086 AIRCRAFT 801 FLIGHT 5019 CHARLOTTE TO AUGUSTA; EMERGENCY CABIN LIGHTS WOULD NOT TEST DURING PREFLIGHT. MAINTENANCE REMO VED AND REPLACED THE EMERGENCY BATTERIES DUE TO LOW VOLTAGE. SYSTEM GROUND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001102400160 20011024 00160 NM 2001 10 24 PCAA0110120 1 20011017 A 5347 85330217001 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 838EX 220 DURING C-INSPECTION LEFT AFT SEATRAIL AT STATION 525 TO STATION 595 HAS CORROSION BEYOND LIMITS. SEATRAIL SECTION REPLA CED IAW DEHAVILLAND DRAWINGS RD8-53-4472, RD8-51-015 ASSEMBLY DRAWINGS 85330115, 85330112, 85330453, 85330217 AND CALLAH AN REPAIR SERVICES DER CAS-AAL20, CAS-AAL21. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001102400161 20011024 00161 NM 2001 10 24 QXEA0101645 1 20011004 A 5410 STRUCTURE DHAV DHC8 DHC8202 2809007 NM RT NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - RIGHT NACELLE AFT WHEEL WELL CHAFED AT ROCK GUARD BOTTOM TWO ATTACH POINTS. REPAIRED IAW SRM 51-20-16, SRM 51-20- 36 AND SRM 51-20-51. 2 H 7 2 4T RT A13NM 2001102400162 20011024 00162 NM 2001 10 24 QXEA0101646 1 20011005 A 5412 HEAT SHIELD DHAV DHC8 DHC8202 2809007 NM RT NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - RIGHT NACELLE OUTBOARD DISHED HEAT SHIELD CHAFED TOP OF FINGERNAIL DECK. REPAIRED IAW DHC-8 SRM 51-40-11, PAGE 1. 2 H 7 2 4T RT A13NM 2001102400163 20011024 00163 NM 2001 10 24 QXEA0101647 1 20011004 A 5540 RUDDER DHAV DHC8 DHC8202 2809007 NM TAIL CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - TRAILING RUDDER HAS CHAFE DAMAGE AT RIVET LINE, RIGHT-HAND SIDE 12 INCHES FROM TOP. REPAIRED IAW DHC-8-200 SRM 55 -40-11, FIGURE 1 ITEM 12, SRM 51-20-16 AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2001102400165 20011024 00165 WP 2001 10 24 0103559759 1 20011003 A 5310 PRESSURE PANEL DOUG DC9 DC941 302207N WP CRACKED A NWAA O OTHER O OTHER IN INSP/MAINT 1 GL 01 759NW 47287 EA 97-185179 During H-ck at ATL Base Maintenance a crack was found in the horizontal pressure panel Web P/N 9910073-3-13 at sta 105 and X 25rh. the crack is typical and was trimmed out. The repair was accomplished IAW NWA tRM 53-10-02 dated april 18/01. Material .040" 2024-t3 al clad sheet. 2 L 7 2 4F A6WE 2001102400166 20011024 00166 NM 2001 10 24 QXEA0101648 1 20011011 A 5230 STOP FITTING DHAV DHC8 DHC8202 2809007 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - BAGGAGE DOOR LOWER AFT PRESSURE STOP FITTING ON DOOR IS GOUGED ON LOWER OUTER EDGE. REPAIRED IAW HORIZON AIR EA 2 -52-111. 2 H 7 2 4T RT A13NM 2001102400167 20011024 00167 NM 2001 10 24 QXEA0101649 1 20011007 A 5714 WEB DHAV DHC8 DHC8202 2809007 NM CENTER WING BOX CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - CENTER WING FORWARD WING BOX AT STATION YW02.858 AND X374.500 THERE IS A CRACK IN THE WEB. REPAIRED IAW RD 8-53-5 437. 2 H 7 2 4T RT A13NM 2001102400169 20011024 00169 NM 2001 10 24 QXEA0101650 1 20011006 A 5540 FITTING DHAV DHC8 DHC8202 2809007 NM RUDDER CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - AFT RUDDER LOWER HINGE RADIUS ROD LUG HAS CHAFE DAMAGE. REPAIRED IAW RD 8-55-132, STEP 1. 2 H 7 2 4T RT A13NM 2001102400172 20011024 00172 NM 2001 10 24 QXEA0101651 1 20011007 A 5320 ANGLE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - BLEED AIR SUPPORT ANGLE, CENTER WING FORWARD OF WING BOX BLEED AIR SUPPORT ANGLE CRACKED IN RADIUS ON RIGHT-HAND S IDE. REPAIRED IAW RD 8-53-5437 AND DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001102400174 20011024 00174 NM 2001 10 24 QXEA0101673 1 20011011 A 5720 ANGLE DHAV DHC8 DHC8202 2809007 NM RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - RIGHT-HAND WING AT FORWARD SPAR A Z-ANGLE SUPPORT IS CRACKED AT TOP AND DOWN TWO RIVETS. REPLACED Z-ANGLE IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001102400175 20011024 00175 NM 2001 10 24 QXEA0101674 1 20011008 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - LEFT-HAND INBOARD SEAT TRACK HAS CORROSION AT INBOARD CAMLOCK RECEPTACLE CUTOUTS BETWEEN STATIONS X224.0 AND X262. REPAIRED IAW RD 8-53-4473, RD 8-53-2295 AND RD 8-53-1102. 2 H 7 2 4T RT A13NM 2001102400176 20011024 00176 NM 2001 10 24 QXEA0101675 1 20011005 A 5753 FLAP DHAV DHC8 DHC8202 2809007 NM LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - LEFT-HAND OUTBOARD FLAP JUST OUTBOARD OF THE NACELLE OF WING STATION YW174.0 IS CHAFED. REPAIRED IAW DHC-8 SRM 51 -20-16 AND SRM 51-20-51. 2 H 7 2 4T RT A13NM 2001102400177 20011024 00177 NM 2001 10 24 QXEA0101676 1 20011010 A 5753 FLAP DHAV DHC8 DHC8202 2809007 NM RT< WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - LEFT-HAND AND RIGHT-HAND WING TRAILING EDGE FRAMES ARE CAUSING CHAFING DAMAGE TO OUTBOARD FLAP AT YW171.20. REPAI RED IAW RD 8-57-1549. 2 H 7 2 4T RT A13NM 2001102400178 20011024 00178 NM 2001 10 24 QXEA0101677 1 20011005 A 5310 DOOR FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - CORROSION FOUND UNDER SEVERAL NUT PLATES AT CARGO BAY DOOR SURROUND STRUCTURE, LOWER THRESHOLD. REPAIRED IAW DHC- 8 SRM 53-00-16, PAGE 3 TABLE 1, SHEET 2. 2 H 7 2 4T RT A13NM 2001102400180 20011024 00180 EU 2001 10 24 QXEA0101686 1 20011015 A 3350 6008903 BATTERY PACK FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 477AU 9353 4271 11226 PDX - LOWER EGRESS LIGHTS ARE INOPERABLE. REMOVED AND REPLACED EGRESS LIGHT BATTERY PACK. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001102400181 20011024 00181 EU 2001 10 24 QXEA0101687 1 20011018 A 3350 6008903 BATTERY PACK FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 498US 7603 3632 11181 PDX - THE AFT 3 CABIN EMERGENCY LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED THE NUMBER 7 BATTERY PACK. OPERATIONA L CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001102400182 20011024 00182 NM 2001 10 24 QXEA0101688 1 20011019 A 3350 82410162007 CONTROL BOX DHAV DHC8 DHC8102 2809003 NM CABIN MALFUNCTIONED A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 830PH 314 SEA- EMERGENCY LIGHTS ILLUMINATED IN FLIGHT. RECYCLED SWITCH AS PER CHECKLIST. LIGHTS ILLUMINATED AGAIN AFTER A SHORT WHILE. REMOVED AND REPLACED EMERGENCY LIGHT CONTROL BOX. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001102400185 20011024 00185 EU 2001 10 24 QXEA0101689 1 20011018 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 475AU 11222 GEG- EXIT SIGN AT FORWARD CABIN INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURN ED TO SERVICE. 2 L 7 2 4F RT A20EU 2001102400186 20011024 00186 EU 2001 10 24 QXEA0101690 1 20011018 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 497US 11173 BOI- EXIT LOCATING SIGN AT GALLEY ENTRANCE HAS SEVERAL BULBS INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001102400187 20011024 00187 EU 2001 10 24 QXEA0101691 1 20011015 A 3350 RELAY FOKKER F28 F28MK4000 4990810 EU COCKPIT FAILED A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 499US 11182 PDX- COCKPIT EMERGENCY LIGHTS ILLUMINATED WHEN EXTERNAL POWER IS ON. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHTS RELA Y LV3-164. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001102400188 20011024 00188 2001 10 24 SWAA012830 4 20011015 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2001102400189 20011024 00189 NM 2001 10 24 SWAA012836 1 20011016 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICE CORRODED AT BS 968, STR 25L. REMOVED AND REPLACED STR SPLICE PER SRM . 2 L 7 2 4F RT A16WE 2001102400190 20011024 00190 NM 2001 10 24 SWAA012840 1 20011016 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED PM CHECK, FOUND FWD ENTRY DOOR OVERHEAD AND SEVERAL BULLNOSE EMERGENCY EXIT LIGHTS INOP. REMOVED AND R EPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001102400191 20011024 00191 NM 2001 10 24 SWAA012842 1 20011017 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 312, LBL 11.0. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2001102400192 20011024 00192 NM 2001 10 24 SWAA012843 1 20011017 A 5315 6546568 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED 1/2D CHECK, FOUND LOWER CHORD BULGED AT 1016 BULKHEAD, BL 0. REMOVED AND REPLACED LOWER CHORD PER SRM. 2 L 7 2 4F RT A16WE 2001102900063 20011029 00063 WP 2001 10 29 IXXA0100066O 1 20011022 A 2752 57726413 ACTUATOR DOUG DC8 DC871F 302199D WP T/E FLAP LEAKING A IXXA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SW 11 822BX 84635 462 45813 DURING DESCENT FROM DXB TO BRU, THE FLIGHT CREW NOTICED A DECLINE IN THE THE HYDRAULIC QUANTITY SYSTEM. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND CONTINUED TO BRU FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND LOC ATED A DEFECTIVE FLAP ACTUATOR ON THE LEFT INBOARD SIDE. MAINTENANCE REPLACED THE ACTUATOR AND PERFORMED AN OPERATIONAL CHECK IN ACCORDANCE WITH THE DACO MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2001102400193 20011024 00193 WP 2001 10 24 IXXA0100068S 1 20010717 A 5313 LONGERON DOUG DC8 DC862 3021970 WP F.S. 21 CORRODED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 31CX 73325 2986 45911 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED AT FUSELAGE STATION 902 BETWEEN LONGERONS LONGERON 21R AND LON GERONS 20R. REPAIR ACCOMPLISHED REOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION REPAIR FILLERS AN EXTERNAL DOUBLER S IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING ORDER 53-DC8-1808. 2 L 7 4 4F 4A25 2001102400194 20011024 00194 WP 2001 10 24 IXXA0100067S 1 20010725 A 5315 FLOORBEAM DOUG DC8 DC862 3021970 WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 31CX 73325 2986 45911 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE FLOOR BEAM AT FUSELAGE STATION 879, LBL-61. REPAIR ACCOMP LISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A BEAM FILLER AND REPAIR SPLICE ANGLES IN ACCORDANCE WIT H DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING ORDER 51-DC8-1809. 2 L 7 4 4F 4A25 2001102400196 20011024 00196 2001 10 24 SWAA012844 4 20011016 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 645SW 28330 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001102400197 20011024 00197 NM 2001 10 24 SWAA012845 1 20011016 A 5753 6546486 PANEL BOEING 737 7373A4 1384585 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 DURING SCHEDULED C4 CHECK, FOUND T/E INBOARD MIDFLAP WEDGE PANEL DELAMINATED AT OUTBOARD UPPER SURFACE. REMOVED AND REP LACED WEDGE PANEL PER MM. 2 L 7 2 4F RT A16WE 2001102400199 20011024 00199 NM 2001 10 24 SWAA012848 1 20011017 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 350SW 24409 EMERGENCY FLASHLIGHT INOP IN FWD CABIN. RESEATED FLASHLIGHT PER MM, OPS CK GOOD. 2 L 7 2 4F RT A16WE 2001102400201 20011024 00201 NM 2001 10 24 SWAA012854 1 20011014 A 2121 65771 FAN BOEING 737 7373H4 1384600 NM E/E BAY OVERHEATED A SWAA O OTHER J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 380SW 26587 EQUIPMENT COOLING LIGHT ILLUMINATED IN FLIGHT (350) FOLLOWED BY BURNING ODOR. SELECTED ALTERNATE, LIGHT EXTINGUISHED AN D SMELL RETURNED TO NORMAL. REMOVED AND REPLACED EQUIPMENT COOLING FAN PER MM. 2 L 7 2 4F RT A16WE 2001102400206 20011024 00206 NM 2001 10 24 SWAA012857 1 20011017 A 7920 3352546033 LINE BOEING 737 7375H4 138449D NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE LOOSE A SWAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 522SW 26564 722394 ENGINE SHUT DOWN, DECLARED EMERGENCY. DURING FLIGHT SHUT DOWN NR 2 ENGINE 0 OIL QUANTITY, LOW OIL PRESS. FOUND NR 5 B EARING SUMP EXTERNAL OIL LINE LOOSE. TIGHTENED AND SAFETIED, SERVICED AND RAN ENG. NO LEAKS NOTED AND OPS CK GOOD PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2001102400207 20011024 00207 NM 2001 10 24 SWAA012858 1 20011018 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM CABIN DEFECTIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 FOUND FWD SERVICE DOOR OVERHEAD EMERGENCY LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED FWD SVC DOOR OVERHEAD EMERGE NCY LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 2001102400208 20011024 00208 2001 10 24 SWAA012860 4 20011018 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001102400209 20011024 00209 NM 2001 10 24 SWAA012870 1 20011017 A 3350 0L3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 795SW 30606 FOUND FWD EEPLS FLOOR TRACK LIGHTS INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2001103100019 20011031 00019 NM 2001 10 31 SWAA012871 1 20011018 A 5312 148A2232 BULKHEAD BOEING 737 7377H4 1384404 NM FUSELAGE CANNING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 703SW 27837 DURING SCHEDULED SERVICE CHECK (SI 11157-53) FOUND BS 1016 AFT PRESS BULKHEAD UPPER SKIN AT S-3L ABOVE LT WIRE BUNDLE H AD EVIDENCE OF OIL CANNING. MX FERRY TO DAL FOR EVAL AND CORRECTIVE ACTION. OCT 20, 2001 REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 2001102400210 20011024 00210 EU 2001 10 24 UPS01137095 1 20011019 A 2433 TRANSFORMER AIRBUS A300 A300F4622R 3930360 EU COCKPIT FAILED A IPXA A UNSCHED LANDING B P SMOKE/FUMES/ODORS/SPARKS NO WARNING INDICATION CL CLIMB 1 SO 01 129UP 0814 INSPECTION TYPE:N/A CREW SMELLED SMOKE AND DECLARED EMERGENCY. A/C LANDED AND TAXIED WITHOUT INCIDENT. NO ECAM MESSAGE - ESSENTIAL XFORMER RECIFIER FAILED. REMOVED AND REPLACED ESS TR AND RESET CB. PERFORMED OPS CHECK, CHECKS OK. 2 L 7 2 4F RT A35EU 2001102400211 20011024 00211 NM 2001 10 24 UPS01237092 1 20011018 A 2910 6517840145 HYDRAULIC LINE BOEING 727 727180C 138406G NM HYDRAULIC SYS CRACKED A IPXA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 01 920UP 19873 INSPECTION TYPE:N/A SYSTEM A-HYDRAULIC FAILURE, QTY ZERO. FOUND NR 13 SPOILER ACTUATOR RETURN LINE CRACKED. PER GMM IN STALLED A FLEX HOSE. CHECKED CASE DRAIN FILTERS, REPLACED NR 2 HYD EDP. SERVICED SYSTEM AND OPS CHK'D GOOD. PUMPED CHA NGED DUE TO BYPASS SOLENOID FAILURE. ALL CASE DRAIN FILTERS FOUND CLEAN. 2 L 7 3 4F A3WE 2001102400212 20011024 00212 NM 2001 10 24 UPS01237094 1 20011018 A 3350 BATTERY BOEING 727 72727C 138400J NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 909UP 19115 INSPECTION TYPE:N/A, OVERHEAD LIGHTS ABOVE CREW ENTRY DOOR INOP. REPLACED BATTERIES IAW 33-50-00. OPS CHECKS GOOD. 2 L 7 3 4F A3WE 2001102400213 20011024 00213 NM 2001 10 24 UPS01237133 1 20011020 A 5610 57176242 WINDOW BOEING 727 72725C 138400H NM COCKPIT CRACKED A IPXA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 950UP 19718 INSPECTION TYPE:N/A, F/O SLIDING WINDOW CRACKED. REMOVED AND REPLACED NR 2 WINDOW ASSY PER MM 56-12-11. OPS CHECKS NORM AL P/N OFF/ON 5-71762-42 SN OFF 56WIN1244 ON UP01358. 2 L 7 3 4F A3WE 2001102400214 20011024 00214 NM 2001 10 24 UPS01437077 1 20010908 A 5320 65B169522 FITTING BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C RT BATH TUB FITTING FOUND 1 BOLT HOLE CRACK (STRINGER ATTACH SURFACE) AT UPPER LEG O/B SURFACE RUNNING UP AND DOWN, BOTH CRACK APPROX 0.030 INCHES IN LENGTH. RT BATH FITTING REPLACED AS PER SRM 51-10-01 P8. 2 L 7 4 4F A20WE 2001102400215 20011024 00215 NM 2001 10 24 UPS01437078 1 20010907 A 5512 65B038873 PANEL BOEING 747 747121 1384871 NM HORIZ STAB DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C, EMP - LT STAB UPPER T/E PNL FOUND DELAMINATED AT ELEV STA 256. LT HORIZ STAB UPPER T/E PNL IN ELEV S TA 256 AREA P/N 65B03713-3 REPLACED AS PER MM 20-51-00. 2 L 7 4 4F A20WE 2001102400216 20011024 00216 NM 2001 10 24 UPS01437079 1 20010907 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C M/D - BS 220 RBL 10 FLOORBEAM SURFACE FOUND CRACKED AS MARKED. REPAIRED FLOORBEAM AT BS 220 BETWEEN R BL 7 TO RBL 13 PER SRM 53-10-07 FIG 10. 2 L 7 4 4F A20WE 2001102400217 20011024 00217 NM 2001 10 24 UPS01437080 1 20010907 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C BS 980 RT S38R FOUND CRACKED AT FWD CARGO COMPT. REPAIRED STRINGER AS PER SRM 53-10-03. 2 L 7 4 4F A20WE 2001102400218 20011024 00218 NM 2001 10 24 UPS01437081 1 20010907 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C, APU COMPARTMENT INTERIOR FRAME FOUND CRACKED AT APPROX BS 2658 TO BS 2664 RBL 50 (JUST ABOVE RT DOOR FWD CORNER). STA BS 2658 TO BS 2664 RBL 50 FRAME REPAIRED AS PER SRM 51-40-03 FIG 1. HFEC CUTOUT AS PER NTM PART 6, 51 -00-00 FIG 4 CRACK FREE BEYOND STOP HOLE. 2 L 7 4 4F A20WE 2001102400219 20011024 00219 NM 2001 10 24 UPS01437082 1 20010907 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C APU COMPARTMENT INTERIOR FRAME FOUND CRACKED AT APPROX BS 2742-2752 LBL 10. THE COMPARTMENT HORIZONTA L FRAME AT BS 2742 TO 2752 LBL 10 WAS REPAIRED AS PER SRM 51-40-03 FIG 1. HFEC INSP CONFIRMED CRACK FREE PER NTM PT6, 5 1-00-00 FIG 4. THE COMPT CUTOUT SEAL RETAINER WAS REFITTED FOR ACCESS PER MM 20-51-01. 2 L 7 4 4F A20WE 2001102400220 20011024 00220 NM 2001 10 24 UPS01437083 1 20010907 A 5320 FITTING BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C M/D - NR 3R DOOR FWD CUTOUT LWR CORNER REVEAL FITTING FOUND CRACKED. FITTING REPLACED PER SRM 51-10-0 1. 2 L 7 4 4F A20WE 2001102400221 20011024 00221 NM 2001 10 24 UPS01437084 1 20010907 A 5320 FITTING BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C M/D - NR 3L DOOR FWD CUTOUT LWR CORNER REVEAL FITTING FOUND CRACKED. FITTING REPLACED PER SRM 51-10-0 1. 2 L 7 4 4F A20WE 2001102400222 20011024 00222 NM 2001 10 24 UPS01437085 1 20010906 A 5320 ANGLE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C, RIGHT MLG W/W OUTBOARD UPPER AT FS 1265 AREA OUTBOARD VERTICAL ANGLE LOWER END CRACKED AS MARKED. RI GHT VERTICAL ANGLE REPAIRED PER SRM 51-40-03. 2 L 7 4 4F A20WE 2001102400223 20011024 00223 NM 2001 10 24 UPS01437086 1 20010906 A 5320 STRUCTURE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C, LT SIDE BS 2231, TWO FASTENER HOLES CRACK REVEALED AT BETWEEN STR 24L AND STR 26L DRAWING ON REVEALED AREA. DETAIL PLEASE REFER ATT DRAWING. REVEALED REPAIRED PER HX RS R53-62-34682. 2 L 7 4 4F A20WE 2001102400224 20011024 00224 NM 2001 10 24 UPS01437124 1 20010907 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C CRACK REVEALED ON LT FUSELAGE SKIN AT APPROX BS 970 AND S39 AT ONE FASTENER HOLE BY APPROX .1875 INCH LONG AS MARKED. CRACKED HOLE REPAIRED AS PER HX RS NR R53-43-34686. 2 L 7 4 4F A20WE 2001102400225 20011024 00225 NM 2001 10 24 UPS01437125 1 20010911 A 5230 65B074528 STOP FITTING BOEING 747 747121 1384871 NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C FX - BULK CARGO DOOR AFT EDGE NR 5 STOP FITTING INNER ATTACH FITTING FOUND CRACK AS MARKED (COUNT FROM TOP). BULK CARGO DOOR AFT EDGE NR 5 STOP FITTING REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001102500031 20011025 00031 NM 2001 10 25 CALA0100968 1 20011024 A 5320 9507835 ANGLE BOEING 737 7373T0 1384582 NM RT TE ATTACH WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69333 23571 T ANGLE ON FUSELAGE FORWARD END AT FILLET FAIRING SUPPORT ANGLE THAT ATTACHES TO UPPER WING TRAILING EDGE WORN. REMOVED AND REPLACED ANGLE PER SRM 51-10-2 AND 51-40-00. 2 L 7 2 4F RT A16WE 2001102500032 20011025 00032 NM 2001 10 25 CALA0100970 1 20011024 A 5311 53600711 FRAME BOEING 737 7373T0 1384582 NM BS727 AT S-21L DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69333 23571 FRAME 727B UPPER CAP DENTED AT S-21LT. FABRICATED AND INSTALLED REPAIR PER SRM 51-70-11. 2 L 7 2 4F RT A16WE 2001102500033 20011025 00033 EU 2001 10 25 WRNA200100017 1 20011025 A 5310 A53973128 STRINGER AIRBUS 300 A300B4203 3930306 EU CORRODED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 501TR 40242 053 DURING WALK AROUND FOUND CORROSION ON FUSELAGE AT BULK CARGO DOOR AREA. LOCATED AFT, L/H LOWER CORNER. STA. 365 STRINGER 47RCORRECTIVE ACTION: REPAIR CARRIED OUT I/A/W SRM 53-10-20 FIG. 701 SHEET 3 LAP JOINT REPAIR 2 L 7 2 4F RT A35EU 2001102500047 20011025 00047 WP 2001 10 25 0103549759 1 20011008 A 5711 SPAR CAP DOUG DC9 DC932 3022066 WP RT WING CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 759NW 47287 DURING H CHECK IN ATL, CORROSION WAS FOUND ON RT WING REAR SPAR UPPER CAP AROUND THE HOLE FOR NR 3 FLAP HINGE STUD. THE HOLE WAS CLEANED UP WITH A DEPTH OF .040 INCH AND DIAMETER OF 1.26 INCH EXTRUSION 4911204, PER EA 97-185168. 2 L 7 2 4F A6WE 2001102500048 20011025 00048 WP 2001 10 25 0103579607 1 20011013 A 5320 591000549 CAP DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 607NW 47232 DURING H-CHECK AT ATL BASE MAINTENANCE A 2 INCH CRACK WAS FOUND IN THE SLANT PANEL LOWER CAP (P/N 5910005-49) AT XCW=20 LT. THE CRACK WAS STOP DRILLED AND A REPAIR ANGLE INSTALLED. 2 L 7 2 4F A6WE 2001102500049 20011025 00049 GL 2001 10 25 01FDEA00795 2 20010831 A 7200 ENGINE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 2 SHUTDOWN A FDEA O OTHER X ENGINE FLAMEOUT LD LANDING 1 SO 25 391FE 46625 INFLT SHUTDOWN OF NR 2 ENG IN DESCENT THROTTLES RETARDED. 2 L 7 3 4F 4 F A22WE E23EA 2001102500051 20011025 00051 EU 2001 10 25 2001F00472 1 20011004 A 2121 EXT345477 FAN AIRBUS 320 A320233 EU CABIN MALFUNCTIONED A RJEF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 462TA 1334 GUA - FLT 581 - DURING CRUISE, MESSAGE ON ECAM PAGE SHOWN VENT BLOWER FAULT/EXTRACT FAN FAULT, VENT SKIN VALVE FAULT ECA M ACTION WAS PERFORMED AND THE AIRCRAFT RETURNED TO GUA STATION FOR INSPECTION. AFTER LANDING, THE EXTRACT FAN MESSAGE ON ECAM WAS ENTERED DEFERRED. BLOWER FAN WAS INTERCHANGED WITH EXTRACT FAN IAW OPERATIONAL PROCEDURE MEL 21-26-01. BLO WER FAN WAS INSPECTED ACCORDING TO AMM 21-26-51. ALSO, VENT SKIN VALVE WAS INSPECTED ACCORDING TO AMM 21-25-00. THE A/ C RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F RT A28NM 2001102500052 20011025 00052 WP 2001 10 25 0103659998 1 20011017 A 5330 DOOR FRAME DOUG DC9 DC931 3022065 WP CRACKED A NWAA O OTHER O OTHER IN INSP/MAINT 1 GL 01 8934E 47143 During H-ck in Atl inspection of subject area revealed a typical crack less than 2 inches in the door corner. Repair was accomplished per sr09530117 and EA 99-185210. Section 1 provides for an alternate fastener configuration due to restric ted access and structural interferance as shown on figure 1. 2 L 7 2 4F A6WE 2001102500053 20011025 00053 WP 2001 10 25 0103669998 1 20011017 A 5330 DOOR FRAME DOUG DC9 DC931 3022065 WP CRACKED A NWAA O OTHER O OTHER IN INSP/MAINT 1 GL 01 8934E 47143 During H-ck in ATL inspection of subject area per Ref A revealed a typical crack under 2 inches in the door corner. Repa ired per EA and SRM 53-04. Reported as part of repair assesment program. Repaired EA 99-185209. 2 L 7 2 4F A6WE 2001102500054 20011025 00054 WP 2001 10 25 0103629853 1 20011003 A 5310 BRACKET DOUG DC9 DC951 3022051 WP CRACKED A NWAA O OTHER O OTHER IN INSP/MAINT 1 GL 01 762NC 47710 During M ck in ATL and while accomplishing the rework per amitask Job #116. The left and Right brackets, P/N 995786-5/-6 brackets, made from .063" thick 7075-t6 aluminum clad sheet. Repaired per EA 98-185170. 2 L 7 2 4F RT A6WE 2001102500055 20011025 00055 WP 2001 10 25 0103619853 1 20010928 A 5310 BULKHEAD DOUG DC9 DC951 3022051 WP CRACKED A NWAA O OTHER O OTHER IN INSP/MAINT 1 GL 01 762NC 47710 A radial crack was found in the 5910130-13 doubler that ran under the 5910130-11 channel. Inspection was unable to verif y if the radial crack had terminated in a fastener hole or if it had been previously stopdrilled since the 5910130-11 ch annel covers the end of the crack. Repaired per EA 98-185173. 2 L 7 2 4F RT A6WE 2001102500056 20011025 00056 WP 2001 10 25 0103639758 1 20011017 A 5310 SHIM DOUG DC9 DC941 302207N WP CRACKED A NWAA O OTHER O OTHER IN INSP/MAINT 1 GL 01 758NW 47286 During a RON in DTW, A shim angle P/N 5919159-15 located on the aft door jamb on the RHS aft emergency exit was found cr acked. Repaired per EA 97-185229. 2 L 7 2 4F A6WE 2001102500057 20011025 00057 NE 2001 10 25 ASOA01084S 3 20010618 A 6110 PROPELLER EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE HAMSTD 14RF 14RF9 NE LT ENGINE OVERSPEED A ASOA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 SO 11 505AS 120279 FLT 4291 - DURING FINAL APPROACH INTO AVL, AIRCRAFT EXPERIENCED A PROPELLER OVERSPEED. CREW DECLARED AN EMERGENCY AND P ERFORMED THE IMMEDIATE ACTION ITEMS FOR A PROPELLER OVERSPEED. AIRCRAFT LANDED SAFELY IN AVL. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE AND PROPELLER COMPONENTS. THE TEARDOWN REPORT STATED THAT THE PROPELLER OVERSPEED WAS MOST LIKELY NOT CAUSED BY THE FAILURE OF AN INTERNAL ENGINE COMPONENT OR BY A MALFUNCTION OF THE FUEL SYSTEM OR PROP CONTROL SYSTEM. THE EXACT CAUSE OF THE EVENT REMAINS UNKNOWN, PARTIALLY DUE TO THE LACK OF INFORMATION FROM THE FLIGHT DATA RECORDER M ALFUNCTIONING. THIS ENGINE WILL BE SCRAPPED. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 6 C P11NE 2001102500058 20011025 00058 NE 2001 10 25 ASOA01112S 2 20010722 A 7260 311196801 TOWERSHAFT EMB 120 EMB120 3260201 SO PWA 118 PW118 NE LT ENGINE BROKEN A ASOA A UNSCHED LANDING J Y WARNING INDICATION ENGINE STOPPAGE CR CRUISE 1 SO 11 236AS 17351 120049 115146 FLT 4254 - DURING CRUISE FLIGHT FROM ILM TO ATL, THE LEFT ENGINE FAILED. AN EMERGENCY WAS DECLARED. AIRCRAFT DIVERTED TO AGS AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE. THE TEARDOWN REPORT FROM STANDARD AE RO REVEALED A TOWERSHAFT FAILURE. THE HP SPOOL COULD NOT BE TURNED THROUGH THE START/GENERATOR GEAR. ENGINE WAS REPAIR ED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 2001102500059 20011025 00059 EU 2001 10 25 MALA010761 1 20011018 A 3230 AIR130902 DOWNLOCK SWITCH SAAB SF340 340B 7860101 EU DEFECTIVE A MALA K NONE J WARNING INDICATION LD LANDING 1 GL 15 415XJ 340B415 During Flight #3101, the LH Main Landing gear didn't show down and locked. Completed QRH and cycled gear. All 3 showed down and locked, then the LH Green light flickered off/on several times, continued to flicker while taxing to the gate. Maintenance replaced LH Main Gear Downlock Switch, PN Air130902, all checks good. All work done IAW Saab MM Chap 32-6 1-05. 2 L 7 2 4T RT A52EU 2001102500060 20011025 00060 EU 2001 10 25 MALA010763 1 20011022 A 3020 24665165 INTAKE DUCT SAAB SF340 340B 7860101 EU DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 436XJ 340B436 After departing DTW switched on Engine anti-ice after 4 minutes received RH Intake Caution light ran QRH, did not solve problem. Air return to DTW. Maintenance replaced RH Lower Intake Duct PN 24665-165, SN/off L290790, SN/on L169248 IAW AMM 30 Ops check good. 2 L 7 2 4T RT A52EU 2001102500064 20011025 00064 NE 2001 10 25 ASOA01116S 2 20010724 A 7230 3036212 BLADE EMB 120 EMB120 3260201 SO PWA 118 PW118A NE RT ENGINE FRACTURED A ASOA H E A DEACTIVATE SYST/CIRCUITS ENGINE SHUTDOWN UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 11 243AS 19268 120072 FLT 4830 - DURING FLIGHT FROM DFW TO TUL, CREW REPORTED SMELLING SMOKE IN THE CABIN. AFTER ISOLATING THE RT BLEED AND R T PACK THE SMOKE DIDN'T CLEAR. RECEIVED A RT ENGINE LOW OIL PRESSURE WARNING AND THE GAUGE WAS FLUCTUATING. THE RT ENGI NE OIL PRESSURE DROPPED BELOW 40 PSID. THE RT ENGINE WAS SHUT DOWN. RETURNED TO DFW AND LANDED SAFELY. MX R&R THE RT ENGINE. THE TEARDOWN REPORT STATED THE FRACTURE OF THE LP BLADE, SUGGESTS THAT THE TRAILING EDGE OF THE BLADE FRACTURED IN HIGH CYCLE FATIGUE AND THE BLADE FRACTURED IN TENSILE OVERLOAD. THIS MOST LIKELY OCCURRED DUE TO BLADES BEING OPERA TED BEHIND A BURNED THROUGH HP VANE ASSY. THE HP VANE SEGMENTS WERE FOUND TO BE BURNED AT TWO LOCATIONS. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 2001102500065 20011025 00065 SO 2001 10 25 ASOA01151S 1 20010831 A 5311 FRAME EMB 120 EMB120 3260201 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 273AS 120222 DURING C-CHECK INSPECTION IN BNA, FOUND CORROSION AT FRAME 21, STRINGERS 18 LEFT TO 18 RIGHT. MAINTENANCE REPAIRED AIRC RAFT IAW ASA EO120-53-0166. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001102500066 20011025 00066 NM 2001 10 25 USAA011279 1 20010911 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE CRACKED A K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 22962 CLT - FOUND FLOORBEAM CRACKED 4 INCHES, STATION 663 BL 0. INSTALLED WEB, SPLICE ANGLE REPAIR. (M) 2 L 7 2 4F A16WE 2001102500067 20011025 00067 NM 2001 10 25 USAA011297 1 20010910 A 5310 WEB BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 44257 23235 CLT - FOUND WEB CRACKED .5 INCH, BS 178 WL 213 RBL 6 AND WL 207 LBL 1. INSTALLED REPAIR DOUBLER PER EO 5300V153. (M) 2 L 7 2 4F RT A16WE 2001102500070 20011025 00070 EA 2001 10 25 ASOA01172 1 20010917 A 7931 MS2951504 O-RING CNDAIR CL600 CL600* EA LT ENGINE DAMAGED A ASOA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 11 842AS 7304 DURING CLIMB-OUT OF PIA EN ROUTE TO ATL, CAPTAIN REPORTED THE LEFT ENGINE OIL PRESSURE WARNINGS AND ANALOG INDICATION FL UXED FROM 45 TO 24 PSI. INDICATIONS WERE NORMAL AT LOWER POWER SETTINGS. AIRCRAFT DIVERTED TO EVV AND THE CAPTAIN SHUT DOWN THE LEFT ENGINE ON APPROACH DUE TO THE LOW OIL PRESSURE WARNING. AIRCRAFT LANDED IN EVV WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE O-RING ON THE OIL PRESSURE SWITCH. MAINTENANCE ALSO SERVICED THE LEFT ENGINE WITH 6 QUARTS OF OIL. GROUND RUNS WERE GOOD. NO LEAKS WERE FOUND. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2001102500071 20011025 00071 SO 2001 10 25 ASOA01173 1 20010917 A 3350 3071BPE LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 638AS 120282 DURING HANGAR MAINTENANCE IN MCN, THE FLOOR TRACK LIGHTING WAS FOUND WITH ONE RED LIGHT INOPERATIVE AT ROW 8. MAINTENAN CE REMOVED AND REPLACED BURNED OUT LAMP ON THE EMERGENCY FLOOR TRACK LIGHTING AT ROW 8. OPS CHECKS GOOD. AIRCRAFT OK FO R SERVICE. (M) 2 L 7 2 4T RT A31SO 2001102500072 20011025 00072 SO 2001 10 25 ASOA01174 1 20010917 A 3350 D36604001 BATTERY PACK EMB 120 EMB120 3260201 SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 260AS 120132 DURING SCHEDULED MAINTENANCE IN TXK, SEVERAL EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPL ACED THE NR 1 EMERGENCY LIGHTING BATTERY PACK. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001102500073 20011025 00073 SO 2001 10 25 ASOA01175 1 20010918 A 5713 12016085002 STRINGER EMB 120 EMB120 3260201 SO RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 260AS 120132 DURING SCHEDULED MAINTENANCE IN TXK, STRINGER 10 ON THE RIGHT WING WAS FOUND CRACKED AT THE OUTBOARD EDGE OF THE NR 1 FU EL PANEL. MAINTENANCE REPAIRED STRINGER 10 ON THE RIGHT WING AT THE OUTBOARD EDGE OF THE NR 1 FUEL PANEL IAW EMB-120 SR M 57-20-03. THE NR 1 FUEL PANEL ON THE RIGHT WING WAS REINSTALLED IAW ASA EO 120-51-0005. LEAK CHECK GOOD AND RII INSP ECTION COMPLIED WITH. (M) 2 L 7 2 4T RT A31SO 2001102500074 20011025 00074 SO 2001 10 25 ASOA01176 1 20010918 A 5720 12017054613 BRACKET EMB 120 EMB120 3260201 SO LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 260AS 120132 DURING SCHEDULED MAINTENANCE IN TXK, RIB 8 WAS FOUND WITH CRAKES SKIN SUPPORT BRACKET AFT OF THE NR 1 FUEL PANEL ON THE LEFT WING. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT BRACKET AT RIB 8 ON THE AFT SIDE OF THE NR 1 FUEL PANEL ON THE LEFT WING. MAINTENANCE THEN REINSTALLED THE LEFT WING NR 1 FUEL PANEL IAW ASA EO 120-51-0005. LEAK CHECK GOOD. A IRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001102500075 20011025 00075 SO 2001 10 25 ASOA01177 1 20010918 A 3397 FO2A250V1A WIRE EMB 120 EMB120 3260201 SO CABIN SHORTED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 284AS 120249 FLT 4059 - DURING GROUND INSPECTION IN ATL, THE EMERGENCY TRACK LIGHTS BY GALLEY WERE FOUND TO BE INOPERATIVE. MAINTENA NCE REPAIRED A SHORT IN THE WIRING AND REPLACED FUSE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001102500076 20011025 00076 EA 2001 10 25 ASOA01178 1 20010915 A 2910 601R7530129 HYDRAULIC LINE CNDAIR CL600 CL600* EA HYDRAULIC SYS CRACKED A ASOA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 11 823AS 7196 FLT 4757 - DURING CRUISE FLIGHT FROM ATL TO DSM, CAPTAIN RECEIVED A HYDRAULIC 1 LOW PRESSURE CAUTION MESSAGE. AFTER COM PLYING WITH ABNORMAL PROCEDURES CAPTAIN DETERMINED A LOSS OF HYDRAULIC FLUID. AN EMERGENCY WAS DECLARED AND AIRCRAFT LA NDED UNEVENTFULLY IN DSM. MAINTENANCE INSPECTED AND DISCOVERED A TOTAL LOSS OF HYDRAULIC QUANTITY AND PRESSURE. MAINTE NANCE REMOVED AND REPLACED THE LEFT ENGINE DRIVEN HYDRAULIC PUMP DUE TO IT BEING RUN DRY. THE HYDRAULIC FLEX LINE WAS C HANGED AS A PRECAUTION. AFTER SERVICING THE HYDRAULIC SYSTEM MAINTENANCE INSPECTED THE LEFT FUEL TANK AREA AND FOUND A CRACK IN THE LINE AT FUEL PANEL 550DB. MAINTENANCE REPAIRED CRACK IN LINE. (M) 2 L 7 2 4F RT A21EA 2001102500077 20011025 00077 SO 2001 10 25 ASOA01180 1 20010922 A 3350 BATTERY PACK EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 266AS 120188 FLT 4881 - DURING GROUND INSPECTION IN DFW, THE CENTER SECTION OF THE CABIN EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANC E REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY PACK. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001102500078 20011025 00078 SO 2001 10 25 ASOA01190 1 20010927 A 3397 MSS75941229 WIRE EMB 120 EMB120 3260201 SO CABIN BROKEN A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 257AS 120126 DURING HANGAR INSPECTION IN TXK, MAINTENANCE FOUND A BROKEN WIRE ON THE EMERGENCY EXIT SIGN AT ROW 8. MAINTENANCE REPAI RED THE BROKEN WIRE ON THE ROW 8 EMERGENCY EXIT SIGN. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001102500079 20011025 00079 EA 2001 10 25 ASOA01191 1 20010929 A 5610 NP1393215 WINDSHIELD CNDAIR CL600 CL600* EA COCKPIT CRACKED A ASOA K NONE O OTHER DE DESCENT 1 SO 11 860AS 2716 7433 WHILE DESCENDING INTO DSM, AT 17,000 FEET, THE CAPTAIN FORWARD WINDSHIELD CRACKED. AIRCRAFT LANDED SAFELY IN DSM. MAIN TENANCE REMOVED AND REPLACED THE LEFT MAIN WINDSHIELD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001102500080 20011025 00080 EA 2001 10 25 ASOA01192 1 20011001 A 3350 601R461011 LIGHT CNDAIR CL600 CL600* EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 837AS 7271 FLT 4414 - DURING GROUND INSPECTION IN MGM, CREW FOUND THE FLOOR PATH LIGHTS AT BOTH WING EMERGENCY EXITS AS WELL AS THE WHITE FLOOR PATH LIGHTING FORWARD INOPERATIVE. THE CREW ALSO NOTED THE LOWER GREEN EXIT LIGHTS FOR THE WING EMERGENCY EXITS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT TRACK BETWEEN ROWS 5 AND 8. OPERATIONAL C HECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001102500081 20011025 00081 NM 2001 10 25 P2EA01172 1 20010907 A 5330 SKIN BOEING 737 737230 1384401 NM FUSELAGE CANNING A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 123NJ 22121 SJO - DURING C-CHECK, FOUND EXTERNAL FUSELAGE, BS 952, BETWEEN STRINGER 23 AND 24 RIGHT SKIN WITH OIL CAN. S/D - REPAIR ED FUSELAGE SKIN SECTION FROM BS 943 TO BS 958, BETWEEN STRINGER 21 AND 25 RIGHT DUE TO OIL CAN IAW SRM 53-30-3 FIG 17 D ETAIL V. (M) 2 L 7 2 4F RT A16WE 2001102500082 20011025 00082 NM 2001 10 25 P2EA01174 1 20010907 A 5330 SKIN BOEING 737 737230 1384401 NM FUSELAGE DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 123NJ 22121 DURING C-CHECK, FOUND EXTERNAL FUSELAGE BS 1065, BETWEEN STRINGER 28 LEFT AND 28 RIGHT, SKIN WITH DENT OUT OF LIMITS. RE PAIRED FUSELAGE SKIN SECTION FROM BS 1062 TO BS 1075, BETWEEN STRINGER 27 LEFT AND STRINGER 27 RIGHT, DUE TO DENT OUT OF LIMITS IAW SRM 53-50-3, FIG 6. (M) 2 L 7 2 4F RT A16WE 2001102500083 20011025 00083 NM 2001 10 25 P2EA01175 1 20010907 A 5330 SKIN BOEING 737 737230 1384401 NM FUSELAGE DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 123NJ 22121 SJO - DURING C-CHECK, EXTERNAL FUSELAGE BS 461, STRINGER 16RT SKIN WITH DENT OUT OF LIMITS. REPAIRED FUSELAGE SKIN SECT ION FROM BS 455 TO BS 466.5, BETWEEN STRINGER 15 AND 17 RIGHT, DUE TO DENT IAW RM 53-30-3, FIG 17 DETAIL V. (M) 2 L 7 2 4F RT A16WE 2001102500084 20011025 00084 NM 2001 10 25 0103706642 1 20011024 A 5415 ATTACH FITTING BOEING 747 747212B 1384886 NM FRETTED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 642NW 21942 During "PCK" found fretting corrosion in several areas of number 3 strut aft diagonal brace attach fitting. Repaired per EA 66-186713. 2 L 7 4 4F A20WE 2001102500085 20011025 00085 NM 2001 10 25 0103716642 1 20011006 A 5315 ATTACH FITTING BOEING 747 747212B 1384886 NM CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 642NW 21942 During "PCK" found corrosion/pitting on number 4 strut to aft diagonal brace attach fitting. Repaired per EA 66-186714. 2 L 7 4 4F A20WE 2001102500086 20011025 00086 NM 2001 10 25 USAA011236 1 20010912 A 5320 FASTENER BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 601AU 22193 CLT - FOUND FASTENER CORRODED, BS 1279 BELOW STRINGER 23L. REMOVED SURFACE CORROSION PER SRM 53-60-03, 53-60-04, 53-60- 07. (M) 2 L 7 2 4F RT A2NM 2001102500087 20011025 00087 NM 2001 10 25 USAA011250 1 20010915 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 46526 22959 PIT - FOUND FRAME CRACKED .1875 INCH, BS 887 ABOVE S9L TIE CLIP AT RIVET HOLE. INSTALLED DOUBLER PER TYPICAL REPAIR 53- 10-14. (M) 2 L 7 2 4F RT A16WE 2001102500088 20011025 00088 NM 2001 10 25 USAA011251 1 20010915 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 46526 22959 PIT - FOUND FRAME CRACKED .25 INCH, BS 847 ABOVE S9R TIE CLIP AT RIVET HOLE. INSTALLED DOUBLER PER TYPICAL REPAIR 53-10 -14. (M) 2 L 7 2 4F RT A16WE 2001102500089 20011025 00089 NM 2001 10 25 USAA011252 1 20010916 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 46526 22959 PIT - FOUND FRAME CRACKED .1875 IN TWO PLACES, BS 847 ABOVE S9L AT RIVET HOLE. INSTALLED DOUBLER PER TYPICAL REPAIR 53- 10-14. (M) 2 L 7 2 4F RT A16WE 2001102500090 20011025 00090 NM 2001 10 25 USAA011253 1 20010916 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 46526 22959 PIT- FOUND BEAM CAP CORRODED SEVERAL AREAS APPROXIMATELY 1 INCH, AT SCREW HOLES ON CENTER SECTION OF BS 312 FLOORBEAM. (M) 2 L 7 2 4F RT A16WE 2001102500091 20011025 00091 NM 2001 10 25 USAA011254 1 20010916 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 46526 22959 PIT - FOUND FRAME CRACKED .1875 INCH IN TWO PLACES, BS 827 ABOVE S9R AT RIVET HOLE. INSTALLED DOUBLER PER TYPICAL REPAI R 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001102500092 20011025 00092 NM 2001 10 25 USAA011256 1 20010916 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 22959 PIT - FOUND FRAME CRACKED TWO PLACES .125 INCH, BS 887R ABOVE S9R TIE CLIP AT RIVET HOLE. INSTALLED DOUBLER PER TYPICAL REPAIR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2001102500093 20011025 00093 NM 2001 10 25 USAA011280 1 20010924 A 5313 STRINGER BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 48384 22962 CLT - FOUND STRINGER CORRODED 2 INCHES BY 1 INCH, STATION 968 STRINGER 25L. INSTALLED STRINGER REPAIR PER SRM 53-10-3. (M) 2 L 7 2 4F A16WE 2001102500094 20011025 00094 NM 2001 10 25 USAA011281 1 20010928 A 5320 STRUCTURE BOEING 737 737201 1384454 NM FUSELAGE CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 22962 CLT - FOUND WEAR CHAFING FROM APU BLEED DUCT .250 BY 3 INCH, STATION 1064. INSTALLED REPAIR DOUBLER PER EA 85490. (M) 2 L 7 2 4F A16WE 2001102500095 20011025 00095 NM 2001 10 25 USAA011282 1 20010913 A 5320 654795711 BEAM BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 48384 22962 CLT - FOUND BEAM CORRODED, AFT CARGO STATION 797 S26R. REPLACED STRAP 65-47957-11 SRM 51-10-01. (M) 2 L 7 2 4F A16WE 2001102500096 20011025 00096 NM 2001 10 25 USAA011283 1 20010930 A 5320 INTERCOSTAL BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 48384 22962 CLT - FOUND INTERCOSTAL CORRODED .5 INCH BY 10 INCHES, STATION 1006 TO STATION 1016 BBL 0. REPAIRED PER SRM 51-30-2. ( M) 2 L 7 2 4F A16WE 2001102500097 20011025 00097 NM 2001 10 25 USAA011284 1 20010911 A 5320 INTERCOSTAL BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 48384 22962 CLT - FOUND BEAM INTERCOSTAL CORRODED 2 INCHES BY 26 INCHES, BS 990-1016 LBL 6 TO LBL 16. REPLACED INTERCOSTAL PER SRM 51-10-1 AND 51-30-3. (M) 2 L 7 2 4F A16WE 2001102500098 20011025 00098 NM 2001 10 25 USAA011285 1 20010911 A 5347 SEAT TRACK BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 48384 22962 CLT - FOUND SEAT TRACK CORRODED AT CLIP NUT HOLES 2 INCHES BY 60 INCHES, BS 986, LBL 6 TO RBL 54, WL 207. INSTALLED NEW T-CAP. (M) 2 L 7 2 4F A16WE 2001102500099 20011025 00099 NM 2001 10 25 USAA011286 1 20010919 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 22962 CLT - FOUND SKIN WITH PREVIOUSLY INSTALLED DOUBLER 10 INCHES BY 8 INCHES, STATION 380 BETWEEN S24 AND S23. INSTALLED NE W DOUBLER PER SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 2001102500100 20011025 00100 NM 2001 10 25 USAA011287 1 20010920 A 5311 FRAME BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 283AU 50355 23116 CLT - FOUND OUTER CHORD CRACKED 1 INCH, BS 178 WL 207 RBL 25. INSTALLED NEW RIGHT CHORD SEGMENTS AND SPLICE PARTS PER E O 5300V157. (M) 2 L 7 2 4F A16WE 2001102500101 20011025 00101 NM 2001 10 25 USAA011289 1 20010911 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 48384 22962 CLT - FOUND BEAM CORRODED 2 INCHES BY 33 INCHES, BS 1016 BBL 0 LBL 33. INSTALLED T-CAP PER T/R 53-60-02. (M) 2 L 7 2 4F A16WE 2001102500102 20011025 00102 NM 2001 10 25 USAA011290 1 20010911 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 48384 22962 CLT - FOUND BEAM/CHANNEL/WEB CORRODED 5 INCHES, BS 1014-1019 BBL 0 LBL 6. INSTALLED T-CAP. (M) 2 L 7 2 4F A16WE 2001102500103 20011025 00103 NM 2001 10 25 USAA011291 1 20010906 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 48384 22962 CLT - FOUND SKIN DENTED 1 INCH, BS 280 STRINGER 24R. REMOVED DAMAGE, INSTALLED REPAIR PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 2001102500105 20011025 00105 NM 2001 10 25 USAABB01089 1 20010827 A 4930 388250017 FCU BOEING 757 7572B7 1384964 NM APU FAULTY A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 616AU 27147 SEA - FLT 108/9280 - WHILE AWAITING TAKEOFF IN SEA, CREW RECEIVED A RIGHT IDG WARNING. FLIGHT WAS REDISPATCHED WITH THE RIGHT GENERATOR ON MEL AND THE APU OPERATING. APPROXIMATELY THIRTY MINUTES INTO FLIGHT, THE APU FAULTED AND SHUTDOWN. FLIGHT RETURNED TO SEA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE INLET PRESSURE SENSOR. ON THE SU BSEQUENT FLIGHT, THE APU AGAIN FAULTED AND SHUTDOWN. THE FLIGHT AGAIN RETURNED TO SEA. MAINTENANCE REPLACED THE FUEL C ONTROL UNIT. (M) 2 L 7 2 4F RT A2NM 2001102500114 20011025 00114 EA 2001 10 25 COMA0160844 1 20011024 A 5320 60034017351 ANGLE CNDAIR CL600 CL6002B19 EA F.S.280 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 984CA 9666 7171 FWD/J - ANGLE AT F.S. 280 HAS CORROSION.REPAIRED FWD J-ANGLE I/A/W WVAC EO 601R-53-2775. 2 L 7 2 4F RT A21EA 2001102500115 20011025 00115 EA 2001 10 25 COMA0160845 1 20011024 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 937CA 16523 7044 R/H LOWER WING PLANK CRACKED AT W.S. 56.68 PANEL #640AB AND L/H LOWER WING PLANK CRACKED AT W.S. 95.950 PANEL #640DB.BLE NDED OUT DAMAGE AREAS AND ROTO-PEENED I/A/W REO 601R-67-21-030. 2 L 7 2 4F RT A21EA 2001102500116 20011025 00116 EA 2001 10 25 COMA0160846 1 20011023 A 2760 4916405 FCU CNDAIR CL600 CL6002B19 EA AVIONICS BAY FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 951CA 13266 7091 FLIGHT 5010. DURING TAKE OFF ROLL RECEIVED A SPOILER CONFIGURTION MESSAGE, TAKE OFF WAS ABORTED AND RETURNED TO THE GAT E.REPLACED THE SPOLIER ELECTRONIC CONTROL UNIT. 2 L 7 2 4F RT A21EA 2001102500118 20011025 00118 EA 2001 10 25 COMA0160847 1 20011023 A 2760 601R591473 FCU CNDAIR CL600 CL6002B19 EA AVIONICS BAY FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 951CA 10803 7091 FLIGHT #5010. DURING TAKE OFF ROLL RECEIVED A SPOILER CONFIGURATION MESSAGE, TAKE OFF WAS ABORTED AND RETURNED TO THE G ATE.REPLACED THE SPOILER ELECTRONIC CONTROL UNIT. 2 L 7 2 4F RT A21EA 2001102500124 20011025 00124 EA 2001 10 25 COMA0160848 1 20011023 A 2760 270007 PCU CNDAIR CL600 CL6002B19 EA WING FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 951CA 16856 7091 FLIGHT #5010. DURING TAKE OFF ROLL RECEIVED A SPOILER CONFIGURATION MESSAGE, TAKE OFF WAS ABORTED AND RETURNED TO THE G ATE.REPLACED THE LEFT FLIGHT SPOILER INBOARD POWER CONTROL UNIT. 2 L 7 2 4F RT A21EA 2001102500127 20011025 00127 NM 2001 10 25 USAABB01098 1 20010919 A 3260 WARNING SYSTEM BOEING 757 7572B7 1384964 NM COCKPIT MALFUNCTIONED A USAA L ABORTED APPROACH N E FALSE WARNING VIBRATION/BUFFET AP APPROACH 1 EA 19 623AU 27244 PHL - FLT 186 - ON APPROACH TO PIT, CREW RECEIVED THE EICAS MESSAGE 'GEAR DISAGREE' AND THE NOSE GEAR DOWN LIGHT DID NOT ILLUMINATE. WITH THE GEAR RETRACTED, A HEAVY VIBRATION FROM THE NOSE AREA WAS FELT AND THE GEAR DOORS LIGHT STAYED ILL UMINATED. THE CREW PERFORMED TOWER FLY-BYS TO ENSURE THAT THE GEAR WAS EXTENDED. FLIGHT LANDED WITHOUT FURTHER INCIDEN T. MAINTENANCE JACKED THE AIRCRAFT AND CYCLED THE GEAR SEVERAL TIMES. NO PROBLEMS WERE ENCOUNTERED. THE RIGHT DOWN SE NSOR ADJUSTMENT WAS HIGH BUT WITHIN LIMITS. THE SENSOR WAS ADJUSTED AND THE PSEU REPLACED AS A PRECAUTION. (M) 2 L 7 2 4F RT A2NM 2001102500131 20011025 00131 NM 2001 10 25 USAABB01099 1 20010925 A 3397 WIRE BOEING 767 767201 1385125 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 647US 23899 CLT - FOUND FLOOR PROXIMITY LIGHTING INOPERATIVE ON RIGHT SIDE NEAR ROWS 8 THROUGH 11. MAINTENANCE FOUND AND REPAIRED B ROKEN WIRING. (M) 2 L 7 2 4F RT A1NM 2001102500132 20011025 00132 EA 2001 10 25 COMA0160849 1 20011023 A 2760 270007 PCU CNDAIR CL600 CL6002B19 EA WING FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 951CA 11106 7091 FLIGHT #5010. DURING TAKE OFF ROLL RECEIVED A SPOILER CONFIGURATION MESSAGE, TAKE OFF WAS ABORTED AND RETURNED TO THE G ATE.REPLACED THE FLIGHT SPOILER OUTBOARD POWER CONTROL UNIT. 2 L 7 2 4F RT A21EA 2001102500135 20011025 00135 NM 2001 10 25 USAABB01100 1 20010929 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 604AU 22199 BWI - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 6 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2001102500137 20011025 00137 NM 2001 10 25 USAABB01101 1 20011001 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 604AU 22199 BWI - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 1, 4, 9, 13, 18, 23, 26 AND 29 WEAK. MAINTENANCE REPLACED THE BATTERIE S AS A PRECAUTION. (M) 2 L 7 2 4F RT A2NM 2001102500138 20011025 00138 2001 10 25 COMA0160850 4 20011023 A 3130 RECORDER CNDAIR CL600 CL6002B19 EA A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 986CA 7174 FLIGHT #5352. FLIGHT DATA RECORDER MESSAGE ON EICAS.C/W TEST OF DFDR SYSTEM, NO DEFECTS. 2 L 7 2 4F RT A21EA 2001102500141 20011025 00141 WP 2001 10 25 USAAD01163 1 20010922 A 3350 9721055 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 829US 49429 PHL - THE LOW LEVEL EMERGENCY LIGHTS IN THE FIRST CLASS SECTION OF THE PASSENGER CABIN WERE INOPERATIVE. MAINTENANCE RE PLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001102500147 20011025 00147 WP 2001 10 25 USAAD01164 1 20010926 A 2130 39271011 VALVE DOUG DC9 DC981 3022081 WP CABIN PRESSURE FAILED A USAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 826US 48026 MSY-CLT - FLT 1278 - DURING CRUISE, AT THE TOP OF THE DESCENT, THE CABIN FLOW LIGHT ILLUMINATED WITH NO INDICATION OF A FAULT IN THE CABIN PRESSURE CONTROL. THE CREW INITIATED AN EMERGENCY DESCENT FROM 33,000 FEET TO 19,000 FEET. THE AIRC RAFT CONTINUED TO ITS DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT PNEUMATIC AUGMENTATION VAL VE. (M) 2 L 7 2 4F A6WE 2001102500155 20011025 00155 EA 2001 10 25 COMA0160852 1 20011023 A 2760 SPOILER CNDAIR CL600 CL6002B19 EA A COMA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 420CA 7451 FLIGHT #5258. FLIGHT SPOILER AND OUTBD GROUND SPOILER STATUS MESSAGE.RESET SYSTEM, MESSAGE CLEARED. COULD NOT DUPLICAT E. 2 L 7 2 4F RT A21EA 2001102500156 20011025 00156 WP 2001 10 25 USAAD01165 1 20011002 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 819US 48099 IND - THE LOW LEVEL EMERGENCY LIGHTS AND THE AFT SECTION OF CEILING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPL ACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES AND THE AFT CEILING EMERGENCY LIGHT POWER SUPPLY. (M) 2 L 7 2 4F A6WE 2001102500157 20011025 00157 WP 2001 10 25 USAAD0162 1 20010921 A 3350 1001191 LIGHT DOUG DC9 DC981 3022081 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 819US 48099 THE FORWARD ENTRANCE DOOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. (M) 2 L 7 2 4F A6WE 2001102500159 20011025 00159 EU 2001 10 25 USAAF01074 1 20010921 A 3350 6104789 BATTERY FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 867US 11312 RIC - THE FIRST CLASS EMERGENCY TRACK LIGHTING AND NR 1 CEILING EMERGENCY LIGHT WERE FOUND INOPERATIVE. MAINTENANCE REP LACED THE NR 9 SUPPLY BATTERY. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT 2001102500160 20011025 00160 EU 2001 10 25 USAASA01040 1 20010801 A 3350 ASTM5X6NE1 LIGHT AIRBUS A319 A319112 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 720US 1089 SAN - THE EMERGENCY LIGHT SYSTEM WILL NOT TEST PROPERLY. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT BULB. (M) 2 L 7 2 4F RT A28NM 2001102500161 20011025 00161 EU 2001 10 25 USAASA01046 1 20010825 A 3397 WIRE AIRBUS A319 A319112 EU CABIN DAMAGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 711UW 1033 CLT - THE EMERGENCY AISLE LIGHT AT SEAT 17C WAS INOPERATIVE. MAINTENANCE REPAIRED WIRING AT SEAT 17C EMERGENCY LIGHT CO NNECTOR. (M) 2 L 7 2 4F RT A28NM 2001102500162 20011025 00162 2001 10 25 USAASB01237 4 20010819 A 2210 4051601935 CONTROL PANEL BOEING 737 7373B7 1384580 NM COCKPIT FAILED A USAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 EA 19 515AU 34702 23701 CLT - FLT 572 - APPROACH TO CLT,'B' A/P ON, A/C MADE UNCOMMANDED 30 DEGREE ROLL TO THE RT. AFTER A 20 DEGREE HEADING CH ANGE (30 DEGREE AOB SELECTED ON TURN KNOB), A/P CORRECTED TO HEADING SELECTED. NO DEFLECTION WAS NOTED ON RUDDER PEDALS . AFTER CORRECTION TO HEADING, A/P FLEW A/C NORMALLY. THRUST WAS SYMMETRIC. THE SPEEDBRAKE HANDLE MUST BE PULLED BACK M ORE THAN USUAL TO GET THE SPEEDBRAKE ARMED. IT WAS IN THE ARMED POSITION DURING THE ROLL. NO DEFLECTION WAS ON THE YA W DAMPER DURING THE ROLL AND THE CONTROL COLUMN DID NOT MOVE UNTIL THE A/P CORRECTED BACK TO THE SELECTED HEADING. IT T HEN DEFLECTED LEFT TO GET BACK ON HEADING. LANDED WITHOUT INCIDENT. REPLACED 'B' FLIGHT CONTROL COMPUTER (P/N 4051600- 2 L 7 2 4F RT A16WE 2001102500168 20011025 00168 NM 2001 10 25 USAASB01256 1 20010915 A 3260 189929 SAFETY SWITCH BOEING 737 737401 1384701 NM RT MLG WW FAULTY A USAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 420US 23987 MCO - FLT 1263 - EN ROUTE FROM PHL, AT FL220, RECEIVED AN ALERT FOR CABIN PRESSURIZATION AS CABIN ALTITUDE CLIMBED ABOVE 10,000 FT. DECLARED EMERGENCY AND ACCOMPLISHED AN EMERGENCY DESCENT. BOTH TRANSPONDERS FAILED-NO FAIL LIGHT ILLUMINATED , CABIN CHIMES AND FORWARD SMOKE DETECTOR SOUNDING, SPEED BRAKE LIGHT GOING GREEN TO AMBER INTERMITTENTLY AND A/T AND TC AS FAILING INTERMITTENTLY. DIVERTED TO MCO AND LANDED WITHOUT INCIDENT. MX FOUND A DEFECTIVE C/B AT P6-1 PANEL, E-13 PO SITION, NR 2 ELEC A/C BUS. R&R CIRCUIT BREAKER. ALL SYSTEMS CHECK GOOD AT THIS TIME. THE PROBLEM REPEATED THAT DAY. F OUND THE GROUND SAFETY SWITCH CYCLING BETWEEN AIR AND GROUND. R&R S105 GROUND SAFETY SENSOR AND M990 GROUND SENSING CIR 2 L 7 2 4F RT A16WE 2001102500176 20011025 00176 WP 2001 10 25 0103679998 1 20011017 A 5530 SUPPORT FITTING DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8934E 47143 During H ck at ATL base maintenance, two 1.00" cracks were found on verticle stabilizer actuator support fittings. Both cracks emenated from the end fastener hole forward the edge of the firrigns flange. The repair involved the installation of a repair doubler at each location with a min of 5 fasteners fromthe end fastener. 0.80" 7075-651. Repaired per EA 99 -185202. 2 L 7 2 4F A6WE 2001102500177 20011025 00177 WP 2001 10 25 0103689930 1 20010929 A 5340 FITTING DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 89S 47042 Found 1/2" crack in large flat casting that bolts to the top of the trap fitting lt w/well. Replaced fitting. l/p 167601 9 2 L 7 2 4F A6WE 2001102500178 20011025 00178 EU 2001 10 25 AALA20011555 1 20010803 A 3260 WARNING SYSTEM AIRBUS 300 A300B4605R 3930308 EU COCKPIT FALSE INDICATION A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 14056 463 MIA - FLT 2111 - EN ROUTE LIM NOSE GEAR INDICATION MESSAGE AFTER TAKEOFF. LANDED MIA WITHOUT INCIDENT. PERFORMED OVERW EIGHT LANDING INSPECTION. NO DISCREPANCIES NOTED. (M) 2 L 7 2 4F RT A35EU 2001102500179 20011025 00179 EU 2001 10 25 AALA20011611 1 20010811 A 5730 SKIN AIRBUS 300 A300B4605R 3930308 EU LT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 11060 470 TUL - FOUND CORROSION IN THE FORM OF A HOLE THROUGH SKIN ON LEFT WING LOWER SKIN L/E JUST INBOARD OF RIB 20. REMOVED CO RROSION AND INSTALLED DOUBLER PER ESO30595 DATED 10 AUG 01. (M) 2 L 7 2 4F RT A35EU 2001102500180 20011025 00180 EU 2001 10 25 AALA20011612 1 20010809 A 5320 FITTING AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14056 463 TUL - FOUND LAV TIE DOWN PITTING, CORRODED AT LAV M BETWEEN FRAME 32 AND 33. INSTALLED LAV TIE DOWN FRAME 32-33 PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 2001102500181 20011025 00181 2001 10 25 0103739853 4 20011017 A 2565 113317 SLIDE 104375 DOUG DC9 DC951 3022051 WP FWD FUSELAGE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 762NC 43153 4710 47710 DURING LINE CHECK, DISCOVERED RESERVOIR TO BE AT ZERO PSI. REPLACED THE SLIDE AND RETURNED REMOVED SLIDE TO SHOP FOR REPAIR. 2 L 7 2 4F RT A6WE 2001102500182 20011025 00182 WP 2001 10 25 0103749854 1 20011017 A 2710 PULLEY DOUG DC9 DC951 3022051 WP RT AILERON FROZEN A NWAA O OTHER F FLT CONT AFFECTED CL CLIMB 1 GL 01 763NC 47716 CREW NOTICED AILERONS SEEMED STIFF DURING FLIGHT CONTROL CHECK WHEN TAXIING OUT FOR DEPARTURE. AFTER TAKEOFF, THE AILERO NS WERE VERY TIGHT AND DIFFICULT TO TURN IN RIGHT BANKS BUT NORMAL IN LEFT TURNS. THE CONTROLS SEEMED TO FREE UP SOME BU T THEN BINDING TO THE RIGHT AGAIN. FLIGHT DECLARED AN EMERGENCY AND RETURNED TO DTW WITH AN UNEVENTFUL LANDING. MAINTENA NCE FOUND A CABIN PULLEY ON THE RIGHT WING FROZEN. REPLACED THE PULLEY, RERIGGED, AND TENSIONED THE CABLE RUN. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2001102500183 20011025 00183 EU 2001 10 25 AALA20011613 1 20010813 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14056 463 TUL - FOUND RIGHT SEAT TRACK C (3RD FROM R-2 DOOR) HAS CORROSION TOP SIDE, FRAME 30 TO FRAME 33. REPLACED RIGHT SEAT TR ACK C PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 2001102500184 20011025 00184 EU 2001 10 25 AALA20011646 1 20010809 A 5320 SPLICE AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14056 463 TUL - FOUND CRACK FOUND ON ATTACHMENT ANGLE ABOVE WINDOW STRINGER CROSS OVER POINT AND FRAME 47 RIGHT. INSTALLED NEW MA NUFACTURED STRINGER SPLICE ANGLE, WET WITH NEW FASTENERS AT FRAME 47 RIGHT, AND STRINGER 18R. (M) 2 L 7 2 4F RT A35EU 2001102500187 20011025 00187 EU 2001 10 25 AALA20011673 1 20010822 A 5310 DOOR FRAME AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14056 463 TUL - FOUND CORROSION AT AFT LOWER DOOR FRAME CUT OUT. INSTALLED TRACK SPLICE PER SRM 53-10-15. (M) 2 L 7 2 4F RT A35EU 2001102500191 20011025 00191 EU 2001 10 25 AALA20011732 2 20010910 A 7200 ENGINE FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAYMK65015 EU NR 1 MALFUNCTIONED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 1442E 11437 FLT 2388- EN ROUTE DFW-MDW - DETECTED NR 1 ENGINE OIL PRESSURE LIGHT ILLUMINATE. UNABLE TO START ENGINE. DIVERTED STL AND LANDED WITHOUT FURTHER INCIDENT. REPLACED NR 1 ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F RT 2001102500194 20011025 00194 NM 2001 10 25 AALA20011781 1 20010915 A 2530 86901 OVEN BOEING 767 767323 1385205 NM CABIN DIRTY A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 360AA 24041 CDG - FLT 62 - EN ROUTE MIA-CDG - DETECTED BURNING SMELL AT NR 1 FIRST CLASS OVEN. TURNED OFF OVEN. LANDED CDG WITHOUT FURTHER INCIDENT. CLEANED NUMBER ONE FIRST CLASS OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001102500197 20011025 00197 EU 2001 10 25 AALA20011789 1 20010917 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 50051 459 TUL - FOUND STRINGER CORRODED FS 69-70. REPLACED STRINGER. (M) 2 L 7 2 4F RT A35EU 2001102500198 20011025 00198 EU 2001 10 25 AALA20011790 1 20010917 A 5320 SPLICE AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 50051 459 TUL - FOUND SPLICE ANGLE CORRODED. REPLACED SPLICE ANGLE. (M) 2 L 7 2 4F RT A35EU 2001102500199 20011025 00199 EU 2001 10 25 AALA20011791 1 20010917 A 5320 SPLICE AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 50051 459 TUL - FOUND SPLICE ANGLE CORRODED. REPLACED SPLICE ANGLE. (M) 2 L 7 2 4F RT A35EU 2001102500201 20011025 00201 EU 2001 10 25 AALA20011792 1 20010917 A 5320 SPLICE AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 50051 459 TUL - FOUND CORRODED STRINGER SPLICE ANGLE. REPLACED STRINGER SPLICE. (M) 2 L 7 2 4F RT A35EU 2001102500203 20011025 00203 EU 2001 10 25 AALA20011793 1 20010917 A 5320 SPLICE AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 50051 459 TUL - FOUND CORRODED SPLICE ANGLE. REPLACED SPLICE ANGLE. (M) 2 L 7 2 4F RT A35EU 2001102500205 20011025 00205 EU 2001 10 25 AALA20011794 1 20010917 A 5320 SPLICE AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 50051 459 TUL - FOUND CORROSION ON STRINGER SPLICE ANGLE. REPLACED SPLICE ANGLE. (M) 2 L 7 2 4F RT A35EU 2001102500206 20011025 00206 EU 2001 10 25 AALA20011795 1 20010917 A 5320 SPLICE AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 50051 459 TUL - FOUND CORROSION OF SPLICE ANGLE. REPLACED SPLICE ANGLE. (M) 2 L 7 2 4F RT A35EU 2001102500208 20011025 00208 EU 2001 10 25 AALA20011796 1 20010914 A 5320 SPLICE AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 50051 459 TUL - FOUND CORRODED STRINGER SPLICE ANGLE AT FRAME 65. REPLACED SPLICE ANGLE. (M) 2 L 7 2 4F RT A35EU 2001102500210 20011025 00210 NM 2001 10 25 AALA20014059 1 20010913 A 5330 SKIN BOEING 767 767223 1385123 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 301AA 22307 AFW - FOUND FUSELAGE SKIN AT STATION 553 UNDER S36L HAD CORROSION BLENDED BEYOND SRM LIMITS. REMOVED CORROSION, APPLY A LODINE, PRIMER SURFACES, FILL BLENDS WITH BMS5-95. (M) 2 L 7 2 4F RT A1NM 2001102500213 20011025 00213 EU 2001 10 25 ALA20011672 1 20010822 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14056 463 TUL - FOUND CORROSION ON STRINGER 46R FROM STATION FRAME 65, FRAME 70. REPLACED CORRODED STRINGER SPLICES AND STRINGER SEGMENTS PER SRM 51-75-10. (M) 2 L 7 2 4F RT A35EU 2001102500215 20011025 00215 NM 2001 10 25 USAA011261 1 20010908 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 48384 22962 CLT - FOUND FLOORBEAM CORRODED 4 FEET BY 2 INCHES, STATION 328, BL 0 RIGHT TO SERVICE DOOR. FABRICATED AND INSTALLED T- CAP. (M) 2 L 7 2 4F A16WE 2001102500217 20011025 00217 NM 2001 10 25 USAA011262 1 20010918 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 519AU 23705 CLT - FOUND FUSELAGE SKIN CRACKED, STATION 727D, S23R. INSTALLED REPAIR DOUBLER, PER EA 85486. (M) 2 L 7 2 4F RT A16WE 2001102500220 20011025 00220 NM 2001 10 25 USAA011263 1 20010922 A 5310 SHEAR TIE BOEING 737 737201 1384454 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 22962 CLT - FOUND SHEAR TIE WITH WORKING FASTENERS, STATION 360 ATTACH LUG, BETWEEN STRINGER 28R AND 27R. REPAIRED SHEAR TIE PER SRM 53-10-4 FIG 9A. (M) 2 L 7 2 4F A16WE 2001102500227 20011025 00227 NM 2001 10 25 USAA011264 1 20010919 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 48384 22962 CLT - FOUND SKIN CRACKED 1 INCH, STATION 328 S17R. REPAIR PREVIOUSLY ACCOMPLISHED PER BOEING REPAIR DRAWING 65C2757. ( M) 2 L 7 2 4F A16WE 2001102500230 20011025 00230 NM 2001 10 25 USAA011265 1 20010813 A 5311 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 44029 23742 CLT - FOUND CHORD CRACKED .5 INCH, BS 178, WL 207, LBL 28. SPLICED IN NWE CHORD SECTION PER EO 85479. (M) 2 L 7 2 4F RT A16WE 2001102500232 20011025 00232 NM 2001 10 25 USAA011266 1 20010915 A 5311 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 44029 23742 CLT - FOUND CHORD CRACKED .250 INCH, BS 178, WL 184, LBL 55. SPLICED IN NEW CHORD SECTION. (M) 2 L 7 2 4F RT A16WE 2001102500233 20011025 00233 NM 2001 10 25 USAA011267 1 20010920 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 48384 22962 CLT - FOUND FRAME CRACKED .250 INCH BS 300 S8R. REPLACED UPPER DOOR FRAME WITH LIKE PART. (M) 2 L 7 2 4F A16WE 2001102500234 20011025 00234 NM 2001 10 25 USAA011268 1 20010925 A 5310 6545871523 DOOR FRAME BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 48384 22962 CLT - FOUND DOOR FRAME CRACKED .200 INCH, FORWARD SERVICE DOOR AFT FRAME NR 3 FITTING CUT OUT. INSTALLED DOUBLER PER EA 85464. (M) 2 L 7 2 4F A16WE 2001102500235 20011025 00235 NM 2001 10 25 USAA011270 1 20010921 A 5312 BULKHEAD BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 44029 23742 CLT - FOUND WEB CRACKED .5 INCH, BS 178 WL 207 LBL 1. REMOVED CRACK AND INSTALLED DOUBLER. (M) 2 L 7 2 4F RT A16WE 2001102500236 20011025 00236 NM 2001 10 25 USAA011271 1 20010921 A 5312 BULKHEAD BOEING 737 737301 1384611 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 23742 CLT - FOUND WEB WITH OLD REPAIR REMOVED, STATION 178 WL 187 BL 0. MADE NEW REPAIR AND INSTALLED SAME. (M) 2 L 7 2 4F RT A16WE 2001102500237 20011025 00237 NM 2001 10 25 USAA011272 1 20010813 A 5320 INTERCOSTAL BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 44029 23742 CLT - FOUND INTERCOSTAL CRACKED .250 INCH, BS 178 WL 207 RBL 28. REMOVED AND REPLACED PER EO 5300V157. (M) 2 L 7 2 4F RT A16WE 2001102500238 20011025 00238 NM 2001 10 25 USAA011273 1 20010928 A 5320 STRAP BOEING 737 737301 1384611 NM FUSELAGE BENT A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 44029 23742 CLT - FOUND STRAP BENT AND GOUGED, BS 178 BL 0 WL 181.5. FABRICATED REPLACEMENT STRAP AND INSTALLED. (M) 2 L 7 2 4F RT A16WE 2001102500239 20011025 00239 NM 2001 10 25 USAA011274 1 20010930 A 5312 BULKHEAD BOEING 737 737301 1384611 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 44029 23742 CLT - FOUND WEB DENTED 4 INCHES BY 4 INCHES, BS 178 WL 181.5 BL 0. INSTALLED DOUBLER. (M) 2 L 7 2 4F RT A16WE 2001102500240 20011025 00240 NM 2001 10 25 USAA011275 1 20010813 A 5312 BULKHEAD BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 44029 23742 CLT - FOUND WEB CRACKED 1 INCH, BS 178 WL 213 RBL 5.9 AND LBL 5.9 AND LBL 5.5. CUT OUT DAMAGE AND INSTALLED DOUBLER. ( M) 2 L 7 2 4F RT A16WE 2001102500241 20011025 00241 NM 2001 10 25 USAA011276 1 20010920 A 5347 SEAT TRACK BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 48384 22962 CLT - FOUND SEAT TRACK SECTION CORRODED 1 INCH BY 3 INCHES, STATION 328 TO 360 RBL 55. SPLICE IN NEW SECTION OF TRACK P ER 51-10-1. (M) 2 L 7 2 4F A16WE 2001102500242 20011025 00242 NM 2001 10 25 USAA011277 1 20010929 A 5320 STIFFENER BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 44029 23742 CLT - FOUND CHORD VERTICAL CRACKED .25 INCH, BS 178 WL 184 LBL 505. INSTALLED ANGLE AND STRAP. (M) 2 L 7 2 4F RT A16WE 2001102500243 20011025 00243 NM 2001 10 25 USAA011278 1 20010813 A 5312 BULKHEAD BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 44029 23742 CLT - FOUND WEB CRACKED 1 INCH, BS 178 WL 213 RBL 6. CRACK CUT OUT AND DOUBLER INSTALLED. (M) 2 L 7 2 4F RT A16WE 2001102500244 20011025 00244 NM 2001 10 25 USAA011294 1 20010921 A 5311 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 44029 23742 CLT - FOUND CHORD CRACKED .5 INCH, BS 178 SIDE CHORD RADIUS AT WL 207 LBL 26. CUT OUT DAMAGED SECTION AND SPLICED IN NE W PER EO 5300V157. (M) 2 L 7 2 4F RT A16WE 2001102500245 20011025 00245 NM 2001 10 25 USAA011295 1 20010813 A 5311 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 44029 23742 CLT - FOUND CHORD CRACKED 1 INCH, BS 178 WL 207 RBL 28. CUT OUT DAMAGED SECTION AND SPLICED IN NEW PER EO5300V157. (M) 2 L 7 2 4F RT A16WE 2001102500246 20011025 00246 NM 2001 10 25 USAA011296 1 20010910 A 5311 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 44257 23235 CLT - FOUND CHORD CRACKED .25 INCH, BS 178 WL 207 LBL 26 AND RBL 26. DAMAGE AREAS WERE CUTOUT, SIDE CHORD SPLICE REPAIR S INSTALLED PER EO 5300V157. (M) 2 L 7 2 4F RT A16WE 2001102500247 20011025 00247 NM 2001 10 25 USAA011298 1 20010928 A 5320 655384422 SUPPORT BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 38151 23879 TPA - FOUND CARGO TIE DOWN SUPPORT CORRODED APPROXIMATELY 24 INCHES, STATION 787-847. DEFECTIVE PART REPLACED WITH IDEN TICAL PART NR. (M) 2 L 7 2 4F RT A16WE 2001102500248 20011025 00248 NM 2001 10 25 USAASB01262 1 20010919 A 5230 10608211 SEAL BOEING 737 7373B7 1384580 NM CARGO DOOR OUT OF POSITION A USAA B EMER. DESCENT O OTHER CL CLIMB 1 EA 19 390US 23312 PHL - FLT 867 - ON CLIMB-OUT FROM GSO, AT FL240, THE CABIN ALTITUDE CLIMBED TO 9,700 FEET. NO AUTO FAIL INDICATION WAS NOTED. CREW COULD NOT CONTROL CABIN IN STANDBY OR MANUAL PRESSURIZATION MODES. FLIGHT DESCENDED TO FL100 AND CONTINUED ONTO PHL WHERE THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE FORWARD CARGO DOOR SEAL, AT BOTTOM, OUT OF TH E TRACK. REINSTALLED DOOR SEAL AND PERFORMED OPERATIONAL TEST PER MM 21-31-00. PRESSURIZED AIRCRAFT. NO FAULTS NOTED. (M) 2 L 7 2 4F RT A16WE 2001102500249 20011025 00249 NM 2001 10 25 USAASB01263 1 20010919 A 5210 65C80736354 DOOR BOEING 737 737401 1384701 NM L1 OUT OF RIG A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 421US 23988 PHL - FLT 987 - ON CLIMB-OUT FROM PHL, EN ROUTE TO MCO, CAPTAIN RECEIVED A DOOR LIGHT FOR THE FORWARD MAIN ENTRY DOOR. FIRST OFFICER WENT BACK TO CHECK ON DOOR AND FOUND THE DOOR HANDLE LOOSE. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WI THOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE CHECKED RIGGING OF DOOR AND ADJUSTED AS EPR MM 52-11-00 . OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001102500250 20011025 00250 NM 2001 10 25 USAASB01264 1 20010920 A 5210 DOOR BOEING 737 7373B7 1384580 NM MAIN ENTRY NOT CLOSED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 374US 22953 BUF - FLT 1105 - ON CLIMB-OUT FROM BUF, EN ROUTE TO PHL, THE CABIN WOULD NOT PRESSURIZE. THE FORWARD MAIN ENTRY DOOR WA S SQUEALING SO THE CREW ELECTED TO RETURN TO FIELD AT BUF. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DE CLARED. MAINTENANCE FOUND THE FORWARD MAIN ENTRY DOOR FALSELY LOCKED AS DOOR WAS NOT AGAINST THE FRAME. RECLOSED DOOR AND PRESSURIZED AIRCRAFT. NO LEAKS NOTED. DOOR OPERATION CHECKED NORMAL. (M) 2 L 7 2 4F RT A16WE 2001102500251 20011025 00251 NM 2001 10 25 USAASB01265 1 20010921 A 3260 WARNING SYSTEM BOEING 737 7373B7 1384580 NM COCKPIT MALFUNCTIONED A USAA O OTHER N FALSE WARNING AP APPROACH 1 EA 19 505AU 23380 CLT - FLT 357 - ON APPROACH INTO CLT FROM ATL, CREW RECEIVED THREE GREEN AND THREE RED GEAR LIGHTS AFTER GEAR EXTENSION. CREW RECYCLED GEAR AND RECEIVED NORMAL GEAR INDICATION, THREE GREEN AND NO RED GEAR LIGHTS. FLIGHT LANDED WITHOUT INC IDENT. MAINTENANCE PINNED ALL THREE GEAR AND CYCLED GEAR HANDLE. ALL GEAR INDICATIONS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2001102500252 20011025 00252 NM 2001 10 25 USAASB01266 1 20010922 A 3350 900835A POWER SUPPLY BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 242US 22444 BWI - THE EMERGENCY LIGHTS FOR THE LAST FIVE SEAT ROWS IN THE PASSENGER CABIN WERE INOPERATIVE. MAINTENANCE REPLACED TH E EMERGENCY LIGHT POWER SUPPLY. (M) 2 L 7 2 4F A16WE 2001102500253 20011025 00253 NM 2001 10 25 USAASB01267 1 20010924 A 3350 S106 BATTERY BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 270AU 22882 BWI - THE EMERGENCY EXIT LIGHT ABOVE THE MAIN ENTRY DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATT ERY. (M) 2 L 7 2 4F A16WE 2001102500254 20011025 00254 NM 2001 10 25 USAASB01271 1 20010927 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 775AU 24933 BOS - MAINTENANCE FOUND THE AFT RIGHT SECTION OF CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED T HE BATTERY CHARGER ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001102500255 20011025 00255 NM 2001 10 25 USAASB01272 1 20010927 A 3350 1000679 LIGHT BOEING 737 7372B7 1384560 NM PAX CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 270AU 22882 BWI - THE LEFT AFT EMERGENCY EXIT DOOR LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. (M) 2 L 7 2 4F A16WE 2001102500256 20011025 00256 NM 2001 10 25 USAASB01279 1 20011002 A 3350 29131A BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 335US 23232 TPA - MAINTENANCE FOUND THE EMERGENCY LIGHTS, FROM ROW 4 THROUGH EMERGENCY EXIT ROW, INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED THE MID-CABIN BATTERY PACK, RIGHT SIDE. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001102500257 20011025 00257 NM 2001 10 25 USAASB01280 1 20011003 A 3350 S106 BATTERY BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 279AU 22891 TPA - THE EMERGENCY LIGHT ABOVE THE AFT RIGHT SERVICE DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BA TTERY. (M) 2 L 7 2 4F A16WE 2001102500258 20011025 00258 NM 2001 10 25 USAASB01281 1 20011003 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 428US 24550 MIA - MAINTENANCE FOUND THE EXTERIOR EMERGENCY LIGHT AT R2 DOOR AND THE INTERIOR EMERGENCY LIGHT AT L2 DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001102500264 20011025 00264 EU 2001 10 25 01FDEA00873 1 20011002 A 2760 SPOILER AIRBUS 310 A310203 EU RT WING MALFUNCTIONED A FDEA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 25 407FE 254 ON T/O NR 2 SPOILER POPPED UP ON RT WING. RESET FCC 1 & 2, RESET SPOILER PBS. CHECK OK. 2 L 7 2 4F RT A35EU 2001102500266 20011025 00266 NE 2001 10 25 01FDEA00898 2 20011021 A 7230 COMPRESSOR AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2A5 NE NR 2 ENGINE STALLED A FDEA A UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 25 676FE 790 705265 DURING CLIMBOUT, SEVERE COMPRESSOR STALL NR 2 ENG. 2 L 7 2 4F 4 F RT A35EU E13NE 2001102500267 20011025 00267 WP 2001 10 25 01FDEA00900 1 20011021 A 3230 LANDING GEAR DOUG DC10 DC1030F 3023504 WP NLG & MLG MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 320FE 47835 AFTER T/O, LANDING GEAR WOULD NOT RETRACT. 2 L 7 3 4F RT A22WE 2001102500268 20011025 00268 EU 2001 10 25 01FDEA00902 1 20011023 A 3230 INDICATOR AIRBUS 310 A310 EU LT MGL DAMPER OUT OF POSITION A FDEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 25 424FE 241 UNABLE TO RAISE LG IN POS 1. SWITCH TO POS 2, NO SUCCESS. RESET LT MLG PITCH DAMPER PRESS DROP IND. CHECK OK. 2 L 7 2 4F RT A35EU 2001102500270 20011025 00270 EU 2001 10 25 RAIA00110007 1 20011019 A 2700 C850176 VANE JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 571HK 14299 14299 41090 7214-STL-RIGHT STALL CAPTION ILLUMINATED DURING TAXI. MAINTENANCE REMOVED AND REPLACED THE RIGHT STALL VANE. 2 L 7 2 4T RT A41NM 2001102500271 20011025 00271 2001 10 25 RAIA00110008 4 20011024 A 3400 7011672112 SYMBOL GENERATOR JETAIR JETSTM JETSTM4101 1500501 EU FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 560HK 11893 41076 7200-STL-#2 SYMBOL GENERATOR FAILED. MAINTENANCE REMOVED AND REPLACED # 2 SYMBOL GENERATOR. 2 L 7 2 4T RT A41NM 2001102500272 20011025 00272 EU 2001 10 25 RAIA00110009 1 20011024 A 2700 C850176 VANE JETAIR JETSTM JETSTM4101 1500501 EU FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 571HK 20 20 41090 7071-STL-RIGHT STALL CAPTION LIGHT CAME ON DURING TAXI. MAINTENANCE REMOVED AND REPLACED STALL VANE. 2 L 7 2 4T RT A41NM 2001102600001 20011026 00001 SO 2001 10 26 C2XA01TY161 1 20011025 A 3350 1683 BULB EMB EMB 145 EMB145ER SO CABIN BLOWN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15926 NA 145005 TYS During a scheduled inspection the right emergency exit ceiling light was found not working. Maintenance removed an d replaced the emergency light bulb, operational checks good I.A.W.-EMB-MM-33-50-08. Aircraft will be released upon comp lection of inspection. 2 L 7 2 4F RT T00011AT 2001102600002 20011026 00002 NM 2001 10 26 01FDEA00798 1 20010831 A 2620 COUPLING BOEING 727 72722C 138400F NM EXTINGUISH SYS DEFECTIVE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 105FE 19194 FIRE PROTECTION ENG STRUT FIRE X NOZZLE INSP COMPLY WITH FLEET CAMPAIGN DIRECTIVE 7-26-020. REMOVED AND REPLACED LINE A COUPLING. 2 L 7 3 4F A3WE 2001102600004 20011026 00004 NM 2001 10 26 01FDEA00909 1 20011023 A 2781 WARNING SYSTEM BOEING 727 727173C 1384059 NM COCKPIT MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 199FE 19509 LEADING EDGE NR 6 FAILED DURING FLAP RETRACTION. OPERATED FLAPS & SLATS, ALL IND NORMAL PER MM 27-81-000-0. 2 L 7 3 4F A3WE 2001102600005 20011026 00005 NM 2001 10 26 01FDEA00910 1 20011024 A 2613 WARNING LIGHT BOEING 727 7272S2F 1384O81 NM COCKPIT ILLUMINATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 213FE 22935 ON CLIMB NR 1 ENG STRUT OVERHEAT LIGHT ILLUM. REMOVED AND REPLACED HIGH PRESSURE SUPPLY LINE PER MAINT PRACTICE. 2 L 7 3 4F A3WE 2001102600006 20011026 00006 NM 2001 10 26 CALA0100974 1 20011025 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM BS290 RBL35 CORRODED A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 59338 23576 SEAT TRACK CORRODED BS290 RBL 35. REPLACED SEAT TRACK PER SRM 53-00-52. 2 L 7 2 4F RT A16WE 2001102600007 20011026 00007 NM 2001 10 26 CALA0100975 1 20011025 A 5320 654797321 WEB BOEING 737 7373T0 1384582 NM STA616 17LT CRACKED A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 59338 23576 WEB CRACKED AT STATION 616 AND STR 17 LEFT BELOW LEFT EXIT OPENING. REMOVED AND REPLACED CRACKED WEB PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001102600008 20011026 00008 NM 2001 10 26 CALA0100978 1 20011025 A 5520 65C26388 BRACKET BOEING 737 7373T0 1384582 NM LEFT ELEVATOR CRACKED A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 69333 23571 LEFT ELEVATOR #4 HINGE UPPER ACCESS COVER OUTBOARD ATTACH BRACKET CRACKED. FABRICATED AND INSTALLED NEW BRACKET ON ELEVA TOR PER SRM 51-40-01. 2 L 7 2 4F RT A16WE 2001102600013 20011026 00013 CE 2001 10 26 2001F00473 1 20011023 A 2731 1095243293 TRIM MOTOR BEECH 1900 1900C 1154161 CE ELEVATOR FAILED E JIKA K NONE F FLT CONT AFFECTED AP APPROACH 1 WP 01 31701 548 548 UB2 ON APPROACH TO LANDING PILOT ATTEMPTED TO TRIM NOSE UP WITH NO RESPONSE USING ELECTRIC TRIM. PILOT ATTEMPTED TO USE MAN UAL TRIM AND THE TRIM WHEEL WOULD NOT TURN. PILOT LANDED AIRCRAFT WITHOUT INCIDENT. UPON INSPECTION OF ELEVATOR TRIM S YSTEM FOUND ELECTRIC TRIM SERVO SHAFT WOULD NOT TURN. REPLACED TRIM SERVO ELECTRIC TRIM, OPS CHECK OK. 2 L 7 2 4T RT A24CE 2001102600020 20011026 00020 NM 2001 10 26 2001UALA01714 1 20010813 A 7722 WO635 HARNESS BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 2 ENGINE FAULTY A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 771UA 20675 20675 26932 777049 FLIGHT RETURNED TO FIELD AND LANDED AMBER ALERT DUE TO A HIGH ENGINE TEMPERATURE INDICATION. CREW REPORTS NR 2 EGT BLAN KED ON TAKEOFF. RECOVERED AFTER TAKEOFF BUT WAS FLUCTUATING. MAINTENANCE REPLACED ELECTRICAL HARNESS WO635, AFTER WHIC H THE FAULT DID NOT REOCCUR. THE HARNESS FROM THIS EVENT WAS NOT RECOVERED FOR ENGINEERING ANALYSIS. TYPICAL FAILURE M ODES WHICH HAVE BEEN FOUND WITH EGT HARNESSES IN OTHER CASES INCLUDE LOOSE TERMINALS, INTERNAL AL/CR FAILURE, AND INTERN AL SHORT CIRCUITS. WO635 WAS JUDGED TO BE MOST PROBABLE CAUSE OF THIS EVENT ON ENGINE 777049. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001102600023 20011026 00023 EU 2001 10 26 2001UALA02087 1 20010927 A 2710 31073110 SERVO AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT AILERON MALFUNCTIONED A UALA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 WP 29 442UA 780 UNCOMMANDED RIGHT ROLL IN EXCESS OF 10 DEGREES EXPERIENCED AFTER ENCOUNTER WITH TURBULENCE. THE RT GREEN AILERON SERVO CONTROL WAS REPLACED AND THE OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2001121700099 20011217 00099 NE 2001 12 17 2001UALA02119 2 20011012 A 7230 8A2727 VANE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE FRACTURED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 595UA 9165 28748 726577 NUMBER 1 ENGINE FAILED. UPON DISASSEMBLY THE ROOT CAUSE FOR THE FAILURE WAS LOW PRESSURE TURBINE (LPT) 4TH VANE SULFIDA TION FRACTURE. WHEN THESE VANES FAILED, IT RESULTED IN HEAVY DAMAGE TO THE 5TH, 6TH, & 7TH STAGES OF THE LPT. 2 L 7 2 4F 4 F RT A2NM E17NE 2001102600032 20011026 00032 NM 2001 10 26 2001UALA02121 1 20011012 A 5311 FRAME BOEING 737 737291 138448W NM PWA JT8 JT8D9A 52048 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 981UA 21546 BODY STATION 188 LEFT HAND CHORD CRACKED AT APPROX WL207. MAJOR REPAIR ACCOMPLISHED. STOP DRILLED CHORD. INSTALLED RE PAIR ANGLE. 2 L 7 2 4F 4 F A16WE E2EA 2001102600033 20011026 00033 NM 2001 10 26 2001UALA02122 1 20011014 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 918UA 25385 EXTERNAL FUSELAGE LEFT HAND SIDE STATION 1006 AT STRINGER 13 SKIN HAS 5 DENTS. MAJOR REPAIR ACCOMPLISHED. INSTALLED DO UBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001110800038 20011108 00038 NE 2001 11 8 2001UALA02123 2 20011014 A 7314 S010224 PUMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 ENGINE FAULTY A UALA O OTHER R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 29 527UA 25364 14102 24995 726537 UNABLE TO DEVELOP TAKEOFF POWER ON NUMBER 2 ENGINE. REPLACED ENGINE. ENGINE WAS PLACED IN TEST CELL. FUEL PUMP OUTPUT PRESSURE WAS FOUND TO BE LOW, AT HIGH POWER SETTINGS. PUMP WAS REPLACED AND THE ENGINE DEVELOPED TAKEOFF POWER. 2 L 7 2 4F 4 F RT A2NM E17NE 2001102600034 20011026 00034 2001 10 26 2001UALA02124 4 20011013 A 3414 INDICATOR BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE COCKPIT FAILED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 935UA 26663 ABORTED TAKEOFF AT 120 KNOTS DUE TO INOPERATIVE FIRST OFFICER'S SPEED INDICATOR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121700100 20011217 00100 NM 2001 12 17 2001UALA02126 1 20011013 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 520UA 24890 CABIN FLOOR BEAM CORRODED BETWEEN RBL6 TO RBL 56. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REPLACED T-CAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2001111500021 20011115 00021 NM 2001 11 15 2001UALA02127 1 20011012 A 2910 272T4500313 HYDRAULIC LINE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LT MLG WW SHEARED A UALA K NONE K J FLUID LOSS WARNING INDICATION LD LANDING 1 WP 29 620UA 21880 ON LANDING ROLLOUT EICAS C HYD SYSTEM PRESSURE AND RES QTY LIGHT ILLUMINATED, LOST CENTER SYSTEM COMPLETELY, NOSEWHEEL T ILLER AND FLAPS WOULD NOT RESPOND. FOUND ADP PRESSURE SUPPLY LINE IN LEFT WHEEL SHEARED OFF AT PRESSURE MODULE REF IPC 29-11-76 ITEM 592. REPLACED HYD LINE. THREE EACH HYD LINE MOUNTING BRACKETS FOR ADP PRESSURE LINE DESCRIBED ABOVE ARE CRACKED AND PEELED OFF THE KEEL BEAM. MADE INTERIM REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001102600035 20011026 00035 NM 2001 10 26 2001UALA02128 1 20011015 A 5312 BULKHEAD BOEING 737 737291 138448W NM PWA JT8 JT8D9A 52048 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 981UA 21546 BODY STATION 178 BULKHEAD CRACK INDICATIONS AT WL 190, WL 195, WL 198 AND WL 203 RBL 5 TO RBL 5.7. MAJOR REPAIR ACCOMPL ISHED. INSTALLED 5 X 20 INCHES DOUBLER. 2 L 7 2 4F 4 F A16WE E2EA 2001102600036 20011026 00036 NM 2001 10 26 2001UALA02129 1 20011015 A 5320 INTERCOSTAL BOEING 737 737291 138448W NM PWA JT8 JT8D9A 52048 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 981UA 21546 BODY STATION 188 RIGHT SIDE INTERCOSTAL CRACKED AT WL 207. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F A16WE E2EA 2001102600037 20011026 00037 WP 2001 10 26 01FDEA00914 1 20011025 A 5410 SKIN DOUG DC10 DC1010 3022110 WP #2 ENG INLET CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 N 192 & N 351 #2 ENG INLET, AFT SIDE CRACK IN SKIN. R&R SKIN PER SRM 54-10-00 & 55-31-01 & EA 8-5410-56140. 2 L 7 3 4F A22WE 2001110800017 20011108 00017 NM 2001 11 8 01FDEA00918 1 20011025 A 5531 65174635 STRINGER BOEING 727 727233 138408A NM VERTICAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 279FE 22346 VERTICAL STABILIZER MAIN BOX INTERIOR STRINGER IS CRACKED AT FIN BS 157.2, STR 8 RT. REMOVED AND REPLACED STRINGER PER S RM 55-30-4 & EA 7-5530-59891. 2 L 7 3 4F RT A3WE 2001110800019 20011108 00019 NM 2001 11 8 01FDEA00920 1 20011025 A 5531 65174637 STRINGER BOEING 727 727233 138408A NM VERTICAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 279FE 22346 VERTICAL STAB MAIN BOX INTERIOR STRINGER IS CRACKED AT FIN STA 110.4, STR 9 LT. REMOVED AND REPLACED STRINGER PER SRM 55 -30-4 FIG 1 & EA 7-5530-59892. 2 L 7 3 4F RT A3WE 2001110700119 20011107 00119 NM 2001 11 7 01FDEA00926 1 20011026 A 5311 65159362 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 279FE 22346 FRAME DENTED BS 660 JUST ABOVE STR 24L. REMOVED AND REPLACED FRAME PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 2001110800039 20011108 00039 NE 2001 11 8 2001UALA02130 2 20011014 A 7397 158309 SHIELD BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE LT ENGINE DAMAGED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 207UA 30213 222102 AFTER TAKEOFF AND ABOUT 4000 FT, THE FUEL FILTER BLOCKAGE EICAS MSG CAME ON ASSOCIATED WITH LEFT ENGINE. CREW DECLARED AN EMERGENCY AND RETURNED TO IAD. LANDED WITHOUT INCIDENT. THIS ENG HAS EXPERIENCED 2 INSTANCES OF FUEL FILTER STATUS M SG. THE FUEL FILTER DIFF PRESSURE SWITCH WAS REPLACED ON 12OCT AND THE MSG REOCCURRED ON 14OCT. THE FILTERWAS CKD, NO CONTAMINATION WAS FOUND, AND THE FILTER WAS REPLACED. ACCOMPLISHED WIRE CKS. REPLACED CONNECTOR (DS73001) AT SWITCH (S 73001) AND FOUND SHIELDING DAMAGED. REPAIRED SHIELDING. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001110800040 20011108 00040 NM 2001 11 8 2001UALA02131 1 20011014 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 520UA 24890 CABIN FLOORBEAM HAS EXCESSIVE CORROSION BETWEEN RBL 6 - RBL 56 STATION 365. MAJOR REPAIR ACCOMPLISHED. INSTALLED T-CAP SPLICE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001102600038 20011026 00038 NM 2001 10 26 2001UALA02132 1 20011015 A 5311 FRAME BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 181UA 25278 FORWARD PIT FRAME WEB AT STATION 620 RBL 40 PUNCTURED. MAJOR REPAIR ACCOMPLISHED TO FORWARD PIT WEB AT STATION 620 RBL 40. 2 L 7 4 4F 4 F RT A20WE E24NE 2001102600039 20011026 00039 NM 2001 10 26 2001UALA02133 1 20011016 A 5312 BULKHEAD BOEING 737 737291 138448W NM PWA JT8 JT8D9A 52048 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 981UA 21546 BULKHEAD 178 HAS DEEP GOUGES IN SKIN AT WL 206 LBL 24. MAJOR REPAIR ACCOMPLISHED. INSTALLED SKIN DOUBLER REPAIR. 2 L 7 2 4F 4 F A16WE E2EA 2001102600040 20011026 00040 NM 2001 10 26 2001UALA02134 1 20011017 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 917UA 25384 MULTIPLE DAMAGE AREAS WERE FOUND ON UPPER AND LOWER SKIN ASSY DUE TO CORROSION AND OBLONG HOLES STATION 992 - 1016 STRIN GER 10L - 14L. STRINGERS 12 - 14L ALSO DAMAGED DUE TO OBLONG HOLES. MAJOR REPAIR ACCOMPLISHED AT BODY STATION 992 - 10 16. STRINGERS 12L - 14L AND SKIN SECTION REPLACED, INSTALLED DOUBLER AND TRIPLER LOWER SKIN SPLICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2001102600041 20011026 00041 NM 2001 10 26 2001UALA02135 1 20011019 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 336UA 24240 STATION 978 WL 209 LBL 45 STRINGER 17 ZEE CREASE BEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM. 2 L 7 2 4F 4 F RT A16WE E2GL 2001102600042 20011026 00042 NM 2001 10 26 2001UALA02136 1 20011018 A 5310 DOOR FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 917UA 25384 AFT PIT DOOR CUTOUT AFT FRAME BETWEEN STRINGER 23 & 22 CARGO DOOR SKIN CUTOUT FRAME, SKIN DENTED. MAJOR REPAIR ACCOMPL ISHED. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001102600043 20011026 00043 NM 2001 10 26 2001UALA02137 1 20011017 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 336UA 24240 AFT CABIN RIGHT HAND CREASE BEAM HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM FROM STA TION 927 TO 990. 2 L 7 2 4F 4 F RT A16WE E2GL 2001102600044 20011026 00044 NM 2001 10 26 2001UALA02138 1 20011017 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 336UA 24240 FORWARD RIGHT HAND FUSELAGE DENT JUST AFT OF STATION 294 BETWEEN STRINGER 20 & STRINGER 21R. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR AND INCORPORATE TEARSTRAP REPAIR WITH DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001102600045 20011026 00045 NM 2001 10 26 2001UALA02139 1 20011017 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 646UA 25283 FLOORBEAM AT BODY STATION 347, BL 48 IS CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER ON FLOORBEAM. 2 L 7 2 4F 4 F RT A1NM E24NE 2001102600046 20011026 00046 NM 2001 10 26 2001UALA02140 1 20011017 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 646UA 25283 CORROSION ON FLOORBEAM AT STATION 1188 TO 1197, RBL 38, AFT CARGO COMPARTMENT. MAJOR REPAIR ACCOMPLISHED. INSTALLED NE W T-CAP SECTION. 2 L 7 2 4F 4 F RT A1NM E24NE 2001102600047 20011026 00047 NM 2001 10 26 2001UALA02141 1 20011017 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 646UA 25283 CABIN FLOORBEAM CRACKED AT STATION 303, LBL 57. MAJOR REPAIR ACCOMPLISHED. INSTALLED T-CAP AND DOUBLER ON FLOORBEAM. 2 L 7 2 4F 4 F RT A1NM E24NE 2001102600048 20011026 00048 NM 2001 10 26 2001UALA02145 1 20011019 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 918UA 25385 STATION 188 TO 196 HORIZONTAL OUTBOARD WEB LEFT HAND SIDE AT WL 207 REPLACED INSTALLED SKIN DOUBLER. MAJOR REPAIR ACCO MPLISHED. INSTALLED DOUBLER WITH TRIPLERS AT STATION 178 TO 193 AND WL 195 TO 215. 2 L 7 2 4F 4 F RT A16WE E2GL 2001110800041 20011108 00041 NM 2001 11 8 2001UALA02146 1 20011019 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 336UA 24240 FUSELAGE FRAME CRACKED AT STATION 400 STRINGER 9L. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED REINFORCEMENT REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001102600049 20011026 00049 NM 2001 10 26 UPS01237178 1 20011021 A 2730 ANGLE BOEING 727 72722C 138400F NM STN. 35.0 APPROX CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE:C R/H ELEVATOR (REF X-RAY) CRACK NOTED IN LWR ANGLE INTERNAL APPROX LO CATION 6" AFT OF FRONT SPAR AT ST N 35.0 REPLACED LWR ANGLE AT STN. 35.0 IAW DRAWING 65-25634 2 L 7 3 4F A3WE 2001102600050 20011026 00050 EA 2001 10 26 COMA0160851 1 20011019 A 2760 COMPUTER CNDAIR CL600 CL6002B19 EA A COMA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 01 420CA 7451 FLIGHT #5880 CONFIG SPOILERS AND RUDDER MESSAGE DURING T/O.RESET SYSTEM, OPERATIONAL CHECK NORMAL. COULD NOT DUPLICATE. 2 L 7 2 4F RT A21EA 2001102600051 20011026 00051 WP 2001 10 26 ABXA010541 1 20011009 A 5320 5912494501 PAN DOUG DC9 DC933F 302207A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 FORWARD LOWER CARGO LOWER DOOR JAMB HAD CORROSION BULGE BETWEEN THE LOWER STOPS. REPAIRED AREA IAW REA D953-42441-MR. LEVEL  CORROSION. 2 L 7 2 4F A6WE 2001102600052 20011026 00052 2001 10 26 COMA0160853 4 20011024 A 2210 13740002 SWITCH CNDAIR CL600 CL6002B19 EA COCKPIT FAULTY A COMA O OTHER S AFFECT SYSTEMS IN INSP/MAINT 1 SO 01 960CA 7117 FLIGHT #5570. DURING TEST OF THE YAW DAMPER SYSTEM THE #2 WOULD NOT ENGAGE.REPLACED THE YAW DAMPER SWITCH. 2 L 7 2 4F RT A21EA 2001102600053 20011026 00053 WP 2001 10 26 ABXA010548 1 20011011 A 5320 992345946 ATTACH ANGLE DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 INTERCOSTAL ATTACH ANGLES WERE CRACKED INSIDE THE ANTI-COLLISION LIGHT PANEL AT THE RIGHT BUTT LINE 8.0 AND THE LEFT BUT T LINE FS 743. REPLACED THE ANGLES IAW DC-9 SRM 51-30-1, P/N 9923459-46 AND 9923459-45. 2 L 7 2 4F A6WE 2001102600054 20011026 00054 NE 2001 10 26 ARWA0011010 2 20011019 A 7200 ENGINE LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B402 54555 NE NR 3 VIBRATION A ARWA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 19 308GB 193U1133 EXPERIENCED SUDDEN INCREASE IN VIBRATION ON NR 3 ENGINE FROM 1.2 TO 2.4. RETURNED TO MIAMI FOR AN UNEVENTFUL LANDING. LUBED CLAPPERS, CHECKED CHIP DETECTORS ACCOMPLISHED TEST NR 11 VIBRATION SURVEY IAW L1011 FORM 7102B VIBRATION WITHIN LI MITS. 2 L 7 3 4F 4 F A23WE E12EU 2001102600055 20011026 00055 NE 2001 10 26 ARWA0011011 2 20011019 A 7200 ENGINE LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B402 54555 NE NR 3 VIBRATION A ARWA C ABORTED TAKEOFF E J VIBRATION/BUFFET WARNING INDICATION TO TAKEOFF 1 SO 19 308GB 193U1133 ON TAKEOFF ROLL C&W PANEL ENGINE VIBRATION FILTER PRESS LIGHT ON NR 3 ENGINE INDICATING 2.6 UNITS FAN POSITION. ABORTED TAKEOFF AT 80 KNOTS POWER SETTING .427 EPR. CHECKED CHIP DETECTORS AND MAIN OIL SCREEN, ALL OK. LUBED BLADES IAW MM 7 2-31-05, PERFORMED TEST 11 VIBRATION SURVEY WITHIN LIMITS IAW MM 71-91-00. BOROSCOPE DEFERRED FOR 25 HRS IAW 71-00-00. 2 L 7 3 4F 4 F A23WE E12EU 2001102600056 20011026 00056 NE 2001 10 26 ARWA0011012 2 20011020 A 7230 COMPRESSOR LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B402 54555 NE NR 3 ENGINE VIBRATION A ARWA E ENGINE SHUTDOWN E VIBRATION/BUFFET CR CRUISE 1 SO 19 308GB 193U1133 AIRFRAME VIBRATION FELT FOLLOWED BY INCREASED VIBRATION ON NR 3 ENGINE. ENGINE SHUTDOWN PER CHECKLIST, REPORTED TIME 16 :50Z. REMOVED AND REPLACED LP FAN BLADES IAW MM 72-31-05, REMOVED 3 HOLE BALANCE WEIGHT FROM THRUST RING. RAN ENGINE N R 3, PERFORMED TEST NR 16 IAW MM 71-00-00. VIBRATION SURVEY WITHIN LIMITS. ENGINE OK FOR SERVICE. 2 L 7 3 4F 4 F A23WE E12EU 2001102600057 20011026 00057 SO 2001 10 26 C2XA01CL218 1 20011021 A 2120 ODOR EMB 145 EMB145LR SO CABIN DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 16961 145103 CLE, THE CREW REPORTED A BURNING SMELL COMING FROM PACK 2. MAINTENANCE INSPECTED AND OPERATIONAL CHECKS WERE PERFORMED ON THE AIR CONDITIONING SYSTEM. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001102600058 20011026 00058 NM 2001 10 26 CALA0100966 1 20011022 A 5315 BAC1506210 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69333 23571 FLOORBEAM STATION 986.5 HAS SEVERAL CORRODED HOLES AT UPPER FLANGE (TOP AND BOTTOM). REPAIRED FLOORBEAM PER EC/RA 5310- 03851. 2 L 7 2 4F RT A16WE 2001102600059 20011026 00059 NM 2001 10 26 CALA0100969 1 20011024 A 5314 KEEL BOEING 737 7373T0 1384582 NM FUSELAGE WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69333 23571 STRUCTURE AROUND HOLES FOR ATTACHMENT OF WHEEL WELL FAIRING WORN IN LEFT MLG. REPAIRED AREA ON KEEL REQUIRED BY EC/RA 5 310-03740. 2 L 7 2 4F RT A16WE 2001102600060 20011026 00060 NM 2001 10 26 CALA0100971 1 20011024 A 5512 6573783 SKIN BOEING 737 7373T0 1384582 NM HORIZ STAB DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69333 23571 DENT IN LEADING EDGE OF RIGHT HORIZONTAL STABILIZER AT STATION 263. PERFORMED INTERIM REPAIR PER SRM 55-10-01. PERMANE NT REPAIR REQUIRED IN 18 MONTHS. 2 L 7 2 4F RT A16WE 2001102600061 20011026 00061 NM 2001 10 26 DHL2001712018 1 20011023 A 2610 CLAMP BOEING 727 72729 1384007 NM DETECTION SYS LOOSE A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 712DH 19401 NR 3 CIRCUIT DETECTOR GROUND LIGHT ILLUMINATED IN FLIGHT. FOUND LOOSE GROUND CLAMP. RESECURED LOOSE CLAMP IAW B-M/M 26 -14-000, OPS CHECK GOOD. 2 L 7 3 4F A3WE 2001102600062 20011026 00062 NM 2001 10 26 DHL2001712019 1 20011023 A 2612 FIRE LOOP BOEING 727 72729 1384007 NM NR 3 ENGINE OUT OF POSITION A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 712DH 19401 NR 3 FIRE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED AFTER TAKEOFF. NR 3 FIRE LOOP REPOSITIONED AWAY FROM COWL. GROUND FAULT LIGHTS. OPS OK PER BMM 26-11-00. 2 L 7 3 4F A3WE 2001102600063 20011026 00063 NM 2001 10 26 DHL2001742523 1 20011020 A 5311 FRAME BOEING 727 727225 1384077 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 DURING C-CHECK, FRAME CRACK LT STA 360 12 INCHES ABOVE FLOOR PANEL. CUT OUT DAMAGED AREA. INSTALLED FRAME REPAIR. 2 L 7 3 4F A3WE 2001102600064 20011026 00064 2001 10 26 DHL2001749001 4 20011023 A 2211 COMPUTER BOEING 727 727200 138407E NM AUTOPILOT SYS MALFUNCTIONED A DHLA O OTHER F FLT CONT AFFECTED DE DESCENT 1 SO 01 749DH 22013 DESCENDING THRU 12,000 FEET WITH AUTO PILOT ENGAGED, AIRCRAFT WENT INTO UNCOMMANDED ROLL TO THE RIGHT. REMOVED AND REPL ACED ROLL CHANNEL, IAW B727 MM 22-11-111, OPS CHECKED GOOD IAW B727 MM 22-10-0. OPS CHECKED GOOD. 2 L 7 3 4F RT A3WE 2001102600065 20011026 00065 WP 2001 10 26 DHL2001801527 1 20011010 A 5532 SKIN DOUG DC8 DC873F 302199F WP VERTICAL STAB DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 VERTICAL STABILIZER LEFT OUTER SKIN DENTED 3 INCHES AT 2 R 159.961. REMOVED DAMAGED SKIN FROM VERTICAL STABILIZER AND F ABRICATED NEW ONE PER SRM 55-2-0 PG 1-2 AND SRM 55-51 FIG 1. INSTALLED NEW SKIN PER SRM 55-2-0 PG 1-2. 2 L 7 4 4F RT 4A25 2001102600066 20011026 00066 WP 2001 10 26 DHL2001801528 1 20011010 A 5210 SKIN DOUG DC8 DC873F 302199F WP PAX DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 FWD PASSENGER DOOR INNER SKIN UPPER PART CRACKED .5 INCH. STOP DRILLED CRACK PER SRM 53-2-0 FIG 1B. FABRICATED DOUBLER PER SRM 53-2-0 FIG 1B. INSTALLED DOUBLER PER SRM 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 2001102600067 20011026 00067 WP 2001 10 26 DHL2001801529 1 20011009 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 RT WING CNTR L/E INTERIOR RIB CRACKED .5 INCH (LWR) AT XFS 385.000. STOP DRILLED CRACK PER SRM 57-2-1 PAR 7. FABRICATE D REINFORCING ANGLE PER SRM 57-2-1 PAR 7. INSTALLED REINFORCING ANGLE PER SRM 57-2-1 PAR 7. 2 L 7 4 4F RT 4A25 2001110600090 20011106 00090 NM 2001 11 6 P2EA2001V0001 1 20011019 A 5330 SKIN BOEING 737 737230 1384401 NM FUSELAGE DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 124NJ 22122 DURING C CHECK: EXTERNAL FUSELAGE AT BS 1042 BETWEEN STR 14L AND 15L SKIN WITH DENT. FUSELAGE SKIN SECTION REPAIRED FROM BS 1039 TO BS 1048 BETWEEN STR 13L TO STR 16L IAW SRM 53-30-3 FIG 6. 2 L 7 2 4F RT A16WE 2001110600093 20011106 00093 NM 2001 11 6 P2EA2001V0004 1 20011019 A 5314 KEELBEAM BOEING 737 737230 1384401 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 124NJ 22122 DURING C CHECK FOUND THE AFT CARGO COMPARTMENT STR 27R AT BS 727+16 KEEL BEAM CHORD WITH CRACK. FUSELAGE KELL BEAM SECTI ON REPAIRED AT STR 27R, BETWEEN BS 727+9.75 AND BS 727A+7.25 DUE TO CRACK IAW COOPESA E.O NR COO-3-53-585-01. DOCUMENTED ON FAA FORM 8110-3 APPROVED BY FAA DER. 2 L 7 2 4F RT A16WE 2001110600096 20011106 00096 NM 2001 11 6 P2EA2001V0007 1 20011019 A 5230 CROSSBEAM BOEING 737 737230 1384401 NM CARGO DOOR CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 124NJ 22122 DURING C CHECK WAS FOUND THE FWD CARGO DOOR, FWD LOWER CORNER CROSS BEAM CRACKED. FWD CARGO DOOR CROSS BEAM FWD T CHORD AND PERFORMED PREVENTIVE MODIFICATION IAW SB 737-52A1100 REV 4, SECTION III FIG 4 AND 6. 2 L 7 2 4F RT A16WE 2001103100017 20011031 00017 NM 2001 10 31 SABA011057 1 20011026 A 7603 MS24166D1 RELAY DHAV DHC8 DHC8103 1386005 NM NR 2 ENGINE FAILED A SABA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 33 801WP 086 FLIGHT 5212 GREENVILLE, NC TO CHARLOTTE; AIRCRAFT ABORTED TAKEOFF DUE TO NUMBER TWO ENGINE WAS SLOW TO ACCELERATE. ENGI NE CONTROL UNIT SEEMED TO BE WORKING AS IT SHOULD. PILOT ALSO REPORTED A TWO KNOB SPLIT ON THE POWER LEVERS WITH NUMBER TWO LAGGING BEHIND. MAINTENANCE CHECKED ECU AND CHECKED GOOD. THE NUMBER TWO ENGINE UP-TRIM RELAY WAS FOUND BAD. REM OVED AND REPLACED RELAY (K-12), GROUND RUN AND OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 2001102800001 20011028 00001 SO 2001 10 28 C2XA01TY163 1 20011028 A 5315 13500467401 FLOOR SUPPORT EMB 135 EMB135ER 3260203 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16510 145251 TYS Several areas of corrosion were found on the aft side of service door aft of frame 22.Maintenance removed floor sup port and replaced it with a new part IAW emb135/145 SRM 51-40-02 and 51-10-02-Work was satisfactory and aircraft will be released upon completion of scheduled maintenance. 2 L 7 2 4F RT T00011AT 2001102900001 20011029 00001 2001 10 29 C2XA01TY164 4 20011028 A 3445 DMNI5042 ANTENNA EMB 135 EMB135ER 3260203 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16510 145251 TYS During a scheduled inspection the lower TCAS antenna was found with corrosion on the base. Maintenance removed and replaced the antenna, operational checked good. I.A.W.-EMB-AMM-34-43-03. Repair procedure was satisfactory and the aircr aft will be released upon complection of inspection. 2 L 7 2 4F RT T00011AT 2001102900002 20011029 00002 SO 2001 10 29 C2XA01TY165 1 20011028 A 5321 14521725013 SEAL EMB 135 EMB135ER 3260203 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16510 145251 TYS During a scheduled inspection, corrosion was found on the right floor seal at frame 18. Maintenance removed surface corrosion, alodined, primed and painted. I.A.W.-EMB135/145-CMP-51-21-04,05 and 06. Repair procedure was satisfactory an d the aircraft will be released upon complection of inspection. 2 L 7 2 4F RT T00011AT 2001102900003 20011029 00003 SO 2001 10 29 C2XA01TY166 1 20011028 A 5320 14522460005 GUSSET EMB 135 EMB135ER 3260203 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16510 145251 TYS During a scheduled inspection, corrosion was found on the floor gussets at the entrance to the cockpit, between fra mes 15 and 18. Maintenance removed and replaced gusset and center section of forward digital plate (fabricated doubler, shims and cockpit step bracket),alodined, primed and painted. I.A.W.-EMB135/145-SRM-51-40-02 and CMP-51-21-04,05 and 06. , and EC5320-01059. Repair procedure was satisfactory and the aircraft will be released upon complection of inspection. 2 L 7 2 4F RT T00011AT 2001102900004 20011029 00004 SO 2001 10 29 C2XA01TY168 1 20011028 A 3500 214C40183 SWITCH EMB 135 EMB135ER 3260203 SO INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16510 3265 145251 TYS During a scheduled inspection, When doing inspection task card # 35-20-00-720-001-A00, the cabin oxygen masks did n ot deploy in auto mode. Maintenance removed and replaced the altitude sensing switch. I.A.W.-EMB-135-AMM-51-40-02. opera tional checked good. Repair procedures where satisfactory, aircraft will be released upon complection of inspection. 2 L 7 2 4F RT T00011AT 2001102900005 20011029 00005 2001 10 29 SWAA012873 4 20011019 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM AFT ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 527SW 26569 AFT ENTRY DOOR EMERGENCY EVAC SLIDE FASTENER LOOSE ON SLIDE CONTAINER. SECURED CONTAINER PER MM. 2 L 7 2 4F RT A16WE 2001102900006 20011029 00006 NM 2001 10 29 SWAA012874 1 20011018 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 705SW 27839 EEPLS WIRES EXPOSED AT ROW 8. REINSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2001102900007 20011029 00007 NM 2001 10 29 SWAA012875 1 20011021 A 2560 A170033 STRAP BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 617SW 27700 FWD EMERGENCY FLASH LIGHT STRAP BROKEN. R&R STRAP PER MM. 2 L 7 2 4F RT A16WE 2001102900008 20011029 00008 NM 2001 10 29 SWAA012876 1 20011021 A 2560 A170033 STRAP BOEING 737 7373L9 1384470 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 AFT LOWER EMERGENCY FLASH LIGHT STRAP BROKEN. R&R STRAP PER MM.. 2 L 7 2 4F RT A16WE 2001102900009 20011029 00009 NM 2001 10 29 SWAA012881 1 20011017 A 5310 6546546 SHEAR TIE BOEING 737 7373Q8 1384670 NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 847, RBL 2 & WL156. R&R SHEAR TIE PER SR M. 2 L 7 2 4F RT A16WE 2001102900010 20011029 00010 NM 2001 10 29 SWAA012882 1 20011017 A 5310 6546569 FRAME BOEING 737 7373Q8 1384670 NM AFT CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 1018, RBL 1 & WL 191. REPAIRE D FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001102900011 20011029 00011 NM 2001 10 29 SWAA012885 1 20011020 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 FUSELAGE SKIN CRACKED AT APPROX BS 882, ABOVE LAP JOINT RH SIDE. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001102900012 20011029 00012 NM 2001 10 29 SWAA012886 1 20011020 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 FUSELAGE SKIN CRACKED AT APPROX BS 787, STR 10R. REPAIRED SKIN PER SWA RA 1-A53-2545. 2 L 7 2 4F RT A16WE 2001102900013 20011029 00013 NM 2001 10 29 SWAA012887 1 20011021 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED 2.5 INCHES AT BS 520, STR 12L. REPA IRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001102900014 20011029 00014 NM 2001 10 29 SWAA012896 1 20011019 A 3350 101114 LENS BOEING 737 7373Q8 1384670 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED C4 CHECK, FOUND LH OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2001102900015 20011029 00015 NM 2001 10 29 SWAA012899 1 20011019 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 2 INCHES AT BS 967, STR 22L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001102900016 20011029 00016 NM 2001 10 29 SWAA012900 1 20011020 A 5310 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 460, STR 17B. REPAIR ED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2001102900017 20011029 00017 NM 2001 10 29 SWAA012901 1 20011020 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FWD SVC DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SVC DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM & SWA RA 1-353-2681. 2 L 7 2 4F RT A16WE 2001102900018 20011029 00018 NM 2001 10 29 SWAA012902 1 20011022 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 063SW 22061 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED ATBS 760, STR 21L REPAIRED S KIN PER SRM. 2 L 7 2 4F A16WE 2001102900019 20011029 00019 NM 2001 10 29 SWAA012903 1 20011021 A 5752 6546455 TAB BOEING 737 7373H4 1384600 NM LH AILERON DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND LH AILERON TAB DELAMINATED AT T/E. R&R TAB PER MM. 2 L 7 2 4F RT A16WE 2001102900020 20011029 00020 NM 2001 10 29 SWAA012904 1 20011022 A 5310 6546536 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, BETWEEN STR 8R & 9R. REPA IRED FRAME PER BFG ER 01-0885. 2 L 7 2 4F RT A16WE 2001102900021 20011029 00021 NM 2001 10 29 SWAA012905 1 20011021 A 5753 6546435277 FLAP BOEING 737 7373H4 1384600 NM LH WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 655WN 28400 DURING SCHEDULED C4 CHECK, FOUND OTBD AFT T/E FLAP DELAMINATED AT INBD END. R&R FLAP PER MM. 2 L 7 2 4F RT A16WE 2001102900022 20011029 00022 NM 2001 10 29 SWAA012907 1 20011018 A 5310 6546529 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 8L. R&R SHEAR TIE PER BFG ER 0 1-0908. 2 L 7 2 4F RT A16WE 2001102900023 20011029 00023 NM 2001 10 29 SWAA012908 1 20011022 A 5754 6573714 SLAT BOEING 737 7373H4 1384600 NM LH WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED C3 CHECK, FOUND ( 7 EA ) CRACKS AT # 2 L/E SLAT ON AFT ROW OF RIVETS LOWER T/E. REPAIRED SLAT PER SWA RA 1-357-1125. 2 L 7 2 4F RT A16WE 2001102900024 20011029 00024 NM 2001 10 29 SWAA012909 1 20011020 A 5330 6545773 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT RH WINDOW'S JUST BELOW STR 11L, BS 384, 424, 444, 484, 500, 500A & 500B. REPAIRED SKIN PER SWA RA 1-353-2685. 2 L 7 2 4F RT A16WE 2001102900025 20011029 00025 NM 2001 10 29 SWAA012911 1 20011023 A 5310 6545629 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 360, BETWEEN STR'S 28L & 28R. REPAIRED SHEAR TIE PER SRM & BFG ER 01-0911. 2 L 7 2 4F RT A16WE 2001102900026 20011029 00026 NM 2001 10 29 SWAA012912 1 20011023 A 5330 6545774 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED ( 2 EA ) AT BS 727, STR 20L, 3 INCHES LONG & BS 767, STR 19R, 2 INCHES LONG. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001102900027 20011029 00027 NM 2001 10 29 SWAA012913 1 20011022 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 719SW 27853 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS BROKEN ( 26 EA ) IN CABIN. R&R COVERS PER M M. 2 L 7 2 4F RT A16WE 2001102900028 20011029 00028 NM 2001 10 29 SWAA012916 1 20011023 A 3350 6949956 LENS BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 527SW 26569 DURING SCHEDULED C1 CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 2DEF. R&R LENS PER MM. 2 L 7 2 4F RT A16WE 2001102900029 20011029 00029 NM 2001 10 29 SWAA012917 1 20011023 A 5510 65C25727 SKIN BOEING 737 7373G7 1384595 NM LH HORIZ STAB. CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED C4 CHECK, FOUND SKIN CRACKED 2 INCHES LONG ON LH HORIZONTAL STAB LOWER SURFACE, .062 INCH FROM SURFACE ROOT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001102900030 20011029 00030 NM 2001 10 29 SWAA012918 1 20011024 A 5330 6545776 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 957 TO BS 961, STR 21L. REPA IRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001102900031 20011029 00031 2001 10 29 SWAA012927 4 20011024 A 2565 61620468 SLIDE BOEING 737 7375H4 138449D NM FWD SVC DOOR DIRTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 512SW 24189 DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND WINDOW DIFFICULT TO SEE THROUGH. CLEANED WINDOW PER MM. 2 L 7 2 4F RT A16WE 2001102900032 20011029 00032 NM 2001 10 29 SWAA012929 1 20011024 A 3350 6949956 LENS BOEING 737 7373G7 1384595 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 683SW 24008 DURING SCHEDULED C4 CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY LIGHT LENS BROKEN AT ROW 3 ABC. R&R LENS PER MM. 2 L 7 2 4F RT A16WE 2001102900033 20011029 00033 NM 2001 10 29 SWAA012930 1 20011025 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 324SW 23414 DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR CUTOUT SKIN CRACKED AT BS 300, WL 210. REPAIRED SKIN PER SWA RA. 2 L 7 2 4F RT A16WE 2001102900034 20011029 00034 NM 2001 10 29 C1HA200184013 1 20011012 A 3350 6013211 BATTERY PACK BOEING 727 7272S7 138407Z NM INOPERATIVE A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 684CA 22491 BOTH L-2 & R-2 DOOR EXTERIOR EMERGENCY EXIT LIGHTS INOP. (EMERGENCY ESCAPE SLIDE LTS) ACTION TAKEN: R&R AFT EMERGENCY ESCAPE SLIDE EXIT DOOR LIGHT BATTERY & POWER SUPPLY IAW MM 33-50-51 OPS. CHECK GOOD. 2 L 7 3 4F A3WE 2001102900035 20011029 00035 NM 2001 10 29 C1HA200192009 1 20011011 A 3350 900542 BATTERY PACK BOEING 727 727212 138407G NM INOPERATIVE A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 AFT AIRSTAIRS EMERGENCY EXIT LIGHT INOP. ACTION TAKEN: REPLACED BATTERY PACK AND OPS CHECK GOOD PER MM 33-50-1. 2 L 7 3 4F A3WE 2001102900036 20011029 00036 NE 2001 10 29 C1HA200182013 2 20011004 A 7270 JT8D17A ENGINE BOEING 727 7272S7 138407Z NM PWA JT8 JT8D17AR 52049 NE A C1HA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 682CA 22019 689893 AFTER DEPARTURE IN CANCUN, #3 ENGINE BYPASS LIGHT ILLUMINATED ALSO LOUD VIBRATION IN #3 ENGINE PULLED POWER TO FLIGHT ID LE. ACTION TAKEN: REPLACED #3 ENGINE, TRIMMED AND OPS CHECKED GOOD IAW CHAMPION AIR TASK CARD 7101. 2 L 7 3 4F 4 F A3WE E2EA 2001102900037 20011029 00037 NM 2001 10 29 C1HA200197007 1 20011014 A 3350 400542 LIGHT BOEING 727 727270 138408P NM INOPERATIVE A C1HA K NONE O OTHER UK UNKNOWN 1 GL 15 697CA 23052 AFT OVERHEAD EMERGENCY LIGHT INOPERATIVE. ACTION TAKEN: REPLACED AFT BATTERY POWER SUPPLY OPS CHECKS GOOD IAW MM 33-50 -71. 2 L 7 3 4F RT A3WE 2001102900038 20011029 00038 NM 2001 10 29 C1HA200197008 1 20011008 A 3350 900542 LIGHT BOEING 727 727270 138408P NM INOPERATIVE A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 NEST TO AFT OVERHEAD EMERGENCY LIGHT INOPERATIVE. ACTION TAKEN: REPLACED NEXT TO AFT OVERHEAD LIGHT, OPS CHECKS GOOD I AW MM 33-50-71. 2 L 7 3 4F RT A3WE 2001103000061 20011030 00061 NM 2001 10 30 DHL2001742542 1 20011008 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM FUSELAGE BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, SEAT TRACK HAS BROKEN LUGS AT BS 720C LBL 48. REMOVED AND REPLACED SEAT TRACK FROM BS 620 TO BS 740 LBL 48 A S PER B-727 SRM 51-30-2 AND 53-10-5 FIGURE 7. 2 L 7 3 4F A3WE 2001112000099 20011120 00099 2001 11 20 AWXA200100536 4 20011023 A 3417 46502003030312 COMPUTER AIRBUS A319 A319132 3930340 NM E/E BAY UNRELIABLE A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 812AW 2460 1178 PHX - ABORTED TAKEOFF - FLT 231 -C- ON TAKEOFF ROLL AT 90 KTS FLIGHT CREW OBSERVED ECAM MESSAGE ALT LAW AND NO AIRSPEED INDICATION ON PFD NR 2 AND THE TAKEOFF WAS REJECTED. MAINTENANCE TROUBLESHOT AND REPLACED THE NR 2 ADIRU. AFTER ALIGNI NG THE ADIRU BITE CHECKS WERE GOOD. MAINTENANCE ALSO RAN THE NR 2 PITOT SYSTEM TO 150 KTS WITH TEST SET AND NR 2 AIRSPE ED INDICATIONS WERE NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. TEAR-DOWN REPORT INDICATES A THERMAL CALIBRATION PERFORM ED AND TESTED. NO OTHER DEFECTS NOTED ON THIS UNIT. 2 L 7 2 4F RT A28NM 2001102900039 20011029 00039 NM 2001 10 29 DHL2001712020 1 20011024 A 2612 BRACKET BOEING 727 72729 1384007 NM NR 3 ENGINE MISSING A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 712DH 19401 THE NR 3 DETECTOR CIRCUIT GROUND LIGHT CAME ON AT FLT LEVEL 330 AND WOULD NOT GO OUT. FOUND TWO BRACKETS MISSING. INST ALLED BRACKETS AND RESECURED FIRE LOOP, OPS CHECKS SERVICEABLE PER B727 M/M REF 26-11-01. 2 L 7 3 4F A3WE 2001102900040 20011029 00040 NM 2001 10 29 DHL2001747007 1 20011023 A 2750 FLAP BOEING 727 727224 1384076 NM LT WING OUT OF ADJ A DHLA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SO 01 747DH 22253 AIRCRAFT ROLLS TO RIGHT DURING CLIMB, CRUISE AND DESCENT NEAR 300 KNOTS. DOES NOT ROLL WITH FLAPS EXTENDED. MOVING SPE ED BRAKE HANDLE OUT OF DETENT CORRECTS PROBLEM. AIRCRAFT FLIES LEVEL WITH NO TRIM, FLAPS 5 DEG. ADJUSTED LT OUTBOARD. FLAP ECCENTRICS, OPS CHECK GOOD IAW 727 M/M 27-51-2. 2 L 7 3 4F A3WE 2001102900041 20011029 00041 WP 2001 10 29 DHL2001801530 1 20011010 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 LT EXHAUST GATE SHOWS 2 DENTS 1 AND 2 IN ON UPPER SKIN. REMOVED DAMAGED SKIN FROM EXHAUST GATE PER SRM 57-2-0 PG 1-2. FABRICATED NEW SKIN PER SRM 57-71 PG 4. INSTALLED NEW SKIN PER SRM 57-2-0 PG 1-2. 2 L 7 4 4F RT 4A25 2001102900042 20011029 00042 WP 2001 10 29 DHL2001801531 1 20011010 A 5753 SKIN DOUG DC8 DC873F 302199F WP T/E FLAP DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 RIGHT I/B FLAP L/E UPPER SKIN SURFACE DENTED STA XW 115. REMOVED DAMAGED SKIN FROM RIGHT I/B FLAP PER SRM 57-2-0 PG 1. FABRICATED NEW SKIN PER SRM 57-7-1 PG 1. INSTALLED NEW SKIN PER SRM 57-2-0 PG 1-2. 2 L 7 4 4F RT 4A25 2001102900043 20011029 00043 WP 2001 10 29 DHL2001801532 1 20011010 A 5753 SKIN DOUG DC8 DC873F 302199F WP T/E FLAP DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 LEFT WING I/B FLAP UPPER SKIN DENTED 1 INCH AT XW 115.000. REMOVED DAMAGED SKIN FROM LEFT I/B FLAP PER SRM 57-2-0 PG 1- 2. FABRICATED NEW SKIN PER SRM 57-2-0 PG 1-2. INSTALLED NEW SKIN PER SRM 53-2-0 PG 1-2. 2 L 7 4 4F RT 4A25 2001102900044 20011029 00044 WP 2001 10 29 DHL2001801533 1 20011004 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 MAIN CARGO SEAT TRACK NR 2 LT TRACK LUG WORN AT STA 1600.000. CUT OUT DAMAGED AREA PER SRM 53-2-3 PG 49-50. FABRICATED SPLICES PER SRM 53-2-3 PG 49-50. INSTALLED NEW SPLICES AND TRACK PER SRM 53-2-3 PG 49-50. 2 L 7 4 4F RT 4A25 2001102900045 20011029 00045 WP 2001 10 29 DHL2001801534 1 20011010 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 MAIN CARGO SEAT NR 2 LT TRACK LUG WORN STA 320.000. CUT DAMAGED AREA PER SRM 53-2-3 PG 49-50. FABRICATED SPLICES PER S RM 53-2-3 PG 49-50. INSTALLED NEW SPLICES AND TRACK PER SRM 53-2-3 PG 49-50. 2 L 7 4 4F RT 4A25 2001102900046 20011029 00046 WP 2001 10 29 DHL2001801535 1 20011006 A 5310 SUPPORT DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 FWD CARGO COMPT B-2 DOOR SUPPORT FRAME CRACKED 1.5 INCH BETWEEN STA 520.000 TO 560.000. REMOVED DAMAGED AREA PER SRM 53 -2-0 FIG 1B. FABRICATED REINFORCING ANGLE PER SRM 53-2-0 FIG 1B. INSTALLED REINFORCING ANGLE PER SRM 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 2001102900047 20011029 00047 WP 2001 10 29 DHL2001801536 1 20011002 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 MAIN CARGO SEAT TRACK NR 2 LT HAS LUGS WORN FROM STA 160.000 - 165.000. CUT OUT DAMAGED AREA PER SRM 53-2-3 PG 49-50. FABRICATED SPLICES PER SRM 53-2-3 PG 49-50. INSTALLED SPLICES AND TRACK PER SRM 53-2-3 PG 49-50. 2 L 7 4 4F RT 4A25 2001102900048 20011029 00048 WP 2001 10 29 DHL2001801538 1 20011005 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 MAIN CARGO SEAT TRACK NR 2 LUG WORN STA 960.000. CUT DAMAGED AREA PER SRM 53-2-3 PG 49-50. FABRICATED SPLICES PER SRM 53-2-3 PG 49-50. INSTALLED TRACK AND SPLICES PER SRM 53-2-3 PG 49-50. 2 L 7 4 4F RT 4A25 2001102900049 20011029 00049 WP 2001 10 29 DHL2001801539 1 20011002 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 RT WING L/E INTERIOR RIB CRACKED .5 INCH AT XFS 385 UPPER PART. STOP DRILLED CRACK PER SRM 57-2-0 PG 1-2. FABRICATED R EINFORCING ANGLE PER SRM 57-2-0 PG 1-2. INSTALLED REINFORCING ANGLE PER SRM 57-2-0 PG 1-2. 2 L 7 4 4F RT 4A25 2001102900050 20011029 00050 WP 2001 10 29 DHL2001801540 1 20011005 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 BELLY DOOR-SUPPORT TRACK INTERCOSTAL CRACKED 2 INCHES. STOP DRILLED CRACK PER SRM 53-2-0 FIG 18. FABRICATED DOUBLER PE R SRM 53-2-0 FIG 18. INSTALLED DOUBLER PER SRM 53-2-0 FIG 18. 2 L 7 4 4F RT 4A25 2001102900051 20011029 00051 WP 2001 10 29 DHL2001801541 1 20011002 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 FWD CARGO COMPT-FLOOR SUPPORT ANGLE CRACKED .75 INCH AT STA 380.000 AND L-31L. STOP DRILLED CRACK PER SRM 53-2-0 FIG 1B . FABRICATED SUPPORT ANGLE WITH STEEL PER SRM 53-2-0 FIG 1B. INSTALLED SUPPORT ANGLE PER SRM 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 2001102900052 20011029 00052 WP 2001 10 29 DHL2001801542 1 20010929 A 5320 RIVET DOUG DC8 DC873F 302199F WP FUSELAGE MISSING A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 FWD CARGO COMPT-CEILING RT SIDE BETWEEN STA 420.000 TO 440.000 SHOWS RIVETS MISSING AT SUBFLOOR. INSTALLED RIVETS PER S RM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2001102900053 20011029 00053 WP 2001 10 29 DHL2001801543 1 20011001 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 FWD CARGO COMPT-FLOOR SUPPORT ANGLE CRACKED .5 INCH AT STA 560.000, L-35R TO L36R. STOP DRILLED CRACK AND FABRICATED RE INFORCING ANGLE PER SRM 53-2-0 PG 1-2. INSTALLED ANGLE PER SRM 53-2-0 PG 1-2. 2 L 7 4 4F RT 4A25 2001102900054 20011029 00054 WP 2001 10 29 DHL2001801544 1 20011003 A 5320 ATTACH ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AFT CARGO COMPT FLOOR LINING ATTACH ANGLE CRACKED 1 INCH BETWEEN STA 1340.000 AND L-31R. STOP DRILLED CRACK PER SRM 53- 2-0 PG 2E. FABRICATED REINFORCING ANGLE PER SRM 53-2-0 PG 2E-2F. INSTALLED ANGLE PER SRM 53-20 PG 2E-2F. 2 L 7 4 4F RT 4A25 2001102900055 20011029 00055 WP 2001 10 29 DHL2001801545 1 20011003 A 5320 ATTACH ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AFT CARGO COMPT FLOOR LINING ATTACH ANGLE CRACKED 1 INCH BETWEEN STA 1480.000 AND L35L. STOP DRILLED CRACK PER SRM 53-2 -0 PG 2E-2F. FABRICATED REINFORCING ANGLE PER SRM 53-2-0 PG 2E-2F. INSTALLED ANGLE PER SRM 53-2-0 PG 2E-2F. 2 L 7 4 4F RT 4A25 2001102900056 20011029 00056 WP 2001 10 29 DHL2001802015 1 20011023 A 7931 WARNING SYSTEM DOUG DC8 DC873 302199C WP COCKPIT ACTIVATED A DHLA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 802DH 46076 LOST OIL PRESSURE ON NR 4 ENG, PARAMETERS DROPPING. AFTER SHUT DOWN ENG WINDMILLING, W N1 30 - 27 PERCENT, N2 18 PERCEN T OIL PRESS APPROX 2 PSI 50 MIN WINDMILLING. PERFORMED TROUBLESHOOTING PROCEDURES PER CFM 71-00-00 FAULT 51. INSPECTE D ENGINE INLET AND EXHAUST, INSPECTED FUEL FILTER, SPECIFIC GRAVITY, ALL OIL CHIP DETECTORS. NO DEFECTS NOTED. 2 L 7 4 4F RT 4A25 2001102900057 20011029 00057 WP 2001 10 29 DHL2001803014 1 20011019 A 2612 FIRE WARNING DOUG DC8 DC873 302199C WP COCKPIT FALSE ACTIVATION A DHLA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 803DH 46123 AFTER LANDING NR 4 ENG SHORT CIRCUIT LIGHT ILLUMINATED AND FIRE BELL NR 4 FIRE LIGHT HANDLE CAME ON BRIEFLY. NR 4 ENG W AS ALREADY SHUT DOWN. PERFORMED RESISTANCE CHECK ON A & B SYSTEM AND INSPECTED ALL LOOPS. NO DEFECT NOTED AT THIS TIME IAW DAW 26-10-00. 2 L 7 4 4F RT 4A25 2001102900059 20011029 00059 NM 2001 10 29 HNAA0100068 1 20011022 A 5320 CROSSBEAM DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 907HA 011 A .075 INCH CRACK IN NOSE GEAR BAY CROSS BEAM AT STATION X97. CRACK BRANCHES OUT OF LOWER LT RIVET UNDER DRAG STRUT ACT UATOR MOUNTING BRACKET INTO J-CHANNEL RADIUS. REPAIRED IAW EO8-53-01-504. 2 H 7 2 4T RT A13NM 2001102900060 20011029 00060 EU 2001 10 29 C2XA01BT173 1 20011029 A 3350 7012210 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 99838 259 DURING 3 A INSPECTION MAINTENANCE FOUND EMERGENCY LIGHT ON PASSENGER STAIRS INOPERATIVE. REMOVED AND REPLACED BULB AS R EQUIRED IAW ATR42 MM 33-50-00. OPS.CHECKED GOOD. 2 H 7 2 4T RT A53EU 2001102900061 20011029 00061 NM 2001 10 29 HNAA0100069 1 20011023 A 5320 CROSSBEAM DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 936HA 145 CRACK IN NOSE GEAR BAY CROSSBEAM AT STATION X97. CRACK IS AT BOTTOM OF J-CHANNEL AT DRAG STRUT ACTUATOR BRACKET. REPAI RED IAW EO8-53-01-508. 2 H 7 2 4T RT A13NM 2001102900062 20011029 00062 NM 2001 10 29 HNAA0100070 1 20011023 A 5720 ANGLE DHAV DHC8 DHC8102 2809003 NM LT WING CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 914HA 53 CRACK IN CLOSING ANGLE BETWEEN OUTBOARD SIDE OF NR 1 NACELLE AND WING FRONT SPAR. REPAIRED IAW EO8-57-01-509. 2 H 7 2 4T RT A13NM 2001102900064 20011029 00064 EU 2001 10 29 C2XA01BT174 1 20011029 A 3350 7012210 LIGHT AEROSP ATR42 ATR42320 8680930 EU EXTERIOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 99838 259 DURING 3A INSPECTION MAINTENANCE FOUND EXTERIOR EMERGENCY LIGHT 16WL INOPERATIVE. REMOVED AND REPLACED BULB AS REQUIRED, OPS.CHECKED GOOD IAW ATR42 MM 33-50-00. 2 H 7 2 4T RT A53EU 2001103100014 20011031 00014 NE 2001 10 31 P2EA2001M0009 2 20011019 A 7200 JT8D17A ENGINE BOEING 737 73725A 1384481 NM PWA JT8 JT8D217A 52053 NE NR 1 DAMAGED A P2EA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 CE 05 239NJ 23789 709416 DURING TAKEOFF LOUD BANG WAS HEARD. ABORTED TAKEOFF AND RETURNED TO GATE WITHOUT INCIDENT. DAMAGE REPORTED TO EXHAUST AREA OF NR 1 ENGINE. REMOVED AND REPLACED NR 1 ENGINE IAW TASK CARD J271-00-01. 2 L 7 2 4F 4 F RT A16WE E9NE 2001102900065 20011029 00065 NM 2001 10 29 PCAA0110122 1 20011022 A 2120 SMOKE DHAV DHC8 DHC8102 2809003 NM CABIN DETECTED A PCAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 13 826EX 389 PHL- FLIGHT 3885, FLIGHT ATTENDANT DETECTED SMOKE IN CABIN ON CLIMBOUT. NO SMOKE OR HAZE NOTED BY CAPTAIN, ONLY ACRID S MELL. MAINTENANCE INSPECTED LIGHTING AND ELECTRICAL EQUIPMENT. AIRCRAFT RUN UP WITH CREW, NOTHING NOTED FROM BLEED SYS TEM OR CABIN ELECTRICAL SYSTEM. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001102900066 20011029 00066 NM 2001 10 29 PCAA0110123 1 20011018 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 804EX 227 DURING ROUTINE MAINTENANCE VISIT ONE FLOOR LEVEL EGRESS LIGHT AT ROW 8 FOUND OUT OF PLACE AND DOES NOT ILLUMINATE. BROK EN WIRE REPAIRED TO EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001102900067 20011029 00067 NM 2001 10 29 PCAA0110124 1 20011017 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN MALFUNCTIONED A PCAA K NONE O OTHER NR NOT REPORTED 1 EA 13 814EX 318 SYR- FLIGHT 3992, FLIGHT ATTENDANT REPORTED EMERGENCY LIGHTS CYCLED ON INTERMITTENTLY DURING FLIGHT. MAINTENANCE CHECKE D EMERGENCY LIGHT BATTERIES, FLIGHT ATTENDANTS SWITCH. COULD NOT DUPLICATE PROBLEM. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001102900068 20011029 00068 NM 2001 10 29 QXEA0101472 1 20010908 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - BAGGAGE DOOR SKIN HAS DAMAGE ON UPPER LEFT CORNER. REMOVED DAMAGED SECTION AT SKIN, FABRICATED SKIN FILLER REPAIR STRIP AND INSTALLED IAW RD 8-52-029. 2 H 7 2 4T RT A13NM 2001102900069 20011029 00069 NM 2001 10 29 QXEA0101692 1 20011018 A 5753 SKIN DHAV DHC8 DHC8* NM T/E FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - LEFT WING FLAP TRAILING EDGE LOWER SKIN HAS DAMAGE AT STATION YW207.00. REPAIRED DAMAGE IAW EA 6-57-07. 2 H 7 2 4T RT A13NM 2001102900070 20011029 00070 NM 2001 10 29 QXEA0101693 1 20011019 A 5414 SKIN DHAV DHC8 DHC8202 2809007 NM RT NACELLE BUCKLED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - RIGHT NACELLE IS BENT AND BUCKLED JUST AFT OF THE LOWER COWL. REPAIRED IAW RD 8-54-063. 2 H 7 2 4T RT A13NM 2001102900071 20011029 00071 EU 2001 10 29 QXEA0101694 1 20011020 A 3350 5515900004 PRINTED CKT BOAR FOKKER F28 F28MK4000 4990810 EU CABIN DEFECTIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481US 11230 PDX - FORWARD EMERGENCY EXIT SIGN ABOVE COCKPIT DOOR HAS BURNED OUT BULBS. REMOVED AND REPLACED FORWARD EMERGENCY EXIT SIGN LAMP CARD. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001102900072 20011029 00072 EU 2001 10 29 QXEA0101695 1 20011021 A 3350 5515900004 PRINTED CKT BOAR FOKKER F28 F28MK4000 4990810 EU CABIN DEFECTIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 494US 11167 GEG - BOTH FORWARD EXIT SIGNS HAVE INOPERABLE BULBS. REMOVED AND REPLACED EXIT SIGN CIRCUIT BOARD. OPERATIONAL CHECK I S GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001102900073 20011029 00073 NM 2001 10 29 QXEA0101696 1 20011019 A 5230 HANDLE DHAV DHC8 DHC8* NM CARGO DOOR OPEN A QXEA K NONE J WARNING INDICATION UK UNKNOWN 1 NM 09 404QX 4046 SEA - HIT LIGHT TO MODERATE TURBULENCE AT 10,000 FEET. GOT MESSAGE WARNING AND FUSELAGE DOOR WARNING. HEARD LOUD HISS AT REAR OF AIRCRAFT, AIRCRAFT DEPRESSURIZED. FOUND OUTSIDE DOOR HANDLE POPPED OPEN. LOCKING MECHANISM NOT PROPERLY LAT CHED. NO DISCREPANCIES FOUND. LATCH OPERATING PROPERLY. 2 H 7 2 4T RT A13NM 2001102900074 20011029 00074 EU 2001 10 29 QXEA0101697 1 20011023 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478US 11227 GEG-EXIT SIGN FORWARD CABIN INOPERATIVE. REMOVED AND REPLACED SIGN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERV ICE. 2 L 7 2 4F RT A20EU 2001102900077 20011029 00077 NE 2001 10 29 SWIA200110245 2 20011011 A 7321 FCU EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT ENGINE OUT OF ADJ A SWIA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 NM 07 301YV 120301 RIGHT TORQUE FLUCTUATED 5 - 8 PERCENT AFTER TAKEOFF. RETURNED TO FAT. PERFORMED ENGINE RUNS IAW EMB 120 MM 71-00-00. OPS CHECKS GOOD. NO DEFECTS NOTED AT THIS TIME. UPDATE 10/12/2001: PREVIOUS OPS CHECK DONE WITH EECS OFF. RAN AND AD JUSTED TRIM ON RIGHT ENGINE. RAN RIGHT ENGINE AT DIFFERENT PARAMETERS WITH EEC ON. COULD NOT DUPLICATE. OPS CHECK GOO D AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 2001102900078 20011029 00078 2001 10 29 SWIA200110246 4 20011011 A 3425 COMPUTER EMB 120 EMB120RT SO COCKPIT MALFUNCTIONED A SWIA L A ABORTED APPROACH UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 NM 07 196SW 120156 FLYING ILS INTO JAC WHEN APP MODE SELECTED ON FCP, THE COMMAND BARS STARTED MOVING UP AND DOWN RAPIDLY, GYRO AND COMPUTE R FLAGS APPEARED AND ATTITUDE DISPLAY APPEARED ON MAP. RESET ATT MON PER QRH, WHICH CANCELLED FLAGS, BUT PRESSING APPR MODE IT ALL HAPPENED AGAIN. RETURNED TO SLC AND RESET. ATTITUDE MONITOR OK. PERFORMED OPS CHECK OF FLIGHT DIRECTOR, A HRS AND AUTOPILOT. NO FAULTS FOUND. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001102900079 20011029 00079 SO 2001 10 29 SWIA200110247 1 20010906 A 5310 SHEAR TIE EMB 120 EMB120RT SO COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 137H 120137 FORMER CRACKED JUST AFT OF PILOT'S DIRECT VISION WINDOW AFT CENTER. REMOVED AND REPLACED CRACKED BRACKET WITH NEW SERVI CEABLE BRACKET OF SAME P/N FOR THIS LOCATION. ALL WORK PERFORMED IN ACCORDANCE WITH THE SRM 51-70-00. ALL CHECKS GOOD. P/N: 120-12545-001. 2 L 7 2 4T RT A31SO 2001102900080 20011029 00080 SO 2001 10 29 SWIA200110248 1 20010906 A 5342 ANGLE EMB 120 EMB120RT SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 137H 120137 CRACK AND PULLED RIVET IN VERTICAL STABILIZER TO EMPENNAGE SUPPORT ANGLE LEFT SIDE. REPLACED LEFT L-FORWARD PROFILE PER PART II OF SB 120-053-0074 AND EMBRAER AUTHORIZATION GST-3216/01. P/N: SB120-53-0074 KIT 1. 2 L 7 2 4T RT A31SO 2001102900081 20011029 00081 SO 2001 10 29 SWIA200110249 1 20011011 A 5270 CONTACTOR EMB 120 EMB120ER 3260203 SO CARGO DOOR DIRTY A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 224SW 120294 DOORS AURAL WARNING AND CARGO DOOR LIGHT ILLUMINATED DURING FLIGHT. CLEANED CONTACTORS. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2001102900082 20011029 00082 EA 2001 10 29 SWIA200110250 1 20011009 A 2760 CONTROL UNIT CNDAIR CL600 CL6002B19 EA SPOILER FAILED A SWIA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 433SW 7550 ON TAXI OUT FLT SPLRS AND SPOILERON CAUTION LIGHT ON. INSTALLED SERVICEABLE SECU AT LEFT POSITION. PERFORMED OPS CHECK OF SPOILER SYSTEM. OPS CHECK GOOD. S/N OFF: 1329. 2 L 7 2 4F RT A21EA 2001102900083 20011029 00083 SO 2001 10 29 SWIA200110251 1 20011014 A 2752 3431001001 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 560SW 120334 LOST BLUE HYDRAULIC SYSTEM ON FINAL APPROACH INTO SAN. REPLACED LT NACELLE FLAP ACTUATOR IAW EMB120 MM CHAPTER 27-50-00 . OPS AND LEAK CHECK GOOD. 2 L 7 2 4T RT A31SO 2001102900084 20011029 00084 SO 2001 10 29 SWIA200110252 1 20011012 A 2751 3471001001 CONTROL PANEL EMB 120 EMB120ER 3260203 SO COCKPIT FAULTY A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 213SW 120277 NACELLE FLAPS GO TO 2 DOTS AND STICK. FIRST CONTROL FAULT, THEN DISAGREEMENT. REMOVED AND REPLACED FLAP ANNUNCIATOR CO NTROL PANEL IAW MM 75-50-05. OPS CHECK GOOD IAW 27-50-00. 2 L 7 2 4T RT A31SO 2001102900085 20011029 00085 SO 2001 10 29 SWIA200110253 1 20011015 A 3232 BOLT EMB 120 EMB120RT SO LT MLG BROKEN A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 200CD 120200 UPON GEAR RETRACTION LEFT MAIN GEAR DOOR STAYED OPEN. RECYCLED GEAR AND IT STILL REMAINED OPEN. FOUND A BROKEN BOLT ON THE LEFT INBOARD FORWARD DOOR ACTUATOR ARM. INSTALLED A NEW BOLT. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001102900086 20011029 00086 WP 2001 10 29 DHL2001801546 1 20011017 A 5755 4645822 BRACKET DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 NOSE SECTION WING SPOILER CONTROL SHOWS BROKEN BRACKET (HIDDEN DAMAGE).REPLACED AND SECURED BRACKET PER SRM 51-3-0 PG 1 AND SRM 51-3-1 PG 2D.REF N/R 0533 FOR OPS CHK. 2 L 7 4 4F RT 4A25 2001102900087 20011029 00087 WP 2001 10 29 DHL2001801549 1 20011014 A 5280 56453021 HINGE DOUG DC8 DC873F 302199F WP BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 L/H MAIN LANDING GEAR INBD DOOR CNTR HINGE BROKEN.REMOVED AND REPLACED L/H MLG I/B DOOR CTR HINGE PER SRM 51-1-21 PG 1 A ND SRM 51-1-20D PG 21-29 2 L 7 4 4F RT 4A25 2001102900088 20011029 00088 WP 2001 10 29 DHL2001801551 1 20011018 A 2550 37502557503 FITTING DOUG DC8 DC873F 302199F WP A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AFT CARGO COMPT SPLICE FITTING 5 IN CRACKED BETWEEN STA 1040.000 AND 1060.000,L31L.REMOVED CRACKED SPLICE FITTING PER SR M 51-1-20 D PG 21.CLEANED TREATED AND PRIMED PER SRM 51-1-8B.INSTALLED NEW FITTING PERSRM 51-1-20 PG 9. 2 L 7 4 4F RT 4A25 2001102900089 20011029 00089 WP 2001 10 29 DHL2001801552 1 20011016 A 5412 47723971 FITTING DOUG DC8 DC873F 302199F WP A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AFT BULKHEAD JOINT FITTING CRACKED 1/2 IN AT STA 7266.000 AT L176.REMOVED CRACKED FITTING PER SRM 51-1-20D.CLEANED TREAT ED AND PRIMED PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2001102900090 20011029 00090 WP 2001 10 29 DHL2001801553 1 20011018 A 2550 3754473501B FITTING DOUG DC8 DC873F 302199F WP A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AFT CARGO COMPT SPLICE FITTING CRACKED 4 IN BETWEEN STA 1300.000 AND STA 1320.000 L-31L.REMOVED CRACKED FITTING PER SRM 51-1-20D.CLEANED TREATED AND PRIMED PER SRM 51-1-8B.INSTALLED NEW FITTING PRE SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2001102900091 20011029 00091 WP 2001 10 29 DHL2001801554 1 20011010 A 5230 3754051501 FITTING DOUG DC8 DC873F 302199F WP A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 C- BELLY DOOR LWR T BOLT # 6 SHOWS CRACKED FITTING.REMOVED CRACKED FITTING PER SRM 51-1-20D PG 4.CLEANED TREATED AND PR IMED PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2001102900092 20011029 00092 WP 2001 10 29 DHL2001801556 1 20011014 A 5714 4646547 FITTING DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 CTR WING (MAIN CARGO COMPT) FITTING CRACKED 1 IN AT STA 381.000 XCW 23L/H.REMOVED CRACKED FITTING PER SRM 51-1-20D.CLEAN ED TREATED AND PRIMED AERA PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-120D PG 9. 2 L 7 4 4F RT 4A25 2001102900093 20011029 00093 WP 2001 10 29 DHL2001801557 1 20011011 A 5714 4646547 FITTING DOUG DC8 DC873F 302199F WP A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 CENTER WING FITTING CRACKED AT STA 717.XCW 23 L/H.REMOVED CRACKED FITTING PER SRM 51-1-20D.CLEANED TREATED AND PRIMED AR EA PER SRM 51-1-8B.INSTALLED NEW FITTING PERSRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2001102900094 20011029 00094 WP 2001 10 29 DHL2001801558 1 20011013 A 2530 3754041501 FITTING DOUG DC8 DC873F 302199F WP A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 FWD CARGO COMPT FITTING CRACKED AT L/H UPPER SECTION STA 300.000 L-27L.REMOVED CRACKED FITTING PER SRM 51-1-20D.CLEANED TERATED AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2001102900095 20011029 00095 WP 2001 10 29 DHL2001801559 1 20011011 A 5714 4646547 FITTING DOUG DC8 DC873F 302199F WP A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 CENTER WING (MAIN CARGO COMPT)FITTING CRACKED 1 IN AT STA 759.000, XCW 23L/H.REMOVED CRACKED FITTING PER SRM 51-1-20D.CL EANED TREATED AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2001110700120 20011107 00120 NM 2001 11 7 01FDEA00928 1 20011026 A 5330 SKIN BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 279FE 22346 EMPENNAGE SKIN DENT AT BS 1338, 38' BELOW VERT STAB LT SIDE. REMOVED AND REPLACED SKIN PER SRM 51-40-2. 2 L 7 3 4F RT A3WE 2001111400019 20011114 00019 NM 2001 11 14 01FDEA00932 1 20011026 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 279FE 22346 CORROSION ON FLOORBEAM BS 1070, LBL 45, WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8 FIG 3. 2 L 7 3 4F RT A3WE 2001102900096 20011029 00096 EA 2001 10 29 SWIA200110254 1 20011015 A 2497 GROUND WIRE CNDAIR CL600 CL6002B19 EA APU GENERATOR LOOSE A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 407SW 7034 APU FAULT LIGHT COMES ON WITH APU BATT OFF LIGHT INTERMITTENT, VARIABLE VOLTS ON THE APU BATTERY DISPLAY AND THE APU CHA RGER INDICATION CYCLING ON AND OFF ERRATICALLY. FOUND APU GENERATOR GROUND WIRE LOOSE AT ATTACH POINT. APU CHARGER AND APU OPS CHECK GOOD AFTER REPAIR AND RE-ATTACHMENT OF APU GENERATOR GROUND WIRE. 2 L 7 2 4F RT A21EA 2001102900097 20011029 00097 SO 2001 10 29 SWIA200110255 1 20011016 A 2752 CONNECTOR EMB 120 EMB120ER 3260203 SO T/E FLAP DIRTY A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 223SW 120291 WHEN FLAPS 45 SELECTED DISAGREEMENT ON OUTBOARD FLAPS, 2 BARS DIFFERENCE. CLEANED OUTBOARD FLAP ACTUATOR CANNON PLUGS. CLEANED FLAP TRACKS AND ROLLERS. CYCLED FLAPS 2 DOZEN TIMES. CLEARED COMPUTER FAULTS. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001102900098 20011029 00098 EA 2001 10 29 SWIA200110256 1 20011016 A 2750 FLAP CNDAIR CL600 CL6002B19 EA WING MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 903SW 7425 AFTER LANDING, DURING RETRACTION OF FLAPS, RECEIVED FLAPS FAIL CAUTION MESSAGE WHEN FLAP HANDLE WAS MOVED FROM 20 DEGREE S TO 8 DEGREES. FLAPS WOULD NOT GO OUT OF 20 DEGREES. VISUAL INSPECTION CONFIRMS FLAPS AT 20 DEGREES. COMPLIED WITH A D 98-20-01. ALL CHECK GOOD. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2001102900099 20011029 00099 SO 2001 10 29 SWIA200110257 1 20011019 A 2752 3430001001 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 250YV 120250 UPON INITIAL POWER-UP, INBOARD FLAPS SHOWED 1 LIGHT BAR W/DISAGREEMENT ALARM. AFTER FOLLOWING MX PROCEDURES, INBOARD FL APS SHOW ONLY 2 BARS W/45 DEGREES FLAPS SELECTED AND DISAGREEMENT. RESET OF FLAPS THEN GO TO 45 DEGREES, INBOARD FLAPS DON'T EXTEND AT ALL. REPLACED LEFT INBOARD FLAP ACTUATOR IAW MM 27-50-07. OPS CHECK GOOD AT THIS TIME. REPAIR DONE IN YYJ BY SEA MAINTENANCE. 2 L 7 2 4T RT A31SO 2001102900100 20011029 00100 SO 2001 10 29 SWIA200110258 1 20011022 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO EXTERIOR INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 235SW 120310 LEFT FORWARD EXTERIOR EMERGENCY LIGHT INOP. REPLACED LIGHT BULB IN LEFT FORWARD EXTERIOR EMERGENCY LIGHT. OPS CHECK GO OD. 2 L 7 2 4T RT A31SO 2001102900101 20011029 00101 SO 2001 10 29 SWIA200110259 1 20011022 A 3241 RELAY EMB 120 EMB120ER 3260203 SO ANTI-SKID SYS FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 NM 07 235SW 120310 OUTBOARD ANTI-SKID LIGHT CAME ON WHEN GEAR SELECTED DOWN. RETURNED TO LAX. REPLACED ANTI-SKID RELAY K0021. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001102900102 20011029 00102 NM 2001 10 29 UPS01437122 1 20010908 A 5343 FITTING BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C FX - LT UPPER S38L DRAG SPLICE FITTING 3 BOLT HOLES AREA FOUND CORROSION AT UNDER WING DRAG FTG COMMON HOLE AREA. LT S38L UPP DRAG SPLICE FITTING 3 HOLE BORE CORROSION CLEANED UP AND INSTALLED WITH 3 SLEEVE BOLTS AS PER H XRS NR R53-43-34686 SPLICE FITTING REPAIR REQUIREMENT. 2 L 7 4 4F A20WE 2001111400144 20011114 00144 NM 2001 11 14 UPS01237190 1 20011026 A 5755 SUPPORT BOEING 727 72730C 1384009 NM SPOILER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 917UP 19310 INSPECTION TYPE:IN RT WING INBOARD GROUND SPOILER ACTUATOR FITTING ASSY LT AND RT PANEL SUPPORT BRACKETS CRACKED. REMOV ED AND REPLACED INBOARD AND OUTBOARD GROUND SPOILER PANEL SUPPORT BRACKETS REF IPC 57-40-00 FIG 4A ITEM 186 & 188. 2 L 7 3 4F A3WE 2001102900103 20011029 00103 NM 2001 10 29 UPS01437123 1 20010908 A 5343 FITTING BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C FX EXTERIOR LT S38L DRAG FITTING MOUNT BOLT HOLES FOUND CORROSION AT BS 980 - 990 AREA. LT S38L DRAG FTG 3 CORROSION BOLT HOLES AT BS 980 - 990 AREA CLEANED UP AND INSTALLED WITH 3 SLEEVE BOLTS. ALSO 1 SKIN AREA ATTACHME NT BOLT ADJACENT FWD SLEEVE BOLT AREA WAS REPLACED BY ANOTHER SLEEVE BOLT TO PREVENT INTERFERENCE PROBLEM AS PER HX RS N R R 53-43-34686 SPLICE FITTING REPAIR REQUIREMENT. 2 L 7 4 4F A20WE 2001102900104 20011029 00104 NM 2001 10 29 UPS01437126 1 20010908 A 5343 FITTING BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C FX EXTERIOR RT S38R DRAG FITTING MOUNT BOLT HOLES FOUND CORROSION AT BS 980 - 990 AREA. RT S38R DRAG FTG 3 CORROSION BOLT HOLES AT BS 980 - 990 AREA CLEANED UP AND INSTALLED WITH 3 SLEEVE BOLTS AS PER HX RS NR R-53-43-346 86 SPLICE FITTING REPAIR REQUIREMENT. 2 L 7 4 4F A20WE 2001102900106 20011029 00106 WP 2001 10 29 UPS01837088 1 20010926 A 5720 FITTING DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:SV RIGHT WING NR 3 ALT TANK STRINGER 51 END FITTING ON O/B SIDE IS CRACKED. PERFORMED HFEC INSPECTION T O VERIFY CRACK IAW DAC NDT SPM 06-10-01-0 01. REMOVED CRACKED FITTING. LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51 -1-24 AND DAC DWG 5613423. INSTALLED IAW DC8 SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 2001102900107 20011029 00107 WP 2001 10 29 UPS01837089 1 20010926 A 5720 FITTING DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:SV RIGHT WING NR 3 MAIN TANK STRINGER 51 END FITTING ON I/B SIDE IS CRACKED. REMOVED STRINGER 51 END FI TTING ON I/B SIDE IAW DC8 SRM 51-3-2. LOCATED DRILLED AND INSTALLED NEW END FITTING IAW DAC DWG 5613423. 2 L 7 4 4F RT 4A25 2001102900108 20011029 00108 WP 2001 10 29 UPS01837090 1 20011018 A 5610 SLIDING WINDOW DOUG DC8 DC871F 302199D WP COCKPIT OUT OF ADJ A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:PFLT CAPTAIN SLIDING WINDOW WILL NOT OPEN. ADJUSTED PER MM 56-10-00. OPS CHECKS GOOD. 2 L 7 4 4F RT 4A25 2001102900109 20011029 00109 WP 2001 10 29 UPS01837091 1 20010821 A 2510 LINER DOUG DC8 DC873F 302199F WP COCKPIT UNSECURE A IPXA K NONE O OTHER NR NOT REPORTED 1 SO 01 804UP 46004 INSPECTION TYPE:N/A TRIM AROUND FIRST OFFICER SWING WINDOW HANDLE IMPEDES OPERATION IF OPENING DURING AN EMERGENCY IS RE QUIRED. SECURED TRIM AT FWD PART OF F/O'S SLIDING WINDOW, CLEARANCE NOW ALLOWS HAND TO RELEASE HANDLE IN CASE OF AN EME RGENCY EXIT REQUIRED, OK FOR SERVICE. 2 L 7 4 4F RT 4A25 2001102900110 20011029 00110 WP 2001 10 29 UPS01837096 1 20011004 A 5320 37503301 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 STA 610 LONG 26R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750330 AND SRM 51 -1-20D, 53-1-0. 2 L 7 4 4F RT 4A25 2001102900111 20011029 00111 WP 2001 10 29 UPS01837097 1 20011003 A 5330 FINGER DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 STA 130 LONG 31L FINGER DOUBLER IS CRACKED. TRIMMED OFF CRACKED FINGER ON FINGER DOUBLER IAW ENGINE ERING RESPONSE AND SRM CHAPTER 51 GUIDELINES. 2 L 7 4 4F RT 4A25 2001102900112 20011029 00112 WP 2001 10 29 UPS01837098 1 20011003 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 847.5. REPAIRED RIBS IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001102900113 20011029 00113 WP 2001 10 29 UPS01837099 1 20011003 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 747.5, XFS 753.75, XFS 760. REPAIRED RIBS IAW SRM 57-2- 0 FIG 2. 2 L 7 4 4F RT 4A25 2001102900114 20011029 00114 WP 2001 10 29 UPS01837100 1 20011003 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 660. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001102900115 20011029 00115 CE 2001 10 29 00005 1 20011025 A 2910 HYDRAULIC LINE LEAR 24 24F 5170317 CE HYDRAULIC SYS LEAKING E HAEA K NONE K FLUID LOSS AP APPROACH 1 SW 05 444TW 348 LEAK AT THE RETURN LINE TO ENGINE DRIVEN HYDRAULIC PUMP IN HELL HOLE OF AIRCRAFT. 2 L 7 2 4J A10CE 2001102900116 20011029 00116 WP 2001 10 29 0103649870 1 20011014 A 5280 DOOR DOUG DC9 DC951 3022051 WP RT MLG CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 779NC 48101 DURING WALK-AROUND AT MSP, THE RT MAIN LANDING GEAR DOOR WAS FOUND TO HAVE A 1.25 INCH CRACK COMMON TO THE FORWARD .050 INCH THICK DOOR PAN 9 INCHES INBOARD OF THE LATCH FITTING. REPAIRED PER EA 98-186641. 2 L 7 2 4F RT A6WE 2001102900117 20011029 00117 WP 2001 10 29 0103699920 1 20011022 A 2742 95901 MOTOR DOUG DC9 DC932 3022066 WP STABILIZER LEAKING A NWAA A UNSCHED LANDING K F FLUID LOSS FLT CONT AFFECTED CL CLIMB 1 GL 01 942N 47459 ON CLIMBOUT, THE PRIMARY TRIM CONTROL AND BOTH YOKE SWITCHES WERE INOPERATIVE. CREW RESET THE CIRCUIT BREAKERS AND CHEC KED THE CUTOUT WITH NO HELP. ALTERNATE TRIM VIA AUTOPILOT DID OPERATE NORMALLY. FLIGHT RETURNED TO MSP WITHOUT INCIDEN T. MAINTENANCE FOUND THE PRIMARY TRIM ACTUATOR MOTOR LEAKING OIL. REPLACED THE PRIMARY TRIM ACTUATOR MOTOR. OPERATION AL CHECK OK. 2 L 7 2 4F A6WE 2001102900118 20011029 00118 WP 2001 10 29 01FDEA00912 1 20011025 A 5754 SLAT TRACK DOUG DC10 DC1010 3022110 WP LT WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 LEFT WING UPPER L/E INBOARD SLAT TRACK NR 1. REMOVED AND REPLACED PER IAW EA 8-5410-56154 & SRM 57-20-00. 2 L 7 3 4F A22WE 2001102900119 20011029 00119 WP 2001 10 29 01FDEA00913 1 20011025 A 5210 DOOR DOUG DC10 DC1010 3022110 WP L1 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 BS 415 L1 DOOR CORROSION ON FWD LWR LEG. REMOVED AND REPLACED DOOR PER SRM 53-20-00. 2 L 7 3 4F A22WE 2001102900120 20011029 00120 WP 2001 10 29 01FDEA00915 1 20011025 A 5410 FAIRING DOUG DC10 DC1010 3022110 WP NR 2 PYLON DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 PYLON NR 2 AFT FAIRING EDGE LT SIDE IS DISBONDED AND MISSING RIVETS. REMOVED AND REPLACED TRAILING EDGE PER EA 8-5410-5 6153 & SRM 54-12-02. 2 L 7 3 4F A22WE 2001110700115 20011107 00115 NM 2001 11 7 01FDEA00916 1 20011025 A 5711 SPAR BOEING 727 727233 138408A NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 279FE 22346 RIGHT WING I/B MIDFLAP, AFT FLAP CONTROL ROD CUT OUT IN THE LWR SPAR CHORD CRACKED. REMOVED AND REPLACED CHORD PER SRM 5 1-40-4, 51-30-2. 2 L 7 3 4F RT A3WE 2001110700116 20011107 00116 NM 2001 11 7 01FDEA00917 1 20011025 A 5330 SKIN BOEING 727 727233 138408A NM FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 279FE 22346 BS 720, STR 19 LT FUSELAGE EXTERNAL SKIN CHAFED. REMOVED AND REPLACED SKIN PER SRM 53-30-3. 2 L 7 3 4F RT A3WE 2001110800018 20011108 00018 NM 2001 11 8 01FDEA00919 1 20011025 A 5530 65168123 FRAME BOEING 727 727233 138408A NM VERTICAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 279FE 22346 VERTICAL STABILIZER MAIN BOX INTERIOR CHORD IS CRACKED AT FIN BS 157.2, STR 8 LT. REMOVED AND REPLACED CHORD PER SRM 55- 30-5 FIG 1 & EA 7-5530-59891. 2 L 7 3 4F RT A3WE 2001111400014 20011114 00014 NM 2001 11 14 01FDEA00921 1 20011026 A 5510 65241899 BEAM BOEING 727 727233 138408A NM HORIZ STAB CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 279FE 22346 LEFT HORIZ STAB LOWER TRAILING EDGE BEAM HAS CHAFE DAMAGE AND MISSING SPACER BLOCK AT THE 3RD RUB PAD FROM O/B END. REM OVED AND REPLACED BEAM PER EA 7-5510-60563. 2 L 7 3 4F RT A3WE 2001110800020 20011108 00020 NM 2001 11 8 01FDEA00922 1 20011026 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 279FE 22346 CORROSION C53-224-01,1 ON TOP CHORD OF BS 720A FLOORBEAM RBL 7 OUT OF LIMITS. REMOVED AND REPLACED FLOORBEAM PER EA 7-53 10-60567. 2 L 7 3 4F RT A3WE 2001110700117 20011107 00117 NM 2001 11 7 01FDEA00923 1 20011026 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 279FE 22346 CORROSION ON UPPER CHORD OF FLOORBEAM BS 1050, RBL 35 AND RBL 55, WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8 & 51-30-2. 2 L 7 3 4F RT A3WE 2001110700118 20011107 00118 NM 2001 11 7 01FDEA00925 1 20011026 A 5314 KEELBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 279FE 22346 CORROSION ON KEEL BEAM AT BS 934, STR 29 RIGHT O/B. REMOVED AND REPLACED BEAM PER DWG SR 27-53-023. 2 L 7 3 4F RT A3WE 2001111400016 20011114 00016 NM 2001 11 14 01FDEA00927 1 20011026 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 279FE 22346 CORROSION (C53-224-01, 2) ON LWR CHORD OF FLOORBEAM, BS 1110, RBL 41, WL 200. REMOVED AND REPLACED CORROSION PER EA 7-53 10-59897. 2 L 7 3 4F RT A3WE 2001102900122 20011029 00122 2001 10 29 C2XA01BT172 4 20011019 A 2213 7021170951 CONTROLLER EMB 145 EMB145LR SO COCKPIT FAULTY A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 13978 145180 CREW REPORTED ON TAXI, SMOKE IN COCKPIT ELECTRICAL BURNING SMELL IN COCKPIT ONLY. CONTRACT MAINTENANCE FOUND FAULTY AP PUSHBUTTON SWITCH ON AUTOPILOT CONTROL PANEL. REMOVED AND REPLACED FLIGHT GUIDANCE CONTROLLER IAW EMB145 MM 22-11-01. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2001102900123 20011029 00123 SO 2001 10 29 C2XA01TY162 1 20011028 A 5210 PE64042H4016 BUSHING EMB 135 EMB135ER 3260203 SO PAX DOOR BACKED OUT A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16510 145251 TYS DURING A SCHEDULED INSPECTION THE PAX-DOOR HOLD OPEN PIN LOWER BUSHING WAS FOUND TO BE MIGRATING OUT. MAINTENANCE I NSTALLED BUSHING FROM THE BOTTOM IN REFERENCE TO GST-1662/01. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED ON COMPLET ION OF AIRCRAFT MAINTENANCE INSPECTION. 2 L 7 2 4F RT T00011AT 2001102900124 20011029 00124 SO 2001 10 29 C2XA01TY167 1 20011028 A 5320 14522460013 FLOOR SUPPORT EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16510 145251 TYS DURING A SCHEDULED INSPECTION, SEVERAL AREAS OF CORROSION WAS FOUND ON THE CENTER FLOORBEAM GUSSET BETWEEN FRAMES 1 8-22. MAINTENANCE REMOVED AND REPLACED GUSSET TOP CAP. IAW-EMB-135/145-SRM-51-40-02. REPAIR PROCEDURES WERE SATISFACTO RY, AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001102900125 20011029 00125 NM 2001 10 29 CALA0100972 1 20011025 A 5320 BAC1503100028 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59338 23576 CABIN LAVATORY WALL FLOOR SUPPORT ANGLE CORRODED AT STATION 995 LBL 13 - 42. REMOVED AND REPLACED L-ANGLE PER SRM 51-10 -02. 2 L 7 2 4F RT A16WE 2001102900126 20011029 00126 NM 2001 10 29 CALA0100973 1 20011025 A 5320 BAC1510335 CHANNEL BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59338 23576 CORROSION ON SUPPORT CHANNEL STATION 995 LBL 13 - 42. REMOVED AND REPLACED HAT SECTION PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001102900127 20011029 00127 WP 2001 10 29 ZW0A0110202 1 20011025 A 3350 58222 BATTERY PACK DOUG DC9 DC982 3022082 WP MID CABIN A ZW0A K NONE O OTHER NR NOT REPORTED 1 CE 13 956U 49701 THE EGRESS LIGHTING REMAINED ON AT ROWS 16 TO 21 WITH THE SWITCH IN ARM POSITION. REPLACED THE BATTERY PACK. CHECK-C 9 -8-01 STL. --CLOSED-- 2 L 7 2 4F A6WE 2001102900128 20011029 00128 NM 2001 10 29 CALA0100976 1 20011025 A 5320 65C161216 MOUNT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59338 23576 L1 DOOR FORWARD GIRT LATCH MOUNT CORRODED. REMOVED AND REPLACED LATCH MOUNT BRACKET PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001102900129 20011029 00129 NM 2001 10 29 CALA0100977 1 20011025 A 5320 65C161215 MOUNT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59338 23576 L1 DOOR AFT GIRT LATCH MOUNT CORRODED. REMOVED AND REPLACED GIRT MOUNT PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001102900131 20011029 00131 NM 2001 10 29 DHL2001712021 1 20011024 A 3040 MOTOR BOEING 727 72729 1384007 NM WINSHIELD WIPER FAILED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 712DH 19401 CAPTAIN'S WIPER DOES NOT WORK ON ANY SPEED. REPLACED CAPTS (LT) WIPER MOTOR ASSY, OPS CHECK NORMAL PER M/M 30-42-01. 2 L 7 3 4F A3WE 2001102900132 20011029 00132 WP 2001 10 29 UPS01837101 1 20011003 A 5730 5769635 DOUBLER DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 LEFT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 585. REMOVED, FABRICATED AND REPLACED DOUBLE R IAW DWG 5769600 AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001102900133 20011029 00133 WP 2001 10 29 UPS01837102 1 20011002 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 610. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001102900134 20011029 00134 WP 2001 10 29 UPS01837103 1 20011002 A 5730 576960036 DOUBLER DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 RIGHT WING L/E INTERNAL DOUBLER IS CRACKED NAT XFS 585. REMOVED, FABRICATED, AND REPLACED DOUBLER I AW DWG 5769600 AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001102900135 20011029 00135 WP 2001 10 29 UPS01837104 1 20011003 A 5730 576960040 DOUBLER DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 LEFT WING L/E INTERNAL WRAP AROUND DOUBLER IS CRACKED AT XFS 566.25. REMOVED, FABRICATED, AND REPLA CED DOUBLER IAW DWG 5769600, AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001102900136 20011029 00136 WP 2001 10 29 UPS01837105 1 20011002 A 5730 576960039 DOUBLER DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 RIGHT WING L/E INTERNAL DOUBLER IS CRACKED AT XFS 566.25. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769600, AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001102900137 20011029 00137 WP 2001 10 29 UPS01837106 1 20011002 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 FUSELAGE SKIN IS CRACKED AT CANTED STA 1723.076 LONG 15R. REPAIRED SKIN IAW SRM 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 2001102900138 20011029 00138 WP 2001 10 29 UPS01837107 1 20011004 A 5320 3754032U1 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 STA 280 LONG 21R FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754032, AND SRM 51 -1-20D. 2 L 7 4 4F RT 4A25 2001102900139 20011029 00139 NM 2001 10 29 AWXA200100538 1 20011021 A 5330 654577560 SKIN BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - C13 CK - "C" - CRACK FOUND IN CREASE IN FUSELAGE SKIN AT BS 912, BETWEEN STR 24R - 25R, .75" LONG. MAINTENANCE REM OVED DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED IAW B737 SRM 53-00-01, FIG 202, PG 204 - 206. 2 L 7 2 4F RT A16WE 2001102900140 20011029 00140 NM 2001 10 29 AWXA200100542 1 20010905 A 5311 143N1012 FRAME BOEING 757 7572S7 1384962 NM DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 PHX - C8 CK - "C" - DENT FOUND FWD CARGO COMPARTMENT FRAME FLANGE AT BS 660, STR 23L & 24L. MAINTENANCE CUT OUT DAMAGED AREAS, FABRICATED REPAIR ANGLE AND INSTALLED IAW B757 SRM51-70-11, FIG 1, PG 1. 2 L 7 2 4F RT A2NM 2001102900141 20011029 00141 NM 2001 10 29 AWXA200100543 1 20010905 A 5311 143N1013 FRAME BOEING 757 7572S7 1384962 NM DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 PHX - C8 CK - "C" - DENT IN FRAME UPPER FLANGE AT BS 680, STR 24R. MAINTENANCE CUT OUT DAMAGED AREA, FRABRICATED REPAIR ANGLE AND INSTALLED IAW B757 SRM 51-70-11, FIG 1, PG 1. 2 L 7 2 4F RT A2NM 2001102900142 20011029 00142 NM 2001 10 29 AWXA200100544 1 20010905 A 5311 143N1013 FRAME BOEING 757 7572S7 1384962 NM DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 PHX - C8 CK - "C" - DENT FOUND IN FRAME UPPER FLANGE AT BS 680, STR 23L & 24L. MAINTENANCE CUT OUT DAMAGED AREAS, FABRIC ATED REPAIR ANGLE AND INSTALLED IAW B757 SRM 51-70-11, FIG 1, PG 1. 2 L 7 2 4F RT A2NM 2001102900143 20011029 00143 NM 2001 10 29 AWXA200100546 1 20010911 A 5311 146N1016 FRAME BOEING 757 7572S7 1384962 NM DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 PHX - C8 CK - "C" - DENT FOUND IN FRAME UPPER FLANGE AT BS 1540, STR 25R. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED R EPAIR ANGLE AND INSTALLED IAW B757 SRM 51-70-11, FIG 1, PG 1 - 7. 2 L 7 2 4F RT A2NM 2001102900144 20011029 00144 NM 2001 10 29 AWXA200100548 1 20010908 A 5320 140N2506 INTERCOSTAL BOEING 757 7572S7 1384962 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 PHX - C8 CK - "C" - CRACK FOUND IN INTERCOSTAL ON AFT SIDE OF FLOOR BEAM AT BS 1320, RBL 45.5, .5" LONG. MAINTENANCE REM OVED DAMAGED INTERCOSTAL, FABRICATED REPLACEMENT PART AND INSTALLED IAW B757 SRM 51-20-02, 51-40-02, PG 1 AND BOEING DWG #140N2506. 2 L 7 2 4F RT A2NM 2001102900145 20011029 00145 NM 2001 10 29 AWXA200100549 1 20010913 A 5311 BAC14902763 FRAME BOEING 757 7572S7 1384962 NM DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 PHX - C8 CK - "C" - DENT FOUND ON UPPER FLANGE OF FRAME AT BS 1600, STR 25L. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATE D REPAIR ANGLE AND INSTALLED IAW B757 SRM 51-70-11, FIG 1, PG 1 - 7. 2 L 7 2 4F RT A2NM 2001102900146 20011029 00146 NM 2001 10 29 AWXA200100550 1 20010905 A 5311 143N1012 FRAME BOEING 757 7572S7 1384962 NM BENT A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 PHX - C8 CK - "C" - BEND IN RADIUS OF FRAME UPPER FLANGE AT BS 660, STR 24R. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATE D REPAIR ANGLE AND INSTALLED IAW B757 SRM 51-70-11, FIG 1, PG 3. 2 L 7 2 4F RT A2NM 2001102900147 20011029 00147 NM 2001 10 29 AWXA200100551 1 20010906 A 5320 141N51869 FLOOR SUPPORT BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 PHX - C8 CK - "C" - CORROSION FOUND ON FLOOR SUPPORT AT BS 398, RBL 24 TO RBL 44, BEYOND SRM LIMITS AFTER CLEAN UP. MAIN TENANCE REMOVED FLOOR SUPPORT, FABRICATED REPLACEMENT PARTS AND INSTALLED IAW B757 SRM 51-40-02, PG 1 & 51-20-01, PG 1 A ND BOEING DWG 141N5186-9, -15 & -16. 2 L 7 2 4F RT A2NM 2001102900148 20011029 00148 NM 2001 10 29 AWXA200100552 1 20010913 A 5320 141N518610 CHANNEL BOEING 757 7572S7 1384962 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 PHX - C8 CK - "C" - CORROSION FOUND ON FLOOR SUPPORT CHANNEL STIFFENER ON THE LOWER SIDE AROUND A NUT PLATE AT BS 400, R BL 29. MAINTENANCE REMOVED CORRODED CHANNEL, FABRICATED REPLACEMENT PART AND INSTALLED IAW B757 SRM 51-40-02, PG 1. 2 L 7 2 4F RT A2NM 2001102900149 20011029 00149 NM 2001 10 29 AWXA200100553 1 20010906 A 5320 654N02438 FLOOR SUPPORT BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 PHX - C8 CK - "C" - CORROSION FOUND ON FLOOR SUPPORT AT BS 395 TO 400, RBL 22. MAINTENANCE REMOVED FLOOR SUPPORT, FABRIC ATED AND INSTALLED REPLACEMENT PART IAW B757 SRM 51-40-02, PG 1 AND BOEING DWG 141N5186. 2 L 7 2 4F RT A2NM 2001102900150 20011029 00150 NM 2001 10 29 AWXA200100554 1 20010911 A 5320 146N8522 FRAME BOEING 757 7572S7 1384962 NM AFT CARGO COMP. BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 PHX - C8 CK - "C" - E-6 EQUIPMENT RACK, CENTER LOWER I/B SUPPORT FRAME AT CARGO FLOOR LEVEL FOUND BROKEN BETWEEN BS 1440 & 1480. MAINTENANCE REMOVED DAMAGED SUPPORT, FABRICATED REPLACEMENT PART AND INSTALLED IAW B757 SRM 51-40-02, PG 1 AND BOEING DWG 284N1474. 2 L 7 2 4F RT A2NM 2001102900151 20011029 00151 NM 2001 10 29 AWXA200100555 1 20010906 A 5320 141N518619 FLOOR SUPPORT BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 PHX - C8 CK - "C" - CORROSION FOUND ON FLOOR SUPPORT AT BS 365, RBL 50 TO RBL 60, BEYOND SRM LIMITS AFTER CLEAN UP. MAIN TENANCE REMOVED DAMAGED FLOOR SUPPORT, FABRICATED REPLACEMENT PART AND INSTALLED IAW B757 SRM 51-40-02, PG 1 AND BOEING DWG 141N5186. 2 L 7 2 4F RT A2NM 2001102900152 20011029 00152 NM 2001 10 29 AWXA200100556 1 20010904 A 5330 144N31401 SKIN BOEING 757 7572S7 1384962 NM IMPROPER A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 PHX - C8 CK - "C" - RIVITS ON EXTERNAL FUSELAGE SKIN REPAIR AT BS 1100, STR 6L FOUND NOT TO BE PROPERLY SEATED. MAINTENA NCE REMOVED EXTERNAL REPAIR AND REPLACED WITH FLUSH REPAIR IAW AWA ER 19-5331-01274-DL1. 2 L 7 2 4F RT A2NM 2001102900153 20011029 00153 NM 2001 10 29 AWXA200100557 1 20010913 A 5320 141N517048 SUPPORT BOEING 757 7572S7 1384962 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 PHX - C8 CK - "C" - CORROSION FOUND AROUND NUTPLATES ON L-1 DOOR THROUGH SUPPORT ANGLE, BS 370, LBL 60, WL 208. MAINTENA NCE REMOVED SUPPORT ANGLE AND REPLACED WITH NEW PART IAW B757 SRM 51-20-01, PG 1. 2 L 7 2 4F RT A2NM 2001102900154 20011029 00154 NM 2001 10 29 AWXA200100558 1 20010904 A 5347 6945679145 BRACKET BOEING 757 7572S7 1384962 NM FWD / AFT CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 PHX - C8 CK - "C" - CORROSION FOUND ON LOWER FWD CENTER CARGO TIE DOWN FITTING FWD & AFT FACE AT BS 1556 TO 1600, STR 27 R. MAINTENANCE REMOVED FITTING ASSY AND REPLACED FWD & AFT BRACKETS IAW B757 SRM 51-40-02, PG 1 AND BOEING DWG 69-45579. 2 L 7 2 4F RT A2NM 2001102900155 20011029 00155 NM 2001 10 29 AWXA200100559 1 20010906 A 5320 141N842241 ANGLE BOEING 757 7572S7 1384962 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 PHX - C8 CK - "C" - CORROSION FOUND ON FLOOR SUPPORT ANGLE AT BS 324 TO 395, RBL 60. MAINTENANCE REMOVED CORRODED SUPPOR T ANGLE AND REPLACED IAW B757 SRM 51-40-02, PG1. 2 L 7 2 4F RT A2NM 2001102900156 20011029 00156 NM 2001 10 29 AWXA200100560 1 20010911 A 5311 BAC14902770 FRAME BOEING 757 7572S7 1384962 NM DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 PHX - C8 CK - "C" - DENT FOUND ON AFT CARGO COMPARTMENT FRAME UPPER FLANGE AT BS 1300, STR 25R. MAINTENANCE CUT OUT DAMA GED AREA, FABRICATED REPAIR ANGLE AND INSTALLED IAW B757 SRM 51-70-11, FIG 1, PG 1 - 7. 2 L 7 2 4F RT A2NM 2001102900157 20011029 00157 WP 2001 10 29 UPS01837108 1 20011010 A 5720 3644046502 FITTING DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 RIGHT WING STRINGER 64 SPLICE FITTING IS CRACKED AT APPROX XRS 510. REMOVED, FABRICATED, AND REPLAC ED FITTING IAW DWG 3644046 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001102900158 20011029 00158 WP 2001 10 29 UPS01837109 1 20011006 A 5510 ANGLE DOUG DC8 DC873F 302199F WP HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 LEFT HORIZONTAL STAB T/E UPPER ANGLE IS CRACKED AT XE 29. REPAIRED ANGLE IAW SRM 55-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001102900159 20011029 00159 WP 2001 10 29 UPS01837111 1 20011004 A 5720 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 834. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001102900160 20011029 00160 WP 2001 10 29 UPS01837112 1 20011004 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 335.25. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001102900161 20011029 00161 WP 2001 10 29 UPS01837113 1 20011004 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XS 515.72. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001102900162 20011029 00162 WP 2001 10 29 UPS01837114 1 20011004 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 316.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001102900163 20011029 00163 WP 2001 10 29 UPS01837115 1 20011004 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 366.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001102900164 20011029 00164 WP 2001 10 29 UPS01837116 1 20011004 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XS 497.491. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001102900165 20011029 00165 WP 2001 10 29 UPS01837117 1 20011004 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XS 491.193. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001102900166 20011029 00166 WP 2001 10 29 UPS01837118 1 20011004 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 RIGHT WING L/E LOWER RIB IS CRACKED AT XOLDI 6.225. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001102900167 20011029 00167 WP 2001 10 29 UPS01837119 1 20011004 A 5720 576958976 CLIP DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 RIGHT WING L/E INTERCOSTAL ATTACH CLIP IS CRACKED AT XOLDI 6.225. REMOVED, FABRICATED, AND REPLACED CLIP IAW DWG 5769589, AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001102900168 20011029 00168 WP 2001 10 29 UPS01837120 1 20011004 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 404. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001102900169 20011029 00169 NM 2001 10 29 F3LA200100115 1 20011022 A 5270 PROXIMITY SWITCH BOEING 737 7373S1 138447S NM OUT OF ADJ A F3LA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 03 311FL 2117 24856 REJECTED TAKEOFF. FLIGHT CREW REPORTED AFT CARGO COMPARTMENT DOOR LIGHT ILLUMINATED UPON REACHING TAKEOFF THRUST. ADJU STED AFT CARGO COMPARTMENT DOOR PROXIMITY SWITCH. 2 L 7 2 4F RT A16WE 2001102900170 20011029 00170 WP 2001 10 29 UPS01837121 1 20011002 A 5751 5764617U51 PANEL DOUG DC8 DC873F 302199F WP LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 LEFT O/B AILERON I/B WEIGHT PANEL IS CORRODED BEYOND LIMITS BETWEEN. REMOVED AND REPLACED WEIGHT PA NEL IAW DWG 5764617U51, AND REMOVED, FABRICATED, AND REPLACED SKIN IAW DWG 5763133, AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001102900171 20011029 00171 WP 2001 10 29 UPS01837130 1 20011004 A 5713 STRINGER DOUG DC8 DC871F 302199D WP WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:SV FOUND CRACKED STRINGER IAW HFEC PER NDT SRM 06-10-01.003 AT STA APPROX 240.000 XLS STRINGER 58. REMO VED 80 INCHES OF STRINGER AND SPLICED IN NEW SECTION OF STRINGER IAW DC8 SRM 51-1-24, 57-2-2 AND 51-1-8. 2 L 7 4 4F RT 4A25 2001102900172 20011029 00172 WP 2001 10 29 UPS01837131 1 20011004 A 5730 SKIN DOUG DC8 DC871F 302199D WP WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:SV BOTTOM SKIN OF NR 4 MAIN I/B SIDE OF NR 3 PYLON BY PUMP HOUSING LOWER SKIN CRACKED AT FASTENER HOLE S TA XCW 172.000 STR 58. COUNTERBORED HOLE TO .630 .003, FABRICATED BUSHING FOR SKIN, INSTALLED COUNTERSUNK BUSHING IAW REO G08431. 2 L 7 4 4F RT 4A25 2001102900173 20011029 00173 WP 2001 10 29 UPS01837132 1 20011004 A 5320 3750257U1 SPLICE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 STA 440 - 460 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001102900174 20011029 00174 NM 2001 10 29 VNAA0110013 1 20011017 A 3350 321430 BATTERY PACK DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 457PS 12081 3048 THE CREW REPORTED THAT THE EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BA TTERY AT THE 6LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001102900175 20011029 00175 NM 2001 10 29 VNAA0110014 1 20011018 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 439JS 14153 3057 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 1 THROUGH 4 WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLA CED THE EMERGENCY BATTERY AT THE 4LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECK S WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001103000001 20011030 00001 CE 2001 10 30 COE2001F00001 1 20011005 A 2710 065006001 SERVO CESSNA 208 208B 2073701 CE PWA PT6 PT6A11 52043 NE COVER/AILERON MISALIGNED A COEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 13 775FE 208B0272 19155 ON CLIMB OUT FOR DEPARTURE, PILOT EXPERIENCED BINDING IN THE AILERON CONTROL SYSTEM. THE PILOT INITIATED AN AIR TURN BA CK AND LANDED WITHOUT FURTHER INCIDENT. NO INFLIGHT EMERGENCY WAS DECLARED. TROUBLESHOOTING REVEALED THE COVER ON THE ROLL SERVO WAS MISALIGNED. THE COVER WAS REMOVED AND REINSTALLED IN THE PROPER POSITION. A FUNCTIONAL CHECK FLIGHT WAS ACCOMPLISHED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 H 7 1 3T 3 T A37CE E4EA 2001103000003 20011030 00003 NM 2001 10 30 CALA0100979 1 20011026 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM STA 370 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59338 23576 INSPECTION FOUND L/H O/B SEAT TRACK CORRODED AT STA 370. A REPAIR WAS INSTALLED IAW SRM 53-00-52, FIGURE 202. 2 L 7 2 4F RT A16WE 2001103000004 20011030 00004 NM 2001 10 30 CALA0100982 1 20011028 A 5754 SKIN BOEING 737 7373T0 1384582 NM #1 SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69333 23571 INSPECTION FOUND #1 SLAT SKIN CRACKED AT AFT ROW OF RIVETS APPROXIMATELY 1/8" ON EITHER SIDE OF RIVET, 43" O/B OF I/B EN D. A REPAIR WAS INSTALLED IAW SRM 57-43-01, FIGURE 206. 2 L 7 2 4F RT A16WE 2001103000005 20011030 00005 NM 2001 10 30 CALA0100983 1 20011029 A 5340 ATTACH ANGLE BOEING 737 7373T0 1384582 NM BS 305 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59338 23576 INSPECTION FOUND A 1" CRACK IN STRINGER 4L ATTACH ANGLE AT BS 305. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51- 10-02. 2 L 7 2 4F RT A16WE 2001103000006 20011030 00006 NM 2001 10 30 CALA0100984 1 20011029 A 5320 WEB BOEING 737 7373T0 1384582 NM STA 637 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59338 23576 INSPECTION FOUND A 3" CRACK IN WEB AT FLOOR LINE BELOW R/H EXIT OPENING AT STA 637, S17R. THE WEB WAS REMOVED AND REPLAC ED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001103000007 20011030 00007 WP 2001 10 30 CALA0100985 1 20011029 A 5730 SKIN DOUG DC9 DC982 3022082 WP WS XOS 286 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35832 49492 INSPECTION FOUND A 1.5" CRACK IN R/H WING UPPER L/E SKIN BETWEEN #2 & #3 SLAT PANELS AT WS XOS 286. A SKIN DOUBLER REPAI R WAS INSTALLED IAW ECRA 5720-01731. 2 L 7 2 4F A6WE 2001103000008 20011030 00008 EA 2001 10 30 COMA0160854 1 20011029 A 5415 601370102 PYLON CNDAIR CL600 CL6002B19 EA EMPENNAGE CORRODED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 978CA 10969 7158 DURING REMOVAL OF THE RIGHT ENGINE ASSEMBLY DISCOVERED CORROSION ON THE AFT ENGINE PYLON THRUST FITTING MOUNTING RIB.REP AIRED I/A/W REO 601R-54-50-032. 2 L 7 2 4F RT A21EA 2001103000009 20011030 00009 EA 2001 10 30 COMA0160855 1 20011017 A 3350 LAMP CNDAIR CL600 CL6002B19 EA A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 783CA 7315 FLIGHT #5480. FLOOR PATH EMERGENCY LIGHTING, ROWS 9 THRU 13, ARE INOPERABLE.RECONECTED LOOSE LIGHT STRIP - SYSTEM TEST NORMAL. 2 L 7 2 4F RT A21EA 2001111400021 20011114 00021 NM 2001 11 14 01FDEA00935 1 20011029 A 5313 STRINGER BOEING 727 727233 138408A NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 279FE 22346 STRINGER 27L EDGE DAMAGE BS 480, WL 149. REMOVED AND REPLACED STRINGER PER EA 7-5310-59896. 2 L 7 3 4F RT A3WE 2001103000011 20011030 00011 EA 2001 10 30 COMA0160856 1 20011025 A 3350 363782 LAMP CNDAIR CL600 CL6002B19 EA CABIN FLOOR INOPERATIVE A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 943CA 7062 FLIGHT #5800 - EMERGENCY FLOOR PATH LIGHTING, ROWS 9 AFT, ARE INOPERABLE.REPLACED DAMAGED FLOOR PATH LIGHTING STIRP. 2 L 7 2 4F RT A21EA 2001103000013 20011030 00013 EU 2001 10 30 2001F00474 1 20010920 A 7714 0177555170 CONTROL BOX SNIAS 350 AS350BA 8680817 EU ENGINE FAILED A KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 230SH 2337 BLEED VALVE OPENED IN FLIGHT, TROUBLESHOOTING. FOUND TACH BOX NOT WORKING. INSTALLED SERVICEABLE UNIT. (M) 1 G 7 1 3U NC H9EU 2001103000014 20011030 00014 2001 10 30 2001F00475 4 20010920 A 3452 KT76A TRANSPONDER SNIAS 350 AS350BA 8680817 EU COCKPIT FAILED A KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 230SH 2337 TRANSPONDER FAILED INFLIGHT. INSTALLED SERVICEABLE UNIT. (M) 1 G 7 1 3U NC H9EU 2001103000015 20011030 00015 EU 2001 10 30 2001F00476 1 20010930 A 6510 350A34021005 DRIVE SHAFT SNIAS 350 AS350BA 8680817 EU TAIL ROTOR WORN A KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 2273A 2273 DRIVE SHAFT WORN OUT OF LIMITS AT BEARINGS PLANE OF ROTATION. INSTALLED SERVICEABLE T/R DRIVESHAFT. (M) 1 G 7 1 3U NC H9EU 2001103000016 20011030 00016 EU 2001 10 30 2001F00477 1 20010929 A 7931 6200KAA10T5PN ADAPTER SNIAS 350 AS350BA 8680817 EU OIL SYSTEM DEFECTIVE A KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 37SH 2300 NO OIL PRESSURE INDICATIONS ON THE GAUGE. REPLACED WITH SERVICEABLE ADAPTER PIGTAIL. (M) 1 G 7 1 3U NC H9EU 2001103000017 20011030 00017 2001 10 30 2001F00478 4 20010930 A 2312 KY196A RADIO SNIAS 350 AS350B2 8680813 EU VHF SYS FAULTY A KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 345SH 3345 NO VOICE ON TRANSMITTER. THIS RADIO WAS REINSTALLED IN ANOTHER AIRCRAFT AND WAS FOUND TO FUNCTION PROPERLY. REPLACED W ITH SERVICEABLE VHF RADIO. (M) 1 G 7 1 3U H9EU 2001103000018 20011030 00018 EU 2001 10 30 2001F00479 1 20010930 A 5630 3501CC20256 WINDOW SNIAS 350 AS350BA 8680817 EU RT FWD DOOR CRACKED A KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 270SH 1864 RIGHT FRONT DOOR WINDOW CRACKED. REPLACED WITH SERVICEABLE WINDOW W/REF TO CHAPTER 52 AEC MWC. (M) 1 G 7 1 3U NC H9EU 2001103000019 20011030 00019 EU 2001 10 30 2001F00480 1 20010929 A 2150 060018 BELT SNIAS 350 AS350* EU AIR CONDITIONING FAILED A KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 115SH 3141 AIRCONDITIONING INOPERATIVE. REPLACED A/C BELT. (M) 1 G 7 1 3U H9EU 2001103000020 20011030 00020 EU 2001 10 30 2001F00481 1 20010830 A 2913 GHC1003 POWERPACK UROCOP EC120 EC120B 8680987 EU HYDRAULIC SYS MALFUNCTIONED A CAXA O OTHER O OTHER NR NOT REPORTED 1 WP 15 408DC 1151 NOT SHUTTING OFF. HYDRAULIC UNIT P/N GHC100-3. (M) 1 G 7 2 3U NC R0001RD 2001103000021 20011030 00021 EU 2001 10 30 2001F00482 1 20010830 A 2120 SC50911 SERVO UROCOP EC120 EC120B 8680987 EU AIR DISTRIBUTION UNSERVICEABLE A CAXA O OTHER O OTHER NR NOT REPORTED 1 WP 15 408DC 254 1151 REPLACED SERVO. (M) 1 G 7 2 3U NC R0001RD 2001103000023 20011030 00023 NM 2001 10 30 AALA20011652 1 20010818 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 848AA 20989 DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIR EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHEC KED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001103000024 20011030 00024 NM 2001 10 30 AALA20011654 1 20010818 A 3350 P4010049 BATTERY PACK BOEING 727 727223 1384074 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 872AA 21384 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT PATH LIGHTING AT R1 AND L1 DOOR INOPERATIVE. REPLACED BATTERY PACKS. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001103000025 20011030 00025 NM 2001 10 30 AALA20011681 1 20010823 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 721AA 20729 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY OVERHEAD EXIT LIGHT AT R1 DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2001103000026 20011030 00026 EU 2001 10 30 AALA20011696 1 20010825 A 3350 P4010049 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1430D 11415 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT R4 INOPERATIVE. REPAIRED BROKEN WIRE AND REPLACED BATTERY PACK . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001103000027 20011030 00027 NM 2001 10 30 AALA20011700 1 20010823 A 3350 LIG5714 LIGHT BOEING 727 727223 1384074 NM AFT AIRSTAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 885AA 21524 TUL - FOUND VENTRAL STAIRS EMERGENCY LIGHT INOPERATIVE. INSTALLED SERVICEABLE VENTRAL STAIRS EMERGENCY LIGHT PER MM 33- 50-061-4 PAGE 403, REPAIRED ON E-58 4012889. (M) 2 L 7 3 4F A3WE 2001103000028 20011030 00028 EU 2001 10 30 AALA20011705 1 20010829 A 3350 321441 POWER SUPPLY AIRBUS 300 A300B4605R 3930308 EU CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70054 461 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS AT L2 DOOR INOPERATIVE. REPLACED POWER SUPPLY. SYSTEM GROUND CHEC KED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2001103000029 20011030 00029 NM 2001 10 30 AALA20011780 1 20010916 A 3350 SOCKET BOEING 767 767323 1385205 NM CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 386AA 27060 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT SOCKET. SYSTEM GROU ND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001103000030 20011030 00030 NM 2001 10 30 AALA20011785 1 20010918 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 372AA 25199 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 10AB INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEA T 10AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001103000031 20011030 00031 NM 2001 10 30 AALA20011787 1 20010913 A 2421 GEN3014 IDG BOEING 777 777223 1385213 NM LT ENGINE FAILED A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 779AN 29955 ELECTRICAL GEN SYSTEM LEFT ON STATUS ELECT GEN OFF LEFT ON EICAS SYNOPTIC INDICATES CSD DISCONNECTED. REPLACED LEFT ENG INE IDG AND GCU LEAK AND OPS CHECK OK ON ENGINE RUN UP DISCONNECT CHECK OK. (M) 2 L 7 2 4F RT T00001SE 2001103000032 20011030 00032 NM 2001 10 30 AALA20011797 1 20010913 A 2424 CON5330 GCU BOEING 767 767223 1385123 NM E/E BAY FAILED A AALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 SW 21 320AA 22321 AFTER TAKEOFF, RIGHT GEN OFF PLUS RIGHT GEN DRIVE LIGHT ON STEADY. GEN DISCONNECTED BY CREW. PLACARD RIGHT GEN INOPERA TIVE PER MEL ENTERED IN MIC SHEET VERIFIED BOTH IDG'S AND APU OIL FULL IAW MEL 24-1 IDG REMAINS DISCONNECTED. BITE CHEC K OF BPCU SHOWS NO FAULT UP TO 10 FLIGHT LOGS, ON RIGHT GCU. MEG CHECK SHOWED NO SHORTS. SHOOK HAR 5272 WIRING. NO OP ENS NOTED. REPLACED RIGHT ENGINE GCU. RAN ENGINE. LOADED RIGHT GENERATOR, NO FAULTS. RIGHT GENERATOR OPS CHECK NORMA L. REMOVED DEV 9-221DC-A MEL REP 24-1. CLEARED MIC SHEET. REPLACED IDG HARNESS HAR 5272 RAN RIGHT ENGINE SYSTEM CHECK S NORMAL. (M) 2 L 7 2 4F RT A1NM 2001103000033 20011030 00033 NM 2001 10 30 AALA20011798 1 20010919 A 3350 SOCKET BOEING 767 767323 1385205 NM L4 DOOR DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 352AA 24033 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L4 DOOR INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT SOCKET AT L4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001103000034 20011030 00034 NM 2001 10 30 AALA20011799 1 20010919 A 3350 0201820001S LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 352AA 24033 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM G ROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001103000035 20011030 00035 NM 2001 10 30 AALA20011800 1 20010920 A 1420 CONNECTOR BOEING 767 767323 1385205 NM CABIN FAULTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 390AA 27450 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 31B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT SIDE WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001103000036 20011030 00036 NM 2001 10 30 AALA20011809 1 20010924 A 1420 CONNECTOR BOEING 767 767223 1385123 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 329AA 22329 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 28H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECT OR AT SEAT 28H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001103000037 20011030 00037 NM 2001 10 30 AALA20011810 1 20010925 A 1420 CONNECTOR BOEING 767 767323 1385205 NM CABIN FAULTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 353AA 24034 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SET 23B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTO R. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001103000038 20011030 00038 NM 2001 10 30 AALA20011812 1 20010918 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 876AA 21388 TUL - FOUND SATION 1130 TOP OF FLOORBEAM BETWEEN LEFT SEAT TRACKS CORRODED. FABRICATED AND INSTALLED REPAIR STRAP PER E SO 11697 DATED 9-17-01. (M) 2 L 7 3 4F A3WE 2001103000039 20011030 00039 NM 2001 10 30 AALA20011813 1 20010919 A 5311 FRAME BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 876AA 21388 TUL - FOUND CORROSION ON FRAME STATION 370 BELOW FLOOR LINE RBL 65. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER ESO 11697 ATED 9-14-2001. (M) 2 L 7 3 4F A3WE 2001103000040 20011030 00040 NM 2001 10 30 AALA20011814 1 20010912 A 5320 SPLICE BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 876AA 21388 TUL - FOUND LIGHT CORROSION ON END OF STRINGER SPLICE, STATION 686, STRINGER 28R. REMOVED AND REPLACED WITH NEW STRINGE R SPLICE PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 2001103000041 20011030 00041 NM 2001 10 30 AALA20011816 1 20010924 A 2421 GEN5103 IDG BOEING 767 767323 1385205 NM RT ENGINE FAILED A AALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SW 21 351AA 24032 FLT 96 - THREE HOURS INTO FLIGHT RIGHT GEN DRIVE LIGHT CAME ON STEADY. DISCONNECTED RIGHT GEN IAW PROCEDURES. PART NIS AT MXP. ENTERED IN MIC SERVICED BOTH IDGS. ADDED 2 PTS ON RIGHT AND 0 FOR THE LEFT IDG. BPCU TEST SHOWN IDG/OIL IN BUL B WIRING. REPLACED RIGHT IDG. LEAK AND OPS CHECKED OK. (M) 2 L 7 2 4F RT A1NM 2001103000042 20011030 00042 NM 2001 10 30 AALA20011838 1 20010927 A 5313 STRINGER BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 875AA 21387 TUL - FOUND CORROSION ON STRINGER TIE STATION 1133 ON INBOARD SIDE OF STRINGER 27L. CUT OUT CORRODED SECTION OF STRINGE R STATION 1116 TO 1134. INSTALLED NEW STRINGER SECTION AND REPAIR SPLICE PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 2001103000043 20011030 00043 NM 2001 10 30 AALA20011839 1 20010926 A 5310 SHEAR TIE BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 875AA 21387 TUL - FOUND CORROSION ON SHEAR TIE STATION 700 BETWEEN STRINGER 28R AND 29R. TRIMMED OFF DAMAGED SECTION OF SHEAR TIE A ND INSTALLED REPAIR AT SKIN ATTACHMENT AS PER SRM 53-10-4 FIG 15 SHEET 3. (M) 2 L 7 3 4F A3WE 2001103000044 20011030 00044 NM 2001 10 30 AALA20011840 1 20010926 A 5310 SHEAR TIE BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 875AA 21387 TUL - FOUND CORROSION ON SHEAR TIE STATION 680 BETWEEN STRINGER 28R AND STR 29R. REMOVED CORRODED SHEAR TIE FLANGE AND INSTALLED REPAIR ANGLE PER SRM 53-10-4 FIG 14. (M) 2 L 7 3 4F A3WE 2001103000045 20011030 00045 NM 2001 10 30 AALA20014060 1 20010914 A 5230 BEAM BOEING 767 767223 1385123 NM CARGO DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 301AA 22307 AFW - FOUND FORWARD CARGO DOOR BEAM NR 3 HAS CORROSION BLENDED ON INBOARD SURFACE BEYOND SRM LIMITS. REMOVE CORROSION A ND BLENDING, FABRICATED REPAIR STRAP, FABRICATE FILLER RETAINING STRAP, FINISHED ALL BARE SURFACES AND REPAIR PARTS WITH ALODINE AND TWO COATS PRIMER. (M) 2 L 7 2 4F RT A1NM 2001103000046 20011030 00046 NM 2001 10 30 AALA20014061 1 20010914 A 5230 BEAM BOEING 767 767223 1385123 NM CARGO DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 301AA 22307 AFW - FORWARD CARGO DOOR BEAM NR 7 HAS CORROSION REMOVED ON INBOARD SURFACE. REMOVED CORROSION AND BLENDING PER REFIG, FABRICATE REPAIR STRAP. FABRICATE FILLER RETAINING STRAP. FINISH ALL BARE SURFACES AND REPAIR PARTS WITH ALODINE. (M) 2 L 7 2 4F RT A1NM 2001103000051 20011030 00051 NM 2001 10 30 DHL2001742524 1 20011019 A 5311 FRAME BOEING 727 727225 1384077 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 DH 21290 AT C-CHECK, FUSELAGE FRAME HAS CRACK IN LOWER INTERIOR WALKWAY BEAM LT SIDE BS 320 JUST ABOVE WALKWAY BEAM SKIN. 2 L 7 3 4F A3WE 2001103000052 20011030 00052 NM 2001 10 30 DHL2001742525 1 20011003 A 5730 ANGLE BOEING 727 727225 1384077 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, FUSELAGE LEFT WING T/E AREA, UPPER FIXED PANEL TOP OF I/B FLAP O/B JACKSCREW HAS SUPPORT ANGLE CRACKED ALONG RIVET. 2 L 7 3 4F A3WE 2001103000053 20011030 00053 NM 2001 10 30 DHL2001742526 1 20011003 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 DURING C-CHECK, CABIN FLOORBEAM HAS CRACKED WEB BS 825.95 LEFT O/B LBL 60, CRACK STARTS FROM ABOVE GUSSET FASTENER HOLE. REMOVED WEB AT BS 825.95 LBL 60 AS PER B-727 SRM 51-30-2. FABRICATE NEW WEB AS PER B-727 SRM 53-10-2 FIGURE 7. INSTALL ED WEB AS PER B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2001103000054 20011030 00054 NM 2001 10 30 DHL2001742527 1 20011018 A 5320 FLOOR SUPPORT BOEING 727 727225 1384077 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 DURING C-CHECK, AFT BAG BIN, AFT OF STA 950F, FLOOR SUPPORT HOT SECTION NR 4 HAS MULTIPLE HOLES, SOME ON EDGE OF BEAM HA S DENTS. REMOVED AND REPLACED SECTION OF FLOOR SUPPORT FROM STA 950 E TO 990 AS PER B-727 SRM 51-40-3 AND B-727 SRM 51-3 0-2. 2 L 7 3 4F A3WE 2001103000055 20011030 00055 NM 2001 10 30 DHL2001742528 1 20011010 A 5320 WEB BOEING 727 727225 1384077 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 DURING C-CHECK, AFT CABIN HAS CORROSION AT LWR WEB AT STA 1177 AND RBL 17. ROUTED OUT CORROSION AT LWR WEB AT STA 1172 AND RBL 17 AS PER B-727 SRM 51-40-2. INSTALLED DOUBLER REPAIR IAW B-727 SRM 51-40-2 FIGURE 1. 2 L 7 3 4F A3WE 2001103000056 20011030 00056 NM 2001 10 30 DHL2001742529 1 20011004 A 5320 WEB BOEING 727 727225 1384077 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 DURING C-CHECK, AFT CABIN HAS SHEAR WEB PLATE WITH CORROSION IN TWO PLACES BS 1166 AND 1148 RBL 15. CUT OUT CORRODED AR EA OF SHEAR WEB AT BS 1148 AND 1166 RBL 15. INSTALLED DOUBLER REPAIR AT BS 1148 AND 1166 AS PER B-727 SRM 51-40-2 FIGUR E 1. 2 L 7 3 4F A3WE 2001103000057 20011030 00057 NM 2001 10 30 DHL2001742530 1 20011004 A 5320 PLATE BOEING 727 727225 1384077 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 DURING C-CHECK, AFT CABIN HAS SHEAR VIEW PLATE HAS CRACK AROUND BOLT, AND BOLT IMPROPERLY INSTALLED BS 1176 RBL 30. REM OVED FASTENER AND CUT OUT DAMAGE AREA FOR CRACK AT AFT CABIN STA 1176 RBL 30. REMOVED AND REPLACED DOUBLER AT CABIN BS 1176 RBL 30. 2 L 7 3 4F A3WE 2001103000058 20011030 00058 NM 2001 10 30 DHL2001742531 1 20011009 A 5330 SKIN BOEING 727 727225 1384077 NM FUSELAGE BULGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, LOWER FUSELAGE HAS BULGING SKIN AT BS 1050 & STRINGER R28. 2 L 7 3 4F A3WE 2001103000059 20011030 00059 NM 2001 10 30 DHL2001742540 1 20011009 A 5330 SKIN BOEING 727 727225 1384077 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, LWR FUSE HAS BULGING SKIN AT BS 1050 & STR R28. CUT OUT DAMAGED STR 35. REMOVED PREVIOUS DOUBLER REPAIR AT STR 28R AND STA 1050. REMOVED CORROSION ON INNER SKIN AT STA 1050, STR 28R, FOUND TO BE OUT OF LIMITS. CUT OUT CORROD ED AREA AT LWR SKIN AT BS 1050 AND STR R28. INSTALLED STRINGER REPAIR FROM BS 1030 TO BS 1080 AT STR 28R AND FUSELAGE D OUBLER REPAIR. 2 L 7 3 4F A3WE 2001103000060 20011030 00060 NM 2001 10 30 DHL2001742541 1 20011001 A 5720 ANGLE BOEING 727 727225 1384077 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, LEFT WING HAS A CRACK AT LEFT EDGE FRONT SPAR VERTICAL ANGLE LOWER END AT WBL 92.8 MARKED. CUT OFF LOWER SE CTION OF ANGLE AT WBL 92.8 LEFT WING L/E AS PER B-727 SRM 51-40-4 FIGURE 2. FABRICATE NEW ANGLE AS PER B-727 SRM 51-40- 4. ALODINED AND PRIMED, INSTALLED ANGLE REPAIR. 2 L 7 3 4F A3WE 2001103000062 20011030 00062 NM 2001 10 30 DHL2001742543 1 20011009 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM FUSELAGE BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, MAIN CABIN SEAT TRACK AT LBL 48 SHOW BROKEN LUGS AT BS 670, 710, BS 730. REMOVED CABIN SEAT TRACK LBL 48 FR OM BS 620 TO BS 740 AS PER B-727 SRM 51-30-2. INSTALLED NEW SEAT TRACK FROM BS 620 TO 740 AS PER B-727 SRM 53-10-5 FIGU RE 7. 2 L 7 3 4F A3WE 2001103000063 20011030 00063 NM 2001 10 30 DHL2001742544 1 20011001 A 5720 ANGLE BOEING 727 727225 1384077 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, LT WING HAS A CRACK AT LEADING EDGE FRONT VERTICAL ANGLE LOWER END AT WBL 92.8. 2 L 7 3 4F A3WE 2001103000064 20011030 00064 NM 2001 10 30 DHL2001742545 1 20011003 A 2782 651720927 ATTACH FITTING BOEING 727 727225 1384077 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, LT WING L/E NR 4 SLAT ACTUATOR FRONT SPAR ATTACH I/B FITTING CRACKED 2 PLACES. REMOVED AND INSTALLED NEW I/ B FITTING AT LT WING NR 4 SLAT ACTUATOR SUPPORT. 2 L 7 3 4F A3WE 2001103000065 20011030 00065 NM 2001 10 30 DHL2001742546 1 20011020 A 5311 FRAME BOEING 727 727225 1384077 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, FRAME CRACK LT STA 360, 12 INCHES ABOVE FLOOR PANEL. CUT OUT DAMAGE AREA AT FRAME LT STA 360 12 INCHES ABOV E FLOOR PANEL. INSTALLED FRAME REPAIR. 2 L 7 3 4F A3WE 2001103000066 20011030 00066 2001 10 30 DHL2001745016 4 20011025 A 2210 CONTROL PANEL BOEING 727 727224 1384076 NM COCKPIT FAULTY A DHLA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 01 745DH 20665 ALTITUDE SELECTOR MODE WHEN ENGAGED, WILL START TO PORPOISE IN BOTH A & B MODE. REMOVED AND REPLACED AUTOPILOT CONTROL PANEL AND PERFORMED OPS CHECK IAW B727 MM 22-11-181. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2001103000067 20011030 00067 2001 10 30 DHL2001745017 4 20011026 A 2212 CONTROLLER BOEING 727 727224 1384076 NM AUTOPILOT SYS FAULTY A DHLA O OTHER O OTHER CR CRUISE 1 SO 01 745DH 20665 AUTO PILOT ALT HOLD MODE ON, HOLDS ALT FOR SHORT TIME. ALT DEVIATION OCCURS, INITIALLY USES YOKE TO COMPENSATE, THEN US ES EXCESSIVE TRIM INPUTS. REMOVED AND REPLACED AUTO PILOT PITCH CONTROL CHANNEL. TESTED IAW B727 M/M CHAPTER 22-11-01. OPS CHECKS NORMAL ON GROUND. 2 L 7 3 4F A3WE 2001103000068 20011030 00068 WP 2001 10 30 DHL2001801547 1 20011017 A 5714 ANGLE DOUG DC8 DC873F 302199F WP CNTR WING BOX CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 CENTER WING BEAM LOWER SUPPORT ANGLE CRACKED 1 INCH AT STA 683 XCW 23 R. REMOVED CRACKED SUPPORT ANGLE PER SRM 51-1-20 PG 21. FABRICATED NEW SUPPORT ANGLE PER SRM 53-2-0 PG 1-2. INSTALLED NEW SUPPORT ANGLE PER SRM 51-1-20 PG 9. 2 L 7 4 4F RT 4A25 2001103000069 20011030 00069 WP 2001 10 30 DHL2001801548 1 20011016 A 5320 WEB DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 MAIN CARGO COMPT SUBFLOOR CRACKED 1 INCH AT STA 1550 L-21 RT. STOP DRILLED CRACK PER SRM 53-2-0. FABRICATED DOUBLER PE R SRM 53-2-0 PG 1-2. INSTALLED NEW SUPPORT ANGLE PER SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2001103000070 20011030 00070 EA 2001 10 30 COMA0160857 1 20011029 A 3350 363782 LAMP CNDAIR CL600 CL6002B19 EA CABIN FLOOR INOPERATIVE A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 811CA 7380 EMERGENCY FLOOR PATH LIGHTING AT ROW 4 IS INOPERABLE.REPLACED DEFECTIVE SECTION OF FLOOR LIGHTING. 2 L 7 2 4F RT A21EA 2001103000071 20011030 00071 EA 2001 10 30 COMA0160858 1 20011029 A 3350 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 EA A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 719CA 7253 FLIGHT #5407. EMERGENCY LIGHTS CIRCUIT BREAKER IS TRIPPED.RESET BREAKER AND FUNCTION CHECKED SYTEM. NO FAULTS FOUND. 2 L 7 2 4F RT A21EA 2001103000072 20011030 00072 WP 2001 10 30 DHL2001801550 1 20011015 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 MAIN CARGO DOOR UPPER FRAME SKIN FROM STA 200 TO 240.000 SHOWS BREAKS OF 3.5 , 2 INCH. TRIMMED OUT DAMAGED AREA PER SRM 53-2-0 FIG 15. FABRICATED FILLER AND DOUBLER PER SRM 53-2-0 FIG 15. INSTALLED FILLER AND DOUBLER PER SRM 53-2-0 FIG 1 5. 2 L 7 4 4F RT 4A25 2001103000073 20011030 00073 WP 2001 10 30 DHL2001801555 1 20011014 A 5320 SUPPORT DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 FWD CARGO COMPT- FRAME SUPPORT SHOWS A 1 INCH CRACK AT LWR SECTION STA 200.000 L-33 TO L-34 R. REMOVED DAMAGED FRAME SU PPORT PER SRM 51-1-20D PG 21. FABRICATED NEW SUPPORT PER SRM 53-2-0 FIG 2. INSTALLED SUPPORT PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001103000074 20011030 00074 WP 2001 10 30 DHL2001801560 1 20011014 A 5753 SKIN DOUG DC8 DC873F 302199F WP T/E FLAP DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 RIGHT WING O/B FLAP UPPER SKIN DENTED 5 INCHES AT XW 250.000. REMOVED DAMAGED SKIN PER SRM 57-20 PG 7-2. FABRICATED SK IN PER SRM 57-7-1 FIG 4. INSTALLED NEW SKIN PER SRM 57-2-0 PG 1-2. 2 L 7 4 4F RT 4A25 2001110800037 20011108 00037 NM 2001 11 8 2001UALA02120 1 20011011 A 3350 LIGHT BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE CABIN MISWIRED A UALA K NONE W L INADEQUATE Q C NO TEST NR NOT REPORTED 1 WP 29 105UA 26473 LEFT HAND FUSELAGE EMERGENCY LIGHT AT MOST FORWARD POSITION INOP. FOUND LIGHT ASSEMBLY WIRED WRONG (POWER TO GROUND). R EWIRED LIGHT ASSEMBLY AND REPLACED FUSE. OPS CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2001103000075 20011030 00075 WP 2001 10 30 DHL2001801561 1 20011012 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 LEFT WING T/E PANEL UPPER SKIN SHOWS CRACKS (1.5 - 0.5 IN) NEAR REAR SPAR XRS 162.000. CUT OUT DAMAGED SKIN AND FABRICA TED FILLER AND DOUBLER PER SRM 57-2-0 FIG 2A AND SRM 57-2-0 FIG 2A. INSTALLED FILLER AND DOUBLER PER SRM 51-1-21 FIG 33 AND DACO TR 51-96. 2 L 7 4 4F RT 4A25 2001103000076 20011030 00076 WP 2001 10 30 DHL2001801562 1 20011016 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AFT BULKHEAD LONGERON L-1AL CRACKED 3 INCHES STA 1766.000. REMOVED DAMAGED LONGERON PER SRM 51-1-20D PG 21. FABRICATED NEW LONGERON WITH EXTRUSION PER SRM 53-2-2 PG 1-5. INSTALLED NEW LONGERON PER SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2001103000077 20011030 00077 WP 2001 10 30 DHL2001801563 1 20011004 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AFT BULKHEAD LONGERON 17 R STA 1766.000 NEAR TO JOINT FITTING CRACKED 3 INCHES. REMOVED CRACKED LONGERON PER SRM 51-1-2 1 PG 1. INSTALLED NEW LONGERON PER SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2001103000078 20011030 00078 2001 10 30 DHL2001801564 4 20011024 A 2210 PLUG DOUG DC8 DC873F 302199F WP ACCELEROMETER DIRTY A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 ACCY COMPT AFT PITCH ACCELEROMETER SHOWS PLUG DIRTY AND CLAMP LOOSE. CLEANED AFT PITCH ACCELEROMETER PLUG PER M/M 20-50 -1. TIGHTENED ALL WIRING CLAMPS PER M/M 22-11-0. PERFORMED OPS CHECK OF SYSTEM PER M/M 22-10-10. 2 L 7 4 4F RT 4A25 2001103000079 20011030 00079 WP 2001 10 30 MWEA011407 1 20011017 A 3070 H161 HEATER DOUG DC9 DC981 3022081 WP ANTI- ICE SYS MALFUNCTIONED A MWEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 807ME 48033 AIRCRAFT WAS PARKED ON TAXI-WAY AWAITING GATE. AFTER 10 MINUTES, THE FORWARD WATER SYSTEM FREEZE PROTECTION SYSTEM C/B POPPED. TWO MINUTES THEREAFTER, THE F/A'S NOTICED A LIGHT SMOKE IN CABIN, EVACUATION CHECKLIST WAS PERFORMED. AIRCRAFT WAS EVACUATED VIA THE FORWARD AIRSTAIRS. MX RAN RIGHT HAND ENGINE, APU, RIGHT HAND AND LEFT HAND PACKS AT SAME TIME. CHECKED TAIL COMPARTMENT R2-366 & R2-307 FOR POTABLE WATER FREEZE PROTECTION SYSTEM. NO VISIBLE DEFECTS NOTED. CHECKED EQUIPMENT COOLING FAN, OPS GOOD. SUSPECT POTABLE WATER FREEZE PROTECTION SYSTEM FAILED. OK FOR SERVICE. 2 L 7 2 4F A6WE 2001103000086 20011030 00086 EU 2001 10 30 XN0A01027 1 20011019 A 3397 WIRE AIRBUS 300 A300B4203 3930306 EU NAV LIGHT DAMAGED A XN0A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 474AS 219 DURING TAXI, NAV FLIGHT LIGHT C/B POPPED OUT. RESETTING, NO HELP. REPAIRED LT NAV LIGHT WIRE. OPS CHECK NORMAL IAW A3 00MM 33-41-00. 2 L 7 2 4F RT A35EU 2001103000087 20011030 00087 WP 2001 10 30 ZW0A0109401 1 20011004 A 3231 DOOR DOUG DC9 DC932 3022066 WP NLG OPEN A ZW0A A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CE 13 996Z 47028 AFTER GEAR RETRACTION PILOT NOTED A VIBRATION IN THE NOSE GEAR AREA. CREW ACCOMPLISHED FLY BY FOR VISUAL CHECK OF NOSE AREA, THEN RETURNED TO STL. FOUND LEFT NOSE GEAR DOOR NOT MANUALLY LATCHED. SECURED DOOR AND CHECKED MANUAL LOCK OPERA TION. 2 L 7 2 4F A6WE 2001103000088 20011030 00088 WP 2001 10 30 ZW0A0109702 1 20011011 A 5342 ATTACH ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9620D 53591 DURING CHECK-C MAINT FOUND CRACK BETWEEN 2 FASTENERS AT ATTACH ANGLE FROM FUSELAGE TO VERTICAL STABILIZER, 7 INCHES FROM AFT END OF THE STABILIZER AT RT SIDE. STOP DRILLED SMALL CRACK PER SRM 53-05, FIG 23. ACCOMP HIGH FREQ EDDY CURRENT P ER NDT 51-00-03. CHECKED STOP DRILL. INSTALLED DOUBLER PER SRM 53-05 FIG 23. INSTALLED HI-LOKS PER SRM 51-30-5. 2 L 7 2 4F RT A6WE 2001103000089 20011030 00089 WP 2001 10 30 ZW0A0109801 1 20011018 A 3350 408822101 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 958U 49703 THE EMERGENCY LIGHTS IN THE TAIL CONE CATWALK WERE DIM AND THE CHUTE LIGHT WAS INOPERATIVE. REPLACED THE BATTERIES IN P OWER PACK B5-28 AND B5-27. 2 L 7 2 4F A6WE 2001103000090 20011030 00090 WP 2001 10 30 ZW0A0109901 1 20011020 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 905TW 49157 THE CABIN CEILING EMERGENCY LIGHTS WERE INOPERATIVE ROWS 12 TO 21 AND 28 TO 29, AND THE EGRESS LIGHTS WERE INOPERATIVE R OW 1 TO 14. REPLACED THE BATTERIES P/N 408822-101 IN THE BATTERY PACK FOR THE CEILING LIGHTS, AND REPLACED THE BATTERY PACK P/N 5822-2 FOR THE EGRESS LIGHTS. 2 L 7 2 4F A6WE 2001103000091 20011030 00091 WP 2001 10 30 DHL2001803015 1 20011026 A 2612 AMPLIFIER DOUG DC8 DC873 302199C WP NR 4 ENGINE INOPERATIVE A DHLA O OTHER L NO TEST NR NOT REPORTED 1 SO 01 803DH 46123 ENG 4 SHORT CIRCUIT WILL NOT TEST WITH EITHER LOOP A OR B. REMOVED AND REPLACED NR 4 ENG DETECTION AMPLIFIER UNIT IAW D C-8 M/M 26-10-2, OPS CHECK SERVICEABLE. 2 L 7 4 4F RT 4A25 2001103000092 20011030 00092 EU 2001 10 30 2001F00487 1 20010813 A 3350 8GH00544828 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 259AE 340B259 RDU - MAINTENANCE REPORTED THE EMERGENCY LIGHT AT ROW 5 AND FLOOR PROXIMITY EMERGENCY LIGHT AT ROW 5 TO BE INOPERATIVE. MAINTENANCE REPLACED THE TWO BULBS FOR ROW 5 EMERGENCY LIGHTS. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200122501. (M) 2 L 7 2 4T RT A52EU 2001103000093 20011030 00093 EU 2001 10 30 2001F00488 1 20010821 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 174AE 340B174 CREW REPORTED THE EMERGENCY LIGHTS WILL NOT TEST. MAINTENANCE REMOVED AND REPLACED ALL FIVE EMERGENCY LIGHT POWER SUPPL Y UNIT IAW SAAB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200123301. (M) 2 L 7 2 4T RT A52EU 2001103000094 20011030 00094 EU 2001 10 30 2001F00489 1 20010821 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 174AE 340B174 SHV - FLT 3536 - CREW REPORTED THE EMERGENCY LIGHTS WILL NOT TEST. MAINTENANCE REMOVED AND REPLACED ALL FIVE EMERGENCY LIGHT POWER SUPPLY UNIT IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20012330 1 (M) 2 L 7 2 4T RT A52EU 2001103000095 20011030 00095 EU 2001 10 30 2001F00490 1 20010821 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 174AE 340B174 SHV - FLT 3536 - CREW REPORTED THE EMERGENCY LIGHTS WILL NOT TEST. MAINTENANCE REMOVED AND REPLACED ALL FIVE EMERGENCY LIGHT POWER SUPPLY UNIT IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20012330 1 (M) 2 L 7 2 4T RT A52EU 2001103000096 20011030 00096 EU 2001 10 30 2001F00491 1 20010821 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 174AE 340B174 SHV - FLT 3536 - CREW REPORTED THE EMERGENCY LIGHTS WILL NOT TEST. MAINTENANCE REMOVED AND REPLACED ALL FIVE EMERGENCY LIGHT POWER SUPPLY UNIT IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20012330 1 (M) 2 L 7 2 4T RT A52EU 2001103000097 20011030 00097 EU 2001 10 30 2001F00492 1 20010821 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 358RZ 340B358 SAN - FLT 3214 - CREW REPORTED THE OVERHEAD EMERGENCY LIGHTS AT SEATS 7A AND 8BC, AND THE FLOOR PROXIMITY AT ROWS 6, AND 7 TO BE INOPERATIVE. AIRCRAFT WAS FERRIED TO LAW WHERE POWER SUPPLY UNITS 24LN AND 23LN WERE REMOVED AND REPLACED IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200123302. (M) 2 L 7 2 4T RT A52EU 2001103000098 20011030 00098 EU 2001 10 30 2001F00493 1 20010823 A 3350 66362 LIGHT SAAB SF340 340B 7860101 EU CABIN LOOSE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 374AE 340B374 LAX - MAINTENANCE REPORTED THE EMERGENCY LIGHT STRIP ON THE RIGHT SIDE IS LOOSE. MAINTENANCE REPLACED THE LIGHT STRIP F ROM SEAT 3A TO SEAT 8A IAW SAAB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200123501. (M) 2 L 7 2 4T RT A52EU 2001103000099 20011030 00099 EU 2001 10 30 2001F00494 1 20010823 A 3350 74331 LIGHT SAAB SF340 340B 7860101 EU CABIN LOOSE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 374AE 340B374 LAX - MAINTENANCE REPORTED THE EMERGENCY LIGHT STRIP ON THE RIGHT SIDE IS LOOSE. MAINTENANCE REPLACED THE LIGHT STRIP F ROM SEAT 3A TO SEAT 8A IAW SAAB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200123501. (M) 2 L 7 2 4T RT A52EU 2001103000100 20011030 00100 EU 2001 10 30 2001F00495 1 20010823 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN MALFUNCTIONED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 222NE 340B222 DFW - FLT 3518 - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHT AT SEAT 7BC TO BE INOPERATIVE. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL CHECK WAS GOOD IAW ATR MM AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001103000101 20011030 00101 EU 2001 10 30 SIMA200122001 1 20010808 A 3350 3013000 POWER SUPPLY AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 541AT 541 DFW - DURING SCHEDULED PS-2 CHECK, MAINTENANCE REPORTED SEVERAL EMERGENCY LIGHTS TO BE INOPERATIVE DURING OPERATIONAL CH ECK OF EMERGENCY LIGHTING SYSTEM. MAINTENANCE REMOVED AND REPLACED A POWER SUPPLY UNIT, OPERATIONAL CHECK WAS GOOD IAW ATR JIC 33-51-21 ABD AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001103000102 20011030 00102 EU 2001 10 30 SIMA200122101 1 20010809 A 3350 66362 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 380AE 340B380 ABI - FOUND CREW REPORTED THE FLOOR PROXIMITY LIGHT STRIP AT ROWS 4 AND 5 TO BE INOPERATIVE. MAINTENANCE REPLACED THE F LOOR PROXIMITY EMERGENCY LIGHT STRIP IAW SAAB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001103000103 20011030 00103 EU 2001 10 30 SIMA200122201 1 20010810 A 3350 PIN SAAB SF340 340B 7860101 EU CABIN DEFECTIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 375AE 340B375 ABI - MAINTENANCE REPORTED THE LEFT EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED A CONTACT PIN ON THE LEFT E MERGENCY LIGHT ASSEMBLY IAW SAAB 340 MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001103000104 20011030 00104 EU 2001 10 30 SIMA200122404 1 20010812 A 3350 LIGHT AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 135MQ 135 MIA - FLT 5247 - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHT AT ROW 9AB TO BE INOPERATIVE. PUT ON MEL AT THIS TIM E. (M) 2 H 7 2 4T RT A53EU 2001103000105 20011030 00105 EU 2001 10 30 SIMA200122501 1 20010813 A 3350 8GH00544828 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 259AE 340B259 RDU - MAINTENANCE REPORTED THE EMERGENCY LIGHT AT ROW 5 AND FLOOR PROXIMITY EMERGENCY LIGHT AT ROW 5 TO BE INOPERATIVE. MAINTENANCE REPLACED THE TWO BULBS FOR ROW 5 EMERGENCY LIGHTS. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001103000106 20011030 00106 EU 2001 10 30 SIMA200122701 1 20010815 A 3397 WIRE AEROSP ATR72 ATR72212A 8680902 EU CABIN BROKEN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 529AM 529 SGF - DURING SCHEDULED PS-2 CHECK MAINTENANCE, REPORTED A FLOOR PROXIMITY LIGHT AT ROW 5 TO BE INOPERATIVE. MAINTENANCE FOUND AND REPAIRED A BROKEN WIRE AT THE LIGHT CONNECTION. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERV ICE. (M) 2 H 7 2 4T RT A53EU 2001103000107 20011030 00107 SO 2001 10 30 145450B 1 20010727 A 3610 54722250 CLAMP EMB 135 EMB135ER 3260203 SO ALLSN AE300 AE3007A GL BLEED AIR SYS LOOSE E CWQA K NONE O OTHER IN INSP/MAINT 1 GL 05 486TM 145364 DURING ACCEPTANCE INSPECTION, IT WAS NOTED THAT THE V BAND CLAMPS ON THE BLEED AIR CHECK VALVE WERE LOOSE DURING PHYSICA L CHECK OF THE CLAMP. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001103000108 20011030 00108 EU 2001 10 30 QXEA0101703 1 20011028 A 3350 23531 BATTERY FOKKER F28 F28MK4000 4990810 EU INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 6986 676 11159 PDX - THE AFT EXTERIOR EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY LOCATED IN THE AFT CARGO AREA . OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001103000118 20011030 00118 CE 2001 10 30 8292001N39CK 1 20010831 A 3260 1EN18 SWITCH LEAR 25 25 5170506 CE GE CJ610 CJ6105 30006 NE RT MLG FAILED E KKFA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 23 39CK 005 LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO AIRPORT. UNEVENTFUL LANDING ACCOMPLISHED. REPLACED RIGHT MAIN GE AR TRUNNION SWITCH WITH NEW AND ADJUSTED IN ACCORDANCE WITH THE SAME. 2 L 7 2 4J 4 J A10CE 1E16 2001103000119 20011030 00119 CE 2001 10 30 AC12001F00000 1 20010910 A 3610 65550393 ELBOW CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE BLEED AIR SYS LEAKING A AC1R K NONE O OTHER IN INSP/MAINT 1 SO 01 351WC 2856 5600330 DURING ENGINE RUN TO CHECK FOR LEAKS AFTER PHASE 1 AND 2 INSPECTION, RIGHT OB BLEED LINE WAS FOUND LEAKING. LEAK WAS LO CATED IN FLEXIBLE SECTION OF ELBOW ASSEMBLY. BLEED AIR PIPING ON THIS ENGINE CAUSE FLEX JOINT TO HAVE PRONOUNCED CURVE. PIPING WAS ADJUSTED APPROX. 300 HOURS PREVIOUS TO THIS EVENT IN HOPE OF PREVENTING THIS TYPE OF FAILURE. PIPING FORWA RD OF THIS ELBOW ASSY IS ATTACHED TO INLET BLEED VALVE WHICH IS HARD BOLTED TO INLET. THE STRAIN ON THE FLEX JOINT OVER TIME CAUSED IT TO FAIL. INSTALLED NEW ELBOW ASSY. 2 L 7 2 4F 4 F RT A22CE E25EA 2001103000120 20011030 00120 CE 2001 10 30 AC12001F00001 1 20010910 A 3233 99121201 ACTUATOR CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE NLG DEFECTIVE A AC1R K NONE O OTHER IN INSP/MAINT 1 SO 01 351WC 2856 499 5600330 WHILE PERFORMING THE GEAR RETRACTION CHECK IN THE PHASE 2 REQUIREMENTS THE NOSE GEAR WOULD NOT RETRACT. THE HYDRAULIC C ART WAS CHECKED AND IT WAS PUTTING OUT 1500 PSI. A KICK TO THE BACKSIDE OF THE NOSE WHEEL CAUSED THE NOSE GEAR TO RETRA CT. THE GEAR WOULD RUN DOWN AND LOCK NORMALLY. AFTER FIVE ATTEMPTS AT RAISING THE NOSE GEAR AND FIVE KICKS TO GET IT T O WORK, THE NOSE GEAR THEN STARTED WORKING NORMALLY. FINISHED THE GEAR CHECKS AND THEN ORDERED ANOTHER NOSE GEAR ACTUAT OR. APPARENTLY SOMETHING IN THE LOCKING MECHANISM WOULD NOT LET NOSE GEAR RETRACT. THE DOWN AND LOCKED LIGHT WOULD GO OUT, BUT NO RETRACTION WOULD ACTUATOR HAD BEEN REPAIRED BY MFG. INSTALLED EXCHANGE ACTUATOR AND RIGGED, OPS CHECK OK. 2 L 7 2 4F 4 F RT A22CE E25EA 2001103000121 20011030 00121 GL 2001 10 30 ALG2001F00025 2 20010824 A 7200 23005297 ENGINE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30 03013 GL NR 2 MAKING METAL E ALGA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 99 1547N 760088 CAE890031S DURING RUN UP NR 2 ENGINE CHIP LIGHT ILLUMINATED. METAL SAW FOUND IN OIL SYSTEM CHIP PLUGS. ENGINE WAS REMOVED AND REP LACE. 1 G 7 2 3U 3 U H1NE E1GL 2001103000122 20011030 00122 CE 2001 10 30 BAQ2001F00001 1 20010919 A 2910 2307006167 HYDRAULIC LINE LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE731* 01518 WP HYDRAULIC SYS LOOSE A BAQA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 03 40DK 15 92 SCHEDULED LANDING GEAR HOSE CHANGE PERFORMED 15.5 HOURS EARLIER. AIRCRAFT WAS EN ROUTE, ABOUT 1.5 HOURS INTO FLIGHT, HY DRAULIC PRESSURE DROPPED TO 1000 PSI. AFTER 20 MINUTES, PRESSURE DROPPED TO ZERO. PILOT ELECTED TO DIVERT AND AN EVENT FUL LANDING WAS MADE. AIRCRAFT WAS PLACED ON JACKS. MAINTENANCE DISCOVERED UPPER END OF SUBJECT HOSE HAD LOOSENED FROM SLIGHT MISALIGNMENT. REPOSITIONED HOSE AND RETORQUED. OPS CHECKED OK. 2 L 7 2 4F 4 F A10CE E6WE 2001103000123 20011030 00123 CE 2001 10 30 BEM2001F00000 1 20011009 A 2750 995240253 MOTOR BEECH 80 65B80 1152812 CE T/E FLAP DAMAGED E BEMA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 GL 15 106BA LD409 FLAPS FAILED TO MOVE. 1 L 7 2 3O 3A20 2001103000124 20011030 00124 NM 2001 10 30 C8Y2001F00000 1 20010805 A 3242 26094724 BRAKE DOUG MD11 MD11F 3023600 NM MLG DAMAGED A C8YY K NONE O OTHER IN INSP/MAINT 1 EA 33 DALCD 6395 48784 DURING REGULAR WHEEL REPLACEMENT, HEAVILY DAMAGED BRAKE WAS FOUND. 2 L 7 3 4F RT A22WE 2001103000125 20011030 00125 SO 2001 10 30 LR7A01112 1 20011030 A 5311 CAP LKHEED 382 382G 526414U SO FS 770 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 667 4590 DURING SCHEDULED B3 INSPECTION PER JOB CARD HB0505 FOUND FS 770 RH BULKHEAD CAP CRACKED AT RBL 63, WL 155.REPAIRED IAW S RM SMP 583-53-50-14. NR 2007. 2 H 7 4 4T A1SO 2001123100055 20011231 00055 SO 2001 12 31 LR7A01113 1 20011030 A 5312 CAP LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 667 4590 DURING SCHEDULED B3 INSPECTION FOUND FS 792 RT BULKHEAD CAP CRACKED AT RBL 63, WL 160. REPAIRED IAW SRM SMP 583-53-50-1 4. 2 H 7 4 4T A1SO 2001103000126 20011030 00126 SO 2001 10 30 LR7A01114 1 20011030 A 5522 SKIN LKHEED 382 382G 526414U SO LHSS 73 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 667 4590 DURING SCHEDULED B3 INSPECTION PER JOB CARD HB0503 FOUND LH ELEVATOR LOWER SKIN CRACKED AT REPAIR DOUBLER AT FS 1130, LH SS 73, WL 277.REPAIRED IAW SRM SMP 583-51-140-12. NR 2017 2 H 7 4 4T A1SO 2001103000127 20011030 00127 SO 2001 10 30 LR7A01115 1 20011030 A 5311 FRAME LKHEED 382 382G 526414U SO FS 477 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 667 4590 DURING SCHEDULED B3 INSPECTION PER JOB CARD HB0505 FOUND FS 477 FRAME CRACKED AT LBL 52, WL 260REPAIRED IAW LAC MEA 382- 53-01-070. NR 2023 2 H 7 4 4T A1SO 2001103100001 20011031 00001 SO 2001 10 31 C2XA01IA382 1 20011021 A 3260 14521495403 PROXIMITY SWITCH EMB 145 EMB145LR SO NOSE GEAR FAULTY A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 22971 145149 TYS - FLIGHT 9379 - AFTER DEPARTURE, THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE, ALONG WITH A ENGINE 1/2 R EV DISAGREE MESSAGE. THE AIRCRAFT RETURNED TO TYS AND LANDED WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR WEIGHT ON WHEELS PROXIMITY SWITCH. THE AIRCRAFT OPERATIONALLY CHECKED GOOD AND WAS APPREOVED FOR RETU RN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001103100002 20011031 00002 SO 2001 10 31 C2XA01IA385 1 20011027 A 3350 BS2197 BATTERY EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 51726 4178 54 120174 DURING SCHEDULED MAINTENANCE THE EMERGENCY LIGHTING SYSTEM IN THE CABIN WAS FOUND TO BE DIM. MAINTENANCE REMOVED AND REP LACED THE #2 EMERGENCY LIGHTING BATTERY, PERFORMED AN OPERATIONAL CHECK OF THE SYSTEM AND APPROVE3D THE AIRCRAFT FOR RET URN TO SERVICE. 2 L 7 2 4T RT A31SO 2001103100003 20011031 00003 EU 2001 10 31 C2XA01IA386 1 20011028 A 3350 LP1670 LAMP AEROSP ATR42 ATR42320 8680930 EU CABIN BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18814 103 DURING SCHEDULED MAINTENANCE THE EMERGENCY EXIT FLOOR PROXIMITY LIGHTS AT SEATS 7A AND 1A WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE LAMPS TO BE BURNED OUT AT THESE LOCATIONS. THE AFFECTED LAMPS WERE REMOVED AND REPLACED AND THE AI RCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001103100004 20011031 00004 WP 2001 10 31 DHL2001803016 1 20011026 A 3240 CONTROL CABLE DOUG DC8 DC873 302199C WP LT BRAKE FAILED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 803DH 46123 NO BRAKE ON BOTH CAPT AND F/O LEFT BRAKE PEDAL. REMOVED AND REPLACED 85/86AA BRAKE CABLE FOR THE LT BRAKES AS PER DACO MM 32-41-0. PERFORMED OPS CHECK, NO FAULTS NOTED. OPS CHECKED OK. 2 L 7 4 4F RT 4A25 2001103100005 20011031 00005 EU 2001 10 31 C2XA01IA387 1 20011031 A 3350 7012210 LAMP AEROSP ATR42 ATR42320 8680930 EU CABIN BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18814 103 DURING SCHEDULED MAINTENANCE THE CABIN OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE AFFECTED LAMP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001103100006 20011031 00006 EU 2001 10 31 C2XA01IA388 1 20011031 A 3350 3011206 LAMP AEROSP ATR42 ATR42320 8680930 EU EXT FUSELAGE BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18814 103 DURING SCHEDULED MAINTENANCE THE EXTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D THE AFFECTED EXTERIOR LAMPS AND APPROVED THE AIRCRAFT FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001103100007 20011031 00007 WP 2001 10 31 DHL2001804021 1 20011027 A 5610 SLIDING WINDOW DOUG DC8 DC873F 302199F WP COCKPIT LACK OF LUBE A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 804DH 46124 CAPT SIDE WINDOW WILL NOT OPEN. LUBED SIDE WINDOW OPERATING MECHANISMS IAW 56-10-0, OPS GOOD. CAPT'S SLIDING WINDOW RE SEALED AND RE-RIG CAPT'S SLIDING WINDOW IAW MM 56-10-0. READY FOR SERVICE. CAPT'S SLIDING WINDOW REQUIRES PRESSURE CHE CK. 2 L 7 4 4F RT 4A25 2001103100009 20011031 00009 SO 2001 10 31 GLBA2001219 1 20011023 A 3250 WARNING SYSTEM EMB 120 EMB120 3260201 SO COCKPIT FALSE ACTIVATION A GLBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 01 108GL 120108 NOSE STEERING DISCONNECT ON T/O ROLL. COULD NOT DUPLICATE, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A31SO 2001103100010 20011031 00010 CE 2001 10 31 GLBA2001225 1 20011030 A 7720 1303800415 INDICATOR BEECH 1900 1900D 1154162 CE #2 FAILED A GLBA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 01 254GL 11554 UE254 #2 ITT INDICATOR FAILED INFLIGHT, REPLACED OPS CHECKED SYSTEM SATISFACTORY 2 L 7 2 4T RT A24CE 2001103100011 20011031 00011 SO 2001 10 31 GLBA2001221 1 20011024 A 3231 DOOR EMB 120 EMB120ER 3260203 SO LT MLG OUT OF ADJ A GLBA O OTHER J WARNING INDICATION CL CLIMB 1 CE 01 71GL 120071 LANDING GEAR WOULD NOT RETRACT ON T/O. ADJUSTED LEFT GEAR DOOR, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A31SO 2001110800057 20011108 00057 NM 2001 11 8 2001UALA02158 1 20011016 A 5315 141W851817 FLOORBEAM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 769UA 26034 26921 STA 246 WEB CRACKED AT RBL 26.06 JUST OUTBOARD OF UPPER FASTENER COMMON TO MID-CHORD. MAJOR REPAIR: DAMAGE REMOVED AND DOUBLER INSTALLED. NOTED CRACKING OF THE 141W8518-17 WEB IS DUE TO THERMAL CONTRACTION THAT RESULTS IN HIGHER THAN EXPE CTED IN-SERVICE LOADING OF THE DOUBLE DEPTH STATION 246 FLOORBEAM. PART IS BEING REPAIRED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001110900048 20011109 00048 CE 2001 11 9 GLBA2001223 1 20011026 A 3610 1299700321 LINE BEECH 1900 1900D 1154162 CE BLEED AIR PIN HOLE A GLBA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 01 255GL UE255 RIGHT BLEED AIR FAIL. REPLACED INSTRUMENT BLEED AIR LINES (P/N 129-970032-1 & 129-550084-1). REPAIRED EVA TUBING, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001103100012 20011031 00012 EU 2001 10 31 MALA010762 1 20011022 A 2120 SMOKE SAAB SF340 SF340A 7850100 EU CABIN DETECTED A MALA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 GL 15 79XJ 340A079 AFTER LANDING FLIGHT 3382, FLIGHT ATTENDANT AND PASSENGERS CLAIMED SMOKE IN THE CABIN. AIRCRAFT WAS SHUTDOWN PER QRH, P ASSENGERS EVACUATED. MAINTENANCE INSPECTED AVIONICS RACK, INTERIOR LIGHTING SYSTEM, BLEED AIR SYSTEM AND PERFORMED TEST FLIGHT. OPS CHECKS AND TEST FLIGHT SATISFACTORY. NO DEFECTS NOTED. COMPLETED WORK PACKAGE DATED 10-23-01, FIRE BOTTL ES CHANGES HAS BEEN COMPLETED. 2 L 7 2 4T RT A52EU 2001103100013 20011031 00013 EU 2001 10 31 MALA010764 1 20011020 A 7933 4053T73P01 BULB SAAB SF340 340B 7860101 EU RT ENGINE DEFECTIVE A MALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 15 407XJ 340B407 DURING FLIGHT 3316, RT PROP OIL TEMP FLUCTUATING 100-160 DEGREES. AIR TURNBACK TO DTW. MAINTENANCE REMOVED AND REPLACE D RT PGB TEMPERATURE BULB P/N 4053T73P01, S/N ON LEW5137. RAN ENGINES, ALL CHECK GOOD AT THIS TIME. ALL IAW SF340 AMM. 2 L 7 2 4T RT A52EU 2001110600091 20011106 00091 NM 2001 11 6 P2EA2001V0002 1 20011018 A 5330 SKIN BOEING 737 737230 1384401 NM FUSELAGE CANNING A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 124NJ 22122 DURING C CHECK WAS FOUND THE EXTERNAL FUSELAGE SKIN AT BS 1078 BETWEEN STR 23R AND STR 24R WITH OIL CAN. FUSELAGE SKIN S ECTION REPAIRED FROM BS 1054 TO BS 1088 BETWEEN STR 16R AND STR 25R IAW COOPESA EO COO-3-53-581-01, DOCUMENT ON FAA 810- 3 APPROVED BY FAA DER. 2 L 7 2 4F RT A16WE 2001110600092 20011106 00092 NM 2001 11 6 P2EA2001V0003 1 20011019 A 5330 SKIN BOEING 737 737230 1384401 NM FUSELAGE DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 124NJ 22122 DURING C CHECK FOUND THE EXTERNAL FUSELAGE SKIN AT BS 909.25 BETWEEN STR 21R AND 22R WITH DENT OUT LIMITS. FUSELAGE SKIN SECTION REPAIRED FROM BS 907 TO BS 912 BETWEEN STR 21R AND STR 23R IAW SRM 53-30-3 FIG 28. 2 L 7 2 4F RT A16WE 2001110600094 20011106 00094 NM 2001 11 6 P2EA2001V0005 1 20011018 A 5230 SKIN BOEING 737 737230 1384401 NM CARGO DOOR DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 124NJ 22122 DURING C CHECK: FWD CARGO DOOR EXTERNAL SKIN WITH SEVERAL DENTS OUT LIMITS. FWD CARGO DOOR SKIN REPLACED IAW SRM 52-30-2 FIG 3. 2 L 7 2 4F RT A16WE 2001110600095 20011106 00095 NM 2001 11 6 P2EA2001V0006 1 20011018 A 5330 SKIN BOEING 737 737230 1384401 NM FUSELAGE DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 124NJ 22122 DURING C CHECK EXTERNAL FUSELAGE BS 374 STR 20R SKIN WITH DENT OUT LIMITS. SKIN SECTION REPAIRED FROM BS 367 TO 381.5 BT W STR 19R AND STR 21R IAW COOPESA EO COO-3-53-580-01 APPROVED BY DER. 2 L 7 2 4F RT A16WE 2001110900060 20011109 00060 NM 2001 11 9 P2EA2001V0008 1 20011022 A 4910 SHROUD BOEING 737 737230 1384401 NM APU CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 124NJ 22122 DURING C-CHECK FOUND APU SHROUD (COWL) LEFT AFT SIDE CRACKED. APU LOWER SHROUD SKIN REPAIRED IAW COOPESA EO COO-3-49-58 7-01, DOCUMENTED ON FAA FORM 8110-3. 2 L 7 2 4F RT A16WE 2001103100015 20011031 00015 NM 2001 10 31 P5CA0100603 1 20011021 A 3350 1356B37 LIGHT BOEING 747 7472U3B NM CABIN INOPERATIVE A P5CA K NONE L NO TEST IN INSP/MAINT 1 WP 23 923FT 22769 UPPER DECK CENTER EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY PER MM 33-51-00. 2 L 7 4 4F RT A20WE 2001103100016 20011031 00016 NM 2001 10 31 P5CA0100604 1 20011031 A 7830 NONE LIGHT BOEING 747 747283B 1384867 NM FALSE INDICATION A P5CA D RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 23 921FT 21575 #4 REVERSER LIGHT CAME ON DURING TAKE OFF ROLL. RETURNED TO RAMP. AMBER IN-TRANSIT LIGHT FLASHES. VERIFIED #4 ENG. T/R CORRECTLY LOCKED OUT AS PER MM 78-30-01 PROCEDURES AS PER CREW REQUEST. ALL FOUND O.K. 2 L 7 4 4F A20WE 2001103100020 20011031 00020 2001 10 31 SWAA012872 4 20011019 A 2565 61620468 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 311SW 23333 FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001103100021 20011031 00021 NM 2001 10 31 SWAA012877 1 20011021 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 525SW 26567 EEPLS INOP FWD CABIN. REMOVED AND REPLACED LIGHT BASE AND INSTALLED END CAP SPACER PER MM. 2 L 7 2 4F RT A16WE 2001103100022 20011031 00022 NM 2001 10 31 SWAA012878 1 20011019 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CRACKED AT BS 663, BL 0. REPAIRED FLOORBEAM PER SWA RA 1-357-1116. 2 L 7 2 4F RT A16WE 2001103100023 20011031 00023 NM 2001 10 31 SWAA012879 1 20011019 A 5315 6545410 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 767 TO 787, RBL 3. REPAIRED FLOORBEAM PER SWA RA 1-A53-2021. 2 L 7 2 4F RT A16WE 2001103100024 20011031 00024 NM 2001 10 31 SWAA012880 1 20011018 A 3350 100885 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED PM CHECK, FOUND EEPLS INOP FWD CABIN. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001103100025 20011031 00025 NM 2001 10 31 SWAA012883 1 20011018 A 5314 6545866 KEELBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED D-CHECK, FOUND RT KEEL BEAM CORRODED AT BS 540. REPAIRED KEEL BEAM PER BFG ER 01-0905. 2 L 7 2 4F RT A16WE 2001103100026 20011031 00026 NM 2001 10 31 SWAA012884 1 20011019 A 3350 610478 BATTERY BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 765SW 29805 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT LT SIDEWALL. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001103100027 20011031 00027 NM 2001 10 31 SWAA012888 1 20011022 A 3350 BR2013 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED A2 CHECK, FOUND EEPLS INOP AT ROW 18. RELAMPED EEPLS PER MM. 2 L 7 2 4F A16WE 2001103100028 20011031 00028 NM 2001 10 31 SWAA012889 1 20011021 A 3350 BR2013 LIGHT BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED C1 CHECK, FOUND EEPLS LOOSE IN AFT CABIN. SECURED EEPLS PER MM. 2 L 7 2 4F A16WE 2001103100029 20011031 00029 2001 10 31 SWAA012890 4 20011021 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2001103100030 20011031 00030 NM 2001 10 31 SWAA012891 1 20011021 A 3350 6949956 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 655WN 28400 DURING SCHEDULED C4 CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 22ABC. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001103100031 20011031 00031 NM 2001 10 31 SWAA012892 1 20011021 A 3350 90083 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 091SW 22963 DURING SCHEDULED SERVICE CHECK, FOUND FWD FUSELAGE EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2001103100032 20011031 00032 2001 10 31 SWAA012893 4 20011022 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 735SA 27867 FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001103100033 20011031 00033 2001 10 31 SWAA012894 4 20011021 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001103100034 20011031 00034 NM 2001 10 31 SWAA012895 1 20011022 A 3350 65C27093 LENS BOEING 737 7373Y0 1384671 NM ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 665WN 23497 FWD ENTRY DOOR EMERGENCY EXIT LIGHT BEZEL FELL OFF. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001103100035 20011031 00035 NM 2001 10 31 SWAA012897 1 20011019 A 3350 65C27093 LIGHT BOEING 737 7373Q8 1384670 NM SERVICE DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR VERTICAL EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001103100036 20011031 00036 2001 10 31 SWAA012898 4 20011019 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001103100037 20011031 00037 NM 2001 10 31 SWAA012906 1 20011018 A 5315 6546804 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 987, RBL 21 TO RBL 44, WL 208. REPAIRED FLOORBEAM PER BFG ER 0 1-0891. 2 L 7 2 4F RT A16WE 2001103100038 20011031 00038 NM 2001 10 31 SWAA012910 1 20011023 A 5311 6516304 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND RT SIDE CHORD CRACKED AT BS 210. REMOVED AND REPLACED CHORD PER SWA ACO 7342-53. 2 L 7 2 4F RT A16WE 2001103100039 20011031 00039 NM 2001 10 31 SWAA012914 1 20011023 A 2782 6544651 ACTUATOR BOEING 737 7372H4 138448C NM L/E SLAT FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 073SW 22673 (AIR TURNBACK ) AFTER TAKEOFF L/E FLAP TRANSIT LIGHT ILLUMINATED AFTER FLAP RETRACTION. RIGHT OUTBOARD SLAT CONFIRMED P ARTIALLY EXTENDED. REMOVED AND REPLACED NR 6 L/E SLAT ACTUATOR PER MM. 2 L 7 2 4F A16WE 2001103100040 20011031 00040 NE 2001 10 31 SWAA012915 2 20011022 A 7200 7B22618 ENGINE BOEING 737 7377H4 1384404 NM GE CFM56 CFM56* 13802 NE NR 1 MAKING METAL A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 719SW 27853 888149 DURING SCHEDULED C4 CHECK, FOUND METAL CHIPS AT NR 1 ENG AGB / TGB MAGNETIC CHIP DETECTOR, CHIPS EXCEED LIMITS GIVEN IN SWA TASK 4118. REMOVED AND REPLACED NR 1 ENG PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2001103100041 20011031 00041 NM 2001 10 31 SWAA012919 1 20011023 A 3350 6556633 COVER BOEING 737 7373T5 1384608 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 RIGHT OVERWING EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001103100042 20011031 00042 2001 10 31 SWAA012920 4 20011023 A 2565 FASTENER BOEING 737 7377H4 1384404 NM ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 730SW 27862 FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINING HOOK HAS LOOSE FASTENER. REMOVED AND REPLACED GIRT BAR FASTENER PER SRM. 2 L 7 2 4F RT A16WE 2001103100043 20011031 00043 NM 2001 10 31 SWAA012921 1 20011019 A 2121 215201 GASPER FAN BOEING 737 7373H4 1384600 NM CARGO BAY FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 606SW 27926 FOUND GASPER FAN NOISY AND PRODUCING ELECTRICAL ODOR. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 2001103100044 20011031 00044 2001 10 31 SWAA012922 4 20011024 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2001103100045 20011031 00045 NM 2001 10 31 SWAA012923 1 20011025 A 3350 101073 LIGHT BOEING 737 7372H4 138448C NM AFT ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM. 2 L 7 2 4F A16WE 2001103100046 20011031 00046 2001 10 31 SWAA012924 4 20011025 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 063SW 22061 AFT SERVICE DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2001103100047 20011031 00047 2001 10 31 SWAA012925 4 20011025 A 3425 7771825001 INDICATOR BOEING 737 7373H4 1384600 NM COCKPIT FAULTY A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 322SW 23343 AIR TURNBACK, CAPT'S HORIZONTAL SITUATION IND HDG FLAG IN VIEW AND SMOKE SMELL IN COCKPIT. REMOVED AND REPLACED CAPT'S HORIZONTAL SITUATION IND PER MM. 2 L 7 2 4F RT A16WE 2001103100048 20011031 00048 2001 10 31 SWAA012926 4 20011024 A 2565 FASTENER BOEING 737 7375H4 138449D NM SERVICE DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 512SW 24189 DURING SCHEDULED C2 CHECK, FOUND LOOSE FASTENER AT FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINING HOOK. SECURED G IRT BAR HOOK PER MM. 2 L 7 2 4F RT A16WE 2001103100049 20011031 00049 2001 10 31 SWAA012928 4 20011024 A 2565 FASTENER BOEING 737 7375H4 138449D NM ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 512SW 24189 DURING SCHEDULED C2 CHECK, FOUND LOOSE FASTENER AT FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINING HOOK. SECURED GIRT BAR HOOK PER MM. 2 L 7 2 4F RT A16WE 2001103100050 20011031 00050 2001 10 31 SWAA012931 4 20011024 A 2565 61621469 SLIDE BOEING 737 7375H4 138449D NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 512SW 24189 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001103100051 20011031 00051 SO 2001 10 31 SWIA200110260 1 20011023 A 3010 BOOT EMB 120 EMB120ER 3260203 SO LT WING FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 224SW 120294 LEFT WING MIDDLE AND RIGHT WING MIDDLE DEICE BOOT FAILED IN FLIGHT BOTH TIMES. RETURNED TO SLC. REMOVED AND REPLACED L EFT MIDDLE DEICE BOOT WITH NEW IAW EMB 120 MM 30 AND GOODRICH FAST BOOT INSTALLATION INSTRUCTIONS. OPS CHECK GOOD. P/N P29S-7D5135-27, S/N ON MT25530, S/N OFF MK84510. 2 L 7 2 4T RT A31SO 2001103100052 20011031 00052 EA 2001 10 31 SWIA200110261 1 20011020 A 2913 PV304448 PUMP CNDAIR CL600 CL6002B19 EA LT ENGINE LEAKING A SWIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 595SW 7292 DURING FLIGHT HYDRAULIC SYSTEM NR 1 QUANTITY DROPPED TO 0 PERCENT. PSI REMAINED AT 3000 PSI. RETURNED TO SLC. FOUND N R 1 HYDRAULIC QUANTITY AT 15 PERCENT, SERVICED IAW 12-12-29. RAN NR 1 ENGINE, NO LEAKS NOTED AT ENGINE HYDRAULIC PUMP. OPERATED NR 1 ELECTRIC HYDRAULIC PUMP, FLUID LEVEL GOOD, TEMPERATURE OK. HYDRAULIC LEAK LEFT ENGINE. REPLACED LEFT EN GINE HYDRAULIC PUMP IAW 31-00-03. OPS AND LEAK CHECKS GOOD. S/N OFF MX6066207. 2 L 7 2 4F RT A21EA 2001103100053 20011031 00053 SO 2001 10 31 SWIA200110262 1 20011021 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 196SW 120151 RIGHT WING LOWER SURFACE STRINGER NR 10 CRACKED NEAR OUTBOARD END OF FUEL CELL OPENING JUST INBOARD OF NACELLE. REPAIRE D STRINGER IAW SRM 57-20-03. 2 L 7 2 4T RT A31SO 2001103100054 20011031 00054 SO 2001 10 31 SWIA200110263 1 20011022 A 5270 SWITCH EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE PAX DOOR DIRTY A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 218SW 120287 FORWARD DOOR LIGHT ILLUMINATED ON TAKEOFF. RETURNED TO GATE. REMOVED TRASH FROM DOOR MICROSWITCH. RESET BREAKER AND R EPLACED BULBS. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001103100055 20011031 00055 SO 2001 10 31 SWIA200110264 1 20011023 A 2701 BUSHING EMB 120 EMB120ER 3260203 SO CONTROL COLUMN STIFF A SWIA K NONE F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 393SW 120330 AILERONS ARE VERY STIFF OUT OF NEUTRAL POSITION. PULLED AILERON DISCONNECT AND DETERMINED THE STIFFNESS IS COMING FROM THE F/O'S SIDE. REMOVED AND REPLACED BOTH BUSHINGS IN RIGHT AILERON CONTROL COLUMN IAW 27-11-01. RERIGGED COCKPIT LOOP IAW 27-10-01. OPS CHECK GOOD WITH NO DISCREPANCIES. 2 L 7 2 4T RT A31SO 2001103100056 20011031 00056 SO 2001 10 31 SWIA200110265 1 20011022 A 2133 2091G010800 OUTFLOW VALVE EMB 120 EMB120ER 3260203 SO CABIN PRESSURE MALFUNCTIONED A SWIA O OTHER O OTHER TO TAKEOFF 1 NM 07 218SW 1492 1492 120287 DURING TAKEOFF ROLL, CABIN PRESSURIZED UP TO 2000+ PER MIN THEN UPON POWER REDUCTION DROPPED TO -2000 RAPIDLY. REPLACED ELECTRO PNEUMATIC OUTFLOW VALVE IAW RII CARD 21-302. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001103100057 20011031 00057 SO 2001 10 31 SWIA200110266 1 20011024 A 5753 PE610261 ROLLER EMB 120 EMB120ER 3260203 SO T/E FLAP WORN A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 190SW 120050 CONTROL FAULT ON INBOARD FLAPS. FOUND CONTAMINATION IN INBOARD ACTUATOR CANNON PLUGS. ALSO FOUND WORN ROLLERS ON LEFT INBOARD FLAP. CLEANED CANNON PLUGS AND REMOVED AND REPLACED ROLLER LEFT INBOARD FLAP. REINSTALLED PANELS. OPS CHECK G OOD. ROLLER P/N: PE61026-1. 2 L 7 2 4T RT A31SO 2001103100058 20011031 00058 EA 2001 10 31 SWIA200110267 1 20011022 A 2750 7455001 CONTROL HANDLE CNDAIR CL600 CL6002B19 EA COCKPIT FAULTY A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 903SW 7425 ON TAKEOFF, FLAPS FAIL CAUTION MESSAGE APPEARED WHEN ATTEMPTING TO RETRACT FLAPS FROM 20 DEGREES TO 8 DEGREES. VISUAL I NSPECTION SHOWS FLAPS AT 20 DEGREES. COMPLIED WITH AD 98-20-01 PER AD COMPLIANCE FORM. FOUND FAULT CODE ON FLAP CONTRO L LEVER. REMOVED AND REPLACED FLAP CONTROL LEVER IAW CRJ 27-51-01. OPS CHECK GOOD. P/N ON 7-45500-1, S/N ON 0067, S/N OFF 0054. 2 L 7 2 4F RT A21EA 2001103100059 20011031 00059 EA 2001 10 31 SWIA200110268 1 20011024 A 3030 CONTROLLER CNDAIR CL600 CL6002B19 EA ANTI-ICE SYS MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 413SW 7102 RIGHT PITOT HEAT, TAT AND RIGHT AOA HEAT MESSAGES ILLUMINATED AFTER TAKEOFF. RETURNED TO SLC. INSTALLED SERVICEABLE PI TOT HEAT CONTROLLER TO RIGHT POSITION. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2001103100060 20011031 00060 SO 2001 10 31 SWIA200110269 1 20011024 A 2720 PCU EMB 120 EMB120ER 3260203 SO RUDDER MALFUNCTIONED A SWIA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CR CRUISE 1 NM 07 250YV 120250 UNCOMMANDED YAW INFLIGHT WITH FLUTTER MOTION IN TRIM AND ON RUDDER PEDALS. USED QRH PROCEDURE AND TURNED RUDDERS OFF. REMOVED AND REPLACED RUDDER POWER CONTROL UNIT PER AMM 27-22-01. SYSTEM OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001103100061 20011031 00061 SO 2001 10 31 SWIA200110270 1 20011025 A 6120 78249046 PCU EMB 120 EMB120ER 3260203 SO RT ENGINE MALFUNCTIONED A SWIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 NM 07 581SW 949 949 120349 SHORTLY AFTER TAKEOFF, NOTICED ENGINES EXTREMELY OUT OF SYNC. COULD NOT FIX PROBLEM BY CHANGING POWER. RETURNED TO LAN D. NR 2 ENGINE WAS AT 98 PERCENT WHILE NR 1 ENGINE WAS AT 100.1 PERCENT. REMOVED AND REPLACED RIGHT PCU IAW MM 61-21- 00 AND 61-20-02. 2 L 7 2 4T RT A31SO 2001103100062 20011031 00062 SO 2001 10 31 SWIA200110271 1 20011025 A 3233 1959500007 ACTUATOR EMB 120 EMB120ER 3260203 SO LT MLG FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 580SW 120348 LEFT MAIN GEAR WOULD NOT RETRACT AT ALL. RETURNED TO SEA. REMOVED AND REPLACED LEFT MAIN GEAR ACTUATOR IAW EMB 120 MM 32-32-10. OPS CHECK GOOD. S/N OFF T86691. 2 L 7 2 4T RT A31SO 2001103100063 20011031 00063 SO 2001 10 31 SWIA200110272 1 20011024 A 3350 FUSE EMB 120 EMB120ER 3260203 SO CABIN BLOWN A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 301YV 120301 EMERGENCY EXIT SIGNS AT 2A AND ON EITHER SIDE OF JUMPSEAT FAIL TO ILLUMINATE. REPLACED CENTER EMERGENCY LIGHTING BATTER Y PACK FUSE. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001103100064 20011031 00064 SO 2001 10 31 SWIA200110273 1 20011025 A 3350 BATTERY PACK EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 301YV 120301 BACKUP BATTERY/EMERGENCY LIGHTS FAILED WHEN TESTED. REPLACED FORWARD, MIDDLE EMERGENCY LIGHTING BATTERY PACKS. OPS CHE CK GOOD. 2 L 7 2 4T RT A31SO 2001103100065 20011031 00065 2001 10 31 SWIA200110274 4 20011025 A 3418 COMPUTER EMB 120 EMB120RT SO STALL WARNING FAULTY A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 1117H 120117 ON TAKEOFF ROLL SYSTEM NR 1 STALL WARNING LIGHTS ILLUMINATED. ABORTED TAKEOFF. REPLACED NR 1 STALL WARNING COMPUTER. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001103100066 20011031 00066 SO 2001 10 31 SWIA200110275 1 20011024 A 3297 CONNECTOR EMB 120 EMB120ER 3260203 SO LANDING GEAR CORRODED A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 189SW 120050 LEFT MAIN LANDING GEAR DISAGREEMENT LIGHT REMAINED ON AFTER LIFT OFF. A VISUALLY VERIFIED LEFT GEAR DOORS REMAINED OPEN . RECYCLED GEAR RECEIVED SAME INDICATION. DURING CRUISE FLIGHT DISAGREEMENT B LEFT SIDE ILLUMINATED. VISUALLY SAW RIG HT MAIN GEAR DOOR OPEN AND GEAR PARTIALLY HANGING DOWN, BUT NO DISAGREEMENT LIGHTS FOR THAT SIDE. REPLACED CONNECTOR 1J 0316 DUE TO CORROSION. ALSO CLEANED CORROSION FROM 2J0316 AND 1 & 2J0319. FOUND GEAR OPERATION NORMAL AND SENSOR ADJUS TMENT OK. 2 L 7 2 4T RT A31SO 2001103100067 20011031 00067 SO 2001 10 31 SWIA200110276 1 20011024 A 5753 FLAP TRACK EMB 120 EMB120ER 3260203 SO T/E FLAP DIRTY A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 268UE 120207 WITH FLAPS SELECTED 45 DEGREES, OUTBOARD PAIR OF FLAPS GO INTO DISAGREEMENT MODE. FLAPS GO TO 45 DEGREES BELOW 125 KTS. TROUBLESHOT WITH FLAP BREAKOUT BOX. FOUND ALL RESISTANCE READINGS TO BE WITHIN PARAMETERS. INSPECTED OUTBOARD FLAP T RACKS AND FOUND TO BE EXTREMELY SOILED. CLEANED FLAP TRACKS (OUTBOARD SIDE). 2 L 7 2 4T RT A31SO 2001103100068 20011031 00068 2001 10 31 SWIA200110277 4 20011024 A 2210 6225798013 CONTROL PANEL EMB 120 EMB120ER 3260203 SO COCKPIT FAULTY A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 268UE 891 891 120207 WITH THE AUTOPILOT SELECTED TO THE CAPTAIN OR FIRST OFFICER, THE AUTOPILOT FAILS SHORTLY AFTER BEING ENGAGED WITH AN AUT OPILOT AND TRIM FAIL AURAL WARNING. REPLACED FCP65 WITH SERVICEABLE UNIT. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001103100069 20011031 00069 EA 2001 10 31 SWIA200110278 1 20011027 A 2760 4916405 ECU CNDAIR CL600 CL6002B19 EA SPOILER MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION UK UNKNOWN 1 NM 07 903SW 7437 OUTBOARD GROUND SPOILER FAULT STATUS MESSAGE ON EICAS. INSPECTED LEFT AND RIGHT OUTBOARD SPOILERON PCU. OHMS CHECK NO RMAL. CLEARED FAULTS. GROUND CHECKS NORMAL. AS A PRECAUTION (FAULT CODE 05, 04, FF, 13) REPLACED SECU NR 1 IAW 27-61- 05. GROUND CHECK NORMAL. 2 L 7 2 4F RT A21EA 2001103100070 20011031 00070 EA 2001 10 31 SWIA200110279 1 20011027 A 2742 83963 ACTUATOR CNDAIR CL600 CL6002B19 EA HORIZ STAB FAILED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 594SW 7285 STAB TRIM AND MACH TRIM MESSAGE AFTER TAKEOFF. RE-ENGAGED BOTH SYSTEMS. BOTH SYSTEMS FAILED AGAIN. RETURNED TO SLC. REMOVED AND REPLACED HSTA WITH A SERVICEABLE UNIT IAW AMM 27-42-01. ALSO REMOVED AND REPLACED MCU WITH A SERVICEABLE UN IT IAW AMM 27-42-05. PERFORMED OPS CHECKS OF HSTCA & MCU PER MM 27-40-00. OPS CHECK GOOD. CAT II UPGRADE. HSTA S/N OFF: 951, MCU P/N: 7062-3, S/N ON: 606, S/N OFF: 468. 2 L 7 2 4F RT A21EA 2001103100071 20011031 00071 NE 2001 10 31 SWIA200110280 2 20011028 A 7200 ENGINE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RIGHT FLUCTUATES A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 582SW 120350 ON TAKEOFF ROLL RIGHT NP DID NOT REACH 100 PERCENT AND FLUCTUATED BETWEEN 96 AND 98.5 PERCENT. TAKEOFF WAS ABORTED. PE RFORMED ENGINE RUNS AND OPS CHECKED PROP SYNC. SIMULATED TAKEOFF ROLL. NO FAULTS NOTED. COULD NOT DUPLICATE ERROR. A LL ENGINE PARAMETERS NORMAL. ALSO CHECKED RIGHT ENGINE PROP SYNC CANNON PLUG (CLEANED AND OHMED). NO FAULTS. CHECKED PROP SYNC GAP. ALL CHECKS GOOD. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001103100073 20011031 00073 2001 10 31 UPS01237191 4 20011026 A 2565 SLIDE BOEING 727 72762C 138402C NM DOOR UNSECURE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 912UP 19244 INSPECTION TYPE:IN DOOR PARTIALLY OPENED FROM EXTERIOR WITH SLIDE ARMED SLIDE FELL FROM DOOR BUT DID NOT DEPLOY. RESECU RED SLIDE ASSY. 2 L 7 3 4F A3WE 2001103100074 20011031 00074 NM 2001 10 31 UPS01437149 1 20011006 A 5320 65B083535 FITTING BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C LT BS 1350 UPPER AFT BATHTUB FITTING LOWER PORTION MATING SURFACES FOUND HEAVY CORROSION AFTER FITTING REMOVAL. FX LT BS 1350 UPPER AFT BOTH LOWER FITTING REPAIRED PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001103100075 20011031 00075 NM 2001 10 31 0103755637 1 20011029 A 5347 SEAT TRACK BOEING 757 757251 1384970 NM CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 537US 26484 During "H" check found corrosion on seat track at BS 720 RBL 45. Repaired per EA 56-187026. 2 L 7 2 4F RT A2NM 2001103100076 20011031 00076 EA 2001 10 31 COMA0160859 1 20011028 A 5346 60135006 WEB CNDAIR CL600 CL6002B19 EA A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 938CA 7046 CRACK FOUND ENTERING FROM 7TH RIVET TO THE RIGHT OF BL0 ON ENGINE SUPPORT BEAM LOWER SKIN.REPAIRED I/A/W REO 53-61-345. 2 L 7 2 4F RT A21EA 2001103100077 20011031 00077 EA 2001 10 31 COMA0160860 1 20011030 A 5346 60135006 WEB CNDAIR CL600 CL6002B19 EA BEAM CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 973CA 7049 ENGINE SUPPORT BEAM LOWER WEB CRACKED. LEFT AND RIGHT SIDE AT FWD VB CORNER OF ACCESS PANEL CUTOUTS.CUT OUT DAMAGED SECT IONS OF LOWER WEB AND INSTALLED REPAIRS ON THE LEFT AND RIGHT SIDES. I/A/W REO 601R-53-61-366. 2 L 7 2 4F RT A21EA 2001103100078 20011031 00078 NM 2001 10 31 UPS01437150 1 20011008 A 5320 SPLICE BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C BS 1350 SKIN SPLICE STRAP I/B FACE AFT UPPER BATHTUB FITTING MATING SURFACE AREA FOUND CORROSION AFTER FITTING REMOVAL. FX BS 1350 LT AFT SPLICE ANGLE AT S29 TO 31L REPLACED PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001103100079 20011031 00079 NM 2001 10 31 UPS01437156 1 20011006 A 5320 FITTING BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C LT BS 1350 UPPER AFT SHEAR / BATHTUB ATTACH FITTING LWR SILL UPPER MATING SURFACE, FOUND CORROSION AFT ER FITTINGS REMOVAL. LT BS 1350 UPPER AFT SHEAR / BATHTUB ATTACH FITTING SPLICE FITTING OTHER UPPER MATING SURFACE CORR OSION CLEANED UP, REPAIRED AS PER HX RS R54-43-34687 ITEM B1. 2 L 7 4 4F A20WE 2001103100080 20011031 00080 NM 2001 10 31 UPS01437157 1 20011018 A 5320 ANGLE BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C LEFT BS 1350 FWD CHORD ANGLE I/B AND FWD MATING SURFACE FOUND CORROSION AFTER FWD UPPER BATHTUB FITTIN G REMOVAL. LEFT BS 1350 FWD CHORD ANGLE I/B AND FWD MATING UPPER CHORD CORROSION CLEANED UP AND REPAIRED AS PER HX RS R 53-43-34687 ITEM C1. 2 L 7 4 4F A20WE 2001103100081 20011031 00081 NM 2001 10 31 UPS01437158 1 20011010 A 5312 BULKHEAD BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C LEFT BS 1350 BULKHEAD WEB O/B LWR CORNER FWD FACE FOUND CORROSION AFTER UPPER FWD SHEAR AND BATHTUB FI TTING REMOVAL. LEFT BS 1350 BULKHEAD WEB O/B LOWER CORNER FWD FACE CORROSION CLEANED UP AND REPAIRED AS PER HX RS R53-4 3-34687 ITEM C2. 2 L 7 4 4F A20WE 2001103100082 20011031 00082 NM 2001 10 31 UPS01437159 1 20011006 A 5312 BULKHEAD BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C LEFT BS 1350 BULKHEAD WEB O/B LWR CORNER REAR FACE FOUND CORROSION AFTER UPPER AFT SHEAR AND BATHTUB F ITTING REMOVAL. LEFT BS 1350 BULKHEAD WEB O/B LWR CORNER REAR FACE CORROSION CLEANED UP AND REPAIRED AS PER HX RS R53-4 3-34687 ITEM B2. 2 L 7 4 4F A20WE 2001103100083 20011031 00083 NM 2001 10 31 UPS01437160 1 20011010 A 5320 SILL BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C LEFT BS 1350 UPPER FWD SHEAR BATHTUB ATTACH FITTING SILL UPPER MATING SURFACE FOUND CORROSION AFTER FI TTINGS REMOVAL. LEFT BS 1350 UPPER FWD SHEAR BATHTUB ATTACH FITTING SILL UPPER MATING CORROSION CLEANED UP AND REPAIRED AS PER HX RS R53-43-34687 ITEM C3. 2 L 7 4 4F A20WE 2001103100084 20011031 00084 NM 2001 10 31 UPS01437161 1 20011012 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C CRACK REVEALED ON SKIN AT ONE EA BOLT HOLE AT LT BS 1350 UPPER FWD FITTING AREA AT LOWER MOST AND AFT ONE BY APPROX 0.030 INCH LONG AS PER ATTACH FIGURE. CRACKED HOLE FINAL REAMED TO 0.625 INCH AND CONFIRMED CRACK FREE, A BOLT P/N: BACB30UU10K WAS INSTALLED AS PER HX RS R53-43-34687 ITEM C3 REQUIREMENT. 2 L 7 4 4F A20WE 2001103100085 20011031 00085 EA 2001 10 31 COMA0160861 1 20011028 A 5346 60135006 BEAM CNDAIR CL600 CL6002B19 EA CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 938CA 7046 CRACK FOUND EXTENDING FROM LEFT ENGINE SUPPORT BEAM LEFT ACCESS PANEL.REPAIRED I/A/W REO 53-61-366. 2 L 7 2 4F RT A21EA 2001103100086 20011031 00086 EA 2001 10 31 COMA0160862 1 20011030 A 5322 601R3114863 THRESHOLD CNDAIR CL600 CL6002B19 EA FLOOR CORRODED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 973CA 7044 L/H FLOOR SUPPORT SILL CORRODED.REMOVED THRESHOLD AND REPLACED WITH NEW PART I/A/W SRM 51-42-00 AND 51-45-00. 2 L 7 2 4F RT A21EA 2001103100087 20011031 00087 EU 2001 10 31 2001F00496 1 20010902 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 344SB 340B344 SPS - FLT 3512 - CREW REPORTED EMERGENCY LIGHTS IN CABIN ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY UNITS 20LN, 21LN, 22LN, 23LN, AND 24LN. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200124501. (M) 2 L 7 2 4T RT A52EU 2001103100088 20011031 00088 EU 2001 10 31 2001F00497 1 20010902 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 344SB 340B344 SPS - FLT 3512 - CREW REPORTED EMERGENCY LIGHTS IN CABIN ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY UNITS 20LN, 21LN, 22LN, 23LN, AND 24LN. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200124501. (M) 2 L 7 2 4T RT A52EU 2001103100089 20011031 00089 EU 2001 10 31 2001F00498 1 20010902 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 344SB 340B344 SPS - FLT 3512 - CREW REPORTED EMERGENCY LIGHTS IN CABIN ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY UNITS 20LN, 21LN, 22LN, 23LN, AND 24LN. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200124501. (M) 2 L 7 2 4T RT A52EU 2001103100090 20011031 00090 EU 2001 10 31 2001F00499 1 20010902 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 344SB 340B344 SPS - FLT 3512 - CREW REPORTED EMERGENCY LIGHTS IN CABIN ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY UNITS 20LN, 21LN, 22LN, 23LN, AND 24LN. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200124501. (M) 2 L 7 2 4T RT A52EU 2001103100091 20011031 00091 EU 2001 10 31 SIMA200122901 1 20010817 A 3350 66902 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 393AE 340B393 DFW - FLT 3507 - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTING ON LEFT EXIT AND IN FRONT OF SEAT 7A, AND 8A TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT STRIP AT SEAT 7A AND 8A IAW SAAB MM. OPERATIONAL CHECK WAS GO OD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001103100092 20011031 00092 EA 2001 10 31 COMA0160863 1 20011030 A 3350 59465 CONNECTOR CNDAIR CL600 CL6002B19 EA CABIN FLOOR LOOSE A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 987CA 7199 FLIGHT #5706 - EMERGENCY FLOOR PATH LIGHT IS INOPERABLE AT ROW 1.RECONNECTED LOOSE WIRING CONNECTION AT FLOOR LIGHT. SYS TEM CHECK SATISFACTORY. 2 L 7 2 4F RT A21EA 2001103100093 20011031 00093 EA 2001 10 31 COMA0160864 1 20011030 A 3150 6229820008 COMPUTER CNDAIR CL600 CL6002B19 EA AVIONICS MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 781CA 2136 7312 FLIGHT #5559 CONFIG AILERON WARNING, T/O ABORTED.REPLACED THE #2 DCU. 2 L 7 2 4F RT A21EA 2001103100094 20011031 00094 EA 2001 10 31 COMA0160866 1 20011030 A 3260 172825 SENSOR CNDAIR CL600 CL6002B19 EA R/H MLG LOOSE A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 947CA 7077 FLIGHT #5646 - GEAR DISAGREE WARNING, R/H MLG INDICATED UNSAFE AFTER RETRACTION.TIGHTENED LOOSE PROX SENSOR TARGET ON R/ H MLG UPLOCK 2 L 7 2 4F RT A21EA 2001103100095 20011031 00095 NM 2001 10 31 CALA0100986 1 20011030 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM STA 947 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59338 23576 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 947, BL 0 TO LBL 6. A REPAIR WAS INSTALLED IAW SRM 53-60-51. 2 L 7 2 4F RT A16WE 2001103100096 20011031 00096 NM 2001 10 31 CALA0100987 1 20011030 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM STA 294.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59338 23576 INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AROUND SEVERAL FASTENERS AT STA 294.5, LBL 35-51. A NEW CHORD SECTION WA S INSTALLED IAW SRM 53-10-51, FIGURE 205, SHEETS 1-4. 2 L 7 2 4F RT A16WE 2001103100097 20011031 00097 NM 2001 10 31 CALA0100988 1 20011030 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM STA 917-923 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59338 23576 INSPECTION FOUND CABIN L/H I/B SEAT TRACK CORRODED AT STA 917-923, LBL 15. THE SEAT TRACK WAS REMOVED AND REPLACED IAW S RM 53-00-52. 2 L 7 2 4F RT A16WE 2001103100098 20011031 00098 NM 2001 10 31 CALA0100989 1 20011030 A 5754 SKIN BOEING 737 7373T0 1384582 NM #6 SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69333 23571 INSPECTION FOUND CRACKS COMING FROM THREE RIVETS ON LOWER SIDE OF #6 SLAT SKIN BELOW I/B AUX TRACK. REPAIRED SLAT IAW SR M 57-43-01. 2 L 7 2 4F RT A16WE 2001103100099 20011031 00099 WP 2001 10 31 CALA0100990 1 20011030 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP STA 1174 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35832 49492 INSPECTION FOUND INTERCOSTAL CORRODED AT LOWER SECTION OF AFT BAGGAGE BIN DOOR CUTOUT, STA 1174. THE INTERCOSTAL WAS REM OVED AND REPLACED IAW SRM 53-01, FIGURE 1 AND 51-30-2. 2 L 7 2 4F A6WE 2001103100100 20011031 00100 EU 2001 10 31 SIMA200123001 1 20010818 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 223AT 223 MIA - FLT 5370 - CREW REPORTED BOTH BOTTOM EMERGENCY EXIT LIGHTS ON THE FRONT SIGN TO BE INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE BATTERY PACKS AT POWER SUPPLY UNITS 29WL AND 10WL. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETU RNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001103100101 20011031 00101 EU 2001 10 31 SIMA200123201 1 20010820 A 3350 AQ51000 BATTERY AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST NR NOT REPORTED 1 SW 21 270AT 270 DFW - FLT 3574 - CREW REPORTED SOME FLOOR PROXIMITY EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY IN EMERGENCY POWER SUPPLY UNIT 67WL. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001103100102 20011031 00102 EU 2001 10 31 SIMA200123301 1 20010821 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 174AE 340B174 CREW REPORTED THE EMERGENCY LIGHTS WILL NOT TEST. MAINTENANCE REMOVED AND REPLACED ALL FIVE EMERGENCY LIGHT POWER SUPPL Y UNIT IAW SAAB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001103100103 20011031 00103 NM 2001 10 31 2001F00405 1 20010823 A 3220 MS2000940 BOLT LKHEED P2V P2V7 5260112 NM WRIGHT R3350 972TC18DA1 67037 EA NLG DEFECTIVE A CILG O OTHER O OTHER DE DESCENT 1 NM 05 14447 8010 NOSE LANDING GEAR DID NOT LOCK WHEN EXTENDED. FLIGHT CREW MANUALLY LOCKED AND PINNED GEAR. NORMAL LANDING WAS THEN MAD E. POSSIBLE IMPROPER TORQUE OR FATIGUE. COMPLIANCE INSPECTED AS PER AIRCRAFT SERVICE CHANGE ASC 803. 4 M 7 4 4R 4 R RT A1RM E272 2001103100106 20011031 00106 NM 2001 10 31 P5CA0100606 1 20011031 A 5310 NONE WEB BOEING 747 747249F 1384849 NM NOSE WHEEL WELL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 NOSE GEAR WHEEL WELL FRAME WEB CRACKED, APPROX. 1/8" LONG, BY INSULATION HOLES FIRST & FOUR FROM FLOOR CHORD ANGLE ON RI GHT SIDE. OPENED HOLES TO 7/16", RE-INSPECTED BY H.F.E.C. - NO INDICATIONS. REPAIRED IAW BOEING SERVICE LETTER PAO-LGB -01-0015514, SB74752a2293 & MA #a5310-33-01. 2 L 7 4 4F A20WE 2001103100118 20011031 00118 SO 2001 10 31 RAIA00110012 1 20011021 A 5320 14522460015 GUSSET EMB 145 EMB145ER SO CORRODED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 802HK 7916 145066 MX-STL- DURING MAINTENANCE CHECK FOUND CORROSION ON FWD GUSSET AT CENTER LINE FRAME 18 BETWEEN Y AXIS 0.0 AND -.459. MAI NTENANCE REMOVED AND REPLACED FWD GUSSET AT CENTER LINE FRAME 18 Y AXIS 0.0-.459 IAW EMB145 SRM 2 L 7 2 4F RT T00011AT 2001103100124 20011031 00124 SO 2001 10 31 RAIA00110015 1 20011021 A 5320 14522461011 DOUBLER EMB 145 EMB145ER SO CORRODED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 802HK 7916 145066 MX-STL- DURING MAINTENANCE CHECK FOUND CORROSION ON FWD AND AFT DOUBLERS AT SERVICE DOOR FRAMES 20 AND 22 AT Y AXIS -.45 9. MAINTENANCE REMOVED AND REPLACED THE FWD AND AFT DOUBLERS AT SERVICE DOOR FRAMES 20 AND 22 AT Y AXIS -.459 IAW EMB 14 5 SRM 2 L 7 2 4F RT T00011AT 2001110100001 20011101 00001 EU 2001 11 1 UPS01137192 1 20011030 A 2432 2520 BATTERY AIRBUS A300 A300F4622R 3930360 EU E/E BAY DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 127UP 0812 INSPECTION TYPE: N/A AT DEPARTURE, FLT CREW REPORTED THAT THE EMERGENCY ESCAPE SLIDE WARNING LIGHT AND HORN WOULD NOT TE ST. DURING TROUBLESHOOTING FOUND THAT NR 2 SHIP BATTERY DISCHARGED WITH ONLY 1V. REMOVED AND REPLACED BATTERY. SYSTEM OPERATION CHECKED NORMAL. 2 L 7 2 4F RT A35EU 2001110100002 20011101 00002 EU 2001 11 1 UPS01137195 1 20011030 A 2432 BATTERY AIRBUS A300 A300F4622R 3930360 EU E/E BAY DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 127UP 0812 INSPECTION TYPE:IN EVACUATION SLIDE WARNING LIGHT AND BUZZER INOP, NO SLIDE ARM INDICATION ON ECAM EITHER. REMOVED AND REPLACED NR 2 MAIN SHIP BATTERY PER MM 24-31-11 SYSTEM OPS. 2 L 7 2 4F RT A35EU 2001110100003 20011101 00003 NM 2001 11 1 UPS01237193 1 20011030 A 5312 BULKHEAD BOEING 727 7272A1 138407F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE:IN FWD SIDE OF BS 1342 NR 2 ENGINE BULKHEAD IS CORRODED AT APPROX LBL TO LBL 40 AS VIEWED LOOKING AFT ST ANDING ON AIRSTAIRS JUST O/B OF NR 2 ENGINE GENERATOR FEEDER CABLES NUMEROUS FASTENERS ARE CORRODED AS IS A STIFFENER. CLEANED AND TREATED AREA AND REMOVED CORROSION PER SRM. 2 L 7 3 4F A3WE 2001110100004 20011101 00004 NM 2001 11 1 UPS01237194 1 20011029 A 3350 BATTERY BOEING 727 72727C 138400J NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 909UP 19115 INSPECTION TYPE:IN CREW ENTRANCE DOOR EMERGENCY EXIT LIGHT WENT DIM SHORTLY AFTER TESTING LIGHTS. REPLACED BATTERIES WI TH CHARGED UNITS. OPS CHECKED GOOD IAW MM 33-51-01 PG 104. P/N S106 2 L 7 3 4F A3WE 2001110100005 20011101 00005 NM 2001 11 1 UPS01437162 1 20011009 A 5320 SILL BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C LEFT BS 1350 UPPER FWD SHEAR / BATHTUB ATTACH FITTING LWR SILL O/B FLANGE FWD HOLE FOUND CORROSION AFT ER BOLT REMOVAL. LEFT BS 1350 UPPER FWD SHEAR / BATHTUB ATTACH FITTING LWR SILL O/B FLANGE FWD HOLE CORROSION CLEANED U P AFTER HOLE REAMED TO FINAL SIZE 0.812 INCH. REPAIRED CARRIED AT AS PER HX RS R53-43-34687 ITEM C3. 2 L 7 4 4F A20WE 2001110100006 20011101 00006 NM 2001 11 1 UPS01437163 1 20011006 A 5320 SILL BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C FX - LEFT BS 1350 UPPER AFT SHEAR / BATHTUB ATTACH FITTING LWR SILL O/B FLANGE FWD HOLE FOUND CORROSIO N AFTER BOLT REMOVAL. FX - LEFT BS 1350 UPPER AFT SHEAR / BATHTUB ATTACH FITTING LWR SILL O/B FLANGE FWD HOLE CORROSION CLEANED UP AFTER HOLE REAMED TO FINAL SIZE 0.812 INCH. REPAIRED CARRIED OUT AS PER HX RS R53-43-34687 ITEM C3. 2 L 7 4 4F A20WE 2001110100007 20011101 00007 NM 2001 11 1 UPS01437164 1 20011006 A 5320 SILL BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C FX - LEFT BS 1350 UPPER AFT SHEAR / BATHTUB ATTACH FITTING LWR SILL O/B FLANGE AFT HOLE FOUND CORROSIO N AFTER BOLT REMOVAL. FX - LEFT BS 1350 UPPER AFT SHEAR / BATHTUB ATTACH FITTING LWR SILL O/B FLANGE AFT HOLE CORROSION CLEANED UP AFTER HOLE REAMED TO FINAL SIZE 0.812 INCH. REPAIRED CARRIED OUT AS PER HX RS R53-43-34687 ITEM C3. 2 L 7 4 4F A20WE 2001110100008 20011101 00008 NM 2001 11 1 UPS01437165 1 20011009 A 5320 SILL BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C LEFT BS 1350 UPPER FWD SHEAR / BATHTUB ATTACH FITTING LWR SILL O/B SILL O/B FLANGE AFT HOLE FOUND CORR OSION AFTER BOLT REMOVAL. LEFT BS 1350 UPPER FWD SHEAR / BATHTUB ATTACH FITTING LWR SILL O/B SILL O/B FLANGE AFT HOLE C ORROSION CLEANED UP AFTER HOLE REAMED TO FINAL SIZE 0.812 INCH. REPAIRED CARRIED OUT AS PER HX RS R53-43-34687 ITEM C3. 2 L 7 4 4F A20WE 2001110100009 20011101 00009 NM 2001 11 1 UPS01437167 1 20011009 A 5320 65B079795 FITTING BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C LEFT BS 1350 FWD BATHTUB FITTING CORROSION FOUND AT BOTTOM AREA. FWD UPPER BATHTUB FITTING REPLACED A S PER HX RS 53-43-34687, SRM 51-10-01. 2 L 7 4 4F A20WE 2001110100010 20011101 00010 NM 2001 11 1 UPS01437168 1 20011008 A 5320 SPLICE BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C BS 1350 SKIN SPLICE STRAP I/B FACE AFT UPPER BATHTUB FITTING MATING SURFACE AREA FOUND CORROSION AFTER FITTING REMOVAL. BS 1350 SKIN SPLICE STRAP I/B FACE AFT UPPER BATHTUB FITTING MATING SURFACE AREA CORROSION CLEANED UP AND REPAIRED AS PER HX RS R53-43-34687 ITEM B2 WITH 1EA SPLICE STRAP AT BS 1350 S29 - S31 AREA REPLACED AS PER SRM 51-1 0-01. 2 L 7 4 4F A20WE 2001110100011 20011101 00011 NM 2001 11 1 UPS01437169 1 20011009 A 5320 FITTING BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C BS 1350 UPPER AFT SHEAR / BATHTUB FITTING ATTACH BOLT HOLE, ONE EACH HOLE FOUND CRACK AT STRAP INNER S URFACE 8 O'CLOCK POSITION VIEW LOOKING O/B, .125 INCH APPROX. REFER ATTACHED DRAWING FOR LOCATION. FASTENER HOLE CRACK CLEARED AFTER REAMED TO 0.500 INCH, HOLE FINAL OVERSIZED TO 0.562 INCH AND INSTALLED WITH FREEZE PLUG AS THE REPAIR REQ UIREMENT OF HX RS R53-43-34687 ITEM B3. 2 L 7 4 4F A20WE 2001110100012 20011101 00012 NM 2001 11 1 UPS01437170 1 20011010 A 5320 SILL BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C LEFT BS 1350 ATTACH FITTING LWR SILL CTR BOLT HOLE BORE COMMON TO FWD UPPER BATHTUB FITTING BASE HOLE FOUND CORROSION AFTER BOLT REMOVAL. LEFT BS 1350 ATTACH FITTING LWR SILL CTR BOLT HOLE BORE COMMON TO FWD UPPER BATHTU B FITTING BASE HOLE REAMED 1.343 INCH AND CONFIRM CORROSION CLEANED UP, HOLE FINALLY OVERSIZED TO 1.375 INCH AND BOLT P/ N BACB30US22K86, INSTALLED TOGETHER WITH TAPE FILLER AND ALIGNMENT WASHER SA PER HX RS R53-43-34687 ITEM C3 REQUIREMENT. 2 L 7 4 4F A20WE 2001110100013 20011101 00013 WP 2001 11 1 ABXA010562 1 20010605 A 5300 37502571 FITTING DOUG DC8 DC863 302198A WP STA. 450 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 LONGERON SPLICE FITTING AT STATION 450, LONGERON 31 LEFT WAS CRACKED. REPLACED SPLICE FITTING IAW DAC DWG 3750257 AND DC -8 SRM 51-1-8. 2 L 7 4 4F 4A25 2001110100014 20011101 00014 WP 2001 11 1 ABXA010564 1 20010605 A 5340 57738454 SKIN DOUG DC8 DC863 302198A WP VERT. STAB. CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 CORROSION ON EXTERNAL SKIN OF THE VERTICAL STABILIZER, JUST ABOVE THE FUSELAGE TO VERTICAL ATTACHING ANGLE REPAIR DOUBLE R. REPAIRED AREA AND INSTALLED NEW SKIN IAW DC-8 SRM 55-2-0, 51-1-21, 51-3-0, 51-1-22, 51-9-0, 51-1-26, 51-1-20D, 51-1-1 5, 51-1-16, AND DC-8 DWG 5773845. 2 L 7 4 4F 4A25 2001110100015 20011101 00015 NM 2001 11 1 UPS01437171 1 20010909 A 5320 65B083593 FITTING BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C LEFT SIDE BS 1350 BULKHEAD SHEAR FITTING AFT SIDE CRACK FOUND AT THE LOCATION OF VERTICAL FLANGE O/B A REA THE CRACK THRU TWO BOLT HOLES 3.5 INCH LENGTH. LEFT BS 1350 BULKHEAD AFT UPPER CRACKED SHEAR FITTING WAS REPLACED A S PER BOEING SB 747-53-2213 INCLUDING FIG 3, 4, 8, 9 & 12. ALSO DURING FITTING REPLACEMENT ADJACANT STRUCTURE FOUND COR ROSION AND SKIN CRACK. 2 L 7 4 4F A20WE 2001110100016 20011101 00016 NM 2001 11 1 UPS01437172 1 20010909 A 5320 65B112723 FITTING BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C LEFT SIDE BS 1350 BULKHEAD SHEAR FITTING ONE BOLT HOLE FOUND CRACK AT THE LOCATION FWD SIDE OF THE VER TICAL FLANGE 2 O'CLOCK POSITION VIEW LOOKING AFT .125 INCH APPROX. LEFT BS 1350 BULKHEAD FWD UPPER CRACKED SHEAR FITTIN G WAS REPLACED AS PER BOEING SB 747-53-2213 INCLUDING FIG 3, 6, 10, 11 AND 12. ALSO DURING FITTING REPLACEMENT, ADJACEN T STRUCTURE FOUND CORROSION AND SKIN HOLE CRACK. 2 L 7 4 4F A20WE 2001110100017 20011101 00017 NM 2001 11 1 UPS01437173 1 20011010 A 5320 SPLICE BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C BS 1350 SKIN SPLICE STRAP I/B FACE FWD UPPER BATHTUB FITTING MATING SURFACE AREA FOUND CORROSION AFTER FITTING REMOVAL. BS 1350 SKIN SPLICE STRAP I/B FACE FWD UPPER BATHTUB FITTING MATING SURFACE AREA CORROSION CLEANED UP AND REPAIRED AS PER HX RS R 53-43-34687 ITEM C2. 2 L 7 4 4F A20WE 2001110100018 20011101 00018 WP 2001 11 1 UPS01837110 1 20011005 A 5511 RIB DOUG DC8 DC873F 302199F WP HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 RIGHT HORIZONTAL STAB LOWER RIB IS CRACKED AT XFS 135. REPAIRED RIB IAW SRM 55-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001110100019 20011101 00019 WP 2001 11 1 UPS01837134 1 20011004 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 LEFT WING L/E UPPER RIB IS CRACKED AT XOLDI 6.225. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001110100020 20011101 00020 WP 2001 11 1 UPS01837135 1 20011005 A 5510 37014271N FITTING DOUG DC8 DC873F 302199F WP HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 LEFT HORIZONTAL STAB LOWER FLANGE FITTING AT FRONT SPAR IS CRACKED AT XFS 47. REMOVED AND REPLACED FITTING IAW DWG 3701427 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001110100021 20011101 00021 WP 2001 11 1 UPS01837136 1 20011003 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 578.75, XFS 585. REPAIRED RIBS IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001110100022 20011101 00022 WP 2001 11 1 UPS01837137 1 20011003 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 628.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001110100023 20011101 00023 WP 2001 11 1 UPS01837138 1 20011003 A 5320 SPLICE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 STA 210 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754220, AND SRM 5 1-1-20D. 2 L 7 4 4F RT 4A25 2001110100024 20011101 00024 WP 2001 11 1 UPS01837139 1 20011003 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 RIGHT WING L/E LOWER RIBS ARE CRACKED AT XFS 822.5, XFS 828.75, XFS 835. REPAIRED RIBS IAW SRM 57-2 -0 FIG 2. 2 L 7 4 4F RT 4A25 2001110100025 20011101 00025 WP 2001 11 1 UPS01837140 1 20011004 A 5720 57701707 ANGLE DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 LEFT WING L/E UPPER RIB ANGLE IS CRACKED AT XS 472.099. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 5770170, AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001110100026 20011101 00026 WP 2001 11 1 UPS01837141 1 20011006 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 STA 55 RT SIDE FRAME IS CRACKED ABOVE FITTING AT CUSP. REPAIRED FRAME IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001110100027 20011101 00027 WP 2001 11 1 UPS01837142 1 20011015 A 5320 559764677 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 FWD ENTRY DOOR AFT TORQUE BOX HAS A CRACKED INTERCOSTAL STA 60-70 BETWEEN LONG 14L-15L. REMOVED AND REPLACED INTERCOSTAL IAW DWG 5597646, AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001110100028 20011101 00028 WP 2001 11 1 UPS01837143 1 20011005 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 SEAT TRACK IS CORRODED BEYOND LIMITS STA 1130-1150 AT LBL 60. REPAIRED SEAT TRACK IAW SRM 53-2-3 FI G 8A, AND DC8-53B-003-501. 2 L 7 4 4F RT 4A25 2001110100029 20011101 00029 WP 2001 11 1 UPS01837144 1 20011006 A 5330 577991641 FINGER DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 STA 70-120 LONG 31R FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED DOU BLER IAW DWG 5779916, AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001110100030 20011101 00030 WP 2001 11 1 UPS01837145 1 20011012 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 STA 1240 FRAME IS CORRODED BEYOND LIMITS LONG 35R-36. REPAIRED FRAME IAW 8110-3 APPROVED DH SK 836- 901, BY INSTALLING A REPAIR STRAP IAW DH SK 836-901. 2 L 7 4 4F RT 4A25 2001110100031 20011101 00031 WP 2001 11 1 UPS01837146 1 20011005 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 STA 12 FRAME AND WEB ARE CORRODED BEYOND LIMITS AT RBL 48. REPAIRED FRAME BY INSTALLING FILLER AND ANGLE DOUBLER IAW 8110-3 APPROVED DH SK 836-869, AND REPAIRED WEB IAW SR08530026. 2 L 7 4 4F RT 4A25 2001110100032 20011101 00032 WP 2001 11 1 UPS01837147 1 20011005 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 SEAT TRACK STA 1400-1540 RBL 60 IS CORRODED BEYOND LIMITS. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 1 4. 2 L 7 4 4F RT 4A25 2001110100033 20011101 00033 WP 2001 11 1 UPS01837148 1 20011005 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 SEAT TRACK STA 1020-1040 RBL 60 IS CORRODED BEYOND LIMITS. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8 A. 2 L 7 4 4F RT 4A25 2001110100034 20011101 00034 WP 2001 11 1 UPS01837152 1 20011020 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 STA 1520 LBL 55 SEAT TRACK IS CRACKED. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 14. 2 L 7 4 4F RT 4A25 2001110100035 20011101 00035 WP 2001 11 1 UPS01837155 1 20011003 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C23 R-2 DOOR UPPER AFT CORNER OF OPENING SKIN, INTERNAL DOUBLER, AND LONGERON 11R ARE CRACKED AT STA 165 4. REPAIRED SKIN AND INTERNAL DOUBLER, AND LONGERON IAW 8110-3 APPROVED DH SK 936-267, AND DC8-5330-15557-A. 2 L 7 4 4F RT 4A25 2001110100036 20011101 00036 WP 2001 11 1 UPS01837179 1 20011016 A 5320 4611067N FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 STA 70 LONG 27R END FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 4611067, AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001110100037 20011101 00037 WP 2001 11 1 UPS01837180 1 20011015 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 RIGHT WING T/E UPPER RIB IS CRACKED AT XW 5. REMOVED FASTENERS, STOP DRILLED CRACK, NDT VERIFIED STO P DRILL TERMINATED CRACK, FABRICATED AND INSTALLED DOUBLERS IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001110100038 20011101 00038 WP 2001 11 1 UPS01837181 1 20011017 A 5540 565507423 WEB DOUG DC8 DC871F 302199D WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 LOWER RUDDER MEMBRANE IS CRACKED BETWEEN ZR 54.2 AND ZR 61.156, VERTICAL MEMBRANE APPROX 12 INCHES AF T AF L/E. REMOVED, FABRICATED, AND REPLACED WEB/MEMBRANE IAW DWG 5655074, AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001110100039 20011101 00039 WP 2001 11 1 UPS01837182 1 20011017 A 5511 RIB DOUG DC8 DC871F 302199D WP HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 LEFT HORIZONTAL STAB L/E RIB IS CRACKED AT XFS 91.25. REMOVED FASTENERS, STOP DRILLED CRACK, NDT VER IFIED STOP DRILL TERMINATED CRACK, FABRICATED AND INSTALLED DOUBLERS IAW SRM 55-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001110100040 20011101 00040 WP 2001 11 1 UPS01837183 1 20011017 A 5511 RIB DOUG DC8 DC871F 302199D WP HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 LT HORIZONTAL STAB L/E LOWER RIB IS CRACKED AT XFS 116.25. REMOVED FASTENERS, STOP DRILLED CRACK, ND T VERIFIED STOP DRILL TERMINATED CRACK, FABRICATED AND INSTALLED DOUBLERS IAW SRM 55-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2001110100041 20011101 00041 WP 2001 11 1 UPS01837185 1 20011026 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:IN EMERGENCY LIGHTS NOT ILLUMINATING. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW MM 33-50-01, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2001110100042 20011101 00042 WP 2001 11 1 UPS01837196 1 20011017 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 STA 940 LONG 24L IS CRACKED. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATED CRACK, FABRICATE D, AND INSTALLED DOUBLERS IAW SRM 53-2-0 FIG 5. 2 L 7 4 4F RT 4A25 2001110100043 20011101 00043 WP 2001 11 1 UPS01837197 1 20011018 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 R-2 DOOR UPPER AFT CORNER HAS CRACKED SKIN, INTERNAL DOUBLER AND LONGERON 11R. TRIMMED CRACKED SKIN AND INTERNAL DOUBLER, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND STRAP IAW 8110-3 APPROVED SH SK 718-455, DC8-5330-1 5612-A, AND SRM 53-2-0 FIG 16. 2 L 7 4 4F RT 4A25 2001110100044 20011101 00044 WP 2001 11 1 UPS01837198 1 20011017 A 5313 4772397U1 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 STA 1770 LONG 17R LONGERON AND END FITTING ARE CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397 , AND SRM 51-1-21, 51-1-20D, AND REMOVED, FABRICATED, AND REPLACED LONGERON IAW DWG S-1616757, AND SRM 51-1-20D, 51-1-21 . 2 L 7 4 4F RT 4A25 2001110100045 20011101 00045 WP 2001 11 1 UPS01837199 1 20011017 A 5320 97540242 SUPPORT DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 STA 1220 LONG 27R FLOORBEAM SUPPORT IS CRACKED AT LOWER END. REMOVED AND REPLACED SUPPORT IAW DWG 97 54024, AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001110100046 20011101 00046 WP 2001 11 1 UPS01837200 1 20011018 A 5510 SE085500093 FITTING DOUG DC8 DC871F 302199D WP HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 LT HORIZONTAL STAB L/E LOWER FITTING IS CRACKED AT O/B END BETWEEN XFS 47.5 TO XFS 60. REMOVED AND R EPLACED FITTING IAW DWG SE08550009, AND SRM 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 2001110100047 20011101 00047 2001 11 1 UPS01M37186 4 20011019 A 2565 BATTERY DOUG MD11 MD11F 3023600 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 250UP INSPECTION TYPE:IN REF M 224780 LT ESCAPE SLIDE BOTTLE LOW LIGHT WILL NOT TEST. REMOVED AND REPLACED BATTERIES FOR LOW PRESS TEST LIGHT IAW 25-61-01, CHECKS GOOD. 2 L 7 3 4F RT A22WE 2001110100048 20011101 00048 2001 11 1 UPS01M37187 4 20011014 A 2565 LIGHT DOUG MD11 MD11F 3023600 NM CABIN WILL NOT TEST A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 250UP INSPECTION TYPE:IN LT ESCAPE SLIDE LOW PRESS WARNING LIGHT INOP WILL NOT TEST. 2 L 7 3 4F RT A22WE 2001110100049 20011101 00049 2001 11 1 UPS01M37188 4 20011021 A 2565 SLIDE DOUG MD11 MD11F 3023600 NM CABIN WILL NOT TEST A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 250UP INSPECTION TYPE:IN M224780 LOW PRESSURE LIGHT WILL NOT TEST. REPLACED SLIDE/RAFT ASSY PER MM 25-61-01. OPS CHECKS NORM AL. 2 L 7 3 4F RT A22WE 2001110100050 20011101 00050 NM 2001 11 1 01FDEA00936 1 20011030 A 5230 FRAME BOEING 727 727233 138408A NM DOORS CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 282FE 22349 N 202 #2 LOWER CARGO DOOR EDGE HAS IMPACT DAMAGED & CRACKED. R&R FRAME PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2001110100051 20011101 00051 NM 2001 11 1 01FDEA00937 1 20011030 A 5340 BRACKET BOEING 727 727233 138408A NM FUSELAGE TOP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 282FE 22349 N 126 #3 ENGINE START CABLE SUPPORT BRACKET CRACKED. R&R BRACKET PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2001110100052 20011101 00052 NM 2001 11 1 01FDEA00938 1 20011030 A 5230 52FX153613 RETAINER BOEING 727 727233 138408A NM FUSELAGE TOP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 282FE 22349 N 724 MAIN CARGO DOOR PRESSURE SEAL RETAINER CRACKED AT LWR AFT CORNER OF DOOR. ** S/D ** COMING 2 L 7 3 4F RT A3WE 2001110100053 20011101 00053 NM 2001 11 1 01FDEA00940 1 20011031 A 2710 ARH7057515 ACTUATOR DOUG MD11 MD11F 3023600 NM FAILED A FDEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 25 605FE 48514 01-356 ON T/O UPON FLAP RETRACTION RECEIVED LEVEL 2 DEFLECTED AILERON DISAGREE ALERT. ** S/D ** COMING 2 L 7 3 4F RT A22WE 2001110100054 20011101 00054 NM 2001 11 1 VNAA0110015 1 20011023 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 432JS 11938 3045 THE CREW REPORTED THE EMERGENCY LIGHTING AT ROWS 7 THROUGH 9 WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED T HE EMERGENCY BATTERY AT THE 6LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WER E PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001110100055 20011101 00055 EU 2001 11 1 XN0A01028 1 20011025 A 3260 MODULE AIRBUS 300 A300B4203 3930306 EU LANDING GEAR FAILED A XN0A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 473AS 203 LANDING GEAR FAILED TO SELECT UP SYS 1 OR 2. LANDING PERFORMED AT 300 FT PER MINUTE. FOUND FAILED PROXIMITY MODULE UNI T. REMOVED AND REPLACED PROXIMITY DETECTOR MODULE UNIT IAW MM 32-61-12. OPS CHECK AND TEST NORMAL IAW 32-61-00. 2 L 7 2 4F RT A35EU 2001110900061 20011109 00061 NM 2001 11 9 P2EA2001V0009 1 20010310 A 5230 SKIN BOEING 737 737230 1384401 NM CARGO DOOR DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 124NJ 22122 ON LEADING EDGE OF AFT CARGO DOOR SKIN APPROXIMATELY 18 INCHES FROM LOWER EDGE WITH BOEING TEMPORARY REPAIR PER VAG-MCI- 01-0002H DUE DENT OUT LIMITS. INSTALLED PERMANENT REPAIR PER SRM 52-00-3 FIG 5 AT AFT CARGO DOOR EXTERNAL SKIN FROM BS 796 TO BS 800.5 BETWEEN BEAM 1 AND 3. 2 L 7 2 4F RT A16WE 2001110900064 20011109 00064 NM 2001 11 9 P2EA2001V0011 1 20011018 A 5753 654643089 SKIN BOEING 737 737230 1384401 NM T/E FLAP WORN A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 124NJ 22122 DURING C-CHECK, FOUND THE LEFT WING T/E FORE FLAP P/N 65-46430-89, S/N BN 436 UPPER SKIN WORN. LT WING I/B FORE FLAP RE PAIRED FROM WBL 74.5 TO WBL 79.5 IAW SRM 51-40-20 REPAIR 21 FIG 30. 2 L 7 2 4F RT A16WE 2001110100064 20011101 00064 2001 11 1 0103726628 4 20011021 A 2330 PROJECTOR BOEING 747 747251B 1384892 NM E-ZONE MELTED A NWAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 01 628US 22389 APPROXIMATELY 1.5 HOURS OUT OF SFO, FLIGHT ATTENDANT REPORTED BURNING ODOR FROM REAR LAV AREA. ODOR CONFIRMED BY FLIGHT CREW AND AIRCRAFT RETURNED TO SFO AND LANDED WITHOUT INCIDENT. FOUND E-ZONE PROJECTOR MELTED INSIDE. REPLACED THE PRO JECTOR. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F A20WE 2001110100065 20011101 00065 NM 2001 11 1 HNAA0100072 1 20011023 A 5300 8530686101 THRESHOLD DHAV DHC8 DHC8201 2809001 NM CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 988HA 14359 426 AIRSTAIR DOOR THRESHOLD PLATE CORRODED ON TOP SURFACE UNDER PLASTIC STRIP. REPLACED THRESHOLD PLATE. 2 H 7 2 4T RT A13NM 2001110100066 20011101 00066 NM 2001 11 1 HNAA010074 1 20011025 A 5300 85321069S101 BRACKET DHAV DHC8 DHC8201 2809001 NM CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 988HA 14359 426 AIRSTAIR DOOR THRESHOLD CENTER LOWER SUPPORT ANGLE BRACKET AT STATION X240.5 IS CRACKED. REPLACED BRACKET. 2 H 7 2 4T RT A13NM 2001110100072 20011101 00072 2001 11 1 2001F00502 4 20010606 A 3416 150201182 ALTIMETER SNIAS 350 AS350B3 8680954 EU COCKPIT INOPERATIVE A R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 392LG 558 3252 ALTIMETER IS INOPERATIVE. READS 100 FEET TO 150 FEET LOW. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 1 3U H9EU 2001110100073 20011101 00073 2001 11 1 2001F00503 4 20010806 A 3414 250201162 INDICATOR SNIAS 350 AS350B3 8680954 EU COCKPIT STICKS A R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 52285 791 3251 AIRSPEED INDICATOR STICKS AT 40 KNOTS. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M) 1 G 7 1 3U H9EU 2001110100074 20011101 00074 EU 2001 11 1 2001F00504 1 20010726 A 3030 PR6123 ELEMENT BOLKMS BK117 BK117C1 5626025 EU PITOT HEAT FAILED A R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 117SU 499 7527 PITOT HEAT INOPERATIVE. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M) 1 G 7 2 3U NC H13EU 2001110100075 20011101 00075 EU 2001 11 1 2001F00506 1 20010829 A 6320 4638001001 TRANSMISSION BOLKMS 105 BO105CBS 5626008 EU MAIN ROTOR MAKING METAL A R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 105LC 522 S789 MAIN ROTOR TRANSMISSION MAKING METAL. TWO PRIOR PROBLEMS WITH MM WERE REPAIRED UNDER WARRANTY BY ECL. REPLACED WITH NE W UNIT CORRECTED PROBLEM. (M) 1 G 7 2 3U NC H3EU 2001110100076 20011101 00076 EU 2001 11 1 2001F00512 1 20010424 A 6410 704A33633116 BEARING SNIAS 350 AS350B3 8680954 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 392LG 477 3252 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM 1 KIT P/N 355A09-1036-1 CORRECTED PROBLEM. FO UR HALF SHELLS EQUALS 1 KIT. (M) 1 G 7 1 3U H9EU 2001110100077 20011101 00077 EU 2001 11 1 2001F00513 1 20010521 A 6410 704A33633116 BEARING SNIAS 350 AS350B3 8680954 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 52281 266 3249 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM 1 EACH KIT P/N 355A09-1036-01 CORRECTED PROBLE M. FOUR HALF SHELLS EQUALS 1 KIT. (M) 1 G 7 1 3U H9EU 2001110100078 20011101 00078 EU 2001 11 1 2001F00514 1 20010726 A 6410 704A33633116 BEARING SNIAS 350 AS350B3 8680954 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 104LN 549 3134 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM 1 EACH KIT P/N 355A09-1036-01 CORRECTED PROBLE M. FOUR HALF SHELLS EQUALS 1 KIT. (M) 1 G 7 1 3U H9EU 2001110100079 20011101 00079 EU 2001 11 1 2001F00515 1 20010321 A 6410 704A33633116 BEARING SNIAS 350 AS350B2 8680813 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 852HW 295 2630 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM 1 EACH KIT P/N 355A09-1036-01 CORRECTED PROBLE M. FOUR HALF SHELLS EQUALS 1 KIT. (M) 1 G 7 1 3U H9EU 2001110100080 20011101 00080 EU 2001 11 1 2001F00516 1 20010109 A 6410 704A33633116 BEARING SNIAS 350 AS350B 8680801 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 3593X 327 1081 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM 1 KIT PART NR 355A09-1036-01 CORRECTED PROBLEM . FOUR HALF SHELLS EQUALS 1 KIT. (M) 1 G 7 1 3U H9EU 2001110100081 20011101 00081 EU 2001 11 1 2001F00517 1 20010703 A 6410 704A33633171 BEARING SNIAS 350 AS350* EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 30LG 361 5065 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM 1 EACH KIT PART NR 355A33-2153-00 CORRECTED PR OBLEM. 2 TEETERING BEARINGS EQUALS 1 KIT. (M) 1 G 7 1 3U H9EU 2001110100082 20011101 00082 EU 2001 11 1 2001F00518 1 20010529 A 6410 704A3363317 BEARING SNIAS 350 AS350B3 8680954 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 52281 710 3249 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM 1 KIT P/N 355A33-2153-00 CORRECTED PROBLEM. 2 TEETERING BEARINGS EQUALS 1 KIT. (M) 1 G 7 1 3U H9EU 2001110100083 20011101 00083 EU 2001 11 1 2001F00519 1 20010430 A 6410 704A33633171 BEARING SNIAS 350 AS350B2 8680813 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 96LG 467 2817 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM 1 EACH KIT P/N 355A33-2153-00 CORRECTED PROBLE M. 2 TEETERING BEARINGS EQUALS 1 KIT. (M) 1 G 7 1 3U H9EU 2001110100084 20011101 00084 EU 2001 11 1 2001F00520 1 20010817 A 6410 704A33633171 BEARING SNIAS 350 AS350B2 8680813 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 94LG 731 2728 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM 1 EACH KIT PART NR 355A33-2153-00 CORRECTED PR OBLEM. 2 TEETERING BEARINGS EQUAL 1 KIT. (M) 1 G 7 1 3U H9EU 2001110100085 20011101 00085 EU 2001 11 1 2001F00521 1 20010424 A 6220 117775P BALL JOINT SNIAS 350 AS350B3 8680954 EU MAIN ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 392LG 3252 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M) 1 G 7 1 3U H9EU 2001110100086 20011101 00086 EU 2001 11 1 2001F00522 1 20010513 A 6220 117775P BALL JOINT SNIAS 350 AS350B3 8680954 EU MAIN ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 103LN 501 3128 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M) 1 G 7 1 3U H9EU 2001110100087 20011101 00087 EU 2001 11 1 2001F00523 1 20010501 A 6220 117775P BALL JOINT SNIAS 350 AS350B2 8680813 EU MAIN ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 96LG 467 2817 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M) 1 G 7 1 3U H9EU 2001110100088 20011101 00088 EU 2001 11 1 2001F00524 1 20010109 A 6220 117775P BALL JOINT SNIAS 350 AS350B 8680801 EU MAIN ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 01 3593X 465 1081 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M) 1 G 7 1 3U H9EU 2001110100089 20011101 00089 NE 2001 11 1 2001F00525 2 20010623 A 7230 COMPRESSOR SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE ENGINE SEIZED A R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 52285 3251 22036 COMPRESSOR SEIZED. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M) 1 G 7 1 3U 3 U H9EU E00054EN 2001110100090 20011101 00090 EU 2001 11 1 2001F00531 1 20010829 A 3340 6485000 LIGHT UROCOP EC135 EC135P1 8680990 EU ANTI-COLLISION INOPERATIVE A R7MA K NONE L NO TEST IN INSP/MAINT 1 NM 07 427AE 10 EC1350162 ANIT-COLLISION LIGHT INOPERATIVE. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M) 1 G 7 2 3U O H88EU 2001110100091 20011101 00091 EU 2001 11 1 2001F00532 1 20010718 A 3340 6485000 LIGHT UROCOP EC135 EC135P1 8680990 EU ANTI-COLLISION INOPERATIVE A R7MA K NONE L NO TEST IN INSP/MAINT 1 NM 07 426AE 47 EC1350159 ANTI-COLLISION LIGHT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 2 3U O H88EU 2001110100092 20011101 00092 EU 2001 11 1 2001F00540 1 20010621 A 2150 5AS35034 COMPRESSOR SNIAS 350 AS350D 8680803 EU AIR CONDITIONING SEIZED A R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 350RM 10 1024 AIR CONDITIONING COMPRESSOR SEIZED. CLUTCH SLIPPAGE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 1 3U H9EU 2001110100093 20011101 00093 EU 2001 11 1 2001F00541 1 20010615 A 2150 5AS35034 CLUTCH SNIAS 350 AS350D 8680803 EU AIR CONDITIONING FAILED A R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 350RM 9 1024 AIR CONDITIONING COMPRESSOR CLUTCH FAILURE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 1 3U H9EU 2001110100094 20011101 00094 EU 2001 11 1 2001F00542 1 20010608 A 2150 5AS35034 COMPRESSOR SNIAS 350 AS350D 8680803 EU AIR CONDITIONING SEIZED A R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 350RM 280 1024 AIR CONDITIONING COMPRESSOR SEIZED CAUSING DRIVE BELT FAILURE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 1 3U H9EU 2001110100095 20011101 00095 SW 2001 11 1 2001F00543 1 20010616 A 3340 099799100 LIGHT BELL 407 407 1182206 SW EXTERIOR INOPERATIVE A R7MA K NONE L NO TEST IN INSP/MAINT 1 NM 07 911LN 115 53446 SEARCH LIGHT ASSEMBLY INOPERATIVE. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M) 1 G 7 1 3U O H2SW 2001110100096 20011101 00096 SW 2001 11 1 2001F00552 1 20010828 A 6510 407340339103 BEARING BELL 407 407 1182206 SW TAIL ROTOR WORN A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 405AL 22 53480 FOUND DURING DAILY, BLACK GREASE EMANATING FROM BEARING. (M) 1 G 7 1 3U O H2SW 2001110100097 20011101 00097 SW 2001 11 1 2001F00553 1 20010828 A 6510 407340339103 BEARING BELL 407 407 1182206 SW TAIL ROTOR WORN A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 405AL 22 53480 DURING DAILY, BLACK GREASE EMANATING FROM BEARING. (M) 1 G 7 1 3U O H2SW 2001110100098 20011101 00098 SW 2001 11 1 2001F00556 1 20010828 A 6510 407340339103 BEARING BELL 407 407 1182206 SW TAIL ROTOR ROUGH A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 567AL 56 53246 DAILY INSPECTION, ROUGH BEARING AND EMITTING BLACK GREASE. (M) 1 G 7 1 3U O H2SW 2001110100099 20011101 00099 SW 2001 11 1 2001F00557 1 20010828 A 6510 407340339103 BEARING BELL 407 407 1182206 SW TAIL ROTOR ROUGH A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 567AL 56 53246 DAILY INSPECTION, FOUND ROUGH BEARING AND EMITTING BLACK GREASE. (M) 1 G 7 1 3U O H2SW 2001110100100 20011101 00100 SW 2001 11 1 2001F00559 1 20010903 A 6510 407340339101 BEARING BELL 407 407 1182206 SW TAIL ROTOR WORN B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 607AL 358 53264 DURING DAILY, HIGH VIBE AND TEMP AT FORWARD BEARING, GREY GREASE. (M) 1 G 7 1 3U O H2SW 2001110100101 20011101 00101 SW 2001 11 1 2001F00560 1 20010903 A 6510 407340339103 BEARING BELL 407 407 1182206 SW TAIL ROTOR WORN B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 467AL 532 53190 DURING DAILY, HIGH TEMP AND VIBE FROM 103 BEARINGS, GREY GREASE. (M) 1 G 7 1 3U O H2SW 2001110100102 20011101 00102 SW 2001 11 1 2001F00561 1 20010830 A 6510 407340339101 BEARING BELL 407 407 1182206 SW TAIL ROTOR WORN A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 403AL 47 53478 DURING DAILY, GREY/BLACK GREASE EMANATING FROM BEARING. (M) 1 G 7 1 3U O H2SW 2001110100103 20011101 00103 SW 2001 11 1 2001F00563 1 20010830 A 6510 407340339101 BEARING BELL 407 407 1182206 SW TAIL ROTOR WORN A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 403AL 47 53478 DURING DAILY, GREY/BLACK GREASE EMANATING FROM BEARING. (M) 1 G 7 1 3U O H2SW 2001110100104 20011101 00104 SW 2001 11 1 2001F00564 1 20010828 A 6510 407340339103 BEARING BELL 407 407 1182206 SW TAIL ROTOR WORN A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 405AL 22 53480 DURING DAILY, BLACK GREASE EMANATING FROM BEARING. (M) 1 G 7 1 3U O H2SW 2001110100105 20011101 00105 GL 2001 11 1 2001F00565 2 20010811 A 7200 ENGINE BOLKMS 105 BO105CBS 5626008 EU ALLSN 250C 250C20B 03013 GL NR 1 FLAMED OUT A ALGA O OTHER X ENGINE FLAMEOUT IN INSP/MAINT 1 SW 03 493HL S809 DURING POWER ASSURANCE CHECK, AT 1000 FEET AGL NR 1 ENGINE WAS PULLED OFFLINE. JUST POWER TO IDLE DETENT. NR 1 ENGINE FLAMED OUT. ATTEMPTED AIR START, ENGINE WOULD NOT START. AIRCRAFT WAS LANDED SINGLE ENGINE. AFTER THE LANDING, THE E NGINE WAS STARTED WITH NO PROBLEM. (M) 1 G 7 2 3U 3 U NC H3EU E4CE 2001110100106 20011101 00106 EU 2001 11 1 SIMA200123302 1 20010821 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 358RZ 340B358 SAN - FLT 3214 - CREW REPORTED THE OVERHEAD EMERGENCY LIGHTS AT SEATS 7A AND 8BC, AND THE FLOOR PROXIMITY AT ROWS 6, AND 7 TO BE INOPERATIVE. AIRCRAFT WAS FERRIED TO LAW WHERE POWER SUPPLY UNITS 24LN AND 23LN WERE REMOVED AND REPLACED IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001110100107 20011101 00107 EU 2001 11 1 SIMA200123304 1 20010821 A 3397 WIRE AEROSP ATR42 ATR42300 8680920 EU CABIN BROKEN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 233RM 235 MIA - FLT 5223 - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHT AT SEAT 12 TO BE INOPERATIVE. LIGHT PUT ON MEL AT TH IS TIME. MAINTENANCE REPAIRED A BROKEN WIRE AND TERMINAL AT ROW 12 FLOOR PROXIMITY EMERGENCY LIGHT. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001110100108 20011101 00108 EU 2001 11 1 SIMA200123305 1 20010821 A 3350 LP1670 LIGHT AEROSP ATR72 ATR72212 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 410AT 410 DFW - FLT 3826 - CREW REPORTED THE FLOOR PROXIMITY LIGHTS AT ROWS 1 AND 3 TO BE INOPERATIVE. MAINTENANCE REPLACED THE B ULBS, OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001110100109 20011101 00109 EU 2001 11 1 SIMA200123429 1 20010822 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 550LL 550 DFW - FOUND SEVERAL FLOOR PROXIMITY LIGHTS AND EXIT SIGN LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AT POWER SUPPLY UNIT 43WL IAW ATR MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001110100110 20011101 00110 EU 2001 11 1 SIMA200123501 1 20010823 A 3350 66902 LIGHT SAAB SF340 340B 7860101 EU CABIN LOOSE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 374AE 340B374 LAX - MAINTENANCE REPORTED THE EMERGENCY LIGHT STRIP ON THE RIGHT SIDE IS LOOSE. MAINTENANCE REPLACED THE LIGHT STRIP F ROM SEAT 3A TO SEAT 8A IAW SAAB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001110200001 20011102 00001 SO 2001 11 2 C2XA01IA389 1 20011031 A 3350 BS2197 BATTERY EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16731 120190 IAH- DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHTS IN THE BACK OF THE CABIN FAILED TO ILLUMINATE. IAH- MAIN TENANCE REMOVED AMD REPLACED THE EMERGENCY LIGHT AFT BATTERY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SY STEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001110200002 20011102 00002 EU 2001 11 2 SIMA200123502 1 20010823 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 540AM 540 MAINTENANCE REPORTED SEVERAL FLOOR PROXIMITY EMERGENCY LIGHT TO BE INOPERATIVE IN THE AFT CABIN. MAINTENANCE REMOVED AN D REPLACED THE BATTERY PACK IN POWER SUPPLY UNIT 62WL IAW ATR MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVI CE. (M) 2 H 7 2 4T RT A53EU 2001110200003 20011102 00003 EU 2001 11 2 SIMA200123601 1 20010824 A 3350 1397 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 309AE 340B309 ROC - FLT 5013 - CREW REPORTED THE EMERGENCY LIGHTS ABOVE SEAT 12BC TO BE INOPERATIVE. MAINTENANCE REPLACED THE BULB AT SEAT 12BC. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001110200004 20011102 00004 EU 2001 11 2 SIMA200123701 1 20010825 A 3350 LH6151 SOCKET AEROSP ATR42 ATR42300 8680920 EU CABIN BROKEN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 233RM 235 MCO - MAINTENANCE REPORTED THE FLOOR PROXIMITY LIGHT AT SEAT 12AB TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED T HE LIGHT SOCKET AT SEAT 12 AB IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001110200005 20011102 00005 EU 2001 11 2 SIMA200123801 1 20010826 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 548AT 548 DFW - FLT 3892 - CREW REPORTED SEVERAL FORWARD CABIN EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED AND REPLACE D THE BATTERY PACK IN POWER SUPPLY UNIT 43WL. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001110200006 20011102 00006 EU 2001 11 2 SIMA200123802 1 20010826 A 3350 LIGHT AEROSP ATR42 ATR42300 8680920 EU CABIN LOOSE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 233RM 235 MIA - FLT 5255 - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHT AT ROW 3AB TO BE INOPERATIVE. MAINTENANCE FOUND THE BULB LOOSE IN SOCKET. BULB WAS RESECURED AND OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001110200007 20011102 00007 EU 2001 11 2 SIMA200123901 1 20010827 A 3350 192411A FUSE SAAB SF340 340B 7860101 EU CABIN BLOWN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 905AE 340B319 DFW - FLT 3543 - CREW REPORTED THE EMERGENCY LIGHT ABOVE SEAT 7A TO BE INOPERATIVE. MAINTENANCE REPLACED FUSE 72LN IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001110200008 20011102 00008 EU 2001 11 2 SIMA200124001 1 20010828 A 3350 192411A FUSE SAAB SF340 340B 7860101 EU CABIN BLOWN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 905AE 340B319 DFW - FLT 3474 - CREW REPORTED THE OVERHEAD EMERGENCY LIGHTS AT SEATS 8BC AND 10BC ARE INOPERATIVE. MAINTENANCE REPLACE D FUSE 72 LN. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001110200009 20011102 00009 EU 2001 11 2 SIMA200124002 1 20010828 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN MALFUNCTIONED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 347SB 340B347 BOS - FLT 4899 - CREW REPORTED THE FLOOR PROXIMITY LIGHT AT ROW 10 TO BE INOPERATIVE. PUT ON MEL AT THIS TIME. MAINTEN ANCE COULD NOT DUPLICATE DISCREPANCY. OPS CHECK AS GOOD IAW SAAB MM AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001110200010 20011102 00010 EU 2001 11 2 SIMA200124501 1 20010902 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 344SB 340B344 SPS - FLT 3512 - CREW REPORTED EMERGENCY LIGHTS IN CABIN ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY UNITS 20LN, 21LN, 22LN, 23LN, AND 24LN. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001110200011 20011102 00011 EU 2001 11 2 SIMA200124502 1 20010902 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN INCORRECT A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 238AE 340B238 BOS - FLT 4915 - FLOOR PROXIMITY EMERGENCY LIGHTING WAS INOPERATIVE AT ROW 14 AND WAS ISSUED MEL. FOUND INCORRECT BULB WAS INSTALLED BY MAINTENANCE. BULB WAS REMOVED AND REPLACED WITH CORRECT BULB P/N 3071PEGL. (M) 2 L 7 2 4T RT A52EU 2002052900146 20020529 00146 EU 2002 5 29 SIMA200124601 1 20010903 A 3350 LIGHT AEROSP ATR72 ATR72212A 8680902 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 550LL 550 DFW - FLT 3656 - EMERGENCY FLOOR LIGHTING AT SEAT 6A INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT LAMP AT SEAT 6A. OPERATIONALLY CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 2001110200012 20011102 00012 EU 2001 11 2 SIMA200124801 1 20010905 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 345SB 340B345 SYR - FLT 5062 - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHT AT SEAT 7BC TO BE INOPERATIVE. LIGHT PUT ON MEL AT T HIS TIME. (M) 2 L 7 2 4T RT A52EU 2001110200013 20011102 00013 EU 2001 11 2 SIMA200124903 1 20010906 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN MALFUNCTIONED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 358RZ 340B358 SAN - FLT 3360 - EMERGENCY FLOOR PROXIMITY LIGHTING AT SEATS 6, 7, AND 8 EXTINGUISHES AFTER 15 SECONDS. MAINTENANCE PER FORMED OPS TEST OF THE EMERGENCY LIGHTING SYSTEM PER SAAB 340 AMM. PROBLEM COULD NOT BE DUPLICATED. (M) 2 L 7 2 4T RT A52EU 2001110200014 20011102 00014 EU 2001 11 2 SIMA200126003 1 20010917 A 3397 CONNECTOR AEROSP ATR42 ATR42300 8680920 EU CABIN LOOSE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 282AT 282 MIA - FLT 5245 - CREW REPORTED THE EMERGENCY LIGHT OVER FORWARD DOOR TO BE INOPERATIVE. MAINTENANCE FOUND THE CANNON PL UG TO BE LOOSE. CANNON PLUG WAS RESECURED AND OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001110200015 20011102 00015 EU 2001 11 2 SIMA200126004 1 20010917 A 7712 10225N01W00 GAUGE SAAB SF340 340B 7860101 EU COCKPIT FAULTY A SIMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 21 387AE 340B387 DFW - FLT 3685 - LEFT ENGINE TORQUE WENT TO ZERO ON TAKEOFF. LEFT TORQUE CIRCUIT BREAKER POPPED. ABORTED TAKEOFF. REM OVED AND REPLACED LEFT TORQUE GAUGE. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001110200016 20011102 00016 2001 11 2 SIMA200126005 4 20010917 A 3416 INDICATOR SAAB SF340 340B 7860101 EU COCKPIT MALFUNCTIONED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 349SB 340B349 CAPTAINS ALTITUDE INDICATOR HAD A RED FLAG ON TAKEOFF ROLL. ABORTED TAKEOFF. MAINTENANCE COULD NOT DUPLICATE DISCREPAN CY. PERFORMED OPS CHECK IAW SAAB AMM ON THE ADC OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2001110200017 20011102 00017 EU 2001 11 2 SIMA200126101 1 20010918 A 3350 LIGHT AEROSP ATR72 ATR72212A 8680902 EU CABIN MALFUNCTIONED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 499AT 499 DFW - FLT 3695 - CREW REPORTED SEVERAL EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001110200018 20011102 00018 EU 2001 11 2 SIMA200126102 1 20010918 A 3350 9HB00593312 SIGN SAAB SF340 340B 7860101 EU CABIN BROKEN A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 231LN 340B231 FLT 5002 - BOS - FOUND EMERGENCY EXIT SIGN ABOVE SEAT 8A BROKEN. MAINTENANCE REMOVED AND REPLACED EXIT SIGN OVER SEAT 8 A. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001110200019 20011102 00019 EU 2001 11 2 SIMA200126103 1 20010918 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU E/E BAY DIRTY A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 329AE 340B329 LAX - FLT 3269 - CREW REPORTED THE AVIONICS SMOKE LIGHT CAME ON DURING TAKEOFF. TAKEOFF WAS ABORTED AND AIRCRAFT WAS RE TURNED TO GATE. MAINTENANCE CLEANED THE AVIONICS SMOKE DETECTOR. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVI CE. (M) 2 L 7 2 4T RT A52EU 2001110200020 20011102 00020 2001 11 2 0103795522 4 20011022 A 2565 D31041139 SLIDE BOEING 757 757251 1384970 NM EXIT DOOR 3L RUPTURED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 522US 13029 13029 23616 DURING SLIDE SHOP TEST, INFLATABLE SUB ASSEMBLY SEAM RUPTURED AT NORMAL OPERATING PRESSURE. NEW INFLATABLE SUB ASSEMBLY WAS INSTALLED. 2 L 7 2 4F RT A2NM 2001110200021 20011102 00021 SO 2001 11 2 2001F00484 1 20010831 A 2731 6225734002 SERVO EMB 120 EMB120 3260201 SO ELEVATOR BINDING A ASOA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 11 275AS 120234 FLT 4810 - FLT FROM DFW-TUL, THE A/C WAS HARD TO CONTROL. WHEN THE A/P WAS DISCONNECTED, ELEVATOR AND RUDDER WERE HEAVY AS IF THEY WERE STILL CONNECTED TO THE A/P. PULLED THE A/P CIRCUIT BREAKERS, DID NOT FIX PROBLEM. DECLARED EMERGENCY AND A/C LANDED IN TUL W/O INCIDENT. INSP A/C FLT CONTROLS SYSTEMS, FLT CONTROL SURFACES, AND CABLE BELLCRANKS AND FOUND NO DEFECTS. FOUND ELEV TRIM SERVO MOTOR BINDING. REMOVED AND REPLACED ELEVATOR TRIM SERVO MOTOR (P/N 6225734002). RECONNECT ED ELEVATOR TRIM CABLES AND TENSIONED. OPERATIONAL CHECK GOOD. AFTER TEST FLT, PILOT REPORTED THAT WITH YAW DAMPER ENGAG ED, RUDDER PEDALS WOULD NOT MOVE. MAINTENANCE FOUND RUDDER SERVO MOUNT DEFECTIVE. REMOVED AND REPLACED THE RUDDER SERVO 2 L 7 2 4T RT A31SO 2001110200022 20011102 00022 NM 2001 11 2 SCNA01357 1 20011018 A 5322 SEAT TRACK BOEING 727 727225 1384077 NM BS344-380 RBL 54 CORRODED A SCNA O OTHER O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE INSPECTION SEAT TRACK AT BS 344 TO 380 RBL 54 WAS FOUND CORRODED OUT OF LIMITS. REMOVED CORROSI ON IAW B727 SRM 511006. REMOVED SEAT TRACK IAW B727 SRM 513002. FABRICATED NEW SEAT TRACK PER SAMPLE FROM BAC 1520792. T REATED AND PRIMED IAW B727 SRM 511002 & MM 512002. INSTALLED IAW B727 SRM 513002. 2 L 7 3 4F A3WE 2001110200023 20011102 00023 SO 2001 11 2 2001F00485 1 20010831 A 2720 6225735004 MOUNT EMB 120 EMB120 3260201 SO RUDDER SERVO DEFECTIVE A ASOA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 11 275AS 120234 FLT 4810 - FLT FROM DFW-TUL, THE A/C WAS HARD TO CONTROL. WHEN THE A/P WAS DISCONNECTED, ELEVATOR AND RUDDER WERE HEAVY AS IF THEY WERE STILL CONNECTED TO THE A/P. CREW PULLED THE A/P CIRCUIT BREAKERS, BUT DID NOT FIX THE PROBLEM. DECLARED AN EMERGENCY AND A/C LANDED IN TUL W/O INCIDENT. WHILE INSP THE A/P SYS, FOUND ELEVATOR TRIM SERVO MOTOR BINDING. REMOVE D AND REPLACED THE ELEVATOR TRIM SERVO (P/N 6225734002). OPS CHECK GOOD. AFTER TEST FLT, PILOT REPORTED WITH YAW DAMPER ENGAGED, RUDDER PEDALS WOULD NOT MOVE. UPON INSP, FOUND RUDDER SERVO MOUNT DEFECTIVE. MAINTENANCE REMOVED AND REPLACED THE RUDDER SERVO MOUNT (P/N 6225735004) OPS CHECKS GOOD. (M) 2 L 7 2 4T RT A31SO 2001110200024 20011102 00024 NM 2001 11 2 2001F00486 1 20010628 A 2612 0881031007 SWITCH BOEING 737 737* NM COCKPIT FAILED A P7UR O OTHER O OTHER NR NOT REPORTED 1 EA 17 A6MRM 32450 TWO SWITCHES SHORTED INTERNALLY SHOULD, RETURN TO N/O CONDITION. LOOKED LIKE MICROSWITCH FAILED INTERNALLY IN ASSY. RE MOVED AND REPLACED SWITCHES, RETESTED NO MALFUNCTION OR DEFECTS NOTED. FIRE BELL CUTOUT SWITCHES OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A16WE 2001110200025 20011102 00025 NM 2001 11 2 2001F00500 1 20010827 A 2612 0881031007 SWITCH BOEING 737 737* NM COCKPIT FAILED B P7UR O OTHER O OTHER NR NOT REPORTED 1 EA 17 374BJ 32451 SWITCH ASSEMBLY SHORTED INTERNAL CONDITION SHOWS SYSTEM AURAL WARNING BEING RESET WITHOUT DEPRESSING SWITCH. INTERNAL F AILURE OF MICROSWITCH ASSY. REMOVED AND REPLACED SWITCH ASSEMBLY, SYSTEM OPS CHECKS GOOD. (M) 2 L 7 2 4F RT A16WE 2001110200026 20011102 00026 NE 2001 11 2 2001F00501 2 20010820 A 7200 ENGINE CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE ENGINE FAILED A FRKA O OTHER Y ENGINE STOPPAGE DE DESCENT 1 NE 01 245CC 5500212 71131 APPARENT CATASTROPHIC FAILURE OF ENGINE WHILE ON DESCENT TO LAND RESULTING IN ENGINE SHUTDOWN. (M) 1 L 7 2 4F 4 F A22CE E1NE 2001110200027 20011102 00027 CE 2001 11 2 2001F00582 1 20010818 A 5711 1181000219 SPAR CAP BEECH 1900 1900D 1154162 CE LT WING CORRODED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 860CA UE134 DURING FUEL TANK INSPECTION, FOUND CORROSION ON LEFT AND RIGHT WING LOWER SPAR CAP AT WING STATION 124.25 WAS NOTED. (M ) 2 L 7 2 4T RT A24CE 2001110200028 20011102 00028 CE 2001 11 2 2001F00583 1 20010615 A 5711 1181000219 SPAR CAP BEECH 1900 1900D 1154162 CE RT WING CORRODED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 861CA UE164 DURING FUEL TANK INSPECTION, CORROSION ON LEFT AND RIGHT WING LOWER SPAR CAP AT WING STATION 124.5 WAS NOTED. (M) 2 L 7 2 4T RT A24CE 2001110200029 20011102 00029 CE 2001 11 2 2001F00584 1 20010711 A 5711 1181000219 SPAR CAP BEECH 1900 1900D 1154162 CE LT WING CORRODED B JJBR K NONE O OTHER IN INSP/MAINT 1 EA 01 84703 14960 UE52 DURING FUEL TANK INSPECTION, CORROSION ON LEFT AND RIGHT WING SPAR CAP AT WING STATION 124.25 AS NOTED. (M) 2 L 7 2 4T RT A24CE 2001110200030 20011102 00030 CE 2001 11 2 2001F00585 1 20010727 A 5711 1181000219 SPAR CAP BEECH 1900 1900D 1154162 CE RT WING CORRODED B JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 83206 16484 UE22 DURING FUEL TANK INSPECTION, FOUND CORROSION ON LEFT AND RIGHT WING LOWER SPAR CAP AT WING STATION 124.25 WAS NOTED. (M ) 2 L 7 2 4T RT A24CE 2001110200031 20011102 00031 CE 2001 11 2 2001F00586 1 20010927 A 3230 504501025 TORQUE TUBE CESSNA 310 310R 2074245 CE LT MLG CRACKED A AJPA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 GL 11 1914G 310R0059 AIRCRAFT YAW, UNABLE TO AFFECT NORMAL ACCELERATION, COCKPIT INDICATION NORMAL. SUSPECT LEFT MAIN GEAR DID NOT RETRACT. CYCLED GEAR DOWN, 3 GREEN LIGHTS. NORMAL LANDING. NO AD'S, SB'S STC'S PMA'S APPLICABLE. NO SUGGESTION EXCEPT INCREAS ED MAINTENANCE VIGILANCE ON HIGH TIME, HIGH FREQUENCY USE. (M) 1 L 7 2 3O 3A10 2001110200032 20011102 00032 NM 2001 11 2 2001F00587 1 20010921 A 2612 65249203 DETECTOR BOEING 727 727225 1384077 NM E/E BAY FAULTY A RYNA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 07 8878Z 21451 WHEEL WELL FIRE WARNING LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. COMPLIED WITH EMERGENCY CHECKLIST AND EMERGENCY WAS DE CLARED. AIRCRAFT RETURNED TO DAYTON AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE FIRE DETECTOR BOX AND BOTH M AIN WHEEL WELL FIRE LOOPS IAW B-727 MM 26-12-11 AND 26-12-01. COMPLIED WITH OPERATIONAL CHECKS IAW B727 MM 26-12-00. ( M) 2 L 7 3 4F A3WE 2001110200033 20011102 00033 NM 2001 11 2 SWAA012932 1 20011026 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 501SW 24178 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 23L. REPAIRED SKIN PE R SRM. 2 L 7 2 4F RT A16WE 2001110200034 20011102 00034 NM 2001 11 2 SWAA012935 1 20011026 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 780SW 27885 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVER LOOSE AT ROW 11. R&R EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2001110200035 20011102 00035 NM 2001 11 2 SWAA012937 1 20011027 A 5310 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 382SW 26588 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE FRAME CORRODED AT BS 747, BETWEEN STR 26R & 27R. REPAIRED SHEAR TIE FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001110200036 20011102 00036 NM 2001 11 2 SWAA012939 1 20011026 A 5330 6545866 SKIN BOEING 737 7373H4 1384600 NM MLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED C4 CHECK, FOUND KEEL BEAM SKIN CRACKED 2 INCHES BETWEEN MLG W/W CUT OUTS RH SIDE. REPAIRED SKIN PER SWA T1-153-009. 2 L 7 2 4F RT A16WE 2001110200037 20011102 00037 NM 2001 11 2 SWAA012940 1 20011026 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, ABOVE STR 11L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001110200038 20011102 00038 NM 2001 11 2 SWAA012941 1 20011026 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED 2 INCHES AT BS 727E + 12, STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001110200039 20011102 00039 NM 2001 11 2 SWAA012946 1 20011028 A 5320 6517582 WEB BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED SPECIAL VISIT, FOUND BS 182 VERTICAL WEB CRACKED, LBL 5.7, WL 175. REPAIRED WEB PER SWA ACO. 2 L 7 2 4F A16WE 2001110200040 20011102 00040 NM 2001 11 2 SWAA012947 1 20011027 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 313SW 23335 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXT SKIN CRACKED, BS 500D, STRINGER 15L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001110200041 20011102 00041 NM 2001 11 2 SWAA012949 1 20011028 A 3350 101073 LENS BOEING 737 7373Q8 1384670 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED C4 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2001110200042 20011102 00042 NM 2001 11 2 SWAA012953 1 20011029 A 5312 6516300 WEB BOEING 737 7373H4 1384600 NM ACFT NOSE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 382SW 26588 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED, LBL 5, WL 201. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001110200043 20011102 00043 NM 2001 11 2 SWAA012955 1 20011029 A 5240 6969854 FRAME BOEING 737 7373H4 1384600 NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 382SW 26588 DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR AFT LOWER FRAME CRACKED. REPAIRED FRAME PER BAC DRAWING. 2 L 7 2 4F RT A16WE 2001110200044 20011102 00044 NM 2001 11 2 SWAA012960 1 20011019 A 5310 6545857 STRAP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 324SW 23414 DURING SCHEDULED 1/2D CHECK, FOUND AFT SERVICE DOOR LOWER FWD CUT OUT BEAR STRAP CRACKED. REPAIRED STRA P ASSY PER SWA RA. 2 L 7 2 4F RT A16WE 2001110200045 20011102 00045 NM 2001 11 2 SWAA012962 1 20011030 A 3350 81000 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 641SW 27714 FOUND EEPLS WIRE COVER MISSING. INSTALLED EEPLS WIRE COVER. 2 L 7 2 4F RT A16WE 2001110200046 20011102 00046 NM 2001 11 2 SWAA012963 1 20011027 A 5310 6516300 WEB BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SPECIAL VISIT, FOUND VERTICAL WEB CRACKED AT BS 182, LBL 17.1, WL 175. REPAIRED WE B PER SWA RA. 2 L 7 2 4F A16WE 2001110200047 20011102 00047 NM 2001 11 2 SWAA012965 1 20011030 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED 1/4D CHECK, FOUND FRAME CRACKED AT BS 360, BELOW STR 14R. REPAIR ED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001110200048 20011102 00048 NM 2001 11 2 SWAA012966 1 20011025 A 5310 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED 1/4D CHECK, FOUND FRAME CRACKED AT BS 360, ABOVE STR 14R. REPAIRED FRA ME PER SRM. 2 L 7 2 4F RT A16WE 2001110200049 20011102 00049 NM 2001 11 2 SWAA012967 1 20011030 A 5310 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 313SW 23335 DURING SCHEDULED C2 CHECK, FOUND 2 INCH FUSELAGE SKIN CRACK AT BS 927, STR 21L. REPAIRED SKIN PER S RM. 2 L 7 2 4F RT A16WE 2001110200050 20011102 00050 NM 2001 11 2 SWAA012968 1 20011030 A 5310 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 313SW 23335 DURING SCHEDULED C2 CHECK, FOUND 1 INCH FUSELAGE SKIN CRACK AT BS 500B, STR 10R. REPAIRED SKIN PER SR M. 2 L 7 2 4F RT A16WE 2001110200051 20011102 00051 NM 2001 11 2 SWAA012969 1 20011029 A 5310 6545409 WEB BOEING 737 7373H4 1384600 NM RH MLG W/W. CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 324SW 23414 DURING SCHEDULED 1/2D CHECK, FOUND WEB IN RH MLG W/W CEILING CRACKED AT BS 675, RBL 35. REPAIRED WEB PER SWA TI. 2 L 7 2 4F RT A16WE 2001110200052 20011102 00052 NM 2001 11 2 SWAA012970 1 20011029 A 5310 5889358 POST BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 324SW 23414 DURING SCHEDULED 1/2D CHECK, FOUND F/O'S UPPER WINDOW POST CRACKED. REPAIRED F/O'S WINDOW POST PER SRM. 2 L 7 2 4F RT A16WE 2001110200053 20011102 00053 NM 2001 11 2 SWAA012971 1 20011029 A 5312 6516300 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 382SW 26588 DURING SCHEDULED 1/4D CHECK, FOUND WEB CRACKED AT BS 178, RBL 5, WL 201. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001110200054 20011102 00054 NM 2001 11 2 SWAA012973 1 20011030 A 3350 8100022601 COVER BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 650SW 27720 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS BROKEN AT ROWS 14, 16 & 17. R&R EEPLS COVERS P ER MM. 2 L 7 2 4F RT A16WE 2001110200055 20011102 00055 NM 2001 11 2 SWAA012976 1 20011030 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 080SW 22675 DURING WALKAROUND INSP, FOUND 2 INCH FUSELAGE SKIN CRACK AT BS 727A+13, BETWEEN STR'S 21L & 22L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001110200056 20011102 00056 NM 2001 11 2 SWAA012978 1 20011031 A 5753 6546434 FLAP BOEING 737 7373H4 1384600 NM RH WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 616SW 27699 DURING RON, FOUND RH T/E INBD AFT FLAP DELAMINATED. R&R FLAP PE R MM. 2 L 7 2 4F RT A16WE 2001110200057 20011102 00057 2001 11 2 SWAA012980 4 20011031 A 2565 63551101 SLIDE BOEING 737 7377H4 1384404 NM AFT SVC DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 766SW 29806 AFT SVC DOOR EMERGENCY EVAC SLIDE DEPLOYED INADVERTENTLY. R& R SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001110200058 20011102 00058 NM 2001 11 2 SWAA012983 1 20011026 A 5310 65C27314 CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED 1/4D CHECK, FOUND SEVERAL TIE CLIPS CRACKED AT BS 616. R&R TIE CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001110200059 20011102 00059 NM 2001 11 2 SWAA012984 1 20011026 A 5313 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED 1/4D CHECK, FOUND STR 4L SPLICE CRACKED AT BS 908. R&R S PLICE PER SRM. 2 L 7 2 4F RT A16WE 2001110200060 20011102 00060 NM 2001 11 2 SWAA012985 1 20011029 A 5311 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 15L. R&R SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2001110200061 20011102 00061 NM 2001 11 2 SWAA012986 1 20011026 A 5313 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED 1/4D CHECK, FOUND STR SPLICE CRACKED AT BS 908, STR 4L. R&R STR S PLICE PER SRM. 2 L 7 2 4F RT A16WE 2001110200062 20011102 00062 NM 2001 11 2 SWAA012987 1 20011026 A 5342 6573790 ANGLE BOEING 737 7373H4 1384600 NM VERT STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL STAB AFT RH ATTACH FITTING FWD DRAG ANGLE CRACKED. REPAIRED DRAG ANGLE PER SRM. 2 L 7 2 4F RT A16WE 2001110200063 20011102 00063 NM 2001 11 2 SWAA012989 1 20011031 A 5330 589357 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 382SW 26588 DURING SCHEDULED 1/4D CHECK, FOUND 1.5 INCH CRACK AT CAPT'S FWD UPPER WINDOW POST. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001110200064 20011102 00064 2001 11 2 SWAA012990 4 20011026 A 2565 6945735 BRACKET BOEING 737 7373H4 1384600 NM AFT SVC DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 383SW 26589 DURING SCHEDULED 1/4D CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE COVER BRACKET BROKEN. R&R BRACKET PER SRM. 2 L 7 2 4F RT A16WE 2001110200065 20011102 00065 NM 2001 11 2 SWAA012991 1 20011031 A 5312 6516300 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 398SW 27692 DURING SPECIAL VISIT, FOUND WEB CRACKS AT BS 178, WL 213, RBL 5 & LBL 5. REPA IRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001110200066 20011102 00066 NM 2001 11 2 SWAA012993 1 20011030 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 790SW 30604 DURING SCHEDULED BC3 CHECK, FOUND EEPLS HAD 4 TRACK COVERS CRACKED. R&R COVERS PER MM. 2 L 7 2 4F RT A16WE 2001110200067 20011102 00067 NM 2001 11 2 2001F00588 1 20010921 A 2612 356644400 FIRE LOOP BOEING 727 727225 1384077 NM MLG WW FAILED A RYNA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 07 8878Z 21451 WHEEL WELL FIRE WARNING LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. COMPLIED WITH EMERGENCY CHECKLIST AND EMERGENCY WAS DE CLARED. AIRCRAFT RETURNED TO DAYTON AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE FIRE DETECTOR BOX AND BOTH M AIN WHEEL WELL FIRE LOOPS IAW B-727 MM 26-12-11 AND 26-12-01. COMPLIED WITH OPERATIONAL CHECKS IAW B727 MM 26-12-00. ( M) 2 L 7 3 4F A3WE 2001110200068 20011102 00068 EU 2001 11 2 2001F00589 1 20010929 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY MALFUNCTIONED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SW 21 347SB 340B347 JFK - FLT 5116 - CARGO SMOKE INDICATION ON FINAL APPROACH EMERGENCY DECLARED AND CARGO EXTINGUISHER NR 1 ACTIVATED. REP LACED BOTH FORWARD AND AFT CARGO COMP SMOKE DETECTORS IAW SAAB AMM. OPERATIONAL CHECKS GOOD. REF SIMA200127201. (M) 2 L 7 2 4T RT A52EU 2001110200070 20011102 00070 EU 2001 11 2 2001F00590 1 20010930 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 904AE 340B314 ALL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REMOVED AND REPLACED ALL POWER SUPPLIES IAW SAAB 340AMM. OPS CHECKE D GOOD. REF SIMA200127302. (M) 2 L 7 2 4T RT A52EU 2001110200071 20011102 00071 EU 2001 11 2 2001F00591 1 20010930 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 904AE 340B314 ALL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REMOVED AND REPLACED ALL POWER SUPPLIES IAW SAAB 340AMM. OPS CHECKE D GOOD. REF SIMA200127302. (M) 2 L 7 2 4T RT A52EU 2001110200072 20011102 00072 EU 2001 11 2 2001F00592 1 20010930 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 904AE 340B314 ALL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REMOVED AND REPLACED ALL POWER SUPPLIES IAW SAAB 340AMM. OPS CHECKE D GOOD. REF SIMA200127302. (M) 2 L 7 2 4T RT A52EU 2001110200073 20011102 00073 EU 2001 11 2 2001F00593 1 20010930 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 904AE 340B314 ALL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REMOVED AND REPLACED ALL POWER SUPPLIES IAW SAAB 340AMM. OPS CHECKE D GOOD. REF SIMA200127302. (M) 2 L 7 2 4T RT A52EU 2001110200074 20011102 00074 WP 2001 11 2 2001F00594 1 20011002 A 3040 1634896102 WINDSHIELD LKHEED 1011 10113851 5265010 WP COCKPIT SHORTED A AMTA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 186AT 193C1074 DURING CRUISE, SMOKE AND FUMES IN THE COCKPIT. NOTICED RIGHT HIGH VOLTAGE POST AND LEADS ON CO-PILOTS WINDOW SMOKING. PULLED C/B 2B12, 14, 15, 16, 19, 10 AND 21. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED F/O'S WINDSHIELD REF MM 56-1 0-01. (M) 2 L 7 3 4F A23WE 2001110200075 20011102 00075 NE 2001 11 2 SABA011058 2 20011031 A 7200 3039242 SENSOR DHAV DHC8 DHC8103 1386005 NM PWA 120 PW120 NE SHORTED A SABA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 33 801WP 086 121401 Aircraft 801 on flight 5025 from Charlotte to Tallahassee; after take-off the pilot reported a full knob split on the po wer levers with number two engine lagging behind. Aircraft returned to Charlotte and landed with no other problems. No e mergency was declared. Maintenance removed and replaced the NH and NP probes. Aircraft was ground run and opa checked go od. Aircraft was returned to service. 2 H 7 2 4T 4 T RT A13NM E20NE 2001110200076 20011102 00076 SO 2001 11 2 C2XA01BT175 1 20011031 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO INTERIOR FAULTY A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 13979 145181 EWR---CO4130, "FLOOR EMERGENCY LIGHT WILL NOT COME ON, AND TOP EMERGENCY SIGN." MAINTENANCE REMOVED AND REPLACED EMERG ENCY LIGHT DC/AC INVERTER IAW EMB145 AMM #33-50-11. OPS.CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2001110200077 20011102 00077 EU 2001 11 2 2001F00595 1 20010928 A 3234 102697001 SELECTOR VALVE STBROS SD3 SD360 8100606 EU LANDING GEAR LACK OF LUBE A PIVA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 13 711MP SH3698 MAIN LANDING GEAR INDICATORS STAYED GREEN ON GEAR UP SELECTION, ACCOMPLISHED NORMAL AND ABNORMAL CHECKLIST. THE PROBLEM PERSISTED. FLIGHT RETURNED TO HOME BASE. NO OTHER DIFFICULTIES OCCURRED THROUGHOUT THE FLIGHT. FURTHER INSPECTION FO UND 3 WAY SELECTOR VALVE ASSY NOT SEATED PROPERLY. LUBED SELECTOR LEVER, CYCLED SEVERAL TIMES AND PERFORMED LANDING GEA R EXTENSION/RETRACTION SEVERAL TIMES IAW SHORTS MM. OPERATIONAL CHECK VERY GOOD. AIRCRAFT RELEASED FOR SERVICE WITH NO FURTHER TROUBLE. (M) 2 H 7 2 4T A41EU 2001110200078 20011102 00078 WP 2001 11 2 2001F00596 1 20010503 A 5320 BRACKET DOUG DC9 DC982 3022082 WP CARGO BAY DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 MID LOWER CARGO COMPARTMENT AFT LATCH FITTING SUPPORT BRACKET CLIP DAMAGE. INSTALLED BRACKET IAW SRM MD 80 51-10-2. (M) 2 L 7 2 4F A6WE 2001110200079 20011102 00079 EU 2001 11 2 2001F00507 1 20010719 A 7712 117940691 TORQUEMETER BOLKMS 117 BK117A3 5626015 EU COCKPIT ERRATIC A R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 424MB 7082 TORQUEMETER INDICATOR INOPERATIVE. NR 1 NEEDLE JUMPS ERRATICALLY. RECEIVED NEW WITH A3 AND A4 CONVERSION KIT. THIS UN IT IS BRAND NEW MANUFACTURE, NOT OVERHAULED OR REPAIRED. REPLACED WITH REPAIRED UNIT CORRECTED PROBLEM. (M) 1 G 7 2 3U H13EU 2001110200080 20011102 00080 NE 2001 11 2 2001F00508 2 20010309 A 7261 350A54113800 VENT LINE SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE OIL SYS CRACKED A R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 52281 599 3249 AIR VENT OIL TUBE CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M) 1 G 7 1 3U 3 U H9EU E19EU 2001110200081 20011102 00081 NE 2001 11 2 2001F00509 2 20010529 A 7261 350A54113800 VENT LINE SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE OIL SYS CRACKED A R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 52285 3251 AIR VENT OIL TUBE CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M) 1 G 7 1 3U 3 U H9EU E19EU 2001110200082 20011102 00082 EU 2001 11 2 2001F00510 1 20010618 A 2400 SP381200 SWITCH SNIAS 350 AS350B3 8680954 EU ELECTRICAL SYS WORN A R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 52285 722 3251 MICROSWITCH WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M) 1 G 7 1 3U H9EU 2001110200083 20011102 00083 EU 2001 11 2 2001F00511 1 20010424 A 6321 350A32501000 SUPPORT SNIAS 350 AS350B3 8680954 EU MAIN ROTOR WORN A R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 392LG 172 3252 BRAKE LINING SUPPORT WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 1 3U H9EU 2001110200084 20011102 00084 EU 2001 11 2 2001F00526 1 20010731 A 6410 117317411 BLADE BOLKMS BK117 BK117C1 5626025 EU TAIL ROTOR DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 117SU 1427 7527 TAIL ROTOR BLADE ASSEMBLY PAINTED. INSPECT AND REPAIR AS REQUIRED. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M) 1 G 7 2 3U NC H13EU 2001110200085 20011102 00085 NM 2001 11 2 2001F00527 1 20010604 A 5320 900R1103001113 BUMPER BLOCK DOUG MD900 MD900 3027375 NM BEAM SEPARATED A R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 901CF 1201 90000012 SEPARATION OF TRAILING EDGE IN 'Y' AREA. REPLACED WITH NEW UNIT CORRECTED PROBLEM. CORE SHIPPED TO MDH FOR INSPECTION. (M) 1 G 7 2 3U NC H19NM 2001110200086 20011102 00086 2001 11 2 2001F00528 4 20010808 A 3160 B19030MC02 DISPLAY SNIAS 350 AS350B2 8680813 EU COCKPIT FAULTY A R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 392GL 456 3252 LINE 1 SCREEN IS DARK, NO CODES, CYCLED BATTERY SWITCH. LINE 2 BRIGHTNESS CODES (5). REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M) 1 G 7 1 3U H9EU 2001110200087 20011102 00087 NM 2001 11 2 CALA0100991 1 20011031 A 5754 SKIN BOEING 737 7373T0 1384582 NM #3 SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59338 23576 INSPECTION FOUND A 1/4" CRACK AT 2 EACH RIVETS IN L/H WING #3 SLAT SKIN. REPAIRED SKIN IAW SRM 57-43-01, FIGURE 206. 2 L 7 2 4F RT A16WE 2001110200088 20011102 00088 NM 2001 11 2 CALA0100992 1 20011031 A 5320 STIFFENER BOEING 737 7373T0 1384582 NM STA 1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59338 23576 INSPECTION FOUND AFT PRESSURE BULKHEAD FORWARD STIFFENER LOWER CORNER CORRODED ON R/H SIDE JUST AFT OF STA 1016, BL 0. A TYPICAL FORMED SECTION REPAIR WAS INSTALLED IAW SRM 51-70-11. 2 L 7 2 4F RT A16WE 2001110200089 20011102 00089 NM 2001 11 2 GAIA01311OP 1 20011003 A 3350 LIGHT BOEING 727 727251 138408H NM COCKPIT DISCONNECTED A GAIA K NONE O OTHER CR CRUISE 1 SW 07 252US 19971 FLT 1713 - HSV-FWA - DURING CRUISE, THE COCKPIT EMERGENCY EXIT LIGHT BECAME DISCONNECTED FROM IT FIXED MOUNT. THE AIRCR AFT CONTINUED ITS FLIGHT TO FWA AND LANDED WITHOUT ANY FURTHER DIFFICULTIES. REINSTALLED THE COCKPIT EMERGENCY EXIT LIG HT. IT WAS FOUND TO OPERATIONALLY CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001110200090 20011102 00090 NM 2001 11 2 UPS01237216 1 20011023 A 7160 PANEL BOEING 727 72722C 138400F NM #2 ENG. INTAKE DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE:C DELAM ON CORNER OF PANEL ON DOG BOX HOUSIG (#2 ENG. INTAKE) AT BS 11 50 AT 9 O CLOCK POS. REPAIRED IAW SRM 51-40-9 2 L 7 3 4F A3WE 2001110200091 20011102 00091 NM 2001 11 2 UPS01237218 1 20011024 A 2810 ACCESS PANEL BOEING 727 72722C 138400F NM #2 TANK CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE:C CORROSION ON LH #1 ACCESS PANEL FOR #2 TANK LH INTEGRAL REPLACED IAW MM 28-11-21 2 L 7 3 4F A3WE 2001110200092 20011102 00092 NM 2001 11 2 UPS01237219 1 20011023 A 5400 HINGE BOEING 727 72722C 138400F NM BS 1376 #2 ENG. CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE:C ENG. #2 PYLON, CRACK ON R/H COWLING HINGE CUTOUT AT BS 1376 CRACK ON HINGE CUTOUT STOP DRILLED IAW SRM 51-10-1 REPAIR CARRIED OUT IAW SMRO EO 2001-050-002 UPS ENGINEERING FILE NO 727-54-20016 2 L 7 3 4F A3WE 2001110200093 20011102 00093 NM 2001 11 2 UPS01237237 1 20011019 A 2710 6521753501 TAB HINGE BOEING 727 72722C 138400F NM L/H I/B TAB AIL CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE:C L/H INBD AILERON TAB O/B HINGE CORRODED. HINGE REPLACED IAW OHM 57-50-11 2 L 7 3 4F A3WE 2001110200094 20011102 00094 NE 2001 11 2 GTIA010370 2 20010516 A 7230 BLADE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE RT ENGINE SHINGLED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 RIGHT ENGINE HAS 1 FAN BLADE WITH EVIDENCE OF SHINGLING. REMOVED 2 BLADE SETS WITH EVIDENCE OF SHINGLING. INSTALLED TH E 2 BLADE SETS ON THE 1ST STAGE COMPRESSOR IAW MD80 MM 73-33-21 PAGE 401. (M) 2 L 7 2 4F 4 F A6WE E9NE 2001110200095 20011102 00095 WP 2001 11 2 GTIA010916 1 20010503 A 5320 BRACKET DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - AFT LOWER CARGO DOOR, FORWARD LATCH FITTING SUPPORT BRACKET CLIP CHAFING. UPON FURTHER INSPECTION, FOUND SUPPORT BRACKET CRACKED. REMOVED SUPPORT BRACKET IAW SRM MX-80 51-30-01. FORMED SUPPORT BRACKET, IAW MD80 SRM 51-10-2. INSTAL LED SUPPORT BRACKET IAW SRM 51-30-01. (M) 2 L 7 2 4F A6WE 2001110200096 20011102 00096 WP 2001 11 2 GTIA010918 1 20010530 A 5320 BRACKET DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FORWARD LOWER CARGO COMPARTMENT AFT LATCH FITTING SUPPORT BRACKET CLIP DAMAGE. REMOVED DAMAGED BRACKET IAW MD80 S RM 51-30-1. INSTALLED NEW BRACKET IAW SRM MX-80 51-30-1 P/N 5910141-116. (M) 2 L 7 2 4F A6WE 2001110200097 20011102 00097 WP 2001 11 2 GTIA010919 1 20010530 A 5320 BRACKET DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FORWARD LOWER CARGO DOOR, FORWARD LATCH FITTING SUPPORT BRACKET CLIP DAMAGE. REMOVED DAMAGE BRACKET IAW SRM MC-80 51-30-1. INSTALLED NEW BRACKET IAW SRM MD-80 51-30-1. (M) 2 L 7 2 4F A6WE 2001110200098 20011102 00098 EU 2001 11 2 NSVA0113 1 20010918 A 3320 BA0806281 BALLAST SAAB SF340 340B 7860101 EU CABIN OVERHEATED A NSVA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 EA 27 299CJ 340B299 PILOT REPORTED STRONG ODOR (BURNING PLASTIC) COMING FROM OVERHEAD SEAT 5A, 6A IN FLIGHT. CREW DECLARED EMERGENCY INBOUN D TO PIT. FIRE DEPARTMENT DISPATCHED, NO FIRE REPORTED. PSA MAINTENANCE FOUND A BURNED BALLAST UNIT CAUSING ODOR. MAI NTENANCE DEACTIVATED UNIT, RAN ENGINES FOR 30 MINUTES, NO ODOR PRESENT. AIRCRAFT WAS RELEASED FROM MX WITH MEL ON OVERH EAD LIGHTING. (M) 2 L 7 2 4T RT A52EU 2001110200099 20011102 00099 CE 2001 11 2 NSVA0114 1 20010913 A 5730 SKIN BEECH 1900 1900C 1154161 CE LT WING DENTED A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 550CJ UC50 DURING ROUTINE MAINTENANCE/INSPECTION, SOME DAMAGE WAS DISCOVERED ON THE LEFT WING LEADING EDGE AREA. AIRCRAFT WAS REPA IRED IAW DER REPORT 01-249, WO 20354. (M) 2 L 7 2 4T RT A24CE 2001110200100 20011102 00100 CE 2001 11 2 NSVA0115 1 20011001 A 2460 1143810237 CONTROL PANEL BEECH 1900 1900C 1154161 CE COCKPIT FAULTY A NSVA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 EA 27 129CJ UC129 DURING TAKEOFF ROLL FROM ACK, PILOTS NOTED AUTO FEATHER LIGHT DID NOT COME ON, ALSO LEFT AND RIGHT ANTI-ICE C/B POPPED. CAPTAIN ELECTED TO ABORT TAKEOFF AND RETURN TO GATE. MAINTENANCE TROUBLESHOT PROBLEM DOWN TO BAD LEFT BUS TIE RELAY. REMOVED AND REPLACED LEFT DC POWER PANEL. OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A24CE 2001110200101 20011102 00101 NE 2001 11 2 NSVA0117 2 20010920 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NR 2 ENGINE MALFUNCTIONED A NSVA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 EA 27 221CJ UE221 LGA - DURING TAXI BACK TO GATE AFTER LANDING. PILOT WAS NOTIFIED VIA RAMP CONTROL THAT ANOTHER AIRCRAFT APPARENTLY SAW SPARKS AND FLAMES COMING FROM THE NR 2 ENGINE EXHAUST. THE CREW DID NOT HAVE ANY INDICATION OF FIRE FROM MASTER CAUTION PANEL. MAINTENANCE CONDUCTED A FULL INSPECTION OF THE ENGINE AND FOUND NO ABNORMALITIES, AND NO EVIDENCE OF FIRE RAN ENGINES AT LOW POWER. COULD NOT DUPLICATE. AIRCRAFT WAS RELEASED FOR FLIGHT. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 2001110200102 20011102 00102 EA 2001 11 2 NSVA0118 2 20011010 A 7200 FIRE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA NR 2 ENGINE DETECTED A NSVA O OTHER A FLAME/FIRE NR NOT REPORTED 1 EA 27 32017 UC37 IAD - DURING ENGINE START OF NR 2 ENGINE THE GROUND CREW NOTICED A SIX FOOT FLAME FROM THE TAIL PIPE. PILOT SHUT FUEL O FF AND FLAMES EXTINGUISHED. MX MOTORED ENGINE AND FOUND NO DAMAGE OR EVIDENCE OF RESIDUAL FUEL IN TAIL PIPE. PILOT RES TARTED ENGINE WITH NO FURTHER OCCURRENCE. (M) 2 L 7 2 4T 4 T RT A24CE E4EA 2001110200103 20011102 00103 EU 2001 11 2 NSVA0119 1 20011001 A 7714 10223N01R00 INDICATOR SAAB SF340 340B 7860101 EU COCKPIT MALFUNCTIONED A NSVA O OTHER N FALSE WARNING TO TAKEOFF 1 EA 27 233CJ 340B233 PILOT REPORTED, DURING TAKEOFF ROLL RT RPM GAUGE DROPPED TO ZERO. MAINTENANCE RAN RIGHT ENGINE ON GROUND. OPS CHECK GO OD, SWAPPED GAUGES, P/N 10223N01R00, S/N ON RIGHT NOW IS 150 AND S/N ON LEFT IS 113. (M) 2 L 7 2 4T RT A52EU 2001110200104 20011102 00104 EU 2001 11 2 NSVA0120 1 20011007 A 3350 F8T5CW LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A NSVA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 27 294CJ 340B294 PILOT REPORTED TO MAINTENANCE CONTROL THAT SEAT 11A HAD A LIGHT OUT AND THAT AN ODOR WAS EMITTING FROM THE SAME AREA. M AINTENANCE REPLACED BULB, PILOT BELIEVED THAT THE ODOR WAS FROM THE REMOVED BULB. NEW BULB CHECKED GOOD NO FURTHER EVID ENCE OF FUMES DETECTED. (M) 2 L 7 2 4T RT A52EU 2001110200105 20011102 00105 EU 2001 11 2 SIMA200126201 1 20010919 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 358BZ 340B358 LAX - FLT 3340 - EMERGENCY FLOOR LIGHTING AT SEATS 6B AND 7B WERE FOUND TO BE INOPERATIVE. REMOVED AND REPLACED POWER S UPPLY 22LN IAW SAAB 240B AMM. OPS CHECKS GOOD. (M) 2 L 7 2 4T RT A52EU 2001110200106 20011102 00106 NE 2001 11 2 SIMA200126602 2 20010923 A 7321 6071520P16 ECU SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE MALFUNCTIONED A SIMA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 SW 21 371AE 340B371 DFW - FLT 3787 - WHILE IN CRUISE FLIGHT, LEFT ENGINE BEGAN TO SURGE. CREW PLACED LEFT ENGINE CONDITION LEVER TO TORQUE MOTOR LOCK OUT AND RETURNED TO DALLAS. REMOVED AND REPLACED LEFT DECU IAW SAAB AMM. OPERATIONALLY CHECKED GOOD. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 2001110200107 20011102 00107 EU 2001 11 2 SIMA200127101 1 20010928 A 3350 3013000 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 550LL 550 DFW - FLT 3620 - MAINTENANCE FOUND TWO FORWARD FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTE RY POWER PACK AT LOCATION 46WL. (M) 2 H 7 2 4T RT A53EU 2001110200108 20011102 00108 EU 2001 11 2 SIMA200127201 1 20010929 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY MALFUNCTIONED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SW 21 347SB 340B347 JFK - FLT 5116 - CARGO SMOKE INDICATION ON FINAL APPROACH EMERGENCY DECLARED AND CARGO EXTINGUISHER NR 1 ACTIVATED. REP LACED BOTH FORWARD AND AFT CARGO COMP SMOKE DETECTORS IAW SAAB AMM. OPERATIONAL CHECKS GOOD. (M) 2 L 7 2 4T RT A52EU 2001110200109 20011102 00109 EU 2001 11 2 SIMA200127202 1 20010929 A 3320 8ES00558800 MODULE AEROSP ATR42 ATR42300 8680920 EU CABIN FAULTY A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 47AE 047 EYW - FLT 5226 - AFTER TAKEOFF SMOKE DETECTED FROM READING LIGHT AREA OVER SEAT 7D/7C. REMOVED AND REPLACED POWER MODUL E FOR READING LIGHTS 7C/7D IAW ATR 42 AMM. OPERATIONALLY CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 2001110200110 20011102 00110 EU 2001 11 2 SIMA200127301 1 20010930 A 3350 LIGHT AEROSP ATR72 ATR72212A 8680902 EU CABIN MALFUNCTIONED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 540AM 540 CRP - FLT 9731 - CREW REPORTED THE EMERGENCY LIGHTS TO BE INOPERATIVE. AIRCRAFT WAS ISSUED A SPECIAL FLIGHT PERMIT TO F ERRY THE AIRCRAFT TO DFW FOR MAINTENANCE. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPS CHECK WAS GOOD IAW ATR MM A ND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001110200111 20011102 00111 EU 2001 11 2 SIMA200127302 1 20010930 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 904AE 340B314 ALL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REMOVED AND REPLACED ALL POWER SUPPLIES IAW SAAB 340AMM. OPS CHECKE D GOOD. (M) 2 L 7 2 4T RT A52EU 2001110200112 20011102 00112 EU 2001 11 2 SIMA200127705 1 20011002 A 3350 301121 LIGHT AEROSP ATR42 ATR42300 8680920 EU DOOR STEP INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 319AM 319 MIA - FLT 5037 - FOUND CABIN DOOR STEP EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY IAW ATR 42 AMM. (M) 2 H 7 2 4T RT A53EU 2001110200113 20011102 00113 EU 2001 11 2 SIMA200127801 1 20011003 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 272AE 340B272 ROC - FLT 4806 - FOUND NR 2 AND NR 3 RIGHT FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY IAW SAAB 340 AMM. OPERATIONALLY CHECKED GOOD. (M) 2 L 7 2 4T RT A52EU 2001110200114 20011102 00114 EU 2001 11 2 SIMA200127802 1 20011004 A 3350 3012701 LIGHT AEROSP ATR72 ATR72212A 8680902 EU PAX DOOR INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 529AM 529 DFW - FLT 3640 - FOUND PASSENGER DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY ON THE PASSENGER DOOR IAW ATR 72 AMM. (M) 2 H 7 2 4T RT A53EU 2001110200115 20011102 00115 EU 2001 11 2 SIMA200128001 1 20011007 A 3350 3011210 LIGHT AEROSP ATR42 ATR42300 8680920 EU EXTERIOR INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 242AT 242 MIA - FLT 5082 - CREW REPORTED THE PASSENGER DOOR EXTERIOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED THE EMERGENCY LIGHT ASSEMBLY IAW ATR MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001110200116 20011102 00116 NM 2001 11 2 TSAA0136136 1 20011004 A 3620 1296942 SENSOR BOEING 737 73773A 1384606 NM NR 1 ENGINE FAILED A TSAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 13 739AL 28500 FLT 478 - KOA-OAK-LAS - NR 2 BLEED TRIP OFF ILLUMINATED IN FLIGHT. RESET AND TRIPPED AGAIN. DIVERTED TO AND LANDED IN HNL, UNEVENTFUL LANDING. REPLACED THE 450 DEGREE TEMP SENSOR ON THE NR 2 ENGINE POWER MM 36-11-5. ENGINE RUN AND OPS C HECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001110200119 20011102 00119 WP 2001 11 2 ZIAA06001 1 20010624 A 5730 PLANK LKHEED 188 188A 5262602 WP LT WING CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 346HA 188A1043 NR 2 PLANK CRACKED. LEFT WING INBOARD OF CENTER RISER. (M) 2 L 7 4 4T RT 4A22 2001110200120 20011102 00120 WP 2001 11 2 2001F00597 1 20010830 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - FUSELAGE SKIN HAS 6 DENTS IN NORM MORE THAN 10 INCHES STATION 351, 360 BETWEEN LONGERON 4 AND 5 RIGHT. REWORKED D ENT TO ORIGINAL CONTOUR IAW MD80 SRM 53-04 FIG 38 CHECKED AREA FOR CRACK IAW NDT MANUAL 08-00-00. NO CRACK FOUND IAW ND T MANUAL 08-00-00. FABRICATE DOUBLER IAW MD80 SRM 53-04. INSTALLED NEW DOUBLER REPAIR IAW MD80 SRM 53-04 FIG 38. (M) 2 L 7 2 4F RT A6WE 2001110200121 20011102 00121 WP 2001 11 2 GTIA010322 1 20010510 A 5752 SKIN DOUG DC9 DC982 3022082 WP AILERON TAB DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 2700 48087 FOUND LEFT AILERON CONTROL TAB HAS TWO DENTS ON UPPER SURFACE. REMOVED DAMAGE TO AND AROUND DENTED TAB IAW DC9 MD-80 SR M 57-03. FABRICATED REPAIR IAW DC9 MD80 SRM 57-03. INSTALLED REPAIR ON TAB SURFACE IAW DC9 MD80 SRM 57-03. (M) 2 L 7 2 4F A6WE 2001110200122 20011102 00122 WP 2001 11 2 GTIA010323 1 20010510 A 5752 SKIN DOUG DC9 DC982 3022082 WP AILERON TAB DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - LEFT AILERON, TRIM TAB, UPPER SURFACE HAS TWO DENTS DOT 124. REMOVED DAMAGE TO AND AROUND DENTED TAB SURFACE IAW DC9 MD80 SRM 57-03. FABRICATED REPAIR IAW DC9 MD80 SRM 57-03. INSTALLED REPAIR IAW DC9 MD80 SRM 57-03. (M) 2 L 7 2 4F A6WE 2001110200123 20011102 00123 WP 2001 11 2 GTIA010380 1 20010516 A 5210 ANGLE DOUG DC9 DC982 3022082 WP ENTRY DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - MAIN ENTRY DOOR, LOWER GATE ANGLE IS CRACKED AND HAS SPINNING RIVETS. REPLACED LOWER GATE HINGE DOOR L1 IAW MD80 SRM 51-10-2. (M) 2 L 7 2 4F A6WE 2001110200124 20011102 00124 WP 2001 11 2 GTIA010381 1 20010516 A 5523 TAB DOUG DC9 DC982 3022082 WP ELEVATOR DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - RIGHT ELEVATOR ANTI-FLOAT TAB HAS DENTS AND AREA OF DELAMINATION. REMOVED AREAS OF DENTS AND DELAMINATION TO ANTI -FLOAT TAB IAW DC9 MD80 SRM 55-04. FABRICATED REPAIR IAW DC9 MD80 SRM 55-04. INSTALLED REPAIR ON ANTI-FLOAT TAB IAW DC 9 MD80 SRM 55-04. (M) 2 L 7 2 4F A6WE 2001110200125 20011102 00125 WP 2001 11 2 GTIA010382 1 20010516 A 5523 TAB DOUG DC9 DC982 3022082 WP ELEVATOR DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - RIGHT ELEVATOR GEARED TAB HAS DENTS AND AREA OF DELAMINATION. REMOVED DAMAGE TO AND AROUND AREAS OF DENTS AND DEL AMINATION. REPAIRED DENTS AND DELAMINATION ON TAB USING CARBON GRAPHITE CLOTH OVERLAY PROCEDURES IAW DC9 MD80 SRM 55-04 . (M) 2 L 7 2 4F A6WE 2001110200126 20011102 00126 WP 2001 11 2 GTIA010383 1 20010516 A 5523 TAB DOUG DC9 DC982 3022082 WP ELEVATOR DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - RIGHT ELEVATOR CONTROL TAB HAS SEVERAL DENTS AND AREAS OF DELAMINATION. REMOVED DAMAGE TO AND AROUND DENTS AND DE LAMINATED AREAS IAW DC9 MD80 SRM 55-04. FABRICATED REPAIR IAW DC9 MD80 SRM 55-04. INSTALLED REPAIR IAW DC9 SRM 55-04. (M) 2 L 7 2 4F A6WE 2001110200127 20011102 00127 WP 2001 11 2 GTIA010920 1 20010530 A 5230 DOOR FRAME DOUG DC9 DC982 3022082 WP CARGO DOOR DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - AFT CARGO DOOR AFT HINGE CUT OUT (LOWER SECTION) HAS A SECTION 3 INCHES LONG TORN OUT OF FRAME. REMOVED DAMAGED A REA IN CARGO DOOR AFT HINGE CUT OUT IAW MD80 SRM 52-05 PAGE 214A. FORMED REPAIR DOUBLER AND SHIM IAW MD80 SRM 52-05. ( M) 2 L 7 2 4F A6WE 2001110200128 20011102 00128 WP 2001 11 2 GTIA010923 1 20010503 A 5220 HANDLE DOUG DC9 DC982 3022082 WP EMERGENCY EXIT DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - EMERGENCY ESCAPE HATCHES HAVE DAMAGED PULL TO RELEASE HANDLES, ALL FOUR DOT 101. REMOVED OLD HANDLES IAW 52-21-01 MM MD-80, INSTALLED NEW PULL TO RELEASE HANDLE COVER IAW 52-21-01 MM MD-80. (M) 2 L 7 2 4F A6WE 2001110200129 20011102 00129 WP 2001 11 2 GTIA010924 1 20010504 A 2560 ESCAPE ROPE DOUG DC9 DC982 3022082 WP COCKPIT FRAYED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - CO-PILOT ESCAPE LINE IS FRAYED/DAMAGED. INSTALLED NEW ESCAPE LINE ON FIRST OFFICERS SIDE IAW MD-80 MM 25-61-00. (M) 2 L 7 2 4F A6WE 2001110200130 20011102 00130 WP 2001 11 2 GTIA010925 1 20011009 A 5230 PAN DOUG DC9 DC982 3022082 WP CARGO DOOR DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FORWARD CARGO DOOR PAN FLANGE DAMAGED JUST BELOW LOCKING MECH, LEFT SIDE AFT. REPAIRED DAMAGE AREA PER MD-80 SRM 52-01. (M) 2 L 7 2 4F A6WE 2001110200131 20011102 00131 WP 2001 11 2 GTIA010926 1 20010507 A 5523 TAB DOUG DC9 DC982 3022082 WP ELEVATOR DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - INBOARD TRAILING EDGE OF RIGHT GEARED TAB HAS DAMAGED AREA. REMOVED DAMAGE TO INBOARD TRAILING EDGE OF RIGHT GEAR ED TAB IAW DC-9 MD-80 SRM 55-04. REPAIRED DAMAGE OF INBOARD TRAILING EDGE RIGHT GEARED TAB USING EPOXY RESIN REPAIRED I AW DC-9 MD-80 SRM 55-04. (M) 2 L 7 2 4F A6WE 2001110200132 20011102 00132 WP 2001 11 2 GTIA010928 1 20011009 A 3350 110049 CHARGER DOUG DC9 DC931 3022065 WP CABIN FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 969ML 47268 ACY - EMERGENCY FLOOR PATH LIGHTS IN TAIL CONE INOPERATIVE. REMOVED AND REPLACED CHARGING UNIT, OPS CHECK NORMAL IAW DC 9 MM 33-50-0. (M) 2 L 7 2 4F A6WE 2001110200133 20011102 00133 WP 2001 11 2 GTIA010929 1 20011006 A 3350 60030431 BATTERY PACK DOUG DC9 DC981 3022081 WP TAIL CONE DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 819NK 48016 DTW - OVERHEAD EMERGENCY LIGHTS IN TAILCONE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD IAW MD80 MM 33-51-00. (M) 2 L 7 2 4F A6WE 2001110200134 20011102 00134 WP 2001 11 2 GTIA010930 1 20010505 A 5751 ATTACH ANGLE DOUG DC9 DC982 3022082 WP AILERON CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - RIGHT AILERON INBOARD LOWER FLANGE CRACKED. REMOVED NOSE CAP ATTACHING ANGLE IAW SRM MD-80 51-30-2. FABRICATED A TTACH ANGLE IAW MD80 SRM 51-10-2. (M) 2 L 7 2 4F A6WE 2001110200135 20011102 00135 WP 2001 11 2 GTIA010931 1 20010507 A 5540 RUDDER DOUG DC9 DC982 3022082 WP TAIL DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - LEFT SIDE OF RUDDER TRAILING EDGE HAS SMALL DAMAGED AREA. REMOVED DAMAGE, FABRICATED REPAIR DOUBLER IAW MD80 DC9 SRM 55-04. INSTALLED REPAIR IAW DC9 MD80 SRM 55-04. (M) 2 L 7 2 4F A6WE 2001110200136 20011102 00136 EU 2001 11 2 QXEA0101708 1 20011031 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN BURNED OUT A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 493US 11161 PDX- CABIN FORWARD EMERGENCY EXIT SIGN HAS NUMEROUS LAMPS BURNED OUT. REMOVED AND REPLACED CIRCUIT BOARD. OPERATIONAL CH ECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001110200137 20011102 00137 WP 2001 11 2 GTIA010933 1 20010904 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - FOUND DENTS AT FUSELAGE STATION Y218 BETWEEN LONGERON 7L AND 8L. REWORKED DENT TO ORIGINAL CONTOUR IAW MD80 SRM 5 3-04 FIG 38 CHECK AREA FOR CRACK IAW NDT MANUAL 08-00-00. NO CRACK FOUND IAW NDT MANUAL 08-00-00. FABRICATED DOUBLER I AW MD80 SRM 53-04 FIG 38. INSTALLED NEW REPAIR IAW MD80 SRM 53-04. (M) 2 L 7 2 4F RT A6WE 2001110200138 20011102 00138 WP 2001 11 2 GTIA010934 1 20010828 A 7110 NOSE COWL DOUG DC9 DC983 3022083 WP RT ENGINE ERODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - RIGHT NOSE COWL 12 O'CLOCK POSITION HAS DENT AND ERODED BETWEEN 10 AND 2 O'CLOCK. DENT MEASURES 3.50 INCH SPAN BY 1.8 INCH CHORD TO .140 INCH OUT OF LIMITS PER MD80 SRM 54.04A. RIGHT ENGINE NOSE COWL REPLACED WITH SERVICEABLE P/N SQ 30645-5093N001919 CHORD B016-7-N-0009. (M) 2 L 7 2 4F RT A6WE 2001110200139 20011102 00139 WP 2001 11 2 GTIA010938 1 20010504 A 5520 TIP CAP DOUG DC9 DC982 3022082 WP ELEVATOR DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 LEFT ELEVATOR TIP TRAILING EDGE HAS AN AREA THAT AN OLD REPAIR NEEDS TO BE REWORKED. REMOVED DAMAGED TIP IAW MD-80 SRM 51-30-2. FABRICATED NEW TIP IAW MD-80 SRM 51-10-2. INSTALLED TIP REPAIR IAW MD-80 SRM 51-30-2 AND 55-20-2. (M) 2 L 7 2 4F A6WE 2001110200140 20011102 00140 WP 2001 11 2 GTIA010939 1 20010505 A 5522 DOUBLER DOUG DC9 DC982 3022082 WP ELEVATOR DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - LEFT ELEVATOR OUTBOARD STATIC WICK BASE DOUBLER DAMAGED ON BOTTOM SIDE. REMOVED DAMAGED DOUBLER IAW MD80 SRM 51-3 0-2. FABRICATED NEW DOUBLER IAW MD80 SRM 51-10-2. INSTALLED WICK BASE IAW MD-80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2001110200141 20011102 00141 EA 2001 11 2 MASAM01126 1 20011020 A 7400 ENGINE CNDAIR CL600 CL6002B19 1900309 EA A MASA K NONE X ENGINE FLAMEOUT AP APPROACH 1 SW 07 97325 7325 WHILE ON FINAL APPROACH, THE NR 2 ENGINE FLAMED OUT. THE CREW DECLARED AN EMERGENCY AND WAS ABLE TO SUCCESSFULLY RESTAR T THE ENGINE AND LAND WITHOUT FURTHER INCIDENT. THE CREW ALERTED MAINTENANCE CONTROL THAT ALTHOUGH THE PRECIPITATION WA S MEDIUM, THEY DID NOT HAVE THEIR CONTINUOUS IGNITION ON. MAINTENANCE PERFORMED A THOROUGH INSPECTION AND WAS NOT ABLE TO FIND ANY DEFECTS. THE CREW WENT ON A TEST FLIGHT THROUGH PRECIPITATION AND EVERYTHING FUNCTIONED NORMALLY. 2 L 7 2 4F RT A21EA 2001110200142 20011102 00142 WP 2001 11 2 GTIA010940 1 20010516 A 2710 BRACKET DOUG DC9 DC982 3022082 WP AILERON SYS CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - AILERON AND TAB CONTROL MIXER BRACKET CORRODED IN NUMEROUS PLACES TO INCLUDE AROUND GUIDE PINS AND PULLEY MOUNTS. REMOVED RIGHT LATERAL CONTROL MIXER AS PER BOEING MD80 MM 27-61-04. INSTALLED REPLACEMENT LATERAL CONTROL MIXER BRACKE T AS PER BOEING M80 MM 27-61-04. (M) 2 L 7 2 4F A6WE 2001110200143 20011102 00143 WP 2001 11 2 GTIA010941 1 20010821 A 5230 LOCK DOUG DC9 DC983 3022083 WP CARGO DOOR CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 AFT CARGO COMPARTMENT DOOR FORWARD AND AFT LOCKING MECH ARE OXIDIZED. REMOVED OXIDATION AFT CARGO DOOR FORWARD LOCKING MECH MATERIAL LOST FOUND TO BE OUT OF LIMIT IAW MD80 SRM 52-01. REMOVED AND REPLACED TUBE LOCKING MECH IAW MD80 MM 52-3 1-00. (M) 2 L 7 2 4F RT A6WE 2001110200144 20011102 00144 2001 11 2 GTIA010942 4 20010821 A 3460 COMPUTER DOUG DC9 DC983 3022083 WP COCKPIT FAULTY A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - ALTITUDE SELECTOR ON DFGCP IS INTERMITTENT. REMOVED DFGCP IAW MD80 MM 22-01-02. INSTALLED DFGCP IAW MD80 MM 22-01 -02. DFGS RTS WILL BE ACCOMPLISHED ON C-CHECK CARD B16-09R-01. (M) 2 L 7 2 4F RT A6WE 2001110200145 20011102 00145 WP 2001 11 2 GTIA010943 1 20010913 A 2540 SUPPORT DOUG DC9 DC983 3022083 WP FWD LAVATORY CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - FORWARD LAVATORY SIDE WALL UNATTACHED AND CORRODED AT LOWER AREA. FABRICATED PART IAW SRM MD80 51-10-2. PRIOR TO LINE 1 REMOVED 2 CORRODED SUPPORTS IAW MD 80 SRM 51-30-0. INSTALLED 2 SUPPORTS IAW MD80 SR 51-30-01. (M) 2 L 7 2 4F RT A6WE 2001110200146 20011102 00146 WP 2001 11 2 GTIA010944 1 20010831 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - R1 DOOR FLOORBOARD SUPPORT CORRODED. PARTS FOUND TO BE OUT OF LIMITS IAW MD80 SRM 51-10-03. FABRICATED AND DRILL ED PARTS IAW SRM 51-10-02, 51-10-04. (M) 2 L 7 2 4F RT A6WE 2001110200147 20011102 00147 NM 2001 11 2 FX72001F00000 1 20010823 A 7910 ENGINE BOEING 727 727276 138408R NM PWA JT8 JT8D15 52051 NE NR 3 LACK OF LUBE A FX7A E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 19 908PG 20951 FLIGHT VH531 ENROUTE KSFB TO SVMI ACCOMPLISHED A PRECAUTIONARY SHUTDOWN OF ENGINE NR 3 SERIAL NR 700116, DUE TO LOW OIL QUANTITY INDICATION AND OIL PRESSURE DECREASING BELOW 42 PSI AIRCRAFT LANDED WITH OUT INCIDENT. TROUBLE SHOT NR 3 ENGIN E OIL QUANTITY SYSTEM AND SERVICED NR 3 ENGINE WITH APPROXIMATELY 16 QUARTS OF ENGINE OIL. PERFORMED ENGINE RUN FOR ENG INE OIL LEAK CHECKS NO LEAKS NOTED. ENGINE OPERATING WITH IN ALL PARAMETERS. ENGINE PLACED ON ENGINE OIL WATCH PER FAE GMM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F RT A3WE E2EA 2001110200148 20011102 00148 EU 2001 11 2 C2XA01IA390 1 20011031 A 2422 559012A INVERTER AEROSP ATR42 ATR42320 8680930 EU 90 VU RACK OVERHEATED A C2XA K NONE O OTHER UK UNKNOWN 1 SW 27 14819 156 IAH- DURING PERFLIGHT THE CREW NOTED A PLASTIC BURNING SMELL IN THE COCKPIT. IAH- MAINTENANCE REMOVED AND REPLACED TH ESTATIC INVERTER, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001110800021 20011108 00021 NM 2001 11 8 01FDEA00952 1 20011102 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 279FE 22346 CORROSION (C53-224-01) ON TOP OF FLOORBEAM BS 344, RBL 3 - LBL 31, WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 51-10- 6. 2 L 7 3 4F RT A3WE 2001110500001 20011105 00001 WP 2001 11 5 01FDEA00955 1 20010911 A 5310 DOOR FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 N 33 FS 960, LONG 40R TO 41R, FWD CARGO DOOR FRAME, AFT FRAME SKIN WORN. R&R FRAME PER SRM & EA. 2 L 7 3 4F A22WE 2001110500002 20011105 00002 2001 11 5 SWIA200110281 4 20011029 A 3425 RELAY EMB 120 EMB120ER 3260203 SO E/E BAY FAULTY A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 295UX 120295 EFIS & ATT INDICATIONS WHEN POWER LEVER ADVANCED FOR TAKEOFF WITH RIGHT AUX GEN OFF. COULD NOT DUPLICATE DPU FAILURE. RAN ENGINE AND HAD SCREENS FLASH. DPU FAIL CAME UP FOR APPROXIMATELY 3-5 SECONDS. THIS IS NORMAL. REPLACED RELAYS K01 19, K0227 AND K0029. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001110500003 20011105 00003 WP 2001 11 5 ZW0A0110001 1 20011023 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 913TW 49184 DURING CHECK-C MAINT FOUND CORROSION AT STA 1250, LBL 24 INCHES TO LBL 44 INCHES, CABIN FLOOR FRAME. REMOVED AND TREATE D CORROSION PER SPM 6-80-01 AND SRM 51-10-3. INSTALLED FLOOR SUPPORT PER SPM 6-70-01 AND SRM 51-30-5. 2 L 7 2 4F A6WE 2001110500004 20011105 00004 WP 2001 11 5 ZW0A0110002 1 20011018 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9618A 53565 DURING CHECK-C MAINT THE LT VENT BOX AREA, SHIELD WEB WAS CRACKED AT UPPER AFT CORNER INSIDE THE VENT BOX. STOP DRILLED CRACK PER SRM 51-01 PAGE 6. INSTALLED DOUBLER PER SRM 51-70-4. 2 L 7 2 4F RT A6WE 2001110500005 20011105 00005 WP 2001 11 5 ZW0A0110003 1 20011022 A 5320 STRUCTURE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9618A 53565 DURING CHECK-C MAINT FOUND LT MAIN LANDING GEAR WHEEL WELL AFT INBOARD LOWER CORNER HAD CRACK IN AFT FACE. ACCOMPLISHED HIGH FREQ EDDY CURRENT AND CONFIRMED CRACK PER 51-00-03, PART 6. INSTALLED NEW PART PER SPM 6-70-01. 2 L 7 2 4F RT A6WE 2001110500006 20011105 00006 WP 2001 11 5 ZW0A011001 1 20011019 A 5320 STRUCTURE DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9618A 53565 DURING CHECK-C MAINT THE SKIN STANDOFF WAS DAMAGED AT BELT RING STA 1443, BETWEEN LONGERON 16L AND 17L. REPAIRED PER SR M 53-03, PAGE 7 AND PAINTED PER SRM 51-10-3. 2 L 7 2 4F RT A6WE 2001110500007 20011105 00007 NM 2001 11 5 ZW0A0110201 1 20011028 A 3350 20131 BATTERY PACK BOEING 767 7673Q8 1385142 NM CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 634TW 28132 THE EGRESS LIGHTING WAS INOPERATIVE FROM SEAT ROW 24H TO 37H. REPLACED BATTERY PACK (P/N 2013-1ASMI), AND THE BATTERY C HARGER (P/N 2012-1). CHECK-C 10-25-00 LAX. 2 L 7 2 4F RT A1NM 2001110500008 20011105 00008 WP 2001 11 5 ZW0A0110301 1 20011029 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A ZW0A K NONE O OTHER CR CRUISE 1 CE 13 923TW 49379 THE EGRESS LIGHTING SYSTEM FLICKERED IN FLIGHT. UNABLE TO DUPLICATE THE PROBLEM. OPERATIONAL CHECKED NORMAL. 2 L 7 2 4F A6WE 2001110500009 20011105 00009 WP 2001 11 5 ZW0A0110302 1 20011023 A 5320 STRUCTURE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9618A 53565 DURING CHECK-C MAINT, THE RT MAIN LANDING GEAR WHEEL WELL RT GEAR DOOR CUTOUT WAS CRACKED ON THE AFT OUTBOARD END. ACCO MP INSPECTION PER NDT 51-00-03 AND FOUND CRACK CONTAINED. STOP DRILLED CRACK. INSTALLED REPAIR DOUBLERS PER SRM 53-01, PAGE 10. 2 L 7 2 4F RT A6WE 2001110500010 20011105 00010 WP 2001 11 5 ZW0A0110303 1 20011022 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 913TW 49184 DURING CHECK-C MAINT THE FLOOR TRACK WAS CORRODED IN SEVERAL AREAS AT LBL 21 INCHES, STA 1136 TO 1309. REMOVED AND REPL ACED TRACK PER SRM 53-05 AND SPM 6-30-01, LBL 21 AND STA 1117 TO 1329. 2 L 7 2 4F A6WE 2001110500011 20011105 00011 WP 2001 11 5 ZW0A0110304 1 20011024 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 913TW 49184 DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT ANGLE AT STA 1155, BETWEEN LBL 27 INCHES TO 45 INCHES, HAD CORROSION. RE MOVED RIVETS. IDENTIFIED MATERIAL PER SRM 53-14-3, FIG 12 SHEET 1 AND 2. FABRICATED NEW AND INSTALLED PER SRM 51-20-0. 2 L 7 2 4F A6WE 2001110500012 20011105 00012 WP 2001 11 5 ZW0A0110305 1 20011024 A 5320 PLATE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 913TW 49184 DURING CHECK-C MAINT IN THE FWD CABIN FOUND HEAVY CORROSION 12 INCHES INBOARD OF THE FWD SERVICE DOOR THRESHOLD, ON FLOO R PLATE. REMOVED OLD FLOOR PLATE AND REPLACED WITH NEW. INSTALLED PER SPM 6-70-01. 2 L 7 2 4F A6WE 2001110500013 20011105 00013 WP 2001 11 5 ZW0A0110306 1 20011025 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 913TW 49184 DURING CHECK-C MAINT THE LT TIE DOWN TRACK WAS CORRODED IN THE MID CARGO COMPT AT STA 636 TO 693. REPLACED TRACK FROM S TA 514 TO 790 PER SRM 53-05, FIG 6, AND SRM 51-30 AND 51-6. 2 L 7 2 4F A6WE 2001110500014 20011105 00014 WP 2001 11 5 ZW0A0110307 1 20011026 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 913TW 49184 DURING CHECK-C MAINT IN THE FWD CARGO COMPT FOUND THE FLOOR TO AFT BULKHEAD SUPPORT WAS CRACKED IN THE RADIUS, STA 541 A ND LONGERON 29L. REPLACED CRACKED ANGLE PER 51-30 AND 51-10-3, USING ORIGINAL TYPE FASTENERS. 2 L 7 2 4F A6WE 2001110500015 20011105 00015 WP 2001 11 5 ZW0A0110308 1 20011029 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9618A 53565 DURING CHECK-C MAINT IN THE AFT CARGO COMPT, BETWEEN STA 1250 TO 1271, THE RT CARGO TIE DOWN TRACK SCREW HOLES HAD CORRO SION. INSTALLED NEW TIE DOWN TRACK PER SRM 51-30-1 AND 51-30-2, PER SPM 6-70-01 AND DRAWING 5936663. 2 L 7 2 4F RT A6WE 2001110500016 20011105 00016 WP 2001 11 5 ZW0A0110309 1 20011029 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9618A 53565 DURING CHECK-C MAINT THE LT CARGO TIE DOWN TRACK HAD CORROSION IN SCREW HOLES AND EDGES AT STA 1123 TO 1287. INSTALLED NEW TRACK USING FASTENERS PER SRM 51-30-1 AND SPM 6-70-01. 2 L 7 2 4F RT A6WE 2001110500017 20011105 00017 WP 2001 11 5 ZW0A0110401 1 20011029 A 2750 CONTROL CABLE DOUG DC9 DC982 3022082 WP T/E FLAP BROKEN A ZW0A K NONE F FLT CONT AFFECTED LD LANDING 1 CE 13 960TW 49231 CREW REPORTED FLAP SPLIT INDICATION ACCOMPANIED WITH ROLL TENDENCY. FOUND T/E FLAP BUS CABLE BROKEN DUE TO CORROSION AN D FATIGUE. CHANGED CABLE RUNS 33A AND B, AND 34A AND B. CHANGED CABLES PART NUMBERS C04564-2, C04564-1, 3922841-527, A ND 3922841-531. 2 L 7 2 4F A6WE 2001110500018 20011105 00018 NM 2001 11 5 ZW0A0110402 1 20011031 A 5330 SKIN BOEING 767 7673Y0 NM FUSELAGE DENTED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 640TW 25411 DURING CHECK-C MAINT FOUND FUSELAGE SKIN DENT AT STA 1800 AND STRINGER 38R, AT SKIN LAP IN NON PRESSURIZED AREA. REMOVE D DAMAGE, FABRICATED AND INSTALLED DOUBLERS PER SRM 53-00, 16 IN BY 17 IN, PER ARA 17848. 2 L 7 2 4F RT A1NM 2001110500019 20011105 00019 NM 2001 11 5 ZW0A0110403 1 20011031 A 5330 SKIN BOEING 767 7673Y0 NM FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 640TW 25411 DURING CHECK-C MAINT FOUND SKIN AT LAP SEAM WITH .75 INCH CUT UNDER STRINGER 38R, STA 1798. FABRICATED AND INSTALLED DO UBLER PER SRM 53-00-01, 11 IN BY 11.5 IN, PER ARA 17848. 2 L 7 2 4F RT A1NM 2001110500020 20011105 00020 WP 2001 11 5 2001F00598 1 20011008 A 3350 9721055 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 830US 49443 IND - THE RIGHT SIDE WALL EMERGENCY LIGHT AT SEAT ROW 19, THE LEFT AFT SERVICE DOOR EMERGENCY LIGHT, AND TWO LOW LEVEL S EAT MOUNTED EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. REF USAAD00168. (M ) 2 L 7 2 4F A6WE 2001110500021 20011105 00021 NM 2001 11 5 USAABB01104 1 20011006 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 627AU 27805 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 18 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001110500022 20011105 00022 NM 2001 11 5 USAABB01105 1 20011006 A 3350 8731002511REV14 LIGHT BOEING 757 7572B7 1384964 NM L2 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 627AU 27805 BDL - FOUND L2 EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001110500023 20011105 00023 NM 2001 11 5 USAABB01106 1 20011007 A 3350 9221009 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 624AU 27245 BDL - FOUNDS R4 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2001110500024 20011105 00024 WP 2001 11 5 USAAD01166 1 20011004 A 3350 AD4002P BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 828US 48028 PIT - THE FORWARD CABIN EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 2001110500025 20011105 00025 WP 2001 11 5 USAAD01168 1 20011008 A 3350 9721050 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 830US 49443 IND - THE RIGHT SIDE WALL EMERGENCY LIGHT AT SEAT ROW 19, THE LEFT AFT SERVICE DOOR EMERGENCY LIGHT, AND TWO LOW LEVEL S EAT MOUNTED EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001110500026 20011105 00026 EU 2001 11 5 USAASA01053 1 20011006 A 3397 CONNECTOR AIRBUS 320 A320214 3930316 EU ESCAPE SLIDE DISCONNECTED A USAA K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 19 101UW 0936 TPA - RECEIVED 'EPSU EX LOAD FORWARD L ER LOAD AFT LT' FAULT DURING CHECK. MAINTENANCE RECONNECTED THE AFT LEFT EMERGEN CY ESCAPE SLIDE LIGHT CONNECTOR. OPS CHECKED NORMAL. (M) 2 L 7 2 4F RT A28NM 2001110500027 20011105 00027 NM 2001 11 5 USAASB01275 1 20010929 A 3350 20121 POWER SUPPLY BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 436US 24558 PHL - MAINTENANCE FOUND SEVERAL EMERGENCY LIGHTS IN THE AFT GALLEY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EM ERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001110500028 20011105 00028 NM 2001 11 5 USAASB01276 1 20010930 A 3350 20121 CHARGER BOEING 737 737301 1384611 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 335US 23232 TPA - MAINTENANCE FOUND THE AFT LEFT ENTRY DOOR AND AFT RIGHT SERVICE DOOR EXTERIOR EGRESS EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT RIGHT EMERGENCY BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK OF ALL EMERGENCY LIGHTS GOOD. (M) 2 L 7 2 4F RT A16WE 2001110500029 20011105 00029 NM 2001 11 5 USAASB01277 1 20010930 A 3350 1012623 LIGHT BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 780AU 24997 PHL - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT AT SEAT ROW 11ABC, LEFT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001110500030 20011105 00030 NM 2001 11 5 USAASB01278 1 20011002 A 3397 WIRE BOEING 737 737201 1384454 NM CABIN DAMAGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 263AU 22869 LGA - THE FLOOR PATH EMERGENCY LIGHT WAS INOPERATIVE AT SEAT ROW 7. MAINTENANCE REPAIRED A WIRE UNDER THE SEAT ASSEMBLY . (M) 2 L 7 2 4F A16WE 2001110500031 20011105 00031 NM 2001 11 5 USAASB01282 1 20011003 A 3350 20121 CHARGER BOEING 737 7373B7 1384580 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 393US 23315 CLT - MAINTENANCE FOUND THE LEFT AND RIGHT FORWARD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE F ORWARD EMERGENCY LIGHT BATTERY PACKS (P/N 2013-1A) AND THE RIGHT FORWARD CHARGER ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001110500032 20011105 00032 NM 2001 11 5 USAASB01283 1 20011006 A 3350 S106 BATTERY BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 279AU 22891 PVD - THE EMERGENCY LIGHT ABOVE THE AFT RIGHT SERVICE DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BA TTERY. (M) 2 L 7 2 4F A16WE 2001110500033 20011105 00033 NM 2001 11 5 USAASB01285 1 20011007 A 3350 20131A BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 785AU 25024 CLT - MAINTENANCE FOUND THE CABIN EMERGENCY LIGHTS FROM SEAT ROWS SIX THROUGH NINE AND THE LEFT EXTERIOR LIGHTS BETWEEN ESCAPE DOORS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2001110500034 20011105 00034 NM 2001 11 5 USAASB01289 1 20011010 A 3350 900835A POWER SUPPLY BOEING 737 737201 1384454 NM CARGO BAY DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 254AU 22796 LGA - THE OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMERGENCY LIGHT POWER SUPPLY. (M) 2 L 7 2 4F A16WE 2001110500042 20011105 00042 CE 2001 11 5 AC1R178790 1 20010824 A 2435 S28435 RELAY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE STARTER SYSTEM MALFUNCTIONED B AC1R E ENGINE SHUTDOWN O OTHER IN INSP/MAINT 1 SO 01 351WC 2843 5600330 TROUBLESHOOTING ANTI-ICE PROBLEM, RT START LIGHT STAYED ON AFTER START CYCLE. PUSHING START DISENGAGE BUTTON DID NOT EXT LIGHT. GEN WOULD COME ON LINE. RT ENGINE WAS SHUTDOWN FIRST, SHUTDOWN WAS NORMAL RELAY WAS NOT WELDED SHUT. TROUBLESHOO TING OF LIGHT REVEALED IT STAYED ON EVEN WITH BATTERY SWITCH IN OFF POSITION. ONLY WAY TO EXT THE LIGHT WAS TO UNPLUG BA TTERY OR PULL START LIGHT CIRCUIT BREAKER, CB 281. ACCESS WAS GAINED TO AFT POWER J BOX AND RELAY WAS TAPPED WITH SCREWD RIVER, LIGHT WENT OUT. MECHANICAL CONNECTION INSIDE RELAY THAT PROVIDES POWER FOR LIGHT HAD COME IN CONTACT WITH HOT BAT TERY SIDE OF BATTERY RELAY, TAPPING RELAY BROKE THAT CONNECTION. NEW RELAY WAS INSTALLED, OPERATION CHECKED OK. 2 L 7 2 4F 4 F RT A22CE E25EA 2001110500044 20011105 00044 CE 2001 11 5 BLI2001F00000 1 20010808 A 2613 SENSOR CESSNA 500 500CESSNA 2076602 CE PWA JT15 JT15D1 52060 NE AIR DUCT FAILED E BLIA O OTHER N FALSE WARNING CR CRUISE 1 GL 17 58TC 5000261 AIR DUCT OVERHEAT ANNUNCIATOR ON IN FLIGHT. AIRCRAFT LANDED, DUCT SENSOR REPLACED BY REPAIR STATION. SYSTEM OPS CHECKE D GOOD. RETURNED TO SERVICE. 1 L 7 2 4F 4 F A22CE E1NE 2001110500045 20011105 00045 CE 2001 11 5 BLI2001F00001 1 20010815 A 2612 WIRE CESSNA 421 421B 2076014 CE CONT O520 TSIO520C 17040 SO FIRE DETECTOR CHAFED E BLIA O OTHER N FALSE WARNING AP APPROACH 1 GL 17 208V 421B0866 ON APPROACH, RIGHT ENGINE FIRE WARNING ON. AIRCRAFT INSPECTED FOR EVIDENCE OF DAMAGE OR EXHAUST LEAK. NONE NOTED. EX TENSIVE GROUND RUNS COULD NOT DUPLICATE. AIRCRAFT RETURNED TO SERVICE. FURTHER DETAILED INSPECTION FOUND WIRES TO ONE FIRE DETECTOR CHAFED. INSULATED WIRES REROUTED AND SECURED WIRE BUNDLE. EXTENSIVE OPS CHECK, FLIGHT INCLUDING SEVERAL APPROACHES PERFORMED TO VERIFY FIX. 1 L 7 2 3O 3 O A7CE E8CE 2001110500046 20011105 00046 NM 2001 11 5 AWXA200100564 1 20011031 A 2910 AS116080264 HOSE BOEING 737 7373G7 1384595 NM R/H WHEEL WELL RUPTURED A AWXA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 WP 28 305AW 24012 LAS - AIR TURNBACK - FLT 870 - "C" - DURING CLIMB OUT OF LAS THE # 2 ENG "B" SYSTEM HYD PRESS. LIGHT STARTED FLICKERING AND THE "B" SYSTEM HYD QUANTITY DECREASED TO 1/4 FULL. THE CREW SHUT OF THE "B" SYSTEM HYDRAULICS AND RETURNED TO LAS MA KING AN UNEVENTFUL LANDING. MAINTENANCE FOUND THE "B" SYS ELECTRIC HYD PUMP PRESSURE HOSE HAD RUPTURED IN THE R/H MAIN L ANDING GEAR WHEEL WELL. MAINTENANCE REPLACED THE LINE, SERVICED THE "B" SYSTEM HYDRAULICS AND PERFORMED LEAK CHECKS. NO FURTHER DISCREPANCIES HAVE BEEN REPORTED. 2 L 7 2 4F RT A16WE 2001110500047 20011105 00047 CE 2001 11 5 BLI2001F00002 1 20010815 A 7714 INDICATOR CESSNA 500 500CESSNA 2076602 CE PWA JT15 JT15D1 52060 NE COCKPIT MALFUNCTIONED E BLIA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 17 58TC 5000261 RIGHT ENGINE FAN RPM INDICATOR TAPE JITTERED, THEN WENT TO MAX INDICATION. REMOVED AND REPLACED FAN SPEED INDICATOR. O PS CHECKED GOOD. 1 L 7 2 4F 4 F A22CE E1NE 2001110500048 20011105 00048 CE 2001 11 5 BLI2001F00003 1 20010610 A 5230 LATCH CESSNA 500 500CESSNA 2076602 CE PWA JT15 JT15D1 52060 NE CARGO DOOR OUT OF ADJ E BLIA O OTHER J WARNING INDICATION CR CRUISE 1 GL 17 58TC 5000261 DOOR WARNING LIGHT ON, IN FLIGHT. TAIL CONE BAGGAGE DOOR LATCH ADJUSTED AND RESET BY MECH. 1 L 7 2 4F 4 F A22CE E1NE 2001110500050 20011105 00050 CE 2001 11 5 BLI2001F00004 1 20010610 A 3000 J-BOX CESSNA 500 500CESSNA 2076602 CE PWA JT15 JT15D1 52060 NE DE-ICE SYS INTERMITTENT E BLIA O OTHER J WARNING INDICATION CR CRUISE 1 GL 17 58TC 5000261 L ICE FAIL, LIGHT ON IN FLIGHT IN ICE AND ON GROUND WITH SYSTEM ON. RESET TWO CIRCUIT BREAKERS ON LEFT ICE J-BOX. PERF ORMED RESISTANCE CHECK OF HEAT ELEMENT. FOUND SERVICEABLE. OPS CHECK FLIGHT SHOWED NO DEFECT. L ICE SYSTEM OPS, NORMA L. 1 L 7 2 4F 4 F A22CE E1NE 2001110500051 20011105 00051 CE 2001 11 5 BLIA512C82801 1 20010828 A 7714 972019002 INDICATOR CESSNA 500 500CESSNA 2076602 CE PWA JT15 JT15D1 52060 NE COCKPIT FAILED E BLIA O OTHER N FALSE WARNING CL CLIMB 1 GL 17 58TC 5000261 AFTER TAKE OFF, RIGHT FAN RPM TAPE JITTERED THEN WENT TO MAX INDICATION. REDUCED RIGHT ENGINE POWER, CHECKED OTHER PARAM ETERS, NORMAL. TROUBLESHOT AND DETERMINED TO BE BAD GAUGE. ACQUIRED LOANER FROM MFG AND INSTALLED. OPS CHECKED GOOD. 1 L 7 2 4F 4 F A22CE E1NE 2001110500052 20011105 00052 CE 2001 11 5 BLIA512C8801 1 20010808 A 2613 991206914 SENSOR CESSNA 500 500CESSNA 2076602 CE PWA JT15 JT15D1 52060 NE A/C BAY INOPERATIVE E BLIA O OTHER N FALSE WARNING CR CRUISE 1 GL 17 58TC 7596 5000261 IN FLIGHT: DUCT OVER-TEMP ANNUNCIATOR ON. FOLLOWED FLT MANUAL PROCEDURES. CALLED MAINTENANCE. ARRANGED FOR SENSOR TO BE REPLACED. CABIN TEMPERATURE SYSTEM OPS CHECKED GOOD. 1 L 7 2 4F 4 F A22CE E1NE 2001110500053 20011105 00053 CE 2001 11 5 BLIA512CB1701 1 20010815 A 2612 WIRE CESSNA 421 421B 2076014 CE CONT O520 GTSIO520F 17032 SO FIRE DETECTION CHAFED E BLIA O OTHER N FALSE WARNING AP APPROACH 1 GL 17 65AE 5769 421B0953 APPROACH TO AIRPORT: RIGHT ENGINE FIRE WARNING ON. REDUCED POWER, CO-PILOT LOOKED FOR SMOKE. NONE NOTED, LIGHT OUT LAN DED, CALLED MAINTENANCE AIRCRAFT DID NOT RETURN TO BASE. LIGHT INDICATOR PROBLEM INSPECTED, EXHAUST AND ENGINE FOUND NO EVIDENCE OF DAMAGE OR EXHAUST LEAK. EXTENSIVE GROUND RUNS COULD NOT DUPLICATE. AIRCRAFT RETURNED IRS. DETAILED FURTH ER INSPECTED FOUND WIRES TO ONE FIRE DETECTOR CHAFED AND CAPABLE OF SHORTING AGAINST SEAT TUBE WIRE. INSULATED WIRES, R EROUTED AND SECURED WIRE BUNDLE. OPS CKD FLIGHTS INCLUDING CRUISE FLIGHT AND SEVERAL APPROACHES INDICATE PROBLEM CORRE CTED. 1 L 7 2 3O 3 O A7CE E7CE 2001110500054 20011105 00054 EU 2001 11 5 CAXA106177 1 20011002 A 2435 160SG1409 STARTER GEN UROCOP EC120 EC120B 8680987 EU TMECA ARRIUS ARRIU2F NE ENGINE FAILED A CAXA O OTHER O OTHER NR NOT REPORTED 1 WP 15 408DC 489 1151 PART REQUIRED MAJOR REPAIR MUCH TOO EARLY. 1 G 7 2 3U 3 U NC R0001RD E34NE 2001110500055 20011105 00055 EU 2001 11 5 CCA2001F00000 1 20010611 A 5753 T700A5755097000 CARRIAGE SOCATA TBM TBM700 8682000 EU PWA PT6 PT6* 52043 EA T/E FLAP CRACKED B CCAR K NONE O OTHER IN INSP/MAINT 1 EA 17 700TJ 1954 25 UPON COMPLIANCE WITH AD, DETECTED A CRACK COMPLETELY THROUGH CAST WEB. INSTALLED NEW CARRIAGE ASSEMBLY PN 7700AS75509700 0. NEW PART WEB THICKNESS IS APPROX 3X THICKER. POSSIBLE CAUSE; HIGH FLAP OPERATING SPEED. REPLACEMENT PART APPEAR TO BE REINFORCED IN AFFECTED AREA. 1 L 7 1 3T 3 T RT A60EU E2NE 2001110500056 20011105 00056 EU 2001 11 5 CCA2001F00001 1 20010611 A 5753 T700A5755098001 CARRIAGE SOCATA TBM TBM700 8682000 EU PWA PT6 PT6* 52043 EA T/E FLAP CRACKED B CCAR K NONE O OTHER IN INSP/MAINT 1 EA 17 700TJ 1954 25 UPON COMPLIANCE WITH AD, DETECTED A CRACK COMPLETELY THROUGH CAST WEB. INSTALLED NEW CARRIAGE ASSEMBLY PN T700A57550980 01. NEW PART WEB THICKNESS IS 3X THICKER. POSSIBLE CAUSE; HIGH KIT FLAP OPERATING SPEED. REPLACEMENT PART APPEARS TO BE REINFORCED IN AFFECTED AREA. 1 L 7 1 3T 3 T RT A60EU E2NE 2001110500057 20011105 00057 2001 11 5 COE2001F00000 4 20011016 A 3422 060001500 GYRO CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE COCKPIT FAILED A COEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 13 720FX 208B0452 19334 ON CLIMBOUT AFTER DEPARTURE OF FLIGHT HSI(ARTIFICIAL HORIZON) AND RMI(RADIO MAGNETIC INDICATOR) FLAGGED. PILOT HAD NOT YET ENTERED IMC(INSTRUMENT MET SYSTEM) BUT CONTINUED FLIGHT WOULD REQUIRE THIS SYSTEM. PILOT INITIATED AIR TURNBACK AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED AND THE DIRECTIONAL GYRO WAS REMOVED AND REPLACED. AIRCRAFT WAS R ETURNED TO SERVICE. 1 H 7 1 3T 3 T A37CE E4EA 2001110500058 20011105 00058 NE 2001 11 5 CUC2001F00000 2 20011008 A 7320 LINE BELL 212 212 1181420 SW PWA PT6T PT6T3B 52045 NE NR 1 ENGINE CRACKED A CUCA K NONE O OTHER IN INSP/MAINT 1 WP 17 911VR 30998 CPPS60754 WHILE TROUBLESHOOTING NR 1 ENGINE FOR SLOW START, FOUND P3 LINE AT FILTER HOUSING CRACKED. REPLACED P3 LINE ASSEMBLY WI TH NEW. LINE WAS CRACKED ON BACK SIDE, FLUSH THE P3 HOUSING. 1 G 7 1 4U 4 U H4SW E22EA 2001110500059 20011105 00059 SO 2001 11 5 CWQ2001F00000 1 20010806 A 3610 54722250 CLAMP EMB 135 EMB135ER 3260203 SO ALLSN AE300 AE3007A GL BLEED AIR SYS LOOSE A CWQA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 05 926FM 145466 DURING ADDITIONAL ACCEPTANCE INSPECTION, IT WAS AGAIN NOTED THE AIRFRAME BLEED AIR CHECK VALVE V-BAND CLAMPS WERE NOT IN STALLED CORRECTLY IAW COMMON INDUSTRY PRACTICE OR AS RECOMMENDED BY THE CLAMP MANUFACTURE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001110500060 20011105 00060 SO 2001 11 5 CY42001F00000 2 20010911 A 8530 SA52000A20P CYLINDER CESSNA 207 207A 2073604 CE CONT O520 IO520F 17032 SO ENGINE CRACKED A CY4R K NONE O OTHER IN INSP/MAINT 1 AL 03 70076 1441 20700547 240939 CYLINDER INSTALLED 8/13/99, CRACK FOUND AROUND SPARK PLUG HOLE. 1 H 7 1 3O 3 O A16CE E5CE 2001110500061 20011105 00061 SO 2001 11 5 CY42001F00001 2 20010911 A 8530 SA52000A20P CYLINDER CESSNA 206 U206G 2073356 CE CONT O520 IO520* 17032 SO ENGINE CRACKED A CY4R K NONE O OTHER IN INSP/MAINT 1 AL 03 733KD 1103 U20604772 279984R CYLINDER INSTALLED 5/28/98, PLACED IN SERVICE 6/29/98. FOUND CRACK FROM SPARK PLUG HOLE AROUND INTAKE SIDE OF CYLINDER. 1 H 7 1 3O 3 O A4CE E5CE 2001110500062 20011105 00062 CE 2001 11 5 E272001F00000 1 20011001 A 2432 A703FSS CONTACTOR RAYTHN DH125 HAWKER800XP CE GARRTT TFE731 TFE731* 01518 WP BATTERY WRONG PART A E27R K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 07 29B 256 258518 AIRCRAFT FOUND TO HAVE START CONTACTOR PN A703FSS INSTALLED IN PLACE OF BATTERY CONTACTOR PN A770RSS. PILOT REPORTED LO SS OF NR 1 AND NR 2 BATTERY CONTACTORS IN FLIGHT. (INSTALLED BY MANUFACTURER) 2 L 7 2 4F 4 F RT A3EU E6WE 2001110500063 20011105 00063 EU 2001 11 5 E4G2001F00000 1 20011025 A 2520 A37201665 LINK SAAB SF340 340B 7860101 EU GE CT7TS CT71 30030 NE PAX SEAT BELT DEFECTIVE A E4GR K NONE O OTHER IN INSP/MAINT 1 SW 13 222NE 340B222 AIRCRAFT ARRIVED FOR MBV CHECK AND 20 EACH SEAT BELT LINKS WERE DEFECTIVE. THE CONNECTING RIVET IS PULLING OUT. SEVERA L LINKS WERE ALMOST ALL THE WAY APART. THIS AFFECTS CUSTOMER SAFETY. 2 L 7 2 4T 4 U RT A52EU E8NE 2001110500064 20011105 00064 SO 2001 11 5 E4G2001F00001 1 20011010 A 2730 14524986005 BUSHING EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL CONTROL QUADRANT OUT OF POSITION A E4GR K NONE O OTHER IN INSP/MAINT 1 SW 13 624AE 145111 BUSHINGS ARE MIGRATING CAUSING EXCESSIVE WEAR TO ELEVATOR CONTROL QUADRANT SUPPORT FITTINGS. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2001110500065 20011105 00065 SO 2001 11 5 EEJ2001F00001 1 20011012 A 3250 95394000 CHANNEL PIPER PA34 PA34200T 7103406 SO CONT O360 TSIO360EB 17025 SO NLG STEERING CRACKED E EEJA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 07 81659 348070143 807690R NOSE WHEEL STEERING CHANNEL CRACKED AT RIGHT REAR WELD. MADE POPPING NOISE WHILE TAXING. DUE TO STEERING AIRCRAFT ON G ROUND, NOSE WHEEL STEERING (WHERE BALL GOES INTO SAID CHANNEL) STRESSES THE WELDS ON FORWARD AND AFT ENDS THUS CRACKING THE WELDS. 1 L 7 2 3O 3 O A7SO E9CE 2001110500066 20011105 00066 SO 2001 11 5 C2XA01CL223 1 20011102 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO FUSELAGE INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13955 145075 DURING ROUTINE OVERNIGHT MAINTENANCE THE RIGHT HAND EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE.MAINTENANCE INS PECTED AND REPLACED THE LIGHT.OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2001110500067 20011105 00067 NM 2001 11 5 PCAA0111131 1 20011104 A 5210 8SC0156 STRUT DHAV DHC8 DHC8102 2809003 NM WEAK A PCAA K NONE O OTHER NR NOT REPORTED 1 EA 13 805EX 228 MDT- FLIGHT #3555. CREW REPORTED PASSENGER DOOR HARD TO OPEN FROM THE INSIDE. MAINTENANCE REPLACED PASSENGER DOOR HANDLE STRUT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001110500068 20011105 00068 NM 2001 11 5 PCAA0111132 1 20011102 A 5610 NP15790214 WINDOW DHAV DHC8 DHC8102 2809003 NM FIRST OFFICERS CRACKED A PCAA K NONE O OTHER NR NOT REPORTED 1 EA 13 848EX 12103 331 ALB- FLIGHT#3512. CREW REPORTED TWO ONE INCH CRACKS NEAR LOWER EDGE MOUNTING BOLT ON FIRST OFFICERS SIDEWINDOW. MAINTENA NCE REPLACED FIRST OFFICERS SIDE WINDOW IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL 56-10-16. AIRCRAFT RETU RNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001110500069 20011105 00069 NM 2001 11 5 UPS01237213 1 20011018 A 5310 LAP JOINT BOEING 727 72722C 138400F NM BS 1141 STR. 4 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE:C SUSPECT CORROSION AT LAP JOINT AT BS 1141 STR 4 R LFEC CARRIED OUT, 30%CORROSION INDICATED. AREA O F DAMAGE , CUTOUT HF EC NDF. REPAIR PARTS FABRICATED AND INSTALLED IAW UPS EO B727-5330-0 509 APPENDIX 8.3. AREA REPROTE CTED IAW SRM. 2 L 7 3 4F A3WE 2001110500070 20011105 00070 WP 2001 11 5 ABXA010569 1 20011026 A 5100 99234343 DOUBLER DOUG DC9 DC941 302207N WP FWD. CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 SKIN DOUBLER WAS CRACKED AND EXFOLIATED IN TWO PLACES, FORWARD SIDE OF F.S. 617 AND LONGERON 30, AND FUSELAGE DRAIN AT F .S. 632. REPLACED KIDNEY DOUBLER. 2 L 7 2 4F A6WE 2001110500071 20011105 00071 WP 2001 11 5 ABXA010567 1 20011101 A 7931 M832481236 PACKING DOUG DC9 DC941 302207N WP DEFECTIVE A ABXA E ENGINE SHUTDOWN Y ENGINE STOPPAGE CL CLIMB 1 GL 23 964AX 47781 RIGHT ENGINE LOST OIL PRESSURE ON CLIMBOUT, FOR DURATION OF 9 MINUTES ENGINE WINDMILLED. OIL PRESSURE DECREASED AS OIL Q UANTITY DECREASED. IN FLIGHT SHUT-DOWN. REPLACED THE MAIN OIL FILTER HOUSING CAP O-RING AND INSPECTED THE MAIN OIL FILTE R, NO METAL FOUND, IAW DC-9 MM 72-20-06. 2 L 7 2 4F A6WE 2001110500072 20011105 00072 EA 2001 11 5 COMA0160867 1 20011101 A 2916 73021 RESERVOIR CNDAIR CL600 CL6002B19 1900309 EA AFT EQUIP LEAKING A COMA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 01 729CA 6629 7265 FLIGHT #5092. HYDRAULIC SYSTEM #2 LOW PRESSURE CAUTION. QUANTITY INDICATED ZERO.REPLACED #2 HYDRAULIC RESERVOIR ASSY. 2 L 7 2 4F RT A21EA 2001110500073 20011105 00073 EA 2001 11 5 COMA0160868 1 20011104 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 815CA 7397 FLIGHT #5515. FLAPS FAILED AT 30 DEGREES DURING APPROACH.RESET THE FLAP SYSTEM PER AD 98-20-01 AND DEFERRED FURTHER MAI NTENANCE. 2 L 7 2 4F RT A21EA 2001110500074 20011105 00074 EA 2001 11 5 COMA0160869 1 20011104 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA LAMP BURNED OUT A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 969CA 7141 FLIGHT #5497. ONE CABIN EMERGENCY LIGHT IS INOPERABLE.REPLACED LIGHT BULB. 2 L 7 2 4F RT A21EA 2001110500075 20011105 00075 WP 2001 11 5 GTIA010937 1 20010822 A 5523 SKIN DOUG DC9 DC983 3022083 WP ELEVATOR TAB DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - RIGHT ELEVATOR CONTROL TAB HAS MANY DENT (TOP SIDE). CLEANED DENT AREAS 6 ON RIGHT INBOARD ELEVATOR CONTROL TAB I AW DC9/MD-80 SRM 55-04 PAR 5B. REPAIRED DENTS ON RIGHT ELEVATOR CONTROL TAB IAW DC9 MD80 SRM 55-04. (M) 2 L 7 2 4F RT A6WE 2001110500076 20011105 00076 WP 2001 11 5 GTIA010945 1 20010911 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - FOUND FLOOR SUPPORT AT STATION 1136 BETWEEN LONGERONS 28L TO 28R BROKEN IN HALF. REMOVED FLOOR SUPPORT PER SRM MD 80 51-30-2. LOCATE AND DRILLED NEW FLOOR SUPPORT PER MD80 SRM 51-10-4. INSTALLED FLOOR SUPPORT AT STATION 1136 BETWEEN LONGERONS 28L TO 28R IAW MD80 SRM 51-30-5. (M) 2 L 7 2 4F RT A6WE 2001110500077 20011105 00077 WP 2001 11 5 GTIA010946 1 20010831 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - EVIDENCE OF DENT LOCATED APPROXIMATELY STATION 579 L20R C/O 97165-4. REWORKED DENT TO ORIGINAL CONTOUR IAW MD80 S RM 53-04 FIG 38. CHECK AREA FOR CRACK IAW NDT MANUAL 08-00-00. NO CRACK FOUND IAW NDT MANUAL 08-00-00. FABRICATED DOU BLER REPAIR IAW MD80 SRM 53-04. INSTALLED NEW REPAIR IAW MD80 SRM 5-04 FIG 38. (M) 2 L 7 2 4F RT A6WE 2001110500078 20011105 00078 WP 2001 11 5 GTIA010947 1 20010902 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - A .100 INCH DIAMETER HOLE IN FLOOR SUPPORT CHANNEL AND FLOOR AT FS 197 BL 55 LEFT. AREA FOUND TO BE OUT OF LIMITS PER MD80 SRM 53-01-0. FABRICATED NEW DOUBLER PER MD80 SRM 53-01 AND 51-10-4. INSTALLED DOUBLER PER MD80 SRM 53-01. ( M) 2 L 7 2 4F RT A6WE 2001110500079 20011105 00079 WP 2001 11 5 GTIA010949 1 20010830 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - FLOOR SUPPORT ANGLE AT AFT LOWER CORNER OF L1 DOOR CORRODED, FS 200L, BL 55L. REMOVED CORROSION IAW MD80 SRM 51-1 0-3. FABRICATED FLOOR SUPPORT PER SRM MD80 51-10-2. INSTALLED FLOOR SUPPORT IAW MD80 SRM 51-10-3. (M) 2 L 7 2 4F RT A6WE 2001110500080 20011105 00080 WP 2001 11 5 GTIA010950 1 20010830 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - FLOOR SUPPORT CORRODED, FS 168R, BL 11R. REMOVED CORROSION ON FLOOR SUPPORT FS 168R, BL 11R IAW MD80 SRM 53-01. FABRICATED NEW FLOOR SUPPORT FS 168R, BL 11R IAW MD80 SRM 53-01. INSTALLED NEW FLOOR SUPPORT FS 168R, BL 11R, IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2001110500081 20011105 00081 WP 2001 11 5 GTIA010951 1 20010830 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - PASSENGER CABIN SEAT TRACK HAS CORROSION AND BARE METAL IN SEVERAL PLACES AT FS 1174-1287 AT X PLUS 36 INCHES. RE MOVED CORROSION IAW MD80 SRM 53-01. REMOVED CORRODED SECTION STATION 1184 TO 1141 IAW SRM MD80 53-05. INSTALLED COMPLE TE SEAT TRACK SECTION FROM STATION 1184 TO 1241 AND 2 SPLICES IAW SRM MD80 53-05. (M) 2 L 7 2 4F RT A6WE 2001110500082 20011105 00082 WP 2001 11 5 GTIA010952 1 20010830 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - PASSENGER CABIN SEAT TRACK HAS CORROSION AND BARE METAL IN SEVERAL PLACES AT FS 1174-1287 AT X PLUS 18 INCHES. RE MOVED CORROSION IAW MD80 SRM 51-10-3. REMOVED DAMAGE SEAT TRACK. INSTALLED SEAT TRACK IAW MD80 SRM 51-30-1. (M) 2 L 7 2 4F RT A6WE 2001110500083 20011105 00083 WP 2001 11 5 GTIA010953 1 20010830 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - AFT CARGO FLOOR SUPPORT HOLE ELONGATED AND SURFACE CORROSION STATION 1322 L29. ELONGATED HOLE FOUND TO BE OUT OF LIMITS IAW MD-80 SRM 51-10-04. FABRICATED DOUBLER. INSTALLED DOUBLER ON FLOOR SUPPORT AT STATION 1322 L29 IAW MD80 SRM 51-30-02. (M) 2 L 7 2 4F RT A6WE 2001110500084 20011105 00084 WP 2001 11 5 GTIA010954 1 20010830 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - PASSENGER CABIN SEAT TRACK HAS CORROSION AT FS 200-408 AT X-18 INCHES. REMOVED CORROSION. REMOVED SEAT TRACK FRO M STATION IAW MD-80 SRM 53-04. INSTALLED NEW SEAT TRACK IAW MD-80 SRM 53-04. (M) 2 L 7 2 4F RT A6WE 2001110500085 20011105 00085 WP 2001 11 5 GTIA010955 1 20010828 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - PASSENGER CABIN SEAT TRACK HAS CORROSION IN SEVERAL PLACES AT FS 503-674. REMOVED CORROSION. LOCATED AND DRILLED NEW SEAT TRACK IAW MD-80 SRM 51-10-04 AND 53-05. (M) 2 L 7 2 4F RT A6WE 2001110500086 20011105 00086 WP 2001 11 5 GTIA010956 1 20010830 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - FORWARD LOWER CARGO COMPARTMENT CORRODED AT RIGHT FLOOR SUPPORT, ABOVE STRINGER 29 RIGHT STATION 408 TO STATION 42 7. REMOVED CORROSION, REMOVED FLOOR SUPPORT. LOCATED AND DRILLED NEW FLOOR SUPPORT IAW MD-80 SRM 51-10-04. (M) 2 L 7 2 4F RT A6WE 2001110500087 20011105 00087 WP 2001 11 5 GTIA010957 1 20010830 A 5310 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - CENTER LOWER CARGO COMPARTMENT CORRODED AT LOWER CUTOUT DOOR JAMB FROM STATION 635 TO STATION 693. REMOVED CORROS ION ON JAMB. REMOVED JAMB BEAM. INSTALL NEW JAMB BEAM IAW MD-80 SRM 51-30-02. (M) 2 L 7 2 4F RT A6WE 2001110500088 20011105 00088 WP 2001 11 5 GTIA010958 1 20010827 A 5753 WEDGE DOUG DC9 DC983 3022083 WP T/E FLAP OUT OF ADJ A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - FOUND INBOARD FLAP LEFT, INBOARD TO OUTBOARD SECTIONS ARE OUT OF ALIGNMENT. REMOVED TRAILING EDGE WEDGE. INSTALL ED NEW TRAILING EDGE WEDGES IAW MD-80 SRM 51-30-02. (M) 2 L 7 2 4F RT A6WE 2001110500089 20011105 00089 WP 2001 11 5 GTIA010959 1 20010830 A 5753 WEDGE DOUG DC9 DC983 3022083 WP T/E FLAP DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 RIGHT WING, INBOARD FLAP INBOARD OUTBOARD TRAILING EDGE DELAMINATION. REMOVED 2 INBOARD FLAP TRAILING EDGE WEDGES. INS TALLED NEW WEDGES IAW MD-80 SRM 51-30-07. (M) 2 L 7 2 4F RT A6WE 2001110500090 20011105 00090 WP 2001 11 5 GTIA010960 1 20011010 A 5520 PLATE DOUG DC9 DC983 3022083 WP ELEVATOR DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - RIGHT ELEVATOR INBOARD L/E UPPER PLATE ROD BENT AND CRACKED POPOUT THROUGH THE HEAD OF RIVET AS MARKED. REMOVED P LATE FORM NEW PLATE. LOCATED AND DRILLED. INSTALLED NEW PLATE IAW MD-80 SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2001110500091 20011105 00091 2001 11 5 GTIA010961 4 20010830 A 2565 SLIDE DOUG DC9 DC983 3022083 WP TAIL CONE IMPROPER A GTIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 814NK 49619 FTW - TAILCONE EMERGENCY EVACUATION SLIDE PACKED IMPROPERLY. REMOVED TAILCONE EMERGENCY EVACUATION SLIDE, INSTALLED EME RGENCY EVACUATION SLIDE IAW MD-80 25-62-00. (M) 2 L 7 2 4F RT A6WE 2001110500092 20011105 00092 WP 2001 11 5 GTIA010962 1 20011002 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 814NK 49619 FTW - FOUND 4 OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED BATTERY PACK. INSTALLED BATTERY POWER SUPPLY IAW MM 33-50- 00 SYSTEM OP CHECKS GOOD. (M) 2 L 7 2 4F RT A6WE 2001110500093 20011105 00093 WP 2001 11 5 GTIA010963 1 20010830 A 5230 SKIN DOUG DC9 DC983 3022083 WP CARGO DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FORWARD CARGO DOOR SKIN AROUND HANDLE IS BENT. STRAIGHTENED SKIN TO ORIGINAL COUNTER, FOUND CRACK TO SKIN. FABRICATED DOUBLER IAW MD-80 SRM 52-05. (M) 2 L 7 2 4F RT A6WE 2001110500094 20011105 00094 WP 2001 11 5 GTIA010966 1 20010822 A 1420 TERMINAL DOUG DC9 DC983 3022083 WP WARNING HORN BROKEN A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 814NK 49619 FTW - APU FIRE WARNING HORN WILL NOT SOUND DURING SYSTEM TEST. REPLACED BROKEN TERMINAL LUG FOR HORN GROUND. OPS CHECK GOOD PER MD-80 MM 26-10-00. (M) 2 L 7 2 4F RT A6WE 2001110500095 20011105 00095 WP 2001 11 5 ABXA010549 1 20011020 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC932F 3022067 WP COCKPIT DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 909AX 47148 EMERGENCY LIGHTS IN FLIGHT COMPARTMENT INOPERATIVE. REPLACED THE EMERGENCY LIGHT BATTERIES IAW DC-9 AMM 33-53-00-4-0109. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2001110500096 20011105 00096 NM 2001 11 5 ABXA010550 1 20011026 A 3260 LIGHT BOEING 767 767200 1385120 NM COCKPIT INOPERATIVE A ABXA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 23 785AX 23018 RIGHT MAIN LANDING GEAR LAMP INOPERATIVE ON GEAR EXTENSION. SWAPPED LEFT LAMP IN AND INDICATED GOOD ON THE RIGHT SIDE. C REW ELECTED TO DO A FLY BY OVER THE TOWER AT PDX. EMERGENCY EQUIPMENT WAS DISPATCHED. NO GEAR RECYCLE WAS ANNOTATED IN T HE LOG BOOK. RELAMPED THE RIGHT MAIN LANDING GEAR INDICATION LIGHT. OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2001110500097 20011105 00097 WP 2001 11 5 ABXA010551 1 20011026 A 3297 WIRE DOUG DC9 DC941 302207N WP LT MLG BROKEN A ABXA K NONE N FALSE WARNING AP APPROACH 1 GL 23 973AX 47511 UPON APPROACH, NO GREEN OR RED GEAR EXTENSIONS FOR THE LEFT MAIN GEAR. ALTERNATE GEAR INDICATION WORKED NORMALLY. AIRCRA FT DIVERTED TO ILN. FOUND TWO BROKEN WIRES ON THE LEFT MAIN LANDING GEAR SIDE BRACE CONDUIT. REPAIRED WIRES. SWUNG GEAR IAW DC-9 MM. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2001110500098 20011105 00098 WP 2001 11 5 ABXA010552 1 20010413 A 5312 DOUBLER DOUG DC8 DC863F 302198F WP FUSELAGE BULGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 BULGING FINGER DOUBLER AND RIVET HEADS WERE SHEARED ON THE UPPER SURFACE OF THE PRESSURE WEB BETWEEN FUSELAGE STATION 88 0 AND BUTT LINE 00. REPAIRED AREA AND INSTALLED NEW FINGER DOUBLER IAW DC-8 SRM 51-1-21, 51-1-8, 53-2-0, 51-9-0, 51-1-20 D, 51-1-11, AND DRAWING NR 5645332, AND REA D853-40767-MR. 2 L 7 4 4F 4A25 2001110500099 20011105 00099 WP 2001 11 5 ABXA010553 1 20010503 A 5310 DOOR FRAME DOUG DC8 DC863F 302198F WP FUSELAGE GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 STATION 170, BETWEEN LONGERON 17 LEFT AND 18 LEFT, ON MAIN CARGO DOOR FRAME WAS GOUGED. BLENDED OUT GOUGE AND INSTALLED NEW DOUBLER IAW REA D852-40805-MR, AND DC8 SRM 51-1-8, 51-1-15, AND 51-1-20D. 2 L 7 4 4F 4A25 2001110500100 20011105 00100 WP 2001 11 5 ABXA010554 1 20010415 A 5312 PRESSURE PANEL DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 CORROSION ON THE UPPER SURFACE OF THE PRESSURE WEB AND ON FINGER DOUBLER. ALSO RIVET HEADS WERE SHEARED OFF BETWEEN FS 9 20-980. REPAIRED AREA AND REPLACED THE DOUBLER IAW DC-8 SRM 51-1-8, 53-2-0, AND REA D853-40413-MR, AND DAC DRAWING NR 56 45332. 2 L 7 4 4F 4A25 2001110500101 20011105 00101 WP 2001 11 5 ABXA010555 1 20010413 A 5312 PRESSURE PANEL DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 CORROSION AND SEVERAL RIVET HEADS SHEARED OFF BETWEEN FS 900-940, ON UPPER SURFACE OF PRESSURE WEB AT BUTT LINE 00. REPA IRED AREA AND REPLACED DOUBLER AND GUSSET IAW DC-8 SRM 51-1-20, 51-1-11, 51-3-0, 51-1-21, 51-1-8, 53-20, AND DAC DRAWING NR 5645332, AND REA D853-40767-MR. 2 L 7 4 4F 4A25 2001110500102 20011105 00102 WP 2001 11 5 ABXA010556 1 20011026 A 3350 5708458503 BATTERY DOUG DC8 DC863 302198A WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 822AX 46079 EMERGENCY LIGHTING WAS INOPERATIVE. REPLACED BATTERY EMERGENCY LIGHT RACK ASSEMBLY. EMERGENCY LIGHT OPS CHECKED GOOD PER AMM 33-50-02. 2 L 7 4 4F 4A25 2001110500103 20011105 00103 WP 2001 11 5 ABXA010557 1 20011029 A 3350 LIGHT DOUG DC9 DC933F 302207A WP COCKPIT MALFUNCTIONED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 930AX 47363 COCKPIT EMERGENCY LIGHTS WOULD NOT TEST. MECHANIC WENT TO GET NEW BATTERIES. UPON MECHANIC'S RETURN, THE CREW INFORMED H IM THAT THE LIGHTS WERE WORKING, BUT ONE BULB WAS OUT. WHEN MECHANIC WIGGLED THE BULB IT CAME ON. REPLACED THE BULB AS A PRECAUTION. 2 L 7 2 4F A6WE 2001110500104 20011105 00104 WP 2001 11 5 ABXA010558 1 20010609 A 5312 BULKHEAD DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 MAIN CABIN AFT PRESSURE BULKHEAD WAS CRACKED APPROXIMATELY 63 INCHES ABOVE THE FLOOR BETWEEN THE LEFT BUTT LINE 28 TO LE FT BUTT LINE 40. REPAIRED AREA IAW DAC DWG SRO 8530007, DC-8 SRM 51-1-8, 51-1-20D, 51-3-0, 51-3-1, AND 53-8-5. 2 L 7 4 4F 4A25 2001110500105 20011105 00105 WP 2001 11 5 ABXA010559 1 20010607 A 5330 SKIN DOUG DC8 DC863 302198A WP FUSELAGE DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 REMOVED AND REPLACED THE AFT LOWER SKIN, STATION 1350-1490. REPLACED THE AFT LOWER SKIN IAW DC-8 SRM 51-1-21, 51-3-2, 51 -1-11, 51-1-26, 51-3-1, AND 51-3-3. 2 L 7 4 4F 4A25 2001110500106 20011105 00106 WP 2001 11 5 ABXA010560 1 20010604 A 5411 SPAR CAP DOUG DC8 DC863 302198A WP NR 4 PYLON GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 NR 4 PYLON INBOARD UPPER SPAR CAP GOUGED AT STATION YN 295. REPAIRED AREA IAW REA D854-40850-MR. 2 L 7 4 4F 4A25 2001110500107 20011105 00107 WP 2001 11 5 ABXA010561 1 20010604 A 5312 BULKHEAD DOUG DC8 DC863 302198A WP FUSELAGE GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 FORWARD RADOME BULKHEAD, FORWARD SIDE, LOWER 0600 POSITION, GOUGE IN WEB. REPAIRED AREA IAW DC-8 SRM 53-2-0, 51-1-21, 51 -1-8, 51-1-20, AND DAC DWG 4644898. 2 L 7 4 4F 4A25 2001110500108 20011105 00108 WP 2001 11 5 ABXA010563 1 20010605 A 5350 SKIN DOUG DC8 DC863 302198A WP TAIL CONE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 TAILCONE HAD CORROSION AND DETERIORATING SEALANT JUST ABOVE THE LOWER TAILCONE LIGHT IN THE SEAM. REPAIRED AREA AND INST ALLED NEW SKIN IAW DC-8 SRM 51-1-8, 53-2-0, 51-1-21, 51-1-11, AND DC-8 DWG 5704665. 2 L 7 4 4F 4A25 2001110500109 20011105 00109 WP 2001 11 5 ABXA010565 1 20010607 A 5512 SKIN DOUG DC8 DC863 302198A WP HORIZ STAB CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 RIGHT HORIZONTAL STABILIZER LOWER SKIN WAS CORRODED AND BULGED, XE 149. REPAIRED AREA AND REPLACED SKIN IAW TSRM 95T0345 001, DC-8 SRM 51-1-8, 51-1-21, AND 51-1-20D. 2 L 7 4 4F 4A25 2001110500110 20011105 00110 WP 2001 11 5 ABXA010566 1 20011029 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC931 3022065 WP COCKPIT DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 908AX 47008 AFT COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC-9 AMM 33-53-02 -4-0001. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2001110500111 20011105 00111 WP 2001 11 5 ABXA010568 1 20011018 A 5730 59127351 PANEL DOUG DC9 DC941 302207N WP WING DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 UPPER OUTBOARD TRAILING EDGE PANEL HAD SEVERAL AREAS OF DELAMINATION. REPLACED PANEL IAW DC-9 SRM 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 2001110500112 20011105 00112 WP 2001 11 5 ABXA010570 1 20011020 A 5320 59560809 FLOOR SUPPORT DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 SMALL CRACK IN THE OUTBOARD EDGE OF THE E&E FLOOR SUPPORT JUST FORWARD OF FS 218, ABOVE LONGERON 28 RIGHT. REPLACED FLOO R SUPPORT IAW DC-9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2001110600001 20011106 00001 NE 2001 11 6 2001F00601 1 20010402 A 6320 E6893672 PINION GEAR SKRSKY S76 S76A 8143006 NE GEARBOX SPALLED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 709AL 760278 UPON INSPECTION OF GEARBOX PARTS, LIGHTS SPALLING AND GALLING ON PINION GEAR TEETH CAUSING LIGHT SPALLING ON T/M GEAR GE ARTEETH. (M) 1 G 7 2 3U H1NE 2001110600002 20011106 00002 GL 2001 11 6 2001F00602 2 20010815 A 7250 23053299 TURBINE BLADES BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL ENGINE CORRODED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 343AL 1449 51372 DURING DISASSEMBLY TO REPAIR FOR LOW POWER. SULPHADATION ON FRONT SIDES OF BLADES. HAVE WHEELS TESTED FOR PROPER COATI NG. (M) 1 G 7 1 3U 3 U H2SW E1GL 2001110600003 20011106 00003 SW 2001 11 6 2001F00603 1 20010419 A 6320 6893673 GEAR BELL 407 407 1182206 SW GEARBOX DAMAGED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 847AL 53150 UPON DISASSEMBLY OF GEARBOX FOR N2 OVERSPEND INSPECTION, T/M GEAR HAS IMPROPER AND UNFINISHED MACHINING ON AFT SIDE OF L ARGE GEAR TEETH. SECONDARY DAMAGE, PINION GEAR P/N 6893672 S/N NN76746 TT INK. SCRAP GALLING GEAR TEETH. ASSURE GEAR HARDNESS AND PROPER MACHINING AT FACTORY. (M) 1 G 7 1 3U O H2SW 2001110600004 20011106 00004 GL 2001 11 6 2001F00604 2 20010803 A 7250 6898735 TURBINE WHEEL BOLKMS 105 BO105CBS 5626008 EU ALLSN 250C 250C20 03013 GL ENGINE BROKEN B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 5416F 794 TURBINE RECEIVED FROM FIELD, REMOVED COMB CASE FOUND SULPHADATION ON NR 1 WHEEL. WHEEL HAS BROKEN BLADES DUE TO SULPHAD ATION. (M) 1 G 7 2 3U 3 U NC H3EU E4CE 2001110900015 20011109 00015 WP 2001 11 9 ARWA0011013 1 20011030 A 7722 430200 THERMOCOUPLE DOUG DC8 DC861 3021952 WP NR 1 ENGINE FAULTY A ARWA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 19 30UA 45888 IN CRUISE AT FL 29.0 NR 1 ENGINE EGT FLUCTUATED FROM 210 C TO 380 C, ALL OTHER PARAMETERS AS FOLLOWS: EPR 1.74, N2 97.5 PERCENT, FF 4900 LBS, N1 102.5 PERCENT, OIL TEMP 76 C, OIL PRESS 52 PSI, OAT -19 C. PERFORMED IN-FLIGHT ENGINE SHUTDOW N ABNORMAL CHECKLIST. NOTE: WINDMILLING OIL PRESS 22 PSI, TIME 22:27 Z. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THREE EGT THERMOCOUPLES AND REMOVED AND REPLACED THE #1 EGT INDICATOR IAW MM 77-20-1 AND 77-20-0 SYSTEM OPS CK NORMAL IAW 71-00 ALL PARAMETERS NORMAL. 2 L 7 4 4F 4A25 2001110600005 20011106 00005 GL 2001 11 6 2001F00605 2 20010824 A 7200 6898607 BEARING SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL ENGINE FAILED B ALGR O OTHER O OTHER NR NOT REPORTED 1 SW 03 1547N 760088 ENGINE MAKING METAL. BEARING FAILED. (M) 1 G 7 2 3U 3 U H1NE E1GL 2001110600006 20011106 00006 SW 2001 11 6 2001F00606 1 20010822 A 6510 407340340103 DISC PACK BELL 407 407 1182206 SW TAIL ROTOR CRACKED A ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 537AL 53230 DAILY INSPECTION, COUPLING IS CRACKED, PROBABLE CAUSE IS EXCESSIVE RIGIDITY IN THE BEARING MOUNT SYSTEM. ALLOW TAILROTO R DRIVESHAFT TO FLOAT SO DISC PACKS DO NOT FLEX AS MUCH OR AS OFTEN. (M) 1 G 7 1 3U O H2SW 2001110600008 20011106 00008 SW 2001 11 6 2001F00608 1 20010122 A 6510 407340340101 DISC PACK BELL 407 407 1182206 SW TAIL ROTOR CRACKED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 697AL 53374 DURING 25 HOUR AD INSPECTION, THE COUPLING IS CRACKED, PROBABLE CAUSE IS EXCESSIVE RIGIDITY IN BEARING MOUNT SYSTEM. AL LOW TAILROTOR DRIVESHAFT TO FLOAT SO DISC PACKS DO NOT FLEX AS MUCH OR AS OFTEN. (M) 1 G 7 1 3U O H2SW 2001110600009 20011106 00009 SW 2001 11 6 2001F00609 1 20010822 A 6510 407340340103 DISC PACK BELL 407 407 1182206 SW TAIL ROTOR CRACKED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 1116H 53046 DURING 25 HOUR AD INSPECTION, COUPLING IS CRACKED, PROBABLE CAUSE IS EXCESSIVE RIGIDITY IN THE BEARING MOUNT SYSTEMS. A LLOW TAILROTOR DRIVESHAFT TO FLOAT SO DISC PACKS DO NOT FLEX AS MUCH OR AS OFTEN. (M) 1 G 7 1 3U O H2SW 2001110600010 20011106 00010 SW 2001 11 6 2001F00610 1 20010827 A 6510 407340340101 DISC PACK BELL 407 407 1182206 SW TAIL ROTOR CRACKED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 1116H 53046 DURING 25 AD INSPECTION, THE COUPLING IS CRACKED, PROBABLE CAUSE IS EXCESSIVE RIGIDITY IN THE BEARING MOUNT SYSTEM. ALL OW TAILROTOR DRIVESHAFT TO FLOAT SO DISC PACKS DO NOT FLEX AS MUCH OR AS OFTEN. (M) 1 G 7 1 3U O H2SW 2001110600011 20011106 00011 SW 2001 11 6 2001F00611 1 20010822 A 6510 407340340103 DISC PACK BELL 407 407 1182206 SW TAIL ROTOR CRACKED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 437AL 53141 DAILY INSPECTION OF TAILROTOR DRIVESHAFT BEARINGS AND FOUND CRACKED DISC PACK. THE COUPLING IS CRACKED, PROBABLE CAUSE IS EXCESSIVE RIGIDITY IN THE BEARING MOUNT SYSTEM. ALLOW TAILROTOR DRIVESHAFT TO FLOAT SO DISC PACKS DO NOT FLEX AS MUC H OR AS OFTEN. (M) 1 G 7 1 3U O H2SW 2001110600012 20011106 00012 WP 2001 11 6 IXXA0100070O 1 20011105 A 2121 FAN DOUG DC8 DC862 3021970 WP FWD BELLY DEFECTIVE A IXXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 11 31CX 73590 265 45911 ENROUTE FROM RMS TO AVB, THE FLIGHT CREW SENSED AN ODOR IN THE COCKPIT WHEN THE LEFT RECIRCULATION FAN WAS OPERATING. TH E FLIGHT CREW SECURED THE FAN AND THE ODOR SUBSIDED. THE FLIGHT CONTINUED TO AVB FOR AN UNEVENTFUL LANDING. MAINTENACE I NSPECT THE FAN WHICH WAS FOUND DEFECTIVE. MAINTENANCE PLACED THE FAN ON DEFERRAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2001110600013 20011106 00013 SW 2001 11 6 2001F00612 1 20010823 A 6510 407340340101 DISC PACK BELL 407 407 1182206 SW TAIL ROTOR CRACKED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 547AL 53240 DURING 25 HOUR AD INSPECTION, THE COUPLING IS CRACKED, PROBABLE CAUSE IS EXCESSIVE RIGIDITY IN THE BEARING MOUNT SYSTEM. ALLOW TAILROTOR DRIVESHAFT TO FLOAT SO DISC PACKS DO NOT FLEX AS MUCH OR AS OFTEN. (M) 1 G 7 1 3U O H2SW 2001110600014 20011106 00014 SW 2001 11 6 2001F00613 1 20010824 A 6510 407340339103 BEARING BELL 407 407 1182206 SW TAIL ROTOR DISINTEGRATED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 587AL 53248 DURING DAILY, BEARING ON THE SHAFT WAS DISINTEGRATED DUE TO LOSS OF GREASE. BEARING WAS SCRAPPED AND C/W ASB 407-01-44. (M) 1 G 7 1 3U O H2SW 2001110600015 20011106 00015 SW 2001 11 6 2001F00614 1 20010820 A 6510 407340340103 DISC PACK BELL 407 407 1182206 SW TAIL ROTOR CRACKED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 697AL 53374 DAILY INSPECTION OF TAILROTOR DRIVESHAFT BEARINGS FOR OVERHEATING. NR 4 TAILROTOR DISC, (ONE) FORWARD IS CRACKED, PROBA BLE CAUSE IS EXCESSIVE RIGIDITY IN THE BEARING MOUNT SYSTEM. ALLOW THE TAILROTOR DRIVESHAFT TO FLOAT SO DISC PACKS DO N OT FLEX AS MUCH OR AS OFTEN. (M) 1 G 7 1 3U O H2SW 2001110600016 20011106 00016 SW 2001 11 6 2001F00615 1 20010820 A 6510 407040302107 DISC PACK BELL 407 407 1182206 SW TAIL ROTOR CRACKED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 627AL 53284 DURING 25 HOUR INSPECTION, COUPLING IS CRACKED, PROBABLE CAUSE IS EXCESSIVE RIGIDITY IN THE BEARING MOUNT SYSTEM. ALLOW TAILROTOR DRIVESHAFT TO FLOAT SO DISC PACKS DO NOT FLEX AS MUCH OR AS OFTEN. (M) 1 G 7 1 3U O H2SW 2001110600017 20011106 00017 EU 2001 11 6 AWXA200100566 1 20011102 A 3610 IAE A1 AIRBUS 320 A320231 3930325 EU A AWXA A O UNSCHED LANDING OTHER J O WARNING INDICATION OTHER CR CRUISE 1 WP 28 621AW V0075 053 PHX - DIVERTED FLIGHT - FLT 613 - "C" - ON LEVEL OFF AT FL 370 ENROUTE FROM LAS TO ATL, ECAM MESSAGE APPEARED FOR LEFT P ACK OVER PRESSURE FOLLOWED BY #2 BLEED OVER PRESSURE FAULT. CREW WAS UNABLE TO CONTROL CABIN PRESS AND DESCENDED TO FL 2 00 WHERE THEY REGAINED CONTROL OF CABIN PRESS. THE AIRCRAFT DIVERTED TO PHX MAKING AN UNEVENTFUL LANDING. MAINTENANCE TR OUBLESHOT AND FOUND THE #1 ENG PRV DOWN STREAM LINE LEAKING DUE TO BEING CROSS THREADED. REPLACED TUBE AND HOSE ASSEMBLI ES. #1 ENG TLT WAS FOUND LEAKING AT THE INLET UNION AND WAS REPLACED. ALSO THE R/H POTABLE WATER PRESS SUPPLY LINE CHECK VALVE WAS FOUND TO BE BAD ALLOWING PRESS TO THE #2 SIDE OF THE CROSS BLEED VALVE, APPROXIMATELY 14 TO 16 PSI. THE CHECK 2 L 7 2 4F RT A28NM 2001110600018 20011106 00018 SW 2001 11 6 2001F00617 1 20010824 A 6510 BEARING BELL 407 407 1182206 SW TAIL ROTOR DISINTEGRATED B ALGR O OTHER E VIBRATION/BUFFET CR CRUISE 1 SW 03 457AL 53151 AFTER 2 HOURS OF FLIGHT AIRCRAFT EXPERIENCED INTERMITTENT MEDIUM FREQUENCY VIBRATION SUBSEQUENT INSPECTION REVEALED THE BEARING FAILURE OF NR 2 TAILROTOR DRIVESHAFT. FORWARD BEARING ON SHAFT DISINTEGRATED DUE TO LOSS OF GREASE. BEARING SC RAPPED AND C/W ASB 407-01-44. (M) 1 G 7 1 3U O H2SW 2001110600019 20011106 00019 SW 2001 11 6 2001F00618 1 20010821 A 5320 PANEL BELL 407 407 1182206 SW FUSELAGE CRACKED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 527AL 53211 UPON DAILY, OIL COOLER DECK P/N IS CRACKED IN FORWARD SIDE AT STATION 192-204. (M) 1 G 7 1 3U O H2SW 2001110600020 20011106 00020 SW 2001 11 6 2001F00619 1 20010820 A 5320 407030734103A PANEL BELL 407 407 1182206 SW FUSELAGE CRACKED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 1116H 53046 UPON DAILY, OIL COOLER DECK P/N 407-030-734-103A IS CRACKED ON FORWARD SIDE AT STATION 192-204. (M) 1 G 7 1 3U O H2SW 2001110600021 20011106 00021 SW 2001 11 6 2001F00620 1 20010927 A 6310 406040516101 SHAFT BELL 407 407 1182206 SW FREEWHEEL UNIT WORN A ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 617AL 53265 AT OVERHAUL, DRIVE SPLINES WORN BELOW MINIMUM LIMITS. (M) 1 G 7 1 3U O H2SW 2001110600022 20011106 00022 EU 2001 11 6 2001F00533 1 20010320 A 8010 845UN01Q4AA5F SWITCH SNIAS 350 AS350B3 8680954 EU STARTER FAILED A R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 103LN 898 3128 SWITCH IS INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 1 3U H9EU 2001110600023 20011106 00023 EU 2001 11 6 2001F00534 1 20010814 A 8010 845UN01Q4AA5F SWITCH SNIAS 350 AS350B3 8680954 EU STARTER FAILED A R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 397LG 80 3268 SWITCH IS INOPERATIVE. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M) 1 G 7 1 3U H9EU 2001110600024 20011106 00024 EU 2001 11 6 2001F00535 1 20010225 A 3340 356H2802 POWER SUPPLY SNIAS 350 AS350B3 8680954 EU EXTERIOR LIGHT INOPERATIVE A R7MA K NONE L NO TEST NR NOT REPORTED 1 NM 07 52281 585 3249 POWER SUPPLY BOX INOPERATIVE. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M) 1 G 7 1 3U H9EU 2001110600025 20011106 00025 EU 2001 11 6 2001F00536 1 20010511 A 6230 350A37112602 LINK SNIAS 350 AS350B2 8680813 EU SWASHPLATE WORN A R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 96LG 821 2817 UPPER EQUIPPED SCISSOR LINK WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M) 1 G 7 1 3U H9EU 2001110600026 20011106 00026 2001 11 6 2001F00537 4 20010813 A 3120 B1894522282A CLOCK SNIAS 350 AS350B3 8680954 EU INSTRUMENT PANEL INOPERATIVE A R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 397LG 23 3268 CLOCK IS INOPERATIVE. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M) 1 G 7 1 3U H9EU 2001111400022 20011114 00022 NM 2001 11 14 01FDEA00956 1 20011021 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 279FE 22346 CORROSION ON LOWER CHORD OF FLOORBEAM AROUND NUT PLATE HOLES. REMOVED AND REPLACED FLOORBEAM PER EA 7-5310-59894. 2 L 7 3 4F RT A3WE 2001110600027 20011106 00027 NM 2001 11 6 01FDEA00958 1 20011026 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 279FE 22346 CORROSION ON FLOORBEAM BS 1970, LBL 45, WL 208. 2 L 7 3 4F RT A3WE 2001111400023 20011114 00023 NM 2001 11 14 01FDEA00965 1 20011106 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 279FE 22346 CORROSION (C53-224-01, 1) ON TOP OF FLOORBEAM AT FASTENER HOLES BS 312, LBL 3 TO LBL 50, WL 208. REMOVED AND REPLACED F LOORBEAM PER SRM 53-10-8, FIG 9. 2 L 7 3 4F RT A3WE 2001110600028 20011106 00028 SW 2001 11 6 2001F00539 1 20010713 A 6730 222382001103 ACTUATOR BELL 222 222UT 1182148 SW MAIN ROTOR LEAKING A R7MA O OTHER K FLUID LOSS NR NOT REPORTED 1 NM 07 404EM 407 47514 DUAL HYDRAULIC SERVO ACTUATOR LEAKING BEYOND SERVICEABLE LIMITS. LOWER BEARING BECAME UNSTAKED. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M) 1 G 7 2 3U H9SW 2001110600029 20011106 00029 NE 2001 11 6 2001F00549 2 20010215 A 7421 9550168770 IGNITER SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE ENGINE WORN A R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 103LN 888 3128 IGNITER WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 1 3U 3 U H9EU E00054EN 2001110600030 20011106 00030 NE 2001 11 6 2001F00551 2 20010327 A 7412 9550173220 EXCITER SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE ENGINE INOPERATIVE A R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 52285 584 3251 IGNITION EXCITER INOPERATIVE. ENGINE FAILS TO START. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 1 3U 3 U H9EU E00054EN 2001110600031 20011106 00031 SO 2001 11 6 C2XA01CL219 1 20011031 A 5542 12061385009 SKIN EMB 145 EMB145LR 3260212 SO RUDDER CRACKED A C2XA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 SW 27 13908 741 145465 DURING OVERNIGHT MAINTENANCE RUDDER II SKIN WAS FOUND TO BE CRACKED 8 INCHES LONG AND ALSO HAD A I 1/4 INCH HOLE IN IT. THE CRACK STARTED APPROX 4 INCH FROM THE BOTTOM OF THE RUDDER. THE CRACK FOLLOWED THE TRAILING EDGE. MAINTENANCE REMOVED AND REPLACED RUDDER II OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001110600032 20011106 00032 SO 2001 11 6 C2XA01CL220 1 20011029 A 2120 ODOR EMB 145 EMB145LR 3260212 SO CABIN DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 13955 145075 CLE FLIGHT NR 4247 THE CREW REPORTED A STRONG FUEL SMELL EACH TIME THE APU WAS STARTED. MAINTENANCE INSPECTED AND PERFOR MED OPERATIONAL CHECKS OF APU WITH THE BLEED SYSTEM ON AND NO FUEL SMELL WAS NOTED.THE AIRCRAFT WAS RELEASED FOR SERVICE . 2 L 7 2 4T RT T00011AT 2001110600033 20011106 00033 SO 2001 11 6 C2XA01CL221 1 20011030 A 2530 CBC16707 RECEPTACLE EMB 135 EMB135ER 3260203 SO GALLEY BURNED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 14505 145192 CLE FLIGHT NR 3898 THE CREW REPORTED A BURNING SMELL COMING FROM THE COFFEE WARMERS WHEN EVER THEY WERE ON.MAINTENANCE I NSPECTED AND REPLACED THE RECEPTACLE PLUG FOR THE WARMER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SE RVICE. 2 L 7 2 4F RT T00011AT 2001110600034 20011106 00034 SO 2001 11 6 C2XA01CL222 1 20011102 A 2611 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO LAVATORY DIRTY A C2XA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 27 13978 145180 CLE FLIGHT NR 3323 THE CREW REPORTED SMOKE IN CABIN AND COCKPIT ALONG WITH A LAV SMOKE INDICATION. THE CREW DECLARED A E MERGENCY AND RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND CLEANED DEBRIS FROM LA V SMOKE DETECTOR. THE DEBRIS WAS LINT AND DUST. OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001110600035 20011106 00035 SO 2001 11 6 C2XA01CL224 1 20011102 A 3350 110049 CHARGER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13955 145075 DURING ROUTINE MAINTENANCE THE SERVICE DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D THE NR 1 BATTERY CHARGER AND REPAIRED WIRING IN SERVICE DOOR FOR THE LIGHT. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001110600036 20011106 00036 SO 2001 11 6 C2XA01CL225 1 20011104 A 3350 7287103507 MODULE EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 15910 244 145455 CLE FLIGHT NR 3117 THE CREW REPORTED THE EMERGENCY LIGHTS ILLUMINATE WHEN THE SWITCH IS IN THE ARMED POSITION. MAINTENAN CE INSPECTED AND REPLACED THE LIGHT CONTROL MODULE.OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001110600037 20011106 00037 EU 2001 11 6 C2XA01IA381 1 20011021 A 3260 D22924010 CONNECTOR AEROSP ATR42 ATR42320 8680930 EU LT MLG DIRTY A C2XA K NONE O OTHER AP APPROACH 1 SW 27 14834 193 SHV FLIGHT 3340 - CREW REPORTED THAT THERE WAS NOT ANY GEAR INDICATION FOR SYSTEM 2. THE AIRCRAFT LANDED AT SHV WITHOUT INCIDENT WHERE MAINTENANCE CLEANED THE LEFT MLG DOWNLOCK CANNON PLUG AND PERFORMED AN OPERATIONAL CHECK OF THE GEAR INDI CATION SYSTEM. THE AIRCRAFT OPERATIONALLY CHECKED GOOD AND WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001110600038 20011106 00038 SO 2001 11 6 C2XA01IA383 1 20011023 A 2120 ODOR EMB 145 EMB145LR 3260212 SO CABIN DETECTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 13955 145075 CLE FLIGHT 3928 - CREW REPORTED THAT A STRONG ODOR OF FUEL WAS PRESENT AFTER THE APU WAS STARTED. THE APU WAS PLACED ON MEL AND THE AIRCRAFT DISPATCHED FOR SERVICE. ON 10/23/2001 IN BNA, MAINTENANCE PERFORMED GROUND RUNS OF THE APU WITH THE LEFT AND RIGHT ENVIROMENTAL SYSTEMS OPERATING AND COULD NOT DETECT ANY FUEL SMELL. THE APU WAS REMOVED FROM MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001110600039 20011106 00039 SO 2001 11 6 C2XA01IA384 1 20011025 A 3350 744437 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14993 145289 DURING SCHEDULED MAINTENANCE THE LEFT EMERGENCY EXIT SIDEWALL LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001110600040 20011106 00040 SO 2001 11 6 C2XA01IA391 1 20011024 A 2530 CBC16707 RECEPTACLE EMB 145 EMB145LR 3260212 SO GALLEY BURNED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 14993 3470 145289 IAH- THE CREW NOTED A ELECTRIC SMELL FROM THE GALLEY HOT JUG AREA. MAINTENANCE INSPECTED THE AIRCRAFT, AND, THE AIRCRA FT WAS RELEASED IAW MEL. MAINTENANCE C-CHECK, REMOVED AND REPLACED RECEPTACLE CONNECTORS AT AFT GALLEY AREA, PERFORMED A OPERATIONAL CHECK OF THE HOT JUG SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001110600041 20011106 00041 SO 2001 11 6 C2XA01IA392 1 20011025 A 5315 14521713003 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13994 3372 145291 IAH- DURING 1C INSPECTION IT WAS NOTED THAT THE LEFT FLOOR BEAM AT FRAME 20 WAS CORRODED. C CHECK MAINTENANCE REPAIRED THE FLOOR BEAM IAW EMB 145 SRM 53-21-10,AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001110600042 20011106 00042 SO 2001 11 6 C2XA01TY 1 20011029 A 5230 14522493003 SKIN EMB 135 EMB135ER 3260203 SO CARGO DOOR CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16510 145251 TYS DURING A SCHEDULED 1C INSPECTION,THE CARGO DOOR SKIN WAS FOUND CHAFED AROUND THE HANDLE CUTOUT. MAINTENANCE BLENDED OUT THE AREA IAW EC5230-01068--5120-04--5120-05 AND 5120-06. ALL WORK WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETIO N OF THE SCHEDULED MAINTENANCE. 2 L 7 2 4F RT T00011AT 2001110600043 20011106 00043 SO 2001 11 6 C2XA01TY169 1 20011029 A 5320 14534818001 FLOOR SUPPORT EMB 135 EMB135ER 3260203 SO FUSELAGE BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16510 145251 TYS DURING A SCHEDULED INSPECTION A FAIRLEAD FLOOR SUPPORT AT THE CENTER OMEGA BEAM WAS FOUND BROKEN AT FR21. MAINTENANC E R/R THE FAIRLEAD FLOOR SUPPORT AND THE WORK WAS FOUND SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION O F ALL SCHEDULED MAINTENANCE. 2 L 7 2 4F RT T00011AT 2001110600044 20011106 00044 SO 2001 11 6 C2XA01TY170 1 20011029 A 5312 SD40ALPSA FIREWALL EMB 135 EMB135ER 3260203 SO FUSELAGE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16510 145251 TYS DURING A SCHEDULE 1-C INSPECTION,MAINTENANCE FOUND A HOLE RUBBED INTO THE FIREWALL BLANKET. MAINTENANCE USED EC5330 -01166 FOR THE REPAIR. ALL WORK WAS DONE IAW THE EC AND AIRCRAFT WILL BE RELEASED UPON COMPLETION OF ALL SCHEDULE MAINTE NANCE. 2 L 7 2 4F RT T00011AT 2001110600045 20011106 00045 SO 2001 11 6 C2XA01TY171 1 20011029 A 5230 14522493003 SKIN EMB 135 EMB135ER 3260203 SO CARGO DOOR CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16510 145251 TYS DURING A SCHEDULED 1C INSPECTION,THE CARGO DOOR SKIN WAS FOUND CHAFED AROUND THE HANDLE CUTOUT. MAINTENANCE BLENDED OUT THE AREA IAW EC5230-01068--5120-04--5120-05 AND 5120-06. ALL WORK WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETIO N OF THE SCHEDULED MAINTENANCE. 2 L 7 2 4F RT T00011AT 2001110600047 20011106 00047 SO 2001 11 6 C2XA01CL226 1 20011105 A 2611 3601133500230 FIRE LOOP EMB 145 EMB145 3260210 SO #1 ENGINE BROKEN A C2XA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 27 13958 145085 CLE FLIGHT#3011 THE CREW REPORTED ON TAXI OUT THEY RECEIVED A #1 ENGINE FIRE DETECT FAIL MESSAGE ON THE ECIAS.THE AIRCRA FT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE #1 ENGINE FIRE DETECTOR LOOP.OPE RATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001110600051 20011106 00051 NM 2001 11 6 UPS01237210 1 20011018 A 2760 ROD BOEING 727 72722C 138400F NM NR 7 SPOILER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE:C O/B TENSION TIE ROD FOR NR 7 SPOILER O/B HINGE BRACKET CRACKED. TIE ROD FOR NR 7 SPOILER REPLACED IAW MM 20-80-01 2 L 7 3 4F A3WE 2001110600052 20011106 00052 NM 2001 11 6 UPS01237211 1 20011017 A 2710 LEVER BOEING 727 72722C 138400F NM LT MLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE:C LT W/W AILERON PCU, LINKAGE/CRANK TO TAB DRUM IS BADLY PITTED. LEVER ASSY REMOVED IAW OHM 27-17-01, N EW LEVER ASSY INSTALLED IAW OH M 27-17-01 FASTENERS INSTALLED IAW SRM 51-30-02 2 L 7 3 4F A3WE 2001110600053 20011106 00053 NM 2001 11 6 UPS01237215 1 20011018 A 5755 HINGE BRACKET BOEING 727 72722C 138400F NM NR 7 SPOILER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE:C NR 7 SPOILER I/B HINGE BRACKET CRACKED. BRACKET REPLACED IAW SRM 51-30-02 & DRAWING 65-98296 2 L 7 3 4F A3WE 2001110600054 20011106 00054 NM 2001 11 6 UPS01237238 1 20011018 A 3350 LIGHT BOEING 727 72722C 138400F NM ENTRY DOOR INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE:C FWD ENTRY DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED FWD ENTRY DOOR EMERG EXIT LIGHT AS PER MM 33-50-01 2 L 7 3 4F A3WE 2001110600055 20011106 00055 NM 2001 11 6 UPS01237239 1 20011022 A 5521 HINGE BOEING 727 72722C 138400F NM ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE:C NR 5 BALANCE PANEL RT ELEV ATTACH HINGE CRACKED AT O/B MOST HINGE SEGMENT. HINGE HALF REPLACED IAW MM 20-80-02 2 L 7 3 4F A3WE 2001111400149 20011114 00149 NM 2001 11 14 UPS01437244 1 20011031 A 5312 BULKHEAD BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 524UP INSPECTION TYPE:IN CRACK IN NOSE WHEEL WELL PRESS BULKHEAD. CRACK IN FRAME OF STATION 400 AFT SIDE PRESSURE BULKHEAD BWL 118 LT OF CENTER 22.5 INCH. PERFORMED OPEN HOLE HFEC OF THE 4 HOLES COMMON TO THE AFT WALL AND STIFFENER AT CRACKED HO RZ FRAME PER BOEING. NO CRACKS AT HOLES NOTED CRACK IS IN HORZ SECTION AND EXTENDS TO RADIUS BUT NOT BEYOND TO UPPER FA STENER HOLE. ACCOMPLISHED EO B747-5310-15648 APPENDIX A AS REQUIRED. 2 L 7 4 4F RT A20WE 2001110600056 20011106 00056 WP 2001 11 6 UPS01837202 1 20011014 A 5320 ANGLE DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 UPPER FUSELAGE ANGLE AT BASE OF VERTICAL STAB AT STA 1723.076 CANTED FRAME IS CORRODED BEYOND LIMITS CUT OUT CORRODED AREA,NDT CUTOUT,NO CRACKS NOTED FABRICATED AND INSTALLED FILLER AND REPAIR ANGLE IAW SRM 53-2-5 FI G 16A. 2 L 7 4 4F RT 4A25 2001110600057 20011106 00057 WP 2001 11 6 UPS01837203 1 20011018 A 5320 3619434505N SPLICE DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 STA 190 LONG 36 SPLICE FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 36194 34,AND SRM. 51-1-20D. 2 L 7 4 4F RT 4A25 2001110600058 20011106 00058 WP 2001 11 6 UPS01837204 1 20011018 A 5320 3757794502 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 STA 280 ST LONG 32R TO 33R CORNER T-FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3757794,AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001110600059 20011106 00059 WP 2001 11 6 UPS01837205 1 20011014 A 5320 ANGLE DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 UPPER FUSELAGE RIGHT SIDE ANGLE AT BASE OF VERTICAL STAB IS CORRODED BEYOND LIMITS AT STA 1722. CUT OUT CORRODED AREA, NDT AT CUTOUT,NO CRACKS NOTED,FABRICATED AND INSTALLED FILLER AND REPAIR DOUBLER IAW SRM 53-2-5 FIG 1 6A. 2 L 7 4 4F RT 4A25 2001110600060 20011106 00060 WP 2001 11 6 UPS01837206 1 20011016 A 5320 5894282501 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 STA 1210 LONG 33R BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 589 4282,AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001110600061 20011106 00061 WP 2001 11 6 UPS01837207 1 20011015 A 5320 37558271N FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 STA 340 LONG 33R BANANA FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 37558 27,AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001110600062 20011106 00062 WP 2001 11 6 UPS01837208 1 20011015 A 5330 5645332127 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 STA 883 BL 0 UPPER SURFACE OF WHEEL WELL PRESSURE WEB HAS A FINGER DOUBLER CORRODED BEYOND LIMITS REMOVED,FABRICATED,AND REPLACED DOUBLER IAW DWG 5645332,AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001110600063 20011106 00063 WP 2001 11 6 UPS01837209 1 20011017 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 FINGER DOUBLER AND SKIN IS CORRODED BEYOND LIMITS STA 1350 LONG 34L-35L. REMOVED, FABRICATED, AND REP LACED DOUBLER IAW DWG 5779915, CUTOUT CORRODED AREA, NDT FOR CRACKS, NO CRACKS NOTED, FABRICATED AND INSTALLED FILLER, D OUBLER, AND FINGER DOUBLERS IAW SRM 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 2001110600064 20011106 00064 WP 2001 11 6 UPS01837222 1 20011015 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 A-PIT DOOR OPENING FWD LOWER CORNER SKIN IS GOUGED AND CRACKED AT STA 280 LONG 31R-32R APPROX. CUT OU T DAMAGED AREA, NDT FOR CRACKS AT CUTOUT, NO CRACKS NOTED, FABRICATED AND INSTALLED FILLER, DOUBLER, AND TRIPLER IAW SRM 53-2-0 FIG 20 AND SRO8530019. 2 L 7 4 4F RT 4A25 2001110600065 20011106 00065 WP 2001 11 6 UPS01837223 1 20011016 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 L-1 DOOR LOWER AFT CORNER DOUBLER DOES NOT CONFORM TO SRM 53-2-0, AND SKIN IS CRACKED AT STA 55 LONG 21L AREA. CUT OUT CRACKED AREA, NDT VERIFIED NO CRACKS AROUND CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FIL LER IAW SRM 53-2-0 FIG 15. 2 L 7 4 4F RT 4A25 2001110600066 20011106 00066 WP 2001 11 6 UPS01837224 1 20011014 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 FUSELAGE SKIN IS CRACKED AT STA 1723.076 LONG 15R. CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS AROUND CUTOUT, FABRICATED AND INSTALLED DOUBLER, FINGER DOUBLERS, AND FILLERS IAW SRM 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 2001110600067 20011106 00067 WP 2001 11 6 UPS01837225 1 20011016 A 5320 3755847U501 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 STA 1152 LONG 33R BANANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755847, AND SRM 51 -1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001110600068 20011106 00068 WP 2001 11 6 UPS01837226 1 20011017 A 5320 4758514507 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 STA 1240 LONG 33R I/B INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IA W DWG 4758514, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001110600069 20011106 00069 WP 2001 11 6 UPS01837227 1 20011015 A 5320 37558272N FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 STA 280 LONG 33R O/B BANANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755827, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001110600070 20011106 00070 WP 2001 11 6 UPS01837228 1 20011017 A 5320 4758514512 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 STA 1260 LONG 33R O/B AFT SIDE INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IA W DWG 4758514, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001110600071 20011106 00071 WP 2001 11 6 UPS01837233 1 20011013 A 5230 SKIN DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 NR 1 (A-PIT) CARGO DOOR SKIN IS DAMAGED AT LOWER AFT CORNER AT STA 330 LONG 32R. CUT OUT CRACKED AREA , NDT VERIFIED NO CRACKS AT CUT OUT, FABRICATED AND INSTALLED FILLER DOUBLER, AND SHIM IAW SRM 52-2-3 FIG 10A. 2 L 7 4 4F RT 4A25 2001110600072 20011106 00072 WP 2001 11 6 UPS01837234 1 20011016 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 INTERCOSTAL IS CRACKED AT STA 1435 BL 0 ABOVE D-PIT DOOR. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1D. 2 L 7 4 4F RT 4A25 2001110600073 20011106 00073 WP 2001 11 6 UPS01837235 1 20011016 A 5320 3755843501N FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 STA 1220 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG 34R TO 35R. REMOVED AND REPLACED FITT ING IAW DWG 3755843, AND SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 2002032900141 20020329 00141 NE 2002 3 29 AWXA200100565 2 20011102 A 7230 2A1165 BEARING AIRBUS A319 A319132 3930340 NM IAE V2524 V2524A5 NE NR 1 ENGINE FRACTURED A AWXA B A EMER. DESCENT UNSCHED LANDING J E B WARNING INDICATION VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 814AW 1281 V10778 EN ROUTE ECAM MESSAGE FOR NR 1 ENG OIL FILTER CLOG APPEARED, FOLLOWED BY NR 1 ENG OIL PRESSURE RISE INTO THE RED AREA, N R 1 ENG HIGH VIBRATION & SMOKE IN THE CABIN. EXECUTED EMERGENCY DESCENT & LANDED AT MAF. MX REMOVED MAIN OIL FILTER & CHIP DETECTORS AND FOUND THEM CONTAMINATED WITH METALIC DEBRIS, ENG WAS REMOVED. TEAR DOWN OF NR 1 ENGINE REVEALED NR 3 BEARING FRACTURE AS CAUSE OF INCIDENT. NR 3 BEARING OUTER RING WAS FRACTURED AND EXHIBITED SIGNS OF RACEWAY SPALLING W ITH OUTSIDE DIAMETER OF OUTER RING DISPLAYING SIGNS OF LOCALIZED FRETTING, FRACTURE INITIATED FROM OUTSIDE DIAMETER FRET TING AREA. 2 L 7 2 4F 4 F RT A28NM E40NE 2001110600074 20011106 00074 EA 2001 11 6 COMA0160870 1 20011104 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING FAULTY A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 943CA 15247 7062 FLAW INDICATION WERE NOTED BY EDDY CURRENT METHOD AT LOWER WING SURFACE ACCESS OPENINGS AT 640 EB W/S 116.366, 640 CB W. S. 76.161 AND 640 EB W.S. 116.366, 540 AB W.S. 56.68.BLENDED DAMAGE AT 4 ACCESS PANEL CUT OUTS I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2001110600075 20011106 00075 EA 2001 11 6 COMA0160871 1 20011029 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 943CA 15247 7062 OVERWING SKIN CRACKED ON FUSELAGE AT STA F.S.520.00 TO F.S. 528.7.REPAIRED BY REMOVING DAMAGE AND INSTALLING DOUBLERS I/ A/W REO 601R-53-51-069. 2 L 7 2 4F RT A21EA 2001110600076 20011106 00076 EA 2001 11 6 COMA0160872 1 20011104 A 5346 60135006 WEB CNDAIR CL600 CL6002B19 1900309 EA BEAM CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 943CA 15247 7062 ENGINE SUPPORT BEAM CRACKED ON UPPER WEB.CUT OUT DAMAGE SECTION AND INSTALLED TEMPORARY REPAIR TO UPPER AND LOWER WEB. I/A/W REO 601R-53-61-345. 2 L 7 2 4F RT A21EA 2001110600077 20011106 00077 EA 2001 11 6 COMA0160873 1 20011104 A 5346 60135006 WEB CNDAIR CL600 CL6002B19 1900309 EA AFT EQUIP BAY CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 943CA 15247 7062 ENGINE SUPPORT BEAM CRACKED AT THE LEFT AND RIGHT LOWER WEB ACCESS PANEL.CUT OUT DAMAGE AND INSTALLED REPAIR TO LEFT AND RIGHT LOWER WEB I/A/W REO 601R-53-61-366. 2 L 7 2 4F RT A21EA 2001110600078 20011106 00078 EA 2001 11 6 COMA0160874 1 20011105 A 2710 601R5122623 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A COMA O OTHER S F AFFECT SYSTEMS FLT CONT AFFECTED CR CRUISE 1 SO 01 807CA 7364 FLIGHT #5464. AILERON TRIM WOULD NOT WORK.REPLACED THE TRIM CONTROL PANEL. 2 L 7 2 4F RT A21EA 2001110600079 20011106 00079 EA 2001 11 6 COMA0160875 1 20011105 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 940CA 7048 FLIGHT #5872. FLAPS FAILED WHEN SELECTED FOR APROACH.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2001110600080 20011106 00080 WP 2001 11 6 MWEA011408 1 20011026 A 7711 LG80AZ TRANSMITTER DOUG DC9 DC932 3022066 WP LT ENGINE FAILED A MWEA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 31 215ME 47744 AT FL330 THE LEFT ENGINE EPR GAUGE FROZE, ALL OTHER INDICATIONS NORMAL - N1, N2, EGT. CHECKED PT2 AND PT7 LINES FOR BLOC KAGE AND LEAK CHECKED FROM ENGINE TO TRANSMITTER, REFERENCE DC9 MAINTENANCE MANUAL 77-11-0. MEGGED ALL WIRES, DID A THOR OUGH INSPECTION OF CONNECTORS AND NO DEFECT NOTED IN ACCORDANCE WITH MAINTENANCE MANUAL 77-11-00. REPLACED LEFT ENGINE P RESSURE RATIO CIRCUIT BREAKER AND TRANSMITTER. OPERATION CHECK GOOD. 2 L 7 2 4F A6WE 2001110600081 20011106 00081 NM 2001 11 6 MWEA011409 1 20011028 A 3610 39271012 CLAMP DOUG MD88 MD88 3023688 NM RT ENGINE LEAKING A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 601ME 49762 TAIL COMPARTMENT TEMPERATURE HIGH ANNUNCIATOR CAME ON AND ISOLATED PROBLEM TO RIGHT ENGINE. RESEATED AND RETORQUED AUGM ENTATION VALVE "V" BAND CLAMP. OPS AND LEAK CHECK GOOD. 2 L 7 2 4F RT A6WE 2001110600082 20011106 00082 WP 2001 11 6 MWEA011410 1 20011030 A 5320 993658091 INTERCOSTAL DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 INTERCOSTAL BEAM FUSELAGE STATION 218-237 BETWEEN SEAT TRACK NR 1 AND NR 2 REQUIRES REMOVAL. REMOVED, DRILLED AND LOCATE D NEW INTERCOSTAL. 2 L 7 2 4F A6WE 2001110600083 20011106 00083 WP 2001 11 6 MWEA011411 1 20011030 A 5330 5912285515 DOUBLER DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 TWO AREAS OF CRACKS AROUND FASTENERS ON WINDOW INNER DOUBLER AT STATION 654 LOWER RIGHT CORNER AND AT STATION 643 UPPER LEFT CORNER OF DOUBLER. FABRICATED AND INSTALLED DOUBLERS. 2 L 7 2 4F A6WE 2001110600084 20011106 00084 WP 2001 11 6 MWEA011413 1 20011030 A 5313 591022829 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 STATION 1087 LONGERON 7 LEFT IS CRACKED. REMOVED, FABRICATED AND INSTALLED LONGERON. 2 L 7 2 4F A6WE 2001110600085 20011106 00085 WP 2001 11 6 MWEA011414 1 20011030 A 5313 591022830 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 STATION 1087 LONGERON 7 RIGHT IS CRACKED. FABRICATED AND INSTALLED NEW LONGERON AND LONGERON SPLICE. 2 L 7 2 4F A6WE 2001110600086 20011106 00086 WP 2001 11 6 MWEA011415 1 20011101 A 5313 591142347 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 CORROSION ON LONGERON 21 LEFT AT STATION 990 AFT PIT. BLENDED, DRILLED, LOCATED AND INSTALLED NEW LONGERON. 2 L 7 2 4F A6WE 2001110600087 20011106 00087 WP 2001 11 6 MWEA011416 1 20011101 A 5320 591142375 STRAP DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 CORROSION ON STRAP IN LONGERON 23 LEFT AT STATION 945 AFT PIT. BLENDED, FABRICATED AND INSTALLED LONGERON. 2 L 7 2 4F A6WE 2001110600088 20011106 00088 WP 2001 11 6 MWEA011417 1 20011102 A 5320 991224314 CLIP DOUG DC9 DC915 3022036 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 RIGHT LAVATORY HAS A CRACKED SHEAR CLIP AT STATION 786. FABRICATED AND INSTALLED SHEAR CLIP. 2 L 7 2 4F A6WE 2001110600089 20011106 00089 WP 2001 11 6 MWEA011419 1 20011106 A 5230 LATCH DOUG DC9 DC914 3022034 WP CARGO DOOR UNSECURE A MWEA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 600ME 45725 AFTER TAKE OFF, AIRCRAFT WOULD NOT PRESSURIZE IN AUTO OR MANUAL WITH GOOD PACK PRESSURES. REMOVED DEBRIS IN AFT PORTION OF FWD CARGO DOOR. THE AFT LATCH WAS NOT SECURED ON FWD CARGO DOOR. 2 L 7 2 4F A6WE 2001110600098 20011106 00098 NM 2001 11 6 SWAA012933 1 20011026 A 3350 1000679 LIGHT BOEING 737 7373H4 1384600 NM COCKPIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED C3 CHECK, FOUND COCKPIT EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001110600099 20011106 00099 NM 2001 11 6 SWAA012934 1 20011024 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. R&R STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2001110600100 20011106 00100 NM 2001 11 6 SWAA012936 1 20011026 A 5320 6517582 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 382SW 26588 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL STIFFENER WEB CRACKED AT BS 178, RBL 17.1, WL 234. REPAIRED STIFFENER PER S RM. 2 L 7 2 4F RT A16WE 2001110600101 20011106 00101 NM 2001 11 6 SWAA012938 1 20011027 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 382SW 26588 DURING SCHEDULED 1/4D CHECK, FOUND FLOOR BEAMS CORRODED ( 2 EA ) AT BS 910, RBL 14 & BS 945, LBL 17. REPAIRED FLOOR BEAM S PER SRM. 2 L 7 2 4F RT A16WE 2001110600102 20011106 00102 2001 11 6 SWAA012942 4 20011028 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001110600103 20011106 00103 NM 2001 11 6 SWAA012943 1 20011027 A 5753 6546435 FLAP BOEING 737 7372H4 138448C NM LT WING DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED SERVICE CHECK, FOUND LT OTBD AFT FLAP, INBD BELL CRANK BROKEN & FOLLOW UP TRACK WORN. R&R BELL CRANK & T/E FLAP ASSY. 2 L 7 2 4F A16WE 2001110700001 20011107 00001 NM 2001 11 7 SWAA012994 1 20011101 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM UPPER FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED BC4 CHECK, FOUND FUSELAGE SKIN CRACKED 3.75 INCHES, BS 522, STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001110700002 20011107 00002 NM 2001 11 7 SWAA012995 1 20011029 A 5330 589357 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 383SW 26589 DURING SCHEDULED 1/4D CHECK, FOUND CAPT'S UPPER WINDOW POST C/D SKIN CRACKED. REPAIRED WINDOW POST PER SRM. 2 L 7 2 4F RT A16WE 2001110700003 20011107 00003 NM 2001 11 7 SWAA012997 1 20011031 A 3350 101073 LENS BOEING 737 7373A4 1384585 NM FWD CABIN OBSTRUCTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT LIGHT LENS OBSTRUCTED AFT OF L1 DOOR. CLEANED LENS PER MM. 2 L 7 2 4F RT A16WE 2001110700004 20011107 00004 NM 2001 11 7 SWAA012998 1 20011030 A 5312 6517582 WEB BOEING 737 7373T5 1384608 NM FWD FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED SPECIAL VISIT, FOUND BS 179 VERTICAL BEAM WEB CRACKED, LBL 17.1, WL 225. R&R VERTICAL BEAM W EB PER SRM. 2 L 7 2 4F RT A16WE 2001110700005 20011107 00005 NM 2001 11 7 SWAA013000 1 20011103 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 728SW 27860 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER CRACKED AT ROW 17. R&R COVER PER MM. 2 L 7 2 4F RT A16WE 2001110700006 20011107 00006 NM 2001 11 7 SWAA013001 1 20011103 A 5753 6546434 FLAP BOEING 737 7373H4 1384600 NM RH WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 609SW 27929 DURING SCHEDULED C1 CHECK, FOUND RH INBD AFT FLAP DELAMINATED AT OTBD END. R&R FLAP PER MM. 2 L 7 2 4F RT A16WE 2001110700007 20011107 00007 NM 2001 11 7 SWAA013005 1 20011101 A 5312 6517582 WEB BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED ( 2 EA ) AT BS 180, RBL 17.1, WL 182 & WL 227. REPAIRED WEB PER SRM & SWA RA 1-353-2699. 2 L 7 2 4F RT A16WE 2001110700008 20011107 00008 NM 2001 11 7 SWAA013007 1 20011103 A 5312 6516300 WEB BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED ( 5 EA ) AT BS 178, RBL 5.0, WL 199 TO WL 218. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001110700009 20011107 00009 NM 2001 11 7 SWAA013012 1 20011105 A 5240 6545871 FRAME BOEING 737 7373H4 1384600 NM FWD SVC DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 380SW 26587 DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR AFT FRAME CRACKED AT CUTOUT 3RD STOP FROM BOTTOM. REPAIRED FRAME PER SWA T1-152-003. 2 L 7 2 4F RT A16WE 2001110700010 20011107 00010 NM 2001 11 7 SWAA013013 1 20011105 A 5310 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED ( 2 EA ) AT BS 328, STR 21R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001110700011 20011107 00011 NM 2001 11 7 SWAA013014 1 20011102 A 5310 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED ( 14 EA ) AT BS 520, STR 7R, 6R, 7L & 8L, BS 578, STR 8L & 8R, BS 597, STR 8L, BS 616, STR 4R, BS 727B, STR 3L & 3R, BS 727C, STR 3L, BS 727E, STR 3L, 3R & 2R. R&R STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001110700012 20011107 00012 NM 2001 11 7 SWAA013016 1 20011105 A 5330 6545890 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING WALK AROUND INSPECTION FOUND FUSELAGE SKIN CRACKED 2.2 INCH LONG AT BS 308, STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001110700013 20011107 00013 NM 2001 11 7 SWAA013019 1 20011104 A 5312 6516300 WEB BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 682SW 23496 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED ( 8 EA ) AT BS 178. REPAIRED BULK HEAD WEB PER SRM. 2 L 7 2 4F RT A16WE 2001110700014 20011107 00014 NM 2001 11 7 SWAA013020 1 20011104 A 5310 6517582 WEB BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 682SW 23496 DURING SCHEDULED SPECIAL VISIT, FOUND ( 2 EA ) VERTICAL BEAM WEBS CRACKED AT BS 178, WL 227 & WL 232, LBL 17.1 & RBL 17 .1. R&R WEBS PER SRM. 2 L 7 2 4F RT A16WE 2001110700015 20011107 00015 WP 2001 11 7 DHL2001801568 1 20011011 A 5101 4646547 FITTING DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 WING CNTR SECTION (MAIN CARGO COMT)FITTING CRACKED 1 IN AT STA 798.000,XCW 23L/H.REMOVED CRACKED FITTING PER SRM 51-120D PG 21.CLEANED TREATED AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2001110800082 20011108 00082 NM 2001 11 8 2001UALA02184 1 20011031 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 328UA 24148 CABIN STATION 344 AT STRINGER 11R STRINGER CLIP IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2001110800087 20011108 00087 EU 2001 11 8 2001UALA02191 1 20011031 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 460UA 1248 FUSELAGE SKIN DENTED AT FUSELAGE STATION 3320 BETWEEN STRINGER 3 AND 4 LEFT. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED HI GH FREQUENCY EDDY CURRENT TO AREA. NO CRACKS EXIST. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A28NM E40NE 2001110800092 20011108 00092 NM 2001 11 8 2001UALA02200 1 20011101 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 FUSELAGE DENT ON A STRINGER STATION 620 STRINGER 16L. MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW STRINGER AND INSTALLED EXTERNAL DOUBLER ON FUSELAGE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001110800093 20011108 00093 NM 2001 11 8 2001UALA02201 1 20011101 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 554UA 26644 STRINGER 16L DENTED AT STATION 613. MAJOR REPAIR ACCOMPLISHED. STRINGER SPLICE CHANNEL INSTALLED WITH SPACER WHERE STR INGER WAS REMOVED. 2 L 7 2 4F 4 F RT A2NM E17NE 2001110700016 20011107 00016 NM 2001 11 7 SWAA012944 1 20011024 A 5312 6546569 BULKHEAD BOEING 737 7377H4 1384404 NM FUSELAGE CANNING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 706SW 27840 DURING SCHEDULED A2 CHECK ( SI 11157-53 ), FOUND AFT PRESSURE BULKHEAD AFT SIDE OIL CANNED AT STR'S 3L, 5L, 7L & 9L. REPAIRED PRESS BULKHEAD PER SRM & SWA RA 1-753-2690. 2 L 7 2 4F RT A16WE 2001110700017 20011107 00017 NM 2001 11 7 SWAA012945 1 20011027 A 2910 AE706293 HYDRAULIC LINE BOEING 737 7373H4 1384600 NM NR 2 ENGINE RUPTURED A SWAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 643SW 27716 DECLARED EMERGENCY, B SYSTEM HYDRAULIC FLUID QUANTITY STARTED DECREASING FOLLOWED BY NR 2 ENG LOW PRESSURE LIGHT ILLUMIN ATING. QRH FOLLOWED & LANDING ACCOMPLISHED. FOUND HYD FLEX LINE BETWEEN ACOUSTIC FILTER & MODULAR PACKAGE RUPTURED. R&R LINE, HYD PUMP & FILTER PER MM. 2 L 7 2 4F RT A16WE 2001110700018 20011107 00018 WP 2001 11 7 0103829151 1 20010720 A 5310 DUCT DOUG DC9 DC914 3022034 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8909E 45770 During an aircraft overnight in MSP at gate G7, The electrical compartment exhaust duct outlet, common to the fuselage s kin was found with a crack. The crack length is approximately 1.00" and is in the lower transition from the skin contour to the duct exhaust contour. Repaired per EA 91-184952. 2 L 7 2 4F A6WE 2001110700019 20011107 00019 WP 2001 11 7 0103839612 1 20010731 A 5310 FRAME DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612NW 47436 During an Hck in Atl, a crack was found on the RH MLG door hinge support frame at sta 737. The crack stopped at a fasten er hole and is .5" long. Material 7075-t6, repaired per EA 96-181352. 2 L 7 2 4F A6WE 2001110700020 20011107 00020 WP 2001 11 7 0103849612 1 20010731 A 5520 ELEVATOR DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612NW 47436 During Hck in Atl the RH elevator skin at XET=167 was found cracked at the outboard end where the gear tab fairing is at tached . Doubler made of 2014-t6 elevator assembly 5910411-526 s/n 00397. Repaired per EA 96-185011. 2 L 7 2 4F A6WE 2001110700021 20011107 00021 WP 2001 11 7 0103859612 1 20010803 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612NW 47316 DURING AN HCK IN ATL, TWO CRACKS WERE FOUND IN THE VERTICAL WEB OF THE STA 237 FLOORBEAM. THE CRACKS ARE AT X=6 AND ARE APPROXIMATELY 1" LONG. THE CRACK ENDS ARE STOPPED DRILLED AND DOUBLER INSTALLED. 7075-T6511. REPAIRED PER EA 96-185017. 2 L 7 2 4F A6WE 2001110700022 20011107 00022 WP 2001 11 7 0103869612 1 20010809 A 5310 FRAME DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612NW 47436 During Hck in ATL the fuselage frame at sta 756 were inspected per EO 5311-01157, A 1.75 inch crack was found in the fra me and a 2.0 crack was found in the right frame. The right frame was removed and replaced per EO 5311-01157 7075-t6 alum inum. the left frame was put on monitor.Repaired per EA 96-186084 2 L 7 2 4F A6WE 2001110700023 20011107 00023 WP 2001 11 7 0103879612 1 20010810 A 5330 SKIN DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612NW 47436 During Hck in Atl a crack was found in the fuselage skin at the forward service door jamb, lower aft corner. the crack w as trimmed out and repaired. .050" 2024-t3 clad aluminum. Repaired per EA 96-185032. 2 L 7 2 4F A6WE 2001110700024 20011107 00024 CE 2001 11 7 2001F00621 1 20011004 A 2750 10138000001 SHAFT BEECH 1900 1900C 1154161 CE T/E FLAP DAMAGED A TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 153GA UB34 INSPECTION OF THE FLAP CABLES AS OUTLINED IN BEECH S/B 27-3397 PER AD 2001-18-07 REVEALED THE CABLES DIAGONAL WRAP TO BE UNWINDING. CONTINUED INSPECTION REVEALED THAT THREE OF THE FOUR CABLES TO BE UNWINDING. THE CABLES WERE INSTALLED IN THE CORRECT FASHION. (M) 2 L 7 2 4T RT A24CE 2001110700025 20011107 00025 CE 2001 11 7 2001F00622 1 20011004 A 2750 1013800006 SHAFT BEECH 1900 1900C 1154161 CE T/E FLAP DAMAGED A TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 153GA UB34 INSPECTION OF THE FLAP CABLES AS OUTLINED IN BEECH S/B 27-3397 PER AD 2001-18-07 REVEALED THE CABLES DIAGONAL WRAP TO BE UNWINDING. CONTINUED INSPECTION REVEALED THAT THREE OF THE FOUR CABLES TO BE UNWINDING. THE CABLES WERE INSTALLED IN THE CORRECT FASHION. (M) 2 L 7 2 4T RT A24CE 2001110700026 20011107 00026 CE 2001 11 7 2001F00623 1 20011004 A 2750 1013800006 SHAFT BEECH 1900 1900 1154160 CE T/E FLAP DEFECTIVE A TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 172GA 1286 UB11 INSPECTION OF FLAP CABLES AS OUTLINED IN BEECH S/B 27-3397 PER AD 2001-18-07 REVEALED THE RIGHT OUTBOARD FLAP CABLE DEFE CTIVE. THE INNER SHAFT RETAINER WAS NOT ATTACHED TO THE FERRULE AS REQUIRED. (M) 2 L 7 2 4T RT A24CE 2001110700027 20011107 00027 CE 2001 11 7 2001F00624 1 20011004 A 2750 1013800005 SHAFT BEECH 1900 1900C 1154161 CE T/E FLAP DAMAGED A TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 153GA UB34 INSPECTION OF THE FLAP CABLES AS OUTLINED IN BEECH S/B 27-3397 PER AD 2001-18-07 REVEALED THE CABLES DIAGONAL WRAP TO BE UNWINDING. CONTINUED INSPECTION REVEALED THAT THREE OF THE FOUR CABLES TO BE UNWINDING. THE CABLES WERE INSTALLED IN THE CORRECT FASHION. (M) 2 L 7 2 4T RT A24CE 2001110700028 20011107 00028 EU 2001 11 7 2001F00625 1 20010928 A 3234 102697001 SELECTOR VALVE STBROS SD3 SD360 8100606 EU LANDING GEAR LACK OF LUBE A PIVA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 13 711MP SH3698 MAIN LANDING GEAR INDICATORS STAYED GREEN ON GEAR UP SELECTION. ACCOMPLISHED NORMAL AND ABNORMAL CHECKLIST. THE PROBLE M PERSISTED. FLIGHT RETURNED TO HOME BASE. NO OTHER DIFFICULTIES OCCURRED THROUGHOUT THE FLIGHT. FURTHER INSPECTION F OUND 3 WAY SELECTOR VALVE ASSY NOT SEATED PROPERLY. LUBED SELECTOR LEVER, CYCLED SEVERAL TIMES AND PERFORMED LANDING GE AR EXTENSION/RETRACTION SEVERAL TIMES IAW SHORTS MM OPERATIONAL CHECK VERY GOOD. AIRCRAFT RELEASED FOR SERVICE WITH NO FURTHER TROUBLE. (M) 2 H 7 2 4T A41EU 2001110700029 20011107 00029 WP 2001 11 7 2001F00626 1 20011012 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 805US 48053 IND - THE CEILING EMERGENCY LIGHTS AT THE AFT OF THE PASSENGER CABIN, SEAT MOUNTED EMERGENCY LIGHTS AND THE TAILCONE EME RGENCY LIGHT RECEIVER WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. REF USAAD01170. (M) 2 L 7 2 4F A6WE 2001110700030 20011107 00030 WP 2001 11 7 2001F00627 1 20011012 A 3350 9721050 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 805US 48053 IND - THE CEILING EMERGENCY LIGHTS AT THE AFT OF THE PASSENGER CABIN, SEAT MOUNTED EMERGENCY LIGHTS AND THE TAILCONE EME RGENCY LIGHT RECEIVER WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001110700031 20011107 00031 WP 2001 11 7 2001F00628 1 20011015 A 3350 60030451LB BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 821US 49138 IND - THE EXTERIOR NACELLE EMERGENCY LIGHTS AND THE EMERGENCY LIGHT AT THE FORWARD ENTRY AREA WERE INOPERATIVE. MAINTEN ANCE REPLACED THE NACELLE EMERGENCY LIGHT BATTERY AND THE FORWARD ENTRY ARE EMERGENCY LIGHT POWER SUPPLY. REF USAAD0117 1. (M) 2 L 7 2 4F A6WE 2001110700032 20011107 00032 SO 2001 11 7 2001F00629 1 20011005 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 614AE 145086 ORD - FLT 4370 - CREW REPORTED THAT DURING POST FLIGHT CHECK, THE EMERGENCY LIGHTS ON INSIDE OF SERVICE DOOR WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY POWER SUPPLY AND BATTERY CHARGER. OPERATIONAL CHE CK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200127807. (M) 2 L 7 2 4T RT T00011AT 2001110700033 20011107 00033 WP 2001 11 7 GTIA010967 1 20010822 A 5523 TAB DOUG DC9 DC983 3022083 WP ELEVATOR DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - RIGHT ELEVATOR GEAR TAB HAS MANY DENTS. CLEANED DENTS. REPAIRED DENTS ON RIGHT ELEVATOR GEAR TAB IAW MD-80 SRM 5 5-04. (M) 2 L 7 2 4F RT A6WE 2001110700034 20011107 00034 WP 2001 11 7 GTIA010968 1 20010830 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - AFT CARGO LONGERON NR 22 RIGHT HAS CORROSION BETWEEN STATION 1309 AND 1322. REMOVED CORROSION. CORROSION OUT OF L IMITS. CUT OUT DAMAGE SECTION OF LONGERON FROM STATION 1297. LOCATED AND DRILLED LONGERON AND FITTINGS IAW MD-80 SRM 5 3-20-00. (M) 2 L 7 2 4F RT A6WE 2001110700035 20011107 00035 WP 2001 11 7 GTIA010969 1 20010824 A 5542 SKIN DOUG DC9 DC983 3022083 WP RUDDER DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - FOUND LEFT SIDE OF RUDDER HAS DELAMINATED IN MANY PLACES. REMOVED DAMAGED AREAS OF DELAMINATED. REPAIRED LEFT SI DE OF RUDDER IAW BOEING. BALANCED RUDDER PER SRM 55-40-01. (M) 2 L 7 2 4F RT A6WE 2001110700036 20011107 00036 NM 2001 11 7 NOCA0501 1 20010930 A 3242 FIRE BOEING 757 75728A 1384976 NM RT MLG BRAKE DETECTED A NOCA K NONE A FLAME/FIRE TX TAXI/GRND HDL 1 EA 15 756NA 32448 AIRCRAFT EXPERIENCED NORMAL LANDING AT MIA. WHILE A/C WAS TAXIING TO GATE RAMP AGENT REPORTED SEEING A BRAKE FIRE ON TH E RIGHT SIDE. THE FIRE WAS IMMEDIATELY EXTINGUISHED. THE CREW WAS ADVISED AND REPORTED THE HIGHEST TEMPERATURE RECORDE D WAS 3 ON BRAKE NR 7. INSPECTION OF THE RIGHT BOGY INCLUDING ALL 4 BRAKES AND TIRES FOUND NO EVIDENCE OF HEAT OR FIRE DAMAGE. ALL 4 TIRES HAD FUSE PLUGS INTACT. AXLE AND AREA INSPECTION PERFORMED. NO EVIDENCE OF HEAT OR FIRE DAMAGE FOU ND PRECAUTIONARY REPLACEMENT OF BRAKES AND TIRES AT POSITION 4, 5, 6, 7 PERFORMED. (M) 2 L 7 2 4F RT A2NM 2001110700037 20011107 00037 2001 11 7 NSVA0121 4 20011014 A 3422 6226136002 GYRO BEECH 1900 1900D 1154162 CE E/E BAY FAILED A NSVA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 EA 27 221CJ UE221 ON A REPOSITION FLIGHT FROM HEF TO HYA, THE CREW ENCOUNTERED ERRONEOUS HEADING INFORMATION WITH A SUBSEQUENT HEADING COM PARATOR ANNUNCIATOR. BECAUSE OF IMC CONDITIONS, THE CREW ELECTED TO DECLARE AN EMERGENCY AND DIVERT INTO ALB WHERE VMC CONDITIONS PREVAILED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MECHANICS WERE DISPATCHED AND REPLACED THE AFT DIRECTIONAL GYRO. THE AIRCRAFT WAS RELEASED ON A SPECIAL FLIGHT PERMIT TO HEF. AT HEF MAINTENANCE PERFORMED A COMPASS SYSTEM CHEC K AND A TEST FLIGHT AND RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A24CE 2001110700038 20011107 00038 EU 2001 11 7 SIMA200121501 1 20010803 A 3320 S2521658700000 MODULE AEROSP ATR42 ATR42300 8680920 EU CABIN FAULTY A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 319AM 319 FLL - FLT 5419 - DURING CLIMB, THE FLIGHT ATTENDANT REPORTED THE SMELL OF SMOKE FOLLOWED BY VISIBLE SMOKE IN CABIN. CRE W COMPLIED WITH AIR CONDITION SMOKE PROCEDURES AND SMOKE SEEMED TO STOP. AFTER FLIGHT, FURTHER REPORTS INDICATE THAT SM OKE POSSIBLY CAME FROM THE AFT RIGHT (10 OR 11CD) OVERHEAD LIGHTING FIXTURES (READING LIGHTS). MAINTENANCE FOUND THE RE ADING LIGHT MODULE AT SEAT 11CD TO BE AT FAULT. MODULE WAS REMOVED AND REPLACED IAW ATR MM. OPERATIONAL CHECK AS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001110700039 20011107 00039 EU 2001 11 7 SIMA200122102 1 20010809 A 3350 AD3127 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 269AT 269 MCO - FLT 5278 - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS AT SEAT 5, 6, AND 7 ARE INOPERATIVE. MAINTENANCE RE MOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY UNIT 10WL IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETUR NED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001110700040 20011107 00040 SO 2001 11 7 SIMA200126202 1 20010919 A 3150 WARNING SYSTEM EMB 135 EMB135LR 3260305 SO COCKPIT ACTIVATED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 735TS 145386 ORD - FLT 4522 - ON CLIMB-OUT, CREW GOT EICAS MESSAGE OF ELECTRICAL EMERGENCY ABNORMAL AND EMERGENCY LIGHTS NOT ARMED, T HEY RETURNED TO FIELD FOR MAINTENANCE. (M) 2 L 7 2 4F RT TOOO11AT 2001110700041 20011107 00041 SO 2001 11 7 SIMA200126921 1 20010926 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 646AE 3514 145213 ABI - DURING MBV INSPECTION, FOUND CENTER BEAM GUSSET CORRODED AND CHAFED. REMOVED AND REPLACED GALLEY CENTER BEAM GUSS ET IAW EMB 145 SRM 51-40-22. (M) 2 L 7 2 4T RT T00011AT 2001110700042 20011107 00042 SO 2001 11 7 SIMA200126922 1 20010926 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 646AE 3514 145213 ABI - DURING MBV INSPECTION, FOUND FORWARD CENTER DIGITAL 2 INCH AFT OF COCKPIT WALL CORRODED. REPAIRED CENTER DIGITAL IAW EMB REPAIR STATEMENT GST 3196/01. (M) 2 L 7 2 4T RT T00011AT 2001110700043 20011107 00043 SO 2001 11 7 SIMA200127601 1 20010927 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 647AE 145222 ABI - DURING AN MBV INSPECTION AIRCRAFT 647AE CORROSION WAS FOUND ON THE GALLEY FLOOR CENTER BEAM AT FRAME 20. REMOVED CORROSION BY BLENDING AND CUT OUT DAMAGED AREA. PERFORMED AN NDT INSPECTION OF THE AREA WITH NO REJECTION INDICATED. F ABRICATED A FILLER, AND DOUBLER IAW EMB GST-3215/01 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2001110700044 20011107 00044 SO 2001 11 7 SIMA200127602 1 20011001 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 647AE 145222 DURING AN MBV INSPECTION, CORROSION WAS FOUND ON THE LEFT OMEGA FLOORBEAM AT FRAME 20. REMOVED CORROSION BY CUTOUT. FA BRICATED A FILLER AND DOUBLER ANGLE. A PLATE AND TWO SHIMS IAW EMB145 (SRM 145/1142 CHAPTER 53 REV 14) 53-21-10, PG 204 , FIG 201, SHEET 1 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2001110700045 20011107 00045 SO 2001 11 7 SIMA200127608 1 20011001 A 5320 14522461011 PLATE EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 647AE 145222 ABI - THIS IS A LEVEL TWO FINDING ON A CORROSION REPAIR ITEM CARD NR 23844. RIGHT GALLEY AFT GUSSET PLATE CORRODED. BL ENDED CORROSION. INSTALLED SERVICEABLE RIGHT GALLEY AFT GUSSET PLATE IAW EMB145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2001110700046 20011107 00046 SO 2001 11 7 SIMA200127609 1 20011001 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 647AE 145222 ABI - THIS IS A LEVEL 3 FINDING ON A CORROSION REPAIR ITEM CARD NR 23803. LEFT OMEGA BEAM CORRODED AT FRAME 20. REPAIR ED LEFT OMEGA BEAM AT FRAME 20 IAW EMB 145 SRM 53-21-10 FIG 201, PAGE 20. (M) 2 L 7 2 4T RT T00011AT 2001110700047 20011107 00047 SO 2001 11 7 SIMA200127710 1 20011002 A 5320 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 647AE 3301 145222 FOUND CENTER BEAM GUSSET CORRODED. INSTALLED NEW SERVICEABLE CENTER BEAM GUSSET IAW EMB145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2001110700048 20011107 00048 SO 2001 11 7 SIMA200127711 1 20011002 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 647AE 3301 145222 FOUND FORWARD DIGITAL CORRODED. REPAIRED FORWARD DIGITAL IAW EMB145 SRM. (M) 2 L 7 2 4T RT T00011AT 2001110700049 20011107 00049 SO 2001 11 7 SIMA200127807 1 20011005 A 3350 110049 POWER SUPPLY EMB 145 EMB145 3260210 SO CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 612AE 145079 ORD - FLT 4370 - CREW REPORTED THAT DURING POST FLIGHT CHECK, THE EMERGENCY LIGHTS ON INSIDE OF SERVICE DOOR WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY POWER SUPPLY AND BATTERY CHARGER. OPERATIONAL CHE CK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2001110700050 20011107 00050 SO 2001 11 7 SIMA200128501 1 20011011 A 3210 14571035412 CAP EMB 145 EMB145LR 3260212 SO LT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 621AE 5310 145105 ABI - FOUND LEFT MAIN LANDING GEAR FORWARD LOWER BEARING CAP CORRODED. REMOVED AND REPLACED SERVICEABLE LEFT MLG FORWAR D LOWER BEARING CAP IAW EMB 145 AMM. (M) 2 L 7 2 4T RT T00011AT 2001110700051 20011107 00051 SO 2001 11 7 SIMA200128502 1 20011011 A 3210 14571035412 CAP EMB 145 EMB145LR 3260212 SO RT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 621AE 5310 145105 ABI - FOUND BOTH FORWARD AND AFT LOWER BEARING CAPS ON RIGHT MLG CORRODED. REMOVED AND REPLACED BOTH FORWARD AND AFT LO WER BEARING CAPS ON RIGHT MLG IAW EMB145 AMM. (M) 2 L 7 2 4T RT T00011AT 2001110700052 20011107 00052 SO 2001 11 7 SIMA200128503 1 20011011 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 645AE 145212 ABI - FOUND SERVICE DOOR CENTER SILL CORRODED. REPAIRED SERVICE DOOR CENTER SILL IAW EMB145 SRM AND EMB REPAIR STATEMEN T GST-3309/01. (M) 2 L 7 2 4T RT T00011AT 2001110700053 20011107 00053 NM 2001 11 7 TSAA0133140 1 20011010 A 3350 873100151 LIGHT BOEING 737 7372Q9 138448M NM CABIN INOPERATIVE A K NONE L NO TEST IN INSP/MAINT 1 WP 13 804AL 21719 REPLACED FORWARD OVERHEAD EMERGENCY AISLE LIGHT ASSEMBLY PACK DUE TO NO TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4F A16WE 2001110700054 20011107 00054 NM 2001 11 7 TSAA0133141 1 20011020 A 3350 86210066 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A K NONE L NO TEST IN INSP/MAINT 1 WP 13 804AL 21719 REPLACED FORWARD SERVICE DOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F A16WE 2001110700055 20011107 00055 NM 2001 11 7 TSAA0133142 1 20011020 A 3350 900542 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED AFT OVERHEAD PATH EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE . (M) 2 L 7 2 4F A16WE 2001110700056 20011107 00056 NM 2001 11 7 2001F00630 1 20010215 A 5712 RIB BOEING 727 727223 1384074 NM RT WING CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 879AA 21391 TUL - FOUND BS 760.95 RIGHT RIB CHORD HFEC INDICATED CRACK ON VERTICAL LEG STOPPING AT TOP OF RADIUS. ACCOMPLISHED RIB CHORD REPAIR PER ESO 11697 (DATED 2-14-01), SB 727-57-0112 PART IV, LARGE REPAIR, DWG 65C33202. (M) 2 L 7 3 4F A3WE 2001110700057 20011107 00057 WP 2001 11 7 AALA20000991A 1 20010606 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 488AA 49681 TUL - FOUND FORWARD DOORWAY WEB IS CRACKED AT LOWER LIGHTING HOLE STATION 1152 BETWEEN LONGERON 27R AND 28R, AFT CARGO. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-24. (M) 2 L 7 2 4F A6WE 2001110700061 20011107 00061 CE 2001 11 7 NSVA01034 1 20010323 A 5260 11440002317 HINGE BEECH 1900 1900C 1154161 CE AIRSTAIRS CRACKED A NSVA O OTHER O OTHER NR NOT REPORTED 1 EA 27 550CJ UC50 CREW REPORTED AIRSTAIR DOOR WAS DIFFICULT TO OPEN FROM THE INSIDE. MAINTENANCE ADJUSTED MAIN CABIN DOOR LATCH AND LUBRI CATED CAMS AS REQUIRED. UPON FURTHER INVESTIGATION MAINTENANCE DISCOVERED THE AIRSTAIR DOOR SEAL RETAINER TRACK RIVETS WERE SHEARED AND CRACKS WERE RADIATING FROM BOLT HOLES ON THE REVERSE SIDE OF THE AIRSTAIR DOOR TO AIRFRAME HINGE. THE DOOR TO AIRFRAME HINGE WAS REPLACED AND THE DOOR LATCH POST WAS RIGGED IAW BEECH MM 52-00-00 AND DRAWING 114-4023-1. (M ) 2 L 7 2 4T RT A24CE 2001110700062 20011107 00062 SO 2001 11 7 SIMA200127603 1 20011001 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 647AE 145222 ABI - DURING A MBV INSPECTION, CORROSION WAS FOUND ON THE GALLEY FLOOR FORWARD DIGITAL. REMOVED CORROSION BY BLENDING O UT. PERFORMED NDT INSPECTION OF THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR DOUBLER IAW EMB GST-3215/ 01 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2001110700063 20011107 00063 SO 2001 11 7 SIMA200127604 1 20011001 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 647AE 145222 ABI - THIS IS A LEVEL TWO FINDING ON A CORROSION REPAIR ITEM CARD NR 23851. SERVICE DOOR CENTER SILL CORRODED. BLENDED CORROSION SERVICE DOOR CENTER SILL IAW EMB145 CP 51-14-02. REPAIRED SERVICE DOOR CENTER. SILL IAW EMB GST-3215/01. ( M) 2 L 7 2 4T RT T00011AT 2001110700064 20011107 00064 SO 2001 11 7 SIMA200127605 1 20011001 A 5320 SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 647AE 145222 THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM CARD NR 23846. PAX DOOR THRESHOLD SUPPORTS CORRODED. BLENDED CORR OSION IAW EMB CPM 51-14-02. PERFORMED THICKNESS TEST AND EDDY CURRENT. NO DEFECTS. REPAIRED PAX DOOR THRESHOLD SUPPOR T IAW EMB GST-3215/01. (M) 2 L 7 2 4T RT T00011AT 2001110700065 20011107 00065 SO 2001 11 7 SIMA200127606 1 20011001 A 5320 145224600 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 647AE 145222 ABI - THIS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM CARD NR 23843. CENTER BEAM GUSSET CORRODED. REMOVED CORROSION IAW EMB SRM 51-10-02. INSTALLED NEW SERVICEABLE CENTER BEAM GUSSET IAW EMB145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2001110700066 20011107 00066 SO 2001 11 7 SIMA200127607 1 20010926 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 646AE 145213 ABI - THIS IS LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. FORWARD DIGITAL CENTER 2 INCH AFT OF COCKPIT WALL CORRODED. BLENDED, INSPECTED AND ACCEPTED AS IS IAW EMB GS 3196/01. (M) 2 L 7 2 4T RT T00011AT 2001110700067 20011107 00067 EU 2001 11 7 SIMA200127701 1 20011002 A 5321 FLOOR PANEL SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 241AE 340B241 ABI - DURING AN MBV INSPECTION, FOUND GALLEY FLOOR CORRODED AT FRAME STATION 358. REPAIRED GALLEY FLOOR IAW SAAB 340 SR M. (M) 2 L 7 2 4T RT A52EU 2001110700068 20011107 00068 SO 2001 11 7 SIMA200127702 1 20011002 A 3220 14524475001 CAP EMB 145 EMB145LR 3260212 SO NLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 645AE 3655 145212 ABI - FOUND NOSE LANDING GEAR BEARING CAPS CORRODED. REMOVED AND REPLACED NLG BEARING CAPS IAW EMB 145 AMM. (M) 2 L 7 2 4T RT T00011AT 2001110700069 20011107 00069 SO 2001 11 7 SIMA200127703 1 20011002 A 3210 14571035409 CAP EMB 145 EMB145LR 3260212 SO RT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 645AE 3646 145212 ABI - FOUND RIGHT MAIN LANDING GEAR SWIVEL BEARING CAPS CORRODED. REMOVED AND REPLACED RIGHT MLG SWIVEL BEARING CAPS IA W EMB 145 AMM. (M) 2 L 7 2 4T RT T00011AT 2001110700070 20011107 00070 SO 2001 11 7 SIMA200127704 1 20011002 A 3210 14571033407 CAP EMB 145 EMB145LR 3260212 SO LT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 645AE 3655 145212 ABI - FOUND LEFT MLG SWIVEL BEARING CAPS CORRODED. REMOVED AND REPLACED LEFT MLG BEARING CAPS IAW EMB 145 AMM. (M) 2 L 7 2 4T RT T00011AT 2001110700071 20011107 00071 SO 2001 11 7 SIMA200127706 1 20011002 A 5320 SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 646AE 3514 145213 ABI - FOUND CENTER BEAM RAMP SUPPORT CORRODED. INSTALLED SERVICEABLE CENTER BEAM RAMP SUPPORT IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2001110700072 20011107 00072 SO 2001 11 7 SIMA200127707 1 20011002 A 5320 14522461011 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 646AE 3514 145213 ABI - FOUND FORWARD DIAMOND GUSSET CORRODED. REMOVED AND REPLACED GALLEY AFT DIAMOND GUSSET IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2001110700073 20011107 00073 SO 2001 11 7 SIMA200127708 1 20011002 A 5320 14521725615 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 647AE 3301 145222 ABI - FOUND SERVICE DOOR AFT SILL CORRODED. REMOVED AND INSTALLED SERVICEABLE AFT SILL AT SERVICE DOOR IAW EMB145 SRM 5 1-40-02. (M) 2 L 7 2 4T RT T00011AT 2001110700074 20011107 00074 SO 2001 11 7 SIMA200127709 1 20011002 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 647AE 3301 145222 ABI - FOUND GALLEY FLOOR CENTER BEAM CORRODED AT FRAME 20. REPAIRED GALLEY FLOOR CENTER BEAM CORROSION AT FRAME 20 IAW EMB145 REPAIR STATEMENT GST 3215/01. (M) 2 L 7 2 4T RT T00011AT 2001110700075 20011107 00075 SO 2001 11 7 SIMA200127803 1 20011004 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 645AE 3655 145212 ABI - DURING MBV INSPECTION, FOUND CORROSION ON THE LEFT OMEGA FLOOR BEAM AT FRAME 20. REPAIRED LEFT OMEGA FLOORBEAM IA W EMB 145 SRM. (M) 2 L 7 2 4T RT T00011AT 2001110700076 20011107 00076 SO 2001 11 7 SIMA200127804 1 20011004 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 645AE 3655 145212 ABI - FOUND GALLEY CENTER BEAM GUSSET CORRODED. INSTALLED SERVICEABLE CENTER BEAM GUSSET IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2001110700077 20011107 00077 SO 2001 11 7 SIMA200127805 1 20011004 A 5510 14540881001 FITTING EMB 145 EMB145LR 3260212 SO HORIZ STAB CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 645AE 3655 145212 ABI - FOUND CORROSION AND GOUGES ON RIGHT HORIZONTAL STABILIZER FITTING BEARING MATING SURFACE. REPAIRED RIGHT HORIZONT AL STABILIZER SPHERICAL BEARING HOUSING IAW EMB145 SRM. (M) 2 L 7 2 4T RT T00011AT 2001110700078 20011107 00078 SO 2001 11 7 SIMA200127806 1 20011004 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 645AE 3655 145212 ABI - FOUND SERVICE DOOR AFT SILL CORRODED. REPAIRED SERVICE DOOR AFT SILL IAW EMB REPAIR STATEMENT GST-3308/01. (M) 2 L 7 2 4T RT T00011AT 2001110700079 20011107 00079 SO 2001 11 7 SIMA200128101 1 20011008 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 645AE 145212 THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. SERVICE DOOR FORWARD SILL HAS CORROSION. PERFORMED EDDY CURRENT AND THICKNESS CHECK, NO DEFECTS NOTED. INSTALLED REPAIR DOUBLER ON SERVICE DOOR FORWARD SILL IAW EMB GST-3309/01. (M) 2 L 7 2 4T RT T00011AT 2001110700080 20011107 00080 SO 2001 11 7 SIMA200128102 1 20011008 A 5320 14521725001 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 645AE 145212 ABI - THIS IS A LEVEL 2 FINDING ON CORROSION REPAIR ITEM CARD NR 27528. PAX DOOR AFT SILL HAS CORROSION. REMOVED AND I NSTALLED SERVICE PAX DOOR AFT SILL IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2001110700081 20011107 00081 SO 2001 11 7 SIMA200128103 1 20011008 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 645AE 145212 ABI - THIS IS LEVEL 2 FINDING ON A CORROSION REPAIR ITEM CARD NR 27521. CORROSION HAS BEEN FOUND ON GALLEY FORWARD DIGI TAL. REPAIRED FORWARD DIGITAL IAW EMB GST-3309/01. (M) 2 L 7 2 4T RT T00011AT 2001110700082 20011107 00082 SO 2001 11 7 SIMA200128104 1 20011008 A 5320 14522461011 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 645AE 145212 THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. FORWARD DIAMOND GUSSET CORRODED IN GALLEY AREA. INSTALLED SERVIC EABLE DIAMOND FORWARD GUSSET IAW EMB145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2001110700083 20011107 00083 SO 2001 11 7 SIMA200128105 1 20011008 A 5320 14522461011 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 645AE 145212 THIS IS LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. AFT DIAMOND GUSSET CORRODED IN GALLEY AREA. INSTALLED SERVICEABLE AFT DIAMOND GUSSET IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2001110700084 20011107 00084 SO 2001 11 7 SIMA200128305 1 20011010 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 645AE 3655 145212 ABI - FOUND GALLEY AFT DIGITAL CORRODED. REPAIRED GALLEY DIGITAL IAW EMB 145 REPAIR STATEMENT GST 3309/01. (M) 2 L 7 2 4T RT T00011AT 2001110700085 20011107 00085 SO 2001 11 7 SIMA200129009 1 20011018 A 3210 CAP EMB 145 EMB145LR 3260212 SO RT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 648AE 3646 145225 ABI - RIGHT MLG SWIVEL BEARING CAPS WERE FOUND TO BE CORRODED. REPLACED RIGHT FORWARD AND AFT MLG GEAR BEARING CAPS IAW EMB AMM. (M) 2 L 7 2 4T RT T00011AT 2001110700086 20011107 00086 SO 2001 11 7 SIMA200129010 1 20011017 A 3210 CAP EMB 145 EMB145LR 3260212 SO LT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 648AE 3646 145225 ABI - LEFT MAIN LANDING GEAR SWIVEL BEARING CAPS WERE FOUND TO BE CORRODED. REMOVED AND REPLACED LEFT MLG SWIVEL BEARIN G CAPS IAW EMB AMM. (M) 2 L 7 2 4T RT T00011AT 2001110700087 20011107 00087 SO 2001 11 7 SIMA200129011 1 20011017 A 3220 14522475001 CAP EMB 145 EMB145LR 3260212 SO NLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 648AE 3646 145225 ABI - NOSE LANDING GEAR RIGHT TRUNNION SWIVEL BEARING CAP WAS FOUND TO BE CORRODED. REMOVED AND REPLACED NOSE LANDING G EAR RIGHT TRUNNION SWIVEL CAP IAW EMB 145 AMM. (M) 2 L 7 2 4T RT T00011AT 2001110700088 20011107 00088 SO 2001 11 7 SIMA200129012 1 20011017 A 5320 CROSSBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 648AE 3646 145225 ABI - CROSSBEAM AND PROFILE AT FRAME 23 WAS FOUND TO BE CORRODED. REMOVED AND REPLACED CROSSBEAM AND PROFILE IAW EMB145 SRM. (M) 2 L 7 2 4T RT T00011AT 2001110700089 20011107 00089 SO 2001 11 7 SIMA200129013 1 20011017 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 648AE 3646 145225 ABI - LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REPAIRED LEFT OMEGA BEAM IAW EMB145 SRM. (M) 2 L 7 2 4T RT T00011AT 2001110700090 20011107 00090 SO 2001 11 7 SIMA200129014 1 20011017 A 5320 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 648AE 3646 145225 ABI - FORWARD DIAMOND GUSSET AS FOUND TO BE CORRODED. REMOVED AND REPLACED FORWARD DIAMOND GUSSET IAW EMB 145 SRM. (M) 2 L 7 2 4T RT T00011AT 2001110700091 20011107 00091 NM 2001 11 7 P5CA0100607 1 20011106 A 5310 NONE WEB BOEING 747 747123 1384873 NM NOSE WHEEL WELL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NOSE WHEEL WELL - BS320, LEFT VERTICAL BEAM WEB - (3) CRACKS 1/8" LONG EA. LOCATED AT 2ND, 3RD & 5TH INSULATION HOLES FR OM FLOOR BEAM CHORD. OPENED HOLE TO 9/16". H.F.E.C. NO INDICATIONS. INSTALLED REPAIR DOUBLERS AS PER BOEING TELEX PAO -LGB-01-00155H & MA #A510-33-01. 2 L 7 4 4F A20WE 2001110700092 20011107 00092 NM 2001 11 7 P5CA0100608 1 20011106 A 5310 NONE WEB BOEING 747 747123 1384873 NM NOSE WHEEL WELL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NOSE WHEEL WELL - BS300, LEFT VERTICAL BEAM WEB, 1/8" LONG CRACK AT 3RD INSULATION HOLE FROM FLOOR BEAM CHORD. OPENED H OLE TO 9/16". H.F.E.C. NO INDICATIONS. INSTALLED REPAIR DOUBLERS AS PER BOEING TELEX PAO-LGB-01-00155H & MA #A5310-33- 10. 2 L 7 4 4F A20WE 2001110700093 20011107 00093 NM 2001 11 7 P5CA0100609 1 20011106 A 5310 NONE WEB BOEING 747 747123 1384873 NM NOSE WHEEL WELL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NOSE WHEEL WELL - BS320, RIGHT VERTICAL BEAM WEB, 2" LONG CRACK AT 2ND INSULATION HOLE FROM FLOOR BEAM CHORD. REPAIRED BY REMOVING EXISTING FASTENERS, CUTTING OUT DAMAGE, INSTALLING DOUBLER, SPLICE FILLER, SHIM & (2) EA. "T" SECTIONS IAW B OEING TELEX PAO-LGB-01-00155H & MA #A510-33-01. 2 L 7 4 4F A20WE 2001110700094 20011107 00094 NM 2001 11 7 P5CA0100610 1 20011106 A 5310 NONE WEB BOEING 747 747123 1384873 NM NOSE WHEEL WELL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NOSE WHEEL WELL - BS 300, RIGHT VERTICAL BEAM WEB, 1" LONG CRACK AT 3RD INSULATION HOLE FROM FLOOR BEAM CHORD. REPAIRED BY REMOVING EXISTING FASTENERS & BRACKETS, CUTTING OUT DAMAGED SECTION, INSTALLING DOUBLERS & (2) EA. "T" SECTIONS IAW BOEING TELEX PAO-LGB-01-00155G & MA #A510-33-01. 2 L 7 4 4F A20WE 2001110700095 20011107 00095 SO 2001 11 7 SIMA200129015 1 20011017 A 5320 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 648AE 3646 145225 ABI - CENTER BEAM GUSSET WAS FOUND TO BE CORRODED. REMOVED AND REPLACED NEW CENTER BEAM GALLEY GUSSET IAW EMB145 SRM. (M) 2 L 7 2 4T RT T00011AT 2001110700096 20011107 00096 SO 2001 11 7 SIMA200129016 1 20011017 A 5320 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 648AE 3646 145225 ABI - FORWARD DIAMOND GUSSET WAS FOUND TO BE CORRODED. REMOVED AND REPLACED FORWARD DIAMOND GUSSET IAW EMB 145 SRM. (M ) 2 L 7 2 4T RT T00011AT 2001110700097 20011107 00097 SO 2001 11 7 SIMA200129017 1 20011017 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 648AE 3646 145225 ABI - LEFT OMEGA BEAM AT FRAMES 19 THROUGH 23 WAS FOUND TO BE CORRODED. REPAIRED LEFT OMEGA BEAM AT FRAMES 19 THROUGH 2 3 IAW EMB 145 REPAIR GST-3414.01. (M) 2 L 7 2 4T RT T00011AT 2001110700098 20011107 00098 NM 2001 11 7 TSAA0133143 1 20011020 A 3350 1000629 LIGHT BOEING 737 7372Q9 138448M NM CABIN INOPERATIVE A K NONE L NO TEST IN INSP/MAINT 1 WP 13 809AL 21720 REPLACED AFT SERVICE DOOR EMERGENCY LIGHT ASSEMBLY DUE TO INOPERATIVE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2001110700099 20011107 00099 NM 2001 11 7 TSAA0133144 1 20011020 A 3350 86210066 BATTERY PACK BOEING 737 737230 1384401 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED NR 5 AND NR 6 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001110700100 20011107 00100 NM 2001 11 7 USAA010001A 1 20010115 A 5320 STIFFENER BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 245US 49326 22751 CLT - FOUND STIFFENER CORRODED 7 INCHES BY 1 INCH, BS 235, RBL 10, WL 195 FORWARD UPPER ACCESS PANEL. INSTALLED ANGLE AN D STIFFENER PER SRM 53-10-2 AND 53-30-0. (M) 2 L 7 2 4F A16WE 2001110700101 20011107 00101 NM 2001 11 7 USAA010002A 1 20010115 A 5210 FRAME BOEING 737 737201 1384454 NM ENTRY DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 245US 49867 22751 CLT - FOUND FRAME CRACKED 3 INCHES, FORWARD ENTRY DOOR BOTTOM FRAME. REPLACED FRAME PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2001110700102 20011107 00102 NM 2001 11 7 USAA010003A 1 20010115 A 5320 INTERCOSTAL BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND INTERCOSTAL CRACKED 1 INCH, STATION 178, WL 195, RBL 26 AND LBL 26. REPLACED INTERCOSTAL PER SRM 53-10-1. (M) 2 L 7 2 4F A16WE 2001110700103 20011107 00103 NM 2001 11 7 USAA010112A 1 20010205 A 5320 WEB BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 50470 22757 CLT - FOUND WEB CRACKED .25 INCH, STATION 334 STRINGER 8R AT FORWARD SERVICE DOOR. REPLACED SHEAR WEB PER DRAWING 65C33 288. (M) 2 L 7 2 4F A16WE 2001110700104 20011107 00104 WP 2001 11 7 USAAD01169 1 20011011 A 2421 976J2526 GENERATOR DOUG DC9 DC981 3022081 WP RT ENGINE FAILED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 808US 48040 BOS-CLT - FLT 323 - DURING CRUISE, THE RIGHT ENGINE DRIVEN GENERATOR BECAME INOPERATIVE. AS THE LEFT ENGINE GENERATOR W AS ALREADY INOPERATIVE AND RELEASED PER MEL PROCEDURES, THE AIRCRAFT DIVERTED AND LANDED AT RIC WITHOUT INCIDENT. MAINTE NANCE REPLACED THE RIGHT ENGINE DRIVEN GENERATOR AND CSD, AND THE LEFT GENERATOR CONTROL UNIT AND VOLTAGE REGULATOR. (M ) 2 L 7 2 4F A6WE 2001110700105 20011107 00105 WP 2001 11 7 USAAD01170 1 20011012 A 3350 AD4002P BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 805US 48053 IND - THE CEILING EMERGENCY LIGHTS AT THE AFT OF THE PASSENGER CABIN, SEAT MOUNTED EMERGENCY LIGHTS AND THE TAILCONE EME RGENCY LIGHT RECEIVER WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001110700106 20011107 00106 SO 2001 11 7 LR7A01116 1 20011104 A 5343 36058712 FITTING LKHEED 382 382G 526414U SO FS 165 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 143 4698 DURING SCHEDULED A CHECK INSPECTION PER JOB CARD HA1200 FOUND RH FS 165 NLG TRUNNION FITTING CRACKED APPROX. 1.0 IN AT F TG. OUTBD EDGE TO OUTBD. LOWER BOLT HOLE, RBL 18, WL 170.AIRCRAFT FERRIED TO EGSC FOR REPAIR. AT EGSC RH NLG TRUNNION F ITTING REPLACED IAW SRM SMP 583-53-40. WORK ORDER 02/06/01. 2 H 7 4 4T A1SO 2001110700107 20011107 00107 WP 2001 11 7 USAAD01171 1 20011015 A 3350 MISC0639 BATTERY DOUG DC9 DC982 3022082 WP CEILING DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 821US 49138 IND - THE CEILING EMERGENCY LIGHTS AT THE AFT OF THE PASSENGER CABIN, SEAT MOUNTED EMERGENCY LIGHTS AND THE TAILCONE EME RGENCY LIGHT RECEIVER WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001110700108 20011107 00108 NM 2001 11 7 USAASB01290 1 20011009 A 2841 1003710000153M4 INDICATOR BOEING 737 737301 1384611 NM COCKPIT SHORTED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 336US 39760 23233 CLT - FLT 997 - EN ROUTE FROM PHL TO MSY, ALL THREE FUEL QUANTITY INDICATORS WENT BLANK. CREW FOUND FUEL QUANTITY CIRCU IT BREAKER TRIPPED BUT ATTEMPTS TO RESET THE BREAKER FAILED. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT . NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE COCKPIT NR 1 FUEL QUANTITY INDICATOR SHORTED OUT. REMOVED AND REPL ACED THE NR 1 FUEL QUANTITY INDICATOR PER MM 28-41-51. RESET OF CIRCUIT BREAKER GOOD. OPERATIONAL CHECK OF INDICATION SYSTEM GOOD. (M) 2 L 7 2 4F RT A16WE 2001110700122 20011107 00122 WP 2001 11 7 01FDEA00933 1 20011026 A 3234 CONTROL HANDLE DOUG DC10 DC1030F 3023504 WP COCKPIT LACK OF LUBE A FDEA O OTHER J WARNING INDICATION LD LANDING 1 SO 25 307FE 48291 WHEN GEAR HANDLE LOWERED FOR LAND AT BOTH PANELS IND. CLEANED AND LUBED GEAR HANDLE PER MM 32-31-02-7, 32-31-02-2. OPS CHECK NORMAL. 2 L 7 3 4F RT A22WE 2001110700123 20011107 00123 NE 2001 11 7 01FDEA00934 2 20011029 A 7200 ENGINE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE NR 2 MAKING METAL A FDEA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 25 602FE 48402 702920 NR 2 ENG N1 FAILED TO ATTAIN T/O THRUST. MAINTENANCE FOUND METAL IN THE TAILPIPE. 2 L 7 3 4F 4 F RT A22WE E31N3 2001111600065 20011116 00065 NM 2001 11 16 01FDEA00939 1 20011029 A 5744 ARB062111 ATTACH FITTING DOUG MD11 MD11F 3023600 NM RT WING OUT OF POSITION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING INBOARD FLAP OUTBOARD HINGE ATTACH FITTING TO REAR WING SPAR MIGRATED. REMOVED AND REPLACED PER DWG ARB0621 & M M 27-50-20-4. 2 L 7 3 4F RT A22WE 2001110700124 20011107 00124 WP 2001 11 7 01FDEA00941 1 20011030 A 5347 S4929147 SEAT TRACK DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 BS 1877 TO 1887 X=10.Z=-19 SEAT TRACK HAS CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM. 2 L 7 3 4F RT A22WE 2001110700126 20011107 00126 WP 2001 11 7 01FDEA00943 1 20011030 A 5347 4929150 SEAT TRACK DOUG DC10 DC1030F 3023504 WP FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 BS 1175, X=-48 SEAT TRACK IN MAIN CABIN GOUGE. REMOVED AND REPLACED SEAT TRACK PER SRM. 2 L 7 3 4F RT A22WE 2001110700127 20011107 00127 WP 2001 11 7 01FDEA00944 1 20011030 A 5347 4929150 SEAT TRACK DOUG DC10 DC1030F 3023504 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 BS 615 AND 635 X=-27 SEAT TRACK IN MAIN CABIN GOUGED AND OBLONG. REMOVED AND REPLACED SEAT TRACK PER SRM. 2 L 7 3 4F RT A22WE 2001110700128 20011107 00128 WP 2001 11 7 01FDEA00945 1 20011030 A 5347 4929149 SEAT TRACK DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 BS 1079-1099 LONG 27R EXFOLIATING CORROSION ON FLOORBOARD SEAT TRACK. REMOVED AND REPLACED SEAT TRACK PER SRM. 2 L 7 3 4F RT A22WE 2001110700129 20011107 00129 WP 2001 11 7 01FDEA00946 1 20011030 A 5311 AGA70987 FRAME DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 BS 1841, LBL 53-58, WL 97 AFT SIDE FRAME CORRODED. REMOVED AND REPLACED CAP PER SRM. 2 L 7 3 4F RT A22WE 2001110700130 20011107 00130 WP 2001 11 7 01FDEA00947 1 20011030 A 5347 ABA71915 SEAT TRACK DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 BS 1936, LBL 27, WL 80 SEAT TRACK CORRODED SEAT TRACK CHANNEL. REMOVED AND REPLACED SEAT TRACK PER SRM. 2 L 7 3 4F RT A22WE 2001110700131 20011107 00131 WP 2001 11 7 01FDEA00948 1 20011030 A 5330 SKIN DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 BS 1028-1068 LONG 52 OML DEEP PITTED CORROSION TO EXTERIOR SKIN BOTTOM. REMOVED AND REPLACED SKIN PER SRM & EA. 2 L 7 3 4F RT A22WE 2001110700132 20011107 00132 WP 2001 11 7 01FDEA00949 1 20011030 A 5330 SKIN DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 BS 1028-1068 LONG 52 OML DEEP PITTED CORROSION TO EXTERIOR SKIN BOTTOM. REMOVED AND REPLACED SKIN PER SRM & EA. 2 L 7 3 4F RT A22WE 2001110700133 20011107 00133 WP 2001 11 7 01FDEA00950 1 20011030 A 5320 INTERCOSTAL DOUG DC10 DC1030F 3023504 WP FUSELAGE BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 BS 450 TO 460 X=-21 LOWER AVIONICS SKIN BENT INTERCOSTAL. REMOVED AND REPLACED INTERCOSTAL PER SRM. 2 L 7 3 4F RT A22WE 2001110700134 20011107 00134 WP 2001 11 7 01FDEA00953 1 20011101 A 5753 VANE DOUG DC10 DC1010F 3022111 WP T/E FLAP GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 364FE 46600 LEFT HAND OUTBOARD FLAP VANE HAS GOUGE. REMOVED AND REPLACED FLAP PER SRM 51-71-00. 2 L 7 3 4F A22WE 2001110700135 20011107 00135 WP 2001 11 7 01FDEA00954 1 20011101 A 5753 SKIN DOUG DC10 DC1010F 3022111 WP T/E FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 364FE 46600 LEFT HAND INBOARD FLAP OUTER SKIN HAS .5 INCH CRACK. REMOVED AND REPLACED SKIN PER SRM 57-00-01. 2 L 7 3 4F A22WE 2001110700136 20011107 00136 WP 2001 11 7 01FDEA00957 1 20011024 A 5720 BRACKET DOUG DC10 DC1010 3022110 WP WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 CRACK AT TOP OF CORNER ANGLE BRACKET. REMOVED AND REPLACED BRACKET PER EA 8-5710-56175 & S/B 57-88. 2 L 7 3 4F A22WE 2001110700137 20011107 00137 NM 2001 11 7 01FDEA00959 1 20011103 A 5510 65241899 BEAM BOEING 727 727233 138408A NM HORZ STAB CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 279FE 22346 LT HORIZ STAB LOWER TRAILING EDGE BEAM HAS CHAFE DAMAGE AND MISSING SPACER. 2 L 7 3 4F RT A3WE 2001112900123 20011129 00123 NM 2001 11 29 01FDEA00960 1 20011104 A 5320 65442344 SUPPORT BOEING 727 7272S2F 1384O81 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 201FE 22924 CORROSION (C53-111-01, 2) ON CENTER CEILING SUPPORT BEAM AROUND NUT PLATES BS 720+10 TO 720C+3, BL 0, WL 200. REMOVED A ND EPLACED CHORD PER SRM 51-40-4. 2 L 7 3 4F A3WE 2001110700138 20011107 00138 NM 2001 11 7 AWXA200100568 1 20011025 A 5330 6545767 SKIN BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 MCN - C13 CK - "C" - CRACK FOUND IN FUSELAGE SKIN, .280" LONG, AT BS 500B, BETWEEN STR 15R & 16R, AT THE FWD UPPER EDGE OF THE R/H WING ICE LIGHT CUTOUT. MAINTENANCE ROUTED OUT THE CRACK, FABRICATED REPAIR DOUBLER AND INSTALLED IAW AWA ER 1 5-5313-01305-TB2. 2 L 7 2 4F RT A16WE 2001110700139 20011107 00139 NM 2001 11 7 AWXA200100570 1 20011021 A 5320 654541041 WEB BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - C13 CK - "C" - CRACK FOUND ON FLOOR SUPPORT WEB AT FASTENER HOLE, .250" LONG AT BS 709, BL 0, WL 204. MAINTENANCE REMOVED WEB SECTION FROM BS 700 TO BS 715, FABRICATED REPAIR WEB, FILLER AND DOUBLER AND INSTALLED IAW AWA ER 03-5702-01 303-TB1. 2 L 7 2 4F RT A16WE 2001110700140 20011107 00140 SO 2001 11 7 SWIA200110282 1 20011027 A 3020 211C117183 PRESSURE SWITCH EMB 120 EMB120ER 3260203 SO RT ENGINE MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 284YV 120284 RIGHT ENGINE AIR INLET BOOT FAILED AT 17,000 FT, -5 DEGREES CELSIUS. RECYCLED MULTIPLE TIMES. FINALLY WORKED DURING DE SCENT WITH POSITIVE TEMPS. BOOT CYCLE WAS VISIBLE BUT MAP LIGHT INDICATED FAILURE.REPLACED RIGHT ENGINE DEICE PRESSURE SWITCH IAW MM 30-20-03. RAN FOR SEVERAL MINUTES WITHOUT FAULT. P/N: 211C117-183 S/N ON: S50860A S/N OFF: S30815A 2 L 7 2 4T RT A31SO 2001110800001 20011108 00001 WP 2001 11 8 0103769907 1 20011031 A 2150 20495055 ACM DOUG DC9 DC931 3022065 WP A/C BAY LEAKING A NWAA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 957N 47253 JUST AFTER TAKEOFF ROTATION, A STRONG ODOR OF EXHAUST FUMES FILLED THE CABIN. FUMES CLEARED WHEN THROTTLES WERE RETARDE D FOR LANDING AFTER TURNBACK. LANDING WAS UNEVENTFUL. FUMES RETURNED DURING TAXI TO THE GATE AND CLEARED WHEN PACKS WE RE SHUT DOWN. MAINTENANCE FOUND THE LEFT ACM LEAKING OIL INTERNALLY. OIL WAS IN THE DUCTS AND SENSE LINES. REPLACED T HE ACM AND WATER SEPARATORS. DUCTS CLEARED OUT AND CABIN VENTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001110800002 20011108 00002 WP 2001 11 8 0103779931 1 20011030 A 2120 DUCT DOUG DC9 DC931 3022065 WP A/C BAY BLOWN A NWAA B EMER. DESCENT O OTHER CR CRUISE 1 GL 01 90S 47244 DURING CLIMBOUT AND UPON REACHING CRUISE ALTITUDE, THE CABIN CONTINUED TO CLIMB. CREW REQUESTED TO DEPART FL240 AND DES CENDED TO 9000 FT FOR THE DURATION OF THE FLIGHT. CABIN ALTITUDE WAS 10,000 FT AT FL240 AND WAS 6000 FT WHEN AIRCRAFT W AS AT 9000 FT. LANDING AT OMA WAS UNEVENTFUL. MAINTENANCE REPLACED A BLOWN DUCT ON THE LEFT ACM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001110800003 20011108 00003 EU 2001 11 8 CA011018006 1 20011002 A 2922 NAS161228 O-RING 4324442 AIRBUS 330 A330322 3930325 EU PWA 4168 PW4168 NE HYD SYSTEM FRETTED W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA (CAN) A/C EXPERIENCED LOSS OF YELLOW HYDRAULIC SYS, ECAM WARNING - HYD RSVR LO/HYD SYS LO PR, APPROX 1(ONE) HR INTO F LT. FLT CREW SECURED SYS AS PER THE AFM&DIVERTED FLT TO MAN. UPON ARRIVAL IN MAN, MAINT FOUND FLUID DRIPPING FROM NR 2 ENGINE THRUST REVERSER PYLON DRAIN TUBE. THRUST REVERSER HYDRAULIC FILTER ASSY FOUND TO BE WET WITH HYDRAU LIC FLUID. FILTER ASSY DISASSEMBLED & FOUND O-RING FRETTED. O-RING REPLACED AS PER SB & YELLOW HYDRAULIC SYS CHECKED, YELLOW HYDRA ULIC PUMP CASE DRAIN FILTER CHECKED NO ABNORMALITIES NOTED. THE SYS GROUND CHECKED SERVICEABLE. 2 L 7 2 4F 4 F RT A46NM E36NE 2001110800006 20011108 00006 NE 2001 11 8 CA011019009 2 20010926 A 7200 71300421 ENGINE PWA PW4060 BOEING 767 767333 1385301 NM PWA 4060 PW4060 52119 NE LT ENGINE FAILED W O OTHER E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 CA P724343 (CAN) DURING INITIAL CLIMB ON GEAR RETRACTION LEFT ENGINE HAD A RECOVERABLE SURGE. (MOMENTARY WITH LOUD BANG) WITH NO V ARIANCE IN ENGINE PARAMETERS. FLIGHT DATA RECORDER READ OUT PERFORMED REVEALING ENGINE SUSTAINED A CATEGORY LEVEL 3 SUR GE. LT ENGINE REPLACED AS PER MAINTENANCE MANUAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2001110800009 20011108 00009 NM 2001 11 8 01FDEA00930 1 20011027 A 7830 783012583 THRUST REVERSER BOEING 727 7272S2F 1384O81 NM NR 1 ENGINE LEAKING A FDEA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 25 205FE 22927 HYD PRESS LOST, BOTH PRESS LIGHT ILLUM. REMOVED AND REPLACED NR 1 T/R AND 2 PUMP CASE DRAIN FILTERS PER IAW MM 29-11-04 1-2. 2 L 7 3 4F A3WE 2001110800010 20011108 00010 NM 2001 11 8 01FDEA00931 1 20011026 A 2910 HYDRAULIC SYSTEM BOEING 727 72725 1384006 NM A SYSTEM LEAKING A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 155FE 18288 A-SYS QUANTITY DECREASING. SERVICED A-HYD SYS, NO LEAKS NOTED. OK FOR SERVICE. 2 L 7 3 4F A3WE 2001113000017 20011130 00017 NM 2001 11 30 01FDEA00962 1 20011031 A 5311 FRAME BOEING 727 7272S2F 1384O81 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 201FE 22924 FRAME CRACKED AT BS 783, RBL 66, WL 193 AFT SIDE. REMOVED AND REPLACED FRAME PER EA 7-5310-7-3367. 2 L 7 3 4F A3WE 2001110800011 20011108 00011 NE 2001 11 8 01FDEA00963 2 20011103 A 7200 ENGINE AIRBUS 310 A310203 3930313 EU GE CF6 CF680A3 30025 NE NR 1 STALLED A FDEA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 25 411FE 359 585132 NR 1 ENG WILL NOT ACCELERATE IN NORMAL MANOR (REPEAT WRITE UP). 2 L 7 2 4F 4 F RT A35EU E13NE 2001110800012 20011108 00012 NM 2001 11 8 01FDEA00964 1 20011102 A 3610 CLAMP BOEING 727 72722 1384002 NM NR 1 ENGINE LOOSE A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SO 25 151FE 19147 NR 1 ENG STRUT OVERHEAD LIGHT ILLUM. SECURED CLAP AND CONNECTOR PER MM 36-00-000-5. OPS CHECK OK. 2 L 7 3 4F A3WE 2001110800013 20011108 00013 2001 11 8 0103783244 4 20011012 A 2565 D30665109 SLIDE AIRBUS 320 A320212 3930322 EU EXIT DOOR LEAKING A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 344NW 7462 7462 388 DURING SLIDE SHOP TEST, FAILED LEAK CHECK. OVERHAULED AND REPAIRED PER AIR CRUISERS MAINTENANCE MANUAL PA 15609 AND PAC KING PUBLICATION 26657. 2 L 7 2 4F RT A28NM 2001110800014 20011108 00014 NM 2001 11 8 0103806311 1 20011025 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 671US 26477 DURING LINE CHECK, FOUND THREE SETS OF EMERGENCY LIGHTS INOPERATIVE ON THE LEFT SIDE AND TWO SETS OF EMERGENCY LIGHTS IN OPERATIVE ON THE RIGHT SIDE. REPLACED THE POWER SUPPLY AT DOOR 3L AND LIGHT ASSEMBLY AT STA 1871. OPERATIONAL CHECK GO OD. 2 L 7 4 4F RT A20WE 2001110800015 20011108 00015 NM 2001 11 8 0103816313 1 20011027 A 2612 285N002821 CIRCUIT BOARD BOEING 747 747451 1384940 NM FIRE DETECTION FAULTY A NWAA F ACTIVATE FIRE EXT. N FALSE WARNING LD LANDING 1 GL 01 673US 10461 10461 30268 DURING LANDING, RECEIVED A FIRE CARGO AFT MESSAGE AND THE FIRE BELL SOUNDED. THERE WAS NO SIGN OF FIRE BUT FOLLOWED THE AFT CARGO FIRE PROCEDURE AND PROCEEDED TO THE GATE WITHOUT INCIDENT. REPLACED THE AFOLTS CARD A32 AND FOUR FIRE BOTTLE S. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2001110800016 20011108 00016 WP 2001 11 8 0103889614 1 20010813 A 5310 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 614NW 47128 AT LCK VISIT A .125 INCH CRACK WAS DETECTED EMANATING FROM NR 6 AFT DOOR STOP IN FWD DIRECTION. A PREVIOUSLY EXISTING R EPAIR DOUBLER WAS DISCOVERED STARTING FORWARD OF THE UPPER TANGENT POINT OF THE UPPER AFT CORNER OF THE L1 DOOR. THE DO UBLE EXTENDS AROUND THE CORNER AND ENCOMPASSES AFT DOOR STOPS NR 1 THROUGH NR 5. REPAIRED PER EA 96-184001. 2 L 7 2 4F A6WE 2001110800022 20011108 00022 NM 2001 11 8 01FDEA00966 1 20011106 A 3610 132712 LINE BOEING 727 72722 1384002 NM NR 1 PYLON BLOWN A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 SO 25 151FE 19147 NR 1 ENGINE STRUT OVERHEAD LIGHT CAME ON. REMOVED AND REPLACED BLOWN T/R HOSE IN NR 1 PYLON AREA. NO LEAKS NOTED. OK FOR SERVICE. 2 L 7 3 4F A3WE 2001110800023 20011108 00023 NM 2001 11 8 01FDEA00967 1 20011106 A 3260 WARNING LIGHT DOUG MD11 MD11F 3023600 NM COCKPIT ILLUMINATED A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 612FE 48605 UPON GEAR RETRACTION, RIGHT MLG LIGHT STAY ILLUM ON BOTH PRIMARY AND SECONDARY GEAR DISPLAYS. 2 L 7 3 4F RT A22WE 2001110800024 20011108 00024 EU 2001 11 8 2001F00580 1 20011017 A 3233 70839 ACTUATOR PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL RT MLG LEAKING E S4WA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 07 613NA 2864 197 PR0052 HJ978 DURING 100 HR INSPECTION, FOUND RIGHT GEAR ACTUATOR SEEPING HYDRAULIC FLUID DURING RETRACTION TESTS. REMOVED AND REPLAC ED ACTUATOR WITH SERVICEABLE PART IAW AMM CHPT 32 AND OPS CHECK OK. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001110800025 20011108 00025 EU 2001 11 8 2001F00581 1 20011004 A 2163 9599020121 SENSOR PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL ECS SYSTEM FAULTY E S4WA K NONE N FALSE WARNING AP APPROACH 1 WP 07 308NA 2580 226 PR0082 HJ803 DURING FINAL APPROACH THE ECS CAWS LIGHT ILLUMINATED AND THE ECS SYSTEM SHUT DOWN. TROUBLESHOT SYSTEM AND FOUND THE DUC T TEMP SENSOR TO BE FAULTY. REMOVED AND REPLACED WITH SERVICEABLE IAW AMM CHPT 21 AND OPS CHECK OK. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001110800042 20011108 00042 EA 2001 11 8 COMA0160876 1 20011107 A 5346 601R5361345 WEB CNDAIR CL600 CL6002B19 1900309 EA AFT EQUIPMENT BA CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 948CA 14268 7079 R/H ENGINE SUPPORT BEAM I/B FORWARD CORNER CRACKED.PERFORMED A MAJOR REPAIR TO R/II ENGINE SUPPORT BEAM I/A/W CRJ REO 60 1R-53-61-366 REV C. 2 L 7 2 4F RT A21EA 2001110800043 20011108 00043 EA 2001 11 8 COMA0160877 1 20011106 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING S O AFFECT SYSTEMS OTHER CR CRUISE 1 SO 01 967CA 7134 FLIGHT #5101 CABIN DOOR OUTER HANGLE CAUTION MESSAGE DURING CRUISE FLIGHT, AIRCRAFT DIVERTED TO MDT.COULD NOT DUPLICATE. INSPECITON AND OPERATION OF CABIN DOOR REVEALED NO DEFECTS. 2 L 7 2 4F RT A21EA 2001110800044 20011108 00044 EA 2001 11 8 COMA0160878 1 20011107 A 5346 601R5361345 WEB CNDAIR CL600 CL6002B19 1900309 EA AFT EQPT BAY CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 948CA 14268 7079 L/H ENGINE SUPPORT BEAM I/B FORWARD CORNER CRACKEDPERFORMED A MAJOR REPAIR TO L/H ENGINE SUPPORT BEAM I/A/W CRJ REO 601R -53-61-366 REV C AND WVAC EO 601R-33-2822. 2 L 7 2 4F RT A21EA 2001110800045 20011108 00045 NM 2001 11 8 AWXA200100571 1 20011021 A 5320 654541041 WEB BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - C13 CK - "C" - CRACK FOUND IN FLOOR SUPPORT WEB, .750" LONG AT BS 707, BL 0, WL 204. MAINTENANCE REMOVED DAMAGED S ECTION OF FLOOR SUPPORT WEB FROM BS 700 TO BS 715, FABRICATED REPAIR WEB, FILLER AND DOUBLER AND INSTALLED IAW AWA ER 03 -5702-01303-TB1. 2 L 7 2 4F RT A16WE 2001110800046 20011108 00046 NM 2001 11 8 AWXA200100572 1 20011021 A 5320 654541041 WEB BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - C13 CK - "C" - CRACK FOUND ON FLOOR SUPPORT WEB 1" LONG AT BS 704, LBL 24, WL 204. MAINTENANCE REMOVED DAMAGED SEC TION OF FLOOR SUPPORT WEB, FABRICATED REPAIR WEB, FILLER AND DOUBLER AND INSTALLED REPAIR PARTS IAW AWA ER 03-5702-01303 -TB1. 2 L 7 2 4F RT A16WE 2001110800047 20011108 00047 EA 2001 11 8 COMA0160879 1 20011107 A 5312 NA WEB CNDAIR CL600 CL6002B19 1900309 EA AFT PRESS BULKHE CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 948CA 14268 7079 THE AFT PRESSURE BULKHEAD HAS A HOLE WORN IN THE WEB STRUCTURE FROM A FASTENER THAT PROTRUDED BEYOND THE CARGO LINER INS TALLATION.PERFORMED A MAJOR REPAIR TO 621 BULKHEAD I/A/W WVAC EO 601R-53-2820A. 2 L 7 2 4F RT A21EA 2001110800048 20011108 00048 EA 2001 11 8 COMA0160880 1 20011107 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA WING BURNED OUT A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 781CA 7312 FLIGHT #5324 L/H FWD OVERWING EMERGENCY LIGHT IS INOP.REPLACED LIGHT BULB. 2 L 7 2 4F RT A21EA 2001110800050 20011108 00050 NM 2001 11 8 2001UALA02149 1 20011020 A 5730 SKIN PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RT WING DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 RIGHT HAND WING OUTBOARD LOWER SKIN PANEL FORWARD OF OUTBOARD AILERON DAMAGE. MAJOR REPAIR ACCOMPLISHED. PANEL REPLAC ED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001110800051 20011108 00051 NM 2001 11 8 2001UALA02150 1 20011019 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 918UA 25385 STATION 897 RBL 12 TO RBL 15. CABIN FLOORBEAM UPPER CAP HAS AREAS BLENDED BEYOND 15 PERCENT LIMIT. MAJOR REPAIR ACCOMP LISHED. CUT OUT DAMAGED SECTION. MANUFACTURED AND INSTALLED REPAIR DOUBLERS AND FILLERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2001110800052 20011108 00052 NM 2001 11 8 2001UALA02151 1 20011021 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 918UA 25385 CABIN FLOORBEAM UPPER CAP IS CORRODED BODY STATION 947, RBL 29 - 60, WL 208. MAJOR REPAIR ACCOMPLISHED. INSTALLED UPPE R CAP SPLICE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001110800053 20011108 00053 NM 2001 11 8 2001UALA02152 1 20011021 A 5512 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE HORIZ STAB DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 918UA 25385 RIGHT HAND HORIZONTAL STABILIZER LEADING EDGE SKIN HAS A DENT AT STABILIZER STATION 123. MAJOR REPAIR ACCOMPLISHED. AC COMPLISHED FLUSH PATCH. 2 L 7 2 4F 4 F RT A16WE E2GL 2001110800054 20011108 00054 NM 2001 11 8 2001UALA02153 1 20011021 A 2700 3945122505 COMPUTER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE E/E BAY FAULTY A UALA A UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 821UA 944 ELEVATOR AILERON COMPUTER (ELAC) NR 1 FAILURE MESSAGE DISPLAYED ON UPPER ELECTRONIC CENTRALIZED AIRCRAFT MONITORING. RES ET OF THE ELAC CAUSED ELECTRICAL ODOR IN FLIGHT DECK. THE ELAC1 WAS REPLACED AND OPERATIONAL CHECK WAS GOOD. SHOP FIND INGS REVEALED INTERNAL POWER SUPPLY BOARD EXISTED WITH BURNT TRACES. 2 L 7 2 4F 4 F RT A28NM E40NE 2001110800055 20011108 00055 NM 2001 11 8 2001UALA02154 1 20011021 A 5320 STIFFENER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 336UA 24240 FORWARD BULKHEAD STATION 178 AFT SIDE LBL 5.7 VERTICAL WEB T-CHORD CRACKED WL 183 INBOARD RADIUS. MAJOR REPAIR ACCOMPLIS HED. ACCOMPLISHED REINFORCEMENT REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001110800056 20011108 00056 NM 2001 11 8 2001UALA02156 1 20011023 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 520UA 24890 CABIN FLOORBEAM CORRODED BETWEEN RBL 6 AND RBL 56, STA 365. MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW T-CAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2001111500024 20011115 00024 NM 2001 11 15 2001UALA02157 1 20011021 A 2530 9F21904501 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE GALLEY EXPOSED A UALA O OTHER A FLAME/FIRE NR NOT REPORTED 1 WP 29 182UA 25279 FLIGHT ATTENDANT REPORTED BRIEF FIRE IN AFT GALLEY FROM CART N54 PIGTAIL HAS EXPOSED WIRE. THE 9F21904-501 PIGTAIL CABL E IN THE G5 GALLEY WAS DAMAGE DUE TO THE CABLE BEING PINCHED BETWEEN THE NEW TECH CART AND GALLEY COUNTER TOP. THE CABL E WAS REPLACED WITH NO FURTHER WRITE-UPS. 2 L 7 4 4F 4 F RT A20WE E24NE 2001110800058 20011108 00058 NM 2001 11 8 2001UALA02159 1 20011024 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 336UA 24240 FORWARD FUSELAGE AFT SIDE OF THE BODY STATION 188 FRAME WL 207, STRINGER 17L IS CRACKED. MAJOR REPAIR ACCOMPLISHED. DO UBLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001110800059 20011108 00059 NM 2001 11 8 2001UALA02160 1 20011024 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 357UA 24378 STATION 178 WEB AT WL 204 RBL 5.7 IS CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001110800060 20011108 00060 NM 2001 11 8 2001UALA02161 1 20011024 A 5315 141W85191 FLOORBEAM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 769UA 24034 26921 STATION 246 RBL 26.06 CHORD CRACKED 2 PLACES UNDER WEB. MAJOR REPAIR ACCOMPLISHED. REPAIR NR 2 SPLICED IN NEW SECTION O F CHORD, RBL 50 TO LBL 21. NOTED CRACKING OF THE 141W8519-1 MID CHORD IS DUE TO THERMAL CONTRACTION THAT RESULTS IN HIG HER THAN EXPECTED IN-SERVICE LOADING OF THE DOUBLE DEPTH STATION 246 FLOORBEAM. PART IS BEING REPAIRED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001110800061 20011108 00061 NM 2001 11 8 2001UALA02162 1 20011030 A 5312 PRESSURE PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 AFT CABIN PRESSURE DECK UPPER SURFACE HAS CORROSION AT STATION 1680, RBL 12 TO LBL 55. MAJOR REPAIR ACCOMPLISHED. INST ALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2001110800062 20011108 00062 NM 2001 11 8 2001UALA02163 1 20011030 A 5312 PRESSURE PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 AFT CABIN PRESSURE DECK CORRODED AT STATION 1680, RBL 39. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED AREA HFEC FOR CRA CK AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2001110800065 20011108 00065 NM 2001 11 8 2001UALA02167 1 20011025 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 339UA 24243 STATION 178 BULKHEAD AT WL 201 LBL 5.7 WEB IS CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001110800066 20011108 00066 NM 2001 11 8 2001UALA02168 1 20011025 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 339UA 24243 STATION 178 WEB CRACKED AT WL 201 RBL 5.7. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001110800067 20011108 00067 NM 2001 11 8 2001UALA02169 1 20011025 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 339UA 24243 STATION 178 WEB CRACKED AT WL 210 LBL 5.7. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001110800068 20011108 00068 NM 2001 11 8 2001UALA02170 1 20011025 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 357UA 24378 STATION 178 BULKHEAD CRACKED AT WL 210 LBL 5.7. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001110800069 20011108 00069 NM 2001 11 8 2001UALA02171 1 20011025 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 357UA 24378 STATION 178 BULKHEAD CRACKED AT WL 204 LBL 5.7. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001110800070 20011108 00070 NM 2001 11 8 2001UALA02172 1 20011024 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 176UA 24383 EMERGENCY LIGHT INOP, DOOR 4 RIGHT, AFT EXIT SIGN. REPLACED BATTERY PACK. CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2001110800071 20011108 00071 NM 2001 11 8 2001UALA02173 1 20011026 A 5320 STRUCTURE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 674UA 29242 GOUGE FORWARD OF THE BULK CARGO PIT THAT IS 2 FEET VERTICAL IN LENGTH AND 2 MM DEEP. MAJOR REPAIR ACCOMPLISHED. INSTAL LED DOUBLER REPAIR AT BODY STATION 1427 BETWEEN STRINGER 34L AND 36L. 2 L 7 2 4F 4 F RT A1NM E24NE 2001110800072 20011108 00072 NM 2001 11 8 2001UALA02176 1 20011028 A 5310 ATTACH ANGLE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 918UA 25385 FUSELAGE FRAME STATION 188 WL 207 RADIUS CRACKED IN SKIN ATTACH FLANGE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001110800073 20011108 00073 NM 2001 11 8 2001UALA02177 1 20011029 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 336UA 24240 FWD GALLEY DOOR AFT DOOR FRAME AT, 3RD STOP FITTING FROM BOTTOM, CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER TO FRAME CUTOUT. 2 L 7 2 4F 4 F RT A16WE E2GL 2001110800074 20011108 00074 NM 2001 11 8 2001UALA02178 1 20011026 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 918UA 25385 AFT PIT BODY FRAME INNER FLANGE HAS A DENT AT BODY STATION 727A STRINGER 24R. MAJOR REPAIR ACCOMPLISHED. SPLICE ANGLE D OUBLER MANUFACTURED AND INSTALLED. STRINGER CLIP INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001110800075 20011108 00075 NM 2001 11 8 2001UALA02179 1 20011030 A 5240 DOOR FRAME BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE R2 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 181UA 25278 NR 2 RIGHT HAND MED UPPER DOOR FRAME AT GATE HAS CRACK ATTACH HOLE. DOOR SHOP ACCOMPLISHED REPAIR. 2 L 7 4 4F 4 F RT A20WE E24NE 2001110800076 20011108 00076 NM 2001 11 8 2001UALA02180 1 20011030 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 920UA 25387 RIGHT HAND OVERWING FRAME CRACKED AT STA 166 WATER LINE 208 FROM LOWER FASTENER TO FRAME CHORD. MAJOR REPAIR ACCOMPLISH ED. SPLICED IN NEW WEB SECTION WITH REINFORCING ANGLE SUPPORT. 2 L 7 2 4F 4 F RT A16WE E2GL 2001110800078 20011108 00078 WP 2001 11 8 MWEA011423 1 20011030 A 5330 591342137 SKIN DOUG DC9 DC982 3022082 WP STATION 110 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 CRACK IN FUSALAGE SKIN COMING FROM RIGHT HAND AFT NOSE GEAR DOOR AFT HINGE CUT OUT -- INSTALLED REPAIRED DOUBLER. 2 L 7 2 4F A6WE 2001110800079 20011108 00079 WP 2001 11 8 MWEA011424 1 20011030 A 5330 591342137 SKIN DOUG DC9 DC982 3022082 WP STATION 110 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 CRACK IN FUSALAGE SKIN COMING FROM LEFT HAND AFT NOSE GEAR DOOR AFT HINGE CUT OUT -- INSTALLED REPAIRED DOUBLER. 2 L 7 2 4F A6WE 2001110800080 20011108 00080 NM 2001 11 8 2001UALA02182 1 20011029 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 336UA 24240 BODY STATION 188 FRAME, WL 207 AT STRINGER 17 RT IS CRACKED. MAJOR REPAIR ACCOMPLISHED. CRACK STOP DRILLED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001110800081 20011108 00081 NM 2001 11 8 2001UALA02183 1 20011030 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 647UA 25284 MAIN CABIN FLOORBEAM STATION 798 LBL 19-15 UPPER CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED FLOORBEAM SPLICE P ER SRM 53-00-51 FIG 203. 2 L 7 2 4F 4 F RT A1NM E24NE 2001110800083 20011108 00083 NM 2001 11 8 2001UALA02185 1 20011031 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCONNECTED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 193UA 26890 EMERGENCY EEL LIGHT JUST FORWARD OF AFT LAV 17. FOUND FEEDER CABLE NOT HOOKED UP TO POWER CABLE. CONNECTED AND REPLACE D CABLE CONNECTED TO EEL LIGHT ASSY, OPS CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2001110800084 20011108 00084 NM 2001 11 8 2001UALA02186 1 20011101 A 5753 RUB STRIP BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE T/E FLAP MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 920UA 25387 RIGHT HAND INBOARD MID FLAP CENTER FOREFLAP TRACK SUPPORT RIB IS GOUGED IN BORE FOR FORWARD ROLLER INBOARD RIB AND RIGHT HAND INBOARD MID FOREFLAP TRACK SUPPORT RIB IS WORN DUE TO MISSING WEAR STRIP CENTER TRACK OUTBOARD RIB. MAJOR REPAIR ACCOMPLISHED. REPLACED RIGHT HAND INBOARD MID FLAP, INBOARD AND OUTBOARD CENTER FOREFLAP TRACK SUPPORT RIBS. 2 L 7 2 4F 4 F RT A16WE E2GL 2001110800085 20011108 00085 NM 2001 11 8 2001UALA02187 1 20011031 A 5320 WEB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 328UA 24148 BODY STATION 198 WL 207 FLOOR WEB RIGHT HAND SIDE CRACKED AT LIGHTNING HOLE. MAJOR REPAIR ACCOMPLISHED. REPLACED INTE RCOSTAL WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2001110800086 20011108 00086 NM 2001 11 8 2001UALA02190 1 20011031 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 FUSELAGE DENT ON A STRINGER 15L STA.610. MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW STRINGER AND INSTALLED FUSELAGE EXTE RNAL DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2001121700101 20011217 00101 EU 2001 12 17 2001UALA02193 1 20011031 A 5270 PROXIMITY SWITCH AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY EXIT OUT OF ADJ A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 453UA 1001 LEFT AFT OVERWING EMERGENCY EXIT OPEN ELECTRONIC CENTRALIZED AIRCRAFT MONITORING (ECAM) WARNING DURING CLIMB THROUGH FL 200. NO DEPRESSURIZATION. ECAM DISAPPEARED IN DESCENT BELOW 8000 FEET. FOUND EMERGENCY HANDLE COVER PROXIMITY SWITCH O UT OF TARGET. ADJUSTED TARGET AND TEST OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2001110800089 20011108 00089 NM 2001 11 8 2001UALA02194 1 20011101 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 328UA 24148 RIGHT FUSELAGE STATION 425, BETWEEN STRINGER 24R & 25R, DENT IS OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. INSTALLED FL USH REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001110800090 20011108 00090 NM 2001 11 8 2001UALA02195 1 20011101 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 328UA 24148 AFT CABIN STATION 947 LBL 12 TO LBL 13 WL 208 FLOORBEAM UPPER AFT FLANGE HAS 20 PERCENT MATERIAL REMOVED DURING REWORK. L-ANGLE DOUBLER MANUFACTURED AND INSTALLED. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001110800091 20011108 00091 NM 2001 11 8 2001UALA02196 1 20011101 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 336UA 24240 STATION 663.75 FUSELAGE FRAME HAS A CRACK STRINGER 1, STRINGER 2L, STRINGER 2R, STRINGER 3, STRINGER 3L. DAMAGE REMOVED . INSTALLED EXTERNAL SKIN DOUBLER AND TRIPLER AND STRAP REPAIR ON LOWER FLANGE. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121700102 20011217 00102 NM 2001 12 17 2001UALA02198 1 20011031 A 2751 WIRE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE T/E FLAP BROKEN A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 29 605UA 21866 FLAPS STUCK AT F5 DURING RETRACTION. A BROKEN WIRE BETWEEN THE NR 4 T/E FLAP POSITION TRANSMITTER AND THE FLAP/SLAT ELE CTRONICS UNIT (FSEU) CAUSED THE FSEU TO INITIATE T/E FLAP SHUT DOWN AND ILLUMINATE BOTH THE T/E FLAP SHUTDOWN AND T/E FL AP DISAGREE MESSAGE ON EICAS WITH T/E FLAP CAUTION LIGHT. REPAIRED WIRING AS REQUIRED. REPLACED FSEU AND NR 4 T/E FLAP POSITION TRANSMITTER PER APPLICABLE MAINTENANCE MANUAL AS PRECAUTION. OPS CHECKED T/E FLAP SYSTEM PER APPLICABLE MAIN TENANCE MANUAL AND ALL OPS CHECKS ARE NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 2001110800094 20011108 00094 EA 2001 11 8 A6WA200100057 1 20011025 A 2781 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A A6WA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 31 407AW 7424 FLAP FAIL CAS MESSAGE ON APPROACH. MAINTENANCE C/W AWAC SUPPLEMENT 98-18 OPS GOOD ECU CODES, JAM, RBPSU, PDU DIFF. 2 L 7 2 4F RT A21EA 2001110800095 20011108 00095 WP 2001 11 8 ABXA010571 1 20011104 A 2160 60714621 CONTROL VALVE DOUG DC9 DC931 3022065 WP CABIN TEMP DEFECTIVE A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 929AX 1159 45874 SLOW BUT STEADY LOSS OF CABIN PRESSURIZATION AT FLIGHT LEVEL 350, FOLLOWED BY ODOR OF HEAT FILLING THE COCKPIT. EMERGEN CY DECLARED. SELECTED HIGH PRESSURE BLEED OFF. ODOR PERSISTED. BELOW 10,000 FEET, VENTED AIRCRAFT, ODOR GONE. INSPEC TED TAIL COMPARTMENT WITH ENGINES AND APU RUNNING. NO LEAKS NOTED. PRESSURIZED AIRCRAFT WITH ENGINE AND APU PNEUMATICS . NO ODOR NOTED. REPLACED THE RIGHT CABIN TEMPERATURE CONTROL VALVE IAW DC-9 MM 21-60-00. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2001110800096 20011108 00096 NM 2001 11 8 AT0100233 1 20011101 A 3350 K2081746009G LIGHT BOEING 717 717200 1383700 NM CABIN LOOSE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 959AT 55021 FOUND EMERGENCY PATH LIGHT ASSEMBLY LOOSE AT SEAT 24. REMOVED AND REPLACED LIGHT FAIRING ON SEAT 24 IAW B717 MM 25-23. 2 L 7 2 4F TR A6WE 2001110800097 20011108 00097 NM 2001 11 8 2001F00633 1 20010126 A 3244 039781R TIRE BOEING 737 737297 1384480 NM LT MLG SEPARATED A KNNA O OTHER S AFFECT SYSTEMS TO TAKEOFF 1 WP 25 147AW 22630 LOSS OF A SYSTEM HYDRAULICS. LEFT INBOARD TIRE LOST TREAD DURING TAKEOFF ROLL. PIECES OF THE TIRE TREAD DAMAGED HYDRAU LIC LINES AND CONTROL CABLES LOCATED IN THE LEFT WHEEL WELL. ALSO, DAMAGE FROM FLYING RUBBER TO LEFT FORE FLAP, MID FLA P AND TRAILING EDGE FLAP ASSY. REPLACED NR 2 MAIN WHEEL/TIRE ASSY. REPLACED DAMAGED HYDRAULIC LINES AND DAMAGED FLIGHT CONTROL CABLES. (M) 2 L 7 2 4F A16WE 2001110800098 20011108 00098 NE 2001 11 8 2001F00634 2 20010405 A 7261 3031697CL SEAL PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE ENGINE COKED A S4WA O OTHER O OTHER NR NOT REPORTED 1 WP 07 308NA 226 PCEPR0082 THE ENGINE OIL USAGE HAD INCREASED SIGNIFICANTLY. UP TO 1 QUART IN ONE HOUR OF FLIGHT TIME. WE SPLIT THE ENGINE AND IN SPECT THE NR 2 MAIN BEARING LABYRINTH SEAL AREA. THERE IS A KNOWN PROBLEM OF THIS AREA RUNNING HOTTER THAN NORMAL AND A COKING PROBLEM HAS OCCURRED. THE ACTION TAKEN WAS TO INCORPORATE PW SB 14320 WHICH CHANGED THE OIL JET FOR THE NR 2 MAI N BEARING AND THE NR 2 BEARING COVER AND SEAL. ALSO, REMOVED THE CARBON DEPOSITS FROM THE SEAL SURFACES. THIS ALLOWS M ORE COOLING IN THE AREA AND THIS REDUCING THE CHANCES OF THE COKING PROBLEM RECURRING. FLEW AIRCRAFT FOR APPROXIMATELY 1 HOUR TO VERIFY THAT THE OIL USE AGE PROBLEM HAD SUBSIDED. CHECKED OK. (M) 1 L 7 1 3T 4 T RT A78EU E26NE 2001110800100 20011108 00100 SO 2001 11 8 ASOA01193 1 20011001 A 5313 12005710002 STRINGER EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 245AS 120075 WHILE PERFORMING MAINTENANCE IN MCN, CORROSION WAS FOUND ON STRINGER 21 RIGHT, BETWEEN FRAMES 19 AND 20 AND ALSO BETWEEN FRAMES 21 AND 22. MAINTENANCE WILL REPAIR CORROSION IAW SRM 53-10-04. THIS SRM OUTLINES REPAIR SPECIFICATIONS FOR FOR WARD FUSELAGE REPAIR AND REPLACEMENT. (M) 2 L 7 2 4T RT A31SO 2001110800101 20011108 00101 SO 2001 11 8 ASOA01194 1 20011001 A 5313 12005710005 STRINGER EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 245AS 120075 WHILE PERFORMING MAINTENANCE IN MCN, CORROSION WAS FOUND ON STRINGER 18 RIGHT, BETWEEN FRAMES 19 AND 20. MAINTENANCE WI LL REPAIR CORROSION IAW SRM 53-10-04. THIS SRM OUTLINES REPAIR SPECIFICATIONS FOR FORWARD FUSELAGE REPAIR AND REPLACEME NT. (M) 2 L 7 2 4T RT A31SO 2001110800102 20011108 00102 SO 2001 11 8 ASOA01195 1 20011001 A 5320 SUPPORT EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 245AS 120075 WHILE PERFORMING MAINTENANCE IN MCN, CORROSION WAS FOUND ON THE SKIN SUPPORTS BETWEEN STRINGER 20 AND 21 RIGHT AT FRAMES 17, 18, 18A, 18B AND 21. CORROSION WAS ALSO FOUND ON THE SKIN SUPPORTS BETWEEN STRINGER 20 AND 19 RIGHT AT FRAMES 20 A ND 21. MAINTENANCE WILL REPAIR CORROSION IAW SRM 53-10-04. THIS SRM OUTLINES REPAIR SPECIFICATIONS FOR FORWARD FUSELAG E REPAIR AND REPLACEMENT. (M) 2 L 7 2 4T RT A31SO 2001110800103 20011108 00103 SO 2001 11 8 ASOA01196 1 20011003 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT 3260202 SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 242AS 120069 FLT 4349 - DURING GROUND INSPECTION IN ATL, THE EMERGENCY DOOR/CLOSET EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REM OVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001110800104 20011108 00104 EU 2001 11 8 ASOA01197 1 20011003 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 636AS 375 DURING GROUND INSPECTION IN ATL, CREW REPORTED THE EMERGENCY EXIT LIGHT OVER THE AFT SERVICE DOOR WAS INOPERATIVE. MAIN TENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2001110800105 20011108 00105 SO 2001 11 8 ASOA01198 1 20011003 A 3242 21661 BRAKE EMB 120 EMB120ER 3260203 SO RT MLG FAILED A ASOA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 11 500AS 120272 FLT 4066 - CREW REPORTED THE RIGHT MAIN LEFT INBOARD BRAKE LOCKED UP DURING TAXI OUT OF ATL. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN LEFT INBOARD BRAKE ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETUR NED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001110800106 20011108 00106 SO 2001 11 8 ASOA01199 1 20011004 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT 3260202 SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 247AS 23247 120113 FLT 4659 - DURING SCHEDULED INSPECTION IN ABY, THE NR 1 EMERGENCY LIGHTING BATTERY WAS WEAK. THIS CAUSED THE FORWARD RO W OF ESCAPE PATH LIGHTS TO GO OUT AFTER APPROXIMATELY TEN SECONDS. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHTING BATTERY PACK. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001110800107 20011108 00107 SO 2001 11 8 ASOA01200 1 20011005 A 5330 12022788017 SKIN EMB 120 EMB120RT 3260202 SO FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 274AS 120229 DURING SCHEDULED MAINTENANCE IN TXK, A SKIN CRACK, APPROX .75 INCH LONG, WAS FOUND .5 INCH ABOVE THE TOP BRACKET FASTENE R ON THE CAPTAINS LOWER FORWARD CORNER OF THE DV WINDOW POST. MAINTENANCE PERFORMED A TEMPORARY REPAIR IAW ASA EO 120-5 3-0168. THIS EO PROVIDES FOR A TEMPORARY FLIGHT AUTHORIZATION FOR A SKIN CRACK BELOW THE CAPTAINS DV WINDOW. THIS EO A LSO OUTLINES THE REMOVAL OF A SHEAR CLIP, REFERENCING SERVICE BULLETIN 120-53-0073. THIS AIRCRAFT REQUIRES DAILY INSPEC TION FOR PROPAGATION DURING THE NEXT 100 FLIGHT CYCLES. (M) 2 L 7 2 4T RT A31SO 2001110800108 20011108 00108 EU 2001 11 8 ASOA01201 1 20011005 A 3350 E0062B1A4AC0A SWITCH AEROSP ATR72 ATR72212 8680945 EU COCKPIT BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 532AS 458 FLT 4050 - DURING GROUND INSPECTION IN ATL, CREW REPORTED THE EMERGENCY LIGHTS REMAINED ON WITH THE COCKPIT SWITCH IN TH E ARM POSITION AND THE GENERATORS ONLINE. MAINTENANCE INSPECTED AND FOUND THE EMERGENCY LIGHT TOGGLE SWITCH TO BE INTER NALLY BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT TOGGLE SWITCH. EMERGENCY LIGHT SYSTEM OPERATES NORM ALLY. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2001110800109 20011108 00109 SO 2001 11 8 ASOA01202 1 20011006 A 3350 1317 LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 266AS 120188 DURING SCHEDULED MAINTENANCE IN MCN, THE LEFT FORWARD OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE LEFT FORWARD OVERWING EMERGENCY EXIT LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001110800110 20011108 00110 SO 2001 11 8 ASOA01203 1 20011007 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT 3260202 SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 238AS 120053 DURING HANGAR MAINTENANCE IN MCN, BOTH LEFT AND RIGHT SIDE AFT EXTERIOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTE NANCE REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHTING BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001110800111 20011108 00111 EA 2001 11 8 MASA01010 1 20010121 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37342 7342 FLT 5764 - STL-PHL - EMERGENCY FLOOR PATH PROXIMITY LIGHTING SECTIONS 9 THROUGH 12 WILL NOT ILLUMINATE DURING EMERGENCY LIGHT PRE-FLIGHT OPS CHECK. MAINTENANCE FOUND LOOSE CONNECTOR AT FLOOR STRIP. RECONNECTED, OPS CHECKS GOOD. THE AIRCR AFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001110900001 20011109 00001 2001 11 9 SWAA013025 4 20011105 A 2565 65C19901 CABLE BOEING 737 737317 138447P NM AFT SVC DOOR FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. R&R SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2001110900002 20011109 00002 NM 2001 11 9 SWAA013027 1 20011106 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 735SA 27867 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS BROKEN ( 8 EA ). R&R COVERS PER MM. 2 L 7 2 4F RT A16WE 2001110900003 20011109 00003 NM 2001 11 9 SWAA013031 1 20011103 A 5753 6573735 FLAP BOEING 737 7375H4 138449D NM LH WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 528SW 26570 DURING SCHEDULED C2 CHECK, FOUND LH OTBD AFT FLAP T/E CORNER DELAMINATED. REPAIRED FLAP P ER SRM. 2 L 7 2 4F RT A16WE 2001110900004 20011109 00004 NM 2001 11 9 SWAA013033 1 20011107 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 781WN 30601 DURING SCHEDULED C4 CHECK, FOUND SEVERAL EEPLS COVERS CRACKED IN FWD CABIN. R&R COVERS PER MM . 2 L 7 2 4F RT A16WE 2001110900005 20011109 00005 NM 2001 11 9 SWAA013035 1 20011106 A 5753 6546434 FLAP BOEING 737 7373H4 1384600 NM LH WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 626SW 27702 DURING SCHEDULED C2 CHECK, FOUND LH INBD AFT FLAP DELAMINATED AT OTBD FWD END. R&R FLAP P ER MM. 2 L 7 2 4F RT A16WE 2001110900006 20011109 00006 NM 2001 11 9 SWAA013036 1 20011107 A 5312 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 380SW 26587 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, WL 227 & RBL 17.1. R &R VERTICAL BEAM PER SRM. 2 L 7 2 4F RT A16WE 2001110900007 20011109 00007 NM 2001 11 9 SWAA013037 1 20011106 A 5320 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 27L. R&R SHEAR TIE PE R SRM. 2 L 7 2 4F RT A16WE 2001110900008 20011109 00008 NM 2001 11 9 SWAA013038 1 20011107 A 5310 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 20R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001110900009 20011109 00009 NM 2001 11 9 CALA0100994 1 20011106 A 5320 WEB BOEING 737 7373T0 1384582 NM STA 492 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59338 23576 INSPECTION FOUND A 1/4" CRACK IN FORWARD BAGGAGE BIN WEB AT DOOR JAMB, STA 492, S25R. REPAIRED WEB IAW SRM 51-70-13. 2 L 7 2 4F RT A16WE 2001110900010 20011109 00010 NM 2001 11 9 CALA0100995 1 20011107 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 807 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59338 23576 INSPECTION FOUND FUSELAGE SKIN DENTED AND INTERNAL INTERCOSTALS BROKEN AT STA 807 FROM LBL 10 TO RBL 10. REPAIRED IAW SR M 51-10-02. 2 L 7 2 4F RT A16WE 2001110900011 20011109 00011 WP 2001 11 9 CALA0100996 1 20011108 A 5320 INTERCOSTAL DOUG DC9 DC983 3022083 WP STA 1155 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14879 49526 INSPECTION FOUND INTERCOSTAL CORRODED IN AFT BAGGAGE BIN BETWEEN LONGERON 30 AND 29R JUST FORWARD OF FRAME STA 1155. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-5. 2 L 7 2 4F RT A6WE 2001112700031 20011127 00031 NM 2001 11 27 SABA011060 1 20011106 A 2932 7G773 PRESSURE SWITCH DHAV DHC8 DHC8103 1386005 NM HYDRAULIC SYS BACKED OUT A SABA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 33 801WP 086 AIRCRAFT 801 ON FLIGHT 5025 HAD A NUMBER TWO HYDRAULIC SYSTEM FAILURE. FLIGHT WAS DIVERTED. IN-FLIGHT EMERGENCY WAS DE CLARED AND EMERGENCY PROCEDURES WERE USED. AIRCRAFT LANDED WITH NO OTHER PROBLEMS. MAINTENANCE FOUND THE NUMBER NUMBER TWO HYDRAULIC PRESSURE SWITCH SAFETY WIRE BROKEN AND THE SWITCH HAD BACKED OUT. THIS WAS ALLOWING FLUID TO LEAK OVERBO ARD. REMOVED AND REPLACED O-RING, RETORQUED SWITCH, SERVICED SYSTEM AND SYSTEM OPS CHECKED GOOD. HYD PUMP AND FILTERS WERE CHANGED DUE TO CAVITATION OF SYSTEM. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001110900012 20011109 00012 SW 2001 11 9 2001F00635 1 20010131 A 3213 2751540003 PIN SWRNGN SA227 SA227AC 8780603 SW RT MLG BROKEN A BSAA O OTHER O OTHER NR NOT REPORTED 1 NM 05 27465 755B RIGHT MLG UPPER TORQUE LINK PIN BROKE IN TWO PLACES. REPLACED BROKEN PIN, INSPECTED GEAR, ATTACH TRUNNION, KEELSON WEBS, DRAG LINK ATTACH EARS, AND PERFORMED GEAR SWING. NO DEFECTS NOTED. ONE FRACTURE PLANE EXTENDED THROUGH APPROX 25 PERCEN T OF THE PIN, THIS IS THE SUSPECTED ORIGINAL FRACTURE. IT IS SUSPECTED THAT THE INITIAL FRACTURE PLANE GREW UNTIL THE RE MAINING CROSS SECTION OF THE PIN WASN'T SUFFICIENT TO MAINTAIN INTEGRITY. AT THAT TIME THE REMAINING CROSS-SECTION OF T HE ONE END OF THE PIN FAILED. THIS IS THE SUSPECTED ORIGINAL BREAKAGE POINT. WHEN THIS HALF OF THE PIN FAILED, THE OTH ER SIDE WAS SUBJECTED TO SUCH A HIGH LOAD THAT IT COMPLETELY FAILED AT ONE TIME, DURING THE LAST LANDING. (M) 2 L 7 2 4T RT A8SW 2001110900013 20011109 00013 GL 2001 11 9 SIMA0931A 2 20010403 A 7200 ENGINE EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL RIGHT LEAKING A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 723AE 145288 CAE311470 CMH - FLT 4975 - LAVATORY SMOKE INDICATION CAME ON DURING TRANSITION FROM APU BLEED TO ENGINE BLEED. POSSIBLE ENGINE OI L LEAK. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE IAW EMB MM. OPS AND LEAK CHECKS WERE GOOD AND AIRCRAFT WAS RE TURNED TO SERVICE. (M) 2 L 7 2 4F 4 F RT TOOO11AT TE6CH 2001111500027 20011115 00027 NM 2001 11 15 2001UALA02174 1 20011028 A 5330 143W23303 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUSELAGE BURNED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 770UA 26334 26925 STATION 718 AT STRINGER 44R HAS SKIN BURNED. NEEDS BURNISHING AND HIGH FREQUENCY EDDY CURRENT INSPECTION AND TREATMENT AND PAINT. MAJOR REPAIR ACCOMPLISHED. SKIN WAS BLENDED BEYOND LIMITS. INSTALLED REPAIR DOUBLER AND TRIPLER. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001110900014 20011109 00014 WP 2001 11 9 ANCF200100021 1 20011029 A 2133 CONNECTOR DOUG DC9 DC983 3022083 WP OUTFLOW VALVE DIRTY W ANCF D RETURN TO BLOCK G MULTIPLE FAILURE CL CLIMB 1 SO 23 593AN 53093 AFTER TAKEOFF AUTO PRESSURIZATION LEFT AND RIGHT INOPERATIVES. FLIGHT RETURNED TO BAQ. BITE ON BOTH PRESSURIZATION CON TROLLERS WAS PERFORMED, CONNECTOR ON OUT FLOW VALVE ACTUATORS WERE CLEANED AND ADJUSTED IN ACCORDANCE WITH AMM 21-32-00 PAGE 201. 2 L 7 2 4F RT A6WE 2001110900016 20011109 00016 NM 2001 11 9 AT0100234 1 20011101 A 3350 K2081740009G LIGHT BOEING 717 717200 1383700 NM CABIN LOOSE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 959AT 55021 FOUND EMERGENCY PATH LIGHT ASSEMBLY LOOSE AT SEAT 26. REMOVED AND REPLACED LIGHT FAIRING ON SEAT 26 IAW B717 MM 25-23. 2 L 7 2 4F TR A6WE 2001110900017 20011109 00017 NM 2001 11 9 AWXA200100537 1 20011003 A 5312 6545409245 PRESSURE PANEL BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - C16 CK - C - CRACK FOUND ON PRESSURE WEB IN LT MAIN LANDING GEAR WELL, CONFIRMED WITH HFEC, BS 664, LBL 32, 1.25 I NCH LONG. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW AWA ER 03-5702-01286-GF1. 2 L 7 2 4F RT A16WE 2001110900018 20011109 00018 NM 2001 11 9 AWXA200100539 1 20010909 A 5414 311N5002 SKIN BOEING 757 7572S7 1384962 NM NR 1 PYLON CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 PHX - C8 CK - C - CRACK FOUND ON NR 1 PYLON O/B SIDE SKIN AND DOUBLER 3 INCHES LONG AT PPS 156, PPWL 140, COMMON TO LOWE R CHORD. MAINTENANCE FABRICATED REPAIR DOUBLER AND INSTALLED IAW AWA ER 19-5450-01283-TB3. 2 L 7 2 4F RT A2NM 2001110900019 20011109 00019 NM 2001 11 9 AWXA200100540 1 20010909 A 5410 311N5002413 STIFFENER BOEING 757 7572S7 1384962 NM NR 1 PYLON CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 PHX - C8 CK - C - CRACK FOUND IN NR 1 PYLON, O/B SIDE VERTICAL STIFFENER, 1 INCH LONG AT PPS 153, PPWL 143. MAINTENANCE REMOVED AND REPLACED THE STIFFENER IAW B757 SRM 51-10-02, PG 2. 2 L 7 2 4F RT A2NM 2001110900020 20011109 00020 NM 2001 11 9 AWXA200100541 1 20010908 A 5311 146N1007 FRAME BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 PHX - C8 CK - C - GOUGE AND CRACK FOUND IN FRAME RADIUS AT BS 1320, STR 26R, .25 INCH LONG. MAINTENANCE CUT OUT DAMAGED SECTION OF FRAME, FABRICATED REPAIR ANGLES AND FILLER AND INSTALLED IAW B757 SRM 53-60-07 AND 51-70-11. 2 L 7 2 4F RT A2NM 2001110900021 20011109 00021 NM 2001 11 9 AWXA200100545 1 20010906 A 5315 141N5113 FLOORBEAM BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 PHX - C8 CK - C - CORROSION FOUND ON TOP CAP OF FLOORBEAM AT BS 377, LBL 15 TO LBL 60, BEYOND SRM ALLOWABLE LIMITS. MAI NTENANCE REMOVED DAMAGED SECTION OF FLOORBEAM UPPER CAP, FABRICATED REPAIR PARTS AND INSTALLED IAW AWA ER 19-5311-01269- DL4. 2 L 7 2 4F RT A2NM 2001110900022 20011109 00022 NM 2001 11 9 AWXA200100547 1 20010908 A 5311 146N1008 FRAME BOEING 757 7572S7 1384962 NM FUSELAGE GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 PHX - C8 CK - C - DENT FOUND IN FRAME WITH A GOUGE IN THE RADIUS AT BS 1340, STR 26R. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED REPAIR ANGLE AND INSTALLED IAW B757 SRM 51-70-11 FIG 1, PG 1 - 7. 2 L 7 2 4F RT A2NM 2001110900023 20011109 00023 NM 2001 11 9 AWXA200100561 1 20010905 A 5330 144N3100903 SKIN BOEING 757 7572S7 1384962 NM FUSELAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 PHX - C8 CK - C - INTERIM FUSELAGE SKIN EXTERNAL REPAIR AT BS 1180, STR 6L REQUIRES REPLACEMENT. MAINTENANCE REMOVED EX ISTING REPAIR AND REPLACED WITH PERMANENT FLUSH REPAIR IAW AWA ER 19-5341-01288-TB1A. 2 L 7 2 4F RT A2NM 2001110900024 20011109 00024 NM 2001 11 9 AWXA200100569 1 20011027 A 5315 65498841 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 MCN - C13 CK - C - CORROSION FOUND FLOORBEAM UPPER FLANGE AT BS 967.5, RBL 8 TO RBL 50, BEYOND SRM LIMITS AFTER CLEAN UP . MAINTENANCE CUT OUT DAMAGED SECTION OF FLOORBEAM UPPER FLANGE (PREVIOUSLY REPAIRED), FABRICATED REPAIR ANGLES AND STR APS AND INSTALLED IAW B737 SRM 53-10-9, FIG 2, PG 7 - 11. 2 L 7 2 4F RT A16WE 2001110900025 20011109 00025 NM 2001 11 9 AWXA20010062 1 20010928 A 5315 BAC150510617 FLOORBEAM BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 PHX - C8 CK - C - CORROSION FOUND ON FLOORBEAM UPPER CAP AT BS 365.25, RBL 18, BEYOND SRM LIMITS AFTER CORROSION REMOVAL . MAINTENANCE MADE STRAP REPAIR ON FLOORBEAM UPPER CAP IAW AWA ER 19-5310-01289-KB1. 2 L 7 2 4F RT A2NM 2001110900026 20011109 00026 NM 2001 11 9 C1HA200181015 1 20011021 A 7997 CONNECTOR BOEING 727 7272S7 138407Z NM OIL SYSTEM DIRTY A C1HA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 15 681CA 22020 ENGINE NR 2 ON TAKEOFF NR 2 OIL QUANTITY GAUGE WENT TO 0 QUANTITY. ABORTED TAKEOFF. CLEANED CANNON PLUG AT TANK UNIT. SERVICED OIL TO FILL. INDICATION WAS NORMAL. REFERENCED MM 79-32. 2 L 7 3 4F A3WE 2001110900027 20011109 00027 NM 2001 11 9 C1HA200184012 1 20011011 A 3350 900835A LIGHT BOEING 727 7272S7 138407Z NM CABIN INOPERATIVE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 684CA 22491 LEFT OVERWING EMERGENCY LIGHTS INOPERATIVE. RELAMPED, REMOVED AND REPLACED BATTERY PACK IAW 33-50-21 AND 33-50-11. 2 L 7 3 4F A3WE 2001110900028 20011109 00028 NM 2001 11 9 C1HA200194019 1 20011019 A 2750 FLAP BOEING 727 727290 138408W NM WING OUT OF POSITION A C1HA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 15 294AS 22146 APPLIED POWER FOR TAKEOFF, WARNING HORN CAME ON. PULLED OFF THE RUNWAY, RECONFIGURED THE FLAPS, ADVANCED EACH POWER LEV ER PAST 1.6 EPR. THERE WAS NO TAKEOFF WARNING HORN THIS TIME. TAKEOFF WARNING CHECKED, ALL CHECKS NORMAL AT THIS TIME IAW MM CH 31-26. 2 L 7 3 4F A3WE 2001110900029 20011109 00029 NM 2001 11 9 C1HA200194020 1 20011022 A 2611 SMOKE DETECTOR BOEING 727 727290 138408W NM LAVATORY FAILED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 294AS 22146 FORWARD LAVATORY SMOKE DETECTOR DOESN'T TEST. OPS TESTED SMOKE DETECTOR, TESTED NORMAL. 2 L 7 3 4F A3WE 2001110900030 20011109 00030 NM 2001 11 9 C1HA200195016 1 20011017 A 3610 CLAMP BOEING 727 727290 138408W NM BLEED AIR LOOSE A C1HA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 295AS 22147 AFTER TAKEOFF AT 3000 FT, AFTER SETTING CLIMB POWER ENGINE NR 3 STRUT OVERHEAT WARNING LIGHT ILLUMINATED. UTILIZED EMER GENCY AND NORMAL PROCEDURES. UNABLE TO SAFELY CONTINUE FLIGHT TO DESTINATION WITH ONE PACK OFF (AT LOWER ALTITUDE). DU MPED FUEL TO BELOW LANDING WEIGHT. LANDED AT MMUM SAFELY. ENG NR 3 MODULATING AND SHUTOFF VALVE CLAMPS WERE TIGHTENED. ENGINE NR 3 RUN UP PER MM 75-31-0 AND SETTING EPR AT 1.8. NO LEAKS FOUND. 2 L 7 3 4F A3WE 2001110900031 20011109 00031 NM 2001 11 9 C1HA200195017 1 20011017 A 3610 CLAMP BOEING 727 727290 138408W NM BLEED AIR LOOSE A C1HA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 295AS 22147 AFTER TAKEOFF AT 12,500 FT WITH CLIMB POWER SET, ENGINE NR 3 STRUT OVERHEAT WARNING LIGHT ILLUMINATED. UTILIZED EMERGEN CY AND NORMAL PROCEDURES. UNABLE TO SAFELY CONTINUE FLIGHT TO DESTINATION WITH ONE PACK OFF (AT LOWER ATTITUDE) DUMPED FUEL TO BELOW, MAX LANDING WEIGHT AT MMUN SAFELY. ENG NR 3 7TH STAGE CLAMPS AND 6TH STAGE CLAMPS ON DUCTS LEAKS REPAIRE D AS REQUIRED. RUN UP ENG WITH A/C PACK RT ON, TEST ON GROUND OK. NO LEAKS. 2 L 7 3 4F A3WE 2001110900032 20011109 00032 NM 2001 11 9 C1HA200197009 1 20011027 A 3350 BATTERY PACK BOEING 727 727270 138408P NM CABIN DISCHARGED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 697CA 23052 AFT EMERGENCY EXIT LIGHTS INOP. REPLACED AFT BATTERY PACK AND OPS CHECK GOOD PER MM 33-50-01. 2 L 7 3 4F RT A3WE 2001110900034 20011109 00034 NM 2001 11 9 CALA0100980 1 20011028 A 2612 43367310044061 SWITCH BOEING 757 757224 1384958 NM CARGO BAY CONTAMINATED A CALA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 09 21108 27298 THE FORWARD CARGO FIRE LIGHT AND BELL ACTIVATED WHILE EN ROUTE FROM IAH TO CUN. A FIRE BOTTLE WAS DISCHARGED AND THE FL IGHT WAS DIVERTED TO MID. THE FIRE LIGHT EXTINGUISHED ABOUT THREE MINUTES LATER. THE AIRCRAFT LANDED AT MID WITHOUT IN CIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE OR SMOKE. A LIGHT TEST WAS PERFORMED AND A FIRE WARNING OCCURRED. THE C ARGO FIRE ARMING SWITCH WAS REMOVED AND REPLACED DUE TO CONTAMINATION FOUND. OPERATION AND INDICATIONS CHECKED GOOD. B OTH CARGO FIRE BOTTLES WERE REMOVED AND REPLACED IAW MM 26-23-02. 2 L 7 2 4F RT A2NM 2001110900035 20011109 00035 NM 2001 11 9 CALA0100981 1 20011026 A 5347 CARGO TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69333 23571 INSPECTION FOUND TIE DOWN RAIL CORRODED AROUND FASTENER HOLES AT STA 727-945.5, RBL 26. THE CORRODED SECTIONS OF TIE DO WN RAIL WERE REMOVED AND REPLACED IAW SRM 53-00-53, FIGURE 202. 2 L 7 2 4F RT A16WE 2001110900036 20011109 00036 NM 2001 11 9 CALA0100993 1 20011031 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59338 23576 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 950, RBL 9-17. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001110900037 20011109 00037 SO 2001 11 9 CHQ0034 1 20011031 A 2730 SWITCH EMB 145 EMB145 3260210 SO COCKPIT INOPERATIVE A CHQA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 GL 11 265 145226 BOTH TRIM SWITCHES INOP. 2 L 7 2 4F RT T00011AT 2001110900038 20011109 00038 2001 11 9 CNMA200100034 4 20011025 A 3418 9654020003 SENSOR BOEING 75 A75L300 1380132 CE STALL WARNING MALFUNCTIONED A CNMA J A DUMP FUEL UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SW 07 450 754781 ON ROTATION GOT THE STICK SHAKER AND AURO SLAT EXTENDED, PULLED STALL WARNING CIRCUIT BREAKERS ACCORDING TO CHECKLIST. DUMPED 20,000 LBS OF FUEL AND RETURNED TO AIRPORT. REMOVED AND REPLACED AOA SENSOR IAW MM 22-33, OPS CHECKED GOOD. 1 Q 7 1 3R A743 2001110900039 20011109 00039 EA 2001 11 9 COMA0160865 1 20011030 A 3397 6464 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN DIRTY A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 420CA 7451 FLIGHT 5904 EMERGENCY FLOOR PATH LIGHTING, ROWS 2 THRU 5 DO NOT ILLUMINATE AT FULL INTENSITY. REPLACED FLOOR LIGHTS CAB LE ASSY, SYSTEM TEST NORMAL. 2 L 7 2 4F RT A21EA 2001110900040 20011109 00040 EU 2001 11 9 DHL2001362034 1 20011102 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU CARGO BAY WILL NOT TEST A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 362DH 84 AFT DUCT CARGO SMOKE DETECT WILL NOT TEST. RERACKED LOWER CARGO SMOKE DETECTOR UNIT BOX IAW A-300 MM 26-14-00, OPS CHEC K SERVICEABLE. 2 L 7 2 4F RT A35EU 2001110900042 20011109 00042 NM 2001 11 9 DHL2001743013 1 20011102 A 3040 MOTOR BOEING 727 727225 1384077 NM WINDSHIELD FAILED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 743DH 22438 CAPTAINS WIPER DOES NOT WORK AT ANY SPEED. REMOVED AND REPLACED CAPTAINS WINDSHIELD WIPER DRIVE ASSY IAW MM CH 30-42-12 . OPS CHECK GOOD. 2 L 7 3 4F A3WE 2001110900043 20011109 00043 NM 2001 11 9 DHL2001748006 1 20011102 A 2612 GROMMET BOEING 727 727225 1384077 NM FIRE LOOP LOOSE A DHLA O OTHER N FALSE WARNING TO TAKEOFF 1 SO 01 748DH 22440 FIRE PROTECTION SYSTEM NR 1 ENG DETECTION LIGHT ON DURING T/O & CLIMB, OFF IN CRUISE. RESECURED TWO GROMMETS ON FIRE LO OP. OPERATIONAL CHECK SERVICEABLE IAW B727 MM 26-11-00. 2 L 7 3 4F A3WE 2001110900044 20011109 00044 WP 2001 11 9 DHL2001801565 1 20011022 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 FRAME CRACKED 1 INCH AT STA 131.000, L-32R (CAP). TRIMMED OUT SKIN SEGMENT TO REMOVE FRAME CAP AND FABRICATED SPLICE DO UBLER PER DHL EO 011017, EO 2672, SEMAN EO 2001388. REMOVED DAMAGED FRAME CAP PER EA 2001385. INSTALLED FRAME CAP, SPL ICE AND DOUBLER PER EO DHL 011017, EO 2672 AND SEMAN EO 2001388. 2 L 7 4 4F RT 4A25 2001110900045 20011109 00045 WP 2001 11 9 DHL2001801566 1 20011001 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 LEFT WING L/E LWR SKIN CRACKED .5 INCH AT XFS 597.500. STOP DRILLED CRACK AND FABRICATED DOUBLER PER EO DHL 011003, EO 2653 AND SEMAN EO 2001368. INSTALLED DOUBLER REPAIR PER EO DHL 011003, EO 2652 AND SEMAN EO 2001368. 2 L 7 4 4F RT 4A25 2001110900046 20011109 00046 WP 2001 11 9 DHL2001801567 1 20010930 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 RIGHT WING L/E HAS A .5 INCH CRACK ON LWR SURFACE, STA XFS 597.500. STOP DRILLED CRACK AND FABRICATED REPAIR DOUBLER PE R DHL EO 011002, EO 2654 AND SEMAN EO 2001369. INSTALLED DOUBLER REPAIR PER DHL EO 011002, EO 2654, AND SEMAN EO 2001369 . 2 L 7 4 4F RT 4A25 2001110900047 20011109 00047 WP 2001 11 9 DHL2001803017 1 20011104 A 2612 WIRE DOUG DC8 DC873 302199C WP NR 4 ENGINE CHAFED A DHLA E ENGINE SHUTDOWN N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 803DH 46123 NR 4 ENGINE SHORT CIRCUIT LIGHT FLASHING ON, THEN FIRE WARNING BELL CAME ON WHILE ENGINE WAS SHUTDOWN DURING PARKING IN TJSJ. TROUBLESHOOT AND FOUND WIRE 4W5122C16 CHAFING TO GROUND BEHIND J-BOX CONN. RS-7008. REPAIR AND SECURE WIRE IAW M M 20-50-1. GROUND OPS CHECKED NORMAL IAW MM 26-10-0. 2 L 7 4 4F RT 4A25 2001110900049 20011109 00049 CE 2001 11 9 GLBA2001226 1 20011101 A 2150 1183800043 SWITCH BEECH 1900 1900D 1154162 CE A/C BAY FAILED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 97UX 3161 UE97 DUAL ENVIRONMENTAL FAILURE. INSPECTED AND REPLACED OVERPRESSURE SWITCH, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001123100043 20011231 00043 CE 2001 12 31 GLBA2001228 1 20011106 A 2750 FLAP BEECH 1900 1900D 1154162 CE WING MALFUNCTIONED A GLBA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 03 253GL UE253 FLAPS WOULD NOT RETRACT FROM 17 PERCENT. COULD NOT DUPLICATE, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001112100126 20011121 00126 CE 2001 11 21 GLBA2001229 1 20011106 A 2150 A/C PACK BEECH 1900 1900D 1154162 CE A/C BAY MALFUNCTIONED A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 03 257GL UE257 LEFT ENVIRONMENTAL FAIL ON T/O. INSPECTED, COULD NOT DUPLICATE. 2 L 7 2 4T RT A24CE 2001110900050 20011109 00050 NM 2001 11 9 HNAA0100071 1 20011023 A 5347 SEAT TRACK DHAV DHC8 DHC8201 2809001 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 988HA 426 RIGHT INBOARD SEAT RAIL HAS SEVERAL AREAS OF CORROSION BETWEEN STATIONS X204 AND X214.5. MAX DEPTH IS .048 INCH. REPAI RED IAW EO8-53-01-517. 2 H 7 2 4T RT A13NM 2001110900051 20011109 00051 NM 2001 11 9 HNAA0100073 1 20011023 A 5347 SEAT TRACK DHAV DHC8 DHC8201 2809001 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 988HA 426 LEFT INBOARD SEAT RAIL HAS CORROSION ON OUTBOARD FLANGE FROM STATION X203 TO X222. MAX DEPTH IS .021 INCH. REPAIRED IA W EO8-53-01-513. 2 H 7 2 4T RT A13NM 2001110900052 20011109 00052 WP 2001 11 9 IXXA0100069O 1 20011031 A 3297 CONNECTOR DOUG DC8 DC862 3021970 WP NLG LOOSE A IXXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 11 31CX 73562 237 45911 EN ROUTE FROM RMS TO AVB, AFTER THE LANDING GEAR WAS RETRACTED THE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. THE FLIGHT C REW CYCLED THE LANDING GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT RETURNED TO RMS FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE LANDING GEAR WARNING SYSTEM LOCATING A LOOSE CANNON PLUG ON THE NOSE LANDING GEAR PO SITION SWITCH. MAINTENANCE SECURED THE CANNON PLUG, PERFORM A SUCCESSFUL OPERATIONAL CHECK IN ACCORDANCE WITH THE MAINT ENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2001110900053 20011109 00053 SO 2001 11 9 LR7A01117 1 20011107 A 5320 FITTING LKHEED 382 382G 526414U SO FUSELAGE MISMANUFACTURED A LR7A K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 402LC 4698 DURING RIGHT NLG TRUNNION FITTING REPLACEMENT ON WORK ORDER 02/06/01 FOUND FS 165 PRESSURE BULKHEAD LOWER ATTACH ANGLE L UG INCORRECTLY MANUFACTURED AT RBL 18, WL 170. REPAIRED IAW SRM SMP 583-53-30-15. 2 H 7 4 4T A1SO 2001110900054 20011109 00054 EU 2001 11 9 MALA010765 1 20011025 A 3411 DRAIN LINE SAAB SF340 SF340A 7850100 EU PITOT/STATIC SYS CONTAMINATED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 119XJ 340A119 DURING FLIGHT 3327, INFLIGHT REACHING CRUISE, RUDDER LIMIT ILLUMINATED, LT AIR SPEED 195 KTS, AND STBY A/S 255 KTS. AIR RETURN TO MSP. MAINTENANCE FOUND WATER IN STBY PITOT DRAIN. PURGED DRAIN SYSTEM. COMPLETED PITOT STATIC LEAK CHECK O F STBY SYSTEM LEAK CHECKS GOOD. INSPECTED STBY PITOT TUBE DRAIN HOLE. NO DEFECTS NOTED, STBY PITOT HEAT CHECKS GOOD. STBY A/S INDICATOR AND ALT CHECK GOOD IAW SF340 AMM/ CHAP 34. LT A/S INDICATOR AND PITOT SYSTEM LEAK CHECK GOOD. 2 L 7 2 4T RT A52EU 2001110900055 20011109 00055 EU 2001 11 9 MALA010766 1 20011025 A 3020 44730501 CONTROL UNIT SAAB SF340 SF340A 7850100 EU ANTI-ICE SYS FAULTY A MALA K NONE J WARNING INDICATION CR CRUISE 1 GL 15 107XJ 340A107 DURING FLIGHT 3172, RT ENGINE INTAKE LIP ACCUMULATED SIGNIFICANT ICE WITH ALL ENGINE ANTI-ICE SYSTEMS WORKING OK. MAINT ENANCE CONDUCTED OPERATIONAL CHECK IAW SF340 MM CHAP 30. ALL CHECKS GOOD, INSTALLED SERVICEABLE DE-ICE CONTROL MODULE P /N 44730-501, S/N ON 6248467, S/N OFF AO0482. RE-INSTALLED PANELS 465BR & 465AE. ALL CHECK GOOD REPAIRED WIRING. 2 L 7 2 4T RT A52EU 2001110900056 20011109 00056 NE 2001 11 9 MWEA011418 2 20011105 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE LEFT VIBRATION A MWEA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 31 601ME 49762 P725366D FLIGHT ATTENDANTS REPORTED NR 1 ENGINE VIBRATION ON DEPARTURE. VIBRATION REMAINED WITH POWER REDUCTION. REPLACED LEFT HAND ENGINE. 2 L 7 2 4F 4 F RT A6WE E9NE 2001110900057 20011109 00057 WP 2001 11 9 MWEA011420 1 20011106 A 5523 5910413509 SKIN DOUG DC9 DC932 3022066 WP ELEVATOR TAB DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 LEFT HAND ELEVATOR CONTROL TAB UPPER SURFACE HAS A DENT BETWEEN THE NR 3 AND NR 4 HINGE POINTS, .75 BY .5 INCH. FABRICA TED CORE, FILLER AND DOUBLER. HOT BONDED REPAIR AND REPAINTED TRIM TAB. PERFORMED WEIGHT AND BALANCE. 2 L 7 2 4F A6WE 2001110900058 20011109 00058 WP 2001 11 9 MWEA011421 1 20011106 A 5330 591970731 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 CORROSION ON INNER FUSELAGE SKIN ST STATION 889 AND 897 ON RIGHT HAND SIDE OF INTERCOSTAL AFT PIT. REMOVED, FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001110900059 20011109 00059 NM 2001 11 9 MWEA011422 1 20011104 A 3320 BALLAST DOUG MD88 MD88 3023688 NM CABIN FAULTY A MWEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 31 601ME 49762 FLIGHT ATTENDANTS REPORTED HOT INSULATION ODOR IN VICINITY OF ROW 12/13. REPLACED BALLAST. 2 L 7 2 4F RT A6WE 2001110900062 20011109 00062 WP 2001 11 9 ABXA010572 1 20011107 A 3260 7000010101 SWITCH DOUG DC9 DC931 3022065 WP DEFECTIVE A ABXA O OTHER O OTHER CL CLIMB 1 GL 23 938AX 47009 LEFT MAIN GEAR UNSAFE LIGHT ILLUMINATED AFTER LANDING GEAR WAS RETRACTED. LANDING GEAR HANDLE WAS RECYCLED AND LIGHT WEN T OUT. REPLACED THE LEFT MAIN GEAR DOWNLOCK SWITCH. OPS CHECKED GOOD IAW DC-9 MM 32-60-01-2. 2 L 7 2 4F A6WE 2001110900063 20011109 00063 NM 2001 11 9 P2EA2001V0010 1 20011018 A 5730 SKIN BOEING 737 737230 1384401 NM RT WING DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 124NJ 22122 DURING C-CHECK RIGHT WING L/E SECTION FSS 338 OUTER SKIN WITH DENT. RIGHT WING L/E SECTION BETWEEN FSS 333.8 AND FSS 34 5.8 DUE TO DENT IAW SRM 57-30-4 FIG 5. 2 L 7 2 4F RT A16WE 2001110900065 20011109 00065 NM 2001 11 9 P5CA0100605 1 20011031 A 3350 6016123 POWER SUPPLY BOEING 747 747123 1384873 NM CABIN DISCHARGED A P5CA K NONE L NO TEST IN INSP/MAINT 1 WP 23 859FT 20326 CREW RIGHT UPPER DECK DOOR FRAME MOUNTED EXIT LIGHTS DO NOT ILLUMINATE DURING EMERGENCY LIGHT TEST. REMOVED AND REPLACE D UPPER DECK RT CREW DOOR FRAME LIGHT POWER SUPPLY IAW MM 33-51-04. 2 L 7 4 4F A20WE 2001110900066 20011109 00066 NM 2001 11 9 PCAA0110128 1 20011028 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 820EX 019 DURING ROUTINE MAINTENANCE VISIT SEVERAL FLOOR PATH EMERGENCY LIGHTS FOUND TO BE INOPERATIVE ON LEFT SIDE. NEW VISTA EM ERGENCY LIGHT JUMPER INSTALLED AT SEATS 4AC. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001110900067 20011109 00067 NM 2001 11 9 PCAA0110129 1 20011030 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN DAMAGED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 817EX 191 DURING ROUTINE MAINTENANCE VISIT FIRST FOUR RED LIGHTS ON EMERGENCY FLOOR LIGHTING FOUND TO BE INOPERATIVE. WIRING REPA IRED AT FIRST LAMP. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001110900068 20011109 00068 NM 2001 11 9 QXEA0101698 1 20011023 A 7921 28E997 OIL COOLER DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE NR 1 ENGINE CRACKED A QXEA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 09 357PH 6799 1348 504 PCE123077 PDX- DEPARTED SEA HEADING FOR MFR, LEVELING AT 21,000 FT THE MASTER WARNING LIGHT FLICKERED A FEW TIME THEN CAME ON STEA DY. THE NR 1 ENGINE OIL PRESSURE LIGHT WAS ILLUMINATED. STARTED THE OIL PRESSURE CHECKLIST. DURING CHECKLIST PROCESS, OIL PRESSURE DROPPED TO 20 PSI. SHUT DOWN NR 1 ENGINE. LANDED IN PDX WITHOUT INCIDENT. REPLACED THE NR 1 ENGINE AND OIL COOLER. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2001110900069 20011109 00069 EU 2001 11 9 QXEA0101699 1 20011026 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 491US 11156 BOI - EXIT SIGN AT PASSENGER COMPARTMENT LINTEL HAS NO EMERGENCY LIGHTS WORKING. REPLACED EXIT SIGN ASSEMBLY. OPERATIO NAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001110900070 20011109 00070 NM 2001 11 9 QXEA0101700 1 20011025 A 3350 6038443 BATTERY PACK DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 374PH 7902 108 528 SEA - OUTSIDE RIGHT EMERGENCY LIGHT, CABIN CENTER EXIT SIGN, AND AFT CABIN OVERHEAD EMERGENCY LIGHTS ARE INOPERABLE. RE PLACED BATTERY PACK. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001110900071 20011109 00071 EU 2001 11 9 QXEA0101701 1 20011028 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 499US 11182 PDX - EMERGENCY EXIT SIGN FACING AFT AT THE MIDDLE CABIN POSITION HAS BULB SEGMENTS THAT ARE INOPERATIVE. REMOVED AND R EPLACED THE EXIT SIGN ASSEMBLY. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001110900072 20011109 00072 EU 2001 11 9 QXEA0101702 1 20011028 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 499US 11182 PDX - EMERGENCY EXIT SIGN FACING FORWARD AT THE MIDDLE CABIN POSITION IS INOPERATIVE IN THE ARMED MODE. REPLACED THE EX IT SIGN. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001110900073 20011109 00073 NM 2001 11 9 QXEA0101704 1 20011029 A 5410 ANGLE DHAV DHC8 DHC8202 2809007 NM RT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX - RIGHT NACELLE HAS CRACKED CLOSING ANGLE ON THE OUTBOARD SIDE OF FIREWALL. REPAIRED RIGHT NACELLE IAW RD 8-54-806, RD 8-54-109, SRM 51-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001110900074 20011109 00074 EU 2001 11 9 QXEA0101705 1 20011029 A 4920 APU FOKKER F28 F28MK4000 4990810 EU APU BAY MALFUNCTIONED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 475AU 11222 PDX - AIRCRAFT FILLED WITH SMOKE WHILE SITTING AT THE GATE WITH NO PASSENGERS ABOARD. PERFORMED BLEED AIR SYSTEM BLOW O UT IAW MAINTENANCE TASK CARD 8361002. PLACED AUXILIARY POWER UNIT ON MEL 49-1, RSI 330723. 2 L 7 2 4F RT A20EU 2001110900075 20011109 00075 EU 2001 11 9 QXEA0101706 1 20011030 A 4920 38075412 APU FOKKER F28 F28MK4000 4990810 EU APU BAY MALFUNCTIONED A QXEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 09 475AU 19618 1310 11222 PDX - AFTER DEPARTURE, THE AIRCRAFT FILLED WITH SMOKE. TURNED BLEEDS OFF. SMOKE DID NOT SEEM TO GET WORSE. RETURNED TO FIELD. REMOVED AND REPLACED AUXILIARY POWER UNIT IAW MAINTENANCE TASK CARD 8491001. GROUND RAN AIRCRAFT. NO SMOKE NOT ED IN COCKPIT OR CABIN. 2 L 7 2 4F RT A20EU 2001110900076 20011109 00076 NM 2001 11 9 QXEA0101709 1 20011101 A 5753 FLAP DHAV DHC8 DHC8202 2809007 NM LT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - DAMAGE TO LEFT INBOARD FLAP ON OUTBOARD TRAILING EDGE. INSTALLED ONE RIVET AND COMPLETED REPAIR IAW EA 2-57-146 A ND RD 8-57-050. 2 H 7 2 4T RT A13NM 2001110900077 20011109 00077 EU 2001 11 9 QXEA0101710 1 20011101 A 5210 R5320 ACTUATOR FOKKER F28 F28MK4000 4990810 EU PAX DOOR FAILED A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 480AU * * 11229 GEG- MAIN CABIN DOOR WILL NOT OPEN OR CLOSE. ACTUATOR FAILED. REMOVED AND REPLACED MAIN CABIN DOOR ACTUATING MECHANISM . OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001110900078 20011109 00078 NM 2001 11 9 QXEA0101779 1 20011103 A 5410 STRUCTURE DHAV DHC8 DHC8102 2809003 NM RT NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 314 PDX - THERE IS A CHAFE IN THE RIGHT NACELLE ON THE OUTBOARD SIDE OF THE FIREWALL FLANGE APPROXIMATELY 3.5 INCHES DOWN FR OM PREVIOUS REPAIR. REPAIRED IAW RD8-54-081. 2 H 7 2 4T RT A13NM 2001110900079 20011109 00079 SO 2001 11 9 RAIA00110010 1 20011021 A 5315 FLOORBEAM EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 802HK 145066 MX-STL- DURING MAINTENANCE CHECK FOUND CORROSION ON LT OMEGA BEAM AT FLOORBOARD SUPPORT CENTER AISLE AT FRAME 20 Y AXIS -.459. MAINTENANCE REPAIRED LT OMEGA BEAM AT FLOORBOARD SUPPORT CENTER AISLE AT FRAME 20 Y AXIS-.459 IAW EMB I45 SRM. 2 L 7 2 4F RT T00011AT 2001110900080 20011109 00080 SO 2001 11 9 RAIA00110011 1 20011021 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 802HK 7916 145066 MX-STL-DURING MAINTENANCE CHECK FOUND CORROSION ON AFT GUSSET AT CENTER LINE FROM FRAME 17 TO 23 AT Y AXIS 0.0. MAINTEN ANCE REMOVED AND REPLACED AFT GUSSET AT CENTER LINE FROM FRAME 17 TO 23 AT Y AXIS 0.0 IAW EMB 145 SRM. 2 L 7 2 4F RT T00011AT 2001110900081 20011109 00081 SO 2001 11 9 RAIA00110013 1 20011021 A 5320 CHANNEL EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 802HK 145066 MX-STL-DURING MAINTENANCE CHECK FOUND CORROSION ON HAT SECTION BEAM AT FRAME 20 AT Y AXIS 0.0. MAINTENANCE REPAIRED HAT SECTION BEAM AT FRAME 20 AND Y AXIS 0.0 IAW EMB ENGINEERING ORDER GST3506/01. 2 L 7 2 4F RT T00011AT 2001110900082 20011109 00082 SO 2001 11 9 RAIA00110014 1 20011021 A 5315 FLOORBEAM EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 802HK 145066 MX-STL- DURING MAINTENANCE CHECK FOUND CORROSION ON FWD DIGITAL AT COCKPIT ENTRANCE AT FRAME 18 AND Y AXIS 0.0. MAINTEN ANCE REPAIRED DIGITAL AT FRAME 18 AND Y AXIS 0.0 IAW EMB ENGINEERING ORDER GST2322/01. 2 L 7 2 4F RT T00011AT 2001110900083 20011109 00083 EU 2001 11 9 SABA011059 1 20011108 A 3350 311701 BATTERY PACK BAG JETSTM JETSTM3201 1500217 EU CABIN DISCHARGED A SABA K NONE O OTHER TX TAXI/GRND HDL 1 SO 33 959AE 959 DURING PREFLIGHT OF AIRCRAFT 959 FOR FLIGHT 5048 PILOT CALLED IN FOR LOW VOLTAGE ON EMERGENCY LIGHT BATTERIES. MAINTENA NCE REMOVED AND REPLACED THE BATTERIES. SYSTEM OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A56EU 2001110900084 20011109 00084 NM 2001 11 9 SCNA01358 1 20011018 A 5315 FLOORBEAM BOEING 727 727282 138408T NM FUSELAGE CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 281SC 21949 DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS AT BS 420 0 BL FLOORBEAM TEE CAP. REMOVED CORROSI ON IAW B277 SRM 511006. CUT OUT DAMAGED SECTION IAW B727 SRM 531008. FABRICATED REPAIRS IAW B727 SRM 531008. INSTALLED IAW B727 SRM 513002. 2 L 7 3 4F RT A3WE 2001110900085 20011109 00085 NM 2001 11 9 SCNA01359 1 20011018 A 5315 FLOORBEAM BOEING 727 727282 138408T NM FUSELAGE CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 281SC 21949 DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS BS 400 LBL 20 TO RBL 44 FLOORBEAM TEE CAP. REMOVE D CORROSION IAW B727 SRM 511006. REMOVED DAMAGED AREA IAW B727 SRM 531008. REMOVED FLOOR SUPPORT AND INTERCOSTAL IAW B 727 SRM 513002. FABRICATED FLOORBEAM REPAIRS IAW B727 SRM 531008. INSTALLED IAW B727 SRM 513002 AND 531008. 2 L 7 3 4F RT A3WE 2001110900086 20011109 00086 NM 2001 11 9 SCNA01360 1 20011018 A 5315 FLOORBEAM BOEING 727 727282 138408T NM FUSELAGE CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 281SC 21949 DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON FLOORBEAM TEE CAP AT BS 380 LBL 20 TO RBL 64. R EMOVED CORROSION IAW B727 SRM 511006. REMOVED DAMAGED SECTION IAW B727 SRM 513002. FABRICATED REPAIRS AND INSTALLED I AW B727 SRM 513002. 2 L 7 3 4F RT A3WE 2001110900088 20011109 00088 NM 2001 11 9 SCNA01362 1 20011018 A 5347 SEAT TRACK BOEING 727 727282 138408T NM FUSELAGE CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 281SC 21949 DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON SEAT TRACK AT BS 344 TO 420 RBL 44. REMOVED CO RROSION IAW B727 SRM 511006. REMOVED DAMAGED SECTION IAW B727 SRM 513002. FABRICATED NEW SEAT TRACK PER SAMPLE INSTALL ED IAW B727 SRM 513002. 2 L 7 3 4F RT A3WE 2001110900089 20011109 00089 NM 2001 11 9 SCNA01363 1 20011102 A 3350 900542 CHARGER BOEING 727 727282 138408T NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 281SC 21949 DURING HEAVY MAINTENANCE INSPECTION THE FORWARD OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND INOP. REPLACED CHARGER IAW B727 MM 335081. OPS CHECK NORMAL IAW B727 MM 335001. 2 L 7 3 4F RT A3WE 2001110900090 20011109 00090 NM 2001 11 9 SCNA01724 1 20011031 A 3350 LIGHT BOEING 727 7272J4 1384006 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 285SC 21676 FWD CABIN EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT. 2 L 7 3 4F RT A3WE 2001110900091 20011109 00091 NM 2001 11 9 SWAA012948 1 20011027 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 384SW 26590 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP BETWEEN ROWS 11-17. REPAIRED EEPLS WIRING PER MM. 2 L 7 2 4F RT A16WE 2001110900092 20011109 00092 NM 2001 11 9 SWAA012950 1 20011029 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 394SW 27380 EEPLS INOP BETWEEN ROWS 13-22. REPAIRED EEPLS WIRING AND RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2001110900093 20011109 00093 NM 2001 11 9 SWAA012951 1 20011028 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT LIGHT ABOVE AFT ENTRY DOOR LOOSE AT FWD END. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 2001110900094 20011109 00094 NM 2001 11 9 SWAA012952 1 20011029 A 5311 963820 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 382SW 26588 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD LT SIDE CHORD CRACKED AT WL 207. REMOVED AND REPLACED LT SIDE CHORD PER SWA ACO. 2 L 7 2 4F RT A16WE 2001110900095 20011109 00095 NM 2001 11 9 SWAA012954 1 20011029 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 382SW 26588 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO BIN FLOORBEAM CORRODED, BS 771 BETWEEN LBL 8-LBL 13. REPAIRED BEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2001110900096 20011109 00096 NM 2001 11 9 SWAA012956 1 20011028 A 5320 6517583 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 383SW 26589 DURING SCHEDULED 1/4D CHECK, FOUND 3 CRACKS AT BS 178 BULKHEAD VERTICAL BEAM, RBL 17.1, BETWEEN WL 225-230. REPAIRED BE AM PER SRM. 2 L 7 2 4F RT A16WE 2001110900097 20011109 00097 NM 2001 11 9 SWAA012957 1 20011028 A 3350 65C34691 LIGHT BOEING 737 7373Q8 1384670 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2001110900098 20011109 00098 NM 2001 11 9 SWAA012958 1 20011028 A 5320 6517583 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 382SW 26588 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 VERTICAL STIFFENER CRACKED, RBL 5.7, WL 184. REPAIRED STIFFENER PER SWA RA. 2 L 7 2 4F RT A16WE 2001110900099 20011109 00099 NM 2001 11 9 SWAA012959 1 20011022 A 2730 251A2317 CONTROL UNIT BOEING 737 7377H4 1384404 NM ELEVATOR INOPERATIVE A SWAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 SW 07 798SW 28436 DURING DESCENT, STAB TRIM LIGHT ILLUMINATED, DISCONNECTED AUTOPILOT SYS, AND CONTROL COLUMN FORE/AFT OPERATION WAS UNAVA ILABLE FROM APPROX 15,000 FEET TO 4,000 FEET. C/W AUTOPILOT BITE CK. REMOVED AND REPLACED STAB TRIM RELAY AND ACTUATOR . ALL OPS CK GOOD. MX FERRY TO DAL, WHERE ENTIRE ELEV CONTROL SYS WAS INSP AND NO DISCREPANCIES NOTED. C/W DFCS BITE CK. ALL OPS CK GOOD. REMOVED AND REPLACED FDR FOR MX CONVENIENCE. LATER MX FERRY FROM JAX BACK TO DAL PER MX CONTROL REQUEST FOR BOEING EVALUATION. REMOVED AND REPLACED ELEVATOR FEEL / CENTERING UNIT, AND LOWER ELEVATOR TORQUE TUBE PER BOEING REQUEST AND EVALUATION OF THESE COMPONENTS. ALL MX C/W AND OPS CK GOOD PER MM. 2 L 7 2 4F RT A16WE 2001110900100 20011109 00100 NM 2001 11 9 SWAA012961 1 20011026 A 5330 6545877 BEAR STRAP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 324SW 23414 DURING SCHEDULED 1/2D CHECK, FOUND 2 CRACKS AT FWD SERVICE DOOR LOWER HINGE CUTOUT BEAR STRAP. REPAIRED STRAP ASSY PER SWA RA. 2 L 7 2 4F RT A16WE 2001110900101 20011109 00101 NM 2001 11 9 SWAA012964 1 20011029 A 5311 6546546 BELTFRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED 1/4D CHECK, FOUND BELT FRAME CORRODED AT BS 787, BL 0. REPAIRED BELT FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001110900102 20011109 00102 NM 2001 11 9 SWAA012972 1 20011030 A 3350 8100022607 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 388SW 26591 DURING SERVICE CHECK, FOUND SEVERAL EEPLS LIGHTS INOP. REMOVED AND REPLACED EEPLS LIGHT ASSY'S PER MM. 2 L 7 2 4F RT A16WE 2001110900103 20011109 00103 2001 11 9 SWAA012974 4 20011029 A 2565 61620468 SLIDE BOEING 737 7373A4 1384585 NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001110900104 20011109 00104 2001 11 9 SWAA012975 4 20011029 A 2565 61621469 SLIDE BOEING 737 7373A4 1384585 NM AFT ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001110900105 20011109 00105 NM 2001 11 9 SWAA012977 1 20011031 A 3397 81000 WIRE BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 391SW 27378 EEPLS WIRE BROKEN AT ROW 13. REMOVED AND REPLACED TRACK COVER AND REPAIRED WIRE PER MM. 2 L 7 2 4F RT A16WE 2001110900106 20011109 00106 2001 11 9 SWAA012979 4 20011028 A 2565 61620468 SLIDE BOEING 737 737317 138447P NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001110900107 20011109 00107 NM 2001 11 9 SWAA012981 1 20011030 A 3350 AD20131A BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2001110900108 20011109 00108 NM 2001 11 9 SWAA012982 1 20011031 A 3350 100885 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED A1 CHECK, FOUND EEPLS BATTERY INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2001110900109 20011109 00109 NM 2001 11 9 SWAA012988 1 20011031 A 3350 101042 LENS BOEING 737 7373H4 1384600 NM CABIN OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 324SW 23414 DURING SCHEDULED 1/2D CHECK, FOUND BULLNOSE MOUNTED EMERGENCY LIGHT LENS AT 7C OUT OF ADJUST. ADJUSTED LENS PER MM. 2 L 7 2 4F RT A16WE 2001110900110 20011109 00110 NM 2001 11 9 SWAA012992 1 20011030 A 5312 6546568 BULKHEAD BOEING 737 7377H4 1384404 NM FUSELAGE CANNING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 728SW 27860 DURING SCHEDULED A2 CHECK (SI 11157-53), FOUND OIL CANNING AT AFT PRESS BULKHEAD WEB, BS 1016, STR 3L. REPAIRED WEB PER SWA RA. 2 L 7 2 4F RT A16WE 2001110900111 20011109 00111 NM 2001 11 9 SWAA012996 1 20011101 A 5311 963820 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 398SW 27692 DURING SCHEDULED SPECIAL VISIT, FOUND BOTH BS 178 BULKHEAD SIDE CHORDS CRACKED. REMOVED AND REPLACED BOTH SIDE CHORDS P ER SWA ACO. 2 L 7 2 4F RT A16WE 2001111100001 20011111 00001 EU 2001 11 11 RAIA00111001 1 20011105 A 2912 ER18326 FILTER AEROSP ATR42 ATR42300 8680920 EU LEAKING A RAIA O OTHER K FLUID LOSS DE DESCENT 1 CE 03 426TE 228 7176-STL- GREEN HYDRAULIC SYSTEM LOW PRESSURE ON DECENT. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LEAKING ACOUSTIC FILTER OPS AND LEAK CHECKED GOOD IAW ATR MAINTENANCE MANUAL 2 H 7 2 4T RT A53EU 2001111100002 20011111 00002 EU 2001 11 11 RAIA00111004 1 20011106 A 3350 WIRE JETAIR JETSTM JETSTM4101 1500501 EU DISCONNECTED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 561HK 41077 7003-STL- DURING PRE-FLIGHT INSPECTION, FOUND PATH LIGHTS INOP AT SEAT 7. MAINTENANCE REPAIRED WIRE TO ESCAPE PATH LIGHT S AND OPS CK GOOD IAW J41 MAINTENANCE MANUAL. 2 L 7 2 4T RT A41NM 2001111100003 20011111 00003 EU 2001 11 11 RAIA00111005 1 20011107 A 2913 4019501 PUMP AEROSP ATR42 ATR42300 8680920 EU DEFECTIVE A RAIA O OTHER J WARNING INDICATION DE DESCENT 1 CE 03 426TE 8204 7754 228 7493-SBN- GREEN HYDRAULIC SYSTEM LOW PRESSURE ON DECENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED GREEN SYSTEM HYDRAU LIC PUMP IAW ATR MAINTENANCE MANUAL. 2 H 7 2 4T RT A53EU 2001111100004 20011111 00004 EU 2001 11 11 RAIA00111006 1 20011103 A 3350 6047051 POWER SUPPLY JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 571HK 13626 241 41090 7003-STL-DURING PRE-FLIGHT INSPECTION FOUND EMERGENCY LIGHTS OUT AT SEAT 9A. MAINTENANCE REMOVED AND REPLACED THE #3 EME RGENCY LIGHT POWER SUPPLY. 2 L 7 2 4T RT A41NM 2001111200001 20011112 00001 NM 2001 11 12 CALA0100997 1 20011109 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 674 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71314 23365 INSPECTION FOUND A 3.5" CRACK IN KEEL BEAM SKIN AT STA 674, RBL 5. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS I NSTALLED IAW SRM 53-60-12, FIGURE 202. 2 L 7 2 4F RT A16WE 2001111200002 20011112 00002 NM 2001 11 12 CALA0100998 1 20011109 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 699 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71314 23365 INSPECTION FOUND A 1.3" CRACK IN KEEL BEAM SKIN AT STA 699, RBL 5 AND A 1/2" CRACK WAS FOUND IN KEEL BEAM SKIN AT STA 69 9, LBL 5. A DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 53-60-12. 2 L 7 2 4F RT A16WE 2001111500082 20011115 00082 WP 2001 11 15 ARWA0011014 1 20011109 A 2913 57155A PUMP DOUG DC8 DC862 3021970 WP HYDRAULIC SYS LEAKING A ARWA O OTHER K FLUID LOSS CR CRUISE 1 SO 19 802BN 45909 IN CRUISE, HYDRAULIC QUANTITY DROPPED SLIGHTLY ABOVE EMERGENCY LEVEL. PERFORMED LOSS OF HYDRAULIC PRESSURE ABNORMAL EME RGENCY CHECKLIST. FLIGHT RESTRICTED TO MACH .65 AND 230 KIAS. CONTINUED WITHOUT INCIDENT. AFTER LANDING, MX FOUND AUX RUDDER PUMP LEAKING. REMOVED, REPLACED AND LEAKED CHECK PUMP, SERVICED FLUID, AND RETURNED AIRCRAFT TO SERVICE. 2 L 7 4 4F 4A25 2001111200003 20011112 00003 NM 2001 11 12 ZW0A0110902 1 20011109 A 3350 8100022602 LAMP BOEING 767 767300 1385204 NM A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 691LF 25137 THE EGRESS LIGHT WAS INOPERATIVE FORWARD OF SEAT ROW 1 ON LH SIDE OF CABIN. REPLACED THE LAMP. CHECK-C 9-23-00 LAX. -- CLOSED-- 2 L 7 2 4F RT A1NM 2001111200004 20011112 00004 2001 11 12 SABA011062 4 20011110 A 6122 89741016 GOVERNOR BAG JETSTM JETSTM3201 1500217 EU UNCONTROLLABLE A SABA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 33 961AE 961 Aircraft 961 on flight 5152 from Charlotte to Lewisburg. After take-off pilot reported the number two engine prop govern or will not hold set RPM and makes erratic & rapid changes between 99 to 101.5%. Aircraft returned to Charlotte and land ed with no other problems. No in-flight emergency was declared. Maintenance removed and replaced the number two Prop Gov ernor. A test flight was flown and ops checked good Aircraft was returned to service. 2 L 7 2 4T RT A56EU 2001111300001 20011113 00001 2001 11 13 C2XA01TY176 4 20011111 A 3445 DMNI5042 ANTENNA EMB 135 EMB135ER 3260203 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15509 145238 TYS During a scheduled inspection the lower TCAS antenna was found corroded. Maintenance removed and replaced the TCAS antenna I.A.W.-EMB-135-AMM-34-43-03, operational checks were satisfactory. Aircraft released for service. 2 L 7 2 4F RT T00011AT 2001111300002 20011113 00002 NM 2001 11 13 AWXA200100567 1 20011102 A 5210 FE240004 CYLINDER AIRBUS A319 A319132 3930340 NM R1 DOOR FAILED A AWXA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 28 814AW 4800 1281 MAF - EMERGENCY EVACUATION - FLT 786 -O- REFERENCE SDR AWXA200100565, DURING EMERGENCY EVACUATION THE R-1 DOOR DAMPER CY LINDER (POWER ASSIST) FAILED TO FULLY OPEN THE R-1 DOOR AND THE ESCAPE SLIDE FAILED TO DEPLOY. THE L-1 & L-2 DOORS WERE USED FOR EVACUATION AND FUNCTIONED NORMALLY. LATER THE CAPTAIN MOVED THE R-1 DOOR FULLY OPEN BY HAND AND THE ESCAPED S LIDE DEPLOYED AND INFLATED NORMALLY. THE R-1 DOOR DAMPER CYLINDER WAS REMOVED AND TURNED OVER TO THE NTSB ON SITE AT MA F. SERVICEABLE SLIDES AND DOOR DAMPER CYLINDER ASSEMBLIES WERE INSTALLED ON THE L-1, L-2 & R-1 POSITIONS. 2 L 7 2 4F RT A28NM 2001111300003 20011113 00003 NM 2001 11 13 SCNA01356 1 20011017 A 5311 FRAME BOEING 727 727225 1384077 NM FUSELAGE CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE INSPECTION THE WALKWAY WEB SUPPORT ANGLE WAS FOUND CORRODED OUT OF LIMITS AT BS 335 RBL 14. RE MOVED CORROSION IAW B727 SRM 511006. SHORED AIRCRAFT IAW B727 SRM 515001. REMOVED WEB IAW B727 SRM 513002. REMOVED ST IFFENERS IAW B727 SRM 513002. REMOVED CHORD IAW B727 SRM 513002. TRANSFERRED HOLES TO NEW CHORD IAW B727 SRM 511001. INSTALLED IAW B727 SRM 513002. 2 L 7 3 4F A3WE 2001111300004 20011113 00004 2001 11 13 SWAA012999 4 20011101 A 2565 61620468 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 379SW 26586 FWD ENTRY DOOR EVACUATION SLIDE DEPLOYED INADVERTENTLY. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001111300005 20011113 00005 NM 2001 11 13 SWAA013002 1 20011101 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 749SW 29801 DURING SCHEDULED CHECK, FOUND EEPLS COVER MISSING AT ROW 2 & EEPLS INOP AT ROW 1. RELAMPED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001111300006 20011113 00006 NM 2001 11 13 SWAA013003 1 20011104 A 5320 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001111300007 20011113 00007 NM 2001 11 13 SWAA013043 1 20011108 A 5310 6546529 TIE CLIP BOEING 737 7373H4 1384600 NM FWD CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED 1/4D CHECK, FOUND TIE CLIP CRACKED AT BS 420, STR 14R. R&R TIE CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001111300008 20011113 00008 NM 2001 11 13 SWAA013044 1 20011108 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR UPPER AFT CUT OUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001111300009 20011113 00009 NM 2001 11 13 SWAA013046 1 20011105 A 5310 6546543 FRAME BOEING 737 7373H4 1384600 NM AFT CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 3L. REPAIRED FRAME PER SRM . 2 L 7 2 4F RT A16WE 2001111300010 20011113 00010 NM 2001 11 13 SWAA013047 1 20011108 A 5310 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FWD CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED 1/4D CHECK, FOUND FRAME SHEAR TIE CRACKED AT BS 360, ABOVE STR 14L. REPAIRED SHEAR T IE PER SRM. 2 L 7 2 4F RT A16WE 2001111300011 20011113 00011 2001 11 13 SWAA013004 4 20011102 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 663SW 23256 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001111300012 20011113 00012 NM 2001 11 13 SWAA013006 1 20011104 A 5320 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (6 EA) AT BS 500D, STR 7R, 8R, 2R, 8L, 6L & 5L. REMOVED AND REPL ACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001111300013 20011113 00013 NM 2001 11 13 SWAA013052 1 20011109 A 3350 101114 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 758SW 27873 AFT ENTRY EMERGENCY EXIT LIGHT LENS MISSING. R&R LENS PER MM. 2 L 7 2 4F RT A16WE 2001111300014 20011113 00014 NM 2001 11 13 SWAA013055 1 20011111 A 5310 BAC1490 STIFFENER BOEING 737 737317 138447P NM FWD CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED D CHECK, FOUND CRACKED STIFFENER AT BS 328, RBL 32 & WL 201. REPAIRED STIFFENER P ER SRM. 2 L 7 2 4F RT A16WE 2001111300015 20011113 00015 NM 2001 11 13 SWAA013056 1 20011109 A 5330 589357 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 380SW 26587 DURING SCHEDULED 1/4D CHECK, FOUND BOTH R-1 & L-1 COCKPIT WINDOW FRAMES CRACKED AT UPPER OTBD CORNER. REPAIRED WINDOW FRAMES PER SRM. 2 L 7 2 4F RT A16WE 2001111300016 20011113 00016 NM 2001 11 13 SWAA013058 1 20011108 A 5753 6546435277 FLAP BOEING 737 7373H4 1384600 NM LH WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED BC1 CHECK, FOUND LH OTBD AFT FLAP DELAMINATED ON INBD END. R&R FLAP PER MM. 2 L 7 2 4F RT A16WE 2001111300017 20011113 00017 NM 2001 11 13 SWAA013059 1 20011111 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 912, STR 21L. REPAIRED SKIN PER S RM. 2 L 7 2 4F RT A16WE 2001111300018 20011113 00018 NM 2001 11 13 SWAA013060 1 20011108 A 5240 6545871 DOOR FRAME BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR FRAME CRACKED AT # 5 STOP PIN. REPAIRED DOO R FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001111300019 20011113 00019 NM 2001 11 13 SWAA013061 1 20011109 A 5313 6551698 STRINGER BOEING 737 7373H4 1384600 NM FWD CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER WEBS CRACKED ( 2 EA ) AT BS 294.5, STR'S 7L & 8L. R&R WEBS PER SRM. 2 L 7 2 4F RT A16WE 2001111300020 20011113 00020 2001 11 13 VNAA0110021 4 20011029 A 3100 870004MODB PSEU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 459PS 11888 3070 25 MINUTES AFTER DEPARTING PIT, THE CREW RECEIVED A PROXI SYSTEM FAIL INDICATION. THE CREW CONTACTED MAINTENANCE CONTRO L AND WERE ADVISED TO RETURN TO PIT. MAINTENANCE INSPECTED AND REPLACED THE PSEU UNIT IN ACCORDANCE WITH DORNIER MAINTE NANCE MANUAL 31-00-00.OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001111300021 20011113 00021 NM 2001 11 13 SWAA013008 1 20011103 A 5320 BAC1505 STIFFENER BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL CHORD CRACKED .25 INCH LONG AT BS 178, WL 184 & LBL 5.8. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2001111300022 20011113 00022 NM 2001 11 13 SWAA013009 1 20011103 A 2910 1062030192 HYDRAULIC LINE BOEING 737 7373Q8 1384670 NM LT MLG DAMAGED A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 672SW 23406 (AIR TURNBACK) A-SYSTEM HYDRAULIC FAILURE AFTER TAKEOFF AND GEAR RETRACTION. FOUND HOLE IN LT MLG RETRACT LINE. REMOVE D AND REPLACED LINE, OPS AND LEAK CHECK GOOD PER MM. 2 L 7 2 4F RT A16WE 2001111300023 20011113 00023 NM 2001 11 13 SWAA013010 1 20011104 A 3350 BR2013 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 073SW 22673 DURING SCHEDULED C1 CHECK, FOUND EEPLS INOP AT THREE PLACES IN CABIN. RELAMPED EEPLS PER MM. 2 L 7 2 4F A16WE 2001111300024 20011113 00024 2001 11 13 SWAA013011 4 20011102 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 385SW 26600 AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001111300025 20011113 00025 NM 2001 11 13 SWAA013015 1 20011104 A 5315 BAC1490 FLOORBEAM BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 328, WL 208 & RBL 20 TO RBL 49. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2001111300026 20011113 00026 NM 2001 11 13 SWAA013017 1 20011105 A 2910 65C268411185 HYDRAULIC LINE BOEING 737 7373H4 1384600 NM RT MLG WW CRACKED A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 326SW 23690 (AIR TURNBACK) A-SYSTEM HYDRAULIC FAILURE, PRESSURE TO ZERO, LOW PRESS LIGHT AND FEEL DIFFERENTIAL PRESSURE LIGHT ILLUMI NATED. FOUND A-SYSTEM HYD PRESSURE SPOILER LINE CRACKED. REMOVED AND REPLACED LINE PER MM. 2 L 7 2 4F RT A16WE 2001111300027 20011113 00027 NM 2001 11 13 SWAA013018 1 20011102 A 5753 6546481106 CARRIAGE BOEING 737 7373H4 1384600 NM T/E FLAP BROKEN A SWAA K NONE F FLT CONT AFFECTED AP APPROACH 1 SW 07 366SW 26577 WITH FLAPS EXTENDED 4 TO 5 DEGREES, ACFT ROLLS TO THE LEFT. FOUND RT OUTBOARD MID FLAP, INBOARD CARRIAGE BROKEN. REMOV ED AND REPLACED CARRIAGE ASSY PER MM. MX FERRY TO DAL. REMOVED AND REPLACED RT OUTBOARD MID FLAP ASSY, REMOVED AND REP LACED RT OUTBOARD EXHAUST GATE DUE TO WORN ATTACH POINT BEARING, AND REMOVED AND REPLACED ALTERNATE FLAP DRIVE MOTOR PER MM. 2 L 7 2 4F RT A16WE 2001111300028 20011113 00028 NM 2001 11 13 SWAA013021 1 20011105 A 3350 57771 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED C3 CHECK, FOUND EEPLS END CAP MISSING. INSTALLED END CAP PER MM. 2 L 7 2 4F A16WE 2001111300029 20011113 00029 NM 2001 11 13 SWAA013022 1 20011106 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIPS CRACKED (2 EA) AT BS 663 & BS 706, STR 10L. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001111300030 20011113 00030 NM 2001 11 13 SWAA013023 1 20011106 A 5312 6517582 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 361SW 26572 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL WEB CRACKED AT BS 178, RBL 23. REMOVED AND REPLACED VERTICAL WEB PER SRM . 2 L 7 2 4F RT A16WE 2001111300031 20011113 00031 NM 2001 11 13 SWAA013024 1 20011106 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 361SW 26572 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 7 & WL 213. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001111300032 20011113 00032 NM 2001 11 13 SWAA013026 1 20011106 A 5311 963820 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 682SW 23496 DURING SCHEDULED SPECIAL VISIT, FOUND LT & RT SIDE CHORDS CRACKED AT BS 178, WL 207. REPAIRED CHORDS PER SWA ACO 7342-5 3. 2 L 7 2 4F RT A16WE 2001111300033 20011113 00033 NM 2001 11 13 SWAA013028 1 20011106 A 3350 65C27093 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 627SW 27935 FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001111300034 20011113 00034 NM 2001 11 13 SWAA013029 1 20011106 A 2530 W25800214 WIRE BOEING 737 7372H4 138448C NM AFT GALLEY ARCED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 068SW 22357 (DIVERSION) AFT COFFEEMAKER BEGAN TO SMOKE IN FLT. CIRCUIT BREAKERS PULLED, CHECKLIST COMPLIED WITH, UNEVENTFUL LANDING . FOUND COFFEEMAKER CONNECTOR WIRES ARCHED. REPAIRED WIRES PER MM. 2 L 7 2 4F A16WE 2001111300035 20011113 00035 NM 2001 11 13 SWAA013030 1 20011106 A 3397 BR2013 WIRE BOEING 737 7377H4 1384404 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 703SW 27837 EEPLS WIRES EXPOSED IN CABIN. SECURED EEPLS WIRES PER MM. 2 L 7 2 4F RT A16WE 2001111300036 20011113 00036 NM 2001 11 13 SWAA013032 1 20011105 A 5312 6546568 BULKHEAD BOEING 737 7377H4 1384404 NM FUSELAGE CANNING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 732SW 27864 DURING SCHEDULED SERVICE CHECK, SI 1157-53 FOUND AFT PRESS BULKHEAD OIL CANNED, BETWEEN STR 2R & 3R. REPAIRED BULKHEAD PER SWA RA 1-753-2705. 2 L 7 2 4F RT A16WE 2001111300037 20011113 00037 NM 2001 11 13 SWAA013034 1 20011103 A 5320 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (3 EA) AT BS 727A, STR 3R, BS 600, STR 8R & BS 560, STR 10R. REM OVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001111300038 20011113 00038 NM 2001 11 13 SWAA013039 1 20011107 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM COCKPIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 063SW 22061 DURING SCHEDULED SERVICE CHECK, FOUND COCKPIT EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 2001111300039 20011113 00039 NE 2001 11 13 SWAA013040 2 20011106 A 7200 CFM563 ENGINE BOEING 737 7373H4 1384600 NM GE CFM56 CFM56* 13802 NE NR 1 OVERTEMP A SWAA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 07 613SW 27931 721146 (AIR TURNBACK) DURING CLIMB NR 1 ENG HAD 2 HIGH EGT INDICATIONS, (1100 DEGS & 950 DEGS), FOLLOWED BY ANOTHER HIGH EGT DU RING APPROACH (950 DEG). REMOVED AND REPLACED NR 1 ENG PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2001111300040 20011113 00040 SO 2001 11 13 SWIA200110283 1 20011004 A 2720 CONTROL CABLE EMB 120 EMB120ER 3260203 SO RUDDER WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 218SW 120287 LEFT AND RIGHT OUTBOARD AND INBOARD RUDDER CABLES IN TAIL WORN AT PRESSURE SEAL. REPLACED RUDDER CABLES IAW EMB120 MM 2 7-00-01. 2 L 7 2 4T RT A31SO 2001111300041 20011113 00041 SO 2001 11 13 SWIA200110284 1 20011004 A 2730 CONTROL CABLE EMB 120 EMB120ER 3260203 SO ELEVATOR WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 218SW 120287 LEFT AND RIGHT INBOARD AND OUTBOARD ELEVATOR CABLES WORN IN TAIL AREA. REPLACED AFT ELEVATOR CABLES IAW EMB120 MM 27-00 -01. 2 L 7 2 4T RT A31SO 2001111300042 20011113 00042 SO 2001 11 13 SWIA200110285 1 20011004 A 2711 CONTROL CABLE EMB 120 EMB120ER 3260203 SO AILERON TAB WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 218SW 120287 AILERON TRIM CABLES WORN. REPLACED ALL AILERON TRIM CABLES IAW EMB120 MM 27-00-01. 2 L 7 2 4T RT A31SO 2001111300043 20011113 00043 SO 2001 11 13 SWIA200110286 1 20011004 A 2710 CONTROL CABLE EMB 120 EMB120ER 3260203 SO AILERON WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 218SW 120287 RIGHT AND LEFT AILERON CONTROL CABLES (UPPER AND LOWER) WORN AT WING. REPLACED AILERON CONTROL CABLES IAW EMB120 MM 27- 00-01. 2 L 7 2 4T RT A31SO 2001111300044 20011113 00044 SO 2001 11 13 SWIA200110287 1 20011004 A 2720 CONTROL CABLE EMB 120 EMB120ER 3260203 SO RUDDER WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 218SW 120287 RIGHT INBOARD AND OUTBOARD RUDDER CONTROL CABLES WORN FORWARD OF WING BOX AT CABIN AREA. REPLACED RIGHT INBOARD AND OUT BOARD RUDDER CONTROL CABLES IAW EMB120 MM 27-00-01. 2 L 7 2 4T RT A31SO 2001111300045 20011113 00045 NM 2001 11 13 ZW0A0110501 1 20011103 A 3397 58541 CABLE BOEING 757 7572Q8 1384972 NM CABIN BROKEN A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 701TW 28160 THE EGRESS LIGHTS AT THE REAR LAVATORY WOULD NOT TEST. REPLACED THE FLEX CABLE. 2 L 7 2 4F RT A2NM 2001111300046 20011113 00046 WP 2001 11 13 ZW0A0110502 1 20011031 A 5320 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9618A 53565 DURING CHECK-C MAINT FOUND CRACKED INTERCOSTAL AT CANT LINE 1510, 2 O'CLOCK POSITION, AFTER BODY. REMOVED CRACKED INTER COSTAL AT CANT LINE 1510, 2 O'CLOCK POSITION AND INSTALLED NEW INTERCOSTAL PER TWA SPM 6-70-01, AND DRAWING 9911875, SRM 51-30-01, SRM 51-30-02, AND SRM 51-30-5. 2 L 7 2 4F RT A6WE 2001111300047 20011113 00047 WP 2001 11 13 ZW0A0110503 1 20011031 A 5320 SUPPORT BRACKET DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9619V 53566 DURING CHECK-C MAINT, THE LT WHEEL WELL, AFT FRAME FOR GEAR DOOR INBOARD SUPPORT BRACKET HAD CRACKED. REPLACED SUPPORT ANGLE PER DOUGLAS DRAWING 5936395. 2 L 7 2 4F RT A6WE 2001111300048 20011113 00048 NM 2001 11 13 ZW0A0110504 1 20011031 A 5330 SKIN BOEING 767 7673Y0 NM FUSELAGE GOUGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 640TW 25411 DURING CHECK-C MAINT FOUND DEEP GOUGE IN FUSELAGE SKIN CAUSED BY EMBEDDED BOLT IN ACCESS PANEL 313CRX, STA 1809.5, ABOVE STRINGER 22. INSTALLED METAL DOUBLERS AND FILLER PER SRM 53-80-01. 2 L 7 2 4F RT A1NM 2001111300049 20011113 00049 WP 2001 11 13 ZW0A0110601 1 20011104 A 5240 ANGLE DOUG DC9 DC982 3022082 WP SERVICE DOOR CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 927TW 49358 DURING CHECK-C MAINT THE FWD RT SERVICE DOOR LOWER HINGE ARM SUPPORT BEAM WAS CRACKED IN ANGLE RADIUS. REPLACED ANGLE P ER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-05 AND 51-30-02. 2 L 7 2 4F A6WE 2001111300050 20011113 00050 WP 2001 11 13 ZW0A0110602 1 20011101 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 913TW 49184 DURING CHECK-C MAINT THE FUSELAGE SKIN ALONG THE AFT SIDE OF THE FWD CARGO DOOR ENTRY WAY, STA 427, WAS BENT AND DAMAGED . BLENDED DAMAGED AREA PER SRM 51-02-E. ACCOMPLISHED NDT AND NO CRACKS FOUND PER PART 6-51-00-03. DOUBLER INSTALLED P ER SRM 53-05, FIG 82. 2 L 7 2 4F A6WE 2001111300051 20011113 00051 WP 2001 11 13 ZW0A0110603 1 20011102 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 913TW 49184 DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND CORROSION ON LONGERON 22L, STA 1290. REPLACED CORRODED SECTION OF LON GERON. SPLICED IN NEW SECTION PER SRM 53-02, FIG 18. 2 L 7 2 4F A6WE 2001111300052 20011113 00052 WP 2001 11 13 ZW0A0110604 1 20011105 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 913TW 49184 DURING CHECK-C MAINT FOUND CORROSION ON FORMER FROM STA 1309 LONGERON TO LONGERON 29L. PREVIOUS FORMER SPLICE REMOVED. TREATED PER SPM 6-50-1 AND SRM 51-10-3. REINSTALLED SPLICE SECTION PER SRM 53-03, FIG 2A. 2 L 7 2 4F A6WE 2001111300053 20011113 00053 NM 2001 11 13 2001F00636 1 20011010 A 3350 6104789 BATTERY PACK BOEING 737 7372B7 1384560 NM CARGO BAY DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 277AU 22889 BWI - MAINTENANCE FOUND THE FORWARD ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED T HE BATTERY PACK (P/N 61-0478-9) AND POWER SUPPLY (P/N 6013211). OPERATIONAL CHECK GOOD. REF USAASB01293. (M) 2 L 7 2 4F A16WE 2001111300054 20011113 00054 NM 2001 11 13 AALA20011149A 1 20010522 A 5711 SPAR BOEING 727 727227 1384078 NM RT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 728AA 20735 TUL - FOUND RIGHT WING FORWARD SPAR CORRODED AT LOWER CHORD 8 INCHES INBOARD OF DEFUEL VALVE BELOW NR 4 L/E FLAP ACT MOU NT. CUT OUT DAMAGED MATERIAL AND INSTALLED DOUBLER PER ESO 11697. (M) 2 L 7 3 4F A3WE 2001111300055 20011113 00055 WP 2001 11 13 AALA20011912 1 20010924 A 5345 FITTING DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 439AA 49457 TUL - - FOUND STATION 215 G2 FORWARD TIE DOWN CORRODED. REPLACED CORRODED TIE DOWN BRACKET WITH NEW BRACKET AND HARDWAR E SRM 51-01. (M) 2 L 7 2 4F RT A6WE 2001111300056 20011113 00056 WP 2001 11 13 AALA20011913 1 20011009 A 5311 BELTFRAME DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 439AA 49457 TUL - FOUND BELTFRAME DENTED BETWEEN L26L AND L27L STATION 1250. INSTALLED DOUBLER PER AARD 53-10-00-17. (M) 2 L 7 2 4F RT A6WE 2001111300057 20011113 00057 WP 2001 11 13 AALA20011914 1 20011001 A 5230 BEAM DOUG DC9 DC983 3022083 WP CARGO DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 439AA 49457 TUL - FOUND CORROSION ON VERTICAL AND HORIZONTAL LEGS OF DOOR BEAM FROM STATION 1155-1212, SEVERAL AREAS. INSTALLED DOU BLER AND FASTENERS, TREATED AND PRIMED AREAS PER ESO 80559 DATED 9/28/01. (M) 2 L 7 2 4F RT A6WE 2001111300058 20011113 00058 WP 2001 11 13 ABXA010574 1 20011022 A 5300 591140615 LONGERON DOUG DC9 DC915 3022036 WP FS 160 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 LONGERON 3 LEFT WAS CRACKED AT F.S. 160. REPLACED CRACKED LONGERON IAW DC-9 SRM 53-02. 2 L 7 2 4F A6WE 2001111300059 20011113 00059 WP 2001 11 13 ABXA010575 1 20011023 A 5500 9918420505 RIB DOUG DC9 DC915 3022036 WP XFS 95 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 LEFT HORIZONTAL STABILIZER LEADING EDGE RIB WAS CRACKED AT XFS 95. REPAIRED RIB IAW DC-9 SSRM K0-5159. PROTECTED AREA AG AINST CORROSION IAW DC-9 SRM 51-10-3. 2 L 7 2 4F A6WE 2001111300060 20011113 00060 WP 2001 11 13 ABXA010576 1 20011023 A 5500 99184201 RIB DOUG DC9 DC915 3022036 WP XFS 77 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 LEFT HORIZONTAL STABILIZER RIB WAS CRACKED AT XFS 77. REPAIRED RIB EDGE IAW DC-9 SRM 55-01. PROTECTED AREA AGAINST CORRO SION IAW DC-9 SRM 51-10-3. 2 L 7 2 4F A6WE 2001111300061 20011113 00061 WP 2001 11 13 ABXA010577 1 20011023 A 5400 99582213 WEB DOUG DC9 DC915 3022036 WP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 LEFT PYLON 45 DEGREE WEB JUST FORWARD OF AFT ENGINE MOUNT CRACKED AT LOWER ATTACH ANGLE. REPAIRED WEB IAW DC-9 SSRM K051 59. 2 L 7 2 4F A6WE 2001111300062 20011113 00062 WP 2001 11 13 ABXA010578 1 20011023 A 5300 99118385 FRAME DOUG DC9 DC915 3022036 WP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 FRAME AT F.S. 930 WAS CRACKED AT LONGERON 3 RIGHT. REPAIRED FRAME IAW DC-9 SSRM K05159. 2 L 7 2 4F A6WE 2001111300063 20011113 00063 WP 2001 11 13 ABXA010579 1 20011030 A 5700 5911305503 SPAR CAP DOUG DC9 DC915 3022036 WP XCW 3 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 CRACK ON REAR SPAR LOWER T-CAP AT APPROXIMATELY XCW 3. REPAIRED AREA IAW DC-9 SRM 57-09. 2 L 7 2 4F A6WE 2001111300064 20011113 00064 WP 2001 11 13 AALA20011915 1 20010927 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 439AA 49457 TUL - FOUND STATION 218 RBL 58 CORRODED ON CUSP MEMBRANE AND STATION 230 RBL 58 CORROSION ON CUSP MEMBRANE. REMOVED AND REPLACED CUSP STATION 218 TO 237 PER SRM 51-01. (M) 2 L 7 2 4F RT A6WE 2001111300065 20011113 00065 WP 2001 11 13 AALA20011916 1 20011002 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 439AA 49457 TUL - FOUND CORROSION ON TIE DOWN TRACK. REPLACED TIE DOWN TRACK W/NEW TRACK PER SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2001111300066 20011113 00066 WP 2001 11 13 AALA20011917 1 20010921 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 439AA 49457 TUL - FOUND CORROSION ON UPPER SURFACE OF NR 3 SEAT TRACK FROM STATION 1301 TO 1305 AT AFT GALLEY MOUNT. REMOVED CORROS ION AND INSTALLED PLUG REPAIR IN TRACK PER SRM 53-05 FIG 4. (M) 2 L 7 2 4F RT A6WE 2001111300067 20011113 00067 WP 2001 11 13 AALA20011918 1 20010924 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 439AA 49457 TUL - FOUND CORROSION ON NR 6 SEAT TRACK. INSTALLED SEAT TRACK PLUG, SRM 53-03 FIG 41. (M) 2 L 7 2 4F RT A6WE 2001111300068 20011113 00068 WP 2001 11 13 AALA20011919 1 20010924 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 439AA 49457 TUL - FOUND WORN AREA ON NR 6 SEAT TRACK FROM BS 702-705. INSTALLED SEAT TRACK PLUG PER SRM 53-20-00-10. (M) 2 L 7 2 4F RT A6WE 2001111300069 20011113 00069 WP 2001 11 13 AALA20011920 1 20010925 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 439AA 49457 TUL - FOUND LEFT CUSP CORROSION AT STATION 708. CUT OUT CORRODED AREA PER SRM 51-10-3. INSTALLED DOUBLER REPAIR PER SR M 53-01 FIG 4 SH 3. (M) 2 L 7 2 4F RT A6WE 2001111300070 20011113 00070 WP 2001 11 13 AALA20011921 1 20010926 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 439AA 49457 TUL - WORN AREA ON FRAME STATION 1418, LONGERON 7L TO 8L. INSTALLED DOUBLER PER AARD 53-10-00-14. (M) 2 L 7 2 4F RT A6WE 2001111300071 20011113 00071 WP 2001 11 13 AALA20011922 1 20010926 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 439AA 49457 TUL - FOUND SEAT TRACK NR 5 CORRODED STATION 200. INSTALLED TRACK SPLICE ON NR 5 SEAT TRACK STATION 200-265 PER SRM 53- 05-00. (M) 2 L 7 2 4F RT A6WE 2001111300072 20011113 00072 WP 2001 11 13 AALA20011923 1 20010926 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 439AA 49457 TUL - FOUND CORROSION ON SEAT TRACK FROM BS 234 TO BS 237. INSTALLED TRACK SPLICE ON NR 5 SEAT TRACK STATION 200 THROUG H 265 PER SRM 53-05-00. (M) 2 L 7 2 4F RT A6WE 2001111300073 20011113 00073 WP 2001 11 13 AALA20011924 1 20010927 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 439AA 49457 TUL - FOUND CORROSION ON RIGHT TIE DOWN TRACK AT 1136 AND 1142. REMOVED OLD TRACK AND INSTALLED NEW TIE DOWN TRACK SRM 51-01. (M) 2 L 7 2 4F RT A6WE 2001111300074 20011113 00074 WP 2001 11 13 AALA20011925 1 20010925 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 439AA 49457 TUL - FOUND LEFT CUSP CORROSION AT STATION 725. REMOVED CORROSION BY DRILLING .25 INCH HOLE, PLUGGED HOLE WITH FASTENER PER SRM 53-01 FIG 1, SH 2. (M) 2 L 7 2 4F RT A6WE 2001111300075 20011113 00075 WP 2001 11 13 AALA20011926 1 20010925 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 439AA 49457 TUL - FOUND DENT ON FUSELAGE UNDER RIGHT STATION 1305 BETWEEN LONGERON 18R AND 19R ADL NR 4390015. INSTALLED DOUBLER PE R SRM 53-04 FIG 38. (M) 2 L 7 2 4F RT A6WE 2001111300076 20011113 00076 WP 2001 11 13 AALA20011927 1 20010925 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 439AA 49457 TUL - FOUND CRACK IN LONGERON L4 AT STATION 160. REMOVED DAMAGED SECTION OF LONGERON AND REPAIRED PER SRM 53-02 PAGE 48 . (M) 2 L 7 2 4F RT A6WE 2001111300077 20011113 00077 WP 2001 11 13 AALA20011928 1 20010925 A 5310 STOP FITTING DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 439AA 49457 TUL - FOUND LEFT CENTER VAULT DOOR CUTOUT STOP SUPPORT CASTING HAS VISUAL INDICATION OF CRACK OF BOTTOM OF PAD BOLT. IN STALLED SERVICEABLE CASTING SRM 51-01. (M) 2 L 7 2 4F RT A6WE 2001111300078 20011113 00078 WP 2001 11 13 AALA20011929 1 20010924 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 439AA 49457 TUL - FOUND CORROSION ON NR 6 SEAT TRACK FROM STATION 826 TO 830. REMOVED DAMAGED AREA AND INSTALLED PLUG PER AARD 53-2 0-00-10. (M) 2 L 7 2 4F RT A6WE 2001111300079 20011113 00079 WP 2001 11 13 AALA20011930 1 20010924 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 439AA 49457 TUL - FOUND DIAPHRAGM WEB BELOW G2 TIE DOWN CORRODED STATION 218 RBL 13 INCHES. CUT OUT CORRODED AREA AND INSTALLED DOU BLER REPAIR PER AARD 53-00-00-02. (M) 2 L 7 2 4F RT A6WE 2001111300080 20011113 00080 NM 2001 11 13 ASAA0140087A 1 20010607 A 5210 6951337 GUIDE BOEING 737 7374Q8 NM L1 DOOR DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 769AS 25103 SEA - DURING PREFLIGHT CHECK, FOUND THE L1 DOOR STIFF AND DIFFICULT TO OPEN. REPLACED GUIDE ARM. DOOR THEN OPERATED NO RMALLY. (M) 2 L 7 2 4F RT A16WE 2001111300081 20011113 00081 SO 2001 11 13 ASOA01153S 1 20010831 A 2731 SERVO EMB 120 EMB120RT 3260202 SO ELEVATOR WORN A ASOA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 11 275AS 120234 FLT 4810 - DURING FLIGHT, REPORTED THAT THE A/C WAS HARD TO CONTROL. WHEN THE AUTOPILOT WAS DISCONNECTED, THE ELEV AND R UDDER WERE HEAVY AS IF THEY WERE STILL CONNECTED TO THE AUTOPILOT. PULLED THE AUTOPILOT CIRCUIT BREAKERS, BUT THIS DIDN` T FIX THE PROBLEM. DECLARED AN EMERGENCY AND A/C LANDED IN TUL WITHOUT INCIDENT. THE TEARDOWN REPORT STATE THERE WERE PR OBLEMS WITH THE ELEV TRIM SERVO AS WELL AS THE RUDDER SERVO MOUNT. THE ELEV TRIM SERVO WAS FOUND TO HAVE A WORN CLUTCH WHICH COULD CAUSE THE TRIM SERVO TO ENGAGE AND DISENGAGE IMPROPERLY. THE TEARDOWN ON THE RUDDER SERVO MOUNT FOUND THAT THE CAPSTAN WAS WORN MORE THAN USUAL. BOTH COMPONENTS WILL BE OVERHAULED. (M) 2 L 7 2 4T RT A31SO 2001111300082 20011113 00082 EU 2001 11 13 ASOA01204 1 20011008 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72 EU CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 643AS 18895 413 FLT 4285 - DURING GROUND INSPECTION IN ATL, THE EMERGENCY FLOOR LIGHTS WERE INOPERATIVE AT SEVERAL ROWS. MAINTENANCE RE MOVED AND REPLACED THE EMERGENCY LIGHTING POWER SUPPLY AT POSITION 61WL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERV ICE. (M) 2 H 7 2 4T RT 2001111300083 20011113 00083 2001 11 13 ASOA01205 4 20011009 A 2350 509111 AUDIO PANEL EMB 120 EMB120RT 3260202 SO COCKPIT FAULTY A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 11 275AS 120234 FLT 4916 - ON DESCENT INTO DFW, FIRST OFFICER SMELLED AN ELECTRICAL SMELL FOLLOWED BY VISUALLY SEEING SMOKE COMING FROM HIS COMM PANEL. AN EMERGENCY WAS NOT DECLARED, BUT FIRE TRUCKS WERE REQUESTED. AIRCRAFT LANDED SAFELY IN DFW. AFTER L ANDING NO FURTHER SMOKE WAS VISIBLE. UPON INSPECTION MAINTENANCE FOUND THE FIRST OFFICERS AUDIO CONTROL PANEL TO BE HOT AND EMITTING A BURNING SMELL. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS AUDIO CONTROL PANEL. OPERATIONAL CH ECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001111300084 20011113 00084 EA 2001 11 13 ASOA01206 1 20011009 A 2740 70608 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB FAILED A ASOA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 11 840AS 6237 7290 FLT 4736 - DURING CRUISE FLIGHT FROM ATL TO ICT, THE AIRCRAFT STAB AND MACH TRIM FAILED. THE CAPTAIN RESET AND THE TRIM FAILED AGAIN. THE AUTOPILOT DID NOT DROP OFF. AN EMERGENCY WAS DECLARED. AIRCRAFT LANDED IN ICT WITHOUT FURTHER INCI DENT. THE SYSTEM WAS RESET ON THE GROUND AND ALL OPERATIONS WERE NORMAL. ON THE RETURN FLIGHT INTO ATL, THE STAB TRIM BECAME INOPERATIVE ONCE AGAIN. AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE INSPECTED AND FOUND THE NR 1 STAB TRIM INOPE RATIVE. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER TRIM CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRA FT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001111300085 20011113 00085 2001 11 13 HALA0100250 4 20011018 A 3417 ADC DOUG DC10 DC1010 3022110 WP NR 2 FAILED A HALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 13 126AA 46947 ATO - DURING TAKEOFF NO AIRSPEED INDICATION ON F/O'S AIRSPEED INDICATOR. REPLACED NR 2 ADC. OPS CHECK OF NR 2 ADC CHEC KED GOOD PER 34-16-01. INSPECTED F/O'S PITOT TUBE, PRESSURE CHECK GOOD. (M) 2 L 7 3 4F A22WE 2001111300086 20011113 00086 EA 2001 11 13 MASA01045 1 20010530 A 2612 FIRE LOOP CNDAIR CL600 CL6002B19 1900309 EA JET PIPE BROKEN A MASA K NONE N FALSE WARNING CR CRUISE 1 SW 07 97325 7325 FLT 6427 - PHX-EUG - ENGINE FIRE DETECTION LIGHT CAME ON FOR 1 SECOND. THE MESSAGE WAS NOT ASSOCIATED WITH A AURAL WARN ING HORN. THE PLANE CONTINUED ON TO EUG WITHOUT ANY FURTHER INCIDENT. AFTER LANDING MAINTENANCE TROUBLESHOT AND FOUND BROKEN WIRE IN THE JET PIPE LOOP. OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001111300087 20011113 00087 EA 2001 11 13 MASA01046 1 20010524 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN DAMAGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17337 7337 FLT 6534 - CMH - THE FLOOR LEVEL EMERGENCY LIGHTS PARTIALLY INOPERATIVE FROM ROW 9 AFT. MAINTENANCE REPLACED ONE WIRE S TRIP AND REPAIRED WIRES ON THE OTHER STRIP. OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001111300088 20011113 00088 EA 2001 11 13 MASA01054 1 20010620 A 2560 P2070001214 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17337 7337 DURING PREFLIGHT IT WAS DISCOVERED THAT THE PILOTS EMERGENCY FLASHLIGHT LED WAS INOPERATIVE. THE PILOTS EMERGENCY FLASH LIGHT WAS REPLACED. OPS CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001111300089 20011113 00089 SO 2001 11 13 SIMA200125601 1 20010913 A 5320 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 ABI - DURING MBV, FOUND SERVICE DOOR AFT SILL CORRODED. INSTALLED REPAIR DOUBLER ON SERVICE DOOR AFT SILL IAW EMB 135 S ERVICE LETTER GST 3128/01. (M) 2 L 7 2 4F RT TOOO11AT 2001111300090 20011113 00090 SO 2001 11 13 SIMA200126007 1 20010917 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 ABI - DURING MBV INSPECTION, CENTER FLOORBEAM BETWEEN FRAMES 24 AND 26 WAS FOUND TO BE CORRODED. REMOVED CORROSION IAW EMB 135 SRM 51-10-02. INSTALLED REPAIR DOUBLER ON CENTER FLOORBEAM IAW EMB 135 SERVICE LETTER GST 3143/01. (M) 2 L 7 2 4F RT TOOO11AT 2001111300091 20011113 00091 SO 2001 11 13 SIMA200126008 1 20010917 A 3210 14571035411 CAP EMB 135 EMB135LR 3260305 SO LT & RT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 ABI - LEFT AND RIGHT MLG FORWARD AND AFT BEARING CAPS CORRODED. REMOVED AND REPLACED BEARING CAPS IAW EMB AMM. (M) 2 L 7 2 4F RT TOOO11AT 2001111300092 20011113 00092 SO 2001 11 13 SIMA200126009 1 20010917 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 ABI - DURING MBV, FOUND FORWARD DIGITAL TO BE CORRODED. REMOVED CORROSION AND FOUND TO BE ACCEPTABLE IAW EMB135 SERVICE LETTER GST 3128/01. (M) 2 L 7 2 4F RT TOOO11AT 2001111300093 20011113 00093 SO 2001 11 13 SIMA200126010 1 20010917 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 ABI - DURING MBV RIGHT FLOORBEAM WAS TO BE CORRODED BETWEEN FRAMES 17 AND 18. REMOVED CORROSION IAW EMB 135 SRM 51-10-0 2. (M) 2 L 7 2 4F RT TOOO11AT 2001111300094 20011113 00094 SO 2001 11 13 SIMA200126011 1 20010917 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 DURING MBV, LEFT FLOORBEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 23 AND 24. REMOVED CORROSION IAW EMB 135 SRM. (M) 2 L 7 2 4F RT TOOO11AT 2001111300095 20011113 00095 SO 2001 11 13 SIMA200126012 1 20010917 A 5320 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 ABI - DURING MBV INSPECTION, RIGHT SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 25 AND 31. REMOVED CORROSION IAW EMB135 SRM. (M) 2 L 7 2 4F RT TOOO11AT 2001111300096 20011113 00096 SO 2001 11 13 SIMA200126013 1 20010917 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 ABI - DURING MBV INSPECTION, FOUND CORROSION ON THE LEFT FLOORBEAM AT FRAME 20. FABRICATED FILLER AND DOUBLER AND INSTA LLED ON AIRCRAFT IAW EMB 135 SRM. (M) 2 L 7 2 4F RT TOOO11AT 2001111300097 20011113 00097 SO 2001 11 13 SIMA200126014 1 20010917 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 ABI - DURING MBV INSPECTION, FOUND CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 CORRODED. FABRICATED REPAIR DOUBLER AND I NSTALLED ON AIRCRAFT IAW EMB 135 REPAIR STATEMENT GST-2930/01 AND EMB 135 SRM. (M) 2 L 7 2 4F RT TOOO11AT 2001111300098 20011113 00098 SO 2001 11 13 SIMA200126105 1 20010918 A 5320 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 ABI - DURING MBV INSPECTION, SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. REPAIRED CORRODED SERVICE DOOR FORWARD SILL IAW EMB 135 REPAIR STATEMENT GST-3128/01. (M) 2 L 7 2 4F RT TOOO11AT 2001111300099 20011113 00099 NM 2001 11 13 2001UALA02216 1 20011102 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 FRAME AT STATION 1180 BETWEEN STRINGER 8R AND 9R HAS FIVE DRILL MARKS. MAJOR REPAIR ACCOMPLISHED.BLENDED DAMAGE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001111300100 20011113 00100 NM 2001 11 13 2001UALA02219 1 20011021 A 5313 CLIP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 650UA 25287 MAJOR BS1175 STRINGER 35L CLIP CORRODED SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STR INGER CLIP 2 L 7 2 4F 4 F RT A1NM E24NE 2001111300101 20011113 00101 NM 2001 11 13 2001UALA02220 1 20011021 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 650UA 25287 MAJOR BS 852 RBL30 WL200 FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM SECTION AND SPLICES 2 L 7 2 4F 4 F RT A1NM E24NE 2001111300102 20011113 00102 NM 2001 11 13 2001UALA02221 1 20011021 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 650UA 25287 MAJOR FS 785.9 FLOORBEAM CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM SECTION AND SPLICES. 2 L 7 2 4F 4 F RT A1NM E24NE 2001111300103 20011113 00103 NM 2001 11 13 2001UALA02222 1 20011021 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 650UA 25287 MAJOR BS 852 RBL 50 WL 200 FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM AND SPLIC ES. 2 L 7 2 4F 4 F RT A1NM E24NE 2001111300104 20011113 00104 NM 2001 11 13 2001UALA02223 1 20011207 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 506US 23195 DURING "H" CHECK FOUND CRACK IN FLOORBEAM UPPER CAP AT BS 700 LBL 25. REPAIRED PER EA 55-186814 2 L 7 2 4F RT A2NM 2001111300105 20011113 00105 SO 2001 11 13 SIMA200126106 1 20010918 A 5320 13500469401 STRUCTURE EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 ABI - DURING MBV INSPECTION, FOUND FORWARD INBOARD RIGHT CROSS MEMBER AT FRAME 22 CORRODED. INSTALLED NEW CROSS MEMBER IAW EMB 135 SRM. (M) 2 L 7 2 4F RT TOOO11AT 2001111300106 20011113 00106 SO 2001 11 13 SIMA200126402 1 20010921 A 2161 6071T20P16 CONTROL VALVE EMB 145 EMB145LR 3260212 SO AIR CONDITIONING FAULTY A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 21 628AE 145124 ORD - FLIGHT CREW FOUND SMOKE IN CABIN ON GROUND. REMOVED AND REPLACED DUEL TEMPERATURE CONTROL VALVE IAW EMB 145 AMM. OPERATIONALLY CHECKED GOOD. (M) 2 L 7 2 4T RT T00011AT 2001111300107 20011113 00107 SO 2001 11 13 SIMA200126920 1 20010926 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 646AE 3514 145213 ABI - DURING MBV INSPECTION, FOUND SERVICE DOOR AFT SILL CORRODED FROM FRAME 21 TO 23. REMOVED AND REPLACED AFT DOOR SI LL IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2001111300108 20011113 00108 SO 2001 11 13 SIMA200126923 1 20010926 A 5320 BEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 646AE 3514 145213 ABI - DURING MBV INSPECTION, FOUND CENTER BEAM AT FRAME 21 CORRODED. REPAIRED CENTER BEAM AT FRAME 21 IAW EMB REPAIR ST ATEMENT GST-3196/01. (M) 2 L 7 2 4T RT T00011AT 2001111300109 20011113 00109 SO 2001 11 13 SIMA200126924 1 20010926 A 5320 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 646AE 3514 145213 ABI - DURING MBV INSPECTION, FOUND AFT PAX DOOR FLOOR SUPPORT CORRODED. REPAIRED AFT PAX DOOR FLOOR SUPPORT IAW EMB REP AIR STATEMENT GST-3196/01. (M) 2 L 7 2 4T RT T00011AT 2001111300110 20011113 00110 SO 2001 11 13 SIMA200128008 1 20011007 A 3610 V8545A7257226 O-RING EMB 145 EMB145 3260210 SO BLEED AIR SYS DAMAGED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 611AE 145074 ORD - FLT 4263 - DURING CLIMB-OUT, CREW NOTED RIGHT ENGINE BLEED LEAK INDICATION. CREW RETURNED TO FIELD IN ORD AND DEC LARED AN EMERGENCY. REPLACED O-RING IN BLEED DUCT IAW EMB 145 AMM. NO FURTHER LEAKS NOTED. (M) 2 L 7 2 4F RT T00011AT 2001111300111 20011113 00111 EA 2001 11 13 COMA0160882 1 20011109 A 5311 6003603024 FRAME CNDAIR CL600 CL6002B19 1900309 EA F.S.780.0 R/II CRACKED A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 710CA 7676 7241 DISC CRACKED FRAME FLANGE @F.S.718 R/H SIDE.CORRECTIVE ACTION; CUT OUT DAMAGED FRAME, FABRICATED AND INSTALLED REPAIR SECTION MADE FROM P/N 600-36030-24. ALL WORK PERFORMED I/A/W WVAC EO 601R-53-2828, CANADAIR CRJ REO 601R-53-61-193 AND CRJ SRM REF LOG PAGE #470315 AND COMAIR W/O #29873. 2 L 7 2 4F RT A21EA 2001111300112 20011113 00112 EA 2001 11 13 COMA0160883 1 20011111 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 958CA 13917 7111 R/H LOWER WING PLANK CRACKED AT 650 BB W.S. 188.040.DAMAGE GOES BEYOND THE LIMITS IN REO 601R-57-21-030. BLENDED OUT DA MAGE AND ROTO-PEENED I/A/W REO 601R-57-21-030 AND REO 601R-57-21-156. 2 L 7 2 4F RT A21EA 2001111300113 20011113 00113 EA 2001 11 13 COMA0160885 1 20011110 A 5346 601350061 WEB CNDAIR CL600 CL6002B19 1900309 EA FS 625.3 TO FS 6 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 710CA 7676 7241 THE ENGINE SUPPORT BEAM LOWER WEB WAS CRACKED AT L/H AND R/H SIDES.REMOVED THE CRACKED PORTIONS OF THE LOWER WEB AND PER FORMED A MAJOR REPAIR I/A/W REO 601R-53-61-366 REV D. 2 L 7 2 4F RT A21EA 2001111300114 20011113 00114 SO 2001 11 13 SIMA20126104 1 20010918 A 5320 14522461011 GUSSET EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 ABI - DURING MBV - INSPECTION, FOUND SERVICE DOOR FORWARD AND AFT GUSSET PLATES CORRODED. REMOVED AND REPLACED FORWARD AND AFT GUSSET PLATES IAW EMB 135 SRM. (M) 2 L 7 2 4F RT TOOO11AT 2001111300115 20011113 00115 NM 2001 11 13 UIEA00052A 1 20010427 A 5330 SKIN BOEING 747 7472D3B 1384805 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 78537 21251 DURING HFEC INSPECTION PER SB 747-53A2488 FOUND LOWER LOBE CARGO COMPARTMENT AFT DOOR UPPER CUT OUT, FORWARD CORNER CRAC KED UNDER 2 INCHES. SHIMS OVER .055 THICK. TRIMMED OUT CRACK. FABRICATED FILLER AND REPAIR DOUBLER. INSTALLED IAW SR M 53-30-03 TYPE II DETAIL II. (M) 2 L 7 4 4F RT A20WE 2001111500131 20011115 00131 EA 2001 11 15 COMA0160884 1 20011111 A 5730 PLANK CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 958CA 7111 LT LOWER WING PLANK CRACKED AT 540 FS 540 WS 136.676. BLENDED OUT DAMAGE AND ROTO-PEENED IAW REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 2001111500128 20011115 00128 SO 2001 11 15 COMA0110155 1 20011111 A 3246 31544 WHEEL EMB 120 EMB120RT 3260202 SO RT MLG CRACKED A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 259CA 7956 43 120252 FLIGHT 5825 DURING PREFLIGHT INSPECTION, THE CREW NOTICED THAT THE RIGHT MAIN INBOARD WHEEL INNER HALF WAS CRACKED AND A PORTION OF THE FLANGE WAS SLIGHTLY PROTRUDING. THE WHEEL FLANGE HAD GOUGED THE LOWER TORQUE-LINK OF THE RIGHT MAIN GE AR.THE WHEEL ASSEMBLY, AND THE LOWER TORQUE-LINK WERE REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 2001111500129 20011115 00129 EA 2001 11 15 COMA0160881 1 20011107 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 938CA 7046 FLIGHT 5884 CABIN DOOR OUTER HANDLE MESSAGE, A/C DIVERTED TO IND. COULD NOT DUPLICATE. OPERATION OF CABIN DOOR NORMAL . NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 2001111300116 20011113 00116 NM 2001 11 13 UIEA01098 1 20010930 A 2913 6506606 PUMP BOEING 747 747341 NM NR 4 ENGINE FAILED A UIEA E F A ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 15 355MC 23395 SHORTLY AFTER LEVEL OF AT 39.0, NR 4 ENGINE FIRE WARNING LIGHT ILLUMINATED. BOTH A/B FIRE LOOPS INDICATED FIRE. ACCOMP LISHED EMERGENCY FIRE PROCEDURES. AIRCRAFT RETURNED TO MIA. FOUND NR 4 EDP AT FAULT. REMOVED AND REPLACED EDP P/N 650 6606. OPS AND LEAK CHECK OK. ALSO, FOUND 8TH STAGE DUCT CLAMP LEAKING NEAR FIRE WARNING ELEMENT. REPLACED CLAMP, PERF ORMED OPS AND LEAK CHECK. ALL OK. (M) 2 L 7 4 4F RT A20WE 2001111300117 20011113 00117 NM 2001 11 13 UIEA01099 1 20010930 A 2611 327LSVAS15 LIGHT BOEING 747 747212B 1384886 NM CARGO BAY FAULTY A UIEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 15 808MC 21048 AIRCRAFT ATB DUE TO LOWER AFT CARGO AND BULK CARGO COMPARTMENT FIRE WARNING INDICATION. PERFORMED TROUBLE SHOOTING PER MM 26-16-00 AND FOUND NR 4, NR 5 AND NR 6 SMOKE DETECTOR LAMPS AT FAULT. REMOVED AND REPLACED LAMPS AND PERFORMED SYSTE M TEST. ALL OPS OK. (M) 2 L 7 4 4F A20WE 2001111300118 20011113 00118 NM 2001 11 13 UIEA01100 1 20011005 A 2612 FIRE WARNING BOEING 747 7472D3B 1384805 NM COCKPIT FALSE INDICATION A UIEA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 EA 15 506MC 21252 ATB DUE LOWER AFT CARGO FIRE LIGHT ON AT ROTATION NR 1 BOTTLE DISCHARGED, FALSE INDICATION. LOWER AFT CARGO INSPECTED. NO SIGNS OF FIRE (NO CARGO IN SECTION). ITEM TRANSFERRED TO DMI PAGE 03049 AND DEFERRED PER MEL 26-14-2D AND ALL DDPG PROCEDURES FOLLOWED. (M) 2 L 7 4 4F RT A20WE 2001111300119 20011113 00119 NM 2001 11 13 UIEA01101 1 20011008 A 2611 P490499R3 SMOKE WARNING BOEING 747 74747UF 1384949 NM LAVATORY MALFUNCTIONED A UIEA O OTHER N FALSE WARNING AP APPROACH 1 EA 15 408MC 29261 10 MINUTES INTO FINAL APPROACH, LAVATORY SMOKE DETECTOR SOUNDED CONTINUOUSLY UNTIL ARRIVAL AT PARKING STAND WHEN MX RESE T SMOKE DETECTOR. FIRE DEPT CONFIRMED NO SMOKE OR FIRE. LAVATORY COMPARTMENT AND COMPONENTS UNDERNEATH TOILET SHROUD I NSPECTED AND FOUND NO EVIDENCE OF BURN MARKS OR SHORTED ELECTRICAL WIRES. SMOKE DETECTOR TESTED PER MM CHAPTER 26-13-01 . FOUND OK. (M) 2 L 7 4 4F RT 1384945 2001111300120 20011113 00120 NM 2001 11 13 USAA010455 1 20010425 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 515AU 44427 23701 TPA - FOUND FUSELAGE SKIN DAMAGED 4 INCHES, BS 747, BETWEEN S18L AND S19L. INSTALLED DOUBLER PER SRM 53-00-01, FIG 202. (M) 2 L 7 2 4F RT A16WE 2001111300121 20011113 00121 EU 2001 11 13 USAA011293 1 20010913 A 5330 SKIN AIRBUS A319 A319112 3930323 EU FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 760US 2897 1354 CLT - FOUND SKIN DENTED 4 INCHES BY 4 INCHES, 3 FT FORWARD OF LEFT AFT DOOR ON FUSELAGE. INSTALLED DOUBLER. (M) 2 L 7 2 4F RT A28NM 2001111300122 20011113 00122 NM 2001 11 13 USAA011299 1 20011010 A 5210 BEAM BOEING 737 737201 1384454 NM ENTRY DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 48384 22962 CLT - FOUND BEAM CRACKED 1.5 INCH, LOWER INTERIOR FORWARD CORNER OF FORWARD ENTRY DOOR BEAM. INSTALLED A NEW BEAM ASSY PER SRM 51-10-1 AND 51-30-2. (M) 2 L 7 2 4F A16WE 2001111300123 20011113 00123 NM 2001 11 13 USAA011300 1 20011003 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 48384 22962 CLT - FOUND SKIN CRACKS 1.5 INCH AND .250 INCH, BS 380 EQUIP COOLING EXHAUST. INSTALLED REPAIR DOUBLER PER T/R 53-30-04 . (M) 2 L 7 2 4F A16WE 2001111300124 20011113 00124 WP 2001 11 13 ABXA010581 1 20011111 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC933F 302207A WP CABIN DEFECTIVE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 COCKPIT EMERGENCY LIGHTS WOULD NOT COME ON. REPLACED EMERGENCY LIGHT BATTERIES IAW DC-9 AMM 33-53-0-2-4-0001. 2 L 7 2 4F A6WE 2001113000054 20011130 00054 WP 2001 11 30 ARWA0011015 1 20011112 A 3260 UPLOCK SWITCH DOUG DC8 DC862 3021970 WP LT MLG DIRTY A ARWA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 19 8969U 46070 WHILE PERFORMING THE UPLATCH CHECK, LIGHT STAYED ILLUMINATED. COMPLETED ABNORMAL PROCEDURE AND RETURNED TO RODN. LUBRI CATED LANDING GEARS AND UPLATCH MECHANISM, CLEANED AND SECURED LT MLG UPLATCH SWITCH IAW MM 32-60-0. OPERATION CHECK NO RMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2001111300125 20011113 00125 NM 2001 11 13 USAA011301 1 20010912 A 5313 STRINGER BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 225US 48384 21667 CLT - FOUND STRINGER CORRODED 1.5 INCH BY 13 INCHES, STRINGER 27L BETWEEN STATION 900 AND 913. INSTALLED DOUBLER AND SE CTION OF STRINGER. (M) 2 L 7 2 4F A16WE 2001111300126 20011113 00126 NM 2001 11 13 USAA011302 1 20010912 A 5310 SHEAR TIE BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 48384 22962 CLT - FOUND SHEAR TIE CRACKED .5 INCH, AT STRINGER 25R TO FRAME AT STATION 947.5. REPLACE TIE CLIP. (M) 2 L 7 2 4F A16WE 2001111300127 20011113 00127 NM 2001 11 13 USAA011303 1 20010913 A 5347 SEAT TRACK BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 48384 22962 CLT - FOUND FLOOR TRACK CORRODED 1 INCH BY 1 INCH, AFT CARGO STATION 806 S26R. INSTALLED REPAIR TIE DOWN FLOOR SUPPORT PER SRM 53-10-5 FIG 11. (M) 2 L 7 2 4F A16WE 2001111300128 20011113 00128 NM 2001 11 13 USAA011304 1 20011004 A 5313 STRINGER BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 48384 22962 CLT - FOUND STRINGER CRACKED 6 INCHES, STRINGER 20L STATION 777. INSTALLED STRINGER REPAIR PER SRM 53-10-3 DETAIL VII. (M) 2 L 7 2 4F A16WE 2001111300129 20011113 00129 NM 2001 11 13 USAA011306 1 20010912 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 48384 22962 CLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH, STATION 847 JUST ABOVE STRINGER 26R. INSTALLED DOUBLER. (M) 2 L 7 2 4F A16WE 2001111300130 20011113 00130 NM 2001 11 13 USAA011307 1 20010913 A 5311 FRAME BOEING 737 737201 1384454 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 48384 22962 CLT - FOUND FRAME DENTED 1 INCH BY 1 INCH, AFT CARGO STATION 767 ABOVE STRINGER 24R. INSTALLED DOUBLER AT STATION 767 P ER SRM 51-40-3. (M) 2 L 7 2 4F A16WE 2001111300131 20011113 00131 NM 2001 11 13 USAA011309 1 20010918 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 48384 22962 CLT - FOUND SKIN CRACKED 15 INCHES BY 13 INCHES, STATION 947 S15R. INSTALLED DOUBLER AND TRIPLER PER SRM 53-30-3 FIG 35 . (M) 2 L 7 2 4F A16WE 2001111300132 20011113 00132 NM 2001 11 13 USAA011310 1 20010928 A 5310 WINDOW POST BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 46526 22959 PIT - FOUND WINDSHIELD POST CRACKED .375 INCH, PILOTS UPPER WINDSHIELD POST OUTBOARD CORNER. STAR DOUBLER INSTALLED PER SRM 53-10-01 FIG 210/EO 56937096. (M) 2 L 7 2 4F RT A16WE 2001111300133 20011113 00133 NM 2001 11 13 USAA011311 1 20010928 A 5240 DOOR FRAME BOEING 737 7373B7 1384580 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 46526 22959 PIT - FOUND FRAME/JAMB SPACER CRACKED 2 INCHES, JOINING SPACER OF FORWARD SERVICE DOOR. MANUFACTURED NEW SPACER OUT OF 2024-T3 .080 PER OM-26 NR J3-46-52500-C-002. (M) 2 L 7 2 4F RT A16WE 2001111300134 20011113 00134 NM 2001 11 13 USAA011312 1 20011006 A 5320 ATTACH ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 46526 22959 PIT - FOUND FLOORBOARD ATTACH ANGLE CORRODED IN SEVEN AREAS 1 INCH BY 4 INCHES, STATION 773 FROM 25L-25R. REMOVED CORROD ED SECTION AND INSTALLED REPAIR ANGLES IAW TYPICAL REPAIR 53-10-06B. (M) 2 L 7 2 4F RT A16WE 2001111300135 20011113 00135 NM 2001 11 13 USAA011313 1 20010915 A 5320 ATTACH ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 46526 22959 PIT - FOUND FLOORBOARD ATTACH ANGLE CORRODED 100 INCHES BY 3 INCHES, STATION 727-727E ABOVE STRINGER 25L. REMOVED CORRO SION, TREATED, PRIMED AND PAINTED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001111300136 20011113 00136 NM 2001 11 13 USAA011314 1 20010927 A 5320 ATTACH ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 46526 22959 PIT - FOUND FLOORBOARD ATTACH ANGLE CORRODED 71 INCHES BY 2 INCHES, STATION 782-853 ABOVE STRINGER 26R. REMOVED AND REP LACED TIE DOWN RAIL TRACK EXTRUSION REPLACED PER SRM 53-00-53. (M) 2 L 7 2 4F RT A16WE 2001111300137 20011113 00137 NM 2001 11 13 USAA011315 1 20010915 A 5320 THRESHOLD BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 46526 22959 PIT - FOUND THRESHOLD PLATE CORRODED IN MULTIPLE AREAS 1 INCH BY 1 INCH, STATION 800 TO 845 THRESHOLD FOR AFT CARGO DOOR . CORROSION REMOVED, TREATED WITH ALODINE, PRIMED, PAINTED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001111300138 20011113 00138 NM 2001 11 13 USAA011316 1 20010915 A 5320 FLOOR SUPPORT BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 46526 22959 PIT - FOUND FLOOR PANEL ATTACH PADS CORRODED 1 INCH BY 1 INCH BY 5 AREAS, STA 791 STRINGER BETWEEN 20L-24L. REMOVED COR ROSION, TREATED, PRIMED AND PAINTED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001111300139 20011113 00139 NM 2001 11 13 USAA011317 1 20010915 A 5311 BELTFRAME BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 46526 22959 PIT - FOUND BELTFRAME CORRODED 1 INCH BY 7 INCHES, STATION 727D AT STRINGER 25L. REMOVED CORROSION, TREATED, PRIMED AND PAINTED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001111300140 20011113 00140 NM 2001 11 13 USAA011318 1 20010915 A 5320 FLOOR SUPPORT BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 46526 22959 PIT - FOUND FLOORBOARD ATTACH CROSS BRACE CORRODED 36 INCHES BY 2 INCH AREA, STATION 727D. CORROSION REMOVED, TREATED, PAINTED AND PRIMED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001111300141 20011113 00141 NM 2001 11 13 USAA011319 1 20011017 A 5320 FLOOR SUPPORT BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 46526 22959 CLT - FOUND FLOORBOARD ATTACH RAIL CORRODED 40 INCHES BY 3 INCHES, STATION 727E-767 ABOVE 25R. (M) 2 L 7 2 4F RT A16WE 2001111300142 20011113 00142 NM 2001 11 13 USAA011320 1 20010915 A 5320 FLOOR SUPPORT BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 46526 22959 PIT - FOUND FLOORBOARD ATTACH RAIL CORRODED 66 INCHES BY 3 INCH AREA, FS 727E-793 AT STRINGER 25L. REMOVED CORROSION, T REATED, PRIMED, PAINTED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001111300143 20011113 00143 NM 2001 11 13 USAA011321 1 20010915 A 5320 ATTACH ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 46526 22959 PIT - FOUND FLOORBOARD ATTACH ANGLE CORRODED 1 INCH BY 1 INCH AREA, STA 727E, 3 INCHES LEFT OF C/L. REMOVED CORROSION, TREATED, PRIMED, PAINTED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001111300144 20011113 00144 NM 2001 11 13 USAA011322 1 20010915 A 5311 BELTFRAME BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 22959 PIT - FOUND BELTFRAME CORRODED 1 INCH BY 10 INCH AREA, STATION 787 STRINGER 23L-25L. REMOVED CORROSION, TREATED, PRIMED AND PAINTED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001111300145 20011113 00145 NM 2001 11 13 USAA011323 1 20010915 A 5320 FLOOR SUPPORT BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 46526 22959 PIT - FOUND FLOORBOARD ATTACH RAIL CORRODED 25 INCH BY 3 INCH AREA, STATION 767-792 ABOVE 25R. REMOVED CORROSION, TREAT ED, PRIMED, PAINTED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001111300146 20011113 00146 NM 2001 11 13 USAA011324 1 20010913 A 5320 FLOOR SUPPORT BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 22959 PIT - FOUND FLOORBOARD ATTACH RAIL CORRODED 55 INCH BY 3 INCH AREA, STATION 792-847 ABOVE STRINGER 25L. REMOVED CORROSI ON, TREATED, PRIMED, PAINTED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001111300147 20011113 00147 NM 2001 11 13 USAA011325 1 20010914 A 5320 ATTACH ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 46526 22959 PIT - FOUND FLOORBOARD ATTACH ANGLE CORRODED 4 INCH BY 6 INCH AREA, STATION 947.5 ABOVE STRINGER 25L AND 26L. BLENDED P ER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001111300148 20011113 00148 NM 2001 11 13 USAA011326 1 20010915 A 5311 BELTFRAME BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 46526 22959 PIT - FOUND BELTFRAME CORRODED 1 INCH BY 1 INCH AREA, STATION 887 BETWEEN STRINGER 24L AND 25L. REMOVED CORROSION, TREA TED, PRIMED, PAINTED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001111300149 20011113 00149 NM 2001 11 13 USAA011327 1 20010915 A 5311 BELTFRAME BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 46526 22959 PIT - FOUND BELTFRAME CORRODED 1 INCH BY 7 INCH AREA, STATION 727D AT STRINGER 25R. REMOVED CORROSION, TREATED, PRIMED, PAINTED PER SRM 53-60-13. (M) 2 L 7 2 4F RT A16WE 2001111300150 20011113 00150 NM 2001 11 13 USAA011328 1 20010915 A 5320 ATTACH ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 46526 22959 PIT - FOUND FLOORBOARD ATTACH ANGLE CORRODED 1 INCH BY 1 INCH AREA, STATION 727B ABOVE STRINGER 27L. CORROSION REMOVED, TREATED, PRIMED, PAINTED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2001111300151 20011113 00151 NM 2001 11 13 USAA011329 1 20011011 A 5753 FLAP BOEING 737 737301 1384611 NM WING DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 592US 44131 23937 PIT - FOUND INBOARD AFT FLAP DELAMINATED 15 INCHES BY 7 INCHES ROLLER AND 24 INCHES FROM INBOARD END, INBOARD AFT FLAP, BOTTOM SURFACES SKIN, INBOARD ROLLER SUPT. REPAIRED PER EA 72583, SRM 51-70-10, SRM 57-43-01 FIG 1. (M) 2 L 7 2 4F RT A16WE 2001111300152 20011113 00152 NM 2001 11 13 USAA011330 1 20011011 A 5542 35501 SKIN BOEING 737 7373B7 1384580 NM RUDDER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 46526 22959 PIT - FOUND RUDDER DELAMINATED 2.5 INCHES BY 8 INCH AREA, LEFT SIDE STATION 33 AND 34 APPROXIMATELY 10 INCHES FROM LEADI NG EDGE. REPAIRED PER EA 72581 AND SRM 51-70-17. (M) 2 L 7 2 4F RT A16WE 2001111300153 20011113 00153 NM 2001 11 13 USAA011331 1 20011017 A 5320 CLIP BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 46526 22959 PIT - FOUND SKIN CLIP CRACKED IN 3 PLACES, 1.75 INCH, TWO AT .5 INCH, ABOVE AND BELOW S14 AT STATION 727. CUT OUT DAMAG E AND INSTALLED STRINGER SPLICE REPAIR PER EA 72562. (M) 2 L 7 2 4F RT A16WE 2001111300154 20011113 00154 EU 2001 11 13 USAABA01011 1 20011020 A 3350 32146220 POWER SUPPLY AIRBUS 330 A330323 3930335 EU R2 DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 672UW 0333 PHL - EPSU AT THE R2 DOOR FAILS BATTERY CHECK. MAINTENANCE REPLACED THE EPSU. (M) 2 L 7 2 4F RT A46NM 2001111300155 20011113 00155 CE 2001 11 13 FD62001F00000 1 20010822 A 3340 24002544 STROBE BEECH 58 58P 1152744 CE CONT O520 TSIO520* 17040 SO CABIN BURNED OUT B FD6R D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 11 162Z TJ433 PRIOR TO ROLLOUT, PILOT ACTIVATED THE PULSELIGHT SWITCH. AS HE WAS ON ROLLOUT, THERE WAS SMOKE IN THE CABIN. PILOT ABO RTED TAKEOFF AND THE AIRCRAFT WAS TAKEN TO MAINTENANCE. THE TECH FOUND THE INSTALLATION NOT TO BE IAW THE STC INSTALLAT ION INSTRUCTIONS. (THERE WAS NO CIRCUIT BREAKER INSTALLED). MAINTENANCE INSTALLED THE PROPER CIRCUIT BREAKER, REPLACED T HE BURNED WIRES AND RETURNED THE AIRCRAFT TO SERVICE. 1 L 7 2 3O 3 O A23CE E8CE 2001111400012 20011114 00012 NM 2001 11 14 0103896306 1 20011031 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 666US 23821 DURING LINE CHECK, FOUND ZONE-D RIGHT SIDE AND ZONE-B LEFT SIDE EMERGENCY FLOOR PATH LIGHTS INOPERATIVE. REPAIRED FLOOR PATH LIGHTING. OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 2001111400024 20011114 00024 EU 2001 11 14 01FDEA00970 1 20011107 A 3260 WARNING LIGHT AIRBUS 300 A300F4605R 3930327 EU COCKPIT FALSE INDICATION A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 680FE 794 AFTER T/O GEAR DOOR IND UNSAFE SYS 1 & 2 FWD AND OVERHEAD PANEL, LOWERED GEAR IND SAFE, NOSE DOOR STILL SHOW UNSAFE. 2 L 7 2 4F RT A35EU 2001111600070 20011116 00070 WP 2001 11 16 01FDEA00971 1 20011107 A 7830 AVB7052503 HINGE DOUG DC10 DC1010 3022110 WP NR 2 T/R BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 054FE 47808 NR 2 ENGINE LEFT T/R CENTER HINGE ATTACH BEARING MIGRATED (PYLON HINGE ASSY BROKEN). REMOVED AND REPLACED HINGE BRACKET PER MM 78-32-11-2. 2 L 7 3 4F A22WE 2001111400025 20011114 00025 NM 2001 11 14 01FDEA00972 1 20011108 A 2751 INDICATOR BOEING 727 727233 138408A NM COCKPIT MALFUNCTIONED A FDEA L ABORTED APPROACH O OTHER AP APPROACH 1 SO 25 223FE 20935 REPEAT - OUTBOARD FLAPS STUCK AT 5 DEG UPON FLAP EXT. REMOVED AND REPLACED BOTH T/E FLAP IND AS PRECAUTION PER 27-52-02 1-2. 2 L 7 3 4F RT A3WE 2001111400030 20011114 00030 SO 2001 11 14 SWIA200110288 1 20011004 A 2730 CONTROL CABLE EMB 120 EMB120ER 3260203 SO ELEVATOR WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 218SW 120287 RIGHT INBOARD AND OUTBOARD ELEVATOR CABLES WORN FORWARD OF WING BOX. REPLACED RIGHT INBOARD AND OUTBOARD ELEVATOR CONTR OL CABLES IAW EMB120 MM 27-00-01. 2 L 7 2 4T RT A31SO 2001111400033 20011114 00033 SO 2001 11 14 SWIA200110289 1 20011004 A 5520 BUSHING EMB 120 EMB120ER 3260203 SO ELEVATOR WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 218SW 120287 RIGHT ELEVATOR OUTBOARD HINGE BUSHING WORN. REMOVED AND REPLACED RIGHT ELEVATOR OUTBOARD HINGE BEARING ASSEMBLY AND SHI MMED IAW MM 27-31-02. 2 L 7 2 4T RT A31SO 2001111400036 20011114 00036 SO 2001 11 14 SWIA200110290 1 20011004 A 5753 ROLLER EMB 120 EMB120ER 3260203 SO T/E FLAP WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 218SW 120287 REMOVE AND REPLACE ALL LEFT WING FLAP ROLLERS FOR WEAR. REMOVED AND REPLACED ALL LEFT WING FLAP ROLLERS IAW EMB120 MM 2 7-50-12. 2 L 7 2 4T RT A31SO 2001111400037 20011114 00037 SO 2001 11 14 SWIA200110291 1 20011004 A 5753 12033041003 FLAP TRACK EMB 120 EMB120ER 3260203 SO T/E FLAP WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 218SW 120287 LEFT INBOARD FLAP, INBOARD STATIONARY TRACK WORN. REPLACED LEFT INBOARD FLAP INBOARD STATIONARY TRACK. P/N: 120-33041 -003. 2 L 7 2 4T RT A31SO 2001111400038 20011114 00038 SO 2001 11 14 SWIA200110292 1 20011004 A 5753 BEARING EMB 120 EMB120ER 3260203 SO T/E FLAP WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 218SW 120287 LEFT OUTBOARD FLAP INBOARD BEARING ON MOVEABLE CHANNEL WORN. REPLACED OUTBOARD FLAP INBOARD BEARING. 2 L 7 2 4T RT A31SO 2001111400039 20011114 00039 SO 2001 11 14 SWIA200110293 1 20011004 A 2710 BEARING EMB 120 EMB120ER 3260203 SO AILERON WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 218SW 120287 LEFT AILERON QUADRANT ASSEMBLY WORN AT PIVOT PIN. REPLACED LEFT AILERON QUADRANT BEARINGS IAW EMB120 MM 27-11-05. 2 L 7 2 4T RT A31SO 2001111400040 20011114 00040 SO 2001 11 14 SWIA200110294 1 20011004 A 2752 LINK EMB 120 EMB120ER 3260203 SO FLAP ACTUATOR WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 218SW 120287 RIGHT OUTBOARD FLAP ACTUATOR ATTACHMENT LINK WORN. REPLACED ATTACHMENT LINK IAW 27-50-00. 2 L 7 2 4T RT A31SO 2001111400041 20011114 00041 SO 2001 11 14 SWIA200110295 1 20011004 A 2752 ROD END EMB 120 EMB120ER 3260203 SO FLAP ACTUATOR WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 218SW 120287 RIGHT NACELLE FLAP ACTUATOR ROD END WORN. REPLACED RIGHT NACELLE FLAP ACTUATOR ROD END IAW 27-50-08. 2 L 7 2 4T RT A31SO 2001111400042 20011114 00042 SO 2001 11 14 SWIA200110296 1 20011004 A 2711 5301 ACTUATOR EMB 120 EMB120ER 3260203 SO AILERON TAB WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 218SW 120287 RIGHT AILERON TRIM TAB ACTUATOR, ROD ATTACH FITTING SLOPPY/WORN AS MARKED. REMOVED AND REPLACED AILERON TRIM TAB ACTUAT OR WITH SERVICEABLE ACTUATOR IAW EMB120 MM 27-11-00. 2 L 7 2 4T RT A31SO 2001111400043 20011114 00043 SO 2001 11 14 SWIA200110297 1 20011004 A 5753 ROLLER EMB 120 EMB120ER 3260203 SO T/E FLAP WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 218SW 120287 REMOVE AND REPLACE ALL RIGHT WING FLAP ROLLERS FOR WEAR. REMOVED AND REPLACED ALL RIGHT WING FLAP ROLLERS IAW EMB120 MM 27-50-12. 2 L 7 2 4T RT A31SO 2001111400044 20011114 00044 SO 2001 11 14 SWIA200110298 1 20011004 A 5753 BEARING EMB 120 EMB120ER 3260203 SO T/E FLAP WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 218SW 120287 LEFT NACELLE FLAP INBOARD HINGE BEARING WORN. REPLACED HINGE ARM IAW 120 SRM 51-10-02, PAGE 3 SECTION 3A. 2 L 7 2 4T RT A31SO 2001111400045 20011114 00045 SO 2001 11 14 SWIA200110299 1 20011004 A 5753 RIVET EMB 120 EMB120ER 3260203 SO T/E FLAP LOOSE A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 218SW 120287 RIGHT NACELLE FLAP INBOARD BEARING ARM HAS LOOSE RIVETS. REMOVED AND REPLACED RIVETS IAW EMB120 SRM 51-40-02. 2 L 7 2 4T RT A31SO 2001111400049 20011114 00049 SO 2001 11 14 SWIA200110300 1 20011004 A 5751 BOSS EMB 120 EMB120ER 3260203 SO AILERON ELONGATED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 218SW 120287 LEFT AILERON 2ND FROM INBOARD END HINGE POINT ELONGATED. REPLACED BOSS IAW 120 SRM 51-10-02. 2 L 7 2 4T RT A31SO 2001111400053 20011114 00053 2001 11 14 SWIA200110301 4 20011026 A 3160 DISPLAY CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 407SW 7034 EICAS PRIMARY DISPLAY FAILED ON TAKEOFF ROLL ACCOMPANIED WITH AN EICAS COMP INOP MESSAGE. ABORTED TAKEOFF. REMOVED NR 1 PRIMARY EFD AND REPLACED IT WITH A SERVICEABLE ONE IAW CL600 MM 31-41-00. OPS CHECK GOOD. S/N ON: DN4T, S/N OFF: 9 64. 2 L 7 2 4F RT A21EA 2001111400056 20011114 00056 EA 2001 11 14 SWIA200110302 1 20011027 A 2740 70608 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB FAILED A SWIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 497SW 7482 STAB TRIM INOP STATUS MESSAGE ILLUMINATED DURING TAXI OUT. REMOVED AND REPLACED HSTCU IAW MM 27-41-01. OPS CHECK IAW M M 27-40-00-710-801. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2001111400058 20011114 00058 SO 2001 11 14 SWIA200110303 1 20011030 A 2460 RELAY EMB 120 EMB120ER 3260203 SO ELECTRICAL SYS FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 578SW 120346 WHEN CLIMBING TO ALTITUDE THE ELEC LIGHT ON MAP LIGHT UP AND EMERGENCY BUS OFF LIGHT CAME ON, ON THE OVERHEAD PANEL. EM ERGENCY BUS 2CB (F10) AND DC INDICATION NR 2 (G4) BOTH POPPED. ATTEMPTED ONE RESET AND SAME THING HAPPENED AGAIN. BOTH TIMES THE CB'S POPPED AS AIRCRAFT ENCOUNTERED TURBULENCE. DIVERTED TO SFO. INSPECTED OVERHEAD CB'S PANEL, LEFT AND RI GHT DC RELAY BOXES. NO DEFECT FOUND. REPLACED EMERGENCY DC BUS 2 OFF RELAY K0440. RESET CB'S. OPS CHECK GOOD ON ENGI NE RUN. UNABLE TO DUPLICATE DISCREPANCY. 2 L 7 2 4T RT A31SO 2001111400060 20011114 00060 SO 2001 11 14 SWIA200110304 1 20011029 A 3260 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 289YV 120289 LEFT MAIN LANDING GEAR INDICATED DOWN AND LOCKED AFTER GEAR RETRACTION. PERFORMED GEAR SWING. NO DEFECTS NOTED. 2 L 7 2 4T RT A31SO 2001111400062 20011114 00062 SO 2001 11 14 SWIA200110305 1 20011029 A 2752 3203001005 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 190SW 658 658 120050 CONTROL FAULT WOULD NOT RESET PER QRH. INBOARD FLAPS SHOWED 10 DEGREES. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATO R PER MM 27-50-00. OPS CHECK, LEAK CHECKS GOOD. 2 L 7 2 4T RT A31SO 2001111400063 20011114 00063 SO 2001 11 14 SWIA200110306 1 20011028 A 5310 WINDOW FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 218SW 120287 LEFT SIDE DV WINDOW FRAME IS CRACKED. COMPLIED WITH SB 120-53-0072 STEPS 2.1 THROUGH 2.7 - INSTALLATION OF NEW DOUBLERS AND REPLACEMENT RIVETS. 2 L 7 2 4T RT A31SO 2001111400064 20011114 00064 SO 2001 11 14 SWIA200110307 1 20011030 A 7722 SELOC19EG INDICATOR EMB 120 EMB120ER 3260203 SO COCKPIT FAULTY A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 217SW 120286 NR 2 ENGINE T6 INDICATOR FLUCTUATES AT TAKEOFF POWER SETTINGS. CAUSED ABORTED TAKEOFF. REPLACED RT ENGINE T-6 INDICATO R AND REPOSITIONED THE RIGHT ENGINE BLEED AIR LINE. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001111400065 20011114 00065 2001 11 14 SWIA200110308 4 20011028 A 3417 8220372140 ADC CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A SWIA O OTHER G MULTIPLE FAILURE CL CLIMB 1 NM 07 413SW 7102 EICAS NR 1 AND NR 2 BOTH FLICKERED OFF FOR APPROXIMATELY 1-2 MINUTES THEN CAME BACK ON. FMS GETS FMS NAV INVALID ON GRO UND. UNABLE TO GET COURSE UNTIL AIRCRAFT INFLIGHT. CAPTAIN'S PFD LOSES DATA AND LOTS OF DATA ON DISPLAY. DISPLAY BLAN KS ON TAKEOFF AND UNABLE TO GET FMS ENGINE TAKEOFF DATA UNTIL AIRBORNE (ON THRUST LIMITS PAGE). REMOVED AND REPLACED NR 1 ADC IAW CRJ MM 34-13-01. OPS AND LEAK CHECK GOOD. RAN EICAS 1 & 2 FOR SEVERAL HOURS, NO FLICKERING NOTED. 2 L 7 2 4F RT A21EA 2001111400070 20011114 00070 SO 2001 11 14 SWIA200110310 1 20011014 A 5320 BRACKET EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 299SW 120329 BRACKET AT FRAME 13 AFT OF DIRECT VISION WINDOW ON LEFT SIDE OF COCKPIT CRACKED. REPLACED BRACKET AT FRAME 13 AFT OF DV WINDOW ON LEFT SIDE OF COCKPIT IAW MM 53-00-00. 2 L 7 2 4T RT A31SO 2001111400074 20011114 00074 SO 2001 11 14 SWIA200110311 1 20011024 A 5243 DOOR EMB 120 EMB120ER 3260203 SO LT HYDRAULIC MISSING A SWIA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 NM 07 190SW 120050 LEFT HYDRAULIC DOOR MISSING. (DISCOVERED ON WALK AROUND INSPECTION.) FIT AND INSTALLED A NEW LEFT HYDRAULIC BAY DOOR I AW EMB SRM 51-00-00 AND 51-40-02. 2 L 7 2 4T RT A31SO 2001111400077 20011114 00077 2001 11 14 SWIA200110312 4 20011014 A 2350 1621BMOD1 CONNECTOR EMB 120 EMB120ER 3260203 SO COMM ANTENNA CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 299SW 120329 CORROSION FOUND INSIDE CO-AX CONNECTOR OF COMM NR 2 ANTENNA. ANTENNA REQUIRES REPLACEMENT. REPLACED NR 2 COMM ANTENNA WITH NEW SERVICEABLE ANTENNA. ALL WORK CONFORMS TO MM REMOVAL AND REPLACEMENT INSTRUCTIONS CHAPTER 34-55-01. P/N OFF: 16-21B MOD 1 S/N OFF: 10443. 2 L 7 2 4T RT A31SO 2001111400078 20011114 00078 SO 2001 11 14 SWIA200110313 1 20011014 A 2710 CONTROL CABLE EMB 120 EMB120ER 3260203 SO AILERON WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 299SW 120329 AILERON CABLES WORN. REPLACED AILERON CABLES WITH TIN CARBON STEEL CABLE PER EMB120 MM 27-00-01. 2 L 7 2 4T RT A31SO 2001111400079 20011114 00079 2001 11 14 SWIA200110314 4 20011102 A 3425 6226190204 COMPUTER EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING I J FLT. ATTITUDE INST. WARNING INDICATION CL CLIMB 1 NM 07 268UE 120207 AFTER TAKEOFF CAPTAIN'S AHRS DISPLAY DISAPPEARED, ATTITUDE DISPLAY ALERT ILLUMINATED WITH CHIME HEADING AND ROLL FLAGS A PPEARING ON BOTH SIDES. THIS REOCCURRED AFTER RESET ATTITUDE DISPLAY. REPLACED RELAYS K0395 AND K0397, 10 MIN BACK UPF USE AND REPLACED NR 1 AHRS AHC85. TESTED SYSTEM IAW 34-00-00. NR 1 AHRS TEST GOOD. 2 L 7 2 4T RT A31SO 2001111400081 20011114 00081 SO 2001 11 14 SWIA200110315 1 20011102 A 2752 3203001005 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP FAILED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 NM 07 268UE 120207 WHEN FLAPS 45 IS SELECTED OUTBOARDS DO NOT COME DOWN UNTIL TOUCHDOWN CAUSING DISAGREEMENT. REPLACED RIGHT OUTBOARD FLAP ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-50-00. S/N OFF: 0400. 2 L 7 2 4T RT A31SO 2001111400082 20011114 00082 EA 2001 11 14 SWIA200110316 1 20011101 A 2740 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB FAULTY A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 497SW 7482 STAB TRIM CH1 INOP MESSAGE INFLIGHT - WAS ABLE TO RESET, BUT CONTINUES TO FAIL EVERY FEW MINUTES; IE, FAILED 7 TIMES IN 20 MINUTES. REMOVED AND REPLACED HSTA AND MOTOR CONTROL UNIT IAW 27-42-01. OPS CHECK GOOD. AIRCRAFT RETURNED TO CAT I I STATUS. HSTA P/N: 8396-3 S/N ON: 311 S/N OFF: 555. 2 L 7 2 4F RT A21EA 2001111400083 20011114 00083 SO 2001 11 14 SWIA200110317 1 20011103 A 3297 12022622501 HARNESS EMB 120 EMB120ER 3260203 SO RT MLG FAULTY A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 190SW 120050 AFTER GEAR RETRACTION, RIGHT MAIN GEAR B-GREEN LIGHT REMAINS ILLUMINATED WITH ALL OTHER LIGHTS OUT. RECYCLED GEAR WITH SAME RESULT. B-GREEN LIGHT DID FINALLY GO OUT 10 MINUTES AFTER SECOND GEAR RETRACTION. REPLACED RIGHT MLG PROXIMITY HA RNESS-B IAW 32-61-01. GEAR CYCLED THREE TIMES. OPS CHECK GOOD. P/N: 120-22622-501, S/N ON: T02148, S/N OFF: A00571 0710. 2 L 7 2 4T RT A31SO 2001111400084 20011114 00084 NM 2001 11 14 P2EA2001M0010 1 20011110 A 8012 2730426 START VALVE BOEING 737 73725A 1384481 NM NR 1 ENGINE FAILED A P2EA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 05 239TA 23789 NR 1 ENGINE START VALVE WOULD NOT OPEN. AIRCRAFT RETURNED TO GATE. REMOVED AND REPLACED START VALVE IAW MM 80-11-21. OPE RATIONAL CHECK NORMAL. 2 L 7 2 4F RT A16WE 2001111400085 20011114 00085 SO 2001 11 14 SWIA200110318 1 20011104 A 3230 SEQUENCE VALVE EMB 120 EMB120ER 3260203 SO NLG WW MALFUNCTIONED A SWIA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NM 07 269UE 120207 LANDING GEAR WOULD NOT COME DOWN AFTER SELECTING GEAR LEVER DOWN. ALL RED A & B LIGHTS, EXCEPT LEFT MAIN A LIGHT, STAYE D ON. LT MAIN GREEN A LIGHT WAS ALSO ILLUMINATED. ON THE GO-AROUND THE GEAR EXTENDED AND GOT NORMAL GREEN LIGHTS EXCEP T LEFT MAIN A LIGHT REMAINED OFF FOR ABOUT 10 SECONDS. UPDATE 11/5: ON APPROACH SELECTED GEAR DOWN WITH NO RESPONSE. GEAR DOORS REMAINED CLOSED. STARTED TO FOLLOW QRH PROCEDURE, ELECTRICAL OVERRIDE, WHEN GEAR FINALLY CAME DOWN. REMOVED AND REPLACED LANDING GEAR CONTROL BOX WITH SERVICEABLE UNIT. OPS CHECK GOOD. UPDATE: 11/5: REMOVED AND REPLACED SE QUENCE VALVE IN NOSE BAY. SYSTEM OPS CHECK GOOD AS PER EMB MM 32-30-00. 2 L 7 2 4T RT A31SO 2001111400086 20011114 00086 SO 2001 11 14 SWIA200110319 1 20011014 A 5320 BRACKET EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 299SW 120329 UPPER BRACKET FORWARD OF FRAME 9 IS CRACKED ON LEFT AND RIGHT SIDES OF COCKPIT. ELIMINATED SHEAR CLIPS AND CUT END OF L EFT AND RIGHT FRAME 9 CHANNEL PER SB 120-53-0073. 2 L 7 2 4T RT A31SO 2001111400087 20011114 00087 SO 2001 11 14 SWIA200110320 1 20011028 A 3397 CONNECTOR EMB 120 EMB120ER 3260203 SO CABIN DISCONNECTED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 218SW 120287 FOUR EMERGENCY EXIT FLOOR LIGHTS INOP. RECONNECTED FLOOR EMERGENCY LIGHTING CONNECTOR. 2 L 7 2 4T RT A31SO 2001111400088 20011114 00088 SO 2001 11 14 SWIA200110321 1 20011108 A 3260 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO LT MLG OUT OF ADJ A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 296SW 120325 AFTER TAKEOFF LEFT MAIN GEAR RED LIGHTS WON'T EXTINGUISH. COULD FEEL GEAR NOT RETRACTING. FOLLOWED QRH PROCEDURES AND RECYCLED WITH SAME RESULTS. ADJUSTED LEFT MAIN LANDING GEAR PROXIMITY SENSOR. CYCLED GEAR SEVERAL TIMES. SYSTEM OPS C HECK GOOD. 2 L 7 2 4T RT A31SO 2001111400089 20011114 00089 2001 11 14 SWIA200110322 4 20011031 A 3425 6226190204 COMPARATOR EMB 120 EMB120ER 3260203 SO COCKPIT FAILED A SWIA O OTHER I FLT. ATTITUDE INST. CR CRUISE 1 NM 07 226SW 102 102 120296 CAPTAIN'S EHSI/ADI COMPLETE FAILURE IN FLIGHT. REMOVED AND REPLACED AHC-85 CAPTAIN'S SIDE (NR 1). OPS CHECKS GOOD PER MM 34-21-01 & 34-21-00. 2 L 7 2 4T RT A31SO 2001111400090 20011114 00090 SO 2001 11 14 SWIA200110323 1 20011022 A 2897 WIRE EMB 120 EMB120ER 3260203 SO LT WING DAMAGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 565SW 120340 VENT VALVE WIRING LINE INSIDE FUEL TANK NEAR LEFT WING TIP HAS DAMAGE. REPLACED LEFT VENT VALVE WIRING LINE ASSY. 2 L 7 2 4T RT A31SO 2001111400091 20011114 00091 SO 2001 11 14 SWIA200110324 1 20011010 A 3411 PITOT TUBE EMB 120 EMB120ER 3260203 SO LT & RT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 297SW 120327 LEFT AND RIGHT PITOT TUBES EXCESSIVELY CORRODED. REPLACED PITOT/STATIC TUBES IAW MM 34-11-01. TESTED GOOD IAW 34-11-00 (LEAK CHECK, OP CHECK). VERIFIED HEATER OPERATIONAL. P/N: 856NF, 85NB1 S/N: 159057, 165026. 2 L 7 2 4T RT A31SO 2001111400092 20011114 00092 SO 2001 11 14 SWIA200110325 1 20011010 A 2730 CONTROL CABLE EMB 120 EMB120ER 3260203 SO ELEVATOR WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 297SW 120327 RIGHT OUTBOARD AND INBOARD ELEVATOR CABLES ARE WORN AT REAR PRESSURE BULKHEAD. REMOVED AND REPLACED RIGHT SIDE ELEVATOR CABLES WITH A SERVICEABLE CABLES IAW MM 27-00-01. 2 L 7 2 4T RT A31SO 2001111400097 20011114 00097 SO 2001 11 14 SWIA200110326 1 20011010 A 5320 12006158002 SILL EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 297SW 120327 BUTT STRAP BETWEEN FRAMES 39-44 HAS LARGE AMOUNT OF CORROSION AND NEED REPLACED ON RIGHT SIDE (SILL). REPLACED SILL WIT H A NEW PART IAW EMB SRM 51-00-00 AND 51-40-02. P/N: 120-06158-002. 2 L 7 2 4T RT A31SO 2001111400100 20011114 00100 SO 2001 11 14 SWIA200110327 1 20011010 A 5320 12046163001 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 297SW 120327 BUTT STRAP ON LEFT SIDE HAS LARGE AMOUNT OF CORROSION AND NEEDS REPLACED BETWEEN FRAMES 34-38. FABRICATED AND INSTALLED BUTT STRAP BETWEEN FRAMES 34-38 IAW SRM 51-00-00 AND 51-40-02. P/N: 120-46163-001. 2 L 7 2 4T RT A31SO 2001111400101 20011114 00101 SO 2001 11 14 SWIA200110328 1 20011010 A 5320 12046163001 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 297SW 120327 BUTT STRAP BETWEEN FRAMES 34-38 ON RIGHT SIDE NEEDS REPLACED DUE TO A LARGE AMOUNT OF CORROSION. REMOVED AND REPLACED B UTT STRAP BETWEEN FRAMES 34-38 IAW SRM 51-00-00 AND 51-40-02. P/N: 120-46163-001. 2 L 7 2 4T RT A31SO 2001111400102 20011114 00102 SO 2001 11 14 SWIA200110329 1 20011010 A 5320 12046163003 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 297SW 120327 BUTT STRAP RIGHT SIDE BETWEEN FRAMES 30-34 HAS LARGE AMOUNTS OF CORROSION AND NEEDS REPLACED. INSTALLED NEW BUTT STRAP IAW SRM 51-00-00 AND 51-40-02. P/N: 120-46163-003. 2 L 7 2 4T RT A31SO 2001111400103 20011114 00103 SO 2001 11 14 SWIA200110330 1 20011010 A 5320 27929001 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 297SW 120327 BUTT STRAP CENTER BETWEEN FRAMES 34-38 HAS LARGE AMOUNTS OF CORROSION AND NEEDS REPLACED. REMOVED AND REPLACED BUTT STR AP BETWEEN FRAMES 34-38 IAW SRM 51-00-00 AND 51-40-02. P/N: 27929-001. 2 L 7 2 4T RT A31SO 2001111400104 20011114 00104 SO 2001 11 14 SWIA200110331 1 20011010 A 2710 CONTROL CABLE EMB 120 EMB120ER 3260203 SO AILERON WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 297SW 120327 RIGHT AILERON UPPER AND LOWER CABLES WORN. REMOVED AND REPLACED RIGHT UPPER AND LOWER AILERON CABLES IAW MM 27-00-01. 2 L 7 2 4T RT A31SO 2001111400105 20011114 00105 SO 2001 11 14 SWIA200110332 1 20011010 A 2711 CONTROL CABLE EMB 120 EMB120ER 3260203 SO AILERON TRIM WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 297SW 120327 AILERON TRIM CABLES WORN AT RIGHT NACELLE FEED THROUGH. REMOVED AND REPLACED TRIM CABLES FROM TRIM KNOB TO AILERON TRIM ACTUATOR IAW EMB MM 27-12-00 AND RII 27-301. 2 L 7 2 4T RT A31SO 2001111400106 20011114 00106 SO 2001 11 14 SWIA200110333 1 20011010 A 2710 CONTROL CABLE EMB 120 EMB120ER 3260203 SO AILERON WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 297SW 120327 LEFT AILERON CABLES UPPER AND LOWER AT NACELLE WORN. REMOVED AND REPLACED LEFT UPPER AND LOWER AILERON CABLES WITH SERV ICEABLE CABLES IAW MM 27-00-01. 2 L 7 2 4T RT A31SO 2001111400107 20011114 00107 SO 2001 11 14 SWIA200110334 1 20011022 A 2710 CONTROL CABLE EMB 120 EMB120ER 3260203 SO AILERON WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 565SW 120340 UPPER AND LOWER AILERON CABLES WORN AT INBOARD NACELLE FAIRLEADS, RIGHT SIDE. REPLACED RIGHT UPPER AND LOWER AILERON CA BLES IAW EMB120 MM 27-00-01. 2 L 7 2 4T RT A31SO 2001111400108 20011114 00108 SO 2001 11 14 SWIA200110335 1 20011022 A 2711 CONTROL CABLE EMB 120 EMB120ER 3260203 SO AILERON TAB WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 565SW 120340 UPPER AND LOWER AILERON TRIM CABLES WORN ON RIGHT SIDE. REPLACED RIGHT UPPER AND LOWER AILERON TRIM CABLES IAW EMB120 M M 27-00-01. 2 L 7 2 4T RT A31SO 2001111400109 20011114 00109 SO 2001 11 14 SWIA200110336 1 20011022 A 2710 CONTROL CABLE EMB 120 EMB120ER 3260203 SO AILERON WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 565SW 120340 LEFT AILERON UPPER AND LOWER CABLES WORN ON WING. REPLACED LEFT UPPER AND LOWER AILERON CABLES IAW EMB120 MM 27-00-01. 2 L 7 2 4T RT A31SO 2001111400110 20011114 00110 SO 2001 11 14 SWIA200110337 1 20011022 A 2720 CONTROL CABLE EMB 120 EMB120ER 3260203 SO RUDDER WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 565SW 120340 RIGHT RUDDER INBOARD AND OUTBOARD CABLES FORWARD OF THE WING BOX IS WORN NEAR LIMITS. REPLACED RIGHT RUDDER INBOARD AND OUTBOARD CABLES FORWARD OF WING BOX IAW EMB120 MM 27-00-01. 2 L 7 2 4T RT A31SO 2001111400111 20011114 00111 SO 2001 11 14 SWIA200110338 1 20011022 A 2720 CONTROL CABLE EMB 120 EMB120ER 3260203 SO RUDDER WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 565SW 120340 LEFT OUTBOARD RUDDER CABLE IN AFT RIGGING BAY IS WORN NEAR LIMITS. REPLACED LEFT OUTBOARD RUDDER AFT CABLE IAW EMB120 M M 27-00-01. 2 L 7 2 4T RT A31SO 2001111400112 20011114 00112 SO 2001 11 14 SWIA200110339 1 20011104 A 3233 2060500005 ACTUATOR EMB 120 EMB120RT 3260202 SO NLG FAILED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 1105G 120105 NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED NOSE GEAR RETRACTION ACTUATOR. SWUNG GEAR CHECK GOOD. LEAK CHECK GOOD. 2 L 7 2 4T RT A31SO 2001111400116 20011114 00116 EU 2001 11 14 MALA010770 1 20011109 A 3230 HTE94904 LANDING GEAR BAC 146 AVRO146RJ85A 1500097 EU A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 526XJ E2351 After Takeoff on Flight #3557, Red gear intransit light illuminated, also light in Gear Handle tried to recycle, unsucce ssful. Light went out after 30 minutes. Flight diverted to DTW due to full load, repair and spare. Maintenance remove d and repaired Landing Gear Selector Valve PN HTE9490-4. All work done IAW RJ85 MM 32-20. All checks good at this time . 2 H 7 4 4F RT A49EU 2001111400119 20011114 00119 SO 2001 11 14 C2XA01CL228 1 20011112 A 2742 3622001011 ACTUATOR EMB 135 EMB135ER 3260203 SO TAIL FAILED A C2XA A B UNSCHED LANDING EMER. DESCENT F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 27 16502 4798 1096 145166 MSN FLIGHT#3110 THE CREW REPORTED THE HORIZONTAL STABILIZER PITCH TRIM FAILED AFTER TAKEOFF.THE CREW DECLARED AN EMERGEN CY AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE REPLACED THE HORIZONTAL STABILIZER PITCH TRIM ACTUATOR AND THE HORIZO NTAL STABILIZER CONTROL UNIT.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.HORIZONTAL STAB CONTROL UNIT P/N 362100-1007 S/N 1207 TOTAL TIME:4724 CSN:4448 2 L 7 2 4F RT T00011AT 2001111400120 20011114 00120 SO 2001 11 14 COMA0110156 1 20011112 A 3350 D36604001 BATTERY EMB 120 EMB120RT 3260202 SO CABIN DISCHARGED A COMA O OTHER H ELECT. POWER LOSS-50 PC IN INSP/MAINT 1 SO 01 264CA 14351 120256 FLIGHT #5044. EMERGENCY LIGHTS ARE INOP.REPLACED THE EMERGENCY LIGHTS BATTERY. 2 L 7 2 4T RT A31SO 2001111400123 20011114 00123 EA 2001 11 14 COMA0160887 1 20011113 A 5346 WEB CNDAIR CL600 CL6002B19 1900309 EA AFT EQUIPMENT BA CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 945CA 15092 7069 ENGINE SUPPORT BEAM UPPER PLATE AT RBL3 HAS A CRACK GOING FROM THE AFT EDGE INTO A RIVET HOLE.PERFORMED A TEMPORARY MAJO R REPAIR TO CENTER ENGINE SUPPORT BEAM I/A/W CRJ REO 601R-53-61-345 REV B. 2 L 7 2 4F RT A21EA 2001111400124 20011114 00124 EA 2001 11 14 COMA0160888 1 20011111 A 2750 854D100MD101 ACTUATOR CNDAIR CNDAIR CL600 CL6002B19 1900309 EA R/H #4 OUT OF TOLERANCE A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 932CA 13472 SBRJ039 7038 FLIGHT #5039. FLAPS FAIL MESSAGE WHEN SELECTED FOR LANDING.R/H OUTBD FLAP FOUND TWISTED - REPLACED THE FLAP, BOTH ACTUAT ORS AND THE FLEX DRIVE CABLES. 2 L 7 2 4F RT A21EA 2001111400128 20011114 00128 2001 11 14 COMA0160889 4 20011110 A 3140 6229820008 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA C ABORTED TAKEOFF F N FLT CONT AFFECTED FALSE WARNING TO TAKEOFF 1 SO 01 721CA 1245 7259 FLIGHT #5625 - CONFIG AILERON WARNING DURING T/O.REPLACED THE #2 DCU. 2 L 7 2 4F RT A21EA 2001111400129 20011114 00129 EA 2001 11 14 COMA0160890 1 20011110 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA D RETURN TO BLOCK S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 932CA 7038 FLIGHT #5318 FLAPS FAILED WHEN SELECTED TO 20 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2001111400130 20011114 00130 EA 2001 11 14 COMA0160891 1 20011111 A 2750 852D10011 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA R/H #1 OUT OF TOLERANCE A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 977CA 3086 7157 FLIGHT #6016 FLAPS FAIL CAUTION MESSAGE WHEN FLAP SELECTED UP AFTER T/O.REPLACED THE R/H #1 FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2001111400131 20011114 00131 SO 2001 11 14 SWIA200110340 1 20011108 A 3231 12032943001 SEQUENCE VALVE EMB 120 EMB120ER 3260203 SO RT MLG STICKS A SWIA O OTHER F J E FLT CONT AFFECTED WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 NM 07 234SW 120308 ON GEAR RETRACTION FROM MTJ, RIGHT SIDE A & B LIGHTS (RED) STAYED ILLUMINATED WITH NOISE AND VIBRATION. CYCLED THE GEAR AND PROBLEM WENT AWAY SHORTLY THEREAFTER. F/O WAS ABLE TO SEE AFT OUTBOARD GEAR DOOR DOWN DURING THE PROBLEM. SWUNG G EAR, UNABLE TO DUPLICATE. FOUND RIGHT INBOARD SEQUENCE VALVE STICKING. REPLACED VALVE. SWUNG GEAR. OPS CHECK GOOD. NO LEAKS NOTED. 2 L 7 2 4T RT A31SO 2001111600099 20011116 00099 EA 2001 11 16 COMA0160886 1 20011114 A 7120 601370102 MOUNT CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 926CA 18780 7027 DURING ENGINE CHANGE FOUND CORROSION/FRETTING ON RIGHT ENGINE THRUST MOUNT FITTING FROM 12 O'CLOCK POSITION, TO 6 O'CLOC K POSITION. REPAIRED DAMAGE PER REO 601R-54-50-034. RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2001111400132 20011114 00132 SO 2001 11 14 SWIA200110341 1 20011107 A 3260 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO LT MLG OUT OF ADJ A SWIA A UNSCHED LANDING F J E FLT CONT AFFECTED WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 NM 07 296SW 120325 AFTER TAKEOFF LEFT MAIN GEAR RED LIGHTS WON'T EXTINGUISH. COULD FEEL GEAR NOT RETRACTING. FOLLOWED QRH, RECYCLED - SAM E RESULT. ADJUSTED LEFT GEAR PROXIMITY SENSOR. CYCLED GEAR SEVERAL TIMES. SYSTEM OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001111400133 20011114 00133 SO 2001 11 14 SWIA200110342 1 20011109 A 3230 12043270501 CONTROL BOX EMB 120 EMB120ER 3260203 SO LANDING GEAR MALFUNCTIONED A SWIA A UNSCHED LANDING F J E FLT CONT AFFECTED WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 NM 07 268UE 120207 AFTER TAKEOFF SELECTED GEAR UP, ALL LIGHTS A & B, GREEN & RED ILLUMINATED AND LANDING GEAR STAYED IN DOWN POSITION. REC YCLED GEAR HANDLE 10 TIMES WITH NO RETRACTION. RETURNED TO RDM. INSPECTED LANDING GEAR WITH NO DAMAGE TO GEAR NOTED. REMOVED FLAGS AND INSTALLED GEAR SAFETY PINS AND SAFETIED INTO POSITION. SAFE FOR FLIGHT. FERRIED TO SEA. REMOVED AND REPLACED LANDING GEAR RELAY BOX IAW MM 32-31-02. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001111400134 20011114 00134 SO 2001 11 14 SWIA200110343 1 20011102 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 186SW 1411 1411 120034 THREE CONSECUTIVE WHITE EMERGENCY LIGHTS (ROW 3-6), 1 RED FLOOR EMERGENCY LIGHT OUT AT ROW 6, 4 EXIT SIGNS AT ROW 6 OUT, 2 OVERHEAD WHITE EXIT LIGHTS OUT AT ROW 6. INSTALLED SERVICEABLE ELBP IN MID EMERGENCY LIGHT SECTION IAW MM 33-50-00. CHECKS GOOD. 2 L 7 2 4T RT A31SO 2001111400135 20011114 00135 SO 2001 11 14 SWIA200110344 1 20011108 A 3020 16321 TIMER EMB 120 EMB120ER 3260203 SO LT ENGINE MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 190SW 120050 LEFT ENGINE AIR INLET FAILED 14 MINUTES INTO FLIGHT PASSING THROUGH FL180. TURNED OFF FOR A FEW MINUTES AND THEN ON FOR ANOTHER 14 MINUTES DURING RETURN TO SLC AND IT DID NOT FAIL AGAIN. REMOVED AND REPLACED LEFT ENGINE DEICE TIMER IAW MM 30-20-05. REMOVED AND REPLACED DEICE MONITOR IAW MM 30-00-01. OPS CHECK GOOD. DE-ICE MONITOR P/N 0552-01-001, S/N O FF 132/10-87. 2 L 7 2 4T RT A31SO 2001111400136 20011114 00136 SO 2001 11 14 SWIA200110345 1 20011022 A 2720 CONTROL CABLE EMB 120 EMB120ER 3260203 SO RUDDER WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 565SW 120340 RIGHT INBOARD RUDDER CABLE IN AFT RIGGING BAY IS WORN NEAR LIMITS. REPLACED RIGHT INBOARD AFT RUDDER CABLE IAW EMB120 M M 27-00-0. 2 L 7 2 4T RT A31SO 2001111400137 20011114 00137 SO 2001 11 14 SWIA200110346 1 20011022 A 2730 CONTROL CABLE EMB 120 EMB120ER 3260203 SO ELEVATOR WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 565SW 120340 LEFT INBOARD AND OUTBOARD ELEVATOR CABLES IN AFT RIG BAY ARE WORN NEAR LIMITS. REPLACED LEFT INBOARD AND OUTBOARD AFT E LEVATOR CABLES IAW EMB120 MM 27-00-01. P/N: 120-27655-017. 2 L 7 2 4T RT A31SO 2001111400138 20011114 00138 SO 2001 11 14 SWIA200110347 1 20011022 A 2730 CONTROL CABLE EMB 120 EMB120ER 3260203 SO ELEVATOR WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 565SW 120340 RIGHT INBOARD AND OUTBOARD ELEVATOR CABLES IN AFT RIG BAY ARE WORN NEAR LIMITS. REPLACED RIGHT INBOARD AND OUTBOARD AFT ELEVATOR CABLES IAW EMB120 MM 27-00-01. 2 L 7 2 4T RT A31SO 2001111400139 20011114 00139 SO 2001 11 14 SWIA200110348 1 20011022 A 2720 CONTROL CABLE EMB 120 EMB120ER 3260203 SO RUDDER WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 565SW 120340 RIGHT RUDDER AFT OUTBOARD CABLE WORN. REPLACED RIGHT AFT OUTBOARD RUDDER CABLE IAW EMB120 MM 27-00-01. 2 L 7 2 4T RT A31SO 2001112700089 20011127 00089 NM 2001 11 27 UPS01237265 1 20011110 A 5230 STOP FITTING BOEING 727 72731C 1384011 NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:N/A AFT CARGO DOOR AFT NR 1 STOP FITTING CRACKED. AFT CARGO DOOR NR 1 STOP FITTING REPLACED IAW EO B727 -5230-0032 APP C AND DRAWING 65-18625. 2 L 7 3 4F A3WE 2001111400150 20011114 00150 WP 2001 11 14 IXXA0100071O 1 20011110 A 2610 CONNECTOR DOUG DC8 DC871F 302199D WP ENGINE DEFECTIVE A IXXA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 SW 11 826BX 83918 1806 45998 ENROUTE FROM TOL TO BFI, ON DESCENT THE NUMBER FOUR ENGINE FIRE WARNING SHORT CIRCUIT LIGHT ILLUMINATED. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND SECURED THE ENGINE. THE FLIGHT CONTINUED TO BFI FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE ENGINE WITH NO EVIDENCE OF A FIRE. FURTHER INVESTIGATION REVEALED A DEFECTIVE ELECTRICAL CONNECTOR ON THE SENSING ELEMENT AND WAS REPLACED. MAINTENANCE PERFORMED A SUCCESFUL OPERATIONAL TEST IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2001111400151 20011114 00151 NM 2001 11 14 UPS01437257 1 20011105 A 3350 LIGHT BOEING 747 747200 1384847 NM CABIN INTERMITTENT A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:N/A RIGHT EMERGENCY LIGHT JUST AFT OF COCKPIT DOOR INTERMITTENT. REMOVED AND REPLACED LIGHT, OPS CHECK GOOD PER 33-51-07. 2 L 7 4 4F RT A20WE 2001111400153 20011114 00153 NM 2001 11 14 UPS01437272 1 20011101 A 5310 FRAME BOEING 747 747200 1384847 NM NOSE WHEEL WELL CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C R/H BS 300 NOSE WHEEL WELL FRAME CRACK FOUND AT WEB 4EA FASTENER HOLES, PLS REFER ATT FIG. R/H BS 300 NOSE WHEEL WELL STR R 39 TO R 41 FRAME CRACKED AREA REPAIRED AS PER SRM 51-40-03 FIG 1. 2 L 7 4 4F RT A20WE 2001111400154 20011114 00154 NM 2001 11 14 UPS01437273 1 20011101 A 5310 FRAME BOEING 747 747200 1384847 NM NOSE W/W CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C L/H BS 300 NOSE WHEEL WELL FRAME CRACK FOUND AT WEB 2EA FASTENER HOLES, PLS REFER ATT FIG. LH BS 3 00 WHEEL WELL FRAME AT STR L 39 TO STR L 41 CRACKED AREA REPAIRED AS PER SRM 51-40-03 FIG 1. 2 L 7 4 4F RT A20WE 2001111400155 20011114 00155 NM 2001 11 14 UPS01437274 1 20011106 A 5310 141U11076 WEB BOEING 747 747200 1384847 NM RH SIDE NWW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C R/H SIDE NWW ON BS 300 VERTICAL BEAM WEB FOUND CRACKED AT #5 CLIP ( COUNTED FROM TOP ) ATTACHED FASTEN ER HOLE, THE MOST I/B FASTENER HOLE, APPROX 3/16" IN LENGHT AS MARKED. WEB REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F RT A20WE 2001111400156 20011114 00156 NM 2001 11 14 UPS01437275 1 20011101 A 5310 141U11074 WEB BOEING 747 747200 1384847 NM RH SIDE NWW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C R/H SIDE NWW AT BS 320 VERTICAL BEAM WEB FASTENER 1EA COMMON TO THE INNER CHORD CRACKED JUST BETWEEN # 5 AND #6 STIFFENER ( COUNTED FROM TOP ) AS MARKED. R/H NOSE WHEEL WELL BS 320 VERTICAL BEAM WEB REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F RT A20WE 2001111400157 20011114 00157 NM 2001 11 14 UPS01437278 1 20011101 A 5310 141U11073 WEB BOEING 747 747200 1384847 NM LH SIDE NWW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C L/H SIDE NWW AT BS 320 VERTICAL BEAM WEB FOUND ONE EACH STAND OFF HOLE CRACKED, JUST BETWEEN 31 AND #2 STIFFENER ( COUNTED FROM TOP ) AS MAKRED. REF NRC GJ58782 VERTICAL WEB REPLACED AS PER SRM 51-30-02. 2 L 7 4 4F RT A20WE 2001111400163 20011114 00163 NM 2001 11 14 UPS01437263 1 20011108 A 3350 LIGHT BOEING 747 747121 1384871 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:PFLT CREW SERVICE DOOR CEILING EMERGENCY LIGHT INOP. REMOVED AND REPLACED CEILING EMERGENCY LIGHT ASSY IAW B747 MM 33-51- 07, OPS CHECKS GOOD. 2 L 7 4 4F A20WE 2001112100135 20011121 00135 NE 2001 11 21 UPS01437264 2 20011110 A 7200 ENGINE BOEING 747 747121 1384871 NM PWA JT9 JT9D7AH 52054 NE NR 4 FAILED A IPXA E ENGINE SHUTDOWN A FLAME/FIRE CL CLIMB 1 SO 01 681UP 19661 662243 INSPECTION TYPE:N/A DURING CLIMBOUT, THE NR 4 ENG SURGED LOUDLY AND VIOLENTLY MULTIPLY TIMES WITH VISIBLE FLAMES SHOOTIN G OUT OF THE INLET. YAW ASSOCIATED WITH SURGES. OIL TEMP READ OVER 135 EGT 946 OIL QUANTITY 5.3, N2, 18 PERCENT. RAN CHECKLISTS AT TOD, HAD 10 PSI OIL QTY 5.3 NR 4 EDP SELECTED TO SUPPLY OFF AT AROUND 1135 WINDMILLED FOR 17 MINUTES. LAN DING UNEVENTFUL. REPLACED NR 4 ENGINE IAW TASK CARD NR 5000. ENG S/N ON 662410, ENG S/N OFF P610981. 2 L 7 4 4F 4 F A20WE E20EA 2001111400164 20011114 00164 NM 2001 11 14 UPS01537259 1 20011107 A 5610 LINK BOEING 757 75724APF 1384969 NM SLIDING WINDOW OUT OF ADJ A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 434UP 25465 INSPECTION TYPE:PFLT CAPT L2 EMERGENCY EXIT WINDOW VERY DIFFICULT TO OPEN. RELEASE LEVER JAMS ABOUT HALF WAY BACK. ADJU STED LINK ARM PER MM 56-11-02 REF FIG 504 WINDOW OPS CHECKS GOOD. 2 L 7 2 4F RT A2NM 2001111400165 20011114 00165 WP 2001 11 14 UPS01837247 1 20011014 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 L-2 DOOR FWD LOWER CORNER FUSELAGE SKIN AND INTERNAL DOUBLER ARE CRACKED AT STA 1620 AT LONG 21L, AND EXISTING DOUBLER DOES NOT CONFORM TO THE SRM. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS. FABRICATED AND INSTALLED FILLER S, DOUBLER AND TRIPLER IAW 8110-3 APPROVED DH SK 718-700. 2 L 7 4 4F RT 4A25 2001111400166 20011114 00166 WP 2001 11 14 UPS01837248 1 20011015 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 L-1 DOOR FWD UPPER CORNER DOUBLER DOES NOT CONFORM TO THE SRM AND SKIN IS CRACKED AT STA 30 LONG 10L. REMOVED EXISTING DOUBLER AND CUT OUT DAMAGE, NDT VERIFIED NO CRACKS. FABRICATED AND INSTALLED FILLER, DOUBLER AND TRI PLER IAW 8110-3 APPROVED DH SK 718-779. 2 L 7 4 4F RT 4A25 2001111400167 20011114 00167 WP 2001 11 14 UPS01837250 1 20011017 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 LONG 35L IS CORRODED BEYOND LIMITS BETWEEN STA 1380 TO 1400. CUT OUT DAMAGED LONGERON SECTION, FABRI CATED AND SPLICED IN SECTION OF LONGERON IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2001111400168 20011114 00168 WP 2001 11 14 UPS01837251 1 20011017 A 5320 WEB DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 RT UPPER CUSP IS CORRODED BEYOND LIMITS STA 1000-1110 LONG 21R. REMOVED, FABRICATED, AND REPLACED SE CTION OF CUSP FROM STA 1080-1110 IAW SRM 53-2-5 FIG 15. 2 L 7 4 4F RT 4A25 2001111400169 20011114 00169 WP 2001 11 14 UPS01837253 1 20011017 A 5350 5704650111 DOUBLER DOUG DC8 DC871F 302199D WP TAIL CONE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 TAIL CONE INNER DOUBLER AT 62 ACCESS HOLE, AND LT OUTER SKIN IS CORRODED BEYOND LIMITS STA 1861-1890 APPROX. REMOVED, FABRICATED, AND REPLACED DOUBLER AND SKIN SECTION IAW DWG 5704650, AND SRM 53-1-0, 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 2001111400170 20011114 00170 WP 2001 11 14 UPS01837254 1 20011105 A 5320 STIFFENER DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE:B COMPARTMENT 60 AFT PRESS BULKHEAD J-BEAM 5TH FROM BOTTOM OF LT SIDE HAS CRACK AS MARKED. STOP DRILLED CRACK REF DC8-5310-15663-A14596. FABRICATED UPPER REPAIR BRACKET PER PRELIMINARY EO DC8-5310-15663-A DP 70236. 2 L 7 4 4F RT 4A25 2001111400171 20011114 00171 WP 2001 11 14 UPS01837255 1 20011016 A 5320 3755841501 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 STA 1200 BATHTUB FITTING IS CRACKED AT LONG 34R. REMOVED AND REPLACED FITTING IAW DWG 3755841, AND S RM 51-1-20D. 2 L 7 4 4F RT 4A25 2001111400172 20011114 00172 WP 2001 11 14 UPS01837256 1 20011018 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 STA 1690 LONG 30L IS CORRODED BEYOND LIMITS. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPLA CEMENT SECTION OF LONGERON IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2001111400173 20011114 00173 2001 11 14 UPS01837258 4 20011107 A 2565 SLIDE DOUG DC8 DC873F 302199F WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:PFLT REF M226149 EMERGENCY ESCAPE SLIDE INOP. REMOVED AND REPLACED ESCAPE SLIDE COVER WITH SERVICEABLE UNIT. 2 L 7 4 4F RT 4A25 2001111400174 20011114 00174 NE 2001 11 14 UPS01837260 2 20011107 A 7310 O-RING DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE NR 3 ENGINE LEAKING A IPXA O OTHER X ENGINE FLAMEOUT CL CLIMB 1 SO 01 803UP 46073 692586 INSPECTION TYPE:N/A NR 3 ENGINE FLAME-OUT CLIMBING THRU FL 350. RESTARTED DESCENDING THRU FL240. FOUND 2 GHAMMA COUPLI NG O-RINGS LEAKING DURING FUEL LINE NEG PRESS CHECK. O-RINGS WERE REPLACED AND ENGINE RUN ACCOMPLISHED PER 28-22-12. 2 L 7 4 4F 4 F RT 4A25 E2GL 2001121700125 20011217 00125 WP 2001 12 17 UPS01837266 1 20011109 A 5312 BULKHEAD DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:N/A 4 CRACKS AT AFT PRESS BULKHEAD 65.5 FROM FLOOR LBL 23 TO LBL 38. REPAIRED IAW DC-8 SRM 53-2-5/3. 2 L 7 4 4F RT 4A25 2001112100151 20011121 00151 WP 2001 11 21 UPS01837267 1 20011109 A 5320 STIFFENER DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:N/A J-BEAM CRACKED AT AFT PRESS BULKHEAD. REMOVED PREVIOUS REPAIR ANGLE ON BOTTOM FLANGE AND FASTENERS ON UPPER FLANGE FOR REPAIR 0340 . STOP DRILLED CRACK. ROUGH CUT REPAIR ANGLES AND PICKED UP EXISTING FASTENER HOLD 003 40. 2 L 7 4 4F RT 4A25 2001112800020 20011128 00020 WP 2001 11 28 UPS01837268 1 20011109 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT BATTERY PACK VOLTAGE DEAD. REMOVED AND REPLACED EMERGENCY BATTERY PACK AND REL AY UNIT IAW 33-50-01. 2 L 7 4 4F RT 4A25 2001111400175 20011114 00175 WP 2001 11 14 AALA20011788 1 20010901 A 5551 PLATE DOUG DC9 DC983 3022083 WP HOTIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 437AA 49455 TUL - FOUND HORIZONTAL STAB LUG PLATES CORRODED IN BORE AND OUTBOARD FACE, 4 LUG PLATES. REMOVED AND REPLACED 4 LUG PLA TES WITH NEW PER SRM 51-01-00 AND 1PC 55-50-00. (M) 2 L 7 2 4F RT A6WE 2001111400176 20011114 00176 WP 2001 11 14 AALA20011861 1 20010921 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7520A 49897 TUL - FOUND FLOOR SUPPORT CORRODED, STATION 148, RBL 6 INCHES. REMOVED AND REPLACED FLOORBOARD SUPPORT WITH NEW SUPPORT SRM 51-01. (M) 2 L 7 2 4F A6WE 2001111400177 20011114 00177 WP 2001 11 14 AALA20011862 1 20010920 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7520A 49897 TUL - FOUND STATION 1260-1309, OUTBOARD SEAT TRACK NR 2 HAS CORROSION AROUND TOPS BOTTOM OF BOLT ACCESS HOLES. HEAVY CO RROSION OF TOP OF SEAT TRACK STATION 1299 TO 1309. INSTALLED NEW SEAT TRACK SPLICE FOR NR 2 TRACK, STATION 1260-1309 PE R SRM 53-05-00. (M) 2 L 7 2 4F A6WE 2001111400178 20011114 00178 WP 2001 11 14 AALA20011863 1 20010919 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7520A 49897 TUL - FOUND CORROSION SEAT TRACK NR 3 STATION 1165-1307. REMOVED AND INSTALLED NEW SEAT TRACK STATION 1165-1307 SRM 53- 05. (M) 2 L 7 2 4F A6WE 2001111400179 20011114 00179 WP 2001 11 14 AALA20011864 1 20010924 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7520A 49897 TUL - FOUND GOUGE IN SKIN AT STATION 349 LONGERON 29L. REMOVED DAMAGED AREA OF FUSELAGE SKIN AND INSTALLED REPAIR PER S RM 53-04 FIG 38 SHEET 24. (M) 2 L 7 2 4F A6WE 2001111400180 20011114 00180 WP 2001 11 14 AALA20011865 1 20010917 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7520A 49897 TUL - FOUND LOWER FLANGE OF FLOORBEAM WORN STATION 389 RBL 1. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER AARD 53-20 -00-21. (M) 2 L 7 2 4F A6WE 2001111400181 20011114 00181 NM 2001 11 14 AWXA200100578 1 20011026 A 5230 654795211 WEB BOEING BOEING 737 737277 1384570 NM AFT CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 189 22656 MCN - C13 CK - "C" - 2 CRACKS (.5") FOUND ON AFT CARGO DOOR INNER SKIN AT FWD LIGHTNING HOLES JUST ABOVE CENTERLINE. MAI NTENANCE TRIMED OUT THE CRACKS, FABRICATED REPAIR DOUBLERS AND INSTALLED IAW B737 SRM 51-40-2, FIG 1, PG 1 - 3. 2 L 7 2 4F RT A16WE 2001111400182 20011114 00182 NM 2001 11 14 AWXA200100579 1 20011028 A 5240 6545849158 SKIN BOEING BOEING 737 737277 1384570 NM R2 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 189 22656 MCN - C13 CK - "C" - CRACK FOUND ON R2 DOOR (.25") AT LOWER HINGE CUTOUT, UPPER EDGE, BS 958. MAINTENANCE TRIMMED OUT TH E CRACK, FABRICATED REPAIR DOUBLER AND INSTALLED IAW B737 SRM 52-00-3, FIG 5, PG 8, 8A,B,C & 9. 2 L 7 2 4F RT A16WE 2001111400183 20011114 00183 NM 2001 11 14 AWXA200100580 1 20011028 A 5330 65458000 SKIN BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 MCN - C13 CK - "C" - CRACKS FOUND ON FUSELAGE SKIN, ( 2 EA, .312" & .125") AT THE L-1 DOOR CUTOUT, UPPER FWD CORNER BS 3 13 - 314, BETWEEN STR 6L & 7L. MAINTENANCE TRIMED OUT THE DAMAGED AREA, FABRICATED REPAIR FILLERS, DOUBLER, TRIPLER AND SHIMS AND INSTALLED IAW AWA ER 15-5310-01310-SS2. 2 L 7 2 4F RT A16WE 2001111400184 20011114 00184 NM 2001 11 14 AWXA200100582 1 20011030 A 5313 655162829 STRINGER BOEING 737 737277 1384570 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 MCN - C13 CK - "C" - CORROSION FOUND ON STR 27L, BS 947 TO 996, BEYOND SRM LIMITS. FUSELAGE SKIN HAD MINOR CORROSION ON INSIDE SURFACE IN THE LOCATION WHICH WAS REMOVED AND FOUND TO BE WITHIN LIMITS. MAINTENANCE REMOVED DAMAGED SECTION OF S TR 27L, FABRICATED AND INSTALLED REPAIR SECTION OF STRINGER AND TREATED THE AREA PER B737 SRM 53-10-3, FIG 1, PG 3 - 10. 2 L 7 2 4F RT A16WE 2001111500002 20011115 00002 WP 2001 11 15 0103909607 1 20011018 A 5310 ANGLE DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 607NW 47232 During Hck in ATL, an existing repair angle was found cracked on the sta 1076 frame at the longeron 2R. The repair angle was removed and replaced with an identical repair. The repair angle was installed because a B/P 0.25 inch hole used to attach th 5910090-735 tie rod was found oversized to 5/16 inch diameter.Repaired per EA 96-185206. 2 L 7 2 4F A6WE 2001111500003 20011115 00003 WP 2001 11 15 0103919604 1 20011022 A 5330 DOUBLER DOUG DC9 DC932 3022066 WP DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 604NW 47222 While stationed at Dothan for an HCK, and in conjunction with a lower skin panel replacement per reference, a pre-existi ng corner repair was removed. Upon removal of the existing repair doubler, damage was found. Repaired per EA. 96-186757. Material .050" 2014-T6. Damage type not specified 2 L 7 2 4F A6WE 2001111500004 20011115 00004 WP 2001 11 15 0103929607 1 20011024 A 5410 ANGLE DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 607NW 47232 During Hck at ATL Base Maintenance, an existing repair angle was found cracked at sta 176 RHS at the aft portion of the lower cap of the pylon closing rib. Also, the lower cap was found trimmed at this location. The existing repair angle wa s removed and discarded. The lower cap was trimmed at 165. The lower cap portion aft of the trim line was removed and di scarded. A new lower section was installed and spliced with a repair angle. .040"ti-6ai-4v EA.96-185252 2 L 7 2 4F A6WE 2001111500005 20011115 00005 WP 2001 11 15 0103949869 1 20011103 A 5410 ANGLE DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 778NC 48100 During Line MTC., activities at the ATL base MTC. The lower angle (9959159-58) angle was found cracked at the 176 RHS at the aft end portion of the lower cap of the pylon closing rib. A new lower cap section was installed and spliced with a repair angle. 0.040" TI-6AI-4V, EA 98-185280 2 L 7 2 4F RT A6WE 2001111500006 20011115 00006 WP 2001 11 15 0103979929 1 20011018 A 5230 FLANGE DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8923E 45838 EO 5230-01119 installs a hold open latch on the fwd end of the fwd cargo door to minimize the the possibility of inadver tant closure. However, investigation has revealed cracking of the cargo door flange. EA 99-186086 2 L 7 2 4F A6WE 2001111500007 20011115 00007 WP 2001 11 15 0103989998 1 20011022 A 5720 CAP DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8934E 47143 During H ck in Atl, The rear spar, lower cap aft flange at approx. at approximately sta xrs 80 was found to be corroded and cracked. The damage was blended out and protected against corrosion. Material 2024-t3511 EA 99-185232 2 L 7 2 4F A6WE 2001111500011 20011115 00011 NM 2001 11 15 01FDEA00973 1 20011109 A 3230 LINKAGE BOEING 727 72722C 138400F NM LANDING GEAR DEFECTIVE A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 101FE 19197 LANDING GEAR FAILED TO RETRACT AFTER T/O. REMOVED AND REPLACED LANDING GEAR VALVE ACTUATING LINK PER AMM 32-31-00-5. T EST OK FOR SERVICE. 2 L 7 3 4F A3WE 2001113000018 20011130 00018 NM 2001 11 30 01FDEA00975 1 20011106 A 5310 SHEAR TIE BOEING 727 7272S2F 1384O81 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 201FE 22924 WHILE WORKING N296 FOUND CRACK IN SHEAR TIE BS 720, RBL 11, WL 150. REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-4, 51- 10-3. 2 L 7 3 4F A3WE 2001113000019 20011130 00019 NM 2001 11 30 01FDEA00976 1 20011108 A 5531 SPAR BOEING 727 727200 138407E NM VERTICAL STAB CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 201FE 22924 LEFT HAND VERTICAL STABILIZER MID SPAR CHORD CHAFED AT FIN STA 229. REMOVED AND REPLACED PER SRM 55-30-6 FIG 3. 2 L 7 3 4F RT A3WE 2001113000020 20011130 00020 NM 2001 11 30 01FDEA00977 1 20011106 A 5315 FLOORBEAM BOEING 727 7272S2F 1384O81 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 201FE 22924 CORROSION BS 344, FLOORBEAM UPPER CHORD RBL 17 - LBL 55, WL 208. REMOVED AND REPLACED CHORD PER SRM 51-10-2, 51-10-6, 53 -10-1, & 53-10-8. 2 L 7 3 4F A3WE 2001113000021 20011130 00021 NM 2001 11 30 01FDEA00979 1 20011106 A 5311 FRAME BOEING 727 7272S2F 1384O81 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 201FE 22924 DENT IN FRAME UPPER FLANGE BS 500, STR 24L. REMOVED AND REPLACED FRAME PER SRM 51-40-3, 51-40-2, 53-30-5 & EA 7-5310-605 91. 2 L 7 3 4F A3WE 2001111500013 20011115 00013 NM 2001 11 15 01FDEA00980 1 20011109 A 3260 WARNING SYSTEM DOUG MD11 MD11F 3023600 NM COCKPIT FALSE INDICATION A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 619FE 48770 NOSE GEAR LIGHT STAYED AFTER GEAR RETRACTION. CHECKED PHYSICAL CONDITION SENSORS AND TARGETS. NO DEFECTS NOTED. OK FO R SERVICE. 2 L 7 3 4F RT A22WE 2001111500014 20011115 00014 NM 2001 11 15 01FDEA00981 1 20011111 A 3260 WARNING SYSTEM DOUG MD11 MD11F 3023600 NM COCKPIT ACTIVATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 619FE 48770 NOSE GEAR UNSAFE IND AFTER GEAR RETRACTION, CYCLED GEAR. 2 L 7 3 4F RT A22WE 2001111500015 20011115 00015 NE 2001 11 15 01FDEA00982 2 20011112 A 7230 COMPRESSOR AIRBUS 310 A310222 3930315 EU PWA JT9 JT9D7R4D 52054 NE NR 1 ENGINE STALLED A FDEA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 25 419FE 345 E1H600 NR 1 ENG STALLED COMPRESSOR REPEATED EPR GAUGE ERRATIC UNABLE TO MAINTAIN. 2 L 7 2 4F 4 F RT A35EU E3NE 2001111500030 20011115 00030 NM 2001 11 15 2001UALA02197 1 20011102 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 331UA 24192 CREASE BEAM CRACKED AT STATION 178 WL 207 RIGHT HAND SIDE. MAJOR REPAIR ACCOMPLISHED. REPAIRED CREASE BEAM. 2 L 7 2 4F 4 F RT A16WE E2GL 2001111500031 20011115 00031 NM 2001 11 15 2001UALA02202 1 20011102 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 331UA 24192 STATION 178 WL 207 RIGHT HAND SIDE CHORD CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED CHORD. 2 L 7 2 4F 4 F RT A16WE E2GL 2001111500033 20011115 00033 NM 2001 11 15 2001UALA02203 1 20011102 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 331UA 24192 STATION 178 AT WL 207 WEB CRACKED AT LBL 17. MAJOR REPAIR ACCOMPLISHED. REPAIR WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2001111500034 20011115 00034 NM 2001 11 15 2001UALA02204 1 20011102 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 336UA 24240 AFT PIT FRAME FLANGE GOUGED-DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001111500035 20011115 00035 NM 2001 11 15 2001UALA02205 1 20011102 A 5312 PRESSURE PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 RIGHT HAND HORIZONTAL WEB AT STATION 178 AND WL 207 CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2001111500038 20011115 00038 NM 2001 11 15 2001UALA02206 1 20011104 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 920UA 25387 STATION 188 LEFT FUSELAGE FRAME AT WL 207 CRACKED ON AFT SIDE OUTER RADIUS. MAJOR REPAIR ACCOMPLISHED. FRAME DOUBLER I NSTALLED, EXTENDED SKIN CUTOUT FROM STATION 188 FOR ACCESS AND REPAIR DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001111500039 20011115 00039 NM 2001 11 15 2001UALA02207 1 20011103 A 5330 BEAR STRAP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 336UA 24240 FORWARD PIT DOOR CUTOUT, AFT SIDE BEAR STRAP BLENDED GOUGES EXCEED 20 PERCENT MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER, TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001111500040 20011115 00040 NM 2001 11 15 2001UALA02208 1 20011104 A 5753 FLAP BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE RT WING WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 920UA 25387 RIGHT INBOARD TRAILING EDGE AFT FLAP LEADING EDGE HAS DEEP WEAR AREA THAT EXTENDS THROUGH EXTERNAL SKIN (ALUMINUM) JUST INBOARD OF 2ND FROM INBOARD TRACK. MAJOR REPAIR ACCOMPLISHED. FLAP LEADING EDGE REPAIR AND SPLICE PLATE INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001111500041 20011115 00041 NM 2001 11 15 2001UALA02209 1 20011104 A 5512 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE HORIZ STAB GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 920UA 25387 RIGHT HORIZONTAL STABILIZER UPPER SKIN GOUGES AT STABILIZER STATION 46, 7 INCHES AFT OF SKIN LEADING EDGE. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001111500042 20011115 00042 NM 2001 11 15 2001UALA02210 1 20011104 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 331UA 24192 WL 207 RIGHT HAND CHORD AT BODY STATION 178 BULKHEAD CRACKED. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED REINFORCEMENT RE PAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001111500043 20011115 00043 NM 2001 11 15 2001UALA02211 1 20011104 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 331UA 24192 WL 207 LEFT HAND CHORD AT BODY STATION 178 BULKHEAD CRACKED. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED REINFORCEMENT REP AIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001111500044 20011115 00044 NM 2001 11 15 2001UALA02212 1 20011104 A 5312 PRESSURE PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 LEFT HAND HORIZONTAL WEB JUST AFT OF BULKHEAD 178 CRACKED AT WL 207 LBL 28. MAJOR REPAIR ACCOMPLISHED. WEB CRACK REPAI RED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001111500046 20011115 00046 NM 2001 11 15 2001UALA02214 1 20011104 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 BODY STATION 178 BULKHEAD WEB CRACKED UNDER RIGHT HAND LOWER RADAR ANTENNA MOUNT RBL 5 WL 199 APPROX 1 INCH CRACK. MAJO R REPAIR ACCOMPLISHED. WEB CRACK REPAIRED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001111500047 20011115 00047 NM 2001 11 15 2001UALA02215 1 20011104 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 BODY STATION 178 BULKHEAD WEB CRACKED UNDER RIGHT HAND LOWER RADAR ANTENNA MOUNT RBL 5 WL 202 APPROX 1 INCH CRACK. MAJO R REPAIR ACCOMPLISHED. WEB CRACK REPAIRED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001111500048 20011115 00048 NM 2001 11 15 2001UALA02217 1 20011105 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 328UA 24148 BODY STATION 188 LEFT HAND FUSELAGE FRAME CHORD CRACKED AT WL 207. MAJOR REPAIR ACCOMPLISHED. REPAIR ANGLE DOUBLER MAN UFACTURED AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001111500052 20011115 00052 NM 2001 11 15 2001UALA02225 1 20011106 A 5312 PRESSURE PANEL BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 919UA 25386 NOSE AREA RIGHT HAND BODY STATION 195 AT WL 207 OUTBOARD WEB CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2001111500053 20011115 00053 NM 2001 11 15 2001UALA02226 1 20011106 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 919UA 25386 NOSE AREA RIGHT HAND BODY STATION 188 AT WL 207 FRAME WEB CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2001111500054 20011115 00054 NM 2001 11 15 2001UALA02227 1 20011106 A 5312 PRESSURE PANEL BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 919UA 25386 NOSE AREA LEFT HAND BODY STATION 195 AT WL 207 OUTBOARD WEB CRACKED. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED W EB. 2 L 7 2 4F 4 F RT A16WE E2GL 2001111500057 20011115 00057 NM 2001 11 15 2001UALA02228 1 20011106 A 5330 BEAR STRAP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 336UA 24240 FORWARD PIT DOOR CUTOUT, FORWARD SIDE HAS BLEND GOUGES EXCEEDING 20 PERCENT MATERIAL LOSS ON BEAR STRAP. MAJOR REPAIR A CCOMPLISHED. INSTALLED DOUBLERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2001111500060 20011115 00060 NM 2001 11 15 2001UALA02229 1 20011106 A 5320 STIFFENER BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 919UA 25386 DURING ACCOMPLISHMENT OF THE 178 BULKHEAD SIDE CHORD AND WEB MOD (NOT WEB RPL), CRACKS WERE FOUND ON THE VERTICAL BEAM L OWER WEB AT RBL 17. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2001111500062 20011115 00062 NM 2001 11 15 2001UALA02233 1 20011105 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 121UA 29167 AFT EEL LIGHT INOP AT SEATS 2J, 1A AND 3A. REPLACED LAMPS AND CHECKED GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2001111500065 20011115 00065 NM 2001 11 15 2001UALA02234 1 20011105 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 121UA 29167 SECOND TO LAST FORWARD EMERGENCY WING LIGHT INOP RIGHT. RELAMPED, OPS CHECKS GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2001111500066 20011115 00066 NM 2001 11 15 2001UALA02235 1 20011107 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 128UA 30023 INOP EMERGENCY LIGHTS UPPER DECK CEILING ABOVE SEATS 16, 17 AND AFT OF SEATS 18 BETWEEN STAIRWELL AND CLOSET. RELAMPED, CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2001111500072 20011115 00072 2001 11 15 HEEA076915 4 20011024 A 3457 N0002000 GPS BELL 407 407 1182206 SW COCKPIT MALFUNCTIONED E K NONE O OTHER IN INSP/MAINT 1 SW 03 GPS WON'T TRANSMIT. 1 G 7 1 3U O H2SW 2001111500073 20011115 00073 EA 2001 11 15 COMA0160892 1 20011114 A 5300 SKIN CNDAIR CL600 CL6002B19 1900309 EA CABIN DOOR DENTED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 945CA 15092 7069 FUSELAGE SKIN AT FS310.0 NEAR PAX DOOR HAS TEMPORARY REPAIR THAT REQUIRES PERMANENT REPAIR.PERFORMED A PERMANENT MAJOR R EPAIR TO FUSELAGE SKIN AT FS 310.0 I/A/W CRJ REO 601R-53-21-180 AND WVAC EO 601R-53-2832. 2 L 7 2 4F RT A21EA 2001111500074 20011115 00074 EA 2001 11 15 COMA0160893 1 20011114 A 5346 60135006 BEAM CNDAIR CL600 CL6002B19 1900309 EA AFT EQUIPMENT BA CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 936CA 17166 7043 1" CRACK ON TOP LEFT SIDE OF ENGINE SUPPORT BEAM FOUND. LOCATED 7 RIVETS TO THE LEFT OF BL0.0.REPAIRED DAMAGE I/A/W REO 601R-53-61-345 BY INSTALLING DOUBLERS AT TOP AND BOTTOM OF ENGINE SUPPORT BEAM AT BLO.0. 2 L 7 2 4F RT A21EA 2001111500075 20011115 00075 EA 2001 11 15 COMA0160894 1 20011111 A 3350 363782 LAMP CNDAIR CL600 CL6002B19 1900309 EA CABIN FLOOR INOPERATIVE A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 987CA 7199 EMERGENCY FLOOR PATH LIGHTING AT ROW 2 IS INOPERABLE.INSTALLED NEW LIGHT STRIP. 2 L 7 2 4F RT A21EA 2001111500076 20011115 00076 EA 2001 11 15 COMA0160895 1 20011114 A 5346 60135006 BEAM CNDAIR CL600 CL6002B19 1900309 EA AFT EQUIPMENT BA CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 936CA 17166 7043 CRACK APPROXIMATELY 1" LONG AT ENGINE SUPPORT BEAM LEFT LOWER ACCESS PANEL.REPAIRED DAMAGE I/A/W REO 601R-53-61-366 BY R EMOVING DAMAGE AND INSTALLING A DOUBLER. 2 L 7 2 4F RT A21EA 2001111500077 20011115 00077 EA 2001 11 15 COMA0160896 1 20011028 A 3810 601R431621 TANK CNDAIR CL600 CL6002B19 1900309 EA AVIONCIS SHORTED A COMA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 995CA 7229 FLIGHT #5819 - F/A REPORTED SMOKE SMELL. GALLEY AND LAV WATER SERVICE INOP. GALLEY BREAKERS WERE TRIPPED.REPLACED THE G ALLEY WATER TANK. 2 L 7 2 4F RT A21EA 2001111500078 20011115 00078 WP 2001 11 15 ABXA010573 1 20011112 A 3231 DOOR DOUG DC9 DC941 302207N WP NLG OPEN A ABXA O OTHER E VIBRATION/BUFFET CL CLIMB 1 GL 23 957AX 47759 ON GEAR RETRACTION, RECEIVED SERIOUS VIBRATION AND A LOUD NOISE AS IF THE TIRE WAS STILL ROTATING. BUT WOULD NOT DISSIP ATE AS IF TIRE SPIN STOPPED. ALL GEAR LIGHT INDICATIONS WERE NORMAL. GEAR RECYCLE. UPON ARRIVAL WHILE TAXIING TO BLOC KS, NOTICED THE RIGHT GEAR DOOR WAS OPEN. INSPECTED THE LEFT AND RIGHT NOSE GEAR DOORS, CABLES, LINKAGE AND LANDING GEA R. NO DAMAGE NOTED. LUBED THE NOSE GEAR DOORS. 2 L 7 2 4F A6WE 2001111500079 20011115 00079 WP 2001 11 15 ABXA010580 1 20011113 A 3350 CONTACTOR DOUG DC9 DC933F 302207A WP BATTERY PACK DIRTY A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 930AX 47363 COCKPIT EMERGENCY LIGHTS WOULD NOT COME ON. CLEANED BATTERY PACK AND CONTACTS. SYSTEM OPS CHECKED GOOD IAW DC-9 AMM 33 -53-02-4-0001. 2 L 7 2 4F A6WE 2001111500080 20011115 00080 WP 2001 11 15 ABXA010582 1 20011109 A 3350 TERMINAL DOUG DC9 DC931 3022065 WP BATTERY PACK DIRTY A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 941AX 47419 EMERGENCY LIGHTS INOPERATIVE. CLEANED TERMINALS ON BATTERIES IN EMERGENCY BATTERY PACK AS REQUIRED. OPS CHECKED GOOD IA W DC-9 MM. 2 L 7 2 4F A6WE 2001111500081 20011115 00081 WP 2001 11 15 ABXA010583 1 20011113 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 946AX 47003 EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK IAW DC-9 AMM 33-50-01-2-0001. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2001111500083 20011115 00083 NM 2001 11 15 AWXA200100573 1 20011020 A 5315 6549885 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - C13 CK - C - CORROSION FOUND ON FLOORBEAM UPPER T-CHORD AT BS 986.5, LBL 43 TO RBL 43 BEYOND SRM LIMITS AFTER CLEA N UP. MAINTENANCE REMOVED FLOORBEAM UPPER T-CHORD, FABRICATED AND INSTALLED REPLACEMENT UPPER T-CHORD IAW B737 SRM 53-6 0-51, PG 207 - 208, 51-40-02, PG 6 - 11 AND BOEING DWG 65-46811. 2 L 7 2 4F RT A16WE 2001111500084 20011115 00084 NM 2001 11 15 AWXA200100574 1 20011022 A 5315 6546810 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - C13 CK - C - CORROSION FOUND ON FLOORBEAM UPPER FLANGE AT BS 967, RBL 46, BEYOND SRM LIMITS AFTER CLEAN UP, (HAD A PREVIOUS BLEND REPAIR IN THE SAME SPOT). MAINTENANCE TREATED AND FILLED BLENDED AREA, FABRICATED REPAIR STRAP AND SHIM S AND INSTALLED IAW B737 SRM 53-00-51, PG 212 - 215. 2 L 7 2 4F RT A16WE 2001111500085 20011115 00085 NM 2001 11 15 AWXA200100575 1 20011028 A 5314 646212518 KEELBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - C13 CK - C - CORROSION FOUND ON KEEL BEAM CHORD, LOWER O/B FLANGE AT BS 532 TO BS 534.6, RBL 6.5, WL 148.5, BEYOND SRM LIMITS AFTER CLEAN UP. MAINTENANCE REMOVED DAMAGED SECTION OF O/B FLANGE, FABRICATED REPAIR ANGLE AND FILLERS AND INSTALLED IAW AWA ER 03-5310-01309-SS1. 2 L 7 2 4F RT A16WE 2001111500086 20011115 00086 NM 2001 11 15 AWXA200100576 1 20011106 A 5330 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 LAS - B3 CK - C - CRACK FOUND IN FUSELAGE SKIN 1.375 INCH LONG AT BS 727D, STR 23L. MAINTENANCE ROUTED OUT THE CRACK, F ABRICATED REPAIR DOUBLER AND INSTALLED IAW AWA ER 03-5331-01310-TB1. 2 L 7 2 4F RT A16WE 2001111500087 20011115 00087 SO 2001 11 15 C2XA01CL227 1 20011108 A 3230 355022002MOD2 CONTROL UNIT EMB 135 EMB135LR 3260305 SO COCKPIT INTERMITTENT A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 12519 4419 145366 CLE FLIGHT 3077 THE CREW REPORTED THE GEAR WOULD NOT RETRACT IMMEDIATELY AFTER TAKEOFF. RECYCLED THE GEAR HANDLE AND TH E GEAR RETRACTED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT TOOO11AT 2001111500088 20011115 00088 SO 2001 11 15 C2XA01IA393 1 20011105 A 2150 8152403 ACM EMB 135 EMB135LR 3260305 SO A/C BAY SEIZED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 12513 135292 IAH-WHILE AT THE GATE THE CREW NOTED THAT THE CABIN FILLED WITH SMOKE. IAH- MAINTENANCE REMOVED AND REPLACED THE NR 2 A CM, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT TOOO11AT 2001111500089 20011115 00089 EU 2001 11 15 C2XA01IA394 1 20011109 A 2120 SMOKE AEROSP ATR42 ATR42320 8680930 EU CABIN DETECTED A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 34817 152 MOB- FLIGHT 3953, DURING TAXI THE CREW NOTED A ELECTRIC SMOKE SMELL IN THE COCKPIT AND RETURNED TO THE GATE. MOB- MAIN TENANCE POWERED UP THE AIRCRAFT, STARTED BOTH ENGINES, CYCLED ENVIRONMENTAL SYSTEM, CYCLED ALL ELECTRICAL SYSTEMS, CYCLE D FLIGHT CONTROLS, COULD NOT DUPLICATE THE SMELL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001111500090 20011115 00090 SO 2001 11 15 C2XA01IA395 1 20011110 A 3350 3025101 LIGHT EMB 145 EMB145ER 3260211 SO EXTERIOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12946 145052 IAH- MAINTENANCE NOTED THAT THE RIGHT FRONT EMERGENCY LIGHT FAILED TO ILLUMINATE. IAH- MAINTENANCE REMOVED AND REPLAC ED THE EXTERIOR EMERGENCY LIGHT ASSEMBLY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOT ED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001111500091 20011115 00091 SO 2001 11 15 C2XA01IA396 1 20011110 A 3350 78241 BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13979 145181 IAH- DURING POST FLIGHT THE CREW NOTED THAT THE REAR EMERGENCY FLOOR LIGHTS FAILED TO ILLUMINATE. IAH- MAINTENANCE RE MOVED AND REPLACED THE NUMBER 4 EMERGENCY BATTERY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DE FECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001111500092 20011115 00092 SO 2001 11 15 C2XA01IA397 1 20011108 A 3230 LANDING GEAR EMB 120 EMB120ER 3260203 SO NLG & MLG MALFUNCTIONED A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 27 16729 120185 ROW - CREW REPORTED THAT THE LANDING GEAR SYSTEM FAILED TO EXTEND WHILE ON APPROACH. THE CREW PERFORMED A MANUAL EXTENS ION OF THE GEAR AND LANDED AT ROW WITHOUT FURTHER INCIDENT. AWAITING A MAINTENANCE ACTION TO COMPLETE THIS REPORT. 2 L 7 2 4T RT A31SO 2001111500100 20011115 00100 SO 2001 11 15 C2XA01TY173 1 20011109 A 5320 14522460013 FLOOR SUPPORT EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15509 145238 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE AFT GUSSET AT FRAME 18. MAINTENANCE REMOVED AND REPLACED AFT GUSSET AT FRAME 18 IAW EMB-135 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLE TION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001111500101 20011115 00101 SO 2001 11 15 C2XA01TY174 1 20011111 A 5720 14522141407 ROD END EMB 135 EMB135ER 3260203 SO RT WING CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15509 145238 TYS DURING A 1-C INSPECTION THE RIGHT FUSELAGE TO SPAR 3 ROD ASSEMBLY HAD CORROSION ON THE LOWER ROD ENDS. MAINTENANCE REMOVED AND REPLACED RIGHT ROD ASSEMBLIES IAW EMB GST-3655A/01 WHICH WAS ACCOMPLISHED. THE AIRCRAFT WILL BE RELEASED TO SERVICE UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001111500102 20011115 00102 SO 2001 11 15 C2XA01TY175 1 20011111 A 5720 14522141407 ROD END EMB 135 EMB135ER 3260203 SO LT WING CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15509 145238 TYS DURING A SCHEDULED 1-C INSPECTION THE LEFT FUSELAGE TO SPAR 3 ROD END ASSEMBLY HAD CORRODED ON THE LOWER ROD END. M AINTENANCE REMOVED AND REPLACED THE LEFT ROD ASSEMBLY IAW GST-3655A-01 WHICH WAS ACCOMPLISHED. THE AIRCRAFT WILL BE REL EASED TO SERVICE UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001111500103 20011115 00103 SO 2001 11 15 C2XA01TY177 1 20011111 A 5315 14521713003 FLOORBEAM EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15509 145238 TYS DURING A SCHEDULED INSPECTION, CORROSION WAS FOUND ON THE LEFT OMEGA BEAM AT FRAME 20. MAINTENANCE REMOVED THE DA MAGED SECTION, FABRICATED NEW ANGLE, SHIM, FILLER AND PLATE. INSTALLED REPAIRED PARTS AND FLOORBEAM IAW EMB-135/145-SRM -53-21-10 & 53-40-02, CPM-51-21-04, 05, 06 AND EC5320-01010 (6.1.3). REPAIR PROCEDURES WERE SATISFACTORY. AIRCRAFT REL EASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001111500104 20011115 00104 SO 2001 11 15 C2XA01TY178 1 20011111 A 5315 14521721005 FLOORBEAM EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15509 145238 TYS DURING A SCHEDULED INSPECTION, CORROSION WAS FOUND ON THE FORWARD DIGITAL BETWEEN FRAMES 15 AND 16 AT CENTER AND L EFT SIDE. MAINTENANCE REMOVED THE DAMAGED SECTION, FABRICATED NEW ANGLE, SHIM, FILLER AND PLATE. INSTALLED REPAIRED PA RTS IAW-EMB-135/145-SRM-51-20-03 & 51-40-02, CPM-51-21-04, 05, AND EC5320-01059. REPAIR PROCEDURES WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001111500105 20011115 00105 SO 2001 11 15 C2XAS01TY172 1 20011108 A 5320 14522459003 ANGLE EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15509 145238 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER OMEGA BEAM RAMP ANGLE AT FRAME 17. MAINTENANCE REM OVED AND REPLACED THE RAMP ANGLE IAW EMB-135 SRM 51-20-03, 51-40-02 AND 51-20-01. THE REPAIR WAS FOUND TO BE SATISFACTO RY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001111500106 20011115 00106 NM 2001 11 15 CALA0100999 1 20011110 A 5311 BELTFRAME BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59338 23576 INSPECTION FOUND BELTFRAME CORRODED IN AFT BAGGAGE BIN AT STA 927, BL 0. THE BELTFRAME WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2001111500107 20011115 00107 WP 2001 11 15 CALA0101000 1 20011112 A 3350 AD4002P BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 33805 49249 THE OVERWING EMERGENCY EXIT IDENTIFIERS ABOVE DOORS ON LT AND RT SIDE OF AIRCRAFT WERE FOUND INOPERATIVE. THE BATTERIES IN EMERGENCY BATTERY PACKS IN O/H BIN AT ROW 20DEF WERE REPLACED IAW MM 33-50-00. 2 L 7 2 4F A6WE 2001111500109 20011115 00109 EU 2001 11 15 CHQ00035 1 20011101 A 6120 CONTROLLER SAAB SF340 SF340A 7850100 EU PROP CONTROL MALFUNCTIONED A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 CHQA 40 AUTO COURSEN WILL NOT ARM AND C TOT INOP. 2 L 7 2 4T RT A52EU 2001111500111 20011115 00111 SO 2001 11 15 CHQ00036 1 20011106 A 3230 LANDING GEAR EMB 145 EMB145 3260210 SO NLG & MLG MALFUNCTIONED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 CHQA 145144 LANDING GEAR NOT RETRACTING. 2 L 7 2 4F RT T00011AT 2001111500117 20011115 00117 2001 11 15 AWXA200100585 4 20011114 A 2350 BOEING BOEING 757 7572S7 1384962 NM A AWXA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 28 903AW D00435 23323 ABQ - DIVERTED FLIGHT - FLT 888 - "O" - ENROUTE FROM LAS TO FLL, AT FL 370, 20 NM WEST OF ABQ THE FLIGHT DECK CREW EXPER IENCED ELECTRICAL FUMES IN THE COCKPIT, NO WARNING INDICATIONS WERE PRESENT, NO FUMES IN THE CABIN. THE AIRCRAFT DIVERTE D TO ABQ MAKING AN UNEVENTFUL LANDING. MAINTENANCE TECHNICIANS WERE SENT FROM PHX TO ABQ. THE SOURCE OF THE FUMES WAS IS OLATED TO THE FIRST OFFICERS AUDIO SELECTOR PANEL. THE AUDIO SELECTOR PANEL WAS REPLACED AND CHECKED GOOD IAW AMM 23-51- 01. NO FURTHER DISCREPANCIES HAVE BEEN REPORTED. NOTE: THE AUDIO SELECTOR PANEL HAD BEEN REPLACED ON THE PREVIOUS FLIGHT IN LAS DUE TO THE VOLUME CONTROL WAS BROKEN. A SUPPLEMENTAL SDR WILL BE SUBMITTED WHEN VENDOR TEAR DOWN INFORMATION IS 2 L 7 2 4F RT A2NM 2001111500124 20011115 00124 SO 2001 11 15 CHQ00038 1 20011107 A 7330 INDICATOR EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL COCKPIT INOPERATIVE A CHQA D RETURN TO BLOCK O OTHER UK UNKNOWN 1 GL 11 271 145305 NR 1 FUEL INDICATION INOP. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001111500126 20011115 00126 SO 2001 11 15 CHQ00039 1 20011109 A 2750 FLAP EMB 145 EMB145 3260210 SO WING MALFUNCTIONED A CHQA C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 GL 11 287 145460 FLAP T/O CONFIG WARNING. 2 L 7 2 4F RT T00011AT 2001111500138 20011115 00138 NM 2001 11 15 UPS01237262 1 20011106 A 5755 69705341 ROD BOEING 727 72731C 1384011 NM SPOILER BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE:PRD INBOARD SPOILER CASTING SUPPORT ROD BROKEN LT WING. INBOARD SPOILER LT WING CASTING SUPPORT ROD REP LACED. 2 L 7 3 4F A3WE 2001111500140 20011115 00140 NM 2001 11 15 C1HA200183008 1 20011111 A 2611 473597402 SMOKE DETECTOR BOEING 727 7272S7 138407Z NM INOPERATIVE A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 683CA 22490 #5 Smoke Detector inop in aft cargo compartment. Action Taken: Replaced #5 smoke detector in aft pit IAW MM 26-25-01, Ops check normal. 2 L 7 3 4F A3WE 2001111500141 20011115 00141 NM 2001 11 15 C1HA200181016 1 20011109 A 3350 BATTERY BOEING 727 7272S7 138407Z NM A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 681CA 22020 Emergency exit light inop between aft lavatories. Action Taken: Removed and replaced emergency exit light battery betw een aft lavs. Ops check normal per 727 MM 33-50. 2 L 7 3 4F A3WE 2001111500142 20011115 00142 NM 2001 11 15 C1HA200186009 1 20011109 A 3350 900835A BATTERY BOEING 727 7272S7 138407Z NM INOPERATIVE A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 686CA 22021 Emergency Exit Light Inop between aft lavs. Action Taken: Removed and replaced emergency exit light battery between af t lavs. Ops check normal per 727 MM 33-50. 2 L 7 3 4F A3WE 2001111500143 20011115 00143 NM 2001 11 15 DHL2001712022 1 20011109 A 2611 CONNECTOR BOEING 727 72729 1384007 NM SMOKE DETECTOR LOOSE A DHLA K NONE L NO TEST UK UNKNOWN 1 SO 01 712DH 19401 NR 1 SMOKE DETECTOR WON'T TEST. RESECURED LOOSE CONNECTOR ON NR 1 SMOKE DETECTOR. SYSTEM TESTS GOOD IAW B727 MM 26-17- 000. 2 L 7 3 4F A3WE 2001111500144 20011115 00144 NM 2001 11 15 DHL2001740006 1 20011113 A 3510 OXYGEN MASK BOEING 727 7272Q9 138448M NM COCKPIT DEFECTIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 740DH 21930 F/O O2 MASK DURING TEST, ANTI SUFFOCATION VALVE WOULD NOT RELEASE. REMOVED AND REPLACED MASK, OPS CK GOOD IAW MM 35-11- 0. 2 L 7 3 4F RT A3WE 2001111500145 20011115 00145 NM 2001 11 15 P5CA0100612 1 20011113 A 5310 NONE WEB BOEING 747 7472U3B 1384846 NM NOSE WHEEL WELL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 923FT 22769 6" CRACK AT STA 300 RH NOSE WHEEL WELL BEAM RUNNING ACROSS WEB, EMINATING FROM INSULATION BLANKET STANDOFF HOLE. NO ADJA CENT FASTENERS LOOSE, SHEARED OR MISSING. REPAIR CARRIED OUT IAW SRM 51-40-02, FIG 1, SHT 5, DETAIL 3. PARTS TREATED W/ ALODINE 1200 & REPAIR PARTS PRIMED W/ BMS 10-11 & INSTALLED. SEALANT APPLIED & REPROTECTED W/ DINOTROL AV 30. 2 L 7 4 4F RT A20WE 2001111500146 20011115 00146 WP 2001 11 15 MWEA011433 1 20011115 A 5310 591015835 WEB DOUG DC9 DC915 3022036 WP STATION 714 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 LIGHT CORROSION AROUND FASTENER HOLES AT STATION 714 AT LONGERON 25 RIGHT -- FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2001111500147 20011115 00147 WP 2001 11 15 MWEA011436 1 20011115 A 5310 99582021 CLIP DOUG DC9 DC915 3022036 WP STATION 544 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 CRACK INDICATION USING EDDY CURRENT ON ANGLE ON AFT SIDE OR FRAME AT STATION 544 LONGERON 10 LEFT. CRACKED IN TWO PLACES AROUND RIVETS -- REMOVED AND INSTALLED NEW CLIP. 2 L 7 2 4F A6WE 2001111500148 20011115 00148 WP 2001 11 15 MWEA011440 1 20011115 A 5310 9958188 BEAM DOUG DC9 DC915 3022036 WP FUSELAGE STA. 80 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 HEAVY CORROSION ON TOP OF FLOOR BEAM RIGHT HAND LAVE AROUND AND IN A SCREW HOLE APPROXIMATELY 2 FEET INBOARD FROM WALL A T FUSELAGE STATION 801 -- REMOVED, FABRICATED AND INSTALLED NEW FLOOR BEAM. 2 L 7 2 4F A6WE 2001111500149 20011115 00149 NM 2001 11 15 DHL2001748007 1 20011106 A 2612 FIRE LOOP BOEING 727 727225 1384077 NM NR 1 ENGINE OUT OF POSITION A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 748DH 22440 FIRE PROTECTION GROUND NR 1 CIRCUIT LIGHT ILLUMINATED INTERMITTENTLY IN FLIGHT. REPOSITIONED FIRE LOOP ON NR 1 ENGINE L IGHT EXTINGUISHED IAW A/C MM CHAP 26-10. 2 L 7 3 4F A3WE 2001111500150 20011115 00150 NM 2001 11 15 DHL2001748008 1 20011107 A 2612 FIRE LOOP BOEING 727 727225 1384077 NM NR 1 ENGINE MALFUNCTIONED A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 748DH 22440 FIRE PROTECTION GROUND NR 1 CIRCUIT LIGHT ILLUMINATED INTERMITTENTLY IN FLIGHT. INSPECTED NR 1 ENGINE FIRE LOOP FOR CON TACT, NO DEFECTS NOTED. SYSTEM TESTED AND OPS CHECKED GOOD IAW MM 26-10-0. 2 L 7 3 4F A3WE 2001111500151 20011115 00151 NM 2001 11 15 DHL2001748009 1 20011107 A 2612 FIRE LOOP BOEING 727 727225 1384077 NM NR 1 OUT OF POSITION A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 748DH 22440 NR 1 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED IN FLIGHT. INSPECTED FIRE LOOP, REPOSITIONED LOOP AND MOUNTING SPACERS. LIGHT EXTINGUISHED, OPS CHECKED GOOD ON THE GROUND AT THIS TIME. 2 L 7 3 4F A3WE 2001111500152 20011115 00152 WP 2001 11 15 AALA20011815 1 20010918 A 5710 STRUCTURE DOUG DC9 DC982 3022082 WP RT WING DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 462AA 49592 TUL - FOUND MAINTENANCE ENTRY DAMAGED RIGHT WING FROM L/E OF NR 5 SLAT BACK TO THE AILERON AT INBOARD ATTACH POINT. FAB RICATED AND INSTALLED DOUBLER TO LOWER RIGHT WING LEADING EDGE OF NR 5 SLAT BACK TO AILERON AT INBOARD ATTACH POINT IAW ESO 80559. (M) 2 L 7 2 4F A6WE 2001111500153 20011115 00153 WP 2001 11 15 AALA20011866 1 20010918 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7520A 49897 TUL - FOUND CUSP DENTED STATION 1077 LEFT SIDE. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2001111500154 20011115 00154 WP 2001 11 15 AALA20011867 1 20010918 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7520A 49897 TUL - WINDOW PANEL CRACKED TOP FORWARD CORNER LEFT WINDOW PANEL STATION 946. STOP DRILLED AND INSTALLED DOUBLER PER AAR D 53-10-00-25. (M) 2 L 7 2 4F A6WE 2001111500155 20011115 00155 WP 2001 11 15 AALA20011868 1 20010920 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7520A 49897 TUL - FOUND WINDOW PANEL CRACKED AT TOP AFT CORNER FASTENER HOLE STATION 1022 LEFT. INSTALLED DOUBLER PER AARD 53-10-00 -25. (M) 2 L 7 2 4F A6WE 2001111500156 20011115 00156 WP 2001 11 15 AALA20011869 1 20010920 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7520A 49897 TUL - FOUND DEEP DENT IN FUSELAGE SKIN APPROX STATION 305 ABOVE LONGERON 24L. REMOVED DAMAGED PART OF SKIN. INSTALLED DOUBLER PER SRM 53-04-00. (M) 2 L 7 2 4F A6WE 2001111500157 20011115 00157 WP 2001 11 15 AALA20011870 1 20010912 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7520A 49897 TUL - FOUND RIGHT CUSP HAS CORROSION STATION 598-617. REMOVED CORRODED AREA THAT WAS BEYOND LIMITS BY CUTTING OUT. INS TALLED DOUBLER PER SRM 53-01 FIG 4. (M) 2 L 7 2 4F A6WE 2001111500158 20011115 00158 WP 2001 11 15 AALA20011871 1 20010922 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7520A 49897 TUL - FOUND WORN AREA ON SEAT TRACK NR 5 AT STATION 200. REPLACED SECTION OF NR 5 SEAT TRACK FROM STATION 200 TO 246 AS PER SRM 53-05. (M) 2 L 7 2 4F A6WE 2001111500159 20011115 00159 WP 2001 11 15 AALA20011872 1 20010919 A 5320 BEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7520A 49897 TUL - FOUND AFT CARGO DOOR BEAM HAS CORROSION STATION 1155 TO 1212. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-3. (M) 2 L 7 2 4F A6WE 2001111500160 20011115 00160 WP 2001 11 15 AALA20011873 1 20010926 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7520A 49897 TUL - FOUND CORROSION ON TOP OF SEAT TRACK STATION 1175 TO 1179. INSTALLED NEW SEAT TRACK FROM STATION 1173 TO 1307 SRM 53-05. (M) 2 L 7 2 4F A6WE 2001111500161 20011115 00161 WP 2001 11 15 MWEA011434 1 20011115 A 5310 99118594 LONGERON DOUG DC9 DC915 3022036 WP FUSELAGE STA. 92 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 FUSELAGE STATION 925 CRACKED AT LONGERON 17 RIGHT -- STOP DRILLED CRACK AND INSTALLED REPAIR ANGLES. 2 L 7 2 4F A6WE 2001111500162 20011115 00162 WP 2001 11 15 MWEA011435 1 20011115 A 5310 99577212 INTERCOSTAL DOUG DC9 DC915 3022036 WP FUSELAGE STA. 88 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 INTERCOSTAL BETWEEN FUSELAGE STATION 880 & 859 CRACKED AT RADIUS NEXT TO 859 ABOVE LONGERON 16 RIGHT -- INSTALLED REPA IR ANGLES. 2 L 7 2 4F A6WE 2001111500163 20011115 00163 WP 2001 11 15 MWEA011437 1 20011115 A 5310 591141917 LONGERON DOUG DC9 DC915 3022036 WP FUSELAGE STA. 78 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 RIGHT LAV HAS A CRACKED LONGERON AT FUSELAGE STATION 786 LONGERON 17 LEFT -- REMOVED DAMAGED SECTION OF LONGERON AND I NSTALLED LONGERON REPAIR SPLICE. 2 L 7 2 4F A6WE 2001111500164 20011115 00164 WP 2001 11 15 MWEA011438 1 20011115 A 5310 591141917 LONGERON DOUG DC9 DC915 3022036 WP FUSELAGE STA. 78 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 LEFT LAV HAS A CRACKED LONGERON AT FUSELAGE STATION 786 AND LONGERON 17 LEFT -- INSTALLED LONGERON REPAIR SPLICE SECTI ON. 2 L 7 2 4F A6WE 2001111500165 20011115 00165 WP 2001 11 15 MWEA011439 1 20011115 A 5310 39162091 SUPPORT FITTING DOUG DC9 DC915 3022036 WP STATION 566 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 AREA OVER CENTER WING LATERAL FLOOR SUPPORT BEAM ATTACH ANGLE IS CRACKED AT STATION 566 XCW 40 LEFT -- REMOVED FLOOR S UPPORT FITTING AND INSTALLED REPAIR ANGLE. 2 L 7 2 4F A6WE 2001111500166 20011115 00166 WP 2001 11 15 AALA20011874 1 20010928 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7520A 49897 TUL - FOUND .5 INCH HOLE IN CUSP, OUTBOARD OF SEAT TRACK NR 5 STATION 736. REMOVED DAMAGE, DYE CHECKED, NO CRACKS. INS TALLED DOUBLER REPAIR PER AARD 53-00-00-02 AND SRM 53-01 FIG. (M) 2 L 7 2 4F A6WE 2001111500167 20011115 00167 WP 2001 11 15 AALA20011875 1 20010928 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7520A 49897 TUL - FOUND CORROSION ON LEFT CUSP SEVERAL PLACES BETWEEN STATION 693 AND 712. CUTOUT CORRODED AREA AND INSTALLED DOUBL ER PER AARD 53-00-00-02 AND SRM 53-01. ALSO, INCORPORATED ESO 80559. (M) 2 L 7 2 4F A6WE 2001111500168 20011115 00168 WP 2001 11 15 AALA20011876 1 20011002 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7520A 49897 TUL - FOUND SEAT TRACK NR 6 DAMAGED AT 730. REPLACED SEAT TRACK NR 6 FROM STATION 718 TO 793 PER SRM 53-05 FIG 4F. (M) 2 L 7 2 4F A6WE 2001111500169 20011115 00169 WP 2001 11 15 AALA20011877 1 20011002 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7520A 49897 TUL - FOUND CUSP DAMAGED AROUND RIVET HEAD, CRACKED. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 2001111500170 20011115 00170 WP 2001 11 15 AALA20011878 1 20011002 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7520A 49897 TUL - FOUND MOST OUTBOARD SEAT TRACK ON LEFT SIDE OF A/C AT STATION 250 IS DAMAGED OUT ON LOWER SIDE. REMOVED AND REPLA CED SECTION OF SEAT TRACK FROM STATION 218 TO STATION 265 AS PER SRM 53-05 SEAT TRACK SPLICE. (M) 2 L 7 2 4F A6WE 2001111500171 20011115 00171 WP 2001 11 15 AALA20011879 1 20010926 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7520A 49897 NR 4 SEAT TRACK, STATION 236, CORRODED. REMOVED CORRODED SEAT TRACK. INSTALLED NEW TRACK SECTION FROM STATION 200 TO 2 65 PER SRM 53-05 FIG 4B. (M) 2 L 7 2 4F A6WE 2001111500172 20011115 00172 WP 2001 11 15 AALA20011880 1 20010927 A 5320 STRUCTURE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7528A 49920 TUL - FOUND CORROSION ON OUTBOARD FLANGE. INSTALLED REPAIR STRAP PER AARD 53-20-00-13. (M) 2 L 7 2 4F A6WE 2001111500173 20011115 00173 WP 2001 11 15 AALA20011881 1 20010921 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7528A 49920 TUL - FOUND DENT IN FUSE SKIN STATION 1079 LONGERON 17L ADL NR 5280015. COLD WORKED DENT AND INSTALLED TWO ROW DOUBLER PER SRM 53-04-38. (M) 2 L 7 2 4F A6WE 2001111500174 20011115 00174 WP 2001 11 15 AALA20011882 1 20010920 A 5310 WINDOW FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7528A 49920 TUL - FOUND PASSENGER WINDOW FRAME CRACKED ON RIGHT SIDE STATION 947 UPPER FORWARD CORNER. ROUTED OUT CRACK. INSTALLED DOUBLER PER AARD 53-10-00-25. (M) 2 L 7 2 4F A6WE 2001111500175 20011115 00175 WP 2001 11 15 AALA20011883 1 20010921 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7528A 49920 TUL - FOUND STATION 579 RIGHT CUSP 1ST LIGHTENING HOLE CORRODED. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-01 FIG 4. (M) 2 L 7 2 4F A6WE 2001111500176 20011115 00176 WP 2001 11 15 AALA20011884 1 20010920 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7528A 49920 TUL - FOUND CORROSION INSIDE SEAT TRACK NR 6 STATION 670-672. CUT OUT DAMAGED AREA INSTALLED SEAT TRACK PLUG REPAIR PER SRM 53-05 FIG 4A. (M) 2 L 7 2 4F A6WE 2001111500177 20011115 00177 WP 2001 11 15 AALA20011885 1 20010928 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7528A 49920 TUL - FOUND TWO INCH LONG PARALLEL GOUGES ON FUSELAGE SKIN AT STATION 229 ABOVE L18L. INSTALLED REPAIR DOUBLER PER ESO 8 0559 (M) 2 L 7 2 4F A6WE 2001111500178 20011115 00178 WP 2001 11 15 AALA20011886 1 20010924 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7528A 49920 TUL - FOUND CORROSION ON WEB (CUSP) INBOARD OF FORWARD GALLEY DOOR. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-01 FIG 4-3. (M) 2 L 7 2 4F A6WE 2001111500179 20011115 00179 NM 2001 11 15 P5CA0100611 1 20011113 A 5310 NONE WEB BOEING 747 7472U3B 1384846 NM NOSE WHEEL WELL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 923FT 22769 1-1/2" CRACK BETWEEN STA 280 & 300 LH OB INTERCOSTAL ON NOSE WHEEL WELL ROOF RUNNING ACROSS UPPER FLANGE & DOWN THE WEB OF THE "Z" SECTION. NO ADJACENT FASTENERS ARE MISSING, LOOSE OR SHEARED. REPAIRED AS PER SRM 51-40-04, FIG 2, DETAIL 2. 2 L 7 4 4F RT A20WE 2001111500180 20011115 00180 SO 2001 11 15 C2XA01IA398 1 20011106 A 3320 5113WW BULB EMB 145 EMB145 3260210 SO GALLEY MALFUNCTIONED A C2XA H DEACTIVATE SYST/CIRCUITS O OTHER CR CRUISE 1 SW 27 14972 145151 iah- during flight 3955 the crew noted a strong burning smell coming from the galley courtesy lights. IAH- MAINTENANC E REMOVED AND REPLACEDTHE GALLEY COURTESY LIGHT BULBS, PERFORMED A OPERATIONAL CHECK OF THE GALLEY LIGHTS, NO DEFECTS NO TED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001111600001 20011116 00001 WP 2001 11 16 AALA20011546 1 20010730 A 2910 HYDRAULIC LINE DOUG DC9 DC982 3022082 WP HYDRAULIC SYS CRACKED A AALA K NONE K J FLUID LOSS WARNING INDICATION LD LANDING 1 SW 21 259AA 49289 LAX - FLT 565 - UPON ARRIVAL LAX FROM AUS LOSS OF LEFT HYDRAULIC SYSTEM. LANDED LAX WITHOUT INCIDENT. REPLACED CRACKED HYDRAULIC LINE IN TAIL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001111600002 20011116 00002 WP 2001 11 16 0103969865 1 20010707 A 5400 FITTING DOUG DC9 DC951 3022051 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 774NC 47776 During SUV the lower beaver tail fitting on the no 2 pylon was found with corrosion on the upper and lower surfaces and 8 holes oversized. Discrepant beavertail is made from AISI 4340 steel forging.Repaired per EA 98-183737 2 L 7 2 4F RT A6WE 2001111600003 20011116 00003 WP 2001 11 16 0104009865 1 20010707 A 5400 FITTING DOUG DC9 DC951 3022051 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 774NC 47776 During SUV the upper beavertail fitting on the No 2 pylon was found with corrosion on the upper and lower surfaces. Fitt ing AISI steel forging. Repaired per EA 98-183738 2 L 7 2 4F RT A6WE 2001111600004 20011116 00004 WP 2001 11 16 0104019858 1 20010806 A 5400 FITTING DOUG DC9 DC951 3022051 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 767NC 47724 During SUV the upper beavertail fitting on the no 1 pylon was found with corrosion on the upper and lower surfaces. Made from AISI 4340 steel forging.Repaired per EA 98-170682. 2 L 7 2 4F RT A6WE 2001111600005 20011116 00005 WP 2001 11 16 0104029858 1 20010806 A 5400 FITTING DOUG DC9 DC951 3022051 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 767NC 47724 During SUV the lower beavertail fitting on the #1 pylon was found with corrosion on the upper and lower surfaces. Made f rom AISI 4340 steel forging.Repaired per EA 98-170683 2 L 7 2 4F RT A6WE 2001111600006 20011116 00006 WP 2001 11 16 0104039858 1 20010806 A 5310 FITTING DOUG DC9 DC951 3022051 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 767NC 47724 During SUV corrosion was found on the left wing to the body fitting which required the part to be replaced. Material 707 5-T651 Repaired per EA 98-186041. 2 L 7 2 4F RT A6WE 2001111600007 20011116 00007 WP 2001 11 16 0104049858 1 20010808 A 5400 FITTING DOUG DC9 DC951 3022051 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 767NC 47724 During SUV the lower beavertail fitting on the #2 pylon was found with corrosion on the upper and lower surfaces that re quired replacement. Material AISI 4340 steel forging. Repaired per EA 98-170684 2 L 7 2 4F RT A6WE 2001111600008 20011116 00008 WP 2001 11 16 0104059860 1 20010808 A 5330 SKIN DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 769NC 47757 During Line MTC in Atl, the fwd fuselage upper nose skin between the cut outs for the nose radome hinge sustained crack damage when the radome was raised.Repaired per EA98-185035. Material 2024-t3 .050" 2 L 7 2 4F RT A6WE 2001111600009 20011116 00009 WP 2001 11 16 0104069868 1 20010817 A 5530 HINGE DOUG DC9 DC951 3022051 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 777NC 47787 During Mck in Atl, two verticle stabilizer hinge plates for the horizontal stabilizer were found corroded. The right out board outer lug, and the right outboard inner lug had corrosion on the surface around the bore.Repaired per EA 98-185043 2 L 7 2 4F RT A6WE 2001111600010 20011116 00010 WP 2001 11 16 0104079868 1 20010821 A 5710 SPAR DOUG DC9 DC951 3022051 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 777NC 47787 During an Mck in ATL, corrosion was found in the left wing front spar web, around station XCW 32. THe corrosion is aroun d two holes in the web for the two harness leads. Material .090 7075-t6 aluminum clad sheet. Repaired per EA 98-185058 2 L 7 2 4F RT A6WE 2001111600011 20011116 00011 WP 2001 11 16 0104089868 1 20010821 A 5310 SUPPORT DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 777NC 47787 During MCK in ATL, A 1" long crack was found on the right nose landing gear support beam at sta 46. Repaired per EA. 98- 185066. 0.050 2024-t42 2 L 7 2 4F RT A6WE 2001111600012 20011116 00012 WP 2001 11 16 0104099868 1 20010821 A 5720 RIB DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 777NC 47787 During Mck in ATL, a 3" crack was found on the leading edge rib at station xrs 129. Material 7075-t6, repaired per EA 98 -185067 and SRM 57-02. 2 L 7 2 4F RT A6WE 2001111600013 20011116 00013 WP 2001 11 16 0104109868 1 20010821 A 5310 BULKHEAD DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 777NC 47787 During Mck in ATL, crack was found at the outboard end of the apb stiffener at Z=24 lh and rh. The crack is removed and the stiffener is repaired per EA 98-185074. Material 0.040" 2024-t42 2 L 7 2 4F RT A6WE 2001111600014 20011116 00014 WP 2001 11 16 0104119868 1 20010823 A 5310 BRACKET DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 777NC 47787 During MCK in ATL found crack .5" long at sta 69 bracket. .063 7075-t6. Repaired per EA 98-185053 2 L 7 2 4F RT A6WE 2001111600015 20011116 00015 EU 2001 11 16 AALA20011728 1 20010831 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 18066 509 JFK - DURING OVERNIGHT MAINTENANCE, FIRST CLASS RIGHT SEAT MOUNTED EMERGENCY LIGHT VERY DIM. REPLACED BATTERY PACK. SY STEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2001111600016 20011116 00016 WP 2001 11 16 AALA20011782 1 20010914 A 2910 HYDRAULIC LINE DOUG DC9 DC982 3022082 WP NR 1 ENGINE LOOSE A AALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 402A 49313 DFW - FLT 2260 - EN ROUTE DFW-ORD, DURING TAXI OUT, DETECTED SMOKE AND HAZE IN COCKPIT AND CABIN. RETURNED DFW GATE WIT HOUT FURTHER INCIDENT. REPLACED WATER SEPARATOR BAGS. TIGHTENED LEFT SIDE HYDRAULIC B-NUT LINE. PERFORMED PACK BURNOU T CHECK PER THE MM. NO SMELL OR SMOKE NOTED. LEAK CHECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001111600017 20011116 00017 WP 2001 11 16 AALA20011786 1 20010914 A 2910 HYDRAULIC LINE DOUG DC9 DC982 3022082 WP THRUST REVERSER LOOSE A AALA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 287AA 49299 MEM - FLT 1076 - EN ROUTE DFW-CLE, DETECTED DECREASE IN HYDRAULIC QUANTITY TO ZERO. TIGHTENED LEFT SIDE THRUST REVERSER CONTROL VALVE LINE. NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001111600018 20011116 00018 NM 2001 11 16 AALA20011821 1 20010926 A 3397 CONNECTOR BOEING 767 767323 1385205 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 387AM 27184 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 34H INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT CON NECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001111600019 20011116 00019 EU 2001 11 16 AALA20011822 1 20010926 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1444N 11447 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STRIP. SYSTEM GROUN D CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001111600020 20011116 00020 NM 2001 11 16 AALA20011831 1 20010929 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 798AN 30797 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT AT L1 DOOR DAMAGED. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001111600021 20011116 00021 NM 2001 11 16 AALA20011833 1 20010930 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 360AA 24041 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 17B INOPERATIVE. RE-SEATED EMERGENCY EXIT LIGHT PIN AT SIDE WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001111600022 20011116 00022 NM 2001 11 16 AALA20011837 1 20010930 A 2912 271T457018 MODULE BOEING 767 767223 1385123 NM HYDRAULIC SYS DEFECTIVE A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 304AA 22310 JFK - FLT 21 - EN ROUTE JFK-LAX - DETECTED LOSS OF CENTER HYDRAULIC SYSTEM FLUID. RETURNED JFK AND LANDED WITHOUT FURTH ER INCIDENT. REPLACED RIGHT CENTER PRESSURE FILTER BOWL MODULE. LEAK CHECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPERAT ION. (M) 2 L 7 2 4F RT A1NM 2001111600023 20011116 00023 EU 2001 11 16 AALA20011847 1 20011007 A 3350 2263778 LIGHT AIRBUS 300 A300B4605R 3930308 EU R3 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 19059 469 JFK - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT AT R3 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT R3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2001111600024 20011116 00024 EU 2001 11 16 AALA20011853 1 20011010 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU R2 DOOR LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7062A 474 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT R2 DOOR INOPERATIVE. RESECURED EMERGENCY EXIT LIGHT WIRE AT R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2001111600025 20011116 00025 NM 2001 11 16 AALA20011855 1 20011010 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39364 24045 LAX - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT AT FIRST CLASS GALLEY INOPERATIVE. REPAIRED EMERGENCY EXIT LIGH T WIRE AT FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001111600026 20011116 00026 WP 2001 11 16 AALA20011887 1 20010926 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7528A 49920 TUL - FOUND CORROSION ON CUSP STATION 1264 INBOARD, STATION 1271 TO STATION 1309 UNDER SEAT TRACK NR 1, CRACKED STATION 1292. REMOVED DAMAGED CUSP STATION 1250 TO 1309, INSTALLED SERVICEABLE CUSP SHEET STATION 1250-1309 SRM 53-01. (M) 2 L 7 2 4F A6WE 2001111600027 20011116 00027 WP 2001 11 16 AALA20011888 1 20010926 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7528A 49920 TUL - FOUND CORROSION ON CUSP STATION 1174 CORROSION ON BOTTOM SIDE OF CUSP 1174. INSTALLED NEW CUSP SHEET STATION 1174 -1250 LEFT SIDE SRM 53-01. (M) 2 L 7 2 4F A6WE 2001111600028 20011116 00028 WP 2001 11 16 AALA20011889 1 20010926 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7528A 49920 TUL - FOUND CRACK INDICATION AT LOWER RIGHT CANT 1485 UNDER STAIR RETRACT MECHANISM. INSTALLED REPAIR SPLICE AS PER AAR D 53-10-00-33. (M) 2 L 7 2 4F A6WE 2001111600029 20011116 00029 WP 2001 11 16 AALA20011890 1 20010926 A 5320 STRUCTURE DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7528A 49920 TUL - FOUND PUNCTURE HOLE, STATION 181 LBL 44.5. INSTALLED DOUBLER PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2001111600030 20011116 00030 WP 2001 11 16 AALA20011891 1 20010924 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7528A 49920 TUL - FOUND CRACK IN SKIN, L14L STATION 1380. STOP DRILLED AND INSTALLED DOUBLER PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2001111600031 20011116 00031 WP 2001 11 16 AALA20011892 1 20010921 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7528A 49920 TUL - FOUND CRACK IN LONGERON 4L AT FASTENER HOLE STATION 160. REMOVED DAMAGED SECTION OF LONGERON AND INSTALLED DOUBLE R REPAIR PER SRM 53-02. (M) 2 L 7 2 4F A6WE 2001111600032 20011116 00032 WP 2001 11 16 AALA20011893 1 20010921 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7528A 49920 TUL - FOUND NICKS, CUTS, SCRATCHES TOP FUSE STATION 200 TO 210 LONGERON 3L AND 4L. BLEND OUT DEEPEST CUT, NICK, SCRATCH 0.012 REQUIRED INTERNAL DOUBLER SRM 53-04 FIG 38. (M) 2 L 7 2 4F A6WE 2001111600033 20011116 00033 WP 2001 11 16 AALA20011894 1 20011001 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7528A 49920 TUL - FOUND CORROSION ON SEAT TRACK NR 2 STATION 1168-1264. REMOVED AND REPLACED SEAT TRACK STATION 1168-1264 PER SRM 5 3-05. (M) 2 L 7 2 4F A6WE 2001111600034 20011116 00034 WP 2001 11 16 AALA20011896 1 20011012 A 2150 CLAMP DOUG DC9 DC982 3022082 WP A/C BAY LOOSE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 7532A 49924 DFW - FLT 315 - AFTER TAKEOFF WHILE CLIMBING THROUGH 21,000 FEET, 'TAIL COMP TEMP HIGH' LIGHT ILLUMINATED. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. CLAMP AT LEFT HEAT EXCHANGER LEAKING. TIGHTENED CLAMP. GROUND CHECK NORMAL OPERATION . (M) 2 L 7 2 4F A6WE 2001111600035 20011116 00035 EU 2001 11 16 AALA20011898 1 20011014 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 41063 506 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 6C AND 14C INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT C ONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2001111600036 20011116 00036 NM 2001 11 16 AALA20011900 1 20011005 A 5320 SPLICE BOEING 727 727223 1384074 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 864AA 21369 TUL - FOUND STRINGER 27R SPLICE CRACKED AND CORRODED AT STATION 685. REMOVED CRACKED SPLICE AND REMOVED CORROSION FROM STRINGER AT STATION 675 AND 685. ALODINED AND PRIMED AREA. REPLACED SPLICE PER SRM 51-10-6. (M) 2 L 7 3 4F A3WE 2001111600037 20011116 00037 EU 2001 11 16 AALA20011901 1 20011014 A 2913 887031 PUMP FOKKER F28 F28MK0100 4990807 EU NR 2 ENGINE LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 1440A 11435 ORD - FLT 1828 - EN ROUTE ORD-YOW - SHORTLY AFTER TAKEOFF DETECTED LOW QUANTITY AND PRESSURE AT NR 2 HYDRAULICS SYSTEM. RETURNED ORD AND LANDED WITHOUT FURTHER INCIDENT. REPLACED NR 2 HYDRAULIC PUMP. NO LEAKS NOTED. SYSTEM GROUND CHECKE D NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001111600038 20011116 00038 NM 2001 11 16 AALA20011902 1 20011011 A 5320 INTERCOSTAL BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 864AA 21369 TUL - FOUND CORROSION ON LOWER END OF INTERCOSTAL O/B OF STRINGER 28L. REMOVED INTERCOSTAL, INSTALLED NEW INTERCOSTAL. REMOVED CORRODED SKIN BENEATH INTERCOSTAL, INSTALLED TRIPLER REPAIR PER SRM 53-30-3 INTERCOSTAL REMOVAL AND INSTALLATIO N PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 2001111600039 20011116 00039 NM 2001 11 16 AALA20011903 1 20011004 A 5730 SKIN BOEING 727 727223 1384074 NM CENTER WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 864AA 21369 TUL - FOUND CORROSION ON WING CENTER SKIN ABOVE LEFT PRIMARY HEAT EXCHANGER PLENUM STATION 900 LBL 28. INSTALLED DOUBLE R PER SRM 57-30-3. (M) 2 L 7 3 4F A3WE 2001111600040 20011116 00040 NM 2001 11 16 AALA20011904 1 20011004 A 5730 SKIN BOEING 727 727223 1384074 NM CENTER WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 864AA 21369 TUL - FOUND CORROSION CENTER WING SKIN ABOVE RIGHT PRIMARY HEAT EXCHANGER PLENUM STATION 903 RBL 30. REMOVED CORROSION AND INSTALLED REPAIRED DOUBLER PER SRM 57-30-3 FIG 10. (M) 2 L 7 3 4F A3WE 2001111600041 20011116 00041 NM 2001 11 16 AALA20011905 1 20011005 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 864AA 21369 TUL - FOUND CORROSION ON TOP OF FLOORBEAM STATION 400 OUTBOARD OF OUTBOARD SEAT TRACK AND AT SCREW HOLE. REMOVED CORROS ION TREATED AND PRIMED WITHIN LIMITS PER ECO 11697. (M) 2 L 7 3 4F A3WE 2001111600042 20011116 00042 NM 2001 11 16 AALA20011907 1 20011004 A 5320 FLOOR SUPPORT BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 864AA 21369 TUL - FOUND FLOOR SUPPORT JUST INSIDE OF FORWARD GALLEY DOOR CUTOUT IS CORRODED FROM BS 362-420. INSTALLED NEW Z-ANGLE AT FORWARD GALLEY DOOR STATION 352-420 PER 51-40-3. (M) 2 L 7 3 4F A3WE 2001111600043 20011116 00043 NM 2001 11 16 AALA20011908 1 20011005 A 5320 BRACKET BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 864AA 21369 TUL - FOUND LEFT PRIMARY HEAT EXCHANGER PLENUM ATTACH BRACKET CORRODED, FS 922. REMOVED ANGLE AND INSTALLED NEW ANGLE P ER 51-40-3. (M) 2 L 7 3 4F A3WE 2001111600044 20011116 00044 NM 2001 11 16 AALA20011909 1 20011005 A 5320 ANGLE BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 864AA 21369 TUL - FOUND FORWARD GALLEY DOOR SILL DRAINS HAVE CORROSION ON CREASE ANGLE STATION 409 TO STATION 410 AND STATION 373 TO STATION 375. REMOVED DRAIN FITTINGS AND CREASE ANGLE. INSTALLED NEW CREASE ANGLE AND REINSTALLED DRAIN FITTINGS PER S RM 51-40-1. (M) 2 L 7 3 4F A3WE 2001111600045 20011116 00045 NM 2001 11 16 AALA20011910 1 20011011 A 5320 INTERCOSTAL BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 864AA 21369 TUL - FOUND CORROSION ON LOWER FLANGE, FS 950F. INSTALLED INTERCOSTAL AT STRINGER 28R, STATION 950F PER 51-10-1. (M) 2 L 7 3 4F A3WE 2001111600046 20011116 00046 NM 2001 11 16 AALA20011911 1 20011010 A 5320 CHANNEL BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 864AA 21369 TUL - FOUND CORROSION ON INBOARD SIDE OF HAT CHANNEL AT STATION 1163 APPROX. REPLACED HAT CHANNEL AND INSTALLED DOUBLER PER SRM 51-40-2. (M) 2 L 7 3 4F A3WE 2001111600048 20011116 00048 NM 2001 11 16 AALA20011936 1 20011012 A 5320 SILL BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 864AA 21369 TUL - FOUND CORROSION BETWEEN UPPER AND LOWER SILL PLATES LOWER FORWARD CORNER OF AFT CARGO DOOR CUTOUT. REPAIRED IAW E SO 11697. (M) 2 L 7 3 4F A3WE 2001111600049 20011116 00049 NM 2001 11 16 AALA20011937 1 20011012 A 5313 STRINGER BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 864AA 21369 TUL - FOUND STRINGER CORRODED STATION 682-691 26R. REMOVED CORRODED STRINGER REPLACED PER ECO11697. (M) 2 L 7 3 4F A3WE 2001111600052 20011116 00052 NM 2001 11 16 AALA20011938 1 20011017 A 5320 STRINGER CLIP BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 864AA 21369 TUL - FOUND CORRODED STRINGER CLIP, FS 1007-1010. INSTALLED NEW STRINGER CLIP PER ESO 11697. (M) 2 L 7 3 4F A3WE 2001111600057 20011116 00057 EU 2001 11 16 AALA20011944 1 20011022 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU L4 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14061 471 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L4 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT L4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2001111600059 20011116 00059 EU 2001 11 16 AALA20011945 1 20011022 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU R1 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14061 471 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT R1 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT R1 DO OR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2001111600062 20011116 00062 2001 11 16 AALA20011946 4 20011023 A 3140 350B53005313 COMPUTER AIRBUS 300 A300B4605R 3930308 EU WARNING SYS FAULTY A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 7083A 645 JFK - FLT 587 - EN ROUTE JFK-SDQ, SHORTLY AFTER TAKEOFF CREW REPORTED FIRST CLASS LAVATORY SMOKE DETECTOR CAME ON. RETU RNED JFK AND LANDED WITHOUT FURTHER INCIDENT. REPLACED NR 1 FLIGHT WARNING COMPUTER. SYSTEM GROUND CHECKED NORMAL OPER ATION. (M) 2 L 7 2 4F RT A35EU 2001111600063 20011116 00063 WP 2001 11 16 0103939758 1 20011017 A 5310 PAD DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 758NW 47286 DURING A RON IN DTW, A CHAFE PAD LOCATED ON THE AFT DOOR JAMB ON THE RHS AFT EMERGENCY EXIT WAS FOUND CRACKED. IN SPITE OF THE DAMAGE, THE CHAFE WAS REPORTED SECURED TO THE STRUCTURE. EA 97-185229. 2 L 7 2 4F A6WE 2001111600064 20011116 00064 WP 2001 11 16 0103999961 1 20011027 A 5320 FITTING DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 924RW 47185 DURING SPECIAL VISIT IN ATL, APB TEE WAS FOUND CRACKED REQUIRING A SPLICE. EA 99-185258. 2 L 7 2 4F A6WE 2001111600068 20011116 00068 NM 2001 11 16 CALA0101001 1 20011113 A 5342 FITTING BOEING 737 7373T0 1384582 NM VERT STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59338 23576 INSPECTION FOUND VERTICAL STABILIZER ATTACH FITTING IN FUSELAGE CORRODED AT R/H AFT O/B FORWARD LUG AND AT L/H AFT O/B F ORWARD LUG. THE CORROSION WAS REMOVED AND AN OVERSIZE BUSHING WAS INSTALLED AT EACH LOCATION IAW ECRA 5340-01356. 2 L 7 2 4F RT A16WE 2001111600069 20011116 00069 NM 2001 11 16 CALA0101002 1 20011114 A 5753 SKIN BOEING 737 7373T0 1384582 NM FOREFLAP GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71314 23365 INSPECTION FOUND THE R/H O/B FOREFLAP L/E O/B EDGE WITH SEVERAL DEEP GOUGES IN SKIN. A REPAIR WAS INSTALLED IAW SRM 57-5 3-01. 2 L 7 2 4F RT A16WE 2001113000022 20011130 00022 NM 2001 11 30 01FDEA00983 1 20011113 A 5330 SKIN BOEING 727 7272S2F 1384O81 NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 201FE 22924 GOUGE AND DENT IN FUSELAGE SKIN AT BS 1310, STR 23L. REMOVED AND REPLACED REPAIR DOUBLER PER SRM 53-30-3 FIG 1. 2 L 7 3 4F A3WE 2001111600071 20011116 00071 NM 2001 11 16 01FDEA00984 1 20011113 A 5320 6517688160 SILL BOEING 727 7272S2F 1384O81 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 201FE 22924 CORROSION ON FWD ENTRY DOOR MOP SILL BS 344-328, LBL 55, WL 208. REMOVED AND REPLACED MOPSILL LT PER SRM 51-30-2. 2 L 7 3 4F A3WE 2001113000023 20011130 00023 NM 2001 11 30 01FDEA00985 1 20011113 A 5311 FRAME BOEING 727 7272S2F 1384O81 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 201FE 22924 SHARP DENT IN FRAME UPPER FLANGE BS 680, STR 24L. REMOVED AND REPLACED FRAME PER SRM 51-40-3. 2 L 7 3 4F A3WE 2001111600072 20011116 00072 WP 2001 11 16 01FDEA00986 1 20011114 A 7110 COWLING DOUG DC10 DC1010F 3022111 WP NR 3 T/R MISSING A FDEA K NONE O OTHER LD LANDING 1 SO 25 059FE 46907 NR 3 T/R OUTBOARD SIDE TRANSLATING COWL MISSING. 2 L 7 3 4F A22WE 2001111600074 20011116 00074 WP 2001 11 16 01FDEA00987 1 20010927 A 5311 AGA70983 FRAME DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 HEAVY CORROSION ON FRAME AFT SIDE X=60, Z=-96, BS 1841 LT. REMOVED AND REPLACED FRAME PER SRM 51-35-01 & 51-33-01. 2 L 7 3 4F RT A22WE 2001111600075 20011116 00075 WP 2001 11 16 01FDEA00988 1 20010830 A 5754 WEB DOUG DC10 DC1030F 3023504 WP L/E SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 CRACK NR 3 SLAT RT WING BS XO8 464 & CRACK IN WEB. REMOVED AND REPLACED WEB PER SRM 51-41-01 EA 8-5510-56177. 2 L 7 3 4F RT A22WE 2001111600076 20011116 00076 WP 2001 11 16 01FDEA00989 1 20011105 A 5311 AGA71253 FRAME DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 FRAME AT BS 1841 ABOVE LONGERON 43R CORRODED. REMOVED AND REPLACED FRAME PER SRM 51-35-01 & 51-33-01. 2 L 7 3 4F RT A22WE 2001111600077 20011116 00077 WP 2001 11 16 01FDEA00990 1 20011105 A 5311 AGA712513 FRAME DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 BS 1841, RBL 56R, WL -96 CORROSION ON FRAME ABOVE LONGERON 43R. REMOVED AND REPLACED CAP PER SRM 51-35-01. 2 L 7 3 4F RT A22WE 2001111600078 20011116 00078 WP 2001 11 16 01FDEA00991 1 20011105 A 5320 AGA717019 FLOOR SUPPORT DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 BS 1841, LBL 22 TO RBL -52, WL -93 ANGLE FLOOR SUPPORT IS CORRODED. REMOVED AND REPLACED ANGLE PER SRM 51-35-01 & 51-33 -01. 2 L 7 3 4F RT A22WE 2001111600079 20011116 00079 WP 2001 11 16 01FDEA00992 1 20011105 A 5320 SUPPORT DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 BS 1841, LBL 54 TO RBL 54 BELOW AFT FLOOR ROLLER TRAY SUPPORT IS CORRODED. REMOVED AND REPLACED SUPPORT PER SRM 51-35-0 1 & 51-33-01. 2 L 7 3 4F RT A22WE 2001111600080 20011116 00080 NE 2001 11 16 2001F00637 2 20011114 A 7200 PT6A67B ENGINE PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE ENGINE MAKING METAL E S4WA K NONE O OTHER IN INSP/MAINT 1 WP 07 562NA 2816 174 PR0027 ENGINE OIL ANALYSIS SHOWED A CLIMBING TREND IN MAGNESIUM AND IRON AMOUNTS. AFTER THREE SAMPLES, IN ACCORDANCE WITH MANU FACTURER, REMOVED AND SENT ENGINE TO THEM FOR INSPECTION AND REPAIR. 1 L 7 1 3T 4 T RT A78EU E26NE 2001111600081 20011116 00081 WP 2001 11 16 ABXA010584 1 20011113 A 2740 RELAY DOUG DC9 DC941 302207N WP HORIZ STAB MALFUNCTIONED A ABXA K NONE F FLT CONT AFFECTED DE DESCENT 1 GL 23 951AX 47616 DURING DESCENT, ALTERNATE LONGITUDINAL TRIM RAN AWAY. AUTOPILOT AND ALTERNATE TRIM CIRCUIT BREAKERS PULLED. COULD NOT DUPLICATE ON GROUND. REPLACED ALTERNATE TRIM BRAKE RELAY R20-14 AND UP AND DOWN RELAYS R20-12 AND R20-13 AS A PRECAUTIO N. OPS CHECKED GOOD IAW DC-9 MM 27-40-00-2. 2 L 7 2 4F A6WE 2001112000097 20011120 00097 NE 2001 11 20 ARWA20011103 2 20011113 A 7200 ENGINE LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B402 54555 NE NR 2 VIBRATION A ARWA E ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SO 19 260FA 57889 9292 1158 14734 SHUTDOWN NR 2 ENGINE AFTER EXPERIENCING VIPS SPIKE 3.0 BOTH CHANNELS AT APPOX 2325Z. 2 L 7 3 4F 4 F A23WE E12EU 2001111600087 20011116 00087 NM 2001 11 16 AWXA200100581 1 20011027 A 5315 6546568107 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 MCN - C13 CK - C - CORROSION FOUND ON FLOORBEAM UPPER FLANGE AT BS 1016, LBL 41 TO RBL 40, (PREVIOUSLY REPAIRED), FOUND TO BE OUT OF LIMITS AFTER CORROSION REMOVAL. MAINTENANCE REMOVED CORRODED UPPER FLANGE, FABRICATED REPAIR PARTS AND INS TALLED IAW AWA ER 15-5365-01309-TB3. 2 L 7 2 4F RT A16WE 2001111600092 20011116 00092 NM 2001 11 16 AWXA200100583 1 20011025 A 5230 654692124 CROSSBEAM BOEING 737 737277 1384570 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 MCN - C13 CK - C - FWD CARGO DOOR LOWER CROSSBEAM TEE VERTICAL LEG CRACKED (.7 INCH), BS 487. MAINTENANCE REPAIRED IAW AWA EO 52-31-04, WHICH INCORPORATES BOEING SB 737-52-1100, REV 4. 2 L 7 2 4F RT A16WE 2001111600094 20011116 00094 NM 2001 11 16 AWXA200100584 1 20011029 A 5311 65465391 FRAME BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 MCN - C13 - C - CRACK FOUND IN VERTICAL FRAME INNER CHORD (1.125 INCH) AT BS 616, LBL 60, WL 200. MAINTENANCE CUT OUT D AMAGED AREA, FABRICATED REPAIR FILLER AND STIFFENER ANGLE AND INSTALLED IAW AWA ER 15-5311-01143-DD2. 2 L 7 2 4F RT A16WE 2001111600095 20011116 00095 NM 2001 11 16 AWXA200100586 1 20011114 A 3040 5893543130 WINDSHIELD BOEING 737 7373G7 1384595 NM COCKPIT ARCED A AWXA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 156AW 22441 23778 LAS - DIVERTED FLIGHT - FLT 771 - C - EN ROUTE FROM PHX TO SMF THE RT FWD (FIRST OFFICER'S NR 1) WINDOW STARTED ARCHING ALONG THE TOP OF THE WINDOW, THE WINDOW HEAT WAS ON AT THE TIME. THE CREW TURNED THE WINDOW HEAT OFF AND REDUCED CABIN PRESSURE IAW THE QRH AND DIVERTED TO LAS. IN LAS MAINTENANCE REPLACED THE FIRST OFFICER'S NR 1 WINDOW IAW AWA TASK CARD R1B56001. THE ASSOCIATED WINDOW HEAT CONTROLLER WAS ALSO REPLACED AS A PRECAUTION. NO FURTHER DISCREPANCIES HAVE BEEN REPORTED.NAME: WINDOW HEAT CONT. UNIT - MFG: PACIFIC ELECTRO DYNAMICS - P/N: 231-2 - S/N: 2932 - COND: PRECAUTIONARY - LOC: MAIN ELEC COMP - TT: 55050 - TC: 43082 - TSR: 2091. 2 L 7 2 4F RT A16WE 2001111600097 20011116 00097 NM 2001 11 16 AWXA200100587 1 20011011 A 5330 654577560 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - C13 CK - C - CRACK FOUND IN FUSELAGE SKIN IN A CREASE AT BS 912, BETWEEN STR 24R & 25R, .75 INCH LONG. MAINTENANC E REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW B737 SRM 53-00-01, FIG 202, PG 204 - 206. 2 L 7 2 4F RT A16WE 2001111600100 20011116 00100 EA 2001 11 16 COMA0160897 1 20011115 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 956CA 13773 7105 LEFT LOWER WING CUT OUT AT 540 FB CRACKED.BLENDED OUT DAMAGE AND ROTOPEENED I/A/W REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 2001111600101 20011116 00101 EA 2001 11 16 COMA0160898 1 20011115 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 956CA 13773 7105 LEFT LOWER WING CUT OUT AT 550AB CRACKED.BLENDED OUT DAMAGE AND ROTO-PEENED I/A/W REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 2001111600105 20011116 00105 NE 2001 11 16 DHL2001801014 2 20011110 A 7260 GARLOCK SEAL DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE NR 1 ENGINE LEAKING A DHLA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 801DH 46033 ENG NR 1 SHUTDOWN - OIL QUANTITY AT 2 QUARTS WITH SLIGHT FLUCTUATION IN PRESSURE - 1 TO 2 POUNDS. FOUND STARTER PAD LE AKING. REMOVED STARTER, REPLACED GARLOCK SEAL & ASSOCIATED O-RINGS, REINSTALLED STARTER PER 80-10-00. PERFORMED RUN, N O LEAKS NOTED. 2 L 7 4 4F 4 F RT 4A25 E2GL 2001111600106 20011116 00106 EA 2001 11 16 COMA0160899 1 20011115 A 5346 60135006 BEAM CNDAIR CL600 CL6002B19 1900309 EA AFT EQUIPMENT BA CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 956CA 13773 7105 ENGINE SUPPORT BEAM UPPER WEB CRACKED.REPAIRED I/A/W REO 601R-53-61-345. 2 L 7 2 4F RT A21EA 2001111600107 20011116 00107 WP 2001 11 16 DHL2001802016 1 20011109 A 2611 CONTACTOR DOUG DC8 DC873 302199C WP SMOKE DETECTOR DIRTY A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 802DH 46076 REF 7682; SPOT NR 14 SMOKE DETECTOR WILL NOT TEST. T/S, CLEANED CONTACTS AT DETECTOR AND OPS CK'D OK PER MM 26-10-0. 2 L 7 4 4F RT 4A25 2001111600108 20011116 00108 WP 2001 11 16 DHL2001803018 1 20011107 A 2510 SEAT DOUG DC8 DC873 302199C WP COCKPIT LACK OF LUBE A DHLA O OTHER O OTHER UK UNKNOWN 1 SO 01 803DH 46123 CAPTAIN'S SEAT SLIPS OUT OF VERTICAL POSITION. LUBED SEAT, OPS CHECK GOOD IAW MM 25-11-1. 2 L 7 4 4F RT 4A25 2001111600110 20011116 00110 WP 2001 11 16 DHL2001807027 1 20011109 A 2612 CONNECTOR DOUG DC8 DC873F 302199F WP FIRE LOOP DIRTY A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 807DH 45990 NR 4 ENGINE SHORT LIGHT REMAINS ILLUMINATED WHEN SELECTED. CLEANED CONNECTORS AT BOTH FAN SECTION FIRE LOOPS SYS TEST N ORMAL IAW 26-10-01. 2 L 7 4 4F RT 4A25 2001111600114 20011116 00114 WP 2001 11 16 GTIA010981 1 20010604 A 5730 PANEL DOUG DC9 DC982 3022082 WP RT WING DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - RIGHT WING INBOARD AFT LOWER PANEL DELAMINATED. REMOVED DELAMINATION IAW MD-80 SRM 51-90-0 PAR 5. REPAIRED DELAM INATION AREA IAW MD-80 PAR 8 SRM 51-90-0. (M) 2 L 7 2 4F A6WE 2001111600118 20011116 00118 WP 2001 11 16 GTIA010984 1 20010627 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - CORROSION FOUND UNDER L-1 DOOR THRESHOLD. ITEM FOUND DURING MOON MAT INSTALLATION. FABRICATED NEW FLOOR SUPPORT IAW MD80 SRM 57-10-01. INSTALLED FLOOR SUPPORT IAW SRM MD-80 SRM 57-10-01. INSTALLED FLOOR SUPPORT IAW SRM MD-80 51-30 -2. (M) 2 L 7 2 4F A6WE 2001111600122 20011116 00122 WP 2001 11 16 GTIA010985 1 20010521 A 5230 DOOR FRAME DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FORWARD CARGO DOOR, LOWER STOPS FRAME CRACKED IN FOUR PLACES. STOP DRILL CRACK, FORMER AND LOCATED DRILL IAW MD-8 0 SRM 52-03. INSTALLED REPAIR DOUBLER IAW SRM MD-80 52-30-0. (M) 2 L 7 2 4F A6WE 2001111600128 20011116 00128 EA 2001 11 16 COMA0160900 1 20011115 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 956CA 13773 7105 RIGHT LOWER WING CUT OUT AT 650 AB CRACKED.BLENDED OUT DAMAGE AND ROTO-PEENED I/A/W REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 2001111600129 20011116 00129 WP 2001 11 16 GTIA010989 1 20010705 A 2760 WIRE DOUG DC9 DC982 3022082 WP SPOILER SYS BROKEN A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 803NK 48087 FTW - SPOILER DEPLOYED LIGHTS INOPERATIVE. T/S SYSTEM FOUND OPEN WIRE BETWEEN R2-292 (2) AND R2-241 (D2). REPLACED WIR E IAW MD80 WDM 27-66-00 AND MD-80 MM 20-50-03. (M) 2 L 7 2 4F A6WE 2001111600131 20011116 00131 EA 2001 11 16 COMA0160901 1 20011115 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 956CA 13773 7105 RIGHT LOWER WING CUT OUT AT 650 BB CRACKED.BLENDED OUT DAMAGE AND ROTO-PEENED I/A/W REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 2001111600135 20011116 00135 EA 2001 11 16 COMA0160902 1 20011115 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 956CA 13773 7105 RIGHT LOWER WING CUT OUT AT 640 C B CRACKED.BLENDED OUT DAMAGE AND ROTO-PEENED I/A/W REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 2001111600136 20011116 00136 EA 2001 11 16 COMA0160903 1 20011114 A 2720 6229968001 DAMPENER CNDAIR CL600 CL6002B19 1900309 EA EMPENNAGE MALFUNCTIONED A COMA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SO 01 783CA 5391 7315 FLIGHT #5437 - AIRCRAFT HAS SIDE TO SIDE YAWING MOTION.REPLACED THE #1 YAW DAMPENER. 2 L 7 2 4F RT A21EA 2001111600138 20011116 00138 EA 2001 11 16 COMA0160904 1 20011114 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA CABIN BURNED OUT A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 915CA 7013 FWD CABIN, CEILING EMERGENCY LIGHT, IS INOP.REPLACED LIGHT BULB. 2 L 7 2 4F RT A21EA 2001111600141 20011116 00141 NM 2001 11 16 UPS01437285 1 20011101 A 5310 141U11075 WEB BOEING 747 747200 1384847 NM LH SIDE NWW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C L/H SIDE NWW AT BS 300 VERTICAL BEAM WEB FOUND ONE EACH STANDOFF HOLE CRACKED JUST BETWEEN #1 AND #2 S TIFFENER ( COUNTED FROM TOP ) AS MARKED. NEW VERTICAL WEB INSTALLED AS PER SRM 51-30-02 2 L 7 4 4F RT A20WE 2001111600142 20011116 00142 WP 2001 11 16 IXXA0100072O 1 20011115 A 2130 LINKAGE DOUG DC8 DC862 3021970 WP TAIL DRY A IXXA B EMER. DESCENT O OTHER CL CLIMB 1 SW 11 41CX 72154 2076 46129 DURING CLIMB FROM QPG TO DNA, THE FLIGHT CREW WAS UNABLE TO MAINTAING CABIN PRESSURIZATION. THE FLIGHT CREW DECLAIRED AN D EMERGENCY AND FOLLOWED COMPANY PROCEDURES AND RETURNED TO QPG FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIR CRAFT WITH NO DISCREPANCIES NOTED. MAINTENANCE LUBRICATED THE OUTFLOW VALVE LINKAGE AND PERFOMRED A SUCCESSFUL OPERATION AL CHECK IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2001111600143 20011116 00143 WP 2001 11 16 IXXA0100073O 1 20011115 A 2900 LINE DOUG DC8 DC862 3021970 WP WHEEL WELL LOOSE A IXXA O OTHER K FLUID LOSS CL CLIMB 1 SW 11 31CX 73645 320 45911 ENROUTE FROM AKJ TO AVB, THE FLIGHT CREW NOTICED A DECLINE IN THE MAIN HYDRAULIC QUANTITY SYSTEM. THE FLIGHT CREW FOLLOW ED COMPANY PROCEDURES AND CONTINUED TO AVB FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECT THE AIRCRAFT LOCATING A LOOSE LINE ON THE RIGHT MAIN HYDRAULIC MANIFOLD. MAINTENANCE SECURED THE LINE AND PERFORM A SUCCESSFUL OPERATIONAL CHECK IN AC CORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2001111600144 20011116 00144 NM 2001 11 16 QXEA0101905 1 20011111 A 3230 54C546349 SOLENOID VALVE DHAV DHC8 DHC8202 2809007 NM DEFECTIVE A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 346PH 11113 11113 477 SEA - AFTER TAKE OFF THE RIGHT DOOR YELLOW LIGHT WAS ON. AFTER GEAR HANDLE WAS DOWN, LEFT MAIN GEAR AND NOSE GEAR WAS DO WN, RIGHT MAIN GEAR STAYED UP. USED ALTERNATE EXTENSION METHOD 1. GOT THREE GREENS AND THREE YELLOW LIGHTS. THE RIGHT YE LLOW AND RIGHT DOOR LIGHT ON WAS NOTICED AT APPROXIMATELY 170 KNOTS INDICATED AIRSPEED. SLOWED AIRCRAFT TO 148 KNOTS IND ICATED AIRSPEED. REMOVED AND REPLACED DEFECTIVE SOLENOID SEQUENCE VALVE. ACCOMPLISHED OVERSPEED EXTENSION INSPECTION ON RIGHT GEAR IAW TASK O5-50-32-280-801. COMPLIED WITH OPERATIONAL CHECK OF LANDING GEAR EXTENSION AND RETRACTION. OPERATIO NAL CHECK IS GOOD. COMPLIED WITH REQUIRED INSPECTION ITEM FOR GEAR SWINGS. 2 H 7 2 4T RT A13NM 2001111600145 20011116 00145 SO 2001 11 16 C2XA01BT176 1 20011115 A 5500 NA RUDDER EMB 145 EMB145LR 3260212 SO RUDDER CRACKED A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 13908 145465 BTV---CO3389, DURING 2A INSPECTION MAINTENANCE FOUND #2 RUDDER ON RIGHTHAND LOWER SIDE IS CRACKED AND HAS A HOLE IN IT.. ....MAINTENANCE REMOVED DAMAGED AREA ON #2 RUDDER RIGHTHAND LOWER SECTION. FABRICATED NEW SKIN PART AND EXTERNAL STRAPS IAW EC5540-01015. INSTALLED NEW SKIN PART AND EXTERNAL STRAPS IAW EC5540-01015. SEALED AND PAITED REPAIRED AREA IAW EC55 40-01015. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2001111600146 20011116 00146 NM 2001 11 16 QXEA0101906 1 20011115 A 3350 6104781 BATTERY DHAV DHC8 DHC8202 2809007 NM INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 5499 55 520 PDX - TWO RED EMERGENCY EXIT TRACK LIGHTS ARE INOPERATIVE AT THE FORWARD EXIT ROW. REPLACED BATTERY PACK. OPERATIONAL CH ECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001111600147 20011116 00147 WP 2001 11 16 GTIA010990 1 20010530 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FORWARD CARGO DOOR LOWER FRAME INTERCOSTAL WEB AND ANGLE ON RIGHT SIDE IS CRACKED UNDER FORWARD STOP. REMOVED DAM AGED INTERCOSTAL WEB IAW MD-80 SRM 51-30-2. FABRICATED WEB. REMOVED ANGLE. DRILL AND LOCATE NEW ANGLE. INSTALLED NEW ANGLE. (M) 2 L 7 2 4F A6WE 2001111600148 20011116 00148 WP 2001 11 16 GTIA010994 1 20010604 A 5520 EYEBOLT DOUG DC9 DC982 3022082 WP ELEVATOR BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - LEFT ELEVATOR NR 6 HINGE, EYE-BOLT IS BROKEN. INSTALLED EYE BOLT NR 6 IAW MD80 MM 27-30-00. (M) 2 L 7 2 4F A6WE 2001111600149 20011116 00149 WP 2001 11 16 GTIA010995 1 20010612 A 5754 RIB DOUG DC9 DC982 3022082 WP L/E SLAT CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND CRACKED RIB AT NR 3 SLAT INBOARD OF PULLEY. REMOVED RIVETS, INSTALLED COMPLETE IAW SRM MD-80 57-01. (M) 2 L 7 2 4F A6WE 2001111600150 20011116 00150 WP 2001 11 16 GTIA011002 1 20010508 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - DENT AT LEFT STATION 110 6 FT BELOW L1 DOOR HOLD OPEN. FOUND DENT OUT OF LIMITS. REMOVED DAMAGED AREA, LOCATED A ND DRILLED. INSTALLED DOUBLER AND FILLER IAW MD-80 SRM 53-04. (M) 2 L 7 2 4F A6WE 2001111600151 20011116 00151 WP 2001 11 16 GTIA011004 1 20010508 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - INTERIM REPAIR LEFT STATION 237 L17 AND L18 INSTALLED IAW EA 00-53-029. REMOVED INTERIM REPAIR. CUT OUT DAMAGED AREA. FABRICATED DOUBLER FILLER. LOCATED AND DRILLED NEW FRAME SUPPORT SRM 53-04. (M) 2 L 7 2 4F A6WE 2001111600152 20011116 00152 WP 2001 11 16 GTIA011009 1 20010708 A 3830 PUMP DOUG DC9 DC982 3022082 WP LAVATORY FAILED A GTIA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 GL 23 803NK 48087 FTW - RIGHT AFT LAVATORY SMOKE DETECTOR SOUNDS WHEN ENGINE POWER IS APPLIED. NOTED STRONG SMELL OF EXHAUST FUMES AND LA V WILL NOT FLUSH. REPLACED PUMP ON RIGHT AFT LAV IAW MD80 MM 38-30-00. (M) 2 L 7 2 4F A6WE 2001111600153 20011116 00153 WP 2001 11 16 GTIA011010 1 20010709 A 2611 SMOKE DETECTOR DOUG DC9 DC982 3022082 WP CARGO BAY FAULTY A GTIA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 23 803NK 48087 FTW - FORWARD PIT CARGO SMOKE DETECTOR FORWARD A AND AFT PIT CARGO B. T/S SYSTEM FOUND TWO BAD SMOKE DETECTOR IN FORWAR D CARGO BAY AND IN AFT CARGO BAY IAW BARFIELD MM 26-22-00. REMOVED AND REPLACED BAD SENSOR IAW BARFIELD SMOKE DETECTOR MM 26-22-00. (M) 2 L 7 2 4F A6WE 2001111600154 20011116 00154 WP 2001 11 16 GTIA011014 1 20011020 A 2740 D17751 TRIM MOTOR DOUG DC9 DC982 3022082 WP HORIZ STAB INOPERATIVE A GTIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 GL 23 816NK 49140 ACY - ALT TRIM INOPERATIVE. REMOVED AND REPLACED ALT TRIM MOTOR, OPS CHECK GOOD IAW 27-40-01. (M) 2 L 7 2 4F A6WE 2001111600155 20011116 00155 WP 2001 11 16 GTIA011017 1 20011023 A 3397 WIRE DOUG DC9 DC981 3022081 WP CABIN ARCED A GTIA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 23 818NK 48018 ACY - EMERGENCY FLOOR PATH LIGHTING ARCING DURING GROUND TEST. REPAIRED AND REPLACED WIRES AND LIGHT STRIP ON EMERGENCY FLOOR PATH LIGHTING IAW 33-53-01, OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2001111600156 20011116 00156 WP 2001 11 16 GTIA011018 1 20010906 A 3597 WIRE DOUG DC9 DC981 3022081 WP PAX OXYGEN CHAFED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 811NK 48017 FTW - OXYGEN MASK DROP TEST FAILED. T/S SYSTEM FOUND WIRES GOING TO CONNECTOR P1-1209 CHAFING. REPAIRED WIRES IAW OPS 20-10-01 SYSTEM TAKEOFF GROUND TEST GOOD IAW MD80 MM 35-20-00. (M) 2 L 7 2 4F A6WE 2001111600157 20011116 00157 WP 2001 11 16 GTIA011021 1 20010829 A 7120 7938004523 ISOLATOR DOUG DC9 DC981 3022081 WP RT PYLON GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - RIGHT PYLON FORWARD UPPER VIBRATION ISOLATOR HAS GOUGES ON INTERIOR SURFACE. REMOVED RIGHT PYLON FORWARD UPPER VI BRATION ISOLATOR P/N 7938004-523 S/N 3823 IAW MD80 MM 71-20-02. INSTALLED NEW UPPER ISOLATORS IAW MD80 MM 71-20-03. (M ) 2 L 7 2 4F A6WE 2001111600158 20011116 00158 WP 2001 11 16 GTIA011022 1 20011024 A 7120 ISOLATOR DOUG DC9 DC981 3022081 WP LT PYLON GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - LEFT PYLON FORWARD UPPER VIBRATION ISOLATOR IS GOUGED. REMOVED LEFT FORWARD UPPER VIBRATION ISOLATOR PER MD80 MM 71-20-02. INSTALLED LEFT FORWARD UPPER VIBRATION ISOLATOR PER MD80 MM 71-20-02. (M) 2 L 7 2 4F A6WE 2001111600159 20011116 00159 WP 2001 11 16 GTIA011026 1 20010815 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - WEB CORRODED AT FRAME FUSELAGE STATION 1412 LOWER AREA. REMOVED CORROSION FROM WEB IAW MD80 SRM 51-10-3. WEB FOU ND TO BE OUT OF LIMITS IAW MD80 SRM 53-01. FABRICATED NEW WEB IAW MD80 SRM 53-14-4. INSTALLED WEB AT STATION 1412 IAW M X80 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 2001111600160 20011116 00160 WP 2001 11 16 GTIA011030 1 20010901 A 3397 WIRE DOUG DC9 DC981 3022081 WP CABIN BROKEN A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 811NK 48017 FTW - R1 DOOR EMERGENCY DOOR LIGHT INOPERATIVE. TROUBLESHOT AND FOUND WIRE BROKEN WIRE AT EMERGENCY LIGHT. RESPLICED W IRE AT LIGHT IAW MD80 WDMSP 20-10-03. OPS CHECK GOOD IAW MD80 MM 33-53-00. (M) 2 L 7 2 4F A6WE 2001111600161 20011116 00161 WP 2001 11 16 GTIA011031 1 20010814 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - AFT LOWER CARGO COMPARTMENT, CORROSION AT FLOOR SUPPORT STATION 1211. FLOOR SUPPORT 1211 WAS FOUND TO BE OUT OF L IMITS. REMOVED FLOOR SUPPORT STATION 1211. INSTALLED AFT CARGO FLOOR SUPPORT STATION 1211 IAW MD80 SRM 51-30-2 AND 51- 30-5. (M) 2 L 7 2 4F A6WE 2001111600164 20011116 00164 SO 2001 11 16 RAIA00111007 1 20011109 A 2460 F0006 FUSE EMB 145 EMB145LR 3260212 SO A RAIA A UNSCHED LANDING G MULTIPLE FAILURE TO TAKEOFF 1 CE 03 812HK 145373 5273-RIC-CREW REPORTED DC BUSS #2 FAILURE, #2 ENGINE POWER LOSS, AND #1 HYDRAULIC SYSTEM FAILURE. MAINTENANCE TROUBLESHO T AND FOUND THE #2 DC BUSS FUSE BLOWN AND REPLACED FUSE IAW EMB 145 MM. 2 L 7 2 4T RT T00011AT 2001111600165 20011116 00165 EU 2001 11 16 RAIA00111008 1 20011109 A 7700 3036927 SIGNAL COND UNIT AEROSP ATR42 ATR42300 8680920 EU INOPERATIVE A RAIA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 CE 03 423TE 18706 16040 119 7490-STL- CREW REPORTED #1 PROP WOULD NOT FEATHER DURING AUTOMATIC TAKE - OFF POWER CONTROL SYSTEM TEST. MAINTENANCE TRO UBLESHOT AND REMOVED AND REPLACED THE TORQUE SIGNAL CONDITIONER IAW. ATR42 MM 2 H 7 2 4T RT A53EU 2001111600166 20011116 00166 EU 2001 11 16 RAIA00111009 1 20011111 A 3350 255010 FUSE JETAIR JETSTM JETSTM4101 1500501 EU A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 565HK 41082 7492-STL-1 ST SECTION OF INTERIOR EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED FUSE AT THE EMERGENC Y LIGHT POWER SUPPLY. 2 L 7 2 4T RT A41NM 2001111600167 20011116 00167 EU 2001 11 16 RAIA00111011 1 20011113 A 3350 AD3127 BATTERY AEROSP ATR42 ATR42300 8680920 EU DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 423TE 5134 303 119 MX-STL- FLOOR EMERGENCY EXIT LIGHTS WILL NOT TEST. MAINTENANCE REMOVED AND REPLACED #1 EMERGENCY LIGHT BATTERY 2 H 7 2 4T RT A53EU 2001111600168 20011116 00168 SO 2001 11 16 RAIA00111012 1 20011114 A 7920 23056413 LINE EMB 145 EMB145 3260210 SO A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 805HK 145096 5268-PIT- CREW REPORTED #2 ENGINE LOW OIL PRESSURE WARNING. MAINTENANCE FOUND CHAFED OIL FEED LINE AND REMOVED AND REPLA CED LINE IAW EMB 145 MM. 2 L 7 2 4F RT T00011AT 2001111800001 20011118 00001 NM 2001 11 18 S01271035 1 20011111 A 7100 OIL SYSTEM BOEING 747 747209B NM PWA JT9 JT9D7A 52054 NE # 1 ENG W SAJF E ENGINE SHUTDOWN M OVER TEMP CL CLIMB 1 WP 03 21454 695832 B-18751 # 1 ENG BREATHER TEMP REACH 220 DEG C DURING CLB. OIL TEMP HIGH BUT OIL TEMP INCREASE GRADUALLY TO AMBER BAND. T HEN OIL QTY DROP DOWN TO ZERO. ENG IN FLT S/D. C/A:1.REPLENISHED # 1 ENG OIL TO NORMAL LEVEL THEN MOTORING CK FOUND OIL LEAKING FROM LH # 3 BEARING AIR VENT TUBE AND MUCH BLACK OIL OF # 1 ENG TAIL PIPE. 2.PERFORMED INSPECTION OF M.C.D. AND OIL FILTER FOUND A LOT OF OIL MUD AROUND THERE. 3.PERFORMED # 1 ENG CHANGE, ENG ON S/N:695746 DELIVERED VIA CI-341/TPE-S IN. 4.PERFORMED # 1 ENG RUN UP TEST NORMAL. 2 L 7 4 4F 4 F RT A20WE E20EA 2001111900003 20011119 00003 NM 2001 11 19 0104206718 1 20011108 A 3310 WIRE BOEING 747 747251F 1384898 NM CAPT GLARESHIELD BURNED A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 01 618US 21122 DURING FLIGHT, A STRONG ELECTRICAL FUME EMITTED IN THE COCKPIT. REMOVED CAPTAIN'S FLUORESCENT GLARESHIELD LIGHTS AND FUM ES DISSIPATED. AIRCRAFT CONTINUED TO DESTINATIONA AND LANDED WITHOUT INCIDENT. REPLACED WIRE AT CAPTAIN'S GLARESHIELD LIGHT. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2001111900011 20011119 00011 WP 2001 11 19 GTIA010987 1 20010521 A 3830 DRAIN MAST DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - E/E BAY, STATION 200 LONGERON 29R, WASTE WATER DRAIN HAS CORROSION. REMOVED CORROSION. VERIFIED OUTER OF LIMITS. FABRICATED NEW DOUBLER. INSTALLED DOUBLER IAW MD-80 SRM 51-30-02. (M) 2 L 7 2 4F A6WE 2001111900014 20011119 00014 NM 2001 11 19 01FDEA00998 1 20011116 A 3200 69553584 LINK BOEING 727 727233 138408A NM LEFT WING INADEQUATE A FDEA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 25 282FE 22349 N 1322 AFTER T/O GEAR HANDLE WOULD NOT GO UP. R&R SENSOR TARGET & GROUND SPOILER ON LINKAGE PER MM 32-09-221-5, 27-62-0 51-5. 2 L 7 3 4F RT A3WE 2001111900015 20011119 00015 NM 2001 11 19 SWAA013064 1 20011111 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 712SW 27846 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS CRACKED AT ROWS 1, 7, 18, 19, 20, & 23. R&R COVE RS PER MM. 2 L 7 2 4F RT A16WE 2001111900016 20011119 00016 NM 2001 11 19 SWAA013065 1 20011111 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 706SW 27840 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS BROKEN ( 4 EA ) IN CABIN. R&R COVERS PER MM. 2 L 7 2 4F RT A16WE 2001111900017 20011119 00017 NM 2001 11 19 SWAA013073 1 20011110 A 5312 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED 1.0 INCH LONG AT BS 179, WL 182 & LBL 17.0. REPAIRED WEB PER SWA RA 1-353-2712. 2 L 7 2 4F RT A16WE 2001111900018 20011119 00018 NM 2001 11 19 SWAA013074 1 20011112 A 5312 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 331SW 23695 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEBS CRACKED ( 2 EA ) AT BS 179, WL 227, RBL 17.1 & LBL 17.1. R&R WEBS PER SRM. 2 L 7 2 4F RT A16WE 2001111900019 20011119 00019 NM 2001 11 19 SWAA013075 1 20011111 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 378SW 26585 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR LWR EMERGENCY EXIT LIGHT LENS BROKEN. R&R EXIT LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2001111900020 20011119 00020 NM 2001 11 19 SWAA013077 1 20011109 A 5312 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 331SW 23695 DURING SCHEDULED SPECIAL VISIT FOUND VERTICAL BEAM WEB CRACKED AT BS 180, RBL 17.1 & WL 180. R EPAIRED WEB PER SWA RA 1-353-2716. 2 L 7 2 4F RT A16WE 2001111900021 20011119 00021 NM 2001 11 19 SWAA013078 1 20011112 A 2612 65582343 DETECTOR BOEING 737 7372H4 138448C NM CFM56 CFM56* 13802 NE # 2 ENGINE ERRATIC A SWAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SW 07 092SW 22964 707328 ( ENGINE SHUTDOWN, DECLARED EMERGENCY )……………………….DURING FLIGHT # 2 ENGINE FIRE WARNING LIGHT ILLUMINATED & BELL SOUNDED. R&R # 2 ENG LOWER FIRE OVERHEAT DETECTOR PER MM. 2 L 7 2 4F 4 F A16WE E2GL 2001111900022 20011119 00022 NM 2001 11 19 SWAA013080 1 20011113 A 5753 6546435 FLAP BOEING 737 7375H4 138449D NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 513SW 24190 DURING SCHEDULED C2 CHECK, FOUND LT OTBD AFT FLAP DELAMINATED AT LOWER SURFACE INBD END. R&R FLAP PER MM. 2 L 7 2 4F RT A16WE 2001111900023 20011119 00023 NM 2001 11 19 SWAA013081 1 20011113 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 495, STR 22R. REPAIRED STR PER SRM. 2 L 7 2 4F RT A16WE 2001111900024 20011119 00024 NM 2001 11 19 SWAA013082 1 20011110 A 5330 6545776 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR UPPER HINGE UPPER CORNER OF CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001111900025 20011119 00025 NM 2001 11 19 SWAA013084 1 20011113 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 23R. REPAIRED SKIN PER SR M. 2 L 7 2 4F RT A16WE 2001111900026 20011119 00026 NM 2001 11 19 SWAA013087 1 20011112 A 5330 6545409 WEB BOEING 737 7373H4 1384600 NM LH W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED 1/2D CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663, LBL 32. REPAIRED WEB PER SWA RA. 2 L 7 2 4F RT A16WE 2001111900027 20011119 00027 NM 2001 11 19 SWAA013090 1 20011113 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 16L. REPAIRED SKIN PE R SRM. 2 L 7 2 4F A16WE 2001111900028 20011119 00028 NM 2001 11 19 SWAA013091 1 20011113 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 27L CORRODED AT BS 420 TO BS 500A. REPAIRED STR PER SRM. 2 L 7 2 4F RT A16WE 2001111900029 20011119 00029 NM 2001 11 19 SWAA013096 1 20011114 A 5310 6517582 WEB BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17.0, WL 225 TO 230. REPAIRED WEB PER SWA RA. 2 L 7 2 4F RT A16WE 2001111900030 20011119 00030 NM 2001 11 19 SWAA013097 1 20011114 A 5310 6517582 WEB BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17.1 & WL 238. R EPAIRED WEB PER SWA RA. 2 L 7 2 4F RT A16WE 2001111900031 20011119 00031 NM 2001 11 19 SWAA013098 1 20011114 A 5310 6547978 WEB BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CORRODED FROM BS 727B TO BS 857, WL 208 LBL 68. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001111900032 20011119 00032 NM 2001 11 19 SWAA013101 1 20011115 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 718SW 27852 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS COVER MISSING AT ROW 2. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2001111900033 20011119 00033 2001 11 19 SWAA013103 4 20011115 A 2565 6556685 BRACKET BOEING 737 7373H4 1384600 NM AFT SVC DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 385SW 26600 DURING SCHEDULED 1/4D CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE MOUNT BRACKET BROKEN. R&R M OUNT BRACKET PER MM. 2 L 7 2 4F RT A16WE 2001111900034 20011119 00034 NM 2001 11 19 SWAA013104 1 20011114 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED 1/2D CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LENS CRACKED AT ROW # 3. R&R LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2001111900035 20011119 00035 NM 2001 11 19 SWAA013109 1 20011114 A 5311 6560552 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED 1/2D CHECK, FOUND WEB CRACKED AT BS 344, STR 12R. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001111900036 20011119 00036 WP 2001 11 19 GTIA011027 1 20010828 A 7120 PLATE DOUG DC9 DC981 3022081 WP RT ENGINE GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - RIGHT FORWARD YOKE UPPER ISOLATOR CUP COVER PLATE GOUGED 2 PLACES INNER RING 4 O'CLOCK AND SCRATCHED AT 10 O'CLOCK POSITION. REMOVED UPPER ISOLATOR IAW MD80 MM 71-20-02. INSTALLED NEW UPPER ISOLATOR CUP IAW MD80 MM 71-20-02. (M) 2 L 7 2 4F A6WE 2001111900037 20011119 00037 WP 2001 11 19 GTIA011028 1 20010828 A 5311 FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - FRAME ASSEMBLY ANGLE AT STATION Y1427 CRACKED NEAR APU EXHAUST DUCT, BETWEEN LONGERON 11R AND 12R. STOP DRILLED C RACK IAW MD80 SRM 53-01 FIG 2. FABRICATED REPAIR DOUBLERS IAW MD80 SRM 53-01 FIG 2. INSTALLED REPAIR AS REQ'D PER MD80 SRM 53-01 FIG 2. (M) 2 L 7 2 4F A6WE 2001111900039 20011119 00039 WP 2001 11 19 GTIA011032 1 20011024 A 5230 49123171 TORQUE TUBE DOUG DC9 DC981 3022081 WP CARGO DOOR CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - AFT LOWER CARGO COMPARTMENT CORRODED AT CARGO DOOR, CRANK SHAFT/TUBE TORQUE. REMOVED CORROSION ON TORQUE TUBE FOU ND TO BE OUT OF LIMITS IAW MD80 SRM 51-10-3. INSTALLED NEW TUBE P/N 49123171. (M) 2 L 7 2 4F A6WE 2001111900044 20011119 00044 WP 2001 11 19 GTIA011033 1 20010821 A 5230 FITTING DOUG DC9 DC981 3022081 WP CARGO DOOR CHAFED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - AFT LOWER CARGO COMPARTMENT CARGO DOOR AFT LATCH FITTING CHAFED. REMOVED LATCH FITTING IAW BOEING MD80 SRM 51-30- 1. FOUND TO BE OUT OF LIMITS IAW BOEING MD80 SRM 53-01 AND 52-30-1. REPLACED LATCH FITTING TORQUE TUBE IAW OHM 52-30-1 . (M) 2 L 7 2 4F A6WE 2001111900046 20011119 00046 WP 2001 11 19 GTIA011034 1 20010820 A 5230 TORQUE TUBE DOUG DC9 DC981 3022081 WP CARGO DOOR DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - FOUND CENTER LOWER CARGO COMPARTMENT, CARGO DOOR TUBE TORQUE/DAMAGE AT F10D LATCH. REMOVED FORWARD TORQUE IAW MD8 0 MM 52-30-00. INSTALLED FORWARD TORQUE TUBE IAW MD80 MM 52-30-00 MD80 OHM 52-30-1. (M) 2 L 7 2 4F A6WE 2001111900048 20011119 00048 WP 2001 11 19 GTIA011035 1 20010820 A 5230 TORQUE TUBE DOUG DC9 DC981 3022081 WP CARGO DOOR CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - CENTER LOWER CARGO COMPARTMENT CARGO DOOR CORRODED AT AFT TUBE TORQUE. REMOVED AFT MID CARGO DOOR TORQUE TUBE IAW MD80 MM 52-30-00. INSTALLED AFT TORQUE TUBE IAW MD80 MM 52-30-0 AND MD80 OHM 52-30-1. (M) 2 L 7 2 4F A6WE 2001111900049 20011119 00049 WP 2001 11 19 GTIA011036 1 20010808 A 5311 FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - CENTER LOWER CARGO COMPARTMENT CORRODED AT DOUBLER LEFT SIDE STRINGER 30 STATION 750. REMOVED CORROSION FROM FORW ARD FRAME AT STATION 750 IAW MD80 SRM 51-10-3. FOUND TO BE OUT OF LIMITS. FRAME P/N 9936454-5. SPLICE AND DOUBLER REMOVE D CORROSION FOUND TO BE OUT OF LIMITS IAW MD80 SRM 51-10-3. FORMED SPLICE IAW MD80 SRM 53-34-0 FIG 2, FORMED DOUBLER IA W MD80 SRM 53-34-0 FIG 2. INSTALLED FRAME, SPLICE AND DOUBLER IAW MD80 SRM 51-30-5 AND 51-30-2. (M) 2 L 7 2 4F A6WE 2001111900050 20011119 00050 WP 2001 11 19 GTIA011037 1 20010809 A 5313 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - CENTER LOWER CARGO COMAT, CORRODED AT 29L STRINGER STATION 712 TO STATION 731. REMOVED CORROSION ON LONGERON 29L IAW MX80 SRM 51-10-3, MATERIAL LOSS OUT OF LIMITS. CUT OUT DAMAGED SECTION OF LONGERON. FABRICATED SPLICE FOR LONGERON P ER DC9/MD80 SRM 53-02 FIG 14. FABRICATED SPLICE PER DC9/MD80 SRM 53-02 FIG 14. INSTALLED LONGERON AND SPLICES (TWO PIEC ES) IAW SRM MD80 53-02 FIG 18 AND SRM MD80 51-30-5. (M) 2 L 7 2 4F A6WE 2001111900051 20011119 00051 WP 2001 11 19 GTIA011039 1 20010812 A 2720 DAMPER DOUG DC9 DC981 3022081 WP RUDDER WORN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - LOWER RUDDER DAMPER CONTROL ARM ATTACH RIVETS ARE SHEARED OFF COMPLETELY. CONTROL ARM SHOWS WEAR FROM FREE MOVEME NT AND DAMPER MAY HAVE FAILED CAUSING SHEAR. REMOVED LOWER RUDDER DAMPER IAW MD80 MM 27-20-05. INSTALLED LOWER RUDDER IAW MD80 MM 27-20-05. (M) 2 L 7 2 4F A6WE 2001111900052 20011119 00052 WP 2001 11 19 GTIA011040 1 20010809 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - FLOOR PANEL CRACKED AFT EDGE FS 927.2R, OUTBOARD PANEL. STOP DRILLED CRACK IAW MD80 SRM 53-05-0. FABRICATED DOUB LER IAW MD80 SRM 53-05-0. INSTALLED DOUBLER IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2001111900054 20011119 00054 WP 2001 11 19 GTIA011041 1 20010809 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - CENTER FLOORBOARD FS 826-886 CRACKED AFT EDGE. AFTER FURTHER EVALUATION P/N 993639-15 (TWO PIECES) AND P/N 993663 9-13 (TWO PIECES) WERE FOUND TO BE OUT OF LIMITS IAW MD80 SRM 51-01. FABRICATED 2 NEW PIECES OF EDGE TRIM IAW MD80 SRM 53-05. INSTALLED SUPPORTS (TWO PIECES) AND EDGE TRIMS (TWO PIECES) PER SRM MD80 51-30-1 ON FLOORBOARD. (M) 2 L 7 2 4F A6WE 2001111900057 20011119 00057 WP 2001 11 19 GTIA011042 1 20010815 A 5341 ATTACH ANGLE DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - CENTER WING TANK TO FUSELAGE SKIN ATTACH ANGLE CORRODED, FS 880L UNDER FLOORWEB. FABRICATED AND DRILLED REPAIR DO UBLERS IAW MD80 SRM 51-10-1 AND EA SCB008. INSTALLED REPAIR IAW EA SCB 008. (M) 2 L 7 2 4F A6WE 2001111900059 20011119 00059 WP 2001 11 19 GTIA011043 1 20010810 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - FLOOR SUPPORT CORRODED AT STATION Y198, X46. REMOVED CORROSION IAW MD-80 51-10-3. FOUND TO BE OUT OF LIMITS IAW MD80 SRM 53-05-00. FABRICATED NEW SUPPORT IAW MD80 SRM 51-00-00. INSTALLED IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2001111900061 20011119 00061 WP 2001 11 19 GTIA011044 1 20010820 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - FOUND FLOOR SUPPORT CORRODED FROM STATION Y244 TO STATION Y249, X14 INCH. VERIFY PORT IS OUT OF LIMITS IAW MD80 S RM 53-05. REMOVED SUPPORT IAW MD80 SRM 51-30-2. INSTALLED NEW FLOOR SUPPORT IAW MD80 SRM 51-30-1 AND 51-30-2. (M) 2 L 7 2 4F A6WE 2001111900062 20011119 00062 WP 2001 11 19 GTIA011045 1 20010818 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - FOUND SEAT TRACK CORRODED FROM STATION Y199 TO STATION Y230, X45 INCHES. REMOVED CORROSION ON SEAT TRACK FROM STA TION 199-230 BY 45 INCHES CORROSION REMOVAL OUT OF LIMITS IAW MD80 SRM 53-05. REMOVED SEAT TRACK AT FS 199 FS 230 IAW M D80 SRM 51-30-2. INSTALLED NEW SEAT TRACK IAW MD80 SRM 53-04 FIG 4 AND MD80 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 2001111900063 20011119 00063 WP 2001 11 19 GTIA011046 1 20010822 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - FLOOR SUPPORT CORRODED AT STATION Y164, X41 INCHES. CORRODED FLOOR SUPPORT FOUND TO BE OUT OF LIMITS IAW MD80 SRM 51-10-3. INSTALLED NEW FLOOR SUPPORT FITTING IAW SRM 51-30-5. (M) 2 L 7 2 4F A6WE 2001111900064 20011119 00064 WP 2001 11 19 GTIA011047 1 20010813 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - FLOOR SUPPORT CORRODED AT STATION Y174, X44 INCH. SUPPORT FOUND TO BE OUR OF LIMITS IAW MD80 SRM 51-24-00. REMOV ED FLOOR SUPPORT IAW MD80 SRM 51-30-2. FABRICATED NEW FLOOR SUPPORT IAW MD80 SRM 51-10-1. INSTALLED FLOOR SUPPORT IAW MD80 SRM 51-50-2. (M) 2 L 7 2 4F A6WE 2001111900065 20011119 00065 WP 2001 11 19 GTIA011048 1 20010824 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - FOUND FLOOR SUPPORT CORRODED AT STATION Y180 X55 INCHES, BEYOND LIMITS. FOUND FLOOR SUPPORT TO BE OUT OF LIMITS I AW MD-80 SRM 51-10-3. REMOVED IAW MD80 SRM 51-30-20 AND 51-30-8. INSTALLED FLOOR SUPPORT AT STATION Y180 X55 INCHES PE R MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2001111900066 20011119 00066 WP 2001 11 19 GTIA011049 1 20010816 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - FLOOR SUPPORT CORRODED AT STATION Y164, X15 INCHES (RECEPTACLE HOLE). REMOVED FLOOR SUPPORT IAW MD80 SRM 53-01. I NSTALLED NEW FLOOR SUPPORT PER SRM MD80 51-10-5. (M) 2 L 7 2 4F A6WE 2001111900067 20011119 00067 WP 2001 11 19 GTIA011050 1 20010818 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - FOUND SEAT TRACK CORRODED FROM STATION Y200 TO STA Y256, -X22. CORROSION OUT OF LIMITS PER 53-05. REMOVED SECTIO N OF SEAT TRACK OUT OF LIMITS STATION 200 TO 265 IAW MD80 SRM 53-05-00. INSTALLED SEAT TRACK IAW SRM 53-05 FIG 4. (M) 2 L 7 2 4F A6WE 2001111900068 20011119 00068 WP 2001 11 19 GTIA011051 1 20010818 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FOUND STATION 1240 SEAT TRACK LEFT INBOARD HAS SURFACE CORROSION. REMOVED CORROSION IAW MD80 SRM 51-10-3. REMAINING MA TERIAL OUT OF LIMITS IAW MD80 SRM 53-05. REMOVED SEAT TRACK FROM STATION 1220-1309 IAW MD80 SRM 51-30-01. INSTALLED NE W SEAT TRACK. (M) 2 L 7 2 4F A6WE 2001111900069 20011119 00069 WP 2001 11 19 GTIA011052 1 20010820 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - FOUND SEAT TRACK LEFT OUTBOARD HAS CORROSION AROUND HI-LOCK. REMOVED CORROSION. REMAINING MATERIAL BEYOND LIMITS . REMOVED SEAT TRACK DAMAGE. REPAIRED SEAT TRACK PER MD80 SRM 53-20-01. INSTALLED SEAT TRACK. (M) 2 L 7 2 4F A6WE 2001111900070 20011119 00070 WP 2001 11 19 GTIA011053 1 20010819 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - SEAT TRACK LEFT INBOARD HAS SURFACE CORROSION AROUND HI-LOCK. REMOVED CORROSION. MATERIAL LOSS FOUND OUT OF LIMI TS. REMOVED SECTION OF SEAT TRACK OUT OF LIMITS. INSTALLED NEW SECTION OF SEAT TRACK IAW MD80 SRM 53-05-0 AND SRM 51-10 -5. (M) 2 L 7 2 4F A6WE 2001111900071 20011119 00071 WP 2001 11 19 GTIA011054 1 20010818 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - FOUND SEAT TRACK LEFT OUTBOARD GOUGED AND HAS SURFACE CORROSION ON TOP OF TRACK. BLENDED GOUGE AND CORROSION. RE MAINING MATERIAL OUT OF LIMITS. REMOVED SEAT TRACK. INSTALLED SEAT TRACK IAW MD80 SRM 53-05. (M) 2 L 7 2 4F A6WE 2001111900072 20011119 00072 WP 2001 11 19 GTIA011056 1 20010828 A 5753 FLAP DOUG DC9 DC981 3022081 WP RT WING MISALIGNED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - RIGHT WING INBOARD FLAP, OUTBOARD T/E LEADING EDGE FLAP MISALIGNMENT PREVIOUS INSTALLATION. REMOVED TRAILING EDGE FOR REPLACEMENT. INSTALLED NEW TRAILING EDGE IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2001111900073 20011119 00073 WP 2001 11 19 0103959870 1 20010609 A 5730 SKIN DOUG DC9 DC951 3022051 WP LT WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 779NC 48101 DURING OVERNIGHT IN MSP, THE LT WING LEADING EDGE NOSE SKIN WAS FOUND WITH A 1.125 INCH CRACK FROM A FASTENER HOLE TO TH E EDGE OF THE SKIN. DAMAGE IS LOCATED JUST OUTBOARD OF NR 2 L/E SLAT DRIVE ACTUATOR CUTOUT. REPAIRED PER EA 98-182743 . 2 L 7 2 4F RT A6WE 2001111900074 20011119 00074 NM 2001 11 19 0104216310 1 20011108 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN DAMAGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 670US 24225 DURING LINE CHECK, FOUND B-ZONE LEFT SIDE FLOOR EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. REPAIRED WIRING AT 10B. OPER ATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2001111900075 20011119 00075 EU 2001 11 19 0104223245 1 20011109 A 3231 DOOR AIRBUS 320 A320212 3930322 EU NLG OUT OF ADJ A NWAA K NONE J WARNING INDICATION CL CLIMB 1 GL 01 345NW 399 AFTER TAKEOFF, NOSE GEAR DOORS DID NOT CLOSE. GEAR RETRACTED NORMALLY. RECYCLED GEAR WITH NO HELP. FLEW AT 250 IAS PE R COM 2.32.9. NOSE GEAR DOORS APPEARED TO BE CLOSED. AIRCRAFT MADE AN UNEVENTFUL LANDING. JACKED AIRCRAFT AND CYCLED GEAR. ADJUSTED RIGHT NOSE LANDING GEAR DOOR 1.2 TURN OUT AND LUBED DOOR LOCK MECHANISM. CYCLED GEAR AND OPERATIONAL CH ECK OK. 2 L 7 2 4F RT A28NM 2001111900076 20011119 00076 2001 11 19 0104239603 4 20011115 A 2211 COMPUTER DOUG DC9 DC932 3022066 WP AUTOPILOT SYS FAULTY A NWAA O OTHER F FLT CONT AFFECTED CL CLIMB 1 GL 01 603NW 47101 THE AIRCRAFT WOULD PORPOISE +-100 FEET DURING CLIMBOUT WITH THE AUTOPILOT ON USING THE THUMB WHEEL. THE AIRCRAFT WOULD NOT HOLD ALTITUDE IN LEVEL FLIGHT WITH PITCH HOLD SELECTED. CREW REFUSED TO HAND FLY THE AIRCRAFT AND THE FLIGHT RETURN ED TO AN UNEVENTFUL LANDING AT MEM. MAINTENANCE REPLACED THE PITCH AXIS COMPUTER AND THE AUTOPILOT CONTROL PANEL. OPER ATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001111900085 20011119 00085 NE 2001 11 19 A6WA200100058 2 20011007 A 7321 77390010 FCU BAC 146 146200A 1500266 EU LYC ALF520 ALF520* 41580 NE NR 3 ENGINE MALFUNCTIONED A A6WA E ENGINE SHUTDOWN O OTHER CL CLIMB 1 GL 31 290UE 24276 4974 E2080 LF05250 DURING CLIMB NR 3 ENGINE DID NOT RESPOND TO THRUST LEVER POWER CHANGES THEN NR 3 ENGINE TGT STARTED CLIMBING TO 870 DEGR ESS PERFORMED SHUTDOWN. MAINTENANCE REMOVED AND REPLACED FUEL CONTROL UNIT. 2 H 7 4 4F 4 F A49EU E6NE 2001111900086 20011119 00086 NE 2001 11 19 A6WA200100059 2 20011111 A 7321 77390010 FCU BAC 146 146100A 1500260 EU LYC ALF520 ALF520* 41580 NE NR 2 ENGINE MALFUNCTIONED A A6WA E ENGINE SHUTDOWN O OTHER CL CLIMB 1 GL 31 463AP 9351 4053 E1063 LF05467A UNABLE TO CONTROL POWER ON NR 2 ENGINE. POWER INCREASED REGARDLESS OF THRUST LEVER POSITION SHUTDOWN ENGINE WITH T-HAND LE. MAINTENANCE REMOVED AND REPLACED FUEL CONTROL UNIT. 2 H 7 4 4F 4 F RT A49EU E6NE 2001111900087 20011119 00087 NM 2001 11 19 A6WA200100060 1 20011010 A 2120 SMOKE DORNER DO32 DO328100 2996000 NM CABIN DETECTED A A6WA D RETURN TO BLOCK B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 GL 31 338PH 3029 DURING RUN UP, GOT SMOKE LAV INDICATION, FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. MAINTENANCE PERFORMED GROUND OPS CHECK OF THE LT/RT BLEED AIR SYSTEMS IAW MM. NO SMOKE OR MESSAGES NOTED. 2 H 7 2 4T RT A45NM 2001111900088 20011119 00088 EU 2001 11 19 QXEA0101910 1 20011115 A 2610 DETECTOR FOKKER F28 F28MK4000 4990810 EU INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 PDX - LAVATORY SMOKE DETECTOR WILL NOT TEST. REMOVED AND REPLACED SMOKE DETECTOR. OPERATIONAL CHECK IS GOOD. AIRCRAFT RE TURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001111900089 20011119 00089 WP 2001 11 19 ABXA010586 1 20011026 A 5300 59122851 DOUBLER DOUG DC9 DC932 3022066 WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 983AX 47257 RIGHT WINDOW DOUBLER CRACKED IN THE UPPER FORWARD CORNER OF WINDOW AT STATION 658. REPAIRED CRACK IAW DC-9 SSRM K07226. 2 L 7 2 4F A6WE 2001111900090 20011119 00090 WP 2001 11 19 ABXA010587 1 20011026 A 5300 59203192 SKIN DOUG DC9 DC932 3022066 WP FWD. CARGO CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 983AX 47257 SKIN BULGED FROM CORROSION AT FORWARD LOWER CARGO DOOR CUTOUT BETWEEN STATION 386 AND 391. REPAIRED SKIN IAW DC-9 SRM. 2 L 7 2 4F A6WE 2001111900091 20011119 00091 NM 2001 11 19 A6WA200100061 1 20011013 A 2612 51653151 CONTROL UNIT DORNER DO32 DO328100 2996000 NM FIRE WARNING FAULTY A A6WA F E A ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 31 335PH 4988 4988 3013 NR 2 ENGINE FIRE WARNING LIGHT AND BELL CAME ON IN-FLIGHT. C/W EMERGENCY CHECKLIST - USED 1 BOTTLE AND LIGHT WENT OUT, SHUTDOWN ENGINE PER CHECKLIST. MAINTENANCE REMOVED AND REPLACED FIRE WARNING CONTROL UNIT. 2 H 7 2 4T RT A45NM 2001070300173 20010703 00173 EU 2001 7 3 USAASA01020 1 20010518 A 3397 WIRE AIRBUS A319 A319112 3930323 EU CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 EA 19 710UW 1019 DCA - THE ESCAPE LIGHT ON SEAT ROW 13 WAS INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRES. OPS CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2001111900092 20011119 00092 EA 2001 11 19 A6WA200100062 1 20011012 A 7910 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 2 ENGINE OVERSERVICED A A6WA E A ENGINE SHUTDOWN UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CR CRUISE 1 GL 31 401AW 7280 872590 NR 2 ENGINE HIGH OIL TEMP, PRECAUTIONARY ENGINE SHUTDOWN, NR 2 ENGINE OIL TEMP 158 DEGREES, PSI 40. MAINTENANCE INSPECT ED AND FOUND NR 2 ENGINE OIL OVERSERVICED. REMOVED EXCESS OIL, GROUND RAN AIRCRAFT, OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2001070200208 20010702 00208 2001 7 2 SWAA011717 4 20010613 A 2565 D31354 WIRE BOEING 737 7377H4 1384404 NM SERVICE DOOR EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 754SW 29849 DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE HAS EXPOSED WIRES. SECURED EMERGENCY EVAC SLIDE WIRE S PER MM. 2 L 7 2 4F RT A16WE 2001111900093 20011119 00093 EA 2001 11 19 A6WA200100063 1 20011115 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A A6WA K NONE F FLT CONT AFFECTED AP APPROACH 1 GL 31 407AW 7424 FLAPS FAIL CAS ON APPROACH, LANDED AT FLAPS ZERO. MAINTENANCE C/W AWAC SUPPLEMENT 98-18 IN AMM CHAPTER 27, NO CODED FAI LS IN LAST 72 HOURS, SYSTEM RESET. 2 L 7 2 4F RT A21EA 2001111900094 20011119 00094 NM 2001 11 19 C1HA200183007 1 20011110 A 2611 SMOKE DETECTOR BOEING 727 7272S7 138407Z NM CARGO BAY INOPERATIVE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 683CA 22490 NR 4 SMOKE DETECTOR INOP IN AFT CARGO COMPARTMENT. REMOVED AND REPLACED NR 4 SMOKE CARGO DETECTOR IN AFT PIT IAW MM 26- 25-01. OPS CHECK NORMAL. 2 L 7 3 4F A3WE 2001111900095 20011119 00095 NM 2001 11 19 C1HA200184014 1 20011019 A 3350 LIGHT BOEING 727 7272S7 138407Z NM CABIN BROKEN A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 684CA 22491 ON THROUGH FLIGHT INSPECTION FOUND RIGHT HAND FORWARD WING EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. REMOVED AND REPLACED R IGHT HAND FORWARD WING EMERGENCY EXIT LIGHT ASSEMBLY IAW MM 33-50-11. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2001111900096 20011119 00096 NM 2001 11 19 C1HA200192010 1 20011105 A 2612 FIRE LOOP BOEING 727 727212 138407G NM NR 3 ENGINE OUT OF POSITION A C1HA K NONE N FALSE WARNING DE DESCENT 1 GL 15 292AS 21458 ON DESCENT INTO LAS, SYSTEM-B ENGINE FIRE DETECTION ON FLIGHT ENGINEER AUXILIARY PANEL FLICKERED/ STEADY ON NR 3 ENGINE. REPOSITIONED NR 3 ENGINE FIRE LOOPS AS REQUIRED. OPS CHECK NORMAL. 2 L 7 3 4F A3WE 2001111900097 20011119 00097 NM 2001 11 19 C1HA200197010 1 20011019 A 3350 LIGHT BOEING 727 727270 138408P NM CABIN INOPERATIVE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 697CA 23052 EXIT LIGHT ON THE CEILING BY AFT DOOR EXITS IS NOT WORKING ON THE LEFT SIDE. RELAMPED EXIT LIGHT ASSEMBLY AFT OVERHEAD CEILING POSITION. GROUND OPS CHECK GOOD. 2 L 7 3 4F RT A3WE 2001111900098 20011119 00098 SO 2001 11 19 C2XA01CL229 1 20011116 A 2530 CBC16707 RECEPTACLE EMB 135 EMB135LR 3260305 SO GALLEY BURNED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 14522 145383 HPN-CLE FLIGHT 3097 THE CREW REPORTED A BURNING SMELL IN THE CABIN AND COCKPIT. THE AIRCRAFT DIVERTED TO EWR AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND THE COFFEE POT RECEPTACLE BURNT. MAINTENANCE REPLACED THE CO FFEE POT RECEPTACLE FOR THE NR 1 COFFEE CONTAINER. ALSO FOUND THE NR 2 CONTAINER RECEPTACLE HAD A LOOSE CONNECTION WITH THE CONTAINER. THE SYSTEM WAS PLACED ON MEL 25-60-02/3. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT TOOO11AT 2001111900099 20011119 00099 SO 2001 11 19 C2XA01IA399 1 20011115 A 2121 AE1711AA0 COOLING FAN EMB 120 EMB120ER 3260203 SO A/C BAY FAILED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 58733 120197 IAH- AFTER TAKEOFF FLIGHT 3917 THE CREW NOTED SMOKE IN THE COCKPIT. THE CREW DECLARED AN EMERGENCY AND RETURNED TO IAH WITHOUT INCIDENT. IAH- MAINTENANCE REMOVED AND REPLACED THE GROUND COOLING FAN, PERFORMED A OPERATIONAL CHECK, NO DEF ECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001111900100 20011119 00100 SO 2001 11 19 C2XA01IA400 1 20011116 A 3610 M832481908 O-RING EMB 120 EMB120ER 3260203 SO BLEED AIR SYS LEAKING A C2XA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SW 27 57734 120199 IAH- DURING FLIGHT 3633 THE CREW NOTED DUCT LEAK ON NUMBER 1 ENGINE IN FLIGHT. SHUT DOWN ENGINE AND DECLARED EMERGENCY , LANDED AT IAH WITHOUT INCIDENT. IAH- MAINTENANCE REPOSITIONED THE WATER SEPARATOR SPRAY NOZZLES AND REMOVED AND REPLA CED ALL O-RINGS IN THE NUMBER ONE MAIN AIR DISTRIBUTION SYSTEM FROM ENGINE TO CROSSBLEED VALVE. PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. REINSTALLED INBOARD LEADING EDGE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001111900101 20011119 00101 SO 2001 11 19 C2XA01IA401 1 20011116 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13994 145291 ZCL- DURING PREFLIGHT THE CREW NOTED THAT THE FIRST STRIP OF FLOOR EMERGENCY LIGHTING IN THE CABIN FAILED TO ILLUMINATE . ZCL- MAINTENANCE PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001111900102 20011119 00102 SO 2001 11 19 C2XA01TY179 1 20011118 A 5315 14522461003 FLOORBEAM EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16511 145267 TYS DURING A SCHEDULED 1C INSPECTION THE FLOORBEAM SPLICE CAP OVER FRAME 20 ON RIGHT SIDE WAS FOUND CORRODED AROUND THE RIVETS. MAINTENANCE REMOVED AND REPLACED THE RIVETS, CLEAN THE CORROSION, REWORKED THE AREA IAW EMB 135/145 SRM 51-40- 02 AND CPM 51-17-00--51-21-07. ALL WORK WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETION OF ALL MAINTENANCE. 2 L 7 2 4F RT T00011AT 2001111900103 20011119 00103 SO 2001 11 19 C2XA01TY180 1 20011118 A 5320 14521725013 SILL EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16511 145267 TYS DURING A SCHEDULED 1-C INSPECTION CORROSION WAS FOUND UNDER THE SERVICE DOOR SILL AND SCREW HOLES. MAINTENANCE REMO VED AND REPLACED ONE NUT PLATE, CLEAN THE CORROSION, REFINISH THE AREA IAW EMB 135/145 SRM 51-40-02 AND CPM 51-17-04--51 -21-07, ALL WORK WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETION OF ALL MAINTENANCE. 2 L 7 2 4F RT T00011AT 2001111900104 20011119 00104 SO 2001 11 19 C2XA01TY181 1 20011118 A 5320 1452172003 FLOOR SUPPORT EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16511 145267 TYS DURING A SCHEDULED 1-C INSPECTION THE LEFT FLOOR SUPPORT PLATE FWD OF SERVICE DOOR WAS FOUND CORRODED AROUND SCREW HOLES. MAINTENANCE REMOVED AND REPLACED THE NUT PLATE, CLEAN THE CORROSION, REFINISH THE AREA IAW EMB 135/145 SRM 51-40 -02, CPM 51-21-17-00 AND 51-21-04, 05 AND 06. ALL WORK WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETION OF ALL MAINT ENANCE. 2 L 7 2 4F RT T00011AT 2001111900105 20011119 00105 NM 2001 11 19 CALA0101003 1 20011114 A 5230 DOUBLER BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59338 23576 INSPECTION FOUND A THREE INCH CRACK RUNNING PAST STOP DRILL IN C-1 DOOR INTERIOR SKIN DOUBLER. A REPAIR DOUBLER WAS INS TALLED IAW ECRA 5230-01637. 2 L 7 2 4F RT A16WE 2001111900106 20011119 00106 NM 2001 11 19 CALA0101004 1 20011115 A 5320 STIFFENER BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59338 23576 INSPECTION FOUND A .125 INCH CRACK IN RT WHEEL WELL AFT PANEL T-CHORD AT BS 727. A NEW T-CHORD WAS INSTALLED IAW SRM 51 -10-2. 2 L 7 2 4F RT A16WE 2001111900107 20011119 00107 EU 2001 11 19 CHQ00040 1 20011116 A 3310 LIGHT SAAB SF340 SF340A 7850100 EU COCKPIT INOPERATIVE A CHQA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 11 121 N121CQ RIGHT HAND BUS LIGHT INOP. 2 L 7 2 4T RT A52EU 2001111900108 20011119 00108 EU 2001 11 19 DHL2001364027 1 20011108 A 2910 HYDRAULIC LINE AIRBUS 300 A300B4203 3930306 EU HYDRAULIC SYS LEAKING A DHLA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 364DH 141 DURING CRUISE, GREEN SYS HYD LEVEL LOW LIGHT ILLUM. MAGNETIC INDICATORS & GREEN SYS PRESS INDICATED NORM. DURING DESCENT , GREEN SYS MAGNETIC INDICATOR WENT AMBER WITH PRESS FLUCTUATING. PUMP PRESS LIGHT ILLUM. GREEN SYS PUMPS WERE TURNED ON . BLUE SYS PUMP WENT AMBER DURING DESCENT, BUT RETURNED TO NORM. EMERG WAS DECLARED. R&R LEAKING SUPPLY LINE AT GREEN S YS RESERVOIR. REPLENISHED GREEN SYS, LEAK AND OPS CHECKED GOOD. R&R AND LEAK CHECKED EMERGENCY EXTENSION FILTERS & RESTO RED TO NORMAL CONFIG. R&R AND LEAK CHECKED CASE DRAIN FILTERS. DURING ENG RUN, NR 1 GREEN HYD PUMP WAS UNABLE TO MAINTA IN SYS PRESS. R&R NR 1 GREEN HYD PUMP IAW MM 29-11-32. OPS & LEAK CHECKED GOOD. 2 L 7 2 4F RT A35EU 2001111900109 20011119 00109 WP 2001 11 19 LCQ 1 20011030 A 3213 PAD DOUG DOUG DC9 DC981 3022081 WP RT MLG CRACKED B K NONE O OTHER IN INSP/MAINT 1 SO 15 807US XC90340 48039 CRACK INDICATIONS AROUND JACK PAD ON BOTTOM OF LOWER SEGMENT OF RT MAIN LANDING GEAR. 2 L 7 2 4F A6WE 2001111900110 20011119 00110 EU 2001 11 19 MALA010767 1 20011026 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 411XJ 340B411 REAR FUSELAGE BOTTOM SKIN PANEL DAMAGED FROM AIRCRAFT WINDMILLING. MAINTENANCE COMPLETED PERMANENT REPAIR IAW EO S53109 . SPLICED IN REAR FUSELAGE BOTTOM SKIN PANEL. 2 L 7 2 4T RT A52EU 2001111900111 20011119 00111 EU 2001 11 19 MALA010768 1 20011106 A 5347 SEAT TRACK SAAB SF340 SF340A 7850100 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 109XJ 340A109 DURING 4K CHECK IN CWA, LT CENTER AISLE SEAT TRACK INBOARD CARGO FLOOR BOARD FLANGE HAS HEAVY AND DEEP CORROSION AT APPR OXIMATELY STA 686.88 TO APPROXIMATELY STA 651. MAINTENANCE COMPLIED WITH REPAIR OF LT CENTER AISLE SEAT TRACK INBOARD C ARGO FLOOR BOARD FLANGE AT APPROXIMATELY STA 651-0-686-88 IAW SAAB SRM 53-70-60 AND EO 53078. 2 L 7 2 4T RT A52EU 2001111900112 20011119 00112 EU 2001 11 19 MALA010769 1 20011108 A 5311 FRAME SAAB SF340 SF340A 7850100 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 109XJ 340A109 DURING 4K-CHECK IN CWA, FRAME AT STA 294 HAS CORROSION. MAINTENANCE REPAIRED IAW EO 52108. 2 L 7 2 4T RT A52EU 2001111900113 20011119 00113 EU 2001 11 19 MALA010771 1 20011111 A 5240 DOOR SAAB SF340 340B 7860101 EU LAV SERVICE OPEN A MALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 15 443XJ 340B443 AFTER TAKEOFF ON FLIGHT 3356, CREW NOTED A STRANGE NOISE AND VIBRATION AFTER TAKEOFF. IN-FLIGHT VIBRATION, LAV SERVICE DOOR OPENED IN-FLIGHT. FLIGHT RETURNED TO DTW. MAINTENANCE INSPECTED LAV SERVICE DOOR FOUND TO BE IN SERVICEABLE CONDI TION. LATCHES LOCK OVERCENTER PROPERLY AND DOOR IS SECURE TO AIRFRAME. ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2001111900114 20011119 00114 EU 2001 11 19 MALA010772 1 20011112 A 7931 IPTE119100200D1 TRANSDUCER SAAB SF340 340B 7860101 EU RT ENGINE FAILED A MALA E ENGINE SHUTDOWN J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 406XJ 340B406 ON LANDING OF FLIGHT 3001, ROLL OUT RT ENGINE OIL PRESSURE DROP TO ZERO. RT OIL PRESSURE LIGHT ALSO ILLUMINATED. CREW SHUTDOWN ENGINE AND FINISHED TAXIING IN ON ONE ENGINE. MAINTENANCE RAN AC, FOUND OIL PRESSURE GEARBOX READING HIGH, REP LACED GEARBOX OIL PRESSURE TRANSDUCER P/N IPTE119100200D1, S/N OFF 5749-10-575, S/N ON 5587-2-390-1 IAW SAAB MM 79-30-05 . ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2001111900115 20011119 00115 WP 2001 11 19 MWEA011425 1 20011108 A 5230 BUNGEE CORD DOUG DC9 DC914 3022034 WP CARGO DOOR BROKEN A MWEA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 600ME 45725 ON TAKEOFF, AIRCRAFT CABIN WOULD NOT PRESSURIZE. ADJUSTED FORWARD CARGO DOOR SHIMS ON FORWARD HINGE AND ADJUSTED HINGE SPRINGS. INSTALLED NEW BUNGEE ASSEMBLY ON FORWARD DOOR. 2 L 7 2 4F A6WE 2001111900116 20011119 00116 WP 2001 11 19 MWEA011426 1 20011114 A 5311 2777930S5 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 CORROSION ON J-CHANNEL FUSELAGE STATION 503 BETWEEN LONGERON 29 LEFT AND RIGHT. REMOVED CORROSION, CUT OUT DAMAGE IN FR AME. INSTALLED REPAIR SPLICE. 2 L 7 2 4F A6WE 2001111900117 20011119 00117 WP 2001 11 19 MWEA011427 1 20011114 A 5320 4912460501 ANGLE DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 GOUGES AND CORROSION ON INNER SKIN AND ANGLE BRACKETS OF LOWER BACK SIDE OF DOOR JAMB AFT PIT STATION 945-889. BLENDED CORROSION AND GOUGES. FABRICATED AND INSTALLED LOWER JAMB/INTERCOSTAL BRACKET. INSTALLED WEB STRAPS AT LONGERON 28 RIG HT AND 29 RIGHT. 2 L 7 2 4F A6WE 2001111900118 20011119 00118 WP 2001 11 19 MWEA011428 1 20011114 A 5311 99115057 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FRAME AT FUSELAGE STATION 83.5 BY 10 LEFT IS CRACKED. LENGTH OF CRACK IS 1.00 INCH. STOPPED DRILL, FABRICATED AND INST ALLED REPAIR ANGLE. 2 L 7 2 4F A6WE 2001111900119 20011119 00119 WP 2001 11 19 MWEA011429 1 20011114 A 5311 99115057 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FRAME IS CRACKED AT FUSELAGE STATION 83.5 AT 10 RIGHT 1 INCH IN LENGTH. REMOVED, STOPPED DRILL, FABRICATED AND INSTALLE D REPAIR ANGLE. 2 L 7 2 4F A6WE 2001111900120 20011119 00120 WP 2001 11 19 MWEA011430 1 20011114 A 5320 99115056 ANGLE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 ANGLE AT FUSELAGE STATION 83.5 HAS A 1 INCH CRACK AT INBOARD END. FABRICATED, DRILLED AND INSTALLED REPAIR ANGLE. 2 L 7 2 4F A6WE 2001111900121 20011119 00121 WP 2001 11 19 MWEA011431 1 20011114 A 5320 99115055 ANGLE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 ANGLE CRACKED AT FUSELAGE STATION 83.5 AT INBOARD END, 1.0625 INCHES IN LENGTH. STOPPED DRILL, FABRICATED AND INSTALLED REPAIR ANGLE. 2 L 7 2 4F A6WE 2001111900122 20011119 00122 WP 2001 11 19 MWEA011432 1 20011115 A 5320 591015837 WEB DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 CORROSION OF AFT PIT DOOR WEB AT STATION 937 JUST FORWARD OF LONGERONS 24 RIGHT TO 26 RIGHT AFT PIT. REMOVED CORROSION, FABRICATED AND INSTALLED WEB. 2 L 7 2 4F A6WE 2001111900123 20011119 00123 NE 2001 11 19 NACA20010036 2 20011107 A 8530 356994 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800* 52026 NE NR 1 ENGINE CRACKED A NACA E A ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CL CLIMB 1 AL 03 43872 842 842 533294 55337 NR 1 ENGINE FEATHERED DUE TO RAPID OIL LOSS. REPLACED THE NR 7 CYLINDER FOR CRACKED HEAD. 2 L 7 4 4R 4 R A781 5E8 2001111900124 20011119 00124 NE 2001 11 19 NACA20010037 2 20011108 A 8530 356993 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800* 52026 NE NR 1 ENGINE LEAKING A NACA E ENGINE SHUTDOWN K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AL 03 43872 850 850 533294 55337 NR 1 ENGINE SMOKES AND EXCESSIVE OIL LOSS. REPLACED NR 2 CYLINDER EXHAUST PIN CAPS, TORQUED AND SAFETIED. 2 L 7 4 4R 4 R A781 5E8 2001111900125 20011119 00125 NM 2001 11 19 NACA20010038 1 20011110 A 2611 SMOKE DETECTOR BOEING 727 72723 1384004 NM CARGO BAY MALFUNCTIONED A NACA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 AL 03 930FT 19387 MECHANICAL INTERRUPTION IN ANCHORAGE AT 1522Z DUE TO LOWER CARGO FIRE WARNING HORN WENT OFF 3 TIMES. OPENED BOTH BELLY DOORS IMMEDIATELY UPON AIRCRAFT RETURN. FOUND NO SMOKE OR FIRE. UNLOADED BELLY'S AND PERFORMED LOWER CARGO SMOKE/FIRE PROTECTOR TEST, IAW HOLLINGSHEAD INTERNATIONAL AIRCRAFT MAINT MANUAL SUPPLEMENT. SYSTEM TESTED OK, NO FAULTS OR DEFECTS FOUND. SUSPECT FREIGHT BEING STACKED TO CEILING WAS THE CAUSE. DEFERRED THE SYSTEM FOR FURTHER TROUBLESHOOTING. FURT HER TESTING, AFTER FLIGHT REVEALED NO FAULT, DEFERRAL REMOVED AND AIRCRAFT CONTINUED IN SERVICE. 2 L 7 3 4F A3WE 2001111900126 20011119 00126 NM 2001 11 19 PCAA0111133 1 20011110 A 3397 PIN DHAV DHC8 DHC8102 2809003 NM CONNECTOR BACKED OUT A PCAA K NONE O OTHER NR NOT REPORTED 1 EA 13 832EX 280 ABE- FLIGHT 3521. CREW REPORTED EMERGENCY LIGHTS FLICKERING ON AND OFF. MAINTENANCE INSPECTED WIRING AND FOUND PIN-B A T CANNON PLUG 9811P45 PUSHED BACK AND NOT LOCKING. PIN REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE . 2 H 7 2 4T RT A13NM 2001111900127 20011119 00127 NM 2001 11 19 PCAA0111134 1 20011112 A 5330 85330272101 SKIN DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 820EX 019 DURING A CHECK INSPECTION LOWER FORWARD CORNER OPENING OF CARGO COMPARTMENT FOUND CRACKED. LOWER FORWARD COAMING SECTIO N OF CARGO DOOR OPENING REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001111900128 20011119 00128 NM 2001 11 19 PCAA0111135 1 20011115 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN DAMAGED A PCAA K NONE L NO TEST NR NOT REPORTED 1 EA 13 847EX 333 LGA- FLIGHT 3874 CREW REPORTED FIRST TWO WHITE EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPAIRED WIRING IN SYSTEM. O PERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001111900129 20011119 00129 SW 2001 11 19 PNSA011001 1 20011031 A 3320 SWITCH SWRNGN SA227 SA227AC 8780603 SW CABIN DEFECTIVE A PNSA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 AL 03 41NE AC741B UPON LANDING SMOKE WAS OBSERVED IN CABIN COMING FROM READING LIGHT SWITCH FOR SEAT 1A. MAINTENANCE REPLACED READING LIG HT SWITCH AND OP CHECK OK. 2 L 7 2 4T RT A8SW 2001111900130 20011119 00130 SO 2001 11 19 PNSA011002 1 20010930 A 2434 BELT PIPER PA32 PA32301 7103207 SO ALTERNATOR FAILED E PNSA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 AL 03 8402S 328106075 EN ROUTE ALTERNATOR STOPPED CHARGING. RETURNED TO DLG WHERE MAINTENANCE REPLACED ALTERNATOR BELT. 1 L 7 1 3O A3SO 2001111900131 20011119 00131 SW 2001 11 19 PNSA011003 1 20011012 A 7722 WIRE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP SRL COMPUTER BROKEN A PNSA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 41NE AC741B DURING CLIMB RT SRL COMPUTER FAIL LIGHT CAME ON. MX CONTACTED AND AIRCRAFT RETURNED TO BASE WHERE BROKEN WIRE WAS REPAI RED AT COMPUTER. 2 L 7 2 4T 4 T RT A8SW E4WE 2001111900132 20011119 00132 SW 2001 11 19 PNSA011005 1 20011027 A 5210 SEAL SWRNGN SA227 SA227AC 8780603 SW DOOR CONTAMINATED A PNSA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 650PA AC775B DURING CLIMB CABIN ALT LIGHT CAME ON. AIRCRAFT RETURNED TO MAINTENANCE BASE WHERE CABIN DOOR SEAL WAS FOUND WITH MOISTU RE PREVENTING CABIN FROM PRESSURIZING. 2 L 7 2 4T RT A8SW 2001111900133 20011119 00133 SW 2001 11 19 PNSA011006 1 20011029 A 3260 WARNING LIGHT SWRNGN SA227 SA227AC 8780603 SW COCKPIT FALSE INDICATION A PNSA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 AL 03 41NE AC741B AFTER TAKEOFF NOSE GEAR INTRANSIT LIGHT WOULD NOT EXTINGUISH. AIRCRAFT INSPECTED AND FERRIED TO ANC MAINTENANCE BASE. NO FAULT FOUND. 2 L 7 2 4T RT A8SW 2001111900134 20011119 00134 NM 2001 11 19 UPS01437296 1 20011103 A 5310 BUSHING BOEING 747 747200 1384847 NM BS 1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C R/H SIDE BS 1480 B/H FASTENER HOLE #1 FOUND CRACKED AT FUSELAGE SKIN, B/H CHORD AND OUTER CHORD SPLICE FITTING, PLS REFER TO ATT SKETCH FOR DETAILS. RH BS 1480 B/H HOLE #1 AT FUS SKIN, B/H CHORD AND OUTER CHORD SPLICE FTG CRACKS REMOVED BUSHING INSTALLED ON OUTER CHORD SPLICE FTG, B/H CHORD AND FUS SKIN HOLE #1 AS PER SB 747-53A2390 PLA N A BUSHING REPAIR CWPC CONTROL SEQUENCE NO.RCBR017060 AND RCBR017084 ATTACHED THIS REPAIR C/OUT I.A.W RS R-53-43-34702 AND EO B747-5310-15717-A. 2 L 7 4 4F RT A20WE 2001111900135 20011119 00135 NM 2001 11 19 UPS01437297 1 20011030 A 5310 DOUBLER BOEING 747 747200 1384847 NM LH #1 MED CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C M/D - LH #1 MED EXTERIOR SKIN LWR HINGE CUTOUT ATT DOUBLER FOUND CRACK AS MARKED. DOUBLER REPLACED AS PER R.S R52-11-34699. 2 L 7 4 4F RT A20WE 2001111900136 20011119 00136 NM 2001 11 19 UPS01437298 1 20011103 A 5310 65B07943557 STIFFENER BOEING 747 747200 1384847 NM NOSE W/W CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C NOSE WHEEL WELL BOX (TUNNEL AREA) STA 360 SIDE WALL PNL ATT HORI NO. 5 STIFFENER FOUND CRACKED AND MAR KED (COUNT FROM TOP). (LHS) STA 360 TO 380 NO.5 HORI-STIFFENER REPLACED PER SRM 51-10-01. 2 L 7 4 4F RT A20WE 2001111900137 20011119 00137 NM 2001 11 19 UPS01437300 1 20011103 A 5310 BUSHING BOEING 747 747200 1384847 NM BS 1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C AFT CARGO COMPT - LH BS 1480 B/H NO.11 HOLE FOUND CRACK AT FX SKIN AND OUTER CHORD SPLICE FITTING (REF ER ATT SKETCHES FOR DETAILS). LH BS 1480 B/H SKIN & OUTER SPLICE FTG HOLE NO.11 CRACKS REMOVED AND EXTENSION FTG, SK IN AND OUTER CHORD SPLICE FTG OVERSIZED TO INSTALL BUSHINGS IN HOLE NO.11 AS PER SB 747-53A2390 FIG.11 PLAN A BUSHING RE PAIR. CWPC CONTROL SEQUENCE NO.RCBR017 080 ATTACHED. 2 L 7 4 4F RT A20WE 2001111900138 20011119 00138 NM 2001 11 19 UPS01437301 1 20011103 A 5310 BUSHING BOEING 747 747200 1384847 NM BS 1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C L/H SIDE BS 1480 B/H FASTENER HOLE #18 FOUND CRACKED AT OUTER CHORD SPLICE FITTING, PLS REFER TO ATT S KETCH FOR DETAILS. LH BS 1480 B/H OUTER CHORD SPLICE FTG HOLE #18 CRACK REMOVED AND OUTER CHORD SPLICE FTG, B/H CHOR D, SKIN & LONGERON EXTENSION FTG OVERSIZED TO INSTALL BUSHINGS IN HOLE #18 AS PER SB 747-53A2390. CWPC CONTROL SEQUENCE NO.RCBR017 081 ATTACHED. 2 L 7 4 4F RT A20WE 2001111900139 20011119 00139 NM 2001 11 19 UPS01437303 1 20011103 A 5310 FITTING BOEING 747 747200 1384847 NM RH BS 1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C R/H SIDE BS 1480 B/H FASTENER HOLE #11 FOUND CRACKED AT B/H LONGERON EXTENSION FITTING, FUSELAGE SKIN AND B/H CHORD, PLS REFER TO ATT SKETCH FOR DETAILS. RH BS1480 B/H HOL #11 AT LONGERON EXTERSION FTG, FX SKIN & B/H C HORD CRACKS REMOVED. BUSH INSTALLED IN LONGERON EXTERSION, SKIN & CHORD HOLE #11 PLAN A BUSH REPAIRED AS PER SB 747-53A2 390. CWPC NO. RCBR017 TASH 057 ATT. RADIUS FILLER INSTALLED TO RH #11 HOLE ON THE LONGERON EXTERSION FTG AS PER RS R53-4 3-34702 & EO B747-5310-15717-A 2 L 7 4 4F RT A20WE 2001111900140 20011119 00140 NM 2001 11 19 UPS01437305 1 20011103 A 5310 FITTING BOEING 747 747200 1384847 NM RH BS 1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C R/H SIDE BS 1480 B/H FASTENER HOLE #9 FOUND CRACKED AT B/H LONGERON EXTENSION FITTING, FUSELAGE SKIN B /H CHORD AND OUTER CHROD SPLICE FITTING, PLS REFER TO ATT SKETCH FOR DETAIL. RH BS 1480 B/H LONGERON EXTENSION FTG F X SKIN, B/H CHORD & OUTER CHORD SPLICE FTG CRACKS REMOVED AT FS HOLE #9 BUSH INSTALLED IN LONGERON EXTENSION FTG, FX SKI N B/H CHORD & OUTER SPLICE FTG AT HOLE #9 AS PER SB 747-53A2390 FIG 11 PLAN A BUSH REPAIR CWPC #RCBR017 083 ATT. THIS RE PAIR AS PER RS R53-43-34702 & EO B747-5310-15717-A. 2 L 7 4 4F RT A20WE 2001111900141 20011119 00141 NM 2001 11 19 UPS01437306 1 20011103 A 5310 FITTING BOEING 747 747200 1384847 NM RH BS 1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C RH BS 1480 BULKHEAD ONE EA BOLT HOLE NO.25 FOUND TWO CRACKS AT OUTER CHORD SPLICE FITTING FWD SURFACE APPROX 0.030" AT 4 O'CLOCK POSITION ( LOOKING FWD ) AND 0.030" APPROX THROUGH THICKNESS AT 10 O'CLOCK POSITON. RH BS 1480 B/H SPLICE FTG BOLT HOLE #25 CRACK REMOVED. BUSHING INSTALLED IN OUTER CHORD SPLICE FTG HOLE NO.25 AS PER SB 747-5 3A2390 FIG 11 PLAN A BUSHING REPAIR RADIUS FILLER INSTALLED AS PER RS R53-43-34702. CWPC CONTROL SEQUENCE NO. RCBR017 05 8 ATTACHED. THIS REPAIR ACCOMPLISHED IAW EO B747-5310-15717-A. 2 L 7 4 4F RT A20WE 2001111900142 20011119 00142 NM 2001 11 19 UPS01437307 1 20011103 A 5310 FITTING BOEING 747 747200 1384847 NM LH BS 1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C AFT CARGO COMPT - LH BS 1480 B/H NO.9 HOLE FOUND CRACK AT EXTENSION FITTING AND OUTER CHORD SPLICE FIT TING ( REFER ATT SKETCHES FOR DETAILS ). LH BS 1480 B/H EXTENSION FTG AND OUTER CHORD SPLICE FTG HOLE NO.9 CRACKS RE MOVED AND BUSHINGS INSTALLED IN LONGERON EXTENSION FTG & OUTER CHORD SPLICE FTG AS PER SB 747-53A2390 PLAN A BUSHING REP AIR CWPC CONTROL SEQUENCE NO. RCBR017 049 ATTAHCED. 2 L 7 4 4F RT A20WE 2001111900143 20011119 00143 NM 2001 11 19 UPS01437308 1 20011101 A 5310 SPLICE PLATE BOEING 747 747200 1384847 NM LH SIDE BS 1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C LH SIDE BS 1480 BULKHEAD ONE EACH BOLT HOLE NO.23 FOUND CRACK AT SPLICE PLATE FWD SURFACE 1/8" APPROX AT 8 O'CLOCK POSITION REFER TO ATTTACHED DRAWING FOR DETAILS. LH BS 1480 B/H SPLICE PLATE AT HOLE #23 CRACK REMOVED AND BUSHING INSTALLED IN SPLICE PLATE AS PER SB 747-53A2390 FIG 11 PLAN A BUSHING REPAIR CWPC CONTROL SEQUENCE NO. RCBR0 17 079 ATTACHED. 2 L 7 4 4F RT A20WE 2001111900144 20011119 00144 NM 2001 11 19 UPS01437309 1 20011101 A 5310 WEB BOEING 747 747200 1384847 NM LH BS 1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C L/H SIDE BS 1480 BULKHEAD ONE EACH BOLT NO.26 FOUND CRACK AT BULKHEAD WEB FWD SURFACE 0.080" APPROX AT 8 O'CLOCK POSITION REFER TO ATTCHED DRAWING FOR DETAILS. LH BS 1480 B/H WEB AT HOLE #26 CRACK REMOVED AND BUSHING I NSTALLED AT WEB AS PER SB 747-53A2390 FIG 11. PLAN A BUSHING REPAIR. CWPC CONTROL SEQUENCE NO. RCBR017 052 ATTACHED. 2 L 7 4 4F RT A20WE 2001111900145 20011119 00145 2001 11 19 PNSA011007 4 20011029 A 2312 RADIO SWRNGN SA227 SA227AC 8780603 SW COCKPIT INOPERATIVE A PNSA K NONE O OTHER CR CRUISE 1 AL 03 640PA AC759B NUMBER ONE COM BECAME UNUSABLE. MAINTENANCE CONTACTED ON NR 2 COM AND RADIO WAS PLACED ON COMPANY MEL. FLIGHT CONTINUE D AND UPON LANDING RADIO WAS REPLACED. 2 L 7 2 4T RT A8SW 2001111900146 20011119 00146 SW 2001 11 19 PNSA011008 1 20011030 A 7620 CONTROL CABLE FRCHLD SA227 SA227DC 3377521 SW EMERGENCY STOP FROZEN A PNSA O OTHER O OTHER TX TAXI/GRND HDL 1 AL 03 30135 DC890B DURING PREFLIGHT EMERGENCY STOP CABLE WAS FROZEN. MAINTENANCE CONTACTED AND PURGED CABLE OF MOISTURE. 2 L 7 2 4T RT A18SW 2001111900147 20011119 00147 WP 2001 11 19 PNSA011009 2 20011031 A 7261 31080272 SCAVENGE PUMP FRCHLD SA227 SA227DC 3377521 SW GARRTT TPE331 TPE33112UA 01514 WP RT ENGINE SEIZED A PNSA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 AL 03 30135 4899 DC890B P70238 RT OIL PRESSURE LIGHT CAME ON. CREW SHUT DOWN ENGINE AND RETURNED TO CDB. MAINTENANCE FOUND EXCESSIVE OIL IN TAILPIPE AREA. ENGINE INSPECTED AND FOUND TURBINE SCAV PUMP SEIZED ALLOWING OIL TO DRAIN OVERBOARD. 2 L 7 2 4T 4 T RT A18SW E4WE 2001111900148 20011119 00148 SW 2001 11 19 PNSA011010 1 20011030 A 5270 SWITCH SWRNGN SA227 SA227AC 8780603 SW DOOR WARNNG INOPERATIVE A PNSA K NONE L NO TEST TX TAXI/GRND HDL 1 AL 03 41NE AC741B CARGO DOOR SECONDARY TEST SWITCH WAS FOUND INOP DURING PREFLIGHT. FLIGHT DELAYED UNTIL MAINTENANCE REPLACED SWITCH. 2 L 7 2 4T RT A8SW 2001111900149 20011119 00149 2001 11 19 QXEA0101713 4 20011016 A 2360 BOLT DHAV DHC8 DHC8202 2809007 NM LT MLG CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - LT MAIN LANDING GEAR FORWARD DOOR AFT SUPPORT ARM BONDING WIRE LOWER ATTACH BOLT HEAD CHAFING ON AFT SIDE OF CUT O UT FOR SUPPORT ARM. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001111900150 20011119 00150 SW 2001 11 19 PNSA11004 1 20011018 A 2910 HYDRAULIC LINE SWRNGN SA227 SA227AC 8780603 SW RT ENGINE CHAFED A PNSA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 AL 03 2719H AC713B RT HYDRAULIC LIGHT ILLUMINATED DURING CRUISE. AIRCRAFT RETURNED TO MAINTENANCE BASE WHERE HYDRAULIC PRESSURE LINE IN RT ENGINE FOR PUMP WAS FOUND CHAFED. 2 L 7 2 4T RT A8SW 2001111900151 20011119 00151 NM 2001 11 19 QXEA0101711 1 20011017 A 5410 FITTING DHAV DHC8 DHC8202 2809007 NM RT NACELLE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - RT MAIN LANDING GEAR H MEMBER WHERE ACTUATOR FITTING IS INSTALLED HAS PITTING CORROSION. REPAIRED IAW RD 8-54-921 . 2 H 7 2 4T RT A13NM 2001111900152 20011119 00152 NM 2001 11 19 QXEA0101712 1 20011021 A 5413 LONGERON DHAV DHC8 DHC8202 2809007 NM RT NACELLE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - RT NACELLE WHEEL WELL AT STATION ZN24.25 LOWER LONGERON XN125.50 HAS A GOUGE IN LONGERON LEFT FORWARD INBOARD SIDE . REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2001111900153 20011119 00153 NM 2001 11 19 QXEA0101714 1 20011018 A 5410 BRACKET DHAV DHC8 DHC8202 2809007 NM NR 2 ENGINE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 NR 2 ENGINE OUTBOARD FIREWALL BRACKET IS CRACKED. REPAIRED IAW RD 8-54-109, PAGES 1, 2, AND 3. 2 H 7 2 4T RT A13NM 2001111900154 20011119 00154 NM 2001 11 19 QXEA0101715 1 20011019 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - RT OUTBOARD SEAT TRACK X374 TO X379 HAS CORROSION PITS IN CHANNEL. REPAIRED IAW DHC-8 SRM 51-40-00 AND SRM 51-40- 11. 2 H 7 2 4T RT A13NM 2001111900155 20011119 00155 NM 2001 11 19 QXEA0101716 1 20011020 A 5520 BALANCE WEIGHT DHAV DHC8 DHC8202 2809007 NM ELEVATOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - HORIZONTAL STABILIZER LEADING EDGE, RT ELEVATOR WEIGHTS HAVE MINOR SCRATCHES/GOUGES ON TOP SURFACE. REPAIRED IAW DHC-8 SRM 51-20-11. 2 H 7 2 4T RT A13NM 2001111900156 20011119 00156 NM 2001 11 19 QXEA0101717 1 20011021 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - CHAFE IN FRAME ON LT SIDE WHERE LT SIDEWALL UPPER SUPPORT HAS BEEN RIDING AT STATION X539.0. REPAIRED IAW DHC-8 S RM 51-20-16, PAGES 1-5. 2 H 7 2 4T RT A13NM 2001111900157 20011119 00157 NM 2001 11 19 QXEA0101718 1 20011016 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - FUSELAGE SKIN, UNDER LOWER TCAS ANTENNA HAS CORROSION AREAS WITH PITTING. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 7 , PARAGRAPH 3 F (1) A AND FIGURE A. 2 H 7 2 4T RT A13NM 2001111900158 20011119 00158 NM 2001 11 19 QXEA0101719 1 20011019 A 5320 NUT PLATE DHAV DHC8 DHC8202 2809007 NM THRESHOLD CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - MAIN CABIN DOOR THRESHOLD HAS FIVE NUT PLATES HOLES WITH CORROSION. REPAIRED IAW DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2001111900159 20011119 00159 NM 2001 11 19 QXEA0101720 1 20011021 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - LT OUTBOARD SEAT TRACK NR 1 X372 TO X375 CHANNEL AND TOP FLANGE HAS CORROSION. INSTALLED NEW SEAT TRACK. 2 H 7 2 4T RT A13NM 2001111900160 20011119 00160 NM 2001 11 19 QXEA0101721 1 20011018 A 3222 STRUT DHAV DHC8 DHC8202 2809007 NM NLG CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - NOSE LANDING GEAR STRUT, LOWER STRUT IS CHAFED AT ELBOW. REPAIRED IAW RD 8-32-289, STEP 2, 3, 4, AND 5. 2 H 7 2 4T RT A13NM 2001111900161 20011119 00161 NM 2001 11 19 QXEA0101722 1 20011017 A 5720 SUPPORT BRACKET DHAV DHC8 DHC8202 2809007 NM LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - LEFT WING UPPER AND LOWER LEADING EDGE FRONT SPAR SUPPORT BRACKETS ARE CRACKED AT STATION YW137.00. REPAIRED IAW DHC-8-200 MM 51-40-00, PAGE 1. 2 H 7 2 4T RT A13NM 2001111900162 20011119 00162 NM 2001 11 19 QXEA0101723 1 20011017 A 5720 SUPPORT BRACKET DHAV DHC8 DHC8202 2809007 NM RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - RIGHT WING UPPER AND LOWER LEADING EDGE FRONT SPAR SUPPORT BRACKETS ARE CRACKED AT STATION YW137.00. REPAIRED IAW DHC-8-200 MM 51-40-00, PAGE 1. 2 H 7 2 4T RT A13NM 2001111900163 20011119 00163 NM 2001 11 19 QXEA0101724 1 20011020 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - RIGHT WING NR 4 FLAP TRACK OUTBOARD SIDE ROLLER, SIDE TRACK HAS 2 HEAVY ROLLER WEAR MARKS AND FINISH COATING MISSI NG. REPAIRED IAW HORIZON AIR EA 2-57-144. 2 H 7 2 4T RT A13NM 2001111900164 20011119 00164 NM 2001 11 19 QXEA0101725 1 20011020 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - RIGHT WING NR 4 FLAP OUTBOARD BOTTOM TRACK HAS 3 ROLLER WEAR MARKS. REPAIRED IAW HORIZON AIR EA 2-57-144. 2 H 7 2 4T RT A13NM 2001111900165 20011119 00165 NM 2001 11 19 QXEA0101726 1 20011020 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - RIGHT WING NR 4 FLAP TRACK INBOARD SIDE TRACK IS PITTED FROM SIDE ROLLER. REPAIRED IAW HORIZON AIR EA 2-57-144. 2 H 7 2 4T RT A13NM 2001111900166 20011119 00166 NM 2001 11 19 QXEA0101727 1 20011020 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - RIGHT WING NR 4 FLAP TRACK INBOARD BOTTOM TRACK HAS WEAR MARKS FROM FRONT OF ROLLER STOP AND AT AFT ROLLER STOP. REPAIRED IAW HORIZON AIR EA 2-57-144. 2 H 7 2 4T RT A13NM 2001111900167 20011119 00167 NM 2001 11 19 QXEA0101728 1 20011020 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - RIGHT WING NR 4 FLAP TRACK TOP TRACK HAS ROLLER WEAR AT FORWARD END OF TRACK AND SURFACE COATING WORN THROUGH. RE PAIRED IAW HORIZON AIR EA 2-57-144. 2 H 7 2 4T RT A13NM 2001111900168 20011119 00168 NM 2001 11 19 QXEA0101729 1 20011021 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - RIGHT WING NR 3 FLAP TRACK ON NACELLE HAS 2 HEAVY WEAR MARKS FROM ROLLERS. REPAIRED IAW RD 8-57-987. 2 H 7 2 4T RT A13NM 2001111900169 20011119 00169 NM 2001 11 19 QXEA0101730 1 20011021 A 5410 SUPPORT DHAV DHC8 DHC8202 2809007 NM NR 2 NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - NR 2 NACELLE AFT OVERBOARD DRAIN TUBE CHAFING ON UNDERSIDE OF FINGERNAIL SUPPORT DECK. REPAIRED IAW RD 8-54-097. 2 H 7 2 4T RT A13NM 2001111900170 20011119 00170 NM 2001 11 19 QXEA0101731 1 20011020 A 5753 FLAP DHAV DHC8 DHC8202 2809007 NM RT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - RIGHT WING OUTBOARD FLAP HAS CUT IN FLAP. REPAIRED IAW RD 8-57-1734 AND DASH 9 MM 20-32-02 AND MM 20-34-11. 2 H 7 2 4T RT A13NM 2001111900171 20011119 00171 NM 2001 11 19 QXEA0101732 1 20011021 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - CARGO DOOR HAS CHAFE DAMAGE ON OUTSIDE SKIN LOCATED AT UPPER AFT SIDE OF DOOR ON REPAIR STRAP. REPAIRED IAW DHC-8 -200 SRM 51-20-26. 2 H 7 2 4T RT A13NM 2001111900172 20011119 00172 NM 2001 11 19 QXEA0101733 1 20011020 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - THE FORWARD EDGE OF FRAME AT STATION X618.00 BETWEEN STRINGER 21R AND 22R, HAS DAMAGE. REPAIRED IAW DHC-8 SRM 51- 20-11. 2 H 7 2 4T RT A13NM 2001111900173 20011119 00173 NM 2001 11 19 QXEA0101734 1 20011021 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - LT NR 1 UPPER FLAP TRACK UNDERSIDE SHOWS SIGNS OF ROLLER WEAR. REPAIRED IAW RD 8-57-985. 2 H 7 2 4T RT A13NM 2001111900174 20011119 00174 NM 2001 11 19 QXEA0101735 1 20011021 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - LT NR 1 LOWER FLAP TRACK TOP SIDE SHOWS SIGNS OF ROLLER WEAR. REPAIRED IAW RD 8-57-985. 2 H 7 2 4T RT A13NM 2001111900175 20011119 00175 NM 2001 11 19 QXEA0101736 1 20011021 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - LT NR 2 UPPER FLAP TRACK UNDERSIDE SHOWS SIGNS OF ROLLER WEAR. REPAIRED IAW RD 8-57-986. 2 H 7 2 4T RT A13NM 2001111900176 20011119 00176 NM 2001 11 19 QXEA0101737 1 20011021 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - LT NR 2 LOWER FLAP TRACK TOP SIDE SHOWS SIGNS OF ROLLER WEAR. REPAIRED IAW RD 8-57-986. 2 H 7 2 4T RT A13NM 2001111900177 20011119 00177 NM 2001 11 19 QXEA0101738 1 20011021 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - LT NR 3 UPPER FLAP TRACK UNDERSIDE SHOWS SIGNS OF WEAR IN TWO PLACES. REPAIRED IAW RD 8-57-987. 2 H 7 2 4T RT A13NM 2001111900178 20011119 00178 NM 2001 11 19 QXEA0101739 1 20011021 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - LT NR 3 LOWER FLAP TRACK TOP SIDE SHOWS SIGNS OF WEAR IN THREE PLACES. REPAIRED IAW RD 8-57-987. 2 H 7 2 4T RT A13NM 2001111900179 20011119 00179 NM 2001 11 19 QXEA0101740 1 20011020 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - LT NR 4 FLAP TRACK TOP SHOWS SIGNS OF ROLLER WEAR. REPAIRED IAW HORIZON AIR EA 2-57-143. 2 H 7 2 4T RT A13NM 2001111900180 20011119 00180 NM 2001 11 19 QXEA0101741 1 20011020 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - LT NR 4 FLAP TRACK INBOARD LOWER TRACK SHOWS SIGNS OF WEAR. REPAIRED IAW HORIZON AIR EA 2-57-143. 2 H 7 2 4T RT A13NM 2001111900181 20011119 00181 NM 2001 11 19 QXEA0101742 1 20011020 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - LT NR 4 FLAP TRACK OUTBOARD UPPER TRACK SHOWS SIGNS OF ROLLER WEAR. REPAIRED IAW HORIZON AIR EA 2-57-143. 2 H 7 2 4T RT A13NM 2001111900182 20011119 00182 NM 2001 11 19 QXEA0101743 1 20011020 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - LT NR 4 FLAP TRACK OUTBOARD LOWER TRACK SHOWS SIGNS OF ROLLER WEAR. REPAIRED IAW HORIZON AIR EA 2-57-143. 2 H 7 2 4T RT A13NM 2001111900183 20011119 00183 NM 2001 11 19 QXEA0101744 1 20011018 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - LT NR 5 FLAP TRACK TOP SHOWS SIGNS OF ROLLER WEAR IN TWO PLACES. REPAIRED IAW HORIZON AIR EA 2-57-145. 2 H 7 2 4T RT A13NM 2001112000001 20011120 00001 NE 2001 11 20 01EVA006 2 20011118 A 7200 CF680C2D1FG07 ENGINE DOUG MD11 MD11 3023602 NM GE CF6 CF680C2D1F 30025 NE UNSERVICEABLE W QOCF C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 03 105EV 48544 704599 1.AIRCRAFT LOW SPEED T/O ABORTED (ABOUT 95 KTS) DUE TO "ENG FAIL" LT ON WITH "BAN" SOUD HEARD. AFTER ABORT ACTION COMPLE TED. "ENG FAIL" RED LT WENT OFF. 2.GND VISUAL INSPETED NO. ENG EXHAUST SLEEVE, FOUND METAL CHIP AROUND INNER SURFACE, AN D METAL CHIPS FOUND ON THE OIL MMCD. 3. PFM NO.1 ENG, FND HPC-1 AND THE FOLLOWING STAGES ALL WERE DAMAGED AND OVERLIMIT PER MM 72-00-07. 4.PFM NO.1 ENG CHANGED PER MM 71-00-00 AND PFM "PRE-TESTED TEST", ALL COND NML AND NO LEAK FND. 2 L 7 3 4F 4 F RT A22WE E31N3 2001112000002 20011120 00002 WP 2001 11 20 0104149868 1 20010904 A 5330 DOUBLER DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 777NC 47787 During Mck in ATL, four cracks were found in the ground air conditioning access panel doubler. Two of the cracks are lo cated where the latches for the access cover contact the panel doubler. The cracks were trimmed out. Material 0.050" thi ck 2014-t6 aluminum clad sheet.Repaired per EA. 98-185041. 2 L 7 2 4F RT A6WE 2001112000003 20011120 00003 WP 2001 11 20 0104179886 1 20010905 A 5330 SKIN DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 600TR 47783 While in DHN for Hck, one hole for a NAS 1097 AD6 rivet station 69.5 was found with crack indication. This hole location is not covered by reference. Repaired per EA 98-185678. 2 L 7 2 4F RT A6WE 2001112000004 20011120 00004 WP 2001 11 20 0104199868 1 20010914 A 5310 FITTING DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 777NC 47787 During Mck in Atl., A crack was found in the forward airstair aft support fitting. The crack was 5/8 long. Material 7075 -t7651 aluminum plate . Repaired per EA 98-185142. 2 L 7 2 4F RT A6WE 2001112000005 20011120 00005 WP 2001 11 20 0104129994 1 20011108 A 5310 PRESSURE PANEL DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8979E 47328 During Hck in ATL, a crack was found in the flight compartment horizontal pressure panel at station 105. The 1.5" crack is located at X=35. Material 0.040" thick 2024-t3 aluminum clad sheet. EA 99-185277 2 L 7 2 4F A6WE 2001112000006 20011120 00006 WP 2001 11 20 0104139916 1 20011108 A 5410 RIB DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 949N 47566 During Hck at ATL, the pylon closing rib was found cracked at sta YN 176 LHS, at the portion of the lower cap. A new low er cap section was installed and spliced with repair angle. Material 0.040 TI-6AI-4V titanium. Repaired per EA 99-185300 2 L 7 2 4F A6WE 2001080700021 20010807 00021 EA 2001 8 7 MASA01066 1 20010114 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 07 37228 7228 FLT 6019 - COS-PHX - DURING PRE-FLIGHT, PILOT FOUND LOWER EMERGENCY EXIT SIGN OUT. MAINTENANCE REPAIRED A BROKEN WIRE B EHIND THE SIGN. OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001112000007 20011120 00007 EA 2001 11 20 COMA0160905 1 20011118 A 5346 60135006 BEAM CNDAIR CL600 CL6002B19 1900309 EA AFT EQUIPMENT BA CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 940CA 16622 7048 CRACK ON ENGINE SUPPORT BEAM UPPER WEB.REPAIRED I/A/W REO 601R-53-61-345. 2 L 7 2 4F RT A21EA 2001112000008 20011120 00008 NM 2001 11 20 0104246642 1 20011017 A 5315 FLOORBEAM BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 642NW 21942 DURING "H" CHECK FOUND CORROSION ON FLOORBEAM LOWER CHORD AT BS 1780 LBL 24. REPAIRED PER EA 66-186583. 2 L 7 4 4F RT A20WE 2001112000009 20011120 00009 NM 2001 11 20 0104256642 1 20011003 A 5315 FLOORBEAM BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 642NW 21942 DURING "H" CHECK FOUND CORROSION ON UPPER DECK FLOORBEAM UPPER CHORD AT BS 500 LBL 46. REPAIRED PER EA 66-186643. 2 L 7 4 4F RT A20WE 2001112000010 20011120 00010 NM 2001 11 20 0104266642 1 20011031 A 5311 FRAME BOEING 747 747212B 1384886 NM CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 642NW 21942 During "H" check found crack in frame at BS 2231 at door 5L S24L and S25L. Repaired per EA 66-186830. 2 L 7 4 4F A20WE 2001112000011 20011120 00011 NM 2001 11 20 0104276642 1 20011110 A 5730 SKIN PANEL BOEING 747 747212B 1384886 NM CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 642NW 21942 During "H" check found corrosion on center wing upper skin panel at WS 1050 RBL 125 and S27. Repaired per EA 66-186829. 2 L 7 4 4F A20WE 2001112000012 20011120 00012 EA 2001 11 20 COMA0160906 1 20011115 A 5610 601R330333 WINDOW CNDAIR CL600 CL6002B19 1900309 EA L/H CRACKED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 916CA 12818 7014 FLIGHT #6363 - PILOTS SIDE WINDOW CRACKED DURING FLIGHT.REPLACED THE PILOTS SIDE WINDOW. 2 L 7 2 4F RT A21EA 2001112000013 20011120 00013 EA 2001 11 20 COMA0160907 1 20011115 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR BURNED OUT A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 779CA 7306 FLIGHT #5392. FWD EXTERIOR EMERGENCY LIGHTS ARE INOP.REPLACED THE FWD L/H AND R/H EMERGENCY LIGHT BULBS. 2 L 7 2 4F RT A21EA 2001112000014 20011120 00014 EA 2001 11 20 COMA0160908 1 20011115 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA R/H EXT BURNED OUT A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 969CA 7141 R/H EXTERIOR EMERGENCY LIGHT INOP.REPLACED LIGHT BULB. 2 L 7 2 4F RT A21EA 2001112000015 20011120 00015 EA 2001 11 20 COMA0160909 1 20011115 A 2730 DL2428M4 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA VERT STAB MALFUNCTIONED A COMA O OTHER F FLT CONT AFFECTED UK UNKNOWN 1 SO 01 798CA 4460 7348 FLIGHT #5182. FORCE TO MOVE ELEVATORS IS EXCESSIVE.REPLACED THE R/H PITCH FEEL ACTUATOR. 2 L 7 2 4F RT A21EA 2001112000016 20011120 00016 WP 2001 11 20 0104299949 1 20011112 A 5310 LONGERON DOUG DC9 DC931 3022065 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8928E 45865 During HCK in ATL, The 5911415-113 Longeron #11 left was found to have corrosion on the lower horizontal flange at the f wd end (sta 756). Material 0.050 7075-t6 extrusion. Repaired per EA 99-185303. 2 L 7 2 4F A6WE 2001112000017 20011120 00017 WP 2001 11 20 2001F00639 1 20011018 A 3350 AD4002P BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 822US 49139 IND - THE LOW LEVEL EMERGENCY LIGHTS AT SEAT ROWS 3 AND 25 AND THE CEILING EMERGENCY LIGHTS BETWEEN SEAT ROWS 5 AND 8 AN D 27 AND 30 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. REF USAAD01172. (M) 2 L 7 2 4F A6WE 2001112000018 20011120 00018 NM 2001 11 20 USAA011269 1 20010928 A 5330 SKIN BOEING 757 7572B7 1384964 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 615AU 27146 CLT - FOUND SKIN DENT .375 INCH WIDE BY .035 DEEP, LEFT FUSELAGE STATION 600 BETWEEN S15L AND S19L. INSTALLED REPAIR DO UBLER. (M) 2 L 7 2 4F RT A2NM 2001112000019 20011120 00019 NM 2001 11 20 USAA011288 1 20010831 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 601AU 22193 CLT - FOUND SKIN DENTED 9 INCH BY 10 INCH, S23L TO S24L STATION 240-250. INSTALLED REPAIR DOUBLER PER 53-00-01 FIG 204. (M) 2 L 7 2 4F RT A2NM 2001112000020 20011120 00020 NM 2001 11 20 USAA011305 1 20010831 A 5242 SKIN BOEING 757 757225 1384959 NM E/E DOOR DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 601AU 54736 22193 CLT - FOUND E/E DOOR EXT SKIN 5 INCH BY 6 INCHES, STATION 460 STRINGER 28L TO 29L MAIN E/E DOOR. PREVIOUSLY INSTALLED P ATH. (M) 2 L 7 2 4F RT A2NM 2001112000021 20011120 00021 NM 2001 11 20 USAA011308 1 20011002 A 5310 146NS2465 CREASE BEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 611AU 30450 27123 CLT - FOUND CREASE BEAM CORRODED .250 INCH BY .250 INCH, LEFT DOOR SILL AREA L4. REMOVED AND REPLACED PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 2001112000022 20011120 00022 NM 2001 11 20 CALA011006 1 20011120 A 5230 FRAME BOEING 737 7373T0 1384582 NM AFT CARGO DR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71314 23365 INSPECTION FOUND A 1" CRACK IN AFT CARGO DOOR FORWARD FRAME BETWEEN #3 & #4 STOP FITTINGS. THE FRAME WAS REMOVED AND A N EW FRAME WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001112000023 20011120 00023 NM 2001 11 20 CALA011007 1 20011120 A 5320 ANGLE BOEING 737 7373T0 1384582 NM STA 870 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71314 23365 INSPECTION FOUND AFT L-ANGLE SUPPORT FOR SILL WEB CORRODED AT AFT PIT THRESHOLD, STA 870, LONGERON 25L. THE ANGLE WAS RE MOVED AND REPLACED IAW SRM 51-40-00. 2 L 7 2 4F RT A16WE 2001112000024 20011120 00024 EU 2001 11 20 USAABA01012 1 20011024 A 3350 321430 BATTERY AIRBUS 330 A330323 3930335 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 670UW 315 PHL - EPSU'S AT DOORS L2 AND L3 FAIL SELF-TEST. MAINTENANCE REPLACED THE BATTERIES FOR THE EPSU'S. (M) 2 L 7 2 4F RT A46NM 2001112000025 20011120 00025 NM 2001 11 20 USAABB01102 1 20010930 A 3350 9221009 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 629AU 27807 CLT - FOUND R4 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2001112000026 20011120 00026 NM 2001 11 20 USAABB01107 1 20011021 A 3350 8731002511REV14 SIGN BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 609AU 22205 PHL - FOUND THE R2 DOOR EMERGENCY EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE IDENTIFIER ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001112000027 20011120 00027 NM 2001 11 20 USAABB01108 1 20011021 A 3350 873100151REV12 LIGHT BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 609AU 22205 PHL - FOUND LOW LEVEL EMERGENCY LIGHT AT ROW 6 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001112000028 20011120 00028 NM 2001 11 20 USAABB01109 1 20011021 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 632AU 27810 CLT - FOUND THE FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 1, 4, 6 AND 9 DIM. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2001112000029 20011120 00029 NM 2001 11 20 USAABB01110 1 20011024 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 610AU 27122 LAX - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 1 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001112000030 20011120 00030 WP 2001 11 20 USAAD01172 1 20011018 A 3350 971055 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 822US 49139 IND - THE LOW LEVEL EMERGENCY LIGHTS AT SEAT ROWS 3 AND 25 AND THE CEILING EMERGENCY LIGHTS BETWEEN SEAT ROWS 5 AND 8 AN D 27 AND 30 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001112000031 20011120 00031 WP 2001 11 20 USAAD01173 1 20011021 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 800US 48034 BOS - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 2001112000032 20011120 00032 WP 2001 11 20 USAAD01174 1 20011021 A 3260 WARNING LIGHT DOUG DC9 DC982 3022082 WP COCKPIT ILLUMINATED A USAA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 EA 19 818US 48098 PIT - BOS - FLT 564 - AFTER TAKEOFF, THE LANDING GEAR HANDLE WAS PLACED IN THE UP POSITION. THE MAIN GEAR RETRACTED BUT THE NOSE GEAR UNSAFE LIGHT ILLUMINATED ALONG WITH VIBRATION. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INC IDENT. MAINTENANCE INSPECTED AND LUBED THE NOSE GEAR. THE GEAR WAS SWUNG SEVERAL TIMES, ALL INDICATIONS AND OPERATION WAS NORMAL. (M) 2 L 7 2 4F A6WE 2001112000033 20011120 00033 2001 11 20 USAAD01175 4 20011021 A 2565 D29985103 SLIDE DOUG DC9 DC981 3022081 WP SERVICE DOOR UNSERVICEABLE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 803US 48035 PIT - THE L2 SERVICE DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS LOW. MAINTENANCE REPLACED THE EMERGE NCY EVACUATION SLIDE. (M) 2 L 7 2 4F A6WE 2001112000034 20011120 00034 EU 2001 11 20 USAAF01054 1 20010726 A 5220 A20401978 DOOR FOKKER F28 F28MK0100 4990807 EU CABIN UNSERVICEABLE A USAA K NONE O OTHER CL CLIMB 1 EA 19 857US 11289 FLT 835 - EN ROUTE PIT-STL, DURING CLIMB-OUT, THE RIGHT OVERWING EMERGENCY EXIT DOORS BEGAN TO MAKE NOISE, THEN THE COVE RS FOR THE EMERGENCY DOOR EMERGENCY RELEASE HANDLE FELL OFF. THE PASSENGERS IN THE EXIT ROWS WERE RESEATED AND THE FLIG HT CONTINUED TO STL. AFTER LANDING, THE EMERGENCY EXIT DOORS FELL OUT OF THE EMERGENCY EXIT OPENINGS ONTO THE EMERGENCY ROW SEATS. MAINTENANCE REPLACED THE RIGHT SIDE OVER-WING EMERGENCY EXIT DOORS. ACCOMPLISHED RIGH AND LEAK CHECKS, AND FOUND OK. (M) 2 L 7 2 4F RT 2001112000035 20011120 00035 EU 2001 11 20 USAAF01055 1 20010726 A 5220 A20401978 DOOR FOKKER F28 F28MK0100 4990807 EU CABIN UNSERVICEABLE A USAA K NONE O OTHER CL CLIMB 1 EA 19 857US 11289 CLT - FLT 9281 - EN ROUTE STL-CLT - DURING THE FLIGHT, THE RIGHT OVER-WING EMERGENCY EXIT DOORS BECAME UNLATCHED. AFTER LANDING, THE EMERGENCY EXIT DOORS FELL OUT OF THE EMERGENCY EXIT OPENINGS ONTO THE EMERGENCY ROW SEATS. MAINTENANCE RE PLACED THE RIGHT SIDE OVER-WING EMERGENCY EXIT DOORS. ACCOMPLISHED RIGHT AND LEAK CHECKS, AND FOUND OK. (M) 2 L 7 2 4F RT 2001082100068 20010821 00068 EA 2001 8 21 COMA0160615 1 20010819 A 3297 WIRE CNDAIR CL600 CL6002B19 1900309 EA NR 2 DISPLAY LOOSE A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 933CA 7040 FLIGHT 5931. DURING TAXI OUT OF CVG RECEIVED A PROXIMITY FAULT STATUS MESSAGE ON ELECTRONIC DISPLAY NR 2, AIRCRAFT RETUR NED TO THE GATE.REPAIRED WIRING AND SECURED GROUNDING STUD. 2 L 7 2 4F RT A21EA 2001112000036 20011120 00036 EU 2001 11 20 USAAF01075 1 20011006 A 3232 125005 ACTUATOR FOKKER F28 F28MK0100 4990807 EU NLG DOOR FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 882US 11334 RIC-CLT - FLT 1008 - AFTER TAKEOFF, THE NOSE LANDING GEAR FAILED TO RETRACT. THE GEAR WAS CYCLED WITH NO CHANGE. THE A IRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE GEAR AND FOUND SAFE TO FERRY TO PI T WITH THE GEAR DOWN. PIT MAINTENANCE REPLACED THE NOSE LANDING GEAR DOOR ACTUATOR. (M) 2 L 7 2 4F RT 2001112000037 20011120 00037 EU 2001 11 20 USAAF01076 1 20011007 A 3233 415005 ACTUATOR FOKKER F28 F28MK0100 4990807 EU LT MLG FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 881US 1643 11333 PIT-RDU - FLT 280 - AFTER TAKEOFF, THE LEFT MAIN LANDING GEAR WOULD NOT RETRACT. WHEN TRYING TO EXTEND THE LANDING GEAR , THE NOSE GEAR EXTENDED BUT NOT THE MAIN GEAR. THE ALTERNATE GEAR EXTENSION WAS USED TO EXTEND THE GEAR. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN GEAR RETRACT ACTUATOR. (M) 2 L 7 2 4F RT 2001112000038 20011120 00038 EU 2001 11 20 USAAF01077 1 20011011 A 2150 22034802 A/C PACK FOKKER F28 F28MK0100 4990807 EU A/C BAY RUPTURED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 19 851US 11278 PIT-SDF - FLT 1912 - ON SHORT FINAL, CREW FELT A BUMP AS IF THE AIRCRAFT HAD BEEN STRUCK, AND SHORTLY AFTER HEAVY SMOKE ENTERED BOTH THE COCKPIT AND THE CABIN. MAINTENANCE REPLACED THE LEFT AIR CONDITIONING REFRIGERATION UNIT. (M) 2 L 7 2 4F RT 2001112000039 20011120 00039 EU 2001 11 20 USAAF01078 1 20011015 A 2170 5391 COALESCER BAG FOKKER F28 F28MK0100 4990807 EU A/C BAY CONTAMINATED A USAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 EA 19 892US 11372 RDU-CLT - FLT 487 - SHORTLY AFTER TAKEOFF, THE RIGHT LAVATORY SMOKE DETECTOR ACTIVATED. 30 SECONDS LATER THE LEFT LAVAT ORY SMOKE DETECTOR ALSO ACTIVATED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. BOTH SMOKE DETECTOR ALARMS STOPPED BEFORE LANDING. MAINTENANCE REPLACED THE RIGHT AIR CONDITIONING PACK WATER SEPARATOR BAG AND CLEANED TH E FINGER SCREEN AT THE SEPARATOR. (M) 2 L 7 2 4F RT 2001112000040 20011120 00040 EU 2001 11 20 USAASA01019 1 20010511 A 3350 32145510 POWER SUPPLY AIRBUS A321 A321211 3930370 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 161UW 946 1403 LAX - THE EMERGENCY LIGHTS DO NOT TEST PROPERLY. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNITS. TESTED OK. (M) 2 L 7 2 4F RT A28NM 2001112000041 20011120 00041 EU 2001 11 20 USAASA01051 1 20010923 A 3242 BRAKE AIRBUS 320 A320214 3930316 EU NR 2 OVERHEATED A USAA K NONE M OVER TEMP CR CRUISE 1 EA 19 109UW 6723 1065 DEN - FLT 183 - EN ROUTE PHL-DEN, AFTER TAKEOFF AND LANDING GEAR RETRACTION, THE NR 2 BRAKE WENT FROM 300 TO 500 DEGREES IN SEVERAL SECONDS TIME. THE LANDING GEAR WAS LOWERED AND THE BRAKE FAN ACTIVATED. THE BRAKE TEMPERATURE THEN DECREAS ED TO BELOW 100 DEGREES IN SEVERAL SECONDS TIME. THE FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. (M) 2 L 7 2 4F RT A28NM 2001112000042 20011120 00042 2001 11 20 USAASA01052 4 20010927 A 2350 C12848AA01 CONTROL PANEL AIRBUS A319 A319112 3930323 EU COCKPIT SHORTED A USAA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 717UW 7285 1069 PBI - FLT 270 - EN ROUTE MIA-PIT, AFTER TAKEOFF, RECEIVED A NR 1 RADIO MANAGEMENT PANEL ELECTRICAL FAULT LIGHT, NAVIGATI ON ILS FAULT, AND GROUND PROXIMITY FAULT. THE RADIOS ALSO BECAME INOPERATIVE. AFTER A RESET OF THE CIRCUIT BREAKERS, A BURNING ELECTRICAL SMELL BECAME PRESENT IN THE COCKPIT. THE FLIGHT DIVERTED TO PBI AND LANDED WITHOUT FURTHER INCIDENT . MAINTENANCE REPLACED THE NR 1 AND 2 RADIO MANAGEMENT PANELS. OPERATIONALLY CHECKED NORMALLY. (M) 2 L 7 2 4F RT A28NM 2001112000043 20011120 00043 EU 2001 11 20 USAASA01054 1 20011009 A 3350 0L815BPR LIGHT AIRBUS A319 A319112 3930323 EU CABIN WRONG PART A USAA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 EA 19 762US 1358 CLT - AFTER REPLACEMENT OF SEAT ROW 3 ABC, IT WAS DISCOVERED THAT THE EMERGENCY EXIT LIGHT INSTALLED ON THE SEAT WAS AN INCORRECT PART AND WOULD NOT ILLUMINATE. MAINTENANCE REPLACED THE BULBS. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2001112000044 20011120 00044 NM 2001 11 20 VNAA0111008 1 20011118 A 2100 56826000 SWITCH DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 434JS 16557 3051 AFTER DEPARTING PHL, THE CREW RECEIVED A PACK FAIL AND OVER PRESSURE INDICATION. MAINTENANCE CONTROL AND DISPATCH DECID ED THAT FLIGHT 4062 SHOULD DIVERT TO CAK. MAINTENANCE AT CAK INSPECTED AND REPLACED THE OVERPRESSURE SWITCH IN ACCORDAN CE WITH DORNIER MAINTENANCE MANUAL 21-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVIC E. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001112000045 20011120 00045 EU 2001 11 20 USAASA01055 1 20011016 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319112 3930323 EU CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 743UW 1277 PHL - THE RIGHT EMERGENCY POWER SUPPLY UNIT FAULTED. MAINTENANCE REPLACED THE RIGHT EMERGENCY POWER SUPPLY UNIT. OPERA TIONAL CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2001112000046 20011120 00046 NM 2001 11 20 USAASB01273 1 20010928 A 5230 SEAL BOEING 737 737301 1384611 NM CARGO DOOR OUT OF POSITION A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 19 591US 23936 JAX - FLT 1505 - DURING DESCENT, FLIGHT ATTENDANTS AND PAX NOTICED AN ELEC BURNING SMELL IN THE AFT CABIN WITH A LOUD SQ UEALING NOISE. PAX WERE HOLDING THEIR EARS AND COMPLAINING OF THE NOISE. FLIGHT LANDED WITHOUT INCIDENT. MX INSPECTED OF ALL CABIN LIGHTS, COFFEE MAKERS IN AFT GALLEY, AFT LAVATORIES AND TRASH CONTAINERS, SMOKE DETECTORS AND LIGHTING SYS TEM IN CARGO BINS. TESTED OUTFLOW VALVE AND INSPECTED JACKSCREW COMPARTMENT AREA. NO SOURCE OF SMELL FOUND. INSPECTE D DOOR SEALS AND BULKHEAD. NO DEFECTS NOTED. THE NEXT DAY, THE LOUD SQUEAL REPEATED ON DESCENT THROUGH 15,000 FEET. MX FOUND THE AFT CARGO DOOR HAD TWO INCHES OF SEAL OUT OF TRACK. ALSO, FOUND DEBRIS IN AFT SINK CAUSING LOUD SQUEAL. OPERA 2 L 7 2 4F RT A16WE 2001112000047 20011120 00047 NM 2001 11 20 USAASB01274 1 20010930 A 3260 189929 SENSOR BOEING 737 7374B7 1384702 NM RT MLG OUT OF ADJ A USAA L A ABORTED APPROACH UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 438US 24560 ALB - FLT 977 - ON CLIMB-OUT FROM ALB, EN ROUTE TO PHL, CREW COULD NOT GET THE LANDING GEAR LEVER TO THE UP POSITION. Q UICK REFERENCE HANDBOOK PROCEDURES WERE ACCOMPLISHED AND PULLING OVERRIDE TRIGGER BROUGHT THE GEAR UP. HOWEVER, WHEN TH RUST LEVERS MOVED FORWARD OF THE VERTICAL POSITION AND THE FLAPS RETRACTED, THE TAKEOFF WARNING HORN SOUNDED CONTINUOUSL Y. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND RETURNED TO FIELD AT ALB FOR FLYBY AND LANDING. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE AIRSAFETY SENSOR OUT OF LIMITS WITH TARGET . ADJUSTED SENSOR PER MM. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001112000048 20011120 00048 NM 2001 11 20 USAASB01284 1 20011006 A 3230 LANDING GEAR BOEING 737 737301 1384611 NM NLG & MLG LACK OF LUBE A USAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 19 341US 23510 CLT - FLT 237 - AFTER TAKEOFF FROM ORF, EN ROUTE TO CLT, CREW RECEIVED MAIN LANDING GEAR RED UNSAFE LIGHTS WITH GEAR HAN DLE SELECTED TO OFF POSITION. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND LIGHTS EXTINGUISHED. FLIGHT CO NTINUED ONTO CLT. ON EXTENSION FOR LANDING, GEAR INDICATION WAS NORMAL. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE F OUND ALL THREE LANDING GEAR LACKING LUBRICATION. LUBRICATED LANDING GEAR PER MAINTENANCE MANUAL. CYCLED LANDING GEAR S EVERAL TIMES. ALL SYSTEMS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2001112000049 20011120 00049 NM 2001 11 20 USAASB01287 1 20011008 A 3260 189929 UPLOCK SENSOR BOEING 737 737301 1384611 NM LT MLG DEFECTIVE A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 19 351US 23554 PHL - FLT 8959 - AFTER TAKEOFF AND GEAR RETRACTION FROM MCO, EN ROUTE TO PHL, THE LEFT MAIN LANDING GEAR RED UNSAFE LIGH T ILLUMINATED STEADY, THEN INTERMITTENTLY AND THEN EXTINGUISHED. CREW RECYCLED GEAR AND GEAR INDICATION WAS NORMAL. FL IGHT CONTINUED ONTO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LEFT MAIN LANDING GEAR UPLOCK SENSOR DEFECTIVE. REMOVED AND REPLACED SENSOR. OPS CHECK OF INDICATION SYSTEM NORMAL. (M) 2 L 7 2 4F RT A16WE 2001112000050 20011120 00050 NM 2001 11 20 USAASB01288 1 20011008 A 2751 2061141 INDICATOR BOEING 737 737301 1384611 NM COCKPIT FAULTY A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 354US 23557 BUF - FLT 1157 - AFTER TAKEOFF FROM BUF, EN ROUTE TO CLT, CREW EXPERIENCED A FLAP ASYMMETRY PROBLEM DURING FLAP RETRACTI ON. ONE FLAP WAS IN THE 5 DEGREE POSITION AND THE OTHER WAS IN THE 2 DEGREE POSITION. CREW DECLARED AN EMERGENCY AND R ETURNED TO FIELD AT BUF WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP POSITION INDICATOR AND INSP ECTED/CLEANED CANNON PLUG ON FLAP TRANSMITTER. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001112000051 20011120 00051 NM 2001 11 20 USAASB01291 1 20011009 A 4950 10327431 SEAL BOEING 737 7374B7 1384702 NM APU TORN A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 432US 24554 CLT - FLT 1108 - EN ROUTE, WITH MEL 26-13 APPLIED. AT FL250, CREW WAS UNABLE TO MAINTAIN CABIN ALTITUDE WITH ONLY THE L T PACK OPERATING. OUTFLOW VALVE WAS IN THE CLOSED POSITION AND STANDBY OR MANUAL PRESSURIZATION MODE WAS NO HELP, CREW COULD NOT MAINTAIN CABIN ALTITUDE. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MX FOUND THE APU AIR DUCT SEAL, WHERE THE APU DUCT PASSES THROUGH THE AFT PRESSURE BULKHEAD, TORN AND CLAMP DISENGAGED. REPLACE D SEAL AND CLAMP. PRESSURIZED AIRCRAFT. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2001112000052 20011120 00052 NM 2001 11 20 USAASB01293 1 20011010 A 3350 6013211 BATTERY PACK BOEING 737 7372B7 1384560 NM CARGO BAY DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 277AU 22889 BWI - MAINTENANCE FOUND THE FORWARD ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED T HE BATTERY PACK (P/N 61-0478-9) AND POWER SUPPLY (P/N 6013211). OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 2001112000053 20011120 00053 NM 2001 11 20 USAASB01294 1 20011013 A 3350 6104789 BATTERY PACK BOEING 737 737201 1384454 NM CARGO BAY DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 251AU 22757 BWI - THE RIGHT OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK. (M) 2 L 7 2 4F A16WE 2001112000054 20011120 00054 WP 2001 11 20 GTIA010390 1 20010516 A 5511 CHANNEL DOUG DC9 DC982 3022082 WP HORIZ STAB DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - NR 2 RIGHT AFT SPAR HAT CHANNEL HAS DAMAGE DOT LEFT -30 (RT HORIZ) XHS 50.00 XHS 104.00. REMOVED HAT CHANNEL FOR REPAIR IAW BOEING MD80 SRM 55-01 FIG 1. PERFORMED CHANNEL IAW BOEING MD80 SRM 55-01 FIG 1. INSTALLED CHANNEL IAW BOEIN G MD80 SRM 55-01 FIG 1. (M) 2 L 7 2 4F A6WE 2001112000055 20011120 00055 WP 2001 11 20 GTIA010427 1 20010519 A 5523 TAB DOUG DC9 DC982 3022082 WP ELEVATOR DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND DAMAGE ON ANTI-FLOAT TAB SPRING QUADRANT (RT HORIZ) DAMAGE IS ON CASTING ONLY (FRAME). REMOVED ANTI-FLOAT T AB SPRING QUADRANT AS PER MD80 MM 27-30-14. INSTALLED ANTI-FLOAT. TAB SPRING QUADRANT IAW MD80 MM 27-30-14. (M) 2 L 7 2 4F A6WE 2001112000056 20011120 00056 WP 2001 11 20 GTIA010973 1 20011011 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 812NK 48021 DTW - FOUND L2 AND AFT CABIN EMERGENCY EXIT SIGNS INOPERATIVE. REPAIRED WIRING AT AFT BATTERY PACK. OPS CHECK NORMAL I AW MD80 MM 33-63-01. (M) 2 L 7 2 4F A6WE 2001112000057 20011120 00057 2001 11 20 GTIA010974 4 20011009 A 2565 LANYARD DOUG DC9 DC982 3022082 WP L1 DOOR BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 957AS 49126 L1 DOOR EMERGENCY EXIT DOOR EVACUATION SLIDE CABLE ATTACH TO GIRT BAR BROKEN. REMOVED AND REPLACED LANYARD ASSY ON L1 D OOR IAW MM CH 25-60-00. (M) 2 L 7 2 4F A6WE 2001112000058 20011120 00058 WP 2001 11 20 GTIA010975 1 20011011 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 DALLO 53012 FLL - PORTABLE EMERGENCY LIGHT AT L1 DOOR INOPERATIVE. REMOVED AND REPLACED PORTABLE EMERGENCY LIGHT AT L1 DOOR. OPS C HECK NORMAL IAW MD-80 MM 33-50-00. (M) 2 L 7 2 4F RT A6WE 2001112000059 20011120 00059 WP 2001 11 20 GTIA010977 1 20010518 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND CORROSION ON ANGLE AT STRINGER 28R AT STATION 1136. REMOVED ANGLE IAW MD-80 SRM 51-30-1. FABRICATED ANGLE BRACKET IAW MD-80 SRM 51-10-03. (M) 2 L 7 2 4F A6WE 2001112000060 20011120 00060 WP 2001 11 20 GTIA010980 1 20010530 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FUSELAGE SKIN REPAIR BETWEEN STATION 200-229 AND L15R AND L18R. CHECK FUSELAGE FOR SMOOTH SKIN LIMITS. DENT AT S TATION 229 RIGHT OF FUSELAGE BETWEEN LONGERON 17 AND 18, FOUND TO BE OUT OF LIMITS IAW SRM MD-80 53-04 FIG 38. CUT DAMA GED AREA ON DENT OUT OF LIMITS IAW SRM MD80 53-04. FORMED REPAIR IAW MD80 SRM 53-04 OK TO TREAT AND PRIME. INSTALLED R EPAIRED PARTS IAW MD80 SRM 53-04. (M) 2 L 7 2 4F A6WE 2001112000061 20011120 00061 WP 2001 11 20 GTIA011057 1 20010828 A 5753 FLAP DOUG DC9 DC981 3022081 WP RT WING MISALIGNED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - RIGHT WING INBOARD FLAP INBOARD TRAILING EDGE FLAP MISALIGNMENT PREVIOUS INSTALLATION. REMOVED T/E WEDGE ON INBOA RD FLAP. LOCATE AND DRILL TRAILING EDGE. INSTALLED NEW TRAILING EDGE IAW MD80 SRM 51-10-3. (M) 2 L 7 2 4F A6WE 2001112000062 20011120 00062 WP 2001 11 20 GTIA011058 1 20010825 A 5753 WEDGE DOUG DC9 DC981 3022081 WP T/E FLAP MISALIGNED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - LEFT INBOARD TRAILING EDGE IS MISALIGNED BETWEEN INBOARD AND OUTBOARD SECTIONS. REMOVED LEFT, INBOARD, TRAILING E DGE FLAP THAT WAS MISALIGNED BETWEEN INBOARD AND OUTBOARD SECTIONS. LOCATE AND DRILL T/E WEDGE. INSTALLED TRAILING EDG E WEDGE IAW MD80 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 2001112000063 20011120 00063 WP 2001 11 20 GTIA011059 1 20010817 A 5753 FLAP DOUG DC9 DC981 3022081 WP LT WING DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - LEFT OUTBOARD TRAILING EDGE FLAP HAS BEEN TEMP REPAIRED AT TRAILING EDGE, OUTBOARD SURFACE. CUT OUT DAMAGED SECTI ON OF LEFT, OUTBOARD, TRAILING EDGE FLAP. REPAIRED DAMAGED SECTION OF LEFT, OUTBOARD, TRAILING EDGE FLAP IAW DC9 MD80 S RM 57-03. (M) 2 L 7 2 4F A6WE 2001112000064 20011120 00064 WP 2001 11 20 GTIA011060 1 20010826 A 5751 AILERON DOUG DC9 DC981 3022081 WP LT WING DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - LEFT WING AILERON TRAILING EDGE IS DELAMINATING. REPAIRED DAMAGED AREA PER SRM MD80 57-03. BALANCED LEFT AILERON PER BOEING DC9/MD80 SRM 57-50-1. (M) 2 L 7 2 4F A6WE 2001112000065 20011120 00065 NM 2001 11 20 SWAA013116 1 20011116 A 5310 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 385SW 26600 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 183, WL 233 & RBL 17.1. R&R WEB PER SRM. 2 L 7 2 4F RT A16WE 2001112000066 20011120 00066 NM 2001 11 20 SWAA013117 1 20011116 A 5310 6516300 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED 1/2D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234 & LBL 12. REPAIRE D WEB PER SRM. 2 L 7 2 4F RT A16WE 2001112000067 20011120 00067 NM 2001 11 20 SWAA013118 1 20011113 A 5310 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14L & 15L. REP AIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2001112000068 20011120 00068 NM 2001 11 20 SWAA013119 1 20011118 A 5310 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS178, RBL 17.1. R&R WEB PER SRM. 2 L 7 2 4F RT A16WE 2001112000069 20011120 00069 NM 2001 11 20 SWAA013122 1 20011115 A 3246 0320143 TIRE BOEING 737 7372H4 138448C NM RH NLG BLEW OUT A SWAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 060SW 21812 ( AIR TURNBACK, DECLARED EMERGENCY )…………………………..DURING T/O RH NOSE TIRE BLEW DAMAGING TCAS ANTENNA AND FUSELAGE SKIN FWD OF TCAS ANTENNA. R&R BOTH NLG TIRE/WHEEL ASSY'S. R&R LWR TCAS ANTENNA & REPAIRED SKIN PER SWA RA. 2 L 7 2 4F A16WE 2001112000070 20011120 00070 WP 2001 11 20 GTIA011061 1 20010817 A 5753 FLAP DOUG DC9 DC981 3022081 WP LT WING DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 LEFT WING OUTBOARD FLAP TRAILING EDGE IS DELAMINATING. CUT OUT DAMAGED SECTION OF LEFT WING OUTBOARD FLAP TRAILING EDGE . REPAIRED DAMAGED SECTION OF LEFT WING OUTBOARD FLAP IAW DC9/MD-80 SRM 57-03. (M) 2 L 7 2 4F A6WE 2001112000071 20011120 00071 WP 2001 11 20 GTIA011062 1 20010811 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP COCKPIT CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - COCKPIT FLOOR PANEL BENEATH CO-PILOTS SEAT IS CORRODED. REMOVED FLOOR PANEL, CORRODED OUT OF LIMITS. FORM NEW PA NEL PER MD80 SRM 51-10-2. (M) 2 L 7 2 4F A6WE 2001112000072 20011120 00072 WP 2001 11 20 GTIA011063 1 20010811 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP COCKPIT CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 COCKPIT FLOOR PANEL BENEATH PILOT SEAT IS CORRODED. FOUND TO BE OUT OF LIMITS. FORMED NEW PANEL IAW MD80 SRM 53-21-0. (M) 2 L 7 2 4F A6WE 2001112000073 20011120 00073 WP 2001 11 20 GTIA011064 1 20010818 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - SEAT TRACK RIGHT OUTBOARD CRACKED IN CENTER OF TRACK. REMOVED SECTION OF SEAT TRACK. FABRICATED SEAT TRACK. INS TALLED SEAT TRACK IAW MD80 SRM 53-40-1. (M) 2 L 7 2 4F A6WE 2001112000074 20011120 00074 WP 2001 11 20 GTIA011065 1 20010821 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - FOUND SEAT TRACK RIGHT INBOARD HAVE CORROSION. REMOVED SEAT TRACK. FABRICATED SEAT TRACK AND DRILLED AS REQUIRED . INSTALLED SEAT TRACK IAW MD80 MM 53-40-1. (M) 2 L 7 2 4F A6WE 2001112000075 20011120 00075 WP 2001 11 20 GTIA011066 1 20010821 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - FOUND SEAT TRACK RIGHT INBOARD HAS SURFACE CORROSION. REMOVED SEAT TRACK. FABRICATED NEW SEAT TRACK. INSTALLED SEAT TRACK IAW MD80 SRM 53-05. (M) 2 L 7 2 4F A6WE 2001112000076 20011120 00076 WP 2001 11 20 GTIA011067 1 20010818 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FOUND SEAT TRACK RIGHT INBOARD GOUGED. FOUND CORROSION TO BE OUT OF LIMITS. CUT OUT THE SECTION OF SEAT TRACK. DRILLE D AND LOCATE (FABRICATE) SEAT TRACK. INSTALLED SEAT TRACK AT STATION 1031 IAW MD80 SRM 53-05. (M) 2 L 7 2 4F A6WE 2001112000077 20011120 00077 WP 2001 11 20 GTIA011068 1 20010813 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - FOUND SEAT TRACK RIGHT INBOARD GOUGED AND PITTED. REMOVED AND SEAT TRACK. FABRICATED, DRILLED AND LOCATED SEAT T RACK. INSTALLED SEAT TRACK IAW MD80 SRM 53-04. (M) 2 L 7 2 4F A6WE 2001112000078 20011120 00078 WP 2001 11 20 0104159868 1 20010905 A 5310 DOOR FRAME DOUG DC9 DC951 3022051 WP FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 777NC 47787 DURING MCK IN ATL CORROSION FOUND AND A DOUBLE DRILLED HOLE WERE FOUND IN THE LOWER SECTION OF THE JAMB OF THE AFT VENTR AL DOOR. THE CORROSION WAS REMOVED BY CUTTING OUT THE JAMB. AFTER REMOVAL OF THE REPAIR, CORROSION WAS ALSO FOUND IN T HE JAMB. REPAIRED PER EA 98-185086. 2 L 7 2 4F RT A6WE 2001112000079 20011120 00079 WP 2001 11 20 0104169868 1 20010905 A 5320 TEE FITTING DOUG DC9 DC951 3022051 WP FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 777NC 47787 DURING MCK IN ATL, CORROSION WAS FOUND IN THE FUSELAGE CUSP TEE AT STA 1165. THE DAMAGE PORTION OF THE TEE WAS CUT AT S TATION 1160. REPAIRED PER EA 98-185119. 2 L 7 2 4F RT A6WE 2001112000080 20011120 00080 WP 2001 11 20 0104189866 1 20010909 A 5310 DOOR FRAME DOUG DC9 DC951 3022051 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 775NC 47785 DURING LINE CHECK IN CMH, A CRACK WAS NOTED IN THE APB VENTRAL DOOR JAMB PAN. THE CRACK WAS LOCATED 24 INCHES UP FROM T HE FLOOR LINE ON THE LHS SIDE BY THE ROLLER ASSEMBLY. THE .375 INCH CRACK IS IN THE RADIUS OF THE DOOR JAMB. REPAIRED PER EA 98-164476. 2 L 7 2 4F RT A6WE 2001112000081 20011120 00081 WP 2001 11 20 0104289994 1 20011109 A 5315 FLOORBEAM DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8979E 47328 DURING HCK IN ATL A CRACK WAS DISCOVERED IN THE WEB OF THE STA Y 237 FLOORBEAM AT X=7 LEFT. THE CRACK MEASURES 2.75 INC H IN LENGTH. MATERIAL 7075-T6511 ALUMINUM EXTRUSION. REPAIRED PER EA 99-185262. 2 L 7 2 4F A6WE 2001112000082 20011120 00082 WP 2001 11 20 01FDEA001001 1 20011113 A 7830 GEARBOX DOUG DC10 DC1010 3022110 WP NR 1 T/R MALFUNCTIONED A FDEA K NONE O OTHER LD LANDING 1 SO 25 367FE 46605 NR 1 THRUST REVERSER FAILED TO STOW AFTER LANDING. REMOVED AND REPLACED ALL CABLES AND GEAR BOX ASSY PER MM 78-32-07. 2 L 7 3 4F A22WE 2001112000083 20011120 00083 NM 2001 11 20 01FDEA00993 1 20011115 A 3230 LANDING GEAR DOUG MD11 MD11F 3023600 NM NLG MALFUNCTIONED A FDEA J DUMP FUEL J WARNING INDICATION CL CLIMB 1 SO 25 619FE 48770 FLT 5081 WRI, AFTER T/O NOSE GEAR WOULD NOT RETRACT. 2 L 7 3 4F RT A22WE 2001112000084 20011120 00084 NM 2001 11 20 01FDEA00994 1 20011115 A 2841 WARNING SYSTEM DOUG MD11 MD11 3023602 NM COCKPIT ACTIVATED A FDEA K NONE J WARNING INDICATION CR CRUISE 1 SO 25 586FE 48487 FLT 5155 WRI, NR 1 ALERT TANK 3 TIP FUEL LOW. 2 L 7 3 4F RT A22WE 2001112000085 20011120 00085 NE 2001 11 20 01FDEA00995 2 20011115 A 7200 ENGINE AIRBUS 310 A310222 3930315 EU PWA JT9 JT9D7R4E1 52054 NE NR 1 SURGES A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 419FE 345 716114 MULTIPLE ENGINE SURGE NR 1 ENGINE WITH ENG AND WING ANTI-ICE ON. 2 L 7 2 4F 4 F RT A35EU E3NE 2001113000024 20011130 00024 EU 2001 11 30 01FDEA00996 1 20011116 A 3411 SENSOR AIRBUS 310 A310222 3930315 EU PITOT/STATIC SYS FAULTY A FDEA A UNSCHED LANDING N A FALSE WARNING FLAME/FIRE CR CRUISE 1 SO 25 422FE 346 LOSS ALL PURGE NR 1 ENGINE WITH ENG AND WING ANTI-ICE ON. CK SENSOR FAULT NIL, PERF PITOT SYS LEAK CK. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2001112000086 20011120 00086 NM 2001 11 20 01FDEA00997 1 20011115 A 3242 BRAKE BOEING 727 727233 138408A NM MLG FIRE A FDEA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 SO 25 222FE 20933 BRAKE FIRE ON NR 3 AND 4 RED. REMOVED AND REPLACED 3 & 4 BRACKET, AND MAIN WHEEL ASSY PER AMM 32-45-001-4, 32-42-001-5. 2 L 7 3 4F RT A3WE 2001112000087 20011120 00087 2001 11 20 01FDEA00999 4 20011116 A 3452 4816R22555 CONNECTOR BOEING 727 727233 138408A NM TRANSPONDER NOT SEATED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 282FE 22349 NR 1 & 2 TRANSPONDER INOP. RESET CONNECTOR ON ATC CONTROL PANEL. OPS CK GOOD PER MM 34-43-00-5 & BOEING SWPM 20-60-06. 2 L 7 3 4F RT A3WE 2001112000088 20011120 00088 EU 2001 11 20 01FDEA01000 1 20011117 A 7722 WARNING SYSTEM AIRBUS 310 A310221 3930310 EU PWA JT9 JT9D7R4E1 52054 NE COCKPIT ACTIVATED A FDEA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 25 416FE 288 716117 ON CLIMBOUT NR 1 EGT PEGGED AT MAX GAUGE NOSE GEAR SHOW UNSAFE. 2 L 7 2 4F 4 F RT A35EU E3NE 2001112000089 20011120 00089 EU 2001 11 20 01FDEA01002 1 20011117 A 2612 FIRE WARNING AIRBUS 300 A300F4605R 3930327 EU COCKPIT ACTIVATED A FDEA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 25 665FE 769 RECEIVED MAIN CARGO DECK 1 & 2 FIRE IND. SHUTDOWN A/C AND INSP APU. 2 L 7 2 4F RT A35EU 2001112000090 20011120 00090 2001 11 20 2001F00600 4 20011106 A 2564 710FAUL030110 LIFE RAFT GULSTM G1159 GIV 3980115 SO CABIN PUNCTURED Z K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 99 1 N254GA A LIFE RAFT WAS RECEIVED FROM MARSHALL AEROSPACE FOR INSPECT, TEST, AND RECERTIFICATION. THE RAFT HAD BEEN OVERHAULED A MONTH PREVIOUSLY BY A REPAIR STATION THAT HAD JAR-145 APPROVAL (BUT DID NOT HAVE FAR-145 APPROVAL). DURING LEAK CHECK TEST, IT WAS FOUND THAT THE RAFT WAS CONTINUOUSLY DEFLATING DUE TO PUNCTURES IN THE FABRIC. THIS DAMAGE WAS PROBABLY CAU SED DURING PACKING. 2 L 7 2 4F RT A12EA 2001112000094 20011120 00094 NE 2001 11 20 2001UIA007 2 20011106 A 7230 V2525D5 COMPRESSOR DOUG MD90 MD9030 3023690 NM IAE V2525 V2525D5 NE LT ENGINE DAMAGED Z B EMER. DESCENT O OTHER CR CRUISE 1 TW 00 17923 4795 53534 V20091 IN FLIGHT, LT ENG SURGE, EGT HIGH TO 660 C, MAIN IDLE TO LAND (IDLE N2:68.5 EGT:426 N1:33 EPR:0.9). THE ENG PFM BSI FOU ND STAGE 6 HPC DAMAGE. REPLACED SERVICEABLE ENG IAW AMM71-00-10, AND IAW AMM 71-02-10 ENG RUN-UP CHECK NORMAL. 2 L 7 2 4F 4 F RT A6WE A40NE 2001112000095 20011120 00095 NM 2001 11 20 A6WA200100064 1 20011114 A 2612 51653151 CONTROL UNIT DORNER DO32 DO328100 2996000 NM NR 2 ENGINE FAULTY A A6WA F ACTIVATE FIRE EXT. N FALSE WARNING NR NOT REPORTED 1 GL 31 329ML 2686 2686 3087 NR 2 ENGINE FIRE INDICATION ON GROUND WITH ENGINE NOT RUNNING. DISCHARGED NR 2 ENGINE FIRE BOTTLE. MAINTENANCE REMOVED AND REPLACED FIRE WARNING CONTROL UNIT. 2 H 7 2 4T RT A45NM 2001112000096 20011120 00096 WP 2001 11 20 ABXA010585 1 20011026 A 5330 59122851 DOUBLER DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 983AX 47257 LEFT WINDOW DOUBLER CRACKED IN THE UPPER FORWARD CORNER OF WINDOW AT STATION 699. REPAIRED CRACK IAW DC-9 SSRM K07226. 2 L 7 2 4F A6WE 2001112000098 20011120 00098 WP 2001 11 20 ARWA20011104 1 20011118 A 2910 HYDRAULIC LINE DOUG DC8 DC861 3021952 WP LT MLG LEAKING A ARWA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 19 29UA 46159 AFTER T/O LOST HYDRAULIC FLUID TO STAND PIPE AND PRESS 0, PERFORMED LOSS OF HYDRAULIC FLUID AND PRESS CHECKLIST AND RETU RNED TO MIAMI. LANDED IN MIAMI OVERWEIGHT AT 272,600 WITHOUT INCIDENT. FOUND LT MLG BUNGEE CYLINDER PRESSURE LINE LEAK ING. REMOVED AND REPLACED LINE IAW MM 20-12-0, SERVICED HYDRAULIC SYSTEM IAW MM 12-30-1. PERFORMED LEAK CHECK IAW MM 2 9-00 FOUND NORMAL NO LEAK NOTED. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION A-INSPECTION IAW FA DC8 MM J/C 6100, NO DIS CREPANCIES NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2001112000100 20011120 00100 NM 2001 11 20 QXEA0101745 1 20011018 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - LT NR 5 FLAP TRACK INBOARD UPPER TRACK HAS ROLLER WEAR IN TWO PLACES. REPAIRED IAW HORIZON AIR EA 2-57-145. 2 H 7 2 4T RT A13NM 2001112000101 20011120 00101 NM 2001 11 20 QXEA0101746 1 20011018 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - LT NR 5 FLAP TRACK OUTBOARD LOWER TRACK HAS ROLLER WEAR IN 2 PLACES. REPAIRED IAW HORIZON AIR EA 2-57-145. 2 H 7 2 4T RT A13NM 2001112000102 20011120 00102 NM 2001 11 20 QXEA0101747 1 20011020 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - RIGHT WING NR 4 FLAP TRACK INBOARD BOTTOM TRACK HAS PITTING 1.5 INCHES FROM ATTACH POINT TO 2 INCHES FROM ATTACH P OINT. REPAIRED IAW HORIZON AIR EA 2-57-144. 2 H 7 2 4T RT A13NM 2001112000103 20011120 00103 NM 2001 11 20 QXEA0101748 1 20011018 A 5320 BRACKET DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - RT OUTBOARD SEAT TRACK BRACKET AT X262.400 HAS CORROSION AT TOP AFT RIVET HOLE AREA. REPAIRED IAW DHC-8 SRM 51-20 -11, PAGE 7. 2 H 7 2 4T RT A13NM 2001112000104 20011120 00104 NM 2001 11 20 QXEA0101749 1 20011025 A 5410 BRACKET DHAV DHC8 DHC8202 2809007 NM NR 1 ENGINE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - NR 1 ENGINE INBOARD FIREWALL BRACKET IS CRACKED. REPAIRED IAW HORIZON AIR EA 2-54-111. 2 H 7 2 4T RT A13NM 2001112000105 20011120 00105 NM 2001 11 20 QXEA0101750 1 20011024 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - LT INBOARD SEAT TRACK (NR 4) FROM X170 TO X255 SEAT TRACK CAMLOCK RECEPTACLE HOLES SHOW CORROSION UNDER DRIP TRAY. REPAIRED IAW DHC-8-200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001112000106 20011120 00106 NM 2001 11 20 QXEA0101751 1 20011024 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - RT INBOARD SEAT TRACK NR 7 FROM X170 TO X255 CAMLOCK RECEPTACLES ON INBOARD FLANGE SHOW CORROSION. REPAIRED IAW D HC-8-200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001112000107 20011120 00107 NM 2001 11 20 QXEA0101752 1 20011023 A 5322 BEAM DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - INBOARD COAT CLOSET MOUNT BEAM HAS CORROSION AT NUT PLATE X218 Y16L. REPAIRED IAW DHC-8-200 SRM 51-20-11, PAGE 7, PARAGRAPH 3. 2 H 7 2 4T RT A13NM 2001112000108 20011120 00108 NM 2001 11 20 QXEA0101753 1 20011023 A 5322 BEAM DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - OUTBOARD BEAM FOR COAT CLOSE PAN X202 TO X218 AT 433L HAS LIGHT CORROSION AT NUT PLATES. REPAIRED IAW DHC-8-200 S RM 51-20-11. 2 H 7 2 4T RT A13NM 2001112000109 20011120 00109 NM 2001 11 20 QXEA0101754 1 20011023 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - RT OUTBOARD SEAT TRACK NR 11 X436 TO X439 HAS NICKS ON THE TOP FLANGE. REPAIRED IAW DHC-8-200 SRM 51-20-16, PAGE 4. 2 H 7 2 4T RT A13NM 2001112000110 20011120 00110 NM 2001 11 20 QXEA0101755 1 20011023 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - RT OUTBOARD SEAT TRACK NR 12 X551 HAS ONE NICK ON THE TOP FLANGE. REPAIRED IAW DHC-8 SRM 51-20-16, PAGE 4, 2 H 7 2 4T RT A13NM 2001112000111 20011120 00111 NM 2001 11 20 QXEA0101756 1 20011023 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - RT OUTBOARD SEAT TRACK NR 12 X561 HAS ONE NICK/GOUGE IN THE CHANNEL. REPAIRED IAW DHC-8 SRM 51-20-16, PAGE 4. 2 H 7 2 4T RT A13NM 2001112000112 20011120 00112 NM 2001 11 20 QXEA0101757 1 20011023 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - RT INBOARD SEAT TRACK NR 9 X562 TO X565 HAS CHANNEL GOUGES FROM BULKHEAD. REPAIRED IAW DHC-8 SRM 51-20-16, PAGE 4 . 2 H 7 2 4T RT A13NM 2001112000113 20011120 00113 NM 2001 11 20 QXEA0101758 1 20011023 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - RT INBOARD SEAT TRACK NR 9 X562 TO X570 HAS NO PAINT AND LIGHT CORROSION PITS. REPAIRED IAW DHC-8 SRM 51-20-16, P AGE 4. 2 H 7 2 4T RT A13NM 2001112000114 20011120 00114 NM 2001 11 20 QXEA0101759 1 20011023 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - LT INBOARD SEAT TRACK NR 5 HAS NICKS ON TOP FLANGE AT X453 TO S456. REPAIRED IAW DHC-8-200 SRM 51-20-16, PAGE 4, PARAGRAPH C. 2 H 7 2 4T RT A13NM 2001112000115 20011120 00115 NM 2001 11 20 QXEA0101760 1 20011023 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - LT INBOARD SEAT TRACK NR 5 HAS NICK ON TOP FLANGE AT X486. REPAIRED IAW DHC-8 SRM 51-20-16, PAGE 4, PARAGRAPH C. 2 H 7 2 4T RT A13NM 2001112000116 20011120 00116 NM 2001 11 20 QXEA0101761 1 20011023 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - LT INBOARD SEAT TRACK X528 HAS SEVERAL NICKS ON TOP FLANGE. REPAIRED IAW DHC-8-200 SRM 51-20-16, PAGE 4, PARAGRAP H C. 2 H 7 2 4T RT A13NM 2001112000117 20011120 00117 NM 2001 11 20 QXEA0101762 1 20011023 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - LT INBOARD SEAT TRACK NR 6 X530 HAS NICKS IN CHANNEL. REPAIRED IAW DHC-8-200 SRM 51-20-16, PAGE 4, PARAGRAPH C. 2 H 7 2 4T RT A13NM 2001112000118 20011120 00118 NM 2001 11 20 QXEA0101763 1 20011024 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - LT INBOARD SEAT TRACK NR 6 X545 TO X548 HAS NICKS IN CHANNEL. REPAIRED IAW RD 8-53-4936. 2 H 7 2 4T RT A13NM 2001112000119 20011120 00119 NM 2001 11 20 QXEA0101764 1 20011024 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - LT INBOARD SEAT TRACK NR 6 HAS LIGHT PITTING CORROSION WHERE PAINT IS MISSING. REPAIRED IAW RD 8-53-4936. 2 H 7 2 4T RT A13NM 2001112000120 20011120 00120 NM 2001 11 20 QXEA0101765 1 20011023 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - LT OUTBOARD SEAT TRACK NR 2 X517.5 TO X515.5 HAS TOP FLANGE NICKS. REPAIRED IAW DHC-8-200 SRM 51-20-16, PAGE 4, P ARAGRAPH C. 2 H 7 2 4T RT A13NM 2001112000121 20011120 00121 NM 2001 11 20 QXEA0101766 1 20011023 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - LT OUTBOARD SEAT TRACK NR 3 X530.5 HAS TOP FLANGE NICKS. REPAIRED IAW DHC-8-200 SRM 51-20-16, PAGE 4, PARAGRAPH C . 2 H 7 2 4T RT A13NM 2001112000122 20011120 00122 NM 2001 11 20 QXEA0101767 1 20011023 A 5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - LIGHT CORROSION AT FIVE NUT PLATE HOLES, STA 215.5 BELOW COAT CLOSET AT FLOOR BOARD SUPPORTS. REPAIRED IAW DHC-8- 200 SRM 51-20-11, PAGE 7, PARAGRAPH 3. 2 H 7 2 4T RT A13NM 2001112000123 20011120 00123 NM 2001 11 20 QXEA0101769 1 20011023 A 5410 STIFFENER DHAV DHC8 DHC8202 2809007 NM NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - UNDERSIDE FINGERNAIL DECK OUTBOARD STIFFENER CRACKED. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2001112000124 20011120 00124 NM 2001 11 20 2001UALA02232 1 20011106 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 FRAME AT STATION 1400 BETWEEN STRINGERS 26L AND 27L CRACKED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACOCMPLISHED.INSTALL ED DOUBLER REPAIR TO FRAME. 2 L 7 2 4F 4 F RT A2NM E17NE 2001112000125 20011120 00125 NM 2001 11 20 2001UALA02240 1 20011108 A 5313 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 INTERCOSTAL AT STATION 1666 TO 1681.8 RBL 57 TO RBL 54 CORRODED ON UPPER SURFACE BELOW GUTTER IN DOORWAY 4R. SUPPLEME NTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REMOVED AND INSTALLED NEW PART (J-ANGLE) INTERCOSTAL.. 2 L 7 2 4F 4 F RT A2NM E17NE 2001112000126 20011120 00126 NM 2001 11 20 2001UALA02241 1 20011108 A 5414 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 521UA 24891 #2 PYLON FWD INBD SKIN PANEL CUTOUT, SKIN CRACKED AT AFT UPPER CORNER OF CUTOUT AS SEEN FROM INSIDE, CRACK APPROXIMATELY .250" LONG. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. APPLIED DOUBLER, TRIPLER,QUADRUPLER REPAIR TO SKIN. 2 L 7 2 4F 4 F RT A2NM E17NE 2001112000127 20011120 00127 NM 2001 11 20 2001UALA02254 1 20011106 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 FRAME AT STATION 1400 BETWEEN STRINGERS 26L AND 27L. CRACKED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. DOUBLE R REPAIR INSTALLED ON THE FRAME. 2 L 7 2 4F 4 F RT A2NM E17NE 2001112000128 20011120 00128 NM 2001 11 20 2001UALA02256 1 20011112 A 5313 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 LEFT CABIN CREASE BEAM FLOORBOARD SUPPORT DAMAGED. STA 1355-1383, LBL 65 SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLIS HED.SPLICED NEW ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001112000129 20011120 00129 NM 2001 11 20 2001UALA02257 1 20011111 A 5300 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 CABIN FLOOR INTERCOSTAL BELOW DOORWAY DRAIN GUTTER CORRODED ON UPPER SURFACE BETWEEN STA 324 AND 345, RBL 61 AT STRINGER 17R. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPLACED Z-ANGLE SHAPED INTERCOSTAL WITH NEW PART. 2 L 7 2 4F 4 F RT A2NM E17NE 2001112000130 20011120 00130 NM 2001 11 20 2001UALA02258 1 20011111 A 5300 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 521UA 24891 MID CABIN CREASE BEAM BODY STATION 1020 TO BODY STATION 1040 AT STRINGER 17R HAS CORROSION ON UPPER SURFACE WEB. SUPPLEM ENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.WEB REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2001112000131 20011120 00131 NM 2001 11 20 2001UALA02259 1 20011111 A 5300 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 521UA 24891 MID CABIN CREASE BEAM BODY STATION 1000 TO BODY STATION 1020 AT STRINGER 17R HAS CORROSION ON UPPER SURFACE OF WEB. SUPP LEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. WEB REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2001112000132 20011120 00132 NM 2001 11 20 2001UALA02260 1 20011111 A 5313 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 521UA 24891 MID CABIN CREASE BEAM BODY STATION 960 TO BODY STATION 980 STRINGER 17L HAS TOOLING DAMAGE ON WEB. SUPPLEMENTAL DATA UPD ATE MAJOR REPAIR ACCOMPLISHED.WEB REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2001112000133 20011120 00133 NM 2001 11 20 2001UALA02263 1 20011111 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 521UA 24891 AFT PIT LEFT HAND SIDE AT STATION 1440 FRAME IS DENTED BETWEEN STRINGER 25L AND 26L. SUPPLEMENTAL DATA UPDATE MAJOR REP AIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2001113000028 20011130 00028 NM 2001 11 30 2001UALA02267 1 20011108 A 2740 MS2764640G BEARING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE STAB TRIM FAILED A UALA K NONE F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 399UA 24674 TRIM WHEEL MAKES LOUD GRINDING NOISE. MAINTENANCE REPORTED TRIM VERY DIFFICULT TO OPERATE. STABILIZER TRIM CONTROL SHA FT BEARING WAS DISINTEGRATED RESULTING IN DAMAGE TO SHAFT, SPACER AND RT TRIM WHEEL. REPAIRED BY REPLACING SHAFT AND TR IM WHEEL, AND ACCOMPLISHING BOEING SB 737-27-1204. 2 L 7 2 4F 4 F RT A16WE E2GL 2001112000134 20011120 00134 NM 2001 11 20 2001UALA02289 1 20011115 A 5300 FLANGE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 521UA 24891 AFT PIT FRAME STATION 1460 UPPER FLANGE DENTED BETWEEN STRINGER 25L AND 26L. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPA IR SPLICE CHANNEL. 2 L 7 2 4F 4 F RT A2NM E17NE 2001113000035 20011130 00035 NM 2001 11 30 2001UALA02292 1 20011115 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 521UA 24891 AFT PIT LT SIDEWALL STATION 1420 FRAME IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. DAMAGE REMOVED, INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2001113000036 20011130 00036 NM 2001 11 30 2001UALA02293 1 20011115 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 521UA 24891 CABIN LT OUTBOARD FLOOR SUPPORT CORRODED AT STATION 758 AND LBL 60. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAI R. 2 L 7 2 4F 4 F RT A2NM E17NE 2001112000135 20011120 00135 WP 2001 11 20 MWEA011452 1 20011120 A 5310 99118593 LONGERON DOUG DC9 DC915 3022036 WP LONGERON 16 LEFT CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 FUSELAGE STATION 925 CRACKED AT LONGERON 16 LEFT -- STOP DRILLED CRACK. DRILLED ANGLES AND FRAME AND INSTALLED REPAIR ANGLES. 2 L 7 2 4F A6WE 2001112000136 20011120 00136 NM 2001 11 20 QXEA0101770 1 20011025 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - REMOVED LT OUTBOARD FLAP ASSEMBLY FOR ACCESS TO FLAP TRACKS. REINSTALL WHEN TRACK BLENDING COMPLETED AND CARRIAGE RIG COMPLIED WITH. REPAIRED IAW DHC-8 MM 27-51-11 AND 27-50-00. 2 H 7 2 4T RT A13NM 2001112000137 20011120 00137 NM 2001 11 20 P2EA2001V0026 1 20011120 A 5753 6579953 FLAP BOEING 737 737230 1384401 NM DELAMINATED A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 122NJ 22120 During "c" Check Inspection.-L-H Imb Mid Flap, P/N 65-79953 T/E With Delamination.-Repair T/E of Imb Mid Flap P/N 65-799 53 Due to Delamination IAW COOPESA EO No.COO-CMP-3-57-611-01 Dated Nov 06,2001 & Documented on FAA 8110-3 Form Approved by DERT-710167SW.Note: See COOPESA Work Order No.O10863 5-48, VAM100 No.235 & 122SDA103. 2 L 7 2 4F RT A16WE 2001112000138 20011120 00138 NM 2001 11 20 QXEA0101774 1 20011025 A 5412 FIREWALL DHAV DHC8 DHC8202 2809007 NM NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - CRACK IN FIREWALL SKIN FROM EDGE TO BOTTOM INBOARD HOLE THAT MATES CLOSING MEMBER P/N 85410449. REPAIRED IAW HORI ZON EA 2-54-111. 2 H 7 2 4T RT A13NM 2001112000139 20011120 00139 NM 2001 11 20 QXEA0101775 1 20011025 A 5210 DOOR DHAV DHC8 DHC8202 2809007 NM PAX DOOR OUT OF ADJ A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - MAIN CABIN DOOR SKIN FLUSHNESS GAP IS GREATER THAN .100 INCH AT APERTURE SKIN AT FRONT AND REAR EDGES. REPAIRED I AW HORIZON AIR EA 2-52-113. 2 H 7 2 4T RT A13NM 2001112000140 20011120 00140 NM 2001 11 20 QXEA0101776 1 20011026 A 3233 ATTACH FITTING DHAV DHC8 DHC8202 2809007 NM LT MLG CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - LEFT MAIN LANDING GEAR RETRACTION ACTUATOR ATTACHMENT FITTING HAS CORROSION AND PITTING ON FACE OF BRACKET. REPAI RED IAW WORK CARD 429ME3220461, ITEM 11 A, B, C. 2 H 7 2 4T RT A13NM 2001112000141 20011120 00141 NM 2001 11 20 QXEA0101777 1 20011028 A 5753 FLAP DHAV DHC8 DHC8202 2809007 NM WING OUT OF TOLERANCE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - MINIMAL CLEARANCE EXISTS BETWEEN TOP OF OUTBOARD FLAP AND FRAME 85410863 AT STATION YW171.20. REPAIRED IAW RD 8-5 7-1549. 2 H 7 2 4T RT A13NM 2001112000142 20011120 00142 NM 2001 11 20 QXEA0101778 1 20011028 A 5753 FLAP DHAV DHC8 DHC8202 2809007 NM WING OUT OF TOLERANCE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - MINIMAL CLEARANCE EXISTS BETWEEN TOP OF OUTBOARD FLAP AND FRAME 85410 AT STATION YW171.20. REPAIRED IAW RD 8-57-1 54. 2 H 7 2 4T RT A13NM 2001112000143 20011120 00143 EU 2001 11 20 QXEA0101780 1 20011112 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 492US 11159 BOI- EXIT LOCATING SIGN ABOVE COCKPIT DOOR HAS 28V BULBS INOP. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD . AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001112000144 20011120 00144 EU 2001 11 20 QXEA0101781 1 20011109 A 3350 6008905 POWER SUPPLY FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478US 8859 11227 SEA- ALL EMERGENCY LIGHTS BATTERY POWER SUPPLIES ARE DEAD. REPLACED ALL EMERGENCY LIGHT BATTERY POWER SUPPLIES. OPERAT IONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. THE BATTERY POWER SUPPLIES REPLACED ARE: S/N 1112 (8859,8668), S/N 11 51 (8896, 8717), S/N 2357 (9228, 9092) S/N 345 (3391, 3116) S/N 476 (14091, 14926) S/N 480 (9319, 9253) S/N 877 (10127, 10541) S/N 886 (8859, 8668). 2 L 7 2 4F RT A20EU 2001112000145 20011120 00145 EU 2001 11 20 QXEA0101782 1 20011109 A 3350 6008905 POWER SUPPLY FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 479AU 11228 PDX- NR 6 OVERHEAD EVACUATION LIGHT AND CABIN CEILING EXIT SIGN INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY RIGHT HAND NR 3. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001112000146 20011120 00146 NM 2001 11 20 QXEA0101783 1 20011107 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX- CHAFE ON CARGO DOOR SKIN AT FORWARD LOWER CORNER. REPAIRED IAW DHC-8 RD 8-52-230 AND SRM 51-40-11 AND 51-40-00. 2 H 7 2 4T RT A13NM 2001112000147 20011120 00147 NM 2001 11 20 QXEA0101784 1 20011107 A 5230 STRUCTURE DHAV DHC8 DHC8202 2809007 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX- GOUGE ON UPPER AFT CARGO DOOR. REPAIRED IAW DHC-8 RD 8-52-029 AND SRM 52-00-16. 2 H 7 2 4T RT A13NM 2001112000148 20011120 00148 EU 2001 11 20 QXEA0101785 1 20011112 A 3350 5515800106 LIGHT FOKKER F28 F28MK4000 4990810 EU CABIN DEFECTIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - THE NUMBER TWO OVERHEAD EVACUATION LIGHT IS DIM AND UNREADABLE. REMOVED AND REPLACED LAMP ASSEMBLY. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001112000149 20011120 00149 EU 2001 11 20 QXEA0101786 1 20011112 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US 11161 PDX - EXIT SIGN AT PASSENGER ENTRANCE IS INOPERATIVE. REPLACED EXIT SIGN. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNE D TO SERVICE. 2 L 7 2 4F RT A20EU 2001112000150 20011120 00150 NM 2001 11 20 QXEA0101787 1 20011113 A 5210 DOOR DHAV DHC8 DHC8* NM AFT PAX DOOR BINDING A QXEA O OTHER O OTHER UK UNKNOWN 1 NM 09 409QX 4051 SEA - THE AFT PASSENGER DOOR WILL NOT OPEN. RESECURED LOOSE DOOR INTERIOR HANDLE TRIM PIECE THAT WAS BINDING ON HANDLE. DOOR OPENS AND CLOSES NORMALLY. 2 H 7 2 4T RT A13NM 2001112000151 20011120 00151 EU 2001 11 20 QXEA0101788 1 20011105 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FUSELAGE BELLY SKIN CHAFED BETWEEN FRAMES 15205 AND 15635, STRINGERS 8 AND 9. REPAIRED IAW FOKKER SRM 51-10-4, PA GE 8. 2 L 7 2 4F RT A20EU 2001112000152 20011120 00152 EU 2001 11 20 QXEA0101789 1 20011108 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 499US 11182 PDX - EMERGENCY EXIT SIGN ABOVE THE COCKPIT DOOR HAS NUMEROUS LIGHTS OUT. REPLACED EMERGENCY EXIT SIGN. OPERATIONAL CH ECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001112000153 20011120 00153 NM 2001 11 20 QXEA0101790 1 20011110 A 3610 VALVE DHAV DHC8 DHC8202 2809007 NM BLEED AIR FAULTY A QXEA D RETURN TO BLOCK B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 361PH 516 PDX - LAVATORY SMOKE DETECTOR SOUNDED ON TAXI OUT WITH A SMELL AND HAZE AROUND LAVATORY AND ENTIRE CABIN. REPLACED NUMB ER 2, 2.5 AND P-3 AIR PRESSURE VALVES. RAN BLEEDS UP TO RED LINE. NO HAZE OR SMOKE NOTED. NO CHANGE IN ENGINE OIL LEV EL NOTED. 2 H 7 2 4T RT A13NM 2001112700036 20011127 00036 2001 11 27 SABA011064 4 20011119 A 3417 ADC DHAV DHC8 DHC8103 1386005 NM E/E BAY MALFUNCTIONED A SABA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 801WP 086 AIRCRAFT 801 ON FLIGHT 5025; DURING CLIMBOUT PASSING THROUGH 8000 FEET THE AIR DATA COMPUTER WENT OFF LINE. AIRCRAFT RE TURNED AND LANDED WITH NO OTHER PROBLEMS. NO EMERGENCY PROCEDURES WERE USED. MAINTENANCE PERFORMED AN AVIONICS SYSTEM FUNCTION CHECK. SYSTEM CHECKED GOOD, COULD NOT DUPLICATE PROBLEM. AIRCRAFT WAS RETURNED TO SERVICE WITH NO REPEAT OF T HIS PROBLEM. 2 H 7 2 4T RT A13NM 2001112000154 20011120 00154 EU 2001 11 20 QXEA0101791 1 20011114 A 2150 ACM FOKKER F28 F28MK4000 4990810 EU A/C BAY ODOR A QXEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 478US 11227 PDX - STRONG EXHAUST ODOR COMING FROM THE NUMBER ONE AIR CYCLE MACHINE. PLACED AIR CYCLE MACHINE ON MEL 21-1, RSI 33095 4. 2 L 7 2 4F RT A20EU 2001112000155 20011120 00155 EU 2001 11 20 QXEA0101792 1 20011106 A 5541 RIB FOKKER F28 F28MK4000 4990810 EU RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FOUND NR 6 RIB CRACKED BEHIND PANEL 573. REMOVED AND REPLACED RIB PER FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001112000156 20011120 00156 EU 2001 11 20 QXEA0101793 1 20011107 A 5542 SKIN FOKKER F28 F28MK4000 4990810 EU RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RUDDER APERTURE FOR PANEL 574 IS CRACKED AT NUT PLATE HOLES. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001112000157 20011120 00157 EU 2001 11 20 QXEA0101795 1 20011107 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RIGHT WING FUEL PANEL 72A HAS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 57-01-01 AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 2001112000158 20011120 00158 EU 2001 11 20 QXEA0101796 1 20011107 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRETTING CORROSION AROUND SCREW HOLES ON PANEL 74C. REPAIRED IAW FOKKER SRM 57-01-01 AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 2001112000159 20011120 00159 EU 2001 11 20 QXEA0101797 1 20011112 A 5315 FLOORBEAM FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FLOORBEAM BL600L FROM FRAME 3820 TO 4900 TOP TIE PLATE HAS LARGE BUBBLES OF PAINT AND CORROSION. REPAIRED IAW FOK KER SRM 51-10-4 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001112000160 20011120 00160 EU 2001 11 20 QXEA0101798 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RT OUTBOARD SEAT TRACK HAS PITTING ON OUTBOARD FLANGE AT APPROXIMATELY STATION 656-567. REPAIRED IAW FOKKER SRM 5 1-10-4, PAGE 9. 2 L 7 2 4F RT A20EU 2001112000161 20011120 00161 EU 2001 11 20 QXEA0101799 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RT OUTBOARD SEAT TRACK HAS A CHAFE ON OUTBOARD FLANGE AT APPROXIMATELY STATION 583. REPAIRED IAW FOKKER SRM 53-40 -01, FIGURE 204. 2 L 7 2 4F RT A20EU 2001112100001 20011121 00001 EU 2001 11 21 QXEA0101794 1 20011107 A 5720 BOLT FOKKER F28 F28MK4000 4990810 EU WING STRIPPED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - INSIDE FUEL PANEL 72A, 5TH VENT STRUT FROM FORWARD SPAR TOP AND BOTTOM OUTBOARD MOUNTING BOLTS WILL NOT TIGHTEN UP . REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001112100002 20011121 00002 EU 2001 11 21 QXEA0101800 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RT OUTBOARD SEAT TRACK HAS A WORN SPOT ON TOP RAIL AT APPROXIMATELY STATION 593. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9-B2. 2 L 7 2 4F RT A20EU 2001112100003 20011121 00003 EU 2001 11 21 QXEA0101801 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RT OUTBOARD SEAT TRACK HAS PITTING ON OUTBOARD FLANGE AT APPROXIMATELY STATION 520-531. REPAIRED IAW FOKKER SRM 5 1-10-4, PAGE 9-B2. 2 L 7 2 4F RT A20EU 2001112100004 20011121 00004 EU 2001 11 21 QXEA0101802 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RT OUTBOARD SEAT TRACK HAS GOUGE ON TOP RAIL AT APPROXIMATELY STATION 434. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9-B2. 2 L 7 2 4F RT A20EU 2001112100005 20011121 00005 EU 2001 11 21 QXEA0101803 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RT OUTBOARD SEAT TRACK HAS A GOUGE IN INBOARD FLANGE AT APPROXIMATELY STATION 503. REPAIRED IAW FOKKER SRM 51-10- 4, PAGE 9-B2. 2 L 7 2 4F RT A20EU 2001112100006 20011121 00006 EU 2001 11 21 QXEA0101804 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RT OUTBOARD SEAT TRACK HAS PITTING ON INBOARD FLANGE AT APPROXIMATELY STATION 388-405. REPAIRED IAW FOKKER SRM 51 -10-4, PAGE 9-B2. 2 L 7 2 4F RT A20EU 2001112100007 20011121 00007 EU 2001 11 21 QXEA0101805 1 20011108 A 5347 PAINT FOKKER F28 F28MK4000 4990810 EU SEAT TRACK MISSING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RT INBOARD SEAT TRACK HAS PAINT MISSING IN BOTTOM CHANNEL AT APPROXIMATELY STATION 623-638. REPAIRED IAW FOKKER S RM 51-10-4, PAGE 9-B2. 2 L 7 2 4F RT A20EU 2001112100008 20011121 00008 EU 2001 11 21 QXEA0101806 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RT INBOARD SEAT TRACK HAS HOLE EDGE DAMAGE ON TOP OF RAIL AT APPROXIMATELY STATION 653. REPAIRED IAW FOKKER SRM 5 1-10-4, PAGE 9-B2. 2 L 7 2 4F RT A20EU 2001112100009 20011121 00009 EU 2001 11 21 QXEA0101807 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RT OUTBOARD SEAT TRACK HAS WEAR ON TOP OF RAIL AT APPROXIMATELY STATION 195-196. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9-B2. 2 L 7 2 4F RT A20EU 2001112100010 20011121 00010 EU 2001 11 21 QXEA0101808 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RT OUTBOARD SEAT TRACK HAS A GOUGE ON THE TOP RAIL AT APPROXIMATELY STATION 337-338. REPAIRED IAW FOKKER SRM 51-1 0-4, PAGE 9-B2. 2 L 7 2 4F RT A20EU 2001112100011 20011121 00011 NE 2001 11 21 2001F00640 2 20011010 A 7397 CONNECTOR BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE RT ENGINE DIRTY A BUEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 99 9PW RK007 RIGHT ENGINE ELECTRONIC FUEL CONTROL (EFC) ANNUNCIATOR ILLUMINATED. OBTAINED FERRY PERMIT FROM ROC TO PTK. CLEANED WIR ING CONNECTORS AT ENGINE TEMPERATURE SENSOR CONNECTOR, ELECTRONIC ENGINE CONTROL (EEC) WIRING CONNECTOR AND EEC FIREWALL WIRING CONNECTOR. (M) 2 H 7 2 4F 4 F RT A16SW E25EA 2001112100012 20011121 00012 NM 2001 11 21 2001F00641 1 20011025 A 3150 WARNING SYSTEM BOEING 727 727225 1384077 NM COCKPIT MALFUNCTIONED A MYWA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 19 803MA 22434 DURING TAKEOFF ROLL, TAKEOFF WARNING HORN SOUNDED. ABORTED TAKEOFF BELOW 50 KNOTS, CLEARED RUNWAY, DOUBLED CHECKED FLT CONTROLS FOR TAKEOFF CONFIGURATION FOUND NORMAL, VISUAL INSPECTION OUTSIDE AIRCRAFT TO VERIFY FLT CONTROLS CONFIGURATION . PERFORMED TAKEOFF WARNING SYSTEM TEST OPS NORMAL PER MM 31-26-0. NO DEFECTS NOTED ON GROUND. AIRCRAFT RETURN TO SER VICE. (M) 2 L 7 3 4F A3WE 2001112100013 20011121 00013 NE 2001 11 21 2001F00642 2 20011009 A 7321 WARNING LIGHT BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE COCKPIT MALFUNCTIONED A BUEA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 23 9PW RK007 MOMENTARY ELECTRONIC FUEL CONTROL (EFC) LIGHT ON RIGHT ENGINE. RAN UP ENGINE, PERFORMED CHECK, COULD NOT DUPLICATE PROB LEM. (M) 2 H 7 2 4F 4 F RT A16SW E25EA 2001112100014 20011121 00014 NM 2001 11 21 2001F00643 1 20011015 A 2910 6517844143 HYDRAULIC LINE BOEING 727 727224 1384076 NM HYDRAULIC SYS LEAKING A FX7A O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 19 79750 22452 FLT 523 - ARRIVING FROM SVMI, AFTER LANDING INTO MIA, HYDRAULIC SYSTEM 'A' PRESSURE AND QUANTITY INDICATION DROPPED TO 0 . AIRCRAFT CONTINUED TO GATE WITHOUT INCIDENT. MAINTENANCE T/S AND FOUND THE HYDRAULIC SYSTEM 'A' RETURN LINE FROM THE ENGINE NR 2 HYDRAULIC PUMP, FORWARD OR STATION NR 1342, LEAKING HYDRAULIC FLUID. AIRCRAFT WAS REMOVED FROM SERVICE AND HYDRAULIC LINE AND HYDRAULIC FILTERS WERE REMOVED AND REPLACED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001112100015 20011121 00015 NM 2001 11 21 2001F00644 1 20011021 A 5240 149N7314116 DOOR BOEING 757 757200 1384950 NM RT AIR START MISSING A N8TA K NONE D INFLIGHT SEPARATION UK UNKNOWN 1 WP 19 512NA 26962 AFTER LANDING THE RIGHT AIR START DOOR WAS FOUND MISSING. INSPECTED AIRCRAFT FOR AND REPAIRED COLLATERAL DAMAGE. REPLA CED DOOR ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001112100016 20011121 00016 NM 2001 11 21 2001F00645 1 20011027 A 7830 FS2118 BOLT BOEING 757 757236 1384971 NM THRUST REVERSER OUT OF POSITION A N8TA K NONE O OTHER NR NOT REPORTED 1 WP 19 522NA 25133 AFTER LANDING, RIGHT THRUST REVERSER WOULD NOT STOW. INVESTIGATION REVEALED THAT THE ROD END BOLT AT THE SLEEVE ATTACH POINT HAD MIGRATED OUT. REPLACED BOLT, THRUST REVERSER OPERATIONAL CHECKED GOOD. (M) 2 L 7 2 4F RT A2NM 2001112100017 20011121 00017 NM 2001 11 21 2001F00646 1 20010813 A 3350 86210144 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED MAINTENANCE, FOUND AFT CABIN EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED EXIT LIGHT AS SEMBLY AND BATTERY, LIGHT TESTED NORMAL. REF ASAA0110556. (M) 2 L 7 2 4F RT A16WE 2001112100018 20011121 00018 WP 2001 11 21 2001F00647 1 20011026 A 3350 9721050 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 811US 48043 MCO - THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS AND THE LEFT FORWARD EXIT IDENTIFIER LIGHTS WERE INOPERATIVE. MAINTEN ANCE REPLACED THE EMERGENCY LIGHT BATTERIES. REF USAAD01176. (M) 2 L 7 2 4F A6WE 2001112100019 20011121 00019 EA 2001 11 21 2001F00648 1 20010825 A 3350 BM10006002 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 47202 7202 FLT 5753 - DURING PREFLIGHT, THE CREW NOTED THAT THE RIGHT WING FORWARD MOST EXTERNAL EMERGENCY FLOOR LIGHT WAS INOPERAT IVE. MAINTENANCE LATER REMOVED AND REPLACED THE OVERWING EMERGENCY LIGHTS. OPS CHECKED GOOD AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001112100020 20011121 00020 NM 2001 11 21 AALA20011826 1 20010926 A 2421 IDG BOEING 777 777223 1385213 NM RT ENGINE FAILED A AALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SW 21 778AN 29587 AFTER HALF HOURS FLIGHT GOT ELEC GENERATOR OFF RIGHT, AFTER A SHORT TIME GOT ELEC GEN DRIVE RT GEN DRIVE DISCONNECTED. DEFERRED RIGHT IDG AS PER MEL 24-03 AUTH NB LGW9-67DC-A. PERFORMED MPM 24-03 PROCEDURE INSTALLED PLACARD ITEM TRANSFERR ED TO MIC SHEET. REPLACED RIGHT IDG, RAN ENGINE. OPS AND LEAK CHECK OK. REMOVED MEL 9-167DC-A CLEARED MIC SHEET. (M) 2 L 7 2 4F RT T00001SE 2001112100021 20011121 00021 NM 2001 11 21 ASAA0110461 1 20010702 A 5311 6546593 FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 500A, STRINGER 21R-25R CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001112100022 20011121 00022 NM 2001 11 21 ASAA0110462 1 20010702 A 5320 69514761 FLOOR SUPPORT BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT AT BODY STATION 520-540, LEFT BUTTOCK LINE 25 CORRODED. REPAIRED PE R SRM. (M) 2 L 7 2 4F RT A16WE 2001112100023 20011121 00023 NM 2001 11 21 ASAA0110463 1 20010702 A 5320 695147624 FLOOR SUPPORT BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT AT BS 520-540, LEFT BUTTOCK LINE 24.7 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001112100024 20011121 00024 NM 2001 11 21 ASAA0110464 1 20010702 A 5347 6554968512 SEAT TRACK BOEING 737 7372X6C 1384552 NM FUSELAGE WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND SEAT TRACK LUGS AT BS 420-480, LEFT BUTTOCK LINE 24.5 WORN. REPAIRED PER SRM. (M ) 2 L 7 2 4F RT A16WE 2001112100025 20011121 00025 NM 2001 11 21 ASAA0110466 1 20010702 A 5320 6546544533 ATTACH ANGLE BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND ATTACH ANGLES AT BODY STATION 695, LEFT BUTTOCK LINE 60 CORRODED. REPAIRED PER BO EING DRAWING. (M) 2 L 7 2 4F RT A16WE 2001112100026 20011121 00026 NM 2001 11 21 ASAA0110467 1 20010702 A 5320 6546544531 ATTACH ANGLE BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND ATTACH ANGLES AT BS 695, LEFT BUTTOCK LINE 60 CORRODED. REPAIRED PER BOEING DRAWI NG. (M) 2 L 7 2 4F RT A16WE 2001112100027 20011121 00027 NM 2001 11 21 ASAA0110468 1 20010702 A 5320 6546544527 ATTACH ANGLE BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND ATTACH ANGLES AT BS 695, LEFT BUTTOCK LINE 60 CORRODED. REPAIRED PER BOEING DRAWI NG. (M) 2 L 7 2 4F RT A16WE 2001112100028 20011121 00028 NM 2001 11 21 ASAA0110471 1 20010705 A 5320 69353525 TIE CLIP BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND TIE CLIP AT BS 867, STRINGER 27L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001112100029 20011121 00029 NM 2001 11 21 ASAA0110473 1 20010705 A 5320 69724951 ANGLE BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND ANGLE AT BS 695, STRINGER 18L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001112100030 20011121 00030 NM 2001 11 21 ASAA0110474 1 20010706 A 5320 6546877141 STRAP BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND STRAP AT BODY STATION 696-705, STRINGER 18L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001112100031 20011121 00031 NM 2001 11 21 ASAA0110475 1 20010706 A 5320 6546877139 STRAP BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND STRAP AT BODY STATION 693-696, LEFT BUTTOCK LINE 60-66 CORRODED. REPAIRED PER SRM . (M) 2 L 7 2 4F RT A16WE 2001112100032 20011121 00032 NM 2001 11 21 ASAA0110556 1 20010813 A 3350 873100211 SIGN BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED MAINTENANCE, FOUND AFT CABIN EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED EXIT LIGHT AS SEMBLY AND BATTERY, LIGHT TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2001112100033 20011121 00033 NM 2001 11 21 ASAA0140096 1 20010808 A 3397 8100022601 WIRE BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 771AS 25104 JNU - DURING PREFLIGHT, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE AT ROWS 21 AND 22. RECONNECTED FLOOR TRACK LIG HTING WIRE, OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A16WE 2001112100034 20011121 00034 NM 2001 11 21 ASAA0140120 1 20011022 A 5320 65479573 WEB BOEING 737 7374Q8 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 764AS 25101 PAE - DURING C-CHECK, FOUND CORROSION ON SUB THRESHOLD WEB BS 795-847 AND RBL 18 AFT CARGO BAY. REMOVED AND REPLACED WE B IAW SRM. (M) 2 L 7 2 4F RT A16WE 2001112100035 20011121 00035 NM 2001 11 21 ASAA0140622 1 20011019 A 5320 69353521 TIE CLIP BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING C-CHECK, FOUND CORROSION ON STRINGER TIE AT STATION 532 AND STRINGER 26R. REMOVED AND REPLACED STRINGER TI E IAW SRM. (M) 2 L 7 2 4F A16WE 2001112100036 20011121 00036 NM 2001 11 21 ASAA0140623 1 20011019 A 5230 SKIN BOEING 737 7372Q8C 138448S NM CARGO DOOR CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING C-CHECK, FOUND FORWARD CARGO DOOR INNER SKIN LOWER EDGE 26 IN FROM EDGE OF DOOR IS CORRODED. REPAIRED IAW SRM. (M) 2 L 7 2 4F A16WE 2001112100037 20011121 00037 NM 2001 11 21 ASAA0140624 1 20011019 A 5313 BAC1498155 STRINGER BOEING 737 7372Q8C 138448S NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING C-CHECK, FOUND DAMAGED STRINGER 12L AT STATION 1037.5. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001112100038 20011121 00038 NM 2001 11 21 ASAA0140626 1 20011019 A 5310 6546534 SHEAR TIE BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING C-CHECK, FOUND CORROSION ON SHEAR TIE AT STATION 520 AND STRINGER 27L TO 28L. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2001112100039 20011121 00039 WP 2001 11 21 ASAA0180236 1 20010809 A 3350 0105606003 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 951AS 49111 SEA - DURING LINE CHECK, A TRACK LIGHT WAS FOUND TO BE INOPERATIVE AT ROW 1. REPAIRED SOCKET AND RELAMPED. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001112100040 20011121 00040 WP 2001 11 21 ASAA0180237 1 20010809 A 3350 0105606003 MODULE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 961AS 53075 SFO - DURING PREFLIGHT CHECK, TRACK LIGHTS FROM FORWARD GALLEY TO MID 1ST CLASS WERE FOUND TO BE INOPERATIVE. RECONNECT ED LIGHTING MODULES. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001112100041 20011121 00041 WP 2001 11 21 ASAA0180238 1 20010811 A 3397 0105606003 WIRE DOUG DC9 DC983 3022083 WP CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 973AS 53449 SEA - DURING PREFLIGHT CHECK, FORWARD TRACK LIGHTING WAS DETERMINED TO BE INOPERATIVE. REPAIRED CONNECTION WIRE AT ROW 3. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001112100042 20011121 00042 WP 2001 11 21 ASAA0180239 1 20010811 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 935AS 49236 SEA - DURING LINE CHECK, ROW 1-3 TRACK LIGHTING WAS DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BATTERY PACK ASSE MBLY. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001112100043 20011121 00043 WP 2001 11 21 EIA2001242 1 20010814 A 5730 SKIN DOUG DC9 DC915F 3022037 WP LT WING DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 915F 47061 MZJ - FOUND SCREW HOLE WAS FOUND TO HAVE METAL TORN OUT AND EDGE OF METAL BENT ON LEFT WING INBOARD LEADING EDGE 19TH HO LE FROM OUTBOARD END. TRIMMED DAMAGE, HFEC AREA, FABRICATED FILLER AND DOUBLER. INSTALLED PER ECRA 915-57-057-2. (M) 2 L 7 2 4F A6WE 2001112100044 20011121 00044 WP 2001 11 21 EIA2001243 1 20010811 A 5310 DOUBLER DOUG DC9 DC915F 3022037 WP FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 915F 47061 MZJ - FORWARD PASSENGER DOOR UPPER FORWARD CORNER HAS A CRACK IN INNER MOST DOUBLER. REPAIRED PER ECRA 915-53-058-2 BY REPLACEMENT OF DOUBLER AFTER TRIMMING OUT DAMAGE. (M) 2 L 7 2 4F A6WE 2001112100045 20011121 00045 NM 2001 11 21 KPVA200121 1 20011025 A 3350 6104789 POWER SUPPLY DHAV DHC8 DHC8103 1386005 NM CABIN DISCHARGED A KPVA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806WP 357 HNL - DS1, DS2 EMERGENCY PATH LIGHTS DON'T COME ON. REMOVED AND REPLACED EMERGENCY LIGHTS ESCAPE PATH POWER SUPPLY AT S TATION 3352 PS2. OPS CHECK GOOD IAW DHC 8 MM 33-51-00 PAGE 201-202. NO DEFECTS NOTED. (M) 2 H 7 2 4T RT A13NM 2001112100046 20011121 00046 NM 2001 11 21 TSAA0133145 1 20011027 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST NR NOT REPORTED 1 WP 13 807AL 23443 REPLACED NR 3 FLOOR LIGHT ASSEMBLY BATTERY PACK DUE TO BEING INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2001112100047 20011121 00047 NM 2001 11 21 TSAA0133146 1 20011027 A 3350 86210066 BATTERY PACK BOEING 737 737230 1384401 NM CABIN DISCHARGED A TSAA K NONE L NO TEST NR NOT REPORTED 1 WP 13 818AL 22117 REPLACED LEFT OVERWING IDENT POWER PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001112100048 20011121 00048 NM 2001 11 21 UIEA0100 1 20011005 A 2612 FIRE WARNING BOEING 747 7472D3B 1384805 NM COCKPIT FALSE INDICATION A UIEA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 15 506MC 21252 ATB - DUE LOWER AFT CARGO FIRE LIGHT ON AT ROTATION. NR 1 BOTTLE DISCHARGED (FALSE INDICATION). LOWER AFT CARGO INSPEC TED. NO SIGNS OF FIRE (NO CARGO IN SECTION). ITEM TRANSFERRED TO DMI PAGE 03049 AND DEFERRED PER MEL 26-14-2D AND ALL DDPG PROCEDURES FOLLOWED M01-050. (M) 2 L 7 4 4F RT A20WE 2001112100049 20011121 00049 NM 2001 11 21 UIEA01102 1 20010926 A 7722 JTK34AAR1 HARNESS BOEING 747 7472D3B 1384805 NM NR 1 ENGINE MISSING A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 DURING ROUTINE ENGINE INSPECTION FOUND NR 1 ENGINE LOWER EGT HARNESS MISSING. REPLACED NR 1 ENGINE EGT HARNESS AS PER M M 77-20-03. (M) 2 L 7 4 4F RT A20WE 2001112100050 20011121 00050 2001 11 21 UIEA01103 4 20011028 A 2210 DAMPER BOEING 747 7472D7B 1384803 NM AUTOPILOT SYS MALFUNCTIONED A UIEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 15 522MC 21783 DURING CLIMB-OUT FROM MIA PASSING FL 33, FELT ABRUPT UNCOMMANDED YAW OF AIRCRAFT. LOWER RUDDER INDICES SHOWED DISPLACEM ENT 5 DEGREES RIGHT OF CENTER. UPPER RUDDER INDICES SHOWED CENTERED. TURNED OFF LOWER YAW DAMPER, CONDITION STOPPED. INITIATED RETURN TO MIA. (M) 2 L 7 4 4F RT A20WE 2001112100051 20011121 00051 NM 2001 11 21 UIEA01104 1 20011030 A 2612 FIRE WARNING BOEING 747 747212B 1384886 NM COCKPIT FALSE INDICATION A UIEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 15 808MC 21048 DURING TAKEOFF ROLL FROM SUU AT ABOUT 80 KTS, HAD A CARGO FIRE WARNING LIGHT. REJECTED TAKEOFF PERFORMED. PERFORMED VI SUAL INSPECTION OF FORWARD AND AFT CARGO COMPARTMENTS. BOTH COOL, NO EVIDENCE OF HEAT OR OVERHEAT CONDITION EXISTS. IN SPECTED AFT CARGO HEAT CONTROL VALVE FOR OPERATION AND CONDITION AND PERFORMED FORWARD/AFT HEAT AND SMOKE DETECTION TEST . ALL TEST NORMAL. PERFORMED CHAPTER 5 CONDITIONAL INSPECTION FOR HIGH ENERGY STOP. (M) 2 L 7 4 4F A20WE 2001112100052 20011121 00052 NM 2001 11 21 USAA011333 1 20011017 A 5314 KEELBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 46526 22959 PIT - FOUND BEAM CRACKED 1 INCH, WEB IN KEEL BEAM 18 INCHES FORWARD STATION 722 UNDER AUX HYDRAULIC PUMP. REPAIR ANGLE PER SRM 51-70-11 FIG 1. (M) 2 L 7 2 4F RT A16WE 2001112100053 20011121 00053 NM 2001 11 21 USAA011334 1 20011002 A 5313 1129575 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 46526 22959 PIT - FOUND SHELF CRACKED 2 INCHES, RIGHT MLG W/W S18A SHELF AT STATION 727. REMOVED AND REPLACED RT S18A SHELF WITH ID ENT PART NR. (M) 2 L 7 2 4F RT A16WE 2001112100054 20011121 00054 NM 2001 11 21 USAA011335 1 20011029 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 336US 44590 23233 PIT - ON WALKAROUND FOUND SKIN CRACKED 1.625 INCH, STATION 740 .5 INCH BELOW STRINGER 23R. CUT OUT DAMAGE, INSTALLED FI LLER AT STRINGER, INSTALLED DOUBLER PER B737-300 SRM 53-00-01 FIG 201. (M) 2 L 7 2 4F RT A16WE 2001112100055 20011121 00055 NM 2001 11 21 USAA011336 1 20011029 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 448US 31658 24892 TPA - FOUND SKIN CRACKED 1 INCH, BELOW STRINGER 16L STATION 727B. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202 AND MPP 30 8-60. (M) 2 L 7 2 4F RT A16WE 2001112100056 20011121 00056 NM 2001 11 21 USAA011348 1 20011002 A 5320 STRAP BOEING 737 737201 1384454 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 48384 22962 CLT - FOUND DAMAGED TEAR STRAP 8.9 INCHES, STATION 500 STRINGER 24L TO S25L. INSTALLED DOUBLER AND TRIPLER. (M) 2 L 7 2 4F A16WE 2001112100057 20011121 00057 NM 2001 11 21 USAA011350 1 20011012 A 5320 ANGLE BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 48384 22962 CLT - FOUND DRAG ANGLE CRACKED, STATION 540, JUST ABOVE STRINGER 23L. FABRICATED PART PER T/R 53-50-03A. (M) 2 L 7 2 4F A16WE 2001112100058 20011121 00058 NM 2001 11 21 USAA011351 1 20011023 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 48384 22962 CLT - FOUND SKIN DENTED 4 INCHES BY 3 INCHES, BETWEEN BS 908 TO 951 S17R AND S20R. INSTALLED DOUBLER AND TRIPLER PER EA 85513. (M) 2 L 7 2 4F A16WE 2001112100059 20011121 00059 NM 2001 11 21 USAA011359 1 20010915 A 5320 ATTACH ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 46526 22959 PIT - FOUND FLOORBOARD ATTACH ANGLE CORRODED 100 INCHES BY 3 INCHES, STATION 727-727E ABOVE STRINGER 25R. (M) 2 L 7 2 4F RT A16WE 2001112100060 20011121 00060 EU 2001 11 21 USAABA01013 1 20011026 A 3350 321430 BATTERY AIRBUS 330 A330323 3930335 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 673UW 0337 PHL - FOUND 3 EPSU'S FAILED ON TEST. MAINTENANCE REPLACED THE EPSU BATTERIES AT 16WL, 12WL AND 17WL. (M) 2 L 7 2 4F RT A46NM 2001112100061 20011121 00061 NM 2001 11 21 USAABB01111 1 20011028 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 629AU 27807 BDL - FOUND FLOOR MOUNTED EMERGENCY LIGHTS AT ROWS 4, 6, 9, 13, 18, 23, 26, 29 AND 33 DIM. MAINTENANCE REPLACED ALL THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2001112100062 20011121 00062 NM 2001 11 21 USAABB01112 1 20011028 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 629AU 27807 PIT - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 9 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001112100063 20011121 00063 NM 2001 11 21 USAABB01115 1 20011028 A 3350 LIGHT BOEING 767 767201 1385125 NM CABIN DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 648US 23900 CDG - FOUND AISLE EMERGENCY LIGHTING ON THE RIGHT SIDE, ROW 3 AND FORWARD, INOPERATIVE. MAINTENANCE FOUND THE TRACK LIG HTING DISCONNECTED AT ROW 3 AND RECONNECTED SAME. (M) 2 L 7 2 4F RT A1NM 2001112100064 20011121 00064 NM 2001 11 21 USAABB01116 1 20011101 A 3350 20121 CHARGER BOEING 767 767201 1385125 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 647US 23899 BRU - FOUND FORWARD RIGHT SIDE EMERGENCY TRACK LIGHTING INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER (M730). (M) 2 L 7 2 4F RT A1NM 2001112100065 20011121 00065 NM 2001 11 21 USAABB01117 1 20010111 A 3040 HEATER BOEING 767 7672B7 1385107 NM R1 DOOR MALFUNCTIONED A USAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 19 655US 25257 CLT - FLT 281 - ON DESCENT INTO CLT, ELECTRICAL SMELL AND SMOKE WERE NOTED IN THE FORWARD PORTION OF THE CABIN. AFTER L ANDING, THE R1 DOOR HEATER WAS SEEN TO BE EMITTING SPARKS AND SMOKE. THE DOOR HEATER CIRCUIT BREAKER AND UTILITY BUSSES WERE SECURED. THE SYSTEM WAS PLACED ON MEL. (M) 2 L 7 2 4F RT A1NM 2001112100066 20011121 00066 NM 2001 11 21 USAABB0113 1 20011027 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 633AU 27811 BWI - FOUND FLOOR MOUNTED EMERGENCY LIGHTS AT ROWS 29 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2001112100067 20011121 00067 NM 2001 11 21 USAABB0114 1 20011027 A 3350 9221009 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 633AU 27811 BWI - FOUND EXIT IDENTIFIERS AT DOORS L3, R3 AND R4 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2001112100068 20011121 00068 WP 2001 11 21 USAAD01176 1 20011026 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 811US 48043 MCO - THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS AND THE LEFT FORWARD EXIT IDENTIFIER LIGHTS WERE INOPERATIVE. MAINTEN ANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2001112100069 20011121 00069 WP 2001 11 21 USAAD01177 1 20011101 A 3350 9721055 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 815US 48095 IND - THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS AND THE TAIL CONE REMOTE EMERGENCY LIGHT RECEIVER BATTERY WERE INOPERA TIVE. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT AND REMOTE RECEIVER BATTERIES. (M) 2 L 7 2 4F A6WE 2001112100070 20011121 00070 EU 2001 11 21 USAASA01056 1 20011024 A 3397 CONNECTOR AIRBUS A319 A319112 3930323 EU CABIN LOOSE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 706US 0946 MCO - THE EMERGENCY LIGHTS FAILED THE TEST FOR 'EXT LOAD' ON THE FORWARD LEFT AND THE AFT LEFT DOORS. MAINTENANCE SECUR ED THE CONNECTOR FOR EMERGENCY LIGHTS AT THE R1 AND L2 DOOR SLIDES. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2001112100071 20011121 00071 EU 2001 11 21 USAASA01058 1 20011105 A 3350 321430 BATTERY AIRBUS A321 A321211 3930370 EU CABIN DISCHARGED A USAA K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 19 176UW 1499 MCO - RECEIVED EMERGENCY POWER SUPPLY UNIT BATTERY 'EXIT L' FAULT DURING TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT BATTERY. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2001112100072 20011121 00072 NM 2001 11 21 USAASB01299 1 20011017 A 2740 CONTROLLER BOEING 737 7373B7 1384580 NM STAB TRIM BINDING A USAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 19 530AU 24412 IND - FLT 1598 - ON CLIMB-OUT FROM IND, EN ROUTE TO PHL, THE CREW NOTICED THE STABILIZER TRIM AS BINDING AND NOISY ON TH E FIRST OFFICERS SIDE PEDESTAL. FLIGHT RETURNED TO FIELD AT IND AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE OPENED PEDESTAL AND INSPECTED AREA AND CONTROLS FOR STABILIZER TRIM. RAN STABILIZER TRIM FULL UP AND DOWN NUMEROUS TIMES. STABILIZER TRIM RAN SMOOTH AND FREE WITH NO NOISE NOTED. CLOSED PEDESTAL. AIRCRAFT OK FOR S ERVICE. (M) 2 L 7 2 4F RT A16WE 2001112100073 20011121 00073 NM 2001 11 21 USAASB01303 1 20011026 A 2751 2061141 INDICATOR BOEING 737 737401 1384701 NM COCKPIT FAILED A USAA O OTHER N FALSE WARNING AP APPROACH 1 EA 19 409US 23879 BOS - FLT 926 - ON APPROACH TO BOS, FROM PIT, CREW REPORTED THE FLAPS AND SLATS WOULD NOT EXTEND. CAPTAIN ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND PERFORMED THE ALTERNATE METHOD FOR FLAP EXTENSION. FLIGHT LANDED WITHOUT FURTHE R INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE RESET THE FLAP ASYMMETRY SWITCH IN THE E/E COMPARTMENT AND REMOVED AND REPLACED FLAP POSITION INDICATOR. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001112100074 20011121 00074 NM 2001 11 21 USAASB01306 1 20011103 A 2751 CONNECTOR BOEING 737 737301 1384611 NM COCKPIT NOT SEATED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 577US 23742 PHL - FLT 562 - AFTER TAKEOFF FROM PHL, CREW RECEIVED AN ASYMMETRICAL FLAP INDICATION WHEN FLAPS WERE RETRACTED FROM 5 T O 1 UNITS. CREW FOLLOWED PROCEDURES AND RETURNED TO FIELD AT PHL. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENC Y WAS DECLARED. MAINTENANCE RESET CIRCUIT BREAKERS AND CLEANED/RESEATED FLAP POSITION INDICATOR CANNON PLUG. REINSTALL ED FLAP POSITION INDICATOR. OPERATIONAL CHECK OF SYSTEM NORMAL. (M) 2 L 7 2 4F RT A16WE 2001112100075 20011121 00075 NM 2001 11 21 2001UALA02239 1 20011108 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 328UA 24148 CRACKED FRAMES AT STRINGER 9 AT STATION 827L, 847L AND R 867L AND STA 887L. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED AN GLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001112100076 20011121 00076 NM 2001 11 21 2001UALA02242 1 20011109 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 919UA 25386 NOSE AREA LEFT HAND BODY STATION 188 AT WL 207 FRAME WEB CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIR PERFORMED WHICH RE MOVED EXISTING SKIN DOUBLER CUTTING OUT CRACKED SECTION OF WEB AND T-CHORD SECTION. FABRICATED REPAIR ANGLE AND DOUBLER AND INSTALLED. FABRICATED NEW SKIN DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001112100077 20011121 00077 NM 2001 11 21 2001UALA02243 1 20011109 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 919UA 25386 MAIN CABIN FLOOR BEAM T-CAP STATION 951 CORRODED BEYOND LIMITS BETWEEN RBL 24 AND RBL 30. MAJOR REPAIR ACCOMPLISHED. REMOVED FLOOR SUPPORT RBL 15 AND RBL 45 BETWEEN STATION 951 AND 967. FABRICATED NEW T-CAP AND STRAPS INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001112100078 20011121 00078 NM 2001 11 21 2001UALA02244 1 20011109 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 919UA 25386 FOUND DENT TO BE ON LEFT SIDE STATION 227 STRINGER 15L. MAJOR REPAIR ACCOMPLISHED. CUT OUT AFFECTED DAMAGED AREA AND M ANUFACTURED DOUBLER AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001112100079 20011121 00079 NM 2001 11 21 2001UALA02245 1 20011109 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 328UA 24148 FLOORBEAM UPPER CAP WAS CORRODED AT STATION 986.5 LBL 29 WITH EXCESSIVE MATERIAL LOSS AT WL 207. MAJOR REPAIR ACCOMPLIS HED. ACCOMPLISHED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001112100080 20011121 00080 NM 2001 11 21 2001UALA02246 1 20011109 A 5310 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE BUCKLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 328UA 24148 AFT PIT FRAME STATION 807 SHEAR TIES BETWEEN STRINGER 27L AND 27R ARE BUCKLED. MAJOR REPAIR ACCOMPLISHED. SHEAR TIE MA NUFACTURED AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001112100081 20011121 00081 NM 2001 11 21 2001UALA02247 1 20011109 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 336UA 24240 AFT PIT CIRCUMFERIAL FRAME AT BODY STATION 767 STRINGER 25R RBL 22 FRAME HAS ELONGATED HOLE IN WEB AREA. MAJOR REPAIR A CCOMPLISHED. FABRICATED AND INSTALLED EXTERNAL REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001112100082 20011121 00082 NM 2001 11 21 2001UALA02248 1 20011110 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 328UA 24148 FORWARD BULKHEAD STATION 178 WEB WAS CRACKED AT WX RADAR MOUNT LEFT HAND UPPER, LEFT HAND LOWER AND RIGHT HAND LOWER ATT ACH POINTS. MAJOR REPAIR ACCOMPLISHED. SINGLE WEB REPAIR OVER ALL DEFECT AREAS INCLUDING UNDER RIGHT HAND UPPER ATTACH POINT AS A PRECAUTIONARY MEASURE. WEB DOUBLER WAS INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121700103 20011217 00103 2001 12 17 2001UALA02249 4 20011111 A 2565 WIRE BOEING 757 757222 1384956 NM EVAC SLIDE CHAFED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 594UA 28145 LEFT WING SLIDE EICAS MSG AND EMER DOORS LIGHT ILLUMINATED SUPPLEMENTAL DATA UPDATE REPLACED LEFT OVERWING SLIDE DOOR PR OX SENSOR S10373. FOUND BAD GROMMET AND CHAFED SENSOR WIRES WHERE WIRES PASS THROUGH SLIDE COMPARTMENT FWD BULKHEAD TO LEFT WHEELWELL. REPLACED DAMAGED SECTION OF WIRES USING ENVIRONMENTAL SPLICES AND REPLACED GROMMET. 2 L 7 2 4F RT A2NM 2001112100083 20011121 00083 NM 2001 11 21 2001UALA02251 1 20011112 A 5320 STRAP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 328UA 24148 AFT CABIN STATION 951 STRAP AT STRINGER 5R TOP 2 HOLES HAVE CRACK INDICATION WITH HFEC. MAJOR REPAIR ACCOMPLISHED. STR AP REPAIR WITH FILLER MADE AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121700104 20011217 00104 NM 2001 12 17 2001UALA02252 1 20011111 A 2432 MR24244 BATTERY BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE E/E BAY SHORTED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 210UA 5855 700 30216 MAIN BATTERY AND MAIN CHARGER EICAS MESSAGE WITH ACCOMPANIED 'NO LAND THREE'. AIRCRAFT RETURNED TO LAX. THE MAIN BATTERY CHARGER AND OVERHEAD BATTERY SWITCH WERE INITIALLY REPLACED. THE CORRECTIVE ACTION WAS MAIN BATTERY REPLACEMENT.THE MA IN BATTERY CHARGER TESTED WITH NO FAULTS FOUND. PRELIMINARY VENDOR REPORT INDICATES A BATTERY FAILURE DUE TO A SHORTED CELL. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001112100084 20011121 00084 NM 2001 11 21 2001UALA02253 1 20011109 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 CABIN FLOORBEAM CORRODED AT BODY STATION 365 RBL 9 TO RBL 15. MAJOR REPAIR ACCOMPLISHED. REPLACED UPPER CAP FROM BL 0 TO CREASE BEAM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001112100085 20011121 00085 NM 2001 11 21 2001UALA02255 1 20011111 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 CABIN FLOORBEAM UPPER T-CAP CORRODED AT STATION 324 RBL 42 AND OUT TO 68 RBL STRINGER 17. MAJOR REPAIR ACCOMPLISHED. REMOVED CORRODED SECTION OF T-CAP FROM 10 LBL TO 68 RBL. INSTALLED NEW PIECE OF T-CAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2001112100086 20011121 00086 NM 2001 11 21 2001UALA02261 1 20011111 A 5414 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 521UA 24891 NR 2 PYLON FORWARD OUTBOARD ACCESS PANEL CUTOUT PYLON SKIN IS CRACKED AT THE 2 O'CLOCK POSITION. MAJOR REPAIR ACCOMPLIS HED. INSTALLED DOUBLER ON PYLON SKIN CUTOUT. 2 L 7 2 4F 4 F RT A2NM E17NE 2001112100087 20011121 00087 NM 2001 11 21 2001UALA02262 1 20011111 A 5414 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR2 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 521UA 24891 NR 2 PYLON FORWARD OUTBOARD ACCESS PANEL CUTOUT PYLON SKIN IS CRACKED AT THE 1 O'CLOCK AND 2 O'CLOCK POSITION. MAJOR RE PAIR ACCOMPLISHED. INSTALLED DOUBLERS ON PYLON SKIN. 2 L 7 2 4F 4 F RT A2NM E17NE 2002010300091 20020103 00091 NM 2002 1 3 2001UALA02264 1 20011109 A 5315 141W851817 FLOORBEAM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 774UA 23878 26936 FORWARD SIDE OF 246 FLOORBEAM WEB AT RBL 7.88 HAS DEEP GOUGE IN EXCESS OF 50 PERCENT WEB THICKNESS. MAJOR REPAIR ACCOMP LISHED. DOUBLER REPAIR ACCOMPLISHED PER 777 SRM 53-10-51-201. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001121700105 20011217 00105 NM 2001 12 17 2001UALA02265 1 20011112 A 2932 211C223326 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE HYDRAULIC SYS MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 537UA 25157 ELEV LT HYD PRESS STATUS MSG. REPLACED LEFT HYDRAULIC PRESSURE SWITCH S10002. 2 L 7 2 4F 4 F RT A2NM E17NE 2001121800007 20011218 00007 NM 2001 12 18 2001UALA02266 1 20011113 A 2910 AS11504D0232 HYDRAULIC LINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT MLG RUPTURED A UALA K NONE K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 504UA 24625 AIRCRAFT ARRIVED AT GATE WITH RIGHT MLG DOOR OPEN AND LEFT HYDRAULIC SYSTEM INOP. RIGHT DOWN LOCK ACTUATOR LINE LEAKING. REPLACED HOSE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001112100088 20011121 00088 NM 2001 11 21 2001UALA02268 1 20011112 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 360UA 24453 FUSELAGE DENTED AND GOUGED AT STA 243, BELOW AND FWD OF LAV SERVICE PANEL. DAMAGED AREA MEASURES 4.5 X 4.75 X .375 INCH DEEP. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE AND FABRICATED REINFORCEMENT REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001112100089 20011121 00089 NM 2001 11 21 2001UALA02270 1 20011112 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 328UA 24148 EXTERNAL FUSELAGE SKIN DENTED AND GOUGED 3 EACH AREAS STATION 797 BETWEEN STRINGER 27L AND 27R. MAJOR REPAIR ACCOMPLISH ED. SKIN DOUBLER MANUFACTURED AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001112100090 20011121 00090 NM 2001 11 21 C1HA200181017 1 20011116 A 3350 BATTERY PACK BOEING 727 7272S7 138407Z NM INOPERATIVE A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 681CA 22020 Aft cabin overhead emergency exit light inoperative at STA 1095. Action Taken: Removed and replaced battery pack for a ssociated exit sign at STA 1095 with serviceable. Illumination check good. Work done IAW MM 33-50. 2 L 7 3 4F A3WE 2001112100091 20011121 00091 NM 2001 11 21 C1HA200181018 1 20011116 A 3350 BATTERY PACK BOEING 727 7272S7 138407Z NM INOPERATIVE A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 681CA 22020 Forward overhead emergency exit sign flashes when emergency exit lights on. (Attached) to forward life raft. Action Ta ken: Removed and replaced battery pack for associated sign at STA 354 with serviceable. Illumination check good. Work done IAW B-727-200 M/M. 2 L 7 3 4F A3WE 2001112100092 20011121 00092 NM 2001 11 21 2001UALA02271 1 20011114 A 5313 STRINGER BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 921UA 25388 BODY STATION 310 STRINGER 28R LEFT HAND FLANGE DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001112100093 20011121 00093 NM 2001 11 21 2001UALA02272 1 20011114 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 921UA 25388 EXTERNAL FUSELAGE SKIN GOUGED STATION 485 STRINGER 24R. MAJOR REPAIR ACCOMPLISHED. INSTALLED SKIN DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001112100094 20011121 00094 NM 2001 11 21 2001UALA02273 1 20011113 A 5512 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HORIZ STAB GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 328UA 24148 RIGHT HAND HORIZONTAL STABILIZER LEADING EDGE EXTERNAL SKIN IS GOUGED STABILIZER STATION 110. MAJOR REPAIR ACCOMPLISHED . ACCOMPLISHED FLUSH REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001112100095 20011121 00095 NM 2001 11 21 2001UALA02274 1 20011114 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 173UA 24380 EEL OPPOSITE LAV 102 INOP. FOUND CONNECTOR LOOSE. SECURED EEL CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2001112100096 20011121 00096 NM 2001 11 21 2001UALA02275 1 20011109 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 190UA 26879 EEL LIGHTS INOP SEATS 6G THROUGH 8G. SECURED CONNECTOR AT AFT GALLEY SIDEWALL STRIP, OPS CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2001113000029 20011130 00029 NM 2001 11 30 2001UALA02276 1 20011109 A 3350 20131 BATTERY PACK BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 605UA 21866 EMERGENCY EXIT LIGHTS ON BY LEFT OVERWING. REPLACED EEL LIGHT EXIT SIGN AT LEFT OVERWING DOOR, CHARGER AND BATTERY PACK . EXIT SIGN (P/N 5820-11). 2 L 7 2 4F 4 F RT A1NM E3NE 2001112100098 20011121 00098 NM 2001 11 21 2001UALA02278 1 20011113 A 5313 STRINGER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 650UA 25287 BODY STATION 286 STRINGER 20 RBL 88 UPPER T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CAP AN D SPLICES. 2 L 7 2 4F 4 F RT A1NM E24NE 2001121800008 20011218 00008 NM 2001 12 18 2001UALA02279 1 20011110 A 2530 2676 CHILLER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE GALLEY ODOR A UALA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 605UA 21866 ELECTRICAL BURNING TYPE ODOR NOTICED IN FWD GALLEY AREA. TURNED OFF UTILITY BUSSES, GASPER FAN AND RECYCLE FAN. HAD NO EFFECT. PERFORMED VISUAL INSPECTION OF WIRE BUNDLES IN RIGHT HAND NOSE TUNNEL AND ON P37 PANEL, P51 PANEL, P54 PANEL, AND P50 PANEL. FOUND NO INDICATION OF BURNT OR SHORTED EQUIPMENT OR WIRES. OPENED SIDE PANEL ON CHILLER UNIT AND DETEC TED ACRID SMELL. REPLACED FWD CHILLER. RAN CHILLER. NO ODORS DETECTED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001121800009 20011218 00009 NE 2001 12 18 2001UALA02280 2 20011110 A 7321 FCU BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE ENGINE OUT OF ADJ A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 606UA 21867 707506 ENGINES DO NOT ACCELERATE OR DECELERATE EVENLY CAUSING EXCESSIVE AUTO-THROTTLE HUNTING. RIGHT SIDE DECELERATE MUCH MORE QUICKLY THAN LEFT AND REQUIRES HALF KNOB SPLIT NEAR IDLE TO MATCH N1'S SUPPLEMENTAL DATA UPDATE THIS IS CAUSED BY EITHE R A FAULTY TOTAL TEMPERATURE (TT2) SENSOR, OR THE FUEL CONTROL(FCU) DECELERATION(DECEL) SCHEDULE BEING TO CLOSE TO THE E NGINE'S STEADY STATE OPERATING LINE. THE FCU WILL CYCLE THE 3.0 AND 3.5 BLEEDS, TRYING TO KEEP UP WITH THE FCU DECEL SC HEDULE AND THE ENGINE OPERATING LINE, WHICH CAUSES POWER FLUCTUATIONS. THIS POWER FLUCTUATION IS CORRECTED BY EITHER RE PLACING THE TT2 SNSOR OR ADJUSTING THE FCU DECEL SCHEDULE AWAY FROM THE STEADY STATE OPERATING LINE. 2 L 7 2 4F 4 F RT A1NM E3NE 2002010300092 20020103 00092 NM 2002 1 3 2001UALA02281 1 20011111 A 3510 MC1019101 OXYGEN MASK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 663UA 27160 CAPTAINS OXYGEN MASK ASSEMBLY HEADBAND LEAKS AND WILL NOT COLLAPSE AROUND HEAD. MASK FAILED DUE TO NORMAL WEAR AND TEAR . 2 L 7 2 4F 4 F RT A1NM E24NE 2001112100099 20011121 00099 NM 2001 11 21 2001UALA02283 1 20011114 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 340UA 24244 STATION 178 BULKHEAD WEB CRACKED AT LBL 5.7, WL 212. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED WEB REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001112100100 20011121 00100 NM 2001 11 21 2001UALA02284 1 20011114 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 340UA 24244 STATION 178 BULKHEAD CRACKED AT LBL 5.7, WL 209. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED WEB REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001112100101 20011121 00101 NM 2001 11 21 2001UALA02285 1 20011114 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 122UA 29168 EMERGENCY CEILING LIGHT INOP AT ROW 12. RELAMPED, CHECKED GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2001112100102 20011121 00102 NM 2001 11 21 2001UALA02286 1 20011113 A 3350 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE POWER SUPPLY BLOWN A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 180UA 25224 EMERGENCY LIGHTS AFT LEFT LOWER TWO INOP. REPLACED FUSE ON POWER SUPPLY M7919 AND LIGHT ASSEMBLY AT STATION 1586. OPS CHECK GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2001121800010 20011218 00010 NM 2001 12 18 2001UALA02287 1 20011114 A 3233 273T11027 ACTUATOR BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LT MLG FAILED A UALA K NONE J WARNING INDICATION AP APPROACH 1 WP 29 615UA 21876 CAPTAIN CONTACTED DISPATCH ON APPROACH TO SFO WITH A LEFT MAIN GEAR UNSAFE INDICATION. FLIGHT LANDED SAFELY. LEFT MLG RETRACT ACTUATOR PISTON HAD TENSILE FAILURE AT ROD END ATTACHMENT. SUBSEQUENT FREEFALL DAMAGED DOWNLOCK SENSOR. SENSOR REPLACED 2 L 7 2 4F 4 F RT A1NM E3NE 2001112100103 20011121 00103 NM 2001 11 21 2001UALA02288 1 20011115 A 5320 CHANNEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 521UA 24891 CABIN FLOOR CHANNEL STATION 329 AND RBL 40 CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED CABIN FLOOR CHANNEL. 2 L 7 2 4F 4 F RT A2NM E17NE 2001112100104 20011121 00104 SO 2001 11 21 C2XA01IA404 1 20011121 A 5315 14522459001 SUPPORT EMB 145 EMB145 3260210 SO FRAME 20L CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27962 145110 DURING C-CK INSPECTION THE FLOOR SUPPORT AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFE CTED FLOOR SUPPORT IN ACCORDANCE WITH THE EMB 145 SRM 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001112100105 20011121 00105 WP 2001 11 21 MWEA011441 1 20011120 A 5340 591014323 SEAT TRACK DOUG DC9 DC915 3022036 WP STA. 200 & 218 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 SEAT TRACK 4 BETWEEN STATION 200 AND 218 IS CORRODED AT FORWARD END AND AROUND FASTENER HOLES ON UPPER SURFACE AND LOWER SURFACE -- REMOVED, FABRICATED AND INSTALLED SEAT TRACK. 2 L 7 2 4F A6WE 2001112100106 20011121 00106 WP 2001 11 21 MWEA011444 1 20011120 A 5230 83277JD60228U3 PAN DOUG DC9 DC915 3022036 WP FWD CARGO DOOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 FORWARD CARGO DOOR JAMB ENTIRE BOTTOM PAN FACE HAS LIGHT TO MODERATE CORROSION -- REMOVED LOWER SECTION OF CARGO DOOR PAN. TRIMMED, LOCATED, DRILLED AND INSTALLED DOOR JAMB PAN. 2 L 7 2 4F A6WE 2001112100107 20011121 00107 WP 2001 11 21 MWEA011449 1 20011120 A 5210 995575915 BEAM DOUG DC9 DC915 3022036 WP MAIN CABIN DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 MAIN CABIN DOOR BEAM NUMBER 8 HAS A CRACK ON FORWARD END -- REMOVED, DRILLED AND INSTALLED NEW BEAM. 2 L 7 2 4F A6WE 2001112100108 20011121 00108 WP 2001 11 21 MWEA011451 1 20011120 A 5210 995575621 BEAM DOUG DC9 DC915 3022036 WP MAIN CABIN DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 MAIN CABIN DOOR BEAM NUMBER 5 IS CRACKED ON FORWARD END -- LOCATED, DRILLED AND INSTALLED NEW DOOR BEAM. 2 L 7 2 4F A6WE 2001112100109 20011121 00109 EA 2001 11 21 COMA0160912 1 20011117 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 1900309 EA R/H MALFUNCTIONED A COMA O OTHER J WARNING INDICATION UK UNKNOWN 1 SO 01 984CA 12851 7171 FLIGHT #6054 FLAPS FAILED AT 8 DEGREES.REPLACED THE R/H BPSU. 2 L 7 2 4F RT A21EA 2001112100110 20011121 00110 EA 2001 11 21 COMA0160911 1 20011116 A 5210 DOOR LATCH CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 924CA 7026 FLIGH 6594 CABIN DOOR LATCH MESSAGE AFTER T/O.ADJUSTED DOOR LATCH LINKAGE. ACFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2001112100111 20011121 00111 WP 2001 11 21 ABXA010588 1 20011118 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 937AX 47074 COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC-9 AMM 33-53-02-4- 0001. 2 L 7 2 4F A6WE 2001112600019 20011126 00019 EA 2001 11 26 COMA0160910 1 20011118 A 7333 912768 TRANSDUCER CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE FAILED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 920CA 14604 7022 FLIGHT 6075 RT FUEL FLOW INDICATION WENT TO ZERO DURING T/O. REPLACED THE RT ENGINE FUEL FLOW TRANSDUCER. 2 L 7 2 4F RT A21EA 2001112100112 20011121 00112 WP 2001 11 21 ABXA010589 1 20011119 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 974AX 47623 EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC-9 AMM 33-53-00-8-0001. 2 L 7 2 4F A6WE 2001112100113 20011121 00113 2001 11 21 AWXA200100577 4 20011105 A 2216 BACC63BN18C14S8 CONNECTOR BOEING 737 737277 1384570 NM AUTOPILOT SYS WORN A AWXA A UNSCHED LANDING F E FLT CONT AFFECTED VIBRATION/BUFFET CL CLIMB 1 WP 28 184AW 22651 AFTER T/O, HEARD LOUD THUMP DURING GEAR RETRACTION, INDICATIONS NORM. IN FLT W/AP ENGAGED ACFT STARTED PORPOISING. AP WA S DISENGAGED, DIFFICULTY CONTROLLING PITCH ATTITUDE. DIVERTED. ON APPROACH 165 KTS BUFFETING FELT, FLAPS 15, 170 KTS. F ERRIED, A COMPLETE VERT STAB & ELEV CHECK INCLUDING CABLES, PULLEYS, BEARINGS, SURFACES & ELECT CONTROL SYS PERFORMED. AUTO PILOT STAB TRIM SERVO CONNECTOR (D381) PIN NR 3 FOUND LOOSE & WORN THRU INSULATION. REPLACED CONNECTOR, STAB TRIM BRAKE, AUTO PILOT STAB TRIM SERVO MOTOR, FLAPS UP LIMIT SWITCH (S245), STAB TRIM CUTOUT SWITCH (S272) & STAB ELEC ACT LI MIT & TAKEOFF WARNING SWITCH (S546). LOUD THUMP DETERMINED TO BE NOSE GEAR LOCK ACTUATOR, WHICH WAS REPLACED. 2 L 7 2 4F RT A16WE 2001112100114 20011121 00114 NM 2001 11 21 AWXA200100588 1 20011116 A 5330 SKIN BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 PHX - MAJOR REPAIR -C- DENT FOUND IN FUSELAGE SKIN AFT OF L-2 DOOR, 3 X 3 X .156 INCH DEEP AT BS 780 AT STR 16L. AFTER ACCESSING INTERNAL AREA, STR 16L FOUND TO BE DEFORMED AND CRACKED ABOUT 1 INCH. MAINTENANCE MADE A STRINGER SPLICE REPA IR IAW B757 SRM 53-00-03, FIG 201 AND CUT OUT THE DAMAGED SKIN AREA, FABRICATED REPAIR PARTS AND INSTALLED A FLUSH REPAI R IAW B757 SRM 53-00-01. 2 L 7 2 4F RT A2NM 2001112100115 20011121 00115 EU 2001 11 21 AWXA200100589 1 20011115 A 2432 35OL5100508 LIMITER AIRBUS 320 A320232 3930326 EU E/E BAY MALFUNCTIONED A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 655AW 8359 1075 OMA - DIVERTED FLIGHT - FLT 722 -C- EN ROUTE TO ORD FROM LAS THE FLIGHT DECK CREW OBSERVED ECAM WARNING BCL NR 1 FAULT A ND THE NR 1 BATTERY DROPPED OFF LINE, NR 2 BATTERY WAS SHOWING 24 VOLTS AND NOT CHARGING. THE AIRCRAFT DIVERTED TO OMA MAKING AN UNEVENTFUL LANDING. MAINTENANCE PERFORMED BITE AND OPERATIONAL CHECKS OF NR 1 & 2 BCL (BATTERY CHARGER LIMITE R) IAW AMM 24-38-710-001, THE SYSTEM RESET AND CHECKED NORMAL. THE FLIGHT CONTINUED TO ORD AND BACK TO PHX WITH NO FURT HER DISCREPANCIES. IN PHX THE NR 1 BCL WAS REPLACED AS A PRECAUTION PER AWA LIAISON ENGINEERING REQUEST. 2 L 7 2 4F RT A28NM 2001112100116 20011121 00116 EU 2001 11 21 AWXA200100590 1 20011116 A 2822 568127202002 PUMP AIRBUS 320 A320231 3930325 EU FUEL TANK FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 634AW 33607 3765 091 CMH - DIVERTED FLIGHT - FLT 683 -C- EN ROUTE FROM PHX TO EWR DURING CLIMB THE FLIGHT DECK CREW OBSERVED ECAM MESSAGE CTR TK PUMP 1 LO PRESS, FOLLOWED BY PUMP 2 LO PRESS. THE CREW CONTACTED MAINTENANCE CONTROL AND WERE INSTRUCTED TO TRY MAN UAL MODE, BUT STILL HAD CENTER TANK NR 1 & 2 FUEL PUMP FAULTS. THE AIRCRAFT WAS DIVERTED TO CMH. MAINTENANCE TROUBLESH OT AND REPLACED THE NR 1 & 2 CENTER TANK FUEL PUMPS IAW AMM 28-21-51-401. OPERATIONAL CHECKS WERE GOOD AND NO FURTHER D ISCREPANCIES HAVE BEEN REPORTED. PART NAME: FUEL PUMP - MFG: GEC-MARCONI AVIONICS LTD. - P/N: 568-1-27202-002 - S/N: 70 4 - COND: FAILED - LOC: NR 1 CENTER - TT: 37841 - TC: 17491 - TSR: 10558 - 2 L 7 2 4F RT A28NM 2001112100117 20011121 00117 SO 2001 11 21 C2XA01BT177 1 20011116 A 2530 RECEPTACLE EMB 135 EMB135LR 3260305 SO GALLEY BURNED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 14522 145383 EWR---CO3097, EN ROUTE HPN-CLE, CREW REPORTED BURNING SMELL IN CABIN AND COCKPIT THAT DID NOT SUBSIDE WITH THE RECIRCULA TION FANS BEING TURNED OFF. EWR MAINTENANCE FOUND BOTH COFFEE POT CONNECTOR RECEPTACLES HAD BURNT PINS. REMOVED AND RE PLACED CONNECTOR RECEPTACLE FROM NR 1 COFFEE POT POSITION AND REPLACED BURNT PINS ON NR 2 COFFEE POT POSITION IAW EMB14 5 SERVICE BULLETIN 145-25-0113 AND 145-25-0200. OPS CHECKED GOOD WITH KNOWN GOOD COFFEE POTS. AIRCRAFT RETURNED TO SER VICE. 2 L 7 2 4F RT TOOO11AT 2001112100118 20011121 00118 SO 2001 11 21 C2XA01TY182 1 20011119 A 3350 487190 CONNECTOR EMB 135 EMB135ER 3260203 SO CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16511 145267 TYS DURING A SCHEDULED 1-C INSPECTION, PANEL 251 HF EMERGENCY LIGHT STRIP, WAS INOPERATIVE, DUE TO A BROKEN CONNECTOR. MAINTENANCE INSTALLED A NEW CONNECTOR ON PANEL 251 HF IAW EMB 135/145 AMM AND PERFORM A OPS CHECK, EVERYTHING WAS ACCOMP LISH AND WILL BE RELEASED UPON COMPLETION OF ALL MAINTENANCE. 2 L 7 2 4F RT T00011AT 2001112100119 20011121 00119 NM 2001 11 21 CALA011005 1 20011116 A 5314 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59338 23576 INSPECTION FOUND THE RT W/W AFT FAIRING ATTACH HARDWARE HAD WORN INTO RT KEEL BEAM LOWER O/B CHORD AT STA 678-727. REPA IRED IAW ECRA 5310-04218. 2 L 7 2 4F RT A16WE 2001112100120 20011121 00120 NM 2001 11 21 DHL2001724010 1 20011116 A 3040 WINDSHIELD WIPER BOEING 727 727228 1384083 NM WINDSHIELD INTERMITTENT A DHLA O OTHER O OTHER TO TAKEOFF 1 SO 01 724DH 19862 F/O'S WINDSHIELD WIPER INTERMITTENT ON TAKEOFF. REMOVED AND REPLACED F/O'S WINDSHIELD WIPER ASSY IAW B-727 M/M 30-42-42 , OPS CHECK SERVICEABLE. 2 L 7 3 4F RT A3WE 2001112100121 20011121 00121 NM 2001 11 21 UPS01437324 1 20011101 A 5410 FRAME BOEING 747 747200 1384847 NM #4 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C #4 PYLON NAC STA 221 FRAME SEVERAL LOOSE AND SHEARED FASTENERS ON LHS 1/2" CRACK EMINATING FROM FASTEN ER HOLE. THE PYLON STA 221 FRAME WAS REPAIRED AS PER HX RS-53-34698 / UPS-HKG -01-00114H CONTINUE INSP REQUIRE PER S B 747-54A2202 AT 18 MONTH OR 1200 CYCLES WHATEVER EAILER REF UPS REPAIR/ALTERATION AUTHORIZATION, ENGINEERING FILE NO.74 7-54-20007 THE PNEU. DUCTING & THE ANTI-ICING VALVE REINSTALLED AIR LEAK CHK & OPN CHK C/OUT MM 36-11-01,30-21-03. 2 L 7 4 4F RT A20WE 2001112100122 20011121 00122 NM 2001 11 21 UPS01437329 1 20011030 A 5410 FRAME BOEING 747 747200 1384847 NM #4 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C #4 PYLON NAC STA 235.94 APPROX PYLON VALVE ACCESS PNL #483EL CUTOUT FWD FRAME CRACKED AS MARKED. C UTOUT FWD FRAME CRACK STOP DRILLED & NDT INSPECTION CONFIRMED CRACK FREE BEYOND DRILLED HOLE AS PER NTM PT6, 51-00-00 FI G 4 AND FRAME REPAIRED AS PER SRM 54-14-03 FIG 1 PYLON VALVE WAS REFITTED, AIR LEAK CHK AND OPN CHK CARRIED OUT MM 36-11 -01, 36-11-00. 2 L 7 4 4F RT A20WE 2001112100123 20011121 00123 NM 2001 11 21 DHL2001726008 1 20011117 A 3260 DOWNLOCK SENSOR BOEING 727 727228 1384083 NM LT MLG FAILED A DHLA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 01 726DH 20409 ON GEAR EXTENSION GOT UNSAFE LEFT GEAR LIGHT ON FWD INST PANEL AND CONSTANT GEAR WARNING HORN WITH FLAPS AT 25 OR 30 DEG . SECONDARY GEAR INDICATION LIGHTS (S/O PANEL) NORMAL. COMPLIED WITH ABNORMAL CHECKLIST. CYCLED GEAR 3 TIMES, HAND CRAN KED LEFT MAIN, CONDUCTED LOW FLYBY AND LANDED WITH UNSAFE INDICATION. REMOVED AND REPLACED LT MAIN GEAR DOWNLOCK SENSOR IAW MM 32-61-91. OPS CHECK. 2 L 7 3 4F RT A3WE 2001112100124 20011121 00124 NM 2001 11 21 DHL2001748010 1 20011115 A 2612 ISOLATOR BOEING 727 727225 1384077 NM NR 1 ENGINE MISSING A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 748DH 22440 ENGINE FIRE PROTECTION SYSTEM NR 1 DETECTOR GROUND CIRCUIT LIGHT ILLUMINATED EN ROUTE. FOUND NR 1 ENG FIRE LOOP ISOLATOR CLAMP HARDWARE MISSING, LOOP TOUCHING CLAMP. INSTALLED NEW CLAMP AND ISOLATOR IAW MM 26-11-21. SYS OPS CHECKS GOOD I AW MM 26-11-00. CLEARS DMI 7747. 2 L 7 3 4F A3WE 2001112100125 20011121 00125 CE 2001 11 21 GLBA2001227 1 20011101 A 3610 LINE BEECH 1900 1900D 1154162 CE BLEED AIR OUT OF POSITION A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 260GL UE260 CABIN PRESSURIZATION FAILED. REROUTED PNEUMATIC LINE, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001112100127 20011121 00127 CE 2001 11 21 GLBA2001230 1 20011118 A 3620 AYLF206 GASKET BEECH 1900 1900D 1154162 CE BLEED AIR LEAKING A GLBA D RETURN TO BLOCK O OTHER CR CRUISE 1 NM 03 249GL UE249 RIGHT BLEED AIR FAILURE. INSPECTED REPAIRED EVA TUBING AND REPLACED GASKET ON OVER TEMP SENSOR. OPS CHECKED SYSTEM SAT ISFACTORY. 2 L 7 2 4T RT A24CE 2001112100128 20011121 00128 NM 2001 11 21 OZIA200143005 1 20010915 A 2710 43282 CONTROL UNIT DORNER DO32 DO328300 NM AILERON MISWIRED A OZIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 05 430Z 3127 DURING REMOVE AND REPLACE OF AILERON DISCONNECT UNIT, FOUND UNIT TO BE WIRED INCORRECTLY (PINS B & C WERE INCORRECT). S WAPPED WIRES B & C ON THE AILERON DISCONNECT UNIT TO CONFORM WITH THE AIRCRAFT WIRING MANUAL IAW DORNIER SPR RESPONSE A0 0025599. UNIT INSTALLED AND OPS CHECKED GOOD. 2 H 7 2 4T RT A55NM 2001112100129 20011121 00129 NM 2001 11 21 PCAA0111136 1 20011118 A 3222 88303 CAP DHAV DHC8 DHC8102 2809003 NM NLG STRUT CRACKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 833EX DCL18689 282 DURING ROUTINE MAINTENANCE VISIT, PISTON CAP FOR NOSE LANDING GEAR SHOCK STRUT FOUND BROKEN AT BOTTOM FLANGE. NOSE GEAR SHOCK STRUT PISTON CAP, AND LOWER PIN AND BUSHING FOR NOSE GEAR LOWER LINK REPLACED. WORK COMPLETED IN ACCORDANCE WITH COMPONENT MAINTENANCE MANUAL AND ALLEGHENY JOB CARD 008-3220-379. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001112100130 20011121 00130 NM 2001 11 21 PCAA0111137 1 20011119 A 5250 LATCH DHAV DHC8 DHC8102 2809003 NM COCKPIT DOOR LACK OF LUBE A PCAA K NONE O OTHER NR NOT REPORTED 1 EA 13 821EX 173 BWI-FLIGHT 3909. CREW REPORTED COCKPIT DOOR LATCH MECHANISM IS BINDING AND HARD TO TURN PREVENTING EGRESS. MAINTENANCE LUBED LATCH. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001112100131 20011121 00131 EU 2001 11 21 QXEA0101962 1 20011117 A 3350 6008105 BATTERY PACK FOKKER F28 F28MK4000 4990810 EU CARGO BAY DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US 8365 263 11161 PDX-BOTH AFT EXTERIOR EVACUATION LIGHTS INOPERATIVE. REMOVED AND REPLACED AFT CARGO PIT EVACUATION LIGHTS BATTERY PACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001112100132 20011121 00132 NM 2001 11 21 QXEA0101958 1 20011115 A 2610 4462531 DETECTOR DHAV DHC8 DHC8202 2809007 NM INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX-LAVATORY FIRE DETECTOR WILL NOT TEST. REMOVED AND REPLACED LAVATORY FIRE DETECTOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001112100133 20011121 00133 NM 2001 11 21 UPS01237293 1 20011115 A 3350 LIGHT BOEING 727 727247 138408F NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 209UP 21698 INSPECTION TYPE:N/A COCKPIT EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED EMERGENCY LIGHT ASSY PER MM 33-50-01, OP S CHECKS GOOD. 2 L 7 3 4F A3WE 2001112100134 20011121 00134 EU 2001 11 21 QXEA0101961 1 20011118 A 3350 900835A BATTERY FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US 11161 PDX-EMERGENCY EGRESS LIGHTS AT ROW 11-14 INOP. REMOVED AND REPLACED THE CARTRIDGE BATTERY AS NEEDED. OPERATIONAL CHECK G OOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001112100136 20011121 00136 NM 2001 11 21 UPS01437282 1 20011112 A 5711 SPAR BOEING 747 747123F NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:SP RIGHT WING REAR SPAR HAS A 1.5 INCH CRACK IN AFT WING SPAR WEB AT STA 1238 REF DMI D-226421. STOP DR ILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-10-05 FIG 2. 2 L 7 4 4F A20WE 2001112100137 20011121 00137 NM 2001 11 21 UPS01437286 1 20011109 A 5411 FRAME BOEING 747 747200 1384847 NM NR 4 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C NR 4 PYLON NAC STA 221.94 ENG AFTER MOUNT BULKHEAD REAR O/B SIDE LOWER PORTION SUPPORT FRAME FOUND CRA CK FROM REAR EDGE TO FWD ABOUT .75 INCH LONG APPROX AS MARKED AFTER THE AREA CLEAN UP. NR 4 PYLON NAC STA 221.94 O/B SI DE FRAME REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F RT A20WE 2001112100138 20011121 00138 NM 2001 11 21 UPS01437287 1 20011101 A 5311 FRAME BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C RIGHT BS 320 NOSE WHEEL WELL FRAME CRACK AT 5 EA FASTENER HOLES WHICH 4 EA AT WEB AND 1 EA AT CHORD FO R DETAIL, PLS REFER ATTACHED FIGURE. FRAME REPAIRED AS PER SRM 51-40-03 FIG 1. CHORD REPAIRED AS PER SRM 51-40-04 FIG 2. 2 L 7 4 4F RT A20WE 2001112100139 20011121 00139 NM 2001 11 21 UPS01437292 1 20011114 A 3350 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:N/A STAIRWAY OVERHEAD LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT IAW B747 MM 33-51-00, OPS CHECKS GOOD. 2 L 7 4 4F A20WE 2001112100140 20011121 00140 NM 2001 11 21 UPS01437294 1 20011116 A 3350 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP AT CREW ESCAPE DOOR. REMOVED BATTERY POWER SUPPLY IAW AMM 33-51-04 RED A7 29592 TLS 86245. REINSTALLED SAME POWER SUPPLY MODULE IAW B747 MM 33-51-04. RELAMPED LIGHTED EXIT SIGN IAW B747 MM 33- 51-02, OPS CHECKS GOOD. 2 L 7 4 4F A20WE 2001112100141 20011121 00141 NM 2001 11 21 UPS01437299 1 20011101 A 5411 65B903118 FRAME BOEING 747 747200 1384847 NM NR 4 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C, NR 4 PYLON (O/B STRUT) AFT TORQUE BULKHEAD VERTICAL CHORD FOUND 1 FASTENER HOLE CRACK AT CHORD FWD SU RFACE RUNNING O/B AT 4 O'CLOCK POSITION APPROX .125 INCH LENGTH. CRACK HOLE REAMED ECCENTRICALLY TO 0.500 INCH AND NDT INSPECTION CONFIRMED CRACK FREE REF NTM PT6, 51-00-00 FIG 4. INSURANCE CUT AND FREEZE PLUG CUTOUT ON CHORD AS PER SRM 5 1-10-08, ANGLE AND DOUBLER, FABRICATED, INSTALLED DETAILS REF PROCESS CARD AND RCBR017 & UPS-EO- 747-5410-13496 PG 58 F IG 2, TELEX UPS-HKG01-00116H & RS 54-53-34701. 2 L 7 4 4F RT A20WE 2001112100142 20011121 00142 NM 2001 11 21 AWXA200100592 1 20011111 A 5313 6545767512 STRINGER BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 311AW 24712 MCN - C12 CK - "C" - CRACK FOUND AT FWD EDGE OF WING SCANNING LIGHT CUTOUT AT BS 500C+4, STR 16R, 1.1" LONG. MAINTENANCE REMOVED CRACKED STRINGER END, FABRICATED REPAIR CHANNEL AND FILLER AND INSTALLED REPAIR PARTS IAW AWA ER 03-5312-01094- DD1 REFERENCING BOEING SB 737-53-1145. 2 L 7 2 4F RT A16WE 2001112100143 20011121 00143 WP 2001 11 21 MWEA011442 1 20011120 A 5310 99124535 SHEAR TIE DOUG DC9 DC915 3022036 WP F.S. STA. 370 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 SHEAR TIE AT FUSELAGE STATION 370 BETWEEN LONGERON 30 AND LONGERPM 29 RIGHT IS CORRODED -- REMOVED, FABRICATED AND INS TALLED SHEAR TIE. 2 L 7 2 4F A6WE 2001112100144 20011121 00144 WP 2001 11 21 MWEA011443 1 20011120 A 5310 99124575 SHEAR TIE DOUG DC9 DC915 3022036 WP F.S. STA. 370 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 SHEAR TIE AT FUSELAGE STATION 377.5, BETWEEN LONGERON 29 RIGHT AND LONGERON 29 LEFT IS CORRODED -- REMOVED, FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F A6WE 2001112100145 20011121 00145 WP 2001 11 21 MWEA011445 1 20011120 A 5310 59164411 LONGERON DOUG DC9 DC915 3022036 WP FS STA 313-330 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 MODERATE CORROSION IN LONGERON CHANNEL 29 LEFT FROM 313 TO 332 -- FABRICATED AND INSTALLED REPAIR FITTING ON LONGERON 29 LEFT AT STATION 313-332. 2 L 7 2 4F A6WE 2001112100146 20011121 00146 WP 2001 11 21 MWEA011446 1 20011120 A 5230 J0602283 WEB DOUG DC9 DC915 3022036 WP F.S. STA. 370 MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 FORWARD CARGO DOOR JAMB WEB (GUSSET) MISDRILLED 2 PLACES AT FUSELAGE STATION 377.5 AND LONGERON 29 RIGHT -- REMOVED, F ABRICATED AND INSTALLED WEB REPAIR. 2 L 7 2 4F A6WE 2001112100147 20011121 00147 WP 2001 11 21 MWEA011454 1 20011120 A 5210 995575013 FORMER DOUG DC9 DC915 3022036 WP HOOK ACTUATOR ELONGATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 PASSENGER DOOR INTERCOSTAL (FORMER) HAS ELONGATED ON END NEAR HOOK ACTUATOR CRANK -- LOCATED AND DRILLED HOLES IN NEW FORMER. INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001112100148 20011121 00148 NM 2001 11 21 UPS01437312 1 20011116 A 3350 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:N/A EMERGENCY LIGHTS EXIT SIGN OVER CREW SERVICE DOOR INOP. REMOVED BATTERY POWER SUPPLY IAW MM 33-51-0 4. REINSTALLED SAME POWER SUPPLY MODULE IAW B747 MM 33-51-04. RELAMPED LIGHTED EXIT SIGN IAW B747 MM 33-51-02, OPS CHE CKS GOOD. 2 L 7 4 4F A20WE 2001112100149 20011121 00149 NM 2001 11 21 UPS01637280 1 20011113 A 3350 CONTROL PANEL BOEING 767 767300 1385204 NM CABIN DEFECTIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 312UP 27763 INSPECTION TYPE:N/A EMERGENCY LIGHT SWITCH INWARDS MISSING SWITCH DOES NOT ARM AUTO WHEN CLOSING GUARD. WORKS OK MANUAL LY. REMOVED AND REPLACED EMERGENCY LIGHT PANEL ASSY. OPS CHECKS GOOD. 2 L 7 2 4F RT A1NM 2001112100150 20011121 00150 NM 2001 11 21 UPS01637290 1 20011115 A 5610 WINDOW BOEING 767 76734AF 1385212 NM COCKPIT LEAKING A IPXA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 303UP 27241 INSPECTION TYPE:N/A ATB-L1 WINDOW AIR LEAK. RETORQUED WINDOW, PRESSURIZED, GOOD REFERENCE D226668. 2 L 7 2 4F RT A1NM 2001112100152 20011121 00152 NM 2001 11 21 SWAA013041 1 20011108 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAMS CRACKED (3 EA) AT BS 787, 747 & 727D, RBL 14. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2001112100153 20011121 00153 NM 2001 11 21 SWAA013042 1 20011108 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4R. REPAIRED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2001112100154 20011121 00154 NM 2001 11 21 SWAA013045 1 20011108 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REPAIRED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2001112100155 20011121 00155 2001 11 21 SWAA013048 4 20011108 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 089SW 22904 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2001112100156 20011121 00156 2001 11 21 SWAA013049 4 20011108 A 3425 7057VR INDICATOR BOEING 737 7373H4 1384600 NM COCKPIT FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 364SW 26575 (AIR TURNBACK) DURING FLIGHT STANDBY HORIZON ATTITUDE INDICATOR FAILED (WARNING FLAG AND TUMBLED). REMOVED AND REPLACED STANDBY ATTITUDE HORIZON INDICATOR PER MM. 2 L 7 2 4F RT A16WE 2001112100157 20011121 00157 NM 2001 11 21 SWAA013050 1 20011110 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 798SW 28436 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER CRACKED IN FWD CABIN. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2001112100158 20011121 00158 2001 11 21 SWAA013051 4 20011108 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001112100159 20011121 00159 2001 11 21 SWAA013053 4 20011107 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 740SW 29276 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001112100160 20011121 00160 2001 11 21 SWAA013054 4 20011108 A 2565 63551101 SLIDE BOEING 737 7377H4 1384404 NM AFT ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 406WN 27894 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001112100161 20011121 00161 NM 2001 11 21 SWAA013057 1 20011108 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 294.5, LBL 12 TO RBL 12. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2001112100162 20011121 00162 NM 2001 11 21 SWAA013062 1 20011109 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 380SW 26587 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, WL 201, LBL 5 & RBL 5. REPAIRED BULKHEAD WEB PER SRM. 2 L 7 2 4F RT A16WE 2001112100163 20011121 00163 NM 2001 11 21 SWAA013063 1 20011110 A 2781 60890500 SWITCH BOEING 737 7373Y0 1384671 NM L/E SLAT FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 308SA 23498 (AIR TURNBACK) AFTER TAKEOFF, NR 3 & 5 L/E SLATS AND FLAPS LIGHTS ILLUMINATED UPON FLAP RETRACTION. REMOVED AND REPLACE D NR 3 SLAT ROD END SWITCH AND CLEANED NR 5 ROD END SWITCH. OPS CK GOOD PER MM. 2 L 7 2 4F RT A16WE 2001112100164 20011121 00164 NM 2001 11 21 SWAA013066 1 20011112 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED A2 CHECK, FOUND AFT SVC DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT PER MM. 2 L 7 2 4F A16WE 2001112100165 20011121 00165 NM 2001 11 21 SWAA013067 1 20011111 A 3350 57771 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED C2 CHECK, FOUND EEPLS END CAP MISSING IN AFT CABIN. INSTALLED END CAP PER MM. 2 L 7 2 4F A16WE 2001112100166 20011121 00166 2001 11 21 SWAA013068 4 20011111 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 793SA 27888 AFT ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001112100167 20011121 00167 NM 2001 11 21 SWAA013069 1 20011111 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM SERVICE DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 060SW 21812 FWD SVC DOOR EMERGENCY EXIT LIGHT ASSY LOOSE. SECURED EXIT LIGHT PER MM. 2 L 7 2 4F A16WE 2001112100168 20011121 00168 2001 11 21 SWAA013070 4 20011112 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 FWD ENTRY DOOR EMERGENCY EVC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001112100169 20011121 00169 NM 2001 11 21 SWAA013071 1 20011112 A 5320 6551698 SPLICE BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED D-CHECK, FOUND STR SPLICE'S CRACKED (2 EA) AT BS 908, STR 4L & 4R. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2001112100170 20011121 00170 NM 2001 11 21 SWAA013072 1 20011112 A 5320 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001112100171 20011121 00171 NM 2001 11 21 SWAA013076 1 20011111 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED (6 EA) AT BS 178, BETWEEN LBL 1 & RBL 1. REPAIRED WEB PER SR M. 2 L 7 2 4F RT A16WE 2001112100172 20011121 00172 NM 2001 11 21 SWAA013079 1 20011113 A 3260 6565352 UPLOCK SENSOR BOEING 737 7372H4 138448C NM NLG FAILED A SWAA K NONE N FALSE WARNING CL CLIMB 1 SW 07 105SW 23249 AFTER GEAR RETRACTION RED NOSE GEAR LIGHT STAYED ON. CYCLED GEAR, LIGHT STAYED ON WITH GEAR UP. REMOVED AND REPLACED U PLOCK SENSOR ON NLG PER MM. 2 L 7 2 4F A16WE 2001112100173 20011121 00173 NM 2001 11 21 P2EA2001V0012 1 20011112 A 5210 DOOR FRAME BOEING 737 737230 1384401 NM L1 DOOR CRACKED A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 122NJ 22120 DURING C CHECK INSPECTION, L1 DOOR FWD AND AFT LOWER CORNER AND LOWER PAN WITH A CRACK. REPAIRED DOOR FRAME IAW SRM 51-4 0-3 FIG 1. 2 L 7 2 4F RT A16WE 2001112100174 20011121 00174 NM 2001 11 21 P2EA2001V0013 1 20011112 A 5532 SKIN BOEING 737 737230 1384401 NM VERTICAL STAB DENTED A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 122NJ 22120 C CHECK, VERTICAL FIN WITH DENTS BETWEEN FIN STA 191.5 - 180.3. REPAIRED SKIN IAW SRM 55-30-6 FIG 2. 2 L 7 2 4F RT A16WE 2001112100175 20011121 00175 NM 2001 11 21 P2EA2001V0014 1 20011112 A 5414 FAIRING BOEING 737 737230 1384401 NM WORN A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 122NJ 22120 During "C" Check Inspection:-No.2 Engine Pylon, Aft Fairing Worn at Imb Side.-No. 2 Pylon Imboard Fairing Outer Skin Rep aired due to Wear, IAW COOPESA E.O. No. EO-COO-3-54-609-01, Dated Nov 06, 2001, Documented on FAA 8110-3 form approved b y DERT710167SW.Note: See COOPESA Work Order No. O10863 4-12, VAM100 No.138 & 122SDA100. 2 L 7 2 4F RT A16WE 2001112100176 20011121 00176 NM 2001 11 21 P2EA2001V0015 1 20011112 A 5330 SKIN BOEING 737 737230 1384401 NM DENTED A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 122NJ 22120 During "c" Check Inspection:-Fuselage, BS1086, Between Str 25 & 26 R-H Skin With Dent Out of Limits.-Repaired Fuselage S kin Section From BS1069.5 to BS1090.5, Between Str 20 & 27 R-H due to Dent, IAW COOPESA E.O. No.EO-100-3-53-604-01, Date d Nov 05, 2001 Documented on FAA 8110-3 Form, Approved by DERT-710167-SW.Note: See COOPESA Work Order No.O10863 1-11, Va m100 No. 048 & 122SDA064. 2 L 7 2 4F RT A16WE 2001112100177 20011121 00177 NM 2001 11 21 P2EA2001V0016 1 20011112 A 5414 FAIRING BOEING 737 737230 1384401 NM WORN A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 122NJ 22120 During "C" Check Inspection.-Engine No.1, Nacelle Fairing, Imb Aft Section, Outter Skin With Wear.-Engine No.1, Nacelle Fairing, Imb Aft Section, Outter Skin Repaired due to Wear, IAW COOPESA E.O. No. EO-100-3-54-609-01, Dated Nov 06, 2001 Documented on FAA8110-3 Form Approved by DERT710167SW.Note: See COOPESA Work Order No. O10863 4-13, VAM 100 No. 113 & 12 2SDA101. 2 L 7 2 4F RT A16WE 2001112100178 20011121 00178 NM 2001 11 21 P2EA2001V0017 1 20011112 A 5314 SKIN PANEL BOEING 737 737230 1384401 NM CRACKED A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 122NJ 22120 During "C" Check Inspection.-Fuselage, Keel Beam Panel Cracked at BS 698 and With Loose Rivets at BS726, Str27 L-H.-Repl aced Fuselage Keel Beam Skin Panel from BS 661.75 to BS 726.75, Between LBL 6.30 to RBL 6.30 due to Cracks IAW Boeing S/ B 737-53-1104, Section III, Part II, Fig 3, 6 & 7, Rev. 4.Note: See COOPESA Work Order No. O10863 1-10, VAM100 No. 045 & 122SDA096. 2 L 7 2 4F RT A16WE 2001112100179 20011121 00179 NM 2001 11 21 P2EA2001V0018 1 20011112 A 5330 SKIN BOEING 737 737230 1384401 NM DENTED A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 122NJ 22120 During "C" Check Inspection.-Fuselage, at BS390, Between Str 17 & 18 L-H, Skin With Dent Out of Limits.-Repaired Fuselag e Skin Section From BS387 to BS396, Between Str17 & 18 L-H,IAW SRM53-30-3 Fig17Note: See COOPESA Work Order No. O10863 1 -9, VAM100 No.046 & 122SDA062. 2 L 7 2 4F RT A16WE 2001112100180 20011121 00180 NM 2001 11 21 P2EA2001V0019 1 20011112 A 5313 STRINGER BOEING 737 737230 1384401 NM CRACKED A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 122NJ 22120 During "C" Check Inspection.-Fuselage, BS1080, Str 22 R-H With Crack.-Fuselage Stringer Section Repaired at Str 22 R-H, From BS1050 to BS1088, IAW SRM 53-10-3, Fig 1Note: See COOPESA Work Order No. O10863 1-70, VAM100 No. 227 & 122SDA099. 2 L 7 2 4F RT A16WE 2001112100181 20011121 00181 NM 2001 11 21 P2EA2001V0020 1 20011113 A 5330 SKIN BOEING 737 737230 1384401 NM DENTED A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 122NJ 22120 During "C" Check Inspection.-Fuselage at BS984, Between Str 24 & 25 L-H, Skin With Dent Out of Limits.-Fuselage Skin Sec tion Repaired From BS982 to BS986.5, Between Str 24 & 25 L-H, Due to Dent IAW SRM 53-30-3 Fig 5.Note: See COOPESA Work O rder No.O10863 1-17, VAM 100 No. 056 & 122SDA068. 2 L 7 2 4F RT A16WE 2001112100182 20011121 00182 NM 2001 11 21 P2EA2001V0021 1 20011113 A 5330 SKIN BOEING 737 737230 1384401 NM DENTED A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 122NJ 22120 During "C" Check Inspection.-Fuselage at BS499, Between Str 26 & 27 R-H, Skin With Dent Out of Limits.-Fuselage Skin Sec tion Repaired From BS492 to BS504.5, Between Str 25 & 28 R-H, Due to Dent, IAW Boeing Telex COO-SJO-01-00893H & COOPESA E.O. No.COO-3-53-607-01 Dated NOV 06,2001, Approved on FAA 8110-3 Form by DERY-635303-NM, Dated NOV 12,2001.Note: See CO OPESA Work Order No. O10863 1-16, VAM100 No.055 & 122SDA067. 2 L 7 2 4F RT A16WE 2001112100183 20011121 00183 NM 2001 11 21 P2EA2001V0022 1 20011114 A 5344 SKIN BOEING 737 737230 1384401 NM CRACKED A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 122NJ 22120 During "C" Check Inspection.-L2 Door Area, Fuselage Lower Hinge Cut out, Lower Section, Skin With Sharp Edges & Crack.-R epaired Fuselage Skin Section at L2 door Lower Hinge Cut out, From BS945to BS956, Between Str 13 & 16 L-H, IAW SRM 53-30 -3, Fig 34.Note: See COOPESA Work Order No. O10863 2-27, VAM100 No.091 & 122SDA071. 2 L 7 2 4F RT A16WE 2001112100184 20011121 00184 NM 2001 11 21 P2EA2001V0023 1 20011114 A 5330 SKIN BOEING 737 737230 1384401 NM DENTED A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 122NJ 22120 During "C" Check Inspection.-Fuselage at BS325, Between Str 20 & 21 R-H, Skin With Dent Out of Limits.-Fuselage Skin Sec tion Repaired, From BS320 to BS350.5, Between Str 19 & 24 R-H, IAW SRM 53-30-3, Fig 17.Note: See COOPESA Work Order No.O 10863 1-8, VAM100 No. 047 & 122SDA063. 2 L 7 2 4F RT A16WE 2001112100185 20011121 00185 NM 2001 11 21 P2EA2001V0024 1 20011114 A 5312 ATTACH ANGLE BOEING 737 737230 1384401 NM CRACKED A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 122NJ 22120 During "C" Check Inspection.-Control Cabin, Fwd Pressure Bulkhead BS178, R-H Side Chord Cracked Between WL 207 & 210.-Pr eventive Modification accomplished at Fwd Pressure Bulkhead BS178, R-H Chord, Between WL184 & 230 due to Crack IAW Boein g S/B 737-53A1173, REV3, Section III Part XI Paragraph I Fig 71.Note: See COOPESA Work Order No. O10863 2-37, VAM100 No. 213 & 122SDA094. 2 L 7 2 4F RT A16WE 2001112100186 20011121 00186 NM 2001 11 21 P2EA2001V0025 1 20011120 A 5280 6550520504 DOOR BOEING 737 737230 1384401 NM DELAMINATED A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 122NJ 22120 During "C" Check Inspection.-R-H NLG Door, P/N 65-50520-504, S/N BNW330 Found With Delamination.-Repaired R-H NLG Door D ue to Delamination From BS294.5 to BS262.5, IAW COOPESA EO No.COO-CMP-3-52-614-01, Dated Nov 07, 2001 & Documented on FA A 8110-3 Form Approved by DERT-7101676-SW.Note: See COOPESA Work Order No. O10863 6-46, VAM100 No.238 & 122SDA102. 2 L 7 2 4F RT A16WE 2001112100187 20011121 00187 NM 2001 11 21 P2EA2001V0027 1 20011121 A 5753 6546434140 FLAP BOEING 737 737230 1384401 NM DELAMINATED A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 122NJ 22120 During "C" Check Inspection.-R-H Wing Imb Aft Flap Delaminated & Dented.-Repaired R-H Wing Imb Flap P/N 65-46434-140, S/ N BN442 Due to Delamination From Wbl 180.75 to 165.875 & From Wbl 155.75 to 143 IAW COOPESA EO No.COO-CMP-3-57-612-01 Da ted Nov 06, 2001, Approved on FAA 8110-3 Form By DERT-710167-SW.Note: See COOPESA Work Order No. O10863 6-48, VAM100 No. 234 & 122SDA065. 2 L 7 2 4F RT A16WE 2001112100188 20011121 00188 NM 2001 11 21 P2EA2001V0028 1 20011121 A 5753 654643090 FLAP BOEING 737 737230 1384401 NM WORN A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 122NJ 22120 During "C" Check Inspection.-R-H Wing Imb Fore Flap Skin Worn at Imb Side.-Repaired R-H Imb Fore Flap, P/N 65-46430-90, S/N BN436 Due to Worn Skin IAW COOPESA EO No. COO-CMP-3-57-608-01, Dated Nov 06, 2001 Approved on FAA 8110-3 Form By DER T-710167SW.Note: See COOPESA Work Order No. O10863 6-47 & 122SDA066. 2 L 7 2 4F RT A16WE 2001112100189 20011121 00189 NM 2001 11 21 P2EA2001V0029 1 20011121 A 5753 657193091 FLAP BOEING 737 737230 1384401 NM DELAMINATED A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 122NJ 22120 During "C" Check Inspection.-L-H Wing Outb Flap Imb Hinge Flap, T/E Section Delaminated.-Repaired L-H Outb Flipper Flap, P/N 65-71930-91 Due to Delamination IAW COOPESA EO No. COO-CMP-3-57-610-01, Dated Nov 06, 2001 Approved on FAA 8110-3 F orm By DERT710167SW.Note: See COOPESA Work Order No.01 0863 5-50, VAM100 No. 239 & 122SDA076. 2 L 7 2 4F RT A16WE 2001112100190 20011121 00190 NM 2001 11 21 P2EA2001V0030 1 20011121 A 5753 654643089 FLAP BOEING 737 737230 1384401 NM DELAMINATED A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 122NJ 22120 During "C" Inspection.-L-H Wing Imb Fore Flap upper Surface WBL 150.4 Delaminated.-Repaired L-H Wing Imb Fore Flap P/N 6 5-46430-89, S/N BN-430 Due to Delamination From WBL 73.00 to 89 & From WBL 156.15 to 145.15 IAW COOPESA EO No. COO-CMP-3 -57-613-01, Dated Nov 06,2001 And Approved on FAA 8110-3 Form By DERT-710167SW.Note: See COOPESA Work Order No. O10863 5 -47, VAM100 No.236, 122 & 122SDA077. 2 L 7 2 4F RT A16WE 2001112700154 20011127 00154 EU 2001 11 27 SABA011065 1 20011116 A 2910 104A70303A HYDRAULIC SYSTEM BAG JETSTM JETSTM3201 1500217 EU MAIN CONTAMINATED A SABA O OTHER O OTHER CL CLIMB 1 SO 33 961AE 961 AIRCRAFT 961 ON FLIGHT 5103 FROM HICKORY TO CHARLOTTE: JUST AFTER TAKE-OFF, PILOT REPORTED THE RETRACTION OF RIGHT MAIN GEAR WAS SLOW. UPLOCK INDICATED NORMAL. AIRCRAFT LANDED IN CHARLOTTE WITH NO OTHER PROBLEM. NO EMERGENCY PROCEDURES W ERE USED. MAINTENANCE ADJUSTED THE UPLOCK LIMIT SWITCH AND BLED AIR FROM SYSTEM. RETRACTION CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A56EU 2001112300008 20011123 00008 EA 2001 11 23 COMA0160913 1 20011121 A 5346 601R5361345 BEAM CNDAIR CL600 CL6002B19 1900309 EA AFT EQUIPMETN BA CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 946CA 17747 7072 ENGINE SUPPORT BEAM AT F.S. 625 L/H WEB CRACKED, R/H SIDE WEB REPAIR INSTALLED PER CUSTOMER REQUEST. ALSO CENTER BEAM, U PPER AND LOWER WEBS CRACKED.PERFORMED A MAJOR REPAIR TO F.S. 625 ENGINE SUPPORT BEAM L/H AND R/H LOWER WEBS IAW REO 601R -53-61-366 REV C. REF MAINT LOG PAGES #390151 AND #390156. PERFORMED TEMPORARY REPAIR TO F.S. 625 ENGINE SUPPORT BEAM CE NTER, UPPER AND LOWER WEBS IAW REO 601R-53-61-345 REV B. REF MAINT LOG PAGE #390142. 2 L 7 2 4F RT A21EA 2001112300009 20011123 00009 EA 2001 11 23 COMA0160914 1 20011122 A 5320 NA BEAM CNDAIR CL600 CL6002B19 1900309 EA FLOOR CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 946CA 14747 7072 VERTICAL BEAM AT F.S. 409+128 RBL 27 CRACKED. VERTIDCAL BEAM AT F.S. 49+128 RBL 18 CRACKED. VERTICAL BEAM AT 409+128 LBL 27 CRACKED. NOTE: ALL BEAMS WERE CRACKED AT THE BOTTOM RIVET REF MAINT LOG PAGES #390153,#390154,#390155.VERTICAL BEA MS WERE REPAIRED I/A/W WVAC EO 601R-53-2838 AND STANDARD CRJ SRM PRACTICES. 2 L 7 2 4F RT A21EA 2001112300010 20011123 00010 WP 2001 11 23 ARWA20011105 1 20011120 A 5522 PLATE DOUG DC8 DC862 3021970 WP A ARWA O OTHER O OTHER IN INSP/MAINT 1 SO 19 1808E JW5103 46105 N/R 192 - DURING "C" CHECK INSPECTION, FOUND THE FOLLOWING: LH ELEVATOR LWR SKIN WITH CORRUGATION & OIL CANNING IN SEVE RAL POINTS, BETWEEN STA. XE 28.343 AND XE 200.218.CORRECTIVE ACTION: REMOVED LH ELEVATOR LWR PLATING; FABRICATED NEW PLA TING IAW AS ELEVEN, INC. DWG # AS11309, SH. 1 & 2, DATED 08/25/01. PRIMED PLATING IAW DC-8 SRM 51-1-8 & INSTALLED PLATI NG IAW AS ELEVEN, INC. DWG # AS11309. PAINTED ELEVATOR IAW SRM 51-20-0, PERFORMED WEIGHT & BALANCE OF THE LH ELEVATOR I AW DC8 SRM 51-4-4, PAGE1,2&3. 2 L 7 4 4F 4A25 2001113000055 20011130 00055 WP 2001 11 30 ARWA20011107 1 20011120 A 5320 37515142N FITTING DOUG DC8 DC862 3021970 WP FUSELAGE CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 1808E 46105 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: AFT CARGO COMPT STA 980 BULKHEAD LT STIFFENER WITH 1.5 INCH CRACK, NEAR MAIN CARGO DOOR COMPARTMENT FLOOR. REMOVED FITTING AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 2001112300011 20011123 00011 WP 2001 11 23 ARWA20011108 1 20011120 A 5512 PLATE DOUG DC8 DC862 3021970 WP A ARWA O OTHER O OTHER IN INSP/MAINT 1 SO 19 1808E 46105 N/R 412 - DURING "C" CHECK INSPECTION, FOUND THE FOLLOWING: RH HORIZONTAL STABILIZER TIE STA. XE 77.000 AND 92.000 UPPER SKIN WITH INNER CORROSION.CORRECTIVE ACTION: REMOVED CORROSION IAW DC8 SRM 51-1-8; FOUND TO BE OUT OF LIMITS IAW DC8 S RM 55-2-0. REMOVED UPPER PLATING; FABRICATED NEW PLATING & HATCHES IAW AS ELEVEN INC. DWG # AS11308, SH.1 & 2, DATED 08/ 25/01. PRIMED & INSTALLED PARTS IAW DC8 SRM 51-1-8 & AS ELEVEN INC. DWG # AS11308, DATED 08/25/01. 2 L 7 4 4F 4A25 2001112300012 20011123 00012 WP 2001 11 23 ARWA20011110 1 20011120 A 5713 5644972502 FITTING DOUG DC8 DC862 3021970 WP A ARWA O OTHER O OTHER IN INSP/MAINT 1 SO 19 1808E 46105 N/R 440 - DURING "C" CHECK INSPECTION, FOUND THE FOLLOWING: RH WING # 4 ALT. TANK INTERIOR STA. XRS 408.00 STRINGER # 58 END FITTING WITH CRACK.CORRECTIVE ACTION: OPENED FUEL TANK PLATE IAW DC8 MM 57-30-0; REMOVED & REPLACED FITTINGS IAW DC 8 SRM 51-1-20D AND CLOSED FUEL TANK PLATE IAW DC8 MM 57-30-0. LEAK CHECK ACCOMPLISHED ON FORM JW-48, ZONE 1, PAGE 15, I TEM 1. 2 L 7 4 4F 4A25 2001112300013 20011123 00013 WP 2001 11 23 ARWA20011112 1 20011120 A 5753 PLATE DOUG DC8 DC862 3021970 WP A ARWA O OTHER O OTHER IN INSP/MAINT 1 SO 19 1808E 46105 N/R 1068 - DURING "C" CHECK, THE FOLLOWING WAS FOUND: LH WING I/B FLAP LOWER SKIN WITH DENT AT STA. XW L7.CORRECTIVE ACT ION: FOUND DENT OUT OF LIMITS IAW DC8 SRM 57-1-0; REMOVED DAMAGED AREA; FABRICATED NEW SOLID PLATING, FILLER & SPLICE ST RAP IAW AS ELEVEN INC. DWG.# AS11324, SH.1 TO 3, DATED 09/12/01. PRIMED & INSTALLED PARTS IAW DC8 SRM 51-1-8 & AS ELEVE N INC. DWG.# AS11324, SH.1 TO 3, DATED 09/12/01. 2 L 7 4 4F 4A25 2001112300014 20011123 00014 WP 2001 11 23 ARWA20011113 1 20011120 A 5753 SKIN PANEL DOUG DC8 DC862 3021970 WP A ARWA O OTHER O OTHER IN INSP/MAINT 1 SO 19 1808E 46105 N/R 1076 - DURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND: RH INBOARD FLAP LOWER SKIN WITH CRACK OF 0.500" BETWEEN STA. XW 92 & XW 104 FAIRING AREA.CORRECTIVE ACTION: REMOVED SKIN PANEL; FABRICATED NEW SKIN PANEL IAW AS ELEVEN INC. DW G # AS11321, SH 1 & 2, DATED 09/07/01. PRIMED & INSTALLED NEW SKIN PANEL IAW DC8 SRM 51-1-8 AND AS ELEVEN INC. DWG.# AS 11321, SH. 1 & 2, DATED 09/07/01. 2 L 7 4 4F 4A25 2001112300015 20011123 00015 WP 2001 11 23 ARWA20011114 1 20011120 A 5315 FLOORBEAM DOUG DC8 DC862 3021970 WP FUSELAGE CRACKED A ARWA O OTHER O OTHER IN INSP/MAINT 1 SO 19 1808E 46105 DURING "C" CHECK INSPECTION, STA 1120, X=10 RT SIDE, FLOORBEAM WEB WITH CORROSION. ACCOMPLISHED HFEC INSPECTION IAW DC- 8 NDT MANUAL CHAPTER 06, FOUND CRACK OF 0.562 INCHES LENGTH DUE TO CORROSION & MATERIAL LOSS. TRIMMED OUT DAMAGED AREA; FABRICATED FILLER ANGLE & PLATE IAW AS ELEVEN DWG AS11323, SH 1 TO 5, DATED 09/11/01. PRIMED & INSTALLED PARTS IAW DC8 SRM 51-1-8 & AS ELEVEN INC DWG AS11323. 2 L 7 4 4F 4A25 2001112300016 20011123 00016 WP 2001 11 23 ARWA20011115 1 20011120 A 5713 STRINGER DOUG DC8 DC862 3021970 WP A ARWA O OTHER O OTHER IN INSP/MAINT 1 SO 19 1808E 46105 N/R 1080 - DURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND: RH WING # 3 MAIN FUEL TANK INTERIOR BETWEEN STA. XRS 74 & SRS 107, STIFFENER 69 WITH 1.500" CRACK.CORRECTIVE ACTION: CUT-OUT DAMAGE SECTION OF STRINGER IAW DC8 SRM 57-2-2, PAG E 2, MADE SPLICE FITTINGS & NEW STRINGER SECTION IAW DC8 SRM 57-2-2, FIG. 3D, PAGE 2, & 57-4-2, PAGE 11. PRIMED & INSTA LLED PARTS IAW DC8 SRM 51-1-8 & 51-1-20D. NO LEAKS NOTED IAW DC8 MM 28-00. 2 L 7 4 4F 4A25 2002030700149 20020307 00149 EU 2002 3 7 SABA011067 1 20011121 A 5270 91SE13 SWITCH BAG JETSTM JETSTM3201 1500217 EU PAX DOOR OUT OF ADJUST A SABA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 33 965AE 965 AIRCRAFT 065 FLIGHT 5042 FROM CHARLESTON SC TO RALEIGH. AFTER TAKEOFF, PASSENGER DOOR LIGHT ILLUMINATED. NO CABIN PRES SURE WAS LOST. AIRCRAFT RETURNED TO CHARLESTON AND LANDED WITH NO OTHER PROBLEMS. NO EMERGENCY PROCEDURES WERE USED. DOOR LOCKS WERE CHECKED. ALL LOCKS INDICATED LOCKED. AFTER RETURNING TO CHARLOTTE. MAINTENANCE ADJUSTED THE UPPER MIC RO SWITCH. SYSTEM GROUND CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A56EU 2001112500001 20011125 00001 NM 2001 11 25 S01257036 1 20011112 A 5700 65B085645 JACKSCREW BOEING 747 747209B NM PWA JT9 JT9D7Q 52054 NE # 2 FITTING FRACTURED W SAJF O OTHER O OTHER IN INSP/MAINT 1 WP 03 22447 B-18755 GRD CHK FOUND # 2 FLAP TRACK JACKSCREW FITTING BROKEN.C/A:1.ISSUED REVISION OF EO 740-57-50-0004 TO PERFORM THE REPLACEMENT/OVERHAUL IN LIEU OF INSPECTION. 2.ISSUED THE EON 57-632472-002 TO DETECT THE CORROSION AND CRACK TO AIRPLANE S THAT FITTINGS REPLACEMENT/OVERHAUL WAS NOT DONE. THIS EON WILL BE ACCOMPLISHED BEFORE DEC. 15, 2001. 3.ISSUED EON 57-6 32472-004 TO PERFORM ADDITIONAL INSTRUCTIONS PER BOEING RECOMMENDED FOR B-18755 ON NOV. 19, 2001. 4.PROVIDE BROKEN FITTI NG TO BOEING FOR FURTHER ANALYSIS REQUESTED. 5.OPEN THIS CASE FOR FURTHER ACTION AS REQUIRED. 2 L 7 4 4F 4 F RT A20WE E3NE 2001112600001 20011126 00001 NE 2001 11 26 COMA0110157 2 20011116 A 7320 3034652 SENSOR EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE RT ENGINE MALFUNCTIONED A COMA A UNSCHED LANDING S AFFECT SYSTEMS TO TAKEOFF 1 SO 01 269CA 120263 FLIGHT 5049 - THREE KNOB POWER LEVER SPLIT DURING T/O. REPLACED THE RT ENGINE T2 SENSOR. 2 L 7 2 4T 4 T RT A31SO E20NE 2001112600002 20011126 00002 WP 2001 11 26 0104619750 1 20011117 A 2611 473925 CONTROL UNIT DOUG DC9 DC941 302207N WP CARGO BAY MALFUNCTIONED A NWAA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 GL 01 750NW 47114 WHILE ON FINAL APPROACH FOR LANDING, THE FORWARD CARGO SMOKE DETECTOR LIGHTS FLICKERED. UPON LANDING, THE ALARM SOUNDED AND REMAINED ON. CREW REQUESTED CFR AND FIRED THE NR 1 CARGO FIRE BOTTLE. MAINTENANCE DID NOT FIND EVIDENCE OF FIRE O R SMOKE IN THE FORWARD CARGO BIN. THE FIRE BOTTLE AND SMOKE CEU WERE REPLACED AND TESTED WITH NO FAULTS FOUND. REPLACE D THE FIRE CONTROL PANEL AND TESTED OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001112600004 20011126 00004 CE 2001 11 26 0122 1 20011121 A 5270 SWITCH BEECH MU300 400A 1155402 CE PAX DOOR OUT OF ADJ E DJFA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 23 418CW RK18 AIRCRAFT WAS DEPARTING DENVER, AT 90 KTS THE DOOR WARNING LIGHT ILLUMINATED. ABORTED TAKEOFF AND MAINTENANCE INSPECTED DOOR SWITCH AND ADJUSTED. NO FURTHER PROBLEMS WERE NOTED. 2 H 7 2 4F RT A16SW 2001112600005 20011126 00005 EA 2001 11 26 0123 1 20011122 A 2612 24406322 SENSING ELEMENT CNDAIR CL600 CL6002B16 1900305 EA NR 1 ENGINE FAULTY E DJFA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 EA 23 653CW 5053 AT FL390 AIRCRAFT HAD A FIRE WARNING ON THE NR 1 ENGINE ALL CHECKLIST PROCEDURES WERE FOLLOWED AND ENGINE WAS SHUT DOWN. THE RED LIGHT DID NOT EXTINGUISH SO THE PILOTS DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE PROB LEM WAS FOUND TO BE FAULTY SENSING ELEMENT. AIRCRAFT WAS REPAIRED AND RELEASED. 2 L 7 2 4F RT A21EA 2001112600006 20011126 00006 2001 11 26 2001UALA02231 4 20011101 A 2565 SQUIB BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN ACTIVATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 SUSPECT LEFT SLIDE AND LEFT SPOILER ACTIVATION SQUIBS ACTIVATED. INITIALLY, THE LEFT HAND OFF WING SPOILER OVERRIDE ACT UATOR SQUIB BLEW. THIS ACTUATOR IS ELECTRICALLY FIRED, WHICH INDICATES THAT THE SYSTEM WAS NOT PROPERLY AND COMPLETELY DISARMED PRIOR TO OPENING THE EMERGENCY ESCAPE HATCH FOR MAINTENANCE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001112600007 20011126 00007 WP 2001 11 26 ARWA20011106 1 20011120 A 5512 SKIN DOUG DC8 DC862 3021970 WP HORIZ STAB CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 1808E 46105 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: RT HORIZONTAL STABILIZER T/E BETWEEN STA 175.000 & STA 190.000 UPPER SK IN WITH INNER CORROSION. REMOVED CORROSION IAW DC8 SRM 51-1-8; FOUND TO BE OUT OF LIMITS IAW DC8 SRM 55-2-0. REMOVED U PPER PLATING; FABRICATED NEW PLATING & HATCHES IAW AS ELEVEN INC DWG AS11308, SHEET 1 & 2. PRIMED AND INSTALLED PARTS I AW DC8 SRM 51-1-8 AND AS ELEVEN INC DWG AS11308. 2 L 7 4 4F 4A25 2001112600008 20011126 00008 WP 2001 11 26 ARWA20011111 1 20011120 A 7810 NOZZLE DOUG DC8 DC862 3021970 WP NR 4 ENGINE CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 1808E 46105 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: NR 4 ENGINE EXHAUST NOZZLE SPLITTER WITH CRACK AT 2 O'CLOCK. REMOVED S PLITTER; FABRICATED NEW SPLITTER IAW DC8 SRM 78-3-2, FIG 8, ITEM C. PRIMED AND INSTALLED IAW DC8 SRM 51-1-8 & 51-1-21. 2 L 7 4 4F 4A25 2001113000059 20011130 00059 WP 2001 11 30 ARWA20011119 1 20011120 A 5320 SUPPORT DOUG DC8 DC85F54 3021926 WP FUSELAGE CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 426FB 45667 UPON INSPECTION THE FOLLOWING WAS FOUND: VERTICAL SUPPORT AT STATION 980 RT SIDE LOWER END CORRODED, WHERE SUPPORT ATTA CHES TO CIRCUMFERENTIAL FRAME. REPAIRED VERTICAL SUPPORT AT STA 980 LT LOWER END IAW DRAWING NR AS 11355. 2 L 7 4 4F RT 4A25 2001113000060 20011130 00060 WP 2001 11 30 ARWA20011120 1 20011120 A 5330 SKIN DOUG DC8 DC85F54 3021926 WP FUSELAGE CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 426FB 45667 AT STATIONS 960 TO 980 PITTING CORROSION AT INNER SIDE OF FUSELAGE SKIN BETWEEN STRINGERS 28R & 25R. REPAIRED FUSELAGE SKIN BETWEEN STATION 980 TO 1020 STR 28 & 25L IAW DRAWING AS 11354. 2 L 7 4 4F RT 4A25 2001113000066 20011130 00066 WP 2001 11 30 ARWA2001118 1 20011120 A 5311 FRAME DOUG DC8 DC85F54 3021926 WP FUSELAGE CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 426FB 45667 UPON INSPECTION THE FOLLOWING WAS FOUND: AT STATION 980 AFT BELLY COMPARTMENT, APPROX S-31 CORROSION AT CIRCUMFERENTIAL . REPAIR STA 980 CIRCUMFERENTIAL APPROX S-31L IAW DRAWING AS 11356. 2 L 7 4 4F RT 4A25 2001112600011 20011126 00011 NM 2001 11 26 AT0100235 1 20011120 A 3397 HARNESS BOEING 717 717200 1383700 NM CABIN LOOSE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 946AT 55009 E-PATH LIGHT INOPERATIVE AT ROW 17. FOUND HARNESS LOOSE. RECONNECTED HARNESS AND RESECURED TO SEAT ASSEMBLY IAW AVIO I NTERIOR CMM 25-24. OPS CHECKED GOOD. 2 L 7 2 4F TR A6WE 2001112600012 20011126 00012 NM 2001 11 26 AWAX200100591 1 20011116 A 5312 6545409245 PRESSURE PANEL BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 PHX - MAJOR REPAIR - C - CRACK FOUND LT WHEEL WELL PRESSURE WEB BS 665, WL 202.6, LBL 32, 3 INCHES LONG. MAINTENANCE TR IMMED OUT DAMAGED AREA, FABRICATED REPAIRED DOUBLERS AND INSTALLED IAW AWA ER 03-5715-01324-TB1. 2 L 7 2 4F RT A16WE 2001112600013 20011126 00013 NM 2001 11 26 AWXA200100593 1 20011112 A 5330 6573742 SKIN BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 PHX - MAJOR REPAIR - C - 9 CRACKS FOUND IN FUSELAGE SKIN .125 INCH LONG ORIGINATING FROM FASTENER HOLES ALONG STR 17L, S TA 390 TO 415 VERIFIED BY HFEC. MAINTENANCE CUT OUT AND REMOVED DAMAGED AREA OF SKIN AND FABRICATED FILLER AND DOUBLER, INSTALLED IAW SRM 53-30-3, FIG 25, PG 88A. 2 L 7 2 4F RT A16WE 2001112600014 20011126 00014 SO 2001 11 26 C2XA01IA403 1 20011121 A 5315 14590141001 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27962 145110 DURING C-CK INSPECTION THE LEFT FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED AND CRACKED. MAINTENANCE REMOVED AND REP LACED THE FLOORBEAM IN ACCORDANCE WITH EMB 145 SRM 51-40-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001112600015 20011126 00015 SO 2001 11 26 C2XA01TY183 1 20011123 A 2612 3601133500 FIRE LOOP EMB 135 EMB135ER 3260203 SO LT ENGINE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16511 3253 3253 145267 TYS DURING A SCHEDULE INSPECTION THE LEFT HAND ENGINE FIRE DETECTION LOOP WAS FOUND TO BE CHAFED BEYOND MANUFACTURES LI MITS. MAINTENANCE REMOVED AND REPLACED THE FIRE DETECTION LOOP IAW EMB135 MM 26-11-01, OPERATIONAL CHECKS WERE SATISFAC TORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001112600016 20011126 00016 SO 2001 11 26 C2XA01TY184 1 20011123 A 5315 14522460009 FLOORBEAM EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16511 145267 TYS DURING A SCHEDULED INSPECTION THE CENTER FLOORBEAM TOP CAP WAS FOUND CORRODED BETWEEN FRAMES 19 AND 22. MAINTENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB135 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED U PON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001112600017 20011126 00017 SO 2001 11 26 C2XA01TY185 1 20011123 A 5313 14526795001 STRINGER EMB 135 EMB135ER 3260203 SO FUSELAGE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16511 145267 TYS DURING A SCHEDULED INSPECTION THE EXTERNAL STRINGER 19L WAS FOUND CHAFED JUST AFT OF HYDRAULIC PUMP. MAINTENANCE A CCOMPLISHED A BLEND OUT REPAIR OF STRINGER 19L IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION 5310-0120 7, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001112600018 20011126 00018 SO 2001 11 26 C2XA01TY186 1 20011123 A 5315 14522460015 FLOORBEAM EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16511 145267 TYS DURING A SCHEDULED INSPECTION THE FORWARD DIGITAL PLATE LOCATED JUST AFT OF THE COCKPIT ENTRANCE DOOR WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE FORWARD DIGITAL PLATE IAW EMB 135 SRM 51-40-02 AND EC 35320-01059, TH E REPAIR WAS FOUND TO BE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001112600020 20011126 00020 NM 2001 11 26 DHL2001724011 1 20011121 A 2510 SEAT BELT BOEING 727 727228 1384083 NM COCKPIT DEFECTIVE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 CAPTAIN`S SEAT BELT DETACHES BY ITSELF ON LEFT SIDE. REMOVED AND REPLACED CAPTAIN'S SEAT BELT ON LEFT SIDE IAW B-M/M 25 -10-41. 2 L 7 3 4F RT A3WE 2001112600021 20011126 00021 NE 2001 11 26 DHL2001742014 2 20011120 A 7520 DUCT BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE OUT OF POSITION A DHLA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 742DH 21290 NR 2 DETECTOR CIRCUIT GROUND ILLUMINATES INTERMITTENTLY DURING FLIGHT. FOUND GEN COOLING DUCT SEALS TORN AND DUCT CONTA CTING FIRE LOOP. REINSTALLED GEN COOLING DUCT AND REPLACED SEALS, OPS GOOD IAW MM 75-21-0 & 26-11-01. 2 L 7 3 4F 4 F A3WE E2EA 2001112600022 20011126 00022 NM 2001 11 26 DHL2001742015 1 20011122 A 2612 FIRE LOOP BOEING 727 727225 1384077 NM NR 2 ENGINE OUT OF POSITION A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 742DH 21290 ENGINE NR 2 DETECTION CIRCUIT GROUND LIGHT INTERMITTENTLY FLICKERS IN FLIGHT. PRESS TO TEST DOES NOT ILLUMINATE LIGHT. REPOSITIONED NR 2 ENGINE FIRE LOOP IAW MM 26-11-01. REMOVED AND REPLACED NR 2 GROUND FAULT LIGHT BULB IAW MM CHAP 33. SYSTEM OP'S CHECKED GOOD. 2 L 7 3 4F A3WE 2001112600023 20011126 00023 NM 2001 11 26 DHL2001743014 1 20011122 A 2612 SENSING ELEMENT BOEING 727 727225 1384077 NM NR 1 ENGINE OUT OF POSITION A DHLA K NONE N FALSE WARNING NR NOT REPORTED 1 SO 01 743DH 22438 NR 1 ENGINE FIRE DETECTOR FAULT GROUND LIGHT IS ILLUMINATED. DEFERRED NR 1 ENGINE FIRE DETECTOR GROUND FAULT LIGHT IAW DHL MEL 26-9 ASSIGNED CONTROL NR 7811 AS PER MXC PLACARD INSTALLED. CLEANED AND REPOSITIONED NR 1 ENG SENSING ELEMENT. OPS CHECKED GOOD, NO LIGHT. 2 L 7 3 4F A3WE 2001112600024 20011126 00024 NM 2001 11 26 DHL2001747008 1 20011120 A 3260 POSITION SWITCH BOEING 727 727224 1384076 NM RT MLG DOOR FAULTY A DHLA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 01 747DH 22253 AFTER GEAR EXTENSION ON APPROACH INTO DAL, RIGHT MAIN GEAR DOOR LIGHT REMAINED ILLUMINATED ON S/O'S AND FORWARD PANEL. CREW EXECUTED MISSED APPROACH, RECYCLED THE GEAR, BUT DOOR OPEN WAS STILL INDICATED. RE-INITIATED THE APPROACH, AND LAN DED IN DAL WITHOUT INCIDENT. REMOVED AND REPLACED RIGHT MLG DOOR POSITION SW PER BMM 32-62-11. SYSTEM OPS CHECKED GOOD . 2 L 7 3 4F A3WE 2001112600025 20011126 00025 NM 2001 11 26 SWAA013141 1 20011119 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 DURING WALKAROUND INSP FOUND FUSELAGE SKIN CRACKED AT BS 540A, STR 10L. REPAIRED SKIN PER SWA RA. 2 L 7 2 4F A16WE 2001112600026 20011126 00026 WP 2001 11 26 DHL2001805025 1 20011120 A 2711 ACTUATOR DOUG DC8 DC873F 302199F WP AILERON TRIM LACK OF LUBE A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 805DH 46125 AILERON TRIM FROZE UP IN FLIGHT FOR ENTIRE FLIGHT AT AND BELOW FREEZING TEMPERATURES. INSPECTED AND LUBED TRIM ACTUATOR S. OPS CHECKED TRIM SYSTEM PER MM 27-10-0 OK. 2 L 7 4 4F RT 4A25 2001112600027 20011126 00027 2001 11 26 SWAA013126 4 20011118 A 2565 D31591475 SLIDE BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001112600028 20011126 00028 NM 2001 11 26 SWAA013130 1 20011118 A 3350 101114 LENS BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 514SW 25153 DURING SCHEDULED C1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2001112600029 20011126 00029 NM 2001 11 26 SWAA013131 1 20011118 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 20R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001112600030 20011126 00030 NM 2001 11 26 SWAA013132 1 20011119 A 5310 6547978 WEB BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 616, RBL 64 AND WL 208. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001112600031 20011126 00031 NM 2001 11 26 SWAA013133 1 20011119 A 5330 589357 WINDOW POST BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 385SW 26600 DURING SCHEDULED 1/4D CHECK, FOUND CAPTIAN'S WINDOW POST CRACKED BETWEEN NR 1 AND NR 2 WINDOWS. REPAIRED WINDOW POST PE R SRM. 2 L 7 2 4F RT A16WE 2001112600032 20011126 00032 NM 2001 11 26 SWAA013134 1 20011119 A 5315 6546804 FLOORBEAM BOEING 737 7373Q8 1384670 NM FWD CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 312, BETWEEN RBL 8 AND LBL 8, WL 208. REPAIRED FLOORBEAM PER S RM. 2 L 7 2 4F RT A16WE 2001112600033 20011126 00033 NM 2001 11 26 SWAA013135 1 20011119 A 5754 6573714 SLAT BOEING 737 7375H4 138449D NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 514SW 25153 DURING SCHEDULED C1 CHECK, FOUND NR 1 L/E SLAT CRACKED 20 INCHES INBD OF ACTUATOR. REPAIRED NR 1 L/E SLAT PER SWA RA.. 2 L 7 2 4F RT A16WE 2001112600034 20011126 00034 NM 2001 11 26 SWAA013137 1 20011118 A 5310 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEBS CRACKED (2 EA) AT BS 178, WL 183, RBL 17.1 AND LBL 17.1. REPAIRED WEBS PERSWA RA. 2 L 7 2 4F RT A16WE 2001112600035 20011126 00035 NM 2001 11 26 SWAA013138 1 20011117 A 5330 6545765 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C PLUS 4, STR 10R. REPAIRED SKIN PER SWA RA. 2 L 7 2 4F RT A16WE 2001112600036 20011126 00036 NM 2001 11 26 SWAA013139 1 20011117 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED(6 EA) BETWEEN BS 727D AND BS 887, STR 19R TO STR 24R. REPAIRED SKIN P ER SRM. 2 L 7 2 4F RT A16WE 2001112600037 20011126 00037 NM 2001 11 26 SWAA013140 1 20011116 A 5330 6545765 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED(2 EA) AT BS 752 AND BS 763, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001123100044 20011231 00044 2001 12 31 GLBA2001231 4 20011119 A 2562 ELT1104 ELT BEECH 1900 1900D 1154162 CE CABIN FAULTY A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 150GL 2567 10 UE150 ELT WILL NOT SILENCE. REPLACED ELT, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001112600038 20011126 00038 NM 2001 11 26 HNAA0100075 1 20011119 A 2923 PUMP DHAV DHC8 DHC8102 2809003 NM NR 1 ENGINE MALFUNCTIONED A HNAA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 EA 07 917HA 075 DURING SINGLE ENGINE TAXI, NR 2 AC GENERATOR ON LINE, NR 1 STANDBY HYDRAULIC PUMP FAILED CAUSING LOSS OF NR 1 HYDRAULIC PRESSURE. RECYCLED NR 2 AC GENERATOR, NR 1 STANDBY HYDRAULIC PUMP RETURNED TO NORMAL. INSPECTED BRAKES AND HYDRAULIC S YSTEM, NO LEAKS NOTED. STARTED AND TAXIED AIRCRAFT AROUND AIRPORT, COULD NOT DUPLICATE. 2 H 7 2 4T RT A13NM 2001112600039 20011126 00039 WP 2001 11 26 MWEA011448 1 20011120 A 5320 5910130394N1 STIFFENER DOUG DC9 DC915 3022036 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 POSSIBLE CRACK INDICATION ON AFT PRESSURE BULKHEAD TEE JUST ABOVE LONGERON 18 RIGHT REQUIRES CHEMICAL REMOVAL OF PRIMES FOR FURTHER EVALUATION. REMOVED, FIT, DRILLED AND INSTALLED TEE SECTION. 2 L 7 2 4F A6WE 2001112600040 20011126 00040 WP 2001 11 26 MWEA011453 1 20011120 A 5753 39176601 FITTING DOUG DC9 DC915 3022036 WP T/E FLAP CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 LEFT HAND INBOARD FLAP FITTING IS CRACKED AND BENT. REMOVED, LOCATED, DRILLED AND INSTALLED LEFT HAND INBOARD FLAP FITT ING. 2 L 7 2 4F A6WE 2001112600041 20011126 00041 WP 2001 11 26 MWEA011455 1 20011120 A 5753 995800139 STIFFENER DOUG DC9 DC915 3022036 WP T/E FLAP CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 LEFT HAND INBOARD FLAP STIFFENER P/N 9958001-39 IS CRACKED. REMOVED, FABRICATED AND INSTALLED NEW STIFFENER. 2 L 7 2 4F A6WE 2001112600042 20011126 00042 EU 2001 11 26 QXEA0101809 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RT OUTBOARD SEAT TRACK HAS PITTING ON OUTBOARD FLANGE AT APPROXIMATELY STATION 387-398. REPAIRED IAW FOKKER SRM 5 1-10-4, PAGE 9-B2. 2 L 7 2 4F RT A20EU 2001112600043 20011126 00043 EU 2001 11 26 QXEA0101810 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RT INBOARD SEAT TRACK HAS PITTING ON INBOARD FLANGE AT APPROXIMATELY STATION 256-272. REPAIRED IAW FOKKER SRM 51- 10-4, PAGE 9-B2. 2 L 7 2 4F RT A20EU 2001112600044 20011126 00044 EU 2001 11 26 QXEA0101811 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RT INBOARD SEAT TRACK HAS PITTING ON INBOARD FLANGE AT APPROXIMATELY STATION 193-200. REPAIRED IAW FOKKER SRM 51- 10-4, PAGE 9-B2. 2 L 7 2 4F RT A20EU 2001112600045 20011126 00045 EU 2001 11 26 QXEA0101812 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RT INBOARD SEAT TRACK HAS PITTING CORROSION ON INBOARD AND OUTBOARD FLANGES AT APPROXIMATELY STATION 202-256. REP AIRED IAW FOKKER SRM 51-10-4 PAGE 9-B2. 2 L 7 2 4F RT A20EU 2001112600046 20011126 00046 EU 2001 11 26 QXEA0101813 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RT INBOARD SEAT TRACK HAS LIGHT CORROSION ON TOP OF RAIL AT APPROXIMATELY STATION 180.5 TO 187. REPAIRED IAW FOKK ER SRM 51-10-4, PAGE 9-B2. 2 L 7 2 4F RT A20EU 2001112600047 20011126 00047 EU 2001 11 26 QXEA0101814 1 20011112 A 5320 RIVET FOKKER F28 F28MK4000 4990810 EU ATTACH ANGLE MISSING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - ATTACH ANGLES MISSING RIVETS ABOVE RT FIXED WINDOW, FRAME STATION 4050 AND STRINGER 45. REPAIRED IAW FOKKER MM 51 -31-01. 2 L 7 2 4F RT A20EU 2001112600048 20011126 00048 EU 2001 11 26 QXEA0101815 1 20011112 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - POSSIBLE CRACK IN CASTELLATION ADJACENT TO DIMPLE AT LOWER RIVET IN FRAME 17565, ABOVE STRINGER 19. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001112600049 20011126 00049 EU 2001 11 26 QXEA0101816 1 20011113 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CASTELLATION CRACKED BEYOND 1ST STOP DRILL ON FRAME 17565 ABOVE STRINGER 14. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001112600050 20011126 00050 EU 2001 11 26 QXEA0101817 1 20011113 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CASTELLATION WORKING POSSIBLY CRACKED WITH LOOSE RIVETS ON FRAME 17565 BETWEEN STRINGERS 9 AND 10. REPAIRED IAW F OKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001112600051 20011126 00051 EU 2001 11 26 QXEA0101818 1 20011112 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CASTELLATION CRACKED AT JOGGLE FOR LOWER RIVET ON FRAME 17565 ABOVE STRINGER 50. REPAIRED IAW FOKKER SRM 53-10-05 , PP 601A AND SRM 53-02-13, PAGE 5. 2 L 7 2 4F RT A20EU 2001112600052 20011126 00052 EU 2001 11 26 QXEA0101819 1 20011112 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - EMPENNAGE SKIN GOUGED FROM INSIDE, FORWARD OF OBLIQUE FRAME 58.5-2, ABOVE STRINGER 9, APPROXIMATELY .2 INCHES LONG , .050 INCH WIDE, .040 INCH DEEP. REPAIRED IAW FOKKER SRM 53-02-01, PAGE 3. 2 L 7 2 4F RT A20EU 2001112600053 20011126 00053 EU 2001 11 26 QXEA0101820 1 20011111 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CASTELLATION CRACKED IN RADIUS LOWER END OF FRAME 32-2, FORWARD SIDE ABOVE STRINGER 23. REPAIRED IAW FOKKER MM 53 -10-05, PAGE 610-601A. 2 L 7 2 4F RT A20EU 2001112600054 20011126 00054 EU 2001 11 26 QXEA0101821 1 20011112 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CASTELLATION CRACKED PAST PREVIOUS STOP DRILL ON AFT SIDE OF FRAME 16-2, ABOVE STRINGER 29. REPAIRED IAW FOKKER S RM 53-10-05, PAGE 601-601A AND FOKKER MM 51-31-01. 2 L 7 2 4F RT A20EU 2001112600055 20011126 00055 EU 2001 11 26 QXEA0101822 1 20011112 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CASTELLATION CRACKED AT LOWER RIVET ON FORWARD SIDE OF FRAME 50-2, ABOVE STRINGER 25. REPAIRED IAW FOKKER SRM 51- 10-4, SRM 53-02-13, PAGE 5 AND SRM 53-10-05. 2 L 7 2 4F RT A20EU 2001112600056 20011126 00056 EU 2001 11 26 QXEA0101823 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT INBOARD SEAT TRACK HAS LIGHT PITTING CORROSION ON OUTBOARD FLANGE AT APPROXIMATELY STATION 684-695. REPAIRED I AW FOKKER SRM 51-10-4, PARAGRAPH 4B(2). 2 L 7 2 4F RT A20EU 2001112600057 20011126 00057 EU 2001 11 26 QXEA0101824 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT INBOARD SEAT TRACK HAS LIGHT PITTING CORROSION ON INBOARD FLANGE AT APPROXIMATELY STATION 561-563. REPAIRED IA W FOKKER SRM 51-10-4, PARAGRAPH 4B(2). 2 L 7 2 4F RT A20EU 2001112600058 20011126 00058 EU 2001 11 26 QXEA0101825 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT INBOARD SEAT TRACK HAS LIGHT PITTING CORROSION IN BOTTOM OF CHANNEL AT APPROXIMATELY STATION 559-562. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4B(2). 2 L 7 2 4F RT A20EU 2001112600059 20011126 00059 EU 2001 11 26 QXEA0101826 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT INBOARD SEAT TRACK HAS SEVERAL GOUGES IN TOP OF RAIL THE DEEPEST APPROXIMATELY .003 INCH AT APPROXIMATELY STATI ON 510-512. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4B(2). 2 L 7 2 4F RT A20EU 2001112600060 20011126 00060 EU 2001 11 26 QXEA0101827 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT INBOARD SEAT TRACK HAS LIGHT PITTING CORROSION ON OUTBOARD FLANGE AT APPROXIMATELY STATION 510-520. REPAIRED I AW FOKKER MM 53-40-01, PAGE 205, FIGURE 204 AND SRM 51-10-4, PARAGRAPH 4B(2). 2 L 7 2 4F RT A20EU 2001112600061 20011126 00061 EU 2001 11 26 QXEA0101828 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT INBOARD SEAT TRACK HAS LIGHT PITTING ON OUTBOARD FLANGE AT APPROXIMATELY STATION 475-478. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4B(2). 2 L 7 2 4F RT A20EU 2001112600062 20011126 00062 EU 2001 11 26 QXEA0101829 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT INBOARD SEAT TRACK HAS LIGHT PITTING CORROSION ON INBOARD FLANGE AT APPROXIMATELY STATION 376-425. REPAIRED IA W FOKKER SRM 51-10-4, PARAGRAPH 4B(2). 2 L 7 2 4F RT A20EU 2001112600063 20011126 00063 EU 2001 11 26 QXEA0101830 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT INBOARD SEAT TRACK HAS SLIGHT DAMAGE TO HOLE EDGE AT APPROXIMATELY STATION 370-371. REPAIRED IAW FOKKER SRM 51 -10-4, PARAGRAPH 4B(2). 2 L 7 2 4F RT A20EU 2001112600064 20011126 00064 EU 2001 11 26 QXEA0101831 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT INBOARD SEAT TRACK HAS LIGHT PITTING CORROSION IN BOTTOM OF CHANNEL AT APPROXIMATELY STATION 357-359. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4B(2). 2 L 7 2 4F RT A20EU 2001112600065 20011126 00065 EU 2001 11 26 QXEA0101832 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT INBOARD SEAT TRACK HAS LIGHT PITTING CORROSION ON OUTBOARD FLANGE AT APPROXIMATELY STATION 347-357. REPAIRED I AW FOKKER SRM 51-10-4, PARAGRAPH 4B(2). 2 L 7 2 4F RT A20EU 2001112600066 20011126 00066 EU 2001 11 26 QXEA0101833 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT INBOARD SEAT TRACK HAS LIGHT PITTING CORROSION AT APPROXIMATELY STATION 331-333 ON INBOARD FLANGE. REPAIRED IA W FOKKER SRM 51-10-4, PARAGRAPH 1B(2). 2 L 7 2 4F RT A20EU 2001112600067 20011126 00067 EU 2001 11 26 QXEA0101834 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT INBOARD SEAT TRACK HAS LIGHT PITTING CORROSION ON INBOARD FLANGE AT APPROXIMATELY STATION 327 TO 330. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4B(2). 2 L 7 2 4F RT A20EU 2001112600068 20011126 00068 EU 2001 11 26 QXEA0101835 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT INBOARD SEAT TRACK HAS LIGHT PITTING CORROSION INBOARD FLANGE AT APPROXIMATELY STATION 306. REPAIRED IAW FOKKE R SRM 51-10-4, PARAGRAPH 4B(2). 2 L 7 2 4F RT A20EU 2001112600069 20011126 00069 EU 2001 11 26 QXEA0101836 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT INBOARD SEAT TRACK HAS WORN AREA FRONT TOP EDGE OF RAIL AT APPROXIMATELY STATION 254. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4B(2). 2 L 7 2 4F RT A20EU 2001112600070 20011126 00070 EU 2001 11 26 QXEA0101837 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT INBOARD SEAT TRACK HAS LIGHT PITTING CORROSION ON INBOARD FLANGE AT APPROXIMATELY STATION 248-249. REPAIRED IA W FOKKER SRM 51-10-4, PARAGRAPH 4B(2). 2 L 7 2 4F RT A20EU 2001112600071 20011126 00071 EU 2001 11 26 QXEA0101838 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT INBOARD SEAT TRACK HAS LIGHT PITTING CORROSION AT APPROXIMATELY STATION 228 TO 242, BOTTOM OF CHANNEL. REPAIRE D IAW FOKKER SRM 51-10-4, PARAGRAPH 4B(2). 2 L 7 2 4F RT A20EU 2001112600072 20011126 00072 EU 2001 11 26 QXEA0101839 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT INBOARD SEAT TRACK HAS LIGHT PITTING CORROSION BOTTOM OF CHANNEL AT APPROXIMATELY STATION 223 TO 225. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4B(2). 2 L 7 2 4F RT A20EU 2001112600073 20011126 00073 EU 2001 11 26 QXEA0101840 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT OUTBOARD SEAT TRACK HAS A SCRATCH ON TOP OF RAIL AT APPROXIMATELY STATION 491. REPAIRED IAW FOKKER SRM 51-10-4 , PARAGRAPH 4B(2). 2 L 7 2 4F RT A20EU 2001112600074 20011126 00074 EU 2001 11 26 QXEA0101841 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT OUTBOARD SEAT TRACK HAS A GOUGE ON TOP OF TRACK AT APPROXIMATELY STATION 673.5. REPAIRED IAW FOKKER SRM 51-10- 4, PARAGRAPH 4B(2). 2 L 7 2 4F RT A20EU 2001112600075 20011126 00075 EU 2001 11 26 QXEA0101842 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT OUTBOARD SEAT TRACK HAS SEVERAL GOUGES ON TOP OF RAIL AT APPROXIMATELY STATION 677 TO 683. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4B(2). 2 L 7 2 4F RT A20EU 2001112600076 20011126 00076 EU 2001 11 26 QXEA0101843 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT OUTBOARD SEAT TRACK HAS LIGHT PITTING CORROSION ON OUTBOARD FLANGE AT APPROXIMATELY STATION 331 TO 335. REPAIR ED IAW FOKKER SRM 51-10-4, PARAGRAPH 4B(2). 2 L 7 2 4F RT A20EU 2001112600077 20011126 00077 EU 2001 11 26 QXEA0101844 1 20011105 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - BELLY SKIN CHAFED FROM CONTACT WITH PANEL 91BD ALONG FUSELAGE BETWEEN FRAMES 14755 AND 15205 AND STRINGER 67 AND 6 8. REPAIRED IAW FOKKER SRM 51-10-01, PAGE 9, ITEM 60, SRM 51-10-4, PAGE 9 4B AND SRM 51-10-9, PAGE 8 3C. 2 L 7 2 4F RT A20EU 2001112600078 20011126 00078 EU 2001 11 26 QXEA0101845 1 20011105 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FUSELAGE BELLY SKIN CHAFED FROM LOWER EDGE OF PANEL 92BD ON RT FUSELAGE BETWEEN FRAMES 14755 AND 15205 AND STRINGE R 67 AND 68. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5, SRM 53-23-01, PAGE 9, ITEM 51, SRM 51-10-4, PAGE 9 AND SRM 51-10 -4, PAGE 8-3C. 2 L 7 2 4F RT A20EU 2001112600079 20011126 00079 EU 2001 11 26 QXEA0101846 1 20011105 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FUSELAGE BELLY SKIN CHAFED FROM PANEL 92BD, RT FUSELAGE BETWEEN FRAMES 15205 AND 15635 AND STRINGER 66 AND 65. RE PAIRED IAW FOKKER SRM 53-01-01, PAGE 5F, SRM 53-23-01, PAGE 9, ITEM 51, SRM 51-10-4, PAGE 94B AND SRM 51-10-4, PAGE 8-3C . 2 L 7 2 4F RT A20EU 2001112600080 20011126 00080 EU 2001 11 26 QXEA0101847 1 20011112 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME CLIP CRACKED AT STRINGER 47 AND FRAME 16060. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001112600081 20011126 00081 EU 2001 11 26 QXEA0101848 1 20011109 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT OUTBOARD SEAT TRACK HAS WORN AREA AT BOTTOM OF GROOVE APPROXIMATELY STATION 192. REPAIRED IAW FOKKER SRM 51-10 -4, PARAGRAPH 4B(2). 2 L 7 2 4F RT A20EU 2001112600082 20011126 00082 EU 2001 11 26 QXEA0101849 1 20011109 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT WING FUEL ACCESS PANEL 73C MATING FLANGE ON WING SHOWS LIGHT FRETTING CORROSION. REPAIRED IAW FOKKER SRM 51-30 -03, PAGES 703-704, PARAGRAPH 3-C, STEPS 1-10. 2 L 7 2 4F RT A20EU 2001112600084 20011126 00084 EU 2001 11 26 QXEA0101851 1 20011109 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT WING FUEL ACCESS PANEL 73A, MATING FLANGE ON WING SHOWS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 51-30-03, PAGES 703 AND 704, PARAGRAPH 3-C, STEPS 1 THRU 10. 2 L 7 2 4F RT A20EU 2001112600085 20011126 00085 EU 2001 11 26 QXEA0101852 1 20011107 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT WING FUEL ACCESS PANEL 71A, MATING FLANGE ON WING SHOWS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 51-30-03, PAGE 703, PARAGRAPH 3 A-C. 2 L 7 2 4F RT A20EU 2001112600086 20011126 00086 EU 2001 11 26 QXEA0101853 1 20011107 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRETTING CORROSION PRESENT ON LT WING FUEL PANEL 73C FLANGE. REPAIRED IAW FOKKER SRM 57-01-01 AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 2001112600087 20011126 00087 EU 2001 11 26 QXEA0101854 1 20011107 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRETTING CORROSION PRESENT ON LT WING FUEL PANEL 73B FLANGE. REPAIRED IAW FOKKER SRM 57-01-01 AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 2001112600088 20011126 00088 EU 2001 11 26 QXEA0101855 1 20011107 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRETTING CORROSION PRESENT ON LT WING FUEL PANEL 73A FLANGE. REPAIRED IAW FOKKER SRM 57-01-01, PARAGRAPH 4 AND SR M 51-10-4. 2 L 7 2 4F RT A20EU 2001112600089 20011126 00089 EU 2001 11 26 QXEA0101856 1 20011107 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRETTING CORROSION PRESENT ON LT WING FUEL PANEL 71A FLANGE. REPAIRED IAW FOKKER SRM 57-01-01, PARAGRAPH 4 AND SR M 51-10-4. 2 L 7 2 4F RT A20EU 2001112600090 20011126 00090 EU 2001 11 26 QXEA0101857 1 20011113 A 5220 SKIN FOKKER F28 F28MK4000 4990810 EU EMERGENCY EXIT CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RT AFT EMERGENCY EXIT DOOR IS CRACKED IN RADUIS ON OUTER SKIN. REPAIRED IAW FOKKER SRM 52-02-03, FIGURE 3, 2 L 7 2 4F RT A20EU 2001112600091 20011126 00091 EU 2001 11 26 QXEA0101858 1 20011107 A 5330 DOUBLER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - DOUBLER FORWARD OF FRAME 16660 BETWEEN STRINGER 1 AND 74 CORRODED. REPAIRED IAW FOKKER SRM 52-01-01, PAGE 6 AND S RM 51-10-4. 2 L 7 2 4F RT A20EU 2001112600092 20011126 00092 EU 2001 11 26 QXEA0101860 1 20011106 A 5541 RIB FOKKER F28 F28MK4000 4990810 EU RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RUDDER STRUCTURE RIB NR 4 IS CRACKED BETWEEN RIVETS. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001112600093 20011126 00093 EU 2001 11 26 QXEA0101861 1 20011106 A 5541 RIB FOKKER F28 F28MK4000 4990810 EU RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RUDDER STRUCTURE RIB NR 5 IS CRACKED BETWEEN RIVETS. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001112600094 20011126 00094 EU 2001 11 26 QXEA0101862 1 20011110 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AFT CARGO BAY FRAME 16060 HAS CORROSION ON TOP SURFACE OF LOWER FLANGE ON FORWARD SIDE BETWEEN STRINGER 1 AND 74. REPAIRED IAW FOKKER SRM 51-10-01 AND SRM 51-10-04. 2 L 7 2 4F RT A20EU 2001112600095 20011126 00095 WP 2001 11 26 IXXA0100074O 1 20011122 A 2121 FAN DOUG DC8 DC862 3021970 WP FWD BELLY DEFECTIVE A IXXA O OTHER O OTHER CR CRUISE 1 SW 11 728PL 80916 4521 45918 ENROUTE FROM KWA TO HIK, THE FLIGHT CREW SENSED AN ODOR IN THE COCKPIT AND THE AFT PASSENGER COMPARTMENT WHEN THE RIGHT RECIRCULATION FAN WAS OPERATING. THE FLIGHT CREW SECURED THE FAN AND THE ODOR SUBSIDED. THE FLIGHT CONTINUED TO HIK FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE FAN WHICH WAS FOUND DEFECTIVE. MAINTENANCE PLACED THE FAN ON DEFERRAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2001112600096 20011126 00096 NM 2001 11 26 SWAA013143 1 20011119 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT BULL NOSE LIGHT LOOSE AT ROW NR 3 ABC. SECURED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001112600097 20011126 00097 NM 2001 11 26 SWAA013146 1 20011120 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 091SW 22963 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 2.5 INCHES LONG AT BS 791, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001112600098 20011126 00098 NM 2001 11 26 SWAA013147 1 20011117 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 15L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001112600099 20011126 00099 NM 2001 11 26 SWAA013149 1 20011119 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR AT UPPER HINGE CUT OUT. REPAIRED SKIN PER SR M. 2 L 7 2 4F RT A16WE 2001112600100 20011126 00100 NM 2001 11 26 SWAA013150 1 20011119 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED 1.5 INCHES AT BS 500, STR 10L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001112600101 20011126 00101 NM 2001 11 26 SWAA013151 1 20011120 A 5754 6573714 SLAT BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED C4 CHECK, FOUND NR 2 L/E SLAT CRACKED(3 EA), 38 INCHES FROM OTBD END. REPAIRED NR 2 L/E SLAT PER SRM. 2 L 7 2 4F RT A16WE 2001112600102 20011126 00102 NM 2001 11 26 SWAA013152 1 20011120 A 5754 6573714 SLAT BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED C4 CHECK, FOUND NR 1 L/E SLAT CRACKED (3 EA), 45 INCHES FROM INBD END. REPAIRED NR 1 L/E SLAT PER SWA RA. 2 L 7 2 4F RT A16WE 2001112600103 20011126 00103 NM 2001 11 26 SWAA013153 1 20011120 A 5753 6546434 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED C4 CHECK, FOUND LT INBD AFT T/E FLAP DELAMINATED ON LOWER SKIN. REMOVED AND REPLACED T/E FLAP PER MM. 2 L 7 2 4F RT A16WE 2001112600104 20011126 00104 NM 2001 11 26 SWAA013154 1 20011120 A 5330 6545769 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED .4 INCH AT BS 510, BETWEEN STR 27L AND 28L. REPAIRED SKIN PER SW A RA. 2 L 7 2 4F RT A16WE 2001112600105 20011126 00105 NM 2001 11 26 SWAA013155 1 20011120 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING WALK AROUND ON SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 328, STR 21R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001112600106 20011126 00106 EU 2001 11 26 QXEA0101863 1 20011105 A 7120 SUPPORT FOKKER F28 F28MK4000 4990810 EU RT ENGINE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FORWARD ENGINE SUPPORT BEAM SHACKLES HAVE SURFACE CORROSION AT RT STUBWING. REPAIRED IAW IPC 71-20-01, FIGURE 1, ITEM 15 AND 4313-1B, CHAPTER 6, PARAGRAPH 165. 2 L 7 2 4F RT A20EU 2001112600107 20011126 00107 EU 2001 11 26 QXEA0101864 1 20011105 A 7120 BOLT FOKKER F28 F28MK4000 4990810 EU ENGINE MOUNT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FORWARD ENGINE MOUNT BEAR ATTACH BOLTS AND NUTS HAVE SURFACE CORROSION ON RT STUB WING. REPAIRED IAW REF:43-13-1B , CHAPTER 6, PARAGRAPH 165. 2 L 7 2 4F RT A20EU 2001112600108 20011126 00108 EU 2001 11 26 QXEA0101865 1 20011105 A 5410 FITTING FOKKER F28 F28MK4000 4990810 EU NR 2 NACELLE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - NR 2 NACELLE AFT MOUNT BEAM AT ENGINE CHATTER PROOF BOLT END HAS SURFACE CORROSION ON FORWARD LUG. REPAIRED IAW F OKKER SRM 51-01-04. 2 L 7 2 4F RT A20EU 2001112600109 20011126 00109 EU 2001 11 26 QXEA0101866 1 20011111 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AFT CARGO BAY FRAME 15205 CASTELLATION TIE-IN TO BELLY SKIN HAS CORROSION ON TOP SURFACE AT STRINGER 3. REPAIRED IAW FOKKER SRM 53-01-01 AND SRM 51-10-04. 2 L 7 2 4F RT A20EU 2001112600110 20011126 00110 EU 2001 11 26 QXEA0101867 1 20011108 A 5320 STRINGER CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 13815B AND STRINGER 45 CLIP CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 2001112600111 20011126 00111 SO 2001 11 26 COMA0110158 1 20011125 A 5320 12003041001 RIB EMB 120 EMB120RT 3260202 SO COCKPIT OVERHEAD CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 269CA 22839 120263 DURING A SERVICE CHECK, MECHANIC NOTICED A CRACK LOCATED AT THE COCKPIT OVERHEAD CREW ASSIST HANDLE MOUNT ON LEFT SIDE.D AMAGE WAS REMOVED FROM THE RIB. A FILLER AND A DOUBLER WAS FABRICATED AND INSTALLED. WORK WAS ACCOMPLISHED IN ACCORDANC E WITH AERODESIGN REPORT #3641-1, REV B, 11-24-01. 2 L 7 2 4T RT A31SO 2001112600112 20011126 00112 EU 2001 11 26 QXEA0101868 1 20011112 A 5320 STRINGER CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 13815B AND STRINGER 47 CLIP CRACKED. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001112600113 20011126 00113 EU 2001 11 26 QXEA0101869 1 20011108 A 5320 STRINGER CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 13815B AND STRINGER 41 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 2001112600114 20011126 00114 EU 2001 11 26 QXEA0101870 1 20011108 A 5320 STRINGER CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 13815B AND STRINGER 40 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 2001112600115 20011126 00115 EU 2001 11 26 QXEA0101871 1 20011108 A 5320 STRINGER CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 13815B AND STRINGER 32 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 2001112600116 20011126 00116 EU 2001 11 26 QXEA0101872 1 20011112 A 5320 STRINGER CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 14285 AND STRINGER 47 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001112600117 20011126 00117 EU 2001 11 26 QXEA0101873 1 20011112 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 15205 AND STRINGER 52 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001112600118 20011126 00118 EU 2001 11 26 QXEA0101874 1 20011112 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 15205 AND STRINGER 53 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 9 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001112600119 20011126 00119 EU 2001 11 26 QXEA0101875 1 20011112 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 15205 AND STRINGER 21 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 9 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001112600120 20011126 00120 EU 2001 11 26 QXEA0101876 1 20011112 A 5330 RIVET FOKKER F28 F28MK4000 4990810 EU FUSELAGE LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FUSELAGE SKIN TO FRAME 13815A RIVET IS LOOSE AND DOES NOT FILL THE COUNTERSINK. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001112600121 20011126 00121 EU 2001 11 26 QXEA0101877 1 20011108 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FUSELAGE BELLY FAIRING FRAME CLIP IS CRACKED AT FRAME 13815B AT THE 6 O'CLOCK POSITION. REPAIRED IAW FOKKER SRM 5 1-31-01. 2 L 7 2 4F RT A20EU 2001112600122 20011126 00122 EU 2001 11 26 QXEA0101878 1 20011108 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AFT CARGO BAY FRAME 13815B CASTELLATION TIE IN TO BELLY SKIN IS CRACKED AT STRINGER NR 2. REPAIRED IAW FOKKER SRM 53-02-11, FIGURE 1, PAGE 2. 2 L 7 2 4F RT A20EU 2001112600123 20011126 00123 EU 2001 11 26 QXEA0101879 1 20011108 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AFT CARGO BAY FRAME 13815B CASTELLATION TIE IN TO BELLY SKIN IS CRACKED AT STRINGER 73. REPAIRED IAW FOKKER SRM 5 3-02-11, FIGURE 1, PAGE 2. 2 L 7 2 4F RT A20EU 2001112600124 20011126 00124 EU 2001 11 26 QXEA0101880 1 20011112 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 13345 AND STRINGER 36 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001112600125 20011126 00125 EU 2001 11 26 QXEA0101881 1 20011112 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 13345 AND STRINGER 28 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001112600126 20011126 00126 EU 2001 11 26 QXEA0101882 1 20011112 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 13815A AND STRINGER 31 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001112600127 20011126 00127 EU 2001 11 26 QXEA0101883 1 20011112 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 13815A AND STRINGER 41 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001112600128 20011126 00128 EU 2001 11 26 QXEA0101884 1 20011112 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 13815A AND STRINGER 46 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001112600129 20011126 00129 EU 2001 11 26 QXEA0101885 1 20011106 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AFT CARGO BAY INTERIOR BELLY SKIN HAS CORROSION 1 INCH INBOARD OF STRINGER 73 EXTENDING UNDER FRAME 13815A CASTELL ATION TIE-IN AT AFT SIDE OF FRAME. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6 AND SRM 51-10-04, PAGE 4. 2 L 7 2 4F RT A20EU 2001112600130 20011126 00130 EU 2001 11 26 QXEA0101886 1 20011106 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AFT CARGO BAY FRAME 13815A CASTELLATION TIE-IN TO BELLY SKIN BETWEEN STRINGER 73 AND 74 HAS CORROSION ON TOP SIDE. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6 AND SRM 51-10-04, PAGE 4. 2 L 7 2 4F RT A20EU 2001112600131 20011126 00131 EU 2001 11 26 QXEA0101887 1 20011108 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 10346 AND STRINGER 32 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 2001112600132 20011126 00132 WP 2001 11 26 MWEA011456 1 20011126 A 5210 5934796523 BEAM DOUG DC9 DC915 3022036 WP DOOR BEAM #7 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 MAIN CABIN DOOR BEAM NUMBER 7 HAS A CRACK ON AFT END -- STOP DRILLED CRACK. DRILLED UP NEW -53 DOUBLER. INSTALLED DOUB LER, FITTING AND DOOR STOP. 2 L 7 2 4F A6WE 2001112600133 20011126 00133 WP 2001 11 26 MWEA011457 1 20011126 A 5310 59114123 SKIN DOUG DC9 DC915 3022036 WP F.S 370 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 SKIN CORRODED AT SHEAR TIE BETWEEN LONGERON 30 AND LONGERON 29 RIGHT AT FUSELAGE STATION 370 -- FABRICATED AND INSTAL LED REPAIR DOUBLERS: INTERNAL FINGER DOUBLER, INTERNAL STRAP DOUBLER, FILLER PLUG, EXTERNAL DOUBLER AND SHIM. 2 L 7 2 4F A6WE 2001112600134 20011126 00134 WP 2001 11 26 MWEA011458 1 20011126 A 5310 9957909508 INTERCOSTAL DOUG DC9 DC915 3022036 WP STA. 370-377.5 ELONGATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 INTERCOSTAL FROM STATION 370-377.5, LONGERON 29 RIGHT HAS DOUBLE-DRILLED HOLE AT STATION 377.5 -- REMOVED, FABRICATED AND INSTALLED "T" FITTING AND INTERCOSTAL. 2 L 7 2 4F A6WE 2001112600135 20011126 00135 EU 2001 11 26 QXEA0101888 1 20011108 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 10966 AND STRINGER 43 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 2001112600136 20011126 00136 EU 2001 11 26 QXEA0101889 1 20011108 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 10966 AND STRINGER 44 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 2001112600137 20011126 00137 EA 2001 11 26 COMA0160916 1 20011123 A 5330 NA SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DENTED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 951CA 14153 7091 THE FUSELAGE SKIN WAS DAMAGED BY GROUND EQUIPMENT BETWEEN FS625 AND 640 AND BETWEEN STRINGERS 21L AND 22L.REPAIRED FUSEL AGE SKIN I/A/W WVAC EO 601R-53-2853. 2 L 7 2 4F RT A21EA 2001112600138 20011126 00138 WP 2001 11 26 ABXA010590 1 20010827 A 5340 3887799 FITTING DOUG DC8 DC861 3021952 WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 848AX 46032 MAIN CABIN, STATION 450 AND LONGERON 14 RIGHT, LONGERON TIE FITTING WAS CRACKED. INSTALLED NEW FITTING AND REPAIRED AREA IAW DC-8 SRM 51-1-20D, 51-1-8, AND DAC DWG #3887799. 2 L 7 4 4F 4A25 2001112600139 20011126 00139 WP 2001 11 26 ABXA010591 1 20010827 A 5340 37797621 FITTING DOUG DC8 DC861 3021952 WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 848AX 46032 MAIN CABIN, STATION 678 AND LONGERON 7 RIGHT, LONGERON TIE FITTING WAS CRACKED. INSTALLED NEW FITTING AND REPAIRED AREA IAW DC-8 SRM 51-1-20D AND 51-1-23. 2 L 7 4 4F 4A25 2001112600140 20011126 00140 WP 2001 11 26 ABXA010592 1 20010827 A 5340 37797621 FITTING DOUG DC8 DC861 3021952 WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 848AX 46032 MAIN CABIN, STATION 682 AND LONGERON 5 RIGHT, LONGERON TIE FITTING WAS CRACKED. INSTALLED NEW FITTING AND REPAIRED AREA IAW DC-8 SRM 51-1-24, 51-1-20D AND 51-1-23. 2 L 7 4 4F 4A25 2001112600141 20011126 00141 WP 2001 11 26 ABXA010593 1 20010827 A 5340 37797621 FITTING DOUG DC8 DC861 3021952 WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 848AX 46032 MAIN CABIN, STATION 682 AND LONGERON 10 RIGHT, LONGERON TIE FITTING WAS CRACKED. INSTALLED NEW FITTING AND REPAIRED AREA IAW DC-8 SRM 51-1-20D AND 51-1-23. 2 L 7 4 4F 4A25 2001112600142 20011126 00142 WP 2001 11 26 ABXA010594 1 20010906 A 5340 FITTING DOUG DC8 DC861 3021952 WP AFT LWR CARGO MISDRILLED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 848AX 46032 AFT LOWER CARGO FRAME WAS MISDRILLED AT STAION 1140 RIGHT AND LONGERON 30 RIGHT. INSTALLED NEW FILLER AND DOUBLER AND RE PAIRED AREA IAW DC-8 SRM 51-1-8 AND REA D853-40922MR. 2 L 7 4 4F 4A25 2001112600143 20011126 00143 EA 2001 11 26 COMA0160917 1 20011123 A 5330 NA POST CNDAIR CL600 CL6002B19 1900309 EA FS409+128 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 951CA 14153 7091 THE INBOARD LOWER POST AT LBL27 AT FS409+128 IS CRACKED.REPAIRED THE CRACKED LOWER POST I/A/W WVAC 601R-53-2855. 2 L 7 2 4F RT A21EA 2001112600144 20011126 00144 EA 2001 11 26 COMA0160918 1 20011123 A 5320 6003106819 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FS.460@RBL9 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 951CA 14154 7091 FLOOR SUPPORT FITTING AT F.S. 460, RBL9 IS CRACKED.REMOVED DAMAGED FITTING AND INSTALLED NEW FITTING P/N 600-31068-19 I/ A/W WVAC EO 601R-53-2854 AND STANDARD CRJ SRM PRACTICES, REF MAINT LOG PAGE #476347 AND COMAIR W.O. #29882. 2 L 7 2 4F RT A21EA 2001112600145 20011126 00145 EU 2001 11 26 QXEA0101890 1 20011108 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 11405 AND STRINGER 32 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 2001112600146 20011126 00146 EU 2001 11 26 QXEA0101891 1 20011112 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 11405 AND STRINGER 43 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 2001112600147 20011126 00147 EU 2001 11 26 QXEA0101892 1 20011108 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 12405 AND STRINGER 36 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 2001112600148 20011126 00148 EU 2001 11 26 QXEA0101893 1 20011108 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 12405 AND STRINGER 39 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 2001112600149 20011126 00149 EU 2001 11 26 QXEA0101894 1 20011108 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 12405 AND STRINGER 40 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 2001112600150 20011126 00150 EU 2001 11 26 QXEA0101895 1 20011108 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 12405 AND STRINGER 42 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 2001112600151 20011126 00151 EU 2001 11 26 QXEA0101896 1 20011108 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 12405 AND STRINGER 43 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 2001112600152 20011126 00152 EU 2001 11 26 QXEA0101897 1 20011108 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 12875 AND STRINGER 36 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 2001112600153 20011126 00153 NM 2001 11 26 CALA0101008 1 20011121 A 5512 SKIN BOEING 737 7373T0 1384582 NM HOR STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71314 23365 INSPECTION FOUND A 2" CRACK IN L/H HORIZONTAL STABILIZER SKIN FORWARD OF I/B BALANCE PANEL. THE CRACKED AREA WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5510-01608. 2 L 7 2 4F RT A16WE 2001112600154 20011126 00154 NM 2001 11 26 CALA0101009 1 20011123 A 5720 BRACKET BOEING 737 7373T0 1384582 NM #6 FLAP TRK CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17309 23360 INSPECTION FOUND A 1/4" CRACK IN R/H WING #6 FLAP TRACK FAIRING I/B SUPPORT BRACKET. A NEW BRACKET WAS INSTALLED IAW MM 51-10-02. 2 L 7 2 4F RT A16WE 2001112600155 20011126 00155 WP 2001 11 26 CALA0101010 1 20011124 A 5320 WEB DOUG DC9 DC981 3022081 WP STA 1338 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16883 48073 INSPECTION FOUND A 1/2" CRACK IN WEB AT FORWARD FACE OF AFT BULKHEAD STA 1338 BETWEEN LONGERON 25L AND 26L. FILLER AND D OUBLER WERE INSTALLED IAW SRM 51-70-4. 2 L 7 2 4F A6WE 2001112600156 20011126 00156 NM 2001 11 26 CALA0101011 1 20011125 A 5320 ANGLE BOEING 737 7373T0 1384582 NM STA 704 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71314 23365 INSPECTION FOUND FORWARD L-ANGLE SUPPORT FOR SILL WEB CORRODED AT THRESHOLD OF AFT PIT, STA 704, STRINGER 25R. A NEW ANG LE WAS INSTALLED IAW BOEING DRAWING 69-43233 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001112600157 20011126 00157 NM 2001 11 26 CALA0101012 1 20011125 A 5311 FRAME BOEING 737 7373T0 1384582 NM STA 794.3 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71314 23365 INSPECTION FOUND AFT CARGO DOOR CUTOUT FORWARD FRAME CORRODED AT STA 794.3, STRINGER 25R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-70-11, FIGURE 1. 2 L 7 2 4F RT A16WE 2001112600158 20011126 00158 EU 2001 11 26 QXEA0101898 1 20011112 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 12875 AND STRINGER 42 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001112600159 20011126 00159 EA 2001 11 26 COMA0160919 1 20011123 A 5320 60034017373 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FS280, LBL9 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 951CA 14153 7091 THE VERTICAL J ANGLE CLIP LOCATED IN CBP1 AT LBL9 WAS FOUND CRACKED.REMOVED THE CRACKED ANGLE. FABRICATED A NEW ANGLE, H EAT TREATED AND INSTALLED THE REPAIR ANGLE I/A/W WVAC EO 601R-53-2857. 2 L 7 2 4F RT A21EA 2001112600160 20011126 00160 EU 2001 11 26 QXEA0101899 1 20011106 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AFT CARGO BAY FRAME 13815A CASTELLATION TIE-IN TO BELLY SKIN BETWEEN STRINGER 1 AND 2 HAS CORROSION ON TOP SURFACE . REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4B, PAGE 9. 2 L 7 2 4F RT A20EU 2001112600161 20011126 00161 EU 2001 11 26 QXEA0101900 1 20011106 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AFT CARGO BAY FRAME 13815A HAS CORROSION ON TOP OF FRAME UNDER FLOOR SUPPORT 4 WAY TIE-IN AT STRINGER 74. REPAIRE D IAW FOKKER SRM 51-10-04, PARAGRAPH 4B, C, PAGE 9. 2 L 7 2 4F RT A20EU 2001112600162 20011126 00162 EU 2001 11 26 QXEA0101901 1 20011105 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AFT CARGO BAY FRAME 13815A CASTELLATION TIE-IN TO BELLY SKIN IS CRACKED AT STRINGER 73. REPAIRED IAW FOKKER SRM 5 3-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 2001112600163 20011126 00163 EU 2001 11 26 QXEA0101902 1 20011105 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AFT CARGO BAY FRAME 13815A CASTELLATION TIE IN TO BELLY SKIN IS CRACKED AT STRINGER 2. REPAIRED IAW FOKKER SRM 53 -02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 2001112600164 20011126 00164 EU 2001 11 26 QXEA0101903 1 20011106 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AFT CARGO BAY FRAME 13015 CASTELLATION TIE IN TO BELLY SKIN BETWEEN STRINGER 1 AND 74 HAS CORROSION ON TOP SURFACE . REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9 AND SRM 53-01-01, PAGE 6. 2 L 7 2 4F RT A20EU 2001112600165 20011126 00165 EA 2001 11 26 COMA0160920 1 20011124 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FS484 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 951CA 14154 7091 F.S. 484, LBL27 @ W.L. 73.0 INTERCOSTAL CRACKED .5".REPAIRED I/A/W WVAC E/O 601R-53-2856A AND STANDARD CRJ SRM PRACTICES . 2 L 7 2 4F RT A21EA 2001112600166 20011126 00166 EU 2001 11 26 QXEA0101904 1 20011106 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AFT CARGO BAY FRAME 13015 CASTELLATION TIE IN TO BELLY SKIN OUTBOARD OF STRINGER 1 HAS CORROSION ON TOP SURFACE. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4B, C, PAGE 9. 2 L 7 2 4F RT A20EU 2001112600167 20011126 00167 NM 2001 11 26 QXEA0101907 1 20011112 A 5410 MOUNT BRACKET DHAV DHC8 DHC8* NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - LEFT NACELLE FINGER NAIL MOUNTING HOLES AND MOUNTING BRACKET ARE CRACKED. REPAIRED NACELLE DECK AND STIFFENER IAW EA 6-54-31, AND EA 6-54-33. 2 H 7 2 4T RT A13NM 2001112600168 20011126 00168 NM 2001 11 26 QXEA0101908 1 20011112 A 5410 MOUNT BRACKET DHAV DHC8 DHC8* NM RT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - RIGHT NACELLE FINGERNAIL MOUNTING BRACKET STIFFENER AND MOUNTING POINT ARE CRACKED. REPAIRED IAW EA 6-54-32 AND 6 -54-34. 2 H 7 2 4T RT A13NM 2001112600169 20011126 00169 NM 2001 11 26 QXEA0101909 1 20011116 A 5220 HANDLE DHAV DHC8 DHC8* NM EMERGENCY EXIT OBSTRUCTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - AFT LEFT EMERGENCY EXIT DOOR WON'T OPEN FROM INSIDE. REMOVED EXCESS MATERIAL FROM FLAP COVER INTERFACING WITH EXT ERIOR DOOR HANDLE. OPENED AND CLOSED DOOR FROM INSIDE AND OUTSIDE. OPERATIONAL CHECK IS GOOD. 2 H 7 2 4T RT A13NM 2001113000097 20011130 00097 EA 2001 11 30 COMA0160915 1 20011123 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 938CA 16591 7046 LEFT LOWER WING CUTOUT CRACKED AT 540 DB. BLENDED OUT DAMAGE AND ROTOPEENED IAW REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 2001112600170 20011126 00170 NM 2001 11 26 QXEA0101911 1 20011115 A 3350 6050251 BATTERY PACK DHAV DHC8 DHC8* NM CABIN DISCHARGED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 406QX 4048 GEG- FORWARD EMERGENCY EXIT LIGHT POWER SUPPLY HAS WEAK BATTERY PACKS, FAILS TO ILLUMINATE ASSOCIATED LIGHTS. REMOVED A ND REPLACED FORWARD BATTERY PACKS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001112600171 20011126 00171 NM 2001 11 26 QXEA0101912 1 20011116 A 3260 PROXIMITY SWITCH DHAV DHC8 DHC8* NM NLG FAULTY A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 407QX 4049 SEA - NOSE GEAR CYCLED TWICE. LIGHTS CAME ON BOTH TIMES. REMOVED AND REPLACED NOSE GEAR PROXIMITY SENSORS AND RE-RIGGE D IAW TASK 32-61-06830-801. OPERATIONAL CHECK IS GOOD. 2 H 7 2 4T RT A13NM 2001112600172 20011126 00172 EU 2001 11 26 QXEA0101915 1 20011117 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RT INBOARD SEAT TRACK HAS LIGHT CORROSION ON OUTBOARD FLANGE AT APPROXIMATELY STATION 180.5 TO 191. REPAIRED IAW FOKKER SRM 51-31-01, SRM 51-11-4, AND SRM 51-30-02. 2 L 7 2 4F RT A20EU 2001112600173 20011126 00173 EU 2001 11 26 QXEA0101916 1 20011112 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CASTELLATION CRACKED AT LOWER RIVET OF FORWARD SIDE OF FRAME 50-2 ABOVE STRINGER 14. REPAIRED IAW FOKKER SRM 53-1 0-05, PAGE 601-601A AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001112600174 20011126 00174 EU 2001 11 26 QXEA0101917 1 20011118 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CLIP ON CASTELLATION, FRONT SIDE OF FRAME 50-2 IS CHAFING INTO STRINGER 27. REPAIRED IAW FOKKER SRM 53-01-01, PAG E 5, PARAGRAPH 3E AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 2001112600175 20011126 00175 EU 2001 11 26 QXEA0101919 1 20011112 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CASTELLATION CRACKED IN RADIUS AT JOGGLE ON AFT SIDE OF FRAME 32-2 ABOVE STRINGER 29. REPAIRED IAW FOKKER SRM 53- 10-05, PAGE 601-601A AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001112600176 20011126 00176 EU 2001 11 26 QXEA0101920 1 20011112 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CASTELLATION CRACKED AT LOWER RIVET ON FORWARD SIDE OF FRAME 41-2 ABOVE STRINGER 61. REPAIRED IAW FOKKER SRM 51-3 1-01, PAGE 14(E) AND SRM 53-10-05, PAGE 601-601A. 2 L 7 2 4F RT A20EU 2001112600177 20011126 00177 EU 2001 11 26 QXEA0101921 1 20011112 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CASTELLATION CRACKED AT LOWER RIVET ON FORWARD SIDE OF FRAME 50-2 ABOVE STRINGER 61. REPAIRED IAW FOKKER SRM 53-1 0-05, PAGE 601-601A, SRM 51-31-01, PAGE 14(E). 2 L 7 2 4F RT A20EU 2001112600178 20011126 00178 EU 2001 11 26 QXEA0101922 1 20011115 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CASTELLATION AT TOP OF OBLIQUE FRAME 41-2 AT STRINGER 43 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 6, PAGE 8, SRM 51-10-4 AND 53-31-01. 2 L 7 2 4F RT A20EU 2001112600179 20011126 00179 EU 2001 11 26 QXEA0101923 1 20011112 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CASTELLATION CRACKED IN RADIUS UPPER AND AFT SIDE OF FRAME 50-2 BELOW STRINGER 24. REPAIRED IAW FOKKER SRM 53-10- 05, PAGE 601-601A AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001112600180 20011126 00180 EU 2001 11 26 QXEA0101924 1 20011113 A 5720 SUPPORT FOKKER F28 F28MK4000 4990810 EU LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT WING SKIN LOWER SURFACE SUPPORT STRUCTURE CHAFED. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5 AND SRM 51-30-00, P AGE 701-706. 2 L 7 2 4F RT A20EU 2001112600181 20011126 00181 EU 2001 11 26 QXEA0101925 1 20011113 A 5220 SKIN FOKKER F28 F28MK4000 4990810 EU EMERGENCY EXIT CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RT FORWARD EMERGENCY EXIT DOOR IS CRACKED IN RADIUS ON OUTER SKIN. REPAIRED IAW FOKKER SRM 52-02-03, FIGURE 3 AND SRM 51-31-05. 2 L 7 2 4F RT A20EU 2001112600182 20011126 00182 EU 2001 11 26 QXEA0101926 1 20011113 A 5220 SKIN FOKKER F28 F28MK4000 4990810 EU EMERGENCY EXIT CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RT AFT EMERGENCY EXIT DOOR IS CRACKED IN RADIUS ON OUTER SKIN. REPAIRED IAW FOKKER SRM 52-02-03, FIGURE 3 AND SRM 51-31-05. 2 L 7 2 4F RT A20EU 2001112600183 20011126 00183 EU 2001 11 26 QXEA0101927 1 20011113 A 5220 SKIN FOKKER F28 F28MK4000 4990810 EU EMERGENCY EXIT CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT AFT EMERGENCY EXIT DOOR IS CRACKED IN RADIUS ON OUTER SKIN. REPAIRED IAW FOKKER SRM 52-02-03, FIGURE 3. 2 L 7 2 4F RT A20EU 2001112600184 20011126 00184 EU 2001 11 26 QXEA0101928 1 20011113 A 5220 SKIN FOKKER F28 F28MK4000 4990810 EU EMERGENCY EXIT CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT FORWARD EMERGENCY EXIT DOOR IS CRACKED IN RADIUS ON OUTER SKIN. REPAIRED IAW FOKKER SRM 52-02-03, FIGURE 3 AND SRM 51-31-05. 2 L 7 2 4F RT A20EU 2001112600185 20011126 00185 EU 2001 11 26 QXEA0101929 1 20011113 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CASTELLATION CRACKED ADJACENT TO DIMPLE AT LOWER RIVET IN FRAME 17565 ABOVE STRINGER 20. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 3, PAGE 5 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001112600186 20011126 00186 EU 2001 11 26 QXEA0101930 1 20011114 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CASTELLATION CRACKED AT LOWER RIVET ON FRAME 20075 ABOVE STRINGER 45. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 3, PAGE 5. 2 L 7 2 4F RT A20EU 2001112600187 20011126 00187 NM 2001 11 26 AWXA200100597 1 20011114 A 5311 BAC15113769 STRAP BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 PHX - MAJOR REPAIR - "C" - CRACK FOUND ON FRAME RADIUS STRAP ON UPPER FLANGE ABOVE STRINGER 27R FOWARD PIT STA 492. MAIN TENANCE REMOVED RADIUS STRAP FABRICATED STRAP AND FILLER AND INSTALLED IAW DWG 65-20723 AND SRM 50-30-2 2 L 7 2 4F RT A16WE 2001112600188 20011126 00188 EU 2001 11 26 QXEA0101931 1 20011112 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CASTELLATION CRACKED ADJACENT TO LOWER RIVET ON OBLIQUE FRAME 16-2 ABOVE STRINGER 12. REPAIRED IAW FOKKER SRM 53 -10-05, PAGE 601-601A AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001112600189 20011126 00189 EU 2001 11 26 QXEA0101932 1 20011112 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CASTELLATION CRACKED AT LOWER RIVET HOLE ON FRAME 32-2 ABOVE STRINGER 14. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 601-601A AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001112600190 20011126 00190 EU 2001 11 26 QXEA0101933 1 20011112 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AFT CARGO BAY ANGLED FRAME THAT TIES INTO FORWARD END OF DOOR LOWER TORSION BOX AT FRAME 15810 HAS CORROSION AT FO RWARD AND AFT SIDE OF STRINGER 1 AND 74 CUTOUTS. REPAIRED IAW FOKKER SRM 53-01-01 AND SRM 51-10-04. 2 L 7 2 4F RT A20EU 2001112600191 20011126 00191 EU 2001 11 26 QXEA0101934 1 20011112 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AFT CARGO BAY BELLY SKIN HAS AREAS MARKED WITH CORROSION AT AFT EDGE OF LOWER CONNECTION ANGLE OF FRAME 15635 TO 8 INCHES AFT OF FRAME BETWEEN STRINGER 2 AND 73. REPAIRED IAW FOKKER SRM 53-01-01 AND SRM 51-10-04. 2 L 7 2 4F RT A20EU 2001112600192 20011126 00192 EU 2001 11 26 QXEA0101935 1 20011112 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AFT CARGO BAY FRAME 15635 HAS CORROSION ON AFT SIDE BOTTOM CONNECTION FLANGE TO SKIN BETWEEN STRINGER 3 AND 73. R EPAIRED IAW FOKKER SRM 53-01-01 AND SRM 51-10-04. 2 L 7 2 4F RT A20EU 2001112600193 20011126 00193 EU 2001 11 26 RAIA00111015 1 20011125 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 422TE 4427 399 106 MX - STL - DURING PRE-FLIGHT FOUND SEVERAL OVERHEAD EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 5 EMERGENCY LIGHT BAT TERY PACK IAW ATR MAINTENANCE MANUAL. 2 H 7 2 4T RT A53EU 2001112700001 20011127 00001 2001 11 27 SWAA013157 4 20011121 A 2565 65659723 BRACKET BOEING 737 7373A4 1384585 NM FWD SVC DOOR. BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 680AA 23505 FWD SVC DOOR EMERGENCY EVAC SLIDE BAR BRACKET BROKEN. REMOVED AND REPLACED BRACKET PER MM. 2 L 7 2 4F RT A16WE 2001112700002 20011127 00002 2001 11 27 SWAA013164 4 20011124 A 2565 001591475 SLIDE BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTANTLY DEPLOYED. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001112700003 20011127 00003 NM 2001 11 27 SWAA013165 1 20011125 A 5753 6546435 FLAP BOEING 737 7373Q8 1384670 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED D CHECK, FOUND RT OTBD AFT T/E FLAP DELAMINATED ON UPPER SURFACE INBD END. REPAIRED T/E FLAP PER MM.. 2 L 7 2 4F RT A16WE 2001112700004 20011127 00004 NM 2001 11 27 SWAA013166 1 20011125 A 5310 6546546 SHEAR TIE BOEING 737 7373Q8 1384670 NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 747, RBL 9. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2001112700005 20011127 00005 NM 2001 11 27 SWAA013167 1 20011125 A 5310 BAC1503 STIFFENER BOEING 737 7373Q8 1384670 NM LT MLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED D CHECK, FOUND LT VERTICAL STIFFENER CRACKED AT BS 663.75, WL 165. REMOVED AND REPLACED VERTICAL STIFF ENER PER SRM. 2 L 7 2 4F RT A16WE 2001112700006 20011127 00006 NM 2001 11 27 SWAA013168 1 20011124 A 5310 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM AFT CARGO CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2001112700007 20011127 00007 NM 2001 11 27 SWAA013169 1 20011124 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 846, RBL 3. REPAIRED FLOORBEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2001112700008 20011127 00008 NM 2001 11 27 SWAA013170 1 20011124 A 5310 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 364SW 26575 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17.1 AND WL 182. REPAIRED WEB PER SWA RA . 2 L 7 2 4F RT A16WE 2001112700009 20011127 00009 NM 2001 11 27 SWAA013171 1 20011124 A 5754 65C26603 SLAT BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 369SW 26580 DURING SCHEDULED C2 CHECK, FOUND NR 4 L/E SLAT TRAILING WEDGE DELAMINATED AT INBD END. REMOVED AND REPLACED NR 4 L/E SL AT PER MM. 2 L 7 2 4F RT A16WE 2001112700010 20011127 00010 NM 2001 11 27 SWAA013172 1 20011122 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 073SW 22673 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 769, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001112700011 20011127 00011 NM 2001 11 27 SWAA013173 1 20011123 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA), BS 500A, STR 10R, BS 500B, STR 4L AND BS 500D, STR 10R.. REPAIREDSKIN PER SRM. 2 L 7 2 4F RT A16WE 2001112700012 20011127 00012 NM 2001 11 27 SWAA013174 1 20011123 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 20L, BS 767 AND 787. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001112700013 20011127 00013 NM 2001 11 27 SWAA013175 1 20011125 A 5310 6547978 CREASE BEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED D CHECK, FOUND LT CREASE BEAM CORRODED AT BS 780 AND BS 873 AND CRACKED AT BS 641. REPAIRED CREASE BEA M PER SRM. 2 L 7 2 4F RT A16WE 2001112700014 20011127 00014 NM 2001 11 27 SWAA013178 1 20011125 A 5310 6546546 SHEAR TIE BOEING 737 737317 138447P NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 767, LBL 3 TO LBL 5, WL 146 AND WL 147. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2001112700015 20011127 00015 NM 2001 11 27 SWAA013179 1 20011125 A 5310 6546546 SHEAR TIE BOEING 737 737317 138447P NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 767, RBL 7 TO RBL 10, WL 146. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2001112700016 20011127 00016 EU 2001 11 27 QXEA0101859 1 20011106 A 5755 SPOILER FOKKER F28 F28MK4000 4990810 EU RT WING DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - DENT ON RT NR 5 LIFE DUMPER PANEL 82G. REPAIRED IAW FOKKER SRM 51-70-0, PAGE 13, FIGURE 7, PARAGRAPH C. 2 L 7 2 4F RT A20EU 2001112700017 20011127 00017 NE 2001 11 27 QXEA0101957 2 20011120 A 7510 VALVE DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE NR 2 ENGINE MALFUNCTIONED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 351PH 490 PDX - SMOKE IN CABIN AFTER ENGINE START. REPLACED NR 2 ENGINE P2.5/3 SWITCHING VALVE. OPERATIONAL CHECK GOOD. AIRCRAF T RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2001112700018 20011127 00018 EA 2001 11 27 QXEA0101959 1 20011117 A 5210 STRIKER CNDAIR CL600 CL6002C10 EA PAX DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 606QX 10023 PDX-MAIN CABIN DOOR STRIKER DAMAGED MIDWAY ALONG FORWARD LENGTH OF DOOR APERTURE. REPAIRED IAW HORIZON AIR EA R-53-06. 2 L 7 2 4F RT A21EA 2001112700019 20011127 00019 EA 2001 11 27 QXEA0101960 1 20011119 A 5210 DOOR CNDAIR CL600 CL6002C10 EA PAX DOOR LEAKING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 PDX-MAIN CABIN DOOR HAS SQUEAL AT ALL ALTITUDES. REPAIRED IAW HORIZON AIR EA R-53-08. 2 L 7 2 4F RT A21EA 2001112700020 20011127 00020 GL 2001 11 27 RAIA00110016 2 20011016 A 7510 C1460092 ANTI-ICE VALVE EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL RT ENGINE FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 804HK 3577 145082 311257 5298-LIT-RT ENGINE ANTI-ICE VALVE FAILED DURING TAXI. MAINTENANCE INSPECTED AND DEFERRED PER MEL30-21-01C. MAINTENANCE CLEARED DMI REMOVING AND REPLACING THE RT ENGINE ANTI-ICE VALVE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001112700021 20011127 00021 EU 2001 11 27 RAIA00111003 1 20011106 A 2910 NAS161204 O-RING AEROSP ATR42 ATR42300 8680920 EU HYDRAULIC SYS LEAKING A RAIA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 424TE 124 7137-STL-GREEN HYDRAULIC SYSTEM WENT TO ZERO PSI. MAINTENANCE INSPECTED, REMOVED AND REPLACED LEAKING PRESSURE TRANSMIT TER O-RING. LEAK CK OK IAW ATR MAINTENANCE MANUAL. 2 H 7 2 4T RT A53EU 2001112700022 20011127 00022 EU 2001 11 27 RAIA00111010 1 20011112 A 3350 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 551HK 41040 MX-STL- DURING PRE-FLIGHT PREPARATION REAR FLOOR TRACK LIGHTS WOULD NOT TEST. MAINTENANCE RE-SECURED LIGHT TRACK AND OP S CK OK IAW J41 MM. 2 L 7 2 4T RT A41NM 2001112700023 20011127 00023 SO 2001 11 27 C2XA01CL230 1 20011121 A 2120 BLANKET EMB 135 EMB135ER 3260203 SO FORWARD FUSELAGE LOOSE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 27506 145206 CLE-CVG FLIGHT#3093 THE CREW REPORTED ON 20 MILE FINALE APPROACH INTO CVG THE COCKPIT FILLED WITH ELECTRIC SMOKE AND WEN T AWAY AFTER TOUCHDOWN.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND FOUND THE INSULATION BLANK ET PULLED AWAY FROM THE AVIONICS COOLING FAN.THEY RESURCED THE INSULATION BLANKET AND PERFORMED OPERATIONAL CHECKS OF TH E COOLING FAN.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001112700024 20011127 00024 SO 2001 11 27 C2XA01CL231 1 20011124 A 5210 PE2504109837 PIN EMB 135 EMB135ER 3260203 SO MAIN DOOR BROKEN A C2XA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 27 27506 145206 CLE FLIGHT#3062 THE CREW REPORTED THE MAIN CABIN DOOR CATCHES WHEN BEING OPENED AND THE INTERIOR HANDLE APPEARED TO BE B ROKEN.MAINTENANCE INSPECTED AND FOUND THE ROLL PIN FOR THE INTERIOR LOCKING HANDLE TO BE BROKEN. THEY REPLACED THE PIN A ND FUNCTIONALY CHECKED THE MAIN CABIN DOOR.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001112700025 20011127 00025 EA 2001 11 27 COMA0160921 1 20011121 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA ROW 5 BURNED OUT A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 991CA 7216 EMERGENCY CEILING LIGHT AT ROW 5 IS INOP.REPLACED THE LIGHT BULB. 2 L 7 2 4F RT A21EA 2001112700027 20011127 00027 EA 2001 11 27 COMA0160922 1 20011118 A 2750 853D10018 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA R/H #3 SEIZED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 408CA 5365 7440 FLIGHT #5571. FLAPS FAILED AT 42 DEGREES DURING APPROACH.REPLACED THE R/H #3 FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2001113000061 20011130 00061 WP 2001 11 30 ARWA20011121 1 20011123 A 2810 FUEL CAP LKHEED 1011 1011385115 5265015 WP LT WING MISSING A ARWA J A DUMP FUEL UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 19 307GB 193U1131 AFTER T/O, FUEL LEAK FROM TOP OF LEFT WING. APPROX 10,000 LBS LOST FROM 2L; TANK NR 1 DID NOT DUMP FUEL INTRANSIT LIGHT DID NOT BLINK WITH SWITCH ON. APPROX 10,000 LBS FUEL JETTISON TO REDUCE LANDING WEIGHT. AIRCRAFT RETURNED TO TTPP AND LANDED WITHOUT INCIDENT. FOUND LT WING FUEL CAP MISSING OVERWING, REPLACED CAP IAW MM 28-40-0. 2 L 7 3 4F A23WE 2001112700032 20011127 00032 NM 2001 11 27 SABA011061 1 20011108 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A SABA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 33 813SN 032 AIRCRAFT 813, FLIGHT 5078. DURING PREFLIGHT TWO CABIN FLOOR EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE CHECKED BULBS AND REPAIRED A BROKEN WIRE. SYSTEM GROUND TEST GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001112700033 20011127 00033 EU 2001 11 27 SABA011063 1 20011118 A 7997 WIRE BAG JETSTM JETSTM3201 1500217 EU OIL SYSTEM DAMAGED A SABA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 33 964AE 964 AIRCRAFT 964 ON FLIGHT 5222 ABORTED TAKEOFF DUE TO OIL TEMPERATURE FLUCTUATION WHEN POWER WAS APPLIED. NO EMERGENCY PRO CEDURES WERE USED. AIRCRAFT RETURNED TO GATE. MAINTENANCE REPAIRED WIRES TO THE OIL TEMP BULB. SYSTEM GROUND RUN AND OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A56EU 2001112700034 20011127 00034 NM 2001 11 27 UPS01237314 1 20011117 A 2611 SMOKE DETECTOR BOEING 727 72727C 138400J NM CARGO BAY INOPERATIVE A IPXA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 01 914UP 19246 INSPECTION TYPE:N/A TARGET ALERT H20824 LOWER CARGO SMOKE DETECTION. LOWER CARGO SMOKE DETECTOR MX LT ILLUM. TECH RECO MMENDS: SUSPECT A-CHANNEL OF CCU FAILED. REPLACE CCU. PERFORMED ADJUSTMENT TEST PER MM 26-18-01, VERIFIED SN OF SMOKE DETECTORS. NO FURTHER DISCREPANCIES FOUND, SYSTEM HAS BEEN OPERATING NORMAL SINCE 11/08/01. 2 L 7 3 4F A3WE 2001112700035 20011127 00035 WP 2001 11 27 UPS01837269 1 20011109 A 2742 FASTENER DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE:N/A SEVERAL FASTENERS CORRODED IN COMPARTMENT 60 HORZ STABILIZER ACTUATING MECHANISM AREA ITEM SUBMITTED BY FOG TEAM. REMOVED AND REPLACED FASTENERS. CLEANED CORROSION FROM MARKET BOTLS APPROX 120 EA HUCK FASTENERS EXTENDI NG THROUGH LIGHTENING HOLES. CLEANED 20 EACH FASTENERS AND HEADS. 2 L 7 4 4F RT 4A25 2001112700037 20011127 00037 2001 11 27 SWAA013083 4 20011112 A 2565 6556685 RETAINER BOEING 737 7373A4 1384585 NM ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 680AA 23505 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE COVER GIRT BAR HOLDER LOOSE. SECURED HOLDER PER MM . 2 L 7 2 4F RT A16WE 2001112700038 20011127 00038 2001 11 27 SWAA013085 4 20011112 A 2565 61621469 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 641SW 27714 DURING SCHEDULED A2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC S LIDE PER MM. 2 L 7 2 4F RT A16WE 2001112700039 20011127 00039 NM 2001 11 27 SWAA013086 1 20011113 A 5311 96380 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND LT VERTICAL CHORD CRACKED .25 INCH LONG AT BS 178, WL 184 & LBL 5.7. REPAIR ED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2001112700040 20011127 00040 2001 11 27 SWAA013088 4 20011113 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 063SW 22061 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001112700041 20011127 00041 2001 11 27 SWAA013089 4 20011113 A 2565 1061323468 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 608SW 27928 DURING SCHEDULED RON, FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY INFLATED. REMOVED AND REPLACED EVAC SLIDE PER M M. 2 L 7 2 4F RT A16WE 2001112700042 20011127 00042 2001 11 27 SWAA013092 4 20011113 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 063SW 22061 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001112700043 20011127 00043 NM 2001 11 27 SWAA013093 1 20011114 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED RON, FOUND EMERGENCY FLASHLIGHT INOP AFT CABIN TOP POSITION. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2001112700044 20011127 00044 2001 11 27 SWAA013094 4 20011113 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001112700045 20011127 00045 2001 11 27 SWAA013095 4 20011114 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 749SW 29801 FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001112700046 20011127 00046 NM 2001 11 27 SWAA013099 1 20011113 A 5312 148A22804 BULKHEAD BOEING 737 7377H4 1384404 NM FUSELAGE CANNING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 709SW 27843 DURING SCHEDULED A2 CHECK, SI 11157-53 FOUND AFT PRESSURE BULKHEAD OIL CANNED BETWEEN STR 5L & 11L AND BETWEEN STR 9R & 11R. REPAIRED BULKHEAD PER SWA RA. 2 L 7 2 4F RT A16WE 2001112700047 20011127 00047 NM 2001 11 27 SWAA013100 1 20011114 A 2120 SMOKE BOEING 737 7377H4 1384404 NM CABIN DETECTED A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 712SW 27846 (DECLARED EMERGENCY) STRONG SMELL OF ELECTRICAL FIRE AND SOME SMOKE (ALTHOUGH LIMITED AS REPORTED BY FLIGHT ATTENDANT) U NKNOWN SOURCE. INSP OVERHEAD CABIN (DROPPED PANELS). REMOVED AND REPLACED BOTH PACK COALESCER BAGS, CHECKED CHIP DETEC TORS BOTH ENG (LEAK CK OK ). REMOVED AND REPLACED RECIRC FILTER, INSP DISTRIBUTION BAY, INSP GASPER AND RECIRC FANS, CH ECKED ALL CABIN LIGHTS AND EMERG LIGHTS AND INSP GALLEYS. NO DECREPANCIES FOUND, ODOR HAS DISSIPATED AND NO SMOKE EVIDE NT, ALL CK'S PER MM. 2 L 7 2 4F RT A16WE 2001112700048 20011127 00048 2001 11 27 SWAA013102 4 20011114 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 625SW 27701 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001112700049 20011127 00049 NM 2001 11 27 SWAA013105 1 20011114 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM ENTRY DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 060SW 21812 DURING SCHEDULED RON, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 2001112700050 20011127 00050 2001 11 27 SWAA013106 4 20011114 A 2565 22D22900131 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 074SW 22674 DURING SCHEDULED SERVICE CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED S LIDE PER MM. 2 L 7 2 4F A16WE 2001112700051 20011127 00051 2001 11 27 SWAA013107 4 20011114 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 627SW 27935 AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001112700052 20011127 00052 2001 11 27 SWAA013108 4 20011114 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 073SW 22673 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2001112700053 20011127 00053 NM 2001 11 27 SWAA013110 1 20011115 A 5312 6516300 BULKHEAD BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 506SW 24183 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED (6 EA) AT BS 178, BETWEEN LBL 10 & RBL 11. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001112700054 20011127 00054 WP 2001 11 27 MWEA011459 1 20011125 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP CEILING FAILED A MWEA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 31 216ME 47740 COCKPIT LIGHTS CABIN SIDEWALL LIGHTS AND THE EMERGENCY EXIT LIGHTS ABOVE THE FORWARD PAX AND GALLEY DOOR ARE ALL PULSING . -- REPLACED EMERGENCY BATTERY PACK. 2 L 7 2 4F A6WE 2001112700055 20011127 00055 EA 2001 11 27 COMA0160923 1 20011121 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA CABIN BURNED OUT A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 926CA 7027 FORWARD EMERGENCY CEILING LIGHT IS INOP.REPLACED LIGHT BULB. 2 L 7 2 4F RT A21EA 2001112700056 20011127 00056 EA 2001 11 27 COMA0160924 1 20011123 A 3231 DOOR ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA A COMA L ABORTED APPROACH S AFFECT SYSTEMS AP APPROACH 1 SO 01 929CA 7035 FLIGHT #5902. GER DISAGREE WARNING - NLG INDICATED UNSAFE. NLG THEN INDICATED DOWN AND LOCK DURING GO AROUND.ADJUSTED T HE NLG DOORS ACTUATOR AND MECHANISM. SYSTEM OPERATED NORMALLY. 2 L 7 2 4F RT A21EA 2001112700057 20011127 00057 2001 11 27 SWAA013111 4 20011117 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 063SW 22061 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2001112700058 20011127 00058 NM 2001 11 27 SWAA013112 1 20011116 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED RON, FOUND FWD SVC DOOR EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001112700059 20011127 00059 2001 11 27 SWAA013113 4 20011116 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2001112700060 20011127 00060 NM 2001 11 27 SWAA013114 1 20011116 A 3350 20121 CHARGER BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 384SW 26590 DURING SCHEDULED BC2 CHECK, FOUND EEPLS INOP AT MID CABIN. REMOVED AND REPLACED BATTERY CHARGER AND REPAIRED WIRES PER MM. 2 L 7 2 4F RT A16WE 2001112700061 20011127 00061 NM 2001 11 27 SWAA013115 1 20011115 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED C4 CHECK, FOUND EEPLS LOOSE AT BOTH FWD AND AFT CABIN. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001112700062 20011127 00062 NE 2001 11 27 SWAA013120 2 20011115 A 7200 CFM56 ENGINE BOEING 737 7377H4 1384404 NM GE CFM56 CFM56* 13802 NE NR 1 FAILED A SWAA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SW 07 799SW 28209 874130 (IN-FLIGHT ENG SHUT DOWN, DECLARED EMERGENCY, DIVERSION ) DURING CRUISE NR 1 ENGINE ABRUPTLY MADE A LOUD BANG, FOLLOWED BY A/C SHUTTER AND ABRUPT ROLLBACK OF BOTH N1 & N2 AND EGT (SCALES WENT BLANK). LANDED WITH NR 1 ENG SHUT DOWN. FOUND METAL AT THE NR 1 ENG FWD SUMP CHIP DETECTOR. REMOVED AND REPLACED NR 1 ENG PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2001112700063 20011127 00063 NM 2001 11 27 SWAA013121 1 20011116 A 2133 7110033 OUTFLOW VALVE BOEING 737 7373G7 1384595 NM CABIN PRESSURE FAILED A SWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 07 691WN 23781 (DECLARED EMERGENCY) AT 29,000 FEET CABIN PRESS HORN SOUNDED AND CABIN PRESS CONTROL INOP. REMOVED AND REPLACED AFT OUT FLOW VALVE PER MM. 2 L 7 2 4F RT A16WE 2001112700064 20011127 00064 NM 2001 11 27 SWAA013123 1 20011118 A 3350 6104781 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 342SW 24133 DURING SCHEDULED SERVICE CHECK, FOUND BOTH FWD SVC AND FWD ENTRY DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001112700065 20011127 00065 NM 2001 11 27 SWAA013124 1 20011118 A 3350 10107451 SIGN BOEING 737 7373H4 1384600 NM ENTRY DOOR DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 637SW 27710 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT SIGN DAMAGED. REMOVED AND REPLACED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2001112700066 20011127 00066 2001 11 27 SWAA013125 4 20011117 A 2565 D31354 SLIDE BOEING 737 7372T4 1384492 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001112700067 20011127 00067 NM 2001 11 27 SWAA013127 1 20011119 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 703SW 27837 EEPLS LOOSE AT ROW 14 AND 15. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001112700068 20011127 00068 2001 11 27 SWAA013128 4 20011118 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 068SW 22357 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2001112700069 20011127 00069 NM 2001 11 27 SWAA013129 1 20011118 A 3350 6104781 BATTERY BOEING 737 7373Y0 1384671 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 682SW 23496 DURING SCHEDULED PM CHECK, FOUND BOTH FWD ENTRY AND FWD SVC DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTE RY PER MM. 2 L 7 2 4F RT A16WE 2001112700070 20011127 00070 NM 2001 11 27 SWAA013136 1 20011119 A 5312 6516300 BULKHEAD BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, WL 206 AND RBL 1.5, WL 234 AND RBL 8. REPAIRED W EB PER SWA ACO. 2 L 7 2 4F RT A16WE 2001112700071 20011127 00071 NM 2001 11 27 SWAA013142 1 20011119 A 3350 101073 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR LOWER EMERGENCY EXIT LIGHT MISSING COVER. REMOVED AND REPLACED LIGHT AS SY PER MM. 2 L 7 2 4F RT A16WE 2001112700072 20011127 00072 NM 2001 11 27 SWAA013144 1 20011119 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 758SW 27873 DURING SCHEDULED C3 CHECK, FOUND EEPLS COVERS CRACKED (6 EA). REMOVED AND REPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2001112700073 20011127 00073 2001 11 27 SWAA013145 4 20011119 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001112700074 20011127 00074 NM 2001 11 27 SWAA013148 1 20011117 A 5311 BAC1505 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL CHORD CRACKED AT BS 178, LBL 5.7 AND WL 185. REPAIRED CHORD PER SWA RA. 2 L 7 2 4F RT A16WE 2001112700075 20011127 00075 NM 2001 11 27 SWAA013158 1 20011120 A 3350 57771 CAP BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 651SW 27721 DURING SCHEDULED C1 CHECK, FOUND EEPLS END CAP MISSING AT FWD CABIN. INSTALLED END CAP PER MM. 2 L 7 2 4F RT A16WE 2001112700076 20011127 00076 2001 11 27 SWAA013159 4 20011122 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001112700077 20011127 00077 NM 2001 11 27 SWAA013160 1 20011123 A 3350 20131A BATTERY BOEING 737 7375H4 138449D NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 519SW 25318 DURING SCHEDULED RON, FOUND FWD SVC DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001112700078 20011127 00078 2001 11 27 SWAA013161 4 20011124 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 600WN 27694 DURING SCHEDULED BC3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001112700079 20011127 00079 NM 2001 11 27 SWAA013162 1 20011124 A 3397 WIRE BOEING 737 7377H4 1384404 NM CABIN DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 769SW 30588 DURING SCHEDULED PM CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REPAIRED WIRE PER MM. 2 L 7 2 4F RT A16WE 2001112700080 20011127 00080 2001 11 27 SWAA013163 4 20011123 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 068SW 22357 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2001121200039 20011212 00039 NM 2001 12 12 01FDEA01005 1 20011123 A 5330 SKIN BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 285FE 22622 CORROSION ON SKIN FWD CARGO BAY BS 705-717 O/B OF STR 28L. REMOVED AND REPLACED DOUBLER PER SRM 53-30-3. 2 L 7 3 4F RT A3WE 2001121200040 20011212 00040 NM 2001 12 12 01FDEA01006 1 20011121 A 5311 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 285FE 22622 DENT IN FRAME UPPER FLANGE AT BS 1070 BETWEEN STR 26R-27R. REMOVED AND REPLACED FRAME PER SRM 51-40-3 FIG 1 & EA 7-5310 -62617. 2 L 7 3 4F RT A3WE 2001112700081 20011127 00081 NM 2001 11 27 SWAA013176 1 20011120 A 5312 6546568 BULKHEAD BOEING 737 7377H4 1384404 NM FUSELAGE CANNING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 752SW 29804 DURING SCHEDULED SERVICE CHECK, FOUND AFT PRESS BULKHEAD OIL CANNED, BS 1016, FIRST CIRCUMFERENTIAL STRAP. MX FERRY TO PAE, REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 2001112700082 20011127 00082 NM 2001 11 27 SWAA013177 1 20011121 A 5312 6546568 BULKHEAD BOEING 737 7377H4 1384404 NM FUSELAGE CANNING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 744SW 29490 DURING SCHEDULED A1 CHECK, FOUND AFT PRESS BULKHEAD OIL CANNED BETWEEN STR 5R AND 6R. MX FERRY TO PAE, REPAIRED BULKHEA D PER BFG ER. 2 L 7 2 4F RT A16WE 2001112700083 20011127 00083 NM 2001 11 27 SWAA013180 1 20011121 A 5314 6512125 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED BC3 CHECK, FOUND KEEL BEAM CORRODED FROM BS 520 TO BS 526, LT SIDE. REPAIRED KEEL BEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2001112700084 20011127 00084 NM 2001 11 27 SWAA013181 1 20011122 A 7933 56B94 BULB BOEING 737 7373H4 1384600 NM NR 2 ENGINE FAULTY A SWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 359SW 26596 DIVERSION, DURING CRUISE NR 2 ENG OIL TEMP CLIMBED TO YELLOW MARKING. TO MAINTAIN TEMP IT WAS NECESSARY TO REDUCE POWER TO 69 PERCENT N1. REMOVED AND REPLACED NR 2 ENG OIL TEMP BULB AND CHECKED CHIP DETECTORS. OPS CHECKED GOOD PER MM. 2 L 7 2 4F RT A16WE 2001112700085 20011127 00085 NM 2001 11 27 2001UALA02300 1 20011117 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 521UA 24891 EXTERNAL FUSELAGE SKIN BODY STATION 640 STRINGER 18L HAS TWO EACH DENTS. MAJOR REPAIR ACCOMPLISHED. INSTALLED 16"X10" S KIN DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2001112700087 20011127 00087 NM 2001 11 27 2001UALA02312 1 20011121 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 515UA 24840 FUSELAGE SKIN DAMAGED STATION 1697 AT STRINGER 20LT AND STRINGER 21LT. MAJOR REPAIR ACCOMPLISHED.STRINGER 20LT AND 21LT REPAIRED. FILER AND DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2001112700088 20011127 00088 EA 2001 11 27 SWIA200110349 1 20010925 A 5720 BOLT CNDAIR CL600 CL6002B19 1900309 EA RT WING CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 410SW 7066 RIGHT WING TRAILING EDGE NEAR AILERON POSITIONING TRANSMITTER HAS 3 CORRODED BOLTS. NEW HARDWARE INSTALLED IAW CRJ MM 2 7-15-01. 2 L 7 2 4F RT A21EA 2001112700090 20011127 00090 NM 2001 11 27 UPS01437304 1 20011104 A 5311 FRAME BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C CRACK REVEALED ON RT BS 1480 BULKHEAD CHORD AT FASTENER HOLE NR 3 BY APPROX 0.060 INCH LONG AND RUNNIN G AFT UP AS PER ATTACH FIGURE. RIGHT BS 1480 B/H CHORD HOLE NR 3 CRACK REMOVED AND BUSH INSTALLED IN B/H CHORD HOLE NR 3 AS PER SB 747-53A2390 FIG 11. PLAN A BUSH REPAIR CWPC NR RCBR017 054 ATTACHED. THIS REPAIR ACCOMPLISHED AS PER RS R- 53-43-34702 AND EO B747-5310-15717-A. 2 L 7 4 4F RT A20WE 2001112700091 20011127 00091 NM 2001 11 27 UPS01437310 1 20011103 A 5320 SPLICE BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C RT SIDE BS 1480 B/H FASTENER HOLE NR 5 FOUND CRACKED AT OUTER CHORD SPLICE FITTING. RT BS 1480 B/H OU TER CHORD SPLICE FITTING HOLE NR 5 CRACK REMOVED AND BUSHING INSTALLED IN OUTER CHORD SPLICE FITTING HOLE NR 5 AS PER SB 747-53A2390 FIG 11. PLAN A BUSHING REPAIR CWPC CONTROL SEQUENCE NR RCBR017 055 ATTACHED. THIS REPAIR ACCOMPLISHED AS PER RS R-53-43-34702 AND EO B747-5310-15717-A. 2 L 7 4 4F RT A20WE 2001112700092 20011127 00092 NM 2001 11 27 UPS01437325 1 20011031 A 5311 FRAME BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C RIGHT BS 2231 FRAME ONE FASTENER HOLE CRACK FOUND ON S25R, AT INNER CHORD RUNNING FWD AND AFT THROUGH THICKNESS, REFER ATTACH SKETCH. FRAME INNER CHORD REPAIRED AT S25R AS PER SRM 53-10-04 FIG 115. 2 L 7 4 4F RT A20WE 2001112700093 20011127 00093 NM 2001 11 27 UPS01437326 1 20011031 A 5311 FRAME BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C RT BS 2231 FRAME, ONE FASTENER HOLE CRACK FOUND AT REVEAL BETWEEN S24 AND S25R RUNNING AFT APPROX .125 INCH LONG. BETWEEN S24 AND S25R FRAME REVEAL REPAIRED AS PER MM 53-10-04 FIG 115. 2 L 7 4 4F RT A20WE 2001112700094 20011127 00094 SO 2001 11 27 2001F00656 1 20011016 A 2611 FDS765A2 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A MASA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 825MJ 145179 FLT 5752 - IN FLIGHT, THE CREW RECEIVED A LAVATORY SMOKE DETECTOR MESSAGE ON THE EICAS. THE AIRCRAFT RETURNED TO THE FI ELD AND UPON LANDING THE INDICATION CLEARED. THE FIRE DEPARTMENT INSPECTED THE LAVATORY AND FOUND NO PROBLEMS. THE SMO KE DETECTOR WAS RETESTED AND FOUND TO BE IN WORKING ORDER. NO FURTHER ACTION WAS TAKEN. (M) 2 L 7 2 4T RT T00011AT 2001112700095 20011127 00095 NM 2001 11 27 2001F00657 1 20011017 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 446YV 446 DURING A ROUTINE LINE CHECK INSPECTION, THE LEFT AFT EXTERIOR EMERGENCY EGRESS AND NR 2 CEILING EMERGENCY LIGHTS WOULD N OT ILLUMINATE. THE NR 3 EMERGENCY LIGHT POWER SUPPLY WAS REPLACED WITH NO FURTHER DEFECTS NOTED. (M) 2 H 7 2 4T RT A13NM 2001112700096 20011127 00096 EA 2001 11 27 2001F00658 1 20011019 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37208 7208 FLT 5890 - CLT-MOB - THE CREW FOUND THE AFT EMERGENCY CEILING FLOOD LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2001112700097 20011127 00097 NM 2001 11 27 2001F00659 1 20011022 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 456YV 456 DURING A ROUTINE LINE CHECK INSPECTION, THE LEFT AFT EXTERIOR EMERGENCY EGRESS LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REPLACED THE NR 3 EMERGENCY LIGHT POWER SUPPLY AND NO FURTHER DEFECTS WERE NOTED. (M) 2 H 7 2 4T RT A13NM 2001112700098 20011127 00098 EA 2001 11 27 2001F00660 1 20011023 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37208 7208 FLT 5759 - PHL-BHM - THE CREW FOUND ONE AFT LEFT EXTERIOR FUSELAGE EMERGENCY FLOOR LIGHT INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE EMERGENCY LIGHT AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2001112700099 20011127 00099 NM 2001 11 27 2001F00661 1 20011023 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 446YV 446 DURING A 12 MONTH INSPECTION TASK, THREE FORWARD EMERGENCY ESCAPE PATH LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REPLACE D THE NR 2 EMERGENCY LIGHT POWER SUPPLY AND OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A13NM 2001112700100 20011127 00100 NM 2001 11 27 2001F00662 1 20011023 A 3350 6104799 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN FAULTY A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 446YV 446 DURING A 12 MONTH INSPECTION TASK, THE RIGHT DC EMERGENCY LIGHT CIRCUIT BREAKER POPPED. MAINTENANCE REPLACED THE NR 2 E MERGENCY LIGHT POWER SUPPLY AND OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A13NM 2001112700101 20011127 00101 EA 2001 11 27 2001F00663 1 20011024 A 3350 362624 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7264V 7264 DURING A ROUTINE SERVICE CHECK, THE CREW FOUND A FLOOR EMERGENCY LIGHT IN AISLE 5 INOPERATIVE. MAINTENANCE REPLACED THE BULB AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2001112700102 20011127 00102 SO 2001 11 27 2001F00664 1 20011025 A 3350 66368 LIGHT EMB 145 EMB145LR 3260212 SO CABIN BROKEN A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 838MJ 145384 FLT 5845 - CLT-MGM - THE FLOOR EMERGENCY TRACK LIGHT WAS FOUND BROKEN AT ROW 13 AND 14. TWO LIGHTS AFT WERE ALSO INOPER ATIVE DUE TO THE DAMAGED LIGHT. MAINTENANCE INSTALLED LIGHTING STRIPS AND OPS CHECKED GOOD. (M) 2 L 7 2 4T RT T00011AT 2001112700103 20011127 00103 EA 2001 11 27 2001F00665 1 20011031 A 3350 OL3071BPEGPL LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77260 7260 DURING A ROUTINE SERVICE CHECK, THE CREW FOUND A OVERHEAD EMERGENCY EXIT LIGHT BESIDE THE PASSENGER DOOR INOPERATIVE. M AINTENANCE REPLACED THE BULB AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2001112700104 20011127 00104 EA 2001 11 27 2001F00666 1 20011031 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7305V 7305 DURING NIGHT SHIFT SCHEDULED MAINTENANCE, THE CREW FOUND THE RIGHT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANC E REPLACED THE BULB AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2001112700105 20011127 00105 EA 2001 11 27 2001F00667 1 20011102 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77302 7302 DURING A ROUTINE SERVICE CHECK, THE CREW FOUND THE EXTERIOR EMERGENCY LIGHT NR 6 INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2001112700106 20011127 00106 EA 2001 11 27 2001F00649 1 20010929 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA LT WING FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77260 7260 DURING AN OVERNIGHT SCHEDULED MAINTENANCE CHECK, THE CREW FOUND A LEFT FORWARD EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BULB AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2001112700107 20011127 00107 NM 2001 11 27 2001F00650 1 20010914 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A MASA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 07 437YV 437 FLT 6389 - PHX-YUM - DURING TAXI-OUT, THE CREW HAD AN OVERHEAD EMERGENCY LIGHT INOPERATIVE AND THE MAIN DOOR EMERGENCY E XIT SIGN INOPERATIVE. THE PROBLEM WAS TROUBLESHOT TO THE EMERGENCY LIGHT BATTERIES. MAINTENANCE REMOVED AND REPLACED T HE 1, 2 AND 3 POWER SUPPLIES AS REQUIRED. OPS CHECKED GOOD AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 2001112700108 20011127 00108 EA 2001 11 27 2001F00651 1 20011003 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77260 7260 A RIGHT EXTERIOR MID EMERGENCY LIGHT WAS FOUND INOPERATIVE DURING A ROUTINE CHECK. MAINTENANCE REPLACED THE BULB AND OP S CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2001112700109 20011127 00109 SO 2001 11 27 2001F00652 1 20011011 A 3397 BC10020002 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN DISCONNECTED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 828MJ 145218 FLT 5873 - WHEN THE FLIGHT ATTENDANT TESTED THE EMERGENCY LIGHTS, THE LAST SECTION OF THE CABIN WAS INOPERATIVE. MAINTE NANCE CAME OUT AND FOUND THAT THE LAST SECTION OF LIGHTS WERE UNPLUGGED. RESECURED THE CONNECTOR AND OPS CHECKED GOOD. (M) 2 L 7 2 4T RT T00011AT 2001112700110 20011127 00110 EA 2001 11 27 2001F00653 1 20011011 A 3350 601R3140443 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37208 7208 FLT 5890 - CLT-MOB - THE PILOT REPORTED A RIGHT OVERWING EMERGENCY EXIT ANNUNCIATOR INOPERATIVE. MAINTENANCE SWAPPED TH E EXITS AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2001112700111 20011127 00111 NM 2001 11 27 2001F00654 1 20011014 A 3350 GE316 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 444YV 444 FLT 6382 - YUM-PHX - THE CREW FOUND THE AFT CEILING OVERHEAD EMERGENCY FLOOD LIGHT INOPERATIVE. MAINTENANCE REPLACED TH E BULB AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 2001112700112 20011127 00112 EA 2001 11 27 2001F00655 1 20011014 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27318 7318 DURING NIGHT SHIFT SCHEDULED MAINTENANCE, THE CREW FOUND THE FORWARD CABIN EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REP LACED THE BULB AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2001112700113 20011127 00113 NM 2001 11 27 2001F00668 1 20010901 A 3350 883200312 RECEIVER BOEING 737 7372Q8C 138448S NM CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROW 11 WERE SLOW TO RESPOND AND WOULD NOT EXTINGUISH. RE MOVED AND REPLACED BATTERY PACK P/N 8821004, AND REMOTE ASSEMBLY RECEIVER P/N 883200312, THEN LIGHTS TESTED NORMAL. REF ASAA0110571 (M) 2 L 7 2 4F A16WE 2001112700114 20011127 00114 NM 2001 11 27 2001F00669 1 20010714 A 3350 8821004 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 JNU - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROW 26 WOULD NOT EXTINGUISH. REPLACED EMERGENCY EXIT BAT TERY PACK AND REMOTE ASSEMBLY RECEIVER, LIGHTS THEN TESTED NORMAL. REF ASAA0110491. (M) 2 L 7 2 4F RT A16WE 2001112700116 20011127 00116 EU 2001 11 27 SABA011069 1 20011124 A 2610 51224127 FIRE LOOP BAG JETSTM JETSTM3201 1500217 EU CHAFED A SABA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 33 964AE 964 L/H Engine Fire Warning Indication Sytem illuminated during take off hold position. Crew discharged both engine fire bot tles and returned to gate.Maintenance trouble shot fire warning system and found a small chafe on FWD Fire Wire. Removed and replaced FWD Fire Wire and Fire Bottles. Aircraft returned to service. 2 L 7 2 4T RT A56EU 2001112700117 20011127 00117 NM 2001 11 27 ASAA0110459 1 20010702 A 3350 8821004 BATTERY PACK BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY TRACK LIGHTS ILLUMINATED AND WOULD NOT EXTINGUISH. REMOVED AND REPLACED BATTERY PACK, THEN LIGHTS OPERATED NORMAL. (M) 2 L 7 2 4F A16WE 2001112700118 20011127 00118 NM 2001 11 27 ASAA0110465 1 20010702 A 5320 6546544525 ATTACH ANGLE BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND ATTACH ANGLES AT BS 695, LEFT BUTTOCK LINE 60 CORRODED. REPAIRED PER BOEING DRAWI NG. (M) 2 L 7 2 4F RT A16WE 2001112700119 20011127 00119 NM 2001 11 27 ASAA0110469 1 20010704 A 3350 6013211 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHT WOULD NOT EXTINGUISH. REPLACED EMERGENCY EXIT BATTE RY PACK, LIGHTS THEN TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2001112700120 20011127 00120 NM 2001 11 27 ASAA0110470 1 20010705 A 3350 RECEIVER BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS P/N 88-3-2003-1-2, 88-2-1004, WOULD NOT ILLUMINATE. REPLACE D EMERGENCY EXIT BATTERY PACK AND REMOTE ASSEMBLY RECEIVER, LIGHTS THEN TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2001112700121 20011127 00121 NM 2001 11 27 ASAA0110481 1 20010707 A 5320 608306 FLOOR SUPPORT BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT AT BS 887-916, STRINGER 26R-27R CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001112700122 20011127 00122 NM 2001 11 27 ASAA0110483 1 20010707 A 5320 694147314 INTERCOSTAL BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL AT BS 440-460, STRINGER 26L CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001112700123 20011127 00123 NM 2001 11 27 ASAA0110490 1 20010712 A 3350 87310021 LIGHT BOEING 737 737290C 138448V NM R2 DOOR INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 ANC - DURING MAINTENANCE CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EXIT LIGHT ASSEMBL Y THEN LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2001112700124 20011127 00124 NM 2001 11 27 ASAA0110491 1 20010714 A 3350 883200312 RECEIVER BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 JNU - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROW 26 WOULD NOT EXTINGUISH. REPLACED EMERGENCY EXIT BAT TERY PACK AND REMOTE ASSEMBLY RECEIVER, LIGHTS THEN TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2001112700125 20011127 00125 NM 2001 11 27 ASAA0110492 1 20010721 A 5210 507945178 DOOR BOEING 737 7372X6C 1384552 NM L1 OUT OF ADJ A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 JNU - DURING MAINTENANCE CHECK, FOUND L1 DOOR DIFFICULT TO OPEN AND CLOSE. ADJUSTED L1 DOOR PER MM AND DOOR OPENED NORM ALLY. (M) 2 L 7 2 4F RT A16WE 2001112700126 20011127 00126 NM 2001 11 27 ASAA0110512 1 20010726 A 3350 873100211 SIGN BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT SIGN INOPERATIVE. REPLACED EMERGENCY EXIT SIGN, SIGN THEN TESTED N ORMAL. (M) 2 L 7 2 4F RT A16WE 2001112700127 20011127 00127 NM 2001 11 27 ASAA0110565 1 20010831 A 5320 65515253 TIE CLIP BOEING 737 737210C 1384459 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER TIE AT BS 728, STRINGER 20L CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001112700128 20011127 00128 WP 2001 11 27 MWEA011447 1 20011126 A 5310 99124513 FRAME DOUG DC9 DC915 3022036 WP F.S 377.5 MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 FRAME (FORMER) AT FUSELAGE STATION 377.5 AND BETWEEN LONGERON 30 AND LONGERON 28 RIGHT MISDRILLED -- REMOVED INTERCOST AL. FABRICATED AND INSTALLED STACKED ANGLE REPAIR DOUBLERS. 2 L 7 2 4F A6WE 2001112700129 20011127 00129 NM 2001 11 27 ASAA0110568 1 20010831 A 5320 69771174 TIE CLIP BOEING 737 737210C 1384459 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER TIE AT BS 728, STRINGER 23L CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001112700130 20011127 00130 NM 2001 11 27 ASAA0110569 1 20010831 A 5312 6516300512 BULKHEAD BOEING 737 737210C 1384459 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND BULKHEAD AT BS 178, RIGHT BUTTOCK LINE 20 CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2001112700131 20011127 00131 NM 2001 11 27 ASAA0110571 1 20010901 A 3350 8821004 BATTERY PACK BOEING 737 7372Q8C 138448S NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROW 11 WERE SLOW TO RESPOND AND WOULD NOT EXTINGUISH. RE MOVED AND REPLACED BATTERY PACK P/N 8821004, AND REMOTE ASSEMBLY RECEIVER P/N 883200312, THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F A16WE 2001112700132 20011127 00132 NM 2001 11 27 ASAA0110572 1 20010902 A 5210 6529994 GUIDE BOEING 737 7372Q8C 138448S NM L1 DOOR OUT OF ADJ A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 ANC - DURING MAINTENANCE CHECK, FOUND L1 DOOR DIFFICULT TO CLOSE. ADJUSTED GUIDE ARM AND DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2001112700133 20011127 00133 NM 2001 11 27 ASAA0140090 1 20010704 A 3350 8100022601 LIGHT BOEING 737 7374Q8 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 776AS 25109 ANC - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE AT ROW 13 TO 16. REPLACED EMERGENCY FLOOR TRA CK LIGHTING. OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001112700134 20011127 00134 NM 2001 11 27 ASAA0140091 1 20010707 A 3350 8100022602 LIGHT BOEING 737 7374Q8 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 765AS 25102 ANC - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE AT ROW 13 TO 15. RECONNECTED EMERGENCY FLOOR TRACK LIGHTING. OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001112700135 20011127 00135 NM 2001 11 27 ASAA0140092 1 20010711 A 3350 8100022603 LIGHT BOEING 737 737490 1384715 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 768AS 27082 ANC - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE AT ROW 19 TO 20. RECONNECTED EMERGENCY FLOOR TRACK LIGHTING. OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001112700136 20011127 00136 NM 2001 11 27 ASAA0140097 1 20010820 A 5753 65C348124 FLAP TRACK BOEING 737 737400 NM T/E FLAP CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 772AS 25105 SEA - DURING C-CHECK, FOUND RIGHT OUTBOARD FLAP TRACK NR 8 AND NR 7 CORRODED FROM UPPER SURFACE AT REAR SPAR, SHIM NOT S EALED PROPERLY. REMOVED AND REPLACED IAW MM. (M) 2 L 7 2 4F RT A16WE 2001112700137 20011127 00137 NM 2001 11 27 ASAA0140098 1 20010820 A 5753 65C348124 FLAP TRACK BOEING 737 737400 NM T/E FLAP CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 772AS 25105 SEA - DURING C-CHECK, FOUND LEFT OUTBOARD FLAP TRACK NR 2 CORRODED FROM UPPER SURFACES AT REAR SPAR, SHIM NOT SEALED PRO PERLY. REMOVED AND REPLACED IAW MM. (M) 2 L 7 2 4F RT A16WE 2001112700138 20011127 00138 NM 2001 11 27 ASAA0140621 1 20011016 A 5320 6562107502 THRESHOLD BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING C-CHECK, FOUND CORROSION ON MAIN CARGO DOOR THRESHOLD WEB AT STATION 400-497. REMOVED AND REPLACED DAMAGED SECTION OF WEB PER SRM AND ENGINEERING REPAIR. (M) 2 L 7 2 4F A16WE 2001112700139 20011127 00139 WP 2001 11 27 ASAA0180215 1 20010705 A 3350 0105606003 MODULE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 958AS 53024 SEA - DURING PRE-FLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS DISCONNECTED AT ROW 3. RECONNECTED LIGHT MODULE SOCKE T. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001112700140 20011127 00140 WP 2001 11 27 ASAA0180216 1 20010705 A 5610 5613217519 PIN DOUG DC9 DC983 3022083 WP COCKPIT NOT SEATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 34510 53024 SEA - DURING PREFLIGHT CHECK, THE CAPTAINS SLIDING CLEARVIEW WINDOW COULD NOT BE OPENED. RESEATED WINDOW UPPER ARM PIN. WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001112700141 20011127 00141 2001 11 27 ASAA0180217 4 20010705 A 2565 3961899501 LANYARD DOUG DC9 DC982 3022082 WP SERVICE DOOR DETACHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 935AS 49236 PHX - DURING PREFLIGHT CHECK, R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED FROM DOOR. REATTACHED LANYARD B ETWEEN GIRT BAR AND DOOR SLIDE COVER. (M) 2 L 7 2 4F A6WE 2001112700142 20011127 00142 WP 2001 11 27 ASAA0180218 1 20010705 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP TAILCONE DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 960AS 53074 PDX - DURING LINE CHECK, OVERHEAD EMERGENCY LIGHT IN TAILCONE WAS DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BAT TERY PACK AND REPAIRED WIRING. LIGHT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001112700143 20011127 00143 WP 2001 11 27 ASAA0180219 1 20010706 A 5610 59644201 WINDOW DOUG DC9 DC982 3022082 WP COCKPIT LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 954AS 44036 49387 LAX - DURING PREFLIGHT CHECK, CAPTAINS SLIDING CLEARVIEW WINDOW WAS HARD TO OPEN. LUBRICATED WINDOW. WINDOW THEN OPERA TED PROPERLY. (M) 2 L 7 2 4F A6WE 2001112700144 20011127 00144 WP 2001 11 27 ASAA0180220 1 20010711 A 3350 0105606003 MODULE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 973AS 53449 SEA - DURING PREFLIGHT CHECK, FOUND FIRST SEVEN EMERGENCY FLOOR TRACK LIGHTS DISCONNECTED. RECONNECTED LIGHT MODULES. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001112700145 20011127 00145 WP 2001 11 27 ASAA0180221 1 20010711 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 933AS 49234 PDX - DURING PRE-FLIGHT CHECK, FOUND FIRST NINE EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE. REPLACED ASSOCIATED BATTERY P ACKS. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001112700146 20011127 00146 WP 2001 11 27 ASAA0180224 1 20010713 A 3350 0105606003 MODULE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 LAX - DURING PRE-FLIGHT CHECK, FOUND FIRST SIX EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE. RECONNECTED LIGHT MODULES. LI GHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001112700147 20011127 00147 WP 2001 11 27 ASAA0180227 1 20010724 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 974AS 53450 SEA - DURING LINE CHECK, FOUND THAT FORWARD EMERGENCY FLOOR TRACK LIGHTS ILLUMINATED WHEN POWER IS TURNED OFF. REPLACED BATTERY PACK AT B5-24. ALL LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001112700148 20011127 00148 WP 2001 11 27 ASAA0180233 1 20010801 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP TAILCONE DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 958AS 53024 PDX - DURING LINE CHECK, OVERHEAD EMERGENCY LIGHT IN TAILCONE WAS DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BAT TERY PACK. LIGHT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001112700149 20011127 00149 WP 2001 11 27 ASAA0180234 1 20010802 A 3397 0105606003 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 951AS 49111 SEA - DURING PRE-FLIGHT CHECK, A TRACK LIGHT WAS FOUND TO BE INOPERATIVE AT ROW 1. SPLICED BROKEN WIRE UNDER TRACK COVE R. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001112700150 20011127 00150 WP 2001 11 27 ASAA0180240 1 20010812 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 965AS 53079 PDX - DURING PREFLIGHT CHECK, 1ST CLASS EMERGENCY FLOOR TRACK LIGHTING WAS DETERMINED TO BE INOPERATIVE. RECONNECTED LO OSE LIGHT MODULE SOCKET. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001112700151 20011127 00151 WP 2001 11 27 ASAA0180241 1 20010814 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 950AS 53023 LAX - DURING SERVICE CHECK, EMERGENCY FLOOR TRACK LIGHTING WAS DETERMINED TO BE INOPERATIVE AT AFT EXIT. REPLACED ASSOC IATED BATTERY PACK. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001112700152 20011127 00152 NM 2001 11 27 ASAA0190001 1 20010722 A 3350 D71702001 POWER SUPPLY BOEING 737 737* NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 305AS 30013 SEA - DURING A LINE MAINTENANCE CHECK, THE AFT EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED POWER SUPPLY. EX IT LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 2001112700153 20011127 00153 NM 2001 11 27 AWXA200100600 1 20011124 A 3350 864705 POWER SUPPLY BOEING 737 737277 1384570 NM CABIN ILLUMINATED A AWXA K NONE O OTHER UK UNKNOWN 1 WP 28 186AW 22653 PHX - EEL - "C" - DURING PREFLIGHT CHECK ROWS 1 THROUGH 5 EMERGENCY LIGHTS REMAINED ILLUMINATED. REMOVED AND REPLACED BA TTERY PACK AND POWER SUPPLY, OPERATIONAL CHECK GOOD. PART NAME: BATTERY PACK, MFG: IDD AEROSPACE, P/N: 9008-3-5A, COND .: PARTIALLY DISCHARGED, LOCATION: CABIN. 2 L 7 2 4F RT A16WE 2001112700155 20011127 00155 NM 2001 11 27 P5CA0100613 1 20011118 A 5510 65B0371029 FAIRING BOEING 747 747249F 1384849 NM STAB STA 560 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 L/H HORIZONTAL STABILIZER STA 560 OUTBOARD TIP - AFT WEDGE 6" SECTION BROKEN OFF. REMOVED & REPLACED T/E & BOTTOM ACCESS PANELS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2001112700156 20011127 00156 NM 2001 11 27 P5CA0100614 1 20011118 A 2710 65B021002 AILERON BOEING 747 747122 1384872 NM R/H O/B WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 R/H OUTBD AILERON TOP CENTER HONEYCOMB PANEL TOP SKIN DELAMINATED 5' FROM I/B END, APPROX. 15" DIA. REMOVED & REPLACED R/H OUTBD AILERON PER MM 27-11-02 2 L 7 4 4F A20WE 2001112700157 20011127 00157 EA 2001 11 27 SWIA200110350 1 20010925 A 5415 BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE PYLON CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 410SW 7066 ENGINE PYLON BOX BEAM LOWER WEB CRACKING FROM ANCHOR NUTS AT STRESS PANEL FS 640 LEFT AND RIGHT SIDES. REPAIRS ACCOMPLI SHED IAW REO 601R-53-61-366, LEFT AND RIGHT SIDES OF BOX BEAM. HFEC INSPECTION CARRIED OUT IAW REO 53-61-366. NO CRACK S FOUND. 2 L 7 2 4F RT A21EA 2001112700158 20011127 00158 EA 2001 11 27 SWIA200110351 1 20010925 A 5415 BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGNE PYLON CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 410SW 7066 ENGINE PYLON BOX BEAM UPPER WEB HAS 2 CRACKS AT LBL 8.0 AND RBL 7.5, RADIATING FWD FROM TRAILING EDGE OF BEAM. CARRY OU T REPAIRS TO LOWER BOX BEAM WEB IAW REO 601R-53-61-345 AND 601R-53-61-368. CARRY OUT REPAIRS TO UPPER BOX BEAM WEB IAW REO 601R-53-61-442. NDT HFEC CARRIED OUT IAW REO'S 601R-53-61-345 AND 601R-53-61-442. 2 L 7 2 4F RT A21EA 2001112700159 20011127 00159 SO 2001 11 27 SWIA200110352 1 20011111 A 2131 22201T011400 CONTROLLER EMB 120 EMB120ER 3260203 SO CABIN PRESSURE MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 213SW 120277 WHILE ADVANCING POWER LEVERS FOR TAKEOFF, PRESSURIZATION SYSTEM WENT TO FULL SCALE (>2000 FPM) DOWN. ABORTED TAKEOFF AN D SYSTEM WENT FULL SCALE UP. CHECKED ALL SWITCHES AND CONFIRMED SYSTEM WAS IN AUTO MODE. INSTALLED ELECTRONIC ALTITUDE CONTROLLER. OPS CHECK AUTO AND MANUAL PRESSURIZATION GOOD WITH BREAKOUT BOX. 2 L 7 2 4T RT A31SO 2001112700160 20011127 00160 SO 2001 11 27 SWIA200110353 1 20011111 A 3230 12043270501 CONTROL BOX EMB 120 EMB120ER 3260203 SO LANDING GEAR MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 213SW 120277 LANDING GEAR LEVER WAS SELECTED TO DOWN POSITION AND THE GEAR DID NOT COME DOWN. USED ELECTRIC OVERRIDE TO LOWER THE LA NDING GEAR. REPLACED RELAY CONTROL BOX ASSEMBLY. C/W OPS CHECK AND GEAR SWING. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001112700161 20011127 00161 SO 2001 11 27 SWIA200110354 1 20011114 A 3260 PROXIMITY SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT MLG MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 294SW 120325 VIBRATION AND NOISE DURING ROTATION AT TAKEOFF, THEN RIGHT SYSTEM B-GREEN GEAR LIGHT WOULD NOT EXTINGUISH WITH GEAR HAND LE IN UP POSITION. CHECKED GEAR DOOR AND LINKAGE AT RIGHT MAIN GEAR AND FOUND GOOD. CYCLED GEAR FOUND B-SYSTEM PROXIMI TY SENSOR BAD. DEFERRED RIGHT GEAR B-SYSTEM INDICATION PER MEL 32-60-1C. TROUBLESHOT RT MAIN (B) INDICATION INTERMITTE NT, FOUND THE FOLLOWING; PROXIMITY SENSOR CAPS WITHIN LIMITS, HARNESS INTEGRITY GOOD, PROXIMITY SENSOR ALIGNMENT GOOD, C LEANED CANNON PLUGS. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001112800001 20011128 00001 SO 2001 11 28 C2XA01TY189 1 20011127 A 3350 1683 BULB EMB EMB 145 EMB145ER 3260211 SO DOOR WAY BLOWN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14940 NA 145033 TYS During a scheduled routine check the emergency light at the cabin door was not working. Maintenance found the wrong bulb installed, removed and replaced the bulb, operational checked good, I.A.W.-EMB-145-mm-33-50-00. Aircraft released for service. 2 L 7 2 4F RT T00011AT 2001112800002 20011128 00002 NM 2001 11 28 C1HA200184015 1 20011124 A 2560 FLASHLIGHT BOEING 727 7272S7 138407Z NM INOPERATIVE A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 684CA 22491 3EA Emergency flash light inop. Replaced as necessary per MM 33-50-01. 2 L 7 3 4F A3WE 2001122000056 20011220 00056 NM 2001 12 20 0104625507 1 20011126 A 4940 5198586 STARTER BOEING 757 757251 1384970 NM APU DEFECTIVE A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 01 507US 39033 1863 23196 WHILE AT THE GATE, STRONG BURNING SMELL/ODOR BEGAN TO ENTER THE COCKPIT AND CABIN. PASSENGERS WERE DEPLANED THROUGH THE JETWAY. MAINTENANCE FOUND THE APU STARTER EMITTING BURNING ODOR CONTAMINATING APU BLEED AIR. APU STARTER REPLACED. 2 L 7 2 4F RT A2NM 2001112800003 20011128 00003 EU 2001 11 28 SABA011066 1 20011120 A 2840 WARNING SYSTEM BAG JETSTM JETSTM3201 1500217 EU COCKPIT MALFUNCTIONED A SABA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 33 964AE 964 AIRCRAFT 964 ON FLIGHT 5070 TAKEOFF WAS ABORTED DUE TO FUEL LOW PRESSURE LIGHT ILLUMINATING. NO EMERGENCY PROCEDURES WE RE USED. AIRCRAFT RETURNED TO GATE. AIRCREW RAN AIRCRAFT IN ALL RANGES AND CHECKED GOOD. DISCREPANCY WAS DEFERRED TO MSL 112001-02C. AFTER ARRIVING IN CHARLOTTE, MAINTENANCE RAN AIRCRAFT IN ALL RANGES, ALL FUEL PRESSURES WERE GOOD. MSL WAS CLEARED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A56EU 2001112800004 20011128 00004 SO 2001 11 28 SWIA200110355 1 20011114 A 5246 FASTENER EMB 120 EMB120RT 3260202 SO FUEL DOOR LOOSE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 196CA 120196 SERVICE DOOR LIGHT ILLUMINATED ON CLIMB THROUGH 10,000 FEET. LIGHT WENT OUT ON DESCENT WHILE SLOWING. RETURNED TO FAT. FOUND 1 CAMLOCK ON INBOARD FUEL SERVICE DOOR LOOSE. RESECURED CAMLOCK AND INSPECTED ALL SERVICE DOORS MICROSWITCHES. NO FAULTS FOUND. WARNING SYSTEM CHECKS GOOD. 2 L 7 2 4T RT A31SO 2001112800005 20011128 00005 EA 2001 11 28 SWIA200110356 1 20011113 A 2751 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A SWIA K NONE F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 NM 07 594SW 7285 FLAP FAIL CAUTION ON AT DEPLOYMENT TO 8 DEGREES. C/W AD 98-20-01. FLAP FAIL MESSAGE RESET. CHECKS OK. 2 L 7 2 4F RT A21EA 2001112800006 20011128 00006 SO 2001 11 28 SWIA200110357 1 20011112 A 5610 WINDSHIELD EMB 120 EMB120ER 3260203 SO COCKPIT CRACKED A SWIA K NONE O OTHER TX TAXI/GRND HDL 1 NM 07 234SW 120308 DURING TAXI IN, CAPTAIN'S WINDSHIELD OUTER LAYER SHATTERED. PRIOR TO WINDOW BREAKING, THE WIPER WAS OPERATING AND MAKIN G AN UNUSUAL NOISE. REMOVED AND REPLACED CAPTAIN'S SIDE WINDSHIELD IAW EMB 120 MM 56-10-01. 2 L 7 2 4T RT A31SO 2001112800007 20011128 00007 EA 2001 11 28 SWIA200110358 1 20011119 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA NLG OUT OF ADJ A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 408SW 7055 AFTER TAKEOFF AND SELECTING GEAR LEVER UP GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGES ILLUMINATED IN EICAS. CONSU LTED QRH AND RETURNED TO AIRPORT. ADJUSTED GAP ON OLEO STRUT - CENTERED PROXIMITY SENSOR PER 32-61-05. JACKED AIRCRAFT AND CYCLED GEAR. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2001112800008 20011128 00008 EA 2001 11 28 SWIA200110360 1 20011115 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DEFECTIVE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 412SW 7101 AT 1500 FT AGL PASSENGER DOOR UNSAFE CAUTION AT 11,000 FT. RED PASSENGER DOOR UNSAFE MESSAGE. RETURNED TO AIRPORT. IN SPECTED PASSENGER DOOR FOR LOOSE OR DAMAGED PARTS. REPLACED OUTER HANDLE AND INNER HANDLE DETENT ROLLER (CLEANED). PRE SSURIZED TO APPROXIMATELY 6 PSI. OPS AND LEAK CHECK GOOD IAW 52-10-04. 2 L 7 2 4F RT A21EA 2001112800009 20011128 00009 2001 11 28 SWIA200110361 4 20011116 A 3422 6225812004 FLUX DETECTOR EMB 120 EMB120ER 3260203 SO LT & RT FAULTY A SWIA A UNSCHED LANDING J I WARNING INDICATION FLT. ATTITUDE INST. CL CLIMB 1 NM 07 224SW 120294 FIRST OFFICER'S HDG AND GYRO FLAGS ON EHSI & ADI. REMOVED AND REPLACED LEFT AND RIGHT FLUX DETECTORS PER 34-21-03. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001112800010 20011128 00010 NM 2001 11 28 NACA20010040 1 20011127 A 2610 182528003752 DETECTOR PWA 7B BOEING 727 72746 1384013 NM #3 ENGINE GROUNDED A NACA K NONE N FALSE WARNING CR CRUISE 1 AL 03 190AJ 995 655399 18878 DISCREPANCY: Fire detection light on #3 engine came on in flight. (ground fault).CORRECTIVE ACTION: Replaced #3 engine fire detector. 2 L 7 3 4F A3WE 2001112800011 20011128 00011 2001 11 28 SWIA200110362 4 20011116 A 3460 8220021202 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 07 427SW 7497 SMELL OF SMOKE. FMS UNIT WAS HOT TO TOUCH AND LOSS OF COLORS ON SCREEN. REMOVED AND REPLACED FMS UNIT PER CRJ MM 34-16 -01. 2 L 7 2 4F RT A21EA 2001112800012 20011128 00012 SO 2001 11 28 SWIA200110363 1 20011120 A 2997 GROUND WIRE EMB 120 EMB120ER 3260203 SO LT MLG WW LOOSE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 188SW 120039 LEFT GEAR WELL EMITTED A SHOWER OF SPARKS WHEN THE LEFT ELECTRIC HYDRAULIC PUMP WAS TURNED ON. FABRICATED AND INSTALLED DOUBLER OVER ARC-WELDED HOLE AND RE-ATTACHED GROUND FOR HYDRAULIC PUMP IAW SRM 51-70-06 AND 51-40-02. 2 L 7 2 4T RT A31SO 2001112800013 20011128 00013 NM 2001 11 28 UPS01437327 1 20011103 A 5320 STRAP BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C, 3 EACH CRACKS FOUND AT BS 2231 RT SIDE BETWEEN S24R TO S26R AT THE FRAME STRAP FWD COLUMN OF FASTENER S CRACK LENGTH FROM .125 INCH, .25 INCH AND .5 INCH LONG RESPECTIVELY. S24R TO S26R FRAME STRAP REPAIRED AS PER SRM 53- 10-04 FIG 115. 2 L 7 4 4F RT A20WE 2001112800014 20011128 00014 EA 2001 11 28 SWIA200110367 1 20011122 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 07 409SW 7056 LEFT WINDSHIELD STARTED CRACKING DURING TAXI OUT. REMOVED & REPLACED LEFT WINDSHIELD PER MM 56-11-01 & RII56-401. OPS C HECK/LEAK CHECK GOOD. PN ON NP-139321-9 SN OFF 00151H8911. 2 L 7 2 4F RT A21EA 2001112800015 20011128 00015 EA 2001 11 28 SWIA200110370 1 20011118 A 5240 FASTENER CNDAIR CL600 CL6002B19 1900309 EA ACCESS DOOR UNLATCHED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 426SW 7468 SHORTLY AFTER TAKEOFF HIGH PITCH SQUEAL EMITTED FROM LEFT FRONT OF AIRCRAFT. RETURNED TO SLC. FOUND THUMB LATCH ON EXTE RNAL ACCESS PANEL UNLATCHED. INSPECTED DOOR AND RE-SECURED THUMB LATCH AS REQUIRED. NO DAMAGE NOTED. 2 L 7 2 4F RT A21EA 2001112800016 20011128 00016 NM 2001 11 28 UPS01437332 1 20011103 A 5311 FRAME BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C RT TUNNEL BS 320 STR 41 AFT CORNER NR 5 RIVET HOLE (COUNTER FROM I/B TO O/B) FOUND A RIVET HOLE CRACKE D AS MARKED (AFT BOTTOM ANGLE REMOVE FINDING. FRAME REPAIRED AS PER SRM 54-40-03 FIG 1, CHORD REPAIRED AS PER SRM 51-40 -04 FIG 2. 2 L 7 4 4F RT A20WE 2001112800017 20011128 00017 NM 2001 11 28 UPS01437334 1 20011103 A 5311 FRAME BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C CRACK FOUND AT ONE FASTENER HOLE AT LT SIDE OF BS 1265 FRAME WEB JUST BELOW FLOOR LEVEL AREA. TWO CRA CKS FOUND AT THE HOLE - ONE IS .25 INCH LONG AT FIVE O'CLOCK AND ANOTHER IS .0625 INCH LONG AT 11 O'CLOCK POSITION ON (L OOKING FWD). REPAIR CARRIED OUT AS PER EO B747-5310-12070-I. 2 L 7 4 4F RT A20WE 2001112800018 20011128 00018 NM 2001 11 28 UPS01537331 1 20011121 A 2913 PUMP BOEING 757 75724APF 1384969 NM LT ENGINE LEAKING A IPXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 453UP 25474 INSPECTION TYPE:N/A LOST LT HYDRAULIC QTY IN FLIGHT LEFT HYD SYS FAILURE IN FLT (LOW QTY) PUMPS ON, NO FLUID FOR 5 MIN. PUMPS OFF FOR 37 MIN, NO FLUID FOR 37 MIN. REPLACED EDP PER MM 29-11-05. OPS CHECK AND LEAK CHECK GOOD. HYD LINES AT PUMP FLUSHED. REPLACED CASE DRAIN AND PRESS FILTERS. SERVICED SYSTEM AND RAN LT ENG. REPLACED CASE DRAIN AND PRESS FILTERS PRECAUTIONARY (FILTERS BOTH TIMES WERE CLEAN) AGAIN. LEAK CHECK GOOD. ALL WORK PERFORMED FOR LT SYS. 2 L 7 2 4F RT A2NM 2001112800019 20011128 00019 NM 2001 11 28 UPS01637321 1 20011120 A 5754 PANEL BOEING 767 76734AF 1385212 NM L/E SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 314UP 27742 INSPECTION TYPE:IN L-SHAPED CRACK IN NR 6 L/E SLAT LOWER SIDE, FWD OF INBOARD TRACK. REPAIRED SLAT CLOSE OUT PANEL AS P ER SRM 51-70-07. 2 L 7 2 4F RT A1NM 2001112800021 20011128 00021 WP 2001 11 28 UPS01837283 1 20011112 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT BATTERY PACK DISCHARGED. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. 2 L 7 4 4F RT 4A25 2001112800022 20011128 00022 WP 2001 11 28 UPS01837284 1 20011113 A 3350 LIGHT DOUG DC8 DC873F 302199F WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:N/A EMERGENCY LIGHT WILL NOT DISARM. RELAMPED EMERGENCY DISARM LIGHT, OPS CHECKS GOOD. 2 L 7 4 4F RT 4A25 2001112800023 20011128 00023 WP 2001 11 28 UPS01837288 1 20011113 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:N/A EMERGENCY LIGHTS ON CREW PREFLT APPEARS INOP. REMOVED AND REPLACED BATTERY PACK, TESTED OK. 2 L 7 4 4F RT 4A25 2001112800024 20011128 00024 WP 2001 11 28 UPS01837289 1 20011109 A 3350 LIGHT DOUG DC8 DC873F 302199F WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:N/A EMERGENCY DISARM LIGHTS WILL NOT DISARM. RELAMPED EMERGENCY DISARM LIGHT, OPS CHECKS GOOD. 2 L 7 4 4F RT 4A25 2001112800025 20011128 00025 WP 2001 11 28 UPS01837311 1 20011116 A 3350 LIGHT DOUG DC8 DC873F 302199F WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:N/A EMERGENCY DISARM LIGHTS WILL NOT DISARM. RELAMPED EMERGENCY DISARM LIGHT. OPS CHECKS GOOD. 2 L 7 4 4F RT 4A25 2001112800026 20011128 00026 WP 2001 11 28 UPS01837315 1 20011114 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:N/A RT WING T/E RIB CRACKED AT FORWARD SURFACE VERTICAL CHANNEL AT XW33. THIRD OUTBOARD WAS PREVIOUSLY REPAIRED PER A/C ENGINEERING AMC HAS ASSIGNED INFORMATIONAL ITEM I226648 ASSIGNED. 2 L 7 4 4F RT 4A25 2001120500080 20011205 00080 WP 2001 12 5 UPS01837316 1 20011117 A 5210 DOOR FRAME DOUG DC8 DC871F 302199D WP ENTRY DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:IN COCKPIT DOOR DAMAGED - CREW FWD ENTRY DOOR HAS A CRACK IN THE AFT DOOR FRAME NEAR LATCH. REMOVED 2 D OOR STOP FITTINGS AND FASTENERS 6 INCHES ABOVE AND BELOW DAMAGE. DYE PEN INSPECTED DAMAGED AREA. STOP DRILLED 1.125 IN CH CRACK. VERIFIED STOP DRILL ENDS OF CRACK. INSTALLED REPAIR IAW EO DC8-5310-1 5740 COMPLETED. 2 L 7 4 4F RT 4A25 2001112800027 20011128 00027 WP 2001 11 28 UPS01837317 1 20011114 A 5610 WINDOW DOUG DC8 DC871F 302199D WP COCKPIT LEAKING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:IN LOUD SQUEAL FROM CAPTAIN`S CLEAR VIEW WINDOW TOP. CHECKED CAPTS CLEAR VIEW WINDOW SEAL FOUND NO EVID ENCE OF SEAL TORN. CLEANED WINDOW SEAL AND FRAME. PRESSURIZED AND NO NOTICE OF LOUD SQUEAL. 2 L 7 4 4F RT 4A25 2001112800028 20011128 00028 WP 2001 11 28 UPS01837318 1 20011119 A 3350 6012235 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:N/A EMERGENCY LIGHTS WILL NOT COME ON WHEN ACTIVATED. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS BATTER Y PACK PER DC8 MM 33-50-01. OPS OK. 2 L 7 4 4F RT 4A25 2001112800029 20011128 00029 WP 2001 11 28 UPS01837319 1 20011120 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:IN EMERGENCY LIGHTS FAILED TO TEST. REMOVED AND REPLACED BATTERY PACK. 2 L 7 4 4F RT 4A25 2001112800030 20011128 00030 WP 2001 11 28 UPS01837320 1 20011119 A 3350 6012235 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:IN EMERGENCY LIGHTS WOULD NOT COME ON. REMOVED EMERGENCY BATTERY PACK. LIGHTS OPS CK OK. 2 L 7 4 4F RT 4A25 2001120500097 20011205 00097 WP 2001 12 5 UPS01837322 1 20011120 A 5754 FRAME DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE: IN, FORMER CRACKED JUST INBOARD OF ACCESS PNL 523 LT WING L/E. REMOVED RIVETS IN AREA OF CRACK. FABR ICATED AND DRILLED REPAIR PARTS PER SRM 57-2-0. INSTALLED FASTENERS IAW DC8 SRM 51-20-1. 2 L 7 4 4F RT 4A25 2001112800031 20011128 00031 WP 2001 11 28 UPS01837323 1 20011120 A 5310 DOOR FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:IN CRACK IN COCKPIT DOOR FRAME, JUST ABOVE AND OUTBOARD OF DOOR (CLOSED) CATCH. INSTALLED DOUBLER ON DO OR FRAME AT DOOR CATCH PER DC-8 SRM 53-2-0. 2 L 7 4 4F RT 4A25 2001112800032 20011128 00032 SO 2001 11 28 C2XA01CL233 1 20011127 A 3233 21180100011 ACTUATOR EMB 135 EMB135ER 3260203 SO NOSE GEAR LEAKING A C2XA O OTHER E VIBRATION/BUFFET CL CLIMB 1 SW 27 27512 3066 145274 CLE FLIGHT#3128 THE CREW REPORTED INFLIGHT WITH GEAR UP INDICATION.THERE WAS A LOUD NOISE AND VIBRATION COMING FROM THE NOSE AREA.THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND FOUND THE RIGHT HAND NOSE LANDING GEAR DOOR ACTUATOR LEAKING.THEY REPLACED THE ACTUATOR AND OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT TEST FLIGHT WAS GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001112800033 20011128 00033 NE 2001 11 28 UPS01837333 2 20011123 A 7200 ENGINE DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE NR 3 FLAMED OUT A IPXA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 SO 01 709UP 45914 INSPECTION TYPE:N/A AT FL370 NR 3 ENG BEGAN TO ROLLBACK SLOWLY. NO RESPONSE TO THROTTLE. TURNED OFF PMC, NO HELP. ATT EMPTED RESTART AT FL330, NO RESTART. ATTEMPTED 2ND RESTART AT 17000 FT, NORMAL START. PERFORMED FUEL LINE NEGATIVE PRE SSURE CHECK IAW MM 28-22-12, NO DEFECTS NOTED. BEGAN T/S OF NR 3 FLAME-OUT PER 71-00-00. REPLACED FUEL FILTER IAW 73-1 0-01 MM AS PRECAUTIONARY. NO DEFECTS NOTED IN FILTER. ACCOMPLISHED TROUBLESHOOTING OF ENG FLAME-OUT AS PER M/M. 2 L 7 4 4F 4 F RT 4A25 E2GL 2001112800034 20011128 00034 WP 2001 11 28 UPS01837335 1 20011124 A 5410 FITTING DOUG DC8 DC873F 302199F WP NR 3 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:B NR 3 ENGINE PYLON AFT SPAR TO CANTED RIB FITTING CRACKED. 2 L 7 4 4F RT 4A25 2001120500098 20011205 00098 WP 2001 12 5 UPS01837336 1 20011123 A 5320 SUPPORT DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:B LT VERT MAIN SUPPORT ANGLE ON AFT SIDE OF AFT PRESS BULKHEAD IS CRACKED IN HALF ABOUT 1 INCH FROM TOP OF BULKHEAD (AS VIEWED FROM LT ACCESS HOLE IN CANTED BULKHEAD). *S/D* LT VERT SUPPORT ANGLE P/N 57735701 1 PREVIOUSLY REPAIRED IN 4-94 IAW UPS EO DC8 5310 5665A BY INSTALLING 53 503 REV DOUGLAS FAA APPROVAL MISC 1742/GLP AND DC8. 2 L 7 4 4F RT 4A25 2001120500109 20011205 00109 WP 2001 12 5 UPS01837337 1 20011124 A 5230 HINGE FITTING DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:N/A PIT34 LWR AFT BELLY CARGO DOOR UPPER FWD HINGE POINT STRUCTURE CRACKED. DOOR COMES OFF TRACK AND WI LL NOT CLOSE. CLOSED DOOR AND TAPED HANDLE IN STOWED POSITION. REPAIRED IAW DC8 SRM 52-2-0 LOG PAGE 780026 AND 780028. 2 L 7 4 4F RT 4A25 2001112800035 20011128 00035 2001 11 28 VNAA0110020 4 20011026 A 3418 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 426JS 3038 DURING TAKEOFF, THE CREW RECEIVED A PUSHER FAIL AND AOA CAS MESSAGES AND ABORTED TAKEOFF. THE MESSAGES WENT OUT ALMOST IMMEDIATELY AND THE CREW ATTEMPTED ANOTHER TAKEOFF. FLIGHT 4052 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001112800036 20011128 00036 NM 2001 11 28 VNAA0111001 1 20011101 A 3150 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 440JS 3058 AT THE BEGINNING OF THE TAKEOFF ROLL, THE CREW RECEIVED A TAKEOFF CONFIGURATION CAS MESSAGE AND ABORTED TAKEOFF. MAINTE NANCE ALONG WITH THE CREW INSPECTED AND TROUBLESHOT THE PROBLEM BUT COULD NOT DUPLICATE OR FIND ANY DISCREPANCIES. FLIG HT 4190 WAS CLEARED FOR ANOTHER TAKEOFF, ATTEMPT AND DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001112800037 20011128 00037 2001 11 28 VNAA0111002 4 20011102 A 3418 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 426JS 3038 AT THE BEGINNING OF THE TAKEOFF ROLL, THE CREW RECEIVED A PUSHER CAS MESSAGE AND ABORTED TAKEOFF. AFTER CLEARING THE RU NWAY THE MESSAGES CLEARED. THE CREW AND MAINTENANCE FELT THE STRONG WINDS HAD CAUSED THESE INDICATIONS AND FLIGHT 4032 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4032 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001112800038 20011128 00038 NM 2001 11 28 VNAA0111003 1 20011102 A 2432 DTSP400L BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LEFT OVERHEATED A VNAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 440JS 12939 3058 DURING CRUISE, THE CREW RECEIVED A RED WARNING PANEL INDICATION FOR A NR 2 BATTERY OVERHEAT. MAINTENANCE CONTROL REQUES TED THAT FLIGHT 4169 TO RETURN TO PIT WHERE MAINTENANCE REPLACED THE NUMBER 2 MAIN BATTERY IN ACCORDANCE WITH DORNIER MA INTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001112800039 20011128 00039 NM 2001 11 28 VNAA0111004 1 20011105 A 2450 230GC02Y03 PANEL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FAILED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 436JS 8788 3052 DURING CLIMBOUT, THE CREW RECEIVED A RIGHT HAND GENERATOR FAIL CAS MESSAGE AND RETURNED TO PIT. MAINTENANCE INSPECTED A ND REPLACED THE 1VE PANEL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001112800040 20011128 00040 NM 2001 11 28 VNAA0111005 1 20011112 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 437JS 12743 3055 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 3, 4, AND 5 WERE BLINKING. MAINTENANCE INSPECTED AND REPLACED THE 5LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND TH E AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001112800041 20011128 00041 NM 2001 11 28 VNAA0111006 1 20011113 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 328JS 2640 3030 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 6, 7, AND 8 WERE NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE 6LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001112800042 20011128 00042 NM 2001 11 28 VNAA0111007 1 20011116 A 2450 230GC02Y03 PANEL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 461PS 839 3075 WHILE CLIMBING THROUGH 6,000 FEET, THE CREW RECEIVED A LEFT HAND GENERATOR FAIL CAS MESSAGE AND RETURNED TO PIT AFTER TH E QUICK REFERENCE HANDBOOK PROCEDURE DID NOT RESET THE GENERATOR. MAINTENANCE INSPECTED AND REPLACED THE 1VE PANEL IN A CCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001112800043 20011128 00043 WP 2001 11 28 WRNA200100018 1 20011113 A 2170 COVER HAMSTD LKHEED 1011 10113851 5265010 WP WATER SEPARATOR SEPARATED A WRNA J A DUMP FUEL UNSCHED LANDING O OTHER CR CRUISE 1 SO 05 311EA 193A1012 AT 27,000 FEET NR 2 PACK WATER SEPARATOR COVER BLEW OFF. CREW UNABLE TO MAINTAIN PRESSURIZATION ON NR 3 PACK ONLY. AIR CRAFT RETURNED TO BQN. FUEL DUMPED. AIRCRAFT LANDING NORMAL. WATER SEPARATOR COVER REINSTALLED AND CLAMP SECURED AND TORQUED IAM MM 21-51-07. OPERATIONAL CHECK AND LEAK CHECK PERFORMED. 2 L 7 3 4F A23WE 2001112800044 20011128 00044 NM 2001 11 28 AWXA200100601 1 20011128 A 3350 BMS13311122 WIRE BOEING 737 7373G7 1384595 NM SEAT 5 DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 LAS - EEL - "C" - EMERGENCY LIGHT AT SEAT 5 INOPERATIVE. REPAIRED DAMAGED WIRE AT SEAT 5, OPERATIONALLY CHECKED GOOD. 2 L 7 2 4F RT A16WE 2001112800045 20011128 00045 NM 2001 11 28 AWXA200100602 1 20011124 A 3350 14803180 PLUG BOEING 737 7373G7 1384595 NM SEAT 19 DISCONNECTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 24634 LAS - EEL - "C" - DURING MAINTENANCE INSPECTION FOUND EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT ROW 19. RECONNECTED PLU G SEAT 19 L/H, OPERATIONALLY CHECKED GOOD. 2 L 7 2 4F RT A16WE 2001112800046 20011128 00046 EU 2001 11 28 XN0A01029 1 20011106 A 3230 MODULE AIRBUS 300 A300B4203 3930306 EU LANDING GEAR MALFUNCTIONED A XN0A A UNSCHED LANDING O OTHER CL CLIMB 1 GL 23 473AS 203 AFTER TAKEOFF AT GEAR RETRACT, GEAR HANDLE WOULD NOT GO PAST NEUTRAL. PERFORMED QRH L/G LEVER INTERLOCKED CHECK LIST. TRIED SYS 2 AND SAME AS SYS 1, GEAR HANDLE NEUTRAL. NO OTHER LIGHTS ONLY DOWN GREEN ARROWS. REMOVED AND REPLACED POSIT ION DETECTOR UNIT AND LANDING GEAR SWITCH MODULE. PERFORMED GEAR SWING IAW A300MM 32-30-00. OPS CHECK NORMAL. 2 L 7 2 4F RT A35EU 2001112800047 20011128 00047 WP 2001 11 28 ZW0A0110701 1 20011105 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 927TW 49358 DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR SUPPORTS BELOW FLOOR PANELS NUMBER 2 AND 3 A & B, STA 160 TO 200. R EMOVED CORRODED SUPPORTS. FABRICATED AND INSTALLED NEW SUPPORTS PER SPM 6-70-01. 2 L 7 2 4F A6WE 2001112800048 20011128 00048 WP 2001 11 28 ZW0A0110702 1 20011105 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 913TW 49184 DURING CHECK-C MAINT FOUND CABIN FLOOR AT L-1 CABIN DOOR, THE OUTBOARD SUPPORT FOR FLOOR PANEL NUMBER 16 WAS CORRODED. REPLACED SUPPORT PER SPM 6-70-01. 2 L 7 2 4F A6WE 2001112800049 20011128 00049 WP 2001 11 28 ZW0A0110703 1 20011106 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 913TW 49184 DURING CHECK-C MAINT FOUND FLOOR TRACK AT LBL 44, STA 1260 TO 1300, HAD CORROSION. REPLACED TRACK FROM STA 1041 TO 1309 PER SRM 53-05, FIG 4F. 2 L 7 2 4F A6WE 2001112800050 20011128 00050 WP 2001 11 28 ZW0A0110801 1 20011107 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9619V 53566 DURING CHECK-C MAINT IN THE AFT CARGO COMPT THE RT FLOOR TRACK WAS CORRODED AROUND NUT PLATE HOLES IN SEVERAL LOCATIONS, STA 1211 TO 1322. MADE AND INSTALLED NEW CARGO TRACK PER SPM 6-70-01, PAGE 3, AND DOUGLAS PRINT 5936663. 2 L 7 2 4F RT A6WE 2001112800051 20011128 00051 WP 2001 11 28 ZW0A0110802 1 20011107 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 927TW 49358 DURING CHECK-C MAINT FOUND FLOOR SUPPORT CORROSION AT LBL 54, BETWEEN STA 160 TO 200. REPLACED SUPPORT PER SPM 6-70-01. 2 L 7 2 4F A6WE 2001112800052 20011128 00052 WP 2001 11 28 ZW0A0110803 1 20011107 A 5320 FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 927TW 49358 DURING CHECK-C MAINT FOUND LIGHT SURFACE CORROSION ON CABIN FLOORBEAM AT STA 218, BL 0, AND ON AFT INBOARD GALLEY HOLD D OWN FITTING. REMOVED CORROSION, TREATED AND PAINTED FLOORBEAM PER SRM 51-10-3. REMOVED AND REPLACED GALLEY FLOOR FITTI NG PER SPM 6-70-01 AND SPM 6-80-01. 2 L 7 2 4F A6WE 2001112800053 20011128 00053 WP 2001 11 28 ZW0A0110804 1 20011108 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 913TW 49184 DURING CHECK-C MAINT, THE NUMBER 1 (LT OUTBOARD) FLOOR TRACK WAS CORRODED BEYOND LIMITS AT STA 797 TO 1003. REPLACED FL OOR TRACK PER SRM 51-30-1 AND SPM 6-70-01. 2 L 7 2 4F A6WE 2001112800054 20011128 00054 NM 2001 11 28 ZW0A0110901 1 20011104 A 3350 362624 LIGHT BOEING 767 7673Q8 1385142 NM CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 634TW 28132 THE CABIN EGRESS LIGHTS WERE INOPERATIVE AT SEAT 5H, BETWEEN ROW 16 AND 23 ON RT SIDE, AND AT THE J LAVATORY. REPLACED FLEX LAMP P/N 36262-4 AT SEAT 5H, RECONNECTED LOOSE WIRES FOR ROW 16 TO 23, AND REPLACED FLEX LAMP P/N 36262-4 AT THE J LAVATORY. 2 L 7 2 4F RT A1NM 2001112800055 20011128 00055 NM 2001 11 28 ZW0A0110904 1 20011110 A 3350 LIGHT BOEING 767 76733AER 1385230 NM CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 637TW 25403 THE CABIN EGRESS LIGHT WAS INOPERATIVE ON THE LT SIDE OF FIRST CLASS, AT SEATS 12B AND 22H, AND WAS MISSING AT SEAT 6B. REPLACED POWER SUPPLY P/N 5822-43 FOR FIRST CLASS, CONNECTED LOOSE LAMP ASSEMBLY AT SEAT 12B, REPLACED LAMP ASSEMBLY P/ N 36262-4 AT SEAT 22H, AND INSTALLED MISSING FLEX LAMP P/N 36262-4 AT SEAT 6B. 2 L 7 2 4F RT A1NM 2001112800056 20011128 00056 WP 2001 11 28 ZW0A0111001 1 20011109 A 5320 SILL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 913TW 49184 DURING CHECK-C MAINT THE AFT CARGO COMPT DOOR SILL WAS CORRODED AT STA 1155 TO 1212. INSTALLED NEW BEAM PER SPM 6-70-1, SRM 51-30-2 AND SRM 51-30-5. TREATED AREA PER SRM 51-10-3. 2 L 7 2 4F A6WE 2001112800057 20011128 00057 WP 2001 11 28 ZW0A0111002 1 20011111 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 913TW 49184 DURING CHECK-C MAINT THE FLOOR SUPPORT HAD A 4 INCH CRACK AT STA 927, LBL 44, BELOW THE OUTBOARD TRACK. INSTALLED BEAM PER DOUGLAS DRAWING 593056, P/N 9915527-505. 2 L 7 2 4F A6WE 2001112800058 20011128 00058 WP 2001 11 28 ZW0A0111003 1 20011112 A 5320 THRESHOLD DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 913TW 49184 DURING CHECK-C MAINT THE AFT EMERGENCY DOOR (VAULT DOOR) THRESHOLD PLATE BELOW THE FLOOR LINE WAS HEAVILY CORRODED. REP AIRED AREA PER 51-10-3, 51-30-2, AND 51-30-8. 2 L 7 2 4F A6WE 2001112800059 20011128 00059 WP 2001 11 28 ZW0A0111101 1 20011109 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9619V 53566 DURING CHECK-C MAINT IN THE AFT CARGO COMPT, STA 1221 TO 1332, THE LT FLOOR TRACK HAD CORROSION AROUND NUT PLATE HOLES I N SEVERAL LOCATIONS. INSTALLED NEW TRACK AND FASTENERS PER PRINT 5936663-503, AND SRM 51-30-2. 2 L 7 2 4F RT A6WE 2001112800060 20011128 00060 WP 2001 11 28 ZW0A0111102 1 20011109 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9619V 53566 DURING CHECK-C MAINT THE AFT CARGO BIN, LT FLOOR TRACK HAD CORROSION AROUND NUT PLATE HOLES IN SEVERAL LOCATIONS, STA 12 18 TO 1221. INSTALLED NEW TRACK AND FASTENERS PER PRINT 5936663-503, AND SRM 51-30-2. 2 L 7 2 4F RT A6WE 2001112800061 20011128 00061 NM 2001 11 28 TSAA0136137 1 20011016 A 3610 32895625 SEAL BOEING 737 73773A 1384606 NM BLEED AIR SYS WORN A TSAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 13 739AL 28500 FLT 478 - HNL-OAK/LAS - AFTER MX ACTIONS, DEPARTED HNL AND HAD NR 2 BLEED TRIP OFF, CLIMBING THROUGH 25,000 FEET. RESET AND TRIPPED AGAIN AT 26,500 FEET. RETURNED TO HNL, UNEVENTFUL LANDING. REPLACED WORN KISS SEAL P/N 32895625, (FAN AIR VALVE) JUST AFT OF NR 2 ENGINE PRECOOLER CONTROL VALVE, P/N 82C100201. REPLACED THE NR 2 ENGINE PRECOOLER CONTROL VALV E AS A PRECAUTION IAW MM 36-12-02, PAGE 401-408. OPS CHECK OK ON GROUND. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001112800062 20011128 00062 NM 2001 11 28 USAASB01295 1 20011013 A 3240 13162003 SELECTOR VALVE BOEING 737 737401 1384701 NM BRAKE SYS DEFECTIVE A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 420US 23987 LGA - FLT 579 - ON CLIMB-OUT FROM LGA, ENROUTE TO CLT, THE A/C EXPERIENCED A SEVERE VIBRATION THROUGH BOTH THE FIRST OFF ICERS AND CAPTAINS RUDDER PEDALS. THE FORWARD CABIN AREA, EXPERIENCED VIBRATION AS WELL. NO VIBRATION IN AFT CABIN AREA. TURNING OFF YAW DAMPER HAD NO EFFECT ON VIBRATION. RETURNED TO FIELD AT LGA AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MX R&R THE ALTERNATE BRAKE SELECTOR VALVE PER MM 32-41-93 AND THE LT RUDDER PEDAL ALTERNATE BRAKE METERING VALVE (P/N 1316200-3) PER MM 32-41-31. OPS CHECK AND LEAK CHECK GOOD. ACCOMPLISHED YAW DAMPER COUPLER TEST OF THE PRESS URE REDUCER PER MM 22-12-32 AND TEST OF THE FEEL AND CENTERING UNIT PER MM 27-21-82. BOTH TESTS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001112800063 20011128 00063 NM 2001 11 28 F3LA200100119 1 20011116 A 7110 NOSE COWL BOEING 737 7372L9 1384497 NM NR 1 ENGINE WORN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 3902 22733 DURING C-1 CHECK, INSPECTION REPORTED NR 1 ENGINE NOSE COWL AT 2 O'CLOCK POSITION MATING SURFACE WORN. CUT AWAY DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND FILLER PER SRM 54-10-03, 51-20-1 AND MM 51-21-99. 2 L 7 2 4F RT A16WE 2001112800067 20011128 00067 WP 2001 11 28 USAAD01178 1 20011107 A 3350 9721055 BATTERY DOUG DC9 DC982 3022082 WP PAX CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 821US 49138 BOS - THE LOW LEVEL EMERGENCY LIGHTS AT SEAT ROWS 16 AND 20 AND THE AFT CEILING PANEL EMERGENCY LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY AT SEAT ROW 16, THE LIGHT ASSEMBLY AT SEAT ROW 20, AND THE EMERGENCY L IGHT BATTERY FOR THE AFT CEILING PANEL. (M) 2 L 7 2 4F A6WE 2001112800072 20011128 00072 WP 2001 11 28 ABXA010597 1 20010730 A 5300 FINGER DOUBLER DOUG DC8 DC861 3021952 WP COCKPIT CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 843AX 46017 COCKPIT FLOOR, STATION 10, THE RIGHT SIDE HAD CORROSION AROUND AND UNDER THE FINGER DOUBLER. INSTALLED NEW FINGER DOUBLE R AND REPAIRED AREA IAW DC-8 SRM 51-1-8, 53-2-0, 51-1-21, 51-1-20D, DAC DWG. # 56I12298 AND REA D853-40886MR. 2 L 7 4 4F 4A25 2001112800073 20011128 00073 WP 2001 11 28 ABXA010598 1 20010813 A 5320 527576OR ANGLE DOUG DC8 DC861 3021952 WP CABIN CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 843AX 46017 LEFT SIDE UPPER SURFACE OF CUSP FITTING HAD CORROSION AT STAION 1060. INTALLED NEW CUSP DOUBLER AND REPAIRED AREA IAW DC -8 SRM 53-2-0, 53-2-5 AND 51-1-20D. 2 L 7 4 4F 4A25 2001112800075 20011128 00075 EA 2001 11 28 COMA0160926 1 20011124 A 2620 47259701 CONTROL BOX CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA F ACTIVATE FIRE EXT. N FALSE WARNING LD LANDING 1 SO 01 804CA 4452 7352 FLIGHT #5639 - APU FIRE WARNING DURING LANDING.COULD NOT DUPLICATE. FOUND NO EVIDENCE OF FIRE OR OVERHEAT. REPLACED TH E FIRE WARNING CONTROLLER FOR TROUBLESHOOTING. 2 L 7 2 4F RT A21EA 2001112800076 20011128 00076 EA 2001 11 28 COMA0160927 1 20011124 A 3150 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 810CA 7370 FLIGHT #5832, T/O ABORTED DUE TO SEVERAL AURAL WARNINGS.C/W RTO INSPECTION NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 2001112800077 20011128 00077 NM 2001 11 28 F3LA200100120 1 20011117 A 5414 SKIN BOEING 737 7372L9 1384497 NM RT PYLON GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 3902 22733 DURING C-1 CHECK, INSPECTION REPORTED GOUGES IN SKIN AND SCRATCHES ON OTBD SIDE OF RT ENGINE PYLON, AFT END AREA ABOVE T HRUST REVERSER FAIRING. PERFORMED TYPICAL WEB REPAIR PER SRM 51-40-01 AND 51-30-02. 2 L 7 2 4F RT A16WE 2001112800078 20011128 00078 WP 2001 11 28 MWEA011461 1 20011128 A 5240 99115793 BEAM DOUG DC9 DC915 3022036 WP GALLEY SVC DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 GALLEY SERVICE DOOR BEAM #1 HAS A CRACK ON AFT END -- STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2001112800079 20011128 00079 EA 2001 11 28 COMA0160928 1 20011125 A 5240 SERVICE DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 01 983CA 7169 FLIGHT #5363 - STALL FAIL MESSAGE AFTER T/O.FOUND 02 SERVICE DOOR OPEN WHICH DISRUPTED AIR FLOW OVER THE #2 AOA VANE. CL OSED AND LATCHED DOOR. 2 L 7 2 4F RT A21EA 2001112800080 20011128 00080 NM 2001 11 28 HNAA0100076 1 20011118 A 2900 21565 BRAKE DHAV DHC8 DHC8102 2809003 NM LEAKING A HNAA K NONE K FLUID LOSS NR NOT REPORTED 1 EA 07 908HA 2326 212 015 #1 AND #2 HYDRAULIC SYSTEMS FLUID LOSS. #2 RUDDER ISO VALVE CAUTION LIGHT ILLUMINATED. HYD PRESSURES NORMAL. ON LANDING NORMAL BRAKES FAILED. REPLACED #3 BRAKE ASSY. 2 H 7 2 4T RT A13NM 2001112800081 20011128 00081 EA 2001 11 28 COMA0160929 1 20011125 A 2841 73664310 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 926CA 11984 7027 FLIGHT #5647, FUEL GAUGE FLUCTUATING BETWEEN 7700 AND 8400 LBS.REPLACED THE FUEL COMPUTER. 2 L 7 2 4F RT A21EA 2001113000098 20011130 00098 EA 2001 11 30 COMA0160925 1 20011127 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DENTED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 798CA 7348 7348 SMALL DENT JUST FWD AND BELOW CARGO DOOR AT FS 589.00. REPAIRED DAMAGED SKIN BELOW CARGO DOOR AT FS 589.00 BY INSTALLIN G REPAIR PARTS IAW CRJ SRM 53-00-31 REPAIR NUMBER 5. 2 L 7 2 4F RT A21EA 2001120400065 20011204 00065 NM 2001 12 4 SABA011068 1 20011124 A 3260 WARNING SYSTEM DHAV DHC8 DHC8102 2809003 NM COCKPIT MALFUNCTIONED A SABA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 33 883CC 162 AFTER TAKEOFF MLG LEFT AND RIGHT DOOR/GEAR INTRANSIT LIGHTS REMAINED ILLUMINATED AND NOSE GEAR INDICATED UP AND LOCKED. CREW CYCLED GEAR AND STILL HAD MAIN GEAR/DOOR INTRANSIT LIGHTS. SELECTED GEAR DOWN AND HAD THREE GREEN DOWN AND LOCKED INDICATION. RETURNED TO FIELD WITH NO EMERGENCY DECLARED, LANDED SAFELY. MAINTENANCE PERFORMED GEAR RETRACTION CHECKS IAW DHC-8 M/M 32-30, COULD NOT DUPLICATE PROBLEM AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001112800082 20011128 00082 NM 2001 11 28 F3LA200100122 1 20011118 A 5410 PYLON BOEING 737 7372L9 1384497 NM NR 1 ENGINE GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 3902 22733 DURING C-1 CHECK, INSPECTION REPORTED GOUGE IN NR 1 ENGINE PYLON, AFT OTBD LOWER CORNER. REMOVED GOUGE PER SRM 51-10-2. FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-2. 2 L 7 2 4F RT A16WE 2001112900001 20011129 00001 NM 2001 11 29 0104635644 1 20011124 A 2160 3987865 VALVE BOEING 757 757251 1384970 NM FWD CARGO DEFECTIVE A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 544US 41917 4866 26491 Enroute after an attempt to adjust inflight deck temperature using alternate procedures specified in the COM, smoke was detected in the cabin. The procedure was terminated (trim air was turned on again) and the smoke dissipated. Maintenance replaced the Flight Compartment Trim Air Modulating Valve with a serviceable unit. System tests were satisfactory. 2 L 7 2 4F RT A2NM 2001112900002 20011129 00002 EU 2001 11 29 2001F00670 1 20011025 A 5347 7253799379 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 350CF 340B350 ABI - DURING MBV INSPECTION, FOUND CORROSION ON SEAT TRACK AT BL 18.3L, BETWEEN STATIONS 297 TO 348 TO BE OUT OF SRM LIM ITS. CUT OUT A 56 INCH SECTION OF EXISTING SEAT TRACK. PREPARED A SEAT TRACK REPAIR EXTRUSION AND A REPAIR U-BEAM. IN STALLATION DONE IAW SAAB 340 SRM (72LKS 3079 REV 38) 53-70-60, AND STANDARD SRM PRINCIPLES. REF SIMA200130302. (M) 2 L 7 2 4T RT A52EU 2001112900003 20011129 00003 WP 2001 11 29 2001F00671 1 20011107 A 3350 9731004 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 821US 49138 BOS - THE LOW LEVEL EMERGENCY LIGHTS AT SEAT ROWS 16 AND 20 AND THE AFT CEILING PANEL EMERGENCY LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY AT SEAT ROW 16, THE LIGHT ASSEMBLY AT SEAT ROW 20, AND THE EMERGENCY L IGHT BATTERY FOR THE AFT CEILING PANEL. REF USAAD01178. (M) 2 L 7 2 4F A6WE 2001112900004 20011129 00004 WP 2001 11 29 2001F006721 1 20011107 A 3350 AD4002P BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 821US 49138 BOS - THE LOW LEVEL EMERGENCY LIGHTS AT SEAT ROWS 16 AND 20 AND THE AFT CEILING PANEL EMERGENCY LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY AT SEAT ROW 16, THE LIGHT ASSEMBLY AT SEAT ROW 20, AND THE EMERGENCY L IGHT BATTERY FOR THE AFT CEILING PANEL. REF USAAD01178. (M) 2 L 7 2 4F A6WE 2001112900005 20011129 00005 NM 2001 11 29 2001F00673 1 20011103 A 4990 OIL SYSTEM BOEING 737 7378Q8 13844BX NM APU LOW A NOCA K NONE J WARNING INDICATION CR CRUISE 1 EA 15 800NA 28215 APU LOW OIL PRESSURE LIGHT ILLUMINATED IN FLIGHT FOLLOWED BY APU AUTO SHUTDOWN. A/C CONTINUED FLIGHT 60 MINUTE RULE. O N GROUND SERVICED APU OIL AND CHECKED APU FOR LEAKS, NONE FOUND. APU OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2001112900006 20011129 00006 NM 2001 11 29 2001F00674 1 20011022 A 5743 PIN BOEING 727 727225 1384077 NM RT WING DAMAGED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 886MA 21855 RIGHT WING OUTBOARD LG WALKING BEAM PIN AND BUSHING NEEDS REWORK AND R/R. REPAIRED RIGHT WING OUTBOARD LANDING GEAR WAL KING BEAM PIN AND BUSHING PER BOEING TLX NR MIB-MIA-01-00091H. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001112900007 20011129 00007 NM 2001 11 29 ASAA0110165 1 20010330 A 5315 6554906 FLOORBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 500B, RIGHT BUTTOCK LINE 24, LEFT BUTTOCK LINE 44, CORRODED. REPA IRED PER EA. (M) 2 L 7 2 4F RT A16WE 2001112900008 20011129 00008 NM 2001 11 29 ASAA0110201 1 20010406 A 5320 6941757503 INTERCOSTAL BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL AT BS 500B-520, STRINGER 25L-26L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001112900009 20011129 00009 NM 2001 11 29 ASAA0110476 1 20010706 A 5320 6546877137 STRAP BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND STRAP AT BS 690-693, LEFT BUTTOCK LINE 60-66 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001112900010 20011129 00010 NM 2001 11 29 ASAA0110477 1 20010706 A 5320 65593733 STRAP BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND STRAP AT BS 540-727, LEFT BUTTOCK LINE 60 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001112900011 20011129 00011 NM 2001 11 29 ASAA0110478 1 20010706 A 5320 6546877143 STRAP BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND STRAP AT BS 680-690, LEFT BUTTOCK LINE 60-66 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001112900012 20011129 00012 NM 2001 11 29 ASAA0110479 1 20010707 A 5320 6546877145 INTERCOSTAL BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL AT BS 685, LEFT BUTTOCK LINE 60-66 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001112900013 20011129 00013 WP 2001 11 29 AT0100236 1 20011129 A 3350 41B004AD0763 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 866AT 47168 FOUND EMERGENCY LIGHTS WILL NOT EXTINGUISH. CORRECTIVE ACTION: REMOVED AND REPLACED NICAD BATTERY PACK, D5-28, B5-27. IAW DC9 MM 33-50 2 L 7 2 4F A6WE 2001112900014 20011129 00014 NM 2001 11 29 ASAA0110480 1 20010707 A 5320 6546877147 INTERCOSTAL BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL AT BS 705, LEFT BUTTOCK LINE 60-66 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2001112900015 20011129 00015 NM 2001 11 29 ASAA0110514 1 20010730 A 3350 8821004 BATTERY PACK BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 740AS 22578 ANC - DURING TAXI TO GATE, EMERGENCY TRACK LIGHTS AT SEAT PALLET 7-7 ILLUMINATED. REMOVED AND REPLACED BATTERY PACK, TH EN LIGHTS OPERATED NORMAL. (M) 2 L 7 2 4F A16WE 2001112900016 20011129 00016 NM 2001 11 29 ASAA0140093 1 20010731 A 3350 8100022603 LIGHT BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 754AS 25095 ANC - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE OVERWING EXITS. RECONNECTED EMERGENCY FLOOR T RACK LIGHTING. OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001112900017 20011129 00017 NM 2001 11 29 ASAA0140094 1 20010731 A 3350 8100022603 LIGHT BOEING 737 7374Q8 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 754AS 25095 ANC - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE AT ROW 10. REPLACED EMERGENCY FLOOR TRACK LIG HTING. OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001112900018 20011129 00018 NM 2001 11 29 ASAA0170006 1 20010731 A 3350 D71702001 POWER SUPPLY BOEING 737 737790 13844CN NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 615AS 30344 PDX - DURING LINE MAINTENANCE, THE RIGHT NR 2 DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE POWER SUPPLY. THE EMERGENCY LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 2001112900019 20011129 00019 WP 2001 11 29 ASAA0180229 1 20010726 A 3350 0105606003 LIGHT DOUG DC9 DC982 3022082 WP CABIN MISSING A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 967AS 49103 SEA - DURING PRE-FLIGHT CHECK, FOUND ONE EMERGENCY FLOOR TRACK LIGHT MISSING AT ROW 7. REPLACED MISSING LIGHT MODULE. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001112900020 20011129 00020 WP 2001 11 29 ASAA0180230 1 20010727 A 3350 60030451 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 965AS 53079 PHX - DURING PREFLIGHT, THE EMERGENCY EXIT LIGHTS IN FIRST CLASS WERE FOUND TO BE INOPERATIVE. REPLACED THE POWER SUPPL Y AND THE LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001112900021 20011129 00021 WP 2001 11 29 ASAA0180231 1 20010729 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 973AS 53449 ANC - DURING LINE MAINTENANCE, THE TRACK LIGHTING WAS FOUND TO BE INOPERATIVE AT ROW 22. FOUND WIRE PULLED FROM LIGHT S OCKET. REPLACED MODULE. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001112900022 20011129 00022 SO 2001 11 29 ASOA01153 1 20010831 A 2722 62265735004 MOUNT EMB 120 EMB120 3260201 SO RUDDER SERVO DEFECTIVE A ASOA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 11 275AS 120234 FLT 4810 - DURING FLIGHT, REPORTED THE A/C WAS HARD TO CONTROL. WHEN THE A/P WAS DISCONNECTED, THE ELEV AND RUDDER WERE HEAVY AS IF THEY WERE STILL CONNECTED TO THE A/P. PULLED THE A/P C/B, BUT DID NOT FIX PROBLEM. DECLARED AN EMERGENCY AN D A/C LANDED WITHOUT INCIDENT. MX INSP A/C FLT CONTROL SYS, CONTROL SURFACES, AND CABLE BELLCRANKS AND FOUND NO DEFECTS. THE A/P PANEL WAS R&R BY MX AS A PRECAUTIONARY MEASURE. WHILE INSPECTING THE A/P SYS, MX FOUND ELEV TRIM SERVO MOTOR B INDING. MX R&R THE ELEV TRIM SERVO MOTOR. MX R&R THE ELEV TRIM SERVO. OPS CHECK GOOD. AFTER TEST FLT, WITH YAW DAMPER EN GAGED, RUDDER PEDALS WOULD NOT MOVE. INSP, MX FOUND RUDDER SERVO MOUNT DEFECTIVE. MAINTENANCE REMOVED AND REPLACED THE R 2 L 7 2 4T RT A31SO 2001112900023 20011129 00023 NM 2001 11 29 BJNA011003 1 20011026 A 3350 1000679 LIGHT BOEING 737 737214 138446R NM COCKPIT INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 457TM 20156 FOUND COCKPIT EMERGENCY LIGHT WOULD NOT TEST. REMOVE AND REPLACED EMERGENCY EXIT LIGHT IAW 33-51-51 OF BMM, OPS CHECK N ORMAL. (M) 2 L 7 2 4F A16WE 2001112900024 20011129 00024 SO 2001 11 29 SIMA200128702 1 20011014 A 2932 156221 PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO HYDRAULIC SYS LEAKING A SIMA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 605RR 145059 GRR - FLT 3795 - CREW REPORTED THE NR 2 HYDRAULIC LOST ALL FLUID, ENGINE AND ELECTRIC PUMP SHUTDOWN AND EMERGENCY WAS DE CLARED. MAINTENANCE FOUND THE NR 2 HYDRAULIC SYSTEM PRESSURE SWITCH TO BE LEAKING. A NEW PRESSURE SWITCH WAS INSTALLED IAW EMB MM. OPERATIONAL AND LEAK CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001112900025 20011129 00025 EU 2001 11 29 SIMA200129004 1 20011011 A 3350 7239410802 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 235AE 340B235 FOUND FLOOR EMERGENCY EXIT LIGHT OUT AT 10B. REMOVED AND REPLACED LIGHT ASSEMBLY AT 10B IAW SAAB 340 AMM. OPERATIONALL Y CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001112900026 20011129 00026 SO 2001 11 29 SIMA200129601 1 20011023 A 5620 12047934019 WINDOW EMB 145 EMB145LR 3260212 SO CABIN FAILED A SIMA A UNSCHED LANDING D Z INFLIGHT SEPARATION SIGNIFICANT FAILURE REPORT CR CRUISE 1 SW 21 640AE 145183 DURING FLIGHT AT FL330, THE PAX WINDOW AT SEAT 17C CRACKED AND PART OF WINDOW DEPARTED THE AIRCRAFT (OUTER PANEL). LOUD NOISE WAS NOTED BUT NO LOSS OF PRESSURIZATION WAS EXPERIENCED. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REP LACED THE PASSENGER WINDOW IAW EMB MM. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2001112900027 20011129 00027 EU 2001 11 29 SIMA200130302 1 20011025 A 5347 7253799383 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 350CF 340B350 ABI - DURING MBV INSPECTION, FOUND CORROSION ON SEAT TRACK AT BL 18.3L, BETWEEN STATIONS 297 TO 348 TO BE OUT OF SRM LIM ITS. CUT OUT A 56 INCH SECTION OF EXISTING SEAT TRACK. PREPARED A SEAT TRACK REPAIR EXTRUSION AND A REPAIR U-BEAM. IN STALLATION DONE IAW SAAB 340 SRM (72LKS 3079 REV 38) 53-70-60, AND STANDARD SRM PRINCIPLES. (M) 2 L 7 2 4T RT A52EU 2001112900028 20011129 00028 SO 2001 11 29 SIMA200130303 1 20011025 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 712AE 145247 ABI - DURING MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON THE FORWARD DIGITAL IN GALLEY AREA. REMOVED CORROSION BY BL ENDING IT OUT. PERFORMED AN NDT INSPECTION OF THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED REPAIR DOUBLER IAW E MB135 GST-3493/01 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT TOOO11AT 2001112900029 20011129 00029 SO 2001 11 29 SIMA200130304 1 20011025 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 712AE 145247 DURING MBV INSPECTION, FOUND CORROSION ON THE GALLEY LEFT OMEGA BEAM AT FRAME 20. REMOVED CORROSION BY CUTOUT. FABRICAT ED FILLER AND DOUBLER. REPAIR DONE IAW EMB 145 (SRM 145/1142 CHAPTER 53 REV 15). 53-21-10, PAGE 204, FIG 201 AND STANDA RD SRM PRACTICES. (M) 2 L 7 2 4F RT TOOO11AT 2001112900030 20011129 00030 SO 2001 11 29 SIMA200130305 1 20011025 A 5320 14522459003 SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 601GH 145046 ABI - THIS IS LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. GALLEY AREA FLOOR RAMP SUPPORT CORRODED. REMOVED CORRODED GA LLEY FLOOR RAMP SUPPORT AND INSTALLED SERVICEABLE RAMP IAW EMB145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2001112900031 20011129 00031 SO 2001 11 29 SIMA200130306 1 20011025 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 601GH 145046 THIS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. CENTER GUSSET IN GALLEY HAS CORROSION. REMOVED GUSSET AND INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2001112900032 20011129 00032 EU 2001 11 29 SIMA200131001 1 20011106 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 174AE 340B174 LFT - FLT 9305 - SEVERAL EMERGENCY LIGHTS INOPERATIVE. FERRIED TO DFW. REMOVED AND REPLACED POWER SUPPLIES. ALL P/NS OFF ARE THE SAME, S/N OFF AT 20LN-1868, 22LN-18400, 23LN-18375, 24LN-17497. (M) 2 L 7 2 4T RT A52EU 2001112900033 20011129 00033 NM 2001 11 29 0104656614 1 20011119 A 3320 NW02219 BALLAST BOEING 747 747251B 1384892 NM DEFECTIVE A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 01 614US 20359 During flight, smoke emitted from galley #3. Pulled galley circuit breaker and smell dissipated. Aircraft continued to d estination and landed without incident. Replaced #3 galley light ballast and six sockets. Operational check good. 2 L 7 4 4F A20WE 2001112900034 20011129 00034 NM 2001 11 29 0104646743 1 20011128 A 2611 215680 SMOKE DETECTOR BOEING 747 747249F 1384849 NM CARGO COMPARTMEN DIRTY A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 01 643NW 22245 During flight, the #5 main deck cargo smoke detector light illuminated accompanied with alarm lights and fire bell. Airc raft continued to destination and landed without incident. Cleaned both detectors. Operational check good. 2 L 7 4 4F A20WE 2001112900035 20011129 00035 NM 2001 11 29 TSAA0129152 1 20011113 A 2910 BACH8A06EE0260T HYDRAULIC LINE BOEING 737 737209 NM RT MLG LEAKING A TSAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 13 827AL 23913 FLT 62, HNL-OGG, THE HYDRAULIC ANNUNCIATOR CAME ON AFTER TAKEOFF. BOTH 'A' SYSTEM HYDRAULIC LOW PRESSURE LIGHTS ILLUMIN ATED. THE 'A' SYSTEM QUANTITY READ '0'. DECLARED EMERGENCY AND RETURNED TO HNL FOR AN UNEVENTFUL LANDING. REPLACED TH E RIGHT LANDING GEAR ACTUATOR RETURN LINE IAW MM 32-32-11. LEAK CHECK OK. (M) 2 L 7 2 4F RT A16WE 2001112900036 20011129 00036 NM 2001 11 29 TSAA0133150 1 20011108 A 3350 86210066 BATTERY PACK BOEING 737 737230 1384401 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 820AL 22138 REPLACED FORWARD SERVICE AND ENTRY DOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURN ED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001112900037 20011129 00037 NM 2001 11 29 TSAA0153149 1 20011105 A 5330 65457701 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 807AL 23443 FOUND FUSELAGE CRACKED AT BS 767, S19L. TRIM OUT CRACK COMPLETED AND VERIFIED CUT OUT USING HFEC METHOD, NO DEFECTS NOT ED. FABRICATED AND INSTALLED REPAIR DOUBLER. CLEANED AND TREATED ALL EXPOSED SURFACES IAW SRM 53-30-3 FIGURE 1. AIRCR AFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2001112900038 20011129 00038 NM 2001 11 29 TSAA0153151 1 20011031 A 5312 65163007 BULKHEAD BOEING 737 737282 13844AT NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 824AL 23045 FOUND RIVET HOLES CRACKED AT BS 178 LEFT AND RIGHT LBL 9 WL 234. REMOVED CRACK PER SRM 53-10-11 PAGE 1, PROCEDURE 1. VE RIFIED CRACK REMOVED USING HFEC. INSTALLED REPAIR DOUBLER IAW ECO 3138 PART 1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001112900039 20011129 00039 NM 2001 11 29 USAABB01118 1 20011104 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 629AU 27807 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 13 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001112900040 20011129 00040 EU 2001 11 29 USAAF01079 1 20011016 A 3350 362624 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 894US 11379 PIT - A FIRST CLASS SECTION OF THE FLOOR PROXIMITY EMERGENCY LIGHTS WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT SECTION. (M) 2 L 7 2 4F RT 2001112900041 20011129 00041 EU 2001 11 29 USAAF01080 1 20011101 A 3350 6104789 BATTERY FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 859US 11293 CLT - THE EMERGENCY FLOOR LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F RT 2001112900042 20011129 00042 EU 2001 11 29 USAAF01081 1 20011104 A 3350 6104789 BATTERY FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 865US 11308 CLT - THE EMERGENCY FLOOR LIGHTS AT SEAT ROWS 4 TO 8 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY . (M) 2 L 7 2 4F RT 2001112900043 20011129 00043 EU 2001 11 29 USAAF01082 1 20011105 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 855US 11283 CLT - THE EMERGENCY FLOOR LIGHT AT SEAT ROW 4 WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT THE LIGHT. (M) 2 L 7 2 4F RT 2001112900044 20011129 00044 EU 2001 11 29 00007 1 20011120 A 3231 MY2029310F10 ARM AMD FALC20 FALCON 2720302 EU LT MLG DOOR BROKEN E HAEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 240TW 12673 40 LEFT LANDING GEAR DOOR DID NOT RETRACT, RED LIGHT WAS ON AFTER GEAR WAS EXTENDED. LEFT INBOARD GEAR DOOR FORWARD ARM BR OKE AT ACTUATOR ATTACH POINT. REMOVED AND REPLACED LEFT INBOARD GEAR DOOR. 2 L 7 2 4F A7EU 2001112900045 20011129 00045 NM 2001 11 29 FX72001F00001 1 20010726 A 3222 532363152 PIN BOEING 727 727251 138408H NM PWA JT8 JT8D9A 52048 NE NLG LOOSE A FX7A O OTHER O OTHER LD LANDING 1 SO 19 266US 19985 UPON LANDING INC CCS, NOSE GEAR SCISSOR LINK CAME LOOSE. RECONNECTED PIN AND CONTINUE TO THE RAMP. PRECAUTIONARY REPLA CED NLG APEX PIN RETURNED AIRCRAFT TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2001112900046 20011129 00046 NM 2001 11 29 FX72001F00002 1 20010730 A 2910 BACH8A08NN0360T HYDRAULIC LINE BOEING 727 727259 138408J NM PWA JT8 JT8D15 52051 NE RT MLG LEAKING A FX7A J A DUMP FUEL UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 19 203AV 22474 AFTER TAKE-OFF LOSS OF QUANTITY AND PRESSURE OF A SYSTEM (A) HYDRAULIC. DUMPED REQUIRED FUEL FOR RETURN TO AIRPORT. AI RCRAFT RETURNED WITH NO EMERGENCY DECLARED AIRCRAFT LANDED, UNEVENTFUL. T/S HYD LOSS TO RT MLG FLEX HOSE RETURN. REMOV ED AND REPLACED RIGHT MLG ACTUATOR HOSE ASSEMBLY, OPS AND LEAK CHECKED NORMAL PER MM. RETURNED AIRCRAFT TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2001112900047 20011129 00047 NM 2001 11 29 FX72001F00003 1 20010820 A 2150 1843601 HEAT EXCHANGER BOEING 727 727224 1384076 NM PWA JT8 JT8D15 52051 NE A/C BAY CRACKED A FX7A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 79750 22452 AFTER TAKEOFF AIRCRAFT WOULD NOT PRESSURIZE. BOTH AIRCRAFT PACKS DID NOT WORK AND AFTER RESETTING BOTH PACKS TO (ON) AI RCRAFT WILL NOT PRESSURIZE. RETURNED TO AIRPORT WITHOUT INCIDENT. TROUBLESHOT AIRCRAFT PRESSURE SYSTEM, FOUND CRACKED P RIMARY HEAT EXCHANGER REMOVED AND REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2001112900048 20011129 00048 NM 2001 11 29 FX72001F00004 1 20010730 A 2910 BACH8A08NN0360T HYDRAULIC LINE BOEING 727 727259 138408J NM PWA JT8 JT8D15 52051 NE RT MLG LEAKING A FX7A J A DUMP FUEL UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 19 203AV 22474 AFTER TAKEOFF, LOSS OF QUANTITY AND PRESSURE OF SYSTEM (A) HYDRAULIC. DUMPED REQUIRED FUEL FOR RETURN TO AIRPORT. AIRC RAFT RETURNED WITH NO EMERGENCY DECLARED, AIRCRAFT LANDED UNEVENTFUL. T/S HYDRAULIC LOSS TO RIGHT MAIN LANDING GEAR FLE X HOSE RETURN. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR ACTUATOR HOSE ASSEMBLY. OPS AND LEAK CHECKED NORMAL PER MM . RETURNED AIRCRAFT TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2001112900049 20011129 00049 CE 2001 11 29 HYI2001F00001 1 20011002 A 2460 CM358950 MASTER SWITCH CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO AVIONICS FAILED E HYIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NE 01 660CA 1000 402C0406 WHILE AIRCRAFT WAS TAXING, AVIONICS SYSTEM FAILED. CREW ENGAGED EMERGENCY AVIONICS BY PASS SWITCH, AND RETURNED TO THE GATE. MECHANICS REMOVED AND REPLACED AVIONICS MASTER SWITCH AND RELEASE AIRCRAFT BACK TO SERVICE. 1 L 7 2 3O 3 O A7CE E8CE 2001112900050 20011129 00050 CE 2001 11 29 HYI2001F00002 1 20011008 A 2460 CM358950 MASTER SWITCH CESSNA 402 402C 207590R CE AVIONICS INOPERATIVE E HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 6813J 1017 402C0641 CREW REPORTED AVIONICS MASTER SWITCH INOPERATIVE ON PREFLIGHT. MAINTENANCE REMOVED AND REPLACED SWITCH AND RETURNED AIR CRAFT TO SERVICE. (PTRS-2001B5540) 1 L 7 2 3O A7CE 2001112900051 20011129 00051 CE 2001 11 29 HYI2001F00003 1 20011011 A 2460 CM358950 MASTER SWITCH CESSNA 402 402C 207590R CE AVIONICS FAILED E HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 6875D 402C0511 ON PREFLIGHT INSPECTION, AVIONICS MASTER SWITCH FAILED. MAINTENANCE REPLACED SWITCH AND RETURNED AIRCRAFT TO SERVICE. 1 L 7 2 3O A7CE 2001112900052 20011129 00052 CE 2001 11 29 HYI2001F00004 1 20010915 A 2460 CM358950 CIRCUIT BREAKER CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO AVIONICS FAILED E HYIA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 NE 01 7037E 402C0471 AVIONIC CIRCUIT BREAKER/SWITCH FAILED IN FLIGHT CAUSING COMPLETE AVIONIC FAILURE CREW UTILIZED EMERGENCY AVIONIC BUS SWI TCH AND LANDED WITHOUT INCIDENT. SEVERAL SUCH FAILURES RECORDED RECENTLY. THIS SWITCH HAS A HIGH UTILIZATION FACTOR.(K) 1 L 7 2 3O 3 O A7CE E8CE 2001112900053 20011129 00053 CE 2001 11 29 HYI2001F00005 1 20011105 A 2460 CM358950 MASTER SWITCH CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO INST PANEL FAILED E HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 6879R 1000 402C0611 ON PREFLIGHT INSPECTION AVIONIC MASTER SWITCH FAILED. MAINTENANCE REPLACED SWITCH AND RETURNED AIRCRAFT TO SERVICE.(K) 1 L 7 2 3O 3 O A7CE E8CE 2001112900054 20011129 00054 CE 2001 11 29 HYI2001F00006 1 20011029 A 2460 CM358950 MASTER SWITCH CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO INST PANEL FAILED E HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 68391 1000 402C0483 ON PREFLIGHT INSPECTION AVIONICS MASTER SWITCH AND RETURNED AIRCRAFT TO SERVICE. 1 L 7 2 3O 3 O A7CE E8CE 2001112900055 20011129 00055 CE 2001 11 29 HYI2001F00007 1 20011106 A 3230 51420025 DRAG BRACE CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO NLG CRACKED D K NONE O OTHER IN INSP/MAINT 1 NE 01 769EA 1687 402C0303 REGULAR SCHEDULED INSPECTION FOUND NOSE GEAR DRAG BRACE CRACKED AT ACTUATOR ATTACH LUG. MECHANIC REMOVED AND REPLACED D RAG BRACE.(K) 1 L 7 2 3O 3 O A7CE E8CE 2001112900056 20011129 00056 CE 2001 11 29 HYI2001F00008 1 20011106 A 3230 51420025 DRAG BRACE CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO NLG CRACKED D HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 763EA 1990 402C0497 REGULAR SCHEDULED INSPECTION, FOUND NOSE GEAR DRAG BRACE CRACKED AT ACTUATOR ATTACH LUG. MECHANIC REMOVED AND REPLACED NOSE GEAR DRAG BRACE.(K) 1 L 7 2 3O 3 O A7CE E8CE 2001112900057 20011129 00057 CE 2001 11 29 HYI2001F00009 1 20011106 A 3230 51420025 DRAG BRACE CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO NLG CRACKED D HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 83PB 2041 402C0350 REGULAR SCHEDULED INSPECTION, MECHANIC FOUND NOSE GEAR DRAG BRACE CRACKED AT ATTACH LUG CALCULATOR. REMOVED AND REPLACE D DRAG BRACE.(K) 1 L 7 2 3O 3 O A7CE E8CE 2001112900058 20011129 00058 NM 2001 11 29 IU62001F00012 1 20011031 A 2782 1U11032 ACTUATOR BOEING 727 727* NM L/E SLAT FLAKING B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 CHROME PLATING IS FLAKING OFF INSIDE THE BORE. 2 L 7 3 4F RT A3WE 2001112900059 20011129 00059 NM 2001 11 29 IU62001F00013 1 20011031 A 2710 654484511 MANIFOLD BOEING 737 737 UTILSYS NM AILERON CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 54639 7571 MANIFOLD IS CRACKED AROUND THE FILTER BOWL AREA. 2 L 7 2 4F RT A16WE 2001112900060 20011129 00060 NM 2001 11 29 IU62001F00017 1 20011023 A 3240 511531 HOUSING PNEUDRAULICS BOEING 737 737* NM SHUTTLE VALVE CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 1319 HOUSING IS CRACKED INSIDE ONE OF THE BOLT MOUNTING HOLES. LEAKS AT PROOF PRESSURE. FATIGUE, DEFECT IN THE CASTING OF T HE HOUSING AND/OR OVERTORQUING OF BOLT ON INSTALLATION. 2 L 7 2 4F RT A16WE 2001112900061 20011129 00061 NM 2001 11 29 IU62001F00018 1 20011023 A 3230 65446924 HOUSING BOEING BOEING 737 737* NM MLG MODULE CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 68948 1340 HOUSING IS CRACKED IN THE (D) PRIORITY PORT FLOW PASSAGE. FATIGUE, HIGH TIME ON UNIT. SET A TIME LIMIT BETWEEN OVERHAU L CYCLES TO CHECK FOR CRACKS. 2 L 7 2 4F RT A16WE 2001112900062 20011129 00062 NM 2001 11 29 IU62001F00015 1 20011023 A 2761 654494710 HOUSING BOEING BOEING 737 737* NM ACTUATOR CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 ACA1423 HOUSING IS CRACKED INSIDE THE RETRACT PORT. INSTALLED HOUSING.(K) 2 L 7 2 4F RT A16WE 2001112900063 20011129 00063 NM 2001 11 29 IU62001F00016 1 20011023 A 2761 654494710 HOUSING BOEING BOEING 737 737* NM ACTUATOR CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 492 HOUSING IS CRACKED INSIDE THE RETRACT PORT. INSTALL HOUSING. 2 L 7 2 4F RT A16WE 2001112900064 20011129 00064 NM 2001 11 29 IU62001F00014 1 20011031 A 3243 654458212 HOUSING BOEING BOEING 737 737* NM SHUT OFF VALVE CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 6859 1169 HOUSING IS CRACKED IN THE AREA BETWEEN THE TWO VALVE BORES. 2 L 7 2 4F RT A16WE 2001112900066 20011129 00066 EA 2001 11 29 COMA0160930 1 20011128 A 5346 60135006 BEAM CNDAIR CL600 CL6002B19 1900309 EA AFT EQUIPMENT BA CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 918CA 19340 7018 ENGINE SUPPORT BEAM CRACKED.REPAIRED DAMAGE I/A/W REO 601-53-345. 2 L 7 2 4F RT A21EA 2001112900069 20011129 00069 GL 2001 11 29 LU42001F00001 3 20011001 A 6110 C2987 BEARING CESSNA 402 402B 207590P CE CONT O520 TSIO520E 17040 SO MCAULY 3AF32C 3AF32C87 GL PROPELLER CRACKED B LU4R K NONE O OTHER IN INSP/MAINT 1 SO 17 87144 402B0933 757716 757716 RELEVANT INDICATION. 1 L 7 2 3O 3 O A7CE E8CE 5 C P22EA 2001112900070 20011129 00070 GL 2001 11 29 LU42001F00002 3 20011017 A 6110 C3411 BEARING CESSNA 337 337G 2075730 CE CONT O360 IO360G 17025 SO MCAULY 2A34C D2A34C* GL PROPELLER FAILED B LU4R K NONE O OTHER IN INSP/MAINT 1 SO 17 11FT 33701745 765154 RELEVANT INDICATION. 1 H 7 2 3O 3 O A6CE E1CE 5 C P3EA 2001112900071 20011129 00071 NM 2001 11 29 USAABB01120 1 20011110 A 3350 CONTACTOR BOEING 767 7672B7 1385107 NM CABIN LOOSE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 655US 25257 PHL - FOUND CEILING EMERGENCY LIGHT INOPERATIVE AT ROW 13. MAINTENANCE RESECURED A LOOSE CONNECTION. (M) 2 L 7 2 4F RT A1NM 2001112900072 20011129 00072 NM 2001 11 29 USAABB01121 1 20011110 A 3350 20121 CHARGER BOEING 767 7672B7 1385107 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 655US 25257 PHL - FOUND FLOOR EMERGENCY LIGHTS INOPERATIVE FROM ROW 13 THROUGH ROW 24. MAINTENANCE REPLACED THE BATTERY CHARGER AT ROW 16. (M) 2 L 7 2 4F RT A1NM 2001112900073 20011129 00073 NM 2001 11 29 USAABB01122 1 20011110 A 3350 CONTACTOR BOEING 767 767201 1385125 NM CABIN LOOSE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 645US 23897 PHL - FOUND FLOOR EMERGENCY LIGHT INOPERATIVE AT ROW 24. MAINTENANCE RESECURED A LOOSE CONNECTION. (M) 2 L 7 2 4F RT A1NM 2001112900074 20011129 00074 NM 2001 11 29 USAABB01125 1 20011112 A 3350 873100151REV12 LIGHT BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 605AU 22201 IAD - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 23 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001112900075 20011129 00075 NM 2001 11 29 USAABB01126 1 20011113 A 3350 86210066 BATTERY PACK BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 628AU 27806 MCO - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 6, 23, 26 AND 29 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS. (M) 2 L 7 2 4F RT A2NM 2001112900076 20011129 00076 NM 2001 11 29 USAABB01127 1 20011113 A 3350 20121 CHARGER BOEING 767 767201 1385125 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 646US 23898 CLT - AFT RIGHT SIDE FLOOR EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER. (M) 2 L 7 2 4F RT A1NM 2001112900077 20011129 00077 NM 2001 11 29 USAABB01128 1 20011114 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 625VJ 27246 PHL - FOUND SEVEN FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2001112900078 20011129 00078 NM 2001 11 29 USAABB01129 1 20011114 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 625VJ 27246 PHL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW FOUR INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001112900079 20011129 00079 2001 11 29 USAASA01059 4 20011108 A 2565 62293105 SLIDE AIRBUS A321 A321211 3930370 EU CABIN FAULTY A USAA K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 19 166US 1436 MCO - RECEIVED AN 'EPSU EXT LOAD EXIT L' FAULT DURING TEST. MAINTENANCE REPLACED THE L3 DOOR SLIDE ASSEMBLY. OK FOR SE RVICE. (M) 2 L 7 2 4F RT A28NM 2001112900080 20011129 00080 EU 2001 11 29 USAASA01060 1 20011108 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319112 3930323 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 746UW 1297 PIT - THE EMERGENCY LIGHTS FAILED THE WEEKLY CHECK OPERATIONAL TEST. MAINTENANCE REPLACED THE LEFT EMERGENCY POWER SUPP LY UNIT AND A DECODER-ENCODER UNIT. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2001112900081 20011129 00081 EU 2001 11 29 2001F00676 1 20011027 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE K FLUID LOSS TX TAXI/GRND HDL 1 SW 21 297AE 340B297 YQB - CREW REPORTED THAT WHEN THE EMERGENCY LIGHTS WERE SELECTED ON, THEY WOULD ILLUMINATE FOR A SECOND AND THEN EXTINGU ISH. AIRCRAFT WAS FERRIED TO BOS FOR REPAIR. MAINTENANCE REMOVED AND REPLACED ALL FIVE POWER SUPPLY UNITS IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200130002 (M) 2 L 7 2 4T RT A52EU 2001112900082 20011129 00082 EU 2001 11 29 2001F00677 1 20011027 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 297AE 340B297 YQB - CREW REPORTED THAT WHEN THE EMERGENCY LIGHTS WERE SELECTED ON, THEY WOULD ILLUMINATE FOR A SECOND AND THEN EXTINGU ISH. AIRCRAFT WAS FERRIED TO BOS FOR REPAIR. MAINTENANCE REMOVED AND REPLACED ALL FIVE POWER SUPPLY UNITS IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200130002 (M) 2 L 7 2 4T RT A52EU 2001112900083 20011129 00083 EU 2001 11 29 2001F00678 1 20011027 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 297AE 340B297 YQB - CREW REPORTED THAT WHEN THE EMERGENCY LIGHTS WERE SELECTED ON, THEY WOULD ILLUMINATE FOR A SECOND AND THEN EXTINGU ISH. AIRCRAFT WAS FERRIED TO BOS FOR REPAIR. MAINTENANCE REMOVED AND REPLACED ALL FIVE POWER SUPPLY UNITS IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200130002 (M) 2 L 7 2 4T RT A52EU 2001112900084 20011129 00084 EU 2001 11 29 2001F00679 1 20011027 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 297AE 340B297 YQB - CREW REPORTED THAT WHEN THE EMERGENCY LIGHTS WERE SELECTED ON, THEY WOULD ILLUMINATE FOR A SECOND AND THEN EXTINGU ISH. AIRCRAFT WAS FERRIED TO BOS FOR REPAIR. MAINTENANCE REMOVED AND REPLACED ALL FIVE POWER SUPPLY UNITS IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200130002 (M) 2 L 7 2 4T RT A52EU 2001112900085 20011129 00085 EU 2001 11 29 2001F00680 1 20011016 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 209AT 209 MIA - FLT 4964 - MAIN DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACKS 15 WL AND 18WL IAW ATR 42 AMM. OPERATIONALLY CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200129007. (M) 2 H 7 2 4T RT A53EU 2001112900086 20011129 00086 EU 2001 11 29 2001F00681 1 20011009 A 3350 3013017 BALLAST AEROSP ATR72 ATR72212A 8680902 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 548AT 548 SGF - FLT 3516 - EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BALLAST 61WL IAW ATR 72 AMM. REF S IMA200128301. (M) 2 H 7 2 4T RT A53EU 2001112900087 20011129 00087 EU 2001 11 29 SIMA200127610 1 20011003 A 2730 MS2115110C BUSHING SAAB SF340 340B 7860101 EU ELEVATOR CORRODED A SIMA O OTHER E VIBRATION/BUFFET CR CRUISE 1 SW 21 313AE 340B313 BOS - FLT 4566 - DURING CLIMB CREW REPORTED AN ABNORMAL VIBRATION FELT IN THE CONTROL COLUMN, MORE PROMINENTLY IN FORWAR D AND BACK MOTION. MAINTENANCE FOUND THE LEFT ELEVATOR PUSH PULL ROD BUSHING CORRODED. PUSH PULL ROD WAS REMOVED AND R EPLACED IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001112900088 20011129 00088 EU 2001 11 29 SIMA200128301 1 20011009 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 548AT 548 MIA - FLT 4964 - MAIN DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACKS 15 WL AND 18WL IAW ATR 42 AMM. OPERATIONALLY CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001112900089 20011129 00089 EU 2001 11 29 SIMA200128302 1 20011009 A 5310 DOOR FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 345SB 340B345 ABI - DURING MBV INSPECTION, FOUND CORROSION ON THE RIGHT FORWARD EXIT CUTOUT, INSIDE FORWARD LOWER CORNER. REPAIRED EX IT CUTOUT IAW SAAB REPAIR STATEMENT 340SDS002802 AND STANDARD SRM REPAIR PRACTICES. (M) 2 L 7 2 4T RT A52EU 2001112900090 20011129 00090 EA 2001 11 29 COMA0160931 1 20011126 A 2750 860D10018ABC FCU CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS LD LANDING 1 SO 01 926CA 7717 7027 FLIGHT #5285. FLAPS FAIL MESSAGE DURING LANDING.REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2001112900091 20011129 00091 EA 2001 11 29 COMA0160932 1 20011126 A 2760 864202 SENSOR CNDAIR CL600 CL6002B19 1900309 EA L/H MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 708CA 7235 FLIGHT #5681. GROUND SPOILER DEPLOYED CAUTION MESSAGE.REPLACED THE L/H INBD G.L.D. PROXIMITY SENSOR. 2 L 7 2 4F RT A21EA 2001112900092 20011129 00092 EU 2001 11 29 SIMA200128303 1 20011009 A 3350 LH6151 SOCKET AEROSP ATR42 ATR42300 8680920 EU CABIN DEFECTIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 282AT 282 MIA - FLT 4986 - ROW 1 FLOOR PROX LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED LAMP HOLDER SOCKET ON ROW 1 I AW ATR AMM 20-42-13. OPERATIONALLY CHECKED GOOD AT THIS TIME. (M) 2 H 7 2 4T RT A53EU 2001112900093 20011129 00093 EA 2001 11 29 COMA0160933 1 20011127 A 2740 6225027001 SWITCH CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A COMA A UNSCHED LANDING F S FLT CONT AFFECTED AFFECT SYSTEMS CL CLIMB 1 SO 01 952CA 9438 7092 FLIGHT #5843. COPILOTS STABILIZER TRIM IS INTERMITTENT.REPLACED THE COPILOTS TRIM SWITCH. 2 L 7 2 4F RT A21EA 2001112900094 20011129 00094 SO 2001 11 29 SIMA200128401 1 20011008 A 5610 163500110 WINDSHIELD EMB 135 EMB135LR 3260305 SO COCKPIT CRACKED A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 717AE 145272 BWI - FLT 4756 - CREW REPORTED DURING CLIMB, THE RIGHT FRONT WINDSHIELD HEATING ELEMENT STARTED TO GLOW. A FEW SECONDS AFTER THAT THE WINDSHIELD SHATTERED. REMOVED AND REPLACED FRONT RIGHT WINDSHIELD IAW EMB 135 AMM. OPERATIONALLY CHECKE D GOOD. (M) 2 L 7 2 4F RT TOOO11AT 2001112900095 20011129 00095 EU 2001 11 29 SIMA200128701 1 20011013 A 3350 161321 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 339SB 340B339 BOS - FLT 4719 - CREW REPORTED SEVERAL EMERGENCY LIGHTS OUT IN THE CABIN. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY UNIT AT SEAT 3B. OPS CHECK WAS FOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001112900096 20011129 00096 SO 2001 11 29 SIMA200129001 1 20011014 A 5610 163500112 WINDSHIELD EMB 135 EMB135LR 3260305 SO COCKPIT CRACKED A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 721HS 145283 ORD 0 FLT 4019 - FIRST OFFICERS WINDSHIELD CRACKED IN FLIGHT. AIRCRAFT RETURNED TO FIELD. REMOVED AND REPLACED FIRST O FFICERS WINDSHIELD IAW EMB 135 AMM. OPERATIONALLY CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001112900097 20011129 00097 EU 2001 11 29 SIMA200129002 1 20011015 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 282AT 282 MIA - FLT 5036 - EVACUATION PATH LIGHTING WAS FOUND TO BE INOPERATIVE IN FORWARD CABIN. REMOVED AND REPLACED EMERGENCY ESCAPE LIGHTING BATTERY PACK 3WLA IAW ATR 42 AMM. OPERATIONALLY CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001112900098 20011129 00098 EU 2001 11 29 SIMA200129006 1 20011016 A 3350 AD3127 BATTERY AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 242AT 242 MIA - EMERGENCY EXIT FLOOR PROXIMITY LIGHTS WERE FOUND TO BE DIM WHEN ON AT ROW 5 THROUGH 8 AND STAY ON WHEN SWITCHED OF F. REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY 10WLA IAW ATR 42 AMM. OPERATIONALLY CHECKED GOOD AND AIRCRAFT W AS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001112900099 20011129 00099 EA 2001 11 29 COMA0160934 1 20011128 A 3220 PIN CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 966CA 7132 FLIGHT #5786 NLG WOULD NOT RETRACT.REMOVED DOWNLOCK SAFETY PIN FROM NLG, INSPECTED NLG AND ACFT RETUREND TO SERVICE. 2 L 7 2 4F RT A21EA 2001112900100 20011129 00100 EU 2001 11 29 SIMA200129007 1 20011016 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 209AT 209 MIA - FLT 4964 - MAIN DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACKS 15 WL AND 18WL IAW ATR 42 AMM. OPERATIONALLY CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001112900101 20011129 00101 EU 2001 11 29 SIMA200129018 1 20011017 A 3397 WIRE AEROSP ATR42 ATR42300 8680920 EU CABIN BROKEN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 277AT 277 MIA - FLOOR PROXIMITY EMERGENCY LIGHTING AT ROW 2AB WAS FOUND TO BE INOPERATIVE. REPAIRED BROKEN WIRE AT EMERGENCY LIGH T ON ROW 2AB IAW ATR 42 AWM. (M) 2 H 7 2 4T RT A53EU 2001112900102 20011129 00102 EU 2001 11 29 SIMA200129801 1 20011025 A 3350 LIGHT AEROSP ATR72 ATR72212A 8680902 EU CABIN OUT OF POSITION A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 545AT 545 DFW - MAINTENANCE REPORTED THE ROW 6 FLOOR PROXIMITY EMERGENCY LIGHT DOES NOT ILLUMINATE DURING TEST. MAINTENANCE FOUND THE BULB NOT POSITIONED CORRECTLY. BULB WAS REPOSITIONED IN SOCKET, OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SE RVICE. (M) 2 H 7 2 4T RT A53EU 2001112900103 20011129 00103 EU 2001 11 29 SIMA200129901 1 20011026 A 3350 SIGN AEROSP ATR42 ATR42300 8680920 EU CABIN MALFUNCTIONED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 209AT 209 RSW - FLT 5082 - CREW REPORTED THE EMERGENCY EXIT SIGN AT ROW 1 RIGHT SIDE TO BE INOPERATIVE. MAINTENANCE COULD NOT DUP LICATE DISCREPANCY. OPERATIONAL CHECK WAS GOOD IAW ATR JIC 33-51-24 AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001112900104 20011129 00104 EU 2001 11 29 SIMA200129902 1 20011026 A 3397 WIRE AEROSP ATR72 ATR72212 8680945 EU CABIN LOOSE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 348AE 349 DFW - FLT 3624 - MAINTENANCE SAFETY TEAM FOUND ONE FLOOR PROXIMITY EMERGENCY LIGHT BETWEEN ROWS 7 AND 8 TO BE INOPERATIV E. MAINTENANCE FOUND A LOOSE WIRE FOR THE FLOOR LIGHT. WIRE WAS RECONNECTED, AN OPERATIONAL CHECK WAS GOOD AND AIRCRAF T WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001112900105 20011129 00105 EU 2001 11 29 SIMA200129903 1 20011026 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU E/E BAY FAULTY A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 247AE 340B247 MRY - FLT 3334 - DURING TAKEOFF ROLL, CREW REPORTED THE AVIONICS SMOKE LIGHT ILLUMINATED ON THE CWP. CREW PERFORMED EME RGENCY PROCEDURES AND RETURNED TO THE GATE. MAINTENANCE FOUND NO EVIDENCE OF SMOKE FROM THE AVIONICS RACK. MAINTENANCE REMOVED AND REPLACED THE AVIONICS SMOKE DETECTOR IAW SAAB MM. OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SER VICE. (M) 2 L 7 2 4T RT A52EU 2001112900106 20011129 00106 NM 2001 11 29 HNAA0100077 1 20011121 A 2900 DSC252B40124 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003 NM LEAKING A HNAA A UNSCHED LANDING K FLUID LOSS NR NOT REPORTED 1 EA 07 912HA 41442 040 #2 HYDRAILIC SYSTEM FLUID LOSS DOWN TO ISOLATION VALVE ACTUATION. PRESSURE REMAINED NORMAL WITH APPROX. 1/2 QT. INDICATE D RESERVOIR QUANTITY. AIRCRAFT DIVERTED TO SAV. FOUND FLEX LINE TO NLG DRAG STRUT ACTUATOR LEAKING. REPLACED FLEX LINE. 2 H 7 2 4T RT A13NM 2001112900107 20011129 00107 EU 2001 11 29 SIMA200130001 1 20011027 A 3350 3013000 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 536AT 536 DFW - FLT 3756 - CREW REPORTED AN EMERGENCY BATTERY NOT HOLDING A CHARGE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT 91WL IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001112900108 20011129 00108 EU 2001 11 29 SIMA200130002 1 20011027 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 297AE 340B297 YQB - CREW REPORTED THAT WHEN THE EMERGENCY LIGHTS WERE SELECTED ON, THEY WOULD ILLUMINATE FOR A SECOND AND THEN EXTINGU ISH. AIRCRAFT WAS FERRIED TO BOS FOR REPAIR. MAINTENANCE REMOVED AND REPLACED ALL FIVE POWER SUPPLY UNITS IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001112900109 20011129 00109 EU 2001 11 29 SIMA200130101 1 20011028 A 3350 3011210 LIGHT AEROSP ATR72 ATR72212 8680945 EU PAX DOOR INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 274AT 274 MIA - FLT 5012 - CREW REPORTED THE EMERGENCY EXIT LIGHT IN THE PASSENGER DOOR TO BE INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE LIGHT ASSEMBLY IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001112900110 20011129 00110 EU 2001 11 29 SIMA200130201 1 20011029 A 3350 LIGHT AEROSP ATR72 ATR72212 8680945 EU CABIN ILLUMINATED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 426AT 426 MIA - FLT 5075 - CREW REPORTED THE REAR EMERGENCY LIGHTS REMAIN ON. (M) 2 H 7 2 4T RT A53EU 2001112900111 20011129 00111 EU 2001 11 29 SIMA200130202 1 20011029 A 3350 3012701 LIGHT AEROSP ATR72 ATR72212A 8680902 EU PAX DOOR INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 545AT 545 DFW - DURING SCHEDULED OPS-2 CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHT IN THE PASSENGER DOOR TO BE INOPERATIVE. MAIN TENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW ATR MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M ) 2 H 7 2 4T RT A53EU 2001112900112 20011129 00112 EU 2001 11 29 SIMA200130301 1 20011030 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 326AE 340B326 BGR - FLT 4620 - CREW REPORTED THE EMERGENCY EXIT SIGN OVER 9A AND EMERGENCY OVERHEAD LIGHTS AT 9A AND 11A TO BE INOPERA TIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY UNIT AT 23LN IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCR AFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001112900113 20011129 00113 NM 2001 11 29 2001F00682 1 20011113 A 2720 60B800318 CONTROLLER BOEING 747 747230B 1384889 NM RUDDER FAILED A Q2SA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 23 742SA 22669 ON TAKEOFF, APPROXIMATELY AT 150 KNOTS SIGNIFICANT RIGHT RUDDER NEEDED TO MAINTAIN CONTROL. DURING CRUISE AFTER 1 HOUR OF FLIGHT, RUDDER RATION LIGHT BLINKED FOR ABOUT 15 MINUTES THEN WENT OUT. REMOVED AND REPLACED YAW DAMPER COMPUTER FOR PRECAUTIONARY COMPLETED UPPER AND LOWER YAW DAMPER COMPUTER INSTALLATION BYTE TEST PER MM 22-16-02 PAGE 401. ACCOMPLIS HED YAW DAMPER CONFIDENCE OPERATIONAL TEST. REMOVED AND REPLACED RUDDER RATIO CONTROLLER IAW 27-21-12. (M) 2 L 7 4 4F A20WE 2001112900114 20011129 00114 SO 2001 11 29 2001F00684 1 20011010 A 2750 FLAP EMB 120 EMB120ER 3260203 SO WING MALFUNCTIONED A HSYA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 05 223AS 120021 BGI - FLT 7106 - FIVE MINUTES INTO FLIGHT, FLIGHT CREW RECEIVED A FLAP DISAGREE FAULT INDICATION AND RETURNED TO BGI AND PERFORMED FLAPLESS LANDING DURING WHICH THE FAULT CLEARED ITSELF. INSPECTED FLAPS AND CYCLED FLAPS THROUGH ALL POSITIO NS THREE TIMES AND COULD NOT DUPLICATE PROBLEM. ALL INDICATORS WERE NORMAL AND CONSISTENT. AIRCRAFT WAS RETURNED TO SE RVICED AND DEPARTED WITHOUT INCIDENT. (M) 2 L 7 2 4T RT A31SO 2001112900115 20011129 00115 2001 11 29 2001F00505 4 20010828 A 2210 41800876000 ACTUATOR UROCOP EC135 EC135P1 8680990 EU YAW CHANNEL INOPERATIVE A R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 135N 20 0086 SMART ELECT MECHAN ACTUATOR IS INOPERATIVE. WITH AUTO-PILOT ENGAGED FCDM DISPLAYS YAW DEGRADED. AUTO-PILOT WILL NOT SE LF TEST. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 2 3U O H88EU 2001112900116 20011129 00116 NE 2001 11 29 2001F00529 2 20010718 A 7250 L621M1006103 SEAL UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE ENGINE TORN A R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 426AE 47 EC1350159 BELLOWS IS TORN AROUND CLAMP AND FOLD AREAS. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M) 1 G 7 2 3U 3 U O H88EU E42NE 2001112900117 20011129 00117 NE 2001 11 29 2001F00530 2 20010829 A 7250 L621M1006103 SEAL UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE ENGINE TORN A R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 427AE EC1350162 BELLOWS IS TORN AROUND CLAMP AND FOLD AREAS. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M) 1 G 7 2 3U 3 U O H88EU E42NE 2001112900118 20011129 00118 SW 2001 11 29 2001F00558 1 20010823 A 6210 206010200133 BLADE BELL 206 206B 1181511 SW MAIN ROTOR CORRODED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 116AL 1942 2389 DISCOVERED DURING ROUTINE AIRFRAME INSPECTION, TRAILING EDGE EXTRUSION EXFOLIATED AT STATION 65.5. REPLACED MAIN ROTOR BLADE. TOTAL DAMAGE AREA APPROXIMATELY .5 INCH WIDE BY .75 INCH LONG. (M) 1 G 7 1 3U H2SW 2001123100137 20011231 00137 NM 2001 12 31 SPAA0100047 1 20011129 A 3350 6013211 BATTERY PACK BOEING 737 7372Y5 1384554 NM CABIN DISCHARGED A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 28 712S 23038 AFT CABIN EMERGENCY LIGHTS INTERMITTENT. REPLACED POWER SUPPLY BATTERY PACK PER MM 33-51-71, OPS CHECK GOOD. 2 L 7 2 4U RT A16WE 2001112900119 20011129 00119 SW 2001 11 29 2001F00567 1 20010807 A 6220 407310101101 BEARING BELL BELL 407 407 1182206 SW MAIN ROTOR WORN B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 497AL A190 53172 2500 HOUR INSPECTION, REPLACED ELASTOMER SEPARATOR. (M) 1 G 7 1 3U O H2SW 2001112900120 20011129 00120 NM 2001 11 29 SABA011070 1 20011126 A 3350 6104789 BATTERY DHAV DHC8 DHC8102 2809003 NM DISCHARGED A SABA O OTHER L NO TEST IN INSP/MAINT 1 SO 33 813SN 032 Aircraft 813 flight 5047 from Charlotte to Tallahassee; During Pilots Pre-Flight inspection three foward red floor emerg ency lights were inop. Maintenance removed and replaced battery packs and system ops checked good. 2 H 7 2 4T RT A13NM 2001112900121 20011129 00121 NE 2001 11 29 2001F00685 2 20010413 A 7260 230093304 BEARING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ENGINE DAMAGED B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 202HN 223 7115 EXCESSIVE PITTING ON ANNULAR BALL BEARING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 2 3U 3 U H13EU E5NE 2001112900122 20011129 00122 NM 2001 11 29 BJNA011002 1 20011026 A 3350 1000679 LIGHT BOEING 737 737214 138446R NM CABIN INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 457TM 20156 R-3 OVERHEAD EMERGENCY EXIT LIGHT WILL NOT TEST. REMOVED AND REPLACED R-3 EMERGENCY EXIT LIGHT IAW BMM 33-51-51. (M) 2 L 7 2 4F A16WE 2001112900124 20011129 00124 NM 2001 11 29 PCAA0111138 1 20011123 A 3320 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN DEFECTIVE A PCAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 13 805EX 228 BWI- CREW REPORTED BURNING SMELL IN FORWARD CABIN. MAINTENANCE DETERMINED OVERHEAD BULB CAUSING ARCING. BULB REMOVED. AI RCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001112900125 20011129 00125 NM 2001 11 29 PCAA0111139 1 20011120 A 3397 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 820EX 019 DURING ROUTINE MAINTENANCE VISIT SEVERAL EMERGENCY LIGHTS IN FLOOR FOUND INOPERATIVE. CONNECTORS ON LEFT SEAT RAIL FOUND LOOSE AND WERE RESECURED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001112900126 20011129 00126 NM 2001 11 29 PCAA0111140 1 20011125 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN DAMAGED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 836EX 297 DURING ROUTINE MAINTENANCE VISIT ROW 1 EMERGENCY LIGHT FLOOR PATH RED PROXIMITY LIGHT FOUND INOPERATIVE. PROXIMITY LIGHT WIRING REPAIRED AT ROW 1 AS REQUIRED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001112900127 20011129 00127 NM 2001 11 29 PCAA0111141 1 20011124 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN DAMAGED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 842EX 341 DURING ROUTINE MAINTENANCE VISIT ONE SECTION OF EMERGENCY PATHWAY LIGHTS FOUND INOPERATIVE. LOOSE CONNECTION FOUND AND W IRING REPAIRED. OPERATIONAL CHECK GOOD . AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001112900128 20011129 00128 NM 2001 11 29 PCAA0111142 1 20011111 A 3222 88255 LINK DHAV DHC8 DHC8102 2809003 NM NLG WORN A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 805EX DCL039 228 DURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY, TRAILING ARM LINK AND PIN FOUND WORN. WORN PARTS WERE REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001112900129 20011129 00129 NM 2001 11 29 PCAA0111143 1 20011020 A 3222 88255 LINK DHAV DHC8 DHC8102 2809003 NM NLG WORN A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 807EX DCL29290 292 DURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY, TRAILING ARM LINK ,& LOWER PIN FOUND WORN. WORN PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001112900130 20011129 00130 NM 2001 11 29 PCAA0111144 1 20011020 A 3222 88255 LINK DHAV DHC8 DHC8102 2809003 NM NLG WORN A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 810EX DCL33591 308 DURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY, TRAILING ARM LINK AND PIN FOUND WORN.REPLAC ED NOSE GEAR TRAILING ARM LINK , LOWER PIN, AND O RING. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001112900131 20011129 00131 NM 2001 11 29 PCAA0111145 1 20011022 A 3222 88255 LINK DHAV DHC8 DHC8102 2809003 NM NLG WORN A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 811EX DCL244 201 DURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY, TRAILING ARM LINK AND PIN FOUND WORN. DISAS SEMBLED NOSE GEAR SHOCK STRUT, INSPECTED PARTS. REPLACED TRAILING ARM LOWER LINK AND LOWER PIN. REASSEMBLED NOSE GEAR SH OCK STRUT ASSEMBLY. ALL WORK DONE IN ACCORDANCE WITH DOWTY COMPONENT MAINTENANCE MANUAL 32-20-01. AIRCRAFT RETURNED TO S ERVICE. 2 H 7 2 4T RT A13NM 2001112900132 20011129 00132 NM 2001 11 29 PCAA0111146 1 20011106 A 3222 88255 LINK DHAV DHC8 DHC8102 2809003 NM NLG WORN A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 818EX DCL0198485 235 DURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY, TRAILING ARM LINK BEARING AND PIN FOUND WOR N. REPLACED LOWER LINK BEARING AND PIN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001112900133 20011129 00133 NM 2001 11 29 PCAA0111147 1 20011019 A 3222 88255 LINK DHAV DHC8 DHC8102 2809003 NM NLG WORN A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 820EX DCL469 019 DURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY, TRAILING ARM LINK AND PIN FOUND WORN. WORN PARTS REPLACED. LUBED AND SERVICED STRUT. OPERATIONAL CHECK GOOD.AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001112900134 20011129 00134 NM 2001 11 29 PCAA0111148 1 20011104 A 3222 88255 LINK DHAV DHC8 DHC8102 2809003 NM NLG WORN A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 822EX DCL256 187 DURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY, TRAILING ARM LINK AND PIN FOUND WORN.REPLAC ED LINK ASSEMBLY AND LOWER PIN. ALL WORK COMPLETED IN ACCORDANCE WITH COMPONENT MAINTENANCE MANUAL. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001112900135 20011129 00135 NM 2001 11 29 PCAA0111149 1 20011101 A 3222 88255 LINK DHAV DHC8 DHC8102 2809003 NM NLG WORN A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 826EX DCL420 389 DURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY, TRAILING ARM LINK, PIN AND PISTON END CAP F OUND WORN. REPLACED STRUT LINK PN 8825-5, LOWER PIN PN 8871-1, UPPER PIN PN 8827-1, AND PISTON END CAP PN 8829-5 IN ACCO RDANCE WITH MAINTENANCE MANUAL. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001112900136 20011129 00136 NM 2001 11 29 PCAA0111150 1 20011017 A 3222 88255 LINK DHAV DHC8 DHC8102 2809003 NM NLG WORN A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 825EX DCL419 388 DURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY, TRAILING ARM LINK AND PIN FOUND TO HAVE PLA Y. REPLACED PISTON CAP TRAILING LINK, AND UPPER AND LOWER PINS. OPERATIONAL CHECK GOOD IN ACCORDANCE WITH COMPONENT MAIN TENANCE MANUAL 32-20-11 AND 12-10-32 SHOCK STRUT SERVICING. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001112900137 20011129 00137 NM 2001 11 29 PCAA0111151 1 20011016 A 3222 88255 LINK DHAV DHC8 DHC8102 2809003 NM NLG WORN A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 EICHP DCL342 258 DURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY, LOWER TRAILING ARM STRUT LINK FOUND WORN. R EPLACED LOWER TRAILING ARM STRUT LINK, AND LOWER PIN IN ACCORDANCE WITH COMPONENT MAINTENANCE MANUAL 32-20-01. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001112900138 20011129 00138 NM 2001 11 29 PCAA0111152 1 20011026 A 3222 88255 LINK DHAV DHC8 DHC8102 2809003 NM NLG WORN A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 848EX DCL345 331 DURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY, TRAILING ARM LOWER LINK BUSHING AND PIN FOU ND WORN. REPLACED LINK AND LOWER & UPPER PINS IN ACCORDANCE WITH COMPONENT MAINTENANCE MANUAL 32-20-01. SERVICED STRUT A S REQUIRED IN ACCORDANCE WITH MAINTENANCE MANUAL.AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001112900139 20011129 00139 NM 2001 11 29 PCAA0111153 1 20011108 A 3222 88255 LINK DHAV DHC8 DHC8102 2809003 NM NLG WORN A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 849EX DCL380 337 DURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY FOUND EXCESSIVE PLAY AT LOWER LINK. TRAILING ARM LINK AND PISTON CAP REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001112900140 20011129 00140 NM 2001 11 29 PCAA0111154 1 20011108 A 3222 88255 LINK DHAV DHC8 DHC8102 2809003 NM NLG WORN A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 EICBJ DCL247 258 DURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY,FOUND PLAY BETWEEN LINK AND ARM. REPLACED LO WER PIN AND LOWER BUSHING OF THE LINK IN ACCORDANCE WITH MAINTENANCE MANUAL 32-20-00 OPERATIONAL CHECK GOOD. AIRCRAFT RE TURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001112900141 20011129 00141 NM 2001 11 29 PCAA0111155 1 20011116 A 3222 88285 LINK DHAV DHC8 DHC8102 2809003 NM NLG WORN A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 841EX DCL387 249 DURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY, TRAILING ARM LINK BUSHING AND PIN FOUND WOR N. LOWER LINK BUSHING AND LOWER PIN REPLACED IN ACCORDANCE WITH MAINTENANCE MANUAL. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001112900142 20011129 00142 NM 2001 11 29 PCAA0111156 1 20011114 A 3222 88255 LINK DHAV DHC8 DHC8102 2809003 NM NLG WORN A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 834EX DCL270 285 DURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY, TRAILING ARM LINK AND PIN FOUND WORN. REPLA CED PIN AND BUSHING IN ACCORDANCE WITH COMPONENT MAINTENANCE MANUAL 32-20-01. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001112900143 20011129 00143 NM 2001 11 29 PCAA0111157 1 20011016 A 3222 88255 LINK DHAV DHC8 DHC8102 2809003 NM NLG WORN A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 835EX DCL396 289 DURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY, FOUND PISTON CAP PIN GOUGED BEYOND LIMITS, TRAILING ARM WORN, AND TRAILING ARM ASSEMBLY WITH A GOUGE. TRAILING ARM ASSEMBLY REPLACED IN ACCORDANCE WITH MAINTENANCE MANUAL 32-20-11, TRAILING ARM PIN REPLACED IN ACCORDANCE WITH MAINTENANCE MANUAL 32-20-01. AIRCRAFT RETURNED TO SERVICE . 2 H 7 2 4T RT A13NM 2001112900144 20011129 00144 NM 2001 11 29 PCAA0111158 1 20011031 A 3222 88711 PIN DHAV DHC8 DHC8102 2809003 NM NLG WORN A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 828EX DCL423 392 DURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY, FOUND NOSE GEAR PISTON CAP PIN WORN.REPLACE D NOSE GEAR SHOCK STRUT PISTON CAP PIN IN ACCORDANCE WITH MAINTENANCE MANUAL. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001112900145 20011129 00145 NM 2001 11 29 PCAA0111159 1 20011120 A 3222 88255 LINK DHAV DHC8 DHC8102 2809003 NM NLG WORN A PCAA K NONE O OTHER LD LANDING 1 EA 13 809EX DCL320 302 MDT- CREW REPORTED NOSE WHEEL SHIMMY ON LANDING ROLL OUT. MAINTENANCE REPLACED THE NOSE LANDING GEAR SHOCK STRUT PISTON CAP, LINK , UPPER AND LOWER PINS. ALSO REPLACED WERE THE NOSE GEAR STEERING ACTUATOR LINKS. AIRCRAFT RETURNED TO SERVICE . 2 H 7 2 4T RT A13NM 2001112900146 20011129 00146 NM 2001 11 29 PCAA0111160 1 20011123 A 3222 88255 LINK DHAV DHC8 DHC8102 2809003 NM NLG WORN A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 827EX DCL421 390 DURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY, LOWER TRAILING ARM LINK BUSHING FOUND WORN. LINK BUSHING REPLACED IN ACCORDANCE WITH MAINTENANCE MANUAL. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001112900147 20011129 00147 NM 2001 11 29 PCAA0111161 1 20011128 A 3222 88255 LINK DHAV DHC8 DHC8102 2809003 NM NLG WORN A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 847EX DCL367 333 DURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY, TRAILING ARM LINK LOWER BUSHING AND PIN FOU ND WORN. LOWER PIN AND BUSHING REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001112900148 20011129 00148 SO 2001 11 29 M01090 1 20010814 A 3350 66364 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 828MJ 145218 MAINTENANCE WAS CALLED WHEN THE CREW FOUND THE FLOOR LIGHT STRIPS INOPERATIVE. THE TROUBLESHOT THE PROBLEM AND FOUND TH AT THE LIGHT ASSEMBLY WAS BAD. MAINTENANCE REMOVED AND REPLACED THE LIGHT STRIP, OPS CHECKED GOOD AND THE AIRCRAFT RETU RNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2001112900149 20011129 00149 EA 2001 11 29 M01093 1 20010819 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SO 07 77286 7286 DURING ROUTINE MAINTENANCE, THE CREW FOUND THE FORWARD NR3 EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BULB A ND OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2001112900150 20011129 00150 EA 2001 11 29 M01094 1 20010819 A 3350 BC10020004 LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27318 7318 ON PREFLIGHT, THE CREW NOTICED ONE CABIN CEILING EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOD LIGHT. 2 L 7 2 4F 4 F RT A21EA E15NE 2001112900151 20011129 00151 EA 2001 11 29 M01100 1 20010908 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CARGO BAY MALFUNCTIONED A MASA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 07 77302 7302 IN FLIGHT, THE CARGO SMOKE DETECTOR WARNING CAME ON. THE PILOT DISCHARGED THE BOTTLES AND LANDED SAFELY, WITHOUT INCIDE NT. MAINTENANCE INSPECTED THE COMPARTMENT AND FOUND NO EVIDENCE OF FIRE OR SMOKE. 2 L 7 2 4F 4 F RT A21EA E15NE 2001112900152 20011129 00152 EA 2001 11 29 MO1109 1 20010918 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE EXTERIOR INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37228 7228 DURING A ROUTINE SERVICE CHECK THE CREW FOUND A LEFT HAND PASSENGER DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENA NCE REPLACED THE BULB, OPS CHECKED GOOD AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2001112900153 20011129 00153 NM 2001 11 29 DL73K011738 1 20011030 A 5330 654576988 SKIN BOEING 737 737247 138448D NM FS 460, S-26R PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 245WA 23519 FUSELAGE / SKIN / FS 460 / STRG. 26R : GROUND DAMAGE CUTOUT REPAIR THE FUSELAGE SKIN WAS DAMAGED BY GROUND EQUIPMENT AT FS 460 BELOW STRINGER 26R. THE DAMAGE WAS REMOVED WITH A CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 382029-14, REV A. 2 L 7 2 4F A16WE 2001112900154 20011129 00154 NM 2001 11 29 DL73K011749 1 20011102 A 5311 6546561508 FRAME BOEING 737 737232 1384475 NM CABIN CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 322DL 23094 CORROSION WAS FOUND ON THE FS 947 FRAME AT STR 17R. THE DAMAGE WAS REMOVED BY TRIMMING OFF THE INBOARD FLANGE. THE FRAME WAS REPAIRED PER B737-200 SRM 51-40-3, FIG. 1 AT HMV. 2 L 7 2 4F RT A16WE 2001112900155 20011129 00155 NM 2001 11 29 DLM88011760 1 20011103 A 2610 000000 BATTERY DOUG MD88 MD88 3023688 NM CABIN DISCONNECTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 970DL 43173 RT AFT LAV SMOKE DETECTOR WILL NOT TEST RESEATED BATTERY. OPN NML. 2 L 7 2 4F RT A6WE 2001112900156 20011129 00156 NM 2001 11 29 DL73K011762 1 20011105 A 5321 6546803508 BEAM BOEING 737 737232 1384475 NM CABIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 322DL 23094 A CRACK WAS FOUND IN THE RADIUS OF THE UPPER CAP OF THE FS 520 FLOOR BEAM. IT WAS LOCATED AT LBL 24.75. THE CRACK WAS REPAIRED PER S/B 737-53-1120 AT HMV. 2 L 7 2 4F RT A16WE 2001112900157 20011129 00157 NM 2001 11 29 DLM88011763 1 20011102 A 5330 5911410 SKIN DOUG MD88 MD88 3023688 NM FS 240, L-18L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 903DL 49534 FUSELAGE / SKIN / FS 229-256 / LONG. 18L-19L : GROUND DAMAGE CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND DENTED AND CREASED BETWEEN FS 229 & 256 JUST BELOW THE LONGERON 18L CUSP LINE. THE DAMAGED AREA OF SKIN WAS REMOVED WITH A 20" X 6" CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 382046-14, REV A. 2 L 7 2 4F RT A6WE 2001112900158 20011129 00158 NE 2001 11 29 DL76S011789 2 20011112 A 7230 CF680A2 ENGINE BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE #2 ENGINE DAMAGED A DALA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SO 27 122DL 37754 1179 23436 580363 CLIMBING THRU 19000FT, LOUD BANG ON THE RIGHT SIDE. TEMP ONNO 2 ENG WENT TO 959 DEG. PULLED ENG TO IDLE. SUBSEQUENT ENG OIL EICAS MSG. SHUT DOWN ENG. ON ARRIVAL AT GATE, MTC FOUND OIL DRAINING FROM COWL, METAL IN TAIL PIPE AND FAN DIFFICULT TO TURN. REPLACED #2 ENGINE 2 L 7 2 4F 4 F RT A1NM E13NE 2001112900159 20011129 00159 NM 2001 11 29 DL72S011793 1 20011112 A 2900 ACTUATOR 10605582 BOEING 727 727232 1384082 NM #3 KRUEGER FLAP LEAKING A DALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 27 516DA 6739DEFCK 21432 LOST A SYSTEM HYDRAULICS ON CLIMBOUT FROM ABQ. LOST PRESSUREAND QUANTITY BOTH TO ZERO. _REPLD NBR 3 L/E FLAP ACTUATOR 2 L 7 3 4F A3WE 2001112900160 20011129 00160 NM 2001 11 29 DL73K011796 1 20011113 A 5740 654643915 TRACK BOEING 737 737232 1384475 NM TE FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 321DL 23093 THE REAR ENGINE MOUNT ATTACH HOLES ON THE #2 AND #3 TE O/B FLAP TRACKS WERE FOUND CORRODED. THE BORES WERE OVERSIZED TO .939" AND NEW BUSHINGS WERE INSTALLED. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001112900161 20011129 00161 NM 2001 11 29 DL72S011797 1 20011112 A 2560 1000677 LIGHT BOEING 727 727232 1384082 NM 1L DOOR UNSERVICEABLE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 544DA 22493 EXIT SIGN ABOVE 1L DOOR DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS TESTED. REPLACED LIGHT ASSY 2 L 7 3 4F A3WE 2001112900162 20011129 00162 NM 2001 11 29 DL757011802 1 20011113 A 2550 LIGHT BOEING 757 757232 1384965 NM 4L DOOR UNSERVICEABLE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 622DL 22912 4L ENTRY DOOR OUTSIDE EMERGENCY LIGHT INOP__C/A REPLACED LIGHT 2 L 7 2 4F RT A2NM 2001112900163 20011129 00163 NM 2001 11 29 DLM88011816 1 20011115 A 5330 5910082507 SKIN DOUG MD88 MD88 3023688 NM FS 200, L-17L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 997DL 53364 FUSELAGE / SKIN / FS 200 / LONG. 17L : DENT REPAIR THE FUSELAGE SKIN WAS FOUND WITH A DEEP DENT JUST AFT OF THE L1 DOOR AT FS 200 AND LONGERON 17L. THE DENT WAS REMOVED WITH A CUTOUT THROUGH ALL SKIN LAYERS. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER PER ER/A 382116-14, REV B. 2 L 7 2 4F RT A6WE 2001112900164 20011129 00164 NM 2001 11 29 DL757011825 1 20011116 A 5330 146N37505 SKIN BOEING 757 757232 1384965 NM FS 1700, S-18L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 656DL 24396 FUSELAGE / SKIN / FS 1700 / STRG. 18L-19L : DENT CUTOUT REPAIR THE FUSELAGE SKIN WAS DENTED AT FS 1700 BETWEEN STRINGERS 17L & 18L. THE DAMAGE WAS REMOVED WITH A 18" X 4.5" CUTOUT. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM DOUBLERS PER ER/A 382089-14, REV A. 2 L 7 2 4F RT A2NM 2001112900165 20011129 00165 NM 2001 11 29 DL757011828 1 20011119 A 3340 767 LAMP BOEING 757 757232 1384965 NM LT OVERWING BURNED OUT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 658DL 24420 OVERWING EMERGENCY LIGHT INOP - RELAMPED 2 L 7 2 4F RT A2NM 2001112900166 20011129 00166 NM 2001 11 29 DL73K011835 1 20011121 A 5311 65465511 FRAME BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 322DL 23094 A CRACK WAS FOUND IN THE FS 807 FRAME AT THE STR 13L SHEAR TIE. THE CRACK WAS CUT OUT AND A DOUBLER INSTALLED. THE DA MAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001112900167 20011129 00167 NM 2001 11 29 DL73K011836 1 20011121 A 5311 65465501 FRAME BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 322DL 23094 A CRACK WAS FOUND IN THE FS 787 FRAME AT THE STR 13L SHEAR TIE. THE DAMAGE WAS CUT OUT AND A DOUBLER INSTALLED. THE D AMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001112900168 20011129 00168 NM 2001 11 29 DL757011839 1 20011120 A 5330 146N351112 SKIN BOEING 757 757232 1384965 NM FS 1420, S-29L GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 656DL 24396 FUSELAGE / SKIN / FS 1416-1435 / STRG. 29L : REPAIR OF GOUGES THE FUSELAGE SKIN WAS FOUND WITH SEVERAL GOUGES AND DINGS BETWEEN FS 1416 & 1435 NEAR STRINGER 29L. THE DAMAGED AREA OF SKIN WAS REMOVED WITH A 15" X 4" CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 382096-14, REV A. 2 L 7 2 4F RT A2NM 2001112900169 20011129 00169 NM 2001 11 29 DL72S011854 1 20011124 A 3350 S106 BATTERY BOEING 727 727232 1384082 NM L1 DOOR DISCHARGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 528DA 21702 EMERGENCY LIGHT ABOVE 1L DOOR INOP.___BATTERIES DEAD. _REPLACED BATTERIES IN LIGHT ASSY. OP CKS NML. 2 L 7 3 4F A3WE 2001112900170 20011129 00170 NM 2001 11 29 DL75A011861 1 20011122 A 5330 146N853017 BEAR STRAP BOEING 757 757212 1384951 NM FS 1440, S-25R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 757AT 23127 FUSELAGE / SKIN / C2 DOOR CUTOUT / FS 1440 / STRG. 25R-26R: CORROSION BLEND REPAIR THE INTERNAL BEAR STRAP AROUND THE C2 DOOR CUTOUT WAS FOUND WITH AN AREA OF CORROSION NEAR THE AFT EDGE OF THE DOOR AT FS 1440 BETWEEN STRINGERS 25R & 26R. THE CORROSION WAS MACHINED AWAY AND THE AREA REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 382009-14, REV A. 2 L 7 2 4F RT A2NM 2001112900171 20011129 00171 NM 2001 11 29 DL72S011869 1 20011127 A 5750 651622291 ANGLE BOEING 727 727232 1384082 NM NBR 3 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 529DA 21703 NBR 3 SLAT AFT ANGLE CRACKED AT ACTUATOR ROD END ATTACH REPAIR PER MM 57-54-000-8 FIG 807 2 L 7 3 4F A3WE 2001112900172 20011129 00172 NM 2001 11 29 DL72S011871 1 20011127 A 5700 651622292 ANGLE BOEING 727 727232 1384082 NM NBR 6 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 529DA 21703 1.5 INCH CRACK UNDER STOP PAD NBR 6 SLAT OUTBOARD STOP PAD. COVE SKIN ANGLE REPAIRED PER M/M 57-54-000-8 2 L 7 3 4F A3WE 2001112900173 20011129 00173 NM 2001 11 29 DL73K011873 1 20011128 A 5311 6546541504 FRAME BOEING 737 737232 1384475 NM CABIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 322DL 23094 CRACKS WERE FOUND IN THE FS 663.75 FRAME AT STR 3L, 2L, AND 2R. THE CRACKS WERE REMOVED AND REPAIRED PER SRM 53-10-4, FIG 14. DUE TO ED PROBLEMS HOLES WERE CUT IN THE FUSELAGE SKIN AT EACH LOCATION AND REPAIRED BY INSTALLING A EXTERNAL DOUBLER AND TRIPLER. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001112900174 20011129 00174 NM 2001 11 29 DL72W011875 1 20011128 A 5700 65162242 ANGLE BOEING 727 727247 138408F NM NBR 8 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 292WA 22110 NBR 8 SLAT ANGLE CRACKED AT ANTIICE T DUCT CUTOUT FOUND ON F1 LETTER CHECK REPAIRED PER MM 57-54-000-8 2 L 7 3 4F A3WE 2001112900175 20011129 00175 NM 2001 11 29 DL72W011876 1 20011128 A 5700 651622370 ANGLE BOEING 727 727247 138408F NM NBR 7 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 292WA 22110 NBR 7 SLAT ANGLE CRACKED AT INBD STOP PAD ATTACH FOUND AT F1 LETTER CK REPAIRED PER MM 57-54-000-8 2 L 7 3 4F A3WE 2001112900176 20011129 00176 NM 2001 11 29 DL75A011648 1 20011010 A 5330 143N36912 SKIN BOEING 757 757212 1384951 NM FS 690, S-24R DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 750AT 23126 FUSELAGE / SKIN / FS 690 / STRG. 24R-25R : SKIN CUTOUT REPAIR AN EXISTING SKIN REPAIR DOUBLER WAS DAMAGED AND REMOVED. THE UNDERLYING SKIN WAS CLEANED UP WITH A 8" X 4" CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 381721-14, REV A. 2 L 7 2 4F RT A2NM 2001112900177 20011129 00177 NM 2001 11 29 DL72W011652 1 20011011 A 5700 ANGLE BOEING 727 727247 138408F NM RT WING L/E CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 295WA 22532 A/C IN TPA FOR E2 LETTER CK. NBR 7 SLAT ANTIICE T DUCT CUTOUT CRACKED. REPAIRED PER MM 57-54-000-8. 2 L 7 3 4F A3WE 2001112900178 20011129 00178 NM 2001 11 29 DLM88011658 1 20011012 A 3210 NA TARGET DOUG MD88 MD88 3023688 NM LT GEAR DOOR BROKEN A DALA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 SO 27 946DL 49819 ON APPROACH TO ATL GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS DOWN AND LOCKED. REPLACED LEFT GEAR DOOR PROX TARGET 2 L 7 2 4F RT A6WE 2001112900179 20011129 00179 NM 2001 11 29 DL72S011661 1 20011012 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM LT FWD O/W SLIDE DISCHARGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 531DA 21814 LT FWD O/W SLIDE LIGHT INOP. REPLCD BATT PACK. OPS CKS GOOD 2 L 7 3 4F A3WE 2001112900180 20011129 00180 NM 2001 11 29 DL73K011673 1 20011016 A 5310 6546561509 FRAME BOEING 737 737232 1384475 NM R-2 DOOR FRAME CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 314DA 23086 1" CRACK IN R-2 DOOR CUTOUT FRAME, JUST BELOW UPPER FWD. ROLLER CASTING REMOVE & REPLACE FRAME SECTION PER DRAWING 2 L 7 2 4F RT A16WE 2001112900181 20011129 00181 NM 2001 11 29 DL73K011675 1 20011016 A 3350 20131A BATTERY BOEING 737 737232 1384475 NM FWD CABIN UNSERVICEABLE A DALA O OTHER L NO TEST IN INSP/MAINT 1 SO 27 313DL 23085 FWD CABIN EMEGENCY EXIT LIGHTS INOP RPLD BATTERY PACK NOW OPS NML 2 L 7 2 4F RT A16WE 2001112900182 20011129 00182 NM 2001 11 29 DLM88011681 1 20011017 A 7710 LG80E1 ENGINE DOUG MD88 MD88 3023688 NM #2 ENGINE ERRATIC A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 968DL 24999 53161 726827 SIGNIFIGANT THROTTLE REDUCTION AFTER T/O LT ENG EPR READ 2.08. RT ENG READ 1.54 ALL OTHER INDICATIONS NORMAL. REPLACED NBR 2 ENG. EPR TRANSMITTER. 2 L 7 2 4F RT A6WE 2001112900183 20011129 00183 NM 2001 11 29 DL72S011682 1 20011017 A 5700 ANGLE BOEING 727 727232 1384082 NM R/H SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 LWR COVE SKIN ANGLE IS CRACKED AT #7 SLAT I/B UPSTOP PAD. SLAT SER # BN324. REPAIRED PER M/M 57-54-000-8 2 L 7 3 4F A3WE 2001112900184 20011129 00184 NM 2001 11 29 DL72S011688 1 20011018 A 5300 SKIN BOEING 727 727225A 1384077 NM R1 DOOR CUTOUT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8882Z 21579 FOUND ON C2 LETTER CK 5/16 IN CRACK FUSELAGE SKIN R-1 DOOR LOWER AFT CUTOUT. REPAIRED PER ERA 381969-14 AND EO 4-58974-3AD. 2 L 7 3 4F RT A3WE 2001112900185 20011129 00185 NM 2001 11 29 DL767011691 1 20011020 A 3350 20131A BATTERY PACK BOEING 767 767232 1385132 NM SEAT 03A WALL DISCHARGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 102DA 22214 ON L/O FOUND L-1DOOR AND 3 LT OVERWING EGRESS EMER LTS. INOPREPLACED M-736 BATTERY PACK, OPS CK GOOD 2 L 7 2 4F RT A1NM 2001112900186 20011129 00186 NM 2001 11 29 DL73K011697 1 20011022 A 5311 FRAME BOEING 737 737232 1384475 NM CABIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 327DL 23099 THE FRAMES AT FS 727B-RH, 747-LH, 787-RH, 787-RH, 827-LH, 847-LH AND 907-RH WERE ALL FOUND CRACKED AT STR 9. THE DAMAGED FLANGES WERE CUT OUT AND REPAIRED PER SRM 51-40-3, FIG 1. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001112900187 20011129 00187 NM 2001 11 29 DL73K011698 1 20011022 A 5311 65465417 FRAME BOEING 737 737232 1384475 NM CABIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 327DL 23099 THE FS 663.75 FRAME WAS FOUND CRACKED AT STR 1 AND STR 3L. THE CRACKS WERE CUT OUT, THE AREA NDT INSPECTED AND A REPAIR PER SRM 53-10-4, FIGURE 14 INSTALLED. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001112900188 20011129 00188 NM 2001 11 29 DL73K011699 1 20011022 A 5330 654577882 SKIN BOEING 737 737232 1384475 NM SKIN DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 327DL 23099 A CRACK AND DENT WERE FOUND AT THE LOWER HINGE CUTOUT OF THEAFT GALLEY DOOR. THE DAMAGES WERE CUTOUT AND A DOUBLER, TRIPLER, AND QUADRUPLER WERE INSTALLED. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001112900189 20011129 00189 NM 2001 11 29 DL73K011705 1 20011019 A 5330 SKIN BOEING 737 737247 138448D NM FS 727B, S-18R CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 379DL 23606 FUSELAGE / SKIN / FS 727B / STRG. 18R : CRACK REPAIR INSPECTION OF THE FUSELAGE SKIN REVEALED A 1" AT FS 727B JUST ABOVE THE WAFFLE DOUBLER LINE AT STRINGER 18R. THE CRACK WAS REMOVED WITH A CUTOUT AT THE STRINGER. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 381960-14. 2 L 7 2 4F A16WE 2001112900190 20011129 00190 NM 2001 11 29 DL72S011714 1 20011021 A 5330 SKIN BOEING 727 727225A 1384077 NM R1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8882Z 21579 FUSELAGE / SKIN / FWD GALLEY DOOR CUTOUT / LWR AFT CORNER : CRACK REPAIR THE LOWER AFT CORNER OF THE FWD GALLEY DOOR CUTOUT WAS FOUNDWITH A CRACK EMANATING FROM A FASTENER HOLE. THE CRACK IS TYPICAL OF BAC S/B 727-53-0188. THE CRACK WAS IN THE SKIN ONLY AND WAS REMOVED WITH A CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL REPAIR DOUBLER PER THE S/B AND PER ER/A 381969-14. 2 L 7 3 4F RT A3WE 2001112900191 20011129 00191 NM 2001 11 29 DL72W011716 1 20011024 A 5500 6572784 ELEVATOR BOEING 727 727247 138408F NM TAIL CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 294WA 22112 1/4" CRACK AT RIVET UPPER SKIN OF R/H ELEVATOR APPROX. 14" FWD OF TAB CENTER HINGE. REPAIRED PER DRD 55-20-3D,AND RESTENCILED ELEVATOR 2 L 7 3 4F A3WE 2001112900192 20011129 00192 NM 2001 11 29 DL72S011722 1 20011016 A 5720 65162221 SLAT BOEING 727 727232 1384082 NM # 3 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 543DA 22392 MULTIPLE RIBS CRACKED,REPAIRED PER AMM 57-54-000-8 FIG 814 2 L 7 3 4F A3WE 2001112900193 20011129 00193 NM 2001 11 29 AWXA200100605 1 20011126 A 5311 65465962 FRAME BOEING 737 737277 1384570 NM STA 727B CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 PHX- MAJOR REPAIR - "C" - DURING INSPECTION MAINTENANCE DISCOVERED SKIN SLIGHTLY RAISED WITH 4 LOOSE RIVETS AND 1 POPPED RIVIT AT STA 727B 6" FORWARD OF ANTENNA. FURTHER INSPECTION REVEALED BOTTOM LEG OF FRAME BOTTOM CORRODED AT STA 727B BE TWEEN STR 27L AND 27R. MAINTNENACE REMOVED EXISTING FRAME STA 727B BETWEEN STR 27L AND 27R AND CORRODED SECTION OF FRAME TO STR 26L. CORROSION WAS REMOVED FROM FUSELAGE SKIN, THICKNESS CHECKED WITHIN LIMITS. FABRICATED BLANKING PLATE, FRAME SECTION, AND SPLICE ANGLES AND INSTALLED IAW SRM 51-40-3 FIG 1. PG 1. 2 L 7 2 4F RT A16WE 2001113000001 20011130 00001 WP 2001 11 30 0104309751 1 20010621 A 5310 FORMER DOUG DC9 DC941 302207N WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 751NW 47115 During Inspection in CMH a crack was found in the -45 former. The crack extended from the O/B most fastener hole. Repair ed per EA 97-181291. 2 L 7 2 4F A6WE 2001113000002 20011130 00002 WP 2001 11 30 0104489927 1 20010604 A 5310 FITTING DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8920E 45835 During H ck in ATL the longeron 26r end fitting was found cracked at sta 598. Repaired per EA. 99-181209. 2 L 7 2 4F A6WE 2001113000003 20011130 00003 WP 2001 11 30 0104499994 1 20011119 A 5310 TEE FITTING DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8979E 47328 During H ck at ATL, a tee at sta 756 floor beam outboard end LHS was found cracked. Material 7075-t6511 Aluminum. Repair ed per EA 99-185274. 2 L 7 2 4F A6WE 2001113000004 20011130 00004 WP 2001 11 30 0104329971 1 20010606 A 5322 SEAT TRACK DOUG DC9 DC931 3022065 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9335 47337 During H ck in ATL, The outboard seat track x=-22 rh was found corrosion between 588 and 746. Repaired per EA 99-1812575 . 2 L 7 2 4F A6WE 2001113000005 20011130 00005 WP 2001 11 30 0104339971 1 20010607 A 5310 PRESSURE PANEL DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9335 47337 During H ck in ATL, two cracks were found in the horizontal pressure panel at station 105 at x=25 and x=27. The crack at x=25 is typical of the cracks repaired in the dc-9 trm, 53-10-02 except this crack is 2.4" long. The crack at station x =27 is 1/2" long. Material 0.040" 2024-t3 Al. Repaired per EA 99-181213. 2 L 7 2 4F A6WE 2001113000006 20011130 00006 WP 2001 11 30 0104349909 1 20010607 A 5310 BULKHEAD DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 959N 47255 During H ck in ATL, one crack 1/2" long was found in the station 756 bulkhead. The crack is located in the upper end of the verticle stiffener at x=-22. Material 2014-t6511 AL. Repaired per EA 99-181259. 2 L 7 2 4F A6WE 2001113000007 20011130 00007 WP 2001 11 30 0104359971 1 20010608 A 5310 STIFFENER DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9335 47337 During H ck in ATL, two .75" long cracks were found in the Sta 756 bulkhead. The cracks are located in the upper ends of the verticle stiffeners at x=-11 and x=-22. Repaired per EA 99-181222. Material 2014-t6511 AL. 2 L 7 2 4F A6WE 2001113000008 20011130 00008 WP 2001 11 30 0104369927 1 20010611 A 5340 FITTING DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8920E 45835 During Hck at the ATL Maintenance. The LHS MLG door hinge fitting AFT lug was found cracked. Material 7075-t6511, repair ed per EA 99-181272 2 L 7 2 4F A6WE 2001113000009 20011130 00009 WP 2001 11 30 0104379971 1 20010612 A 5740 SKIN DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9335 47337 During A H Ck inATL, a crack was found in the lower skin of the LH inbd slat at station Xis =136.42. Stopped drilled and doubler installed 2014-t6 AL. Repaired per EA 99-181273 2 L 7 2 4F A6WE 2001113000010 20011130 00010 WP 2001 11 30 0104399978 1 20010629 A 5520 SKIN DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9342 47391 During Hck in ATL, the LH Elevator skin at XET 167 was found cracked at the outboard end where the gear tab fairing is a ttached. Material 0.025" 2014-t6 AL. Repaired per EA 99-181274. 2 L 7 2 4F A6WE 2001113000011 20011130 00011 WP 2001 11 30 0104409922 1 20010705 A 5330 DOUBLER DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 945N 47664 During an Mck in ATL the production finger doubler along Longeron 18L was found with a cracked finger sta 850. Material .025" 2014-t6 AL. Repaired per EA 99-181280. 2 L 7 2 4F A6WE 2001113000012 20011130 00012 WP 2001 11 30 0104419958 1 20010706 A 5410 RIB DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 917RW 47145 During Mck in ATL, The aft portion of the lower cap of the pylon closing rib was found cracked. The crack is approximate ly .7" long and extends from a hole 3.7" from the end of the cap. Material TI-6AI-4V. Repaired per EA. 99-181307. 2 L 7 2 4F A6WE 2001113000013 20011130 00013 WP 2001 11 30 0104429989 1 20010706 A 5310 WEB DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8945E 47181 During H ck in ATL a 5" long crack was found in the RH floorbeam web cusp membrane at STA 617. The damaged section of th e cusp membrane extends from station 598 to sta 658. Material .202" 7075-t6 AL. Repaired per EA 99-181334. 2 L 7 2 4F A6WE 2001113000014 20011130 00014 WP 2001 11 30 0104439989 1 20010709 A 5310 WEB DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8945E 47181 During Hck in ATL, a .25" crack was found on the doorjamb web at station 617 RHS. Repaired per EA 99-181318. Material 20 24-t42 AL 2 L 7 2 4F A6WE 2001113000015 20011130 00015 WP 2001 11 30 0104449922 1 20010709 A 5310 INTERCOSTAL DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 945N 47664 During M ck in ATL, A crack was found in the outboard end of the 923484-9 intercostal at station 180 at x=-20. Material 7075-t6 AL. Repaired per EA 99-181321. 2 L 7 2 4F A6WE 2001113000016 20011130 00016 WP 2001 11 30 0104459864 1 20010710 A 5330 SKIN DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 773NC 47775 During CK in MSP, A skin crack was found near the aft cargo door cutout in the skin at the lower aft corner. Skin is .06 3 2024-t3. Repaired per EA 99-183545. 2 L 7 2 4F RT A6WE 2001113000025 20011130 00025 WP 2001 11 30 01FDEA01007 1 20011127 A 5320 WEB DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 303FE 46802 AFT CARGO TUNNEL BS 1897-1902, STR 27R INTERCOSTAL PANEL CORRODED. REMOVED AND REPLACED WEB AND CHANNEL PER SRM 51-00-0 0, 51-21-01, 51-35-01 & 51-33-01. 2 L 7 3 4F RT A22WE 2001113000026 20011130 00026 WP 2001 11 30 01FDEA01008 1 20011127 A 5320 INTERCOSTAL DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 303FE 46802 AFT CARGO TUNNEL BS 1847-1857, STR 28R INTERCOSTAL PANEL CORRODED. REMOVED AND REPLACED INTERCOSTAL PER SRM. 2 L 7 3 4F RT A22WE 2001113000027 20011130 00027 NM 2001 11 30 2001UALA02230 1 20011030 A 7930 WARNING SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE OIL SYSTEM ACTIVATED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 590UA 28708 727249 NR 2 ENGINE EICAS MSG OIL FILTER DISPLAYED. OIL FILTER CHECKED CLEAN. REPLACED FILTER AND THE DIFFERENTIAL PSI SWITCH. SUBSEQUENT WRITE UP FOR SAME MESSAGE, OIL FILTER CHECKED CLEAN. REPLACED FILTER AND THE DIFFERENTIAL PSI SWITCH. DRA INED AND FILLED THE MAIN GEAR BOX AND OIL TANK DUE TO SUSPECTED HIGH CARBON CONTENT IN THE OIL. 2 L 7 2 4F 4 F RT A2NM E17NE 2001113000031 20011130 00031 NM 2001 11 30 CALA0101013 1 20011127 A 5414 SKIN BOEING 737 7373T0 1384582 NM #1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17309 23360 INSPECTION FOUND A 1/2" CRACK IN #1 PYLON SKIN PANEL #5727L. REPAIRED IAW ECRA 5430-01230. 2 L 7 2 4F RT A16WE 2001113000032 20011130 00032 NM 2001 11 30 CALA0101014 1 20011128 A 5311 BELTFRAME BOEING 737 7373T0 1384582 NM STA 500 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14307 23358 INSPECTION FOUND FORWARD BAGGAGE BIN BELTFRAME CORRODED AT STA 500, AFT SIDE, O/B, S27R. REPAIRED BELTFRAME IAW SRM 53-0 0-09, FIGURE 203, PAGE 207-209. 2 L 7 2 4F RT A16WE 2001113000033 20011130 00033 NM 2001 11 30 CALA0101016 1 20011128 A 5311 FRAME BOEING 737 7373T0 1384582 NM STA 1006 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17309 23360 INSPECTION FOUND FRAME CORRODED AT STA 1006 BETWEEN S16R AND S15R. A FRAME REPAIR SECTION AND SPLICES WERE INSTALLED IAW SRM 53-00-07, FIGURE 201. 2 L 7 2 4F RT A16WE 2001113000034 20011130 00034 NM 2001 11 30 CALA0101017 1 20011130 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM STA 887-907 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17309 23360 INSPECTION FOUND CABIN L/H O/B SEAT TRACK CORRODED AT STA 887-907. REPAIRED SEAT TRACK IAW SRM 53-00-52, FIGURE 204. 2 L 7 2 4F RT A16WE 2001113000037 20011130 00037 NM 2001 11 30 2001UALA02294 1 20011116 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 921UA 25388 AFT CABIN FLOORBEAM STATION 947 RBL 22 IS CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2001113000038 20011130 00038 NM 2001 11 30 2001UALA02295 1 20011116 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 921UA 25388 AFT CABIN STATION 947 RBL 27 FLOORBEAM CAP HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2001113000039 20011130 00039 NM 2001 11 30 2001UALA02296 1 20011117 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 921UA 25388 DENT IN EXTERNAL FUSELAGE BODY STATION 1013, 9 O'CLOCK. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001113000040 20011130 00040 NM 2001 11 30 2001UALA02297 1 20011117 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 921UA 25388 STATION 294.5 WL 210 INCORRECT REPAIR ON FRAME. MAJOR REPAIR ACCOMPLISHED. REMOVED OLD REPAIR. INSTALLED DOUBLER REPA IR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001113000041 20011130 00041 NM 2001 11 30 2001UALA02299 1 20011114 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 122UA 29168 ROW 34C EMERGENCY CEILING LIGHT IS INOP. RELAMPED, OPS CHECKED EMERGENCY CEILING LIGHT OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2001113000042 20011130 00042 NM 2001 11 30 2001UALA02301 1 20011117 A 5330 DOUBLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 521UA 24891 LEFT EXT FUSE SKIN DOUBLER DENTED AT STATION 612 STRINGER 16L. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2001113000043 20011130 00043 NM 2001 11 30 2001UALA02303 1 20011118 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 521UA 24891 AFT CARGO COMPT BODY STATION 1480 INNER CHORD ON CIRCUMFERENTIAL FRAME IS DENTED ABOVE STRINGER 26L. MAJOR REPAIR ACCOM PLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2001113000044 20011130 00044 NM 2001 11 30 2001UALA02304 1 20011118 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 521UA 24891 AFT CARGO COMPARTMENT BODY STATION 1400 CIRCUMFERENTIAL FRAME INNER CHORD IS DAMAGED ABOVE STRINGER 26L. MAJOR REPAIR A CCOMPLISHED. DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2001113000045 20011130 00045 NM 2001 11 30 2001UALA02305 1 20011118 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 521UA 24891 FWD CABIN FLOORBEAM T-CAP BODY STATION 310 RBL 40 HAS SURFACE CORROSION AND ADJACENT WEB DAMAGED DURING INTERCOSTAL REMO VAL. MAJOR REPAIR ACCOMPLISHED. STRAP AND ANGLE REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2001113000046 20011130 00046 NM 2001 11 30 2001UALA02306 1 20011118 A 5320 ANGLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 650UA 25287 CABIN R-1 DOOR THRESHOLD LOWER CHORD ANGLE IS CORRODED AT THE FORWARD SECTION. MAJOR REPAIR ACCOMPLISHED. REPLACED DOO R CHORD ANGLE. 2 L 7 2 4F 4 F RT A1NM E24NE 2001113000047 20011130 00047 NM 2001 11 30 2001UALA02307 1 20011119 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 178 BULKHEAD WEB SHOWS CRACK INDICATION AT RBL 5.7 AT WL 197. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001113000048 20011130 00048 NM 2001 11 30 2001UALA02308 1 20011119 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 178 BULKHEAD WEB SHOWS CRACK INDICATION ON RBL 5.7 WL 212. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001113000049 20011130 00049 NM 2001 11 30 2001UALA02309 1 20011119 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 178 BULKHEAD WEB SHOWS CRACK INDICATION AT LBL 5.7 ON WL 212. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001113000050 20011130 00050 NM 2001 11 30 2001UALA02310 1 20011120 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 921UA 25388 FUSELAGE EXTERIOR SKIN DENTED STATION 410 BELOW STRINGER 26R NEXT TO SKIN LAP. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBL ER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001113000051 20011130 00051 WP 2001 11 30 ABXA010595 1 20011127 A 5610 TRACK DOUG DC9 DC932 3022066 WP COCKPIT WINDOW DIRTY A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 CAPTAIN'S CLEAR VIEW WINDOW WAS STUCK CLOSED. OPENED WINDOW AND CLEANED THE TRACK. OPS CHECKED GOOD IAW DC-9 MM. 2 L 7 2 4F A6WE 2001113000052 20011130 00052 WP 2001 11 30 ABXA010596 1 20011128 A 5250 DOOR DOUG DC9 DC931 3022065 WP COCKPIT STUCK A ABXA K NONE O OTHER CR CRUISE 1 GL 23 944AX 47550 INFORMED BY THE CREW AFTER FLIGHT, THE COCKPIT DOOR WAS STUCK IN FLIGHT. INSPECTED THE COCKPIT DOOR, HINGE, HANDLE, AND ALL THE SURROUNDING AREAS. NO DEFECT FOUND. OPS CHECKED GOOD IAW DC-9 MM. 2 L 7 2 4F A6WE 2001113000053 20011130 00053 WP 2001 11 30 ABXA010599 1 20011122 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC932F 3022067 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 909AX 47148 ON SERVICE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC-9 AMM 33-5 3-00-8-0001. 2 L 7 2 4F A6WE 2001113000056 20011130 00056 WP 2001 11 30 ARWA20011116 1 20011120 A 5410 STRAP DOUG DC8 DC862 3021970 WP NR 4 PYLON CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 1808E 46105 DURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND: NR 4 PYLON ACCESS DOOR 409 RT WITH TEMPORARY REPAIR, AFTER EVALUATI ON, FOUND CRACK ON OUTBOARD UPPER STRAP AT STA YUS 217. REPLACED STRAP IAW DC8 SRM 54-3-2,FIG 35, ITEM 5, NOTE 10. ACC OMPLISHED SB 54-70. REWORKED UPPER SPAR STRAP AND FABRICATED SHIMS IAW DC8 S/B 54-70, FIG 1. 2 L 7 4 4F 4A25 2001113000057 20011130 00057 NM 2001 11 30 F3LA200100124 1 20011114 A 2161 6075103 CONTROLLER BOEING 737 7372L9 1384497 NM A/C BAY FAILED A F3LA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B E SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET CL CLIMB 1 NM 03 271FL 656 22734 AIR TURN BACK. FLIGHT CREW REPORTED LOUD RUMBLE NOISE NEAR RT. PACK, ASSOCIATED WITH STRONG SMELL. TURNED PACK AND RT. BLEED OFF AND SMELL AND NOISE WENT AWAY. LOW VIBRATION CONTINUED. MAINTENANCE RAN RT. PACK AND COULD NOT DUPLICATE DIS CREPANCY. OPENED PACK BAY DOOR AND INSPECTED AREA WITH PACK ON. NO ABNORMALITIES WERE FOUND. AIRCRAFT WAS FERRIED TO DEN WITH NO ABNORMAL NOISE OR SMELLS OBSERVED. UPON ARRIVAL IN DEN, MAINTENANCE FOUND WATER SEPARATOR BAG HEAVILY ICED AND 35 DEG.TEMP. CONTROL SYSTEM INOPERATIVE IN RT. A/C BAY. REPLACED RT. 35 DEG. TEMP. CONTROLLER. 2 L 7 2 4F RT A16WE 2001113000058 20011130 00058 NE 2001 11 30 ARWA20011117 2 20011119 A 7200 RB211524B402 ENGINE LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B402 54555 NE NR 3 MAKING METAL A ARWA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 19 308GB 48009 2989 193U1133 14620 AT CRUISE 33,000; NR 3 ENGINE OIL PRESSURE DROPPED TO 30 PSI - MOVED THROTTLE TO IDLE, OIL PRESSURE REDUCED TO 20 PSI; C OMPLETED ENGINE SHUTDOWN PROCEDURE AT 23:45 ZULU. OIL QUANTITY IS OK. INSPECTION REVEALED METAL IN OIL SYSTEM. ACCOMP LISHED NR 3 ENGINE CHANGE IAW ARROW AIR RB 211 MAINTENANCE FORM L-1011-7104A & ENGINE OPERATIONAL CHECK IAW ARROW AIR RB 211 MAINTENANCE FORM L-1011-7102B ENGINE OPS CHECKED NORMAL. ACCOMPLISHED ADJUSTMENT AND TEST ALT ALERT, OPS NORMAL IA W MM 22-17-00 PG 512. 2 L 7 3 4F 4 F A23WE E12EU 2001113000062 20011130 00062 NM 2001 11 30 F3LA200100125 1 20011117 A 7110 DOUBLER BOEING 737 7372L9 1384497 NM NR 2 COWLING TORN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 3902 22733 DURING C-1 CHECK, INSPECTION REPORTED NR 2 ENGINE OTBD ENGINE COWL DOUBLER METAL TORN AT LATCH CUTOUT, 5TH LATCH FROM AF T. FABRICATED AND INSTALLED DOUBLER AND STRIKER PLATE PER SRM 51-40-2. 2 L 7 2 4F RT A16WE 2001113000063 20011130 00063 WP 2001 11 30 ARWA20011122 1 20011124 A 3230 450100109 MODULE LKHEED 1011 1011385115 5265015 WP LANDING GEAR DEFECTIVE A ARWA O OTHER O OTHER DE DESCENT 1 SO 19 308GB 193U1133 COULD NOT EXTEND LANDING GEAR NORMALLY AT MIA; EXTENDED GEAR BY ABNORMAL ALTERNATE EXTENSION PROCEDURES. REMOVED AND RE PLACED LANDING GEAR CONTROL (MODULE) & 4 WAY SOLENOID VALVE IAW MM 32-31-14 & 32-31-02. PERFORMED LANDING GEAR RETRACTI ON AND EXTENSION TEST AND WAS NORMAL IAW MM 32-20-00. 2 L 7 3 4F A23WE 2001113000064 20011130 00064 2001 11 30 GLBA2001234 4 20011127 A 3100 1303800057 INDICATOR BEECH 1900 1900D 1154162 CE #2 LEAKING A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 03 211GL 1618 10 UE211 AIR SPEED INDICATOR FAILED ON T/O, REPLACED OPS CHECKED SYSTEM SATISFACTORY 2 L 7 2 4T RT A24CE 2001113000065 20011130 00065 2001 11 30 GLBA2001232 4 20011124 A 3100 1143800351 INDICATOR BEECH 1900 1900D 1154162 CE #2 ERRATIC A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 202UX 342 UE202 #2 VSI FLUX, REPLACED INDICATOR OPS CHECKED SYSTEM SATISFACTORY 2 L 7 2 4T RT A24CE 2001121900124 20011219 00124 NM 2001 12 19 F3LA200100127 1 20011125 A 5754 RIVET BOEING 737 737228 13844AG NM L/E SLAT LOOSE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED RT WING NR 5 SLAT HAD WORKING RIVETS ON LOWER T/E SKIN AROUND ACTUATOR AND INBD OF TRACKS. REPLACED RIVETS PER SRM 51-30-02. 2 L 7 2 4F RT A16WE 2001121900125 20011219 00125 NM 2001 12 19 F3LA200100128 1 20011125 A 5754 RIVET BOEING 737 737228 13844AG NM L/E SLAT LOOSE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED RT WING NR 4 SLAT LOWER INNER SKIN RIVETS LOOSE FROM INSIDE STRUCTURE BETWEEN ACTU ATOR AND OTBD OF TRACKS. REPLACED LOOSE FASTENERS PER SRM 51-30-2. 2 L 7 2 4F RT A16WE 2001121900126 20011219 00126 NM 2001 12 19 F3LA200100129 1 20011125 A 5754 RIVET BOEING 737 737228 13844AG NM L/E SLAT LOOSE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED RT WING NR 6 SLAT HAD PULLED AND WORKING RIVETS ON LOWER SKIN T/E AROUND ACTUATOR. REPLACED FASTENERS PER SRM 51-30-02. 2 L 7 2 4F RT A16WE 2001121900127 20011219 00127 NM 2001 12 19 F3LA200100130 1 20011125 A 5754 RIVET BOEING 737 737228 13844AG NM L/E SLAT LOOSE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED RT WING NR 6 L/E SLAT HAD PULLED AND WORKING RIVETS ON INSIDE L/E OTBD OF ACTUATOR AND INBD OF OTBD MAIN TRACK. REPLACED FASTENERS PER SRM 51-30-02. 2 L 7 2 4F RT A16WE 2001113000067 20011130 00067 NM 2001 11 30 C1HA200195018 1 20011124 A 3350 LIGHT BOEING 727 727290 138408W NM CABIN INOPERATIVE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 295AS 22147 RIGHT AFT EMERGENCY EXIT OVERWING LIGHT RT AFT CARGO DOOR INOP. RELAMPED IAW MM 33-50-11, OPS CHECK NORM. 2 L 7 3 4F A3WE 2001113000068 20011130 00068 NM 2001 11 30 C1HA200197011 1 20011124 A 3350 BATTERY BOEING 727 727270 138408P NM CABIN DISCHARGED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 697CA 23052 FWD EXTERIOR SLIDE LIGHT INOP. REMOVED AND REPLACED BATTERY PWR SUPPLY PER MM 33-50-51. OPS CHECK GOOD. 2 L 7 3 4F RT A3WE 2001113000069 20011130 00069 NM 2001 11 30 C1HA200197012 1 20011128 A 3350 LIGHT BOEING 727 727270 138408P NM CABIN INOPERATIVE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 697CA 23052 EMERGENCY EXIT LIGHT BULBS BURNED OUT FWD ENTRY, ROWS, CENTER AND AFT CABIN. RELAMPED EMERGENCY EXIT LIGHTING AS REQUIR ED. 2 L 7 3 4F RT A3WE 2001113000070 20011130 00070 SO 2001 11 30 C2XA01CL232 1 20011125 A 2611 SMOKE WARNING EMB 135 EMB135ER 3260203 SO COCKPIT MALFUNCTIONED A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 14508 145220 CLE FLIGHT 3207 THE CREW REPORTED AFTER TAKEOFF RECEIVED A LAV SMOKE WARNING. THE AIRCRAFT RETURNED TO MDT AND LANDED W ITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE LAV SMOKE SYSTEM. NO DEFECTS WE RE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001113000071 20011130 00071 SO 2001 11 30 C2XA01CL234 1 20011128 A 2120 ODOR EMB 145 EMB145LR 3260212 SO CABIN DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 13955 145075 CLE FLIGHT 3189 THE CREW REPORTED A FUEL ODOR WHEN SELECTING THE PACKS ON WITH THE APU BLEED ON. MAINTENANCE INSPECTED AND RAN PACKS OFF THE APU BLEED AND FOUND NO DEFECTS. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001113000072 20011130 00072 NE 2001 11 30 C2XA01CL235 2 20011129 A 7261 M832481113 O-RING EMB 135 EMB135ER 3260203 SO PWA 118 PW118 NE NR 2 ENGINE DAMAGED A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 27 17507 145215 CLE FLIGHT 3237 THE CREW REPORTED NR 2 ENGINE OIL LEVEL AND PRESSURE WAS DROPPING. THE NR 2 ENGINE WAS SHUT DOWN AND TH E AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE SHAFT O-RING ON THE NR 4 GENERATOR. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 T RT T00011AT E20NE 2001113000073 20011130 00073 SO 2001 11 30 C2XA01TY187 1 20011126 A 3350 1317 LIGHT EMB 135 EMB135LR 3260305 SO ENTRY DOOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17521 145378 TYS DURING A SCHEDULED INSPECTION THE CABIN ENTRANCE DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANC E REMOVED AND REPLACED THE LIGHT BULB IN THE ENTRANCE DOOR EMERGENCY EXIT LIGHT ASSEMBLE IAW EMB-135 MM 33-26-04. THE O PERATIONAL CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT TOOO11AT 2001113000074 20011130 00074 2001 11 30 C2XA01TY188 4 20011126 A 3418 6235 MOTOR EMB 145 EMB145ER 3260211 SO STICK SHAKER FAILED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14942 9072 9072 145037 TYS DURING A SCHEDULED INSPECTION THE CAPTAINS STICK PUSHER FAILED OPERATIONAL CHECKS. MAINTENANCE REMOVED AND REPLAC ED THE CAPTAINS STICK PUSHER MOTOR IAW EMB-145 27-36-04, OPERATIONAL CHECKS WERE SATISFACTORY. THE AIRCRAFT RELEASED FO R SERVICE. 2 L 7 2 4F RT T00011AT 2001113000075 20011130 00075 SO 2001 11 30 C2XA01TY190 1 20011129 A 5315 14521721009 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17513 145292 TYS DURING A SCHEDULED INSPECTION THE FORWARD DIGITAL PLATE LOCATED BENEATH THE FLOOR AND JUST AFT OF THE COCKPIT ENTR ANCE DOOR WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE REMOVED THE DAMAGED AREA AND ACCOMPLISHED A FILLER/ DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5320-01059, EMB SRM 51-20-03, 51-40-02 AND CPM 51-21-04, 05 AND 06. THE REPAI R WAS SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT TOOO11AT 2001113000076 20011130 00076 SO 2001 11 30 CHQ00042 1 20011122 A 3230 LANDING GEAR EMB 145 EMB145 3260210 SO NLG & MLG MALFUNCTIONED A CHQA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 CHQA 145391 LG/LEVER DISAGREE MESSAGE ON EICAS AND GEAR WOULD NOT GO UP. 2 L 7 2 4F RT T00011AT 2001113000077 20011130 00077 WP 2001 11 30 MWEA011464 1 20011130 A 5310 59114272 SKIN DOUG DC9 DC915 3022036 WP STATION 815 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 EXTERIOR SKIN IS CRACKED AT STATION 815 LONGERON 17 RIGHT -- CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001113000078 20011130 00078 NE 2001 11 30 CHQ00043 2 20011123 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LEFT OVERTEMP A CHQA C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 GL 11 158CQ 158 LEFT ENGINE OVERTEMP DURING TAKEOFF ROLL, ABORTED TAKEOFF. 2 L 7 2 4T 4 T RT A52EU E8NE6 2001113000079 20011130 00079 NE 2001 11 30 CHQ00044 2 20011124 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LEFT OVERTEMP A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 CHQA 150 LEFT ENGINE OVERTEMP DURING TAKEOFF ROLL WITH CTOT ON. 2 L 7 2 4T 4 T RT A52EU E8NE6 2001113000080 20011130 00080 WP 2001 11 30 ABXA010600 1 20011112 A 5712 991707341 RIB DOUG DC9 DC933F 302207A WP LEFT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 EXFOLIATION CORROSION ON LEFT WING REAR SPAR RIB, ABOVE THE CENTER ATTACH POINT OF THE INBOARD BUTE DOOR. REPLACED RIB I AW DC-9 SRM 51-30-2, 51-30-5 AND 51-30-8. 2 L 7 2 4F A6WE 2001113000081 20011130 00081 WP 2001 11 30 ABXA010602 1 20011113 A 5230 59101417 PAN DOUG DC9 DC933F 302207A WP FWD. CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 FORWARD LOWER CARGO DOOR STOP FITTING CRACKED ON AFT EDGE OF DOOR, 2ND FROM TOP. REPAIRED AREA IAW DC-9 SRM 52-05 AND SH OP TRAVELER # ST-0148-04. NOTE: CRACK WAS IN DOOR INNER PAN, NOT THE FITTING. 2 L 7 2 4F A6WE 2001113000082 20011130 00082 WP 2001 11 30 ABXA010603 1 20011113 A 5230 59101419 PANEL DOUG DC9 DC933F 302207A WP FWD. CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 FORWARD LOWER CARGO DOOR FORWARD EDGE AT 2ND STOP FROM BOTTOM CRACKED AT STOP FITTING. REPAIRED AREA IAW DC-9 SRM 52-05 AND SHP TRAVELER # ST-0148-04. 2 L 7 2 4F A6WE 2001113000083 20011130 00083 WP 2001 11 30 ABXA010604 1 20011113 A 5200 995766437 FORMER DOUG DC9 DC933F 302207A WP FWD. CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 FORWARD LOWER CARGO DOOR FRAME CRACKED INSIDE FORWARD LOWER LIGHTENING HOLE. REPLACED ANGLE IAW DC-9 SRM. 2 L 7 2 4F A6WE 2001113000084 20011130 00084 WP 2001 11 30 ABXA010605 1 20011113 A 5300 992345948 ANGLE DOUG DC9 DC933F 302207A WP WHEEL WELL CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 SMALL ANGLE CRACKED BENEATH KEEL, LOCATED RIGHT OF ANTI-COLLISION LIGHT WIRE FEED THROUGH. INSTALLED NEW ANGLE IAW DC-9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 2001113000085 20011130 00085 WP 2001 11 30 ABXA010606 1 20011113 A 5300 99578551 TRACK DOUG DC9 DC933F 302207A WP CABIN CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 FIRST OFFICER'S FORWARD LEFT SEAT TRACK CORRODED AT FORWARD AND AFT MOUNT AREAS. REPLACED SEAT TRACK IAW DC-9 SRM 51-30- 1. 2 L 7 2 4F A6WE 2001113000086 20011130 00086 WP 2001 11 30 ABXA010608 1 20011113 A 5310 99220422 SUPPORT DOUG DC9 DC933F 302207A WP FWD CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 VERTICAL SUPPORT FITTING AT STATION 332, LONGERON 24 RIGHT CRACKED. REPAIRED AREA IAW DC-9 SSRM DWG K05159. 2 L 7 2 4F A6WE 2001113000087 20011130 00087 WP 2001 11 30 ABXA010609 1 20011113 A 5310 99220422 SUPPORT DOUG DC9 DC933F 302207A WP FWD CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 VERTICAL SUPPORT FITTING AT STATION 256, LONGERON 24 RIGHT WAS CRACKED. REPLACED FITTING IAW DC-9 SSRM DWG K05159. 2 L 7 2 4F A6WE 2001113000088 20011130 00088 WP 2001 11 30 ABXA010610 1 20011113 A 5310 99220422 SUPPORT DOUG DC9 DC933F 302207A WP FWD CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 VERTICAL SUPPORT FITTING AT STATION 237, LONGERON 24 RIGHT WAS CRACKED. REPLACED FITTING IAW DC-9 SSRM DWG K05159. 2 L 7 2 4F A6WE 2001113000089 20011130 00089 WP 2001 11 30 ABXA010611 1 20011113 A 5310 99220421 SUPPORT DOUG DC9 DC933F 302207A WP FWD CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 VERTICAL SUPPORT FITTING AT STATION 256, LONGERON 24 LEFT CRACKED. REPAIRED FITTING IAW DC-9 SSRM. 2 L 7 2 4F A6WE 2001113000090 20011130 00090 WP 2001 11 30 ABXA010612 1 20011113 A 5310 99220422 SUPPORT DOUG DC9 DC933F 302207A WP FWD CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 VERTICAL FLOOR SUPPORT FITTING CRACKED F.S. 541 AT LONGERON 24 RIGHT. REPAIRED FITTING IAW DC-9 SSRM DWG K05159, DC-9 SR M 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2001113000091 20011130 00091 WP 2001 11 30 ABXA010614 1 20011127 A 2611 775003 SMOKE DETECTOR DOUG DC9 DC941 302207N WP CABIN DEFECTIVE A ABXA O OTHER N FALSE WARNING DE DESCENT 1 GL 23 990AX 6033 47493 WHILE DESCENDING THROUGH APPROXIMATELY 18,000 FEET, THE #9 UPPER CARGO SMOKE DETECTOR BLINKED FOR APPROXIMATELY 3 MINUTE S. CREW COMPLETED EMERGENCY CHECKLIST. LIGHT WENT OUT AND STAYED OUT. NO SMOKE OBSERVED. REPLACED THE #9 UPPER SMOKE DET ECTOR UNIT. OPS CHECKED GOOD IAW DC-9 MM. 2 L 7 2 4F A6WE 2001113000092 20011130 00092 2001 11 30 CHQ00045 4 20011124 A 3160 DISPLAY EMB 145 EMB145 3260210 SO COCKPIT MALFUNCTIONED A CHQA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 11 266SK 145241 CAPTAINS MAIN DISPLAY WENT BLANK DURING CLIMB. 2 L 7 2 4F RT T00011AT 2001113000093 20011130 00093 SO 2001 11 30 CHQ00046 1 20011127 A 2611 SMOKE DETECTOR EMB 145 EMB145 3260210 SO LAVATORY ACTIVATED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 290SK 145474 LAV SMOKE DETECTOR WENT OFF WHEN DOING A/I TEST, THEN ON CLIMBOUT. 2 L 7 2 4F RT T00011AT 2001113000094 20011130 00094 NE 2001 11 30 CNMA200100035 2 20011120 A 7520 DUCT DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 3 ENGINE BLOWN A CNMA F J A ACTIVATE FIRE EXT. DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 540AX 46595 517726 ENGINE FIRE INDICATION ON TAKEOFF CLIMBOUT 2 APPROX 400 FT AGL ON NR 3 ENGINE. COMMENCE ENG FIRE SEVERE DAMAGE CHECKLIS T PERFORMED. FIRE INDICATION WENT OUT. DUMPED APPROX 29,000 LBS FUEL AND RETURNED TO LICZ. FOUND 14TH STAGE BLEED DUC T BLOWN. 2 L 7 3 4F 4 F A22WE E23EA 2001113000095 20011130 00095 WP 2001 11 30 MWEA011463 1 20011130 A 5310 59114282 SKIN DOUG DC9 DC915 3022036 WP STATION 818 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 EXTERIOR SKIN IS CRACKED AT STATION 818, LONGERON 19 RIGHT, BETWEEN EXISTING DOUBLER AND SKIN BUTT SPLICE -- REMOVED, STOP DRILLED AND INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001113000096 20011130 00096 WP 2001 11 30 CNMA200100036 1 20011123 A 2620 INDICATOR DOUG DC10 DC1030 3023501 WP COCKPIT MALFUNCTIONED A CNMA F J A ACTIVATE FIRE EXT. DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 540AX 4305 46595 ENGINE FIRE INDICATION ON T/O CLIMBOUT AT APPROX 400 FT AGL ON NR 3 ENGINE. ENGINE FIRE SEVER DAMAGE CHECKLIST PERFORME D. FIRE INDICATION WENT OUT. DUMPED APPROX 29,000 LBS FUEL AND RETURNED TO LICZ. ON ENGINE FIRE SEVER DAMAGE PROCEDUR ES, WHEN AGENT NR 1 SELECTED FOR DISCHARGE, LIGHT DID NOT INDICATE AGENT LOW. FIRE INDICATION WENT OUT, NO AGENT DISCHA RGED INDICATION ON ENGINE NR 3. UPPER DUCT FROM HIGH STAGE VALVE BLOWN. REMOVED AND REPLACED DUCT. NR 3 I/B REVERSER DAMAGED. REMOVED AND REPLACED REVERSER. NR 3 ENGINE LPT COOLING HARNESS DAMAGED. REMOVED AND REPLACED HARNESS. CARTR IDGE ON NR 3 ENGINE OUTBOARD FIRE BOTTLE BLOWN, BOTTLE DISC NOT RUPTURED. REMOVED AND REPLACED BOTTLE AND CARTRIDGE. 2 L 7 3 4F A22WE 2001113000099 20011130 00099 NM 2001 11 30 DHL2001708014 1 20011128 A 2612 FIRE LOOP BOEING 727 72725 1384006 NM NR 2 ENGINE OUT OF POSITION A DHLA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 708DH 18275 NR 2 ENGINE GROUND DET LIGHT ON DIM. OPENED COWLING, CLEARED FIRE LOOP FROM COWLING, CLOSED COWLING AND OP TEST NORMAL PER MM 26-00. 2 L 7 3 4F A3WE 2001113000101 20011130 00101 NM 2001 11 30 DHL2001740007 1 20011129 A 2612 FIRE DETECTOR BOEING 727 7272Q9 138448M NM APU FAILED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 740DH 21930 APU WILL NOT FIRE TEST. FOUND BAD APU FIRE DETECTOR UNIT. REPLACED UNIT PER MM 26-15-00 AND OPS NORMAL. 2 L 7 3 4F RT A3WE 2001113000102 20011130 00102 NM 2001 11 30 DHL2001743015 1 20011123 A 2612 FIRE LOOP BOEING 727 727225 1384077 NM NR 1 ENGINE OUT OF POSITION A DHLA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 743DH 22438 NR 1 ENG FIRE DETECTOR GROUND FAULT LIGHT ILLUMINATED. CLEANED AND REPOSITIONED NR 1 ENG SENSING ELEMENT. OPS CHECK, N O LIGHT. OP'S OK IAW MM 26-11-022. 2 L 7 3 4F A3WE 2001113000103 20011130 00103 NM 2001 11 30 DHL2001743016 1 20011128 A 2612 CLAMP BOEING 727 727225 1384077 NM NR 1 ENGINE LOOSE A DHLA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 743DH 22438 NR 1 ENG FIRE FAULT DETECTION LIGHT ILLUMINATED ON GROUND. NR 1 ENG GROUND FAULT LIGHT ILLUMINATED ON GROUND. FOUND 1 CLAMP UNDONE. RESECURED CLAMP, CKS GOOD PER 26-10-0. 2 L 7 3 4F A3WE 2001113000104 20011130 00104 WP 2001 11 30 DHL2001801015 1 20011129 A 7910 OIL CAP DOUG DC8 DC873F 302199F WP NR 1 ENGINE LOOSE A DHLA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 801DH 30928 2190 46033 LOSS OF OIL QUANTITY NR 1 ENGINE. GAUGE INDICATED LESS THAN 1 QUART, OIL PRESS 17 PSI, OIL TEMP 75 DEGREES C. PERFORME D OIL QUANTITY LOW ABNORMAL PROCEDURE AND INFLIGHT ENGINE SHUTDOWN. FOUND ON ARRIVAL NR 1 ENG OIL CAP WAS NOT SECURED. SERVICED NR 1 ENG OIL PER M/M 12-20-1. NO LEAKS NOTED PER JRH 13.2 2 L 7 4 4F RT 4A25 2001113000105 20011130 00105 WP 2001 11 30 DHL2001803019 1 20011124 A 3260 PROXIMITY SWITCH DOUG DC8 DC873 302199C WP GEAR DOOR CONTAMINATED A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 803DH 46123 UPON UPLATCH CHECK DOOR NOT LATCHED LIGHT ILLUMINATED. CLEANED LANDING GEAR DOOR PROX SWITCHES AND TARGETS DUE FOUND TO O MUCH GREASE. PERFORMED GEAR DOOR SELF TEST IAW MM 32-60-0, FOUND OK. 2 L 7 4 4F RT 4A25 2001113000106 20011130 00106 NM 2001 11 30 F3LA200100117 1 20011126 A 2120 SMOKE AIRBUS A319 A319111 3930336 NM CABIN DETECTED A F3LA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 03 904FR 1579 FLIGHT CREW REPORTED SMOKE IN CABIN AFTER LANDING. COULD NOT DETERMINE ORIGIN. SMOKE DISSIPATED AFTER 10 MIN. MAINTEN ANCE PERFORMED TASK 71-00-00-810-802 FOR SMOKE IN CABIN. FOUND NO EVIDENCE OF OIL CONTAMINATION. FOUND EVIDENCE OF WAT ER INGESTION AT NR 1 ENGINE RAM AIR INLET. PERFORMED ENGINE RUN, WITH NO SMOKE OR ODOR. 2 L 7 2 4F RT A28NM 2001113000107 20011130 00107 NM 2001 11 30 F3LA200100118 1 20011116 A 7830 DOOR BOEING 737 7372L9 1384497 NM THRUST REVERSER CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 3902 22733 DURING C-1 CHECK, INSPECTION REPORTED CRACK IN OUTER SKIN OF NR 2 ENGINE TOP OUTBOARD THRUST REVERSER FAIRING DOOR. INS TALLED SCAB PATCH PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001113000108 20011130 00108 NM 2001 11 30 F3LA200100121 1 20011117 A 5532 SKIN BOEING 737 7372L9 1384497 NM VERTICAL STAB DENTED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 3902 22733 DURING C-1 CHECK, INSPECTION REPORTED SEVERAL DENTS IN SKIN OF DORSAL FIN FWD OF VERTICAL STABILIZER. FABRICATED AND IN STALLED EXTERNAL REPAIR PER SRM 55-30-6 AND 51-20-1. 2 L 7 2 4F RT A16WE 2001113000109 20011130 00109 NM 2001 11 30 F3LA200100123 1 20011125 A 3397 WIRE BOEING 737 73736N 1384408 NM CABIN BROKEN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 306FL 28563 PRIOR TO DEPARTURE, FLIGHT CREW REPORTED EMERGENCY EXIT FLOOR PATH WIRING EXPOSED AT ROW 15. SPLICED BROKEN WIRE PER ST ANDARD PRACTICES 20-30-12, PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHT SYSTEM AND CHECKED OKAY. 2 L 7 2 4F RT A16WE 2001113000110 20011130 00110 EU 2001 11 30 MALA010773 1 20011022 A 5260 C14647 HAND RAIL BAC 146 AVRO146RJ85A 1500097 EU AIRSTAIRS CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 509XJ E2321 DURING C-CHECK IN CVG, MAINTENANCE FOUND CORROSION BEYOND LIMITS ON O/B AIRSTAIR RAIL. MAINTENANCE REMOVED AND REPLACED IB/OB AIRSTAIR RAILS (P/N C14647/ C14648) IAW SRM 53-00-32 & 51-43-00. 2 H 7 4 4F RT A49EU 2001113000111 20011130 00111 EU 2001 11 30 MALA010774 1 20011022 A 5320 PLATE BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 509XJ E2321 DURING C-CHECK IN CVG, FOUND CORROSION BEYOND LIMITS ON PLATE BETWEEN AIRSTAIR BEYOND LIMITS ON PLATE BETWEEN AIRSTAIR R AILS. MAINTENANCE REPLACED CORRODED HARDWARE IN FRAME 20, SAC PLATE IAW BAE SRM 51-43-00 AND INSTALLED PROTECTIVE COATIN G TO FRAME 20 PLATE IAW BAE AMM 20-10-11. 2 H 7 4 4F RT A49EU 2001113000112 20011130 00112 EU 2001 11 30 MALA010775 1 20011022 A 5320 SILL BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 509XJ E2321 DURING C-CHECK IN CVG, WHILE REPAIRING SEAT TRACK FOUND CORROSION ON SILL PLATE BELOW THRESHOLD PLATE FOR LEFT PAX DOOR. MAINTENANCE REMOVED AND REPLACED PAX DOOR SILL PLATE FWD AND INSPECTED ATTACHED FITTINGS IAW BAE SRM 51-42-00, 51-43-0 0 AND AMM 20-10-11, 20-10-12. 2 H 7 4 4F RT A49EU 2001113000113 20011130 00113 EU 2001 11 30 MALA010776 1 20011022 A 5347 HC532H90B204 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 509XJ E2321 DURING C-CHECK IN CVG, NR 1 SEAT RAIL HAD CORROSION BEYOND LIMITS, BETWEEN FRAME 19 AND 20 P/N HC532H90B-204. AT NEXT C -CHECK HAVE A SPLICE REPAIR IAW SRM 53-00-32-201. MAINTENANCE REPLACED FORWARD SECTION OF NR 1 SEAT RAIL IAW EO A53026. 2 H 7 4 4F RT A49EU 2001113000114 20011130 00114 EU 2001 11 30 MALA010777 1 20011022 A 5330 SKIN BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 509XJ E2321 DURING C-CHECK IN CVG, EO A53064 DENT IN LT FWD FUSELAGE AT FRAME 19. MAINTENANCE REPAIRED PER NOTED EO A53064. 2 H 7 4 4F RT A49EU 2001113000115 20011130 00115 2001 11 30 MALA010778 4 20011119 A 3425 6226190113 COMPUTER SAAB SF340 SF340A 7850100 EU E/E BAY FAULTY A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 109XJ 340A109 DURING FLIGHT 3023, F/O'S SIDE AVIONICS, INFLIGHT EHSI NORMAL EXCEPT RED HEADING FLAG, EADI PITCH MISSING, COLOR GONE, A HRS FAILURE, ALSO AUTO PILOT/YD FAILED. LANDS HARD AND FLYS CROOKED. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLA CED NR 2 AHRS COMPUTER (P/N 622-6190-113). SN/ON 2681, SN/OFF 2917. NR 2 AHRS OPS CHECKS GOOD IAW SF340 MM CHAP 22. 2 L 7 2 4T RT A52EU 2001113000116 20011130 00116 EU 2001 11 30 MALA010779 1 20011123 A 3040 2312M782 CONVERTER SAAB SF340 SF340A 7850100 EU WINSHIELD FAILED A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 99XJ 340A099 DURING FLIGHT 3345, F/O'S WINDSHIELD WIPER FROZE STRAIGHT UP AFTER TAKEOFF. CREW HEARD GRINDING NOISE. AIR TURNBACK TO MSP. MAINTENANCE REMOVED AND REPLACED FL'S WIPER CONVERTER (P/N 2312M78-2) SN/OFF 00636, SN/ON 00819. OPS CHECKS GOOD . DONE IAW SAAB AMM 30-45-10-4. 2 L 7 2 4T RT A52EU 2001113000117 20011130 00117 NE 2001 11 30 MALA010780 2 20011120 A 7200 200304015 ENGINE BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 2 FAILED A MALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 513XJ E2329 DURING FLIGHT 3445, NR 2 ENGINE FAILED AFTER TAKEOFF. ENGINE SHUTDOWN, AIR TURNBACK TO MSP. MAINTENANCE REMOVED AND RE PLACED NR 2 ENGINE. OPS AND LEAK CHECKS GOOD P/N ON & OFF 2-003-040-15, S/N OFF P07700, S/N ON LF07588. 2 H 7 4 4F 4 F RT A49EU E6NE 2001113000118 20011130 00118 WP 2001 11 30 MWEA011460 1 20011122 A 5320 991224617 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 RIGHT HAND WEB IN AFT ACCESSORY COMPARTMENT HAS A CRACK EXTENDING FROM LIGHTENING HOLE JUST OF STRINGER 11 AT STATION 10 38. INSTALLED DOUBLER IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL 53-01 FIGURE 2, SHEET 3. 2 L 7 2 4F A6WE 2001113000119 20011130 00119 WP 2001 11 30 MWEA011462 1 20011128 A 5280 DOOR DOUG DC9 DC914 3022034 WP NLG UNSECURE A MWEA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 31 600ME 45725 NOSE GEAR VIBRATION AFTER GEAR SELECTED UP. RESECURED RIGHT HAND NOSE LANDING GEAR DOOR. 2 L 7 2 4F A6WE 2001113000120 20011130 00120 NE 2001 11 30 NACA20010039 2 20011124 A 8530 356993 CYLINDER DOUG DC6 DC6A 3021706 WP PWA R2800 R2800* 52026 NE NR 2 ENGINE CRACKED A NACA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 AL 03 99330 454 454 43576 P37244 SHUTDOWN NR 2 ENGINE AT 0315Z DUE TO LOW OIL QUANTITY. NR 4 CYLINDER CRACKED. REPLACED THE NR 4 CYLINDER. 2 L 7 4 4R 4 R 6A3 5E8 2001113000121 20011130 00121 NM 2001 11 30 P2EA2001M0011 1 20011123 A 2520 PSU BOEING 737 7372Q8 138448K NM CABIN UNSECURE A P2EA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 05 121NJ 21735 PSU PANEL ABOVE ROW 15 RIGHT FELL DOWN DURING TAXI-OUT. AIRCRAFT RETURNED TO BLOCKS WITH NO INCIDENT. PSU PANEL RESECU RED IAW MM 25-23-11. 2 L 7 2 4F RT A16WE 2001113000122 20011130 00122 NM 2001 11 30 P5CA0100615 1 20011125 A 2424 746011L GCU BOEING 747 747* NM NR 1 ENGINE FAILED A P5CA J A DUMP FUEL UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CL CLIMB 1 WP 23 451PA 30809 FIVE SECONDS AFTER LIFT OFF, EICAS MESSAGE APPEARED: ELEC AC BUS - NR 1 AC BUS BECAME ISOLATED AND UNPOWERED. WOULD NO T RESET PER NNL ELEC AC BUS CHECKLIST. FOUND NR 1 GCU DIFFERENTIAL LOCK OUT. REPLACED NR 1 GCU WITH KLM LOAN PART. CA RRIED OUT CMC GROUND TEST & OPS CHECK ON ENG RUN. ALL SATISFACTORY. 2 L 7 4 4F RT A20WE 2001113000123 20011130 00123 2001 11 30 PCAA0111163 4 20011126 A 2360 STATIC WICK DHAV DHC8 DHC8102 2809003 NM ELEVATOR MISSING A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 826EX 389 DURING A REPLACEMENT OF A STATIC WICK FOR BEING MISSING, IT WAS DISCOVERED THAT THE LEFT ELEVATOR HORN OUTBOARD RIB AND UPPER AND LOWER TRANSITION STRAPS HAVE LIGHTNING DAMAGE AT THE TRAILING EDGE, AS WELL AS THE TRAILING EDGE FAIRING FOR T HE ELEVATOR HORN. OUTBOARD RIB AND FAIRING REPLACED. STRAPS WERE REPLACED WITH THOSE FABRICATED IN ACCORDANCE WITH DEH AVILLAND STRUCTURAL REPAIR MANUAL. ELEVATOR ASSEMBLY BALANCED CHECKED PER STRUCTURAL REPAIR MANUAL 55-20-61. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001113000124 20011130 00124 EU 2001 11 30 QXEA0101936 1 20011114 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AFT CARGO BAY FRAME 15205 CASTELLATION TIE-IN TO BELLY SKIN BETWEEN STRINGER 1 AND 74 HAS CORROSION ON TOP SURFACE WITH POSSIBLE CRACKS ON VERTICAL WEB. REPAIRED IAW FOKKER SRM 51-10-01, PAGE 6 AND SRM 51-10-04, PARAGRAPH 4B, C, PAGE 9. 2 L 7 2 4F RT A20EU 2001113000125 20011130 00125 EU 2001 11 30 QXEA0101937 1 20011112 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - DENT IN FORWARD CARGO DOOR APERTURE, FRAME 5805, WL 50.0. REPAIRED IAW FOKKER SRM 53-02-16, PAGE 3, FIGURE 1. 2 L 7 2 4F RT A20EU 2001113000126 20011130 00126 EU 2001 11 30 QXEA0101938 1 20011115 A 5753 VANE FOKKER F28 F28MK4000 4990810 EU T/E FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT WING INBOARD, TRAILING EDGE FLAP, VANE, LEADING EDGE IS CHAFED AT OUTBOARD END. REPAIRED IAW FOKKER SRM 51-10- 4, SRM 57-01-01, PAGE 3 AND FOKKER MM 51-30-00. 2 L 7 2 4F RT A20EU 2001113000127 20011130 00127 WP 2001 11 30 ZW0A0111501 1 20011128 A 2120 5910090653 DUCT DOUG DC9 DC983 3022083 WP LH PACK A ZW0A A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 13 948TW 49575 AFTER TAKEOFF SMOKE APPEARED IN THE COCKPIT. CREW SHUT OFF THE LH PACK AND RETURNED TO STL. FOUND Y DUCT WITH HOLE WORN IN IT. WELDED THE DUCT. CHECK-C 3-1-01 JFK. --CLOSED-- 2 L 7 2 4F RT A6WE 2001113000128 20011130 00128 EU 2001 11 30 QXEA0101940 1 20011115 A 5230 DOUBLER FOKKER F28 F28MK4000 4990810 EU CARGO DOOR TORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - BOTTOM TRAILING CORNER OF REPAIR DOUBLER TORN, CENTER CARGO DOOR INNER SKIN, 10 INCHES FORWARD OF TRAILING EDGE OF CENTER CARGO DOOR, ALONG BOTTOM OF DOOR. REPAIRED IAW HORIZON AIR EA 4-52-462 AND FOKKER MM 51-30-00 AND FOKKER SRM 51 -31-01. 2 L 7 2 4F RT A20EU 2001113000129 20011130 00129 NM 2001 11 30 DL72E011725 1 20011026 A 3350 S106 BATTERY BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 831WA 21483 R-2 EMERGENCY EXIT LIGHT INOP FOUND ON L/O. REPLACED BATTERIES 2 L 7 3 4F A3WE 2001113000130 20011130 00130 NM 2001 11 30 DL72E011730 1 20011026 A 5310 6516350314 BEAM BOEING 727 727247 138408F NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 BULKHEAD FS 1183 VERTICAL BEAM RBL 8 WL 182 CRACKED. THE RBL 8 VERTICAL BEAM ON THE FS 1183 BULKHEAD WAS FOUND WITH A 1 INCH CRACK AT THE LOWER END AT WL 182. THE CRACK IS TYPICAL OF BAC SB 727-53-0175. THE CRACK WAS REPAIRED PER THE SB AN D PER ER/A 382022-14. 2 L 7 3 4F A3WE 2001113000131 20011130 00131 NM 2001 11 30 DL72E011771 1 20011107 A 5754 ATTACH ANGLE BOEING 727 727247 138408F NM L/E SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2829W 21481 FOUND ON F1 CK NR 8 SLAT INBD STOP ATTACH ANGLE CRACKED. REPAIRED PER MM 57-54-000-8. 2 L 7 3 4F A3WE 2001120300001 20011203 00001 EU 2001 12 3 01FDEA01017 1 20011130 A 5610 WINDSHIELD AIRBUS 310 A310203 3930313 EU CRACKED A FDEA A UNSCHED LANDING O Z OTHER SIGNIFICANT FAILURE REPORT CL CLIMB 1 SO 25 442FE 353 1-381 CAPT'S WINDSHIELD CRACKED OUTER LAYER. REPLACD WINDSHIELD, CONTROLLER & REGULATOR. 2 L 7 2 4F RT A35EU 2001120300002 20011203 00002 EU 2001 12 3 MALA010786 1 20011124 A 2750 676801007 ECU BAC 146 AVRO146RJ85A 1500097 EU A MALA O OTHER J WARNING INDICATION LD LANDING 1 GL 15 512XJ E2326 During Flight #3489 AC did a zero Flap landing in BTR. Crew had a Flap Inop and Flap Fault Indication. Flap Inop/Flap F ault in Flight all 4 brakes exceeded 750 degress Celsius, tried a Flap Fault reset on the ground per Mxc request, Flap F ault illuminated again with no flap movement. Maintenance inspected AC and found safe for one time Ferry Flight from BTR to MEM, after manually setting Flaps to 18 degress. AMM 27-50-00. Maintenance transferred to 409 Card # 049813 detail s reset trapped Torque Limiter cycled Flaps from 0 to 30 degrees checks good complied with High Energy Brake 1, Flapless Landing Inspections, no defects noted. A/C ok for continued service. Maintenance reset tripped Torque Limiter IAW AMM 2 H 7 4 4F RT A49EU 2001120300003 20011203 00003 NM 2001 12 3 SWAA013213 1 20011128 A 5310 6546546 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 387SW 26602 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 747, STR 26R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001120300004 20011203 00004 NM 2001 12 3 SWAA013215 1 20011128 A 5310 963089 WEB BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 502SW 24179 DURING SCHEDULED SPECIAL VISIT, FOUND HORIZONTAL WEBS CRACKED (2 EA) AT BS 179, WL 207, LBL 27.0 AND RBL 27.0. REMOVED AND REPLACED WEBS PER SRM. 2 L 7 2 4F RT A16WE 2001120300005 20011203 00005 NM 2001 12 3 SWAA013216 1 20011128 A 5310 6517582 WEB BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 502SW 24179 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, WL 226 AND RBL 17.1. REMOVED AND REPLACED WE B PER SRM. 2 L 7 2 4F RT A16WE 2001120300006 20011203 00006 NM 2001 12 3 SWAA013217 1 20011128 A 5314 6545808 BULKHEAD BOEING 737 7373H4 1384600 NM NLG W/W PUNCTURED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 632SW 27707 DURING SCHEDULED RON, FOUND A .9 BY 1.6 HOLE PUNCTURED AT NLG W/W AFT BULKHEAD. MX FERRY TO DAL AND REPAIRED BULKHEAD P ER SWA RA. 2 L 7 2 4F RT A16WE 2001120300007 20011203 00007 NM 2001 12 3 SWAA013218 1 20011129 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED ( 3 EA ) AT STRINGER 16R, BS 445,BS 465 AND BS 535. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001120300008 20011203 00008 NM 2001 12 3 SWAA013219 1 20011129 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 752, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001120300009 20011203 00009 NM 2001 12 3 SWAA013220 1 20011129 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001121900041 20011219 00041 2001 12 19 C8GA20010018 4 20011128 A 3442 MI5851622 INDICATOR BOEING 727 7272A1 138407F NM COCKPIT OVERHEATED A C8GA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 15 287SC 1209 21345 FLT 739 FROM DEN TO MCI. UPON APPROACHING THE PARKING RAMP AREA AFTER LANDING IN MCI, SMOKE WAS OBSERVED RISING FROM CE NTER PEDESTAL OF THROTTLE QUADRANT. FLIGHT ENGINEER DEPOWERED AIRCRAFT COMPLETELY AND MAINTENANCE PERSONNEL ARRIVED TO TROUBLESHOOT THE AIRCRAFT. AFTER FURTHER INSPECTION FOUND THAT THE WEATHER RADAR SYSTEM WAS AT FAULT. DEFERRED THE WEA THER RADAR SYSTEM PER MEL 34-21 AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2001120300010 20011203 00010 2001 12 3 SWAA013186 4 20011125 A 2565 6551463 CLIP BOEING 737 7373H4 1384600 NM L1/R1 DOORS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 373SW 26581 DURING SCHEDULED C1 CHECK, FOUND BOTH FWD DOOR EVACUATION SLIDE GIRT BARS CLIP HOOKS LOOSE. SECURED BOTH CLIP HOOKS PER MM. 2 L 7 2 4F RT A16WE 2001120300011 20011203 00011 NM 2001 12 3 SWAA013188 1 20011126 A 5320 65C27314 CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED D CHECK, FOUND 13 EA STRINGER CLIPS CRACKED, STR 10R, BS 663 AND BS 787, STR 2R, BS 639 AND BS 787, STR 3L, BS 727D AND BS 747, STR 2L, BS 639, STR 3R, BS 767, STR'S 4L AND 4R, BS 639, STR 6R,BS 500C, STR'S 1 AND 5L, BS 520 . REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001120300012 20011203 00012 NM 2001 12 3 SWAA013189 1 20011126 A 5753 65C30462 FLAP BOEING 737 7373Q8 1384670 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED D CHECK, FOUND LT OUTBD T/E FOREFLAP DELAMINATED ON BOTH SURFACES NEAR INBD END. REPAIRED FLAP PER SR M. 2 L 7 2 4F RT A16WE 2001120300013 20011203 00013 NM 2001 12 3 SWAA013190 1 20011124 A 5311 6546546 SHEAR TIE BOEING 737 737317 138447P NM AFT CARGO COMPT CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED D CHECK, FOUND 2 EA AFT CARGO COMPT SHEAR TIES CORRODED, BS 747, RBL 1-7, AND BS 767, LBL 7-10. REPAIR ED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 2001120300014 20011203 00014 NM 2001 12 3 SWAA013191 1 20011126 A 5511 6547501 SPAR BOEING 737 737317 138447P NM LT HORZ STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED D CHECK, FOUND RT HORIZONTAL STAB UPPER REAR SPAR CHORD CORRODED BETWEEN STA 279 AND STA 305. REPAIRED SPAR PERSRM. 2 L 7 2 4F RT A16WE 2001120300015 20011203 00015 NM 2001 12 3 SWAA013192 1 20011126 A 5314 6545866 BEAM BOEING 737 737317 138447P NM LOWER FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED D CHECK, FOUND KEEL BEAM CORRODED, BS 500D PLUS 6, LT SIDE, OUTBD FLANGE. REPAIRED KEEL BEAM PER SRM. 2 L 7 2 4F RT A16WE 2001120300016 20011203 00016 NM 2001 12 3 SWAA013193 1 20011124 A 5311 6546527 SHEAR TIE BOEING 737 7375H4 138449D NM FWD CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 525SW 26567 DURING SCHEDULED D CHECK, FOUND 2 EA SHEAR TIES CRACKED, BS 344 AND BS 360, BETWEEN STRINGERS 14R-15R. REPAIRED SHEAR T IES PER SRM. 2 L 7 2 4F RT A16WE 2001120300017 20011203 00017 NM 2001 12 3 SWAA013194 1 20011125 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN FLOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 768SW 30587 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER BROKENAT ROW 1. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2001120300018 20011203 00018 NM 2001 12 3 DL72E011772 1 20011023 A 5754 274702781 ATTACH ANGLE BOEING 727 727247 138408F NM L/E SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 1/4 INCH CRACK IN NR 1 SLAT COVE SKIN LWR ATTACH ANGLE BELOW TAI DUCT. REPAIRED PER 727 M/M 57-54-000-8 FIG 805A 2 L 7 3 4F A3WE 2001121200041 20011212 00041 NM 2001 12 12 01FDEA01009 1 20011121 A 5311 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 285FE 22622 DENT IN FRAME UPPER FLANGE AT BS 1090, STR 25L. REMOVED AND REPLACED FLANGE PER SRM 51-40-3 FIG 1 & EA 7-5310-62617. 2 L 7 3 4F RT A3WE 2001121200043 20011212 00043 NM 2001 12 12 01FDEA01011 1 20011125 A 5330 SKIN BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 285FE 22622 CORROSION ON SKIN FWD CARGO BAY BS 700-720, STR 28R. REMOVED AND REPLACED SKIN PER SRM 53-30-3 FIG 3 & EA 7-5310-62617. 2 L 7 3 4F RT A3WE 2001120300019 20011203 00019 NM 2001 12 3 DL72E011779 1 20011108 A 5312 BULKHEAD BOEING 727 727247 138408F NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2829W 21481 FUSELAGE BULKHEAD STA 1183 RBL 8, A 3/8 INCH CRACK WAS FOUND IN THE FS 1183 BULKHEAD WEB UNDER THE LOWER END OF THE RBL VERTICAL STIFFENER NEAR WL 182. THE CRACK IS TYPICAL OF BAC S/B 727-53-0175. THE CRACK WAS REMOVED AND REPAIR INSTALLED PER ER/A 382099-14. 2 L 7 3 4F A3WE 2001120300020 20011203 00020 NM 2001 12 3 DL72E011780 1 20011107 A 5311 FRAME BOEING 727 727247 138408F NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 FUSELAGE FRAME STA 760, AN UNIDENTIFIED REPAIR WAS REMOVED FROM THE FS 760 LT OVERWING EXIT FRAME. THE FRAME WAS FOUND WITH A TYPICAL CRACK PER BAC S/B 727-53-0197. A NEW FRAME REPAIR WAS INSTALLED PER THE REQUIREMENTS OF THE S/B AND PER ER/A 382044-14AD, REV A. 2 L 7 3 4F A3WE 2001120300021 20011203 00021 2001 12 3 DL72E011852 4 20011124 A 2210 2588880901 COUPLER BOEING 727 727247 138408F NM YAW DAMPER FAILED A DALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 27 283WA 21485 AFTER TAKEOFF A/C BEGAN TO FISHTAIL. NO YAW DAMPER FLAGS IN VIEW. NO MOVEMENT OF INDICES ON YD INSTRUMENT. RETURN TO AIR PORT FOR LANDING. FOUND LOWER YAW DAMPER FLAG IN VIEW. WILL NOT RETRACT. REPLD YAW DAMP COUPLER. ALSO FOUND LOWER RUDDER POSITION SENSOR SHORTED. REPLACED SAME. YAW DAMP OPEN NORMAL. 2 L 7 3 4F A3WE 2001120300022 20011203 00022 NM 2001 12 3 DL72E011860 1 20011125 A 3350 900542 CHARGER BOEING 727 727247 138408F NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 282WA 21484 FOUND ON S/C THAT FWD OVERWING LIGHTS WERE INOP.REPLACED BATTERY PACK AND CHARGER. 2 L 7 3 4F A3WE 2001120300023 20011203 00023 NM 2001 12 3 DL72E011877 1 20011128 A 3350 S106 BATTERY BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 831WA 21483 OVERHEAD EMERGENCY LIGHT AT 29 ABC INOP - REPLACED BATTERY 2 L 7 3 4F A3WE 2001120300024 20011203 00024 NM 2001 12 3 DL72E011878 1 20011128 A 3350 900835A BATTERY BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 830WA 21482 OVERWING EMERGENCY LIGHT SIGNS BLINKING. REPLACED BATTERY PACK 2 L 7 3 4F A3WE 2001120300025 20011203 00025 NE 2001 12 3 DL72L011689 2 20011020 A 7200 ENGINE BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 1 POWER LOSS A DALA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 506DA 21308 687469 ON TAKEOFF ROLL, N1 ROLLED BACK TO 80 PERCENT, EPR FOLLOWED. THROTTLE PUSHED BACK UP, ROLLED BACK AGAIN. INSPECTED FCU B URNER PRESSURE LINE, OK. SERVICED BELLOWS AND RAN PER PFHB, NO TROUBLE FOUND. 2 L 7 3 4F 4 F A3WE E2EA 2001120300026 20011203 00026 NE 2001 12 3 DL72L011814 2 20011115 A 7200 JT8D15AHK ENGINE BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 2 SHUTDOWN A DALA O OTHER Y ENGINE STOPPAGE CR CRUISE 1 SO 27 509DA 68318 21311 695271 NO 2 ENG SHUTDOWN INADVERTENTLY IN FLT AT FL270. RESTARTED ENGINE WITH ALL PARAMETERS NORMAL. OPERATED NORMALLY FOR DURA TION OF FLIGHT. PERFORMED WINDMILL INSPECTION AND CHECKED CHIP DETECTORS AND OIL FILTER. ALL NORMAL, OK FOR SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2001120300027 20011203 00027 2001 12 3 DL72L011845 4 20011123 A 2210 COUPLER BOEING 727 727232 1384082 NM YAW DAMPER INTERMITTENT A DALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 27 504DA 21306 ON TAKEOFF SLIGHT RUDDER OSCILLATIONS WITH HIGH WIND. AFTER TAKEOFF EXCESSIVE RUDDER MOVEMENT. FOLLOWED YAW DAMP INOP POM PROC. NO HELP. REMOVED AND REPLACED UPPER AND LOWER YAW DAMP COUPLERS PER M/M. SYSTEM TEST NORMAL. 2 L 7 3 4F A3WE 2001120300028 20011203 00028 NM 2001 12 3 SWAA013197 1 20011127 A 5310 6516300 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED 1/4D CHECK, FOUND WEB CRACKED .125 INCH LONG AT BS 178, WL 234 AND LBL 14. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001120300029 20011203 00029 NM 2001 12 3 SWAA013198 1 20011126 A 5310 6545866 STIFFENER BOEING 737 7373H4 1384600 NM LT MLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED 1/4D CHECK,(SI11051-53) FOUND VERTICAL STIFFENER CRACKED AT BS 663, LBL 6.15. REMOVED AND REPLACED VER TICAL STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 2001120300030 20011203 00030 NM 2001 12 3 SWAA013199 1 20011127 A 5310 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 387SW 26602 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL WEBSCRACKED (2 EA) AT BS 180, WL 231, LBL 17.1 AND RBL 17.1. REMOVED AND R EPLACED WEBS PER SRM. 2 L 7 2 4F RT A16WE 2001120300031 20011203 00031 NM 2001 12 3 SWAA013200 1 20011127 A 5310 6516300 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 399WN 27693 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, WL 201, LBL 5 AND RBL 5. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001120300032 20011203 00032 2001 12 3 DL72L011847 4 20011123 A 2210 GM1032 TRANSMITTER BOEING 727 727232 1384082 NM YAW DAMPER FAILED A DALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 27 504DA 21306 AFTER T/O RUDDER OSCILLATIONS FOLLOWED POM PROCEDURE. FOUND POSITION TRANSMITTER COIL OPEN REMOVED AND REPLACED POS XMTR PER MM ADJ/TEST OF YAW DAMP CHKS GOOD PER MM. 2 L 7 3 4F A3WE 2001120300033 20011203 00033 NM 2001 12 3 01FDEA001003 1 20011118 A 3297 CONNECTOR BOEING 727 727233 138408A NM LANDING GEAR LOOSE A FDEA O OTHER N FALSE WARNING DE DESCENT 1 SO 25 277FE 22042 DURING DESCENT NR 1 ENG STRUT LIGHT ILLUM. REMOVED AND REPLACED GEAR PINS AND SECURED LOOSE CONNECTOR. OK FOR SERVICE. 2 L 7 3 4F RT A3WE 2001120300034 20011203 00034 SO 2001 12 3 CHQ00041 1 20011121 A 7331 INDICATOR EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL COCKPIT FAILED A CHQA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 261SK 145144 LOSS OF FUEL QUANTITY INDICATION. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001120300035 20011203 00035 NM 2001 12 3 SWAA013203 1 20011128 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 730SW 27862 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS CRACKED AT ROWS 1, 2 ,3, 5, 6, 16, AND 17. REMOVED AND REPLACED COVERS PE R MM. 2 L 7 2 4F RT A16WE 2001120300036 20011203 00036 NM 2001 12 3 SWAA013204 1 20011127 A 5310 6547978 WEB BOEING 737 7373Q8 1384670 NM CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED D CHECK, FOUND LT CREASE BEAM WEB CORRODED AT BS 616 TO BS 639. REPAIRED WEB SECTION PER SRM. 2 L 7 2 4F RT A16WE 2001120300037 20011203 00037 NM 2001 12 3 SWAA013208 1 20011124 A 5230 6545871 FRAME BOEING 737 7373H4 1384600 NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO DOOR, AFT FRAME CRACKED ABOVE LWR DOOR STOP FITTIING. REMOVED AND REPLACED AFT CARGO DOOR FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001120300038 20011203 00038 EU 2001 12 3 QXEA0101939 1 20011115 A 5330 STRAP FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - THREE RIVETS PULLED THROUGH STRAP ON BELLY SKIN JUST AFT OF RT MAIN LANDING GEAR DOOR. REPAIRED IAW FOKKER SRM 51 -31-05. 2 L 7 2 4F RT A20EU 2001120300039 20011203 00039 EU 2001 12 3 QXEA0101941 1 20011114 A 5230 STRUCTURE FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - DENT IN CENTER CARGO DOOR, FORWARD, LOWER CORNER, 2.5 INCHES LONG, 1.2 INCHES WIDE, APPROXIMATELY .150 INCH DEEP. REPAIRED IAW FOKKER SRM 51-10-4 AMD SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001120300040 20011203 00040 2001 12 3 SWAA013182 4 20011126 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 063SW 22061 AFT SERVICE DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001120300041 20011203 00041 NM 2001 12 3 SWAA013183 1 20011122 A 3260 6558206 SENSOR BOEING 737 7373H4 1384600 NM MLG INTERMITTENT A SWAA K NONE N FALSE WARNING CL CLIMB 1 SW 07 322SW 23343 AFTER TAKEOFF, GEAR RETRACTION, FWD PANEL GEAR WARNING LIGHTS ILLUMINATED. RESET GEAR WARNING LIGHTS C/B, RECYCLED LAND ING GEAR HANDLE, AND LIGHTS EXTINGUISHED. REMAINING OF THE FLIGHT WAS NORMAL. OPERATED LANDING GEAR SYS. NO DEFECTS N OTED. OPS CK GOOD PER MM. 2 L 7 2 4F RT A16WE 2001120300042 20011203 00042 2001 12 3 SWAA013184 4 20011126 A 2565 1061323 SLIDE BOEING 737 7372T4 1384492 NM R1 DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE PRESS IND LOW. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2001120300043 20011203 00043 NM 2001 12 3 SWAA013185 1 20011125 A 5320 6517583 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 364SW 26575 DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA VERTICAL BEAM WEBS CRACKED, BS 178-184, LBL 17.1 AND RBL 17.1. REMOVED AND R EPLACED BOTH VERTICAL WEBS PER SRM. 2 L 7 2 4F RT A16WE 2001120300044 20011203 00044 NM 2001 12 3 SWAA013187 1 20011126 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 655WN 28400 DURING SCHEDULED A1 CHECK, FOUND BULL NOSE EMERGENCY LIGHT INOP AT ROW 14 ABC. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2001120300045 20011203 00045 NM 2001 12 3 SWAA013210 1 20011128 A 2560 P2070001 BATTERY BOEING 737 7377H4 1384404 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 796SW 27889 DURING SCHEDULED RON, FOUND EMERGENCY FLASHLIGHT INOP AT AFT CABIN LT SIDE. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2001120300046 20011203 00046 2001 12 3 SWAA013211 4 20011129 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 626SW 27702 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001120300047 20011203 00047 2001 12 3 SWAA013212 4 20011129 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 073SW 22673 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2001120300048 20011203 00048 NM 2001 12 3 SWAA013214 1 20011129 A 5312 6516300 BULKHEAD BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 502SW 24179 DURING SCHEDULED SPECIAL VISIT, FOUND WEB CRACKED AT BS 178, WL 234 AND LBL 10. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001120300049 20011203 00049 2001 12 3 SWAA013195 4 20011127 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 629SW 27704 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001120300050 20011203 00050 NM 2001 12 3 SWAA013196 1 20011119 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 703SW 27837 EEPLS LOOSE AT ROW 14 AND ROW 15. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001120300051 20011203 00051 NM 2001 12 3 SWAA013201 1 20011127 A 5311 96380 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 399WN 27693 DURING SCHEDULED SPECIAL VISIT, FOUND BOTH LT AND RT OUTBOARD CHORD ANGLES CRACKED AT BS 178, WL 207. REMOVED AND REPLA CED CHORD ANGLES PER SWA ACO. 2 L 7 2 4F RT A16WE 2001120300052 20011203 00052 NM 2001 12 3 SWAA013202 1 20011127 A 2761 654456114 ACTUATOR BOEING 737 7375H4 138449D NM SPOILER FAILED A SWAA O OTHER F FLT CONT AFFECTED UK UNKNOWN 1 SW 07 512SW 24189 NR 7 SPOILER WOULD NOT DEPLOY. FOUND NR 7 SPOILER CABLE LOOSE OUTSIDE THE SPOILER HOUSING AND NR 7 SPOILER ACTUATOR INO P. REMOVED AND REPLACED SPOILER CONTROL CABLES AND SPOILER ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2001120300053 20011203 00053 NM 2001 12 3 SWAA013205 1 20011126 A 5320 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001120300054 20011203 00054 NM 2001 12 3 SWAA013206 1 20011128 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 640SW 27713 DURING SCHEDULED 1/2D CHECK, FOUND LT CREASE BEAM WEB CORRODED AT BS 827 TO BS 847. REPAIRED CREASE BEAM WEB SECTION PE R SRM. 2 L 7 2 4F RT A16WE 2001120300082 20011203 00082 NM 2001 12 3 VNAA0111011 1 20011128 A 2400 8160121 GENERATOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LH FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 459PS 13056 3070 DURING TAKE OFF, THE CREW RECEIVED A DECREASE IN TORQUE INDICATION AND ABORTED TAKE OFF. WHILE PULLING ONTO THE TAXI WA Y, THE CREW RECEIVED A LEFT HAND GENERATOR FAIL MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND GENERATOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FO R SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001123100025 20011231 00025 WP 2001 12 31 AT0100238 1 20011204 A 3350 6011779 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 823AT 47529 FOUND RIGHT NACELLE EMERGENCY LIGHT WOULD NOT ILLUMINATE. REMOVED AND REPLACED THE RIGHT NACELLE LIGHT EMERGENCY BATTER Y PACK IAW DC9 MM 33-53. 2 L 7 2 4F A6WE 2001120300084 20011203 00084 EU 2001 12 3 QXEA0101942 1 20011114 A 5230 RIVET FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RIVET HEAD CHAFED THROUGH, NEAR LATCHING MECHANISM ON CENTER CARGO DOOR SUPPORT ROD. REMOVED AND REPLACED RIVET W ITH CR3223 5-2 RIVET. 2 L 7 2 4F RT A20EU 2001120300085 20011203 00085 EU 2001 12 3 QXEA0101943 1 20011114 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 11405 LT SIDE TO CENTER WING TIE BRACKET IS CRACKED. REPAIRED IAW HORIZON AIR EA 4-53-1520. 2 L 7 2 4F RT A20EU 2001120300086 20011203 00086 EU 2001 12 3 QXEA0101944 1 20011115 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AFT CARGO BAY FRAME 14755 CASTELLATION TIE-IN TO BELLY SKIN AT STRINGER 70 IS CRACKED. REPAIRED IAW FOKKER SRM 53 -02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 2001120300087 20011203 00087 EU 2001 12 3 QXEA0101945 1 20011115 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AFT CARGO BAY FRAME 15205 CASTELLATION TIE-IN TO BELLY SKIN AT STRINGER 6 IS CRACKED. REPAIRED IAW FOKKER SRM 53- 02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 2001120300088 20011203 00088 EU 2001 12 3 QXEA0101946 1 20011115 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AFT CARGO BAY FRAME 15205 CASTELLATION TIE-IN TO BELLY SKIN AT STRINGER 5 IS CRACKED. REPAIRED IAW FOKKER SRM 53- 02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 2001120300089 20011203 00089 EU 2001 12 3 QXEA0101947 1 20011115 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AFT CARGO BAY FRAME 15205 CASTELLATION TIE-IN TO BELLY SKIN AT STRINGER 4 IS CRACKED. REPAIRED IAW FOKKER SRM 53- 02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 2001120300090 20011203 00090 EU 2001 12 3 QXEA0101948 1 20011114 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AFT CARGO BAY FRAME 14755 HAS CORROSION ON TOP SIDE OF UPPER FLANGE FROM STRINGER 2 TO 72. REPAIRED IAW FOKKER SR M 51-10-04. 2 L 7 2 4F RT A20EU 2001120300091 20011203 00091 EU 2001 12 3 QXEA0101949 1 20011113 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - DENT IN FUSELAGE SKIN APPROXIMATELY .040 INCH DEEP, 1 INCH WIDE, 1 INCH LONG, LOCATED 9.375 INCH FORWARD OF CUT OU T FOR THE RT SERVICE EMERGENCY DOOR JUST BELOW STRINGER 55. REPAIRED IAW FOKKER SRM 53-02-02. 2 L 7 2 4F RT A20EU 2001120300092 20011203 00092 EU 2001 12 3 QXEA0101950 1 20011112 A 5310 STOP FITTING FOKKER F28 F28MK4000 4990810 EU FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT AFT OVERWING EMERGENCY EXIT APERTURE STOP PLATES TWO EACH ARE STEP WORN. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001120300093 20011203 00093 EU 2001 12 3 QXEA0101951 1 20011113 A 5541 STRINGER FOKKER F28 F28MK4000 4990810 EU RUDDER BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RUDDER, RT STRINGER BROKEN AT RIB 6, BEHIND PANEL 57Y. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001120300094 20011203 00094 EU 2001 12 3 QXEA0101952 1 20011115 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CORROSION ON FUSELAGE SKIN CUTOUT NEXT TO RIVETS AND NUT PLATES WHERE AFT BLANKING PLATE ATTACHES FOR RADIO ALTIME TER ANTENNA. REPAIRED IAW HORIZON AIR EA 4-53-1521. 2 L 7 2 4F RT A20EU 2001120300095 20011203 00095 NM 2001 12 3 SWAA013209 1 20011127 A 5210 6547952 DOUBLER BOEING 737 7373T5 1384608 NM ENTRY DOOR UNSECURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 667SW 23063 FWD ENTRY DOOR SCAB PATCH ON FWD LOWER CORNER COMING OFF. MX FERRY TO DAL. REMOVED OLD REPAIR AND INSTALLED REPAIR PER SRM. 2 L 7 2 4F RT A16WE 2001120300097 20011203 00097 WP 2001 12 3 ZW0A0111201 1 20011125 A 3412 4024130903 INDICATOR DOUG DC9 DC982 3022082 WP COCKPIT INTERMITTENT A ZW0A A UNSCHED LANDING O OTHER CL CLIMB 1 CE 13 915TW 49186 DURING TAKE-OFF IT WAS NOTED THAT THE RAT GAUGE WAS INTERMITTENT. PLACARDED PER MEDP. THE IND WAS LATER REPLACED. 2 L 7 2 4F A6WE 2001120300098 20011203 00098 EA 2001 12 3 COMA0160935 1 20011130 A 5500 600210617 BUSHING CNDAIR CL600 CL6002B19 1900309 EA L/H VERT STAB LU FAULTY A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 712CA 7802 7244 VERTICAL STABILIZER, L/II HORIZONTAL ATTACH LUG BUSHING MIGRATED.REPLACED BUSHING P/N #600-21061-7 IAW SERVICE BULLETIN 601R-55-007, REF MAINT LOG PAGE #243117 AND COMAIR W/O #169071. 2 L 7 2 4F RT A21EA 2001120300099 20011203 00099 WP 2001 12 3 ZW0A0111202 1 20011125 A 4910 INLET DOUG DC9 DC982 3022082 WP APU CONTAMINATED A ZW0A K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CE 13 918TW 49367 DURING PREFLIGHT INSPECTION IT WAS NOTED THERE WAS SMOKE OR HAZE IN THE CABIN. FOUND OIL AROUND APU INLET. SUSPECT EXCES S OIL RAN DOWN INTO APU INLET. 2 L 7 2 4F A6WE 2001120300100 20011203 00100 WP 2001 12 3 ZW0A0111203 1 20011125 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 9305N 49395 DURING PREFLIGHT INSPECTION IT WAS NOTED THE RH MID ZONE EGRESS LIGHTS WERE INOP. REPAIRED BROKEN WIRE AT ROW 16 RH SIDE . 2 L 7 2 4F RT A6WE 2001120300101 20011203 00101 WP 2001 12 3 ZW0A011121 1 20011125 A 3412 4034241973 INDICATOR DOUG DC9 DC982 3022082 WP COCKPIT INTERMITTENT A ZW0A A UNSCHED LANDING O OTHER CL CLIMB 1 CE 13 915TW 49186 DURING TAKE-OFF IT WAS NOTED THAT THE RAT GAUGE WAS INTERMITTENT. PLACARDED PER MEDP. -OPEN- 2 L 7 2 4F A6WE 2001120300102 20011203 00102 WP 2001 12 3 ZW0A011122 1 20011125 A 4910 INLET DOUG DC9 DC982 3022082 WP APU CONTAMINATED A ZW0A K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CE 13 918TW 49367 DURING PREFLIGHT INSPECTION IT WAS NOTED THERE WAS SMOKE OR HAZE IN THE CABIN. FOUND OIL AROUND APU INLET. SUSPECT EXCES S OIL RAN DOWN INTO APU INLET. 2 L 7 2 4F A6WE 2001120300103 20011203 00103 WP 2001 12 3 ZW0A011123 1 20011125 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 9305N 49395 DURING PREFLIGHT INSPECTION IT WAS NOTED THE RH MID ZONE EGRESS LIGHTS WERE INOP. REPAIRED BROKEN WIRE AT ROW 16 RT SIDE . 2 L 7 2 4F RT A6WE 2001120300104 20011203 00104 EA 2001 12 3 COMA0160936 1 20011201 A 5311 600360302331 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FS718.0 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 712CA 7802 7244 THE L/H SIDE FRAME AND AFT DOUBLER AT FS718.0 WERE CRACKED BETWEEN STRINGERS 10 AND 12.REMOVED THE CRACKED AFT DOUBLER A ND DAMAGED SECTION OF FRAME. INSTALLED NEW SECTION OF FRAME SPLICE AND NEW AFT DOUBLER I/A/W REO 601R-53-61-193 REV A. 2 L 7 2 4F RT A21EA 2001120300105 20011203 00105 NM 2001 12 3 ZW0A0111301 1 20011119 A 3350 80741 LAMP BOEING 767 767* NM CABIN MISSING A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 639TW 26208 THE EGRESS LIGHT AT CABIN SEAT 33B WAS MISSING. INSTALLED LAMP ASSEMBLY. 2 L 7 2 4F RT A1NM 2001120300106 20011203 00106 WP 2001 12 3 ZW0A0111302 1 20011117 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9401W 53137 DURING CHECK-C MAINT THE NUMBER 2 RT LONGERON WAS CRACKED .125 INCH AT STA 1220. REPAIRED PER SRM 53-02, PAGES 49 THRU 53. 2 L 7 2 4F RT A6WE 2001120300107 20011203 00107 EA 2001 12 3 COMA0160937 1 20011203 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 804CA 4510 7352 EDDY CURRENT INSPECTION SHOWS A CRACK INDIATION ON THE LEFT LOWER WING PLANK AT 540 FB.REMOVED DAMAGE AND ROTO-PEENED SU RFACT I/A/W REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 2001120300118 20011203 00118 NM 2001 12 3 SPAA0100048 1 20011129 A 3350 6104791 BATTERY BOEING 737 7372T4 1384492 NM FWD L1 DOOR INTERMITTENT A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 FORWARD EMERGENCE ESCAPE SLIDE LIGHTS INTERMITTENT. REPLACED FWD EMERGENCY SLIDE LIGHTS BATTERY POWER SUPPLY PER MM 33-5 1-71. OPS CHECK GOOD. 2 L 7 2 4F A16WE 2001120300124 20011203 00124 EA 2001 12 3 SWIA200110403 1 20011129 A 5270 PROXIMITY SWITCH CNDAIR CL600 CL6002B19 1900309 EA PASSENGER DOOR OUT OF ADJ A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 416SW 7089 CLIMBING THRU 20,000', WE GOT A DOOR LATCH CAUTION MESSAGE. CLIMBING THRU 23,000', WE GOT A PASSENGER DOOR WARNING. TH E WARNING WENT OUT DESCENDING THRU 14,000'. LATCH CAUTION CAME BACK ON, CAUTION WENT OUT AT 10,000'. ACCOMPLISHED PAX DOOR WARNING ADJUSTMENT TEST IAW 52-70-04. FOUND PROXIMITY SENSOR PS9MB OUT OF ADJUSTMENT. ADJUSTED SENSOR AND TESTED PASSENGER DOOR WARNING SYSTEM IAW CRJ MM 52-70-04. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2001120300129 20011203 00129 SW 2001 12 3 AC22001F00000 1 20011005 A 2120 3136171 SOLENOID BELL 430 430 1182150 SW ALLSN 250B 250B* GL DIVERTER VALVE FAILED E AC2A O OTHER O OTHER NR NOT REPORTED 1 SW 03 430CV 49072 DIVERTER VALVE NOT OPENING OR CLOSING. TOO MUCH COLD AIR COMING OUT OF LOWER VENTS. REPLACED WITH NEW SOLENOID. IT FI XED PROBLEM. 1 G 7 2 3U 3 T RT H9SW E10CE 2001120300130 20011203 00130 SW 2001 12 3 AC22001F00001 1 20010923 A 5320 206033107055 STIFFENER BELL 206 206L3 1182108 SW ALLSN 250C 250C20 03013 GL FUSELAGE CRACKED E AC2A K NONE O OTHER IN INSP/MAINT 1 SW 03 715CC 51380 STIFFENER PART IS CRACKED. REPLACED WITH NEW PART. 1 G 7 1 3U 3 U H2SW E4CE 2001120300131 20011203 00131 SW 2001 12 3 AC22001F00002 1 20010923 A 5320 206033107054 STIFFENER BELL 206 206L3 1182108 SW ALLSN 250C 250C20 03013 GL FUSELAGE CRACKED E AC2A K NONE O OTHER IN INSP/MAINT 1 SW 03 715CC 10225 51380 STIFFENER, PART IS CRACKED. REPLACED WITH NEW PART. 1 G 7 1 3U 3 U H2SW E4CE 2001120300132 20011203 00132 SW 2001 12 3 AC22001F00003 1 20010923 A 5320 206033107053 STIFFENER BELL 206 206L3 1182108 SW ALLSN 250C 250C20 03013 GL FUSELAGE CRACKED E AC2A K NONE O OTHER IN INSP/MAINT 1 SW 03 715CC 10225 51380 STIFFENER, PART IS CRACKED. REPLACED WITH NEW PART. 1 G 7 1 3U 3 U H2SW E4CE 2001120300133 20011203 00133 SW 2001 12 3 AC22001F00004 1 20010925 A 5320 206033107052 CLIP BELL 206 206L3 1182108 SW ALLSN 250C 250C20 03013 GL FUSELAGE CRACKED E AC2A K NONE O OTHER IN INSP/MAINT 1 SW 03 715CC 10225 51380 CLIP, PART IS CRACKED. REPLACED WITH NEW PART. 1 G 7 1 3U 3 U H2SW E4CE 2001120300134 20011203 00134 SW 2001 12 3 AC22001F00005 1 20011017 A 3212 206073926103 VALVE BELL 206 206L3 1182108 SW ALLSN 250C 250C30 03013 GL MLG FAILED E AC2A O OTHER O OTHER NR NOT REPORTED 1 SW 03 17237 234 51478 VALVE, RETURNING PART FOR WARRANTY CREDIT DUE TO IT FAILING AFTER ONLY 234 HOURS. 1 G 7 1 3U 3 U H2SW E1GL 2001120300135 20011203 00135 SW 2001 12 3 AC22001F00006 1 20011018 A 7810 206064300005 EXHAUST STACK BELL 206 206L3 1182108 SW ALLSN 250C 250C30 03013 GL ENGINE CRACKED E AC2A O OTHER O OTHER NR NOT REPORTED 1 SW 03 7159J 711 51408 EXHAUST ASSEMBLY, CRACKED. REPLACED WITH NEW EXHAUST STACK. 1 G 7 1 3U 3 U H2SW E1GL 2001120300136 20011203 00136 SW 2001 12 3 AC22001F00007 1 20010823 A 7810 206064300005 EXHAUST STACK BELL 206 206L3 1182108 SW ENGINE CRACKED E AC2A O OTHER O OTHER NR NOT REPORTED 1 SW 03 53702 11952 51249 EXHAUST ASSEMBLY CRACKED. REPLACED WITH SERVICEABLE EXHAUST STACK. 1 G 7 1 3U H2SW 2001120300137 20011203 00137 2001 12 3 AC22001F00008 4 20011025 A 3425 956A14B659889 SWITCH BELL 430 430 1182150 SW COCKPIT FAILED E AC2A O OTHER O OTHER NR NOT REPORTED 1 SW 03 430CV 750 49072 EADI (TOP TUBE) WOULD NOT SHUT OFF. TUBE WOULD ILLUMINATE WHEN BATTERY SWITCH PLACED ON . REPLACED SWITCH. CURED PROB LEM. 1 G 7 2 3U RT H9SW 2001120300138 20011203 00138 NE 2001 12 3 AC92001F00000 2 20010626 A 8530 116731 CYLINDER DOUG DC3 DC3C 3021457 WP PWA R1830 R183090D 52020 NE LT ENGINE CRACKED A AC9T A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 GL 05 9923S 649 25964 BP436078 AT CRUISE POWER, LEFT ENGINE DEVELOPED A SLIGHT VIBRATION. AIRCRAFT WAS ENROUTE FROM DEPART TO ARRIVAL, DIVERTED. FO UND NR 14 CYLINDER, LEFT ENGINE CRACKED AT EXHAUST PORT. 2 L 7 2 4R 4 R A669 5E4 2001120300139 20011203 00139 NE 2001 12 3 ALG2001F00026 1 20011016 A 2612 MS3476L106S PLUG SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL NR 2 ENGINE CONTAMINATED E ALGA K NONE L NO TEST IN INSP/MAINT 1 SW 03 741SW 760070 CAE890236S DURING PRESTART CHECK, AFT DETECTOR ON NR2 ENGINE WOULD NOT TEST. WATER WAS FOUND IN THIS PLUG, IT WAS DRIED OUT AND TE STED GOOD. 1 G 7 2 3U 3 U H1NE E1GL 2001120300140 20011203 00140 NE 2001 12 3 ALG2001F00027 1 20011016 A 2620 6590102458103 RELAY SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL EXTINGUISH SYS FAULTY E ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 519AL 760058 CAE890588S DURING PRESTART CHECK OF THE ENGINE FIRE EXTINGUISHING SYSTEM, BOTTLE FIRED DURING TEST, RELAY COIL FOUND FAULTY. 1 G 7 2 3U 3 U H1NE E1GL 2001120300141 20011203 00141 GL 2001 12 3 ALG2001F00028 2 20011011 A 7250 23053299 BLADE ALLSN BELL 206 206L3 1182108 SW ALLSN 250C 250C30 03013 GL ENGINE CORRODED E ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 351AL 1732 CAT98247 51431 CAE895516 TURBINE TIME CHANGE DUE 1ST AND 2ND STAGE WHEELS, CYCLED OUT. TURBINE HAD A MFG LINER INSTALLED. REMOVED COMBUSTION SE CTION AND FOUND SULFIDATION ON NR 1 WHEEL BLADES. (K) 1 G 7 1 3U 3 U H2SW E1GL 2001120300142 20011203 00142 2001 12 3 AWXA200100608 4 20011130 A 2565 D3186511 SLIDE AIRBUS A319 A319132 3930340 NM DEPLOYED A AWXA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 WP 28 825AW 1384 274 1527 SJC - GROUND DAMAGE - FLT 548 - "C" - WHILE AT GATE, ECAM DOOR PAGE DISPLAYED LEFT OVER WING EMERGENCY ESCAPE SLIDE NOT ARMED; MAINTENANCE WAS CALLED AND ALSO VERIFIED LEFT OVER WING EXIT LIGHT WAS NOT ILLUMINATED. WHILE ATTEMPTING TO RESET THE L/H OVER WING EXIT DOOR ARMING LATCH PIN THE SLIDE WAS INADVERTENTLY DEPLOYED DAMAGING THE AERODYNAMIC SEAL AT L/H WING TO BODY FAIRING. AIRCRAFT WAS MAINTENANCE FERRIED BACK TO PHX WHERE BOTH THE DAMAGED SEAL AND L/H OVER WING EXIT SL IDE WERE REPLACED. SLIDE REPLACED IAW T/C R1A25301. 2 L 7 2 4F RT A28NM 2001120300143 20011203 00143 GL 2001 12 3 ALG2001F00030 2 20011019 A 7250 23053299 BLADE BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL ENGINE CORRODED E ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 3174Y 1830 51038 CAE895796 TURBINE RECEIVED FOR TIME CHANGE ON 3RD AND 4TH STAGE WHEEL RETIREMENT. TURBINE HAD A MFG LINER INSTALLED. REMOVED COM BUSTION SECTION AND FOUND SULFIDATION ON 1ST STAGE WHEEL BLADES. CHECK 1ST STAGE WHEELS FOR PROPER COATING.(K) 1 G 7 1 3U 3 U H2SW E1GL 2001120300144 20011203 00144 SW 2001 12 3 ALG2001F00031 1 20011001 A 6210 206015001119 SPAR BELL BELL 206 206L1 1182107 SW ALLSN 250C 250C30 03013 GL M/R BLADE CORRODED E ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 1067D 786 45435 DISCOVERED DURING ROUTINE MAINTENANCE INSPECTION. SPAR EXFOLIATION WAS DETECTED ON LOWER SURFACE SKIN/SPAR SPLICE JOINT , CONSIDERED A MATERIAL DEFECT. BLADE WAS REMOVED FROM SERVICE AND SCRAPPED. 1 G 7 1 3U 3 U H2SW E1GL 2001120300145 20011203 00145 NE 2001 12 3 ALG2001F00032 1 20011016 A 2620 6590102458103 RELAY SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30 03013 GL EXTIGUISHING SYS FAULTY E ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 519AL 760058 DURING PRESTART CHECK OF THE ENGINE FIRE EXTINGUISHING SYSTEM. BOTTLE FIRED DURING TEST, RELAY COIL WAS FOUND FAULTY. 1 G 7 2 3U 3 U H1NE E1GL 2001120300146 20011203 00146 NE 2001 12 3 ALG2001F00033 1 20011016 A 2612 MS3476L106S PLUG SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL NR 2 ENGINE CONTAMINATED E ALGA K NONE L NO TEST IN INSP/MAINT 1 SW 03 741SW 760070 CAE890236S DURING PRESTART CHECK. AFT DETECTOR ON NR 2 ENGINE WOULD NOT TEST. WATER WAS FOUND IN THIS PLUG, IT WAS DRIED OUT AND TESTED GOOD. 1 G 7 2 3U 3 U H1NE E1GL 2001120300148 20011203 00148 SW 2001 12 3 ALG2001F00035 1 20011005 A 6510 407340340103 DISC PACK BELL 407 407 1182206 SW ALLSN 250C 250C30 03013 GL TAIL ROTOR CRACKED E ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 58236 53069 ON TAIL ROTOR DRIVESHAFT, DURING 25 HOUR AD INSPECTION, CRACKED DISC. 1 G 7 1 3U 3 U O H2SW E1GL 2001120300149 20011203 00149 SW 2001 12 3 ALG2001F00036 1 20011009 A 6230 406010427109 RING BELL 407 407 1182206 SW ALLSN 250C 250C47B GL MAIN ROTOR CORRODED E ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 587AL 1653 53248 CAE847250 DURING PHASE INSPECTION. CORROSION BEYOND MAXIMUM LIMITS. 1 G 7 1 3U 3 U O H2SW E1GL 2001120300150 20011203 00150 SW 2001 12 3 ALG2001F00037 1 20011003 A 6220 407310101101 BEARING BELL 407 407 1182206 SW ALLSN 250C 250C47B GL MAIN ROTOR DELAMINATED E ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 617AL 2372 53265 CAE847158 ON DAILY INSPECTION, DELAMINATED ELASTOMER ON BEARING. 1 G 7 1 3U 3 U O H2SW E1GL 2001120300151 20011203 00151 SW 2001 12 3 ALG2001F00038 1 20010928 A 6510 407340339103 BEARING BELL BELL 407 407 1182206 SW ALLSN 250C 250C47B GL TAIL ROTOR FAILED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 406AL 29 A565 53481 BEARING FAILED, COMPLIED WITH ASB 407-01-44. 1 G 7 1 3U 3 U O H2SW E1GL 2001120300152 20011203 00152 SW 2001 12 3 ALG2001F00039 1 20011005 A 6510 47340340103 DISC PACK BELL 407 407 1182206 SW ALLSN 250C 250C47B GL TAIL ROTOR CRACKED E ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 627AL 53284 DURING 25 HOUR AD INSPECTION, FOUND TAIL ROTOR DRIVESHAFT DISC CRACKED. 1 G 7 1 3U 3 U O H2SW E1GL 2001120300153 20011203 00153 GL 2001 12 3 ALG2001F00040 2 20011003 A 7260 23066678 BEARING ALLSN BELL 407 407 1182206 SW ALLSN 250C 250C20 03013 GL ENGINE MISMARKED E ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 497AL GAG47258 53172 UPON VERIFICATION OF PN AND SN AFTER CHECKING OUT OF STOCK. INNER RACE AND ROLLER RETAINER BOTH HAVE 2 DIFFERENT SERIAL NUMBERS ETCHED ON THE PART. ASSURE THE PART NUMBER AND SERIAL NUMBER AT FACTORY. 1 G 7 1 3U 3 U O H2SW E4CE 2001120300154 20011203 00154 GL 2001 12 3 ALG2001F00041 2 20011003 A 7260 23066678 BEARING ALLSN C47B BELL 407 407 1182206 SW ALLSN 250C 250C47B GL GEARBOX FAILED E ALGA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 497AL 4254 CAG47258 53172 CAE847517 UPON DISASSEMBLY OF GEARBOX DUE TO CHIP LIGHT. NR 4 BEARING FAILURE. TOOTH MISSING FROM GEAR ON PINION GEAR, AND DAMAG ED GEAR TEETH ON T/M GEAR. 1 G 7 1 3U 3 U O H2SW E1GL 2001120300155 20011203 00155 SW 2001 12 3 ALG2001F00042 1 20011004 A 6510 407340340103 COUPLER BELL BELL 407 407 1182206 SW ALLSN 250C 250C20 03013 GL TAIL ROTOR CRACKED E ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 457AL A1178 53151 CAE847197 DAILY 25 HOUR INSPECTION FOUND NR 7 DISC PACK COUPLING CRACKED. 1 G 7 1 3U 3 U O H2SW E4CE 2001120300156 20011203 00156 SO 2001 12 3 C2XA01IA407 1 20011203 A 3350 AD2047 BATTERY EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17728 411 120182 IAH- DURING MAINTENANCE THE MECHANIC NOTED THAT THE AFT EXTERNAL EMERGENCY LIGHTS FAILED TO ILLUMINATE. IAH- MAINTENA NCE REMOVED AND REPLACED THE AFT EMERGENCY BATTERY,AND, BATTERY PACK,AND,PERFORMED A OPERATIONAL CHECK,NO DEFECTS NOTED, AND, THE AIRCRAFT WEA APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001120400001 20011204 00001 NM 2001 12 4 01FDEA01024 1 20011204 A 2613 LOOP BOEING 727 727233 138408A NM FAULTY A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 270FE 22035 1-385 DUR CLB LWR AFT BODY OVERHEAT LIGHT CAME ON. REPOSITIONED LOOP IN LEFT SIDE OF CENTRAL STAIRS PER MM 26-14-001-2. 2 L 7 3 4F RT A3WE 2001120400002 20011204 00002 NM 2001 12 4 CALA0101018 1 20011202 A 5320 WEB BOEING 737 7373T0 1384582 NM CARGO DR SILL CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71314 23365 INSPECTION FOUND AFT CARGO DOOR THRESHOLD SILL WEB CORRODED ON TOP AND UNDER SIDE. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001120400003 20011204 00003 EU 2001 12 4 QXEA0101953 1 20011113 A 2150 DUCT FOKKER F28 F28MK4000 4990810 EU ACM EXHAUST CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RT ACM EXHAUST DUCT HAS A 2.5 INCH CRACK ALONG A WELD AT BOTTOM EDGE OF PANEL. REPAIRED IAW FOKKER MM 21-50-8, PA GE 401, PARAGRAPH 2 AND AMM 51-30-00, PAGE 701-706. 2 L 7 2 4F RT A20EU 2001120400004 20011204 00004 EU 2001 12 4 QXEA0101954 1 20011113 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT SIDE COCKPIT EXTERNAL SKIN HAS A 1.2 INCH LONG BY .150 INCH WIDE CHAFE MARK 3 INCHES FORWARD OF FRAME 1890, CHA FE IS THROUGH CLAD LAYER. REPAIRED IAW FOKKER SRM 53-01-01, PARAGRAPH D, AREA B AND SRM 51-01-4, AMM 51-30-00, PAGE 701 -706. 2 L 7 2 4F RT A20EU 2001120400005 20011204 00005 EU 2001 12 4 QXEA0101955 1 20011113 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT SIDE COCKPIT EXTERNAL SKIN HAS A .75 INCH LONG X .100 INCH WIDE CHAFE MARK, 5 INCH FORWARD OF FRAME 1890, CHAFE IS THROUGH ALCLAD LAYER. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 3, AREA B. 2 L 7 2 4F RT A20EU 2001120400006 20011204 00006 EU 2001 12 4 QXEA0101956 1 20011113 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT SIDE COCKPIT EXTERNAL SKIN HAS A .25 INCH LONG X .100 INCH WIDE CHAFE MARK, 10 INCHES FORWARD OF FRAME 1890, CH AFE IS THROUGH ALCLAD LAYER. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 3, AREA B AND AMM 51-30-00, PAGE 701-706. 2 L 7 2 4F RT A20EU 2001123100100 20011231 00100 NM 2001 12 31 QXEA0101963 1 20011121 A 3260 401070101 PROXIMITY SENSOR DHAV DHC8 DHC8* NM LT MLG FAILED A QXEA K NONE J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 NM 09 407QX 4049 PDX-LEFT MAIN GEAR DOOR CYCLING IN FLIGHT. LEFT GEAR DOOR LIGHT WOULD ILLUMINATE AND BE ACCOMPANIED BY A SLIGHT VIBRATI ON. REMOVED AND REPLACED LEFT HAND MAIN LANDING GEAR UPLOCK PROXIMITY SENSOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURN ED TO SERVICE. 2 H 7 2 4T RT A13NM 2001120400007 20011204 00007 NM 2001 12 4 QXEA0101964 1 20011125 A 5210 DOOR DHAV DHC8 DHC8101 2809002 NM PAX DOOR MALFUNCTIONED A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 830PH 314 SEA- FLIGHT ATTENDANT UNABLE TO OPEN MAIN CABIN DOOR. INSPECTED MAIN CABIN DOOR AND ACTUATOR. NO DEFECTS NOTED. NO PA RTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001120400008 20011204 00008 EU 2001 12 4 QXEA0101965 1 20011126 A 3350 6008905 POWER SUPPLY FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 499US * 2727 11182 PDX- BOTH FORWARD EXTERIOR EVACUATION LIGHTS FAIL TO ILLUMINATE WHEN SELECTED ON. REMOVED AND REPLACED POWER SUPPLY. O PERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001120400009 20011204 00009 EU 2001 12 4 QXEA0101966 1 20011120 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FUSELAGE FRAME 16060 TIE IN CLIP TO BELLY SKIN HAS CORROSION ON TOP SURFACE AROUND (3) RIVETS BETWEEN STRINGERS 73 AND 74. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2, PAGE 4. 2 L 7 2 4F RT A20EU 2001120400010 20011204 00010 EU 2001 12 4 QXEA0101967 1 20011120 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FUSELAGE FRAME 16060 TIE IN CLIP TO BELLY SKIN HAS CORROSION ON TOP SURFACE ROUND RIVETS BETWEEN STRINGERS 1 AND 7 4. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6 AND SRM 51-10-04, PARAGRAPH 4B, C, PAGE 9. 2 L 7 2 4F RT A20EU 2001121400008 20011214 00008 NE 2001 12 14 ARWA20011124 2 20011201 A 7230 640702 BLADE DOUG DC8 DC85F54 3021926 WP PWA JT3D JT3D3B 52039 NE ENGINE FAILED A ARWA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 SO 19 426FB 1639 45667 669322 ON TAKE OFF MIAMI A LOUD BANG FOLLOWED BY HIGH VIBRATION ON NR 2 ENGINE REJECTED THE TAKE OFF ROLL. FOUND C2 BLADE FAILU RE. REMOVED AND REPLACED NR 2 ENGINE. OPS AND LEAK CHECK NORMAL. 2 L 7 4 4F 4 F RT 4A25 1E8 2001120400011 20011204 00011 EU 2001 12 4 QXEA0101968 1 20011120 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FUSELAGE BELLY STRINGER 1 HAS CORROSION AT TIE IN CLIP AREA AFT SIDE OF FRAME 16060. REPAIRED IAW FOKKER SRM 51-1 0-01, 4B, C, PAGE 9. 2 L 7 2 4F RT A20EU 2001120400012 20011204 00012 EU 2001 12 4 QXEA0101969 1 20011120 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FUSELAGE INTERIOR BELLY SKIN AT AFT SIDE OF FRAME 16060 BETWEEN STRINGER 1 AND 2 HAS CORROSION. REPAIRED IAW FOKK ER SRM 51-10-04, PARAGRAPH 4B, C, PAGE 9. 2 L 7 2 4F RT A20EU 2001120400013 20011204 00013 EU 2001 12 4 QXEA0101970 1 20011120 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FUSELAGE FRAME 16060 TIE IN CLIP TO BELLY SKIN HAS CORROSION ON TOP SURFACE AROUND (3) RIVETS BETWEEN STRINGERS 1 AND 2. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2, PAGE 4. 2 L 7 2 4F RT A20EU 2001120400014 20011204 00014 EU 2001 12 4 QXEA0101971 1 20011120 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FUSELAGE FRAME 16060 TIE IN CLIP TO BELLY SKIN HAS CORROSION ON TOP SURFACE AROUND (3) RIVETS BETWEEN STRINGERS 2 AND 3. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4B, C, PAGE 9. 2 L 7 2 4F RT A20EU 2001120400015 20011204 00015 EU 2001 12 4 QXEA0101972 1 20011120 A 5330 DOUBLER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FUSELAGE INTERIOR BELLY SKIN DOUBLER HAS CORROSION AROUND (3) RIVETS AT AFT SIDE OF ANGLED FRAME 15810 BETWEEN STR INGERS 1 AND 2. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 6. 2 L 7 2 4F RT A20EU 2001120400016 20011204 00016 EU 2001 12 4 QXEA0101973 1 20011120 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - ANGLED FRAME 15810 HAS CORROSION ON FORWARD AND AFT SIDES AT CUTOUTS AROUND STRINGERS 1 AND 74. REPAIRED IAW FOKK ER SRM 51-10-04, PARAGRAPH 4B, C, PAGE 9. 2 L 7 2 4F RT A20EU 2001120400017 20011204 00017 EU 2001 12 4 QXEA0101974 1 20011120 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - ANGLED FRAME 15810 TIE IN CLIP TO FUSELAGE BELLY SKIN HAS CORROSION ON TOP SURFACE BETWEEN STRINGERS 73 AND 74. R EPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001120400018 20011204 00018 EU 2001 12 4 QXEA0101975 1 20011120 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FUSELAGE INTERIOR BELLY SKIN HAS CORROSION AROUND (8) RIVETS BETWEEN FRAMES 15635 AND 15810, FROM STRINGER 73 AND 74. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4B, C, PAGE 9 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001120400019 20011204 00019 EU 2001 12 4 QXEA0101976 1 20011120 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FUSELAGE FRAME 15635 TIE IN CLIP TO BELLY SKIN HAS CORROSION ON TOP SURFACE AROUND RIVETS BETWEEN STRINGER 73 AND 74. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001120400020 20011204 00020 EU 2001 12 4 QXEA0101977 1 20011115 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 16660 CLIP CRACKED AT INBOARD END IN RADIUS. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2, PAGE 4. 2 L 7 2 4F RT A20EU 2001120400021 20011204 00021 EU 2001 12 4 QXEA0101979 1 20011118 A 5315 FLOORBEAM FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FLOORBEAM REPAIR BL 0 JUST FORWARD OF FRAME 4900 TOP TIE PLATE HAS LIGHT CORROSION. REPAIRED IAW HORIZON AIR EA 4 -53-1526. 2 L 7 2 4F RT A20EU 2001120400022 20011204 00022 EU 2001 12 4 QXEA0101980 1 20011118 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RT OUTBOARD SEAT TRACK HAS PITTING ON INBOARD FLANGE AT APPROXIMATELY STATION 349 - 357. REPAIRED IAW HORIZON AIR EA 4-53-1528. 2 L 7 2 4F RT A20EU 2001120400023 20011204 00023 EU 2001 12 4 QXEA0101981 1 20011118 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RT OUTBOARD SEAT TRACK HAS PITTING ON OUTBOARD FLANGE AT APPROXIMATELY STATION 325 - 327. REPAIRED IAW HORIZON AI R EA 4-53-1528. 2 L 7 2 4F RT A20EU 2001120400024 20011204 00024 EU 2001 12 4 QXEA0101982 1 20011118 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RT OUTBOARD SEAT TRACK HAS THREE PITS ON OUTBOARD FLANGE AT APPROXIMATELY STATION 232 - 234. REPAIRED IAW HORIZON AIR EA 4-53-1528. 2 L 7 2 4F RT A20EU 2001120400025 20011204 00025 EU 2001 12 4 QXEA0101983 1 20011118 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RT INBOARD SEAT TRACK IS PITTED ON INBOARD FLANGE AT APPROXIMATELY STATION 676 - 685. REPAIRED IAW HORIZON AIR EA 4-53-1527. 2 L 7 2 4F RT A20EU 2001120400026 20011204 00026 EU 2001 12 4 QXEA0101984 1 20011118 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RT INBOARD SEAT TRACK HAS PITTING ON INBOARD FLANGE AT APPROXIMATELY STATION 340-404. REPAIRED IAW HORIZON AIR EA 4-53-1527. 2 L 7 2 4F RT A20EU 2001120400027 20011204 00027 EU 2001 12 4 QXEA0101985 1 20011118 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RT INBOARD SEAT TRACK HAS PITTING ON INBOARD FLANGE AT APPROXIMATELY STATION 306 - 327. REPAIRED IAW HORIZON AIR EA 4-53-1527. 2 L 7 2 4F RT A20EU 2001120400028 20011204 00028 EU 2001 12 4 QXEA0101986 1 20011114 A 5230 FLANGE FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CENTER CARGO DOOR LOWER FORWARD CORNER FLANGE ABOVE SEAL MATING SURFACE CRACKED. REPAIRED IAW FOKKER SRM 52-02-04 . 2 L 7 2 4F RT A20EU 2001120400029 20011204 00029 EU 2001 12 4 QXEA0101987 1 20011114 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CASTELLATION CRACKED BEYOND 1ST STOP DRILL AND PROGRESSING UP WEB OF CASTELLATION ON FRAME 17565, ABOVE STRINGER 1 0. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001120400030 20011204 00030 EU 2001 12 4 QXEA0101988 1 20011113 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CASTELLATION CRACKED AT TOP RIVET ON FRAME 17565 BELOW STRINGER 53. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5. 2 L 7 2 4F RT A20EU 2001120400031 20011204 00031 EU 2001 12 4 QXEA0101989 1 20011113 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CASTELLATION CRACKED ADJACENT TO LOWER RIVET ON FRAME 17565 ABOVE STRINGER 55. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 8-9 AND SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001120400032 20011204 00032 EU 2001 12 4 QXEA0101990 1 20011115 A 5755 STRAP FOKKER F28 F28MK4000 4990810 EU SPEEDBRAKE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - SPEEDBRAKE ACCUMULATOR FORWARD MOUNT ASSEMBLY TOP FINGER STRAP CRACKED. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001120400033 20011204 00033 EU 2001 12 4 QXEA0101991 1 20011115 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CASTELLATION CRACKED AT LOWER RIVET ON FRAME 20075 ABOVE STRINGER 28. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 3, SRM 51-31-01 AND SRM 53-10-05. 2 L 7 2 4F RT A20EU 2001120400034 20011204 00034 EU 2001 12 4 QXEA0101992 1 20011114 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CASTELLATION CRACKED IN RADIUS ON FORWARD SIDE OF FRAME 50-2 ABOVE STRINGER 48. REPAIRED IAW FOKKER SRM 51-10-0, SRM 53-02-18, PAGE 5 AND SRM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 2001120400035 20011204 00035 NM 2001 12 4 SWAA013224 1 20011201 A 5310 6516300 WEB BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234 AND LBL 10. REPAIRED WEB PER SRM. 2 L 7 2 4F A16WE 2001120400036 20011204 00036 NM 2001 12 4 SWAA013225 1 20011201 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 616SW 27699 EEPLS COVER MISSING AT ROW 8. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2001120400037 20011204 00037 NM 2001 12 4 SWAA013226 1 20011130 A 5310 6935352 TIE CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 767, STR 11R. REMOVED AND REPLACED TIE CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001120400038 20011204 00038 EU 2001 12 4 QXEA0101993 1 20011118 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 22293 CRACKED APPROXIMATELY 1.25 INCH IN OUTBOARD RADIUS AT AFT END OF STRINGER 21A. REPAIRED IAW HORIZON A IR EA 4-53-1524. 2 L 7 2 4F RT A20EU 2001120400039 20011204 00039 EU 2001 12 4 QXEA0101994 1 20011119 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 22293 CRACKED APPROXIMATELY .5 INCH IN OUTBOARD RADIUS. REPAIRED IAW HORIZON AIR EA 4-53-1524. 2 L 7 2 4F RT A20EU 2001120400040 20011204 00040 EU 2001 12 4 QXEA0101995 1 20011119 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 22293 CRACKED APPROXIMATELY 1.5 INCH IN OUTBOARD RADIUS AT AFT END OF STRINGER 53A. REPAIRED IAW HORIZON AI R EA 4-53-1524. 2 L 7 2 4F RT A20EU 2001120400041 20011204 00041 EU 2001 12 4 QXEA0101996 1 20011114 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AFT VHF LOWER COMM ANTENNA LOCATION HAS SURFACE CORROSION ON FUSELAGE. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, P ARAGRAPH 4 A AND B, SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001120400042 20011204 00042 EU 2001 12 4 QXEA0101997 1 20011116 A 5350 SUPPORT FOKKER F28 F28MK4000 4990810 EU FAIRING BENT A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - BENT FAIRING SUPPORT STRUCTURE IS BENT. REPAIRED IAW FOKKER SRM 53-53-11, PAGE 35, ITEM 265, SRM 51-10-4, PARAGRA PH 4 B AND C. 2 L 7 2 4F RT A20EU 2001120400043 20011204 00043 EU 2001 12 4 QXEA0101998 1 20011111 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 16660 CLIP CORRODED AT STRINGER 74. REPAIRED IAW FOKKER SRM 53-01-01 AND SRM 51-10-04. 2 L 7 2 4F RT A20EU 2001120400044 20011204 00044 EU 2001 12 4 QXEA0101999 1 20011115 A 5511 RIB FOKKER F28 F28MK4000 4990810 EU HORIZ STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - HORIZONTAL STABILIZER LEADING EDGE 51B THIRD RIB FROM INBOARD END CRACK TOP FORWARD. REPAIRED IAW FOKKER SRM 51-1 0-4, SRM 51-31-01, PAGE 13, PARAGRAPH 7B. 2 L 7 2 4F RT A20EU 2001120400045 20011204 00045 EU 2001 12 4 QXEA0102000 1 20011114 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AFT CARGO BAY FRAME 15635 DRAIN HOLE AND 90 DEGREE FLANGE AREA TOP SURFACE IS CORRODED BETWEEN STRINGER 1 AND 74 A T FORWARD SIDE OF FRAME 15635. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6 AND SRM 51-10-04, PARAGRAPH 4 B AND C, PAGE 9. 2 L 7 2 4F RT A20EU 2001120400046 20011204 00046 EU 2001 12 4 QXEA0102001 1 20011114 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AFT CARGO BAY ANTENNA BOX STRUCTURE AND AIRCRAFT INTERIOR BELLY SKIN FORWARD OF AND INSIDE BOX IS CORRODED BETWEEN STRINGER 1 AND 74 AT AFT SIDE OF FRAME 15205. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-31-05. 2 L 7 2 4F RT A20EU 2001120400047 20011204 00047 EU 2001 12 4 QXEA0102002 1 20011114 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AFT CARGO BAY FRAME 15205 CASTELLATION TIE IN TO BELLY SKIN AT STRINGER 74 HAS CORROSION ON TOP SURFACE AROUND RIV ET HOLE. REPAIRED IAW FOKKER SRM 53-02-13, SRM 51-10-04 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001120400048 20011204 00048 EU 2001 12 4 QXEA0102003 1 20011115 A 5230 STRUCTURE FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - DENT 1.8 INCH LONG, 1.2 INCH WIDE, APPROXIMATELY .10 INCH DEEP ON TOP EDGE OF CENTER CARGO DOOR, 15INCHES AFT OF L EADING EDGE OF DOOR. REPAIRED IAW MM 51-00-00, PAGE 1 AND MM 51-30-02. 2 L 7 2 4F RT A20EU 2001120400049 20011204 00049 EU 2001 12 4 QXEA0102004 1 20011110 A 5540 RUDDER FOKKER F28 F28MK4000 4990810 EU TAIL DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - REMOVE RUDDER FOR SHEET METAL REPAIR. REPAIRED IAW FOKKER MM 27-20-01, PAGE 404, PARAGRAPH 3D AND MM 27-20-02, PA GE 201. 2 L 7 2 4F RT A20EU 2001120400050 20011204 00050 EU 2001 12 4 QXEA0102005 1 20011120 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AFT CARGO BAY FRAME 15205 CASTELLATION TIE IN TO BELLY SKIN BETWEEN STRINGER 1 AND 2 HAS CORROSION ON TOP SURFACE WITH POSSIBLE CRACK AT VERTICAL FLANGE. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6 AND SRM 51-10-04, PARAGRAPH 4 B AND C, PAGE 9. 2 L 7 2 4F RT A20EU 2001120400051 20011204 00051 EU 2001 12 4 QXEA0102006 1 20011120 A 5710 STRUCTURE FOKKER F28 F28MK4000 4990810 EU LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - STRUCTURE IS CHAFED AT LOWER ATTACH POINT FOR LT WING ROOT FAIRING 91J. REPAIRED IAW HORIZON AIR EA 4-57-569. 2 L 7 2 4F RT A20EU 2001120400052 20011204 00052 EU 2001 12 4 QXEA0102007 1 20011114 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AFT CARGO BAY FRAME 14755 CORROSION TOP SURFACE AND UNDERSIDE OF TOP FLANGE AT STRINGER 72. REPAIRED IAW FOKKER S RM 53-01-01 AND SRM 51-10-04, PARAGRAPH 4 B AND C, PAGE 9. 2 L 7 2 4F RT A20EU 2001120400053 20011204 00053 EU 2001 12 4 QXEA0102008 1 20011119 A 5311 DOUBLER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 11905 RT COLD SLEEVE REPAIR PLATE HAS 10/32 SCREW CHAFE DAMAGE AT .023 DEEP. REPAIRED IAW HORIZON AIR EA 4- 53-1523. 2 L 7 2 4F RT A20EU 2001120400054 20011204 00054 EU 2001 12 4 QXEA0102009 1 20011118 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CLIP CONNECTING LOWER WING TO FUSELAGE FAIRING SUPPORT AT FRAME 13815A AND CENTER RIB IS CRACKED. REPAIRED IAW FO KKER SRM 53-53-04, FIGURE 5, ITEM 190, SRM 51-30-01. 2 L 7 2 4F RT A20EU 2001120400055 20011204 00055 EA 2001 12 4 QXEA0102010 1 20011128 A 2120 SMOKE CNDAIR CL600 CL6002C10 EA COCKPIT DETECTED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 602QX 10010 BOI- DURING DEICING, AIRCRAFT CABIN AND COCKPIT FILLED WITH SMOKE. INSPECTED APU INTAKES. NO DEFECTS NOTED. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2001120400056 20011204 00056 EU 2001 12 4 QXEA0102011 1 20011114 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AFT CARGO BAY FRAME 14755 HAS CORROSION ON TOP SURFACE AND UNDER SIDE OF TOP FLANGE AT STRINGER 3. REPAIRED IAW F OKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2001120400057 20011204 00057 EU 2001 12 4 QXEA0102012 1 20011127 A 5720 SHIM FOKKER F28 F28MK4000 4990810 EU LT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT WING FUEL ACCESS APERTURE 71A, SHIM HAS BEEN BLENDED COMPLETELY THROUGH AT SEVERAL SCREW HOLES. REPAIRED IAW H ORIZON AIR EA 4-57-568. 2 L 7 2 4F RT A20EU 2001120400058 20011204 00058 EA 2001 12 4 QXEA0102013 1 20011130 A 2810 79888211 PANEL CNDAIR CL600 CL6002C10 EA FUSELAGE DEFECTIVE A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 606QX 10023 GEG- FUELER REPORTED ELECTRICAL SMELL COMING FROM REFUEL/DEFUEL PANEL. REMOVED AND REPLACED REFUEL/DEFUEL PANEL. OPERA TIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2001120400059 20011204 00059 SO 2001 12 4 RAIA00111013 1 20011118 A 3412 102AU1AF PROBE EMB 145 EMB145 3260210 SO TAT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 804HK 8147 493 145082 5293-STL-NUMBER ONE TOTAL AIR TEMP FAILED DURING TAXI. MAINTENANCE REMOVED AND REPLACED NR 1 TAT PROBE. 2 L 7 2 4F RT T00011AT 2001120400060 20011204 00060 EU 2001 12 4 RAIA00111014 1 20011120 A 3397 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN DISCONNECTED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 555HK 41072 MX - STL - DURING PRE-FLIGHT FOUND PATH LIGHTING INOP ROWS 2-5. RECONNECTED PATH LIGHTING ELECTRICAL CONNECTOR AT SEAT 5A IAW J41 MAINTENANCE MANUAL. 2 L 7 2 4T RT A41NM 2001120400061 20011204 00061 EU 2001 12 4 RAIA00111016 1 20011126 A 3397 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 556HK 41073 MX-STL- DURING PREFLIGHT FOUND SOME ESCAPE PATH LIGHTS INOPERATIVE. RESECURED CONNECTOR AT FLOOR TRACK PATH LIGHTS OPS OK IAW J41 MAINTENANCE MANUAL. 2 L 7 2 4T RT A41NM 2001120400062 20011204 00062 NM 2001 12 4 01FDEA01025 1 20011204 A 3230 SOLENOID BOEING 727 727233 138408A NM LG CONTROL LEVER INOPERATIVE A FDEA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SO 25 221FE 20932 1-386 AFT T/O LG HANDLE WOULD NOT RAISE PAST OFF POS. R&R LG CONTROL LEVER SOLENOID PER MM 32-31-016-4. 2 L 7 3 4F RT A3WE 2001120400063 20011204 00063 SO 2001 12 4 RAIA00111017 1 20011126 A 3397 CONNECTOR EMB 145 EMB145 3260210 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 803HK 145077 MX-STL- DURING PREFLIGHT FOUND AFT SECTION OF FLOOR EMERGENCY EXIT LIGHTS INOP. RESECURED CANNON PLUG AT NR 4 EMERGENCY LIGHT POWER SUPPLY; OPS CK GOOD IAW EMB 145 MAINTENANCE MANUAL. 2 L 7 2 4F RT T00011AT 2001120400064 20011204 00064 EU 2001 12 4 RAIA00111018 1 20011127 A 3397 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 551HK 41040 DURING PREFLIGHT FOUND FLOOR PATH LIGHTS OUT AT ROWS 8, 9, & 10. RESECURED EMERGENCY PATH LIGHTING CONNECTOR AT SEAT 8A ; OPS CHECK OK YAW J41 MAINTENANCE MANUAL. 2 L 7 2 4T RT A41NM 2001120400067 20011204 00067 EA 2001 12 4 SWIA200110365 1 20011113 A 5270 PROXIMITY SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE PAX DOOR OUT OF ADJ A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 594SW 7285 PAX DOOR OUTER HANDLE CAUTION - WOULD NOT GO OUT PER QRH PROCEDURE, DID EXTINGUISH ON DESCENT. RETURNED TO RNO. INSPECT ED PASSENGER DOOR PER 52-70-04, CHECKS NORMAL. INSPECTED AND FOUND DOOR TO BE SECURE. PROBLEM IS INDICATION ONLY. ADJ USTED PASSENGER DOOR OUTER HANDLE PROXIMITY SWITCH IAW RJ MM 52-70-04. SYSTEM OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2001120400068 20011204 00068 EU 2001 12 4 2001F00686 1 20011025 A 3320 6500006 LIGHT SAAB SF340 340B 7860101 EU CABIN SHORTED A CX7A H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 03 305CE 340B202 DURING FLIGHT, FLIGHT ATTENDANT SMELLED A STRONG ODOR OF BURNING RUBBER. FIRST OFFICER CONCURRED AND SAID IT WS LOCATED AROUND ROW 5. FLIGHT ATTENDANT TURNED OFF ALL LIGHTS AND SMELL DISSIPATED. (M) 2 L 7 2 4T RT A52EU 2001120400075 20011204 00075 NM 2001 12 4 AUS20011040 1 20010912 A 3232 731412 HOUSING BOEING 727 72777C 1380420 NM PWA JT8 JT8D15 52051 NE MLG DOOR ACT CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 AU S 249 (AUS) MAIN LANDING GEAR DOOR ACTUATOR LOWER BODY HOUSING CRACKED. LOSS OF HYDRAULIC FLUID. 2 L 7 3 4F 4 F A3WE E2EA 2001120400077 20011204 00077 WP 2001 12 4 AUS20011044 1 20010930 A 2910 511258235 LINE DOUG DC3 DC3CS1C3G 3021458 WP PWA R1830 R183092 52020 NE HAMSTD 23E 23E50 NE HYD INDICATOR CRACKED W O OTHER K FLUID LOSS NR NOT REPORTED 1 AU S (AUS) LANDING GEAR HYDRAULIC DOWNLINE, PRESSURE SIGNAL LINE FLARE IS CRACKED AT ATTACHMENT TO PRESSURE GAUGE. 2 L 7 2 4R 4 R A669 5E4 6 C P603 2001120400079 20011204 00079 NM 2001 12 4 AUS20011052 1 20011005 A 3246 BOLT BOEING 737 737476 NM CFMINT CFM56 CFM563C 13802 EU MLG WHEEL BROKEN W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LT OUTBOARD MAIN WHEEL TIE BOLTS (5OFF) BROKEN. TIRE DEFLATED AND BRAKE DAMAGED. 2 L 7 2 4F 4 F RT A16WE E21EU 2001120400081 20011204 00081 EU 2001 12 4 AUS20011054 1 20010930 A 2130 D73208425 LINE FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAY62015 04564 NE CABIN PRESSURE FAILED W O OTHER O OTHER CL CLIMB 1 AU S (AUS) PRESSURISATION SYSTEM PRIMARY OUTFLOW VALVE SENSE LINE FROM THE MANUAL CONTROL TO THE SENSE PANEL IS CORRODED INTE RNALLY CAUSING THE LINE TO SPLIT. 2 L 7 2 4F 4 F RT E25NE 2001120400084 20011204 00084 NM 2001 12 4 AUS20011068 1 20011003 A 3260 PROXIMITY SENSOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE MLG FAULTY W O OTHER N FALSE WARNING CL CLIMB 1 AU S (AUS) LT MAIN LANDING GEAR DOOR WARNING SYSTEM PROXIMITY SENSOR FAULTY. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001120400085 20011204 00085 SO 2001 12 4 AUS20011069 1 20011008 A 5751 120179313233005 BALANCE WEIGHT EMB 120 EMB120 3260201 SO PWA 118 PW118A NE HAMSTD 14SF 14SF9 NE AILERONS CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LT AND RT AILERON INBOARD, CENTRE AND OUTBOARD BALANCE WEIGHTS CORRODED. FOUND DURING INSPECTION IAW AD/EMB120/24 PT2. (SB 120-27-077 PT2). 2 L 7 2 4T 4 T RT A31SO E20NE 6 N P11NE 2001120400086 20011204 00086 SO 2001 12 4 AUS20011070 1 20011008 A 5751 120179313233005 BALANCE WEIGHT EMB 120 EMB120 3260201 SO PWA 118 PW118A NE HAMSTD 14SF 14SF9 NE AILERONS CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LT AND RT AILERON INBOARD, CENTRE AND OUTBOARD BALANCE WEIGHTS CORRODED. FOUND DURING INSPECTION IAW AD/EMB120/24 PT2. (SB 120-27-077 PT2). 2 L 7 2 4T 4 T RT A31SO E20NE 6 N P11NE 2001120400087 20011204 00087 SO 2001 12 4 AUS20011071 1 20011008 A 5751 120179313233005 BALANCE WEIGHT EMB 120 EMB120 3260201 SO PWA 118 PW118 NE HAMSTD 14SF 14SF9 NE AILERONS CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LT AND RT AILERON INBOARD, CENTRE AND OUTBOARD BALANCE WEIGHTS CORRODED. FOUND DURING INSPECTION IAW AD/EMB120/24 PT2. (SB 120-27-077 PT2). 2 L 7 2 4T 4 T RT A31SO E20NE 6 N P11NE 2001120400088 20011204 00088 NM 2001 12 4 AUS20011074 1 20011014 A 3230 696603 VALVE BOEING 737 737476 NM CFMINT CFM56 CFM563C 13802 EU MLG FAULTY W O OTHER O OTHER DE DESCENT 1 AU S 884 (AUS) LANDING GEAR TRANSFER VALVE FAULTY. 2 L 7 2 4F 4 F RT A16WE E21EU 2001120400101 20011204 00101 SO 2001 12 4 AUS20011115 1 20011018 A 2750 FLAP EMB 120 EMB120 3260201 SO PWA 118 PW118A NE HAMSTD 14SF 14SF9 NE TRAILING EDGE FL FAULTY W K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 AU S (AUS) AIRCRAFT EXPERIENCED FLAP ASYMMETRIC FAULT. INVESTIGATION COULD FIND NO CAUSE FOR THE DEFECT. 2 L 7 2 4T 4 T RT A31SO E20NE 6 N P11NE 2001120400108 20011204 00108 NM 2001 12 4 AUS20011141 1 20011018 A 2910 7972129508 PIPE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE HYDRAULIC SYSTEM LEAKING W O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 AU S (AUS) RT HYDRAULIC SYSTEM PRESSURE PIPE FAILED AT A BRAZED FITTING LOCATED INBOARD OF THE RT PRESSURE BULKHEAD TO PYLON. 2 L 7 2 4F 4 F TR A6WE E00061EN 2001120400114 20011204 00114 NM 2001 12 4 AUS20011162 1 20011103 A 3230 AE246163E0192 HOSE BOEING 737 7373Q8 1384670 NM CFMINT CFM56 CFM563C 13802 EU LANDING GEAR RET LEAKING W D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 AU S (AUS) LT MAIN LANDING GEAR DOWNLOCK ACTUATOR HOSE LEAKING. LOSS OF HYDRAULIC FLUID. 2 L 7 2 4F 4 F RT A16WE E21EU 2001120400116 20011204 00116 NM 2001 12 4 AUS20011166 1 20011105 A 2761 654456115 ACTUATOR BOEING 737 737376 NM CFMINT CFM56 CFM563C 13802 EU SPOILER FAULTY W O OTHER F FLT CONT AFFECTED DE DESCENT 1 AU S 4300 (AUS) LT NR 2 SPOILER ACTUATOR FAULTY. ACTUATOR WOULD OSCILLATE WHEN A LOAD WAS APPLIED TO THE SPOILER TRAILING EDGE. 2 L 7 2 4F 4 F RT A16WE E21EU 2001120400118 20011204 00118 NM 2001 12 4 AUS20011172 1 20011107 A 5247 ACTUATOR BOEING 767 767238 1385114 NM PWA JT9 JT9D7R4E 52054 NE APU DOORS FAULTY W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) APU DOOR ACTUATOR FAULTY. 2 L 7 2 4F 4 F RT A1NM E3NE 2001120400122 20011204 00122 NM 2001 12 4 AUS20011179 1 20011108 A 3230 BACH8A06EE0250T LINE BOEING 737 737376 NM CFMINT CFM56 CFM563C 13802 EU MLG LEAKING W O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 AU S (AUS) LT MAIN LANDING GEAR ACTUATOR FORWARD HYDRAULIC LINE LEAKING. LOSS OF HYDRAULIC SYSTEM "A" HYDRAULIC FLUID. 2 L 7 2 4F 4 F RT A16WE E21EU 2001120400123 20011204 00123 SO 2001 12 4 AUS20011180 1 20011108 A 5330 12017417021 SKIN EMB 2024T363 EMB 120 EMB120 3260201 SO PWA 118 PW118A NE HAMSTD 14SF 14SF9 NE FUSELAGE CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) AFT FUSELAGE LOWER SKIN CORRODED IN AREA OF SUB ZONE 250 BETWEEN BS 13255 AND BS 13630. AREA OF CORROSION APPROXIM ATELY 645.16SQMM (10SQIN). EVIDENCE OF SOME SMALL PIN HOLES. 2 L 7 2 4T 4 T RT A31SO E20NE 6 N P11NE 2001120400126 20011204 00126 NM 2001 12 4 AUS20011185 1 20011104 A 2750 MS2764816 BEARING HAMSTD 734382E DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE HAMSTD 14SF 14SF23 NE TE FLAPS SEIZED W K NONE O OTHER IN INSP/MAINT 1 AU S 2115 (AUS) LT WING FLAP DRIVE TORQUE TUBE ASSEMBLY BEARING SEIZED BETWEEN INNER AND OUTER RACES AND ALSO IN THE BEARING RETAI NER ASSEMBLY PNO 720534A. THE SHAFT PNO 741156A HAD BEEN TURNING INSIDE THE INNER RACE AND HAD WORN ENOUGH TO LET THE TE NSION OFF THE BEARING RETAINING NUT. THE NUT WAS STILL LOCKED IN POSITION BY THE KEYED RETAINING WASHER. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001120400128 20011204 00128 NM 2001 12 4 AUS20011189 1 20011111 A 2530 GENM2585015 OVEN BOEING 737 737476 NM CFMINT CFM56 CFM563C 13802 EU GALLEY FAILED W F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AU S (AUS) STRONG ELECTRICAL SMELL AND SMOKE COMING FROM OVEN. BURN MARKS EVIDENT AT ENTRY TO FAN MOTOR. FIRE EXTINGUISHER U SED. 2 L 7 2 4F 4 F RT A16WE E21EU 2001120400129 20011204 00129 NM 2001 12 4 AUS20011191 1 20011023 A 5313 STRINGER BOEING 737 737376 NM CFMINT CFM56 CFM563C 13802 EU FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) STRINGER 17 RT CONTAINED CRACKS IN THE AREA OF BS 178. FOUND DURINGEDDY CURRENT INSPECTION. 2 L 7 2 4F 4 F RT A16WE E21EU 2001120400130 20011204 00130 NM 2001 12 4 AUS20011192 1 20011030 A 1430 BOLT BOEING 737 737376 NM CFMINT CFM56 CFM563C 13802 EU FUSELAGE FAULTY W K NONE L NO TEST IN INSP/MAINT 1 AU S (AUS) AFT PRESSURE BULKHEAD BOLTS FAILED SPECIFIED TORQUE TESTS. TEST NR 1 - BOLTS FAILED 59. TEST NR 2 - BOLTS FAILED 224. FOUND DURING INSPECTION IAW BSB 737-53-1229. 2 L 7 2 4F 4 F RT A16WE E21EU 2001120400131 20011204 00131 NM 2001 12 4 AUS20011194 1 20011107 A 3260 PSEU DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE MLG FAULTY W O OTHER N FALSE WARNING DE DESCENT 1 AU S (AUS) LANDING GEAR PROXIMITY SENSOR ELECTRONIC UNIT (PSEU) FAULTY. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001120400133 20011204 00133 2001 12 4 AUS20011196 4 20011108 A 2210 7003652611 PANEL HONEYWELL SPZ8000 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE AUTOPILOT SYSTEM FAULTY W O OTHER F FLT CONT AFFECTED CR CRUISE 1 AU S (AUS) AUTOFLIGHT CONTROL SYSTEM (AFCS) CONTROL PANEL FAULTY. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001120400135 20011204 00135 NM 2001 12 4 AUS20011198 1 20011102 A 5754 65162251 HINGE BOEING 65162251 BOEING 727 72777C 1380420 NM PWA JT8 JT8D15 52051 NE LE FLAPS FAILED W O OTHER F FLT CONT AFFECTED LD LANDING 1 AU S 57969 BN796 (AUS) NR 3 LEADING EDGE FLAP ACTUATOR HINGE FAILED. 2 L 7 3 4F 4 F A3WE E2EA 2001120400138 20011204 00138 NM 2001 12 4 AUS20011204 1 20011031 A 2750 113T22526 FITTING BOEING 767 767238 1385114 NM PWA JT9 JT9D7R4E 52054 NE TE FLAPS CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LT AND RT INBOARD FLAP TORQUE TUBE SPLINES AND COLLAR FITTINGS CORRODED. FOUND DURING INSPECTION IAW AD/B767/108. 2 L 7 2 4F 4 F RT A1NM E3NE 2001120400140 20011204 00140 NM 2001 12 4 AUS20011208 1 20011108 A 2434 97636598 GENERATOR BOEING 727 727277 138408S NM PWA JT8 JT8D15 52051 NE DC GENERATOR-ALT FAILED W O OTHER H ELECT. POWER LOSS-50 PC DE DESCENT 1 AU S 4540 (AUS) NR 2 GENERATOR STATOR RETAINING SCREW HEAD SHEARED. 2 L 7 3 4F 4 F RT A3WE E2EA 2001120400141 20011204 00141 NM 2001 12 4 AUS20011210 1 20011114 A 7931 8D1437 PRESSURE SWITCH CUSTOMCOMP 8D1437 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE ENGINE OIL FAILED W O OTHER E K J VIBRATION/BUFFET FLUID LOSS WARNING INDICATION CL CLIMB 1 AU S 044 (AUS) NR 2 ENGINE OIL PRESSURE WARNING LIGHT PRESSURE SWITCH FAILED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001120400147 20011204 00147 NE 2001 12 4 AUS20011223 2 20011119 A 7230 9074M74G38 STRUT GE CF680A BOEING 767 767277 1385128 NM GE CF6 CF680A 30025 NE COMPRESSOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S 35315 (AUS) ENGINE FAN MODULE NR 9 FAN FRAME STRUT CRACKED PARALLEL TO THE WELD LINE AT THE INNER RADIAL END OF THE STRUT ADJA CENT TO THE SUMP HOUSING. 2 L 7 2 4F 4 F RT A1NM E13NE 2001120400150 20011204 00150 NM 2001 12 4 AUS20011233 1 20011121 A 3230 LANDING GEAR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE MAIN MALFUNCTIONED W O OTHER J WARNING INDICATION DE DESCENT 1 AU S (AUS) LANDING GEAR WOULD NOT LOCK DOWN. LANDING GEAR DOORS CYCLING OPEN AND CLOSED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001120400151 20011204 00151 NE 2001 12 4 AUS20011235 2 20011119 A 7310 LP3038454 FILTER PWA PW123D DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE HAMSTD 14SF 14SF23 NE ENGINE FUEL CONTAMINATED W O OTHER E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 AU S 201 (AUS) NR 2 LOW PRESSURE FUEL FILTER CONTAMINATED BY A SMALL AMOUNT OF FOREIGN MATERIAL. FILTER BYPASS LIGHT ILLUMINATED . 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001120400159 20011204 00159 NE 2001 12 4 AUS20011248 2 20011127 A 7230 JT9D7R4E FAN BLADE PWA JT9D7R4E BOEING 767 767238 1385114 NM PWA JT9 JT9D7R4E 52054 NE COMPRESSOR FAILED W A UNSCHED LANDING E B VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 AU S 5597 P716610 (AUS) LT ENGINE FAN BLADE FAILED. BLADE EXITED THROUGH COWL. 2 L 7 2 4F 4 F RT A1NM E3NE 2001120400167 20011204 00167 WP 2001 12 4 MWEA011468 1 20011204 A 5320 9910078677 CHANNEL DOUG DC9 DC915 3022036 WP STATION 200 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 FLOOR SUPPORT CHANNEL CORRODED ON UNDER SIDE AT 3 MOST INBOARD FASTENER HOLES AND INBOARD END AT STATION 200 AND OUTBOAR D OF SEAT TRACK, #4 -- REMOVED, FABRICATED AND INSTALLED FLOOR SUPPORT CHANNEL. 2 L 7 2 4F A6WE 2001120400168 20011204 00168 WP 2001 12 4 MWEA011469 1 20011204 A 5710 591000644 ANGLE DOUG DC9 DC915 3022036 WP LONG. 22&23 R CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 RIGHT WING - FORWARD LOWER WING TO FUSELAGE ATTACH ANGLE UPPER FLANGE IS CRACKED BETWEEN LONGERON 22 AND 23 RIGHT -- R EMOVED CRACKED ANGLE. LOCATED AND INSTALLED NEW ANGLE. 2 L 7 2 4F A6WE 2001120400171 20011204 00171 EU 2001 12 4 2001F00687 1 20011013 A 2612 WARNING SYSTEM SAAB SF340 340B 7860101 EU RT ENGINE MALFUNCTIONED A CX7A O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 03 306CE 340B203 TAILPIPE HOT RIGHT ENGINE ILLUMINATED AT 100 KTS. REMOVED TAIL COWLING NACELLE, CLEANED AND INSPECTED WIRE CONNECTION. PERFORMED ENGINE RUNUP. NO DEFECTS NOTED AT THIS TIME. (M) 2 L 7 2 4T RT A52EU 2001120400173 20011204 00173 2001 12 4 COMA0110159 4 20011203 A 2210 GYRO EMB 120 EMB120RT 3260202 SO A COMA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 SO 01 463CA 120267 FLIGHT #5049 - AFTER T/O, RED FD FLAP ON PILOTS AND COPILOTS EADI.COULD NOT DUPLICATE. SYSTEM TEST WAS NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 2001120400175 20011204 00175 SO 2001 12 4 COMA0110160 1 20011201 A 7603 POWER LEVER EMB 120 EMB120RT 3260202 SO A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 269CA 120263 FLIGHT #5056. POWER LEVER SPLIT DURING T/O.POWER LEVER SPLIT WITHIN LIMITS. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 2001120400176 20011204 00176 2001 12 4 2001F00688 4 20011023 A 6122 89741016 GOVERNOR FRCHLD SA227 SA227DC 3377521 SW NR 1 ENGINE FAILED A I7WA O OTHER J WARNING INDICATION CR CRUISE 1 NM 05 885ML 1347 DC885B EWR - FLT 8133 - LARGE TORQUE FLUCTUATIONS ON NR 1 ENGINE. REPLACED UNIT, SENT OUT SOAP SAMPLE FLUSH ENGINE OIL SYSTEM. FAILED PROP GOVERNOR. (M) 2 L 7 2 4T RT A18SW 2001120400181 20011204 00181 NE 2001 12 4 2001F00706 2 20011119 A 7200 ENGINE BOEING 737 737201 1384454 NM PWA JT8 JT8D15A 52051 NE RIGHT FAILED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING F J B FLT CONT AFFECTED WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 262AU 22868 709096 MIA-BWI - FLT 2738 - DURING CRUISE, THE FLIGHT CREW HEARD A LOUD BANG AND THE AIRCRAFT YAWED. THE RIGHT ENGINE N1 AND N 2 DIMINISHED AND THE EGT CLIMBED ABOVE THE RED LINE. THE ENGINE SPOOLED DOWN AS THE CREW INITIATED SHUTDOWN PROCEDURES. A PASSENGER REPORTED SPARKS OUT THE TAILPIPE. THE AIRCRAFT DIVERTED TO CLT AND LANDED WITHOUT INCIDENT. 19 MINUTES S INGLE ENGINE TIME. (M) 2 L 7 2 4F 4 F A16WE E2EA 2001120400182 20011204 00182 EA 2001 12 4 2001F00707 1 20011111 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 37342 7342 FLT 5772 - CLT-LIT - DURING PREFLIGHT, THE CREW REPORTED THE PAX DOOR WAS HARD TO CLOSE. MAINTENANCE LUBED THE ENTIRE D OOR. OPS CHECKED GOOD AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001120400185 20011204 00185 SW 2001 12 4 2001F00710 1 20011011 A 2150 20475546 ACM SWRNGN SA227 SA227AC 8780603 SW A/C BAY FAILED A BSAA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 05 158MC AC726B LIGHT SMOKE STARTED TO FILL THE CABIN, CREW SHUT OFF BOTH BLEEDS RETURNED TO STATION. INITIALLY DEFERRED THE ACM PER TH E MEL, THEN REPLACED THE MEL. (M) 2 L 7 2 4T RT A8SW 2001120400187 20011204 00187 NM 2001 12 4 2001F00711 1 20011114 A 7810 JP55201 NOZZLE BOEING 757 75723N 1384973 NM NR 2 ENGINE CRACKED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 523AT 8281 30232 DURING A-CHECK, THE NR 2 ENGINE COMMON NOZZLE ASSY WAS FOUND CRACKED AT THE INBOARD HOIST ATTACH POINT. MAINTENANCE REP AIRED THE ASSY IAW AMTA ERA-757-78R-4616 AND ROLLS-ROYCE TECHNICAL VARIANCE DOCUMENT F37183. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A2NM 2001120400189 20011204 00189 NM 2001 12 4 P5CA0100616 1 20011123 A 5310 NONE WEB BOEING 747 747122 1384872 NM NOSE WHEEL WELL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NOSE WHEEL WELL VERTICAL BEAM INSPECTION IAW MA A5310-33:01 REVEALED A CRACK AT STANDOFF HOLE 2-3/8" LONG AT VERTICAL BEAM STN 320 R/H SIDE, WEB 2. CRACK REPAIRED IAW SRM 51-40-02, PAGE5, DETAIL 111. 2 L 7 4 4F A20WE 2001120400190 20011204 00190 NM 2001 12 4 P5CA0100617 1 20011123 A 5310 NONE WEB BOEING 747 747122 1384872 NM NOSE WHEEL WELL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NOSE WHEEL WELL VERTICAL BEAM INSPECTION IAW MA A5310-33:01 REVEALED A CRACK 1-3/8" LONG AT WEB TO CHORD FASTENER LOCATI ON AT VERTICAL BEAM STN 320 R/H SIDE, WEB 2. REPAIRED IAW SRM 51-40-02, PAGE 5, DETAIL 111. 2 L 7 4 4F A20WE 2001120400191 20011204 00191 NM 2001 12 4 2001F00712 1 20011114 A 7810 JP55201 NOZZLE BOEING 757 75723N 1384973 NM NR 1 ENGINE CRACKED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 522AT 11387 29330 DURING ROUTINE MAINTENANCE AT MDW, THE NR 1 ENGINE COMMON NOZZLE ASSY WAS FOUND TO BE CRACKED AT BOTH INBOARD AND OUTBOA RD HOIST ATTACH POINTS. MAINTENANCE REMOVED AND REPLACED THE NOZZLE ASSY. (M) 2 L 7 2 4F RT A2NM 2001120400193 20011204 00193 NM 2001 12 4 2001F00713 1 20011114 A 7810 JP55201 NOZZLE BOEING 757 75723N 1384973 NM NR 1 ENGINE CRACKED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 523AT 30232 DURING A-CHECK, THE NR 1 ENGINE COMMON NOZZLE ASSY WAS FOUND CRACKED AT BOTH THE INBOARD AND OUTBOARD HOIST ATTACH POINT S. MAINTENANCE REMOVED AND REPLACED THE NOZZLE ASSY. (M) 2 L 7 2 4F RT A2NM 2001120400195 20011204 00195 WP 2001 12 4 AALA016085 1 20011114 A 8012 39279621 START VALVE DOUG DC9 DC983 3022083 WP RT ENGINE FAILED A AALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 21 836RA 53046 RIGHT START VALVE OPEN LIGHT CAME ON IN FLIGHT, PASSING 16,000 FT ABOUT 10 MINUTES AFTER TAKEOFF. REMOVED AND REPLACED RIGHT ENGINE START VALVE IAW MD MM 80-10-02. OPS CHECKED GOOD IAW MD80 MM 71-00-00 AND 81-10-02 PAGE 204 THROUGH 207. (M) 2 L 7 2 4F RT A6WE 2001120400196 20011204 00196 NE 2001 12 4 AALA016086 2 20011114 A 7200 ENGINE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE LEFT FAILED A AALA O OTHER J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 SW 21 754RA 49641 708175 DURING CLIMB-OUT, NOTED LEFT ENGINE OIL PRESSURE WENT TO ZERO, TEMP WAS 58, QUANTITY WAS 16 QUARTS, TEMPERATURE SLOWLY D ECREASED TO 40, HAD NO VIBRATIONS OR OTHER ABNORMAL INDICATIONS. ABOUT 10 MINUTES LATER LEFT ENGINE STARTED TO VIBRATE, IMMEDIATELY SHUT ENGINE DOWN, SHUTDOWN WAS NORMAL. ENGINE IS SCHEDULED FOR REMOVAL. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2001120400197 20011204 00197 NM 2001 12 4 BJNA011101 1 20011109 A 3350 60384431 BATTERY PACK BOEING 737 737214 138446R NM CABIN DEFECTIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 457TM 20156 RIGHT OVERWING EMERGENCY LIGHT BATTERY PACK CAUSES AN ELECTRIC DRAIN ON BATTERY WITH EMERGENCY LIGHT SWITCH OFF. REMOVE D AND REPLACED BATTERY PACK PER BMM 33-51-33. OPS CHECK NORMAL. (M) 2 L 7 2 4F A16WE 2001120400198 20011204 00198 NE 2001 12 4 COMA0160938 2 20011129 A 7261 4028T24P01 INSERT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE ENGINE LOOSE A COMA E A ENGINE SHUTDOWN UNSCHED LANDING K Y J FLUID LOSS ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SO 01 798CA 7348 807593 FLIGHT #5639 - LEFT ENGINE OIL PRESSURE WARNING. IFSD FOUND ENGINE OIL FILTER INSERT LOOSE, TIGHTENED FILTER INSERT AND ACFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2001120400199 20011204 00199 NE 2001 12 4 COMA0160939 2 20011201 A 7260 5018T48P01 SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE ENGINE LEAKING A COMA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 SO 01 798CA 7348 807593 FLIGHT #5639. LEFT ENGINE OIL PRESSURE WARNING.REPLACED THE IDG AND STARTER DRIVE, CARBON SEALS. 2 L 7 2 4F 4 F RT A21EA E15NE 2001120400201 20011204 00201 NM 2001 12 4 BJNA011102 1 20011112 A 3350 1691 LIGHT BOEING 737 737282 13844AT NM EXTERIOR INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 789TM 23046 L1 DOOR EMERGENCY EXTERIOR LIGHT INOPERATIVE. RELAMPED LIGHT, OPS CHECK NORMAL IAW 33-51-61. (M) 2 L 7 2 4F RT A16WE 2001120400202 20011204 00202 NM 2001 12 4 BJNA011104 1 20011113 A 7830 THRUST REVERSER BOEING 737 737282 13844AT NM PWA JT8 JT8D17A 52049 NE NR 2 ENGINE DAMAGED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 789TM 23046 709406 ON WALK AROUND, DISCOVERED 2 INCH BY 1 INCH HOLE IN SUPPRESSION MATERIAL OF ENGINE NR 2 THRUST REVERSER. PERFORMED FERR Y FLIGHT INSPECTION IAW WITH CASINO EXPRESS MPP CHAPTER 8-1, FOUND A/C OK FOR FERRY FLIGHT FROM CLT TO GSO. REMOVED AND REPLACED THRUST REVERSER. REMOVED NR 2 ENGINE AND INSTALLED ENGINE. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 2001120400203 20011204 00203 NM 2001 12 4 GAIA01316OP 1 20011119 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM L1 DOOR DEFECTIVE A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6831 20184 DURING ROUTINE MAINTENANCE AT DFW, IT WAS DISCOVERED THAT THE L1 EMERGENCY EXIT LIGHT WAS DIM. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001120400204 20011204 00204 2001 12 4 GTIA010847 4 20010903 A 3460 4034242934 CONTROL PANEL DOUG DC9 DC982 3022082 WP COCKPIT FAULTY A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 816NK 49140 FLL - FLT 139 - SPD/MACH BUTTON WILL NOT SWITCH WHEN PUSHED. REMOVED AND REPLACED FLIGHT GUIDANCE CONTROL PANEL. (M) 2 L 7 2 4F A6WE 2001120400205 20011204 00205 WP 2001 12 4 GTIA010927 1 20011004 A 2611 CGAB140001 SMOKE DETECTOR DOUG DC9 DC981 3022081 WP CARGO BAY FAULTY A GTIA K NONE N FALSE WARNING IN INSP/MAINT 1 GL 23 819NK 48016 RSW - CARGO DETECTION LOOP LIGHT ANNUNCIATOR ACCOMP BY SMOKE DETECTOR LOOP ILLUMINATED AT START FORWARD PIT. REMOVED AN D REPLACED FORWARD 'A' LOOP SMOKE DETECTOR. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2001120400206 20011204 00206 2001 12 4 GTIA010972 4 20011010 A 3460 4034241971 COMPUTER DOUG DC9 DC981 3022081 WP NR 1 FAULTY A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 818NK 48018 FLL - FLT 171 - AUTO THROTTLES WOULD NOT REMAIN ENGAGED WITH DFGC NR 1 SELECTED. WORKED NORMAL ON DFGC NR 2. REMOVED A ND REPLACED NR 1 DFGC RTS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2001120400207 20011204 00207 NE 2001 12 4 COMA0160940 2 20011129 A 7321 EEC CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE A COMA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 01 926CA 7027 FLIGHT #5553 LEFT ENGINE ROLLED BACK TO IDLE THRUST DURING CRUSIE FLIGHT - 7 MINUTES LATER POWER RETURNED TO NORMAL.DEF ERRED THE LEFT ENIGNE A.P.R. SYSTEM PER MEL. AIRCRAFT CONTINUED SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2001120400208 20011204 00208 2001 12 4 GTIA010978 4 20011016 A 2230 WIRE DOUG DC9 DC983 3022083 WP AUTOTHROTTLE SYS BROKEN A GTIA O OTHER O OTHER TO TAKEOFF 1 GL 23 814NK 49619 FLT 874 - LAX - AUTO THROTTLE INOPERATIVE ON TAKEOFF AND WOULD NOT ENGAGE. REPAIRED BROKEN WIRE AT 330-59 NR 4, AUTO TH ROTTLE SYSTEM, OPS CHECK GOOD. RTS ON BOTH NR 1 AND NR 2 CHECKED GOOD. (M) 2 L 7 2 4F RT A6WE 2001120400209 20011204 00209 2001 12 4 GTIA011012 4 20011017 A 3460 4034241971 COMPUTER DOUG DC9 DC982 3022082 WP NR 1 FAILED A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 823NK 48020 ACY - AUTO PILOT INOPERATIVE IN CMP NR 1. REMOVED AND REPLACED NR 1 DFGC, OPS CHECK NORMAL. (M) 2 L 7 2 4F A6WE 2001120400210 20011204 00210 2001 12 4 GTIA011016 4 20011019 A 3417 2587400436 ADC DOUG DC9 DC931 3022065 WP E/E BAY FAULTY A GTIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 GL 23 969ML 47268 MYR - FLT 619 - WHEN AUTOPILOT IN VERTICAL SPEED MODE AIRCRAFT CLIMBS 500 FPM MORE THAN SELECTED AND DESCENDS 500 FPM LE SS THAN SELECTED. REMOVED AND REPLACED NR 1 ADC, OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2001120400211 20011204 00211 EA 2001 12 4 COMA0160941 1 20011202 A 2740 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA VERT STAB MALFUNCTIONED A COMA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 963CA 3595 7127 FLIGHT #5011. STABILIZER TRIM INOP.REPLACED THE HORZ. STAB. TRIM ACTUATOR. 2 L 7 2 4F RT A21EA 2001120400212 20011204 00212 EA 2001 12 4 COMA0160942 1 20011202 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA R/H MALFUNCTIONED A COMA O OTHER O OTHER AP APPROACH 1 SO 01 915CA 1221 7013 FLIGHT #5528 - FLAPS FAILED WHEN SELECTED TO 20 DEGREES.REPALCED THE R/H BPSU. 2 L 7 2 4F RT A21EA 2001120400213 20011204 00213 WP 2001 12 4 GTIA011069 1 20011024 A 5753 FLAP DOUG DC9 DC982 3022082 WP LT WING DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 DTW - LEFT WING FLAP TRAILING EDGE DAMAGE. REMOVED DAMAGE SECTION OF LEFT WING FLAP TRAILING EDGE AND INSTALLED NEW SEC TION IAW MD-80 MM 57-30. (M) 2 L 7 2 4F A6WE 2001120400214 20011204 00214 EA 2001 12 4 COMA0160943 1 20011203 A 2130 10275B03C02 MODULE CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA B A EMER. DESCENT UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CR CRUISE 1 SO 01 924CA 15586 7026 FLIGHT #5625 - ACFT CABIN ALTITUDE EXCEEDED 10,000 FT AT FL 240.REPLACED THE CPAM. 2 L 7 2 4F RT A21EA 2001120400215 20011204 00215 WP 2001 12 4 GTIA011071 1 20011023 A 3397 CONNECTOR DOUG DC9 DC981 3022081 WP CABIN LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 819NK 48016 DTW - AFT OVERWING LEFT AND RIGHT EMERGENCY EXIT LIGHT INOPERATIVE. RESEATED CANNON PLUG AT BATTERY PACK, OPS CHECK GOO D ON EMERGENCY PATH LIGHTING PER MD80 MM 33-53-00. NO OTHER DISCREPANCIES NOTED. (M) 2 L 7 2 4F A6WE 2001120400216 20011204 00216 WP 2001 12 4 GTIA011073 1 20011022 A 3350 BATTERY PACK DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 805NK 48058 FLL - DURING DAILY CHECK, FOUND NUMEROUS EMERGENCY LIGHTS INOPERATIVE REF BATTERY PACKS AT STATIONS 211, 579, 731, 927 A ND TWO PACKS AT STATION 886, SEE WDM 33-51-01. REMOVED AND REPLACED BATTERIES AT PACK (B5-23) STATION 211, (B5-37) STAT ION 579 (B5-72) STATION 731, (B5-33) STATION 886 FORWARD, (B5-23) STATION 886 AFT AND STATION 927 (B5-73). ALL OPS NORM AL AS PER MM 33-53-00. (M) 2 L 7 2 4F A6WE 2001120400217 20011204 00217 2001 12 4 GTIA011076 4 20011029 A 2565 SLIDE DOUG DC9 DC981 3022081 WP L2 DOOR OUT OF POSITION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 FTW - L2 DOOR SLIDE FALLS OFF. INSTALLED SLIDER STOP IAW MD-80 MM 25-62-00. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2001120400218 20011204 00218 WP 2001 12 4 GTIA011080 1 20011017 A 5320 SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 FTW - AFT LOWER CARGO COMP, AFT CORNER CUTOUT DOOR AS MARKED. CORROSION FOUND ON LT SUPPORT. INSTALLED SUPPORT PER SRM MD-80 51-10-5. (M) 2 L 7 2 4F A6WE 2001120400219 20011204 00219 WP 2001 12 4 GTIA011083 1 20011010 A 5310 DOOR FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 FTW - FORWARD LOWER CARGO COMP, FORWARD SIDE OF LOWER DOOR JAMB CORRODED AT STATION 370 TO STATION 427. INBOARD FACE OF AREA FOUND TO BE OUT OF LIMITS IAW MD-80 SRM 53-01-00. CUT OUT DAMAGE SECTION OF PAN. INSTALLED ANGLES REPAIR AT FORW ARD AND AFT SECTION PER SRM MD-80 53-05. (M) 2 L 7 2 4F A6WE 2001120400222 20011204 00222 WP 2001 12 4 GTIA011085 1 20010905 A 5320 SPLICE DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 FTW - CENTER LOWER CARGO COMPARTMENT, L30 DOUBLER HAS CORRODED HIGH LOCK THROUGH THE HOLES AS MARKED. REMOVED CORRODED FASTENERS ON SPLICE. SPLICE OUT OF LIMITS. DUPLICATED SPLICE PER BOEING DC-9/MD-80 SRM 53-14-2. INSTALLED FWD SPLICE IAW MD-80 SRM 51-30-05. (M) 2 L 7 2 4F A6WE 2001120400224 20011204 00224 WP 2001 12 4 GTIA011086 1 20011018 A 5320 ATTACH FITTING DOUG DC9 DC981 3022081 WP FUSELAGE BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 FTW - AFT BAGGAGE BAY FS 1231 R28 LONGERON TITANIUM STRIP FOR FLOOR ATTACH, HOLE BROKEN OUT AFT SIDE OF FS 1230 FRAME. INSTALLED REPAIR DOUBLERS IAW MD-80 SRM 51-30-05. (M) 2 L 7 2 4F A6WE 2001120400225 20011204 00225 WP 2001 12 4 GTIA011087 1 20011015 A 5320 SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 FTW - SUPPORT ANGLE STATION 1155 BETWEEN LONGERON 27R AND 28R ATTACHED TO SKIN CORRODED. REMOVED SUPPORT ANGLE IAW MD-8 0 SRM 51-10-04. LOCATED AND DRILLED NEW SUPPORT ANGLE. INSTALLED SUPPORT ANGLE AT STATION 1155 BETWEEN LONGERON 27R AN D 28R. (M) 2 L 7 2 4F A6WE 2001120400226 20011204 00226 WP 2001 12 4 GTIA011088 1 20010904 A 5313 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 FTW - FOUND CENTER LOWER CARGO COMPARTMENT LONGERON 30, AT STATION 636 TO STATION 617 HAS CORROSION AS MARKED. REMOVED LONGERON SECTION. FABRICATED AND INSTALLED LONGERON IAW MD-80 51-30-5. (M) 2 L 7 2 4F A6WE 2001120400227 20011204 00227 WP 2001 12 4 GTIA011089 1 20010911 A 5310 DOOR FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 FTW - AFT LOWER CARGO COMPARTMENT FORWARD SIDE OF LOWER DOOR CORRODED FROM STATION 1155 TO 1212 AS MARKED. CORRODED OUT OF LIMITS AT LOWER CARGO DOOR JAMB. REMOVED CARGO DOOR JAMB BEAM. LOCATED AND DRILLED HOLES CARGO DOOR JAMB BEAM. IN STALLED LOWER CARGO COMP JAMB BEAM PER SRM MD-80 SRM 51-30-05. (M) 2 L 7 2 4F A6WE 2001120400228 20011204 00228 WP 2001 12 4 GTIA011090 1 20011101 A 7603 THROTTLE DOUG DC9 DC983 3022083 WP COCKPIT LACK OF LUBE A GTIA O OTHER O OTHER DE DESCENT 1 GL 23 808NK 49504 LAX - DURING APPROACH AND DESCENT, THE RIGHT THROTTLE WOULD NOT ADVANCE FROM ITS IDLE STOP, ONCE THE RIGHT THROTTLE WAS MOVED FORWARD OFF TAIL STOP IT WOULD ADVANCE AND MATCH THE LEFT. CLEANED AND LUBED THROTTLES. PLACARD REMOVED. (M) 2 L 7 2 4F RT A6WE 2001120400229 20011204 00229 WP 2001 12 4 GTIA011091 1 20011101 A 3350 60030431 BATTERY PACK DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 FLL - EMERGENCY CEILING LIGHTS BETWEEN SEATS 16/18 ILLUMINATE WHEN A/C ELECTRICAL POWER REMOVED FROM A/C. REMOVED BATTE RY FROM PACK AT STATION 731R. REMOVED AND REPLACED BATTERY PACK AND BATTERIES, IAW MM 33-53-00. OPS CHECK OK. (M) 2 L 7 2 4F A6WE 2001120400230 20011204 00230 NM 2001 12 4 AWXA200100610 1 20011130 A 3350 BMS13311122 WIRE BOEING 737 7373S3 1384711 NM SEAT ROW 17 DETACHED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 YVR - EEL - "C" - DURING C-15 CHECK DISCOVERED BLACK WIRE PULLED OUT OF SPLICE IN FLOOR CONDUIT ON L/H SEAT MOUNTED ESCA PE PATH LIGHTING SEAT ROW 17. MAINTENANCE RE-SPLICED WIRE PER STANDARD WIRING PRACTICES MANUAL 20-30-12, PG. 3. 2 L 7 2 4F RT A16WE 2001120400231 20011204 00231 EU 2001 12 4 AWXA200100613 1 20011130 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU ZONE 263 DEFECTIVE A AWXA K NONE O OTHER UK UNKNOWN 1 WP 28 621AW 053 LAS - EEL - FLT 0116 - "C" - CAPTAIN REPORTED L2 AND R2 EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED POWER SU PPLY 13WL IAW AMM 33-51-38, OPERATIONALLY CHECKED GOOD. 2 L 7 2 4F RT A28NM 2001120400232 20011204 00232 WP 2001 12 4 HALA0100248 1 20011010 A 2460 RCCB DOUG DC10 DC1030 3023501 WP ELECTRICAL SYS FAILED A HALA O OTHER H ELECT. POWER LOSS-50 PC CR CRUISE 1 WP 13 12061 47851 LAX - FLT 32 - AIR DIVERSION AT 3 HOURS INTO FLIGHT, LT EMERGENCY AC BUS OFF LIGHT ILLUMINATED, RESTORED SYSTEM. FOLLOW ED CHECKLIST, 5 MINUTES LATER PROBLEM REOCCURRED. NR 1 GALLEY POWER OFF LIGHT ILLUMINATED. COULD NOT RESTORE POWER BY RESETTING, REMAINED OFF FOR ENTIRE FLIGHT. REPLACED RCCB B1-136. RAN ENGINE GEN AND APU AND EXIT POWER ALL OPERATION A ND INDICATION NORMAL. (M) 2 L 7 3 4F A22WE 2001120400233 20011204 00233 2001 12 4 HALA0100263 4 20011119 A 3417 ADC DOUG DC10 DC1010 3022110 WP COCKPIT FAILED A HALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 13 127AA 46948 ATO - ON TAKEOFF ROLL, FIRST OFFICERS AIRSPEED INDICATOR INDICATED 0 AIRSPEED, ABORTED TAKEOFF. REMOVED AND REPLACED CA DC, OPS AND LEAK CHECK GOOD. SECOND BLOCK TURNBACK DUE TO NO AIRSPEED INDICATION. FOUND DEBRIS IN FIRST OFFICERS PITOT TUBE. (M) 2 L 7 3 4F A22WE 2001120400234 20011204 00234 EU 2001 12 4 SIMA200129005 1 20011016 A 3350 3012000 BATTERY PACK AEROSP ATR72 ATR72212 8680945 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 274AT 274 MIA - FORWARD OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK/POWER SUPPLY IAW ATR72 AMM. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001120400235 20011204 00235 EU 2001 12 4 SIMA200129008 1 20011017 A 3350 301307 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 540AM 540 SGF - AFT SECTION OF EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT 73WL IAW ATR 7 2 AMM. OPERATIONALLY CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001120400236 20011204 00236 NM 2001 12 4 TSAA0153154 1 20011115 A 5330 6957743 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 817AL 39735 DISCOVERED BULGING AT BS 1088, S-20R FUSELAGE SKIN. REMOVED THE CORRODED PORTION OF THE STRAP, FABRICATED AND INSTALLED REPAIR DOUBLER AND TRIPLER. RECEIVED 8110-3 APPROVAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001120400237 20011204 00237 NM 2001 12 4 USAABB01054 1 20010701 A 7920 MANIFOLD BOEING 767 7672B7 1385107 NM GE CF6 CF680C2B2 30025 NE LT ENGINE CLOGGED A USAA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 EA 19 652US 24765 695145 PHL - FLT 14, AFTER TAKEOFF, THE LEFT ENGINE WAS REPORTED TO HAVE LOST OIL PRESSURE AND THE N2 WAS AT 0 PERCENT. THE FL IGHT RETURNED TO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED ENGINE. ENGINE TEARDOWN REVEALED THAT THE OIL M ANIFOLD THAT FEEDS IN INLET GEARBOX (IGB) SPLINE AREA WAS CLOGGED. THE SPLINE DISINTEGRATED TO THE POINT WHERE THE HIGH PRESSURE COMPRESSOR ROTOR DISCONNECTED FROM THE IGB. ONCE IGB ROTATION WAS LOST, THE TRANSFER GEARBOX AND ACCESSORY GE ARBOX (AGB) ALSO LOST ROTATION. THE AGB DRIVES THE FUEL, OIL AND ELECTRICAL POWER CONTROL SYSTEM FOR THE ENGINE. WITH THE LOSS OF THE AGB, THE ENGINE SHUT DOWN. (M) 2 L 7 2 4F 4 F RT A1NM E13NE 2001120400238 20011204 00238 NM 2001 12 4 USAABB01130 1 20011115 A 3350 20121 POWER SUPPLY BOEING 767 767201 1385125 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 649US 23901 PHL - FOUND RIGHT CENTER AND RIGHT AFT EXTERIOR OVERWING LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY (M73 1). (M) 2 L 7 2 4F RT A1NM 2001120400239 20011204 00239 NM 2001 12 4 USAABB01131 1 20011116 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 601AU 22193 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 13 AND 18 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2001120400240 20011204 00240 NM 2001 12 4 USAABB01132 1 20011116 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 625VJ 27246 PHL - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 1 AND 18 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2001120400241 20011204 00241 NM 2001 12 4 USAABB01133 1 20011118 A 3350 8731002511REV14 SIGN BOEING 757 757225 1384959 NM R3 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 600AU 22192 BDL - FOUND EXIT IDENTIFIER AT THE R3 DOOR INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2001120400242 20011204 00242 NM 2001 12 4 USAABB01134 1 20011118 A 3397 WIRE BOEING 767 7672B7 1385107 NM CABIN DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 651US 24764 CDG - FOUND FLOOR PROXIMITY LIGHTING INOPERATIVE AT ROWS 4 THROUGH 6. MAINTENANCE RECONNECTED THE WIRING AT ROW FOUR. (M) 2 L 7 2 4F RT A1NM 2001120400243 20011204 00243 EU 2001 12 4 USAAF01083 1 20011113 A 3350 6104789 POWER SUPPLY FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 851US 11278 CLT - A SECTION OF FLOOR EMERGENCY LIGHTS WAS INOPERATIVE. MAINTENANCE REPLACED A BATTERY POWER SUPPLY UNIT. (M) 2 L 7 2 4F RT 2001120400244 20011204 00244 NM 2001 12 4 USAASB01253 1 20010915 A 3350 20131A BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 342US 23511 DCA - MAINTENANCE FOUND THE FORWARD EMERGENCY LIGHTS AND THE L1 DOOR EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND RE PLACED THE FORWARD EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001120400245 20011204 00245 NM 2001 12 4 USAASB01257 1 20010916 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 397US 23319 IAD - MAINTENANCE FOUND SIX SEAT MOUNTED EMERGENCY LIGHTS, IN THE AFT CABIN, WOULD NOT ILLUMINATE WHEN TESTED. MAINTENA NCE REMOVED AND REPLACED THE AFT EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001120400246 20011204 00246 NM 2001 12 4 USAASB01258 1 20010916 A 3350 20131A BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 775AU 24933 PHL - MAINTENANCE FOUND SEVERAL EMERGENCY EXIT LIGHTS, IN THE CABIN, WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPL ACED THE AFT EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001120400247 20011204 00247 NM 2001 12 4 USAASB01259 1 20010919 A 3350 20121 CHARGER BOEING 737 737301 1384611 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 336US 23233 GSO - MAINTENANCE FOUND SEVERAL EMERGENCY LIGHTS, IN THE AFT CABIN, THAT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK (P/N 2013-1A) AND CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001120400248 20011204 00248 NM 2001 12 4 USAASB01298 1 20011018 A 3350 6104789 BATTERY PACK BOEING 737 7372B7 1384560 NM CARGO BAY DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 279AU 22891 LGA - THE LEFT OVERWING EMERGENCY LIGHT WAS DIM. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK. (M) 2 L 7 2 4F A16WE 2001120400249 20011204 00249 NM 2001 12 4 USAASB01300 1 20011018 A 3350 S106 BATTERY BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 279AU 22891 LGA - THE EMERGENCY LIGHT ABOVE THE R2 SERVICE DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A16WE 2001120500007 20011205 00007 NM 2001 12 5 01FDEA01027 1 20011204 A 3260 DOWNLOCK SWITCH BOEING 727 72722 1384002 NM RIGHT LAND GEAR FAULTY A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 193FE 19142 1-387 AFTER T/O UNSAFE GEAR LIGHT ILLUMINATED. R&R R/H LAND GEAR DOWNLOCK SWITCH & ACCESSORY UNIT PER MM 32-61-021-4, 3 2-09-111-4. 2 L 7 3 4F A3WE 2001120500008 20011205 00008 NM 2001 12 5 DL72S011655 1 20011011 A 2782 1U109592A ACTUATOR BOEING 727 727232 1384082 NM L/E SLAT MALFUNCTIONED A DALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 27 542DA 22391 UPON FLAP RETRACTION FROM 2 TO 0, NR 7 L/E SLAT STAYED FULLY EXTENDED WITH FLAPS UP. VERIFIED AT S/O PANEL. APPROX 45 SECS LATER, NR 7 L/E SLAT RETRACTED ON ITS OWN. NO HYD PRESSURE OR QUANTITY FLUCTUATIONS NOTED. AIRCRAFT DID HAVE A RO LLING TENDENCY (ATLMCC/RJH) OVERWEIGHT LANDING 160,000 LBS. NORMAL TOUCHDOWN AND BRAKING. NO ABNORMALITIES NOTED. 2 L 7 3 4F A3WE 2001120500009 20011205 00009 NE 2001 12 5 DL72S011659 2 20011012 A 7230 COMPRESSOR BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE STALLED A DALA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 SO 27 531DA 67790 21814 695307 AT APPROX 80 KTS WITH POWER STABILIZED, AT45 (194/197/194) WINDS 170/17, AIRSPEED AT 90 KTS NR 2 ENG COMPRESSOR STALLED . EPR DROPPED TO APPROX 1.70 AND RECOVERED. PERFORMED BORESCOPE AND COMPRESSOR WASH, NO DAMAGE FOUND. 2 L 7 3 4F 4 F A3WE E2EA 2001120500010 20011205 00010 NM 2001 12 5 DL72S011678 1 20011002 A 5315 BAC150529222 FLOORBEAM BOEING 727 727225A 1384077 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 FOUND DURING CORROSION MID VISIT INSP MV4. CORROSION ON UPPER SURFACE OF FLOORBEAM STA 344 OUTBOARD OF INBOARD SEAT TRA CK. SPLICED IN NEW T-CAP SECTION PER SRM 53-10-8D FIG 802D FROM RBL 10 TO TERMINATION OF FLOORBEAM AT RBL 60. 2 L 7 3 4F RT A3WE 2001120500013 20011205 00013 NM 2001 12 5 DL72S011701 1 20011019 A 5320 655612910 SILL BOEING 727 727225A 1384077 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 THE OUTER CHORD OF THE C2 DOOR CUTOUT LOWER SILL STRINGER BEAM WAS FOUND WITH SEVERAL AREAS OF CORROSION ON THE OUTER FL ANGE. THE CORROSION WAS REMOVED WITH SEVERAL LOCAL BLENDS AND TRIM OUTS IN THE FLANGE ALONG WITH SEVERAL OVERSIZED FAST ENER HOLES. THE CHORD WAS REPAIRED WITH TWO EXTERNAL STEEL REPAIR STRAPS INSTALLED PER ER/A 381893-14. 2 L 7 3 4F RT A3WE 2001120500017 20011205 00017 NM 2001 12 5 DL72S011702 1 20011019 A 5712 RIB BOEING 727 727225A 1384077 NM RT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 INSPECTION OF THE RBL 70.5 UPPER RIB CHORD AT FS 760.95 ON THE RT WING PER BAC S/B 727-57-0112 AND AD 94-07-08 REVEALED CRACK INDICATIONS IN TWO FASTENER HOLES. THE HOLES WERE OVERSIZED AND BUSHED TO REMOVE THE CRACKS. THE AREA WAS REPAIR ED WITH A REPAIR ANGLE PER THE BAC S/B AND PER ER/A 381903-14AD. 2 L 7 3 4F RT A3WE 2001120500019 20011205 00019 NM 2001 12 5 DL72S011727 1 20011028 A 3350 1000677 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 524DA 21584 FWD EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY. 2 L 7 3 4F A3WE 2001120500022 20011205 00022 NM 2001 12 5 DL72S011743 1 20011031 A 5743 656233514 BEAM BOEING 727 727225A 1384077 NM RT WING CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 THE RT MLG BEAM WAS FOUND WITH CORROSION IN THE 2ND LUG LOCATION FROM THE INBOARD END OF THE BEAM. THE CORROSION WAS R EMOVED BY OVERSIZING THE HOLE BORE AND MACHINING A .035 INCH SPOTFACE ON THE FWD FACE OF THE LUG. THE BORE WAS RESTORED WITH AN OVERSIZE BUSHING AND A FILLER IN THE SPOTFACE PER ER/A 382015-14. 2 L 7 3 4F RT A3WE 2001120500023 20011205 00023 NM 2001 12 5 DL72S011765 1 20011105 A 3250 334101877 BATTERY BOEING 727 727232 1384082 NM AIRSTAIRS DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 532DA 22045 AFT AIRSTAIR EMERGENCY LIGHT VERY DIM. REPLACED BATTERIES. 2 L 7 3 4F A3WE 2001120500025 20011205 00025 NM 2001 12 5 DL72S011774 1 20011107 A 3350 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 524DA 21584 BOTH AFT SERVICE DOOR SLIDE LIGHTS INOP. RELAMPED BOTH BULBS AND REPLACED BATTERY PACK FOR M983. 2 L 7 3 4F A3WE 2001120500026 20011205 00026 NM 2001 12 5 DL72S011778 1 20011106 A 5343 65864481 ATTACH FITTING BOEING 727 727225A 1384077 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 THE AFT LOWER LUG OF THE FS 940 MLG SUPPORT BEAM ATTACH LINK WAS FOUND WITH CORROSION ON THE FWD FACE OF THE LUG. THE C ORROSION WAS REMOVED BY SPOTFACING THE LUG FACE AND SHIMMING THE GAP CREATED. THE WORK WAS ACCOMPLISHED PER ER/A 382016 -14, REV A. 2 L 7 3 4F RT A3WE 2001120500027 20011205 00027 NM 2001 12 5 DL72S011788 1 20011111 A 3350 BATTERY PACK BOEING 727 727225A 1384077 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8891Z 21860 LEFT OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK AND BATTERY RACK FOR EMERGENCY LIGHTS. ALL EMERGENCY L IGHTS OP NORMAL. 2 L 7 3 4F RT A3WE 2001120500028 20011205 00028 NM 2001 12 5 DL72S011790 1 20011111 A 5310 DOOR FRAME BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 543DA 22392 THE FWD FRAME OF THE C1 DOOR OPENING AT FS 560 WAS FOUND WITH TWO WEB CRACKS AT EXISTING FASTENER LOCATIONS BELOW THE UP PER DOOR SILL. THE CRACKS ARE TYPICAL OF BAC S/B 727-53-0219 AND AD 99-23-13. THE CRACKS WERE CUT OUT OF THE WEB AND R EPAIRED WITH A TITANIUM DOUBLER INSTALLED PER ER/A 382085-14AD, REV C. 2 L 7 3 4F A3WE 2001120500029 20011205 00029 NM 2001 12 5 DL72S011801 1 20011113 A 3350 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 542DA 22391 ON L/O FOUND R-1 DOOR OVERHEAD EMERGENCY LIGHT WILL NOT TURN ON BRIGHT WHEN EMERGENCY LIGHTS TURNED ON. REPLACED BATTER IES AND LIGHT ASSY, OPS CHECKS OK. 2 L 7 3 4F A3WE 2001120500030 20011205 00030 NM 2001 12 5 DL72S011803 1 20011113 A 3350 900835A BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 529DA 21703 ON LAYOVER FOUND RT AFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY. 2 L 7 3 4F A3WE 2001120500031 20011205 00031 NM 2001 12 5 DL72S011822 1 20011117 A 3350 LIGHT BOEING 727 727232 1384082 NM L1 DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 533DA 22046 L1 DOOR EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY. 2 L 7 3 4F A3WE 2001120500032 20011205 00032 NM 2001 12 5 DL72S011829 1 20011119 A 3350 RPS1 POWER SUPPLY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 518DA 21469 FIRST CLASS EMERGENCY PATH LIGHTS INOP. REPLACED FIRST CLASS EMERGENCY LIGHT POWER SUPPLY/CHARGER. 2 L 7 3 4F A3WE 2001120500034 20011205 00034 NM 2001 12 5 DL72S011841 1 20011121 A 3350 BATTERY BOEING 727 727225A 1384077 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8891Z 21860 R2 EMERGENCY LIGHTS INOP. REPLACED R2 RACK AND BATTERY, OP CHECKS OK. 2 L 7 3 4F RT A3WE 2001120500036 20011205 00036 NM 2001 12 5 DL72S011849 1 20011123 A 3350 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 528DA 21702 EMERGENCY EXIT LIGHT OVER CENTER AISLE BETWEEN 2L AND 2R DOORS INOP. RELAMPED LIGHT ASSY AND OPERATION NORMAL. 2 L 7 3 4F A3WE 2001120500037 20011205 00037 NM 2001 12 5 DL72S011870 1 20011127 A 5743 BEAM BOEING 727 727232 1384082 NM LT MLG CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 529DA 21703 MLG SUPPORT BEAM CHAFED I/B FWD END OF T/E PANEL I/B END. REPAIR PER MM 57-43-000-8 FIG 801. 2 L 7 3 4F A3WE 2001120500038 20011205 00038 NM 2001 12 5 SWAA013221 1 20011119 A 5320 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 525SW 26567 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 22R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001120500039 20011205 00039 2001 12 5 SWAA013222 4 20011201 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT OUT OF ADJUST. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001120500042 20011205 00042 NM 2001 12 5 SWAA013223 1 20011201 A 3350 M1133 BATTERY BOEING 737 7373H4 1384600 NM SERVICE DOOR DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 330SW 23694 DURING SCHEDULED SERVICE CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATT ERY PER MM. 2 L 7 2 4F RT A16WE 2001120500045 20011205 00045 NM 2001 12 5 SWAA013227 1 20011128 A 5320 6935352 TIE CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 685, STR 4R. REMOVED AND REPLACED TIE CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001120500047 20011205 00047 EA 2001 12 5 SWIA200110366 1 20011116 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILERON FAULTY A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 594SW 7285 SPOILERONS FAULT STATUS MESSAGE (RIGHT SPOILERON). REMOVED AND REPLACED RIGHT INBOARD PCU FOR SPOILERON IAW 27-62-01. OPS AND LEAK CHECK GOOD ON RIGHT INBOARD SPOILERON. 2 L 7 2 4F RT A21EA 2001120500051 20011205 00051 SO 2001 12 5 SWIA200110369 1 20011120 A 3080 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO ICE PROTECTION MALFUNCTIONED A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 564SW 120339 WHILE EN ROUTE, CRUISE THE ICE PROTECTION MONITOR FAILED. FLIGHT RETURNED TO SFO. RESET DEICE MONITOR CB'S AND PERFORM ED AN A/C POWER DOWN TO RESET SYSTEM. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2001120500059 20011205 00059 SO 2001 12 5 SWIA200110371 1 20011121 A 3010 BOOT EMB 120 EMB120ER 3260203 SO RIGHT WING DAMAGED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 569SW 120344 OUTBOARD LEFT WING AND OUTBOARD RIGHT WING LEADING EDGE DEICERS FAILED SIMULTANEOUSLY AT FL200. SYSTEM OPERATED NORMALL Y FOR 10 MINUTES PRIOR TO FAILURE. BOTH TIMERS 1 AND 2 RESULTED IN FAILURES AS PER QRH. INSPECTED AND FOUND HOLE IN RI GHT BOOT - OUTER TOP AREA. REPAIRED WITH BFG DEICER PATCH. OPERATIONALLY CHECKS GOOD. LIGHTS AND FUNCTION OF INFLATIO N OK. 2 L 7 2 4T RT A31SO 2001120500060 20011205 00060 SO 2001 12 5 SWIA200110372 1 20011122 A 5753 BUSHING EMB 120 EMB120ER 3260203 SO T/E FLAP WORN A SWIA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 NM 07 569SW 120344 LEFT NACELLE FLAP INBOARD HINGE POINT BUSHINGS HAVE PLAY, INBOARD AND OUTBOARD. REMOVED AND REPLACED BUSHINGS IAW SRM 5 4-20-02. (P/N 120-39902-005) 2 L 7 2 4T RT A31SO 2001120500061 20011205 00061 EA 2001 12 5 SWIA200110373 1 20011121 A 2760 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILERON MALFUNCTIONED A SWIA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 903SW 7425 O/B GND SPLR FAULT ADVISORY MESSAGE ACCOMPANIED BY SPOILERONS, FLT SPOILERS AND GND SPOILERS CAUTION MESSAGES. RETURNED TO GAT. SWAPPED NR 1 AND NR 2 SECU'S FROM SIDE TO SIDE. PERFORMED BIT TEST AND SYSTEM RESET TEST. GROUND OPS CHECK G OOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2001120500062 20011205 00062 EA 2001 12 5 SWIA200110374 1 20011123 A 3350 BB10001013 SOCKET CNDAIR CL600 CL6002B19 1900309 EA CABIN FAULTY A SWIA K NONE O OTHER TX TAXI/GRND HDL 1 NM 07 410SW 7066 EMERGENCY LIGHTS ARE ON WITH THE SWITCH IN ARMED POSITION. REMOVED AND REPLACED EMERGENCY EXIT LIGHT REFLECTOR AND SOCK ET ASSEMBLY AFT OF RT OVERWING EMERGENCY EXIT DUE TO FAULTY CONTACTOR IAW MM 33-51-21. EMERGENCY EXIT LIGHTING SYSTEM OPERATIONAL AND FUNCTIONAL CHECKS GOOD IAW MM 33-51-00. REFLECTOR (P/N BM5-0017-901), SOCKET (P/N BB1-0001-013). 2 L 7 2 4F RT A21EA 2001120500063 20011205 00063 SO 2001 12 5 SWIA200110375 1 20011122 A 5751 BEARING EMB 120 EMB120ER 3260203 SO AILERON FAILED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 569SW 120344 RIGHT AILERON INBOARD HINGE BEARING IS FALLING APART. REMOVED AND REPLACED INBOARD HINGE BEARING IAW MM 20-40-00. 2 L 7 2 4T RT A31SO 2001120500064 20011205 00064 2001 12 5 UPS01237341 4 20011127 A 2565 SLIDE BOEING 727 72762C 138402C NM ENTRY DOOR UNSECURE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 912UP 19244 INSPECTION TYPE:N/A ESCAPE SLIDE CAME OFF WHEN CREW CLOSED DOOR. SLIDE RE-INSTALLED NOTE: SLIDE DID NOT DEPLOY. 2 L 7 3 4F A3WE 2001120500065 20011205 00065 NE 2001 12 5 UPS01237343 2 20011128 A 7200 JT8D ENGINE BOEING 727 727247 138408F NM PWA JT8 JT8D NE NR 1 FAILED A IPXA A UNSCHED LANDING R X PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT CL CLIMB 1 SO 01 211UP 21700 687435 INSPECTION TYPE:N/A NR 1 ENGINE FAILURE - NOSE COWL AND BULLET DAMAGED. RETURNED TO LAN. REMOVED AND REPLACED NR 1 EN GINE PER UPS TC 1201 S/N OFF P687435B, ON 6 87439. 2 L 7 3 4F 4 F A3WE E2EA 2001120500066 20011205 00066 NM 2001 12 5 UPS01437302 1 20011103 A 5512 SKIN BOEING 747 747200 1384847 NM HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C, RT STAB UPPER FACE SURFACE CORROSION ALONG FASTENER HEADS AT SKIN AREA FROM S1 - S15, STAB STA 143 - 240. REPAIRED RT HORIZONTAL STAB UPPER SKIN AT HS STA 223 TO 182 STR 5. 2 L 7 4 4F RT A20WE 2001120500067 20011205 00067 NM 2001 12 5 UPS01437342 1 20011126 A 5753 FLAP BOEING 747 747200 1384847 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 1 INSPECTION TYPE:PFLT RT I/B TRAILING EDGE OF AFT FLAP HAS CRACK IN COMPOSITE POSSIBLE DELAMINATION O/B OF I/B CANOE, MAR KED. INSPECTED AREA AND SPEED TAPED PER EO B747-5750-15750-A. REINSPECT AT 50 DAY INTERVALS AND PERMANENT REPAIR NO L ATER THAN C-CHECK. 2 L 7 4 4F RT A20WE 2001121700121 20011217 00121 NM 2001 12 17 UPS01437344 1 20011130 A 2612 LANYARD BOEING 747 747200 1384847 NM COCKPIT DETACHED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:PFLT COCKPIT SMOKE EVAC HANDLE. LANYARD FOR SEXTON HANDLE FELL OFF. RE-INSTALLED LANYARD CHECK GOOD. 2 L 7 4 4F RT A20WE 2001120500068 20011205 00068 NM 2001 12 5 UPS01437345 1 20011202 A 3350 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:IN EMERGENCY LIGHT INOP ON MAIN DECK. EMERGENCY LIGHT REPLACED. 2 L 7 4 4F A20WE 2001120500081 20011205 00081 NM 2001 12 5 2001UALA02325 1 20011121 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 521UA 24891 LEFT HAND FUSELAGE AT BODY STATION 1587 AND STRINGER 20 LH HAS DENT IN SKIN. MAJOR REPAIR ACCOMPLISHED. DAMAGE WAS REMO VED AND SKIN LAP DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2001120500082 20011205 00082 EU 2001 12 5 2001UALA02326 1 20011121 A 5313 STRINGER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE BENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 444UA 824 DEEP GOUGE 2 FT AFT OF DR 2L, AND 1 FT UP FROM DOOR BOTTOM.. MAJOR REPAIR ACCOMPLISHED. FRAME 69, STRINGER 23 REMOVED. REWORKED STRINGER & MFG DOUBLER AND INSTALLED. 2 L 7 2 4F 4 F RT A28NM E40NE 2001120500083 20011205 00083 NM 2001 12 5 2001UALA02329 1 20011127 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 521UA 24891 EXT. FUSELAGE STATION 1760 STRINGER 19R SKIN PUNCTURED. MAJOR REPAIR ACCOMPLISHED. DOUBLER AND FLLER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2001120500084 20011205 00084 NM 2001 12 5 2001UALA02330 1 20011126 A 5210 6545871132 DOOR 6969854 BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 921UA 28747 25388 DOOR 1R LOWER FRAME OUTBOARD STOP FITTING CRACKED. MAJOR REPAIR ACCOMPLISHED.INSTALLED SPLICE REPAIR ON FRAME. 2 L 7 2 4F 4 F RT A16WE E2GL 2001120500085 20011205 00085 NM 2001 12 5 2001UALA02332 1 20011127 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 648UA 25285 BULK CARGO DOOR EXTERNAL SKIN DENTED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBL ER. 2 L 7 2 4F 4 F RT A1NM E24NE 2001120500086 20011205 00086 NM 2001 12 5 2001UALA02335 1 20011106 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 919UA 25386 DENT 1 INCH LONG BY 1/4 INCH WIDE.010 DEEP 3 FEET AFT OF MAIN ENTRY DOOR 2L. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCO MPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001120500087 20011205 00087 NM 2001 12 5 2001UALA02336 1 20011106 A 5312 WEB BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 919UA 25386 DURING ACCOMPLISHMENT OF THE 178 BLKHD SIDE CHORD AND WEB MOD, CRACKS WERE FOUND ON THE VERTICAL BEAM LOWER WEB AT RBL17 . SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2001120500088 20011205 00088 NM 2001 12 5 2001UALA02337 1 20011106 A 5311 WEB BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 919UA 25386 NOSE AREA RIGHT HAND BODY STATION 195 AT WL 207 OB WEB CRACKED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPA LCED WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2001120500089 20011205 00089 NM 2001 12 5 2001UALA02338 1 20011106 A 5311 WEB BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 919UA 25386 NOSE AREA RIGHT HAND BODY STATION 188 AT WL 207 FRAME WEB CRACKED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. R EPAIRED WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2001120500090 20011205 00090 NM 2001 12 5 2001UALA02339 1 20011106 A 5311 WEB BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 919UA 25386 NOSE AREA RIGHT HAND BODY STATION 188 AT WL 207 FRAME WEB CRACKED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. R EMOVED AND REPLACED WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2001120500091 20011205 00091 NM 2001 12 5 2001UALA02340 1 20011109 A 5311 WEB BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 919UA 25386 NOSE AREA LEFT HAND BODY STATION 188 AT WL 207 FRAME WEB CRACKED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. RE MOVED DAMAGE. FABRICATED REPAIR ANGLE AND DOUBLER AND INSTALLED. FABRICATED NEW SKIN DOUBLER AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001120500092 20011205 00092 NM 2001 12 5 2001UALA02342 1 20011109 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 919UA 25386 FOUND DENT ON LEFT SIDE STATION 227 STRINGER 15L. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. MANUFACTURED DOUBL ER AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001120500093 20011205 00093 NM 2001 12 5 2001UALA02343 1 20011128 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 922UA 26642 CABIN FLOORBEAM AT STATION 328, RBL 48 HAS DEEP GOUGE ON UPPER SURFACE. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE. IN STALLED SPLICE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001120500094 20011205 00094 NM 2001 12 5 2001UALA02345 1 20011127 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 STATION 178 BULKHEAD RBL 5.7 WL 200 HAS 2 EA CRACKS. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBL ER AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001120500095 20011205 00095 NM 2001 12 5 2001UALA02346 1 20011128 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 STATION 178 BULKHEAD LBL 5.7 AT WL 210 HAS CRACK INDICATION. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICA TED FILLER AND DOUBLER AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001120500096 20011205 00096 NM 2001 12 5 2001UALA02347 1 20011128 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 STATION 178 BULKHEAD RBL 5.7 AT WL 210 HAS CRACK INDICATION. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICA TED FILLER AND DOUBLER AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001120500099 20011205 00099 SW 2001 12 5 ALG2001F00029 1 20011019 A 6420 406012108107 PITCH HORN BELL 407 407 1182206 SW T/R HUB CORRODED E ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 427AL 53107 DURING 2500 HOUR OVERHAUL, CORROSION BEYOND LIMITS ON ENTIRE SURFACE OF PARTS DUE TO POOR QUALITY OF MATERIAL AND PAINTI NG PROCEDURE. SCRAPPED PARTS. USE BETTER QUALITY ALUMINUM AND PAINTING PROCEDURE. 1 G 7 1 3U O H2SW 2001120500100 20011205 00100 WP 2001 12 5 MWEA011470 1 20011204 A 5210 59100817 SKIN DOUG DC9 DC981 3022081 WP FWD PAX DOOR DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 FORWARD PASSENGER DOOR HAS A DENT ON EXTERNAL SKIN JUST AFT OF FORWARD VERTICAL FRAME BETWEEN #1 AND #2 HORIZONTAL BEAM -- REMOVED DAMAGED AREA, FABRICATED FAIRING, DOUBLER AND TAPERED SHIM. LOCATED, DRILLED AND INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001120500101 20011205 00101 WP 2001 12 5 MWEA011471 1 20011204 A 5230 995766438 ANGLE DOUG DC9 DC981 3022081 WP AFT CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 AFT CARGO DOOR AFT LOWER STOP FITTING ATTACH ANGLE CRACKED -- REMOVED, DRILLED UP NEW ATTACH ANGLE AND INSTALLED NEW L OWER STOP FITTING. 2 L 7 2 4F A6WE 2001120500102 20011205 00102 WP 2001 12 5 MWEA011472 1 20011204 A 5230 3926046501 FITTING DOUG DC9 DC981 3022081 WP MID CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 MID CARGO DOOR LOWER AFT STOP FITTING TO PAN ATTACH FITTING CRACKED -- REMOVED, LOCATED, DRILLED AND INSTALLED STOP FI TTING. 2 L 7 2 4F A6WE 2001120500103 20011205 00103 WP 2001 12 5 MWEA011473 1 20011204 A 5750 9957450162 ANGLE DOUG DC9 DC981 3022081 WP R/H FLAP CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 RIGHT HAND FLAP HAS EXFOLIATION CORROSION PRESENT ON AN ANGLE THAT CONNECTS A FLAP RIB TO THE LEADING EDGE FLAP SPAR. AN GLE IS LOCATED APPROXIMATELY 24 INCHES INBOARD OF FLAP MIDDLE SUPPORT FITTING -- REMOVED LEADING EDGE RIB TO FACILIATA TE OTHER MAINTENANCE. REMOVED, FABRICATED AND INSTALLED ANGLE STIFFENER. INSTALLED LEADING EDGE RIB. 2 L 7 2 4F A6WE 2001120500104 20011205 00104 WP 2001 12 5 MWEA011475 1 20011204 A 5230 995766442 INTERCOSTAL DOUG DC9 DC981 3022081 WP AFT CARGO DOOR MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 AFT CARGO DOOR LOWER AFT STOP INTERCOSTAL MISDRILLED -- REMOVED, FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2001120500105 20011205 00105 WP 2001 12 5 MWEA011476 1 20011204 A 5230 995766444 ANGLE DOUG DC9 DC981 3022081 WP AFT CARGO DOOR MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 AFT CARGO DOOR LOWER AFT STOP INTERCOSTAL INSTALL INNER ANGLE MISDRILLED -- REMOVED, DRILLED UP AND INSTALLED NEW ANGL E. 2 L 7 2 4F A6WE 2001120500106 20011205 00106 SW 2001 12 5 ALG2001F00044 1 20011003 A 6510 407340340103 DISC PACK BELL 407 407 1182206 SW ALLSN 250C 250C47B GL TAIL ROTOR CRACKED E ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 427AL 53107 CAE847416 DAILY INSPECTION OF TAILROTOR HANGER BEARINGS. CRACKED DISC NR5 AND NR6 TAILROTOR HANGER BEARINGS. ALLOW THE TAILROTOR DRIVESHAFT TO FLOAT SO DISC PACKS DO NOT FLEX AS MUCH OR AS OFTEN. 1 G 7 1 3U 3 U O H2SW E1GL 2001120500107 20011205 00107 SW 2001 12 5 ALG2001F00045 1 20011008 A 5310 206032305131 FRAME BELL 407 407 1182206 SW ALLSN 250C 250C47B GL FUSELAGE CRACKED E ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 937AL 1486 53383 DAILY INSPECTION, CRACKED DOUBLER AND FRAME AT RIGHT HAND NUT PLATE TAB. 1 G 7 1 3U 3 U O H2SW E1GL 2001120500108 20011205 00108 GL 2001 12 5 ALG2001F00046 2 20010929 A 7250 23053299 WHEEL BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE CORRODED E ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 937AL 1004 53383 CAE8472770 DURING INSPECTION FOR METAL IN OIL, SULFIDATION ON BLADES. ENSURE PROPER COATING APPLIED. 1 G 7 1 3U 3 U O H2SW E1GL 2001120500110 20011205 00110 EU 2001 12 5 BRM2001F00002 1 20011114 A 2824 D107318E PUMP BOLKMS 105 BO105LSA3 5626020 EU ALLSN 250C 250C28 03013 GL MAIN FUEL TANK INOPERATIVE A BRMA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 07 93LF 788 2038 INTERUPTION TO FLIGHT SUMMARY, 11/13/2001. ON A FLIGHT, THE LOW LEVEL FUEL LIGHT ILLUMINATED. PRECAUTIONARY LANDING MA DE AT THAT TIME. UPON INSPECTION BOTH FUEL PUMPS IN MAIN FUEL TANK FOUND INOPERATIVE. REPLACED FUEL PUMPS WITH 0.0 TSO UNITS, LEAK AND OPERATIONAL CHECKS REVEALED NO ABNORMALITIES. 1 G 7 2 3U 3 U H3AU E1GL 2001120500111 20011205 00111 SW 2001 12 5 CYX2001F00000 1 20011113 A 6230 406010432101 LINK BELL 407 407 1182206 SW SWASHPLATE DAMAGED B CYXR K NONE O OTHER IN INSP/MAINT 1 CE 01 407LG 956 53143 BEARING (PN 406-310-403-101) SLID OUT OF THE SWASHPLATE ANTI-DRIVE LINK UPPER END APPROXIMATELY .280 INCH. THIS ALLOWED THE UPPER END OF THE DRIVE LINK TO CONTACT THE SWASHPLATE LUG AND CAUSE SOME REPAIRABLE DAMAGE TO THE SWASHPLATE LUG. THE ANTI-DRIVE LINK WAS DAMAGED BEYOND REPAIR. AN INSUFFICIENT ROLL STAKE PROBABLY ALLOWED THE BEARING TO COME OUT OF T HE LINK. THIS CONDITION WAS DISCOVERED DURING A ROUTINE INSPECTION.(K) 1 G 7 1 3U O H2SW 2001120500112 20011205 00112 EU 2001 12 5 EHA2001F00004 1 20010930 A 5302 1053040210012 ATTACH FITTING BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20B 03013 GL TAILBOOM CRACKED A EHAA K NONE O OTHER IN INSP/MAINT 1 AL 03 500KM S76 CRACK DISCOVERED IN TAIL ROTOR GEARBOX ATTACH CASTING PN 105-30402-100.12 PROGRESSING FROM UPPER LEFT CORNER THROUGH FIR ST LOWER WEB (ABOVE UPPER LEFT BOLT HOLE) AND ENDING JUST PRIOR TO THE MAIN CENTER WEB. DISCREPANCY DISCOVERED AT THE 1 00 HOUR INSPECTION. PROBABLE CAUSE: VIBRATION DUE TO WORN FEATHER BEARINGS. 1 G 7 2 3U 3 U H3EU E4CE 2001120500113 20011205 00113 WP 2001 12 5 UPS01837338 1 20011124 A 2611 100064901MOD2 SMOKE DETECTOR DOUG DC8 DC871F 302199D WP CARGO BAY FAULTY A IPXA K NONE N FALSE WARNING CR CRUISE 1 SO 01 708UP 46048 INSPECTION TYPE:N/A REPEAT ITEM (2) - DURING FLIGHT AMBER MX LIGHT ILLUMINATED. TECH RECOMENDS: REVIEW MX HISTORY. DUR ING SMOKE DETECTOR TEST MX INDICATES ON TWO OCCASIONS THAT SDU FB7739 IS FAULTED. REPLACED BATTERIES, NO HELP. REMOVE AND REPLACE SAID SDU. REPLACED LWR SMOKE DETECTOR FB 7739 PER MM 26-18-00. OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2001120500114 20011205 00114 SW 2001 12 5 FKF2001F00000 1 20011008 A 3340 000030279 LENS BELL 430 430 1182150 SW ALLSN 250B 250B* GL EXTERIOR LIGTH CRACKED A FKFR K NONE O OTHER IN INSP/MAINT 1 SO 03 430CE 90 49064 LENS FOUND CRACKED AND 1 WAS CRACKED AND PART OF THE LENS IS MISSING. DURING PRE-FLIGHT CHECK. LENS WAS CRACKED AT MOU LDING POINT ACROSS BOTH SIDES. THE AFT PART OF LENS WAS STILL INTAKE WITH SCREW IN PLACE. NO DAMAGE TO AIRCRAFT NOTED. LENS THAT WAS BROKEN AND MISSING WAS IN FRONT OF TAIL ROTOR. 1 G 7 2 3U 3 T RT H9SW E10CE 2001120500115 20011205 00115 SW 2001 12 5 GUR2001F00000 1 20011021 A 6220 2040111219 PITCH HORN BELL 212 212 1181420 SW M/R HUB OUT OF TOLERANCE A GURR K NONE O OTHER IN INSP/MAINT 1 SW 09 9937K 8939 2222 30778 DURING INSPECTION OF THE MAIN ROTOR GRIP PITCH HORN TO GRIP COUNTER BORES, MEASURED THE BORES USING A TELESCOPING GAUGE AND MICROMETER. 1 G 7 1 4U H4SW 2001120500116 20011205 00116 WP 2001 12 5 UPS01837339 1 20011126 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHTS BATTERY PACK DEAD. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CH ECKS NORMAL. 2 L 7 4 4F RT 4A25 2001120500117 20011205 00117 SW 2001 12 5 GUR2001F00001 1 20011021 A 6220 2040111219 PITCH HORN BELL 212 212 1181420 SW M/R HUB OUT OF TOLERANCE A GURR K NONE O OTHER IN INSP/MAINT 1 SW 09 9937K 8939 2222 30778 DURING INSPECTION OF THE MAIN ROTOR GRIP PITCH HORN TO GRIP COUNTER BORES, MEASURED THE BORES USING A TELESCOPING GAUGE AND MICROMETER. 1 G 7 1 4U H4SW 2001120500118 20011205 00118 SW 2001 12 5 GUR2001F00002 1 20011022 A 6220 PITCH HORN BELL 212 212 1181420 SW MAIN ROTOR DAMAGED A GURR K NONE O OTHER IN INSP/MAINT 1 SW 09 8223V 30728 DURING INSPECTION OF THE MAIN ROTOR GRIP PITCH HORN TO GRIP COUNTER BORES USING A TELESCOPING GAUGE AND MICROMETER. 1 G 7 1 4U H4SW 2001120500119 20011205 00119 WP 2001 12 5 UPS01837340 1 20011126 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW DC8 MM 33-50-01, EMERG ENCY EXIT LIGHTS CHECK NORMAL. 2 L 7 4 4F RT 4A25 2001120500120 20011205 00120 SW 2001 12 5 GUR2001F00003 1 20011022 A 6220 2040111219 PITCH HORN BELL 212 212 1181420 SW PWA PT6 PT6* 52043 EA M/R HUB OUT OF TOLERANCE A GURR K NONE O OTHER IN INSP/MAINT 1 SW 09 8145Y 1030 30795 DURING INSPECTION OF THE MAIN ROTOR GRIP PITCH HORN TO GRIP COUNTER BORES, MEASURED THE BORES USING A TELESCOPING GAUG E AND MICROMETERS. 1 G 7 1 4U 3 T H4SW E2NE 2001120500121 20011205 00121 EU 2001 12 5 XN0A01030 1 20011122 A 3411 PITOT TUBE AIRBUS 300 A300B4203 3930306 EU PITOT/STATIC SYS OBSTRUCTED A XN0A C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 23 473AS 203 ABORTED TAKEOFF DUE TO CPT AIRSPEED IND FAILURE. REMOVED DEBRIS FROM PILOT TUBE, FUNCTIONALLY. OPS CHECK GOOD IAW A300 MM 34-11-40. 2 L 7 2 4F RT A35EU 2001120500122 20011205 00122 EU 2001 12 5 XN0A01031 1 20011127 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU COCKPIT MALFUNCTIONED A XN0A D RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 23 372PC 196 FLT DECK SMOKE LIGHT ON TAKEOFF ROLL 90 KTS. CLEANED AND RE-SECURED FLT DECK SMOKE DET C/P, OPS CHECK NORMAL IAW A300 M M 26-10-00. 2 L 7 2 4F RT A35EU 2001120500123 20011205 00123 NE 2001 12 5 JYD2001F00001 1 20010620 A 6320 643520078105 SHAFT SKRSKY S64 CH54A 8142501 NE GEARBOX CRACKED A JYDR K NONE O OTHER IN INSP/MAINT 1 NM 09 176AC 1430 64062 EIGHT CRACKS FOUND IN LOWER SPLINES OF MAIN ROTOR SHAFT. MAIN GEARBOX PN 6435200400065, SN A6171 WAS REMOVED FOR OVERHA UL HAVING A TOTAL TIME OF 8857.7 AND 1430.6 HOURS TIME SINCE OVERHAUL. THIS INCLUDES COMPLETING A 130.6 HOUR EXTENSION. DURING THE INSPECTION PROCESS, EIGHT CRACKS WERE DETECTED BY FLUORESCENT MAGNETIC PARTICLE INSPECTION IN THE LOWER SPL INE AREA. CRACK LENGTHS ARE AS FOLLOWS: TWO AT .025, THREE AT .050, TWO AT .075 AND ONE AT .125. AS MANY AS THREE CRA CKS WERE FOUND ON ONE SPLINE. 2 G 7 2 4U H16NM 2001120500124 20011205 00124 NE 2001 12 5 JYD2001F00002 1 20010620 A 6320 643520229105 PLATE SKRSKY S64 S64E 8142604 NE GEARBOX CRACKED A JYDR K NONE O OTHER IN INSP/MAINT 1 NM 09 176AC 8857 64003 CRACKS FOUND IN ROOT AREA OF THREE INTERNAL SPLINES OF LOWER PLATE OF 2ND STAGE PLANETARY PLATE ASSY. MAIN GEARBOX WAS REMOVED FOR OVERHAUL. DURING THE INSPECTION PROCESS, THREE CRACKS WERE DETECTED BY FLUORESCENT PENETRANT INSPECTION INT HE INTERNAL SPLINES OF THE CENTER HUB OF THE LOWER 2ND STAGE PLANETARY PLATE. UPPER SIDE OF LOWER PLATE (BEARING RIDING SURFACE) APPROXIMATE CRACK LOCATIONS IN CENTER HUB BORE AND THEIR LENGTHS. ALL CRACKS REMAINED IN THE ROOT AREA OF INT ERNAL SPLINES. CRACKED REMAINED IN THE ROOT AREA. 2 G 7 2 4U H4EA 2001120500125 20011205 00125 EU 2001 12 5 XN0A01032 1 20011204 A 2612 GROUND WIRE AIRBUS 300 A300B4203 3930306 EU NR 2 ENGINE DAMAGED A XN0A E ENGINE SHUTDOWN N FALSE WARNING TX TAXI/GRND HDL 1 GL 23 371PC 157 FIRE INDICATION NR 2 ENGINE INDICATION REMAINED ON WITH THROTTLE AT IDLE. SHUT ENGINE DOWN WITH FUEL LEVER. FIRE INDIC ATION EXTINGUISHED. REPAIRED 2 EACH GROUND WIRES ON FIRE LOOP NR 2 ENGINE IAW 20-44-00. OPS CHECK GOOD IAW A300 MM 26- 12-00. 2 L 7 2 4F RT A35EU 2001120500126 20011205 00126 NE 2001 12 5 JYD2001F00003 2 20010809 A 7230 670403 COMPRESSOR WHEEL SKRSKY S64 S64E 8142604 NE PWA JFTD12 JFTD12A4A 52047 NE ENGINE CRACKED E K NONE O OTHER IN INSP/MAINT 1 NM 09 164AC 3147 64034D COMPRESSOR, PN JFTD12A4A, SN 672491 HAVING A TOTAL TIME OF7090.9 AND A TIME SINCE OVERHAUL OF 3147.9 WAS REMOVED FOR OVE RHAUL. DURING INSPECTION, 14 CRACKS WERE DETECTED IN THE 3RD STAGE COMPRESSOR DISK PN670403, SN M103AA0069 BY LIQUID PE NETRANT INSPECTION. ALL CRACKS ORIGINATED FROM TIE ROD HOLES AND EXTENDED OUTWARD. THE LONGEST CRACK WAS APPROXIMATELY .322 INCH. 2 G 7 2 4U 4 U H4EA E15EA 2001120500127 20011205 00127 EU 2001 12 5 XN0A01033 1 20011204 A 2913 PUMP AIRBUS 300 A300B4203 3930306 EU NR 1 ENGINE FAILED A XN0A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 472AS 125 RETURNED TO THE GATE DUE NR 1 ENGINE GREEN HYD PUMP INOP. REMOVED AND REPLACED NR 1 ENGINE GREEN HYD PUMP IAW MM 29-11- 00. OPS CHECK/LEAK CHECK GOOD. 2 L 7 2 4F RT A35EU 2001120500129 20011205 00129 NM 2001 12 5 VNAA0111015 1 20011130 A 2100 APU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE A VNAA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 07 432JS 3045 WHILE ADDING POWER DURING TAKE OFF, THE CABIN FILLED WITH SMOKE AND THE CREW ABORTED TAKE OFF. THE CREW ENSURED ALL PAS SENGERS WERE FIT TO RETURN TO THE GATE. AFTER RETURNING TO THE GATE, MAINTENANCE INSPECTED AND FOUND DE-ICE FLUID HAD G OTTEN INTO THE APU ANDHAD CAUSED THE SMOKE. MAINTENANCE THEN PERFORMED A GROUND OPERATIONAL CHECK WITH THE AIRCRAFT. BOTH THE PACK SYSTEM AND APU SYSTEM CHECKED GOOD. THE AIRCRAFTWAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001120500131 20011205 00131 WP 2001 12 5 ZW0A0111401 1 20011119 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 927TW 49358 DURING CHECK-C MAINT FOUND CORROSION ON CHAIR TRACK AT STA 1079 TO 1240. REMOVED AND REPLACED FLOOR TRACK FROM STA 1079 TO 1240 PER SRM 53-05, FIG 4F. 2 L 7 2 4F A6WE 2001120500132 20011205 00132 WP 2001 12 5 ZW0A0111402 1 20011114 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 927TW 49358 DURING CHECK-C MAINT FOUND CORROSION ON CHAIR TRACK NUMBER 2 FROM STA 1136 TO 1079. REMOVED CORRODED TRACK FROM STA 107 9 TO 1309, AND INSTALLED NEW TRACK FROM STA 1079 TO 1309. INSTALLED SPLICE ASSEMBLY AT STA 1079 WITH HI-LOKS, WASHERS, AND NUTS AND PR1422 SEALANT PER SRM 53-05, FIG 4 PAGE 1. 2 L 7 2 4F A6WE 2001120500133 20011205 00133 GL 2001 12 5 JYD2001F00005 2 20010917 A 7230 712701 HUB SKRSKY S64 S64E 8142604 NE GE CT58 CT58* 30011 GL COMPRESSOR WHEEL CRACKED B JYDR K NONE O OTHER IN INSP/MAINT 1 NM 09 194AC 6694 2995 64017 FRONT HUB, PN 712701, SN 3V4170 FOUND CRACKED DURING OVERHAUL. COMPRESSOR WAS REMOVED FROM SERVICE DUE TO REACHING ITS OVERHAUL INTERVAL. DURING THE OVERHAUL INSPECTION, TWO CRACKS WERE DETECTED BY FLUORESCENT PENETRANT INSPECTION(FPI). 1ST CRACK LOCATION DETECTED BY FPI WAS IN THE CENTER RING OF FRONT HUB, EXTENDING FROM A BLADE PIN HOLE AT A 45 DEGREE A NGLE THROUGH THE 45 DEGREE CHAMFER TO THE OUTER DIAMETER OF CENTER RING. TOTAL LENGTH OF CRACK IS APPROX .625 INCH. 2N D CRACK IS IN ADJACENT PIN HOLE, ON FRONT RADIUS, EXTENDING AT A 45 DEGREE ANGLE FROM HOLE. CRACK APPROXIMATELY .125 IN CH IN LENGTH. NO PROBABLE CAUSE DETERMINED OR RECOMMENDATIONS TO PREVENT RECURRENCE. 2 G 7 2 4U 4 U H4EA 1E3 2001120500134 20011205 00134 NE 2001 12 5 JYE2001F00000 1 20011016 A 6720 S61406561211 CABLE SKRSKY S61 S61A 814210C NE GE CT58 CT58* 30011 GL TAIL ROTOR FRAYED B JYER A UNSCHED LANDING O OTHER NR NOT REPORTED 1 NM 09 1048Y 4 61161 068 TAIL ROTOR CABLE (PN S6140-65612-11) WAS FOUND BADLY FRAYED AND BROKEN AFTER PILOT MADE AN UNEVENTFUL LANDING, AT AN A IRPORT. THE PROBABLE CAUSE IS THE CABLE HAD BEEN ROUTED OVER THE CABLE GUARD PIN INSTEAD OF THE PULLEY. THE CABLE IS B EING SENT OUT FOR METALLURGY AND FAILURE ANALYSIS. OPERATOR CALLED FSDO TO ADVISE THAT METALLURGY ANALYSIS RESULTS INDI CATED THAT THE CABLE FAILURE WAS A RESULT OF WEAR. OPERATOR WILL CIRCULATE A LETTER TO ALL FIELD AND SHOP MECHANICS ADV ISING REMOVAL OF GUIDE PINS UNTIL RIGGING IS COMPLETED, WHEN INSTALLING CABLE. THIS IS THE PROCEDURE USED FOR THE S61 C IVILIAN MODELS. (K) 2 G 7 2 4U 4 U H2EA 1E3 2001120500135 20011205 00135 WP 2001 12 5 ZW0A0111403 1 20011115 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 913TW 49184 DURING CHECK-C MAINT FOUND CORROSION IN AFT CARGO COMPT ON FORMER FRAME AT STA 1322, FROM LONGERON 29L TO 29R. REMOVED CORROSION PER SRM 51-10-3. REPAIRED PER SRM 53-03, FIG 2A. 2 L 7 2 4F A6WE 2001120500136 20011205 00136 EU 2001 12 5 KBM2001F00002 1 20010925 A 2150 060018 BELT SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE AIR CONDITIONER BROKEN E KBMA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 19 115SH 2760 3141 AIR CONDITIONER BELT, BURNING SMELL. REPLACED AIR CONDITIONER BELT. 1 G 7 1 3U 3 U H9EU E19EU 2001120500137 20011205 00137 EU 2001 12 5 KBM2001F00003 1 20010921 A 7931 350A674023 HARNESS SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE OIL PRESSURE DAMAGED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 115SH 3013 3141 ENGINE OIL PRESSURE GAUGE. SHOWED SUSTAINED INDICATION IN THE PRD-FOUND BROKEN WIRES ADJACENT TO TOP CANNON PLUG. REPL ACED OIL PRESSUE HARNESS. 1 G 7 1 3U 3 U H9EU E19EU 2001120500138 20011205 00138 WP 2001 12 5 ZW0A0111404 1 20011116 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 913TW 49184 DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND FORMER CORRODED FROM LONGERON 28R TO 28L, STA 1271. REMOVED CORROSION PER SPM 6-80-1 AND SRM 51-10-3. REPAIRED PER SRM 53-03, FIG 2. 2 L 7 2 4F A6WE 2001120500139 20011205 00139 EU 2001 12 5 KBM2001F00004 1 20010925 A 2912 806966 FILTER ELEMENT SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE HYD SYSTEM BYPASSING E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 115SH 3018 3018 FILTER ELEMENT, HYDRAULIC FILTER BYPASS INDICATOR POPPED. INSTALLED NEW FILTER. 1 G 7 1 3U 3 U H9EU E19EU 2001120500140 20011205 00140 EU 2001 12 5 KBM2001F00005 1 20010919 A 3260 645300684 GAUGE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE NLG INACCURATE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 37SH 2300 NOSE GEAR GAUGE - NOSE GEAR GAUGE INDICATES 1.5 PERCENT HIGHER THAN ACTUAL NOSE GEAR SP FRO. INSTALLED NOSE GEAR GAUGE. 1 G 7 1 3U 3 U NC H9EU E19EU 2001120500141 20011205 00141 EU 2001 12 5 KBM2001F00006 1 20010921 A 7920 0292105210 PUMP SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE OIL DEFECTIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 115SH 2036 3141 ENGINE OIL PRESSURE GAUGE SHOWED SUSTAINED INDICATION IN THE RED. INSTALLED OIL PUMP/REPLACED DEFECTIVE ORING UNDER FIL TER HOUSING. CHECK BI LEVEL PRESSURE. WILL GAUGE AND FOUND TO BE SERVICEABLE. 1 G 7 1 3U 3 U H9EU E19EU 2001120500142 20011205 00142 WP 2001 12 5 ZW0A0111405 1 20011119 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 913TW 49184 DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND CORROSION ON INTERCOSTAL AT STA 1309 TO 1322, BELOW THE LT CHAIR TRACK . REMOVED CORROSION PER SRM 51-10-3. INSTALLED FITTING PER DRAWING 3936595, ATTACHING INTERCOSTAL TO FORMER. 2 L 7 2 4F A6WE 2001120500143 20011205 00143 WP 2001 12 5 ZW0A0111406 1 20011119 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 913TW 49184 DURING CHECK-C MAINT IN THE AFT CARGO COMPT THE LT TIE DOWN TRACK WAS CORRODED FROM STA 1212 TO 1322. INSTALLED NEW TRA CK PER SRM 51-30-2, AND 51-30-8. INSTALLED SPLICE PER SRM 53-05, FIG 4G. 2 L 7 2 4F A6WE 2001120500144 20011205 00144 EU 2001 12 5 KBM2001F00008 1 20011028 A 2150 SD507 COMPRESSOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE AIR CONDITIONER INOPERATIVE A KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 37SH 2300 AIR CONDITIONER BLOWS WARM. INSTALLED SERVICEABLE COMPRESSOR, SERVICE OF SYSTEM WITH 3.5 LBS OF P134A. 1 G 7 1 3U 3 U NC H9EU E19EU 2001120500145 20011205 00145 WP 2001 12 5 ZW0A0111407 1 20011119 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 913TW 49184 DURING CHECK-C MAINT IN THE AFT CARGO COMPT THE RT TIE DOWN WAS CORRODED FROM STA 1212 TO 1322. REPLACED WITH NEW TRACK PER SRM 51-30-1, STA 1212 TO 1322. 2 L 7 2 4F A6WE 2001120500146 20011205 00146 WP 2001 12 5 ZW0A0111408 1 20011119 A 5753 RUB STRIP DOUG DC9 DC983 3022083 WP T/E FLAP WORN A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9628W 53598 DURING CHECK-C MAINT THE LT INBOARD FLAP HAD HOLE WORN THRU THE LEADING EDGE WEAR STRIP OF THE FLAP, 51 INCHES FROM THE INBOARD EDGE OF THE FLAP. REMOVED DAMAGED AREA AND REPAIRED PER SRM 57-09, FIG 43. 2 L 7 2 4F RT A6WE 2001120500147 20011205 00147 NM 2001 12 5 DL72W011674 1 20011016 A 3350 1000000361 BATTERY PACK BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 295WA 22532 THE 1R & 1L EXTERIOR EMERGENCY LIGHT OUT. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 2001120500148 20011205 00148 WP 2001 12 5 P2EA2001M0012 1 20011204 A 5610 NA WINDSHIELD DOUG DC9 DC982 3022082 WP A P2EA K NONE O OTHER AP APPROACH 1 CE 05 135NJ 49440 FLIGHT 325 FROM MCI TO DEN ON SHORT FINAL TO RUNWAY 16. AIRCRAFT CAPT'S L-1 WINDOW INCOUNTERED A BIRD STRIKE. INSPECTED WINDOW I.A.W. BMM 05-51-08 NO DEFECTS NOTED. 2 L 7 2 4F A6WE 2001120500149 20011205 00149 2001 12 5 DL72W011676 4 20011016 A 2565 146110018 SLIDE BOEING 727 727247 138408F NM L2 DOOR UNSERVICEABLE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 291WA 22109 DURING LAYOVER CHECK, FOUND EMERGENCY SLIDE 2 LEFT PRESSURE LOW. REPLACED SLIDE. 2 L 7 3 4F A3WE 2001120500150 20011205 00150 NE 2001 12 5 KBM2001F00009 2 20011027 A 7200 ENGINE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE REAR BEARING FAILED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 345SH 9229 3345 ENGINE CHIPLIGHT ILLUMINATED. DISASSEMBLED ENGINE ASSEMBLY AND FOUND REAR BEARING TO HAVE ONE ROLLER FLATTENED APPREARS TO HAVE SKID. RETURNED ENTIRE ENGINE ASSEMBLY FOR REPAIR. INSTALLED RENTAL ENGINE. 1 G 7 1 3U 3 U H9EU E19EU 2001120500151 20011205 00151 EU 2001 12 5 KBMA111953 1 20011002 A 5320 350A34102321 FLANGE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE SPLINED FLANGE VIBRATION A KBMA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 WP 19 230SH 42833 2337 SPLINED FLANGE, HIGH FREQUENCY VIBRATION FELT IN CABIN. 1 G 7 1 3U 3 U NC H9EU E19EU 2001120500152 20011205 00152 EU 2001 12 5 KBMA111954 1 20011002 A 7120 350A51200520 MOUNT SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE VIBRATION A KBMA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 WP 19 230SH 4283 2337 ENGINE REAR MOUNT, HIGH FREQUENCY VIBRATION FELT IN CABIN. INSTALLED NEW ENGINE MOUNT. 1 G 7 1 3U 3 U NC H9EU E19EU 2001120500153 20011205 00153 NM 2001 12 5 DL72W011720 1 20011025 A 5521 657278419 SPAR BOEING 727 727247 138408F NM ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 294WA 22112 INSPECTION OF THE LT ELEVATOR REAR SPAR PER BAC S/B 727-55-0089 AND AD 96-06-05 REVEALED A TYPICAL CRACK EMANATING FROM A TAB HINGE SHEAR PLATE. THE CRACK WAS WITHIN LIMITS OF THE S/B AND WAS STOP DRILLED ON A TEMPORARY BASIS UNTIL THE SP AR MOD IS ACCOMPLISHED PER THE S/B. THE WORK WAS ACCOMPLISHED PER ER/A 382010-14AD. 2 L 7 3 4F A3WE 2001120500154 20011205 00154 NM 2001 12 5 DL72W011742 1 20011031 A 3350 90052 RACK BOEING 727 727247 138408F NM L2 DOOR FAULTY A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2819W 21057 L2 DOOR EMERGENCY LIGHT INOP. FOUND BATTERY MOUNT RACK BAD. REPLACED BATTERY RACK AND BATTERY. CHECKS GOOD. 2 L 7 3 4F A3WE 2001120500155 20011205 00155 NM 2001 12 5 DL72W011787 1 20011111 A 3350 1000677 LIGHT BOEING 727 727247 138408F NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 295WA 22532 EMERGENCY LIGHT OUT AT R1 AND CENTER OVERWING. REPLACED EMERGENCY LIGHT ASSY AT R1, REPLACED EMERGENCY LIGHT BATTERY AT OVERWING EXIT, OPS CHECKS OK. 2 L 7 3 4F A3WE 2001120500156 20011205 00156 NM 2001 12 5 DL72W011810 1 20011113 A 3350 900835A BATTERY PACK BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 296WA 22533 FOUND RIGHT AFT OVERWING EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 2001120500157 20011205 00157 NM 2001 12 5 DL72W011815 1 20011113 A 3350 900835A BATTERY PACK BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 296WA 22533 RIGHT AFT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 2001120500158 20011205 00158 NE 2001 12 5 KBMA111956 2 20011004 A 7250 BLADE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE TURBINE DISK BROKEN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 270SH 7527 1864 ENGINE HAS BROKEN TURBINE BLADE. FOUND FIRST STAGE TURBINE DISK HAD BROKEN BLADE. NOTE: IGNITOR WAS MISSING THE ELECT RODE AND APPEARED IT HAD GONE THROUGH THE ENGINE( PN SC2036. REMOVED ENGINE ASSEMBLY AND REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2001120500159 20011205 00159 NE 2001 12 5 KBMA111957 2 20011004 A 7421 9550168760 IGNITER SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE BROKEN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 270SH 7527 1864 IGNITER WAS MISSING THE ELECTRODE. REMOVED AND REPLACED IGNITER. 1 G 7 1 3U 3 U NC H9EU E19EU 2001120500160 20011205 00160 EU 2001 12 5 KBMA111959 1 20011006 A 6321 704A34130044 CABLE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE ROTOR BRAKE MALFUNCTIONED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 313LV 560 3296 ROTOR BRAKE NOT FUNCTIONING PROPERLY. REPLACED BRAKE CABLE. 1 G 7 1 3U 3 U H9EU E19EU 2001120500161 20011205 00161 EU 2001 12 5 KBMA111960 1 20011006 A 6321 350A32501000 BRAKE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE ROTOR INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 313LV 560 3296 ROTOR BRAKE NOT FUNCTIONING PROPERLY. INSTALLED SERVICEABLE ROTOR BRAKE. 1 G 7 1 3U 3 U H9EU E19EU 2001120500162 20011205 00162 NE 2001 12 5 KBMA111961 2 20011008 A 7320 0164448430 FUEL CONTROL SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 350SH 296 2957 FUEL DROPS FROM DECELERATION DRAIN. REPLACED WITH SERVICEABLE UNIT. REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U NC H9EU E19EU 2001120500163 20011205 00163 EU 2001 12 5 KBMA111962 1 20011010 A 6720 350A3310583 LEVER SNIAS 350 AS350B1 8680811 EU CONTROL LEVER DEBONDED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 53SH 5531 2009 TAIL ROTOR PATCH CHANGE CONTROL LEVER BUSHING DEBONDED. THIS UNIT WAS INSPECTED AND FOUND TO ONLY NEED REBONDING AND TH EN CAN BE PLACED BACK IN SERVICE. REPLACED WITH A SERVICEABLE PATCH CHANGE CONTROL LEVER. 1 G 7 1 3U H9EU 2001120500164 20011205 00164 EU 2001 12 5 KBMA111979 1 20011028 A 2150 SD507 COMPRESSOR SNIAS 350 AS350BA 8680817 EU AIR CONDITIONER INOPERATIVE A KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 37SH 10193 2300 AIR CONDITIONER BLOWS WARM. INSTALLED SERVICEABLE COMPRESSOR, SERVICE FOR SYSTEM WITH 3.5 LBS P134A. 1 G 7 1 3U NC H9EU 2001120500165 20011205 00165 EU 2001 12 5 KBMA111980 1 20011028 A 6730 AC67244 SERVO SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE RT LATERAL LEAKING A KBMA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 19 270SH 541 1864 RIGHT LATERAL SERVO LEAKING BEYOND DYNAMIC. INSTALLED SERVICEABLE UNIT. 1 G 7 1 3U 3 U NC H9EU E19EU 2001120500166 20011205 00166 NE 2001 12 5 KBMA111981 2 20011023 A 7250 BLADE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE 1ST STG TURBINE DAMAGED A KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 37SH 502 2300 ENGINE HAD CHIPPED TURBINE BLADES AND ONE CRACKED (1ST STAGE TURBINE BLADES) RETURNED FOR REPAIR. INSTALLED REPLACEMEN T ENGINE. 1 G 7 1 3U 3 U NC H9EU E19EU 2001120500167 20011205 00167 NM 2001 12 5 DL72W011827 1 20011119 A 3260 656021132 ACCESSORY UNIT BOEING 727 727247 138408F NM E/E BAY FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 294WA 22112 AFTER T/O AND GEAR RETRACTION WHEN GEAR HANDLE WAS PLACED TO THE OFF POSITION IT DID NOT CATCH IN THE DETENT. GEAR DISA GREE LIGHT AND DOORS LIGHT ILLUMINATED. GEAR WAS THEN CYCLED WITH A/C SPEED AT 230 KNOTS CAUSING OVERSPEED CONDITION ON GEAR. GEAR WAS RETRACTED AND ALL RETURNED TO NORMAL. REPLACED LANDING GEAR ACCESSORY MODULE. SWUNG LANDING GEAR, CHE CKS OUT OK. 2 L 7 3 4F A3WE 2001120500168 20011205 00168 EU 2001 12 5 KBMA112018 1 20011025 A 6410 350A33215300 BEARING SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR CRACKED B KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 2273A 2959 2273 BEARINGS ARE CRACKED, REPLACED WITH NEW BEARINGS. 1 G 7 1 3U 3 U NC H9EU E19EU 2001120500169 20011205 00169 NM 2001 12 5 DL72W011867 1 20011126 A 3350 1001141 LIGHT BOEING 727 727247 138408F NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 295WA 22532 AFT AIRSTAIR OVERHEAD EMERGENCY LIGHTS INOP. REPLACED LIGHT ASSY AND BATTERIES. 2 L 7 3 4F A3WE 2001120500170 20011205 00170 EU 2001 12 5 KBMA112019 1 20011025 A 6410 355A09103601 BEARING SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR CRACKED B KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 2273A 498 2273 BEARINGS ARE CRACKED AND DELAMINATING. REPLACED WITH SERVICABLE BEARINGS. 1 G 7 1 3U 3 U NC H9EU E19EU 2001120500171 20011205 00171 NM 2001 12 5 DL733011709 1 20011023 A 2424 GCU BOEING 737 737347 1384647 NM NR 1 ENGINE FAILED A DALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 27 307WA 22147 23440 60281 APU OVERSPEED, NR 1 GEN WAS ALREADY ON MCO. RESET OVERSPEED ON APU ACCY UNIT. APU WORKS NORMAL. REPLACED NR 1 GCU NR 1 GEN WORKS NORMAL. 2 L 7 2 4F RT A16WE 2001120500172 20011205 00172 NM 2001 12 5 DL733011754 1 20011103 A 5270 SENSOR BOEING 737 737347 1384647 NM CARGO DOOR DIRTY A DALA D RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 27 308WA 23441 CLIMBING THRU 4000 FT FWD CARGO LIGHT ILLUMINATED. RETURNED FOR LANDING. MAINTENANCE CONFIRMED DOOR CLOSED AND LOCKED. CLEANED FWD SENSOR OF FOREIGN SUBSTANCE, OP CHECKS GOOD. 2 L 7 2 4F RT A16WE 2001120500173 20011205 00173 NM 2001 12 5 DL738011715 1 20011022 A 5312 148A22811 BULKHEAD BOEING 737 737832 13844CF NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 372DA 29620 THE FS 1016 AFT PRESSURE DOME WEB WAS FOUND WITH A 6 X 8 X .125 INCH DEEP SMOOTH INDENTATION. INSPECTION OF BOTH SIDES OF THE P-DOME PER BAC S/B 737-53A1238, REVEALED NO FURTHER DAMAGED. THE DAMAGED AREA WAS REPAIRED WITH AN ALUMINUM STIF FENER AND STRAP PER THE B737-800 SRM AND PER ER/A 381941-14AD, REV C. 2 L 7 2 4F RT A16WE 2001120500174 20011205 00174 NM 2001 12 5 DL738011726 1 20011027 A 2750 FLAP BOEING 737 737832 13844CF NM WINGS MALFUNCTIONED A DALA K NONE F FLT CONT AFFECTED AP APPROACH 1 SO 27 383DN 30346 ON LANDING PREPARATION FLAPS STOPPED AT 18 DEGREES/15 FLAP. LANDING WAS MADE, NO UNUSUAL CONTROL INPUTS NEEDED. RAN AS EU BITE PROCEDURE PER TASK 27-51-801, NO EXISTING FAULTS. HISTORY SHOWED LAST FLT FAULT RT 28VDC EXC INV CODE27-53-280, PERFORMED TASK 27-51-823. DETERMINED TO BE INTERMITTENT FAULT. RAN FLAPS THRU 3 CYCLES, NO TROUBLE FOUND. 2 L 7 2 4F RT A16WE 2001120500175 20011205 00175 EA 2001 12 5 COMA0160944 1 20011119 A 5310 WEB CNDAIR CL600 CL6002B19 1900309 EA F.S.640 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 916CA 19606 7014 DURING INSPECTION I/A/W E.O. 53-021 OF ENGINE SUPPORT BOX BEAM, A .250 INCH CRACK WAS FOUND IN THE UPPER WEB AT F.S. 640 AND BL 9.5 RT.C/W TEMPORARY REPAIR I/A/W REO 601R-53-61-345. 2 L 7 2 4F RT A21EA 2001120500176 20011205 00176 NM 2001 12 5 DL738011680 1 20011017 A 5242 DOOR BOEING 737 737832 13844CF NM EXTERNAL POWER OPEN A DALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 27 3741S 30487 LOUD VIBRATION AND BUZZING NOISE ON CLIMBOUT AND LEVEL OFF. SPEED SENSITIVE. VIBRATION ON ALL CONTROLS AND IN FLOOR. UPON ARRIVAL FOUND EXT GROUND POWER DOOR OPEN AND UNLATCHED. INSPECTED DOOR AND AREA. NO DAMAGE NOTED. INSPECTED A/C. NO OTHER PROBLEMS NOTED. 2 L 7 2 4F RT A16WE 2001120500177 20011205 00177 NM 2001 12 5 DL738011728 1 20011027 A 3350 D71701001 POWER SUPPLY BOEING 737 737832 13844CF NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 3741S 30487 EMERGENCY AISLE LIGHTS AT 15DEF-17ABC AND EXIT LOCATOR SIGN AT ROW 17 INOP. REPLACED POWER SUPPLY ON RIGHT SIDE AT STAT ION 583. OPERATIONAL CHECKS OK. 2 L 7 2 4F RT A16WE 2001120500178 20011205 00178 NM 2001 12 5 DL738011729 1 20011028 A 2120 ODOR BOEING 737 737832 13844CF NM COCKPIT DETECTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 3757D UNK ON CLIMBOUT STRONG BURNING SMELL IN COCKPIT AND CABIN. PERFORMED HIGH POWER RUN-UP WITH LT AND RT A/C PACKS ON FOR 5 MI NS WITH ALL OVENS RUNNING, NO SMELL NOTED. ALL LIGHT IN CAB OK. CHECKED ALL LAVS AND ALL OK. 2 L 7 2 4F RT A16WE 2001120500179 20011205 00179 NE 2001 12 5 DL738011736 2 20011030 A 7321 EEC BOEING 737 737832 13844CF NM GE CFM56 CFM567B24 NE NR 1 ENGINE MALFUNCTIONED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 390DA 4800 30536 876291 ENGINE CONTROL LIGHT ON TAKEOFF ROLL. ABORTED TAKEOFF. PERFORMED EEC BITE. LT AND RT EEC FAULT 73-31671. PROBE HEAT FAULT. T/S PER FIM, CKD OK. RAN ENGINE TO TAKEOFF PWR. NO FAULTS, NO LIGHTS. OK FOR SERVICE. NOTE: PROBLEM INVOLVE D BOTH ENGINES. CREW NOT SURE IF ANTI-ICE WAS TURNED ON. 2 L 7 2 4F 4 F RT A16WE E00055EN 2001120500180 20011205 00180 EA 2001 12 5 COMA0160945 1 20011119 A 5310 WEB CNDAIR CL600 CL6002B19 1900309 EA F.S. 630 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 916CA 19606 7014 DURING INSPECTION I/A/W E.O. 53-021 OF ENGINE SUPPORT BOX BEAM, A 1.0 INCH CRACK WAS FOUND IN THE LOWER WEB L/H ACCESS P ANEL CUTOUT OF F.S. 630 BL 40 LT.C/W REPAIR I/A/W REO 601R-53-61-366. 2 L 7 2 4F RT A21EA 2001120500181 20011205 00181 NM 2001 12 5 DL738011848 1 20011124 A 2720 3815001003 PCU BOEING 737 737832 13844CF NM RUDDER LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 3754A 29626 TOP DESCENT NOTICED NR 1 ENG DRIVEN HYD LOW PRESSURE LIGHT FLICKERING. A SYSTEM QTY 21 PERCENT PRESSURE 3000. B-SYSTEM QTY 88 PERCENT PRESSURE NORMAL. FOUND RUDDER PCU LEAKING AT LOWER SPLIT. REMOVED AND REPLACED SAME. 2 L 7 2 4F RT A16WE 2001120500182 20011205 00182 EA 2001 12 5 COMA0160946 1 20011201 A 3000 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 987CA 7199 FLIGHT 5616 T/O ABORTED AT 120 KTS DUE TO ANTI-ICE DUCT WARNING.C/W RTO INSPECTION, NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 2001120500183 20011205 00183 NM 2001 12 5 DL738011857 1 20011125 A 2910 HYDRAULIC SYSTEM BOEING 737 737832 13844CF NM A SYSTEM CONTAMINATED A DALA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 SO 27 3754A 29626 ON GEAR RETRACTION BOTH A-SYSTEM LOW PRESS LIGHTS ILLUM AND GEAR HESITATED THEN SLOWLY RETRACTED. SYS-A QTY DROPPED FRO M 99 PERCENT TO 66 PERCENT. A/C FELT LIKE IT WENT INTO MANUAL REVERSION ON FLIGHT CONTROLS. AFTER TURNING SYSTEM-A FLT CONTROL SWITCH TO OFF FLIGHT CONTROLS WOULD CYCLE BETWEEN NORMAL AND MANUAL REVERSION. BLED AIR FROM HYDRAULIC SYSTEM. 2 L 7 2 4F RT A16WE 2001120500184 20011205 00184 NM 2001 12 5 DL73K011651 1 20011011 A 5330 655298890 SKIN BOEING 737 737232 1384475 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 318DL 23090 DAMAGE FOUND IN THE L2 DOOR SURROUND BEAR STRAP AT THE UPPER HINGE CUTOUT, THE SKIN IS ALSO DAMAGED AT THIS LOCATION. E R/A 360175-14 REV B. 2 L 7 2 4F RT A16WE 2001120500185 20011205 00185 NM 2001 12 5 DL73K011684 1 20011018 A 7120 654685010 MOUNT BOEING 737 737232 1384475 NM ENGINE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 301DL 23073 FWD ENGINE MOUNT SUPPORT FITTING ASSY WAS FOUND WITH OVERSIZED MOUNT HOLES. REPAIR PER ER/A 410550-14AD. 2 L 7 2 4F RT A16WE 2001120500186 20011205 00186 NM 2001 12 5 DL73K011685 1 20011017 A 2530 5374AD COFFEEMAKER BOEING 737 737247 138448D NM AFT GALLEY OVERHEATED A DALA A UNSCHED LANDING M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 378DL 23605 ELECTRICAL ODOR IN AFT GALLEY, GALLEY WALL HOT TO TOUCH. FOUND NR 2 COFFEEMAKER OVERHEATING. REPLACED BOTH COFFEEMAKER S IN AFT GALLEY. OPN NORMAL. CKD WALL AFTER 1 HR OF OPN WITH NO ABNORMALITIES FOUND. 2 L 7 2 4F A16WE 2001120500187 20011205 00187 NM 2001 12 5 DL73K011692 1 20011020 A 3510 MC1017100 OXYGEN MASK BOEING 737 737247 138448D NM COCKPIT LEAKING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 381DL 23608 FOUND F/O OXYGEN MASK LEAKING WHEN WORKING MSU TO CHECK OXYGEN SYSTEM FOR LEAKS. REPLACED MASK LEAK CHECK NOW GOOD. 2 L 7 2 4F A16WE 2001120500188 20011205 00188 NM 2001 12 5 DL73K011693 1 20011020 A 3510 MC1017100 OXYGEN MASK BOEING 737 737247 138448D NM COCKPIT LEAKING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 381DL 23608 OBSERVERS SEAT OXYGEN MASK BROKEN. FOUND WHEN WORKING MSU TO CHECK FOR OXYGEN SYSTEM LEAKS. REMOVED MASK FROM OBSERVER S POSITION. OBSERVERS SEAT INOP. FWD TO MCO AND PLACARD. 2 L 7 2 4F A16WE 2001120500189 20011205 00189 NM 2001 12 5 DL73K011694 1 20011021 A 3320 LIGHT BOEING 737 737247 138448D NM CABIN INOPERATIVE A DALA D H RETURN TO BLOCK DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 379DL 23606 ON TAXI OUT, F/A NOTED STRONG ELECT SMELL FROM MID OF ACFT ROW 1-15 NIGHT PORTION OF LIGHTS INOP. RETURNED TO GATE. MA INT FOUND NO ELECT SMELL WHEN BACK AT GATE. SUSPECT NIGHT LIGHT TRANSFORMER. PULLED AND CLAMPED C/B FOR LIGHTS AND DEF PER MEL 33-00-02. 2 L 7 2 4F A16WE 2001120500190 20011205 00190 NM 2001 12 5 DL73K011708 1 20011023 A 3221 STRUT BOEING 737 737247 138448D NM NLG OVERSERVICED A DALA K NONE W J B INADEQUATE Q C WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 382DL 23609 ON TAXI IN, THE MASTER CAUTION LIGHT AND THE STALL WARNING AND ISOLATION LIGHTS ON THE OVERHEAD PANEL WERE FLICKERING ON AND OFF. HEARD CIRCUITS POPPING ON AND OFF ON THE C/B PANEL. SMELLED OZONE/BURNING SMELL ON THE TAXI IN. FOUND NOSE STRUT OVERSERVICED. SERVICED NOSE STRUT PER MM. ALL CHECKS GOOD. SUSPECT NOSE STRUT OVERSERVICING. CAUSED CYCLING OF AIR-GROUND RELAY SYSTEM. RAN BOTH ENGINES AND ALL ELECTRICAL SYSTEMS OK. NO ODORS. 2 L 7 2 4F A16WE 2001120500191 20011205 00191 NM 2001 12 5 DL73K011713 1 20011024 A 7830 THRUST REVERSER BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE INOPERATIVE A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 324DL 47421 23096 709154 T/O ABORTED ON 13R AT 120 KNOTS FOLLOWING NR 1 T/R LIGHT FLICKERING AND THEN STEADY. T/O WT 103,00 LBS. LOCKED OUT NR 1 ENGINE REV PER MEL 78-00-01A. FWD TO MCO. 2 L 7 2 4F 4 F RT A16WE E2EA 2001120500192 20011205 00192 NM 2001 12 5 DL73K011718 1 20011024 A 5751 SKIN BOEING 737 737232 1384475 NM AILERON DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 318DL 23090 DAMAGE TO UPPER SKIN OF AILERON. REPAIRED PER ER/A 410406-14. 2 L 7 2 4F RT A16WE 2001120500193 20011205 00193 WP 2001 12 5 2001F00714 1 20011107 A 3350 60030451LB BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 821US 49138 BOS - TWO LOW LEVEL EMERGENCY LIGHTS AND THE AFT CABIN CEILING PANEL EMERGENCY LIGHT WERE INOPERATIVE. MAINTENANCE REPL ACED THE LOW LEVEL BATTERIES AND THE AFT CABIN CEILING LIGHT POWER SUPPLY. (M) 2 L 7 2 4F A6WE 2001120500194 20011205 00194 EA 2001 12 5 2001F00715 1 20011105 A 2560 P4010021 BATTERY CNDAIR CL600 CL6002B19 1900309 EA FLASHLIGHT DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27185 7185 WHILE PERFORMING ROUTINE MAINTENANCE, THE CREW FOND THE F/O EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED THE FLASHLIGHT BATTERY AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2001120500195 20011205 00195 EA 2001 12 5 2001F00716 1 20011110 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7305V 7305 DURING A ROUTINE SERVICE CHECK, THE CREW FOUND A RIGHT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED T HE BULB AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2001120500196 20011205 00196 EA 2001 12 5 2001F00717 1 20011113 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17156 7156 FLT 5772 - CLT-LIT - DURING A PREFLIGHT INSPECTION, THE PILOT REPORTED AN EMERGENCY EXIT FLOOD LIGHT ON THE SERVICE DOOR INOPERATIVE. MAINTENANCE REPLACED THE LIGHT AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2001120500197 20011205 00197 EA 2001 12 5 2001F00718 1 20011113 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17156 7156 FLT 5772 - CLT-LIT - DURING A PREFLIGHT INSPECTION, THE PILOT REPORTED A CABIN DOOR EMERGENCY EXIT FLOOD LIGHT INOPERATI VE. MAINTENANCE REPLACED THE LIGHT AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2001120500198 20011205 00198 NM 2001 12 5 2001F00719 1 20011113 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 448YV 448 DURING A LINE CHECK INSPECTION, THE CREW REPORTED THAT THE NR 1 AND NR 3 CEILING AND LEFT AFT EMERGENCY EGRESS LIGHT WOU LD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT POWER SUPPLY AND NO FURTHER DEFECTS WERE N OTED. (M) 2 H 7 2 4T RT A13NM 2001120500199 20011205 00199 EA 2001 12 5 2001F00720 1 20011114 A 3350 OL3071BPE LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77331 7331 FLT 5772 - LIT-CLT - AFTER LANDING, THE PILOT NOTED THAT THE MAIN CABIN DOOR EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MAI NTENANCE REPLACED THE LIGHT AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2001120500200 20011205 00200 2001 12 5 2001F00721 4 20011116 A 2310 7926140001 COUPLER BOEING 737 7372T4 1384492 NM HF COMM DEFECTIVE A TSAA O OTHER O OTHER CR CRUISE 1 WP 13 808AL 23445 FLT 351 - HNL-JON - DURING THE VERIFICATION PHASE OF FLIGHT AND CHECKING THE HF RADIO SYSTEM, THE NR 1 HF HAD NO TUNE AN D THE TRANSMIT WAS INOPERATIVE. RETURNED TO HNL FOR AN OVERWEIGHT LANDING, VERY LOW SINK RATE. REPLACED NR 1 HF TRANSC EIVER (P/N 6223371001). OPS CHECK ON GROUND WITH SFO AND SELCAL CHECK OK. VERIFICATION FLIGHT REQUIRED. PERFORMED OVE RWEIGHT LANDING INSPECTION IAW FORM M-121. NO DEFECTS NOTED IN PHASE 1 STEP 2A. OK FOR SERVICE. SUBSEQUENTLY, THE HF COUPLER WAS REPLACED (P/N 792-6140-001) AND VERIFIED AS THE CAUSE. AIRCRAFT RETURNED TO SERVICE. REF TSAA0123113. (M) 2 L 7 2 4F A16WE 2001120500201 20011205 00201 NE 2001 12 5 2001F00545 2 20010608 A 7310 200038 VALVE SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE ENGINE INOPERATIVE A R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 52285 704 3251 ELECTRO VALVE INOPERATIVE. MOTOR ENERGIZES BUT VALVE WILL NOT OPEN. THE PROBLEM IS INTERMITTENT. REPLACED WITH NEW UNI T, CORRECTED PROBLEM. (M) 1 G 7 1 3U 3 U H9EU E00054EN 2001120500202 20011205 00202 2001 12 5 2001F00571 4 20010819 A 3422 103002201 GYRO BELL 407 407 1182206 SW INSTRUMENT PANEL FAULTY A ALGA O OTHER M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 03 567AL 53246 FLAG APPEARED IN DIRECTIONAL GYRO DURING CLIMB-OUT. CYCLED DIRECTIONAL GYRO SWITCH WAS HOT TO THE TOUCH, 2-3 SECONDS LA TER LIGHT SMOKE AND SMELL OF BURNING WAS NOTED. INSPECTED C/B PANEL AND INSTRUMENT PANEL FOR BURNED OR ARCED WIRING. N O DEFECTS NOTED. REPLACED DIRECTIONAL GYRO. (M) 1 G 7 1 3U O H2SW 2001120500203 20011205 00203 GL 2001 12 5 2001F00574 2 20010810 A 7250 23053299 TURBINE WHEEL BELL 407 407 1182206 SW ALLSN 250C 250C47B GL TURBINE CORRODED B ALGR O OTHER O OTHER NR NOT REPORTED 1 SW 03 687AL 1706 53366 TURBINE RECEIVED FROM FIELD FOR HOWLING NOISE. REMOVED COMBUSTION SECTION AND FOUND SULFADATION ON 1ST STAGE WHEEL. TH IS TURBINE HAD A ROLLS ROYCE COMBUSTION LINER. WHEEL HAS MISSING AND BROKEN BLADES DUE TO SULFADATION. (M) 1 G 7 1 3U 3 U O H2SW E1GL 2001120500204 20011205 00204 GL 2001 12 5 2001F00575 2 20010822 A 7250 6895801 TURBINE WHEEL BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL ENGINE CORRODED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 02 2025G 986 45690 WHEN TURBINE CAME IN FOR NR 3 AND NR 4 WHEEL CHANGE AND VISUAL INSPECTION ON TURBINE HOT END. NR 1 WHEEL SHOWED EARLY A TTACK OF SULFIDATION. (M) 1 G 7 1 3U 3 U H2SW E1GL 2001120500205 20011205 00205 GL 2001 12 5 2001F00576 2 20010807 A 7250 23053299 TURBINE WHEEL SKRSKY S76 S76 8143010 NE ALLSN 250C 250C30S 03013 GL ENGINE CORRODED B ALGR O OTHER O OTHER NR NOT REPORTED 1 SW 03 707AL 1110 760189 TURBINE CAME IN FOR SHOP VISIT FOR LOW POWER. BEGAN DISASSEMBLY OF TURBINE. REMOVED OUTER COMBUSTION CASE AND FOUND SU LPHIDATION ON 1ST STAGE WHEEL. HAD 1 BLADE MISSING AND SEVERAL BROKEN BLADES. (M) 1 G 7 2 3U 3 U H1NE E1GL 2001120500206 20011205 00206 GL 2001 12 5 2001F00577 2 20010815 A 7250 23053299 BLADE BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL ENGINE CORRODED B ALGR O OTHER O OTHER NR NOT REPORTED 1 SW 03 343AL 1459 51372 DURING DISASSEMBLY TO REPAIR FOR LOW POWER, SULPHIDATION ON FRONT SIDES OF BLADES. (M) 1 G 7 1 3U 3 U H2SW E1GL 2001120500207 20011205 00207 GL 2001 12 5 2001F00578 2 20010810 A 7250 23053299 BLADE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE MISSING A ALGR O OTHER O OTHER NR NOT REPORTED 1 SW 03 687AL 1706 53366 TURBINE RECEIVED FROM FIELD FOR HOWLING NOISE. REMOVED COMBUSTION SECTION AND FOUND SULFADATION ON 1ST STAGE WHEEL. WH EEL HAS MISSING AND BROKEN BLADES DUE TO SULPHADATION. (M) 1 G 7 1 3U 3 U O H2SW E1GL 2001120500209 20011205 00209 GL 2001 12 5 2001F00599 2 20010824 A 7250 6886407 BLADE BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL ENGINE CORRODED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 158H 2974 DURING DISASSEMBLY TO INSPECT FOR HIDDEN DAMAGE. SULFIDATION ON BACK SIDE OF BLADES. ENSURE PROPER APPLICATIONS OF COA TING IS COMPLIED WITH. (M) 1 G 7 1 3U 3 U H2SW E4CE 2001120500210 20011205 00210 CE 2001 12 5 2001F00683 1 20011009 A 5230 DOOR CESSNA 208 208 2073702 CE CARGO DOOR UNSECURE A HSYA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 NM 05 800FE 20800007 BOI - FLT 7861 - ON TAKEOFF ROLL, DOOR WARNING ANNUNCIATOR ILLUMINATED. CARGO NOT SECURED PROPERLY. AIRCRAFT RETURNED TO RAMP WHERE CARGO DOOR WAS CYCLED AND RESECURED. THE AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. (M) 1 H 7 1 3T NT A37CE 2001120500211 20011205 00211 NE 2001 12 5 2001F00689 2 20010413 A 7260 230001303 BEARING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE GEARBOX DAMAGED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 202HN 223 7115 FOUND EXCESSIVE PITTING ON ANNULAR BALL BEARING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 2 3U 3 U H13EU E5NE 2001120500212 20011205 00212 2001 12 5 2001F00692 4 20011009 A 3421 5040017901 GYRO BELL 407 407 1182206 SW COCKPIT INOPERATIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 407SJ 825 53422 HORIZON GYRO INOPERATIVE. WILL NOT CAGE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 1 3U O H2SW 2001120500213 20011205 00213 EU 2001 12 5 2001F00693 1 20010925 A 2432 RG390E BATTERY BOLKMS 117 BK117B2 5626013 EU MAIN DEFECTIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 62LF 47 7163 LEAD ACID BATTERY WILL NOT HOLD CHARGE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 2 3U NC H13EU 2001120500214 20011205 00214 NM 2001 12 5 2001F00694 1 20010901 A 7810 900P2630115106 NOZZLE DOUG MD900 MD900 3027375 NM RT ENGINE CRACKED B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 901CF 856 90000012 RIGHT PRIMARY EXHAUST NOZZLE ASSEMBLY CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M ) 1 G 7 2 3U NC H19NM 2001120500215 20011205 00215 EU 2001 12 5 2001F00695 1 20010919 A 2450 45023500 ELECTRICAL BOX UROCOP EC135 EC135P1 8680990 EU ELECTRICAL SYS SHORTED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 135SJ 122 0054 RIGHT FULL OPT ELECTRICAL MASTER BOX INTERNAL SHORT. APU CIRCUIT BREAKER POPPED, SMOKE EMITTING FROM BOX. REPLACED WIT H NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 2 3U O H88EU 2001120500216 20011205 00216 EU 2001 12 5 2001F00696 1 20010802 A 7931 ZRA25500 TRANSMITTER SNIAS 350 AS350B3 8680954 EU OIL SYSTEM INTERMITTENT B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 392LG 685 3252 OIL PRESSURE TRANSMITTER OPERATES INTERMITTENTLY, NO VEMD INDICATIONS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 1 3U H9EU 2001120600001 20011206 00001 SW 2001 12 6 KBMA88816 1 20010921 A 7722 12444412 INDICATOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL TOT FLUCTUATES A KBMA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 19 73DP 639 2513 SHOWS RAPID RISE IN TEMPERATURE, INSTALLED SERVICEABLE UNIT. 1 G 7 1 3U 3 U H2SW E4CE 2001120600002 20011206 00002 SW 2001 12 6 KBMA88817 1 20010921 A 7921 853499P OIL COOLER BELL 206 206B 1181511 SW ALLSN 250B 250B* GL ENGINE LEAKING A KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 188TV 9985 2704 ENGINE OIL COOLER FANS SHOW TRACES OF FRESH OIL. INSTALLED SERVICEABLE UNIT. 1 G 7 1 3U 3 T H2SW E10CE 2001120600003 20011206 00003 SW 2001 12 6 NUU2001F00000 1 20011112 A 6797 WIRE BELL BELL 430 430 1182150 SW ALLSN 250C 250C40B 03032 NE CYCLIC STICK DAMAGED B NUUY K NONE O OTHER IN INSP/MAINT 1 EA 35 VPBKO 1062 49008 844014 UNCOMMANDED AUTOPILOT DISCONNECT. WHEN PILOT CYCLIC PRESS TO TRANSMIT SWITCH OPERATED. CYCLIC HANDLE WIRING FOUND CUT THROUGH BY THE OPERATION OF THE TRANSMIT TRIGGER. WIRING REPLACED AND REROUTED. CO PILOT CYCLIC HANDLE INSPECTED, WIRI NG FOUND DAMAGED BY THE TRIGGER, WIRING REPLACED AND REROUTED. MANUFACTURER ADVISED. AIRCRAFT RETURNED TO SERVICE. 1 G 7 2 3U 3 U RT H9SW E1GL 2001120600004 20011206 00004 SW 2001 12 6 NXT2001F00000 1 20011026 A 5720 22031830101 BOLT BELL 222 222U 1182140 SW STUB WING ATTACH WORN E NXTA O OTHER O OTHER NR NOT REPORTED 1 SW 19 144CF 47535 INSPECTION FOUND THE STUB WING TO HAVE SLIGHT UP AND DOWN MOVEMENT. REMOVAL OF THE STAB WING FROM THE AIRFRAME REVEALED BOTH UPPER AND LOWER STUB WING ATTACHMENT BOLTS PN 222031830101(UPPER) & PN 222031831101(LOWER). TO HAVE THE LINING MAT ERIAL WORN OFF, ALMOST ALL AROUND THE ENTIRE CIRCUMFERENCE OF THE BOLT. INSPECTION OF THE STUB WING FITTING BUSHINGS FO UND THEY WERE WORN ON BOTH THE BUSHING O.D. & I.D. THIS RESULTED IN THE ATTACHMENT BOLTS BECOMING LOOSE IN THE BUSHING AND THE BUSHING BEING LOOSE IN THE STUB WING FITTING. PROBABLE CAUSE MAY BE A/C AGE AT 10940.3 TT. RECOMMEND BHT REVIS E THE INSPECTION REQUIREMENTS TO INCLUDE ALLOWABLE WEAR/MOVEMENT LIMITS, AND SET INSPECTION INTERVALS.(K) 1 G 7 2 3U H9SW 2001120600005 20011206 00005 SW 2001 12 6 NXT2001F00001 1 20011026 A 5320 222031472101 BUSHING BELL 222 222U 1182140 SW STUB WING FITTNG WORN E NXTA K NONE O OTHER IN INSP/MAINT 1 SW 19 144CF 47535 INSPECTION FOUND THE STUB WING TO HAVE SLIGHT UP & DOWN MOVEMENT. REMOVAL OF THE STUB WING FROM THE AIRFRAME REVEALED B OTH UPPER & LOWER STUB WING ATTACHMENT BOLTS PN 222031830101(UPPER) & PN 222031331101(LOWER) TO HAVE THE LINING MATERIAL WORN OFF, ALMOST ALL AROUND THE ENTIRE CIRCUMFERENCE OF THE BOLTS. INSPECTION OF THE STUB WING FITTING BUSHINGS FOUND THEY WERE WORN ON BOTH THE BUSHING O.D. & I.D. THIS RESULTED IN THE ATTACHMENT BOLTS BECOMING LOOSE IN THE BUSHING AND THE BUSHING BEING LOOSE IN THE STUB WING FITTING. PROBABLE CAUSE MAY BE A/C AGE AT 10940.3 TT. RECOMMEND BHT REVISE TH E INSPECTION REQUIREMENTS TO INCLUDE ALLOWABLE WERE/MOVEMENT LIMITS, AND JET INSPECTION INTERVALS.(K) 1 G 7 2 3U H9SW 2001120600006 20011206 00006 SW 2001 12 6 NXT2001F00002 1 20011026 A 5320 222031831101 BOLT BELL 222 222U 1182140 SW STUB WING ATTACH WORN E NXTA K NONE O OTHER IN INSP/MAINT 1 SW 19 144CF 10940 47535 INSPECTION FOUND THE STUB WING TO HAVE A SLIGHT UP & DOWN MOVEMENT. REMOVAL OF THE STUB WING FROM THE AIRFRAME REVEALED BOTH UPPER & LOWER STUB WING ATTACHMENT BOLTS PN 222031830101(UPPER) & PN 222031331101(LOWER) TO HAVE THE LINING MATERI AL WORN OFF, ALMOST ALL AROUND THE ENTIRE CIRCUMFERENCE OF THE BOLTS. INSPECTION OF THE STUB WING FITTING BUSHINGS FOU ND, THEY WERE WORN ON BOTH THE BUSHING O.D. & I.D. THIS RESULTED IN THE ATTACHMENT BOLTS BECOMING LOOSE IN THE BUSHING AND THE BUSHING BEING LOOSE IN THE STUB WING FITTING. PROBABLE CAUSE MAY BE AIRCRAFT AGE AT 109940.3 TT. RECOMMEND BHT REVISE THE INSPECTION REQUIREMENTS TO INCLUDE ALLOWABLE WEAR/MOVEMENT LIMITS, AND SET INSPECTION INTERVALS.(K) 1 G 7 2 3U H9SW 2001120600007 20011206 00007 EU 2001 12 6 R7M2001F00001 1 20011023 A 2150 060018 BELT SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE AIR CONDITIONER DEBONDED E R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 97LG 490 2917 AIR CONDITIONER DRIVE BELT PN 060018. TT 490.0 ALSO, HYDRAULIC DRIVE BELT PN 704A33690004, TT 490.0 CAUSING IT TO FAIL . BOTH BELTS REPLACED AT THE SAME TIME. THE AIRCRAFT SUSTAINED A HARD LANDING WITH SOME DAMAGE TO THE MAIN LANDING GEA R. THE AIRCRAFT IS NOT ABLE TO BE CONTROLLED WITHOUT HYDRAULIC POWER FOR MORE THAN A VERY SHORT TIME. MAINTENANCE PERS ONNEL INDICATE AT A PREVIOUS MAINTENANCE EVENT ON ANOTHER AIRCRAFT (AS350B3), A IFS A/C BELT WAS FOUND TO BE DEBONDING W ITH ONLY APPROXIMATELY 200 HOURS TT. RUN DATE 10/24/2001, 5:33 P.M. 1 G 7 1 3U 3 U H9EU E19EU 2001120600008 20011206 00008 EU 2001 12 6 R7M2001F00002 1 20011023 A 2913 704A33690004 BELT SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE HYD DRIVE FAILED E R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 97LG 490 2917 INTEGRATED FLIGHT SYSTEMS AIR CONDITIONER DRIVE BELT PN 060018, TT:490.0. HYDRAULIC DRIVE BELT PN 704A33690004, TT:490 SUSPECTED IFS AC DRIVE BELT FAILED DUE TO DEBONDING AND SUBSEQUENTLY DAMAGED THE AIRCRAFT HYDRAULIC DRIVE BELT CAUSING IT TO FAIL. BOTH BELTS REPLACED AT THE SAME TIME 490.0 HOURS PREVIOUSLY. THE AIRCRAFT SUSTAINED A HARD LANDING WITH SO ME DAMAGE TO THE MAIN LANDING GEAR. THE AIRCRAFT IS NOT ABLE TO BE CONTROLLED WITHOUT HYDRAULIC POWER FOR MORE THAN A V ERY SHORT TIME. MAINTENANCE PERSONNEL INDICATE AT A PREVIOUS MAINTENANCE EVENT ON ANOTHER AIRCRAFT (AS350B3). AN IFS AC BELT WAS FOUND TO BE DEBONDING WITH ONLY APPROXIMATELY 200 HOURS TT. RUN DATE 10/24/2001 5:33 PM. 1 G 7 1 3U 3 U H9EU E19EU 2001120600009 20011206 00009 2001 12 6 R7MA33660 4 20010827 A 3457 0110028000 GPS BELL 407 407 1182206 SW ALLSN 250C 250C47B GL COCKPIT INOPERATIVE E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 407SJ 735 53422 UNIT INOPERATIVE. SKIPS PAGE 3. UPDATE WITH MOST RECENT SOFTWARE PATCHES. REPLACED WITH NEW UNIT CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2001120600010 20011206 00010 2001 12 6 R7MA33662 4 20010815 A 3421 5040017901 GYRO BELL 407 407 1182206 SW ALLSN 250C 250C47B GL HORIZON INTERMITTENT E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 407SJ 711 53422 UNIT OPERATES INTERMITTENTLY. REPLACED WITH NEW UNIT CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2001120600011 20011206 00011 2001 12 6 R7MA33663 4 20010815 A 3416 0660303101 ALTIMETER BELL 407 407 1182206 SW RADAR ALT INTERMITTENT E R7MA K NONE L NO TEST IN INSP/MAINT 1 NM 07 407SJ 711 53422 UNIT OPERATES INTERMITTENTLY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U O H2SW 2001120600012 20011206 00012 2001 12 6 R7MA33671 4 20010813 A 3454 071010520000 TRANSMITTER SNIAS 350 AS350B2 8680813 EU MAGNETIC INOPERATIVE E R7MA K NONE L NO TEST IN INSP/MAINT 1 NM 07 92LG 4414 2575 UNIT INOPERATIVE. CAUSES HSI TO PRECESS WHILE SLAVED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 2001120600013 20011206 00013 EU 2001 12 6 R7MA33674 1 20010818 A 2840 L316M30C1002 DISPLAY UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE COCKPIT MISSING E R7MA K NONE L NO TEST IN INSP/MAINT 1 NM 07 135N 297 0086 DISPLAY SEGMENTS MISSING AT MAIN FUEL QUANTITY. MORE SEGEMENTS MISSING AT NUMBER 1 TORQUE INDICATION. HORIZONTAL LINE OF LIGHTS MISSING ON UPPER DISPLAY AT THE SECOND CAUTION ROW. REPLACED WITH NEW UNIT CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2001120600014 20011206 00014 NM 2001 12 6 0104466642 1 20011030 A 5412 BULKHEAD BOEING 747 747212B 1384886 NM CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 642NW 21942 During "H" check found 2 1/4 inch crack in number 3 pylon rear engine mount bulkhead frame assembly. Repaired per EA 66- 185922. 2 L 7 4 4F A20WE 2001120600015 20011206 00015 2001 12 6 R7MA33675 4 20010829 A 3160 L316M30C1003 DISPLAY UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE COCKPIT INOPERATIVE E R7MA K NONE L NO TEST IN INSP/MAINT 1 NM 07 135N 311 0086 LOWER DISPLAY, TOP LINE LEFT SIDE IS UNREADABLE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2001120600016 20011206 00016 GL 2001 12 6 R7MA33681 2 20010815 A 7532 23005366 BLEED VALVE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL COMPRESSOR LEAKING E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 407SJ 664 53422 LEAKING AIR BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2001120600017 20011206 00017 GL 2001 12 6 R7MA33684 2 20010815 A 7240 23030911 COMBUST CHAMBER BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE DAMAGED E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 407SJ 711 53422 CAE847459 BURNER DRAW VALVE WAS NOT COATED WITH ANTI-SEIZE FROM THE FACTORY. DURING REMOVAL OF THE VALVE, THREAD DAMAGE OCCURRED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2001120600018 20011206 00018 NE 2001 12 6 R7MA33689 2 20010710 A 7321 0164248770 FUEL CONTROL SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1B2 60030 NE ENGINE WORN E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 92LG 4377 2575 ESCESSIVE SPLINE WEAR. 1 G 7 1 3U 3 U H9EU E19EU 2001120600019 20011206 00019 EU 2001 12 6 2001F00538 1 20010725 A 2121 011648000 COOLING FAN UROCOP EC135 EC135P1 8680990 EU INST PANEL INOPERATIVE A R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 426AE 20 EC1350159 PROPIMAX FAN INOPERATIVE. FAN WILL NOT ROTATE WHEN POWER APPLIED. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M) 1 G 7 2 3U O H88EU 2001120600021 20011206 00021 NE 2001 12 6 2001F00690 2 20010701 A 7230 430124203 BEARING BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ENGINE DAMAGED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 625MB 304 7108 FOUND EXCESSIVE PITTING ON ANNULAR BALL BEARING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 2 3U 3 U H13EU E5NE 2001120600022 20011206 00022 NE 2001 12 6 2001F00691 2 20010421 A 7230 430151801 BEARING BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ENGINE DAMAGED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 625MB 257 7108 FOUND EXCESSIVE PITTING ON CYLINDER ROLLER BEARING NR 2. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 2 3U 3 U H13EU E5NE 2001120600023 20011206 00023 NM 2001 12 6 SWAA013248 1 20011204 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 653SW 28398 DURING SCHEDULED C1 CHECK, FOUND SEVERAL EEPLS COVERS CRACKED IN FWD CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM. 2 L 7 2 4F RT A16WE 2001120600024 20011206 00024 NM 2001 12 6 SWAA013249 1 20011203 A 5320 6517582 BEAM BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 183, WL 232 AND RBL 17.1. REMOVED AND REPLACED WEB P ER SRM. 2 L 7 2 4F A16WE 2001120600025 20011206 00025 NM 2001 12 6 SWAA013250 1 20011204 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 14R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001120600026 20011206 00026 NM 2001 12 6 SWAA013251 1 20011204 A 5310 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED 1/4D CHECK, FOUND FRAME SHEAR TIES CRACKED (2 EA) AT BS 360 BETWEEN STRS 13L AND 15L. REPAIRED SHEAR T IES PER SRM. 2 L 7 2 4F RT A16WE 2001120600027 20011206 00027 NM 2001 12 6 SWAA013253 1 20011203 A 5330 6545765 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 665WN 23497 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, BELOW STR 12L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001120600028 20011206 00028 NM 2001 12 6 SWAA013254 1 20011204 A 3250 6596288 COLLAR BOEING 737 7373H4 1384600 NM NLG WORN A SWAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 07 396SW 27690 NOSE WHEEL STEERING FAILED DURING START OF T/O ROLL, TILLER JAMMED TO THE LEFT, WAS PHYSICALLY UNABLE TO MOVE IT TO NEUT RAL OR TO THE RIGHT. REMOVED AND REPLACED STEERING COLLAR ASSY AND BEARINGS PER MM ANDSWA RA, ALSO REMOVED AND REPLACED UPPER AND LOWER LINKS PER MM. 2 L 7 2 4F RT A16WE 2001120600029 20011206 00029 EU 2001 12 6 R7MA33696 1 20010910 A 2150 0500847 BLOWER SNIAS 350 AS350B3 8680954 EU BLOWER INOPERATIVE E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 52281 862 3249 UNIT INOPERATIVE. CAUSES FEEDBACK IN PILOT HEADSET. POSSIBLE SHIELDING PROBLEM. REPLACED WITH NEW UNIT, CORRECTED PRO BLEM. 1 G 7 1 3U H9EU 2001120600030 20011206 00030 NM 2001 12 6 R7MA33713 1 20010824 A 6300 900C2010183107 LINK DOUG MD900 MD900 3027375 NM PWA PW206 PW206A NE MAIN ROTOR WORN E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 901CF 4952 90000012 WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U NC H19NM E42NE 2001120600031 20011206 00031 NM 2001 12 6 R7MA33716 1 20010817 A 7921 312110901 TUBE DOUG MD900 MD900 3027375 NM PWA PW206 PW206A NE OIL SYSTEM LEAKING E R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 07 901CF 4938 90000012 LEAKING BEYOND SERVICEABLE LIMITS. TUBE IS NO BENT BUT IS LEAKING FROM THE SWEDGE AND BRAZING AT (T) END. REPLACED WIT H NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U NC H19NM E42NE 2001120600032 20011206 00032 GL 2001 12 6 2001F00697 2 20010822 A 7320 1564T1005 ACTUATOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL FUEL CONTROL INTERMITTENT B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 485EC 322 S754 THROTTLE TRIM LINK ACTUATOR, OPERATES INTERMITTENTLY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 2 3U 3 U H3EU E4CE 2001120600033 20011206 00033 2001 12 6 R7MA33719 4 20010618 A 3160 10648BH151 SWITCH BELL 407 407 1182206 SW ALLSN 250C 250C47B GL COCKPIT STUCK E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 911LN 453 53446 STUCK IN MANUAL MODE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2001120600034 20011206 00034 SW 2001 12 6 R7MA33720 1 20010519 A 7160 470632 VALVE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL AIR INTAKE STUCK E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 911LN 371 53446 STUCK IN OPEN POSITION. REPLACED WITH NEW UNIT CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2001120600036 20011206 00036 NM 2001 12 6 2001F00698 1 20010919 A 5320 900R1103001113 BEAM DOUG MD900 MD900 3027375 NM FUSELAGE SEPARATED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 901CF 689 90000012 BUMPER ASSEMBLY FLEXBEAM SEPARATION ALONG TRAILING EDGE OF 'Y'. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 2 3U NC H19NM 2001120600037 20011206 00037 NM 2001 12 6 2001F00699 1 20010824 A 5320 900R1103001113 BEAM DOUG MD900 MD900 3027375 NM FUSELAGE SEPARATED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 901CF 1430 90000012 BUMPER ASSEMBLY FLEXBEAM SEPARATION AT TRAILING EDGE OF 'Y'. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 2 3U NC H19NM 2001120600038 20011206 00038 SW 2001 12 6 R7MA33724 1 20011113 A 6510 407340339103 BEARING BELL 407 407 1182206 SW ALLSN 250C 250C47B GL TAIL ROTOR WORN E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 407SJ 648 53422 WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2001120600039 20011206 00039 SW 2001 12 6 R7MA33725 1 20010705 A 6510 407340339103 BEARING BELL 407 407 1182206 SW ALLSN 250C 250C47B GL TAIL ROTOR WORN E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 407SJ 648 53422 WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2001120600040 20011206 00040 EU 2001 12 6 2001F00700 1 20010604 A 7334 9550162490 PRESSURE SWITCH BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE FUEL SYSTEM FAILED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 117SU 1313 7527 PRESSURE SWITCH INOPERATIVE. WILL NOT SWITCH LIGHT OFF WHEN THERE IS FUEL PRESSURE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 2 3U 3 U NC H13EU E19EU 2001120600041 20011206 00041 GL 2001 12 6 R7MA33726 2 20011113 A 7320 23056915 SENSOR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL T1 INOPERATIVE E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 407SJ 648 53422 UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2001122000011 20011220 00011 NM 2001 12 20 01FDEA01035 1 20011204 A 5330 SKIN BOEING 727 727233 138408A NM FUSELAGE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 285FE 22622 BS 720D+12, STR 19L SKIN PITTED AND WORN FROM FAIRING (C53-100-01). REMOVED AND REPLACED SKIN PER SRM 53-30-3 PER FIG 1 4. 2 L 7 3 4F RT A3WE 2001120600042 20011206 00042 EU 2001 12 6 2001F00701 1 20010416 A 7710 9550168670 SENSOR SNIAS 350 AS350B3 8680954 EU ENGINE FAULTY B R7MR O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 103LN 977 3128 N2 SENSOR PICK-UP INTERMITTENT FAILURE CODES. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 1 3U H9EU 2001120600043 20011206 00043 SW 2001 12 6 R7MA33727 1 20011113 A 2400 MS24509A10 SWITCH BELL 407 407 1182206 SW ALLSN 250C 250C47B GL COCKPIT STUCK E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 407SJ 711 53422 STICKS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2001120600044 20011206 00044 NE 2001 12 6 R7MA33729 2 20011113 A 7230 410105262 IMPELLER BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE COMPRESSOR CRACKED E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 158BK 8187 7058 CRACKED COMPRESSOR IMPELLER BLADE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2001120600045 20011206 00045 EU 2001 12 6 2001F00702 1 20010807 A 7334 9550171990 PRESSURE SWITCH SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE FUEL SYSTEM INOPERATIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 392LG 477 3252 LOW FUEL PRESSURE SWITCH IS INOPERATIVE. PIN 1 AND 2 FAILED CLOSING PSI. PIN 1 AND 3 NOTHING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 1 3U 3 U H9EU E19EU 2001120600046 20011206 00046 EU 2001 12 6 2001F00703 1 20010416 A 7334 9550171990 PRESSURE SWITCH SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE FUEL SYSTEM INTERMITTENT B R7MR O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 103LN 227 3128 LOW FUEL PRESSURE SWITCH INTERMITTENT WARNING LIGHT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 1 3U 3 U H9EU E00054EN 2001120600047 20011206 00047 2001 12 6 R7MA33732 4 20010918 A 3457 0110028000 GPS BELL 407 407 1182206 SW ALLSN 250C 250C47B GL COCKPIT INOPERATIVE E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 407SJ 778 53422 WILL NOT TRANSMITT, BUT WILL RECEIVE. REPLACED WITH LOANER UNIT CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2001120600048 20011206 00048 NE 2001 12 6 R7MA33740 2 20010906 A 7412 9550173220 EXCITER SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE ENG IGNITION INOPERATIVE E R7MA K NONE L NO TEST IN INSP/MAINT 1 NM 07 52285 832 3251 22036 UNIT INOPERATIVE WHEN HOT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E00054EN 2001120600049 20011206 00049 NM 2001 12 6 DL738011858 1 20011125 A 2120 SMOKE BOEING 737 737832 13844CF NM COCKPIT DETECTED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 379DA 30349 005393 SMOKE ENTERED COCKPIT WHEN PACKS SELECTED. NO SMOKE NOTED IN CABIN. APU PRESS WEAK IN SLC, JUST ENOUGH TO START ENGINE S. SMOKE HAD ODD ODOR (SWEET). DE-ICED IN SLC. OPERATED RT/LT PACKS WITH APU. NO SMOKE OR ODOR NOTED. ALL PACK INDI CATIONS CHECK OK. 2 L 7 2 4F RT A16WE 2001120600050 20011206 00050 2001 12 6 R7MA33743 4 20010711 A 3160 066031252600 DISPLAY UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE COCKPIT INOPERATIVE E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 135N 250 0086 UNIT INOPERATIVE. JAGGED VERTICAL LINE DOWN THROUGH CENTER OF DISPLAY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2001120600051 20011206 00051 NE 2001 12 6 R7MA33745 2 20010525 A 7240 408209401 LOCKING CUP BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ENGINE WORN E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 117NY 6034 7110 WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2001120600052 20011206 00052 NE 2001 12 6 R7MA33788 2 20011117 A 7250 411100720 SHROUD BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE GAS PRODUCER WORN E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 911BY 6728 7127 LE45134EA EXCESSIVE GP BLADE TIP RUB. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2001120600053 20011206 00053 NM 2001 12 6 DL73K011737 1 20011030 A 2916 6544546382 DRAIN LINE BOEING 737 737232 1384475 NM RESERVOIR DAMAGED A DALA K NONE J WARNING INDICATION LD LANDING 1 SO 27 315DL 23087 ON EXTENSION OF LANDING GEAR ENG 1 AND 2 HYD SYSTEMS LOW PRESSURE LIGHTS CAME ON. HYD PRESSURE A WENT TO ZERO AND HYD Q UANT APPEARED TO GO TO ZERO. CHANGED BOTH CASE DRAIN FILTERS BOTH WERE CLEAN. OPERATED ALL FLT CONTROLS AND LANDING GE AR CYCLED WITH GEAR PINS INSTALLED, NO LEAKS. HYD QUANTITY WAS FULL. FOUND HYD HEAD PRESS AT ZERO. REPAIRED RSVR DRAI N TUBE. RAN ENGINES AND CHECKED PUMPS, ALL OK. 2 L 7 2 4F RT A16WE 2001120600055 20011206 00055 NM 2001 12 6 DL73K011739 1 20011031 A 5312 6546568578 BULKHEAD BOEING 737 737232 1384475 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 327DL 23099 CORROSION WAS FOUND ON THE WEB, Y-CHORD AND STIFFENER OF THE FS 1016 BULKHEAD. THE CORRODED AREAS WERE CUT OUT AND REPA IRS INSTALLED. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001120600056 20011206 00056 2001 12 6 R7MA33832 4 20011011 A 2300 9910951 TRANSCEIVER BELL 407 407 1182206 SW COCKPIT INOPERATIVE E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 107LN 105 53483 BACK LIGHT TOO DIM TO READ DISPLAY. REPLACED WITH LOANER UNIT SN JD1022 CORRECTED PROBLEM. 1 G 7 1 3U O H2SW 2001120600057 20011206 00057 2001 12 6 R7MA33894 4 20011009 A 3422 060001500 GYRO BELL 407 407 1182206 SW ALLSN 250C 250C47B GL COCKPIT PRECESSES E R7MA K NONE L NO TEST IN INSP/MAINT 1 NM 07 407SJ 825 53422 45312 UNIT INOPERATIVE. PRECESES. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2001120600058 20011206 00058 NM 2001 12 6 DL73K011740 1 20011030 A 5230 6546921528 DOOR FRAME BOEING 737 737232 1384475 NM CARGO DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 321DL 23093 FWD CARGO DOOR LWR FWD AND AFT FRAMES WERE FOUND CRACKED. REPAIRED PER ER/A 410587-14AD. 2 L 7 2 4F RT A16WE 2001120600059 20011206 00059 GL 2001 12 6 R7MA36679 2 20010815 A 7240 6854255 VALVE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE DAMAGED E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 407SJ 711 53422 CAE847459 THREADS NOT TREATED WITH LOCK-TITE PRIOR TO RE INSTALLATION INTO THE OUTER COMBUSTION CASE, WHICH RESULTED IN THREAD DAM AGE TO THE CASE ITSELF. THE REMOVED VALVE WAS LOST IN SHIPPING. REPLACED WITH NEW UNIT CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2001120600060 20011206 00060 NM 2001 12 6 DL73K011782 1 20011107 A 5553 ATTACH FITTING BOEING 737 737232 1384475 NM VERTICAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 321DL 23093 CORROSION WAS FOUND IN THE VERTICAL STABILIZER ATTACH LUG BORES. ER/A 398140-14AD. 2 L 7 2 4F RT A16WE 2001120600061 20011206 00061 NM 2001 12 6 DL73K011784 1 20011102 A 5511 STRINGER BOEING 737 737232 1384475 NM HORIZ STAB DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 307DL 23079 LT AND RT HORIZONTAL STABILIZER UPPER SKIN PANEL STRINGER DELAMINATION. REPAIRED PER ERA 410394-14. 2 L 7 2 4F RT A16WE 2001120600062 20011206 00062 NM 2001 12 6 DL73K011806 1 20011114 A 2530 9550168670 COFFEEMAKER BOEING 737 737232 1384475 NM GALLEY MALFUNCTIONED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 305DL 23077 AFT COFFEEMAKER HAD SMALL AMOUNT OF SMOKE REPORTED BY FLT ATTENDANT. COFFEEMAKER TURNED OFF, SMOKE STOPPED. REQUESTED INSPECTION OF COFFEMAKER. INSPECTED WIRING AT COFFEEMAKERES 1 AND 2, ALL OK. COULD NOT DETERMINE 1 OF 2 INOP. PULLED AND COLLARED 1 AND 2 COFFEEMAKER C/B'S. FWD TO MCO, PLAC PER MEL 25-00-10. AFT COFFEEMAKERS INOP. 2 L 7 2 4F RT A16WE 2001120600063 20011206 00063 NM 2001 12 6 DL73K011817 1 20011108 A 5247 6550904271 DOOR BOEING 737 737247 138448D NM APU DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 376DL 23603 APU DOOR HOLE IN OUTER SKIN. REPAIRED PER SRM 52-00-3 FIG 6. 2 L 7 2 4F A16WE 2001120600064 20011206 00064 NM 2001 12 6 DL73K011821 1 20011117 A 3350 20131 BATTERY PACK BOEING 737 737232 1384475 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 315DL 23087 ON LAYOVER CK FOUND L1 AND R1 DOOR SMALL EXIT SIGNS AND EMERGENCY FLOOR PATH LIGHTS OUT FROM FWD GALLEY THRU ROW 4. REP LACED BATTERY PACK AT M9221. ALL EMERGENCY LIGHTS NOW TEST NORMALLY. 2 L 7 2 4F RT A16WE 2001120600065 20011206 00065 NM 2001 12 6 DL73K011826 1 20011115 A 5330 6545768238 SKIN BOEING 737 737232 1384475 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 321DL 23093 DENT DAMAGE WAS FOUND DURING HMV ON THE FUSELAGE SKIN AT FS 440 AND STR 22R TO 24R. A PREVIOUS DOUBLER REPAIR WAS LOCAT ED IN THE AREA, THEREFORE THE PREVIOUS REPAIR WAS REMOVED AND A NEW DOUBLER/TRIPLER REPAIR WAS INSTALLED. ER/A 257875-1 4, REV E. 2 L 7 2 4F RT A16WE 2001120600066 20011206 00066 NM 2001 12 6 DL73K011834 1 20011120 A 2121 M215201 GASPER FAN BOEING 737 737232 1384475 NM CARGO BAY FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 323DL 23095 DESCENDING THROUGH 10K SMELLED AN ELECTRICAL OR OZONE ODOR. TURNED OFF GASPER FAN AND GALLEY POWER FUMES DISSIPATED. R EPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 2001120600067 20011206 00067 NM 2001 12 6 DL73K011846 1 20011123 A 3350 BPS73 POWER SUPPLY BOEING 737 737247 138448D NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 373DL 23520 2L EMERGENCY EXIT LIGHT INOP. REPLACED POWER SUPPLY. 2 L 7 2 4F A16WE 2001120600068 20011206 00068 NM 2001 12 6 DL73K011862 1 20011126 A 5551 ATTACH FITTING BOEING 737 737232 1384475 NM HORIZ STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 322DL 23094 SEVERAL OF THE BORES AND FACES OF THE LT AND RT ATTACH LUGS ON THE HORIZONTAL STABILIZER WERE FOUND CORRODED. THE DAMAG E WAS CLEANED UP AND OVERSIZED BUSHINGS WERE INSTALLED. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001120600069 20011206 00069 NM 2001 12 6 DL73K011863 1 20011126 A 5551 ATTACH FITTING BOEING 737 737232 1384475 NM HORIZ STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 322DL 23094 THE HORIZONTAL STABILIZER CLEVIS ATTACH LUGS WERE FOUND CORRODED ON THE FACES AND BORES. THE DAMAGE WAS CLEANED UP AND OVERSIZED BUSHINGS WERE INSTALLED. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001120600070 20011206 00070 NM 2001 12 6 DL73K011864 1 20011126 A 5551 ATTACH FITTING BOEING 737 737232 1384475 NM HORIZ STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 322DL 23094 THE REAR SPAR UPPER CLEVIS FITTING OF THE HORIZONTAL STAB WAS FOUND CORRODED. THE DAMAGE WAS REMOVED AND OVERSIZED BUSH INGS WERE INSTALLED. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001120600071 20011206 00071 NM 2001 12 6 DL73K011865 1 20011124 A 2430 B451 CIRCUIT BREAKER BOEING 737 737247 138448D NM ELECTRICAL SYS DEFECTIVE A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 27 378DL 23605 ON PUSHBACK ENG START NR 2 GEN ON LINE POWER DUMPED AND ALL FUEL PUMPS C/BS POPPED EXCEPT AFT NR 1 LOW PRESS LIGHTS AND NO PWR ON TR 2 & 3. CHECKED C/BS FOUND SEVERAL OPEN. RESET C/BS, OPN GOOD ON CLIMBOUT PASSING FL200 A/P DISCONNECTED S AME IND BEFORE FUEL LOW PRESS LIGHTS TR 2 & 3, 0 VOLTS NO 2 RADIO, NO F/O NAV, NO STAB TRIM, NO RT SIDE PITOT HEAT OR AN TI-ICE. REPLACED NR 2 GEN BREAKER AND GCU OPS CKS ON ENG RUN. 2 L 7 2 4F A16WE 2001120600072 20011206 00072 NM 2001 12 6 DL757011654 1 20011011 A 3350 BPS73 CHARGER BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 631DL 23612 R-2 DOOR EXT EMERGENCY LIGHT INOP. REPLACED BATTERY CHARGER. OP CHECKS GOOD. 2 L 7 2 4F RT A2NM 2001120600073 20011206 00073 NM 2001 12 6 DL757011662 1 20011013 A 3260 LIGHT BOEING 757 757232 1384965 NM COCKPIT MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 SO 27 648DL 24372 ON APPROACH, PLACED GEAR HANDLE DOWN, DID NOT GET LEFT GEAR SAFE LIGHT. LIGHT TESTED GOOD. RAN GEAR LIGHT DISAGREEMENT CHECKLIST. IT FELT AS IF THE LEFT MAIN GEAR CAME DOWN AT THAT TIME, BUT NO GREEN LIGHT AND WOULD NOT TEST. COULD NOT RELAMP EASILY. REPLACED GREEN DOWN LIGHT ASSEMBLY. LUBED LT AND RT MAIN GEARS. PERFORMED GEAR SWING PER MM. OPS CHEC K NORMAL. 2 L 7 2 4F RT A2NM 2001120600074 20011206 00074 NM 2001 12 6 DL757011664 1 20011014 A 3350 BPS73 CHARGER BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 676DL 25981 ON LAYOVER, FOUND SOME EMERGENCY LIGHTS INOP. REPLACED BATTERY CHARGER. 2 L 7 2 4F RT A2NM 2001120600075 20011206 00075 NM 2001 12 6 DL757011683 1 20011017 A 2560 61020 POWER UNIT BOEING 757 757232 1384965 NM FLASHLIGHT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 684DA 27104 POWER UNIT, EMERGENCY FLASHLIGHT IS LOW BY R2 DOOR. REMOVED AND REPLACED POWER UNIT PER MM, CHECK OKAY. 2 L 7 2 4F RT A2NM 2001120600077 20011206 00077 SW 2001 12 6 R7MR33699 1 20010927 A 6320 407040006107 TRANSMISSION BELL 407 407 1182206 SW MAIN ROTOR MAKING METAL A R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 107LN 55 53483 MAKING METAL. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U O H2SW 2001120600078 20011206 00078 EU 2001 12 6 RYMA33656 1 20010829 A 6320 4638001001 TRANSMISSION BOLKMS 105 BO105CBS 5626008 EU ALLSN 250C 250C20 03013 GL MAIN ROTOR FAILED E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 105LC 7646 S789 MAKING METAL. TWO PRIOR PROBLEMS WITH MM WERE REPAIRED UNDER WARRANTY BY MFG. REPLACED WITH NEW UNIT CORRECTED PROBLEM . 1 G 7 2 3U 3 U NC H3EU E4CE 2001120600079 20011206 00079 NE 2001 12 6 VE32001F00000 2 20011002 A 7297 70BM035420 MODULE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE ENGINE FAILED A VE3R K NONE O OTHER IN INSP/MAINT 1 WP 23 226LA 10522 3310 9698 MO2 AND MO3 WERE REPLACED ON ENG. GRND RUNS WERE PERFORMED. VIBR TESTS AT FRONT AND RR PNTS WERE NML. OIL PRESS TESTS WERE NML. OIL FLOW AT RR BRG WAS MEAS AT 180 ML. NO FUEL OR OIL LKS NOTED ON ANY OF GRND RUNS. AT APPROX. 1000 FT AGL, AND ENG CHIP LIGHT ILLUMINATED, AFTER WHICH PILOT INITIATED LANDING. DURING DESCENT, BURNING SMELL WAS NOTED IN CO CKPIT, AND APX. 70FT AGL FIRE AND GEN CAUTION LTS ILLUMINATED. AC LANDED WITH FIRE BURNING IN ENG COMPARTMENT, WHICH WAS EXT USING AC FIRE EXT. INSP PRIOR TO T/D REVEALED THREE THINGS: OIL WAS EVIDENT AT REAR BRG AREA AND ON OUTSIDE O F M04. ENG WAS MOTORED AND NOISE CAME FROM REAR BRG AREA. MTL CHIPS FOUND AT RR BRG SCAVENGE CHIP DET AND IN SCREEN. 1 G 7 1 3U 3 U H9EU E19EU 2001120600080 20011206 00080 NM 2001 12 6 DL757011687 1 20011019 A 3510 MS938505 O-RING BOEING 757 757* NM COCKPIT LEAKING A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 900PC 28446 CREW O2 AFTER TAKEOFF DROPPED AT A RATE OF 10 PSI PER MIN. AT TAKEOFF O2 LEVEL WAS 1850 AFTER 2 HRS OF FLT O2 HAD DROPP ED TO 1380 PSI. FOUND BOTTLE REGULATOR FITTING LEAKING. REPLACED FITTING O-RING SEAL, SERVICED BOTTLE TO 1760 PSI AND LEAK CHECKS OK. 2 L 7 2 4F RT A2NM 2001120600081 20011206 00081 NE 2001 12 6 DL757011690 2 20011020 A 7200 PW2037RTC ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 FAILED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 649DL 39634 24389 716510 NR 2 ENG LOST OIL PRESS ON T/O ROLL. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001120600082 20011206 00082 NM 2001 12 6 DL757011703 1 20011022 A 2120 ODOR BOEING 757 757232 1384965 NM CABIN DETECTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 617DL 22907 FUMES REPORTED FROM REAR OF CABIN. INSPECTED AFT GALLEY AREA, NO PROBLEM FOUND INCLUDING COFFEEMAKERS AND POTABLE WATER COMPRESSOR. 2 L 7 2 4F RT A2NM 2001120600083 20011206 00083 NM 2001 12 6 DL757011710 1 20011023 A 3397 CONNECTOR BOEING 757 757232 1384965 NM CABIN LOOSE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 6700 30337 WHITE AISLE SIDE EMERGENCY LIGHT INOP SEAT ROW 5CD. SECURED LOOSE CONNECTION. 2 L 7 2 4F RT A2NM 2001120600084 20011206 00084 2001 12 6 DL757011735 4 20011030 A 2565 D30654131 SLIDE BOEING 757 757232 1384965 NM R1 DOOR FAILED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 633DL 23614 SLIDE PACK FAILED TO DEPLOY WHEN DOOR OPENED WITH SLIDE ENGAGED. FOUND SLIDE DEPLOY MECHANISM LOCATED ON SLIDE PACK JAM MED NOT ALLOWING DEPLOYMENT. REPLACED SLIDE PACK WITH PART BORROWED FROM UAL. 2 L 7 2 4F RT A2NM 2001120600085 20011206 00085 NM 2001 12 6 DL757011744 1 20011101 A 2530 ODOR BOEING 757 757232 1384965 NM FWD GALLEY DETECTED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 643DL 23997 ELECTRICAL BURN ODOR COMING FROM FORWARD GALLEY. UTILITY BUSES TURNED OFF IN FLIGHT. RE-APPLIED POWER, FULLY LOADED GA LLEY POWER. DEMAND OPS OK, NO FURTHER ODOR NOTED. 2 L 7 2 4F RT A2NM 2001120600086 20011206 00086 NM 2001 12 6 DL757011766 1 20011105 A 5754 SPAR BOEING 757 757232 1384965 NM L/E SLAT DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 602DL 22809 NR 9 SLAT NOSE BEAM SPAR WAS FOUND WITH SEVERAL DAMAGED FASTENER HOLES. REPAIR PER ER/A 410486-14. 2 L 7 2 4F RT A2NM 2001120600087 20011206 00087 2001 12 6 DL757011786 4 20011110 A 2565 S416N205 PIN BOEING 757 757232 1384965 NM ESCAPE SLIDE BENT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 617DL 22907 AFTER TAXI IN LEFT EMERGENCY ESCAPE TEST LIGHT (P61) ON ALL THE TIME. REPLACED P61 PANEL, NO HELP. RE-INSTALLED ORIG. REPLACED RELAY K10486, NO HELP. RE-INSTALLED SIDEWALL AND BOTH HATCHES, REMOVED FOR ACCESS TO P78 PANEL. INSPECTED CA NNON PLUG ON PRESSURE BOTTLE FOR EMERGENCY ESCAPE FOUND PIN BENT. STRAIGHTEN PIN, OPS TEST NORMAL. NO MESSAGES. 2 L 7 2 4F RT A2NM 2001120600088 20011206 00088 NM 2001 12 6 DL757011792 1 20011112 A 2560 P20700030 BATTERY BOEING 757 757232 1384965 NM FLASHLIGHT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 614DL 22821 L-1 DOOR FLASHLIGHT BATTERY LOW. REPLACED FLASHLIGHT ASSY, OPS NORMAL. 2 L 7 2 4F RT A2NM 2001120600089 20011206 00089 NM 2001 12 6 DL757011795 1 20011112 A 3242 AHA1884 BRAKE ASSY BOEING 757 757232 1384965 NM NR 4 MLG FIRE A DALA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 SO 27 646DL 24217 UPON ARRIVAL AT GATE C08 NR 4 MLG BRAKE ASSY ON FIRE. EXTINGUISHED WITH DRY CHEMICAL EXTINGUISHER. BRAKE TEMP IN COCKP IT READS 3 WITH BLUE BOX. NR 8 MAIN TEMP READS 3 WITH WHITE BOX. ALL OTHER BRAKE TEMPS INDICATE 1 OR 2. REPLACED BRAK E ASSEMBLY. 2 L 7 2 4F RT A2NM 2001120600090 20011206 00090 NM 2001 12 6 DL757011823 1 20011117 A 3350 334202645 LIGHT BOEING 757 757232 1384965 NM CABIN DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 604DL 22811 LIGHT ASSY DAMAGED. REPLACED LIGHT ASSY. 2 L 7 2 4F RT A2NM 2001120600091 20011206 00091 NM 2001 12 6 DL757011830 1 20011119 A 2560 P4010021 BATTERY BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 673DL 25978 EMERGENCY FLASHLIGHT BATTERY INOP IN MID GALLEY. REPLACED BATTERY. 2 L 7 2 4F RT A2NM 2001120600092 20011206 00092 NM 2001 12 6 DL757011833 1 20011120 A 3350 BPS73 POWER SUPPLY BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 649DL 24389 LAST EIGHT ROWS OF COACH CLASS EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY AND BATTERY CHECKS OK. 2 L 7 2 4F RT A2NM 2001120600093 20011206 00093 NM 2001 12 6 DL757011842 1 20011122 A 3397 653954319 HARNESS BOEING 757 757232 1384965 NM CARGO DOOR OPEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 645DL 24216 EMERGENCY LIGHT ON C-2 CARGO DOOR INOP. DOOR HARNESS HAS OPEN. REPLACED SAME. 2 L 7 2 4F RT A2NM 2001120600094 20011206 00094 NM 2001 12 6 DL75A011649 1 20011008 A 5310 146N851210 DOOR FRAME BOEING 757 757212 1384951 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 750AT 23126 THE LOWER SILL BEAM OF THE C2 DOOR OPENING WAS BADLY CORRODED AND REQUIRED REPLACEMENT. TO REMOVE AND INSTALL A NEW SEC TION, THE OUTER CHORD OF THE FS 1440 OPENING FRAME WAS CUT AT STRINGER 26R AND THE WEB CUT AT STRINGER 23R. THE LOWER S ECTIONS WERE REMOVED AND RE-INSTALLED AFTER THE SILL REPLACEMENT. THE WEB WAS SPLICED PER SRM AND THE CHORD WITH ALUMIN UM ANGLES PER ER/A 381623-14, REV A. 2 L 7 2 4F RT A2NM 2001120600095 20011206 00095 NM 2001 12 6 DL75A011657 1 20011011 A 5310 146N851118 DOOR FRAME BOEING 757 757212 1384951 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 750AT 23126 THE FWD FRAME OF THE C2 DOOR OPENING AT FS 1380 WAS FOUND WITH CORROSION ON THE OUTER FRAME CAP NEAR STRINGER 27R. THE CHORD WAS CUT JUST ABOVE THE DAMAGE AND THE LOWER SECTION REMOVED. A NEW SECTION OF CHORD WAS FABRICATED AND SPLICED IN WITH REPAIR ANGLES. THE REPAIR WAS ACCOMPLISHED PER ER/A 381629-14, REV A. 2 L 7 2 4F RT A2NM 2001120600096 20011206 00096 WP 2001 12 6 ABXA010620 1 20011126 A 5511 995823869 FORMER DOUG DC9 DC931 3022065 WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 949AX 47325 SHEARTIE AT STATION 980 WAS CRACKED AT LONGERON 14 LEFT. REPLACED SHEARTIE IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2001120600097 20011206 00097 WP 2001 12 6 MWEA011477 1 20011206 A 5310 5912494501 PAN DOUG DC9 DC981 3022081 WP FWD CARGO COMPT. CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 FORWARD CARGO COMPARTMENT AIRCRAFT DOOR JAMB BOTTOM HAS 3 AREAS OF CORROSION-BOTH DOOR STOP FITTINGS AND ONE SPOT IN BET WEEN -- REMOVED EXTERNAL SCUFF PLATE AND FLOOR BOARD SUPPORTS TO FACILITATE OTHER MAINTENANCE. REMOVED LOWER PAN SECTI ON. INSTALLED SCUFF PLATE, FLOOR BOARD SUPPORTS AND NEW LOWER PAN SECTION. 2 L 7 2 4F A6WE 2001120600098 20011206 00098 2001 12 6 GTIA010874 4 20010909 A 2210 SWITCH DOUG DC9 DC981 3022081 WP COCKPIT INOPERATIVE A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 819NK 48016 A/P WILL NOT ENGAGE APPEARS TO BE PROBLEM WITH F/O'S A/P CONTROL WHEEL DISENGAGE SW NOT FUNCTIONING PROPERLY. REMOVED A ND REPLACED F/O SWITCH FOR AUTO PILOT. (M) 2 L 7 2 4F A6WE 2001120600099 20011206 00099 WP 2001 12 6 GTIA011092 1 20011106 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 816NK 49140 POST FLIGHT 616, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE FROM GALLEY TO ABOUT ROW 7 ALSO EXIT IDENTIFIERS INOPE RATIVE AT GALLEY EXIT AND MAIN ENTRANCE DOOR. REMOVED AND REPLACED BATTERY PACK IN OVERHEAD BIN, OPS CHECK OK IAW MD80 MM 33-53-00. NO DEFECTS NOTED. (M) 2 L 7 2 4F A6WE 2001120600100 20011206 00100 WP 2001 12 6 GTIA011094 1 20011017 A 7110 SKIN DOUG DC9 DC981 3022081 WP NOSE COWL DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 FTW - NOSE COWL AT 6 O'CLOCK POSITION O/B SURFACE HAS DELAMINATION. REMOVED DAMAGED PLIES OF CARBON SKIN IAW DC9/MD80 S RM 51-90-0. REPAIRED DELAMINATION AREA IN NOSE COWL AT 6 O'CLOCK POSITION IAW DC9 MD80 SRM 51-90-0. (M) 2 L 7 2 4F A6WE 2001120600101 20011206 00101 WP 2001 12 6 GTIA011096 1 20011019 A 7110 WEB DOUG DC9 DC981 3022081 WP NR 1 NOSE COWL DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 FTW - NR 1 ENGINE NOSE COWL AFT WEBBING DENTED AND DAMAGED AT 9 O'CLOCK POSITION. CUT DAMAGE AREA PER SRM MD80 54-01. FABRICATED SECTION AND SPLICES TWO PER SRM MD80 54-01. INSTALLED SPLICES AND WEB IAW MD80 SRM 51-30-2 AND 51-30-1. (M) 2 L 7 2 4F A6WE 2001120600102 20011206 00102 2001 12 6 GTIA011097 4 20011023 A 2565 SLIDE DOUG DC9 DC981 3022081 WP TAILCONE FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 810NK 48015 FTW - TAILCONE DOOR SLIDE DEPLOYMENT SYSTEM FAIL TEST ESCAPE SLIDE, BECAME UNPACKED DURING TEST. REMOVED TAIL SLIDE IAW MD80 MM 25-61-00. INSTALLED SLIDE IAW MD80 MM 25-62-01 PERFORMED OPERATIONAL CHECK TAIL CONE SLIDE DEPLOYMENT SYSTEM P ER SPIRIT AIRLINES TASK CARD 05-R-00079, ALL CHECKS NORMAL. (M) 2 L 7 2 4F A6WE 2001120600103 20011206 00103 WP 2001 12 6 GTIA011098 1 20011017 A 3520 LATCH DOUG DC9 DC981 3022081 WP CABIN FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 810NK 48015 FTW - OXYGEN MASK AT AFT INOPERATIVE CEILING PANEL DO NOT PASS TEST ON AUTO AND MANUAL MODES. REMOVED BAD LATCH AND INS TALLED NEW ONE IAW MD80 MM 35-21-01. OPS CHECK GOOD IAW MD80 MM 35-20-00. (M) 2 L 7 2 4F A6WE 2001120600104 20011206 00104 WP 2001 12 6 GTIA011099 1 20010826 A 5330 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 FTW - DENT IN FUSELAGE AFT OF ENTRANCE DOOR AT LONGERON 16-17 AND STATION 237. CUT OUT DAMAGE AREA AT FUSELAGE AFT ON E NTRANCE DOOR AT LONGERON 16-17. LOCATED AND DRILLED FINGER DOUBLER AND SKIN PLUG IAW MD80 SRM 51-10-04. INSTALLED REPA IR PARTS AT FUSELAGE AFT OF ENTRANCE DOOR AT LONGERON 16-17 AND STATION 237 IAW MD80 SRM 53-04. (M) 2 L 7 2 4F A6WE 2001120600105 20011206 00105 WP 2001 12 6 GTIA011100 1 20010826 A 5330 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 FTW - FOUND DENT AT STATION 224 BETWEEN LONGERON 18 AND 17R. FABRICATED REPAIR PARTS IAW MD80 SRM 53-04. INSTALLED REP AIR PARTS AT STATION 224 BETWEEN LONGERON 18 AND 17R IAW MD80 SRM 53-04. (M) 2 L 7 2 4F A6WE 2001120600106 20011206 00106 WP 2001 12 6 GTIA011101 1 20011107 A 5753 FLAP DOUG DC9 DC981 3022081 WP LT WING DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 ACY - LEFT FLAP INBOARD TRAILING EDGE DELAMINATED. REPAIRED T/E INBOARD FLAP LEFT FIBERGLASS REPAIR IAW MD80 SRM 57-03. (M) 2 L 7 2 4F A6WE 2001120600107 20011206 00107 WP 2001 12 6 GTIA011102 1 20011105 A 3350 60030431 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 823NK 48020 FLL - EMERGENCY CEILING LIGHTS BETWEEN STATION 800 AND 925 INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY POWER SU PPLY (B5-107) IAW MM 33-53-00, OPS CHECK OK REF WDM 33-51-01. (M) 2 L 7 2 4F A6WE 2001120600108 20011206 00108 WP 2001 12 6 GTIA011104 1 20011021 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP COCKPIT CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 FTW - FLIGHT COMPARTMENT CAPTAINS SIDE FLOORBOARD CORRODED, UPPER SEAT AREA. REMOVED FLOOR BOARD PER MD80 SRM 51-30-1. FORMED NEW FLOOR PANEL. INSTALLED FLOOR PANEL PER MD80 SRM 51-30-1. (M) 2 L 7 2 4F A6WE 2001120600109 20011206 00109 WP 2001 12 6 GTIA011105 1 20010829 A 5330 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 FTW - FOUND FUSELAGE STA Y160 LEFT FUSELAGE FORWARD FORWARD AIR STAIR CUT OUT FORWARD LOWER, CORNER HAS A CRACK. REMOVE D DAMAGE AREA IN LOWER FORWARD CORNER IAW MD80 SRM 53-05. UPON REMOVAL OF PREVIOUS REPAIR FORWARD AIRSTAIR AFT LOWER CO RNER FOUND ONE CRACK IN FUSELAGE SKIN BETWEEN FASTENERS. REMOVED DAMAGE ON AFT CORNER OF FUSELAGE SKIN IAW MD80 SRM 53- 05. UPON REMOVAL OF DAMAGE AT AFT LOWER CORNER (FWD STAIRWELL CUT OUT) FOUND CRACK ON INNER DOUBLER. FABRICATED NEW DO UBLER FOR UPPER DOOR HINGE FOR FORWARD AIRSTAIR. INSTALLED FORWARD AND AFT SHIMS AND DOUBLERS. (M) 2 L 7 2 4F A6WE 2001120600110 20011206 00110 WP 2001 12 6 GTIA011106 1 20011010 A 5330 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 FTW - RIGHT WING TO BODY FAIRING RUB STRIP HAS CORROSION. REMOVED CORROSION PER MD80 SRM 51-10-3 AT RIGHT SKIN FUSELAGE FROM STATION Y 745 TO STA Y 815 BETWEEN LONGERON 29, 28 RIGHT. FOUND BLENDED AREA TO BE OUT OF LIMITS PER SRM MD80 53- 01. FABRICATED AND INSTALLED DOUBLERS IAW MD80 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 2001120600111 20011206 00111 WP 2001 12 6 GTIA011107 1 20010829 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - FLOOR SUPPORT CORRODED, FS 1338, APPROX BL 45R TOP OF SUPPORT, RIGHT AFT LAVATORY AREA. REMOVED CORROSION IAW MD8 0 SRM 51-10-3, FLOOR SUPPORT REPLACEMENT WILL BE ACCOMPLISHED ON N/R CARD. (M) 2 L 7 2 4F RT A6WE 2001120600112 20011206 00112 WP 2001 12 6 GTIA011108 1 20010829 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FOUND FLOOR SUPPORT, LEFT AFT LAVATORY AREA, CORRODED TWO PLACES, FS 1338L, APPROX BL24L AND BL60. REMOVED FLOOR SUPPOR T IAW MD80 SRM 51-30-2 AND 51-30-5. FABRICATED ANGLE SUPPORT AND INSTALLED PER MD80 SRM 51-30-2 AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2001120600113 20011206 00113 WP 2001 12 6 GTIA011109 1 20010831 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - PASSENGER CABIN SEAT TRACK HAS CORROSION AND BARE METAL IN SEVERAL PLACES AT FS 927-1136. UPON FURTHER EVALUATION , FOUND TO BE OUT OF LIMITS WITH PITS STILL EXISTING IN TRACK. FABRICATED AND INSTALLED NEW SEAT TRACK IAW MD80 SRM 53-0 5. (M) 2 L 7 2 4F RT A6WE 2001120600114 20011206 00114 WP 2001 12 6 GTIA011110 1 20010830 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - PAX CABIN SEAT TRACK HAS CORROSION AT FS 200-408 AT X-36 INCHES. FOUND OUT OF LIMITS AT STATION 237.5 IAW MD80 SR M 53-05. FABRICATED AND INSTALLED SEAT TRACK AT STATION 237.5 AND 408 IAW MD80 SRM 51-10-7. (M) 2 L 7 2 4F RT A6WE 2001120600115 20011206 00115 WP 2001 12 6 GTIA011111 1 20011114 A 5310 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - AFT CARGO COMPARTMENT JAMB AREA PLATE HAS CORROSION BETWEEN STATION 1155, 1211. FOUND CORROSION TO BE OUT OF LIMI TS IAW MD80 SRM 53-01. REMOVED CARGO DOOR JAMB BEAM. INSTALLED NEW AFT CARGO DOOR JAMB BEAM IAW MD80 SRM 51-30-5. (M) 2 L 7 2 4F RT A6WE 2001120600116 20011206 00116 WP 2001 12 6 GTIA011112 1 20011102 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FORWARD ENTRY AREA, FLOOR PAN CRACKED AT STA Y 2A-X43. CUT OUT DAMAGED AREA IAW MD80 SRM 53-01. FABRICATED NEW F LOOR PER REPAIR IAW MD80. INSTALLED NEW PER REPAIR IAW MD80 SRM 53-01. (M) 2 L 7 2 4F A6WE 2001120600117 20011206 00117 WP 2001 12 6 GTIA011113 1 20011030 A 5210 RIB DOUG DC9 DC982 3022082 WP L1 DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FORWARD PAX DOOR L1 HAS LEAK AT STATION Y 190 Z34.5 BETWEEN LL BEAM NR 5 AND LL BEAM NR 4. REMOVED CRACKED RIB IA W MD80 SRM 51-30. FOUND BEAM IAW MD80 SRM 52-05. DURING REMOVAL FOUND TEE ANGLE CRACKED. FORMED 'T' ANGLE IAW MD80 SR M 52-05. DRILLED UP AND LOCATED RIB. INSTALLED RIB. INSTALLED 'T' ANGLE PER MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2001120600118 20011206 00118 WP 2001 12 6 GTIA011114 1 20011114 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 603CA 49508 DTW - FOUND EMERGENCY LIGHTS INOPERATIVE BETWEEN ROWS 6-11 AND 31-31 FLOOR. REPLACED BATTERY PACK BETWEEN ROWS 6-11 AND RELAMPED 31 AND 32. OPS CHECK GOOD IAW MM 33-53-00. (M) 2 L 7 2 4F A6WE 2001120600119 20011206 00119 WP 2001 12 6 GTIA011115 1 20011113 A 3350 60030451 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 809NK 49503 DTW - FORWARD OVERWING EXIT LIGHT ON WITH POWER OFF. REMOVED AND REPLACED BATTERY POWER SUPPLY IAW SYSTEM, OPS CHECK GO OD. (M) 2 L 7 2 4F RT A6WE 2001120600120 20011206 00120 WP 2001 12 6 GTIA011117 1 20011101 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FOUND RIGHT INBOARD SEAT TRACK HAS A GOUGE AT FS 1079. REMOVED SEAT TRACK SECTION FROM STATION 1032 TO STA Y 1032 TO ST A Y 1146 (RIGHT INBOARD SEAT TRACK) IAW MD80 SRM 53-05. (M) 2 L 7 2 4F A6WE 2001120600121 20011206 00121 WP 2001 12 6 GTIA011118 1 20011101 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FOUND LEFT INBOARD SEAT TRACK FROM STATION 1035 TO 1150 DAMAGED. SEAT TRACK WAS FOUND OUT OF LIMITS. LOCATED AND DRILLED SEAT TRACK. INSTALLED PER MD80 SRM 53-05. (M) 2 L 7 2 4F A6WE 2001120600122 20011206 00122 WP 2001 12 6 GTIA011119 1 20011101 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - RIGHT OUTBOARD SEAT TRACK HAS BARE METAL AT FS 1293 TO 1267. REMOVED (DAMAGE SEAT) TRACK SECTION FROM STATION 124 0 TO STATION 1309. FABRICATED DRILLED AND LOCATED NEW SEAT TRACK AND SPLICE. INSTALLED SEAT TRACK FROM STATION 1240 TO STATION 1309 IAW MD80 SRM 51-30-1. (M) 2 L 7 2 4F A6WE 2001120600123 20011206 00123 WP 2001 12 6 GTIA011120 1 20011101 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CHAFED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - LEFT INBOARD SEAT TRACK STATION 1175 TO 1150 CHAFING. SEAT TRACK WAS FOUND OUT OF LIMITS FROM STATION 1150 TO 112 2. LOCATED AND DRILLED PER MD80. INSTALLED SEAT TRACK AND SPLICE PER MD80 SRM 53-05. (M) 2 L 7 2 4F A6WE 2001120600124 20011206 00124 WP 2001 12 6 GTIA011121 1 20011101 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - LEFT OUTBOARD SEAT TRACK STATION 1007 GOUGE. CUT OUT SEAT TRACK FROM STATION 937 TO 1032. INSTALLED SEAT TRACK FR OM STATION 937 TO 1032 IAW MD80 SRM 53-05. (M) 2 L 7 2 4F A6WE 2001120600125 20011206 00125 WP 2001 12 6 GTIA011125 1 20011103 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 RIGHT OUTBOARD SEAT TRACK HAS CORROSION AND GOUGED AREAS FROM STATION 955 TO 967. REMOVED DAMAGED SEAT TRACK FROM STATI ON 914 TO 1032. INSTALLED NEW SEAT FROM STATION 924 TO 1032 IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2001120600126 20011206 00126 WP 2001 12 6 GTIA011126 1 20011103 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 RIGHT OUTBOARD SEAT TRACK HAS CORROSION AND GOUGES FROM STATION 851-865. REMOVED DAMAGED SEAT TRACK FROM STATION 797-91 4. INSTALLED NEW SEAT TRACK FROM STATION 740 TO STATION 914 IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2001120600127 20011206 00127 WP 2001 12 6 GTIA011128 1 20011103 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CHAFED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - LEFT INBOARD SEAT TRACK STATION 596 TO 589 GAUGE WITH CHAFING. SEAT TRACK WAS FOUND OUT OF LIMITS IAW MD80 SRM 53 -05. INSTALLED SEAT TRACK AND SPLICE IAW MD80 SRM 51-30-5 AND 51-3-01. (M) 2 L 7 2 4F A6WE 2001120600128 20011206 00128 WP 2001 12 6 GTIA011129 1 20011103 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CHAFED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - LEFT INBOARD SEAT TRACK STATION 747 TO 734 GAUGE AND CHAFING. SEAT TRACK WAS FOUND OUT OF LIMITS. INSTALLED SEAT TRACK AND SPLICE IAW MD80 SRM 53-05. (M) 2 L 7 2 4F A6WE 2001120600129 20011206 00129 WP 2001 12 6 GTIA011130 1 20011112 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - CABIN CENTER FLOORBOARD STATION 617 IS CRACKED AND DAMAGED AT AFT END. REMOVED FLOOR PANEL, CABIN CENTER STATION 617 PER MD80 SRM 53-20-01. REPAIRED DAMAGED END, INSTALLED FLOOR PANEL PER MD80 SRM 53-20-01. (M) 2 L 7 2 4F A6WE 2001121900131 20011219 00131 NM 2001 12 19 F3LA200100134 1 20011203 A 5315 FLOORBEAM BOEING 737 737228 13844AG NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM AT STA 312, FROM LBL 13 TO RBL 13. REMOVED DAMAGED SECTION OF FLOOR BEAM, FABRICATED REPLACEMENT FLOORBEAM AND ANGLE SPLICES AND INSTALLED PER SRM 53-10-4. 2 L 7 2 4F RT A16WE 2001120600130 20011206 00130 WP 2001 12 6 GTIA011131 1 20011102 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - LEFT INBOARD SEAT TRACK STATION 869 GAUGE AND BARE METAL. SEAT TRACK WAS FOUND OUT OF LIMITS FROM STATION 788-920 . INSTALLED SEAT TRACK PER MD80 SRM 53-05. (M) 2 L 7 2 4F A6WE 2001120600131 20011206 00131 WP 2001 12 6 GTIA011132 1 20011103 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CHAFED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - LEFT INBOARD SEAT TRACK STATION 368 TO 348 CHAFING. INSTALLED SEAT TRACK AND SPLICE IAW MD80 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 2001120600132 20011206 00132 2001 12 6 GTIA011137 4 20011012 A 3460 4034241971 COMPUTER DOUG DC9 DC981 3022081 WP NR 2 FAULTY A GTIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 23 810NK 48015 FTW - NR 2 DFGC P/N 4034241-971, S/N 88081643 WILL NOT ALLOW AUTO PILOT TO ENGAGE. ALSO, NR 2 FLIGHT DIRECTOR FLAG IN V IEW. REMOVED NR 2 DFGC IAW MD80 MM 22-01-01. INSTALLED NR 2 DFGC IAW MD80 MM 22-01-01. (M) 2 L 7 2 4F A6WE 2001120600133 20011206 00133 WP 2001 12 6 USAAD01179 1 20011111 A 3350 9721055 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 823US 49142 IND - THE INTERVALVE LOW LEVEL LIGHTS DO NOT TEST AT SEATS 1, 3, 6, 11, 16, 20, 25 AND 30. MAINTENANCE REPLACED THE BAT TERY PACKS. SYSTEMS TESTS OK. (M) 2 L 7 2 4F A6WE 2001120600134 20011206 00134 WP 2001 12 6 USAAD01181 1 20011107 A 3350 9721055 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 821US 49138 BOS - TWO LOW LEVEL EMERGENCY LIGHTS AND THE AFT CABIN CEILING PANEL EMERGENCY LIGHT WERE INOPERATIVE. MAINTENANCE REPL ACED THE LOW LEVEL BATTERIES AND THE AFT CABIN CEILING LIGHT POWER SUPPLY. (M) 2 L 7 2 4F A6WE 2001120600135 20011206 00135 NM 2001 12 6 USAASB01009 1 20010118 A 3397 WIRE HARNESS BOEING 737 737301 1384611 NM CABIN OUT OF POSITION A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 300AU 23228 LGA - MAINTENANCE FOUND THE EMERGENCY EXIT PATH LIGHTING AT SEAT 16C INOPERATIVE. MAINTENANCE REPOSITIONED WIRING HARNE SS FOR SEAT ROW 16ABC EMERGENCY EXIT PATH LIGHTING. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001120600137 20011206 00137 WP 2001 12 6 MWEA011478 1 20011206 A 5310 9911842101 FRAME DOUG DC9 DC981 3022081 WP FRAME 1485 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 CANTED FRAME 1485, AFT ACCESSORY COMPARTMENT HAS A 5/8 INCH CRACK AROUND A FASTENER LOCATED APPROXIMATELY 6 INCHES OUTBO ARD OF EMERGENCY LIGHT CLUSTER -- STOP DRILLED CRACK, FABRICATED, LOCATED AND DRILLED UP DOUBLER. INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001120600138 20011206 00138 NM 2001 12 6 USAASB01268 1 20010923 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 521AU 23856 CLT - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE LAST SIX ROWS OF EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001120600149 20011206 00149 SO 2001 12 6 C2XA01IA409 1 20011201 A 2150 DL1020M324 ACTUATOR EMB 120 EMB120ER 3260203 SO FUSELAGE FROZEN A C2XA K NONE O OTHER CR CRUISE 1 SW 27 17728 120182 IAH - Crew reported that there was a smoke smell in the cockpit when the #1 pack was operated. The pack was turned off a nd the smell went away. The aircraft landed at IAH without incident. Maintenance found the left ram air valve door to be stuck in the open position. Maintenance removed and replaced the affected ram air door actuator, and the aircraft was a pproved for return to service. 2 L 7 2 4T RT A31SO 2001120700001 20011207 00001 EU 2001 12 7 2001F00547 1 20010807 A 7130 0292827110 HEAT SHIELD SNIAS 350 AS350B2 8680813 EU ENGINE CRACKED A R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 102LN 954 3065 HEAT SHIELD CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 1 3U H9EU 2001120700002 20011207 00002 SO 2001 12 7 C2XA01CL237 1 20011204 A 2560 CBC16207 CONNECTOR EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 13990 145277 CLE FLIGHT#3308 THE CREW REPORTED A BURNING SMELL COMING FROM THE #2 HOT JUG.MAINTENANCE RELEASED AIRCRAFT I/A/W MEL 25- 60-02/3.MAINTENANCE CLEARED THE MEL BY REPLACING THE #2 HOT JUG CONNECTOR.OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2001120700003 20011207 00003 EU 2001 12 7 2001F00550 1 20010522 A 7710 0292767070 GUARD SNIAS 350 AS350B3 8680954 EU ENGINE CRACKED A R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 103LN 1034 3128 HARNESS GUARD CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 1 3U H9EU 2001120700004 20011207 00004 EU 2001 12 7 2001F00704 1 20010424 A 6220 126892P BALL JOINT SNIAS 350 AS350B3 8680954 EU MAIN ROTOR WORN B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 392LG 477 3252 LEFT THREAD BALL JOINT WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 1 3U H9EU 2001120700005 20011207 00005 EU 2001 12 7 2001F00705 1 20010525 A 8010 845UN01Q4AA5F SWITCH SNIAS 350 AS350B3 8680954 EU STARTER INOPERATIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 52285 226 3251 SWITCH INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 1 3U H9EU 2001120700006 20011207 00006 SO 2001 12 7 C2XA01CL238 1 20011206 A 2150 8152403 ACM EMB 145 EMB145LR 3260212 SO FUSELAGE SEIZED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 17984 4382 145246 CLE FLIGHT#3222 THE CREW REPORTED SMOKE IN THE CABIN WITH #2 PACK ON OPERATED OFF THE APU BLEED.MAINTENANCE INSPECTED AN D REPLACED THE #2 PACK ACM.OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2001120700007 20011207 00007 SW 2001 12 7 2001F00709 1 20011029 A 7920 B-NUT SWRNGN SA227 SA227AC 8780603 SW ENGINE LOOSE A BSAA E ENGINE SHUTDOWN K J R FLUID LOSS WARNING INDICATION PARTIAL RPM/PWR LOSS DE DESCENT 1 NM 05 425MA AC640 FLT 6003 - SEA - CREW OBSERVED THAT THE LEFT OIL PRESS LOW CAME ON PRESSURE DROPPING TO ZERO DURING DESCENT INTO SEA. TH E LEFT ENGINE TORQUE ALSO STARTED TO DROP. THE LEFT ENGINE TORQUE INDICATION ALSO STARTED TO DROP. THE CREW FEATHERED AN D SHUTDOWN THE ENGINE. CREW NOTICED OIL LEAKING ON THE GROUND DURING THE POST FLIGHT. A LOOSE B-NUT WAS FOUND AT THE NTS 4-WAY UNION ON THE LINE GOING TO THE TAPPING PORT FITTING FOR CHECKING NTS PRESSURE. THE B-NUT IS NORMALLY INSTALLED AN D TIGHTENED DURING ENGINE INSTALLATION. THERE WAS NO MAINTENANCE PERFORMED IN THIS AREA AT THE LAST INSPECTION. THE ENGI NE WAS INSTALLED AT A/C TAT 26,567.6, TAC 33,918. THE ENGINE HAD BEEN INSTALLED RO 358.5 HOURS AND 524 CYCLES. (M) 2 L 7 2 4T RT A8SW 2001120700008 20011207 00008 NM 2001 12 7 0104475506 1 20011206 A 5347 SEAT TRACK BOEING 757 757251 1384970 NM CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 506US 23195 During "H" check found corrosion on seat track at BS 400 RBL 24.75. Repaired per EA 55-187323. 2 L 7 2 4F RT A2NM 2001120700009 20011207 00009 NM 2001 12 7 0104506613 1 20011205 A 5330 SKIN PANEL BOEING 747 747251B 1384892 NM CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 613US 20358 During line check found corrosion on skin panel at lap splice from BS 1835-1961, stringer 12R. Repaired per EA 66-187305 . 2 L 7 4 4F A20WE 2001120700010 20011207 00010 NM 2001 12 7 2001F00722 1 20011116 A 3610 1074925 REGULATOR VALVE BOEING 737 73773A 1384606 NM BLEED AIR MALFUNCTIONED A TSAA O OTHER O OTHER CL CLIMB 1 WP 13 739AL 28500 FLT 100 - HNL-KOA - DURING THE REPOSITIONING FLIGHT, LEFT DUCT PRESSURE IN CLIMB VARIABLE 23-30 PSI. RIGHT DUCT PRESSUR E 40-45 PSI IN CLIMB. LEVEL FLIGHT, LEFT DUCT WS 40 PSI AND THE RIGHT DUCT WAS 42 PSI. IN DESCENT, THE LEFT AND RIGHT STAYED CLOSE TO MATCHED PSI. RETURNED TO HNL FOR AN UNEVENTFUL LANDING. REMOVED AND REPLACED THE PRECOOLER VALVE (P/N 3289562-5) IAW MM 36-12-02-4. OPS CHECK OK. REMOVED AND REPLACED THE 450 DEGREE SENSOR (P/N 129666-2) PER MM 36-11-05- 04. OPS CHECK OK. REMOVED AND REPLACED THE BLEED AIR REGULATOR (P/N 107492-5) IAW MM 36-11-03-4. OPS CHECK OK. AIRCR AFT RETURNED TO SERVICE. FLIGHT VERIFICATION OK DURING NEXT FLIGHT. (M) 2 L 7 2 4F RT A16WE 2001120700011 20011207 00011 NM 2001 12 7 2001F00723 1 20011116 A 3620 1296662 SENSOR BOEING 737 73773A 1384606 NM BLEED AIR MALFUNCTIONED A TSAA O OTHER O OTHER CL CLIMB 1 WP 13 739AL 28500 FLT 100 - HNL-KOA - DURING THE REPOSITIONING FLIGHT, LEFT DUCT PRESSURE IN CLIMB VARIABLE 23-30 PSI. RIGHT DUCT PRESSUR E 40-45 PSI IN CLIMB. LEVEL FLIGHT, LEFT DUCT WS 40 PSI AND THE RIGHT DUCT WAS 42 PSI. IN DESCENT, THE LEFT AND RIGHT STAYED CLOSE TO MATCHED PSI. RETURNED TO HNL FOR AN UNEVENTFUL LANDING. REMOVED AND REPLACED THE PRECOOLER VALVE (P/N 3289562-5) IAW MM 36-12-02-4. OPS CHECK OK. REMOVED AND REPLACED THE 450 DEGREE SENSOR (P/N 129666-2) PER MM 36-11-05- 04. OPS CHECK OK. REMOVED AND REPLACED THE BLEED AIR REGULATOR (P/N 107492-5) IAW MM 36-11-03-4. OPS CHECK OK. AIRCR AFT RETURNED TO SERVICE. FLIGHT VERIFICATION OK DURING NEXT FLIGHT. (M) 2 L 7 2 4F RT A16WE 2001120700012 20011207 00012 NM 2001 12 7 GAIA01313OP 1 20011110 A 2910 6517844 HYDRAULIC LINE BOEING 727 727224 1384076 NM HYDRAULIC SYS CRACKED A GAIA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 79748 22450 FLT 3850 - MSP-FWA - DURING CRUISE, THE FLIGHT CREW NOTICED THAT THE 'A' SYSTEM HYDRAULIC SYSTEM WAS ISOLATED THE AIRCRA FT CONTINUED TO FWA. THE AIRCRAFT MADE AN UNEVENTFUL LANDING. INSPECTION REVEALED A CRACKED HYDRAULIC LINE AT FUSELAGE STATION 1303. THE LINE AND THE NR 1 AND NR 2 ENGINE DRIVEN HYDRAULIC PUMPS AND FILTERS WERE REPLACED. THE SYSTEM OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001120700013 20011207 00013 NM 2001 12 7 GAIA01314OP 1 20011110 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE CHAFED A GAIA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 79748 22450 FLT - 3850 - MSP-FWA - DURING CRUISE, THE FLIGHT CREW NOTICED THAT THE 'A' SYSTEM HYDRAULIC FLUID QUANTITY WAS DECREASIN G. AN EMERGENCY WAS DECLARED AND THE HYDRAULIC SYSTEM WAS ISOLATED THE AIRCRAFT CONTINUED TO FWA. THE AIRCRAFT MADE AN UNEVENTFUL LANDING. FURTHER INSPECTION REVEALED THAT A FUSELAGE FRAME AND A HYDRAULIC LINE WERE DAMAGED FROM CHAFING. INSPECTION REVEALED A HYDRAULIC LINE HAD CHAFED AGAINST THE FRAME AT FUSELAGE STATION 1303. THE LINE AND THE NR 1 AND NR 2 ENGINE DRIVEN HYDRAULIC PUMPS AND FILTER WERE REPLACED. THE FRAME WAS REPAIRED IAW FV1 DRAWING 53-01590-1. THE SY STEM OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001120700014 20011207 00014 NM 2001 12 7 GAIA01315OP 1 20011113 A 3350 1000679 LIGHT BOEING 727 727243 138408D NM L1 DOOR DEFECTIVE A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 1269Y 21269 DURING ROUTINE MAINTENANCE AT FWA, IT WAS DISCOVERED THAT THE L1 EMERGENCY EXIT LIGHT WAS DIM. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2001120700015 20011207 00015 NM 2001 12 7 KPVA200123 1 20011108 A 3350 10005511 LIGHT DHAV DHC8 DHC8103 1386005 NM CABIN DEFECTIVE A KPVA K NONE O OTHER IN INSP/MAINT 1 WP 13 807WP 357 PORTABLE EMERGENCY LIGHT DIM. REMOVED AND REPLACED PORTABLE EMERGENCY LIGHT ASSEMBLY. OPS CHECK GOOD IAW DHC 8 MM 33-5 1-00 PAGE 201-202. NO DEFECTS NOTED. (M) 2 H 7 2 4T RT A13NM 2001120700016 20011207 00016 NM 2001 12 7 KPVA200124 1 20011114 A 3350 10006611 BUTTON DHAV DHC8 DHC8103 1386005 NM PORTABLE LIGHT BROKEN A KPVA K NONE O OTHER IN INSP/MAINT 1 WP 13 806WP 357 OVERHEAD REMOVABLE EMERGENCY LIGHT 'TEST' PUSH BUTTON BROKEN. REMOVED PORTABLE EMERGENCY LIGHT (BROKEN) AND INSTALLED S ERVICEABLE PORTABLE EMERGENCY LIGHT. NO DEFECTS NOTED. REF DHC 8 MM 33-51-00 PAGE 8/9 PARAMETERS 2A AND 2B. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 2001120700017 20011207 00017 2001 12 7 TSAA0123113 4 20011116 A 2310 6223371001 TRANSCEIVER BOEING 737 7372T4 1384492 NM HF COMM MALFUNCTIONED A TSAA O OTHER O OTHER CR CRUISE 1 WP 13 808AL 23445 FLT 351 - HNL-JON - DURING THE VERIFICATION PHASE OF FLIGHT AND CHECKING THE HF RADIO SYSTEM, THE NR 1 HF HAD NO TUNE AN D THE TRANSMIT WAS INOPERATIVE. RETURNED TO HNL FOR AN OVERWEIGHT LANDING, VERY LOW SINK RATE. REPLACED NR 1 HF TRANSC EIVER (P/N 6223371001). OPS CHECK ON GROUND WITH SFO AND SELCAL CHECK OK. VERIFICATION FLIGHT REQUIRED. PERFORMED OVE RWEIGHT LANDING INSPECTION IAW FORM M-121. NO DEFECTS NOTED IN PHASE 1 STEP 2A. OK FOR SERVICE. SUBSEQUENTLY, THE HF COUPLER WAS REPLACED (P/N 792-6140-001) AND VERIFIED AS THE CAUSE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2001120700019 20011207 00019 NM 2001 12 7 TSAA0136139 1 20011116 A 3610 32895625 VALVE BOEING 737 73773A 1384606 NM BLEED AIR MALFUNCTIONED A TSAA O OTHER O OTHER CL CLIMB 1 WP 13 739AL 28500 FLT 100 - HNL-KOA - DURING THE REPOSITIONING FLIGHT, LEFT DUCT PRESSURE IN CLIMB VARIABLE 23-30 PSI. RIGHT DUCT PRESSUR E 40-45 PSI IN CLIMB. LEVEL FLIGHT, LEFT DUCT WS 40 PSI AND THE RIGHT DUCT WAS 42 PSI. IN DESCENT, THE LEFT AND RIGHT STAYED CLOSE TO MATCHED PSI. RETURNED TO HNL FOR AN UNEVENTFUL LANDING. REMOVED AND REPLACED THE PRECOOLER VALVE (P/N 3289562-5) IAW MM 36-12-02-4. OPS CHECK OK. REMOVED AND REPLACED THE 450 DEGREE SENSOR (P/N 129666-2) PER MM 36-11-05- 04. OPS CHECK OK. REMOVED AND REPLACED THE BLEED AIR REGULATOR (P/N 107492-5) IAW MM 36-11-03-4. OPS CHECK OK. AIRCR AFT RETURNED TO SERVICE. FLIGHT VERIFICATION OK DURING NEXT FLIGHT. (M) 2 L 7 2 4F RT A16WE 2001122000012 20011220 00012 NM 2001 12 20 01FDEA01036 1 20011121 A 5330 SKIN DOUG MD11 MD11 3023602 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 RIGHT FUSELAGE BS 1841, S-39 TO 2-41 EXTERIOR SKIN DENTED. REMOVED AND REPLACED SKIN PER SRM 53-20-00 FIG 2. 2 L 7 3 4F RT A22WE 2001121200069 20011212 00069 WP 2001 12 12 01FDEA01037 1 20011206 A 5320 NCA60488 ANGLE DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 HORIZ PRESS BULKHEAD RT OUTBOARD ANGLE IS CRACKED FROM BS 535-555. REMOVED AND REPLACED ANGLE PER EA 8-5310-57067. 2 L 7 3 4F A22WE 2001121200070 20011212 00070 WP 2001 12 12 01FDEA01038 1 20011206 A 5320 NCA60487 ANGLE DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 HORIZ PRESS BULKHEAD LT ANGLE PIN CRACKED FROM BS 555-575 AT LONGERON 30L. REMOVED AND REPLACED PER EA 8-5310-57067. 2 L 7 3 4F A22WE 2001120700020 20011207 00020 WP 2001 12 7 0104599917 1 20011201 A 2150 DUCT DOUG DC9 DC932 3022066 WP WATER SEPARATOR LOOSE A NWAA B EMER. DESCENT O OTHER CR CRUISE 1 GL 01 967N 47573 IN CRUISE FLIGHT, THE AUTO TEMPERATURE WAS NOT WORKING. CREW WENT TO MANUAL TO COOL THE CABIN AND THE CABIN ALTITUDE CLI MBED TO 10,000 FT. AN EMERGENCY WAS DECLARED, DESCENDED TO 25,000 FT, AND MADE AN UNEVENTFUL LANDING AT CLT. MSP MAIN TENANCE FOUND A DUCT OFF THE INLET TO THE RIGHT PACK WATER SEPARATOR AND RESECURED IT. OPERATIONAL CHECK OK. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F A6WE 2001120700021 20011207 00021 WP 2001 12 7 0104671225 1 20011128 A 2421 GENERATOR DOUG DC10 DC1030 3023501 WP A NWAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 01 225NW 53069 341 46582 DURING CRUISE ENROUTE TO HNL, THE NBR 1 GENERATOR DROPPED OFF LINE. FLIGHT CREW FOLLOWED COM PROCEDURE AND DISCONNECTED CSD AND GENERATOR. FLIGHT CONTINUED TO HNL AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NBR 1 GENERATOR FAILURE RES ULTED IN STRUCTURAL DAMAGE TO THE GENERATOR HOUSING. IN ADDITION, COLLATERAL DAMAGE OCCURRED TO SEVERAL LINES AND TUBES ADJACENT TO GENERATOR. THE NBR 1 GENERATOR WAS REPLACED AND OPERATIONAL CHECK OK. AIRCRAFT WAS FERRIED TO MSP FOR ADDITI ONAL MAINTENANCE TO ENGINE. 2 L 7 3 4F A22WE 2001121400026 20011214 00026 WP 2001 12 14 ARWA20011203 1 20011205 A 3242 1542522 BRAKE DOUG DC8 DC861 3021952 WP MLG SEIZED A ARWA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 19 29UA 378 46159 NR 2 MAIN LANDING GEAR BRAKE ASSEMBLY LOCKED-UP CAUSING NR 2 TIRE TO BLOW. BRAKE TEMPERATURE CHECK AND WITHIN LIMITS. REMOVED AND REPLACED NR 2 MAIN GEAR BRAKE ASSEMBLY IAW DC-8 MM 32-42-1. REMOVED AND REPLACED NR 2 MAIN GEAR WHEEL AND T IRE ASSEMBLY IAW MM 32-40-1. REMOVED AND REPLACED NR 1 MAIN GEAR WHEEL AND TIRE ASSEMBLY IAW MM 32-40-1. 2 L 7 4 4F 4A25 2001120700022 20011207 00022 NM 2001 12 7 TSAA0153157 1 20011114 A 5310 65C38452 WINDOW FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 817AL 39735 PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION PER S/B 737-53A1177R6 AND DISCOVERED DEFECTS IN NUMEROUS AREAS AT LT FU SELAGE WINDOW CORNERS; 2 BETWEEN BS 500-520 AND 33 BETWEEN BS 727-907, RT FUSELAGE WINDOW CORNERS; 8 BETWEEN BS 360-540 AND 1 AT BS 727A-727B FOR A TOTAL OF 44 DEFECTS NOTED AT WINDOW CORNERS UTILIZING HFEC METHOD. OVERSIZED FASTENER HOLE AND INSTALLED RIVET OR OVERSIZE HI-LOCK. THE FASTENER HOLES WITH THE 44 DEFECTS WERE OVERSIZED UNTIL THE INDICATIONS WE NT AWAY OR REPAIRED WINDOW BY TRIMMING OUT CRACKED HOLES. INSTALLED FILLER, FABRICATED AND INSTALLED REPAIR DOUBLER, RE PAIR TRIPLER, AND SPLICE PLATES. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001120700023 20011207 00023 NM 2001 12 7 TSAA0153161 1 20011121 A 5330 6545713 SKIN BOEING 737 737230 1384401 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 820AL 22138 DISCOVERED CRACK AT BS 727A, S-15R. FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLER. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001120700024 20011207 00024 NM 2001 12 7 TSAA0157155 1 20011109 A 5730 69578332 SKIN BOEING 737 7372X6C 1384552 NM LT WING CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 817AL 39735 DISCOVERED CORROSION ON LEFT LOWER WING SURFACE, WS 500. REMOVED CORROSION, CONFIRMED REMOVAL OF CORROSION, FLAP PEENED REWORKED AREAS PER SOPM 20-10-03. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001120700025 20011207 00025 NM 2001 12 7 TSAA0157156 1 20011107 A 5730 69578332 SKIN BOEING 737 7372X6C 1384552 NM LT WING CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 817AL 39735 DISCOVERED CORROSION AT LEFT LOWER WING SURFACE, WS 515.5. REMOVED CORROSION, CONFIRMED REMOVAL OF CORROSION, FLAP PEEN ED REWORKED AREAS PER SOPM 20-10-03. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001120700026 20011207 00026 NM 2001 12 7 UIEA01105 1 20011110 A 8011 102448113S CONNECTOR BOEING 747 747341 NM START VALVE SHORTED A UIEA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 EA 15 354MC 23394 NR 1 ENGINE START VALVE OPEN LIGHT CAME ON AT TOP OF DESCENT (INTO XXW) ALTITUDE 27,000 FEET. SHUT DOWN ENGINE IAW FHB. NO ENGINE PARAMETERS EXCEEDED. FIRE SWITCH NOT USED. FOUND SHORT AT CONNECTOR DV86B OF START VALVE. REPAIRED CONNEC TOR IAW 20-60-00. FUNCTION CHECK CARRIED OUT OK 71-00-00. (M) 2 L 7 4 4F RT A20WE 2001120700027 20011207 00027 NM 2001 12 7 USAASB01180 1 20010619 A 2450 10608061035 CIRCUIT BREAKER BOEING 737 737401 1384701 NM COCKPIT FAULTY A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 19 405US 23885 CLT - FLT 682 - UPON DESCENT INTO CLT, FROM MIA, CAPTAIN DECLARED AN EMERGENCY WHEN HE HEARD A LOUD POP AND LOST HIS FLI GHT INSTRUMENTS. FIRST OFFICERS FLIGHT INSTRUMENTS SEEMED TO BE WORKING FINE. ONCE ON THE TAXI-WAY, THERE WAS REPORT O F A SMOKE SMELL. EVACUATION WAS ORDERED. AFTER EVACUATION, THE AIRCRAFT TAXIED TO THE GATE UNDER ITS OWN POWER. MAINT ENANCE ACCOMPLISHED A VISUAL INSPECTION OF THE CABIN AND CARGO BINS AND DID NOT FIND ANYTHING ABNORMAL. FOUND THE NR 1 NORMAL TRANSFER BUS CIRCUIT BREAKER POPPED. REMOVED AND REPLACED CIRCUIT BREAKER AS PRECAUTIONARY. ALL SYSTEMS CHECK N ORMAL. NO SMELL OF SMOKE FOUND. REPLACED ALL FOUR DOOR EMERGENCY ESCAPE SLIDES. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2001120700028 20011207 00028 NM 2001 12 7 USAASB01269 1 20010924 A 3350 1012721 LIGHT BOEING 737 7373B7 1384580 NM CABIN DISCONNECTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 391US 23313 TPA - MAINTENANCE FOUND THE EMERGENCY LIGHT AT ROW 4, LEFT SIDE, DISCONNECTED FROM SEAT. MAINTENANCE RECONNECTED LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001120700029 20011207 00029 NM 2001 12 7 CALA0101019 1 20011204 A 5241 SKIN BOEING 737 7373T0 1384582 NM R-1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17309 23360 INSPECTION FOUND A 1/4" CRACK AT LOWER HINGE OF R-1 DOOR EXTERIOR SKIN. A REPAIR WAS INSTALLED IAW ECRA 5210-01458. 2 L 7 2 4F RT A16WE 2001120700030 20011207 00030 NM 2001 12 7 CALA0101020 1 20011204 A 5210 SKIN BOEING 737 7373T0 1384582 NM L-1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14307 23358 INSPECTION FOUND L-1 DOOR SKIN AT AFT INTERIOR EDGE CRACKED AT 4TH AND 5TH STOP FROM BOTTOM. THE CRACKS WERE 1" LONG. TH E CRACKED AREAS WERE REMOVED AND A DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 51-70-11, FIGURE 1. 2 L 7 2 4F RT A16WE 2001120700031 20011207 00031 NM 2001 12 7 USAASB01270 1 20010924 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 533AU 24515 PIT - MAINTENANCE FOUND THE AFT EMERGENCY SEAT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001120700032 20011207 00032 NM 2001 12 7 USAASB01292 1 20011011 A 3350 30043229 LIGHT BOEING 737 737301 1384611 NM EXTERIOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 589US 23934 TPA - MAINTENANCE FOUND THE EXTERIOR AFT SERVICE DOOR ESCAPE SLIDE LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXTERIOR AFT SERVICE DOOR ESCAPE LIGHT ASSY (SOCKET AND REFLECTOR ASSY). OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001120700033 20011207 00033 NM 2001 12 7 USAASB01297 1 20011016 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 504AU 23379 TPA - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE AISLE EMERGENCY LIGHTS, IN THE LAST SIX ROWS OF AFT CABIN, INOPERATI VE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001120700034 20011207 00034 NM 2001 12 7 USAASB01301 1 20011021 A 3350 S106 BATTERY BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 22796 BSI - THE EMERGENCY LIGHT ABOVE THE 1R EXIT FLASHES ON AND OFF. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A16WE 2001120700035 20011207 00035 NM 2001 12 7 USAASB01304 1 20011031 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 776AU 24934 ALB - MAINTENANCE FOUND THE EMERGENCY LIGHTS INOPERATIVE AT ROW 7 BULLNOSE, CEILING EXIT SIGN AT EXIT ROW, AISLE LIGHTS AT ROWS 6 THROUGH 10 AND LEFT OVERWING EXIT SIGN AT ROW 10. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK (P/N 2013 -1A) AND CHARGER ASSEMBLY ABOVE CEILING EXIT SIGN AT LEFT OVERWING EXIT ROW. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001120700036 20011207 00036 NM 2001 12 7 USAASB01305 1 20011101 A 3350 20131A BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 575US 23740 PHL - MAINTENANCE FOUND THE AISLE EMERGENCY LIGHTS, IN THE CABIN, INOPERATIVE. MAINTENANCE FOUND SEVERAL BATTERY PACKS DISCHARGED. REMOVED AND REPLACED BATTERY PACKS IN ASSOCIATION WITH MM 33-51-01. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001120700037 20011207 00037 NM 2001 12 7 USAASB01307 1 20011105 A 3350 20131A BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 586US 23931 CLT - MAINTENANCE FOUND THREE SECTIONS OF CABIN EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THREE CABIN EMERGENCY LIGHT BATTERY PACKS. OPS CHECK OF EMERGENCY LIGHTS GOOD. (M) 2 L 7 2 4F RT A16WE 2001120700038 20011207 00038 NM 2001 12 7 USAASB01308 1 20011106 A 3260 UPLOCK SENSOR BOEING 737 7373B7 1384580 NM LT MLG FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 531AU 24478 CLT - FLT 217 - ON CLIMB-OUT FROM CLT, EN ROUTE TO ATL, CREW RECEIVED A LEFT MLG RED LIGHT AFTER GEAR RETRACTION. CREW ACCOMPLISHED, QUICK REFERENCE HANDBOOK PROCEDURES AND RECYCLED THE GEAR. WHEN GEAR WAS CYCLED DOWN, CREW RECEIVED THREE GREEN GEAR LIGHTS BUT WHEN GEAR WAS RAISED, THEY RECEIVED THE LEFT MLG RED LIGHT AGAIN. FLIGHT RETURNED TO FIELD AT CL T. CREW RECEIVED THREE GREEN GEAR LIGHTS ON GEAR EXTENSION AND THE FLIGHT LANDED AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE LEFT MLG UPLOCK PROXIMITY SENSOR. OPERATIO NAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2001120700039 20011207 00039 NM 2001 12 7 USAASB01309 1 20011106 A 2120 ODOR BOEING 737 737301 1384611 NM CABIN DETECTED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 562AU 23550 CLT - FLT 2135 - AFTER TAKEOFF FROM CLT, EN ROUTE TO MCO, THE FLIGHT ATTENDANTS AND PASSENGERS REPORTED A STRONG SMELL O F BURNING PLASTIC. FLIGHT ATTENDANT REPORTED THAT THE ODOR WAS INTENSIFYING. FLIGHT RETURNED TO FIELD AT CLT AND LANDE D WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE ACCOMPLISHED STATIC CHECKS OF ALL AIR CONDITIONING AND HEAT SYSTEMS, APU BAY, E/E COMPARTMENTS, BAGGAGE BINS, GALLEYS, LAVATORIES AND CABIN. OPS CHECK OF AIR CONDITIONING AND HEAT SYSTEM, WITH AIRCRAFT PRESSURIZED, CHECKS NORMAL. NO UNUSUAL SMELL OR ODOR NOTED. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2001120700040 20011207 00040 NM 2001 12 7 USAASB01310 1 20011112 A 3350 20121 CHARGER BOEING 737 737401 1384701 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 407US 23877 TPA - MAINTENANCE FOUND THE BULLNOSE EMERGENCY LIGHT AT ROW 9, RIGHT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D THE BATTERY CHARGER ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001120700041 20011207 00041 NM 2001 12 7 USAASB01311 1 20011111 A 3350 20131A BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 589US 23934 CLE - MAINTENANCE FOUND THE EMERGENCY LIGHT ABOVE THE FORWARD ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001120700042 20011207 00042 NM 2001 12 7 USAASB01312 1 20011115 A 3350 S106 BATTERY BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 282AU 23115 LGA - MAINTENANCE FOUND THE FORWARD SERVICE DOOR AND FORWARD ENTRY DOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE BATTERIES. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 2001120700043 20011207 00043 NM 2001 12 7 USAASB01314 1 20011117 A 3397 WIRE BOEING 737 7373B7 1384580 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 375US 22954 CLT - PILOT REPORTED WIRES HANGING DOWN FROM BELOW SEAT 1C AND EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPAIRED BROKEN SEAT WIRES. OPERATIONAL CHECK OF EMERGENCY LIGHT NORMAL. (M) 2 L 7 2 4F RT A16WE 2001120700044 20011207 00044 NM 2001 12 7 USAASB01315 1 20011119 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 510AU 23385 TPA - MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY LIGHT EXTINGUISHES AFTER A FEW SECONDS OF OPERATION. MAINTENANCE RE MOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001120700045 20011207 00045 NM 2001 12 7 USAASB01316 1 20011117 A 3350 1000679 LIGHT BOEING 737 7372B7 1384560 NM COCKPIT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 278AU 22890 LGA - COCKPIT EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. (M) 2 L 7 2 4F A16WE 2001120700046 20011207 00046 EA 2001 12 7 2001F00724 2 20011120 A 7200 ENGINE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA RIGHT MALFUNCTIONED A NSVA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 119CJ UC19 AUG - DURING TAKEOFF ROLL, RIGHT OIL PRESS LIGHT CAME ON. ABORTED TAKEOFF. TAXI BACK TO GATE, OIL PRESS GAUGE READ BET WEEN 30-50 PSI. REMOVED AND REPLACED RIGHT ENGINE LEAK AND OPS CHECK GOOD. (M) 2 L 7 2 4T 4 T RT A24CE E4EA 2001120700047 20011207 00047 NM 2001 12 7 2001F00725 1 20011001 A 5330 65B070551 SKIN BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 PAE - FOUND INSPECTION OF FUSELAGE SKIN EXTERNAL, DETECTED A CRACK IN THE SKIN. SKIN WAS ALSO PILLOWED. INTERNAL INSPE CTION REVEALED INNER SKIN EXFOLIATION. PERFORMED MAJOR REPAIR ON EXTERNAL FUSELAGE SKIN AT BS 800 STRINGER 46R IAW GOOD RICH ENGINEERING REPAIR NR 01-5402. (M) 2 L 7 4 4F A20WE 2001120700048 20011207 00048 NM 2001 12 7 2001F00726 1 20011006 A 5743 FITTING BOEING 747 747273C 1384896 NM RT WING CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 PAE - FOUND RIGHT WING LANDING GEAR SUPPORT BEAM END FITTING HAD A CRACK INDICATION ADJACENT TO LUG BUSHING. CORRODED N OTED UPON REMOVAL. REMOVED AND REPLACED FITTING. (M) 2 L 7 4 4F A20WE 2001120700049 20011207 00049 NM 2001 12 7 2001F00727 1 20011106 A 3411 PITOT TUBE BOEING 727 727225 1384077 NM PITOT/STATIC SYS OBSTRUCTED A MYWA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 19 803MA 22434 NO AIRSPEED INDICATION ON CAPTAIN AIRSPEED INDICATOR WHEN AT 100 KNOT AS PER F/O INDICATION DURING TAKEOFF RUN. FOUND D EBRIS INSIDE CAPTAIN PITOT PROBE. FLUSHED CAPTAIN PITOT SYSTEM. SYSTEM OPS CHECK NORMAL IAW MM 34-11-00. AIRCRAFT RET URN TO SERVICE. (M) 2 L 7 3 4F A3WE 2001120700050 20011207 00050 NM 2001 12 7 2001F00728 1 20011027 A 3350 58851 BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 804MA 22435 ON PREFLIGHT TRANSIT, FOUND R1 EMERGENCY EXIT LIGHT INOPERATIVE. TROUBLE SHOT SYSTEM AND FOUND BATTERY PACK CHARGE LOW. REMOVED AND REPLACED BATTERY PACK IAW 33-50-31. OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 3 4F A3WE 2001120700051 20011207 00051 NM 2001 12 7 2001F00729 1 20011027 A 3350 58851 BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 804MA 22435 ON PREFLIGHT TRANSIT, FOUND RT WING FORWARD EMERGENCY EXIT LIGHT INOPERATIVE. TROUBLESHOT SYSTEM AND FOUND BATTERY PACK CHARGE LOW. REMOVED AND REPLACED BATTERY PACK IAW 33-50-31. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. ( M) 2 L 7 3 4F A3WE 2001120700052 20011207 00052 NM 2001 12 7 ASAA0110591 1 20011001 A 3350 88210044 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT IDENTIFIER ON L1, R1 AND R2 DOORS INOPERATIVE. REMOVED AND REPLACE D REMOTE ASSEMBLY BATTERIES (3) AND ALL SIGNS OPERATED NORMAL. (M) 2 L 7 2 4F RT A16WE 2001120700053 20011207 00053 NM 2001 12 7 ASAA0110629 1 20011024 A 3350 8821004 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 FAI - DURING LINE CHECK, FOUND FLOOR TRACK LIGHTING INOPERATIVE AT ROWS 2-3. REMOVED AND REPLACED BATTERY PACK, OPERATI ONAL CHECKS NORMAL. (M) 2 L 7 2 4F RT A16WE 2001120700054 20011207 00054 NM 2001 12 7 ASAA0140114 1 20011013 A 3350 8100022605 LIGHT BOEING 737 7374Q8 NM CABIN MISSING A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 754AS 25095 SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHT MISSING. REPLACED TRACK LIGHT, OPS CHECKED NORMAL. (M) 2 L 7 2 4F RT A16WE 2001120700055 20011207 00055 NM 2001 12 7 ASAA0140118 1 20011021 A 3397 8100022608 WIRE BOEING 737 7374Q8 NM CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 765AS 25102 YVR - BEFORE FLIGHT FOUND EMERGENCY TRACK LIGHTS AT ROW 16 DAMAGED WIRE. REPAIR WIRE, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001120700056 20011207 00056 NM 2001 12 7 ASAA0140135 1 20011104 A 3397 810022608 WIRE BOEING 737 7374Q8 NM CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 780AS 25112 SEA - DURING RON CHECK, FOUND EMERGENCY LIGHT INOPERATIVE AT ROW 1-3. REPAIRED WIRE, OPS NORMAL. (M) 2 L 7 2 4F RT A16WE 2001120700057 20011207 00057 NM 2001 12 7 ASAA0170010 1 20011009 A 3350 1010428 LIGHT BOEING 737 737790 13844CN NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 614AS 30343 SEA - DURING A LINE MAINTENANCE CHECK, THE EMERGENCY LIGHT ABOVE THE OVERWING EMERGENCY EXIT HATCH WAS FOUND INOPERATIVE . REPLACED OVERHEAD STORAGE EMERGENCY EXIT LIGHT. EMERGENCY EXIT LIGHTS NOW OPERATE NORMALLY. (M) 2 L 7 2 4F RT A16WE 2001120700058 20011207 00058 WP 2001 12 7 ASAA0180292 1 20011028 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 958AS 53024 SEA - DURING A LINE MAINTENANCE CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE IN FIRST CLASS CABIN. RECO NNECTED MODULE IN AFT PART OF FIRST CLASS. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2001120700059 20011207 00059 WP 2001 12 7 ASAA0180294 1 20011030 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 933AS 49234 SEA - DURING LINE MAINTENANCE CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE IN FORWARD CABIN. REPLACED D ISCHARGED BATTERY PACK AND REPAIRED BROKEN WIRE AT PIN 1 IN THE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001120700060 20011207 00060 WP 2001 12 7 ASAA0180298 1 20011104 A 3350 0105606 MODULE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 935AS 49236 SEA - DURING PRE-FLIGHT CHECK, ROW 6 TRACK LIGHTING WAS DETERMINED TO BE INOPERATIVE. REPLACED MODULE AT ROW 6. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2001120700061 20011207 00061 SO 2001 12 7 ASOA01219 1 20011107 A 3350 D36604001 BATTERY EMB 120 EMB120RT 3260202 SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 260AS 120132 DURING HANGAR INSPECTION IN TXK, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE NR 1 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001120700062 20011207 00062 SO 2001 12 7 ASOA01220 1 20011109 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT 3260202 SO CABIN DISCHARGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 237AS 120051 FLT 4812 - DURING GROUND INSPECTION IN DFW, THE EMERGENCY LIGHT CIRCUIT BREAKER POPPED. MAINTENANCE REMOVED AND REPLACE D THE NR 2 EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001120700063 20011207 00063 SO 2001 12 7 ASOA01221 1 20011110 A 3350 10130115 SIGN EMB 120 EMB120ER 3260203 SO CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 261AS 120141 FLT 4831 - DURING GROUND INSPECTION IN DFW, THE FLIGHT ATTENDANT EMERGENCY EXIT SIGN WAS FOUND BROKEN. MAINTENANCE REMO VED AND REPLACED THE EMERGENCY EXIT SIGN AT THE BOTTOM EDGE OF THE FLIGHT ATTENDANTS JUMPSEAT. OPERATIONAL CHECK NORMAL . AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001120700064 20011207 00064 NE 2001 12 7 ASOA01222 2 20011111 A 7200 ENGINE AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE RIGHT FAILED A ASOA E A ENGINE SHUTDOWN UNSCHED LANDING A FLAME/FIRE CL CLIMB 1 SO 11 641AS 387 FLT 4037 - AFTER TAKEOFF FROM ATL, THE RIGHT ENGINE QUIT PRODUCING POWER. THE TORQUE DROPPED SUDDENLY TO APPROXIMATELY 15-20 PERCENT AND FLUCTUATED BETWEEN 15-20 PERCENT. THE FLIGHT ATTENDANT REPORTED SEEING FRAMES. THE CAPTAIN SECURED T HE ENGINE AND DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE. (M) 2 H 7 2 4T 4 T RT E20NE 2001120700065 20011207 00065 EA 2001 12 7 ASOA01223 1 20011111 A 5610 NP1393219 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A ASOA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 11 862AS 7476 FLT 4783 - DURING FLIGHT FROM DFW TO AMA, AT FL370, THE LEFT FRONT WINDSHIELD SHATTERED. AN EMERGENCY WAS DECLARED. AI RCRAFT DIVERTED AND LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE LEFT WINDSHIELD ASSEMBLY. AIRCRAFT RETU RNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001120700066 20011207 00066 EA 2001 12 7 ASOA01224 1 20011111 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INTERMITTENT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 836AS 7263 FLT 4431 - DURING GROUND INSPECTION IN ATL, THE EMERGENCY FLOOR LIGHTS WORKED INTERMITTENTLY BETWEEN ROWS 5 AND 8. MAIN TENANCE INSPECTED AND PERFORMED EMERGENCY FLOOR LIGHTING OPERATIONAL CHECKS. ALL LIGHTS WERE OPERATIONAL AT THAT TIME. NO DEFECTS WERE NOTED. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2001120700067 20011207 00067 EU 2001 12 7 ASOA01225 1 20011111 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 636AS 375 DURING C-CHECK INSPECTION IN BNA, BOTH TOP AND BOTTOM SURFACES OF THE FLOORBEAM TOP FLANGE WAS FOUND CORRODED AT FRAMES 36, 38, 39, 40 AND 41. MAINTENANCE REPAIRED CORROSION IAW ASA EO72-53-0119. THE EO REF FORM 8110-3, REPORT NR 01-286, WHICH INCLUDES REPAIR SPECIFICATIONS. (M) 2 H 7 2 4T RT A53EU 2001120700068 20011207 00068 EU 2001 12 7 ASOA01226 1 20011111 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 836AS 375 DURING C-CHECK INSPECTION IN BNA, THE LEFT NR 2 SEAT TRACK OUTBOARD FLOOR BOARD FLANGE, AT A CLIP NUT FASTENER HOLE JUST FORWARD OF FRAME 17, WAS FOUND CORRODED BEYOND ALLOWABLE LIMITS. MAINTENANCE REPAIRED CORROSION IAW ASA EO72-53-0119. THIS EO REFERENCE FAA FORM 8110-3, REPORT NR 01-286, WHICH INCLUDES REPAIR SPECIFICATIONS. (M) 2 H 7 2 4T RT 2001120700069 20011207 00069 EU 2001 12 7 ASOA01227 1 20011111 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 636AS 375 DURING C-CHECK INSPECTION IN BNA, THE LEFT NR 1 SEAT TRACK HAD CORROSION ON THE CLIP NUT HOLE FORWARD OF FRAME 16. CORR OSION WAS ALSO FOUND ON THREE CENTER CLIP NUT HOLES BETWEEN FRAMES 16 AND 17 AND TWO CENTER CLIP HOLES BETWEEN FRAMES 19 AND 20. MAINTENANCE REPAIRED CORROSION IAW ASA E072-53-0119. (M) 2 H 7 2 4T RT A53EU 2001120700070 20011207 00070 EA 2001 12 7 ASOA01228 1 20011112 A 7920 M832481908 LINE CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE LEAKING A ASOA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 11 843AS 7310 ON TAKEOFF FROM ATL, AT 1500 FEET, CAPTAIN NOTED RIGHT ENGINE OIL PRESSURE WAS AT 32 PSI AND FLUCTUATING. THE CAPTAIN T HEN RECEIVED A RIGHT ENGINE OIL PRESSURE WARNING. THE ENGINE WAS SECURED, AND AN EMERGENCY WAS DECLARED. AIRCRAFT LAND ED SAFELY IN ATL. MAINTENANCE INSPECTED AND FOUND THE B AND C SUMP LINES LEAKING. MAINTENANCE REMOVED AND REPLACED THE B AND C FITTING O-RINGS AND TIGHTENED THE OIL LINES AT THE OIL PUMP. THE ENGINE WAS RUN FOR FIVE MINUTES AT 85 PERCENT WITH NO LEAKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001120700071 20011207 00071 SO 2001 12 7 ASOA01229 1 20011112 A 3350 3071BPE LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 504AS 120278 DURING HANGAR MAINTENANCE IN MCN, ONE RED LIGHT WAS DISCOVERED OUT ON THE FLOOR TRACK LIGHTING AT THE OVERWING EXIT. MA INTENANCE REMOVED AND REPLACED LAMP ON THE FLOOR TRACK ASSEMBLY AT THE OVERWING EXIT. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001120700072 20011207 00072 EA 2001 12 7 ASOA01230 1 20011112 A 3350 601R461011 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 836AS 7263 DURING GROUND INSPECTION IN ATL, THE EMERGENCY LIGHT STRIP AT ROW 6 WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE FLOOR LIGHTING STRIP AT ROW 6. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2001120700073 20011207 00073 SO 2001 12 7 ASOA01231 1 20011110 A 5347 12015995003 SEAT TRACK EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 280AS 120231 DURING C-CHECK INSPECTION IN BNA, THE LEFT FLOOR SEAT TRACK, CENTER SECTION, WAS FOUND CORRODED BETWEEN FRAMES 22 AND 32 . MAINTENANCE REMOVED THE SEAT TRACK IAW SRM 51-40-2. A NEW SEAT TRACK WAS LOCATED AND DRILLED IAW SRM 51-25-00 AND 51 -40-6. AIRCRAFT WILL RETURN TO SERVICE UPON COMPLETION OF C-CHECK. (M) 2 L 7 2 4T RT A31SO 2001120700074 20011207 00074 SO 2001 12 7 ASOA01232 1 20011110 A 5347 12016000003 SEAT TRACK EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 280AS 120231 DURING C-CHECK INSPECTION IN BNA, THE RIGHT FLOOR SEAT TRACK, CENTER SECTION, WAS FOUND CORRODED BETWEEN FRAMES 24 AND 3 2. MAINTENANCE REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW CPM 51-14-00. THE SEAT TRACK WAS REMOVED IAW SRM 51-40- 02. A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-40-02. AIRCRAFT WILL RETURN TO SERVICE UPON COMPLETION OF C-CHECK. (M) 2 L 7 2 4T RT A31SO 2001120700075 20011207 00075 NM 2001 12 7 AWXA200100616 1 20011124 A 5311 654655017 FRAME BOEING 737 7373B7 1384580 NM DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 328AW 23377 MCN - MAJOR REPAIR - "C" - FRAME BS 787 UPPER FLANGE BETWEEN STR 24 AND 25 R/H SIDE DENTED OUT OF LIMITS PER B737-300 SR M 53-00-07, PG 101, 102, FIG 1. REMOVED DENTED PORTION OF FRAME AT BS 787 BETWEEN STR 24 AND 25 R/H SIDE IAW B737-300 SR M 51-70-11, PG 1-6, FIG 1. 2 L 7 2 4F RT A16WE 2001120700076 20011207 00076 NM 2001 12 7 AWXA200100617 1 20011124 A 5313 6545767512 STRINGER BOEING 737 7373B7 1384580 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 328AW 23377 MCN - MAJOR REPAIR - "C" - STR 16 L/H BS 504C HAS .5" CRACK, VISUALLY CONFIRMED BY 10X MAGIFICATION. MAINTENANCE CUT OUT CRACKED AREA ON STR 16 L/H BS 504C, FABRICATED A NEW CHANNEL AND INSTALLED IAW AWA ER 03-5312-01094-DD1. 2 L 7 2 4F RT A16WE 2001120700077 20011207 00077 NM 2001 12 7 AWXA200100619 1 20011127 A 5311 BAC14902808 FRAME BOEING 737 7373B7 1384580 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 328AW 23377 MCN - MAJOR REPAIR - "C" - 4" X 1" AREA OF FUSELAGE FRAME AND 6" X 4" AREA OF FUSELAGE SKIN CORRODED AT BS 499, WL 158, LBL 2 TO RBL 2. MAINTENANCE REMOVED CORROSION ON SKIN AND FRAME AT BS 499, LBL 2 TO RBL 2 IAW B737-300 SRM 51-10-02, PG 19 & 20. SKIN WITHIN LIMITS IAW B737-300 SRM 530-00-01, PG 102-108, FRAME WAS OUT OF LIMITS IAW B737-300 SRM 53-00-07 PG 101-104. CUT OUT CORRODED SECTION OF FRAME; FABRICATED AND INSTALLED FILLER AND SUPPORT IAW B737-300 SRM 51-40-02 PG 2- 4 AND SRM 53-00-07, 201 PG 210-212. 2 L 7 2 4F RT A16WE 2001120700078 20011207 00078 SO 2001 12 7 ASOA01233 1 20011110 A 5330 SKIN EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 280AS 120231 DURING C-CHECK INSPECTION IN BNA, THE LOWER FUSELAGE WAS FOUND CORRODED ON THE EXTERNAL SKIN BETWEEN FRAMES 7 AND 8 WHER E THE DME ANTENNA MOUNTS BETWEEN STRINGERS 21 LEFT AND 21 RIGHT. MAINTENANCE REMOVED CORROSION IAW CPM 51-14-00. A NEW INSIDE DOUBLER WAS FABRICATED IAW SRM 51-25-00. INSTALLED PER SRM 51-40-02. AN EXTERNAL DOUBLER WAS FABRICATED IAW SR M 53-00-01 AND INSTALLED IAW SRM 51-40-02. AIRCRAFT WILL RETURN TO SERVICE UPON COMPLETION OF C-CHECK. (M) 2 L 7 2 4T RT A31SO 2001120700079 20011207 00079 EU 2001 12 7 ASOA01236 1 20011111 A 5330 SKIN AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 636AS 375 DURING C-CHECK INSPECTION IN BNA, A CRACK WAS DISCOVERED AT THE RIGHT LAP SEAM BETWEEN STRINGER 10 RIGHT AND 11 RIGHT AT FRAMES 25-29. MAINTENANCE REPAIRED THE CRACK IAW ASA EO72-53-0120. THIS EO REF ATR SRM 53-00-00, FIGURE 425. AIRCRAF T RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001120700080 20011207 00080 EA 2001 12 7 ASOA01237 1 20011115 A 3350 100865 BATTERY CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 850AS 7355 FLT - 4460 - DURING GROUND INSPECTION IN MGM, CREW REPORTED THE EMERGENCY LIGHTING SYSTEM WOULD NOT TEST. THE SYSTEM VO LTS FELL TO 4.5 VOLTS IN 30 SECONDS. CAPTAIN CHARGED THE SYSTEM BATTERIES FROM 0750 TO 0851. MAINTENANCE OBSERVED THE EMERGENCY LIGHTING TEST FOR ONE MINUTE. SYSTEM TEST GOOD. NO FAULTS WERE DISCOVERED. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2001120900001 20011209 00001 NM 2001 12 9 PCAA0112167 1 20011206 A 2910 82940014107 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003 NM CENTER WING LEAKING A PCAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 EA 13 817EX 191 PHL-HPN FLIGHT #3668. CREW REPORTED THEY LOST #2 HYDRAULIC SYSTEM CONTENTS, AND #2 HYDRAULIC ISOLATION VALVE CAUTION LIG HT ILLUMINATED.EMERGENCY WAS DECLARED AIRCRFAFT RETURNED TO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND F OUND SPOILER HYDRAULIC LINE BETWEEN WINGS TO BE LEAKING.2 HYDRAULIC FLEX LINES WERE INSTALLED AS AN INTERIM REPAIR IN AC CORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL 20-50-52. OPERATIONAL CHECK GOOD PER DASH 8 MAINTENANCE MANUAL.AIRCR AFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001120900002 20011209 00002 2001 12 9 RAIA00111019 4 20011129 A 3400 7011672112 SYMBOL GENERATOR JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 570HK 165 41089 7145-MEM-SYMBOL GENERATOR FAILED ON TAKE OFF ROLL. MAINTENANCE REMOVED AND REPLACED SYMBOL GENERATOR IAW J41 MAINTENANCE MANUAL. 2 L 7 2 4T RT A41NM 2001120900003 20011209 00003 EU 2001 12 9 RAIA00111020 1 20011129 A 2130 32149602 VALVE AEROSP ATR72 ATR72202 8680940 EU FAULTY A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 723TE 20508 10553 283 7126-STL-RIGHT PACK VALVE FAULTED DURING TAXI. MAINTENANCE REMOVED AND REPLACED RIGHT PACK VALVE IAW ATR MAINTENANCE MAN UAL. 2 H 7 2 4T RT A53EU 2001120900004 20011209 00004 EU 2001 12 9 RAIA00112001 1 20011204 A 3350 16701 LIGHT AEROSP ATR72 ATR72202 8680940 EU CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 721TE 217 MX-STL-FOUND SEVERAL FLOOR PATH LIGHTS INOP. REPLACED BULBS IAW ATR MAINTENANCE MANUAL 2 H 7 2 4T RT A53EU 2001121000001 20011210 00001 NM 2001 12 10 SWAA013267 1 20011205 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 363SW 26574 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 525, ABOVE STR 10R. REPAIRED SKIN PER SWA RA AND SRM. 2 L 7 2 4F RT A16WE 2001121000002 20011210 00002 NM 2001 12 10 SWAA013268 1 20011204 A 5320 6546546 TIE CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 386SW 26601 DURING SCHEDULED 1/4D CHECK, FOUND TIE CLIP CRACKED AT BS 727B, STR 26R. REMOVED AND REPLACED TIE CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001121000003 20011210 00003 NM 2001 12 10 SWAA013270 1 20011203 A 5315 6545410 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED D CHECK, FOUND LONGITUDINAL BEAM CRACKED (2 EA) AT BS 727A, WL 208, LBL 44 AND RBL 23. REPAIRED BEAM P ER BFG ER. 2 L 7 2 4F RT A16WE 2001121000004 20011210 00004 NM 2001 12 10 SWAA013272 1 20011205 A 5330 6545768 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 338, STR 17L , FWD ENTRY DOOR CUT OUT. REPAIRED SKIN PER RA. 2 L 7 2 4F A16WE 2001121000005 20011210 00005 NM 2001 12 10 SWAA013273 1 20011205 A 5330 6545776 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 800, FWD CORNER CUT OUT OF AFT CARGO DOOR. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001121000006 20011210 00006 NM 2001 12 10 SWAA013274 1 20011206 A 5313 BAC1498 STRINGER BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CRACKED FROM BS 344 TO BS 360, STR 8R. REMOVED AND REPLACED STR SECTION PER SRM. 2 L 7 2 4F A16WE 2001121000007 20011210 00007 NM 2001 12 10 SWAA013276 1 20011206 A 5310 6546543 TIE CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 663.5, STR 4R. REMOVED AND REPLACED STR TIE CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001121000008 20011210 00008 NM 2001 12 10 SWAA013277 1 20011206 A 5310 6516300 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED 1/4D CHECK, FOUND WEB CRACKED AT BS 178, LBL 17.1 AND WL 183. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001121000009 20011210 00009 NM 2001 12 10 SWAA013256 1 20011205 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 643SW 27716 EEPLS TRACK COVERS OUT OF POSITION. SECURED COVERS PER MM. 2 L 7 2 4F RT A16WE 2001121000010 20011210 00010 NM 2001 12 10 SWAA013258 1 20011204 A 5240 6545871 DOOR FRAME BOEING 737 7372T4 1384492 NM R2 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED 1/4D CHECK, FOUND AFT SERVICE DOOR FWD FRAME CRACKED JUST BELOW UPPER DOOR HINGE. REMOVED AND REPLACED DOOR PERMM. 2 L 7 2 4F A16WE 2001121000011 20011210 00011 NM 2001 12 10 SWAA013259 1 20011205 A 5230 6545871 DOOR FRAME BOEING 737 7373H4 1384600 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 327SW 23691 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR FWD FRAME CRACKED AT UPPER SECTION. REMOVED AND REPLACED DOOR PER MM.. 2 L 7 2 4F RT A16WE 2001121000012 20011210 00012 NM 2001 12 10 SWAA013261 1 20011205 A 5753 6546430 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 640SW 27713 DURING SCHEDULED 1/2D CHECK, FOUND LT INBD T/E FOREFLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED FLAP ASSY PE R MM. 2 L 7 2 4F RT A16WE 2001121000013 20011210 00013 NM 2001 12 10 SWAA013262 1 20011204 A 2750 AV13J5144 BYPASS VALVE BOEING 737 7373G7 1384595 NM T/E FLAP ERRATIC A SWAA K NONE F FLT CONT AFFECTED AP APPROACH 1 SW 07 671SW 23785 T/E FLAPS WOULD NOT STOP AT 35 DEGS WHEN FLAP HANDLE WAS MOVED FROM 30 TO 40 DEGS. WORKS OK ON THE GROUND. REMOVED AND REPLACED T/E FLAP BYPASS VALVE AND FLAP DRIVE MOTOR PER MM. 2 L 7 2 4F RT A16WE 2001121000014 20011210 00014 NM 2001 12 10 SWAA013263 1 20011205 A 5754 65C26644 ANGLE BOEING 737 7373A4 1384585 NM L/E SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED A1 CHECK, FOUND NR 3 L/E SLAT T-ANGLE CRACKED AT ACTUATOR ATTACH AREA. REMOVED AND REPLACED SLAT ASSY. 2 L 7 2 4F RT A16WE 2001121000015 20011210 00015 NM 2001 12 10 SWAA013264 1 20011204 A 5531 6550577 SPAR BOEING 737 737317 138447P NM VERTICAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED D CHECK, FOUND VERTICAL FIN FRONT SPAR CRACKED AT SLING ATTACH POINT FASTENER HOLE. REPAIRED SPAR PER ER 01-5587. 2 L 7 2 4F RT A16WE 2001121000016 20011210 00016 NM 2001 12 10 DL75A011665 1 20011014 A 2750 285N001132M FSEU BOEING 757 757212 1384951 NM FLAP/SLAT SYS MALFUNCTIONED A DALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SO 27 750AT 23126 IN CRUISE RECEIVED EICAS MSG LEADING EDGE SLAT ASYMMETRY WITH LEADING EDGE INDICATOR LIGHT. FLAPS INDICATED BETWEEN UP AND 1 POSITION. HANDLE WAS IN UP OR 0 POSITION. VISUAL CHECK CONFIRMED LEADING EDGE SLATS IN UP POSITION. CYCLED FLAP S AND SLATS AFTER CLEARING FSEU NR 1. FAULTING SLAT HANDLE OUT OF DETENT, ALL MESSAGES CLEARED. FSEU NR 1 REPLACED PRE CAUTIONARY. GOOD FOR SERVICE. 2 L 7 2 4F RT A2NM 2001121000017 20011210 00017 NM 2001 12 10 DL75A011670 1 20011012 A 5315 146N51116 FLOORBEAM BOEING 757 757212 1384951 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 750AT 23126 THE UPPER CAP OF THE FS 1681 PASSENGER FLOORBEAM WAS FOUND CORRODED IN SEVERAL AREAS. THE ENTIRE CAP WAS CUT OFF TO REM OVE ALL CORROSION. A NEW CAP WAS FABRICATED AND INSTALLED IN PLACE OF THE REMOVED CAP PER ER/A 381633-14, REV A. 2 L 7 2 4F RT A2NM 2001121000018 20011210 00018 NM 2001 12 10 DL75A011837 1 20011120 A 5320 SILL BOEING 757 757212 1384951 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 757AT 23127 THE LOWER DOOR SILL OF THE C2 DOOR OPENING WAS BADLY CORRODED AND NEEDED TO BE REPLACED. 2 L 7 2 4F RT A2NM 2001121000019 20011210 00019 NM 2001 12 10 DL75A011838 1 20011120 A 5411 311N3110 SPAR BOEING 757 757212 1384951 NM NR 2 PYLON GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 757AT 23127 THE FWD UPPER SPAR WEB OF THE NR 2 PYLON WAS FOUND WITH A DEEP GOUGE AT NAC STA 128 AT RBL 2. THE WEB WAS CUT FWD AND A FT OF THE DAMAGE AND THE DAMAGED SECTION OF WEB WAS REMOVED. A NEW SECTION OF WEB WAS SPLICED IN WITH ALUMINUM DOUBLERS PER ER/A 381993-14, REV A. 2 L 7 2 4F RT A2NM 2001121000020 20011210 00020 NM 2001 12 10 DL764011653 1 20011011 A 2750 INDICATOR BOEING 767 767432ER 1385134 NM COCKPIT MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 836MH 29709 AIR TURNBACK- TRAILING EDGE FLAP DISAGREE MESSAGE ON DEPARTURE, FLAPS LOWERED USING ALTN FLAPS. MAINT-- FSEU BITE SEE F IM 27-51104 MSG, T/S PER FIM 27-51-00 PG 150 FIG 105A SHT 1 AND 2. FOUND OVERLOAD TRIP INDICATORS ON TRAILING EDGE ACTU ATORS NR 3, 6 & 8. RESET INDICATORS, NO PREVIOUS TRIP RECORDED, OPERATED FLAPS NUMEROUS TIMES, CHECKS NORMAL. VISUAL I NSPECTION OF LEADING EDGE AND TRAILING EDGE FLAP, SYS CHECKS OK. 2 L 7 2 4F RT A1NM 2001121000021 20011210 00021 NM 2001 12 10 DL764011733 1 20011028 A 7334 1335M77P01 PRESSURE SWITCH BOEING 767 767424ER 1385270 NM GE CF6 CF680 30025 NE NR 2 ENGINE LEAKING A DALA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 27 833MH 29706 706193 FOUND RIGHT ENGINE LEAKING FUEL. FOUND FUEL PRESSURE SWITCH LEAKING AT END. REPLACED FUEL PRESSURE SWITCH PER M/M 73-3 3-01, OPS LEAK CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E13NE 2001121000022 20011210 00022 NM 2001 12 10 DL764011755 1 20011102 A 3397 CONNECTOR BOEING 767 767432ER 1385134 NM CABIN LOOSE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 839MH 29712 EGRESS LIGHTING AT SEATS 10AB, 26AB THRU 32AB INOP. TIGHTENED LOOSE CONNECTOR, OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 2001121000023 20011210 00023 NM 2001 12 10 DL764011872 1 20011127 A 3350 LIGHT BOEING 767 767432ER 1385134 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 825MH 29696 THE 29AB EMERGENCY LIGHT INOP. INSTALLED BULBS AND LENS COVER, OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 2001121000024 20011210 00024 NM 2001 12 10 DL767011700 1 20011022 A 5753 113T23018A RIB BOEING 767 767232 1385132 NM T/E FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 101DA 22213 INBOARD AFT RT FLAP WAS FOUND WITH ELONGATED FASTENER HOLES IN THE LEADING EDGE RIBS. REPAIR PER ER/A 410559-14 AND NOR DAM EWO E0034025, REV A. 2 L 7 2 4F RT A1NM 2001121000025 20011210 00025 NM 2001 12 10 DL767011717 1 20011024 A 5755 113T510223G SKIN BOEING 767 767232 1385132 NM SPOILER DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 103DA 22215 DELAMINATION TO THE UPPER SKIN OF THE SPOILER. REPAIRED PER ER/A 410579-14. 2 L 7 2 4F RT A1NM 2001121000026 20011210 00026 NM 2001 12 10 DL767011723 1 20011026 A 2781 TARGET BOEING 767 767232 1385132 NM L/E SLAT OUT OF ADJ A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 103DA 22215 ON T/O, LEADING EDGE LIGHT FLICKERED AND STICK SHAKER AFTER T/O LIGHT CAME ON STBY FLAPS WERE RETRACTED BUT STUCK BETWEE N UP AND 1 HAD ASSOCIATED L/E SLAT ASYM EICAS MSG. FOUND TARGETS ON SLATS NUMBER 2 AND 7 OUT OF ADJUSTMENT. ADJUSTED T ARGETS AND PERFORMED BITE TEST OF PSEU. NO FAULTS NOTED. 2 L 7 2 4F RT A1NM 2001121000027 20011210 00027 NM 2001 12 10 DL767011844 1 20011122 A 3350 3015645 SOCKET BOEING 767 767232 1385132 NM EXTERIOR DEFECTIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 105DA 22217 LEFT OFFWING SLIDE LIGHT INOP. REPLACED LIGHT SOCKET, OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 2001121000028 20011210 00028 NM 2001 12 10 DL76G011677 1 20011015 A 5742 112T700529 FITTING BOEING 767 7673P6 1385105 NM LT WING MISMANUFACTURED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 152DL 24984 DURING ACCOMPLISHMENT OF REWORK TO THE LT STRUT AS DETAILED IN THE STRUT IMPROVEMENT PROGRAM THE INBOARD AFT PITCH LOAD FITTING WAS INCORRECTLY MACHINED. REPAIR ER/A 398045-14AD. 2 L 7 2 4F RT A1NM 2001121000029 20011210 00029 2001 12 10 DL76G011769 4 20011031 A 3417 4040800911 ADC BOEING 767 767332 1382001 NM E/E BAY FAILED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 1605 30198 AIR TURNBACK DUE TO AIRSPEED AND ALTITUDE EICAS DISAGREE. ALTIMETERS SPLIT BY 400 FT AND INCREASING. UNABLE TO ENTER R VSM. CADC REPLACED. 2 L 7 2 4F RT A1NM 2001121000030 20011210 00030 NM 2001 12 10 DL76G011791 1 20011112 A 2120 ODOR BOEING 767 767332 1382001 NM CABIN DETECTED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 1602 29694 BURNING SMELL IN AFT GALLEY OVERHEAD JUMPSEATS. INSPECTED AFT GALLEY AREA. OVENS COFFEEMAKERS AND EQUIP NORMAL. INSPE CTED IN OVERHEAD AREA. ALL LIGHTING AND EQUIP NORMAL. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2001121000031 20011210 00031 2001 12 10 DL76G011807 4 20011114 A 2330 PROJECTOR BOEING 767 7673P6 1385105 NM CABIN MALFUNCTIONED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 153DL 24985 SMOKE SMELL FROM FORWARD PROJECTOR AREA IN MAIN CABIN AS WELL AS VIDEO CLOSET RED POWER SWITCHES 2. SMELL PERSISTED AS LONG AS POWER WAS ON THE PROJECTOR. GREEN STATUS LIGHT ON UNIT LIT. SMELL DIMINISHED WHEN CB/S PULLED. NO SMOKE SEEN ONLY BAD HOT SMELL PRESENT. REPLACED PROJECTOR WHICH WAS ALSO BAD FROM STOCK. DEFER TO MCO. 2 L 7 2 4F RT A1NM 2001121000032 20011210 00032 NM 2001 12 10 DL76G011812 1 20011115 A 3810 ROD BOEING 767 7673P6 1385105 NM WATER TANK SHEARED A DALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 27 153DL 24985 ON TAKEOFF FROM FRA HEARD BANGING SOUND, THERE AFTER LOST ALL POTABLE WATER. FOUND 2 TIE RODS SHEARED AND MAIN WATER TA NK LEAKING AT LOWER FITTING AND FIBERGLASS SURROUND. DRAINED WATER TANK AND SECURED TANK WITH CARGO STRAP, WATER COMPRE SSOR C/B ON P33 PNL PULLED/COLLARED. REQ TANK REPAIR AND 2 TIE RODS (P/N 381202073). FWD TO MCO AND PLACARD PER MEL 38 -10-0.IPC REF 38-11-01-01. 2 L 7 2 4F RT A1NM 2001121000033 20011210 00033 NM 2001 12 10 DL76G011818 1 20011117 A 2421 IDG BOEING 767 7673P6 1385105 NM LT ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 156DL 26511 25354 P1098 FLT 83/17 NCE/JFK DIVERTED YQX DUE APU FAULTED. AFTER IT WAS STARTED DUE THE LT IDG DRIVE LIGHT AND THE LT IDG WAS DISC ONNECTED. A/C LANDED SAFELY AT YQX. THE APU WAS SERVICED AND THE LT IDG WAS PLACED ON MCO. A/C RELEASED PER MEL. 2 L 7 2 4F RT A1NM 2001121000034 20011210 00034 NM 2001 12 10 DL76L011696 1 20011021 A 3350 20121 CHARGER BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1200K 28457 BATTERY CHARGER MID-LEFT CABIN INOP. 2 L 7 2 4F RT A1NM 2001121000035 20011210 00035 WP 2001 12 10 CALA0101022 1 20011207 A 5320 CHANNEL DOUG DC9 DC982 3022082 WP R FWD MLG DR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77827 49487 INSPECTION FOUND A 2.5" CRACK IN R/H W/W FORWARD DOOR JAMB CHANNEL, O/B OF CENTER SPLICE. THE DOOR JAMB CHANNEL WAS REMO VED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-30-0. 2 L 7 2 4F A6WE 2001121000036 20011210 00036 NM 2001 12 10 CALA0101023 1 20011208 A 5347 TRACK BOEING 737 7373T0 1384582 NM STA 727-727E CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14307 23358 INSPECTION FOUND AFT CARGO L/H O/B FLOOR TRACK CORRODED AT STA 727-727C. THE FLOOR TRACK WAS REMOVED AND REPLACED IAW SR M 53-60-53 AND 53-00-53. 2 L 7 2 4F RT A16WE 2001121000037 20011210 00037 NM 2001 12 10 CALA0101025 1 20011209 A 5414 PLATE BOEING 737 7373T0 1384582 NM #1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14307 23358 INSPECTION FOUND A 4" CRACK IN #1 I/B PYLON NUTPLATE STRIP BETWEEN PANEL #5742 AND #5743. THE NUTPLATE STRIP WAS REMOVED AND REPLACED IAW SRM 51-10-2 AND 54-50-71. 2 L 7 2 4F RT A16WE 2001121000038 20011210 00038 NM 2001 12 10 DL76L011751 1 20011101 A 2120 ODOR BOEING 767 767332 1382001 NM COCKPIT DETECTED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 192DN 28449 PRIOR TO DESCENT HAD A STRONG ELECTRICAL BURNING SMELL WITH NO VISUAL CUES. CHECKED C/BS AND TURNED BOTH UTILITY BUSSES OFF AND SMELL DISAPPEAR. INSPECTED MAIN AVIONICS BAY, UNDERNOSE BAY AND REAR OF MAINT TEST PANEL FOR ANOMALIES OR BUR NING SMELL. KEPT GALLEY POWER AND ALL AVIONICS TURNED ON FOR ALL TRANSIT TIME, NOTHING TO REPORT. 2 L 7 2 4F RT A1NM 2001121000039 20011210 00039 NM 2001 12 10 DL76L011753 1 20011102 A 3610 77328810 SHUTOFF VALVE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE BLEED AIR MALFUNCTIONED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 173DN 24800 724165 LEFT DUCT PRESS FLUCTUATED PLUS/MINUS 15 PSI DURING CLIMBOUT. RETURNED TO JFK. REPLACED PRV CONTROLLER AND PRSOV VLV P ER M/M. T/O PWR RUN PER PFHB, ALL NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2001121000040 20011210 00040 NM 2001 12 10 DL76L011768 1 20011105 A 3350 BPS73 POWER SUPPLY BPS73 BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 183DN 11915 27110 SEAT 1-5AB EMERGENCY INOP. REPLACED POWER SUPPLY, OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 2001121000041 20011210 00041 2001 12 10 DL76L011820 4 20011117 A 2330 1303400100 ENTERTAIN SYS BOEING 767 767332 1382001 NM VIDEO CLOSET SHORTED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 199DN 28456 STRONG ELECTRICAL ODOR EMANATING FROM VICINITY OF ENTERTAINMENT SYSTEM. FOUND PESCV COOLING FAN SHORTED. REPLACED PESC V (P/N 1303400+100). 2 L 7 2 4F RT A1NM 2001121000042 20011210 00042 NM 2001 12 10 DL76L011868 1 20011127 A 3697 WIRE BOEING 767 767332 1382001 NM BLEED AIR BROKEN A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 180DN 25985 ON CLIMBOUT, LEFT ENGINE PRV MESSAGE APPEARED ON EICAS. TRIED CYCLING BLEED AND RESETTING SEVERAL C/B`S, NO HELP. FOUN D BROKEN WIRES ON PRV. REPAIRED WIRES AND RUNUP OK. 2 L 7 2 4F RT A1NM 2001121000043 20011210 00043 NM 2001 12 10 DL76L011879 1 20011128 A 3350 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 176DN 25061 EMERGENCY AISLE LIGHT POWER SUPPLY FOR ROWS 6 THROUGH 20 LT SIDE INOP. REPLACED POWER SUPPLY AT ROW 6 LT SIDE, OPS CHEC KS OK. 2 L 7 2 4F RT A1NM 2001121000044 20011210 00044 NM 2001 12 10 DL76S011650 1 20011011 A 5412 311T12315 BULKHEAD BOEING 767 767332 1382001 NM NR 2 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 120DL 23279 DURING ACCOMPLISHMENT OF PYLON SIP MOD, CRACK INDICATIONS WERE FOUND IN THE MID STRUT BULKHEAD LAYER. REPAIR ER/A 39805 1-14AD. 2 L 7 2 4F RT A1NM 2001121000045 20011210 00045 NM 2001 12 10 DL76S011656 1 20011011 A 5730 112T41022 SKIN BOEING 767 767332 1382001 NM RT WING WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 120DL 23279 DURING ACCOMPLISHMENT OF SIP MOD ON THE NR 2 PYLON WEAR DAMAGE FROM A HYDRAULIC LINE CLAMP SCREW WAS FOUND ON THE LOWER WING SKIN. THE DAMAGE IS LOCATED AT APPROX WS 420 AND IS BETWEEN WING STRINGERS L7 AND L8. THE WORN AREA WAS APPROXIMA TELY .11 INCH IN DEPTH AND .375 INCH IN DIAMETER. REPAIR ER/A 398071-14. 2 L 7 2 4F RT A1NM 2001121000046 20011210 00046 NM 2001 12 10 DL76S011695 1 20011020 A 3350 SOCKET BOEING 767 767332 1382001 NM EXTERIOR DEFECTIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 137DL 25306 SLIDE EMERGENCY LIGHT INOP LEFT AFT CABIN DOOR EXTERIOR. REPLACED POWER SUPPLY, NO HELP. REPLACED SOCKET ASSY, OPS CHE CKS OK. 2 L 7 2 4F RT A1NM 2001121000047 20011210 00047 NM 2001 12 10 DL76S011707 1 20011022 A 3350 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 118DL 23277 ON L/O, FOUND LEFT WING OVERWING EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY AND BATTERY PACK, CHECKS GOOD. 2 L 7 2 4F RT A1NM 2001121000048 20011210 00048 NM 2001 12 10 DL76S011805 1 20011114 A 5755 015T141534 SKIN BOEING 767 767332 1382001 NM SPOILER DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 116DL 23275 THE RT WING, INBOARD SPOILER UPPER AND LOWER SKINS WERE FOUND DAMAGED DURING OVERHAUL AT NORDAM. REPAIR PER ER/A 410639 -14. 2 L 7 2 4F RT A1NM 2001121000049 20011210 00049 NM 2001 12 10 DL76S011808 1 20011114 A 3610 SHUTOFF VALVE BOEING 767 767332 1382001 NM BLEED AIR MALFUNCTIONED A DALA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 128DL 24078 ON CLIMBOUT APPROX 5 MIN AFTER T/O, F/A'S REPORTED STRONG ODOR/FUMES HOT SMELL IN MID CABIN AREA. UPON TURNING OFF RT P ACK SMELL WENT AWAY. RECYCLED RT PACK AND HOT SMELL RETURNED. RETURNED TO ATL. MTC IN PROGRESS. REPLACED RT ENG HPSO V AND CONTROLLER PER M/M. BOTH CHECK GOOD. RAN BOTH PACKS O OF ENG AIR AT HIGH POWER. NO SMELLS/FUMES NOTED. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2001121000050 20011210 00050 NM 2001 12 10 DL76S011811 1 20011114 A 3610 CONTROLLER BOEING 767 767332 1382001 NM BLEED AIR MALFUNCTIONED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 128DL 24078 580253 ON CLIMBOUT APPROX 5 MIN AFTER TAKEOFF. FLIGHT ATTENDANT REPORTED STRONG ODOR AND HOT SMELL IN MID CABIN AREA. UPON TU RNING OFF RIGHT PACK SMELL WENT AWAY. RECYCLED RIGHT PACK AND HOT SMELL RETURNED. RETURNED TO ATL. REPLACED RT ENG HP VALVE, RT HP CONTROLLER, RAN BOTH PACKS AND ENGINE AT HIGH PWR SETTINGS. THERE WERE NO FUMES OR HOT SMELL NOTICED. 2 L 7 2 4F RT A1NM 2001121000051 20011210 00051 NM 2001 12 10 DL76S011832 1 20011120 A 2920 CHECK VALVE BOEING 767 767332 1382001 NM RAT MODULE FAILED A DALA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 27 118DL 23277 THE CHECK VALVE ON THE RAT MODULE IN THE RT WHEEL WELL BLEW OUT CAUSING A LOSS OF HYD QTY AND PRESSURE IN THE CENTER SYS TEM. REPLACED MODULE. 2 L 7 2 4F RT A1NM 2001121000052 20011210 00052 2001 12 10 DL777011748 4 20011101 A 2230 AUTOTHRUST SYS BOEING 777 777232 1385232 NM COCKPIT MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 862DA 29734 AFTER ENG START WITH BRAKES SET THE AUTOTHROTTLES ENGAGED BY THEMSELVES AND ADVANCED TO THE TAKEOFF POWER. NO PRESENT L EG FAULTS NO EXISTING FDES. PERFORMED SYS TEST, RESET OF LT AND RT AIMS CABINETS, PERFORMED LT AND RT TMC. CABINET SER VO LOOP TESTS ALL CKS GOOD. 2 L 7 2 4F RT T00001SE 2001121000053 20011210 00053 NM 2001 12 10 DLM11011734 1 20011029 A 2121 6054578 FAN DOUG MD11 MD11 3023602 NM CABIN FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 809DE 48480 NOXIOUS ODOR IN CABIN AREA ACCOMPANIED BY LOUD NOISE IN THE OVERHEAD AREA AT ROW 11. COORDINATED WITH MCC VIA SATCOM. ADVISED PULLING PASS AIR OUTLET FAN CTRL C/B N8. ODOR DISSIPATED AND NOISE SILENCED. VERIFIED PASS AIR OUTLET FAN BAD /NOISY. REPLACED SAME. 2 L 7 3 4F RT A22WE 2001121000054 20011210 00054 NM 2001 12 10 DLM11011773 1 20011107 A 3233 ACTUATOR DOUG MD11 MD11 3023602 NM CENTER GEAR BENT A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 808DE 48479 ATB DUE TO CENTER GEAR WILL NOT RETRACT. FOUND CENTER GEAR RETRACT ACTUATOR BENT. REPLACING SAME. 2 L 7 3 4F RT A22WE 2001121000055 20011210 00055 NM 2001 12 10 DLM11011783 1 20011108 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZ STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 803DE 48474 CORROSION FOUND IN THE HORIZONTAL STABILIZER ATTACH BOLT BARREL NUT BORES. REPAIRED ER/A 398116-14. 2 L 7 3 4F RT A22WE 2001121000056 20011210 00056 NM 2001 12 10 DLM11011851 1 20011124 A 2121 19A6511 FAN DOUG MD11 MD11 3023602 NM LAVATORY FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 803DE 48474 LIGHT ELECTRICAL FUMES IN 2R LAV. REPLACED 2R LAV VENT FAN. 2 L 7 3 4F RT A22WE 2001121000057 20011210 00057 NM 2001 12 10 DLM11011853 1 20011124 A 3040 9615046004 CONTROLLER DOUG MD11 MD11 3023602 NM E/E BAY FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 803DE 48474 LEFT WINDSHIELD HEAT FAIL LEVEL 1 ALERT SMELLED FUMES TURNED HEAT OFF. REMOVED AND REPLACED LEFT WINDSHIELD ANTI-ICE CO NTROLLER PER M/M CHECKS GOOD. NO ODORS OR DEFECTS NOTED. 2 L 7 3 4F RT A22WE 2001121000058 20011210 00058 NM 2001 12 10 DLM11011866 1 20011126 A 3397 M2430822F CONNECTOR DOUG MD11 MD11 3023602 NM CABIN BURNED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 814DE 48769 AFT CABIN OVERHEAD AND SIDEWALL LIGHTS INOP. CIRCUIT BREAKER TRIPPED AND WILL NOT RESET. FOUND CONNECTOR BURNT AT AFT CABIN LIGHTS DIMMER. REPLACED CONNECTOR AND DIMMER. 2 L 7 3 4F RT A22WE 2001121000059 20011210 00059 NM 2001 12 10 DLM88011660 1 20011012 A 3350 20131ASM1 BATTERY PACK DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 966DL 53115 EMERGENCY TRACK LIGHTING FAILED TEST ROWS 1 THROUGH 12. REPLACED BATTERY PACK, OPS NORMAL. 2 L 7 2 4F RT A6WE 2001121000060 20011210 00060 NM 2001 12 10 DLM88011666 1 20011014 A 3350 8039001 POWER SUPPLY DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 904DE 53409 BOTH FWD OVERWING EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY. 2 L 7 2 4F RT A6WE 2001121000061 20011210 00061 NM 2001 12 10 DLM88011686 1 20011018 A 2170 COALESCER BAG DOUG MD88 MD88 3023688 NM A/C BAY CONTAMINATED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 900DE 53372 FUMES REPORTED BY F/A IN AFT CABIN. PERFORMED DUCT BURNOUT. 2 L 7 2 4F RT A6WE 2001121000062 20011210 00062 NM 2001 12 10 DLM88011706 1 20011022 A 3320 SOCKET DOUG MD88 MD88 3023688 NM CABIN BURNED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 923DL 49705 STRONG ODOR, POSSIBLY ELECTRICAL IN AREA OF CABIN OVERWING. FOUND LOWER SIDEWALL LIGHT SOCKET BURNED AT ROW 25 RIGHT. REPLACE SAME. 2 L 7 2 4F RT A6WE 2001121000063 20011210 00063 NM 2001 12 10 DLM88011724 1 20011026 A 3350 D691454004 BATTERY DOUG MD88 MD88 3023688 NM COCKPIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 906DL 49537 FWD ENTRY DOORS AND COCKPIT EMERGENCY LIGHT INOP. REPLACED BATTERIES. 2 L 7 2 4F RT A6WE 2001121000064 20011210 00064 NM 2001 12 10 DLM88011732 1 20011029 A 2560 P20700030 FLASHLIGHT DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 977DL 53258 FWD ENGINE FLASHLIGHT INOP. REPLACED LIGHT ASSY, OPS NORMAL. 2 L 7 2 4F RT A6WE 2001121000065 20011210 00065 NM 2001 12 10 DLM88011741 1 20011030 A 3397 0201991008 WIRE HARNESS DOUG MD88 MD88 3023688 NM CABIN FAULTY A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 987DL 53338 SEAT 3C EMERGENCY TRACK LIGHT INTERMITTENT. REPLACED SEAT CABLE PER M/M, OPS CHECK OK. 2 L 7 2 4F RT A6WE 2001121000066 20011210 00066 NM 2001 12 10 DLM88011745 1 20011101 A 2913 623337 PUMP DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE FAILED A DALA O OTHER J WARNING INDICATION CR CRUISE 1 SO 27 975DL 53243 718101 LEFT SYS HYD FAILURE AT FLT 290 WITH 19 QT OF FLUID AT ZERO PRESSURE. ATTEMPT TO RESTORE HYD POWER AS PER POM WITH AUX PUMP ON AND TRANSFER PUMP ON IN FLT AND STILL HAD NO PRESSURE IN THE LEFT SIDE. REPLACED LEFT ENGINE HYD PUMP. ALSO, R EPLACED ALL FILTERS. 2 L 7 2 4F 4 F RT A6WE E9NE 2001121000067 20011210 00067 NE 2001 12 10 DLM88011746 2 20011101 A 7250 TURBINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE FAILED A DALA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 27 994DL 30597 53346 725507 IN CRUISE AT 28K FEET HEARD BANG ON RT SIDE. RIGHT ENGINE SHUT DOWN. CREW WENT THROUGH POM PROCEDURE, FUEL LEVER OFF. THEN NOTICED OIL PRESS AND QTY AT ZERO. DID NOT TRY RESTART. WINDMILLED FOR APPROX 20 MINUTES WITH NO OIL PRESSURE. ON INSPECTION MTC FOUND TURBINE FAILED, WAS CONTAINED. ENGINE CHANGE. 2 L 7 2 4F 4 F RT A6WE E9NE 2001121000068 20011210 00068 NM 2001 12 10 DLM88011747 1 20011101 A 2560 61020 BATTERY DOUG MD88 MD88 3023688 NM FLASHLIGHT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 982DL 53273 ON INSPECTION FOUND EMERGENCY FLASHLIGHT ABOVE F/C FLIGHT ATTENDANT SEAT NOT TESTING. REPLACED BATTERY PACK PER MM, OPN OF FLASHER NORMAL. REPLACED STRAP. 2 L 7 2 4F RT A6WE 2001121000069 20011210 00069 NM 2001 12 10 DLM88011752 1 20011102 A 8012 POSITION SWITCH DOUG MD88 MD88 3023688 NM START VALVE FAILED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 925DL 49712 4657C RIGHT ENG START VALVE LIGHT ILLUMINATED AT FL120. POM PROCEDURES FOLLOWED. A/C DIVERTED TO MCO. FOUND VALVE POS SWITC H FAILED IN OPEN POSITION. REPLACED VALVE AND CKD SYS PER M/M. PART BORROWED FROM TWA. 2 L 7 2 4F RT A6WE 2001121000070 20011210 00070 NM 2001 12 10 DLM88011775 1 20011108 A 2560 61020 BATTERY DOUG MD88 MD88 3023688 NM FLASHLIGHT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 996DL 53363 FWD FLASHLIGHT LOW BATTERY AND SEAL BROKEN. REPLACED BATTERY. 2 L 7 2 4F RT A6WE 2001121000071 20011210 00071 NM 2001 12 10 DLM88011776 1 20011108 A 3397 WIRE DOUG MD88 MD88 3023688 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 952DL 49883 ON LAYOVER, FOUND SEAT 19CDE EMERGENCY LIGHT OUT. FOUND HARNESS WIRE BROKEN. RESECURED WIRE, OPS NORMAL. 2 L 7 2 4F RT A6WE 2001121000072 20011210 00072 NM 2001 12 10 DLM88011781 1 20011109 A 2780 SLAT DOUG MD88 MD88 3023688 NM WING MALFUNCTIONED A DALA C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 SO 27 961DL 49980 AUTO SLAT FAIL MESSAGE ON T/O ROLL AT 65 KNOTS. RTO. TESTED SYSTEM PER M/M. 2 L 7 2 4F RT A6WE 2001121000073 20011210 00073 NM 2001 12 10 DLM88011785 1 20011110 A 4920 APU DOUG MD88 MD88 3023688 NM APU BAY LEAKING A DALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 966DL 10744 53115 STRONG BURNT ODOR FROM ROW 18 AFT. REPLACED APU FOR INTERNAL OIL LEAK. 2 L 7 2 4F RT A6WE 2001121000074 20011210 00074 NE 2001 12 10 DLM88011794 2 20011112 A 7261 RELIEF VALVE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE FAULTY A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 984DL 37987 716782 53311 716782 INFLIGHT NR 1 ENG OIL PRESSURE 65 PSI AND FLASHING. REPLACED PRESSURE RELIEF VALVE. RAN ENG, OPN CHECK NORMAL. 2 L 7 2 4F 4 F RT A6WE E9NE 2001121000075 20011210 00075 NM 2001 12 10 DLM88011798 1 20011113 A 2432 D31BAA RELAY DOUG MD88 MD88 3023688 NM E/E BAY FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 906DL 49537 ELECTRICAL ODOR COMING FROM E/E. FOUND VAPOR COMING FROM BATTERIES. REPLACED BATTERIES, CHARGER, TEMP SENSOR AND R2-56 RELAY. 2 L 7 2 4F RT A6WE 2001121000076 20011210 00076 NM 2001 12 10 DLM88011809 1 20011114 A 3222 STRUT DOUG MD88 MD88 3023688 NM NLG LOW A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 950DL 49881 AFTER TAKEOFF NOSE GEAR WOULD NOT SHOW UP AND LOCKED. SERVICED NOSE STRUT TO PROPER LEVEL. 2 L 7 2 4F RT A6WE 2001121000077 20011210 00077 NM 2001 12 10 DLM88011843 1 20011120 A 2120 SMOKE DOUG MD88 MD88 3023688 NM CABIN DETECTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 938DL 49811 AT FL270 F/A NOTIFIED US OF SMOKE /FUMES /STRONG BURNING ODOR. SMOKE PREVALENT AT OVERWING EXITS ROW 24 TO 27. ODOR MO VED FORWARD TO COCKPIT. SMOKE COMING OUT OF ALL AIR VENTS IN MAIN AND FIRST CLASS CABIN. CABIN FULL OF SMOKE FOR 3-5 M INS. C/W STEPS 1-4 OF OPN 5088 BORESCOPED NR 1 AND 2 ENGINES NR 3 CARBON SEAL. NO LEAKS FOUND. COMPLETED OPN 5088, NO EVIDENCE OF SMOKE OR FUMES DURING OPN 5088. PERFORMED VERIFICATION FLT, NO ABNORMALITIES. 2 L 7 2 4F RT A6WE 2001121000078 20011210 00078 NM 2001 12 10 DLM88011850 1 20011124 A 2611 SA308C DETECTOR DOUG MD88 MD88 3023688 NM LAVATORY FAULTY A DALA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 SO 27 901DL 49532 RIGHT AFT LAV SMOKE DETECTOR SOUNDED. DETECTOR APPEARED TO HAVE BEEN TAMPERED WITH. REPLACED SAME. 2 L 7 2 4F RT A6WE 2001121000079 20011210 00079 NM 2001 12 10 DLM88011855 1 20011124 A 2910 31914912 PACKING DOUG MD88 MD88 3023688 NM NR 2 ENGINE LEAKING A DALA H DEACTIVATE SYST/CIRCUITS K FLUID LOSS CL CLIMB 1 SO 27 994DL 53346 RIGHT HYD QTY FELL TO 1 QUART. TURNED OFF RT SYSTEM. FOUND RT FWD OUTBOARD MODULE FITTING LEAKING FROM PACKING. REPLA CED PACKING. 2 L 7 2 4F RT A6WE 2001121000080 20011210 00080 NM 2001 12 10 DLM88011874 1 20011128 A 2910 AS15508K0240 HYDRAULIC LINE DOUG MD88 MD88 3023688 NM HYDRAULIC SYS LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 963DL 49982 DURING CLIMBOUT, L HYD QTY AND PRESS DECREASING. FOLLOWED CHECKLIST, RETURNED TO ATL. REMOVED PRESS LINE FLEX HOSE AT FILTER MODULE. INSTALLED NEW CASE DRAIN FILTER RETURN FLEX LINE REDUCER AND PACKING. NO LEAKS NOTED DURING ENGINE RUN. 2 L 7 2 4F RT A6WE 2001121000081 20011210 00081 2001 12 10 SWAA013244 4 20011203 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 638SW 27711 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001121000082 20011210 00082 NM 2001 12 10 SWAA013245 1 20011204 A 3350 BR2013 LENS BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 EEPLS LENS LOOSE AT ROW 8. REMOVED AND REPLACED EEPLS LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001121000083 20011210 00083 NM 2001 12 10 SWAA013246 1 20011203 A 3350 57771 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 090SW 22905 DURING SCHEDULED C2 CHECK, FOUND EEPLS END CAP MISSING IN AFT CABIN. INSTALLED END CAP PER MM. 2 L 7 2 4F A16WE 2001121000084 20011210 00084 2001 12 10 SWAA013247 4 20011203 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 090SW 22905 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2001121000085 20011210 00085 NM 2001 12 10 0104686623 1 20011116 A 5330 SKIN BOEING 747 747251B 1384892 NM CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 623US 21705 During "L" check found crack in fuselage skin at upper forward corner of aft cargo door cutout. Repaired per EA 66-18612 5. 2 L 7 4 4F A20WE 2001121000086 20011210 00086 NM 2001 12 10 SWAA013252 1 20011204 A 5320 65C27314 TIE CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER TIE CLIPS CRACKED (2 EA) AT BS 616, STRS 5L AND 5R. REMOVED AND REPLACED TI E CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001121000087 20011210 00087 2001 12 10 SWAA013255 4 20011205 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 396SW 27690 FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER INADVERTENTLY. RE INSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001121000088 20011210 00088 SO 2001 12 10 C2XA01CL239 1 20011209 A 5210 AN313A BOLT EMB 145 EMB145LR 3260212 SO CABIN DOOR LOOSE A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 15980 145202 CLE FLIGHT#3242 THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN AND CLOSE.MAINTENANCE INSPECTED AND RESECURED BOL T ON THE INNER HANDLE OF MAIN CABIN DOOR.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001121000089 20011210 00089 EA 2001 12 10 COMA0160947 1 20011206 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 940CA 7048 FLIGHT #5996 FLAPS FAILED AT ZERO WHEN SELECTED DOWN.RESET THE FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2001121000090 20011210 00090 EA 2001 12 10 COMA0160949 1 20011206 A 3230 4622 VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 926CA 18936 7027 FLIGHT 5865 LANDING GEAR DISAGREE WARNING.REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2001123100067 20011231 00067 EU 2001 12 31 MTNA200112 1 20011128 A 3234 AC61078 SELECTOR VALVE FOKKER F27 F27MK500 4990629 EU COCKPIT LEAKING A MTNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 717FE 93 10455 ON TAKEOFF OUT OF MEM, WHEN THE LANDING GEAR WAS SELECTED UP THE MAIN PNEUMATIC SYSTEM WENT TO ZERO. THE LANDING GEAR W OULD NOT RETRACT. THE CREW DECLARED AN EMERGENCY AND RETURNED TO MEM. THE AIRCRAFT LANDED WITHOUT ANY OTHER PROBLEMS. 2 H 7 2 4T A817 2001121000091 20011210 00091 NM 2001 12 10 SWAA013257 1 20011204 A 2560 P2070001 FLASHLIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED C3 CHECK, FOUND AFT UPPER EMERGENCY FLASHLIGHT BLINKING LIGHT INDICATION INOP. REMOVED AND REPLACED FL ASHLIGHT PER MM. 2 L 7 2 4F A16WE 2001121000092 20011210 00092 NM 2001 12 10 SWAA013260 1 20011204 A 5312 6517583 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 363SW 26574 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BLKHD, 2 EA VERTICAL BEAM WEBS CRACKED, LBL 17.1 AND RBL 17.1. REMOVED AND REPLACED BOTH WEBS PER SRM. 2 L 7 2 4F RT A16WE 2001121000093 20011210 00093 2001 12 10 SWAA013265 4 20011205 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT DOORS OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 074SW 22674 DURING SCHEDULED C1 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF VIEW. REPOSITIONED SL IDES PER MM. 2 L 7 2 4F A16WE 2001121000094 20011210 00094 NM 2001 12 10 SWAA013266 1 20011206 A 2560 P2070001 FLASHLIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 527SW 26569 EMERGENCY FLASHLIGHT INOP AT FWD CABIN UPPER POSITION. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2001121000095 20011210 00095 NM 2001 12 10 SWAA013269 1 20011204 A 5320 6551698 SPLICE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2001121000096 20011210 00096 EU 2001 12 10 00048 1 20011128 A 3020 THERMISTER SAAB SF340 SF340A 7850100 EU LT INTAKE MALFUNCTIONED A CHQA D RETURN TO BLOCK J WARNING INDICATION UK UNKNOWN 1 GL 11 CHQA 108 LEFT INTAKE HEAT INOP. SWAPPED THERMISTORS, CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2001121000097 20011210 00097 2001 12 10 DLM90011824 4 20011118 A 3417 4074730901 ADC DOUG MD90 MD9030 3023690 NM E/E BAY FAULTY A DALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 27 901DA 53381 ABORTED TAKEOFF AT 100 KTS. CAPTAINS AIRSPEED FROZE AT 80 KTS, F/O AIRSPEED INDICATED 100 KTS. ALSO HAD WINDSHEER INOP ON OAP. REPLACED CAPTAINS AIR DATA COMPUTER. BITE COMPUTER CHECKS GOOD. PERFORMED PITOT TEST NR 1 AND NR 2, CKS GOOD . 2 L 7 2 4F RT A6WE 2001121000098 20011210 00098 NM 2001 12 10 DLM90011859 1 20011125 A 2497 WIRE DOUG MD90 MD9030 3023690 NM ELECTRICAL SYS BROKEN A DALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 SO 27 916DN 53396 AIR TURNBACK DUE TO LEFT GENERATOR CYCLED RAPIDLY WITH RELAY CLICKING SOUND AFTER TAKEOFF. AFTER TAKING GENERATOR OFF L INE THE CLICKING STOPPED. REPLACED COTA AND REPAIRED BROKEN WIRE. 2 L 7 2 4F RT A6WE 2001121000099 20011210 00099 NM 2001 12 10 SWAA013271 1 20011206 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER SPLICES CRACKED (2 EA) AT STR 4L, BS 360 AND BS 908. REMOVED AND REPLACED S TR SPLICES PER SRM. 2 L 7 2 4F RT A16WE 2001121000100 20011210 00100 NM 2001 12 10 SWAA013275 1 20011203 A 3242 2601042 BRAKE BOEING 737 7373H4 1384600 NM MLG OUT OF ADJ A SWAA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 335SW 23939 BRAKES SPONGY, FOUND THE CLEARANCE BETWEEN THE LEFT NORMAL BRAKE METERING VALVE PLUNGER AND ROLLER OUT OF TOLERANCE. AD JUSTED SAME GAP TO WITHIN TOLERANCE IAW MM. PERFORMED BRAKE SYSTEM TEST AND A/C TAXI CHECK, BRAKES OPERATE NORMAL. 2 L 7 2 4F RT A16WE 2001121000101 20011210 00101 SO 2001 12 10 ASOA01234 1 20011113 A 2120 ODOR EMB 120 EMB120RT 3260202 SO COCKPIT DETECTED A ASOA H DEACTIVATE SYST/CIRCUITS B P SMOKE/FUMES/ODORS/SPARKS NO WARNING INDICATION CL CLIMB 1 SO 11 286AS 120268 UPON DEPARTURE FROM OKC, AT APPROXIMATELY 5000 FEET, CAPTAIN STARTED TO SMELL A HOT BURNING ODOR COMING FROM THE AIR VEN TS. HE TURNED THE PACKS OFF, AND THE SMELL WENT AWAY. NO WARNING INDICATIONS WERE RECEIVED FROM THE AIR CONDITIONING S YSTEM. AIRCRAFT LANDED IN DFW WITHOUT INCIDENT. MAINTENANCE RAN ENGINES AND OPERATED PACKS BUT COULD NOT DUPLICATE THE SMELL. ENGINE AND PACKS BOTH OPERATED NORMALLY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001121000102 20011210 00102 SO 2001 12 10 ASOA01235 1 20011113 A 3350 12043411501 CONTROL PANEL EMB 120 EMB120ER 3260203 SO CABIN DEFECTIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 267AS 120198 FLT 4315 - ON PUSHBACK OUT OF ATL, THE EMERGENCY LIGHT CIRCUIT BREAKER POPPED WHEN THE FLIGHT ATTENDANT MOVED THE SWITCH TO TEST. THE CIRCUIT BREAKER WAS RESET AND THE FLIGHT ATTENDANT AGAIN MOVED THE SWITCH TO TEST AND THEN TO THE ON POSI TION. AT THIS TIME ONLY THE LIGHTS FROM ROW 5 AFT CAME ON. MAINTENANCE REMOVED AND REPLACED THE FLIGHT ATTENDANT EMERG ENCY LIGHT SWITCH PANEL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001121000103 20011210 00103 SO 2001 12 10 ASOA01238 1 20011115 A 3350 3071BPE LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 267AS 120198 DURING GROUND INSPECTION IN ATL, THE CREW REPORTED THE FORWARD EXIT LIGHT ON THE FORWARD CLOSET DOESN'T ALWAYS TEST. MA INTENANCE REMOVED AND REPLACED 4 BULBS IN THE FORWARD EMERGENCY EXIT SIGN ON THE FORWARD CLOSET. MAINTENANCE ALSO CHARG ED THE EMERGENCY LIGHT BATTERY. OPERATIONAL CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2001121000104 20011210 00104 SO 2001 12 10 ASOA01239 1 20011111 A 5313 12005744017 STRINGER EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 280AS 120231 DURING C-CHECK INSPECTION IN BNA, CORROSION WAS DISCOVERED ON STRINGER 20 RIGHT BETWEEN FRAMES 14 AND 15. MAINTENANCE R EMOVED CORROSION IAW CPM 51-14-00. THE DAMAGED SECTION OF THE STRINGER WAS REMOVED. A NEW SECTION OF STRINGER WAS CUT AND DRILLED IAW SRM 51-40-00. (M) 2 L 7 2 4T RT A31SO 2001121000105 20011210 00105 SO 2001 12 10 ASOA01240 1 20011110 A 5313 12005744002 STRINGER EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 280AS 120231 DURING C-CHECK INSPECTION IN BNA, STRINGER 18 RIGHT WAS FOUND TO BE CORRODED BETWEEN FRAMES 14 AND 16. MAINTENANCE REMO VED CORROSION IAW CPM 51-14-00. THE DAMAGED SECTION OF THE STRINGER WAS REMOVED. A NEW SECTION OF STRINGER WAS CUT AND DRILLED IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2001121000106 20011210 00106 EA 2001 12 10 ASOA01241 1 20011117 A 3350 CONTACTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN DIRTY A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 856AS 7404 DURING GROUND INSPECTION IN ATL, THE FORWARD SECTION OF THE EMERGENCY TRACK LIGHTING WAS INOPERATIVE. MAINTENANCE CLEAN ED CONTACTORS ON BOTH LIGHT ASSEMBLIES. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2001121000107 20011210 00107 NM 2001 12 10 EIA2001247 1 20011006 A 5743 FITTING BOEING 747 747273C 1384896 NM LT WING CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 PAE - LEFT WING LANDING GEAR SUPPORT BEAM END FITTING HAD A CRACK INDICATION ADJACENT TO LUG BUSHING. CORROSION NOTED U PON REMOVAL. REMOVED AND REPLACED FITTING. (M) 2 L 7 4 4F A20WE 2001121000108 20011210 00108 NM 2001 12 10 EIA2001250 1 20011001 A 5330 65B043132 SKIN BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 PAE - FOUND INSPECTION OF FUSELAGE SKIN EXTERNAL, DETECTED A CRACK IN THE SKIN. SKIN WAS ALSO PILLOWED. INTERNAL INSPE CTION REVEALED INNER SKIN EXFOLIATION. PERFORMED MAJOR REPAIR ON EXTERNAL FUSELAGE SKIN AT BS 800 STRINGER 46R. (M) 2 L 7 4 4F A20WE 2001121000127 20011210 00127 SO 2001 12 10 LR7A01118 1 20011203 A 5311 FRAME LKHEED 382 382G 526414U SO FS 847 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2332 5025 DURING SCHEDULED C2 INSPECTION PER JOB CARD HSP5330 FOUND FS 847 LH FRAME CRACKED AT LBL 61, WL 189.REPAIRED IAW SRM SMP 583-51-140-21. NR 2010. 2 H 7 4 4T A1SO 2001121000128 20011210 00128 SO 2001 12 10 LR7A01119 1 20011203 A 5311 FRAME LKHEED 382 382G 526414U SO FS 847 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2332 5025 DURING SCHEDULED C2 INSPECTION PER JOB CARD HSP5330 FOUND FS 847 LH FRAME CRACKED AT LBL 61, WL 187.REPAIRED IAW LAC MEA 382-53-01-080. NR 2011. 2 H 7 4 4T A1SO 2001121000129 20011210 00129 SO 2001 12 10 LR7A01120 1 20011203 A 5312 341973L FITTING LKHEED 382 382G 526414U SO FS 477 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2332 5025 DURING SCHEDULED C2 INSPECTION PER JOB CARD HSP5369 FOUND LH FS 477 BEAM END FITTING CRACKED AT LBL 62, WL 250.REPLACED FITTING IAW SRM SMP 583-51-10, PG 6. NR 2023. 2 H 7 4 4T A1SO 2001121000130 20011210 00130 SO 2001 12 10 LR7A01121 1 20011203 A 5312 BEAM LKHEED 382 382G 526414U SO FS 557 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2332 5025 DURING SCHEDULED C2 INSPECTION PER JOB CARD HSP5369 FOUND LH FS 557 BOW BEAM CRACKED AT LBL 62, WL 200.REPAIRED IAW SRM SMP 583-53-40-14. NR 2024. 2 H 7 4 4T A1SO 2001121000131 20011210 00131 SO 2001 12 10 LR7A01122 1 20011203 A 5220 SKIN LKHEED 382 382G 526414U SO FS 427 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2332 5025 DURING SCHEDULED C2 INSPECTION PER JOB CARD HC05297 FOUND RH SIDE EXIT DOOR SKIN LOWER AFT CORNER CRACKED AT FS 427, WL 200.REPAIRED IAW SRM SMP 583-51-140-12. NR 2026. 2 H 7 4 4T A1SO 2001121000132 20011210 00132 SO 2001 12 10 LR7A01123 1 20011203 A 5311 3884952 FRAME LKHEED 382 382G 526414U SO FS 597 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2332 5025 DURING SCHEDULED C2 INSPECTION PER JOB CARD HC53115 FOUND RH FS 597 FRAME CRACKED AT RBL 66, WL 148.REPAIRED IAW SMP 583 -53-40-31. NR 2039. 2 H 7 4 4T A1SO 2001121000133 20011210 00133 SO 2001 12 10 LR7A01124 1 20011203 A 5531 WEB LKHEED 382 382G 526414U SO FS 1095 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2332 5025 DURING SCHEDULED C2 INSPECTION PER JOB CARD HSP5539 FOUND VERTICAL STAB REAR BEAM WEB CRACKED AT FS 1095, LBL 6, VSS 20. REPAIRED IAW SRM SMP 583-51-140-17. NR 2040. 2 H 7 4 4T A1SO 2001121000147 20011210 00147 SW 2001 12 10 ALG2001F00043 1 20011009 A 6710 406010426101 LINK BELL 407 407 1182206 SW ALLSN 250C 250C47B GL MAIN ROTOR CORRODED E ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 427AL 1494 53107 CAE847416 DURING PHASE INSPECTION. CORROSION BEYOND MAXIMUM LIMITS. RETURN TO 206 SERIES ALLOY USED ON LINKS AND LEVERS. BETTER ALLOY AND/OR SURFACE PROTECTION. 1 G 7 1 3U 3 U O H2SW E1GL 2001121100001 20011211 00001 2001 12 11 SWAA013278 4 20011208 A 2565 61620 SLIDE BOEING 737 7375H4 138449D NM FWD ENTRY DOOR DEPLOYED A SWAA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 515SW 25154 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED UPON ARRIVAL. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001121100002 20011211 00002 NM 2001 12 11 SWAA013280 1 20011207 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 793SA 27888 DURING SCHEDULED C3 CHECK, FOUND EEPLS COVERS MISSING AT ROWS 1 AND 17. INSTALLED COVERS PER MM. 2 L 7 2 4F RT A16WE 2001121100003 20011211 00003 NM 2001 12 11 SWAA013281 1 20011207 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 379SW 26586 EMERGENCY EXIT LIGHT BROKEN AT FWD F/A'S SEAT STATION. REMOVED AND REPLACED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2001121100004 20011211 00004 NM 2001 12 11 SWAA013283 1 20011208 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 067SW 22356 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 777, STR 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2001121100005 20011211 00005 NM 2001 12 11 SWAA013289 1 20011208 A 5311 6546546 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 525SW 26567 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (3 EA) BETWEEN STRS 8R AND 9R, BS 380, 747 AND 787. REPAIRED FR AMES PER BFG ER. 2 L 7 2 4F RT A16WE 2001121100006 20011211 00006 NM 2001 12 11 SWAA013290 1 20011208 A 5311 6546546 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 525SW 26567 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (4 EA) BETWEEN STRS 8L AND 9L, BS 520, 747, 787 AND 827. REPAIR ED FRAMESPER BFG ER. 2 L 7 2 4F RT A16WE 2001121100007 20011211 00007 NM 2001 12 11 SWAA013291 1 20011209 A 5320 6517583 WEB BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 340LV 23738 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED AT BS 180, WL 177 AND LBL 5.7. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001121100008 20011211 00008 NM 2001 12 11 SWAA013292 1 20011208 A 5312 6516300 WEB BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 340LV 23738 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND BULKHEAD WEB CRACKED (4 EA) AT BS 178, WL 234 AND LBL 12.0, WL 199 AND LBL 5 .0, WL 201 AND RBL 5.0, WL 199 AND RBL 5.0. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001121100009 20011211 00009 NM 2001 12 11 SWAA013293 1 20011208 A 5312 6517582 WEB BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 340LV 23738 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED AT BS 183, WL 223 AND RBL 17.1. REPAIRED WEB PER SRM.. 2 L 7 2 4F RT A16WE 2001123100049 20011231 00049 CE 2001 12 31 GLBA2001238 1 20011207 A 7331 1303800101 INDICATOR BEECH 1900 1900D 1154162 CE COCKPIT FAILED A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 245GL 184 UE245 LEFT FUEL FLOW GAUGE FAILED, REPLACED INDICATOR OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001121100018 20011211 00018 SO 2001 12 11 BH22001F00000 1 20011031 A 3244 606C662 TIRE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA LANDING GEAR DEFECTIVE E BH2R K NONE O OTHER IN INSP/MAINT 1 WP 07 20LX 285 317552121 GOODYEAR FLIGHT CUSTOM II 6PLY. THIS IS THE SECOND TIRE. I HAVE CHANGED DUE TO THIS CONDITION I DID NOT SAVE THE FIRST TIRE. WHEN I CHANGED IT LAST AND THOUGHT THE BLISTER WAS FROM AGE. THIS IS THE SECOND TIRE, LOOKS LIKE MAYBE THERE IS A WEAK SPOT OR DEFECT. 1 L 7 2 3O 3 O A20SO E14EA 2001121100019 20011211 00019 NE 2001 12 11 BLI2001F00005 2 20011031 A 7412 IO3815502 EXCITER CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE ENGINE FAILED E BLIA K NONE O OTHER TX TAXI/GRND HDL 1 GL 17 505RP 3588 5500450 71287 LEFT ENGINE FAILED TO START. CALLED DIRECTOR OF MAINTENANCE, ARRIVED TO REPAIR AIRCRAFT. REPLACED BOTH IGNITERS BUT FA ILED TO START. REPLACED IGNITER EXCITER. STARTS NORMAL. AIRCRAFT RETURNED TO NORMAL. 1 L 7 2 4F 4 F A22CE E1NE 2001121100020 20011211 00020 CE 2001 12 11 BSY2001F00015 1 20011005 A 7931 ST4H TRANSMITTER LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP ENGINE FAULTY E BSYA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 55F 147 P74871 RIGHT ENGINE OIL PRESSURE RUNNING HIGH, OIL TEMPERATURE, RED LINE AT FLIGHT LEVEL 37,000. FOUND OIL PRESSURE TRANSMITTE R 12 PSI HIGH, REMOVED AND REPLACED OIL PRESSURE TRANSMITTER OIL PRESSURE, CHECKS GOOD. COULD NOT DUPLICATE OIL TEMPERA TURE PROBLEM. 2 L 7 2 4F 4 F A10CE E6WE 2001121100021 20011211 00021 SO 2001 12 11 BTVR216048 1 20011018 A 5610 1159SCB31029 WINDSHIELD GULSTM G1159 GIV 3980115 SO COCKPIT CRACKED B BTVR O OTHER O OTHER CR CRUISE 1 GL 23 1SL 3552 1167 DURING A ROUTINE RETURN TRIP ACROSS THE ATLANTIC DURING CRUISE, THE OUTER GLASS PLY OF THE PILOTS WINDSHIELD SHATTERED. UPON INSPECTION, IT APPEARS THE HEATING ELEMENTS FAILED, ARCED AND CAUSED THE GLASS TO SHATTER. THIS IS NOT AN UNCOMMO N OCCURRENCE WITH THESE WINDSHIELDS. A NEW PART WAS INSTALLED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A12EA 2001121100022 20011211 00022 CE 2001 12 11 BUE2001F00000 1 20011112 A 7810 10995000061 EXHAUST STACK BEECH 90 C90A 1152911 CE PWA PT6 PT6* 52043 EA ENGINE BROKEN B BUER K NONE O OTHER IN INSP/MAINT 1 GL 23 1031Y LJ1431 DURING SCHEDULED INSPECTION FOUND LEFT ENGINE EXHAUST STACK INLET HEAT AIR TUBE BROKEN AWAY FROM EXHAUST STACK.(K) 1 L 7 2 3T 3 T RT 3A20 E2NE 2001121100023 20011211 00023 CE 2001 12 11 BV92001F00000 1 20011127 A 3230 WIRE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LANDING GEAR CHAFED B BV9T O OTHER J WARNING INDICATION CL CLIMB 1 EA 25 15SK 3037 5600395 AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. FOUND WIRE BUNDLE IN LEFT WHEEL WELL CHAFED ON HYDRAULIC LINE. 2 L 7 2 4F 4 F RT A22CE E25EA 2001121100024 20011211 00024 CE 2001 12 11 CNQ2001F00000 1 20011106 A 7931 23062618 SENSOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL LT ENGINE INTERMITTENT E CNQR O OTHER N FALSE WARNING CR CRUISE 1 CE 07 505MA 1123 7500057 330133 THE LEFT ENGINE OIL PRESSURE DROPPED IN FLIGHT. TROUBLESHOT TO AN INTERMITTENT OIL PRESSURE SENSOR. REMOVED AND REPLAC ED THE SENSOR. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2001121100025 20011211 00025 CE 2001 12 11 DXT2001F00002 1 20010924 A 3244 237K232 TIRE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP RT MLG SEPARATED E DXTR O OTHER O OTHER TO TAKEOFF 1 NM 07 817QS 304 258517 GOODYEAR FLIGHT EAGLE PN 237K23-2, SN 10961491 FAILED ON TAKE-OFF. SEPARATED TREAD PENETRATED WING UPPER SURFACE, ALSO DAMAGED FUSELAGE SIDE FAIRING AND RIGHT ENGINE NACELLE. A BRAKE HYDRAULIC LINE WAS ALSO RUPTURED. CAUSE OF FAILURE UN KNOWN AT THIS TIME. AIRCRAFT TT 304 HOURS. 2 L 7 2 4F 4 F RT A3EU E6WE 2001121100026 20011211 00026 CE 2001 12 11 DXT2001F00003 1 20011026 A 3230 664062217 CABLE CESSNA 560 560XL 2076702 CE EMR GEAR RELEASE CHAFED E DXTA K NONE O OTHER IN INSP/MAINT 1 GL 07 603QS 17 5605203 CABLE RUN JUST FORWARD OF BATTERY COMPARTMENT, INBOARD SIDE OF HYDRAULIC PRESSURE LINE, RUBBING ON BULKHEAD.STATION FS39 0.(K) 2 L 7 2 4F RT A22CE 2001121100027 20011211 00027 CE 2001 12 11 EAS2001F00000 1 20011025 A 3260 232710018 SEAT LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE731* 01518 WP LT MLG SCORED E EASA O OTHER O OTHER AP APPROACH 1 EA 23 646G 7899 016 LEFT LANDING GEAR DOWN INDICATION SLOW TO ILLUMINATE. FOUND DOWN LOCK SWITCH ACTUATING BALL SEAT SCORED. POSSIBLY CAUS ING SWITCH TO ACTUATE SLOWLY. 2 L 7 2 4F 4 F A10CE E6WE 2001121100028 20011211 00028 EU 2001 12 11 EHA2001F00005 1 20010628 A 2435 31038281 SPLINE ADAPTER LUCAS CASA C212 C212CC 2410204 EU GARRTT TPE331 TPE331* 01514 WP STARTER GEN STRIPPED E EHAA O OTHER O OTHER TX TAXI/GRND HDL 1 AL 03 352CA 806 5169 190 37246 STARTER GENERATOR FAILED TO TURN OVER THE ENGINE ON COMMAND. INVESTIGATION REVEALED THE PLASTIC SPLINE HAD STRIPPED OUT ON THE INTERNAL THREADS. 2 H 7 2 4T 3 T A43EU E2WE 2001121100029 20011211 00029 EU 2001 12 11 EHA2001F00006 1 20010628 A 2435 31038281 SPLINE ADAPTER LUCAS CASA C212 C212CC 2410204 EU GARRTT TPE331 TPE331* 01514 WP STARTER GEN STRIPPED E EHAA O OTHER O OTHER TX TAXI/GRND HDL 1 AL 03 352CA 806 190 37246 STARTER GENERATOR FAILED TO OVER THE ENGINE ON COMMAND. INVESTIGATION REVEALED THE PLASTIC SPLINE ADAPTER HAD STRIPPED OUT ON THE INTERNAL THREADS. 2 H 7 2 4T 3 T A43EU E2WE 2001121100031 20011211 00031 EU 2001 12 11 EZ22001F00000 1 20010810 A 5330 74005151431 PANEL AIRBUS 320 A320* EU FUSELAGE DEBONDED A EZ2R K NONE O OTHER IN INSP/MAINT 1 SW 15 WHILE ATTEMPTING TO REPAIR A DEBOND ON THE PERFORATE SKIN (LOWER FORWARD) OF THE C-DUCT BOND PANEL, IT WAS DISCOVERED TH AT THERE WAS ADHESIVE BACKING LEFT UNDER THE PERFORATE SKIN IN THE NON-ACOUSTIC AREA DURING THE PREVIOUS BONDING PROCESS . 2 L 7 2 4F RT A46NM 2001121100033 20011211 00033 NE 2001 12 11 FE62001F00001 2 20010921 A 7310 5282009109 ADAPTER PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE ENGINE LEAKING B FE6R O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 11 277PC 37 277 PCEPR0135 FLIGHT CREW REPORTS FUEL SMELL IN COCKPIT ON THIS LOW TIME AC. MAINTENANCE FOUND RAW FUEL IN THE ENGINE COWLING. FUEL IS NOTED TO BE SEEPING FROM THE INLET FITTING (ADAPTER) ON THE LOW PRESSURE ENGINE DRIVEN FUEL PUMP. REPLACING THE ADAP TER RESOLVED THE DISCREPANCY.(K) 1 L 7 1 3T 4 T RT A78EU E26NE 2001121100034 20011211 00034 CE 2001 12 11 FFSA90153 1 20011024 A 5610 10138402521 WINDSHIELD BEECH 1900 1900C 1154161 CE PWA PT6 PT6* 52043 EA COCKPIT CRACKED A FFSA A UNSCHED LANDING O OTHER CL CLIMB 1 AL 01 575Z UC136 ON CLIMBOUT AT ABOUT 15,000 FEET ALTITUDE THE PILOTS HEATED WINDSHIELD SUDDENLY DEVELOPED CRACKS RUNNING THROUGHOUT THE WINDOW. THE AIRCRAFT DESCENDED AND RETURNED TO AIRPORT. 2 L 7 2 4T 3 T RT A24CE E2NE 2001121100035 20011211 00035 CE 2001 12 11 FGQ2001F00000 1 20011201 A 5740 FITTING CESSNA 182 182F 2072714 CE CONT O470 O470* 17026 SO LT WING CORRODED E FGQR K NONE O OTHER IN INSP/MAINT 1 SO 01 3562Y 18254462 INSPECTION OF LEFT WING ASSEMBLY REVEALED SEVERE EXFOLIATION CORROSION OF WING ATTACH FITTING (FWD) EXTENDING, APPROXIMA TELY 18 INCHES OUTBOARD WING SKIN WAS LIFTED UP FROM SPAR. 1 H 7 1 3O 3 O NT 3A13 E273 2001121100036 20011211 00036 CE 2001 12 11 FPI2001F00000 1 20010917 A 3221 12430097 TRUNNION CESSNA 210 T210N 2073456 CE CONT O520 TSIO520* 17040 SO NLG CRACKED E FPIA K NONE O OTHER IN INSP/MAINT 1 SO 15 4702C 7008 21063591 THE PN 1243009-7 TRUNNION ASSEMBLY CRACKED AT THE TRUNNION ASSEMBLY-LOWER (ITEM 14), WHERE THE TWO LEGS MEET THE CIRCULA R PORTION THAT ATTACHES TO THE BARREL ASSEMBLY. THIS PART SHOWED SIGNS OF A PRE-EXISTING CRACK AT BOTH LEGS. THIS AREA IS DIFFICULT TO INSPECT BECAUSE OF ITS LOCATION. THE AREA IS PRONE TO DIRT AND GREASE ACCUMULATION WHICH ALSO HINDER I NSPECTION. 1 H 7 1 3O 3 O 3A21 E8CE 2001121100037 20011211 00037 SO 2001 12 11 FPI2001F00001 2 20010904 A 7314 6462121 PUMP CESSNA 210 210N 2073453 CE CONT O520 IO520* 17032 SO ENGINE FAULTY E FPIA O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 SO 15 5229A 1025 1025 21063320 ENGINE HAD LOW POWER PROBLEM. ENGINE MAX FUEL PRESSURE WAS 26 PSI AT 2700 RPM. SPECS 28 TO 31 PSI. THE HIGH PRESSURE ADJUSTMENT WAS BOTTOMED OUT. THE FUEL PUMP WAS REMOVED AND REPLACED. 1 H 7 1 3O 3 O 3A21 E5CE 2001121100038 20011211 00038 SO 2001 12 11 FPI2001F00002 2 20011023 A 7414 M3081 CAM SLICK CESSNA 210 210N 2073453 CE CONT O520 IO520L 17032 SO MAGNETO WORN A FPIA K NONE O OTHER IN INSP/MAINT 1 SO 15 4637Y 1081 0050437 21063965 295081R ON 500 HOUR INSPECTION, FOUND POINTS AND CAM ASSEMBLY WORN OUT. 1 H 7 1 3O 3 O 3A21 E5CE 2001121100039 20011211 00039 SO 2001 12 11 FPI2001F00003 2 20011012 A 7414 K3823 BEARING SLICK CESSNA 210 210N 2073453 CE CONT O520 IO520* 17032 SO DISTRIBUTOR BLK WORN E FPIA K NONE O OTHER IN INSP/MAINT 1 SO 15 4637Y 1081 00050443 21063965 295081R UPON 500 HOUR INSPECTION FOUND DISTRIBUTOR BLOCK BEARINGS WORN. FOUND BRUSH WORN THROUGH COIL FINGER AND BRUSH WORN OUT . ALSO, FOUND POINTS AND CAM ASSEMBLY PN M3081, WORN OUT. 1 H 7 1 3O 3 O 3A21 E5CE 2001121100040 20011211 00040 SO 2001 12 11 FWRA2001005 1 20011031 A 2140 B4500 TUBE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA HEATER FAILED A FWRA K NONE O OTHER IN INSP/MAINT 1 AL 01 222CC 781 318052095 HEATER SENT TO REPAIR STATION, FAILED HEATER DECAY TEST. THE COMBUSTION TUBE WAS REPLACED BUT NO INFORMATION ON WHY. WOULD ASSUME IT HAD CRACK OR HOLE TO CAUSE THE FAILED TEST. THIS FAILURE IS A CONCERN BECAUSE THIS IS A CERAMIC COATED TUBE WITH NO APPLICABLE AD AGAINST IT. 1 L 7 2 3O 3 O A20SO E14EA 2001121100041 20011211 00041 WP 2001 12 11 FXG2001F00000 1 20010705 A 7810 ADAPTER DOUG DC6 C118A 3021710 WP PWA R2800 R2800* 52026 NE EXHAUST PIPE WORN A FXGA O OTHER J WARNING INDICATION NR NOT REPORTED 1 AL 01 888DG 244 44675 P33776 FLIGHT CREW HAD A ZONE 1 FIRE WARNING WITH NO OTHER INDICATIONS. ON INSPECTION ON THE ENGINE, NR 14 CYLINDER WAS FOUND TO HAVE A LOOSE EXHAUST VALVE GUIDE CAUSING THE COMBUSTION CHARGE ACCESS TO THE EXHAUST SYSTEM. THE EXHAUST PIPE ADAPTE R FOR THIS CYLINDER WAS WORN AND IT IS SUSPECTED THAT FLAMES FROM THIS CYLINDER LEAKED ONTO THE FIRE WARNING SYSTEM. T HE FIRE WARNING SYSTEM ALSO HAD A 3 OHMS RESISTANCE VS. 2 OHMS WHICH WOULD HAVE MADE THE SYSTEM MORE SENSITIVE. NO OTHE R FAULTS FOUND. 2 L 7 4 4R 4 R 6A3 5E8 2001121100042 20011211 00042 NE 2001 12 11 FXG2001F00001 2 20010705 A 8530 327626 VALVE GUIDE DOUG DC6 C118A 3021710 WP PWA R2800 R2800* 52026 NE CYLINDER LOOSE A FXGA O OTHER J WARNING INDICATION NR NOT REPORTED 1 AL 01 888DG 44675 P33776 FLIGHT CREW HAD A ZONE 1 FIRE WARNING WITH NO OTHER INDICATIONS. ON INSPECTION ON THE ENGINE, NR 14 CYLINDER WAS FOUND TO HAVE A LOOSE EXHAUST VALVE GUIDE CAUSING THE COMBUSTION CHARGE ACCESS TO THE EXHAUST SYSTEM. THE EXHAUST PIPE ADAPTE R FOR THIS CYLINDER WAS WORN AND IT IS SUSPECTED THAT FLAMES FROM THIS CYLINDER LEAKED ONTO THE FIRE WARNING SYSTEM. TH E FIRE WARNING SYSTEM ALSO HAD A 3 OHMS RESISTANCE VS. 2 OHMS WHICH WOULD HAVE MADE THE SYSTEM MORE SENSITIVE. NO OTHER FAULTS FOUND. 2 L 7 4 4R 4 R 6A3 5E8 2001121100043 20011211 00043 WP 2001 12 11 FXG2001F00002 1 20011102 A 2612 339583 CONTROL PANEL DOUG DC6 DC6B 3021712 WP PWA R2800 R2800* 52026 NE COCKPIT FAULTY A FXGA F E A ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 AL 01 6586C 45222 P28812 AIRCRAFT DEPARTED AND 10 MINUTES INTO FLIGHT HAD A ZONE 1 FIRE WARNING ON NR 2 ENGINE. FIRE BOTTLES DISCHARGED, ENGINE FEATHERED AND AIRCRAFT RETURNED TO AIRPORT. SUSPECTED FAULTY FIRE WARNING PANEL AND 3 DETECTORS REPLACED AFTER THROUGH INSPECTION OF ENGINE AND QEC WHICH SHOWS NO EVIDENCE OF ACTUAL FIRE. 2 L 7 4 4R 4 R 6A4 5E8 2001121100044 20011211 00044 NM 2001 12 11 ASAA01400109 1 20011004 A 3397 8100022607 WIRE BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 774AS 25107 SEA - BEFORE FLIGHT, FOUND LAST TWO EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE (RED) IN AFT CABIN. RECONNECTED WIRES, OPE RATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001121100045 20011211 00045 NM 2001 12 11 ASAA0140127 1 20011028 A 3350 8100022607 LIGHT BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 762AS 25099 SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 9-10. RECONNECTED FLOOR TRACK LIGHTS, OP S NORMAL. (M) 2 L 7 2 4F RT A16WE 2001121100046 20011211 00046 NM 2001 12 11 ASAA0140128 1 20011030 A 3350 7024091007 LIGHT BOEING 737 7374Q8 NM L2 DOOR INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 754AS 25095 SEA - DURING LIGHT CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT, OPS NORMAL. (M) 2 L 7 2 4F RT A16WE 2001121100047 20011211 00047 NM 2001 12 11 ASAA0140136 1 20011104 A 2720 654486112 PCU BOEING 737 737490 1384715 NM RUDDER FAULTY A ASAA K NONE F FLT CONT AFFECTED CR CRUISE 1 NM 01 793AS 28888 SEA - DURING TEST FLIGHT, LEFT RUDDER RESTRICTION IN FLIGHT. LEFT RUDDER COULD BE MOVED APPROX 2 INCH AND STOPPED, STAN DBY HAD MORE AUTHORITY BUT HAS RESTRICTIONS. REMOVED AND REPLACED PCU, OPS NORMAL. (M) 2 L 7 2 4F RT A16WE 2001121100048 20011211 00048 WP 2001 12 11 GTIA011138 1 20011121 A 5753 DOUBLER DOUG DC9 DC981 3022081 WP T/E FLAP CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 ACY - FOUND SCAB PATCH ON SECONDARY FLAP CRACKED, LEFT WING. REPAIRED LEFT WING SECONDARY FLAP IAW SRM 57-50-09 AND CH 57-0105 SRM. (M) 2 L 7 2 4F A6WE 2001121100049 20011211 00049 WP 2001 12 11 GTIA011139 1 20011121 A 5753 FLAP DOUG DC9 DC981 3022081 WP LT WING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 ACY - LEFT TRAILING EDGE FLAP HAS CRACK AT APPROX STATION XW154. REPAIRED FLAP TRAILING EDGE FLAP IAW SRM 57-03 AS REQU IRED. (M) 2 L 7 2 4F A6WE 2001121100050 20011211 00050 WP 2001 12 11 GTIA011140 1 20011120 A 3350 60030431 BATTERY PACK DOUG DC9 DC981 3022081 WP A/C BAY DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 819NK 48016 FLL - EMERGENCY LIGHTS INOPERATIVE IN TAILCONE AREA REF STATION 1152 TO 1237. REMOVED AND REPLACED AFT BATTERY PACKS AS SEMBLIES (85-27 AND B5-28). RELAMPED SEVERAL LIGHTS. FOUND WIRE L794E10 GROUNDED TO FRAME AT TERMINAL STRIP 53-179. R EPOSITIONED WIRE AS PER MM 33-51-01. EMERGENCY LIGHTS, OPS NORMAL AS PER MM 33-51-01. (M) 2 L 7 2 4F A6WE 2001121100051 20011211 00051 WP 2001 12 11 GTIA011141 1 20011124 A 3350 LIGHT DOUG DC9 DC981 3022081 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 819NK 48016 DTW - EMERGENCY FLOOR PATH LIGHTING NOT ILLUMINATING ROWS 23-29. REPAIRED EMERGENCY FLOOR PATH LIGHT AT ROW 23. SYSTEM OPS CHECK GOOD MD80 M/M 33-53-01. (M) 2 L 7 2 4F A6WE 2001121100052 20011211 00052 WP 2001 12 11 GTIA011142 1 20011119 A 7110 WEB DOUG DC9 DC981 3022081 WP NR 2 COWL CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FOUND NR 1 ENGINE COWLING WEB CRACKED AT 3 O'CLOCK POSITION. REPAIRED DAMAGED WEB IAW DC9/MD80 SRM 54-01. (M) 2 L 7 2 4F A6WE 2001121100053 20011211 00053 WP 2001 12 11 GTIA011143 1 20011126 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 801NK 48048 DTW - FOUND 2ND TO LAST RED FLOOR TRACK LIGHT OUT. FOUND BROKEN WIRE ON FLOOR TRACK LIGHTING. REPAIRED BROKEN WIRE IAW MD-80 M/M CH 20-50-01. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2001121100054 20011211 00054 EU 2001 12 11 SIMA200112001 1 20010430 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 332AE 340B332 MRY - FLT 3034 - FORWARD EMERGENCY LIGHTS ONLY STAY ON FOR 40 SECONDS. AIRCRAFT WAS FERRIED TO LAX WHERE MAINTENANCE RE MOVED AND REPLACED TWO BATTERY PACKS (S/N'S 8086, 17693) IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETUR NED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001121100055 20011211 00055 EU 2001 12 11 SIMA200130802 1 20011104 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 548AT 548 DFW - DURING SCHEDULED PS-2 CHECK, MAINTENANCE REPORTED THE EMERGENCY LIGHT FAILED THE OPERATIONAL CHECK. MAINTENANCE R EMOVED AND REPLACED THE POWER SUPPLY UNIT BATTERY PACKS (S/N'S 1366, 1604) AT POSITIONS 62WL AND 73WL IAW ATR MM 33-51-2 1. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001121100056 20011211 00056 EU 2001 12 11 SIMA200130901 1 20011105 A 3320 BALLAST AEROSP ATR72 ATR72212 8680945 EU CABIN SHORTED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 270AT 270 SDQ - FLT 3979 - CREW REPORTED THE OVERHEAD COMPARTMENT BALLAST LIGHT SHORTING AT THE TERMINAL END AT SEAT POSITIONS 13/ 14 A/B WITH VISIBLE SMOKE. LIGHT WAS PUT ON MEL. (M) 2 H 7 2 4T RT A53EU 2001121100057 20011211 00057 EU 2001 12 11 SIMA200130902 1 20011105 A 3350 3012000 BATTERY PACK AEROSP ATR72 ATR72212 8680945 EU CABIN DISCHARGED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 440AM 440 CRP - DURING PREFLIGHT, AFTER TESTING EMERGENCY LIGHTS, THE FORWARD HALF WOULD NOT TURN OFF. MAINTENANCE REMOVED AND RE PLACED THE POWER SUPPLY UNIT BATTERY PACK AT 43WL. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M ) 2 H 7 2 4T RT A53EU 2001121100058 20011211 00058 EU 2001 12 11 SIMA200131502 1 20011111 A 3350 3011210 LIGHT AEROSP ATR42 ATR42300 8680920 EU PAX DOOR INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 277AT 277 MIA - FLT 5088 - DURING POST FLIGHT, CREW REPORTED THE EMERGENCY LIGHT IN THE PASSENGER DOOR TO BE INOPERATIVE. MAINTEN ANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVIC E. (M) 2 H 7 2 4T RT A53EU 2001121100059 20011211 00059 EU 2001 12 11 SIMA200131701 1 20011113 A 3350 3013000 POWER SUPPLY AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 494AE 494 MIA - MAINTENANCE REPORTED SOME EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED ONE OF THE EMER GENCY LIGHT POWER SUPPLY UNITS. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001121100060 20011211 00060 EU 2001 12 11 SIMA200131801 1 20011114 A 3350 192411A FUSE SAAB SF340 340B 7860101 EU CABIN BLOWN A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 905AE 340B319 LAW - FLT 3635 - DURING A PHASE THREE INSPECTION, MAINTENANCE FOUND THE EMERGENCY LIGHT AT SEAT 11A TO BE INOPERATIVE. MAINTENANCE REPLACED THE FUSE 26LN IAW SAAB WM 33-50-00. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVIC E. (M) 2 L 7 2 4T RT A52EU 2001121100061 20011211 00061 EU 2001 12 11 SIMA200131802 1 20011114 A 3320 6510732 BALLAST SAAB SF340 340B 7860101 EU CABIN DEFECTIVE A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 338SB 340B338 DFW - FLT 3525 - DURING PREFLIGHT, CREW NOTED A STRONG SMELL OF BURNING WIRE OR INSULATION. MAINTENANCE FOUND A BAD LIG HT BALLAST AT LOCATION 22. BALLAST WAS REMOVED AND REPLACED IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS R ETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001121100062 20011211 00062 SO 2001 12 11 SIMA200132003 1 20011116 A 3350 20131A BATTERY PACK EMB 135 EMB135LR 3260305 SO CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 704PG 145174 BOS - FLT 4554 - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHT AT ROW 1 TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A BATTERY PACK IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2001121100063 20011211 00063 EU 2001 12 11 01FDEA01040 1 20011207 A 5320 A5378184120000 CROSSBEAM AIRBUS 310 A310222 3930315 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 418FE 343 MAIN DECK CARGO FLOOR CROSSBEAM DAMAGED AT BS 37 BETWEEN LBL 26.5 & 37.5. R&R CROSSBEAM PER SRM 53-10-15 FIG 201. 2 L 7 2 4F RT A35EU 2001121100064 20011211 00064 WP 2001 12 11 01FDEA01041 1 20011210 A 5310 BULKHEAD DOUG DC10 DC1010 3022110 WP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 392FE 46626 SNRM 539 RMLG W/W FWD BULKHEAD & CTR TANK UPR AFT CHORD WITH PANEL CORRODED. ** S/D ** COMING 2 L 7 3 4F A22WE 2001121100065 20011211 00065 NM 2001 12 11 01FDEA01042 1 20011210 A 5260 STEP BOEING 727 727277 138408S NM FUSELAGE LOWER CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 N 285 AIRSTAIRS STEP #13 CORRODED AT BS 1303-1313, RBL 14.25 TO LBL 14.25. R&R STEP PER SRM 51-10-1. 2 L 7 3 4F RT A3WE 2001121100066 20011211 00066 NM 2001 12 11 01FDEA01043 1 20011210 A 5260 STEP BOEING 727 727277 138408S NM FUSELAGE LOWER CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 N 284 AIRSTAIRS STEP #12 CRACKED AT BS 1293-1303, RBL 14.25 TO LBL 14.25. R&R STEP PER SRM 51-10-1. 2 L 7 3 4F RT A3WE 2001121100067 20011211 00067 NM 2001 12 11 01FDEA01044 1 20011210 A 5260 STEP BOEING 727 727277 138408S NM FUSELAGE LOWER CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 N 281 AIRSTAIRS STEP #10 CRACKED AT BS 1273-1283, RBL 14.25-LBL 14.25. R&R STEP PER SRM 51-10-1. 2 L 7 3 4F RT A3WE 2001121100068 20011211 00068 NM 2001 12 11 01FDEA01045 1 20011210 A 5260 STEP BOEING 727 727277 138408S NM FUSELAGE LOWER CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 N 282 AIRSTAIRS STEP #11 CORRODED BS 1283-1293, RBL 14.25-LBL 14.25. R&R STEP PER SRM 51-10-1. 2 L 7 3 4F RT A3WE 2001121100069 20011211 00069 NM 2001 12 11 01FDEA01046 1 20011210 A 5260 STEP BOEING 727 727277 138408S NM FUSELAGE LOWER CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 N 280 AIRSTAIRS STEP #4 CRACKED BS 1203-1213, RBL 14.25-LBL 14.25. R&R STEP PER SRM 51-10-1. 2 L 7 3 4F RT A3WE 2001121100070 20011211 00070 NM 2001 12 11 01FDEA01047 1 20011210 A 5347 TRACK BOEING 727 727277 138408S NM FUSELAGE TOP CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 N 1438 CORROSION ON #2 CARGO TRACK BS 480, LBL 45.5, WL 210. R&R PER SRM 53-10-5. 2 L 7 3 4F RT A3WE 2001121100071 20011211 00071 NM 2001 12 11 01FDEA01048 1 20011210 A 5350 BRACKET BOEING 727 727277 138408S NM FUSELAGE LOWER CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 N 1391 BRACKET CRACKED UNDER #4 CARGO TRACK AT BS 950A, BL0, WL 207. R&R BRACKET PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2001121100072 20011211 00072 NM 2001 12 11 01FDEA01049 1 20011210 A 5347 TRACK BOEING 727 727277 138408S NM FUSELAGE TOP CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 N 1390 #2 CARGO TRACK CORRODED BS 340-380, LBL 45.5, WL 210. R&R TRACK PER SRM 53-10-5. 2 L 7 3 4F RT A3WE 2001121100073 20011211 00073 NM 2001 12 11 01FDEA01050 1 20011210 A 5320 GUSSET BOEING 727 727277 138408S NM FUSELAGE LOWER CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 N 1361 GUSSET CRACKED AT BS 950F, RBL 20, WL 146. R&R GUSSET PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 2001121100074 20011211 00074 NM 2001 12 11 01FDEA01051 1 20011210 A 5347 TRACK BOEING 727 727277 138408S NM FUSELAGE TOP CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 N 1320 #6 CARGO TRACK CORRODED AND GOUGED BS 560-660, RBL 45.5. R&R TRACK PER SRM 53-10-5. 2 L 7 3 4F RT A3WE 2001121100075 20011211 00075 EU 2001 12 11 SIMA200132201 1 20011118 A 3350 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 277AT 277 MAINTENANCE REPORTED SEVERAL EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED ALL SIX POWER SUPPLY U NITS IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001121100076 20011211 00076 EU 2001 12 11 SIMA200132202 1 20011118 A 3350 3011004 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 135MQ 135 MIA - MAINTENANCE REPORTED SOME FLOOR PROXIMITY EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TH E POWER SUPPLY UNIT 10WL IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001121100077 20011211 00077 EU 2001 12 11 SIMA200132301 1 20011119 A 3350 3011210 LIGHT AEROSP ATR72 ATR72212 8680945 EU PAX DOOR INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 308AE 309 MIA - FLT 5053 - CREW REPORTED THE PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED T HE LIGHT ASSEMBLY IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001121100078 20011211 00078 EU 2001 12 11 SIMA200132302 1 20011119 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 348AE 349 MIA - MAINTENANCE REPORTED SEVERAL FLOOR PROXIMITY EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY UNIT 61WL. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001121100079 20011211 00079 SO 2001 12 11 SIMA200132401 1 20011120 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 602AE 145048 ABI - DURING AN MBV INSPECTION, FOUND CORROSION ON THE LEFT OMEGA BEAM AT FRAME 29. REMOVED CORROSION BY CUT OUT. FABR ICATED A DOUBLER ANGLE, FILLER, AND SHIMS. REPAIR DONE IAW EMB GST-3354/01, EMB 145 (SRM145/1142 CHAPTER 53 REV 15) 53- 21-10 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2001121100080 20011211 00080 SO 2001 12 11 SIMA200132402 1 20011120 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 602AE 145048 ABI - DURING INSPECTION, FOUND CORROSION ON THE LEFT OMEGA BEAM BETWEEN FRAMES 21 AND 23. REMOVED CORROSION BY BLENDING . PERFORMED AN NDT INSPECTION OF THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR DOUBLER. REPAIR DONE IA W EMB GST-3679/01 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2001121100081 20011211 00081 SO 2001 12 11 SIMA200132403 1 20011120 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 602AE 145048 ABI - DURING A MBV INSPECTION, FOUND CORROSION ON THE LEFT OMEGA BEAM (PREV REPAIR) AT FRAME 20. REMOVED PREVIOUS REPAI R (CORROSION LIMITED TO PREV REPAIR). FABRICATED A DOUBLER ANGLE AND FILLER. WORK DONE IAW EMB 145 (SRM-145/1142 CHAPTE R 53 REV 15) 53-21-10 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2001121100082 20011211 00082 SO 2001 12 11 SIMA200132404 1 20011120 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 602AE 145048 ABI - DURING MBV INSPECTION, FOUND CORROSION ON THE LEFT OMEGA BEAM GOING UNDER CENTER AISLE SUPPORT AT FRAME 58. REMOV ED CORROSION BY CUT OUT. FABRICATED A REPAIR FILLER AND SHIMS. REPAIR DONE IAW EMB GST-3679/01 PARA 3B AND STANDARD SR M PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2001121100084 20011211 00084 EA 2001 12 11 COMA0160950 1 20011207 A 2740 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA VERT STAB MALFUNCTIONED A COMA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 01 963CA 8119 7127 FLIGHT #5797 STAB CHANNEL 1 INOP MESSAGE.REPLACED THE HSTA. 2 L 7 2 4F RT A21EA 2001121100085 20011211 00085 SO 2001 12 11 SIMA200132406 1 20011120 A 5720 ALCLAD2024T3 BRACKET EMB 145 EMB145LR 3260212 SO RT WING CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 602AE 145048 DURING INSPECTION, FOUND RIGHT WING TIP LOWER ATTACHMENT BRACKET CRACKED. REMOVED CRACK BY CUT OUT. FABRICATED A DOUBL ER ANGLE AND A FILLER. REPAIR DONE IAW EMB GST 3691/01 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2001121100086 20011211 00086 SO 2001 12 11 SIMA200132601 1 20011121 A 3397 CONNECTOR EMB 145 EMB145 3260210 SO CABIN DISCONNECTED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 609AE 145069 MKE - FLT 4118 - AFT OVERHEAD EMERGENCY LIGHT INOPERATIVE. FOUND CANNON PLUG P8644 DISCONNECTED. RECONNECTED CANNON PL UG AND OPS CHECK GOOD. (M) 2 L 7 2 4F RT T00011AT 2001121100087 20011211 00087 EA 2001 12 11 COMA0160951 1 20011209 A 3220 PIN CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 721CA 7259 FLIGHT #5686 NLG DOES NOT RETRACT WHEN LANDING GEAR SELECTED UP.FOUND NLD DOWN LOCK SAFETY PIN INSTALLED. - REMOVED PIN AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2001123100036 20011231 00036 EA 2001 12 31 COMA0160952 1 20011209 A 5415 601370102 FITTING CNDAIR CL600 CL6002B19 1900309 EA RT PYLON CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 964CA 12888 7129 DURING REMOVAL OF THE RIGHT ENGINE ASSEMBLY, DISCOVERED PITTING CORROSION ON THE AFT ENGINE PYLON THRUST FITTING MOUNTIN G RIB. REPAIRED IAW REO 601R-54-50-040. 2 L 7 2 4F RT A21EA 2001121100088 20011211 00088 GL 2001 12 11 SIMA200132602 2 20011121 A 7200 CARBON SEAL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL ENGINE FAILED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 602AE 145048 ABI - FLT 9305 - RETURN TO FIELD ABI, SMOKE IN LAVATORY, EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. REPLACED O-RING AND ZERO CARBON SEAL ON RT ENGINE. (M) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2001121100089 20011211 00089 EU 2001 12 11 SIMA201280801 1 20011104 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN MALFUNCTIONED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 905AE 340B319 DFW - FLT 3913 - DURING PREFLIGHT, CREW REPORTED THE FLOOR EMERGENCY LIGHT AT 7 B/C TO BE INOPERATIVE. MAINTENANCE COUL D NOT DUPLICATE DISCREPANCY. OPERATIONAL CHECK WAS GOOD IAW SAAB MM AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001121100090 20011211 00090 EU 2001 12 11 SIMA20130601 1 20011102 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN MISINSTALLED A SIMA K NONE W L INADEQUATE Q C NO TEST TX TAXI/GRND HDL 1 SW 21 388AE 340B388 CREW REPORTED THE EMERGENCY EXIT LIGHT ABOVE FLIGHT ATTENDANT JUMPSEAT IS INOPERATIVE. MAINTENANCE FOUND THE LIGHT ASSE MBLY TO BE INSTALLED INCORRECTLY. LIGHT ASSEMBLY WAS REINSTALLED CORRECTLY IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2001121100091 20011211 00091 NM 2001 12 11 TSAA0153163 1 20011125 A 5330 6545866688 SKIN BOEING 737 7372S2C 138448G NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 806AL 21927 FUSELAGE SKIN CRACKED AT APPROXIMATELY BS 620 BL 6LT AND 6 RT (KEEL BEAM). TRIMMED OUT DAMAGE AREA, HFEC INSPECTION ARO UND CUTOUT AREA NO DEFECTS NOTED. FABRICATED AND INSTALLED DOUBLER. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2001121100092 20011211 00092 NM 2001 12 11 USAA011361 1 20011107 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 22757 PIT - FOUND SKIN CRACKED .20, FUSELAGE SKIN BETWEEN FRAME 727A AND 727B STRINGER 16R. INSTALLED DOUBLER AND REPAIR ANGL E PER EA 72869 AND SRM 53-30-3. (M) 2 L 7 2 4F A16WE 2001121100093 20011211 00093 NM 2001 12 11 01FDEA01052 1 20011210 A 5315 FLOORBEAM BOEING 727 727277 138408S NM FUSELAGE TOP CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 N 1289 UPPER CHORD OF FLOORBEAM CORRODED AT BS 340, RBL 2-8, WL 208.1. R&R FLOORBEAM PER SRM 53-10-8. 2 L 7 3 4F RT A3WE 2001121100094 20011211 00094 NM 2001 12 11 01FDEA01053 1 20011210 A 5315 FLOORBEAM BOEING 727 727277 138408S NM FUSELAGE TOP CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 N 1288 UPPER CHORD OF FLOORBEAM CORRODED BS 340, RBL 40-55, WL 208.1. R&R FLOORBEAM PER SRM 53-10-8. 2 L 7 3 4F RT A3WE 2001121100095 20011211 00095 NM 2001 12 11 01FDEA01054 1 20011210 A 5320 ANGLE BOEING 727 727277 138408S NM FUSELAGE TOP CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 N 1089 "Z" ANGLE CORRODED AT BS 340, RBL 18-40. R&R ANGLE PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2001121100096 20011211 00096 NM 2001 12 11 01FDEA01055 1 20011210 A 5320 TIE CLIP BOEING 727 727277 138408S NM FUSELAGE TOP CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 N 947 STRINGER TIE CLIP CRACKED AT BS 1070, STR 5L. R&R CLIP PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2001121100097 20011211 00097 NM 2001 12 11 01FDEA01056 1 20011210 A 5320 CLIP BOEING 727 727277 138408S NM FUSELAGE TOP CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 N 946 STRINGER TIE CLIP CRACKED BS 970, STR 4L. R&R CLIP PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2001121100098 20011211 00098 NM 2001 12 11 01FDEA01057 1 20011210 A 5320 TIE CLIP BOEING 727 727277 138408S NM FUSELAGE TOP CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 N 945 STRINGER TIE CLIP CRACKED AT BS 950E, STR 6R. R&R CLIP PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2001121100099 20011211 00099 NM 2001 12 11 01FDEA01058 1 20011210 A 5330 SKIN BOEING 727 727277 138408S NM FUSELAGE LOWER CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 N 906 CORROSION ON FUSELAGE SKIN AT BS 720D, STR 27R. R&R SKIN PER SRM 53-30-3. 2 L 7 3 4F RT A3WE 2001121100100 20011211 00100 EU 2001 12 11 USAASA01057 1 20011029 A 2120 SMOKE AIRBUS A319 A319112 3930323 EU CABIN DETECTED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 19 739US 1263 FLT 477 - EN ROUTE PHL-TPA - DURING SHORT FINAL INTO TPA, THE CABIN CREW REPORTED POSSIBLE SMOKE IN THE AFT GALLEY. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AFT GALLEY AND FOUND NO SMOKE EVIDENT WITH ANY GALLEY SYSTEM OPERATING. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2001121100101 20011211 00101 NM 2001 12 11 01FDEA01059 1 20011209 A 5320 GUSSET BOEING 727 727277 138408S NM FUSELAGE LOWER CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 N 733 FLOOR SUPPORT GUSSET CRACKED BS 480, STR 28L. R&R GUSSET PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2001121100102 20011211 00102 NM 2001 12 11 01FDEA01060 1 20011209 A 5320 ANGLE BOEING 727 727277 138408S NM FUSELAGE LOWER CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 N 730 FLOOR TO BULKHEAD ANGLE CRACKED AT BS 480, RBL 18, STR 27R. R&R ANGLE PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2001121100103 20011211 00103 NM 2001 12 11 AWXA200100626 1 20011115 A 5330 65457743 SKIN BOEING 737 7373G7 1384595 NM DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 311AW 24712 MCN - C12 CK - "C" - EXTERNAL SKIN HAS 3.9" X 1.9" DENT AT BS 727D TO 727E, STR 22 L/H TO 23 L/H. MAINTENANCE CONFIRMED THE DENT WAS OUT OF LIMIT USING 737-300 SRM 53-00-01, PG 104. DAMAGED AREA OF SKIN WAS CUT OUT AND A HFEC INSPECTION WAS PERFORMED TO CHECK FOR CRACKS, (NONE WERE FOUND). REPAIR PLATE WAS FORMED AND INSTALLED IAW B737-300 SRM 53-00-01, PG 2 04-206. 2 L 7 2 4F RT A16WE 2001121100104 20011211 00104 NM 2001 12 11 AWXA200100627 1 20011115 A 5330 654688195 SKIN BOEING 737 7373G7 1384595 NM DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 311AW 25776 MCN - C-12 CK - "C" - EXTERNAL SKIN HAS 3.3" X 1.7" DENT .056 DEEP AT BS 1040, STR 25 R/H, WL 192. MAINTENANCE CONFIRMED DENT WAS OUT OF LIMITS IAW B737-300 SRM 53-00-01, PG 104. DAMAGED AREA OF SKIN WAS CUT OUT AND HFEC INSPECTION WAS ACCO MPLISHED TO CHECK FOR CRACKS (NO CRACKS WERE FOUND). REPAIR PLATE WAS FORMED AND INSTALLED AT BS 1040 STR 25 R/H IAW B73 7-300 SRM 53-00-01, PG 204. 2 L 7 2 4F RT A16WE 2001121100105 20011211 00105 NM 2001 12 11 AWXA200100628 1 20011115 A 5330 65457759 SKIN BOEING 737 7373G7 1384595 NM DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 311AW 24712 MCN - C12 CK - "C" - EXTERNAL SKIN HAS 2.10" X 1.95" DENT .036 DEEP AT BS 887, STR 23 R/H TO STR 24 R/H. MAINTENANCE CON FRIMED DENT WAS OUT OF LIMITS PER B737-300 SRM 53-00-01, PG 104. DAMAGED AREA OF SKIN WAS CUT OUT AND HFEC INSPECTION WA S ACCOMPLISHED TO CHECK FOR CRACKS (NO CRACKS WERE FOUND). REPAIR PLATE FABRICATED AND INSTALLED AT BS 887, STR 23 R/H T O STR 24 R/H, IAW B737-300 SRM 53-50-01, PG 204-206. 2 L 7 2 4F RT A16WE 2001121100106 20011211 00106 NM 2001 12 11 AWXA200100630 1 20011117 A 5311 654580519 FRAME BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 311AW 24712 MCN - C12 CK - "C" - FUSELAGE FRAME HAS 1" CRACK AT BS 277 JUST ABOVE STR 16R, VERIFIED BY HFEC INSPECTION. MAINTENANCE CUT OUT CRACKED AREA OF FRAME AT BS 277 AND ACCOMPLISHED HFEC INSPECTION TO CHECK FOR CRACKS (NO CRACKS WERE FOUND). FAB RICATED AND INSTALLED FILLER AND DOUBLER IAW 737-300 SRM 51-70-11, PG 1-6. 2 L 7 2 4F RT A16WE 2001121100107 20011211 00107 NM 2001 12 11 AWXA200100631 1 20011120 A 5330 65C45721 SKIN BOEING 737 7373G7 1384595 NM GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 311AW 24712 MCN - C12 CK - "C" - FUSELAGE SKIN HAS .4" X .080" GOUGE .019 DEEP AT BS 1004.75, STR 2L. GOUGE MEASURED OUT OF LIMITS P ER B737-300 SRM 53-00-01, FIG 101, DETAIL II, PG 104. MAINTENANCE REMOVED 3 STRINGER CLIPS, 2 BRACKETS, AND A STRINGER E ND FITTING AT STR 2L BETWEEN BS 986 AND 1016. GOUGED AREA OF SKIN WAS CUT OUT AND HFEC INSPECTION WAS ACCOMPLISHED TO CH ECK FOR CRACKS (NO CRACKS WERE FOUND). FABRICATED AND INSTALLED -1 DOUBLER AND -2 STRINGER AT BS 1004.75 STR 2L, IAW B73 7-300 SRM 53-00-01, PG 201, AND SRM 51-40-02, PG 3-4. REINSTALLED 3 STRINGER CLIPS, STRINGER END FITTING, AND 2 BRACKETS AT STR 2L BETWEEN BS 986 AND 1016, IAW 737-300 SRM 51-40-02 PG 10-11 & 74. 2 L 7 2 4F RT A16WE 2001121100108 20011211 00108 NM 2001 12 11 AWXA200100632 1 20011111 A 5313 6545767512 STRINGER BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 311AW 24712 MCN - C12 CK - "C" - 1" CRACK FOUND AT FWD EDGE OF WING SCANNING LIGHT CUTOUT AT BS 500C+4, STR 16L. MAINTENANCE REMOVED STRINGER END, FABRICATED REPAIR CHANNEL AND FILLER, AND INSTALLED REPAIR PARTS IAW AWA ER 03-5312-01094-DD1. 2 L 7 2 4F RT A16WE 2001121100109 20011211 00109 NM 2001 12 11 AWXA200100633 1 20011130 A 5330 657378337 SKIN BOEING 737 7373G7 1384595 NM DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 311AW 24712 MCN - C12 CK - "C" - LEADING EDGE OF L/H HORIZONTAL STAB HAS 2" DENT .150 DEEP APPROXIMATELY 194" FROM HORIZONTAL STAB R OOT, STAB STA 122.7. MAINTENANCE REMOVED DAMAGED AREA; FABRICATED DOUBLER AND FILLER, AND INSTALLED REPAIR PARTS AT STAB STA 122.7 IAW AWA ER 03-5513-01327-ESI. 2 L 7 2 4F RT A16WE 2001121100110 20011211 00110 NM 2001 12 11 AWXA200100635 1 20011127 A 5310 500826162 WEB BOEING 737 7373S3 1384711 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 PHX - MAJOR REPAIR - "C" - 1.5" CRACK FOUND ON RADIUS OF INTERCOASTAL AND STRAP AT FWD LAV ATTACH POINT BS 305, STR 5L. MAINTENANCE REMOVED CRACKED INTERCOASTAL AT BS 305 AND STRAP AT STR 5L: FABRICATED NEW INTERCOASTAL AND STRAP, AND INSTA LLED REPAIR PARTS IAW PL-50-8261, AND B737-300 SRM 51-40-02, FIG 1, PG 1. 2 L 7 2 4F RT A16WE 2001121100114 20011211 00114 EU 2001 12 11 SABA011071 1 20011207 A 7100 310440001 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TFE33112UHR WP STRIPPED A SABA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 33 963AE 11432 6023 963 66102 Aircraft 963 on flight 5042 from Charleston SC to Raleigh NC. As aircraft was passing through 9500 feet, the left engine lost engine oil pressure, torque and RPM. Engine was shutdown by the aircrew. Aircraft returned to Charleston with no o ther problems. Inflight Emergency was declared and Emergency procedures were used. Maintenance found the NTS Valve hela- coil pulled from engine case. Causing the lost of engine oil supply. Engine was removed and replaced. Aircraft was retur ned to service. 2 L 7 2 4T 4 T RT A56EU E4WE 2001121100117 20011211 00117 WP 2001 12 11 G1F2001F00001 2 20011017 A 7321 307080022 FCU BRAERO DH125 HS125700A 4230170 EU GARRTT TFE731 TFE7313R1H 29001 WP RT ENGINE DEFECTIVE B G1FR K NONE X ENGINE FLAMEOUT IN INSP/MAINT 1 GL 13 101FC 14085 208 NA0263 P84210 DURING NORMAL OPERATION (GROUND RUN) OF RIGHT ENGINE, THE ENGINE FLAMED OUT AFTER IDLE HAD BEEN SELECTED. THIS CONDITIO N COULD BE REPEATED AND WAS INTERMITTENT WHEN THE THROTTLE LEVER WAS RETARDED TO IDLE POSITION. AFTER TROUBLESHOOTING F UEL SYSTEM PER MM, THE FUEL CONTROL WAS REMOVED AND REPLACED WITH A REPAIRED UNIT. FUNCTIONAL CHECKS WERE PERFORMED IAW MM WITH NO OPERATIONAL DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE AND FLIGHT EVALUATED WITH NO FURTHER DISCREPANC IES. 2 L 7 2 4F 4 F A3EU E6WE 2001121100118 20011211 00118 EU 2001 12 11 G1X2001F00000 1 20011113 A 5610 17820110 WINDSHIELD ISRAEL GALAXY GALAXY 4500307 EU PWA 306 PW306B NE COCKPIT CRACKED B G1XR O OTHER O OTHER CR CRUISE 1 SW 19 878CS 114 027 WINDSHIELD ON COPILOTS SIDE SHATTERED IN FLIGHT. 2 L 7 2 4F 4 F RT A53NM E35NE 2001121100119 20011211 00119 EU 2001 12 11 G1X2001F00001 1 20011113 A 5610 1782011 WINDSHIELD ISRAEL GALAXY GALAXY 4500307 EU COCKPIT CRACKED B G1XR O OTHER O OTHER CR CRUISE 1 SW 19 505GA 653 005 AFTER APPROXIMATELY 5 HOURS OF FLIGHT AT FL430, THE PILOTS WINDSHIELD SHATTERED IN THE INNER LAYERS. WINDSHIELD HEAT WA S ON LOW. NO ICING CONDITIONS OR INDICATION OF STRIKE HAD OCCURRED. 2 L 7 2 4F RT A53NM 2001121100120 20011211 00120 EU 2001 12 11 G1X2001F00002 1 20011113 A 5610 17820110 WINDSHIELD ISRAEL GALAXY GALAXY 4500307 EU COCKPIT CRACKED B G1XR O OTHER O OTHER DE DESCENT 1 SW 19 83EJ 362 009 AIRCRAFT DESCENDED FROM FL410 TO FL250 AND HEARD A LOUD POP SOUND. THE COPILOTS WINDSHIELD WAS SHATTERED IN THE INNER L AYERS. NO ICING CONDITIONS OR INDICATION OF STRIKE HAD OCCURRED. 2 L 7 2 4F RT A53NM 2001121100121 20011211 00121 NM 2001 12 11 G2L2001F00000 1 20010106 A 5714 693188 ANGLE BOEING 707 707 UTILUSE NM WING BOX CRACKED E G2LR K NONE O OTHER IN INSP/MAINT 1 SO 15 770FW 20016 DURING VISUAL INSPECTION PERFORMED IN CONJUNCTION WITH FUEL TANK SEALING ON B707 AIRCRAFT, TWELVE(12) SUPPORT ANGLES WER E DISCOVERED CRACKED AT THE TOP OF THE WING CENTER SECTION ATTACH. FRONT SPAR STIFFENERS AT FS 600K, WL195, R/L BL 7,13 ,20,28,35,42. SIMILAR OCCURENCES TO VARYING DEGREES WERE NOTED. THE AFOREMENTIONED CRACK WERE VERIFIED WITH HIGH FREQUE NCY EDDY CURRENT PER MM. THE CONTRACTOR, REMOVED SUPPORT ANGLE PER ANALYSIS. ANALYSIS SHOWED THE CRACK TO BE LOAD VERS US FATIGUE INDUCED. 2 L 7 4 4J RT 4A21 2001121100122 20011211 00122 WP 2001 12 11 GTIA010906 1 20010922 A 2560 S168MA MEGAPHONE DOUG DC9 DC981 3022081 WP PWA JT8 JT8D9 52048 NE CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 805NK 48058 FORWARD RIGHT EMERGENCY MEGAPHONE, INOPERATIVE. REMOVED AND REPLACED FORWARD RIGHT EMERGENCY MEGAPHONE, IAW MM, OPS CHE CKED GOOD. 2 L 7 2 4F 4 F A6WE E2EA 2001121100123 20011211 00123 CE 2001 12 11 HUK2001F00001 1 20010906 A 7933 624600615 INDICATOR CESSNA 207 T207 2073612 CE CONT O520 IO520F 17032 SO COCKPIT SHORTED E HUKA O OTHER O OTHER NR NOT REPORTED 1 NM 01 7405 51 20700147 OIL TEMPERATURE GAUGE SUPPLIED WITH SERVICE KIT-OIL GAUGE SHORTED OUT INTERNALLY BLOWING OUT POWER CONVERTER. THIS WAS THE 3RD GAUGE IN 4 YEARS. WHEN POWER CONVERTER BLEW POWER SURGE/SHORT CREATED MALFUNCTION IN ENGINE INSTRUMENT CLUSTER AND CREATING BURNING SMELL, AMONG ITEMS DAMAGED BEING REPLACED, AN ELECTRIC OIL TEMPERATURE UNIT WITH ORIGINAL CAPILLARY TYPE UNIT. 1 H 7 1 3O 3 O A16CE E5CE 2001121100124 20011211 00124 CE 2001 12 11 HYI2001F00010 1 20011106 A 2435 99103971 RELAY CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO STARTER FAILED E HYIA O OTHER H ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 NE 01 780EA 402C0257 ENROUTE , AIRCRAFT EXPERIENCED LOSS OF ELECTRICAL POWER. CREW LANDED WITHOUT INCIDENT. MECHANIC FOUND RIGHT STARTER RE LAY ENGAGED, RESHUT STARTER, ALLOWING THE ALTERNATORS TO DROP OFF LINE. MECHANIC REPLACED STARTER, STARTER RELAY AND BA TTERY AND RETURNED AIRCRAFT TO SERVICE. 1 L 7 2 3O 3 O A7CE E8CE 2001121100126 20011211 00126 SW 2001 12 11 I7W2001F00000 1 20010619 A 7931 WARNING SYSTEM SWRNGN SA227 SA227AC 8780603 SW COCKPIT FALSE INDICATION E I7WA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 05 787C AC550 PILOT OBSERVED OIL AND EGT FLUCTUATIONS AND A LOW OIL PRESSURE LIGHT. DID A PRECAUTIONARY ENGINE SHUTDOWN WITHOUT FURTH ER PROBLEMS. MECHANIC FOUND NO CAUSE, DID SOME TROUBLESHOOTING AND AN INSPECTION. FOUND SMALL OIL LEAK FROM PROP SEAL BUT LEAK WAS WITHIN NORMAL LIMITS. GROUND RUN ENGINE WITHOUT DUPLICATING THE INDICATION PROBLEM, SO THEY RELEASED IT TO SERVICE. 2 L 7 2 4T RT A8SW 2001121100127 20011211 00127 SW 2001 12 11 I7W2001F00001 1 20010626 A 2420 WIRE SWRNGN SA227 SA227* SW GARRTT TPE331 TPE331* 01514 WP ELEC CONSOLE LOOSE E I7WA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 05 898ML DC898B PILOT SMELLED ELECTRICAL ODOR AND GENERATORS WOULD NOT COME ON TOGETHER. MECHANIC FOUND A LOOSE CABLE IN THE RIGHT ELEC TRICAL CONSOLE THAT WAS ARCING. CLEANED AND TORQUED CABLE. PARALLELED GENERATORS. 2 L 7 2 4T 3 T RT A5SW E2WE 2001121100128 20011211 00128 CE 2001 12 11 IBU2001F00000 1 20011119 A 2434 BOLT CESSNA 421 421C 2076016 CE CONT O520 GTSIO520C 17032 SO ALTERNATOR SHEARED A IBUA O OTHER O OTHER NR NOT REPORTED 1 WP 07 748CA 35 A193680 421C0905 ALTERNATOR CASE THIN BOLTS ARE SHEARING. BOLTS THAT RECOVERED FROM ENGINE COWLING, SHOWS SIGNS OF STRETCHING. BOLTS PO SSIBLE OVER TORQUED FROM FACTORY. 1 L 7 2 3O 3 O A7CE E7CE 2001121100129 20011211 00129 CE 2001 12 11 IMJ2001F00000 1 20011011 A 7830 1217243 DRIVE SHAFT LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP THRUST REVERSER DISENGAGED A IMJA O OTHER O OTHER LD LANDING 1 EA 25 50MJ 12269 164 ON LANDING THE NR 1 THRUST REVERSER WOULD NOT STOW. THE FLEXIBLE DRIVESHAFT (OUTBOARD) BECAME DISENGAGED FROM THE AIR M OTOR DRIVE ASSEMBLY. WITH ONLY ONE SIDE DRIVING THE THRUST REVERSER, THE MECHANISM COCKED AND BOUND UP. ALTHOUGH THIS PROBLEM MAY HAVE RESULTED FROM BEAR, A BETTER RETENTION METHOD MIGHT BE CONSIDERED FOR THE DRIVESHAFT. 2 L 7 2 4F 4 F A10CE E6WE 2001121100130 20011211 00130 CE 2001 12 11 J4V2001F00000 1 20010905 A 3230 710501 MOTOR BEECH 300 300BEECH 1152930 CE PWA PT6 PT6A60A 52043 NE LANDING GEAR FAILED E J4VA O OTHER J WARNING INDICATION AP APPROACH 1 SW 03 3AH 6521 FA130 LANDING GEAR FAILED TO EXTEND DUE TO INOPERATIVE MOTOR. THERE ARE NO AIRWORTHINESS LIMITATIONS ON THIS COMPONENT. RECO MMEND CYCLE LIMITS BE CONSIDERED. 2 L 7 2 4T 4 T A24CE E4EA 2001121100131 20011211 00131 EU 2001 12 11 JGV2001F00011 1 20010927 A 3246 5000425 WHEEL AMD FALC10 FALCON10 2730101 EU MLG CRACKED A JGVR K NONE O OTHER IN INSP/MAINT 1 EA 11 720DF 2495 26 DISASSEMBLED WHEEL TO INSPECT AFTER A CRACK WAS NOTED IN THE OUTBOARD WHEEL HALF. REMOVAL OF PAINT REVEALED A CRACK RAD IATING FROM A LIGHTENING HOLE INWARD TOWARD THE BEARING RACE AT A 45 DEGREE ANGLE AND ABOUT 1.5 INCHES IN LENGTH. FURTH ER INVESTIGATION REVEALED THAT A PERMANENT WEIGHT HAD BEEN REMOVED FROM THE INBOARD WHEEL HALF AND REPLACED IT WITH 5 LA RGE AREA WASHERS AND AN INCORRECT RETAINING BOLT. THE BOLT IS TOO LONG AND CONTACTS THE OUTBOARD WHEEL HALF AFTER ASSEM BLY. TORQUEING OF THE WHEEL BOLTS DURING ASSEMBLY CREATED A STRESS POINT RESULTING IN A CRACK. 2 L 7 2 4F A33EU 2001121100132 20011211 00132 CE 2001 12 11 JJB2001F00003 1 20010908 A 2821 1189200403 STRAINER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A65AR 52043 NE FUEL SYSTEM MISSING A JJBA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 01 852CA 2483 VE389 DURING SCHEDULED MAINTENANCE, (FUEL TANK INSPECTION) FOUND RIGHT AFT TRANSFER PUMP FUEL STRAINER AND HOSE NOT INSTALLED ON AIRCRAFT. NOTE: NOT INSTALLED BY MFG. 2 L 7 2 4T 4 T RT A24CE E4EA 2001121100133 20011211 00133 CE 2001 12 11 JJB2001F00004 1 20010908 A 2820 15600512D050 HOSE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A65AR 52043 NE FUEL SYSTEM MISSING A JJBA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 01 852CA 2483 UE389 DURING SCHEDULED MAINTENANCE, (FUEL TANK INSPECTION) FOUND RIGHT AFT TRANSFER PUMP FUEL STRAINER AND HOSE NOT INSTALLED ON AIRCRAFT. NOTE: NOT INSTALLED BY MFG. 2 L 7 2 4T 4 T RT A24CE E4EA 2001121100134 20011211 00134 NE 2001 12 11 JJB2001F00005 2 20011114 A 7200 SMOKE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ENGINE DETECTED A JJBA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 01 856CA VE403 PSO403 TOWER REPORTED SMOKE COMING FROM THE RIGHT ENGINE ON CLIMB OUT. CAUSE OF PROBLEM UNKNOWN, INSPECTED AND LEAK CHECKED EN GINE. CHECKED OIL LEVEL AND PERFORMED GROUND RUN. NO DISCREPANCIES NOTED. 2 L 7 2 4T 4 T RT A24CE E26NE 2001121100135 20011211 00135 SO 2001 12 11 JOP2001F00000 1 20010905 A 3246 1627753156 WHEEL PIPER PA23 PA23250 7102308 SO LYC O540 TIO540* 41532 EA LT MLG SEPARATED A JOPA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 17 54828 3600 277554125 1955948A AIRCRAFT TAXIED ON THE RUNWAY FOR TAKEOFF AND BEFORE THE TAKEOFF BEGAN THE LEFT MAIN WHEEL OUTER HALF, SEPARATED AND THE TAKEOFF WAS ABORTED. 1 L 7 2 3O 3 O 1A10 E14EA 2001121100137 20011211 00137 EU 2001 12 11 KBMA112020 1 20011101 A 3150 CH5070105 WARNING HORN SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT SHORTED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 230SH 2337 HORN DOES NOT BLOW, SHORTED INTERNALLY. INSTALLED SERVICEABLE HORN. 1 G 7 1 3U 3 U NC H9EU E19EU 2001121100138 20011211 00138 NM 2001 12 11 M522001F00000 1 20010826 A 5312 PRESSURE PANEL BOEING 737 73733A 1384673 NM FUSELAGE CRACKED B M52R K NONE O OTHER IN INSP/MAINT 1 SO 11 165AW 23626 LEFT HAND W/W FUS STATION 664.0 PRESSURE WEB CRACKED IN 1 LOCATIONS LBL 34. 2 L 7 2 4F RT A16WE 2001121100139 20011211 00139 EU 2001 12 11 M7I2001F00002 1 20011122 A 3260 1EN114N119 DOWNLOCK SWITCH STBROS SD3 SD360 8100606 EU PWA PT6 PT6* 52043 EA RT MLG FAILED A M7IR L ABORTED APPROACH N FALSE WARNING LD LANDING 1 GL 13 367AC SH3626 ON APPROACH TO RUNWAY, THE CAPTAIN CALLED FOR GEAR DOWN AND APPROACH CHECKS. GEAR IS MOVED TO THE DOWN POSITION. THE N OSE AND LEFT INDICATE DOWN AND LOCKED, BUT THE RIGHT INDICATES IT IS STILL IN TRANSIT. THE GEAR WAS CYCLE, BUT STILL SH OWED IN TRANSIT. THE AIRCRAFT WAS FLOWN BY THE ATC TOWER AND THE CREW WAS TOLD IT LOOKED LIKE IT WAS DOWN. IAW THE EME RGENCY PROCEDURES IN THE AFM THE CREW T HANDLED IT DOWN. REPLACED THE DOWNLOCK SWITCH. OPS CHECK GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 3 T A41EU E2NE 2001121100140 20011211 00140 EA 2001 12 11 MAS2001F00002 1 20011006 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE COCKPIT MALFUNCTIONED A MASA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 7291Z 7291 IN FLIGHT, THE CREW RECEIVED A PASSENGER DOOR OUTER HANDLE WARNING MESSAGE. THE AIRCRAFT DIVERTED, WHERE ON CALL MAINTE NANCE INSPECTED AND CHECKED THE DOOR HANDLE MECHANISM. THEY OPERATED THE DOOR SEVERAL TIMES WITH NO WARNING MESSAGES AN D THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2001121100141 20011211 00141 WP 2001 12 11 MZA2001F00000 1 20010910 A 2780 ARH0602597 CONTROL CABLE DOUG DC10 DC1030F 3023504 WP GE CF6 CF650* 30018 NE L/E SLAT BROKEN A MZAR K NONE O OTHER IN INSP/MAINT 1 SO 09 1859U 47819 DURING C-CHECK, FOUND NR 3 RIGHT SLAT EXTEND CABLE BROKEN. CAUSE UNDER INVESTIGATION. 2 L 7 3 4F 4 F RT A22WE E23EA 2001121100142 20011211 00142 2001 12 11 NSV2001F00001 4 20011102 A 6122 8210212 GOVERNOR BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA PROPELLER FAILED A NSVA O OTHER R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 EA 27 550CJ 39 UC50 32626 RKD-RH PROP RPM DROPPED TO 1400 DURING TAKE OFF ROLL. OFF WAS ABORTED AIRCRAFT RETURNED TO GATE. MECHANIC REMOVED AND REPLACED PROP GOVERNOR, RIGGED AS REQUIRED. OPS CHECKED GOOD. 2 L 7 2 4T 4 T RT A24CE E4EA 2001121100143 20011211 00143 CE 2001 12 11 NSVA0107 1 20010818 A 2612 24412886 FIRE LOOP BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA LT ENGINE DAMAGED A NSVA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 15031 UC103 32063 LEFT ENGINE FIRE LIGHT CAME ON DURING TAXI. PRELIMINARY INSPECTION LOCATED FAULT, AIRCRAFT RELEASED UNDER SFP TO HYA. MAINTENANCE REMOVED AND REPAIRED FORWARD SECTION OF FIRE LOOP, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A24CE E4EA 2001121100144 20011211 00144 NM 2001 12 11 NTB2001F00000 1 20010823 A 3230 LANDING GEAR LKHEED P2V P2V7 5260112 NM WRIGHT R3350 972TC18DA1 67037 EA NLG MALFUNCTIONED A NTBR O OTHER J WARNING INDICATION AP APPROACH 1 NM 05 14447 8010 NOSE LANDING GEAR DID NOT LOCK WHEN EXTENDED. FLIGHT CREW MANUALLY LOCKED AND PINNED GEAR. NORMAL LANDING WAS THEN MAD E. POSSIBLE IMPROPER TORQUE OR FATIGUE. 4 M 7 4 4R 4 R RT A1RM E272 2001121100145 20011211 00145 CE 2001 12 11 OKT2001F00000 1 20011120 A 3230 6041H220 RELAY CESSNA 340 340A 2076405 CE CONT O520 TSIO520* 17040 SO LANDING GEAR FAILED E OKTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 19 2670H 4850 340A0738 LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF, AIRCRAFT LANDED WITHOUT INCIDENT. TROUBLESHOT LANDING GEAR SYSTEM AND FOU ND LANDING GEAR RELAY TO BE INOPERATIVE. PROBABLE CAUSE FOUND TO BE CYCLIC TIME OF PART. LANDING GEAR FUNCTIONAL CHECK SATISFACTORY AT PREVIOUS INSPECTION. 1 L 7 2 3O 3 O 3A25 E8CE 2001121100146 20011211 00146 NM 2001 12 11 P7U2001F00001 1 20010628 A 2612 0881031007 SWITCH BOEING 737 737* NM COCKPIT FAILED B P7UR O OTHER O OTHER NR NOT REPORTED 1 EA 17 VPBHN 7 32438 FIRE BELL CUTOUT SWITCH: SWITCHES, 2 EACH SHORTED INTERNALLY, SHOULD RETURN TO N/O CONDITION. MICRO SWITCH FAILED INTE RNALLY IN ASSEMBLY. REMOVED AND REPLACED WITH NEW SWITCHES. RETESTED SYSTEM, NO MALFUNCTIONS OR DEFECTS NOTED. OPS CH ECKED GOOD 2 L 7 2 4F RT A16WE 2001121100147 20011211 00147 NM 2001 12 11 P7U2001F00002 1 20010831 A 2612 0881031007 SWITCH BOEING 737 737* NM COCKPIT FAILED B P7UR O OTHER O OTHER NR NOT REPORTED 1 EA 17 375BJ 14 32807 SWITCH ASSEMBLY SHORTED INTERNALLY. CONDITION SHOWS SYSTEM AURAL WARNING BEING RESET WITHOUT DEPRESSING SWITCH. INTERN AL FAILURE OF MICRO SWITCH ASSEMBLY. REMOVED AND REPLACED ASSEMBLY, SYSTEM OPERATIONAL, CHECK SATISFACTORY.(K) 2 L 7 2 4F RT A16WE 2001121100148 20011211 00148 NM 2001 12 11 P7U2001F00003 1 20010831 A 3150 0881031006 SWITCH BOEING 737 737* NM COCKPIT FAILED B P7UR O OTHER O OTHER NR NOT REPORTED 1 EA 17 375BJ 14 32807 SWITCH CONTACTS REMAINED IN OPEN CONDITION CAUSING MASTER CAUTION SYSTEM TO BE IN A RESET STATE AT ALL TIMES. THERE FOR NOT ALLOWING MASTER CAUTION WARNINGS TO BE DISPLAYED. INTERNAL MICROSWITCH FAILURE. REMOVED AND REPLACED SWITCH ASSEM BLY, SYSTEM OPERATIONAL, CHECK SATISFACTORY.(K) 2 L 7 2 4F RT A16WE 2001121100149 20011211 00149 NM 2001 12 11 P7U2001F00004 1 20010831 A 3150 SWITCH BOEING 737 737* NM COCKPIT FAILED B P7UR O OTHER O OTHER NR NOT REPORTED 1 EA 17 379BJ 32777 SWITCH ASSEMBLY SHORTED INTERNALLY. CONDITION SHOWS SYSTEM AURAL WARNING BEING RESET WITHOUT DEPRESSING SWITCH. INTERN AL FAILURE OF MICROSWITCH ASSEMBLY. REMOVED AND REPLACED SWITCH ASSEMBLY, SYSTEM OPERATIONAL, CHECK SATISFACTORY.(K) 2 L 7 2 4F RT A16WE 2001121100150 20011211 00150 NM 2001 12 11 P7U2001F00005 1 20010831 A 3150 0881031006 SWITCH BOEING 737 737* NM COCKPIT FAILED B P7UR O OTHER O OTHER NR NOT REPORTED 1 EA 17 379BJ 8 32777 SWITCH CONTACTS REMAINED IN OPEN CONDITION CAUSING MASTER CAUTION SYSTEM TO BE IN A RESET STATE AT ALL TIMES; NOT ALLOW ING MASTER CAUTION WARNINGS TO BE DISPLAYED. INTERNAL MICROSWITCH FAILURE. REMOVED AND REPLACED SWITCH ASSEMBLY, SYSTE M OPERATIONAL, CHECK SATISFACTORY.(K) 2 L 7 2 4F RT A16WE 2001121100151 20011211 00151 SO 2001 12 11 RNT2001F00000 1 20011018 A 5730 62061002 DOUBLER PIPER PA28 PA28181 7102807 SO LYC O360 O360* 41514 EA WING CRACKED D RNTG K NONE O OTHER IN INSP/MAINT 1 CE 09 8150A 6499 288090228 DOUBLER SEVERELY CRACKED UNDER WING WALK AREA OF WING. TOP SKIN WAS OK. AREA WAS CONSIDERABLY WEAKENED AND WOULD DEFLE CT UPON ENTERING OR EXITING THE AIRCRAFT. 1 L 7 1 3O 3 O 2A13 E286 2001121200001 20011212 00001 NM 2001 12 12 HNAA0100078 1 20011210 A 3350 6104791X POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM INOPERATIVE A HNAA K NONE O OTHER NR NOT REPORTED 1 EA 07 923HA 36646 099 THREE EMERGENCY LIGHTS WOULD NOT EXTINGUISH. REPLACED EMERGENCY LIGHTS POWER SUPPLY 3351-PS2. 2 H 7 2 4T RT A13NM 2001121200002 20011212 00002 NM 2001 12 12 01FDEA01061 1 20011209 A 3210 CYLINDER BOEING 727 727277 138408S NM LAND GEAR CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 N 491 CHICKEN WIRE CRACKS ON CHROME OF RMG INNER CYLINDER. R&R PER E.A. 7-3210-60399. 2 L 7 3 4F RT A3WE 2001121200003 20011212 00003 NM 2001 12 12 01FDEA01062 1 20011209 A 5350 BRACKET BOEING 727 727277 138408S NM FUSELAGE LOWER CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 N 311 SUPPORT BRACKET CRACKED FOR FUSELAGE FAIRING BS 720E, STR 28L. ** S/D ** COMING 2 L 7 3 4F RT A3WE 2001121200004 20011212 00004 NM 2001 12 12 01FDEA01063 1 20011209 A 5330 SKIN BOEING 727 727277 138408S NM FUSELAGE LOWER CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 N 87 CORROSION & CRACK IN LOWER SKIN AT BS 727C, STR 27R. R&R SKIN PER SRM 53-30-3 & STR PER SRM 53-10-3. 2 L 7 3 4F RT A3WE 2001121200005 20011212 00005 CE 2001 12 12 CA011003008 1 20010821 A 2750 BZ7RW82255518T SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE TE FLAPS FAILED W O OTHER J WARNING INDICATION DE DESCENT 1 CA (CAN) DURING DESCEND IN PREPARATION FOR LANDING FLIGHT CREW SELECTED FLAPS DOWN TO 17 DEGREES. THE FLAPS DID NOT OPERATE AND THE SELECTOR WAS RETURNED TO ZERO. CREW LANDED AIRCRAFT WITH ZERO FLAPS. MAINTENANCE DISCOVERED THE R/H SPLIT FLAP SAFETY SWITCH FAILED DISABLING POWER TO THE FLAP MOTOR. SPLIT FLAP SWITCH REPLACED AND FLAP OPERATION CHECKED OKAY. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2001121200006 20011212 00006 EA 2001 12 12 CA011005010 1 20010920 A 2611 473052 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CARGO BAY FAILED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA (CAN) PILOT REPORT "SMOKE CARGO" INDICATION IN FLIGHT. MAINTENANCE REMOVED AND REPLACED SMOKE DETECTOR AND AIRCRAFT BAC K IN SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2001121200007 20011212 00007 EA 2001 12 12 CA011005012 1 20010920 A 2913 M832481039 PACKING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT HYD PAD BROKEN W E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 CA (CAN) PILOT REPORT LT ENGINE IN FLIGHT SHUT DOWN WAS CARRIED OUT AS A PRECAUTIONARY MEASURE. MAINTENANCE FOUND PACKING ON HYDRAULIC PAD BROKEN. PACKING REMOVED AND REPLACED.AIRCRAFT BACK IN SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2001121200008 20011212 00008 EA 2001 12 12 CA011101007 1 20011012 A 5610 NP1393215 WINDSHIELD CNDAIR CL6002B19 CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED W K NONE O OTHER CR CRUISE 1 CA (CAN) LT SIDE WINDOW CRACKED 35 CM. THE DETAILED INSPECTION SHOWED CRACKS IN THE INNER PLY IN THE LOWER PART OF THE WIND OW. REMOVED AND REPLACED THE WINDOW. 2 L 7 2 4F 4 F RT A21EA E15NE 2001121200009 20011212 00009 EA 2001 12 12 CA011101014 1 20011019 A 5610 NP1393221 WINDOW PPG CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE COCKPIT CRACKED W O OTHER D INFLIGHT SEPARATION CR CRUISE 1 CA 14536 95115H6950 (CAN) LT SIDE WINDOW SHATTERED IN CRUISE AT 29,000 FT. LT SIDE WINDOW REMOVED AND REPLACED. AIRCRAFT BACK IN SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2001121200010 20011212 00010 EA 2001 12 12 CA011101017 1 20011017 A 5610 NP1393215 WINDSHIELD PPG CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED W O OTHER O OTHER CR CRUISE 1 CA 00035H9058 (CAN) PILOT REPORT DURING FLIGHT LT WINDSHIELD INNER PLY CRACKED. PILOT CARRIED OUT THEIR QRH. MAINTENANCE REMOVED AND R EPLACED LT COCKPIT WINDOW.AIRCRAFT BACK IN SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2001121200012 20011212 00012 NE 2001 12 12 CA011119003 2 20011107 A 7200 ENGINE PWA JT8D15A BOEING 727 727260 NM PWA JT8 JT8D15 52051 NE NR 3 FAILED W E ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION DE DESCENT 1 CA 687342 (CAN) ON DESCENT, THRUST AT IDLE, NR 3 START LEVER VIBRATED IN DETENT. NR 3 EGT 100 DEGREES HIGHER THAN ENGINES NR 1 AND 2. "WHINING NOISE" AND VIBRATION FELT IN FLOOR WHEN THRUST LEVER ADVANCED. ENGINE SHUT DOWN IN FLIGHT. BORESCOPE INSP ECTION CARRIED OUT ON AFFECTED ENGINE. ENGINE REJECTED, REMOVED FROM SERVICE AND ROUTED TO REPAIR FACILITY. AWAITING S HOP EVALUATION. 2 L 7 3 4F 4 F RT A3WE E2EA 2001121200013 20011212 00013 EA 2001 12 12 CA011122004 1 20011109 A 5610 NP1393215 WINDSHIELD PPG NP1393215 CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED W O OTHER O OTHER CR CRUISE 1 CA 99054H1089 (CAN) DURNG CRUISE AT FL260, DELTA P 7.8 PSI, THE LT WINDSHIELD OUT PLY CRACKED. THE FLIGHT WAS COMPLETED UNEVENTFULLY A ND THE WINDSHIELD WAS REPLACED IN MUNICH. AIRCRAFT RETURNED IN SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2001121200014 20011212 00014 SO 2001 12 12 00050 1 20011129 A 3610 GASKET EMB 145 EMB145 3260210 SO BLEED AIR SYS LEAKING A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 276SK 145348 RT ENGINE ITT 50 DEGREES HOTTER THAN LT ITT. INSPECTED AIRCRAFT NR 2 ENG, PERFORMED BORESCOPE OF COMPRESSOR TURBINE SEC TION HOT SECTION WITHIN LIMITS. PERFORMED LEAK CHECK OF BLEED LINE, FOUND LEAKS AND REPLACED GASKETS. ALL CHECK GOOD A T THIS TIME. 2 L 7 2 4F RT T00011AT 2001121200015 20011212 00015 NM 2001 12 12 SWAA013295 1 20011209 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 737JW 27869 EEPLS COVER LOOSE AT FWD CABIN. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2001121200016 20011212 00016 2001 12 12 SWAA013296 4 20011210 A 2565 6949956 CABLE BOEING 737 7373A4 1384585 NM AFT ENTRY DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINING CABLE IMPROPERLY ROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2001121200017 20011212 00017 2001 12 12 SWAA013299 4 20011210 A 2565 1061323 SLIDE BOEING 737 7373Q8 1384670 NM FWD ENTRY DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 317WN 24068 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED AT THE GATE. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001121200018 20011212 00018 NM 2001 12 12 SWAA013300 1 20011207 A 5313 6547978 WEB BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 357, STR 16L. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001121200019 20011212 00019 NM 2001 12 12 SWAA013302 1 20011210 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 15L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001121200020 20011212 00020 WP 2001 12 12 0104319750 1 20010907 A 5310 DOOR FRAME DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 750NW 47114 DURING RON IN CMH A CRACK WAS NOTED IN THE APB VENTRAL DOOR JAMB PAN. THE CRACK WAS LOCATED 52.25 INCHES FROM THE FLOOR LINE ON THE LT BY THE ROLLER ASSEMBLY. REPAIRED PER 97-185133. 2 L 7 2 4F A6WE 2001121200021 20011212 00021 WP 2001 12 12 0104389989 1 20010628 A 5315 FLOORBEAM DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8945E 47181 DURING H-CK AT ATL BASE MTC, THE UPPER CAP OF THE STATION 200 FLOORBEAM T-CAP WAS FOUND WITH A CRACK AT X=44 RT. REPAIRE D PER EA 99-181292. 2 L 7 2 4F A6WE 2001121200022 20011212 00022 WP 2001 12 12 0104579858 1 20011119 A 2450 976J2544 CONTROL PANEL DOUG DC9 DC951 3022051 WP COCKPIT MALFUNCTIONED A NWAA C ABORTED TAKEOFF J H WARNING INDICATION ELECT. POWER LOSS-50 PC TO TAKEOFF 1 GL 01 767NC 47724 CREW NOTICED THE LEFT GENERATOR OFF ANNUNCIATOR DURING TAKEOFF ROLL. ABORTED TAKEOFF AT APPROXIMATELY 120 KTS. THE LEF T GENERATOR INDICATED NO VOLTAGE FREQUENCY AND NO LOAD. MAINTENANCE INSPECTED THE LEFT GENERATOR SYSTEM AND FOUND NO FA ULTS BUT REPLACED THE GENERATOR CONTROL PANEL AS A PRECAUTION. OPERATIONAL CHECK GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2001121200023 20011212 00023 2001 12 12 0104589902 4 20011129 A 3414 8020081104 INDICATOR DOUG DC9 DC931 3022065 WP COCKPIT READS HIGH A NWAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 01 952N 47073 DURING TAKEOFF ROLL, THE CAPTAIN NOTICED A DISCREPANT READING BETWEEN HIS AND FIRST OFFICER'S AIRSPEED INDICATORS. NR 1 WAS INDICATING 110 KTS AND NR 2 INDICATED 80 KTS. THE TAKEOFF WAS ABORTED SAFELY AND THE AIRCRAFT RETURNED TO THE GATE . MAINTENANCE REPLACED THE NR 1 AIRSPEED INDICATOR AFTER CHECKING THAT ALL LINES AND CONNECTIONS WERE SECURE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001121200024 20011212 00024 WP 2001 12 12 0104609853 1 20011128 A 2120 DUCT DOUG DC9 DC951 3022051 WP A/C BAY SEPARATED A NWAA B A EMER. DESCENT UNSCHED LANDING O OTHER CR CRUISE 1 GL 01 762NC 47710 WHILE EN ROUTE AT 33,000 FT WITH CABIN PRESSURIZATION OPERATING IN MANUAL MODE, THE CREW HAD DIFFICULTIES MAINTAINING CA BIN ALTITUDE WITHOUT OPERATING THE LEFT PACK AT FULL HOT. THE PACK'S OVERTEMP PROTECTION TRIPPED AND CREW LOST CONTROL OF PRESSURIZATION. THE CABIN CLIMBED TO 10,000 FT. PERFORMED COM PROCEDURE AND THE CREW MADE AN EMERGENCY DESCENT TO 1 0,000 FT. FLIGHT DIVERTED TO MEM AND LANDED SAFELY. MAINTENANCE FOUND A 4 INCH DUCT ON THE FORWARD SIDE OF THE ACM AND 1.25 INCH DUCT ON THE AFT SIDE OF THE ACM SEPARATED. RE-ATTACHED THE DUCTS, REPLACED THE CLAMPS, AND RETURNED THE AIRC RAFT TO SERVICE. 2 L 7 2 4F RT A6WE 2001121200025 20011212 00025 WP 2001 12 12 0104661227 1 20011121 A 3230 ACTUATOR DOUG DC10 DC1030 3023501 WP LANDING GEAR MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 227 46969 AFTER TAKEOFF, GEAR HANDLE COULD NOT BE MOVED TO RETRACT POSITION. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE BLED TRIM ACTUATOR AND TRIM POSITION CYLINDER. OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 2001121200026 20011212 00026 EA 2001 12 12 COMA0160953 1 20011208 A 5320 POST CNDAIR CL600 CL6002B19 1900309 EA FS409+128 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 927CA 18312 7031 THE OUTBOARD LOWER POST AT RBL 18.0, FS 409+128 WAS CRACKED.REPAIRED THE CRACKED POST BY TRIMMING OUT THE DAMAGED AREA A ND INSTALLING A REPAIR ANGLE I/A/W WVAC EO 601R-53-2874. 2 L 7 2 4F RT A21EA 2001121200027 20011212 00027 EA 2001 12 12 COMA0160954 1 20011208 A 5330 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FS484 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 947CA 14520 7077 ANGLE CRACKED F.S. 484, RBL27, INBOARD SIDE, W.L. 73.0. FLANGE OF INTERCOSTAL CRACKED F.S. 484, RBL 36, OUTBD SIDE, W.L. 73.REPAIRED THE F.S. 484, RBL27 AND RBL36 I/A/W WVAC EO 601R-53-2863. 2 L 7 2 4F RT A21EA 2001121200028 20011212 00028 EA 2001 12 12 COMA0160955 1 20011208 A 5330 FITTING CNDAIR CL600 CL6002B19 1900309 EA FS460 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 947CA 14520 7077 MACHINED FITTING CRACKED F.S. 460, LBL9, OUTSIDE W.L. 73.0REPAIRED F.S. 460 LBL 9 I/A/W WVAC E.O. 601R-53-2862. 2 L 7 2 4F RT A21EA 2001121200029 20011212 00029 NM 2001 12 12 2001UALA02353 1 20011130 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 611UA 21872 STRINGER 30L AT BODY STATION 470, STRINGER SPLICE REQUIRES REPLACEMENT REF CF9059. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED PERMANENT STRINGER REPAIR SPLICE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001121800029 20011218 00029 NM 2001 12 18 2001UALA02357 1 20011123 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 175UA 24382 THE RIGHT HAND EXTERIOR SKIN WAS PUNCTURED JUST AFT OF DOOR 5R. BODY STATION 2290, NEAR STRINGER 21R. MAJOR REPAIR ACCO MPLISHED, A DOUBLER REPAIR WAS INSTALLED. 2 L 7 4 4F 4 F RT A20WE E24NE 2001121200030 20011212 00030 NM 2001 12 12 2001UALA02360 1 20011204 A 5311 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 AFT PIT FRAME AT STATION 1520, FRAME SPLICE HAS 3 AREAS OF DAMAGE FROM SIDEWALL PANEL SCREWS-SCREWS GOUGED INTO FRAME SP LICE STRINGER 24R. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPLACED SPLICE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001121200031 20011212 00031 NM 2001 12 12 2001UALA02373 1 20011206 A 5330 SKIN BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 602UA 21863 FUSE SKIN CRACKED AT STATION 1654 BETWEEN STRINGER 4R TO 5R. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALL ED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A1NM E3NE 2001121200032 20011212 00032 NM 2001 12 12 2001UALA02376 1 20011205 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 CABIN STATION 725 RBL 63 AFT EDGE OF DR 2R FLOOR SUPPORT IS CORRODED AT TOP SURFACE. MAJOR REPAIR ACCOMPLISHED. REPLACE D CHANNEL. 2 L 7 2 4F 4 F RT A2NM E17NE 2001121800050 20011218 00050 NM 2001 12 18 2001UALA02382 1 20011207 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 FRAME CRACKED STATION 1862, RBL 5. REPAIR ACCOMPLISHED, INSTALLED ANGLE DOUBLERS. 2 L 7 2 4F 4 F RT A2NM E17NE 2001121200033 20011212 00033 EA 2001 12 12 COMA0160956 1 20011208 A 5346 60135006 BEAM CNDAIR CL600 CL6002B19 1900309 EA AFT EQUIP BAY CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 958CA 13810 7111 ENGINE SUPPORT BEAM CRACK.REPAIRED DAMAGE IN ACCORDANCE WITH CANADAIRE REO 601-53-61-345. 2 L 7 2 4F RT A21EA 2001121200034 20011212 00034 2001 12 12 0125 4 20011127 A 3160 6227236001 DISPLAY BRAERO DH125 BAE125800A 1500285 EU COCKPIT MALFUNCTIONED E DJFA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 816CW 258016 AIRCRAFT WAS EN ROUTE TO BED, EXPERIENCED SMOKE IN THE COCKPIT. DECLARED AN EMERGENCY AND LANDED AT CHS. FOUND THE MFD AS THE PROBLEM. 2 L 7 2 4F RT A3EU 2001121200035 20011212 00035 EA 2001 12 12 COMA0160957 1 20011208 A 5346 6013500 BEAM CNDAIR CL600 CL6002B19 1900309 EA AFT EQUP BAY CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 958CA 13810 7111 ENGINE SUPPORT BEAM CRACKED.REPAIRED DAMAGE I/A/W CANADAIR REO 601R-53-61-366. 2 L 7 2 4F RT A21EA 2001121200042 20011212 00042 NM 2001 12 12 01FDEA01010 1 20011121 A 5311 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 285FE 22622 DENT IN FRAME UPPER FLANGE AT BS 1050, STR 26R. REMOVED AND REPLACED FRAME PER SRM 51-40-3, 51-30-2 & EA 7-5310-62617. 2 L 7 3 4F RT A3WE 2001121200044 20011212 00044 NM 2001 12 12 01FDEA01012 1 20011128 A 2613 OVERHEAT LOOP BOEING 727 727227 1384078 NM NR 1 ENGINE OUT OF POSITION A FDEA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CL CLIMB 1 SO 25 492FE 21530 DURING CLIMBOUT NR 1 ENG STRUT OVERHEAT LIGHT ILLUM. NO LEAKS FOUND WITH ENG. REPOSITIONED OVERHEAT LOOP. 2 L 7 3 4F A3WE 2001121200045 20011212 00045 2001 12 12 01FDEA01013 4 20011129 A 3442 RECEIVER BOEING 727 72722 1384002 NM WEATHER RADAR FAULTY A FDEA A UNSCHED LANDING O OTHER UK UNKNOWN 1 SO 25 149FE 19087 RADAR INTERMITTENT GIVES GOOD PRESENTATION THEN GETS DISTORTED. REMOVED AND REPLACED WEATHER RADAR RECEIVER/ TRANSMITTE R AND COLOR IND PER MM 34-41-041-4. 2 L 7 3 4F A3WE 2001121200046 20011212 00046 WP 2001 12 12 01FDEA01014 1 20011129 A 5320 SUPPORT DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 VERTICAL SUPPORT AT BS 495, X=73 HAS CRACK. 2 L 7 3 4F RT A22WE 2002010900061 20020109 00061 WP 2002 1 9 01FDEA01015 1 20011129 A 5320 FLOOR SUPPORT DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 VERTICAL SUPPORT AT BS 555, X=71 HAS CRACK. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-31-01, 51-00-00, 51-21-01. 2 L 7 3 4F RT A22WE 2002010900062 20020109 00062 WP 2002 1 9 01FDEA01016 1 20011129 A 5320 FLOOR SUPPORT DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 VERTICAL SUPPORT AT BS 575, X=73 HAS A CRACK. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-31-01, 51-00-00, 51-21-01. 2 L 7 3 4F RT A22WE 2001121200047 20011212 00047 WP 2001 12 12 01FDEA01018 1 20011201 A 2450 CIRCUIT BREAKER DOUG DC10 DC1010F 3022111 WP COCKPIT LACK OF LUBE A FDEA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 SO 25 052FE 47806 NR 1 BUS LOST AT ROTATION. RESET NR 1 BUS, LUBRICATED C/B. OK FOR SERVICE. 2 L 7 3 4F A22WE 2001121200048 20011212 00048 WP 2001 12 12 01FDEA01019 1 20011203 A 2450 CONTROL UNIT DOUG DC10 DC1010CF 3023502 WP ELECTRICAL SYS FAILED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 052FE 48291 ON T/O ROLL, NR 1 BUS FAILED. REMOVED AND REPLACED GENERATOR RELAY 1, BUS CONTROL AND CIRCUIT BREAKER PER MM 24-00-00-2 . 2 L 7 3 4F RT A22WE 2001121200049 20011212 00049 EU 2001 12 12 01FDEA01020 1 20011130 A 3610 SEAL AIRBUS 300 A300F4605R 3930327 EU BLEED AIR LEAKING A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 652FE 735 BLEED VALVE 1 LEAK ON CLIMBOUT. REMOVED AND REPLACED SEAL DUCT EXPANSION JOINT AT FR 39. 2 L 7 2 4F RT A35EU 2001121200050 20011212 00050 WP 2001 12 12 01FDEA01022 1 20011201 A 2780 ARH7024617 CONTROL CABLE DOUG DC10 DC1010F 3022111 WP L/E SLAT BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 398FE 46634 NR 7 RIGHT SLAT RETRACT CABLE HAS BROKEN STRANDS. REMOVED AND REPLACED CABLE AND CONTROL PULLEY PER MM 27-89-13, 27-80- 00. 2 L 7 3 4F A22WE 2001123100006 20011231 00006 NM 2001 12 31 01FDEA01026 1 20011204 A 5320 ANGLE BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 285FE 22622 CORROSION (C53-224-01, 1) UNDER MOPSILL AROUND FWD DRAIN FITTING BS 310, LBL 54, WL 208. REMOVED AND REPLACED MOPSILL R EINFORCEMENT ANGLE BS 274 - 312 LBL 54 WL 208 PER SRM 51-3-2. 2 L 7 3 4F RT A3WE 2001121200052 20011212 00052 WP 2001 12 12 01FDEA01029 1 20011204 A 2751 WARNING LIGHT DOUG DC10 DC1010 3022110 WP COCKPIT FALSE INDICATION A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 385FE 46619 DURING CLIMBOUT AFTER FLAPS/SLAT HANDLE RAISED, DISAGREE LIGHT ILLUMINATED. INSPECTED SLATS/FLAPS, NO DEFECTS FOUND. O K FOR SERVICE. 2 L 7 3 4F A22WE 2001121200053 20011212 00053 WP 2001 12 12 01FDEA01030 1 20011107 A 5320 STANCHION DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 303FE 48802 AFT FUSELAGE BS 1967, STR 50R CORRODED STANCHION SUPPORT. REMOVED AND REPLACED STANCHION PER SRM 51-35-01. 2 L 7 3 4F RT A22WE 2001121200054 20011212 00054 WP 2001 12 12 01FDEA01031 1 20011121 A 5347 SEAT TRACK DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 CORRODED SEAT TRACK AT X=108.00 Z=-19.00 BS 1539-1553. REMOVED AND REPLACED SEAT TRACK PER SRM 53-70-00. 2 L 7 3 4F RT A22WE 2001121200055 20011212 00055 WP 2001 12 12 01FDEA01032 1 20011126 A 5320 CHANNEL DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 FWD CARGO BS 939 X=-99 Z=30 CEILING SUPPORT CHANNEL CRACKED. REMOVED AND REPLACED CHANNEL AND BRACKETS PER SRM 51-10-01 & 51-35-01. 2 L 7 3 4F RT A22WE 2001121200056 20011212 00056 EU 2001 12 12 CHQ00051 1 20011130 A 7930 CHIP DETECTOR SAAB SF340 SF340A 7850100 EU RT ENGINE DIRTY A CHQA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 GL 11 CHQA 149 RIGHT ENGINE CHIP DETECTOR LIGHT CAME ON. CLEANED CHIP DETECTOR, INSPECTED AND GROUND RAN ALL WITHIN LIMITS. 2 L 7 2 4T RT A52EU 2001121200057 20011212 00057 SO 2001 12 12 CHQ00052 1 20011202 A 2131 CONTROLLER EMB 135 EMB135LR 3260305 SO CABIN PRESSURE MALFUNCTIONED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 CHQA 145535 PRESSURIZATION INDICATION PROBLEMS. CABIN ALTITUDE AND CABIN RATE OF CLIMB SHOWING YELLOW DASHES. POWERED DOWN A/C. 2 L 7 2 4F RT TOOO11AT 2001121200058 20011212 00058 EU 2001 12 12 CHQ00055 1 20011203 A 3150 CONTROL UNIT SAAB SF340 SF340A 7850100 EU WARNING SYSTEM MALFUNCTIONED A CHQA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 11 CHQA 125 ON TAKEOFF CONFIG WARNING. REMOVED AND REPLACED WEU, GROUND RAN OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2001121200059 20011212 00059 EU 2001 12 12 CHQ00056 1 20011203 A 5270 WARNING LIGHT SAAB SF340 SF340A 7850100 EU COCKPIT ACTIVATED A CHQA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 CHQA 006 CARGO DOOR LIGHT ILLUMINATED. DEFERRED. 2 L 7 2 4T RT A52EU 2001121200060 20011212 00060 SO 2001 12 12 CHQ00058 1 20011205 A 2612 FIRE LOOP EMB 145 EMB145LR 3260212 SO NR1 ENGINE FAULTY A CHQA K NONE N FALSE WARNING UK UNKNOWN 1 GL 11 CHQA 145199 E1 FIRE DETECT FAIL ON EICAS. REMOVED AND REPLACED E1 FIRE DET LOOP AND OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2001121200061 20011212 00061 SO 2001 12 12 CHQ00060 1 20011209 A 2750 LEVER EMB 145 EMB145LR 3260212 SO FLAP DAMAGED A CHQA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 CHQA 145522 LANDING GEAR AIR GROUND FAIL WITH AURAL WARNING. REPAIRED FLAP LEVER ASSEMBLY. 2 L 7 2 4T RT T00011AT 2001121200062 20011212 00062 2001 12 12 SWAA013279 4 20011208 A 2565 31354 SLIDE BOEING 737 7373T5 1384608 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001121200063 20011212 00063 NM 2001 12 12 SWAA013282 1 20011207 A 5310 6545813 DOOR FRAME BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR CUTOUT AFT FRAME WEB CRACKED AT UPPER DOOR STOP FITTING. REPAIRED FRAME PER SWARA. 2 L 7 2 4F A16WE 2001121200064 20011212 00064 NM 2001 12 12 SWAA013284 1 20011208 A 3350 BR2013 LIGHT BOEING 737 7373Y0 1384671 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED C3 CHECK, FOUND EEPLS LOOSE IN FWD CABIN. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001121200065 20011212 00065 NM 2001 12 12 SWAA013286 1 20011208 A 3350 300432 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 704SW 27838 DURING SCHEDULED C2 CHECK, FOUND LT EXTERNAL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2001121200066 20011212 00066 NM 2001 12 12 SWAA013287 1 20011209 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 601WN 27695 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, RBL 5.7 AND WL 203, LBL 5.7 AND WL 199. RE PAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001121200067 20011212 00067 2001 12 12 SWAA013288 4 20011208 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 386SW 26601 DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001121200068 20011212 00068 NM 2001 12 12 01FDEA01033 1 20011206 A 3242 BRAKE BOEING 727 7272S2F 1384O81 NM MLG OVERHEATED A FDEA O OTHER M OVER TEMP TX TAXI/GRND HDL 1 SO 25 210FE 22932 NR 3 MAIN WHEEL AND BRAKE HOT AND LONG ROLL OUT. REMOVED AND REPLACED NR 2 MAIN TIRE AND BRAKE PER MM 32-45-01 & 32-41- 032-4. 2 L 7 3 4F A3WE 2001122000010 20011220 00010 NM 2001 12 20 01FDEA01034 1 20011205 A 5311 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 285FE 22622 DENT IN UPPER FLANGE OF FRAME BS 970 AT STR 26L. REMOVED AND REPLACED FRAME PER SRM 51-40-3 & EA 7-5310-62617. 2 L 7 3 4F RT A3WE 2001121200071 20011212 00071 WP 2001 12 12 01FDEA01039 1 20011207 A 5313 LONGERON DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 303FE 46802 CORRODED LONGERON 18 LEFT AT BS 1215. REMOVED AND REPLACED LONGERON PER SRM 53-10-00. 2 L 7 3 4F RT A22WE 2001121200072 20011212 00072 WP 2001 12 12 01FDEA01064 1 20011212 A 2131 CONTROLLER DOUG DC10 DC1010 3022110 WP CABIN PRESSURE MALFUNCTIONED A FDEA O OTHER O OTHER CL CLIMB 1 SO 25 371FE 46609 AT CLIMB CABIN PRESS EXCEEDED 10,000. AC RELEASE PER MEL AUTO AND SEMI AUTO CABIN ALTITUDE CONTROL SYSTEM INOP. 2 L 7 3 4F A22WE 2001121200073 20011212 00073 2001 12 12 01FDEA01065 4 20011212 A 3417 HG480B13 ADC BOEING 727 7272S2F 1384O81 NM E/E BAY FAULTY A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 210FE 22932 ON ROTATION AIR DATA COMPUTER NR 2 C/B POPPED SEVERAL TIMES. REMOVED AND REPLACED CADC PER MM 34-12-011-4. 2 L 7 3 4F A3WE 2001121200074 20011212 00074 NE 2001 12 12 CHQ00063 2 20011210 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LEFT FLUCTUATES A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 CHQA 006 ABORTED TAKEOFF FOR LT ENGINE TORQUE FLUX. GROUND RAN A/C, NO DEFECTS NOTED. 2 L 7 2 4T 4 T RT A52EU E8NE6 2001121200075 20011212 00075 2001 12 12 SWAA013294 4 20011209 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 362SW 26573 DURING SCHEDULED BC1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001121200076 20011212 00076 NM 2001 12 12 SWAA013297 1 20011210 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 394SW 27380 EEPLS IS LOOSE AND WIRES EXPOSED AT ROW 15. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2001121200077 20011212 00077 2001 12 12 SWAA013298 4 20011210 A 2565 1061323 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 365SW 26576 FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001121200078 20011212 00078 NM 2001 12 12 SWAA013301 1 20011210 A 5320 51696 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 10R. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2001121200079 20011212 00079 2001 12 12 SWAA013303 4 20011207 A 3422 25883024 GYRO BOEING 737 7372H4 138448C NM E/E BAY FAILED A SWAA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 SW 29 073SW 22673 (AIR TURNBACK) COMPASS FLAG ON CAPT HSI AND F/O RMDI DISPLAYED. REMOVED AND REPLACED NR 2 DG AND NR 2 COMPASS RACK. 2 L 7 2 4F A16WE 2001121200080 20011212 00080 2001 12 12 GMA2001F00001 4 20011015 A 2297 WIRE LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP AUTOPILOT SYS BROKEN A GMAL K NONE O OTHER IN INSP/MAINT 1 NM 09 873LP 5406 659 IN SERVICE OF WIRE BUNDLE CAUSED THE SHIELDING TO BREAK, AND A WIRE TO BREAK AT THE AIRFRAME-TO-WIRE BUNDLE CLAMP. SERV ICE LOOP DID NOT APPEAR TO BE OF SUFFICIENT SIZE TO ALLOW FOR THE NEEDED FLEXING OF THE WIRE BUNDLE. FORCE SENSOR DID N OT FUNCTION. 2 L 7 2 4F 4 F A10CE E6WE 2001121200081 20011212 00081 SW 2001 12 12 MV52001F00001 1 20011019 A 5330 31041725 SKIN GULSTM 690TP 690B 7630516 SW GARRTT TPE331 TPE331* 01514 WP FUSELAGE CRACKED B MV5R K NONE O OTHER IN INSP/MAINT 1 GL 11 771BA 7563 11429 UPPER FUSELAGE SKIN CRACKED AT COMM ANTENNA MOUNTING BASE LOCATED AT STATION 210, FIVE INCHES LEFT OF AIRCRAFT CENTERLIN E. ANTENNA INSTALLATION WAS ORIGINAL FROM AIRCRAFT MANUFACTURE. CRACK ATTRIBUTED TO INSUFFICIENT METAL THICKNESS TO BO TH OUTER SKIN OF .025 AND MOUNTING DOUBLER OF .032. 1 H 7 2 3T 3 T 2A4 E2WE 2001121200082 20011212 00082 NE 2001 12 12 PI22001F00001 2 20010421 A 7230 CASE BOEING 757 757200 1384950 NM RROYCE RB211 RB211535C37 54555 NE COMPRESSOR CRACKED B PI2R K NONE O OTHER IN INSP/MAINT 1 CE 07 GBIKJ 30632 22181 30045 ON INSPECTING THE EXTERIOR OF THE AREA OF CONCERN, THE FOLLOWING ITEMS WERE FOUND. THERE ARE MULTIPLE CRACKS IN THE CIR CUMFERENTIAL DIRECTION TOTALING 60 INCHES. 2 L 7 2 4F 4 F RT A2NM E12EU 2001121200083 20011212 00083 SO 2001 12 12 QU22001F00000 1 20010726 A 3246 AH55031 HEAT SHIELD GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU LT MLG CONTAMINATED B QU2R O OTHER A FLAME/FIRE NR NOT REPORTED 1 EA 17 777SA 1081 AC HAD POSSIBLE BRAKE FIRE AT LEFT OB WHEEL/BRAKE ASSY AREA. FOUND AREA ON IB SIDEWALL OF TIRE, SHOWED EVIDENCE OF FIRE , RUBBER WAS CHARRED IN AREA FROM WHEEL RIM AND OUT TO TREAD AREA ABOUT 3 INCHES IN LENGTH, 1.5 INCHES WIDE LIKE A WATER TEAR DROP. OPERATOR NOTIFIED AND PROVIDED WITH BUILT UP WHEEL AND TIRE ASSY. THE MFG SAID CAUSE WAS WHEN WHEEL ASSY W AS CLEANED FOR INSP WHOLE WHEEL ASSY WAS SUBMERGED IN CLEANING FLUID. THIS ALLOWED LAMINATED HEAT SHIELD TO COLLECT CLE ANING FLUID. WHEN UNIT WAS NEXT INSTALLED ON AC THE HEAT FROM THE BRAKES DRIED OUT THE LAM SHIELD, AFTER NR OF LANDINGS , ALLOWING HOT BRAKE TO IGNITE LAM HT SHIELD. INSTALLED A REPLACEMENT ASSY. DEFECTIVE WHEEL ASSY WAS RETURNED TO OPER. 2 L 7 2 4F 4 F RT A12EA E25NE 2001121200084 20011212 00084 SO 2001 12 12 SIM2001F00000 1 20010830 A 2730 14524986005 BUSHING EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CONTROL QUADRANT WORN A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 643AE 145200 BUSHINGS ARE MIGRATING CAUSING EXCESSIVE WEAR TO ELEVATOR CONTROL QUADRANT SUPPORT FITTINGS. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2001121200085 20011212 00085 CE 2001 12 12 TIM2001F00008 1 20010906 A 2121 1143800285 MOTOR BEECH 1900 1900C 1154161 CE PWA PT6 PT6* 52043 EA AIR DISTRIBUTION SHORTED E TIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 153GA UB34 AIRCRAFT FILLED WITH SMOKE, CREW MADE AN EMERGENCY LANDING. CHECK OF AIRCRAFT SYSTEMS FOUND THE FORWARD EVAPORATOR MOTO R SHORTED. AIRCRAFT WAS FURTHER INSPECTED FOR DAMAGE, NONE FOUND. 2 L 7 2 4T 3 T RT A24CE E2NE 2001121200086 20011212 00086 SW 2001 12 12 UNF2001F00000 1 20011105 A 5320 222031831101 BOLT BELL 222 222 1182122 SW LYC LTS101 LTS101600A 41560 NE STUB WING ATTACH WORN A UNFR K NONE O OTHER IN INSP/MAINT 1 SW 19 29KH 3417 47053 FOUND METAL TO METAL FRETTING WEAR AND MAKING MUD ON BOTTOM SIDE OF WING (222-031-800-101). BOLTS LOOSE ENOUGH TO ALLOW LOWER SKIN ON WING TO CAUSE SEVERE CHAFING DAMAGE BETWEEN LOWER WING SKINS (222-030-812-135/812-136) AND FUSELAGE STRUC TURAL SKINS (222-030-466-105/107) AND (222-031-464-115/116). LOWER WING SKIN WORE COMPLETELY THROUGH FUSELAGE STRUCTUR AL SKINS. SKINS WERE REPLACED WITH NEW SKINS AND LOWER WINGLET SKINS WERE TRIMMED BACK TO PREVENT FUTURE DAMAGE TO FUS ELAGE SKINS. DAMAGED BOLTS WERE REPLACED WITH NO KNOWN WEAR LIMITS. MFG S.B. WAS COMPLIED WITH ADDING A THICKER WASHER TO BOLTS TO AID IN TORQUE RETENTION OF WING ATTACHMENT BOLTS. AC WAS RETURNED TO SERVICE 1 G 7 2 3U 3 U H9SW E5NE 2001121200087 20011212 00087 SO 2001 12 12 VJ32001F00010 2 20011109 A 7414 DISTRIBUTOR BLK SLICK BEECH 33 F33A 1151425 CE CONT O520 IO520B 17032 SO MAGNETO FAILED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 5582X 890 00030786 CE1353 MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW THE MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM M AGNETO. DISTRIBUTOR BLOCK ASSEMBLY SENT TO MFG FOR INSPECTION. NEW DISTRIBUTOR BLOCK ASSEMBLY INSTALLED IN MAGNETO.(K) 1 L 7 1 3O 3 O 3A15 E5CE 2001121200088 20011212 00088 SO 2001 12 12 VJ32001F00011 2 20011109 A 7414 DISTRIBUTOR BLK SLICK BEECH 33 F33A 1151425 CE CONT O520 IO520B 17032 SO MAGENTO FAILED E VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 5582X 890 00030943 CE1353 820397R MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNE TO. DISTRIBUTOR BLOCK ASSEMBLY INSTALLED IN MAGNETO. (K) 1 L 7 1 3O 3 O 3A15 E5CE 2001121200089 20011212 00089 SO 2001 12 12 WVB2001F00000 1 20011126 A 3245 0923150 TUBE PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA NLG TIRE DAMAGED E WVBA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 AL 01 3582P 30 318052103 PILOT TAXIED OUT TO RUNWAY AND REPORTED NOSE TIRE WENT FLAT AIRCRAFT WAS RECOVERED. AFTER INSTALLING NEW WHEEL ASSEMBL Y IT WAS FOUND THAT THE TUBE HAD A HOLE IN THE CENTER. THIS IS THE THIRD INCIDENT WITH THIS TUBE MANUFACTURER. SUSPECT THE MATERIAL, A BUTYL RUBBER, A FACTOR WHEN COMBINED WITH LOW WINTER TEMPERATURES.(K) 1 L 7 2 3O 3 O A20SO E14EA 2001121200090 20011212 00090 EA 2001 12 12 WVB2001F00001 2 20011029 A 7314 62E22581 PUMP PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA RT ENGINE LEAKING E WVBA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 01 3582P 353 318052103 DURING INSPECTION IT WAS NOTICED THAT THE RIGHT FUEL PUMP WAS LEAKING AT THE BODY GASKET THE PUMP WAS REMOVED FROM SERVI CE. THIS IS A M STYLE PUMP.(K) 1 L 7 2 3O 3 O A20SO E14EA 2001121200099 20011212 00099 SO 2001 12 12 BTH2001F00002 1 20011129 A 5720 6676101 FITTING PIPER PA32 PA32R300 7103213 SO LYC O540 TIO540* 41532 EA WING FRETTED A BTHA K NONE O OTHER IN INSP/MAINT 1 AL 01 75387 15370 32R7680298 DISCOVERED DURING 100 HOUR INSPECTION NOTED MOVEMENT OF WING AT FORWARD WING ATTACH FITTING WHEN WING WAS PUSHED FROM BO TTOM OR TOP. 1 L 7 1 3O 3 O A3SO E14EA 2001121200100 20011212 00100 2001 12 12 CL92001F00000 4 20011128 A 6113 05503671 SPINNER CESSNA 172 172S 2072439 CE LYC O360 IO360A1A 41514 EA PROPELLER CRACKED A CL9T K NONE O OTHER IN INSP/MAINT 1 WP 01 586SP 832 172S8516 DURING PHASE INSPECTION FOUND SPINNER DOME CRACKED AT BLADE CUT OUT, REPLACED SPINNER DOME. 1 H 7 1 3O 3 O NT 3A12 1E10 2001121200101 20011212 00101 2001 12 12 CL92001F00001 4 20011128 A 6113 05503671 SPINNER CESSNA 172 172S 2072439 CE PROPELLER CRACKED A CL9T K NONE O OTHER IN INSP/MAINT 1 WP 01 851SP 513 172S8759 DURING PREFLIGHT, PILOT FOUND SPINNER DOME CRACKED AT BLADE CUT OUT, REPLACED SPINNER DOME WITH NEW, THIS IS THE SECOND CRACKED SPINNER DOME. 1 H 7 1 3O NT 3A12 2001121200102 20011212 00102 CE 2001 12 12 CRJ2001F00000 1 20011120 A 2750 500000862 CONTROL CABLE CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO T/E FLAP BROKEN A CRJA O OTHER F FLT CONT AFFECTED AP APPROACH 1 CE 01 6764C 6894 402C0628 ON APPROACH WHEN FLAPS WERE SELECTED DOWN, A LOUD BANG WAS HEARD, FOLLOWED BY A SUDDEN RIGHT ROLL OF THE AIRCRAFT. CONT ROL WAS REGAINED AND AIRCRAFT WAS LANDED UNEVENTFULLY. UPON INSPECTION, IT WAS DISCOVERED THAT THE RIGHT FLAP CABLE WAS BROKEN AT RBL 18.5, OUTBOARD OF PULLEY (PN 5378.4) LOCATED AT 17.52 RBL. PROBABLE CAUSE APPEARS TO BE FATIGUE. FLAPS HAD BEEN AT 15 DEGREES. HAD THE FLAPS BEEN EXTENDED FULL TRAVEL THE PILOT MAY NOT HAVE REGAINED CONTROL. 1 L 7 2 3O 3 O A7CE E8CE 2001121200103 20011212 00103 SO 2001 12 12 FL93116 1 20011123 A 2750 48667784126 SHAFT PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA T/E FLAP STIFF A FFSA K NONE O OTHER TX TAXI/GRND HDL 1 AL 01 4112K 318353006 FLAPS WOULD NOT RETRACT AFTER LANDING. FINDINGS: THE RIGHT FLAP FLEXIBLE SHAFT ASSEMBLY TURNS VERY STIFFLY AND CONTRIB UTED TO FAILURE OF THE FLAP ACTUATOR MOTOR. THE LEFT FLEXIBLE SHAFT ASSEMBLY TURNS FREELY.(K) 1 L 7 2 3O 3 O A20SO E14EA 2001121200104 20011212 00104 EU 2001 12 12 GLA2001F00000 1 20010827 A 5610 MY20264105 SLIDING WINDOW AMD FALC20 FALCON 2720302 EU GARRTT TFE731 TFE731* 01518 WP COCKPIT CRACKED E GLAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 205K 319 AFTER APPROXIMATELY 1 HOUR INTO THE FLIGHT, THE PILOT NOTICED NUMEROUS SMALL CRACKS IN THE LEFT SLIDING WINDOW. CRACKS WERE LOCATED IN THE UPPER LEFT HAND CORNER OF THE SLIDING WINDOW. THE AIRCRAFT RETURNED TO BASE AND AFTER LANDING, CLOS ER EXAMINATION REVEALED CRACKS WERE ALSO LOCATED IN THE LOWER FORWARD PORTION OF THE WINDOW. PROBABLE CAUSE: UNKNOWN. 2 L 7 2 4F 4 F A7EU E6WE 2001121200105 20011212 00105 2001 12 12 GMA2001F00000 4 20011016 A 2297 WIRE LEAR 35 35A 5170602 CE AUTOPILOT SYS BROKEN A GMAL K NONE O OTHER IN INSP/MAINT 1 NM 09 873LP 5406 659 IN SERVICE FLEXING OF WIRE BUNDLE CAUSED THE SHIELDING AND A WIRE TO BREAK AT THE AIRFRAME-TO-WIRE BUNDLE CLAMP. SERVIC E LOOP DID NOT APPEAR TO BE OF SUFFICIENT SIZE TO ALLOW THE NEEDED FLEXING OF THE WIRE BUNDLE. FORCE SENSOR DID NOT FUN CTION. 2 L 7 2 4F A10CE 2001121200107 20011212 00107 WP 2001 12 12 IZ22001F00001 2 20011015 A 7310 69254513 VALVE MTSBSI MU2 MU2B60 5780460 CE GARRTT TPE331 TPE331* 01514 WP ENGINE LEAKING B IZ2R O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 15 360RA 251 740SA P36034 VALVE REPLACED DUE TO FUEL LEAK BETWEEN SOLENOID AND VALVE BODY. 1 H 7 2 3T 3 T RT A10SW E2WE 2001121200108 20011212 00108 WP 2001 12 12 IZ22001F00002 2 20011015 A 7310 69254513 VALVE MTSBSI MU2 MU2B36A 5780413 CE GARRTT TPE331 TPE331* 01514 WP RT ENGINE LEAKING B IZ2R O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 15 9NB 251 728SA VALVE REPLACED DUE TO OIL LEAK BETWEEN SOLENOID AND VALVE BODY. 1 H 7 2 3T 3 T A10SW E2WE 2001121200109 20011212 00109 WP 2001 12 12 IZ22001F00003 2 20011025 A 7261 31020472 HOUSING HONEYWELL MTSBSI MU2 MU2B25 5780409 CE GARRTT TPE331 TPE331* 01514 WP OIL PUMP CRACKED B IZ2R O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 15 281MA 103 11405700117 261 PILOT REPORTED OIL PRESSURE LOSS OF APPROXIMATELY 20 PSI IN FLIGHT. 1 H 7 2 3T 3 T A2PC E2WE 2001121200110 20011212 00110 WP 2001 12 12 IZ22001F00004 2 20011107 A 7310 69254513 SOLENOID VALVE MTSBSI MU2 MU2B36A 5780413 CE GARRTT TPE331 TPE33110T WP ENGINE LEAKING B IZ2R K NONE K FLUID LOSS IN INSP/MAINT 1 SW 15 895MA 322 723SA P105010 PILOT REPORTED FUEL LEAKING FROM COWLING. INVESTIGATION FOUND FUEL LEAK FROM MATING SURFACES OF PRIMARIES ONLY SOLENOID VALVE. REPLACED VALVE WITH SN 3894. 1 H 7 2 3T 4 T A10SW E4WE 2001121200111 20011212 00111 NE 2001 12 12 OEZ2001F00000 2 20010621 A 7532 310082903 BLEED VALVE DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A60A 52043 NE LT ENGINE CONTAMINATED A OEZA O OTHER R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 19 237SA 683 THIS ENGINE WAS TESTED AT A REPAIR STATION WITH NO OPERATIONAL DEFECTS FOUND. THE ENGINE WAS REINSTALLED ON THE SAME AI RCRAFT AND TEST FLOWN SUCCESSFULLY. ON 06/21 THE FLIGHT CREW REPORTED UNABLE TO ACHIEVE TAKEOFF POWER AND UNUSUAL SOUND COMING FROM ENGINE. THE COMPRESSOR BLEED AIR VALVE WAS REPLACED AND ENGINE PERFORMANCE RETURNED TO NORMAL. BLEED VALV E TEARDOWN REPORT SHOWED INTERNAL CONTAMINATION WITH OIL AND DIRT AND A HOLE IN THE DIAPHRAGM. 1 H 7 2 3T 4 T RT A9EA E4EA 2001121200112 20011212 00112 NE 2001 12 12 PI22001F00002 2 20010421 A 7240 CASE BOEING 757 757200 1384950 NM RROYCE RB211 RB211535C37 54555 NE COMBUSTION CRACKED B PI2R K NONE O OTHER IN INSP/MAINT 1 CE 07 GBIKH 30401 22179 30060 ON INSPECTING THE EXTERIOR OF THE AREA OF CONCERN, THE FOLLOWING ITEMS WERE FOUND. THERE ARE MULTIPLE CRACKS IN THE CIR CUMFERENTIAL DIRECTION TOTALING APPROX 30 INCHES. 2 L 7 2 4F 4 F RT A2NM E12EU 2001121200113 20011212 00113 SO 2001 12 12 POF2001F00000 1 20011029 A 2460 SWITCH PIPER PA34 PA34200 7103405 SO LYC O360 IO360A1A 41514 EA ELECTRICAL PANEL OVERHEATED H P0FS O OTHER M OVER TEMP NR NOT REPORTED 1 NE 03 88AG 347450093 ALTERNATOR SWITCH OVERHEATED. 1 L 7 2 3O 3 O A7SO 1E10 2001121200114 20011212 00114 NE 2001 12 12 T4O2001F00000 2 20010829 A 7321 VALVE HONEYWELL ISRAEL 1124 1124 4500102 EU GARRTT TFE731 TFE73131G 29003 NE FCU STUCK B T4OR C ABORTED TAKEOFF X ENGINE FLAMEOUT TO TAKEOFF 1 NE 03 819RC 62 A3240CTP 192 P77129 THE RIGHT ENGINE FLAMED OUT ON POWER UP FOR TAKE OFF ROLL. FUEL CONTROL FOUND TO BE THE CAUSE. SUBSEQUENT REPORT FROM MFG FOUND A STUCK, PARTIALLY OPEN PRESSURIZING VALVE. TIME SINCE OVERHAUL: 62.7 HOURS. 2 M 7 2 4F 4 F A2SW E6WE 2001121200115 20011212 00115 CE 2001 12 12 U9R2001F00000 1 20010919 A 2432 32824001 CELL BEECH 200 B200 1152922 CE PWA PT6 PT6A27 52043 EA BATTERY DEFECTIVE A U9RR O OTHER O OTHER NR NOT REPORTED 1 SW 19 67SD 140 BB1327 DURING FIRST FEW WEEKS OF FLYING, BEGAN TO BLOW ONE MAIN 325 AMP CURRENT LIMITS. BATTERY WAS NOT DUE ANY MAINTENANCE, B UT REMOVED AND BENCH CHECKED IT BECAUSE OF POSSIBLE HIGH CURRENT DRAW. FOUND CELL NR 9 TO NOT MEET SPECS. IN RELATION T O MM CAP CHECK. THIS WAS ADVERTISED AS A MAINTENANCE BATTERY. 1 L 7 2 4T 4 T A24CE E4EA 2001121200116 20011212 00116 SW 2001 12 12 PNSA011102 1 20011101 A 3150 2782174151 ANNUNCIATOR SWRNGN SA227 SA227AC 8780603 SW FAULTY A PNSA K NONE L NO TEST TX TAXI/GRND HDL 1 AL 03 2719H AC713B During pre engine start checklist pilot observed several annunciator lghts inop. Maintenance contacted and main annunica tor panel changed. 2 L 7 2 4T RT A8SW 2001121300001 20011213 00001 SO 2001 12 13 C2XA01TY192 1 20011212 A 3810 13500604403 LINE EMB 135 EMB135ER 3260203 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 TYS During a scheduled inspection the pottable water line was found corroded at the fuselage to tube fitting. Maintenan ce removed and replaced the potable water overflow line I.A.W.-EMB-135-AMM-38-10-07. Repairs where satisfactory and the aircraft will be released upon complection of the inspection. 2 L 7 2 4F RT T00011AT 2001121300002 20011213 00002 NM 2001 12 13 SWAA013304 1 20011211 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED (3 EA) AT BS 663.5, STRS 2L, 3L AND 2R. REPAIRED FRAME PER SR M. 2 L 7 2 4F RT A16WE 2001121300003 20011213 00003 NM 2001 12 13 SWAA013305 1 20011211 A 5330 6545890 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKINCRACKED AT FWD ENTRY DOOR LOWER HINGE CUT OUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001121300004 20011213 00004 NM 2001 12 13 SWAA013306 1 20011211 A 2731 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 705SW 27839 DURING SCHEDULED SERVICE CHECK, (SI 11038-55) LT ELEVATOR TAB BUSHINGS WORN AT HINGES NR 2, NR 3 AND NR 4. REMOVED AND REPLACED BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2001121300005 20011213 00005 NM 2001 12 13 SWAA013307 1 20011211 A 2731 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 705SW 27839 DURING SCHEDULED SERVICE CHECK, (SI 11038-55) RT ELEVATOR TAB BUSHINGS WORN AT HINGES NR 1 AND NR 4. REMOVED AND REPLAC ED BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2001121300006 20011213 00006 NM 2001 12 13 SWAA013308 1 20011211 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 724SW 27856 DURING SCHEDULED A1 CHECK, FOUND EEPLS COVERS BROKEN AT ROWS 1, 2, 8, 9, 22 AND 23. REMOVED AND REPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2001121300007 20011213 00007 NM 2001 12 13 SWAA013309 1 20011210 A 3220 6544610 ACTUATOR BOEING 737 7373H4 1384600 NM NLG WORN A SWAA K NONE O OTHER AP APPROACH 1 SW 07 316SW 23338 NOSE GEAR MAKES A GRINDING NOISE DURING EXTENSION. REMOVED AND REPLACED NLG RETRACT ACTUATOR AND NLG DOOR RT CRANK ARM ASSY. 2 L 7 2 4F RT A16WE 2001121300008 20011213 00008 NM 2001 12 13 SWAA013310 1 20011209 A 5751 65C25931 STIFFENER BOEING 737 7372H4 138448C NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED C2 CHECK, FOUND LT WING AILERON BALANCE BAY STIFFENER CRACKED 1.2 INCHES AT SECOND HINGE, WS 574. REPA IRED STIFFENER PER SWA RA. 2 L 7 2 4F A16WE 2001121300009 20011213 00009 NM 2001 12 13 SWAA013311 1 20011211 A 5241 2520691 WEB BOEING 737 7373H4 1384600 NM FWD SVC DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 386SW 26601 DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR AFT WEB BEAM CRACKED AT LOWER FITTING. REMOVED AND REPLACED WEB PER SRM . 2 L 7 2 4F RT A16WE 2001121300010 20011213 00010 CE 2001 12 13 FPI2001F00004 1 20010613 A 3710 20010 SPRING CESSNA 210 T210N 2073456 CE CONT O520 IO520* 17032 SO FLAPPER DOOR BROKEN E FPIA O OTHER O OTHER NR NOT REPORTED 1 SO 15 2145U 456 21064776 289166R SPRING ON SHUTTLE VALVE FLAPPER DOOR (ENGINE DRIVEN VACUUM PUMP SIDE) BROKE SHELLING OUT ENGINE DRIVEN VACUUM PUMP THUS ALLOWING ENGINE VACUUM TO VENT THROUGH ENGINE DRIVEN PUMP, CAUSING TOTAL LOSS OF VACUUM SYSTEM. 1 H 7 1 3O 3 O 3A21 E5CE 2001121300011 20011213 00011 NE 2001 12 13 GXPA0119 2 20010831 A 7200 TUBE AMD FALC20 FALCOND 2720304 EU GE CF700 CF700* 30010 NE ENGINE FAULTY A GXPA O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 GL 23 619GA 215 NR 1 ENGINE MAKING 1-44 EPR. MAXIMUM NEEDED 1-54 FOR TAKEOFF. EGT WAS 690 DEGREES. REPLACED SHORT TUBE ON ENGINE TO AIR FRAME. OPS CHECKED GOOD AT OUTSIDE TEMPERATURE 21 DEGREES. CALL FOR 1-54 EPR, MAKES 1-59 EPR. 2 L 7 2 4F 4 F A7EU E7EA 2001121300012 20011213 00012 EU 2001 12 13 JGV2001F00012 1 20010712 A 3220 BIGLS40TAG BEARING CAGE AMD FALC50 FALCON900 2700160 EU GARRTT TFE731 TFE7312 01518 WP NLG CORRODED A JGVR K NONE O OTHER IN INSP/MAINT 1 CE 09 902NC 4140 97 DURING NOSE GEAR INSTALLATION INSPECTION OF BALL JOINT FOUND CORROSION ON OUTBOARD DIAMETER OF BEARING CAGE. NO OBVIOUS SIGNS OF CORROSION PROTECTION DURING ORIGINAL INSTALLATION. PROBABLE CAUSE: WHEEL WELL ENVIRONMENT WITHOUT USE OF COR ROSION PROTECTION. 2 L 7 3 4F 4 F RT A46EU E6WE 2001121300013 20011213 00013 CE 2001 12 13 JGV2001F00014 1 20011102 A 2742 543500513 ACTUATOR LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE731* 01518 WP HORIZ STAB DAMAGED B JGVR K NONE O OTHER IN INSP/MAINT 1 CE 09 73GP 127 FOUND SCREW ASSEMBLY SEIZED AROUND MID RANGE OF TRAVEL AND UNABLE TO MOVE. DISASSEMBLED AND FOUND THE NUT SEIZED ON THE SCREW IN AN AREA WHERE FIVE INDEXED THREADS WERE GALLED AT THE TOP END OF THE NUT. THE GREASE ON THE NUT AND SCREW WAS ADEQUATE. THE PHYSICAL APPEARANCE OF THE THREADS OUTSIDE THE GALLED AREA WAS GOOD. 2 L 7 2 4F 4 F A10CE E6WE 2001121300014 20011213 00014 SO 2001 12 13 LD22001F00009 1 20010717 A 3040 GAR835NL1 RELAY GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE WINDSHIELD HEAT OVERHEATED B LD2R O OTHER M OVER TEMP NR NOT REPORTED 1 GL 15 73M 1013 547 11203 LEFT FRONT AND RIGHT WINDSHIELD HEAT WILL NOT SHUT OFF WHEN DESELECTED. FOUND LEFT FRONT WINDSHIELD HEAT CONTROL RELAY AND SOCKET OVERHEATED. THE WIRES CONNECTED TO CONTACTS A1, A2, B1 AND B2 WERE BROWN FROM OVERHEATING. THE PLASTIC ON T HE SOCKET HAD STARTED TO DEFORM FROM OVERHEATING, RELAY AND SOCKET WERE MELTED TOGETHER SO WE COULD NOT GET THEM APART. REPLACED THE RELAY SOCKET AND ASSOCIATED WIRING. FEEL THAT THE WIRING, THE SOCKET AND RELAY ARE NOT MADE OF A HEAVY EN OUGH MATERIAL TO HANDLE THE LOADS THAT ARE CARRIED. RELAY PN GAR835NL1, SOCKET PN GAS5825BA1. 2 L 7 2 4F 4 F RT A12EA E00057EN 2001121300015 20011213 00015 SO 2001 12 13 LD22001F00010 1 20010717 A 3040 GAS5825BA1 SOCKET GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE WINDSHIELD HEAT OVERHEATED B LD2R O OTHER M OVER TEMP NR NOT REPORTED 1 GL 15 73M 1013 547 11204 LEFT AND RIGHT FRONT WINDSHIELD HEAT WILL NOT SHUT OFF WHEN DESELECTED. FOUND LEFT FRONT WINDSHIELD HEAT CONTROL RELAY AND SOCKET OVERHEATED. THE WIRES CONNECTED TO CONTACTS A1, A2, B1 AND B2 WERE BROWN FROM OVERHEATING. THE PLASTIC ON T HE SOCKET HAD STARTED TO DEFORM FROM OVERHEATING, RELAY AND SOCKET WERE MELTED TOGETHER SO WE COULD NOT GET THEM APART. REPLACED THE RELAY, SOCKET AND ASSOCIATED WIRING. FEEL THAT THE WIRING, THE SOCKET AND THE RELAY ARE NOT MADE OF HEAV Y ENOUGH MATERIAL TO HANDLE THE LOADS CARRIED. RELAY PN GAR835ML1, SOCKET PN GAS5825BA1. 2 L 7 2 4F 4 F RT A12EA E00057EN 2001121300016 20011213 00016 2001 12 13 ME42001F00002 4 20011005 A 6122 A30672 BUSHING BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA HARTZL HCB4M HCB4MP3 GL BETA VALVE SWOLLEN B ME4R O OTHER O OTHER NR NOT REPORTED 1 SO 19 38SU UC38 FWA3276 PROP WAS REPAIRED FOR FAILURE TO GO INTO FEATHER. REALIGNED TWISTED BETA COLLAR AND REPAIR SPRING KIT. PROP WAS JERKING AS IT WENT INTO FEATHER, BETA RING DID NOT COME BACK TO FULLY EXTENDING POSITION. 2 OF 4 BETA SUPPORT GUIDE LUG BUSHIN GS WERE FOUND SWOLLEN WHICH PREVENTED BETA RODS FROM TRAVELING FULL LENGTH, WHICH KEPT BETA VALVE SLIGHTLY OPEN. THIS AL LOWED GOVERNOR OIL TO BYPASS PROP, PROP WOULD NOT COME OUT OF FEATHER. THIS COULD PREVENT PROP FROM OPERATING AT HIGH RPMS AND CHANGE PITCH UNCOMMANDED. GUIDE LUGS WERE REPLACED, RESEALED, AND PROP WAS REASSEMBLED. PROP OPERATES SMOOTHL Y FROM FEATHER THROUGH TO REVERSE WITH NO BINDING OR STICKING NOTED. PROP WAS REINSTALLED ON THE AC AND OPS CHECKED OK. 2 L 7 2 4T 4 T RT A24CE E4EA 6 C P56GL 2001121300017 20011213 00017 EA 2001 12 13 MHJ2001F00001 2 20011101 A 8520 MAIN BEARING PIPER PA60 PA60601 7106010 NM LYC O540 IO540S1A5 41532 EA ENGINE DELAMINATED E MHJA K NONE O OTHER IN INSP/MAINT 1 SW 05 601PJ 610264102 L2015648A FOUND NONFERROUS METAL IN SUCTION OIL SCREEN, CUT OPEN OIL FILTER AND FOUND NONFERROUS METAL IN OIL FILTER, DISASSEMBLED ENGINE, FOUND NR 2 AND NR 4 MAIN BEARINGS TO BE DELAMINATING. OIL ANALYSES SHOWS METAL TO BE CONSISTENT WITH BEARING M ATERIAL. 1 M 7 2 3O 3 O RT A17WE 1E4 2001121300019 20011213 00019 GL 2001 12 13 NSV2001F00000 3 20011101 A 6111 M10877 BLADE BEECH 1900 1900C 1154161 CE PWA PT6 PT6* 52043 EA HARTZL HCB4M HCB4MP3 GL PROPELLER CHIPPED A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 32017 11982 1107 UC37 FWA3520 MIX DISCOVERED A CHIP IN THE BLADE FACE OF THE NR 1 PROP DURING A PREFLIGHT INSPECTION. MECHANIC LOG ENTRY READS OK FOR CONTINUED SERVICE (IAW 811303 FROM HARTZELL PROPELLERS) 2 L 7 2 4T 3 T RT A24CE E2NE 6 C P56GL 2001121300021 20011213 00021 NE 2001 12 13 PI22001F00000 2 20010416 A 7230 HOUSING BOEING 757 757236 1384971 NM RROYCE RB211 RB211535C37 54555 NE ENGINE CRACKED B PI2R K NONE O OTHER IN INSP/MAINT 1 CE 07 GBIKI 24630 22180 DURING INSPECTION THE HP OUTLET GUIDE VANE LEADING EDGE VANE FILLET REGION. ACCESS THROUGH HIGH PRESSURE COMPRESSOR STA GE 6 AIR OFFTAKE. A BORESCOPE INSPECTION NOTED ON THE LEFT SIDE 3 CRACKS OVER 5 INCHES. RIGHT SIDE 2 CRACKS ON THE HO USING MEASURING 7 INCHES AND 1 OPEN FISSURE MEASURING APPROX 16 INCHES. 2 L 7 2 4F 4 F RT A2NM E12EU 2001121300022 20011213 00022 EU 2001 12 13 QY52001F00000 1 20010926 A 3232 A2373003 SWITCH AMD FALC20 FALCON 2720302 EU GE CF700 CF700* 30010 NE MLG DOOR ACT DAMAGED A QY5R K NONE L NO TEST IN INSP/MAINT 1 NE 01 20NY 61 DURING SCHEDULED MAINTENANCE, A GEAR SWING WAS BEING ATTEMPTED BUT WAS UNABLE TO RETRACT GEAR. FOUND RIGHT, MAIN LANDI NG GEAR DOOR ACTUATOR SWITCH FAULTY, COULD NOT MAKE CONTACT ON A&B TERMINALS. REMOVED SWITCH FROM ACTUATOR AND FOUND IN TERNAL DAMAGE IN ACTUATOR SWITCH RECEPTACLE. CAUSE OF INTERNAL DAMAGE UNKNOWN. POSSIBLY DAMAGED DURING OVERHAUL ASSEMB LY. 2 L 7 2 4F 4 F A7EU E7EA 2001121300023 20011213 00023 EU 2001 12 13 QY52001F00001 1 20010629 A 2810 MY20117022 FITTING AMD FALC20 FALCON 2720302 EU GE CF700 CF700* 30010 NE LT FUEL TANK CORRODED A QY5R K NONE O OTHER IN INSP/MAINT 1 NE 01 20NY 61 LEFT FUEL DRAIN UNION WAS REMOVED FROM MAIN WING TANK TO SEAL LEAK. UNION WAS FOUND TO BE RUSTED AND PITTED ON INSIDE D IAMETER. PITTING ESTIMATED TO BE ONE THIRD OF WALL THICKNESS. 2 L 7 2 4F 4 F A7EU E7EA 2001121300024 20011213 00024 SO 2001 12 13 COMA0110161 1 20011211 A 7712 SEDLOC2R GAUGE EMB 120 EMB120RT 3260202 SO INST. PANEL MALFUNCTIONED A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 462CA 24913 120264 FLIGHT 5070 R/H ENGINE TORQUE GAUGE FAILED DURING T/O.REPLACED THE TORQUE INDICATOR. 2 L 7 2 4T RT A31SO 2001121300025 20011213 00025 CE 2001 12 13 R292001F00000 1 20011129 A 2434 MDW100211 BOLT CESSNA 206 TU206F 2073353 CE CONT O520 TSIO520* 17040 SO ALTERNATOR LOOSE B R29R K NONE O OTHER IN INSP/MAINT 1 SW 19 3160L 500 A149763 U20602815 DURING INSPECTION, MECHANIC DISCOVERED THE FOUR INTERNAL WRENCHING BOLTS (PN:MDW 10021-1) THAT HOLD THE FRONT CASE (PN A SG 120561) HALVES TOGETHER, WERE LOOSE. THE SAFETY WIRE FROM THE BOLT HEAD TO THE THROUGH BOLT RETAINER (PN ASG 100091) ON EACH BOLT WAS STILL INTACT. SUSPECT ALTERNATOR WAS NOT PROPERLY ASSEMBLED WITH BOLTS ONLY SNUGGED DOWN VICE BEING T ORQUED TO THE PROPER VALUE PRIOR TO BE SAFETY WIRED. 1 H 7 1 3O 3 O A4CE E8CE 2001121300026 20011213 00026 CE 2001 12 13 R292001F00001 1 20011129 A 2434 MDW100211 BOLT CESSNA 206 U206G 2073356 CE CONT O520 IO520* 17032 SO ALTERNATOR LOOSE B R29R K NONE O OTHER IN INSP/MAINT 1 SW 19 9815Z 310 A149756 U20606678 DURING INSPECTION, MECHANIC DISCOVERED THE FOUR INTERNAL WRENCHING BOLTS (PN MDW 10021-1) THAT HOLD THE FRONT CASE (PN A SG 12057-1) AND REAR CASE (PN ASG 12056-1) HALVES TOGETHER, WERE LOOSE. THE SAFETY WIRE FROM THE BOLT HEAD TO THE THROU GH BOLT RETAINER (PN ASG 10009-1) ON EACH BOLT WAS STILL INTACT. SUSPECT ALTERNATOR WAS NOT PROPERLY ASSEMBLED WITH BOL TS ONLY SNUGGED DOWN VICE BEING TORQUED TOT HE PROPER VALUE PRIOR TO BEING SAFETY WIRED. 1 H 7 1 3O 3 O A4CE E5CE 2001121300027 20011213 00027 EA 2001 12 13 COMA0160958 1 20011211 A 5346 BEAM CNDAIR CL600 CL6002B19 1900309 EA F.S.460 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 927CA 18312 7031 ENGINE SUPPORT BEAM L/H AND R/H LOWER WEBS CRACKED.PERFORMED A MAJOR REPAIR TO THE L/H AND R/H LOWER WEB SECTIONS OF THE ENGINE SUPPORT BEAM I/A/W CANADAIR R.E.O. 601R-53-61-366 REV C. 2 L 7 2 4F RT A21EA 2001121300028 20011213 00028 EA 2001 12 13 COMA0160960 1 20011210 A 5346 WEB CNDAIR CL600 CL6002B19 1900309 EA F.S.460 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 947CA 14520 7077 ENGINE SUPPORT BEAM L/H LOWER WEB CRACKED.PERFORMED A MAJOR REPAIR TO THE L/H LOWER WEB SECTION OF THE ENGINE SUPPORT BE AM I/A/W CANADAIR REO 601R-53-61-366 REV C. 2 L 7 2 4F RT A21EA 2001121300029 20011213 00029 WP 2001 12 13 ABXA010624 1 20011211 A 3260 H146 SWITCH DOUG DC9 DC932 3022066 WP DEFECTIVE A ABXA O OTHER O OTHER AP APPROACH 1 GL 23 987AX 47364 ON GEAR EXTENSION, NOSE GEAR GREEN LIGHT FAILED TO ILLUMINATE WITH ASSOCIATED RED GEAR UNSAFE LIGHT. LIGHT ILLUMINATED A FTER CYCLING GEAR TWICE TO GET NORMAL INDICATION. NOSE LANDING GEAR DOWNLOCK SWITCH LEVER MECHANICALLY BINDING. REPLACED DOWNLOCK SWITCH IAW DC-9 MM. 2 L 7 2 4F A6WE 2001121300030 20011213 00030 WP 2001 12 13 ABXA010626 1 20011126 A 5313 592480223 LONGERON DOUG DC9 DC941 302207N WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 LONGERON 17 RIGHT WAS CRACKED AT F.S. 408. CRACK WAS LOCATED AT LOWER HI-LOCK AND WAS APPROXIMATELY .50 INCHES LONG. REP AIRED LONGERON 17 RIGHT IAW DC-9 SRM 53-02. 2 L 7 2 4F A6WE 2001121300031 20011213 00031 SO 2001 12 13 RMM2001F00000 1 20011023 A 3213 7873802 STRUT PIPER PA28 PA28151 7102805 SO LYC O320 O320* 41508 EA LT MLG CRACKED B RMMR K NONE O OTHER IN INSP/MAINT 1 CE 01 1195X 287515324 DURING A SCHEDULED INSPECTION A CRACK WAS FOUND IN ONE LEFT GEAR LOWER TORQUE LINK ATTACHMENT EAR. THIS CONDITION HAS BEEN FOUND PREVIOUSLY OVERHAULED MID TO HIGH TIME AIRCRAFT USED IN TRAINING. TIME ON PART COULD NOT BE DETERMINED. AIR CRAFT TOTAL HOURS 11,650. CRACKS HAVE BEEN FOUND ON EITHER EAR AND FROM TOP OR BOTTOM 1 L 7 1 3O 3 O 2A13 E274 2001121300032 20011213 00032 WP 2001 12 13 MWEA011480 1 20011212 A 5330 59114024 SKIN DOUG DC9 DC981 3022081 WP FWD SVC DOOR GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 FUSELAGE SKIN GOUGED AT AFT EDGE OF FORWARD SERVICE DOOR HOLD OPEN CUP -- BLENDED DAMAGE. INSTALLED REPAIR PLATE AND D OUBLERS IN ACCORDANCE WITH SRM 53-04, FIGURE 24. 2 L 7 2 4F A6WE 2001121300033 20011213 00033 WP 2001 12 13 MWEA011483 1 20011212 A 5750 5912125502 SPAR CAP DOUG DC9 DC981 3022081 WP R/H FLAP CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 RIGHT HAND FLAP LOWER AFT FLAP SPAR CUP IS CRACKED JUST OUTBOARD OF FLEX JOINT -- REMOVED CRACKED SPAR CAP, LOCATED, D RILLED AND INSTALLED NEW SPAR CAP. 2 L 7 2 4F A6WE 2001121300034 20011213 00034 WP 2001 12 13 MWEA011484 1 20011212 A 5240 99115793 BEAM DOUG DC9 DC981 3022081 WP GALLEY SVC DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 GALLEY SERVICE DOOR #1 BEAM IS CRACKED IN OUTBOARD RADIUS AT FORWARD END -- STOP DRILLED CRACK. LOCATED, DRILLED AND I NSTALLED REPAIR DOUBLERS. 2 L 7 2 4F A6WE 2001121300035 20011213 00035 WP 2001 12 13 MWEA011485 1 20011212 A 5240 99115809 FITTING DOUG DC9 DC981 3022081 WP GALLEY SVC DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 GALLEY SERVICE DOOR #3 BEAM IS CRACKED IN OUTBOARD RADIUS AT FORWARD END -- STOP DRILLED CRACK. REMOVED AND REPLACED F ITTING. 2 L 7 2 4F A6WE 2001121300036 20011213 00036 CE 2001 12 13 2001F00738 1 20010914 A 7920 646685 GASKET CESSNA 421 421B 2076014 CE OIL SYSTEM LEAKING A BLIA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 17 208V 421B0866 OIL LEAK DISCOVERED AFTER ARRIVING AT SAW. GROUNDED AIRCRAFT AND CALLED MAINTENANCE. LEAK CAUSED BY BAD GASKET BETWEEN COOLER AND ENGINE CASE. GASKET REPLACED. ENGINE LEAK CHECKED GOOD. AIRCRAFT RETURNED IRS. (M) 1 L 7 2 3O A7CE 2001121300037 20011213 00037 2001 12 13 2001F00731 4 20011027 A 2340 656021032 ACCESSORY UNIT BOEING 727 727225 1384077 NM E/E BAY INOPERATIVE A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 804MA 22435 ON PREFLIGHT TRANSIT, FOUND COCKPIT EMERGENCY INTERPHONE INOPERATIVE. TROUBLE SHOT SYSTEM AND FOUND NR 2 AUDIO ACCESSOR Y UNIT INOPERATIVE. REMOVED AND REPLACED NR 2 AUDIO ACCESSORY UNIT IAW 24-41-01. OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 3 4F A3WE 2001121300038 20011213 00038 NM 2001 12 13 2001F00732 1 20011110 A 3150 32EN614 SWITCH BOEING 727 727225 1384077 NM TAKEOFF WARNING STICKS A MYWA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 19 803MA 22434 TAKEOFF WARNING HORN CAME ON PRIOR TO BRAKE RELEASE ON RUNWAY. ISSUED MAINTENANCE FERRY PERMIT IN SFB. IN MIA, FOUND U PPER TAKEOFF WARNING SWITCH STICKING. REPLACED UNIT, OPS TEST NORMAL IAW MM 31-26-24. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 3 4F A3WE 2001121300039 20011213 00039 EU 2001 12 13 2001F00733 1 20011018 A 6410 355A01103601 BEARING SNIAS 350 AS350* EU TAIL ROTOR DELAMINATED A KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 115SH 640 3141 HALF PAULST SHELL BEARING WORN BEYOND LIMIT DELAMINATIONS. REPLACED WITH NEW BEARING. (M) 1 G 7 1 3U H9EU 2001121300042 20011213 00042 WP 2001 12 13 AALA20011556 1 20010803 A 2424 947F9453 GCU DOUG DC9 DC982 3022082 WP RT ENGINE FAILED A AALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 SW 21 587AA 53250 LIT - FLT 1121 - EN ROUTE BOS-DFW, RIGHT AC BUSS LOSS. LANDED LIT WITHOUT INCIDENT. REPLACED RIGHT CSD, GENERATOR AND GENERATOR CONTROL UNIT P/N 947F9453. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001121300043 20011213 00043 WP 2001 12 13 AALA20011726 1 20010830 A 3350 SIGN DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 471AA 49601 DFW - DURING OVERNIGHT MAINTENANCE, LOWER SIDE WALL EMERGENCY EXIT SIGN AT AFT GALLEY SERVICE DOOR INOPERATIVE. REPLACE D EMERGENCY EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001121300044 20011213 00044 WP 2001 12 13 AALA20011784 1 20010918 A 3350 SWITCH DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 471AA 49601 SFO - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHT AT ROW 12 THROUGH 19 INOPERATIVE. REPLACED EMERGENCY E XIT LIGHT POWER SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001121300045 20011213 00045 WP 2001 12 13 AALA20011802 1 20010920 A 3397 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70529 49921 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 20 INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT EMERG ENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001121300046 20011213 00046 WP 2001 12 13 AALA20011806 1 20010923 A 3397 WIRE DOUG DC9 DC982 3022082 WP AFT AIRSTAIRS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 275AA 49272 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WI RE AT AFT AIRSTAIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001121300047 20011213 00047 WP 2001 12 13 AALA20011807 1 20010923 A 3397 WIRE DOUG DC9 DC982 3022082 WP AFT AIRSTAIRS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 476AA 49651 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS INOPERATIVE. RESECURED EMERGENCY EXIT LIGHT W IRE AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001121300048 20011213 00048 WP 2001 12 13 AALA20011808 1 20010923 A 3397 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 77421 49333 DFW - DURING OVERNIGHT MAINTENANCE, OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RESECURED EMERGENCY EXIT LIGHT CONNECTOR . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001121300049 20011213 00049 WP 2001 12 13 AALA20011819 1 20010927 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 471AA 49601 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 24 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT ROW 24. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001121300050 20011213 00050 WP 2001 12 13 AALA20011820 1 20010925 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 472AA 49647 SEA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM G ROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001121300051 20011213 00051 WP 2001 12 13 AALA20011830 1 20010928 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 462AA 49592 SAT - DURING OVERNIGHT MAINTENANCE, FORWARD GALLEY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001121300053 20011213 00053 WP 2001 12 13 AALA20011856 1 20011009 A 3350 SOCKET DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 249AA 49269 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 4C AND 35C INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT S OCKET AT ROW 4C AND 35C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001121300054 20011213 00054 WP 2001 12 13 AALA20011935 1 20011018 A 3350 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7528A 49920 TUL - FOUND BROKEN WIRE AT SEAT 19 DEF. FOUND BROKEN WIRE AT SEAT 19 DEF WHILE OPS CHECKING EMERGENCY LIGHTS. REPAIRED WIRE PER WDM 20-10-03. (M) 2 L 7 2 4F A6WE 2001121300055 20011213 00055 WP 2001 12 13 AALA20011954 1 20011023 A 3350 SOCKET DOUG DC9 DC982 3022082 WP CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 407AA 49318 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 26 INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT SOCKET AT SEAT 26. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001121300056 20011213 00056 WP 2001 12 13 AALA20011957 1 20011025 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 248AA 49259 SAN - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. RESECURED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROU ND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001121300057 20011213 00057 WP 2001 12 13 AALA20011958 1 20011027 A 3397 WIRE DOUG DC9 DC982 3022082 WP A/C BAY DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 485AA 49678 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT TAILCONE INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT OVERHEAD CATWALK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001121300058 20011213 00058 WP 2001 12 13 AALA20011966 1 20011029 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 451AA 49477 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PORTABLE LIGHT AT ENTRY DOOR INOPERATIVE. REPLACED EMERGENCY EXIT PO RTABLE LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001121300059 20011213 00059 WP 2001 12 13 AALA20011980 1 20011118 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 424AA 49336 TUL - FOUND DENT AND CREASE IN SKIN ABOVE LONGERON 22L, STATION 400 (ADL). CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-04-00 VIEW H. (M) 2 L 7 2 4F A6WE 2001121300060 20011213 00060 WP 2001 12 13 AALA20011981 1 20011023 A 5311 BELTFRAME DOUG DC9 DC982 3022082 WP FUSELAGE CHAFED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 424AA 49336 TUL - FOUND BELL FRAME HAS DEEP CUT, RUB MARK STATION 522 AT LONGERON L6. BLENDED OUT DAMAGE AD INSTALLED DOUBLER REPAI R PER 53-10-00-14 FIG 1. (M) 2 L 7 2 4F A6WE 2001121300061 20011213 00061 WP 2001 12 13 AALA20011982 1 20011023 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 424AA 49336 TUL - FOUND DEEP GOUGE IN FUSELAGE AT L19L STATION 223. INSTALLED DOUBLER PER SRM 53-04 FIG 38, VIEW E. (M) 2 L 7 2 4F A6WE 2001121300062 20011213 00062 WP 2001 12 13 AALA20011983 1 20011022 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 424AA 49336 TUL - FOUND CUSP CRACKED AT STATION 1103. CUT OUT CRACKED AREA DYE CHECKED TO CONFIRM CRACK. REMOVAL AND INSTALLED DOU BLER PER SRM 53-30. (M) 2 L 7 2 4F A6WE 2001121300063 20011213 00063 WP 2001 12 13 AALA20011984 1 20011023 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 424AA 49336 TUL - FOUND CREASE IN FUSELAGE SKIN STATION 408 BETWEEN L29R AND L30. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SR M 53-04 FIG 38. (M) 2 L 7 2 4F A6WE 2001121300064 20011213 00064 NM 2001 12 13 ZW0A0112002 1 20011212 A 3350 8039251 POWER SUPPLY BOEING 717 717200 1383700 NM CABIN MALFUNCTIONED A ZW0A K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CE 13 2417F 55084 ON APPROACH NOTICED A BURNING ODOR IN FIRST FEW ROWS OF COACH SECTION WITH EMERGENCY LIGHTS FLASHING ON AND OFF SEVERAL TIMES. FOUND EMERGENCY LIGHT POWER SUPPLY HOT, AND REPLACED SAME. 2 L 7 2 4F TR A6WE 2001121300065 20011213 00065 WP 2001 12 13 AALA20011985 1 20011025 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 424AA 49336 TUL - FOUND NR 1 SEAT TRACK CRACKED APPROXIMATELY AT STATION 1280. REPLACED SEAT TRACK FROM STATION 1171 TO 1307 LEFT S RM 53-01. (M) 2 L 7 2 4F A6WE 2001121300066 20011213 00066 WP 2001 12 13 AALA20011986 1 20011025 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 424AA 49336 TUL - FOUND WEAR MARK ON FRAME 1401 AT L15L. BLENDED OUT WEAR, INSTALLED DOUBLER PER AARD 53-10-00-14. (M) 2 L 7 2 4F A6WE 2001121300067 20011213 00067 WP 2001 12 13 AALA20011987 1 20011025 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 424AA 49336 TUL - FOUND LEFT INTERCOSTAL CRACKED AT STATION 988 ON BOTTOM OF KEEL BEAM LBL 4.5 INCH IN UPPER BEND RADIUS. REPLACED LEFT INTERCOSTAL AT STATION 988 AS PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2001121300068 20011213 00068 WP 2001 12 13 AALA20011988 1 20011025 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 424AA 49336 TUL - FOUND CORROSION ON NR 2 SEAT TRACK STATION 1203-1205. INSTALLED SEAT TRACK PLUG REPAIR PER SRM 53-05 FIG 4. (M) 2 L 7 2 4F A6WE 2001121300069 20011213 00069 WP 2001 12 13 AALA20011989 1 20011030 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 424AA 49336 TUL - FOUND AFT CARGO DOOR CUTOUT LOWER BEAM HAS HEAVY CORROSION STATION 1165 TO 1211. REMOVED CORRODED DOOR BEAM AND I NSTALLED NEW ONE PER SRM 51-01. ALSO INSTALLED/SPLICED IN NEW WEB SECTION (PREVIOUSLY REPAIRED) PER AARD 53-10-00-24 ON E58 NR 4042956. (M) 2 L 7 2 4F A6WE 2001121300070 20011213 00070 WP 2001 12 13 AALA20011990 1 20011029 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 424AA 49336 TUL - FOUND LONGERON 2L CRACKED JUST AFT OF STATION 1418. REPAIRED LONGERON 2L PER AARD 53-30-00-2. (M) 2 L 7 2 4F A6WE 2001121300071 20011213 00071 WP 2001 12 13 AALA20011991 1 20011030 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 424AA 49336 TUL - FOUND CRACK IN LONGERON 11L AT STATION 579. INSTALLED DOUBLER IN LONG 11L AT STATION 579 AND APPROX 13 INCH LONGE RON 11 PER SRM 53-02 FIG 3. (M) 2 L 7 2 4F A6WE 2001121300072 20011213 00072 WP 2001 12 13 AALA20012016 1 20011105 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70401 49312 DFW - DURING OVERNIGHT MAINTENANCE, L1 DOOR PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED L1 DOOR PORTABLE EMERGENCY L IGHT. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001121300073 20011213 00073 SO 2001 12 13 C2XA01CL242 1 20011212 A 3350 1317 BULB EMB 135 EMB135ER 3260203 SO SERVICE DOOR BURNED OUT A C2XA O OTHER L NO TEST IN INSP/MAINT 1 SW 27 25504 145186 DURING A 1A INSPECTION MAINTENANCE FOUND THE SERVICE DOOR EMERGENCY LIGHT WAS INOPERATIVE.MAINTENANCE REPLACED THE LIGHT BULB FOR THE SERVICE DOOR EMERGENCY LIGHT AND OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001121300074 20011213 00074 WP 2001 12 13 AALA20012019 1 20011023 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 593AA 53256 TUL - FOUND TEMPORARY DOUBLER INSTALLED ON LEFT SIDE OF FUSELAGE, JUST FORWARD OF STATION 579, L20L - L21L. REMOVED TEM PORARY REPAIR AND INSTALLED NEW CLASS 1 PERMANENT REPAIR PER SRM 53-04 FIG 128. (M) 2 L 7 2 4F RT A6WE 2001121300075 20011213 00075 WP 2001 12 13 AALA20012020 1 20011029 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 593AA 53256 TUL - FOUND CANTED FRAME AT STATION 1485 AT AFT AIRSTAIR ACTUATOR IS CRACKED. CUT OUT DAMAGED AREA AND INSTALLED DOUBLE R PER AARD 53-10-00-33 PAGE 1. (M) 2 L 7 2 4F RT A6WE 2001121300076 20011213 00076 WP 2001 12 13 AALA20012021 1 20011016 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 593AA 53256 TUL - FOUND NR 1 SEAT TRACK HAS HEAVY CORROSION IN CHANNEL FROM BS 1205 TO 1208. REMOVED CORROSION AND INSTALLED SEAT T RACK PLUG PER AARD 53-20-00-10. (M) 2 L 7 2 4F RT A6WE 2001121300077 20011213 00077 WP 2001 12 13 AALA20012022 1 20011019 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 593AA 53256 TUL - FOUND DENT APPROXIMATELY 2.5 INCHES AFT OF FORWARD ENTRY DOOR IN RED STRIPE. INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M) 2 L 7 2 4F RT A6WE 2001121300078 20011213 00078 WP 2001 12 13 AALA20012023 1 20011023 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 593AA 53256 TUL - FOUND DENT IN FUSELAGE SKIN AT STATION 237 BETWEEN LONGERON 18L AND LONGERON 19L. COLD WORK DENT AND INSTALLED DO UBLER PER SRM 53-30-00-9. (M) 2 L 7 2 4F RT A6WE 2001121300079 20011213 00079 WP 2001 12 13 AALA20012025 1 20011108 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 577AA 53154 DTW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 8 INOPERATIVE. REPLACED BATTERY FOR EMERGENCY EXIT LIGH T AT ROW 8. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001121300080 20011213 00080 WP 2001 12 13 AALA20012026 1 20011108 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 290AA 49302 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT ESCAPE PATH LIGHTS BETWEEN ROW 18 AND 21 INOPERATIVE. REPLACED BATTER Y PACK FOR EMERGENCY EXIT ESCAPE PATH LIGHTS BETWEEN ROW 18 AND 21. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001121300081 20011213 00081 WP 2001 12 13 AALA20012027 1 20011108 A 3350 CIRCUIT BREAKER DOUG DC9 DC982 3022082 WP COCKPIT MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 452AA 49553 ORD - FOUND DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS DID NOT ILLUMINATE WITH COCKPIT SWITCH. RESET OVERHEAD EMERG ENCY LIGHT CIRCUIT BREAKER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001121300082 20011213 00082 WP 2001 12 13 AALA20012035 1 20011109 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 279AA 49295 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT WIRE AT CONNECTOR LOOSE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001121300083 20011213 00083 WP 2001 12 13 O3X01119261 2 20011117 A 7320 31021451 LINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP LT ENGINE LOOSE A O3XA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 03 926AE 10253 3016 926 P66357 EN ROUTE FROM BRL-STL, WHEN THE LEFT ENGINE STARTED TO HAVE TORQUE AND TEMPERATURE FLUCTUATIONS NORMAL PROCEDURES WERE F OLLOWED. ENGINE TORQUE AND TEMP REMAINED ERRATIC. AN EMERGENCY WAS DECLARED AND THE LEFT ENGINE SHUT DOWN IAW AFM EMER GENCY PROCEDURES. THE AIRCRAFT DIVERTED TO UIN AND LANDED WITHOUT FURTHER INCIDENTS. THE ENGINE WAS INSPECTED BY MX PE RSONNEL. THE INSPECTION REVEALED THAT LINE FROM THE P2T2 SENSOR TO THE FUEL CONTROL WAS LOOSE. THE LINE WAS RETORQUED. ENGINE RUNS WERE SATISFACTORY, NO OTHER DISCREPANCIES NOTED. ALL OTHER LINES IN THE FUEL CONTROL AREA WERE CHECKED FO R PROPER TORQUE AS WELL. NO OTHER DISCREPANCIES NOTED. THE AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 2001121300085 20011213 00085 EU 2001 12 13 01FDEA01070 1 20011213 A 2612 SMOKE WARNING AIRBUS 310 A310222 3930315 EU SMOKE A FDEA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 25 448FE 260 1-396 RECEIVED MAIN DECK CARGO SMOKE WARNING. BITE CHECK PER MM 26-19-00-5. NO FAULT FOUND. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2001121300086 20011213 00086 WP 2001 12 13 DIN2001F00001 2 20011129 A 7260 M274263116A RETAINER LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE7313A 01518 WP DRIVE SHAFT BROKEN B DINR O OTHER O OTHER TX TAXI/GRND HDL 1 EA 13 127GT 067 P85244 ENG WOULD NOT START. INVESTIGATION FOUND ACCESSORIES AND STARTER MOTOR WOULD TURN BUT ENGINE N1 AND N2 ROTORS DID NOT. FOUND HORIZ DR SHAFT (PN 3070201-11) HAD UNCOUPLED FROM ACCY GEARBOX DUE TO RETAINER RING (M27426-3116A) BECOMING UNLOC KED AND ALLOWING MOVEMENT OF SHAFT. PRIOR TO 2000, RETAINER RINGS NOT ROUTINELY REMOVED FROM TRANSFER GB HSGS. IF REMO VED, WERE PERMITTED TO BE REUSED, ONLY BEING REPLACED (ON CONDITION). AFTER 11/2000, ALL ENG UNDERGOING MPI OR GREATER INSP ARE REQUIRED TO HAVE RETAINER RING REMOVED AND REPLACED NEW. REPLACEMENT IS NOW MANDATORY AND ROUTINE. 2 L 7 2 4F 4 F A10CE E6WE 2001121300087 20011213 00087 EA 2001 12 13 RMM2001F00001 2 20011023 A 7322 105009 CARBURETOR AMRGEN AA5 AA5A 3960106 SO LYC O320 O320* 41508 EA ENGINE SEPARATED B RMMR O OTHER O OTHER NR NOT REPORTED 1 CE 01 26411 1700 AA5A0571 OPERATOR REPORTED ENGINE WOULD NOT RUN WELL AT LOW SPEEDS. FOUND CARBURETOR BODY TO BOWL LOOSE. LOCK TABS ARE WERE IN LOCKED POSITIONS. THIS IS THE SECOND OCCURRENCE ON THIS AIRCRAFT IN APPROXIMATELY 200 HRS OF FLYING. THE BOWL THREADS APPEARED TO BE EXCESSIVELY WORN. A SERVICEABLE BOWL WAS INSTALLED. EXACT CAUSE COULD NOT BE DETERMINED. GASKET SHRINK AGE IS SUSPECTED SERIAL NUMBER WAS NOT RECORDED. 1 L 7 1 3O 3 O A16EA E274 2001121300088 20011213 00088 GL 2001 12 13 RRI2001F00000 3 20010923 A 6110 R334482F13 PROPELLER CASA C212 C212CD 2410209 EU GARRTT TPE331 TPE331* 01514 WP ROTOL R334 R334482F13 GL LT ENGINE SEPARATED D RRIM O OTHER O OTHER NR NOT REPORTED 1 SO 05 7241E 16005 1446 318 P37386C DRG1723184 PROP HUB SEPARATED AT BOLTS, LEAVING JUST THE AREA OF THE HUB THAT THE BOLTS ATTACH TO. THE HUB WAS NEW AT THE OVERHAUL . THERE WAS NO VIBRATION AT ALL DURING THE FLIGHTS AND STARTS THAT LOOK PLACE EARLY THAT DAY OR THE DAY BEFORE. THERE WAS NO EVIDENCE OF OIL LEAKS DURING ANY TIME PRIOR. THE PROP SEPARATED CLEANLY FROM THE AIRCRAFT CAUSING NO DAMAGE TO T HE AIRCRAFT. FIRST THOUGHT WAS THAT THE BOLTS HAD BEEN OVER TORQUED AS THE PROP HAD BEEN REINSTALLED JUST 94.9 HOUR EAR LIER. NEED TO LOOK CLOSER AT THE BASE OF THE PROP HUB FOR ANY SIGNS OF CRACKS DURING EACH OF THE REQUIRED INSPECTIONS. 2 H 7 2 4T 3 T RT A43EU E2WE 6 C P61GL 2001121300089 20011213 00089 NM 2001 12 13 RRX2001F00000 1 20011116 A 2782 14110322 ACTUATOR BOEING 727 727222 1384073 NM PWA JT8 JT8D1 52044 NE L/E SLAT LEAKING A RRXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 05 7638U 19911 LOST (A) SYSTEM HYDRAULIC PRESSURE DURING CLIMB OUT FROM MSY. ACCOMPLISHED EMERGENCY CHECKLIST RELATING TO LOSS OF (A) S YSTEM HYDRAULICS. EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED NR 3 SLAT ACTUATOR ASSEMBLY AND OP ERATIONAL CHECK SYSTEM IAW MM.(K) 2 L 7 3 4F 4 F A3WE E2EA 2001121300090 20011213 00090 CE 2001 12 13 T19A2770914 1 20010918 A 2435 30B10719A STARTER GEN LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE7313 01518 WP RT ENGINE FAILED E T19A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 19 277AL 1649 104 P94108 SHORTLY AFTER TAKEOFF THE RIGHT ENGINE FIRE WARNING ILLUMINATED. POWER WAS REDUCED TO THE RIGHT ENGINE AND THE WARNING LIGHT EXTINGUISHED. A PRECAUTIONARY LANDING WAS MADE AT THE DEPARTURE AIRPORT. INVESTIGATION REVEALED THE RIGHT GENERA TOR EXPERIENCED A CATASTROPHIC FAILURE. THE FIRE SENSING ELEMENT IS ROUTED OVER THE GENERATOR AND WAS THE CAUSE IF THE FIRE INDICATION. PRELIMINARY INSPECTION REVEALED POSSIBLE BEARING FAILURE WITHIN THE GENERATOR. 2 L 7 2 4F 4 F A10CE E6WE 2001121300091 20011213 00091 CE 2001 12 13 T402001F00000 1 20011127 A 5330 5012015681 SKIN BEECH 90 E90 1152914 CE PWA PT6 PT6A60A 52043 NE FUSELAGE CRACKED B T40R K NONE O OTHER IN INSP/MAINT 1 NE 03 965LG 11516 LW204 RIGHT CENTER SECTION SKIN CRACKED 2.25 INCHES BETWEEN RIVETS AND BEYOND AT DOUBLE ROW RIVET SKIN JOINT BETWEEN RIVETS. LOCATION ON SKIN IS JUST AFT OF MAIN WING SPAR CAP AT BL 16.25. THIS AREA IS PART OF THE PRESSURE VESSEL BEFORE TRANSIT ION TO THE UNPRESSURIZED WING. PROBABLE CAUSE UNKNOWN. MAY BE RESULT OF PRESSURE CYCLES, OR FATIGUE FROM LANDING CYCLE S, OR VIBRATION. 1 L 7 2 3T 4 T 3A20 E4EA 2001121300092 20011213 00092 CE 2001 12 13 T402001F00001 1 20010320 A 5330 5012015682 SKIN BEECH 90 E90 1152914 CE PWA PT6 PT6A60A 52043 NE FUSELAGE CRACKED B T40R K NONE O OTHER IN INSP/MAINT 1 NE 03 4495N 8938 LW14 RIGHT CENTER SECTION SKIN CRACKED BETWEEN RIVETS AND BEYOND AT DOUBLE ROW RIVET SKIN JOINT, BETWEEN RIVETS. LOCATION ON SKIN IS JUST AFT OF MAIN WING SPAR CAP AT BL 16.25. THIS AREA IS PART OF THE PRESSURE VESSEL BEFORE TRANSITION TO THE UNPRESSURIZED WING. PROBABLE CAUSE UNKNOWN. MAY BE RESULT OF PRESSURE CYCLES, OR FATIGUE FROM LANDING CYCLES, OR VIBRA TION. 1 L 7 2 3T 4 T 3A20 E4EA 2001121300093 20011213 00093 CE 2001 12 13 TIM2001F00006 1 20010522 A 7920 B-NUT BEECH 1900 1900 1154160 CE OIL SYSTEM LOOSE A TIMA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 NM 07 172GA UB11 OIL LINE TO THE TORQUE MANIFOLD, B-NUT CAME LOOSE, OIL PRESSURE FLUCTUATED AND ENGINE SHUT DOWN. AIRCRAFT LANDED. ENGI NE WAS INSPECTED AS PER MM, LOW OIL PRESSURE PROCEDURE. NO DAMAGE FOUND - OIL SERVICED AND ENGINE TEST RUN PER P/W CHE CK. 2 L 7 2 4T RT A24CE 2001121300094 20011213 00094 CE 2001 12 13 TIM2001F00007 1 20010823 A 5730 114120036613 PANEL BEECH 1900 1900C 1154161 CE PWA PT6 PT6* 52043 EA LT WING DEBONDED A TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 195GA UB65 LEFT INBOARD UPPER WING PANEL AFT OF WING SPAR DE-BONDING BETWEEN UPPER WING SKIN AND HONEYCOMB INSIDE FUEL BAY AREA. 2 L 7 2 4T 3 T RT A24CE E2NE 2001121300095 20011213 00095 CE 2001 12 13 TIM2001F00009 1 20011015 A 7110 1189100421 BULKHEAD BEECH 1900 1900 1154160 CE PWA PT6 PT6A60A 52043 NE LT COWLING CRACKED E TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 UB34 31058 UB34 THE LEFT COWLING BULKHEAD AT STATION 238.18 THAT THE LOWER FRONT ENGINE COWLING ATTACHES TO WAS BROKEN OUT ON THE RIGHT LOWER SIDE. THE LOCATION IS WHERE ONE OF THE FOUR BOLTS SECURE THE COWL TO THE BULKHEAD. PICTURES INCLUDED. 2 L 7 2 4T 4 T RT A24CE E4EA 2001121300096 20011213 00096 CE 2001 12 13 TIM2001F00010 1 20011015 A 7110 1189100421 BULKHEAD BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE RT COWLING CRACKED E TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 153GA 31058 UB34 THE RIGHT ENGINE COWLING BULKHEAD AT STATION 238.18 THAT THE LOWER FRONT ENGINE COWLING ATTACHES TO WAS CRACKED ON THE R IGHT LOWER SIDE. THIS LOCATION IS WERE ONE OF THE FOUR BOLTS SECURE THE LOWER COWL TO THE BULKHEAD. (PICTURES INCLUDED ) 2 L 7 2 4T 4 T RT A24CE E4EA 2001121300097 20011213 00097 CE 2001 12 13 TIM2001F00011 1 20011016 A 3097 20GTEF WIRE BEECH 1900 1900 1154160 CE COCKPIT BROKEN E TIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 172GA UB11 THE ICE VANE CONTROL WIRE NUMBER 20A20 BROKE AT THE TERMINAL END UNDER THE PANEL AT INST ZONE 245 CAUSING A SHORT WHICH CAUSED SMOKE IN THE COCKPIT. 2 L 7 2 4T RT A24CE 2001121300098 20011213 00098 CE 2001 12 13 TIM2001F00012 1 20011029 A 2750 101380005 CONTROL CABLE BEECH 1900 1900C 1154161 CE PWA PT6 PT6* 52043 EA T/E FLAP DEFECTIVE E TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 195GA UB65 INSPECTION OF FLAP CABLES AS OUTLINED IN MFG SB AS REQUIRED BY AD REVEALED THE LEFT OUTBOARD FLAP CABLE DEFECTIVE. THE CABLE HAD STARTED TO UNWIND. 2 L 7 2 4T 3 T RT A24CE E2NE 2001121300099 20011213 00099 2001 12 13 UG82001F00003 4 20010823 A 2350 7510280901 PRINTED CKT BOAR CESSNA 650 650 2076802 CE GARRTT TFE731 TFE731* 01518 WP NR 2 COMM DEFECTIVE A UG8A O OTHER O OTHER NR NOT REPORTED 1 GL 23 5117 1738 6507064 NR 2 COMM INOPERATIVE. REPLACED STRAPPING PC CARD ON NR 2 COMM UNIT, OPERATION NORMAL CHECKED 1 & 2 TRANSPONDERS. 2 L 7 2 4F 4 F A9NM E6WE 2001121300100 20011213 00100 2001 12 13 UG82001F00005 4 20010907 A 3440 7014940901 MODULE CESSNA 750 750 2076810 CE ALLSN AE300 AE3007A GL E/E BAY FAILED E UG8A O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 5114 2329 7500017 PRIOR TO TAXI THE CREW NOTED AND AMBER CONFIG MISMATCH CAS MESSAGE. FAILED NR 2 CONFIGURATION MODULE. REPLACED NR 2 CO NFIGURATION MODULE PER AMM. OPERATIONAL CHECK IS GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2001121300101 20011213 00101 SO 2001 12 13 UG82001F00006 1 20010911 A 2913 3029091001 PUMP GULSTM GV GV 3980116 SO RROYCE BR700 BR700710A110 NE RT ENGINE DAMAGED E UG8A O OTHER O OTHER NR NOT REPORTED 1 GL 23 910DC 1052 544 ENGINE DRIVEN HYDRAULIC PUMP, DAMAGED. 2 L 7 2 4F 4 F RT A12EA E00057EN 2001121300102 20011213 00102 SO 2001 12 13 UG82001F00007 1 20010911 A 2913 3029091001 PUMP GULSTM GV GV 3980116 SO RROYCE BR700 BR700710A110 NE LT ENGINE DAMAGED E UG8A O OTHER O OTHER NR NOT REPORTED 1 GL 23 910DC 1052 544 ENGINE DRIVEN HYDRAULIC PUMP, DAMAGED. 2 L 7 2 4F 4 F RT A12EA E00057EN 2001121300103 20011213 00103 CE 2001 12 13 UG82001F00008 1 20011005 A 2910 HYDRAULIC SYSTEM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL LEFT MALFUNCTIONED E UG8A O OTHER E J VIBRATION/BUFFET WARNING INDICATION NR NOT REPORTED 1 GL 23 5116 7500019 VIBRATION FELT ON CABIN FLOOR AS WELL AS HUM. LEFT HYDRAULIC (A) SYSTEM FLUCTUATED BETWEEN 2400-3300 PSI. WHEN GEAR WAS SELECTED DOWN LEFT HYDRAULIC PRESSURE WAS 2100 AND RIGHT HAD AN OT(AMBER) LIGHT. UPON LANDING THEY GOT A (B) SYSTEM FA LL MESSAGE, BOTH SYSTEM PRESSURES WERE 1800 PSI. APPARENT CAUSE: HYDRAULIC SYSTEM MALFUNCTIONED. MAINTENANCE CORRECTIO N IN PROGRESS. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2001121300104 20011213 00104 CE 2001 12 13 UG82001F00009 1 20011018 A 2910 99144644 POWER UNIT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL HYDRAULIC SYS FAILED E UG8A O OTHER E J VIBRATION/BUFFET WARNING INDICATION NR NOT REPORTED 1 GL 23 5116 2369 7500019 VIBRATION FELT ON CABIN FLOOR AS WELL AS HUM. LT HYD (A) SYSTEM FLUCTUATED BETWEEN 2400-3300 PSI. WHEN GEAR WAS SELECTE D DOWN LT HYD PRES WAS 2100 AND RT HAD AN OT (AMBER) LIGHT. UPON LANDING THEY GOT A (B) SYSTEM FAIL MESSAGE, BOTH SYSTE M PRESSURES WERE 1800 PSI. HYDRAULIC SYSTEM MALFUNCTION DUE TO FAILED HYDRAULIC POWER TRANSFER UNIT. FAILED UNIT CAUSE CONTAMINATION IN THE LEFT HYDRAULIC SYSTEM WHICH NECESSITATED THE REPLACEMENT OF THE LEFT HYDRAULIC PUMP, ALL (A) SYSTE M FILTERS AND FLUSHING AND BLEEDING OF THE HYDRAULIC SYSTEM. REPLACED THE HYDRAULIC SYSTEM PTU, LEFT ENGINE DRIVEN PUMP AND ALL (A) SYSTEM FILTERS. HYDRAULIC SYSTEM WAS FLUSHED AND BLED PER AIRCRAFT MAINTENANCE MANUAL. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2001121300105 20011213 00105 CE 2001 12 13 UG82001F00010 1 20011024 A 5270 S32441 SWITCH CESSNA 750 750 2076810 CE ALLSN AE300 AE3007A GL CABIN DOOR BENT E UG8A O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 23 5114 2396 7500017 DOOR LIGHT WONT EXTINGUISH. MALFUNCTION OF CABIN DOOR WARNING SYSTEM. STRAIGHTENED FORWARD LOWER DOOR SWITCH PLUNGER, OPS CHECK NORMAL. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2001121300106 20011213 00106 CE 2001 12 13 UG82001F00011 1 20011120 A 2742 991450911 SEAL CESSNA 750 750 2076810 CE ALLSN AE300 AE3007A GL ACTUATOR DAMAGED E UG8A K NONE O OTHER IN INSP/MAINT 1 GL 23 5115 1371 1371 7500018 HORIZONTAL STABILIZER TRIM ACTUATOR TEFLON SEAL ON JACKSCREW DAMAGED AND PROTRUDING. FOUND DURING SCHEDULED LUBRICATION CALL OUT. REPLACED WITH SERVICEABLE UNIT.(K) 2 L 7 2 4J 4 F RT T00007WI TE6CH 2001121300107 20011213 00107 EA 2001 12 13 UNI2001F00000 2 20011012 A 7310 3032917 FUEL LINE CESSNA 208 208B 2073701 CE PWA PT6 PT6* 52043 EA ENGINE SPLIT A UNIA O OTHER R PARTIAL RPM/PWR LOSS IN INSP/MAINT 1 WP 11 127HA 7269 208B0148 PCE17154 WHILE PERFORMING A ROUTINE PERFORMANCE RUN THE TORQUE AND FUEL FLOW DROPPED. FOUND METERED FUEL FLOW TUBE FROM FUEL FLO W TRANSMITTER TO FCU SPLIT ON INBOARD SIDE ABOUT 1 INCH LONG IN THE CENTER BEND RADIUS. NEW TUBE INSTALLED, LEAK CHECKE D AND RETURNED TO SERVICE. 1 H 7 1 3T 3 T A37CE E2NE 2001121300108 20011213 00108 EU 2001 12 13 UO22001F00007 1 20010727 A 2520 303620301B8051 SEAT BELT ISRAEL GALAXY GALAXY 4500307 EU PWA 306 PW306B NE CABIN MISMANUFACTURED B UO2R K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 19 62GX 031 ON THREE NEW SEAT BELTS, THE METAL CLASP PART ON THE MALE SIDE, WAS .032 INCHES TO .040 INCHES TOO WIDE TO INSERT IN THE 1.125 INCH RECEPTACLE. 2 L 7 2 4F 4 F RT A53NM E35NE 2001121300109 20011213 00109 EU 2001 12 13 UO22001F00008 1 20010727 A 3610 NAS5201216 COUPLING ISRAEL GALAXY GALAXY 4500307 EU PWA 306 PW306B NE BLEED AIR SPLIT A UO2R O OTHER O OTHER NR NOT REPORTED 1 GL 19 168EC 25 038 FOUND THIS CABIN PRESSURIZATION, LOW PRESSURE, BLED AIR COUPLING(HOSE) SPLIT. THE SPLIT WAS APPROX 1 INCH FROM THE END OF THE HOSE AND 50 PERCENT AROUND IT, RUNNING PARALLEL TO ITS END. UNABLE TO DETERMINE IF IT SPLIT WAS CAUSED BY DAMAGE AT INSTALLATION OR FAULTY HOSE. 2 L 7 2 4F 4 F RT A53NM E35NE 2001121300110 20011213 00110 EU 2001 12 13 UO22001F00009 1 20010809 A 5620 4AS3421001009 CLIP ISRAEL GALAXY GALAXY 4500307 EU PWA 306 PW306B NE CABIN WINDOW BROKEN B UO2R K NONE O OTHER IN INSP/MAINT 1 GL 19 168EC 25 038 FOUND THE WINDOW CLIP, PN 4AS3421001009 LOCATED AT THE 7 O'CLOCK POSITION ON THE LEFT HAND NR 4 WINDOW COMPLETELY BROKEN OFF, APPROXIMATELY 1.40 INCHES FROM THE SCREW HOLD DOWN END. THE BREAK RAN NEARLY STRAIGHT, AND NEARLY PARALLEL WITH T HE EDGE OF THE WINDOW. UNABLE TO DETERMINE IF CAUSE WAS BY DAMAGE AT INSTALLATION OR FAULTY PART. INSPECTION OF THESE PARTS IS DIFFICULT DUE TO THE PART BEING COATED WITH A THIN RUBBER MATERIAL. 2 L 7 2 4F 4 F RT A53NM E35NE 2001121300111 20011213 00111 WP 2001 12 13 UO22001F00010 2 20010926 A 7250 30723112 BLADE BRAERO DH125 HS125700A 4230170 EU GARRTT TFE731 TFE7313R1H 29001 WP ENGINE FAILED B UO2R E ENGINE SHUTDOWN O OTHER NR NOT REPORTED 1 GL 19 913V 3693 NA0345 FIRST STAGE LPT BLADE FAILED CAUSING MAJOR DAMAGE TO RELATED TURBINE PARTS AND RESULTING IN AN INFLIGHT SHUT DOWN. 2 L 7 2 4F 4 F A3EU E6WE 2001121300112 20011213 00112 WP 2001 12 13 UO22001F00011 2 20011018 A 7260 3587523 BEARING HAWKER BAE125 BAE125700B 7450007 EU GARRTT TFE731 TFE7313R 01518 WP TOWER SHAFT FAILED A UO2R O OTHER O OTHER NR NOT REPORTED 1 GL 19 405TP 6098 257130 P84295 LOWER TOWER SHAFT BEARING FAILED CAUSING DAMAGE TO RELATED SHAFT AND CARRIERS ALSO CAUSING METAL CONTAMINATION TO OIL SY STEM. 2 L 7 2 4F 4 F RT A3EU E6WE 2001121300113 20011213 00113 SO 2001 12 13 V0X2001F00000 1 20011022 A 2140 A23D047 REGULATOR VALVE JANITROL PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA HEATER LEAKING E VOXA O OTHER K FLUID LOSS NR NOT REPORTED 1 NM 07 27423 5019140 317752173 VALVE WAS REPLACED WITH NEW. HEATER OPERATED 30.4 HOURS SINCE WORK ACCOMPLISHED NEW VALVE DEVELOPED FUEL LEAK AT SOLENO ID. (LARGE)(LEAK) REPLACED VALVE AGAIN. 1 L 7 2 3O 3 O A20SO E14EA 2001121300114 20011213 00114 SO 2001 12 13 VDQ2001F00000 2 20011012 A 8530 CYLINDER CESSNA 207 T207 2073612 CE CONT O520 GTSIO520C 17032 SO ENGINE CRACKED A VDQC K NONE O OTHER IN INSP/MAINT 1 AL 03 90193 781 20700007 ALL 6 CYLINDER CRACKED AT 781.6 HOURS SINCE NEW. SERIAL NUMBERS: 52A0016149, 52A0016150, 52A0016201, 52A0016202, 52A0016 215, 52A0016217 1 H 7 1 3O 3 O A16CE E7CE 2001121300115 20011213 00115 SO 2001 12 13 VDQ2001F00001 2 20011012 A 8530 CYLINDER CESSNA 207 T207 2073612 CE CONT O520 GTSIO520C 17032 SO ENGINE CRACKED A VDQC K NONE O OTHER IN INSP/MAINT 1 AL 03 90193 781 20700007 ALL 6 CYLINDERS CRACKED AT 781.6 HOURS SINCE NEW. SERIAL NUMBERS: 52A0016149, 52A0016150, 52A0016201, 52A0016202, 52A00 16215, 52A0016217. 1 H 7 1 3O 3 O A16CE E7CE 2001121300116 20011213 00116 SO 2001 12 13 VDQ2001F00002 2 20011012 A 8530 CYLINDER CESSNA 207 T207 2073612 CE CONT O520 GTSIO520* 17032 SO ENGINE CRACKED A VDQC K NONE O OTHER IN INSP/MAINT 1 AL 03 90193 781 20700007 ALL 6 CYLINDER CRACKED AT 781.6 HOURS SINCE NEW. SERIAL NUMBERS: 52A0016149, 52A0016150, 52A0016201, 52A0016202, 52A001 6215, 52A0016217. 1 H 7 1 3O 3 O A16CE E7CE 2001121300117 20011213 00117 SO 2001 12 13 VDQ2001F00003 2 20011012 A 8530 CYLINDER CESSNA 207 T207 2073612 CE CONT O520 GTSIO520C 17032 SO ENGINE CRACKED A VDQC K NONE O OTHER IN INSP/MAINT 1 AL 03 90193 20700007 ALL 6 CYLINDERS CRACKED AT 781.6 HOURS SINCE NEW. SERIAL NUMBERS: 52A0016149, 52A0016150, 52A0016201, 52A0016202, 52A00 16215, 52A0016217. 1 H 7 1 3O 3 O A16CE E7CE 2001121300118 20011213 00118 SO 2001 12 13 VDQ2001F00004 2 20011012 A 8530 CYLINDER CESSNA 207 T207 2073612 CE CONT O520 GTSIO520* 17032 SO ENGINE CRACKED A VDQC K NONE O OTHER IN INSP/MAINT 1 AL 03 90193 20700007 ALL 6 CYLINDERS CRACKED AT 781.6 HOURS SINCE NEW. SERIAL NUMBERS: 52A0016149, 52A0016150, 52A0016201, 52A0016202, 52A001 6215, 52A0016217. 1 H 7 1 3O 3 O A16CE E7CE 2001121300119 20011213 00119 SO 2001 12 13 VDQ2001F00005 2 20011012 A 8530 CYLINDER CESSNA 207 T207 2073612 CE CONT O520 GTSIO520* 17032 SO ENGINE CRACKED A VDQC K NONE O OTHER IN INSP/MAINT 1 AL 03 90193 781 20700007 ALL 6 CYLINDERS CRACKED AT 781.6 HOURS SINCE NEW. SERIAL NUMBERS: 52A0016149, 52A0016150, 52A0016201, 52A0016202, 52A00 16215, 52A0016217. 1 H 7 1 3O 3 O A16CE E7CE 2001121300120 20011213 00120 SO 2001 12 13 VJ32001F00001 2 20011029 A 7314 64621216A2 PUMP BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO ENGINE LEAKING B VJ3R O OTHER K FLUID LOSS NR NOT REPORTED 1 WP 07 5582X 887 CE1353 820397R LEAKING FUEL FROM CASE DRAIN. 1 L 7 1 3O 3 O 3A15 E5CE 2001121300121 20011213 00121 SO 2001 12 13 VJ32001F00002 2 20011029 A 7414 M3004 BRUSHES SLICK BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO MAGNETO WORN B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 5521A 455 01041993 CE1338 820460R MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNE TO AND FOUND THE CARBON BRUSH WORN. CARBON DUST WAS FOUND ON THE FLAT PART OF THE CAP. WHERE IT LOOKS LIKE A SMALL SPA RK LINE TO GROUND. THE WEAR ON THIS BRUSH IS ABOVE NORMAL FOR 500 HOURS (PN M3004 BRUSH). 1 L 7 1 3O 3 O 3A15 E5CE 2001121300122 20011213 00122 SO 2001 12 13 VJ32001F00003 2 20011029 A 7414 M3004 BRUSHES SLICK BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO MAGNETO WORN B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 8268T 998 00051555 CE1547 820321 MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISRUPTER BLOCK FROM MAGNETO AND FOUND THE CARBON BRUSH WORN. CARBON DUST WAS FOUND ON THE FLAT PART OF THE CAP. WHERE IT LOOKS LIKE A SMALL SPARK LINE TO GROUND. THE WEAR ON THIS BRUSH IS ABOVE NORMAL FOR 500 HOURS. (PN M3004 BRUSH) 1 L 7 1 3O 3 O 3A15 E5CE 2001121300123 20011213 00123 SO 2001 12 13 VJ32001F00004 2 20011029 A 7414 M3004 BRUSHES SLICK BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO MAGNETO WORN B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 38071 504 00111836 CE935 820386R MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNE TO AND FOUND THE CARBON BRUSH WORN. CARBON DUST WAS FOUND ON THE FLAT PART OF THE CAP. WHERE IT LOOKS LIKE A SMALL SPA RK LINE TO GROUND. THE WEAR ON THIS BRUSH IS ABOVE NORMAL FOR 500 HOURS. (PN M3004 BRUSH) 1 L 7 1 3O 3 O 3A15 E5CE 2001121300124 20011213 00124 SO 2001 12 13 VJ32001F00005 2 20011029 A 7414 M3004 BRUSHES SLICK BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO MAGNETO WORN B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 38071 504 00111749 CE935 820386R MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNE TO AND FOUND THE CARBON BRUSH WORN. CARBON DUST WAS FOUND ON THE FLAT PART OF THE CAP. WHERE IT LOOKS LIKE A SMALL SPA RK LINE TO GROUND. THE WEAR ON THIS BRUSH IS ABOVE NORMAL FOR 500 HOURS. (PN M3004 BRUSH) 1 L 7 1 3O 3 O 3A15 E5CE 2001121300125 20011213 00125 SO 2001 12 13 VJ32001F00006 2 20011029 A 7324 6314272A20 FLOW DIVIDER BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO ENGINE STICKS B VJ3R O OTHER O OTHER NR NOT REPORTED 1 WP 07 5582X 887 CE1353 820397R ENGINE RUN ROUGH AND SOMETIME WOULD NOT SHUT DOWN. THE FUEL FLOW DIVIDER WOULD STICK OPEN LETTING FUEL TOO CONTINUAL TO THE ENGINE. THE FLOW DIVIDER WAS REMOVED AND REPLACED WITH A NEW ONE, OPERATION OF ENGINE CHECKED OUT NORMAL. 1 L 7 1 3O 3 O 3A15 E5CE 2001121300126 20011213 00126 SO 2001 12 13 VJ32001F00007 2 20011029 A 7414 M3004 BRUSHES SLICK BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO MAGNETO WORN B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 5521A 455 01042023 CE1338 820460R MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNE TO AND FOUND THE CARBON BRUSH WORN. CARBON DUST WAS FOUND ON THE FLAT PART OF THE CAP. WHERE IT LOOKS LIKE A SMALL SPA RK LINE TO GROUND. THE WEARER ON THIS BRUSH IS ABOVE NORMAL FOR 500 HOURS. (PN M3004 BRUSH) 1 L 7 1 3O 3 O 3A15 E5CE 2001121300127 20011213 00127 SO 2001 12 13 VJ32001F00008 2 20011029 A 7414 M3004 BRUSHES SLICK BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO MAGNETO WORN B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 8268T 998 00051554 CE1547 820321 MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNE TO AND FOUND THE CARBON BRUSH WORN. CARBON DUST WAS FOUND ON THE FLAT PART OF THE CAP, WHERE IT LOOKS LIKE A SMALL SPAR K LINE TO GROUND. THE WEAR ON THIS BRUSH IS ABOVE NORMAL FOR 500 HOURS.(PN M3004 BRUSH) 1 L 7 1 3O 3 O 3A15 E5CE 2001121300128 20011213 00128 SO 2001 12 13 VJ32001F00009 2 20011108 A 7414 M3004 BRUSHES SLICK BEECH 33 F33A 1151425 CE CONT O520 IO520* 17032 SO MAGNETO WORN B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 5585Y 01042022 CE1389 820461R MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW THE MAINTENANCE MANUAL. REMOVED THE REAR COVER AND THE DISTRIBU TOR BLOCK FROM MAGNETO AND FOUND THE CARBON BRUSH WORN. CARBON DUST WAS FOUND ON THE FLAT PART OF THE CAP. WHERE IT LO OKS LIKE A SMALL SPARK LINE TO GROUND. THE WEAR ON THIS BRUSH IS ABOVE NORMAL FOR 500 HOURS (PN M3004 BRUSH) 1 L 7 1 3O 3 O 3A15 E5CE 2001121300129 20011213 00129 SO 2001 12 13 VJ32001F00012 2 20011109 A 7414 DISTRIBUTOR BLK BEECH 33 F33A 1151425 CE CONT O520 IO520B 17032 SO MAGNETO FAILED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 1565A 1003 00050391 CE1331 820311R MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNE TO. DISTRIBUTOR BLOCK ASSEMBLY SENT TO MFG FOR INSPECTION. NEW DISTRIBUTOR BLOCK ASSEMBLY INSTALLED IN MAGNETO. 1 L 7 1 3O 3 O 3A15 E5CE 2001121300130 20011213 00130 EU 2001 12 13 RAIA0011102 1 20011106 A 2721 1415502297 BRACKET JETAIR JETSTM JETSTM4101 1500501 EU WORN A RAIA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 CE 03 558HK 41071 7003-STL-CREW REPORTED MODERATE AIRFRAME VIBRATION AT ALL POWER SETTINGS, DECREASES AND INCREASES WITH AIR SPEED. MAINTE NANCE INSPECTED AND REMOVED AND REPLACED WORN RUDDER TRIM TAB BRACKET IAW J41 MAINTENANCE MANUAL. 2 L 7 2 4T RT A41NM 2001121300131 20011213 00131 EU 2001 12 13 RAIA00108002 1 20010806 A 2120 RA50A54 SEAL AEROSP ATR72 ATR72202 8680940 EU LEFT WING L/E FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 723TE 283 7320-STL-RIGHT AIR-CONDITIONING PACK VALVE FAULTED ON TAXI, LEFT PACK VALVE FAULTED ON TAXI. MAINTENANCE INSPECTED AND C LEANED RIGHT PACK VALVE ELECTRICAL CONNECTOR, MAINTENANCE INSPECTED AND REPLACED LEFT BLEED AIR SEALS. 2 H 7 2 4T RT A53EU 2001121300132 20011213 00132 EU 2001 12 13 RAIA00104012 1 20010412 A 2621 30903894 SQUIB JETAIR JETSTM JETSTM4101 1500501 EU LEFT HAND BLOWN A RAIA O OTHER J WARNING INDICATION CL CLIMB 1 CE 03 563HK 41079 5404-EWR-DURING CLIMB LEFT ENGINE FIRE INDICATION AT 2000 FEET, FIRE BOTTLE WAS BLOWN AND WARNING LIGHT WENT OUT. MAINTE NANCE REMOVED AND REPLACED THE LEFT HAND FIRE BOTTLE, BOTH SQUIBS AND THE LEFT HAND FIFR LOOP IAW J41 MAINTENANCE MANUAL . 2 L 7 2 4T RT A41NM 2001121300133 20011213 00133 EU 2001 12 13 RAIA00104011 1 20010412 A 2621 30903894 SQUIB JETAIR JETSTM JETSTM4101 1500501 EU LEFT HAND BLOWN A RAIA O OTHER J WARNING INDICATION CL CLIMB 1 CE 03 563HK 41079 5404-EWR-DURING CLIMB LEFT HAND ENGINE FIRE INDICATION AT 2000 FEET, FIRE BOTTLE WAS BLOWN AND WARNING LIGHT WENT OUT. M AINTENANCE REMOVED AND REPLACED THE LEFT HAND FIR BOTTLE, BOTH SQUIBS, AND LEFT HAND ENGINE FIRE LOOP IAW J41 MAINTENANC E MANUAL. 2 L 7 2 4T RT A41NM 2001121300134 20011213 00134 CE 2001 12 13 WVE2001F00000 1 20010809 A 5320 3513608 BRACKET LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE A/C BAY CRACKED E WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 246FX 1075 183 DURING 14 MONTH INSPECTION, THE MOUNTING BRACKET FOR THE AIR CONDITIONER COMPRESSOR WAS FOUND CRACKED APPROX. 2 INCHES L EFT MOUNTING BOLT POSITION AT FORWARD FLANGE. THIS SAME BRACKET WAS FOUND CRACKED. PROBABLE CAUSE: METAL FATIGUE. 2 L 7 2 4F 4 F RT A10CE E35NE 2001121300135 20011213 00135 SO 2001 12 13 YWB2001F00000 2 20010924 A 8520 6466131 CRANKCASE BEECH 58 58 1152740 CE CONT O550 IO550C SO ENGINE CRACKED B YWBR K NONE K FLUID LOSS IN INSP/MAINT 1 WP 17 873AN 528 TH1680 DURING ROUTINE INSPECTION AN OIL LEAK WAS NOTICED AFT OF NR 2 CYLINDER. FURTHER INVESTIGATION REVEALED CRACK IN CRANKCA SE STARTING AT 7TH STUD LOCATION NR 2 CYLINDER RUNNING AFT APPROX 2 INCHES IN LENGTH ENGINE REMOVED FROM SERVICE. 1 L 7 2 3O 3 O 3A16 E3SO 2001121900022 20011219 00022 SO 2001 12 19 C2XA01IA411 1 20011207 A 3350 AD2047 BATTERY EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16731 120190 IAH- DURING MAINTENANCE TEST IT WAS NOTED THAT THE FLOOR EMERGENCY AISLE PATH LIGHT STRIP IN THE AFT CABIN FAILED TO IL LUMINATE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY BATTERY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LI GHTING SYSTEM, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001121400001 20011214 00001 SO 2001 12 14 C2XA01IA412 1 20011209 A 3350 AD2047 BATTERY EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 40717 120133 IAH- DURING MAINTENANCE TEST OF THE EMERGENCY LIGHTING SYSTEM IT WAS NOTED THAR THE FORWARD SECTION OF THE CABIN EMERGE NCY LIGHT STRIP FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 1 EMERGENCY BATTERY, PERFORMED A OPER ATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001121400002 20011214 00002 EU 2001 12 14 C2XA01IA414 1 20011213 A 3610 ASNA214505 CLAMP AEROSP ATR42 ATR42320 8680930 EU ENGINE DAMAGED A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 93840 271 IAH- FLIGHT 3699, NUMBER 1 ENGING ON CLIMB OUT @ 200 FEET EXCEEDED 800 DEGREES C. ON ITT. WE COULD ONLY MAINTAIN 45% T ORQUE WITHOUT EXCEEDING THE ITT LIMITATION. THEREFORE, RETURNED FO0R PRECAUTIONARY LANDING. IAH. MAINTENANCE REMOVED AND REPLACED A DAMAGED BAND CLAMP ON HP BLEED VALVE,PREFORMED A OPERATIONAL CHECK OF THE ENGINE,NO DEFECTS NOTED,AND, TH E AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001121400003 20011214 00003 NM 2001 12 14 CALA0101026 1 20011212 A 5210 WEB BOEING 737 7373T0 1384582 NM L-1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14307 23358 INSPECTION FOUND A 2" CRACK IN L-1 DOOR LOWER FORWARD WEB AT LOWER FORWARD STOP FITTING. THE CRACK WAS STOP DRILLED. A D OUBLER AND RADIUS BLOCK REPAIR WAS INSTALLED IAW ECRA 5265-01005 REV D AND ECRA 5210-01461. 2 L 7 2 4F RT A16WE 2001121400004 20011214 00004 NM 2001 12 14 CALA0101027 1 20011212 A 5511 SPAR CAP BOEING 737 7373T0 1384582 NM R/H HOR STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14307 23358 INSPECTION FOUND R/H HORIZONTAL STABILIZER AFT UPPER SPAR CAP CORRODED ON TOP SIDE O/B END UNDER T/E SKIN PANEL. REPAIRE D IAW ECRA 5510-01611. 2 L 7 2 4F RT A16WE 2001121400005 20011214 00005 NE 2001 12 14 MALA010793 2 20011211 A 7230 BLEED BAND BAC 146 AVRO146RJ85A 1500097 EU LF507 LF5071F NE BROKEN A MALA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 GL 15 515XJ E2333 During Climbout on Flight #3589, #4 Engine would not produce max cond. on departure without Over Temp.(Temp 648 for 19 S ec) Air return to MSP. Maintenance replaced broken Bleed Band and completed Borescope Inspection of Combustor and 1st Turbine nozzle due to Overtemp. Found to be serviceable. 2 H 7 4 4F 4 F RT A49EU E6NE 2001121400006 20011214 00006 EA 2001 12 14 VK62001F00000 1 20010302 A 2752 SC14000062 BEARING EATON CNDAIR CL600 CL6002B19 1900309 EA FLAP ACTUATOR FAILED B VK6R O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 GL 09 VHKJU 1195 1393 CL657405 THRUST BEARING FAILURE DUE TO LACK OF LUBRICATION AND POSSIBLE PRELOAD CONDITION. 2 L 7 2 4F RT A21EA 2001121400009 20011214 00009 NM 2001 12 14 A6WA200100065 1 20011127 A 7110 SERVICE DOOR DORNER DO32 DO328100 2996000 NM COWLING OPEN A A6WA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 340LS 3040 OIL SERVICE DOOR ON COWL 422BL OPENED INFLIGHT. MAINTENANCE SECURED DOOR CLOSED. INSPECTED COWL, NO DAMAGE NOTED. 2 H 7 2 4T RT A45NM 2001121400010 20011214 00010 NM 2001 12 14 A6WA200100066 1 20011207 A 7920 OIL FILTER DORNER DO32 DO328100 2996000 NM PWA 119 PW119C NE NR 1 ENGINE OBSTRUCTED A A6WA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 31 335PH 3013 PCE116036 LEFT ENGINE OIL PSI HIGH IN CRUISE. MAINTENANCE FOUND LT BYPASS FILTER CAS MESSAGE. REMOVED AND REPLACED NR 1 OIL FILT ER AND SCAVENGE FILTERS. 2 H 7 2 4T 4 T RT A45NM E20NE 2001121400011 20011214 00011 WP 2001 12 14 ABXA010601 1 20011112 A 5312 9911500129 BULKHEAD DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 CRACK AT RIVET ON FORWARD FACE OF STATION 37 BULKHEAD, APPROXIMATELY 18 LEFT. REPAIRED AREA IAW DC-9 SRM 53-01. 2 L 7 2 4F A6WE 2001121400012 20011214 00012 WP 2001 12 14 ABXA010607 1 20011113 A 5711 59113041 SPAR DOUG DC9 DC933F 302207A WP CENTER WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 LEFT UPPER REAR SPAR HAD A HORIZONTAL CRACK IN THE UPPER INBOARD CORNER FROM LEFT BUTT LINE 5 TO BUTT LINE 0. REPAIRED AREA IAW DC-9 SRM 57. 2 L 7 2 4F A6WE 2001121400013 20011214 00013 WP 2001 12 14 ABXA010613 1 20011114 A 5320 99107557 WEB DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 CUSP WEB CRACKED BETWEEN STATION 870 AND 889 AT LEFT BUTT LINE 54. REPAIRED CUSP WEB IAW DC-9 SRM 53-01. 2 L 7 2 4F A6WE 2001121400014 20011214 00014 NM 2001 12 14 ABXA010615 1 20011129 A 7603 SWITCH BOEING 767 767281 1385109 NM THROTTLE WORN A ABXA K NONE O OTHER TX TAXI/GRND HDL 1 GL 23 769AX 22787 DURING TAXI INTO GATE, THE NR 2 THRUST REVERSER DEPLOYED UNCOMMANDED, WOULD NOT STOW. DFDR DATA WAS REVIEWED AND THE DA TA SHOWED THAT THE REVERSER DID NOT STOW AFTER LANDING. THE THROTTLE MICROSWITCH PACK WAS FOUND WORN WHICH PREVENTED TH E THRUST REVERSER FROM STOWING AFTER LANDING. MICROSWITCH PACK WAS REPLACED IAW DC-9 MM. OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2001121400015 20011214 00015 WP 2001 12 14 ABXA010616 1 20011128 A 2611 26AA191 PANEL DOUG DC9 DC941 302207N WP COCKPIT DEFECTIVE A ABXA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 990AX 47493 ON SHORT FINAL AT BHM, THE NR 9 CARGO SMOKE DETECTOR STARTED BLINKING. NO SMOKE OBSERVED. REPLACED THE SMOKE DETECTOR PANEL. OPS CHECKED GOOD IAW DC-9 MM. 2 L 7 2 4F A6WE 2001121400016 20011214 00016 WP 2001 12 14 ABXA010617 1 20011130 A 5315 4640968 FLOORBEAM DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 817AX 45928 FLOORBEAM CRACKED AND EXFOLIATED CORROSION IN THE LEFT WHEEL WELL AT FS STATION 902, LEFT BUTT LINE 50. REPLACED THE FL OORBEAM IAW DC-8 MM AND REA D853-42779. 2 L 7 4 4F 4A25 2001121400017 20011214 00017 WP 2001 12 14 ABXA010618 1 20011202 A 3230 56165545503ABXA1 CYLINDER DOUG DC8 DC863 302198A WP RT MLG DEFECTIVE A ABXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 822AX 2154 46079 WHEN GEAR HANDLE WAS PLACED IN THE UP POSITION AFTER TAKEOFF, THE REG GEAR UNSAFE LIGHT STAYED ON. ALL GREEN LIGHTS WER E OUT. THE RIGHT MAIN LANDING GEAR DOOR NOT LOCKED LIGHT WAS ON. ABNORMALS COMPLETE. REPLACED THE RIGHT BOGIE TRIM CY LINDER DUE TO SWIVEL DETACHED FROM TRIM CYLINDER. NEW CYLINDER INSTALLED BY ALTERNATE METHOD IAW DC-8 MM 32-33-01-2. O PS AND LEAK CHECKED GOOD. 2 L 7 4 4F 4A25 2001121400018 20011214 00018 WP 2001 12 14 ABXA010619 1 20011129 A 5230 HANDLE DOUG DC8 DC863F 302198F WP CARGO DOOR UNSECURE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 THE CARGO DOOR HAND CRANK TOOL DID NOT STOW PROPERLY TO HOLDING CLIPS PREVENTING CREW EGRESS SAFETY OF FLIGHT. INSTALLE D VELCRO TO HOLD CARGO DOOR HAND CRANK. 2 L 7 4 4F 4A25 2001121400019 20011214 00019 WP 2001 12 14 ABXA010621 1 20011126 A 5313 59114279 LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 949AX 47325 LONGERON 17 LEFT WAS CRACKED ON UPPER AND LOWER FLANGE AT STATION 945 FRAME. REPAIRED AREA IAW DC-9 SRM 53-02. 2 L 7 2 4F A6WE 2001121400020 20011214 00020 WP 2001 12 14 ABXA010622 1 20011127 A 5320 D0489832 WEB DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 949AX 47325 CUSP WEB CRACKED AT SEAT TRACK HOLE RIGHT BUTT LINE 54, STATION 795. REPAIRED CUSP WEB IAW DC-9 SRM 51-00. 2 L 7 2 4F A6WE 2001121400021 20011214 00021 WP 2001 12 14 ABXA010623 1 20011203 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC932 3022066 WP COCKPIT DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 986AX 47543 COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC-9 MM 33-53-0. 2 L 7 2 4F A6WE 2001121400022 20011214 00022 NE 2001 12 14 ANCF200100022 2 20011201 A 7200 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE LEFT MALFUNCTIONED W ANCF A UNSCHED LANDING J R WARNING INDICATION PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 23 632CT 49632 P725455D AFTER TAKEOFF, LT ENGINE WAS REDUCED DUE TO IMPENDING HIGH EGT (576°C), THE BEHAVIOR OF THE LEFT ENGINE WAS NORMAL UNTIL CLIMBING, THROUGH APPROXIMATELY FL 280, A STRONG STALL NOISE WAS FELT WITH AIRCRAFT YAWING. LT ENGINE EPR WAS DECREASE D AND EGT ROSE UP. ENGINE WAS REDUCED TO IDLE UNTIL LANDING. FLIGHT RETURNED TO PTY. CHECK PROCEDURES WERE ACCOMPLISH ED IAW AMM 72-00-00 AND FUEL CONTROL WAS REPLACED. ENGINE STALL DURING TEST. LT ENGINE WAS REPLACED. 2 L 7 2 4F 4 F RT A6WE E9NE 2001121400023 20011214 00023 NE 2001 12 14 ANCF200100023 2 20011203 A 7320 SENSE LINE DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE RT ENGINE LOOSE W ANCF A UNSCHED LANDING O OTHER CR CRUISE 1 SO 23 583AN 53183 P726832D IN ALL PHASES OF FLIGHT THE ENGINE PARAMETERS PRESENT A LARGE DIFFERENCE, IN ORDER TO MAINTAIN EPRS THRUST LEVERS HAVE T O BE PLACE TWO KNOBS, LEFT FURTHER FWD THAN RIGHT. FLIGHT RETURNED TO BOG. RT ENGINE PT2 LINES WERE ADJUSTED AND TIGHT ENED IAW TROUBLESHOOTING AMM 71-11-01 PG 505. RUN UP TEST WAS PERFORMED OK, WITH LT AND RT ENGINES. 2 L 7 2 4F 4 F RT E9NE 2001121400024 20011214 00024 WP 2001 12 14 ARWA20011123 1 20011130 A 3246 26014112 WHEEL DOUG DC8 DC863 302198A WP LT MLG BROKEN A ARWA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 19 345JW 49 46042 AFTER LANDING IN SDQ NR 3 WHEEL INBOARD BROKE AND NR 3 TIRE EXITED THE WHEEL. NR 3 TIRE AND HUB CAUSED DAMAGE TO LT MLG DOOR AND NR 1 ENGINE COWLING, NR 1 OSCILLANTING RING, LT GEAR DOOR BRACKET. REMOVED AND REPLACED NR 3 AND NR 4 MAIN WH EEL ASSY IAW MM 32-40-1. AIRCRAFT WAS FERRIED, WHERE THE REPAIRS WILL BE ACCOMPLISHED. AIRCRAFT RETURN TO REVENUE SERV ICE. 2 L 7 4 4F 4A25 2001123100020 20011231 00020 WP 2001 12 31 ARWA20011201 1 20011201 A 2410 CSD DOUG DC8 DC85F54 3021926 WP NR 4 ENGINE FAILED A ARWA C ABORTED TAKEOFF J H WARNING INDICATION ELECT. POWER LOSS-50 PC TO TAKEOFF 1 SO 19 426FB 45667 ON TAKEOFF AT KMIA, NR 4 GENERATOR ZNS FAULT; ABORTED TAKEOFF AT 90 KTS AND F/O LOST LIGHTS, INSTRUMENTS AND RADIO COMMU NICATION. F/O'S INSTRUMENTS AND LIGHT OPS CK NORMAL AFTER BUS RESET IAW MM 23-2-0 & 24-1-0. REMOVED AND REPLACED NR 4 E NGINE CSD ASSY IAW MM 24-1-3. ALSO REMOVED AND REPLACED NR 4 AC CONTROL PANEL IAW MM 24-5-7, OPS CHECKED NORMAL IAW MM 24-5-0; OPS CHECKED NORMAL RUN UP IAW MM 71-00 & 24-7-0 & 24-0. 2 L 7 4 4F RT 4A25 2001121400025 20011214 00025 2001 12 14 ARWA20011202 4 20011203 A 3422 25883024 GYRO DOUG DC8 DC862 3021970 WP E/E BAY FAILED A ARWA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 810BN 45905 FIRST OFFICER'S COMPASS INOPERATIVE AFTER 1000 FEET. AIRCRAFT RETURNED TO KMIA AND PERFORMED OVERWEIGHT LANDING WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 PDI, INSTRUMENT AMPLIFIER AND DIRECTIONAL GYRO IAW MM 34-00. PERFORMED OPERATIONA L CHECK COMPASS SYSTEM IAW MM 34-21-0, FOUND ALL SYSTEM NORMAL. 2 L 7 4 4F 4A25 2001121400027 20011214 00027 EU 2001 12 14 AWXA200100594 1 20011125 A 2934 C60AA0062 SWITCH AIRBUS 320 A320231 3930325 EU HYDRAULIC SYS FAILED A AWXA O OTHER N FALSE WARNING CL CLIMB 1 WP 28 643AW 20617 315 PHX - EMERGENCY LANDING - FLT 614 - 10 MIN AFTER TAKEOFF FROM SAN TO PHX ECAM MESSAGE APPEARED FOR YELLOW HYDRAULIC SYST EM RESERVOIR LOW LEVEL. FLIGHT CONTINUED TO PHX MAKING AN UNEVENTFUL LANDING. MAINTENANCE VERIFIED NO FLUID LOSS AND T ROUBLESHOT SYSTEM REPLACING A YELLOW HYDRAULIC SYSTEM PRESSURE SWITCH 3151GN WITH NO HELP. PLACED YELLOW HYDRAULIC LOW LEVEL INDICATION ON MEL 29-30-04 COND 5. MAINTENANCE REPLACED YELLOW HYDRAULIC SYSTEM RESERVOIR LOW LEVEL SWITCH IAW AM M 29-13-41-000-004, LEAK AND OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2001121400028 20011214 00028 EU 2001 12 14 AWXA200100595 1 20011125 A 2910 NAS161212 O-RING AIRBUS 320 A320231 3930325 EU HYDRAULIC SYS LEAKING A AWXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 627AW 66 CLE - EMERGENCY LANDING - FLT 534 - C - EN ROUTE FROM PHX TO CLE RECEIVED YELLOW HYDRAULIC SYSTEM RESERVOIR LOW LEVEL QU ANTITY INDICATION WITH PRESSURE INDICATING NORMAL, 1 HR 30 MIN LATER SYSTEM LOST ALL PRESSURE. DECLARED EMERGENCY LANDI NG INTO CLE, LANDING WAS UNEVENTFUL. MAINTENANCE TROUBLESHOT AND REPLACED DEFECTIVE O-RING ON QUICK DISCONNECT COUPLING AE99116K ON YELLOW SYSTEM HYDRAULIC MANIFOLD. MAINTENANCE ALSO DISCOVERED NR 2 ENGINE HYDRAULIC PUMP CASE DRAIN FILTER DIFFERENTIAL BUTTON POPPED, AS PRECAUTION REPLACED CASE DRAIN FILTER AND NR 2 ENGINE HYDRAULIC PUMP IAW AMM 29-13-51-40 1. 2 L 7 2 4F RT A28NM 2001121400029 20011214 00029 NM 2001 12 14 AWXA200100598 1 20011123 A 3350 1012721 LIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 156AW 23778 LAS - EEL -C- DURING ROUTINE INSPECTION EMERGENCY LIGHT ON SEAT 20 LT DOES NOT ILLUMINATE. REPLACED SEAT LIGHT ASSEMBLY , OPERATIONALLY CHECKED GOOD. 2 L 7 2 4F RT A16WE 2001121400030 20011214 00030 NM 2001 12 14 AWXA200100599 1 20011127 A 3350 900835A BATTERY PACK BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 184AW 22651 PHX - EEL - C - DURING ROUTINE MAINTENANCE INSPECTION FOUND R1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLA CED BATTERY PACK AT R1 DOOR, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2001121400031 20011214 00031 NM 2001 12 14 AWXA200100603 1 20011127 A 2130 VFT300B00 VALVE AIRBUS A319 A319132 3930340 NM CABIN PRESSURE FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 820AW 467 1397 DEN - AIR TURNBACK -C - WHILE EN ROUTE ACFT RECEIVED ECAM MESSAGE FOR VENT SKIN FAULT. DURING TURN AT DEN DEACTIVATION OF THE VENT SKIN AIR VALVE WAS ACCOMPLISHED. UPON TAKEOFF FROM DEN TO LAS ECAM MESSAGE REAPPEARED AND ACFT WOULD NOT PR ESSURIZE, ACFT TURNED BACK TO DEN AND MADE UNEVENTFUL LANDING. MX TROUBLESHOT SYSTEM & FOUND VENT SKIN AIR VALVE IN OPE N POSITION. DEACTIVATION OF VENT AIR SKIN VALVE IN CLOSED POSITION WAS CORRECTLY RE-ACCOMPLISHED AND CPC TEST 1 AND 2 W AS PERFORMED WITH NO DEFECTS NOTED, ACFT WAS RETURNED TO SERVICE. REPLACED THE VENT SKIN AIR VALVE. NO FURTHER DISCREP ANCIES HAVE BEEN REPORTED. 2 L 7 2 4F RT A28NM 2001121400032 20011214 00032 NM 2001 12 14 0104695506 1 20011207 A 5330 SKIN BOEING 757 757251 1384970 NM CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 506US 23195 During "H" check found corrosion on fuselage skin from BS 640 to BS 660 BL 0. Repaired per EA 55-187420. 2 L 7 2 4F RT A2NM 2001121400033 20011214 00033 NM 2001 12 14 0104705506 1 20011207 A 5311 FRAME BOEING 757 757251 1384970 NM CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 506US 23195 During "H" check found corrosion on upper surface of fuselage frame at BS 1240 from LBL 16 to LBL 28 and BS 1260 from LB L 18 to LBL 21 and BS 1260 from RBL 19 to RBL 25. Repaired per EA 55-187411. 2 L 7 2 4F RT A2NM 2001121400034 20011214 00034 NM 2001 12 14 0104715506 1 20011206 A 5315 FLOORBOARD BOEING 757 757251 1384970 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 506US 23195 DURING "H" CHECK FOUND CRACK IN FLOORBEAM UPPER CAP AT BS 700 LBL 45. REPAIRED PER EA 55-186813. 2 L 7 2 4F RT A2NM 2001121400035 20011214 00035 EU 2001 12 14 AWXA200100606 1 20011121 A 3210 D5744359901239 BRACKET AIRBUS 320 A320232 3930326 EU LT MLG LOOSE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 651AW 866 DURING PHASE 5 INSPECTION FOUND L/E PANEL 521EB LT DISCOLORED. INVESTIGATION REVEALED DAMAGE TO 2 FIRE LOOPS, 6 GENERAT OR FEEDER WIRES, A WIRE HARNESS BRACKET, AND THE FORWARD WING SPAR INSIDE L/E FLAP BAY. DAMAGE OCCURRED WHEN HARDWARE T HAT SECURED LANDING ASSY TO AIRFRAME WORE THROUGH THE METAL. THIS ALLOWED LANDING ASSY TO BREAK FREE & LODGE BETWEEN L/ E FLAP TORQUE TUBE & GENERATOR FEEDER WIRES CHAFING THROUGH PROTECTIVE COATING ON WIRES. THIS CAUSED ARCING DAMAGE TO W IRES, HARNESS BRACKET & WING SPAR. MX REPLACED 2 FIRE LOOPS, L/E PANEL 521EB LT & WIRE HARNESS BRACKET. WING SPAR WAS BLENDED WITHIN LIMITS. GENERATOR FEEDER WIRES WERE REPAIRED. CONTINUITY CHECK & BITE TEST CHECKED GOOD ON ENG RUN. 2 L 7 2 4F RT A28NM 2001121400036 20011214 00036 NM 2001 12 14 AWXA200100607 1 20011201 A 3260 655825029 CIRCUIT BOARD BOEING 737 7373G7 1384595 NM E/E BAY FAULTY A AWXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 154AW 23776 DURING T/O, NLG RED WARN LIGHT REMAINED ILLUM AFTER L/G WAS RETRACTED. GEAR WAS SAFELY LOWERED & ACFT LANDED BACK IN PH X. MX PERFORMED CONTINUITY CHECKS FROM S78 PIN 6 TO PIN 4 ON JACK D5082J & GROUND GD-2702-DC TO PIN 51 ON PLUG D2596. BOTH CHECKS GOOD. CIRCUIT CARDS M1214, M1215, M983 WERE REPLACED ON THE E11 LOGIC SHELF, BUT RED LIGHT REMAINED. MX RE MOVED ALL CIRCUIT CARDS ON E11 SHELF & SHELF ASSY ITSELF. THE E11 SHELF ASSY & ALL CIRCUIT CARDS WERE REINSTALLED, EXCE PT ENG SPEED CARD M1190. ENG SPEED CARD M1190 WAS REPLACED. THE NLG POSITION SENSOR REPLACED, BUT RED LIGHT REMAINED. REPLACED CIRCUIT CARDS M1214, M1215, AND M983 & RED LIGHT EXTINGUISHED. ALL LOGIC CARDS CHECKED OUT. 2 L 7 2 4F RT A16WE 2001121400037 20011214 00037 EU 2001 12 14 AWXA200100609 1 20011201 A 5270 WARNING SYSTEM AIRBUS 320 A320231 3930325 EU COCKPIT MALFUNCTIONED A AWXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 28 629AW 076 LAS - ABORTED TAKEOFF - FLT 0193 - C - ON TAKEOFF ROLL RUNWAY 22R AT 60 KTS AFT CARGO DOOR OPEN INDICATION APPEARED ON E CAM; TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED UNEVENTFULLY TO THE GATE. AT THE GATE MAINTENANCE VISUALLY CONFIRMED CAR GO DOOR WAS CLOSED AND A DPI WAS ISSUED FOR MEL 52-70-01 COND 7 CARGO DOOR INDICATION INOPERATIVE AND AIRCRAFT CONTINUED ON SCHEDULED FLIGHTS. AT CMH MAINTENANCE CHECKED ALL PROXIMITY SWITCHES AND TARGETS IWA AMM 52-71-12-75-050, ALL CHECK S WERE GOOD. AIRCRAFT HISTORY WAS RESEARCHED AND VERIFIED TO HAVE NO PREVIOUS EVENTS FOR CARGO DOOR FAULTS, MEL WAS CLE ARED. 2 L 7 2 4F RT A28NM 2001121400038 20011214 00038 NM 2001 12 14 AWXA200100611 1 20011130 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319132 3930340 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 817AW 1373 LAS - EEL - O - CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLIES 11WL AND 12WL, OPERATIONAL TEST OF CABIN EMERGENCY EXIT LIGHTS WAS GOOD. 2 L 7 2 4F RT A28NM 2001121400039 20011214 00039 NM 2001 12 14 AWXA200100612 1 20011202 A 3350 900835A BATTERY PACK BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 189AW 22656 PHX - EEL - C - LT AND RT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY PACK M1053 CENTER CEILING JUST FORWARD STA 664, OPERATIONALLY CHECKED GOOD PER 33-51-11. 2 L 7 2 4F RT A16WE 2001121400040 20011214 00040 EU 2001 12 14 AWXA200100614 1 20011201 A 3350 321430 BATTERY PACK AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 648AW 770 LAS - EEL - C - EMERGENCY LIGHTS DID NOT TEST. MAINTENANCE REPLACED ALL 4 BATTERY PACKS IN EMERGENCY POWER SUPPLY UNITS 10WL (ZONE 221), 11WL (ZONE 241), 12WL (ZONE 242), AND 13WL (ZONE 263) IAW T/C R1C33301, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A28NM 2001121400041 20011214 00041 NM 2001 12 14 AWXA200100615 1 20011204 A 3350 2514303 SIGN AIRBUS A319 A319132 3930340 NM CABIN BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 814AW 1281 PHX - EEL - C - EMERGENCY EXIT SIGN HOUSING AND LENS BROKEN AT L1 DOOR. MAINTENANCE REMOVED AND REPLACED L1 EMERGENCY E XIT SIGN HOUSING AND LENS IAW AMM 33-51-16-401A. 2 L 7 2 4F RT A28NM 2001121400042 20011214 00042 NM 2001 12 14 AWXA200100618 1 20011125 A 5311 BAC14902808 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 328AW 23377 MCN - MAJOR REPAIR - C - FRAME HAS .5 INCH CRACK AT BS 500 NEAR UPPER FLANGE RBL 2 IN FORWARD CARGO COMPARTMENT AREA. M AINTENANCE CUT OUT CRACKED AREA OF FRAME AT BS 500 BETWEEN RBL 2 AND RBL 3, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW B737-300 SRM 51-70-11 PG 1, 2, 4, & 5, SRM 51-20-01 PG 10, & 47, AND SRM 51-20-01 PG 2-4. 2 L 7 2 4F RT A16WE 2001121400043 20011214 00043 NM 2001 12 14 AWXA200100620 1 20011127 A 5312 6545408245 PRESSURE PANEL BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 328AW 23377 MCN - MAJOR REPAIR - C - LT WHEEL WELL UPPER PRESSURE WEB HAS 1.5 INCH CRACK AT BS 664, LBL 32. MAINTENANCE CUT OUT DAM AGED SECTION OF PRESSURE WEB AND PERFORMED HFEC INSPECTION FOR CRACKS, NO CRACKS NOTED. FABRICATED AND INSTALLED DOUBLE R, FILLERS, AND STIFFENERS IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001121400044 20011214 00044 NM 2001 12 14 AWXA200100621 1 20011130 A 5315 654681138 FLOORBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 328AW 23377 MCN - MAJOR REPAIR - C - CORROSION FOUND ON UPPER FLOORBEAM BS 986.5, LBL 45 TO RBL 45. REMOVED AND REPLACED ENTIRE UPP ER T-CORD OF CORRODED FLOORBEAM AT BS 986.5, LBL 52 TO RBL 52 IAW AWA ER 03-5310-01334-JS2. 2 L 7 2 4F RT A16WE 2001121400045 20011214 00045 NM 2001 12 14 AWXA200100622 1 20011117 A 5320 65C807351 SILL BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 328AW 23377 MCN - MAJOR REPAIR - C - CORROSION FOUND ON INNER CHORD UNDER THRESHOLD DRAIN OF R2 DOOR. MAINTENANCE REMOVED CORROSION AND FOUND REMAINING MATERIAL TO BE OUT OF LIMITS IAW B737-300 SRM 51-40-02, PG 104-107. REMOVED AND REPLACED RT INNER CHORD FROM BS 917 TO 1016 IAW B737-300 SRM 51-40-02, PG 38 FIG 8, AND PG 10-11. 2 L 7 2 4F RT A16WE 2001121400046 20011214 00046 EU 2001 12 14 AWXA200100623 1 20011206 A 2910 HYDRAULIC LINE AIRBUS 320 A320232 3930326 EU LT MLG RUPTURED A AWXA K NONE K J FLUID LOSS WARNING INDICATION AP APPROACH 1 WP 28 638AW 455 EWR- EMERGENCY LANDING - FLT 687 - O - EN ROUTE FROM PHX TO EWR AIRCRAFT LOST GREEN HYDRAULIC SYSTEM PRESSURE ON SHORT F INAL APPROACH, PILOT DID NOT HAVE TIME TO DECLARE EMERGENCY. INITIAL MAINTENANCE FINDINGS AT EWR IDENTIFIED A RUPTURED LT MLG DOOR HYDRAULIC LINE. 2 L 7 2 4F RT A28NM 2001121400047 20011214 00047 NM 2001 12 14 AWXA200100624 1 20011114 A 5210 655287399 SKIN BOEING 737 7373G7 1384595 NM L2 DOOR DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 311AW 24712 MCN - C12 CK - C - LOWER AFT CORNER OF L2 DOOR HAS 4.1 X .5 INCH DENT IN SKIN .031 INCH DEEP AT BS 986.5. MAINTENANCE R EMOVED LOWER DOOR GATE AND CUT OUT DAMAGED PORTION OF EXTERNAL SKIN AND REMOVED BRACKET FROM INNER SKIN OF LOWER AFT COR NER L2 DOOR BS 986.5. FABRICATED AND INSTALLED DOUBLER, FILLER, AND SKIN IAW B737-300 SRM 52-00-01, PG 203-206, AND DWG 65-52873. LOWER DOOR GATE WAS REINSTALLED IAW BMM 52-13-61 PG 401. 2 L 7 2 4F RT A16WE 2001121400048 20011214 00048 NM 2001 12 14 AWXA200100625 1 20011114 A 5315 BAC1505100246 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 311AW 24712 MCN - C12 CK - C - TOP OF FLOORBEAM CORRODED AT SCREW HOLES BS 312, RBL 10. MAINTENANCE REMOVED CORRODED FLOORBEAM UPPE R CHORD AT BS 312. FABRICATED AND INSTALLED NEW FLOORBEAM UPPER CHORD AND REPAIR ANGLES IAW B737-300 SRM 53-10-51, FIG 205, PG 222 & 223. 2 L 7 2 4F RT A16WE 2002031800110 20020318 00110 NM 2002 3 18 AWXA200100629 1 20011110 A 5315 6545812 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 311AW 24712 MCN - C12 CK - C - TOP OF FLOORBEAM CORRODED AT BS 328, RBL 12 TO RBL 26. MAINTENANCE CLEANED CORROSION AND PERFORMED D EPTH CHECK (OUT OF LIMITS). 2 L 7 2 4F RT A16WE 2001121400049 20011214 00049 NM 2001 12 14 AWXA200100634 1 20011129 A 5315 6545410163 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 311AW 24712 MCN - C12 CK - C - .25 INCH CRACK FOUND AT LOWER FWD CORNER OF LIGHTING HOLE IN FLOORBEAM UPPER CHORD OF LONGITUDINAL BS 668, LBL 24, VERIFIED BY HFEC INSPECTION. MAINTENANCE STOP DRILLED CRACK; REVERIFIED WITH HFEC INSPECTION CRACK WAS CO NTAINED; FABRICATED AND INSTALLED REPAIR CHANNEL IAW AWA ER 03-5715-01333-ESI, PG 1-2. 2 L 7 2 4F RT A16WE 2001121400050 20011214 00050 NM 2001 12 14 AWXA200100636 1 20011208 A 3350 20121 CHARGER BOEING 757 757225 1384959 NM CABIN FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 915AW 22209 PHX - EEL - C - EMERGENCY EXIT LIGHTS AT L1 AND R1 DOORS INOPERATIVE. MAINTENANCE REPLACED FWD BATTERY PACK CHARGER BS 340 IAW BMM 33-51-07. 2 L 7 2 4F RT A2NM 2001121400051 20011214 00051 NE 2001 12 14 SWAA013312 2 20011210 A 7310 405742 SHUTOFF VALVE BOEING 737 7372T4 1384492 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE FAILED A SWAA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SW 07 721WN 22697 ABORTED TAKEOFF, POWERING UP FOR TAKEOFF, NR 2 ENGINE ROLLED BACK AT APPROX 2500-3000 LBS FUEL FLOW; THROTTLE COULD BE P USHED UP TO FULL PWR WITH NO INCREASE IN THRUST. REMOVED AND REPLACED NR 2 ENG FUEL SHUTOFF VALVE AND REPAIRED FUEL SHU T OFF VALVE WIRING HARNESS PER MM. 2 L 7 2 4F 4 F A16WE E2EA 2001121400052 20011214 00052 2001 12 14 SWAA013313 4 20011211 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 317WN 24068 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002011500104 20020115 00104 WP 2002 1 15 ARWA20011204 1 20011205 A 7931 LIMITER DOUG DC8 DC862 3021970 WP NR 4 ENGINE OUT OF ADJ A ARWA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 19 810BN 45905 WHILE SETTING MAX POWER TAKEOFF, NR 4 ENGINE OIL PRESSURE MAXED OUT. PERFORMED ENGINE RUN IAW MM 71-00; FOUND OIL PRESS URE AT TAKEOFF 58 PSI WITHIN LIMITS IAW AA DC8 MM PAGES 5-35-90. ADJUSTED UPPER LIMIT TO 54 PSI IAW MM 79-20-5. OPS NO RMAL, 41 PSI AT IDLE 54 PSI AT TAKEOFF. OPS NORMAL. 2 L 7 4 4F 4A25 2001121400053 20011214 00053 WP 2001 12 14 0104519917 1 20010719 A 5310 ANGLE DOUG DC9 DC932 3022066 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 967N 47573 During Hck in ATL, Corrosion was found on the horizontal flange of the fuselage cusp angle at sta 120. Due to depth of c orrosion, it was elected to trim the flange to remove the damaged area. Material .071 7075-t6 AL, .020 7075-t6 Al. Repai red per EA 99-181362. 2 L 7 2 4F A6WE 2001121400054 20011214 00054 WP 2001 12 14 0104529922 1 20010727 A 5310 PAN DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 945N 47664 During Mck in ATL, A crack was found between 2 fasteners in the aft cargo doorjamb pan at sta 937, between longerons 26r and 27r. Material .050" 2024-t42 AL, and .090"2024-t42 AL. Repaired per EA 99-181313. 2 L 7 2 4F A6WE 2001121400055 20011214 00055 WP 2001 12 14 0104539922 1 20010724 A 5330 SKIN DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 945N 47664 During Mck in ATL a .25" crack was found in the fuselage skin at sta 1019, between longerons 14L and 15L. The crack eman ated from one fastener hole common to the pylon upper attach angle and was removed using a 1" diameter cut out. Material .032 TI-6AI-4v. Repaired per EA 99-181338. 2 L 7 2 4F A6WE 2001121400056 20011214 00056 WP 2001 12 14 0104549922 1 20010727 A 5410 SPAR DOUG DC9 DC932 3022066 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 945N 47664 During an Mck in ATL, Corrosion was found in the left and right upper beaver tails. The Beaver tails were removed to acc omplish corrosion removal. After the beaver tail removal it was noted that 11 fasteners common to the pylon spar were el ongated. Repaired per EA 99-181347. 2 L 7 2 4F A6WE 2001121400060 20011214 00060 NM 2001 12 14 DLM88011882 1 20011130 A 3610 BOOT DOUG MD88 MD88 3023688 NM RIGHT TORN A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 916DL 49591 ON CLIMB OUT PASSING THRU 25000 FT, GOT TAIL COMPARTMENT TEMP LIGHT. FOLLOWED THE PROCEDURES, BOTH X FEED CLOSED NO A NTI ICE. THE TEMP LIGHT WENT OUT AFTER FOUR MINUTES. _T/S FOUND RT FLOW CONTROL VALVE BOOT TORN, ALSO RT DIVERTER VALVE CLAMP LOOSE. REPLACED BOOT AND SECURED CLAMP, RAN THE ENGINES CK'S OK. 2 L 7 2 4F RT A6WE 2001121400061 20011214 00061 NM 2001 12 14 DLM88011893 1 20011204 A 3200 39370601 BOLT DOUG MD88 MD88 3023688 NM RIGHT GEAR SHEARED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 931DL 49718 IRREG: GEAR DOOR OPEN AND RT GEAR UNSAFE LIGHT IN FLT CORR. ACT: FOUND LWR. BOLT FOR ACTUATOR LINK ASSY. SHEARED REPLD BOLT. 2 L 7 2 4F RT A6WE 2001121400062 20011214 00062 NM 2001 12 14 DL72S011895 1 20011204 A 5300 FRAME BOEING 727 727225A 1384077 NM STA 500 STR 28L CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 MADE 2 EA REPAIRS TO STA 520 SHEAR TIES ON INBD AND OUTBD SIDES OF STR 28L PER SRM 53-10-4 FIG 15. SSI DATA RETRIEVAL FORM COMPLETED AND SENT. 2 L 7 3 4F RT A3WE 2001121400063 20011214 00063 NM 2001 12 14 DL72S011896 1 20011204 A 5300 FRAME BOEING 727 727225A 1384077 NM STA 580 STR 28L DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 REPAIRED STA 580 SHEAR TIE JUST OUTBD OF STR 28L PER SRM 53-10-4 FIG 15. SSI DATA RETRIEVAL FORM COMPLETED AND SENT 2 L 7 3 4F RT A3WE 2001121400064 20011214 00064 NM 2001 12 14 DL757011904 1 20011206 A 5330 141N33317 SKIN BOEING 757 757232 1384965 NM FS 300, S-16L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 672DL 25977 FUSELAGE / SKIN / FS 297-310 / STRG. 16L-17L : GROUND DAMAGE CUTOUT REPAIR THE FUSELAGE SKIN WAS DENTED AND GOUGED BY GROUND EQUIPMENT BETWEEN FS 297 & 310 AND BETWEEN STRINGERS 16L & 17L. THE DAMAGE WAS REMOVED WITH A 17" X 5" CUTOUT. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM DOUBLERS INSTALLED PER ER/A 382187-14, REV A. 2 L 7 2 4F RT A2NM 2001121400065 20011214 00065 NM 2001 12 14 DLM88011912 1 20011209 A 2430 021904000 BATTERY DOUG MD88 MD88 3023688 NM E.E COMPARTMENT OVERHEATED A DALA O OTHER M OVER TEMP TX TAXI/GRND HDL 1 SO 27 904DE 53409 AT APU START ATTEMPT ON GATE A LOUD BANG WAS HEARD UNDER TH E GALLEY - FOUND A/C BATTERY SWELLED - PROBABLE EXPLOSION 2 L 7 2 4F RT A6WE 2001121400066 20011214 00066 NM 2001 12 14 DL73K011915 1 20011210 A 5321 654541039 WEB BOEING 737 737232 1384475 NM CABIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 322DL 23094 CRACKS WERE FOUND IN THE WEBS OF THE RBL AND LBL 24 FLOOR BEAMS AT F.S. 680. THE CRACKS WERE CUT OUT AND A DOUBLER INSTALLED PER ERA 398177-14AD. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2001121400067 20011214 00067 NM 2001 12 14 DL73K011916 1 20011209 A 5330 SKIN BOEING 737 737247 138448D NM FS 727B, S-18R CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 373DL 23520 FUSELAGE / SKIN / FS 727B / STRG. 18R : CRACK REPAIR INSPECTION OF THE FUSELAGE SKIN REVEALED A 5" CRACK JUST ABOVE STRINGER 18R AT FS 727B. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER THE B737 SRM AND PER ER/A 382255-14. 2 L 7 2 4F A16WE 2001121400068 20011214 00068 NM 2001 12 14 DL757011928 1 20011211 A 2910 000AE9080200 LINE BOEING 757 757232 1384965 NM CNTR HYD BAY FAILED A DALA C ABORTED TAKEOFF K FLUID LOSS CR CRUISE 1 SO 27 630DL 22920 CENTER HYDRAULIC SYST QUANTITY LOSS WITH 'C HYD QTY' EICAS MSG. REPLACED FLEX LINE AT CENTER HYD BAY. LEAK CHECKS GOOD SERVICED SYSTEM TO FULL. 2 L 7 2 4F RT A2NM 2001121400069 20011214 00069 NM 2001 12 14 DL72S011931 1 20011126 A 2780 651622369 SLAT BOEING 727 727225A 1384077 NM #2 POSITION CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 REPAIRED #2 SLAT LOWER COVE SKIN ATTACH ANGLE PER 727 M/M 57-54-000-8 FIG 807A AND ERA 382247-14 REV ORG 2 L 7 3 4F RT A3WE 2001121400070 20011214 00070 NM 2001 12 14 DL76G011932 1 20011212 A 3350 767 LAMP BOEING 767 767332 1382001 NM RIGHT EXTERIOR BURNED OUT A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 16065 30199 RIGHT HAND EXTERIOR EMERGENCY LIGHT BURNED OUT. RELAMPED, OPS CHECK OK. 2 L 7 2 4F RT A1NM 2001121400071 20011214 00071 NE 2001 12 14 ARWA20011205 2 20011211 A 7300 ENGINE DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE A ARWA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 19 1804 63413 270 45896 671362 LOG PAGE 101856. DISCREPANCY: ON ADVANCING THROTTLE FOR TAKE OFF #4 ENGINE HUNG, CARRIED OUT ABNORMAL PROCEDURE FOR ENGI NE HUNG WITH THRUST LEVER IN REVERSE ENGINE STARTED TO ACCELERATE. CANCELED REVERSE THRUST ENGINE CONTINUED TO ACCELERAT E WITH THROTTLE CLOSED. ENGINE WAS SHUT DOWN. AIRCRAFT RETURNED TO THE RAMP. CORRECTIVE ACTION: PERFORMED ENGINE INSPECT ION AND FOUND FCU THROTTLE LINKAGE BOLT BACKING OUT AND INTERFERING WITH THROTTLE OPERATION. REINSTALLED AND SAFETIED IA W MM 73-10-00. PERFORMED ENGINE RUN UP AND CHECKED NORMAL IAW MM 71-00. AIRCRAFT WAS RELEASE FOR FLIGHT. 2 L 7 4 4F 4 F 4A25 1E8 2001123100037 20011231 00037 EA 2001 12 31 COMA0160959 1 20011212 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DENTED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 943CA 15446 7062 FUSELAGE SKIN FWD OF PAX DOOR FS 310.00 DENTED APPROXIMATELY .020 DEEP. FABBED REPAIR PARTS AND INSTALLED IAW CANADAIR REO 601R-53-21-180. 2 L 7 2 4F RT A21EA 2001121400072 20011214 00072 EA 2001 12 14 COMA0110162 1 20011212 A 2710 601R5122623 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA INST PANEL STUCK A COMA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CL CLIMB 1 SO 01 810CA 7370 FLIGHT 5281 AILERON TRIM STICKING INTERMITTENTLY.REPLACED THE AILERON/RUDDER TRIM CONTROL PANEL. 2 L 7 2 4F RT A21EA 2001121400075 20011214 00075 WP 2001 12 14 DIN2001F00002 2 20011129 A 7260 M274263116A RETAINER LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE7313A 01518 WP DRIVE SHAFT BROKEN B DINR O OTHER Y ENGINE STOPPAGE CR CRUISE 1 EA 13 127GT 067 P85244 DURING FLIGHT, LEFT HAND ENGINE EXPERIENCED UNCOMMANDED SHUTDOWN. INVESTIGATION FOUND HORIZONTAL DRIVE SHAFT (PN 307020 1-11) HAD UNCOUPLED FROM THE ACCESSORY GEARBOX DUE TO RETAINER RING (M27426-8116A) BREAKING ALLOWING MOVEMENT OF THE SHA FT TO OCCUR. PRIOR TO 2000, RETAINER RINGS WERE NOT ROUTINELY REMOVED FROM TRANSFER GB HSGS. THEY WERE PERMITTED TO BE REUSED, ONLY BEING REPLACED (ON CONDITION). AFTER 2000, ENG UNDERGOING MPIS OR GREATER INSP ARE REQUIRED TO HAVE RETAI NER RING REMOVED AND REPLACED WITH NEW. REPLACEMENT IS NOW MANDATORY AND ROUTINE. 2 L 7 2 4F 4 F A10CE E6WE 2001121400076 20011214 00076 CE 2001 12 14 HYI2001F00011 1 20011120 A 3230 51420025 DRAG BRACE CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO NLG CRACKED E HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 120PC 1933 402C0079 DURING SCHEDULED INSPECTION, MECHANIC FOUND NOSE GEAR DRAG BRACE CRACKED AT ACTUATOR ATTACH LUG. REMOVED AND REPLACED D RAG BRACE AND RETURNED AIRCRAFT TO SERVICE. 1 L 7 2 3O 3 O A7CE E8CE 2001121400077 20011214 00077 CE 2001 12 14 HYI2001F00012 1 20011119 A 2460 CM358950 MASTER SWITCH CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO INST PANEL FAILED E HYIA K NONE L NO TEST IN INSP/MAINT 1 NE 01 548GA 1000 402C0653 ON PREFLIGHT INSPECTION, AVIONICS MASTER SWITCH FAILED. MAINTENANCE REPLACED SWITCH AND RETURNED AIRCRAFT TO SERVICE. 1 L 7 2 3O 3 O A7CE E8CE 2001121400079 20011214 00079 CE 2001 12 14 IJA2001F00000 1 20011203 A 3230 NAS464P628M BOLT BEECH 90 C90 1152913 CE PWA PT6 PT6A11 52043 NE MLG DRAG BRACE DAMAGED E IJAA K NONE O OTHER IN INSP/MAINT 1 CE 07 403EM 561 LJ1000 BOLT (PN NAS464P6-28M) RIDES INSIDE BUSHING (PN 105740X-YA1007) WHICH FITS INTO LOWER END OF DRAG BRACE AND ATTACHES TO A CASTING ON MAIN GEAR TRUNNION. AT 5338 AFTT, BOLT WAS FOUND TO HAVE STAGGERED SHANK DUE TO HIGH SHEAR LOAD. SHANK WA S STAGGERED APPROX .020 INCH. JOINT HAD BEEN DISASSEMBLED AT 477 AFTT, BUSHING REPLACED. INSPECT DRAG BRACE FREE PLAY B Y GENTLY ROCKING MAIN GEAR FORE AND AFT. STAGGERED BOLT WILL BIND AS IT TURNS AND THREAD END WILL NOT TURN TRUE. BOLT (PN NAS464P6-28M HAS BEEN SUPERCEEDED TO DIFFERENT BOLT PN 130909B130. REPLACED BUSHING WITH NEW. RETURNED THE AC TO S ERVICE. 1 L 7 2 3T 3 T 3A20 E4EA 2001121400080 20011214 00080 CE 2001 12 14 JGV2001F00015 1 20011031 A 5310 DOOR FRAME LEAR 55 55LEAR 5170702 CE FUSELAGE CORRODED B JGVR K NONE O OTHER IN INSP/MAINT 1 CE 09 816MC 6584 035 CORROSION OF LOWER AFT DOOR FRAME AND SUPPORT BOX STRUCTURE. CONTAMINATION OF FIBERGLASS INSULATION WITH WATER LED TO C ORROSION OF STRUCTURE IN THIS UNACCESSIBLE AND CLOSED AREA. (PN OF CORRODED PARTS: 5410160-39, 5410557-112, 5415572-46, 5410557-16, 5410557-2, 5410160-24, 5410558-14, 5410558-27) 2 L 7 2 4F A10CE 2001121400081 20011214 00081 CE 2001 12 14 WC72001F00000 1 20010919 A 3213 59411007 LINK CESSNA 425 425 2076018 CE PWA PT6 PT6A11 52043 NE MLG CORRODED A WC7R K NONE O OTHER IN INSP/MAINT 1 GL 25 425PL 5587 4250010 THE TRAILING LINK ASSEMBLY ON LEFT AND RIGHT MAIN LANDING GEAR HAD CORROSION AND PITTING PRESENT IN THE LIGHTENING BORE AT THE FORWARD OR UPPER END. PITTING IN AREAS WAS APPROXIMATELY .025. AFTER BLENDING AND REMAINING THICKNESS DETERMINE D WITH UT THE PART WAS DETERMINED TO BE WITHIN LIMITS BY MFG. THE BORES WERE REQUIRED TO BE SHOT PEENED BEFORE RETURN T O SERVICE, (AND PAINTED). 1 L 7 2 3T 3 T RT A7CE E4EA 2001121400082 20011214 00082 CE 2001 12 14 WD42001F00000 1 20011101 A 2810 10192006137 VALVE BEECH 200 A200 1152921 CE PWA PT6 PT6A41 52043 EA FUEL FILLER MISMANUFACTURED B WD4R K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 17 638B BC65 NEW REPLACEMENT PARTS FOR THE ANTI-SIPHON VALVE ASSEMBLY ARE BEING MFG INCORRECTLY. PROBLEM IS THE FLAPPER ASSEMBLY GAS KET AND BACKUP PLATE WERE TRIMMED INCORRECTLY AND HINGE IS EXPOSED LEAVING A GAP WHERE FUEL CAN BE SIPHONED OUT DURING F LIGHT IF THE FUEL CAP WERE TO COME OFF IN FLIGHT. MFG HAS BEEN NOTIFIED OF PROBLEM. 1 L 7 2 4T 4 T A24CE E4EA 2001121400083 20011214 00083 CE 2001 12 14 WIB2001F00000 1 20010728 A 3040 322867003 SHUTOFF VALVE LEAR 35 35A 5170602 CE BLEED AIR LEAKING A WIBR K NONE O OTHER IN INSP/MAINT 1 SW 11 81MR 622 MAINTENANCE PERSONNEL DETECTED BLEED AIR LEAK IN TAILCONE DURING GROUND OPERATION. TRACED SOURCE TO CENTER MATING SURFA CES OF WINDSHIELD ANTI-ICE SHUTOFF VALVE. REPLACED VALVE WITH OVERHAULED UNIT. PROBABLE CAUSE: BLOWN GASKET IN VALVE. 2 L 7 2 4F A10CE 2001121400084 20011214 00084 CE 2001 12 14 WIB2001F00001 1 20011015 A 2520 3A0350005015 SEAT LEAR 35 31 5170530 CE GARRTT TFE731 TFE731* 01518 WP CABIN CRACKED A WIBR K NONE O OTHER IN INSP/MAINT 1 SW 11 5VG 014 BACKPLATE OF SEAT IS CRACKED AT THREE OF THE FOUR CORNERS OF THE HOLE WHERE THE SHOULDER STRAP INERTIA REEL MOUNTS. FOU ND DURING INSPECTION. 2 L 7 2 4F 4 F RT A10CE E6WE 2001121400085 20011214 00085 SO 2001 12 14 WVBA2001052 1 20011115 A 2140 A23D04 REGULATOR PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HEATER LEAKING E WVGA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 01 4082T 58 318152089 UPON INSPECTING THE FUEL PRESSURE REG IT WAS FOUND THAT THE REGULATOR WAS LEAKING PROBABLY FROM THE LOWER BODY PARTING SURFACES. REMOVED AND REPLACED UNIT LEAK CHECK GOOD. 1 L 7 2 3O 3 O A20SO E14EA 2001121400086 20011214 00086 2001 12 14 WVE2001F00001 4 20010809 A 2297 354105230 WIRE HARNESS LEAR 45 45LEAR 5170805 CE GARRTT TFE731 TFE7312B WP RUDDER BOOST CHAFED A WVER K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 09 409FX 787 095 DURING POST DOCK RUNS THE RUDDER BOOST EICAS LIGHT ILLUMINATED. INSPECTION/TROUBLE SHOOTING FOUND WIRING HARNESS CHAFED THROUGH THE POWER LINES. PROBABLE CAUSE: ROUTING THROUGH LIGHTING HOLE WITHOUT CHAFE PROTECTION AT TIME OF MANUFACTUR E. 2 L 7 2 4F 4 F RT T00008WI E6WE 2001121400087 20011214 00087 SO 2001 12 14 XPC2001F00000 1 20011112 A 7920 8002605 HOSE PIPER PA31T PA31T 7103124 SO PWA PT6 PT6A60A 52043 NE OIL SYSTEM CRACKED E XPCA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 11 111KV 1326 31T7920035 RIGHT ENGINE SHUT DOWN IN FLIGHT DUE TO WARNING OF LOW OIL PRESSURE. FOUND OIL COOLER INLET NOSE FAILED AT BEND RADIUS. SUSPECT HOSE WAS ROUTED INCORRECTLY DURING A RECENT ENGINE INSTALLATION. 1 L 7 2 3T 4 T A8EA E4EA 2001121400088 20011214 00088 2001 12 14 YAD2001F00008 4 20010725 A 3444 1013840281 SWITCH BEECH 1900 1900C 1154161 CE ALTITUDE WARN FAILED E YADA O OTHER P NO WARNING INDICATION CR CRUISE 1 AL 03 45GL 9096 UC45 CABIN ALTITUDE WAS NOTED AT 16,000 FT (DUE IMPACT - DAMAGE TO FUSELAGE) IN FLIGHT - CREW STATED USING SUPPLEMENTAL OXYG EN AT THIS POINT. CABIN ALTITUDE WARNING DID NOT FUNCTION, WARNING LIGHT SHOULD COME ON AT 12,250 FT. REPLACED DEFECTI VE SWITCH. WARNING SWITCH FOR CABIN PRESSURIZATION/ ALTITUDE, DID NOT FUNCTION DURING PRESSURIZATION LOSS. 2 L 7 2 4T RT A24CE 2001121400089 20011214 00089 CE 2001 12 14 YAD2001F00009 1 20010724 A 2841 1183800001 GAUGE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE COCKPIT SHORTED E YADA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 AL 03 41UE UC41 SMELL OF SMOKE, PULLED RIGHT FUEL GAUGE CIRCUIT BREAKER, SMELL WENT AWAY. VERIFIED SMOKE WAS FROM RIGHT FUEL GAUGE, PUL LED AND BANDED RIGHT FUEL GAUGE CIRCUIT BREAKER. RIGHT FUEL QUANTITY GAUGE PREVIOUSLY DEFERRED. 2 L 7 2 4T 4 T RT A24CE E4EA 2001121400090 20011214 00090 SO 2001 12 14 YWB2001F00001 2 20010924 A 8540 642087A55 ADAPTER BEECH 58 58 1152740 CE CONT O550 IO550C SO ENGINE FAILED B YWBR K NONE O OTHER IN INSP/MAINT 1 WP 17 876AN 199 TH1683 DURING ROUTINE INSPECTION FOUND METAL (STEEL) IN FILTER. REMOVED STARTER ADAPTER AND FOUND SHAFT GEAR NEEDLE BEARING PN 630890 IN ENGINE CASE HAD FAILED. NEEDLES FROM FAILED BEARING HAD ALSO DAMAGED CRANKSHAFT AND IDLER GEARS. SOME DAMAG E DONE TO ENGINE CASE AT BEARING LOCATION. ENGINE REMOVED FROM SERVICE. 1 L 7 2 3O 3 O 3A16 E3SO 2001121400091 20011214 00091 NM 2001 12 14 BJN2001F00000 1 20011118 A 3397 CONNECTOR BOEING 737 737282 13844AT NM PWA JT8 JT8D17 52049 NE CABIN DISCONNECTED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 789TM 23046 EMERGENCY ESCAPE PATH MARKING SYSTEM INOPERATIVE FROM ROW 1 TO ROW 15. FOUND FLOOR CONNECTOR UNPLUGGED, RECONNECTED, OP S CHECK GOOD, OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2001121400092 20011214 00092 NM 2001 12 14 BJN2001F00001 1 20011113 A 3350 1000679 LIGHT BOEING 737 737282 13844AT NM PWA JT8 JT8D17 52049 NE L2 DOOR INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 233TM 23043 L2 DOOR EMERGENCY EXIT PORTABLE LIGHT INOPERATIVE. REMOVED AND REPLACED PORTABLE EMERGENCY EXIT LIGHT ON L2 DOOR, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A16WE E2EA 2001121400093 20011214 00093 NM 2001 12 14 BJN2001F00002 1 20011127 A 2910 HYDRAULIC SYSTEM BOEING 737 737214 138446R NM PWA JT8 JT8D9 52048 NE A & B SYSTEM FAILED A BJNA O OTHER J WARNING INDICATION DE DESCENT 1 WP 11 457TM 20156 DURING DESCENT NOTICED A SYSTEM HYDRAULIC QUANTITY LEVEL DROPPING . A SYSTEM LOW PRESSURE LIGHT ILLUMINATED. CONFIGURE D AC FOR A SYSTEM HYDRAULIC FAILURE CONTINUED FLIGHT WITH B SYSTEM. APPROX 5 MINUTES LATER, LOW PRESSURE WARNING ILLUMI NATED ON BOTH B SYSTEM LOW PRESSURE WARNING LIGHTS, FLIGHT CREW OBSERVED A AND B PRESSURE INDICATION DROPPED TO ZERO AT THE SAME TIME B SYSTEM LOW QUANTITY DID NOT ILLUMINATE. CONFIGURED AC FOR MANUAL REVERSION, DIVERTED, MADE UNEVENTFUL L ANDING. 2 L 7 2 4F 4 F A16WE E2EA 2001121400094 20011214 00094 NM 2001 12 14 BJN2001F00004 1 20011203 A 5410 LATCH BOEING 737 737282 13844AT NM PWA JT8 JT8D17 52049 NE NACELLE UNLATCHED A BJNA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 11 789TM 23046 DURING FLIGHT, THE SR FLIGHT ATTENDANT NOTIFIED THE CAPTAIN THAT A PIECE OF COWLING WAS LOOSE. THE CAPT CONFIRMED THAT THE NACELLE FAIRING THAT LIES BETWEEN THE WING AND THE ENGINE COWLING WAS LOOSE, THE COWLING LATCH HAD COME UNDONE AND T HE FAIRING WAS AJAR AND RAISED FROM THE NORMAL POSITION. THE CAPTAIN MADE THE DECISION TO LAND AND HAVE THE FAIRING SEC URED. MAINTENANCE INSPECTED AREA, SECURED THE LOOSE LATCH, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2EA 2001121700001 20011217 00001 2001 12 17 SWAA013314 4 20011212 A 2565 6949956 CABLE BOEING 737 7372K6 1364440 NM FWD SVC DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINING CABLE IMPROPERLY ROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2001121700002 20011217 00002 NM 2001 12 17 SWAA013316 1 20011211 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 645SW 28330 EEPLS COVER MISSING. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2001121700003 20011217 00003 NM 2001 12 17 SWAA013317 1 20011212 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 750SA 29802 EEPLS LENS LOOSE IN FWD CABIN. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2001121700004 20011217 00004 NM 2001 12 17 SWAA013318 1 20011212 A 5312 6516300 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 604SW 27955 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, WL201, RBL 5.0 AND LBL 5.0. REPAIRED WEB P ER SRM. 2 L 7 2 4F RT A16WE 2001121700005 20011217 00005 NM 2001 12 17 SWAA013319 1 20011212 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CRACKED AT BS 500C, STR 15R. REPAIRED STR PER SRM. 2 L 7 2 4F RT A16WE 2001121700006 20011217 00006 NM 2001 12 17 SWAA013320 1 20011212 A 5311 6546536 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 540, STR 10R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001121700007 20011217 00007 NM 2001 12 17 BJN2001F00003 1 20011127 A 2910 65445102391 HYDRAULIC LINE BOEING 737 737214 138446R NM PWA JT8 JT8D9 52048 NE HYDRAULIC SYS CHAFED A BJNA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 WP 11 457TM 20156 DURING DESCENT NOTICED A SYS HYDRAULIC QUANTITY LEVEL DROPPING. A SYS LOW PRESSURE LIGHT ILLUMINATED. CONFIGURED AC FO R A SYS HYDRAULIC FAILURE CONTINUED FLIGHT WITH B SYS. APPROX 5 MINUTES LATER, LOW PRESSURE WARNING ILLUMINATED ON BOTH B SYS LOW PRESSURE WARNING LIGHTS, FLIGHT CREW OBSERVED A AND B PRESSURE INDICATION DROPPED TO ZERO AT THE SAME TIME, B SYS LOW QUANTITY DID NOT ILLUMINATE. CONFIGURED AC FOR MANUAL REVERSION, DIVERTED, MADE UNEVENTFUL LANDING. B SYS DID NOT LOSE FLUID. REPLACED HYDRAULIC TUBE ASSEMBLY TO 1 ENGINE DRIVEN HYDRAULIC PUMP ALSO CHANGED NR 2 ENGINE DRIVEN HYD RAULIC PUMP AND THE MANIFOLD PRESSURIZATION REGULATOR, NO FURTHER DISCREPANCIES. AC RETURNED TO SERVICE. 2 L 7 2 4F 4 F A16WE E2EA 2001121700008 20011217 00008 EU 2001 12 17 COEA0103702 2 20011116 A 7260 601016968 GASKET FOKKER F27 F27MK600 4990706 EU RROYCE DART DART532* EU NR 2 ENGINE WORN A COEA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 13 702FE 10350 NR 2 ENGINE GEAR BOX OIL PRESSURE LIGHT CAME ON IN FLIGHT. PILOT PERFORMED PRECAUTIONARY IN FLIGHT SHUTDOWN ON NR 2 ENG INE. NO EMERGENCY DECLARED. MAINTENANCE FOUND OIL LEAKING FROM AROUND MOUNTING PAD OF PNEUMATIC COMPRESSOR. GASKET AN D OIL TRANSFER BOBBIN SEALS WERE REMOVED AND REPLACED. GEARBOX OPERATION AND LEAK CHECK GOOD. AC RETURNED TO SERVICE. 2 H 7 2 4T 4 T A817 E297 2001121700009 20011217 00009 EA 2001 12 17 COMA0160961 1 20011215 A 5310 601R32201 POST CNDAIR CL600 CL6002B19 1900309 EA RBL 18 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 927CA 18312 7031 THE OUTBOARD LOWER POST AT RBL 18.0, FS 409 + 128 IS CRACKED (LOWER AFT CORNER).REMOVED DAMAGED AREA AND REPAIRED I/A/W WVAC E.O. 601R-53-2874. 2 L 7 2 4F RT A21EA 2001121700010 20011217 00010 GL 2001 12 17 DFM2001F00000 2 20011202 A 7320 MS2740723F SWITCH BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20B 03013 GL FUEL SYSTEM INTERMITTENT A DFMA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 CE 03 692DD S149 834574 25 MINUTES INTO REPOSITIONING FLIGHT NR 1 ENGINE N1 DECREASED SLOWLY. ATTEMPT TO REGAIN OPERATING NR 1 UNSUCCESSFUL. P ILOT INITIATED SINGLE ENGINE PROCEDURES TO A SUCCESSFUL SINGLE ENGINE LANDING. NO AIRCRAFT DAMAGE, NO PERSONAL INJURIES . TROUBLESHOOTING TO DETERMINE CAUSE IS IN PROGRESS. 1 G 7 2 3U 3 U H3EU E4CE 2001121700012 20011217 00012 CE 2001 12 17 JJB2001F00007 1 20011201 A 2450 118364021 PANEL BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA COCKPIT SHORTED A JJBA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 01 854CA 2333 UE399 SMELL OF SMOKE IN COCKPIT DURING FLIGHT, SMOKE COMING FROM LEFT SIDE OF INSTRUMENT PANEL. INSPECTED: FOUND SHORTED EL PANEL WIRE TO BUS BAR TERMINAL BEHIND FUEL QUANTITY INDICATOR PANEL. (WIRE X31F20) ALSO REPLACED WIRES: X30E20, 31E20, 30H20,31G20, 30J20, 31K20, 30K20, 30L20, 31L20, 31M20, 30F20, 31J20, 30A20, 30B20, 31A20, 63A22, 32A20N 2 L 7 2 4T 3 T RT A24CE E2NE 2001121700013 20011217 00013 SW 2001 12 17 UNF2001F00001 1 20011105 A 5320 222031830101 BOLT BELL 222 222 1182122 SW LYC LTS101 LTS101600A 41560 NE WING STUB ATTACH LOOSE A UNFR K NONE O OTHER IN INSP/MAINT 1 SW 19 29KH 3417 47053 FOUND METAL TO METAL FRETTING WEAR AND MAKING MUD ON BOTTOM SIDE OF WING (22-031-800-101). BOLTS LOOSE ENOUGH TO ALLOW LOWER SKIN ON WING TO CAUSE SEVERE CHAFING DAMAGE BETWEEN LOWER WING SKINS (222-030-812-135/812-136) AND FUSELAGE STRUCT URAL SKINS (222-030-466-105/107) AND (222-031-464-115/116). LOWER WING SKIN WORE COMPLETELY THROUGH FUSELAGE STRUCTURAL SKINS. SKINS WERE REPLACED WITH NEW MFG SKINS AND LOWER WINGLET SKINS WERE TRIMMED BACK TO PREVENT FUTURE DAMAGE TO FU SELAGE SKINS. DAMAGED BOLTS WERE REPLACED WITH NO KNOWN MFG WEAR LIMITS PUBLISHED. A THICKER WASHER TO BOLTS TO AID IN TORQUE RETENTION OF WING ATTACHMENT BOLTS AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 2 3U 3 U H9SW E5NE 2001121700014 20011217 00014 SO 2001 12 17 W452001F00000 1 20011029 A 7722 10100103 PROBE PIPER PA46 PA46350P 7104602 SO LYC O540 TIO540AE2A 41532 EA EGT SYSTEM FAILED B W45R O OTHER O OTHER NR NOT REPORTED 1 WP 07 68CP 16 4636238 L1033161A AFTER INSTALLATION AND CALIBRATION IAW 99-15-04, UNIT LASTED 16.3 HRS. THIS SEEM TO BE A CONTINUING PROBLEM WITH THIS A ND SIMILAR UNITS. THIS IS THE 2ND TIME IN 1 WEEK THIS PN FAILED. 1 L 7 1 3O 3 O RT A25SO E14EA 2001121700015 20011217 00015 EA 2001 12 17 COMA0160962 1 20011214 A 5346 601R5361345 WEB CNDAIR CL600 CL6002B19 1900309 EA AFT EQUP BAY CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 971CA 12383 7145 ENGINE SUPPORT BEAM UPPER AND LOWER WEB CRACKED.REPAIRED I/A/W REO 601R-5361-345. 2 L 7 2 4F RT A21EA 2001121700016 20011217 00016 EA 2001 12 17 COMA0160963 1 20011214 A 5610 NP1393221 WINDOW CNDAIR CL600 CL6002B19 1900309 EA L/H INOPERATIVE A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 784CA 5503 7319 FLIGHT - LEFT WINDOW HEAT FAIL MESSAGE.REPLACED THE PILOTS LEFT SIDE WINDOW. 2 L 7 2 4F RT A21EA 2001121700017 20011217 00017 NM 2001 12 17 0104775506 1 20011207 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 506US 23195 DURING "H" CHECK FOUND CRACK IN FLOORBEAM UPPER CAP AT BS 700 LBL 25. REPAIRED PER EA 55-186814 2 L 7 2 4F RT A2NM 2001121700018 20011217 00018 NM 2001 12 17 0104786307 1 20011206 A 5320 FLOOR SUPPORT BOEING 747 747451 1384940 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 667US 24222 DURING "H" CHECK FOUND CORROSION ON FLOOR SUPPORT BETWEEN BS 510-520 LBL 41.5. REPAIRED PER EA 63-186876. 2 L 7 4 4F RT A20WE 2001121700019 20011217 00019 EA 2001 12 17 COMA0160964 1 20011208 A 2730 276003 PCU CNDAIR CL600 CL6002B19 1900309 EA L/H ELEVATOR INOPERATIVE A COMA O OTHER F L FLT CONT AFFECTED NO TEST IN INSP/MAINT 1 SO 01 924CA 19069 7026 (A CHECK INSPECTION) - L/H ELEVATOR IS INOP USING #1 HYDRAULIC SYSTEM.REPALCED THE L/H #1 SYSTEM ELEVATOR PCU. 2 L 7 2 4F RT A21EA 2001121700020 20011217 00020 EA 2001 12 17 COMA0160965 1 20011213 A 3010 355483255 ELEMENT CNDAIR CL600 CL6002B19 1900309 EA R/H FUSELAGE FAULTY A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 420CA 7451 FLIGHT 5584 ANTI-ICE DUCT MESSAGE DURING FLIGHT - WING ANTI-ICE WAS NOT ON.REPLACED THE R/H FUSELAGE ANTI ICE DUCT LEAK SENSING ELEMENT. 2 L 7 2 4F RT A21EA 2001121700021 20011217 00021 NM 2001 12 17 DL72S011886 1 20011202 A 3350 RPS1 POWER SUPPLY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 518DA 21469 FOUND FWD CLOSET, ROW 1-4, ROW 10-11 EMERGENCY ESCAPE PATH LIGHTING INOP. REPLACED POWER SUPPLY AND BATTERY PACK CKS G OOD 2 L 7 3 4F A3WE 2001121700022 20011217 00022 NM 2001 12 17 DL72S011894 1 20011204 A 2120 ODOR BOEING 727 727232 1384082 NM CABIN DETECTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 525DA 21585 IN CRZ FLT ATTENDANT REPORTED SMOKE IN CABIN. ELECTED TO DIVERT TO COS - NTF ON INSPECTION. 2 L 7 3 4F A3WE 2001121700023 20011217 00023 NM 2001 12 17 DL72S011897 1 20011204 A 3350 BATTERY BOEING 727 727232 1384082 NM AFT AIRSTAIRS DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 529DA 21703 AFT AIRSTAIR EMERGENCY LIGHT INOP. REPLACED BATTERIES IN LIGHT ASSY 2 L 7 3 4F A3WE 2001121700024 20011217 00024 NM 2001 12 17 DL72S011902 1 20011206 A 2781 40173 SWITCH BOEING 727 727232 1384082 NM L/E FLAP INTERMITTENT A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 516DA 21432 L/E FLAP LIGHT ILLUMINATED WHEN WING ANTI ICE SELECTED ON. REPLACED NR 4 AND NR 5 L/E FLAP POSITION XMITTERS. 2 L 7 3 4F A3WE 2001121700025 20011217 00025 NM 2001 12 17 CALA0101028 1 20011214 A 5311 FRAME BOEING 737 7373T0 1384582 NM STA 500 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 63305 23356 INSPECTION FOUND FRAME CORRODED AT STA 500, L27R. REPAIRED IAW SRM 51-70-11. 2 L 7 2 4F RT A16WE 2001121700026 20011217 00026 NM 2001 12 17 CALA0101030 1 20011214 A 5240 6552873195 TORQUE TUBE BOEING 737 7373T0 1384582 NM R-2 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 60312 23363 INSPECTION FOUND R-2 DOOR FUSELAGE TORQUE TUBE CORRODED. THE TORQUE TUBE WAS REMOVED AND REPLACED IAW MM 52-41-41. 2 L 7 2 4F RT A16WE 2001121700027 20011217 00027 NM 2001 12 17 DL72S011907 1 20010130 A 5754 651622291 SLAT BOEING 727 727225A 1384077 NM WING DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 NR 3 SLAT, B727 REPAIRED PER M/M 57-54-000-8 FIG. 814 AND 804, S/N: BN29, P/N: 65-16222-91 2 L 7 3 4F RT A3WE 2001121700028 20011217 00028 NM 2001 12 17 DL72S011914 1 20011209 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 527DA 21587 LT O/W FWD EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATT PACK. 2 L 7 3 4F A3WE 2001121700029 20011217 00029 NM 2001 12 17 DL72S011926 1 20011126 A 2752 ATTACH FITTING BOEING 727 727225A 1384077 NM FLAP ACTUATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 1/4 INCH CRACK NR 5 L/E FLAP ACTUATOR ATTACH BOX O/B RIB. REPAIRED PER MM 57-20-021-8 2 L 7 3 4F RT A3WE 2001121700030 20011217 00030 NM 2001 12 17 DL72S011935 1 20011212 A 5320 6592681 BEAM BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 546DA 22677 INSPECTIONS OF THE VENTRAL STAIRWAY OPENING TORQUE BOX STRUCTURE REVEALED TYPICAL CRACKS IN THE UPPER BEAM CAPS OF THE FS 1263 AND 1273 BEAMS ON THE RT SIDE. THE CRACKS ARE TYPICAL OF BAC S/B 727-53-0129. THE CRACKED STRUCTURE WAS REMOVE D AND NEW PARTS INSTALLED. THE WORK WAS ACCOMPLISHED PER ER/A 382272-14AD. 2 L 7 3 4F A3WE 2001121700031 20011217 00031 NM 2001 12 17 DL72S011936 1 20011211 A 5320 6516350313 STIFFENER BOEING 727 727225A 1384077 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 A 1 INCH CRACK WAS FOUND AT THE LOWER END OF THE LBL 8 VERTICAL BEAM AT WL 182 ON THE FS 1183 BULKHEAD. THE CRACK IS TY PICAL OF BAC S/B 727-53-0175. THE CRACK WAS REPAIRED PER THE S/B AND PER ER/A 382193- 14. 2 L 7 3 4F RT A3WE 2001121700032 20011217 00032 NM 2001 12 17 DL72S011937 1 20011211 A 5330 6518420761 SKIN BOEING 727 727225A 1384077 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 THE LOWER HINGE CUTOUT OF THE L1 DOOR OPENING WAS FOUND WITH A 3/8 INCH CRACK IN THE SKIN AND UNDERLYNG BEARSTRAP. THE CRACK WAS ROUTED OUT OF THE SKIN AND BEARSTRAP STACK-UP TO REMOVE THE DAMAGE. THE ROUTE OUT WAS REPAIRED PER ER/A 3821 70-14, REV A. 2 L 7 3 4F RT A3WE 2001121700033 20011217 00033 NM 2001 12 17 DL733011881 1 20011130 A 5753 SPAR BOEING 737 737347 1384647 NM T/E FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 303WA 23183 THE NR 3 MID FLAP FRONT SPAR UPPER CHORD AND WEB WERE FOUND DAMAGED. REPAIRED PER ER/A 410644-14. 2 L 7 2 4F RT A16WE 2001121700034 20011217 00034 NM 2001 12 17 DL733011903 1 20011207 A 5753 SPAR BOEING 737 737347 1384647 NM T/E FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 303WA 23183 FORWARD SPAR DAMAGED AT THE CUTOUT FOR THE EXHAUST GATE ACTUATOR ROD. DAMAGE CAUSED BY INSTALLATION OF INCORRECT ARM THA T MADE THE ROD TOO HIGH AND BOLT ATTACHING ROD TO ARM CONTACT THE SPAR. 2 L 7 2 4F RT A16WE 2001121700035 20011217 00035 NM 2001 12 17 DL738011887 1 20011202 A 5523 183A82101 SKIN BOEING 737 737832 13844CF NM ELEVATOR TAB ERODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 386DA 30373 WHILE ACCOMPLISHING INSPECTIONS OF THE LT ELEVATOR TAB PER AD 2001-08-09 & 2001-14-05, A SMALL AREA OF EROSION WAS FOUN D ON THE UPPER SKIN OF TRAILING EDGE. THE DAMAGE WAS REPAIRED WITH A SEALING REPAIR PER THE B737-800 SRM AND APPROVED/ DOCUMENTED PER ER/A 382205-14AD. 2 L 7 2 4F RT A16WE 2001121700036 20011217 00036 NM 2001 12 17 DL738011899 1 20011206 A 4930 FUEL LINE BOEING 737 737832 13844CF NM APU LEAKING A DALA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 3743H 2020 30836 ON TAXI OUT LIT HAD APU FIRE WARNING. CREW FIRED BOTTLE AND RTN TO GATE. UPON FURTHER INVESTIGATION CONTRACT MTC FOUND WHAT APPEARS TO BE A SMALL BURNT SPOT IN INSULATION BLANKET CAUSED BY WHAT APPEARS TO BE A LEAKING FUEL LINE ON APU. C A REMOVED AND REPLACED APU. 2 L 7 2 4F RT A16WE 2001121700037 20011217 00037 NE 2001 12 17 DL73K011885 2 20011202 A 7230 COMPRESSOR BOEING 737 737232 1384475 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE STALLED A DALA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 314DA 44310 23086 709161 IR - COMPRESSOR STALL NR 1 ENG ON TAKE TAKE OFF. INITIATED ABORT BETWEEN 70-80 KTS. DEAD HEATING CAPT REPORTED BRIGHT FL ASH FROM NR 1 ENG SHORTLY AFTER T/O PWR ADDED. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A16WE E2EA 2001121700038 20011217 00038 NM 2001 12 17 DL73K011922 1 20011210 A 5315 6545410224 FLOORBEAM BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 313DL 23085 INSPECTION OF THE RBL 24 FLOORBEAM UPPER CAP PER AD 2001-17-18 REVEALED A TYPICAL CRACK AT FS 680 AT THE AILERON QUADRAN T CUTOUT IN THE FLOORBEAM. A PREVIOUS ALUMINUM DOUBLER REPAIR WAS INSTALLED FOR THE WEB. THE CRACKED UPPER CHORD WAS R EMOVED, THE WEB INSPECTED, AND A NEW CHORD INSTALLED PER ER/A 396684-14AD, REV B. 2 L 7 2 4F RT A16WE 2001121700039 20011217 00039 NM 2001 12 17 DL757011889 1 20011203 A 3350 20131A BATTERY PACK BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 649DL 24389 R3 EXIT LIGHT DOES NOT ILLUMINATE. REPLACED BATTERY PACK, OPS CK. GOOD 2 L 7 2 4F RT A2NM 2001121700040 20011217 00040 NM 2001 12 17 DL757011923 1 20011210 A 2840 300710404 COMPUTER BOEING 757 757232 1384965 NM E/E BAY FAULTY A DALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 27 6702 30188 LT AND RT FUEL QUANTITY INDICATOR SHOWS ERROR CODES. REPLACED FUEL QUANTITY PROCESSOR. 2 L 7 2 4F RT A2NM 2001121700041 20011217 00041 NM 2001 12 17 DL757011925 1 20011211 A 2750 GEARBOX BOEING 757 757232 1384965 NM T/E FLAP MALFUNCTIONED A DALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 SO 27 661DN 7875 24972 NA DURING FLAP EXTENSION FROM UP TO 1 A STATUS MSG T/E FLAP DISAGREE MSG APPEARED, ACFT CONTROL FELT NORMAL. USED ALTERNATE MEANS TO LOWER FLAPS. TROUBLESHOT PER FIM 27-51-00 FIG 107 SH 1. NR 4 AND 5 FLAP GEARBOX PINS EXTENDED. SERVICED GEARBO X AND FLAP CLUTCHES. OPS CK GOOD. NO MSG ON FSEU AND EICAS. NO GEARBOX PINS EXTENDED. 2 L 7 2 4F RT A2NM 2001121700042 20011217 00042 NM 2001 12 17 DL757011927 1 20011212 A 3232 ACTUATOR BOEING 757 757232 1384965 NM NLG DOOR LACK OF LUBE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 660DL 24422 ACFT OUT AND OFF RETURNED TO GATE DUE TOO NOSE GEAR DOORS WOULD NOT CLOSE AFTER GEAR RETRACTION. C/A LUBED NOSE GEAR DOO R ACTUATOR AND BYPASS AND ALL SPRING ASSY. OPS CHECKS NORMAL. 2 L 7 2 4F RT A2NM 2001121700043 20011217 00043 NM 2001 12 17 DL757011929 1 20011211 A 3242 BRAKE ASSY BOEING 757 757232 1384965 NM LT MLG FIRE A DALA K NONE A FLAME/FIRE TX TAXI/GRND HDL 1 SO 27 620DL 22910 ON TAXI IN LT GEAR BRAKE FIRE, EXTINGUISHED NO DAMAGE. REPLACED NR 1-2 WHEEL ASSYS ALSO NR 1 BRAKE. 2 L 7 2 4F RT A2NM 2001121700044 20011217 00044 NM 2001 12 17 DL76G011911 1 20011209 A 3040 CONTROLLER BOEING 767 7673P6 1385105 NM SLDING WINDOW FAILED A DALA A UNSCHED LANDING A FLAME/FIRE CL CLIMB 1 SO 27 154DL 25241 AT DEPARTURE CAPT SLIDING SHORTED AND GOT FIRE. REPLACED SLIDING WINDOW IAW MM AND REPLACED WINDOW HEAT CONTROLLER. 2 L 7 2 4F RT A1NM 2001121700045 20011217 00045 EU 2001 12 17 2001F00735 1 20010217 A 7910 5725339201 FILLERCAP BRAERO DH125 HS125700A 4230170 EU RT ENGINE NOT SEATED A APJA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 11 302PC 257125 APPROXIMATELY 1.5 HOURS INTO FLIGHT AT 35,000 FT, THE OIL PRESSURE GAUGE FLUCTUATED FOR THE RT ENGINE AND PROCEEDED TO I NDICATE MINIMUM PRESSURE. AS A PRECAUTION, THE PIC SHUTDOWN THE RIGHT ENGINE WHEN THE OIL PRESSURE REACHED 25 PSI (MIN PRESSURE). UPON LANDING, IT WAS DETERMINED THAT THE OIL FILLER CAP WAS IMPROPERLY SEATED CAUSING LOSS OF OIL AND PRESSU RE. THE RIGHT ENGINE WAS CLEANED AND SERVICED WITH THREE QUARTS OF OIL. PERFORMED SEVERAL ENGINE RUNUPS. NO FURTHER L EAKS AND OIL PRESSURE GAUGE INDICATED PROPERLY. (M) 2 L 7 2 4F A3EU 2001121700046 20011217 00046 CE 2001 12 17 2001F00736 1 20011003 A 3230 1CH16 SWITCH LEAR 24 24 5170302 CE LANDING GEAR FAILED A X5CA O OTHER O OTHER AP APPROACH 1 GL 17 993TD 166 ON FINAL APPROACH INTO JVL, LANDING GEAR FAILED TO EXTEND NORMALLY. LANDING WAS ASSURED AFTER SUCCESSFUL ALTERNATE GEAR EXTENSION. PROBLEM WAS NORMAL SWITCH WEAR, GEAR OPERATION NORMAL AFTER SWITCH REPLACEMENT PER LEAR M/M. (M) 2 L 7 2 4J A10CE 2001121700047 20011217 00047 SO 2001 12 17 2001F00737 1 20011019 A 2751 1159SCC503003 POSITION SWITCH GULSTM GV GULFSTREAMGV 3980116 SO T/E FLAP FAULTY A UG8A D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 23 661GA 910 561 SAV - FLT 2786 - FLAPS/STAB WARNING LIGHT CAME ON WHILE TAXIING OUT. RETURNED TO GULFSTREAM. LEFT FLAP POSITION RESOLV ER. REPLACED LEFT FLAP POSITION RESOLVER IAW CMP CODE 275401. (M) 2 L 7 2 4F RT A12EA 2001121700048 20011217 00048 WP 2001 12 17 AALA20011992 1 20011031 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 59523 49915 TUL - FOUND AREA OF FUSELAGE SKIN GROUND DEEP AT STATION 275 BELOW LONGERON 25L. INSTALLED DOUBLER PER SRM 53-04 FIG 38 . (M) 2 L 7 2 4F A6WE 2001121700049 20011217 00049 WP 2001 12 17 AALA20011993 1 20011031 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 59523 49915 TUL - LOWER AFT CARGO DOOR JAMB CORRODED FROM STATION 1155 TO STATION 1212 AT STRINGER 28R. INSTALLED REPAIR DOUBLER OV ER OUT OF LIMIT AREA PER AARD 53-10-00-16 AND AARD 53-10-00-3. (M) 2 L 7 2 4F A6WE 2001121700050 20011217 00050 WP 2001 12 17 AALA20011994 1 20011023 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 59523 49915 TUL - FOUND CORROSION ON SEAT TRACK NR 3. REPLACED SEAT TRACK SRM 51-01. (M) 2 L 7 2 4F A6WE 2001121700051 20011217 00051 WP 2001 12 17 AALA20011995 1 20011122 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 59523 49915 TUL - AFT HINGE CUT OUT FOR AFT LEFT NOSE GEAR DOOR CRACKED. ROUTED OUT CRACK AND INSTALLED DOUBLER PER SRM 53-05-00. (M) 2 L 7 2 4F A6WE 2001121700052 20011217 00052 WP 2001 12 17 AALA20011996 1 20011024 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 59523 49915 TUL - FOUND CORROSION ON LEFT CUSP STATION 583-584. CUT OUT CORRODED AREA AND INSTALLED DOUBLER PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2001121700053 20011217 00053 WP 2001 12 17 AALA20011997 1 20011024 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 59523 49915 TUL - FOUND CORROSION ON LEFT CUSP, STATION 592-595. CUT OUT CORRODED AREA AND INSTALLED DOUBLER PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2001121700054 20011217 00054 WP 2001 12 17 AALA20011998 1 20011024 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 59523 49915 TUL - FOUND CORROSION ON LEFT CUSP, STATION 606-609. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2001121700055 20011217 00055 WP 2001 12 17 AALA20011999 1 20011024 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 59523 49915 TUL - FOUND CORROSION ON LEFT CUSP, STATION 611-613. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-01, INCORPORATE D WITH DOUBLER FORWARD. (M) 2 L 7 2 4F A6WE 2001121700056 20011217 00056 WP 2001 12 17 AALA20012000 1 20011012 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 59523 49915 TUL - NR 2 SEAT TRACK CORRODED AT STATION 1203-1206. REMOVED SEAT TRACK AND INSTALLED NEW TRACK PER SRM 53-03. (M) 2 L 7 2 4F A6WE 2001121700057 20011217 00057 WP 2001 12 17 AALA20012001 1 20011026 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 59523 49915 TUL - FOUND STATION 300 LEFT LONGERON 28, 4 INCH SCRATCH AND DENT BELOW FORWARD LAVATORY SERVICE PANEL ON FUSE SKIN. IN STALLED DOUBLER PER SRM 53-04-00 FIG 12B. (M) 2 L 7 2 4F A6WE 2001121700058 20011217 00058 WP 2001 12 17 AALA20012002 1 20011026 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 59523 49915 TUL - FOUND CORROSION ON LEFT CUSP STATION 991-993. INSTALLED DOUBLER PER 53-00-00-02 AARD. (M) 2 L 7 2 4F A6WE 2001121700059 20011217 00059 WP 2001 12 17 AALA20012003 1 20011026 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 59523 49915 TUL - FOUND CORROSION AND DEEP GOUGE WITH CREASE 1 INCH BY .125 INCH ON RIGHT CUSP AT STATION 1218. INSTALLED DOUBLER A T STATION 1218 PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2001121700060 20011217 00060 WP 2001 12 17 AALA20012004 1 20011025 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 59523 49915 TUL - FOUND CORROSION AND DEEP GOUGE WITH CREASE 1 BY .125 INCH ON RIGHT CUSP STATION 1215. INSTALLED DOUBLER PER SRM 5 3-01. (M) 2 L 7 2 4F A6WE 2001121700061 20011217 00061 WP 2001 12 17 AALA20012005 1 20011023 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 59523 49915 TUL - FOUND CORROSION ON LEFT CUSP STATION 400. INSTALLED DOUBLER PER 53-00-00-02 AARD. (M) 2 L 7 2 4F A6WE 2001121700062 20011217 00062 WP 2001 12 17 AALA20012006 1 20011024 A 5551 FITTING DOUG DC9 DC982 3022082 WP HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 59523 49915 TUL - FOUND HORIZONTAL STAB PIVOT BEARING LUG PLATES HAVE CORROSION IN BORE AND ARE BELOW MINIMUM THICKNESS. REMOVED AN D REPLACED LEFT INBOARD AND OUTBOARD LUG PLATES. REMOVED AND REPLACED RIGHT INBOARD AND OUTBOARD LUG PLATES PER SRM 51 AND 55. (M) 2 L 7 2 4F A6WE 2001121700063 20011217 00063 WP 2001 12 17 AALA20012007 1 20011001 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 59523 49915 TUL - FOUND CORROSION ON NR 5 SEAT TRACK STATION 200 TO 208 AND STATION 208 TO 240. REMOVED DAMAGED SECTION OF SEAT TRA CK AND INSTALLED NEW SECTION OF SEAT TRACK STATION 200 TO 246 PER AARD 53-20-00-10. (M) 2 L 7 2 4F A6WE 2001121700064 20011217 00064 WP 2001 12 17 AALA20012008 1 20011028 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 59523 49915 TUL - FOUND CORROSION ON CUSP STATION 444 LEFT. REMOVED CORROSION. INSTALLED DOUBLER AT STATION 444 LEFT SIDE PER SRM 53-01 FIG 4. (M) 2 L 7 2 4F A6WE 2001121700065 20011217 00065 WP 2001 12 17 AALA20012009 1 20011018 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 59523 49915 TUL - FOUND CORROSION ON LEFT CUSP WEB STATION 727. REMOVED CORROSION. INSTALLED DOUBLER REPAIR PER SRM 53-10 FIG 4. (M) 2 L 7 2 4F A6WE 2001121700066 20011217 00066 WP 2001 12 17 AALA20012010 1 20011029 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 59523 49915 TUL - FOUND TWO CRACKS ON LONGERON 4L AT FASTENER ATTACH POINT TO STATION 160 FRAME. REMOVED DAMAGED SECTION OF LONGERO N AND INSTALLED 1 LONGERON SPLICE AND ONE END PIECE PER SRM 53-02. (M) 2 L 7 2 4F A6WE 2001121700067 20011217 00067 WP 2001 12 17 AALA20012011 1 20011026 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 59523 49915 TUL - FOUND ANGLE CRACKED AT FORWARD UPPER CRACK OF WINDOW FRAME STATION 1175 LEFT. REMOVED AND REPLACED CRACKED ANGLE PER AARD 53-10-00-25. (M) 2 L 7 2 4F A6WE 2001121700068 20011217 00068 WP 2001 12 17 AALA20012024 1 20011023 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 593AA 53256 TUL - FOUND DEEP GOUGE IN FUSELAGE SKIN STATION 402 AT LONGERON 30 AT ANTENNA MOUNT. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-04 FIG 12B. (M) 2 L 7 2 4F RT A6WE 2001121700069 20011217 00069 NM 2001 12 17 TSAA0133162 1 20011126 A 3350 9221009 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED LEFT OVERWING IDENT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2001121700070 20011217 00070 NM 2001 12 17 TSAA0133164 1 20011126 A 3350 BATTERY PACK BOEING 737 737282 13844AT NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 23045 REPLACED LEFT OVERWING IDENT BATTERY PACKED DUE TO LOW VOLTAGE. OP CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001121700071 20011217 00071 NM 2001 12 17 USAA011362 1 20011112 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 346US 41530 23515 TPA - FOUND SKIN CORRODED 3 SQUARE INCHES, STRINGER 25L STATION 975. SPLICED IN SECTION OF STRINGER PER SRM 53-00-03 PA GE 201. (M) 2 L 7 2 4F RT A16WE 2001121700072 20011217 00072 NM 2001 12 17 USAA011363 1 20011112 A 5522 665C2574696 SKIN BOEING 737 7373B7 1384580 NM ELEVATOR DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 385US 31633 22958 PIT - FOUND RIGHT ELEVATOR HAS DELAMINATION TOP SKIN PEELING 2 SPOTS 7.5 INCHES LONG BY 1 INCH WIDE, INBOARD EDGE 84 INC HES OUTBOARD FROM INBOARD 7.5 INCHES LONG BY 1 INCH WIDE. TRAILING EDGE DAMAGE, DELAMINATED AND TOP SKIN TAPE PEELING I N 2 SPOTS REPAIRED PER EA 72905. (M) 2 L 7 2 4F RT A16WE 2001121700073 20011217 00073 NM 2001 12 17 USAA011364 1 20011115 A 5754 SKIN BOEING 737 7373B7 1384580 NM L/E SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 45563 23315 PIT - FOUND ON WALK AROUND, FOUND SKIN CRACKED 3 INCHES, NR 6 SLAT BOTTOM INBOARD END. CUT OUT DAMAGED SKIN, INSTALLED FILLER AND DOUBLER PER SRM 57-43-01, FIG 206. (M) 2 L 7 2 4F RT A16WE 2001121700074 20011217 00074 NM 2001 12 17 USAA011365 1 20011112 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 375US 48438 22954 CLT - FOUND SKIN CRACKED 1.5 INCH, STATION 727 BELOW STRINGER 23R. INSTALLED DOUBLER PER SRM 53-00 FIG 202. (M) 2 L 7 2 4F RT A16WE 2001121700075 20011217 00075 NM 2001 12 17 USAA011370 1 20011120 A 5512 SKIN BOEING 737 7374B7 1384702 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 34253 24554 PIT - FOUND DAILY SKIN CRACKED 2 INCHES, LEFT HORIZ STAB STATION 124-126 LOWER REAR SPAR CHORD. CUT OUT DAMAGED SKIN, H FEC INSPECTION, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 55-10-07A, SRM 55-10-01. (M) 2 L 7 2 4F RT A16WE 2001121700076 20011217 00076 NM 2001 12 17 USAA011371 1 20011116 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 507AU 47167 23382 TPA - FOUND SKIN CRACKED 1 INCH, UPPER HINGE CUT OUT (MFD) STATION 312 STRINGER 11-12. INSTALLED DOUBLER USING FASTENER S PER EA 94247. (M) 2 L 7 2 4F RT A16WE 2001121700077 20011217 00077 NM 2001 12 17 USAA011372 1 20011117 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 507AU 47167 23382 TPA - FOUND SKIN CRACKED .400 INCH SKIN LOWER HINGE CUTOUT (AFT SERVICE DOOR) STATION 947-967. INSTALLED FILLER AND DOU BLERS PER SRM 53-60-01 FIG 208. (M) 2 L 7 2 4F RT A16WE 2001121700084 20011217 00084 EU 2001 12 17 DHL2001362035 1 20011130 A 2760 WARNING LIGHT AIRBUS 300 A300B4203 3930306 EU COCKPIT FALSE INDICATION A DHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 362DH 84 WHILE ATTEMPTING TO STOW SPEED BRAKES INFLIGHT, SPEED BRAKE LIGHT REMAINED ILLUMINATED WITH HANDLE STOW. LIGHT EXTINGUI SHED ONCE BELOW 180 KIAS. PERFORMED OP'S CHECK OF SPEED BRAKE SYS. OP'S CHECK GOOD IAW 27-60-00. 2 L 7 2 4F RT A35EU 2001121700085 20011217 00085 EU 2001 12 17 DHL2001365041 1 20011127 A 5310 A5377561120251 STRUCTURE AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH 149 CORROSION ON CONNECTING SECTION AT FR 26L AT STR 50L. REMOVED SECTION PER SRM 51-30-29. INSTALLED NEW SECTION PER SRM 51 -30-29. 2 L 7 2 4F RT A35EU 2001121700086 20011217 00086 EU 2001 12 17 DHL2001365042 1 20011127 A 5310 A5377560820151 STRUCTURE AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH 149 CORROSION ON CONNECTING SECTION AT FR 26R AT STR 48R. REMOVED CONNECTING SECTION PER SRM 51-30-29. NEW SECTION INSTALLED PER SRM 51-30-29. 2 L 7 2 4F RT A35EU 2001121700087 20011217 00087 WP 2001 12 17 MWEA011486 1 20011217 A 5244 991115793 BEAM DOUG DC9 DC981 3022081 WP GALLEY SVC DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 GALLEY SERVICE DOOR #4 BEAM IS CRACKED IN OUTBOARD RADIUS AT FWD END -- STOP DRILLED CRACK. LOCATED, DRILLED AND INS TALLED REPAIR DOUBLERS. 2 L 7 2 4F A6WE 2001121700088 20011217 00088 EU 2001 12 17 DHL2001365043 1 20011129 A 5320 SILL AIRBUS 300 A300B4203 3930306 EU FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH 149 CRACKED SILL BEAM AFT CARGO FRAME 62. REMOVED FASTENERS AND CUT OUT DAMAGED AREA PER SRM 53-17-00. FABRICATED AND TREATE D REPAIR PARTS. INSTALLED PER SRM 51-40-20. 2 L 7 2 4F RT A35EU 2001121700089 20011217 00089 EU 2001 12 17 DHL2001365536 1 20011123 A 5313 LONGERON AIRBUS 300 A300B4203 3930306 EU FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH 149 CRACK FOUND ON FR 28R OUTER FLANGE BETWEEN 2 VERT FASTENERS BETWEEN STR 14-15 RT DURING NDT INSP. REMOVED FASTENERS PER SRM 51-30-30. REMOVED LONGERON PER SRM 57-30-30. INSTALLED NEW LONGERON PER SRM 57-30-30. 2 L 7 2 4F RT A35EU 2001121700090 20011217 00090 SO 2001 12 17 SWIA200110364 1 20011029 A 5311 FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 215SW 120281 ULTRASONIC INSPECTION OF FRAME 21 FROM STRINGER 20L TO 20R FOUND 2 AREAS, 1 APPROX 1 INCH IN LENGTH BETWEEN FASTENERS TO TAL LOSS OF BACKWALL IN AREA AND SECOND APPROX 1/2 INCH IN LENGTH BETWEEN FASTENERS LOWEST READING .030 INCH. COMPLIED W ITH REPAIR FOR FRAME 21 FROM STRINGER 20L TO 20R IAW SRM 53-00-01 PER SB 120-53-0065. 2 L 7 2 4T RT A31SO 2001121700091 20011217 00091 SO 2001 12 17 SWIA200110376 1 20011123 A 3020 3D237606 EJECTOR VALVE EMB 120 EMB120ER 3260203 SO RT ENGINE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 216SW 120285 LEFT OUTBOARD STAB AND RT ENGINE INLET DEICE BOOTS FAILED INFLIGHT. RAN QRH, RETURNED TO IDA. REMOVED AND REPLACED EJEC TOR VALVE FOR RT ENGINE INLET BOOTS. OPS CHECK GOOD WITH BOTH ENGINES RUNNING. CYCLED BOOTS 6 CYCLES. ALL CHECKS GOOD . P/N: 3D2376-06 S/N OFF: PL352 2 L 7 2 4T RT A31SO 2001121700092 20011217 00092 SO 2001 12 17 SWIA200110377 1 20011124 A 7603 CONTROL CABLE EMB 120 EMB120ER 3260203 SO RT ENGINE FAULTY A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 197SW 120186 RIGHT POWER LEVER WOULD NOT RETARD TO FLIGHT IDLE IN CRUISE FL22.0 OAT-15. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN CHEC K. INSPECTED CABLE FROM POWER LEVER AND ENGINE QUADRANT. CYCLED POWER LEVER SEVERAL TIMES. INSPECTED CABLE FROM ENGINE QUADRANT TO HMU. CABLE WAS TIGHT. REMOVED AND REPLACED CABLE ASSEMBLY IAW 76-10-02. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001121700093 20011217 00093 NM 2001 12 17 01FDEA01073 1 20011215 A 2612 SMOKE DETECTOR BOEING 727 727233 138408A NM INOPERATIVE A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 SO 25 218FE 21101 1-398 IN CLBOUT #6 MAIN CARGO SMOKE DETECTOR LIGHT CAME ON. R&R #6 SMOKE DETECTOR PER MM 26-16-011-4. 2 L 7 3 4F RT A3WE 2001121700094 20011217 00094 NE 2001 12 17 2001UALA01538 2 20010730 A 7250 54L201 BLADE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE ENGINE FRACTURED A UALA E C ENGINE SHUTDOWN ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 WP 29 773UA 8107 8107 26929 777037 APPROX 110 KTS LEFT ENG FAILURE WITH SEVERE DAMAGE. EGT 565, FF0, OIL PRESS 1. ENGINE SHUTDOWN, ABORTED T-O, BRAKE TE MP NORMAL, NORMAL STOP, NO OTHER INDICATIONS. RETURN TO BLOCKS. ENGINE WAS REMOVED DUE TO METAL IN TAILPIPE. FAILURE O RIGINATED AT HIGH PRESSURE TURBINE STAGE 1 BLADE FRACTURED JUST ABOVE THE PLATFORM. THERE WAS EVIDENCE OF STRESS CORROS ION CRACKING. SB PW4G-112-72-240 AND -245 HAD NOT BEEN INCORPORATED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001121700095 20011217 00095 WP 2001 12 17 CNMA200100037 1 20011214 A 3350 EMBS1392 BATTERY PACK DOUG DC10 DC1030 3023501 WP A CNMA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SW 07 720AX 48252 EMERG. LITES WILL NOT GIVE GREE LITE DURING TEST-ALL LIGHTS OPERATEFOUND MID CABIN EMERG LITES POWER SUPPLY INOP R/R MID CABIN PWR SUPPLY OPS CKD NORMALLY PER M/M 33-51 2 L 7 3 4F A22WE 2001121700096 20011217 00096 EA 2001 12 17 COMA0160966 1 20011215 A 3010 6243843 SENSOR CNDAIR CL600 CL6002B19 1900309 EA R/H WING MALFUNCTIONED A COMA A UNSCHED LANDING L NO TEST CR CRUISE 1 SO 01 965CA 12873 7131 FLIGHT - R/H WING OVERHEAT FLOW LINE IS MISSING DURING WING OVERHEAT TEST.REPLACED R/H WING OVERHEAT SENSOR. 2 L 7 2 4F RT A21EA 2001121700097 20011217 00097 NM 2001 12 17 C1HA200194021 1 20011210 A 2560 BATTERY BOEING 727 727290 138408W NM A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 294AS 22146 FLASH LIGHT AT FWD FLT ATT STA. INOPAND PLASTIC SPROCKET MISSING. ACTION TAKEN: R&R FLASHLIGHT BATTERRY AND INSTALLED N EW STRAPS PER M.M. 25-64-01. OK FOR SVC. 2 L 7 3 4F A3WE 2001121700107 20011217 00107 WP 2001 12 17 ZW0A0111601 1 20011129 A 5320 STRUCTURE DOUG DC9 DC983 3022083 WP LT MLG WW CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9628W 53598 DURING CHECK-C MAINT THE LT MAIN LANDING GEAR WHEEL WELL HAD CRACK ON AFT OTBD CORNER OF W/W OPENING. ACCOMP EDDY CURRE NT INSP PER NDT 51-00-01, AND FOUND CRACK CONTAINED. INSTALLED DOUBLER REPAIR PER SRM 53-01, FIG 2, PAGE 10. 2 L 7 2 4F RT A6WE 2001121700108 20011217 00108 WP 2001 12 17 ZW0A0111602 1 20011130 A 5230 SKIN DOUG DC9 DC983 3022083 WP CARGO DOOR CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9628W 53598 DURING CHECK-C MAINT THE AFT CARGO DOOR HAD 1/4 INCH LONG CRACK IN THE DOOR SKIN AT HANDLE CUT OUT. CONFIRMED BY EDDY C URRENT. ACCOMP EDDY CURRENT PER NDT 51-00-03, PART 6. REPAIRED PER SRM 52-05, FIG 30. 2 L 7 2 4F RT A6WE 2001121700109 20011217 00109 WP 2001 12 17 ZW0A0111701 1 20011204 A 5320 STRINGER CLIP DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9628W 53598 DURING CHECK-C MAINT AT FUSELAGE STA 1437 LEFT, INSIDE TAIL COMPT JUST LT OF ACFT CENTER LINE, 1 EA STRINGER TIE CLIP WA S CRACKED, TOP OF FUSELAGE JUST INBD OF FIRST STRINGER LT SIDE. MADE NEW ANGLE PER DRAWING 9911860 AND INSTALLED PER SR M 51-30-5. 2 L 7 2 4F RT A6WE 2001121700110 20011217 00110 WP 2001 12 17 ZW0A0111801 1 20011129 A 5753 WEDGE DOUG DC9 DC982 3022082 WP T/E FLAP DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 912TW 49183 DURING CHECK-C MAINT THE RT WING T/E FLAP, OTBD END OF THE OTBD AFT FLAP HAD DAMAGE TO THE T/E WEDGE. REPAIRED T/E WEDG E PER SRM 57-09, FIG 45. 2 L 7 2 4F A6WE 2001121700111 20011217 00111 NM 2001 12 17 ZW0A0111901 1 20011206 A 3350 LIGHT BOEING 757 7572Q8 1384972 NM CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 713TW 28173 THE EMERGENCY LIGHT AT SEAT ROW 2D, AND THE EGRESS LIGHTS ROW 14 TO 18, WERE INOPERATIVE. REPLACED THE LAMP, PN 8074-1, AT ROW 2D, AND REPLACED SPLICE, PN 65801-003, AT ROW 14 FOR THE EGRESS LIGHTS AT ROW 14 TO 18. 2 L 7 2 4F RT A2NM 2001121700112 20011217 00112 WP 2001 12 17 ZW0A0111902 1 20011206 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 912TW 49183 DURING CHECK-C MAINT THE FLOOR SUPPORT WAS CORRODED AT STA 1155, LBL 22 TO LBL 44. REMOVED AND REPLACED CORRODED PART P ER SPM 6-70-01, PAGE 1. 2 L 7 2 4F A6WE 2001121700113 20011217 00113 2001 12 17 ZW0A0112001 4 20011212 A 3441 CG1237BD01 CONTROL UNIT BOEING 717 717200 1383700 NM IRU MALFUNCTIONED A ZW0A H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 13 2417F 55084 THE NUMBER 1 IRS HAD SMOKE COMING OUT AROUND THE SWITCH DURING POWER DOWN IN THE GATE. REPLACED THE MODE SELECT UNIT. O PEN 2 L 7 2 4F TR A6WE 2001121700114 20011217 00114 WP 2001 12 17 ZW0A0112003 1 20011207 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 912TW 49183 DURING CHECK-C MAINT FOUND CORROSION ON TOP OF FLOOR BEAM CAP AT STA 1250 FROM LBL 24 TO LBL 43. REMOVED PART AND REMOV ED CORROSION PER SPM 6-80-01. INSTALLED PART PER SRM 51-30-2. 2 L 7 2 4F A6WE 2001121700115 20011217 00115 WP 2001 12 17 ZW0A0112004 1 20011207 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 912TW 49183 DURING CHECK-C MAINT THE TIE DOWN TRACK HAD CORROSION AT STA 1127 TO 1140, LBL 34 TO LBL 37. INSTALLED NEW TRACK. 2 L 7 2 4F A6WE 2001121700116 20011217 00116 WP 2001 12 17 ZW0A0112005 1 20011210 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 912TW 49183 DURING CHECK-C MAINT THE FWD CARGO COMPT FLOOR SUPPORT WAS CORRODED AT STA 427, LBL 15 TO RBL 12. REPLACED SUPPORT PER SRM 53-01. 2 L 7 2 4F A6WE 2001121700117 20011217 00117 WP 2001 12 17 ZW0A0112006 1 20011211 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 912TW 49183 DURING CHECK-C MAINT, IN THE FWD CARGO COMPT FOUND A 1/2 INCH CRACK EMANATING FROM EACH SIDE OF RIVET HOLE WHERE AFT BUL KHEAD VERTICAL SUPPORT MOUNTS TO CEILING PANEL SUPPORT, ONE INCH FROM THE LT SIDE WALL, STA 541. INSTALLED STACK DOUBLER AT RIVET HOLE WHERE 2 CRACKS START PER SRM 53-01, PAGE 10. 2 L 7 2 4F A6WE 2001121700118 20011217 00118 2001 12 17 DHL2001363027 4 20011215 A 2565 SLIDE AIRBUS 300 A300B4203 3930306 EU CABIN UNSERVICEABLE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 ESCAPE SLIDE PRESSURE GAUGE IS IN THE RED, NO GO. R&R ESCAPE SLIDE PER M/M 25-61-12. 2 L 7 2 4F RT A35EU 2001121700119 20011217 00119 NM 2001 12 17 UPS01237348 1 20011204 A 5260 UPLOCK CABLE BOEING 727 72725C 138400H NM AFT AIRSTAIR FAILED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:N/A DEPARTURE, AFT AIRSTAIR FAILED TO RETRACT (UPLATCH CABLE FAILED) REPLACED UPLATCH CABLE. 2 L 7 3 4F A3WE 2001121700120 20011217 00120 NM 2001 12 17 UPS01237360 1 20011210 A 3350 100067 LIGHT BOEING 727 72725C 138400H NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 933UP 19857 INSPECTION TYPE:N/A BOTH EMERGENCY LIGHTS INOP. REPLACED BATTERIES IN COCKPIT EMERGENCY LIGHTS. REPLACED EMERGENCY LIGHT ASSY OVER EXIT DOOR P/N ON AND OFF 10-0067, S/N OFF 42-11, S/N O N 27025. OPS CHECKS GOOD 2 L 7 3 4F A3WE 2001121700122 20011217 00122 NM 2001 12 17 UPS01437353 1 20011205 A 3350 LIGHT BOEING 747 747259B 1384804 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 527UP 21730 INSPECTION TYPE:N/A TWO EMERGENCY LIGHTS INOP. (CAPTS/CENTER) RELAMPED LIGHTS IAW MM 33-10-00 CK OK. 2 L 7 4 4F RT A20WE 2001121700123 20011217 00123 NM 2001 12 17 UPS01437358 1 20011203 A 5210 HANDLE BOEING 747 747123 1384873 NM L1 DOOR BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:N/A L1 DOOR INNER HANDLE BROKEN. REMOVED AND REPLACED HANDLE IAW 52-11-13. HANDLE OPS CHECKS OK. 2 L 7 4 4F A20WE 2001121700124 20011217 00124 NM 2001 12 17 UPS01537361 1 20011211 A 3350 BPS73 POWER SUPPLY BOEING 757 75724APF 1384969 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 438UP 25469 INSPECTION TYPE:IN AFTER REPLACING SEVERAL LAMPS, EMERGENCY EXIT LIGHT CAME ON, THEN WENT OUT. UNABLE TO GET IT BACK ON. R&R EMERGENCY EXIT LIGHT POWER SUPPLY AND BATTERY ASSY IAW 33-51-07-2. OPS CHECKS GOOD. 2 L 7 2 4F RT A2NM 2001121700126 20011217 00126 WP 2001 12 17 UPS01837349 1 20011204 A 2612 FIRE WARNING DOUG DC8 DC871F 302199D WP COCKPIT FALSE ACTIVATION A IPXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 713UP 46014 INSPECTION TYPE:N/A ATB-LOWER CARGO COMPT FIRE WARNING LIGHT ILLUM TEMPORARY. PERFORMED MX TEST ON CARGO COMP LOWER PIT SMOKE DETECTOR SYSTEM, NO FAULTS NOTED SYSTEM OPERATES NORMALLY IAW SECURAPLANE TECHNOLOGIES LLC AIRCRAFT MAINT MANUAL. 2 L 7 4 4F RT 4A25 2001121700127 20011217 00127 WP 2001 12 17 UPS01837350 1 20011204 A 3510 REGULATOR DOUG DC8 DC871F 302199D WP COCKPIT FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:N/A DEPARTURE-F/O'S OXY REG EMER SELECTOR FAILED. R&R F/O'S OXY REG 2 L 7 4 4F RT 4A25 2001121700128 20011217 00128 NM 2001 12 17 AWXA200100637 1 20011208 A 3350 20121 CHARGER BOEING 757 757225 1384959 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 915AW 22209 PHX - EEL - C - EMERGENCY EXIT LIGHTS ON SEATS IN FIRST CLASS INOPERATIVE LT SIDE. MAINTENANCE REMOVED AND REPLACED FWD LT SEAT EMERGENCY LIGHT BATTERY PACK AND CHARGER BS 368, IAW BMM 33-51-07. 2 L 7 2 4F RT A2NM 2001121700129 20011217 00129 NM 2001 12 17 AWXA200100638 1 20011208 A 3397 FRFO327SW03 CONNECTOR BOEING 757 757225 1384959 NM CABIN DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 915AW 22209 PHX - EEL - "C" - EMERGENCY DOOR EXIT SIGNS AND ISLE LIGHTS AFT OF MAIN CABIN REMAIN ILLUMINATED AFTER AIRCRAFT IS SHUTD OWN. MAINTENANCE TROUBLESHOT AND FOUND CONNECTOR D40488J & P DAMAGED WITH BENT PINS. REPLACED BOTH J & P CONNECTORS AND PERFORMED EMERGENCY LIGHT OPERATIONAL AND FUNCTIONAL TESTS IAW BMM 33-51-00 PG 501-505. 2 L 7 2 4F RT A2NM 2001121700130 20011217 00130 EU 2001 12 17 AWXA200100639 1 20011212 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 627AW 66 CMH - EEL - "C" - SEVERAL EMERGENCY LIGHTS INOPERATIVE MID CABIN LT SIDE. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UN IT AT 11WL, ZONE 241 IAW AMM 33-51-38-000-001. 2 L 7 2 4F RT A28NM 2001121700131 20011217 00131 EU 2001 12 17 AWXA200100640 1 20011211 A 3350 321430 BATTERY PACK AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 620AW 052 LAX - EEL - "C" - TWO SEAT LIGHTS OUT LEFT FORWARD CABIN. MAINTENANCE REPLACED FORWARD EMERGENCY BATTERY PACK 10WL AT ZO NE 221 PER T/C F1C33301, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2001121700132 20011217 00132 EU 2001 12 17 AWXA200100641 1 20011214 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 644AW 317 SAN - EEL - "C" - RT OVERWING EXIT SIGN 42WL INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY UNIT 12WL AT ZONE 242 IAW AMM 33-51-38-000-001, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2001121700133 20011217 00133 NM 2001 12 17 AWXA200100642 1 20011213 A 2823 405742 CONNECTOR BOEING 737 7373G7 1384595 NM CFMINT CFM56 CFM563B2 13802 EU FUEL SHUTOFF CONTAMINATED A AWXA D RETURN TO BLOCK X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 WP 28 311AW 24712 721658 MCI - RETURN TO BLOCK - FLT 451 - "C" - AFTER PUSH BACK FROM GATE WITH NR 1 ENGINE STARTED, ATTEMPTED TO START NR 2 ENGI NE WHEN NR 1 ENGINE SHUTDOWN, AIRCRAFT WAS PUSHED BACK TO GATE. MAINTENANCE TROUBLESHOT AND FOUND MOISTURE IN THE NR 1 E NGINE FUEL SHUT OFF VALVE ACTUATOR CANNON PLUG. THE CANNON PLUG WAS CLEANED AND RECONNECTED IAW BMM 28-22-11, AND THE FU EL TANK WAS CHECKED FOR WATER (NO WATER FOUND). ENGINES NR 1 AND NR 2 OPERATIONAL CHECKED GOOD AND THE AIRCRAFT WAS RETU RNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2001121700134 20011217 00134 SO 2001 12 17 C2XA01IA417 1 20011216 A 3350 SP9212 SPLICE EMB 145 EMB145LR 3260212 SO CABIN DISCONNECTED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14993 145289 IAH- DURING PREFLIGHT THE CREW NOTED THAT THE EXIT SECTION OF THE EMERGENCY LIGHTS IN THE FLOOR INOPEERATIVE. IAH- MAIN TENANCE RESECURED THE CONNECTORS ON THE EMERGENCY LIGHT FLOOR STRIP BY SEAT 11 and 12, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM,NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001121800001 20011218 00001 NM 2001 12 18 2001UALA02395 1 20011126 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 FWD PIT FRAME DENTED AT STA 660 STR 24R. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REPAIRED WITH FRAME DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2001121800002 20011218 00002 NM 2001 12 18 2001UALA02396 1 20011126 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 AFT CABIN STA 1640 FLOORBEAM UPPER SURFACE HAS CORROSION AROUND N-P HOLES RBL 1 TO RBL 53. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP AND FLANGE CUTOUT REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2001121800003 20011218 00003 NM 2001 12 18 2001UALA02397 1 20011208 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 648UA 25285 MAJOR CABIN FLOORBEAM CORRODED BS 340, RBL 88. CORROSION REMOVAL EXCEEDS SRM LIMITS. MAJOR REPAIR ACCOMPLISHED. REPAI RED FLOORBEAM. 2 L 7 2 4F 4 F RT A1NM E24NE 2001121800004 20011218 00004 NM 2001 12 18 2001UALA02402 1 20011123 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 CABIN FLOORBEAM AT STA 1681 LBL12 HAS CORROSION AROUND NUTPLATE HOLE. MAJOR REPAIR ACCOMPLISHED. FLOORBEAM STRAP & ANG LE DOUBLER INSTALLED. VERIFIED NO CRACKS AFTER DAMAGE REMOVED. 2 L 7 2 4F 4 F RT A2NM E17NE 2001121800005 20011218 00005 EU 2001 12 18 MALA010794 1 20011217 A 3260 UPLOCK SWITCH SAAB SF340 340B 7860101 EU A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 418XJ 340B418 During Flight #3017, Intransit light on Gear Handle remained on when gear up selection was made following Takeoff. Follo wed QRH, same result. Air return to CWA. Landed without incident. Maintenance found NLG Uplock switch to be out of adj ustment. Adjusted NLG Uplock Switch IAW Saab MM 32-61-15. Ops check good. 2 L 7 2 4T RT A52EU 2001121800006 20011218 00006 EU 2001 12 18 MALA010796 1 20011204 A 5320 SEAT TRACK SAAB SF340 340B 7860101 EU CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 406XJ 340B406 During 4K-check in CWA, Cabin Seat Track corrosion at LBL 18.3 Sta 297 to 377. Maintenance replaced Seat Track Section IAW EO S53060. LH Fwd Aisle reail corroded at Flange, out of limits.Maintenance replaced LH Aisle seat rail. 2 L 7 2 4T RT A52EU 2002010300093 20020103 00093 NM 2002 1 3 2001UALA02313 1 20011122 A 5414 311A106577A PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE DEPARTED A UALA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 WP 29 327UA 24147 SERVICE PANEL DEPARTED NR 2 ENGINE ON ROTATION. REINSTALLED PANEL. INSPECTED AREA FOR DAMAGE. NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800011 20011218 00011 NM 2001 12 18 2001UALA02314 1 20011121 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 921UA 25388 DENT ON EXTERIOR FUSELAGE SKIN AT BODY STATION 1004 BELOW STRINGER 14 LEFT. MAJOR REPAIR ACCOMPLISHED, TWO DOUBLERS INS TALLED, ONE BELOW SKIN LAP & ONE ABOVE LAP EXTENDING OVER LAP ONTO LOWER DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800012 20011218 00012 NM 2001 12 18 2001UALA02315 1 20011122 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 921UA 25388 FORWARD NOSE COMPARTMENT RIGHT HAND SIDE 188 FRAME CRACKED IN RADIUS NEAR WL 208.1 ON AFT SIDE OF FRAME. MAJOR REPAIR A CCOMPLISHED, INSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800013 20011218 00013 SO 2001 12 18 C2XA01CL245 1 20011215 A 2760 3605401003 ACTUATOR EMB 145 EMB145LR 3260212 SO LEFT WING LEAKING A C2XA B EMER. DESCENT K FLUID LOSS DE DESCENT 1 SW 27 13913 145438 CLE FLIGHT#3213 THE CREW REPORTED THE #2 HYDRAULIC SYSTEM FAILED.LOST HYDRAULIC QUANTITY.THE AIRCRAFT LANDED IN CLEVELAN D WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE #1 SPEED BRAKE ACTUATOR.OPERATIONAL CHECKS WERE GOOD.T HE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2001121800014 20011218 00014 NM 2001 12 18 2001UALA02316 1 20011121 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 337UA 24241 AFT CARGO DOOR CUT-OUT, FORWARD EDGE STATION 797 AND STRINGER 22R TO 23R, EXTERNAL SKIN GOUGES ON EDGE. MAJOR REPAIR ACC OMPLISHED. REPAIRED AREA WITH DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002010300094 20020103 00094 NM 2002 1 3 2001UALA02317 1 20011123 A 3030 MODULE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 395UA 24670 CAPTAIN AND NR 1 AUX PITOT STATIC HEAT LIGHT ILLUMINATED. PITOT PROBE HEATER FAILED. MAINTENANCE REPLACED OVERHEAD WIN DOW/PITOT HEAT MODULE ASSY AND PITOT PROBE ASSY. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800015 20011218 00015 NM 2001 12 18 2001UALA02318 1 20011123 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 353UA 24321 BODY STATION 178 BULKHEAD RBL 5.7, WL 200 WEB CRACKED. MAJOR REPAIR ACCOMPLISHED, INSTALLED REPAIR DOUBLER ON FORWARD S IDE OF BULKHEAD. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800016 20011218 00016 NM 2001 12 18 2001UALA02319 1 20011123 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 353UA 24321 BODY STATION 178 BULKHEAD WEB CRACKED AT LBL 5.7, WL 122. MAJOR REPAIR ACCOMPLISHED, INSTALLED EXTERNAL DOUBLER ON FORW ARD SIDE OF WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800017 20011218 00017 NM 2001 12 18 2001UALA02321 1 20011123 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 353UA 24321 BODY STATION 178 BULKHEAD WEB CRACKED AT LBL 5.7, WL 197. MAJOR REPAIR ACCOMPLISHED, INSTALLED EXTERNAL DOUBLER ON FORW ARD SIDE OF WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800018 20011218 00018 NM 2001 12 18 2001UALA02324 1 20011125 A 5330 SKIN BOEING 757 757222 1384956 NM FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 595UA 28748 FUSELAGE SKIN DENTED AT STATION 1440 JUST BELOW S20L. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER. 2 L 7 2 4F RT A2NM 2001121800019 20011218 00019 NM 2001 12 18 2001UALA02331 1 20011127 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 STATION 178 BULKHEAD RBL 5.7 WL 200 HAS 2 CRACK INDICATIONS FOUND BY NONDESTRUCTIVE TESTING. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED DOUBLER AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800020 20011218 00020 NM 2001 12 18 2001UALA02333 1 20011127 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 648UA 25285 BODY STATION 246 RBL 68 FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED FLOOR BEAM. 2 L 7 2 4F 4 F RT A1NM E24NE 2001121800021 20011218 00021 NM 2001 12 18 2001UALA02341 1 20011109 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 919UA 25386 MAIN CABIN FLOORBEAM T-CAP STATION 951 CORRODED BEYOND LIMITS BETWEEN RBL 24 AND RBL 30. MAJOR REPAIR ACCOMPLISHED, FAB RICATED NEW T-CAP AND STRAPS INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800022 20011218 00022 NM 2001 12 18 2001UALA02344 1 20011129 A 5320 STRAP BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 921UA 25388 STRAP CRACKED UNDER UPPER CAP OF BODY STATION 727A FRAME AT RBL 18. MAJOR REPAIR ACCOMPLISHED, THE END OF THE STRAP WAS TRIMMED OFF TO REMOVE THE CRACK. REPAIR WAS INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800023 20011218 00023 NM 2001 12 18 2001UALA02348 1 20011129 A 5312 BULKHEAD BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 922UA 26642 STATION 178 BULKHEAD SKIN IS CRACKED 3 INCHES BELOW EXISTING REPAIR. LBL 5 BELOW WL 200. MAJOR REPAIR ACCOMPLISHED, ACCO MPLISHED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800024 20011218 00024 NM 2001 12 18 2001UALA02349 1 20011201 A 5730 DOUBLER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RT WING CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 337UA 24241 RT WING LEADING EDGE SKIN HAS CHAFING WEAR ON SCAB PATCH JUST INBOARD (16 INCHES) OF NR 2 ENGINE. MAJOR REPAIR ACCOMPLIS HED, FABRICATED AND INSTALLED NEW DOUBLER AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800025 20011218 00025 NM 2001 12 18 2001UALA02350 1 20011201 A 5310 DOOR FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 922UA 26642 FORWARD GALLEY DOOR CUTOUT FORWARD LOWER STUB FRAME HAS 2 EACH CRACKS JUST ABOVE FLOOR LEVEL AT STATION 294 RBL 55. MA JOR REPAIR ACCOMPLISHED, REMOVED DAMAGE. FILLER AND FORMED SECTION REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800026 20011218 00026 NM 2001 12 18 2001UALA02351 1 20011130 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 STATION 178 BULKHEAD WEB SHOW CRACK INDICATION AT LBL 5.7 AT WL 212. MAJOR REPAIR ACCOMPLISHED, FABRICATED & INSTALLED D OUBLER AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800027 20011218 00027 NM 2001 12 18 2001UALA02352 1 20011202 A 5320 ANGLE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 922UA 26642 CABIN FLOOR ANGLE AT BL 0 CRACKED FROM STATION 927-947. MAJOR REPAIR ACCOMPLISHED, REPLACED ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800028 20011218 00028 NM 2001 12 18 CALA0101031 1 20011217 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 876-885 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 60312 23363 INSPECTION FOUND FUSELAGE SKIN GOUGED BELOW FORWARD END OF DORSAL FIN ON R/H SIDE AT STA 876-885, RBL 5, S1-S2R. THE GOU GED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 201. 2 L 7 2 4F RT A16WE 2002010300097 20020103 00097 EU 2002 1 3 2001UALA02354 1 20011128 A 3231 S4340131004 VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LANDING GEAR FAILED A UALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 WP 29 445UA 826 ONCE GEAR SELECTED DOWN FOR LANDING ALL THREE GEAR DOORS WOULD NOT RETRACT. NOSE WHEEL STEERING INOP BUT NO ELECTRONIC CENTRALIZED AIRCRAFT MONITORING (ECAM). AFTER ENGINES SHUT DOWN GEAR DOORS RETRACTED. REPLACED LANDING GEAR SAFETY VAL VE (49GA). LEAK CHECKED. NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2002010400019 20020104 00019 EU 2002 1 4 2001UALA02355 1 20011130 A 3232 114122010 ACTUATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT MLG DOOR FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 436UA 638 ELECTRONIC CENTRALIZED AIRCRAFT MONITORING (ECAM) - GREEN HYDRAULIC SYSTEM RESERVOIR OVERHEAT. FOUND GREEN HYDRAULIC SY STEM PRESSURE INDICATING 2000 PSI WITH GEAR DOORS UP. DISCOVERED THAT BY OPENING THE RIGHT HAND MAIN LANDING GEAR DOOR, PRESS RETURNS TO 3000 PSI AS NORMAL. RIGHT HAND DOOR OPENING BYPASS VALVE AND ACTUATOR ARE WARM TO TOUCH. LEFT HAND S IDE COLD TO TOUCH IN COMPARISON. SUSPECT DOOR ACTUATOR HAS INTERNAL LEAKAGE. REPLACED RIGHT HAND MAIN LANDING GEAR DOO R RETRACTION ACTUATOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2002010400020 20020104 00020 EU 2002 1 4 2001UALA02356 1 20011201 A 3232 114122010 ACTUATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT MLG DOOR FAULTY A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 436UA 638 CREW REPORTS LANDING GEAR DOORS NOT CLOSED ELECTRONIC CENTRALIZED AIRCRAFT MONITORING (ECAM) MESSAGE AFTER TAKEOFF. FOU ND GREEN HYDRAULIC SYSTEM PRESSURE INDICATING 2000 PSI WITH GEAR DOORS UP. DISCOVERED THAT BY OPENING THE RIGHT HAND MAI N LANDING GEAR DOOR, PRESS RETURNS TO 3000 PSI AS NORMAL. RIGHT HAND DOOR OPENING BYPASS VALVE AND ACTUATOR ARE WARM TO TOUCH. LEFT HAND SIDE COLD TO TOUCH IN COMPARISON. SUSPECT DOOR ACTUATOR HAS INTERNAL LEAKAGE. REPLACED RIGHT HAND M AIN LANDING GEAR DOOR RETRACTION ACTUATOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2002010400023 20020104 00023 EU 2002 1 4 2001UALA02358 1 20011203 A 3232 114122010 ACTUATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT MLG DOOR FAULTY A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 436UA 638 RESERVOIR OVERHEAT DISPLAYED ON UPPER ELECTRONIC CENTRALIZED AIRCRAFT MONITORING (ECAM) SCREEN. FOUND GREEN HYDRAULIC S YSTEM PRESSURE INDICATING 2000 PSI WITH GEAR DOORS UP. DISCOVERED THAT BY OPENING THE RIGHT HAND MAIN LANDING GEAR DOOR , PRESS RETURNS TO 3000 PSI AS NORMAL. RIGHT HAND DOOR OPENING BYPASS VALVE AND ACTUATOR ARE WARM TO TOUCH. LEFT HAND SIDE COLD TO TOUCH IN COMPARISON. SUSPECT DOOR ACTUATOR HAS INTERNAL LEAKAGE. REPLACED RIGHT HAND MAIN LANDING GEAR DO OR RETRACTION ACTUATOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2001121800031 20011218 00031 NM 2001 12 18 2001UALA02361 1 20011204 A 5320 FLOOR SUPPORT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 922UA 26642 RT CREASE BEAM FLOOR SUPPORT ANGLE CORRODED STATION 947 TO 1006. MAJOR REPAIR ACCOMPLISHED, REPLACED CREASE BEAM FLOOR SUPPORT ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800032 20011218 00032 NM 2001 12 18 2001UALA02362 1 20011204 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 922UA 26642 FORWARD CABIN FLOORBEAM AT BODY STATION 328 RBL 48 DAMAGED AT EDGE OF FLOOR BEAM UPPER CHORD. MAJOR REPAIR ACCOMPLISHE D, STRAP REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800033 20011218 00033 NM 2001 12 18 2001UALA02363 1 20011204 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 922UA 26642 FUSELAGE FRAME OUTER CHORD STATION 188 WL 207 LEFT SIDE IS CRACKED IN RADIUS. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUB LER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800034 20011218 00034 NM 2001 12 18 2001UALA02364 1 20011204 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 922UA 26642 AT STATION 1012 STRINGER 12L, FUSELAGE HAS A DENT OUT OF LIMITS, DENT WITHIN 10 INCHES OF SPLICE, AND COMMON TO A STRING ER. MAJOR REPAIR ACCOMPLISHED, DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800035 20011218 00035 NM 2001 12 18 2001UALA02365 1 20011204 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 922UA 26642 EXTERNAL FUSELAGE AT BODY STATION 1012 APPROXIMATELY ON STRINGER 13L SKIN IS DENTED. MAJOR REPAIR ACCOMPLISHED, SKIN DO UBLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800036 20011218 00036 NM 2001 12 18 2001UALA02366 1 20011204 A 5310 SHEAR TIE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 922UA 26642 STATION 1006 SHEAR TIE BETWEEN STRINGER 11L AND 12L NICKED OUTSIDE RADIUS. MAJOR REPAIR ACCOMPLISHED, FABRICATED NEW SH EAR TIE AND REPAIRED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800037 20011218 00037 NM 2001 12 18 2001UALA02367 1 20011205 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 922UA 26642 FUSELAGE FRAME CHORD AT STATION 188 AT WL 207 RIGHT HAND SIDE IS CRACKED IN RADIUS. MAJOR REPAIR ACCOMPLISHED, FRAME CH ORD REPAIRED AND FUSELAGE DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800039 20011218 00039 NM 2001 12 18 2001UALA02369 1 20011205 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 337UA 24241 BODY STATION 520 FLOOR BEAM WEB CRACKED AT LBL 24.75. MAJOR REPAIR ACCOMPLISHED, ACCOMPLISHED REINFORCEMENT REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800040 20011218 00040 NM 2001 12 18 2001UALA02370 1 20011205 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 361UA 24454 STATION 178 BULKHEAD WEB AT RBL 5 WL 202 HAS CRACK. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED DOUBLER AND FIL LER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800041 20011218 00041 NM 2001 12 18 2001UALA02371 1 20011205 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 361UA 24454 STATION 178 BULKHEAD WEB CRACKED AT LBL 5 WL 199. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED DOUBLER AND FILLE R. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800042 20011218 00042 NM 2001 12 18 2001UALA02372 1 20011206 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 922UA 26642 FUSELAGE SKIN DENTED 8 INCHES LEFT OF LOWER CENTERLINE AT STATION 197. MAJOR REPAIR ACCOMPLISHED, SKIN DOUBLER INSTALLE D. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800043 20011218 00043 NM 2001 12 18 2001UALA02374 1 20011205 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 STATION 1640 BBL 63 FLOORBEAM CAP CORRODED. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR 2 L 7 2 4F 4 F RT A2NM E17NE 2001121800045 20011218 00045 NM 2001 12 18 2001UALA02377 1 20011205 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 CABIN FLOOR SUPPORT STATION 660 TO 680 FLOOR SUPPORT ANGLE IS CRACKED 3 PLACES. MAJOR REPAIR ACCOMPLISHED, REPLACED ANG LE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001121800046 20011218 00046 NM 2001 12 18 2001UALA02378 1 20011204 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 922UA 26642 FORWARD CABIN FLOORBEAM AT BODY STATION 328 RBL 48 HAS DAMAGE WHICH EXCEEDS .250 FROM EDGE OF FLOORBEAM UPPER CHORD. MAJ OR REPAIR ACCOMPLISHED, STRAP REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800047 20011218 00047 NM 2001 12 18 2001UALA02379 1 20011206 A 5512 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE HORIZ STAB DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 923UA 26643 LEFT HORIZONTAL STABILIZER LEADING EDGE, 8 FEET FROM INBOARD END, DENT BETWEEN RIBS. MAJOR REPAIR ACCOMPLISHED, DOUBLER REPAIR MANUFACTURED AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800048 20011218 00048 NM 2001 12 18 2001UALA02380 1 20011206 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 337UA 24241 BODY STATION 188 STRINGER 17R CORD CRACKED. MAJOR REPAIR ACCOMPLISHED, REPAIRED STRINGER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800049 20011218 00049 NM 2001 12 18 2001UALA02381 1 20011206 A 5320 WEB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 337UA 24241 FORWARD CARGO DOOR CLOSING WEB CRACKED AT STRINGER 26R BODY STATION 496. MAJOR REPAIR ACCOMPLISHED, CRACK REPAIRED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002010400024 20020104 00024 EU 2002 1 4 2001UALA02383 1 20011204 A 2913 887673 PUMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ENGINE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 447UA 836 YELLOW HYDRAULIC RESERVOIR OVERHEAT WARNING IN FLIGHT. REPLACED YELLOW SYSTEM ENGINE DRIVEN HYDRAULIC PUMP. 2 L 7 2 4F 4 F RT A28NM E40NE 2002011000144 20020110 00144 NM 2002 1 10 2001UALA02384 1 20011205 A 3040 66642870 COMPUTER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT FAILED A UALA A UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 803UA 748 AFTER TAKE-OFF, HEARD A THUMP ON THE RIGHT SIDE OF THE AIRCRAFT. ELECTRONIC CENTRALIZED AIRCRAFT MONITORING WARNING - RIGHT WINDSHIELD HEAT & RIGHT WINDOW HEAT. SLIGHT ELECTRICAL ODOR. CIRCUIT BREAKER ANTI-ICE RIGHT WINDSHIELD POPPED. THE WINDOW HEAT COMPUTER (WHC) WAS REPLACED. OPERATIONAL TEST WAS ACCOMPLISHED WITHOUT ANY PROBLEMS AND NO FURTHER FAI LURES NOTED ON SUBSEQUENT FLIGHTS. 2 L 7 2 4F 4 F RT A28NM E40NE 2001121800051 20011218 00051 NM 2001 12 18 2001UALA02385 1 20011207 A 5313 STRINGER BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 922UA 26642 CABIN STRINGER 13 LEFT AT STATION 1010 DENTED BETWEEN FASTENERS. MAJOR REPAIR ACCOMPLISHED, REINFORCED STRINGER SPLICE R EPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800052 20011218 00052 NM 2001 12 18 2001UALA02387 1 20011212 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 923UA 26643 STATION 188, WL 207, FUSELAGE RIGHT FRAME CHORD CRACKED IN RADIUS. MAJOR REPAIR ACCOMPLISHED, MANUFACTURED & INSTALLED R EPAIR DOUBLERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800053 20011218 00053 NM 2001 12 18 2001UALA02388 1 20011208 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 337UA 24241 BODY STATION 616 BELOW STRINGER 17R INNER CHORD CRACKED ON FRAME. MAJOR REPAIR ACCOMPLISHED, CRACK REPAIRED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800054 20011218 00054 NM 2001 12 18 2001UALA02389 1 20011208 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 349UA 24253 WEB CRACKED ON STATION 178 BULKHEAD AT WL 195, LBL5.7. MAJOR REPAIR ACCOMPLISHED, CRACK REPAIRED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800055 20011218 00055 NM 2001 12 18 2001UALA02390 1 20011209 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 923UA 26643 EXTERNAL FUSELAGE DENTED STATION 1008 STRINGER 11R. MAJOR REPAIR ACCOMPLISHED, REMOVED DAMAGE & INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002020100017 20020201 00017 EU 2002 2 1 2001UALA02392 1 20011207 A 2160 9104A000601 SENSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 PACK FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 482UA 131 1584 AIR CONDITIONING STUCK FULL HOT IN CABIN. SUPPLEMENTAL DATA UPDATE AFTER TROUBLESHOOTING AND IN CONJUNCTION WITH ASSOCIA TED CFDS FAULT, REPLACED PACK NR 2 INLET PRESSURE SENSOR (36HH). NO FURTHER CFDS OR CREW REPORTED FAULTS. 2 L 7 2 4F 4 F RT A28NM E40NE 2002010300098 20020103 00098 NM 2002 1 3 2001UALA02393 1 20011206 A 2530 OVEN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE GALLEY FIRE A UALA F ACTIVATE FIRE EXT. A FLAME/FIRE NR NOT REPORTED 1 WP 29 302UA 23643 CREW REPORTS FORWARD GALLEY OVEN HAD A SMALL DEBRIS FIRE (PAPER). USED HALON BOTTLE TO EXTINGUISH. REMOVED AND REPLACE D FORWARD OVEN, CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 2002031400172 20020314 00172 NE 2002 3 14 2001UALA02398 2 20011211 A 7261 1A821101 VENT LINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE CRACKED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 548UA 25396 726688 NUMBER 1 ENGINE OIL QUANTITY WENT TO ZERO IN CRUISE. NUMBER 1 SCAVENGE BEARING MANIFOLD BREATHER VENT TUBE CRACKED. 2 L 7 2 4F 4 F RT A2NM E17NE 2001121800056 20011218 00056 NM 2001 12 18 2001UALA02403 1 20011123 A 5312 PRESSURE PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 STA 1681 PRESSURE DECK EXCESSIVE MATERIAL LOSS AT LBL 3 & 12 MAJOR REPAIR ACCOMPLISHED, DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002010300101 20020103 00101 NM 2002 1 3 2001UALA02405 1 20011212 A 5315 141W85191 FLOORBEAM BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 783UA 21863 26950 THE BODY STATION 246 FLOORBEAM MID CHORD IS CRACKED AT LBL7.88, RBL26.06 AND RBL 38.00. MAJOR REPAIR ACCOMPLISHED. A N EW ANGLE SECTION WAS SPLICED PER SRM 53-10-51-201 REPAIR 2. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001121800057 20011218 00057 SO 2001 12 18 SWIA200110378 1 20011125 A 3010 BOOT EMB 120 EMB120ER 3260203 SO HORIZ STAB LEAKING A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 197SW 120186 LEADING EDGE DEICE BOOTS FAILED (VERTICAL FIN AND RIGHT OB STAB) BOTH TIMERS. INSPECTED HORIZONTAL AND VERTICAL STAB. DE ICE BOOTS. FOUND RIGHT OUTBOARD BOOT TO HAVE HOLE AND LEAKY PATCH. REPAIRED RIGHT OUTBOARD BOOT IAW 30-00-00. OPS CHE CK GOOD. 2 L 7 2 4T RT A31SO 2001121800058 20011218 00058 SO 2001 12 18 SWIA200110379 1 20011126 A 3232 WTC2246 ACTUATOR EMB 120 EMB120ER 3260203 SO RT MLG DOOR FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 234SW 120308 RT MLG WOULD NOT RETRACT. A&B SYSTEM LIGHTS REMAINED ILLUMINATED. TESTED GEAR LIGHTS AND RECYCLED GEAR AS PER THE SOP. NO CHANGE. R&R RT GEAR DOOR SHUTOFF VALVE AND R OUTBOARD GEAR DOOR ACTUATOR. OPS CHECK GOOD IAW 32-32-05. 2 L 7 2 4T RT A31SO 2001121800059 20011218 00059 EA 2001 12 18 SWIA200110380 1 20011125 A 2613 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 416SW 7089 ON TAKEOFF PRIOR TO V1 RECEIVED A WING OVERHEAT MESSAGE AND ABORTED THE TAKEOFF. MESSAGE DISAPPEARED WITH THE POWER RED UCTION. PERFORMED AN OPERATIONAL TEST OF THE WING ANTI-ICE SYSTEM. OPS CHECK GOOD AT HIGH AND LOWER POWER SETTINGS IAW CRJ MM 30-12-00. 2 L 7 2 4F RT A21EA 2001121800060 20011218 00060 SO 2001 12 18 SWIA200110381 1 20011119 A 2752 WIRE EMB 120 EMB120ER 3260203 SO FLAP ACTUATOR BROKEN A SWIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 07 220SW 120288 ON TAXI OUT FLAP CONTROL FAULT INDICATION OCCURRED UPON FLAP DEPLOYMENT TO 15 DEGREES. LEFT LVDT FLR ON ANNUNCIATOR OUTB OARD PAIR. FOUND BROKEN WIRE AND REPAIRED ON LEFT OUTBOARD FLAP ACTUATOR CANNON PLUG. OPS CHECK GOOD ON FLAP EXTENSION AND RETRACTION. 2 L 7 2 4T RT A31SO 2001121800061 20011218 00061 EA 2001 12 18 SWIA200110382 1 20011126 A 2760 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 595SW 7292 SHORTLY AFTER TAKEOFF GOT THE FOLLOWING STATUS MESSAGES, IB GND SPLR FAULT & OB GND SPLR FAULT. MESSAGES DISAPPEARED AF TER LANDING. POWERED DOWN AIRCRAFT; POWERED UP. PERFORMED TEST OF SPOILER SYSTEM. COULD NOT DUPLICATE. OPS CHECK GOOD . 2 L 7 2 4F RT A21EA 2001121800062 20011218 00062 2001 12 18 SWIA200110383 4 20011126 A 2213 6229815704 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA AUTOPILOT SYS FAULTY A SWIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 07 439SW 7578 CLIMBING OUT OF ELP THE AIRCRAFT CONTINUALLY YAWED LEFT AND RIGHT, NO MESSAGES. PERFORMED TEST OF YAW DAMPENERS IAW 22-2 2-01 AND NOTED FAILURE. REMOVED AND REPLACED NR 2 FCC CARD IAW 22-12-14. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2001121800063 20011218 00063 SO 2001 12 18 SWIA200110384 1 20011126 A 3010 PRESSURE SWITCH EMB 120 EMB120ER 3260203 SO HORIZ STAB MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 563SW 120338 LEFT INBOARD HORIZONTAL DEICE BOOT INOP. INSTALLED SERVICEABLE PRESSURE SWITCH FOR LEFT INBOARD HORIZONTAL DEICE BOOT I AW MM 30-10-05. LEAK CHECK & OPS CHECK OF DEICE BOOT GOOD. 2 L 7 2 4T RT A31SO 2001121800064 20011218 00064 SO 2001 12 18 SWIA200110385 1 20011127 A 2752 3431001001 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP FAILED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 298SW 120328 RIGHT NACELLE FLAP WOULD NOT RETRACT AFTER LANDING. REPLACED RIGHT NACELLE FLAP ACTUATOR. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001121800065 20011218 00065 SO 2001 12 18 SWIA200110386 1 20011127 A 3233 ACTUATOR EMB 120 EMB120ER 3260203 SO LT MLG OUT OF ADJ A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 237SW 120314 LT MLG WOULD NOT RETRACT AFTER TAKEOFF. SYSTEM A&B LIGHTS INDICATED RED WITH GEAR HANDLE IN THE UP POSITION. RETURNED TO SMX. SHORTENED LEFT MAIN GEAR ACTUATOR ROD END 1/2 TURN. CYCLED GEAR MULTIPLE TIMES. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2001121800066 20011218 00066 SO 2001 12 18 SWIA200110387 1 20011127 A 3231 12032943001 SEQUENCE VALVE EMB 120 EMB120ER 3260203 SO RT MLG DOOR MALFUNCTIONED A SWIA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 NM 07 198SW 120227 AFTER DEPARTURE GEAR RETRACTION, NOTICED RIGHT MAIN GEAR A & B INDICATIONS REMAINED RED. COULD FEEL CONTINUOUS GRINDING /RATTLING THROUGH AIRFRAME. ELECTED TO EXTEND GEAR RESULTING IN A NORMAL GEAR DOWN INDICATION. RETURNED TO SLC. REPLA CED RIGHT INBOARD GEAR DOOR SEQUENCE VALVE IAW MM 32-34-00. SWUNG GEAR SEVERAL TIMES. OPS CHECK GOOD. NO LEAKS NOTED AT SEQUENCE VALVE. 2 L 7 2 4T RT A31SO 2001121800067 20011218 00067 SO 2001 12 18 SWIA200110388 1 20011120 A 2611 SMOKE WARNING EMB 120 EMB120ER 3260203 SO COCKPIT FALSE ACTIVATION A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 292UX 120292 DURING TAKEOFF ROLL, TRIPLE CHIME FOLLOWED BY SMOKE ON MAP, FOLLOWED BY LAVATORY SMOKE ALARM.RAN AIRCRAFT UP TO STATIC P OWER WITH PACKS ON. COULD NOT DUPLICATE SMOKE ALARM ON MAP PANEL OR BY LAVATORY ALARM. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001121800068 20011218 00068 EA 2001 12 18 SWIA200110389 1 20011121 A 2421 755469E IDG CNDAIR CL600 CL6002B19 1900309 EA NR 1 ENGINE FAILED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 426SW 30 30 7468 IDG1 MESSAGE ON TAKEOFF ROLL. ABORTED TAKEOFF. RESET GEN BUT CAME OFF LINE AGAIN. REMOVED AND REPLACED NR 1 IDG WITH S ERVICEABLE UNIT IAW MM 24-11-01. LEAK AND OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2001121800069 20011218 00069 2001 12 18 SWIA200110390 4 20011122 A 2210 AUTOPILOT SYS EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 215SW 120281 AUTOPILOT TRIM RED LIGHTS CAME ON DURING TAKE OFF, ABORTED. CYCLED AUTO PILOT CIRCUIT BREAKERS OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001121800070 20011218 00070 EA 2001 12 18 SWIA200110391 1 20011125 A 3260 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 410SW 7066 AFTER TAKEOFF DURING GEAR RETRACTION NOSE GEAR FAILED TO RETRACT AND WAS ACCOMPANIED BY GEAR DISAGREE AND NOSE DOOR OPEN MESSAGES WITH GEAR INDICATION SHOWING BOTH MAINS WHITE AND THE NOSE YELLOW. RETURNED TO THE AIRPORT. PERFORMED LANDIN G GEAR OPERATIONAL CHECKS. SWUNG GEAR 15 CYCLES WITH NO DEFECTS NOTED AT THIS TIME. OPERATIONAL CHECKS SATISFACTORY. 2 L 7 2 4F RT A21EA 2001121800071 20011218 00071 SO 2001 12 18 SWIA200110392 1 20011124 A 3231 SEQUENCE VALVE EMB 120 EMB120ER 3260203 SO RT MLG OUT OF ADJ A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 234SW 120308 RT MAIN LANDING GEAR WOULD NOT RETRACT. RED A & B LIGHTS REMAINED ILLUMINATED. CYCLED THE GEAR MULTIPLE TIMES. LIGHT REMAINED ILLUMINATED. GEAR DID NOT RETRACT. RETURNED TO FIELD. ADJUSTED RT MAIN GEAR DOOR SEQUENCE VALVE. EXTENDED A ND RETRACTED GEAR SEVERAL TIMES. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001121800072 20011218 00072 SO 2001 12 18 SWIA200110393 1 20011124 A 3260 TARGET EMB 120 EMB120ER 3260203 SO NLG OUT OF ADJ A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 212SW 120276 UPON GEAR RETRACTION A FLUTTERING VIBRATION WAS HEARD. NOSE GEAR RED A & B CIRCUITS LIGHTS WERE BOTH ILLUMINATED. CYCL ED GEAR DOWN AND RETURNED TO LAND AT SGU. ADJUSTED NOSE LANDING GEAR UPLOCK TARGETS. SWUNG GEAR SEVERAL TIMES IAW MM 3 2-30-00. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2001121800073 20011218 00073 2001 12 18 SWIA200110395 4 20011127 A 2213 CIRCUIT BOARD CNDAIR CL600 CL6002B19 1900309 EA AUTOPILOT SYS FAULTY A SWIA O OTHER E F VIBRATION/BUFFET FLT CONT AFFECTED DE DESCENT 1 NM 07 594SW 7293 ON DESCENT, NOTICED RUDDER FLUTTER. BOTH RUDDER INDICATION & AERODYNAMIC FLUTTER OBSERVED AT VARIOUS SPEEDS. ON THE GRO UND, STILL OBSERVED RUDDER FLUCTUATIONS (ABOUT 3 DEGREES BOTH SIDES). AT FL330 AND MACH .77 EXPERIENCED AN UNCOMMANDED R UDDER MOVEMENT. VERIFIED BY FEELING A/C MOVE ABOUT VERT AXIS AND FLIGHT CONTROL PAGE. INSPECTED PRIMARY & SECONDARY BREA KOUT FORCE ON RUDDER FEEL MECHANISMS. WITHIN TOLERANCES PER 27-21-00. REPLACED NR 1 AND NR 2 FCC CIRCUIT CARD ASSEMBLIES . AUTOPILOT SYSTEM OPS CHECK GOOD IAW MM22-11-07. 2 L 7 2 4F RT A21EA 2001121800074 20011218 00074 SO 2001 12 18 SWIA200110396 1 20011127 A 2721 CONTROL CABLE EMB 120 EMB120ER 3260203 SO RUDDER TAB FRAYED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 290SW 120317 RUDDER TRIM CABLE IS FRAYED DOWN TO A SINGLE STRAND. IT WAS DISCOVERED DURING APU SHORT TROUBLESHOOTING. REPLACED RIGH T RUDDER TRIM CABLE PER MM 27-11-01. 2 L 7 2 4T RT A31SO 2001121800075 20011218 00075 SO 2001 12 18 SWIA200110397 1 20011124 A 3020 PRESSURE SWITCH EMB 120 EMB120RT 3260202 SO LT INLET FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 593SW 120191 LEFT ENGINE INLET DEICE BOOT FAILS IN FLIGHT. REPLACED AND SECURED LEFT INLET DEICE BOOT PRESSURE SWITCH. COMPLIED WIT H ENGINE RUN OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001121800076 20011218 00076 SO 2001 12 18 SWIA200110398 1 20011127 A 2620 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO COCKPIT FALSE INDICATION A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 198SW 2164 2164 120227 BOTTLE B FIRE EXTINGUISHING (AMBER) CAME ON ON TAKEOFF ROLL. ABORTED TAKEOFF. VERIFIED B BOTTLE PRESSURE, STILL IN GRE EN. REMOVED AND REPLACED RIGHT FIRE BOTTLE PER EMB120 MM 26-21-01. FIRE BOTTLE TESTED GOOD. 2 L 7 2 4T RT A31SO 2001121800077 20011218 00077 SO 2001 12 18 SWIA200110399 1 20011129 A 3010 BOOT EMB 120 EMB120ER 3260203 SO HORIZ STAB LEAKING A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 197SW 120186 VERTICAL FIN AND RIGHT OUTBOARD STAB DEICE BOOTS FAIL ON BOTH TIMERS. REMOVED & REPLACED RIGHT HORIZONTAL DEICE BOOT IA W EMB 30-10-00 & FAST BOOT INSTRUCTION. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2001121800078 20011218 00078 SO 2001 12 18 SWIA200110400 1 20011129 A 3233 1959500007 ACTUATOR EMB 120 EMB120ER 3260203 SO RT MLG FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 198SW 120227 RIGHT MAIN GEAR SHOWED RED LIGHTS & HEARD RUMBLING NOISE AFTER RETRACTION. RECYCLED GEAR, SAME INDICATION. EXTENDED GE AR & RETURNED TO SLC. REMOVED & REPLACED MLG ACTUATOR IAW MM 32-32-10. OPS CHECK GOOD . 2 L 7 2 4T RT A31SO 2001121800079 20011218 00079 SO 2001 12 18 SWIA200110401 1 20011129 A 3010 BOOT EMB 120 EMB120ER 3260203 SO LT WING DAMAGED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 186SW 120034 LEFT AND RIGHT MIDDLE WING DEICE BOOTS LIGHTS CAME ON IN CLIMB.PATCHED HOLE IN LEFT MIDDLE WING DEICE BOOT IAW CMM. 2 L 7 2 4T RT A31SO 2001121800080 20011218 00080 SO 2001 12 18 SWIA200110402 1 20011127 A 2133 OUTFLOW VALVE EMB 120 EMB120ER 3260203 SO CABIN PRESSURE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 291SW 120318 ON TAKEOFF WITH THE CONTROLLER IN MANUAL, THE PRESSURIZATION SYSTEM SHOWED A CLIMB RATE OF 2000 FPM WITH A PRESSURE DIFF ERENTIAL OF 0. WE FOLLOWED WITH A CLIMB TO 9,500 AND TRIED DIFFERENT MANUAL ADJUSTMENTS BUT WE WERE NOT ABLE TO PRESSUR IZE THE CABIN. REPLACED BOTH AUTO CONTROLLERS AND ELECTROPNEUMATIC OUTFLOW VALVE AND PRESSURIZED AIRCRAFT. OPS CHECK G OOD. 2 L 7 2 4T RT A31SO 2001121800081 20011218 00081 SO 2001 12 18 SWIA200110404 1 20011130 A 2752 3430001001 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP FAILED A SWIA O OTHER J WARNING INDICATION UK UNKNOWN 1 NM 07 198SW 120227 FLAP ASYMMETRY INDICATION FOR RIGHT INBOARD FLAPS. REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATOR IAW MM 27-50-07. O PS CHECK IAW 27-50-00. 2 L 7 2 4T RT A31SO 2001121800082 20011218 00082 2001 12 18 SWIA200110405 4 20011201 A 2210 6229968001 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA AUTOPILOT SYS FAULTY A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 439SW 7578 AIRCRAFT OSCILLATED ABOUT YAW AXIS INFLIGHT INTERMITTENTLY. AIRCRAFT OSCILLATING INFLIGHT AROUND YAW AXIS. REMOVED AND REPLACED NR 2 YAW DAMPER IAW 22-22-01. OPS CHECK GOOD. P/N: 622-9508-001 S/N OFF: 2761 REPLACED NR 1 YAW DAMPER ACTUATOR IAW 22-22-00. PERFORMED FUNCTIONAL CHECK OF YAW DAMPER IAW MM 22-22-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2001121800083 20011218 00083 WP 2001 12 18 2001F00740 1 20011206 A 3350 873100272 LIGHT DOUG DC9 DC981 3022081 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 827US 48049 IND - THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS, TAIL CONE EMERGENCY LIGHT RECEIVER, AFT OVERWING EMERGENCY EXIT LIGHT S AND CEILING LIGHTS AT SEAT ROWS 18 TO 21 WERE DIM. THE RIGHT AFT OVERWING IDENTIFIER LIGHT WAS INOPERATIVE. MAINTENA NCE REPLACED THE EMERGENCY LIGHT BATTERIES FOR THE DIM POSITIONS, AND THE RIGHT AFT OVERWING IDENTIFIER LIGHT ASSEMBLY. (M) 2 L 7 2 4F A6WE 2001121800084 20011218 00084 2001 12 18 2001F00741 4 20011107 A 2300 C11 PLUG GULSTM G1159 G1159 3953505 SO COCKPIT GROUNDED A KKYA A UNSCHED LANDING O OTHER CL CLIMB 1 NE 03 92AG 12500 110 DEPARTING SLC EXPERIENCED A RADIO PROBLEM, BOTH COM'S BECAME INTERMITTENT. CIRCLED THE AIRPORT MAINTAINING VFR, AND REE STABLISHED CONTACT WITH ATC FOR THE REMAINDER OF TIME. ELECTED TO LAND AT OGD. MX SUPERVISOR WAS NOTIFIED, AND LOCAL M X T/S THE PROBLEM. THE PILOTS HAND MIC JACK HAD BEEN GROUNDED THUS ACTING TO KEY THE MIC CONTINUOUSLY. THE JACK WAS SE CURED, AND THE CO-PILOTS MICROPHONE WAS REPLACED. NUMEROUS RADIO CHECKS WERE MADE WITHOUT DIFFICULTY. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A12EA 2001121800085 20011218 00085 CE 2001 12 18 2001F00742 1 20011110 A 3234 1013841377 CONTROL HANDLE BEECH 1900 1900D 1154162 CE COCKPIT INTERMITTENT A GUUA O OTHER J WARNING INDICATION AP APPROACH 1 SO 19 69549 UE194 FLT 9159 - NAS/FLL - DURING APPROACH, LANDING GEAR WOULD NOT EXTEND ON FIRST TRY. EXTENDED ON SECOND ATTEMPT. REMOVED AND REPLACED LANDING GEAR SELECTOR. PERFORMED LANDING GEAR EXTENSION AND RETRACTION. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4T RT A24CE 2001121800086 20011218 00086 CE 2001 12 18 2001F00743 1 20010924 A 3260 H111541 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE LT MLG FAILED A GUUA O OTHER J WARNING INDICATION CL CLIMB 1 SO 19 16540 UE172 FLT 9430 - TPA/MIA - AFTER TAKEOFF, RIGHT MLG WOULD NOT FULLY RETRACT. GEAR HANDLE LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED LEFT MAIN GEAR UPLOCK SWITCH AND RIGGED. SYSTEM OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4T RT A24CE 2001121800087 20011218 00087 CE 2001 12 18 2001F00744 1 20011104 A 3260 H111541 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE RT MLG FAILED A GUUA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 19 17534 UE141 FLT 9122 - NAS/FLL - DURING FLIGHT, LANDING GEAR HANDLE LIGHT ILLUMINATED AND GEAR WARNING HORN SOUNDED. REMOVED AND RE PLACED RIGHT UPLOCK SWITCH. OPS CHECK NORMAL. (M) 2 L 7 2 4T RT A24CE 2001121800088 20011218 00088 EA 2001 12 18 COMA0160967 1 20011216 A 3010 32144424 VALVE CNDAIR CL600 CL6002B19 1900309 EA R/H MALFUNCTIONED A COMA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 SO 01 446CA 48 7546 FLIGHT #5371 WING ANTI ICE CAUTION MESSAGE.REPLACED THE R/H MODULATING AND SHUT OFF VALVE. 2 L 7 2 4F RT A21EA 2001121800089 20011218 00089 EA 2001 12 18 COMA0160968 1 20011216 A 2710 6224404001 SERVO CNDAIR CL600 CL6002B19 1900309 EA WING DRAGGING A COMA K NONE F FLT CONT AFFECTED CL CLIMB 1 SO 01 924CA 10913 7026 FLIGHT #5965 - AP RWD AND LWD MESSAGE ON EICAS. AILERON CONTROL BINDING.COULD NOT DUPLICATE. REPLACED THE AILERON SERVO FOR TROUBLE SHOOTING. 2 L 7 2 4F RT A21EA 2001121800090 20011218 00090 CE 2001 12 18 2001F00745 1 20011007 A 3234 1013841379 CONTROL HANDLE BEECH 1900 1900D 1154162 CE COCKPIT WEAK A GUUA O OTHER O OTHER AP APPROACH 1 SO 19 17541 UE203 FLT 9172 - FPO/FLL - DURING APPROACH, LANDING GEAR INTRANSIT LIGHTS INOPERATIVE. REMOVED AND REPLACED LANDING GEAR CONT ROL HANDLE. PERFORMED LANDING GEAR EXTENSION AND RETRACTION. OPS CHECK NORMAL. (M) 2 L 7 2 4T RT A24CE 2001121800091 20011218 00091 NM 2001 12 18 2001F00746 1 20011108 A 4990 380029812 OIL SYSTEM BOEING 757 7572T7 1384914 NM APU LOW A N8TA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 19 513NA 22614 23895 DURING CRUISE, APU OIL ADD LIGHT CAME ON, APU SHUT DOWN. ATTEMPTED RESTART TWICE WITH NO SUCCESS. RIGHT IDG PREVIOUSLY PLACED ON MEL. ACCOMPLISHED UNEVENTFUL, UNSCHEDULED LANDING. SERVICE APU WITH 3 QUARTS OF OIL, CHECKED CHIP DETECTORS . PERFORMED APU BITE CHECK AND CLEARED OIL LOW MESSAGE. OPERATIONALLY AND LEAK CHECKED APU, GOOD. (M) 2 L 7 2 4F RT A2NM 2001121800092 20011218 00092 NM 2001 12 18 2001F00748 1 20011031 A 5610 WINDOW BOEING 727 727259 138408J NM COCKPIT CRACKED A FX7A A UNSCHED LANDING O OTHER CR CRUISE 1 SO 19 203AV 22474 DURING CRUISE AT FLIGHT LEVEL 35,000, LEFT WINDOW L1 CRACKED. AIRCRAFT DIVERTED TO MDSD. AIRCRAFT INSPECTED AS REQUIRE D FOR FERRY FLIGHT PER MM 56-11-0. WINDSHIELD WAS REPLACED PER MM 56-11-11. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001121800093 20011218 00093 NM 2001 12 18 2001F00749 1 20011111 A 2410 700842A CSD BOEING 727 727259 138408J NM NR 3 ENGINE MALFUNCTIONED A FX7A A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 SO 19 203AV 22474 DURING CLIMB-OUT OF SVMI, 25 MINUTES AFTER TAKEOFF NR 3 CSD GEN TEMP IN 160 DEGREES, RISE 25 DEGREES VOLTS 110 FREQS 390 , AFTER REDUCING LOAD AND 10 MINUTES LATER, TEMP 120 RISE 18. AIRCRAFT RETURNED TO SVMI, DUE TO NR 2 CSD ALREADY DEFERR ED. REMOVED AND REPLACED NR 2 AND NR 3 CSD (P/N 700842A AND S/N'S 15340 AND 7366), AND CSD OIL COOLERS (P/N 6A47000 AND S/N'S 9948 AND 10102) IAW MM 24-10-61. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001121800094 20011218 00094 NM 2001 12 18 2001F00750 1 20011111 A 2410 700842A CSD BOEING 727 727259 138408J NM NR 2 ENGINE MALFUNCTIONED A FX7A A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 SO 19 203AV 22474 DURING CLIMB-OUT OF SVMI, 25 MINUTES AFTER TAKEOFF NR 3 CSD GEN TEMP IN 160 DEGREES, RISE 25 DEGREES VOLTS 110 FREQS 390 , AFTER REDUCING LOAD AND 10 MINUTES LATER, TEMP 120 RISE 18. AIRCRAFT RETURNED TO SVMI, DUE TO NR 2 CSD ALREADY DEFERR ED. REMOVED AND REPLACED NR 2 AND NR 3 CSD (P/N 700842A AND S/N'S 15340 AND 7366), AND CSD OIL COOLERS (P/N 6A47000 AND S/N'S 9948 AND 10102) IAW MM 24-10-61. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001121800095 20011218 00095 WP 2001 12 18 2001F00739 1 20011206 A 3350 AD4002P BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 827US 48049 IND - THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS, TAIL CONE EMERGENCY LIGHT RECEIVER, AFT OVERWING EMERGENCY EXIT LIGHT S AND CEILING LIGHTS AT SEAT ROWS 18 TO 21 WERE DIM. THE RIGHT AFT OVERWING IDENTIFIER LIGHT WAS INOPERATIVE. MAINTENA NCE REPLACED THE EMERGENCY LIGHT BATTERIES FOR THE DIM POSITIONS, AND THE RIGHT AFT OVERWING IDENTIFIER LIGHT ASSEMBLY. (M) 2 L 7 2 4F A6WE 2001121800096 20011218 00096 NM 2001 12 18 2001F00753 1 20011103 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 804MA 22435 DURING PREFLIGHT INSPECTION, FOUND CENTER OVERWING LIGHT INOPERATIVE. TROUBLE SHOT SYSTEM, FOUND BATTERY PACK LOW. REM OVED AND REPLACED CENTER OVERWING BATTERY PACK. OPS TEST ON GROUND NORMAL IAW MM 33-10-0 AND 33-50-02. AIRCRAFT RETURN ED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001121800097 20011218 00097 2001 12 18 2001F00754 4 20011130 A 3452 G669024 CONTROL HEAD BOEING 757 757236 1384971 NM TRANSPONDER MALFUNCTIONED A N8TA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 19 547NA 29946 SMOKE FROM AROUND NR 2 TRANSPONDER CONTROL HEAD. REMOVED AND REPLACED NR 2 TRANSPONDER CONTROL HEAD, SYSTEM OPS CHECK G OOD. (M) 2 L 7 2 4F RT A2NM 2001121800098 20011218 00098 WP 2001 12 18 HALA0100277 1 20011126 A 5320 STRUCTURE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 135AA 47830 HNL - EXFOLIATION CORROSION FUSELAGE STATION 1079 LONGERON 46L. REMOVED FASTENERS, CUT OUT DAMAGE. EDDY CURRENT FOUND NO CRACKS. REPAIRED PER DC-10 SRM 53-20-00 FIG 13. (M) 2 L 7 3 4F A22WE 2001121800099 20011218 00099 NM 2001 12 18 HALA0100280 1 20011129 A 2612 2520545 FIRE LOOP BOEING 767 76733A 1385209 NM RT ENGINE DAMAGED A HALA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 13 581HA 28141 HNL - FLT 32 - RIGHT ENGINE FIRE LOOP FAILED. TROUBLE SHOT RIGHT ENGINE FIRE DETECTOR SYSTEM PER FIM 29-11-00 PAGE 101 FIG 104. FOUND AFT UPPER FIREWALL 'B' LOOP HAS HIGH RESISTANCE LOOP P/N 2520545. REPLACED UPPER AFT FIRE WALL ELEMENT ASSY, OPS CHECK OK PER MM 26-11-00. (M) 2 L 7 2 4F RT A1NM 2001121800100 20011218 00100 NM 2001 12 18 USAA011360 1 20011029 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 336US 44590 23233 PIT - FOUND SKIN CRACKED 1.625 INCH, STATION 740 1.5 INCH BELOW STRINGER 23R. CUT OUT DAMAGE, INSTALLED FILLER AT STRIN GER, INSTALLED DOUBLER PER SRM 53-00-01 FIG NR 201. (M) 2 L 7 2 4F RT A16WE 2001121800101 20011218 00101 EU 2001 12 18 USAABA01014 1 20011124 A 7710 O154GT2 PROBE AIRBUS 330 A330323 3930335 EU RT ENGINE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 673UW 0337 PHL - FLT 740 - ON CLIMB-OUT FROM PIT AND FL270, CREW NOTED AN ECAM WARNING AND THAT THE N1 INDICATION HAD FAILED. FLIG HT DIVERTED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE P2T2 PROBE. (M) 2 L 7 2 4F RT A46NM 2001121800102 20011218 00102 EU 2001 12 18 USAABA01015 1 20011130 A 7601 52D279 CONTROL UNIT AIRBUS 330 A330323 3930335 EU RT ENGINE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 673UW 7626 0337 PHL - FLT 126 - EN ROUTE PHL-LGW, CREW RECEIVED THE E/W 'ENGINE 2 EPR MODE FAULT' AND NOTED A TWO INCH THROTTLE SPLIT. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE RELAY CONTROL UNIT. (M) 2 L 7 2 4F RT A46NM 2001121800103 20011218 00103 WP 2001 12 18 USAAD01180 1 20011109 A 3350 LIGHT DOUG DC9 DC981 3022081 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 801US 48037 EWR - THE EMERGENCY LIGHT NOT ARMED BULB INOPERATIVE. MAINTENANCE RESET THE EMERGENCY LIGHTS ARM AND CHARGE CIRCUIT BRE AKER. REPLACED THE FORWARD CONTROL MODULE PRECAUTIONARY. (M) 2 L 7 2 4F A6WE 2001121800104 20011218 00104 WP 2001 12 18 USAAD01182 1 20011122 A 3233 3937030501 LINK DOUG DC9 DC982 3022082 WP LT MLG BROKEN A USAA K NONE J WARNING INDICATION CL CLIMB 1 EA 19 815US 48095 MDT-PIT - FLT 1532 - AFTER TAKEOFF AND LANDING GEAR RETRACTION, THE LEFT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED. T HE LANDING GEAR WAS CYCLED. THE GEAR INDICATED ALL THREE GREEN WITH THE LANDING GEAR EXTENDED, BUT BOTH MAIN LANDING GE ARS INDICATED UNSAFE UPON RETRACTION. THE AIRCRAFT CONTINUED TO ITS DESTINATION AND INDICATED LANDING GEAR SAFE ON GEAR EXTENSION. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE BROKEN LEFT MAIN GEAR ACTUATOR LOWER INNER LINK AND THE CHAFED LEFT MLG GEAR ACTUATOR. (M) 2 L 7 2 4F A6WE 2001121800105 20011218 00105 WP 2001 12 18 USAAD01185 1 20011204 A 2120 DUCT DOUG DC9 DC981 3022081 WP A/C BAY DISCONNECTED A USAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 826US 48026 PHL-RSW - FLT 415 - DURING CRUISE AT 35,000 FEET, THE CABIN ALTITUDE STARTED TO CLIMB A 300 TO 500 FT/MIN AND THE FLOW L IGHT ILLUMINATED. THE CABIN PRESSURE COULD NOT BE CONTROLLED IN MANUAL AND AN EMERGENCY DESCENT WAS INITIATED. CONTROL OF THE CABIN PRESSURE WAS REGAINED AT 20,000 FT. THE AIRCRAFT LANDED AT ITS DESTINATION WITHOUT INCIDENT. MAINTENANCE RECONNECTED THE RUBBER DUCT AT THE WATER SEPARATOR TEMP CONTROL VALVE. (M) 2 L 7 2 4F A6WE 2001121800106 20011218 00106 WP 2001 12 18 USAAD01186 1 20011206 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 827US 48049 IND - THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS, TAIL CONE EMERGENCY LIGHT RECEIVER, AFT OVERWING EMERGENCY EXIT LIGHT S AND CEILING LIGHTS AT SEAT ROWS 18 TO 21 WERE DIM. THE RIGHT AFT OVERWING IDENTIFIER LIGHT WAS INOPERATIVE. MAINTENA NCE REPLACED THE EMERGENCY LIGHT BATTERIES FOR THE DIM POSITIONS, AND THE RIGHT AFT OVERWING IDENTIFIER LIGHT ASSEMBLY. (M) 2 L 7 2 4F A6WE 2001121800107 20011218 00107 EU 2001 12 18 USAAF01085 1 20011122 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 890US 11365 IND - THE AFT SECTION OF THE FLOOR TRACK EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BA TTERY PACK. (M) 2 L 7 2 4F RT 2001121800108 20011218 00108 NM 2001 12 18 USAASB01313 1 20011116 A 3242 214747 BRAKE ASSY BOEING 737 7374B7 1384702 NM LT MLG HUNG UP A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 434US 26245 24556 LGA-FLT 1223 - AFTER LANDING AT LGA, ATC ADVISED THAT SMOKE WAS COMING FROM THE LT MLG. NO FIRE NOTED. A/C PULLED ONTO TAXIWAY, AND HAD THE GEAR INSP. NO PROBLEMS NOTED. A/C TAXIED TO THE GATE WITHOUT PROBLEMS. PIT - FLT 1908 - THE NEXT F LIGHT, CREW REPORTED A STRONG BRAKE AND RUBBER SMELL AFTER TAKEOFF. CREW LEFT GEAR DOWN AFTER DEPARTURE TO COOL DOWN A P OSSIBLE HOT BRAKE. UPON LANDING AT PIT, ATC REPORTED SMOKE COMING FROM THE BRAKE. AGAIN, NO FIRE WAS NOTED BUT FIRE EQUI PMENT WAS CALLED OUT. AIRCRAFT WAS CHECKED PRIOR TO BEING ALLOWED TO TAXI TO THE GATE. MAINTENANCE FOUND THE NR 1 BRAKE HANGING UP. REMOVED AND REPLACED THE NR 1 BRAKE ASSEMBLY. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001121800109 20011218 00109 NM 2001 12 18 AWXA200100644 1 20011213 A 5313 BAC1498156 STRINGER BOEING 737 7373G7 1384595 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - "C" - DURING C-15 CHECK MAINTENANCE FOUND CORROSION ON INSIDE OF STRINGER 25L AT BS 960. CORROSION WAS CLEANED AND VERIFIED OUT OF LIMITS WITH .032 MATERIAL LOST. REMOVED CORRODED SECTION OF STRINGER 25L FROM BS 947 TO BS 987, FABRICATED REPAIR PART AND INSTALLED IAW B737 SRM 53-00-03, PG 201-207, FIG 201. 2 L 7 2 4F RT A16WE 2001121800110 20011218 00110 NM 2001 12 18 AWXA200100645 1 20011213 A 5315 654654039 ANGLE BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - "C"- DURING C-15 CHECK MAINTENANCE FOUND CRACK ON VERTICAL SUPPORT ANGLE AT BS 639, BL 45 L/H. MAIN TENANCE REMOVED, FABRICATED, AND INSTALLED NEW SUPPORT ANGLE AT BS 637, BL 45 L/H, IAW DWG 65-46540 AND 737-300 SRM 51-4 0-02, PG 10-11. 2 L 7 2 4F RT A16WE 2001121800111 20011218 00111 NM 2001 12 18 AWXA200100647 1 20011214 A 5314 659187911 PANEL BOEING 737 7373G7 1384595 NM LOOSE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - "C" - DURING C-15 CHECK MAINTENANCE FOUND RIVETS AND CHERRY MAX FASTNERS LOOSE THAT SECURE KEEL BEA M PANEL BETWEEN WHEEL WELLS AT BS 663 TO BS 727, LBL 4 TO RBL 4, PANEL HAS TWO PREVIOUS REPAIRS. MAINTENANCE DRILLED OUT RIVETS AND REMOVED OLD PANEL, DRILLED TO FIT NEW PANEL AND INSTALLED IAW BOEING DWG 65-91879. 2 L 7 2 4F RT A16WE 2001121800112 20011218 00112 NE 2001 12 18 USAASB01318 2 20011120 A 7230 3350889510SET BLADE BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE NR 2 ENGINE DAMAGED A USAA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 EA 19 576US 8090 23741 721341 BUF - FLT 1563 - APPLIED T/O PWR, A SLIGHT NOISE AND VIBRATION WAS NOTED. ENG INDICATIONS WERE NORMAL WITH NO LIMITS EXC EEDED. SHORTLY AFTER BECOMING AIRBORNE, RT ENG VIBRATION METER WENT OFF SCALE. A LOUD ENG NOISE WAS HEARD ON THE FLT DEC K AND THE FLT ATTNS REPORTED A VIBRATION AT THE MID CABIN FLOOR AREA. PWR WAS REDUCED BUT RT ENG VIBRATION METER STAYED OFF SCALE TO THE RT. FLT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. CAPTAIN SHUT DOWN THE ENGINE. NO EMERGENCY DECLA RED. MX FOUND THE NR 2 ENG FIRST STAGE FAN BLADES TIGHT, NO SHINGLED. UNLOCKED FAN BLADES AND ACCOMPLISHED ENGINE POWER RUN. ALL VIBRATION PARAMETERS WERE NORMAL. A/C WAS RELEASED FOR MX FERRY FLT FOR FAN BLADE LUBE. MX ACCOMPLISHED FAN B 2 L 7 2 4F 4 F RT A16WE E2GL 2001121800113 20011218 00113 NM 2001 12 18 USAASB01320 1 20011121 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 507AU 23382 CLT - MAINTENANCE FOUND AN EMERGENCY LIGHT IN THE MID CABIN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY P ACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001121800114 20011218 00114 NM 2001 12 18 USAASB01323 1 20011122 A 2410 735511A CSD BOEING 737 7373B7 1384580 NM NR 2 ENGINE FAILED A USAA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 EA 19 504AU 38142 23379 STL - FLT 398 - APPROX 35 MIN OUT OF MCI, EN ROUTE TO PIT, THE NR 2 GENERATOR FAILED. FOLLOWED QRH PROCEDURES BUT THE GE NERATOR WOULD NOT RESET. THE APU WAS ALREADY ON MEL, CREW WAS REQUIRED TO LAND AT THE NEAREST AIRPORT. FLT DIVERTED AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MX SWAPPED GCU AND HAD CREW RUN THE ENGINE WITH NO HELP. GCU WERE S WAPPED BACK TO ORIGINAL POSITIONS. MX R&R THE NR 2 ENGINE CSD, GENERATOR (P/N 976J498-2) AND OIL COOLER (P/N UA538551-2) PER MM. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001121800115 20011218 00115 NM 2001 12 18 USAASB01324 1 20011123 A 3350 20131A BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 437US 24559 CLT - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT ROWS 6 THROUGH 9 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001121800116 20011218 00116 NM 2001 12 18 USAASB01325 1 20011124 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 428US 24550 CLE - MAINTENANCE FOUND THE AFT LEFT EXTERIOR OVERWING EMERGENCY LIGHT, THE RIGHT INTERIOR OVERWING CEILING EMERGENCY LI GHT, THE FORWARD SEAT EXIT AND LOW LEVEL EXIT SIGNS AND THE EMERGENCY EXIT LIGHT ON SEAT ROW 2 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE M1479 BATTERY PACK (P/N 2013-1A) AND CHARGER ASSEMBLY AND RECONNECTED PLUG AT SEAT ROW 2. OPS CHECK OF EMERGENCY LIGHT GOOD. (M) 2 L 7 2 4F RT A16WE 2001121800117 20011218 00117 NM 2001 12 18 USAASB01326 1 20011125 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 511AU 23594 GSO - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT OVER THE FORWARD SERVICE DOOR INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001121800118 20011218 00118 NM 2001 12 18 USAASB01327 1 20011125 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 384US 22957 CLT - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY EXIT LIGHT AND THE CENTER AISLE OVERHEAD EME RGENCY EXIT LIGHT AT THE OVERWING EXIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK A T THE CENTER AISLE OVERHEAD LOCATION AT EMERGENCY EXIT ROWS. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001121800119 20011218 00119 NM 2001 12 18 USAASB01329 1 20011127 A 3350 110049 CHARGER BOEING 737 7373B7 1384580 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 525AU 23860 TPA - MAINTENANCE FOUND THE FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND THE FORWARD EMERGENCY LIGHT B ATTERY CHARGER INOPERATIVE. REPLACED BATTERY CHARGER AND BATTERY PACK (P/N 2013-1A). OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001121800120 20011218 00120 NM 2001 12 18 USAASB01330 1 20011128 A 3350 20131A BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 584US 23743 TPA - MAINTENANCE FOUND THE FORWARD SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATT ERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001121800121 20011218 00121 NM 2001 12 18 USAASB01331 1 20011129 A 3350 20131A BATTERY PACK BOEING 737 737401 1384701 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 409US 23879 LGA - MAINTENANCE FOUND THE FORWARD OVERWING EMERGENCY EXIT LIGHT, LEFT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPL ACED THE BATTERY PACK AT STATION 598R. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001121800122 20011218 00122 NM 2001 12 18 USAASB01332 1 20011202 A 3350 SOCKET BOEING 737 7374B7 1384702 NM CABIN SHORTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 445US 24863 BUF - MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY PATH LIGHTING FROM SEAT ROWS 12 THROUGH 19 INOPERATIVE. MAINTENANCE FOUND TWO FUSES IN THE M1136 CHARGER ASSEMBLY BLOWN AND THE RIGHT OVERWING LIGHT SOCKET SHORTED. REPAIRED LIGHT SOCKET AND REPLACED FUSES (P/N 21031-0005). OPS CHECK OF EMERGENCY LIGHTS GOOD. (M) 2 L 7 2 4F RT A16WE 2001121800123 20011218 00123 NM 2001 12 18 USAASB01333 1 20011202 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 371US 22950 PIT - MAINTENANCE FOUND THE MID CABIN, CENTER OVERHEAD EMERGENCY EXIT LIGHT, INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2001121800124 20011218 00124 NM 2001 12 18 USAASB01334 1 20011203 A 3397 WIRE BOEING 737 7373B7 1384580 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 517AU 23703 EWR - MAINTENANCE FOUND THE EMERGENCY LIGHT AT SEAT ROW 17 INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE TO THE EMERG ENCY LIGHT AT SEAT ROW 17. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2001121900001 20011219 00001 SO 2001 12 19 C2XA01TY205 1 20011218 A 3350 1317 BULB EMB 145 EMB145ER 3260211 SO CABIN BLOWN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16927 145006 TYS During a scheduled inspection, The emergency light above seat 12A was found not working. Maintenance removed and re placed the light bulb, operational checkes good I.A.W.-EMB-145-MM-33-50-08, Aircraft will be released to service upon co mplection of inspection. 2 L 7 2 4F RT T00011AT 2001121900002 20011219 00002 NM 2001 12 19 SWAA013322 1 20011213 A 5330 6545802 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKEDAT BS 270, 16 INCHES ABOVE FLOOR LINE. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001121900003 20011219 00003 NM 2001 12 19 SWAA013324 1 20011213 A 5312 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 389SW 26592 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, WL 227 AND RBL 17.1. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001121900004 20011219 00004 NM 2001 12 19 SWAA013325 1 20011213 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, ABOVE STR 14L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001123100024 20011231 00024 WP 2001 12 31 ARWA20011209 1 20011216 A 3260 801814 SENSOR LKHEED 1011 1011385115 5265015 WP RT MLG FAILED A ARWA O OTHER O OTHER CL CLIMB 1 SO 19 308GB 193U1133 LANDING GEAR LEVER COULD NOT BE RAISED, HAD TO DEPRESS BUTTON TO RAISE SELECTOR. TROUBLESHOOT SYSTEM, REMOVED AND REPLA CED RT MLG AIR/GROUND SENSOR IAW MM 32-63-01, OPS CHECKED SYSTEM NORMAL IAW MM 32-63-0. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A23WE 2001121900005 20011219 00005 2001 12 19 SWAA013330 4 20011215 A 2565 D31591 SLIDE BOEING 737 7373Q8 1384670 NM FWD SVC DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED RON, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MM . 2 L 7 2 4F RT A16WE 2001121900006 20011219 00006 NM 2001 12 19 SWAA013333 1 20011216 A 3350 207377 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 365SW 26576 DURING SCHEDULED PM CHECK, FOUND EEPLS LENS MISSING AT ROW 12. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2001121900007 20011219 00007 EA 2001 12 19 COMA0160969 1 20011212 A 2710 601R5122623 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA INST PANEL STUCK A COMA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CL CLIMB 1 SO 01 810CA 7370 FLIGHT 5281 AILERON TRIM STICKING INTERMITTENTLY.REPLACED THE AILERON/RUDDER TRIM CONTROL PANEL. 2 L 7 2 4F RT A21EA 2001121900008 20011219 00008 NM 2001 12 19 C1HA200181019 1 20011129 A 3350 LIGHT BOEING 727 7272S7 138407Z NM COCKPIT INOPERATIVE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 681CA 22020 ON PREFLIGHT INSPECTION, FLIGHT DECK EMERGENCY EXIT LIGHT FAILED TO ILLUMINATE. REMOVED AND REPLACED FLT DECK EMERGENCY EXIT LIGHT PER M/M 33-50-91. OPS CHECK GOOD ON GROUND. 2 L 7 3 4F A3WE 2001121900009 20011219 00009 NM 2001 12 19 SWAA013339 1 20011217 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 328SW 23692 DURING WALKAROUND INSPECTION, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 500D, STRINGER 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001121900010 20011219 00010 NM 2001 12 19 SWAA013342 1 20011217 A 5315 6545410 BEAM BOEING 737 7373H4 1384600 NM CENTER WING BOX CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED 1/4D CHECK, FOUND BS 663 FLOORBEAM CRACKED, BBL 0. REPAIRED BEAM PER BOEING SB 737-57-1210 2 L 7 2 4F RT A16WE 2001121900011 20011219 00011 2001 12 19 SWAA013344 4 20011216 A 2565 65C19901 CABLE BOEING 737 7373H4 1384600 NM L2 DOOR FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 374SW 26582 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM. 2 L 7 2 4F RT A16WE 2001121900012 20011219 00012 NM 2001 12 19 SWAA013346 1 20011215 A 5311 6546546 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED D CHECK, FOUND 9 EA FUSELAGE FRAMES CRACKED, BS 747, BS 480, BS 767, BS 807, BS 827, BS 847,BS 867, BS 887, AND BS 907, BETWEEN STRINGERS 8L AND 9L. REPAIRED FRAMES PER ER 01-5457 AND SRM. 2 L 7 2 4F RT A16WE 2001121900013 20011219 00013 NM 2001 12 19 SWAA013347 1 20011215 A 5311 6546546 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED D CHECK, FOUND 5 EA FUSELAGE FRAMES CRACKED, BS 480, BS 807, BS 827, BS 867, AND BS 887, BETWEEN STRING ERS 8R AND 9R. REPAIRED FRAMES PER ER 01-5457 AND SRM. 2 L 7 2 4F RT A16WE 2001121900014 20011219 00014 NM 2001 12 19 SWAA013349 1 20011216 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED, BS 933 TO BS 935, STRINGER 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001121900015 20011219 00015 NM 2001 12 19 C1HA200185013 1 20011125 A 7711 JG298A5 INDICATOR BOEING 727 7272S7 138407Z NM COCKPIT FLUCTUATES A C1HA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 685CA 22492 WHILE EN ROUTE ENG NR 2 EPR FLUCTUATED BETWEEN 1.9 & 2.0 AND N1 FLUCT BETWEEN 84 & 86 PERCENT EGT 4750 AND N2 FLUCT ALSO PARAMETERS NOT NOTED. REMOVED AND REPLACED NR 2 EPR INDICATOR NR 2 N1 INDICATOR DRAINED AND CHECKED MOISTURE TRAP, ENG TRIM CK IAW ENG TRIM CHART NO FLUCTUATION NOTED. 2 L 7 3 4F A3WE 2001121900016 20011219 00016 SO 2001 12 19 C2XA01CL236 1 20011130 A 2621 336000575 FIRE BOTTLE EMB 145 EMB145ER 3260211 SO NR 1 ENGINE DEFECTIVE A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 27 14937 3876 133 145026 CLE FLIGHT 3157 THE CREW REPORTED A ENGINE 1 (2) EXTINGUISHER BOTTLE A INOP MESSAGE DURING FLIGHT. THE MESSAGE WENT OUT DURING DESCENT. MAINTENANCE REPLACED THE FIRE BOTTLE A. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2001121900017 20011219 00017 SO 2001 12 19 C2XA01CL241 1 20011209 A 2530 CBC16707 RECEPTACLE EMB 145 EMB145ER 3260211 SO GALLEY BURNED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 15941 145035 CLE FLIGHT 3169 THE CREW REPORTED A BURNING SMELL IN GALLEY. MAINTENANCE INSPECTED AND FOUND THE RIGHT COFFEE JUG RECEP TACLE TO BE BURNT. MAINTENANCE REPLACED THE LEFT AND RIGHT HOT JUG RECEPTACLES. OPERATIONAL CHECKS WERE GOOD. THE AIR CRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2001121900018 20011219 00018 SO 2001 12 19 C2XA01IA405 1 20011127 A 3260 12043270501 CONTROL BOX EMB 120 EMB120ER 3260203 SO COCKPIT FAULTY A C2XA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 SW 27 17728 120182 IAH- DURING TAXI THE CREW NOTED THAT THE LANDING GEAR LEFT GREEN A LIGHT ILLUMINATED WITH LOW POWER SETTING AND GEAR HA NDLE UP AND THE AIRCRAFT WAS RELEASED IAW MEL CONTROL NUMBER 017946. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR RELAY BOX, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001121900019 20011219 00019 SO 2001 12 19 C2XA01IA406 1 20011201 A 3350 MS354781683 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13997 3452 145298 IAH- DURING C-CHECK INSPECTION IT WAS NOTED THAT THE EMERGENCY LIGHT ABOVE SEAT 12BC FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED A ND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2001121900020 20011219 00020 EU 2001 12 19 C2XA01IA408 1 20011129 A 2612 CONNECTOR AEROSP ATR42 ATR42320 8680930 EU FIRE LOOP DIRTY A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 97841 280 DURING FLIGHT 3905, FROM LIT TO IAH, THE CREW NOTED THAT ENGINE NR 2 LOOP-B FAULTED IN FLIGHT. MAINTENANCE INSPECTED TH E ENGINE AND RELEASED THE AIRCRAFT IAW MEL. MAINTENANCE CLEANED CANNON PLUG 408BC, PERFORMED ENGINE RUNS AND TESTED FIR E LOOP SYSTEM ON NR 2 ENGINE, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001121900021 20011219 00021 SO 2001 12 19 C2XA01IA410 1 20011207 A 3260 922AAZYA6P2722 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO RT MLG OUT OF ADJ A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 51726 120174 LCH- DURING FLIGHT 3817, THE CREW NOTED THAT RIGHT MAIN GEAR, SYSTEM B-RED LIGHT FLASHES ON/OFF IN FLIGHT WITH GEAR UP. MAINTENANCE ADJUSTED THE UPLOCK PROX SENSOR ON THE RIGHT MAIN GEAR, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED AN D THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001121900023 20011219 00023 SO 2001 12 19 C2XA01IA413 1 20011209 A 4920 4501968D APU EMB 145 EMB145ER 3260211 SO APU BAY FAULTY A C2XA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 16944 145045 IAH- DURING FLIGHT NUMBER 3973 FROM PNS TO IAH, IN FLIGHT, THE APU WAS STARTED AND STRONG SMELL OF JET-A FUEL WAS NOTE D IN THE COCKPIT AND CABIN. DURING START, APU RPM REACHED 15 PERCENT, THEN 10 PERCENT, BEFORE STARTING UPWARD TO 103 PE RCENT. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL. MAINTENANCE REMOVED AND REPLACED THE APU, PERFORMED A OPERATIONAL CH ECK AND A LEAK CHECK, NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2001121900024 20011219 00024 SO 2001 12 19 C2XA01IA415 1 20011207 A 3260 WARNING LIGHT EMB 120 EMB120ER 3260203 SO COCKPIT FALSE INDICATION A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 51726 120174 DURING FLIGHT 3951 FROM MLU TO IAH THE CREW NOTED THAT THE RIGHT MAIN LANDING GEAR SYSTEM B-RED LIGHT ILLUMINATES IN FLI GHT. MAINTENANCE PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROV ED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2001121900025 20011219 00025 SO 2001 12 19 C2XA01TY191 1 20011211 A 2742 3622001011 ACTUATOR EMB 135 EMB135ER 3260203 SO HORIZ STAB FAILED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 3097 3097 145274 TYS DURING A SCHEDULED INSPECTION THE HORIZONTAL STABILIZER ACTUATOR FAILED A FUNCTIONAL CHECK. THE ACTUATOR INNER PIS TON HAS PLAY AND NONE WAS ALLOWED IAW CONTINENTAL EXPRESS TASK CARD 27-40-02-220-001-A00. MAINTENANCE REMOVED AND REPLA CED THE ACTUATOR IAW EMB-135 MM 27-40-02, ALL OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. THE AIRCRAFT WILL BE RELEA SED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001121900026 20011219 00026 SO 2001 12 19 C2XA01TY193 1 20011213 A 5320 14522459003 ANGLE EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 TYS DURING A SCHEDULED INSPECTION THE RAMP ANGLE ON THE CENTER OMEGA BEAM BETWEEN FRAMES 19 AND 20 WAS FOUND TO HAVE SE VERAL AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW EMB-135 SRM 51-40-02, THE REPAIR WAS SATI SFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001121900027 20011219 00027 SO 2001 12 19 C2XA01TY194 1 20011213 A 5315 14521700007 FLOORBEAM EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 TYS DURING A SCHEDULED INSPECTION THE LEFT HAND CENTER OMEGA BEAM AT FRAME 20 WAS FOUND TO HAVE SEVERAL AREAS OF CORROS ION. MAINTENANCE REMOVED THE CORRODED AREA AND ACCOMPLISHED A DOUBLER REPAIR IAW EMB-135 SRM 53-21-10, THE REPAIR WAS S ATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001121900028 20011219 00028 SO 2001 12 19 C2XA01TY195 1 20011213 A 5320 14522460013 FLOOR SUPPORT EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 TYS DURING A SCHEDULED INSPECTION THE TOP CAP ON THE CENTER OMEGA BEAM BETWEEN FRAMES 19 AND 23 WAS FOUND TO HAVE SEVER AL AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB-135 SRM 51-40-02, THE REPAIR WAS SATISFACTO RY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001121900029 20011219 00029 SO 2001 12 19 C2XA01TY196 1 20011213 A 5320 14522450015 GUSSET EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 TYS DURING A SCHEDULED INSPECTION THE SUBFLOOR GUSSET LOCATED JUST AFT OF THE COCKPIT ENTRANCE WAS FOUND TO HAVE SEVERA L AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE GUSSET IAW EMB-135 SRM 51-40-02, THE REPAIR WAS SATISFACTORY . THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001121900030 20011219 00030 SO 2001 12 19 C2XA01TY197 1 20011213 A 5315 14521721009 FLOORBEAM EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 TYS DURING A SCHEDULED INSPECTION THE FORWARD DIGITAL PLATE LOCATED BELOW THE FLOORING AND JUST AFT OF THE COCKPIT ENT RANCE WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE FORWARD DIGITAL IAW EMB-135 SR M 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001121900031 20011219 00031 NM 2001 12 19 VNAA0111013 1 20011130 A 2700 AILERON DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE JAMMED A VNAA O OTHER F FLT CONT AFFECTED CL CLIMB 1 GL 07 434JS 3051 AILERONS MOMENTARILY JAMMED IN FLIGHT. JERKED FREE AND CONTROLS REMAINED STIFF. FLIGHT 4064 RETURNEDTO PIT. MAINTENAN CE VISUALLY INSPECTED AILERON CONTROL CABLES AND PULLEYS IN ACCORDANCE WITH DORNIER MAINTENANCE JIC 27-11-03. NO DEFEC TS NOTED. PERFORMED FU NCTIONAL CHECK FLIGHT, FOUND TO BE SATISFACTORY AT THIS TIME. AIRCRAFT RELEASEDFOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001121900032 20011219 00032 SO 2001 12 19 C2XA01TY198 1 20011213 A 2730 14523597001 LIMITER EMB 135 EMB135ER 3260203 SO ELEVATOR GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 TYS DURING A SCHEDULED INSPECTION THE LEFT HAND ELEVATOR INBOARD LIMITER TUBE WAS FOUND TO BE GOUGED. MAINTENANCE ACCO MPLISHED THE BLEND-OUT REPAIR AND PERFORMED A DYE PENETRANT INSPECTION IAW EMBRAER GST-3934/01, THE REPAIR AND INSPECTIO N WERE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001121900033 20011219 00033 NM 2001 12 19 VNAA0112004 1 20011205 A 3200 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LH A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 432JS 3045 AT 100 FEET AGL THE CREW RETRACTED THE GEAR AND THE LEFT HAND GEAR INDICATION REMAINED IN TRANSIT. THE CREW CALLED MAIN TENANCE CONTROL AND STATED THAT WHEN EXTENDED THE INDICATIONS SHOW ALL DOWN. MAINTENANCE CONTROL HAD FLIGHT 9405 RETURN TO DAYTON WHERE MAINTENANCE ADJUSTED THE UPLOCK PROXI SENSOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. O PERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASEDFOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001121900034 20011219 00034 NM 2001 12 19 VNAA0112005 1 20011206 A 3200 2240500004 UPLOCK DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LH FAILED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 432JS 3 3045 UPON GEAR RETRACTION, THE CREW RECEIVED A LEFT HAND GEAR NOT LOCKED INDICATION RADIOED MAINTENANCE CONTROL AND RETURNED TO DAY. MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND UPLOCK ASSEMBLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONALCHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001121900035 20011219 00035 GL 2001 12 19 C2XA01TY199 2 20011214 A 7220 14575033007 INLET EMB 135 EMB135ER 3260203 SO ALLSN AE300 AE3007A GL RT ENGINE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND ENGINE AIR INLET WAS FOUND TO HAVE TWO NICKS ON THE ACOUSTIC PERFORAT ED INNER SKIN. MAINTENANCE REWORKED THE NICKS (BLEND-OUT) IAW EMB-135 SRM 54-20-01 AND EMBRAER GST 3879/01, THE REPAIR WAS FOUND TO BE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001121900036 20011219 00036 NM 2001 12 19 F3LA200100137 1 20011215 A 3210 69518383 COLLAR BOEING 737 7372L9 1384497 NM CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 3902 22733 DURING C-1 CHECK, INSPECTION REPORTED LT. MLG BELLCRANK RETAINING COLLAR CORRODED. REPLACED RETAINING COLLAR PER MM 32- 32-31. 2 L 7 2 4F RT A16WE 2001121900037 20011219 00037 SO 2001 12 19 C2XA01TY200 1 20011214 A 5320 14524243001 FLOOR SUPPORT EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 TYS DURING A SCHEDULED INSPECTION THE FLOOR SUPPORT ANGLES LOCATED BELOW THE THRESHOLD STRIP AT THE MAIN ENTRY DOOR WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR IAW EMB-135 SRM 51-20-03, 51-40- 02 AND CPM 51-21-04,05,06. THE REPAIR WAS FOUND TO BE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF I NSPECTION. 2 L 7 2 4F RT T00011AT 2001121900038 20011219 00038 SO 2001 12 19 C2XA01TY201 1 20011214 A 2520 PE290511 ATTACH FITTING EMB 135 EMB135ER 3260203 SO CABIN DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 TYS DURING A SCHEDULED INSPECTION THE LEFT HAND COCKPIT PARTITION WALL ATTACHMENT POINTS WERE FOUND TO BE DAMAGED. MA INTENANCE ACCOMPLISHED A BLEND-OUT REPAIR AND PERFORMED A DYE PENETRANT INSPECTION IAW EMBRAER GST 3877/01, EMB-135 CPM 51-21-04, 51-21-05 AND 51-21-06. THE REPAIR WAS FOUND TO BE SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2001121900039 20011219 00039 GL 2001 12 19 C2XA01TY203 2 20011215 A 7270 23062267 BYPASS JACKET EMB 135 EMB135ER 3260203 SO ALLSN AE300 AE3007A GL NR 1 ENGINE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 TYS DURING A SCHEDULE INSPECTION, BETWEEN THE FAN CASE AND THE OUTER BYPASS, OXIDATION WAS FOUND ON NR 1 ENGINE. MAINT ENANCE REMOVED THE OXIDATION, PERFORMED TOUCH UP OF PERMANENT RESIN COATING ON ACCESS, GEAR BOX MOUNTS, PLACED A CHEMICA L-FILM COATING FOR MAGNESIUM AND PAINTED WITH A CORROSION PAINT IAW AE3007EC7220-01009, AESPM70-32-03 AND AE3007ASMM70-0 0-00 WHICH WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001121900040 20011219 00040 SO 2001 12 19 C2XA01TY204 1 20011215 A 5330 14520557007 SKIN EMB 135 EMB135ER 3260203 SO FUSELAGE DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 TYS DURING A SCHEDULE INSPECTION THE FUSELAGE WAS DAMAGED BEHIND FRAME 31 BETWEEN STRINGER 12 AND 13R. REMOVED DAMAGED AREA. FABRICATED A DOUBLER, ALODINED AND INSTALLED, SEALED, PRIMED AND PAINTED IAW EMB 135 SRM 51-40-02 AND 51-22-01 AN D CPM 51-21-05. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL INSPECTIONS. 2 L 7 2 4F RT T00011AT 2001123100042 20011231 00042 NM 2001 12 31 F3LA200100138 1 20011215 A 5740 65827682 BUSHING BOEING 737 7372L9 1384497 NM RT WING CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 3902 22733 DURING C-1 CHECK, INSPECTION REPORTED ALL BUSHINGS CORRODED ON RT WING SWING LINK ASSY. REPLACED RT WING SWING LINK ASS Y PER BOEING DRAWING 65-82770 AND MM 57-15-0, STEP 5E. 2 L 7 2 4F RT A16WE 2001121900042 20011219 00042 NM 2001 12 19 C8GA20010019 1 20011204 A 7603 BOLT BOEING 727 727227 1384078 NM PWA JT8 JT8D17 52049 NE ENGINE CONTROL MISSING A C8GA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CL CLIMB 1 SO 15 89427 21365 688286 FLT 201 FROM MIA TO CCS. AFTER TAKEOFF NR 1 ENGINE STAYED AT FULL POWER AND WOULD NOT RESPOND TO THROTTLE MOVEMENT. AC COMPLISHED NR 1 ENGINE SHUTDOWN AND AIR TURNBACK TO MIA AND LANDED WITHOUT ANY INCIDENT. INVESTIGATION FOUND THE LOWER THRUST CRANK BOLT WAS MISSING IN NR 1 ENGINE. REINSTALLED BOLT AND COTTER PIN IAW MM 71-00 AND ENGINE RUN OPERATIONAL C HECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2001121900043 20011219 00043 NM 2001 12 19 CALA0101015 1 20011129 A 2530 72067002 FAN BOEING 737 737524 1384721 NM OVEN FAILED A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 14613 25326 27326 CREW REPORTED SMOKE IN CABIN AFTER TAKEOFF FROM IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. TROUBLESHOOTING BY MAINTENANCE FOUND THAT THE FIRST CLASS GALLEY NR 1 OVEN WAS ON AND THE EXHAUST FAN WAS NOT OPERATIN G. THE OVEN AND CONTROLLER WERE REMOVED AND REPLACED. BOTH PACK COALESCER BAGS WERE REPLACED. THE ENGINES WERE OPERAT ED AT TAKEOFF POWER AND A HEAT CYCLE WAS RUN WITH NO DEFECTS NOTED. 2 L 7 2 4F RT A16WE 2001121900044 20011219 00044 NM 2001 12 19 CALA0101021 1 20011204 A 3350 D71702001 POWER SUPPLY BOEING 767 767424ER 1385270 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 66051 29446 INSPECTION FOUND THE EXTERIOR EMERGENCY SLIDE ILLUMINATION LIGHT AT R-4 DOOR INOPERATIVE. THE M734 EMERGENCY LIGHTS POW ER SUPPLY WAS REMOVED AND REPLACED IAW MM 33-51-07, PAGE 201. 2 L 7 2 4F RT A1NM 2001121900045 20011219 00045 NM 2001 12 19 CALA0101024 1 20011208 A 2612 G718505 CONTROL PANEL BOEING 737 7373T0 1384582 NM COCKPIT FAULTY A CALA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 09 39343 2726 23581 A CARGO FIRE WARNING LIGHT ILLUMINATED AT FL 330 WHILE EN ROUTE FROM PHX TO IAH. BOTH FIRE BOTTLES WERE DISCHARGED IAW QRH PROCEDURES AND THE FLIGHT WAS DIVERTED TO AUS WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FI RE. TROUBLESHOOTING FOUND THE COCKPIT FIRE SUPPRESSION PANEL AT FAULT. THE PANEL WAS REMOVED AND REPLACED IAW MM 26-23 -10. IN ADDITION, BOTH FIRE BOTTLES WERE REMOVED AND REPLACED. SYSTEM FUNCTIONAL TESTS CHECKED GOOD IAW MM 26-23-10. 2 L 7 2 4F RT A16WE 2001121900046 20011219 00046 NM 2001 12 19 CALA0101029 1 20011214 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 63305 23356 INSPECTION FOUND A .5 INCH CRACK IN FLOOR SUPPORT AT STA 500-500A, L27R. REPAIRED IAW SRM 51-70-11. 2 L 7 2 4F RT A16WE 2001121900047 20011219 00047 2001 12 19 CHQ00065 4 20011211 A 3417 ADC EMB 145 EMB145 3260210 SO E/E BAY MALFUNCTIONED A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 286 145443 RUDDER 1 & 2 INOP LIGHT ON DURING T/O ROLL. RESET ADC 1 & 2 CIRCUIT BREAKERS N2 CIRCUIT BREAKERS, CYCLES RUDDER SYS 1 & 2 SWITCHES, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2001121900048 20011219 00048 SO 2001 12 19 CHQ00066 1 20011212 A 3412 PROBE EMB 145 EMB145 3260210 SO TAT SYSTEM FAILED A CHQA D RETURN TO BLOCK J WARNING INDICATION CR CRUISE 1 GL 11 285 145435 NR 1 TAT HEAT FAILED IN FLIGHT. REMOVED AND REPLACED NR 1 TAT PROBE FUNCTIONAL CHECK GOOD. 2 L 7 2 4F RT T00011AT 2001121900049 20011219 00049 SO 2001 12 19 CHQ00067 1 20011213 A 2612 FIRE LOOP EMB 145 EMB145 3260210 SO NR 1 ENGINE FAULTY A CHQA O OTHER N FALSE WARNING DE DESCENT 1 GL 11 267 145268 E1 FIRE DETECT FAIL EICAS MSG CAME ON INTERMITTENTLY DURING DESCENT. REPLACE ENGINE FIRE DETECTION LOOP AND RESET CONTR OL MOD, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2001121900050 20011219 00050 NE 2001 12 19 CHQ00068 2 20011213 A 7397 CONNECTOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RT ENGINE DIRTY A CHQA O OTHER J X WARNING INDICATION ENGINE FLAMEOUT CR CRUISE 1 GL 11 150 150 367488 ON TRAINING FLIGHT CREW REPORTED ACCOMPLISHED V1 CUT AND AT ADDITION OF TORQUE TO RT ENGINE FLAMED OUT IN FLIGHT. CLEAN ED CANNON PLUGS, GROUND RAN, TEST FLEW AND COULD NOT DUPLICATE THE PROBLEM. 2 L 7 2 4T 4 T RT A52EU E8NE6 2001121900051 20011219 00051 SO 2001 12 19 CHQ00069 1 20011214 A 2611 SMOKE DETECTOR EMB 145 EMB145 3260210 SO LAVATORY ACTIVATED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 277 145355 RTF FOR LAV SMOKE DETECTION WARNING ON RETURN MADE OVERWEIGHT LANDING. COMPLIED WITH HEAVY LANDING INSPECTION AND TROUB LESHOT THE LAV SMOKE DETECTION SYSTEM. 2 L 7 2 4F RT T00011AT 2001121900052 20011219 00052 NE 2001 12 19 CHQ00071 2 20011214 A 7260 CHIP DETECTOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE FALSE INDICATION A CHQA K NONE N FALSE WARNING AP APPROACH 1 GL 11 158CQ 158 LEFT ENGINE CHIP DETECTOR LIGHT CAME ON DURING APPROACH. FOUND NO METALLIC PARTICLES ON CHIP DETECTOR. CLEANED CHIP DE TECTOR, GROUND RAN A/C 15 MIN, OPS CHECK GOOD IAW GE AMM 72-00-00. NO LEAKS NOTED. 2 L 7 2 4T 4 T RT A52EU E8NE6 2001121900053 20011219 00053 SO 2001 12 19 CHQ00073 1 20011215 A 2612 FIRE WARNING EMB 145 EMB145 3260210 SO COCKPIT INTERMITTENT A CHQA K NONE N FALSE WARNING LD LANDING 1 GL 11 267 145268 ENGINE NR 1 FIRE DETECT FAIL MASTER CAUTION EICAS MESSAGE INTERMITTENTLY, OPS CHECK OF FIRE DETECTION SYSTEM OPS CHECK G OOD. 2 L 7 2 4F RT T00011AT 2001121900054 20011219 00054 EU 2001 12 19 DHL2001365501 1 20011118 A 5730 SKIN AIRBUS 300 A300B4203 3930306 EU RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH 149 CORROSION FOUND ON REAR LOWER SKIN PANEL RT WING AT NR 3 FLAP TRACK POSITION. FABRICATED SKIN PER DWG 03173301 FIG 1. INSTALLED REPAIR. 2 L 7 2 4F RT A35EU 2001121900055 20011219 00055 EU 2001 12 19 DHL2001365537 1 20011125 A 5320 FITTING AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH 149 CORROSION ON SILL BEAM-ROLLER TRACK CONNECTING WEB AT FR 60. REMOVED CORROSION PER SRM 51-40-11. DEPTH OF CORROSION RE MOVED 0.030, OUTSIDE LIMITS. REMOVED SILL ROLLER TRACK AND CORRODED FITTING PER SRM 51-30-30 AND TORSION BOX COVER AND TORSION BOX PER SRM 51-30-30. REPLACED TORSION BOX PLATE PER SRM 51-30-30. REFIT SILL BEAM ROLLER TRACK PER M/M 51-30- 30. 2 L 7 2 4F RT A35EU 2001121900056 20011219 00056 EU 2001 12 19 DHL2001365539 1 20011130 A 5313 STRINGER AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH 149 CORROSION ON STR 36L-46L AT FRAME 72. REMOVED CORROSION PER SRM 51-40-11 (NEGLIGIBLE MTL REMOVED). CUT OUT 2 FT SECTIO N AND REPLACED PER SRM 53-10-10. 2 L 7 2 4F RT A35EU 2001121900057 20011219 00057 EU 2001 12 19 DHL2001365544 1 20011129 A 5330 SKIN AIRBUS 300 A300B4203 3930306 EU FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH 149 2 DENTS IN SKIN, ONE 4 IN AFT OF FR 29 AT STR 33R AND THE OTHER AT FR 29 BETWEEN STR 32-33R, OUT SIDE OF SRM 53-10-00 FI G 609 ASSESSMENT LIMIT. CUT OUT DENTS IN SKIN AS PER FSI INSTRUCTION REF BAE-FTN 01-0083 ITEM 1. FABRICATED DOUBLER AN D SPACERS PER EO REF ITEM 3. REPLACED DAMAGED SECTION OF STRINGER PER FSI INSTRUCTION BAE-FTN 01-0083. INSTALLED DOUBL ER PER EO ITEM 6. SEALED REPAIR PER SRM 51-40-20. 2 L 7 2 4F RT A35EU 2001121900058 20011219 00058 EU 2001 12 19 DHL2001365545 1 20011130 A 5330 SKIN AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH 149 DURING REPLACMENT OF FWD CARGO DOOR LOWER AFT CORNER SECTION, DOOR SEAL WAS REMOVED FOR ACCESS AND CORROSION WAS OBSERVE D ON LOWER LONGERON AND SKIN. LOWER LONGERON AND INNER SKIN PLATE REPAIRED PER SRM 51-30-30. 2 L 7 2 4F RT A35EU 2001121900059 20011219 00059 NM 2001 12 19 DHL2001705007 1 20011204 A 3350 LIGHT BOEING 727 72722C 138400F NM COCKPIT OUT OF POSITION A DHLA O OTHER O OTHER CR CRUISE 1 SO 01 705DH 19191 EMERGENCY EXIT LIGHT IN COCKPIT FELL OFF. REINSTALLED EMERGENCY EXIT LIGHT ASSY. OPS CHECK GOOD IAW MM 33-50-01. 2 L 7 3 4F A3WE 2001121900060 20011219 00060 NM 2001 12 19 DHL2001707014 1 20011214 A 3040 WINDSHIELD WIPER BOEING 727 72722 1384002 NM WINDSHIELD OUT OF ADJ A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 707DH 18321 RANGE OF MOTION ON WINDSHIELD WIPERS, BOTH CAPT AND F/O ARE INADEQUATE FOR NORMAL FIELD OF VISION (DO NOT COME UP HIGH E NOUGH). WINDSHIELD WIPERS NEED REPLACING (BLADES). TESTED AND ADJUSTED NR 1 AND NR 2 WIPER ASSB IAW 727 MM CHP 30-42. GROUND CKS NORMAL AT THIS TIME. REMOVED AND REPLACED WIPER BLADES IAW 727 MM CH 30-42. 2 L 7 3 4F A3WE 2001121900061 20011219 00061 2001 12 19 DHL2001707015 4 20011214 A 2210 AUTOPILOT SYS BOEING 727 72722 1384002 NM COCKPIT MALFUNCTIONED A DHLA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 01 707DH 18321 WHILE ON FINAL APPROACH COURSE WITH BOTH LOCALIZERS AND GLIDESLOPE INITIALLY CAPTURED ON AUTOPILOT, THE AUTOPILOT WAS NO T CAPABLE OF FLYING THE GLIDESLOPE. AIRCRAFT DOVE FOR THE GROUND. PERFORMED OPERATIONAL CHECK OF AUTOPILOT SYSTEM IAW 727 MM CH 22-00 AND SELF TEST OF PITCH COMPUTER IAW 727 MM CH 22-00 PG 511. NO FAULTS FOUND. 2 L 7 3 4F A3WE 2001121900062 20011219 00062 NM 2001 12 19 SWAA013315 1 20011212 A 5754 6546422 SLAT BOEING 737 7372H4 138448C NM RT WING DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 087SW 22903 ON WALKAROUND, FOUND DAMAGE TO TOP SIDE OF NR 5 L/E SLAT AND SKIN UNDER NR 5 SLAT PEELED BACK. REMOVED AND REPLACED L/E SLAT AND REPAIRED L/E SKIN PER SRM. 2 L 7 2 4F A16WE 2001121900063 20011219 00063 2001 12 19 SWAA013321 4 20011212 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2001121900064 20011219 00064 NM 2001 12 19 SWAA013326 1 20011213 A 2751 1812996 INDICATOR BOEING 737 7373Y0 1384671 NM COCKPIT FAILED A SWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 07 682SW 23496 AIR TURNBACK, AFTER T/O TRAILING EDGE FLAPS WOULD NOT RETRACT BEYOND ABOUT 2 DEG. FLAPS WERE LOWERED USING ALT FLAPS. REMOVED AND REPLACED TRAILING EDGE FLAP POSITION INDICATOR PER MM. 2 L 7 2 4F RT A16WE 2001121900065 20011219 00065 NE 2001 12 19 SWAA013328 2 20011212 A 7321 8063208 MEC BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 2 ENGINE FAULTY A SWAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 07 373SW 26581 AIR TURNBACK, DECLARED EMERGENCY, NR 2 ENGINE UNWOUND FROM TAKEOFF THRUST TO IDLE RPM WITH NO THRUST LEVER MOVEMENT. RE MOVED AND REPLACED MEC AND FUEL PUMP PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2001121900066 20011219 00066 2001 12 19 SWAA013329 4 20011214 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 793SA 27888 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001121900067 20011219 00067 NM 2001 12 19 SWAA013331 1 20011215 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN ILLUMINATED A SWAA K NONE O OTHER AP APPROACH 1 SW 07 789SW 29816 RT OVERWING EMERGENCY EXIT LIGHT ILLUMINATED JUST PRIOR TO LANDING. CYCLED POWER FROM APU TO GROUND, LIGHT WENT OUT PER MM. 2 L 7 2 4F RT A16WE 2001121900068 20011219 00068 NM 2001 12 19 SWAA013332 1 20011216 A 3350 BR2013 LIGHT BOEING 737 7372T4 1384492 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 EEPLS LOOSE AT ROW 2. SECURED EEPLS PER MM. 2 L 7 2 4F A16WE 2001121900069 20011219 00069 2001 12 19 SWAA013334 4 20011213 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 650SW 27720 AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001121900070 20011219 00070 NM 2001 12 19 SWAA013335 1 20011214 A 2560 P4010021 FLASHLIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 104SW 23110 EMERGENCY FLASHLIGHT INOP AFT CABIN TOP UNIT. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F A16WE 2001121900071 20011219 00071 NM 2001 12 19 P5CA0100618 1 20011215 A 3231 10605451435 BEARING BOEING 747 747249F 1384849 NM L/BODY GEAR WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 L/BODY GEAR STRUT DOOR LINK ROD ATTACH FITING BEARING WORN. REMOVED & REPLACED FITTING/BEARING PER MM 32-14-06. 2 L 7 4 4F A20WE 2001121900072 20011219 00072 NM 2001 12 19 P5CA0100619 1 20011215 A 5415 NONE DOUBLER BOEING 747 747249F 1384849 NM TORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 #2 PYLON INBD SIDE, AFT END, ABOVE AFT MOUNT, HAS A 1" RIP IN DOUBLER. REPAIRED PER SRM 54-12-01 & SRM 51-40-00. 2 L 7 4 4F A20WE 2001121900073 20011219 00073 NM 2001 12 19 P5CA0100622 1 20011217 A 7932 691718 SEAL BOEING 747 747249F 1384849 NM #4 ENGINE LEAKING A P5CA E D ENGINE SHUTDOWN RETURN TO BLOCK J K WARNING INDICATION FLUID LOSS CR CRUISE 1 WP 23 920FT 22237 AT APPROX. 15 MIN. INTO CRUISE (FL 33.0), #4 OIL QTY RAPIDLY DROPPED TO ZERO. FWD CAUTION PANEL LOW OIL PRESSURE LIGHT C AME ON. PRECAUTIONARY ENG SHUTDOWN ACCOMPLISHED PER ABNORMAL PROCEDURES. UPON INSPECTION FOUND GEARBOX N2 FULL OF OIL W / TANK EMPTY.REPAIRED BY CHANGING PUMP, OIL TANK, CDS & STARTER SEALS. CHANGED PRESSURE RELIEF VALVE AS A PRECAUTION. N IL LEAKS ON RUN UP. OIL QTY MAINTAINED W/ NO EVIDENCE OF LOSS. A/C RELEASED TO SERVICE. 2 L 7 4 4F A20WE 2001121900074 20011219 00074 2001 12 19 SWAA013336 4 20011209 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 621SW 28037 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2001121900075 20011219 00075 WP 2001 12 19 IXXA0100077O 1 20011214 A 2700 CABLE DOUG DC8 DC871F 302199D WP WING BROKEN A IXXA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SW 11 825BX 82406 2304 45978 ENROUTE FROM ANC TO SEA, AFTER TAKEOFF THE FLIGHT CREW NOTICED A SIGNIFICANT AIRCRAFT ROLL TO THE LEFT AND REQIURED RUDD UR INPUT. THE FLIGHT RETURNED TO ANC FOR AN UNVENTFUL LANDING. MANITHEANCE INSPECTED THE AIRCRAFT WHICH REVEALED A SEGME NT OF THE LEFT WING FLIGHT SPOILER RETRACT CABLE BROKEN. MAINTENANCE REPLACED THE CABLE IN ACCORDANCE WITH THE MAINTENCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2001121900076 20011219 00076 NE 2001 12 19 COMA0110163 2 20011217 A 7321 789841500826 EEC EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE L/H MALFUNCTIONED A COMA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 SO 01 259CA 13463 120252 FLIGHT 5061 - LEFT ENGINE WILL NOT ACHIEVE REQUIRED TORQUE.REPLACED THE L/H ENGINE EEC. 2 L 7 2 4T 4 T RT A31SO E20NE 2001121900077 20011219 00077 EA 2001 12 19 COMA0160973 1 20011217 A 3350 6464 POWER SUPPLY CNDAIR CL600 CL6002B19 1900309 EA CABIN FLOOR MISINSTALLED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 914CA 7012 FLIGHT 5999 EMERGENCY FLOOR PATH LIGHTS ARE INOP FORWARD OF ROW 5.FOUND POWER STRIPS INSTALLED WRONG. REINSTALLED POWER STRIPS I/A/W M/M. 2 L 7 2 4F RT A21EA 2001121900078 20011219 00078 EA 2001 12 19 COMA0160972 1 20011217 A 3220 PROXIMITY SWITCH CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 975CA 7150 FLIGHT 5970 - CONFIG OK MESSAGE WENT OUT DURING T/O.REMOVED DIRT FROM NLG PROX SWITCHES. 2 L 7 2 4F RT A21EA 2001121900079 20011219 00079 EA 2001 12 19 COMA0160971 1 20011217 A 3040 2315M1082 BLADE CNDAIR CL600 CL6002B19 1900309 EA R/H BROKEN A COMA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 SO 01 971CA 7145 FLIGHT 5109 - COPILOTS WINDSHIELD WIPER IS BROKEN AND IS HITTING THE AIRCRAFT.INSTALLED A SERVICEABLE WIPER BLADE. 2 L 7 2 4F RT A21EA 2001121900080 20011219 00080 EA 2001 12 19 COMA0160970 1 20011218 A 5500 600210615 BUSHING CNDAIR CL600 CL6002B19 1900309 EA VERTICAL STAB SCORED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 810CA 3923 7370 THE VERTICTAL STABILIZER HINGE BUSHINGS DAMAGED AND REQUIRE REPLACEMENT.REMOVED AND REPLACED VERTICAL STABILIZER HINGE B USHING I/A/W WVAC EO 601R-55-2892. 2 L 7 2 4F RT A21EA 2001121900087 20011219 00087 CE 2001 12 19 BSY2001F00016 1 20011109 A 7603 63255535 THROTTLE ARM BEECH 58 58 1152740 CE CONT O520 IO520C 17032 SO RT ENGINE FAILED E BSYA E ENGINE SHUTDOWN O OTHER AP APPROACH 1 GL 07 2064V TH1004 840935R RT ENGINE STAYED AT 2100 RPM ON APPROACH, SHUT ENGINE DOWN. INSTALLED NEW CONTROL LEVER ARM TO SHAFT THROTTLE ASSEMBLY OPS CHECKS GOOD. 1 L 7 2 3O 3 O 3A16 E5CE 2001121900088 20011219 00088 SO 2001 12 19 BSY2001F00017 1 20011109 A 3260 WIRE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA DOWNLOCK SWITCH BROKEN E BSYA O OTHER N FALSE WARNING AP APPROACH 1 GL 07 22427 318152065 147168A (AGC)(MIR) NO LEFT GEAR DOWN AND LOCK INDICATION. FOUND BROKEN WIRE ON LEFT DOWN LOCK SWITCH. REPAIRED WIRE, OPS CHECK S GOOD. 1 L 7 2 3O 3 O A20SO E14EA 2001121900089 20011219 00089 CE 2001 12 19 BSY2001F00018 1 20011109 A 3260 1EN18 DOWNLOCK SWITCH LEAR 35 35LEAR 5170600 CE GARRTT TFE731 TFE73122B 01518 WP LT MLG FAILED E BSYA O OTHER N FALSE WARNING AP APPROACH 1 GL 07 959SA 076 P74230 (ALT)(MIR) GOING INTO ATL, HAD NO LEFT GEAR DOWN AND LOCK LIGHT. FERRIED AIRCRAFT TO (PDK) FOR MAINTENANCE. REMOVED AN D REPLACED LEFT GEAR DOWN AND LOCK SWITCH OPS CHECKS GOOD. 2 L 7 2 4F 4 F A10CE E6WE 2001121900090 20011219 00090 CE 2001 12 19 BSY2001F00019 1 20011207 A 2437 99100943 SENSOR CESSNA 310 310R 2074245 CE CONT O520 IO520* 17032 SO ALTENATOR SYS FAILED E BSYA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 07 5238J 310R0810 811581R (MKE)(MIR) LOST BOTH ALTERNATORS, THEN, RIGHT SIDE CAME BACK ON. REMOVED AND REPLACED BOTH ALTERNATOR OUT SENSORS. OPS CHECKS GOOD. 1 L 7 2 3O 3 O 3A10 E5CE 2001121900091 20011219 00091 CE 2001 12 19 BSY2001F00020 1 20011207 A 3260 1EN18 DOWNLOCK SWITCH LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP NLG FAILED E BSYA O OTHER N FALSE WARNING AP APPROACH 1 GL 07 51LC 302 P74751LT (CMH)(MIR) HAD NO NOSE GEAR DOWN LIGHT. REMOVED AND REPLACED DOWN AND LOCK SWITCH. OPS CHECKS GOOD. 2 L 7 2 4F 4 F A10CE E6WE 2001121900092 20011219 00092 NM 2001 12 19 BSY2001F00021 1 20010207 A 3231 DOOR PIPER PA60 PA60600 7106001 NM LYC O540 IO540K1J5 41532 EA NLG MALFUNCTIONED E BSYA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 6076L 600713796122 L1841548A (BWI)(MIR) AFTER TAKE OFF HAD NO GEAR UP LIGHT, RETURNED TO BWI, FOUND NOSE GEAR DOORS HOLDING GEAR FROM GOING ALL THE W AY UP IN WHEEL WELL. REPAIRED DOORS. OPS CHECKS GOOD. 1 M 7 2 3O 3 O RT A17WE 1E4 2001121900093 20011219 00093 SO 2001 12 19 BSY2001F00022 2 20011207 A 7414 106006061 MAGNETO CESSNA 310 310R 2074245 CE CONT O520 IO520C 17032 SO RT ENGINE FAILED E BSYA O OTHER Y ENGINE STOPPAGE CL CLIMB 1 GL 07 6160X 310R1305 277585R (OMA)(MIR) RIGHT ENGINE ON CLIMB OUT, SURGED, THEN SHUT DOWN. FOUND LEFT MAGNETO ON RIGHT ENGINE INOPERATIVE. REMOVED AND REPLACED MAG OPS CHECKS GOOD. 1 L 7 2 3O 3 O 3A10 E5CE 2001121900094 20011219 00094 CE 2001 12 19 BSY2001F00023 1 20011207 A 7602 COTTER PIN BEECH 58 58 1152740 CE CONT O520 IO520C 17032 SO RT ENGINE SHEARED E BSYA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 GL 07 9189Q TH148 823785R (CLT)(MIR) RIGHT ENGINE SHUT DOWN IN FLIGHT. COTTER PIN SHEARED NUT BACKED OFF MIXTURE CABLE CAUSING MIXTURE TOO LEAN. REPLACED BOLT, NUT AND COTTER PIN. OPS CHECKED OK. 1 L 7 2 3O 3 O 3A16 E5CE 2001121900095 20011219 00095 SO 2001 12 19 BTV2001F00003 1 20011203 A 3610 18368041 COOLER GULSTM G1159 G1159 3953505 SO RROYCE SPEY SPEY5118 54523 EU BLEED AIR FAILED B BTVR K NONE O OTHER IN INSP/MAINT 1 GL 23 55RG 8117 1 DURING A HIGH POWER GROUND MAINTENANCE RUN-UP, THE MECHANIC IN THE COCKPIT OBSERVED THAT THE BLEED AIR PRESSURE SUDDENLY DROPPED TO NEAR ZERO, FROM 40 AND PSI. INVESTIGATION REVEALED THE LEFT HP AIR PRECOOLER HAD FAILED (BLOWN), EFFECTIVEL Y OPENING THE BLEED AIR MANIFOLD, NO OTHER DAMAGE WAS DONE. EXTREME AGE OF THE PART IS THE MOST LIKELY CAUSE. 2 L 7 2 4F 4 F RT A12EA E2EU 2001121900096 20011219 00096 SO 2001 12 19 BTV2001F00004 1 20011204 A 3213 1159SCL5010211 BEARING BFGOODRICH GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE STRUT CRACKED B BTVR K NONE O OTHER IN INSP/MAINT 1 GL 23 502KA 2779 CPT0002NTW 502 DURING A ROUTINE, SCHEDULED LANDING GEAR INSPECTION, THE MECHANIC NOTED WHAT APPEARED TO BE A CRACK ON THE LOWER MOUNT B ALL OF THE RIGHT HAND SHOCK ABSORBER. UPON REMOVAL OF THE SHOCK ABSORBER, VISUAL INSPECTION CONFIRMED THAT THE SPHERICA L BALL PORTION OF THE SWAGED BEARING ASSEMBLY WAS CRACKED THROUGH. THE DEFECTIVE COMPONENT WAS SENT TO MFG. CORPORATION FOR REPAIR AND EVALUATION. NO CAUSE IS KNOWN AT THIS TIME. 2 L 7 2 4F 4 F RT A12EA E00057EN 2001121900097 20011219 00097 CE 2001 12 19 IRG2001F00000 1 20010515 A 2721 2398006801 RELAY LEAR 35 35A 5170602 CE COCKPIT FAILED A IRGA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 14 500HZ 11050 238 RUDDER TRIM INOPERATIVE. IN FLIGHT, REPLACED FAULTY RELAY(K1) IN E504 TRIM RELAY PANEL. OPPS CHECK GOOD. 2 L 7 2 4F A10CE 2001121900098 20011219 00098 CE 2001 12 19 IRG2001F00001 1 20010922 A 2710 501113303 COMPUTER LEAR 35 35A 5170602 CE SPOILERON FAULTY A IRGA K NONE O OTHER IN INSP/MAINT 1 SO 14 500HZ 11215 4659 238 SPOILERON CAU LIGHT. LIGHT COMES ON DURING TEST AND WILL NOT RESET. REPLACED FAULTY SPOILERON COMPUTER AND ADJUSTED FO LLOW-UP ON RIGHT SPOILER. 2 L 7 2 4F A10CE 2001121900099 20011219 00099 NM 2001 12 19 NUZ2001F00000 1 20011120 A 2620 6546858302 TUBE BOEING 737 7374Q8 138447Q NM WING OUT OF POSITION B NUZY K NONE O OTHER IN INSP/MAINT 1 EA 35 234AN 24234 ON INSPECTION OF AREA AROUND NR 6 FLAP TRANSMISSION, A FIRE EXTINGUISHING TUBE WAS FOUND CHAFED THROUGH IN SEVERAL PLACE S, CAUSED BY INBOARD FORE FLAP OUTBOARD CARRIAGE. IT APPEARS THAT TUBE IS WRONGLY POSITIONED. 2 L 7 2 4F RT A16WE 2001121900100 20011219 00100 EU 2001 12 19 S9H2001F00000 1 20011207 A 2910 704A33690004 BELT SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE HYDRAULIC SYS BROKEN E S9HA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 19 360NT 236 2695 4474 PILOT EXPERIENCED HYDRAULIC FAILURE WHEN HYDRAULIC BELT BROKE AFTER CONTACT WITH A BROKEN AIR CONDITION COMPRESSOR BELT. PILOT MADE A CAUTIONARY LANDING WITH NO INCIDENTS AT AIRSTRIP. NEW HYDRAULIC BELT WAS INSTALLED AND AIRCRAFT RETURNED TO BASE WITHOUT FURTHER INCIDENTS. 1 G 7 1 3U 3 U NC H9EU E19EU 2001121900101 20011219 00101 NM 2001 12 19 AALA20011498 1 20010725 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 657AM 24615 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIGNS AT MAIN ENTRY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGNS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001121900102 20011219 00102 NM 2001 12 19 AALA20011803 1 20010920 A 3397 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 686AA 25343 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 3E INOPERATIVE. SECURED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 3E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001121900103 20011219 00103 NM 2001 12 19 AALA20011804 1 20010920 A 3397 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 686AA 25343 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 5E INOPERATIVE. SECURED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001121900104 20011219 00104 NM 2001 12 19 AALA20011829 1 20010928 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 645AA 24603 DFW - DURING OVERNIGHT MAINTENANCE, RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GR OUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001121900105 20011219 00105 NM 2001 12 19 AALA20011836 1 20011001 A 3397 CONNECTOR BOEING 757 757223 1384957 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 647AM 24605 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 20D INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT CON NECTOR AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001121900106 20011219 00106 NM 2001 12 19 AALA20011854 1 20011010 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 612AA 24488 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT STRIP. SYSTEM GROU ND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001121900107 20011219 00107 NM 2001 12 19 AALA20011857 1 20010909 A 3397 CONNECTOR BOEING 757 757223 1384957 NM CABIN NOT SEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 640A 24598 ORD - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT 22D INOPERATIVE. RE-SEATED EMERGENCY EXIT LIGH T CONNECTOR AT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001121900108 20011219 00108 NM 2001 12 19 AALA20011858 1 20011009 A 3350 P2010031302 LIGHT BOEING 757 757223 1384957 NM GALLEY INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 638AA 24596 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEM BLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001121900109 20011219 00109 NM 2001 12 19 AALA20011899 1 20011012 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 616AA 24524 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEATS 1 THROUGH 17 INOPERATIVE. REPLACED EMERGENCY EXIT LIG HT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001121900110 20011219 00110 NM 2001 12 19 AALA20011940 1 20011018 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 612AA 24488 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STRIP. SYSTEM GROU ND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001121900111 20011219 00111 NM 2001 12 19 AALA20011943 1 20011022 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 670AA 25335 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 17D INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT WIR E AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001121900112 20011219 00112 NM 2001 12 19 AALA20011965 1 20011029 A 3350 SOCKET BOEING 767 767323 1385205 NM CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 397AN 29604 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT LAMP SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001121900113 20011219 00113 WP 2001 12 19 AALA20011968 1 20011020 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 221AA 49172 TUL - FOUND 15-18 INCH HOLE THROUGH FUSELAGE SKIN ABOVE FORWARD STRAKE ON LEFT SIDE OF AC. REPAIRED FUSELAGE DAMAGE PER SRM 53-04 FIG 1213 SHT 1. (M) 2 L 7 2 4F A6WE 2001121900114 20011219 00114 NM 2001 12 19 AALA20011972 1 20011101 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 359AA 24040 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001121900115 20011219 00115 NM 2001 12 19 AALA20011973 1 20011031 A 3397 CONNECTOR BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 795AN 30257 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 34 INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT CONNECTOR . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001121900116 20011219 00116 NM 2001 12 19 AALA20011976 1 20011103 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 359AA 24040 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT WIRE BROKEN. REPAIRED EMERGENCY EXIT LIGHT WIRE AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001121900117 20011219 00117 NM 2001 12 19 AALA20011977 1 20011102 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39367 25194 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 26H AND 32H INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT 26H AND 32H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001121900118 20011219 00118 WP 2001 12 19 AALA20011979 1 20011103 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 424AA 49336 TUL - FOUND FUSELAGE SKIN CRACKED FROM FASTENER HOLE STATION 1380, 19 INCHES ABOVE ENGINE, LEFT ENGINE PYLON. STOP DRIL LED CRACK AND INSTALLED DOUBLER PER SRM 53-01 FIG 2 (SHEET 3). (M) 2 L 7 2 4F A6WE 2001121900119 20011219 00119 WP 2001 12 19 AALA20012012 1 20011026 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 59523 49915 TUL - FOUND FLOORBOARD SUPPORT ANGLE CORRODED AT STATION 200 LBL 6. INSTALLED NEW FLOOR SUPPORT HAT CHANNEL AT STATION 200 LBL 6 PER SRM 51-00-00 AND 51-30. (M) 2 L 7 2 4F A6WE 2001121900120 20011219 00120 WP 2001 12 19 AALA20012013 1 20011026 A 5310 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 59523 49915 TUL - FOUND CRACK NEAR 1ST FASTENER .25 INCH LONG IN ANGLE OF WINDOW CUT OUT INTERNAL DOUBLER AT STATION 1137 AND LONGER ON 14R. STOP DRILLED CRACK AND INSTALLED DOUBLER PER AARD 53-10-00-25. (M) 2 L 7 2 4F A6WE 2001121900122 20011219 00122 NM 2001 12 19 F3LA200100 1 20011130 A 2120 ODOR BOEING 737 7372L9 1384497 NM CABIN DETECTED A F3LA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 03 271FL 22734 UPON DEPARTURE FROM ABQ, FLIGHT CREW REPORTED A STRONG PULL TO THE RIGHT JUST AFTER TAKEOFF THRUST WAS SET. FULL LEFT R UDDER WITH A LITTLE TILLER STRAIGHTENED THE AIRCRAFT OUT. CONTINUED TAKEOFF ROLL WHICH APPEARED NORMAL. AT GEAR RETRAC TION, A STRONG BURNING RUBBER WAS SMELLED. CONTINUED TO ELP TO BURN FUEL. DECLARED AN EMERGENCY AND LANDED WITHOUT INC IDENT. MAINTENANCE INSPECTED LT AND RT LANDING GEAR, LT AND RT WINGS AND FLIGHT CONTROLS, TAXIED AIRCRAFT AND RAN BOTH ENGINES TO TAKEOFF POWER. RAN LT AND RT AIR CONDITIONING PACKS. ALL OPERATIONAL CHECKS WERE NORMAL WITH NO DISCREPANC IES NOTED. 2 L 7 2 4F RT A16WE 2001121900123 20011219 00123 NM 2001 12 19 F3LA200100126 1 20011117 A 5330 SKIN BOEING 737 7372L9 1384497 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 3902 22733 DURING C-1 CHECK, INSPECTION REPORTED A 14.5 INCH AREA ON FUSELAGE SKIN LAP AT STR 19R, BS 386-410, SCRATCHED AND GOUGED . REMOVED DAMAGE AT BS 390-404, STR 19R PER SRM 53-30-3, FABRICATED FILLER AND DOUBLER AND INSTALLED PER SRM 53-30-3, 5 1-20-4, 20-10-18 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2001121900128 20011219 00128 NM 2001 12 19 F3LA200100131 1 20011125 A 5754 RIVET BOEING 737 737228 13844AG NM L/E SLAT LOOSE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED RT WING NR 5 SLAT HAD WORKING RIVETS ON INNER SKIN NEXT TO ACTUATOR CUTOUT. REPLA CED FASTENERS PER SRM 51-30-2. 2 L 7 2 4F RT A16WE 2001121900129 20011219 00129 NM 2001 12 19 F3LA200100132 1 20011130 A 2120 ODOR BOEING 737 7372L9 1384497 NM CABIN DETECTED A F3LA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 03 271FL 22734 UPON DEPARTURE FROM ABQ, FLIGHT CREW REPORTED STRONG PULL TO THE RIGHT JUST AFTER TAKEOFF THRUST WAS SET. FULL LEFT RUD DER WITH A LITTLE TILLER STRAIGHTENED THE AIRCRAFT OUT AND CONTINUED TAKEOFF ROLL, WHICH APPEARED NORMAL. ALSO REPORTED A STRONG BURNING RUBBER SMELL AT GEAR RETRACTION, WHICH WAS THOUGHT TO BE A BLOWN TIRE. AIRCRAFT CONTINUED TO ELP TO B URN FUEL. DECLARED AN EMERGENCY IN ELP AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED LT. AND RT. LANDING GEAR, LT . AND RT. WINGS AND FLIGHT CONTROLS, TAXIED AIRCRAFT AND RAN BOTH ENGINES TO TAKEOFF POWER, AND RAN LT. AND RT. PACKS. ALL OPERATIONAL CHECKS WERE NORMAL. 2 L 7 2 4F RT A16WE 2001121900130 20011219 00130 NM 2001 12 19 F3LA200100133 1 20011201 A 3150 WARNING SYSTEM BOEING 737 7373Q8 1384670 NM COCKPIT MALFUNCTIONED A F3LA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 03 319FL 26301 ABORTED TAKEOFF. FLIGHT CREW REPORTED CONFIGURATION WARNING AT LESS THAN 10 KTS. NO BRAKES WERE APPLIED. AIRCRAFT WAS PROPERLY CONFIGURED. FLIGHT CREW MOVED SPEED BRAKE HANDLE, FLAP HANDLE, SET AND RELEASED PARKING BRAKE AND RAN ENGINE, WITH NO WARNING. PROCEEDED WITH NORMAL TAKEOFF. UPON ARRIVAL IN SFO, MAINTENANCE PERFORMED TAKEOFF WARNING TEST PER M M 31-26-00, WITH NO ABNORMAL INDICATIONS. 2 L 7 2 4F RT A16WE 2001121900132 20011219 00132 NM 2001 12 19 F3LA200100135 1 20011216 A 2120 SMOKE AIRBUS A319 A319111 3930336 NM CABIN DETECTED A F3LA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 03 902FR 1515 UPON ARRIVAL, FLIGHT CREW REPORTED SMOKE IN CABIN DURING APU START WHILE TAXIING TO GATE. PERFORMED CHECKS, WITH NO SMO KE OR DEFECTS NOTED. 2 L 7 2 4F RT A28NM 2001121900133 20011219 00133 NM 2001 12 19 AWXA200100651 1 20011215 A 5330 655298813 SKIN BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 MCN - MAJOR REPAIR - "C" - SKIN CRACKED JUST FWD OF POTABLE WATER SERVICE DOOR BS 947.5, STR 24 L/H. MAINTENANCE CUTOUT THE CRACKED AREA OF SKIN AND PERFORMED A HFEC INSPECTION VERIFYING CRACK WAS CONTAINED. A REPAIR DOUBLER AND FILLER WAS FABRICATED AND INSTALLED IAW B737-300 SRM 53-00-01, PG 201-203. 2 L 7 2 4F RT A16WE 2001121900134 20011219 00134 NM 2001 12 19 AWXA200100652 1 20011217 A 5340 65677757 FITTING BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - "C" - DURING C-15 CHECK MAINTENANCE FOUND A 1.2" CRACK ON FRAME ATTACH FITTING AT BS 616, RBL 45. M AINTENANCE REMOVED CRACKED ATTACH FITTING AND FABRICATED A NEW STIFFENING ANGLE AND FILLER. REPAIR WAS INSTALLED AT BS 6 16, RBL 45, IAW AWA ER 03-5311-01143-DD1. 2 L 7 2 4F RT A16WE 2001122000001 20011220 00001 WP 2001 12 20 0104469915 1 20010710 A 5310 DOOR FRAME DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 965N 47417 DURING L-CK IN DHN, A CRACK WAS FOUND IN THE UPPER AFT CORNER OF THE DOOR JAMB. REPAIRED PER AMITASK 5330-01130-2C. RE PAIRED PER EA 99-183995. 2 L 7 2 4F A6WE 2001122000002 20011220 00002 WP 2001 12 20 0104479922 1 20010719 A 5310 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 945N 47664 DURING M-CK IN ATL, A .8 INCH CRACK WAS FOUND IN THE LOWER AFT CORNER OF THE FORWARD CARGO DOOR JAMB. REPAIRED PER EA 9 9-181281. 2 L 7 2 4F A6WE 2001122000003 20011220 00003 WP 2001 12 20 0104559915 1 20010710 A 5310 DOOR FRAME DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 965N 47417 DURING L-CK IN DHN, A CRACK WAS FOUND IN THE UPPER AFT CORNER OF THE DOOR JAMB. REPAIRED PER AMITASK 5330-01130-2C. RE PAIRED PER EA 99-183995. 2 L 7 2 4F A6WE 2001122000004 20011220 00004 WP 2001 12 20 0104569922 1 20010719 A 5310 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 945N 47664 DURING M-CK IN ATL, A .8 INCH CRACK WAS FOUND IN THE LOWER AFT CORNER OF THE FORWARD CARGO DOOR JAMB. REPAIRED PER EA 9 9-181281. 2 L 7 2 4F A6WE 2001122000005 20011220 00005 NM 2001 12 20 0104725644 1 20011204 A 2611 SMOKE DETECTOR BOEING 757 757251 1384970 NM LAVATORY ACTIVATED A NWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 544US 26491 THREE LAV SMOKE DETECTORS WENT OFF EN ROUTE. FLIGHT DIVERTED TO JAX AND LANDED WITHOUT INCIDENT. MAINTENANCE DEFERRED THE APU AND THE FLIGHT CONTINUED TO ITS SCHEDULED DESTINATION. 2 L 7 2 4F RT A2NM 2001122000006 20011220 00006 WP 2001 12 20 0104739903 1 20011208 A 2611 WARNING SYSTEM DOUG DC9 DC931 3022065 WP CARGO BAY MALFUNCTIONED A NWAA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 01 953N 47083 WHILE AT CRUISE FL280, RECEIVED FORWARD CARGO SMOKE INDICATION. THE MASTER WARNING ILLUMINATED ACCOMPANIED WITH A FIRE BELL. COMPLIED WITH COM PROCEDURES AND DISCHARGED BOTH EXTINGUISHER BOTTLES INTO THE FORWARD CARGO AREA. NO SMOKE EVER IN CABIN OR COCKPIT. AN EMERGENCY WAS DECLARED AND THE FLIGHT DIVERTED TO BUF. LANDING WAS UNEVENTFUL EXCEPT AIRCRAFT WAS MET BY CFR EQUIPMENT. NO EVIDENCE OF SMOKE OR FIRE WAS FOUND. MAINTENANCE TESTED BOTH DETECTION AND SUPPRESSION S YSTEMS IN THE CARGO AREAS AND FOUND NO DISCREPANCIES. REPLACED BOTH FORWARD AND AFT CARGO AREA FIRE EXTINGUISHING BOTTL ES. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2001122000007 20011220 00007 NM 2001 12 20 0104746624 1 20011208 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 624US 21706 DURING LINE CHECK, FOUND ZONE 'C' AND 'E' FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2001122000008 20011220 00008 WP 2001 12 20 0104759969 1 20010730 A 5320 CHANNEL DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9333 47246 DURING H-CHECK AT ATL, WHILE ACCOMPLISHING APB INSPECTIONS, A 1.125 INCH CRACK WAS FOUND IN THE UPPER INBOARD BEND RADIU S OF THE 5910130-9 CHANNEL RUNNING DOWNWARD ALONG THE RADIUS. REPAIRED PER EA 99-185020. 2 L 7 2 4F A6WE 2001122000009 20011220 00009 WP 2001 12 20 0104769969 1 20010731 A 5320 DOOR FRAME DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9333 47246 DURING H-CHECK AT ATL BASE, THE VENTRAL STAIR OPENING LHS BEAM UPPER JAMB WAS FOUND CRACKED BETWEEN NR 2 AND NR 3 GUIDE PIN RECEPTACLE. REPAIRED PER EA 99-185020. 2 L 7 2 4F A6WE 2001122000013 20011220 00013 NM 2001 12 20 01FDEA01066 1 20011212 A 5320 STRAP BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 285FE 22622 CORROSION (C53-111-01, 3) ON LOWER SURFACE OF TENSION STRAP AT BS 1130, RBL 45, WL 201. REMOVED AND REPLACED PER SRM 53 -10-1, 53-10-2. 2 L 7 3 4F RT A3WE 2001122000014 20011220 00014 NM 2001 12 20 01FDEA01067 1 20011212 A 2910 O-RING DOUG MD11 MD11 3023602 NM MANIFOLD FILTER BROKEN A FDEA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 588FE 48490 NR 3 HYD FLUID SYS LEAK. REMOVED AND REPLACED NR 3 HYD MANIFOLD FILTER AND O-RING. 2 L 7 3 4F RT A22WE 2001122000015 20011220 00015 WP 2001 12 20 01FDEA01068 1 20011211 A 3260 TARGET DOUG DC10 DC1010F 3022111 WP LANDING GEAR DEFECTIVE A FDEA O OTHER N FALSE WARNING DE DESCENT 1 SO 25 056FE 47810 DID NOT RECEIVE GREEN LANDING GEAR LIGHT WHEN LANDING GEAR SELECTED DOWN. ADJUSTED ROLLER PER MM 32-34-03-2. REMOVED A ND REPLACED TARGET. 2 L 7 3 4F A22WE 2001122000016 20011220 00016 EU 2001 12 20 01FDEA01069 1 20011213 A 2425 WARNING SYSTEM AIRBUS 310 A310203 3930313 EU COCKPIT FALSE INDICATION A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 403FE 230 ON CLIMB APU GENERATOR FAULTED. PERFORMED BIT CHECK, NO FAULT FOUND. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2001122000017 20011220 00017 NM 2001 12 20 01FDEA01071 1 20011212 A 3241 423071 CONTROL UNIT BOEING 727 7272S2F 1384O81 NM ANTI-SKID SYS FAILED A FDEA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 25 210FE 22932 CAPT AND 1ST OFF LEFT BRAKE NOT FUNCTIONING. REMOVED AND REPLACED ANTI-SKID CONTROL UNIT PER MM 32-42-061. 2 L 7 3 4F A3WE 2001122000018 20011220 00018 2001 12 20 01FDEA01074 4 20011218 A 3417 HG480B13 ADC BOEING 727 7272S2F 1384O81 NM E/E BAY FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 210FE 22932 NR 1 ADC FAILED DURING CLIMBOUT. REMOVED AND REPLACED NR 1 ADC PER MM 34-12-011-4. 2 L 7 3 4F A3WE 2001122000019 20011220 00019 EU 2001 12 20 01FDEA01075 1 20011216 A 2612 FIRE WARNING AIRBUS 300 A300F4605R 3930327 EU COCKPIT ACTIVATED A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION AP APPROACH 1 SO 25 662FE 761 RECEIVED ECAM FIRE WARNING MIN EQUIPMENT BAY SMOKE. DEFERRED PER MEL 21-11-12. 2 L 7 2 4F RT A35EU 2001122000020 20011220 00020 WP 2001 12 20 01FDEA01077 1 20011210 A 5312 PRESSURE PANEL DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 392 46626 RT MLG W/W FWD BULKHEAD AND CENTER TANK UPPER AFT CHORD W/SLANT PANEL CORRODED APPROX RBL 70-80. REMOVED AND REPLACED A NGLE CHORD, SUPPORT FITTING APB7090-2 & WEB PER SRM 51-10-00 & 51-31-01 & SRM 51-00-01. PERFORMED FUSELAGE PRESS PER MM 21-00-00-5 GOT 219 SECS/CK'D GOOD. 2 L 7 3 4F A22WE 2001122000021 20011220 00021 WP 2001 12 20 01FDEA01078 1 20011218 A 5743 ARB0642501 FRAME DOUG DC10 DC1010F 3022111 WP RT WING CRACKED A FDEA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 SO 25 363 48263 DURING 1ST FLT TEST - RT MLG RETRACT CYL SUPPORT FRAME ASSY FAILURE OCCURRED, CAUSING LOSS OF NR 3 HYD SYS. FAILURE OCC URRED DURING L/GEAR TESTS W/GEAR EXTENDED. AFTER RECOVERY OF ACFT, DETAILED VISUAL INSP PERF'D PER BOEING MSG ARP-VCE-0 1-00089H 18 DEC 01. FAILED SUPPORT FRAME INSTALLED P/N ARB0642-501 MADE OF TITANIUM. THIS P/N IS AFFECTED BY POSSIBLE FAILURE DUE TO FATIGUE AS PER DOUGLAS SB DC10-57-105. 2 L 7 3 4F A22WE 2001122000022 20011220 00022 NM 2001 12 20 01FDEA01079 1 20011218 A 5754 RIB BOEING 727 727277 138408S NM L/E SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241 20979 RIB CRACKED ON NR 7 L/E SLAT WS 601 AT WBL 492. REPAIRED RIB IAW FEDEX SRM 57-50-3. 2 L 7 3 4F RT A3WE 2001122000023 20011220 00023 EU 2001 12 20 DHL2001365519 1 20011201 A 5313 STRINGER AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH 149 LEVEL 2 CORROSION AT STR 47 LT BETWEEN FR 35 SRM REF 53-14-00 PG 250 ITEM 264. REMOVED FASTENERS PER SRM 51-30-29. CUT OUT DAMAGED AREA PER SRM 53-10-10. FABRICATED REPAIR PARTS PER SRM 53-10-10. CLEANED, TREATED AND PRIMED PER SRM 51-6 0-12. INSTALLED REPAIR PER SRM 51-30-29. 2 L 7 2 4F RT A35EU 2001122000024 20011220 00024 EU 2001 12 20 DHL2001365538 1 20011130 A 5313 STRINGER AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH 149 SEVERAL COUPLING SECTIONS CORRODED BETWEEN FR 33-34 STRINGERS 48-50 LT, 48-50 RT. REMOVED COUPLING AT STR 49L FR 33-34 RT & LT PER SRM 51-30-30. INSTALL NEW COUPLING PER SRM 51-30-30. REMOVED COUPLING AT STR 50L, FR 33-34 PER SRM 51-30-3 0. INSTALLED NEW COUPLING PER SRM 51-30-30. REMOVED AND REPLACED COUPLING AT STR 48R, FR 33-34 PER SRM 51-30-30. REMO VED AND REPLACED COUPLING AT STR 50R PER SRM 51-30-30. 2 L 7 2 4F RT A35EU 2001122000025 20011220 00025 NM 2001 12 20 DHL2001708015 1 20011124 A 5751 SKIN BOEING 727 72725 1384006 NM AILERON CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 LEFT WING INBOARD AILERON UPPER SURFACE HAS 2 CRACKS 5.5 INCHES APART. OUTBOARD CRACK APPROX 2.25 INCHES LONG, INBOARD APPROX 2 INCHES. REMOVED EXISTING I/B AILERON SKIN LT SIDE IAW B727 SRM 57-30-2 (UPPER) REPLACED SKIN IAW B727 SRM 57-1 0-02. INSTALLED UPPER I/B AILERON SKIN IAW B727 SRM 57-30-2. 2 L 7 3 4F A3WE 2001122000026 20011220 00026 2001 12 20 DHL2001715011 4 20011201 A 2211 COMPUTER BOEING 727 727155C 138404Z NM AUTOPILOT SYS FAULTY A DHLA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 01 715DH 19618 WITH AUTO PILOT ENGAGED RAPID DEFLECTION OF CONTROL WHEEL OCCURS BOTH LEFT AND RIGHT OF ABOUT 10 DEGREES. DEFERRED AUTO PILOT SYSTEM AND MX CONTROL WAS NOTIFIED. REMOVED AND REPLACED ROLL CHANNEL COMPUTER, OPS CHECKS GOOD IAW B727 MM 22-1 1-111. 2 L 7 3 4F A3WE 2001122000027 20011220 00027 NM 2001 12 20 DHL2001720015 1 20011130 A 3040 WINDSHIELD WIPER BOEING 727 727228 1384083 NM WINDSHIELD OUT OF ADJ A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 720DH 19544 F/O WIPER BLADE INOP ON LOW AND 1/2 SPEED, INTERMITTENT ON 3/4 WIND-SCREEN WET. RE-ADJUSTED BLADE TENSION PER 727-200 M /M 30-42-42 PG 202. GROUND OP'S CK NORMAL. 2 L 7 3 4F RT A3WE 2001122000028 20011220 00028 NM 2001 12 20 DHL2001721009 1 20011214 A 3040 WINDSHIELD WIPER BOEING 727 727228 1384083 NM WINDSHIELD BINDING A DHLA K NONE O OTHER UK UNKNOWN 1 SO 01 721DH 19545 FIRST OFFICER'S WIPER INOP. FOUND WIPER TO BE BOUND UP. RELEASED TENSION, OPS CHECKED GOOD IAW BMM CH 30-42-01. 2 L 7 3 4F RT A3WE 2001122000029 20011220 00029 NM 2001 12 20 DHL2001727026 1 20011207 A 3350 RELAY BOEING 727 727228 1384083 NM CABIN FAILED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 EMERGENCY EXIT LIGHTS ON WITH SWITCH IN ARMED POSITION. REMOVED AND REPLACED R-70 RELAY IAW WD 33-51-01 AND M/M 33-50-1 01, OPS CHECK NORMAL. 2 L 7 3 4F RT A3WE 2001122000030 20011220 00030 NM 2001 12 20 DHL2001741018 1 20011201 A 3350 BATTERY PACK BOEING 727 7272Q9 138448M NM CABIN DISCHARGED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 741DH 21931 EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK IAW MM 33-50-101. 2 L 7 3 4F RT A3WE 2001122000031 20011220 00031 NM 2001 12 20 DHL2001743017 1 20011204 A 2612 CONNECTOR BOEING 727 727225 1384077 NM FIRE LOOP LOOSE A DHLA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 743DH 22438 NR 1 ENGINE GROUND FAULT INDICATOR ILLUMINATED. PERFORMED NR 1 ENGINE GROUND FAULT INDICATION IAW B727 MEL B 26-9 CAT C CONTROL 7893 PLACARD INSTALLED. FOUND AFT CONNECTOR ON ENGINE FIRE LOOP DIRTY AND SLIGHTLY LOOSE. CLEANED AND SECURED PLUG. FIRE WARNING CKS GOOD PER MM 26-11-00. 2 L 7 3 4F A3WE 2001122000032 20011220 00032 NM 2001 12 20 DHL2001743018 1 20011207 A 2612 FIRE LOOP BOEING 727 727225 1384077 NM NR 1 ENGINE OUT OF POSITION A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 743DH 22438 ENGINE NR 1 FIRE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED. POSITIONED FIRE LOOP SO IT WON`T CONTACT ENG COWL IAW B727 MM 26-11-00. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2001122000033 20011220 00033 NM 2001 12 20 DHL2001743019 1 20011208 A 2612 WARNING LIGHT BOEING 727 727225 1384077 NM COCKPIT INTERMITTENT A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 743DH 22438 ENGINE NR 1 GROUNDED CIRCUIT DETECTION LIGHT INTERMITTENTLY FLICKERS IN FLT. REMOVED AND REPLACED NR 1 ENG FIRE DET GRO UND LIGHT AT P6 PNL ELECTRICAL CONNECTIONS AT HARNESS. CLEANED AND RESEATED DETECTOR CONTROL UNIT FUNCTION CHECKED PER MM 26-11 INDICATIONS SERVICEABLE. 2 L 7 3 4F A3WE 2001122000034 20011220 00034 NM 2001 12 20 DHL2001743020 1 20011213 A 2612 SOCKET BOEING 727 727225 1384077 NM COCKPIT DEFECTIVE A DHLA K NONE N FALSE WARNING UK UNKNOWN 1 SO 01 743DH 22438 ENGINE NR 1 FIRE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED. ISOLATED FIRE LOOP, TESTED GOOD. FOUND LIGHT SOCKET ASSY P /N 91180M BAD. REMOVED AND REPLACED NR 1 ENGINE GROUND FAULT DETECTOR LIGHT SOCKET. OPS CHECKS GOOD. 2 L 7 3 4F A3WE 2001122000035 20011220 00035 NM 2001 12 20 DHL2001745018 1 20011130 A 3260 DOOR BOEING 727 727224 1384076 NM NLG OUT OF ADJ A DHLA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 745DH 20665 NOSE GEAR DOOR LIGHT ILLUMINATED AND REMAINS ON FORWARD PANEL AND ON S/O PANEL. PERFORMED LANDING GEAR DOOR WARNING, AD JUSTMENT AND TEST PER DHL B-727 M/M 32-62-0. NO DEFECTS FOUND. OK FOR FURTHER SERVICE. 2 L 7 3 4F A3WE 2001122000036 20011220 00036 NM 2001 12 20 DHL2001748011 1 20011205 A 2612 WARNING SYSTEM BOEING 727 727225 1384077 NM COCKPIT MALFUNCTIONED A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 748DH 22440 DURING CLIMBOUT NR 2 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED. COULD NOT DUPLICATE, SYS OPS CKS GOOD IAW 26-11-00. 2 L 7 3 4F A3WE 2001122000037 20011220 00037 NM 2001 12 20 DHL2001748012 1 20011210 A 2612 LIGHT BOEING 727 727225 1384077 NM COCKPIT INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 748DH 22440 NR 2 ENGINE GROUND FAULT WILL NOT PRESS TO TEST. RELAMPED NR 2 ENGINE. GROUND FAULT DETECTOR, CHECKS GOOD IAW MM CH 26 -11-0. 2 L 7 3 4F A3WE 2001122000038 20011220 00038 NM 2001 12 20 DHL2001749002 1 20011130 A 3040 WINDSHIELD WIPER BOEING 727 727200 138407E NM WINDSHIELD OUT OF ADJ A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 749DH 22013 CAPT'S W/S WIPER INOP. SERVICEABLE ADJUSTED WIPER TENSION IAW B727 M/M 30-42-42, OPERATIONAL CHECK. 2 L 7 3 4F RT A3WE 2001122000039 20011220 00039 WP 2001 12 20 DHL2001806018 1 20011208 A 2611 SMOKE DETECTOR DOUG DC8 DC873F 302199F WP CARGO BAY FAILED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 806DH 46002 NR 2 UPPER CARGO SMOKE DETECTOR WILL NOT TEST. REMOVED AND REPLACED NR 2 SMOKE DETECTOR, TEST LIGHT BULB OPS CHECKS GOO D PER 26-10-0. 2 L 7 4 4F RT 4A25 2001122000040 20011220 00040 WP 2001 12 20 DHL2001807028 1 20011201 A 5270 WIRE DOUG DC8 DC873F 302199F WP DOOR WARNING CHAFED A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 807DH 45990 BELLY DOOR LIGHT CAME ON DURING CLIMBOUT AT 270 WENT OUT DURING DESCENT AT 16, PRESSURIZATION NORMAL. FOUND NR 3 BELLY DOOR WIRING CHAFING ON FUSELAGE. REPAIRED WIRING SYSTEM CHECKS GOOD IAW 52-70-0. 2 L 7 4 4F RT 4A25 2001122000041 20011220 00041 NM 2001 12 20 DL76K011880 1 20011130 A 2781 849704 PSEU BOEING 767 767332 1382001 NM E/E BAY FAULTY A DALA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 SO 27 172DZ 29691 LEADING EDGE SLAT ASYMMETRY LIGHT ILLUMINATED ON APPROACH. PSEU HAS NUMEROUS TARGET FAULTS. REPLACED PSEU AND OPERATED FLAPS SEVERAL TIMES. OPS CHECK OK. TESTED PSEU PER MM, OPS OK. 2 L 7 2 4F RT A1NM 2001122000042 20011220 00042 EU 2001 12 20 AWXA200100655 1 20011218 A 5753 D57571601272 FLAP AIRBUS 320 A320231 3930325 EU #1 FLAP PUNCTURED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 82 YWG - MAJOR REPAIR - "C" - DURING C-02 CHECK MAINTENANCE DISCOVERED THE L/H OUTBOARD TRAILING EDGE FLAP HAS A PUCTURE ON THE LOWER SURFACE JUST INBOARD OF THE #3 CANOE. MAINTENANCE CUTOUT THE DAMAGED AREA OF SKIN AND FABRICATED, FITTED, AND INSTALLED A HONEYCOMB CORE PLUG IAW AWA ER 26-5753-01351-TB1, SHT 1 & 2. 2 L 7 2 4F RT A28NM 2001122000043 20011220 00043 NM 2001 12 20 AWXA200100656 1 20011218 A 5330 654577518 SKIN BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 MCN - MAJOR REPAIR - "C" - SKIN HAS 2" CRACK JUST AFT OF WING TO BODY FAIRING BS 787, STR 24L. MAINTENANCE REMOVED EXIST ING REPAIR AND CUTOUT 2.5" X 1" OF DAMAGED SKIN. PERFORMED A HFEC INSPECTION VERIFYING CRACK WAS CONTAINED. FABRICATED A ND INSTALLED 2 EACH DOUBLERS, TRIPLERS, AND FILLERS IAW AWA ER 03-5331-01352-TB3. 2 L 7 2 4F RT A16WE 2001122000044 20011220 00044 NM 2001 12 20 AWXA200100657 1 20011219 A 3350 BMS13311122 WIRE BOEING 757 7572G7 1384963 NM BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 910AW 24523 PHX - EEL - "C" - EMERGENCY ISLE LIGHT INOPERATIVE AT ROW 23 L/H. MAINTENANCE DISCOVERED BROKEN SPLICE AT OUTBOARD SEAT TRACK ROW 23 L/H. REPAIRED WIRE WITH ENVIRONMENTAL SPLICE OUTBOARD SEAT TRACK ROW 23 L/H IAW SWPM 20-10-00, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2001122000045 20011220 00045 SO 2001 12 20 C2XA01IA418 1 20011216 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13979 367 239 145181 BNA - The last two emergency aisle path lights were found to be inoperative. Maintenance removed and replaced the #4 eme rgency light battery pack. An operational test of the aisle path lighting was performed successfully and the aircraft wa s returned to service. 2 L 7 2 4T RT T00011AT 2001122000046 20011220 00046 EU 2001 12 20 C2XA01IA419 1 20011219 A 3350 0341315 FUSE AEROSP ATR42 ATR42320 8680930 EU A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15823 165 During a 3A inspection the aisle path lights at seat row 5 were found to be inoperative. Maintenance removed and replace d a fuse in battery pack 3WL. The system operationally checked good, and the aircraft was returned to service. 2 H 7 2 4T RT A53EU 2001122000047 20011220 00047 NM 2001 12 20 DL76P011933 1 20011213 A 2740 285T0015117 MODULE BOEING 767 767332 1382001 NM E/E BAY FAILED A DALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 27 143DA 25991 AFTER T/O STAB TRIM WAS INOP. MANUAL TRIM OK. FLAP IND STOPPED AT 1 DEGREE. REPLACED RIGHT SAM MODULE. 2 L 7 2 4F RT A1NM 2001122000048 20011220 00048 NM 2001 12 20 DL76S011920 1 20011210 A 3350 20131A BATTERY PACK BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 124DE 23438 LEFT FORWARD OVERHEAD EMERGENCY LIGHTS INOP IN CABIN. REMOVED AND REPLACED BATTERY PACK FOR LEFT FORWARD OVERHEAD EMERG ENCY LIGHTS, CHECKS GOOD. 2 L 7 2 4F RT A1NM 2001122000049 20011220 00049 NM 2001 12 20 DL777011898 1 20011204 A 3251 ACTUATOR BOEING 777 777232 1385232 NM STEERING SYS FAILED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 863DA 29735 ABORTED T/O DUE TO MAIN GEAR STEERING AND T/O WARN HORN. MTC MSGS 32-63010 AND 32-63020 ACTIVE. AUTO EVENT RT ACTUATOR FAILED. FWD TO MCO AND PLC. LT ACTUATOR WILL NOT LOCK. PERFORMED MDM BLOCK PROCEDURE TO ZE OUT AND LOCK. 2 L 7 2 4F RT T00001SE 2001122000050 20011220 00050 NM 2001 12 20 DL777011908 1 20011208 A 2520 ODOR BOEING 777 777232 1385232 NM SEAT 11H DETECTED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 866DA 29738 CREW REPORTS POSSIBLE ELECTRICAL SMELL, SEAT 11-H. SEAT OPERATION NORMAL, NO ELECTRICAL SMELL NOTED. INSPECTED WIRES, ALL CHECKS OK. 2 L 7 2 4F RT T00001SE 2001122000051 20011220 00051 NM 2001 12 20 DLM11011918 1 20011210 A 4990 38809981 PUMP DOUG MD11 MD11 3023602 NM APU LEAKING A DALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 809DE 48480 A/C DIVERTED IAD DUE SMOKE IN CABIN. REPLACED APU OIL PUMP AND SEALS. 2 L 7 3 4F RT A22WE 2001122000052 20011220 00052 NM 2001 12 20 DLM11011934 1 20011208 A 5330 AGA3102501 SKIN DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 802DE 48473 CORROSION WAS FOUND DURING MTC ON PREVIOUSLY INSTALLED REPAIR DOUBLERS AT STA 1937 AND 1959 NEAR THE AFT LAV AIR EXHAUST PORTS. THE DOUBLERS HAD BEEN INSTALLED IN NOV 1996. REPAIRED PER ER/A 360666-14, REV B. 2 L 7 3 4F RT A22WE 2001122000053 20011220 00053 NM 2001 12 20 DLM88011888 1 20011203 A 3350 RPS1 CHARGER DOUG MD88 MD88 3023688 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 915DE 53420 ON L/O, FOUND SEAT ROW 1-12 EMERGENCY LIGHTS INOP. T/S PER MM REPLACED CHARGER AND BATTERY FOR SAME PER MM, SYS OPS CHE CK OK. 2 L 7 2 4F RT A6WE 2001122000054 20011220 00054 NM 2001 12 20 DLM88011890 1 20011204 A 3233 329001057 ACTUATOR DOUG MD88 MD88 3023688 NM RT MLG FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 940DL 49813 RT MAIN GEAR UNSAFE LIGHT REMAINS ON AFTER GEAR RETRACTION. PERFORMED POM PROCEDURES, LIGHT REMAINS ON. ALSO GOT AUTO- SPOILER FAIL MSG ON AFTER INITIAL GEAR RETRACTION, LANDING GEAR INDICATION. CHECK PROX SENSORS ALL OK. REPLACED RIGHT MAIN GEAR ACTUATOR ASSY, OPS CHECKS OK, NO LEAK DETECTED. REF M/M 32-32-02-2. 2 L 7 2 4F RT A6WE 2001122000055 20011220 00055 NM 2001 12 20 DLM88011905 1 20011207 A 2910 1240386CR02 HYDRAULIC LINE DOUG MD88 MD88 3023688 NM NR 2 ENGINE LEAKING A DALA K NONE K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 951DL 49882 RIGHT HYD QTY WENT TO ZERO APPROX 15 MIN AFTER T/O. REPLACED NR 2 ENGINE HYDRAULIC PUMP AND PRESSURE FLEX LINE FOR CHAF ING AND LEAKING OF THE LINE. 2 L 7 2 4F RT A6WE 2001122000057 20011220 00057 NM 2001 12 20 AALA20012050 1 20011116 A 2421 GEN3014 IDG BOEING 777 777223 1385213 NM LT ENGINE FAILED A AALA K NONE J WARNING INDICATION DE DESCENT 1 SW 21 799AN 30258 MIA - FLT 57 - LEFT ELECT GENERATOR FAILED DURING DESCENT. ALSO, GOT ICE DETECTOR LEFT AND ELECT GENERATOR L STATUS MES SAGES. REPLACED LEFT ENGINE IDG, RAN ENGINE, OPS CHECK LEAK CHECK GOOD. (M) 2 L 7 2 4F RT T00001SE 2001122000058 20011220 00058 NM 2001 12 20 2001F00751 1 20011111 A 2410 6A47000 COOLER BOEING 727 727259 138408J NM NR 2 ENGINE FAULTY A FX7A A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 SO 19 203AV 22474 DURING CLIMB-OUT OF SVMI, 25 MINUTES AFTER TAKEOFF NR 3 CSD GEN TEMP IN 160 DEGREES, RISE 25 DEGREES VOLTS 110 FREQS 390 , AFTER REDUCING LOAD AND 10 MINUTES LATER, TEMP 120 RISE 18. AIRCRAFT RETURNED TO SVMI, DUE TO NR 2 CSD ALREADY DEFERR ED. REMOVED AND REPLACED NR 2 AND NR 3 CSD (P/N 700842A AND S/N'S 15340 AND 7366), AND CSD OIL COOLERS (P/N 6A47000 AND S/N'S 9948 AND 10102) IAW MM 24-10-61. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001122000059 20011220 00059 NM 2001 12 20 2001F00752 1 20011111 A 2410 6A47000 COOLER BOEING 727 727259 138408J NM NR 3 ENGINE FAULTY A FX7A A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 SO 19 203AV 22474 DURING CLIMB-OUT OF SVMI, 25 MINUTES AFTER TAKEOFF NR 3 CSD GEN TEMP IN 160 DEGREES, RISE 25 DEGREES VOLTS 110 FREQS 390 , AFTER REDUCING LOAD AND 10 MINUTES LATER, TEMP 120 RISE 18. AIRCRAFT RETURNED TO SVMI, DUE TO NR 2 CSD ALREADY DEFERR ED. REMOVED AND REPLACED NR 2 AND NR 3 CSD (P/N 700842A AND S/N'S 15340 AND 7366), AND CSD OIL COOLERS (P/N 6A47000 AND S/N'S 9948 AND 10102) IAW MM 24-10-61. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2001122000060 20011220 00060 WP 2001 12 20 AALA20011805 1 20010921 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 437AA 49455 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 7D INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT CONNE CTOR AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001122000062 20011220 00062 WP 2001 12 20 AALA20011834 1 20010930 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 437AA 49455 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT FIRST CLASS DIVIDER SECTION INOPERATIVE. SECURED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001122000063 20011220 00063 NM 2001 12 20 AALA20011835 1 20011001 A 3397 GROUND WIRE BOEING 767 767223 1385123 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 329AA 22329 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT FROM SEAT 9AB THROUGH 20AB INOPERATIVE. REPLACED EMERGENCY EXI T LIGHT GROUND WIRE AT SEAT 19AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001122000064 20011220 00064 WP 2001 12 20 AALA20011849 1 20011008 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP L1 DOOR LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 596AA 53286 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT PORTABLE ASSEMBLY AT L1 DOOR INOPERATIVE. RECONNECTED EMERGENC Y LIGHT CONNECTOR AT PORTABLE LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001122000065 20011220 00065 WP 2001 12 20 AALA20011934 1 20011011 A 5754 HORN DOUG DC9 DC982 3022082 WP L/E SLAT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7520A 49897 TUL - FOUND NR 0 RIGHT INBOARD SLAT HORN HAS DAMAGE ON INBOARD SIDE LOWER. STRAIGHTENED DENTED AREA PER ESO 80559. REF ORMED AND DYE CHECKED. (M) 2 L 7 2 4F A6WE 2001122000066 20011220 00066 WP 2001 12 20 AALA20011941 1 20011021 A 4920 5940405503 APU DOUG DC9 DC982 3022082 WP APU BAY LEAKING A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 474 49649 EWR - FLT 1643 - EN ROUTE LGA-HOU, SHORTLY AFTER TAKEOFF DETECTED SMOKE IN CABIN AND COCKPIT. DIVERTED EWR AND LANDED W ITHOUT FURTHER INCIDENT. REPLACED APU. SYSTEM GROUND CHECKS NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001122000067 20011220 00067 NM 2001 12 20 AALA20011942 1 20011022 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 373AA 25200 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 23H INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRING AT SEAT 23H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001122000068 20011220 00068 WP 2001 12 20 AALA20011947 1 20011023 A 3610 CLAMP DOUG DC9 DC982 3022082 WP ACM LOOSE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 224AA 49174 DFW - FLT 1086 - EN ROUTE DFW-MSY, DETECTED TAIL HIGH TEMPERATURE LIGHT ILLUMINATE IN COCKPIT. RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. RE-SECURED CLAMP AT LEFT SIDE AIR CYCLE MACHINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M ) 2 L 7 2 4F A6WE 2001122000069 20011220 00069 NM 2001 12 20 AALA20011948 1 20011023 A 3397 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 353AA 24034 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 23D INOPERATIVE. RESECURED EMERGENCY EXIT LIGHT CONNEC TOR AT SEAT 23D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001122000070 20011220 00070 2001 12 20 AALA20011949 4 20011022 A 2565 D31038201 SLIDE DOUG DC9 DC982 3022082 WP L2 DOOR DEFECTIVE A AALA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 473AA 49648 DFW - FLT 1732 - AFT DOOR SLIDE INADVERTENTLY DEPLOYED. SLIDE PARTIALLY DEPLOYED. REPLACED AFT DOOR SLIDE. SYSTEM GRO UND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001122000071 20011220 00071 2001 12 20 AALA20011953 4 20011023 A 3442 PAN5357 CONTROL PANEL BOEING 767 767323 1385205 NM COCKPIT FAILED A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 352AA 24033 WEATHER RADAR UNUSABLE ON 20-40 MILE RANGES ALL RED PLUS SHOWING NO RETURNS, BOTH CAPTAINS AND FIRST OFFICERS. REMOVED AND REPLACED WEATHER RADAR CONTROL PANEL PER MM AND CHECK OPERATION FUNCTION PER MM SYSTEM OK FOR SERVICE. (M) 2 L 7 2 4F RT A1NM 2001122000072 20011220 00072 NM 2001 12 20 AALA20011961 1 20011029 A 3350 4082135 LIGHT BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 391AA 27451 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 3A BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT S EAT 3A. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001122000073 20011220 00073 NM 2001 12 20 AALA20011969 1 20011026 A 2421 GEN3014 IDG BOEING 777 777223 1385213 NM LT ENGINE FAILED A AALA K NONE J WARNING INDICATION CR CRUISE 1 SW 21 787AL 30010 JFK - LEFT GENERATOR TRIPPED OFF IN FLIGHT, DID NOT RESET. SERVICED LT AND RT IDGS AND APU. A/C RESTRICTED TO 120 MINS ETOPS. CHANGED LT GCU, PERFORMED ENGINE RUN UP NO HELP. SHOWS MAINTENANCE MSG 24-31611 IDG LT EXCITER FIELD CURRENT I S OUT OF RANGE. REPLACED LEFT ENGINE IDG OPS AND LEAK CHECK GOOD. (M) 2 L 7 2 4F RT T00001SE 2001122000074 20011220 00074 NM 2001 12 20 AALA20012014 1 20011105 A 3397 CONNECTOR BOEING 767 767223 1385123 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 323AA 22324 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHT INOPERATIVE AT SEAT 28B. RECONNECTED CONNECTOR FOR EMERGENCY EXIT ESCAPE PATH LIGHT AT SEAT 28B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001122000075 20011220 00075 EU 2001 12 20 AALA20012015 1 20011105 A 3397 PIN FOKKER F28 F28MK0100 4990807 EU CONNECTOR DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1438H 11428 ORD - DURING OVERNIGHT MAINTENANCE, RIGHT OVERWING HATCH EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED PIN IN CONNECTOR OF RIGHT OVERWING HATCH EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001122000076 20011220 00076 NM 2001 12 20 AALA20012034 1 20011110 A 3397 PIN BOEING 767 767323 1385205 NM CONNECTOR DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 368AA 25195 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 37H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT PINS. SYSTE M GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001122000077 20011220 00077 EU 2001 12 20 AALA20012037 1 20011109 A 3350 4002243 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 33069 512 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 7D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2001122000078 20011220 00078 WP 2001 12 20 AALA20012040 1 20011112 A 3350 LIGHT DOUG DC9 DC983 3022083 WP TAILCONE INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 595AA 53285 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT TAIL CONE INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMB LY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2001122000079 20011220 00079 NM 2001 12 20 AALA20012041 1 20011112 A 3397 CONNECTOR BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 788AN 30011 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 3G INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT CONNECTO R. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001122000080 20011220 00080 NM 2001 12 20 AALA20012042 1 20011112 A 3397 CONNECTOR BOEING 777 777223 1385213 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 788AN 30011 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 4G INOPERATIVE. RESECURED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 4G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2001122000081 20011220 00081 NM 2001 12 20 AALA20012044 1 20011118 A 3397 PIN BOEING 767 767323 1385205 NM CONNECTOR LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 352AA 24033 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 22H INOPERATIVE. REPINNED EMERGENCY EXIT LIGHT AT SEAT 22H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001122000082 20011220 00082 NM 2001 12 20 AALA20012045 1 20011117 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 373AA 25200 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 29H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBL Y AT SEAT 29H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001122000083 20011220 00083 NM 2001 12 20 AALA20012046 1 20011117 A 3350 4033578 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 373AA 25200 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 28H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBL Y. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001122000084 20011220 00084 2001 12 20 AALA20012049 4 20011116 A 2565 5A33071B PIN BOEING 737 737823 13844BZ NM EVAC SLIDE OUT OF POSITION A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 908AN 29510 TUL - FOUND FORWARD ENTRY DOOR SLIDE FAILED TO DEPLOY DUE TO LANYARD ROLL PIN STICKING OUT LOCKING LANYARD IN FIXED POSI TION MAKING SLIDE UNABLE TO DEPLOY. REPLACED DOOR SLIDE AND LANYARD ASSEMBLY. (M) 2 L 7 2 4F RT A16WE 2001122000085 20011220 00085 NM 2001 12 20 AALA20012051 1 20011121 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 908AN 29510 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 18D INOPERATIVE. RESECURED EMERGENCY EXIT LIGHT AT SEA T 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2001122000086 20011220 00086 NM 2001 12 20 AALA20012052 1 20011113 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 381AN 25450 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 20H INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT AT S EAT 20H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2001122000087 20011220 00087 NM 2001 12 20 AALA20012054 1 20011113 A 3397 CONNECTOR BOEING 757 757223 1384957 NM R2 DOOR LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 609AA 27447 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT R2 DOOR INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT CONNE CTOR AT R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2001122000088 20011220 00088 EU 2001 12 20 AALA20012055 1 20011112 A 2913 862536 PUMP FOKKER F28 F28MK0100 4990807 EU NR 2 ENGINE LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 1433B 11418 ORD - FLT 1842 - EN ROUTE ORD-IAD, NR 2 HYDRAULIC SYSTEM PRESSURE DECREASED TO ZERO. RETURNED ORD AND LANDED WITHOUT FU RTHER INCIDENT. REPLACED NR 1 AND NR 2 HYDRAULIC PUMPS AND FILTERS. RAN BOTH ENGINES. NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001122000089 20011220 00089 SO 2001 12 20 AALA20012057 1 20011114 A 2913 849589 PUMP PIPER PA23 PA23250 7102308 SO NR 1 ENGINE LEAKING A AALA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 952AN 272862 SNA - FLT 1429 - EN ROUTE ORD-SNA - DURING CRUISE NR 1 AND NR 2 HYDRAULIC ENGINE PUMP LOW PRESSURE LIGHTS ILLUMINATED. LANDED SNA WITHOUT FURTHER INCIDENT. REPLACED HYDRAULIC ENGINE PUMPS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 1 L 7 2 3O 1A10 2001122000090 20011220 00090 EU 2001 12 20 AALA20012067 1 20011124 A 3240 005359 MANIFOLD FOKKER F28 F28MK0100 4990807 EU LT MLG DEFECTIVE A AALA K NONE J WARNING INDICATION AP APPROACH 1 SW 21 1445B 11448 ORD - FLT 795 - EN ROUTE PHL-ORD, SHORTLY BEFORE LANDING LEFT MLG WOULD NOT LOCK IN THE DOWN POSITION. AFTER A SECOND A TTEMPT, LANDING GEAR LOCKED DOWN SUCCESSFULLY. LANDED ORD WITHOUT FURTHER INCIDENT. REPLACED BRAKE SWIVEL MANIFOLD. S WUNG GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001122000091 20011220 00091 WP 2001 12 20 AALA20012070 1 20011126 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 297AA 49309 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 30DEF INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001122000092 20011220 00092 EU 2001 12 20 AALA20012080 1 20011127 A 3010 CONNECTOR FOKKER F28 F28MK0100 4990807 EU RT WING LOOSE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 1407D 11360 MSP - FLT 486 - EN ROUTE MSP-ORD, SHORTLY AFTER TAKEOFF WING ANTI-ICE ALERT ILLUMINATED ON MFDU. RETURNED MSP AND LANDE D WITHOUT FURTHER INCIDENT. RECONNECTED RIGHT ANTI-ICE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2001122000093 20011220 00093 2001 12 20 COMA0160974 4 20011219 A 3414 8220372154 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 SO 01 806CA 20881 7359 FLIGHT 5073 - PILOTS AIRSPEED INDICATION INOP DURING T/O.COULD NOT DUPLICATE. PURGED PITOT SYSTEM AND REPLACED AIR DATA COMPUTER FOR TROUBLE SHOOTING. 2 L 7 2 4F RT A21EA 2001122000094 20011220 00094 SO 2001 12 20 ASOA01250 1 20011020 A 5320 12009846001 CROSSBEAM EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 274AS 120229 DURING C-CHECK INSPECTION IN BNA, THE CROSS BEAM AT FRAME 16 WAS CORRODED FROM THE LEFT BUTT STRAP TO THE LEFT WALL. MA INTENANCE REMOVED AND REPLACED CORRODED CROSS BEAM IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2001122000095 20011220 00095 SO 2001 12 20 ASOA01251 1 20011020 A 5320 120272929001 BUTTSTRAP EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 274AS 120229 DURING C-CHECK INSPECTION IN BNA, THE LEFT AFT BUTT STRAP HAS CORROSION BETWEEN FRAMES 32 AND 39. MAINTENANCE REMOVED A ND REPLACED CORRODED BUTT STRAP IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2001122000096 20011220 00096 SO 2001 12 20 ASOA01252 1 20011020 A 5347 SEAT TRACK EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AS 120229 DURING C-CHECK INSPECTION IN BNA, THE LEFT FLOOR SEAT TRACK, FORWARD SECTION, WAS FOUND CORRODED FROM FRAME 17 TO FRAME 26. CORROSION WAS ALSO FOUND ON THE LEFT FLOOR SEAT TRACK, AFT SECTION, FROM FRAME 32 TO 39. MAINTENANCE REMOVED AND R EPLACED BOTH FORWARD AND AFT SECTIONS OF CORRODED FLOOR SEAT TRACKS IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2001122000097 20011220 00097 SO 2001 12 20 ASOA01253 1 20011020 A 5347 SEAT TRACK EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 274AS 120229 DURING C-CHECK INSPECTION IN BNA, THE RIGHT FLOOR SEAT TRACK, FORWARD SECTION, WAS FOUND TO BE CORRODED OUT OF ALLOWABLE LIMITS FROM FRAME 15 TO FRAME 32. MAINTENANCE REMOVED CORRODED FORWARD SECTION OF THE RIGHT FLOOR SEAT TRACK. A NEW S EAT TRACK WAS FABRICATED AND INSTALLED IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2001122000098 20011220 00098 2001 12 20 COMA0160975 4 20011219 A 3414 INDICATOR CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 SO 01 806CA 7359 FLIGHT 5033 - PILOTS AIR SPEED INDICATION INOP DURING T/O.COULD NOT DUPLICATE. SYSTEM TEST WAS NORMAL. 2 L 7 2 4F RT A21EA 2001122000099 20011220 00099 SO 2001 12 20 ASOA01254 1 20011020 A 5347 SEAT TRACK EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 274AS 120229 DURING C-CHECK INSPECTION IN BNA, THE LEFT WALL SEAT TRACK, FORWARD SECTION, WAS FOUND TO BE CORRODED FROM FRAME 17 TO 3 2. THE LEFT, AFT SECTION, OF THE WALL SEAT TRACK WAS ALSO FOUND TO BE CORRODED BETWEEN FRAMES 34 AND 38. MAINTENANCE R EMOVED CORRODED SEAT TRACKS AS WELL AS FABRICATED NEW TRACKS IAW SRM 51-40-02. THE NEW TRACKS WERE INSTALLED IAW SRM 53 -20-11. (M) 2 L 7 2 4T RT A31SO 2001122000100 20011220 00100 EU 2001 12 20 ASOA01255 1 20011112 A 5311 FRAME AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 636AS 375 DURING C-CHECK INSPECTION IN BNA, FRAME 26 WAS CRACKED AT BL0. MAINTENANCE REPAIRED CRACK IAW ASA EO72-53-0118. THIS E O REF SB 72-53-1078 AND INCLUDES REPAIR SPECIFICATIONS FOR CRACK ON AIRCRAFT. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2001122000101 20011220 00101 EA 2001 12 20 COMA0160976 1 20011219 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 420CA 7451 FLIGHT 5602. FLAPS FAILED AT 27 DEGREES DURING RETRACTION.RESET THE FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01 . 2 L 7 2 4F RT A21EA 2001122000102 20011220 00102 NM 2001 12 20 01FDEA01072 1 20011217 A 5531 STRINGER BOEING 727 727233 138408A NM VERTICAL STAB CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 285FE 22622 VERTICAL STAB NR 7 STR LT IS CHAFED 3 INCHES FRONT OF SLIDING SEAT TRACK. REPAIRED CHAFFED AREA OF VERTICAL FIN STR 7 M ID SPAR STA 229 PER SRM 55-30-06 FIG 3 PER FEDEX EA NR 7-5530-54129. 2 L 7 3 4F RT A3WE 2001122000103 20011220 00103 NM 2001 12 20 01FDEA01080 1 20011218 A 5754 RIB BOEING 727 727277 138408S NM L/E SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241 20979 RIB CRACKED ON NR 6 L/E SLAT WS 491 AT WBL 398. REPAIRED RIB IAW FEDEX SRM 57-50-03. 2 L 7 3 4F RT A3WE 2001122000104 20011220 00104 NM 2001 12 20 01FDEA01081 1 20011218 A 5754 RIB BOEING 727 727277 138408S NM L/E SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241 20979 RIB CRACKED ON NR 6 L/E SLAT WS 520 AT WBL 415. REPAIRED RIB IAW FEDEX SRM 57-50-3. 2 L 7 3 4F RT A3WE 2001122000105 20011220 00105 NM 2001 12 20 01FDEA01082 1 20011218 A 5312 BULKHEAD BOEING 727 727277 138408S NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241 20979 BULKHEAD WEB CRACKED AT BS 1183 LBL 66.35 WL 224.5. REPAIRED WEB IAW FEDEX SRM 51-30-2. 2 L 7 3 4F RT A3WE 2001122000106 20011220 00106 NM 2001 12 20 01FDEA01084 1 20011218 A 5310 DOOR FRAME BOEING 727 727277 138408S NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241 20979 AFT LWR CORNER NR 1 CARGO DOOR FRAME CRACKED BS 600. REPAIRED DOOR FRAME IAW FEDEX SRM 51-30-02. 2 L 7 3 4F RT A3WE 2001122000107 20011220 00107 NM 2001 12 20 01FDEA01085 1 20011218 A 5330 SKIN BOEING 727 727277 138408S NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241 20979 CORROSION OF FUSELAGE SKIN BS 720C TO D AT STR 28L. REPAIRED SKIN IAW FEDEX SRM 53-30-3. 2 L 7 3 4F RT A3WE 2001122000108 20011220 00108 NM 2001 12 20 01FDEA01086 1 20011218 A 5511 SPAR BOEING 727 727277 138408S NM HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241 20979 UPPER REAR SPAR OF LT HORIZ STAB HEAVY CORROSION STAB STA 188.65 RSS 116.71. REPAIRED UPPER SPAR IAW FEDEX SRM 55-10-5. 2 L 7 3 4F RT A3WE 2001122000109 20011220 00109 NM 2001 12 20 01FDEA01087 1 20011218 A 3232 SUPPORT FITTING BOEING 727 727277 138408S NM NLG CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241 20979 SUPPORT FITTING NOSE LANDING GEAR DOOR ACT RODS CORRODED BS 227.8 LBL 6. REPLACED SUPPORT FITTING IAW FEDEX MM 32-33-05 14. 2 L 7 3 4F RT A3WE 2001122000110 20011220 00110 NM 2001 12 20 01FDEA01088 1 20011218 A 5320 WEB BOEING 727 727277 138408S NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241 20979 WEB AT C-1 DOOR CUTOUT CRACKED BS 534 TO 540 AT STR 24R. REPAIRED WEB IAW FEDEX SRM 51-40-2. 2 L 7 3 4F RT A3WE 2001122100001 20011221 00001 NM 2001 12 21 SWAA013357 1 20011216 A 5314 65621258 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM CORRODED AT VERTICAL LEG, BETWEEN BS 514-BS 520, STRINGER 28R. REPAIRED PE R SWA RA. 2 L 7 2 4F RT A16WE 2001122100002 20011221 00002 NM 2001 12 21 SWAA013358 1 20011218 A 3350 81000 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 089SW 22904 DURING SCHEDULED C2 CHECK, FOUND EEPLS AFT END CAP MISSING. INSTALLED END CAP PER MM. 2 L 7 2 4F A16WE 2001122100003 20011221 00003 2001 12 21 SWAA013352 4 20011216 A 2565 1061323 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR TORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE GIRT ASSY TORN. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001122100004 20011221 00004 NM 2001 12 21 SWAA013353 1 20011218 A 5320 6517583 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/4D CHECK, FOUND BS 180 VERTICAL WEB CRACKED, WL 183, LBL 17. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2001122100005 20011221 00005 NM 2001 12 21 CALA0101033 1 20011218 A 5320 WEB BOEING 737 7373T0 1384582 NM STA 178 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 60312 23363 INSPECTION FOUND A 1.25" AND 1" CRACK IN CENTER WEB OF FORWARD BULKHEAD AT STA 178, LBL 5.7, BETWEEN WL 195 AND 207. THE CENTER WEB WAS REPLACED IAW EA 5310-03040 AND WORK CARD 99-5310-1-0037. 2 L 7 2 4F RT A16WE 2001122100006 20011221 00006 NM 2001 12 21 CALA0101034 1 20011220 A 5754 SKIN BOEING 737 7373T0 1384582 NM #6 SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 63305 23356 INSPECTION FOUND A 1/4" CRACK IN R/H WING #6 SLAT PANEL SKIN. REPAIRED IAW SRM 57-43-01. 2 L 7 2 4F RT A16WE 2001122100007 20011221 00007 NM 2001 12 21 CALA0101035 1 20011221 A 5320 WEB BOEING 737 7373T0 1384582 NM STA 338 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 60312 23363 INSPECTION FOUND A GOUGE IN WEB ON R/H SIDE OF E&E DOOR JAMB STRUCTURE AT STA 338, RBL 15. A DOUBLER WAS INSTALLED IAW S RM 51-70-13. 2 L 7 2 4F RT A16WE 2001123100007 20011231 00007 NM 2001 12 31 01FDEA01089 1 20011218 A 3234 CONTROL HANDLE DOUG MD11 MD11 3023602 NM COCKPIT FAULTY A FDEA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 578 48458 LANDING GEAR W/N EXTEND WITH GEAR HANDLE PLACED IN DOWN. RECYCLED AND GEAR EXTENDED. REMOVED AND REPLACED LANDING GEAR HANDLE PER MM 32-31-02-4. 2 L 7 3 4F RT A22WE 2002010300095 20020103 00095 2002 1 3 2001UALA02323 4 20011123 A 2210 8220195102 CONTROL PANEL BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE COCKPIT FAILED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 206UA 679 30212 150NM FROM SFO TO ELEC SMELL AND A LITTLE SMOKE IN THE COCKPIT. MODE CONTROL PNL AND AUTO THROTTLE KICKED OFF AND CB PO PPED. SMOKE AND SMELL RAPIDLY DISSIPATED. FLT RETURNED TO SFO. MODE CONTROL PANEL P/N 822-0195-102 REPLACED. PRELIMI NARY FINDINGS BY COMPONENTS SHOP INDICATE A FAILURE OF A CAPACITOR (C6) INSIDE THE MODE CONTROL PANEL P/N 822-0195-102 ( UA MR22411-63). 2 L 7 2 4F 4 F RT T0001SE E46NE 2002010400025 20020104 00025 2002 1 4 2001UALA02394 4 20011208 A 3140 COMPUTER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE RIGHT MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 29 786UA 26938 ACFT RETURNED TO STAND WITH RIGHT ENGINE BLEED PROBLEM. NO STATUS MESSAGE. CONFIRMED RIGHT ENGINE PRSOV NOT OPERATING CORRECTLY. FOUND IOM 004 MODULE IN THE RIGHT AIMS SHOWING HARD FAULT. RESET AIMS MODULE AND SWAPPED RIGHT AIMS IOM 009 WITH RIGHT AIMS IOM 004 FOR TROUBLESHOOTING. ALL MESSAGES CLEARED. PERFORMED ENG RUN PER JRH. BLEED OPS NORMAL. RES ET OF AIMS CORRECTED THE PROBLEM OF NO STATUS MESSAGE. NO AIMS PARTS WERE REPLACED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002010400026 20020104 00026 NM 2002 1 4 2001UALA02399 1 20011209 A 2133 90231570381 OUTFLOW VALVE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN PRESSURE FAILED A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 807UA MR21301245 798 CREW RETURNED TO GATE AFTER CABIN PRESSURE 2 FAULT. CENTRALIZED FAULT DISPLAY SYSTEM REPORTED OUTFLOW VALVE MOTOR 2 FAU LT. REPLACED VALVE AND CABIN PRESSURE CONTROLLER NR 2 AS PRECAUTION. NO FURTHER FAULTS REPORTED. (NOTE: THIS INCIDENT OCCURRED ON THE GROUND SHORTLY AFTER ENGINE START). 2 L 7 2 4F 4 F RT A28NM E40NE 2002010400027 20020104 00027 NM 2002 1 4 2001UALA02400 1 20011207 A 2130 VFT210A VALVE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN PRESSURE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 810UA MR212131333 843 CREW REPORTS AVIONICS SYSTEM FAULT. EXTRACT VALVE SHOWING CLOSED. AIRCRAFT WAS INDICATING FAULTS FOR BOTH THE SKIN AIR INLET AND OUTLET VALVES WITH THE OUTLET VALVE DEFERRED INOPERATIVE. THE SYSTEM WAS REACTIVATED ON THE GROUND AND THE F AULT WAS ISOLATED TO THE INLET VALVE. THE OUTLET VALVE DEFERRAL WAS CLEARED DUE TO THE SUCCESSFUL GROUND TESTING AND TR OUBLESHOOTING, AND THE INLET VALVE WAS SUBSEQUENTLY REPLACED WITH NO FURTHER FAULTS REPORTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2002011000145 20020110 00145 NM 2002 1 10 2001UALA02401 1 20011212 A 2150 DOOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RAM AIR INLET DAMAGED A UALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 29 644UA 25094 EN ROUTE CREW REPORTED SIGNIFICANT VIBRATION AND DIVERTED TO DENVER. LT RAM AIR INLET DOOR SECTION FOUND MISSING. DOOR WAS REMOVED AND SYSTEM WAS DEFERRED PER CDL 21BA. DOOR P/N 213T3010-1 AND ASSOCIATED HARDWARE WERE REPLACED AT DEN. 2 L 7 2 4F 4 F RT A1NM E24NE 2002011000147 20020110 00147 NM 2002 1 10 2001UALA02406 1 20011212 A 5330 RIVET BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUSELAGE WRONG PART A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 769UA 26515 26921 THERE IS A PROTRUDING HEAD RIVET IN THE EXTRA CRITICAL AREA (REF RVSM). RIVET IS LOCATED LEFT SIDE OF FUSELAGE APPROXIM ATELY 2 FEET FORWARD OF STATIC PORTS BELOW DOOR 2L. MAJOR REPAIR ACCOMPLISHED. REPLACED RIVET WITH ONE SIZE OVER FLUSH HEAD AND MICROSHAVED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001122100008 20011221 00008 NM 2001 12 21 2001UALA02407 1 20011213 A 2720 WARNING SYSTEM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT ACTIVATED A UALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 WP 29 359UA 24452 LANDED UNDER AMBER ALERT DUE TO RUDDER CONTROL PROBLEMS. 2 L 7 2 4F 4 F RT A16WE E2GL 2001122100009 20011221 00009 WP 2001 12 21 ABXA010625 1 20011119 A 5755 5910055516 SKIN DOUG DC9 DC941 302207N WP SPOILER DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 INBOARD SPOILER UPPER SURFACE WAS DELAMINATED. REPLACED RIGHT WING INBOARD SPOILER PANEL IAW DC-9 MM 27-61-1-4-0001. 2 L 7 2 4F A6WE 2001122100010 20011221 00010 NM 2001 12 21 ABXA010627 1 20011118 A 7110 FRAME BOEING 767 767281 1385109 NM NR 2 COWL DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 791AX 23141 ENGINE NR 2 RIGHT CORE COWL FRAME NAC STA 304.60, NAC WL 75, FOUND DAMAGE ON FRAME. FABRICATED REPAIR PARTS, INSTALLED AND REPAIRED AREA IAW REA B671-42172MR. 2 L 7 2 4F RT A1NM 2001122100011 20011221 00011 NM 2001 12 21 PCAA0112170 1 20011220 A 5610 NP15790210 WINDOW DHAV DHC8 DHC8102 2809003 NM FIRST OFFICERS CRACKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 841EX 20964 249 MDT- DURING ROUTINE MAINTENANCE VISIT WHILE PERFORMING DEHAVILLAND MAINTENANCE TASK 5310/07C FIRST OFFICERS SIDE WINDOW FOUND TO HAVE CRACKS AROUND THREE BOLT HOLES ALONG BOTTOM EDGE OF WINDOW. FIRST OFFICERS SIDE WINDOW REPLACED IN ACCORDA NCE WITH DEHAVILLAND MAINTENANCE MANUAL 56-10-16. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001122100012 20011221 00012 2001 12 21 WRNA200100019 4 20011218 A 3417 4034100901 ADC AIRBUS 300 A300B4203 3930306 EU Zone 100 FAILED A WRNA A UNSCHED LANDING E VIBRATION/BUFFET TO TAKEOFF 1 SO 05 505TA 704 271 #1 AIR DATA COMPUTER FAILED ON TAKE OFF. WITH FULL THROTTLES AIR SPEED KEPT DECREASING- A/C SHOOK VIOLENTLY- NO STICK SH AKER OR CLACKER.CORRECTIVE ACTION: R&R'D #1 ADC COMPUTER OPS CK'D GOOD PER MM 34-12-34. PERFORMED EXCESSIVE TURBULANCE I NPECTION I/A/W MM 5-51-17 NO FAULTS NOTED, PERFORMED PITOT-STATIC CHECK ON #1 AND #2 SYSTEM, SYSTEMS OPS CK GOOD PER MM 34-11-10 PAGE 501, NO DEFECTS NOTED. FOR CAUSE COMPLIED WITH TEST FLIGHT, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE . 2 L 7 2 4F RT A35EU 2001122100013 20011221 00013 EA 2001 12 21 COMA0160977 1 20011220 A 5346 6015300 BEAM CNDAIR CL600 CL6002B19 1900309 EA AFT EQUIP BAY CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 966CA 12762 7132 ENGINE SUPPORT BEAM CRACKED.REPAIRED DAMAGED I/A/W REO 601R-53-61-366. 2 L 7 2 4F RT A21EA 2001122100014 20011221 00014 EA 2001 12 21 COMA0160978 1 20011220 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA AC PACK MALFUNCTIONED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 708CA 7235 FLIGHT 5835 - CLIMBING THRU 7000' NOTICED A/C PACKS OFF, AND BLEEDS CLOSED. COULD NOT GET A/C PACKS ONLINE. COULD NOT DUPLICATE. OPERATIONAL CHECKS OF A/C, PRESSURIZATION, AND BLEED AIR VALVES WERE NORMAL. 2 L 7 2 4F RT A21EA 2001122100015 20011221 00015 EA 2001 12 21 COMA0160979 1 20011219 A 3010 DUCT CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 987CA 7199 FLIGHT 5692. ANTI-ICE DUCT WARNING MESSAGE DURING T/O.COULD NOT DUPLICATE. GROUND RUNS AND OPERATION OF ANTI-ICE SYSTE M, FOUND NO FAULTS. 2 L 7 2 4F RT A21EA 2001123100003 20011231 00003 WP 2001 12 31 0104889857 1 20011206 A 5743 FITTING DOUG DC9 DC951 3022051 WP LT WING CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 766NC 47739 DURING MCK IN ATL, CORROSION WAS FOUND ON THE LT SIDE MLG FIXED SIDE BRACE LUG. REPAIRED PER EA 98-185385. 2 L 7 2 4F RT A6WE 2001122100016 20011221 00016 SO 2001 12 21 RAIA00112009 1 20011212 A 3350 3625101 LIGHT EMB 145 EMB145 3260210 SO INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 801HK 145053 MX-RIC- CENTER CABIN EMERGENCY DOME LIGHT INOP. MAINTENANCE REMOVED AND REPLACED CENTER CABIN DOME LIGHT ASSEMBLY IAW EM B145 MM 33-50-10. 2 L 7 2 4F RT T00011AT 2001122300001 20011223 00001 EU 2001 12 23 C2XA01IA422 1 20011220 A 3260 D22924010 PROXIMITY SWITCH AEROSP ATR42 ATR42320 8680930 EU RT. MLG FAILED A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 14830 184 CLL- AFTER TAKEOFF,THE RIGHT MAIN GEAR WOULD NOT RETRACT. THE GREEN SYSTEM PRESSURE GAUGE FLUCTUATED ALONG WITH THE GE AR UNSAFE INDICATIONAS WELL AS A LOUD BANGING/RATTLING FROM THE RIGHT SIDE OF AIRCRAFT. FLIGHT CONTINUED AT 160 KIAS WI TH DOWN and THREE (3) GREEN INDICATION. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. IAH- MAINTENANCE REMOVED AND REP LACED THE RIGHT MLG UPLOCK PROX SWITCH, PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR,NO DEFECTS NOTED, AND, THE AIR CRAFT WAS APROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001122300002 20011223 00002 SO 2001 12 23 C2XA01IA423 1 20011220 A 3232 21180100401 ACTUATOR EMB 135 EMB135LR 3260305 SO NLG DOOR DEFECTIVE A C2XA K NONE O OTHER AP APPROACH 1 SW 27 17524 145399 CLE- DURING FLIGHT 3177 THE CREW NOTED THAT THE "LDG GEAR AIR GRD FAIL" ILLUMINATED WHEN GEAR SELECTED DOWN, DISAPPEARS WHEN "3 GREEN"SHOW. CLE- MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND NOSE GEAR DOOR ACTUATOR, PERFORMED A OPERATI ONAL CHECK OF THE LANDING GEAR SYSTEM,NO DEFECTS NOTED,AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT TOOO11AT 2001122400001 20011224 00001 NM 2001 12 24 01FDEA01097 1 20011223 A 5751 RIB BOEING 727 727277 138408S NM LEFT WING CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 N 567 LEFT WING OUTBOARD AILERON #6 RIB CRACKED. R&R AILERON PER MM 27-10-031-2. 2 L 7 3 4F RT A3WE 2001122400002 20011224 00002 WP 2001 12 24 01FDEA01101 1 20011222 A 2611 SMOKE DETECTOR DOUG DC10 DC1010 3022110 WP CABIN FAULTY A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 390FE 46624 NR 12 CABIN CARGO SMOKE DETECTOR LIGHT CAME ON. R&R NR 12 SMOKE DETECTOR PER MM 26-18-01-2. 2 L 7 3 4F A22WE 2001122400003 20011224 00003 NM 2001 12 24 01FDEA01104 1 20011223 A 5712 RIB BOEING 727 727277 138408S NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 RT WING LEAD EDGE RIB CRACKED WS 510, WBL 415. R&R RIB PER SRM 51-40-2. 2 L 7 3 4F RT A3WE 2001122400004 20011224 00004 NM 2001 12 24 01FDEA01105 1 20011223 A 5260 STEP BOEING 727 727277 138408S NM AIRSTAIRS CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 TOP AIRSTAIR STEP CRACKED AT BS 1183-1190. R&R STEP PER SRM 51-10-1. 2 L 7 3 4F RT A3WE 2001122400005 20011224 00005 NM 2001 12 24 F3LA200100139 1 20011223 A 5310 WEB BOEING 737 737228 13844AG NM CORRODED A F3LA O OTHER O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 INSPECTION, INSPECTION REPORTED KEEL BEAM WEB CORRODED FROM B.S. 787 TO B.S. 807, RBL 10. FABRICATED AND INS TALLED REPLACEMENT WEB PER SRM 53-10-2, ITEM 33, PAGE 32, 41. 2 L 7 2 4F RT A16WE 2001122400006 20011224 00006 NM 2001 12 24 AWXA200100659 1 20011206 A 5315 654541041 WEB BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - DURING C-15 CHECK MAINTENANCE DISCOVERED WEB ON LONGITUDINAL FLOOR BEAM CRACKED IN 4 PLACES, BS 706 , LBL .07. MAINTENANCE REMOVED 4 EACH WEB STIFFNERS (BS 700, 706, 711, 715) AND DAMAGED SECTION OF FLOOR BEAM WEB AT LBL .07 BS 700 TO 715. FABRICATED AND INSTALLED FLOOR BEAM WEB, DOUBLER, AND 4 EACH STIFFNERS AT (BS 700, 706, 711, 715) IA W AWA ER 03-5702-01353-TB2. 2 L 7 2 4F RT A16WE 2001122400007 20011224 00007 NM 2001 12 24 AWXA200100664 1 20011222 A 5230 6547952135 FRAME BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - DURING C-15 CHECK MAINTENANCE DISCOVERED AFT CARGO DOOR CRACKED AT AFT LOWER FRAME ON FLANGE BETWEEN #3 & #4 DOOR STOP FITTINGS, AND ON AFT CORNER OF UPPER FRAME AT BS 827. MAINTENANCE REMOVED AND REPLACED BOTH UPPER AND LOWER FRAMES ON AFT CARGO DOOR IAW AWA E.O. 52-33-02. 2 L 7 2 4F RT A16WE 2001122400008 20011224 00008 NM 2001 12 24 AWXA200100665 1 20011222 A 5230 65C2518024 FRAME BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - "C" - DURING C-15 CHECK MAINTENANCE FOUND THE AFT CARGO DOOR UPPER FWD FRAME CRACKED IN 3 PLACES AT BOLT HOLE BS 800. MAINTENANCE REMOVED AND REPLACED UPPER FWD FRAME ON AFT CARGO DOOR BS 800 IAW AWA E.O. 52-33-02. 2 L 7 2 4F RT A16WE 2001122400009 20011224 00009 NM 2001 12 24 AWXA200100666 1 20011222 A 5230 65C2518034 ANGLE BOEING 737 7373G7 1384595 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - "C" - DURING C-15 CHECK MAINTENANCE DISCOVERED A CRACK ON AFT CARGO DOOR FWD UPPER ANGLE 3RD FASTNE R AT AFT END BS 800. MAINTENANCE REMOVED AND REPLACED FWD UPPER ANGLE ON AFT CARGO DOOR BS 800 IAW AWA E.O. 52-33-02. 2 L 7 2 4F RT A16WE 2001122400010 20011224 00010 EA 2001 12 24 SWIA200110443 1 20011215 A 2133 OUTFLOW VALVE CNDAIR CL600 CL6002B19 1900309 EA PRIMARY FOD A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 416SW 7089 AIRCRAFT WOULD NOT PRESSURIZE. RETURNED TO SLC. REMOVED FOD FROM PRIMARY OUTFLOW VALVE. PERFORMED OPS CHECK PER MM 21 -31-00. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2001122400011 20011224 00011 EA 2001 12 24 SWIA200110446 1 20011215 A 5270 PROXIMITY SWITCH CNDAIR CL600 CL6002B19 1900309 EA AFT PAX DOOR CAM OUT OF ADJ A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 416SW 7089 RED PASSENGER DOOR MESSAGE APPEARED AFTER TAKEOFF OUT OF SLC. RETURNED TO THE FIELD. ADJUSTED AFT PASSENGER DOOR CAM P ROXIMITY SWITCH IAW CRJ MM 52-11-02. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2001122400012 20011224 00012 SO 2001 12 24 C2XA01TY206 1 20011224 A 5320 14522460015 GUSSET EMB 135 EMB135LR 3260305 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 TYS, During a scheduled 1C inspection, corrosion was found in several areas of the gusset, aft of the forward digital. Maintenance removed and replaced the gusset I.A.W.-EMB-135/145-SRM-51-40-02, The repair procedures where satisfactory an d the aircraft will be released upon complection of inspection. 2 L 7 2 4F RT TOOO11AT 2001122600010 20011226 00010 WP 2001 12 26 0104799967 1 20011128 A 5310 PRESSURE PANEL DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9331 47263 During Hck in ATL, a .25" crack was found in the flight compartment horizontal pressure panel at station 105. The crack is located at x=-25. This EA authorizes accomplishment of repair. Material .040" 2024-t3 AL. Repaired per EA 99-185345. 2 L 7 2 4F A6WE 2001122600011 20011226 00011 WP 2001 12 26 0104819155 1 20011127 A 5230 PAN DOUG DC9 DC914 3022034 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8914E 45831 During HCK, the forward cargo door inner pan was found to be cracked between stops #1 and #2. The outer pan was also fou nd cracked. Material .050" 2024-t4. Repaired per EA 91-186760. 2 L 7 2 4F A6WE 2001122600012 20011226 00012 WP 2001 12 26 0104829156 1 20011210 A 5330 SKIN DOUG DC9 DC914 3022034 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8915E 45832 During HCK in DHN, two cracks were discovered per REF. B in the upper fuselage nose skin at stations 76.5 LBL20 & 81 LBL 14.5. At station 76.5, one crack location extended outboard of the trimout of an existing repair. Repaired per EA 91-18 7461. 2 L 7 2 4F A6WE 2001122600013 20011226 00013 WP 2001 12 26 0104839855 1 20011127 A 5740 FITTING DOUG DC9 DC951 3022051 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 764NC 47717 During Mck in DHN, the LH MLG fitting side brace lug was found with corrosion on the forward and aft faces. Repaired per EA 98-186771. 2 L 7 2 4F RT A6WE 2001122600014 20011226 00014 WP 2001 12 26 0104849856 1 20011130 A 5410 WEB DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 765NC 47718 During Line check in ATL, the LH pylon closure rib at STA yn164 was found cracked at the lightening hole lower edge. Rep aired per EA 98-185355. 2 L 7 2 4F RT A6WE 2001122600015 20011226 00015 WP 2001 12 26 0104859864 1 20011205 A 5310 PRESSURE PANEL DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 773NC 47775 During M ck in ATL, cracks were found in the flight compartment horizontal pressure panel at sta 105. Located at x=25 .5 "long and x=35 .5"long. Repaired per EA 98-185344. Material .040" 2024-t3 AL. 2 L 7 2 4F RT A6WE 2001122600016 20011226 00016 WP 2001 12 26 0104879864 1 20011205 A 5310 BRACKET DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 773NC 47775 During Mck in ATL, a .25" crack was found to the RHS bracket 9957860-6. Material 7075-t6 AL. Repaired per EA 98-185364 2 L 7 2 4F RT A6WE 2001122600017 20011226 00017 WP 2001 12 26 0104899967 1 20011212 A 5312 BULKHEAD DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9331 47263 During Hck at ATL, cracks were found in the staion 756 bulkhead. The cracks are located in the upper ends of the verticl e stiffener at x=12LH .90", X=24RH 1.00", x=-12RH .70", and x=-24 .90". Repaired per EA 99-185343. 2 L 7 2 4F A6WE 2001122600018 20011226 00018 NM 2001 12 26 2001UALA02413 1 20011215 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 FRAME AT STA.1420 HAS DENTS ON INNER UPPER FLANGE BETWEEN STRINGER 23L AND 26L. MAJOR REPAIR ACCOMPLISHED.FABRICATED AN D INSTALLED J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2001122600019 20011226 00019 NM 2001 12 26 2001UALA02416 1 20011216 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 AFT PIT FUSELAGE FRAME IS DENTED AT STATION 1460 STRINGER 25 LEFT. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED AREA MFG AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2001122600020 20011226 00020 NM 2001 12 26 2001UALA02418 1 20011216 A 5300 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 CABIN FLOOR STRUCTURE INTERCOSTAL AT STATION 324 TO 345 RBL 64" CORRODED ON UPPER SURFACE. MAJOR REPAIR ACCOMPLISHED.IN STALLED NEW U-SHAPED CHANNEL. 2 L 7 2 4F 4 F RT A2NM E17NE 2001122600021 20011226 00021 NM 2001 12 26 2001UALA02420 1 20011216 A 5311 SPLICE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 AFT PIT FUSE FRAME SPLICE CORRODED AT STATION 1520, STRINGER 24R. MAJOR REPAIR ACCOMPLISHED.REPLACED FRAME SPLICE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001122600022 20011226 00022 NM 2001 12 26 2001UALA02426 1 20011218 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 CABIN FUSELAGE STRINGER 16L HAS DAMAGE FROM BODY STATION 603 TO BODY STATION 606. MAJOR REPAIR ACCOMPLISHED.INSTALLED D OUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2001122600023 20011226 00023 NM 2001 12 26 2001UALA02431 1 20011219 A 5400 SPLICE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 PYLON SPAR ANGLE, LEFT AFT SPLICE CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SPLICE PLATE. 2 L 7 2 4F 4 F RT A1NM E24NE 2001122600030 20011226 00030 NM 2001 12 26 CALA0101040 1 20011223 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 373 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 60312 23363 INSPECTION FOUND A 3/8" CRACK IN FUSELAGE SKIN AT STA 373, S28, E&E EXHAUST BAY CUTOUT. REPAIRED IAW ECRA 5330-02894. 2 L 7 2 4F RT A16WE 2001122600032 20011226 00032 SO 2001 12 26 COMA0110164 1 20011221 A 5240 SWITCH EMB 120 EMB120RT 3260202 SO FUEL SERVICE OUT OF ADJ A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 269CA 120263 FLIGHT 5028 - SERVICE DOOR WARNING LIGHT AFTER T/O.ADJUSTED THE FUEL SERVICE DOOR MICRO SWITCH. 2 L 7 2 4T RT A31SO 2001122600033 20011226 00033 SO 2001 12 26 COMA0110165 1 20011221 A 2750 KRP138112VT ROLLER EMB 120 EMB120RT 3260202 SO R/H OUTBD WORN A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 268CA 120262 FLIGHT 5061 - FLAP DISAGREEMENT WARNING WHEN FLAPS SELECTED UP.REPLACED THE R/H OUTBD FLAP SECTION ROLLERS. 2 L 7 2 4T RT A31SO 2001122600034 20011226 00034 EA 2001 12 26 COMA0160981 1 20011223 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA RH MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 815CA 3262 7397 FLIGHT 5296 - FLAPS FAILED AT 30 DEGREES.REPALCED THE R/H BPSU. 2 L 7 2 4F RT A21EA 2001122600035 20011226 00035 EA 2001 12 26 COMA0160982 1 20011222 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA L/H MALFUNCTIONED A COMA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 01 815CA 3256 7397 FLIGHT 5280 - DURING TAXI THE LEFT SPOILERON DEPLOYED UNCOMMANDED AND WOULD NOT RETRACT.REPLACED THE L/H SPOILERON OUTBD PCU. 2 L 7 2 4F RT A21EA 2001122600036 20011226 00036 EA 2001 12 26 COMA0160983 1 20011221 A 2760 4916405 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 01 729CA 7744 7265 FLIGHT 5872 SPOILERON FAULT MESSAGE DURING T/O.REPLACED THE #3 SECU. 2 L 7 2 4F RT A21EA 2002010700007 20020107 00007 EU 2002 1 7 AWXA200100658 1 20011222 A 5270 AB5012110 SENSOR AIRBUS 320 A320232 3930326 EU CARGO DOOR FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 642AW 584 PHX - AIR TURNBACK - FL190 FLIGHT CREW RECEIVED ECAM MESSAGE FOR FWD CARGO DOOR UNSAFE, AIRCRAFT TURNED BACK TO PHX AND MADE AN UNEVENTFUL LANDING. AT GATE MAINTENANCE FOUND CARGO DOOR SECURED. MAINTENANCE TROUBLESHOT AND REPLACED THE FWD C ARGO DOOR SENSOR (30WV), THE CONNECTOR, AND THE BACKSHELL FOR SENSOR (30WV) IAW AMM 52-71-12-401. 2 L 7 2 4F RT A28NM 2001122600037 20011226 00037 NM 2001 12 26 QXEA0102133 1 20011224 A 2510 110823AA SEAT DHAV DHC8 DHC8202 2809007 NM BROKEN A QXEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 09 355PH 9975 9975 500 PDX - FIRST OFFICERS SEAT BACK BROKE. AIRCRAFT RETURNED TO FIELD. REPLACED FIRST OFFICERS SEAT. OPERATIONAL CHECK IS GOO D. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001122600038 20011226 00038 2001 12 26 SWIA200110459 4 20011213 A 3417 ADC CNDAIR CL600 CL6002B19 1900309 EA BOTH A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 407SW 7034 EFIS COMP MON MESSAGE ''ALT''. RETURNED TO DFW.PURGED PITOT STATIC SYSTEM IAW MM 34-11-00-100-807. REMOVED AND REPLACE D #1 AND #2 ADC'S IAW MM 34-13-01. PITOT STATIC CHECK C/W IAW MM 34-13-00-730-001. LEAK CHECK IAW MM 34-11-00-790-801. #1 S/N ON: 1104 S/N OFF: 1810#2 S/N ON: 1594 S/N OFF: 2014 2 L 7 2 4F RT A21EA 2001122700001 20011227 00001 NM 2001 12 27 BJNA011203 1 20011207 A 3350 LAMP BOEING 737 737282 13844AT NM DOOR EMER EXT LT INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 789TM 23046 LT 1 DOOR EMERGENCY EXTERIOR LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP, OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 2001122700002 20011227 00002 CE 2001 12 27 GLBA2001241 1 20011226 A 3230 1013880083 VALVE BEECH 1900 1900D 1154162 CE A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 254GL UE254 LANDING GEAR WOULD NOT RETRACT / R&R HYDRAULIC SERVICE VALVE 2 L 7 2 4T RT A24CE 2001122700003 20011227 00003 NM 2001 12 27 0104916307 1 20011205 A 5315 FLOORBEAM BOEING 747 747451 1384940 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 667US 24222 DURING "H" CHECK FOUND CORROSION ON FLOORBEAM UPPER CHORD AT BS 920 RBL 51. REPAIRED PER EA 63-186690. 2 L 7 4 4F RT A20WE 2001122700019 20011227 00019 SO 2001 12 27 C2XA01CL257 1 20011224 A 5542 2024T3 SKIN EMB 135 EMB135LR 3260305 SO RUDDER II CRACKED A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 24517 145332 DURING OVERNIGHT MAINTENANCE A CRACK ON THE RUDDER II SKIN WAS FOUND.THE CRACK WAS ON THE RIGHT SIDE OF THE RUDDER AND C LOSE TO THE TRAILING EDGE.MAINTENANCE PERFORMED A PERMANENT REPAIR OF THE RUDDER II SKIN AS PER CONTINENTAL EXPRESS EC 5 540-01015.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT TOOO11AT 2001122700021 20011227 00021 NM 2001 12 27 SWAA013373 1 20011221 A 5311 6546539 FRAME BOEING 737 7373T5 1384608 NM AFT CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT 2 EA PLACES, BS 616, LBL65 AND RBL 65, WL 200. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2001122700022 20011227 00022 NM 2001 12 27 SWAA013374 1 20011222 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED BC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT EXTERNAL POWER DOOR CUT OUT .25 INCH LONG ON AFT SECTION. RE PAIRED SKIN PER SWA RA. 2 L 7 2 4F RT A16WE 2001122700023 20011227 00023 NM 2001 12 27 SWAA013375 1 20011222 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 26L CORRODED, BS 500A. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2001122700024 20011227 00024 NM 2001 12 27 SWAA013376 1 20011222 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 28R CORRODED, BS 480. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2001122700025 20011227 00025 NM 2001 12 27 SWAA013377 1 20011222 A 5311 6546532 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CORRODED, BS 480, BETWEEN STRINGERS 27L AND 26L. REPAIRED SHEAR TIE PER SR M. 2 L 7 2 4F RT A16WE 2001122700026 20011227 00026 NM 2001 12 27 SWAA013378 1 20011222 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED, BS 938, STRINGER 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001122700027 20011227 00027 NM 2001 12 27 SWAA013379 1 20011221 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM AFT CABIN ERRATIC A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT ERRATIC. REMOVED AND REPLACED LIGHT ASSY.. 2 L 7 2 4F A16WE 2001122700028 20011227 00028 NM 2001 12 27 SWAA013380 1 20011222 A 5753 6546435152 FLAP BOEING 737 7372H4 138448C NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING WALKAROUND INSPECTION, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM. 2 L 7 2 4F A16WE 2001122700029 20011227 00029 NM 2001 12 27 SWAA013384 1 20011221 A 3350 100031 LIGHT BOEING 737 7377H4 1384404 NM AFT CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 716SW 27850 AFT GALLEY EMERGENCY EXIT LIGHT ASSY LOOSE. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2001122700030 20011227 00030 NM 2001 12 27 SWAA013390 1 20011223 A 5320 65C27314 CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 680AA 23505 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED, BS 727A, STRINGER 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2001122700031 20011227 00031 NM 2001 12 27 SWAA013391 1 20011223 A 5312 BAC1505 ANGLE BOEING 737 7373H4 1384600 NM FWD FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD VERTICAL CHORD ANGLE CRACKED, LBL 5.7, WL 190. REPAIRED VERTICAL CHO RD ANGLE SECTION PER SRM. 2 L 7 2 4F RT A16WE 2001122700032 20011227 00032 NM 2001 12 27 SWAA013392 1 20011223 A 5240 6545871 SKIN BOEING 737 7373H4 1384600 NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/4D CHECK, FOUND SKIN CRACKED AT FWD SERVICE DOOR AROUND LOWER HINGE. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2001122700033 20011227 00033 NM 2001 12 27 SWAA013393 1 20011225 A 5315 6546804 BEAM BOEING 737 7373A4 1384585 NM CABIN FLOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 680AA 23505 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED, BS 986, LBL 29 TO RBL 51.5. REMOVED AND REPLACED FLO ORBEAM UPPER CHORD PER SRM. 2 L 7 2 4F RT A16WE 2001122700034 20011227 00034 NM 2001 12 27 SWAA013395 1 20011225 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN FLOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 394SW 27380 EEPLS TRACK COVERS LOOSE AT ROWS 13 TO 15. SECURED TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 2001122700035 20011227 00035 NM 2001 12 27 SWAA013363 1 20011220 A 3233 141A76502 BEARING BOEING 737 7377H4 1384404 NM NLG OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 715SW 27849 DURING SCHEDULED C1 CHECK, FOUND NOSE LANDING GEAR ACTUATOR UPPER ATTACH FITTING BEARING MIGRATED. REPAIRED PER SWA RA 1-732-0075. 2 L 7 2 4F RT A16WE 2001122700036 20011227 00036 2001 12 27 SWAA013364 4 20011219 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 & R2 DOORS OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED C2 CHECK, FOUND BOTH AFT CABIN DOOR EVACUATION SLIDE PRESSURE INDICATORS OUT OF VIEW. REPOSITIONED BOT H SLIDE PER MM. 2 L 7 2 4F A16WE 2001122700037 20011227 00037 2001 12 27 SWAA013369 4 20011219 A 2565 65C19901 CABLE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 652SW 27722 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE RELEASE CABLE OUT OF POSITION. REPOSITIONED CABLE PER MM. 2 L 7 2 4F RT A16WE 2001122700038 20011227 00038 NM 2001 12 27 SWAA013370 1 20011218 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE BUCKLED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED C3 CHECK, FOUND AFT PRESS BULKHEAD BUCKLED, BS 1016, STRINGER 7L AND STRINGER 14L. REPAIRED BULKHEAD W EB AND STRAP PER SWA RA 1-353-2763 AND SRM. 2 L 7 2 4F RT A16WE 2001122700039 20011227 00039 EU 2001 12 27 MALA010795 1 20011221 A 3230 10GQA RELAY SAAB SF340 SF340A 7850100 EU A MALA B EMER. DESCENT O OTHER DE DESCENT 1 GL 15 106XJ 340A106 During flight 3393, Landing gear normal extension due to popped Landing Gear Control C/B. Breaker was reset, ORH lead to emergency gear, Maintenance replaced relay 10 GA. Ops check good per SF3 MM Chap 32/30/. Ohmed Landing Gear Control Valve, checked within limits. 2 L 7 2 4T RT A52EU 2001122700040 20011227 00040 NM 2001 12 27 AWXA200100671 1 20011224 A 3350 900835A BATTERY BOEING 737 737277 1384570 NM DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 PHX - EEL - "C" - L1 ENTRY DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE L1 DOOR EMERGENCY LIGHT BATTERY PA CK IAW BMM 33-51-11. 2 L 7 2 4F RT A16WE 2001122700041 20011227 00041 NM 2001 12 27 AWXA200100673 1 20011218 A 5330 654577518 SKIN BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 MCN - MAJOR REPAIR - "C" - MAINTENANCE DISCOVERED 2" CRACK ON SKIN JUST AFT OF WING TO BODY FAIRING BS 787, STR 24L. MAI NTENANCE CUTOUT DAMAGED AREA OF SKIN AND PERFORMED HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED. FABRICATED 2 EACH DOUB LERS, TRIPLERS, AND FILLERS AND INSTALLED REPAIRS BS 787, STR 24L, IAW AWA ER 03-5331-01352-TB3. 2 L 7 2 4F RT A16WE 2001122700042 20011227 00042 EU 2001 12 27 C2XA01IA424 1 20011226 A 3350 AD3127 BATTERY AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 42836 200 IAH- WHILE PERFORMING A LINE CHECK THE MECHANIC NOTED THAT WHEN TESTING THE EMERGENCY LIGHTING, SOME OF THE LIGHTS FAIL ED TO ILLUMINATE. IAH- MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY AT LOCATION 15WL, PERFORMED A OPERATIONA L CHECK, NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001122800001 20011228 00001 EA 2001 12 28 COMA0160989 1 20011223 A 3220 601R751461 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 926CA 19054 7027 FLIGHT 5860 N.L.G. DOORS WARNING AFTER T/O.REPLACED THE NLG DOOR SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2001122800002 20011228 00002 EA 2001 12 28 COMA0160988 1 20011221 A 5210 DOOR FRAME CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 729CA 7265 FLIGHT 6294 DOOR WARNING MESSAGE SHORTLY AFTER T/O.CLEANED DEBRIS FROM DOOR SILL AREA - DORO OPERATION CHECKED NORMAL. 2 L 7 2 4F RT A21EA 2001122800003 20011228 00003 EA 2001 12 28 COMA0160987 1 20011221 A 2750 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA ALL MALFUNCTIONED A COMA O OTHER O OTHER AP APPROACH 1 SO 01 940CA 7048 FLIGHT 5957 FLAPS FAILED WHEN SELECTED FOR APPROACH.COULD NOT DUPLICATE DISCREPANCY; ALL 8 FLAP ACTUATORS REPLACED. 2 L 7 2 4F RT A21EA 2001122800004 20011228 00004 EA 2001 12 28 COMA0160986 1 20011226 A 3020 300013000002 VALVE CNDAIR CL600 CL6002B19 1900309 EA R/H MALFUNCTIONED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 SO 01 984CA 1405 7171 FLIGHT 5791 R/H ENGINE COWL ANTI ICE CAUTION MESSAGE.REPLACED THE COWL ANTI ICE VALVE 2 L 7 2 4F RT A21EA 2002010700050 20020107 00050 EA 2002 1 7 COMA0160985 1 20011225 A 3350 59465 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 819CA 7415 FLIGHT 5602 EMERGENCY FLOOR PATH LIGHTS, ROWS 2 THRU 5 ARE INOPERABLE. REPLACED FLOOR LIGHT STRIP. 2 L 7 2 4F RT A21EA 2001122800005 20011228 00005 NM 2001 12 28 SWAA013402 1 20011226 A 3350 07912 COVER BOEING 737 7373A4 1384585 NM CABIN FLOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 EEPLS TRACK COVER LOOSE AT ROW 2. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2001122800006 20011228 00006 NM 2001 12 28 SWAA013405 1 20011226 A 5210 507945178 SKIN BOEING 737 7373H4 1384600 NM L1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR EXTERNAL SKIN CRACKED ON AFT EDGE, 8 INCHES FROM TOP. REPAIRED SKIN P ER SWA RA. 2 L 7 2 4F RT A16WE 2001122800007 20011228 00007 NM 2001 12 28 SWAA013406 1 20011226 A 5320 65C27314 STRINGER CLIP BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED D CHECK, FOUND 2 EA STRINGER CLIPS CRACKED, BS 663, STRINGERS 10L AND 10R. REMOVED AND REPLACED STRING ER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2001122800008 20011228 00008 NM 2001 12 28 SWAA013408 1 20011226 A 5320 65C27314 CLIP BOEING 737 7373T5 1384608 NM AFT FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED, BS 1104, STRINGER 15R. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 2001122800009 20011228 00009 EU 2001 12 28 MALA010799 1 20011219 A 2910 HYDRAULIC LINE BAC 146 AVRO146RJ85A 1500097 EU BROKEN A MALA K NONE K FLUID LOSS CR CRUISE 1 GL 15 516XJ E2334 During Flight #3612 Green System quantity went to zero inflight. Maintenance removed and replaced broken green system H ydraulic line. Ref 409 #101304 and following continuations cards for details. From Log Sheet 1052199 due to discrepancy on Log page 1052197 Dis 1 Maintenance requests a Test F;light to operate all Hydraulic components under "Load" Test Flig ht satisfactory performed walkaround check, no discrepancies noted. 2 H 7 4 4F RT A49EU 2001122800010 20011228 00010 NM 2001 12 28 01FDEA01109 1 20011227 A 5754 RIB BOEING 727 727277 138408S NM L/E SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 NR 3 SLAT INBD RIB CRACKED. R&R RIB PER SRM 57-50-3. 2 L 7 3 4F RT A3WE 2001122800011 20011228 00011 NM 2001 12 28 01FDEA01110 1 20011227 A 5754 RIB BOEING 727 727277 138408S NM RIGHT WING CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 N 241 #7 SLAT OUTBD RIB CRACKED. R&R RIB PER SRM 57-50-3. 2 L 7 3 4F RT A3WE 2001122800012 20011228 00012 SO 2001 12 28 C2XA01TY208 1 20011228 A 5344 PE64042H4016 BUSHING EMB 135 EMB135LR 3260305 SO A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 TYS DURING A SCHEDULED 1-C INSPECTION,THE BOTTOM BUSHING ON THE PAX-DOOR HOLD OPEN ROD WAS FOUND TO BE MIGRATING. MAINTE NANCE R/R THE BUSHING IAW GST-1682/01. THE GST STATED THAT THE BUSHION TO BE INSTALL FROM THE BOTTOM WITH A CORROSION IN HIBITOR AND SEAL THE GAP WITH PR1440 B2. ALL THIS WAS ACCOMPLISH AND WILL BE REL. UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT TOOO11AT 2001122800013 20011228 00013 SO 2001 12 28 C2XA01TY210 1 20011228 A 5321 14522461003 DOUBLER EMB 135 EMB135LR 3260305 SO A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 TYS DURING A SCHEDULED 1-C INSPECTION CORROSION WAS FOUND ON DOUBLER AT FRM. 20 ON THE RIGHT SIDE.MAINTENANCE REMOVED TH E CORROSION IAW 135/145 CPM 51-14-02 APPLIED ALLODINE ,PRIME AND PAINTED IAW EMB. 135/145 CPM 51-21-04,05,06. THE WORK W AS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF 1-C INSPECTION. 2 L 7 2 4F RT TOOO11AT 2001122800014 20011228 00014 EU 2001 12 28 C2XA01IA425 1 20011227 A 3350 LP1670 LAMP AEROSP ATR42 ATR42320 8680930 EU CABIN BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16824 166 IAH- DURING POST FLIGHT INSPECTION THE CREW NOTED THAT THREE AISLE PATH LIGHT BULBS WERE BURNED OUT. IAH- MAINTENANCE REMOVED AND REPLACED THE BURNED OUT AISLE PATH LIGHT BULBS, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYS TEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001122900001 20011229 00001 SO 2001 12 29 C2XA01TY215 1 20011229 A 3241 EMB NA EMB 135 EMB135LR 3260305 SO A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 788 145303 TYS DURING A SCHEDULED 1-C INSPECTION THE EMERG./PARKING BRAKE SYSTEM FAIL A OPS. CHECK. MAINTENANCE R/R THE #2 BRAKE CO NTROL VALVE AND PERFORMED A LEAK AND OPS. CHECK.ALL WORK WAS ACCOMPLISHED IAW EMB 135 AMM 32-41-06 AND WILL BE REL. UPON COMPLETION OF THE C-CHECK INSPECTION. 2 L 7 2 4F RT TOOO11AT 2001123100001 20011231 00001 SO 2001 12 31 C2XA01TY221 1 20011230 A 3500 214C0183 SWITCH EMB 135 EMB135LR 3260305 SO FAULTY A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 3057 3057 145303 TYS, During a scheduled 1C inspection, the oxygen deployement on step 13 of task card #35-20-00-770-001-A00 failed. Main tenance removed and replaced the altitude sensing switch. IAW-EMB-135-AMM-35-20-02, operational checked good. Aircraft w ill be released upon complection of the inspection. 2 L 7 2 4F RT TOOO11AT 2001123100002 20011231 00002 WP 2001 12 31 0104869864 1 20011205 A 5320 FLOOR SUPPORT DOUG DC9 DC951 3022051 WP FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 773NC 47775 DURING MCK AT ATL, CORROSION WAS FOUND ON THE CENTER LINE FLOOR SUPPORT CAP BETWEEN STATIONS 237 AND 294. REPAIRED PER E A 98-185352. 2 L 7 2 4F RT A6WE 2001123100004 20011231 00004 NM 2001 12 31 0104905520 1 20011211 A 2782 5006398E ACTUATOR BOEING 757 757251 1384970 NM L/E SLAT FAILED A NWAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 01 520US 38486 38486 23208 DURING APPROACH, UPON SELECTION OF FLAPS 1, THE LEADING EDGE SLAT DISAGREE WARNING LIGHT ILLUMINATED. AN EMERGENCY WAS DECLARED, THE FLIGHT CONTINUED THE APPROACH, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 20 LEADING EDGE A CTUATOR. SUBSEQUENT SYSTEM TESTS WERE SATISFACTORY. 2 L 7 2 4F RT A2NM 2001123100005 20011231 00005 WP 2001 12 31 0126 2 20011218 A 7260 CHIP DETECTOR CESSNA 650 650 2076802 CE GARRTT TFE731 TFE731* 01518 WP RT ENGINE FAULTY E DJFA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 EA 23 311CW 6500011 DURING DESCENT RT ENGINE CHIP DETECTOR LIGHT ILLUMINATED AND THEN WENT OFF. DESCENDING THE LIGHT CAME BACK ON AND STAYE D ON. THE PILOTS SHUTDOWN THE RT ENGINE AND DECLARED AN EMERGENCY WITH ATC. LANDED WITH NO FURTHER PROBLEMS. FURTHER INSPECTION OF THE ENGINE AND CHIP DETECTOR, MAINTENANCE FOUND NO PROBLEMS. MAINTENANCE TOOK AN OIL SAMPLE AND SHIPPED I T OUT FOR ANALYSIS AND IT CAME BACK OK. 2 L 7 2 4F 4 F A9NM E6WE 2001123100008 20011231 00008 NM 2001 12 31 01FDEA01090 1 20011220 A 5210 ROLLER BOEING 727 727100 1384036 NM ENTRY DOOR OUT OF POSITION A FDEA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SO 25 186 18872 CLIMBOUT UNABLE TO PRESSURIZE - TRIED MANUALLY TO PRESSURIZE, NO HELP. ALL DOOR LIGHT INDICATIONS NORMAL. UPON ARRIVAL IN RST MAIN ENTRY DOOR UPPER AFT GUIDE ROLLER OUT OF GUIDE, CAUSING DOOR TO NOT PROPERLY SEAT. OPENED/CLOSED DOOR FROM INSIDE/OUTSIDE SEVERAL TIMES WITH NO FURTHER DEFECTS NOTED. PERFORMED PRESS CK OF A/C PER JRH 7-13. A/C PRESS NORMALL Y. A/C OK FOR SERVICE. 2 L 7 3 4F RT A3WE 2001123100009 20011231 00009 NM 2001 12 31 01FEDA01083 1 20011218 A 5320 SEAL BOEING 727 727277 138408S NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241 20979 DITCHING SEAL CRACKED BS 1183 LBL 19 WL 208. INSTALLED FIBERGLASS REPAIR IAW FEDEX SRM 51-40-8. 2 L 7 3 4F RT A3WE 2001123100010 20011231 00010 NM 2001 12 31 ABXA010628 1 20011031 A 5414 SKIN BOEING 767 767281 1385109 NM NR 1 STRUT GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 791AX 23141 ENGINE NR 1 STRUT, RIGHT SKIN PANEL OUTER SURFACE, DEEP GOUGE WITH SKIN PUNCTURE WAS FOUND NEAR AN ACCESS DOOR CUT OUT, STA 237, WL 135. FABRICATED REPAIR PARTS AND INSTALLED IAW REA B654-42153MR. 2 L 7 2 4F RT A1NM 2001123100011 20011231 00011 NM 2001 12 31 ABXA010630 1 20011031 A 5330 SKIN BOEING 767 767281 1385109 NM FUSELAGE DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 791AX 23141 DAMAGED AREA NEAR AN EXISTING FASTENER HOLE AT STATION 435, BETWEEN STR 13 LEFT TO STR 14 LEFT, LEFT SIDE ON OUTER SKIN. REPAIRED AREA IAW REA B653-41430MR. 2 L 7 2 4F RT A1NM 2001123100012 20011231 00012 NM 2001 12 31 ABXA010631 1 20011003 A 5313 140T01522 STRINGER BOEING 767 767281 1385109 NM FUSELAGE DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 791AX 23141 AFTER REMOVAL OF 140T015-22 SPLICE FITTING, STRINGER 34 RIGHT AT STATION 434, DAMAGE WAS FOUND ON TWO ENDS OF STRINGER 3 4 RIGHT. FABRICATED NEW PART AND REPAIRED AREA IAW REA B653-41910MR. 2 L 7 2 4F RT A1NM 2001123100013 20011231 00013 NM 2001 12 31 ABXA010632 1 20010821 A 5313 STRINGER BOEING 767 767281 1385109 NM FUSELAGE DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 791AX 23141 ONE ELONGATED HOLE WAS FOUND AT STATION 434, STRINGER 9, LEFT SIDE ON STRINGER, LOWER SIDE. FABRICATED REPAIR PART AND REPAIRED AREA IAW REA B653-41421MR. 2 L 7 2 4F RT A1NM 2001123100014 20011231 00014 NM 2001 12 31 ABXA010634 1 20011030 A 5330 SKIN BOEING 767 767281 1385109 NM FUSELAGE DENTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 791AX 23141 DENT WAS FOUND ON FUSELAGE SKIN BETWEEN STATION 1373 TO STATION 1395 AND BETWEEN STRINGER 25 LEFT TO STRINGER 26 LEFT AT LONGITUDINAL LAP SPLICE, LEFT SIDE. REPAIRED AREA IAW REA B653-41399MR. 2 L 7 2 4F RT A1NM 2001123100015 20011231 00015 NM 2001 12 31 ABXA010638 1 20011008 A 5320 143T500080 CHANNEL BOEING 767 767281 1385109 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 791AX 23141 FORWARD CARGO LOWER LOBE BETWEEN STATION 610 AND STATION 632, LEFT BUTT LINE 6.5, CORRODED FLOOR CHANNEL, P/N 143T5000-8 0, LEFT SIDE. FABRICATED NEW PART AND REPAIRED AREA IAW REA B653-41896MR. 2 L 7 2 4F RT A1NM 2001123100016 20011231 00016 NM 2001 12 31 ABXA010639 1 20010821 A 5311 143T105229 FRAME BOEING 767 767281 1385109 NM FUSELAGE DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 791AX 23141 THREE OVAL HOLES WERE FOUND IN THE 143T1052-29 FRAME AND IN THE EXISTING ANGLE AT THE AFT SIDE OF FRAME, AT STATION 456, BETWEEN STRINGER 7 RIGHT AND STRINGER 8 RIGHT. FABRICATED NEW PART AND REPAIRED AREA IAW REA B653-41426DE. 2 L 7 2 4F RT A1NM 2001123100017 20011231 00017 NM 2001 12 31 ABXA010640 1 20011001 A 5730 SKIN BOEING 767 767281 1385109 NM RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 791AX 23141 UPPER LINK PITCH FITTING REWORK. UPPER WING SKIN CRACKS, RIGHT WING. REPAIRED AREA IAW REA B657-41905MR. 2 L 7 2 4F RT A1NM 2001123100018 20011231 00018 NM 2001 12 31 ABXA010641 1 20011022 A 5414 313T12003 SKIN BOEING 767 767281 1385109 NM NR 1 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 791AX 23141 GOUGE AND CRACK ON P/N 313T1200-3 FAIRING SKIN PYLON NR 1 RIGHT SIDE. FABRICATED REPAIR PARTS AND REPAIRED AREA IAW REA B654-42136MR. 2 L 7 2 4F RT A1NM 2001123100019 20011231 00019 NM 2001 12 31 ABXA010647 1 20010806 A 5230 146T63341 SKIN BOEING 767 767281 1385109 NM CARGO DOOR GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 791AX 23141 A GOUGE WAS FOUND IN THE 146T6334-1 INNER SKIN, NEAR STATION 1439, WATER LINE 131, LOWER SIDE ON BULK CARGO DOOR INNER S KIN. REPAIRED THE AREA IAW REA B652-41387MR. 2 L 7 2 4F RT A1NM 2001123100021 20011231 00021 NE 2001 12 31 ARWA20011206 2 20011212 A 7200 JT3D7 ENGINE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 4 FAILED A ARWA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 19 661AV 65599 578 45969 670990 APPROX 200 MILES OUT OF BAHRAIN AT FL 330 NR 4 ENGINE COMPRESSOR STALLED IN CLEAR WEATHER, FOLLOWED BY DROP IN EPR FROM 1.65 TO 1.15. ALL OTHER PARAMETERS NORMAL, ABOVE 85 PERCENT N2 ENGINE SURGES. AIRCRAFT LANDED WITHOUT INCIDENTS. POST FLIGHT INSPECTION REVEALED PARTICLES OF METAL LAYING IN THE BOTTOM OF NR 4 ENGINE TAILPIPE. AIRCRAFT PREPARED FOR THRE E ENGINE FERRY. REMOVED AND REPLACED NR 4 ENGINE IAW ARROW AIR J/C 6519 & 6522 ENGINE RUN SATISFACTORY. AIRCRAFT RETURNE D TO SERVICE. 2 L 7 4 4F 4 F 4A25 1E8 2001123100022 20011231 00022 WP 2001 12 31 ARWA20011207 1 20011213 A 2780 BRAKE LKHEED 1011 1011385115 5265015 WP L/E SLAT MALFUNCTIONED A ARWA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 19 308GB 193U1133 DURING FLAP EXTENSION NO SLAT INDICATION ON FLIGHT ENGINEER PANEL. AIRCRAFT RETURNED TO BLOCKS. RESET L/E SLAT ASYMMET RY BRAKES AND ACCOMPLISHED ALL REQUIRED TEST. L/E SLAT TESTED GOOD PER MM 27-81-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A23WE 2001123100023 20011231 00023 WP 2001 12 31 ARWA20011208 1 20011215 A 3241 42421 CONTROL BOX DOUG DC8 DC863F 302198F WP ANTI- SKID SYS FAULTY A ARWA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 19 441J 45988 ON TAKEOFF ROLL ANTI-SKID LIGHT ILLUMINATED ON SKID CONTROL MONITOR, RF2 AND LF1 LIGHTS WERE ON. ABORTED TAKEOFF AT 65 KNOTS. AIRCRAFT RETURNED TO BLOCKS. REMOVED AND REPLACED ANTI-SKID CONTROL BOX IAW 32-43-6. OPS CHECK NORMAL IAW MM 3 2-43-0. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2001123100026 20011231 00026 NM 2001 12 31 AWXA200100643 1 20011216 A 2131 21173886 CONTROLLER BOEING 757 757225 1384959 NM CABIN PRESSURE FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 915AW 46040 6592 22209 PHX - AIR TURNBACK - AFTER TAKEOFF FROM PHX EN ROUTE TO CMH THE FLIGHT CREW RECEIVED EICAS MESSAGE FOR CABIN AUTO PRESSU RE INOPERATIVE WITH CABIN 1 AND 2 DISPLAYED; THE AUTO INOPERATIVE LIGHT ILLUMINATED AND CABIN WAS UNABLE TO PRESSURIZE. AIRCRAFT TURNED BACK TO PHX AND MADE AN UNEVENTFUL LANDING. MAINTENANCE TROUBLESHOT THE PROBLEM AND REMOVED AND REPLAC ED THE CABIN PRESSURE CONTROLLER AND THE OUT FLOW VALVE IAW BMM 21-31-03, PG 201-206, AND BMM 21-31-02, PG 401-404. BOT H REPLACED PARTS OPERATIONALLY CHECKED GOOD. 2 L 7 2 4F RT A2NM 2001123100027 20011231 00027 NM 2001 12 31 AWXA200100646 1 20011206 A 5320 655287846 FLOOR SUPPORT BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - C - DURING C-15 CHECK MAINTENANCE FOUND CORROSION ON UPPER SURFACE OF CABIN FLOOR INNER CHORD BS 99 3 TO BS 997, WL 207, LBL 45. MAINTENANCE REMOVED AND REPLACED INNER CHORD AT LBL 45, BS 912 TO BS 1006 IAW 737-300 SRM 51-40-02 PG 2, 3, & 10. 2 L 7 2 4F RT A16WE 2001123100028 20011231 00028 NM 2001 12 31 AWXA200100648 1 20011216 A 5315 65C3453721 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - C - DURING C-15 CHECK MAINTENANCE FOUND A CRACK IN THE LIGHTENING HOLE ON THE UPPER CHORD OF LONGIT UDINAL FLOORBEAM BS 664, LBL 25. MAINTENANCE STOP DRILLED CRACK AND PERFORMED HFEC INSPECTION TO VERIFY CRACK DID NOT P ROCEED THROUGH HOLE, INSTALLED REPAIR CHANNEL AT UPPER CHORD BS 664, LBL 25 IAW AWA ER 03-5715-01349-ES2. 2 L 7 2 4F RT A16WE 2001123100029 20011231 00029 EU 2001 12 31 AWXA200100649 1 20011214 A 5347 D53112092206 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 82 YWG - MAJOR REPAIR - C - DURING C-02 CHECK MAINTENANCE FOUND CORROSION AT NR 4 SEAT TRACK BS FRAME 20, RBL 765. REMOVED , FABRICATED AND INSTALLED 8 INCH SECTION OF TRACK 4 INCHES FORWARD TO 4 INCHES AFT OF FRAME 20, RBL 765 IAW SRM 53-00-1 5, FIG 201, PG 202-206. 2 L 7 2 4F RT A28NM 2001123100030 20011231 00030 EU 2001 12 31 AWXA200100650 1 20011214 A 5347 D53112092206 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 82 YWG - MAJOR REPAIR - C - DURING C-02 CHECK MAINTENANCE FOUND CORROSION AT NR 3 SEAT TRACK BS FRAME 20, RBL 1292. MAINTE NANCE REMOVED, FABRICATED AND INSTALLED 8 INCH SECTION OF TRACK 4 INCHES FORWARD TO 4 INCHES AFT OF FRAME 20, RBL 1292, IAW SRM 53-00-15, FIG 201, PG 202-206. 2 L 7 2 4F RT A28NM 2001123100031 20011231 00031 EU 2001 12 31 AWXA200100653 1 20011218 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN FAULTY A AWXA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 28 644AW 13527 5412 317 PHX - EEL - C - FLIGHT ATTENDANT PANEL INDICATED EMERGENCY LIGHT POWER SUPPLY FAULT LT FWD (10WL). MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY 10WL IAW AMM 33-51-38-000-001, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2001123100032 20011231 00032 NM 2001 12 31 AWXA200100654 1 20011219 A 3350 321430 BATTERY AIRBUS A319 A319132 3930340 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 812AW 1178 LAX - EEL - C - EMERGENCY LIGHTS AT OVERWING EXITS INOP 11WL AND 12WL. MAINTENANCE REMOVED AND REPLACED BATTERIES AT PO WER SUPPLIES 11WL AND 12WL IAW T/C R1C3301. 2 L 7 2 4F RT A28NM 2001123100033 20011231 00033 NM 2001 12 31 C1HA200184016 1 20011020 A 7932 TRANSMITTER BOEING 727 7272S7 138407Z NM NR 3 ENGINE FAULTY A C1HA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 15 684CA 22491 DURING INITIAL TAKEOFF ROLL, ALL OIL QUANTITY INDICATIONS WERE NORMAL AT 1.4 EPR. AS THROTTLES WERE ADVANCED TO FLEX TA KEOFF POWER, THE OIL QUANTITY ON ENGINE NR 3 DECREASED TO 1/2 GALLON INDICATION. ABORTED TAKEOFF AT 90 KNOTS AND RETURN ED TO GATE. REMOVED AND REPLACED NR 3 ENGINE OIL QUANTITY TRANSMITTER PER MM 79-31-01, OPS AND LEAK CHECK GOOD. 2 L 7 3 4F A3WE 2001123100034 20011231 00034 NM 2001 12 31 C1HA200195019 1 20011012 A 2750 FLAP BOEING 727 727290 138408W NM RT WING OUT OF ADJ A C1HA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 GL 15 295AS 22147 FLIGHT LEVEL 290 AND SPEED 80 MACH THE AIRCRAFT VIBRATED MODERATELY. REDUCED SPEED AND RAISED SPEED BRAKES APPROX 5 DEG REES, THE VIBRATION STOPPED. LOWERED SPEEDBRAKE AND 5 MINUTES LATER THE VIBRATION RETURNED. THE ONBOARD MECHANIC NOTED THE OUTBOARD SECTION OF FLAP ON A/C RT SIDE WAS VIBRATING. PERFORMED OUTBOARD AFT FLAP ADJUSTMENT IAW MM 27-51-12. 2 L 7 3 4F A3WE 2001123100035 20011231 00035 NM 2001 12 31 CALA0101032 1 20011218 A 5314 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 60312 23363 INSPECTION FOUND LT WHEEL KEEL BEAM O/B LOWER CHORD CORRODED AT STA 715-724. THE KEEL BEAM WAS REPAIRED IAW ECRA 5310-0 3740. 2 L 7 2 4F RT A16WE 2001123100038 20011231 00038 NM 2001 12 31 DLM11011910 1 20011208 A 7920 70R943 SEAL DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 2 ENGINE LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 809DE 48480 723911 NR 2 ENG APPEARS LOSING OIL. REPLACED HYDRAULIC PUMP FOR LEAKING. 2 L 7 3 4F 4 F RT A22WE E24NE 2001123100039 20011231 00039 2001 12 31 DLM88011913 4 20011209 A 2565 D29982125 PIN DOUG MD88 MD88 3023688 NM EVAC SLIDE PULLED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 933DL 49720 L1 DOOR SLIDE CABLE PINS PULLED. REPLACED SLIDE. 2 L 7 2 4F RT A6WE 2001123100040 20011231 00040 NM 2001 12 31 DLM88011919 1 20011210 A 3397 WIRE DOUG MD88 MD88 3023688 NM CABIN SHORTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 926DL 49713 ON L/O, FOUND AFT EMERGENCY LIGHTS INOP. FOUND AFT POWER SUPPLY FUSE BLOWN. REMOVED AND REPLACED SUPPLY AND BATTERY. STILL NO HELP. FOUND WIRE SHORTED AT SEAT 30E. REPAIRED SAME. REMOVED AND REPLACED POWER SUPPLY. NOW TESTS OK. 2 L 7 2 4F RT A6WE 2001123100041 20011231 00041 NM 2001 12 31 DLM90011906 1 20011208 A 5753 99359405 SKIN DOUG MD90 MD9030 3023690 NM T/E FLAP DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 THE LEFT INBOARD FLAP, INBOARD AFT REMOVABLE WEDGE LOWER SKIN WAS FOUND DENTED. REPAIR PER ER/A 410735-14. 2 L 7 2 4F RT A6WE 2001123100045 20011231 00045 NE 2001 12 31 GLBA2001233 3 20011124 A 6140 1293640919 PRINTED CKT BOAR BEECH 1900 1900D 1154162 CE HARTZL HCE4A HCE4A3A NE PROP INDICATING FAULTY A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 240GL UE240 LEFT AUTO FEATHER ANNUNCIATOR EXTINGUISHED IN FLIGHT. REPLACED PCB, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 5 C P10NE 2001123100046 20011231 00046 CE 2001 12 31 GLBA2001235 1 20011128 A 2750 SWITCH BEECH 1900 1900D 1154162 CE T/E FLAP OUT OF ADJ A GLBA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 03 220GL UE220 FLAPS WOULD NOT RETRACT ON T/O. ADJUST S255 SWITCH, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001123100047 20011231 00047 CE 2001 12 31 GLBA2001236 1 20011206 A 3610 1299700321 LINE BEECH 1900 1900D 1154162 CE BLEED AIR CRACKED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 204GL UE204 RIGHT BLEED AIR FAIL INFLIGHT. REPAIRED EVA TUBING AND REPLACED INSTRUMENT LINE. 2 L 7 2 4T RT A24CE 2001123100048 20011231 00048 2001 12 31 GLBA2001237 4 20011206 A 3425 FLIGHT DIR BEECH 1900 1900D 1154162 CE COCKPIT LOOSE A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 03 169GL UE169 FLIGHT DIRECTOR CAME LOOSE FROM PANEL. RESECURED, RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 2001123100050 20011231 00050 CE 2001 12 31 GLBA2001239 1 20011211 A 5210 SEAL BEECH 1900 1900D 1154162 CE DOOR OUT OF ADJ A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 204GL UE204 CABIN DEPRESSURIZED ON CLIMB. RE-INSTALLED DOOR SEAL IN TRACK, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2001123100051 20011231 00051 NE 2001 12 31 GLBA2001240 3 20011211 A 6140 WARNING SYSTEM BEECH 1900 1900D 1154162 CE HARTZL HCE4A HCE4A3A NE COCKPIT MALFUNCTIONED A GLBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 03 192GL UE192 AUTO FEATHER DISABLE LIGHT STAYED ILLUMINATED ON ROLL AFTER POWER WAS APPLIED. PERFORMED OPS CHECK OF AFX SYSTEM, COULD NOT DUPLICATE. 2 L 7 2 4T RT A24CE 5 C P10NE 2001123100052 20011231 00052 NM 2001 12 31 HNAA0100079 1 20011207 A 2910 HYDRAULIC SYSTEM DHAV DHC8 DHC8102 2809003 NM NR 1 MALFUNCTIONED A HNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 07 982HA 380 LOST NR 1 HYDRAULIC SYSTEM PRESSURE WITH NR 2 ENGINE RUNNING DURING SINGLE ENGINE TAXI. NO NORMAL BRAKING. I/B ROLL SP LR, RUD HYD AND RUD FULL PRESS CAUTION LIGHTS ILLUMINATED. NORMAL BRAKING RETURNED DURING RETURN TAXI TO GATE. MAINTEN ANCE COULD NOT DUPLICATE DISCREPANCY. CYCLED NR 1 STANDBY PUMP CIRCUIT BREAKER AND CLEANED ASSOCIATED CONNECTORS AS A P RECAUTION. 2 H 7 2 4T RT A13NM 2001123100053 20011231 00053 WP 2001 12 31 IJLA20011106 2 20011106 A 7261 MS217904 BOLT LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP RT ENGINE BACKED OUT E IJLA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 19 351TX 760 127 P74456 NR 2 ENGINE OIL LOSS AND OIL PRESSURE LOSS. BOLT THAT HOLDS KEEPER FOR OIL TUBE TO OIL COOLER BACKED OUT AND ALLOWED OI L TO LEAK. ENGINE WAS SHUT DOWN IN CRUISE FLIGHT AND LANDED AS SOON AS PRACTICAL. BOLT HAS NO SAFETY OR SELF LOCKING D EVICE. REPAIRED AND REINSTALLED NEW HARDWARE USING LOCTITE. NO ENGINE DAMAGE OCCURRED DUE TO PILOT SHUTTING DOWN ENGIN E. 2 L 7 2 4F 4 F A10CE E6WE 2001123100054 20011231 00054 NE 2001 12 31 IXXA0100076O 2 20011212 A 7200 CFM562C1 ENGINE DOUG DC8 DC871 302199A WP GE CFM56 CFM562C1 13802 NE NR 1 LEAKING A IXXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 11 829BX 11371 45994 692325 EN ROUTE FROM JFK TO BDL. WHEN LEFT AIR CONDITION PACK WAS TURNED ON SMOKE WAS EMITTING FROM THE VENTS. THE FLIGHT CRE W SECURED THE PACK AND THE SMOKE SUBSIDED. THE FLIGHT CREW THEN NOTICE A DECLINE IN THE NUMBER ONE ENGINE OIL QUANTITY AND OIL PRESSURE REMAINED NORMAL. THE FLIGHT CONTINUED TO BDL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED AIRCRAF T WHICH REVEALED THE NUMBER ONE ENGINE WAS LOW ON OIL. MAINTENANCE SUSPECTS DISCREPANCIES ASSOCIATED WITH THE NR 3 STA TIONARY AFT AIR/OIL SEAL. THE ENGINE WAS REPLACED AND NO DISCREPANCIES WERE NOTED WITH THE LEFT AIR CONDITIONING SYSTEM . THE AIRCRAFT WAS RETURNED TO SERVICE. ADDITIONAL INFORMATION WILL FOLLOW WHEN MADE AVAILABLE. 2 L 7 4 4F 4 F 4A25 E2GL 2001123100056 20011231 00056 EU 2001 12 31 MALA010781 1 20011126 A 3020 24668165 BOOT SAAB SF340 340B 7860101 EU RT INTAKE BURNED A MALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 GL 15 413XJ 340B413 DURING FLIGHT 2896 CREW NOTICED SUDDEN BURNING SMOKE SMELL INFLIGHT. FA IMMEDIATELY REPORTED SMELL. FA CHECKED BINS AN D BATHROOM FOR SMELL AND WARM SURFACES. NO WARM SURFACES NOTED. SMELL CONTINUED TILL LANDING (RT INTAKE COME ON SHORTLY AFTER) COULD NOT RESET. AIR RETURN TO BJI WITHOUT INCIDENT. MAINTENANCE INSPECTED AC AND FOUND NO OTHER DEFECTS BESID ES THE RT DAMAGED FWD INLET. RAN AC AND SYSTEM AND DETERMINED THE ODOR TO BE FROM THE RT INLET OPERATED THE BLEED SYSTE M. CONTRACT MAINTENANCE INSPECTED INTAKE AND FOUND INTAKE HEAT MAT BURNT UP. MAINTENANCE REPLACED RT FWD INLET DUCT P/ N 24668-165, S/N OFF L291142, S/N ON L198073. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2001123100057 20011231 00057 EU 2001 12 31 MALA010782 1 20011122 A 5220 WIRE SAAB SF340 340B 7860101 EU EMERGENCY EXIT BROKEN A MALA K NONE O OTHER NR NOT REPORTED 1 GL 15 420XJ 340B420 DURING FLIGHT 2888, EMERGENCY EXIT COVER ON THE RT FWD DOOR HAS SAFETY WIRE BROKEN. MAINTENANCE REINSTALLED COVER AS NE EDED, AND SAFETIED AS REQUIRED, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2001123100058 20011231 00058 EU 2001 12 31 MALA010784 1 20011127 A 2421 31342003 GENERATOR SAAB SF340 340B 7860101 EU LT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 452XJ 340B452 DURING FLIGHT 2978 IN MSP. LEFT AC GEN FAILED DURING CLIMB. AIR TURNBACK TO MSP. MAINTENANCE REMOVED AND REPLACED LT AC GEN P/N 31342-003, S/N ON 98029, S/N OFF 286. 2 L 7 2 4T RT A52EU 2001123100059 20011231 00059 EU 2001 12 31 MALA010785 1 20011128 A 2434 23080031 GENERATOR SAAB SF340 SF340A 7850100 EU RT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 99XJ 340A099 DURING FLIGHT NR 3020 AC DID AN AIR RETURN FOR THE RIGHT DC GEN FAILING. WEATHER WAS BAD AT DESTINATION (YWG) SO CREW H AD AC TURN AROUND. AIR RETURN TO MSP. MAINTENANCE REPLACED THE RT DC GENERATOR P/N 23080-031, S/N OFF 96289, S/N ON 96 449. 2 L 7 2 4T RT A52EU 2001123100060 20011231 00060 EU 2001 12 31 MALA010787 1 20011118 A 5753 SPAR SAAB SF340 SF340A 7850100 EU T/E FLAP CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 31XJ 340A031 DURING 4K-CHECK IN CWA, LT FLAP REAR SPAR CRACKED AT WS 142.06. COMPLETED REPAIR OF REAR SPAR IAW EO 57007. 2 L 7 2 4T RT A52EU 2001123100061 20011231 00061 EU 2001 12 31 MALA010788 1 20011128 A 5330 SKIN SAAB SF340 SF340A 7850100 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 31XJ 340A031 DURING 4K-CHECK IN CWA, MAINTENANCE NOTICED A DENT IN FUSELAGE SKIN AT STA 356.0 BETWEEN STRINGERS L168 AND L1622 RT. MAINTENANCE REPAIRED IAW EO 53110. 2 L 7 2 4T RT A52EU 2001123100062 20011231 00062 EU 2001 12 31 MALA010789 1 20011204 A 2730 CONNECTOR SAAB SF340 SF340A 7850100 EU ELEVATOR SYS CONTAMINATED A MALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 15 41XJ 340A041 ON FLIGHT 2773, IN-FLIGHT AUTO PILOT ON, SHARP PITCH DOWN FORCE, MANUALLY DISCONNECTED. PHYSICAL FORCE TO OPERATE PITCH AXIS MAIN PITCH TRIM INOP FROM LEFT AND RIGHT SEATS. STANDBY PITCH OK. AC LANDED WITHOUT INCIDENT. MAINTENANCE FOUND MOISTURE IN ACTUATOR CANNON PLUG, CLEANED AND RECONNECTED OPERATIONAL AND TIME CHECKS WERE NORMAL NO OTHER FAULTS NOTED . WRAPPED CANNON PLUG. WORK IAW SAAB AMM 27-32-10. 2 L 7 2 4T RT A52EU 2001123100063 20011231 00063 2001 12 31 MALA010790 4 20011205 A 3422 6225812001 FLUX DETECTOR SAAB SF340 SF340A 7850100 EU NR 2 FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 68XJ 340A068 DURING FLIGHT 3134, DUAL HEADING FAILURE INFLIGHT (COMPARATOR) AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED NR 2 FLUX DETECTOR UNIT P/N 622-5812-001 S/N ON 26179, S/N OFF 15446. NR 2 AHRS OP CHECKS GOOD IAW SF 340 MM CHAP 34.15446. 2 L 7 2 4T RT A52EU 2001123100064 20011231 00064 EU 2001 12 31 MALA010791 1 20011209 A 3260 SQUAT SWITCH SAAB SF340 340B 7860101 EU MLG DIRTY A MALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 15 438XJ 340B438 DURING FLIGHT 3338 CONFIG WARNING ILLUMINATED ON SHORT FINAL GEAR WAS 3 GREEN FLAPS AT 20 QRH CONSULTED. SECOND APPROAC H INITIATED AND WAS UNEVENTFUL. TRIMS WERE IN GREEN ARC'S. MAINTENANCE CLEANED AND INSPECTED ALL SQUAT SWITCHES ON MAI N GEAR. PERFORMED CONFIG WARNING TEST. ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2001123100065 20011231 00065 NE 2001 12 31 MALA010792 2 20011212 A 7510 VALVE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE LT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 110XJ 340A110 369 DURING FLIGHT 2868 LT AIR VALVE LIGHT ILLUMINATED. AIR RETURN TO DTW. WEATHER CONDITIONS WARRANT THE RETURN. MAINTENA NCE REMOVED AND REPLACED THE LT GARRET VALVE, (SWAPPED LEFT TO RIGHT AND PROBLEM FOLLOWED) IAW SAAB MM CH 75. OPS AND S ECURITY CHECK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2001123100066 20011231 00066 EU 2001 12 31 MALA010797 1 20011211 A 2760 POTENTIOMETER BAC 146 AVRO146RJ85A 1500097 EU SPEED BRAKES FAULTY A MALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 15 511XJ E2325 DURING FLIGHT 3477, AIRBRAKE DEPLOYED INFLIGHT. AIRCRAFT STOWED UP AND LIGHT ILLUMINATED. FROM START TO FINISH, ENTIRE EVENT WAS APPROXIMATELY 30 SECONDS. MAINTENANCE REPLACED FEEDBACK POTENTIOMETER S/N ON 01H06892 IAW 27-63-00. 2 H 7 4 4F RT A49EU 2001123100068 20011231 00068 EU 2001 12 31 MTNA200113 1 20011207 A 2612 D237060 WIRE FOKKER F27 F27MK500 4990629 EU LT ENGINE SHORTED A MTNA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 33 719FE 10467 IN FLIGHT FROM MEM TO SDF, THE LEFT ENGINE FIRE INDICATION ILLUMINATED. THE CREW DECLARED AN EMERGENCY AND RETURNED TO MEM. THE AIRCRAFT LANDED WITHOUT ANY OTHER PROBLEMS. MAINTENANCE FOUND TWO BAD FIRE WIRES. MAINTENANCE REMOVED AND RE PLACED TWO EACH FIRE WIRES. THE SYSTEM CHECKED GOOD IAW THE FOKKER MAINTENANCE MANUAL. 2 H 7 2 4T A817 2001123100069 20011231 00069 2001 12 31 MWEA001465 4 20011201 A 3420 1428300001 GYRO DOUG DC9 DC981 3022081 WP E/E BAY FAILED A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 807ME 48033 CAPTAIN'S RADIO MAGNETIC INDICATION FLAGGED ALONG WITH BOTH PRIMARY FLIGHT DIRECTORS SHOWING ATT FAIL AND FIRST OFFICER' S PRIMARY FLIGHT DIRECTOR SHOWED HEADING FAIL. REMOVED AND REPLACED CAPTAIN'S MULTI-FUNCTIONAL GYRO, OPERATION CHECK IS GOOD IN ACCORDANCE WITH MAINTENANCE MANUAL 34-23-01. 2 L 7 2 4F A6WE 2001123100070 20011231 00070 2001 12 31 MWEA011465 4 20011201 A 3420 1428300001 GYRO DOUG DC9 DC981 3022081 WP E/E BAY FAILED A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 807ME 48033 CAPTAIN'S RADIO MAGNETIC INDICATION FLAGGED ALONG WITH BOTH PRIMARY FLIGHT DIRECTORS SHOWING ATT FAIL AND FIRST OFFICER' S PRIMARY FLIGHT DIRECTOR SHOWED HEADING FAIL. REMOVED AND REPLACED CAPTAIN'S MULTI-FUNCTIONAL GYRO, OPERATION CHECK IS GOOD IN ACCORDANCE WITH MAINTENANCE MANUAL 34-23-01. 2 L 7 2 4F A6WE 2001123100071 20011231 00071 WP 2001 12 31 MWEA011466 1 20011203 A 5751 5910046502 SKIN DOUG DC9 DC915 3022036 WP LT AILERON CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 LEFT HAND AILERON HAS CORROSION ALONG LOWER SKIN AT TRAILING EDGE AT APPROXIMATELY STATION XA471. REMOVED DAMAGE. FABR ICATED AND INSTALLED REPAIR. 2 L 7 2 4F A6WE 2001123100072 20011231 00072 WP 2001 12 31 MWEA011467 1 20011203 A 5751 AILERON DOUG DC9 DC915 3022036 WP LT WING DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 REMOVED STATIC WICK AND DOUBLER TO FACILITATE OTHER MAINTENANCE FROM THE LEFT HAND AILERON AT APPROXIMATELY STATION XA47 1. FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 2001123100073 20011231 00073 WP 2001 12 31 MWEA011479 1 20011210 A 2424 976J2544 GCU DOUG DC9 DC932 3022066 WP E/E BAY FAILED A MWEA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 GL 31 401ME 47133 LOST LEFT HAND GENERATOR JUST AFTER TAKEOFF. NORMAL CROSSTIE RAN QRH, RESET GENERATOR, AGAIN LOST LEFT GENERATOR RAN QR H. LEFT HAND GCU HAD GENERATOR CONTROL FAULT LIGHT ON. REMOVED AND REPLACED LEFT HAND GCU. SYSTEMS OPS CHECK GOOD. 2 L 7 2 4F A6WE 2001123100074 20011231 00074 WP 2001 12 31 MWEA011481 1 20011212 A 5753 993593222 ATTACH ANGLE DOUG DC9 DC981 3022081 WP T/E FLAP CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 RIGHT HAND WING FLAP NOSE RIB INBOARD ATTACH ANGLE HAS MODERATE CORROSION PRESENT. THE NOSE RIB IS LOCATED JUST BELOW N R 1 AND NR 2 FIXED VANE SPLICE AREA. REMOVED NOSE RIB ATTACH ANGLE. DRILLED, FABRICATED AND INSTALLED TEE. INSTALLED NOSE RIB. 2 L 7 2 4F A6WE 2001123100075 20011231 00075 WP 2001 12 31 MWEA011482 1 20011212 A 5753 993593210 ATTACH ANGLE DOUG DC9 DC981 3022081 WP T/E FLAP CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 RIGHT HAND WING FLAP NR 8 RIB (COUNTING FROM INBOARD-OUTBOARD) THE LOWER INBOARD ATTACH ANGLE IS EXFOLIATED. REMOVED, F ABRICATED, DRILLED AND INSTALLED LOWER INBOARD ATTACH ANGLE. 2 L 7 2 4F A6WE 2001123100076 20011231 00076 WP 2001 12 31 MWEA011487 1 20011217 A 5313 51415997 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 KEEL AREA LONGERON 27 LEFT HAS A CHAFE AT STATION 655 AB5. REMOVED, DRILLED AND INSTALLED LONGERON. 2 L 7 2 4F A6WE 2001123100077 20011231 00077 NE 2001 12 31 NACA20010041 2 20011130 A 8500 R2800 ENGINE DOUG DC6 DC6B 3021712 WP PWA R2800 R2800* 52026 NE NR 4 ROUGH A NACA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 7919C 2486 1578 43554 33325 NR 4 ENGINE WILL NOT TAKE A LEAN (POSSIBLE LOW COMPRESSION ON THE NR 10, NR 16 CYLINDERS). REPLACED ENGINE, (DUE OVERHA UL). 2 L 7 4 4R 4 R 6A4 5E8 2001123100078 20011231 00078 NE 2001 12 31 NACA20010042 2 20011205 A 7321 PR58E5 CARBURETOR DOUG DC6 DC6 3021702 WP PWA R2800 R2800* 52026 NE NR 2 ENGINE DEFECTIVE A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 779TA 796 796 45529 P35317 NR 2 ENGINE SHUT DOWN DUE TO ERRATIC BMEP, ROUGH RUNNING, AND RAPID LOSS OF CHT. REPLACED NR 2 ENGINE CARBURETOR. 2 L 7 4 4R 4 R A781 5E8 2001123100079 20011231 00079 NM 2001 12 31 P2EA2001M0014 1 20011205 A 2410 CSD BOEING 737 73725A 1384481 NM NR 1 ENGINE MALFUNCTIONED A P2EA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 05 239TA 23789 NR 1 ENGINE CSD LOW OIL PRESSURE LIGHT WOULD NOT EXTINGUISH AFTER ENGINE START. AIRCRAFT RETURNED TO BLOCKS WITH NO INC IDENT. RESET NR 1 ENGINE CSD T-HANDLE. OPERATIONAL CHECK NORMAL IAW MM 24-11-11. 2 L 7 2 4F RT A16WE 2001123100081 20011231 00081 NE 2001 12 31 P2EA2001M0016 2 20011219 A 7200 ENGINE BOEING 737 737247 138448D NM PWA JT8 JT8D9A 52048 NE NR 2 MALFUNCTIONED A P2EA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 05 912MP 19607 ON SCHEDULED PUSHBACK FOR FLIGHT 400 PILOT REPORTED THAT NR 2 ENGINE WOULD NOT START. AIRCRAFT RETURNED TO GATE WITH NO INCIDENT. NR 2 ENGINE OPERATIONAL CHECKED IAW MM 71-09-100. 2 L 7 2 4F 4 F A16WE E2EA 2001123100082 20011231 00082 NE 2001 12 31 P2EA2001M0017 2 20011221 A 7530 658385 CONTROLLER BOEING 737 73725A 1384481 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE FAULTY A P2EA D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 CE 05 239TA 23789 709429 NR 2 ENGINE STALLED THREE TIMES DURING TAXI, ALSO NR 2 EPR STICKING. REMOVED AND REPLACED PRBC IAW MM 75-31-11. REMOVE D AND REPLACED EPR TRANSMITTER IAW 77-11-0. OPERATIONAL CHECKS NORMAL. 2 L 7 2 4F 4 F RT A16WE E2EA 2001123100083 20011231 00083 NM 2001 12 31 P2EA2001M0018 1 20011223 A 3350 LIGHT BOEING 737 7372Q8 138448K NM CABIN LOOSE A P2EA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 CE 05 121NJ 21735 DURING TAXI EMERGENCY EXIT LIGHT CENTER OF AIRCRAFT ON RIGHT LOOSE. RESECURED IAW MM 33-20. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A16WE 2001123100084 20011231 00084 NM 2001 12 31 P5CA0100620 1 20011215 A 5414 RETAINER BOEING 747 747249F 1384849 NM NR 1 PYLON TORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 NR 1 ENGINE PYLON SAILBOAT DOOR, INBOARD SIDE, LOWER FWD END, HAS A 6 INCH RIP IN SEAL RETAINER. REPAIRED PER SRM 51-40 -00. 2 L 7 4 4F A20WE 2001123100085 20011231 00085 NM 2001 12 31 P5CA0100621 1 20011215 A 5753 FLAP BOEING 747 747249F 1384849 NM LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEFT INBOARD T/E FLAP HAS 4 AREA OF SLIGHT DELAMINATION. REPAIRED PER SRM 20-11-14. 2 L 7 4 4F A20WE 2001123100086 20011231 00086 2001 12 31 PCAA0112164 4 20011203 A 3442 071131333 DISPLAY DHAV DHC8 DHC8102 2809003 NM COCKPIT MALFUNCTIONED A PCAA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 13 838EX 220 BWI-BUF FLIGHT 3900. CREW REPORTED SMOKE COMING FROM RADAR GRAPHICS UNIT. SMOKE SUBSIDED WHEN UNIT WAS TURNED OFF. AIR CRAFT DIVERTED TO MDT FOR REPAIRS. NO EMERGENCY DECLARED. MAINTENANCE REPLACED RADAR GRAPHICS UNIT IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001123100087 20011231 00087 NM 2001 12 31 PCAA0112165 1 20011203 A 3222 88255 LINK DHAV DHC8 DHC8102 2809003 NM NLG WORN A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 808EX 299 DURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY FOR WEAR, LOWER TRAILING ARM LINK AND LOWER PIN FOUND WORN. LINK ASSEMBLY AND LOWER PIN REPLACED IN ACCORDANCE WITH COMPONENT MAINTENANCE MANUAL 32-20-01. STRUT S ERVICED IN ACCORDANCE WITH DEHAVILLAND MAINTENANCE MANUAL 12-10-32, WHEELS INSTALLED IN ACCORDANCE WITH DEHAVILLAND MAIN TENANCE MANUAL 32-41-16. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001123100088 20011231 00088 NM 2001 12 31 PCAA0112166 1 20011204 A 3222 88255 LINK DHAV DHC8 DHC8102 2809003 NM NLG WORN A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 824EX 387 DURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY, FOUND WEAR IN TRAILING ARM LINK LOWER BUSHI NG AND LOWER PIN. LOWER TRAILING ARM PIN AND LOWER LINK BUSHING REPLACED. LINK ASSEMBLY GREASED. OPERATIONAL CHECK GO OD IN ACCORDANCE WITH DASH 8 MAINTENANCE MANUAL. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001123100089 20011231 00089 NM 2001 12 31 PCAA0112168 1 20011212 A 3222 88255 LINK DHAV DHC8 DHC8102 2809003 NM NLG WORN A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 845EX 344 DURING FLEET INSPECTION OF NOSE LANDING GEAR FOR WEAR IN THE TRAILING ARM LINK ASSEMBLY, FOUND TRAILING ARM LINK LOWER B USHING AND PIN WORN. TRAILING ARM LINK AND PIN REPLACED IN ACCORDANCE WITH COMPONENT MAINTENANCE MANUAL 32-20-01. SHOC K STRUT SERVICED, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001123100090 20011231 00090 NM 2001 12 31 HNAA0100081 1 20011229 A 2910 HYDRAULIC LINE DHAV DHC8 DHC8201 2809001 NM A HNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 07 985HA 479 Number two engine hydraulic pump caution light illuminated, followed with loss of number two system hydraulic fluid. In stalled temporary flex line on number 2 hydraulic pressure manifold. No bypass indicators popped and no particals found in case drain filter. Engine driven pump ran less than 15 minutes. 2 H 7 2 4T RT A13NM 2001123100091 20011231 00091 NM 2001 12 31 PCAA0112169 1 20011213 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN DAMAGED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 847EX 333 DURING ROUTINE MAINTENANCE VISIT 2 EMERGENCY PATHWAY LIGHTS FOUND INOPERATIVE AT ROW 8DF AND FORWARD LIGHT INOPERATIVE A T ROW 1DF. WIRING REPAIRED AT ROW 8DF AND 1DF. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001123100092 20011231 00092 NM 2001 12 31 PCAA0112171 1 20011220 A 5210 85210240005 STRUT DHAV DHC8 DHC8102 2809003 NM PAX DOOR WEAK A PCAA K NONE O OTHER TX TAXI/GRND HDL 1 EA 13 822EX 187 LGA- CREW REPORTED MAIN CABIN DOOR IS JAMMED AND WILL NOT OPEN. MAINTENANCE REPLACED FORWARD AND AFT DOOR (HANDRAIL) ST RUTS. OPERATIONAL CHECK GOOD IN ACCORDANCE WITH DASH 8 MAINTENANCE MANUAL 52-10-00. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001123100093 20011231 00093 SW 2001 12 31 PNSA011101 1 20011119 A 3610 LINE SWRNGN SA227 SA227AC 8780603 SW RT WING LEAKING A PNSA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 AL 03 640PA AC759B ON CLIMBOUT RT WING OVERHEAT WARNING LIGHT CAME ON. RT ENGINE BLEED AIR SYSTEM SHUTDOWN AND LIGHT EXTINGUISHED. CONTIN UED TO MAINTENANCE BASE WHERE A BLEED AIR LINE WAS FOUND LEAKING AT WING ROOT AND REPAIRED. 2 L 7 2 4T RT A8SW 2001123100094 20011231 00094 SW 2001 12 31 PNSA011103 1 20011106 A 7603 CABLE FRCHLD SA227 SA227DC 3377521 SW ENGINE CONTROL FROZEN A PNSA A UNSCHED LANDING O OTHER CL CLIMB 1 AL 03 892DC DC892B AT LEVEL OFF FROM CLIMB UNABLE TO REDUCE RT ENGINE SPEED. MAINTENANCE FOUND SPEED LEVER CABLE FROZEN. PURGED AND LUBRI CATED AIRFRAME SIDE OF CABLE. 2 L 7 2 4T RT A18SW 2001123100095 20011231 00095 SW 2001 12 31 PNSA011104 1 20011111 A 3230 LIMIT SWITCH FRCHLD SA227 SA227DC 3377521 SW NLG FAILED A PNSA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 30135 DC890B AFTER TAKEOFF NOSE GEAR FAILED TO RETRACT FULLY. RETURNED TO UNK AND AIRCRAFT INSPECTED AND FERRIED TO ANC MAINTENANCE BASE. MAINTENANCE REPLACED UP LIMIT MICROSWITCH. 2 L 7 2 4T RT A18SW 2001123100096 20011231 00096 SW 2001 12 31 PNSA011105 1 20011111 A 7603 CABLE FRCHLD SA227 SA227DC 3377521 SW ENGINE CONTROL FROZEN A PNSA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 AL 03 30135 DC890B COULD NOT SET TAKEOFF POWER FOR RT ENGINE. THAWED AIRFRAME POWER LEVER CABLE AND OP CHECK OK. 2 L 7 2 4T RT A18SW 2001123100097 20011231 00097 SO 2001 12 31 PNSA011107 1 20011117 A 5610 DOUBLER PIPER PA32 PA32301 7103207 SO WINDOW SEPARATED E PNSA K NONE O OTHER CR CRUISE 1 AL 03 8327S 328106039 PILOTS SIDE WINDOW DURING MODERATE TURBULENCE HAD PREVIOUS REPAIR COME LOOSE. AIRCRAFT REPAIRED BY AKN MAINTENANCE PER AC 43.13 PLEXIGLASS REPAIR PROCEDURE. 1 L 7 1 3O A3SO 2001123100098 20011231 00098 SW 2001 12 31 PNSA011109 1 20011123 A 2932 SS10127 PRESSURE SWITCH SWRNGN SA227 SA227AC 8780603 SW HYDRAULIC SYS FAILED A PNSA K NONE N FALSE WARNING DE DESCENT 1 AL 03 640PA AC759B DURING DESCENT RT HYDRAULIC LIGHT CAME ON, HYD PRESSURE WAS NORMAL. AIRCRAFT CONTINUED ON TO ANC. REPLACED HYDRAULIC P RESSURE SWITCH. 2 L 7 2 4T RT A8SW 2001123100099 20011231 00099 SW 2001 12 31 PNSA011110 1 20011126 A 5210 VALVE SWRNGN SA227 SA227AC 8780603 SW PAX DOOR CONTAMINATED A PNSA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 2719H AC713B ON CLIMBOUT AIRCRAFT WOULD NOT FULLY PRESSURIZE. AIRCRAFT MAINT CONTACTED AND AIRCRAFT RETURNED TO ANC. MAINTENANCE FO UND PAX DOOR SEAL NOT INFLATING. THAWED AND PURGED DOOR SEAL VALVE. 2 L 7 2 4T RT A8SW 2001123100101 20011231 00101 EU 2001 12 31 QXEA0102014 1 20011128 A 5532 RIVET FOKKER F28 F28MK4000 4990810 EU VERTICAL STAB LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - VERTICAL STABILIZER SMOKING RIVET JUST BELOW RIB 5 ON 50 PERCENT SPAR RT SIDE. REPAIRED IAW HORIZON AIR EA 4-55-2 99. 2 L 7 2 4F RT A20EU 2001123100102 20011231 00102 EU 2001 12 31 QXEA0102015 1 20011128 A 5532 RIVET FOKKER F28 F28MK4000 4990810 EU VERTICAL STAB LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - VERTICAL STABILIZER SMOKING RIVETS LT SIDE JUST BELOW RIB 5 ON 50 PERCENT SPAR. REPAIRED IAW HORIZON AIR EA 4-55- 299. 2 L 7 2 4F RT A20EU 2001123100103 20011231 00103 EU 2001 12 31 QXEA0102016 1 20011124 A 5315 FLOORBEAM FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FLOORBEAM CRACKED 9 INCHES AFT OF FRAME 3450 AND APPROXIMATELY 30 INCHES FROM SERVICE/EMERGENCY DOOR. REPAIRED IA W HORIZON AIR EA 4-53-1525 AND FOKKER SRM 53-02-14. 2 L 7 2 4F RT A20EU 2001123100104 20011231 00104 EU 2001 12 31 QXEA0102017 1 20011128 A 5320 A34918007 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - REMOVE DAMAGED LOWER THRESHOLD COAMING AND REPLACE WITH A34918-007. REPAIRED IAW HORIZON AIR EA 4-53-904A AND FOK KER MM 51-30-00, PAGE 701-706. 2 L 7 2 4F RT A20EU 2002010800084 20020108 00084 NM 2002 1 8 F3LA200100140 1 20011228 A 5320 INTERCOSTAL BOEING 737 737228 13844AG NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED WEB INTERCOSTAL ON AFT SIDE OF STA 787, STR 25-R, CORRODED. FABRICATED AND INSTAL LED REPLACEMENT INTERCOSTAL PER SRM 53-10-2 AND 51-10-02. 2 L 7 2 4F RT A16WE 2001123100105 20011231 00105 EU 2001 12 31 QXEA0102018 1 20011129 A 5330 RIVET FOKKER F28 F28MK4000 4990810 EU FUSELAGE MISSING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - TWO RIVET HEADS MISSING ON FUSELAGE SKIN AT FRAME 16060 NEAR STRINGER 55. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002011800097 20020118 00097 NM 2002 1 18 QXEA0102019 1 20011205 A 2612 10109601 FIRE LOOP DHAV DHC8 DHC8* NM NR 1 ENGINE FAULTY A QXEA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 NM 09 402QX 1349 4032 PDX - ON APPROACH TO PDX IN IMC FIRE BELL AND NR 1 ENGINE T-HANDLE ILLUM. PROCEEDED WITH IAC UPON SECURING NR 1 ENGINE T -HANDLE LIGHT EXTINGUISHED. ABOUT 1 MINUTE AFTER SECURING NR 1 ENGINE, NR 1 T-HANDLE INDICATION AND FIRE BELL RE-ILLUMIN ATED. FIRED EXTINGUISHERS, T-HANDLE INDICATION EXTINGUISHED WITH 2ND FIRE BOTTLE. REQUESTED CFR, LANDED WITHOUT INCIDEN T, NO INDICATION OF FIRE FOUND UPON INSPECTION. REPLACED PEC, FIRE LOOP, FIRE BOTTLES, FADEC, CVR, FDR, GENERATOR,VALVES , CARTRIDGE, AND RESTRICTOR. CHECKED GOOD. A/C RETURNED TO SERVICE. THE FINAL FIX WAS DETERMINED TO BE BAD PEC FIRE LOO P. FIRE LOOP TRIPED AT 160 DEG F INSTEAD OF 300 DEG F. 2 H 7 2 4T RT A13NM 2001123100106 20011231 00106 EA 2001 12 31 QXEA0102020 1 20011205 A 3260 895302 PSEU CNDAIR CL600 CL6002C10 1390015 EA E/E BAY FAULTY A QXEA K NONE J WARNING INDICATION CL CLIMB 1 NM 09 606QX 538 10023 PDX - AFTER TAKEOFF AND GEAR AND FLAP/SLAT RETRACTION (PROX SYSTEM MESSAGE). ON APPROACH IN PDX SLAT/FLAP EXTENSION NO CHANGE AFTER GEAR HANDLE SELECTED DOWN (PROX SYSTEM MESSAGE) WENT OUT. LANDED WITHOUT INCIDENT. REPLACED PSEU. OPERAT IONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2001123100107 20011231 00107 NM 2001 12 31 QXEA0102021 1 20011205 A 3350 6104781 BATTERY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 357PH 13651 365 504 SEA- EXIT SIGN NEAR FLIGHT DECK DOOR AND GALLEY EXIT DO NOT FUNCTION. REPLACED EMERGENCY LIGHT CONTROL BOX BATTERY UNIT AT PS3. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001123100108 20011231 00108 NM 2001 12 31 QXEA0102022 1 20011204 A 3350 6038443 BATTERY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 364PH 7511 7511 524 SEA- ONE OVERHEAD EMERGENCY LIGHT IN CABIN AND LT AFT EMERGENCY EGRESS LIGHT INOPERATIVE. REPLACED BATTERY AND POWER SU PPLY AT PS3. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001123100109 20011231 00109 NM 2001 12 31 QXEA0102023 1 20011207 A 3350 61047811 BATTERY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 366PH 6404 5 510 SEA- THREE EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001123100110 20011231 00110 NM 2001 12 31 QXEA0102024 1 20011206 A 3350 6104781 BATTERY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 374PH 13479 85 528 SEA- ROW 1 AFT SET OF RED FLOOR LIGHTS INOPERATIVE. REPLACED NUMBER 2 EMERGENCY LIGHTS BATTERY AND POWER SUPPLY. OPERA TIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001123100111 20011231 00111 EU 2001 12 31 QXEA0102025 1 20011208 A 2611 SMOKE DETECTOR FOKKER F28 F28MK4000 4990810 EU LAVATORY MALFUNCTIONED A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 492US 11159 PDX- DURING CLIMB-OUT, LAV SMOKE DETECTOR WENT OFF. NO VISIBLE SMOKE OR FIRE NOTED. AIRCRAFT RETURNED TO FIELD. COMPLI ED WITH MTC 8361002. RE-INSTALLED ORIGINAL SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001123100112 20011231 00112 NM 2001 12 31 QXEA0102026 1 20011206 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM LAVATORY MALFUNCTIONED A QXEA K NONE N FALSE WARNING CL CLIMB 1 NM 09 359PH 514 SEA- LAVATORY SMOKE DETECTOR SOUND INTERMITTENTLY DURING CLIMBOUT THROUGH 6,000 FEET. REMOVED AND REPLACED SMOKE DETECT OR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001123100113 20011231 00113 NM 2001 12 31 QXEA0102027 1 20011207 A 3260 858601 PSEU DHAV DHC8 DHC8202 2809007 NM E/E BAY FAULTY A QXEA K NONE J WARNING INDICATION NR NOT REPORTED 1 NM 09 363PH 6384 6384 520 YVR - RIGHT MAIN GEAR DOWN ADVISORY LIGHT WOULD NOT ILLUMINATE WITH GEAR DOWN SELECTION. HOWEVER LIGHT DID TEST OKAY. GEAR WAS CYCLED AND ON SECOND ATTEMPT ALL THREE GEAR LIGHTS ILLUMINATED. AIRCRAFT LANDED WITHOUT INCIDENT. FERRIED AIR CRAFT TO PDX. PERFORMED TASK 32-61-00 (AFTER FLIGHT PSEU MEMORY RECALL), FOUND CODES 55 AND 53, PSEU MEMORY LIGHT WOULD NOT EXTINGUISH. REPLACED PSEU. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001123100114 20011231 00114 NM 2001 12 31 QXEA0102028 1 20011209 A 3350 82520977001 COVER DHAV DHC8 DHC8202 2809007 NM CABIN CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX- FLOOR PROXIMITY EMERGENCY ESCAPE PATH NR 2 POSITION AT STATION X270.56 WIRE COVER IS CRACKED. REMOVED AND REPLACED FLOOR PROXIMITY EMERGENCY ESCAPE PATH ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001123100115 20011231 00115 EA 2001 12 31 QXEA0102029 1 20011206 A 2611 CONNECTOR CNDAIR CL600 CL6002C10 1390015 EA FIRE DETECTION LOOSE A QXEA K NONE N FALSE WARNING UK UNKNOWN 1 NM 09 609QX 10031 PDX- INTERMITTENT FIRE SYSTEM FAULT STATUS MESSAGE. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND FOLLOWING MESSAGES, ENGINE BOTTLE 2 LOW PRESSURE DETECTED AND LOW RATE DISCHARGE AFT SQUIB AND BOTH BRIDGE WIRES OPEN. FOUND FIRE BOTTLES TO BE W ITHIN LIMITS IAW MM 26-21-07. TIGHTENED CANNON PLUGS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002010800086 20020108 00086 NM 2002 1 8 F3LA200100141 1 20011228 A 5320 ANGLE BOEING 737 737228 13844AG NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED ANGLE CORRODED AT AFT SIDE OF STA 787, STR 25-R. FABRICATED AND INSTALLED REPLACE MENT ANGLE PER SRM 53-10-2 AND 51-10-02. 2 L 7 2 4F RT A16WE 2001123100116 20011231 00116 EA 2001 12 31 QXEA0102030 1 20011209 A 2611 47388904 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY FAULTY A QXEA K NONE J WARNING INDICATION UK UNKNOWN 1 NM 09 609QX 31 31 10031 PDX- FIRE SYSTEM FAULT MESSAGE. REMOVED AND REPLACED FIDEEX CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2001123100117 20011231 00117 EA 2001 12 31 QXEA0102031 1 20011209 A 5210 HINGE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 608QX 10026 PDX - THE FORWARD PASSENGER DOOR HINGE IS DAMAGED. REPAIRED IAW EA 12-53-09. 2 L 7 2 4F RT A21EA 2001123100118 20011231 00118 NM 2001 12 31 QXEA0102032 1 20011213 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX - GOUGES WERE NOTED ON THE CARGO DOOR OUTER SKIN NEAR THE LOWER EDGE. REPAIRED SKIN IAW THE DASH 8 STRUCTURAL REPAI R MANUAL 51-40-11. 2 H 7 2 4T RT A13NM 2001123100119 20011231 00119 EU 2001 12 31 QXEA0102034 1 20011214 A 5210 SWITCH FOKKER F28 F28MK4000 4990810 EU PAX DOOR DIRTY A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 496US 11169 PDX- FLIGHT ATTENDANT REPORTS DIFFICULTY RAISING AND LOWERING MAIN CABIN DOOR. CLEANED MAIN CABIN DOOR HANDLE MICROSWIT CH. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001123100120 20011231 00120 EU 2001 12 31 QXEA0102035 1 20011218 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 498US 11181 PDX- EMERGENCY EXIT SIGN OVER COCKPIT ENTRANCE HAS SEVERAL BULBS INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIO NAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001123100121 20011231 00121 NM 2001 12 31 QXEA0102036 1 20011218 A 3150 WARNING SYSTEM DHAV DHC8 DHC8202 2809007 NM COCKPIT FALSE ACTIVATION A QXEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 09 354PH 498 BLI - DURING ADDITION OF TAKEOFF POWER, THE TAKEOFF WARNING HORN ACTIVATED. TAKEOFF WAS ABORTED AND THE REJECTED TAKEOF F LIST WAS COMPLIED WITH. A SECOND TAKEOFF WAS ATTEMPTED AND AGAIN THE TAKEOFF WARNING SOUNDED. THE REJECTED TAKEOFF L IST WAS COMPLIED WITH AGAIN AND THE AIRCRAFT RETURNED TO THE GATE. AIRCRAFT WAS TROUBLESHOT, NO TAKEOFF WARNING HORN SO UNDED. COMPLIED WITH FUNCTIONAL TEST. COULD NOT DUPLICATE. NO DISCREPANCIES DETECTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2001123100122 20011231 00122 NM 2001 12 31 QXEA0102037 1 20011218 A 5412 FIREWALL DHAV DHC8 DHC8202 2809007 NM NR 1 NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - NR 1 ENGINE AFT FIRE WALL AT ABOUT THE 11:00 POSITION FOUND A CRACK IN THE FIRE LOOP AREA. REPAIRED IAW RD 8-54-1 09. 2 H 7 2 4T RT A13NM 2001123100123 20011231 00123 EU 2001 12 31 QXEA0102129 1 20011219 A 3350 5515900004 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 497US 11173 SEA- EXIT SIGN ABOVE COCKPIT DOOR HAS BULBS INOPERATIVE. REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT R ETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001123100124 20011231 00124 NM 2001 12 31 QXEA0102130 1 20011220 A 5312 BULKHEAD DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - REAR PRESSURE BULKHEAD DAMAGED AT THE 8 O'CLOCK POSITION. REPAIRED IAW HORIZON AIR EA 2-53-352 A. 2 H 7 2 4T RT A13NM 2001123100125 20011231 00125 NM 2001 12 31 QXEA0102131 1 20011220 A 5412 FIREWALL DHAV DHC8 DHC8102 2809003 NM NR 2 NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 054 PDX - NR 2 ENGINE AFT FIREWALL IS CRACKED AT ABOUT 10:00 AT Z-BRACKET. REPAIRED IAW RD 8-54-611. 2 H 7 2 4T RT A13NM 2001123100126 20011231 00126 NM 2001 12 31 QXEA0102132 1 20011220 A 5410 STRUT DHAV DHC8 DHC8102 2809003 NM NR 2 NACELLE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 054 PDX - TWO GOUGES ON NR 2 ENGINE OUTBOARD LOWER TORQUE STRUT AT BOTTOM END. REPAIRED IAW RD 8-54-036. 2 H 7 2 4T RT A13NM 2001123100127 20011231 00127 EU 2001 12 31 QXEA0102134 1 20011224 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 491US 11156 PDX- SEVERAL 28 VOLT LAMPS FAIL TO ILLUMINATE IN AFT CENTER CABIN EXIT SIGN. REMOVED AND REPLACED EXIT SIGN. OPERATION AL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001123100128 20011231 00128 EU 2001 12 31 QXEA0102135 1 20011223 A 3350 6008905 BATTERY FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 499US 16217 2818 11182 SEA- CABIN FORWARD EXIT SIGN IS DIM. REMOVED AND REPLACED BATTERY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERV ICE. 2 L 7 2 4F RT A20EU 2001123100129 20011231 00129 EU 2001 12 31 RAIA00112002 1 20011205 A 3350 LIGHT AEROSP ATR72 ATR72202 8680940 EU CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 722TE 220 MX-STL-FLOOR PATH LIGHT, AFT BULB INOP. SECURED LOOSE AFT BULB IAW ATR MAINTENANCE MANUAL. 2 H 7 2 4T RT A53EU 2001123100131 20011231 00131 EU 2001 12 31 RAIA00112004 1 20011210 A 3397 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN DISCONNECTED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 574HK 41093 MX-STL-PATH LIGHTS FWD SECTION INOP. MAINTENANCE RECONNECTED PATH LIGHT CONNECTOR. 2 L 7 2 4T RT A41NM 2001123100132 20011231 00132 EU 2001 12 31 RAIA00112005 1 20011211 A 3397 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN DISCONNECTED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 561HK 41077 MX-STL-EMERGENCY TRACK LIGHTS INOP 5A TO 10A. MAINTENANCE RE-SECURED TRACK LIGHT CONNECTOR. 2 L 7 2 4T RT A41NM 2001123100133 20011231 00133 EU 2001 12 31 RAIA00112006 1 20011212 A 3397 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN DISCONNECTED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 551HK 41040 MX-STL- ESCAPE PATH LIGHTS INOP. MAINTENANCE RECONNECTED PATH LIGHT CONNECTOR. 2 L 7 2 4T RT A41NM 2001123100134 20011231 00134 EU 2001 12 31 RAIA00112007 1 20011214 A 3397 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN DISCONNECTED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 552HK 41057 MX-STL-FLOOR PATH LIGHTS INOP ROW 1-5. MAINTENANCE RECONNECTED PATH LIGHT CONNECTOR. 2 L 7 2 4T RT A41NM 2001123100135 20011231 00135 EU 2001 12 31 RAIA00112008 1 20011215 A 3260 UPLOCK SWITCH JETAIR JETSTM JETSTM4101 1500501 EU LT MLG DIRTY A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 571HK 41090 5594-STL- LANDING GEAR HANDLE LIGHT ILLUMINATED AFTER GEAR RETRACTION. MAINTENANCE CLEANED LT MAIN LANDING GEAR UPLOCK SWITCH AND RESECURED CANNON PLUG. 2 L 7 2 4T RT A41NM 2001123100136 20011231 00136 EU 2001 12 31 RAIA00112010 1 20011224 A 3397 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN DISCONNECTED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 552HK 41057 MX-STL- FWD ESCAPE PATH LIGHTS INOP. RECONNECTED PATH LIGHT ELECTRICAL CONNECTOR IAW J41 MM. 2 L 7 2 4T RT A41NM 2001123100138 20011231 00138 2001 12 31 SWAA013337 4 20011215 A 3442 066500080406 TRANSCEIVER BOEING 737 7372H4 138448C NM E/E BAY UNRELIABLE A SWAA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 SW 07 089SW 22904 DIVERSION RADAR UNRELIABLE. REMOVED AND REPLACED RADAR R/T PER MM AND REPAIRED BROKEN WIRES AT COOLING FAN PER MM. 2 L 7 2 4F A16WE 2001123100139 20011231 00139 2001 12 31 SWIA200110407 4 20011130 A 2210 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA RUDDER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 07 594SW 7285 IN CRUISE FLIGHT AND DURING DESCENT INTO RNO RUDDER SYSTEM INDICATED UNCOMMANDED RUDDER MOVEMENT LEFT AND RIGHT. REMOVE D AND REPLACED LEFT AND RIGHT YAW DAMPER ACTUATORS AND NR 1 AND NR 2 AHRS COMPUTERS. ALL OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2001123100140 20011231 00140 2001 12 31 SWIA200110408 4 20011130 A 3425 6226190204 COMPARATOR EMB 120 EMB120ER 3260203 SO COCKPIT FAILED A SWIA C ABORTED TAKEOFF I FLT. ATTITUDE INST. TO TAKEOFF 1 NM 07 295UX 125 125 120295 UPON APPLICATION OF TAKEOFF POWER CAPTAIN'S SIDE ATTITUDE INDICATOR BECAME INOPERATIVE SHOWING NO HORIZON INFORMATION AN D DISPLAYING ATT FLAG. REPLACED CAPTAIN'S AHC-85. OPS CHECK GOOD IAW EMB120 MM 34-25-00. 2 L 7 2 4T RT A31SO 2001123100141 20011231 00141 EA 2001 12 31 SWIA200110409 1 20011129 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 905SW 7437 AFTER T/O AT 400 FT RECEIVED FLAP FAIL CAUTION MESSAGE WHEN RETRACTING FLAPS. RAN QRH AND RETURNED TO THE FIELD. COMPL IED WITH AD 98-20-01. CYCLED FLAPS UP AND DOWN. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2001123100142 20011231 00142 SO 2001 12 31 SWIA200110410 1 20011129 A 3020 211C117183 PRESSURE SWITCH EMB 120 EMB120ER 3260203 SO RT ENGINE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 298SW 120328 RIGHT SIDE ENGINE AIR INLET DEICE BOOT FAILED, AMBER LIGHT. RE-ATTEMPTS AT DIFFERENT POWER SETTINGS, ALL FAILED. RETUR NED TO DENVER. INSTALLED SERVICEABLE RT ENGINE AIR INLET PRESSURE SWITCH. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002010800087 20020108 00087 NM 2002 1 8 F3LA200100142 1 20011228 A 5320 INTERCOSTAL BOEING 737 737228 13844AG NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED INTERCOSTAL CRACKED AT STR 26-L, STA 460. FABRICATED AND INSTALLED REPLACEMENT IN TERCOSTAL PER SRM 53-10-2 AND 51-10-02. 2 L 7 2 4F RT A16WE 2001123100143 20011231 00143 SO 2001 12 31 SWIA200110411 1 20011205 A 3230 12043270501 CONTROL BOX EMB 120 EMB120ER 3260203 SO E/E BAY MALFUNCTIONED A SWIA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 NM 07 221SW 120290 RIGHT MAIN A LIGHT ON LANDING GEAR REMAINED ILLUMINATED AFTER T/O WITH CORRESPONDING VIBRATION SIMILAR TO GEAR BEING DOW N. RETURNED TO FIELD. INSPECTED AND ADJUSTED RT MLG UPLOCK PROXIMITY TARGET. ALSO REPLACED LDG RELAY BOX AND LDG SELE CTOR BOX. PERFORMED NUMEROUS GEAR SWINGS. GROUND CHECK NORMAL. RELAY BOX P/N: 120-43270-501, S/N ON: 120154, S/N OF F: 120290. SELECTOR BOX P/N ON: 120-25226-501, S/N ON: 120039, P/N OFF: 120-38594-301, S/N OFF: 137101-304. 2 L 7 2 4T RT A31SO 2001123100144 20011231 00144 EA 2001 12 31 SWIA200110412 1 20011203 A 3010 11513361 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA ANTI-ICE SYS FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 426SW 7468 WING OVERHEAT MESSAGE ON CLIMBOUT. ALSO HAD A RT WING ANTI ICE CAUTION MESSAGE. WING OVERHEAT MESSAGE WAS ON LEFT WING . RETURNED TO FIELD. REMOVED AND REPLACED WING ANTI TEMP CONTROLLER. RAN SYSTEM, OPS CHECKS OK. 2 L 7 2 4F RT A21EA 2001123100145 20011231 00145 EA 2001 12 31 SWIA200110413 1 20011203 A 3020 GASKET CNDAIR CL600 CL6002B19 1900309 EA RT COWL DEFECTIVE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 907SW 7511 CLIMBING THROUGH 2,000 FT R 14TH STAGE WARNING MESSAGE WAS GENERATED. RETARD THRUST LEVER PER QRH. MESSAGE WENT OUT. RETURNED TO AIRPORT PER QRH. RT ENGINE DUCT FAIL LIGHT, R 14TH DUCT LIGHT ILLUMINATED WITH RED EICAS MESSAGE FLOW LINE BETWEEN RT BLEED SOV, NOSE COWL AND WING SOV AT POWER ABOVE 80 PERCENT N1. RETURNED TO FIELD. REMOVED AND REPLACED A D EFECTIVE GASKET FOR THE RIGHT ENGINE COWL ANTI-ICE DUCT AT THE PYLON DISCONNECT. OPERATED THE RIGHT ENGINE AT T/O POWER FOR 20 MINUTES WITH NO FURTHER PROBLEMS. NO LEAKS NOTED. 2 L 7 2 4F RT A21EA 2001123100146 20011231 00146 2001 12 31 SWIA200110414 4 20011204 A 6113 SCREW EMB 120 EMB120ER 3260203 SO PROP SPINNER MISSING A SWIA K NONE D INFLIGHT SEPARATION UK UNKNOWN 1 NM 07 235SW 120310 ON POST FLIGHT WALKAROUND, IT WAS NOTED THAT LEFT PROP SPINNER HAD LOST 6 SCREWS, ALSO 2 BLADES HAD DEEP GOUGES FROM WHE RE SCREWS IMPACTED BLADES. REMOVED AND REPLACED NR 2 & NR 3 BLADES ON LEFT PROP. REPLACED MISSING SPINNER SCREWS. (NR 2) S/N OFF 872960, S/N ON 888803 (NR 3) S/N OFF 869876, S/N ON 890476. 2 L 7 2 4T RT A31SO 2001123100147 20011231 00147 SO 2001 12 31 SWIA200110415 1 20011204 A 3260 WIRE HARNESS EMB 120 EMB120ER 3260203 SO LT MLG DEFECTIVE A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 284YV 120284 AFTER GEAR HANDLE WAS MOVED UP, ALL GREEN LIGHTS STAYED ON AND ALL RED LIGHTS ILLUMINATED EXCEPT A-LEFT MAIN GEAR. GEAR WOULD NOT RETRACT. PDX SWAPPED LEFT MAIN A & B SENSOR LEADS PER SNL 20-32-0015. SWUNG GEAR. DEFERRED RED B-LIGHT IAW MEL 32-60-1A. GEAR OPS CHECK GOOD. FOUND B-UPLOCK PROX TO BE OPERATIONAL. HOWEVER, FOUND A-UPLOCK TO BE INOP. REPLA CED A-UPLOCK PROX HARNESS PER MM 32-61-01. ALL GEAR INDICATIONS CHECK GOOD ON GEAR SWING. 2 L 7 2 4T RT A31SO 2001123100148 20011231 00148 EA 2001 12 31 SWIA200110416 1 20011203 A 3397 POWER CABLE CNDAIR CL600 CL6002B19 1900309 EA CABIN CONTAMINATED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 410SW 7066 CABIN FLOOR EMERGENCY LIGHT FWD SECTION INOP. FOUND ONE LAMP SECTION BAD. REPLACED LAMP. FOUND POWER CABLE FOR FLOOR LIGHT WET AND SHORTING. DRIED FLOOR. DRIED POWER CABLE. OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2001123100149 20011231 00149 SO 2001 12 31 SWIA200110417 1 20011201 A 2731 52991 ACTUATOR EMB 120 EMB120ER 3260203 SO ELEVATOR TAB FAILED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 234SW 120308 ELEVATOR TRIM FROZE INFLIGHT AT 26,000 FT. DID NOT UNFREEZE UNTIL 10,000 FT. AIRCRAFT WAS CONTROLLABLE BY NORMAL CONTR OL PRESSURES. REMOVED AND REPLACED LT AND RT ELEVATOR TRIM TAB ACTUATORS IAW MM 27-32-02. ADJUSTED TRIM TAB CABLE TENS IONS IAW MM 27-00-01. CHECKS GOOD. LT S/N ON: 756 P/N OFF: 5299, S/N OFF: 696, RT S/N ON: 175, P/N OFF: 5299, S /N OFF: 697. 2 L 7 2 4T RT A31SO 2002010800090 20020108 00090 NM 2002 1 8 F3LA200100144 1 20011228 A 5315 FLOORBEAM BOEING 737 737228 13844AG NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM AT STA 294 FROM LBL 17 TO LBL 25. FABRICATED REPAIR AND IN STALLED PER SRM 51-40-3, FIG 1 AND 53-10-9, FIG 5. 2 L 7 2 4F RT A16WE 2001123100150 20011231 00150 SO 2001 12 31 SWIA200110418 1 20011130 A 5753 ROLLER EMB 120 EMB120ER 3260203 SO T/E FLAP WORN A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 188SW 120039 ON CLIMBOUT FLAP DISAGREEMENT, WOULD NOT FIX ITSELF. RAN QRH PROCEDURE. RESET FLAPS TO 15 DEGREES, THEN BACK TO 0. FL AP DISAGREEMENT WENT OUT. REMOVED AND REPLACED RT WING O/B FLAP O/B ROLLER WITH NEW ROLLER. OPS CHECK GOOD AT THIS TIM E. 2 L 7 2 4T RT A31SO 2001123100151 20011231 00151 EA 2001 12 31 SWIA200110428 1 20011216 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 430SW 7523 FLIGHT SPOILERS FAULT MESSAGE APPEARED ON TAXI OUT. REMOVED AND REPLACED PCU WITH SERVICEABLE UNIT PER MM 27-61-00. OP S CHECK GOOD. 2 L 7 2 4F RT A21EA 2001123100152 20011231 00152 EA 2001 12 31 SWIA200110429 1 20011213 A 3030 7858062 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA PITOT HEAT FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 720SW 7297 AFTER TAKEOFF L-PITOT HEAT CAUTION MESSAGE. RETURNED TO SLC. REMOVED AND REPLACED LEFT AIR DATA SENSOR HEATER CONTROLL ER IAW 30-41-00. LEFT PITOT HEAT OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002010400095 20020104 00095 WP 2002 1 4 ARWA20011214 1 20011227 A 7931 41800041 TRANSMITTER DOUG DC8 DC861 3021952 WP NR 4 ENGINE ERRATIC A ARWA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 SO 19 29UA 46159 NR 4 OIL PRESSURE WENT TO 0 PSI AFTER TOP OF DESCENT, NR 4 OIL PRESS LIGHT ILLUMINATED, ENGINE WAS SHUT DOWN. BLED NR 4 ENGINE OIL SYSTEM, REMOVED AND REPLACED MAIN OIL FILTER IAW P&W 72-0, FOUND OIL PRESS XMTR ERRATIC, R&R IAW MM 79-32-1, OPS CKD DURING ENGINE RUN UP OK IAW MM 71-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2001123100153 20011231 00153 SO 2001 12 31 SWIA200110431 1 20011211 A 2752 3431001001 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP FAILED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 207SW 120266 AFTER TAKEOFF A FLAP DISAGREEMENT OCCURRED. TWO SEGMENTS OF THE INBOARD PAIR WERE ILLUMINATED AND 1 BAR OF THE NACELLE AND OUTBOARD PAIR FLASHED. DISAGREEMENT CLEARED AFTER SELECTING 15 DEGREES UP, BUT THEN AN INVALID ANALOG IND WAS DISPL AYED. REMOVED AND REPLACED LEFT NACELLE FLAP ACTUATOR IAW 27-50-08. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2001123100154 20011231 00154 EA 2001 12 31 SWIA200110432 1 20011211 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 403SW 2340 2340 7028 FLOOR EMERGENCY LIGHTS (FRONT HALF) DIM, 1 SECTION OUT NEAR EMERGENCY EXIT. REMOVED FORWARD EMERGENCY LIGHTING BATTERY PACK (ELBP) IN CABIN CEILING AND REPLACED WITH SERVICEABLE ELBP. FOUND ONE FLOOR LIGHT SECTION UNPLUGGED. REPLUGGED TH AT SECTION. OPS CHECK GOOD IAW CRJ MM 33-51-01 AND 33-51-04. 2 L 7 2 4F RT A21EA 2001123100155 20011231 00155 SO 2001 12 31 SWIA200110433 1 20011211 A 3010 CONNECTOR EMB 120 EMB120RT 3260202 SO DEICE SYS CORRODED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 1110J 120110 VERTICAL FIN LEADING EDGE DEICE BOOT FAILED INFLIGHT WITH BOTH TIMERS 1 AND 2. FOUND GREEN CORROSION AROUND PIN-B IN CO NNECTOR AT S0213 (VERTICAL FIN PRESSURE SWITCH). REMOVED AND REPLACED CONNECTOR P1080 AND SOCKET-B IN CONNECTOR. GROUN D OPS CHECK OK WITH LEFT AND/OR RIGHT ENGINE AIR. 2 L 7 2 4T RT A31SO 2001123100156 20011231 00156 EA 2001 12 31 SWIA200110434 1 20011212 A 3150 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 411SW 7067 LEFT PITOT, AOA, BASE HEAT, AND MACH TRIM CAUTION MESSAGES ON TAKEOFF. RETURNED TO DFW. POWERED DOWN/POWERED UP. REIN ITIALIZED COMPUTER. MESSAGES CLEARED. NO DEFECTS. 2 L 7 2 4F RT A21EA 2001123100157 20011231 00157 SO 2001 12 31 SWIA200110435 1 20011211 A 3150 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO COCKPIT FALSE ACTIVATION A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 292UX 120292 TRIPLE CHIME HIGH SPEED WARNING SOUNDED ON TAKEOFF (ABORTED TAKEOFF). HOOKED UP PITOT STATIC SET, RAN UP AND DOWN 5 TIM ES, COULD NOT DUPLICATE. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2001123100158 20011231 00158 SO 2001 12 31 SWIA200110436 1 20011211 A 3230 12061110001 CONTROL BOX EMB 120 EMB120ER 3260203 SO E/E BAY MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 582SW 120354 AFTER TAKEOFF, DOWNLOCK RELEASE NEEDED FOR GEAR RETRACTION. FLIGHT IDLE UNLOCK LIGHTS ILLUMINATED ON GLARESHIELD. AUTO PRESSURIZATION UNABLE TO CONTROL CABIN ALTITUDE. REMOVED AND REPLACED LANDING GEAR RELAY BOX. LANDING GEAR RETRACTION , OPS CHECKS GOOD AT THIS TIME AND FLIGHT IDLE STOP UNLOCK LIGHTS OPS CHECKS GOOD AT THIS TIME. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2001123100159 20011231 00159 SO 2001 12 31 SWIA200110438 1 20011204 A 2730 WIRE EMB 120 EMB120ER 3260203 SO ELEVATOR SYS BROKEN A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 189SW 120048 TRIM AURAL WARNING SOUNDING OFF IN THE GREEN BAND. ABORTED THE TAKEOFF. REPAIRED BROKEN WIRE AND READJUSTED PROXIMITY S ENSOR. OPS CHECK GOOD IAW EMB120 MM 27-32-00. 2 L 7 2 4T RT A31SO 2002010800092 20020108 00092 NM 2002 1 8 F3LA200100145 1 20011228 A 5320 ANGLE BOEING 737 737228 13844AG NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED ANGLE CRACKED AT 178 BULKHEAD, WL 200, LBL 17.1. REPAIRED CRACK IN ANGLE PER SRM 51-20-1 AND 51-30-2. 2 L 7 2 4F RT A16WE 2001123100169 20011231 00169 NM 2001 12 31 BJNA011107 1 20011101 A 3350 6013211 BATTERY PACK BOEING 737 737282 13844AT NM CABIN DISCHARGED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 233TM 23043 LEFT EXTERIOR OVER WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY PACK ASSEMBLY. OPS CHECK OK 2 L 7 2 4F RT A16WE 2001123100170 20011231 00170 WP 2001 12 31 ZW0A0112401 1 20011228 A 3350 60030451LB BATTERY PACK DOUG DC9 DC983 3022083 WP B5-23 A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9622A 53593 THE COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 7-25-01 STL. --CLOSED-- 2 L 7 2 4F RT A6WE 2001123100171 20011231 00171 SO 2001 12 31 LBT2001F00000 1 20010410 A 5730 4050612 SKIN PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA LT WING CORRODED E LBTA K NONE O OTHER IN INSP/MAINT 1 EA 25 66AU 6177 317405178 DURING ANNUAL INSPECTION, CORROSION FOUND ON LOWER LEFT HAND WING SKIN (PN 4050612) STATION NR 239 AFT OF EXHAUST STACKS . REMOVED CORROSION, TREATED AREA AND REPAIRED. 1 L 7 2 3O 3 O A20SO E14EA 2001123100172 20011231 00172 SO 2001 12 31 LBT2001F00001 1 20011010 A 5753 4018512 SKIN PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA T/E FLAP CORRODED E LBTA K NONE O OTHER IN INSP/MAINT 1 EA 25 66AU 6177 317405178 DURING ANNUAL INSPECTION, CORROSION FOUND ON LEADING EDGE OF LEFT AND RIGHT FLAP SKIN. REPLACED SKIN. 1 L 7 2 3O 3 O A20SO E14EA 2001123100173 20011231 00173 SO 2001 12 31 LBT2001F00002 1 20011010 A 5753 4018513 SKIN PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA T/E FLAP CORRODED E LBTA K NONE O OTHER IN INSP/MAINT 1 EA 25 66AU 6177 317405178 DURING ANNUAL INSPECTION, CORROSION FOUND ON LEADING EDGE OF LEFT AND RIGHT FLAP SKIN. REPLACED SKIN. 1 L 7 2 3O 3 O A20SO E14EA 2001123100174 20011231 00174 SO 2001 12 31 LBT2001F00003 1 20011010 A 5753 4018520 SKIN PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA T/E FLAP CRACKED E LBTA K NONE O OTHER IN INSP/MAINT 1 EA 25 66AU 6177 317405178 DURING ANNUAL INSPECTION, CRACKS FOUND ON LEFT FLAP TRAILING EDGE. REPLACED SKIN. 1 L 7 2 3O 3 O A20SO E14EA 2001123100175 20011231 00175 EU 2001 12 31 M7F2001F00000 1 20011214 A 3340 G62504 SEARCH LIGHT BOLKMS 105 BO105S 5626006 EU EXTERIOR MISSING B M7FR K NONE O OTHER IN INSP/MAINT 1 EA 23 105MH S419 BULB ASSEMBLY IS ATTACHED TO SEARCH LIGHT ASSEMBLY BY TWO SET SCREWS TIGHTENED INTO A POST. APPEARS THAT SET SCREWS LOS T TENSION ON POST AND BULB ASSEMBLY SLID OFF POST. NO DAMAGE TO AIRCRAFT. 1 G 7 2 3U H3EU 2001123100176 20011231 00176 2001 12 31 SWAA013340 4 20011217 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 785SW 30602 AFT SERVICE DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2001123100177 20011231 00177 NM 2001 12 31 SWAA013341 1 20011216 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASS Y PER MM. 2 L 7 2 4F A16WE 2002010100001 20020101 00001 SO 2002 1 1 C2XA01IA426 1 20011229 A 4910 4501968D APU EMB 145 EMB145 3260210 SO TAIL LEAKING A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 13970 145146 LCH- DURING TAXI, THE APU SHUT DOWN WITH APU FAIL EICAS MESSAGE,FOLLOWED BY SMOKE IN COCKPIT and CABIN. DOWNPOWERED A/ C. I TRIED TO RESTART AFTER SEVERAL MINUTES,APU SPOOLED ONLY TO 5% FOR TEN SECONDS, THEN SHUT DOWN AGAIN, AIRCRAFT RETU RNED TO GATE. LCH- MAINTENANCE RELEASED THE AIRCRAFT IAW MEL. IAH- MAINTENANCE REMOVED AND REPLACED THE APU,PERFORME D A LEAK CHECK, AND, A OPERATIONAL CHECK, NO DEFECTS NOTED,CLEARED THE MEL, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002010100002 20020101 00002 SO 2002 1 1 C2XA01IA427 1 20011227 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14905 145476 IAH- DURING POST FLIGHT THE CREW NOTED THAT THE AISLE PATH LIGHTING FAILED TO ILLUMINATE BETWEEN ROWS 10 and 14, IAH- MAINTENANCE REMOVED AND REPLACED THE BATTERY UNDER THE FLOOR AT SEAT 12A, PERFORMED A OPERATIONAL CHECK OF THE EMERGENC Y LIGHTING SYSTEM, NO DEFECTS NOTED,AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002010200001 20020102 00001 2002 1 2 SWAA013417 4 20011227 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 FWD ENTRY DOOR EVACUATION SLIDE FALLING OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2002010200002 20020102 00002 SO 2002 1 2 ASOA012006 1 20011005 A 5330 12022788017 SKIN EMB 120 EMB120RT 3260202 SO FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 274AS 120229 DURING SCHEDULED MAINTENANCE IN TXK, A SKIN CRACK, APPROXIMATELY .75 INCH LONG, WAS FOUND .5 INCH ABOVE THE TOP BRACKET FASTENER ON THE CAPTAINS LOWER FORWARD CORNER OF THE DV WINDOW POST. MAINTENANCE PERFORMED A TEMP REPAIR IAW ASA EO 120 -53-1068. MAINTENANCE PERFORMED A PERM REPAIR IAW ASA EO 120-53-0169. (M) 2 L 7 2 4T RT A31SO 2002010200003 20020102 00003 EU 2002 1 2 ASOA01242 1 20011117 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 536AS 465 FLT 4309 - DURING GROUND INSPECTION IN ATL, THE AIR STAIR DOOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY FOR THE AIR STAIR DOOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2002010200004 20020102 00004 EA 2002 1 2 COMA0160984 1 20011221 A 3220 PIN CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 729CA 7265 FLIGHT 5290 NLG WILL NOT RETRACT.REMOVED NLG DOWN LOCK SAFETY PIN AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002010200005 20020102 00005 EU 2002 1 2 ASOA01243 1 20011118 A 3350 LIGHT AEROSP ATR72 ATR72212 8680945 EU CABIN MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 532AS 458 FLT 4304 - DURING GROUND INSPECTION IN ATL, CREW REPORTED THE EMERGENCY LIGHTS WORKED INTERMITTENTLY. WITH THE GPU NOT SELECTED, THE NR 1 GENERATOR ONLINE AND THE EMERGENCY LIGHT SWITCH IN THE ARM POSITION THE EMERGENCY LIGHTS COME ON. TH E LIGHTS STAYED ON WHEN THE SWITCH WAS SELECTED TO DISARM. MAINTENANCE REMOVED PANEL AND INSPECTED WIRES. AFTER REINST ALLING THE PANEL MAINTENANCE RERACKED AND RESET THE BPCU AND GCU. OPERATIONAL CHECKS GOOD. NO DEFECTS WERE NOTED. (M) 2 H 7 2 4T RT A53EU 2002010200006 20020102 00006 SO 2002 1 2 ASOA01244 1 20011020 A 5313 12004137005 STRINGER EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 274AS 120229 DURING C-CHECK INSPECTION IN BNA, STRINGER 17 LEFT WAS FOUND CORRODED BETWEEN FRAME 21 AND STATION 6653.1. MAINTENANCE REMOVED AND REPLACED CORRODED STRINGER IAW SRM 51-25-00, 51-20-00, 51-10-02, AND 51-30-01. (M) 2 L 7 2 4T RT A31SO 2002010200007 20020102 00007 SO 2002 1 2 ASOA01245 1 20011020 A 5313 12005744013 STRINGER EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 274AS 120229 DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON STRINGER 19 LEFT FROM FRAME 13A TO FRAME 18. MAINTENANCE REMOV ED THE CORRODED 19 LEFT STRINGER FROM FRAME 13A TO FRAME 18 IAW SRM 51-25-00. A NEW STRINGER WAS INSTALLED IAW SRM 51-4 0-2. (M) 2 L 7 2 4T RT A31SO 2002010200008 20020102 00008 SO 2002 1 2 ASOA01246 1 20011020 A 5320 12046963001 BUTTSTRAP EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 274AS 120229 DURING C-CHECK INSPECTION IN BNA, THE LEFT BUTT STRAP FROM FRAME 14 TO STATION 6653.1 WAS FOUND CORRODED. THE CORROSION WAS FOUND TO BE OUT OF LIMITS AT FRAMES 14 AND 15. MAINTENANCE REMOVED THE CORRODED BUTT STRAP IAW SRM 51-40-02. A NE W BUTT STRAP WAS INSTALLED PER THE SAME SRM. (M) 2 L 7 2 4T RT A31SO 2002010200009 20020102 00009 SO 2002 1 2 ASOA01247 1 20011020 A 5320 12007089003 BUTTSTRAP EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 274AS 120229 DURING C-CHECK INSPECTION IN BNA, CORROSION FOUND ON THE CENTER BUTT STRAP FROM FRAMES 13 TO 16. MAINTENANCE REMOVED AN D REPLACED THE CORRODED CENTER BUTT STRAP IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002010200010 20020102 00010 SO 2002 1 2 ASOA01248 1 20011020 A 5320 12005805003 BUTTSTRAP EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 274AS 120229 DURING C-CHECK INSPECTION IN BNA, THE CENTER BUTT STRAP, FROM FRAME 16 TO STATION 6653.1, WAS FOUND CORRODED. MAINTENAN CE REMOVED AND REPLACED THE CORRODED CENTER BUTT STRAP IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002010200011 20020102 00011 SO 2002 1 2 ASOA01249 1 20011020 A 5320 12046156001 BUTTSTRAP EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 274AS 120229 DURING C-CHECK INSPECTION IN BNA, THE RIGHT BUTT STRAP WAS DISCOVERED CORRODED FROM FRAME 13 TO STATION 6653.1. MAINTEN ANCE REMOVED AND REPLACED RIGHT CORRODED BUTT STRAP IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002010200012 20020102 00012 EA 2002 1 2 ASOA01256 1 20011120 A 5610 NP1393225 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A ASOA K NONE O OTHER TX TAXI/GRND HDL 1 SO 11 864AS 7502 FLT 4453 - BEFORE DEPARTURE OUT OF DFW, CAPTAIN NOTICED A CRACK IN THE LEFT SIDE WINDSHIELD. MAINTENANCE REMOVED AND RE PLACED CRACKED WINDSHIELD. A PRESSURIZATION CHECK WAS PERFORMED AND NO LEAKS WERE NOTED. THE SEALANT WAS PROPERLY CURE D. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002010200013 20020102 00013 SO 2002 1 2 ASOA01257 1 20011120 A 3350 LIGHT EMB 120 EMB120RT 3260202 SO CABIN MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 269AS 120210 FLT 4963 - DURING GROUND INSPECTION IN DFW, CAPTAIN REPORTED AFTER SHUTDOWN HE TURNED THE EMERGENCY LIGHTS OFF AND THE L IGHTS CAME ON. MAINTENANCE GROUND RAN THE RIGHT ENGINE TO SIMULATE THE PROBLEM. OPERATIONAL CHECKS GOOD. EMERGENCY LI GHTS REMAINED OFF. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002010200014 20020102 00014 EU 2002 1 2 ASOA01258 1 20011121 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72 EU CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 643AS 413 DURING HANGAR MAINTENANCE IN MCN, A SECTION OF EMERGENCY LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING POWER SUPPLY AT THE 61WL POSITION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2002010200015 20020102 00015 SO 2002 1 2 ASOA01259 1 20011124 A 2520 PANEL EMB 120 EMB120ER 3260203 SO CABIN OUT OF POSITION A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 503AS 120275 DURING SCHEDULED MAINTENANCE IN MCN, THE EMERGENCY EXIT AT ROW 8 HIT THE OVERHEAD TRIM AND WOULD NOT OPEN. MAINTENANCE SECURED THE OVERHEAD TRIM AND REPOSITIONED THE SEATS TO CLEAR THE EMERGENCY EXIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002010200016 20020102 00016 WP 2002 1 2 GTIA011188 1 20011107 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FORWARD ENTRY AREA, FLOOR SUPPORT HAS AN ELONGATED HOLE AT STA Y=166 X53 INCHES. REMOVED DISC. FABRICATED NEW PA RT. INSTALLED NEW PART IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002010200017 20020102 00017 WP 2002 1 2 GTIA011189 1 20011119 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP GALLEY CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - G-2 GALLEY LOWER OUTBOARD LEFT SUPPORT CORRODED. REMOVED CORRODED ANGLE. LOCATE AND DRILL ANGLE IAW MD80 SRM 51- 30-1. (M) 2 L 7 2 4F A6WE 2002010200018 20020102 00018 WP 2002 1 2 GTIA011190 1 20011203 A 2612 CONNECTOR DOUG DC9 DC981 3022081 WP FIRE LOOP DIRTY A GTIA O OTHER N FALSE WARNING DE DESCENT 1 GL 23 810NK 48015 FLT 779 - FLL - LOOP A FIRE DETECT LIGHT ON DESCENT. NO OTHER INDICATIONS FOLLOW ABNORMAL CHECK LIST. CHECKED AND CLEA NED ENGINE NR 1 A LOOP SENSING ELEMENT CONNECTORS. REF WDM 26-11-00. OP CHECKED OK REF MM 26-10-00. (M) 2 L 7 2 4F A6WE 2002010200019 20020102 00019 WP 2002 1 2 GTIA011192 1 20011203 A 5755 SPOILER DOUG DC9 DC981 3022081 WP RT WING DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 DTW - RIGHT FLIGHT SPOILER, INBOARD DELAMINATED. REMOVED AND REPLACED RIGHT FLIGHT SPOILER, INBOARD IAW MD80 27-61-01. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2002010200020 20020102 00020 WP 2002 1 2 GTIA011193 1 20011203 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 DALLO 53012 DTW - EMERGENCY FLOOR PATH LIGHTING FROM ROW 5 TO 9 WOULD NOT ILLUMINATE CHANGED BATTERIES, NO HELP. REPLACED EMERGENCY FLOOR PATH LIGHTING WIRING AT SEAT 9. EMERGENCY LIGHTING OPS CHECK GOOD, IAW MD80 MM 33-50-02. (M) 2 L 7 2 4F RT A6WE 2002010200021 20020102 00021 WP 2002 1 2 GTIA011195 1 20011203 A 2730 SWITCH DOUG DC9 DC982 3022082 WP COCKPIT MALFUNCTIONED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 812NK 48021 F/O'S PRIMARY TRIM SWITCH IAW MD80 MM 27-40-02 AND GROUND, OPS CHECKS GOOD. (M) 2 L 7 2 4F A6WE 2002010200022 20020102 00022 WP 2002 1 2 GTIA011196 1 20011205 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 812NK 48021 ACY - EMERGENCY CEILING LIGHT FROM ROW 1 TO 4 INOPERATIVE. REMOVED AND REPLACED LIGHT BATTERIES, OPS CHECK GOOD IAW MD8 0 MM 33-53-01. (M) 2 L 7 2 4F A6WE 2002010200023 20020102 00023 WP 2002 1 2 GTIA011197 1 20011205 A 5753 PANEL DOUG DC9 DC983 3022083 WP T/E FLAP CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 809NK 49503 ACY - FLAP CUT OUT DOOR PANEL CRACKED. REMOVED, REPAIRED AND REINSTALLED FLAP SLAT OUT PANEL IAW MD80 SRM CH 57-03. (M ) 2 L 7 2 4F RT A6WE 2002010200024 20020102 00024 WP 2002 1 2 GTIA011198 1 20011205 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 803NK 48087 FLL - OVERHEAD EMERGENCY LIGHTS ROW 9 FOUND INOPERATIVE. REPLACED BATTERY IN OVERHEAD LIGHTS ROW 9 FORWARD IAW MD80 MM 33-53-00. (M) 2 L 7 2 4F A6WE 2002010200025 20020102 00025 WP 2002 1 2 GTIA012002 1 20011206 A 2611 SMOKE DETECTOR DOUG DC9 DC981 3022081 WP CARGO BAY FAULTY A GTIA K NONE N FALSE WARNING IN INSP/MAINT 1 GL 23 818NK 48018 FLL - 'A' LOOP FAIL LIGHTS STAYS ON OVERHEAD CARGO FIRE EXTINGUISHER AND DETECTION PANEL FOR AFT CARGO COMPARTMENT. REM OVED AND REPLACED AFT CARGO COMPARTMENT 'A' LOOP SMOKE DETECTOR, OPS CHECK IAW 26-50-00, OPS NORMAL. (M) 2 L 7 2 4F A6WE 2002010200026 20020102 00026 WP 2002 1 2 GTIA012003 1 20011206 A 2612 CGAB140001 FIRE LOOP DOUG DC9 DC981 3022081 WP CARGO BAY DEFECTIVE A GTIA K NONE N FALSE WARNING IN INSP/MAINT 1 GL 23 818NK 48018 'B' LOOP FAIL LIGHT STAYS ON OVERHEAD CARGO FIRE EXTINGUISHER AND DETECTION PANEL FOR AFT CARGO COMPARTMENT. REMOVED AN D REPLACED 'B' LOOP FIRE DETECTION UNIT, REF MM 26-30-00. OPS CHECK OK. (M) 2 L 7 2 4F A6WE 2002010200027 20020102 00027 SO 2002 1 2 SIMA200113200 1 20011115 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 602AE 145048 DURING AN MBV INSPECTION, FOUND CORROSION WAS FOUND ON THE GALLEY CENTER FLOOR SUPPORT, OMEGA SHAPE THAT SUPPORTS THE RI GHT INBOARD SEAT TRACK. REMOVED CORRODED GALLEY CENTER FLOOR SUPPORT. REPAIR DONE IAW EMB GST-3686/01/, PARA 1 EMB145 SRM'S 51-20-03, 51-21-04, 51-40-02, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002010200028 20020102 00028 SO 2002 1 2 SIMA200116003 1 20010609 A 2750 3631001007 CONTROL UNIT EMB 135 EMB135LR 3260305 SO T/E FLAP FAILED A SIMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 SW 21 708AE 145205 YQB - FLT 4771 - DURING DESCENT, CREW SELECTED FLAPS TO 9 DEGREES. RECEIVED TOTAL FLAP FAILURE. FLAP FAILED AND SPS AD VANCED ON EICAS. EMERGENCY DECLARED AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW EMB MM 27-53-02. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2002010200029 20020102 00029 SO 2002 1 2 SIMA200131308 1 20011108 A 5320 14522459003 SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 711PH 145235 ABI - THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM CARD NR 27618. GALLEY RAMP SUPPORT CORRODED. REMOVED AND IN STALLED SERVICEABLE RAMP SUPPORT IAW EMB 135 SRM 51-40-02. (M) 2 L 7 2 4F RT TOOO11AT 2002010200030 20020102 00030 SO 2002 1 2 SIMA200131309 1 20011108 A 5320 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 711PH 145235 THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. GALLEY AREA RIGHT FORWARD SILL CORRODED. SILL REPAIRED IAW EMB G ST 3598/01. (M) 2 L 7 2 4F RT TOOO11AT 2002010200031 20020102 00031 SO 2002 1 2 SIMA200131310 1 20011108 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 711PH 145235 ABI - DURING AN MBV INSPECTION, FOUND CORROSION ON THE RIGHT OMEGA FLOORBEAM AT FRAME 20. REMOVED CORROSION BY BLENDING . PERFORMED NDT INSPECTION ON THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED A U REPAIR DOUBLER. REPAIR DONE IAW EMB GST-3598/01 PARA 6 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT TOOO11AT 2002010200032 20020102 00032 SO 2002 1 2 SIMA200131311 1 20011108 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 711PH 145235 ABI - DURING A MBV, FOUND CORROSION ON THE GALLEY CENTER OMEGA BEAM. REMOVED CORROSION BY BLENDING OUT. PERFORMED AN N DT INSPECTION ON THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED A 'Z' REPAIR DOUBLER. REPAIR DONE IAW EMB GST-359 8/01 PARA 7 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT TOOO11AT 2002010200033 20020102 00033 SO 2002 1 2 SIMA200131312 1 20011109 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 711PH 145235 ABI - DURING MBV INSPECTION, CORROSION WAS FOUND ON THE CENTER OMEGA BEAM AT FRAME 24. REMOVED CORROSION BY BLENDING OU T. PERFORMED AN NDT INSPECTION OF THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED A Z REPAIR DOUBLER. REPAIR DONE IAW EMB GST-3598/01, PARA 3 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT TOOO11AT 2002010200034 20020102 00034 SO 2002 1 2 SIMA200131803 1 20011113 A 3230 12303617001 SPRING EMB 135 EMB135LR 3260305 SO LT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 711PH 145235 THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM CARD NR 27613. LEFT MLG UPLOCK SPRING CORRODED. RAI SERVICEABLE L EFT MLG UPLOCK SPRING IAW EMB 135 AMM 32-33-10-000-801A AND 32-33-10-400-801. (M) 2 L 7 2 4F RT TOOO11AT 2002010200035 20020102 00035 SO 2002 1 2 SIMA200131804 1 20011113 A 3230 12303617001 SPRING EMB 135 EMB135LR 3260305 SO RT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 711PH 145235 THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. RIGHT MLG UPLOCK SPRING CORRODED. REMOVED AND REPLACED UPLOCK SP RING IAW EMB135 AMM 32-33-10-000-801A AND 32-33-10-400-801A. (M) 2 L 7 2 4F RT TOOO11AT 2002010200036 20020102 00036 SO 2002 1 2 SIMA200131805 1 20011113 A 5320 14522459033 SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 712AE 145247 THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. GALLEY RAMP SUPPORT CORRODED. REMOVED RAMP SUPPORT AND INSTALLED NEW RAMP IAW EMB 135/145 SRM 51-40-02. (M) 2 L 7 2 4F RT TOOO11AT 2002010200037 20020102 00037 SO 2002 1 2 SIMA200131806 1 20011113 A 5320 14522460013 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 712AE 145247 ABI - THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. GALLEY CENTER BEAM GUSSET CORRODED. RAI SERVICEABLE GALLEY CENTER BEAM IAW EMB 135 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002010200038 20020102 00038 SO 2002 1 2 SIMA200131807 1 20011114 A 5320 14522400013 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 602AE 145048 ABI - THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. CENTER BEAM GUSSET CORRODED IS GALLEY AREA. INSTALLED SERV ICEABLE GUSSET IAW EMB145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002010200039 20020102 00039 SO 2002 1 2 SIMA200131808 1 20011114 A 5320 14521725615 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 602AE 145048 ABI - THIS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. SERVICE DOOR AFT SILL CORRODED. INSTALLED SERVICEABLE SILL IA W EMB145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002010200040 20020102 00040 SO 2002 1 2 SIMA200132001 1 20011115 A 5315 14521713003 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 602AE 145048 THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. GALLEY CENTER FLOORBEAM CORRODED. REMOVED AND INSTALLED SERVICEA BLE GALLEY CENTER BEAM IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002010200041 20020102 00041 SO 2002 1 2 SIMA20013207 1 20011126 A 3210 14571035411 CAP EMB 145 EMB145LR 3260212 SO LT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 145234 ABI - THIS IS A LEVEL 3 FINDING ON A CORROSION REPAIR ITEM. LEFT AFT BEARING CAP CORRODED. REMOVED AND REPLACED BEARIN G CAP IAW EMB 145 AMM 32-10-01-801-A. (M) 2 L 7 2 4T RT T00011AT 2002010200042 20020102 00042 SO 2002 1 2 SIMA200133201 1 20011126 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 145234 DURING INSPECTION, FOUND CORROSION ON THE LEFT OMEGA AT FRAME 20. REMOVED CORROSION. FABRICATED A DOUBLER AND INSTALLE D IAW EMB 145 (SRM 145/1142 CHAPTER 53 REV 15) 53-21-10 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002010200043 20020102 00043 SO 2002 1 2 SIMA200133202 1 20011126 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 145234 DURING INSPECTION, FOUND CORROSION ON THE GALLEY CENTER OMEGA BEAM AT FRAME 20. REMOVED CORROSION. PERFORMED AN NDT IN SPECTION OF THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR DOUBLER AND INSTALLED IAW EMBRAER GST-3729/01, PARA 5 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002010200044 20020102 00044 SO 2002 1 2 SIMA200133203 1 20011126 A 5320 14529150001 CROSSBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 145234 ABI - THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. GALLEY AREA CROSSBEAM AND PROFILE CORRODED. REMOVED AND RE PLACED CROSSBEAM AND PROFILE IAW EMB SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002010200045 20020102 00045 SO 2002 1 2 SIMA200133205 1 20011126 A 5320 14522461011 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 145234 THIS IS A LEVEL 3 FINDING ON A CORROSION REPAIR ITEM. GALLEY AFT GUSSET CORRODED. REMOVED AND REPLACED GUSSET IAW EMB SRM 51-40-01. (M) 2 L 7 2 4T RT T00011AT 2002010200046 20020102 00046 SO 2002 1 2 SIMA200133206 1 20011126 A 5320 14522461011 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 145234 ABI - THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. GALLEY FORWARD GUSSET CORRODED. REMOVED AND INSTALLED SERV ICEABLE GUSSET IAW EMB SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002010200047 20020102 00047 SO 2002 1 2 SIMA200133208 1 20011126 A 3210 14571035411 CAP EMB 145 EMB145LR 3260212 SO RT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 145234 THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM CARD NR 27713. RIGHT AFT BEARING CAP CORRODED/PITTED. REMOVED AND REPLACED RIGHT MLG SWIVEL CAP, IAW EMB AMM 32-10-01-000-801-1 AND 32-10-01-400-801-A. (M) 2 L 7 2 4T RT T00011AT 2002010200048 20020102 00048 SO 2002 1 2 SIMA200133209 1 20011126 A 5320 14522459003 SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 145234 THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. GALLEY RAMP SUPPORT CORRODED. REMOVED AND INSTALLED SERVICEABLE RAMP SUPPORT IAW EMB SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002010200049 20020102 00049 SO 2002 1 2 SIMA200133210 1 20011126 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 145234 ABI - THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. GALLEY AREA CENTER BEAM GUSSET CORRODED. REMOVED AND REPLA CED GUSSET IAW EMB 145 51-40-02 AND 51-40-06. (M) 2 L 7 2 4T RT T00011AT 2002010200050 20020102 00050 SO 2002 1 2 SIMA200133211 1 20011126 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 145234 ABI - THIS IS LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. LEFT OMEGA BEAM CORRODED AT FRAME 20. REPAIRED LEFT OMEGA BE AM IAW EMB145 SRM 53-21-10 AND 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002010200051 20020102 00051 WP 2002 1 2 GTIA011145 1 20011127 A 2742 95906 MOTOR DOUG DC9 DC982 3022082 WP HORIZ STAB FAILED A GTIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 GL 23 812NK 48021 FLT 779 - LGA - PRIMARY STABILIZER TRIM STALLED, AND EXPERIENCED THERMAL SHUTDOWN TWICE ON CLIMB-OUT, AND ONCE IN LEVEL CRUISE. REMOVED AND REPLACED HORIZONTAL STAB PRIMARY LONGITUDINAL TRIM ACTUATOR MOTOR. OPS CHECK NORMAL IAW MM 27-40-0 1. (M) 2 L 7 2 4F A6WE 2002010200052 20020102 00052 WP 2002 1 2 GTIA011147 1 20011127 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 SW 21 801NK 48048 FLOOR TRACK LIGHTING AT REAR OF AIRCRAFT DETACHED FROM FLOOR. RECONNECT BROKEN WIRES FOR EMERGENCY FLOOR PATH LIGHTING, OPS CHECK OK IAW 20-50-04 MD80 MM NO DEFECTS NOTED AT THIS TIME. (M) 2 L 7 2 4F A6WE 2002010200054 20020102 00054 WP 2002 1 2 GTIA011163 1 20011103 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - RIGHT INBOARD SEAT TRACK HAS A GOUGE AT FS 1049. SEAT TRACK BEING REPLACED. (M) 2 L 7 2 4F A6WE 2002010200055 20020102 00055 WP 2002 1 2 GTIA011173 1 20011111 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - LEFT OUTBOARD FLOOR PANEL CRACKED BETWEEN STATION 380 AND 305. STOP DRILLED CRACKS. FABRICATED DOUBLERS. INSTAL LED DOUBLER IAW MD80 SRM 53-01. (M) 2 L 7 2 4F A6WE 2002010200056 20020102 00056 WP 2002 1 2 GTIA011174 1 20011114 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA O OTHER O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - PASSENGER CABIN FLOOR BOARD DAMAGED STATION 650 RIGHT SIDE. REMOVED FLOOR BOARD PANEL TO REPAIR. FABRICATED NEW FLOOR PANEL. INSTALLED FLOOR PANEL IAW MD80 MM 53-20-1. (M) 2 L 7 2 4F A6WE 2002010200057 20020102 00057 WP 2002 1 2 GTIA011175 1 20011114 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - PASSENGER CABIN STATION 1003/1079 FLOORBOARD OUTBOARD RIGHT DAMAGED. REMOVED FLOORBOARD PANEL TO REPAIR. FABRICA TE NEW FLOOR PANEL. INSTALLED FLOOR PANEL IAW MD80 MM 53-20-1. (M) 2 L 7 2 4F A6WE 2002010200058 20020102 00058 WP 2002 1 2 GTIA011176 1 20011109 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - RIGHT OUTBOARD METALLIC FLOOR PANEL, CRACKED AT STATION 460. LOCATED AND DRILLED REPAIR DOUBLER. INSTALLED DOUBL ER PER MD80 SRM 53-05. (M) 2 L 7 2 4F A6WE 2002010200059 20020102 00059 2002 1 2 SWAA013419 4 20011228 A 2565 61620428 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR DEPLOYED A SWAA K NONE O OTHER UK UNKNOWN 1 SW 07 322SW 0 23343 FWD SERVICE DOOR EVACUATION SLIDE INADVERTATLYDEPLOYED. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2002010200060 20020102 00060 NM 2002 1 2 SWAA013421 1 20011228 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 357SW 26594 DURING SCHEDULED D CHECK, FOUND 2 EA STRINGER SPLICES CRACKED, BS 907, STR 4L AND STR 4R. REMOVED AND REPLACED STRINGER SPLICE SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2002010200061 20020102 00061 NM 2002 1 2 SWAA013422 1 20011228 A 5311 6546541 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 680AA 23505 DURING SCHEDULED 1/2D CHECK, FOUND FRAME CRACKED AT 2 EA PLACES, BS 616, LBL 65 AND RBL 65, WL 200. REPAIRED FRAME PER TI-153-018. 2 L 7 2 4F RT A16WE 2002010200062 20020102 00062 NM 2002 1 2 SWAA013423 1 20011228 A 5315 6546804 BEAM BOEING 737 7373A4 1384585 NM CABIN FLOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 680AA 23505 DURING SCHEDULED 1/2D CHECK, FOUND 3 EA FLOORBEAMUPPER CHORDS CORRODED, BS 312, LBL 11 TO RBL 19, BS 328, LBL 11, AND BS 294, LBL 11 TO RBL 22. REMOVED AND REPLACED UPPER CHORD SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2002010200063 20020102 00063 NM 2002 1 2 SWAA013424 1 20011229 A 3350 101073 LENS BOEING 737 7372H4 138448C NM FWD ENTRY LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 089SW 22904 FWD ENTRY EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F A16WE 2002010200064 20020102 00064 NM 2002 1 2 SWAA013425 1 20011229 A 3350 6556633 LENS BOEING 737 7375H4 138449D NM MID CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 503SW 24180 LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2002010200065 20020102 00065 2002 1 2 SWAA013427 4 20011230 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 379SW 26586 FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2002010200066 20020102 00066 NM 2002 1 2 SWAA013429 1 20011230 A 2610 2491548 WIRE BOEING 737 7373H4 1384600 NM TAIL BROKEN A SWAA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SW 07 334SW 23938 AIR TURNBACK, APU FIRE WARNING BELL AND LIGHT ACTIVATED AT FL 110. DISCHARGE APU FIRE BOTTLE AND LIGHT WENT OUT. 2 MIN UTES LATER, LIGHT AND BELL CAME BACK ON AGAIN. FOUND BROKEN WIRE AT APU WIRE BUNDLE SI NR 2491548. REMOVED AND REPLACE D WIRE AND OPS CK GOOD PER MM. 2 L 7 2 4F RT A16WE 2002010200067 20020102 00067 WP 2002 1 2 GTIA011178 1 20011102 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT STATION Y=160 TO STA Y=200, -X7. REMOVED FLOOR SUPPORT STATION 200 TO APP ROX Y 145. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT IAW MD80 SRM 51-30. (M) 2 L 7 2 4F A6WE 2002010200068 20020102 00068 WP 2002 1 2 GTIA011179 1 20011102 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT STATION Y=200 FROM -X9 TO -X44. REMOVED FLOOR SUPPORT. FABRICATED NEW ANGLE. INSTALLED FLOOR SUPPORT IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002010200069 20020102 00069 WP 2002 1 2 GTIA011181 1 20011115 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FOUND DENT AT FS 1220 BETWEEN LONGERON 28L AND 29L, THIS DENT IS BEYOND LIMITS AND MUST BE REPAIRED. FABRICATED DOUBLER . INSTALLED PER MD80 SRM 53-04. (M) 2 L 7 2 4F A6WE 2002010200070 20020102 00070 WP 2002 1 2 GTIA011182 1 20011109 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 L-1 DOOR THRESHOLD, LIGHT CORROSION ON THRESHOLD/FLOORBOARD SUPPORT ANGLE 6 INCHES INBOARD FROM DOOR CUTOUT. REMOVED FL OOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002010200071 20020102 00071 WP 2002 1 2 GTIA011183 1 20011101 A 5320 PAN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FORWARD ENTRY AREA, FLOOR PAN CRACKED AT STATION Y 200, -X40. REMOVED DAMAGED AREA. FORMED DOUBLER. INSTALLED N EW DOUBLER IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002010200072 20020102 00072 WP 2002 1 2 GTIA011184 1 20011107 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - ANGLE SUPPORT CRACKED AT STATION Y 1322 ABOVE LONGERON 30. FABRICATED DOUBLER. STOPPED DRILLED CRACK. INSTALLED DOUBLER IAW MX80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002010200073 20020102 00073 WP 2002 1 2 GTIA011185 1 20011108 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FOUND WEB CRACKED AT STATION Y 1009, X46 INCHES. REMOVED DAMAGED AREA AT WEB STATION Y 1009. LOCATE AND DRILLED DOUBLER AND FILLER IAW MD80 SRM 53-01. INSTALLED REPAIR PARTS. (M) 2 L 7 2 4F A6WE 2002010200074 20020102 00074 WP 2002 1 2 GTIA011186 1 20011116 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FOUND STATION 160 AT BODY CENTER LINE, FLOORBOARD SUPPORT IS CORRODED. FLOORBOARD SUPPORT WAS REMOVED. LOCATED A ND DRILLED NEW ANGLE. INSTALLED ANGLE SUPPORT IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002010200075 20020102 00075 2002 1 2 GTIA011191 4 20011203 A 2210 4034238901 ACCELEROMETER DOUG DC9 DC982 3022082 WP NR 2 FAILED A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 823NK 48020 DTW - FLT 678 - AT 33,000 FT, LOST NR 2 DFGC. SWITCHED TO NR 1. OK FOR 10 SECONDS THEN LOST IT. NO FMA'S, NO FD, NO A UTO PILOT, NO AUTO THROTTLE. COMPLIED WITH ORH, NO SUCCESS. EVERYTHING CAME BACK ALL BY ITSELF AT 12,000. CHECKED STP , FOUND MANY ACCELEROMETER FAULTS. REMOVED AND REPLACED DUAL LATERAL ACCELEROMETER PER MD 80 MM 22-19-02. SYSTEM OPS C HECK GOOD. (M) 2 L 7 2 4F A6WE 2002010200076 20020102 00076 WP 2002 1 2 GTIAS011180 1 20011108 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FORWARD ENTRY AREA, FLOOR PAN CORRODED AT STATION Y200 FROM -X 10 INCHES TO -X30. REMOVED DAMAGED AREA. FABRICAT ED REPAIR PART. INSTALLED REPAIR PART IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002010200077 20020102 00077 SO 2002 1 2 SIMA200131201 1 20011107 A 3260 852701 SQUAT SWITCH EMB 145 EMB145LR 3260212 SO NLG & MLG FAULTY A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 630AE 145132 DFW - FLT 3545 - ON CLIMB-OUT, THRUST REVERSER DISAGREE MESSAGE ON EICAS. DECLARED EMERGENCY AND RETURNED TO DFW C/A RA I NOSE LANDING GEAR AND MLG AIR TO GROUND SWITCHES PART NUMBERS OFF 8-527-01 SERIAL A9940/A8147 AND PART NR ON 8-527-01 SERIAL NR'S A10750/A22001. (M) 2 L 7 2 4T RT T00011AT 2002010200078 20020102 00078 SO 2002 1 2 SIMA200131301 1 20011107 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 711PH 145235 DURING AN MBV INSPECTION, FOUND CORROSION ON THE LEFT OMEGA BEAM AT FRAME 20. REMOVED CORROSION. FABRICATED DOUBLER AN D INSTALLED IAW EMB 145 SRM 145/1142 CHAPTER 53 REV 15, 53-21-10, PAGE 201, FIG 201, SHEET 1 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT TOOO11AT 2002010200079 20020102 00079 SO 2002 1 2 SIMA200131302 1 20011108 A 5320 14522460013 GUSSET EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 711PH 145235 ABI - THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. GALLEY CENTER BEAM GUSSET CORRODED. REMOVED AND INSTALLED GALLEY CENTER BEAM GUSSET IAW EMB 135/145 SRM 51-40-02. (M) 2 L 7 2 4F RT TOOO11AT 2002010200080 20020102 00080 SO 2002 1 2 SIMA200131303 1 20011108 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 711PH 145235 THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. OMEGA BEAM AT FRAME 20 CORRODED. REPAIRED LEFT OMEGA BEAM AT FRA ME 20 IAW EMB 135, SRM 53-210 AND 51-40-02. (M) 2 L 7 2 4F RT TOOO11AT 2002010200081 20020102 00081 SO 2002 1 2 SIMA200131304 1 20011108 A 5320 BEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 711PH 145235 ABI - THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. RIGHT BEAM CORRODED AFT OF FORWARD CROSSBEAM. FABRICATED A ND INSTALLED DOUBLER IAW EMB GST-3598/01. (M) 2 L 7 2 4F RT TOOO11AT 2002010200082 20020102 00082 SO 2002 1 2 SIMA200131305 1 20011108 A 5320 BEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 711PH 145235 ABI - THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. GALLEY CENTER BEAM CORRODED. FABRICATED AND INSTALLED DOUB LER IAW EMB SRM 51-40-02 AND EMB GST 2930/01. (M) 2 L 7 2 4F RT TOOO11AT 2002010200083 20020102 00083 SO 2002 1 2 SIMA200131306 1 20011108 A 5320 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 711PH 145235 THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. LEFT SILL IN GALLEY ARM CORRODED. FABRICATED AND INSTALLED DOUBL ER IAW EMB GST-3598/01. (M) 2 L 7 2 4F RT TOOO11AT 2002010200084 20020102 00084 SO 2002 1 2 SIMA200131307 1 20011108 A 5320 14522461011 GUSSET EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 711PH 145235 ABI - THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. RIGHT BEAM AFT DIAMOND GUSSET CORRODED. INSTALLED SERVICEA BLE RIGHT AFT DIAMOND IAW EMB 135 SRM 51-40-02. (M) 2 L 7 2 4F RT TOOO11AT 2002010200085 20020102 00085 SO 2002 1 2 SIMA200131313 1 20011109 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 711PH 145235 ABI - DURING AN MBV INSPECTION, FOUND CORROSION ON THE LEFT OMEGA BEAM AT FRAME 24. REMOVED CORROSION. PERFORMED AN ND T INSPECTION OF THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED A Z REPAIR DOUBLER. REPAIR DONE IAW EMB GST 3598/0 1, PARA 8 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT TOOO11AT 2002010200086 20020102 00086 EU 2002 1 2 MALA010802 1 20011231 A 3060 BRUSH BLOCK SAAB SF340 340B 7860101 EU BROKEN A MALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 GL 15 436XJ 340B436 Left Prop Anti-ice Heat Inop in norm and max. Air return to MSP. Maintenance found broken wire on brush block, crimped on new terminal end. Ops check good. IAW Saab MM 30-61-00 2 L 7 2 4T RT A52EU 2002010200087 20020102 00087 NM 2002 1 2 2001UALA02454 1 20011222 A 5313 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 AFT PIT STATION 1480 AT STRINGER 22-23 RIGHT FRAME CORRODED AT APU GROUND WIRE CONNECTION. SUPPLEMENTAL DATA UPDATE MAJO R REPAIR ACCOMPLISHED. DAMAGED REMOVED. FILLER REPAIR DOUBLER AND FAIL SAFE CHORD INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002010200088 20020102 00088 NM 2002 1 2 2001UALA02455 1 20011223 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 FRAME AT STATION 365 WAS GOUGED BETWEEN STRINGERS 16R AND 17R. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTA LLED 'L' ANGLE DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002010200089 20020102 00089 NM 2002 1 2 2001UALA02460 1 20011224 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 AFT PIT FRAME FLANGE FROM INBOARD OF STRINGER 25L TO JUST INBOARD OF STRINGER 26L 3 EA DENTS STATION 1400. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED A FORMED FRAME REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002010200090 20020102 00090 NM 2002 1 2 ABXA010629 1 20011021 A 5410 BOLT BOEING 767 767281 1385109 NM LT STRUT IMPROPER A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 791AX 23141 STRUT FASTENERS INSTALLATION GRIP LENGTH NOT PER DWG, LEFT STRUT. REPAIRED AREA IAW REA B654-42145MR. 2 L 7 2 4F RT A1NM 2002010200091 20020102 00091 NM 2002 1 2 ABXA010644 1 20011021 A 5410 BOLT BOEING 767 767281 1385109 NM RT STRUT IMPROPER A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 791AX 23141 STRUT FASTENERS INSTALLATION GRIP LENGTH NOT PER DRAWING, RIGHT STRUT. REPAIRED AREA IAW REA B654-42146MR. 2 L 7 2 4F RT A1NM 2002010200092 20020102 00092 2002 1 2 MALA010783 4 20011122 A 3425 6226190113 COMPUTER SAAB SF340 340B 7860101 EU COCKPIT MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 450XJ 340B450 ON DEPARTURE FROM DTW ON FLIGHT 2787, A/P WOULD NOT ENGAGE. SHORTLY AFTER THE ROLL LIGHT ON BOTH EADI'S CAME ON WITH TH E AVIONICS CAUTION LIGHT. THE FO'S EADI WAS SHOWING A RIGHT 7 DEGREE TURN WHEN STRAIGHT AND LEVEL AFTER LANDING FO'S EA DI SHOWED A 3 DEGREE PITCH DOWN ATTITUDE. AIR RETURN TO DTW. MAINTENANCE COULD NOT DUPLICATED, REPLACED NR 1 AND NR 2 AHRS COMPUTER FOR PRECAUTION. P/N 622-6190-113, S/N ON 2982, S/N OFF 2964. ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2002010200093 20020102 00093 SO 2002 1 2 PNSA011106 1 20011115 A 3234 CONTROL HANDLE PIPER PA31 PA31350 7103110 SO COCKPIT MALFUNCTIONED E PNSA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 3588Z 318052130 AFTER TAKEOFF GEAR HANDLE WOULD NOT RETRACT TO NEUTRAL POSITION. GEAR UNSAFE LIGHT WAS ILLUMINATED. A/C RETURNED TO CD B MAINTENANCE BASE FOR REPAIR. 1 L 7 2 3O A20SO 2002010200094 20020102 00094 2002 1 2 PNSA011108 4 20011119 A 3425 ADI SAAB SF340 340B 7860101 EU COCKPIT MALFUNCTIONED A PNSA A UNSCHED LANDING I FLT. ATTITUDE INST. CL CLIMB 1 AL 03 695PA 340B310 DURING CLIMB COPILOTS EADI WENT BLANK, MAINTENANCE CONTACTED AND AIRCRAFT RETURNED TO ANC. ON LANDING EADI STARTED WORK ING NORMAL. MAINTENANCE SWAPPED AHARS COMPUTERS AND PERFORMED INITIAL BOX PROGRAMMING PER AMM. SUSPECT COLD WEATHER. 2 L 7 2 4T RT A52EU 2002010200095 20020102 00095 NM 2002 1 2 SWAA013338 1 20011212 A 3230 280206 FUSE BOEING 737 737301 1384611 NM NLG FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 659SW 23229 AIR TURNBACK, LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. REMOVED AND REPLACED NOSE GEAR RETRACTION FUSE PER MM, ADJU STED GROUND SPOILER INTERLOCK CABLE AND LANDING GEAR SAFETY SENSORS PER MM. 2 L 7 2 4F RT A16WE 2002010200096 20020102 00096 NE 2002 1 2 SWAA013343 2 20011215 A 7240 9978M53G COMBUSTION LINER BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 1 ENGINE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 857275 DURING SCHEDULED A2 CHECK, FOUND HOLE BURNED AT PANEL NR 3, AT NR 1 ENG COMBUSTION CHAMBER OUTER LINER, 12 O'CLOCK POS. (SIZE OF HOLE IS APPROX 3 TIMES THE SIZE OF THE NEAREST DILUTION HOLE). REMOVED AND REPLACED NR 1 ENG PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002010200097 20020102 00097 2002 1 2 SWAA013345 4 20011214 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED BC3 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002010200098 20020102 00098 NM 2002 1 2 SWAA013348 1 20011216 A 3350 20121 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 394SW 27380 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT AFT SECTION. REMOVED AND REPLACED BATTERY POWER SUPPLY PER MM. 2 L 7 2 4F RT A16WE 2002010200099 20020102 00099 2002 1 2 SWAA013350 4 20011216 A 2565 1061323 SLIDE BOEING 737 7373A4 1384585 NM L2 DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED RON, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESS INDICATION LOW. REMOVED AND REPLACED SLIDE ASSY PER M M. 2 L 7 2 4F RT A16WE 2002010200100 20020102 00100 2002 1 2 SWAA013351 4 20011217 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASS Y PER MM. 2 L 7 2 4F A16WE 2002010200101 20020102 00101 NM 2002 1 2 SWAA013354 1 20011217 A 5312 672036 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 330SW 23694 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178, BOTH LT AND RT LOWER VERTICAL WEBS CRACKED. REMOVED AND REPLACED BOTH WEB S PER SRM. 2 L 7 2 4F RT A16WE 2002010200102 20020102 00102 NM 2002 1 2 SWAA013355 1 20011218 A 3350 B99851 GUARD BOEING 737 7373T5 1384608 NM COCKPIT DEFECTIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 667SW 23063 DURING SCHEDULED C2 CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHT SWITCH GUARD NOT ARMING THE SWITCH. REMOVED AND REPLACED SWITCH GUARD PER MM. 2 L 7 2 4F RT A16WE 2002010200103 20020102 00103 NM 2002 1 2 SWAA013356 1 20011219 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/4D CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHTS INOP AT ROWS 10 ABC AND 7 ABC. REMOVED AND REPLACED L IGHT ASSY'S PER MM. 2 L 7 2 4F RT A16WE 2002010200104 20020102 00104 NM 2002 1 2 SWAA013359 1 20011219 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 394SW 27380 EEPLS INOP AT REAR SECTION. REPAIRED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002010200105 20020102 00105 NM 2002 1 2 SWAA013360 1 20011218 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 336SW 23940 FWD ENTRY WAY UPPER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002010200106 20020102 00106 NM 2002 1 2 SWAA013361 1 20011218 A 5312 6546568 WEB BOEING 737 7373A4 1384585 NM FUSELAGE BUCKLED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED C1 CHECK, FOUND BS 1019 BULKHEAD WEB BUCKLING (10 BY 5 BY .15625 DEEP), STRINGER 10L. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002010200107 20020102 00107 NM 2002 1 2 SWAA013365 1 20011220 A 5310 6584100 BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/4D CHECK, FOUND RT SIDE STRINGER 18A SHEAR BEAM CRACKED AT BS 706. REPAIRED SHEAR BEAM PER SRM. 2 L 7 2 4F RT A16WE 2002010200108 20020102 00108 NM 2002 1 2 SWAA013366 1 20011220 A 5311 963820 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD RT SIDE CHORD CRACKED, WL 207. REMOVED AND REPLACED SIDE CHORD PER S WA ACO. 2 L 7 2 4F RT A16WE 2002010200109 20020102 00109 NM 2002 1 2 SWAA013367 1 20011220 A 5315 BAC1509 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/4D CHECK, FOUND BS 860 AND BS 859, LBL 3, LONGITUDINAL BEAM CORRODED AT NUT PLATE HOLES. REPAIRED FL OORBEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2002010200110 20020102 00110 NM 2002 1 2 SWAA013368 1 20011220 A 5311 963820 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 330SW 23694 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD LT SIDE CHORD CRACKED, WL 207. REMOVED AND REPLACED CHORD PER SWA ACO. 2 L 7 2 4F RT A16WE 2002010200111 20020102 00111 EA 2002 1 2 COMA0260001 1 20011222 A 5346 6015300 BEAM CNDAIR CL600 CL6002B19 1900309 EA AFT EQUIP BAY CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 960CA 13495 7117 ENGINE SUPPORT BEAM CRACKED.REPAIRED DAMAGE I/A/W REO 601R-53-61-366. 2 L 7 2 4F RT A21EA 2002010200112 20020102 00112 EA 2002 1 2 COMA0260002 1 20011220 A 5346 6015300 BEAM CNDAIR CL600 CL6002B19 1900309 EA AFT EQUIP BAY CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 989CA 9056 7215 ENGINE SUPPORT BEAM CRACKED.REPAIRED DAMAGE I/A/W REO 601R-53-61-366. 2 L 7 2 4F RT A21EA 2002010200113 20020102 00113 EA 2002 1 2 COMA0260003 1 20011224 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 960CA 13495 7117 EDDY CURRENT INDICATES CRACKS.BLENDED OUT DAMAGE AND ROTO-PEENED I/A/W REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002010200114 20020102 00114 EA 2002 1 2 COMA0260004 1 20011228 A 5346 60135006 BEAM CNDAIR CL600 CL6002B19 1900309 EA AFT EQUIP BAY CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 954CA 14391 7100 ENGINE SUPPORT BEAM CRACK.REPAIRED DAMAGE IN ACCORDANCE WITH CANADAIR REO 601-53-61-345. 2 L 7 2 4F RT A21EA 2002010200115 20020102 00115 EA 2002 1 2 COMA0260005 1 20011222 A 5346 6015300 BEAM CNDAIR CL600 CL6002B19 1900309 EA AFT EQUIP BAY CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 960CA 13495 7117 ENGINE SUPPORT BEAM CRACKED.REPAIRED DAMAGE I/A/W REO601R-53-61-345. 2 L 7 2 4F RT A21EA 2002010200116 20020102 00116 EA 2002 1 2 COMA0260006 1 20011228 A 5320 6003603031 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FS718.0 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 713CA 7838 7245 THE L/H SIDE AFT DOUBLER AT FS718.0 WAS CRACKED BETWEEN STRINGERS 10 AND 12.REMOVED CRACKED DOUBLER AND INSTALLED A NEW DOUBLER I/A/W REO 601R-53-61-193 REV A AND WVAC EO 601R-53-2902A. 2 L 7 2 4F RT A21EA 2002010200117 20020102 00117 EA 2002 1 2 COMA0260008 1 20011228 A 5530 600210615 BUSHING CNDAIR CL600 CL6002B19 1900309 EA TOP R/H VERT STA MISLOCATED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 713CA 7838 7245 THE R/H SIDE VERTICAL STABILIZER HAS A MIGRATING BUSHING AT HORIZONTAL STABILIZER PIVOT POINT.REMOVED THE MIGRATING BUSH ING. MACHINED AND CADMIUM PLATED A NEW NOMINAL SIZE BUSHING I/A/W WVAC EO 601R-55-2910. INSTALLED THE NEW BUSHING I/A/W CRJ AMM 20-26-00-910-803. 2 L 7 2 4F RT A21EA 2002010200118 20020102 00118 EA 2002 1 2 COMA0260009 1 20011231 A 5300 600360303132 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA F.S.718.00 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 716CA 7773 7250 F.S. 718.00 STRINGER 11 R/H AND L/H AFT DOUBLERS ARE CRACKED.REMOVED AND REPLACED R/H AND L/H AFT DOUBLERS F.S. 718.00 S TRINGER 11. I/A/W CANADAIR R.E.O. 601R-53-61-193 REV A. 2 L 7 2 4F RT A21EA 2002010700052 20020107 00052 NE 2002 1 7 COMA0260010 2 20011230 A 7261 CF343A1 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LEFT LACK OF LUBE A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 912CA 10833 2 7011 807407 FLIGHT 5383 LEFT ENGINE OIL TEMP MESSAGE. SERVICED ENGINE OIL TO PROPER LEVEL. 2 L 7 2 4F 4 F RT A21EA E15NE 2002010200119 20020102 00119 EA 2002 1 2 COMA0260011 1 20011229 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 989CA 7215 FLIGHT 5400 FLAPS FAILED AT 26 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002010200120 20020102 00120 EA 2002 1 2 COMA0260012 1 20011229 A 3030 7858062 CONTROL BOX CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 785CA 5272 7326 FLIGHT 5648 L/H PITOT HEAT CAUTION MESSAGE.REPLACED THE #1 ADSHC. 2 L 7 2 4F RT A21EA 2002010200121 20020102 00121 EA 2002 1 2 COMA0260013 1 20011229 A 3040 NP1393221 WINDOW CNDAIR CL600 CL6002B19 1900309 EA L/H INOPERATIVE A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 951CA 6045 7091 FLIGHT 6086 L/H WINDOW HEAT CAUTION MESSAGE.REPLACED THE L/H COCKPIT WINDOW. 2 L 7 2 4F RT A21EA 2002010200122 20020102 00122 EA 2002 1 2 COMA0260014 1 20011228 A 2750 860D10018 FCU CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS LD LANDING 1 SO 01 796CA 5294 7338 FLIGHT 5764 FLAPS FAILED AT 30 DEGREES DURING LANDING.REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2002010200123 20020102 00123 EA 2002 1 2 COMA0260015 1 20011228 A 2910 601R751133 PUMP CNDAIR CL600 CL6002B19 1900309 EA L/H OVERTEMP A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 806CA 371 7359 FLIGHT 5951 HYDRAULIC SYSTEM #1 HIGH TEMP WARNING.REPLACED THE LEFT ENGINE HYDRAULIC PUMP. 2 L 7 2 4F RT A21EA 2002010200124 20020102 00124 NE 2002 1 2 COMA0260016 2 20011226 A 7200 CF343A1 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE L/H FAULTY A COMA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 01 912CA 10883 1 7011 807407 FLIGHT 5959 L/H ENGINE HIGH OIL TEMP AND LOW OIL PRESSURE I.F.S.D.REPLACED L/H ENGINE 2 L 7 2 4F 4 F RT A21EA E15NE 2002010200125 20020102 00125 EA 2002 1 2 COMA0260017 1 20011227 A 3150 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 710CA 7241 FLIGHT 5371 T/O CONFIG OK MESSAGE WENT OUT DURING T/O.COULD NOT DUPLICATE, ALL T/O CONFIG MESSAGE NORMAL DURING TEST. 2 L 7 2 4F RT A21EA 2002010700051 20020107 00051 EA 2002 1 7 COMA0260007 1 20011228 A 5311 6003603024 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 713CA 7838 7245 THE RT SIDE FRAME AND AFT DOUBLER AT FS 718.0 BETWEEN STRINGERS 10 AND 12 WAS CRACKED. REMOVED CRACKED SECTION OF FRAME AND AFT DOUBLER AND INSTALLED A NEW SECTION OF FRAME AND AFT DOUBLER IAW REO 601R-53-61-193 REV A AND WVAC EO 601R-53-2 902A. 2 L 7 2 4F RT A21EA 2002010200126 20020102 00126 NM 2002 1 2 SWAA013371 1 20011222 A 5315 6546804 FLOORBEAM BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED D-CHECK, FOUND CORROSION AT FLOORBEAM UPPER CHORD, BS 312, LBL 20 TO RBL 22, WL 208. REMOVED AND REPLA CED UPPER CHORD SECTION PER SRM. 2 L 7 2 4F RT A16WE 2002010200127 20020102 00127 NM 2002 1 2 SWAA013372 1 20011222 A 5313 BAC1498 STRINGER BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED D-CHECK, FOUND STRINGER 24L CORRODED, BS 500B+9. REPAIRED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2002010200128 20020102 00128 2002 1 2 SWAA013381 4 20011222 A 2565 22022901151 SLIDE BOEING 737 7372H4 138448C NM R2 DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 080SW 22675 AFT SERVICE DOOR EVACUATION SLIDE PRESS INDICATOR LOW. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2002010200129 20020102 00129 2002 1 2 SWAA013382 4 20011220 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 613SW 27931 DURING SCHEDULED C1 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2002010200130 20020102 00130 NM 2002 1 2 SWAA013383 1 20011221 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED (11 EA), STRINGER 4R, BETWEEN BS 480 AND BS 600, (2 EA) CRACKS, S TRINGER 4L, BS 520, AND (2 EA) CRACKS STRINGER 19L, BS 807. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002010200131 20020102 00131 NM 2002 1 2 SWAA013385 1 20011221 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN NOT SEATED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 394SW 27380 EEPLS INOP FROM ROW 12 AFT. RESEATED LIGHT ASSY'S AND BATTERY PACK. OPS CK GOOD PER MM. 2 L 7 2 4F RT A16WE 2002010200132 20020102 00132 NM 2002 1 2 SWAA013386 1 20011221 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 394SW 27380 EEPLS DIM BETWEEN ROWS 10 TO 14. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2002010200133 20020102 00133 NM 2002 1 2 SWAA013387 1 20011223 A 5310 6547978 CREASE BEAM BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEBS CORRODED, BS 790 RT SIDE AND BS 639 TO 663 LT SIDE. REPAIRED WEB SECTI ONS PER SRM. 2 L 7 2 4F RT A16WE 2002010200134 20020102 00134 NM 2002 1 2 SWAA013388 1 20011223 A 5320 65C27314 STRINGER CLIP BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED D-CHECK, FOUND 2 EA STRINGER CLIPS CRACKED, BS 597, STRINGERS 5L AND 7L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002010200135 20020102 00135 NM 2002 1 2 SWAA013389 1 20011223 A 5310 6546527 SHEAR TIE BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED, BS 360, BETWEEN STRINGERS 14L AND 15L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002010200136 20020102 00136 NM 2002 1 2 SWAA013394 1 20011225 A 3230 A420060283 SOLENOID BOEING 737 7373H4 1384600 NM COCKPIT FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 612SW 27930 AIR TURNBACK, AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. REMOVED AND REPLACED LANDING GEAR LEVER LATCH SOLENOID. OP S CHECK GOOD PER MM. 2 L 7 2 4F RT A16WE 2002010200137 20020102 00137 EA 2002 1 2 SWIA200110406 1 20011130 A 5270 STRAP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 416SW 7089 CLIMBING THROUGH 27,000 FEET CABIN DOOR LATCH CAUTION. FOLLOWED QRH. AT 30,000 FT PASSENGER DOOR WARNING. INITIATED D ESCENT AND RETURNED TO SLC. REPLACED DOOR BONDING STRAP AND OPS CHECKED DOOR WARNING SYSTEM IAW CRJ MM 52-70-04. OPS C HECK GOOD. 2 L 7 2 4F RT A21EA 2002010200138 20020102 00138 EA 2002 1 2 SWIA200110494 1 20011227 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA RT OB SPOILERON MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED UK UNKNOWN 1 NM 07 426SW 7468 RIGHT OUTBOARD SPOILERON MESSAGE. CIRCUIT BREAKER IS POPPED FOR PCU. REMOVED AND REPLACED RIGHT OUTBOARD SPOILERON PCU , REF. MM 27-62-01. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002010200139 20020102 00139 EA 2002 1 2 SWIA200110495 1 20011230 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA RIGHT BROKEN A SWIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 07 408SW 7055 RIGHT WINDSHIELD BROKEN DURING TAXI BEHIND A B737.REMOVED AND REPLACED RIGHT WINDSHIELD IAW CRJ MM 56-11-01. P/N: NP-1 39321-10 S/N ON: 01208H4243 2 L 7 2 4F RT A21EA 2002010200140 20020102 00140 CE 2002 1 2 GLBA2001242 1 20011227 A 7700 1143800653 INDICATOR BEECH 1900 1900D 1154162 CE #2 ERRATIC A GLBA D RETURN TO BLOCK O OTHER CR CRUISE 1 NM 03 170GL 10950 3702 UE170 RIGHT ENGIN TORQUE INDICATOR ERRATIC, REPLACED INDICATOR OPS CHECKED SYSTEM SATISFACTORY 2 L 7 2 4T RT A24CE 2002010200141 20020102 00141 CE 2002 1 2 GLBA2001244 1 20011230 A 5700 10038100511 FUEL CAP BEECH 1900 1900D 1154162 CE RIGHT O/B WING LEAKING A GLBA D RETURN TO BLOCK K FLUID LOSS CL CLIMB 1 NM 03 195GL UE195 LEFT O/B FUEL CAP LEAKING, REPLACED FUEL CAP 2 L 7 2 4T RT A24CE 2002010200142 20020102 00142 2002 1 2 GLBA2001245 4 20011230 A 3400 MS21253347 SWITCH BEECH 1900 1900D 1154162 CE INTERMITTENT A GLBA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 03 151GL UE151 RANDOM OVERSPEED WARNING, RESEATED P450 CONNECTOR AND REPLACED STALL WARNING TEST SWITCH OPS CHECKED SYSTEM SATISFACTORY 2 L 7 2 4T RT A24CE 2002010200143 20020102 00143 EU 2002 1 2 AWXA200100677 1 20011229 A 5270 D5237128000200 HANDLE AIRBUS 320 A320231 3930325 EU AFT CARGO DOOR NOT SEATED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 629AW 076 LAX - ABORTED TAKEOFF - FLT 702 - "C" - WHEN INITIATING TAKEOFF FLIGHT CREW RECEIVED AN AFT CARGO DOOR WARNING LIGHT IND ICATION, TAKEOFF WAS ABORTED WITHOUT INCIDENT AND AIRCRAFT RETURNED TO THE GATE. AT THE GATE MAINTENANCE INSPECTED THE A FT CARGO DOOR AND FOUND THE HANDLE WAS NOT FULLY LATCHED. MAINTENANCE SECURED THE HANDLE TO THE LOCKED POSITION AND THE LIGHT EXTINGUISHED, THE DOOR HANDLE WAS CYCLED SEVERAL TIMES AND OPERATIONALLY CHECKED GOOD. 2 L 7 2 4F RT A28NM 2002010200144 20020102 00144 NM 2002 1 2 AWXA200100678 1 20011230 A 3510 RCF6708 REGULATOR AIRBUS A319 A319132 3930340 NM ZONE 125 FAULTY A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 807AW 9276 3781 1064 CMH - DIVERSION - FLT 820 - "C" - WHILE ENROUTE FROM PHX TO BOS FLIGHT CREW RECEIVED LOWER ECAM WARNING MESSAGE THAT OXY GEN REGULATOR PRESSURE WAS LOW SHORTLY AFTER PILOT TESTED MASK. FLIGHT WAS DIVERTED TO CMH WHERE AIRCRAFT MADE AN UNEVEN TFUL LANDING. AT CMH MAINTENANCE REPLACED BOTH THE CREW OXYGEN BOTTLE IAW T/C R2A35301, AND THE CREW OXYGEN REGULATOR IA W AMM 35-13-15-04. LEAK CHECK OF THE OXYGEN BOTTLE, MASK, AND HOSES WAS GOOD WITH NO LEAKS NOTED. PART NAME: CYLINDER, O XYGEN, MANF: INTERTECHNIQUE, P/N: 891511-14, COND: DEPLEATED, LOC: ZONE 125. 2 L 7 2 4F RT A28NM 2002010300001 20020103 00001 NM 2002 1 3 ABXA010643 1 20010930 A 5740 FITTING BOEING 767 767281 1385109 NM RT WING DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 791AX 23141 DURING THE SIDE LINK FITTING REPLACEMENT ON THE RIGHT WING, DISCOVERED THAT TWO EXISTING ATTACHMENT HOLES WERE ALREADY S ECOND OVERSIZED, WHILE SERVICE BULLETIN ALLOWED THE HOLES TO BE ENLARGED (AFTER COLDWORK) TO A MAXIMUM OF SECOND OVERSIZ E. ONE OF THE HOLES WAS ELONGATED. REPAIRED AREA IAW REA B653-41461MR. 2 L 7 2 4F RT A1NM 2002010300002 20020103 00002 NM 2002 1 3 VNAA0112020 1 20011228 A 5200 DOOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 459PS 3070 WHILE IN CRUISE, THE CREW RECEIVED A RED WARNING PANEL DOOR LIGHT. THE SYSTEMS PAGE SHOWED IT WAS THEMAIN CABIN DOOR. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND DIVERTED TO TRI. OUTSTATION MAINTENANCE FOUND NO DEFECTS SO THE AI RCRAFT WAS FERRIED TO P IT WHERE MAINTENANCE INSPECTED THE AIRCRAFT IN ACCORDANCE WITH DORNIER MAINTENAN CE MANUAL 52-00 -00. NO DEFECTS WERE FOUND AND THE PROBLEM COULD NOT BE DUPLICAT ED. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WASRELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002010300003 20020103 00003 NM 2002 1 3 VNAA0112018 1 20011225 A 3300 321473 POWER SUPPLY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE 5LK FAILED A VNAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 429JS 14893 3043 THE CREW REPORTED THATTHE EMERGENCY LIGHTING STRIP AT ROWS 3-6 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACE D THE EMERGENCY POWER SUPPLY IN ACCORDANCE WITH DORNIER MAINTE NANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS R ELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002010300004 20020103 00004 NM 2002 1 3 SWAA013396 1 20011225 A 3350 20121 POWER SUPPLY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 395SW 27689 DURING SCHEDULED RON, FOUND EEPLS INOP IN AFT SECTION. REMOVED AND REPLACED POWER SUPPLY PER MM. 2 L 7 2 4F RT A16WE 2002010300005 20020103 00005 NM 2002 1 3 VNAA0112014 1 20011220 A 7900 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 328JS 3030 WHILE ENROUTE TO AZO,FLIGHT 4169 RECEIVED A LEFT HAND ENGINE HIGH OIL PRESSURE INDICATION, FOLLOWED THE QUICK REFERENCE HANDBOOK AND DIVERTED TO TOL. MAINTENANCE INSPECTED AND CLEA NED THE OIL PRESSURE SENSOR IN ACCORDANCE WITH DORNIER MA INTENANCE MANUAL 79-00- 00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE . 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002010300006 20020103 00006 2002 1 3 SWAA013397 4 20011224 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM L1 DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 317WN 24068 FWD ENTRY DOOR EVACUATION SLIDE OUT OF ADJUST. READJUSTED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2002010300007 20020103 00007 NM 2002 1 3 VNAA0112016 1 20011221 A 2400 DTSP4OOL BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RH FAILED A VNAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 457PS 2683 3048 THE CREW RECEIVED A NUMBER 2 BATTERY OVERHEAT MESSAGE AND RETURNED TO THE FIELD. MAINTENANCE INSPECTED AND REPLACED THE MAIN BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAF T WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002010300008 20020103 00008 NM 2002 1 3 SWAA013398 1 20011224 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 394SW 27380 EEPLS TRACK COVERS LOOSE. REINSTALLED COVERS PER MM. 2 L 7 2 4F RT A16WE 2002010300009 20020103 00009 NM 2002 1 3 VNAA0112017 1 20011223 A 3600 BLEED VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 424JS 3033 DURING TAKE OFF THE CREW RECEIVED A BLEED VALVE SHUTOFF FAIL MESSAGE AND ABORTED TAKE OFF. THE CREW CALLED MAINTENANCE CONTROL AND RESET THE SYSTEM. FLIGHT 4062 WAS CLEARED FOR ANOTHER TAKE OFF ATTEMPT AND DEPARTED WITH NO FURTHER INCIDEN TS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002010300010 20020103 00010 NM 2002 1 3 SWAA013399 1 20011223 A 2612 100102401 CONTROL UNIT BOEING 737 7373Q8 1384670 NM CARGO BAY FAULTY A SWAA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SW 07 685SW 23401 AFT CARGO COMPT FIRE WARNING BELL SOUNDED AND DISCHARGED FIRE BOTTLE IN AFT CARGO COMPT. C/W WITH INSPECT AND FOUND NO INDICATION OF OF SMOKE OR FIRE DAMAGE. DEFERRED SYS AND INOP BOTH CARGO COMPT'S PER MEL. LATER DURING RON, REMOVED AND REPLACED BOTH FIRE BOTTLES AND DIVERTER VALVE ASSY. REMOVED AND REPLACED FWD SMOKE DETECTOR, AND REMOVED AND REPLACED CCU PER MM. 2 L 7 2 4F RT A16WE 2002010300011 20020103 00011 2002 1 3 SWAA013401 4 20011224 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 398SW 27692 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2002010300012 20020103 00012 2002 1 3 SWAA013403 4 20011224 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM L2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 AFT ENTRY DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2002010300013 20020103 00013 NM 2002 1 3 SWAA013404 1 20011226 A 3260 6555797 UPLOCK SENSOR BOEING 737 7373H4 1384600 NM LT MLG FAILED A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 321SW 23342 AIR TURNBACK, AFTER GEAR RETRACTION, LT RED MLG LIGHT ILLUMINATED. REMOVED AND REPLACED LT MLG UPLOCK SENSOR PER MM. 2 L 7 2 4F RT A16WE 2002010300014 20020103 00014 NM 2002 1 3 SWAA013407 1 20011226 A 5310 6547978 CREASE BEAM BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CORRODED, BS 867 AND BS 887, LT SIDE. REPAIRED CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 2002010300015 20020103 00015 NM 2002 1 3 SWAA013409 1 20011224 A 2612 100064901 FIRE DETECTOR BOEING 737 7373Q8 1384670 NM CARGO BAY FAULTY A SWAA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SW 07 685SW 23401 DECLARED EMERGENCY, AFT CARGO COMPT FIRE WARNING LIGHT ILLUMINATED AND FIRE BOTTLE WAS DISCHARGED. AFTER LANDING NO SIG N OF SMOKE OR FIRE FOUND. DEFERRED CARGO FIRE SYS AND INOP BOTH CARGO COMPTS PER MEL. LATER ON DURING RON REMOVED AND REPLACED BOTH FIRE BOTTLES. REMOVED AND REPLACED DIVERTED VALVE. REMOVED AND REPLACED OVERHEAD CARGO FIRE PANEL, AND REMOVED AND REPLACED CCU'S MODULE PER MM. AFTER DOWN LOADING CCU FOUND 3 EA AFT CARGO COMPT FIRE DETECTORS FAULTY. RE MOVED AND REPLACED SAME PER MM. OPS CK GOOD. 2 L 7 2 4F RT A16WE 2002010300016 20020103 00016 NM 2002 1 3 SWAA013410 1 20011227 A 3350 6104781 BATTERY BOEING 737 7372H4 138448C NM CARGO BAY DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED SERVICE CHECK, FOUND RT EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2002010300017 20020103 00017 NM 2002 1 3 SWAA013412 1 20011226 A 5330 6545772 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED SPECIAL VISIT, FOUND 5 CRACKS AT FUSELAGE EXTERNAL SKIN, BS 500B TO BS 832, STRINGER 10R. REPAIRED SKI N PER SRM AND SWA RA. 2 L 7 2 4F RT A16WE 2002010300018 20020103 00018 NM 2002 1 3 SWAA013413 1 20011226 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 355SW 25250 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY BULLNOSE LIGHT LOOSE AT ROW 3 ABC. REMOVED AND REPLACED RETAINER ASSY PER MM . 2 L 7 2 4F RT A16WE 2002010300019 20020103 00019 2002 1 3 SWAA013414 4 20011226 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM L2 DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 663SW 23256 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2002010300020 20020103 00020 NM 2002 1 3 SWAA013415 1 20011227 A 5310 6546552 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 680AA 23505 DURING SCHEDULED 1/2D CHECK, FOUND BELTFRAME SHEAR TIE CORRODED, BS 842, BETWEEN STRINGER 28L AND 28R. REPAIRED SHEAR T IE PER SRM. 2 L 7 2 4F RT A16WE 2002010300021 20020103 00021 NM 2002 1 3 SWAA013416 1 20011227 A 5315 6546804 FLOORBEAM BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 680AA 23505 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED, BS 986.5, LBL 16.5. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 2002010300022 20020103 00022 NM 2002 1 3 SWAA013418 1 20011229 A 2612 6566207 FIRE LOOP BOEING 737 7373H4 1384600 NM APU ERRATIC A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 334SW 23938 AIR TURNBACK, AFTER APU SHUT DOWN, APU FIRE WARNING BELL ACTIVATED, CK LIST WAS C/W AND WARNING WENT OFF, THEN CAME ON S EVERAL TIMES BEFORE LANDING. C/W APU COMPT INSPECTION, NO DEFECTS FOUND, DEFERRED APU PER MEL. LATER DURING RON AT OAK , APU FIRE DETECT MX FAULT TEST FAILED. REMOVED AND REPLACED APU FIRE CONTROL PANEL AND FIRE DETECT UNIT WITH NO HELP. REINSTALLED ORIGINAL EQUIPMENT, TESTED APU FIRE DETECT LOOP AND CLEANED LOOP CONNECTOR. OPS CK GOOD PER MM. 2 L 7 2 4F RT A16WE 2002010300023 20020103 00023 NM 2002 1 3 SWAA013420 1 20011228 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 357SW 26594 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CORRODED, BS 616 TO BS 639 RT SIDE. REPAIRED BEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2002010300024 20020103 00024 NM 2002 1 3 SWAA013426 1 20011229 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 743SW 29279 DURING SCHEDULED PM CHECK, FOUND 12 EEPLS INOP. RECONNECTED EEPLS WIRING AND REMOVED AND REPLACED LIGHT TRACKS PER MM. 2 L 7 2 4F RT A16WE 2002010300026 20020103 00026 EA 2002 1 3 SWIA200110394 1 20011125 A 2721 TRIM TAB CNDAIR CL600 CL6002B19 1900309 EA RUDDER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 439SW 7578 CLIMBING OUT OF SLC, THE A/C CONTINUALLY YAWED L/R, NO MESSAGES. THE ONLY WAY TO STOP THE YAW WAS TO ADD RT RUDDER. IN SPECTED RUDDER TRIM SYSTEM IAW CRJ MM 27-22-00. NO DEFECTS NOTED. SYSTEM OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002010300027 20020103 00027 SO 2002 1 3 SWIA200110437 1 20011208 A 2131 CONTROLLER EMB 120 EMB120ER 3260203 SO CABIN PRESSURE MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 213SW 120277 CLIMBING THROUGH 9,000, CABIN RATE CLIMBED TO 2,000 FPM, THEN A DESCENT TO 1500 FPM. AT 11,000, PRESSURE DIFFERENTIAL W ENT TO ZERO. THE CABIN ALT LIGHT ON THE MAP ILLUMINATED. PERFORMED THE QRH PROCEDURE. THE MANUAL MODE DID NOT WORK EI THER. UPON RETURN TO CODY, TRIED TO PRESSURIZE ON THE GROUND BUT HAD NO RESPONSE. VISUAL INSPECTION OF CARGO AND FORWA RD DOOR SEALS DID NOT PRESENT ANY IRREGULARITIES. PRESSURIZED SYSTEM. OPS CHECKED GOOD ON GROUND. 2 L 7 2 4T RT A31SO 2002010300028 20020103 00028 SO 2002 1 3 SWIA200110439 1 20011213 A 3231 SV14H11004 SOLENOID VALVE EMB 120 EMB120ER 3260203 SO NLG DOOR FAILED A SWIA L A ABORTED APPROACH UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 NM 07 213SW 120277 ON MISSED APPROACH CLIMBOUT IN JAC, SELECTED GEAR UP. THE GEAR DID NOT RETRACT. RAN QRH PROCEDURE AND CYCLED GEAR HAND LE. GEAR DID NOT RETRACT, STILL INDICATED SIX RED DISAGREEMENT AND SIX GREEN DOWNLOCKED INDICATION LIGHTS. PLACED HAND LE IN DOWN POSITION AND DIVERTED TO COD WITH GEAR EXTENDED. SWUNG GEAR AND COULD NOT DUPLICATE. REMOVED AND REPLACED T HE FORWARD LANDING GEAR DOORS SOLENOID VALVE IAW EMB MM 32-33-01. OPS CHECK GOOD, LEAK CHECK GOOD. 2 L 7 2 4T RT A31SO 2002010300029 20020103 00029 SO 2002 1 3 SWIA200110440 1 20011212 A 3150 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT FALSE ACTIVATION A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 229SW 120305 ABORTED TAKEOFF DUE TO TAKEOFF AURAL WARNING. AURAL WARNING CB FOUND POPPED. COMPLIED WITH TEST OF AURAL WARNING UNIT PER EMB MM 31-53-00. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 2002010300030 20020103 00030 SO 2002 1 3 SWIA200110441 1 20011214 A 3260 WIRE HARNESS EMB 120 EMB120ER 3260203 SO RT MLG DEFECTIVE A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 295UX 120295 RIGHT MAIN B-GREEN LANDING GEAR INDICATION REMAINS ILLUMINATED WITH GEAR UP. RETURNED TO SFO. REMOVED AND REPLACED UPL OCK HARNESS AND SENSOR. SWUNG GEAR SEVERAL TIMES, ALL CHECKS GOOD IAW EMB 120 32-61-01. 2 L 7 2 4T RT A31SO 2002010300031 20020103 00031 SO 2002 1 3 SWIA200110442 1 20011213 A 3010 LIGHT EMB 120 EMB120ER 3260203 SO COCKPIT INOPERATIVE A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 212SW 120276 LEFT DEICE LIGHT INOP. FLYING INTO ICING CONDITIONS, DIVERTED TO SMF. RELAMPED THE LEFT DEICE LIGHT. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002010300032 20020103 00032 SO 2002 1 3 SWIA200110444 1 20011212 A 2497 WIRE EMB 120 EMB120ER 3260203 SO ELECTRICAL SYS BURNED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 209SW 120269 WIRE W110-2230-16N IS BURNED AT CANNON PLUG P0952 PIN 43 TO GROUND. INSPECTED SURROUNDING WIRING AND REPLACED BURNED WI RE IAW WM 20-00-00.` 2 L 7 2 4T RT A31SO 2002010300033 20020103 00033 NM 2002 1 3 SWAA013430 1 20011229 A 5311 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 680AA 23505 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002010300034 20020103 00034 NM 2002 1 3 SWAA013431 1 20011227 A 5330 6545767 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE. CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 468, UNDER NR 1 DME ANTENNA. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002010300035 20020103 00035 NM 2002 1 3 SWAA013433 1 20011230 A 5312 6516300 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 388SW 26591 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 5.4 7 WL 201. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002010300036 20020103 00036 NM 2002 1 3 SWAA013436 1 20011230 A 5312 6516300 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 388SW 26591 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, RBL 5.4, WL 201 AND WL 198. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002010300037 20020103 00037 NM 2002 1 3 SWAA013437 1 20011229 A 3350 6556633 LENS BOEING 737 7373A4 1384585 NM FUSELAGE LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 680AA 23505 DURING SCHEDULED 1/2D CHECK, FOUND LT OVERWING EMERGENCY LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2002010300038 20020103 00038 NM 2002 1 3 SWAA013440 1 20011231 A 5754 6573714 SLAT BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 311SW 23333 DURING SCHEDULED C3 CHECK, FOUND NR 4 L/E SLAT CRACKED (2 EA) ON LOWER T/E RIVET ROW ADJACENT TO OTBD AUX TRACK. REPAIR ED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2002010300039 20020103 00039 NM 2002 1 3 SWAA013441 1 20011230 A 5330 6545765 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 8, STR 10R. REPAIRED SKIN PER SWA RA. 2 L 7 2 4F RT A16WE 2002010300040 20020103 00040 NM 2002 1 3 SWAA013442 1 20011230 A 5330 6545774 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 727D AND BS 727E, STR 20L. REPAIRED SKIN PER SRM AND SWA RA. 2 L 7 2 4F RT A16WE 2002010300041 20020103 00041 2002 1 3 SWIA200110445 4 20011215 A 3425 INDICATOR EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 586SW 120354 HDG FLAG ON NR 1 AND NR 2 EHSI'S EN ROUTE TO CPR. RAN QUICK REFERENCE HANDBOOK PROCEDURES, FLAGS STILL ON. RETURNED TO SLC. PERFORMED FUNCTIONAL CHECK OF AHRS. NO DISCREPANCIES NOTED. AHRS OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002010300042 20020103 00042 2002 1 3 SWIA200110447 4 20011213 A 3425 6226190204 COMPUTER EMB 120 EMB120ER 3260203 SO NR 1 MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 212SW 120276 RUDDER TRIM INEFFECTIVE WITH YAW ENGAGED. RUDDER KICKS OVER WHEN DISENGAGED. REPLACED NR 1 AHRS. SYSTEM OPS CHECKS GO OD IAW 22-10-00/34-25-00. P/N ON 622-6190-214, S/N ON 1359, S/N OFF 2792. 2 L 7 2 4T RT A31SO 2002010300043 20020103 00043 2002 1 3 SWIA200110449 4 20011214 A 3425 COMPUTER EMB 120 EMB120RT 3260202 SO NR 1 MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 137H 120137 CAPTAIN'S ADI WENT BLANK INTERMITTENTLY WITH ATT FLAG, SIMULTANEOUSLY A/P FAILED WITH RED FAILURE CAPTIONS ON CAPTAIN'S FCP AND AUTOPILOT PANEL WITH ASSOCIATED AUTOPILOT FAIL FLAG ON MAP. DIVERTED TO OXR IN VMC CONDITIONS 2255 Z. REINITIA LIZED NR 1 AHARS. CAPT'S ADI AND AUTOPILOT OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2002010300044 20020103 00044 SO 2002 1 3 SWIA200110450 1 20011217 A 2131 CONTROLLER EMB 120 EMB120ER 3260203 SO CABIN PRESSURE MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 216SW 120285 AFTER TAKEOFF, CABIN PRESSURE DIFFERENTIAL INCREASED TO 5 PSI AND CABIN ALTITUDE DROPPED TO 0 MSL. COULD NOT CONTROL WI TH MANUAL CONTROLLER. RETURNED TO SLC. PERFORMED OPERATIONAL CHECK OF MANUALLY CONTROLLED OUTFLOW VALVE IAW MM 21-30-0 0. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002010300045 20020103 00045 SO 2002 1 3 SWIA200110451 1 20011217 A 3397 WIRE EMB 120 EMB120ER 3260203 SO CABIN CHAFED A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 227SW 120304 EMERGENCY LIGHTS CIRCUIT BREAKER B-19 TRIPPED, WOULD NOT RESET. INSULATED CHAFED WIRING AT FLIGHT ATTENDANT EMERGENCY L IGHT SWITCH. EMERGENCY LIGHTS OPERATED NORMALLY. 2 L 7 2 4T RT A31SO 2002010300046 20020103 00046 SO 2002 1 3 SWIA200110452 1 20011214 A 5210 SWITCH EMB 120 EMB120ER 3260203 SO PAX DOOR INTERMITTENT A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 188SW 120039 CABIN DOOR STAYS HYDRAULICALLY PRESSURIZED INTERMITTENTLY AND WILL NOT OPEN. FLIGHT ATTENDANT CABIN DOOR BUTTON NEEDED TO BE TOGGLED TO RELEASE PRESSURE. REMOVED AND REPLACED CABIN PASSENGER DOOR CONTROL SWITCH AT F/A STATION. OPS CHECKS GOOD IAW MM 52-10-00. 2 L 7 2 4T RT A31SO 2002010300047 20020103 00047 SO 2002 1 3 SWIA200110453 1 20011217 A 2752 3203001007 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP FAILED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 188SW 120039 FLAP DISAGREEMENT OUTBOARD AFTER TAKEOFF. FLAPS RETRACTED AFTER QRH PROCEDURE. REMOVED AND REPLACED LEFT OUTBOARD FLAP ACTUATOR. OPS CHECKS GOOD. LEAK CHECKS GOOD IAW MM 27-50-09. 2 L 7 2 4T RT A31SO 2002010300048 20020103 00048 SO 2002 1 3 SWIA200110454 1 20011213 A 2752 3431001001 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP FAILED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 NM 07 213SW 120277 FLAP DISAGREEMENT UPON SELECTION OF FLAPS TO 45 DEGREES. REMOVED AND REPLACED LEFT NACELLE FLAP ACTUATOR IAW EMB MM 27- 50-00. OPS CHECK, LEAK CHECK GOOD. 2 L 7 2 4T RT A31SO 2002010300049 20020103 00049 SO 2002 1 3 SWIA200110455 1 20011219 A 3010 BOOT EMB 120 EMB120ER 3260203 SO HORIZ STAB FAILED A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 271YV 120271 LEFT AND RIGHT OUTBOARD STAB DEICE BOOTS FAILED INFLIGHT, BOTH TIMERS. REPLACED BAD LEFT STABILIZER DEICE BOOT PER MM 3 0-10-00. DEICE SYSTEM OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002010300050 20020103 00050 SO 2002 1 3 SWIA200110456 1 20011215 A 2752 CONNECTOR EMB 120 EMB120ER 3260203 SO FLAP ACTUATOR DIRTY A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 215SW 120281 FLAP DISAGREEMENT ON AFTER TAKEOFF FLAP RETRACTION. REQUIRED QRH PROCEDURE TO CORRECT. INSPECTED FLAP. CLEANED CONNEC TORS FROM ACTUATOR CANNON PLUGS. RAN FLAPS SEVERAL TIMES. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2002010300051 20020103 00051 EA 2002 1 3 SWIA200110457 1 20011215 A 3411 0856KU9 PROBE CNDAIR CL600 CL6002B19 1900309 EA PITOT/STATIC SYS FAULTY A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 407SW 7034 ACCELERATING THROUGH 250 KIAS AT 10,000 FT, ALTIMETERS FLAGGED AND HAD 150 FT DIFFERENCE. AIRSPEED INDICATORS HAD A 5 K NOT SPLIT. AFTER REDUCING AIRSPEED BACK TO AROUND 250 KIAS ALTIMETERS CAME BACK WITHIN TOLERANCE. REMOVED AND REPLACED NR 1 PITOT/STATIC PROBE IAW 34-11-01. OPS AND LEAK CHECKS GOOD. P/N: 0856KU9, S/N OFF: 143377. 2 L 7 2 4F RT A21EA 2002010300052 20020103 00052 SO 2002 1 3 SWIA200110458 1 20011218 A 3010 BOOT EMB 120 EMB120ER 3260203 SO HORIZ STAB DAMAGED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 271YV 120271 OUTBOARD LEFT AND RIGHT STABILIZER DEICE BOOTS FAILED INFLIGHT, BOTH TIMERS. INSTALLED PATCH ON LEFT OUTBOARD STAB DEIC E BOOT. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002010300053 20020103 00053 SO 2002 1 3 SWIA200110460 1 20011121 A 5320 STIFFENER EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 199SW 120237 1ST CROSS MEMBER AFT OF THE PASSENGER DOOR HAS INTERGRANULAR CORROSION. REMOVED AND REPLACED THE CORRODED CROSS MEMBER IAW EMB SRM 51-00-00 & 51-40-02. 2 L 7 2 4T RT A31SO 2002010300054 20020103 00054 SO 2002 1 3 SWIA200110461 1 20011121 A 5410 CHANNEL EMB 120 EMB120ER 3260203 SO LT NACELLE WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 199SW 120237 LEFT NACELLE OUTBOARD J-CHANNEL HAS DEEP GROOVES AT AFT END OUTBOARD OF AFT GEAR DOOR AREA. REPLACED J-CHANNEL REPAIR S ECTION IAW EMB TECH. SUPPORT ENGINEERING APPROVAL, REF SST-1003/97 AND EMB120 SRM 51-40-02. 2 L 7 2 4T RT A31SO 2002010300055 20020103 00055 SO 2002 1 3 SWIA200110463 1 20011121 A 5320 INTERCOSTAL EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 199SW 120237 COCKPIT, CRACK IN INTERCOSTAL LOCATED AFT OF CAPTAIN'S SLIDING WINDOW AFT FRAME AT APPROXIMATE HEIGHT OF OVERHEAD SPEAKE R. FABRICATED AND INSTALLED DOUBLER FOR THE CRACKED INTERCOSTAL IAW EMB SRM 51-70-05. 2 L 7 2 4T RT A31SO 2002010300056 20020103 00056 2002 1 3 SWIA200110464 4 20011218 A 3417 8220372140 ADC CNDAIR CL600 CL6002B19 1900309 EA NR 1 FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 417SW 7400 NR 1 ADC FAILED EN ROUTE. RECEIVED IAS FLAG ON CAPTAIN'S SIDE ASSOCIATED WITH EFIS COMP MON MESSAGE. REMOVED AND REPLA CED NR 1 ADC. OPS CHECK GOOD IAW 34-13-01. 2 L 7 2 4F RT A21EA 2002010300057 20020103 00057 NE 2002 1 3 SWIA200110465 2 20011214 A 7321 EEC EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 294SW 120321 ABORTED ON TAKEOFF ROLL DUE TO LEFT EEC FAILURE AT ABOUT 30 PERCENT TORQUE. OPERATIONALLY CHECKED LEFT ENGINE WITH EEC ON. NO DEFECTS NOTED. COMPLETED ENGINE TRIM IAW MM 71-00-00. ENGINE AND EEC OPERATED NORMALLY. 2 L 7 2 4T 4 T RT A31SO E20NE 2002010300058 20020103 00058 2002 1 3 SWIA200110466 4 20011221 A 2210 AUTOPILOT SYS CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 720SW 7297 AIRCRAFT DISPLAYED DUTCH ROLL TENDENCIES AT FL330 AT .77 MACH. OSCILLATED 1-2 DEGREES LEFT AND RIGHT WITH 3-4 SECONDS I NTERVALS, SKID INDICATOR MOVED APPROXIMATELY 1/8 LENGTH LEFT AND RIGHT. TROUBLESHOT THE SYSTEM IAW MM 22-22-01 AND 22-2 2-04. EVERYTHING CHECKS GOOD AT THIS TIME. COULD NOT DUPLICATE DISCREPANCY AT THIS TIME. 2 L 7 2 4F RT A21EA 2002010300059 20020103 00059 EA 2002 1 3 SWIA200110467 1 20011223 A 2750 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 594SW 7285 FLAPS FAILED AT 11 DEGREES DURING FLAP RETRACTION. REMOVED AND REPLACED LEFT BPSU IAW 27-51-10. ADJUSTED POTENTIOMETER S 6 AND 7 (6 FROM -0.019 TO 0.011; 7 FROM -0.013 TO 0.011). OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002010300060 20020103 00060 EA 2002 1 3 SWIA200110468 1 20011224 A 2750 860D10018 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 594SW 7285 AFTER LEVELING OFF AT FL330, FLAPS FAIL CAUTION MESSAGE ILLUMINATED. REPLACED FECU PER MM 27-51-05. OPS CHECK OF SYSTE M GOOD. 2 L 7 2 4F RT A21EA 2002010300061 20020103 00061 NM 2002 1 3 SWAA013435 1 20011228 A 5210 6545871 FRAME BOEING 737 7373A4 1384585 NM FWD ENTRY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 during scheduled 1/2d check, found forward entry door frame cracked (3 ea) at aft stop pin cutout Nr 5, 6, 7. repaired door frame per srm. 2 L 7 2 4F RT A16WE 2002010300062 20020103 00062 EA 2002 1 3 SWIA200110469 1 20011225 A 3411 PITOT LINE CNDAIR CL600 CL6002B19 1900309 EA NR 2 SYSTEM CONTAMINATED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 595SW 7292 ABORTED TAKEOFF DUE TO EFIS COMP MON MESSAGE AND 60 KTS DISCREPANCY IN AIRSPEED. (CAT II). FOUND MOISTURE IN PITOT SYS TEM NR 2. PERFORMED CONTAMINATION REMOVAL, PURGE AND LEAK TEST PROCEDURES FOR SYSTEMS P1, P2 & P3 IAW MM 34-11-00. FUN CTIONAL TEST GOOD OF ALL SYSTEMS IAW MM TASK 34-11-00-720-804. 2 L 7 2 4F RT A21EA 2002010300063 20020103 00063 EA 2002 1 3 SWIA200110470 1 20011224 A 2742 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB FAILED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 589SW 7072 STAB TRIM AND MACH TRIM DISCONNECT WHEN RUNNING TRIM UP AND DOWN. (CAT II). REMOVED AND REPLACED STAB TRIM ACTUATOR. REMOVED AND REPLACED MOTOR CONTROL UNIT IAW WITH 27-42-01 AND 27-42-05. OPS CHECKS GOOD. STAB TRIM UNIT P/N 8391-3, S /N OFF 254. 2 L 7 2 4F RT A21EA 2002010300064 20020103 00064 SO 2002 1 3 SWIA200110471 1 20011121 A 5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 567SW 120342 FLOOR CROSS BRACE ON RIGHT SIDE PITTED BEYOND LIMITS AT STATION 38.5. REPLACED FLOOR CROSS BRACE ON RIGHT SIDE AT STATI ON 38.5 IAW SRM 53-20-10 WITH SERVICEABLE PART. 2 L 7 2 4T RT A31SO 2002010300065 20020103 00065 SO 2002 1 3 SWIA200110472 1 20011121 A 5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 567SW 120342 FLOORBOARD BRACE ON LEFT SIDE AT STATION 38 CORRODED. REPLACED FLOORBOARD CROSS BRACE WITH SERVICEABLE PART IAW SRM 53- 20-10. 2 L 7 2 4T RT A31SO 2002010300066 20020103 00066 SO 2002 1 3 SWIA200110473 1 20011121 A 5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203 SO FUSLEAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 567SW 120342 REINFORCEMENT ANGLE FOR RIGHT FLOOR PROP AT FRAME 13 CRACKED. REMOVED AND REPLACED BRACKET AT FRAME 13 RIGHT FLOOR PROP WITH A NEW PART. P/N: 120-08000-001. 2 L 7 2 4T RT A31SO 2002010300067 20020103 00067 EA 2002 1 3 SWIA200110474 1 20011224 A 5210 LINK CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF ADJ A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 413SW 7102 ON DEPARTURE OUT OF SLC GOT A PASSENGER DOOR STOW MESSAGE. FLIGHT ATTENDANT CHECKED ALIGNMENT MARKS AND REPORTED MARKS WERE NOT MATCHED. RETURNED TO SLC. TOP MARKS WERE NOT MATCHED. FOUND MICROSWITCH ON OUTER HANDLE TO BE OUT OF LIMITS. REPOSITIONED THE MICRO SWITCH TO .045 IN IAW MM 52-70-04. OPS CHECKS GOOD. ADJUSTED UPPER DOOR LINKS ON PASSENGER DO OR IAW MM 52-11-00. MARKS MATCHED. 2 L 7 2 4F RT A21EA 2002010300068 20020103 00068 SO 2002 1 3 SWIA200110475 1 20011220 A 2731 52991 ACTUATOR EMB 120 EMB120ER 3260203 SO ELEVATOR FAILED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 578SW 120346 DURING CRUISE (23000) ELEVATOR TRIM FAILURE OCCURRED WITH CORRESPONDING STRONG PITCH UP TENDENCY. TRIM CONTROL REGAINED ON DESCENT. REMOVED AND REPLACED LEFT AND RIGHT ELEVATOR TRIM ACTUATORS IAW EMB 27-32-02. LT P/N ON 5299-1, S/N OFF 6 06, RT P/N ON 5299-1, S/N OFF FA1186. 2 L 7 2 4T RT A31SO 2002010300069 20020103 00069 EA 2002 1 3 SWIA200110476 1 20011224 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER AP APPROACH 1 NM 07 590SW 7077 PILOT'S LEFT SIDE WINDOW SHATTERED. REMOVED AND REPLACED LEFT SIDE WINDOW WITH SERVICEABLE UNIT IAW 56-12-01. P/N ON N P-139322-5, S/N OFF 99139H7837. 2 L 7 2 4F RT A21EA 2002010300074 20020103 00074 NM 2002 1 3 VNAA0111009 1 20011124 A 2450 1060003 CONTROL UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 429JS 4035 3043 AFTER DEPARTING PHL, THE CREW RECEIVED A LEFT HAND GENERATOR FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE AIRCRAFT WAS FER RIED TO DAY WHERE MAINTENANCE INSPECTED AND REPLACED THE BUS POWER CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE M ANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002010300075 20020103 00075 NM 2002 1 3 VNAA0111012 1 20011128 A 2421 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE GENERATOR DIRTY A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 438JS 3056 DURING TAKEOFF, THE CREW RECEIVED A ELECTRONIC CONTROL UNIT FAIL MESSAGE AND ABORTED TAKEOFF. THE CAPTAIN REPORTED AN I NTERMITTENT FAILURE DURING TAXI. MAINTENANCE CONTROL HAD OUTSTATION MAINTENANCE CLEAN THE CANNON PLUGS ON THE DIRECT CU RRENT GENERATOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCR AFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002010300076 20020103 00076 NM 2002 1 3 VNAA0111014 1 20011130 A 2432 DTSP400L BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LEFT FAULTY A VNAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 422JS 11277 3018 WHILE IN CRUISE JUST WEST OF CVG, THE CREW RECEIVED A BATTERY OVERHEAT INDICATION ON THE RED WARNING PANEL. THE CREW FO LLOWED THE PROCEDURE IN THE QUICK REFERENCE HANDBOOK AND THE INDICATION WENT OUT. THE CREW CALLED MAINTENANCE CONTROL A ND WERE ADVISED TO DIVERT TO DAY. MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND MAIN BATTERY IN ACCORDANCE WITH 24-0 0-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002010300077 20020103 00077 EU 2002 1 3 YENA200107 1 20011224 A 5311 STRUCTURE AIRBUS 320 A320232 3930326 EU TORN A YENA K NONE O OTHER TX TAXI/GRND HDL 1 EA 15 505JB 1173 At JFK arrival, Flt 67, Ground damage from jetway impact, found a (6" x 4") tear between Frames 23/24 and Stringers 22/2 3.Fuselage skin repair at Frame 24, between Stringers 21 and LHS 24 as per JetBlue Engineering Order 5301242. Repair con sisted in: cutting out the damaged area, installing a repair doubler (clad-2024T3) thickness=0.09". The original alu riv ets (diameter 4mm) have been replaced by HL11VF6, The original Hi lock fasteneres (diameters 4.8mm) have been replaced b y HL411VF6. The other fasteners have been installed according to the E.O 5301242 drawing and Airbus repair design approv al sheet. No cracks, deformations have been detected on the frame 24 and holes. 2 L 7 2 4F RT A28NM 2002010800093 20020108 00093 NM 2002 1 8 F3LA200100146 1 20011231 A 5313 STRINGER BOEING 737 737228 13844AG NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED STR 16-R CRACKED ON FWD AND AFT ENDS OF WING ICE LIGHT AT STA 510. REPAIRED PER S ERVICE BULLETIN B737-53-1145 AND EA 53-737-148. 2 L 7 2 4F RT A16WE 2002010300078 20020103 00078 NM 2002 1 3 01FDEA01091 1 20011220 A 2781 40173 POSITION SWITCH BOEING 727 7272S2F 1384O81 NM L/E FLAP FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 209 22931 WHILE SETTING CLIMB PWR SAW L/E FLAP AMBER LIGHT BEGAN TO FLICKER, THEN ILLUM'D STEADY CK'D L/E PANEL AND IT SHOWED NR 2 L/E FLAP WAS ON. FOLLOWED APPROP LED FAILURE DOWN RETRACTION CKLIST. THEN RETURNED TO MEM. REMOVED AND REPLACED NR 2 L/E FLAP POS SW. ADJUSTED PER MM 27-82-001, OPS CHECK GOOD. 2 L 7 3 4F A3WE 2002010300079 20020103 00079 NM 2002 1 3 01FDEA01092 1 20011220 A 2910 65178218 MODULE BOEING 727 72722 1384002 NM HYDRAULIC SYS BYPASSING A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 189 19082 APPROX 10 MIN AFTER T/O NR 1 & 2 ENG DRIVEN HYS SYS A PUMPS LOW PRESS LIGHTS ILLUM'D HYD QTY REMAINED STEADY 3.5 GAL AL L HYD C/B WERE IN SYS A PRESS WENT TO ZERO AND SYS A FLT CONT LOW PRESS LIGHTS ILLUM'D. REPLACED SYS A MODULAR UNIT IAW AMM 29-11-061-4. RAN NR 1 & 2 ENG AS PER JRH, SYS OPS CHECKS GOOD, NO LEAKS NOTED. 2 L 7 3 4F A3WE 2002010300080 20020103 00080 NM 2002 1 3 01FDEA01093 1 20011220 A 3040 CONTROLLER BOEING 727 7272S2F 1384O81 NM WINDOW HEAT FAILED A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 208 22930 WINDSHIELD PANEL L1 OUTER PANE SUFFERED A TOTAL FAILURE IN FLT AT FL310. WINDSHIELD WAS EXCESSIVELY HOT TO TOUCH. (WIN DSHIELD OVERHEAT PROTECTION DID NOT ACTIVATE) DECLARED EMERGENCY AND DIVERTED TO PHX. (UNABLE TO COMPLETE FLT UTILIZING CREW 02). REMOVED AND REPLACED L1 WINDSHIELD PER MM 56-11-011-4 & AS PER 30-41-042-5 THE PIN NUMBERS OF THE TRANSFORME R TAPS WERE CONNECTED TO 12. PLACED PINS ON 11 PER 30-41-042-5 FIG 501. REMOVED AND REPLACED L1 WIND HEAT CONTROLLER P ER MM 20-10-017-2. 2 L 7 3 4F A3WE 2002010300081 20020103 00081 NM 2002 1 3 01FDEA01094 1 20011220 A 5712 RIB BOEING 727 727277 138408S NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241 20979 RIGHT WING L/E RIB CRACKED WS 491.5 WBL 398. REPAIRED RIB IAW FEDEX SRM 51-40-2. 2 L 7 3 4F RT A3WE 2002010300082 20020103 00082 NM 2002 1 3 01FDEA01095 1 20011220 A 5260 STEP BOEING 727 727277 138408S NM AIRSTAIRS CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241 20979 AIRSTAIRS STEP NR 9 CORRODED BS 1263 TO 1273. REPLACED STEP IAW FEDEX SRM 51-10-1 & DRAWING SR27-52-03 REV C. 2 L 7 3 4F RT A3WE 2002010300083 20020103 00083 NM 2002 1 3 01FDEA01096 1 20011219 A 5280 SKIN BOEING 727 727277 138408S NM RT MLG DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241 20979 RIGHT MLG WING DOOR INNER SKIN CRACKED. REPAIRED INNER SKIN OF RIGHT MLG WING DOOR IAW FEDEX SRM 52-80-2. 2 L 7 3 4F RT A3WE 2002010900063 20020109 00063 NM 2002 1 9 01FDEA01098 1 20011220 A 2782 1U109592 ACTUATOR BOEING 727 72722 1384002 NM L/E SLAT FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 198FE 19154 DURING T/O, NR 7 LEADING EDGE FAILED TO RETRACT. REMOVED AND REPLACED SLAT ACT PER MM 27-81-032-4. 2 L 7 3 4F A3WE 2002010900064 20020109 00064 NE 2002 1 9 01FDEA01099 2 20011221 A 7200 ENGINE BOEING 727 727227 1384078 NM PWA JT8 JT8D17A 52049 NE NR 1 FAULTY A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 479FE 21461 709296 ON CLIMBOUT NR 1 LOW OIL PRESS LIGHT ILLUM. ENG SHUTDOWN. REMOVED AND REPLACED NR 1 ENG PER W/C 70T0001-01. 2 L 7 3 4F 4 F A3WE E2EA 2002010300084 20020103 00084 NM 2002 1 3 01FDEA01100 1 20011221 A 3234 CONTROL VALVE DOUG MD11 MD11 3023602 NM LANDING GEAR FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 578FE 48458 LANDING GEAR WOULD NOT RETRACT. REMOVED AND REPLACED LANDING GEAR CONTROL VALVE PER MM 32-31-20-4. 2 L 7 3 4F RT A22WE 2002010300085 20020103 00085 NM 2002 1 3 01FDEA01102 1 20011224 A 2751 WARNING SYSTEM DOUG MD11 MD11F 3023600 NM COCKPIT MALFUNCTIONED A FDEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 25 617FE 48748 ON FINAL FLAPS GOT DISAGREE ALERT. CHECKED CFDS, NO FAULT FOUND PERFORMED TEST ON PSEU PER FIM 31-71-07-00. 2 L 7 3 4F RT A22WE 2002010300086 20020103 00086 NM 2002 1 3 01FDEA01103 1 20011223 A 5751 RIB BOEING 727 727277 138408S NM AILERON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 LEFT WING OUTBOARD AILERON NR 5 RIB CRACKED. REMOVED AND REPLACED AILERON PER MM 27-10-031-2. 2 L 7 3 4F RT A3WE 2002010300087 20020103 00087 EU 2002 1 3 01FDEA01106 1 20011227 A 7830 WARNING SYSTEM AIRBUS 300 A300F4605R 3930327 EU COCKPIT ACTIVATED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 682FE 0800 DURING T/O, NR 2 REVR PRESSURIZED WARNING ON ECAM. REVR DEACTIVATED IN FWD THRUST POSITION. 2 L 7 2 4F RT A35EU 2002010300088 20020103 00088 WP 2002 1 3 01FDEA01107 1 20011228 A 2131 CONTROLLER DOUG DC10 DC1010 3022110 WP CABIN PRESSURE FAILED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 370FE 46608 ON T/O, A/C WOULD NOT HOLD PRESSURE. 2 L 7 3 4F A22WE 2002010300089 20020103 00089 WP 2002 1 3 01FDEA01111 1 20011129 A 5320 FLOOR SUPPORT DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 VERTICAL SUPPORT AT BS 495 X=73 Z=16 CRACKED BELOW FLOOR. REMOVED AND REPLACED SUPPORT PER SRM 51-10-00 & 51-21-01. 2 L 7 3 4F RT A22WE 2002010300090 20020103 00090 WP 2002 1 3 01FDEA01112 1 20011107 A 5320 SUPPORT DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 303FE 46802 AFT FUSELAGE WASTE TANK COMP BS 1967, STR 47L & 47R Z-ANGLE SIDEWALL PNL SUPPORT CORRODED. REMOVED AND REPLACED Z-ANGLE PER SRM 53-16-01 & 51-35-01. 2 L 7 3 4F RT A22WE 2002011400113 20020114 00113 WP 2002 1 14 01FDEA01113 1 20011226 A 5320 FLOOR SUPPORT DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 FWD LOWER CARGO BS 775 RT FLOOR SUPPORT SIDE STRUT CORRODED. REMOVED AND REPLACED SIDE STRUT PER SRM 53-13-01. 2 L 7 3 4F RT A22WE 2002010800094 20020108 00094 NM 2002 1 8 F3LA200100147 1 20011231 A 5313 STRINGER BOEING 737 737228 13844AG NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED STR 16-L CRACKED ON FWD AND AFT ENDS OF WING ICE LIGHT AT STA 510. REPAIRED PER S ERVICE BULLETIN B737-53-1145 AND EA 53-737-148. 2 L 7 2 4F RT A16WE 2002010800098 20020108 00098 NM 2002 1 8 F3LA200100149 1 20010103 A 5320 FITTING BOEING 737 737228 13844AG NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON R-2 DOOR AFT FITTING, BOTTOM SIDE OF WEB AT STA 986. FABRICATED AND REPLACED WEB AT THRESHOLD OF R-2 DOOR AT STA 947 TO 986 PER SRM 53-20-1 AND 53-30-2. 2 L 7 2 4F RT A16WE 2002010300096 20020103 00096 NM 2002 1 3 2001UALA02327 1 20011123 A 2150 A/C PACK BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE A/C BAY SMOKE A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 WP 29 210UA 30216 AIR CONDITIONING - SMOKING OR SPARKING. DR-3L LAV 135 CABIN TEMP IS MUCH COLDER THAN SELECTED ON CABIN CONTROL PANEL LI KE 6 DEG. FOUND THE FWD LEFT LAV LIGHT INOP, THE LIGHT GOES ON & OFF INTERMITTENTLY. LIGHT STAYS ON FOR ABOUT 15 MINU TES AND THEN GOES OFF. REPLACED THE LAV LIGHT ASSEMBLY AS IT WAS SUSPECTED AN INTERMITTENT SHORT. NO OTHER REPORTED IN CIDENTS AFTER LIGHT ASSY REPLACEMENT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002011000148 20020110 00148 NM 2002 1 10 2001UALA02409 1 20011214 A 5512 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HORIZ STAB DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 337UA 24241 RIGHT HAND HORIZONTAL STABILIZER LEADING EDGE DENTED 5 FEET FROM OUTBOARD END. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED FLUSH REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002010300102 20020103 00102 NM 2002 1 3 2001UALA02410 1 20011216 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 BODY STATION 178 RBL 5.7 WL 200 WEB CRACKED IN 2 PLACES. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER A ND FILLER MATERIAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2002010300103 20020103 00103 NM 2002 1 3 2001UALA02411 1 20011216 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 BODY STATION 178 LBL 5.7 WL 200 WEB CRACKED. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED DOUBLER AND FILLER MATERIAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2002010300104 20020103 00104 NM 2002 1 3 2001UALA02414 1 20011215 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 CABIN FLOORBEAM STATION 365 RBL 13 TO 28 CORRODED ON FWD SIDE OF FLANGE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002010300105 20020103 00105 NM 2002 1 3 2001UALA02415 1 20011215 A 5321 FLOOR PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 AFT CABIN FLOOR DECK HAS 5 LOCATIONS OF EXCESSIVE MATERIAL REMOVED RBL 5, RBL 12, RBL 45, RBL 48, RBL 52, AT STATION 168 2. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIRS. 2 L 7 2 4F 4 F RT A2NM E17NE 2002010300107 20020103 00107 NM 2002 1 3 2001UALA02419 1 20011216 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 CABIN FLOORBEAM UPPER T-CAP CORRODED AT STATION 324 FROM 6 LBL OUT TO RBL AT STRINGER 17L-R. MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW T-CAP BEAM. 2 L 7 2 4F 4 F RT A2NM E17NE 2002010300109 20020103 00109 NM 2002 1 3 2001UALA02422 1 20011217 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 24193 BODY STATION 178 LBL 5.7 WL 211 WEB HAS CRACK INDICATION BY NON-DESTRUCTIVE TESTING. MAJOR REPAIR ACCOMPLISHED. FABRIC ATED AND INSTALLED DOUBLER AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002011000149 20020110 00149 NM 2002 1 10 2001UALA02423 1 20011216 A 5610 SEAL BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE SLIDING WINDOW DEFECTIVE A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 602UA 21863 CAPTAIN'S NR 2 SLIDING WINDOW HAS A VERY LOUD SQUEAL. CREW CONSIDERS IT UNACCEPTABLE FOR FURTHER FLIGHT. BULB SEAL WAS FOUND DEFECTIVE. OLD SEAL WAS REMOVED, SEAL CHANNEL CLEANED AND NEW SEAL INSTALLED AS OUTLINED IN MM 56-11-11 WITH APP ROPRIATE CURE TIMES ALLOWED FOR SEALANT TO SATISFACTORILY CURE. 2 L 7 2 4F 4 F RT A1NM E3NE 2002010300110 20020103 00110 NM 2002 1 3 2001UALA02424 1 20011217 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 MID CABIN FLOORBEAM T-CAP STATION 700 LBL 15 TO RBL 23 GOUGED. MAJOR REPAIR ACCOMPLISHED. REPAIR STRAP AND ANGLE INSTA LLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002010300111 20020103 00111 NM 2002 1 3 2001UALA02425 1 20011218 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 EXT FUSELAGE STATION 610 TO STATION 620 AND STRINGER 16L AND STRINGER 17L DAMAGED. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002011000150 20020110 00150 NM 2002 1 10 2001UALA02427 1 20011218 A 5313 STRINGER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 196UA 28715 RIGHT HAND FUSELAGE STATION 760-1780 STRINGER 36 HAS REPAIR DOUBLER INSTALLED WITH INSUFFICIENT CIRCUMFERENTIAL FASTENER ROWS. MAJOR REPAIR ACCOMPLISHED. REPLACED DOUBLER. 2 L 7 4 4F 4 F RT A20WE E24NE 2002010300112 20020103 00112 NM 2002 1 3 2001UALA02428 1 20011218 A 2120 ODOR BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN DETECTED A UALA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 609UA 21870 ACRID ELECTRICAL BURNING SMELL AND FUMES COMING FROM DOOR 1R CEILING AREA. GALLEY CB U33 PULLED. GALLEY CIRCUIT BREAKE R WAS PULLED. CABIN WAS AIRED OUT. ALL SYSTEMS WERE TURNED ON AGAIN. SMELL COULD NOT BE REPRODUCED. NO HISTORY OF OD OR IN CABIN. 2 L 7 2 4F 4 F RT A1NM E3NE 2002011800066 20020118 00066 NM 2002 1 18 2001UALA02429 1 20011218 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 190UA 26879 EMERGENCY LIGHTS FROM ROW 55 TO DOOR 5 RIGHT WILL NOT TURN OFF. REPLACED DOOR 4 RT AND 5 RT EMERGENCY LIGHT BATTERY PAC KS. 2 L 7 4 4F 4 F RT A20WE E24NE 2002010300113 20020103 00113 NM 2002 1 3 2001UALA02430 1 20011219 A 5230 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 24193 FORWARD CARGO DOOR HAS DENT APPROXIMATELY .3175 TO .3750 OF AN INCH DEEP BY 2.75 INCHES WIDE BY 3.75 INCHES LONG. MAJO R REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002010300114 20020103 00114 NM 2002 1 3 2001UALA02433 1 20011219 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 BODY STATION 347 LBL 48-88 T-CAP IS CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SECTION AND SPLICES. 2 L 7 2 4F 4 F RT A1NM E24NE 2002010300115 20020103 00115 NM 2002 1 3 2001UALA02434 1 20011219 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 CABIN FLOORBEAM UPPER SURFACE OF UPPER CAP HAD GOUGE AT STATION 640 STRINGER 17R AT 12 RBL TO 20 RBL. MAJOR REPAIR ACCO MPLISHED. BLENDED OUT GOUGE AND AFT. INSTALLED TWO TAPERED STRAPS BELOW FWD AND AFT. 2 L 7 2 4F 4 F RT A2NM E17NE 2002010300117 20020103 00117 EA 2002 1 3 COMA0260019 1 20011231 A 2750 865D1007 MOTOR CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 926CA 6202 7027 FLIGHT 5106 FLAPS FAILED WHEN SELECTED DURING TAXI.REPLACED THE FLAP PDU. 2 L 7 2 4F RT A21EA 2002010300118 20020103 00118 EA 2002 1 3 COMA0260020 1 20011231 A 3220 PIN CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 409CA 7441 FLIGHT 5878 LANDING GEAR DISAGREE WARNING.REMOVED NLG DOWNLOCK SAFETY PIN. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002010300119 20020103 00119 EA 2002 1 3 COMA0260021 1 20011230 A 2750 7455001 SWITCH CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS LD LANDING 1 SO 01 868CA 1254 7427 FLIGHT 5949 FLAPS FAIL CAUTION MESSAGE.REPLACED THE FLAP CONTROL LEVER ASSY. 2 L 7 2 4F RT A21EA 2002010300120 20020103 00120 NM 2002 1 3 2001UALA02435 1 20011219 A 5312 PRESSURE PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 STA 1681, PRESS DECK, RBL 47, HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002010300121 20020103 00121 NM 2002 1 3 2001UALA02436 1 20011219 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSLEAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 STATION 1681, RBL 47 RBL 48, FLOORBEAM UPPER CAP HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANG LE DOUBLERS AND FILLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002010300122 20020103 00122 EA 2002 1 3 COMA0260022 1 20011230 A 2760 FE210302 SWITCH CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A COMA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 01 915CA 13289 7013 FLIGHT 5864 SPOILER CONFIG WARNING DURING T/O.REPLACED THE THROTTLE SWITCH CONTROL UNIT. 2 L 7 2 4F RT A21EA 2002011000151 20020110 00151 EU 2002 1 10 2001UALA02437 1 20011218 A 2150 D2157160000000 BELLOWS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 PACK BLOWN A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 406UA 454 CABIN ALTITUDE COULD NOT BE MAINTAINED BELOW 10,000 IN AUTO. PACK NR 2 WAS DEFERRED INOPERATIVE, PACK NR 1 WOULD NOT PR ESSURIZE THE CABIN, FOUND BLOWN COOLING DUCT BELLOWS NR 1 PACK, REPLACED AND OPERATIONALLY CHECKED NORMAL. PACK NR 2 WA S LATER OPERATIONALLY CHECKED AS NORMAL. NO FURTHER DISCREPANCIES REPORTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2002010300125 20020103 00125 NM 2002 1 3 2001UALA02438 1 20011221 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 338UA 24242 CABIN FLOORBEAM STATION 967 RBL 10 HOLE ELONGATED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE. INSTALLED ANGLE REPAIR WITH FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002010300127 20020103 00127 NM 2002 1 3 2001UALA02439 1 20011221 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 338UA 24242 AFT CABIN FLOORBEAM STATION 947 RBL 46 WL 208 BLENDED REPAIR OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED T-CAP. MANUFACTURED NEW T-CAP. INSTALLED NEW CAP AND SPLICE ANGLES. 2 L 7 2 4F 4 F RT A16WE E2GL 2002010300128 20020103 00128 NM 2002 1 3 2001UALA02440 1 20011221 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 338UA 24242 AFT CABIN FRAME (STATION 847) NEXT TO STRINGER 9L IS CRACKED WHERE AIR GRILL CLIP ATTACHES TO FRAME. MAJOR REPAIR ACCOM PLISHED. DAMAGE REMOVAL VERIFIED. DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002020100018 20020201 00018 NE 2002 2 1 2001UALA02442 2 20011221 A 7230 STRUCTURE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RUBSTRIP DAMAGED A UALA C ABORTED TAKEOFF X J ENGINE FLAMEOUT WARNING INDICATION TO TAKEOFF 1 WP 29 426UA 16262 510 V10197 ABORTED TAKEOFF AT 140 KNOTS DUE TO NR 1 ENGINE COMPRESSOR STALL. SUPPLEMENTAL DATA UPDATE INITIAL BORESCOPE INFORMATION INDICATES DISBOND OF C6 ABRADABLE RUBSTRIP MATERIAL, CAUSING C6 BLADE DAMAGE AND COMPRESSOR STALL. 2 L 7 2 4F 4 F RT A28NM E40NE 2002010300130 20020103 00130 NM 2002 1 3 2001UALA02445 1 20011221 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 MID CABIN CREASE BEAM INNER CHORD BODY STATION 1020 LBL 63 HAS SURFACE CORROSION ON UPPER FLANGE. MAJOR REPAIR ACCOMPLI SHED. REPLACED INNER BULB ANGLE WITH SPLICE AT BODY STATION 1010. 2 L 7 2 4F 4 F RT A2NM E17NE 2002010300131 20020103 00131 NM 2002 1 3 2001UALA02446 1 20011221 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 CABIN FLOOR STATION 377 LBL 22 HAS EXCESSIVE MAT LOSS ON UPPER CAP. MAJOR REPAIR ACCOMPLISHED. REPAIR STRAPS INSTALLED . 2 L 7 2 4F 4 F RT A2NM E17NE 2002010300132 20020103 00132 EU 2002 1 3 AWXA200100681 1 20011229 A 3350 E0261CF20 CABLE AIRBUS 320 A320231 3930325 EU SEAT ROW 13 BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 634AW 091 PHX - EEL - "C" - DURING INSPECTION MAINTENANCE FOUND EMERGENCY SEAT LIGHT WIRE BROKEN AT ROW 13. MAINTENANCE REPAIRED B ROKEN WIRE AT ROW 13 IAW ESPM 20-53-20. 2 L 7 2 4F RT A28NM 2002010300133 20020103 00133 NM 2002 1 3 2001UALA02447 1 20011221 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 CABIN FLOOR STATION 77 LBL 42 HAS EXCESSIVE MAT LOSS ON UPPER CAP OF BEAM. MAJOR REPAIR ACCOMPLISHED. REPAIR STRAPS 11 INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002010300134 20020103 00134 NM 2002 1 3 2001UALA02448 1 20011221 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 AFT PIT FUSELAGE FRAME STATION 1440 ABOVE STRINGER 25 LEFT IS CRACKED IN INBOARD CHORD FLANGE. MAJOR REPAIR ACCOMPLISHE D. DAMAGE REMOVED. FRAME REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002010300135 20020103 00135 NM 2002 1 3 2001UALA02449 1 20011222 A 5320 ATTACH ANGLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 CABIN FLOOR CREASE BEAM WEB ATTACH ANGLE BRACKET HAD EXCESSIVE CORROSION, STATION 981 RBL 68 STRINGER 17R. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED REPLACEMENT ATTACH BRACKET. 2 L 7 2 4F 4 F RT A2NM E17NE 2002010300136 20020103 00136 NM 2002 1 3 2001UALA02450 1 20011222 A 5310 143N552027 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 CORROSION ON THE LT CREASE BEAM INNER CHORD P/N 143N5520-27 AT BODY STATION 758 LBL 64 STRINGER 17L. MAJOR REPAIR ACCOM PLISHED. REMOVED COMPLETE SECTION OF CREASE BEAM INNER CHORD AND INSTALLED NEW SECTION. 2 L 7 2 4F 4 F RT A2NM E17NE 2002010400001 20020104 00001 WP 2002 1 4 0104929909 1 20010607 A 5310 STIFFENER DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 959N 47255 During H-CK in ATL, one 1/2"crack was found in the station 756 bulkhead. The crack is located in the upper end of the ve rticle stiffener at X=-22. Repaired per EA 99-181259. 2 L 7 2 4F A6WE 2002010400002 20020104 00002 WP 2002 1 4 0104939915 1 20010710 A 5330 SKIN DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 965N 47417 During L-CK in DHN, A crack was found in the upper aft corner of the FWD Cargo Jamb. Repaired per EA 99-183995. 2 L 7 2 4F A6WE 2002010400003 20020104 00003 WP 2002 1 4 0104949917 1 20010719 A 5310 ANGLE DOUG DC9 DC932 3022066 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 967N 47573 During Hck in ATL, corrosion was found on the horizontal flange of the fuselage cusp angle at station 120. Repair Materi al .071 7075-t6 Aluminum and .020" 7075-t6 Aluminum. Repaired per EA 99-181362. 2 L 7 2 4F A6WE 2002010400004 20020104 00004 WP 2002 1 4 0104969922 1 20010712 A 5720 SPAR DOUG DC9 DC932 3022066 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 945N 47664 During Mck in ATL, corrosion was found in the left and right beaver tails. The beaver tails were removed to accomplish c orrosion removal. After the beaver tail removal, it was noted that 11 fastener holes common to the pylon front spar were elongated on each side of the aircraft. Repaired per EA 99-181347. 2 L 7 2 4F A6WE 2002010400005 20020104 00005 WP 2002 1 4 0104979922 1 20010727 A 5310 PAN DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 945N 47664 During M-ck in ATL, a crack was found at station 937 between longerons 26R and 27R. The crack was between marked holes " c" and "d" on the doorjamb pan. EA 99-181313 2 L 7 2 4F A6WE 2002010400006 20020104 00006 WP 2002 1 4 0104989922 1 20010724 A 5330 SKIN DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 945N 47664 During MCK in ATL, a 1/4" long crack was found in the fuselage skin at staion 1019, between longerons 14L and 15L. The c rack emanated from one fastener hole common to the upper attach angle and was removed using 1" diameter cut out. This EA provides instructions to repair the damage. EA 99-181338. 2 L 7 2 4F A6WE 2002010400007 20020104 00007 WP 2002 1 4 0104999922 1 20010719 A 5330 DOOR FRAME DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 945N 47664 During an MCK in ATL, a .8" crack was found while accomplishing inspection of the lower aft corner of the forward cargo door doorjamb. This EA. 99-181281 provides repair of area. Material .050" 2014-t6 and .090" 2014-t6. 2 L 7 2 4F A6WE 2002010400008 20020104 00008 WP 2002 1 4 0105009922 1 20010706 A 5410 RIB DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 945N 47664 During Mck in ATL, the aft portion of the lower cap of the pylon closing rib was found cracked. The crack is .6" long an d extends from a fasterner hole 3.7" forward from the aft end of the cap. Repaired per EA 99-181307. 2 L 7 2 4F A6WE 2002010400009 20020104 00009 WP 2002 1 4 0105019922 1 20010709 A 5310 INTERCOSTAL DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 945N 47664 During MCK in ATL, a crack was found in the outboard end of intercostal 9923484-9 at sta 180 and at X=-20. Repaired per EA 99-1813231. 2 L 7 2 4F A6WE 2002010400010 20020104 00010 WP 2002 1 4 0105039927 1 20010604 A 5310 LONGERON DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8920E 45835 During an Hck in ATL, the longeron 26r end fitting was found cracked at station 598. Repaired per EA 99-181209. 2 L 7 2 4F A6WE 2002010400011 20020104 00011 WP 2002 1 4 0105049969 1 20010731 A 5320 BEAM DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9333 47246 During HCK at ATL, the ventral stair opening LHS beam upper jamb was found cracked between the #2 and #3 guide pin recep tacle. Repaired per EA 99-185020. 2 L 7 2 4F A6WE 2002010400012 20020104 00012 WP 2002 1 4 0105059969 1 20010730 A 5310 CHANNEL DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9333 47246 During HCK at ATL, a 1.125" crack was found in the upper inboard bend radius of the 5910130-9 channel downward along the radius. Repaired per EA. 99-181359. 2 L 7 2 4F A6WE 2002010400013 20020104 00013 WP 2002 1 4 0105069971 1 20010608 A 5310 STIFFENER DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9335 47337 During HCK in ATL., two .75" cracks were found in the 756 bulkhead. The cracks are located in the upper ends of the vert icle stiffeners at sta X=-11. EA 99-181222. 2 L 7 2 4F A6WE 2002010400014 20020104 00014 WP 2002 1 4 0105079971 1 20010607 A 5720 DOUBLER DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9335 47337 During Hck in ATL, A crack was found on the upper fuel tank access panel doubler. Repaired per EA 99-181239. 2 L 7 2 4F A6WE 2002010400015 20020104 00015 WP 2002 1 4 0105089971 1 20010607 A 5310 PRESSURE PANEL DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9335 47337 During Hck in ATL, Two cracks were found in the horizontal pressure panel at station 105 at X=25 2.4" and X=27 .5"long. Repaired per EA 99-181213. 2 L 7 2 4F A6WE 2002010400016 20020104 00016 WP 2002 1 4 0105099989 1 20010709 A 5310 WEB DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8945E 47181 During Hck in ATL, a .25 inch crack was found on the doorjamb web at station 617 RHS. Material .032" 2024-t42. Repaired per EA. 99-181318. 2 L 7 2 4F A6WE 2002010400017 20020104 00017 WP 2002 1 4 0104959864 1 20010710 A 5330 SKIN DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 773NC 47775 During overnight in MSP, a skin crack was found near the aft cargo door cut out in the skin at the lower aft corner. Rep aired per EA 99-183545. 2 L 7 2 4F RT A6WE 2002010400018 20020104 00018 WP 2002 1 4 01FDEA01108 1 20011218 A 3230 SUPPORT DOUG DC10 DC1010 3022110 WP RT MLG FAILED A FDEA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 363FE 48263 NR 3 HYDRAULIC SYS AND RT MLG RETRACT ACT FAILED. REMOVED AND REPLACED FRAME SUPPORT. 2 L 7 3 4F A22WE 2002010400028 20020104 00028 EU 2002 1 4 2001UALA02408 1 20011213 A 2611 RAI2800M0706 CONTROL UNIT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED A UALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 WP 29 434UA 20 592 CREW REPORTED ELECTRONIC CENTRALIZED AIRCRAFT MONITORING (ECAM) SMOKE LAVATORY & CARGO DETECTION FAULT WITH THE REPORT F ROM A FLIGHT ATTENDANT OF SMOKE IN AFT CABIN. REPLACE THE SDCU (SMOKE DETECTOR CONTROL UNIT). AIRCRAFT FREE OF PROBLEM S SINCE REMOVAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2002010400029 20020104 00029 NM 2002 1 4 PCAA0201004 1 20010103 A 3350 2078 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM AFT INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 819EX 8791 1406 016 DURING ROUTINE MAINTENANCE VISIT ALL EMERGENCY EXIT AND FLOOR LIGHTS FOUND TO BE INOPERATIVE. BLOWN FUSES FOUND IN AFT B ATTERY PACK. AFTER FUSES WERE REPLACED IT WAS DISCOVERED BATTERY PACK WAS BAD. AFT BATTERY PACK REPLACED. OPERATIONAL CH ECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002010400030 20020104 00030 NM 2002 1 4 2001UALA02432 1 20011219 A 5310 BEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 BODY STATION 852 LBL 33 TRANSBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW SECTION AND SPLICE S. 2 L 7 2 4F 4 F RT A1NM E24NE 2002010400031 20020104 00031 NM 2002 1 4 2001UALA02451 1 20011222 A 5230 RETAINER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CARGO DOOR GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 FORWARD CARGO PIT DOOR LOWER AFT CORNER AND LOWER CENTER SECTION OF SEAL DEPRESSERS HAD DEEP GOUGES. MAJOR REPAIR ACCOM PLISHED. REMOVED LOWER CENTER AND AFT CORNER SEAL DEPRESSOR AND INSTALLED NEW PARTS. 2 L 7 2 4F 4 F RT A2NM E17NE 2002011800067 20020118 00067 NM 2002 1 18 2001UALA02456 1 20011226 A 5610 WINDSHIELD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT CRACKED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 504UA 24625 CAPTAIN'S OUTER WINDSHIELD CRACKED. OUTER PANE OF WINDSHIELD IS A NON-STRUCTURAL MEMBER OF WINDSHIELD ASSEMBLY. SUSPEC T FOREIGN OBJECT DAMAGE CREATING STRESS CONCENTRATION DURING TAXI AND SUBSEQUENT FAILURE ON CLIMBOUT. REPLACED CAPTAIN' S NUMBER 1 WINDSHIELD. 2 L 7 2 4F 4 F RT A2NM E17NE 2002010400032 20020104 00032 NM 2002 1 4 2001UALA02457 1 20011224 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 AFT FUSE FRAME AT STATION 1640 BETWEEN STRINGER 7L AND 8L HAS EXCESSIVE MATERIAL REMOVED FROM WEAR BLEND OUT. MAJOR REP AIR ACCOMPLISHED. CUT OUT DAMAGE AREA AND INSTALLED DOUBLE STRAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002010400033 20020104 00033 NM 2002 1 4 2001UALA02458 1 20011223 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSLEAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 CABIN FLOORBEAM UPPER CHORD HAS CORROSION RBL 53 TO RBL 62 STATION 324. MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW SECT ION OF FLOORBEAM UPPER CHORD. 2 L 7 2 4F 4 F RT A2NM E17NE 2002010400034 20020104 00034 NM 2002 1 4 2001UALA02459 1 20011224 A 5313 STRINGER BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 922UA 26642 RIGHT HAND EXTERNAL FUSELAGE BODY STATION 226 STRINGER 19R DENTED 4 INCHES DIAMETER AND IS .075 INCH DEEP. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002011000152 20020110 00152 NM 2002 1 10 2001UALA02461 1 20011221 A 5320 DOUBLER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 BODY STATION 1131 LBL 35 LOWER STRAP DOUBLER CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRAP. 2 L 7 2 4F 4 F RT A1NM E24NE 2002011000153 20020110 00153 NM 2002 1 10 2001UALA02462 1 20011221 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 BODY STATION 347 LBL 88 WL 200 FLOORBEAM T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CAP. 2 L 7 2 4F 4 F RT A1NM E24NE 2002010400035 20020104 00035 NM 2002 1 4 2001UALA02463 1 20011226 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 338UA 24242 AFT CABIN FRAME AT STATION 827 NEAR STRINGER 9L IS CRACKED WHERE AIR GRILL CLIP ATTACHES TO FRAME. MAJOR REPAIR ACCOMPL ISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002010400036 20020104 00036 NM 2002 1 4 2001UALA02464 1 20011226 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 338UA 24242 AFT CABIN FRAME STATION 987, NEXT TO STRINGER 9L CRACKED. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED FRAME REPAIR USING C HANNEL AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002010400037 20020104 00037 NM 2002 1 4 2001UALA02465 1 20011226 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 AFT PIT FRAME STATION 1320, RBL 13 -16 STRINGER 28R, UPPER CAP HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. PARTIAL FRAME CUTOUT REMOVED FROM UPPER CAP. PLUG INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002010400038 20020104 00038 NM 2002 1 4 2001UALA02467 1 20011227 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 BODY STATION 178 BULKHEAD WEB CRACKED WL 212, RBL 5.7. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER ON WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2002010400039 20020104 00039 NM 2002 1 4 2001UALA02468 1 20011227 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 BODY STATION 178 BULKHEAD WEB CRACKED AT WL 215 RBL 5.7. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002020600041 20020206 00041 NM 2002 2 6 2001UALA02469 1 20011227 A 2612 FIRE WARNING BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE COCKPIT FALSE INDICATION A UALA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 WP 29 212UA 30218 ONE MINUTE AFTER TAKEOFF, CREW RECEIVED AFT CARGO FIRE INDICATION. FIRE BOTTLES DISCHARGED AND FIRE INDICATION WARNING DID NOT GO AWAY IMMEDIATELY. CREW DECLARED EMERGENCY AND RETURNED TO HNL. OVERWEIGHT LANDING. UPON LANDING FIRE CREW CHECKED FOR A HEAT SOURCE IN AFT PIT AND FOUND NONE. ONLY LUGGAGE WAS IN THE AFT CARGO PIT. SUBSEQUENT CARGO SMOKE DET ECTION TEST AND FIRE WARNING TEST PASSED. NO MAINTENANCE MESSAGE FAULTS WERE RECORDED THAT DIRECTED TO A SYSTEM FAULT. INLET LINES TO DETECTOR WERE INSPECTED FOR MOISTURE AND NONE WAS FOUND. A/C WAS FLOWN TO SFO UNEVENTFULLY WITH EMPTY P ITS. DURING EXTINGUISHING SYSTEM REFURBISHMENT, NO ABNORMALITIES WERE NOTED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002010400042 20020104 00042 NM 2002 1 4 AUS20011278 1 20011128 A 5230 6546921528 SKIN BOEING 737 737376 NM CFMINT CFM56 CFM563C 13802 EU CARGO DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S 1078 (AUS) FORWARD CARGO DOOR CRACKED IN FORWARD AND AFT LOWER CORNERS. FOUND DURING INSPECTION IAW AD/B737/142 (BSB 737-52- 1100 R2). 2 L 7 2 4F 4 F RT A16WE E21EU 2002010400045 20020104 00045 NM 2002 1 4 AUS20011284 1 20011110 A 7603 BACP30M4 PULLEY PWA JT9D7R4E BOEING 767 767238 1385114 NM PWA JT9 JT9D7R4E 52054 NE POWER LEVER WORN W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT ENGINE THRUST CONTROL CABLE PULLEYS (2OFF) LOCATED AT STA 240.0 WERE FOUND TO BE WORN. FOUND DURING INSPECTION IAW AD/B767/118(EI 762-76-003). 2 L 7 2 4F 4 F RT A1NM E3NE 2002010400049 20020104 00049 EU 2002 1 4 AUS20011300 1 20010910 A 2710 PIPE FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU AILERON CONTROL CRACKED W O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 AU S (AUS) RT AILERON ACTUATOR RETURN PIPE CRACKED AND LEAKING. LOSS OFHYDRAULIC FLUID. 2 L 7 2 4F 4 F RT A20EU E2EU 2002010400050 20020104 00050 EU 2002 1 4 AUS20011302 1 20010917 A 7500 DUCT RROYCE SPEY55515 FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU ENGINE BLEED AIR FAILED W O OTHER J WARNING INDICATION NR NOT REPORTED 1 AU S (AUS) APU AIR DUCT RUPTURED IN AREA DOWNSTREAM OF THE APU LOAD CONTROL AIR VALVE. 2 L 7 2 4F 4 F RT A20EU E2EU 2002010400052 20020104 00052 NM 2002 1 4 AUS20011305 1 20011206 A 7910 3006084 CAP PWA PW120A DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE ENGINE OIL UNLOCKED W O OTHER E K J VIBRATION/BUFFET FLUID LOSS WARNING INDICATION CL CLIMB 1 AU S (AUS) LT ENGINE OIL FILLER CAP UNSEATED AND UNLOCKED. OIL LEVEL CHECK HAD BEEN CARRIED OUT DURING STOP OVER. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002010400053 20020104 00053 SO 2002 1 4 AUS20011308 1 20011125 A 2752 AUK2EMB120NA CONNECTOR EMB 120 EMB120 3260201 SO PWA 118 PW118A NE HAMSTD 14SF 14SF9 NE TE FLAP ACTUATOR CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) BOTH OUTBOARD TRAILING EDGE FLAP ACTUATOR CONNECTORS CORRODED. 2 L 7 2 4T 4 T RT A31SO E20NE 6 N P11NE 2002010400057 20020104 00057 EU 2002 1 4 AUS20011321 2 20011208 A 7320 706M31G04 VALVE GE CFM563C BOEING 737 737476 NM CFMINT CFM56 CFM563C 13802 EU FUEL CONTROL LEAKING W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NR 2 ENGINE TCC VALVE LOWER ACTUATOR LEAKING. 2 L 7 2 4F 4 F RT A16WE E21EU 2002010400058 20020104 00058 EU 2002 1 4 AUS20011323 1 20010822 A 7500 CLAMP RROYCE SPEY55515 FOKKER F28 F28MK4000 4990810 EU RROYCE SPEY SPEY55515 54521 EU ENGINE BLEED AIR LEAKING W O OTHER M J OVER TEMP WARNING INDICATION CR CRUISE 1 AU S (AUS) RT ENGINE BLEED AIR CROSSOVER DUCT CLAMP LEAKING. 2 L 7 2 4F 4 F RT A20EU E2EU 2002010400060 20020104 00060 NM 2002 1 4 AUS20011334 1 20011210 A 2824 VALVE BOEING 737 737376 NM CFMINT CFM56 CFM563C 13802 EU FUEL TRANSFER RESTRICTED W O OTHER J WARNING INDICATION NR NOT REPORTED 1 AU S (AUS) FUEL CROSSFEED VALVE MECHANICAL LEVER RESTRICTED IN OPERATION BY A BONDING LEAD. 2 L 7 2 4F 4 F RT A16WE E21EU 2002010400061 20020104 00061 NM 2002 1 4 AUS20011335 1 20011211 A 3097 WIRE BOEING 737 737376 NM CFMINT CFM56 CFM563C 13802 EU COCKPIT WINDOW FIRE W O OTHER A FLAME/FIRE CR CRUISE 1 AU S (AUS) FIRST OFFICERS SLIDING WINDOW HEATING WIRE CAUGHT FIRE. 2 L 7 2 4F 4 F RT A16WE E21EU 2002010400062 20020104 00062 2002 1 4 AUS20011339 4 20011211 A 3416 804710DH ALTIMETER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE COCKPIT FAULTY W K NONE W INADEQUATE Q C IN INSP/MAINT 1 AU S (AUS) STANDBY ALTIMETER BAROMETRIC SUBSCALE CALIBRATED IN IN HG'. AD/GEN/7 REQUIRES THE SUBSCALE TO BE CALIBRATED IN MI LLIBARS. PERSONNEL/MAINTENANCE ERROR. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002010400063 20020104 00063 EU 2002 1 4 AUS20011342 2 20011211 A 7320 3352504076 LINE GE CFM563C BOEING 737 737476 NM CFMINT CFM56 CFM563C 13802 EU NR 2 ENGINE WORN W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NR 2 ENGINE P6 LINE CHAFING ON DOUBLER LOCATED AT THE FORWARD FACE OF THE STRUT FAIRING. FOUND DURING INSPECTION I AW EI737-72-530R1. 2 L 7 2 4F 4 F RT A16WE E21EU 2002010400065 20020104 00065 EU 2002 1 4 AUS20011351 1 20010827 A 2133 88005B0306 VALVE AIRBUS 310 A310324 3930206 EU PWA 4152 PW4152 NE PRESSURE REGULAT FAULTY W O OTHER J WARNING INDICATION CL CLIMB 1 AU S 2854 226 (AUS) PRESSURISATION SYSTEM FAULTY. FORWARD OUTFLOW VALVE IN AUTO MODE. 2 L 7 2 4F RT A35EU E24NE 2002010400066 20020104 00066 EU 2002 1 4 AUS20011353 1 20011126 A 3232 ACTUATOR FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU MLG DOOR FAULTY W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT MAIN LANDING GEAR DOOR NOT FULLY RETRACTING DUE TO A FAULTY REAR DOOR ACTUATOR. 2 L 7 2 4F 4 F RT A20EU E2EU 2002010400068 20020104 00068 2002 1 4 AUS20011360 4 20011217 A 3418 36058 COMPUTER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE STALL WARNING FAULTY W O OTHER F N FLT CONT AFFECTED FALSE WARNING CR CRUISE 1 AU S 354370 (AUS) SPURIOUS STALL WARNINGS RESULTED IN NR 1 AND NR 2 LIFT COMPUTERS BEING REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002010400069 20020104 00069 NM 2002 1 4 AUS20011367 1 20011213 A 2422 INVERTER DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE HAMSTD 14SF 14SF23 NE AC SYSTEM FAULTY W O OTHER J WARNING INDICATION DE DESCENT 1 AU S (AUS) PRIMARY INVERTER SUSPECT FAULTY. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002010400070 20020104 00070 NM 2002 1 4 AUS20011371 1 20011217 A 6120 87600519001 CONTROL CABLE HAMSTD 14SF23 DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE HAMSTD 14SF 14SF23 NE PROP CONTROL FOULED W K NONE O OTHER IN INSP/MAINT 1 AU S 1955 (AUS) RT PROPELLER CONDITION LEVER CONTROL CABLE HOOKED IN CEILING TRIM ATTACHMENT BRACKET. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002010400071 20020104 00071 NM 2002 1 4 SWAA013443 1 20011230 A 5330 6545774 SKIN BOEING 737 7372K6 1364440 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 780, STR 23L AND BS 845, STR 25L. REPAIRED SKI N PER SRM. 2 L 7 2 4F RT A16WE 2002010400072 20020104 00072 NM 2002 1 4 SWAA013446 1 20011230 A 5310 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 357SW 26594 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 827, WL 148 AND LBL 1. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002010400073 20020104 00073 NM 2002 1 4 SWAA013448 1 20011230 A 5330 6545769 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 388SW 26591 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SIDE OF EQUIPTMENT COOLING EXHAUST CUT OUT. REPAIRED SK IN PER SRM. 2 L 7 2 4F RT A16WE 2002010400074 20020104 00074 NM 2002 1 4 SWAA013449 1 20011228 A 5311 6546529 FRAME BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 312, WL 254 AND LBL 61. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002010400076 20020104 00076 NM 2002 1 4 2001UALA02470 1 20011227 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 STATION 520 BETWEEN STRINGER 24L AND 25L FUSE FRAME UPPER CHORD IS DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLE R. 2 L 7 2 4F 4 F RT A2NM E17NE 2002011000154 20020110 00154 NM 2002 1 10 2001UALA02471 1 20011227 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 STATION 287 RT, FUSELAGE SKIN CREASED. MAJOR REPAIR ACCOMPLISHED. REPAIRED SKIN DAMAGE AND INTERNAL BULKHEAD CHORD ANG LE. 2 L 7 2 4F 4 F RT A1NM E24NE 2002011000155 20020110 00155 NM 2002 1 10 2001UALA02472 1 20011227 A 5313 STRINGER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 E+E BAY AT STATION 287, STATION 26R END FITTING NEEDS TO BE RE-FABRICATED TO FACILITATE STRINGER REPAIR. MAJOR REPAIR A CCOMPLISHED. FABRICATED NEW STRINGER END FITTING. 2 L 7 2 4F 4 F RT A1NM E24NE 2002011000156 20020110 00156 NM 2002 1 10 2001UALA02473 1 20011227 A 5310 BEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 CABIN C-ZONE STATION 852, LBL 54, UPPER TRANSBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM TRANSBEAM SP LICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2002011000157 20020110 00157 NM 2002 1 10 2001UALA02474 1 20011227 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 AFT PIT FLOORBEAM T-CAP LOWER SURFACE HAS CORROSION AT STATION 1197+132 AT STRINGER 33L. MAJOR REPAIR ACCOMPLISHED. RE PAIRED FLOORBEAM T-CAP. 2 L 7 2 4F 4 F RT A1NM E24NE 2002010400077 20020104 00077 NM 2002 1 4 A6WA200100067 1 20011211 A 5270 PROXIMITY SWITCH DORNER DO32 DO328100 2996000 NM EMERGENCY EXIT OUT OF ADJ A A6WA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 31 339PH 3015 DOORS RWP LIGHT ON INFLIGHT AND DOORS PAGE SHOWS THE LT AFT EMERGENCY EXIT DOOR UNSAFE LIGHT. MAINTENANCE ADJUSTED DOOR PROX SWITCH ON LT AFT EMERGENCY DOOR EXIT. OPS CHECK GOOD. 2 H 7 2 4T RT A45NM 2002010400078 20020104 00078 EU 2002 1 4 A6WA200100068 1 20011211 A 2497 SLEEVE BAC 146 146200A 1500266 EU COCKPIT OUT OF POSITION A A6WA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 31 292UE E2087 EN ROUTE NOTICED FAINT ELECTRICAL SMELL, SWITCHED TO FRESH AIR MODE, ODOR DIMINISHED, BUT STILL PRESENT. ON APPROACH SW ITCHED TO APU AIR ODOR GONE. MAINTENANCE RAN ENGINES, TESTED ON ALL AIR SOURCES, INSPECTED BEHIND OVERHEAD ELECTRICAL, REPOSITIONED RUBBER SLEEVE ON OVERHEAD ELECTRICAL PANEL LANYARD. 2 H 7 4 4F A49EU 2002010400079 20020104 00079 NM 2002 1 4 A6WA200100069 1 20011213 A 3020 001A716E1000010 BOOT DORNER DO32 DO328100 2996000 NM PWA 119 PW119C NE NR 2 ENGINE DEFECTIVE A A6WA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 31 332PH 8957 247 3010 PCE116037 RIGHT ENGINE HAD FLUCTUATING TORQUE INDICATION OF 10 - 25 PERCENT IN FLIGHT. MAINTENANCE FOUND INTAKE DE-ICE BOOT INFLA TING AND CHOKING OFF ENGINE AIR INLET SUPPLY. REMOVED AND REPLACED INTAKE. 2 H 7 2 4T 4 T RT A45NM E20NE 2002010400080 20020104 00080 EA 2002 1 4 A6WA200100070 1 20011218 A 3030 WARNING SYSTEM CNDAIR CL600 CL6002B16 1900305 EA COCKPIT MALFUNCTIONED A A6WA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 401AW 7280 AFTER TAKEOFF RIGHT HAND AOA HEAT AMBER MESSAGE FOLLOWED BY LEFT HAND AOA HEAT AMBER MESSAGE. MAINTENANCE DEPOWERED AND REPOWERED AIRCRAFT OPS CHECK GOOD IAW AMM 30-31-15-710. 2 L 7 2 4F RT A21EA 2002010400081 20020104 00081 NM 2002 1 4 A6WA200100071 1 20011226 A 2120 ODOR DORNER DO32 DO328100 2996000 NM COCKPIT DETECTED A A6WA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 329PH 3007 STRONG ODOR FROM PILOTS VENT, CAME AFTER START FROM NR 1 ENGINE. MAINTENANCE RAN NR 1 ENGINE AND PACKS, NO ODOR NOTED. OPS CHECK GOOD. 2 H 7 2 4T RT A45NM 2002010400082 20020104 00082 NM 2002 1 4 A6WA200100072 1 20011227 A 2440 DON183A RECEPTACLE DORNER DO32 DO328100 2996000 NM EXTERNAL POWER BURNED A A6WA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 329PH 3007 STRONG ELECTRICAL BURNING SMELL IN COCKPIT, STRONGEST WHEN STARTING ENGINES. MAINTENANCE REPLACED DC EXT POWER RECEPTAC LE AND CURRENT LIMITER DUE TO BURNT TERMINALS ON PLUG. 2 H 7 2 4T RT A45NM 2002010400083 20020104 00083 WP 2002 1 4 ABXA010649 1 20011220 A 5280 56489332 DOOR DOUG DC8 DC863F 302198F WP RT MLG MISSING A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 815AX 2462 46097 DURING MAINTENANCE POST FLIGHT WALKAROUND, THE RIGHT MAIN LANDING GEAR CENTER DOOR WAS MISSING. INSTALLED THE MAIN GEAR CENTER DOOR IAW DC-8 MM 32-12-01. 2 L 7 4 4F 4A25 2002010400084 20020104 00084 WP 2002 1 4 ABXA010650 1 20011219 A 3310 PLATE DOUG DC8 DC863 302198A WP COCKPIT DEFECTIVE A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 23 824AX 46141 WHEN SHUTTING OFF THE LANDING LIGHTS, SPARKS CAME FROM MISSING BACKGROUND LIGHT SOCKETS FOR THE LANDING LIGHTS PLACARD. REPLACED THE LIGHT PLATE. OPS CHECKED GOOD IAW AMM 33-13-00-2-0009. 2 L 7 4 4F 4A25 2002010400085 20020104 00085 WP 2002 1 4 ABXA010651 1 20011225 A 3350 60030451 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 945AX 47551 WHEN EMERGENCY LIGHTS WERE SELECTED ON, THE PEANUT LIGHTS DID NOT ILLUMINATE. REPLACED THE EMERGENCY LIGHT BATTERY/CHAR GER PACK IAW DC-9 MM. 2 L 7 2 4F A6WE 2002010400086 20020104 00086 WP 2002 1 4 ABXA010652 1 20011225 A 3350 60030451 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 978AX 47628 EMERGENCY EVACUATION LIGHTS WOULD NOT COME ON IN THE ARM POSITION. REPLACED THE EMERGENCY LIGHTS BATTERY SUPPLY UNIT IA W DC-9 MM. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2002010400087 20020104 00087 NM 2002 1 4 PCAA0201005 1 20010104 A 5610 7802 WINDSHIELD DHAV DHC8 DHC8102 2809003 NM LEFT CRACKED A PCAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 13 838EX 3817 220 BUF-BDL FLIGHT#3585. CREW REPORTED CAPTAINS FRONT WINDSHIELD CRACKED ON TO LEFT CORNER ON CLIMBOUT. MAINTENANCE REPLACED CAPTAINS WINDSHIELD IN ACCORDANCE WITH DASH 8 MAINTENANCE MANUAL 56-10. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SE RVICE. 2 H 7 2 4T RT A13NM 2002010400088 20020104 00088 NM 2002 1 4 ABXA010653 1 20011218 A 2782 41004061 MOTOR BOEING 767 767281 1385109 NM L/E SLAT LEAKING A ABXA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 23 787AX 28027 23020 AN OIL ODOR WAS DETECTED IN THE AIR CONDITIONING SYSTEM DURING TAKEOFF. RAN UP PACKS WITH APU. SUSPECT ODOR FROM THE R IGHT PACK. FOUND EVIDENCE OF HYDRAULIC LEAK. SKYDROL AROUND THE PNEUMATIC DUCT CONNECTION IN THE KEEL AREA, RIGHT SIDE OF AIRCRAFT. REPLACED LEAKING INBOARD SLAT DRIVE HYDRAULIC MOTOR IAW B767 MM 27-81-11-4. OPS AND LEAK CHECKED GOOD. PERFORMED AIR CONDITIONING SYSTEM OIL CONTAMINATION REMOVAL IAW B767 MM 21-00-21-2 FOR THE RIGHT AC PACK. 2 L 7 2 4F RT A1NM 2002010400089 20020104 00089 WP 2002 1 4 ABXA010654 1 20011227 A 2611 LIGHT DOUG DC8 DC863 302198A WP SMOKE DETECTOR INOPERATIVE A ABXA K NONE N FALSE WARNING CL CLIMB 1 GL 23 825AX 46115 ON CLIMBOUT, UPPER CARGO SMOKE LIGHT CAME ON. NO SMOKE OR UNUSUAL SMELLS NOTED. NR 3 SMOKE DETECTOR APPEARED TO GIVE F ALSE INDICATION. RELAMPED THE NR 3 UPPER CARGO SMOKE DETECTOR. OPS CHECKED GOOD IAW DC-8 MM 26-10-00. 2 L 7 4 4F 4A25 2002010400090 20020104 00090 WP 2002 1 4 ABXA010655 1 20011224 A 2761 3644322507 ACTUATOR DOUG DC8 DC863F 302198F WP SPOILER BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 ON SERVICE CHECK, FOUND BOTH CRANK ASSEMBLIES TO THE RIGHT WING INBOARD SPOILER RODS BROKEN. REPLACED BOTH INBOARD SPOI LER REAR SPAR ACTUATOR CRANK ASSEMBLIES IAW DC-8 MM 27-61-01-2-0001. 2 L 7 4 4F 4A25 2002010400091 20020104 00091 WP 2002 1 4 ARWA20011210 1 20011218 A 3220 57714073 BRACE DOUG DC8 DC85F54 3021926 WP NLG BROKEN A ARWA O OTHER E VIBRATION/BUFFET AP APPROACH 1 SO 19 426FB 21657 45667 AT FLIGHT LEVEL 31.0 HEARD LOUD BANG NOISE UNDER COCKPIT AREA, ALSO ON APPROACH LOWERING GEAR LARGE BANG AND AIRCRAFT SH OOK. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND LT NOSE LANDING GEAR SIDE BRACE RETRACT ACT LUG BROKEN. REMOVED AND REPL ACED LT NOSE LANDING GEAR SIDE BRACE IAW MM 32-2-0. PERFORMED NOSE LANDING GEAR OPS CHECK IAW MM 32-2-0. OPS NORMAL, N O LEAKS NOTED. 2 L 7 4 4F RT 4A25 2002010400092 20020104 00092 WP 2002 1 4 ARWA20011211 1 20011220 A 3260 FITTING DOUG DC8 DC862 3021970 WP RT MLG EXCESS PLAY A ARWA K NONE N FALSE WARNING CR CRUISE 1 SO 19 1804 45896 DEPARTING KATL, GEAR NOT LATCHED LIGHT ILLUMINATED. ABNORMAL CHECKLIST COMPLETED AND LIGHT DID NOT EXTINGUISH, AFTER EA CH UPLATCH CHECK (IN UPLATCH CHECK POSITION). CORRECTED PLAY AT RIGHT MLG UPLOCK ROLLER FITTING, ALSO LUBRICATED ALL GE ARS. LANDING GEAR OPERATIONAL CHECK PERFORMED SEVERAL TIMES, ALL CKD NORMAL MM 12-81-1 AND MM 32-10-0. AIRCRAFT RETURN ED TO SERVICE. 2 L 7 4 4F 4A25 2002010400093 20020104 00093 NE 2002 1 4 ARWA20011212 2 20011223 A 7532 BLEED VALVE DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE NR 3 ENGINE LACK OF LUBE A ARWA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 19 802BN 45909 671379 NR 3 ENGINE COMPRESSOR STALL AT BRAKE RELEASE MAX POWER 1.89 EPR RETURN TO RAMP FOR CKV & FOR NOTE 13 DEGREE CELSIUS ENG INE ANTI ICE OFF AND NO WIND. LUBED SURGE BLEED VALVE IAW MM 75-30-3, SYSTEM OPS CKD NORMAL IAW MM 71-00 ENGINE RUN. A IRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F 4A25 1E8 2002010400094 20020104 00094 WP 2002 1 4 ARWA20011213 1 20011227 A 2910 HYDRAULIC LINE DOUG DC8 DC862 3021970 WP HYDRAULIC SYS LEAKING A ARWA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 19 810BN 45905 LOSS OF HYDRAULIC FLUID DURING LANDING ROLL IN SKBO. COMPLETED ABNORMAL EMERGENCY CHECKLIST, LEAK STOPPED. TAXIED UNEVE NTFUL TO CARGO RAMP. T/S AND FOUND STANDBY RUDDER ACCUMULATOR PRESSURE HYDRAULIC HOSE TO PUMP LEAKING. REMOVED AND REP LACED HIGH PRESSURE HYDRAULIC HOSE IAW MM 27-24-3, SERVICED MAIN HYD RESERVOIR IAW MM 12-30-1, CK FOR LEAKS AND OPS CKD STANDBY RUDDER SYSTEM IAW MM 27-24-0. NO LEAKS NOTED & OPS CKD GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002012900098 20020129 00098 WP 2002 1 29 ARWA20011216 1 20011229 A 7920 570538 FILTER HOUSING DOUG DC8 DC861 3021952 WP NR 4 ENGINE DEFECTIVE A ARWA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 19 29UA 46159 NR 4 ENGINE OIL PRESSURE ERRATIC FLUCTUATES BETWEEN 0 TO 20 PSI WITH OIL PRESSURE LIGHT ON. ENGINE SHUTDOWN AS PER ABNO RMAL CHECKLIST AND PROCEDURES. AIRCRAFT LANDED UNEVENTFUL. REMOVED AND REPLACED GEARBOX IAW MM 72-00. ACCOMPLISHED RU N UP, NO LEAKS NOTED. OIL PRESSURE FLUCTUATES. REMOVED AND REPLACED OIL FILTER HOUSING. ACCOMPLISHED RUN UP IAW MM 71 -00. OIL PRESSURE NORMAL AND NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002010400096 20020104 00096 WP 2002 1 4 ARWA20011217 1 20011229 A 8011 OIL CAP DOUG DC8 DC861 3021952 WP STARTER LOOSE A ARWA E D ENGINE SHUTDOWN RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 SO 19 30UA 45888 DURING PUSHBACK MECHANIC REPORTED OIL LEAK ON NR 3 ENGINE, SHUTDOWN NR 3 ENGINE AND RETURNED TO RAMP UNDER TOW. FOUND N R 3 STARTER OIL CAP LOOSE, SERVICED AND SECURED OIL CAP IAW MM 80-10-0. LEAK CK ON RUN UP, NO LEAKS NOTED DURING RUN UP IAW MM 71-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002010400097 20020104 00097 NM 2002 1 4 AWXA200100660 1 20011206 A 5312 6545409831 PRESSURE PANEL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - C - DURING C-15 CHECK MAINTENANCE DISCOVERED PRESSURE WEB CRACKED IN TWO PLACES BS 664, RBL 38. MA INTENANCE CUT OUT DAMAGED SECTION OF WEB, FABRICATED AND INSTALLED THE NEW WEB, FILLERS, DOULBERS, TRIPLERS, AND A STIFF ENER AT BS 664, RBL 38 IAW AWA ER 03-5310-01353-TB3. 2 L 7 2 4F RT A16WE 2002010400098 20020104 00098 NM 2002 1 4 AWXA200100661 1 20011206 A 5315 654681138 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - C - DURING C-15 CHECK MAINTENANCE DISCOVERED SURFACE OF CABIN FLOORBEAM CORRODED AT BS 986.5, LBL 1 6 TO RBL 45. MAINTENANCE CLEANED CORROSION, BLENDED AREA, AND MEASURED SURFACE LOSS AT .025 (OUT OF LIMITS PER B737-300 SRM 53-60-51). LOWER ATTACH ANGLE, 2 EACH SUPPORTS, AND THE UPPER T-CHORD LBL 52 TO RBL 52 WERE REMOVED, FABRICATED, A ND INSTALLED IAW B737-300 SRM 51-40-02, PG 10-11, AND AWA ER 03-5365-01352-SS1. 2 L 7 2 4F RT A16WE 2002010400099 20020104 00099 NM 2002 1 4 AWXA200100662 1 20011207 A 5313 6546877144 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - C - DURING C-15 CHECK MAINTENANCE DISCOVERED STR 18A CRACKED AT THE AFT END OF BS 727 RT WHEEL WELL . MAINTENANCE CUT OUT DAMAGED AREA AND PERFORMED HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED. FABRICATED AND INSTALL ED FILLER AND L-STIFFENER BS 727, IAW AWA ER 03-5312-01353-TB1. 2 L 7 2 4F RT A16WE 2002010400100 20020104 00100 NM 2002 1 4 AWXA200100663 1 20011209 A 5313 6546877143 STRINGER BOEING 737 7373G7 1384595 NM FUSLEAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - C - DURING C-15 CHECK MAINTENANCE DISCOVERED STR 18A CRACKED AT INBOARD AFT CORNER LT WHEEL WELL. MAINTENANCE CUT OUT DAMAGED AREA AND PERFORMED HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED. FABRICATED AND INSTALLED FILLER AND L-STIFFENER BS 727, IAW AWA ER 03-5312-01353-TB1. 2 L 7 2 4F RT A16WE 2002010400101 20020104 00101 NM 2002 1 4 AWXA200100667 1 20011222 A 5230 65C8073525 TEE FITTING BOEING 737 7373G7 1384595 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - C - DURING C-15 CHECK MAINTENANCE FOUND AFT CARGO DOOR LWR BEAM TEE CRACKED AT 2 FASTENER HOLES AFT END BS 840. MAINTENANCE REMOVED AND REPLACED UPPER FWD FRAME ON AFT CARGO DOOR BS 840 IAW AWA EO 52-33-02. 2 L 7 2 4F RT A16WE 2002010400102 20020104 00102 NM 2002 1 4 AWXA200100669 1 20011221 A 5330 654578916 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 334AW 23748 MCN - MAJOR REPAIR - C - DURING C-13 CHECK MAINTENANCE DISCOVERED A 2 INCH CRACK AT SCREW HOLE ON EQUIPMENT COOLING EXHA UST PANEL BS 360, STR 25L. HFEC INSPECTION VERIFIED CRACK FROM THE END OF SKIN TO THE SECOND FASTENER HOLE. FABRICATED REPAIR DOUBLER AND SPACER AND INSTALLED REPAIR AT BS 360, STR 25L IAW AWA ER 03-5331-01352-TB4. 2 L 7 2 4F RT A16WE 2002010400103 20020104 00103 NM 2002 1 4 AWXA200100670 1 20011209 A 5230 6546921528A DOOR FRAME BOEING 737 7373Y0 1384671 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 334AW 23748 MCN - MAJOR REPAIR -C- DURING C-13 CHECK MAINTENANCE DISCOVERED A CRACK AT THE AFT END OF FWD CARGO DOOR LOWER TEE CHORD BETWEEN 2 FASTENERS IN THE VERTICAL LEG BS 490. MAINTENANCE CUT OUT DAMAGED AREA OF TEE CHORD AT BS 490, FABRICATED DO UBLER AND FILLER, INSTALLED REPAIR PARTS IAW EO 52-31-04. 2 L 7 2 4F RT A16WE 2002010400104 20020104 00104 NM 2002 1 4 AWXA200100672 1 20011227 A 3350 1012721 LIGHT BOEING 737 737277 1384570 NM CABIN MISSING A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 22651 LAS - EEL - EMERGENCY PATH LIGHT ASSEMBLY MISSING SEAT ROW 12 LT SIDE. MAINTENANCE REPLACED LIGHT ASSEMBLY AT SEAT ROW 12 LT SIDE, FUNCTIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002010400105 20020104 00105 NM 2002 1 4 AWXA200100674 1 20011205 A 3397 1721681 CONNECTOR BOEING 737 7373G7 1384595 NM CABIN DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - EEL - C - DURING C-15 CHECK MAINTENANCE DISCOVERED CABIN SEAT MOUNTED EMERGENCY PATH LIGHT HARNESS WITH NUMEROUS D AMAGED SPLICES AND A BAD CONNECTOR. MAINTENANCE REMOVED AND REPLACED SPLICES AND DAMAGED CONNECTOR IAW B737 SOPM 20-42- 01 PG 21-26, AND B737 SWPM 20-42-01 PG 1-6. SYSTEM WAS OPERATIONAL TEST WAS GOOD IAW AWA T/C A1C33006. 2 L 7 2 4F RT A16WE 2002010400106 20020104 00106 EA 2002 1 4 COMA0260025 1 20011231 A 3610 7G989 SWITCH CNDAIR CL600 CL6002B19 1900309 EA AFT EQUIP MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 956CA 7105 FLIGHT 5527 - AFTER T/O, L/H AC PACK HIGH PRESSURE MESSAGE, FOLLOWED BY BLEED AIR DUCT MESSAGE, FOLLOWED BY L/H JET PIPE OVERHEAT, FOLLWOED BY R/H AC PACK HIGH PRESSURE.REPLACED THE L/H AC PACK PRESSURE SWITCH. 2 L 7 2 4F RT A21EA 2002010400107 20020104 00107 NM 2002 1 4 AWXA200100675 1 20011221 A 3350 CONTACTOR BOEING 737 7373G7 1384595 NM CABIN WORN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 154AW 23776 MCN - EEL - C - DURING C-15 CHECK MAINTENANCE DISCOVERED INOPERATIVE EMERGENCY EXIT LIGHT ABOVE THE R2 SERVICE ENTRY DOO R. MAINTENANCE REPLACED WORN CONTACT AT EXIT LIGHT ASSEMBLY ABOVE R2 SERVICE ENTRY DOOR IAW BSWPM 20-92-00, PG 1-2, OPE RATIONAL CHECK WAS GOOD IAW AWA T/C A1C33009. 2 L 7 2 4F RT A16WE 2002010400108 20020104 00108 NM 2002 1 4 AWXA200100676 1 20011221 A 3350 CONTACTOR BOEING 737 7373G7 1384595 NM CABIN WORN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 154AW 23776 MCN - EEL - C - DURING C-15 CHECK MAINTENANCE DISCOVERED INOPERATIVE EMERGENCY EXIT LIGHT FWD OF THE R2 SERVICE ENTRY DO OR. MAINTENANCE REPLACED WORN CONTACT AT EXIT LIGHT ASSEMBLY FWD OF R2 SERVICE ENTRY DOOR IAW BSWPM 20-92-00, PG 1-2, O PERATIONAL CHECK WAS GOOD IAW AWA T/C A1C33009. 2 L 7 2 4F RT A16WE 2002010400109 20020104 00109 NM 2002 1 4 AWXA200100679 1 20011229 A 3397 BMS13311 WIRE BOEING 737 7373Y0 1384671 NM CABIN CHAFED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 334AW 23747 PHX - EEL - C - ESCAPE PATH LIGHTING IS INOPERATIVE ROWS 7 THROUGH 11. MAINTENANCE FOUND WIRE SHORTED TO SEAT TRACK AT ROW 10 LT. MAINTENANCE REPAIRED AND REPOSITIONED WIRE AT SEAT ROW 10 LT IAW SPWM 20-10-13, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002010400110 20020104 00110 EU 2002 1 4 AWXA200100680 1 20011229 A 3350 321454 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 663AW 2588 1419 PHX - EEL - C - EMERGENCY LIGHT SYSTEM FAILED TEST DURING INSPECTION. MAINTENANCE TROUBLESHOT AND REPLACED THE LT AND R T CENTER CABIN EMERGENCY POWER SUPPLIES 11WL AND 12WL IAW AMM 33-51-38-400-001. 2 L 7 2 4F RT A28NM 2002010400112 20020104 00112 NM 2002 1 4 C1HA200192011 1 20011216 A 3010 VALVE BOEING 727 727212 138407G NM WING LEAKING A C1HA K NONE J WARNING INDICATION CR CRUISE 1 GL 15 292AS 21458 NR 3 ENGINE STRUT LIGHT ILLUMINATED. (DUCT PRESS L-20 R-48). SWAPPED BLEEDS TO NR 2 LIGHT EXTINGUISHED. FOUND WING AN TI-ICE H/P VALVE LEAKING. RESECURED HARDWARE IAW MM 30-11-11. ALSO FOUND CLAMP ON PNEUMATIC DUCT LEAKING. RESECURED I AW MM 36-00-1. LEAK CHECK GOOD AT IDLE AND T/O POWER WITH PANELS REMOVED AND INSTALLED. DUCT PRESSURES WERE NORMAL. 2 L 7 3 4F A3WE 2002010400113 20020104 00113 EU 2002 1 4 C2XA01BT178 1 20011228 A 3350 3011206 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 19812 099 DURING 1A INSPECTION MAINTENANCE FOUND EXTERIOR LEFT FORWARD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EXTERIOR LEFT FORWARD EMERGENCY LIGHT IAW ATR42 JIC 33-51-24. OPS CHECKED GOOD. 2 H 7 2 4T RT A53EU 2002010400114 20020104 00114 SO 2002 1 4 C2XA01BT179 1 20011222 A 2497 WIRE EMB 145 EMB145ER 3260211 SO COCKPIT LOOSE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 13935 145022 CREW REPORTED AFTER SHUTTING DONE ENGINES AT THE GATE, SMOKE NOTICED IN COCKPIT, APU SUBSEQUENTLY SHUTDOWN. MAINTENANCE RAN ENGINES AND FOUND NO SMOKE. OPS CHECKED GOOD. INSPECTED COCKPIT, FOUND TWO WIRES INSIDE PEDESTAL NOT SECURED. RE PAIRED WIRING IAW EMB145 MM 20-00-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2002010400115 20020104 00115 SO 2002 1 4 C2XA01BT180 1 20011226 A 3350 LIGHT EMB 145 EMB145ER 3260211 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 14942 145037 CREW REPORTED TO MCC IN IAH THE EMERGENCY FLOOR LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REPAIRED LIGHTS. 2 L 7 2 4F RT T00011AT 2002010400116 20020104 00116 SO 2002 1 4 C2XA01CL243 1 20011214 A 5230 12050447001 SPRING EMB 145 EMB145LR 3260212 SO CARGO DOOR BROKEN A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 16954 145072 CLE FLIGHT 3171 THE CREW REPORTED A CARGO DOOR OPEN MESSAGE AFTER TAKEOFF. THE AIRCRAFT DIVERTED INTO RIC AND LANDED WI THOUT INCIDENT. MAINTENANCE REPLACED THE CARGO DOOR LOCK SPRING FOR THE VENT DOOR. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2002010400117 20020104 00117 SO 2002 1 4 C2XA01CL244 1 20011214 A 3350 110049 CHARGER EMB 135 EMB135ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 27506 145206 DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE AT BOTH OVERWING EXITS IN THE CABIN. MAINTENANCE REPLACED THE NR 3 BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002010400118 20020104 00118 SO 2002 1 4 C2XA01CL246 1 20011217 A 3610 CLAMP EMB 145 EMB145ER 3260211 SO BLEED AIR LOOSE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 17928 145007 CLE FLIGHT 3011 THE CREW REPORTED A BLEED LEAK WARNING AFTER TAKEOFF ALONG WITH A ANTI-ICE FAIL MESSAGE. THE AIRCRAFT R ETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND RESECURED A V-BAND CLAMP ON THE BLE ED DUCT FOR THE STAB ANTI-ICE SYSTEM IN THE AFT AVIONICS BAY. 2 L 7 2 4F RT T00011AT 2002010400119 20020104 00119 SO 2002 1 4 C2XA01CL247 1 20011217 A 3234 7455501 CONTROL HANDLE EMB 135 EMB135LR 3260305 SO COCKPIT INTERMITTENT A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 15527 1344 145413 CLE FLIGHT 3064 THE CREW REPORTED THE LANDING GEAR DID NOT RETRACT. RECYCLED AND IT WAS SLOW TO RETRACT. MAINTENANCE R EPLACED THE LANDING GEAR HANDLE ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT TOOO11AT 2002010400120 20020104 00120 SO 2002 1 4 C2XA01CL248 1 20011216 A 2120 ODOR EMB 135 EMB135ER 3260203 SO CABIN DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 19503 145176 CLE FLIGHT 3184 THE CREW REPORTED A STRONG FUEL SMELL WHEN THE APU WAS STARTED IN FLIGHT. THE APU WAS SHUT DOWN IMMEDIA TELY. MAINTENANCE INSPECTED AND PERFORMED A OPERATIONAL CHECK OF THE APU AND NO DEFECTS WERE FOUND. THE AIRCRAFT WAS R ELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002010400121 20020104 00121 SO 2002 1 4 C2XA01CL249 1 20011219 A 2520 SCREW EMB 145 EMB145ER 3260211 SO CABIN LOOSE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15948 145056 CLE MAINTENANCE, DURING ROUTINE MAINTENANCE THE LEFT OVERWING EMERGENCY EXIT WOULD NOT OPEN. MAINTENANCE FOUND A LOOSE SCREW FOR THE INTERIOR TRIM PANEL STICKING OUT ENOUGH TO PREVENT THE DOOR FROM WORKING PROPERLY. THE SCREW WAS TIGHTENE D AND OPERATIONAL CHECKS OF THE EMERGENCY EXIT WERE GOOD. 2 L 7 2 4F RT T00011AT 2002010400123 20020104 00123 SO 2002 1 4 C2XA01CL251 1 20011222 A 3230 355022002 CONTROL UNIT EMB 145 EMB145LR 3260212 SO COCKPIT FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14952 9209 7251 145067 CLE FLIGHT 3243 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE IMMEDIATELY AFTER TAKEOFF. THE LANDING GEAR WO ULD NOT RETRACT. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LAND ING GEAR ELECTRONIC UNIT AND THE NOSE GEAR AIR/GROUND PROXIMITY SWITCH. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002010400124 20020104 00124 SO 2002 1 4 C2XA01CL252 1 20011222 A 2120 ODOR EMB 135 EMB135ER 3260203 SO COCKPIT DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 27506 145206 CLE FLIGHT 3160 THE CREW REPORTED A STRONG FUEL SMELL IN THE COCKPIT WHEN THE APU WAS STARTED IN FLIGHT. MAINTENANCE PE RFORMED OPERATIONAL CHECKS OF APU AND APU BLEED SYSTEM AND FOUND NO DEFECTS. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002010400125 20020104 00125 SO 2002 1 4 C2XA01CL253 1 20011222 A 4930 164161100 CHECK VALVE EMB 145 EMB145LR 3260212 SO APU STICKS A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 13955 145075 CLE FLIGHT 3218 THE CREW REPORTED A STRONG FUEL SMELL IN THE COCKPIT AND FORWARD CABIN WHEN THE APU IS STARTED. THE APU WAS PLACED ON MEL. MAINTENANCE REMOVED AND REPLACED THE APU FUEL DRAIN CHECK VALVE. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2002010400126 20020104 00126 SO 2002 1 4 C2XA01CL254 1 20011224 A 3610 S2U226 O-RING EMB 145 EMB145ER 3260211 SO BLEED AIR DETERIORATED A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 17928 145007 CLE FLIGHT 3321 THE CREW REPORTED ON DEPARTURE AT FULL TAKEOFF THRUST, RECEIVED A BLEED 1 LEAK EICAS MESSAGE. QRH COMPL ETED AND THEN RECEIVED A BLEED 2 LEAK MESSAGE. AFTER EXITING ICING CONDITIONS THE MESSAGES CLEARED. MAINTENANCE REPLAC ED THE O-RINGS IN THE BLEED DUCT LINES. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002010400128 20020104 00128 NM 2002 1 4 ZW0A0200301 1 20010104 A 3350 8039001 BATTERY PACK DOUG MD80 MD83 3023681 NM A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 951TW 53470 THE EGRESS FLOOR PATH LIGHTING WAS INOPERATIVE FROM ROW 14 TO 21. REPLACED THE BATTERY PACK. CHECK-C 6-6-01 STL. --CL OSED-- 2 L 7 2 4F RT 2002010400130 20020104 00130 NM 2002 1 4 ASAA0140115 1 20011013 A 3350 8100022605 LIGHT BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 769AS 25103 SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHT AT ROW 14-19 DISCONNECTED. RECONNECTED TRACK LIGHTS, OPERATIONAL C HECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002010400137 20020104 00137 EU 2002 1 4 RAIA00112014 1 20011229 A 3242 AHA1835 BRAKE ASSY JETAIR JETSTM JETSTM4101 1500501 EU DRAGGING A RAIA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 03 555HK 1505 1505 RM202 41072 5523-STL- RIGHT BRAKE LOCKED DURING TAXI. MAINTENANCE REMOVED AND REPLACED BOTH RIGHT MLG BRAKES. BLEED BRAKE PRESSURE S YSTEMS IAW J41 MM 32-41 2 L 7 2 4T RT A41NM 2002010400138 20020104 00138 EU 2002 1 4 RAIA00112015 1 20011230 A 3242 320511 VALVE JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 555HK 13915 41072 5534-STL- DURING TAXI BRAKES LOCKED. MAINTENANCE REMOVED AND REPLACED BRAKE RELAY VALVE IAW J41 MM 32-41-10 2 L 7 2 4T RT A41NM 2002010700001 20020107 00001 NM 2002 1 7 SWAA013452 1 20011231 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED BETWEEN BS BS 616 AND BS 639, STR 4L. REPAIRED SKIN PER SWA RA. 2 L 7 2 4F A16WE 2002010700006 20020107 00006 WP 2002 1 7 ARWA20011215 1 20011228 A 7920 LINE DOUG DC8 DC85F54 3021926 WP PWA JT3D JT3D3B 52039 NE NR 3 ENGINE LEAKING A ARWA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 426FB 45667 644690 NR 3 ENGINE LOSS OF OIL QUANTITY OSCILLATING OIL PRESS AND OIL PRESS WARNING ON AND OFF. SHUT DOWN NR 3 ENGINE AS PER A BNORMAL CHECKLIST OIL PRESS 15 PSI, 1 HOUR WINDMILLING. AIRCRAFT RETURNED TO KMIA UNEVENTFUL. INSPECTED ENGINE AND FOU ND ENGINE OIL COOLER OIL LINE LEAKING. REMOVED AND REPLACED LINE IAW MM 79-1-5. INSPECTED MAIN OIL FILTER, FOUND CLEAN AND NO DEFECT NOTED. SERVICED ENGINE IAW MM 12-20-1. PERFORMED ENGINE OIL LEAK ON GROUND RUN UP, FOUND NO LEAKS AND A LL ENGINE PARAMETERS NORMAL IAW MM 71-00 & 72-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT 4A25 1E8 2002010700008 20020107 00008 SO 2002 1 7 C2XA01CL255 1 20011225 A 2530 CBC16707 RECEPTACLE EMB 145 EMB145LR 3260212 SO GALLEY BURNED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 14916 145415 CLE FLIGHT 4004 THE CREW REPORTED A SMELL OF SMOKE IN THE GALLEY, POSSIBLY FROM THE COFFEE WARMERS. MAINTENANCE INSPECT ED AND REPLACED THE LEFT COFFEE WARMER RECEPTACLE. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2002010700009 20020107 00009 SO 2002 1 7 C2XA01CL256 1 20011223 A 2120 ODOR EMB 135 EMB135LR 3260305 SO COCKPIT DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SW 27 28518 145334 CLE FLIGHT 3051 THE CREW REPORTED A FUEL SMELL IN THE COCKPIT AFTER LANDING AND AFTER STARTING APU. MAINTENANCE INSPECT ED AND STARTED AND RAN APU. NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT TOOO11AT 2002010700010 20020107 00010 SO 2002 1 7 C2XA01CL258 1 20011229 A 5210 BOLT EMB 145 EMB145ER 3260211 SO DOOR HANDLE DEFECTIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15948 145056 DURING ROUTINE MAINTENANCE THE MAIN ENTRY DOOR WAS DIFFICULT TO OPEN FROM OUTSIDE AND WILL NOT CLOSE FROM INSIDE. MAINT ENANCE ADJUSTED THE EXTERNAL ACTUATING HANDLE AND REPLACED BOLTS TO THE INTERIOR HANDLE BRACKET. 2 L 7 2 4F RT T00011AT 2002010700011 20020107 00011 SO 2002 1 7 C2XA01CL259 1 20011230 A 2530 1095 COFFEEMAKER EMB 145 EMB145LR 3260212 SO GALLEY DEFECTIVE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 14907 145468 BDL FLIGHT 3024 THE CREW REPORTED A BURNING SMELL FROM THE COFFEE POT. MAINTENANCE REPLACED THE COFFEE POT. OPERATIONA L CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002010700012 20020107 00012 SO 2002 1 7 C2XA01CL260 1 20011228 A 4930 CHECK VALVE EMB 145 EMB145ER 3260211 SO APU DIRTY A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 14945 145049 CLE FLIGHT 3075 THE CREW REPORTED A STRONG FUEL SMELL IN THE CABIN WITH THE APU BLEED ON. MAINTENANCE INSPECTED AND PLA CED THE APU ON MEL. MAINTENANCE CLEANED COMBUSTOR DRAIN CHECK VALVE. OPERATIONAL CHECKS OF APU WERE GOOD. NO FUEL SME LL WAS NOTED IN CABIN OR COCKPIT. 2 L 7 2 4F RT T00011AT 2002010700013 20020107 00013 SO 2002 1 7 C2XA01IA416 1 20011212 A 2120 ODOR EMB 145 EMB145LR 3260212 SO COCKPIT DETECTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 27 13955 145075 EWR - DURING APPROACH ON FLIGHT 3359, THE CREW REPORTED THAT THERE WAS A STRONG FUEL ODOR IN THE COCKPIT WHEN THE APU WA S STARTED. THE AIRCRAFT LANDED SAFELY AT EWR, WHERE MAINTENANCE RELEASED THE AIRCRAFT UNDER MEL 49-00-00. MAINTENANCE IN CLE PERFORMED OPERATIONAL TESTS OF THE APU AND IT'S ASSOCIATED SYSTEMS. NO FUEL ODOR OR DEFECTS WERE NOTED. 2 L 7 2 4T RT T00011AT 2002010700014 20020107 00014 EU 2002 1 7 C2XA01IA420 1 20011219 A 3260 D22924010 PROXIMITY SWITCH AEROSP ATR42 ATR42320 8680930 EU LT MLG FAILED A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 15827 175 IAH- ON FLIGHT 3659 THE CREW NOTED THAT THE SECONDARY LANDING GEAR INDICATOR WAS SHOWING LEFT MAIN LANDING GEAR UNLOCKED . MAINTENANCE REMOVED AND REPLACED THE LEFT HAND LANDING GEAR PROX SWITCH. PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002010700015 20020107 00015 SO 2002 1 7 C2XA01IA421 1 20011220 A 3397 P0390 CONNECTOR EMB 120 EMB120ER 3260203 SO CABIN LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16718 120136 IAH- DURING A-CHECK, NOTED THAT THE EMERGENCY LIGHT IN TRACK OUT AT SEATS 2A THRU 5A. MAINTENANCE RESECURED THE CONNEC TOR ON THE EMERGENCY BATTERY PACK NUMBER 2, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS N OTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2002010700016 20020107 00016 GL 2002 1 7 C2XA01TY202 2 20011215 A 7270 23062267 BYPASS JACKET EMB 135 EMB135ER 3260203 SO ALLSN AE300 AE3007A GL ENGINE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 TYS DURING A SCHEDULE INSPECTION, BETWEEN THE FAN CASE AND THE OUTER BYPASS, OXIDATION WAS FOUND ON NR 1 AND NR 2 ENGIN E. MAINTENANCE REMOVED THE OXIDATION, PERFORMED TOUCHUP OF PERMANENT RESIN COATING ON ACCESS, GEAR BOX MOUNTS, PLACED A CHEMICAL-FILM COATING FOR MAGNESIUM AND PAINTED WITH A CORROSION PAINT IAW AE3007EC7220-01009, AESPM70-32-03 AND AE3007 ASMM70-00-00 WHICH WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002010700017 20020107 00017 SO 2002 1 7 C2XA01TY207 1 20011224 A 5320 14522460013 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 TYS, DURING A SCHEDULED 1C INSPECTION, CORROSION WAS FOUND ON THE CENTER TOP CAP AFT OF GUSSET. MAINTENANCE REMOVED AN D REPLACED THE TOP CAP IAW EMB-135/145-SRM-51-40-02. THE REPAIR PROCEDURES WHERE SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002010700018 20020107 00018 SO 2002 1 7 C2XA01TY209 1 20011228 A 5320 14521725013 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 TYS DURING A SCHEDULED 1-C INSPECTION CORROSION WAS FOUND ON THE RIGHT SILL AT FRM17 AROUND A NUT PLATE. MAINTENANCE R EMOVED THE CORROSION IAW 135/145 CPM 51-14-02. THIS WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL INSPEC TION. 2 L 7 2 4F RT TOOO11AT 2002010700019 20020107 00019 SO 2002 1 7 C2XA01TY211 1 20011228 A 5315 14521700007 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 TYS DURING A SCHEDULED 1-C INSPECTION CORROSION WAS FOUND AT THE LEFT OMEGA BEAM. MAINTENANCE CLEAN INSPECTED AND OVER SIZE ONE RIVET IAW EMB 135/145 SRM 51-10-02 AND 51-40-02. WILL BE RELEASED UPON COMPLETION OF THE 1-C INSPECTION. 2 L 7 2 4F RT TOOO11AT 2002010700020 20020107 00020 SO 2002 1 7 C2XA01TY212 1 20011228 A 3211 14567069001 BRACE EMB 135 EMB135LR 3260305 SO LT MLG GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 TYS DURING A SCHEDULED 1-C INSPECTION THE LEFT MLG SIDE BRACE WING ATTACHMENT WAS FOUND SCRATCHED AND GOUGED WHICH REQU IRED A GST. WILL BE RELEASED UPON COMPLETION OF THE 1-C INSPECTION. 2 L 7 2 4F RT TOOO11AT 2002010700021 20020107 00021 SO 2002 1 7 C2XA01TY213 1 20011229 A 2620 14531342403 TUBE EMB 135 EMB135LR 3260305 SO APU BAY DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 TYS DURING A SCHEDULED 1-C INSPECTION THE APU FIRE EXTINGUISHER DISCHARGE TUBE WAS FOUND DENTED NEXT TO THE FITTING AT APU FIREWALL. MAINTENANCE REMOVED AND REPLACED THE APU DISCHARGE TUBE IAW EMB 135AMM 20-10-03. ALL WORK WAS ACCOMPLIS HED AND WILL BE RELEASED UPON COMPLETION OF THE 1-C INSPECTION. 2 L 7 2 4F RT TOOO11AT 2002010700022 20020107 00022 SO 2002 1 7 C2XA01TY214 1 20011229 A 3211 14567115403 BRACE EMB 135 EMB135LR 3260305 SO LT MLG GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 TYS DURING A SCHEDULED 1-C INSPECTION THE LEFT MLG SIDE BRACE WING ATTACHMENT WAS FOUND SCRATCHED AND REQUIRED A GST. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF THE 1-C INSPECTION. 2 L 7 2 4F RT TOOO11AT 2002010700023 20020107 00023 SO 2002 1 7 C2XA01TY216 1 20011229 A 5751 14569009407 ATTACH FITTING EMB 135 EMB135LR 3260305 SO AILERON GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 TYS DURING A SCHEDULED 1-C INSPECTION, NOTED THAT THE LEFT AILERON FITTING WAS GOUGED. ALL WORK WAS ACCOMPLISHED AND W ILL BE RELEASED UPON COMPLETION OF C-CHECK INSPECTION. 2 L 7 2 4F RT TOOO11AT 2002010700024 20020107 00024 SO 2002 1 7 C2XA01TY217 1 20011230 A 5320 14521725013 RIVET EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 TYS DURING A SCHEDULED 1-C INSPECTION TWO RIVETS WERE FOUND CORRODED UNDERNEATH THE SERVICE DOOR THRESHOLD. MAINTENANC E REMOVED AND REPLACED THE TWO RIVETS. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF C-CHECK INSPEC TION. 2 L 7 2 4F RT TOOO11AT 2002010700025 20020107 00025 GL 2002 1 7 C2XA01TY218 2 20011230 A 7270 23062267 BYPASS JACKET EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL NR 1 ENGINE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 CAE311500 TYS DURING A SCHEDULED 1-C INSPECTION THE NR 1 FANCASE TO BYPASS HAD CORROSION. MAINTENANCE CLEANED UP THE CORROSION. APPLIED CHEMICAL FILM COATING TO THE MAGNESIUM IAW RR AE3007A MM 70-00-00-300-818 AND APPLIED CORROSION RESISTANT PAINT IAW EC7220-01009. ALL WORK WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETION OF THE C-CHECK INSPECTION. 2 L 7 2 4F 4 F RT TOOO11AT TE6CH 2002010700026 20020107 00026 2002 1 7 C2XA01TY219 4 20011230 A 3445 DMNI5042 ANTENNA EMB 135 EMB135LR 3260305 SO TCAS CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 TYS DURING A SCHEDULED 1-C INSPECTION THE LOWER TCAS ANTENNA WAS CORRODED. MAINTENANCE REMOVED AND REPLACED THE TCAS A NTENNA IAW EMB 135 AMM34-43-03, PERFORMED OPS CHECK IAW EMB 135AMM 34-43-00. ALL WORK WAS ACCOMPLISHED AND WILL BE RELE ASED UPON COMPLETION OF THE C-CHECK INSPECTION. 2 L 7 2 4F RT TOOO11AT 2002010700027 20020107 00027 SO 2002 1 7 C2XA01TY220 1 20011230 A 5320 14522459003 ANGLE EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 TYS DURING A SCHEDULED 1-C INSPECTION CORROSION WAS DETECTED ON CENTER SUPPORT RAMP NEXT TO THE CARBON FIBER CROSSBEAM. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE AND REINSTALLED THE CARBON FIBER CROSSBEAM IAW EMB 135/145 SRM 51-40-0 2. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF THE 1-C INSPECTION. 2 L 7 2 4F RT TOOO11AT 2002010700028 20020107 00028 SO 2002 1 7 C2XA01TY222 1 20011230 A 3350 66364 LIGHT EMB 135 EMB135LR 3260305 SO CABIN BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 TYS, DURING A SCHEDULED 1C INSPECTION, THE NR 6 EMERGENCY TRACK LIGHT WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACE D THE NR 6 TRACK LIGHTING IAW EMB-135-AMM-33-50-12. OPERATIONAL CHECKED GOOD. AIRCRAFT WILL BE RELEASED UPON COMPLETIO N OF THE INSPECTION. 2 L 7 2 4F RT TOOO11AT 2002010700029 20020107 00029 SO 2002 1 7 C2XA01TY223 1 20011230 A 5315 14521721009 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 TYS, DURING A SCHEDULED 1C INSPECTION, CORROSION WAS FOUND ON SEVERAL AREAS OF THE FORWARD DIGITAL. MAINTENANCE REMOVED FORWARD DIGITAL AND CUT OUT DAMAGED AREA, FABRICATED DOUBLERS AND INSTALLED, REINSTALLED DIGITAL IAW-EC5320-01059, EMB- 135/145-SRM-51-20-03/51-40-02 & 06/51-21-04/05/06. REPAIR PROCEDURES WHERE SATISFACTORY AND THE AIRCRAFT WILL BE RELEAS ED UPON COMPLETION OF THE INSPECTION. 2 L 7 2 4F RT TOOO11AT 2002010700032 20020107 00032 NM 2002 1 7 CALA0101036 1 20011221 A 5743 BEAM BOEING 737 7373T0 1384582 NM LT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 63305 23356 INSPECTION FOUND LT MLG ACTUATOR WALKING BEAM HANGER AND BRACKET HARDWARE CORRODED. A NEW WALKING BEAM HANGER AND BRACK ET HARDWARE WERE INSTALLED IAW MM 57-15-00. 2 L 7 2 4F RT A16WE 2002010700033 20020107 00033 NM 2002 1 7 CALA0101037 1 20011221 A 5414 SKIN BOEING 737 7373T0 1384582 NM LT PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 63305 23356 INSPECTION FOUND A .75 INCH CRACK IN LT ENGINE UPPER PYLON SKIN AT PANEL CUTOUT 5727L. A REPAIR DOUBLER WAS INSTALLED I AW ECRA 5430-01230, REV B. 2 L 7 2 4F RT A16WE 2002020400114 20020204 00114 2002 2 4 CALA0101038 4 20011223 A 3160 4073610916 DISPLAY BOEING 737 737824 13844BZ NM INST PANEL BURNED OUT A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 37255 4021 30610 FLIGHT CREW REPORTED THE SMELL OF SMOKE (NO VISIBLE SIGNS) IN THE COCKPIT DURING CLIMB OUT OF EWR AT 23,000 FEET. THE CR EW DONNED THEIR O2 MASKS AND THE FLIGHT WAS DIVERTED TO PHL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE CAPT AIN'S INBOARD DISPLAY UNIT HAD FAILED AND IT WAS THE SOURCE OF THE SMOKE SMELL. THE DISPLAY UNIT WAS REMOVED AND REPLACE D IAW MM 31-62-11 AND SYSTEM CHECKS WERE NORMAL. THE SDR WILL REMAIN OPEN PENDING ENGINEERING INVESTIGATION. VENDOR TEA RDOWN FOUND PHASE 1 DU A7A1 PRINTED WIRING BOARD(PWB) BURNED ALONG WITH TWO CAPACITORS AND TWO RESISTORS. THIS FAILURE H AD BEEN SEEN IN OTHER UNITS DURING VENDOR TEARDOWN. THE UNIT WAS REPAIRED AND AN ENGINEERING MODIFICATION WAS INCORPORAT 2 L 7 2 4F RT A16WE 2002010700034 20020107 00034 NM 2002 1 7 CALA0101039 1 20011222 A 5730 SKIN BOEING 737 7373T0 1384582 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 63305 23356 INSPECTION FOUND A 1 INCH CRACK ABOVE NR 3 SLAT ACTUATOR IN LT WING LEADING EDGE CUTOUT. THE LEADING EDGE WAS REPAIRED IAW MM 51-70-17. 2 L 7 2 4F RT A16WE 2002010700035 20020107 00035 NM 2002 1 7 CALA0101041 1 20011229 A 5320 CAP BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 63305 23356 INSPECTION FOUND END CAP CORRODED AT STA 540, LONGERON 27R. A NEW END CAP WAS INSTALLED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 2002010700036 20020107 00036 2002 1 7 CALA0101042 4 20011229 A 2565 113317 SLIDE DOUG DC9 DC981 3022081 WP R1 DOOR FAILED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14871 48022 THE R-1 DOOR SLIDE FAILED EMERGENCY SLIDE LIGHT TEST. THE SLIDE WAS REMOVED AND REPLACED IAW WORK CARD 08-2560-1-4300. 2 L 7 2 4F A6WE 2002010700037 20020107 00037 2002 1 7 CALA0101043 4 20011229 A 2565 113311 SLIDE DOUG DC9 DC981 3022081 WP L1 DOOR FAILED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14871 48022 THE L-1 DOOR SLIDE FAILED EMERGENCY SLIDE LIGHT TEST. THE SLIDE WAS REMOVED AND REPLACED IAW WORK CARD 08-2560-1-4300. 2 L 7 2 4F A6WE 2002010700038 20020107 00038 SO 2002 1 7 CHQ00076 1 20011220 A 3820 CAP EMB 145 EMB145 3260210 SO WATER TANK OUT OF POSITION A CHQA H DEACTIVATE SYST/CIRCUITS O OTHER CR CRUISE 1 GL 11 277 145355 AFTER TAKEOFF, F/A NOTICED LOUD AIR RUSHING FROM BEHIND LAV MIRROR, CAPT AND F/O VERIFIED AND TURNED OFF EACH PACK SEPAR ATELY, AND TRIED APU BLEED, NOISE CONTINUED. NOTICED WHILE AIRCRAFT WAS PRESSURIZED, FOUND AIR COMING FROM WATER TANK, FOUND CAP THAT ATTACHES TO NIPPLE CAME UNCONNECTED. RECONNECTED CAP AND OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2002010700039 20020107 00039 EU 2002 1 7 CHQ00077 1 20011221 A 7712 ECU SAAB SF340 SF340A 7850100 EU LT ENGINE FAULTY A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 360 360 LEFT ENGINE TQ INDICATION FLUX ON TAKEOFF ROLL. REMOVED AND REPLACED LEFT ECU, GROUND RAN NO DEFECTS NOTED THIS TIME AN D DATE. 2 L 7 2 4T RT A52EU 2002010700040 20020107 00040 EU 2002 1 7 CHQ00078 1 20011222 A 3260 CONNECTOR SAAB SF340 SF340A 7850100 EU RT MLG DIRTY A CHQA K NONE N FALSE WARNING UK UNKNOWN 1 GL 11 138 138 GPWS PROBLEM CALLING OUT TOO LOW GEAR. FERRIED A/C TO IND. REMOVED, CLEANED AND RE SECURED RIGHT MLG DOWNLOCK SWITCH C ONNECTOR AND OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002010700041 20020107 00041 EU 2002 1 7 CHQ00079 1 20011225 A 2421 GENERATOR SAAB SF340 SF340A 7850100 EU LT ENGINE FAILED A CHQA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 148 148 LEFT AC GEN LIGHT ILLUMINATED. PERFORMED THE ABNORMAL CHECKLIST WITH NO EFFECT ON LEFT AC GEN LIGHT. REMOVED AND REPLA CED LEFT AC GEN AND OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002010700042 20020107 00042 GL 2002 1 7 CHQ00080 2 20011226 A 7200 ENGINE EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL NR 2 MAKING METAL A CHQA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 GL 11 265 145226 CAE311350 NR 2 ENGINE ABNORMAL VIBRATION. FOUND CHIPS ON ALL CHIP DETECTOR. REPLACED ENGINE ON AIRCRAFT. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002010700044 20020107 00044 EU 2002 1 7 CHQ00082 1 20011228 A 3260 CONNECTOR SAAB SF340 SF340A 7850100 EU LANDING GEAR LOOSE A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 118 118 OAT FAIL, TCAS FAIL, AND CONFIG WARNING. RESECURED LOOSE CANNON PLUG ON WOW HARNESS, TEST FLIGHT GOOD. 2 L 7 2 4T RT A52EU 2002010700045 20020107 00045 EU 2002 1 7 CHQ00083 1 20011228 A 7722 GAUGE SAAB SF340 SF340A 7850100 EU COCKPIT FAULTY A CHQA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 11 360 006 LEFT ENGINE ITT FLUX. FERRIED A/C TO PIT. REMOVED AND REPLACED ITT GAUGE, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002010700046 20020107 00046 EU 2002 1 7 CHQ00084 1 20011229 A 3260 UPLOCK SWITCH SAAB SF340 SF340A 7850100 EU NLG FAULTY A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 118 118 WHEN GEAR GOES UP TCAS AND OAT FAIL AND GET CONFIG WARNING. REMOVED AND REPLACED NLG UPLOCK SWITCH AND RETRACTED GEAR, OAT OPERATED NORMAL, TCAS OPERATED NORMAL, WHEN BRINGING POWER BACK TO FLIGHT IDLE GOT CONFIG WARNING. INSTALLED NLG SW ITCH AND THEN OPS CHECK GOOD, NO CONFIG WARNING. 2 L 7 2 4T RT A52EU 2002010700053 20020107 00053 EU 2002 1 7 DHL2001365040 1 20011229 A 2612 FIRE LOOP AIRBUS 300 A300B4203 3930306 EU NR 2 ENGINE MALFUNCTIONED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 365DH 149 NR 2 ENGINE A LOOP WILL NOT TEST. PERFORMED OPERATIONAL CHECK OF NR 2 ENGINE A-LOOP IAW MM 26-12-0. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F RT A35EU 2002010700054 20020107 00054 EU 2002 1 7 DHL2001365050 1 20011126 A 5330 SKIN AIRBUS 300 A300B4203 3930306 EU FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH 149 DENT IN SKIN JUST FWD OF FRAME 3 APPROX 5.30 O'CLOCK POSITION EXCEED LIMIT OF SRM 53-10-00 FIG 609. REMOVED FASTENERS P ER SRM 51-30-30. CUT OUT DAMAGED SKIN PER SRM 51-41-00. FABRICATED PARTS PER SRM 51-41-00. INSTALLED REPAIR PER SRM 5 1-30-30. 2 L 7 2 4F RT A35EU 2002010700055 20020107 00055 NM 2002 1 7 DHL2001708016 1 20011218 A 3040 WINDSHIELD WIPER BOEING 727 72725 1384006 NM WINDSHIELD OUT OF ADJ A DHLA K NONE L NO TEST NR NOT REPORTED 1 SO 01 708DH 18275 F/O WINDSHIELD WIPER DOES NOT WORK ON HALF SPEED. RUNS SLOW ON 3/4 SPEED.ADJUSTED WIPER TENSION PER 727 MM CHAPTER 30-4 2-01, OPS CK SATISFACTORY. 2 L 7 3 4F A3WE 2002010700056 20020107 00056 NM 2002 1 7 DHL2001721010 1 20011227 A 2611 SMOKE DETECTOR BOEING 727 727228 1384083 NM NR 4 FAILED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 721DH 19545 ON P/F FOUND NR 4 RIGHT SMOKE DETECTOR WOULD NOT TEST. USED RIDING SPARE SMOKE DETECTOR FOR USE IN NR 4 RT POSITION. R EMOVED AND REPLACED SMOKE DETECTOR WITH A SERV DETECTOR IAW B727 MM 26-17-000. CHECKS GOOD. DEFERRED IAW DHL GMM 3.5 C AT II CONTROL 8129E. DOES NOT AFFECT SAFE. 2 L 7 3 4F RT A3WE 2002010700057 20020107 00057 NM 2002 1 7 DHL2001724012 1 20011219 A 3260 WARNING LIGHT BOEING 727 727228 1384083 NM COCKPIT ILLUMINATED A DHLA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 724DH 19862 LANDING GEAR UNSAFE LIGHTS ILLUMINATED UPON RETRACTION. RECYCLED GEAR. 2 L 7 3 4F RT A3WE 2002010700058 20020107 00058 NM 2002 1 7 DHL2001724013 1 20011220 A 3350 BATTERY BOEING 727 727228 1384083 NM COCKPIT DISCHARGED A DHLA K NONE L NO TEST NR NOT REPORTED 1 SO 01 724DH 19862 COCKPIT EMERGENCY EXIT LIGHT DOES NOT TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES IAW B-M/M 33-50-101. 2 L 7 3 4F RT A3WE 2002010700060 20020107 00060 NM 2002 1 7 DHL2001748013 1 20011218 A 2612 FIRE LOOP BOEING 727 727225 1384077 NM NR 2 ENGINE OUT OF POSITION A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 748DH 22440 THE NR 2 CENTER DETECTOR GROUND CIRCUIT LIGHT ILLUMINATED ON P6-3 PANEL. DEGREASED AND REPOSITIONED NR 2 ENG FIRE LOOP. FIRE LOOP FOUND GROUNDED TO FUEL CONTROL, OPS CK GOOD IAW MM 26-11-0. 2 L 7 3 4F A3WE 2002010700061 20020107 00061 WP 2002 1 7 DHL2001801016 1 20011227 A 3260 SWITCH DOUG DC8 DC873F 302199F WP LT MLG FAILED A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 801DH 46033 AFTER T/O RAISING GEAR DOORS NOT LATCHED AND LEFT DOOR UNSAFE REMAINED ON. CYCLED GEAR IAW PROCEDURES, NO CHANGE REMAIN DER OF FLIGHT .65 M/230KIAS IAW PROCEDURE. REMOVED AND REPLACED SWITCH ASSY LEFT MAIN GEAR DOOR, OPS CHECK GOOD IAW MM 52-30-0. 2 L 7 4 4F RT 4A25 2002010700062 20020107 00062 WP 2002 1 7 DHL2001802017 1 20011221 A 2611 SMOKE DETECTOR DOUG DC8 DC873 302199C WP CABIN WILL NOT TEST A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 802DH 46076 NR 11 MAIN DECK SMOKE DETECTOR WILL NOT TEST. RELAMPED SMOKE DETECTOR, TEST OK IAW DC-8 MM 26-16-0. 2 L 7 4 4F RT 4A25 2002010700063 20020107 00063 WP 2002 1 7 DHL2001807029 1 20011220 A 2612 FIRE LOOP DOUG DC8 DC873F 302199F WP NR 4 ENGINE OUT OF POSITION A DHLA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 45990 NR 4 B-LOOP (FIRE WARNING) SHORT CIRCUIT LIGHT ON. REPOSITION B-LOOP NR 4 ENG, OPS CHECKED GOOD PER MM 26-10-0. 2 L 7 4 4F RT 4A25 2002010700064 20020107 00064 WP 2002 1 7 DHL2001807031 1 20011228 A 2611 SMOKE DETECTOR DOUG DC8 DC873F 302199F WP CARGO BAY WILL NOT TEST A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 807DH 45990 NR 4 MAIN CARGO SMOKE DETECTOR WILL NOT TEST. RELAMPED BEACON LAMP, GROUND OPS CHECKED NORMAL IAW MM 26-10-5. 2 L 7 4 4F RT 4A25 2002010700065 20020107 00065 EU 2002 1 7 MAA010798 1 20011221 A 2930 HE832731 SWITCH BAC 146 AVRO146RJ85A 1500097 EU HYDRAULIC SYS DEFECTIVE A MALA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 527XJ E2352 DURING FLIGHT 3550, AT 29,000 FT, CREW RECEIVED A YELLOW HYDRAULIC SYSTEM HIGH TEMPERATURE WARNING. RAN QRH WHICH CALLE D FOR YELLOW SYSTEM SHUTDOWN. HIGH TEMP WARNING EXTINGUISHED WITHIN 2 MINUTES AFTER SYSTEM SHUTDOWN. MAINTENANCE PERFO RMED YELLOW AND GREEN HYD. SYSTEM CHECK OPS CHECK FOR 20 MINUTES. ALL PRESSURED GOOD ON EDP, PTU, AC PUMP. NO HIGH TE MPS WARNINGS. NO LEAKS NOTED FO SYSTEM. REPLACED YELLOW SYSTEM HYD TEMP SWITCH PER AMM 29/33-11-201, P/N HE 83273-1, S /N ON 1368TW, S/N OFF 1304TW. NO LEAKS NOTED. 2 H 7 4 4F RT A49EU 2002010700066 20020107 00066 EU 2002 1 7 MALA010800 1 20011228 A 5210 PIN SAAB SF340 340B 7860101 EU PAX DOOR LACK OF LUBE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 427XJ 340B427 DURING FLIGHT 3327, MAIN DOOR HANDLE LIGHT ILLUMINATED AFTER DEPARTURE, QRH COMPLETED, AND LOWER INDEX WAS NOT ALIGNED. AIR RETURN TO MSP. MAINTENANCE CLEANED AND LUBED LOWER SHOOT PIN. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002010700067 20020107 00067 2002 1 7 MALA010801 4 20011229 A 2216 SERVO BAC 146 AVRO146RJ85A 1500097 EU AUTOPILOT SYS FAULTY A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 514XJ E2330 UPON ROTATION AND CLIMBOUT OF FLIGHT 3640, CREW ALERTED TO A FTC LOOK-UP LIGHT WITH ELEC PITCH TRIM GOING INOP. ALSO NO TED FGC LIGHT. AIR RETURN TO MSP. MAINTENANCE REPLACED THE ELEVATOR TRIM SERVO MOTOR. 2 H 7 4 4F RT A49EU 2002010700069 20020107 00069 EU 2002 1 7 QXEA0102038 1 20011205 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - FORWARD RADIO ALTIMETER ANTENNA MOUNT AREA ON FUSELAGE SKIN IS CORRODED. REPAIRED IAW F-28 SRM 53-01-01. 2 L 7 2 4F RT A20EU 2002010700070 20020107 00070 EU 2002 1 7 QXEA0102039 1 20011205 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - AFT RADIO ALTIMETER ANTENNA MOUNT AREA ON FUSELAGE SKIN CORRODED. REPAIRED IAW F-28 SRM 53-01-01. 2 L 7 2 4F RT A20EU 2002010700071 20020107 00071 EU 2002 1 7 QXEA0102040 1 20011209 A 5532 RIVET FOKKER F28 F28MK4000 4990810 EU VERTICAL STAB LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - VERTICAL STABILIZER LOWER RT SIDE SKIN HAS THREE LOOSE/SMOKING RIVETS. REPAIRED IAW FOKKER SRM 51-30-00. 2 L 7 2 4F RT A20EU 2002010700072 20020107 00072 EU 2002 1 7 QXEA0102041 1 20011209 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - RIGHT INBOARD SEAT TRACK INBOARD FLANGE HAS FRETTING CORROSION THREE INCHES AFT OF FRAME 9805B. REPAIRED IAW FOKK ER SRM 53-01-01, PAGE 5 AND SRM 51-10-4, PAGE 9, PARAGRAPH 1C. 2 L 7 2 4F RT A20EU 2002010700073 20020107 00073 EU 2002 1 7 QXEA0102042 1 20011208 A 5730 ACCESS PANEL FOKKER F28 F28MK4000 4990810 EU RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - RT WING ACCESS PANEL 74C HAS LIGHT FRETTING CORROSION. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4A. 2 L 7 2 4F RT A20EU 2002010700074 20020107 00074 EU 2002 1 7 QXEA0102043 1 20011208 A 5730 ACCESS PANEL FOKKER F28 F28MK4000 4990810 EU RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - RT WING ACCESS PANEL 74E HAS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4A AND SRM 51 -10-4, PAGE 9, PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 2002010700075 20020107 00075 EU 2002 1 7 QXEA0102044 1 20011208 A 5730 ACCESS PANEL FOKKER F28 F28MK4000 4990810 EU RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - RT WING ACCESS PANEL 74B HAS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH A4A. 2 L 7 2 4F RT A20EU 2002010700076 20020107 00076 EU 2002 1 7 QXEA0102045 1 20011208 A 5710 STRUCTURE FOKKER F28 F28MK4000 4990810 EU RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CORROSION INSIDE RT WING FUEL TANK AT STRINGER 2.36. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 2002010700077 20020107 00077 EU 2002 1 7 QXEA0102046 1 20011209 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - LT OUTBOARD SEAT TRACK CHAFED AT STATION 4830. REPAIRED IAW FOKKER MM 53-10-01, PAGE 202, FOKKER SRM 51-10-4, PAG E 9, PARAGRAPH 4C. 2 L 7 2 4F RT A20EU 2002010700078 20020107 00078 EU 2002 1 7 QXEA0102047 1 20011209 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - LT OUTBOARD SEAT TRACK GOUGED AT STATION 5655. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 3, SRM 51-10-4, PAGE 9, PAR AGRAPH 4C. 2 L 7 2 4F RT A20EU 2002010700079 20020107 00079 EU 2002 1 7 QXEA0102048 1 20011209 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - LT OUTBOARD SEAT TRACK CHAFED BETWEEN STATION 6975 AND 7005. REPAIRED IAW FOKKER SRM 51-01-04, SRM 53-01-01. 2 L 7 2 4F RT A20EU 2002010700080 20020107 00080 EU 2002 1 7 QXEA0102049 1 20011209 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - LT OUTBOARD SEAT TRACK CORRODED AT STATION 7835. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4C. 2 L 7 2 4F RT A20EU 2002010700081 20020107 00081 EU 2002 1 7 QXEA0102050 1 20011209 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - LT OUTBOARD SEAT TRACK IS PITTED AT STATION 14323. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4C. 2 L 7 2 4F RT A20EU 2002010700082 20020107 00082 EU 2002 1 7 QXEA0102051 1 20011207 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - RT OUTBOARD SEAT TRACK HAS BEEN BLENDED BETWEEN STATION 4590 AND 4700. BLEND DONE IAW FOKKER SRM 51-10-04, PAGE 9 , PARAGRAPH 4C. 2 L 7 2 4F RT A20EU 2002010700083 20020107 00083 EU 2002 1 7 QXEA0102052 1 20011209 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - RT OUTBOARD SEAT TRACK HAS TWO CORROSION PITS BETWEEN STATION 5065 AND 5085. REPAIRED IAW FOKKER SRM 51-10-04, PA GE 9, PARAGRAPH 4C. 2 L 7 2 4F RT A20EU 2002010700084 20020107 00084 EU 2002 1 7 QXEA0102053 1 20011209 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - RT OUTBOARD SEAT TRACK HAS CORROSION IN GOUGE AT STATION 11954. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5, AND SRM 51-10-04, PAGE 9, PARAGRAPH 4C. 2 L 7 2 4F RT A20EU 2002010700085 20020107 00085 EU 2002 1 7 QXEA0102054 1 20011209 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - RT OUTBOARD SEAT TRACK HAS MINOR GOUGES AT STATION 12415. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5 AND SRM 51-10- 4, PAGE 9, PARAGRAPH 4C. 2 L 7 2 4F RT A20EU 2002010700086 20020107 00086 EU 2002 1 7 QXEA0102055 1 20011208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - RT INBOARD SEAT TRACK HAS MINOR GOUGES AT STATION 12415. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5 AND SRM 51-10-0 4, PAGE 9, PARAGRAPH 4C. 2 L 7 2 4F RT A20EU 2002010700087 20020107 00087 EU 2002 1 7 QXEA0102056 1 20011208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - RT INBOARD SEAT TRACK HAS CORROSION BETWEEN STATION 5260 AND 5735. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARA GRAPH 4C. 2 L 7 2 4F RT A20EU 2002010700088 20020107 00088 EU 2002 1 7 QXEA0102057 1 20011208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - RT INBOARD SEAT TRACK HAS LIGHT CORROSION AT STATION 4880 - 4900. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 2002010700089 20020107 00089 EU 2002 1 7 QXEA0102058 1 20011208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - RT INBOARD SEAT TRACK CORRODED AT STATION 4950 - 4975. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 2002010700090 20020107 00090 EU 2002 1 7 QXEA0102059 1 20011208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - RT INBOARD SEAT TRACK CORRODED AT STATION 4845 - 4865. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 2002010700091 20020107 00091 EU 2002 1 7 QXEA0102060 1 20011208 A 5320 STRUCTURE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CORROSION ON LT FORWARD OVERWING EXIT APERTURE UNDER TEFLON SEAT. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002010700092 20020107 00092 EU 2002 1 7 QXEA0102061 1 20011209 A 5310 WINDOW POST FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - LT NR 2 WINDOW POST HAS SEVERAL GOUGES AND SCRATCHES ON BOTTOM INSIDE SURFACE. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5, PARAGRAPH 3E (1) AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 2002010700093 20020107 00093 EU 2002 1 7 QXEA0102062 1 20011208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CORROSION ON SEAT RAIL UPPER SURFACE, BL600 RT FROM FRAME 4610 TO 4850. REPAIRED IAW FOKKER SRM 53-01-01 AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 2002010700094 20020107 00094 EU 2002 1 7 QXEA0102063 1 20011209 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CORROSION AROUND CAMLOCK FASTENER HOLE ON SEAT RAIL AT BL600 LT, AT MAIN CABIN DOOR ENTRY WAY, BETWEEN FRAMES 4175 AND 4610. REPAIRED IAW FOKKER SRM 53-01-01, PARAGRAPH 4 AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 2002010700095 20020107 00095 EU 2002 1 7 QXEA0102064 1 20011206 A 5320 BEAM FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CORROSION ON NR 1 GALLEY BEAM AROUND NUT PLATE HOLE, BL600 RT, 6 INCHES FORWARD OF AFT END OF SUPPORT BEAM. REPAI RED IAW FOKKER SRM 53-01-01, PARAGRAPH 4, AND SRM 51-30-00. 2 L 7 2 4F RT A20EU 2002010700096 20020107 00096 EU 2002 1 7 QXEA0102065 1 20011206 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CORROSION ON NR 1 GALLEY SUPPORT AT RIGHT HAND SIDE OF BL1127. REPAIRED IAW FOKKER SRM 53-07-01, 51-10-04 AND SRM 51-30-00. 2 L 7 2 4F RT A20EU 2002010700097 20020107 00097 EU 2002 1 7 QXEA0102066 1 20011206 A 5320 BEAM FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CORROSION ON NR 1 GALLEY SUPPORT BEAM AROUND NUT PLATE HOLE. REPAIRED IAW FOKKER SRM 53-01-00, PARAGRAPH 5 AND SR M 51-10-04. 2 L 7 2 4F RT A20EU 2002010700098 20020107 00098 EU 2002 1 7 QXEA0102067 1 20011209 A 5310 WINDOW POST FOKKER F28 F28MK4000 4990810 EU FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - LT NR 2 WINDOW POST HAS SCRATCH ON INSIDE SURFACE, 2.3 INCHES FROM BOTTOM OF AFT EDGE. REPAIRED IAW FOKKER SRM 53 -01-01, PAGE 5, PARAGRAPH 3E (1) AND SRM 51-10-04. 2 L 7 2 4F RT A20EU 2002010700099 20020107 00099 EU 2002 1 7 QXEA0102068 1 20011208 A 5730 ACCESS PANEL FOKKER F28 F28MK4000 4990810 EU RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - RT WING ACCESS PANEL 74G HAS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 2002010700100 20020107 00100 EU 2002 1 7 QXEA0102069 1 20011209 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - RT OUTBOARD SEAT TRACK HAS LIGHT CORROSION BETWEEN STATION 12923 AND 12943. REPAIRED IAW FOKKER SRM 51-10-04 AND MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 2002010700101 20020107 00101 EU 2002 1 7 QXEA0102070 1 20011209 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - RT INBOARD SEAT TRACK HAS CORROSION BETWEEN STATION 6975 AND 7030. REPAIRED IAW FOKKER SRM 51-10-01, 51-10-04 PAG E 9, PARAGRAPH 4 AND MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 2002010700102 20020107 00102 EU 2002 1 7 QXEA0102071 1 20011210 A 5210 RIVET FOKKER F28 F28MK4000 4990810 EU PAX DOOR OUT OF POSITION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - RIVET IS PULLED AWAY FROM STRUCTURE ON THE MAIN CABIN DOOR INNER SKIN, ADJACENT TO CHANNEL AND DIAPHRAGM. REPAIRE D IAW SRM 52-10-00 AND SRM 51-31-05. 2 L 7 2 4F RT A20EU 2002010700103 20020107 00103 EU 2002 1 7 QXEA0102072 1 20011210 A 5210 RIVET FOKKER F28 F28MK4000 4990810 EU PAX DOOR IMPROPER A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - RIVETS ARE TOO SHORT ON MAIN CABIN DOOR INNER SKIN, AFT/UPPER AREA ADJACENT TO FRAME PLATE. REPAIRED IAW FOKKER S RM 52-10-00 AND SRM 51-31-05. 2 L 7 2 4F RT A20EU 2002011000033 20020110 00033 EU 2002 1 10 QXEA0102073 1 20011210 A 5210 FASTENER FOKKER F28 F28MK4000 4990810 EU PAX DOOR IMPROPER A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - MAIN CABIN DOOR FASTENER IS TOO SHORT, INSIDE SKIN, FORWARD SIDE, 19INCHES UP FROM HINGE END THROUGH CHANNEL UNDER HAND RAIL SUPPORT TOWER. REPAIRED IAW FOKKER SRM 51-31-05. 2 L 7 2 4F RT A20EU 2002010700104 20020107 00104 EU 2002 1 7 QXEA0102074 1 20011210 A 5210 RIVET FOKKER F28 F28MK4000 4990810 EU PAX DOOR PULLED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - MAIN CABIN DOOR RIVETS ARE PULLED THROUGH INNER DOOR STRUCTURE, AFT END, UNDER HAND RAIL SUPPORT. REPAIRED IAW FO KKER SRM 51-31-05. 2 L 7 2 4F RT A20EU 2002010700105 20020107 00105 EU 2002 1 7 QXEA0102075 1 20011212 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - FRAME TO SKIN CONNECTION ANGLE BRACKET CRACKED AT FRAME 17565 AND STRINGER 15. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5 AND SRM 51-31-01, PAGE 13. 2 L 7 2 4F RT A20EU 2002010700106 20020107 00106 EU 2002 1 7 QXEA0102076 1 20011209 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - UPPER ATC ANTENNA MOUNT AREA ON FUSELAGE SKIN CORRODED. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4-B. 2 L 7 2 4F RT A20EU 2002010700107 20020107 00107 EU 2002 1 7 QXEA0102077 1 20011210 A 5210 ANGLE FOKKER F28 F28MK4000 4990810 EU PAX DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - MAIN CABIN DOOR HAS FRETTING CORROSION ON REINFORCEMENT ANGLE. REPAIRED IAW FOKKER SRM 52-01-01, PAGE 7, PARAGRAP H A 4C. 2 L 7 2 4F RT A20EU 2002010700121 20020107 00121 EU 2002 1 7 QXEA0102079 1 20011207 A 2710 PULLEY BRACKET FOKKER F28 F28MK4000 4990810 EU AILERON CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - AILERON CABLE PULLEY BRACKET IS CORRODED AROUND LOWER BOLT HOLE IN LEFT HAND WHEEL WELL. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 8, PARAGRAPH 3C4. 2 L 7 2 4F RT A20EU 2002010700122 20020107 00122 NM 2002 1 7 QXEA0102136 1 20011227 A 3260 PROXIMITY SWITCH DHAV DHC8 DHC8* NM LANDING GEAR OUT OF ADJ A QXEA K NONE O OTHER CR CRUISE 1 NM 09 407QX 4049 GTF - MAIN GEAR DOORS CYCLED IN FLIGHT. ADJUSTED PROX SWITCH. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RE TURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002010700123 20020107 00123 NM 2002 1 7 QXEA0102137 1 20011229 A 3234 CONTROL HANDLE DHAV DHC8 DHC8201 2809001 NM COCKPIT MALFUNCTIONED A QXEA K NONE J WARNING INDICATION DE DESCENT 1 NM 09 363PH 520 SEA - RIGHT MAIN LANDING GEAR DID NOT SHOW DOWN AND LOCKED INDICATION ON GEAR EXTENSION. REPLACED GEAR HANDLE ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002010700124 20020107 00124 NM 2002 1 7 QXEA0102138 1 20011228 A 3150 WARNING SYSTEM DHAV DHC8 DHC8* NM COCKPIT MALFUNCTIONED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 405QX 4047 PIH - TAKEOFF WARNING HORN SOUNDED DURING TAKEOFF AND TAKEOFF WAS ABORTED. MAINTENANCE CYCLED ELEVATOR TRIM THE FULL RA NGE OF MOTION, SET TRIM IN TAKEOFF RANGE, AND IT TESTED WITH NO DEFECTS NOTED. TESTED WITH TRIM OUT OF RANGE AND TAKEOF F WARNING CHECKED NORMAL. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002010700125 20020107 00125 EU 2002 1 7 QXEA0102139 1 20011228 A 3397 CONNECTOR FOKKER F28 F28MK4000 4990810 EU COCKPIT OUT OF POSITION A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 480AU 11229 BOI- FORWARD EMERGENCY LIGHT ABOVE COCKPIT DOOR INOPERATIVE. REPOSITIONED CONNECTION. OPERATIONAL CHECKS GOOD. AIRCRA FT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A20EU 2002010700126 20020107 00126 EU 2002 1 7 QXEA0102140 1 20011228 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INTERMITTENT A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 480AU 11229 PDX- EMERGENCY EXIT SIGN IN GALLEY AREA HAS FAULTY LIGHT, IT INTERMITTENTLY GOES DARK. REMOVED AND REPLACED EMERGENCY E XIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002010700127 20020107 00127 EU 2002 1 7 QXEA0102141 1 20011231 A 3350 6008905 BATTERY FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 8466 2902 11228 PDX - EVACUATION LIGHTS ON EXIT SIGN IN PASSENGER COMPARTMENT COME ON DIM AND THEN GO OFF AFTER ONE TO TWO MINUTES. REP LACED BATTERY POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002010700128 20020107 00128 EA 2002 1 7 QXEA0102142 1 20011227 A 3222 521153 TORQUE LINK CNDAIR CL600 CL6002C10 1390015 EA NLG DISCONNECTED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 609QX 137 137 10031 GEG - AIRCRAFT RETURNED TO FIELD WHEN AFTER DEPARTURE, LANDING GEAR WOULD NOT RETRACT AND WOW INPUT CAUTION MESSAGE APPE ARED. AFTER TOUCHDOWN, NOSE GEAR HAD A SEVERE SHIMMY. MAINTENANCE FOUND NOSE GEAR TORQUE LINKS DISCONNECTED AND NOSE T IRES GALLED AND SCUFFED. REPLACED TIRES AND CLEANED, LUBED AND CONNECTED TORQUE LINKS, CONNECTOR JOINTS AND PULL PIN EX TRACT HANDLES. NO FURTHER DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002010700129 20020107 00129 NM 2002 1 7 QXEA0102143 1 20011231 A 5230 HANDLE DHAV DHC8 DHC8* NM CARGO DOOR OUT OF POSITION A QXEA I A CABIN DEPRESSURIZATION UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 408QX 4050 GEG - FUSELAGE DOORS WARNING LIGHT ILLUMINATED IN FLIGHT. EVENT OCCURRED AFTER 30 MINUTES AT 24,000 FEET. AIRCRAFT WAS DEPRESSURIZED AND DIVERTED TO GEG. MAINTENANCE INSPECTED AND FOUND FORWARD BAGGAGE DOOR HANDLE NOT IN STOWED POSITION. OPERATED DOOR LATCH SEVERAL TIMES. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002010700130 20020107 00130 EA 2002 1 7 QXEA0200001 1 20011227 A 5270 STRIKER CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 606QX 10023 PDX - MAIN CABIN DOOR SEAL STRIKER IS DAMAGED ALONG THE AFT EDGE OF OPENING. REPAIRED MAIN CABIN DOOR APERTURE SEAL STR IKER IAW EA R-53-11. 2 L 7 2 4F RT A21EA 2002010700131 20020107 00131 NM 2002 1 7 SWAA013432 1 20011231 A 3350 900835A BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED A2 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT MID CABIN. REMOVED AND REPLACED EXIT LIGHT BATTE RY PER MM. 2 L 7 2 4F A16WE 2002010700132 20020107 00132 NM 2002 1 7 SWAA013434 1 20011230 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 391SW 27378 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS LIGHT INOP AT EMERGENCY EXIT ROW. REMOVED AND REPLACED EEPLS LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002010700133 20020107 00133 NM 2002 1 7 SWAA013438 1 20011229 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 374SW 26582 EEPLS LOOSE AT ROWS NR 8 AND NR 9. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002010700147 20020107 00147 NM 2002 1 7 SWAA013444 1 20011230 A 3350 2350040 BATTERY BOEING 737 7372H4 138448C NM CARGO BAY DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2002010700148 20020107 00148 NM 2002 1 7 SWAA013445 1 20011230 A 3350 90083 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT AFT CABIN CEILING. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2002010700149 20020107 00149 NM 2002 1 7 SWAA013447 1 20011230 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 357SW 26594 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002010700150 20020107 00150 NM 2002 1 7 SWAA013450 1 20011229 A 5315 6546804 FLOORBEAM BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 294, WL 208 AND LBL 47. REPAIRED FLOORBEAM PER BFG ER. 2 L 7 2 4F RT A16WE 2002010700151 20020107 00151 NM 2002 1 7 SWAA013451 1 20011230 A 5511 183A4000 SPAR BOEING 737 7373T5 1384608 NM HORIZ STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED D-CHECK, FOUND LT STAB UPPER REAR SPAR CHORD CORRODED 37 INCHES FROM OUTBOARD END. REPAIRED SPAR CHORD PER SRM. 2 L 7 2 4F RT A16WE 2002010700153 20020107 00153 2002 1 7 SWIA200110477 4 20011226 A 2210 6229968001 DAMPER CNDAIR CL600 CL6002B19 1900309 EA AUTOPILOT SYS FAILED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 440SW 7589 YAW DAMPER 2 INOP. REMOVE AND REPLACE YAW DAMPER NR 2. OPS CHECK GOOD AT THIS TIME IAW 22-22-01. 2 L 7 2 4F RT A21EA 2002010700155 20020107 00155 SO 2002 1 7 SWIA200110478 1 20011226 A 5270 SWITCH EMB 120 EMB120ER 3260203 SO DOOR OUT OF ADJ A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 561SW 120335 FORWARD DOOR LIGHT CAME ON DURING TAKEOFF ROLL. ABORTED TAKEOFF. ADJUSTED FORWARD DOOR MICROSWITCH. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002010700157 20020107 00157 EA 2002 1 7 SWIA200110479 1 20011226 A 2760 4916405 ECU CNDAIR CL600 CL6002B19 1900309 EA E/E BAY MALFUNCTIONED A SWIA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 426SW 2039 2039 7468 ON TAXI OUT, RECEIVED SPOILERON FAULT MESSAGE. REMOVED AND REPLACED SECU NR 1 DUE TO FAILURE IN SECU NR 1 MODULE-A. OP S CHECK GOOD IAW MM 27-61-00 AND 27-61-05. 2 L 7 2 4F RT A21EA 2002010700158 20020107 00158 SO 2002 1 7 SWIA200110480 1 20011226 A 2120 SMOKE EMB 120 EMB120ER 3260203 SO CABIN DETECTED A SWIA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 NM 07 236SW 120312 DUE TO REPORT OF SMOKE IN THE LAV AREA AND SMOKE DETECTOR GOING OFF CONTINUOUSLY FOR THREE MINUTES INFLIGHT, INSPECT CAB IN FOR SOURCE OF SMOKE AND CORRECT ANY DISCREPANCIES. LAV SMOKE DETECTOR ALARM SOUNDED DURING CRUISE. F/A AND PAX SME LLED SMOKE. ALARM SOUNDED AROUND 3 MINUTES. SMOKE SMELL WENT AWAY DURING DESCENT. INSPECTED AIRCRAFT FOR ELECTRICAL A ND HEAT DAMAGE OR SIGNS OF MALFUNCTION THAT WOULD CAUSE SMOKE OR SMELL OF SMOKE IN CABIN, NONE FOUND. OPERATIONAL CHECK OF ALL LOCAL SYSTEMS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002010700159 20020107 00159 SO 2002 1 7 SWIA200110481 1 20011226 A 2752 PIN EMB 120 EMB120ER 3260203 SO FLAP ACTUATOR DEFECTIVE A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 188SW 120039 AFTER TAKEOFF FLAPS WOULD NOT COMPLETELY RETRACT. A FLAP DISAGREEMENT RESULTED. DID QRH PROCEDURE, IT DID NOT CLEAR. RETURNED TO LAND. AFTER LANDING FLAPS RETURNED OK. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR CONNECTOR PIN. CYC LED FLAPS NUMEROUS TIMES. OPS CHECK GOOD. P/N: MS3476L12-10S. 2 L 7 2 4T RT A31SO 2002010700160 20020107 00160 2002 1 7 SWIA200110482 4 20011225 A 3414 320AS1 INDICATOR EMB 120 EMB120ER 3260203 SO COCKPIT FAULTY A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 188SW 120039 HIGH SPEED AURAL WARNING ON TAKEOFF. ABORTED TAKEOFF. REMOVED AND REPLACED NR 1 AIRSPEED INDICATOR. OPS CHECK GOOD IA W 34-12-01. 2 L 7 2 4T RT A31SO 2002010700161 20020107 00161 WP 2002 1 7 2002F00000 1 20011212 A 3350 9721055 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 817US 48097 IND - THE MAIN ENTRY EMERGENCY LIGHT AND THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPL ACED THE MAIN ENTRY EMERGENCY LIGHT ASSEMBLY AND THE LOW LEVEL EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2002010700162 20020107 00162 WP 2002 1 7 2002F00001 1 20011211 A 3350 873100191 RECEIVER DOUG DC9 DC982 3022082 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 822US 49139 IND - THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS WERE DIM AND THE TAILCONE REMOTE RECEIVER WAS INOPERATIVE. MAINTENANC E REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES AND THE TAIL CONE REMOTE RECEIVER. (M) 2 L 7 2 4F A6WE 2002010700163 20020107 00163 NM 2002 1 7 AALA20012060 1 20011124 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 399AN 29606 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 19B, 20B, AND 22B INOPERATIVE. REPAIRED EMERGENCY EXIT LIGH T WIRE AT 19B, 20B, AND 22B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002010700164 20020107 00164 NM 2002 1 7 AALA20012062 1 20011122 A 3350 LIGHT BOEING 767 767223 1385123 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 339AA 22336 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 32B INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT AT S EAT 32B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002010800001 20020108 00001 NE 2002 1 8 AUS20010946 2 20010829 A 8500 ENGINE DOUG DC3 DC3CS1C3G 3021458 WP PWA R1830 R183092 52020 NE HAMSTD 23E 23E50 NE RIGHT MAKING METAL W O OTHER E F VIBRATION/BUFFET FLT CONT AFFECTED CR CRUISE 1 AU S (AUS) RT ENGINE OIL PRESSURE DECREASED AND TEMPERATURE INCREASED. INVESTIGATION FOUND EXTENSIVE METAL CONTAMINATION. ENG INE WAS ON A TEST FLIGHT FOR RT ENGINE INSTALLATION. THE ENGINE HAD JUST BEEN REPAIRED WITH SUPERCHARGER BEARINGS AND SO ME CYLINDER BAFFLES REPLACED. 2 L 7 2 4R 4 R A669 5E4 6 C P603 2002010800003 20020108 00003 NM 2002 1 8 AUS20010949 1 20010901 A 2520 CONNECTOR BOEING 747 747238B 1384828 NM RROYCE RB211 RB211524D419 54555 NE CABIN BURNED W O OTHER O OTHER CR CRUISE 1 AU S (AUS) SEAT 43AB VIDEO CONNECTOR PINS BURNT AND WIRING CHAFED. 2 L 7 4 4F 4 F A20WE E12EU 2002010800004 20020108 00004 NE 2002 1 8 AUS20010950 2 20010830 A 7532 2161182 BLEED BAND BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE COMPRESSOR BROKEN W O OTHER E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS TO TAKEOFF 1 AU S (AUS) NO3 ENGINE BLEED BAND BROKEN IN AREA UNDER ACTUATOR BODY. 2 H 7 4 4F 4 F A49EU E6NE 2002010800005 20020108 00005 2002 1 8 AUS20010954 4 20010831 A 3442 6225132101 TRANSCEIVER BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL WX RADAR SYS FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 AU S 7999 (AUS) WEATHER RADAR TRANSCEIVER FAILED. CIRCUIT BREAKER TRIPPED. 2 L 7 2 4F 4 F RT A1NM E23EA 2002010800007 20020108 00007 NM 2002 1 8 AUS20010957 1 20010902 A 2910 AS11506K0280 HOSE BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL HYDRAULIC SYSTEM LEAKING W O OTHER K FLUID LOSS LD LANDING 1 AU S (AUS) FLEXIBLE BRAKE HOSE LEAKING. LOSS OF HYDRAULIC FLUID. 2 L 7 2 4F 4 F RT A1NM E23EA 2002010800008 20020108 00008 NE 2002 1 8 AUS20010961 2 20010905 A 7230 MS9390290 PIN BAC 146 146100A 1500260 EU LYC ALF502 ALF502R3A 41580 NE ENGINE MISINSTALLED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) ENGINE FAN DISC RETAINING NUT LOCK CUP WASHER LOCKING PINS FLUSH WITH SHAFT MAKING LOCKING MECHANISM NON FUNCTIONA L. 2 H 7 4 4F 4 F RT A49EU E6NE 2002010800011 20020108 00011 NM 2002 1 8 AUS20010966 1 20010901 A 5240 CABLE BOEING 737 737377 NM SERVICE DOOR FRAYED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) FORWARD SERVICE DOOR RELEASE CABLES FRAYED. FOUND DURINGINSPECTION IAW AD/B737/042. 2 L 7 2 4F RT A16WE 2002010800012 20020108 00012 NM 2002 1 8 AUS20010967 1 20010901 A 5240 CABLE BOEING 737 737377 NM SERVICE DOOR FRAYED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) AFT SERVICE DOOR RELEASE CABLES FRAYED. FOUND DURING INSPECTION IAW AD/B737/042. 2 L 7 2 4F RT A16WE 2002010800013 20020108 00013 NE 2002 1 8 AUS20010968 2 20010905 A 7270 P716915 ACOUSTIC PANEL BOEING 767 767238 1385114 NM PWA JT9 JT9D7R4E 52054 NE RT ENGINE MISSING W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT ENGINE COLD STREAM DUCT ACOUSTIC PANELS MISSING. 2 L 7 2 4F 4 F RT A1NM E3NE 2002010800014 20020108 00014 EU 2002 1 8 AUS20010969 1 20010903 A 2750 676801007 COMPUTER BAC 146 146100A 1500260 EU LYC ALF502 ALF502R5 41580 NE TE FLAP SYSTEM FAULTY W O OTHER F FLT CONT AFFECTED CR CRUISE 1 AU S (AUS) FLAP COMPUTER FAULTY. 2 H 7 4 4F 4 F RT A49EU E6NE 2002010800017 20020108 00017 EU 2002 1 8 AUS20010975 1 20010905 A 2750 JACKSCREW BAC 146 146100A 1500260 EU LYC ALF502 ALF502R5 41580 NE TE FLAPS CONTAMINATED W O OTHER F FLT CONT AFFECTED CR CRUISE 1 AU S (AUS) FLAP SCREWJACK BALLNUTS WATER CONTAMINATION. NR 2 LT, NR 2 RT AND NR 3 RT SCREWJACKS AFFECTED. 2 H 7 4 4F 4 F RT A49EU E6NE 2002010800019 20020108 00019 WP 2002 1 8 AUS20010978 2 20010830 A 7261 31036471 PIPE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP ROTOL R321 R321482F8 GL RT ENGINE CRACKED W O OTHER E K J VIBRATION/BUFFET FLUID LOSS WARNING INDICATION CL CLIMB 1 AU S (AUS) RT ENGINE OIL PIPE FROM PROPELLER PITCH CONTROL TO PROPELLER GOVERNOR CRACKED. LOSS OF ENGINE OIL. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P61GL 2002010800020 20020108 00020 NE 2002 1 8 AUS20010980 2 20010908 A 7200 12684 ENGINE BOEING 747 747238B 1384828 NM RROYCE RB211 RB211524D419 54555 NE NR 1 VIBRATES W O OTHER E F VIBRATION/BUFFET FLT CONT AFFECTED CL CLIMB 1 AU S (AUS) NR 1 ENGINE VIBRATION. OIL QUANTITY SLOWLY DROPPED. METAL CONTAMINATION OF ENGINE OIL SYSTEM. 2 L 7 4 4F 4 F A20WE E12EU 2002010800022 20020108 00022 NM 2002 1 8 AUS20010984 1 20010909 A 5270 656730416 SENSOR BOEING 737 73746B NM CFMINT CFM56 CFM563C 13802 EU DOOR WARNING SYS OUT OF ADJUST W O OTHER N FALSE WARNING TO TAKEOFF 1 AU S (AUS) AFT CARGO DOOR SENSOR OUT OF ADJUSTMENT. 2 L 7 2 4F 4 F RT A16WE E21EU 2002010800024 20020108 00024 NM 2002 1 8 AUS20010988 1 20010823 A 3230 CABLE BOEING 737 737377 NM LANDING GEAR RET STIFF W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NOSE LANDING GEAR EXTENSION SYSTEM CABLE STIFF TO OPERATE. AFORCE IN EXCESS OF 50 POUNDS WAS NEEDED TO OPERATE TH E CABLE. THE MAXIMUM LIMIT IS 28 POUNDS. 2 L 7 2 4F RT A16WE 2002010800026 20020108 00026 2002 1 8 AUS20010995 4 20010912 A 2330 RDAV705705 VIDEO DISPLAY BOEING 747 747338 NM CABIN FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AU S (AUS) VIDEO SCREEN LOCATED AT SEAT 2A SMOKING. MONITOR AT SEAT 17B HAD BURNING SMELL. 2 L 7 2 4F RT A20WE 2002010800027 20020108 00027 NM 2002 1 8 AUS20010996 1 20010910 A 3230 162T30072 SPRING BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL NLG DOWNLOCK MISSING W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NOSE LANDING GEAR DOWNLOCK ASSIST SPRING MISSING. 2 L 7 2 4F 4 F RT A1NM E23EA 2002010800029 20020108 00029 EU 2002 1 8 AUS20011001 2 20010907 A 7200 2500 ENGINE SNIAS AS332 AS332L 8680809 EU TMECA MAKILA MAKILA1A 60040 EU NR 1 MALFUNCTIONED W O OTHER E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS DE DESCENT 1 AU S (AUS) NR 1 ENGINE AUTOMATICALLY REDUCED POWER TO IDLE. INVESTIGATION COULD FIND NO FAULTS. ENGINE WAS GROUND RUN AND TE ST FLOWN WITH ALL SYSTEMS OPERATING CORRECTLY. AIRCRAFT RETURNED TO SERVICE. 2 G 7 2 4U 4 U H4EU E12NE 2002010800030 20020108 00030 NM 2002 1 8 AUS20011002 1 20010914 A 2197 WIRE BOEING 737 737400 138449A NM CFMINT CFM56 CFM563C 13802 EU CONTROLLER CHAFED W O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DE DESCENT 1 AU S (AUS) PRESSURISATION CONTROLLER BURNED DUE TO CHAFED WIRE BEHIND RACK IN EQUIPMENT BAY. 2 L 7 2 4F 4 F RT A16WE E21EU 2002010800031 20020108 00031 NM 2002 1 8 AUS20011003 1 20010916 A 4940 391000102 STARTER BOEING 747 747438 NM APU DISCONNECTED W O OTHER E A VIBRATION/BUFFET FLAME/FIRE NR NOT REPORTED 1 AU S PCE900049 (AUS) APU FIRE. FIRE BOTTLE DISCHARGED. INVESTIGATION FOUND THAT THE STARTER HAD DISCONNECTED FROM THE GEARBOX AND THE SPRAG CLUTCH WAS LYING IN THE COWLS. 2 L 7 4 4F RT A20WE 2002010800032 20020108 00032 SW 2002 1 8 AUS20011005 1 20010918 A 2910 2781032081 PIPE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP ROTOL R321 R321482F8 GL NLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NOSE LANDING GEAR RETRACTION SYSTEM HYDRAULIC PIPE CRACKED IN TWO PLACES IN PIPE BENDS. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P61GL 2002010800036 20020108 00036 NM 2002 1 8 AUS20011013 1 20010914 A 5314 KEELBEAM BOEING 737 737376 NM CFMINT CFM56 CFM563C 13802 EU FUSELAGE CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) KEEL BEAM LOWER CHORD CONTAINED CORROSION AND CRACKING IN AREABETWEEN BS530 AND BS540. FOUND DURING EDDY CURRENT A ND ULTRASONIC INSPECTION. 2 L 7 2 4F 4 F RT A16WE E21EU 2002010800037 20020108 00037 EU 2002 1 8 AUS20011014 1 20010922 A 3230 200877943 HOSE BAC 146 146100A 1500260 EU LYC ALF502 ALF502R5 41580 NE LT MLG LEAKING W O OTHER O OTHER TO TAKEOFF 1 AU S (AUS) LT MAIN LANDING GEAR HYDRAULIC HOSE TO WHEEL AUTO BRAKE FAILED. 2 H 7 4 4F 4 F RT A49EU E6NE 2002010800038 20020108 00038 NM 2002 1 8 AUS20011016 1 20010923 A 7603 CABLE RROYCE RB211524D4 BOEING 747 747338 NM POWER LEVER DISTORTED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NR 3 ENGINE THRUST CABLE KINKED IN THE AREA OF THE STRUT TO WING INTERFACE. 2 L 7 2 4F RT A20WE 2002010800041 20020108 00041 NM 2002 1 8 AWXA200100668 1 20011225 A 3230 664700500A4D CONTROL UNIT AIRBUS A319 A319132 3930340 NM E/E BAY MALFUNCTIONED A AWXA O OTHER J WARNING INDICATION DE DESCENT 1 WP 28 831AW 806 1223 PHX - EMERGENCY LANDING - C - DURING DESCENT INTO PHX FROM SEA FLIGHT CREW RECEIVED ECAM MESSAGES FOR 3 CLASS 1 FAULTS ( 1) NR 2 LANDING GEAR CONTROL INTERFACE UNIT (LGCIU) (2) NR 2 BRAKE ANTISKID AND NOSE WHEEL STEERING, (3) LAVATORY/CARGO SMOKE DETECTION. MAINTENANCE CONTROL ADVISED FLIGHT CREW TO RESET CIRCUIT BREAKER WHICH HAD NO EFFECT. EMERGENCY LANDI NG WAS DECLARED AND AIRCRAFT MADE AN UNEVENTFUL LANDING. MAINTENANCE TROUBLESHOT AND REPLACED THE NR 2 LGCIU IAW AMM 32 -31-71-000-001, AND OPERATIONAL CHECKED GOOD IAW 32-69-00-740-001. THE 3-POLE CONTACTOR WAS ALSO REPLACED IAW AMM 24-51 -55-000-001. 2 L 7 2 4F RT A28NM 2002010800042 20020108 00042 NM 2002 1 8 AUS20011021 1 20010919 A 4920 380029816 APU BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL AFT SHUTDOWN W E O ENGINE SHUTDOWN OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 AU S 1293 (AUS) APU AUTO SHUTDOWN. LIMITED INFORMATION PROVIDED. 2 L 7 2 4F 4 F RT A1NM E23EA 2002010800043 20020108 00043 NM 2002 1 8 DHL2001746004 1 20011227 A 2612 FIRE WARNING BOEING 727 727224 1384076 NM APU INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 746DH 22252 APU FIRE TEST INOP. REMOVED AND REPLACED APU TEST SWITCH S451, NO HELP. RAN WIRES AND FOUND B1 ON S455 GOING TO PIN 1 ON R197, SHOULD BE GOING TO PIN 5. FOUND B2 ON S455 GOING TO PIN 5, SHOULD BE GOING TO PIN 1 SUSPECT BAD RELAY R197 OR ASSY PN. REMOVED AND REPLACED APU POWER UNIT AND FIRE TEST RELAY IAW B727 WDM 49-41-01. OPERATIONAL TEST SERVICEABLE. APU FIRE TEST INOP, SWAPPED APU CONTROL PANEL IAW BMM REF 49-00, NO HELP. SWAPPED APU FIRE TEST BOX IAW BMM REF 49-00 , NO HELP. DMI 8108 REMAINS OPEN. 2 L 7 3 4F A3WE 2002010800046 20020108 00046 NM 2002 1 8 AUS20011025 1 20010921 A 5753 KRP127107VT BEARING BOEING 747 747238B 1384828 NM TE FLAPS COLLAPSED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT OUTBOARD TRAILING EDGE FLAP NR 7 FLAP TRACK CARRIAGE SIDELOAD BEARING COLLAPSED. INTERFERENCE BETWEEN THE OUTBO ARD FLAP AND WING STRUCTURE DAMAGED THE FLAP AND ADJACENT FAIRING. 2 L 7 4 4F A20WE 2002010800047 20020108 00047 WP 2002 1 8 MWEA011474 1 20011204 A 5753 593590622 ATTACH ANGLE DOUG DC9 DC981 3022081 WP T/E FLAP CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 RIGHT HAND WING FLAP NR 8 RIB (COUNTING FROM INBOARD) FORWARD RIB ATTACH ANGLE IS EXFOLIATED. REMOVED, FABRICATED AND I NSTALLED NEW ANGLE. 2 L 7 2 4F A6WE 2002010800049 20020108 00049 WP 2002 1 8 MWEA011488 1 20011217 A 5244 FASTENER DOUG DC9 DC981 3022081 WP ACCESSORY DOOR FAILED A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 812ME 48006 FORWARD ACCESSORY COMPARTMENT DOOR INDICATOR LIGHT CAME ON. REPLACED TWO CAMLOCKS ON FORWARD ACCESSORY DOOR. 2 L 7 2 4F A6WE 2002010800050 20020108 00050 WP 2002 1 8 MWEA011489 1 20011206 A 5313 27779223 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 CABIN LONGERON 4 LEFT IS CRACKED AT FRAME STATION 160. REMOVED, LOCATED, DRILLED AND INSTALLED NEW SECTION OF LONGERON. 2 L 7 2 4F A6WE 2002010800051 20020108 00051 WP 2002 1 8 MWEA011490 1 20011206 A 5313 27779223 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 CABIN LONGERON 4 LEFT IS CRACKED AT FRAME STATION 200. REMOVED, LOCATED, DRILLED AND INSTALLED NEW SECTION OF LONGERON. 2 L 7 2 4F A6WE 2002010800052 20020108 00052 WP 2002 1 8 MWEA011491 1 20011222 A 2130 45D16 SWITCH DOUG DC9 DC914 3022034 WP COCKPIT FAULTY A MWEA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 800ME 45842 AIRCRAFT DEPRESSURIZED DURING CLIMB. REPLACED RIGHT HAND SECOND SEGMENT CLIMB SWITCH. 2 L 7 2 4F A6WE 2002010800056 20020108 00056 EU 2002 1 8 QXEA0102078 1 20011210 A 5210 SKIN FOKKER F28 F28MK4000 4990810 EU PAX DOOR DEFORMED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - DEFORMATION TO EDGE OF LIGHTING HOLE ON MAIN CABIN DOOR INNER SKIN LOWER AFT CORNER. REPAIRED IAW FOKKER SRM 51-1 1-4, PAGE 2. 2 L 7 2 4F RT A20EU 2002010800062 20020108 00062 SO 2002 1 8 SWIA200110484 1 20011224 A 2810 FASTENER EMB 120 EMB120ER 3260203 SO FUEL PANEL LOOSE A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 583SW 120351 ABORTED 2 TAKEOFFS FOR FLICKERING DOOR LIGHT, NO CHIME. TAXIED BACK. ONE FASTENER ON FUEL DOOR WAS LOOSE. RESECURED F UEL PANEL DOORS AS NEEDED. 2 L 7 2 4T RT A31SO 2002010800063 20020108 00063 SO 2002 1 8 SWIA200110485 1 20011225 A 5610 WINDOW EMB 120 EMB120ER 3260203 SO COCKPIT LACK OF LUBE A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 578SW 120346 DIRECT VISION WINDOW ON LEFT PILOT SIDE DOES NOT LOCK PROPERLY. LUBED LOCK ASSEMBLY ON DV WINDOW. LOCKED DV WINDOW SYS TEM. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002010800064 20020108 00064 WP 2002 1 8 ABXA010661 1 20011214 A 5200 3914025501 FITTING DOUG DC9 DC932 3022066 WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 AFT LOWER CARGO DOOR #2 BEAM, AFT END FITTING WAS CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-2, 51-30-1, 51-20-0. 2 L 7 2 4F A6WE 2002010800065 20020108 00065 EA 2002 1 8 SWIA200110487 1 20011230 A 2613 WIRE CNDAIR CL600 CL6002B19 1900309 EA LT WING GROUNDED A SWIA O OTHER N FALSE WARNING CR CRUISE 1 NM 07 426SW 7468 AFTER TAKEOFF OUT OF SLC, RECEIVED WING OVERHEAT MESSAGE. DID QRH PROCEDURE, MESSAGE WENT OUT. THEN A FEW MINUTES LATE R RECEIVED ANTI-ICE DUCT MESSAGE. DID QRH PROCEDURE. ANTI-ICE DUCT MESSAGE CONTINUED THEN WENT OUT AFTER SEVERAL MINUT ES. FOUND A GROUNDED WIRE ON THE WING DUCT OVERHEAT SENSOR OVER LEFT LANDING LIGHT. REPOSITIONED WIRES AWAY FROM ATTAC HING SCREW. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002010800066 20020108 00066 2002 1 8 SWIA200110488 4 20011225 A 3425 FUSE EMB 120 EMB120ER 3260203 SO AHARS COMPUTER MISINSTALLED A SWIA A UNSCHED LANDING I J FLT. ATTITUDE INST. WARNING INDICATION CL CLIMB 1 NM 07 560SW 120334 CAPTAIN AHRS FAILED INFLIGHT (RED HDG/ATT FLAGS) AND F/O'S RMI FAILED AS WELL. FAILED AGAIN INFLIGHT. REPLACED AHRS CO MPUTER. OPS CHECK GOOD. FOUND AHRS FUSE F0029 NOT PROPERLY INSTALLED. RESECURED FUSE CAP. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002010800067 20020108 00067 SO 2002 1 8 SWIA200110489 1 20011228 A 2612 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 198SW 120227 ON DEPARTURE CLIMB, RIGHT PIPE ZONE DET INOP LIGHT ILLUMINATED AND STAYED ON STEADY FOR 8-10 MINUTES, THEN ILLUMINATED I NTERMITTENTLY FOR DURATION OF FLIGHT. INSPECTED RIGHT PIPE FIRE DETECTION SYSTEM, COULD NOT DUPLICATE FAULT. 2 L 7 2 4T RT A31SO 2002010800068 20020108 00068 SO 2002 1 8 SWIA200110490 1 20011223 A 6123 SWITCH EMB 120 EMB120ER 3260203 SO RIGHT OUT OF ADJ A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 235SW 120310 AUTO FEATHER SYSTEM WOULD NOT ARM DURING TAKEOFF. TESTED OK ON FIRST FLIGHT OF THE DAY CHECKS. CLEANED BOTH 62 DEGREE MICRO SWITCHES AND ADJUSTED RIGHT SWITCH IAW MM 76-10-01. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002010800069 20020108 00069 EA 2002 1 8 SWIA200110491 1 20011225 A 2750 601R93100103 POWER UNIT CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 594SW 7285 AFTER SETTING FLAPS 45 DEGREES, FLAPS FAIL CAUTION MESSAGE CAME ON. FLAPS FAILED AGAIN IN SLC. REMOVED AND REPLACED EL ECTRONIC FLAP COMPUTER, OPS CHECK GOOD. REMOVED AND REPLACED PDU IAW CRJ MM 27-52-01, RIGGED BPSU IAW CRJ MM 27-51-10, REMOVED AND REPLACED FLEX SHAFT NR 4 IAW CRJ MM 27-53-10, FUNCTION CHECK OF FLAP SYSTEM GOOD. P/N OFF 601R93100-103, S/N OFF 837. 2 L 7 2 4F RT A21EA 2002010800070 20020108 00070 NE 2002 1 8 SWIA200110492 3 20011215 A 6140 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO HAMSTD 14RF 14RF9 NE COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 582SW 120350 ON TAKEOFF, AUTO FEATHER AURAL WARNING SOUNDED WITH SWITCH IN THE ON POSITION AND SYSTEM ARMED. AUTO FEATHER SYSTEM OPS CHECK GOOD DURING TEST. POWERED DOWN AND BACK UP. PERFORMED HIGH SPEED TAXI. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 6 C P11NE 2002010800071 20020108 00071 SO 2002 1 8 SWIA200110493 1 20011229 A 3234 12043270501 CONTROL BOX EMB 120 EMB120ER 3260203 SO LANDING GEAR FAULTY A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 213SW 408 408 120277 LANDING GEAR HANGING UP FOR MORE THAN AFTER TAKEOFF. REMOVED AND REPLACED LANDING GEAR CONTROL RELAY BOX PER EMB120 MM 32-31-02. SWUNG GEAR. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002010800072 20020108 00072 EA 2002 1 8 SWIA200110496 1 20011230 A 5210 ARM CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 905SW 7437 UNABLE TO OPEN MAIN CABIN DOOR FROM OUTSIDE. DISASSEMBLED LOWER PIVOTING ARM ASSEMBLY. CLEANED AND LUBED AS REQUIRED I AW 52-11-02. 2 L 7 2 4F RT A21EA 2002010800073 20020108 00073 2002 1 8 SWIA200110501 4 20011230 A 2210 8220287401 CIRCUIT BOARD CNDAIR CL600 CL6002B19 1900309 EA AUTOPILOT SYS DEFECTIVE A SWIA K NONE J WARNING INDICATION DE DESCENT 1 NM 07 440SW 7589 YD2 INOP STATUS MSG CYCLED ON & OFF DURING DESCENT. REMOVED AND REPLACED BOTH LHP4001 IAW CRJ MM 22-13-03. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002010800074 20020108 00074 EA 2002 1 8 SWIA200110502 1 20011229 A 3020 ANTI-ICE VALVE CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE FAILED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 440SW 7589 RIGHT COWL ANTI-ICE CAUTION WOULD NOT EXTINGUISH WITH COWL ANTI-ICE TURNED ON. REMOVED RIGHT ENGINE COWL ANTI-ICE VALVE AND INSTALLED A SERVICEABLE VALVE. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2002010800075 20020108 00075 EU 2002 1 8 AUS20011041 1 20010929 A 5610 NP1701022 WINDSHIELD BAG BAE146 BAE146300A 1500267 EU COCKPIT FAULTY W O OTHER E VIBRATION/BUFFET CR CRUISE 1 AU S (AUS) RT B' WINDSHIELD WEATHER SEAL DISBONDED AND VIBRATING. 2 H 7 4 4F RT A49EU 2002010800077 20020108 00077 NM 2002 1 8 AUS20011046 1 20011003 A 2510 ENTEX547 SPRING BOEING 737 737724 13844BY NM CFMINT CFM56 CFM565A1 NE COCKPIT SEAT BROKEN W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) FIRST OFFICERS SEAT TRACK LOCK SPRINGS (2OFF) BROKEN. 2 L 7 2 4F 4 F RT A16WE E29NE 2002010800082 20020108 00082 NM 2002 1 8 150070003 1 20011218 A 5312 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED B RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 ON INSPECTION OF THE 178 BULKHEAD NOTED CRACK FROM AFT SIDE ON PILOTS SIDE. (INSPECTED SIDE CHORD AREA ABOVE WL 207). NOTED APPROX 2 INCHES CRACK DOWN RADIUS OF SIDE CHORD. 2 L 7 2 4F A16WE 2002010800083 20020108 00083 NM 2002 1 8 AUS20011051 1 20010901 A 2160 6937319136 CONTROLLER BOEING 737 737476 NM CFMINT CFM56 CFM563C 13802 EU CABIN TEMP BURNED OUT W O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 AU S (AUS) AIR CONDITIONING CONTROL SWITCHING MODULE P5-10 CARD A3 BURNT. 2 L 7 2 4F 4 F RT A16WE E21EU 2002010800088 20020108 00088 CE 2002 1 8 AUS20011056 1 20011002 A 3246 GYS186C21 BOLT BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE WHEEL LOOSE W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 AU S (AUS) LT MAIN WHEEL TIE BOLTS LOOSE. TIRE DEFLATED. 2 H 7 2 4F 4 F RT A16SW E25EA 2002010800089 20020108 00089 NM 2002 1 8 F3LA200100143 1 20011228 A 5330 SKIN BOEING 737 737228 13844AG NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED CRACK IN RADIUS OF R-2 DOOR TOP HINGE CUTOUT. FABRICATED A FILLER AND INSTALLED R EPAIR DOUBLER PER SRM 53-30-02. 2 L 7 2 4F RT A16WE 2002010800091 20020108 00091 NM 2002 1 8 AUS20011058 1 20011002 A 5311 FRAME BOEING 737 737376 NM CFMINT CFM56 CFM563C 13802 EU FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) FRAME LOCATED AT BS727 STRINGER 18A IN THE LT WHEEL WELL CRACKED IN TWO PLACES. 2 L 7 2 4F 4 F RT A16WE E21EU 2002010800100 20020108 00100 CE 2002 1 8 AUS20011062 1 20011007 A 2810 LINE LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP FUEL SYSTEM CHAFED W D RETURN TO BLOCK E A J VIBRATION/BUFFET FLAME/FIRE WARNING INDICATION TX TAXI/GRND HDL 1 AU S (AUS) LT ENGINE FIRE. DAMAGE TO COWLING. FIRE DAMAGE EVIDENT IN AREA OF STARTER MOTOR. INVESTIGATION FOUND THAT ELECTRIC AL ARCING FROM A CHAFED WIRE TO A P' CLAMP HAD BURNT A SMALL HOLE APPROXIMATELY 1MM (0.039IN) IN DIAMETER IN THE ENGINE FUEL FEED LINE CAUSING THE FUEL TO IGNITE IN THE ACCESSORIES AREA OF THE ENGINE. 2 L 7 2 4F 4 F A10CE E6WE 2002010800102 20020108 00102 2002 1 8 GLBA2001243 4 20011230 A 3421 6224565001 GYRO BEECH 1900 1900D 1154162 CE E/E BAY DEFECTIVE A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 262GL 11607 1980 UE262 CO-PILOTS EADI DROOPS 3 TO 5 DEGREE. REPLACED VERTICAL GYRO, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2002010800103 20020108 00103 NM 2002 1 8 AUS20011063 1 20011009 A 3810 288237 COMPRESSOR BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL POTABLE WATER FAULTY W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 AU S 2436 (AUS) POTABLE WATER COMPRESSOR LOCATED IN AFT CARGO BULK HOLD FAULTY. INVESTIGATION FOUND THE COMPRESSOR MOTOR BEARINGS SEIZED. 2 L 7 2 4F 4 F RT A1NM E23EA 2002010800104 20020108 00104 NM 2002 1 8 AUS20011064 1 20011010 A 7920 4483 O-RING BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C 13802 EU ENGINE OIL FAILED W O OTHER E K VIBRATION/BUFFET FLUID LOSS CR CRUISE 1 AU S 20154 (AUS) RT ENGINE LUBRICATION UNIT MCD HOUSING O RING SEAL PROTRUDING FROM BASE. 2 L 7 2 4F 4 F RT A16WE E21EU 2002010800105 20020108 00105 NM 2002 1 8 AUS20011065 1 20011010 A 4940 5198588 MOTOR BOEING 767 767238 1385114 NM PWA JT9 JT9D7R4E 52054 NE APU STARTER FAULTY W K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 AU S (AUS) APU STARTER FAULTY. 2 L 7 2 4F 4 F RT A1NM E3NE 2002010800106 20020108 00106 CE 2002 1 8 GLBA2001246 1 20011230 A 7714 1143800351 INDICATOR BEECH 1900 1900D 1154162 CE COCKPIT FAULTY A GLBA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 03 151GL 5778 16 UE151 OVERSPEED WARNING AT 190 KNOTS. REPLACED INDICATOR, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2002010800107 20020108 00107 NM 2002 1 8 AUS20011066 1 20011009 A 3320 7076A TRANSFORMER BOEING 747 747338 NM CABIN BURNED OUT W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AU S (AUS) TWO LIGHTING TRANSFORMERS Y7NT02 AND Y7NT03 BURNT. INVESTIGATIONFOUND THAT THE OVERHEATING WAS CAUSED BY INCORRECT PART NUMBERLAMPS FITTED IN TWO LOCATIONS. PERSONNEL/MAINTENANCE ERROR. UNAPPROVED PART. 2 L 7 2 4F RT A20WE 2002010800108 20020108 00108 NE 2002 1 8 AUS20011067 2 20011011 A 7200 ENGINE BAC 146 146100A 1500260 EU LYC ALF502 ALF502R5 41580 NE NR 3 FAILED W O OTHER K E FLUID LOSS VIBRATION/BUFFET CR CRUISE 1 AU S (AUS) NR 3 ENGINE OIL PRESSURE LOSS. ENGINE WAS SHUTDOWN BUT CONTINUED TO WINDMILL IN FLIGHT FOR APPROXIMATELY 40 MINUTE S. 2 H 7 4 4F 4 F RT A49EU E6NE 2002010800109 20020108 00109 NM 2002 1 8 HNAA0100080 1 20011224 A 6120 8210176 PUMP DHAV DHC8 DHC8102 2809003 NM NR 2 ENGINE LEAKING A HNAA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 EA 07 914HA 29079 53 ON TAKEOFF ROLL, TORQUE ON NR 2 ENGINE WENT TO 122 PERCENT. RETURNED TO GATE. FOUND LARGE AMOUNT OF FLUID LEAKING FROM NR 2 ENGINE AND PROP AREA. NO CAUTION LIGHT OR WARNING LIGHTS. REMOVED AND REPLACED PCU PUMP. 2 H 7 2 4T RT A13NM 2002010800112 20020108 00112 NM 2002 1 8 AUS20011073 1 20011012 A 2730 32EN144 LIMIT SWITCH BOEING 737 737* NM CFMINT CFM56 CFM563C 13802 EU ELEVATOR CONTROL FAULTY W A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 AU S (AUS) STABILISER NOSE UP LIMIT SWITCH STICKING. 2 L 7 2 4F 4 F RT A16WE E21EU 2002010800113 20020108 00113 NM 2002 1 8 AUS20011075 1 20011014 A 3320 BALLAST BOEING 747 747338 NM CABIN FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 AU S (AUS) LIGHT BALLAST LOCATED AT SEAT 70HJK BURNT. 2 L 7 2 4F RT A20WE 2002010800115 20020108 00115 NE 2002 1 8 AUS20011080 2 20011016 A 7310 FK29501 TUBE BOEING 747 747438 NM RROYCE RB211 RB211524* NE FUEL DIST LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 AU S (AUS) NR 2 ENGINE FUEL NOZZLE SUPPLY TUBE LEAKING. 2 L 7 4 4F 4 F RT A20WE E12EU 2002010800130 20020108 00130 2002 1 8 AUS20011084 4 20010912 A 2330 RDAV705705 VIDEO DISPLAY BOEING 747 747338 NM ENTERTAINMENT SY FAULTY W O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 AU S (AUS) VIDEO MONITORS LOCATED AT SEAT 2A AND 17B BURNT INTERNALLY. INVESTIGATION FOUND OVERHEATING TRANSISTORS CAUSING TH E PCB AND PROTECTIVE LAYER TO BURN. 2 L 7 2 4F RT A20WE 2002010800135 20020108 00135 WP 2002 1 8 NAFA20010004 1 20011127 A 2140 HEATER DOUG DC6 DC6A 3021706 WP CABIN MALFUNCTIONED I N32B D RETURN TO BLOCK B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 AL 01 7780B 45372 STRONG EXHAUST ODOR IN COCKPIT, CO² DETECTOR TURNING BLACK. INSPECTED CABIN HEATER, NO DEFECTS NOTED. REPLACED CO² DET ECTOR, AND OPERATED CABIN HEATER FOR 1 HOUR, NO EXHAUST ODOR NOTED. CO² DETECTOR REMAINED CLEAR, OK FOR SERVICE. 2 L 7 4 4R 6A3 2002010800136 20020108 00136 NM 2002 1 8 PCAA0112172 1 20011224 A 4950 DUCT DHAV DHC8 DHC8102 2809003 NM APU CONTAMINATED A PCAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 13 EICBJ 215 LGA-FLIGHT 3909 CREW REPORTED OIL SMELL AND SMOKE INTERMITTENTLY COMING FROM BOTH APU BLEEDS ON GROUND AND ENGINE BLEED S IN FLIGHT. MAINTENANCE VERIFIED OIL SMELL AND SMOKE FROM APU BLEED. RAN ENGINE BLEEDS, CLEARED TUBING OF OIL AND SME LL SUBSIDED. MEL 49-01 ISSUED FOR APU. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002010800138 20020108 00138 NM 2002 1 8 PCAA0112173 1 20011226 A 3397 WIRE HARNESS DHAV DHC8 DHC8102 2809003 NM CABIN DAMAGED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 830EX 155 DURING ROUTINE MAINTENANCE VISIT SEVERAL EMERGENCY FLOOR PATH LIGHTS FOUND TO BE INOPERATIVE. WIRING HARNESS REPAIRED A T EMERGENCY EXIT ROW 4. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002010800139 20020108 00139 NM 2002 1 8 PCAA0112174 1 20011230 A 3222 88357 LINK DHAV DHC8 DHC8102 2809003 NM NLG WORN A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 821EX 26188 173 DURING FLEET INSPECTION OF NOSE LANDING GEAR FOR WEAR IN THE TRAILING ARM LINK ASSEMBLY THE TRAILING ARM ASSEMBLY, LINK, UPPER AND LOWER PINS WERE REPLACED DUE TO WEAR. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002010800140 20020108 00140 NM 2002 1 8 PCAA0201001 1 20011216 A 5312 PRESSURE PANEL DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 817EX 191 DURING ROUTINE MAINTENANCE VISIT NOSE GEARWELL UPPER DECK FOUND CRACKED BELOW AND FORWARD OF DC CONTACTOR BOX. CRACK WA S REPAIRED IN ACCORDANCE WITH DEHAVILLAND REPAIR DRAWING RD8-53-582. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002010800141 20020108 00141 NM 2002 1 8 PCAA0201002 1 20010715 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM FUSELAGE DENTED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 824EX 387 DURING ROUTINE MAINTENANCE VISIT DENT AND GOUGE FOUND ON RIGHT FUSELAGE SKIN BETWEEN STATION X445.5 AND X467.0 AND STRIN GERS 17S AND 18S. UNDERLYING STRINGER PART 853330026-141, REPAIRED IN ACCORDANCE WITH DEHAVILLAND STRUCTURAL REPAIR MAN UAL 53-10-21. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002010800142 20020108 00142 NM 2002 1 8 PCAA0201006 1 20010104 A 3397 30242 JUMPER DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 820EX 019 DURING ROUTINE MAINTENANCE VISIT, EMERGENCY FLOOR LIGHTING FOUND TO HAVE AN INOPERATIVE SEGMENT. ONE BROKEN JUMPER REPL ACED, ANOTHER JUMPER WAS RESECURED. ALSO, CLEAR LENS COVER REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SER VICE. 2 H 7 2 4T RT A13NM 2002010800144 20020108 00144 EU 2002 1 8 RAIA00112011 1 20011228 A 5230 LATCH JETAIR JETSTM JETSTM4101 1500501 EU CARGO DOOR UNSECURE A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 558HK 41071 5487-STL- BAGGAGE DOOR CAPTION LIGHT ILLUMINATED DURING TAKEOFF ROLL. MAINTENANCE PROPERLY CLOSED AND SECURED DOOR LATC H IAW J41 MM. 2 L 7 2 4T RT A41NM 2002010800145 20020108 00145 EU 2002 1 8 RAIA00112012 1 20011230 A 3397 WIRE AEROSP ATR72 ATR72202 8680940 EU CABIN FAULTY A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 721TE 217 MX-STL- FLOOR PATH LIGHTING IN REAR HALF OF CABIN INOP. REPAIRED FAULTY WIRE AT FLOOR LIGHTING TRACK IAW ATR72 MM. 2 H 7 2 4T RT A53EU 2002011800121 20020118 00121 SO 2002 1 18 RAIA00112013 1 20011231 A 7830 83990152 SWITCH EMB 145 EMB145ER 3260211 SO THRUST REVERSER BENT A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 808HK 596 145157 5274-PIT- LEFT THRUST REVERSER DISAGREE ON TAKEOFF. MAINTENANCE DEFERRED LEFT THRUST REVERSER PER EMB145 MEL. MAINTENA NCE REMOVED AND REPLACED THE LOWER STOW SWITCH. 2 L 7 2 4F RT T00011AT 2002010800153 20020108 00153 NM 2002 1 8 AALA20012097 1 20011202 A 3397 PIN BOEING 767 767223 1385123 NM CONNECTOR LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 332AA 22331 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 28H INOPERATIVE. RESECURED LOOSE PIN AT SEAT 28H. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002010800154 20020108 00154 NM 2002 1 8 AALA20012139 1 20011207 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 353AA 24034 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 31H, 23B, AND 2B INOPERATIVE. REPAIRED WIRE AT CONNECT OR FOR EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002010800155 20020108 00155 NM 2002 1 8 AALA20012147 1 20011130 A 3350 LIGHT BOEING 767 767323 1385205 NM COCKPIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39364 24045 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED OVERHEAD COCKPIT EMERGE NCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002010800156 20020108 00156 NM 2002 1 8 AALA20012148 1 20011205 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 386AA 27060 DFW - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT 22B INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002010800157 20020108 00157 EU 2002 1 8 AALA20012154 1 20011209 A 7931 5540671 WIRE HARNESS FOKKER F28 F28MK0100 4990807 EU NR 2 ENGINE FAULTY A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 1452B 11464 DFW - FLT 542 - EN ROUTE DFW-TYS, DURING CLIMB-OUT, NR 2 OIL PRESSURE WARNING ILLUMINATED ON MFDU. RETURNED DFW AND LAN DED WITHOUT FURTHER INCIDENT. REPLACED NR 2 ENGINE EMUX HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2002010800158 20020108 00158 WP 2002 1 8 AALA20012155 1 20011210 A 2170 1808492 COALESCER BAG DOUG DC9 DC982 3022082 WP A/C BAY CONTAMINATED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 480AA 49655 ORD - FLT 386 - EN ROUTE ORD-LGA DURING CLIMB-OUT, DETECTED WHITE SMOKE IN COCKPIT. RETURNED TORD AND LANDED WITHOUT FU RTHER INCIDENT. REPLACED COALESCER BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002010800159 20020108 00159 WP 2002 1 8 AALA20012156 1 20011208 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 587AA 53250 DFW - DURING OVERNIGHT MAINTENANCE, FRONT HALF THROUGH ROW 19 INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002010800160 20020108 00160 WP 2002 1 8 AALA20012157 1 20011211 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 570AA 49352 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM G ROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2002010800163 20020108 00163 WP 2002 1 8 ASAA0180279 1 20011009 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 931AS 49232 PDX - DURING LINE CHECK, THREE CABIN OVERHEAD EMERGENCY LIGHTS CAME ON WHEN AIRCRAFT BATTERY WAS SWITCHED OFF. REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY PACK AT B5-107. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2002010800164 20020108 00164 WP 2002 1 8 ASAA0180280 1 20011010 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 934AS 49235 PDX - DURING LINE CHECK, FOUND CABIN FLOOR EMERGENCY TRACK LIGHTING WAS DETERMINED TO BE INOPERATIVE FROM ROW 1 THROUGH 9. REPAIRED BROKEN WIRE AT ROW 6 AND REPLACED FORWARD EMERGENCY LIGHT BATTERY POWER SUPPLY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2002010800165 20020108 00165 WP 2002 1 8 ASAA0180286 1 20011016 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 948AS 53021 SEA - DURING PRE-FLIGHT CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE IN FIRST CLASS CABIN. REPLACED LIG HT MODULE AND RECONNECTED. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002010800166 20020108 00166 WP 2002 1 8 ASAA0180288 1 20011017 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 933AS 49234 LAX - DURING PRE-FLIGHT CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE IN FIRST CLASS CABIN. REPLACED DIS CHARGED BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2002010800167 20020108 00167 WP 2002 1 8 ASAA0180289 1 20011017 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 SEA - DURING PREFLIGHT CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE IN CABIN (PRECISE LOCATION UNSPECIFI ED). REPLACED DISCHARGED BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002010800171 20020108 00171 WP 2002 1 8 ASAA0180290 1 20011018 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 933AS 49234 SEA - DURING PREFLIGHT CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE IN FORWARD CABIN. REPLACED DISCHARG ED BATTERY PACK. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 2002010800172 20020108 00172 EA 2002 1 8 ASOA01262 1 20011126 A 2750 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAILED A ASOA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 11 882AS 7503 FLT 4720 - DURING CLIMB-OUT OF MTY TO ATL, FLAPS RETRACTED ON SCHEDULED. THEN, AT APPROXIMATELY 5000 FEET, THE CAPTAIN RECEIVED A 'FLAPS FAIL' CAUTION MESSAGE. THE FLAPS WERE VERIFIED AT ZERO DEGREES. AN EMERGENCY WAS DECLARED AND THE AI RCRAFT MADE AN UNEVENTFUL LANDING IN ATL. MAINTENANCE REMOVED AND REPLACED THE RIGHT BRAKE AND POSITION SENSOR UNIT. ( M) 2 L 7 2 4F RT A21EA 2002010800173 20020108 00173 SO 2002 1 8 ASOA01263 1 20011128 A 3350 D36604001 BATTERY EMB 120 EMB120ER 3260203 SO CABIN DEFECTIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 267AS 120198 FLT 4347 - DURING GROUND INSPECTION IN ATL, CREW REPORTED THE EMERGENCY LIGHT CIRCUIT BREAKER POPPED WHEN THE FLIGHT ATT ENDANT SWITCH WAS IN THE ON POSITION. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING BATTERY. OPERATIONAL CHE CKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002010800174 20020108 00174 SO 2002 1 8 ASOA01264 1 20011128 A 5711 12016806002 SPAR CAP EMB 120 EMB120RT 3260202 SO RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 281AS 120224 DURING SCHEDULED MAINTENANCE IN MCN, A CRACK WAS FOUND ON THE RIGHT SIDE LOWER SPAR CAP. MAINTENANCE REPAIRED THE CRACK ED SPAR CAP IAW ASA EO 120-57-0117. THE EO REF SRM 57-20-05, FIGURE 201 AND SRM 51. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002010800175 20020108 00175 SO 2002 1 8 ASOA01265 1 20011129 A 3350 D36604001 BATTERY EMB 120 EMB120RT 3260202 SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 237AS 120051 FLT 4092 - DURING GROUND INSPECTION IN ATL, THE MIDDLE SECTION OF EMERGENCY LIGHTING WAS INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE EMERGENCY LIGHTING BATTERY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002010800176 20020108 00176 EA 2002 1 8 ASOA01266 1 20011129 A 3350 3071BPE LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 856AS 7404 FLT 4511 - DURING GROUND INSPECTION IN ATL, THE RIGHT FORWARD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT FORWARD EMERGENCY LIGHT BULB. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002010800177 20020108 00177 EA 2002 1 8 ASOA01267S 1 20011201 A 2910 601R75276553 HYDRAULIC LINE CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A ASOA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 11 827AS 7212 FLT 4721 - APPROACH TO MMY, GEAR WAS SELECTED DOWN, RECEIVED A GEAR DISAGREE WARNING WITHIN FIVE SECONDS. THEN RECEIVED A HYDRAULIC NR 3 LOW PRESSURE AND A ZERO PRESSURE WARNING. WHEN THE GEAR WAS SELECTED UP THE MESSAGES CLEARED. AN EME RGENCY GEAR EXTENSION WAS PERFORMED. EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN MMY. MAINT R&R THE TWO F LEX LINES FOR THE TWO HYDRAULIC PUMPS, 3A AND 3B, AND SERVICED THE HYDRAULIC SYSTEM. THIS WAS NOT THE PROBLEM. UPON FU RTHER INSPECTION, THE LEFT WING AILERON OUTBOARD PCU HYDRAULIC LINE AS FOUND TO BE CRACKED AND LEAKING AT FUEL PANEL 550 GB. MAINTENANCE REPAIRED CRACKED LINE. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002010800178 20020108 00178 EU 2002 1 8 ASOA01268 1 20011202 A 3350 NUT AEROSP ATR72 ATR72212 8680945 EU COCKPIT LOOSE A ASOA K NONE O OTHER CR CRUISE 1 SO 11 532AS 458 FLT 4334 - DURING FLIGHT FROM CHA TO ATL, THE COCKPIT EMERGENCY LIGHT CIRCUIT BREAKER POPPED. AIRCRAFT LANDED WITHOUT I NCIDENT IN ATL. MAINTENANCE INSPECTED THE COCKPIT EMERGENCY LIGHT ASSEMBLY. THERE WERE NO DEFECTS NOTED. A LOOSE JAMN UT WAS FOUND AT THE FLOOD LIGHT CONTROL PANEL RHEOSTAT, PANEL 112VU. MAINTENANCE TIGHTENED THE LOOSE JAM NUT. OPERATIO NAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2002010800179 20020108 00179 SO 2002 1 8 ASOA01269 1 20011203 A 3350 1317 LIGHT EMB 120 EMB120RT 3260202 SO EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 236AS 120049 DURING SCHEDULED MAINTENANCE, THE RIGHT WING UPPER EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TH E BURNED OUT BULB FROM THE RIGHT WING UPPER EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVIC E. (M) 2 L 7 2 4T RT A31SO 2002010800180 20020108 00180 SO 2002 1 8 ASOA01270 1 20011205 A 2611 BATTERY EMB 120 EMB120RT 3260202 SO SMOKE DETECTOR DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 21 284AS 120249 DURING GROUND INSPECTION IN IAH, THE LAVATORY SMOKE DETECTION SYSTEM WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED T HE LAVATORY SMOKE DETECTOR BATTERY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002010800181 20020108 00181 EU 2002 1 8 ASOA01271 1 20011205 A 3350 EO24428A0 RELAY AEROSP ATR72 ATR72212 8680945 EU COCKPIT FAULTY A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 532AS 458 FLT 4271 - DURING GROUND INSPECTION IN ATL, THE CAPTAIN REPORTED THE COCKPIT EMERGENCY LIGHT CIRCUIT BREAKER POPPED. MA INTENANCE REMOVED AND REPLACED THE 14LE RELAY AND RESET THE CIRCUIT BREAKER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2002010800182 20020108 00182 EU 2002 1 8 ASOA01272 1 20011206 A 3350 CIRCUIT BREAKER AEROSP ATR72 ATR72212 8680945 EU COCKPIT TRIPPED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 532AS 458 FLT 4069 - DURING GROUND INSPECTION IN ATL, THE CAPTAIN REPORTED THE COCKPIT EMERGENCY LIGHT CIRCUIT BREAKER POPPED. MA INTENANCE RESET THE EMERGENCY LIGHT CIRCUIT BREAKER. OPS CHECKS OF ALL LIGHT SYSTEMS GOOD. MAINTENANCE CYCLED EXTERNAL POWER, AND NO DEFECTS WERE NOTED. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2002010800183 20020108 00183 EA 2002 1 8 ASOA01273 1 20011207 A 3350 3071BPE LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 825AS 7207 DURING C-CHECK INSPECTION IN MCN, THE FORWARD ENTRY SIDEWALL EMERGENCY EXIT LIGHT WAS FOUND TO BE DAMAGED. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT LIGHT BULB. NO OTHER DAMAGE NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVI CE. (M) 2 L 7 2 4F RT A21EA 2002010800184 20020108 00184 SO 2002 1 8 ASOA01274 1 20011208 A 3040 ODOR EMB 120 EMB120ER 3260203 SO COCKPIT DETECTED A ASOA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 500AS 120272 FLT 4388 - CRUISE FLIGHT FROM ROA TO ATL, AFTER TURNING ON WINDSHIELD HEAT, REPORTED AN ELECTRICAL SMELL IN THE COCKPIT. THE SMELL SEEMED TO GO AWAY WHEN THE WINDSHIELD HEAT WAS TURNED OFF. THE CAPTAIN AGAIN TURNED THE WINDSHIELD HEAT ON. A DEFINITE SMELL OF ELECTRIC SMOKE WAS COMING FROM THE OVERHEAD PANEL. THE CAPTAIN THEN TURNED OFF THE WINDSHIELD HEA T AND LEFT IT OFF. NO FURTHER SMELLS WERE NOTICED. A/C LANDED SAFELY IN ATL. MAINT DROPPED THE OVERHEAD PANEL AND INS PECTED THE WIRES AND SWITCHES. NO DEFECTS NOTED. MAINT RAN THE WINDSHIELD HEAT FOR APPROXIMATELY 10-15 MINUTES AND REC EIVED NO INDICATIONS OF SMOKE OR ELECTRICAL SMELLS. THE PANEL WAS RESECURED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2002010800185 20020108 00185 SO 2002 1 8 ASOA01275 1 20011205 A 5315 12046155504 FLOORBEAM EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 282AS 120226 DURING C-CHECK INSPECTION AT BNA, CORROSION WAS FOUND AT THE FLOOR OMEGA BEAM, FRAME STATION 4088, LEFT SIDE. MAINTENAN CE REPAIRED THE CORRODED FLOOR OMEGA BEAM IAW ASA EO 120-53-0170. (M) 2 L 7 2 4T RT A31SO 2002010800186 20020108 00186 EU 2002 1 8 ASOA01276 1 20011212 A 5311 FRAME AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 635AS 372 DURING C-CHECK INSPECTION IN BNA, A CRACK WAS FOUND ON FRAME 26 AT BL 0. MAINTENANCE REPAIRED THE CRACK IN FRAME 26 IAW ASA E072-53-0121. THIS AIRCRAFT WILL RETURN TO SERVICE UPON COMPLETION OF C-CHECK. (M) 2 H 7 2 4T RT A53EU 2002010900059 20020109 00059 NE 2002 1 9 0104809988 2 20011230 A 7200 JT8D7 ENGINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7 52053 NE RIGHT STALLED A NWAA E A ENGINE SHUTDOWN UNSCHED LANDING R E PARTIAL RPM/PWR LOSS VIBRATION/BUFFET CL CLIMB 1 GL 01 8944E 66352 4625 47167 657250 DURING CLIMBOUT THE RIGHT ENGINE EXPERIENCED A STALL WITH ASSOCIATED VIBRATION AND POWER LOSS. CREW SHUTDOWN THE RIGHT ENGINE AND RETURNED TO DTW. ENGINE OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A6WE E2EA 2002010900060 20020109 00060 WP 2002 1 9 0105029989 1 20010706 A 5320 WEB DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8945E 47181 DURING HCK IN ATL, A 5 INCH LONG CRACK WAS FOUND IN THE RIGHT HAND CUSP MEMBRANE AT STA 617. THE DAMAGED SECTION OF THE CUSP MEMBRANE EXTENDS FROM STA 598 TO 658. THIS EA 99-181334 PROVIDES SPLICE INSTRUCTIONS TO REPLACE ONLY THE PORTION OF MEMBRANE BETWEEN 598 AND 617. 2 L 7 2 4F A6WE 2002012200158 20020122 00158 NM 2002 1 22 02FDEA00002 1 20011227 A 5730 ARB7661 SKIN DOUG MD11 MD11F 3023600 NM RT WINGLET CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 RT WING UPPER WINGLET UPPER O/B SURFACE DENT MARK AND CORROSION. RT WING UPPER WINGLET UPPER O/B DENT MARK MEASURED WIT HIN LIMIT PER SRM 57-00-01 VOL 1. CORROSION SKIN REPAIRED AS PER SRM 57-00-01 FIG 7 VOL 1. REWORK AREA NDT INSP NO CRAC K AS PER NDT SPM PART 06-10-01-001. 2 L 7 3 4F RT A22WE 2002010900065 20020109 00065 EU 2002 1 9 02FDEA00003 1 20011230 A 3251 CONTROL UNIT AIRBUS 300 A300F4605R 3930327 EU NLG STEERING MALFUNCTIONED A FDEA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 25 650FE 726 DURING PUSHBACK AC PUSHED BACK AND FORTH WITH PARK BRAKE SET. AC PROCEEDED TO VEER LEFT REQUIRING FULL RT DIFFERENTIAL STRAIGHTENING. 2 L 7 2 4F RT A35EU 2002010900066 20020109 00066 WP 2002 1 9 02FDEA00004 1 20011025 A 5347 SEAT TRACK DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 303FE 46802 UPPER CARGO SEAT TRACK AT BS 595 TO 765 HAS CRACK AT 655. REMOVED AND REPLACED SEAT TRACK PER SRM 53-70-00 & 51-21-01. 2 L 7 3 4F RT A22WE 2002012900042 20020129 00042 WP 2002 1 29 02FDEA00005 1 20011227 A 2780 CONTROL CABLE DOUG DC10 DC1030F 3023504 WP L/E SLAT BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 305FE 47870 RIGHT WING NR 8 SLAT 2ND SLAT TRACK FROM O/B END CABLE BROKEN. REMOVED AND REPLACED CABLE PER MM 27-89-14-4. 2 L 7 3 4F RT A22WE 2002011500094 20020115 00094 NM 2002 1 15 02FDEA00024 1 20011227 A 5330 SKIN BOEING 727 7272S2F 1384O81 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 205FE 22927 SKIN DENTED AT SKIN LAP BS 1133, STR 20L. REMOVED AND REPLACED SKIN PER SRM 53-30-1. 2 L 7 3 4F A3WE 2002010900079 20020109 00079 CE 2002 1 9 2001F00756 1 20010706 A 7810 NH100089770 CLAMP CESSNA 340 340A 2076405 CE CONT O520 TSIO520NB 17040 SO EXHAUST SYS CRACKED B BIGA K NONE O OTHER IN INSP/MAINT 1 NM 04 114B 191 NEW AEROQUIP EXHAUST CLAMPS ARE CRACKING AROUND OUTER PERIPHERY. APPEAR TO BE MANUFACTURING DEFECTS. 1 L 7 2 3O 3 O 3A25 E8CE 2002010900080 20020109 00080 CE 2002 1 9 2001F00757 1 20011009 A 7810 NH100089770 CLAMP CESSNA 340 340A 2076405 CE CONT O520 TSIO520NB 17040 SO EXHAUST SYS CRACKED B BIGA K NONE O OTHER IN INSP/MAINT 1 NM 04 114BH 539 340A1230 NEW AEROQUIP EXHAUST CLAMPS ARE CRACKING AROUND OUTER PERIPHERY. APPEAR TO BE MANUFACTURING DEFECTS. 1 L 7 2 3O 3 O 3A25 E8CE 2002010900081 20020109 00081 CE 2002 1 9 2001F00758 1 20011210 A 7810 NH100089770 CLAMP CESSNA 340 340A 2076405 CE CONT O520 TSIO520NB 17040 SO EXHAUST SYS CRACKED B BIGA K NONE O OTHER IN INSP/MAINT 1 NM 04 114BH 29 340A1230 NEW AEROQUIP EXHAUST CLAMPS ARE CRACKING AROUND OUTER PERIPHERY. APPEAR TO BE MANUFACTURING DEFECTS. 1 L 7 2 3O 3 O 3A25 E8CE 2002010900082 20020109 00082 CE 2002 1 9 2001F00759 1 20010511 A 7810 NH100089770 CLAMP CESSNA 340 340A 2076405 CE CONT O520 TSIO520NB 17040 SO EXHAUST SYS CRACKED B BIGA K NONE O OTHER IN INSP/MAINT 1 NM 04 118BH 91 340A0003 NEW AEROQUIP EXHAUST CLAMPS ARE CRACKING AROUND OUTER PERIPHERY. APPEAR TO BE MANUFACTURING DEFECTS. 1 L 7 2 3O 3 O 3A25 E8CE 2002010900083 20020109 00083 CE 2002 1 9 2001F00760 1 20010607 A 7810 NH100089770 CLAMP CESSNA 340 340A 2076405 CE CONT O520 TSIO520NB 17040 SO EXHAUST SYS CRACKED B BIGA K NONE O OTHER IN INSP/MAINT 1 NM 04 118BH 51 340A0003 NEW AEROQUIP EXHAUST CLAMPS ARE CRACKING AROUND OUTER PERIPHERY. APPEAR TO BE MANUFACTURING DEFECTS. 1 L 7 2 3O 3 O 3A25 E8CE 2002010900084 20020109 00084 CE 2002 1 9 2001F00761 1 20010612 A 7810 NH100089770 CLAMP CESSNA 340 340A 2076405 CE CONT O520 TSIO520NB 17040 SO EXHAUST SYS CRACKED B BIGA K NONE O OTHER IN INSP/MAINT 1 NM 04 118BH 10 340A0003 NEW AEROQUIP EXHAUST CLAMPS ARE CRACKING AROUND OUTER PERIPHERY. APPEAR TO BE MANUFACTURING DEFECTS. 1 L 7 2 3O 3 O 3A25 E8CE 2002010900085 20020109 00085 CE 2002 1 9 2001F00762 1 20010811 A 7810 NH100089770 CLAMP CESSNA 340 340A 2076405 CE CONT O520 TSIO520NB 17040 SO EXHAUST SYS CRACKED B BIGA K NONE O OTHER IN INSP/MAINT 1 NM 04 118BH 91 340A0003 NEW AEROQUIP EXHAUST CLAMPS ARE CRACKING AROUND OUTER PERIPHERY. APPEAR TO BE MANUFACTURING DEFECTS. 1 L 7 2 3O 3 O 3A25 E8CE 2002010900086 20020109 00086 CE 2002 1 9 2001F00763 1 20011109 A 7810 NH100089770 CLAMP CESSNA 340 340A 2076405 CE CONT O520 TSIO520NB 17040 SO EXHAUST SYS CRACKED B BIGA K NONE O OTHER IN INSP/MAINT 1 NM 04 118BH 52 340A0003 NEW AEROQUIP EXHAUST CLAMPS ARE CRACKING AROUND OUTER PERIPHERY. APPEAR TO BE MANUFACTURING DEFECTS. 1 L 7 2 3O 3 O 3A25 E8CE 2002010900088 20020109 00088 NE 2002 1 9 2002F00002 2 20011228 A 7321 GAGT48179 FCU LEAR 24 24B 5170306 CE GE CJ610 CJ6106 30006 NE ENGINE FAILED E ESUA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 CE 03 600XJ 190 190 251406 ENGINE FLAME OUT DUE TO FUEL CONTROL FAILURE. 2 L 7 2 4J 4 J A10CE 1E16 2002010900089 20020109 00089 CE 2002 1 9 391MT01 1 20011202 A 3260 444EN496 SAFETY SWITCH BEECH 300 300BEECH 1152930 CE LANDING GEAR FAILED E DEBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 391MT 4519 115 FA111 AFTER TAKEOFF, THE LANDING GEAR DID NOT RETRACT AND THE AIRCRAFT WOULD NOT PRESSURIZE. SAFELY CONTINUED THE FLIGHT, REP OSITIONED THE AIRCRAFT TO TAMPA, WHERE RAYTHEON SERVICE CENTER IS LOCATED. THE SQUAT SWITCHES WERE DETERMINED TO BE UNS ERVICEABLE AND WERE BOTH REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T A24CE 2002010900090 20020109 00090 WP 2002 1 9 ABXA010656 1 20011228 A 2612 FIRE WARNING DOUG DC9 DC941 302207N WP COCKPIT MALFUNCTIONED A ABXA K NONE N FALSE WARNING DE DESCENT 1 GL 23 952AX 47615 LOOP-A LEFT ENGINE LIGHT ILLUMINATED DURING DESCENT. PERFORMED ABNORMAL CHECKLIST AND REMAINED ON LOOP-B. INSPECTED LO OP FOR DEFECTS, NONE FOUND. CHECKED CONTINUITY OF LOOP, ALL OK. CLEANED CONNECTOR FROM WATER/OIL SOAKAGE. OPS CHECKED GOOD IAW DC-9 AMM CHAPTER 26. 2 L 7 2 4F A6WE 2002010900091 20020109 00091 WP 2002 1 9 ABXA010657 1 20011230 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 952AX 47615 EMERGENCY LIGHTS FAILED TEST. REPLACED THE EMERGENCY LIGHT BATTERIES IAW DC-9 MM 33-53-02-4-001. OPS CHECKED GOOD IAW DC-9 MM 33-53-00. 2 L 7 2 4F A6WE 2002010900094 20020109 00094 WP 2002 1 9 ABXA010660 1 20011212 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CANNING A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 FUSELAGE EXTERIOR SKIN WAS OIL CANNING UNDER THE NR 2 PYLON, FORWARD OF STATION 965 IN TWO BAYS. REPAIRED IAW DC-9 SRM 53-04. 2 L 7 2 4F A6WE 2002011000167 20020110 00167 NM 2002 1 10 2001UALA02488 1 20011228 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 AFT PIT BODY FRAME INNER FLANGE LOWER SURFACE IS GOUGED BODY STATION 1500, RBL8, WL 147. MAJOR REPAIR ACCOMPLISHED. IN NER J-ANGLE DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002011000169 20020110 00169 NM 2002 1 10 2001UALA02490 1 20011230 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 AFT PIT FUSELAGE FRAME HAS DENT ON INNER FLANGE STATION 1420 STRINGER 25L. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER ON INNER FLANGE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002011000170 20020110 00170 NM 2002 1 10 2001UALA02491 1 20011229 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 EXT FUSELAGE DOUBLER AT STATION 1480 STRINGER 25L REQUIRES REMOVAL TO FACILITATE INSTALLATION OF 25L STRINGER. MAJOR RE PAIR ACCOMPLISHED. DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002011000171 20020110 00171 NM 2002 1 10 2001UALA02492 1 20011230 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 AFT CARGO COMPARTMENT CIRCUMFERENTIAL FRAME BODY STATION 1580 STRINGER 26L HAS DENT ON INNER CHORD. MAJOR REPAIR ACCOMP LISHED. REPAIRED DOUBLER AND STRINGER CLIP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002011000172 20020110 00172 NM 2002 1 10 2001UALA02493 1 20011230 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 AFT PIT BODY FRAME HAS 2 DENTS AT 1520 STRINGER 22L-23L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002011000175 20020110 00175 NM 2002 1 10 2001UALA02496 1 20011230 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 AFT PIT STATION 1473 STRINGER 25L REPAIR HAS FASTENER ON UPPER FLANGE NO EDGE MARGIN. MAJOR REPAIR ACCOMPLISHED. ACCOM PLISHED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002010900107 20020109 00107 NM 2002 1 9 2001UALA02500 1 20011231 A 5313 STRAP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 FORWARD PIT STATION 287 LEFT HAND SIDE, STRINGER 26L TO 29L TEAR STRAP CRACKED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR AC COMPLISHED 2 L 7 2 4F 4 F RT A1NM E24NE 2002010900115 20020109 00115 NM 2002 1 9 F3LA200100151 1 20011231 A 5330 SKIN BOEING 737 7372L9 1384497 NM FUSELAGE GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 3902 22733 DURING C-1 CHECK, INSPECTION REPORTED FUSELAGE SKIN LAP AT STR 19-R, STA 386 TO STA 410 SCRATCHED AND GOUGED. A 14.5 IN CH AREA ON SKIN LAP AT STR 19-R, STA 386 TO STA 410 FOUND TO BE OUT OF LIMITS PER SRM 53-30-01. DAMAGE WAS REMOVED BETW EEN STA 390 AND STA 404, STR 19-R PER SRM 53-30-3. FILLER AND DOUBLER FABRICATED, DRILLED, TREATED AND INSTALLED PER SR M 53-30-3. 2 L 7 2 4F RT A16WE 2002010900118 20020109 00118 NE 2002 1 9 GLBA2001247 2 20011227 A 7314 1143890425 PUMP BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NR 2 ENGINE FAILED A GLBA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 03 179GL 3841 10 UE179 RIGHT LOW PRESSURE FUEL LIGHT. REPLACED LOW PRESSURE FUEL PUMP, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T 4 T RT A24CE E26NE 2002010900119 20020109 00119 NM 2002 1 9 DL757011945 1 20011216 A 3350 1317 BULB BOEING 757 757232 1384965 NM 45D OPEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 646DL 24217 BULL NOSE EMERGENCY LIGHT AT ROW 45D INOP. RELAMPED. OP CK GOOD 2 L 7 2 4F RT A2NM 2002010900120 20020109 00120 NM 2002 1 9 DL757011946 1 20011215 A 5330 143N34719 SKIN BOEING 757 757232 1384965 NM FS 520, S-28L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 657DL 24419 FUSELAGE / SKIN / FS 520 / STRG. 28L : GROUND DAMAGE CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND DENTED AT TWO LOCATIONS BETWEEN STRINGERS 27L & 28L AT FS 518 AND FS 532. THE DAMAGED AREAS WERE REMOVED WITH 2" CUTOUTS IN THE SKIN. THE TWO CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL ALUMINUM DOUBLER PER ER/A 382221-14, REV A. 2 L 7 2 4F RT A2NM 2002010900121 20020109 00121 NM 2002 1 9 DL72S011950 1 20011214 A 5330 65545664 SKIN BOEING 727 727225A 1384077 NM FS 580, S-26L CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 FUSELAGE / SKIN / FS 549-604 / STRG. 25L-28L : CORROSION CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND CORRODED NEXT TO AN EXISTING REPAIR. THE EXISTING REPAIR WAS REMOVED AND ALL DAMAGES REMOVED WITH A 50" X 16" CUTOUT BETWEEN STRINGERS 25L & 28L AND BETWEEN FS 549 & 604. THE CUTOUT WAS REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS PER ER/A 382201-14, REV B. 2 L 7 3 4F RT A3WE 2002010900122 20020109 00122 NM 2002 1 9 DL72S011951 1 20011214 A 5330 65545664 SKIN BOEING 727 727225A 1384077 NM FS 500, S-26L/R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 FUSELAGE / SKIN / FS 481-520 / STRG. 26L-26R : CORROSION REPAIR THE FUSELAGE SKIN WAS CORRODED IN SEVERAL AREAS BETWEEN FS 481 & 520 AND BETWEEN STRINGERS 26L & 26R. THE SKIN WAS CUT AT FS 520 BETWEEN THE LAP JOINT STRINGERS 26L & 26R. THE CORRODED SECTION OF SKIN WAS REMOVED AND REPLACED WITH A NEW SKIN. THE SKIN WAS SPLICED AT FS 520 WITH TWO EXTERNAL ALUMINUM DOUBLERS PER ER/A 382204-14AD, REV A. 2 L 7 3 4F RT A3WE 2002010900123 20020109 00123 2002 1 9 DL757011965 4 20011221 A 3100 BULB BOEING 757 757232 1384965 NM RIGHT FUSELAGE BURNED OUT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 604DL 22811 DURING LAYOVER INSP FOUND R3 DOOR OUTSIDE EMERG LIGHT INOP. RELAMPED, OPS CHECKS OK. AIRCRAFT LOC DNTC. TAYLOR 2 L 7 2 4F RT A2NM 2002010900124 20020109 00124 NM 2002 1 9 DLM11011973 1 20011223 A 3350 BATTERY 6044115 DOUG MD11 MD11 3023602 NM FIRST CLASS WEAK A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 810DE 0737 48565 EMERGENCY LIGHTS BATT 1 LO ILLUMINATES ON EAD DURING EMERG LIGHT TEST. NO SEAT MOUNTED LIGHTS WORK IN FWD BC CABIN. CORR ACT; REPLACED NO.1 BATTERY UNIT. TEST OK. 2 L 7 3 4F RT A22WE 2002010900125 20020109 00125 NM 2002 1 9 DLM88011976 1 20011222 A 7930 5D03451 RELAY DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE #2 ENGINE FAILED A DALA E ENGINE SHUTDOWN Y ENGINE STOPPAGE CL CLIMB 1 SO 27 948DL 49879 725775 INFLIGHT SHUTDOWN OF NBR 2 ENGINE. DIVERSION TO CSG. INCREASING OIL TEMP. TEMP REACHED 142 DEG, ENG SHUTDOWN AFTER 15 MI NUTE LIMIT REACHED. MAINTENANCE DISPATCHED FROM DELTA NORTH ATL TO CSG. FOUND RIGHT ENG FUEL HEAT TIMER RELAY NOT SHUTTI NG OFF, CAUSING FUEL TO OVERHEAT OIL THROUGH FUEL/OIL COOLER. REPLACED RELAY 249201336. EQUIPMENT NBR R2-65, LOC 110 RE LAY PANEL IN E&E COMPARTMENT. 2 L 7 2 4F 4 F RT A6WE E9NE 2002010900126 20020109 00126 NM 2002 1 9 DL76S011984 1 20011228 A 7100 00 MANIFOLD BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE #2 ENGINE LEAKING A DALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 27 127DL 24077 580365 IR - LOST R ENG OIL PRESS (PRESS INDICATING 4 PSI) ENG SHUTDOWN 20 MIN BEFORE LNDG. (4 PSI INDICATING WHILE WINDMILLING. CA - FOUND FUEL POURING FROM FUEL MANIFOLD AT 5 OCLOCK POS. FROM UPPER BRANCH (SECOND NOZZLE BELLOW LOWER IGNITOR PLUG).REMOVED AND REPLACED FUEL MANIFOLD LEAK CHECK AND IDLE RUN OK. PERFORMED TEST 4 TAKE OFF POWER CHK PFHB. HIGH POWER RUN UP OK. 2 L 7 2 4F 4 F RT A1NM E13NE 2002010900127 20020109 00127 NM 2002 1 9 DL757020005 1 20011231 A 5330 143N33203 SKIN BOEING 757 757232 1384965 NM FS 610, S-16L PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 602DL 22809 FUSELAGE / SKIN / FS 590-620 / STRG. 15L-18L : PUNCTURE REPAIR THE FUSELAGE SKIN WAS PUNCTURED BY GROUND EQUIPMENT AT FS 610 AND STRINGER 16L. THE DAMAGE WAS ADJACENT TO 2 EXISTING SKIN REPAIR DOUBLERS. THE EXSTING DOUBLERS WERE REMOVED AND ALL DAMAGED AREAS WERE INCORPORATED INTO ONE LARGE SKIN CUTOUT FROM FS 590-620 AND FROM STRINGERS 15L TO 18L. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 382345-14, REV B. 2 L 7 2 4F RT A2NM 2002010900132 20020109 00132 EA 2002 1 9 2002F00004 1 20011214 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37342 7342 DURING A SERVICE CHECK INSPECTION, THE CREW FOUND A LEFT MID EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BULB AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2002010900133 20020109 00133 EA 2002 1 9 2002F00005 1 20011212 A 3260 PROXIMITY SWITCH CNDAIR CL600 CL6002B19 1900309 EA NLG DOOR OUT OF ADJ A MASA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 27185 7185 FLT 6156 - PHX-SBA - IN FLIGHT, THE CREW RECEIVED A 'NOSE DOOR OPEN' EICAS MESSAGE. THE AIRCRAFT RETURNED TO THE FIELD WHERE MAINTENANCE ADJUSTED THE PS18GA PROXIMITY SWITCH. OPS CHECKED GOOD AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002010900134 20020109 00134 SO 2002 1 9 2002F00006 1 20011203 A 3350 LENS EMB 145 EMB145LR 3260212 SO CABIN CRACKED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 825MJ 145179 FLT 5873 - THE CREW HAD FOUND THE FORWARD EMERGENCY OVERHEAD LIGHT LENS CRACKED. MAINTENANCE REPLACED THE LENS AND OPS CHECKS GOOD. (M) 2 L 7 2 4T RT T00011AT 2002010900135 20020109 00135 SO 2002 1 9 2002F00007 1 20011201 A 3397 P8641 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 829MJ 145228 FLT 5782 - CLT-HSV, THE CREW REPORTED THAT THE CABIN SIDEWALL EMERGENCY LIGHT AT ROW 3 WAS INOPERATIVE. MAINTENANCE FOU ND AND RECONNECTED A LOOSE CONNECTOR AT THE LIGHT SOCKET. THE LIGHT OPS CHECKED GOOD AND THE AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4T RT T00011AT 2002010900136 20020109 00136 EA 2002 1 9 2002F00008 1 20011130 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37342 7342 DURING AN OVERNIGHT INSPECTION, THE CREW FOUND THE RIGHT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BULB AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2002010900137 20020109 00137 EA 2002 1 9 2002F00009 1 20011129 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77260 7260 DURING AN OVERNIGHT INSPECTION, THE CREW FOUND A LEFT MID EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED TH E BULB AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2002010900138 20020109 00138 EA 2002 1 9 2002F00010 1 20011128 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77331 7331 FLT 5769 - BHM-PHL - A LEFT EXTERIOR FUSELAGE AFT EMERGENCY LIGHT WAS FOUND INOPERATIVE BY THE CREW. MAINTENANCE REPLAC ED THE BURNED OUT LAMP AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2002010900139 20020109 00139 NM 2002 1 9 2002F00011 1 20011116 A 3350 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 447YV 447 FLT 6439 - PHX-TUS - THE PILOT REPORTED THAT THE FA'S EMERGENCY LIGHT SWITCH WAS INOPERATIVE. MAINTENANCE RELAMPED THE LIGHT AND THE FLIGHT RESUMED WITHOUT DELAY. (M) 2 H 7 2 4T RT A13NM 2002010900140 20020109 00140 EA 2002 1 9 2002F00012 1 20011031 A 4920 APU CNDAIR CL600 CL6002B19 1900309 EA APU BAY LEAKING A MASA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 07 77260 7260 FLT 6627 - ORD-CMH - EN ROUTE TO CMH, THE LAVATORY SMOKE DETECTOR WARNING ILLUMINATED. THE FLIGHT ATTENDANT WAS ABLE TO CONFIRM THAT THERE WAS NOT A FIRE ONBOARD BUT THERE WAS A TRACE OF AN OILY SMELL. THE AIRCRAFT RETURNED TO THE FIELD W HERE MAINTENANCE WAS ABLE TO CONFIRM THAT THE APU WAS PUMPING TRACES OF OIL INTO THE PACK. THE APU WAS REMOVED AND REPL ACED IAW CRJ MTC-49-10-00 AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2002010900141 20020109 00141 WP 2002 1 9 AALA20012107 1 20011114 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 588AA 53251 TUL - FOUND NR 1 SEAT TRACK CORRODED AT NUTPLATE ATTACH AREA FOR TIE DOWN BOLT. INSTALLED PLUG PER SRM 51-10-3. (M) 2 L 7 2 4F RT A6WE 2002010900142 20020109 00142 CE 2002 1 9 AALA20012125 1 20011126 A 5320 INTERCOSTAL CESSNA 172 172 2072402 CE FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7426A 29526 TUL - FOUND INTERCOSTAL CRACKED IN AFT CARGO BETWEEN FLOORBEAMS STATION 1271-1287. REPLACED INTERCOSTAL PER SRM 51-01. (M) 1 H 7 1 3O NT 3A12 2002010900143 20020109 00143 WP 2002 1 9 AALA20012126 1 20011126 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 426AA 49338 TUL - FOUND SHEAR TIE CRACKED IN AFT ACCESSORY STATION 1437 INBOARD OF LONGERON 3R AFT FACE OF FRAME. REMOVED AND REPLA CED SHEAR TIE PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2002010900144 20020109 00144 WP 2002 1 9 AALA20012128 1 20011203 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 426AA 49338 TUL - FOUND CORROSION ON SEVERAL AREAS OF AFT CARGO DOOR BEAM. REMOVED AND REPLACED AFT CARGO DOOR BEAM PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2002010900145 20020109 00145 WP 2002 1 9 AALA20012129 1 20011126 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 426AA 49338 TUL - FOUND CORROSION ON TOP AND BOTTOM OF LEFT CUSP AROUND LIGHTNING 2 HOLES. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-00-00-02 AND SRM 53-01 FIG 4. (M) 2 L 7 2 4F A6WE 2002010900146 20020109 00146 WP 2002 1 9 AALA20012130 1 20011116 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 426AA 49338 TUL - FOUND CORROSION ON RIGHT CUSP STATION 731. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 2002010900147 20020109 00147 WP 2002 1 9 AALA20012131 1 20011116 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 426AA 49338 TUL - FOUND NR 3 SEAT TRACK CORRODED STATION 1231-1233. INSTALLED SEAT TRACK PLUG REPAIR PER AARD 53-20-00-10, PAGE 2 F IG 1. (M) 2 L 7 2 4F A6WE 2002010900148 20020109 00148 WP 2002 1 9 AALA20012132 1 20011116 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 426AA 49338 TUL - NR 5 SEAT TRACK CORRODED STATION 233. INSTALLED SEAT TRACK PLUG PLUG PER SRM 53-05 FIG 4A. RESTORED PROTECTIVE F INISH. (M) 2 L 7 2 4F A6WE 2002010900149 20020109 00149 WP 2002 1 9 AALA20012133 1 20011126 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 426AA 49338 TUL - FOUND INTERCOSTAL CRACKED IN AFT CARGO BLO STATION 1287-1309 BETWEEN FLOORBEAMS. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2002010900150 20020109 00150 WP 2002 1 9 AALA20012134 1 20011120 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 426AA 49338 TUL - FOUND LONGERON 3L CRACKED IN RADIUS INBOARD OF OUTBOARD FASTENER STATION 160. SPLICED NEW LONGERON FROM STATION 1 70 FORWARD IAW SRM 53-02 FIG 18 SHEETS 1-4-5-6. (M) 2 L 7 2 4F A6WE 2002010900151 20020109 00151 WP 2002 1 9 AALA20012135 1 20011119 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 426AA 49338 TUL - FOUND LONGERON 4L CRACKED AT FRAME STATION 160. CUT OUT DAMAGED AREA AND INSTALLED SPLICE PER SRM 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 2002010900152 20020109 00152 WP 2002 1 9 AALA20012136 1 20011114 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 426AA 49338 TUL - FOUND FUSELAGE SKIN CRACKED ABOVE NR 2 ENGINE PYLON STATION 1380 LONGERON 13R. STOP DRILLED CRACK AND INSTALLED D OUBLER PER SRM 53-01 FIG 2 SHEET 3. (M) 2 L 7 2 4F A6WE 2002010900153 20020109 00153 WP 2002 1 9 AALA20012137 1 20011119 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 426AA 49338 TUL - FOUND .25 INCH BY .25 INCH GOUGE AND DENT ON LEFT FUSELAGE APPROXIMATELY 10 INCHES BELOW FORWARD STATIC PORT. REM OVED DAMAGE AND INSTALLED A DOUBLER PER SRM 53-04 FIG 38 SHEET 23. (M) 2 L 7 2 4F A6WE 2002010900154 20020109 00154 WP 2002 1 9 AALA20012138 1 20011114 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 426AA 49338 TUL - FOUND STATION 1380 ABOVE NR 1 ENGINE PYLON ABOVE LONGERON 13L OUTER SKIN CRACKED 2 PLACES AT SHEAR TIE LOWER RIVET . STOP DRILLED CRACK OK. INSTALLED DOUBLER PER SRM 53-01-00 FIG 2 SHEET 3. (M) 2 L 7 2 4F A6WE 2002010900155 20020109 00155 NM 2002 1 9 AALA20012158 1 20011210 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 362AA 24043 LAX - DURING OVERNIGHT, MAINTENANCE EMERGENCY EXIT LIGHT AT SEAT 39H INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT 39H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002010900156 20020109 00156 NM 2002 1 9 AALA20012159 1 20011209 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 784AN 29588 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT ROW 32C . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002010900157 20020109 00157 WP 2002 1 9 AALA21002127 1 20011127 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 426AA 49338 TUL - FOUND NUT PLATE MISSING FOR GALLEY TIE DOWN. CUT OUT AREA AND INSTALLED SEAT TRACK PLUG PER 53-05. (M) 2 L 7 2 4F A6WE 2002010900158 20020109 00158 EU 2002 1 9 ASOA01277 1 20011212 A 5341 ATTACH FITTING AEROSP ATR72 ATR72212 8680945 EU FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 635AS 372 DURING C-CHECK INSPECTION IN BNA, THE LEFT AFT WING FITTING AT FRAME 27 WAS FOUND TO BE ELONGATED. THE HOLE IN THE FRAM E WAS ALSO ELONGATED. MAINTENANCE FABRICATED A NEW FITTING AND REPAIRED THE ELONGATED HOLE IAW ASA EO 72-53-0122. THIS EO REF SRM 51- AND ATR DRAWING 15S 535R 0181. THIS EO ALSO INCLUDES REPAIR SPECIFICATIONS FOR THE LEFT AFT WING FITTIN G AT FRAME 27 FOR AIRCRAFT. AIRCRAFT WILL RETURN TO SERVICE UPON COMPLETION OF C-CHECK. (M) 2 H 7 2 4T RT A53EU 2002010900159 20020109 00159 EA 2002 1 9 ASOA01278 1 20011211 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 896AS 7428 DURING HANGAR CHECK IN XNA, THE RIGHT SIDE NR 1 AND NR 2 EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REM OVED AND REPLACED BOTH BURNED OUT EMERGENCY LIGHTS BULBS ON THE RIGHT SIDE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR S ERVICE. (M) 2 L 7 2 4F RT A21EA 2002010900160 20020109 00160 EA 2002 1 9 ASOA01279 1 20011212 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 830AS 7236 DURING HANGAR INSPECTION IN XNA, THE RIGHT FORWARD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TH E BLOWN RIGHT FORWARD EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002010900161 20020109 00161 SO 2002 1 9 ASOA01280 1 20011213 A 3040 ODOR EMB 120 EMB120ER 3260203 SO COCKPIT DETECTED A ASOA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 500AS 120272 FLT 4751 - DURING FLIGHT FROM ROA TO ATL, CAPTAIN REPORTED WHEN WINDSHIELD HEAT IS TURNED ON IT CAUSES AN ELECTRICAL SME LL IN THE COCKPIT. WHEN WINDSHIELD HEAT IS TURNED OFF SMELL DISSIPATES. AIRCRAFT LANDED IN ATL WITHOUT FURTHER INCIDEN T. MAINTENANCE INSPECTED WIRES AND CONTACTORS. SYSTEMS OPERATIONAL CHECKS GOOD. MAINTENANCE RAN BOTH THE CAPTAIN AND FIRST OFFICERS WINDSHIELD HEATING SYSTEMS FOR 25 MINUTES. OPERATIONAL CHECKS GOOD. NO DEFECTS WERE NOTED. AIRCRAFT RE TURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2002010900162 20020109 00162 EU 2002 1 9 ASOA01281 1 20011212 A 5321 FLOORBOARD AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 635AS 372 DURING C-CHECK INSPECTION IN BNA, THE TOP AND BOTTOM SURFACES OF THE FLOORBOARDS TOP FLANGE WERE FOUND TO BE CORRODED AT FRAMES 36, 38, 39, AND 40. MAINTENANCE REPAIRED CORROSION IAW WITH ASA EO72-53-0123. THIS EO REFERENCE FAA FORM 8110- 3, REPORT NR 01-295, WHICH INCLUDES REPAIR SPECIFICATIONS FOR AIRCRAFT. (M) 2 H 7 2 4T RT A53EU 2002010900163 20020109 00163 EU 2002 1 9 ASOA01282 1 20011212 A 5321 FLOORBOARD AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 635AS 372 DURING C-CHECK INSPECTION IN BNA, THE FLOORBOARD SCREW HOLES AT FRAMES 9 AND 10 SHOWED SIGNS OF CORROSION AND SEVERAL EL ONGATED HOLES WERE FOUND. MAINTENANCE REMOVED CORROSION AND REPAIRED ELONGATED HOLES WERE FOUND. MAINTENANCE REMOVED C ORROSION AND REPAIRED ELONGATED HOLES IAW ASA E072-53-0123. THIS EO REF FAA FORM 8110-3, REPORT NR 01-295, WHICH INCLUD ES REPAIR SPECIFICATIONS FOR AIRCRAFT. (M) 2 H 7 2 4T RT A53EU 2002010900164 20020109 00164 EU 2002 1 9 ASOA01283 1 20011212 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 635AS 372 DURING C-CHECK INSPECTION IN BNA, THE RIGHT INBOARD SEAT TRACK, AT FRAME 35 TO 36, WAS FOUND TO HAVE CORROSION. MAINTEN ANCE REPAIRED CORRODED IAW ASA E072-53-0123. THIS EO REF FAA FROM 8110-3, REPORT NR 01-295, WHICH INCLUDES REPAIR SPECI FICATIONS FOR AIRCRAFT. (M) 2 H 7 2 4T RT A53EU 2002010900165 20020109 00165 SO 2002 1 9 ASOA01284 1 20011214 A 5713 12016085001 STRINGER EMB 120 EMB120RT 3260202 SO LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 236AS 120049 DURING SCHEDULED MAINTENANCE IN TXK, THE LEFT WING NR 10 STRINGER WAS CRACKED AT THE NR 1 FUEL PANEL. MAINTENANCE REPAI RED THE CRACK IN THE LEFT NR 10 STRINGER IAW EMB-120 SRM 57-20-03. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002010900166 20020109 00166 EA 2002 1 9 ASOA01285 1 20011215 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 896AS 7428 DURING SCHEDULED INSPECTION IN XNA, THE FIRST THREE INTERIOR CEILING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENAN CE REMOVED AND REPLACED THE 3 BURNED OUT EMERGENCY CEILING LIGHT BULBS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVI CE. (M) 2 L 7 2 4F RT A21EA 2002010900167 20020109 00167 SW 2002 1 9 PNSA011203 1 20011219 A 2932 SS10127 PRESSURE SWITCH FRCHLD SA227 SA227DC 3377521 SW A PNSA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 AL 03 30135 DC890B During taxi RH hydraulic pressure warning light came on with normal pressure indication. Maintenance found hyd pressure switch for warning system faulty. 2 L 7 2 4T RT A18SW 2002011000001 20020110 00001 NM 2002 1 10 ANCF200100024 1 20011226 A 2410 CSD DOUG MD80 MD83 3023681 NM LEFT LEAKING W ANCF A UNSCHED LANDING K M FLUID LOSS OVER TEMP CL CLIMB 1 SW 99 583AN 53183 DURING CLIMB THROUGH FL 280, THE LT CSD OIL PRESSURE LOW ANNUNCIATION CAME ON, THE OUTLET AND RISE TEMPERATURES WERE OUT OF LIMITS, CHECK LIST WAS PERFORMED AND IT WAS NECESSARY DISCONNECTED THE LT CSD. ADDITIONALLY AFTER STARTING APU AT FL 280 THE FREQUENCY WAS OUT OF THE ALLOWABLE LIMITS AND THE RPM WAS ABOVE 110 RPM, AND THE APU MADE AUTO SHOUT DOWN.CORRE CTIVE ACTION: WAS ADJUSTED DRAIN FILTER AND SERVICED THE LT CSD IAW AMM 24-10-00 PAGE 301, OIL SYSTEM WAS CHECKED ON GROUND WITH ENGINE RUNNING, FOUND OK. THE APU WAS SERVICED AND ADJUSTED THE LOAD THERMOSTAT IAW AMM 49-00-00 PAGE 301. T HE SYSTEM WORKS PROPERLY. 2 L 7 2 4F RT 2002011000003 20020110 00003 EU 2002 1 10 AUS20011089 1 20011016 A 3222 STRUT AIRBUS 320 A320* EU CFMINT CFM56 CFM565A1 NE NLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NOSE LANDING GEAR SHOCK STRUT CRACKED CIRCUMFERENTIALLY AT THE LT SIDE UPPER ATTACHMENT AREA. CRACK LENGTH 50.8MM (2IN). 2 L 7 2 4F 4 F RT A46NM E29NE 2002011000004 20020110 00004 EU 2002 1 10 AUS20011090 1 20011016 A 3230 HP84830621 CONTROL VALVE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ROTOL R390 R3904123F27 NE MLG FAILED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LANDING GEAR CONTROL VALVE FAULTY. ELECTRICAL POWER TO THE VALVE WAS OK. 2 L 7 2 4T 4 T RT A52EU E8NE 6 C P31NE 2002011000008 20020110 00008 2002 1 10 AUS20011096 4 20011018 A 2565 SLIDE BOEING 737 737376 NM CFMINT CFM56 CFM563C 13802 EU CABIN MISRIGGED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 AU S (AUS) ESCAPE SLIDE INCORRECTLY RIGGED. DEPLOY CABLE ROUTED OVER THE RAFT INSTEAD OF BEHIND. 2 L 7 2 4F 4 F RT A16WE E21EU 2002011000011 20020110 00011 NM 2002 1 10 AUS20011100 1 20011019 A 4920 380029813 APU BOEING 767 767* NM RROYCE RB211 RB211524* NE APU BAY FAILED W O OTHER E VIBRATION/BUFFET TX TAXI/GRND HDL 1 AU S P1511 (AUS) APU SHUTDOWN. 2 L 7 2 4F 4 F RT A1NM E12EU 2002011000012 20020110 00012 EU 2002 1 10 AUS20011101 1 20010829 A 3246 C201801202A WHEEL AMD FALC50 FALCON900 2700160 EU MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S U465 (AUS) MAIN WHEEL INBOARD HALF CRACKED ADJACENT TO BRAKE TANG. FOUND USING EDDY CURRENT INSPECTION. 2 L 7 3 4F RT A46EU 2002011000016 20020110 00016 EU 2002 1 10 AUS20011105 1 20010908 A 3246 C201801202A WHEEL AMD FALC50 FALCON900 2700160 EU MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S U817 (AUS) MAIN WHEEL INBOARD HALF CRACKED ADJACENT TO BRAKE TANG. FOUND DURING EDDY CURRENT INSPECTION. 2 L 7 3 4F RT A46EU 2002011000022 20020110 00022 EU 2002 1 10 AUS20011111 1 20011017 A 2621 57333014 FIRE BOTTLE BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NR 2 & 3 ENGINES MISINSTALLED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NO3 ENGINE NO2 FIRE BOTTLE INCORRECTLY WIRED. PERSONNEL/MAINTENANCE ERROR. 2 H 7 4 4F 4 F A49EU E6NE 2002011000040 20020110 00040 2002 1 10 AUS20011131 4 20011021 A 2565 101630305 SLIDE BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL LT OVERWING MISINSTALLED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 AU S PG0268 (AUS) LT OFF WING ESCAPE SLIDE FITTED TO AIRCRAFT. SLIDE HAD BEEN FITTED FOLLOWING INADVERTANT FIRING OF THE FITTED SLID E. THE SLIDE FITTED WAS FOR A -238 SERIES AIRCRAFT. 2 L 7 2 4F 4 F RT A1NM E23EA 2002011000041 20020110 00041 NM 2002 1 10 AUS20011132 1 20011025 A 7603 575751 CONTROL CABLE RROYCE RB211524D4 BOEING 747 747338 NM RROYCE RB211 RB211524D419 54555 NE POWER LEVER SEIZED W O OTHER F FLT CONT AFFECTED LD LANDING 1 AU S 128 (AUS) NR 1 ENGINE THRUST LEVER PUSH/PULL CABLE SEIZED. 2 L 7 2 4F 4 F RT A20WE E12EU 2002011000042 20020110 00042 NM 2002 1 10 AUS20011133 1 20011025 A 3620 21SN4182 PRESSURE SWITCH BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL NR 1 ENGINE FAULTY W O OTHER J WARNING INDICATION TO TAKEOFF 1 AU S 5032 M0147X (AUS) NR 1 ENGINE PNEUMATIC SYSTEM OVERPRESSURE SWITCH FAULTY. 2 L 7 2 4F 4 F RT A1NM E23EA 2002011000047 20020110 00047 NM 2002 1 10 AUS20011143 1 20011028 A 6123 PROPELLER DHAV DHC8 DHC8315 2809010 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE RIGHT MALFUNCTIONED W C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 AU S (AUS) RT PROPELLER AUTOFEATHER. PROPELLER OVER TORQUED. INVESTIGATION COULD FIND NO FAULT. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011000053 20020110 00053 EU 2002 1 10 AUS20011151 1 20011030 A 7714 INDICATOR BAC 146 146100A 1500260 EU LYC ALF502 ALF502R5 41580 NE ENGINE RPM FAILED W O OTHER E VIBRATION/BUFFET CL CLIMB 1 AU S (AUS) NR 2 ENGINE N1 INDICATION FAILED FOLLOWING TAKEOFF. INDICATION RETURNED PRIOR TO LANDING. INVESTIGATION COULD FIND NO CAUSE FORTHE DEFECT. 2 H 7 4 4F 4 F RT A49EU E6NE 2002011000061 20020110 00061 NM 2002 1 10 AUS20011155 1 20011028 A 2741 32EN614 SWITCH BOEING 737 737* NM CFMINT CFM56 CFM563B2 13802 EU STAB INDICATOR FAULTY W C ABORTED TAKEOFF F N FLT CONT AFFECTED FALSE WARNING TO TAKEOFF 1 AU S (AUS) HORIZONTAL STABILISER UPPER LIMIT SWITCH SUSPECT FAULTY. 2 L 7 2 4F 4 F RT A16WE E21EU 2002011000062 20020110 00062 EU 2002 1 10 AUS20011156 2 20011030 A 7200 ENGINE BOEING 737 73746B NM CFMINT CFM56 CFM563C 13802 EU NR 2 OVERTEMP W C ABORTED TAKEOFF E M VIBRATION/BUFFET OVER TEMP TO TAKEOFF 1 AU S (AUS) NR 2 ENGINE OVERTEMPED TO 938 DEGREES C ON TAKEOFF. BORESCOPE INSPECTION COULD FIND NO FAULTS. 2 L 7 2 4F 4 F RT A16WE E21EU 2002011000063 20020110 00063 NM 2002 1 10 AUS20011159 1 20011029 A 2710 256T34304 GEARBOX BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL AILERON CONTROL FAULTY W K NONE O OTHER IN INSP/MAINT 1 AU S 316 (AUS) RT AILERON GEARBOX OUTPUT CRANK FAILED TO RESPOND TO FLAP POSITION. 2 L 7 2 4F 4 F RT A1NM E23EA 2002011000067 20020110 00067 NE 2002 1 10 AUS20011167 2 20011106 A 7230 13125 COMPRESSOR BOEING 747 747438 NM RROYCE RB211 RB211524G19 NE NR 4 ENGINE FOD W O OTHER E VIBRATION/BUFFET CL CLIMB 1 AU S 12051 (AUS) NR 4 ENGINE FIRST STAGE HP COMPRESSOR DAMAGED BY FOD. FOUND DURING BOROSCOPE INSPECTION FOLLOWING INFLIGHT SHUTDOW N. 2 L 7 4 4F 4 F RT A20WE E30NE 2002011000071 20020110 00071 NM 2002 1 10 AUS20011173 1 20011106 A 2910 NUT BOEING 757 75723A 1384967 NM RROYCE RB211 RB211535E4 54555 NE HYD PUMP LOOSE W K NONE K FLUID LOSS IN INSP/MAINT 1 AU S (AUS) NR 1 ENGINE DRIVEN HYDRAULIC PUMP PRESSURE LINE UNION JAM NUT LOOSE AND LEAKING. INVESTIGATION FOUND THAT IT WAS C HAFED THROUGH FOR 50 PERCENT OF THE CIRCUMFERENCE ON THE JAM NUT SIDE WITH A CORRESPONDING RIDGE (FRACTURE) ON THE INSID E. UNION IS LOCATED IN THE PYLON. SUSPECT CAUSED BY INCORRECT FITMENT OF THE UNION AND PIPE. 2 L 7 2 4F 4 F RT A2NM E12EU 2002011000073 20020110 00073 NM 2002 1 10 AUS20011177 1 20011106 A 2131 CONTROLLER BOEING 747 747400 NM CABIN PRESSURE FAILED W B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AU S (AUS) CABIN PRESSURISATION SYSTEM FAILED. AIRCRAFT MADE AND EMERGENCY DESCENT AND OVERWEIGHT LANDING. AIRCRAFT IS SINGAP ORE REGISTERED. 2 L 7 4 4F RT A20WE 2002011000075 20020110 00075 EU 2002 1 10 RAIA00112016 1 20011231 A 5270 SENSOR JETAIR JETSTM JETSTM4101 1500501 EU CARGO DOOR MALFUNCTIONED A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 558HK 41071 5562-STL- BAGGAGE BAY DOOR WARNING LIGHT ILLUMINATED ON TAKEOFF. MAINTENANCE OPENED THEN CLOSED BAGGAGE DOOR. WARNING SYSTEM OPS CHECK GOOD. 2 L 7 2 4T RT A41NM 2002011000077 20020110 00077 NM 2002 1 10 AUS20011178 1 20011106 A 2910 65B01512830 LINE BOEING 747 747338 NM RROYCE RB211 RB211524D419 54555 NE HYD SYSTEM DAMAGED W O OTHER K FLUID LOSS CL CLIMB 1 AU S (AUS) HYDRAULIC LINE DAMAGED BY CONTACT FROM THE RT WING LANDING GEAR RETRACTION ACTUATOR. LOSS OF NR 4 HYDRAULIC SYSTEM FLUID. 2 L 7 2 4F 4 F RT A20WE E12EU 2002011000082 20020110 00082 NM 2002 1 10 AUS20011190 1 20010828 A 5314 KEELBEAM BOEING 737 737376 NM CFMINT CFM56 CFM563C 13802 EU FUSELAGE CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LOWER FUSELAGE KEEL BEAM CHORDS CORRODED BEYOND LIMITS IN AREA LOCATED BETWEEN BS 663 AND BS 720. 2 L 7 2 4F 4 F RT A16WE E21EU 2002011000083 20020110 00083 2002 1 10 AUS20011193 4 20011107 A 3441 7886580011 INU BOEING 747 747SP38 1384817 NM NAV SYSTEM FAULTY W O OTHER J WARNING INDICATION CR CRUISE 1 AU S (AUS) INERTIAL NAVIGATION UNITS (INU) FAULTY. 2 L 7 4 4F RT A20WE 2002011000084 20020110 00084 2002 1 10 AUS20011200 4 20011107 A 3442 6226514410 TRANSCEIVER BOEING 747 747338 NM WX RADAR SYSTEM FAULTY W K NONE O OTHER IN INSP/MAINT 1 AU S 1466 (AUS) WEATHER RADAR TRANSCEIVER FAULTY. 2 L 7 2 4F RT A20WE 2002011000085 20020110 00085 NM 2002 1 10 AUS20011202 1 20011114 A 1100 433000120 CIRCUIT BREAKER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE AC POWER MISMARKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) REPLACEMENT CIRCUIT BREAKERS (2OFF) INCORRECTLY LABELED. IF THE CIRCUIT BREAKERS HAD BEEN WIRED ACCORDING TO THE L ABELING, THE PHASES WOULD BE REVERSED CAUSING MOTORS TO RUN IN THE INCORRECT DIRECTION. FOUND DURING IMPLEMENTATION OF S B 8-29-27. PERSONNEL/MAINTENANCE ERROR. MANUFACTURING ERROR. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011000086 20020110 00086 NM 2002 1 10 AUS20011203 1 20011114 A 2497 WIRE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE ELECTRICAL POWER CHAFED W K NONE O OTHER IN INSP/MAINT 1 AU S 20931 (AUS) NUMEROUS AREAS OF CHAFING WIRE. WIRE IS CHAFING IN AREAS WHERE THE WIRE RUNS THROUGH METAL CONDUITS IN THE WINGS A ND TAIL SECTIONS. WIRING IN THE LT AND RT AC CONTACTOR BOXES ALSO CHAFING. CHAFED WIRING WAS FOUND TO BE THE CAUSE OF NU MEROUS SYSTEM FAILURES AND PROBLEMS. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011000088 20020110 00088 NM 2002 1 10 AUS20011209 1 20011114 A 7110 LJ17001 PANEL BOEING 747 747438 NM RROYCE RB211 RB211524* NE ENGINE COWLING MISSING W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NR 1 ENGINE MANUAL STARTER ACCESS PANEL MISSING. TRANSLATING SLEEVE CONTAINED A 63.5MM BY 38.1MM (2.5IN BY 1.5IN) HOLE. 2 L 7 4 4F 4 F RT A20WE E12EU 2002011000089 20020110 00089 NM 2002 1 10 AUS20011211 1 20011105 A 5513 106054593A BEARING BOEING 737 737376 NM CFMINT CFM56 CFM563C 13802 EU HORIZONTAL STAB CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT HORIZONTAL STABILISER HINGE BEARING CORRODED IN BEARING BORE CAUSING CHAFING ON THE HINGE PLATE. 2 L 7 2 4F 4 F RT A16WE E21EU 2002011000094 20020110 00094 2002 1 10 AUS20011217 4 20011113 A 2211 37571981 COMPUTER BOEING 747 747SP38 1384817 NM RROYCE RB211 RB211524D419 54555 NE AUTOPILOT FAILED W O OTHER F FLT CONT AFFECTED CR CRUISE 1 AU S (AUS) UPPER YAW DAMPER COMPUTER FAULTY. 2 L 7 4 4F 4 F RT A20WE E12EU 2002011000096 20020110 00096 WP 2002 1 10 AUS20011218 2 20011011 A 7250 31081642 TURBINE BLADES SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP ROTOL R321 R321482F8 GL LT ENGINE FAILED W O OTHER E R J VIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION DE DESCENT 1 AU S (AUS) LT ENGINE FIRST STAGE TURBINE BLADE FAILED. EXTENSIVE SECONDARY DAMAGE TO HOT SECTION COMPONENTS. SOME DAMAGE TO C OMPRESSOR SECTION DUE TO IMBALANCE OF THE ROTATING COMPONENTS. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P61GL 2002011000104 20020110 00104 WP 2002 1 10 GTIA011187 1 20011109 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FORWARD ENTRY AREA, CHANNEL SUPPORT CORRODED AT STATION Y=160 FROM X40 TO X20, BETWEEN FLOOR SUPPORT AND UPPER CHA NNEL. REMOVED CHANNEL SUPPORT. INSTALLED NEW CHANNEL SUPPORT IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002011000105 20020110 00105 WP 2002 1 10 GTIA012062 1 20011026 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FOUND DENT LEFT FUSELAGE STATION 323 BETWEEN LONGERON 23 AND 24. LOCATED AND DRILLED DOUBLER. INSTALLED DOUBLER IAW MD80 SRM 53-04. (M) 2 L 7 2 4F A6WE 2002011000106 20020110 00106 WP 2002 1 10 GTIA012063 1 20011103 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT STATION Y=164, X42. REMOVED FLOOR SUPPORT FITTING. BACK DRILLED NE W BRACKET. INSTALL NEW BRACKET IAW MD80 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 2002011000107 20020110 00107 WP 2002 1 10 GTIA012064 1 20011102 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CHAFED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FOUND LEFT OUTBOARD SEAT TRACK STATION 815 TO 806 CHAFING. UPON REMOVAL OF LEFT FLOOR PANEL STATION 779-826 FOUND CRACK IN LOWER WEB. CUT OUT DAMAGED SEAT TRACK STATION 760-840. FORMED REPAIR DOUBLER. APPLIED AND INSTALLED DOUBLER REPAIR. INSTALLED SEAT TRACK AND SPLICE STATION 760-840 IAW MD80 SRM 53-05. (M) 2 L 7 2 4F A6WE 2002011000108 20020110 00108 WP 2002 1 10 GTIA012065 1 20011113 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FOUND WEB CRACKED AT STA Y=1127 LONGERON 13L, L-2 DOOR WEB JAMB AREA. LOCATE AND DRILL WEB DOUBLER REPAIR. INSTA LLED GUSSETS AND WEB REPAIR DOUBLER AT LONGERONS 12 AND 13 IAW MD80 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 2002011000109 20020110 00109 WP 2002 1 10 GTIA012066 1 20011105 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - PAX CABIN FLOOR SUPPORT CORRODED AT STA Y=200 -X47 TO -X57, LOWER SURFACE. FABRICATED NEW PART. INSTALLED NEW PA RT IAW MD80 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 2002011000110 20020110 00110 WP 2002 1 10 GTIA012067 1 20011102 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FLOOR SUPPORT CORRODED AT STATION Y 193, -X53 INCHES FORWARD ENTRY AREA. REMOVED CORROSION AT FLOOR SUPPORT. FOU ND MATERIAL WITHIN LIMITS. FOUND WEB FLOOR PANEL CRACKED AND CORRODED. FORMED NEW WEB FLOOR. INSTALLED NEW WEB FLOOR IAW IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002011000111 20020110 00111 WP 2002 1 10 GTIA012068 1 20011102 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FOUND SUPPORT CORRODED AT STATION Y=173, -X54 INCHES FORWARD ENTRY AREA. FABRICATED SUPPORT. INSTALLED FLOOR SUP PORT IAW MD80 SRM 51-30-1. (M) 2 L 7 2 4F A6WE 2002011000112 20020110 00112 WP 2002 1 10 GTIA012069 1 20011031 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FOUND EXTERNAL DOUBLER AT LEFT AFT NOSE GEAR DOOR HINGE CUT OUT. THIS DOUBLER MUST BE REPLACED WITH DOUBLER REPAI R GIVEN IN SRM 53-05. REMOVED OLD DOUBLER REPAIR. FORMED DOUBLER REPAIR. INSTALLED DOUBLER REPAIR IAW MD80 SRM 53-05. (M) 2 L 7 2 4F A6WE 2002011000113 20020110 00113 WP 2002 1 10 GTIA012070 1 20011112 A 5320 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FOUND DENT AT FS 408 BETWEEN L28L AND L29L IS BEYOND ALLOWABLE LIMITS. FABRICATE DOUBLER. INSTALLED DOUBLER IAW DC9 SRM 53-04. (M) 2 L 7 2 4F A6WE 2002011000114 20020110 00114 NE 2002 1 10 HALA0100292 2 20011211 A 7321 5996205 FCU DOUG DC10 DC1010 3022110 WP GE CF6 CF66K 30020 NE NR 3 ENGINE MALFUNCTIONED A HALA O OTHER X ENGINE FLAMEOUT AP APPROACH 1 WP 13 128AA 46984 FLT 481 - PPT - NR 3 ENGINE FLAMED OUT ON APPROACH. ENGINE HAD BEEN AT IDLE POWER 5 MINUTES. REMOVED AND REPLACED FUEL CONTROL. OPS AND LEAK CHECK GOOD. (M) 2 L 7 3 4F 4 F A22WE E23EA 2002011000115 20020110 00115 SO 2002 1 10 SIMA200133204 1 20011126 A 5320 BEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 145234 ABI - THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM CARD NR 27707. GALLEY CENTER BEAM CORRODED AT FRAME 20. CEN TER BEAM AT FRAME REPAIRED IAW EMB GST-3729/01. (M) 2 L 7 2 4T RT T00011AT 2002011000116 20020110 00116 SO 2002 1 10 SIMA200133602 1 20011202 A 3350 20131A POWER SUPPLY EMB 135 EMB135LR 3260305 SO CABIN DISCHARGED A SIMA K NONE L NO TEST NR NOT REPORTED 1 SW 21 704PG 145174 LGA - FLT 4454 - CREW REPORTED THE FORWARD CABIN EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED T HE NR 2 BATTERY POWER SUPPLY IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT TOOO11AT 2002011000117 20020110 00117 SO 2002 1 10 SIMA200134101 1 20011206 A 5320 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 600BK 145044 THIS IS LEVEL 2 FINDING ON A CORROSION REPAIR ITEM CARD NR 27730. CENTER GUSSET IN LAV AREA HAS CORROSION. BLENDED COR ROSION IAW EMB 145 SRM 51-10-02. REPAIRED IAW EMB GST-3846/01. (M) 2 L 7 2 4T RT T00011AT 2002011000118 20020110 00118 SO 2002 1 10 SIMA200134102 1 20011206 A 5320 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 600BK 145044 THIS IS LEVEL 2 FINDING ON A CORROSION REPAIR ITEM CARD NR 27731. RIGHT AFT FLOOR SUPPORT IN CARGO HAS CORROSION. BLEN DED CORROSION IAW EMB145 SRM 51-10-02. REPAIRED IAW EMB GST-3846/01. (M) 2 L 7 2 4T RT T00011AT 2002011000119 20020110 00119 SO 2002 1 10 SIMA200134103 1 20011206 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 600BK 145044 ABI - THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM CARD NR 27731. CARGO DOOR SILL HAS CORROSION. BLENDED CORRO SION IAW EMB SRM 51-10-01. REPAIRED IAW EMB GST 3846/01. (M) 2 L 7 2 4T RT T00011AT 2002011000120 20020110 00120 SO 2002 1 10 SIMA200134104 1 20011206 A 5320 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 600BK 145044 ABI - THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. LEFT CENTER CARGO GUSSET HAS CORROSION. BLENDED CORROSION IAW EMB 145 SRM 51-10-02. REPAIRED CORROSION IAW EMB GST-3846/01. (M) 2 L 7 2 4T RT T00011AT 2002011000121 20020110 00121 SO 2002 1 10 SIMA200134105 1 20011206 A 5320 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 600BK 145044 THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. RIGHT GUSSET IN LAVATORY AREA HAS CORROSION. BLENDED CORROSION I AW EMB 145 SRM 51-10-02. REPAIRED IAW EMB GST-3846/01. (M) 2 L 7 2 4T RT T00011AT 2002011000122 20020110 00122 SO 2002 1 10 SIMA200134106 1 20011206 A 5320 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 600BK 145044 ABI - THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. LEFT FLOOR SUPPORT IN LAVATORY AREA HAS CORROSION. BLENDED CORROSION IAW EMB 145 SRM 51-10-02. REPAIRED CORROSION IAW EMBRAER GST 3846/01. (M) 2 L 7 2 4T RT T00011AT 2002011000123 20020110 00123 SO 2002 1 10 SIMA200134201 1 20011207 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 600BK 145044 ABI - DURING AN IMBV INSPECTION, FOUND CORROSION ON THE SERVICE DOOR CENTER SILL. REMOVED CORROSION BY BLENDING. PERFO RMED AND NDT INSPECTION OF THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED REPAIR DOUBLERS. REPAIR DONE IAW EMB GS T-3851/01, ITEM 4 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002011000124 20020110 00124 SO 2002 1 10 SIMA200134202 1 20011207 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 600BK 145044 ABI - DURING AN IMBV, FOUND CORROSION ON THE LEFT OMEGA BEAM AT FRAME 20. REMOVED CORROSION BY CUT OUT. FABRICATED A D OUBLER ANGLE, FILLER, PLATE, AND SHIMS. REPAIR DONE IAW EMB145 (SRM145/1142 CHAPTER 53 REV 16) 53-21-10 AND STANDARD SR M PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002011000125 20020110 00125 SO 2002 1 10 SIMA200134203 1 20011207 A 5311 FRAME EMB 145 EMB145 3260210 SO FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 606AE 145062 ABI - DURING AN IMBV, FOUND A HOLE IN FRAME 23 FLANGE AT STRINGER 17R. REAMED HOLE TO .193 INCH. PARTIALLY COUNTERSUNK AND DEBURRED. PERFORMED ET INSPECTION OF THE HOLE WITH NO REJECTABLE INDICATIONS. WORK DONE IAW EMB GST-3894/01 AND S TANDARD SRM PRATICES. (M) 2 L 7 2 4F RT T00011AT 2002011000126 20020110 00126 SO 2002 1 10 SIMA200134501 1 20011025 A 5320 14522459003 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 601GH 145046 ABI - THIS IS LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. GALLEY AREA FLOOR RAMP SUPPORT CORRODED. REMOVED CORRODED GA LLEY FLOOR RAMP SUPPORT AND INSTALLED SERVICEABLE RAMP IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002011000127 20020110 00127 SO 2002 1 10 SIMA200134502 1 20011025 A 5320 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 601GH 145046 ABI - THIS IS A LEVEL 2 FINDING ON CORROSION REPAIR ITEM. CENTER GUSSET IN GALLEY HAS CORROSION. REMOVED GUSSET AND IN STALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002011000128 20020110 00128 SO 2002 1 10 SIMA200134503 1 20011210 A 5315 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 606AE 145062 ABI - DURING AN IMBV INSPECTION OF A/C, FOUND CORROSION ON THE LEFT OMEGA BEAM AND PREVIOUS REPAIR AT FRAME 20. REMOVED PREVIOUS REPAIR AND CORROSION BY CUT OUT. FABRICATED A DOUBLER ANGLE, FILLER, PLATE AND TWO SHIMS. REPAIR DONE IAW EM B 145 9SRM145/1142 CHAPTER 53 REV 16) 53-21-01 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002011000129 20020110 00129 SO 2002 1 10 SIMA200134504 1 20011210 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 600BK 145044 ABI - DURING AN IMBV INSPECTION OF A/C, FOUND CORROSION ON THE GALLEY CENTER FLOORBEAM. REMOVED CORROSION BY BLENDING. PERFORMED AN NDT INSPECTION OF THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED A U-CHANNEL REPAIR DOUBLER. REPAIR DONE IAW EMB GST3902/01 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002011000130 20020110 00130 SO 2002 1 10 SIMA200134701 1 20011212 A 5320 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 600BK 145044 THIS IS FINDING ON A CORROSION REPAIR ITEM. LEFT FLOOR SUPPORT BETWEEN FRAMES 23 AND 26 HAS CORROSION. REPAIRED LEFT F LOOR SUPPORT IAW EMB 145 GST-3851/01. (M) 2 L 7 2 4T RT T00011AT 2002011000131 20020110 00131 SO 2002 1 10 SIMA200134702 1 20011212 A 5320 14521725615 FLOOR SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 606AE 145062 ABI - THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. GALLEY RAMP SUPPORT CORRODED. REMOVED AND INSTALLED SERVIC EABLE RAMP SUPPORT IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002011000132 20020110 00132 SO 2002 1 10 SIMA200134703 1 20011212 A 5315 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 606AE 145062 ABI - THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. GALLEY CENTER BEAM CORRODED. INSTALLED REPAIR DOUBLERS ON GALLEY CENTER BEAM ON FRAME 20-23 IAW EMB GST-3862/01. (M) 2 L 7 2 4F RT T00011AT 2002011000133 20020110 00133 SO 2002 1 10 SIMA200134704 1 20011212 A 5315 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 606AE 145062 ABI - THIS IS LEVEL 2 FINDING. FORWARD DIGITAL CORRODED. REPAIRED IAW EMB GST-3862/01. (M) 2 L 7 2 4F RT T00011AT 2002011000135 20020110 00135 SO 2002 1 10 SIMA200134705 1 20011212 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 606AE 145062 ABI - THIS IS A LEVEL 2 FINDING, CENTER BEAM GUSSET CORRODED. REMOVED AND INSTALLED SERVICEABLE CENTER BEAM GUSSET IAW EMB 145 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002011000136 20020110 00136 SO 2002 1 10 SIMA200134706 1 20011212 A 5315 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 606AE 145062 ABI - THIS IS A LEVEL 2 FINDING, GALLEY AFT DIGITAL CORRODED. REPAIRED IAW EMB GST-3862/01. (M) 2 L 7 2 4F RT T00011AT 2002011000137 20020110 00137 SO 2002 1 10 SIMA200134707 1 20011212 A 5315 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 606AE 145062 ABI - THIS IS LEVEL 2 FINDING. LEFT OMEGA AT FRAME 20 HAS CORROSION ON PREVIOUS REPAIR. REPAIRED IAW EMB145 SRM 53-21- 10. (M) 2 L 7 2 4F RT T00011AT 2002011000138 20020110 00138 SO 2002 1 10 SIMA200134708 1 20011212 A 5320 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 606AE 145062 THIS A LEVEL 2 FINDING. SERVICE DOOR SILL (FORWARD) CORRODED. INSTALLED REPAIR DOUBLER IAW EMB GST-3862/01. (M) 2 L 7 2 4F RT T00011AT 2002011000139 20020110 00139 SO 2002 1 10 SIMA200134709 1 20011212 A 5320 14522461011 GUSSET EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 606AE 145062 THIS IS A LEVEL 2 FINDING, FORWARD DIAMOND GUSSET CORRODED. REMOVED AND INSTALLED NEW DIAMOND GUSSET IAW EMB 145 SRM 5 1-40-02. (M) 2 L 7 2 4F RT T00011AT 2002011000140 20020110 00140 SO 2002 1 10 SIMA200134710 1 20011212 A 3210 14571035007 CAP EMB 145 EMB145 3260210 SO LT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 606AE 145062 THIS IS A LEVEL 2 FINDING. LEFT FORWARD MLG BEARING CAP CORRODED. REMOVED AND INSTALLED SERVICEABLE STRUT SWIVEL CAP I AW EMB 145 AMM 32-10-01-000-801-A, 32-10-01-400-801-A. (M) 2 L 7 2 4F RT T00011AT 2002011000158 20020110 00158 NM 2002 1 10 2001UALA02475 1 20011228 A 2720 WARNING SYSTEM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE COCKPIT ACTIVATED A UALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 WP 29 941UA 26676 ENCOUNTERED A RUDDER CONTROL PROBLEM EN ROUTE TO DESTINATION. LANDED UNDER ALERT. 2 L 7 2 4F 4 F RT A16WE E2GL 2002020600042 20020206 00042 NM 2002 2 6 2001UALA02476 1 20011230 A 2612 FIRE WARNING BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 2 ENGINE FALSE INDICATION A UALA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING N FALSE WARNING UK UNKNOWN 1 WP 29 778UA 26940 777019 EN ROUTE NR 2 ENG FIRE INDICATION. ENG SHUTDOWN & ACFT DIVERTED. DUMPED FUEL & LANDED UNDER AMBER ALERT. ENG INSPECTE D FOR EVIDENCE OF FIRE & OVERHEAT CONDITIONS, NONE FOUND. FIRE WARN SYS TEST PASSED. NO MX MESSAGE FAULTS RECORDED. T HE HIGH POWER ENG RUN AT BGR & SUBSEQUENT FERRY FLIGHT BACK TO ORD, DID NOT DUPLICATE THE FIRE INDICATION. THE ITEMS RE MOVED AS PRECAUTIONARY: FODC CARD, DUCT VENT VALVE (ALTHOUGH, GASKET WAS FOUND DAMAGED), & UPPER FIRE LOOP HAVE ALL CHE CKED OK PER SHOP. THE A/C WAS INSPECTED FOR FIRE WARNING WIRE INTERFERENCE DESCRIBED ON 777-SL-24-032. THE A/C CHECKED OUT CLEAN. QAR & FDR INFORMATION HAS BEEN COMPILED & WILL BE FWD'D TO BOEING FOR ANALYSIS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002020600043 20020206 00043 NM 2002 2 6 2001UALA02477 1 20011229 A 3350 8100033901 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST UK UNKNOWN 1 WP 29 785UA 26954 EMERGENCY PROX LIGHT AT SEAT 42D IS INOP. BULB IN FLOOR PROXIMITY LIGHT ASSY FAILED. REPLACED FLOOR PROXIMITY LIGHT AS SY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002011000159 20020110 00159 NM 2002 1 10 2001UALA02479 1 20011229 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 STATION 178 BULKHEAD WEB HAS CRACK AT LBL 5.7 SECOND FASTENER OUTBOARD AT WL 234. MAJOR REPAIR ACCOMPLISHED. CUT OUT D AMAGED AREA. FABRICATED AND INSTALLED DOUBLER AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002011000160 20020110 00160 NM 2002 1 10 2001UALA02480 1 20011229 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 STATION 178 BULKHEAD HAS CRACK AT RBL 5.7 INBOARD SIDE AT WL 202. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002011000161 20020110 00161 NM 2002 1 10 2001UALA02481 1 20011231 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 925UA 26646 FUSELAGE SKIN AND STRINGER DENTED AT STATION 479, STRINGER 5L. MAJOR REPAIR ACCOMPLISHED. FUSELAGE DOUBLER INSTALLED A ND STRINGER REPAIRED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002011000163 20020110 00163 NM 2002 1 10 2001UALA02484 1 20011230 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 338UA 24242 FLOORBEAM AT BODY STATION 294.5, REPAIR PLATE ON CAP BETWEEN RBL 28 AND RBL 44, UPPER SURFACE IS CORRODED. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED SPLICE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002011000165 20020110 00165 NM 2002 1 10 2001UALA02487 1 20011231 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 338UA 24242 FUSELAGE SKIN DENTED AT STATION 1005 AFT OF DOOR 2L BETWEEN STRINGER 12L AND 13L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002011000166 20020110 00166 NE 2002 1 10 AUS20011020 2 20010924 A 7321 1853M33P03 EEC BOEING 737 737* NM CFMINT CFM567 CFM567B22 13802 NE ENGINE FAULTY W O OTHER E VIBRATION/BUFFET TO TAKEOFF 1 AU S (AUS) NR 1 ENGINE ELECTRONIC ENGINE CONTROL (EEC) FAULTY. 2 L 7 2 4F 4 F RT A16WE E00055EN 2002011000168 20020110 00168 NM 2002 1 10 2001UALA02489 1 20011230 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 AFT PIT FUSELAGE FRAME HAS DENT STATION 1480 STRINGER 26L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER ON INNER FLANG E. 2 L 7 2 4F 4 F RT A2NM E17NE 2002011000174 20020110 00174 NM 2002 1 10 2001UALA02495 1 20011231 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 STATION 1640 CABIN FLOORBEAM HAS EXCESSIVE MATERIAL LOSS AT RBL 34-50. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED T-CAP R EPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002011000176 20020110 00176 NM 2002 1 10 DL72E011957 1 20011214 A 3610 BACC10DU500AB CLAMP BOEING 727 727247 138408F NM CARGO BAY BROKEN A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 2829W 21481 A/C PERFORMED AIR TURNBACK DUE TO AFT CARGO DETECTION OVERHEAT/FIRE. REPLACED BROKEN CLAMP ON PNEUMATIC DUCT IN AFT BAG BIN. 2 L 7 3 4F A3WE 2002011000180 20020110 00180 NM 2002 1 10 DL72L011979 1 20011225 A 5553 65168721 HINGE FITTING BOEING 727 727232 1384082 NM VERTICAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 509DA 21311 CORROSION WAS FOUND IN THE BORES AND SPOT FACES OF THE VERTICAL STABILIZER HINGE SUPPORT FITTINGS ON THE LT & RT SIDE OF THE STABILIZER. THE CORROSION WAS REMOVED BY OVER SIZING THE BORES AND MACHINING THE SPOT FACES. OVERSIZE REPAIR BUSH INGS WERE INSTALLED TO RESTORE THE LUGS. THE REPAIR WAS ACCOMPLISHED PER ER/A 382340-14, REV A. 2 L 7 3 4F A3WE 2002011000181 20020110 00181 NM 2002 1 10 DL72L011980 1 20011225 A 5510 65434397 HINGE FITTING BOEING 727 727232 1384082 NM HORIZ STAB WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 509DA 21311 THE FACE OF THE INBOARD LUG ON THE LBL 10 HORIZONTAL STABILIZER REAR SPAR HINGE FITTING WAS FOUND WORN. THE FACE WAS SP OTFACED TO REMOVE ALL DAMAGE AND PROVIDE A FLAT SURFACE. AN OVERSIZED FLANGED BUSHING WAS INSTALLED TO RESTORE THE AREA . THE REPAIR WAS ACCOMPLISHED PER ER/A 382339-14, REV A. 2 L 7 3 4F A3WE 2002011000182 20020110 00182 NM 2002 1 10 DL72S011941 1 20011215 A 3350 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 523DA 21583 L2 DOOR EMERGENCY EXIT OVERHEAD LIGHT BATTERIES DEAD. REPLACED BATTERIES. 2 L 7 3 4F A3WE 2002011000183 20020110 00183 NM 2002 1 10 DL72S011952 1 20011214 A 5712 RIB BOEING 727 727225A 1384077 NM RT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 INSPECTIONS OF THE UPPER RIB CHORD ON THE RT WING AT RBL 70.5 PER BAC S/B 727-57-0112 AND AD 94-07-08 REVEALED A CRACK I N A FASTENER HOLE AT FS 760.95. THE HOLE WAS OVERSIZED TO REMOVE THE CRACK AND THEN COLD WORKED. THE HOLE WAS BUSHED A ND THE CHORD REINFORCED WITH AN ALUMINUM ANGLE PER THE BAC S/B AND PER ER/A 382192-14AD, REV A. 2 L 7 3 4F RT A3WE 2002011000184 20020110 00184 NM 2002 1 10 DL72S011954 1 20011218 A 5311 65175061 FRAME BOEING 727 727232 1384082 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 515DA 21431 THE FS 1303 FRAME INNER CHORD WAS FOUND WITH FLANGE DAMAGE FROM A HYDRAULIC CLAMP ATTACH POINT 6 INCHES ABOVE THE RT VEN TRAL STAIRWELL TORQUE BOX STRUCTURE. THE DAMAGE SECTION OF FLANGE WAS TRIMMED OUT AND REPAIRED WITH AN ALUMINUM REPAIR ANGLE PER ER/A 382311-14, REV A. 2 L 7 3 4F A3WE 2002011000185 20020110 00185 2002 1 10 DL72S011974 4 20011223 A 3442 TRANSCEIVER BOEING 727 727225A 1384077 NM WX RADAR FAULTY A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 8890Z 21859 RADAR INOP. REPLACED TRANSCEIVER AND NR 2 VG CHECKS GOOD. 2 L 7 3 4F RT A3WE 2002011000186 20020110 00186 NM 2002 1 10 DL72S011975 1 20011223 A 3397 WIRE BOEING 727 727232 1384082 NM CABIN SHORTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 520DA 21471 FLOOR MOUNTED EMERGENCY LIGHT INOP IN FIRST CLASS. FOUND WIRE W1026-9006 SHORTED TO GROUND BETWEEN C/P D9059P AND DISCO NNECT D9062. REPLACED WIRE. REPLACED POWER SUPPLY M9026 AND BATTERY PACK. SYSTEM TESTS GOOD. 2 L 7 3 4F A3WE 2002011000187 20020110 00187 NM 2002 1 10 P5CA0200623 1 20011229 A 7930 21SN04149 SWITCH BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE #3 ENGINE MALFUNCTIONED A P5CA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 23 920FT 22237 702114 #3 ENGINE OIL PRESSURE LITE ON PILOT'S FWD ANNUNCIATOR PANEL ILLUMINATED. ALT PROCEDURES CHECK LIST ACCOMPLISHED - OIL P RESS, QUANTITY NORMAL - FILTER BYPASS LIGHT EXTINGUISHED. REMOVED & REPLACED LOW OIL PRESS SWITCH PER MM 79-33-01. PER FORMED WINDMILL INSPECTION PER 72-00-00. OIL STRAINED & CHIPS CLEANED . REINSTALLED. LEAK CHECK GOOD. OK FOR SERVICE. 2 L 7 4 4F 4 F A20WE E3NE 2002011000188 20020110 00188 NM 2002 1 10 AWXA200200012 1 20011228 A 5330 654688268 SKIN BOEING 737 7373S3 1384711 NM CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 MCN - MAJOR REPAIR - "C" - DURING C-15 CHECK MAINTENANCE FOUND FUSELAGE SKIN CHAFED BELOW R/H HORIZONTAL STABILIZER APPR OXIMATELY 50" AFT OF STABILIZER LEADING EDGE BS 1133. MAINTENANCE BLENDED CHAFED AREA OF SKIN AND PERFORMED MATERIAL THI CKNESS MEASUREMENT FINDING MATERIAL LOSS OUT OF LIMITS PER B737-300 SRM 53-00-01, PG 101-109. REMOVED 14 RIVITS AND CUTO UT DAMAGED AREA OF SKIN, FABRICATED FILLER AND DOUBLER AND INSTALLED REPAIR IAW B737-300 SRM 51-40-02, PG 201-203. 2 L 7 2 4F RT A16WE 2002011000190 20020110 00190 NM 2002 1 10 AWXA200200016 1 20011228 A 5315 65465391 FRAME BOEING 737 7373S3 1384711 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 MCN - MAJOR REPAIR - "C" - DURING C-15 CHECK MAINTENANCE DISCOVERED CRACKED FRAME AT FASTENER BS 616, LBL 64. MAINTENANC E CUTOUT DAMAGED AREA OF FRAME, DAMAGED AREA WITHIN REPAIRABLE LIMITS IAW AWA ER 03-5311-01143-DD1. HFEC INSPECTION COMP LIED WITH TO VERIFY CRACK CONTAINED, REPAIR STIFFNER AND FILLER WAS FABRICATED AND INSTALLED IAW AWA ER 03-5311-01143-DD 1. 2 L 7 2 4F RT A16WE 2002011100013 20020111 00013 WP 2002 1 11 0105129618 1 20011226 A 2910 HYDRAULIC LINE DOUG DC9 DC932 3022066 WP AUX HYD PUMP RUPTURED A NWAA K NONE K S FLUID LOSS AFFECT SYSTEMS AP APPROACH 1 GL 01 618NW 47433 DURING APPROACH TO LANDING, THE CREW NOTICED LOSS OF RIGHT HYDRAULIC SYSTEM FLUID AND LOW PRESSURE. COMPLIED WITH COM PR OCEDURE AND AIRCRAFT LANDED SAFELY. MAINTENANCE FOUND THE PRESSURE LINE FROM THE AUXILIARY PUMP RUPTURED. REPLACED THE L INE, BOTH THE RIGHT AND AUXILIARY HYDRAULIC PUMPS, ALL RIGHT HYDRAULIC SYSTEM FILTERS, AND BOTH MAIN LANDING GEAR DOOR S KID PLATES. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002011100014 20020111 00014 EA 2002 1 11 COMA0260039 1 20011217 A 3240 50105842 WHEEL CNDAIR CL600 CL6002B19 1900309 EA MAIN WHEEL I/B S CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 729CA 6862 239 7265 VISUAL INSPECTED WHEEL ASSY FOR LEAKAGE AND FOUND I/B SUBASSEMBLY CRACKED AT BOTTOM OF DISK KEY BOSS. 2 L 7 2 4F RT A21EA 2002011100017 20020111 00017 NM 2002 1 11 SABA011073 1 20011215 A 3350 OL3071BPEGPL LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 813SN 032 FLIGHT 5057 FROM TLH TO CLT, DURING PREFLIGHT THE PILOT FOUND THE WHITE FLOOR EMERGENCY LIGHT STRIP INOP. FLIGHT WAS CAN CELED. LIGHTS WERE DEFERRED TO MSL. FERRY FLIGHT WAS ISSUED 3 9475. AIRCRAFT ARRIVED IN CHARLOTTE WITH NO OTHER PROBLEMS . MAINTENANCE REMOVED AND REPLACED BULBS, SYSTEM OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002011100023 20020111 00023 EU 2002 1 11 SABA011074 1 20011217 A 5610 1379510C1 SEAL BAG JETSTM JETSTM3201 1500217 EU A SABA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 33 962AE 962 Flight 5165 from CLT to HTS, During climb-out pilots DV window seal came off. Aircraft returned to Charlotte with no oth er problem. No emergency was declared. Maintenance removed and replaced the seal. System checked good and aircraft was r eturned to service. 2 L 7 2 4T RT A56EU 2002011300002 20020113 00002 SO 2002 1 13 RAIA00201005 1 20010107 A 2730 0861DT5 VANE EMB 145 EMB145 3260210 SO MALFUNCTIONED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 801HK 21 145053 5324-PIT-DURING TAXI GOT WARNING MESSAGE THAT #2 STALL PROTECTION WAS INOP. MAINTENANCE REMOVED AND REPLACED #2 ANGLE OF ATTACK VANE. SYSTEM OPS CK OK. 2 L 7 2 4F RT T00011AT 2002011300003 20020113 00003 SO 2002 1 13 RAIA00201006 1 20010107 A 2730 0020BN4 COMPUTER EMB 145 EMB145 3260210 SO MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 801HK 1057 1006 145053 5324-PIT- DURING TAXI GOT WARNING MESSAGE THAT #2 STALL PROTECTION SYSTEM WAS INOP. MAINTENANCE REMOVED AND REPLACED THE STALL PROTECTION COMPUTER. SYSTEM OPS CK OK. 2 L 7 2 4F RT T00011AT 2002011300004 20020113 00004 SO 2002 1 13 RAIA00201008 1 20010108 A 2730 0861DT5 VANE EMB 145 EMB145 3260210 SO MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 801HK 2962 1 136 145053 5282-PIT- DURING TAXI #2 STALL PROTECTION SYSTEM INOP. MAINTENANCE REMOVED AND REPLACED THE #2 AOA VANE AND THE SPS COMP UTER 2 L 7 2 4F RT T00011AT 2002011400001 20020114 00001 SO 2002 1 14 C2XA02IA004 1 20011228 A 5101 14529150001 FLOOR SUPPORT EMB 145 EMB145 3260210 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13964 7209 145123 IAH- DURING "C" CHECK IT WAS NOTED THAT THE FLOOR BEAM CROSS STRUCTURE ABOVE FUSELAGE FRAME 23 WAS CORRODED AT THE INBO ARD FORWARD CORNER. IAH- MAINTENANCE REMOVED THE DAMAGED AREA,AND, INSTALLED A DOUBLER WITH A FILLER,AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE WHEN RELEASED FROM "C" CHECK. 2 L 7 2 4F RT T00011AT 2002011400006 20020114 00006 NM 2002 1 14 AUS20011130 1 20011024 A 3234 122SM44T2 SWITCH BOEING 737 7378Q8 13844BX NM CFMINT CFM56 CFM565A1 NE MLG STUCK W O OTHER N FALSE WARNING LD LANDING 1 AU S (AUS) LANDING GEAR POSITION SWITCH SUSPECT STICKING. 2 L 7 2 4F 4 F RT A16WE E29NE 2002011400009 20020114 00009 EU 2002 1 14 AUS20011231 2 20011122 A 7310 3352526050 LINE BOEING 737 737376 NM CFMINT CFM56 CFM563C 13802 EU ENGINE FUEL MISINSTALLED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 AU S (AUS) NR 1 ENGINE TCC LINE INCORRECTLY INSTALLED. LINE HAD CHAFED ON THE FUEL SUPPLY LINE AND THE VSV ACTUATOR LINE. 2 L 7 2 4F 4 F RT A16WE E21EU 2002011400010 20020114 00010 NM 2002 1 14 AUS20011232 1 20011115 A 2121 732591C COOLING FAN BOEING 747 747438 NM RROYCE RB211 RB211524G19 NE AIR DISTRIBUTION FAULTY W O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 AU S 2091 (AUS) NR 2 UPPER DECK RECIRCULATION FAN FAULTY. 2 L 7 4 4F 4 F RT A20WE E30NE 2002011400011 20020114 00011 NM 2002 1 14 AUS20011234 1 20011120 A 5280 113T820148SP DOOR BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL MLG SEPARATED W O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 AU S (AUS) RT MAIN LANDING GEAR OLEO DOOR PANEL AND TRUNNION PANEL SEPARATED IN FLIGHT. MINOR DAMAGE TO WING TRAILING EDGE. 2 L 7 2 4F 4 F RT A1NM E23EA 2002011400012 20020114 00012 NM 2002 1 14 AUS20011236 1 20011122 A 2120 ODOR BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL COCKPIT DETECTED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AU S (AUS) STRONG CHLORINE SMELL IN COCKPIT. POTABLE WATER TANK DRAINED AND REFILLED. HUMIDIFIER LINE PURGED. 2 L 7 2 4F 4 F RT A1NM E23EA 2002011400015 20020114 00015 NM 2002 1 14 AUS20011240 1 20011124 A 5753 FITTING BOEING 767 767338 1385151 NM RROYCE RB211 RB211524* NE TE FLAP CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) OUTBOARD TRAILING EDGE FLAP DEFLECTION CONTROL FITTING ON THE REAR SPAR CRACKED AND BROKEN ALLOWING THE TRACK TO M OVE AND CAUSE CRACKING OF THE UPPER TRAILING EDGE FIXED PANEL. 2 L 7 2 4F 4 F RT A1NM E12EU 2002011400016 20020114 00016 EU 2002 1 14 AUS20011249 1 20011015 A 2730 40BC CABLE BAC 146 146100A 1500260 EU LYC ALF502 ALF502R5 41580 NE ELEVATOR CONTROL CHAFED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT ELEVATOR CABLE RUBBING ON STRUCTURE AT LIGHTENING HOLE LOCATED BELOW THE CABLE TENSION REGULATOR AT THE TOP OF THE VERTICAL STABILISER AT STA 565.15. 2 H 7 4 4F 4 F RT A49EU E6NE 2002011400028 20020114 00028 NM 2002 1 14 AUS20011269 1 20011126 A 4920 737M495030101 APU BOEING 737 737476 NM CFMINT CFM56 CFM563C 13802 EU APU BAY FAULTY W O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 AU S P134 (AUS) APU FAULTY. LIMITED INFORMATION PROVIDED. 2 L 7 2 4F 4 F RT A16WE E21EU 2002011400029 20020114 00029 EU 2002 1 14 AUS20011270 1 20011128 A 3240 SHUTTLE VALVE BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE MLG BRAKE SYSTEM FAULTY W O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 AU S (AUS) HYDRAULIC FLUID TRANSFERRED FROM GREEN HYDRAULIC SYSTEM TO YELLOW HYDRAULIC SYSTEM. INVESTIGATION FOUND THAT THE M AIN WHEEL BRAKE SHUTTLE VALVES WERE THE CAUSE OF THE PROBLEM. 2 H 7 4 4F 4 F A49EU E6NE 2002011400031 20020114 00031 NM 2002 1 14 AUS20011274 1 20011129 A 2197 WIRE BOEING 747 747438 NM RROYCE RB211 RB211524G19 NE AIR CONDITIONING BURNED W O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 AU S (AUS) WIRING BURNED AT DP40297D IN AREA APPROXIMATELY 304.8MM (12IN) FROM THE CONNECTOR LOCATED BELOW THE MAIN WIRE HARN ESS, AT THE FORWARD END OF THE FORWARD CARGO COMPARTMENT. 2 L 7 4 4F 4 F RT A20WE E30NE 2002011400032 20020114 00032 NM 2002 1 14 AUS20011275 1 20011129 A 5753 113T83331 FLAP TRACK BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL TE FLAPS CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LT WING OUTBOARD TRAILING EDGE FLAP OUTBOARD END DEFLECTION CONTROL TRACK ASSEMBLY CRACKED THROUGH APPROXIMATELY 3 0 PERCENT OF THE CROSS SECTION. THE CRACK IS LOCATED APPROXIMATELY 304.8MM (12IN) FROM THE FORWARD END AND JUST AFT OF T HE LINK ASSEMBLY LUG. 2 L 7 2 4F 4 F RT A1NM E23EA 2002011400033 20020114 00033 NM 2002 1 14 AUS20011276 1 20011202 A 2130 CONTROLLER BOEING 737 73733A 1384673 NM CFMINT CFM56 CFM563B1US GL CABIN PRESSURE CONTAMINATED W A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CR CRUISE 1 AU S (AUS) PRESSURISATION SYSTEM FAULTY. PASSENGER OXYGEN MASKS DEPLOYED. INVESTIGATION FOUND EVIDENCE OF WATER/COFFEE CONT AMINATION OF THE FORWARD E&E BAY. CONTAMINATION WAS DUE TO REMOVAL OF THE AIRSTAIRS AND DRIP TRAY LOCATED ABOVE THE E&E BAY. SERVICE BULLETIN SB 737-25-1317 THEN CALLS FOR THE INSTALLATION OF A WATER SHIELD AND MOISTURE SHROUDS. THE SB WAS NEVER CARRIED OUT. PERSONNEL/MAINTENANCE ERROR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002011400038 20020114 00038 NM 2002 1 14 AUS20011285 1 20011113 A 5754 114T10518A SKIN BOEING 767 767238 1385114 NM PWA JT9 JT9D7R4E 52054 NE LE SLAT DEBONDED W K NONE O OTHER IN INSP/MAINT 1 AU S 00201 (AUS) NR 8 RT LEADING EDGE SLAT DISBONDED. FOUND DURING INSPECTION IAW AD/B767/73. 2 L 7 2 4F 4 F RT A1NM E3NE 2002011400039 20020114 00039 NM 2002 1 14 AUS20011286 1 20011203 A 7830 32785002 FLEX COUPLING BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL THRUST REVERSER SHEARED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT ENGINE LT THRUST REVERSER HALF ELECTRO-MECHANICAL BRAKE FLEXIBLE DRIVE CABLE ASSEMBLY INNER SHAFT SHEARED IN THE AREA OF THE BASE OF THE SQUARE DRIVE. FOUND DURING INSPECTION IAW QANTAS SPECIAL INSTRUCTION 195506 WHICH REFERS TO AD/B767/88. 2 L 7 2 4F 4 F RT A1NM E23EA 2002011400040 20020114 00040 NM 2002 1 14 AUS20011287 1 20011127 A 2497 WIRE HARNESS BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL ELECTRICAL POWER CHAFED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) WIRING HARNESS CONTAINED CHAFED AND BROKEN WIRES. HARNESS IS LOCATED ADJACENT TO THE CHILLER IN THE RT MEC. 2 L 7 2 4F 4 F RT A1NM E23EA 2002011400041 20020114 00041 EU 2002 1 14 AUS20011289 1 20011205 A 3230 200885006 PLATE BAC 146 146100A 1500260 EU LYC ALF502 ALF502R5 41580 NE RT MLG UPLOCK OUT OF ADJUST W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 AU S (AUS) RT MAIN LANDING GEAR AND LANDING GEAR DOOR UPLOCK STRIKER PLATES OUT OF ADJUSTMENT. 2 H 7 4 4F 4 F RT A49EU E6NE 2002011400042 20020114 00042 NM 2002 1 14 AUS20011290 1 20011205 A 3244 161U00011 TIRE BOEING 747 747438 NM RROYCE RB211 RB211524G19 NE NR 4 REAR FAILED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 AU S (AUS) NR 4 REAR TIRE TREAD SEPARATED. DAMAGE TO COMPOSITE FAIRINGS. 2 L 7 4 4F 4 F RT A20WE E30NE 2002011400043 20020114 00043 NM 2002 1 14 AUS20011291 1 20011207 A 5755 65B023001 STRUCTURE BOEING 747 747* NM RROYCE RB211 RB211524* NE LT NR 5 SPOILER DELAMINATED W O OTHER O OTHER NR NOT REPORTED 1 AU S (AUS) LT NR 5 SPOILER LOWER SURFACE DELAMINATED AND INBOARD EDGE CRACKED. 2 L 7 4 4F 4 F RT A20WE E12EU 2002011400044 20020114 00044 EU 2002 1 14 AUS20011292 1 20011130 A 6210 332A11002407 BLADE SNIAS AS332 AS332L 8680809 EU TMECA MAKILA MAKILA1A 60040 EU MAIN ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S 6330 (AUS) BLUE MAIN ROTOR BLADE CRACKED AT THE ROOT END TRAILING EDGE. 2 G 7 2 4U 4 U H4EU E12NE 2002011400046 20020114 00046 EU 2002 1 14 AUS20011295 1 20011210 A 3260 200671002 WARNING SYSTEM BAC 146 146100A 1500260 EU LYC ALF502 ALF502R5 41580 NE RT MLG FALSE ACTIVATION W O OTHER N FALSE WARNING CR CRUISE 1 AU S 5676 (AUS) RT MAIN LANDING GEAR WARNING LIGHT REMAINED ILLUMINATED FOLLOWING GEAR UP SELECTION. INVESTIGATION CONTINUING. 2 H 7 4 4F 4 F RT A49EU E6NE 2002011400047 20020114 00047 EU 2002 1 14 AUS20011296 1 20011207 A 3297 WIRE HARNESS BAC 146 146100A 1500260 EU LYC ALF502 ALF502R5 41580 NE RT MLG UPLOCK FAULTY W O OTHER N FALSE WARNING CL CLIMB 1 AU S 5669 (AUS) RT MAIN LANDING GEAR UPLOCK HARNESS SUSPECT FAULTY. 2 H 7 4 4F 4 F RT A49EU E6NE 2002011400048 20020114 00048 EU 2002 1 14 AUS20011297 1 20010907 A 3150 110775 WARNING LIGHT FOKKER F28 F28MK4000 4990810 EU RROYCE SPEY SPEY55515 54521 EU CENTRAL WARNING FAULTY W C ABORTED TAKEOFF F N FLT CONT AFFECTED FALSE WARNING TO TAKEOFF 1 AU S (AUS) FLIGHT CONTROL MASTER CAUTION LIGHT ILLUMINATED. NO CAUSE OF THE PROBLEM COULD BE FOUND BUT THE NR 1 AND NR 2 RUDD ER BYPASS SWITCHES WERE REPLACED DUE TO PREVIOUS PROBLEMS. 2 L 7 2 4F 4 F RT A20EU E2EU 2002011400057 20020114 00057 EU 2002 1 14 AUS20011313 1 20011210 A 7110 2382101501 COWLING AIRBUS 320 A320* EU CFMINT CFM56 CFM565A1 NE ENGINE CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S 30014 (AUS) INLET COWL ACOUSTIC PANELS CORRODED. SUSPECT CAUSED BY LACK OF DRAINAGE. 2 L 7 2 4F 4 F RT A46NM E29NE 2002011400058 20020114 00058 NM 2002 1 14 AUS20011315 1 20011206 A 7830 32785002 FLEX COUPLING BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL THRUST REVERSER SHEARED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT ENGINE THRUST REVERSER ELECTRO-MECHANICAL BRAKE FLEXIBLE DRIVE INNER SHAFT PARTIALLY SHEARED. SIMILAR INSPECTI ON OF THE LT ENGINE FLEXIBLE DRIVE FOUND THAT ITEM TO BE ALSO PARTIALLY SHEARED. 2 L 7 2 4F 4 F RT A1NM E23EA 2002011400059 20020114 00059 NM 2002 1 14 AUS20011316 1 20011209 A 2620 NOZZLE BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL CARGO BAY FOULED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 AU S (AUS) FIRE EXTINGUISHER SPRAY NOZZLES LOCATED AT STA 400 AND STA 560 IN THE FORWARD CARGO COMPARTMENT WERE TAPED OVER WI TH FIBREGLASS TAPE. PERSONNEL/MAINTENANCE ERROR. 2 L 7 2 4F 4 F RT A1NM E23EA 2002011400060 20020114 00060 NM 2002 1 14 AUS20011317 1 20011212 A 2497 WIRE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE ELECTRICAL POWER WORN W K NONE O OTHER IN INSP/MAINT 1 AU S 20400 (AUS) AIRCRAFT WIRING WORN THROUGH INSULATION. THE WIRING RUNS THROUGH METAL CONDUITS IN THE WINGS AND TAIL SECTIONS. WI RING IN LT AND RT AC CONTACTOR BOXES ALSO WORN. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011400063 20020114 00063 EU 2002 1 14 AUS20011325 1 20010817 A 2612 FIRE LOOP FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU APU FAULTY W A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 AU S (AUS) APU FIRE WARNING SYSTEM LT SENSING ELEMENT FAULTY. FALSE FIRE WARNING RESULTED IN FIRE BOTTLE BEING FIRED. 2 L 7 2 4F 4 F RT A20EU E2EU 2002011400064 20020114 00064 EU 2002 1 14 AUS20011327 1 20011212 A 3260 WIRE BAC 146 146100A 1500260 EU LYC ALF502 ALF502R5 41580 NE MLG MISINSTALLED W O OTHER N W FALSE WARNING INADEQUATE Q C CR CRUISE 1 AU S (AUS) RT MAIN LANDING GEAR UPLOCK PRINTED CIRCUIT BOARD GJ21 HAD A BARE WIRE WITHOUT THE PIN PUSHED IN AT PIN 29. PERSON NEL/MAINTENANCE ERROR. 2 H 7 4 4F 4 F RT A49EU E6NE 2002011400065 20020114 00065 2002 1 14 AUS20011329 4 20011210 A 2565 D31050105 GIRT BAR BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE ESCAPE SLIDE MISINSTALLED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 AU S (AUS) FORWARD ENTRY DOOR ESCAPE SLIDE GIRT BAR ATTACHED UPSIDE DOWN. PERSONNEL/MAINTENANCE ERROR. 2 H 7 4 4F 4 F A49EU E6NE 2002011400072 20020114 00072 EU 2002 1 14 AUS20011344 1 20011013 A 8011 50111377506A MOTOR BAC 146 146100A 1500260 EU LYC ALF502 ALF502R5 41580 NE ENGINE STARTER FAULTY W A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 AU S 3597 (AUS) NR 2 ENGINE STARTER MOTOR FAULTY. STARTER OPERATING LIGHT ON DURING FLIGHT. 2 H 7 4 4F 4 F RT A49EU E6NE 2002011400073 20020114 00073 NE 2002 1 14 AUS20011345 2 20011213 A 7200 ENGINE AIRBUS 320 A320* EU CFMINT CFM56 CFM565A1 NE NR 1 OVERTEMP W O OTHER M J OVER TEMP WARNING INDICATION CL CLIMB 1 AU S (AUS) NR 1 ENGINE OVERTEMP. LIMITED INFORMATION PROVIDED. 2 L 7 2 4F 4 F RT A46NM E29NE 2002011400074 20020114 00074 SO 2002 1 14 AUS20011346 1 20011216 A 7500 AN919190 FITTING EMB 120 EMB120 3260201 SO PWA 118 PW118A NE HAMSTD 14SF 14SF9 NE ENGINE BLEED AIR MISINSTALLED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT ENGINE BLEED AIR PRESSURE REGULATING VALVE FITTING / PIPE CONNECTION CROSS THREADED. PERSONNEL/MAINTENANCE ERRO R. 2 L 7 2 4T 4 T RT A31SO E20NE 6 N P11NE 2002011400076 20020114 00076 NM 2002 1 14 AUS20011348 1 20011217 A 2722 7801401 CONTROL VALVE BOEING 747 747338 NM RUDDER ACTUATOR LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 AU S 4008 (AUS) HYDRAULIC OIL WAS FOUND LEAKING FROM THE LOWER RUDDER PCU TRANSFER VALVE. 2 L 7 2 4F RT A20WE 2002011400077 20020114 00077 NE 2002 1 14 AUS20011349 2 20011217 A 8500 R1830 ENGINE DOUG DC3 DC3CS1C3G 3021458 WP PWA R1830 R183092 52020 NE HAMSTD 23E 23E50 NE RIGHT MAKING METAL W K NONE O OTHER IN INSP/MAINT 1 AU S 523 (AUS) RT ENGINE OIL FILTER METAL CONTAMINATION. 2 L 7 2 4R 4 R A669 5E4 6 C P603 2002011400079 20020114 00079 EU 2002 1 14 AUS20011352 1 20011128 A 3230 LANDING GEAR FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU MAIN OUT OF ADJUST W O OTHER N FALSE WARNING NR NOT REPORTED 1 AU S (AUS) MAIN LANDING GEAR SUSPECT OUT OF ADJUSTMENT. 2 L 7 2 4F 4 F RT A20EU E2EU 2002011400080 20020114 00080 EU 2002 1 14 AUS20011354 1 20011119 A 3260 UPLOCK FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU LT MLG OUT OF ADJUST W C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 AU S (AUS) LT MAIN LANDING GEAR DOOR UPLOCK SUSPECT OUT OF ADJUSTMENT. 2 L 7 2 4F 4 F RT A20EU E2EU 2002011400081 20020114 00081 EU 2002 1 14 AUS20011355 1 20011108 A 2741 SWITCH FOKKER F28 F28MK4000 4990810 EU RROYCE SPEY SPEY55515 54521 EU STAB POSITION STUCK W O OTHER F N FLT CONT AFFECTED FALSE WARNING TO TAKEOFF 1 AU S (AUS) STABILIZER TRIM WARNING. SUSPECT STICKING MICROSWITCH. 2 L 7 2 4F 4 F RT A20EU E2EU 2002011400082 20020114 00082 EU 2002 1 14 AUS20011356 1 20011110 A 2741 SWITCH FOKKER F28 F28MK4000 4990810 EU RROYCE SPEY SPEY55515 54521 EU STAB POSITION STUCK W A UNSCHED LANDING F N FLT CONT AFFECTED FALSE WARNING CL CLIMB 1 AU S (AUS) HORIZONTAL STABILISER MICROSWITCH STICKING. 2 L 7 2 4F 4 F RT A20EU E2EU 2002011400083 20020114 00083 NM 2002 1 14 AUS20011358 1 20011213 A 3244 H31X97513 TIRE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE RT MLG FAILED W O OTHER O OTHER LD LANDING 1 AU S (AUS) RT MAIN LANDING GEAR INBOARD TIRE SPLIT. TREAD BEGINNING TO SEPARATE OVER THE ENTIRE RADIUS OF THE TIRE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011400084 20020114 00084 NM 2002 1 14 AUS20011359 1 20011214 A 3244 H31X97513 TIRE DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE HAMSTD 14SF 14SF23 NE MLG SEPARATED W O OTHER O OTHER LD LANDING 1 AU S (AUS) MAIN LANDING GEAR TYRE TREAD SEPARATION. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011400086 20020114 00086 NM 2002 1 14 AUS20011362 1 20011218 A 5753 65B134305 CROSSTUBE BOEING 747 747338 NM NR 3 FLAP TRACK DAMAGED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NR 3 FLAP TRACK CARRIAGE AFT BOGIE CROSSTIE ASSEMBLY DAMAGED DUE TO INTERFERENCE WITH THE FLAP TRACK. 2 L 7 2 4F RT A20WE 2002011400087 20020114 00087 EU 2002 1 14 AUS20011363 1 20011217 A 3221 AIR123816 BOLT SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ROTOL R375 R3754123F21 NE NLG SHEARED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NOSE LANDING GEAR STRUT LT TRUNNION PIN RETENTION BOLT SHEARED IN AREA JUST BELOW THE THREADED PORTION. 2 L 7 2 4T 4 T RT A52EU E8NE 6 C P17NE 2002011400090 20020114 00090 EU 2002 1 14 AUS20011368 1 20011219 A 2760 SA767A0006134 HOSE BAC 146 146100A 1500260 EU LYC ALF502 ALF502R5 41580 NE DRAG CONTROL SYS RUPTURED W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 AU S (AUS) AIRBRAKE ACTUATOR RETRACTION HOSE RUPTURED. LOSS OF GREEN SYSTEMHYDRAULIC FLUID. 2 H 7 4 4F 4 F RT A49EU E6NE 2002011400092 20020114 00092 EU 2002 1 14 AUS20011370 1 20011218 A 7732 6917M106 WIRE HARNESS BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE ENGINE VIBRATION CONTAMINATED W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 AU S (AUS) NO3 ENGINE VIBRATION TRANDUCER HARNESS CONTAMINATED WITH WATER. ENGINE HAD PREVIOUSLY SUFFERED A BIRDSTRIKE FOLLOW ED BY A COMPRESSOR WASH TO REMOVE CONTAMINANTS. 2 H 7 4 4F 4 F A49EU E6NE 2002011400093 20020114 00093 NM 2002 1 14 CA010924009 1 20010915 A 3246 3006202 WHEEL DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE MLG BROKEN W D RETURN TO BLOCK P NO WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) SEMI CIRCLE AREA APPROXIMATELY 20 INCHES AROUND BEAD SEAT AREA OF INNER WHEEL HALF SEPARATED FROM WHEEL HALF. INCI DENT HAPPENED ON THE TAXI OUT FOR TAKEOFF. AIRCRAFT RETURNED TO GATE FOR MAINTENANCE ACTION. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011400104 20020114 00104 EA 2002 1 14 CA011001001 1 20010910 A 2810 SEALANT DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE FUEL CELL LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 23474 (CAN) DURING WALKAROUND INSPECTION, THERE WAS A STRONG SMELL OF FUEL EMANTING FROM THE NR 2 LANDING GEAR BAY. MAINTENANC E INVESTIGATION REVEALED A FUEL LEAK AT THE RT INBOARD WING RIB TO BOTTOM SKIN CLOSING ANGLE. PRC SEALANT WAS REPLACED A ND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011400106 20020114 00106 EU 2002 1 14 CA010928001 1 20010924 A 2497 CONNECTOR BRAERO 748 HS7482A 4231001 EU RROYCE DART DART5342 EU WING ROOT SHORTED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING A SCHEDULED ENGINE CHANGE MAINTENANCE SELECTED THE LEFT LP FUEL COCK TO OFF. THE MIMIC INDICATOR WAS OBSERV ED TO BE FLUCTUATING FROM TRANSIT TO OPEN CONTINUOUSLY. INSPECTION OF THE TERMINAL BLOCK AT THE ACTUATOR FOUND POWER AT BOTH SIDES OF THE ACTUATOR. THE PORT WING ROOT CONNECTOR WAS FOUND TO HAVE PINS 23 AND 24 SHORTED INTERNALLY SUPPLYING POWER FROM CB NR 5 TO ON THE PORT DISTRIBUTION PANEL TO GO TO BOTH SIDES OF THE LP COCK ACTUATOR.THIS IS THE 2ND PROBLE M WITH A POST MOD AIRCRAFT WITH THE ACS STC SA 00-59. THE CONNECTOR WILL BE SENT TO THE TSB ALONG WITH THE CB REMOVED FR OM THE AIRCRAFT. 2 L 7 2 3T 4 T A24EU A196 2002011400107 20020114 00107 EA 2002 1 14 CA011001003 1 20010919 A 3320 BV330211150 SOCKET DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE CABIN BURNED W K NONE L NO TEST IN INSP/MAINT 1 CA (CAN) WHILE INVESTIGATING AN INOPERATIVE FLUORESCENT LIGHT AT ROW 1CD, THE TECH FOUND THE AFT TUBE HOLDER TO BE BURNED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011400108 20020114 00108 EU 2002 1 14 CA011001004 1 20010908 A 2910 HC324B0017000 LINE BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE HYD SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) INVESTIGATION OF A HYDRAULIC LEAK REVEALED A CRACKED FLARE ON THE HYDRAULIC LINE BETWEEN THE NR 1 ANTI-SKID VALVE AND A TEE FITTING. 2 H 7 4 4F 4 F A49EU E6NE 2002011400109 20020114 00109 EA 2002 1 14 CA011001005 1 20010920 A 7500 10558000 COOLER DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE NR ENGINE DAMAGED W C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CA 073 (CAN) THE FLIGHT CREW REPORTED THAT, UPON APPLYING TAKEOFF POWER PRIOR TO ROLLING, THERE WAS A SIGNIFICANT VIBRATION FRO M THE NR 1 ENGINE, WITH ACCOMPANYING WHINING NOISE. AFTER SELECTING START/FEATHER ON THE CONDITION LEVER, THE VIBRATION CONTINUED AND COULD BE FELT THROUGH THE POWER LEVER UNTIL SHUTDOWN. INVESTIGATION REVEALED THAT THE BLEED AIR PRECOOLER HAD FAILED, AND THE ECAPING BLEED AIR WAS BLOWING ON THE ENGINE CONTROL CABLES, PRODUCING THE VIBRATION FELT IN THE LEVE RS, AS WELL AS THE WHINING NOISE. THE PRECOOLER WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011400110 20020114 00110 NE 2002 1 14 CA011001008 3 20010916 A 6111 794404 EROSION SHIELD HONEYWELL SFA13NR0A DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE NR 2 BLADE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 86268723 (CAN) DURING ROUTINE INSPECTION, MAINTENANCE DISCOVERED DELAMINATION AT A CRACK IN THE NR 2 BLADE EROSION SHEATH OF THE NR 1 PROPELLER. FURTHER INVESTIGATION REVEALED THAT THE CRACK HAD ORIGINATED AT THE TERMINATION POINT OF THE HEATER ELEM ENT EROSION TAPE ON THE EROSION SHEATH. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011400111 20020114 00111 NM 2002 1 14 CA011001010 1 20010920 A 2910 82970010161 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) INVESTIGATION OF A FLUID LEAK IN THE UPPER AREA OF NR 1 NACELLE RESULTED IN REPLACEMENT OF THE LT LANDING GEAR "UP " LINE, WHICH WAS FOUND TO BE LEAKING AT A FACTORY BEND. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011400112 20020114 00112 EA 2002 1 14 CA011001011 1 20010924 A 3244 22X65010 TIRE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE NLG OUT OF BALANCE W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) INVESTIGATION OF A SET OF NOSEWHEEL TIRES REMOVED TO CURE A NOSE WHEEL VIBRATION SNAG REVEALED THAT THE BALANCING PATCH INSTALLED INSIDE ONE OF THE RECAPPED TIRES HAD BECOME DETACHED FROM THE TIRE. RECAPPED BY THOMPSON TIRE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011400123 20020114 00123 NM 2002 1 14 2001UALA02482 1 20011230 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 338UA 24242 EXPANSION JOINT BOLT IS WEARING INTO FRAME, AT STATION 520 RBL 24, AFT SIDE OF FRAME. MAJOR REPAIR ACCOMPLISHED. EXPAN SION JOINT REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002011400124 20020114 00124 NM 2002 1 14 2001UALA02483 1 20011230 A 5320 FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 338UA 24242 CABIN FLOORBEAM EXPANSION BOLT IS WEARING INTO FITTING AT STATION 520, RBL 45 AFT SIDE OF FLOORBEAM. MAJOR REPAIR ACCOM PLISHED. EXPANSION JOINT REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002011400125 20020114 00125 NM 2002 1 14 2001UALA02497 1 20011231 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 AFT PIT FLOORBEAM T-CAP CORRODED ABOVE STRINGER 36L, STATION 1153. MAJOR REPAIR ACCOMPLISHED. REPAIRED T-CAP. 2 L 7 2 4F 4 F RT A1NM E24NE 2002011400126 20020114 00126 NM 2002 1 14 2001UALA02498 1 20011231 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 AFT PIT FLOORBEAM T-CAP CORRODED UNDER NUT PLATE STRINGER 33L STATION 1197 + 110. MAJOR REPAIR ACCOMPLISHED. T-CAP REP AIRED. 2 L 7 2 4F 4 F RT A1NM E24NE 2002011400127 20020114 00127 NM 2002 1 14 2001UALA02499 1 20011231 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 AFT PIT FLOORBEAM T-CAP CORRODED RBL 8, STATION 1197.66. MAJOR REPAIR ACCOMPLISHED. T-CAP REPAIRED. 2 L 7 2 4F 4 F RT A1NM E24NE 2002011400128 20020114 00128 EU 2002 1 14 2001UALA02501 1 20011230 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 454UA 1104 RIGHT OVERWING EMERGENCY LIGHT POWER SUPPLY FAILS TEST AFTER REPLACEMENT OF THE BATTERY PACK. REPLACED POWER SUPPLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2002020600044 20020206 00044 NM 2002 2 6 2001UALA02502 1 20011231 A 2530 OVEN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE GALLEY DIRTY A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 829UA 1211 FIRST CLASS OVEN SMOKING. PULLED CIRCUIT BREAKER, REMOVED TRAYS AND CLEANED OVEN. RESET CIRCUIT BREAKER AND PERFORMED AN OPERATIONAL CHECK. OVEN CHECKS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2002011400136 20020114 00136 NM 2002 1 14 AWXA200200010 1 20011214 A 5311 65C3372211 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 MCN - MAJOR REPAIR - C - DURING INSPECTION A 2 INCH CRACK WAS DISCOVERED ON CHORD BS 727 LT AT WHEEL SUPPORT ASSEMBLY JU ST 2 INCHES AFT OF PRESSURE BULKHEAD, CRACK WAS VERIFIED BY HFEC. MAINTENANCE REMOVED AND REPLACED DAMAGED CHORD AT BS 727 LT, STR 25 L, LBL 25 IAW AWA ER 03-5363-02004-TB1. 2 L 7 2 4F RT A16WE 2002011400140 20020114 00140 NM 2002 1 14 AWXA200200011 1 20011231 A 5315 65468101 FLOORBEAM BOEING 737 7373S3 1384711 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 MCN - MAJOR REPAIR - C - DURING C-15 CHECK MAINTENANCE FOUND CORRODED FLOORBEAM AT BS 967, FROM RBL 15 TO RBL 18, WL 208 .1. MAINTENANCE CLEANED AND BLENDED CORRODED SECTION OF FLOORBEAM AND PERFORMED MATERIAL THICKNESS MEASUREMENT FINDING MATERIAL LOSS OUT OF LIMITS. REMOVED AND REPLACED CORRODED FLOORBEAM IAW B737-300 SRM 53-60-51 FIG 1 PG 6, 105-114, 53- 00-51 FIG 203 PG 5, 212-215, AND 51-20-01 PG 10, 47. 2 L 7 2 4F RT A16WE 2002011400141 20020114 00141 NM 2002 1 14 AWXA200200017 1 20011231 A 5320 655287855 SUPPORT BOEING 737 7373S3 1384711 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 MCN - MAJOR REPAIR - C - DURING C-15 CHECK MAINTENANCE DISCOVERED SUPPORT ANGLE CORRODED AT FASTENERS BS 995, LBL 46. M AINTENANCE REMOVED AND REPLACED CORRODED INNER CHORD AND SUPPORT ANGLE IAW B737-300 SRM 53-60-13 FIG 101 PG 104-107, 51- 40-05 PG 1-2, 51-40-02 PG 2, 3, 10, 16-17, AND 51-20-01 PG 10 & 47. 2 L 7 2 4F RT A16WE 2002011400142 20020114 00142 NM 2002 1 14 AWXA200200018 1 20011231 A 5320 6545855538 FLOOR SUPPORT BOEING 737 7373S3 1384711 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 MCN - MAJOR REPAIR - C - DURING C-15 CHECK MAINTENANCE DISCOVERED FLOORBOARD SUPPORT ANGLE CORRODED AT BS 947 TO BS 987, RBL 55, WL 208.1. MAINTENANCE REMOVED CORROSION FROM FLOORBOARD SUPPORT ANGLE AND PERFORMED MATERIAL THICKNESS MEASURE MENT WITH LOSS OF MATERIAL OUT OF LIMITS IAW B737-300 SRM 53-60-13 PG 106-107. REMOVED CORRODED SUPPORT ANGLE AND FABRI CATED NEW ANGLE AND FILLER, INSTALLED REPAIR IAW B737-300 SRM 51-70-11 PG 1-6. 2 L 7 2 4F RT A16WE 2002011400147 20020114 00147 NM 2002 1 14 DL72S011977 1 20011225 A 3397 WIRE BOEING 727 727232 1384082 NM CABIN DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 528DA 21702 SEAT 31 DEF EMERGENCY LIGHT INOP. REPAIRED WIRING. 2 L 7 3 4F A3WE 2002011400150 20020114 00150 NM 2002 1 14 DL733011944 1 20011216 A 2910 7321124002 MODULE BOEING 737 737330 13844BJ NM HYDRAULIC SYS DEFECTIVE A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 241DL 37906 105977 23833 AFTER RT ENG START, TURNED RT PACK ON WHILE USING RT ENG AS PNEUMATIC SOURCE. CABIN FILLED WITH SMOKE. ACFT EVACUATED. ALL SLIDES DEPLOYED (1L, 2L, 1R, 2R). BORESCOPED 1-3 STAGES OF HPC AND FRAME TO BOOSTER INTERFACE. NO WETTING FOUND. REPLACED RT ACM AND WATER SEPARATOR BAG AND HEPA FILTER. REPLACED HYD PRESS RSVR MODULE. RAN ACFT TO TAKEOFF PWR. A LL CK'D GOOD. 2 L 7 2 4F RT A16WE 2002011400151 20020114 00151 NM 2002 1 14 DL733011958 1 20011213 A 5330 6547955533 BEAR STRAP BOEING 737 737347 1384647 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 303WA 23183 AT FS 795 AT THE LWR FWD CORNER OF THE C-2 DOOR, A 1 INCH CRACK WAS FOUND IN THE BEARSTRAP. IN ADDITION AN EXISTING SKI N REPAIR NEAR STR 23R. THE EXISTING REPAIR IS FOR A CUTOUT IN THE SKIN AND BEARSTRAP. THE BEARSTRAP CRACK WAS GROWING FROM EXISTING EDGE DAMAGE AND WAS TRIMMED OUT. REPAIRED PER ER/A 412245-14 REV ORIGINAL. 2 L 7 2 4F RT A16WE 2002011400152 20020114 00152 NM 2002 1 14 DL733011991 1 20011230 A 5210 PIN BOEING 737 737347 1384647 NM L-1 DOOR OUT OF ADJ A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 303WA 23183 AT CRUISE ALTITUDE L-1 DOOR HANDLE POPPED UP APPROX .5 INCH. FOUND DOOR STOP PINS AND GATE UPPER AND LOWER RODS OUT OF ADJUSTMENT. RIGGED BOTH PER MM, PRESSURIZED ACFT TO 7.0 PSID, WITH CABIN PRESSURE ON UNABLE TO MOVE HANDLE. 2 L 7 2 4F RT A16WE 2002011400154 20020114 00154 NM 2002 1 14 DL738011970 1 20011222 A 2530 72077500 OVEN BOEING 737 737832 13844CF NM GALLEY SMOKE A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 3757D RTB DURING TAXI TO RUNWAY FLIGHT ATTENDANT REPORTED SMOKE FROM AFT GALLEY OVEN. MTC FOUND MEAL TOUCHING HEATING VENT. REPLACED OVEN. 2 L 7 2 4F RT A16WE 2002011400155 20020114 00155 NM 2002 1 14 DL73K011948 1 20011214 A 5315 6545410138 FLOORBEAM BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 243WA 23517 THE OVERWING LONGITUDINAL FLOORBEAM AT RBL 24 WAS FOUND WITH A CRACK IN THE WEB, WEB REINFORCING DOUBLER AND UPPER CAP A T FS 680. THE UPPER CAP AND REINFORCING DOUBLER WERE REMOVED AND REPLACED. THE WEB DAMAGE WAS TRIMMED OUT AND REPAIRED WITH AN ALUMINUM DOUBLER. A REINFORCING CHANNEL WAS INSTALLED ON THE CAP PER BAC S/B 737-57-1139. THE WORK WAS ACCOMP LISHED PER ER/A 382280-14, REV A. 2 L 7 2 4F A16WE 2002011400156 20020114 00156 NM 2002 1 14 DL73K011956 1 20011219 A 4920 85129E APU BOEING 737 737247 138448D NM APU BAY FAILED A DALA F D ACTIVATE FIRE EXT. RETURN TO BLOCK A B FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 244WA 20605 23518 60366 DURING TAXI OUT, APU DROPPED OFF LINE. TOWER CONFIRMED SMOKE AND FLAME COMING FROM APU AREA. CREW ACCOMPLISHED APU FIR E CHECKLIST. REPLACED APU AND APU FIRE BOTTLE. 2 L 7 2 4F A16WE 2002011400157 20020114 00157 NM 2002 1 14 DL73K011964 1 20011221 A 2150 ACM BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE A/C BAY SEIZED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 325DL 23097 709115 BLEEDS OFF TAKEOFF OUT OF ISP. TURNED RIGHT PACK ON, NO TROUBLE. TURNED LEFT PACK ON, SMOKE IN CABIN ACCOMPANIED WITH RUSHING AIR SOUND. FOUND LEFT ACM SEIZED FWD LEFT PACK TO MCO PER MEL 21-00-01A. 2 L 7 2 4F 4 F RT A16WE E2EA 2002011400159 20020114 00159 NM 2002 1 14 DL73K011969 1 20011222 A 2120 655447010 DUCT BOEING 737 737232 1384475 NM A/C BAY DAMAGED A DALA F H ACTIVATE FIRE EXT. DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 27 325DL 23097 F/A SMELLED SMOKE, CARGO BAY DISCHARGE, LIGHT ON FLOOR WAS HOT BETWEEN ROWS 6 - 7, FIRE BELLS AND WHISTLES FIRED BOTTLES . SHUT OFF LEFT PACK, INDICATIONS WENT AWAY. FOUND LT PACK MIX CHAMBER BLOWN BROKEN DUMPING HOT AIR ON FIRE BOTTLE. S USPECT BOTTLE OVER TEMP AND DISCHARGED, DISCHARGE SET OFF FIRE INDICATION. FWD CARGO FIRE SYST TO MCO/PLAC 26-00-19A AN D FWD LT PACK TO MCO/PLAC 21-00-01A. REPOSITION A/C TO MCO. 2 L 7 2 4F RT A16WE 2002011400160 20020114 00160 NM 2002 1 14 DL73K011981 1 20011226 A 2612 PLUG BOEING 737 737247 138448D NM COCKPIT FAILED A DALA F ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 SO 27 375DL 6968 23602 60327 ON DESCENT INTO JFK FLT NR 2568. APU DET INOP LIGHT CAME ON THEN WENT OUT. APPROX 5 MIN LATER AT 1000 FT AGL, APU FIRE HANDLE AND FIRE WARNING WITH BELL CAME ON. APU FIRE BOTTLE EXTINGUISHED AND RED FIRE HANDLE STAYED ON. APU WAS NOT RU NNING. FOUND APU FIRE INDICATION HARNESS LOOP PLUGS FAILED. REPLACED SAME AND REPLACED APU FIRE BOTTLE. 2 L 7 2 4F A16WE 2002011400161 20020114 00161 NM 2002 1 14 DL73K011993 1 20011228 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 311DL 23083 THE UPPER HINGE CUTOUT OF THE AFT ENTRY DOOR OPENING WAS FOUND WITH A SMALL CRACK IN THE BONDED SKIN ASSY. THE CRACK WA S REMOVED WITH A TRIM-OUT. THE DAMAGE WAS REPAIRED WITH AN EXTERNAL STEEL DOUBLER PER B737 SRM 53-30-3 AND PER ER/A 382 354-14, REV A. 2 L 7 2 4F RT A16WE 2002011400162 20020114 00162 NM 2002 1 14 DL73K011994 1 20011228 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 311DL 23083 THE FWD LOWER CORNER OF THE AFT GALLEY DOOR OPENING WAS FOUND WITH A CRACK IN THE SKIN AND UNDERLYING BEAR STRAP. THE CRACK WAS REMOVED WITH A 1.5 INCH X 1.5 INCH CUTOUT IN ALL LAYERS. THE CUTOUT WAS REPAIRED WITH 3 EXTERNAL ALUMINUM RE PAIR DOUBLER PER B737 SRM 53-30-3 AND ER/A 382358-14, REV A. 2 L 7 2 4F RT A16WE 2002011400164 20020114 00164 NM 2002 1 14 DL757011943 1 20011215 A 3397 WIRE HARNESS BOEING 757 757232 1384965 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 649DL 24389 EMERGENCY PATH LIGHT AT 22DEF INOP. REPAIRED BROKEN WIRING HARNESS, CHECKS OK. 2 L 7 2 4F RT A2NM 2002011400165 20020114 00165 NM 2002 1 14 DL757011963 1 20011221 A 2530 811150417 COFFEEMAKER BOEING 757 757232 1384965 NM GALLEY OVERHEATED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 670DN 25331 HOT ELECT SMELL COMING FROM MID GALLEY AREA PULLED MID GALLEY C/BS. RESET ALL GALLEY C/BS AND OPERATED ALL MID GALLEY E QUIP. FLT ATTEND REPORTED AFT COFFEEMAKER APPEARED TO HAVE OVERHEATED. FWD AFT COFFEEMAKER TO MCO AND PLAC PER 25-20-0 1, C/BS PULLED AND COLLARED. 2 L 7 2 4F RT A2NM 2002011400166 20020114 00166 NM 2002 1 14 DL757011978 1 20011225 A 3260 834802 UPLOCK SENSOR BOEING 757 757232 1384965 NM LT MLG FAILED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 647DL 24218 AFTER T/O, DOOR DISAGREE LIGHT, COCKPIT NOISE AND BUFFET FELT. REPLACED UP LOCK SENSOR. 2 L 7 2 4F RT A2NM 2002011400167 20020114 00167 NE 2002 1 14 DL757011983 2 20011227 A 7200 PW2037RTC ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 LEAKING A DALA C ABORTED TAKEOFF K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TO TAKEOFF 1 SO 27 6708D 4792 30480 728766 AFT LAV SMOKE DETECTOR WENT OFF ON T/O FLT CREW NOTICE SMELL ASSOC WITH AC PACK. FOUND OIL LEAKING FROM NR 1 ENG 2.5 BL EED VLV PORT AT T/O POWER. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002011400168 20020114 00168 NM 2002 1 14 DL757011985 1 20011228 A 3350 20131A BATTERY PACK BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 662DN 24991 R2 EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK, TESTS NORMAL NOW. 2 L 7 2 4F RT A2NM 2002011400169 20020114 00169 EU 2002 1 14 MALA020104 1 20011221 A 5753 7257840082 SUPPORT SAAB SF340 SF340A 7850100 EU T/E FLAP CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 89XJ 340A089 DURING C-CHECK IN CWA, RT INBOARD FLAP SUPPORT AT WS 142 IS CRACKED. MAINTENANCE REMOVED OLD RIB SUPPORT AND INSTALLED NEW SUPPORT P/N 7255900-064 IAW SRM 51-20. MAINTENANCE INSTALLED NEW REAR FRAME P/N 7257840-082 IAW MAL EO 57042, FWD C ORE FRAME DIAGONAL SUPPORT IS CRACKED, INSTALLED NEW P/N 7257840-078, AND 7257840-080, AND REPLACED WORN WEAR STRIP WITH NEW ONE P/N 7257800-101 IAW SRM 57-80-10-2. 2 L 7 2 4T RT A52EU 2002011400185 20020114 00185 EA 2002 1 14 SWIA200110507 1 20011229 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 499SW 7398 FLIGHT SPOILERS FAULT MESSAGE ON TAXI OUT. CONSULTED WITH MAINTENANCE. RESET CIRCUIT BREAKERS AS DIRECTED. OPS CHECK GOOD. WHILE ROLLING THE YOKE LEFT DURING FLIGHT CONTROL CHECK, LEFT SPOILERON AND LEFT FLIGHT SPOILER BOTH DEPLOY, RECE IVED A FLT SPOILERS FAULT STATUS MESSAGE. REMOVED AND REPLACED LEFT OUTBOARD PCU. OPS AND LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2002011400186 20020114 00186 EA 2002 1 14 SWIA200110508 1 20011228 A 5240 SCREW CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR LOOSE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 588SW 7069 AMBER SERVICE DOOR EICAS MESSAGE CAME ON THOUGH 10,000 FT. FOLLOWED QRH, THEN RETURNED TO SLC AIRPORT. CAUTION INDICAT ION REMAINED ILLUMINATED. PSEU SHOWED S38 FOR FORWARD SERVICE DOOR INNER HANDLE SCREWS LOOSE. TIGHTENED SCREWS AS REQU IRED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002011400187 20020114 00187 NE 2002 1 14 SWIA200110509 3 20011231 A 6110 PROPELLER EMB 120 EMB120ER 3260203 SO HAMSTD 14RF 14RF9 NE LT ENGINE FAULTY A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 209SW 120269 ON ROLLING TAKEOFF, TORQUE ON LEFT ENGINE SHOT UP TO 134 PERCENT TQ. TAKEOFF AURAL WARNING AUTO FEATHER SOUNDED WITH SW ITCH ON. ABORTED TAKEOFF. WHEN POWER LEVERS PULLED BACK TO GROUND IDLE, RT ENGINE READ 75 PERCENT TQ AND 53 PERCENT NH . WHEN AUTO FEATHER SWITCH TURNED OFF, RT ENGINE LIMITS/SPEEDS NORMAL. COMPLIED WITH OVER TORQUE INSPECTION ON LEFT EN GINE AND REPLACED LEFT PROPELLER ASSEMBLY. 2 L 7 2 4T RT A31SO 6 C P11NE 2002011400188 20020114 00188 2002 1 14 SWIA200110510 4 20011228 A 3160 DISPLAY EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 07 209SW 120269 DESCENDING THROUGH 16,000 LOST CAPTAIN'S EHSI. NOTICED STRONG BURNING ODOR, SMOKE, WHICH CLEARED ALMOST IMMEDIATELY. N O CIRCUIT BREAKERS POPPED. REMOVED AND REPLACED CAPTAIN'S ELECTRONIC FLIGHT DISPLAY IAW EMB MM 34-22-03. OPS CHECK GOO D. 2 L 7 2 4T RT A31SO 2002011400189 20020114 00189 SO 2002 1 14 SWIA200110511 1 20011229 A 3397 WIRE EMB 120 EMB120ER 3260203 SO CABIN OUT OF POSITION A SWIA K NONE O OTHER TX TAXI/GRND HDL 1 NM 07 209SW 120269 ROW SIX OVERHEAD RECESSED EMERGENCY LIGHTS ARE TOO DIM. BATTERY PACKS NEED TO BE REPLACED ON THAT CIRCUIT, NOT CHARGING . POSITIONED WIRES ON RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT TO CORRECT POSITION. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002011400190 20020114 00190 SO 2002 1 14 SWIA200110512 1 20011231 A 2751 3471001001 ANNUNCIATOR EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 213SW 910 910 120277 OUTBOARD FLAP DISAGREEMENT UPON FLAP RETRACTION IN THE AIR, RESET USING QRH. OPERATES NORMALLY ON THE GROUND. REMOVED AND REPLACED FLAP ANNUNCIATOR UNIT IAW MM 27-50-00. CLEARED FAULTS. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2002011400191 20020114 00191 SO 2002 1 14 SWIA200110514 1 20011228 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 187SW 120037 STRINGER NR 8 CRACKED AT LEFT WING NR 2 FUEL PANEL. REPAIRED STRINGER CRACK IAW EMB SRM 57-20-03. 2 L 7 2 4T RT A31SO 2002011400213 20020114 00213 EU 2002 1 14 U30A200100001 1 20011230 A 2751 WARNING SYSTEM AIRBUS 320 A320214 3930316 EU COCKPIT MALFUNCTIONED A U30A K NONE N FALSE WARNING LD LANDING 1 EA 17 261AV 1615 AFTER LANDING, FLT/CTL FLAP TIP BRK FAULT INDICATION ON ECAM. COMPLIED WITH BITE TEST IAW AMM 27-51-00-740-002 WITH NO FAULTS FOUND. ORIGINAL MESSAGE CLEARED. 2 L 7 2 4F RT A28NM 2002011400214 20020114 00214 EU 2002 1 14 U30A200100002 1 20011231 A 2751 WARNING SYSTEM AIRBUS 320 A320214 3930316 EU COCKPIT MALFUNCTIONED A U30A K NONE N FALSE WARNING LD LANDING 1 EA 17 261AV 1615 ON LANDING, FLT/CTL FLAP TIP BRK FAULT INDICATION ON ECAM. COMPLIED WITH BITE TEST IAW AMM 27-51-00-740-002, NO FAULTS FOUND; ORIGINAL MESSAGE CLEARED. 2 L 7 2 4F RT A28NM 2002011400215 20020114 00215 EU 2002 1 14 U30A200100003 1 20011231 A 2751 WARNING SYSTEM AIRBUS 320 A320214 3930316 EU COCKPIT MALFUNCTIONED A U30A K NONE N FALSE WARNING LD LANDING 1 EA 17 261AV 1615 ON LANDING, FLT/CTL FLAP TIP BRK FAULT INDICATON ON ECAM. COMPLIED WITH BITE TEST IAW AMM 27-51-00-740-002, NO FAULT FO UND; ORIGINAL MESSAGE CLEARED. 2 L 7 2 4F RT A28NM 2002011400216 20020114 00216 EU 2002 1 14 U30A200100004 1 20011231 A 2750 4917011 COMPUTER AIRBUS 320 A320214 3930316 EU T/E FLAP FAULTY A U30A K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 17 261AV 54 54 1615 TROUBLESHOOTING REVEALED NR 2 SLAT FLAP CONTROL COMPUTER (SFCC) FAULTED. REPLACED NR 2 SFCC PER AMM 27-51-34-401 AND PE RFORMED TEST PER AMM 27-54-00-210, OPS CHECK OK. 2 L 7 2 4F RT A28NM 2002011400221 20020114 00221 NM 2002 1 14 UPS01237368 1 20011207 A 3350 LIGHT BOEING 727 72725C 138400H NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 931UP 19858 INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHT IN COCKPIT INOP HGT SPARE PREFLIGHT. EMERGENCY EXIT LIGHT IN COCKPIT CHARGED AND OPERATIONAL PER 33-50, OPS CHECK GOOD OK FOR SERVICE. 2 L 7 3 4F A3WE 2002011400222 20020114 00222 NM 2002 1 14 UPS01237375 1 20011220 A 3350 BATTERY BOEING 727 7272A1 138407F NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE:PFLT CREW ENTRANCE EMERGENCY EXIT LIGHT DOES NOT TEST. REPLACED BATTERIES, OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2002011400223 20020114 00223 NM 2002 1 14 UPS01437371 1 20011218 A 3350 LIGHT BOEING 747 747123 1384873 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:PFLT EMERGENCY INST LIGHT INOP. AFTER TROUBLESHOOTING FOUND LIGHT BULBS BURNT OUT. 2 L 7 4 4F A20WE 2002011400224 20020114 00224 NE 2002 1 14 UPS01437379 2 20011222 A 7200 ENGINE BOEING 747 747212B 1384886 NM PWA JT9 JT9D7Q 52054 NE NR1 & NR2 ENGINE FLAMED OUT A IPXA O OTHER X ENGINE FLAMEOUT DE DESCENT 1 SO 01 526UP 21937 INSPECTION TYPE:N/A PILOT REPORT NR 1 AND NR 2 ENGINE FLAME-OUT. INGN FUEL AND OIL SYS CK PER MM AND ENGINEERING OPRN N ORMAL. 2 L 7 4 4F 4 F A20WE E3NE 2002011400227 20020114 00227 NM 2002 1 14 0105175504 1 20011217 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 504US 23193 DURING "H" CHECK FOUND CRACK IN FLOORBEAM UPPER CAP AT BS 700 LBL 25. REPAIRED PER EA 55-187429. 2 L 7 2 4F RT A2NM 2002011400228 20020114 00228 NM 2002 1 14 0105165504 1 20011231 A 5314 KEELBEAM BOEING 757 757251 1384970 NM CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 504US 23193 During "H" check found corrosion on keel beam between BS 673-680. Repaired per EA 55-187742. 2 L 7 2 4F RT A2NM 2002011400230 20020114 00230 WP 2002 1 14 AAALA20012115 1 20011114 A 5320 STRUCTURE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 588AA 53251 TUL - FOUND CRACK AND CORROSION UNDER G-1 GALLEY DRAIN PAN ALONG AND UNDER BUTT JOINT. CUT OUT DAMAGE AND INSTALLED DOU BLER PER SRM 53-00-00-02. (M) 2 L 7 2 4F RT A6WE 2002011400231 20020114 00231 NM 2002 1 14 AALA20011932 1 20011016 A 5320 CHANNEL BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 681AA 25338 TUL - FOUND HAT CHANNEL ON DECK PLATE CORRODED. REMOVED CHANNEL. REPLACED CHANNEL WITH NEW PART. (M) 2 L 7 2 4F RT A2NM 2002011400232 20020114 00232 NM 2002 1 14 AALA20011933 1 20011016 A 5320 CHANNEL BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 681AA 25338 TUL - FOUND LEFT Z-CHANNEL ON DECK PLATE IS CORRODED. INSTALLED NEW Z-ANGLE. (M) 2 L 7 2 4F RT A2NM 2002011400233 20020114 00233 NM 2002 1 14 AALA20012043 1 20011112 A 5320 FLOOR SUPPORT BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 683A 25340 TUL - FOUND FLOOR SUPPORT STRUCTURE HAS CORROSION AT R-4 DOOR. REPLACED FLOOR STRUCTURE AT R-4 DOOR PER 53-60-51-2. (M ) 2 L 7 2 4F RT A2NM 2002011400234 20020114 00234 NM 2002 1 14 AALA20012064 1 20011120 A 3397 WIRE BOEING 767 767223 1385123 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 327AA 22327 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 17H INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT 17H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002011400235 20020114 00235 NM 2002 1 14 AALA20012065 1 20011122 A 3350 10000679 LIGHT BOEING 767 767223 1385123 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 303AA 22309 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ILLUMINATED. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM G ROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002011400236 20020114 00236 WP 2002 1 14 AALA20012066 1 20011123 A 7930 1163P0041 SWITCH DOUG DC9 DC982 3022082 WP NR 2 ENGINE DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 499AA 49737 BNA - FLT 1855 - EN ROUTE BNA-DFW - SHORTLY AFTER TAKEOFF, RIGHT ENGINE OIL STRAINER LIGHT ILLUMINATED. RETURNED BNA AN D LANDED WITHOUT FURTHER INCIDENT. REPLACED OIL FILTER CLOG SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002011400237 20020114 00237 NM 2002 1 14 AALA20012079 1 20011128 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 376AN 25445 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 35B INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002011400238 20020114 00238 NM 2002 1 14 AALA20012098 1 20011201 A 3397 PIN BOEING 767 767223 1385123 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 323AA 22324 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 25B INOPERATIVE. REPLACED BROKEN PIN AT SEAT 25B. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002011400239 20020114 00239 WP 2002 1 14 AALA20012108 1 20011113 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 588AA 53251 TUL - FOUND DENT IN FUSELAGE STATION 1198 LONGERON 17L. INSTALLED TWO NEW DOUBLER PER SRM 53-04 FIG 38. (M) 2 L 7 2 4F RT A6WE 2002011400240 20020114 00240 WP 2002 1 14 AALA20012109 1 20011112 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 588AA 53251 TUL - FOUND NR 2 SEAT TRACK CORRODED INSIDE TRACK AT STATION 1190. INSTALLED SEAT TRACK PLUG IN SEAT TRACK NR 2 STATION 1190 PER AARD 53-20-00-10. (M) 2 L 7 2 4F RT A6WE 2002011400241 20020114 00241 WP 2002 1 14 AALA20012110 1 20011113 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 588AA 53251 TUL - FOUND CORROSION ON RIGHT CUSP AT STATION 488, LOWER SIDE. INSTALLED DOUBLER AT RT CUSP STATION 488 PER SRM 53-01 53-01-FIG 4-3. (M) 2 L 7 2 4F RT A6WE 2002011400242 20020114 00242 WP 2002 1 14 AALA20012111 1 20011113 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 588AA 53251 TUL - FOUND CORROSION ON RIGHT CUSP AT STATION 565, LOWER SIDE. INSTALLED DOUBLER PER SRM 53-00-00-02. (M) 2 L 7 2 4F RT A6WE 2002011400243 20020114 00243 WP 2002 1 14 AALA20012112 1 20011114 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 588AA 53251 TUL - FOUND SUBFLOOR DAMAGED IN SEVERAL AREAS STATION 213-217 RBL 10-19. INSTALLED REPAIR DOUBLER PER AARD 53-00-00-2. (M) 2 L 7 2 4F RT A6WE 2002011400244 20020114 00244 WP 2002 1 14 AALA20012113 1 20011114 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 588AA 53251 TUL - FOUND STATION 200, SEAT TRACK 5-6, FLOOR/GALLEY SUPPORT ANGLE CORRODED. INSTALLED NEW SERVICEABLE FLOORBOARD SUPP ORT ANGLE AT STATION 200. (M) 2 L 7 2 4F RT A6WE 2002011400245 20020114 00245 WP 2002 1 14 AALA20012114 1 20011120 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 588AA 53251 TUL - FOUND .5 INCH HOLE IN CUSP UNDER SEAT TRACK NR 1 AT STATION 1197. INSTALLED DOUBLER PER AARD 53-00-00-02. (M) 2 L 7 2 4F RT A6WE 2002011400246 20020114 00246 WP 2002 1 14 AALA20012116 1 20011129 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7525A 49917 TUL - FOUND FORWARD SIDE OF FLOORBEAM WEB CORRODED STATION 200 RIGHT SIDE AT BELTFRAME ATTACH. CUT OUT CORRODED SECTION AND INSTALLED DOUBLER PER SRM 51-70-4 PAGE 5 FIG 2. (M) 2 L 7 2 4F A6WE 2002011400247 20020114 00247 WP 2002 1 14 AALA20012117 1 20011203 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7525A 49917 TUL - FOUND CORROSION ON SUB FLOOR STATION 188 TO STATION 200 AT THE FORWARD SERVICE DOOR. CUT OUT DAMAGED AREA AND INS TALLED REPAIR PER SRM 53-01-00 FIG 4 SHT 3. (M) 2 L 7 2 4F A6WE 2002011400248 20020114 00248 WP 2002 1 14 AALA20012118 1 20011127 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7525A 49917 TUL - FOUND RIGHT CUSP CORRODED STATION 636-655. INSTALLED DOUBLER AT STATION 636-655 AS PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2002011400249 20020114 00249 WP 2002 1 14 AALA20012120 1 20011120 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7525A 49917 TUL - FOUND RIGHT CUSP CRACKED AT LIGHTNING HOLE STATION 780. REMOVED CRACK AND INSTALLED DOUBLER PER SRM 53-01 PAGE 18 . (M) 2 L 7 2 4F A6WE 2002011400250 20020114 00250 WP 2002 1 14 AALA20012121 1 20011126 A 5310 PAN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7525A 49917 TUL - FOUND WINDOW RING PAN CRACK AT UPPER RIGHT CORNER AT STATION 947 LEFT. INSTALLED DOUBLER AT STATION 947 UPPER RIG HT CORNER LEFT SIDE PER AARD 53-10-00-25. (M) 2 L 7 2 4F A6WE 2002011400251 20020114 00251 WP 2002 1 14 AALA20012122 1 20011126 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7525A 49917 TUL - FOUND NR 1 SEAT TRACK CORRODED STATION 1281, 1218, 1176, 1188. REPLACED NR 1 SEAT TRACK BETWEEN STATION 1174 AND 1307 PER SRM 53-05. (M) 2 L 7 2 4F A6WE 2002011400253 20020114 00253 WP 2002 1 14 AALA20012123 1 20011126 A 5320 THRESHOLD DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7525A 49917 TUL - FOUND AFT CARGO DOOR OPENING LOWER THRESHOLD IS CORRODED STATION 1155 TO 1211. REPAIRED PER AARD 53-10-00-16, AAR D 53-10-00-3. (M) 2 L 7 2 4F A6WE 2002011400254 20020114 00254 WP 2002 1 14 AALA20012124 1 20011129 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7525A 49917 TUL - FOUND THREE CRACKS EXTENDING FROM TWO RIVET HOLES STATION 1380 10 INCHES ABOVE RIGHT ENGINE PYLON. REPAIRED CRACK S BY INSTALLING DOUBLER IAW SRM 53-04 FIG 18. (M) 2 L 7 2 4F A6WE 2002011400255 20020114 00255 NM 2002 1 14 AALA20012146 1 20011205 A 3350 P401005112 CHARGER BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 315AA 22317 LAX - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY PATH LIGHTING RIGHT ROWS 10-17 INOPERATIVE. REPLACED RIGHT C ONTROL CHARGER MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002011400256 20020114 00256 NM 2002 1 14 AALA20012153 1 20011210 A 3397 CONNECTOR BOEING 767 767323 1385205 NM CABIN FAULTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 399AN 29606 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 19B THROUGH 22B INOPERATIVE. REPLACED EMERGENCY EXIT LI GHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002011400257 20020114 00257 EU 2002 1 14 AALA20012160 1 20011213 A 2910 CPN5648720 VALVE AIRBUS 300 A300B4605R 3930308 EU HYDRAULIC SYS FAILED A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 14065 508 LHR - AFTER TAKEOFF YELLOW SYSTEM HYDRAULIC RESERVOIR AIR LIGHT ILLUMINATE FOLLOWED BY LOSS OF YELLOW SYSTEM PRESS REPEA T OF PIREP N074. REPLACED YELLOW SYSTEM NON-RETURN VALVE FOR HEAD PRESSURE LEAK CHECK AND OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A35EU 2002011400258 20020114 00258 NM 2002 1 14 AALA20014067 1 20011116 A 5522 SKIN BOEING 767 767223 1385123 NM ELEVATOR DELAMINATED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 315AA 22317 AFW - RIGHT OUTBOARD ELEVATOR LOWER SKIN HAS MULTIPLE LAYERS OF DELAMANATION FS 137.5-141.25 AND 160.25-162.0 AS SHOWN O N SKETCH. REQUEST APPROVAL TO CONTINUE SERVICE. TAP TEST AREA FOR DELAMINATIONS. (M) 2 L 7 2 4F RT A1NM 2002011400259 20020114 00259 NM 2002 1 14 AALA20014068 1 20011116 A 5330 140T0110 SKIN BOEING 767 767223 1385123 NM FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 315AA 22317 AFW - ACCOMPLISH REPAIR TO FUSELAGE SIN AT STATION 432. REPAIR SKIN PER REF (A). FABRICATED DOUBLER. SHIMMED STRINGER . FINISHED ALL REPAIR PARTS AND INSTALLED. (M) 2 L 7 2 4F RT A1NM 2002011400260 20020114 00260 NM 2002 1 14 ASAA0110637 1 20011105 A 5210 604364 HINGE BOEING 737 7372X6C 1384552 NM L1 DOOR LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 ANC - L1 DOOR DIFFICULT TO CLOSE. LUBED DOOR HINGE ATTACH POINTS, THEN OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A16WE 2002011400261 20020114 00261 NM 2002 1 14 ASAA0110638 1 20011106 A 5210 6529994 GUIDE BOEING 737 7372X6C 1384552 NM L1 DOOR OUT OF ADJ A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 ANC - L1 DOOR DIFFICULT TO CLOSE. ADJUSTED GUIDE ARM, THEN OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A16WE 2002011400262 20020114 00262 NM 2002 1 14 ASAA0110640 1 20011108 A 5210 6528925 ROD END BOEING 737 737290C 138448V NM L1 DOOR OUT OF ADJ A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 ANC - L1 DOOR DIFFICULT TO CLOSE FROM THE INSIDE. ADJUSTED UPPER ROD END ASSEMBLY THEN OPS CHECKED GOOD. (M) 2 L 7 2 4F A16WE 2002011400263 20020114 00263 NM 2002 1 14 ASAA0140144 1 20011115 A 5320 65C31874 STRAP BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 PAE - DURING SI CHECK, FOUND FLOOR WEB STRAP AT BS 1020 RBL 4 AND LBL 4 AND WL 208 HAS MECHANICAL DAMAGE. REPLACED STRA P PER SRM. (M) 2 L 7 2 4F RT A16WE 2002011400264 20020114 00264 NM 2002 1 14 ASAA0140154 1 20011126 A 3350 8100022607 LIGHT BOEING 737 7374Q8 138447Q NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 775AS 25108 SEA - DURING LINE CHECK, FOUND RED FLOOR TRACK LIGHTS NEAR ROW 1 INOPERATIVE. REMOVED AND REPLACE TRACK LIGHT ASSEMBLY. OPS CHECKED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002011400270 20020114 00270 NM 2002 1 14 ASAA0140165 1 20011128 A 3397 8100022607 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 754AS 25095 SEA - DURING LINE CHECK, FOUND FLOOR TRACK LIGHTS NEAR ROW 1 INOPERATIVE. REATTACHED WIRES ON INOPERATIVE SECTIONS. OP ERATIONAL CHECKED GOOD. (M) 2 L 7 2 4F RT A16WE 2002011400271 20020114 00271 NM 2002 1 14 ASAA0140166 1 20011203 A 3397 8100022601 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 774AS 25107 ANC - DURING LINE CHECK, FOUND FLOOR TRACK LIGHTS INOPERATIVE IN AFT CABIN. CONNECTED WIRES, OPS NORMAL. (M) 2 L 7 2 4F RT A16WE 2002011400272 20020114 00272 NM 2002 1 14 ASAA0140167 1 20011205 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 755AS 25096 SEA - DURING LINE CHECK, FOUND FLOOR TRACK LIGHTS NEAR ROW 1 INOPERATIVE. REATTACHED WIRES ON INOPERATIVE SECTIONS. OP ERATIONAL CHECKED GOOD. (M) 2 L 7 2 4F RT A16WE 2002011400273 20020114 00273 NM 2002 1 14 ASAA0140600 1 20011016 A 5311 6564534 FRAME BOEING 737 7372Q8C 138448S NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING C-CHECK, FOUND FRAME DENT AT STATION 500 BETWEEN STRINGER 24R AND STRINGER 25R. REPAIRED IAW SRM. (M) 2 L 7 2 4F A16WE 2002011400274 20020114 00274 NM 2002 1 14 ASAA0140601 1 20011016 A 5311 6554957507 FRAME BOEING 737 7372Q8C 138448S NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING C-CHECK, FOUND FRAME DENT AT BS 500A BETWEEN STRINGER 24R AND 25R. REPAIRED IAW ENGINEERING REPAIR. (M) 2 L 7 2 4F A16WE 2002011400275 20020114 00275 NM 2002 1 14 ASAA0140602 1 20011016 A 5311 6554957507 FRAME BOEING 737 7372Q8C 138448S NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING C-CHECK, FOUND FRAME DENT AT BS 500A BETWEEN STRINGER 24L AND 25L. REPAIRED IAW ENGINEERING REPAIR. (M) 2 L 7 2 4F A16WE 2002011400276 20020114 00276 NM 2002 1 14 ASAA0140603 1 20011016 A 5313 6935352 STRINGER BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING C-CHECK, FOUND CORROSION ON STRINGER 26R AND STATION 419. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2002011400277 20020114 00277 NM 2002 1 14 ASAA0140604 1 20011016 A 5310 6546534 SHEAR TIE BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE -DURING C-CHECK FOUND CORROSION ON SHEAR TIE STATION 520 BETWEEN STRINGER 26L AND 27L. REPAIRED IAW SRM. (M) 2 L 7 2 4F A16WE 2002011400278 20020114 00278 NM 2002 1 14 ASAA0140605 1 20011016 A 5313 6939322 STRINGER BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 SW 21 741AS 21959 PAE - DURING C-CHECK, FOUND CORROSION ON STRINGER 27R AT STATION 531. REPAIRED IAW SRM. (M) 2 L 7 2 4F A16WE 2002011400279 20020114 00279 NM 2002 1 14 ASAA0140607 1 20011016 A 5320 69353521 STRINGER CLIP BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING C-CHECK, FOUND CORROSION ON STRINGER TIE AT STATION 533 AND STRINGER 27R. REPLACED STRINGER CLIP IAW SRM. (M) 2 L 7 2 4F A16WE 2002011400280 20020114 00280 NM 2002 1 14 ASAA0140608 1 20011016 A 5320 69353521 STRINGER CLIP BOEING 737 7372Q8C 138448S NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING C-CHECK, FOUND CRACKED STRINGER CLIP AT BS 440 AND STRINGER 24L. REPLACED STRINGER CLIP PER SRM. (M) 2 L 7 2 4F A16WE 2002011400281 20020114 00281 NM 2002 1 14 ASAA0140609 1 20011016 A 5320 69353521 STRINGER CLIP BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING C-CHECK, FOUND CORROSION ON STRINGER 35L CLIP AT BS 827 IN AFT CARGO BAY. REPLACED CLIP IAW SRM. (M) 2 L 7 2 4F A16WE 2002011400282 20020114 00282 NM 2002 1 14 ASAA0140610 1 20011016 A 5320 69353521 STRINGER CLIP BOEING 737 7372Q8C 138448S NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING C-CHECK, FOUND CRACKED STRINGER CLIP AT STATION 440 AND STRINGER 24L. REPLACED STRINGER CLIP PER SRM. (M) 2 L 7 2 4F A16WE 2002011400283 20020114 00283 NM 2002 1 14 ASAA0140612 1 20011016 A 5311 65C33509 FRAME BOEING 737 7372Q8C 138448S NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING C-CHECK, FOUND FRAME DENT AT BS 400 AND STRINGER 24L. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2002011400284 20020114 00284 NM 2002 1 14 ASAA0140613 1 20011016 A 5320 65469205 SILL BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING C-CHECK, FOUND CORROSION ON LEFT OVERWING EXIT SILL. REPLACED SILL IAW SRM. (M) 2 L 7 2 4F A16WE 2002011400285 20020114 00285 NM 2002 1 14 ASAA0140614 1 20011016 A 5311 6546595 FRAME BOEING 737 7372Q8C 138448S NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING C-CHECK, FOUND FRAME DENTED AT STRINGER 25R AND BS 727A. REPAIRED IAW SRM. (M) 2 L 7 2 4F A16WE 2002011500013 20020115 00013 SW 2002 1 15 CA011003017 1 20011001 A 2910 2781032135 LINE SWRNGN SA226 SA226TC 8780404 SW HYD SYSTEM CRACKED W D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 CA 14883 (CAN) A/C MADE NORMAL APPROACH & LDG. DURING 180 DEG TURN TO CLEAR RWY, CREW NOTED FLUX IN HYDRAULIC NOSEWHEEL STEERING SYS, BUT TAXIIED IN & SHUTDOWN WITH NO PROBLEMS. ON EXITING A/C, CREW NOTICED SMALL AMOUNT HYDRAULIC FLUID ON GROUND UND ER LT ENGINE FIREWALL AREA. MAINT DISCOVERED LEAKING HYDRAULIC LINE, WHICH HAD CRACK IN ROOT OF FLARE, UNDER FLARE NUT, AT BULKHEAD FITTING IN LT WHEEL WELL. LINE REMOVED, TRIMMED, REFLARED, & REINSTALLED. HYDRAULIC SYS SERVICED, ENGINES G ROUND RUN, & SYS OP & LEAK CHECK VERIFIED. A/C RETURNED TO SERVICE. 2 L 7 2 4T RT A8SW 2002011500015 20020115 00015 NM 2002 1 15 CA011004002 1 20010806 A 7921 D2887155C BYPASS VALVE DHAV DHC8 DHC8* NM PWC 150 PW150A EA OIL COOLER FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) ON CLIMB OUT TO FL250 CREW NOTICED AT FL230 OIL TEMPERATURE IN THE RED, CONTINUED TO CLIMB TO FL250, AND TEMPERAT URE STABILIZED AT 110. CREW POWER BACK AND LOWER TEMP, LOWERED TO 107, CREW DIVERTED TO BACK TO BASE. NO EMERGENCY WA S DECLARED. CREW REPORT: NR 1 ENGINE OIL TEMP WENT TO 110, EXCEEDED LIMITS, TEMP WENT TO 110 FOR 10 MINUTES, THEN 108 FOR 10 MINUTES. MAINTENANCE REPORTED THE OIL TEMPERATURE PEAKED AT 110 AND THE EXCEEDANCE WAS FOR 23.8 MINUTE. REMOVED AND REPLACED OIL COOLER BYPASS VALVE IAW MM 79-21-06. GROUND RUN COMLETED AND TEMPERATURE WAS NORMAL. OPERATION CHECKE D GOOD. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002011500018 20020115 00018 EA 2002 1 15 CA011004006 1 20010921 A 2910 82970009379 LINE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE HYD SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 23365 (CAN) AFTER A MAINTENANCE RUN, THE ENGINEER NOTICED A HYDRAULIC LEAK FROM THE LEFT WHEEL WELL. UPON FURTHER INVESTIGATIO N, IT WAS DETERMINED THAT THE LEAK WAS COMING FROM THE MLG DOWN PRESSURE LINE (RIGID TUBE) IN THE LEFT NACELLE DUE TO A PIN HOLE IN THE TUBE. THE TUBE WAS REPLACED AND ALL FURTHER CHECKS WERE COMPLETED PRIOR TO RETURNING THE AIRCRAFT TO SER VICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011500019 20020115 00019 NM 2002 1 15 CA011004007 1 20010920 A 2434 230880028 STARTER GEN DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE ENGINE FAILED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 18991 (CAN) DURING THE TAKEOFF ROLL, THE NR 2 DC GENEERATOR CAUTION LIGHT ILLUMINATED INDICATING A GENERATOR FAILURE. THE FLIG HT CREW REJECTED THE TAKEOFF AND TAXIIED THE AIRCRAFT BACK TO THE GATE. MAINTENANCE REPLACED THE NR 2 DC STARTER/GENERAT OR AND ALL FURTHER CHECKS WERE COMPLETED PRIOR TO RELEASING THE AIRCRAFT TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011500021 20020115 00021 NM 2002 1 15 CA011004011 1 20010921 A 5610 TERMINAL DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE WINDSHIELD HEAT OVERHEATED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 17503 (CAN) DURING THE FLIGHT, THE FLIGHT CREW NOTED A BURNING SMELL IN THE COCKPIT FOLLOWED BY A "LEFT WINDSHIELD HOT" CAUTIO N LIGHT. SHORTLY THEREAFTER, SMOKE APPEARED IN THE COCKPIT. THE CREW SELECTED THE WINDSHIELD HEATERS OFF AND THE AIRCRAF T DIVERTED TO THE NEAREST AIRPORT.MAINTENANCE FOUND THE LEFT WINDSHIELD HEATER LEAD CONNECTION AT TERMINAL L2 (ON THE WI NDSHIELD) HAD OVERHATED AND BURNED. THE LEFT WINDSHIELD AND HEATER LEADS WERE REPLACED AND ALL FURTHER CHECKS WERE COMPL ETED PRIOR TO RELEASING THE AIRCRAFT TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011500022 20020115 00022 NM 2002 1 15 CA011004012 1 20010922 A 2931 7G772 PRESSURE SWITCH DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE RUDDER FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 30329 (CAN) THE NR 2 RUDDER HYDRAULIC CAUTION LIGHT ILLUMINATED DURING FLIGHT. THE FLIGHT CREW SELECTED THE RUDDER NR 2 SHUT OFF SWITCH AND ALL THREE RUDDER CAUTION LIGHTS CAME ON. THE AIRSPEED WAS REDUCED TO LESS THAN 200 KNOTS AND THE AIRCRAFT RETURNED TO THE STATION. MAINTENANCE REPLACED THE NR 2 RUDDER HYDRAULIC PRESSURE SWITCH, RESET THE SYSTEM AND COMPLETE D ALL FURTHER CHECKS PRIOR TO RELEASING THE AIRCRAFT TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011500023 20020115 00023 NE 2002 1 15 CA011004013 2 20010917 A 7260 312137201 SPUR GEAR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 1 ENGINE AGB FAILED W A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 CA 31173 12571 (CAN) CREW REPORTED NR 1 ENGINE FLAMED OUT DURING THE CLIMB OUT OF YYZ. THE AIRCRAFT RETURNED TO YYZ WITHOUT INCIDENT. U PON MAINTENANCE INVESTIGATION THE NR 1 OIL TANK CHIP DETECTOR WAS FOUND FLAGGED. MAINTENANCE PROCEEDED TO INSPECT THE AC CESSORY DRIVE AND FOUND THE SPUR GEAR (P/N 3121372-01) FOR THE FUEL PUMP HAD ALL THE TEETH SHEARED OFF. THE NR 1 ENGINE WAS REPLACED (TURBO MACHINERY AND REDUCTION GEAR BOX) ALONG WITH THE AC GENERATOR, OIL COOLER AND PROP ACTUATOR FOR POSS IBLE OIL CONTAMINATION. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011500024 20020115 00024 NE 2002 1 15 CA011004015 3 20010914 A 6114 8173881 SEAL CNDAIR CL215 CL2156B11415 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF* NE PROP BLADE BROKEN W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) AFTER LANDING AND A SHORT TAXI, A SMALL AMOUNT OF REVERSE WAS APPLIED, THEN GROUND FINE FOR 30 SECONDS, AND FEATHE R FOR ABOUT 1 MINUTE (AS PER AFM). AT THAT POINT OIL WAS NOTICED ON THE LT SIDE AND THE ENGINE WAS SHUT DOWN. FURTHER I NVESTIGATION REVEALED THAT THE OIL WAS FROM THE LT PROP NR 1 BLADE. THE WELD ON THE SPRING IN THE CSA BLADE SEAL HAD LET GO. THE SEAL WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A14EA E20NE 6 C P7NE 2002011500027 20020115 00027 EA 2002 1 15 CA011004018 1 20010918 A 5610 6003303026 WINDSHIELD CNDAIR CL601 CL6012A12 1900303 EA COCKPIT CRACKED W H DEACTIVATE SYST/CIRCUITS O OTHER CR CRUISE 1 CA (CAN) WINDOW OUTER FACE PLY CRACKED FROM TOP TO BOTTOM IN FLIGHT. 2 L 7 2 4F RT A21AE 2002011500031 20020115 00031 EA 2002 1 15 CA011005005 1 20010821 A 5414 539553 BRACE CNDAIR CL604 CL604 1900301 EA GE CF34 CF343B1 NE COWL DOOR LOOSE W E ENGINE SHUTDOWN E VIBRATION/BUFFET CL CLIMB 1 CA (CAN) AFTER TAKEOFF, AT 700 FEET AGL, CREW THROTTLED BACK & FOUND THAT LEFT THROTTLE WAS STIFF. THEY ATTEMPTED TO REDUCE POWER FURTHER, BUT IT COULD NOT BE REDUCED ANY LOWER THAN 90 PERCENT. THROTTLE COULD BE ADVANCED SLIGHTLY BUT WOULD ONL Y OPERATE BETWEEN 90-92 PERCENT. A FLT ATTENDANT & 2 CO EMPLOYEES WERE ON BOARD. A/C DIVERTED INTO BRADLEY. AN EMERGENCY WAS DECLARED, & ENGINE WAS SHUTDOWN ON FINAL APPROACH AT 50 MILES OUT. INVESTIGATION FOUND UPPER CORE COWL STAY BRACE S TRUT LAYING ACROSS FUEL CONTROL ON THROTTLE LINKAGE, PREVENTING THROTTLE MOVEMENT. COWL WAS LAST OPENED DURING A 2400 HR INSP 9 DAYS 18.8 HRS & 10 CYCLES EARLIER. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011500033 20020115 00033 NE 2002 1 15 CA011005007 2 20010925 A 7200 ENGINE CNDAIR CL601 CL6013A 8070802 EA GE CF34 CF343A1 30015 NE NR 2 FAILED W A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 CA (CAN) DURING CRUISE, NR 2 ENGINE LOW OIL PRESSURE INDICATOR ILLUMINATED AND VERTICAL SCALE SHOWED NO OIL PRESSURE. ENGIN E WAS SHOWING HIGH VIBE INDICATIONS. FLIGHT CREW SECURED ENGINE. MADE UNEVENTFUL LANDING. INVESTIGATION IN PROGRESS. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011500034 20020115 00034 EA 2002 1 15 CA011005008 1 20010914 A 7830 22850808141 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE THRUST REVERSER FAILED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA (CAN) "ON TAKEOFF ROLL AT 80 KTS RT THRUST REVERSER "REV" ICON, "REV UNLOCK" MESSAGE AND UNLOCK LIGHT ON CENTRE PEDESTAL APPEARED".PILOT REPORTED YAW AT THE TIME OF OCCURRENCE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011500035 20020115 00035 EA 2002 1 15 CA011005009 1 20010919 A 2913 848847 PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE HYD SYSTEM DAMAGED W B A EMER. DESCENT UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA (CAN) PILOT REPORT LOSS OF NR 3 HYDRAULIC PRESSURE IN CRUISE. MAINTENANCE REMOVED AND REPLACED EDP (ENGINE DRIVEN PUMP) 3A AND AIRCRAFT BACK IN SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011500036 20020115 00036 EA 2002 1 15 CA011011004 1 20010925 A 3244 128173 TIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT MLG FAILED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA (CAN) PILOT EPORT: AFTER TAKEOFF, THE TOWER NOTIFIED THEY HAD SEEN DEBRIS DEPART THE AIRCRAFT. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LT INBOARD TIRE ON MAIL LANDING GEAR. AIRCRAFT BACK IN SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011500037 20020115 00037 EA 2002 1 15 CA011011005 1 20010928 A 2760 4916405 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SPOILERS FAILED W C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 CA 11045 (CAN) PILOT REPORT: GROUND SPOILER DEPLOYED DURING TAKEOFF ROLL. MAINTENANCE FOUND SECU (SPOILER ELECTRONIC CONTROL UNI T), S/N 396, INTERNAL FAULT. REMOVED AND REPLACED.AIRCRAFT BACK IN SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011500038 20020115 00038 EU 2002 1 15 CA011011006 1 20010912 A 7603 8303989 THROTTLE CABLE BRAERO 748 HS7482A 4231001 EU RROYCE DART DART5342 EU RT MLG WW FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING A DAILY INSPECTION, MAINTENANCE NOTED SCRATCHES ON THE SUPERCHARGER DUCT IN THE RT WHEEL WELL. DETAILED INS PECTION REVEALED WHEN THROTTLE WAS PLACED IN CRUISE POSITION, THE RT THROTTLE CABLE P/N 8302989 WAS SEVERELY FRAYED. THE FRAY WAS ONLY VISIBLE WHEN THE THROTTLE WAS PLACED IN CRUISE. A NEW CABLE WAS INSTALLED AND SUPER CHARGER DUCT REPOSITI ONED. AN INSPECTION OF ALL OTHER AIRCRAFT IN THE FLEET REVEALED NO ANOMOLIES. 2 L 7 2 3T 4 T A24EU A196 2002011500045 20020115 00045 SW 2002 1 15 CA011011013 1 20010927 A 5230 H29495 LATCH SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR WORN W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) WHILE CLIMBING THROUGH 11,000 FT THE CARGO DOOR WARNING LIGHT ILLUMINATED. AS PER THE AFM PROCEDURES, THE FLIGHT C REW BEGAN TO DEPRESSURIZE THE CABIN AND DESCENDED TO 7,000 FT, UPON WHICH TIME THE CARGO DOOR WARNING LIGHT EXTINGUISHED AGAIN. AFTER AN UNEVENTFUL LANDING, MAINTENANCE INSPECTED THE DOOR AND FOUND THE LATCHING MECHANISM, TRAVELS AND INDICA TIONS TO BE NORMAL. THEY DID HOWEVER ELECT TO REPLACE TWO CLICK CLACK LATCHES DUE TO SLIGHT MOVEMENT OF THE LATCH JAWS W HEN DEPRESSED. WITH THE NEW LATCHES INSTALLED AND THE DOOR OPERATION AND INSPECTION COMPLETED, THE AIRCRAFT WAS RELEASED . 2 L 7 2 4T RT A8SW 2002011500046 20020115 00046 NM 2002 1 15 CA011011014 1 20010924 A 7120 87110016009 MOUNT DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE RT ENGINE BROKEN W A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 CA (CAN) CREW REPORTED VIBRATION ON ENGINE NR 2 CONDITION LEVER. AFTER INVESTIGATION WE FOUND THE REAR ENGINE MOUNT (RT ENG INE INBOARD) STRUT VERTICAL ASSEMBLY BROKEN (SEPARATION IN TWO PARTS). 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011500052 20020115 00052 CE 2002 1 15 CA011012004 1 20010831 A 2435 51538001A GCU BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA LT STARTER GEN FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA (CAN) AIRCRAFT DEPARTED SMITHERS, THE LT GENERATOR KICKED OFF LINE FOLLOWED BY A FAINT ELECTRICAL ODOR. THEY RETURNED TO THE SMITHERS AIRPORT AND DEPLANED PASSENGERS. MAINTENANCE FOUND LT GENERATOR CONTROL UNIT TO BE EMITTING ODOR. IT WAS R EPLACED ALONG WITH THE LT GENERATOR. THE SYSTEM TESTED NORMALLY AND THE AIRCRAFT DEPARTED WITH NO FURTHER INCIDENTS. 2 L 7 2 4T 4 T RT A24CE E4EA 2002011500053 20020115 00053 EU 2002 1 15 CA011012005 1 20010910 A 7197 30607621 HARNESS AMD FALC50 FALCON50MYST 2730106 EU GARRTT TFE731 TFE73140 29001 NE NR 3 ENGINE FAILED W A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 CA (CAN) ON CLIMB THROUGH 7,000 FT, ENGINE NR 3 N1 ROLL BACK APPROXIMATELY 10 PERCENT. IGNITION LIGHT WOULD COME ON AND E NGINE RECOVERS. AT 39,000 FT, NR 3 ENGINE N1 ROLL BACK 5 PERCENT. 3 SEPARATE TIMES EACH TIME IGNITION ON AUTOMATICALLY AND ENGINE WOULD RECOVER. FOUND N2 INDICATION TO DEEC IRATIC WITH ALL OTHER PARAMETERS NORMAL. WHEN N2 WOULD FLUCTUATE 5 PERCENT, N1 WOULD ROLL BACK AS WELL. HARNESS REPLACED WITH NEW UNIT. FOUND N2 INDICATION TO DEEC TO BE STABLE NO FURTHE R PROBLEMS. 2 L 7 3 4F 4 F A46EU E1NM 2002011500054 20020115 00054 EA 2002 1 15 CA011012007 1 20010910 A 6310 5610743500060 FREEWHEEL UNIT CARSON S61 S61LSKRSKY EA GE CT58 CT581401 30011 NE GEARBOX WORN W A UNSCHED LANDING D INFLIGHT SEPARATION HO HOVERING 1 CA (CAN) DURING LIFTING OP AT 86 PERCENT Q. PILOT NOTICED TORQUE SPLIT ACCOMPANIED BY THUD NOISE & YAW KICK. A/C RT-SRV ARE A WHERE INPUT FREEWHEEL UNITS WERE REMOVED FOR INSP. HIGHER THAN NORMAL WEAR FOUND ON BOTH UNITS FOR THE TIME IN SERVICE .AFTER GATHERING INFO ON CONDITION OF INPUT FREEWHEELS IT DOES NOT LOOK LIKE THOSE IS ASSY PROBLEM. IS EVIDENCE OF DAMAG E TO ROLLER RETAINERS. BOTH RETAINERS HAVE CONTACTED CAMSHAFTS, IS ABNOR MAL WEAR. WHEY RETAINERS HAVE CONTACTED IS NOT KNOWN AT TIME 2 G 7 2 4U 4 U H8EA 1E3 2002011500076 20020115 00076 NM 2002 1 15 0105105642 1 20011230 A 2750 MECHANISM BOEING 757 757251 1384970 NM T/E FLAP LACK OF LUBE A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 542US 26489 AFTER TAKEOFF UPON SELECTING FLAPS 1, THE TRAILING EDGE FLAP DISAGREE WARNING ILLUMINATED AND THERE WAS NO CHANGE IN THE INDICATED FLAP POSITION. THE FLIGHT DECLARED AN EMERGENCY, RETURNED TO MSP, AND ACCOMPLISHED AN OVERWEIGHT LANDING WIT HOUT INCIDENT. MAINTENANCE INSPECTED THE SYSTEM, RESET THE FLAP OVERLOAD INDICATORS, LUBRICATED THE FLAP MECHANISM, AND SERVICED THE FLAP TRANSMISSIONS. SYSTEM FUNCTIONAL TESTS WERE SATISFACTORY. 2 L 7 2 4F RT A2NM 2002011500077 20020115 00077 WP 2002 1 15 0105139995 1 20011221 A 2780 DUCT DOUG DC9 DC931 3022065 WP L/E SLAT LACK OF LUBE A NWAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 01 8978E 47327 WHEN CONFIGURING THE AIRCRAFT FOR LANDING, THE AIRCRAFT ROLLED LEFT AND STABILIZED. NO BLUE SLAT EXTEND INDICATION BUT SLAT DISAGREEMENT ANNUNCIATOR LIGHT ILLUMINATED. COMPLIED WITH COM PROCEDURE AND LANDING WAS MADE WITHOUT LEADING EDGE SLAT AT GPT. MAINTENANCE WAS NOT ABLE TO DUPLICATE THE DISCREPANCY AND LUBRICATED THE LEFT T-DUCT. AIRCRAFT RETURNED T O SERVICE. 2 L 7 2 4F A6WE 2002011500078 20020115 00078 WP 2002 1 15 0105149962 1 20011220 A 2913 314195 PUMP DOUG DC9 DC931 3022065 WP LT ENGINE FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 924RW 47185 ON CLIMBOUT, THE LEFT HYDRAULIC PRESSURE LOW LIGHT ILLUMINATED. THE LEFT HYDRAULIC PRESSURE DROPPED TO ZERO WITH THE PU MP IN EITHER LOW OR HIGH. QUANTITY AND TEMPERATURE WERE BOTH NORMAL. CREW RESTORED PRESSURE TO NORMAL IN THE LEFT SYST EM BY USING THE ALTERNATE HYDRAULIC PUMP. THE FLIGHT RETURNED TO A SAFE LANDING BACK TO MSP WERE MAINTENANCE REPLACED T HE LEFT ENGINE DRIVEN HYDRAULIC PUMP. THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002011500079 20020115 00079 NE 2002 1 15 0105159988 2 20011230 A 7230 COMPRESSOR DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7 52053 NE RT ENGINE STALLED A NWAA E A ENGINE SHUTDOWN UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 01 8944E 47167 657250 DURING CLIMBOUT, THE RIGHT ENGINE EXPERIENCED A STALL WITH ASSOCIATED VIBRATION AND POWER LOSS. CREW SHUT DOWN THE RIGH T ENGINE AND RETURNED TO DTW. MAINTENANCE REPLACED THE RIGHT ENGINE AND TWO PASSENGER WINDOWS ON THE FIGHT SIDE OF THE AIRCRAFT. ENGINE OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A6WE E2EA 2002011500084 20020115 00084 WP 2002 1 15 CA011017005 2 20010925 A 7320 39423091 SHUTOFF VALVE SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP LT ENGINE FUEL LEAKING W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) ON SHUTDOWN OF THE LT ENGINE THE CREW REPORTED THE RPM WAS SLOW TO DEGRADE ACCOMPANIED WITH A RISING EGT. THE ENGI NE EVENTUALLY SLOWED AND STOPPED WITH EXCESSIVE AMOUNTS OF SMOKE COMING FROM EXHAUST.A SUBSEQUENT INSPECTION REVEALED TH AT THE LT FUEL SHUTOFF VALVE HAD FAILED TO CLOSE COMPLETELY WHEN THE STOP BUTTON WAS DEPRESSED, THERE WAS NO DAMAGE TO T HE ENGINE AS A RESULT OF THIS INCIDENT. THE FUEL SHUTOFF VALVE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A8SW E4WE 2002011500093 20020115 00093 NM 2002 1 15 CA011017009 1 20010917 A 2913 8297000317 PUMP DHAV DHC8 DHC8* NM PWA PW120 PW123 NE HAMSTD 14SF 14SF23 NE HYD SYSTEM LEAKING W O OTHER J WARNING INDICATION AP APPROACH 1 CA (CAN) INITIAL REPORT: NR 2 HYD FLUID HOT THEN NR 2 ENG HYD PUMP CAUTION LIGHTS CAME ON DURING APPROACH. LDG SELECTED DOW N, LDG DOWNLOCKED. NR 2 HYD QUANTITY DROPPED TO 0. NR 2 ENG HYD PUMP CAUTION LIGHT CAME ON.FINDINGS: CONTAMINATION FOUND IN NR 2 CASE DRAIN, RETURN AND PRESSURE FILTERS. NR 2 EDP FOUND TO BE LEAKING. NR 2 ENGINE NACELLE LINE P/N 82970009-31 7 FROM CHECK VALVE TO CASE DRAIN FILTER OVERHEATED. ACTION TAKEN: NR 2 HYD SYSTEM WAS FLUSHED SEVERAL ATIMES. NR 2 CASE DRAIN, PRESSUE AND RETURN FILTERS WRE REPLACED. NR 2 EDP WAS REPLACED.LINE P/N 8297000-317 REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011500107 20020115 00107 NM 2002 1 15 C1HA200181020 1 20011228 A 2530 COFFEEMAKER BOEING 727 7272S7 138407Z NM GALLEY DEFECTIVE A C1HA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 15 681CA 22020 AFT COFFEEMAKER FWD SIDE LET OUT A PUFF OF SMOKE AND NOTICED ELECTRICAL BURNING SMELL. REMOVED AND REPLACED COFFEEMAKER WITH SERVICEABLE ONE. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2002011500108 20020115 00108 NM 2002 1 15 C1HA200183009 1 20011221 A 3350 BATTERY BOEING 727 7272S7 138407Z NM CABIN DISCHARGED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 683CA 22490 AFT MOST OVERHEAD EMERGENCY LIGHT BLINKS ON AND OFF INTERMITTENTLY. REMOVED AND REPLACED EMERGENCY OVERHEAD LIGHT BATTE RY IAW MM 33-50-81. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2002011500109 20020115 00109 NM 2002 1 15 C1HA200183010 1 20011221 A 3350 BATTERY BOEING 727 7272S7 138407Z NM CABIN DISCHARGED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 683CA 22490 AFT MOST OVERHEAD EMERGENCY LIGHT BLINKS ON AND OFF INTERMITTENTLY. REMOVED AND REPLACED EMERGENCY OVERHEAD LIGHT BATTE RY IAW MM 33-50-81. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2002011500110 20020115 00110 NM 2002 1 15 C1HA200183012 1 20010102 A 3350 CHARGER BOEING 727 7272S7 138407Z NM CABIN INOPERATIVE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 683CA 22490 AFT MID CABIN SEC OF EMERGENCY FLOOR TRACK LIGHTING INOP. REMOVED AND REPLACED BATTERY PWR SUPPLY CHARGER FOR MID SEC F LOOR TRACK LIGHTING PER MM 33-50-23 CONF 3, OPS CK NORMAL. 2 L 7 3 4F A3WE 2002011500111 20020115 00111 NM 2002 1 15 C1HA200184017 1 20011223 A 3350 BATTERY BOEING 727 7272S7 138407Z NM CABIN DISCHARGED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 684CA 22491 EMERGENCY TRACK LIGHTING INOP AFT PART OF AIRCRAFT. REPLACED AFT BATTERY POWER SUPPLY, OPS CHECKS GOOD IAW 33-50-23. 2 L 7 3 4F A3WE 2002011500112 20020115 00112 NM 2002 1 15 C1HA200184018 1 20011223 A 3350 BATTERY BOEING 727 7272S7 138407Z NM CABIN DISCHARGED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 684CA 22491 EMERGENCY TRACK LIGHTING INOP FWD PART OF AIRCRAFT. REPLACED FWD BATTERY POWER SUPPLY, OPS CHECKS GOOD IAW MM 33-50-23. 2 L 7 3 4F A3WE 2002011500123 20020115 00123 SO 2002 1 15 C2XA02IA005 1 20011229 A 5315 14521700001 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13964 7209 145123 IAH- DURING C-CHECK INSPECTION IT WAS NOTED THAT THE OMEGA BEAM AT FRAME 20 WAS CORRODED. MAINTENANCE REMOVED THE CORR ODED AREA, FABRICATED A FILLER, REINFORCEMENT AND INSTALLED IT ON THE OMEGA BEAM AND THE AIRCRAFT WAS APPROVED FOR RETUR N TO SERVICE, WHEN RELEASED FROM C-CHECK. 2 L 7 2 4F RT T00011AT 2002011500124 20020115 00124 SO 2002 1 15 C2XA02IA006 1 20011229 A 5320 14521725615 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13964 7209 145123 IAH- DURING C-CHECK IT WAS NOTED THAT THE GALLEY AREA HAS NUMEROUS AREAS OF CORROSION ON UPPER SURFACES OF FLOORBEAMS F ROM FRAME 15 TO FRAME 23. MAINTENANCE REMOVED AND REPLACED THE RIGHT FLOOR SILL FROM FRAME 19 TO FRAME 20 AND THE AIRCR AFT WAS APPROVED FOR RETURN TO SERVICE, WHEN RELEASED FROM C-CHECK. 2 L 7 2 4F RT T00011AT 2002011500125 20020115 00125 NM 2002 1 15 CA011017012 1 20010903 A 2131 92147A020103 CONTROL PANEL DHAV DHC8 DHC8* NM PWC 150 PW150A EA CABIN PRESSURE FAILED W H DEACTIVATE SYST/CIRCUITS O OTHER DE DESCENT 1 CA (CAN) ON DESCENT THE PRESSURIZATION FAILED IN AUTO, FAULT LIGHT ON PRESSURIZATION PANEL. SWITCHED TO MANUAL, STILL NO C ONTROL OVER THE OUT FLOW VALVE. USED FORWARD SAFETY VALVE FOR THE REST OF THE DESCENT. OUTFLOW VALVE OPENED ON LANDING.F OUND THE PRESSURIZATION CONTROL PANEL AT FAULT. PRESSURIZATION CONTROL PANEL REPLACED AND FUNCTION CHECKED SERVICEABLE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002011500126 20020115 00126 SO 2002 1 15 C2XA02IA007 1 20011229 A 5320 14521725013 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13964 7209 145123 IAH- DURING C-CHECK IT WAS NOTED THAT THE GALLEY AREA HAS NUMEROUS AREAS OF CORROSION ON THE UPPER SURFACES OR THE FLOO RBEAMS FROM FRAME 15 TO FRAME 23. MAINTENANCE REMOVED AND REPLACED THE RIGHT FLOOR SILL FROM FRAME 22 TO FRAME 23 AND T HE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE, WHEN RELEASED FROM C-CHECK. 2 L 7 2 4F RT T00011AT 2002011500127 20020115 00127 NM 2002 1 15 CA011017013 1 20010914 A 3230 483023 SEQUENCE VALVE MENASCO 47200 DHAV DHC8 DHC8* NM PWC 150 PW150A EA NLG FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) AFTER TAKEOFF AND LADING SELECTED UP - UNSAFE GEAR INDICATION LIGHT CAME ON (RED NOSE GEAR INDICATION AND YELLOW L IGHT IN HANDLE), LDG SET, DOWN AND AFTER 90 SEC. SAFE DOWN LIGHT CAME ON, AIRCRAFT RETURNED TO BASE. NLG SOLENOID SEQUEN CE VALVE REPLACED AND GEAR SWING CARRIED OUT (25X) SYSTEM OPS CHECKED NORMAL. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002011500128 20020115 00128 NM 2002 1 15 CA011017014 1 20010914 A 3010 153212A VALVE DHAV DHC8 DHC8* NM PWA PW120 PW123 NE HAMSTD 14SF 14SF23 NE DEICE SYSTEM FAILED W O OTHER O OTHER CR CRUISE 1 CA (CAN) AN OPERATOR REPORTED THE FOLLOWING: IN FLIGHT THE FOLLOWING DE-ICE BOOTS ARE PARTIALLY INFLATED WITH THE SELECTOR OFF: LEFT NR 2, 3 & 4, RIGHT NR 4, DE-ICE PRESS 18 PSI. INBOARD DISTRIBUTING VALVE ON PORT WING CHANGED IAW. AMM 30-10-1 6.SINCE REPLACING THE LEFT-HAND INBOARD DE-ICE DISTRIBUTOR VALVE, THE DEFECT HAS NOT RE-OCCURRED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011500132 20020115 00132 2002 1 15 CA011018001 4 20011001 A 3414 2114011342 INDICATOR DHAV DHC8 DHC8* NM PWA 120 PW120 NE AIRSPEED LEAKING W O OTHER O OTHER CR CRUISE 1 CA 251485 (CAN) WHILE FLYING IN CRUISE, THE PILOT'S AIRSPEED INDICATION DROPPED TO ZERO. NR 1 ALTIMETER AND STANDBY ALTIMETER BOTH SHOWED A DESCENT, ERRONEOUS INDICATIONS. FAULT WAS TRACED TO AN INTERNAL (CAPSULE) LEAK INSIDE THE AIRSPEED INDICATOR, WHICH EFFECTED THE OTHER INSTRUMENTS. NR 1 AIRSPEED INDICATOR REPLACED AND SYSTEM TESTED SERVICEABLE. 2 H 7 2 4T 4 T RT A13NM E20NE 2002011500133 20020115 00133 NM 2002 1 15 CA011018002 1 20010927 A 3060 69707012 LEAD DHAV DHC8 DHC8* NM PWC 150 PW150A EA PROP DEICE SYS BURNED W O OTHER E J VIBRATION/BUFFET WARNING INDICATION AP APPROACH 1 CA (CAN) DURING APPROACH CREW RPTED NR 1 NP OVERSPEED, PEC NR 1 CAUTION LIGHT, POWER PLANT MESSAGE ON ED & NR 1 PROP DEICE CAUTION LIGHT CAME ON AT SAME TIME. PROP RPM RPTED AS BEING ERRATIC FOR SEVERAL MOMENTS. MDC SHOWED PROP NP OF 1095 FOR 27 SEC. 4 MORE OVER SPEEDS WERE RECORDED IN NEXT 8 SEC. FAULT CODES PRESENT WERE: LT 160 & 162, RT 156 ALL POINT TO NR 1 MPU OR PEC.INSP OF MPU MOUNTING BLOCK SHOWED LARGE BURN MARK ON FO RWARD FACE. ALSO FOUND ONE OF DEICE LEAD'S FROM SLIP RING TO PROP BLADE HAD CUT & BURN MARKS ON IT AS WELL.THE 2 BURN MARKS LINED UP & APPEAR TO HAVE BEEN PROBLEM. THEY WER E MAKING CONTACT. GAPS ON MPU T O TARGETS CHECKED & RE-RIGGED. FAULTS CLEARED. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002011500134 20020115 00134 NM 2002 1 15 CA011018003 1 20010925 A 2710 82742339001 PULLEY DHAV DHC8 DHC8* NM PWC 150 PW150A EA AILERONS SPLIT W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) FLIGHT CREW REPORTED STIFF AILERON CONTROL. DURING INSPECTION OF THE ROLL CONTROL SYSTEM, DEGRADATION OF PULLEYS P /N 8274339-001 NOTED IN AILERON AND SPOILER CIRCUITS. NEW PULLEYS INSTALLED, SYSTEM RIGGED AND AIRCRAFT RETURNED TO SERV ICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002011500135 20020115 00135 2002 1 15 CA011018007 4 20010828 A 3414 2013011208 INDICATOR SWRNGN SA227 SA227AC 8780603 SW MCAULY 4HFR34 4HFR34C652 NE COCKPIT READS HIGH W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA (CAN) ON TAKEOFF CAPTAIN ASI INCREASED FASTER THAN FO'S ENDED UP READING 30 KTS HIGH. CAPTAIN ASI REMOVED FOR REPAIR AND RE-INSTALLED. 2 L 7 2 4T RT A8SW 6 C 3PNE 2002011500148 20020115 00148 CE 2002 1 15 CA011018010 1 20010925 A 3230 G16D22 WIRE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA MLG CHAFED W O OTHER J WARNING INDICATION LD LANDING 1 CA 16782 (CAN) ON LANDING, CREW SELECTED GEAR DOWN, LANDING GEAR CIRCUIT BREAKER "POPPED", TRANSIT HANDLE LIGHT ILLUMINATED "RED" , MANUAL GEAR EXTENSION PERFORMED, 3 GREEN LIGHTS INDICATED. AIRCRAFT LANDED WITHOUT INCIDENT.MAINTENANCE INVESTIGATIO N FOUND A CHAFED WIRE G16D22 SHORTING BETWEEN J315 & J161 ON THE LANDING GEAR EXTENSION / RETRACTION CIRCUIT AT THE FORW ARD SIDE OF THE FORWARD ENTRY DOOR. THE WIRE WAS REPAIRED AND THE WIRE BUNDLE REPOSITIONED. GEAR SWINGS CARRIED OUT, NO DISCREPANCIES NOTED. SYSTEM CHECKED SERVICEABLE. 2 L 7 2 4T 4 T RT A24CE E4EA 2002011500158 20020115 00158 EA 2002 1 15 CA011018022 1 20011010 A 2132 OXYGEN MASK CNDAIR CL601 CL6012A12 1900303 EA CABIN FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) DURING A SCHEDULED INTENTIONAL DEPRESSURIZATION OF THE AIRCRAFT IN FLIGHT TO VERIFY THE OXYGEN MASK DROP SYSTEM, T HE AIRCRAFT RETURNED WITH THE FOLLOWING SNAG: DURING MASK DROP TEST - IN CLIMB - THE CABIN ALTITUDE INDICATOR FROZE AT 3 ,000 FT - AFTER MASKS DROPPED THE INDICATOR WAS TOPPED AND THE NEEDLE JUMPED TO THE 13,000 FT RANGE. 2 L 7 2 4F RT A21AE 2002011500159 20020115 00159 CE 2002 1 15 CA011019004 1 20010924 A 2121 BEARING ELECTROMECH 1013841761 BEECH B300 B300B350C CE PWA PT6 PT6A60A 52043 NE BLOWER ASSY LOOSE W A UNSCHED LANDING B D F SMOKE/FUMES/ODORS/SPARKS INFLIGHT SEPARATION FLT CONT AFFECTED CR CRUISE 1 CA 2609 (CAN) VIBRATION ON RUDDER PEDALS AND RUMBLE NOISE SEEMS TO BE COMING FROM UNDER CO-PILOT RUDDER PEDALS, AS REPORTED BY C REW. AFTER INSPECTION BY MAINTENANCE PERSONNEL, COCKPIT BLOWER FOUND TO BE DEFECTIVE, BLOWR REPLACED, GROUND CHECK SERVI CEABLE. 2 L 7 2 4T 4 T RT A24CE E4EA 2002011500160 20020115 00160 GL 2002 1 15 CA011019005 2 20010914 A 7260 23061402 BEVEL GEAR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL GEARBOX FRACTURED W A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 CA (CAN) AIR SHUTTLE 5864 CLT-HSV AFTER TAKEOFF, THE NR 1 ENGINE SHUTDOWN. THE CREW PERFORMED EMERGENCY PROCEDURES BUT THER E WAS NO INDICATION AS TO THE REASON FOR THE SHUTDOWN. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITH NO FURTHER PRO BLEMS. MX WAS CALLED. MX REMOVED AND REPLACED NR 1 ENGINE. OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. ENGINE STRIP AT RRC REVEALED THAT THE GEARSHAFT BEVEL PINION RADIAL DRIVE AS FAILED. THE RADIAL DRIVE QUILLSHAFT DRIVES THE ACC ESSORY GEARBOX FAILED PART AND ASSOCIATED PARTS SHIPPED TO ROLLS ROYCE FOR INVESTIGATION. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002011500161 20020115 00161 EA 2002 1 15 CA011019007 1 20010918 A 2450 K1XD RELAY CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE ELECTRICAL FAULTY W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) AFTER TAKEOFF UNABLE TO POWER AC ESSENTIAL BUS EITHER BY AC BUS NR 1 OR AC BUS NR 2 AIRCRAFT RETURN TO TORONTO. FO UND TO BE THE ESSENTIAL BUS SENSE RELAY AT FAULTY.REPLACED AC ESSENTIAL RELAY, POWER AVAILABLE FROM BOTH BUSES. OPERATIO NAL TEST 24-51-27-710-002 CARRIED OUT. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011500162 20020115 00162 NE 2002 1 15 CA011019008 2 20010917 A 7311 500675501B HEAT EXCHANGER BOEING 767 767233 1385113 NM PWA JT9 JT9D7R4D 52054 NE RT ENGINE LEAKING W F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 CA (CAN) RIGHT HAND ENGINE SHUTDOWN AFTER START-UP DUE TO ENGINE FIRE. EMERGENCY EVACUATION ON LEFT END SIDE OF THE AIRCRAF T. ENGINE FIRE BOTTLES DISCHARGED.REPLACED RIGHT ENGINE, AFTER INVESTIGATION FOUND THAT THE CAUSE OF THE TAIL PIPE FIRE WAS A RESULT OF THE FUEL COOLER OIL COOLER HEAT EXCHANGR (FCOC) THAT HAD AN INTERNAL LEAK AS RESULT, THE FUEL WAS FILLIN G UP THE GEARBOXES AND VENTING INTO THE TAIL PIPE.REPLACED ENGINE FOR THE AFFECTED AIRCRAFT, REPLACED THE FCOC AT FAULT ON THIS ENGINE, ENGINE BENCH TESTED AND FOUND SERVICEABLE, RETURN FOR STOCK.FCOC P/N 5006755-01BFCOC S/N P280-13 2 L 7 2 4F 4 F RT A1NM E3NE 2002011500165 20020115 00165 NE 2002 1 15 CA011019014 2 20011003 A 7261 6087T04P05 PUMP CNDAIR CL601 CL6013A 8070802 EA GE CF34 CF343B1 NE NR 2 ENGINE FAILED W E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CA (CAN) DURING CRUISE, NR 2 ENGINE OIL PRESSURE RAPIDLY ROLLED BACK FROM 65 TO 24 PSI. THE FLIGHT CREW THROTTLED BACK THE ENGINE TO IDLE AND OIL PRESSURE SLOWLY CLIMBED TO 45 PSI. CREW ADVANCED THROTTLE TO 90 PERCENT AND OIL PRESSURE AGAIN RO LLED BACK TO 25 PSI. ENGINE WAS AGAIN RETURNED TO IDLE. DURING DESCENT OIL PRESSURE DROPPED TO 10 PSI AND THE LOW OIL PR ESSURE MESSAGE APPEARED. THE CREW SHUTDOWN THE ENGINE AND MADE AN UNEVENTFUL LANDING.THE NR 2 ENGINE LUBE/SCAVENGE PUMP WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011500166 20020115 00166 EA 2002 1 15 CA011019015 1 20010821 A 2910 215T7519424 LINE CNDAIR CL215 CL2156B11415 EA PWA PW120 PW123 NE HYD SYSTEM CHAFED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) THE LT ENGINE DRIVEN PUMP HYDRAULIC PRESSURE LINE PASSING THROUGH THE TRANSITION BOX WAS FOUND CHAFED THROUGH BY 8 0 PERCENT OF IT'S TOTAL WALL THICKNESS. THE CHAFING OCCURS THROUGH THE FIRE WALL SKIN WHERE THE LINE PASSES THROUGH THE GROMMET. 2 H 7 2 4T 4 T RT A14EA E20NE 2002011500167 20020115 00167 EA 2002 1 15 CA011019016 1 20010821 A 2910 215T7519424 LINE CNDAIR CL215 CL2156B11415 EA PWA PW120 PW123 NE HYD SYSTEM CHAFED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) THE LT ENGINE DRIVEN PUMP HYDRAULIC PRESSURE LINE PASSING THROUGH THE TRANSITION BOX WAS FOUND CHAFED THROUGH BY 8 0 PERCENT OF IT'S TOTAL WALL THICKNESS. THE CHAFING OCCURS THROUGH THE FIRE WALL SKIN WHERE THE LINE PASSES THROUGH THE GROMMET. 2 H 7 2 4T 4 T RT A14EA E20NE 2002011500168 20020115 00168 EA 2002 1 15 CA011019017 1 20011002 A 5410 601350061 WEB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 17492 (CAN) DURING C-CHECK COMPLIED WITH SB A601R-53-059. FOUND CRACKS ON UPPER WEB AT LBL 8 (1.2IN ), RBL 8 (3.5IN) AND LOWER WEB AT LBL 8 (0.5").AREAS TO BE REPAIRED IAW REOS 601R-53-61-345 AND -366. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011500178 20020115 00178 NM 2002 1 15 DL757011992 1 20011230 A 5210 BOTTLE BOEING 757 757232 1384965 NM L-2 DOOR LOW A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 631DL 23612 L-2 DOOR EMERGENCY POWER RESERVOIR BOTTLE PRESS LOW. REPLACED L-2 DOOR EMERGENCY POWER RESERVOIR BOTTLE. 2 L 7 2 4F RT A2NM 2002011500179 20020115 00179 NM 2002 1 15 DL757011999 1 20011231 A 3241 427571 MODULE BOEING 757 757232 1384965 NM LT MLG FAULTY A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 685DA 27588 AFTER T/O ANTI-SKID INOP LIGHT EICAS ANTI-SKID ADVISORY AND STATUS MSGS ALTN ANTI-SKID AND NORM ANTI-SKID. PERFORMED BI TE CHECK FAULTS NR 2 XDCR. FOUND BACKSHELL LOOSE AND SECURED SAME. REPLACED ANTI-SKID MODULE. NO CURRENT FAULTS. 2 L 7 2 4F RT A2NM 2002011500180 20020115 00180 NM 2002 1 15 DL757012000 1 20011231 A 3242 AHA1844 BRAKE ASSY BOEING 757 757232 1384965 NM NR 1 FIRE A DALA K NONE A FLAME/FIRE TX TAXI/GRND HDL 1 SO 27 656DL 24396 UPON ARRIVAL SRQ WHILE TAXIING TO THE RAMP. RAMP PERSONNEL SPOTTED A NUMBER 1 BRAKE FIRE. FIRE WAS OUT WHEN A/C STOPPE D AT THE GATE. FLT CREW REPORTED NO SIGN OF ABNORMAL HEAT ON BRAKE TEMP IND. HOTTEST BRAKE WAS NR 5 THAT WAS SHOWING A 3. MTC FOUND NR 1 BRAKE WITH BURN MARK AT HYD LINE HOUSING ON BRAKE ASSY. INSPECTED BOTH MLG ALL TIRES/BRAKES CHECK O K. REPLACED NR 1 BRAKE ASSY. NR 1 WHEEL ASSY WAS OK. NO EXCESSIVE GREASE ON AXLE. 2 L 7 2 4F RT A2NM 2002011500183 20020115 00183 NM 2002 1 15 DL764011953 1 20011217 A 5754 114T41457 BOLT BOEING 767 767432ER 1385134 NM L/E SLAT MISSING A DALA K NONE F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 SO 27 828MH 29699 ON LANDING GEAR ROLL WITH FLAPS AT 30 DEGREES, LEADING EDGE SLAT ASYMMETRY EICAS MESSAGE ILLUMINATED. FOUND NR 4 SLAT O UTBOARD AUXILIARY TRACK BOLT MISSING. ALSO MISSING ARE BEARING, WASHER ASSY (TARGET), NUT AND COTTER PIN. FOUND NR 4 L EADING EDGE PROX TARGET BROKEN. REPLACED PROX TARGET AND NR 4 BEARING ON TARGET, OPS CHECK GOOD. BITE ON FSEU GOOD. 2 L 7 2 4F RT A1NM 2002011500184 20020115 00184 NM 2002 1 15 DL767011942 1 20011215 A 3350 20131A BATTERY PACK BOEING 767 767232 1385132 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 108DL 22220 DURING SVC CHECK LEFT FIRST CLASS OVERHEAD EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK, SYSTEM CHECKS GOOD. 2 L 7 2 4F RT A1NM 2002011500185 20020115 00185 2002 1 15 DL76G011962 4 20011221 A 3417 4040800911 ADC BOEING 767 767332 1382001 NM LEFT MALFUNCTIONED A DALA O OTHER G MULTIPLE FAILURE CR CRUISE 1 SO 27 1611B 30595 DURING FLIGHT LOST BOTH FMC/S AND AUTO PILOTS FOR APPROX 5 MINUTES. ALL THEN CAME BACK. REPLACED LEFT ADC IN SFO, SYST EM CHECKS NORMAL. 2 L 7 2 4F RT A1NM 2002011500187 20020115 00187 NM 2002 1 15 VNAA0112002 1 20011202 A 2450 230GC02Y03 CONTROL PANEL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 438JS 244 3056 AS FLIGHT 4078 WAS READY FOR TAKEOFF THE CREW RECEIVED A RIGHT HAND GENERATOR FAIL CAS MESSAGE AND ABORTED TAKEOFF. FLI GHT 4078 RETURNED TO THE GATE WHERE MAINTENANCE INSPECTED AND SWAPPED 1VE PANELS WITH N427JS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002011500188 20020115 00188 NM 2002 1 15 VNAA0112003 1 20011205 A 3150 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 433JS 3047 DURING THE TAKE ROLL, THE CREW RECEIVED LEFT HAND SHAKER FAIL CAS MESSAGE AND ASSOCIATED AMBER CAS MESSAGES AND ABORTED TAKEOFF. AS THE AIRCRAFT DECELERATED THE INDICATIONS CLEARED. THE CREW CONTACTED MAINTENANCE CONTROL WHO CLEARED THE F LIGHT FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4168 DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002011500189 20020115 00189 2002 1 15 VNAA0112006 4 20011208 A 3444 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 442JS 3060 DURING TAKEOFF, THE CREW RECEIVED A AMBER GPWS CAS MESSAGE AND ABORTED TAKEOFF. AS THE AIRCRAFT TAXIED OFF THE RUNWAY T HE MESSAGE CLEARED. FLIGHT 4048 WAS CLEARED FOR ANOTHER TAKE OFF ATTEMPT AND DEPARTED WITHOUT ANY FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002011500190 20020115 00190 NM 2002 1 15 VNAA0112007 1 20011208 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 429JS 10229 3043 THE CREW REPORTED THAT THE EMERGENCY LIGHTS AT ROWS 3 THROUGH 6 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLAC ED THE EMERGENCY BATTERY AT THE 5LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002011500191 20020115 00191 NM 2002 1 15 VNAA0112008 1 20011207 A 3610 RESTRICTOR VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE PNEUMATIC SYS FAILED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 460PS 3061 DURING CLIMBOUT, THE CREW RECEIVED A PACK OVERPRESSURE INDICATION AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLAC ED THE RESTRICTOR FOR THE RIGHT HAND OVERPRESSURE SWITCH IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 36-00-00. OPERAT IONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002011500192 20020115 00192 NM 2002 1 15 VNAA0112010 1 20011212 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 328JS 917 3030 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 7 TO 9 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 6LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WE RE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002011500193 20020115 00193 NM 2002 1 15 VNAA0112012 1 20011217 A 3150 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 438JS 3056 DURING THE TAKEOFF ROLL, THE FLIGHT CREW RECEIVED MULTIPLE WARNING MESSAGES FOR THE MAIN CABIN DOOR, THE MICRO AIR DATA COMPUTERS AND THE FLIGHT GUIDANCE COMPUTER. THE FLIGHT CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. THE AIRCRAFT WAS INSPECTED AND FERRIED TO CAK WHERE MAINTENANCE PERFORMED OPERATIONAL CHECKS IN ACCORDANCE WITH THE DORNIER MAINTENA NCE MANUALS AND NO ABNORMALITIES WERE FOUND. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002011500194 20020115 00194 NM 2002 1 15 VNAA0112015 1 20011220 A 3060 LEAD DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT PROPELLER FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 328JS 3030 DURING CLIMBOUT FROM PIT, THE CREW RECEIVED A LEFT HAND PROP HEAT FAIL MESSAGE AND RETURNED TO THE PIT. MAINTENANCE IN SPECTED AND REPLACED TWO PROPELLER HEAT LEADS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-00-00. OPERATIONAL CHECK S WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002011500195 20020115 00195 2002 1 15 VNAA0112019 4 20011227 A 3418 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 433JS 3047 DURING THE TAKEOFF, THE CREW RECEIVED A SHAKER AND PUSHER FAIL MESSAGE AND ABORTED TAKEOFF. AS FLIGHT 4023 CLEARED THE RUNWAY THE MESSAGE CLEARED AND FLIGHT 4023 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4023 THEN DEPARTED WITH NO F URTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002011500196 20020115 00196 NM 2002 1 15 DL76L011939 1 20011214 A 3260 SWITCH BOEING 767 767332 1382001 NM LANDING GEAR OUT OF TOLERANCE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 195DN 28452 ON TAKEOFF FROM ATL CREW UNABLE TO RAISE GEAR HANDLE PAST OFF POSITION. ALSO HAD AUTOBRAKES FAIL MESSAGE AND A LEFT/RIG HT ICE DETECTOR FAIL MESSAGE. REMOVED AND REPLACED RELAYS K147AND K209, NO HELP. RANG TILT SENSORS S246S245S268ANDS267 ALL OK. INSTALLED KNOWN GOOD PSEU, NO HELP. INSTALLED ORIGINAL TS PER MM 32-09-02, FOUND S245 AND S267 OF TOLERANCE. ADJUSTED GAP, SYSTEM CHECK GOOD. 2 L 7 2 4F RT A1NM 2002011500197 20020115 00197 NM 2002 1 15 DL76L011989 1 20011229 A 3350 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 185DN 27961 FOUND DURING LAYOVER, OVERHEAD AISLE EMERGENCY LIGHTS INOP AT ROWS 1B THRU 4B. REPLACED PWR SUPPLY AT SEAT ROW 2A SIDE WALL, OPS CHECKS GOOD. 2 L 7 2 4F RT A1NM 2002011500198 20020115 00198 NM 2002 1 15 DL76L011996 1 20011230 A 2611 47310802 SMOKE DETECTOR BOEING 767 767332 1382001 NM CARGO BAY INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 181DN 25986 FWD CARGO DET 2 STATUS MSG RELAMP, NO HELP. REPLACED DETECTOR OPS NORMAL. 2 L 7 2 4F RT A1NM 2002011500199 20020115 00199 NM 2002 1 15 AALA20014070 1 20011204 A 5750 FITTING BOEING 767 767323 1385205 NM WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 39367 25194 AFW - FLAP ATTACH HOLES WERE REAMED TO REMOVE CORROSION. FABRICATE FREEZE FIT PLUGS IN ORDER TO ACHIEVE A MIN 0.001 INC H INTERFERENCE FIT. (M) 2 L 7 2 4F RT A1NM 2002011500200 20020115 00200 NM 2002 1 15 ASAA0110596 1 20011011 A 3350 873100252 SIGN BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 747AS 23124 ANC - DURING SCHEDULED MAINTENANCE, FOUND RIGHT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED EXIT LIG HT ASSEMBLY, LIGHT TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002011500201 20020115 00201 NM 2002 1 15 ASAA0110627 1 20011021 A 3350 86210144 BATTERY PACK BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 FAI - DURING LINE CHECK, FOUND EMERGENCY EXIT LIGHTING AT SEAT PALLET NR 4 INOPERATIVE. REMOVED AND REPLACED EXIT LIGHT BATTERY PACK, OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A16WE 2002011500202 20020115 00202 NM 2002 1 15 ASAA0110648 1 20011203 A 3397 8631001 WIRE BOEING 737 737290C 138448V NM CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - EMERGENCY FLOOR TRACK LIGHTING AT ROW 7, SEAT PALLET 4-9 INOPERATIVE DUE TO BROKEN WIRE. REPAIRED BROKEN WIRE, TH EN LIGHT OPS CHECKED GOOD. (M) 2 L 7 2 4F A16WE 2002011500203 20020115 00203 NM 2002 1 15 ASAA0140113 1 20011011 A 3350 8100022607 LIGHT BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 769AS 25103 SEA - DURING LINE CHECK, FOUND ROW 15C EMERGENCY LIGHTS INOPERATIVE. RECONNECTED TRACK LIGHT, OPERATIONS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2002011500204 20020115 00204 NM 2002 1 15 ASAA0140116 1 20011014 A 3350 8100022605 LIGHT BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 769AS 25103 SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHT AT ROW 14-19 DISCONNECTED. RECONNECTED TRACK LIGHTS, OPERATIONAL C HECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002011500205 20020115 00205 NM 2002 1 15 ASAA0140117 1 20011017 A 3397 8100022605 WIRE BOEING 737 7374Q8 138447Q NM CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 779AS 25111 SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHT WIRING DAMAGE AT ROW 2-7 AND INOPERATIVE. REPLACED LIGHT ASSEMBLY, OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002011500206 20020115 00206 NM 2002 1 15 ASAA0140119 1 20011022 A 3397 8100022608 WIRE BOEING 737 7374S3 1384711 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 SEA - BEFORE FLIGHT, FOUND EMERGENCY TRACK LIGHTS AT ROWS 4-6 DISCONNECTED. RECONNECTED WIRE, OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002011500207 20020115 00207 NM 2002 1 15 ASAA0140138 1 20011107 A 5311 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 PAE - DURING SI CHECK, FOUND STUB FRAME AT BS 294.5, WL 208, RBL 60 IS CRACKED. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002011500208 20020115 00208 NM 2002 1 15 ASAA0140142 1 20011116 A 5311 6546548 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 PAE - DURING SI CHECK, FOUND CRACK AT BS 747 BETWEEN STRINGER 8 AND 9 LEFT. REPAIRED CRACKED FRAME PER SRM. (M) 2 L 7 2 4F RT A16WE 2002011500209 20020115 00209 NM 2002 1 15 ASAA0140143 1 20011115 A 5320 65C31847 STRAP BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 PAE - DURING SI CHECK, FOUND FLOOR WEB STRAP AT BS 1020 RBL 18 AND WL 208 HAS MECHANICAL DAMAGE. REPLACES STRAP PER SRM . (M) 2 L 7 2 4F RT A16WE 2002011500210 20020115 00210 NM 2002 1 15 ASAA0140597 1 20011012 A 3350 86210144 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 ANC - DURING MAINTENANCE FOUND EMERGENCY EXIT LIGHT AT ROW 5 AND 8 INOPERATIVE. REMOVED AND REPLACED BATTERIES OPERATIO NAL CHECK NORMAL. (M) 2 L 7 2 4F A16WE 2002011500211 20020115 00211 NM 2002 1 15 ASAA0140598 1 20011014 A 3350 86210144 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING MAINTENANCE, FOUND EMERGENCY SMOKE BARRIER EXIT INOPERATIVE. REMOVED AND REPLACED BATTERIES OPERATIONAL CH ECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2002011500212 20020115 00212 NM 2002 1 15 ASAA0140615 1 20011016 A 5320 654687781 WEB BOEING 737 7372Q8C 138448S NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING C-CHECK, FOUND SHEAR BEAM WEB TEMPORARY REPAIR AT STATION 727 LBL 65 AND WL 190. REPLACED SHEAR BEAM WEB I AW SRM. (M) 2 L 7 2 4F A16WE 2002011500213 20020115 00213 NM 2002 1 15 ASAA0140616 1 20011016 A 5310 6546534 SHEAR TIE BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING C-CHECK, FOUND CORROSION ON SHEAR TIE AT STATION 520 BETWEEN STRINGER 26L AND 27L. REPAIRED SHEAR TIE IAW SRM. (M) 2 L 7 2 4F A16WE 2002011500214 20020115 00214 NM 2002 1 15 ASAA0140617 1 20011016 A 5311 65C33510 FRAME BOEING 737 7372Q8C 138448S NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING C-CHECK, FOUND FRAME DENT AT STATION 420 AND STRINGER 24L. REPAIRED FRAME IAW SRM. (M) 2 L 7 2 4F A16WE 2002011500215 20020115 00215 NM 2002 1 15 ASAA0140618 1 20011016 A 5230 6546921172 DOOR FRAME BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING C-CHECK, FOUND CORROSION AT FORWARD CARGO DOOR END FRAME 15 INCHES TO 34 INCHES FROM FORWARD EDGE. REPLACE D IAW SRM. (M) 2 L 7 2 4F A16WE 2002011500216 20020115 00216 NM 2002 1 15 ASAA0140619 1 20011016 A 5230 6546921183 ANGLE BOEING 737 7372Q8C 138448S NM CARGO DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING C-CHECK, FOUND FORWARD CARGO DOOR LOWER FRAME WEB OUTER SKIN ANGLE AT LOWER FORWARD DOOR STAY FITTING CRACK ED. REPLACES WEB IAW EA. (M) 2 L 7 2 4F A16WE 2002011500217 20020115 00217 NM 2002 1 15 ASAA0140620 1 20011016 A 5320 6935352 STRINGER CLIP BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING C-CHECK, FOUND CORROSION ON STRINGER CLIP AT BS 986.5 AND STRINGER 27R. REPLACED CLIP AND STRINGER IAW SRM . (M) 2 L 7 2 4F A16WE 2002011500218 20020115 00218 WP 2002 1 15 ASAA01800308 1 20011207 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 976AS 53452 PDX - DURING LINE MAINTENANCE CHECK, THE TAILCONE EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED ASSOCIA TED BATTERY PACK. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2002011500219 20020115 00219 WP 2002 1 15 ASAA0180284 1 20011014 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 948AS 53021 SEA - DURING PREFLIGHT CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE IN FIRST CLASS CABIN. RECONNECTED M ODULE. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002011500220 20020115 00220 WP 2002 1 15 ASAA0180285 1 20011016 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 SEA - DURING PREFLIGHT CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE IN FIRST CLASS CABIN. REPLACED LIGH T MODULE AND CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002011500221 20020115 00221 WP 2002 1 15 ASAA0180291 1 20011019 A 3350 0105606 MODULE DOUG DC9 DC982 3022082 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 933AS 49234 SEA - DURING PRE-FLIGHT CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE IN FORWARD CABIN. RECONNECTED LOOS E LIGHT MODULE. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2002011600004 20020116 00004 EA 2002 1 16 CA011019019 1 20011003 A 3230 75000600 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NLG FAULTY W O OTHER J WARNING INDICATION AP APPROACH 1 CA (CAN) DURING APPROACH WHEN THE LANDING GEAR WAS SELECTED DOWN, THE NOSE LANDING GEAR (NLG) DID NOT COME DOWN AND THE WAR NING MESSAGE "GEAR DISAGREE" WAS POSTED. THE CREW SELECTED THE MANUAL GEAR RELEASE HANDLE AND THE NLG CAME DOWN. THE AIR CRAFT LANDED WITH NO FURTHER ANOMALIE.MAINTENANCE: IT WAS FOUND THAT THE NLG SELECTOR VALVE WAS FAULTY, NLG SELECTOR VAL VE WAS REPLACED AND TESTED SERVICEABLE PER THE AMM. AIRCRAFT HOURS: 10365, A/C CYCLES: 10456 2 L 7 2 4F 4 F RT A21EA E15NE 2002011600005 20020116 00005 EA 2002 1 16 CA011019021 1 20010923 A 5610 601R3303311 WINDOW CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT FAILED W B EMER. DESCENT O OTHER CR CRUISE 1 CA (CAN) PILOT REPORT DURING FLIGHT LT COCKPIT WINDOW INNER PLY SHATTERED. PILOT CARRIED OUT THEIR QRH. MAINTENANCE REMOVED AND REPLACED LT COCKPIT WINDOW.AIRCRAFT BACK IN SERVICE. SERIAL NUMBER: 9929H2174 2 L 7 2 4F 4 F RT A21EA E15NE 2002011600009 20020116 00009 NE 2002 1 16 CA011022001 2 20011011 A 7530 HTE4500019 CHECK VALVE AIRBUS 330 A330243 3930330 EU RROYCE RB211 RB211TRENT77 NE NR 2 ENGINE STUCK W C ABORTED TAKEOFF X J ENGINE FLAMEOUT WARNING INDICATION TO TAKEOFF 1 CA (CAN) NR 2 ENGINE - STALL ECAM WARNING DURING ENGINE SPOOL-UP ON TAKE OFF ROLL. ON ENGINE INSPECTION, THEY FOUND THE PIV OT ATTACHMENT DETACHED , RESULTING IN VALVE NOT CLOSING , THE RESULT BEING H/P COMPRESSOR AIR BACK FEED TO THE I/P COMPR ESSOR AIR CAUSING A COMPRESSOR STALL. THE ENGINE WAS INSPECTED IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE INTERMEDIA TE PRESSURE CHECK VALVE WAS REPLACED AND A GROUND RUN WAS CARRIED OUT SERVICEABLE. NOTE: NR 1 ENGINE I/P CHECK VALVE WAS INSPECTED AS A PRECAUTIONARY MEASURE AND WAS FOUND SERVICEABLE. 2 L 7 2 4F 4 F RT A46NM E39NE 2002011600012 20020116 00012 NM 2002 1 16 CA011025001 1 20011016 A 6120 CONTROLLER DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF23 NE PROP FEATHER MALFUNCTIONED W E ENGINE SHUTDOWN R E PARTIAL RPM/PWR LOSS VIBRATION/BUFFET CR CRUISE 1 CA (CAN) UN-COMMANDED AUTO FEATHER DURING CRUISE FLIGHT . NR 2 ENGINE SHUTDOWN , AIRCRAFT RETURNED TO DEPARTURE BASE . MAI NTENANCE REPLACED NR 2 ENGINE & PROP ASSEMBLIES , INVESTIGATION INTO CAUSE ONGOING. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011600014 20020116 00014 EU 2002 1 16 CA011025003 1 20011022 A 2897 MS3456L3273P CONNECTOR MS3456L327 BRAERO 748 HS7482A 4231001 EU RROYCE DART DART5342 EU BOOST PUMP SHORTED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING GROUND HANDLING THE LT FUEL BOOST PUMP LOW PRESSURE LIGHT WAS OBSERVED TO BE ILLUMINATED WITH THE A/C NOT P OWERED. INVESTIGATION REVEALED THE PROBLEM WAS LOCATED IN THE PL3 WING ROOT CONNECTOR. AN INTERNAL SHORT WAS ALLOWING TH E LOW PRESSURE LIGHT SEE POWER FROM THE LP FUEL COCK CIRCUIT. THIS IS THE THIRD OCCCURENCE OF A SIMILAR TYPE DEFECT AT T HE SAME CONECTOR LOCATION. THE CONNECTOR IS INSTALLED IAW STC SA-0059. 2 L 7 2 3T 4 T A24EU A196 2002011600032 20020116 00032 NM 2002 1 16 CA011029018 1 20011019 A 5541 85540012103 SKIN DHAV DHC8 DHC8106 2809020 NM RUDDER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 23831 (CAN) THE PROBLEM WAS IDENTIFIED DURING "C1, 40,000 CYCLE INSP., 12M, 24M". INSPECTION OF THE ZONAL CARD "323E - EXTERNA L GENERAL VISUAL INSPECTION OF FORE RUDDER", WAS FOUND TO HAVE A CRACKED SKIN AT STA Z335.500. FURTHER INSPECTION OF THI S AREA INDICATED THE UPPER CLOSING RIB P/N 85540027-001 (IPC REF. 55-40-11, FIG.1, ITEM 8) WAS CRACKED AS WELL.POSSIBLE CAUSE: UNKNOWN.REPAIR PERFORMED: REPAIRED IAW DHC-8 RD 8-5-355 ISS. 2 AND REPLACED CLOSING RIB IAW DHC-8 SRM 51-0-00 & 5 1-40-11. 2 H 7 2 4T RT A13NM 2002011600033 20020116 00033 EU 2002 1 16 CA011029019 1 20011028 A 2497 MS3456L3273P CONNECTOR BRAERO 748 HS7482A 4231001 EU RROYCE DART DART5342 EU ROTOL R4304 R2124304 EU ELECTRICAL DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING INSPECTION DUE TO PREVIOUS PROBLEM IN THIS AREA SEVERAL SUSPECT OBSERVATIONS WERE MADE. CONNECTOR PL3 OVERH EATING/AND OR CORROSION INDICATIONS ON PIN 4,5,23,AND 24. PL10 PINS 23,24 INDICATION OF OVERHEATING/AND OR CORROSION AND PL11 CONNECTOR OIL AND WATER INGRESS.AIRCRAFT IS AOG DUE PARTS. 2 L 7 2 3T 4 T A24EU A196 6 C P899 2002011600040 20020116 00040 WP 2002 1 16 CA011030006 2 20011011 A 7260 31035851 HOUSING BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110UG 01514 WP GEARBOX SCORED W E A ENGINE SHUTDOWN UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 CA (CAN) WHILE IN CRUISE AT 18,000 FT, CREW EXPERIENCED LOSS OF POWER ON LT ENGINE. PRIOR TO LOSS OF POWER CREW DID NOT RPT ANY UNUSUAL IND.S. CREW FEATHERED & SECURED ENGINE & LANDED AT NEAREST AVAILABLE FACILITIES. MAINTENANCE REPORTED THAT ENGINE NOT SEIZED, BUT THAT UNUSUAL NOISE CAN BE HEARD FROM GEARBOX AREA UPON ENGINE ROTATION. SUBSTANTIAL AMOUNTS OF NON-FERROUS MATERIAL, ALONG WITH LESSOR AMOUNTS OF FERROUS MATERIAL, FOUND IN ENGINE MAIN OIL FILTER. CHIP DETECTOR CON TAINED SMALL AMOUNTS OF FERROUS MATERIAL. ENGINE REMOVED & IS PRESENTLY ON STAND AT ENGINE SHOP IN WINNIPEG, MAN. PRELIM INARY TEAR DOWN INVESTIGATION REVEALED THAT IDLER GEAR ASSY BEARING FAILED. 2 L 7 2 4T 4 T RT A21EU E4WE 2002011600043 20020116 00043 NE 2002 1 16 CA011031003 2 20011009 A 7200 3012347 TORQUEMETER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE ENGINE ERODED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) A/C EXPERIENCING REOCCURRING PROBLEMS WITH TORQUE IND. & RUDDER BOOST RELATED SYSS OVER PERIOD OF 30 DAYS. SEVERAL ATTEMPTS TO CORRECT VIA CLEANING & REPLACING OF EXTERNAL COMPONENTS WERE COMPLETED & TEMPORARILY CORRECTED PROBLEMS ON E ACH ATTEMPT.AFTER EXHAUSTING ALL POSSIBLE EXTERNAL CONTRIBUTORS, ENGINE SPLIT AT "C" FLANGE & FROM PT DISC FWD TO "A" FL ANGE, DISASSEMBLIED TO ACCESS TORQUEMETER VALVE. VALVE FOUND TO BE ERRODED OR GROUND DOWN BY APPROX 0.125 INCH. ALLOWED PORTING OF OIL AT UNSPECIFIC & UN-CNTLLED TIMES. "SWARF" BEING CREATED BY GRINDING EFFECTS ALSO MOVING ABOUT CAVITY & CA USING SPORATIC EFFECTS OF PISTON MISALIGNMENT WITH OIL PORTS. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2002011600044 20020116 00044 CE 2002 1 16 CA011031004 1 20010819 A 7110 HOOK BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE RT ENGINE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING ROUTINE MAINT, RIGHT ENGINE UPPER FWD COWL HAD BEEN REMOVED. DURING CLOSE UP, ENGINEER RESPONSIBLE FOR CLOS URE OF COWL INADVERTENTLY SECURED EACH OF 4 CAM-HOOK ASSY TOWARDS RELEASED POS. SHORTLY AFTER TAKEOFF, COWL SEPARATED FR OM ENGINE, STRUCK RT AFT FUSELAGE AREA & GLANCED OFF VERTICAL STAB.FOLLOWUP REVEALED SEVERAL ITEMS: 1) "FEEL" OF CAM-HOO KS IS VERY SIMILAR IN BOTH DIRECTIONS OF OP. 2) DUE TO THE CAM-HOOKS BEING MIRROR IMAGE OF EACH OTHER ON RESPECTIVE SIDE S OF COWL, CLOSING & OPENING DIRECTION ARE REVERSED FOR EACH SIDE. 3) UTILIZING RACHET ASSY FOR MANIPULATION OF HEX BOLT ARTIFICIALLY COVERS OPAL ARROWS P RINTED ON HEX BOLT HEAD.CHANGES TO OPE 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2002011600046 20020116 00046 NM 2002 1 16 CA011031006 1 20010926 A 3260 401020101 PROXIMITY SENSOR DHAV DHC8 DHC8* NM PWC 150 PW150A EA NLG MISINSTALLED W A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 CA (CAN) SELECTING GEAR UP, THE CREW GOT RED LIGHT FOR NOSE GEAR & TRANSITION LIGHT IN GEAR HANDLE. RETURNED FOR LANDING. NOSE GEAR DOWN INDICATION ABOUT 30 SECONDS LATER THAN MAIN GEAR.EARLY INDICATION OF THE NOSE GEAR FORWARD DOORS DID N OT FULLY OPEN DURING GEAR RETRACITON. EVIDENT OF GEAR HITTING THE DOORS IN TRANSIT. THE NOSE GEAR DOWNLOCK SENSORS & T HE PSEU WAS REPLACED. FORWARD NLG DOOR REPAIRED. SYSTEM RTS CARRIED OUT AND AIRCRAFT RETURN TO SERVICE.FOUND: NLG PRO XIMITY SENSORS, IMPROPERLY CRIMPED, THE CRIMP WAS NOT ON THE BARREL OF THECONTACT PIN BUT ACTUALLY CAUGHT PART OF THE BARREL AND PART OF THE WIRE INSULATION. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002011600047 20020116 00047 NE 2002 1 16 CA011031007 2 20011008 A 7530 7821004 SWITCH DHAV DHC8 DHC8* NM PWA PW120 PW123 NE HAMSTD 14SF 14SF23 NE BLEED SYSTEM CONTAMINATED W O OTHER W INADEQUATE Q C CR CRUISE 1 CA (CAN) JUST AFTER LEVEL OFF IN CRUISE FL160, BOTH ENGINES STARTED TO SURGE. TRQ READINGS OSCILLATING BETWEEN 70 & 80 PE RCENT. SURGING CONTINUED FOR ALL POWER SETTINGS ABOVE 25 PERCENT WITH PROPS AT 900&1050. ON SHORT FINAL WHEN PROPS INCRE ASED TO MAX, SURGING APPEARED TO STOP. POWER INCREASED TO 40 PERCENT & NO SURGE FELT OR SEEN. ALL OTHER PARAMETERS NORMA L & WELL WITHIN LIMITS. TURNING TH ENGINE BLEEDS OFF RETURNED BOTH ENGINE PARAMETERS TO NORMAL. ALSO SNAG DID NOT OCCUR ON GROUND UNLESS WOW CB'S WERE PULLED.BOTH 55 PSI SWITCHES WERE REMVD&REPL. BOTH HAD WATER CONTAMINATION INSIDE SWITCH, PARTICULARLY LT SWITCH.A/C FLOWN ON CHECK FLT,&ALL ENGINE PARAMETERS CHECKED STABLE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011600048 20020116 00048 NM 2002 1 16 CA011031008 1 20011009 A 2910 82974219005 LINE DHAV DHC8 DHC8* NM PWC 150 PW150A EA HYDRAULIC SYS RUPTURED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) DURING CLIMB (4,000 FT) NR 1 ENGINE HYDRAULIC PUMP CAUTION LIGHT AFTER 10 SECONDS FURUTHER NR 1 HYD ISO VLV AND TH EN ROLL SPLR AND NR 1 RUD HYD CAUTION LIGHT. FLAP PWR FAILURE. QRH APPLIED. SYSTEM NR 1 AND STANDBY INDICATING ZERO RETU RNED FOR FLAPLESS LANDING. TROUBLESHOOTING REVEALED THE HYDRAULIC LINE FROM NR 1 SPU TO THE FILTER MANIFOLD HAS BEEN RU PTURED AT BONDING CLAMP AREA. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002011600049 20020116 00049 NM 2002 1 16 CA011031009 1 20011016 A 2910 82910009143 TUBE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM LEAKING W D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 CA 29700 (CAN) DURING TAXI TO TAKEOFF, THE FLIGHT CREW NOTICED A STRONG ACID ODOUR IN THE COCKPIT. THE AIRCRAFT RETURNED TO THE G ATE WHERE MAINTENANCE DISCOVERED A LEAKING HYDRAULIC LINE IN THE NLG WHEEL WELL. THE LEAKING HYDRAULIC TUBE WAS THE "CLO SE" PRESSURE LINE TO THE NLG DOORS. THE LINE WAS REPLACED AND ALL FURTHER CHECKS WERE COMPLETED PRIOR TO RELEASING THE A IRCRAFT TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011600050 20020116 00050 NM 2002 1 16 CA011031010 1 20011007 A 2910 82970009387 TUBE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM LEAKING W O OTHER K FLUID LOSS LD LANDING 1 CA 21979 (CAN) THE FLIGHT CREW REPORTED THAT THE NR 2 ENGINE DRIVEN PUMP CAUTION LIGHT CAME ON DURING LANDING GEAR EXTENSION. MAI NTENANCE DISCOVERED THE NR 2 HYDRAULIC SYSTEM HAD AIR IN IT AND ALSO THE NR 2 SPOILER LIFT DUMP PRESSURE LINE BETWEEN TH E LIFT DUMP VALVES WAS LEAKING FROM A PIN HOLE. THE HYDRAULIC TUBE WAS REPLACED, THE SYSTEM WAS BLED AND ALL FURTHER CHE CKS WERE COMPLETED PRIOR TO RELEASING THE AIRCRAFT TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011600061 20020116 00061 EU 2002 1 16 00001 1 20011005 A 3010 14640117 ANTI-ICE VALVE AMD FALC20 FALCON 2720302 EU LT WING STUCK E HAEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 05 148TW 148 LEFT ANTI-ICE VALVE LIGHT REMAINED ILLUMINATED. RETURNED TO DEPARTURE AIRPORT, YIP FOR MAINTENANCE. 2 L 7 2 4F A7EU 2002011600094 20020116 00094 EA 2002 1 16 CA011101001 1 20011010 A 5411 601350061 MOUNT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 17739 (CAN) FOUND CRACK ON ENGINE SUPPORT BEAM WHILE PERFORMING SB A601R-53-059. FOUND CRACKS ON UPPER WEB AT LBL 8 FROM THE F ASTENER TO THE AFT EDGE. RBL 8 (1.5 INCHES LONG) AND LOWER WEB EXTENDING FROM EACH ACCESS PANELS CUTOUTS R/H INBOARD FOR WARD RADIUS 0.25 INCHES LONG. LT INBOARD FORWARD RADIUS 1.75 INCHES LONG. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011600095 20020116 00095 NE 2002 1 16 00002 2 20011004 A 7321 FCU LEAR 24 24 5170302 CE GE CJ610 CJ610* 30006 NE RT ENGINE OUT OF ADJ E HAEA B EMER. DESCENT X ENGINE FLAMEOUT CL CLIMB 1 SW 05 333TW 168 241267 RIGHT ENGINE FLAME-OUT DURING CLIMB FROM 390 TO 410. RESTART AT 240 CLIMB BACK TO 390, NO FURTHER PROBLEM. MAINTENANCE PERFORMED DENSITY ADJUSTMENT. 2 L 7 2 4J 4 J A10CE 1E16 2002011600096 20020116 00096 EA 2002 1 16 CA011101002 1 20011011 A 5210 051940 SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR FAILED W B A EMER. DESCENT UNSCHED LANDING O OTHER CL CLIMB 1 CA 12675 (CAN) DURING A FLIGHT IN CLIMB AT FL220, UN-COMMANDED DEPRESSURIZATION OF THE AIRCRAFT OCCURRED. THE CREW DID AN EMERGEN CY DESCENT TO FL60 AND DIVERTED. THE FLIGHT ATTENDANT NOTICED A LOUD WHISTLE COMING FROM THE PAX DOOR AT THE TIME.AIRCRA FT LANDED WITH NO FURTHER ANOMALIES.ON THE GROUND, THE MAINTENANCE CREW NOTICED THAT THE PASSENGER DOOR SEAL WAS OUT OF ITS TRACK BY APPROXIMATELY 400 MM OF LENGTH. THEY ALSO NOTICED THAT 6 OF THE 8 PRESSURIZATION HOLES WERE MISSING ON THE SEAL. THE SEAL WAS PUT BACK IN PLACE AND THE PRESSURIZATION HOLES DONE PER AMM. A CHECK FLIGHT WAS CARRIED OUT WITH NO A NOMALIES. THE AIRCRAFT WAS PUT BACK IN SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011600097 20020116 00097 NE 2002 1 16 00003 2 20011013 A 7250 6003T47G02 CASE LEAR 24 24D 5170311 CE GE CJ610 CJ610* 30006 NE RT ENGINE CRACKED E HAEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 299TW 24299 241008A RIGHT ENGINE FIRE LIGHT ILLUMINATED DURING CLIMB, REDUCTION IN POWER LIGHT WENT OUT. DIVERTED TO YIP FOR MAINTENANCE. CRACK DISCOVERED IN TURBINE EXHAUST CASE ASSEMBLY. CASE WAS WELD REPAIRED BY ENGINE SHOP. 2 L 7 2 4J 4 J A10CE 1E16 2002011600098 20020116 00098 NE 2002 1 16 00004 2 20011016 A 7200 ENGINE AMD FALC20 FALCON 2720302 EU GE CF700 CF700* 30010 NE LEFT FLAMED OUT E HAEA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 SW 05 232TW 32 304226B DURING CRUISE, LT ENGINE FLAME-OUT AT FLT LEVEL 390. DESCENT TO FL 260, RELIGHT NORMAL & ALL INDICATIONS NORMAL. NO FU RTHER PROBLEM. 2 L 7 2 4F 4 F A7EU E7EA 2002011600101 20020116 00101 WP 2002 1 16 ZW0A0112101 1 20011126 A 5230 RECEPTACLE DOUG DC9 DC983 3022083 WP CARGO DOOR DENTED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 982TW 53632 DURING CHECK-C MAINT THE FWD CARGO DOOR, THE FWD AND LOWER EDGE OF THE DOOR HANDLE RECEPTACLE WAS DENTED. REPAIRED PER SRM 52-05 FIG 30. 2 L 7 2 4F RT A6WE 2002011600102 20020116 00102 WP 2002 1 16 ZW0A0112102 1 20011213 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 912TW 49183 DURING CHECK-C MAINT THE AFT CARGO COMPT, AN INTERCOSTAL WAS CORRODED AT STA 1148 TO 1155, LONGERON 29R TO 30. REMOVED CORRODED PART. INSTALLED SERVICEABLE PART PER SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2002011600103 20020116 00103 WP 2002 1 16 ZW0A0112103 1 20011213 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 912TW 49183 DURING CHECK-C MAINT THE FLOOR AT LBL 55 WAS CORRODED AT SEVERAL AREAS, STA 1106 TO 1190. REPLACED TRACK AT STA 1106 TO 1190 PER SRM 51-10-3, 51-30-1 AND 51-30-8. 2 L 7 2 4F A6WE 2002011600104 20020116 00104 WP 2002 1 16 ZW0A0112104 1 20011210 A 5210 SKIN DOUG DC9 DC983 3022083 WP PAX DOOR GOUGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 931TW 49527 DURING CHECK-C MAINT THE FWD LT PASSENGER DOOR, OUTER SKIN AND INTERNAL STRUCTURE WAS GOUGED AND WORN BELOW THE GUST LOC K RECESS. INSTALLED NEW GUST LOCK HOUSING AND REPAIRED DOOR SKIN PER SRM 52-05, FIG 20A. 2 L 7 2 4F RT A6WE 2002011600105 20020116 00105 WP 2002 1 16 ZW0A0112105 1 20011205 A 5280 DOOR DOUG DC9 DC983 3022083 WP LT MLG CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 983TW 53633 DURING CHECK-C MAINT FOUND 2 INCH CRACK IN THE LT MAIN LANDING GEAR DOOR AT AFT OUTBOARD CORNER. LEFT MLG DOOR REPAIRED ON INTERSHOP WORK ORDER 816804 AND INSTALLED PER SRM 51-00 STANDARD PRACTICES. PARTS INSTALLED WET. 2 L 7 2 4F RT A6WE 2002011600106 20020116 00106 WP 2002 1 16 ZW0A0112106 1 20011211 A 5230 SKIN DOUG DC9 DC983 3022083 WP CARGO DOOR BENT A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 984TW 53634 DURING CHECK-C MAINT THE FWD CARGO DOOR SKIN BELOW THE DOOR HANDLE WAS BENT INWARD. INSTALLED DOUBLER PER SRM 52-05, FI G 30. 2 L 7 2 4F RT A6WE 2002011600107 20020116 00107 WP 2002 1 16 ZW0A0112107 1 20011211 A 5230 SKIN DOUG DC9 DC983 3022083 WP CARGO DOOR BENT A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 984TW 53634 DURING CHECK-C MAINT THE MID CARGO DOOR SKIN BELOW THE DOOR HANDLE WAS BENT INWARD. INSTALLED DOUBLER PER SRM 52-05, FI G 30. 2 L 7 2 4F RT A6WE 2002011600108 20020116 00108 WP 2002 1 16 ZW0A0112201 1 20011214 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 912TW 49183 DURING CHECK-C MAINT IN THE MID CARGO COMPT, STA 540 LONGERON 28L TO 28R, THE AFT FACE OF THE FORMER HAD CORROSION. REM OVED CORROSION PER SRM 51-10-3 AND SPM 6-80-01. MADE AND INSTALLED, TREATED AND PAINTED PARTS, PER SRM 53-03 FIG 2A. 2 L 7 2 4F A6WE 2002011600109 20020116 00109 WP 2002 1 16 ZW0A0112202 1 20011214 A 5320 CLIP DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 912TW 49183 DURING CHECK-C MAINT FOUND CRACK AT AFTER BODY BULKHEAD, RT SIDE, AT BASE OF MOUNT BRACKET FOR RUDDER TRIM ACTUATOR. RE PLACED CLIP PER SPM 6-70-01. 2 L 7 2 4F A6WE 2002011600110 20020116 00110 WP 2002 1 16 ZW0A0112203 1 20011214 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 912TW 49183 DURING CHECK-C MAINT ON CABIN FLOOR, FOUND CORROSION ON FLOORBEAM AT STA 1338, RBL 56. MADE CLIP PER SAMPLE AND DRAWING 9930612. 2 L 7 2 4F A6WE 2002011600111 20020116 00111 WP 2002 1 16 ZW0A0112204 1 20011214 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 912TW 49183 DURING CHECK-C MAINT IN MID CARGO COMPT THE FLOOR SUPPORT INTERCOSTAL WAS CORRODED AT STA 769 TO 788, BETWEEN LONGERON 2 8L TO 27L. REMOVED AND REPLACED CORRODED PART PER SRM 51-10-3, 51-30-2, 51-30-5, AND SPM 6-70-01. 2 L 7 2 4F A6WE 2002011600112 20020116 00112 WP 2002 1 16 ZW0A0112205 1 20011218 A 5240 ATTACH ANGLE DOUG DC9 DC982 3022082 WP SERVICE DOOR CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 912TW 49183 DURING CHECK-C MAINT THE RT FWD SERVICE DOOR INTERNAL HAD CRACKED ATTACH ANGLE, INSIDE UPPER 9 INCH BY 6 INCH LIGHTENING HOLE OF DOOR. FABRICATED AND INSTALLED ATTACH ANGLE CLIP PER BOEING DRAWING 9911579. 2 L 7 2 4F A6WE 2002011600113 20020116 00113 WP 2002 1 16 ZW0A0112206 1 20011215 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 912TW 49183 DURING CHECK-C MAINT FOUND CORROSION BETWEEN STA 1042 AND 1072, LONGERON 30, AROUND FASTENER HOLES IN LONGERON, SEVERAL LOCATIONS. REMOVED CORROSION AROUND FASTENERS BETWEEN STA 1042 AND 1072, AT LONGERON 30, PER SPM 6-80-01 PAGE 1 AND 3. 2 L 7 2 4F A6WE 2002011600114 20020116 00114 EA 2002 1 16 CA011101003 1 20011011 A 2910 LINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE HYD SYSTEM LEAKING W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA (CAN) PILOTS REPORTED HYD 1 LO PRESS CAUTION MESSAGE ON IN FLIGHT. PRESSURE AND QUANTITY AT ZERO. EXECUTED APPROPRIATE C HECK LISTS. ENGINE DRIVEN PUMP RAN DRY FOR 37 MINS. REMOVED AND REPLACED NR 1 EDP IAW 29-13-00 DUE TO BEING RAN DRY. REM OVED AND REPLACED NR 1 SYSTEM RETURN LINE DUE TO PIN HOLE FOUND. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011600115 20020116 00115 WP 2002 1 16 ZW0A0112207 1 20011218 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 912TW 49183 DURING CHECK-C MAINT FOUND CORROSION IN AFT CARGO COMPT ON FORMER AT STA 1322, BETWEEN LONGERON 29L AND 29R. REMOVED CO RROSION AND INSTALLED REPAIR PER SRM 53-03 FIG 2A, 51-30-02 AND 51-30-5. 2 L 7 2 4F A6WE 2002011600116 20020116 00116 EA 2002 1 16 CA011101004 1 20011011 A 7120 601350061 WEB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SUPPORT BEAM CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 17311 (CAN) DURING C-CHECK ZONAL INSPECTION COMPLIED WITH SB 601R-53-059, FOUND A CRACK ON ENGINE SUPPORT BEAM AT THE UPPER WE B FS 640, RBL 18. AREA TO BE REPAIRED IAW REO 601R-53-61-439. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011600117 20020116 00117 WP 2002 1 16 ZW0A0112208 1 20011218 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 912TW 49183 DURING CHECK-C MAINT THE MAIN CABIN FLOOR TRACK WAS CORRODED AT LBL 44, STA 1136 TO 1308. REMOVED AND REPLACED TRACK PE R SPM 6-70-01, SRM 51-10-3, 51-30-2, 51-31-1, AT STA 1136 TO 1308. 2 L 7 2 4F A6WE 2002011600118 20020116 00118 WP 2002 1 16 ZW0A0112209 1 20011218 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 912TW 49183 DURING CHECK-C MAINT IN THE MAIN CABIN THE LT INBOARD FLOOR TRACK WAS CORRODED AT STA 1135 TO 1308. REMOVED AND REPLACE D TRACK PER SPM 6-70-01, SRM 51-10-3, 51-30-2 AND 51-30-1, AT STA 1135 TO 1308. 2 L 7 2 4F A6WE 2002011600119 20020116 00119 EA 2002 1 16 CA011101005 1 20011012 A 2752 854D10012 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS INOPERATIVE W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA (CAN) ON APPROACH, WHEN EXTENDING THE FLAPS, THE FLAP FAIL MESSAGE APPEARED AT 23 DEGREES. THE RIGHT OUTBOARD FLAP TWIST ED, (OUTBOARD ACTUATOR STOPPED TRAVELLING). FOUND THE RT OUTBOARD FLAP TWISTED AND ACTUATOR NR 4 NOT OPERATIONAL. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011600120 20020116 00120 EA 2002 1 16 CA011101006 1 20011012 A 5410 WEB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE SUPPORT BEAM CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 16858 (CAN) FOUND CRACK ON ENGINE SUPPORT BEAM WHILE PERFORMING SB A601R-53-059. FOUND CRACKS AT THREE LOCATIONS ON LOWR WEB A T LBL 36, RBL 36 AND BL 0. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011600121 20020116 00121 WP 2002 1 16 ZW0A0112211 1 20011216 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 912TW 49183 DURING CHECK-C MAINT FOUND EXTERNAL DOUBLER INSTALLED WITH BLIND FASTENERS AT STA 285, LONGERON 23L. INSTALLED SRM REPA IR PER 53-04, FIG 12B. 2 L 7 2 4F A6WE 2002011600122 20020116 00122 EA 2002 1 16 CA011101008 1 20011012 A 5410 601350061 BEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ENGING BAY CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 10850 (CAN) TWO CRACKS FOUND ON ENGINE SUPPORT BEAM. ONE EACH AT THE CUT OUT FOR THE ACCESS PANELS. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011600123 20020116 00123 EA 2002 1 16 CA011101009 1 20011015 A 5410 601350061 WEB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SUPPORT BEAM CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 13408 (CAN) TWO CRACKS FOUND ON ENGINE SUPPORT BEAM AT THE LOWER WEB FS 630, BL R36. WHILE PERFORMING SB A601R-53-059.AREA TO BE REPAIRED IAW REO 601R-53-61-361. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011600124 20020116 00124 WP 2002 1 16 ZW0A0112301 1 20011207 A 5320 GUSSET DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 912TW 49183 DURING CHECK-C MAINT FOUND CRACK IN RT MAIN LANDING GEAR AFT INBOARD DOOR FRAME GUSSET. FABRICATED NEW GUSSET PER DRAWI NG 5936395. INSTALLED PER SRM 51-30. 2 L 7 2 4F A6WE 2002011600125 20020116 00125 EA 2002 1 16 CA011101010 1 20011015 A 5410 601350061 WEB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SUPPORT BEAM CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) TWO CRACKS FOUND ON ENGINE SUPPORT BEAM AT THE LOWER WEB FS 630, LBL 36, WHILE PERFORMING SB A601R-53-059.AREA TO BE REPAIRED IAW RBO 601R-53-61-361. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011600126 20020116 00126 WP 2002 1 16 ZW0A0112302 1 20011221 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 931TW 49527 DURING CHECK-C MAINT LONGERON 2 RT WAS FOUND CRACKED AT STA 1418, 1 INCH LONG. REPAIRED 2R LONGERON PER SRM 53-02, FIG 18. 2 L 7 2 4F RT A6WE 2002011600129 20020116 00129 EA 2002 1 16 CA011101013 1 20011019 A 7603 M8372395R1005N CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE GEAR BOX FAILED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA 19371 (CAN) FOUND CONNECTOR P28EZ AT THROTTLE GEAR BOX SHORTED TO GROUND. REPLACED CONNECTOR AND OPS CHECKED SERVICEABLE. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011600130 20020116 00130 WP 2002 1 16 ZW0A0112303 1 20011221 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 931TW 49527 DURING CHECK-C MAINT LONGERON 2 LT HAD A 1 INCH CRACK AT STA 1418. REPAIRED PER SRM 53-02. 2 L 7 2 4F RT A6WE 2002011600131 20020116 00131 NE 2002 1 16 CA011101015 2 20011029 A 7260 NOASSYPN GEARBOX STBROS SD3 SD360300 EU PWA PT6 PT6A65AR 52043 NE RT HYD SYSTEM LEAKING W O OTHER J WARNING INDICATION AP APPROACH 1 CA 24454 (CAN) DURING LAST 2 MINUTES OF APPROACH THE RT HYDRAULIC PRESSURE DROPPED OFF. AIRCRAFT LANDED UNEVENTFULLY AND WAS TOWE D TO HANGAR. RT HYDRAULIC PUMP WAS REPLACED AND AIRCRAFT GROUND RUN. PRESSURE DID NOT RETURN. FURTHER INVESTIGATION REVE ALED AN INTERNAL ACCESSORY DRIVE GEAR FAILURE. VIEWED THROGH THE OIL FILLER NECK SEVERAL GEARS COULD BE SEEN WITH CHIPPE D TEETH AND ONE GEAR COULD BE SEEN LAYING HORIZONTALLY. 2 H 7 2 4T 4 T RT A41EU E4EA 2002011600132 20020116 00132 EA 2002 1 16 CA011101016 1 20011019 A 2913 848847 PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE HYD SYSTEM FAILED W H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION AP APPROACH 1 CA (CAN) THE CREW REPORTED THAT, HYDRAULIC QUANTITY 3 DROPPED TO ZERO. AIRCRAFT LANDED INTO ZARAGOZA. FINDINGS: PUMP 3A WA S REPLACED AND SYSTEM 3 REPLENISHED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011600133 20020116 00133 2002 1 16 CA011101018 4 20010929 A 3420 AR850 INDICATOR CNDAIR CL601 CL6012A12 1900303 EA GE CF34 CF341A NE COCKPIT FAILED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CA (CAN) SMOKE IN CABIN WHEN AIRCRAFT IS PARKED AT BAGOTVILLE AIRPORT. A FAIL RESISTANCE HAS BEEN FOUND ON THE CABIN DISPL AY ALTITUDE REPORTER WHICH IS USED BY MEDICAL PERSONNEL FOR MEDEVAC PURPOSE ONLY. 2 L 7 2 4F 4 F RT A21AE E15NE 2002011600135 20020116 00135 NM 2002 1 16 ZW0A0112402 1 20011221 A 5330 SKIN BOEING 757 7572Q8 1384972 NM FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 709TW 28168 DURING CHECK-C MAINT THE WINDOW BELT LOWER LAP SEAM AT STA 1618, BELOW STRINGER 14R, HAD SKIN DAMAGE. THE LOWER INNER S KIN WAS CRACKED. REPAIRED PER ARA 17863, PAGE 1 THRU 6. 2 L 7 2 4F RT A2NM 2002011600136 20020116 00136 EU 2002 1 16 CA011101021 1 20011009 A 2450 SP4677033A CIRCUIT BREAKER AIRBUS 310 A310304 3930339 EU GE CF6 CF680C2* GL CB PANEL FAILED W C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CA (CAN) 1. ON TAKEOFF, FLIGHT CREW HEARD CB'S POP WITH SMELL OF BURNING PLASTIC.2. EMERGENCY DECLARED & AIRCRAFT RETURNED TO YYZ. AIRCRAFT LANDED WITHOUT INCIDENT. 3. UPON INSPECTION CB'S J71J74 & K73 WERE FOUND POPPED WITH VISIBLE SIGNS OF A RCING. ALL CB'S REPLACED & RELECTED SYSTEMS CHECKED SERVICEABLE IAW TSM 24-00-00. 4. NO FURTHER INCIDENT DURING SUBSEQUE NT FLIGHT. 2 L 7 2 4F 4 F RT A35EU E23EA 2002011600137 20020116 00137 NM 2002 1 16 CA011102001 1 20011027 A 7921 COOLER DHAV DHC8 DHC8* NM PWA 120 PW120 NE HAMSTD 14SF 14SF7 NE ENGINE FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 23943 (CAN) LEVELING OFF AT FL 240 AFTER TAKING OFF NR 1 ENG OIL PRESSURE WARNING LIGHT ILLUMINATED WITH ASSOCIATED BELOW 40 P SI IND. ON GAUGE. ENG SHUTDOWN&PROP FEATHERED AS PER CO POLICY, PILOT CONTACTED MOC&ELECTED TO RETURN BACK TO POINT OF D EPTR&LANDED W/O INCID..MAINT ONSITEAND WERE DISPATCHED TO INCOMING A/C UPON INIT INSP THEY DISCOVERED THAT OIL COOLER LE AKING PARTS WERE SENT FROM YHZ INST&TH E ENG GROUND CHECKED SERVICEABLE. A/C DISPATCHED BACK INTO SERVICE W/O FURTHER IN CID.. ONCE OIL COOLER BACK IN YHZ IT PRESSURE TESTED WHICH REVEALED THAT WELD ON ONE OF TANKS HAD RUPTURED 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011600138 20020116 00138 WP 2002 1 16 ZW0A0200101 1 20011221 A 5240 ATTACH ANGLE DOUG DC9 DC982 3022082 WP SERVICE DOOR CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 912TW 49183 DURING CHECK-C MAINT THE FWD SERVICE DOOR AFT LOWER CORNER HAD CORROSION ON ATTACH ANGLE INSIDE 1.5 INCH BY 2.5 INCHES A T LIGHTENING HOLE. REMOVED CORROSION PER SPM 6-80-01. REPLACED INTERCOSTAL PER SPM 6-70-01. 2 L 7 2 4F A6WE 2002012900048 20020129 00048 NM 2002 1 29 02FDEA00042 1 20011227 A 5311 FRAME BOEING 727 7272S2F 1384O81 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 205FE 22927 FRAME DENTED I/B FLANGE. REMOVED AND REPLACED FRAME PER SRM 53-10-1 & EA 7-5310-62672. 2 L 7 3 4F A3WE 2002012900051 20020129 00051 NM 2002 1 29 02FDEA00043 1 20011227 A 5311 FRAME BOEING 727 7272S2F 1384O81 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 205FE 22927 FRAME DENTED I/B FLANGE. REMOVED AND REPLACED FRAME PER SRM 53-10-1, 51-40-3 & EA 7-5310-62672. 2 L 7 3 4F A3WE 2002012900052 20020129 00052 NM 2002 1 29 02FDEA00045 1 20011229 A 5330 SKIN BOEING 727 7272S2F 1384O81 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 205FE 22927 MECHANICAL DAMAGE ON EXTERNAL FUSELAGE SKIN AT BS 720A AT STR 23L. REMOVED AND REPLACED SKIN PER SRM 53-30-3. 2 L 7 3 4F A3WE 2002011600147 20020116 00147 NM 2002 1 16 AWXA200200038 1 20011230 A 5330 655298871 SKIN BOEING 737 7373S3 1384711 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 MCN - MAJOR REPAIR - "C" - DURING C-15 CHECK MAINTENANCE FOUND A 1 1/2" CRACK AT THE L2 DOOR FWD LOWER CUTOUT THAT EXTEN DS OUT OF A COUNTER SUNK SCREW HOLE BS 960, CRACK WAS VERIFIED BY HFEC INSPECTION. MAINTENANCE CUTOUT CRACKED AREA OF OU TER SKIN AND FABRICATED A FILLER, -1 INNER PLATE DOUBLER, -2 PLATE DOUBLER, AND -3 OUTER PLATE DOUBLER AND INSTALLED REP AIRS AT BS 960 IAW AWA ER 03-5361-02014-TB2. 2 L 7 2 4F RT A16WE 2002011600148 20020116 00148 NM 2002 1 16 AWXA200200039 1 20011231 A 5330 65272571 SKIN BOEING 737 7373S3 1384711 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 MCN - MAJOR REPAIR - "C" - DURING C-15 CHECK 1" CRACK IN FUSELAGE EXTERNAL SKIN WAS FOUND AT THE L1 DOOR LOWER AFT CORNE R OF CUTOUT BS 339.5, CRACK CONFIRMED BY 10X VISUAL AND HFEC INSPECTION. MAINTENANCE STOP DRILLED CRACK AT L1 DOOR CUTOU T LOWER AFT CORNER BS 339.5 AND PERFORMED HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED. FABRICATED AND INSTALLED REPAIR DOUBLER AND STRAP IAW AWA ER 03-5311-02014-SS1. 2 L 7 2 4F RT A16WE 2002011600153 20020116 00153 NM 2002 1 16 AWXA200200023 1 20011228 A 5312 6545409245 PRESSURE PANEL BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 MCN - MAJOR REPAIR - C - DURING C-17 CHECK A 1.5 INCH CRACK WAS FOUND ON THE LT WHEEL WELL PRESSURE WEB AT BS 664, LBL 3 4. MAINTENANCE CUT OUT DAMAGED AREA OF PRESSURE WEB AND PERFORMED HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED. FABRI CATED A DOUBLER, FILLER, AND STIFFENER AND INSTALLED REPAIRS IAW B737-300 SRM 51-40-02, AWA ER 03-5310-02011-ES2. 2 L 7 2 4F RT A16WE 2002011600154 20020116 00154 NM 2002 1 16 AWXA200200024 1 20011228 A 5315 654881138 FLOORBEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 MCN - MAJOR REPAIR - C - DURING C-17 CHECK MAINTENANCE DISCOVERED CORROSION ON FLOORBEAM UPPER FLANGE AT BS 986, RBL 17. REMOVED DAMAGED AREA OF FLOORBEAM UPPER T-CHORD AT BS 986, FABRICATED 2 SPLICE STRAPS, REPAIR ANGLES, NEW UPPER T-CHO RD AND INSTALLED REPAIRS IAW AWA ER 03-5310-02011-ES4. 2 L 7 2 4F RT A16WE 2002011600160 20020116 00160 NM 2002 1 16 DL777011940 1 20011213 A 3233 161W10201 PIN BOEING 777 777232 1385232 NM LT & RT MLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 864DA 29736 CORROSION FOUND ON BOTH LT AND RT LANDING GEAR RETRACT ACTUATOR ATTACH PINS. REPLACED BOTH LEFT AND RIGHT HAND ACT PINS IAW M/M WITH NEW ONES. 2 L 7 2 4F RT T00001SE 2002011600161 20020116 00161 NM 2002 1 16 DLM11011971 1 20011222 A 3320 0200463003 LIGHT DOUG MD11 MD11 3023602 NM CABIN DEFECTIVE A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 803DE 48474 SEAT 35B READING LIGHT WOULD NOT TURN OFF AND SMOKED FOR FEW MINUTES. SMOKE CEASED BEFORE C/B WAS PULLED. REPLACED LAM P ASSY. 2 L 7 3 4F RT A22WE 2002011600162 20020116 00162 NM 2002 1 16 DLM11011986 1 20011229 A 3350 6044115 BATTERY PACK DOUG MD11 MD11 3023602 NM CABIN DISCHARGED A DALA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 27 815DE 48624 EMERGENCY LIGHT BATTERY 6 LOW MESSAGE ON EMERGENCY TEST. REPLACED BATTERY PACK/POWER SUPPLY ASSY. 2 L 7 3 4F RT A22WE 2002011600164 20020116 00164 2002 1 16 DLM88011949 4 20011217 A 2565 3961899501 LANYARD DOUG MD88 MD88 3023688 NM EVAC SLIDE BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 905DL 49536 L2 DOOR SLIDE LANYARD BROKEN. INSTALLED NEW LANYARD. 2 L 7 2 4F RT A6WE 2002011600165 20020116 00165 NM 2002 1 16 DLM88011955 1 20011218 A 3350 SOCKET DOUG MD88 MD88 3023688 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 945DL 49818 PASSENGER SEAT 30D EMERGENCY TRACK LIGHTS INOP. REPLACED SOCKET ASSY, OPS CHECKS NORMAL. 2 L 7 2 4F RT A6WE 2002011600166 20020116 00166 NM 2002 1 16 DLM88011961 1 20011219 A 2150 20495062 ACM DOUG MD88 MD88 3023688 NM A/C BAY LEAKING A DALA O OTHER K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 937DL 49810 LEFT AFT LAV SMOKE DETECTOR ACTIVATED MOMENTARILY DURING INITIAL CLIMB. SLIGHT SMOKE SMELL, BUT NONE VISIBLE. FOUND RT ACM LEAKING OIL INTERNALLY. REPLACED ACM PER M/M. 2 L 7 2 4F RT A6WE 2002011600167 20020116 00167 EU 2002 1 16 QXEA0102080 1 20011214 A 5710 STRUCTURE FOKKER F28 F28MK4000 4990810 EU RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - SUSPECTED CRACK IN WING STRUCTURE RADIATING FROM LOWER SMALL BOLT LOCATED OUTBOARD OF RIGHT MAIN LANDING GEAR AFT TRUNNION POINT AT WS 117.165. REPAIRED IAW FOKKER SRM 51-35-02, PARAGRAPH 2 C (3), PAGE 2 AND SRM 57-02-09, PAGE 2, PAR AGRAPH 3. 2 L 7 2 4F RT A20EU 2002011600168 20020116 00168 EU 2002 1 16 QXEA0102081 1 20011209 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CASTELLATION ON AFT SIDE OF FRAME 13815B BETWEEN STRINGERS 2 AND 3 HAS A CRACK IN THE RADIUS. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002011600169 20020116 00169 EU 2002 1 16 QXEA0102082 1 20011209 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CASTELLATION ON AFT SIDE OF FRAME 13815B BETWEEN STRINGERS 72 AND 73 IS CRACKED IN RADIUS. REPAIRED IAW FOKKER SR M 51-31-01. 2 L 7 2 4F RT A20EU 2002011600170 20020116 00170 EU 2002 1 16 QXEA0102083 1 20011213 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CASTELLATION ON AFT SIDE OF FRAME 13815A BETWEEN STRINGERS 3 AND 2 HAS A CRACK IN THE RADIUS AND A CRACK FROM RIVE T WITH WASHER. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002011600171 20020116 00171 EU 2002 1 16 QXEA0102084 1 20011213 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CASTELLATION ON AFT SIDE OF FRAME 13815A BETWEEN STRINGERS 72 AND 73 IS CRACKED ALONG RIVET LINE. REPAIRED IAW FO KKER SRM 53-02-13 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002011600172 20020116 00172 EU 2002 1 16 QXEA0102085 1 20011212 A 5320 TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CROSSTIE NICKED AT FRAME 7305 AND STRINGER 1. REPAIRED IAW FOKKER SRM 51-31-01, SRM 51-30-02 AND SRM 51-31-05. 2 L 7 2 4F RT A20EU 2002011600173 20020116 00173 EU 2002 1 16 QXEA0102086 1 20011208 A 5320 TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CROSS TIE CRACKED AT FRAME 4900 AND STRINGER 73. REPAIRED IAW FOKKER SRM 51-31-05. 2 L 7 2 4F RT A20EU 2002011600174 20020116 00174 EU 2002 1 16 QXEA0102087 1 20011208 A 5320 TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CROSS TIE CRACKED AT FRAME 4900 AND STRINGER 74. REPAIRED IAW FOKKER SRM 51-31-05. 2 L 7 2 4F RT A20EU 2002011600175 20020116 00175 EU 2002 1 16 QXEA0102088 1 20011208 A 5320 TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CROSSTIE CRACKED AT FRAME 4900 AND STRINGER 1. REPAIRED IAW FOKKER SRM 51-31-05. 2 L 7 2 4F RT A20EU 2002011600176 20020116 00176 EU 2002 1 16 QXEA0102089 1 20011208 A 5320 TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CROSS TIE CRACKED AT FRAME 4900 AND STRINGER 5. REPAIRED IAW FOKKER SRM 51-31-05. 2 L 7 2 4F RT A20EU 2002011600177 20020116 00177 EU 2002 1 16 QXEA0102090 1 20011214 A 5320 BRACKET FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - FRAME TO SKIN CONNECTION ANGLE BRACKET CRACKED APPROXIMATELY 1 INCH IN LENGTH AT FRAME 50-2 AND STRINGER 27. REPA IRED IAW FOKKER SRM 51-31-01 PAGE 9. 2 L 7 2 4F RT A20EU 2002011600178 20020116 00178 EU 2002 1 16 QXEA0102091 1 20011214 A 5320 BRACKET FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - FRAME TO SKIN CONNECTION ANGLE BRACKET CRACKED APPROXIMATELY .5 INCH IN LENGTH AT FRAME 50-2 AND STRINGER 31. REP AIRED IAW FOKKER SRM 53-10-05 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002011600179 20020116 00179 EU 2002 1 16 QXEA0102092 1 20011213 A 5320 BRACKET FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - FRAME TO SKIN CONNECTION ANGLE BRACKET CRACKED APPROXIMATELY .75 INCH IN LENGTH AT FRAME 32-2 AND STRINGER 48. RE PAIRED IAW FOKKER SRM 53-02-13, PAGE 5 AND SRM 53-10-5, PAGE 601. 2 L 7 2 4F RT A20EU 2002011600180 20020116 00180 EU 2002 1 16 QXEA0102093 1 20011213 A 5320 BRACKET FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - FRAME TO SKIN CONNECTION ANGLE BRACKET CRACKED APPROXIMATELY .75 INCH IN LENGTH AT FRAME 32-2 AND STRINGER 27. RE PAIRED IAW FOKKER SRM 53-02-13, PAGE 5 AND 53-10-5, PAGE 601. 2 L 7 2 4F RT A20EU 2002011600181 20020116 00181 EU 2002 1 16 QXEA0102094 1 20011214 A 5320 BRACKET FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - FRAME TO SKIN CONNECTION ANGLE BRACKET CRACKED APPROXIMATELY .75 INCH IN LENGTH AT FRAME 17565 AND STRINGER 8. RE PAIRED IAW FOKKER SRM 53-02-13, PAGE 5 AND SRM 53-02-13. 2 L 7 2 4F RT A20EU 2002011600182 20020116 00182 EU 2002 1 16 QXEA0102095 1 20011213 A 5320 BRACKET FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - FRAME TO SKIN CONNECTION ANGLE BRACKET CRACKED APPROXIMATELY 1.125 INCH AT FRAME 17565, BETWEEN STRINGER 22 AND 23 . REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 B AND C, AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002011600183 20020116 00183 EU 2002 1 16 QXEA0102096 1 20011213 A 5320 BRACKET FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - FRAME TO SKIN CONNECTION ANGLE BRACKET CRACKED APPROXIMATELY 0.5 INCH IN LENGTH AT FRAME 17565 AND STRINGER 51. R EPAIRED IAW FOKKER SRM 53-02-13, PAGE 5. 2 L 7 2 4F RT A20EU 2002011600184 20020116 00184 EU 2002 1 16 QXEA0102097 1 20011213 A 5320 BRACKET FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - FRAME TO SKIN CONNECTION ANGLE BRACKET CRACKED APPROXIMATELY .5 INCH IN LENGTH AT FRAME 17565 AND BETWEEN STRINGER 52 AND 53. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5. 2 L 7 2 4F RT A20EU 2002011600185 20020116 00185 EU 2002 1 16 QXEA0102098 1 20011212 A 5330 RIVET FOKKER F28 F28MK4000 4990810 EU FUSELAGE LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - ONE LOOSE RIVET IN FUSELAGE SKIN AT FRAME 67-2 ABOVE STRINGER 229. REPAIRED IAW FOKKER SRM 51-30-02. 2 L 7 2 4F RT A20EU 2002011700020 20020117 00020 NM 2002 1 17 CA011108006 1 20010927 A 3010 8SC0029029 BOOT DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE DEICE SYSTEM TORN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING ROUTINE INSPECTION, MAINTENANCE DISCOVERED THAT THE LT NR 3 LEADING EDGE DEICE BOOT HAD A 2 INCH RIP IN IT . THIS DEICE BOOT HAD ONLY BEEN IN SERVICE FOR 314 DAYS SINCE INSTALLATION. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011700022 20020117 00022 EA 2002 1 17 CA011108008 1 20011029 A 5720 2153003158 ANGLE CNDAIR CL215 CL2151A10 1900320 EA WING CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WHILE CARRYING OUT INSP CALLED UP IN "B" CHECK TECHNICIAN NOTICED CRACK IN RADIUS OF RT FWD DRAG ANGLE P/N 215-300 31-59. INSPECTION OF OTHER DRAG ANGLES ON SAME A/C REVEALED FWD LT DRAG ANGLE WAS CRACKED IN SAME AREA. CRACK LENGTH ON BOTH LT & RT DRAG ANGLES APPROX 1.5 IN IN LENGTH. REMAINING 3 A/C WERE INSP & NO FAULTS WERE NOTED. DRAG ANGLES WERE PRE V REWORKED TO ALLOW COMPLIANCE WITH SB 215-A463 (AD CF-93-07) ON LOWER WING SPARTANG. SB STATES SHOULD BE 0.750 RADIUS F OR CUTOUT. THESE RADII WERE TIGHTER THAN INSTRUCTIONS & ARE VISIBLE SIGNS OF MACHINING MARKS. AFFECTED DRAG ANGLES WILL BE REPLACED WITH NEW PARTS. 2 H 7 2 4R RT A14EA 2002011700026 20020117 00026 EA 2002 1 17 CA011108010 1 20011031 A 5712 21511002822 RIB CNDAIR CL215 CL2151A10 1900320 EA LT WING DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WHILE ATTEMPTING TO REMOVE WIRE FROM FLEXIBLE CONDUIT TECHNICIAN NOTICED THAT FLEXIBLE CONDUIT HAD BEEN BURNT. UPO N CLOSER INSP FOLLOWING NOTED: 1) HOME MADE PLASTIC CABLE BLOCK (FAIR LEAD) INST 2) FRESH PRIMER WAS BRUSHED ON SEVERAL AREAS INCLUDING WING SPAR. 3)RIB P/N 215-11014-822 IS WRINKLED. 4)3 STRINGERS HAVE BEEN AFFECTED BY HEAT DAMAGE. 5)WIRE BUNDLE SHOWS SIGN OF SMOKE. 6)ONE PIECE OF ANTI CHAFING MATERIAL (CATERPILLAR STRIP) SHOWS SIGNS OF MELTING. NDT CONTRAC TOR COMPLETED CONDUCTIVITY TEST TO DETERMINE STRUCTURAL INTEGRITY OF AREA. WING SPAR TESTED SERVICEABLE, RIB, FALSE RIB, &3 STRINGERS HAVE BEEN HEAT DAMAGED. REQD REPAIRS WILL BE COMPLETED ON A/C PRIOR TO FURTHER FLT. 2 H 7 2 4R RT A14EA 2002011700035 20020117 00035 NM 2002 1 17 HNAA0200003 1 20011118 A 2900 50841 SHUTTLE VALVE DHAV DHC8 DHC8102 2809003 NM INOPERATIVE A HNAA K NONE K FLUID LOSS NR NOT REPORTED 1 EA 07 908HA 43021 015 #1 AND #2 HYDRAULIC SYSTEMS FLUID LOSS. #2 RUDDER ISO VALVE CAUTION LIGHT ILLUMINATED. HYD PRESSURES NORMAL. ON LANDING NORMAL BRAKES FAILED. FOUND LEAK AT #3 BRAKE. #3 SHUTTLE VALVE FAILURE ALLOWED FLUID LOSS FROM BOTH HYD SYSTEMS. REPLACE D #3 SHUTTLE VALVE. 2 H 7 2 4T RT A13NM 2002011700044 20020117 00044 NM 2002 1 17 CA011109015 1 20011104 A 2420 82450026 CONTACTOR DHAV DHC8 DHC8* NM PWA PW120 PW123 NE HAMSTD 14SF 14SF23 NE ELECTRICAL BURNED W O OTHER H ELECT. POWER LOSS-50 PC CR CRUISE 1 CA (CAN) SPU AUXILIARY POWER LIGHT WAS FLICKERING IN FLIGHT. INVESTIGATION CARRIED OUT AND THREE 12 AWG WIRES FOUND CHAFED / BURNT INSIDE THE NR 2 AC CONTACTOR BOX. THE WIRE IDENTS ARE AS FOLLOWS:20005B12C-1, 20003B12B-1 AND 20001B12A-1. THES E WIRES GO BETWEEN CIRCUIT BREAKERS CB8 AND CB6 IN THE RT AC CONTACTOR BOX. THE CHAFF WAS FROM A BOLT ATTACHING A TERMIN AL BLOCK TO THE BACK OF THE CONTACTOR BOX. REPAIR CARRIED OUT. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011700046 20020117 00046 NE 2002 1 17 CA011113001 2 20011102 A 7261 6087T4P05 PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ENGINE OIL FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CR CRUISE 1 CA (CAN) ENGINE FLIGHT SHUT DOWN DUE TO "ENGINE OIL PRESS" MESSAGE AND "ENGINE OIL" AURAL MESSAGE ON THE LEFT ENGINE. THE A IRCRAFT WAS CRUISING AT FL410.OIL LEVEL CHECKED WITHOUT REMARKS, OIL FILTER AND CHIP DETECTOR CHECKED WITHOUT REMARKS, B SUMP SCAVENGES SCREENS CHECKED WITHOUT REMARKS AND GENERAL INSPECTION PERFORMED WITHOUT REMARKS, FINALLY A STATIC ENGIN E RUN UP WAS PERFORMED WITHOUT REMARKS. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011700047 20020117 00047 NM 2002 1 17 CA011113003 1 20011111 A 2910 82970010477 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM SEVERED W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA 22167 (CAN) AFTER TAKE-OFF ONCE THE CREW SELECTED GEAR UP THEY NOTICED THAT THE NR 2 HYDRAULIC QUANTITY WAS AT O. THE A/C RETU RNED TO THE DEPARTURE AIRPORT.INVESTIGATION REVEALED THAT THE MAIN PRESSURE LINE TO THE NR 2 PRESSURE MANIFOLD HAD COMPL ETLY RUPTURED. A TEMPORARY FLEX LINE WAS INSTALLED, SYSTEM TOPPED UP, SYSTEM BLED AND LEAK CHECKS CARRIED OUT. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011700048 20020117 00048 EA 2002 1 17 CA011113004 1 20011022 A 2740 3094334 SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE STAB TRIM FAILED W A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 CA (CAN) DURING FLIGHT 5280 FROM WILKES-BARRE / SCRANTON, PA (AVP) TO CINCINNATI OH (CVG). STAB TRIM & MACH TRIM CAUTION ME SSAGES ON CLIMBOUT. FOLLOWED QRH PROCEDURE AND TRIMS WOULD NOT RESET. DECALRED AN EMERGENCY AND MADE AN UNSCHEDULED LAND ING AT PITTSBURGH, PA (PIT).INTERROGATED MDC AND FOUND CAPTAIN'S TRIM SWITCH FAILED.NOTE: CAPATAIN'S TRIM SWITCH WAS WRI TTEN UP ON OCT 06 BUT DETAILS OF ACTUAL SQUAWK AND FINDINGS ARE NOT KNOWN.R&R'D CAPTAIN'S TRIM SWITCH. CANCELLED FLIGHT 5280. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011700049 20020117 00049 EA 2002 1 17 CA011113005 1 20011024 A 2110 75065917 SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT PACK TEMP FAILED W A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 CA (CAN) AFTER TAKEOFF DURING BLEEDS TRANSFER, LT PACK HI PRESSURE AND RT PACK HI TEMP APPEARED ON EDI.FLIGHT ABORTED. REMO VED AND REPLACED THE RT COMPRESSOR OUTLET TEMP SWTICH. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011700050 20020117 00050 EA 2002 1 17 CA011113006 1 20011113 A 5610 NP1393276 WINDOW CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE COCKPIT CRACKED W O OTHER O OTHER CR CRUISE 1 CA (CAN) FLIGHT DECK RT SIDE WINDOW OUTER PLY CRACKED. AIRCRAFT FERRIED TO WHERE THE WINDOW WAS REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011700053 20020117 00053 EA 2002 1 17 CA011113008 1 20011026 A 2131 808442 BYPASS VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE ACM FAILED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) LT ACM UNCONTROLLABLE IN AUTO OR MANUAL, AFT EQUIPMENT BAY FILLED WITH SMOKE. MCO MAINTENANCE REMOVED AND REPLACED DUEL BYPASS VALVE, DUCT SLEEVE AND COUPLING. ALSO HEAT EXCHANGES WAS REPLACED ON OVERNIGHT IN CVG. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011700054 20020117 00054 EA 2002 1 17 CA011113009 1 20011029 A 7120 60135006 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE ENGINE BAY CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 16212 15921 (CAN) ONE CRACK FOUND ON ENGINE SUPPORT BEAM AT THE LOWER WEB FS 630, BL 0 WHILE PERFORMING SB A601R-53-059.DISCREPANCIE S WILL BE REPAIR USING BOMBARDIER DISPOSITIONS. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011700055 20020117 00055 EA 2002 1 17 CA011113010 1 20011029 A 7120 60135006 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE ENGINE BAY CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 16859 16483 (CAN) CRACKS FOUND AT THREE LOCATIONS ON REPEAT INSPECTION: FS 630, LBL 36 & BL 0 WHILE PERFORMING SB A601R-53-059.DISC REPANCIES WILL BE REPAIR USING BOMBARDIER DISPOSITION. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011700056 20020117 00056 EA 2002 1 17 CA011113011 1 20011029 A 7120 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE ENGINE BAY CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) CRACKS FOUND AT TWO LOCATIONS ON REPEAT INSPECTION: FS 630, LBL 36, RBL 36 WHILE PERFORMING SB A601R-35-059.DISCRE PANCIES WILL BE REPAIR USING BOMBARDIER DISPOSITIONS. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011700058 20020117 00058 EA 2002 1 17 CA011113013 1 20011106 A 2420 ZCDBA023 CONTACTOR CNDAIR CL601 CL6012A12 1900303 EA GE CF34 CF341A NE RT GENERATOR BURNED W O OTHER H Z ELECT. POWER LOSS-50 PC SIGNIFICANT FAILURE REPORT TX TAXI/GRND HDL 1 CA (CAN) AFTER STARTING ENGINES WENT AND TRANSFERED GENRATORS. TURNED ON NR 3A HYD PUMP LARGE POWER SURGE ABOUT 34KVA NR 3 A HYD BREAKER POPPED. TURNED ON NR 1 HYD PUMP, HYD BREAKER POPPED, R/H SIDE WINDOW FAILED. ANY HEAVY LOAD ON RT BUS CR EATED FAILERS. ALSO PROBLEMS WITH NR 1 PITCH TRIM. 2 L 7 2 4F 4 F RT A21AE E15NE 2002011700059 20020117 00059 EA 2002 1 17 CA011113014 1 20011029 A 7120 60135006 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE ENGINE BAY CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 16397 15947 (CAN) CRACK FOUND AT ONE LOCATION ON REPEAT INSPECTION: FS 630, BL 0 WHILE PERFORMING SB A601R-53-059.DISCREPANCIES WILL BE REPAIR USING BOMBARDIER DISPOSITIONS. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011700060 20020117 00060 EA 2002 1 17 CA011113015 1 20011030 A 7120 601350061 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ENGINE BAY CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) FOUND CRACK ON UPPER WEB OF ENGINE SUPPORT BEAM DURING SB A601R-53-059 AT FS 640 NEAR RBL 7.0. CRACK WAS 0.125 INC HES LONG. REPAIRED IAW REO 601R-53-345 (UPPER AND LOWER WEBS). ALSO CARRIED OUT REO 601R-53-61-366 (BOTH SIDES). 2 L 7 2 4F 4 F RT A21EA E15NE 2002011700061 20020117 00061 EA 2002 1 17 CA011113018 1 20011101 A 7120 60135006 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE ENGINE BAY CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 12120 (CAN) CRACK FOUND AT FS 630, BL: LET BL 36. FOUND DURING REPEAT INSPECTION. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011700062 20020117 00062 EA 2002 1 17 CA011113019 1 20011101 A 7120 60135006 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE ENGINE BAY CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 18636 (CAN) FOUND DURING '96 MONTH' INSPECTION CHECK; CRACKED AT FS 640 & BL 00. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011700064 20020117 00064 EA 2002 1 17 CA011113020 1 20011102 A 5321 601R31146 FLOOR PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE CABIN CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 15247 (CAN) A 8 INCH CRACK WAS REPORTED AT FS 520. LBL 36 IN THE PRESSURE FLOOR SKIN 601R31146. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011700065 20020117 00065 2002 1 17 CA011113021 4 20011106 A 3417 8220372140 ADC CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT FAILED W O OTHER H ELECT. POWER LOSS-50 PC CR CRUISE 1 CA (CAN) PRIMARY FLIGHT DISPLAY (PFD) NR 1 AND MULTIFUNCTION FLIGHT DISPLAY (MFD) NR 1, BOTH FLICKERED OFF FOR APPROXIMATEL Y 1-2 MINUTES THEN CAME BACK ON. FMS GETS FMS NAV INVALID ON GROUND. UNABLE TO GET COURSE UNTIL AIRCRAFT INFLIGHT. CAPTA INS PFD LOOSES DATA AND LOTS OF DATA ON DISPLAY. DISPLAY BLANKS ON TAKEOFF AND UNABLE TO GET FMS ENGINE TAKEOFF DATA UNT IL AIRBORNE (ON THRUST LIMITS PAGE).REMOVED AND REPLACED NR 1 ADC IAW CRJ MM 34-13-01. OPS AND LEAK CHECKED GOOD. RAN PF D 1 & MFD NR 1 FOR SEVERAL HOURS, NO FLICKERING NOTED.AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011700066 20020117 00066 EA 2002 1 17 CA011113022 1 20011107 A 2432 237BC1012 CHARGER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BATTERY FAILED W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA (CAN) APU CHARGER STATUS MESSAGE POSTED - CIRCUIT BREAKER POPPED - NO TAXI OUT. WHEN MECHANIC RESET THE C/B THE CONNECTO R PLUG ON TOP OF THE CHARGER CAUGHT FIRE.REPAIRED CONNECTOR PLUG BY REPINNING AND ASSOCIATED WIRES. REPLACED APU BATTERY & CHARGER. AFFECTED COMPONENTS: APU BATTERY CHARGER + BATTERY + CONNECTOR P12PA. BATTERY P/N 4078-3, S/N 082634, TSN: 2 52 HOURS & 254 CYCLES. CONNECTOR P/N MS27473T14B18S. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011700067 20020117 00067 EA 2002 1 17 CA011113023 1 20011105 A 7120 601350061 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ENGINE BAY CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 14363 (CAN) FOUND ON REPAIR INSPECTION. 0.5 INCH CRACK FOUND AT ONE LOCATION ON TIP WEB 7TH RIVET TO THE RIGHT OUT FROM BL 0 ( CLOSE TO RBL 9.50). AIRCRAFT FERRIED FROM CINCINNATI TO HOT SPRINGS FOR REPAIR. WHILE PERFORMING SB A601R-53-059. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011700068 20020117 00068 EA 2002 1 17 CA011113024 1 20011111 A 3310 BVO330002020 SOCKET DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE ROW 2 FAILED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA 23478 (CAN) AFTER DEPLANING THE PASSENGERS THE FLIGHT ATTENDANT NOTED A BURNING SMELL IN FORWARD CABIN AREA.INVESTIGATION REVE ALED THAT THE BULB IN THE CABIN OVERHEAD LIGHTING AT ROW 3 WAS ARCING AT THE AFT SOCKET (PLUNGER TYPE). THE BULB WAS REM OVED AND THE CABIN LIGHTINGAT THIS POSITION DE-ACTIVATED AND DEFERRED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011700069 20020117 00069 EU 2002 1 17 CA011114005 1 20011027 A 3230 UPLOCK AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE MLG OVERSERVICED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) AFTER TAKEOFF, THE "LANDING GEAR NOT UPLOCKED" MESSAGE CAME ON ECAM. GEARS RECYCLED AS PER AOM. NO JOY. AIRCRAFT R ETURNED TO WINNIPEG.LARGE AMOUNT OF GREASE REMOVED FROM MLG UPLOCK 8GA 10GA R/H AS PER CANADIAN TECHNICAL INFORMATION BU LLETIN NO.32-1-98-6 (INCLUDED). EXTENTION AND RETRACTION CARRIED OUT AS PER AMM 32-31-00-500 FREE FALL EXTENTION CARRIED OUT AS PER AMM 32-33-00-500. NIL FAULTS FOUND. AIRCRAFT SERVICEABLE. 2 L 7 2 4F 4 F RT A28NM E29NE 2002011700070 20020117 00070 EA 2002 1 17 CA011114009 1 20011011 A 2750 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE TE FLAPS CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) FLAP FAIL AMBER CAUTION MESSAGE APPEARED DURING APPROACH (SPEED 250 KNOTS, 5000 FT FLAPS SET 0 DEGREES) FOUND CIRC UIT BREAKER 2-F4 TRIPPED. QUICK REFERENCE HANDBOOK PROCEDURE CARRIED OUT AND UNEVENTFUL FLAPLESS LANDING COMPLETED. NOTE : THIS IS LAST OF A LONG LIST OF REPETITIVE SNAGS WITH MANY PARTS CHANGED AND HAVING SNAG REAPPEAR. HEAVY CORROSION FOU ND IN FLAP HARNESS CONNECTOR (2PSCE), HARNESS FROM BPS4 TO 2PSCE REPLACED AND SECURED. TEST FLIGHT CARRIED OUT AND FLAP OPERATION CHECKED SERVICEABLE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011700071 20020117 00071 EU 2002 1 17 CA011114013 1 20010829 A 2751 697657001 GEARBOX AIRBUS A340 A340313 EU CFMINT CFM56 CFM565C4 13802 NE TE FLAPS FAILED W L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 CA (CAN) ON APPROACH, FLAPS 2 SELECTED, FLAPS DID NOT EXTEND. AIRCRAFT WENT AROUND AND LANDED FLAPLESS AND SLATS EXTENDED .FLIGHT CONTROL FLAPS FAULT MESSAGE. AFTER INVESTIGATION FOUND THE TORQUE LIMITERS EXTENDED FOR THE ROTARY ACTUATOR AND THE INPUT GEARBOX. REPLACED THE INPUT GEARBOX AND THE ROTARY ACTUATOR TO BE REPLACED AT THE NEXT C-CHECK. 2 L 7 4 4F 4 F RT A197 E37NE 2002011700100 20020117 00100 CE 2002 1 17 CA011116019 1 20011105 A 3260 D37C15 PRESSURE SWITCH CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG OUT OF ADJUST W O OTHER O OTHER AP APPROACH 1 CA (CAN) DURING TRAINING THE LANDING GEAR WARNING HORN WOULD NOT SOUND WHEN THE AIRCRAFT AIRSPEED WAS BELOW 150 KNOTS. THE AIRSPEED SENSING SWITCH WAS FOUND TO ACTUATE AT 50 KNOTS. THE SWTICH WAS REPLACED AND THE SYSTEM WAS TESTED OK. 2 L 7 2 4F 4 F RT A22CE E25EA 2002011700102 20020117 00102 NM 2002 1 17 DL76S011947 1 20011215 A 5315 654541039 FLOORBEAM BOEING 767 767332 1382001 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 137DL 25306 THE WEB AND LOCAL REINFORCING DOUBLER OF THE LBL 24 LONGITUDINAL FLOORBEAM WAS FOUND CRACKED NEAR AT FS 680. THE CRACKED REINFORCING DOUBLER WAS REMOVED AND WEB CRACK TRIMMED OUT. A NEW REINFORCING DOUBLER WAS INSTALLED AND AN ALUMINUM REP AIR DOUBLER. THE UPPER CAP OF THE FLOORBEAM WAS REINFORCED PER BAC S/B 737-57-1139. THE REPAIR WAS PER ER/A 382279-14A D, REV A. 2 L 7 2 4F RT A1NM 2002011700104 20020117 00104 NM 2002 1 17 DLM88011960 1 20011219 A 3260 833703 SWITCH DOUG MD88 MD88 3023688 NM NLG MALFUNCTIONED A DALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 27 976DL 53257 ON FINAL APPROACH GREEN NOSE GEAR LT DID NOT ILLUMINATE, NO RED LIGHT GEAR WAS CYCLED IAW POM CKLIST WITH SAME RESULT. NOSE GEAR PIN ON THROTTLE QUADRANT INDICATED THE NOSE GEAR WAS DOWN. ON NEXT APPROACH WHEN GEAR WAS LOWERED ALL INDICAT IONS (LTS AND PIN) WERE NORMAL. REPLACED NOSE GEAR LOCKED PROX SW D1-32 AND NOSE GEAR POS INTERLOCK SW S1-412. RAN NOS E GEAR SEVERAL TIMES. ALL INDS NORMAL. OP CHECKS GOOD PER MM. 2 L 7 2 4F RT A6WE 2002011700106 20020117 00106 NE 2002 1 17 DLM88011967 2 20011221 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 SMOKE A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 920DE 32138 725365 53423 725365 ON T/O CREW OF ANOTHER AIRCRAFT OBSERVED SMOKE (WHITE AT RST CHANGING TO DARK SMOKE) COMING OUT OF TAIL ON LEFT ENGINE D URING T/O ROLL AND CLIMBOUT. ALL COCKPIT INDICATIONS INDICATE NORMAL. PERFORMED VISUAL INSP OF INLET/ EXHAUST AND ENGIN E EXTERIOR COMPONENTS. NO FOD, INSPECTED, RAN BOTH ENGINES TO T/O PWR, NO VIBS FELT AND ALL ENGINE PARAMETERS EVENLY MA TCHED. RAN TO T/O PWR 5 TIMES, NO SMOKE NOTED. CONFERENCE CALL WITH ENG ANALYST AND SR COORDINATOR. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A6WE E9NE 2002011700108 20020117 00108 CE 2002 1 17 CA011119009 1 20011101 A 2497 WIRE LEAR 35 35LEAR 5170600 CE GARRTT TFE731 TFE73122B 01518 WP ELECTRICAL BURNED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING UNSCHEDULE MAINTENANCE A WIRE BUNDLE, LOCATED AT CONNECTOR P616, BEHIND CAPTAIN'S INSTRUMENT PANEL E500 WAS FOUND WITH NUMEROUS BURNT WIRES. INSTRUMENT PANEL WAS REMOVED TO GAIN ACCESS TO BUNDLE. INSPECTION IN PROGRESS. 2 L 7 2 4F 4 F A10CE E6WE 2002011700109 20020117 00109 NM 2002 1 17 DLM88011968 1 20011222 A 7933 WARNING SYSTEM DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE COCKPIT ACTIVATED A DALA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 27 948DL 27663 49879 725775 RIGHT ENG OIL TEMP CAUTION WAS ILLUM WITH THE TEMP AT 142 DEGS. INCREASED THRUST FOR 15 MINS AND TEMP DID NOT DECREASE. PER POM SHUTDOWN ENG. ENG WINDMILLED FOR 20 MINS ZERO OIL PRESS. PERFORMED ALL REQUIRED CHECKS, NO TROUBLE FOUND. 2 L 7 2 4F 4 F RT A6WE E9NE 2002011700110 20020117 00110 EA 2002 1 17 CA011119010 1 20011107 A 7830 LINK CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF343A1 30015 NE THRUST REVERSER BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING 1200 HOURS INSPECTION, FOUND LINK P/N 228-50765-105 BROKEN. BLOCKER DOOR NR 9, P/N 228-50219-108 AND THE 6 O'CLOCK DIVERTER FAIRING P/N 228-50691-109 DAMAGED (PRESUMABLY BY LINK). 2 L 7 2 4F 4 F RT A21EA E15NE 2002011700111 20020117 00111 NM 2002 1 17 DLM88011972 1 20011222 A 4990 38005041 APU DOUG MD88 MD88 3023688 NM APU BAY LEAKING A DALA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 921DL 9298 49645 P80532 ON TAKEOFF OUT OF JAC WHEN TAKEOFF PWR WAS SET F/A IN AFT JUMP SEAT NOTICED BURNING ODOR LIKE BURNING OIL LASTED SEVERAL MINUTES THEN DISSIPATED. NO FURTHER ODOR REMAINDER OF FLT. FOUND APU LEAKING OIL. REPLACED APU ASSY PER M/M. OPS AN D LEAK CHECK GOOD. 2 L 7 2 4F RT A6WE 2002011700116 20020117 00116 SW 2002 1 17 CA011120007 1 20011108 A 7603 C8102419 CABLE SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP POWER LEVER BROKEN W E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 CA 12420 (CAN) THE CENTRE CABLE OF THE POWER LEVER CABLE BROKE APPROXIMATELY 4 INCHES FROM THE POWER LEVER. CONTROL CONNECTION TH E A/C WAS ON CLIMB OUT AT 16,000 FT. A/C WAS LEVELED FOR CRUISE WHEN POWER WAS SET THERE WAS NO RESPONSE TO RIGHT ENGINE WHEN POWER LEVER MOVED, AIRCRAFT RETURNED TO BASE WHERE ENG HAD TO BE SHUT DOWN FOR LANDING. 2 L 7 2 4T 4 T RT A8SW E4WE 2002011700119 20020117 00119 NM 2002 1 17 DLM88011982 1 20011227 A 2611 SAAU308C SMOKE DETECTOR DOUG MD88 MD88 3023688 NM LAVATORY INOPERATIVE A DALA K NONE B P SMOKE/FUMES/ODORS/SPARKS NO WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 908DE 53417 SMOKE DETECTOR IN RIGHT AFT LAV DID NOT OPERATE WHEN PASSENGER SMOKED TWO CIGARETTES AND TRASH BIN BEGAN TO SMOLDER. RE PLACED SMOKE DETECTOR, QA INVESTIGATING. 2 L 7 2 4F RT A6WE 2002011700121 20020117 00121 NM 2002 1 17 CA011120014 1 20011115 A 2424 51608002 CONTROLLER DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE AC GENERATOR FAILED W D RETURN TO BLOCK J WARNING INDICATION CR CRUISE 1 CA 25401 25401 (CAN) AFTER DEPARTURE AIRCRAFT HAD A RT AC BUS FAIL , AIRCRAFT RETURNED FOR NORMAL LANDING , AC GEN CONTROL UNIT REPLACE D. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002011700126 20020117 00126 EU 2002 1 17 CA011121006 1 20011113 A 2120 ROTOR BRAERO 748 HS7482B 1500248 EU RROYCE DART DART532* EU SUPERCHARGER DAMAGED W B A EMER. DESCENT UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 CA (CAN) DURING CRUISE, PILOTS SMELLED SMOKE IN COCKPIT. AT SAME TIME FLT ATTENDANT NOTIFIED COCKPIT THAT LAVATORY SMOKE DE TECTOR HAD GONE OFF. A/C DEPRESSURIZED & EMERG DESCENT MADE, FOLLOWED BY UNSCHED LDG IN LA RONGE, SK. AIR-COND SYS OPERA TED NORMALLY ON SUBSEQUENT MAINT GROUND RUNS (NO SMOKE). INVEST. OF CAUSE REVEALED THAT NR 1 SUPERCHARGER HAD DAMAGED RO TOR. APPROX 4 SQUARE IN OF MATERIAL W ERE BROKEN OUT OF ROTOR. DOWNSTREAM DUCTING&COMPONENTS WERE REMVD&INSP FOR DAMAGE & CONTAMINATION, WITH NONE FOUND. ACCESSORY GEAREBOX INSP FOR DAMAGE WITH NONE FOUND. SUPERCHARGER REPL WITH SERVICEABLE UNIT, & A/C DISPATCHED WITH NO FU 2 L 7 2 3T 4 T A24EU E297 2002011700127 20020117 00127 WP 2002 1 17 CA011121007 2 20011113 A 7320 137928L405 LINE BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110UG 01514 WP NR 2 ENGINE BROKEN W E A ENGINE SHUTDOWN UNSCHED LANDING R F J PARTIAL RPM/PWR LOSS FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 CA (CAN) SHORTLY AFTER DEPARTURE FROM LA RONGE, SK, THE CREW NOTICED A HIGH ITT, A REDUCTION IN ENGINE POWER, FOLLOWED BY A BETA LIGHT AND LOW OIL PRESSURE LIGHT WARNING. THE CREW SHUT DOWN AND SECURED NR 2 ENGINE AND RETURNED TO LA RONGE. MAI NTENANCE FOUND THAT THE P3 BLEED AIR LINE HAD FAILED AT THE FLANGE TO COMPRESSOR CASE CONNECTION. ENGINE OIL FILTERS WER E CHECKED, THE LINE WAS REPLACED, AND ENGINE TEST RUN. THE ENGINE RAN NORMALLY. NOTE: BRITISH AEROSPACE OPTIONAL SB 21-J M7797 REPLACES THE AFFECTED LINE WITH AN UPGRADED LINE. THE UPGRADED LINE HAS TWO FLEX SECTIONS (INSTEAD OF JUST ONE SEC TION) TO BETTER WITHSTAND ADDITION VIBRATION STRESSES. 2 L 7 2 4T 4 T RT A21EU E4WE 2002011700133 20020117 00133 EU 2002 1 17 CA011121020 1 20011103 A 2701 95500019007 CONTROL COLUMN AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE COCKPIT FAILED W A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 CA (CAN) AFTER TAKEOFF CREW REPORTED ELAC FLT NR 1 MSG.AIRCRAFT RETURNED TO TORONTO. CAPT. SIDE STICK REPLACED. OPERATIONAL TEST PERFORMED AS PER AMM 27-02-41-710-001. AIRCRAFT SERVICEABLE. 2 L 7 2 4F 4 F RT A28NM E29NE 2002021100035 20020211 00035 EA 2002 2 11 CA011122001 1 20011108 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 20199 (CAN) MAINTENANCE DISCOVERED CRACK ON THE RT AND LT SIDE OF THE FLOOR SUPPORT ANGLE FOR THE COCKPIT FLOOR. THE CRACKS RU N FROM A RADIUS CUT OUT TO THE FIRST ADJACENT RIVET IN THE HORIZONTAL FLANGE. CRACK IS JUST FORWARD OF THE POST AT FS280 IN THE COCKPIT ENTRANCE FLOOR SUPPORT ANGLE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011700134 20020117 00134 EA 2002 1 17 CA011122002 1 20011109 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 20199 (CAN) MAINTENANCE DISCOVERED A CRACK ON TWO FRAME STATIONS IN THE AFT CARGO FLOOR LANDING PLATE AT FS589 AND FS605, WL73 . GENERIC REO 601R-53-61-433 PROVIDED TO OPERATOR FOR REPAIR. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011700135 20020117 00135 EA 2002 1 17 CA011122003 1 20011109 A 5610 NP1393276 WINDOW CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA (CAN) DURING THE FIRST FLIGHT AT CRUISING ALTITUDE THE RIGHT SIDE COCKPIT WINDOW (OUTER PLY) CRACKED, THE PILOT DECIDED TO RETURN THE AIRCRAFT TO POINT OF DEPARTURE. THE RIGHT SIDE COCKPIT WINDOW REPLACED. AIRCRAFT RETURNED IN SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011700136 20020117 00136 EA 2002 1 17 CA011122005 1 20011109 A 2433 TRU3502 TRANSFORMER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE TRU FAULTY W O OTHER Z SIGNIFICANT FAILURE REPORT AP APPROACH 1 CA (CAN) DURING APPROACH , PFD 1 & MFD 1 BLANKED OFF TOGETHER 4 TO 5 TIMES. NO EICAS MESSAGE POSTED. FLIGHT DIRECTOR ENGAGE D IN APP MODE. AUTOPILOT DID NOT DISENGAGE. RUNWAY IN SIGHT AND APPROACH CONTINUED VISUALLY. ON GROUND, ALL SYSTEM NORMA L. ON RETURN FLIGHT TO MUNICH, PFD 1 AND MFD 1 BLANKED OFF 4 TO 5 TIMES DURING APPROACH.DURING TOUBLESHOOTING, FOUND ESS TRU 1 FAULTY.ESS TRU 1 TRU REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011700138 20020117 00138 NM 2002 1 17 DLM90011959 1 20011219 A 3240 60060853 CONTROLLER DOUG MD90 MD9030 3023690 NM BRAKE SYSTEM FAILED A DALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 27 903DA 53383 FLT DIV- AFTER GEAR EXTENSION UNABLE TO ARM AUTO-BRAKES. AUTO-BRAKE FAIL MSG ON OAP. ANTI-SKID FAULT DISPLAYED ON OAP. REPLACED ASAB CONTROLLER. 2 L 7 2 4F RT A6WE 2002011700145 20020117 00145 WP 2002 1 17 ZW0A0200102 1 20011220 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 912TW 49183 DURING CHECK-C MAINT IN THE MID CARGO COMPT THE LT TIE DOWN TRACK HAD SEVERAL CORRODED AREAS, STA 598 TO 788. REMOVED A ND REPLACED TRACK PER SRM 51-10-3 AND 53-05 PAGE 10 FIG 4C, AT STA 598 TO 788. 2 L 7 2 4F A6WE 2002011700146 20020117 00146 WP 2002 1 17 ZW0A0200103 1 20011226 A 5320 STRUCTURE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 912TW 49183 DURING CHECK-C, CABIN FLOOR MEMBRANE HAD CORROSION ON FLOOR PANEL STA 148, RBL 30, MEMBRANE UNDER -A- GALLEY FLOOR DRAIN CORRODED FITTING, CORROSION MEMBRANE STA 132 TO 148, RBL 32, CEILING PANEL IN ELECTRONIC COMPT, FLOOR OF CABIN RT SIDE AT STA 160, FLOOR OF CABIN AT THE GALLEY DRAIN FITTING BADLY CORRODED, CORROSION OF FLOOR PANEL ATTACH ANGLE STA 132 TO 149, RBL 32, CORROSION ON FLOOR PANEL ATTACH ANGLE STA 120, RBL 33 TO 43, ATTACH ANGLES FOR -A- GALLEY DRAIN CORRODED, C ORROSION ON FLOOR ANGLE STA 148 FWD OF A GALLEY DRAIN PANEL, CORROSION ON FLOOR ATTACH ANGLE RBL 44 STA 160 TO 200. INS TALLED ATTACH ANGLE. INSTALLED MEMBRANE. 2 L 7 2 4F A6WE 2002011700147 20020117 00147 WP 2002 1 17 ZW0A0200104 1 20011227 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9304C 49530 DURING CHECK-C MAINT FOUND NUMEROUS DENTS AT STA 216 TO 218, LONGERON 15L TO 17L. CUT OUT DAMAGED AREA AND INSTALLED RE PAIR PER SSRM 53-10-107, FIG 201. 2 L 7 2 4F RT A6WE 2002011700148 20020117 00148 NM 2002 1 17 ZW0A0200105 1 20011220 A 5330 SKIN BOEING 757 7572Q8 1384972 NM FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 713TW 28173 DURING CHECK-C MAINT FOUND TWO STATIC BURN PITS WITH 3 INCH CIRCLE OF LIGHT CORROSION. AREA HAD BEEN GROUND APPROX 0.02 5 DEEP, LOCATED CENTER OF LAP SEAM, STRINGER 4L AND STA 1223. REPAIRED PER ARA 17864. 2 L 7 2 4F RT A2NM 2002011700149 20020117 00149 WP 2002 1 17 ZW0A0200106 1 20011227 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9304C 49530 DURING CHECK-C MAINT FOUND 2 DENTS IN FUSELAGE SKIN , STA 237, LONGERON 17L. CUT OUT DAMAGED SKIN AND INSTALLED REPAIR PER SRM 53-10-107, FIG 207. 2 L 7 2 4F RT A6WE 2002011700150 20020117 00150 WP 2002 1 17 ZW0A0200107 1 20011228 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9304C 49530 DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR SUPPORT AT STA 1280, RBL 14 TO 36. REMOVED AND REPLACED FLOOR SUPPO RT PER SRM 51-30-02. 2 L 7 2 4F RT A6WE 2002011700151 20020117 00151 WP 2002 1 17 ZW0A0200201 1 20011228 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 948TW 49575 DURING CHECK-C MAINT THE FUSELAGE EXTERIOR HAD A BULGE IN THE SKIN AT LONGERON 17L, STA 1293. ACCOMPLISHED EDDY CURRENT INSPECTION PER NDT 51-00-03 AND NO CRACK. ULTRA SOUND INSPECTION INDICATES NO MATERIAL LOOSE DUE TO CORROSION. SHIM B ETWEEN SKIN AND STRINGER TO REMOVE BULGING IN, PER SRM 51-10-9. INSTALLED HI-LOKS PER SRM 51-60-0, PAGE 36. 2 L 7 2 4F RT A6WE 2002011700152 20020117 00152 WP 2002 1 17 ZW0A0200202 1 20011228 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9304C 49530 DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR SUPPORT AT STA 180, RBL 14 TO 36. REMOVED AND REPLACED FLOOR SUPPOR T PER SRM 51-30-02. 2 L 7 2 4F RT A6WE 2002011700153 20020117 00153 WP 2002 1 17 ZW0A0200203 1 20011228 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 948TW 49575 DURING CHECK-C MAINT ON THE FUSELAGE EXTERIOR, STA 1293, FOUND BULGE IN SKIN AT LONGERON 16L. ACCOMPLISHED EDDY CURRENT INSPECTION PER NDT 51-00-03 AND NO CRACK. ULTRA SOUND INSPECTION INDICATES NO MATERIAL LOOSE DUE TO CORROSION. SHIM B ETWEEN SKIN AND STRINGER TO REMOVE BULGING IN, PER SRM 51-09. 2 L 7 2 4F RT A6WE 2002011700154 20020117 00154 WP 2002 1 17 ZW0A0200401 1 20011227 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 912TW 49183 DURING CHECK-C MAINT IN THE FWD CARGO COMPT THE LT HOLD DOWN TRACK HAD LIGHT TO HEAVY CORROSION, STA 365 TO 446. REMOVE D AND REPLACED TRACK PER SRM 51-10-2. 2 L 7 2 4F A6WE 2002011700155 20020117 00155 WP 2002 1 17 ZW0A0200402 1 20011227 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 912TW 49183 DURING CHECK-C MAINT IN THE MID CARGO COMPT, STA 540 TO 560 LT TIE DOWN TRACK WAS CORRODED. REMOVED AND REPLACED TRACK PER SPM 6-70-01. 2 L 7 2 4F A6WE 2002011700165 20020117 00165 NE 2002 1 17 CA011122007 2 20011109 A 7321 5078T55P13 FUEL CONTROL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ENGINE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) NR 2 MFC FUEL LEAK THROUGH THE THROTTLE SHAFT BODY. NR 2 ENGINE FUEL LEAK DISCOVERED DURING ROUTINE INSPECTION. RT ENGINE COWLING OPENED. LEAK COMING FROM THE NR 2 MFC THROTTLE SHAFT BODY. EVIDENCE OF FIRE MARKS IN THE CORE COWL AND J ET PIPE. NO FIRE WARNING MESSAGES REPORTED BY THE FLIGHT CREWS. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011700168 20020117 00168 NM 2002 1 17 2002F00015 1 20011220 A 3350 58791 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 803MA 22434 EPL TRACK LIGHTS INOPERATIVE. REPLACED AFT EPL TRACK LIGHT STRIP, OPS CHECK NORMAL ON GROUND IAW MM 33-50-02. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002011700169 20020117 00169 NM 2002 1 17 2002F00016 1 20011220 A 3397 CONNECTOR BOEING 727 727225 1384077 NM CABIN CONTAMINATED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 803MA 22434 EPL TRACK LIGHTS INOPERATIVE, AFT GALLEY RIGHT SIDE AND L2 DOOR. CLEANED TRAPPED MOISTURE IN TRACK CONNECTORS. OPS TES T NORMAL ON GROUND IAW MM 33-50-02. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002011700170 20020117 00170 NM 2002 1 17 2002F00017 1 20011218 A 3350 20131A BATTERY PACK BOEING 757 757236 1384971 NM CABIN DISCHARGED A N8TA K NONE L NO TEST IN INSP/MAINT 1 WP 19 522NA 25133 R2 EMERGENCY LIGHT ABOVE DOOR AND AISLE AND OUTSIDE DOOR FAILED TEST. REMOVED AND REPLACED BATTERY PACK ABOVE R2 DOOR. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2002011700171 20020117 00171 NM 2002 1 17 AALA20014069 1 20011203 A 5744 BEAM BOEING 767 767323 1385205 NM RT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 39367 25194 AFW - RIGHT INBOARD FLAP SUPPORT BEAM (9-10 BEAM ASSY) HAD THE MOST OUTBOARD FLAP ATTACH HOLE REAMED TO .503 TO REMOVED CORROSION. OVERSIZE HOLE TO REMOVE CORROSION AND VISUALLY INSPECT THE BORE TO ENSURE CORROSION REMOVAL. FABRICATED REP AIR BUSHING. INSTALLED BUSHING NET, REAMED THE BUSHING BORE. INSTALLED REPAIR WASHER AGAINST THE SUPPORT BEAM IN PLACE OF THE ORIGINAL WASHER. (M) 2 L 7 2 4F RT A1NM 2002011700172 20020117 00172 WP 2002 1 17 ASAA0180302 1 20011121 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 976AS 53452 LAX - DURING LINE MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHTING IN ROWS 6 THROUGH 10 WERE FOUND TO BE ON ALL THE TIME. REPLACED BATTERY PACK AT ROW 10. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2002011700173 20020117 00173 WP 2002 1 17 ASAA0180303 1 20011127 A 3350 0105606 MODULE DOUG DC9 DC982 3022082 WP CABIN NOT SEATED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 967AS 49103 SEA - DURING LINE CHECK, TWO EMERGENCY TRACK LIGHTING MODULES WERE DETERMINED TO BE INOPERATIVE IN FORWARD PASSENGER CAB IN. RESEATED MODULES. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2002011700174 20020117 00174 2002 1 17 ASAA0180304 4 20011130 A 2565 3961896501 LANYARD DOUG DC9 DC982 3022082 WP SERVICE DOOR DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 954AS 49387 SEA - DURING PRE-FLIGHT CHECK, R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DETACHED FROM SLIDE COVER. REATTACHED LANYARD TO SLIDE COVER. (M) 2 L 7 2 4F A6WE 2002011700175 20020117 00175 2002 1 17 ASAA0180305 4 20011201 A 2565 3961896501 LANYARD DOUG DC9 DC983 3022083 WP SERVICE DOOR DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 SFO - DURING PRE-FLIGHT CHECK, L-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DETACHED FROM SLIDE COVER. REATTACHED LANYARD TO SLIDE COVER. (M) 2 L 7 2 4F RT A6WE 2002011700178 20020117 00178 WP 2002 1 17 ASAA0180306 1 20011130 A 3397 0105606 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 935AS 49236 LAX - DURING LINE CHECK, EMERGENCY TRACK LIGHTING AT ROW 9 WAS DETERMINED TO BE INOPERATIVE. REPAIRED BROKEN CONNECTOR WIRE. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2002011700179 20020117 00179 2002 1 17 ASAA0180307 4 20011204 A 2565 D29982107 WIRE HARNESS DOUG DC9 DC982 3022082 WP SERVICE DOOR FAILED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 931AS 29788 4168 49232 OAK - DURING C-CHECK, FORWARD SERVICE (R-1) DOOR EMERGENCY SLIDE HARNESS FAILED SYSTEM CHECK. REPLACED EMERGENCY SLIDE. SYSTEM CHECKED OK. (M) 2 L 7 2 4F A6WE 2002011700180 20020117 00180 2002 1 17 ASAA0180309 4 20011208 A 2565 3961896501 LANYARD DOUG DC9 DC983 3022083 WP SERVICE DOOR DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 LAX - DURING PREFLIGHT CHECK, L-2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DETACHED FROM SLIDE COVER. REATTACHED LANYARD TO SLIDE COVER. (M) 2 L 7 2 4F RT A6WE 2002011700181 20020117 00181 NM 2002 1 17 GAIA01320OP 1 20011228 A 3222 65727628 CENTERING CAM BOEING 727 727223 1384074 NM NLG STRUT FAILED A GAIA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 6808 19483 DURING PARKING, MAINTENANCE NOTICED THAT THE NOSE LANDING GEAR SHOCK STRUT WAS EXTENDED ABNORMALLY HIGH AND THE STRUT OU TER SURFACE CHROME PLATE WAS WORN AND GOUGED. UPON DISASSEMBLY INSPECTION REVEALED THAT THE INTERNAL CENTERING CAM MECH ANISM HAD FAILED IN THE NOSE LANDING GEAR SHOCK STRUT. THE NOSE LANDING GEAR WAS REMOVED AND REPLACED PER THE B727 MM. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002011700182 20020117 00182 WP 2002 1 17 GTIA011015 1 20011015 A 2730 CONTROL CABLE DOUG DC9 DC982 3022082 WP ELEVATOR BROKEN A GTIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 23 816NK 49140 ACY - NOT ENOUGH ELEVATOR AUTHORITY TO PROPERLY ROTATE AIRCRAFT AT COMPUTED CG243 AND TRIM 3.2 ANV AT 121524.3 LBS TOW. IN CRUISE AT FL330, 115,900 LBS MACH .76 IAS 270 TRIM INDICATED 4.9 ANU NO TRIM IN MOTION ANNUNCIATION OBSERVED DURING FLIGHT. AFTER LANDING TRIM WOULD NOT INDICATE FORWARD OF 2.8. REMOVED AND REPLACED ELEVATOR CABLE 130B DUE TO BEING BR OKEN IAW 27-40-00. (M) 2 L 7 2 4F A6WE 2002011700183 20020117 00183 WP 2002 1 17 GTIA012004 1 20011203 A 3350 601177X9 POWER SUPPLY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 DTW - FOUND EXTERIOR EMERGENCY LIGHTS STAY ON AT ALL TIMES. REMOVED AND REPLACED EXTERIOR EMERGENCY LIGHTS BATTERY POWE R SUPPLY IAW MD80 M/M 33-50-00. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2002011700184 20020117 00184 WP 2002 1 17 GTIA012005 1 20011101 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FOUND LEFT INBOARD SEAT TRACK STATION 977 GOUGED. INSTALLED SEAT TRACK AND SPLICES FROM STATION 920 TO STATION 101 8 IAW MD80 SRM 53-05. (M) 2 L 7 2 4F A6WE 2002011700185 20020117 00185 WP 2002 1 17 GTIA012006 1 20011029 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 AFT CARGO COMPARTMENT DOOR JAMB BEAM CORRODED, LEVEL 1. REMOVED JAMB BEAM. CARGO TRACK SUPPORT AT STATION 1219 FOUND T O BE OUT OF LIMITS. LOCATED AND DRILLED NEW DOOR JAMB BEAM. INSTALLED CARGO TRACK SUPPORT BRACKET AT STATION 1219. IN STALLED DOOR JAMB BEAM IAW MD80 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 2002011700186 20020117 00186 WP 2002 1 17 GTIA012007 1 20011103 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - AFT B/B LONGERON 30 CORROSION AT STATION 1005 AND STATION 1022 AND DAMAGED SEALANT AROUND PREVIOUS REPAIR. FABRIC ATED REPAIR FITTING. INSTALLED REPAIR FITTING IAW FLIGHT VEHICLES DRAWING 53-01-01-1. (M) 2 L 7 2 4F A6WE 2002011700187 20020117 00187 WP 2002 1 17 GTIA012008 1 20011213 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FOUND DENT AT APPROX STATION 217 BETWEEN LONGERON 18L AND 19L. FABRICATED DOUBLER. INSTALLED DOUBLER IAW MD80 SR M 51-30-2 AND 51-30-5 AND 53-04. (M) 2 L 7 2 4F A6WE 2002011700188 20020117 00188 WP 2002 1 17 GTIA012010 1 20011103 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT STATION Y=164, X31 INCHES. LOCATED AND DRILLED NEW FITTING. INSTAL LED NEW FITTING IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002011700189 20020117 00189 WP 2002 1 17 GTIA012011 1 20011101 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - RIGHT INBOARD SEAT TRACK GOUGED AT FS 1160. LOCATED AND DRILLED RIGHT, INBOARD SEAT TRACK. INSTALLED SEAT TRACK AND SPLICE, FS 1146-1260 RT, INBOARD IAW MD80 SRM 51-10-4. (M) 2 L 7 2 4F A6WE 2002011700190 20020117 00190 WP 2002 1 17 GTIA012012 1 20011101 A 7120 ISOLATOR DOUG DC9 DC982 3022082 WP LT ENGINE UNSERVICEABLE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FOUND LEFT ENGINE FORWARD, LOWER VIBRATION ISOLATOR HAS MISMATCHED ROTATION MARKS. REMOVED VIBRATION ISOLATOR. IN STALLED SERVICEABLE VIBRATOR ISOLATOR IAW MD80 71-20-02. (M) 2 L 7 2 4F A6WE 2002011700191 20020117 00191 WP 2002 1 17 GTIA012013 1 20011101 A 7120 ISOLATOR DOUG DC9 DC982 3022082 WP RT ENGINE UNSERVICEABLE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FOUND RIGHT ENGINE, FORWARD LOWER VIBRATION ISOLATOR HAS MISMATCHED ROTATION MARKS. REMOVED VIBRATION ISOLATOR. INSTALLED O/H, RT ENGINE FORWARD LOWER VIBRATOR ISOLATOR IAW MM MD80 71-20-02. (M) 2 L 7 2 4F A6WE 2002011700192 20020117 00192 WP 2002 1 17 GTIA012014 1 20011031 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - REPAIR AT FS 1212 AT AFT EDGE OF AFT CARGO DOOR. THIS REPAIR MUST BE REPLACED WITH REPAIR IN SRM 53-05. REMOVED OLD REPAIR. LOCATED AND DRILLED REPAIR DOUBLERS. INSTALLED REPAIR DOUBLERS IAW MD80 SRM 53-05. (M) 2 L 7 2 4F A6WE 2002011700193 20020117 00193 WP 2002 1 17 GTIA012016 1 20011102 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FORWARD ENTRY AREA FLOOR SUPPORT CORRODED AT STATION Y=218 X=0, INBOARD SURFACE. FORMED NEW SUPPORT. INSTALLED F LOOR SUPPORT PER MD80 SRM 53-14-1. (M) 2 L 7 2 4F A6WE 2002011700194 20020117 00194 WP 2002 1 17 GTIA012017 1 20011103 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT STATION Y=200 -X5 TO +X5. FORMED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT IAW MD80 SRM 51-30-1. (M) 2 L 7 2 4F A6WE 2002011700195 20020117 00195 WP 2002 1 17 GTIA012018 1 20011102 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FLOOR SUPPORT CORRODED AT STATION Y=198.0, -X54 INCHES FORWARD ENTRY AREA. FABRICATED OF PART, INSTALLED NEW PART IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002011700196 20020117 00196 WP 2002 1 17 GTIA012019 1 20011031 A 5210 BRACKET DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FORWARD PASSENGER DOOR L1 BRACKET CRACKED AT STATION Y-188, Z=32.9 BETWEEN LL BEAM NR 6 AND LL BEAM NR 5. FORMED L-1 ANGLE. INSTALLED V ANGLE IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002011700197 20020117 00197 WP 2002 1 17 GTIA012020 1 20011103 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FOUND LEFT INBOARD SEAT TRACK STATION 770 GOUGED. INSTALLED SEAT TRACK, REF N/R 18-N-00259. (M) 2 L 7 2 4F A6WE 2002011700198 20020117 00198 WP 2002 1 17 GTIA012026 1 20011103 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - RIGHT OUTBOARD SEAT TRACK HAS CORROSION AND GOUGES FROM STATION 826 TO STATION 845. INSTALLED NEW SEAT TRACK, REF N/R 18-N-00214. (M) 2 L 7 2 4F A6WE 2002011700199 20020117 00199 WP 2002 1 17 GTIA012032 1 20011102 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT STATION Y=238 X=0. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLO OR SUPPORT IAW MD80 SRM 53-14-2. (M) 2 L 7 2 4F A6WE 2002011700200 20020117 00200 WP 2002 1 17 GTIA012033 1 20011030 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - AFT AIRSTAIR STATION 1338 CANTED, VERTICAL ANGLE ATTACHED TO RT UPPER SIDE WALL SUPPORT CHANNEL IS CRACKED IN FORW ARD FLANGE RADIUS. REMOVED CANTED VERTICAL ANGLE AT AFT AIRSTAIRS. FABRICATED FORWARD AND AFT FLANGE REPAIR DOUBLERS. INSTALLED CANTED VERTICAL ANGLE IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002011700201 20020117 00201 WP 2002 1 17 GTIA012034 1 20011031 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FOUND DENT AT FS 398.5 BETWEEN LONGERON 17R AND 18R. FABRICATED AND DRILLED REPAIR. INSTALLED DOUBLER IAW MD-80 SRM 51 -30-5. (M) 2 L 7 2 4F A6WE 2002011700202 20020117 00202 WP 2002 1 17 GTIA012035 1 20011031 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FOUND DENT AT FS 1224 BETWEEN LONGERON 23R AND 24R. FABRICATED AND DRILLED REPAIR DOUBLER. INSTALLED DOUBLER IAW MD80 SRM 51-30-2 AND SRM 51-30-5. (M) 2 L 7 2 4F A6WE 2002011700203 20020117 00203 WP 2002 1 17 GTIA012036 1 20011031 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FOUND REPAIR AT FS 1155 AT FORWARD EDGE OF AFT CARGO DOOR. FABRICATED NEW REPAIR. INSTALLED NEW REPAIR IAW MD80 53-05. (M) 2 L 7 2 4F A6WE 2002011700204 20020117 00204 WP 2002 1 17 GTIA012037 1 20011031 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FOUND DENT AT FS 362 BETWEEN LONGERON 24R AND 25R. CUT DAMAGE AREA. FABRICATED PARTS REPAIR DOUBLER. INSTALLED DOUBLER REPAIR IAW MD80 SRM 53-04. (M) 2 L 7 2 4F A6WE 2002011800001 20020118 00001 EA 2002 1 18 CA011122008 1 20011109 A 5410 601350061 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ENGINE BAY CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 17164 (CAN) ENGINE SUPPORT BEAM CRACKED ON TOP WEB 7TH RIVET OUT TO LEFT OF BL 0 AT AFT ROW OF RIVETS. CRACK IS FROM RIVET TO AFT EDGE OF MATERIAL. AIRCRAFT FERRIED FROM CINCINNATI TO HOT SPRINGS FOR REPAIR. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011800003 20020118 00003 EA 2002 1 18 CA011123006 1 20011119 A 5610 601R330333 WINDOW CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 12818 (CAN) CLIMBING THROUGH 22,5000 FT, CAPTAINS SIDE WINDOW CRACKED. DIVERTED TO IND AND LANDED WITHOUT FURTHER INCIDENT. AI RCRAFT FERRIED BACK TO CVG FOR WINDOW REPLACEMENT.CAPTAINS SIDE WINDOW REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011800004 20020118 00004 EA 2002 1 18 CA011123007 1 20011120 A 5410 601350061 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE ENGINE BAY CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 12556 11617 (CAN) CRACKS FOUND AT ONE LOCATION WHILE PERFORMING REPEAT INSPECTION: FS 640, BL 0.0 (UPPER WEB).THIS WAS FOUND WHILE P ERFORMING THE SB A601R-53-059.DISCREPANCIES WILL BE REPAIRED USING BOMBARDIER DISPOSITIONS. 2 L 7 2 4F 4 F RT A21EA E15NE 2002011800010 20020118 00010 NM 2002 1 18 S01257039 1 20011007 A 2750 JACKSCREW BOEING 747 747209B NM PWA JT9 JT9D7A 52054 NE TE FLAPS DAMAGED W SAJF K NONE O OTHER IN INSP/MAINT 1 WP 03 21454 B-18751 GRD CHK FOUND NR 1 FLAPTRACK JACKSCREW FITTING BROKEN.C/A:1.ISSUED REVISION OF EO 740-57-50-0004 TO PERFORM THE REPLACEMENT/OVERHAUL IN LIEU OF INSPECTION. 2.REPLACED WITH NEW FITTING NR 1 THROUGH NR 8 PER 742-57-639359-001R1. 3. PROVIDE BROKEN FITTING TO BOEING FOR FURTHER ANALYSIS REQUESTED. 4.OPEN THIS CASE FOR FURTHER ACTION PER REVISION SB THA T WILL BE PROVIDED ON 12/14/2001. 2 L 7 4 4F 4 F RT A20WE E20EA 2002011800011 20020118 00011 NE 2002 1 18 S01271023 2 20010811 A 7200 ENGINE BOEING 747 747209B NM PWA JT9 JT9D7R4G2 52054 NE NR 2 MALFUNCTIONED W SAJF E A ENGINE SHUTDOWN UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 WP 03 24308 725333 B18771 NR 2 ENGINE SPOOL DOWN AT LEVEL 39000 FT N DRIFT DOWN TO 35000 FT N RESTART SUCCESSFULLY BEFORE RESTART N1 31 N N2 24.55 OIL PRESS AS NML RESTART IS 30000 FT. C/A:1. NR 2 ENGINE CHECK IAW FIM 71-01-00 PG 8 N 209 ALL NML. 2.ENG INL ET N EXHAUST CK NML. 3.FUEL SYS FILTERS CK FOUND NML. 4.ALSO FUEL TANKS SUMP DRAIN VLV DRAINED. 5.FURTHER TO TPEMMCI. TL X 110656 FURTHER CHECK REQ C/OUT.SATIS HI-POWER RUN PERFORMED.IAW MM 71-00-00 ALL PARAMETERS ARE NML ACCELERATION IS NML .LEAK CK C/OUT AFT ENG RUN ALL SATIS. 6.THIS EVENT IS STILL UNDER TROUBLE SHOOTING AND SURVEY ROOT CAUSE. 2 L 7 4 4F 4 F RT A20WE E3NE 2002011800012 20020118 00012 2002 1 18 S01422029 4 20010927 A 2211 COMPUTER BOEING 747 747400 NM PWA 4056 PW4056 NE AUTOPILOT MALFUNCTIONED W SAJF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 03 24311 B-18273 1.A/P AUTO ENGAGED WITH OUT COMMAND DURING A/C T/O. 2.OCT 02, CAPT REPORT 20011002 IS RECEIVED,IAW CAPT DESCRIPT ION,SUSPECT MCP FUNCTION UNSTABLE. 3.MCP WAS REPLACED ON OCT 02. C/A: 1. MCP WAS REPLACED WHEN A/C BACK TO CHECKS AT T HE SAME DAY AND PERFORM ALL THE A/P TEST RESULT SHOW SATISFACTORY. 2.MCP SEND TO COLLINS FOR DETAIL INVESTIGATION. 2 L 7 4 4F 4 F RT A20WE E24NE 2002011800013 20020118 00013 NM 2002 1 18 S01426033 1 20011013 A 2612 CARD BOEING 747 747400 NM PWA 4056 PW4056 NE FIRE DETECTION LOOSE W SAJF C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 03 24311 B18273 DURING T/O ROLLING, AT SPEED 145, A/C REJECT T/O DUE TO AFT FIRE CARGO WARNING SOUND. NRS 2,4,6 & 8 TIRES WERE DE FLATED. A/C STOPED ON THE RUNWAY. C/A: 1. REPLACED DEFLATED TIRES. 2.PERFORM "HIGH ENERGY STOP INSP." IAW AMM 05- 51-10. 3.AFT LOWER CARGO BAY WAS CHECKED NO SIGNS OF FIRE, FIRE SYSTEM TESTED NORMAL. 4.THE LATCH SCREWS OF CARD A32 WE RE FOUND LOOSE. RPLD THE CARD IAW AMM 26-14-03 FOR PRE-CAUTION. 2 L 7 4 4F 4 F RT A20WE E24NE 2002011800014 20020118 00014 NM 2002 1 18 S01430038 1 20011130 A 3097 CWC011210 TERMINAL BOEING 747 747400 NM PWA 4056 PW4056 NE WINDSHIELD HEAT BROKEN W SAJF K NONE B L SMOKE/FUMES/ODORS/SPARKS NO TEST IN INSP/MAINT 1 WP 03 28711 B-18203 WINDOW HEAT IL MSG SHOW DUE TO POWER LINE BROKEN AND BURNED. C/A: 1. GROUND CHECK FOUND A15 CONTROL SENSOR W IRING BROKEN. 2. WIRING (P/N:CWC01-1210) REPLACED AND CMC BITE TEST PASSED. 3. GROUND CHECK MSG DISAPPEARED. 4. ACCOMPLI SHMENT OF EO 744-30-41-0002 WILL PREVENT FUTURE RECURRENCE. 5.744 AMP 30-41-01-4A AT 1A INTERVAL CAN PREVENT THIS OCCURE NCE. 2 L 7 4 4F 4 F RT A20WE E24NE 2002011800015 20020118 00015 NE 2002 1 18 S01472025 2 20010822 A 7261 LINE BOEING 747 747400 NM PWA 4056 PW4056 NE NR 2 ENGINE LEAKING W SAJF E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 03 29219 727666 B-18207 NR 2 ENGINE HIGH N2 VIBRATION. OIL LOST GRADUALLY FOLLOWED HEAVY WHITE SMOKE, NR 2 ENGINE IFSD AND A/C DIVERT TO HNL. C/A: 1. GROUND CHECKED NR 3 BEARING M.C.D AND MAIN OIL FILTER METAL CHIPS WAS FOUND. 2. GROUND INSPECTION FOUND AGB RETURN TO SCAV OIL PUMP TUBE BROKEN; MAIN OIL SUPPLY TUBE OIL LEAKAGE; TURBINE CASE COOLING MANIFOLD 3 EA AIR TUBES BROKEN; NR 3 BEARING WEEP TUBE BROKEN. 3. NR 2 ENGINE WAS REPLACED AND RUN UP CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2002011800016 20020118 00016 NM 2002 1 18 S01472026 1 20010823 A 2910 LINE BOEING 747 747400 NM PWA 4056 PW4056 NE NR 3 ENGINE LEAKING W SAJF E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 WP 03 27965 727728 B-18251 NR 3 ENGINE SURGED AND OVER EGT DURING CLIMB. NR 3 ENGINE IFSD AND ATB. 1. GROUND CHECKED NR 3 ENGINE TAIL PIP E AREA FOUND SEVERAL METAL CHIPS. 2. NR 3 EDP HYD. TUBE FOUND HYD FLUID LEAKING. 3. NR 3 ENGINE REPLACED AND RUN UP CHEC KED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2002011800017 20020118 00017 NM 2002 1 18 S01J26024 1 20010814 A 2612 285N0028136 CARD BOEING 747 747400 NM GE CF6 CF680C2* GL FIRE DETECTION MALFUNCTIONED W SAJF F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 03 30764 B18707 INFLT CREW REPORT. MAIN DECK AFT FIRE WARNING CAME ON. THE CREW ACTUATED 4 LOWER CARGO COMP. FIRE EXTINGUISHERS. C/A: GROUND TEST FOUND MAWEA AFOLTS CARD N.G. 1.REPLACED THE AFOLTS & PER AMM 26-14-00 FUNCTION TEST NML. 2.RPLD 4 EA FIRE BOTTLES PER AMM 26-23-013. 3.RPLD THE FILTERS PER AMM 26-23-044. 4.RPLD 2 EA CREW OXY BOTTLES. 2 L 7 4 4F 4 F RT A20WE E23EA 2002011800018 20020118 00018 NM 2002 1 18 S01J54032 1 20011007 A 5414 PANEL BOEING 747 747400 NM GE CF6 CF6* 30020 GL NACELLE MISSING W SAJF D RETURN TO BLOCK D INFLIGHT SEPARATION CR CRUISE 1 WP 03 30760 B-18702 TPE GROUND CHECK FOUND NR 4 BAY PANEL MISSING. C/A: 1. AFT CHECK, REPLACED ALL DAMAGED PARTS AND REPAIR SKATE ANGLES PER EO 744-54-50-0006. 2.ISSUED EON 744-54-639359-001 TO INFORM THAT CLOSE FAIRING DOOR MUST OBEY THE STANDARD P ROCEDURE PER 747-400 AMM 54-62-00 PARA.5. 3.ENHANCE THE TRAINING FOR CLOSING TRAILING EDGE FAIRING DOOR TO REDURE THE EV ENT CAUSED BY THE NEGLIGENCE OF MAINTENANCE. 2 L 7 4 4F 4 F RT A20WE E23EA 2002011800030 20020118 00030 NE 2002 1 18 2002F00014 2 20010829 A 7230 3027798 STATOR PWA BELL 212 212 1181420 SW PWA PT6T PT6T3B 52045 NE COMPRESSOR FAILED E CUCL K NONE O OTHER IN INSP/MAINT 1 WP 17 911HW 23687 3D841 31101 CPP561773 ENGINE TEARDOWN SHOWS THIRD STAGE STATOR FAILED. 1 G 7 1 4U 4 U H4SW E22EA 2002011800033 20020118 00033 SW 2002 1 18 ALG2002F00000 1 20011126 A 6320 407040035101 BEVEL GEAR BELL 407 BELL 407 407 1182206 SW ALLSN 250C 250C* GL TRANSMISSION MAKING METAL A ALGR O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 417AL 3988 1522 A160 53054 TRANSMISSION MAKING METAL. BEVEL GEAR CRACKED FROM BOLT HOLE. 1 G 7 1 3U 3 U O H2SW E4CE 2002011800034 20020118 00034 NE 2002 1 18 ALG2002F00001 1 20011113 A 2612 CONNECTOR SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL FIRE DETECTION LOOSE A ALGR O OTHER O OTHER TX TAXI/GRND HDL 1 SW 03 518AL 760134 CAE890465S DURING RUN UP CHECKS. CONNECTOR PLUGS FOUND LOOSE IN THE NR 1 ENGINE INTAKE. 1 G 7 2 3U 3 U H1NE E1GL 2002011800035 20020118 00035 SW 2002 1 18 ALG2002F00002 1 20011023 A 6420 407012112101 PITCH HORN BELL 407 407 1182206 SW ALLSN 250C 250C47B GL TAIL ROTOR CORRODED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 687AL 2514 53366 AFTER DISASSEMBLY, CLEANING AND STRIPPING PAINT FOR OVERHAUL. CORROSION ON ENTIRE SURFACE BEYOND LIMITS DUE TO POOR MET AL QUALITY AND POOR PRIME AND PAINT. BETTER QUALITY ALUMINUM AND PAINTING PROCEDURES RECOMMENDED. 1 G 7 1 3U 3 U O H2SW E1GL 2002011800036 20020118 00036 SW 2002 1 18 ALG2002F00003 1 20011218 A 6230 406010426101 LINK BELL 407 407 1182206 SW ALLSN 250C 250C47B GL SWASHPLATE CORRODED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 547AL 1827 53240 IN SHOP REPAIR, EXCESSIVE CORROSION AROUND BUSHINGS AND UNDER BUSHINGS. BETTER ALLOYS, BETTER PRIMER AND SURFACE TREA TMENT RECOMMENDED. 1 G 7 1 3U 3 U O H2SW E1GL 2002011800037 20020118 00037 NE 2002 1 18 ALG2002F00004 1 20011113 A 2611 WIRE SKRSKY S76A SKRSKY S76 S76 8143010 NE ALLSN 250C 250C30S 03013 GL SMOKE DETECTOR BROKEN B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 702AL 760243 890775S DURING RUN UP, BROKEN WIRE AT CONNECTOR PLUG IN BAGGAGE COMPARTMENT. 1 G 7 2 3U 3 U H1NE E1GL 2002011800038 20020118 00038 NE 2002 1 18 ALG2002F00005 1 20011222 A 2435 303001383 BRUSHES SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL STARTER GEN DISINTEGRATED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 917QS 249 464 760217 890253S PILOT WRITE UP AT END OF DAY. WHEN START BUTTON IS DEPRESSED (NR 2 ENGINE) STARTER CHATTERS AND HAS GRINDING NOISE. WH EN RELEASED AND DEPRESSED AGAIN, A FAIRLY NORMAL START IS ACHIEVED. UPON INSPECTION OF STARTER GENERATOR, BRUSHES FOUND TO BE DISINTEGRATED. ARMATURE ALSO DAMAGED DUE TO FAILED BRUSHES. 1 G 7 2 3U 3 U H1NE E1GL 2002011800039 20020118 00039 SW 2002 1 18 ALG2002F00006 1 20011220 A 6510 407340103 DISC PACK BELL 407 407 1182206 SW ALLSN 250C 250C47B GL TAIL ROTOR BROKEN B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 577AL 53247 DURING 25 HOUR AD INSPECTION, BROKEN DISC IN DISC PACK. ALLOW TAIL ROTOR DRIVE SHAFT TO FLOAT SO DISC PACKS DO NOT FLEX AS MUCH OR AS OFTEN. 1 G 7 1 3U 3 U O H2SW E1GL 2002011800040 20020118 00040 NE 2002 1 18 CUC2002F00000 2 20010829 A 7230 3027798 STATOR PWA BELL 212 212 1181420 SW PWA PT6T PT6T3B 52045 NE ENGINE FAILED E CUCA K NONE O OTHER IN INSP/MAINT 1 WP 17 911HW 23687 30841 31101 CPPS617733 ENGINE TEARDOWN SHOWS THIRD STAGE STATOR FAILED. 1 G 7 1 4U 4 U H4SW E22EA 2002011800041 20020118 00041 EU 2002 1 18 FF6R103597 1 20011009 A 6510 770441 MAGNETIC SEAL SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR LEAKING B FF6R K NONE K FLUID LOSS IN INSP/MAINT 1 NM 08 111AK 472 3092 SEAL LEAKING, PART TT 472.9 1 G 7 1 3U 3 U NC H9EU E19EU 2002011800042 20020118 00042 EU 2002 1 18 FF6R103598 1 20011009 A 6510 770441 MAGNETIC SEAL SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR LEAKING B FF6R K NONE K FLUID LOSS IN INSP/MAINT 1 NM 08 105TV 115 2279 TAIL ROTOR MAGNETIC SEAL LEAKING, PART TT 115.2. 1 G 7 1 3U 3 U H9EU E19EU 2002011800043 20020118 00043 SW 2002 1 18 H3V2002F00000 1 20010829 A 6230 MS276405 BEARING BELL BELL 212 212 1181420 SW PWA PT6 PT6* 52043 EA SWASHPLATE DETERIORATED H H3VL K NONE O OTHER IN INSP/MAINT 1 WP 25 811KA 724 KAA51880 30656 CPPS61970 DURING ROUTINE MAINTENANCE INSPECTION BEARING WAS FOUND TO HAVE PLAY. BEARING PLAY WAS FOUND TO BE WITH IN LIMITS IAW M M. POST FLIGHT INSPECTIONS FOUND RAPID DETERATION OF BEARING. SWASHPLATE WAS REMOVED FROM SERVICE AND SERVICEABLE SWAS HPLATE WAS INSTALLED. 1 G 7 1 4U 3 T H4SW E2NE 2002011800044 20020118 00044 EU 2002 1 18 KBMA111986 1 20011128 A 6420 704A33651181 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE T/R DRIVE WORN A KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 115SH 941 3141 TAIL ROTOR DRIVE BEARING, SLEEVE AND BRUSH RUBBER WORN BEYOND LIMITS. REMOVED AND REPLACED WITH NEW. 1 G 7 1 3U 3 U H9EU E19EU 2002011800045 20020118 00045 EU 2002 1 18 KBMA111987 1 20011128 A 6520 350A33215001 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE T/R ROD END WORN A KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 115SH 3177 3141 BEARING WORN BEYOND LIMITS. REMOVED AND REPLACED WITH OVERHAULED UNIT. 1 G 7 1 3U 3 U H9EU E19EU 2002011800046 20020118 00046 EU 2002 1 18 KBMA111988 1 20011205 A 6730 AC67244 SERVO SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE HYD SYSTEM BINDING A KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 270SH 1483 1864 SERVO UNIT IS BINDING. REPLACED WITH OVERHAULED SERVO. 1 G 7 1 3U 3 U NC H9EU E19EU 2002011800051 20020118 00051 NE 2002 1 18 KBMA112014 2 20011128 A 7421 9550168760 IGNITER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE WORN A KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 115SH 3062 3141 IGNITER, CENTER CONDUCTOR WORN. REMOVED AND REPLACED WITH NEW PART. 1 G 7 1 3U 3 U H9EU E19EU 2002011800052 20020118 00052 EU 2002 1 18 KBMA112016 1 20011127 A 6720 350A33214501 PITCH LINK SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR CRACKED A KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 230SH 4433 2337 TAIL ROTOR PITCH LINK CRACKED AT AFT SLEEVE. REMOVED AND REPLACED WITH OVERHAULED UNIT. 1 G 7 1 3U 3 U NC H9EU E19EU 2002011800053 20020118 00053 GL 2002 1 18 KBMA112017 2 20011118 A 7314 7G547 SWITCH BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL FUEL PUMP FAILED A KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 73DP 548 2513 FUEL PUMP FAIL LIGHT DOES NOT LIGHT UP WHEN CIRCUIT BREAKER IS PULLED. REMOVED AND REPLACED WITH NEW SWITCH. 1 G 7 1 3U 3 U H2SW E4CE 2002011800054 20020118 00054 SW 2002 1 18 LX52002F00000 1 20011221 A 6220 206011135105 BOLT BELL BELL 206 206L3 1182108 SW M/R HUB CORRODED A LX5R K NONE O OTHER IN INSP/MAINT 1 GL 19 741LL 799 A501 51165 PITTING AND CORROSION IN BLADE BUSHING, BLADE BOLT AREA WHERE THEY MEET. 1 G 7 1 3U H2SW 2002011800060 20020118 00060 EU 2002 1 18 S9H2001F00001 1 20011207 A 2910 704A33690004 BELT SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE HYD SYSTEM BROKEN E S9HA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 19 360NT 236 2695 4474 PILOT EXPERIENCED HYDRAULIC FAILURE WHEN HYDRAULIC BELT BROKE AFTER CONTACT WITH A BROKEN AIR CONDITION COMPRESSOR BELT. PILOT MADE A PRECAUTIONARY LANDING WITH NO INCIDENTS AT AIRSTRIP. NEW HYDRAULIC BELT WAS INSTALLED AND AIRCRAFT RETUR NED TO BASE WITHOUT FURTHER INCIDENTS. 1 G 7 1 3U 3 U NC H9EU E19EU 2002011800061 20020118 00061 NE 2002 1 18 VE32002F00000 2 20011205 A 7321 0164248850 FUEL CONTROL SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE ENGINE LEAKING A VE3R K NONE K FLUID LOSS IN INSP/MAINT 1 WP 23 217LA 226 3311 DATE: 12-3-2001, AFTER INSTALLATION, WITH BOOST PUMPS ON, FUEL WAS NOTICED LEAKING FROM THE ENGINE DECK DRAIN. FURTHER INSPECTION IDENTIFIED THE SOURCE OF THE LEAK AS THE FUEL CONTROL UNIT. THE FCU WAS LEAKING FROM THE FCU DRAIN. REPLACE MENT OF THE FCU WAS NECESSARY TO CORRECT THIS PROBLEM. MFG HAS NOT OFFERED A CAUSE FOR THIS LEAK. THIS FCU DID NOT ACC UMULATE ANY TIME BEFORE FAILURE DURING THIS INSTALLATION. 1 G 7 1 3U 3 U H9EU E19EU 2002011800063 20020118 00063 NE 2002 1 18 VE32002F00001 2 20011205 A 7321 0164248850 FUEL CONTROL SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE ENGINE LEAKING A VE3R K NONE K FLUID LOSS IN INSP/MAINT 1 WP 23 217LA 200 3311 DATE: 11-20-2001, DURING ROUTINE INSPECTION, A PUDDLE OF FUEL WAS NOTICED ON THE GROUND, UNDER THE ENGINE DECK DRAIN. F URTHER INSPECTION IDENTIFIED THE SOURCE OF THE LEAK AS THE FUEL CONTROL UNIT. THE FCU WAS LEAKING FROM THE FCU DRAIN. REPLACEMENT OF THE FCU WAS NECESSARY TO CORRECT THIS PROBLEM. MFG HAS NOT OFFERED A CAUSE FOR THIS LEAK. 1 G 7 1 3U 3 U H9EU E19EU 2002011800064 20020118 00064 NE 2002 1 18 VE32002F00002 2 20011205 A 7321 0164248850 FUEL CONTROL SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE ENGINE LEAKING A VE3R K NONE K FLUID LOSS IN INSP/MAINT 1 WP 23 223LA 570 3278 DATE: 11-28-2000, DURING ROUTINE INSPECTION, A PUDDLE OF FUEL WAS NOTICED ON THE GROUND, UNDER THE ENGINE DECK DRAIN. F URTHER ON THE GROUND, UNDER THE ENGINE DECK DRAIN. FURTHER INSPECTION IDENTIFIED THE SOURCE OF THE LEAK AS THE FUEL CON TROL UNIT. THE FCU WAS LEAKING FROM THE FCU DRAIN. REPLACEMENT OF THE FCU WAS LEAKING FROM THE FCU DRAIN. REPLACEMENT OF THE FCU WAS NECESSARY TO CORRECT THIS PROBLEM. MFG HAS NOT OFFERED A CAUSE FOR THIS LEAK. 1 G 7 1 3U 3 U H9EU E19EU 2002022800023 20020228 00023 NM 2002 2 28 2001UALA02503 1 20011231 A 3830 VALVE 158000121 BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LAVATORY FAILED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 608UA 043 21869 AFT MID LAV CONTINUOUSLY FLUSHING. LAV WATER OVERFLOWED AND FLOODED AREA INCLUDING MID GALLEY. AIRCRAFT DIVERTED TO OR D FOR REPAIR. TOILET RINSE VALVE FAILED IN THE OPEN POSITION. REMOVED AND REPLACED TOILET ASSY. 2 L 7 2 4F 4 F RT A1NM E3NE 2002011800071 20020118 00071 NE 2002 1 18 VE32002F00004 2 20011205 A 7321 0164248850 FUEL CONTROL SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE ENGINE LEAKING A VE3R K NONE O OTHER IN INSP/MAINT 1 WP 23 217LA 1280 71 3311 7086 DATE: 11-30-2001, DURING ROUTINE INSPECTION, A PUDDLE OF FUEL WAS NOTICED ON THE GROUND, UNDER THE ENGINE DECK DRAIN. F URTHER INSPECTION IDENTIFIED THE SOURCE OF THE LEAK AS THE FUEL CONTROL UNIT. THE FCU WAS LEAKING FROM THE FCU DRAIN. REPLACEMENT OF THE FCU WAS NECESSARY TO CORRECT THIS PROBLEM. MFG HAS NOT OFFERED A CAUSE FOR THIS LEAK. 1 G 7 1 3U 3 U H9EU E19EU 2002011800072 20020118 00072 NE 2002 1 18 VE32002F00005 2 20011205 A 7321 0164248850 FUEL CONTROL SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE ENGINE LEAKING A VE3R K NONE O OTHER IN INSP/MAINT 1 WP 23 221LA 866 3320 9674 DATE: 2-9-2001, DURING ROUTINE INSPECTION, A PUDDLE OF FUEL WAS NOTICED ON THE GROUND, UNDER THE ENGINE DECK DRAIN. FUR THER INSPECTION IFENTIFIED THE SOURCE OF THE LEAK AS THE FUEL CONTROL UNIT. THE FCU WAS LEAKING FROM THE FCU DRAIN. RE PLACEMENT OF THE FCU WAS NECESSARY TO CORRECT THIS PROBLEM. MFG HAS NOT OFFERED A CAUSE FOR THIS LEAK. 1 G 7 1 3U 3 U H9EU E19EU 2002011800073 20020118 00073 NE 2002 1 18 XC42001F00000 1 20011210 A 3240 1331317 STATOR SKRSKY S58 S58E 8141809 NE WRIGHT R1820 R1820* 67020 EA MLG BRAKE ASSY DEFECTIVE B XC4R K NONE O OTHER IN INSP/MAINT 1 SO 19 504 771 0377A 571717 BRAKE ASSEMBLY (PN 2-1661) FAILED PREMATURELY. NR 1 STATOR CRACKED THROUGH IN 2 PLACES CAUSING SIGNIFICANT DAMAGE TO TO RQUE TUBE AND WHEEL ASSEMBLY. PIECE OF STATOR 8 INCHES LONG MISSING. NOTE: MOST RECENT CONFIGURATION OEM PARTS INSTALL ED (KIT NR 304-289 CHG B) 2 G 7 1 4R 4 R 1H11 5E10 2002011800074 20020118 00074 SW 2002 1 18 XJ22002F00000 1 20011002 A 6730 41002521 COVER BELL 407 407 1182206 SW ALLSN 250C 250C* GL SERVO FAILED B XJ2R K NONE O OTHER IN INSP/MAINT 1 WP 01 58236 1452 53069 SERVO WAS REMOVED FOR HOWLING NOISE IN FLIGHT, UNIT WAS DISASSEMBLED FOR OVERHAUL AND PN 41002521 COVER TO RETAIN VALVE, ID CORRODED AND VALVE SPRING WAS RUSTED IN HALF. IF RETAINER FAILED THE SERVO WOULD GO INTO BYPASS AND POSSIBLE HARDOV ER CONDITION. COVER NEEDS TO BE MODIFIED TO ALLOW WATER TO DRAIN OR A BETTER BOOT NOT TO ALLOW WATER TO ENTER VALVE. 1 G 7 1 3U 3 U O H2SW E4CE 2002011800075 20020118 00075 NM 2002 1 18 DLM90011938 1 20011213 A 5320 7961078653 BRACKET DOUG MD90 MD9030 3023690 NM FUSELAGE DAMAGED A DALA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 27 903DA 53383 WORKING INBOUND MCO APU NO START WITH MESSAGE ON OAP. FOUND BRACKET WITH BURNT AREA WHERE GROUND STUD SHOULD HAVE MOUNT ED. BRACKET P/N 7961078-653, STUD P/N AN 6-6. TERMINAL 5D0084-53 NOT DAMAGED. REF MD90 SB MD90-49A010 PAGE 12 OF 13 VIEW A-A FIG 2 (SH 2 OF 2). REMOVED BRACKET FOR REPLACEMENT. LIAISON ENGINEERING CONTACTED FOR REPAIR INSTRUCTIONS. B RACKET LOCATION IS UPPER BRACKET AT STA 1395 AND LONGERON 24-25. 2 L 7 2 4F RT A6WE 2002011800078 20020118 00078 SW 2002 1 18 XJ22002F00001 1 20011002 A 7100 RS62 RETAINER BELL 407 407 1182206 SW ALLSN 250C 250C* GL BYPASS VALVE CORRODED A XJ2R K NONE O OTHER IN INSP/MAINT 1 WP 01 58236 1452 53069 SERVO WAS REMOVED FOR HOWLING NOISE IN FLIGHT, UNIT WAS DISASSEMBLED FOR OVERHAUL AND PN 41002521 COVER TO RETAIN VALVE, ID CORRODED AND PN RS62 RETAINER TO RETAIN BYPASS VALVE SPRING WAS RUSTED IN HALF. IF RETAINER FAILED THE SERVO WOULD GO INTO BYPASS AND POSSIBLE HARD OVER CONDITION. COVER NEEDS TO BE MODIFIED TO ALLOW WATER TO DRAIN OR A BETTER BOOT NO T TO ALLOW WATER TO ENTER VALVE. 1 G 7 1 3U 3 U O H2SW E4CE 2002011800085 20020118 00085 EU 2002 1 18 PNSA011201 1 20011207 A 2932 CONNECTOR SAAB SF340 340B 7860101 EU HYDRAULIC SYS DIRTY A PNSA K NONE N FALSE WARNING CR CRUISE 1 AL 03 695PA 340B310 DURING CRUISE HYDRAULIC LIGHT CAME ON WITH MASTER CAUTION WARNING. CREW CHECK GAUGES FOR HYD PRESSURE AND FOUND TO BE N ORMAL. EMERGENCY ACCUMULATOR INDICATED PRESSURE WAS LOW. NORMAL LANDING WAS MADE AND MAINTENANCE FOUND EMERGENCY ACCUM ULATOR COCKPIT INDICATION READING LOW COMPARED TO ACTUAL ACCUMULATOR READING. CLEANED TRANSDUCER CANNON PLUG AND OP CHE CKED NORMAL. 2 L 7 2 4T RT A52EU 2002011800086 20020118 00086 SW 2002 1 18 PNSA011202 1 20011218 A 3230 LANDING GEAR SWRNGN SA227 SA227AC 8780603 SW NLG LACK OF LUBE A PNSA K NONE J WARNING INDICATION CL CLIMB 1 AL 03 650PA AC775B NOSE GEAR WOULD NOT LOCK IN UP POSITION ON DEPARTURE FROM UNK. MAINTENANCE CONTACTED BY RADIO AND AUTHORIZED FLIGHT TO CONTINUE TO ANC WITH GEAR DOWN. MAINTENANCE CLEANED AND LUBED LANDING GEAR AND OP CHECK OK. 2 L 7 2 4T RT A8SW 2002011800089 20020118 00089 SW 2002 1 18 PNSA020102 1 20010114 A 2910 HYDRAULIC LINE SWRNGN SA227 SA227AC 8780603 SW HYDRAULIC SYS CRACKED A PNSA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 AL 03 640PA AC759B ON CLIMBOUT FROM AKN 3 MINUTES AFTER GEAR RETRACTION HYD WARNING LIGHTS CAME ON WITH LOSS OF HYD PRESSURE. AN EMERGENCY WAS DECLARED AND RETURNED TO AKN. PILOT NOTED ON PREVIOUS FLIGHT NOTICED SMALL PRESSURE FLUCTUATIONS BUT PRESSURE STA YED WITHIN GREEN EXCEPT ONE TIME IT REACHED YELLOW. MAINTENANCE FOUND NOSE GEAR UP LINE AT LT WING ROOT CRACKED IN BEND . A/C LANDING GEAR DEACTIVATED AND HYD SERVICED. A/C FERRIED TO ANC MAINTENANCE BASE FOR REPAIR. THIS WAS THE 3RD OCC URRENCE OF A CRACKED NOSE GEAR UP LINE IN THE LAST WEEK. FOUND HYDRAULIC ACCUMULATOR TO HAVE LOW NITROGEN CHARGE (LAST SERVICED 270 HOURS PREVIOUS) AND CHECKED ALL RIGGING OF NOSE GEAR. BOTH HYDRAULIC PUMPS REPLACED. 2 L 7 2 4T RT A8SW 2002011800098 20020118 00098 EU 2002 1 18 QXEA0102099 1 20011212 A 5330 RIVET FOKKER F28 F28MK4000 4990810 EU FUSELAGE LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - TWO LOOSE RIVETS IN FUSELAGE SKIN AT FRAME 67-2 ABOVE STRINGER 91. REPAIRED IAW FOKKER SRM 51-30-02. 2 L 7 2 4F RT A20EU 2002011800100 20020118 00100 EU 2002 1 18 QXEA0102100 1 20011209 A 5230 WEB FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CRACK ON AFT STEP VERTICAL WALL APPROXIMATELY 2 INCHES ABOVE TOP STEP ON AFT SIDE OF AFT CARGO DOOR. REPAIRED IAW FOKKER SRM 52-30-00 AND 51-31-01. 2 L 7 2 4F RT A20EU 2002011800101 20020118 00101 EU 2002 1 18 QXEA0102101 1 20011209 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - UPPER TCAS MOUNT AREA ON FUSELAGE SKIN CORRODED. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4-B. 2 L 7 2 4F RT A20EU 2002011800102 20020118 00102 EU 2002 1 18 QXEA0102102 1 20011209 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - UPPER NAS/COM ANTENNA MOUNT AREA ON FUSELAGE SKIN CORRODED. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4 -B. 2 L 7 2 4F RT A20EU 2002011800103 20020118 00103 EU 2002 1 18 QXEA0102103 1 20011214 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - FRAME CLIP CRACKED AT FRAME 7305 AND STRINGER 65. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2, PAGE 4. 2 L 7 2 4F RT A20EU 2002011800104 20020118 00104 EU 2002 1 18 QXEA0102104 1 20011209 A 5230 STEP FOKKER F28 F28MK4000 4990810 EU CARGO DOOR BENT A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - TOP OF FORWARD STEP VERTICAL WALL BENT ON CARGO DOOR. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002011800106 20020118 00106 EU 2002 1 18 QXEA0102105 1 20011211 A 5210 HINGE FITTING FOKKER F28 F28MK4000 4990810 EU PAX DOOR SCORED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - MAIN CABIN DOOR HINGE LUGS ARE DEEPLY SCORED. REPAIRED IAW FOKKER SRM 52-02-02, PAGE 7, FIGURE 4 AND HORIZON AIR EA 4-52-463. 2 L 7 2 4F RT A20EU 2002011800107 20020118 00107 EU 2002 1 18 QXEA0102106 1 20011213 A 5330 RIVET FOKKER F28 F28MK4000 4990810 EU FUSELAGE LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - FORWARD FUSELAGE SKIN BETWEEN FRAMES 4175 AND 4610 ON STRINGER 68 HAS LOOSE RIVETS. REPAIRED IAW FOKKER SRM 51-31 -01. 2 L 7 2 4F RT A20EU 2002011800108 20020118 00108 EU 2002 1 18 QXEA0102108 1 20011214 A 5510 FITTING FOKKER F28 F28MK4000 4990810 EU HORIZ STAB DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - HORIZONTAL STABILIZER JUNCTION FITTING, RT LUG HAS PITTING ON LUG. REPAIRED IAW HORIZON AIR EA 4-55-300 AND FOKKE R SRM 55-01-01, PAGE 3, PARAGRAPH 3E, STEP 5. 2 L 7 2 4F RT A20EU 2002011800110 20020118 00110 EU 2002 1 18 QXEA0102109 1 20011214 A 5510 FITTING FOKKER F28 F28MK4000 4990810 EU HORIZ STAB DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - HORIZONTAL STABILIZER JUNCTION FITTING, RT LUG HAS PITTING ON LUG. REPAIRED IAW HORIZON AIR EA 4-55-300 AND FOKKE R SRM 55-01-01, PAGE 3, PARAGRAPH 3E STEP 5. 2 L 7 2 4F RT A20EU 2002011800111 20020118 00111 EU 2002 1 18 QXEA0102110 1 20011214 A 5510 FITTING FOKKER F28 F28MK4000 4990810 EU HORIZ STAB DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - HORIZONTAL STABILIZER JUNCTION FITTING, LT LOWER LUG HAS PITTING ON LUG. REPAIRED IAW HORIZON AIR EA 4-55-300 AND FOKKER SRM 55-01-01, PAGE 3, PARAGRAPH 3E, STEP 5. 2 L 7 2 4F RT A20EU 2002011800112 20020118 00112 EU 2002 1 18 QXEA0102111 1 20011214 A 5510 FITTING FOKKER F28 F28MK4000 4990810 EU HORIZ STAB DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - HORIZONTAL STABILIZER JUNCTION FITTING, LT UPPER LUG HAS PITTING ON LUG. REPAIRED IAW HORIZON AIR EA 4-55-300 AND FOKKER SRM 55-01-01, PAGE 3, PARAGRAPH 3E, STEP 5. 2 L 7 2 4F RT A20EU 2002011800113 20020118 00113 EU 2002 1 18 QXEA0102112 1 20011212 A 5315 FLOORBEAM FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CENTER FLOORBEAM CHAFED AND FRETTING CORROSION AROUND FASTENER HOLE, 4 INCHES FORWARD OF FRAME 13815B. REPAIRED I AW FOKKER SRM 53-01-01, PAGE 8, PARAGRAPH 4-C, STEP 2 AND 3. 2 L 7 2 4F RT A20EU 2002011800114 20020118 00114 EU 2002 1 18 QXEA0102113 1 20011212 A 5315 FLOORBEAM FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CENTER FLOORBEAM CORRODED ON TOP FLANGE AT STATION 6805. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 8, PARAGRAPH 4-C, STEP 3. 2 L 7 2 4F RT A20EU 2002011800116 20020118 00116 EU 2002 1 18 QXEA0102114 1 20011212 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - FUSELAGE FRAME 16660 TIE-IN CLIP TO SKIN IS CRACKED THROUGH RIVET HOLE AT STRINGER 28. REPAIRED IAW FOKKER SRM 53 -02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002011800117 20020118 00117 NM 2002 1 18 QXEA0200009 1 20010108 A 5210 STOP FITTING DHAV DHC8 DHC8202 2809007 NM PAX DOOR DEFECTIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 SEA- EXTERIOR MAIN CABIN DOOR HANDRAIL IS RECESSED TOO FAR. UNABLE TO OPEN MAIN CABIN DOOR. INSTALLED NEW MAIN CABIN DO OR EXTERIOR HANDRAIL BUMPER/STOP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002011800123 20020118 00123 SO 2002 1 18 RAIA00201004 1 20010106 A 2740 CONTROL UNIT EMB 145 EMB145 3260210 SO HORIZ STAB MALFUNCTIONED A RAIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 CE 03 801HK 145053 5278-GRR- CREW REPORTED MAIN PITCH TRIM FAILED AFTER TAKEOFF. MAINTENANCE DID FUNCTIONAL CHECK OF PITCH TRIM SYSTEM. S YS OPS CHECK OK. 2 L 7 2 4F RT T00011AT 2002011800124 20020118 00124 SO 2002 1 18 RAIA00201007 1 20010107 A 2120 UNKNOWN EMB 145 EMB145 3260210 SO CABIN ODOR A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 03 803HK 145077 5257-CID- CREW REPORTED GLYCOL SMELL IN CABIN AFTER DEPARTURE. MAINTENANCE PERFORMED GROUND RUN WITH BOTH PACKS AND APU OPERATING. NO DEFECTS WERE NOTED. 2 L 7 2 4F RT T00011AT 2002011800128 20020118 00128 NM 2002 1 18 AWXA200200044 1 20011226 A 5240 6545871521 SKIN BOEING 737 7373S3 1384711 NM BENT A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 MCN - MAJOR REPAIR - "C" - DURING C-15 CHECK THE UPPER AFT CORNER OF THE FORWARD GALLEY SERVICE DOOR WAS FOUND TO HAVE S KIN BENT OUTWARD. MAINTENANCE REMOVED DAMAGED SKIN AND FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED REPAIRS IAW B7 37-300 SRM 52-00-01, PG 203-204, AND 51-20-01, PG 1. 2 L 7 2 4F RT A16WE 2002011800135 20020118 00135 NM 2002 1 18 2002F00018 1 20011201 A 7830 THRUST REVERSER DOUG DC10 DC1040F 3023507 NM NR 2 ENGINE DAMAGED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 141WE 46661 DURING C-CHECK, THE NR 2 ENGINE THRUST REVERSER LEFT COWL SKIN AS FOUND DAMAGED ON LEADING EDGE. A DOUBLER WAS INSTALLE D IAW REO-GO8284 AND A 8110-3 WAS ISSUED. THE AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (M) 2 L 7 3 4F RT A22WE 2002011800136 20020118 00136 NM 2002 1 18 2002F00020 1 20011201 A 5313 AJC7119501 LONGERON DOUG DC10 DC1040F 3023507 NM FUSELAGE CRACKED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 141WE 51705 46661 DURING C-CHECK, FOUND LONGERON 13L WAS FOUND CRACKED BETWEEN FASTENER HOLES AT CANTED STATION Y2153. LONGERON 13L WAS R EPAIRED IAW TIMCO REO-G08321 REV IR AND FAA FORM 8110-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 2002011800137 20020118 00137 NM 2002 1 18 2002F00021 1 20011201 A 5311 ACA3796501 FRAME DOUG DC10 DC1040F 3023507 NM FUSELAGE CORRODED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 141WE 51705 46661 DURING C-CHECK, THE LEFT NOSE WHEEL WELL CHORD VERTICAL LEG WAS FOUND CORRODED AND BLENDED JUST PAST SRM REPAIRABLE LIMI TS. A REPAIR ANGLE WAS INSTALLED IAW TIMCO REO-G08344 REV IR AND REO G8336 REV IR. THE AIRCRAFT WAS RETURNED TO REVENU E SERVICE. (M) 2 L 7 3 4F RT A22WE 2002011800138 20020118 00138 NM 2002 1 18 2002F00022 1 20011201 A 7830 THRUST REVERSER DOUG DC10 DC1040F 3023507 NM NR 2 ENGINE DAMAGED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 141WE 46661 DURING C-CHECK, THE NR 2 ENGINE THRUST REVERSER LEFT COWL SKIN WAS FOUND DAMAGED ON LEADING EDGE. A DOUBLER WAS INSTALL ED IAW REO-G08284 AND A 8110-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 2002011800139 20020118 00139 NM 2002 1 18 2002F00023 1 20011201 A 5320 ACA70161 ANGLE DOUG DC10 DC1040F 3023507 NM FUSELAGE CORRODED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 141WE 46661 DURING C-CHECK, THE FORWARD LEFT AIR CONDITIONING BAY CAP ANGLE AT STATION 595 BETWEEN LONGERON 47L AND 48L WAS CORRODED PAST SRM LIMITS. A REPAIR DOUBLER WAS INSTALLED ON THE EXTERIOR OF THE SKIN TO REINFORCE THE BLEND AREA IAW TIMCO REO- G08333. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 2002011800140 20020118 00140 NM 2002 1 18 2002F00024 1 20011201 A 5313 AJC7119501 LONGERON DOUG DC10 DC1040F 3023507 NM FUSELAGE CRACKED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 141WE 46661 DURING C-CHECK, LONGERON 13L WAS FOUND CRACKED BETWEEN FASTENER HOLES AT CANTED STATION Y2153. LONGERON 13L WAS REPAIRE D IAW TIMCO REO-GO8321 REV IR AND FAA FORM 8110-3. THE AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (M) 2 L 7 3 4F RT A22WE 2002011800141 20020118 00141 NM 2002 1 18 2002F00025 1 20011201 A 5311 ACA3796501 FRAME DOUG DC10 DC1040F 3023507 NM FUSELAGE CORRODED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 141WE 46661 DURING C-CHECK, THE LEFT NOSE WHEEL WELL CHORD VERTICAL LEG WAS FOUND CORRODED AND BLENDED JUST PAST SRM REPAIRABLE LIMI TS. A REPAIR ANGLE WAS INSTALLED IAW TIMCO REO-G08344 REV IR AND REO G8336 REV IR. THE AIRCRAFT WAS RETURNED TO SERVIC E. (M) 2 L 7 3 4F RT A22WE 2002011800142 20020118 00142 NM 2002 1 18 2002F00026 1 20011123 A 3150 656021132 CONTROL BOX BOEING 727 727251 138408H NM E/E BAY FAULTY A FX7A D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 19 266US 19985 DURING TAXIING SPEED BRAKE/FLAP WARNING TEST FAILED A/C RETURNED TO GATE AURAL WARNING BOX WAS REPLACED PER MM 31-26. A IRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002011800143 20020118 00143 NM 2002 1 18 2002F00027 1 20011124 A 5210 HRS3CCF9 BEARING BOEING 727 727224 1384076 NM L1 DOOR DAMAGED A FX7A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 79749 22451 DURING CLIMB, L1 DOOR HAD LOUD NOISE WHILE PRESSURIZING A/C RETURNED TO CCS MTX REMOVED AND REPLACED BEARING AT L1 DOOR LOWER RAIL PER MM 52-10. AIRCRAFT PRESSURIZED AND CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002011800144 20020118 00144 NM 2002 1 18 2002F00028 1 20011110 A 2410 700842A CSD BOEING 727 727259 138408J NM NR 2 ENGINE MALFUNCTIONED A FX7A K NONE J WARNING INDICATION CL CLIMB 1 SO 19 203AV 22474 DURING CLIMB, NR 2 AND NR 3 GEN LOW OIL PRESSURE LIGHTS COMES ON DRAINED OIL AND REPLACED FILTER ON NR 3 ENGINE. OPS CH ECK GOOD PER MM 24-10 PLACED NR 2 ENG CSD ON MEL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002011800146 20020118 00146 NM 2002 1 18 2002F00029 1 20011111 A 2410 CSD BOEING 727 727259 138408J NM NR 3 ENGINE MALFUNCTIONED A FX7A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 203AV 22474 DURING CLIMB-OUT, 25 MINUTES AFTER TAKEOFF NR 3 CSD GEN TEMP IN 160 DEGREES, RISE 25 DEGREES VOLTS 110 FREQS 390, AFTER REDUCING LOAD AND 10 MINUTES LATER, TEMP 120 RISE 18. AIRCRAFT RETURNED TO SVMI, DUE TO NR 2 CSD ALREADY DEFERRED. REM OVED AND REPLACED NR 2 AND NR 3 CSD, AND CSD OIL COOLERS IAW MM 24-10-61. P/N NR 2 CSD 700842A, S/N 153340. P/N NR 3 CS D 700842A S/N ON 7366. P/N CSD COOLER NR 2 6A47-000 S/N OFF 9948. P/N CSD COOLER NR 3 6A47-000 S/N ON 10102. (M) 2 L 7 3 4F A3WE 2002011800147 20020118 00147 NM 2002 1 18 2002F00030 1 20011127 A 3244 TIRE BOEING 727 727224 1384076 NM MLG FAILED A FX7A K NONE O OTHER TX TAXI/GRND HDL 1 SO 19 79749 22451 UPON LANDING IN CCS, WHEN EXITING RUNWAY NR 4 TIRE BLEW AFTER REPLACING SAME NR 3 NR 2 AND NR 1 TIRE ALSO HAD TO BE REPL ACED PER MM 32-45. AIRCRAFT WAS RETURNED TO SERVICE. NOTE ANTI-SKID WAS ON MEL AT THE TIME. (M) 2 L 7 3 4F A3WE 2002011800148 20020118 00148 NM 2002 1 18 2002F00031 1 20011205 A 2611 21562B SMOKE DETECTOR BOEING 747 747212B 1384886 NM CARGO BAY MALFUNCTIONED A UIEA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 15 808MC 21048 DURING CLIMB-OUT FROM MIA AT APPROXIMATELY 21,000 FEET, THE CARGO LOWER AFT FIRE LIGHT ILLUMINATED. CHECKLIST SECTION I II WAS COMPLETED. THE CARGO FLOOR FELT WARM AT SL, BOTH FORWARD AND AFT CARGO HEAT TURNED OFF. WHILE DESCENDING AT 180 0 FT THE FIRE LIGHTS WENT OUT. REMOVED AND REPLACED ALL FOUR SMOKE DETECTORS AND REMOVED AND REPLACED ALL FOUR SMOKE DE TECTOR AMPLIFIERS. OPERATIONAL CHECK PER MM 26-16-02 PAGE 401. (M) 2 L 7 4 4F A20WE 2002011800149 20020118 00149 NM 2002 1 18 2002F00033 1 20011219 A 2613 SWITCH BOEING 737 737205 1384456 NM COCKPIT DAMAGED A SOKF A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 23 235TA 21765 MIA - FLT 473 - BOTH WING BODY OVERHEAT LIGHT ILLUMINATES DURING TAKEOFF AND REMAINS ILLUMINATED DURING FLIGHT. DURING TROUBLESHOOTING FOUND TEST SWITCH DAMAGED, ENTERED IN DEFERRED ITEM. PERFORMED OPERATIONAL TEST. SYSTEM WORKS NORMAL ON BOTH SENSORS. (M) 2 L 7 2 4F RT A16WE 2002011800150 20020118 00150 EA 2002 1 18 ASOA01267 1 20011201 A 2910 601R75276553 HYDRAULIC LINE CNDAIR CL600 CL6002B19 1900309 EA HYDRAULIC SYS CRACKED A ASOA L ABORTED APPROACH K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 11 827AS 7212 FLT 4721 - APPROACH IN MMY, WHEN GEAR WAS SELECTED DOWN, CAPTAIN RECEIVED A GEAR DISAGREEMENT WARNING WITHIN FIVE SECOND S. THE CAPTAIN THEN RECEIVED A HYDRAULIC NR 3 LOW PRESSURE AND A ZERO PRESSURE WARNING MESSAGE. WHEN THE GEAR WAS SELE CTED UP THE MESSAGES DECLARED AND THE AIRCRAFT LANDED SAFELY IN MMY. MAINTENANCE REMOVED AND REPLACE THE TWO FLEX LINES FOR THE TWO HYDRAULIC PUMPS, 3A AND 3B, AND SERVICED THE HYDRAULIC SYSTEM. THIS WAS DISCOVERED NOT TO BE THE PROBLEM. UPON FURTHER INSPECTION, THE LEFT WING AILERON OUTBOARD PCU HYDRAULIC LINE WAS FOUND TO BE CRACKED AND LEAKING AT FUEL PANEL 550GB. MAINTENANCE REPAIRED CRACKED LINE. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002011800151 20020118 00151 NM 2002 1 18 GAIA01306OP 1 20010908 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6816 19491 DURING MAINTENANCE AT TOL, IT WAS DISCOVERED THAT THE L1 DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACE D THE EMERGENCY EXIT LIGHT. THE SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002011800152 20020118 00152 NM 2002 1 18 GAIA01307OP 1 20010908 A 3350 1000679 CONTACTOR BOEING 727 727225 1384077 NM COCKPIT DIRTY A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 936PG 22441 DURING MAINTENANCE AT TOL, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT WAS INOPERATIVE. INSPECTION FOUND TH E EMERGENCY EXIT LIGHT CONNECTIONS DIRTY. THE CONNECTORS WERE CLEANED AND THE LIGHT WAS REINSTALLED. THE SYSTEM OPERAT IONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002011800153 20020118 00153 NM 2002 1 18 GAIA01308OP 1 20010908 A 3350 10000679 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 936PG 22441 DURING MAINTENANCE AT TOL, IT WAS DISCOVERED THAT THE L1 DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACE D THE EMERGENCY EXIT LIGHT. THE SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002011800154 20020118 00154 NM 2002 1 18 GAIA01317OP 1 20011204 A 2910 AE2463513K64 HYDRAULIC LINE BOEING 727 727224 1384076 NM HYDRAULIC SYS PUNCTURED A GAIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 69735 20664 FLT 1925 - FWA-BNA - DURING CLIMB-OUT, THE CREW NOTICED THAT SYSTEM 'A' WAS LOSING HYDRAULIC FLUID. THE CREW RETURNED T O FWA, AND DECLARED AN EMERGENCY. AN UNEVENTFUL LANDING WAS MADE AT FWA. THE AIRPLANE REQUIRED TOW BACK TO THE MAINTEN ANCE RAMP. MAINTENANCE FOUND A PUNCTURE IN THE NR 2 SYSTEM PRESSURE LINE LOCATED IN THE AFT STAIR WELL. MAINTENANCE RE PLACED THE LINE IAW THE BOEING 727 AMM CHAPTER 29-10. THE AIRCRAFT WAS THEN RETURNED BACK TO SERVICE. (M) 2 L 7 3 4F A3WE 2002011800155 20020118 00155 NM 2002 1 18 GAIA01318ST 1 20011211 A 5230 65569271 FRAME BOEING 727 7272J0 138407E NM CARGO DOOR CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 281KH 21105 DURING TROUBLESHOOTING FOR A PRESSURIZATION PROBLEM A 2 INCH CRACK WAS FOUND ON A FRAME ON THE FORWARD SIDE OF THE NR 3 AFT CARGO DOOR ASSEMBLY. REMOVED AND REPLACED THE NR 3 LOWER AFT CARGO DOOR ASSEMBLY. OPERATIONALLY CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2002011800156 20020118 00156 NM 2002 1 18 GAIA01319OP 1 20011218 A 3350 1000679 LIGHT BOEING 727 727224 1384076 NM L1 DOOR INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 69739 20667 DURING ROUTINE MAINTENANCE AT DFW, IT WAS DISCOVERED THAT THE L-1 EMERGENCY EXIT LIGHT DID NOT ILLUMINATE. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002011800157 20020118 00157 2002 1 18 GTIA010436 4 20010530 A 2210 RELAY DOUG DC9 DC981 3022081 WP AUTOPILOT SYS FAILED A GTIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 23 805NK 48058 EWR - AP AUTOPILOT WAS NOT TRIMMING NOSE UP. REMOVED AND REPLACED TRIM RELAY R20-12 PER WDM 27-43-02. PERFORMED OPS CH ECK A/P SYSTEM PER MM 22-21-00 SOUND NORMAL. (M) 2 L 7 2 4F A6WE 2002011800158 20020118 00158 WP 2002 1 18 GTIA010873 1 20010911 A 2720 ARM DOUG DC9 DC932 3022066 WP RUDDER DIRTY A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 133NK 48111 MACH TRIM INDICATION INOPERATIVE IN OVERRIDE WILL NOT RETRACT. CLEANED MACH TRIM ROCKER ARM, OPS CHECK GOOD IAW DC9 MM 27-20-1. (M) 2 L 7 2 4F A6WE 2002011800159 20020118 00159 WP 2002 1 18 GTIA012038 1 20011205 A 5730 PANEL DOUG DC9 DC983 3022083 WP RT WING CRACKED A GTIA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 23 802NK 53168 DTW - EVIDENCE OF FUEL LEAK AT RIGHT WING LOWER PANEL NR 1406C. FOUND FUEL PANEL 1460C TO BE CRACKED. REMOVED AND REPL ACED FUEL PANEL 1460C AT RT LOWER WING SURFACE IAW MD80 MM 57-30-03, REF M22 12343 FOR LEAK CHECK. (M) 2 L 7 2 4F RT A6WE 2002011800162 20020118 00162 WP 2002 1 18 GTIA012039 1 20010815 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - FOUND FUSELAGE SKIN DENT AT STATION 351 LONGERON 24 DEPTH .03. CUT OUT DAMAGED AREA IAW MD80 SRM 53-04. FABRICAT ED FINGER DOUBLER AND FILLER. INSTALLED REPAIR IAW MD80 SRM 53-04. (M) 2 L 7 2 4F RT A6WE 2002011800163 20020118 00163 WP 2002 1 18 GTIA012040 1 20010821 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - FOUND DENT LEFT FUSELAGE AFT OF L1 DOOR (3FT) DENT IS 2 INCHES BY 3 INCHES BY 0.080. CUTOUT DAMAGED AREA. FORMED FINGER DOUBLER. FORMED SKIN PLUG. INSTALLED DOUBLER AND SKIN PLUG IAW MD80 SRM 51-10-31. (M) 2 L 7 2 4F RT A6WE 2002011800164 20020118 00164 WP 2002 1 18 GTIA012043 1 20010830 A 5522 PLATE DOUG DC9 DC983 3022083 WP ELEVATOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - FOUND LEFT ELEVATOR PAINT PEELING OFF AND BARE METAL INBOARD SIDE. FOUND CRACK AT INBOARD LEADING EDGE PLATE. RE MOVED CRACKED PLATE FROM LEFT ELEVATOR. FABRICATED NEW PLATE. INSTALLED PLATE IAW MD80 SRM 51-20-0 AND 51-30-2. (M) 2 L 7 2 4F RT A6WE 2002011800165 20020118 00165 WP 2002 1 18 GTIA012045 1 20010908 A 5320 BRACKET DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FOUND E/E COMPARTMENT STATION 150, CORRODED ANGLE AT STATION 150 FRAME AND OUTBOARD SIDE OF AFT LOCKING PIN (RT) HOLE IN DOOR FRAME. REMOVED T-BRACKET. INSTALLED NEW T-BRACKET IAW MD80 SRM 51-30-5. (M) 2 L 7 2 4F RT A6WE 2002011800166 20020118 00166 WP 2002 1 18 GTIA012046 1 20011002 A 3350 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 814NK 49619 FTW - FOUND LEFT AND RIGHT LOW OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED BATTERY POWER SUPPLY. INSTALLED BAT TERY POWER SUPPLY IAW MD80 MM 33-53-00. (M) 2 L 7 2 4F RT A6WE 2002011800167 20020118 00167 WP 2002 1 18 GTIA012048 1 20010826 A 5730 SKIN DOUG DC9 DC983 3022083 WP LT WING CHAFED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FTW - LEFT WING L/E TOP SIDE OUTBOARD SLAT IS CHAFING. FOUND TO BE OUT OF LIMITS. LOCATE AND DRILL WING OUTBOARD L/E S UPPORT. INSTALLED O/B, L/E SUPPORT IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2002011800168 20020118 00168 WP 2002 1 18 GTIA012055 1 20010830 A 2742 DRIVE UNIT DOUG DC9 DC983 3022083 WP HORIZ STAB WORN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FOUND HORIZONTAL STABILIZER DRIVE ACME DRIVE AND NUT WEAR OUT OF LIMITS. REMOVED ACME SCREW ASSY FROM LONGITUDE ACTUATO R. INSTALLED ACME SCREW AND NUT ASSY IAW MD80 MM 27-40-01. (M) 2 L 7 2 4F RT A6WE 2002011800169 20020118 00169 NM 2002 1 18 GTIA012057 1 20011204 A 5230 SKIN DOUG MD80 MD83 3023681 NM CARGO DOOR DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 DTW - INSPECT DENT ON AFT CARGO DOOR FOR LIMITS. DENT PLACED ON C/O 0016919-3 WITHIN LIMITS IAW MD-80 SRM 53-04. (M) 2 L 7 2 4F RT 2002011800170 20020118 00170 WP 2002 1 18 GTIA012072 1 20010831 A 5610 RETAINER DOUG DC9 DC981 3022081 WP COCKPIT WINDOW CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 NM 01 810NK 48015 FTW - FOUND COCKPIT OVERHEAD WINDOW OUTER RETAINER CRACKED. REMOVED UPPER WINDOW OUTER RETAINER. LOCATE AND DRILL NEW RETAINER WINDOW. INSTALLED RETAINER WINDOW. INSTALLED EXTERNAL DOUBLER IAW MD80 SERVICE BULLETIN 56-11-R3. (M) 2 L 7 2 4F A6WE 2002011800171 20020118 00171 WP 2002 1 18 GTIA012073 1 20010902 A 5310 STRUCTURE DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 FTW - FOUND LOWER COMPARTMENT CARGO DOOR CUTOUTS FROM STATION 1155 THROUGH 1212 CORRODED. REMOVED CORROSION, REF N/R 18 -N-00027. (M) 2 L 7 2 4F A6WE 2002011800172 20020118 00172 WP 2002 1 18 GTIA012074 1 20010911 A 7110 ACOUSTIC PANEL DOUG DC9 DC981 3022081 WP NR 2 COWLING SEPARATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 FTW - NR 2 ENGINE AT 3:00 POSITION LE OF ACOUSTICAL PANEL SEPARATED 1.4 INCHES SPAN INLET COWL. REPAIR ACOUSTICAL PANEL PER MD80 SRM WITH EA 934 IAW MD80 SRM 54-04. (M) 2 L 7 2 4F A6WE 2002011800173 20020118 00173 WP 2002 1 18 GTIA012076 1 20011028 A 3510 LATCH DOUG DC9 DC981 3022081 WP CABIN OUT OF ADJ A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 810NK 48015 FTW - L-1 FLIGHT ATTENDANT MASK DIDN'T DROP DURING FLIGHT CHECK. ADJUSTED LATCHING MECH IAW MD80 MM 35-20-00. (M) 2 L 7 2 4F A6WE 2002011800174 20020118 00174 WP 2002 1 18 GTIA012078 1 20010822 A 3397 GROUND WIRE DOUG DC9 DC981 3022081 WP CABIN DIRTY A GTIA K NONE L NO TEST IN INSP/MAINT 1 NM 01 810NK 48015 L2 SERVICE DOOR OVERHEAD DROP CEILING LIGHT (EMERGENCY OR STANDBY) INOPERATIVE. CLEANED AC GROUND AND DC GROUND AT LIGH T FIXTURE. RECONNECTED GROUND WIRE TO STUD IAW MD80 MM 23-50-01. (M) 2 L 7 2 4F A6WE 2002011800175 20020118 00175 WP 2002 1 18 GTIA012079 1 20010906 A 5260 HINGE DOUG DC9 DC981 3022081 WP AFT AIRSTAIRS CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 FTW - AFT AIRSTAIRS, CORROSION LOWER HINGE AREAS, BOTH RIGHT AND LEFT SIDES. REMOVED CORROSION ON LOWER HINGE (LEFT) AR EA IAW MD80 SRM 51-10-3, REF WO 500013-11-N-00009. (M) 2 L 7 2 4F A6WE 2002011800176 20020118 00176 WP 2002 1 18 GTIA012080 1 20010906 A 5260 STIFFENER DOUG DC9 DC981 3022081 WP AFT AIRSTAIRS CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 FTW - AFT AIRSTAIRS, LEFT SIDE WALL DOUBLER CORRODED BETWEEN STEP SIDE WALL AND DOUBLER. REMOVED DOUBLER (STIFFENER) IA W MD80 SRM 51-30-2, ALL ITEMS ARE ON W/O 500013-11-N-00005. (M) 2 L 7 2 4F A6WE 2002011800177 20020118 00177 WP 2002 1 18 GTIA012081 1 20011212 A 3220 595224788 DEFLECTOR DOUG DC9 DC981 3022081 WP NLG CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FLL - RIGHT SIDE SPRAY DEFLECTOR ON NOSE GEAR CRACKED ON TOP APPROX 4 INCH FROM CENTER BOLTS. REMOVED AND REPLACED RIGH T NOSE GEAR SPRAY DEFLECTOR IAW MM 32-20-01. (M) 2 L 7 2 4F A6WE 2002011800178 20020118 00178 WP 2002 1 18 GTIA012084 1 20011220 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DAMAGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 DALLO 53012 DTW - FOUND EMERGENCY FLOOR PATH LIGHTING NOT ILLUMINATING SEAT ROWS 6-10. REPAIRED WIRE AT ROWS 10 AND OPS CHECK GOOD IAW MM 33-53-00. (M) 2 L 7 2 4F RT A6WE 2002011800179 20020118 00179 2002 1 18 GTIA012085 4 20011221 A 2210 ACCELEROMETER DOUG DC9 DC983 3022083 WP AUTOPILOT SYS FAULTY A GTIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 23 802NK 53168 DFGS DOES NOT WORK EITHER AP 1 OR 2, WILL NOT CAPTURE ALTITUDE, HOLD ALTITUDE IN A TURN THERE IS IMMEDIATE DESCENT, DOES NOT WORK IN PERF ON EITHER SIDE BOTH COMMAND BARS DISAPPEAR FROM VIEW WHEN TO GO BUTTONS ARE PUSHED PRIOR TO TAKEOFF TH E IAS MACH BUTTON DOES NOT WORK. REMOVED AND REPLACED ACCELEROMETER IAW 22-14-05 AUTO PILOT REQUIRES RTS IAW 22-01-05. (M) 2 L 7 2 4F RT A6WE 2002011800180 20020118 00180 WP 2002 1 18 GTIA012086 1 20011208 A 3110 4034234902 ANNUNCIATOR DOUG DC9 DC983 3022083 WP COCKPIT FAILED A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 808NK 49504 FLL - FLT 774 - FMA DOES NOT DISPLAY IN ANY MODE. FAILED EN ROUTE. REMOVED AND REPLACED F/O'S FMA'S IAW 34-24-00. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 2002011800181 20020118 00181 NM 2002 1 18 HALA0100296 1 20011213 A 2701 COMPUTER BOEING 717 717200 1383700 NM COCKPIT MALFUNCTIONED A HALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 WP 13 484HA 55129 HNL - FLT 191 - FLT CONTROL COLUMN DISCONNECT LIGHT ON IN FLIGHT. AIRCRAFT RETURNED TO HNL WHERE A UNEVENTFUL LANDING W AS MADE. REPLACED AND DATA CONCENTRATOR UNIT PER 2730 TASK 807. (M) 2 L 7 2 4F TR A6WE 2002011800182 20020118 00182 WP 2002 1 18 HALA0100298 1 20011212 A 3230 CONTROL BOX DOUG DC10 DC1010 3022110 WP LANDING GEAR FAULTY A HALA K NONE J WARNING INDICATION CL CLIMB 1 WP 13 152AA 46707 FLT 938 - ANC - RIGHT MAIN GEAR UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION, VISUALLY CHECK GEAR UNLOCK WINDOW IAW FC OM. TROUBLESHOT SYSTEM IAW TAFI 32-14-12-A-109, FOUND NR 12 PROX CTRL INOPERATIVE. REMOVED AND REPLACED BOX IAW 32-14- 00, OP CHECK GOOD. (M) 2 L 7 3 4F A22WE 2002012200050 20020122 00050 WP 2002 1 22 AT0100239 1 20011207 A 3350 1315 LAMP DOUG DC9 DC932 3022066 WP AFT ACCES COMP INOPERATIVE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 819AT 47260 FOUND EMERGENCY LIGHT RIGHT SIDE VENTRAL STAIRS WONT ILLUMINATE. CORRECTIVE ACTION: RELAMPED AS REQUIRED. IAW DC9 MM 33-50 2 L 7 2 4F A6WE 2002012200051 20020122 00051 WP 2002 1 22 AT0100240 1 20011207 A 3350 CM3071PBE LAMP DOUG DC9 DC932 3022066 WP TAIL CONE INOPERATIVE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 819AT 47260 FOUND 1 EACH TAIL CONE RELEASE HANDLE EMERGENCY EXIT LIGHT WONT ILLUMINATE. CORRECTIVE ACTION: RELAMPED A REQURED. IAW DC9 MM 33-51 2 L 7 2 4F A6WE 2002012200052 20020122 00052 WP 2002 1 22 AT0100241 1 20011211 A 3350 60030451 BATTERY PACK DOUG DC9 DC932 3022066 WP AFT ACCY COMP DISCHARGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 810AT 47277 FOUND AFT ACC COMPARTMENT EMERGENCY LIGHT WILL NOT SHUT OFF. CORRECTIVE ACTION: REPLACED BATTERY PACK CHARGER, B5-28 . IAW DCI MM 33-53, 56 2 L 7 2 4F A6WE 2002012200053 20020122 00053 WP 2002 1 22 AT0100242 1 20011211 A 3350 WIRE DOUG DC9 DC932 3022066 WP AFT SIDEWALL A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 837AT 45774 FOUND AFT ACCESSORY SIDEWALL ESCAPE PATH LIGHT INOPERATIVE. CORRECTIVE ACTION: REPAIRED WIRING AS REQUIRED. IAW DC 9 MM 33-50 AND 20-50. 2 L 7 2 4F A6WE 2002012200054 20020122 00054 WP 2002 1 22 AT0100243 1 20011220 A 7931 443330 O-RING DOUG DC9 DC932 3022066 WP OIL COOLER. INOPERATIVE A ZZDA E ENGINE SHUTDOWN K FLUID LOSS CL CLIMB 1 SO 15 836AT 47397 FOUND #1 ENGINE LOST ALL OIL, SHUT DOWN #1 ENGINE AT 38 PSI OIL PRESSURE-ALL OTHER ENGINE PARAMETERS DID NOT EXCEED ILIM ITATIONS. CORRECTIVE ACTION: FOUND BAD O-RING ON GEAR BOX TO OIL COOLER. REPLACED O-RING. IAW DC9 MM 79-20-2 2 L 7 2 4F A6WE 2002012200107 20020122 00107 2002 1 22 RAIA00201009 4 20010108 A 3418 COMPUTER EMB 145 EMB145 3260210 SO STALL WARNING MALFUNCTIONED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 802HK 145066 5308-TOL- STALL WARNING, NR 2 STALL PROTECTION SYSTEM INOP. MAINTENANCE RESET STALL COMPUTER AND OPS CHECK SYSTEM OK. 2 L 7 2 4F RT T00011AT 2002012200113 20020122 00113 EU 2002 1 22 RAIA00201016 1 20010111 A 3397 WIRE AEROSP ATR42 ATR42300 8680920 EU CABIN BROKEN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 421TE 102 MX-STL- CABIN DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED BROKEN WIRE ON EMERGENCY EXIT LIGHT. OPS CHECK OK. 2 H 7 2 4T RT A53EU 2002012200114 20020122 00114 EU 2002 1 22 SABA011072 1 20011217 A 7722 897476PR COMPENSATOR BAG JETSTM JETSTM3201 1500217 EU LT ENGINE OUT OF ADJ A SABA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 33 963AE 963 FLIGHT 5123 FROM CHS TO RDU ABORTED TAKEOFF DUE TO NUMBER ONE ENGINE WOULD NOT MAKE TAKEOFF TORQUE. AIRCRAFT RETURNED T O GATE. AIRCRAFT WAS INSPECTED AND FOUND AIRWORTHY FOR A FERRY FLIGHT 9477 TO CHARLOTTE FOR MAINTENANCE. AIRCRAFT ARR IVED CHARLOTTE WITH NO OTHER PROBLEMS. MAINTENANCE RESET THE LEFT ENGINE TEMP COMPENSATOR TO MAX SETTING 56. ENGINE PE RFORMANCE RUN WAS COMPLETED. ENGINE CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A56EU 2002012200125 20020122 00125 SO 2002 1 22 SWIA200110524 1 20011214 A 3397 TERMINAL EMB 120 EMB120ER 3260203 SO CABIN BROKEN A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 568SW 120343 FORWARD EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. REPAIRED BROKEN TERMINAL END AT EMERGENCY EXIT LIGHT FIXTURE AT FWD C LOSET. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002012200167 20020122 00167 NM 2002 1 22 02FDEA00056 1 20011231 A 5330 SKIN BOEING 727 7272S2F 1384O81 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 205FE 22927 TEMPORARY REPAIR ON EXTERNAL SKIN AT BS 1198 WL 182 BELOW STR 20R. 2 L 7 3 4F A3WE 2002012200177 20020122 00177 NM 2002 1 22 UPS01637365 1 20011214 A 2162 WARNING SYSTEM BOEING 767 76734AF 1385212 NM COCKPIT FALSE INDICATION A IPXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 311UP 27741 INSPECTION TYPE:N/A EICAS MSG: FWD EQPT OVERHEAT DISPLAYED AND OVERHEAT ILLUM. AFT SELECTOR WAS POSITIONED TO STBY, LT RE-ILLUM FOLLOWING 5 MIN DELAY. AFTER SELECTOR WAS POSITIONED TO OVERRIDE, EICAS MSG: FWD EQPT COOLING DISPL AND NO C OOLING LIGHT ILLUM. AS A RESULT AUTO 1 AND 2 PRESS CONTROLLERS FAILED. CABIN ALTITUDE CLIMBED TO 10,000 FEET. T/S PER FIM 21-58-00 FIG 116, NO FAULTS FOUND. T/S BLEED AIR SUPPLY BITE MOD AND PACK CONTROLLERS. NO FAULTS FOUND. CHECK PR ESSURIZATION AND PACK OPS WAS NORMAL. CABIN DIFF/PRESS WAS NORMAL. 2 L 7 2 4F RT A1NM 2002012200178 20020122 00178 WP 2002 1 22 UPS01837351 1 20011204 A 3350 LIGHT DOUG DC8 DC873F 302199F WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:N/A EMERGENCY DISARM LIGHT WILL NOT DISARM. RELAMPED EMERGENCY DISARM LIGHT, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2002012200179 20020122 00179 WP 2002 1 22 UPS01837355 1 20011206 A 5610 WINDSHIELD DOUG DC8 DC871F 302199D WP COCKPIT CRACKED A IPXA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 SO 01 700UP 45900 INSPECTION TYPE:N/A ATB- CAPT'S WINDSHIELD CRACKED. REMOVED AND REPLACED WINDSHIELD PER MM 56-10-02. 2 L 7 4 4F RT 4A25 2002012200180 20020122 00180 WP 2002 1 22 UPS01837357 1 20011208 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:IN EMERGENCY EXIT LIGHTS INOP. REPLACED EMERGENCY LIGHT BATTERY PACK, OPS GOOD. 2 L 7 4 4F RT 4A25 2002012200182 20020122 00182 EU 2002 1 22 NSVA0124 1 20011210 A 2435 23080031 STARTER GEN SAAB SF340 340B 7860101 EU LT ENGINE OVERHEATED A NSVA E ENGINE SHUTDOWN J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 27 299CJ 340B299 PIT - DURING ENGINE START UP, NR 1 ENGINE IGNITION LIGHT ILLUMINATED, LEFT GENERATOR OVER TEMP OVER HEAD LIGHT ILLUMINAT ED. SMOKE FROM TOP OF COWLING OF LEFT ENGINE WAS VISIBLE. ENGINE WAS SHUTDOWN. MAINTENANCE INSPECTED AREA, NO DAMAGE NOTED OTHER THAN STARTER GENERATOR. SUSPECT THAT GENERATOR BURNED UP INTERNALLY. (M) 2 L 7 2 4T RT A52EU 2002012200183 20020122 00183 EU 2002 1 22 SIMA20011296 1 20010509 A 2611 721112122000A SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY MALFUNCTIONED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 SW 21 266AE 340B266 PSP - FLT 3091 - AFTER START CREW GOT A CARGO SMOKE LIGHT INDICATION. CREW COMPLIED WITH CHECKLIST AND DISCHARGED FIRE BOTTLE. AIRCRAFT WAS FERRIED TO LAX FOR MAINTENANCE. MAINTENANCE REMOVED AND REPLACED THE CARGO SMOKE DETECTOR IAW SAA B MM. OPERATIONAL CHECK WAS GOOD. A NEW FIRE BOTTLE AND CARTRIDGE WAS INSTALLED AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2002012200184 20020122 00184 EU 2002 1 22 SIMA200131901 1 20011115 A 5320 WEB SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 356AE 340B356 ABI - DURING AN MBV INSPECTION, FOUND GALLEY FLOOR CORRODED, PREVIOUS REPAIR, BEYOND SRM LIMITS AT FS 258. REMOVED EXIS TING FILLER REPAIR AND REMOVED ADDITION CORROSION BY CUTOUT 1 INCH BY 1 INCH. FABRICATED TWO TRIPLERS ONE 9 INCH BY 4 I NCH, THE OTHER 7 INCH BY 4 INCH, A FILLER 19.5 INCH BY 1 INCH, .040 THICK, AND REUSED THE EXISTING DOUBLER. REPAIR DONE IAW SAAB 340 SRM (72LKS 3079 REV 38) 53-70-30 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT A52EU 2002012200185 20020122 00185 EU 2002 1 22 SIMA200131902 1 20011115 A 5414 SKIN SAAB SF340 340B 7860101 EU LT NACELLE CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 272AE 340B272 ABI - A CRACK WAS FOUND RADIATING FROM A RIVET ON THE LEFT NACELLE FORWARD INBOARD SIDE. REMOVED CRACK BY CUTOUT (1 INC H ROUND). PERFORMED EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED DOUBLER AND A FILLER. WORK DON E IAW SAAB 340 REPAIR STATEMENT SDS002838 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT A52EU 2002012200186 20020122 00186 EU 2002 1 22 SIMA200133401 1 20011130 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST NR NOT REPORTED 1 SW 21 278AE 340B278 BOS - FLT 4530 - EMERGENCY DOME LIGHTS AT 11A, 9A, AND 8A INOPERATIVE. RAI'D EMERGENCY BATTERY PACK, OPS CHECK GOOD. ( M) 2 L 7 2 4T RT A52EU 2002012200187 20020122 00187 EU 2002 1 22 SIMA200133403 1 20011130 A 3350 SIGN SAAB SF340 340B 7860101 EU CABIN MALFUNCTIONED A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 234AE 340B234 ILE - FLT 9305 - CREW REPORTED THE EXIT SIGN ABOVE PASSENGER DOOR AND FLIGHT ATTENDANT SEAT COME ON AND THEN GO OUT VERY QUICKLY. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL CHECK WAS GOOD IAW SAAB MM AND AIRCRAFT WAS RETURNE D TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2002012200188 20020122 00188 EU 2002 1 22 SIMA200133601 1 20011202 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 234AE 340B234 SHV - FLT 3912 - FIRST OFFICER REPORTED THE EMERGENCY EXIT SIGN ABOVE FLIGHT ATTENDANT SEAT ILLUMINATES FOR APPROXIMATEL Y 20 SECONDS AND THEN GOES OUT. THIS IS A REPEAT WRITE UP AND APPEARS TO BE INTERMITTENT. MAINTENANCE REMOVED AND REPL ACED THE POWER SUPPLY UNIT 21LN IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2002012200189 20020122 00189 EU 2002 1 22 SIMA200134107 1 20011207 A 3397 WIRE AEROSP ATR72 ATR72212A 8680902 EU CABIN BROKEN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 541AT 541 FORWARD EMERGENCY FLOOR LIGHTS HAS EVERY OTHER ONE INOPERATIVE MEL'D 33-30. MAINTENANCE FOUND AND REPAIRED A BROKEN WIR E IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002012200190 20020122 00190 EU 2002 1 22 SIMA200134402 1 20011210 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72212 8680945 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 270AT 270 SJU - FLT 3956 - CREW REPORTED THE FORWARD AND AFT EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD BATTERY PACK AND RECONNECTED THE BATTERY PACK IN THE AFT POWER SUPPLY UNIT. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002012200203 20020122 00203 NM 2002 1 22 AWXA200200059 1 20011231 A 5411 311A14507 DOUBLER BOEING 737 73733A 1384673 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 MCN - MAJOR REPAIR - "C" - DURING C-17 CHECK A 1/4" CRACK WAS FOUND ON DOUBLER FOR PYLON ACCESS PANEL 5727L AT NAC 216. MAINTENANCE PERFORMED HFEC INSPECTION TO IDENTIFY END OF CRACK THEN STOP DRILLED CRACK; FABRICATED REPAIR DOUBLER AND IN STALLED REPAIR IAW AWA ER 03-5433-00340-DL1 2 L 7 2 4F RT A16WE 2002012200204 20020122 00204 EU 2002 1 22 SIMA200134601 1 20011212 A 2612 472326 FIRE LOOP SAAB SF340 340B 7860101 EU RT ENGINE CHAFED A SIMA K NONE N FALSE WARNING AP APPROACH 1 SW 21 332AE 340B332 MRY - FLT 3349 - CREW REPORTED THE RIGHT ENGINE FIRE DETECTION LIGHT ILLUMINATED INTERMITTENTLY DURING DESCENT. MAINTEN ANCE FOUND THE FIRE LOOP FOR THE RIGHT ENGINE CHAFFED. FIRE DETECTION LOOP WAS REMOVED AND REPLACED IAW SAAB MM. OPERA TIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2002012200205 20020122 00205 NM 2002 1 22 TSAA0126181 1 20011223 A 2612 655280915 FIRE LOOP BOEING 737 737282 13844AT NM APU DEFECTIVE A TSAA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 13 824AL 23045 FLT 205 - HNL-LIH - EN ROUTE TO LIH, THE APU FIRE WARNING ILLUMINATED THOUGH THE APU WAS PREVIOUSLY MEL'D. THE APU FIRE BOTTLE WAS DISCHARGED AND THE AIRCRAFT RETURNED TO HNL WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS OPERATING UNDER MEL 49-1 FOR A PREVIOUS APU FIRE DETECTION TEST BEING INOPERABLE. MAINTENANCE INSPECTED AND REPLACED THE APU FIRE ELEMENT, AFT TAIL LOOP CONNECTORS, FIRE DETECTION UNIT AND FIRE BOTTLE. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURN ED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002012200206 20020122 00206 NM 2002 1 22 TSAA0133165 1 20011201 A 3350 86210066 BATTERY PACK BOEING 737 7372M6C 1384708 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 REPLACED NR 5 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OP CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002012200207 20020122 00207 NM 2002 1 22 TSAA0133166 1 20011129 A 3350 9221009 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED RIGHT OVERWING EMERGENCY EXIT LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4F A16WE 2002012200208 20020122 00208 NM 2002 1 22 TSAA0133167 1 20011130 A 3350 8731002511 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED NR 2 FLOOR PROXIMITY LIGHT ASSEMBLY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2002012200209 20020122 00209 NM 2002 1 22 TSAA0133168 1 20011202 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED NR 5 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2002012200210 20020122 00210 NM 2002 1 22 TSAA0133169 1 20011130 A 3350 9221009 BATTERY PACK BOEING 727 7272Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 809AL 21720 REPLACED LEFT OVERWING IDENT BATTERY PACKS DUE TO INOPERATIVE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2002012200211 20020122 00211 NM 2002 1 22 TSAA0133170 1 20011201 A 3350 9221009 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED AFT ENTRY EMERGENCY IDENT LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002012200212 20020122 00212 NM 2002 1 22 TSAA0133171 1 20011202 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 39735 REPLACED NR 2 FLOOR PROXIMATELY EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SE RVICE. (M) 2 L 7 2 4F RT A16WE 2002012200213 20020122 00213 NM 2002 1 22 TSAA0133172 1 20011201 A 3350 86210066 BATTERY PACK BOEING 737 73725A 1384481 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 819AL 23791 REPLACED NR 3 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002012200214 20020122 00214 NM 2002 1 22 TSAA0133182 1 20011224 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 807AL 23443 REPLACED NR 3 FLOOR LIGHT ASSEMBLY BATTERY PACK DUE TO BEING INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2002012200215 20020122 00215 NM 2002 1 22 TSAA0133183 1 20011227 A 3350 9221009 BATTERY PACK BOEING 737 737230 1384401 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 REPLACED RIGHT OVERWING LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002012200216 20020122 00216 NM 2002 1 22 TSAA0133184 1 20011227 A 3350 86210066 BATTERY PACK BOEING 737 737282 13844AT NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 23045 REPLACED NR 1 AND NR 3 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OP CHECK OK. AIRCRAFT RETURNED TO SERVIC E. (M) 2 L 7 2 4F RT A16WE 2002012200217 20020122 00217 NM 2002 1 22 USAA011332 1 20011019 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 611AU 27123 CLT - FOUND FLOORBEAM STRAP CRACKED 2 INCHES, BS 365.25, LBL 27. INSTALLED DOUBLER REPAIR PER SRM 53-10-51. (M) 2 L 7 2 4F RT A2NM 2002012200218 20020122 00218 NM 2002 1 22 USAA011337 1 20011024 A 5320 SPLICE BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AU 22201 CLT - FOUND BUTT SPLICE CORROSION, STATION 1620 AT LBL 6 TO RBL 6. INSTALLED REPAIR DOUBLER AND BUTT SPLICE PER EA 8556 3. (M) 2 L 7 2 4F RT A2NM 2002012200219 20020122 00219 NM 2002 1 22 USAA011338 1 20011030 A 5313 STRINGER BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AU 53716 22201 CLT - FOUND STRINGER CORRODED 2 INCHES, STRINGER 30 BL 0 AT STATION 1614. INSTALLED STRINGER SPLICE. (M) 2 L 7 2 4F RT A2NM 2002012300131 20020123 00131 WP 2002 1 23 DHL2002805007 1 20011231 A 5311 ANGLE DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 805DH 75397 46125 N/R 0925AFT. ACCESSORY COMPT. - FRAME TO FUSELAGE ANGLE CRACKED. STA. 660 L21R-L22R 2 L 7 4 4F RT 4A25 2002012300138 20020123 00138 WP 2002 1 23 DHL2002805009 1 20011230 A 5322 INTERCOSTAL DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 805DH 75397 46125 N/R 0860COCKPIT- INTERCOSTAL CRACKED 1/4" STA. 22 LBL 12 2 L 7 4 4F RT 4A25 2002012300140 20020123 00140 WP 2002 1 23 DHL2002805011 1 20011229 A 5300 SKIN DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 805DH 75397 46125 N/R 0051NOSE LANDING GEAR WHEEL WELL R/H AFT CORNER CRACKED 1/4" STA.8.00 L33R (MAJOR REPAIR) 2 L 7 4 4F RT 4A25 2002012300144 20020123 00144 WP 2002 1 23 ABXA010669 1 20011229 A 5320 37502571 SPLICE DOUG DC8 DC861 3021952 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 853AX 46037 AFT CARGO, FS 1040 - 1060, LONGERON 31 RIGHT, SPLICE FITTING WAS CRACKED. RECEIVED NEW FITTING P/N 3750257-1. INSTALLE D IAW DC-8 SRM 51-1-20D. REMOVED DAMAGED FITTING IAW DC-8 SRM 51-3-2. 2 L 7 4 4F 4A25 2002012400053 20020124 00053 NE 2002 1 24 AT0100244 2 20011222 A 7200 JT8 ENGINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE NR 1 FAILED A ZZDA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 15 836AT 47397 FOUND NR 1 ENGINE LOST OIL QUANTITY. OIL TEMPERATURE WENT UP AND OIL PRESSURE WENT DOWN. ENGINE WAS SHUT DOWN, ENGINE TURNED FOR 25-30 MINUTES AT LESS THAN 10 PSI. REMOVED AND REPLACED THE NR 1 ENGINE IAW DC9 72-00. 2 L 7 2 4F 4 F A6WE E2EA 2002012400055 20020124 00055 CE 2002 1 24 2002F00037 1 20011221 A 2730 50934042 TORQUE TUBE CESSNA CESSNA 421 421C 2076016 CE CONT O520 GTSIO520N 17032 SO MCAULY 3FF32 3FF32C501 GL ELEVATOR CORRODED E K NONE O OTHER IN INSP/MAINT 1 WP 09 6793V 4401 1022 421C1022 DURING A AAIP 100 HOUR INSPECTION, SEVERE CORROSION WAS NOTED IN THE RIGHT ELEVATOR TORQUE TUBE. THE CORROSION (RUST) HA S DEPLETED AT LEAST 75% OF THE MATERIAL THICKNESS. THE LEFT ELEVATOR WAS REMOVED TO INSPECT THE TORQUE TUBE FOR CORROSIO N. NONE WAS NOTED. THE RIGHT ELEVATOR HAS THE TRIM TAB ASSEMBLY. THE TORQUE TUBE END IS EXPOSED TO THE ELEMENTS WHERE TH E TRIM TAB ROD END PASSES THROUGH THE ELEVATOR. 1 L 7 2 3O 3 O A7CE E7CE 5 C P45GL 2002012400061 20020124 00061 EU 2002 1 24 MALA020112 1 20011201 A 2770 DAMPENER BAC 146 AVRO146RJ85A 1500097 EU ELEVATOR DEFECTIVE A MALA K NONE O OTHER NR NOT REPORTED 1 GL 15 511XJ E2325 PREVIOUS CREW REPORTED ELEVATORS NOT DAMPENING IN THE WIND. MAINTENANCE REMOVED AND REPLACED LT AND RT ELEVATOR GUST DA MPNERS PER AMM 27-70-14. REPLACED RT ELEVATOR ATTACH FITTING PER AMM 27-10-14. OPS CHECK GOOD. SEE MM 409 NR 101951, AND CONT CARD 67500, 060069, 059040 FOR DETAILS. 2 H 7 4 4F RT A49EU 2002012400067 20020124 00067 EU 2002 1 24 MALA020113 1 20011220 A 2730 BOLT BAC 146 AVRO146RJ85A 1500097 EU ELEVATOR CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 510XJ E2323 DURING C2-CHECK IN CVG, 336AB ON RT ELEVATOR TWO BOLTS FOR ELEVATOR SERVO TAB ACTUATOR ARM HAS CORROSION. MAINTENANCE R EPLACED RT ELEVATOR SERVO TAB ACTUATOR ARM BOLTS TWO EACH IAW AMM 20-10-19. 2 H 7 4 4F RT A49EU 2002012400070 20020124 00070 EU 2002 1 24 MALA020114 1 20011220 A 2730 BOLT BAC 146 AVRO146RJ85A 1500097 EU ELEVATOR CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 510XJ E2323 DURING C2-CHECK IN CVG, IN PANEL 335AB ON LT ELEVATOR TWO BOLTS FOR LT ELEVATOR SERVO TAB ACTUATOR HAVE CORROSION. MAIN TENANCE REPLACED 2 BOLTS BEHIND PANEL 335AB ON LT ELEVATOR SERVO TAB ACTUATOR ARM IAW AMM 20-10-19. 2 H 7 4 4F RT A49EU 2002012400072 20020124 00072 EU 2002 1 24 MALA020115 1 20011223 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 510XJ E2323 DURING C2-CHECK IN CVG, FRAME 18 CORROSION PRESENT IN CORNER AT AREA WHERE SEAT RAIL NR 3 MEETS ON THE SEAT AREA ITSELF. MAINTENANCE REPAIRED SEAT RAIL NR 3 IAW MAL EO A53026. CORROSION ON FRAME 18 FLOORBEAM AT NR 3 & 4 SEAT RAIL AND IN B ETWEEN BEAM AT NR 3 & 4 SEAT RAIL. FRAME 18 FLOORBEAM REPAIRED PER BARA/AVR/5695/01 MGK AND RIL HC531H9251 ISSUE 2-REF EO A53076. 2 H 7 4 4F RT A49EU 2002012400073 20020124 00073 EU 2002 1 24 MALA020116 1 20011222 A 5320 SILL BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 510XJ E2323 DURING C2-CHECK IN CVG, AFT PAX DOOR SILL PLATE HAS CORROSION. MAINTENANCE REMOVED AND REPLACED SILL PLATE, INSTALLED N EW SERVICEABLE SILL PLATE IN ACCORDANCE WITH AMM 51-23-00, 51-42-00, 51-43-00, AND 51-52-11. 2 H 7 4 4F RT A49EU 2002012400075 20020124 00075 EU 2002 1 24 MALA020118 1 20011223 A 5320 PLATE BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 510XJ E2323 DURING C2-CHECK IN CVG, SACRIFICIAL PLATE BETWEEN SEAT RAIL NR 3 AND NR 4 ON FRAME 20 HAS CORROSION ON IT, SRM 53-20-32, FIG 1, ITEM 6. MAINTENANCE REMOVED AND REPLACED SACRIFICIAL PLATE PER SRM 51-42-00/51-52-11-43-00/51-23-00/52-25-00. 2 H 7 4 4F RT A49EU 2002012400076 20020124 00076 EU 2002 1 24 MALA020119 1 20011223 A 5260 C14647 HAND RAIL BAC 146 AVRO146RJ85A 1500097 EU AIRSTAIRS CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 510XJ E2323 DURING C2-CHECK IN CVG, CORROSION BEYOND LIMITS FOUND ON O/B AIRSTAIR RAIL. MAINTENANCE REPLACED O/B AIRSTAIR RAIL P/N C14647 WITH NEW IAW SRM 51-42-00, 51-43-00 AND BAE SYSTEMS FAX BARA/AVR/5714/02-MGK. 2 H 7 4 4F RT A49EU 2002012400085 20020124 00085 WP 2002 1 24 DHL2002805013 1 20011230 A 5712 RIB DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 805DH 75397 46125 N/R 0435RH WING L/E - UPPER RIB (FORMER) @ STA XFS608.000 , .500 CRACKED 2 L 7 4 4F RT 4A25 2002012400088 20020124 00088 WP 2002 1 24 DHL2002805014 1 20011230 A 5712 RIB DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 805DH 75397 46125 N/R 0432RH. WING L/E- UPPER RIB (FORMER) @ STA. XFS 615.000 , CRACKED .500 2 L 7 4 4F RT 4A25 2002012400093 20020124 00093 WP 2002 1 24 DHL2002805015 1 20011230 A 5712 RIB DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 805DH 75397 46125 N/R 0436RH. WING L/E- UPPER RIB @ STA. XFS601.000 , CRACKED .500 2 L 7 4 4F RT 4A25 2002012400100 20020124 00100 CE 2002 1 24 2001F00730 1 20011203 A 2730 DW6 BEARING CESSNA NA CESSNA 500 550 2076604 CE BELLCRANK FROZEN B K NONE O OTHER IN INSP/MAINT 1 SO 11 117TA 6558 903 NA 5500464 AFT ELEVATOR BELLCRANK BEARING DW6 FROZE CAUSING BELLCRANK MOUNTING BOLT TO ROTATE AND ENLARGE MOUNTING HOLES IN BELLCRA NK SUPPORT ASSEMBLY BRACKETS 565344-17 AND 5565344-18. 1 L 7 2 4F A22CE 2002012400114 20020124 00114 NM 2002 1 24 2002F00041 1 20011219 A 2613 SWITCH BOEING 737 737205 1384456 NM OVERHEAT SYS DAMAGED A SOKF A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 23 235TA 21765 MIA - FLT 473 - BOTH WING BODY OVERHEAT LIGHTS ILLUMINATES DURING TAKEOFF AND REMAIN ILLUMINATED DURING FLIGHT. DURING TROUBLESHOOTING FOUND TEST SWITCH DAMAGE, ENTERED IN DEFERRED ITEM. PERFORMED OPERATIONAL TEST, SYSTEM WORKS NORMAL ON BOTH SENSORS. REPLACED TEST SWITCH PER AMM, AND AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2002012400115 20020124 00115 NM 2002 1 24 2002F00043 1 20011226 A 5320 SUPPORT BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND STRINGER SUPPORT TIE CRACKED AT FUSELAGE STATION 727B LONGERON 6L. (M) 2 L 7 2 4F A16WE 2002012400116 20020124 00116 NM 2002 1 24 2002F00019 1 20011201 A 5330 SKIN DOUG DC10 DC1040F 3023507 NM FUSELAGE CORRODED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 141WE 46661 DURING C-CHECK, THE FORWARD LEFT AIR CONDITIONING BAY CAP ANGLE AT STATION 595 BETWEEN LONGERON 47L AND 47L WAS CORRODED PAST SRM LIMITS. A REPAIR DOUBLER WAS INSTALLED ON THE EXTERIOR OF THE SKIN TO REINFORCE THE BLEND AREA IAW TIMCO REO- G08333. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 2002012400117 20020124 00117 NM 2002 1 24 2002F00034 1 20011107 A 3350 8821004 BATTERY PACK BOEING 737 7372Q8C 138448S NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 SEA - EMERGENCY EXIT LIGHT RECEIVER NOT INDICATING AT SEAT PALLET G-9. REMOVED AND REPLACED EMERGENCY EXIT LIGHT RECEIV ER (P/N 883200312) AND BATTERY PACK (P/N 8821004), THEN OPS CHECKED GOOD. REF ASAA0110639. (M) 2 L 7 2 4F A16WE 2002012400118 20020124 00118 NM 2002 1 24 ASAA0110594 1 20011010 A 5313 BAC1498163 STRINGER BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER 27R AT BODY STATION 531-533, CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2002012400119 20020124 00119 NM 2002 1 24 ASAA0110595 1 20011010 A 5320 654659525 TIE BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER TIE AT BODY STATION 727A, STRINGER 27L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2002012400120 20020124 00120 NM 2002 1 24 ASAA0110636 1 20011105 A 3397 8731002142 CONNECTOR BOEING 737 7372X6C 1384552 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - OVERHEAD EMERGENCY EXIT SIGN AT ROW 20 DOES NOT ILLUMINATE. RECONNECTED CANNON PLUG, THEN OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A16WE 2002012400121 20020124 00121 NM 2002 1 24 ASAA0110639 1 20011107 A 3350 883200312 RECEIVER BOEING 737 7372Q8C 138448S NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 SEA - EMERGENCY EXIT LIGHT RECEIVER NOT INDICATING AT SEAT PALLET G-9. REMOVED AND REPLACED EMERGENCY EXIT LIGHT RECEIV ER (P/N 883200312) AND BATTERY PACK (P/N 8821004), THEN OPS CHECKED GOOD. (M) 2 L 7 2 4F A16WE 2002012400122 20020124 00122 NM 2002 1 24 ASAA0110642 1 20011115 A 3350 86210144 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 JNU - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROW 18 WOULD NOT EXTINGUISH. REMOVED AND REPLACED THE RE MOTE ASSEMBLY BATTERY, THEN LIGHTS OPS CHECKED GOOD. (M) 2 L 7 2 4F A16WE 2002012400123 20020124 00123 NM 2002 1 24 ASAA0140137 1 20011107 A 3397 8100022605 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 780AS 25112 SEA - DURING LINE CHECK, FOUND EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 6-12. WIRE DISCONNECTED. RECONNECTED WIRE, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002012400124 20020124 00124 NM 2002 1 24 ASAA0140599 1 20011016 A 5310 6596554501 DOOR FRAME BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING C-CHECK, FOUND CORROSION ON FORWARD SURFACE AFT FRAME OF AFT CARGO DOOR CUT OUT AT STRINGER 25R TO 23R. RE PAIRED DAMAGED FRAME BY INSTALLING DOUBLER PER ENGINEERING REPAIR. (M) 2 L 7 2 4F A16WE 2002012400125 20020124 00125 NM 2002 1 24 ASAA0140606 1 20011016 A 5320 69353521 STRINGER CLIP BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING C-CHECK, FOUND CORROSION ON STRINGER TIE AT STATION 533 AND STRINGER 27L. REPAIRED IAW SRM. (M) 2 L 7 2 4F A16WE 2002012400126 20020124 00126 WP 2002 1 24 ASAA0180299 1 20011111 A 3350 0105606 MODULE DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 967AS 49103 SEA - DURING LINE CHECK, FORWARD CABIN EMERGENCY TRACK LIGHTING WAS DETERMINED TO BE INOPERATIVE. REPLACED LIGHT MODULE . LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2002012400127 20020124 00127 WP 2002 1 24 ASAA0180301 1 20011113 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP COCKPIT DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 954AS 49387 SFO - DURING PREFLIGHT CHECK, FOUND COCKPIT OVERHEAD EMERGENCY LIGHTING WAS INOPERATIVE. REPLACED ASSOCIATED BATTERY PO WER SUPPLY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2002012400128 20020124 00128 EA 2002 1 24 ASOA01286 1 20011215 A 3350 100865 POWER SUPPLY CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 859AS 7421 FLT 4504 - DURING GROUND INSPECTION IN ATL, THE LEFT AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002012400129 20020124 00129 EA 2002 1 24 ASOA01287 1 20011217 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 867AS 7463 FLT 4787 - DURING SCHEDULED INSPECTION IN XNA, THE NR 3 CABIN OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REM OVED AND REPLACED THE NR 3 OVERHEAD EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002012400130 20020124 00130 SO 2002 1 24 ASOA01288 1 20011217 A 3350 BATTERY EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 268AS 120202 DURING HANGAR INSPECTION IN TXK, THE FORWARD SECTION OF EMERGENCY TRACK LIGHTING WAS INOPERATIVE. MAINTENANCE ALLOWED T HE BATTERIES FOR THE EMERGENCY LIGHTS TO CHARGE IN THE ARM POSITION. THEN MAINTENANCE PERFORMED OPERATIONAL CHECKS OUT OF THE ARM POSITION. NO DEFECTS WERE NOTED. FOUND BATTERIES OK. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002012400131 20020124 00131 SO 2002 1 24 ASOA01289 1 20011217 A 3350 F02A250V1A FUSE EMB 120 EMB120RT 3260202 SO CABIN BROKEN A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 245AS 120075 FLT 4078 - DURING GROUND INSPECTION IN ATL, THE FIRST FOUR EMERGENCY FLOOR LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE F OUND A BROKEN FUSE IN THE FORWARD CLOSET. MAINTENANCE REMOVED AND REPLACED THE BROKEN FUSE AND ALSO CLEANED THE TERMINA L ENDS TO THE LIGHTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002012400132 20020124 00132 EA 2002 1 24 ASOA01290 1 20011218 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 823AS 7196 FLT 4787 - DURING SCHEDULED INSPECTION IN XNA, THE MIDDLE INTERIOR CEILING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT MIDDLE CEILING EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SER VICE. (M) 2 L 7 2 4F RT A21EA 2002012400133 20020124 00133 WP 2002 1 24 GTIA012058 1 20011215 A 3350 CHARGER DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 969ML 47268 ACY - TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED AFT EMERGENCY FLOOR PATH CHARGER. OPS CHECK GOOD IA W MM 33-50-0. (M) 2 L 7 2 4F A6WE 2002012400134 20020124 00134 WP 2002 1 24 GTIA012087 1 20011118 A 5751 AILERON DOUG DC9 DC932 3022066 WP LT WING DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND LEFT AILERON OUTBOARD TRAILING EDGE DELAMINATED. REPAIRED LEFT AILERON OUTBOARD TRAILING EDGE IAW DC9/MD80 SRM 57-03. (M) 2 L 7 2 4F A6WE 2002012400135 20020124 00135 WP 2002 1 24 GTIA012091 1 20011108 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CRACK IN SKIN 1 INCH LONG ON FORWARD SIDE OF FASTENER HOLE, 1 INCH LONG ON AFT SIDE OF FASTENER HOLE, 2 INCH ES OVERALL LENGTH. STOP DRILL CRACK. FABRICATE REPAIR DOUBLER. INSTALLED NEW REPAIR IAW DC9 SRM 53-01. (M) 2 L 7 2 4F A6WE 2002012400136 20020124 00136 WP 2002 1 24 GTIA012092 1 20011113 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND AFT ACCESSORY COMPARTMENT RIGHT STATION 1076 RIGHT LONGERON 14 ROD SUPPORT BROKEN. REMOVED DAMAGED PART. F ORMED NEW SUPPORT. INSTALLED SUPPORT IN A/C AFT COMPARTMENT IAW SRM DC9 51-30-1. (M) 2 L 7 2 4F A6WE 2002012400137 20020124 00137 WP 2002 1 24 GTIA012093 1 20011107 A 5752 SKIN DOUG DC9 DC932 3022066 WP AILERON TAB DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND RIGHT WING, INBOARD AILERON TAB, INBOARD CORNER UPPER SIDE DELAMINATION, 1.500 INCH SPAN BY 1 INCH, CHORD. REMOVED DAMAGE TO AILERON TAB. REPAIR TAB PER DC9 MD80 SRM 57-04. (M) 2 L 7 2 4F A6WE 2002012400138 20020124 00138 WP 2002 1 24 GTIA012094 1 20011105 A 5753 VANE DOUG DC9 DC932 3022066 WP T/E FLAP GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND RIGHT WING FIXED FLAP VANE HAS A GOUGE AT STATION XTE 206 (OUTBOARD SURFACE). BLEND OUT LEADING EDGE COVER AND FOUND IT OUT OF LIMITS. LOCATE AND DRILL DOUBLER AND FILLER. INSTALLED REPAIR PARTS IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002012400139 20020124 00139 WP 2002 1 24 GTIA012095 1 20011215 A 7110 DOUBLER DOUG DC9 DC932 3022066 WP NR 2 COWLING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - NR 2 ENGINE NOSE COWL 2ND INTERNAL RIB (FROM AFT) 6 O'CLOCK POSITION REPAIR DOUBLER CRACKED. REMOVED DOUBLER REPA IR CRACKED. FORMED NEW SPLICE DOUBLER, INSTALLED NEW REPAIR IAW DC9 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 2002012400140 20020124 00140 WP 2002 1 24 GTIA012096 1 20011113 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - E/E BAY FLOOR SUPPORT BEAM, STATION 200 HAS DRILL MARKS AND CORROSION NEXT TO NUT PLATES, BOTH INBOARD AND OUTBOAR D ENDS OF FRAME. FORMED NEW REPAIR PARTS. INSTALLED REPAIR PARTS IAW DC9 SRM 51-30-1 AND 51-30-2. (M) 2 L 7 2 4F A6WE 2002012400141 20020124 00141 WP 2002 1 24 GTIA012100 1 20011106 A 5330 DOUBLER DOUG DC9 DC932 3022066 WP FUSELAGE IMPROPER A GTIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND STATION 148 RIGHT HAS A DEN AS MARKED AROUND 02 BLOW OUT DISK. UPON FURTHER EVALUATION FOUND PRODUCTION INT ERNAL DOUBLER HAVE NO CONTOUR. FABRICATE NEW INTERNAL DOUBLER. INSTALLED NEW INTERNAL DOUBLER IAW DC9 SRM 51-30-1. (M ) 2 L 7 2 4F A6WE 2002012400142 20020124 00142 WP 2002 1 24 GTIA012101 1 20011106 A 5542 SKIN DOUG DC9 DC932 3022066 WP RUDDER CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND RUDDER LEFT UPPER SKIN CRACKED AT FASTENER ON RIB LOCATION NR 21. TRIMMED OUT CRACKED SKIN WITH CIRCULAR CU TOUT. FORMED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR DOUBLER AND FILLER IAW DC9 SRM 55-03. (M) 2 L 7 2 4F A6WE 2002012400143 20020124 00143 WP 2002 1 24 GTIA012102 1 20011107 A 7110 WEB DOUG DC9 DC932 3022066 WP LT COWLING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND LEFT POWER PLANT NOSE COWL AFT INNER SECTION CRACK. REMOVED CRACKED WEB DOUBLER FROM NOSE COWL. FABRICATED NEW DOUBLER AND WEB. INSTALLED DOUBLER ON WEB. INSTALLED WEB PER DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002012400144 20020124 00144 WP 2002 1 24 GTIA012103 1 20011115 A 5230 FITTING DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - AFT LOWER CARGO DOOR, CENTER INTERCOSTAL TO PAN ANGLE FITTING CRACKED. REMOVED CRACKED ANGLE FITTING. INSTALLED FITTING IAW DC9 SRM 51-30-1 AND 51-30-5. (M) 2 L 7 2 4F A6WE 2002012400145 20020124 00145 WP 2002 1 24 GTIA012104 1 20011113 A 5320 1591013037 CHANNEL DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND AFT PRESSURE BULKHEAD , AFT SIDE BELOW ENTRY DOOR THRESHOLD, THE 15910130-37 CHANNEL HAS A 1.3 INCH LONG CRA CK 7 INCHES INBOARD FROM LEFT EDGE. REMOVED FITTING. DRILLING NEW FILLING. INSTALLED NEW FITTING IAW DC9 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 2002012400146 20020124 00146 WP 2002 1 24 GTIA012105 1 20011116 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - RIGHT INBOARD FLOORBOARD STATION 579-680 HAS BARE METAL AND SURFACE CORROSION AND DENTS. LOCATED AND DRILLED AND COUNTERSINK FLOORBOARD. INSTALLED FLOORBOARD FS 579-680 RIGHT CENTER IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002012400147 20020124 00147 WP 2002 1 24 GTIA012106 1 20011116 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CORROSION, NICKS AND GOUGES AT X 44 SEAT TRACK FROM STATION 765 TO STATION 860. INSTALLED SECTION OF SEAT T RACK FROM STATION 765 TO Y 860 X 44 IAW SRM DC9 53-05. (M) 2 L 7 2 4F A6WE 2002012400148 20020124 00148 WP 2002 1 24 GTIA012107 1 20011108 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CORROSION, NICKS AND GOUGES AT SEAT TRACK X44 FROM STATION 649 TO STATION 765. INSTALLED SECTION OF SEAT TR ACK FROM STA Y 649 TO Y 765 X 44 IAW SRM DC9 53-05. (M) 2 L 7 2 4F A6WE 2002012400149 20020124 00149 WP 2002 1 24 GTIA012108 1 20011108 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CORROSION, NICKS AND GOUGES AT SEAT TRACK BY 44 INCHES FROM STATION Y 532 TO STA 649. INSTALLED SECTION OF SEAT TRACK FROM STA 532 TO STA 649. (M) 2 L 7 2 4F A6WE 2002012400150 20020124 00150 WP 2002 1 24 GTIA012109 1 20011127 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND ANGLE SUPPORT HAS ELONGATED HOLES, AT LEFT TRAPEZOIDAL PANEL AFT UPPER AREA STA Y 730. UPON FURTHER INVESTI GATION, FOUND CRACK IN SKIN AREA FOUND TO BE OUT OF LIMITS. FABRICATED DOUBLER. INSTALLED REPAIR IAW DC9 SRM 55-03. ( M) 2 L 7 2 4F A6WE 2002012400151 20020124 00151 WP 2002 1 24 GTIA012110 1 20011126 A 5542 SKIN DOUG DC9 DC932 3022066 WP RUDDER CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND RUDDER RIGHT UPPER SKIN, .50 INCH DIAMETER DENT IN SKIN BETWEEN RIBS 17 AND 18. UPON FURTHER INVESTIGATION CRACK FOUND IN SKIN AREA FOUND TO BE OUT OF LIMITS. FABRICATED DOUBLER. INSTALLED REPAIR IAW DC9 SRM 55-03. (M) 2 L 7 2 4F A6WE 2002012400152 20020124 00152 WP 2002 1 24 GTIA012111 1 20011106 A 5330 PANEL DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND RIGHT TRAPEZOIDAL PANEL CRACKED AT FASTENER LOCATIONS NR 8 AND NR 9. REMOVED DAMAGE. FABRICATED ANGLES AND FILLER. INSTALLED REPAIR ANGLES AND FILLER PER DC9 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 2002012400153 20020124 00153 WP 2002 1 24 GTIA012112 1 20011119 A 5320 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CABIN LEFT SIDE CORRODED AT MEMBRANE WEB STATION 908. REMOVED MEMBRANE WEB FROM STATION 897 TO 964. FORMIN G MEMBRANE/WEB. INSTALLED NEW MEMBRANE/WEB IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002012400154 20020124 00154 WP 2002 1 24 GTIA012113 1 20011119 A 5311 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND FRAME CORRODED AT STATION 927 BETWEEN LONGERON 18L TO 15L. FRAME FOUND TO BE OUT OF LIMITS. INSTALLED DOUB LER IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002012400155 20020124 00155 WP 2002 1 24 GTIA012114 1 20011116 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND LEFT OUTBOARD FLOORBOARD STATION 832-894 BENT, CRACKED, OVERSIZE HOLES, SURFACE CORROSION. REMOVED CRACKED STRIP. FABRICATED NEW STRIP. INSTALLED NEW STRIP IAW DC9 SRM 51-70. (M) 2 L 7 2 4F A6WE 2002012400156 20020124 00156 WP 2002 1 24 GTIA012115 1 20011116 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND RIGHT OUTBOARD FLOORBOARD STATION 389-465 FASTENER HOLES OVERSIZED, SURFACE CORROSION, BARE METAL. TWO OVER SIZED HOLES HAVE CRACKS AND PANEL, AFT END OF PANEL HAS FASTENER HOLE CRACK. INSTALLED DOUBLERS ON FORWARD END OF PANEL . (M) 2 L 7 2 4F A6WE 2002012400157 20020124 00157 WP 2002 1 24 GTIA012117 1 20011115 A 5320 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - PAX CABIN FLOOR WEB HAS CRACK STATION 220 X44. FORMED WEB. INSTALLED WEB IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002012400158 20020124 00158 WP 2002 1 24 GTIA012122 1 20011206 A 5321 CHANNEL DOUG DC9 DC932 3022066 WP FLOOR PANEL CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND FORWARD ENTRY FLOOR PANEL HAT CHANNEL HAS CRACKED. REMOVED CRACKED CHANNEL. FABRICATED CHANNEL. INSTALLED CHANNEL IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002012400159 20020124 00159 WP 2002 1 24 GTIA012123 1 20011115 A 5230 PAN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND AFT LOWER CARGO DOOR PAN CRACKED AT FORWARD END OF NR 1 BEAM. FORMED NEW DOUBLER. INSTALLED NEW STRIPS IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002012400160 20020124 00160 WP 2002 1 24 GTIA012124 1 20011121 A 5320 WEB DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND LOWER INNER WEB FORWARD BAG DOOR FS 370 TO FS 427 HAS OVERSIZED HOLES, EXTRA HOLES, CORRODED HOLES, A BAD PR EVIOUS REPAIR AND NUMEROUS DENTS FROM OVER DRIVEN RIVETS. LOCATED AND DRILLED NEW INNER WEB. INSTALLED INNER WEB IAW D C9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002012400161 20020124 00161 WP 2002 1 24 GTIA012125 1 20011115 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CABIN FLOORBOARD CENTER LEFT STATION 832 TO 889, LOWER SURFACES UPPER CORNER HAS AN AREA OF METAL CRACKED 9 INCHES LONG. FLOORBOARD DAMAGE ARE FOUND TO BE OUT OF LIMITS. FABRICATED NEW FLOORBOARD IAW SRM DC9 51-01. (M) 2 L 7 2 4F A6WE 2002012500011 20020125 00011 WP 2002 1 25 0105189985 1 20011221 A 5230 DOOR DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 985US 47479 During HCK in DHN a crack was found in the Aft cargo Door Inner and Outer Pans. The damage to the outer pan was repaired in accordance with TRM 51-72-01. The inner pan was repaired per EA 99-187654. 2 L 7 2 4F A6WE 2002012500012 20020125 00012 WP 2002 1 25 0105199601 1 20011220 A 5240 DOOR DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 601NW 47038 During an Hck in DHN a .6" crack was found in the forward galley service door pan at the #4 door stop. Repaired per EA 9 6-187652. 2 L 7 2 4F A6WE 2002012500013 20020125 00013 WP 2002 1 25 0105209613 1 20011227 A 5710 SPAR CAP DOUG DC9 DC932 3022066 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 613NW 47438 During Mck in DHN the right wing rear spar upper cap was found corroded at the inboard hole. Repaired per EA 96-187657. 2 L 7 2 4F A6WE 2002012500024 20020125 00024 NM 2002 1 25 AWXA200200043 1 20011228 A 5311 65465391 FRAME BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 MCN - MAJOR REPAIR - C - DURING C-15 CHECK MAINTENANCE DISCOVERED CRACKED FRAME AT FASTENER BS 616, RBL 64. MAINTENANCE CUTOUT DAMAGED AREA OF FRAME, HFEC INSPECTION COMPLIED WITH TO VERIFY CRACK CONTAINED, FABRICATED AND INSTALLED REPAIR STIFFENER ANGLE AND FILLER IAW AWA ER 03-5311-01143-DD1. 2 L 7 2 4F RT A16WE 2002012500028 20020125 00028 NM 2002 1 25 AWXA200200060 1 20011231 A 5315 654881138 FLOORBEAM BOEING 737 7373S3 1384711 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 MCN - MAJOR REPAIR - C - DURING C-15 CHECK MAINTENANCE DISCOVERED CORROSION ON MAIN CABIN FLOORBEAM AT PREVIOUS REPAIR F ILLER, BS 967, LBL 28, WL 208.1. MAINTENANCE REMOVED REPAIR ANGLES AND FILLER AT BS 967 BEAM, CLEANED CORROSION ON FILL ER AND FOUND MATERIAL THICKNESS LOSS TO BE WITHIN LIMITS. REINSTALLED REPAIR ANGLES AND FILLER IAW B737-300 SRM 51-40-0 2, PG 10-11, SRM 53--60-51 FIG 101, PG 105-114 AND BMM 51-21-41, PG 701-708. 2 L 7 2 4F RT A16WE 2002012500070 20020125 00070 EU 2002 1 25 QXEA0102116 1 20011212 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - FUSELAGE FRAME 16660 TIE-IN CLIP TO SKIN IS CRACKED THROUGH RIVET HOLE AT STRINGER 32. REPAIRED IAW FOKKER SRM 53 -02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002012500071 20020125 00071 EU 2002 1 25 QXEA0102117 1 20011212 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - FUSELAGE FRAME 16060 TIE-IN CLIP TO SKIN IS CRACKED THROUGH RIVET HOLE AT STRINGER 31. REPAIRED IAW FOKKER SRM 53 -02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002012500073 20020125 00073 EU 2002 1 25 QXEA0102118 1 20011213 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - RT INBOARD SEAT TRACK PITTING CORROSION AT STATION 7805. REPAIRED IAW FOKKER SRM 53-01-01 AND HORIZON AIR EA 4-53 -1542. 2 L 7 2 4F RT A20EU 2002012500074 20020125 00074 EU 2002 1 25 QXEA0102119 1 20011214 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - RT INBOARD SEAT TRACK CORRODED AT STATION 5060-5090. REPAIRED IAW FOKKER SRM 53-01-01 AND HORIZON AIR EA 4-53-154 6. 2 L 7 2 4F RT A20EU 2002012500075 20020125 00075 EU 2002 1 25 QXEA0102120 1 20011213 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - ANGLE BRACKET AT CRACKED AT STATION 1700 ON AIRCRAFT STRUCTURE JUST UNDER INBOARD FLAP FAIRING DOOR. REPAIRED IAW FOKKER SRM 53-02-01 FIGURE 6. 2 L 7 2 4F RT A20EU 2002012500076 20020125 00076 EU 2002 1 25 QXEA0102121 1 20011212 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CORROSION ON FORWARD CLIP FOR DATO PANEL ON LT AFT OVERWING EXIT LOWER APERTURE. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 6, PARAGRAPH 4B AND SRM 51-31-05. 2 L 7 2 4F RT A20EU 2002012500077 20020125 00077 EU 2002 1 25 QXEA0102122 1 20011212 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CORROSION ON AFT CLIP FOR DATO PANEL ON LT FORWARD OVERWING EXIT LOWER APERTURE. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 6, PARAGRAPH 4B AND SRM 51-31-05. 2 L 7 2 4F RT A20EU 2002012500079 20020125 00079 EU 2002 1 25 QXEA0102123 1 20011213 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CORROSION AT NUT PLATES BELOW CROSS TIE AT FRAME 9305 AND STRINGER 74. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5, SRM 51-32-02 AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 2002012500080 20020125 00080 EU 2002 1 25 QXEA0102124 1 20011213 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CORROSION ON STRINGER 73 BELOW FRAME 9305B. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5 AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 2002012500081 20020125 00081 EU 2002 1 25 QXEA0102125 1 20011212 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CORROSION ON FRAME BELOW NUT PLATES, FRAME 9305B AND STRINGER 74. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5 AND SR M 51-10-4. 2 L 7 2 4F RT A20EU 2002012500082 20020125 00082 EU 2002 1 25 QXEA0102126 1 20011214 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - ACCESS DOOR 21A OPENING STRUCTURE HAS DENTS AND SCRATCHES AT SLOTTED GUIDE PIN HOLE, STATION 1890 AND STRINGER 73. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5 AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 2002012500083 20020125 00083 EU 2002 1 25 QXEA0102127 1 20011218 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - LOWER FORWARD VHF ANTENNA MOUNT AREA ON FUSELAGE SKIN CORRODED. REPAIRED IAW HORIZON AIR EA 4-53-1539 AND FOKKER SRM 53-10-4. 2 L 7 2 4F RT A20EU 2002012500084 20020125 00084 EU 2002 1 25 QXEA0102144 1 20011213 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - RT WING FUEL PANEL 74F APERTURE HAS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 57-14-01, PAGE 16, FIGURE 03. 2 L 7 2 4F RT A20EU 2002012500085 20020125 00085 EU 2002 1 25 QXEA0102145 1 20011213 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - RT FUEL PANEL 74E APERTURE HAS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 57-14-01, PAGE 16. 2 L 7 2 4F RT A20EU 2002012500086 20020125 00086 EU 2002 1 25 QXEA0102147 1 20011213 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - RT OUTBOARD SEAT TRACK HAS FRETTING CORROSION BETWEEN STATION 4950 AND 4980. REPAIRED IAW HORIZON AIR EA 4-53-154 1 AND FOKKER SRM 53-01-01. 2 L 7 2 4F RT A20EU 2002012500094 20020125 00094 EU 2002 1 25 QXEA0102148 1 20011219 A 5753 BRACKET FOKKER F28 F28MK4000 4990810 EU T/E FLAP CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - INBOARD FLAP SHROUD DOOR ROLLER BRACKET ON OUTBOARD FLAP IS CRACKED IN RADIUS JUST BELOW MOUNT BOLTS. REPAIRED IA W FOKKER MM 27-50-6, PAGE 501-502, PARAGRAPH 3A. 2 L 7 2 4F RT A20EU 2002012500096 20020125 00096 EU 2002 1 25 QXEA0102149 1 20011219 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CORROSION ON SEAT RAIL UPPER SURFACE ABOVE FRAME 4610, BL1127 RT. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 206, FIG URE 205, SRM 53-02-15 AND SRM 53-31-01. 2 L 7 2 4F RT A20EU 2002012500097 20020125 00097 CE 2002 1 25 2002F00035 1 20011216 A 2510 0151500138 FRAME CESSNA 206 206CESSNA 2073302 CE CONT O520 IO520F 17032 SO HARTZL HCC3Y PHCC3YF1 GL PILOT SEAT CRACKED W O OTHER O OTHER NR NOT REPORTED 1 SW 99 CFJAY 3405 70 01992 293375R EE3022A PILOT'S SEAT BOTTOM FRAME, LF ATTACHING LEG CRACKED. 1 H 7 1 3O 3 O A4CE E5CE 5 C P25EA 2002012500098 20020125 00098 EU 2002 1 25 QXEA0102150 1 20011223 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CORROSION UNDER NUT PLATE ON FRAME 14755, 5 INCHES LEFT OF CENTERLINE. REPAIRED IAW HORIZON AIR EA 4-53-1536 AND FOKKER SRM 53-02-12. 2 L 7 2 4F RT A20EU 2002012500099 20020125 00099 EU 2002 1 25 QXEA0102151 1 20011223 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CORROSION UNDER FOUR NUT PLATES IN FRAME 14755 FROM CENTERLINE OUT TO 4 INCHES RIGHT OF CENTERLINE. REPAIRED IAW HORIZON AIR EA 4-53-1536, FOKKER SRM 51-31-01 AND SRM 51-31-05. 2 L 7 2 4F RT A20EU 2002012500101 20020125 00101 EU 2002 1 25 QXEA0102152 1 20011217 A 5320 STRUCTURE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CRACK AT AFT SIDE OF NOSE WHEEL, 1 INCH FORWARD OF FRAME 4175 AND 2 INCHES ABOVE STRINGER 1. REPAIRED IAW HORIZON AIR EA 4-53-1544. 2 L 7 2 4F RT A20EU 2002012500146 20020125 00146 NM 2002 1 25 AWXA200200074 1 20010108 A 5330 6545775 SKIN BOEING 737 737317 138447P NM CANNING A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 YVR - MAJOR REPAIR - "C" - DURING C-13 CHECK MAINTENANCE FOUND AN AREA OF SKIN WRINKLES WITH ASSOCIATED OIL CANNING ON T HE R/H SIDE OF USELAGE FROM BS 727D TO 767, STR 18R TO STR 20R. ALL DENTS WERE FOUND TO BE WITHIN LIMITS PER B737-300 SR M 53-00-01, FIG 101. PERMANENT REPAIR WAS THEN CARRIED OUT IAW B737-300 SRM 53-00-01, FIG. 210, PG. 227 FOR EXTERNAL REP AIR FOR DAMAGE AT SKIN LAP JOINT. DAMAGED SKIN WAS CUTOUT BS 727D TO BS 767, STR 18R TO STR 20R AND NEW SKIN WAS FABRICA TED AND INSTALLED PER SRM 53-00-01, FIG. 210, PG. 227. 2 L 7 2 4F RT A16WE 2002012500148 20020125 00148 EU 2002 1 25 QXEA0102153 1 20011211 A 5530 RIVET FOKKER F28 F28MK4000 4990810 EU VERTICAL STAB LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - VERTICAL STABILIZER RT CONNECTION ANGLE HAS SIX SMOKING/LOOSE RIVETS AT RIB 6.0 AND 7.0. REPAIRED IAW FOKKER SRM 51-31-02. 2 L 7 2 4F RT A20EU 2002012500149 20020125 00149 EU 2002 1 25 QXEA0102154 1 20011211 A 5530 RIVET FOKKER F28 F28MK4000 4990810 EU VERTICAL STAB LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - LT SIDE OF VERTICAL STABILIZER CONNECTION ANGLE HAS SIX LOOSE/SMOKING RIVETS LOCATED AT RIBS 6.0 AND 7.0. REPAIRE D IAW FOKKER SRM 51-30-02. 2 L 7 2 4F RT A20EU 2002012500150 20020125 00150 EU 2002 1 25 QXEA0102155 1 20011211 A 5532 SKIN FOKKER F28 F28MK4000 4990810 EU VERTICAL STAB CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - TOP LT SIDE OF VERTICAL STABILIZER AT LOWER FORWARD CORNER OF PANEL 55 OPENING HAS THREE CHAFE AREAS TO STAB SKIN. REPAIRED IAW FOKKER SRM 53-01-01 AND SRM 51-10-01. 2 L 7 2 4F RT A20EU 2002012500151 20020125 00151 EU 2002 1 25 QXEA0102156 1 20011219 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - REAR PRESSURE BULKHEAD FORWARD SIDE FRAME 17065 HAS A .25 INCH CIRCULAR CHAFE INBOARD OF SKIN SPLICE AT BL LH425. REPAIRED IAW HORIZON AIR EA 4-53-154. 2 L 7 2 4F RT A20EU 2002012500152 20020125 00152 WP 2002 1 25 GTIA012126 1 20011127 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND FLOOR SUPPORT CRACKED AT STATION Y=238 INCHES. REMOVED DAMAGED FLOOR SUPPORT. FABRICATED LOCATED AND DRILL ED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002012500153 20020125 00153 WP 2002 1 25 GTIA012127 1 20011129 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND FLOOR SUPPORT CORRODED AT STA Y = 160 FROM -X=1 TO -X=21. REMOVED DAMAGED FLOOR SUPPORT. FABRICATED NEW FL OOR SUPPORT. INSTALLED NEW FLOOR SUPPORT IAW DC9 SRM 51-30-1. (M) 2 L 7 2 4F A6WE 2002012500154 20020125 00154 WP 2002 1 25 GTIA012128 1 20011115 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND RIGHT OUTBOARD FLOORBOARD NR 2 HAS ELONGATED HOLES, SURFACE CORROSION AROUND FASTENER HOLES, TORN SKIN. REM OVED DAMAGE AREAS AND FABRICATED REPAIR PARTS. INSTALLED DOUBLER FILLER IAW DC9 SRM 53-05. (M) 2 L 7 2 4F A6WE 2002012500155 20020125 00155 WP 2002 1 25 GTIA012133 1 20011123 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND FORWARD ENTRY AREA FLOOR SUPPORT CORRODED AT STATION Y200 FROM X= 1 INCH TO X= 20 INCHES. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002012500156 20020125 00156 WP 2002 1 25 GTIA012134 1 20011116 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND LEFT INBOARD FLOORBOARD NR 2 COUNTERSINKS PULLED THROUGH, SURFACE CORROSION AND BARE METAL. CRACK WAS FOUND ON END. FABRICATED REPAIR DOUBLER. INSTALLED DOUBLER IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002012500157 20020125 00157 WP 2002 1 25 GTIA012135 1 20011107 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND RIGHT INBOARD FLOORBOARD NR 3 FROM STA Y314 TO STA Y329 HAS BROKEN EDGE (FWD ONE) AND STIFFENERS CRACKED. F ORMED DOUBLER FOR RIGHT INBOARD FLOORBOARD. STOP DRILLED CRACKS, ROUNDED OUT CRACK IN STIFFENER. INSTALLED FORMED DOUB LER IAW DC9 IAW SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002012500158 20020125 00158 WP 2002 1 25 GTIA012136 1 20011107 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND RIGHT OUTBOARD FLOORBOARD NR 2 FROM STATION 237 TO STATION 313 HAS CORROSION, ELONGATED HOLES AND EDGES BROK EN OFF. FABRICATED REPAIR DOUBLER FOR ELONGATED HOLES. FABRICATED REPAIR DOUBLER FOR BROKEN EDGES. INSTALLED REPAIR D OUBLER FOR ELONGATED HOLES. INSTALLED REPAIR DOUBLER FOR BROKEN EDGES IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002012500159 20020125 00159 WP 2002 1 25 GTIA012138 1 20011107 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND RIGHT INBOARD FLOORBOARD NR 10 FROM STATION 639 TO 680 HAS EDGES BROKEN OFF. FABRICATED REPAIR DOUBLER. IN STALLED REPAIR DOUBLER IAW DC9 SRM 53-05. (M) 2 L 7 2 4F A6WE 2002012500160 20020125 00160 WP 2002 1 25 GTIA012139 1 20011115 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CABIN FLOORBOARD STATION 940 TO 965, CRACKS ON PANEL EDGES SURFACE CORROSION AND BARE METAL AREAS ON SKIN, L OWER SIDE INSULATION TORN. REPAIRED CRACKS ON FLOOR PANEL PER DC9 SRM 53-05. (M) 2 L 7 2 4F A6WE 2002012500161 20020125 00161 WP 2002 1 25 GTIA012141 1 20011115 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CABIN FLOORBOARD RIGHT, OUTBOARD STATION 680 TO 756, MOUNT HOLES CRACKED IN SEVERAL AREAS, SEVERE CORROSION ON SKIN. FORM DOUBLERS. INSTALLED IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002012500162 20020125 00162 WP 2002 1 25 GTIA012146 1 20011123 A 5320 STRAP DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND FORWARD CARGO DOOR JAMB AFT STATION 427-438 WEB STRAPS HAVE TOOLING MARKS AND SURFACE CORROSION. FORMED STR AP. LOCATED AND DRILLED STRAP IAW DC9 SRM 51-10-4. (M) 2 L 7 2 4F A6WE 2002012500163 20020125 00163 WP 2002 1 25 GTIA012147 1 20011115 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CABIN FLOOR PANEL FS 699-756 LEFT LOWER COMPOSITE CHAFED STRIPS DISBONDED, BROKEN AND MISSING, UPPER SURFACE CORROSION CORNER MATERIAL BROKEN OFF AND IMPROPERLY INSTALLED BLIND RIVETS. FORMED NEW FLOOR PANEL PER DC9 SRM 53-24-0 . (M) 2 L 7 2 4F A6WE 2002012500164 20020125 00164 WP 2002 1 25 GTIA012148 1 20011129 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND FLOOR SUPPORT CORRODED AT STA Y=200 FROM -X47 INCHES TO -X=56 INCHES. REMOVED SUPPORT ANGLE. FORMED NEW FL OOR SUPPORT ANGLE IAW DC9 SRM 53-11-1. INSTALLED NEW SUPPORT ANGLE IAW DC9 SRM 53-11-1 OR 51-30-8. (M) 2 L 7 2 4F A6WE 2002012500165 20020125 00165 WP 2002 1 25 GTIA012149 1 20011108 A 7110 SKIN DOUG DC9 DC932 3022066 WP RT COWLING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND RIGHT ENGINE NOSE COWL, CRACK IN INNER LIP SKIN AT 6:00 POSITION. REMOVED DAMAGE. FABRICATED REPAIR DOUBLE R AND FILLER. INSTALLED REPAIR PARTS PER DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002012500166 20020125 00166 WP 2002 1 25 GTIA012150 1 20011115 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CABIN FLOORBOARD LEFT, INBOARD STATION 313 TO 389 TWO CRACKS AT FORWARD END EDGES, SEVERE CORROSION AROUND F ASTENER HOLES, BARE METAL AREAS ON SKIN. FABRICATED THREE DOUBLERS FOR CRACKS AT FORWARD END. INSTALLED THREE DOUBLERS . ALL AREAS BUT ONE WITHIN LIMITS. FABRICATED REPAIR DOUBLERS TWO FOR AREA OUT OF LIMITS. INSTALLED TWO DOUBLERS IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002012500167 20020125 00167 WP 2002 1 25 GTIA012151 1 20011116 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND FLOORBOARD STATION 889 TO 965 HAS COUNTERSINKS BROKEN OUT,HOLE IN STIFFENER ON BACK, SURFACE CORROSION. REM OVED STIFFENER FROM FLOORBOARD. FORMED NEW PART. INSTALLED STIFFENER. DOUBLER MADE FOR BROKEN CSKS. INSTALLED DOUBLE R IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002012500168 20020125 00168 WP 2002 1 25 GTIA012152 1 20011108 A 3350 HOUSING DOUG DC9 DC932 3022066 WP CABIN CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND MAIN CABIN OVERHEAD CEILING PANEL BETWEEN ROWS, AFT 15 L/R INNER LIGHT HOUSING CRACKED. REMOVED EMERGENCY L IGHT ASSY. INSTALLED EMERGENCY LIGHT ASSY IAW MD9 33-53-00. (M) 2 L 7 2 4F A6WE 2002012500169 20020125 00169 WP 2002 1 25 GTIA012153 1 20011108 A 3350 LIGHT DOUG DC9 DC932 3022066 WP CABIN MISSING A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND MAIN CABIN, OVERHEAD CEILING PANEL BETWEEN ROWS 13L AND RIGHT LIGHT ASSY MISSING. REMOVED EMERGENCY LIGHT A SSY. REPAIRED WIRING. INSTALLED EMERGENCY LIGHT ASSY IAW MD9 MM 33-53-0. (M) 2 L 7 2 4F A6WE 2002012500170 20020125 00170 WP 2002 1 25 GTIA012154 1 20011119 A 5311 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND FRAME CORRODED/CRACKED AT BRACKET ATTACH SUPPORT, LONGERON 18L. REMOVED BRACKET CRACKED. LOCATE AND DRILL. INSTALLED NEW FITTING IAW DC9 SRM 51-30-1. (M) 2 L 7 2 4F A6WE 2002012500171 20020125 00171 WP 2002 1 25 GTIA012155 1 20011110 A 5310 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FORWARD CARGO COMPARTMENT LOWER DOOR JAMB AREA CORRODED BETWEEN STA Y 330 AND STA Y 427. LOWER DOOR JAMB PAN OUT OF LIMITS. FABRICATED PAN PER DC9 SRM 53-05. INSTALLED DOOR JAMB DOOR PAN FORWARD AND PAN DOUBLERS AND WEB IAW SRM DC9 . (M) 2 L 7 2 4F A6WE 2002012500172 20020125 00172 WP 2002 1 25 GTIA012156 1 20011215 A 7110 WEB DOUG DC9 DC932 3022066 WP RT NOSE COWL CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - RIGHT NOSE COWL INBOARD AREA AT 6 O'CLOCK POSITION DOUBLER CRACKED. REMOVED CRACKED DOUBLER. AFTER FURTHER EVALU ATION FOUND WEB ALSO CRACKED. CUT DAMAGED AREA (ON WEB). FABRICATED DRILLED AND LOCATED REPAIR PARTS FILLED DOUBLER. INSTALLED REPAIR PARTS PE SRM DC9 51-30-2. (M) 2 L 7 2 4F A6WE 2002012500173 20020125 00173 WP 2002 1 25 GTIA012157 1 20011211 A 7110 STRUCTURE DOUG DC9 DC982 3022082 WP RT NOSE COWL DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - NR 2 ENGINE NOSE COWL INLET REPAIR NOT IAW SRM (4 O'CLOCK). REMOVED OLD FILLERS AND DOUBLERS REPAIR. FORMED DOUB LERS. INSTALLED DOUBLERS IAW MD80 SRM 51-30-8. (M) 2 L 7 2 4F A6WE 2002012500174 20020125 00174 WP 2002 1 25 GTIA012159 1 20011223 A 2760 SPOILER DOUG DC9 DC982 3022082 WP WING MALFUNCTIONED A GTIA O OTHER F FLT CONT AFFECTED LD LANDING 1 GL 23 823NK 48020 FLL - FLT 765 - ON TOUCHDOWN, SPOILER HANDLE MOVED AFT THEN FORWARD WAS UNABLE TO MANUALLY EXTEND SPOILERS THEREAFTER W/ O HOLDING THE HANDLE BACK. PERFORMED SYSTEM CHECK OUT IAW MD80 MM 27-60-00. RESET SYSTEM, CHECK OK. AUTOSPOILER DO NO T USE LIGHT OUT. (M) 2 L 7 2 4F A6WE 2002012500175 20020125 00175 WP 2002 1 25 GTIA012160 1 20011114 A 5320 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND WEB CRACKED AT STATION Y=954. REMOVED MEMBRANE/WEB FROM STATION 897 TO 964. INSTALLED NEW MEMBRANE/WEB IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002012500177 20020125 00177 EU 2002 1 25 NSVA0202 1 20011210 A 2435 23080031 STARTER GEN SAAB SF340 340B 7860101 EU LT ENGINE OVERHEATED A NSVA E ENGINE SHUTDOWN J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 27 299CJ 340B299 PIT - DURING ENGINE START UP, NR 1 ENGINE IGNITION LIGHT ILLUMINATED, LEFT GENERATOR OVER TEMP HEAD LIGHT ILLUMINATED. SMOKE FROM TOP OF COWLING OF LEFT ENGINE WAS VISIBLE. ENGINE WAS SHUTDOWN. MAINTENANCE INSPECTED AREA, NO DAMAGE NOTED OTHER THAN STARTER GENERATOR. SUSPECT THAT GENERATOR BURNED UP INTERNALLY. (M) 2 L 7 2 4T RT A52EU 2002012500178 20020125 00178 NE 2002 1 25 SIMA200116104 2 20010610 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LEFT OVERTEMP A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 177AE 340B177 DFW - FLT 3714 - LEFT ENGINE ITT REACHED 929C AT 96 PERCENT TORQUE ON TAKEOFF. ABORTED TAKEOFF. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 2002012500179 20020125 00179 NE 2002 1 25 SIMA200117810 2 20010627 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT FAILED A SIMA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 307AE 340B307 ALB - FLT 4893 - CLIMBING THROUGH 10000 FT EXPERIENCED CATASTROPHIC FAILURE OF RIGHT ENGINE. PERFORMED SHUTDOWN, DECLAR ED EMERGENCY AND RETURNED TO BASE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 2002012500180 20020125 00180 EU 2002 1 25 SIMA200122702 1 20010815 A 2120 SMOKE SAAB SF340 340B 7860101 EU COCKPIT DETECTED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 903AE 340B282 BOS - FLT 4893 - CREW REPORTED SMOKE IN COCKPIT DURING CRUISE FLIGHT. (M) 2 L 7 2 4T RT A52EU 2002012500181 20020125 00181 NM 2002 1 25 USAA011339 1 20011024 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AU 22201 CLT - FOUND SKIN CORRODED 10 INCHES, BUTT LINE STATION 1613 AND LBL 0. INSTALLED REPAIR DOUBLER PER EA 85563. (M) 2 L 7 2 4F RT A2NM 2002012500182 20020125 00182 NM 2002 1 25 USAA011340 1 20011028 A 5313 STRINGER BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AU 53716 22201 CLT - FOUND STRINGER CORRODED, STATION 1408-1420, STRINGER 29R. INSTALLED SHIMS, AND SPLICED STRINGER PER EA 85571. (M ) 2 L 7 2 4F RT A2NM 2002012500183 20020125 00183 NM 2002 1 25 USAA011341 1 20011023 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 55127 22199 CLT - FOUND FLOORBEAM CORRODED 6 INCHES, STATION 1300 FLOORBEAM, LBL 12 AND 18. INSTALLED NEW T-CAP PER TR 53-15-01. ( M) 2 L 7 2 4F RT A2NM 2002012500184 20020125 00184 NM 2002 1 25 USAA011342 1 20011027 A 5310 DOOR FRAME BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AU 53716 22201 CLT - FOUND DOOR FRAME CRACKED 4.75 INCH BY 4.75 INCH, R-4 FUSELAGE CUT OUT FORWARD FRAME LOWER SIDE. STOPPED DRILLED C RACK, INSTALLED DOUBLER PER EA 85569. (M) 2 L 7 2 4F RT A2NM 2002012500185 20020125 00185 NM 2002 1 25 USAA011343 1 20011027 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AU 53716 22201 CLT - FOUND SKIN DENTED 8.5 INCH BY 6.25 INCH, STATION 1700, S18 LT. CUT OUT DAMAGE, FABRICATED REPAIR DOUBLER INSTALLE D HI-LOCKS PER EA 85550. (M) 2 L 7 2 4F RT A2NM 2002012500186 20020125 00186 NM 2002 1 25 USAA011344 1 20011005 A 5320 CHANNEL BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AU 53716 22201 CLT - FOUND FRAME CHANNEL CRACKED 4 INCHES, STATION 1080 APPROXIMATELY FORWARD OUTBOARD SIDE OF MLG WHEEL WELL. FABRICA TED AND INSTALLED NEW FRAME CHANNEL. (M) 2 L 7 2 4F RT A2NM 2002012500187 20020125 00187 NM 2002 1 25 USAA011345 1 20011012 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AU 53716 22201 CLT - FOUND BEAM CORRODED 1 INCH BY 1 INCH, STATION 345 RBL 14. CUTOUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-15-01 TY PICAL REPAIR. (M) 2 L 7 2 4F RT A2NM 2002012500188 20020125 00188 NM 2002 1 25 USAA011346 1 20011010 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AU 53716 22201 CLT - FOUND SKIN WITH EXISTING DOUBLER 5 INCHES BY 4 INCHES, STATION 1750 BETWEEN S13R AND S12R. FLUSH SKIN REPAIR. (M ) 2 L 7 2 4F RT A2NM 2002012500189 20020125 00189 NM 2002 1 25 USAA011347 1 20011024 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 25049 22199 CLT - FOUND SKIN DENTED 3.4 INCHES BY 3 INCHES, STATION 150 AND S24R AFT CARGO DOOR. INSTALLED EXTERNAL DOUBLER PER SRM 53-00-01. (M) 2 L 7 2 4F RT A2NM 2002012500190 20020125 00190 NM 2002 1 25 USAA011349 1 20011009 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AU 53716 22201 CLT - FOUND SKIN WITH FLUSH PATCH REPAIR 1.75 INCH BY 1.75 INCH, STATION 1750 S12L AND S10L. (M) 2 L 7 2 4F RT A2NM 2002012500191 20020125 00191 NM 2002 1 25 USAA011352 1 20011009 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AU 53716 22201 CLT - FOUND SKIN WITH PREVIOUSLY INSTALLED REPAIR, 9 INCHES AND 12 INCHES, STATION 1690 TO STATION 1700 S19R PLUS S20R. INSTALLED DOUBLER. (M) 2 L 7 2 4F RT A2NM 2002012500192 20020125 00192 NM 2002 1 25 USAA011353 1 20011004 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE BULGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AU 53716 22201 CLT - FOUND SKIN WITH EXTERNAL BULGE, RIGHT SIDE STATION 1500 STRINGER 24R AND STRINGER 25R. CUT OUT DAMAGE, INSTALLED DOUBLER, PER SRM 53-00-01 FIG 205. (M) 2 L 7 2 4F RT A2NM 2002012500193 20020125 00193 NM 2002 1 25 USAA011354 1 20011009 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AU 53716 22201 CLT - FOUND SKIN DENTED 1.5 INCH BY 3 INCHES, STATION 1755 BETWEEN S12L AND S10L. INSTALLED FLUSH SKIN REPAIR 53-00-01 FIG 206. (M) 2 L 7 2 4F RT A2NM 2002012500194 20020125 00194 NM 2002 1 25 USAA011355 1 20011009 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AU 53716 22201 CLT - FOUND SKIN DOUBLER 1.75 INCH BY 1.75 INCH, STATION 1758 BETWEEN S13R AND S12R. INSTALLED FLUSH PATCH PER SRM 53-0 0-01 FIG 206. (M) 2 L 7 2 4F RT A2NM 2002012500195 20020125 00195 NM 2002 1 25 USAA011356 1 20011123 A 5310 DOOR FRAME BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AU 53716 22201 CLT - FOUND FRAME CRACKED 1 INCH, STATION 1350 L3 DOOR FRAME AT UPPER AFT STOP FITTINGS. INSTALLED DOUBLER AND FILLER P ER EA 85594. (M) 2 L 7 2 4F RT A2NM 2002012500196 20020125 00196 NM 2002 1 25 USAA011357 1 20011024 A 5754 SKIN BOEING 757 757225 1384959 NM L/E SLAT DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AU 53716 22201 CLT - FOUND SLAT DENTED 2.5 INCHES BY 1.5 INCHES, NR 7 SLAT, 6 INCHES OUTBOARD OF INBOARD EDGE UPPER TRAILING EDGE SURFA CE. INSTALLED REPAIR DOUBLER 51-70-10. (M) 2 L 7 2 4F RT A2NM 2002012500197 20020125 00197 NM 2002 1 25 USAA011358 1 20011031 A 5320 ANGLE BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AU 22201 CLT - FOUND CHORD ANGLE CORRODED 1 INCH BY 30 INCH, UNDER L3 DOOR AT STATION 1320-1360. INSTALLED DOUBLER AND SPLICE PE R SRM 51-70-11 AND EA 85570. (M) 2 L 7 2 4F RT A2NM 2002012700001 20020127 00001 NM 2002 1 27 S01232034 1 20011020 A 3200 65B4750869 LANDING GEAR BOEING 747 747209B NM PWA JT9 JT9D7Q 52054 NE ALT W SAJF O OTHER O OTHER IN INSP/MAINT 1 WP 03 22446 B18753 AFT ALL LDG RETRACTED & DOORS CLOSED, FWD INST PNL GEAR & DOOR OPEN RED LITE KEPT ILLUM WITH GEAR LEVER IN UP OR OFF POS. ALL DOORS WERE CONFIRMED CLOSED.C/A:1.BOTH PRI & ALT LDG LOG CONT MODULES, NLG LOCK SNSR S397, & PROX SNSR S396 WERE RPLC, THUS FIXED THE GEAR SQK, BUT DOOR OPEN XFR TO D/D, AND THE WIRING BETWEEN SNSR & LOGIC CONT MODULES IS CONFI RMED NORMAL. 2.THE D/D WAS CLEARED AFT THE CONT MODULE RPLC. SINCE THE F/E INDICATION WAS ALWAYS NORMAL. HENCE, THE MODU LE IS DETERMINED AS THE ROOT CAUSE OF THE SQK. 3.THE ROMAIC & MHS DATA SHOW THAT THE CONT MODULE HAS HIGH TSO AROUND 270 00 FH MINIMUM, AND LOW REMOVAL REATE OF 9 UNITS REMOVED DURING 11 YEARS, ADDITIONALLY, NO OTHER SQK OF THIS KIND IS RE 2 L 7 4 4F 4 F RT A20WE E3NE 2002012800043 20020128 00043 EU 2002 1 28 QXEA0102115 1 20011212 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - FUSELAGE FRAME 16660 TIE-IN CLIP TO SKIN IS CRACKED THROUGH RIVET HOLE AT STRINGER 29. REPAIRED IAW FOKKER SRM 53 -02-13, PAGE 4, FIGURE 2 AND SRM 51/31/01. 2 L 7 2 4F RT A20EU 2002012800045 20020128 00045 EU 2002 1 28 QXEA0102157 1 20011220 A 5320 BEAM FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - REAR PRESSURE BULKHEAD FORWARD SIDE FRAME 17065, BEAM 3 HAS TWO CRACKS IN RADIUS AT RT MOST OUTBOARD EDGE ON TOP S IDE. REPAIRED IAW FOKKER SRM 53-02-18, PAGE 38, FIGURE 13. 2 L 7 2 4F RT A20EU 2002012800047 20020128 00047 EU 2002 1 28 QXEA0102158 1 20011220 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - REAR PRESSURE BULKHEAD FORWARD SIDE FRAME 17065 RT SIDE ANGLE TO FUSELAGE SKIN HAS CRACK IN RADIUS FROM STRINGER 5 4 TO 55. REPAIRED IAW HORIZON AIR EA 4-53-1150 AND FOKKER SRM 53-02-18. 2 L 7 2 4F RT A20EU 2002012800048 20020128 00048 EU 2002 1 28 QXEA0102159 1 20011218 A 5320 CHANNEL FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - LAVATORY AFT WALL VERTICAL SUPPORT CHANNEL THAT IS RIVETED TO REAR PRESSURE BULKHEAD FRAME 17065 IS CRACKED AROUND TWO RIVETS. REPAIRED IAW FOKKER SRM 53-01-00, PAGE 3, PARAGRAPH 3C AND SRM 51-31-01, PAGES 1 THRU 17. 2 L 7 2 4F RT A20EU 2002012800052 20020128 00052 EU 2002 1 28 QXEA0102160 1 20011220 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CRACK IN SKIN OF RT STUBWING LOWER AFT PANEL. REPAIRED IAW FOKKER SRM 54-02-03, PAGE 4, FIGURE 2 AND SRM 51-31-05 , PAGE 8, PARAGRAPH 7. 2 L 7 2 4F RT A20EU 2002012800053 20020128 00053 EU 2002 1 28 QXEA0102161 1 20011217 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CORROSION AT LOWER FORWARD VHF ANTENNA MOUNT AREA ON FUSELAGE SKIN. REPAIRED IAW HORIZON AIR EA 4-53-1539 AND FOK KER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002012800056 20020128 00056 EU 2002 1 28 QXEA0102162 1 20011221 A 5710 STRUCTURE FOKKER F28 F28MK4000 4990810 EU LT WING LEAKING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - FUEL LEAK ON LT WING LOWER SKIN AT STATION 2635 AND STRINGER 2.9 JUST AFT AND OUTBOARD OF FUEL PANEL 71A. REPAIRE D IAW FOKKER MM 28-11-06, PAGE 403. 2 L 7 2 4F RT A20EU 2002012800057 20020128 00057 EU 2002 1 28 QXEA0102164 1 20011226 A 5230 DOOR FOKKER F28 F28MK4000 4990810 EU CARGO DOOR OUT OF RIG A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CENTER CARGO DOOR LEADING EDGE NOT FLUSH WITH AIRCRAFT SKIN WHEN AIRCRAFT IS PRESSURIZED. REPAIRED IAW HORIZON AI R EA 4-52-464. 2 L 7 2 4F RT A20EU 2002012800058 20020128 00058 EU 2002 1 28 QXEA0102165 1 20011227 A 3350 LIGHT FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 488US 11240 PDX - PASSENGER EXIT LIGHT INOP AT NR 2 GALLEY CURTAIN, WHEN USING COCKPIT ARMING ON SWITCH. REPLACED EXIT LIGHT PANEL WITH SERVICEABLE UNIT. 2 L 7 2 4F RT A20EU 2002012800059 20020128 00059 EU 2002 1 28 QXEA0102166 1 20011210 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - RT WING FUEL PANEL 74A APERTURE HAS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 57-01-01 AND MM 57-12-01, FIGURE 1, PAGE 9. 2 L 7 2 4F RT A20EU 2002012800060 20020128 00060 EU 2002 1 28 QXEA0102167 1 20011212 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - RT WING FUEL PANEL 74B APERTURE HAS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 57-13-01 AND 57-01-01, PAGE 5. 2 L 7 2 4F RT A20EU 2002012800061 20020128 00061 EU 2002 1 28 QXEA0102168 1 20011213 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - RT WING FUEL PANEL 74G APERTURE HAS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 57-01-01, PARAGRAPH 4B AND SRM 57 -14-01, PAGE 16. 2 L 7 2 4F RT A20EU 2002012800063 20020128 00063 EU 2002 1 28 A1U2002F00001 1 20011214 A 2824 1176415103 PUMP BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE FUEL TRANSFER FAILED A A1UA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 211SL 7201 45724 AFTER TAKEOFF, AFT FUEL TRANSFER PUMP LIGHT ILLUMINATED. CIRCUIT BREAKER WAS PULLED AND RESET. SWITCH WAS CYCLED. PRO BABLE CAUSE, BEARINGS SEIZED. 1 G 7 2 3U 3 U H13EU E5NE10 2002012800077 20020128 00077 2002 1 28 BLI2001F00008 4 20011125 A 8300 310428801 PUMP CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE ACCESSORY G/B INOPERATIVE E BLIA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 17 505RP 5500450 ABORTED START; NO OIL PRESSURE OR TURBINE SPEED INDICATION. REMOVED ACCESSORY GEARBOX AND SENT TO MFG. THE ABOVE ENGIN E EXPERIENCED PROBLEMS IN THE FIELD THAT RESULTED IN THE ACCESSORY GEARBOX ASSEMBLY AND THE OIL PUMP TO BE SENT TO MFG F OR REPAIRS. 1 L 7 2 4F 4 F A22CE E1NE 2002012800080 20020128 00080 CE 2002 1 28 BLIA512C11200 1 20011128 A 3230 99100023 MOTOR CESSNA 402 402B 207590P CE CONT O520 TSIO520* 17040 SO LG GEARBOX FAILED A BLIA O OTHER O OTHER NR NOT REPORTED 1 GL 17 371JD 7286 402B1322 LANDING GEAR MANUALLY EXTENDED TO LAND; LOCAL MAINTENANCE SWING GEAR; AIRCRAFT RETURNED IRS ON FERRY PERMIT. CHECKED WI RING AND SQUAT SW, CLEANED RELAY CONTACTS AND REPAIRED LANDING GEAR DRIVE MOTOR WITH TSO:0 OPS CHECKED GOOD. AIRCRAFT TEST FLOWN, RETURNED TO SERVICE. 1 L 7 2 3O 3 O A7CE E8CE 2002012800081 20020128 00081 NM 2002 1 28 QXEA0200018 1 20011231 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - LT INBOARD SEAT TRACK X593 THERE IS CORROSION UNDER A NUT PLATE. REPAIRED IAW DHC-8 SRM 51-20-36 AND SRM 51-40-11 . 2 H 7 2 4T RT A13NM 2002012800083 20020128 00083 NM 2002 1 28 QXEA0200020 1 20011231 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - LOWER FORWARD ATC ANTENNA AIRCRAFT SURFACE IS CORRODED. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 3 AND SRM 51-20-16. 2 H 7 2 4T RT A13NM 2002012800085 20020128 00085 2002 1 28 BLIA512C11250 4 20011125 A 8300 GEARBOX CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE ACCESSORY FAILED E BLIA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 17 505RP 3744 5500450 ABORTED START; NO OIL PRESSURE OR TURBINE SPEED INDICATION. REMOVED ACCESSORY GEARBOX AND SENT TO MFG. UPON RECEIPT, IT WAS EVIDENT THE THE SHAFT HAD SHEARED. THIS WAS APPARENTLY CAUSED BY AN ELEMENT IN THE OIL PUMP ASSEMBLY, INSTALLED NEW AT OVERHAUL, BEING OUTSIDE OF THE BLUEPRINT SPEC FROM MFG. UPON RECEIPT OF THE PARTS, THE ACCESSORY GEARBOX WAS TOR N DOWN, INSPECTED, AND REASSEMBLED. 1 L 7 2 4F 4 F A22CE E1NE 2002012800087 20020128 00087 SO 2002 1 28 BTH2002F00000 1 20011210 A 2432 TERMINAL PIPER PA32 PA32R300 7103213 SO BATTERY CORRODED E BTHA O OTHER O OTHER NR NOT REPORTED 1 AL 01 4352F 32R7680441 AIRPLANE LANDED, LEFT GEAR UNLOCKED AFTER ELECTRICAL POWER FAILURE ON APPROACH TO LAND. INSPECTION OF ELECTRICAL SYSTEM , FOUND BATTERY POST CORRODED ON POSITIVE TERMINAL. 1 L 7 1 3O A3SO 2002012800090 20020128 00090 CE 2002 1 28 CRJ2002F00000 1 20011201 A 3010 3D154902A2 SHUTTLE VALVE CESSNA 340 340A 2076405 CE CONT O520 TSIO520* 17040 SO DEICE BOOT FAILED B CRJR O OTHER O OTHER NR NOT REPORTED 1 CE 01 5421J 4384 340A0108 "INOP BTN" ON VAC GAGE WOULD NOT COME OUT WITH ONE ENG SHUT DOWN. REMOVED MAINFOLD, ONE CK VLV WOULD NOT SEAL. CLEANED VLV WITH ALCOHOL AND FUNC TESTED. REINSTALLED VLV AND FUNC TEST WAS OK. INOP BTN FAILED. REPLACED MANIFOLD PN 1H510 . FUNC TEST SHOWED VLVS WORKING OK. FOUND IF SHUT LT ENG DOWN FIRST, LT INOP BTN ON GAGE WOULD NOT COME OUT. TROUBLESH OT SYS, MANIFOLD WITH HOSES DISCON FROM VAC SYS AND DEICE BOOT SYS, FOUND LT DEICE SHTL VLV WOULD NOT CHK VAC COMING THR OUGH DEICE SYS ALLOWING RT SIDE TO KEEP LT BTN IN WHEN IT SHOULD HAVE BEEN OUT. RECONN SYS AND RAN JUST RT ENG. WHILE BOOT SYS WAS CYC, LT BTN WOULD STAY OUT. BOOTS WENT THROUGH COMPLETE CYC, BTN PULLED BACK IN. LT SHUT VLV REPLACED. 1 L 7 2 3O 3 O 3A25 E8CE 2002012800092 20020128 00092 NM 2002 1 28 QXEA0200026 1 20011230 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - LOWER TCAS ANTENNA HAS CORROSION AT MOUNT HOLES. REPAIRED IAW DHC-8 SRM 51-20-11, SRM 53-00-16 AND SRM 51-20-16. 2 H 7 2 4T RT A13NM 2002012800099 20020128 00099 SO 2002 1 28 CTU2002F00000 1 20011213 A 2140 23O04 REGULATOR PIPER PA34 PA34200T 7103406 SO CONT O360 LTSIO360EB 17025 SO HEATER LEAKING A CTUR K NONE K FLUID LOSS IN INSP/MAINT 1 GL 21 121WA 347970435 268254R HEATER FUEL REGULATOR INSPECTED IAW AD, FOUND TO BE LEAKING. 1 L 7 2 3O 3 O A7SO E9CE 2002012800100 20020128 00100 CE 2002 1 28 CTU2002F00001 1 20010107 A 3222 131378252CL LINK BEECH 90 C90 1152913 CE NLG MISSING A CTUR K NONE O OTHER IN INSP/MAINT 1 GL 21 REMOVED AND REPLACED THE NOSE LANDING GEAR RETRACT DUPLEX CHAIN IN THE NOSE. THE TECH INSTALLED THE CONNECTING LINK PN 13137825CL INSPECTOR FOLLOWED UP AND NOTICED THAT THE CONNECTING LINK WAS MISSING THE TWO CENTER PLATES. WHEN THE TECH WAS ASKED ABOUT THE CONNECTING LINK HE STATED THAT ALL RECEIVED PARTS WERE INSTALLED. 1 L 7 2 3T 3A20 2002012800101 20020128 00101 SO 2002 1 28 CTU2002F00002 1 20011213 A 2140 23O04 REGULATOR PIPER PA34 PA34200T 7103406 SO CONT O360 LTSIO360EB 17025 SO HEATER LEAKING A CTUR K NONE K FLUID LOSS IN INSP/MAINT 1 GL 21 121WA 347970435 268254 HEATER FUEL REGULATOR INSPECTED IAW AD FOUND TO BE LEAKING. 1 L 7 2 3O 3 O A7SO E9CE 2002012800103 20020128 00103 SW 2002 1 28 DO32002F00000 1 20011213 A 2910 790246167 LINE GULSTM 500 500S 0141107 SW LYC O540 IO540* 41532 EA RT MLG WW CHAFED E D03A K NONE O OTHER IN INSP/MAINT 1 EA 03 621TJ 2993 3308 HYDRAULIC PUMP PRESSURE LINE (PN790246-167) AND HYDRAULIC SUPPLY LINE (PN 790246-167). HYDRAULIC LINES ARE LOCATED FORW ARD OF EACH MAIN LANDING GEAR ASSEMBLY ON LOWER REAR F/W. LINES COME FROM ENGINE DRIVEN HYDRAULIC PUMP AND GO TO HYDRAU LIC PRESSURE REGULATOR. THERE IS NO SUPPORT FOR VIBRATIONS FOR THE FIRST 16 INCHES OF THESE LINES WHERE THEY EXIT F/W. LINES ARE PERMITTED TO CHAFE EACH OTHER. THESE LINE CHAFED AND PRESSURE LINE RUPTURED DEPLETING ALL PRESSURE AND HYDRA ULIC FLUID SUPPLY CAUSING LOSS OF USE OF NORMAL BRAKING, FLAPS, AND LANDING GEAR. NORMAL INSPECTION OF THESE LINES IS E XETREMELY HARD TO DO. SUGGEST USING 24 INCH EXTENSION TYPE FLASH LIGHT. 1 H 7 2 3O 3 O 6A1 1E4 2002012800105 20020128 00105 EA 2002 1 28 EEJ2002F00000 2 20011226 A 8520 LW105455 PISTON PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA RT ENGINE FAILED E EEJA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 78GH 1563 317852121 L247368A AIRCRAFT WAS IN CRUISE, WHEN PILOT NOTICE MANIFOLD GO DOWN AND OIL COMING OUT OF ENGINE. 1) ON INSPECTION NR 4 CYLINDER HAD NO COMPRESSION. 2) PISTON HAD BROKEN RINGS TOP TWO PISTON WAS MELTED DOWN SIDE FROM CYLINDER GASES WHERE THE HING W HERE BROKEN. 1 L 7 2 3O 3 O A20SO E14EA 2002012800109 20020128 00109 WP 2002 1 28 DHL2002805018 1 20011229 A 5312 4772397U1 FITTING DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 805DH 75397 46125 N/R 0132AFT PRESSURE BULKHEAD ... JOINT FITTING WITH L17R HAS A .250 CRACK @ STA. 1766 2 L 7 4 4F RT 4A25 2002012800142 20020128 00142 WP 2002 1 28 UPS01837359 1 20011211 A 3350 6012235 BATTERY PACK DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:IN EMERGENCY EXIT LIGHTS BATTERY LOW VOLTAGE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK IA W MM 33-50-01. OPS CHECKS GOOD. 2 L 7 4 4F RT 4A25 2002012800143 20020128 00143 WP 2002 1 28 UPS01837362 1 20011207 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:IN NO ILLUM OF EMERGENCY LIGHTS. REMOVED AND REPLACED BATTERY (EMERGENCY) PACK, OPS CHECK GOOD 33-50. 2 L 7 4 4F RT 4A25 2002012800144 20020128 00144 NE 2002 1 28 UPS01837364 2 20011214 A 7200 ENGINE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE NR 2 FLAMED OUT A IPXA O OTHER X ENGINE FLAMEOUT DE DESCENT 1 SO 01 809UP 46109 INSPECTION TYPE:N/A NR 2 ENG FLAMEOUT ON DESCENT ANTI-ICE 'ON' ING OVERRIDE FLT 15000 - 16000 FT. T/S PER 71-00-00 CFM MANUAL, COMPLIED WITH ALL STEPS FOR ENG FLAME-OUT PER MM 71-00-00 PG 101, 102 & 103. NO DEFECTS NOTED. 2 L 7 4 4F 4 F RT 4A25 E2GL 2002012800145 20020128 00145 WP 2002 1 28 UPS01837366 1 20011213 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:AS EMERGENCY LIGHTS ARE INOP IN TEST. REMOVED, REPLACED, AND TESTED EMERGENCY BATTERY PACK IAW MM 33-50 -01. 2 L 7 4 4F RT 4A25 2002012800146 20020128 00146 NE 2002 1 28 UPS01837369 2 20011218 A 7200 CFM56 ENGINE DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE NR 2 FLAMED OUT A IPXA K NONE X ENGINE FLAMEOUT CR CRUISE 1 SO 01 701UP 45938 692564 INSPECTION TYPE:N/A EXPERIENCED IN FLIGHT FLAME-OUT NR 2 ENG DURING CRUISE. FLAME-OUT OCCURRED APPROX 1 MINUTE AFTER NR 2 X-FEED LEVER PLACED DOWN/OPEN. ALL MAIN BOOST PUMPS ON 1, 3 AND 4 FILL VALVES OPEN. NR 2 TANK 1000 LBS HEAVIER THAN 1, 3 + 4. PERFORMED AIR START IAW CHECKLIST. RESTART NORMAL, RETURNED TO OPS NORMAL. T/S, CHECKED FUEL QTY SYS, AND BOOST PUMPS CKS OK. SUMPED NR 2 TANK. INSPECTED, REMOVED AND REPLACED FUEL FILTER CKS GOOD. INSPECTED CDP AND CIT TUB ES & LINES CKS GOOD. CHECKED MAG CHIP DETECTORS, OK. CHECKED MECH FUEL SHUTOFF LEVER, CHECKS OK. PERFORMED MAX PWR AS SUR RUN CKS GOOD PER MM. 2 L 7 4 4F 4 F RT 4A25 E2GL 2002012800147 20020128 00147 WP 2002 1 28 UPS01837372 1 20011218 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:PFLT EMERGENCY LIGHTS INOP. REPLACED EMERGENCY BATTERY PACK, OPS OK. 2 L 7 4 4F RT 4A25 2002012800148 20020128 00148 WP 2002 1 28 UPS01837373 1 20011219 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:PFLT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK ASSY, OPS CHECKED NORMAL. 2 L 7 4 4F RT 4A25 2002012900003 20020129 00003 CE 2002 1 29 EGQ2002F00000 1 20011109 A 3233 99810057651 ACTUATOR BEECH 100 B100 1152919 CE GARRTT TPE331 TPE331* 01514 WP RT MLG FAILED A EGQA K NONE O OTHER IN INSP/MAINT 1 EA 17 105VY 610 BE109 DURING A TRAINING FLIGHT, PILOTS RETRACTED THE LANDING GEAR. A BANG WAS HEARD. THE RIGHT GEAR STAYED DOWN AND LOCKED W HILE THE NOSE GEAR AND LEFT MAIN GEAR RETRACTED NORMALY. PILOTS EXTENDED THE NOSE AND LEFT MAIN GEAR USING THE EMERGENC Y SYSTEM. A NORMAL LANDING WAS ACCOMPLISHED. INSPECTION REVEALED THE RIGHT GEAR ACTUATOR HAS FAILED INTERNALLY. 1 L 7 2 4T 3 T A14CE E2WE 2002012900004 20020129 00004 CE 2002 1 29 EKI2001F00000 1 20011214 A 2435 EQ6642RE ADAPTER CESSNA 421 421B 2076014 CE CONT O520 TSIO520C 17040 SO STARTER FAILED B EKIR K NONE O OTHER IN INSP/MAINT 1 WP 07 637SC 654 421B0274 235212R STATOR ADAPTOR FAILED AND DAMAGED REAR OF CASE WHERE SHAFT RIDES. ADAPTOR WAS REMOVED 20 HOURS EARLIER AND INSPECTED PE R CSB. NO DEFECTS NOTED. THESE UNITS CONTINUE TO FAIL CAUSING VERY EXPENSIVE REPAIRS. 1 L 7 2 3O 3 O A7CE E8CE 2002012900005 20020129 00005 SO 2002 1 29 EKI2002F00000 1 20011204 A 2822 1062 PUMP PIPER PA31 PA31P 7103120 SO LYC O541 TIGO541E1A 41539 EA FUEL SYS INOPERATIVE A EKIR K NONE O OTHER IN INSP/MAINT 1 WP 07 648SC 91 31P7300143 L24062 MFG OVERHAULED SUBMERSABLE FUEL PUMP FOR RIGHT MAIN FUEL TANK QUIT WORKING AFTER 91.6 HOURS 3 MONTHS. 1 L 7 2 3O 3 O A8EA E19EA 2002012900007 20020129 00007 CE 2002 1 29 FPI2002F00000 1 20011219 A 5400 96980001 CHANNEL BEECH 58 58 1152740 CE CONT O520 IO520CB 17032 SO NACELLE CRACKED A FPIA K NONE O OTHER IN INSP/MAINT 1 SO 15 112BS TH628 299351 THESE AIRCRAFT HAVE AN UPPER AND LOWER FIREWALL CHANNEL AND THE UPPER ALMOST ALWAYS CRACKS BELOW THE ENGINE MOUNT BOLTS. THIS AIRCRAFT HAD BOTH THE LEFT AND RIGHT NACELLES UPPER FIREWALL CHANNELS CRACKED AND HAD TO BE REPLACED WITH NEW. 1 L 7 2 3O 3 O 3A16 E5CE 2002012900008 20020129 00008 SO 2002 1 29 FXG2002F00000 1 20011211 A 7110 6878004 COWLING PIPER PA32 PA32R300 7103213 SO LYC O540 TIO540* 41532 EA LT ENGINE COWL FAILED A FXGA O OTHER D F INFLIGHT SEPARATION FLT CONT AFFECTED NR NOT REPORTED 1 AL 01 108NS 32R7680288 WHILE IN FLIGHT THE LEFT SIDE OF THE UPPER ENGINE COWLING CAME LOOSE. THIS CAUSED THE COWLING TO RISE UP AND RIP OUT TH E FORWARD PINS. A LARGE SECTION OF THE LEFT SIDE WAS TORN AWAY AND LOST. NO DEFECTS OR REPAIRS WERE NOTED ON THIS COW LING PRIOR TO FAILURE. 1 L 7 1 3O 3 O A3SO E14EA 2002012900009 20020129 00009 SW 2002 1 29 GDM2002F00000 1 20011113 A 2497 CONNECTOR BELL 205 205A1 1181414 SW LYC T53 T5317A 41549 NE GENERATOR FIRE A GDMA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. A J FLAME/FIRE WARNING INDICATION LD LANDING 1 NM 09 28HJ 30006 07520C LANDED, PROCEEDED WITH NORMAL SHUTDOWN PROCEDURES. DURING TWO-MINUTE SHUTDOWN, NOTICED GENERATOR CYCLING ON AND OFF, FI RE LIGHT ILLUMINATED MOMENTARILY THEN WENT OUT. FIRE LIGHT CAME ON AGAIN WITH MORE GENERATOR CYCLING. EXITED HELICOPTE R WITH ENGINE AT FLIGHT IDLE AND LOOKED IN ENGINE COMPARTMENT. SAW 8 INCH FLAMES FROM GENERATOR CONNECTOR PLUG IN ENGIN E DECK. SHUT DOWN ENGINE IMMEDIATELY. GOT HAND HELD EXTINGUISHER, OPENED ENGINE COWL AND EXTINGUISHED FIRE. SAW SMOKE COMING FROM OTHER AREAS OF THE HELICOPTER. OPENED OTHER ACCESS PANELS AND LOOKED FOR MORE FIRE. SHOT EXTINGUISHER IN TO THE SIGHT HOLE IN RIGHT SIDE OF AIRCRAFT, UNDER ENGINE DECK, TO HIT BOTTOM SIDE OF GENERATOR CONNECTOR PLUG. 1 G 7 1 4U 4 U H1SW E17EA 2002012900010 20020129 00010 CE 2002 1 29 HYI2001F00014 1 20011102 A 2497 CM358950 SWITCH CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO AVIONICS PANEL FAILED E HYIA K NONE L NO TEST IN INSP/MAINT 1 NE 01 258PB 1500 402C0336 ON PREFLIGHT INSPECTION, AVIONICS SWITCH FAILED, MAINTENANCE REPLACED THE SWITCH AND RETURNED AIRCRAFT TO SERVICE. 1 L 7 2 3O 3 O A7CE E8CE 2002012900013 20020129 00013 CE 2002 1 29 JUK2002F00000 1 20011210 A 2612 FIRE WARNING BEECH 90 65A901 1152901 CE PWA PT6 PT6* 52043 EA LT ENGINE FALSE INDICATION E JUKA A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 SO 33 65JA LM34 LEFT ENGINE FIRE WARNING SYSTEM. AFTER BEGINNING DESCENT FROM 9,000 FEET IN HEAVY RAIN, THE LEFT ENGINE FIRE WARNING SY STEM ACTIVATED. ANUNCIATOR REMAINED ILLUMINATED 2 TO 3 MINUTES AND THEN WENT BACK OFF ABOUT THE SAME TIME THE RAIN LIGH TENED UP. ANOTHER U21 OPERATOR HAS UNVERIFIED REPORT OF A FALSE FIRE WARNING DURING HEAVY RAIN CONDITIONS. 1 L 7 2 3T 3 T 3A20 E2NE 2002012900014 20020129 00014 SW 2002 1 29 KZH2002F00000 1 20011210 A 5711 204312 SPAR CAP AIRTRC AT500 AT502B 0390307 SW PWA PT6 PT6* 52043 EA RT WING CRACKED A KZHG K NONE O OTHER IN INSP/MAINT 1 SO 07 6136M 3133 502B0341 WHILE PERFORMING AN EDDY CURRENT INSPECTION OF THE .3750 DIAMETER BOLT HOLES ON THE LOWER SPAR CAP, 3 SMALL CRACKS WERE INDICATED. AD HAS BEEN ISSUED ADDRESSING THE ABOVE PROBLEM, HOWEVER IT DOES NOT ADDRESS AIRCRAFT OF THIS MODEL BELOW 40 00 TT. I AM CONCERNED THAT THE TIME INTERVAL BEFORE PERFORMING THE INITIAL INSPECTION MAY BE TOO HIGH. WOULD SUGGEST L OWERING THIS TIME. I ALSO FEEL THAT A REPETITIVE INSPECTION INTERVAL NEEDS TO BE ESTABLISHED, EVEN AFTER COMPLIANCE OF THE AD. A ROUTINE INSPECTION OF THE SPAR CAP WILL ALLOW AN OPERATOR TO KNOW IF THE WINGS INTEGRITY HAS BEEN COMPROMISED AND IS IN EFFECT RIDING ON THE FAIL SAFE PLATE. 1 L 7 1 3T 3 T NC A17SW E2NE 2002012900015 20020129 00015 SO 2002 1 29 LAB2002F00000 1 20011214 A 5711 SPAR PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA WING CRACKED A LABA K NONE O OTHER IN INSP/MAINT 1 AL 05 3523Y 5530 317952115 CRACK IN A SPOT THAT IS NOT VISIBLE TO BORESCOPE WHEN COMPLYING WITH AD. 730 HOURS SINCE EFFECTIVE DATE OF AD. 1000 HO URS ALLOWED FROM EFFECTIVE DATE. 1 L 7 2 3O 3 O A20SO E14EA 2002012900016 20020129 00016 SO 2002 1 29 LQU2002F00000 2 20011201 A 8540 PIN CESSNA 421 421B 2076014 CE CONT O520 GTSIO520H 17032 SO IDLER GEAR MISSING A LQUA K NONE O OTHER IN INSP/MAINT 1 WP 09 799 421B0324 21044172H RIGHT ENGINE RAN ROUGH AND VIBRATED BADLY IN FLIGHT, SHUT DOWN. VISUAL INSPECTION FOUND OPEN HOLE IN BACK OF CRANKCASE. IDLER GEAR SUPPORT PIN MISSING. FOUND PIN ON ENGINE NACELLE FLOOR UNDER ENGINE. NO VISUAL DAMAGE NOTED TO PIN. ENGI NE NEEDS PIN TO HOLD IDLER GEAR INSIDE OF CRANKCASE TO RUN ACCESSORIES. PIN FALLS OUT, GEAR WAS LOOSE WITH NO SUPPORT I NSIDE BACK OF CRANKCASE. 1 L 7 2 3O 3 O A7CE E7CE 2002012900017 20020129 00017 SW 2002 1 29 MV52002F00000 1 20011126 A 5260 34000039 TUBE GULSTM 690TP 690B 7630516 SW GARRTT TPE331 TPE3315 01514 WP CABIN STEP CRACKED B MV5R K NONE O OTHER IN INSP/MAINT 1 GL 11 517HP 6803 11517 FORWARD CABIN DOOR STEP TUBE CRACKED AT ROLL PIN (PN MS9048-047) ATTACHMENT. CRACK EXTENDED ONE INCH AFT FROM THE ROLL PIN. 1 H 7 2 3T 4 T 2A4 E4WE 2002012900018 20020129 00018 CE 2002 1 29 OG52002F00000 1 20011227 A 6120 PITCH CONTROL BBAVIA 8 8KCAB 2110612 CE LYC O360 AEIO360H1A 41514 EA HARTZL HCC2Y HCC2YR4 GL PROP PITCH CRACKED B OG5R K NONE O OTHER IN INSP/MAINT 1 GL 21 67ND 66792 L2450351A AU10095B DURING SCHEDULED INSPECTION PITCH CYLINDER OF THE PROPELLER ASSEMBLY, WAS FOUND TO BE CRACKED ON THE FORWARD END. THE C RACK EXTENDED FROM BOTH SIDES OF THE LOW PITCH STOP NUT OUT BOARD. 1 H 7 1 3O 3 O A21CE 1E10 5 C P920 2002012900019 20020129 00019 CE 2002 1 29 QFY2002F00000 1 20011127 A 3350 651810911 POWER SUPPLY CESSNA 500 500CESSNA 2076602 CE CABIN CORRODED A QFYR K NONE L NO TEST IN INSP/MAINT 1 NE 03 15CQ 5000101 REPLACED MELTED CORRODED EMERGENCY POWER SUPPLY WITH NEW POWER SUPPLY DID NOT FUNCTION AT ALL UPON INSPECTION. CLOSER I NSPECTION AT LOST INTERVAL MAY HAVE SHOWN CORROSION. POSSIBLE FAILURE DUE TO CORROSION DISCHARGING POWER SUPPLY RAPIDLY WHILE AIRCRAFT POWER CHARGING SUPPLY. 1 L 7 2 4F A22CE 2002012900021 20020129 00021 NM 2002 1 29 R7MA34258 1 20011116 A 6710 900C3010004109 ACTUATOR DOUG MD900 MD900 3027375 NM PWA PW206 PW206A NE TRIM ACTUATOR INOPERATIVE E R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 901CF 134 90000012 TRIM ACTUATOR UNIT INOPERATIVE. 1 G 7 2 3U 3 U NC H19NM E42NE 2002012900022 20020129 00022 EU 2002 1 29 R7MA34390 1 20010911 A 6220 LINER SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE BALL JOINT WORN E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 397LG 516 3268 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002012900023 20020129 00023 EU 2002 1 29 R7MA34391 1 20011010 A 6220 LINER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE BALL JOINT WORN E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 96LG 394 2817 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002012900026 20020129 00026 NE 2002 1 29 R7MR34029 2 20010723 A 7250 406103101 SLEEVE BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE TURBINE SECTION WORN B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 10UM 561 7231 SLEEVE, WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 2002012900044 20020129 00044 NE 2002 1 29 R7MR34030 2 20010723 A 7230 406108007 RING BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE FLOW FENCE WORN B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 10UM 561 7231 LE45508EFA FLOW RING, WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 2002012900046 20020129 00046 NE 2002 1 29 R7MR34116 2 20010411 A 7230 430124203 BEARING BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE COMPRESSOR DAMAGED B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 911VU 243 7141 TURBINE, ANNULAR BALL BEARING, EXCESSIVE PITTING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 2002012900049 20020129 00049 2002 1 29 R7MR34236 4 20011004 A 3160 L316M30C1002 DISPLAY UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206A NE COCKPIT INOPERATIVE B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 135SJ 947 0054 COCKPIT DISPLAY UNIT, UNIT INOPERATIVE. VISABLE LINE THROUGH TOP PORTION OF READ OUT. REPLACED WITH NEW UNIT, CORRECTE D PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2002012900050 20020129 00050 EU 2002 1 29 R7MR34237 1 20011025 A 6340 DL40438 INDICATOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20 03013 GL TRIPLE TACH FAILED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 485EC S754 TRIPLE RPM INDICATOR, UNIT INOPERATIVE. OUT OF BOX FAILURE. NR 2 NEEDLE READS 12 PERCENT LOW. REPLACED WITH NEW UNIT , CORRECTED PROBLEM. 1 G 7 2 3U 3 U H3EU E4CE 2002012900060 20020129 00060 EU 2002 1 29 R7MR34238 1 20011019 A 6340 117902111 INDICATOR BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE TRIPLE TACH INOPERATIVE B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 117SU 818 7527 TRIPLE TACH INDICATOR, UNIT INOPERATIVE. ROTOR RPM FLUCTUATES. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U NC H13EU E19EU 2002012900062 20020129 00062 EU 2002 1 29 R7MR34239 1 20011021 A 2497 45033501 BUSS TIE UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE ELECTRICAL BOX OPEN B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 426AE 102 0159 UNIT INOPERTIVE. NUMBER 1 BUSS TIE STAYS OPEN. Z 200 CORD INSIDE HAS BURN SPOT. REPLACED WITH NEW UNIT, CORRECTED PRO BLEM. (102HN) (K) 1 G 7 2 3U 3 U O H88EU E42NE 2002012900063 20020129 00063 2002 1 29 R7MR34243 4 20011101 A 3457 0110028000 GPS BELL 407 407 1182206 SW ALLSN 250C 250C47B GL COCKPIT INOPERATIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 407SJ 1 53422 GNS430,GLOBAL NAVIGATIONAL SYSTEM, UNIT INOPERATIVE. WILL NOT TRANSMIT ON COMM SIDE, AT ANY FREQUENCY. 1 G 7 1 3U 3 U O H2SW E1GL 2002012900064 20020129 00064 SW 2002 1 29 R7MR34249 1 20010726 A 2121 ES731861 BLOWER BELL 407 407 1182206 SW ALLSN 250C 250C47B GL CIRCUIT BREAKER OVERHEATED B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 911LN 80 53446 BLOWER ASSEMBLY, OVER HEATS CAUSING CIRCUIT BREAKER TO POP. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2002012900066 20020129 00066 SW 2002 1 29 R7MR34250 1 20010920 A 2121 ES731861 BLOWER BELL 407 407 1182206 SW ALLSN 250C 250C47B GL E/E BAY INOPERATIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 107LN 51 53483 BLOWER ASSEMBLY, UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2002012900075 20020129 00075 SW 2002 1 29 R7MR34252 1 20011005 A 6340 407375001105 INDICATOR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL COCKPIT INOPERATIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 911LN 689 53446 INDICATOR, MGT, UNIT INOPERATIVE. BAD MEMORY WILL NOT HOLD EXCEEDANCES. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2002012900076 20020129 00076 SW 2002 1 29 R7MR34253 1 20011022 A 2915 206076036105 VALVE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL HYDRAULIC SYS LEAKING B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 911LN 734 53446 VALVE, UNIT INOPERATIVE. FAILS TO STOP FLOW OF HYDRAULIC PRESSURE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.(K) 1 G 7 1 3U 3 U O H2SW E1GL 2002012900077 20020129 00077 NM 2002 1 29 R7MR34258 1 20011116 A 6710 900C3010004109 ACTUATOR DOUG MD900 MD900 3027375 NM PWA PW206 PW206A NE MAIN ROTOR TRIM INOPERATIVE B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 901CF 166 90000012 TRIM ACTUATOR ASSEMBLY, UNIT INOPERATIVE. OPERATES IN ONE DIRECTION ONLY. REPLACED WITH NEW, CORRECTED PROBLEM. (K) 1 G 7 2 3U 3 U NC H19NM E42NE 2002012900078 20020129 00078 2002 1 29 R7MR34282 4 20011123 A 2210 41600297004 MODULE UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE AUTO PILOT SHORTED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 426AE 103 0159 UNIT INOPERATIVE. POPS NUMBER 2 APM CIRCUIT BREAKER. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (102HN) (K) 1 G 7 2 3U 3 U O H88EU E42NE 2002012900079 20020129 00079 EU 2002 1 29 R7MR34283 1 20011107 A 6720 41800876800 ACTUATOR UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE TAIL ROTOR FAILED B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 427AE 45 0162 UNIT INOPERATIVE. WOULD NOT PASS PREFLIGHT CHECK. FAILED INDICATION ON PRIMARY FLIGHT DISPLAY. REPLACED WITH NEW UNIT , CORRECTED PROBLEM. (101HN)(K) 1 G 7 2 3U 3 U O H88EU E42NE 2002012900080 20020129 00080 SW 2002 1 29 R7MR34290 1 20011011 A 3340 099799100 SEARCH LIGHT BELL 407 407 1182206 SW ALLSN 250C 250C47B GL EXTERIOR LIGHTS MALFUNCTIONED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 107LN 105 53483 SEARCH LIGHT ASSEMBLY, UNIT INOPERATIVE. UNIT WILL ONLY EXTEND AND RETRACT, WILL NOT ROTATE LEFT OR RIGHT. LIGHT IS ST UCK SLIGHTLY TO THE RIGHT OF CENTER. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.(K) 1 G 7 1 3U 3 U O H2SW E1GL 2002012900081 20020129 00081 SW 2002 1 29 R7MR34291 1 20011119 A 3340 099799100 SEARCH LIGHT BELL 407 407 1182206 SW ALLSN 250C 250C47B GL SEARCH LIGHT INOPERATIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 107LN 106 53483 SEARCH LIGHT ASSEMBLY, UNIT INOPERATIVE. UNIT STOPPED ROTATING LEFT OR RIGHT. REPLACED WITH NEW UNIT, CORRECTED PROBLE M.(K) 1 G 7 1 3U 3 U O H2SW E1GL 2002012900082 20020129 00082 SW 2002 1 29 R7MR34292 1 20011121 A 3340 099799100 SEARCH LIGHT BELL 407 407 1182206 SW ALLSN 250C 250C47B GL EXTERIOR LIGHTS INOPERATIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 107LN 3 53483 SEARCH LIGHT ASSEMBLY, UNIT INOPERATIVE. LAMP WOULD NOT TURN OFF UNTIL THE MASTER WAS SWITCHED OFF. WHEN THE MASTER WA S SWITCHED BACK ON, THE LIGHT WOULD NOT COME BACK ON. REPLACED WITH LOANER UNIT CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2002012900083 20020129 00083 EU 2002 1 29 R7MR34293 1 20011120 A 6220 BUSHING SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE STARFLEX DEBONDED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 52285 953 3251 WORN BEYOND SERVICEABLE LIMITS. BUSHINGS DEBONDED FROM MFG. REPLACED WITH NEW UNITS, CORRECTED PROBLEM. (106LN) (K) 1 G 7 1 3U 3 U H9EU E19EU 2002012900084 20020129 00084 2002 1 29 R7MR34294 4 20011130 A 2210 41600297004 MODULE UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE AUTO PILOT FAILED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 427AE 51 0162 UNIT INOPERATIVE. AUTOPILOT FAULT SHOWS ON PFD AS VERTICAL LINES IN AMBER COLOR. UNABLE TO PERFORM PREFLIGHT AUTOPILOT CHECK. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (N-101HN)(K) 1 G 7 2 3U 3 U O H88EU E42NE 2002012900085 20020129 00085 SW 2002 1 29 R7MR34297 1 20011210 A 6210 407015001117 BLADE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL MAIN ROTOR DEBONDED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 107LN 243 53483 BLADE MR 407(HIGH VISIBILITY), DEBONDING UNDER EROSION STRIP, NEAR BLADE TIP. REPLACED WITH USED BLADE CORRECTED PROBLE M. 1 G 7 1 3U 3 U O H2SW E1GL 2002012900086 20020129 00086 2002 1 29 R7MR34309 4 20011209 A 2312 TFM30G TRANSCEIVER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE VHF/FM INTERMITTENT B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 852HW 36 2630 VHF/FM TRANSCEIVER, UNIT INOPERATIVE. TRANSMITS FIRST TIME THEN FAILS TO TRANSMIT EVEN WHILE TRANSMIT LIGHT IS ILLUMINA TED. ANTENNA CHECKS, OK. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002012900087 20020129 00087 SW 2002 1 29 R7MR34312 1 20011211 A 3340 099799100 SEARCH LIGHT BELL 407 407 1182206 SW ALLSN 250C 250C47B GL EXTERIOR LIGHTS INOPERATIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 107LN 9 53483 SEARCH LIGHT ASSEMBLY, UNIT INOPERATIVE. WILL NOT POWER DOWN WHEN SWITCH IS TURNED OFF. GEARS ARE NOISY WHEN LIGHT ROT ATES IN STOW POSITION (BEFORE LIGHT PARKS IN CENTER POSITION). REPLACED WITH REPAIRED UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2002012900088 20020129 00088 EU 2002 1 29 R7MR34316 1 20010713 A 2460 SP461310 SWITCH BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE DC SYSTEM INTERMITTENT B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 117SU 317 7527 TOGGLE SWITCH, UNIT INOPERATIVE. WILL NOT STAY ON (INTERMITTENT). REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U NC H13EU E19EU 2002012900089 20020129 00089 EU 2002 1 29 R7MR34317 1 20010713 A 2460 SP461310 SWITCH BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE DC SYSTEM INTERMITTENT B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 117SU 317 7527 TOGGLE SWITCH, UNIT INOPERATIVE (INTERMITTENT). WILL NOT STAY ON. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U NC H13EU E19EU 2002012900092 20020129 00092 EU 2002 1 29 R7MR34327 1 20011017 A 7332 9550162490 PRESSURE SWITCH BOLKMS BK117 BK117C1 5626025 EU FUEL SYS INOPERATIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 117SU 247 7527 PRESSURE SWITCH, UNIT INOPERATIVE. FUEL PRESSURE LIGHT IS ON. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H13EU 2002012900093 20020129 00093 EU 2002 1 29 R7MR34329 1 20010219 A 2822 9A2045 CARTRIDGE UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206A NE BOOST PUMP INOPERATIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 135SJ 159 0054 FUEL PUMP CARTRIDGE, UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2002012900094 20020129 00094 EU 2002 1 29 R7MR34341 1 20010713 A 3340 122395R5758 LIGHT UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE ANTI COLLISION INOPERATIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 135N 255 0086 ANTI-COLLISION LIGHT, UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2002012900095 20020129 00095 EU 2002 1 29 R7MR34343 1 20011201 A 3340 315152 LIGHT UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE TAIL SHORTED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 427AE 52 0162 UNIT INOPERATIVE. INTERNAL SHORT CIRCUIT. REGISTERS 1 OHM RESISTENCE WHICH INDICATES NO ELECTRICAL FLOW TO THE BULB. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2002012900096 20020129 00096 2002 1 29 R7MR34344 4 20011201 A 3420 42000332411 INDICATOR UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE COCKPIT ERRATIC B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 427AE 52 0162 UNIT INOPERATIVE. UNIT MAKES ERRATIC COMPASS HEADING FROM 35 TO 50 DEGREES OFF FROM ACTUAL HEADING. FAULT ON PRIMARY F LIGHT DISPLAY AND GYRO ON CAD. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (N-101HN) 1 G 7 2 3U 3 U O H88EU E42NE 2002012900097 20020129 00097 EU 2002 1 29 R7MR34345 1 20010716 A 6230 L713M2144101 BELLOWS UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE MAIN ROTOR WORN B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 135N 259 0086 BELLOWS ASSEMBLY, WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2002012900100 20020129 00100 EU 2002 1 29 R7MR34347 1 20011212 A 2422 SS120 INVERTER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE ELECTRICAL INOPERATIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 220CF 59 3411 STATIC INVERTER 1200VA DC TO 60HZ 1 PHASE, UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002012900102 20020129 00102 EU 2002 1 29 R7MR34348 1 20011205 A 6330 L633M2001106 MOUNT UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206A NE TRANSMISSION LEAKING B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 135SJ 294 0054 Z-ARIS EC 135, LEAKING BEYOND SERVICEABLE LIMITS. EMERGENCY STOP CLEARENCE LESS THAN .020 INCH (COLLAPSED). REPLACED W ITH NEW UNIT, CORRECTED PROBLEM. UNIT SN WI-349 RECEIVED ON S214959 IS SPARE UNIT. 1 G 7 2 3U 3 U O H88EU E42NE 2002012900104 20020129 00104 EU 2002 1 29 R7MR34351 1 20011121 A 7797 430121302 HARNESS BOLKMS 117 BK117B2 5626013 EU LYC LTS101 LTS101750B1 41560 NE ENGINE SHORTED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 62LF 601 7163 FORWARD ELECTRICAL CABLE, INTERNAL SHORT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U NC H13EU E5NE10 2002012900105 20020129 00105 EU 2002 1 29 R7MR34353 1 20011121 A 7797 430121302 HARNESS BOLKMS 117 BK117B2 5626013 EU LYC LTS101 LTS101750B1 41560 NE ENGINE SHORTED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 62LF 772 7163 LE45610EFA FORWARD ELECTRICAL CABLE, INTERNAL SHORT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U NC H13EU E5NE10 2002012900106 20020129 00106 EU 2002 1 29 R7MR34354 1 20010810 A 7797 430121302 HARNESS BOLKMS 117 BK117B2 5626013 EU LYC LTS101 LTS101750B1 41560 NE ENGINE SHORTED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 62LF 385 7163 LE45753EFA FORWARD ELECTRICAL CABLE, INTERNAL SHORT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U NC H13EU E5NE10 2002012900107 20020129 00107 EU 2002 1 29 R7MR34355 1 20010914 A 2842 9550171990 PRESSURE SWITCH SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE FUEL SYS FAILED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 397LG 501 3268 22116 LOW FUEL PRESSURE SWITCH, UNIT INOPERATIVE. FAILED TEST. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E00054EN 2002012900108 20020129 00108 NE 2002 1 29 R7MR34356 2 20011015 A 7412 9550173220 EXCITER SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE IGNITION SYS FRETTED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 392LG 826 3252 22100 IGNITION EXCITER HE 931, FRETTING AND SEPARATION OF FLANKS. SEE SL2061/01/ARRIEL2/11. REPLACED WITH NEW UNIT, CORRECTE D PROBLEM. 1 G 7 1 3U 3 U H9EU E00054EN 2002012900109 20020129 00109 NE 2002 1 29 R7MR34357 2 20011111 A 7412 9550173220 EXCITER SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE IGNITION SYS INOPERATIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 397LG 608 3268 22116 IGNITION EXCITER HE 931, UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E00054EN 2002012900110 20020129 00110 NE 2002 1 29 R7MR34358 2 20011109 A 7412 9550168760 IGNITER SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE IGNITION SYS INOPERATIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 397LG 606 3268 IGNITER, UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002012900112 20020129 00112 2002 1 29 R7MR34360 4 20010816 A 3413 3502011111 INDICATOR SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT MALFUNCTIONED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 52285 791 3251 UNIT INOPERATIVE. SHOWS 20 FEET DOWN. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (106LN) (K) 1 G 7 1 3U 3 U H9EU E19EU 2002012900113 20020129 00113 EU 2002 1 29 R7MR34362 1 20010826 A 3340 356H2802 POWER SUPPLY SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE EXTERIOR LIGHTS INOPERATIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 397LG 490 3268 POWER SUPPLY BOX, UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002012900115 20020129 00115 EU 2002 1 29 R7MR34383 1 20010503 A 6320 1130021089 PRESSURE SWITCH SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE MGB OIL INOPERATIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 6099P 188 2818 PRESSURE SWITCH, UNIT INOPERATIVE. MGB OIL PRESSURE WARNING LIGHT NOT WORKING AT PROPER TIME. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (K) 1 G 7 1 3U 3 U H9EU E19EU 2002012900116 20020129 00116 EU 2002 1 29 R7MR34384 1 20011116 A 6510 593404 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE T/R DRIVE WORN B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 438AE 102 3402 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (385LR) (K) 1 G 7 1 3U 3 U H9EU E19EU 2002012900131 20020129 00131 EU 2002 1 29 R7MR34385 1 20010912 A 8010 845UN1Q4AA5F SWITCH SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE STARTER INOPERATIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 103LN 293 3128 SWITCH INOPERATIVE. START SWITCH FAULT CODE UPON SHUTDOWN. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.(K) 1 G 7 1 3U 3 U H9EU E19EU 2002012900139 20020129 00139 EU 2002 1 29 R7MR34386 1 20010731 A 6220 117775P BALL JOINT SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE MAIN ROTOR WORN B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 93LG 527 2654 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.(K) 1 G 7 1 3U 3 U H9EU E19EU 2002012900140 20020129 00140 EU 2002 1 29 R7MR34388 1 20010817 A 6220 LINER SNIAS 350 AS350B 8680801 EU MAIN ROTOR WORN B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 5771C 283 1369 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REMPLACED WITH NEW UNIT, CORRECTED PROBLEM.(K) 1 G 7 1 3U H9EU 2002012900141 20020129 00141 EU 2002 1 29 R7MR34389 1 20011008 A 6220 117775P BALL JOINT SNIAS 350 AS350B2 8680813 EU MAIN ROTOR WORN B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 92LG 335 2575 STARFLEX, BALL JOINT, TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 2002012900142 20020129 00142 EU 2002 1 29 R7MR34398 1 20011212 A 6340 117902111 INDICATOR BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE TRIPLE TACH INOPERATIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 117SU 109 7527 TRIPLE TACH INDICATOR, UNIT INOPERATIVE. NO 2 ENGINE INDICATION 4 PERCENT HIGH. REPLACED WITH NEW UNIT, CORRECTED PROB LEM. 1 G 7 2 3U 3 U NC H13EU E19EU 2002012900143 20020129 00143 EU 2002 1 29 R7MR34400 1 20011217 A 3340 4361646 LANDING LIGHT UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE EXTERIOR LIGHTS INOPERATIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 427AE 62 0162 UNIT INOPERATIVE. WILL NOT RETRACT OR EXTEND. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (N-101HN) (K) 1 G 7 2 3U 3 U O H88EU E42NE 2002012900144 20020129 00144 EU 2002 1 29 R7MR34401 1 20011221 A 6220 ARM SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE STARFLEX SEPARATED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 392LG 925 3252 STARFLEX ARM SEPARATION(RED BLADE). REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002012900145 20020129 00145 SW 2002 1 29 R7MR34404 1 20011213 A 5330 407070620145 PANEL BELL 407 407 1182206 SW ALLSN 250C 250C47B GL FUSELAGE CRACKED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 407SJ 958 53422 PANEL CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2002012900146 20020129 00146 EU 2002 1 29 RM7R34387 1 20011120 A 6220 LINER SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE STARFLEX WORN B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 52285 447 3251 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (N-106LN)(K) 1 G 7 1 3U 3 U H9EU E19EU 2002012900151 20020129 00151 EA 2002 1 29 S2L2002F00000 2 20010202 A 7414 6361 MAGNETO CESSNA 206 T206H 2073303 CE LYC O540 TIO540* 41532 EA ENGINE FAILED A S2LA O OTHER O OTHER NR NOT REPORTED 1 SO 13 272ME 315 T20608216 THE MAGNETO APPEARS TO HAVE INTERNAL FAILURE. PART SHOWS GUIDENCE OF ARCHING AND EXCESSIVE HEAT. PICTURES ARE AVAILABL E ON REQUEST. 1 H 7 1 3O 3 O RT A4CE E14EA 2002012900163 20020129 00163 WP 2002 1 29 DHL2002805017 1 20011230 A 5522 SKIN DOUG DC8 DC873F 302199F WP ELEVATOR DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 75397 46125 LEFT ELEVATOR LWR SKIN STA 28.843 - 132.750 DENTED, DEFLECTED AND RIVETS LOOSE. 2 L 7 4 4F RT 4A25 2002012900164 20020129 00164 WP 2002 1 29 DHL2002805020 1 20011230 A 5522 5644470507 SKIN DOUG DC8 DC873F 302199F WP ELEVATOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 LEFT ELEVATOR LOWER SKIN (STA XE132.000 - XE246.000) DENTED, DEFLECTED AND CRACKED .250 (MAJOR REPAIR). 2 L 7 4 4F RT 4A25 2002012900165 20020129 00165 WP 2002 1 29 DHL2002805021 1 20011230 A 5522 5644470507 SKIN DOUG DC8 DC873F 302199F WP ELEVATOR DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 LEFT ELEVATOR LOWER SKIN SHOWS DENTS AT OVERALL AREA STA XE246.870-XE285.690. 2 L 7 4 4F RT 4A25 2002012900169 20020129 00169 WP 2002 1 29 DHL2002805008 1 20011231 A 5322 INTERCOSTAL DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 805DH 46125 N/R 1349CTR. FUS. - INTERCOSTAL CRACKED @ STA. 680 BTWN. L29L - L30L 2 L 7 4 4F RT 4A25 2002012900170 20020129 00170 WP 2002 1 29 DHL2002805016 1 20011230 A 5712 RIB DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 805DH 75397 46125 N/R 0438LH. WING L/E - RIB @ STA. XFS 603.750 , CRACKED .500 2 L 7 4 4F RT 4A25 2002012900177 20020129 00177 2002 1 29 RAIA00201033 4 20010116 A 3435 7014300901 SCREEN EMB 145 EMB145 3260210 SO INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 807HK 5762 145119 5278- PIT- F/O MALFUNCTION DISPLAY WENT BLANK DURING TAXI. MAINTENANCE DEFERRED MALFUNCTION. DEFERRAL WAS CLEARED BY REM OVING AND REPLACING THE MALFUNCTION DISPLAY SCREEN. OPS CK OK. 2 L 7 2 4F RT T00011AT 2002013000051 20020130 00051 CE 2002 1 30 T4O2001F00001 1 20011206 A 5520 1016100196 TORQUE TUBE BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA RT ELEVATOR LOOSE A T4OR K NONE O OTHER IN INSP/MAINT 1 NE 03 266RH 7811 BB778 THE RIVETS ON THE RIGHT ELEVATOR TORQUE TUBE TO INBOARD CASTING (FOR PUSHROD) WERE LOOSE AND SMOKING. PROBABLE CAUSE UN KNOWN. INSTALLED A NEW TORQUE TUBE ASSEMBLY FOR THE RT ELEVATOR. 1 L 7 2 4T 4 T A24CE E4EA 2002013000052 20020130 00052 CE 2002 1 30 T4O2001F00002 1 20011206 A 5520 1016100196 TORQUE TUBE BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA RT ELEVATOR LOOSE A T4OR K NONE O OTHER IN INSP/MAINT 1 NE 03 5PX 5012 BB554 THE RIVETS ON THE RIGHT ELEVATOR TORQUE TUBE TO OUTBOARD CASTING (WHERE IT BOLTS TO ELEVATOR) WERE LOOSE AND SMOKING. P ROBABLE CAUSE UNKNOWN. INSTALLED A NEW TORQUE TUBE ASSEMBLY FOR THE RIGHT ELEVATOR. 1 L 7 2 4T 4 T A24CE E4EA 2002013000057 20020130 00057 CE 2002 1 30 T9Z2002F00000 1 20011230 A 3010 14320003 BOOT CESSNA 337 T337H 2075733 CE CONT O360 TSIO360* 17025 SO DEICE SYS CRACKED B T9ZR K NONE O OTHER IN INSP/MAINT 1 NM 09 337SH 3242 33701872 REMOVED HORIZONTAL DEICE BOOT DUE TO CONDITION. DURING CLEANUP AND INSPECTION CRACKS WERE FOUND IN LEADING EDGE AT RIVE T LOCATIONS AT RIBS. DEFECTS APPEAR TO BE CAUSED FROM IMPROPERLY DIMPLED HOLES. THERE ARE NO INSPECTION PANELS FOR LEA DING EDGE, SO VISUAL INSPECTION CAN NOT BE PERFORMED. RECOMMEND USING HAND PRESSURE TO CHECK FOR CRACKS AT RIB LOCATION S. 1 H 7 2 3O 3 O A6CE E9CE 2002013000058 20020130 00058 CE 2002 1 30 TIM2002F00000 1 20011220 A 2730 DSRP4 BEARING BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA LT ELEV HORN WORN E TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 4381Y 36576 U71 THE LEFT ELEVATOR PIVOT BEARING WAS FOUND TO BE LOOSE WHERE THE HORN PIVOTS ON THE INBOARD SIDE IN THE TAIL. THE BEARIN G AND BUSHING WERE REPLACED AND INSTALLED IAW MM. THIS APPEARS TO BE A FREQUENT DISCREPANCY WITH THE MFG AND COULD BE R ELATED TO THE BLAST STREAM OF AIR FROM THE PROP. 1 L 7 2 3T 4 T A14CE E4EA 2002013000061 20020130 00061 CE 2002 1 30 TIM2002F00001 1 20011220 A 2720 504200337 CASTING BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA COCKPIT CRACKED E TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 4381Y 36595 U71 DURING A DETAILED INSPECTION OF THE INTERIOR AND STRUCTURE, CRACKS WERE FOUND EXTENDING FROM THE RIVETS HOLDING UNTPLATE S USED TO SECURE THE RUDDER CONTROL BELLCRANK PIVOT CASTING. FURTHER INSPECTION REVEALED NO OTHER DISCREPANCIES. BEAM WAS REPLACED WITH NEW BEAM. THIS WAS CAUSED BY THE ACCUMULATION OF MANY FLIGHT HOURS AND IS THE RESULT OF A PROPERLY PE RFORMED INSPECTION. 1 L 7 2 3T 4 T A14CE E4EA 2002013000068 20020130 00068 CE 2002 1 30 TIM2002F00002 1 20011126 A 3233 993880081 ACTUATOR BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA MLG LEAKING E TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 14MV U59 THE AIRCRAFT HAD NEEDED INFREQUENT SERVICING OF THE HYD. FLUID RESERVOIR AND YET NO LEAKS HAD BEEN DISCOVERED. SINCE TH E AMOUNT OF FLUID ADDED HAD NEVER BEEN AN ALARMING AMOUNT, THE AIRCRAFT HAD ALWAYS BEEN RETURNED TO SERVICE. THE LEAK O F HYD. FLUID WAS DISCOVERED ON A POST FLIGHT INSPECTION AND REPORTED TO MAINTENANCE. IT WAS DETERMINED THE RIGHT MAIN L ANDING GEAR ACTUATOR SHAFT SEAL WAS THE SOURCE OF THE HYD LEAK. THE ACTUATOR WAS REPLACED AND THE REMAINING ACTUATORS I NSPECTED FOR POTENTIAL LEAKS. NO OTHER DISCREPANCIES FOUND. 1 L 7 2 3T 4 T A14CE E4EA 2002013000069 20020130 00069 CE 2002 1 30 TIM2002F00003 1 20011115 A 3020 5E1319 INLET BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA DEICER BURNED E TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 14MV U59 DURING A POST INSPECTION CHECK OF AIRCRAFT SYSTEMS, IT WAS DETERMINED THE LEFT ENGINE INLET DEICER WAS INOPERATIVE. A CL OSE INSPECTION OF THE SURFACE OF THE DEICER REVEALED IRREGULAR BULGING AND INDICATORS OF HIGH HEAT. THE DEICER WAS REPL ACED AND THE REST OF THE SYSTEM INSPECTED FOR OTHER PROBLEMS. NO OTHER DISCREPANCY WAS FOUND. AGE WAS MORE THAN LIKELY THE CAUSE OF THE CONDITION. BY EXPERIENCE AND CLOSE INSPECTION OF THE SURFACE OF THE DEICER, THE PROJECTED LIFE IS EAS ILY DETERMINED. 1 L 7 2 3T 4 T A14CE E4EA 2002013000078 20020130 00078 CE 2002 1 30 VJ32001F00013 1 20011213 A 3230 SM50D7 RELAY BEECH 33 F33A 1151425 CE CONT O520 IO520B 17032 SO MLG JAMMED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 6311Z CE997 DYNAMIC RELAY CONTROLS THE LANDING GEAR MOTOR. THIS UNIT IS INCONSISTENT IN CONTROL OF MOTOR WHEN POWER TO THE RELAY CO NTROL IS TURNED OFF BY THE ACTUATOR SWITCH ON THE GEAR BOX. WHEN THIS HAPPENS THE GEAR BOX WILL BOTTOM OUT ON THE INTER NAL STOP INSIDE THE GEAR BOX. WHNE THE RELAY FAILS, IT JAMS THE SECTOR GEAR IN THE GEAR BOX TO THE STOP. 1 L 7 1 3O 3 O 3A15 E5CE 2002013000079 20020130 00079 SO 2002 1 30 VJ32001F00014 2 20011213 A 7414 6310 DISTRIBUTOR BEECH 33 F33A 1151425 CE CONT O520 IO520B 17032 SO MAGNETO MELTED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 8240T 875 CE1542 REMOVED MAGNETO FROM ENGINE FOR 500 HOUR. INSPECTION. INSPECTION FOUND THAT THE PLASTIC WAS MELTED ON THE DISTRIBUTOR C AP. MAGNETO WAS SENT TO MFG. 1 L 7 1 3O 3 O 3A15 E5CE 2002013000080 20020130 00080 EA 2002 1 30 VJ32001F00015 2 20011213 A 7414 DISTRIBUTOR BLK PIPER PA28 PA28181 7102807 SO LYC O360 IO360A1A 41514 EA MAGNETO WORN G VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 4163W 504 2843127 R37056 MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW THE MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM M AGNETO AND FOUND THE CARBON BRUSH WORN. CARBON DUST WAS FOUND ON THE FLAT PART OF THE CAP. THE WEARER ON THIS BRUSH IS ABOVE NORMAL FOR 500 HOURS. 1 L 7 1 3O 3 O 2A13 1E10 2002013000081 20020130 00081 SO 2002 1 30 VJ32002F00000 2 20011211 A 7414 DISTRIBUTOR BEECH 33 F33A 1151425 CE CONT O520 IO520B 17032 SO MAGNETO INOPERATIVE B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 5587K 730 CE1392 820445R MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNE TO. DISTRIBTOR BLOCK ASSEMBLY SENT TO MFG FOR INSPECTION. NEW DISTRIBUTOR BLOCK ASSEMBLY. INSTALLED MAGNETO. 1 L 7 1 3O 3 O 3A15 E5CE 2002013000082 20020130 00082 SO 2002 1 30 VJ32002F00001 2 20011211 A 8530 LIFTER BEECH 33 F33A 1151425 CE CONT O520 IO520B 17032 SO INTAKE COLLAPSED A VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 1565A 26 CE1331 820752R ENGINE HAD A CLICKING NOISE AT LOW RPM. REMOVED NR 2 ROCKER COVER AND FOUND THAT THE INTAKE LIFTER WAS COLLAPSED, REMOV ED LIFTER BODY AND INSTALLED NEW LIFTER, GROUND RUN CHECKED OK. PART RETURNED TO MFG FOR WARRANTY. 1 L 7 1 3O 3 O 3A15 E5CE 2002013000083 20020130 00083 CE 2002 1 30 VJ32002F00002 1 20010703 A 2421 648843 ALTERNATOR BEECH 33 F33A 1151425 CE CONT O520 IO520B 17032 SO ENGINE INOPERATIVE A VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 5581T 20 CE1350 ALTERNATOR WILL NOT CARE THE LOAD BELOW 1000 RPM. EMITS A NOISE IN THE HEADSET. EMITS A NOISE IN THE HEADSET. ALTERNA TOR SENT THE MFG FOR WARRANTY. 1 L 7 1 3O 3 O 3A15 E5CE 2002013000084 20020130 00084 SO 2002 1 30 VJ32002F00003 2 20011215 A 7314 64621216 PUMP BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO CASE DRAIN LEAKING B VJ3R K NONE K FLUID LOSS IN INSP/MAINT 1 WP 07 1570A 296 CE1333 820467 LEAKING FUEL FROM CASE DRAIN. 1 L 7 1 3O 3 O 3A15 E5CE 2002013000086 20020130 00086 SW 2002 1 30 W1J2002F00000 1 20011114 A 2730 2835YC ACTUATOR GULSTM 690TP 695B 3970610 SW GARRTT TPE331 TPE331* 01514 WP RT ELEVATOR TRIM SEPARATED E W1JR K NONE O OTHER IN INSP/MAINT 1 WP 01 27VE 176 96202 RT ELEVATOR TRIM ACTUATOR/ADAPTOR SEPERATED CAUSING TRIM TAB TO FLUTTER. TRIM TAB CAUSED ELEVATOR TO FLUTTER AND CONTRO L CHANNELS FOR RIGHT ELEVATOR TO CRACK LOSING RIGHT ELEVATOR CONTROL. NO SPECIFIC MM PROCEDURE FOR INSTALLING ACTUATOR/ ADAPTOR CUTTER PIN. 1 H 7 2 4T 3 T RT 2A4 E2WE 2002013000087 20020130 00087 SO 2002 1 30 WD42002F00000 1 20010905 A 2910 LINE PIPER PIPER PA34 PA34200T 7103406 SO CONT O360 TSIO360* 17025 SO HYD SYSTEM WORN A WD4R A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 17 8186R 2306 348070180 AIRCRAFT TOOK OFF AND LANDING GEAR FAILED TO RETRACT FULLY. OPERATOR CYCLED GEAR DOWN AND THE RIGHT MAIN GEAR DOWN LOCK LIGHT FAILED TO ILLUMINATED. THE AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. EVALUATION OF THE SYSTEM REVE ALED A LEAK IN THE UPPER RETRACT LINE IN THE NOSE WELL WHERE THE LINE HAD CHAFED THROUGH ON AN ADEL CLAMP. SUGGEST THAT WHEN INSPECTING THE GEAR SYSTEM LINES THAT CLAMPS ARE REMOVED AND RELOCATED FOR BETTER VISUAL INSPECTION/ ANALYSIS. 1 L 7 2 3O 3 O A7SO E9CE 2002013000088 20020130 00088 SO 2002 1 30 WD42002F00001 1 20010921 A 2910 9515340 TUBE PIPER PA34 PA34200T 7103406 SO CONT O360 LTSIO360EB 17025 SO HYD SYS CORRODED B WD4R A UNSCHED LANDING B K J SMOKE/FUMES/ODORS/SPARKS FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 17 8186R 2306 348070180 312387 SHORTLY AFTER AIRCRAFT DEPARTURE, THE PILOT SMELLED HYDRAULIC FLUID IN COCKPIT. DECISION WAS MADE TO DIVERT BACK TO AIR PORT. WHEN CYCLING GEAR DOWN, AN UNSAFE CONDITION WAS INDICATED AND GEAR WAS PLACED IN DOWN POSITION BY EMERGENCY PROCE DURES AND LANDED WITHOUT INCIDENT. UPON INSPECTION IT WAS DISCOVERED THAT THE TUBE ASSEMBLY IN THE NOSE WELL HAD CORROD ED AT THE FORWARD ATTACH CLAMP AND HAD PRODUCED A HOLE, ALLOWING HYDRAUIC FLUID TO ESCAPE. 1 L 7 2 3O 3 O A7SO E9CE 2002013000090 20020130 00090 SO 2002 1 30 WVBA2001054 1 20011217 A 2750 64126 CONTROL CABLE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA TE FLAPS FAILED A WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 42WP 318252038 DURING MAINTENANCE FOR RIGGING, THE SYSTEM WAS BEING CHECKED FOR FUNCTION. THE RIGHT FLAP WOULD NOT DRIVE DOWN. THE TE CH THEN REMOVED THE CABLE ENDS AT THE MOTOR AND FOUND THE RIGHT CABLE COULD BE EXTRACTED FOR SEVERAL INCHES. THE TRANSM ISSION END ON THE RIGHT SIDE WAS REMOVED AND IT WAS DISCOVERED THAT THE SHAFT ON THE DRIVE COUPLING HAD FAILED. IT APPE ARED THAT IT HAD WORN FROM CONTACT WITH THE CABLE HOUSING. THE CABLE WAS REMOVED AND WILL BE REPLACED. IT WAS SUGGESTE D THAT DURING FLAP CABLE INSTALLATION, SHARP BENDING OF THE CABLE BE AVOIDED. TO PREVENT DRIVE LINK INSIDE CABLE FROM B EING BENT AND CAUSING CHAFFING. NOTE: THE ASYMMETRY SYSTEM DID WORK. 1 L 7 2 3O 3 O A20SO E14EA 2002013000091 20020130 00091 SO 2002 1 30 XGN2002F00000 2 20011231 A 8540 643199 CRANKCASE BEECH 55 D55 1152730 CE CONT O520 IO520C 17032 SO ENGINE CRACKED A XGNA K NONE O OTHER IN INSP/MAINT 1 SW 05 69RP 1415 TE766 555162 HALF CIRCLE CRACKED AT NR 6 CYLINDER PAD. CRACK RUNS FROM UPPER PART OF CRANKCASE FROM CYLINDER BASE STUD AT 2 OCLOCK P OSITION TO CYLINDER BASE STUD AT 10 OCLOCK POSITION. WITH SEVERAL CRACK RADIATING FROM THE HALF CIRCLE CAUSING A SMALL TRIANGULAR PIECE TO FALL OUT. THERE WAS NO OTHER DAMAGE TO ENGINE. CRANKCASE WILL NOT BE REPAIRABLE. 1 L 7 2 3O 3 O 3A16 E5CE 2002013000097 20020130 00097 NE 2002 1 30 2001UALA02412 2 20011215 A 7261 M832481239 PACKING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE A UALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 WP 29 532UA 25072 726545 LEFT ENGINE OIL QUANTITY DECREASED TO 3 QUARTS IN CRUISE. OIL PRESSURE AND TEMPERATURE NORMAL. SUPPLEMENTAL DATA UPDATE OIL FILTER WAS REPLACED AT DEPARTING STATION DUE TO A FILTER BYPASS MESSAGE. AT MSP OIL WAS FOUND LEAKING AT THE OIL FIL TER HOUSING COVER. IT WAS REPORTED THAT THE O-RING WAS DETERMINED TO BE TOO SMALL AND WAS THROWN AWAY. ANOTHER O-RING WA S INSTALLED AND THE ENGINE CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2002013000112 20020130 00112 SO 2002 1 30 2002F00048 1 20011217 A 2421 30086011 GENERATOR EMB 145 EMB145LR 3260212 SO NR 4 MALFUNCTIONED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 828MJ 145218 FLT 5740 - THE CREW ABORTED TAKEOFF DUE TO THE NR 4 GENERATOR OFF BUSS EICAS MESSAGE. THE CAPTAIN RESET THE GENERATOR A ND DEPARTED WITH NO FURTHER PROBLEMS OR OCCURRENCES. (M) 2 L 7 2 4T RT T00011AT 2002013000113 20020130 00113 EA 2002 1 30 2002F00049 1 20011218 A 3350 64641 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77331 7331 FLT 5765 - DURING POST FLIGHT, THE CAPTAIN FOUND THE EMERGENCY FLOOR PATH LIGHTS WOULD NOT GO OUT WHEN HE WALKED ON THE STRIP. MAINTENANCE WAS CALLED OUT AND FOUND A LOOSE CONNECTION TO THE PATH LIGHTS. THE CONNECTOR WAS RESECURED AND NO FURTHER DEFECTS WERE NOTED. (M) 2 L 7 2 4F RT A21EA 2002013000114 20020130 00114 EA 2002 1 30 2002F00050 1 20011219 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN DEFECTIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7305V 7305 FLT 6587 - CMH-BDL - THE CREW FOUND THE EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. MAINTENANCE REPLACED THE CONNECTOR AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2002013000115 20020130 00115 EA 2002 1 30 2002F00051 1 20011224 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27173 7173 WHILE PERFORMING ROUTINE MAINTENANCE, THE CREW FOUND THE NR 3 EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2002013000116 20020130 00116 NM 2002 1 30 2002F00052 1 20011228 A 3350 MS1557081 LIGHT DHAV DHC8 DHC8202 2809007 NM EXTERIOR INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 455YV 455 DURING A ROUTINE CHECK INSPECTION, THE CREW NOTED THE LEFT FORWARD EXTERIOR EGRESS LIGHT WOULD NOT ILLUMINATE. MAINTENA NCE REPLACED THE BULB WITH NO FURTHER DEFECTS NOTED. (M) 2 H 7 2 4T RT A13NM 2002013000117 20020130 00117 EA 2002 1 30 2002F00053 1 20011230 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27314 7314 WHILE PERFORMING ROUTINE MAINTENANCE, THE CREW FOUND THE NR 7 EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2002013000120 20020130 00120 EA 2002 1 30 2002F00056 1 20011123 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77195 7195 FLT 5708 - SDF-PHL - THE CREW FOUND THE LEFT EXTERIOR FUSELAGE AFT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED TH E BURNED OUT LIGHT AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2002013000121 20020130 00121 NM 2002 1 30 2002F00057 1 20011104 A 3411 PITOT LINE BOEING 727 727223 1384074 NM PITOT/STATIC SYS CONTAMINATED A ULHF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 23 707AA 22464 ON REPOSITION FLIGHT DUE TO IMPENDING HURRICANE ON TAKEOFF ROLL. NO CAPTAINS AIR SPEED INDICATION FLUSHED SYSTEM PER MM 34-11-0 PAGE 209 AND PERFORMED OPS CHECK PER MM 34-11-0. OPS CHECK OK. (M) 2 L 7 3 4F A3WE 2002013000122 20020130 00122 NM 2002 1 30 2002F00058 1 20011104 A 3411 PITOT LINE BOEING 727 727223 1384074 NM PITOT/STATIC SYS CONTAMINATED A ULHF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 23 707AA 22464 ON REPOSITION FLIGHT DUE TO IMPENDING HURRICANE ON TAKEOFF ROLL. NO CAPTAINS AIR SPEED INDICATION FLUSHED SYSTEM PER MM 34-11-0 PAGE 209 AND PERFORMED OPS CHECK PER MM 34-11-0. OPS CHECK OK. (M) 2 L 7 3 4F A3WE 2002013000123 20020130 00123 NE 2002 1 30 2002F00059 2 20010917 A 7320 8010003 FMU DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE NR 2 ENGINE DEFECTIVE A WRLA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 11 275WA 48631 ON CLIMB-OUT FROM JFK, NR 2 WAS SHUT DOWN FOR LOW RPM. NO RESTART OF NR 2 ENGINE WAS ATTEMPTED. THE AIRCRAFT WAS POSIT IONING FROM JFK TO XNA FOR A SCHEDULED A-CHECK. REMOVED AND REPLACED NR 2 ENGINE FUEL METERING UNIT. LEAK AND OPERATIO N CHECK GOOD IAW MD-11 MM 73-21-01. (M) 2 L 7 3 4F 4 F RT A22WE E24NE 2002013000124 20020130 00124 2002 1 30 2002F00060 4 20010915 A 3417 HG280D5 ADC DOUG DC10 DC1030F 3023504 WP NR 2 FAULTY A WRLA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 27 626MD 46998 ABORTED TAKEOFF AT 80 KNOTS CALLED BY FIRST OFFICER DUE TO 25 KNOTS AIRSPEED DISCREPANCY BETWEEN FIRST OFFICER AND CAPTA INS AIRSPEED INDICATORS. TAXI BACK TO GATE FIRST OFFICER AIRSPEED INDICATOR READS 70 KNOTS. REMOVED AND REPLACED NR 2 AIR DATA COMPUTER P/N HG280D5, P/N OFFF HG280D5 S/N ON 596, S/N OFF 515. PERFORMED STATIC CHECK, SYSTEM CHECKED OK. (M ) 2 L 7 3 4F RT A22WE 2002013000125 20020130 00125 NM 2002 1 30 2002F00061 1 20011222 A 5320 FLOOR SUPPORT BOEING 757 757236 1384971 NM FUSELAGE CORRODED A N8TA K NONE O OTHER IN INSP/MAINT 1 WP 19 526NA 24794 DURING C-CHECK, L1 DOOR THRESHOLD FLOOR SUPPORT WAS FOUND CORRODED. REPLACED SUPPORT PER SRM. (M) 2 L 7 2 4F RT A2NM 2002013000127 20020130 00127 NE 2002 1 30 2002F00045 2 20011016 A 7230 COMPRESSOR DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE NR 3 ENGINE DAMAGED A WRLA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING E VIBRATION/BUFFET NR NOT REPORTED 1 SO 11 274WA 48633 SHORTLY AFTER ROTATION HEARD LOAD NOISE WITH VIBRATION EGT PEAKED AT 657 DEGREES NR 3 ENGINE. THE ENGINE WAS SHUT DOWN, THE CREW DUMPED EXCESS FUEL AND LANDED THE AIRCRAFT. CHECKED CHIP DETECTORS, ALL NORMAL, BORESCOPED TURBINE SECTION BL ADES NO DAMAGE BORESCOPED COMPLETE COMPRESSOR FOUND SEVERAL BLADES ON SEVERAL STAGES, WITH MISSING PARTS, SOME OUT OF LI MITS (HPC). REMOVED AND REPLACED ENGINE 3 AS PER WORLD MD11 TASK CARD 0104 SERIAL NR OFF P733783. (M) 2 L 7 3 4F 4 F RT A22WE E24NE 2002013000139 20020130 00139 NE 2002 1 30 SIMA200129019 2 20011015 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT LEAKING A SIMA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 268AE 340B268 LGA - FLT 4445 - RIGHT ENGINE LOST OIL AFTER TAKEOFF AND RETURNED TO LGA. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 2002013100001 20020131 00001 NM 2002 1 31 USAA011366 1 20011104 A 5320 INTERCOSTAL BOEING 767 767201 1385125 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 650US 57659 23902 CLT - FOUND INTERCOSTAL WEB CRACKED 3 INCHES, STATION 764 RBL 73. FABRICATED AND INSTALLED WEB PER EO 5399T503. (M) 2 L 7 2 4F RT A1NM 2002013100002 20020131 00002 NM 2002 1 31 USAA011367 1 20011104 A 5320 ANGLE BOEING 767 767201 1385125 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 650US 57659 23902 CLT - FOUND ANGLE CRACKED 1 INCH, STATION 764, LBL 73. REPLACED BRACKET AND INSTALLED STRAP PER EO 5399T503. (M) 2 L 7 2 4F RT A1NM 2002013100003 20020131 00003 NM 2002 1 31 USAA011368 1 20011112 A 5320 FLOOR SUPPORT BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 608AU 54705 22204 CLT - FOUND FLOOR SUPPORT CORRODED 14 INCHES, STATION 358-364. INSTALLED NEW FLOOR SUPPORT ASSY PER SRM 51-40-02. (M) 2 L 7 2 4F RT A2NM 2002013100004 20020131 00004 NM 2002 1 31 USAA011369 1 20011022 A 5311 FRAME BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 55127 22199 CLT - FOUND FRAME CORRODED, STATION 1300, RBL 4 LOWER CHORD ANGLE. FABRICATED AND INSTALLED NEW SHEAR TIE PER SRM 51-40 -02. (M) 2 L 7 2 4F RT A2NM 2002013100005 20020131 00005 NM 2002 1 31 USAA011373 1 20011119 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 385US 47062 22958 PIT - FOUND SKIN CRACKED .045 INCH DEEP, 3 INCHES LONG BY 2 INCHES WIDE, STATION 420 43 INCHES FORWARD OF CARGO BETWEEN 22R AND 23R. DOUBLER INSTALLED PER SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2002013100006 20020131 00006 NM 2002 1 31 USAA011374 1 20011026 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 385US 47062 22958 PIT - FOUND FRAME CRACKED 2 INCHES, AT STATION 847 BETWEEN STRINGER 8L-9L. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2002013100007 20020131 00007 NM 2002 1 31 USAA011375 1 20011119 A 5320 WEB BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 385US 47062 22958 PIT - FOUND DOOR REINFORCING WEB CRACKED 1 INCH, STATION 921, 1 INCH BELOW S11R IN DOOR REINFORCING WEB. REPAIR DOUBLER INSTALLED PER SRM 51-70-13 AND EA 72800. (M) 2 L 7 2 4F RT A16WE 2002013100008 20020131 00008 NM 2002 1 31 USAA011376 1 20011119 A 5730 SKIN BOEING 737 7373B7 1384580 NM LT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 385US 47062 22958 PIT - FOUND SKIN CRACKED .5 INCH HOLE, LEFT UPPER WING T/E JUST OUTBOARD OF AILERON. REPLACED PANEL PER SRM 57-51-01 AN D EA 72942. (M) 2 L 7 2 4F RT A16WE 2002013100009 20020131 00009 NM 2002 1 31 USAA011377 1 20011105 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 385US 47062 22958 PIT - FOUND SKIN CRACKED 1.5 INCH, STATION 952 STRINGER 11L. INSTALLED DOUBLER PER EA 72801. (M) 2 L 7 2 4F RT A16WE 2002013100010 20020131 00010 NM 2002 1 31 USAA011378 1 20011126 A 5311 FRAME BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 608AU 54705 22204 CLT - FOUND .5 INCH CRACK, FS 680 S23L ON FRAME. INSTALLED DOUBLER. (M) 2 L 7 2 4F RT A2NM 2002013100011 20020131 00011 NM 2002 1 31 USAA011387 1 20011116 A 5210 SKIN BOEING 737 737401 1384701 NM PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 23882 TPA - FOUND SKIN .250 INCH, UPPER HINGE CUTOUT ON MAIN ENTRY DOOR. INSTALLED DOUBLER PER SB 737-52-1096 ALSO EA NR 9424 8. (M) 2 L 7 2 4F RT A16WE 2002013100012 20020131 00012 NM 2002 1 31 USAA011388 1 20011203 A 5320 1123765 ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 23312 PIT - FOUND MED JAMB WEB ANGLE CRACKED 2 INCH, STRINGER 10L STATION 303.9. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-20-01, 51-40-00, 51-10-02. (M) 2 L 7 2 4F RT A16WE 2002013100013 20020131 00013 NM 2002 1 31 USAA011389 1 20011203 A 5313 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 46642 23312 PIT - FOUND STRINGER CRACKED 1.5 INCH STRINGER 5L AT FRAME JUNCTION STATION 380. DOUBLER INSTALLED PER SRM 53-00-03. ( M) 2 L 7 2 4F RT A16WE 2002013100014 20020131 00014 NM 2002 1 31 USAA011390 1 20011203 A 5320 INTERCOSTAL BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 23312 PIT - FOUND INTERCOSTAL 1 SQUARE INCH, FORWARD END OF INTERCOSTAL 525L, BS 947. CLEANED AND TREATED PER SRM 51-20-01. (M) 2 L 7 2 4F RT A16WE 2002013100015 20020131 00015 NM 2002 1 31 USAA011391 1 20011207 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 23231 TPA - FOUND SKIN CRACKED .5 INCH, APPROXIMATE STATION 960 BETWEEN STRINGER 14 AND 15 RIGHT. REPAIRED FOB DOUBLER, FILLE R, TRIPLER, FASTENERS FRO SRM 53-60-01 FIG 207. (M) 2 L 7 2 4F RT A16WE 2002013100016 20020131 00016 NM 2002 1 31 USAA011392 1 20011211 A 5320 FITTING BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 46647 23312 PIT - FOUND FITTING CRACKED .75 INCH, L ANGLE TOP CENTER FITTING STATION 312 (RS) FORWARD SERVICE DOOR. INSTALLED DOUBL ER STRAP PER 51-40-02 AND 51-40-03. (M) 2 L 7 2 4F RT A16WE 2002013100017 20020131 00017 NM 2002 1 31 USAA011393 1 20011217 A 5540 STRUCTURE BOEING 737 737301 1384611 NM RUDDER DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 46642 23228 PIT - FOUND RUDDER DAMAGED, NR 7 HINGE AREA RSTA 225-235 LEADING EDGE. PER SRM 51-70-17 2 EXTRA PLIES WITH HALF OVERLAP PER EA 73066. (M) 2 L 7 2 4F RT A16WE 2002013100018 20020131 00018 NM 2002 1 31 USAA011394 1 20011217 A 5540 STRUCTURE BOEING 737 737301 1384611 NM RUDDER DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 46642 23228 PIT - FOUND RUDDER 8 INCH BY .750 INCH GOUGED, CLOSE TO T/E WEDGE BETWEEN R STA 121164 AND 174.12. REPAIRED PER SRM 51- 70-17 WITH 2 EXTRA PILES WITH .5 OVERLAP PER EA 73065. (M) 2 L 7 2 4F RT A16WE 2002013100019 20020131 00019 NM 2002 1 31 USAA011395 1 20011217 A 5542 SKIN BOEING 737 737301 1384611 NM RUDDER DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 23228 PIT - FOUND RUDDER SCREW PULLED THROUGH SKIN, LEFT SKIN PANEL AT R STATION 225 APPROXIMATELY. TWO EXTRA REPAIR PLIES WI TH .5 INCH PER PLY OVERLAP PER EA 73064. (M) 2 L 7 2 4F RT A16WE 2002013100020 20020131 00020 NM 2002 1 31 USAA011396 1 20011219 A 5320 6545834525 INTERCOSTAL BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 46642 23312 PIT - INTERCOSTAL CRACKED.125 INCH, CABIN FLOOR STATION 344 BL 0 FLOORBEAM AT STATION 344. DRILLED AND INSTALLED 525 IN TERCOSTAL (NEW PART) PER SRM 51-10-2 AND 53-10-51. (M) 2 L 7 2 4F RT A16WE 2002013100021 20020131 00021 NM 2002 1 31 USAA011397 1 20011219 A 5320 INTERCOSTAL BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 46642 23312 PIT - FOUND INTERCOSTAL .125 INCH CRACKED, CABIN FLOOR INTERCOSTAL STATION 344 LBL 12. FABRICATED AND INSTALLED PER SRM 51-10-1 AND 53-10-51. (M) 2 L 7 2 4F RT A16WE 2002013100022 20020131 00022 NM 2002 1 31 USAA011398 1 20011220 A 5542 SKIN BOEING 737 7374B7 1384702 NM RUDDER CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 775AU 31465 24933 PIT - FOUND RUDDER CRACKED, LESS THAN .5 INCH BY .5 INCH BY 6 INCHES, T/E 1 FT ABOVE TOP OF BALANCE WT STA 141.52. REMO VE CORE AND INSTALLED NEW HONEY CONE AND 2 LAYERS OF FABRIC PER SRM 55-40-01 AND 41-70-04. (M) 2 L 7 2 4F RT A16WE 2002013100024 20020131 00024 NM 2002 1 31 USAA011404 1 20011030 A 5320 BEAM BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 445US 24863 PIT - FOUND BEAM CRACKED .5 INCH, STATION 747 LOWER OVERHEAD COMPT ATTACH POINT LEFT SIDE. INSTALLED DOUBLER PER TYP RE PAIR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2002013100025 20020131 00025 NM 2002 1 31 USAA011405 1 20011128 A 5414 SKIN BOEING 737 7373B7 1384580 NM NR 1 PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 46642 23312 PIT - FOUND PYLON SKIN CRACKED .75 INCH, NR 1 ENGINE PYLON UPPER SKIN STRUCTURE AT ACCESS PANEL. STOP DRILLED AND INSTA LLED DOUBLER PER TYP REPAIR 54-30-07. (M) 2 L 7 2 4F RT A16WE 2002013100027 20020131 00027 NM 2002 1 31 USAA011406 1 20011121 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 46642 23312 PIT - FOUND FRAME .5 INCH CRACK, STATION 663.75 AT STRINGER 1 CUTOUT RIGHT SIDE. REPAIR ANGLE AND STRINGER SPLICE PER S RM 53-00-07. (M) 2 L 7 2 4F RT A16WE 2002013100028 20020131 00028 NM 2002 1 31 USAA011407 1 20011102 A 5311 BELTFRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 445US 24863 PIT - FOUND BELTFRAME .5 INCH LONG CRACK, AFT SIDE OF FRAME AT STATION 867 BETWEEN STRINGER 8R AND 9R. INSTALLED REPAIR DOUBLER PER TYP REPAIR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2002013100033 20020131 00033 NM 2002 1 31 USAA011408 1 20011221 A 5320 INTERCOSTAL BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 46642 23312 PIT - FOUND INTERCOSTAL PLATE WITH 1 INCH CRACK, AFT OF RT FRAME 947 AND STRINGER 11R. INSTALLED DOUBLER PER SRM 51-70- 13. (M) 2 L 7 2 4F RT A16WE 2002013100034 20020131 00034 2002 1 31 USAABA01016 4 20011130 A 2565 7A1539114 SLIDE AIRBUS 330 A330323 3930335 EU R2 DOOR MALFUNCTIONED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 673UW 0337 PHL - DURING AN OPERATIONAL TEST OF THE R2 DOOR SLIDE, THE SLIDE DID NOT FREE ITSELF FROM THE SHELL AND DID NOT INFLATE AUTOMATICALLY. ONCE MAINTENANCE PERSONNEL JOSTLED THE SLIDE, THE SHELL FELL AWAY AND THE SLIDE INFLATED NORMALLY AND HE LD PRESSURE. NO DEFICIENCIES WERE FOUND WITH THE SLIDE. ON TWO OTHER AIRCRAFT, THE SLIDES IN THE R2 DOOR POSITION WERE TESTED AND PERFORMED WITHOUT ANY PROBLEM. (M) 2 L 7 2 4F RT A46NM 2002013100035 20020131 00035 EU 2002 1 31 USAABA01017 1 20011204 A 3350 32146220 POWER SUPPLY AIRBUS 330 A330323 3930335 EU L3 & R3 DOOR FAULTY A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 671UW 0323 PHL - FOUND FAULTY EPSU'S AT THE L3 AND R3 DOORS. MAINTENANCE REPLACED THE EPSU'S. (M) 2 L 7 2 4F RT A46NM 2002013100036 20020131 00036 EU 2002 1 31 USAABA01018 1 20011205 A 3350 321430 BATTERY AIRBUS 330 A330323 3930335 EU CABIN FAULTY A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 674UW 0342 PHL - FOUND THE L3, R3, L2, R1 AND L1 DOORS EMERGENCY LIGHT BATTERIES FAULTY. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A46NM 2002013100038 20020131 00038 NM 2002 1 31 USAABB011146 1 20011219 A 3350 86210066 BATTERY PACK BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 616AU 27147 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 23 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) 2 L 7 2 4F RT A2NM 2002013100039 20020131 00039 NM 2002 1 31 USAABB01123 1 20011110 A 2913 6506606 PUMP BOEING 767 7672B7 1385107 NM LT ENGINE OVERHEATED A USAA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION NR NOT REPORTED 1 EA 19 653US 24894 PHL - FLT 1268 - EN ROUTE PHL-SJU, CREW RECEIVED THE EICAS MESSAGE L PRIM HYD OVERHEAT' AND THE ASSOCIATED 'OVHT' LIGHT. CREW DEACTIVATED THE PUMP AND THE LIGHT EXTINGUISHED. FLIGHT RETURNED TO PHL AND LANDED WITH NO FURTHER INCIDENT. MA INTENANCE REPLACED THE LEFT ENGINE DRIVEN PUMP. (M) 2 L 7 2 4F RT A1NM 2002013100040 20020131 00040 NM 2002 1 31 USAABB01124 1 20011111 A 5210 140N275411 MECHANISM BOEING 757 757225 1384959 NM R1 DOOR BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 22198 PIT - CREW UNABLE TO DISARM THE R1 DOOR. MAINTENANCE REPLACED THE LIFTING MECHANISM. (M) 2 L 7 2 4F RT A2NM 2002013100041 20020131 00041 NM 2002 1 31 USAABB01135 1 20011126 A 3320 5200000041 SOCKET BOEING 757 7572B7 1384964 NM CABIN SHORTED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 621AU 27200 CLT - ELECTRICAL SMELL IN CABIN NEAR ROW 29. MAINTENANCE FOUND THE CEILING LIGHTS SHORTED OUT AND REPLACED THE LIGHT SO CKET. (M) 2 L 7 2 4F RT A2NM 2002013100044 20020131 00044 NM 2002 1 31 USA2001F00007 1 20011212 A 3350 30043231 SOCKET BOEING 737 737301 1384611 NM CABIN DEFECTIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 349US 23552 PIT MAINTENANCE FOUND THE FORWARD SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SOCKET ASSEMBLY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2002013100045 20020131 00045 EU 2002 1 31 USA2002F00000 1 20011202 A 5240 HANDLE AIRBUS A319 A319112 3930323 EU SERVICE DOOR LACK OF LUBE A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 743UW 1277 THE AFT RIGHT SERVICE DOOR WOULD NOT OPEN. MAINTENANCE LUBRICATED THE EXTERIOR HANDLE MECHANISM. OPERATIONALLY CHECKS NORMAL DURING OPENING AND CLOSING OF THE DOOR, FROM THE INSIDE AND OUTSIDE OF THE AIRCRAFT. 2 L 7 2 4F RT A28NM 2002013100046 20020131 00046 NM 2002 1 31 USAABB01137 1 20011202 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 607AU 22203 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE AT ROWS 4, 6 AND 13. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2002013100047 20020131 00047 NM 2002 1 31 USAABB01138 1 20011130 A 3610 32896265 VALVE BOEING 757 7572B7 1384964 NM LT ENGINE FAILED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 626AU 27303 PIT - FLT 1570 - IN CRUISE, CREW NOTED THAT THE LEFT DUCT PRESSURE WAS LOW (10 PSI). CABIN CREW ALSO NOTED A SLIGHT BUR NING SMELL. MAINTENANCE REPLACED THE LEFT FAN AIR MODULATING VALVE. (M) 2 L 7 2 4F RT A2NM 2002013100049 20020131 00049 2002 1 31 USAABB01139 4 20011202 A 3460 4052500962 FMC BOEING 767 7672B7 1385107 NM E/E BAY FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 651US 41871 24764 PHL - FLT 42 - EN ROUTE PHL-AMS, CREW NOTED THAT THE RIGHT FMC HAD FAILED. FLIGHT RETURNED TO PHL. MAINTENANCE REPLACE D THE FMC. (M) 2 L 7 2 4F RT A1NM 2002013100050 20020131 00050 NM 2002 1 31 USAABB01140 1 20011203 A 3350 8731002511REV14 SIGN BOEING 757 7572B7 1384964 NM R1 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 628AU 27806 MCO - FOUND R1 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE IDENTIFIER ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2002013100051 20020131 00051 NM 2002 1 31 USAABB01142 1 20011210 A 3350 9221009 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 602AU 22196 BDL - FOUND L3 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2002013100052 20020131 00052 2002 1 31 AALA20011850 4 20011009 A 2210 AUTOPILOT SYS AIRBUS 300 A300B4605R 3930308 EU COCKPIT MALFUNCTIONED A AALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 21 70073 516 LHR - EXTENSIVE VIBRATION IN CONTROL COLUMN FORE AND AFT IN CLIMB-OUT FOR A SHORT PERIOD AND FOR AN EXTENDED PERIOD IN C RUISE. FOUND THE NR 1 AUTO PILOT TO BE AT FAULT. (M) 2 L 7 2 4F RT A35EU 2002013100053 20020131 00053 NM 2002 1 31 USAABB01119 1 20011108 A 2761 60231002 SQUIB BOEING 767 7672B7 1385107 NM RT WING FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 653US 24894 PHL - RIGHT OVERWING SPOILER OVERRIDE ACTUATOR (SQUIB) DID NOT TEST. MAINTENANCE REPLACED THE SQUIB. (M) 2 L 7 2 4F RT A1NM 2002013100054 20020131 00054 NM 2002 1 31 USAABB01143 1 20011208 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 617AU 27148 PHL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 33 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2002013100055 20020131 00055 NM 2002 1 31 USAABB01144 1 20011210 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 623AU 27244 MCO - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 4, 13 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2002013100056 20020131 00056 NM 2002 1 31 USAABB01145 1 20011218 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 607AU 22203 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 18 AND 29 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2002013100057 20020131 00057 NM 2002 1 31 USAABB01147 1 20011219 A 3350 9221009 BATTERY PACK BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 616AU 27147 BDL - FOUND EXIT IDENTIFIER AT R3 DOOR INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) 2 L 7 2 4F RT A2NM 2002013100058 20020131 00058 NM 2002 1 31 USAABB01148 1 20011220 A 3350 9221009 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 625VJ 27246 BOS - FOUND EXIT IDENTIFIER FOR THE L1 DOOR INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2002020100015 20020201 00015 NM 2002 2 1 150070 1 20011213 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED B K NONE O OTHER IN INSP/MAINT 1 SO 15 54SW 70292 21535 FUSELAGE SKIN IS CRACKED AT STA 800 STRINGER 22 LT. CRACK IS 2.6 INCH IN LENGTH. 2 L 7 2 4F A16WE 2002020100016 20020201 00016 NE 2002 2 1 2001UALA02238 2 20011108 A 7200 8198021 ACTUATOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 2 ENGINE SEIZED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 WP 29 767UA 2258 26918 777016 AIRCRAFT DIVERTED INTO SLC DUE TO NR 2 ENGINE OSCILLATING. N1 AND N2 DROPPED TO IDLE WITH EGT INCREASING; EGT 570 DEG. E NGINE SHUT DOWN BY FLT CREW. SUPPLEMENTAL DATA UPDATE RIGHT ENGINE SURGED FOLLOWED BY "ENG FAIL" MESSAGE. MAINTENANCE T ESTED THE COMPRESSOR VARIABLE VANE SYSTEM AND FOUND SYMPTOMS OF STATOR VANE ACTUATOR (SVA) FAILURE. THE SVA WAS REPLACE D, ENGINE PASSED ALL INSPECTIONS AND RUN-UPS AND WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002020100019 20020201 00019 NM 2002 2 1 2001UALA02444 1 20011220 A 3241 TRANSDUCER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE MLG ANTI SKID MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 377UA 24642 PLANE DIVERTED TO LAX DUE TO ANTISKID PROBLEM, AND SHORT RUNWAYS AT BUR. SUPPLEMENTAL DATA UPDATE REPLACED LEFT MLG INB OARD ANTI-SKID TRANSDUCER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002020100023 20020201 00023 NE 2002 2 1 2002UALA00036 2 20011231 A 7261 LINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE LOOSE A UALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 548UA 25396 727193 LEFT ENGINE REQUIRED 12 QUARTS OF OIL. SUPPLEMENTAL DATA UPDATE FOUND OIL PRESSURE TRANSMITTER LINE B-NUT EXTREMLY LOOS E, AND OIL LEAKING FROM IT ON DRY MOTOR. SECURED LINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002020100038 20020201 00038 NM 2002 2 1 USAABB01152 1 20011128 A 3350 873100151REV12 LIGHT BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 603AU 22198 PHL - MAINTENANCE FOUND THE EMERGENCY ESCAPE AISLE LIGHT, AT SEAT ROW 29, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE AISLE LIGHT ASSEMBLY AT SEAT ROW 29. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2002020100039 20020201 00039 NM 2002 2 1 USAABB01153 1 20011228 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 603AU 22198 PHL - FOUND ALL FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2002020100040 20020201 00040 NM 2002 2 1 USAABB01154 1 20011229 A 3350 86210066 LIGHT BOEING 757 7572B7 1384964 NM CABIN MALFUNCTIONED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 627AU 27805 MCO - FLOOR LEVEL EMERGENCY LIGHT AT ROW 1 REMAINED ILLUMINATED. MAINTENANCE CHECKED THE SYSTEM AND COULD NOT DUPLICATE THE DISCREPANCY. REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2002020100041 20020201 00041 WP 2002 2 1 USAAD01184 1 20011129 A 3350 AD4002P BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 811US 48043 PIT - THE FORWARD OVERWING EXIT LIGHTS DID NOT ILLUMINATE WHEN THE AIRCRAFT POWER DROPPED OFF. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY. (M) 2 L 7 2 4F A6WE 2002020100042 20020201 00042 WP 2002 2 1 USAAD01187 1 20011208 A 3350 873100191 RECEIVER DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 817US 48097 PIT - THE CATWALK EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT RECEIVER. (M) 2 L 7 2 4F A6WE 2002020100043 20020201 00043 WP 2002 2 1 USAAD01188 1 20011211 A 3350 8721055 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 822US 49139 IND - THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS WERE DIM AND THE TAIL CONE REMOTE RECEIVER WAS INOPERATIVE. MAINTENAN CE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES AND THE TAIL CONE REMOTE RECEIVER. (M) 2 L 7 2 4F A6WE 2002020100044 20020201 00044 WP 2002 2 1 USAAD01189 1 20011212 A 3350 873100272 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 817US 48097 IND - THE MAIN ENTRY EMERGENCY LIGHT AND THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPL ACED THE MAIN ENTRY EMERGENCY LIGHT ASSEMBLY AND THE LOW LEVEL EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2002020100074 20020201 00074 WP 2002 2 1 USAAD01190 1 20011216 A 3350 9721055 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 830US 49443 BOS - THE PASSENGER SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2002020100075 20020201 00075 WP 2002 2 1 USAAD01191 1 20011216 A 2120 ODOR DOUG DC9 DC982 3022082 WP CABIBN DETECTED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 817US 48097 ORD - PIT - FLT 1194 - THERE WAS A STRONG RUBBER SMELL IN THE AIRCRAFT DURING TAKEOFF. THE SMELL DISAPPEARED SHORTLY AF TER GEAR RETRACTION. MAINTENANCE NOTICED A SLIGHT TIRE RUBBER SMELL IN THE MAIN WHEEL WELLS. THE CONDITION OF THE MAIN WHEEL WELLS AND TIRES WERE CHECK, NO DEFECTS WERE NOTED. THE AIR CONDITIONING PACKS WERE OPERATED BUT COULD NOT DUPLIC ATE ODORS. (M) 2 L 7 2 4F A6WE 2002020100076 20020201 00076 WP 2002 2 1 USAAD01193 1 20011227 A 2761 1040T1005 ACTUATOR DOUG DC9 DC982 3022082 WP SPOILER FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 816US 53841 48096 PHL-RSW - FLT 415 - DURING CLIMB-OUT, SMOKE POURED OUT OF THE RUDDER WELL OF THE FIRST OFFICERS SIDE. THE AIRCRAFT RETU RNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE SPOILER AUTOMATIC ACTUATOR AND COMPLETED AN OVE RWEIGHT LANDING INSPECTION. (M) 2 L 7 2 4F A6WE 2002020100077 20020201 00077 WP 2002 2 1 USAAD02001 1 20010104 A 3350 AD4002P BATTERY DOUG DC9 DC981 3022081 WP FWD ENTRY DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 812US 48092 BOS - THE FORWARD ENTRY DOOR PORTABLE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY . (M) 2 L 7 2 4F A6WE 2002020100078 20020201 00078 EU 2002 2 1 USAAF01084 1 20011121 A 3260 WARNING SYSTEM FOKKER F28 F28MK0100 4990807 EU COCKPIT MALFUNCTIONED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 898US 11398 CMH-PHL - FLT 1147 - AFTER TAKEOFF AND LANDING GEAR RETRACTION, THE CREW RECEIVED A LEFT MLG FAULT DISPLAY ON THE MFDU. THE LANDING GEAR WAS CYCLED BUT THE INTRANSIT LIGHT REMAINED ILLUMINATED AND THE 'MAX AIRSPEED 220 KTS' MESSAGE REMAINE D ON THE MFDU. THE CAPTAIN AND DISPATCHED AGREED TO DIVERT TO PIT RATHER THAN TO CONTINUE TO WITH THE SPEED RESTRICTION . THE FLIGHT LANDED AT PIT WITHOUT INCIDENT. MX JACKED THE AIRCRAFT AND SWUNG THE GEAR SEVERAL TIMES, NO FAULTS WERE F OUND. (M) 2 L 7 2 4F RT 2002020100079 20020201 00079 WP 2002 2 1 USAAF01086 1 20011214 A 3350 6040681 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 822US 49139 ORF - THE FORWARD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 2002020100080 20020201 00080 EU 2002 2 1 USAAF01087 1 20011223 A 2120 ODOR FOKKER F28 F28MK0100 4990807 EU CABIN DETECTED A USAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 EA 19 857US 11289 ILM-CLT - FLT 1546 - DURING CLIMB-OUT THERE WERE STRONG FUMES IN THE CABIN AND THE LAV SMOKE DETECTORS SOUNDED. THE AIR CRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE APU, AIR CONDITIONING PACKS, AND ENG INES. NO ABNORMAL INDICATIONS. ISOLATED EACH SYSTEM INDEPENDENTLY WITH PACK/BLEED SYSTEM. NO NOXIOUS SMELL NOTED. (M ) 2 L 7 2 4F RT 2002020100081 20020201 00081 EU 2002 2 1 USAAF01088 1 20011223 A 2421 740508 IDG FOKKER F28 F28MK0100 4990807 EU RT ENGINGE FAILED A USAA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 EA 19 883US 21250 11337 ABE - PIT - FLT 1660 - DURING ROTATION THE RIGHT ENGINE GENERATOR FAULTED. RESET DID NOT FIX. THE APU FAULTED AFTER RU NNING NORMALLY. THE AIRCRAFT RETURNED TO ABE AND LANDED WITHOUT INCIDENT. MAINTENANCE PLACED THE RIGHT ENGINE GENERATO R ON MEL. THE APU STARTED ON THE GROUND AND RAN NORMALLY. LATER MAINTENANCE REPLACED RIGHT ENGINE IDG. (M) 2 L 7 2 4F RT 2002020100082 20020201 00082 EU 2002 2 1 USAAF01089 1 20011223 A 4920 APU FOKKER F28 F28MK0100 4990807 EU APU BAY MALFUNCTIONED A USAA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 EA 19 883US 11337 ABE-PIT - FLT 1660 - AFTER TAKEOFF, THE APU FAULTED WITH THE RIGHT ENGINE GENERATOR ON MEL. THE AIRCRAFT RETURNED TO TH E FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE IDG AND PLACED THE APU ON MEL. (M) 2 L 7 2 4F RT 2002020100083 20020201 00083 EU 2002 2 1 USAAF01090 1 20011228 A 3350 2LA00538100 LIGHT FOKKER F28 F28MK0100 4990807 EU EXTERIOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 882US 11334 PIT - THE RIGHT FAIRING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT 2002020100084 20020201 00084 EU 2002 2 1 USAASA01061 1 20011123 A 2120 ODOR AIRBUS 320 A320214 3930316 EU CABIN DETECTED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 19 117UW 1224 DEN - FLT 133 - EN ROUTE PIT-DEN. DURING APPROACH, THE FLIGHT ATTENDANTS NOTED A BURNING SMELL IN THE FORWARD GALLEY, W ITH ALL OVENS OFF. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RESET THE POPPED CIRCUIT BREAKER FOR THE PO TABLE WASTE WATER HEATER. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2002020100085 20020201 00085 2002 2 1 USAASA01062 4 20011124 A 2565 D31517113 SLIDE AIRBUS A321 A321211 3930370 EU CABIN UNSERVICEABLE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 176UW 1976 1499 LGA - THE AFT LEFT SLIDE PRESSURE WAS OUT OF THE GREEN BAND. MAINTENANCE REPLACED THE AFT LEFT SLIDE ASSEMBLY. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2002020100086 20020201 00086 EU 2002 2 1 USAASA01063 1 20011126 A 3350 CONNECTOR AIRBUS A321 A321211 3930370 EU CABIN DIRTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 177US 1517 PHL - THE EMERGENCY LIGHTS FAILED THE OPERATIONAL CHECK DURING INSPECTION. MAINTENANCE PERFORMED INDIVIDUAL BITE TESTS, AND CLEANED AND RESET THE CANNON PLUGS OF ALL EMERGENCY POWER SUPPLY UNITS. THE EMERGENCY LIGHT TEST WAS PERFORMED AGA IN AND THE SYSTEM WAS FOUND TO OPERATE NORMALLY. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2002020100087 20020201 00087 EU 2002 2 1 USAASA01065 1 20011126 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319112 3930323 EU CABIN FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 768US 1389 CLT - RECEIVED EMERGENCY POWER SUPPLY UNIT 'INT LOAD EMERGENCY R' MESSAGE DURING THE EMERGENCY LIGHTS OPERATIONAL CHECK. MAINTENANCE REPLACED THE RIGHT EMERGENCY POWER SUPPLY UNIT (12WL). THE SYSTEM CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2002020100088 20020201 00088 EU 2002 2 1 USAASA01066 1 20011201 A 3350 CONNECTOR AIRBUS A319 A319112 3930323 EU CABIN LOOSE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 729US 1170 PHL - THE EMERGENCY LIGHT ON SEAT 8C WAS FOUND INOPERATIVE. MAINTENANCE SECURED A CANNON PLUG ON THE FLOORBOARD. OPERA TIONALLY CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2002020100089 20020201 00089 EU 2002 2 1 USAASA01068 1 20011221 A 5210 D5211009820000 CAM AIRBUS 320 A320214 3930316 EU L1 DOOR BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 103US 0861 BOS - L1 DOOR ARMING CAM BROKE. MAINTENANCE REPLACED THE CAM. SMELL PIECE FELL FROM MAIN ENTRY DOOR. REPLACED DOOR HO OK. OPS OK. (M) 2 L 7 2 4F RT A28NM 2002020100090 20020201 00090 2002 2 1 USAASA01073 4 20011231 A 2565 60592101 BOTTLE AIRBUS 320 A320214 3930316 EU SLIDE LOW A USAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 19 114UW 1148 CLT - FLT 61 EN ROUTE CLT-LGA, DURING PUSHBACK, A CABIN INTERCOMMUNICATION DATA SYSTEM WARNING CAME ON FOR AN OVERWING S LIDE BOTTLE. FLIGHT PUSHED BACK TO GATE. MAINTENANCE REPLACED THE LEFT OVERWING ESCAPE SLIDE BOTTLE. SYSTEM CHECKS GO OD. (M) 2 L 7 2 4F RT A28NM 2002020100091 20020201 00091 NM 2002 2 1 2002F00064 1 20010817 A 3350 86210144 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROWS 8 AND 12 INOPERATIVE. REMOVED AND REPLACED REMOTE A SSEMBLY RECEIVERS AND BATTERIES. LIGHTS TESTED NORMAL. REF ASAA0110557. (M) 2 L 7 2 4F RT A16WE 2002020100095 20020201 00095 NM 2002 2 1 ASAA0110557 1 20010817 A 3350 883200312 RECEIVER BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROWS 8 AND 12 INOPERATIVE. REMOVED AND REPLACED REMOTE A SSEMBLY RECEIVERS AND BATTERIES. LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002020100096 20020201 00096 NM 2002 2 1 ASAA0110575 1 20010912 A 3350 90052 BATTERY PACK BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING PREFLIGHT CHECK, EMERGENCY LIGHT ON PASSENGER BULKHEAD INOPERATIVE. REPLACED BATTERY PACK WITH SERVICEABLE PACK. ASSOCIATED LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2002020100097 20020201 00097 NM 2002 2 1 ASAA0110576 1 20010914 A 3350 883200312 RECEIVER BOEING 737 7372Q8C 138448S NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 ANC - DURING SCHEDULED MAINTENANCE CHECK, FOUND FLOOR TRACK LIGHTING AT SEAT PALLET 9 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY RECEIVER THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F A16WE 2002020400015 20020204 00015 WP 2002 2 4 AJ62002F00000 2 20010820 A 7261 3075541 TUBE HAWKER BAE125 BAE125700B 7450007 EU GARRTT TFE731 TFE7313R1H 29001 WP SCAVENGE PUMP CRACKED E AJ6A E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 GL 23 900JT 10994 656 P84335 30 MINUTES INTO A FLIGHT A LOW OIL PRESSURE WARNING CAME ON. THE PILOT PERFORMED A PRECAUTIONARY IN FLIGHT SHUTDOWN AND RETURNED TO HOME BASE, LANDING WITHOUT INCIDENT. THE AFT BEARING SCAVENGE TUBE WAS FOUND TO HAVE CRACKED AND DEPLETED THE OIL TO AN UNACCEPTABLE LEVEL. THE SCAVENGE LINE WAS REPLACED AND THE ENGINE GROUND RUN AND RETURNED TO SERVICE. TH E CRACK MOST LIKELY RESULTED FROM UNDO STRESS APPLIED TO THE LINE DURING AN UNRELATED MAINTENANCE ACTION. THE AGE AND B RITTLENESS OF THE LINE MAY HAVE BEEN A CONTRIBUTING FACTOR. 2 L 7 2 4F 4 F RT A3EU E6WE 2002020400016 20020204 00016 EU 2002 2 4 AJC2002F00000 1 20010326 A 5280 HINGE ISRAEL 1121 1121A 0142006 EU GARRTT TFE731 TFE731* 01518 WP LT MLG DOOR BROKEN E AJCA K NONE O OTHER IN INSP/MAINT 1 EA 25 387PA 25 LEFT MAIN LANDING GEAR DOOR SEPARATED DURING FLIGHT AT AFT GEAR DOOR HINGE PIN. 2 M 7 2 4J 4 F A2SW E6WE 2002020400019 20020204 00019 NE 2002 2 4 AT0200003 2 20011206 A 7260 GEARBOX BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE NR 1 ENGINE FAILED A ZZDA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SO 15 968AT 55029 MASTER CAUTION ILLUMINATED. FOLLOW BY A/C YAW AT 33,000. LEFT ENGINE SHUT DOWN (AUTO) SUDDENLY. RED BOXED NUMBERS WER E VISIBLE. OIL PRESSURE AND OIL FILTER LEVEL 2 ALERTS WERE ALSO NOTED. CHECKLIST WERE ACCOMPLISHED FOR ENGINE FAILURE (FIRE BOTTLE WAS NOT DISCHARGED) AND THE A/C LANDED WITH LEFT ENGINE SHUTDOWN, WITH NO FURTHER PROBLEMS. (MX SAID IT WA S GEARBOX FAILURE.) CORRECTIVE ACTION: REMOVED AND REPLACED NR 1 ENGINE. 2 L 7 2 4F 4 F TR A6WE E00061EN 2002020400020 20020204 00020 WP 2002 2 4 AT0200004 1 20010529 A 2612 TFC120055101 WARNING SYSTEM DOUG DC9 DC932 3022066 WP CARGO FIRE MALFUNCTIONED A ZZDA O OTHER N FALSE WARNING DE DESCENT 1 SO 15 824AT 47278 CARGO FIRE WARNING TONE SOUNDED WITH MASTER WARNING LIGHT ON DESCENT IN ATL. CONDITION WAS INTERMITTENT, SOUNDED TWICE WAS UNABLE TO DETERMINE WHICH LOOP. CORRECTIVE ACTION: REMOVED AND REPLACED FIRE TEST FAULT PANEL IN E/E BAY. 2 L 7 2 4F A6WE 2002020400036 20020204 00036 WP 2002 2 4 B202002F00002 1 20010830 A 7714 AN55311 WIRE DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE TACH GEN BROKEN I FWOA K NONE O OTHER IN INSP/MAINT 1 AL 01 44911 10461 TACH GENERATOR WIRE BROKE WHERE CONNECTOR PLUG PLUGS IN. 2 L 7 4 4R 4 R A762 5E5 2002020400037 20020204 00037 WP 2002 2 4 B202002F00003 1 20010830 A 3260 313 BULB DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE MLG INDICATOR BURNED OUT I B2OB K NONE O OTHER IN INSP/MAINT 1 AL 01 44911 10461 MAIN LANING GEAR LIGHT BURNED OUT. CHANGED BURNED OUT LIGHT BULB. 2 L 7 4 4R 4 R A762 5E5 2002020400038 20020204 00038 WP 2002 2 4 B202002F00004 1 20010830 A 7111 BUSHING DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE COWL FLAP WORN I B2OB K NONE O OTHER IN INSP/MAINT 1 AL 01 44911 10461 NR 2 ENGINE COWL FLAP BUSHING WORN, REPACED WITH NEW. . 2 L 7 4 4R 4 R A762 5E5 2002020400039 20020204 00039 WP 2002 2 4 B2O2002F00000 1 20010830 A 7111 BUSHING DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE COWL FLAP WORN I B2OB K NONE O OTHER IN INSP/MAINT 1 AL 01 44911 10461 BUSHING AT COWL FLAP, NR 4 ENGINE CHANGED NR 2 AND NR 4 OUTBOARD COWL BUSHING. 2 L 7 4 4R 4 R A762 5E5 2002020400040 20020204 00040 WP 2002 2 4 B2O2002F00001 1 20010830 A 5280 2222440 SHAFT DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE MLG DOOR WORN I B2OB K NONE O OTHER IN INSP/MAINT 1 AL 01 44911 10461 SHAFT AT GEAR DOOR, CHANGED SHAFT NR 4 GEAR DOOR. 2 L 7 4 4R 4 R A762 5E5 2002020400041 20020204 00041 WP 2002 2 4 B2O2002F00002 1 20010830 A 5280 1222437 BUSHING DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE NR 3 MLG DOOR WORN I B2OB K NONE O OTHER IN INSP/MAINT 1 AL 01 44911 10461 NR 3 MLG DOOR BUSHING WORN. REMOVED AND REPLACED. 2 L 7 4 4R 4 R A762 5E5 2002020400042 20020204 00042 WP 2002 2 4 B2O2002F00003 1 20010830 A 5280 2222439 FORK DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE NR 3 MLG DOOR WORN I B2OB K NONE O OTHER IN INSP/MAINT 1 AL 01 44911 10461 NR 3 MLG DOOR FORK WORN. 2 L 7 4 4R 4 R A762 5E5 2002020400043 20020204 00043 WP 2002 2 4 B2O2002F00004 1 20010830 A 5280 2222439 FORK DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE NR 4 MLG DOOR WORN I B2OB K NONE O OTHER IN INSP/MAINT 1 AL 01 44911 10461 NR 4 MLG DOOR FORK WORN. 2 L 7 4 4R 4 R A762 5E5 2002020400044 20020204 00044 WP 2002 2 4 B2O2002F00005 1 20010830 A 5280 1222437 BUSHING DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE NR 4 MLG DOOR WORN I B2OB K NONE O OTHER IN INSP/MAINT 1 AL 01 44911 10461 NR 4 GEAR DOOR BUSHING WORN. REMOVED AND REPLACED. 2 L 7 4 4R 4 R A762 5E5 2002020400045 20020204 00045 WP 2002 2 4 B2O2002F00006 1 20010830 A 5753 TORQUE TUBE DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE RT FLAP WORN I B2OB K NONE O OTHER IN INSP/MAINT 1 AL 01 44911 10461 TORQUE TUBE ON RT WING TE FLAP WORN. 2 L 7 4 4R 4 R A762 5E5 2002020400046 20020204 00046 WP 2002 2 4 B2O2002F00007 1 20010830 A 5753 FOLLOWER DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE RT WING TE FLAPS CRACKED I B2OB K NONE O OTHER IN INSP/MAINT 1 AL 01 44911 10461 FLAP FOLLOWER, HAD SMALL CRACK STARTING AT FLEX POINT, REPLACED WITH NEW. 2 L 7 4 4R 4 R A762 5E5 2002020400047 20020204 00047 WP 2002 2 4 B2O2002F00008 1 20010830 A 5753 TORQUE TUBE DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE TE FLAPS WORN I B2OB K NONE O OTHER IN INSP/MAINT 1 AL 01 44911 10461 LT WING TE FLAP TORQUE TUBE WORN. 2 L 7 4 4R 4 R A762 5E5 2002020400048 20020204 00048 WP 2002 2 4 B2O2002F00010 1 20010830 A 7721 THERMOCOUPLE DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE ENGINE INOPERATIVE I B2OB K NONE O OTHER IN INSP/MAINT 1 AL 01 44911 1000 10461 CHT THERMOCOUPLE INOPERATIVE. CHANGED CHT THERMOCOUPLE. 2 L 7 4 4R 4 R A762 5E5 2002020400049 20020204 00049 WP 2002 2 4 B2O2002F00011 1 20010915 A 3110 BULB DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE INST PANEL BURNED OUT I B2OB K NONE O OTHER IN INSP/MAINT 1 AL 01 44911 10461 CHANGED A COUPLE OF BURNED OUT COCKPIT INSTRUMENT LIGHTS. 2 L 7 4 4R 4 R A762 5E5 2002020400050 20020204 00050 NE 2002 2 4 B2O2002F00013 2 20010830 A 8530 PUSHROD TUBE DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE ENGINE WORN I B2OB K NONE O OTHER IN INSP/MAINT 1 AL 01 44911 1280 10461 HOLE WORN IN PUSHROD TUBE, TUBE LOOSE FROM ENGINE BAFFLE. 2 L 7 4 4R 4 R A762 5E5 2002020400051 20020204 00051 WP 2002 2 4 B2O2002F00015 1 20010830 A 5330 RIVET DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE FUSELAGE LOOSE I B2OB K NONE O OTHER IN INSP/MAINT 1 AL 01 44911 10461 LOOSE RIVETS IN BELLY, RESHOT RIVETS IN 2 PLACES. 2 L 7 4 4R 4 R A762 5E5 2002020400054 20020204 00054 NM 2002 2 4 BJNA011202 1 20011206 A 3260 CIRCUIT BREAKER BOEING 737 737214 138446R NM MLG INDICATOR FAILED A BJNA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 WP 11 457TM 20156 GEAR DOWN LIGHTS FAILED. THE PILOT NOTICED HE DID NOT HAVE A LANDING GEAR DOWN INDICATION (3 GREEN LIGHTS) LANDING GEAR CHECK LIST HAD BEEN COMPLETED. WITH NO INDICATIONS THE TOWER WAS NOTIFIED THE PILOT ELECTED TO DO A GO AROUND AND ASK THE TOWER TO VERIFY THE GEAR WAS DOWN. THE TOWER ADVISED THAT HE COULD SEE ONLY THE NOSE WHEEL AND RIGHT MAIN GEAR DOWN . MAINTENANCE PEOPLE CAME OUT TO VERIFY IF THE LANDING GEAR WAS DOWN. THE PILOT ELECTED TO DO ANOTHER LOW PASS SO MAIN TENANCE COULD VERIFY THE GEAR WAS DOWN. MECHANICS VERIFIED THE LANDING GEAR WAS DOWN, NORMAL LANDING WAS MADE WITH NO I NCIDENT. RESET, CIRCUIT BREAKER CHECKED NORMAL ON GROUND. REQUESTED FLIGHT, ACCEPTANCE FLIGHT OK. 2 L 7 2 4F A16WE 2002020400059 20020204 00059 EA 2002 2 4 SWIA200110430 1 20011208 A 2131 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA CABIN PRESSURE MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 411SW 7067 AIRCRAFT WOULD NOT PRESSURIZE IN FLIGHT. RETURNED TO PHX. PERFORMED SINGLE PACK TRANSFER PROCEDURE IN MEL APPENDIX O-1 A. CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002020400060 20020204 00060 SO 2002 2 4 SWIA200110574 1 20011212 A 5210 STRUCTURE EMB 120 EMB120RT 3260202 SO PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 196CA 120196 C-CHECK, PAX DOOR LOWER AFT TRACK, CRACK ON DOOR STRUCTURE. PERFORMED REPAIR ON PASSENGER DOOR UNDER LOWER AFT TRACK PE R SB 120-052-0034. 2 L 7 2 4T RT A31SO 2002020400108 20020204 00108 WP 2002 2 4 UPS01837376 1 20011220 A 5610 PIVOT DOUG DC8 DC873F 302199F WP SLIDING WINDOW LACK OF LUBE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:PFLT CAPTAIN SLIDING WINDOW WILL NOT OPEN. LUBED PIVOT POINTS, WINDOW NOW OPERATES NORMAL. 2 L 7 4 4F RT 4A25 2002020400109 20020204 00109 WP 2002 2 4 UPS01837377 1 20011221 A 5610 PIVOT DOUG DC8 DC873F 302199F WP WINDOW LACK OF LUBE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:N/A DEPARTURE-L-2 WINDOW WOULD NOT LOCK CLOSED. LUBED PIVOT POINTS, OPS CHECKS OK. 2 L 7 4 4F RT 4A25 2002020400130 20020204 00130 WP 2002 2 4 DHL2002805025 1 20011230 A 5712 RIB DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 805DH 75397 46125 N/R0433RT. WING.. UPPER RIB (FORMER) @ STA. 588.000 CRACKED .500 2 L 7 4 4F RT 4A25 2002020400131 20020204 00131 WP 2002 2 4 DHL2002805026 1 20011230 A 5712 RIB DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 805DH 75397 46125 N/R0434RT. WING LEADING EDGE - UPPER RIB(FORMER) @ STA. XFS593.000 , CRACKED .500 2 L 7 4 4F RT 4A25 2002020400132 20020204 00132 WP 2002 2 4 DHL2002805027 1 20011229 A 2700 ANGLE DOUG DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 805DH 75397 46125 N/R 0146RHT WING INTERNAL SLOT ANGLE HAS A 3" CRACK @ XFS 257.50 2 L 7 4 4F RT 4A25 2002020400138 20020204 00138 NM 2002 2 4 PCAA0201016 1 20011226 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 818EX 235 DURING C-CHECK INSPECTION INBOARD LEFT SEAT RAIL FOUND TO HAVE EXCESSIVE CORROSION AT STATION X208. FORWARD SECTION OF SEAT RAIL WAS SPLICED AT STATION X260 IN ACCORDANCE WITH DEHAVILLAND REPAIR DRAWING RD8-53-3074, RD8-53-1102, & RD8-53-2 295. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002020400152 20020204 00152 NM 2002 2 4 2002F00063 1 20011023 A 3350 900835A BATTERY BOEING 727 727200 138407E NM CABIN DISCHARGED A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 919PG 22604 IAD - RIGHT SIDE EXTERIOR CENTER OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY IAW B727 MM 33-50-1 1. (M) 2 L 7 3 4F RT A3WE 2002020400153 20020204 00153 NM 2002 2 4 2002F00065 1 20011204 A 5320 ANGLE BOEING 757 757236 1384971 NM FUSELAGE CORRODED A N8TA K NONE O OTHER IN INSP/MAINT 1 WP 19 526NA 24794 DURING COMPLIANCE WITH CPCP TASK CORROSION FOUND ON KEEL BEAM LOWER L ANGLE BRACKETS AT BS 1139, LBL 4 TO RBL 4, WL 143. MANUFACTURED AND REPLACED L ANGLE PER SRM. (M) 2 L 7 2 4F RT A2NM 2002020400154 20020204 00154 NM 2002 2 4 2002F00066 1 20011222 A 5753 113N300320 SKIN BOEING 757 757236 1384971 NM T/E FLAP CHAFED A N8TA K NONE O OTHER IN INSP/MAINT 1 WP 19 526NA 24794 RIGHT OUTBOARD MAIN FLAP, OUTBOARD END, LEADING EDGE 56 INCHES FROM INBOARD END. DRESSED OUT AND INSTALLED REPAIR PER S RM. REINSPECTION USING HFEC EVERY C-CHECK. (M) 2 L 7 2 4F RT A2NM 2002020400155 20020204 00155 NM 2002 2 4 2002F00067 1 20011222 A 5753 113N300320 SKIN BOEING 757 757236 1384971 NM T/E FLAP CHAFED A N8TA K NONE O OTHER IN INSP/MAINT 1 WP 19 526NA 24794 RIGHT OUTBOARD MAIN FLAP, INBOARD END, LEADING EDGE GOUGE 24 INCHES LONG. DRESSED OUT AND INSTALLED REPAIR PER SRM. RE INSPECTION USING HFEC EVERY C-CHECK. (M) 2 L 7 2 4F RT A2NM 2002020400156 20020204 00156 NM 2002 2 4 2002F00068 1 20011222 A 5753 113N300319 SKIN BOEING 757 757236 1384971 NM T/E FLAP CHAFED A N8TA K NONE O OTHER IN INSP/MAINT 1 WP 19 526NA 24794 LEFT FORWARD OUTBOARD FLAP, OUTBOARD END, LEADING EDGE CHAFED. DRESSED OUT AND INSTALLED REPAIR EPR SRM. REINSPECTION USING HFEC EVERY C-CHECK. (M) 2 L 7 2 4F RT A2NM 2002020400157 20020204 00157 NM 2002 2 4 2002F00069 1 20011222 A 5753 113N300320 SKIN BOEING 757 757236 1384971 NM T/E FLAP CHAFED A N8TA K NONE O OTHER IN INSP/MAINT 1 WP 19 526NA 24794 RIGHT OUTBOARD MAIN FLAP, OUTBOARD END, LEADING EDGE 3 INCHES FROM END CHAFFED. DRESSED OUT AND INSTALLED REPAIR PER SR M. REINSPECTED USING HFEC EVERY C-CHECK. (M) 2 L 7 2 4F RT A2NM 2002020400158 20020204 00158 NM 2002 2 4 2002F00070 1 20011222 A 5315 141N29321 FLOORBEAM BOEING 757 757236 1384971 NM FUSELAGE CORRODED A N8TA K NONE O OTHER IN INSP/MAINT 1 WP 19 526NA 24794 DURING C-CHECK, FLOORBEAM UPPER CHORD FOUND CORRODED, BS 324, RBL 58, WL 208. REPAIRED UPPER CHORD PER SRM. (M) 2 L 7 2 4F RT A2NM 2002020400159 20020204 00159 NM 2002 2 4 2002F00071 1 20011023 A 3350 BATTERY BOEING 727 727200 138407E NM CABIN DISCHARGED A P9RA K NONE O OTHER IN INSP/MAINT 1 SO 11 919PG 22604 IAD - EMERGENCY EXIT SIGN AFT OF FORWARD GALLEY DOOR OVERHEAD BLINKING. ARMED EMERGENCY LIGHT SYSTEM TO ALLOW TRICKLE C HARGE OF EMERGENCY BATTERIES OPS CHECK GOOD. (M) 2 L 7 3 4F RT A3WE 2002020400160 20020204 00160 NM 2002 2 4 2002F00072 1 20011023 A 3350 BATTERY BOEING 727 727200 138407E NM CABIN DISCHARGED A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 919PG 22604 IAD - LEFT AFT GALLEY DOOR EMERGENCY EXIT SIGN INOPERATIVE. ARMED EMERGENCY LIGHT SYSTEM TO ALLOW TRICKLE CHARGE OF EME RGENCY BATTERIES. OPERATIONAL CHECK GOOD. (M) 2 L 7 3 4F RT A3WE 2002020500024 20020205 00024 NM 2002 2 5 2002F00073 1 20010831 A 2781 INDICATOR BOEING 727 727200 138407E NM COCKPIT MALFUNCTIONED A P9RA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 11 910PG 22606 FLT 2215 - ATL - AFTER TAKEOFF, NR 2 LEADING EDGE FLAP FAILED TO RETRACT, FOLLOWED FOM SECTION 3, PAGE 54. AIRCRAFT RET URNED TO ATLANTA. NR 2 FLAP VERIFIED RETRACTED. DISCREPANCY WAS INDICATION ONLY. PERFORMED OPERATIONAL CHECK IAW AMM 27-81-0 OF ALL LEADING EDGE DEVICES, FLAPS AND SLATS, NO DEFECTS NOTED. CLEANED AND INSPECTED NR 2 FLAP SWITCH (S203) A ND WIRING. PERFORMED OPERATIONAL CHECK IAW AMM 27-81-0 OF ALL LEADING EDGE DEVICES, FLAPS AND SLATS, NO DEFECTS NOTED. (M) 2 L 7 3 4F RT A3WE 2002020500030 20020205 00030 NM 2002 2 5 2002F00074 1 20011013 A 3397 W11200122 WIRE BOEING 727 727200 138407E NM CABIN BROKEN A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 910PG 22606 ORD - WHILE PERFORMING LINE CHECK, IT WAS OBSERVED THAT THE AFT SECTION OF THE EMERGENCY ESCAPE PATH LIGHTING WAS INOPER ATIVE. EMERGENCY ESCAPE PATH LIGHTING WAS TROUBLESHOT, AND FOUND TO HAVE A BROKEN WIRE, REPAIRED WIRE IAW MM 20-10-8. PERFORMED OPERATIONAL CHECK OF SYSTEM IAW MM 33-50. (M) 2 L 7 3 4F RT A3WE 2002020500033 20020205 00033 NM 2002 2 5 2002F00075 1 20011022 A 3350 900542 LIGHT BOEING 727 727200 138407E NM CABIN INOPERATIVE A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 910PG 22606 ORD - FOUND DURING LINE CHECK, AFT DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED AFT DOOR EMERGENCY LIGHT PACK ASSEMBLY. (M) 2 L 7 3 4F RT A3WE 2002020500034 20020205 00034 NM 2002 2 5 2002F00076 1 20011023 A 3350 900542 POWER SUPPLY BOEING 727 727200 138407E NM CABIN DISCHARGED A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 910PG 22606 ORD - EXTERIOR EMERGENCY EXIT LIGHT 'LOWER AFT' FOUND INOPERATIVE DURING MAINTENANCE. REMOVED AND REPLACED BATTERY POWE R SUPPLY. (M) 2 L 7 3 4F RT A3WE 2002020500035 20020205 00035 NM 2002 2 5 2002F00077 1 20011023 A 3350 BATTERY BOEING 727 727200 138407E NM CABIN DISCHARGED A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 919PG 22604 IAD - L1 DOOR EMERGENCY EXIT SIGN INOPERATIVE. ARMED EMERGENCY LIGHT SYSTEM TO ALLOW TRICKLE CHARGE OF EMERGENCY BATTER IES. OPERATIONAL CHECK GOOD. (M) 2 L 7 3 4F RT A3WE 2002020500036 20020205 00036 NM 2002 2 5 2002F00078 1 20011023 A 3350 900835A BATTERY BOEING 727 727200 138407E NM CABIN DISCHARGED A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 919PG 22604 IAD - LEFT SIDE EXTERIOR CENTER OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY IAW B727 MM 33-50-11 . (M) 2 L 7 3 4F RT A3WE 2002020500038 20020205 00038 NM 2002 2 5 2002F00079 1 20011023 A 3350 900835A BATTERY BOEING 727 727200 138407E NM CABIN DISCHARGED A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 919PG 22604 IAD - LEFT SIDE EMERGENCY OVERWING EXIT DOORS LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-50-00. (M) 2 L 7 3 4F RT A3WE 2002020500040 20020205 00040 NM 2002 2 5 2002F00080 1 20011024 A 3350 900835A BATTERY BOEING 727 727200 138407E NM CABIN DISCHARGED A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 919PG 22604 IAD - LEFT SIDE INTERIOR EMERGENCY LIGHT NEEDS OPERATIONAL CHECK. REMOVED AND REPLACED BATTERY IAW B727 MM 33-50. OPS CHECK GOOD. (M) 2 L 7 3 4F RT A3WE 2002020500046 20020205 00046 NM 2002 2 5 2002F00081 1 20011026 A 3350 CONNECTOR BOEING 727 727200 138407E NM CABIN LOOSE A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 919PG 22604 IAD - DOOR L2 WALKAROUND EXIT LIGHT DID NOT ILLUMINATE. TROUBLESHOT AND FOUND BATTERY NOT CHARGING DUE TO BAD CONNECTIO N. REESTABLISHED CONNECTION AND CLEANED CONTACTS. OPERATIONAL CHECK GOOD. (M) 2 L 7 3 4F RT A3WE 2002020500048 20020205 00048 EU 2002 2 5 EGR2002F00001 1 20011215 A 3340 019059 GIMBAL JOINT BOLKMS 117 BK117A3 5626015 EU SEARCH LIGHT CRACKED E EGRA K NONE O OTHER IN INSP/MAINT 1 EA 17 532KH 5616 7069 GIMBAL ARM CRACKED COMPLETELY THROUGH AT RIVETS CAUSING SEARCHLIGHT TO BECOME LOOSE ON ONE SIDE. LIGHT WAS RESTRAINED O NLY BY THE SAFETY CABLE AND OTHER SIDE ARM OF GIMBAL. RIGHT AFT PASSENGER DOOR GAS SUPPORT STRUT DISCONECTED FROM BALL SOCKET. INBOARD AND PUSHED THROUGH TRIM PANEL DURING DOOR CLOSING, WHICH IN TURN PUSHED AGAINST THE RIGHT LATERAL CYCLI C CONTROL ROD CAUSING THE BIND. THIS CONTROL ROD CONNECTS THE CYCLIC STICK TO THE MIXING UNIT THEN TO THE MAIN ROTOR SE RVO. GAS STRUT WAS RECONNEDTED AND SAFETIED. DUCT WAS REPOSITIONED TO PROVIDE CLEARANCE BETWEEN DUCT AND CONTROL ROD. INSTRUCTIONS WERE GIVEN TO ENSURE GAS SPRING IS ATTACHED DURING DOOR CLOSING. 1 G 7 2 3U H13EU 2002020500050 20020205 00050 EU 2002 2 5 R7MR34241 1 20010922 A 7160 9696 MOTOR SNIAS 350 AS350B3 8680954 EU FAN INOPERATIVE B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 52281 882 3249 FAN MOTOR, UNIT INOPERATIVE. MOTOR RUNS ROUGH. REPLACED WITH NEW UNIT CORRECTED PROBLEM. 1 G 7 1 3U H9EU 2002020500051 20020205 00051 NM 2002 2 5 2002F00082 1 20011022 A 3350 900542 POWER SUPPLY BOEING 727 727214 138407R NM CABIN DISCHARGED A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 288SC 20765 ORD - DURING LINE CHECK, FOUND EXTERIOR EMERGENCY LIGHT OUT. REMOVED AND REPLACED BATTERY POWER SUPPLY. (M) 2 L 7 3 4F A3WE 2002020500056 20020205 00056 NM 2002 2 5 2002F00083 1 20011022 A 3350 90052 POWER SUPPLY BOEING 727 727214 138407R NM CABIN DISCHARGED A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 288SC 20765 ORD - DURING LINE CHECK, FOUND AFT EXTERIOR EMERGENCY LIGHT OUT. REMOVED AND REPLACED BATTERY POWER SUPPLY. (M) 2 L 7 3 4F A3WE 2002020500059 20020205 00059 EA 2002 2 5 2002F00084 1 20011217 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A MASA K NONE F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 SW 07 47202 7202 FLT 5865 - SDF-PHL - INBOUND TO SDF, THE CREW HAD A FLAP FAIL CAUTION MESSAGE. THE MESSAGE APPEARED WITH THE FLAPS AT Z ERO AND NOT SELECTED. MAINTENANCE PERFORMED PART A OF THE AD, RESET THE SYSTEM AND THERE WERE NO FURTHER MESSAGES OR DE FECTS. THE AIRCRAFT WAS RETURNED TO SERVICE WHERE DURING OVERNIGHT IN PHL, PART B OF THE AD WAS COMPLIED WITH. (M) 2 L 7 2 4F RT A21EA 2002020500061 20020205 00061 SO 2002 2 5 2002F00085 1 20011014 A 3350 78811 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 837MJ 145367 FLT 5729 - THE CREW FOUND ONE SEGMENT OF EMERGENCY FLOOR LIGHTING INOPERATIVE. MAINTENANCE TROUBLESHOT THE PROBLEM. RE MOVED AND REPLACED THE LIGHT STRIP AND OPS CHECKED GOOD. (M) 2 L 7 2 4T RT T00011AT 2002020500062 20020205 00062 EA 2002 2 5 2002F00086 1 20011109 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27314 7314 WHILE PERFORMING SERVICE CHECK, THE CREW FOUND THE EXTERIOR EMERGENCY LIGHT NR 4 INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED THE EMERGENCY LIGHT AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2002020500063 20020205 00063 NM 2002 2 5 2002F00087 1 20010927 A 3350 MS25231316 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 436YV 436 FLT 6333 - AN EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE DETERMINED THE BULB WAS UNSERVICEABLE. THE BULB WAS R EMOVED AND REPLACED AND OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A13NM 2002020500064 20020205 00064 NM 2002 2 5 2002F00088 1 20011121 A 3350 GE1619 LIGHT DHAV DHC8 DHC8202 2809007 NM EXTERIOR INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 434YV 434 FLT 6200 - FLG-PHX - THE CREW FOUND A LEFT EXTERIOR FUSELAGE AFT EMERGENCY EGRESS LIGHT INOPERATIVE. MAINTENANCE REMOVE D AND REPLACED THE LIGHT AND OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A13NM 2002020500066 20020205 00066 SW 2002 2 5 2002F00090 1 20011205 A 5270 WARNING SYSTEM FRCHLD SA227 SA227DC 3377521 SW COCKPIT MALFUNCTIONED A BSAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 05 850LS DC850B DURING CLIMB-OUT, THE CARGO DOOR WARNING LIGHT CAME ON. CREW RETURNED TO THE STATION. THE CARGO DOOR WARNING LIGHT WEN T OUT WHILE THE AIRCRAFT WAS TAXIING BACK TO THE GATE. MAINTENANCE INSPECTED THE CARGO DOOR CLICK CLACKS AND DOOR WARNI NG SYSTEM AND FOUND NO DEFECTS. THE DOOR WAS OPENED AND SHUT MULTIPLE TIMES WITH CORRECT OPERATION EVERY TIME. FLIGHT WAS CONTINUED WITH NO FURTHER PROBLEMS. (M) 2 L 7 2 4T RT A18SW 2002020500067 20020205 00067 SW 2002 2 5 2002F00091 1 20011214 A 2160 BYLB504371 VALVE FRCHLD SA227 SA227DC 3377521 SW CABIN TEMP FAILED A BSAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 05 453LA DC852B FOUND LEFT ACM STARTED TO BLOW SMOKE AND WOULDN'T ADJUST TO COOLER SETTING. ACM BEARING FAILURE. REPLACED LEFT ACM AND MIXIN VALVE. MIXING VALVE HAD FAILED IN THE HOT POSITION. TEARDOWN OF THE ACM REVEALED IT HAD BEEN OVERSERVICED. A M EMO OF SERVICING OF ACM'S HAS BEEN ISSUED. (M) 2 L 7 2 4T RT A18SW 2002020500077 20020205 00077 SW 2002 2 5 2002F00094 1 20011216 A 5270 SWITCH FRCHLD SA227 SA227DC 3377521 SW CARGO DOOR OUT OF ADJ A BSAA O OTHER N FALSE WARNING CR CRUISE 1 NM 05 850LS DC850B DURING CRUISE, THE CARGO DOOR WARNING LIGHT CAME ON. CREW RETURNED TO STATION. THE CARGO WARNING LIGHT STAYED ON. DOO R HANDLE CLOSURE OR MICROSWITCH RIGGING. ADJUSTED CARGO DOOR REAR BOTTOM BAYONET MICROSWITCH. ALL OTHER SWITCHES, CLIC K CLACKS, AND WARNING SYSTEM WIRING WERE CHECKED, NO DEFECTS WERE NOTED. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A18SW 2002020500078 20020205 00078 CE 2002 2 5 DIN2002F00000 1 20011217 A 2421 PLATE LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP DAMPER CLUTCH WORN B DINR K NONE O OTHER IN INSP/MAINT 1 EA 13 258G 1423 443 CARBON DUST NOTICED COMING FROM A BRUSHLESS GENERATOR. TSO GENERATOR 445 HRS. LOANER UNIT WAS INSTALLED. TEARDOWN INSP FOUND DRIVESHAFTS FRICTION CLUTCH PLATE TO BE WORN REQUIRING REPLACEMENT. THE OVERHAUL SHOP SAID THE FANUFACTURE HAD C HANGED MATERIALS FROM ASBESTOS TO CARBON RECENTLY. THE ASBESTOS PLATES TYPICALLY LASTED 2 OVERHAULS OR 2100 HRS. IT WA S DOUBTFUL THE CARBON MATERIAL WOULD HAVE LAST UNTIL THE FIRST OVERHAUL AT 1050 HRS. A NEW PART WAS INSTALLED, MADE FRO M A THIRD TYPE OF MATERIAL CONSISTING OF CARBON AND BRASS COMBINATION. THESE GENERATORS CONTINUE TOBE A VERY EXPENSIVE COST PER HOUR UNIT TO OPERATE. 2 L 7 2 4F 4 F A10CE E6WE 2002020500079 20020205 00079 EU 2002 2 5 E4G2002F00000 1 20011010 A 2560 SEAT BELT SAAB SF340 340B 7860101 EU GE CT7TS CT71 30030 NE CABIN DEFECTIVE A E4GR K NONE O OTHER IN INSP/MAINT 1 SW 13 345SB 340B345 AIRCRAFT ARRIVED FOR MBV CHECK AND 17 EACH SEAT BELT LINKS WERE DEFECTIVE. THE CONNECTING RIVET IS PULLING OUT. SEVERA L LINKS WERE ALMOST ALL THE WAY APART. THIS AFFECTS CUSTOMER SAFETY. 2 L 7 2 4T 4 U RT A52EU E8NE 2002020500080 20020205 00080 SW 2002 2 5 2002F00095 1 20011205 A 2910 2781032135 HYDRAULIC LINE SWRNGN SA227 SA227AC 8780603 SW HYDRAULIC SYS LEAKING A BSAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 05 702M AC702 FLT 1322 - ON CLIMB-OUT, BOTH HYD LIGHTS CAME ON AND HYDRAULIC PRESSURE GATE WENT TO '0'. CREW LANDED AFTER DECLARING E MERGENCY AND MANUALLY EXTENDING THE GEAR. SUSPECTED BREAK IN HYDRAULIC LINE CAUSING FLUID LOSS LEADING TO HYDRAULIC PRE SSURE LOSS. REPLACED FLAP UP HYDRAULIC LINE FROM POWER PACK TO AFT LEFT NACELLE AREA. (M) 2 L 7 2 4T RT A8SW 2002020500081 20020205 00081 NE 2002 2 5 ESU2002F00000 2 20011228 A 7321 5002794G33 FUEL CONTROL LEAR 24 24B 5170306 CE GE CJ610 CJ6106 30006 NE RT ENGINE FAILED E ESUA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 CE 03 600XJ 7059 4063 190 251406A AS THE AIRCRAFT WAS CLIMBING THROUGH FLIGHT 370. THE RIGHT ENGINE FLAMED OUT. THERE WAS NO FIRE AND NO EMERGENCY WAS D ECLARED. THE PILOTS WENT THROUGH THE RELIGHT PROCEDURE WHEN THEY ARRIVED AT THE RELIGHT ENVELOPE WITH NO SUCCESS AS THE Y WERE UNABLE TO OBTAIN A FUEL FLOW. THEY WERE ABLE TO ACHIEVE 30 PERCENT RPM, HOWEVER, THE AIRCRAFT LANDED WITH NO PRO BLEMS. IT WAS FOUND THAT THE FUEL CONTROL HAD FAILED, EXPLAINING NO FUEL FLOW. 2 L 7 2 4J 4 J A10CE 1E16 2002020500082 20020205 00082 2002 2 5 EVAB2001001 4 20010102 A 6122 4G8P67M GOVERNOR CURTIS C46 C46AFLYTIGER SO PWA R2800 R2800* 52026 NE PROPELLER FAULTY I EVAB O OTHER J WARNING INDICATION NR NOT REPORTED 1 AL 01 1837M 22388 NR 1 ENGINE FEATHERED DUE TO UNCONTROLABLE RPM CAUSED BY A FAULTY PROP GOVERNOR. REPLACED GOVERNOR, GROUND CHECK, GOOD. 2 L 7 2 4R 4 R A772 5E8 2002020500083 20020205 00083 CE 2002 2 5 FE62002F00000 1 20010726 A 2430 UC2814 CONVERTER BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE DC SYSTEM FAILED B FE6R O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 11 400KP 120 RK308 CONVERTER FAILED AND BEGAN TO MELT THE SIDEPANEL CARPET (WHICH WAS LYING ON TOP OF IT). AT THIS TIME THE CAUSE OF THE F AILURE IS UNCERTAIN. 2 H 7 2 4F 4 F RT A16SW E25EA 2002020500084 20020205 00084 SW 2002 2 5 2002F00097 1 20011214 A 2160 VALVE FRCHLD SA227 SA227DC 3377521 SW CABIN TEMP FAILED A BSAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 05 453LA DC852B FLT 1315 - WDG - LEFT ACM STARTED TO BLOW SMOKE AND WOULDN'T ADJUST TO COOLER SETTING. ACM BEARING FAILURE. REPLACED L T ACM AND MIXING VALVE. MIXING VALVE HAD FAILED IN THE HOT POSITION. TEARDOWN OF THE ACM REVEALED IT HAD BEEN OVERSERV ICED. A MEMO OF SERVICING OF ACM'S HAS BEEN ISSUED. (M) 2 L 7 2 4T RT A18SW 2002020500085 20020205 00085 WP 2002 2 5 FXG2002F00001 1 20011102 A 2612 FIRE LOOP DOUG DC6 DC6B 3021712 WP PWA R2800 R2800* 52026 NE NR 2 ENGINE DEFECTIVE A FXGA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 AL 01 6586C 33958 45222 P28812 AIRCRAFT DEPARTED AND 10 MINUTES INTO FLIGHT HAD A ZONE 1 FIRE WARNING ON NR 2 ENGINE. FIRE BOTTLES DISCHARGED, ENGINE FEATHERED AND AIRCRAFT RETURNED TO DEPARTURE AIRPORT. SUSPECTED FAULTY FIRE WARNING PANEL AND 3 DETECTORS REPLACED AFTE R THOROUGH INSPECTION OF ENGINE AND OEC WHICH SHOWS NO EVIDENCE OF ACTUAL FIRE. 2 L 7 4 4R 4 R 6A4 5E8 2002020500087 20020205 00087 CE 2002 2 5 IY22002F00000 1 20011213 A 5710 STRUCTURE LEAR 25 25D 5170514 CE GE CJ610 CJ6108 30006 NE LT WING CORRODED E IY2R K NONE O OTHER IN INSP/MAINT 1 SW 15 972H 370 DURING PREPARATION OF AIRCRAFT FOR PAINT, CORROSION WAS FOUND ON THE TOP OF THE LEFT WING BETWEEN WING STATIONS 125.00 T O 181.10 AND SPAR NR 5 TO 8 UNDER A RAISED BACK COVER. THE CORROSION IS AS MUCH AS .044 INCHES DEEP. WHEN THE COVER WA S REMOVED, NUMEROUS VOIDS WERE IN THE SEALANT AND THE PAINT PRIMER ALSO CAME OFF STILL ATTACHED TO THE SEALANT. THE RIG HT WING IS IN SIMULAR CONDITION AS THE LEFT WING WITH CORROSION UP TO .038 INCHES. 2 L 7 2 4J 4 J A10CE 1E16 2002020500088 20020205 00088 CE 2002 2 5 JEM2002F00000 1 20011217 A 7120 45A343615 MOUNT MTSBSI MU300 MU300 5780602 CE PWA JT15 JT15D4 52112 NE LT ENGINE CRACKED B JEMA K NONE O OTHER IN INSP/MAINT 1 CE 07 417KT 10868 A083SA CONCERNING A VISUAL INSPECTION OF THE LT ENGINE CARRY THROUGH MOUNT BACKET FOR CRACKS ON MFG 400 NAD 400A. IT DOES NOT COVER THE MU-300 SERIES AIRCRAFT. WE IN SPECTED THIS AIRCRAFT AND FOUND A CRACKED MOUNT BRACKET. BUGGEST MFG EXPAND TH E MODELS TO INCLUDE THE MU-300 SERIES OF AIRCRAFT. 2 H 7 2 4F 4 F RT A14SW E1NE 2002020500095 20020205 00095 NE 2002 2 5 AALA20011818 2 20010925 A 7200 ENGINE BOEING 757 757223 1384957 NM RROYCE RB211 RB211535* NE RT AND LT OVERTEMP A AALA C ABORTED TAKEOFF M OVER TEMP TO TAKEOFF 1 SW 21 608AA 27446 LAX - FLT 161 - ON TAKEOFF, ENGINE EGT 901 DEGREES AND RT ENGINE EGT 914 DEGREES FOR APPROX FIVE SECONDS ALL OTHER ENGIN E INDICATIONS NORMAL. PERFORMED EEC BITE TPU BITE BVCU BITE ON BOTH RIGHT AND LEFT ENGINE NO FAULTS NOTED PERFORMED EGT BALLAST AND COMPENSATOR RESISTANCE CHECK ON BOTH ENGINES PER MM. RESISTORS CHECKED GOOD CHECKED EGT HARNESSES LOOSE OR CORRODED CONNECTION HARNESSES CHECK GOOD ON BOTH ENGINE PER FIM 71-05-00 FIG 121 AND 116 ACCOMPLISHED BORESCOPE INSPECT ION ON HP IP AND COMBUSTION SECTION PER MCM CARDS 4224 AND 4223 ON LEFT AND RIGHT ENGINES REF TFI 7723B6 FOR DISPOSITION . 2 L 7 2 4F 4 F RT A2NM E12EU 2002020500096 20020205 00096 EU 2002 2 5 AALA20011851 1 20011009 A 2497 GROUND WIRE AIRBUS 300 A300B4605R 3930308 EU ELECTRICAL SYS BROKEN A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 70072 515 FLT 93 - APU FAULTED IN FLIGHT AND WOULD NOT RESTART. NO FAULTS WERE FOUND ON THE ECB. REPLACED THE ECB AS PRECAUTIONA RY. PROBLEM FOUND TO BE A BROKEN GROUND WIRE TO THE STANDBY GENERATOR CONTROL VALVE. WIRE WAS REPAIRED AND STANDBY GEN ERATOR TEST WAS PERFORMED. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT APU WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A35EU 2002020500119 20020205 00119 NM 2002 2 5 CA011001007 1 20010913 A 7921 28E997 OIL COOLER HONEYWELL DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 2 ENGINE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 13599 11900966 (CAN) THE FLIGHT CREW REPORTED EXCESSIVE OIL ON THE NR 2 LANDING GEAR LEG. MAINTENANCE REPLACED A LEAKING NR 2 ENGINE OI L COOLER. TIME SINCE REPAIR FOR A PREVIOUS LEAK 2843 HOURS. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002020500120 20020205 00120 NM 2002 2 5 CA011019010 1 20010928 A 3234 4105DA SELECTOR VALVE BOEING 737 737217 1384464 NM PWA JT8 JT8D17A 52049 NE MLG FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) AFTER NORMAL TAKEOFF, GEAR IN OFF POSITION, LIGHTS OUT, AT 29,000 FT. SPEED AT 290-300 LANDING GEAR CAME DOWN WITH THREE GREEN LIGHTS, AIR DID AN AIR TURN BACK TO REGINA. FOUND TO BE THE SELECTOR VALVE AT FAULT. LANDING GEAR SELECTOR VALVE REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 2002020500121 20020205 00121 WP 2002 2 5 CA011114002 1 20010928 A 4920 49700011 APU DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE APU BAY FAILED W O OTHER T J ENGINE CASE PENETRATION WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) APU QUIT ON PUSHBACK, OIL LEAK OBSERVED. FOUND APU COMPRESSOR / TURBINE HAD A NON CONTAINED FAILURE CAUSING SEVE RE DAMAGE. (TURBINE BLADES FOUND IN APU COMPARTMENT). REPLACED APU AS PER MM 49-10-00 REPLACED FUEL HEATER AS PER MM 49 -31-01 CROSSOVER DUCT CHECKED FOR FOD (NONE FOUND) 2 L 7 2 4F 4 F A6WE E2EA 2002020500124 20020205 00124 WP 2002 2 5 CA011121016 1 20011101 A 2170 HEAT EXCHANGER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE LT PACK SEPARATED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA (CAN) UNABLE TO MAINTAIN CABIN PRESSURE WITH R/H PACK ONLY. LT PACK ON DEVIATION. FOUND HEAT EXCHANGER SEPARATED AT THE EXCHANGER. RE-SECURED AND PACKS OPERATED NORMALLY. 2 L 7 2 4F 4 F A6WE E2EA 2002020500125 20020205 00125 NM 2002 2 5 CA011121017 1 20011102 A 2750 CONTROL HANDLE BOEING 767 767375 1385217 NM GE CF6 CF680C2B6F 30025 NE TE FLAPS FAILED W A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 CA (CAN) ON APPROACH TO ST-JOHN, NF, WHEN SELECTED FLAP TO 5 DEGREES, FLAP DISAGREE EICAS MSG. CHECKLIST COMPLETED. EMERGEN CY CALLED OUT. FLAP LEVER RVDT AND OUTBOARD SLAT PDU RVDT RE-ADJUSTED. FSEU RESETED AND FLAPS OPERATED SEVERAL TIMES. SY STEM SERVICEABLE. 2 L 7 2 4F 4 F RT A1NM E13NE 2002020500126 20020205 00126 EA 2002 2 5 CA011130009 1 20011128 A 5210 H3451427 HANDLE H3451427 CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 15828 (CAN) AIR TURNBACK DUE TO PASSENGER DOOR WARNING AND PAX DOOR STOW CAUTION MSG POSTED. AT 1,500 FT AGL PASSENGER DOOR U NSAFE CAUTION MESSAGE CAME ON. AT 10,000 FT RED PASSENGER DOOR WARNING MESSAGE WAS POSTED. RETURNED TO AIRPORT. INSPECTE D PASSENGER DOOR FOR LOOSE OR DAMAGED PARTS. REPLACED OUTER HANDLE AND CLEANED INNER HANDLE DETENT ROLLER. PRESSURIZED T O APPROXIMATELY 6 PSI. OPS AND LEAK CHECKED GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002020500127 20020205 00127 EU 2002 2 5 CA011203004 1 20011127 A 4920 4500001A APU 4500001A AIRBUS 320 A320212 3930322 EU CFMINT CFM56 CFM565A3 NE APU BAY FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 1665 (CAN) WHILE ON THE GATE THE APU GENERATOR FAILED. THE APU ASSY AND GENERATOR WERE REPLACED AND A/C RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A28NM E29NE 2002020500131 20020205 00131 NE 2002 2 5 CA011221003 1 20011210 A 2434 30E2097A SHAFT BENDIX 30E2097A SKRSKY S61 S61N 8142104 NE GE CT58 CT581401 30011 NE DC GENERATOR SHEARED W O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 CA 71 (CAN) WHILE ON PAD, WITH ROTORS ENGAGED, IT WAS NOTICED ZERO AMPS ON DC AMMETER. THE GEN IREC SWITCH WAS SELECTED TO REC (RECTIFIED) AND 150 AMPS WAS READ. SUSPECTED DC GEN FAILURE. CARRIED OUT CHECK LIST PROCEDURE & THAT WAS WHEN THE DC GEN LIST ILLUMINATED. UPON REMOVAL OF THE ABOVE UNIT THE SHAFT WAS FOUND SHEARED. UNIT REPLACED & A/C RETURNED TO S ERVICE. 2 G 7 2 4U 4 U 1H15 1E3 2002020500132 20020205 00132 NM 2002 2 5 CA011227002 1 20011223 A 7921 ADAPTER HONEYWELL 28E997 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE OIL COOLER LEAKING W E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA 02901113 (CAN) ON ROTATION OUT, CREW NOTED NR 1 OIL PRESSURE WARNING LIGHT ILLUMINATED, AND LARGE STREAK OF OIL ALONG INBOARD S IDE OF LT NACELLE. CREW ELECTED TO SHUT DOWN NR 1 ENGINE (HAD TO USE ALTERNATE FEATHER PROCEDURE TO FEATHER THE PROPELL ER), AND RETURMED TO BASE. AIRCRAFT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REVEALED NR 1 OIL COOLER LEAKING AT THE OIL SCAVENGE LINE ADAPTER, WITH THREAD DAMAGE AT THE BOLT HOLES (2). OIL COOLER REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002020500134 20020205 00134 NM 2002 2 5 CA020104010 1 20011207 A 2121 GASPER FAN BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE GASPER FAN SEIZED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 42176 42176 (CAN) AIRCRAFT ENROUTE FROM SAN FRANSISCO TO VANCOUVER, DIVERTED TO KLAMATH FALLS OREGON, DUE SMOKE IN THE CABIN. SMO KE DISIPATED WHEN GASPER FAN SELECTED OFF. GASPER FAN FOUND SEIZED. GASPER FAN REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 2002020500135 20020205 00135 NM 2002 2 5 CA020104011 1 20011204 A 7500 DUCT GE CF680C2B6F BOEING 767 767375 1385217 NM GE CF6 CF680C2B6F 30025 NE LT ENGINE DAMAGED W F C ACTIVATE FIRE EXT. ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 703125 (CAN) LT ENGINE FIRE INDICATION AT 11,000 FEET IN CLIMB. ENGINE SHUT DOWN. FIRE BOTTLES DISCHARGED. AIRCRAFT RETURNED TO SYDNEY. FOUND ENGINE PNEUMATIC DUCTING RUPTURED AND ALSO HARNESS DAMAGED. HARNESS TEMPORARY REPAIRED AS PER PRODUC TION PERMIT 6-77-20/351-77-TO52 (-00078). BOTH FIRE EXTINGUISHER BOTTLES REPLACED. SYSTEM TESTED CONSIDERED SERVICEABLE. 2 L 7 2 4F 4 F RT A1NM E13NE 2002020500137 20020205 00137 NE 2002 2 5 CA020110001 2 20011220 A 7200 CF6 ENGINE GE BOEING 767 7673S1 1385211 NM GE CF6 CF680C2B6F 30025 NE LEFT FAILED W C ABORTED TAKEOFF E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CA (CAN) ON TAKEOFF ROLL, AFTER N1 SELECTED ON MCP, ENGINE ACCELERATE NORMALLY TO 50 PERCENT AT 50 PERCENT ENGINE DID NO T ACCELERATE ANY FURTHER. ALL PARAMATERS NORMAL FOR BOTH ENGINES. AN AIRFRAME VIBRATION COULD BE FELT AT 25 - 50 PERCE NT ON LT ENGINE. TAKE OFF CANCELLED. ENGINE REPLACED. 2 L 7 2 4F 4 F RT A1NM E13NE 2002020500146 20020205 00146 EU 2002 2 5 CA020121009 1 20011207 A 2913 861276 SHAFT 974800 AIRBUS 330 A330243 3930330 EU RROYCE RB211 RB211TRENT77 NE SHAFT SPLINES CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA MX6055399 (CAN) UPON REPLACING THE REEN HYDRAULIC PUMP ON THE ENGINE, IT WAS NOTICED THAT WHEN THE HYD PUMP SHAFT WAS REMOVED FR OM THE OLD PUMP AND TRANSFERRED TO THE NEW PUMP (BECAUSE THE NEW PUMP CAME WITHOUT A SHAFT), THE SHAFT SHOWED SIGNS OF CORROSION ON THE SPLINES AND THE SHAFT RETAINING CLIP WAS SHOWING SPLINE WEAR MARKS. THE SHAFT WAS REPLACED. 2 L 7 2 4F 4 F RT A46NM E39NE 2002020500151 20020205 00151 SW 2002 2 5 AUS20011374 1 20011219 A 7714 2719157003 INDICATOR GARRTT TPE33111U SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP ROTOL R321 R321482F8 GL ENGINE RPM FAULTY W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RPM INDICATOR STICKING WITH NOTCHY OPERATION. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P61GL 2002020500159 20020205 00159 NM 2002 2 5 AUS20011391 1 20011222 A 2760 8294100187 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE SPOILER HYD SYS LEAKING W O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 AU S (AUS) SPOILER HYDRAULIC LINE CONTAINED A PINHOLE LEAK IN THE AREA LOCATED JUST FORWARD OF THE ENGINE FIRE BOTTLES IN THE WING CENTRE SECTION. HYDRAULIC FLUID LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002020500160 20020205 00160 NM 2002 2 5 AUS20011392 1 20011227 A 5610 17180005 WINDOW DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE COCKPIT DELAMINATED W O OTHER O OTHER CR CRUISE 1 AU S (AUS) LT COCKPIT SIDE WINDOW OUTER ACRYLIC PANE PARTIALLY DELAMINATED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002020500164 20020205 00164 EU 2002 2 5 AUS20011397 1 20011106 A 2612 FIRE DETECTOR FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU NR 1 ENGINE MALFUNCTIONED W F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 AU S (AUS) NR 1 ENGINE FIRE WARNING ON STARTUP. FIRE BOTTLES ACTIVATED. INSPECTION COULD FIND NO EVIDENCE OF FIRE. INVESTIG ATION FOUND THE ENGINE INNER COWLING FIRE WARNING SENSING ELEMENT FAILED THE INSULATION TEST. 2 L 7 2 4F 4 F RT A20EU E2EU 2002020500165 20020205 00165 EU 2002 2 5 AUS20011398 1 20011113 A 3260 WARNING SYSTEM FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU MLG FAULTY W O OTHER N FALSE WARNING CR CRUISE 1 AU S (AUS) RT MAIN LANDING GEAR LIGHT REMAINED ON AFTER GEAR RETRACTION. INVESTIGATION COULD FIND NO POSITIVE CAUSE OF DEFECT . 2 L 7 2 4F 4 F RT A20EU E2EU 2002020500172 20020205 00172 EU 2002 2 5 AUS20011413 1 20010804 A 2760 95442581 CONTROLLER FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU DRAG CONTROL SYS FAULTY W O OTHER F FLT CONT AFFECTED CR CRUISE 1 AU S 1138 (AUS) LIFT DUMPER BARBER POLE REMAINED ON' AFTER LOCK SWITCH MOVED TO LOCKED POSITION. SUSPECT CAUSED BY FAULTY LIFT DU MPER CONTROL BOX. 2 L 7 2 4F 4 F RT A20EU E2EU 2002020500173 20020205 00173 NM 2002 2 5 AUS20011421 1 20011026 A 7312 312007501 FUEL HEATER PWA PW123D DHAV DHC8 DHC8* NM PWA 120 PW123D 52152 NE FUEL HEATER FAULTY W O OTHER J WARNING INDICATION NR NOT REPORTED 1 AU S 41 (AUS) NR 2 ENGINE FUEL HEATER FAULTY. 2 H 7 2 4T 4 T RT A13NM E20NE 2002020500174 20020205 00174 EU 2002 2 5 AUS20011423 1 20011023 A 3234 LEVER FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU MLG OBSTRUCTED W O OTHER O OTHER CL CLIMB 1 AU S (AUS) LANDING GEAR LEVER OBSTRUCTED. 2 L 7 2 4F 4 F RT A20EU E2EU 2002020500175 20020205 00175 EU 2002 2 5 AUS20011425 1 20010829 A 5330 SKIN FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) FUSELAGE SKIN CRACKED AT THE 12 O'CLOCK POSITION BETWEEN STA 3845 AND STA 4875. CRACK LENGTH APPROXIMATELY 76.2MM (3IN). 2 L 7 2 4F 4 F RT A20EU E2EU 2002020500176 20020205 00176 EU 2002 2 5 AUS20011430 1 20011003 A 3230 SPRING FOKKER F28 F28MK4000 4990810 EU RROYCE SPEY SPEY55515 54521 EU RT MLG BROKEN W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT MAIN LANDING GEAR DOOR UPLOCK LATCH OVERCENTRE SPRING BROKEN. 2 L 7 2 4F 4 F RT A20EU E2EU 2002020500177 20020205 00177 EU 2002 2 5 AUS20011431 1 20011012 A 3620 A74172425 LINE FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU PNEUMATIC INDICA CRACKED W O OTHER J WARNING INDICATION CL CLIMB 1 AU S (AUS) PNEUMATIC SYSTEM BACKUP VALVE TO STUB WING SENSE LINE CRACKED AT FLARE. 2 L 7 2 4F 4 F RT A20EU E2EU 2002020500179 20020205 00179 NM 2002 2 5 AUS20011443 1 20011224 A 7540 7506593 SWITCH PWA PW123D DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE HAMSTD 14SF 14SF23 NE BLEED AIR SYS FAILED W O OTHER J WARNING INDICATION CL CLIMB 1 AU S 9036 (AUS) NR 1 BLEED AIR SYSTEM TEMPERATURE OVERHEAT SWITCH FAILED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002020500181 20020205 00181 EU 2002 2 5 AUS20011448 1 20011209 A 3520 90000200718 REGULATOR FOKKER F28 F28MK4000 4990810 EU RROYCE SPEY SPEY55515 54521 EU PAX OXYGEN FAULTY W O OTHER O OTHER CR CRUISE 1 AU S 3526 095 (AUS) PASSENGER OXYGEN BOTTLE EMPTY. INVESTIGATION FOUND A FAULTY REGULATOR. 2 L 7 2 4F 4 F RT A20EU E2EU 2002020500182 20020205 00182 EU 2002 2 5 AUS20011450 1 20011212 A 5532 SKIN AIRBUS 310 A310324 3930206 EU PWA 4152 PW4152 NE VERTICAL STAB DELAMINATED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) VERTICAL STABILISER LEADING EDGE SKIN DELAMINATED. 2 L 7 2 4F RT A35EU E24NE 2002020500189 20020205 00189 NM 2002 2 5 AUS20011461 1 20011223 A 1400 NUT BOEING 727 727277 138408S NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) VERTICAL STIFFENER ANCHOR NUT ATTACHMENT POINT CORRODED BEYOND LIMITS. 2 L 7 3 4F 4 F RT A3WE E2EA 2002020500190 20020205 00190 NM 2002 2 5 AUS20011462 1 20011223 A 5340 69144581 ATTACH ANGLE BOEING 727 727277 138408S NM PWA JT8 JT8D15 52051 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) SKIN SUPPORT ANGLE CRACKED AT OUTBOARD END DUE TO HEAVY CORROSION ON THE RADIUS. CRACK LENGTH 63.5MM (2.5IN). 2 L 7 3 4F 4 F RT A3WE E2EA 2002020500205 20020205 00205 NM 2002 2 5 P2EA2001M0013 1 20011203 A 2720 65C37059 PCU BOEING 737 7372Q8 138448K NM RUDDER A P2EA K NONE O OTHER TX TAXI/GRND HDL 1 CE 05 121NJ 4668 21735 FLIGHT 350 AT AUS DURING PRE-FLIGHT CHECK THE FLIGHT CREW REPORTED A LATERAL VIBRATION WHEN RUDDER PEDALS WERE BUMPED. C REW SELECTED RUDDER STAND-BY AND FLUTERING OF RUDDER STOPPED. REMOVED AND REPLACED THE RUDDER PCU I.A.W. BMM 27-21-91 OP S AND LEAK CHECKS GOOD. 2 L 7 2 4F RT A16WE 2002020500211 20020205 00211 GL 2002 2 5 KW32002F00000 1 20011202 A 2730 JACKSCREW BOMBDR BD700 BD7001A10 1390006 GL RROYCE BR700 BR700710A110 NE ACTUATOR GALLED B KW3R K NONE O OTHER IN INSP/MAINT 1 WP 07 701WH 0016 9010 UPON INSPECTION OF HORIZONTAL STABILIZER PITCH TRIM ACTUATOR, THE PITCH TRIM ACTUATOR JACK SCREW THREADS WERE FOUND TO H AVE EXCESSIVE GALLING. 2 L 7 2 4F 4 F RT T00003NY E00057EN 2002020500212 20020205 00212 NE 2002 2 5 MVI2001F00000 2 20011128 A 7314 SHAFT BOEING 727 72725C 138400H NM PWA JT8 JT8D7A 52053 NE FUEL PUMP SHEARED B MV1R O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION AP APPROACH 1 EA 17 40 1000 19854 653901 AFTER NORMAL APPROACH WITH A GO AROUND FROM 501 AGL, FULL ENGINE POWER WAS ATTAINED ON ALL ENGINES. AT 700 FT, FE NOTED EPR ROLLBACK ON NR 3 ENGINE. ENGINE SUBSEQUENTLY WOULD NOT RESPOND TO POWER SETTINGS AND WAS SHUTDOWN. INSPECTION FOU ND FUEL PUMP DRIVE SHAFT SHEARED. NO DRIVE TO FUEL CONTROL WHICH PUT FUEL CONTROL IN FAIL SAFE PROTECTION MADE. FUEL P UMP WAS SCHEDULED FOR INSPECTION IAW AD, BUT FAILED PRIOR TO ACCOMPLISHED. 2 L 7 3 4F 4 F A3WE E2EA 2002020500213 20020205 00213 EU 2002 2 5 MZA2002F00000 1 20011211 A 3222 1488TOLT SENSOR AIRBUS 320 A320* EU IAE V2500 V2500A1 NE NLG FAILED A MZAR A UNSCHED LANDING O OTHER CL CLIMB 1 SO 09 4616 479 AFTER ROTATION LANDING GEAR HANDLE COULD NOT PHYSICALLY BE MOVED. ECAM 4G SHOCK ABSORBER FAULT. FOUND LGCIV AND GROUND PROX. SENSOR BAD. 2 L 7 2 4F 4 F RT A46NM E311NE 2002020500214 20020205 00214 NE 2002 2 5 N9W2002F00000 2 20010813 A 7320 30770741 RING GEAR HONEYWELL ISRAEL 1124 1124A 4500103 EU GARRTT TFE731 TFE73131G 29003 NE COMPRESSOR FAILED E N9WA E ENGINE SHUTDOWN O OTHER NR NOT REPORTED 1 EA 11 407W 6553 2803 P77572 407 P77572 ENGINE SHUT DOWN DUE TO FAN SHAFT RING GEAR PN 30770774-1 CAME APART. THE CAUSE OF FAILURE IS NOT KNOWN. PARTS SENT TO MFG FOR ANALYSIS. 2 M 7 2 4F 4 F A2SW E6WE 2002020500215 20020205 00215 EA 2002 2 5 NSV2002F00000 2 20011231 A 7310 3040637 LINE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA LT ENGINE CHAFED A NSVA O OTHER K FLUID LOSS NR NOT REPORTED 1 EA 27 207CJ UC107 32316 MECHANIC FOUND EVIDENCE OF FUEL DRIPPING FROM LEFT ENGINE NACELLE. REMOVED AND REPLACED FUEL LINE, RAN UP, LEAK CHECKED GOOD. (CONTROL NR NSVA 02-03) 2 L 7 2 4T 4 T RT A24CE E4EA 2002020500216 20020205 00216 EU 2002 2 5 O3X2001F00000 1 20011206 A 7603 13769E432 CONTROL CABLE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE331* 01514 WP POWER LEVER BROKEN A O3XA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 03 875JX 26122 1990 875 P66365 AIRCRAFT PREPARED TO DEPART GATE, AS THE POWER LEVERS WERE PUSHED FORWARD. THE CREW NOTICED THAT THE LT ENGINE WAS NOT RESPONDING TO THE INPUT. DURING INSPECTION BY MAINTENANCE PERSONNEL. THE LT POWER LEVER CABLE WAS FOUND SHEARED. THE CABLE HAD SHEARED APPROX. 12 INCHES FROM THE ATTACHMENT POINT OF THE POWER LEVER ARM WHERE THE FIRST UNDER FLOOR CABLE PULLEY IS LOCATED. THESE CABLES ARE SUBJECT OF AD (10,000 CYCLES LIFE LIMIT) THIS CABLE HAD 6125 CYCLES REMAINING. TH E CABLE WAS REPLACED WITH NEW TYPE (PN 1379164E408) AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 3 T RT A56EU E2WE 2002020500217 20020205 00217 NM 2002 2 5 O4H2002F00000 1 20010618 A 3246 2602540 WHEEL BOEING 737 737317 138447P NM MLG FAILED E O4HR O OTHER O OTHER NR NOT REPORTED 1 SW 09 664WN 23495 MAIN WHEEL ASSEMBLY, THROWN TREAD AND 4 BROKEN TIE BOLTS. THROWN TREAD DUE TO LOW PRESSURE CAUSED BY PACKING EXTRUSION PACKING EXTRUSION CAUSED BY BROKEN TIE BOLTS. BROKEN TIE BOLTS CAUSE IS UNDETERMINED. PENDING ENGINEERING EVALUATION. 2 L 7 2 4F RT A16WE 2002020500218 20020205 00218 CE 2002 2 5 OIZ2002F00000 1 20011209 A 7830 234232005 THRUST REVERSER RKWELL NA265 NA265 6402602 CE LEFT ENGINE FAILED E OIZA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 19 891GY NA65 ON LANDING ROLLOUT, THE AIRCRAFT HAD A NOTICEABLE YAW JUST AFTER SELECTION OF THE THRUST REVERSERS. AFTER STOPPING AT F BO IT WAS DISCOVERED THAT THE LEFT THRUST PART OF THE LEFT THRUST REVERSER WAS MISSING FROM THE LEFT ENGINE. THE PROBLE M HAPPENED AT NIGHT AND THE AIRCRAFT WAS INSPECTED THE NEXT DAY DURING DAYLIGHT HOURS. IT WAS NOTED THAT SOME OF THE BO LTS SECURING THE PART OF THE THRUST REVERSER MAY HAVE BEEN CRACKED AND THAT MAY HAVE LEAD TO FAILURE OF THE REMAINING BO LTS. THE AIRCRAFT WILL BE REPAIRED BY MFG AND FULL REPORT REQUESTED TO ATTACH TO THIS REPORT FOR COMPLETE AND DETAILED EXPLANATION.(WP192002B0472) 2 L 7 2 4J A2WE 2002020500219 20020205 00219 CE 2002 2 5 OYG2002F00000 1 20011205 A 7110 COWLING BEECH 1900 1900 1154160 CE NACELLE CRACKED A OYGR K NONE O OTHER IN INSP/MAINT 1 SO 35 199GA UB13 SEVERAL CRACKS WERE FOUND ON THE INSIDE OF THE AIR INLET COWL (HOT LIP) THESE CRACKS RUN HORIZONTALLY AND VERTICALLY ALO NG THE WELD THE POSSIBLE CAUSE MIGHT BE THE HARMONICS OF THE VIBRATIONS FROM THE ENGINE AND PROPELLER. POSSIBLY GOING T O A THICKER GAUGE OF METAL MIGHT STRENGTHEN THE AREA SINCE HIGH TEMPERATURES AND VIBRATIONS ARE FOUND IN THE AREA. 2 L 7 2 4T RT A24CE 2002020500230 20020205 00230 NE 2002 2 5 AALA20011859 2 20011005 A 7200 ENGINE BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E437 54555 NE LEFT FLAMED OUT A AALA F ACTIVATE FIRE EXT. X ENGINE FLAMEOUT LD LANDING 1 SW 21 654AA 24612 LAX - FLT 2469 - EN ROUTE DFW-LAX - ON LANDING, LEFT ENGINE FLAMED OUT. DISCHARGED FIRE BOTTLE. LANDED LAX WITHOUT FUR THER INCIDENT. REPLACED LEFT ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2002020600001 20020206 00001 SW 2002 2 6 AUS20011377 1 20011121 A 5510 NAS120215 FASTENER SWRNGN SA227 SA227AC 8780603 SW HORIZONTAL STAB SHEARED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) HORIZONTAL STABILISER FORWARD SPAR FASTENER HEAD SHEARED OFF. 2 L 7 2 4T RT A8SW 2002020600002 20020206 00002 NE 2002 2 6 AUS20011381 2 20011222 A 7321 B1480 BOLT RROYCE RB211524D4 BOEING 747 747338 NM RROYCE RB211 RB211524D419 54555 NE FUEL CONTROL LOOSE W O OTHER K FLUID LOSS CL CLIMB 1 AU S 9412 B1480 (AUS) NR 1 ENGINE FUEL FLOW REGULATOR (FFR) TO FUEL PUMP PIPE LEAKING. INVESTIGATION FOUND A LOOSE PIPE RETAINING BOLT O N THE FFR. 2 L 7 2 4F 4 F RT A20WE E12EU 2002020600005 20020206 00005 NM 2002 2 6 AUS20011387 1 20011223 A 3246 26123012 WHEEL BOEING 737 737* NM GE CFM56 CFM567B24 NE MLG LEAKING W O OTHER O OTHER LD LANDING 1 AU S (AUS) NR 2 TIRE FLAT. INVESTIGATION FOUND THE WHEEL VALVE STEM CORE LEAKING. 2 L 7 2 4F 4 F RT A16WE E00055EN 2002020600007 20020206 00007 NE 2002 2 6 AUS20011389 2 20011226 A 7200 UL23537 FAIRING BOEING 747 747438 NM RROYCE RB211 RB211524G19 NE NR 1 ENGINE SEPARATED W C ABORTED TAKEOFF E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS TO TAKEOFF 1 AU S (AUS) NR 1 ENGINE RT TRANSFER DRIVE FAIRING SEPARATED. LT TRANSFER DRIVE FAIRING DAMAGED AND ONLY PARTIALLY ATTACHED. P ART NUMBERS OF FAIRINGS; UL23537 AND PNO UL23538. DAMAGE WAS FOUND ON SHAFTS AND PLUMBING IN THE AREA OF THE TRANSFER DR IVE AND THE INA. 2 L 7 4 4F 4 F RT A20WE E30NE 2002020600012 20020206 00012 EU 2002 2 6 AUS20011401 1 20011230 A 2750 676801007 CONTROL UNIT BAC 146 146100A 1500260 EU LYC ALF502 ALF502R5 41580 NE TE FLAPS FAULTY W O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 AU S (AUS) TRAILING EDGE FLAP CONTROL UNIT FAULTY. 2 H 7 4 4F 4 F RT A49EU E6NE 2002020600017 20020206 00017 EU 2002 2 6 AUS20011409 1 20010802 A 2913 57150 PUMP FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU HYDRAULIC SYS MALFUNCTIONED W O OTHER K FLUID LOSS NR NOT REPORTED 1 AU S 2849 (AUS) NR 1 ENGINE NR 2 HYDRAULIC SYSTEM PUMP LOW PRESSURE. 2 L 7 2 4F 4 F RT A20EU E2EU 2002020600019 20020206 00019 EU 2002 2 6 AUS20011416 1 20010808 A 3260 602EN166 DOWNLOCK SWITCH FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU NLG INTERMITTENT W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 AU S (AUS) NOSE LANDING GEAR DOOR DOWNLOCK MICROSWITCH INTERMITTENT IN OPERATION. 2 L 7 2 4F 4 F RT A20EU E2EU 2002020600020 20020206 00020 EU 2002 2 6 AUS20011417 1 20010930 A 2780 CONNECTOR AIRBUS 310 A310324 3930206 EU PWA 4152 PW4152 NE LE SLATS DAMAGED W O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 AU S (AUS) HIGH SPEED VALVE CONNECTORS HAD HIGH RESISTANCE. 2 L 7 2 4F RT A35EU E24NE 2002020600022 20020206 00022 EU 2002 2 6 AUS20011422 1 20011028 A 2612 CONNECTOR FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU NR 1 ENGINE SHORTED W A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 AU S (AUS) NR 1 ENGINE FIRE WARNING PANEL TEST SWITCH CONNECTION SHORT CIRCUITING. FALSE FIRE WARNING RESULTED IN OPERATION O F THE FIRE EXTINGUISHER. 2 L 7 2 4F 4 F RT A20EU E2EU 2002020600023 20020206 00023 EU 2002 2 6 AUS20011424 1 20011110 A 2740 SWITCH FOKKER F28 F28MK4000 4990810 EU RROYCE SPEY SPEY55515 54521 EU STABILIZER STICKING W O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 AU S (AUS) HORIZONTAL STABILISER SWITCH STICKING. 2 L 7 2 4F 4 F RT A20EU E2EU 2002020600024 20020206 00024 EU 2002 2 6 AUS20011426 1 20010830 A 3260 BULB FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU MLG INDICATOR UNAPPROVED PART W O OTHER W INADEQUATE Q C NR NOT REPORTED 1 AU S (AUS) LT MAIN LANDING GEAR DOWNLIGHT FITTED WITH INCORRECT PART NUMBER BULB. UNAPPROVED PART. 2 L 7 2 4F 4 F RT A20EU E2EU 2002020600025 20020206 00025 EU 2002 2 6 AUS20011428 1 20010901 A 3260 WIRE FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU MLG BROKEN W A UNSCHED LANDING O OTHER CL CLIMB 1 AU S (AUS) LANDING GEAR ANTI-RETRACTION SUPPRESSION DIODE WIRE BROKEN OFF AND INSULATION WASHERS BADLY WORN. 2 L 7 2 4F 4 F RT A20EU E2EU 2002020600026 20020206 00026 2002 2 6 AUS20011429 4 20011003 A 3451 INDICATOR FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU DME/TACAN SYSTEM FAULTY W O OTHER O OTHER AP APPROACH 1 AU S (AUS) DME SYSTEM FAULTY. 2 L 7 2 4F 4 F RT A20EU E2EU 2002020600028 20020206 00028 EU 2002 2 6 AUS20011434 1 20011129 A 4990 OIL TANK FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU APU LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 AU S (AUS) APU OIL TANK LEAKING. 2 L 7 2 4F 4 F RT A20EU E2EU 2002020600029 20020206 00029 EU 2002 2 6 AUS20011435 1 20011201 A 2820 CONTROL UNIT AIRBUS 310 A310324 3930206 EU PWA 4152 PW4152 NE AUTO FUEL FEED FAULTY W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) AUTO FUEL FEED FAILS DURING DESCENT. 2 L 7 2 4F RT A35EU E24NE 2002020600030 20020206 00030 NM 2002 2 6 AUS20011437 1 20011230 A 5710 H11 BOLT BOEING 747 747338 NM RROYCE RB211 RB211524D419 54555 NE WING SHEARED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) H11 BOLT LOCATED AT STN 1241/LBBL 127/WL 163 SHEARED. FOLLOWING REMOVAL OF THE BOLT CORROSION WAS FOUND IN THE BU LKHEAD FITTING BORE. FOUND DURING ULTRASONIC INSPECTION. 2 L 7 2 4F 4 F RT A20WE E12EU 2002020600031 20020206 00031 SW 2002 2 6 AUS20011438 1 20011126 A 3242 M834611216 O-RING GOODYEAR 50116401 SWRNGN SA227 SA227* SW BRAKE ASSY WORN W O OTHER K FLUID LOSS NR NOT REPORTED 1 AU S DEC84794 (AUS) NR 4 BRAKE ASSEMBLY PISTON O-RING SEAL WORN AND LEAKING. 2 L 7 2 4T RT A5SW 2002020600034 20020206 00034 SO 2002 2 6 2002F00101 1 20011225 A 2750 FLAP PIPER PA25 PA25235 7102504 SO WING MALFUNCTIONED A MASA K NONE F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 SW 07 7219Z 253136 FLT 5629 - PHX-COS - INBOUND TO COS, THE CREW REPORTED A FLAP FAIL CAUTION MESSAGE. THE CREW DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY. ON CALL, MAINTENANCE PERFORMED PART 'A' OF THE AD, RESET THE SYSTEM AND THERE WERE NO FURTHER MESS AGES OF DEFECTS NOTED. OPS CHECKED GOOD AND THE AIRCRAFT RETURNED TO SERVICE. (M) 1 L 7 1 3O 2A10 2002020600037 20020206 00037 SO 2002 2 6 2002F00099 1 20011219 A 2750 ECU EMB 145 EMB145LR 3260212 SO T/E FLAP FAILED A MASA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SW 07 832MJ 145310 FLT 5864 - HSV-CLT - IN CRUISE FLIGHT, THE CREW REPORTED A FLAP FAIL CAUTION MESSAGE. THE CREW DECLARED AN EMERGENCY AN D THE AIRCRAFT LANDED UNEVENTFULLY WITH FLAPS UP. MAINTENANCE REMOVED AND REPLACED THE FECU AND OPS CHECK GOOD. (M) 2 L 7 2 4T RT T00011AT 2002020600047 20020206 00047 NM 2002 2 6 AUS20011442 1 20011228 A 2520 SEAT BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL CABIN DAMAGED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) PASSENGER SEATS LOCATED AT 34JK AND 35JK WILL NOT LOCK IN THE UPRIGHT POSITION. 2 L 7 2 4F 4 F RT A1NM E23EA 2002020600050 20020206 00050 EU 2002 2 6 AUS20011444 1 20011129 A 2110 3269B0102 COMPRESSOR AMD FALC50 FALCON900 2700160 EU AIR CON SYS LEAKING W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AU S 2410 158 (AUS) AIR CONDITIONING SYSTEM TURBO COMPRESSOR OIL LOSS. SUSPECT CAUSED BY FAILURE OF AN INTERNAL SEAL. RAAF AIRCRAFT RE GISTRATIONA26-074. 2 L 7 3 4F RT A46EU 2002020600052 20020206 00052 EU 2002 2 6 AUS20011449 1 20011201 A 2820 CONTROL UNIT AIRBUS 310 A310324 3930206 EU PWA 4152 PW4152 NE AUTO FUEL FEED FAULTY W O OTHER J WARNING INDICATION DE DESCENT 1 AU S (AUS) AUTO FUEL FEED MALFUNCTION. LIMITED INFORMATION PROVIDED. 2 L 7 2 4F RT A35EU E24NE 2002020600125 20020206 00125 NM 2002 2 6 USAASB01319 1 20011120 A 3260 655825029 CIRCUIT BOARD BOEING 737 737301 1384611 NM E/E BAY DIRTY A USAA O OTHER N FALSE WARNING AP APPROACH 1 EA 19 558AU 23512 ATL - FLT 655 - IN PREPARATION FOR LANDING AT ATL, FROM PIT, CREW REPORTED BOTH THE GREEN AND RED GEAR LIGHTS ILLUMINATE D AND REMAINED ON AFTER GEAR EXTENSION. CREW RECYCLED GEAR AND RECEIVED NORMAL GEAR INDICATION OF ALL GREEN AND NO RED. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND CLEANED LANDING GEAR LOGIC CARD M986. CHECKS GOOD PER MM 32- 09-20. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2002020600129 20020206 00129 NM 2002 2 6 OZIA200141006 1 20011225 A 2435 8160121 STARTER GEN ALIDSG DORNER DO32 DO328300 NM APU FAILED A OZIA K NONE O OTHER UK UNKNOWN 1 CE 05 410Z 2251 536 P196 3125 APU starter/generator inoperative. Removed and replaced unit.In addition to normal wear as compared to other units at ov erhaul, the following items were noted on teardown report:Commutator pitted and heavily groovedDrive and bearing retaine r damagedSpeed sensor assembly and speed sensor disc damagedArmature out of balanceBearings dry and heavily contaminated Catastrophic DE bearing failureDamage due to bearing failure 2 H 7 2 4T RT A55NM 2002020600146 20020206 00146 NM 2002 2 6 USAASB01321 1 20011120 A 3397 WIRE BOEING 737 7372B7 1384560 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 268AU 22880 PVD - THE EMERGENCY LIGHT AT SEAT 12 WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE. (M) 2 L 7 2 4F A16WE 2002020600147 20020206 00147 NM 2002 2 6 USAASB01322 1 20011122 A 3350 S106 BATTERY BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 282AU 23115 TPA - THE EMERGENCY EXIT LIGHT ABOVE THE FORWARD ENTRY DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT B ATTERY. (M) 2 L 7 2 4F A16WE 2002020600148 20020206 00148 NM 2002 2 6 USAASB01328 1 20011128 A 3350 500000043 CHARGER BOEING 737 737201 1384454 NM CABIN FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 22756 LGA - THE MID CABIN AISLE EMERGENCY EXIT SIGN FLICKERED ON AND OFF. MAINTENANCE REPLACED THE EMERGENCY EXIT SIGN CHARGE R. (M) 2 L 7 2 4F A16WE 2002020600149 20020206 00149 NM 2002 2 6 USAASB01335 1 20011205 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 445US 24863 CLT - FOUND EMERGENCY LIGHTS FROM ROW 12 THROUGH ROW 18 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER. (M) 2 L 7 2 4F RT A16WE 2002020600150 20020206 00150 NM 2002 2 6 USAASB01336 1 20011204 A 3260 189915 DOWNLOCK SENSOR BOEING 737 737301 1384611 NM NLG INTERMITTENT A USAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 19 337US 23235 CLT - FLT 841 - ON APPROACH TO CLT, WHEN THE GEAR WAS EXTENDED, THE CREW RECEIVED GREEN INDICATIONS FOR THE MAIN GEAR AN D RED FOR THE NOSE GEAR. ON THE GO-AROUND, THE GEAR WAS CYCLED, AT WHICH TIME THE NOSE GEAR APPEARED RED, THEN CHANGED TO GREEN. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NOSE GEAR LOCK SENSOR. (M) 2 L 7 2 4F RT A16WE 2002020600151 20020206 00151 NM 2002 2 6 USAASB01337 1 20011206 A 3260 806002 CIRCUIT BOARD BOEING 737 7374B7 1384702 NM E/E BAY FAULTY A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 438US 24560 PBI - FLT 714 - AFTER TAKEOFF FROM PBI, EN ROUTE TO CLT, THE LANDING GEAR LEVER WOULD NOT MOVE TO THE UP POSITION TO RAI SE THE GEAR. FOLLOWED QRH PROCEDURES AND DID NOT ATTEMPT TO USE OVERRIDE BECAUSE THE TAKEOFF CONFIGURATION WARNING HORN SOUNDED WITH THE FLAPS FULLY RETRACTED. FLIGHT RETURNED TO FIELD AT PBI AND LANDED WITHOUT FURTHER INCIDENT. WHILE TA XIING IN, THE AIRCRAFT WOULD NOT ACCEPT APU POWER ON THE LEFT BUS. ALL OTHER SYSTEMS APPEARED NORMAL. MAINTENANCE PERF ORMED A DETAILED INSPECTION OF THE LANDING GEAR AND WHEEL WELLS. FOUND AN AIR/GROUND SENSE FAULT ON THE E-11 SHELF. RE MOVED, INSTALLED AND TESTED M991 AIR SENSING SQUAT SWITCH LOGIC CARD PER MM 32-09-20. OPERATIONAL TEST GOOD. (M) 2 L 7 2 4F RT A16WE 2002020600152 20020206 00152 NM 2002 2 6 USAASB01338 1 20011211 A 3350 20131A BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 782AU 25021 BWI - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT ROWS 6 THROUGH 9, THE LEFT ESCAPE HATCH EXIT LIGHT AND THE CENTER O VERHEAD EXIT LIGHT AT EMERGENCY ROWS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE M1134 BATTERY PACK IN CEILING, L EFT SIDE, AT EMERGENCY ROWS. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002020600153 20020206 00153 NM 2002 2 6 USAASB01340 1 20011216 A 2810 20C1444 CHECK VALVE BOEING 737 7373B7 1384580 NM CTR FUEL TANK FAILED A USAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 EA 19 523AU 23858 PIT - FLT 744 - AFTER TAKEOFF FROM PIT, THE TOWER OBSERVED A FUEL STREAM COMING FROM THE RIGHT WING. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED BUT EQUIPMENT WAS CALLED TO THE FIELD. MAINTENAN CE TROUBLESHOT SYSTEM AND FOUND FUEL MIGRATING FROM THE CENTER FUEL TANK TO THE RIGHT FUEL TANK. REMOVED AND REPLACED T HE RIGHT INBOARD FUEL BOOST PUMP CHECK VALVE PER MM 28-22-71. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002020600154 20020206 00154 NM 2002 2 6 USAASB01341 1 20011219 A 3350 1012721 LIGHT BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 396US 23318 PHL - FOUND SEAT MOUNTED EMERGENCY EXIT SIGN INOPERATIVE AT LEFT OVERWING EXIT. MAINTENANCE REPLACED THE LIGHT ASSEMBLY . OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002020600155 20020206 00155 NM 2002 2 6 USAASB01342 1 20011219 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 445US 24863 CLT - FOUND EMERGENCY LIGHTS FROM SEAT ROWS 13 THROUGH 19 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK (P/N 2013- 1A) AND CHARGER ASSEMBLY. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2002020600156 20020206 00156 NM 2002 2 6 USAASB01343 1 20011218 A 2120 ODOR BOEING 737 737401 1384701 NM CABIN DETECTED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 418US 23985 CLT - FLT 222 - EN ROUTE FROM MCO TO CLT,PASSENGERS AND FLIGHT ATTENDANTS NOTED A STRONG SMELL OF FUEL NEAR ROW 6. MAIN TENANCE RAN THE PACKS WITH THE APU AND THE ENGINES AND COULD NOT DUPLICATE THE SMELL. A GENERAL INSPECTION WAS PERFORME D WITH NO DISCREPANCIES FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2002020700001 20020207 00001 EU 2002 2 7 CA011003005 1 20010914 A 2740 1110043A1 CONTROL UNIT FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU HORIZONTAL STAB STICKING W O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 CA 11425 (CAN) AIRCRAFT REPORTED TO HAVING THE FLIGHT MASTER CAUTION LIGHT ILLUMINATED ALONG WITH BOTH STAB CONTROL CAUTION LIGHT S ON TAKEOFF OUT OF TORONTO (YYZ). THE AIRCRAFT RETURNED TO TORONTO FOR AN UNEVENTFUL LANDING. THE HORIZONTAL STABILIZER CONTROL UNIT WAS REPLACED AS PER FOKKER F28 MAINTENANCE MANUAL 27-42-01 IN YYZ. THE AIRCRAFT WAS RELEASED SUBJECT TO SA TISFACTORY TEST FLIGHT AND THEN SATISFACTORY TEST FLIGHT WAS COMPLETED. 2 L 7 2 4F 4 F RT A20EU E2EU 2002020700003 20020207 00003 NM 2002 2 7 CA011010002 1 20011007 A 3230 189929 UPLOCK SENSOR BOEING 737 737200 1384453 NM PWA JT8 JT8D17 52049 NE MLG FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) SHORTLY AFTER TAKEOFF DUE TO UNSAFE LT MLG INDICATION. CREW REPORTED ON CLIMB OUT LEFT MAIN GEAR RED UNSAFE LIGHT ILLUMINATED AFTER GEAR LEVER SELECTED UP. DECISION MADE TO RETURN TO YEG & A/C LANDED W/O INCIDENT. MAINTENANCE INSPECTI ON REVEALED PROBLEM WITH MLG UPLOCK SENSOR ON LEFT GEAR. A/C FERRIED TO YYC. MAINTENANCE IN YYC REPLACED UPLOCK SENSOR AND COMPLETED GEAR SWINGS. SYS GROUND CHECKED SERVICEABLE & A/C RETURNED TO SERVICE WITH NO FURTHER INCIDS TORPT. 2 L 7 2 4F 4 F A16WE E2EA 2002020700024 20020207 00024 NM 2002 2 7 CA011012010 1 20010829 A 5311 FRAME BOEING 727 72722 1384002 NM PWA JT8 JT8D7B 52053 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING INSPECTION, A CRACK WAS FOUND AT A TOOLING HOLE IN THE BS 632 FRAME ABOVE STRINGER 11 RT. CRACK LENGTH 0.50 INCH ON ONE SIDE OF TOOLING HOLE, OTHER SIDE 0.38 INCH IN LENGTH. 2 L 7 3 4F 4 F A3WE E2EA 2002020700032 20020207 00032 NM 2002 2 7 CA011012011 1 20010829 A 5522 SKIN BOEING 65727952 BOEING 727 72722 1384002 NM PWA JT8 JT8D7B 52053 NE RT ELEVATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) 0.50 INCH CRACK FOUND IN RT ELEVATOR LOWER INBOARD SKIN. 2 L 7 3 4F 4 F A3WE E2EA 2002020700033 20020207 00033 NM 2002 2 7 CA011012012 1 20010905 A 5712 RIB BOEING 727 72722 1384002 NM PWA JT8 JT8D7B 52053 NE RT WING CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 71971 (CAN) DURING C-CHECK INSPECTION FOUND RT WING RIB CRACKED APPROXIMATELY 1.25 INCH, LOCATION AT WS 519 STR 6 LOWER FLANGE ATTACH POINT. 2 L 7 3 4F 4 F A3WE E2EA 2002020700034 20020207 00034 NM 2002 2 7 CA011012013 1 20010917 A 5310 6518622 FRAME BOEING 727 72722 1384002 NM PWA JT8 JT8D7B 52053 NE FWD CARGO DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 71971 (CAN) APPROXIMATELY 1 INCH CRACK AT FORWARD CARGO PIT DOOR CUTOUT FRAME LOCATED BS 540 BETWEEN S20 AND S21R AT DOOR STOP . 2 L 7 3 4F 4 F A3WE E2EA 2002020700038 20020207 00038 NM 2002 2 7 CA011017011 1 20010820 A 5310 WINDOW DHAV DHC8 DHC8* NM PWC 150 PW150A EA FUSELAGE PUNCTURED W O OTHER D INFLIGHT SEPARATION CR CRUISE 1 CA (CAN) IN CRUISE CABIN WINDOW AT SEAT ROW 12A, C OUTER PLY PUNCTURED. PUNCTURE OR HOLE ONE INCH LONG BY 3/8 INCH WIDE. PU NCTURE CAUSED BY NR 1 PROP SPINNER RETAINING SCREW BETWEEN BLADES 4&5.AFTER A/C LANDED, MAINTENANCE FOUND THAT ONE OF PR OP SPINNER RETAINING SCREWS HAD SEPARATED FROM SPINNER,&HAD PUNCTURED WINDOW'S OUTER PLY&STUCK IN WINDOW. SCREW REMVD&IN ST BACK IN SPINNER. WINDOW REPLACED, THE SURROUNDING WINDOW FRAME INSP FOR CRACKS, NONE FOUND, PRESSURE RUN COMPLETED. NO LEAKS NOTED. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002020700043 20020207 00043 NM 2002 2 7 CA011018005 1 20011004 A 3231 CONTROL CABLE BOEING 727 727223 1384074 NM PWA JT8 JT8D17 52049 NE NLG DOOR FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) NOSE GEAR WHEEL WELL DOORS LOWER CABLE REPLACED IN ACCORDANCE WITH MAINTENANCE MANUAL. GEAR SWING CARRIED OUT AN D CHECKED SERVICEABLE. 2 L 7 3 4F 4 F A3WE E2EA 2002020700045 20020207 00045 NM 2002 2 7 CA011018019 1 20011008 A 7921 45E041 VALVE JANITROL 28E996 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE OIL COOLER CONTAMINATED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 07840044 (CAN) WHILE CARRYING OUT A OIL FILTER PATCH INSPECTION (SCHEDULED), FOUND FIVE SOLID "SHIMS" WITHIN THE ENGINE MAIN OIL FILTER HOUSING. SHIMS ARE 0.5 INCH IN DIAMETER AND FOUR 0.030 INCH AND ONE 0.010 INCH IN THICKNESS. FOUND THAT THE SAME IDENTICAL SHIMS ARE FOUND WITHIN THE "THERMAL REGULATION VALVE ASSEMBLY", LOCATED INTEGRAL WITH OIL COOLER. AS THERE IS NO WAY SHIMS CAN COME FROM AN ASSEMBLED VALVE ASSY, WE ASSUME THAT THE FOD CAME FROM THE OIL COOLER ITSELF, COOLER HAD J UST BEEN INSTALLED IN MARCH OF THIS YEAR (OVERHAUL ASSY). WE WILL BE CONTACTING THE OVERHAUL VENDOR. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002020700046 20020207 00046 NM 2002 2 7 CA011018023 1 20011017 A 3211 69149974 SHAFT BOEING 727 727227 1384078 NM PWA JT8 JT8D9A 52048 NE MLG SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING A/C WALK AROUND BY MAINTENANCE ON A QUICK TURN FLIGHT, IT WAS DISCOVERED THAT THE PIVOT SHAFT FROM THE RT M LG UPPER TORSION LINK WAS PROTRUDING.MAINTENANCE REMOVED PIVOT SHAFT (FOUND IT SHEARED IN TWO PIECES), CARRIED OUT A DET AILED VISUAL INSPECTION OF LINK ASSY, INSTALLED NEW PIVOT SHAFT AND RETURNED A/C TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2002020700063 20020207 00063 EU 2002 2 7 USAASA01070 1 20011228 A 3350 321430 BATTERY AIRBUS 320 A320214 3930316 EU CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 118US 1264 CLT - THE AFT LEFT PSEU EMERGENCY LIGHT BATTERY SUPPLY WAS LOW. MAINTENANCE REPLACED THE AFT LEFT PSEU BATTERY SUPPLY. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002020700064 20020207 00064 EU 2002 2 7 USAASA01072 1 20011229 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319112 3930323 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 707UW 0949 TPA - THE AFT LEFT EPSU FAILED THE SELF TEST. MAINTENANCE REPLACED THE AFT LEFT EPSU. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002020700070 20020207 00070 NM 2002 2 7 USAABB01149 1 20011226 A 3350 20131A POWER SUPPLY BOEING 767 7672B7 1385107 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 655US 25257 PHL - MAINTENANCE FOUND THE FORWARD MAIN ENTRY DOOR, EXTERIOR EMERGENCY LIGHT, INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE M736 EMERGENCY LIGHTS POWER SUPPLY IN ASSOCIATION WITH MM 33-51-21. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A1NM 2002020700071 20020207 00071 NM 2002 2 7 USAABB01150 1 20011226 A 3350 20131A BATTERY PACK BOEING 767 7672B7 1385107 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 655US 25257 PHL - MAINTENANCE FOUND THE LEFT SLIDE ILLUMINATION LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PAC K. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A1NM 2002020700072 20020207 00072 NM 2002 2 7 USAABB01156 1 20011230 A 3350 8731002511REV14 SIGN BOEING 757 7572B7 1384964 NM R1 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 633AU 27811 PHL - FOUND R1 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2002020700073 20020207 00073 NM 2002 2 7 USAABB02001 1 20010104 A 3397 WIRE BOEING 767 7672B7 1385107 NM CABIN LOOSE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 656US 26847 PHL - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 9-11 INOPERATIVE. MAINTENANCE RESECURED A LOOSE WIRE AT ROW 11. (M) 2 L 7 2 4F RT A1NM 2002020700075 20020207 00075 EU 2002 2 7 USAASA01071 1 20011228 A 3350 321430 BATTERY PACK AIRBUS A321 A321211 3930370 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 161UW 1403 PVD - THE LEFT AND RIGHT BATTERY PACKS WOULD NOT TEST. MAINTENANCE REPLACED THE BATTERY PACKS. OPERATIONALLY CHECKED O K. (M) 2 L 7 2 4F RT A28NM 2002020700078 20020207 00078 NM 2002 2 7 USAASB01344 1 20011218 A 2120 O-RING BOEING 737 7373B7 1384580 NM A/C BAY FAILED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 396US 23318 PHL - FLT 735 - EN ROUTE FROM ROT TO PHL, CREW REPORTED A STRONG EXHAUST SMELL THROUGH OUT THE CABIN THAT DID NOT DISSIP ATE THE ENTIRE FLIGHT. MAINTENANCE FOUND THE RIGHT TURBO FAN DRAIN SEEPING. REMOVED AND REPLACED O-RING. CLEANED PACK BAY ON RIGHT SIDE AND REPLACED WATER SEPARATOR BAG (P/N V121-1). AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2002020700079 20020207 00079 NM 2002 2 7 USAASB01345 1 20011220 A 3350 20131A BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 353US 23556 CLT - MAINTENANCE FOUND THE END BAY EMERGENCY LIGHT AT THE AFT SEAT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE A FT LEFT BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002020700080 20020207 00080 NM 2002 2 7 USAASB01346 1 20011220 A 3350 1012721 LIGHT BOEING 737 737301 1384611 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 560AU 23514 CLT - PILOT REPORTED THE FLOOR PATH EMERGENCY LIGHTING, AT SEAT ROW 13C, IS INOPERATIVE. MAINTENANCE REMOVED AND REPLAC ED THE SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT SEAT ROW 13C. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002020700081 20020207 00081 NM 2002 2 7 USAASB01347 1 20011221 A 3350 1012623 LIGHT BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 526AU 23861 BOS - PILOT REPORTED THE EMERGENCY LIGHT OVER SEAT 10C INOPERATIVE. MAINTENANCE REPAIRED THE EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002020700082 20020207 00082 NM 2002 2 7 USAASB01348 1 20011222 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 437US 24559 TPA - MAINTENANCE FOUND THE AFT SECTION OF EMERGENCY PATHWAY LIGHTS WILL NOT EXTINGUISH. MAINTENANCE REMOVED AND REPLAC ED THE AFT LEFT BATTERY PACK (P/N 2013-1A) AND CHARGER ASSEMBLY. ALSO, REMOVED AND REPLACED THE AFT RIGHT CHARGER ASSEM BLY (P/N 11-0049) DUE TO A BLOWN FUSE. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002020700083 20020207 00083 NM 2002 2 7 USAASB01349 1 20011223 A 3397 WIRE BOEING 737 737301 1384611 NM CABIN DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 300AU 23228 BWI - PILOT REPORTED THE WIRING FOR THE EMERGENCY EXIT LIGHTS UNDER SEAT 21C IS DISCONNECTED AND THE LIGHTS ARE INOPERAT IVE. MAINTENANCE RECONNECTED AND SECURED WIRING. OPS CHECK OF LIGHTS GOOD. (M) 2 L 7 2 4F RT A16WE 2002020700084 20020207 00084 NM 2002 2 7 USAASB01350 1 20011225 A 2131 7638104 CONTROLLER BOEING 737 7373B7 1384580 NM CABIN PRESSURE FAILED A USAA B G A EMER. DESCENT O2 MASK DEPLOYED UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 518AU 23704 CLT - FLT 534 - EN ROUTE FROM PBI TO BWI, AT FL370, THE CABIN PRESSURIZATION STARTED TO CLIMB. A LOUD WHINING NOISE WAS ALSO HEARD. PRESSURIZATION WAS UNCONTROLLABLE IN MANUAL MODE. CREW DECLARED AN EMERGENCY AND AN EMERGENCY DESCENT TO FL110 WAS ACCOMPLISHED. OXYGEN MASKS WERE DEPLOYED AND THE FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER AND ACCOMPLISHED FUNCTIONAL TEST. FUNCTIONAL TEST CHECK S GOOD. (M) 2 L 7 2 4F RT A16WE 2002020700085 20020207 00085 NM 2002 2 7 USAASB01351 1 20011226 A 3350 20131A BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 337US 23235 GSO - MAINTENANCE FOUND THE EMERGENCY LIGHTS IN FIRST CLASS EXTINGUISH AFTER A SHORT PERIOD OF OPERATION. MAINTENANCE R EMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002020700087 20020207 00087 NM 2002 2 7 USAASB01352 1 20011226 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 445US 24863 CLT - DURING EMERGENCY LIGHT OPERATIONAL TEST, MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROWS 12 THROUG H 19 WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. BATTERY PACK CHECKS GOOD. O PERATIONAL CHECK OF EMERGENCY LIGHTING CHECKS GOOD. (M) 2 L 7 2 4F RT A16WE 2002020700089 20020207 00089 NM 2002 2 7 USAASB01353 1 20011226 A 3350 110049 CHARGER BOEING 737 7373B7 1384580 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 531AU 24478 DAY - MAINTENANCE FOUND THE EMERGENCY EXIT SIGNS AT THE FORWARD ENTRY DOOR AND FORWARD SERVICE DOOR INOPERATIVE. MAINTE NANCE REMOVED AND REPLACED THE FORWARD CENTER BATTERY PACK (P/N 2013-1A) AND CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002020700090 20020207 00090 NM 2002 2 7 USAASB01354 1 20011226 A 3397 WIRE BOEING 737 7374B7 1384702 NM CABIN SHORTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 437US 24559 CLT - MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 20 THROUGH 25 INOPERATIVE. MAINTENANCE FOUND WIRES SH ORTED AT SEAT ROWS 24 AND 25. REPAIRED WIRING. ALSO, REMOVED AND REPLACED AFT LEFT AND AFT RIGHT BATTERY CHARGER ASSEM BLIES (P/N 2012-1). OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002020700091 20020207 00091 NM 2002 2 7 USAASB01355 1 20011228 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 445US 24863 MIA - MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY EXIT LIGHTS AT ROWS 12 THROUGH 19 AND THE RIGHT OVERWING EMERGENCY LI GHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY CHARGER ASSEMBLIES M1136 AND M1435 PER MM 33-51-00. OPERATIO N CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002020700092 20020207 00092 NM 2002 2 7 USAASB01356 1 20011228 A 3350 1010428 LIGHT BOEING 737 737301 1384611 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 342US 23511 PHL - PILOT REPORTED THE EMERGENCY PATH LIGHT AT SEAT ROW 2C WAS BROKEN/INOPERATIVE. MAINTENANCE REMOVED AND REPLACED T HE LIGHT ASSEMBLY AT SEAT ROW 2C. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002020700093 20020207 00093 NM 2002 2 7 USAASB01357 1 20011229 A 3397 WIRE BOEING 737 737301 1384611 NM CABIN DAMAGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 340US 23237 ORD - MAINTENANCE FOUND THE EMERGENCY LIGHT AT SEAT ROW 20 INOPERATIVE. MAINTENANCE REPAIRED THE WIRING AT SEAT ROW 20. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002020800003 20020208 00003 NM 2002 2 8 CA011031020 1 20011017 A 2910 69141064 CYLINDER BOEING 737 737210C 1384459 NM PWA JT8 JT8D9A 52048 NE NLG CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) DURING PRE-FLIGHT INSPECTION HYDRAULIC FLUID WAS FOUND TO BE WEEPING FROM THE NOSE GEAR TRANSFER CYLINDER. THE ARE A WAS CLEANED AND DRIED. THE VISUAL INSPECTION DETERMINED THAT THE NOSE GEAR TRANSFER CYLINDER END CAP WAS CRACKED. THE SUSPECT COMPONENT WAS REPLACED. LANDING GEAR SWUNG. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A16WE E2EA 2002020800028 20020208 00028 WP 2002 2 8 CNMA200100038 1 20011128 A 5730 SKIN DOUG DC10 DC1030 3023501 WP LT WING CORRODED A CNMA K NONE O OTHER IN INSP/MAINT 1 SW 07 540AX 46595 FOUND CORROSION ON UPPER LEFT WING SURFACE (LEVEL 2) IN EXCESS OF SRM ALLOWABLE LIMITS IN FOUR (4) LOCATIONS. BOEING CO NTACTED AND BLEND OUT ACCOMPLISHED IAW BOEING INSTRUCTION, 8110-3 ISSUED AS PERMANENT REPAIR. 2 L 7 3 4F A22WE 2002020800042 20020208 00042 NM 2002 2 8 P5CA0200631 1 20010116 A 3350 S7356B37 LIGHT BOEING 747 747122 1384872 NM CABIN DEFECTIVE A P5CA K NONE L NO TEST IN INSP/MAINT 1 WP 23 852FT 19757 EMERGENCY LIGHT IN CEILING AFT OF P6 PANEL ILLUMINATES ONLY MOMENTARILY. REPLACED EMERGENCY LIGHT AFT OF P6. OPS CHECK OK. 2 L 7 4 4F A20WE 2002020800052 20020208 00052 NM 2002 2 8 AALA20011309 1 20010627 A 2120 CLAMP BOEING 757 757223 1384957 NM A/C BAY BROKEN A AALA K NONE J WARNING INDICATION CL CLIMB 1 SW 21 686AA 25343 DFW - FLT 2155 - EN ROUTE LGA-DFW, SHORTLY AFTER TAKEOFF DETECTED ALT WARNING IN COCKPIT. UPON DESCENT HEARD A SQUEALIN G NOISE IN COCKPIT. RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED LEFT SIDE PACK SUPPLY DUCT CLAMP. LEAK CHECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002020800053 20020208 00053 EA 2002 2 8 CA011105010 1 20011103 A 5310 85310382 BEAM DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 24062 24062 (CAN) DURING ACCOMPLISHEMENT OF TASK 5310/27D , CRACK 1.8 INCH FOUND IN TRANSVERSE BEAM & DOUBLER ASSY. CRACK TO BE REPA IRED AS PER RD8-53-2376 PRIOR TO DISPATCH. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002020800054 20020208 00054 NE 2002 2 8 CA011106001 1 20011101 A 6510 S613564019001 SUPPORT SKRSKY SKRSKY S61 S61N 8142104 NE GE CT58 CT581401 30011 NE T/R DRIVESHAFT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ON BOARD VIBRATION MONITORING SYSTEM INDICATED INCREASING VIBRATION LEVELS AT NR 2 TAIL ROTOR DRIVESHAFT HANGER. V ISUAL INSPECTION REVEALED CRACK IN AFT SUPPORT FRAME. 2 G 7 2 4U 4 U 1H15 1E3 2002020800056 20020208 00056 NM 2002 2 8 CA011107002 1 20011030 A 3231 1060779179 ROD END BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING REGULARLY SCHEDULED OVER NIGHT MAINTENANCE INSPECTION, LINE ENGINEER DISCOVERED THE RT MAIN LANDING GEAR O/ B GEAR DOOR ROD END CRACKED. MAINTENANCE REPLACED THE ROD END AS PER MM 32-13-21 AND MM 7-11-11 AND GROUND CHECKED THE S YSTEM AS SERVICEABLE. (IPC REFERENCE NUMBER; 32-10-01, ITEM 135)AIRCRAFT RETURNED BACK TO SERVICE WITH NO FURTHER INCIDE NTS TO REPORT. 2 L 7 2 4F 4 F A16WE E2EA 2002020800058 20020208 00058 NM 2002 2 8 CA011109005 1 20011024 A 5330 SKIN BOEING 727 72725C 138400H NM PWA JT8 JT8D7B 52053 NE FUSELAGE CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 65349 (CAN) DURING ROUTINE INSPECTION CORROSION WAS FOUND IN THE FUSELAGE SKIN ABOVE THE MAIN CARGO DOOR BETWEEN BS 500 AND BS 540 AND FROM STRINGER S-3L TO S-4R (LEVEL 3 CORROSION). 2 L 7 3 4F 4 F A3WE E2EA 2002020800060 20020208 00060 EU 2002 2 8 AALA20012096 1 20011201 A 3350 CHARGER AIRBUS 300 A300B4605R 3930308 EU CABIN FAILED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7062A 474 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS AT ROWS 7C THROUGH 18C DIM. REPLACED BATTERY PACK AND CHARGER. SY STEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2002020800061 20020208 00061 EU 2002 2 8 AALA20012144 1 20011206 A 3350 PIN AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7062A 474 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 31G INOPERATIVE. SECURED LOOSE PIN AT SEAT 31G. SYSTE M GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2002020800062 20020208 00062 NM 2002 2 8 AALA20012168 1 20011218 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 678AN 29428 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 10D INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT 10D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002020800063 20020208 00063 NM 2002 2 8 AALA20011964 1 20011024 A 3244 ETY2132511 TIRE BOEING 757 757223 1384957 NM RT MLG SEPARATED A AALA K NONE O OTHER TO TAKEOFF 1 SW 21 659AA 24617 ORD - FLT 181 - EN ROUTE ORD-LAX, DURING TAKEOFF NR 4 TIRE TREAD SEPARATED. CONTINUED TO LAX AND LANDED WITHOUT FURTHER INCIDENT. REPLACED NR 4 TIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. RIGHT MLG DOOR AND FLAP FAIRING DAMAGED BY RUB BER DEBRIS, BOTH COMPONENTS REMOVED PER CDL. (M) 2 L 7 2 4F RT A2NM 2002020800064 20020208 00064 EU 2002 2 8 AALA20012048 1 20011118 A 3240 DETECTOR AIRBUS 300 A300B4605R 3930308 EU MLG MALFUNCTIONED A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 18066 509 LHR - FLT 101 - BRAKE HOT LIGHT ILLUMINATED IN CRUISE FLIGHT. ECAM INDICATIONS ON WHEELS 1, 2, 5 AND 6 WERE 400-420 DEG REES. ACCOMPLISHED PROCEDURES IAW OPERATING MANUAL. INDICATIONS REMAINED UNCHANGED. REPLACED BRAKE DETECTION UNIT AND LEFT GEAR BRAKE TEMP COMPENSATOR ACCOMPLISHED. OPS CHECK TEST NORMAL PER THE MM. (M) 2 L 7 2 4F RT A35EU 2002020800065 20020208 00065 EU 2002 2 8 AALA20012088 1 20011202 A 3397 SPLICE FOKKER F28 F28MK0100 4990807 EU CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1417D 11396 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT ROW 24 INOPERATIVE. REPAIRED SPLICE AT CONNECTOR FOR EMERG ENCY EXIT LIGHTS AT ROW 24. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2002020800066 20020208 00066 NM 2002 2 8 AALA20012164 1 20011220 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 390AA 27450 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 37B HAS A BROKEN WIRE. REPAIRED EMERGENCY EXIT LIGHT WIRE A T 37B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002020800067 20020208 00067 NM 2002 2 8 AALA20012165 1 20011217 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 393AN 29430 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 19B INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 19B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002020800068 20020208 00068 NM 2002 2 8 AALA20012166 1 20011219 A 3350 LIGHT BOEING 767 767223 1385123 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 327AA 22327 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYST EM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002020800069 20020208 00069 NM 2002 2 8 AALA20012167 1 20011225 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 607AM 27058 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 34D INOPERATIVE. RESECURED EMERGENCY EXIT LIGHT CONNEC TOR AT SEAT 34D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002020800073 20020208 00073 NM 2002 2 8 AALA20012169 1 20011221 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 378AN 25447 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 26J INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT WIRE AT SEAT 26J. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002020800074 20020208 00074 NM 2002 2 8 AALA20012170 1 20011221 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 386AA 27060 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L1 DOOR INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT 2B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002020800075 20020208 00075 WP 2002 2 8 AALA20012171 1 20011223 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 552AA 53034 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUN D CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002020800076 20020208 00076 2002 2 8 AALA20012172 4 20011223 A 2565 D31038201 SLIDE DOUG DC9 DC982 3022082 WP GALLEY DOOR DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 480AA 49655 ATL - DURING OVERNIGHT MAINTENANCE, FORWARD GALLEY DOOR SLIDE PARTIALLY DEPLOYED. REPLACED FORWARD GALLEY DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002020800077 20020208 00077 WP 2002 2 8 AALA20012173 1 20011219 A 3620 10200074 ELEMENT DOUG DC9 DC982 3022082 WP NR 2 ENGINE DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 244AA 49256 SAN - FLT 481 - EN ROUTE SAN-DFW - AFTER TAKEOFF, RIGHT ENGINE SUPPLY HIGH TEMPERATURE LIGHT UNABLE TO EXTINGUISH. RETU RNED SAN AND LANDED WITHOUT FURTHER INCIDENT. REPLACED RIGHT ENGINE SUPPLY TEMPERATURE ELEMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002020800078 20020208 00078 2002 2 8 AALA20012174 4 20011222 A 3454 285T05545 CONTROL PANEL BOEING 757 757223 1384957 NM COCKPIT DEFECTIVE A AALA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 660AM 25294 SJU - FLT 495 - EN ROUTE MIA-SJU, DETECTED ELECTRICAL SMOKE IN COCKPIT. TURNED OFF COCKPIT LIGHTS. SMOKE CEASED. RETUR NED SJU AND LANDED WITHOUT FURTHER INCIDENT. REPLACED VOR PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002020800079 20020208 00079 NM 2002 2 8 AALA20012176 1 20011225 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 390AA 27450 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 32B INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT 32B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002020800080 20020208 00080 NM 2002 2 8 AALA20012177 1 20011225 A 2612 FIRE WARNING BOEING 767 767323 1385205 NM LAVATORY FALSE INDICATION A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 386AA 27060 SFO - FLT 11 - EN ROUTE SFO-JFK - FIRE WARNING INDICATION LIGHT ILLUMINATED FOR AFT LAVATORY. RETURNED SFO AND LANDED W ITHOUT FURTHER INCIDENT. INSPECTED LAVATORY WIRING, PLUMBING, AND COMPONENTS. RAN BOTH ENGINES AND PACKS. NO FAULTS N OTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002020800081 20020208 00081 WP 2002 2 8 AALA20012178 1 20011224 A 2913 314195 PUMP DOUG DC9 DC982 3022082 WP NR 2 ENGINE FAILED A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 214AA 49162 CLT - FLT 303 - EN ROUTE CLT-DFW, RIGHT ENGINE PUMP FAILED. RETURNED CLT AND LANDED WITHOUT FURTHER INCIDENT. REPLACED RIGHT HYDRAULIC PUMP. NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002020800082 20020208 00082 NM 2002 2 8 AALA20012181 1 20011226 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 332AA 22331 SFO - DURING OVERNIGHT, MAINTENANCE EMERGENCY EXIT LIGHT AT SEAT 28HJ INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT CONNEC TOR AT SEAT 28HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002020800083 20020208 00083 EU 2002 2 8 AALA20012184 1 20011229 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80052 460 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 9G INOPERATIVE. RESECURED EMERGENCY EXIT LIGHT CONNECT OR AT SEAT 9G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2002020800084 20020208 00084 NM 2002 2 8 AALA20012186 1 20011231 A 2910 4007543 HYDRAULIC LINE BOEING 757 757223 1384957 NM NR 1 ENGINE LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 620AA 24578 DFW - FLT 1086 - EN ROUTE DFW-BOS, LEFT HYDRAULIC PRESSURE DECREASED TO ZERO. RETURNED DFW AND LANDED WITHOUT FURTHER I NCIDENT. REPLACED LEFT SIDE RETURN LINE. NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002020800085 20020208 00085 WP 2002 2 8 AALA20012187 1 20011231 A 3230 LANDING GEAR DOUG DC9 DC983 3022083 WP NLG MALFUNCTIONED A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 596AA 53286 DFW - FLT 1658 - EN ROUTE DFW-TUL - SHORTLY AFTER TAKEOFF, NOSE LANDING GEAR WOULD NOT RETRACT. RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. ACCOMPLISHED GEAR RETRACTION PER THE MM. NO DEFECTS NOTED. SYSTEM GROUND CHECKED NORMAL OP ERATION. (M) 2 L 7 2 4F RT A6WE 2002021100001 20020211 00001 NM 2002 2 11 CA011114004 1 20011029 A 2131 20224783 MOTOR BOEING 767 7673S1 1385211 NM GE CF6 CF680C2B6F 30025 NE CABIN PRESSURE FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) AFTER TAKEOFF AT 14,000 FT. LOSS OF BOTH AUTO CABIN PRESSURE CONTROL SYSTEMS. AIRCRAFT RETURNED TO ZURICH. AC MOTO R 2 REPLACED AS PER AMM 21-31-03 AND CHECKED SERVICEABLE. 2 L 7 2 4F 4 F RT A1NM E13NE 2002021100002 20020211 00002 NM 2002 2 11 CA011114010 1 20010927 A 2131 CONTROLLER BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE CABIN PRESSURE FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) PRESSURE CONTROLLER FAILED ON CLIMB OUT FROM YYC. A/C RETURNED TO YYC. O2 MASKS DEPLOYED. CABIN PRESSURE CONTROLLE R FAILED FUNCTION TEST ON GROUND. REPLACED O2 MASKS AND REPLACED PRESSURE CONTROLLER. FUNCTION CHECK CARRIED OUT AND A/C RETURNED TO SERVICE. 2 L 7 2 4F 4 F A16WE E2EA 2002021100004 20020211 00004 NM 2002 2 11 CA011114011 1 20010928 A 3234 SELECTOR VALVE BOEING 737 737217 1384464 NM PWA JT8 JT8D17A 52049 NE MLG FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) LOUD NOISE AND ALL 3 GEAR INDICATION LIGHTS BOTH GREEN AND RED ILLUMINATED. A/C RETURNED TO YQR, LANDING GEAR EXTE NDED AND ALL INDICATION NORMAL. RIGGING CHECK CARRIED OUT ALL NORMAL. LANDING GEAR SELECTOR VALVE REPLACED. LANDING GEAR SWING CARRIED OUT ALL OPERATIONS AND INDICATIONS NORMAL. UNI 32-30-0554 1042. MPN 4105DA 2 L 7 2 4F 4 F A16WE E2EA 2002021100009 20020211 00009 NM 2002 2 11 CA011119007 1 20011105 A 2750 6549529 BELLCRANK BOEING 737 737201 1384454 NM PWA JT8 JT8D9A 52048 NE TE FLAPS WRONG PART W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) WHILE THE AIRCRAFT WAS ON A "C" CHECK, RT OUTBOARD FLAP INBOARD FAIRING COULD NOT BE RIGGED. AFTER INVESTIGATION F ROM THE INSPECTOR, FOUND THE WRONG BELLCARANK INSTALLED. RT OUTBOARD WAS INSTALLED AT RT INBOARD. PROPER BELLCRANK INSTA LLED, RIGGING CARRIED OUT AS PER MM 27-51-121. 2 L 7 2 4F 4 F A16WE E2EA 2002021100011 20020211 00011 NM 2002 2 11 CA011120004 1 20011116 A 2910 654476112 CONTROL UNIT BOEING 737 737297 1384480 NM PWA JT8 JT8D9A 52048 NE HYDRAULIC SYS LEAKING W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA (CAN) RETURNED TO YHM DUE TO LOSS OF 'A' SYS HYDRAULIC FLUID. SHORTLY AFTER TAKEOFF OUT OF YHM CREW NOTICED HYD MASTER CAUTION LIGHT HAD ILLUMIINATED, THE 'A' SYS HYDRAULIC FLUID HAD DEPLETED & THE HYDRAULIC LOW PRESSURE WARNING LIGHTS HA D ILLUMINATED. CREW LEVELED OFF AT 10,000 FT. &CONDUCTED 'NON-NORMAL CHECKLIST' THEN SHUTDOWN 'A' SYS HYDRAULIC PUMPS. A/C RETURNED TO YHM & LANDED WITHOUT INCIDENT. 2 L 7 2 4F 4 F A16WE E2EA 2002021100013 20020211 00013 NM 2002 2 11 CA011120012 1 20011110 A 5330 LAP JOINT BOEING 727 72725C 138400H NM PWA JT8 JT8D7B 52053 NE FUSELAGE CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 62789 (CAN) WHILE CARRYING OUT AN EXTERNAL LOW FREQUENCY EDDY CURRENT INSPECTION OF SPECIFIC LAP JOINTS. CORROSION WAS DETEC TED AT STRINGER 24 RT AND LT FROM STA 259 TO 360 AND STRINGER 4 RIGHT STA 1130 TO 1183. AIRCRAFT HAS BEEN FERRIED ON A S PECIAL FLIGHT PERMIT FOR FURTHER EVALUATION AND REPAIR. 2 L 7 3 4F 4 F A3WE E2EA 2002021100017 20020211 00017 NM 2002 2 11 CA011121010 1 20011106 A 3233 ACCESSORY UNIT BOEING 737 737217 1384464 NM PWA JT8 JT8D9A 52048 NE MLG FAILED W A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 CA (CAN) SHORTLY AFTER TAKEOFF OUT OF YYC, THE CREW EXPERIENCED DIFFICULTY GETTING THE LANDING GEAR LEVER TO REMAIN IN TH E 'UP' POSTION. THE CREW PERFORMED THE 'NON-NORMAL CHECKLIST', BUT WERE UNABLE TO RECTIFY THE PROBLEM. THE CREW ELECTED TO RETURN TO YYC AND THE AIRCRAFT LANDED WITHOUT INCIDENT - CFR WAS NOT CALLED OUT. MAIINTENANCE REPLACED THE LANDING GEAR ACCESSSORY UNIT, AND THE SYSTEM CHECKED SERVICEABLE.AIRCRAFT RETURNED TO SERVICE WITH NO FURTHER INCIDENTS TO REPO RT. 2 L 7 2 4F 4 F A16WE E2EA 2002021100024 20020211 00024 EA 2002 2 11 CA011121011 1 20011106 A 5610 6003303025 WINDSHIELD CNDAIR CL604 CL604 1900301 EA COCKPIT CRACKED W A UNSCHED LANDING D INFLIGHT SEPARATION CR CRUISE 1 CA (CAN) IN CRUISE, OUTER LAYER OF LEFT WINDSHIELD CRACKED - COMPLETED UNEVENTFUL LANDING. TEMPORARY REPAIR CARRIED OUT ON WINDSHIELD FACE PLY AS PER CH 56-10-00A-205. AIRCRAFT FERRIED BACK TO YYZ BASE AND WINDSHIELD REPLACED AND AIRCRAFT RET URNED BACK TO SERVICE. 2 L 7 2 4F RT A21EA 2002021100026 20020211 00026 EA 2002 2 11 CA011121012 1 20011108 A 5730 75300154011 PANEL DHAV DHC7 DHC7102 2802708 EA PWA PT6 PT6A50 52043 EA HAMSTD 24PF 24PF305 GL LT WING ROOT SEPARATED W O OTHER D INFLIGHT SEPARATION DE DESCENT 1 CA 25717 (CAN) ON DESCENT, A LOUD BANG WAS HEARD, FOLLOWED SHORTLY THEREAFTER BY ANOTHER SMALLER ONE. THE FLIGHT CARRIED ON TO A NORMAL APPROACH AND LANDING WITHOUT FURTHER INCIDENT. UPON INSPECTION AFTER LANDING, THE CAPTAIN NOTED THE ARMPIT PANEL WAS MISSING FROM UNDER THE LEFT WING ROOT. NO OTHER DAMAGE WAS FOUND AND MAINTENANCE WAS NOTIFIED. (PANEL LOST). 2 H 7 4 4T 4 T A20EA E4EA 6 C P1NE 2002021100030 20020211 00030 EA 2002 2 11 CA011121015 1 20011023 A 2710 6009119153 BEARING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LT AILERON FAILED W O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 CA (CAN) CREW REPORTED AILERON JAMMED IN FLIGHT, QRH CARRIED OUT SYSTEM CHECK SERVICEABLE ON THE GROUND BUT THE AIRCRAFT WA S FERRIED BACK TO MONTREAL FOR FURTHER INVESTIGATION. AN FMR TO REMOVE THE LEFT END AFT AILERON QUADRANT WAS ORDERED DUE TO THE FACT THAT A SUSPECTED CONTAMINATED BEARING OF THAT QUADRANT IS SUSPECTED TO FREEZE IN ALTITUDE. REPLACED QUADRA NT ASSEMBLY. AILERON SYSTEM RIGGED AS PER AMM 27-11-00 AIRCRAFT FOUND SERVICEABLE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021100033 20020211 00033 NM 2002 2 11 CA011121018 1 20011118 A 7500 VENT LINE BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE ENGINE CASE SEPARATED W O OTHER O OTHER NR NOT REPORTED 1 CA (CAN) MAINT IN YHM DISCOVERED NR 2 ENGINE NR 4 BEARING BREATHER VENT LINE ELBOW HAD PULLED OUT OF FAN CASE. LATER INVEST . MAINT FOUND THREADS TO BREATHER LINE HAD STRIPPED & LINE WAS NOT SECURED TO FAN CASING. ENGINEER RESECURED & SEALED LI NE TO ENGINE & COMPLETED ENGINE RUNS WITH NO LEAKS FOUND - A/C DEEMED SERVICEABLE FOR FERRY FLT TO YYC.MAINTENANCE IN YY C REPLACED ENGINE, COMPLETED ENGINE GROUND RUNS - NO LEAKS FOUND. A/C RETURNED TO SERVICE WITH NO FURTHER INCIDENTS TO R EPORT. 2 L 7 2 4F 4 F A16WE E2EA 2002021100037 20020211 00037 SO 2002 2 11 CHQ00059 1 20011207 A 3260 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO COCKPIT FALSE ACTIVATION A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 265SK 145522 LANDING GEAR AURAL WARNING DURING CLIMBOUT. PERFORMED CHECK OF LANDING GEAR WARNING SYSTEM, NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2002021100038 20020211 00038 SO 2002 2 11 CHQ00061 1 20011209 A 2611 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO E/E BAY MALFUNCTIONED A CHQA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 11 260SK 145128 AVIONICS SMOKE LIGHT CAME ON INTERMITTENTLY DURING FLIGHT, NO SMOKE OR FIRE DETECTED IN COCKPIT OR CABIN. FOLLOWED CHEC KLIST PROCEDURES. REMOVED AND REPLACED AVIONICS SMOKE DETECTOR, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2002021100039 20020211 00039 2002 2 11 CHQ00062 4 20011209 A 3425 COMPUTER EMB 145 EMB145 3260210 SO E/E BAY MALFUNCTIONED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 CHQA 145435 DURING CLIMBOUT FROM GSO PASSING THROUGH FL 180 WINDSHEAR INOP, GPWA, INOP, AND RAD ALT NR 1 FAIL MESSAGES WERE DISPLAYE D ON EICAS. AHRS COMPUTERS NR 1 AND NR 2 SWAPPED AIRCRAFT INITIALIZED AHRS TO ALN OPS CHECK GOOD ALL MESSAGES WENT OUT FROM DISPLAYS. 2 L 7 2 4F RT T00011AT 2002021100040 20020211 00040 SO 2002 2 11 CHQ00064 1 20011210 A 7830 THRUST REVERSER EMB 145 EMB145 3260210 SO NR 2 ENGINE MALFUNCTIONED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 CHQA 145500 E2 REV DISAGREE MESSAGE ON CLIMBOUT. DEFERRED E2 THRUST REVERSER. 2 L 7 2 4F RT T00011AT 2002021100054 20020211 00054 EU 2002 2 11 MALA020145 1 20010131 A 3230 UPLOCK BAC 146 AVRO146RJ85A 1500097 EU MLG CONTAMINATED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 501XJ E2208 DURING FLIGHT 3655, BOTH MAIN GEAR INTRANSIT LIGHT FAILED TO EXTINGUISH AFTER GEAR SELECTED UP. CREW FAILED TO ENTER. AIR RETURN TO DTW. MAINTENANCE FOUND BOTH UPLOCKS CONTAMINATED WITH DIRT AND SNOW. CLEANED AND LUBED, SWUNG GEAR IAW 3 2-30-00. ALL CHECKS GOOD AT THIS TIME. 2 H 7 4 4F RT A49EU 2002021100068 20020211 00068 NE 2002 2 11 RO614044 2 20011013 A 7240 213139003 COMBUSTION LINER BAG BAE146 BAE146300A 1500267 EU LYC LF507 LF5071H 41580 NE ENGINE BROKEN B K NONE M OVER TEMP NR NOT REPORTED 1 WP 28 1927 2719 LF07011 ENG RETURNED TO PHOENIX R&O MX DUE TO INCREASING TURBINE TEMP, SEEN IN THE ELC DATA. ENG RETURNED FROM CHINA AVIATION S UPPLIES CORP. CHINA NORTHWEST AIRLINES NANJING. UPON DISASSEMBLY OF THE ENG, HOT-SECTION DISTRESS WAS NOTED AND THE COM BUSTION LINER WAS FOUND TO HAVE A 6.2 INCH PIECE OF THE INNER BAFFLE BROKEN OFF. DISCOVERY OCCURRED WITH COMPLETION OF THE PRELIMINARY MATERIAL ANALYSIS REPORT (121340) ON THE FAILED LINER. BAFFLE DETAIL SEPARATED FROM COMBUSTION LINER DU E TO INSUFFICIENT WELDS & BAFFLE BROKE APART BY FATIGUE. THE BAFFLE MAY HAVE BEEN REPLACED AT HONEYWELL GREER R&O DURIN G LAST COMBUSTION LINER REPAIR, WHICH OCCURRED AT LAST ENG MX EVENT. 2 H 7 4 4F 4 F RT A49EU E6NE 2002021100070 20020211 00070 EA 2002 2 11 CA011122012 1 20011114 A 5410 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 16831 (CAN) CRACKS FOUND AT THREE LOCATIONS WHILE PERFORMING REPEAT INSPECTION. FS 640, BL 0.0 TO LBL 9.50, WL 199.6 DISCREPAN CIES WILL BE REPAIRED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021100072 20020211 00072 EA 2002 2 11 CA011123002 1 20011119 A 5410 601350061 BEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ENGINE SUPPORT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 13602 (CAN) THE ENGINE SUPPORT BEAM UPPER WEB CRACKED AT FS 640 RBL 9.5 AT 7.6 INCHES LONG AND ANGLE CRACKED AT 0.23 INCHES. THIS WAS FOUND WHILE PERFORMING THE SB A601R-53-059.DISCREPANCIES WILL BE REPAIR USING BOMBARDIER DISPOSITIONS. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021100074 20020211 00074 EA 2002 2 11 CA011123008 1 20011022 A 5610 601R3303312 WINDOW CNDAIR CL600 CL6002C10 1390015 EA COCKPIT FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WHILE SITTING INSIDE FLIGHT HANGAR, THE WINDOW SHATTERED - A LOUD BANG WAS HEARD. NOBODY WAS CLOSE TO THE AREA AND THE AIRCRAFT WAS PARKED STATICALLY DOING SOME OTHER MAINTENANCE WORK (NON RELATED).THE WINDOW HAS BEEN REPLACED AND NO OTHER OBVIOUS PROBLEMS FOUND. 2 L 7 2 4F RT A21EA 2002021100075 20020211 00075 EA 2002 2 11 CA011123009 1 20011109 A 5610 601R3303312 WINDOW CNDAIR CL600 CL6002C10 1390015 EA COCKPIT FAILED W B A EMER. DESCENT UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 CA 00036H9095 (CAN) IN CLIMB THROUGH FL350, RT SIDE WINDOW SHATTERED. OUTER WINDOW IS COMPLETELY CRACKED AND INNER WINDOW IS INTACT. E MERGENCY DESCENT TO 10,000 FT WAS INITIATED. PRESSURE REDUCED FROM 8.4 (DELTA P) TO LESS THAN 6.2 (DELTA P). RETURN TO B ASE WAS INITIATED AND LANDING WITHOUT ANY FURTHER INCIDENT. 2 L 7 2 4F RT A21EA 2002021100076 20020211 00076 WP 2002 2 11 CA011123010 1 20011122 A 2434 GENERATOR CVAC 340 340CVAC 242270A WP ALLSN 501D 501D13 03004 GL NR 2 FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 CA (CAN) DURING CLIMB OUT OF YQT THE NR 2 GEN O/H LIGHT ILLUMINATED. CHECK LIST C/W. RETURNED TO YQT. NR 2 DC GENERATOR RE PLACED. 2 L 7 2 4R 4 T 6A6 E282 2002021100079 20020211 00079 EA 2002 2 11 CA011126004 1 20011118 A 2910 DSC252B40124 HOSE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE HYD SYSTEM SPLIT W O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 CA 23720 (CAN) THE FLIGHT CREW REPORTED THAT THE NR 2 HYDRAULIC SYSTEM DECREASED TO 2 QTS ON APPROACH WITH NO LOSS OF SYSTEMS. MA INTENANCE FOUND THE HYDRAULIC FLEX HOSE (UNLOCK) SPLIT NEAR THE B-NUT ON THE NLG DRAG STRUT ACTUATOR. THE HOSE WAS REPLA CED AND ALL FURTHER CHECKS WERE COMPLETED PRIOR TO RELEASING THE AIRCRAFT TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002021100081 20020211 00081 NM 2002 2 11 CA011126006 1 20011008 A 2497 2431155A81 WIRE DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE ELECTRICAL PANEL MELTED W O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CA 25277 (CAN) PILOT REPORTED EXTREME HEAT COMING FROM LT CIRCUIT BREAKER PANEL ASSOCIATED WITH GLOWING LIGHT COMING FROM UNDER P ANEL. FEEDER WIRE 2431-155A8-1 AT BREAKER P2 (LT WING INSPECTION LIGHT) WAS FOUND WITH TERMINAL BURNED AND WIRE ISOLATIO N BURNED ON A LENTH OF 3 INCHES. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002021100115 20020211 00115 WP 2002 2 11 02FDEA00093 1 20011218 A 5743 ARB0642501 FRAME DOUG DC10 DC1010F 3022111 WP RT MLG FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 363FE 48263 RT MLG RETRACT CYLINDER SUPPORT FRAME ASSY FAILURE OCCURRED. REMOVED AND REPLACED STEEL SUPPORT FRAME AND CYLINDER ASSY PER DC10-57-105. 2 L 7 3 4F A22WE 2002021200001 20020212 00001 NE 2002 2 12 CA011127003 3 20011110 A 6114 BEARING BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE PROP HUB FRACTURED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING A SHOP VISIT FOR A SHEATH REPLACEMENT ON ONE OF THE PROP BLADES THE REPAIR SHOP FOUND ONE OF THE BLADE BEAR INGS FRACTURED AND ONLY BEING HELD IN PLACE BY THE MATING OF THE TWO HUB HALVES. THE PROP HAD NO EXTERNAL EVIDENCE OF TH E FRACTURED BEARING SUCH AS BEING LOOSE OR STICKING AND WAS ONLY EVIDENT WHEN THE HUBS WERE SEPARATED. THE FRACTURED PIE CE ALSO CAUSED A FRETTING DAMAGE TO THE HUB WHICH IS NOW BEING ACCESSED BY HARTZELL AND WILL LIKELY BE BEYOND REPAIRABLE LIMITS. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2002021200007 20020212 00007 EU 2002 2 12 CA011127014 1 20011116 A 2780 LIMITER AIRBUS A340 A340313 EU CFMINT CFM56 CFM565C4 13802 NE LE FLAPS FAILED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA (CAN) AIRCRAFT LANDED WITH FLAP LOCKED IN THE RETRACT POSITION. AIRCRAFT DID OVERSHOOT, THEN EXECUTED A FLAPLESS LANDING . RT SYSTEM TORQUE LIMITER AND INPUT GEARBOXES 2-5 FOUND EXTENDED. 2 L 7 4 4F 4 F RT A197 E37NE 2002021200008 20020212 00008 NE 2002 2 12 CA011127015 2 20011118 A 7200 ENGINE AIRBUS A340 A340313 EU CFMINT CFM56 CFM565C4 13802 NE NR 3 FAILED W E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION AP APPROACH 1 CA (CAN) ENROUTE FROM VANCOUVER TO JAPAN, THE FLIGHT EXPERIENCED A POWER LOSS ON NR 3 ENGINE. ROLL BACK TO 77 PERCENT THEN AUTO RE LIGHT OCCURRED RAPIDLY. LATER ON INTO THE FLIGHT, THE FLIGHT CREW HAD THE ENGINE LOW PRESSURE MESSAGE AND ON AP PROACH TO NARITA, THE CREW ELECTED TO SHUTDOWN THE ENGINE. NO EMERGENCY LANDING. ENGINE REPLACED. 2 L 7 4 4F 4 F RT A197 E37NE 2002021200018 20020212 00018 EA 2002 2 12 CA011128001 1 20011119 A 4997 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE APU BATTERY FAILED W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA (CAN) APU CHARGER STATUS MESSAGE CIRCUIT BREAKER POPPED - ON TAXI OUT. WHEN MECHANIC RESET THE CIRCUIT BREAKER THE CONNE CTOR PLUG ON TOP OF THE CHARGER CAUGHT FIRE. REPAIRED CONNECTOR PLUG BY REPINING ALL ASSOCIATED WIRES. REPLACED APU BATT ERY & CHARGER. COMPONENT REPLACED ON TOP OF THE APU BATTERY CHARGER. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021200019 20020212 00019 EA 2002 2 12 CA011128002 1 20011122 A 7120 601350061 MOUNT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) CRACKS FOUND ON THE RIGHT SIDE (2.5 INCHES) AND LEFT (TWO CRACKS = CUMULATIVE MEASUREMENT OF APPROXIMATELY 2 INCHE S )ACCESS PANEL CUT-OUT. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021200020 20020212 00020 EA 2002 2 12 CA011128003 1 20011122 A 7120 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 19607 (CAN) DURING THE INSPECTION OF THE ENGINE SUPPORT BEAM IAW SB A601R-53-059, TWO CRACKS WERE FOUND. ONE ON THE UPPER WEB AT RBL 9.5 AND LEFT LOWARD ACCESS PANEL LEFT FORWARD CORNER. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021200021 20020212 00021 EA 2002 2 12 CA011128004 1 20011122 A 7120 601350061 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 12406 (CAN) DURING INSPECTION PER SB A601R-53-059, ONE CRACK ON THE SUPPORT BEAM LOWER WEB INBOARD FORWARD CORNER (BL 36) WAS FOUND ON THE R/H SIDE AND THE L/H SIDE. REPAIR PER REO 601R-53-61-358 WAS CARRIED OUT. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021200022 20020212 00022 EA 2002 2 12 CA011128005 1 20011122 A 5610 NP1393215 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED W O OTHER O OTHER CL CLIMB 1 CA (CAN) LT COCKPIT WINDSHIELD CRACKED NEARING TOP OF CLIMB - FL335. AIRCRAFT CONTINUED ON WHERE THE WINDSHIELD WAS REPLACE D. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021200023 20020212 00023 EA 2002 2 12 CA011128006 1 20011123 A 7120 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 16083 (CAN) CRACK ON THE ENGINE SUPPORT BEAM. REPAIRED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021200025 20020212 00025 EA 2002 2 12 CA011128010 1 20011018 A 2730 215241152 BOLT CNDAIR CL215 CL2156B11415 EA RT ELEVATOR BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING ANNUAL INSPECTION, ACCESS PANEL WAS LIFTED AND DISCOVERED AN EYE BOLT (OUTBOARD HINGE) HAD BEEN BROKEN ON TOP OF THE SCREW. ALSO FOUND A HINGE FITTING WAS BROKEN AND CRACKED. NO APPARENT SIGN OR ANOMALLY WAS NOTICED DURING THE PREVIOUS FLIGHTS SO THE INCIDENT WAS NOT REPORTED. THE ONLY WAY TO DETECT THE PROBLEM WOULD BE DURING AN ANNUAL INS PECTION. 2 H 7 2 4T RT A14EA 2002021200026 20020212 00026 NM 2002 2 12 CA011128012 1 20011123 A 2913 SEAL BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE HYD PUMP FAILED W O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 CA (CAN) LOSS OF HYDRAULIC QUANTITY TO ZERO ON APPROACH INTO YEG. CREW NOTICED MASTER CAUTION LIGHT WARNING OF HYDRAULIC QUANTITY FOLLOWED BY INDICATION OF ZERO FLUID LEVEL. SYS 'A' PRESSURE FLUCTUATING FROM 500 TO 2500 PSI. SYS 'B' PRES SURE NORMAL. CREW REQ PRIORITY LANDING & A/C LANDED WITH OUT INCIDENT MAINT INSPECTION FOUND NR 2 ENGINE, NR 2 ENGINE D RIVEN PUMP HAD BLOWN SEAL. MAINT REPLACED NR 2 PUMP, ENGINE GROUND RUNS COMPLETED WITH NO LEAKS. AIRCRAFT RETURNED TO SERVICE WITH NO FURTHER INCIDENTS 2 L 7 2 4F 4 F A16WE E2EA 2002021200027 20020212 00027 NE 2002 2 12 CA011128013 2 20011125 A 7230 BLADE BOEING 737 7372T4 1384492 NM PWA JT8 JT8D15 52051 NE NR 2 COMPRESSOR DAMAGED W A UNSCHED LANDING R E J PARTIAL RPM/PWR LOSS VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 CA (CAN) A/C RETURNED TO YYC DUE TO INSUFFICENT NR 1 ENGINE EPR READINGS. CREW REPORTED ON CLIMB OUT THROUGH 12,000FT. ENR OUTE FROM YYC TO YXX, THEY WERE UNABLE TO ACHIEVE ENGINE PRESSURE RATIO ABOVE 1.92 ON NR 1 ENGINE. CREW STATED LARGE TH ROTTLE STAGGER REQUIRED TO ACHIEVE 1.92 EPR & THAT NO LIMITED FROM ADVANCING FURTHER BY MAX EGT. NR 2 ENGINE INDICATING NORMAL READINGS, BOTH ENGINES HAD ANTI-ICE ON SINCE TAKEOFF. MAINT CONTROL ADVISED A/C TO RETURN TO YYC. A/C CIRCLE D TO BURN OFF FUEL THEN LANDED WITHOUT INCIDENT. MAINT INSP DURING BORESCOPE FOUND 'SHINY PARTICLES' THOUGHOUT COMBUSTIO N CANS & TURBINE AREA. THEY ALSO NOTED SOME OF HPC BLADES ON C7 WERE CURLED SLIGHTLY AT LEADING EDGE TIP & SOME HAD NO G 2 L 7 2 4F 4 F A16WE E2EA 2002021200062 20020212 00062 EA 2002 2 12 CA011130008 1 20011128 A 7160 99207SOCN5054T61 BEARING GE 5064T65G03 CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE GUIDE VAIN SHAFT LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA ARHE2426 (CAN) RT ENGINE - VARIABLE GUIDE VANE SHAFT AFT SUPPORT BEARING MIGRATION.SUBJECT MSN WAS UNDERGOING AN A-CHECK.MAINTENA NCE FOUND THAT THE BEARING ON THE VG SHAFT AFT SUPPORT HAD MIGRATED.VG SHAFT AFT SUPPORT WAS REPLACED WITH A NEW ONE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021200063 20020212 00063 EA 2002 2 12 CA011130011 1 20011116 A 2497 XCS1A10N WIRE CNDAIR CL601 CL6013A 8070802 EA E/E BAY CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WIRES WERE DISCOVERED WITH BROKEN AND / OR MISSING OUTER INSULATOR, LEAVING CORE WIRE EXPOSED. THIS DEFECT IS LOC ATED IN BEND RADIUS OF WIRING WHEN ADG IS STOWED. THIS WIRING BEING BENT IS NEAR ADG CONNECTOR PIXC, POSSIBLY CHAFING, DETERIORATED ON BACKSHELL IN ADG BAY RT NOSE PANEL 112AR. INSULATION WERE FOUND VERY BRITTLE.DEFECT WERE OF 3/4 INCH T O 1 INCH IN LENGTH (EXPOSED CORE) LOCATED 1/4 INCH AFT OF CONNECTOR ON ADG, BRITTLE ON INSULATION WAS APPROXIMATELY 2.5 INCH IN LENGTH. 2 L 7 2 4F RT A21EA 2002021200067 20020212 00067 CE 2002 2 12 CA011130016 1 20011116 A 3500 1295600475 FITTING BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE O2 FILLING PORT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 12520 (CAN) DURING SERVICING ON THE O2 SYSTEM THE AME NOTICED A LEAK ON THE FILLING PORT. AFTER INVESTIGATION HE FOUND THAT T HE FILLING LINE BETWEEN THE FILLING PORT AND THE BOTTLE HAD BOTH END FITTING CRACKED. THE LINE WAS REPLACED. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2002021200068 20020212 00068 CE 2002 2 12 CA011130017 1 20011116 A 3500 FITTING BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE O2 FILLING PORT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 12539 (CAN) DURING SERVICING OF THE O2 SYSTEM THE AME NOTICED A LEAK ON THE FILLING PORT. AFTER INVESTIGATION HE FOUND THAT TH E FILLING LINE BETWEEN THE FILLING PORT AND THE BOTTLE HAD BOTH END FITTING CRACKED. THE LINE WAS REPLACED. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2002021200070 20020212 00070 EA 2002 2 12 CA011203002 1 20011201 A 2720 7G7921 PRESSURE SWITCH DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE RUDDER FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 99999 99999 (CAN) AFTER TAKE-OFF "RUD PRES" & "RUD FULL PRESS" CAUTION LIGHTS ILLUMINATED, AIRCRAFT RETURNED FOR NORMAL LANDING , G ROUND SYSTEM FUNCTION CHECK CARRIED OUT, NO FAULTS FOUND. A/C RETURNED TO SERVICE, NEXT DEPARTURE SAME CAUTION LIGHTS ILLUMINATED, AIRCRAFT RETURNED FOR NORMAL LANDING, GRD TESTS CARRIED OUT SERVICEABLE, BOTH RUDDER PRESSURE SWITCHES REPLACED, AIRCRAFT RETURNED TO SERVICE, NORMAL OPERATIONS. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002021200071 20020212 00071 EA 2002 2 12 CA011203003 1 20011201 A 3233 82910016009 ACTUATOR DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE NLG FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA 24114 24114 (CAN) ON APPROACH AFTER GEAR SELECTION, NLG DOORS OPENED, 'RED' INDICATION SHOWN FOR NOSE GEAR, ALTERNATE EXTENSION S YSTEM USED, AIRCRAFT LANDED NORMALLY. NO EVIDENCE OF EXTERNAL HYDRAULIC FLUID LEAKAGE, AIRCRAFT FERRIED TO BASE FOR R EPAIR. INVESTIGATION FOUND NLG ACTUATOR BYPASSING INTERNALLY. ACTUATOR REPLACED, AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002021200073 20020212 00073 NM 2002 2 12 CA011204001 1 20011204 A 2760 85710559001 BRACKET DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE SPOILER ACT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 32736 32736 (CAN) DURING ACCOMPLISHMENT OF ROUTINE ROLL SPOILER MAINTENANCE TASKS, OUTBRD RT ROLL SPOILER ACTUATOR MOVEMENT NOTICE D, CLOSER VISUAL INSPECTION DETECTED CRACK IN RT OUTBRD ROLL SPOILER ACTUATOR MOUNTING BRACKET. AIRCRAFT GROUNDED UNTI L BRACKET REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002021200113 20020212 00113 NM 2002 2 12 CA011207003 1 20011204 A 2422 INVERTER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE AC SYSTEM FAILED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA 26709 (CAN) THE FLIGHT CREW REPORTED SMOKE AND ELECTRICAL SMELL IN THE COCKPIT. THEY NOTICED THAT THE PRIMARY INVERTER CAUTIO N LIGHT WAS ON AS WELL AS THE PRIMARY INVERTER POWER CIRCUIT BREAKER HAD POPPED. MAINTENANCE ISOLATED THE INVERTER BY D ISCONNECTING THE ELECTRICAL CONNECTOR AND THE SMOKE CLEARED. THE PRIMARY INVERTER WAS THEN REPLACED AND CHECKED SERVICE ABLE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002021200116 20020212 00116 NE 2002 2 12 CA011207006 2 20011106 A 7321 FK23330 COVER RROYCE FK14449 AIRBUS 330 A330243 3930330 EU RROYCE RB211 RB211TRENT77 NE EEC DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) FOUND ON BOTH ENGINES ELECTRONIC UNIT PROTECTION COVER ASSY WITH A HOLE AND CHAFFING ON INNER SURFACE OF COVER. C OVER WAS CHAFFING WITH POWER CONTROL UNIT , ENGINE ELECTRONIC CONTROLLER AND ON EEC CONNECTORS. PCU, EEC AND CONNECTORS HAD SLIGHTLY CHAFFING MARKS. COVER ASSY R/R. 2 L 7 2 4F 4 F RT A46NM E39NE 2002021200117 20020212 00117 NE 2002 2 12 CA011207007 2 20011107 A 7297 WIRE AIRBUS 330 A330243 3930330 EU RROYCE RB211 RB211TRENT77 NE ENGINE CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) SHIELDED WIRES FOUND CHAFED TO CENTER CONDUCTORS. THESE WIRES ARE LOCATED ON TOP PORTION E.E.C. ENGINE DISCONNEC T. 4 OF THE WIRES HAVE ARCED & CAUSED LOSS OF ENGINE IDG & THRUST REVERSER OPERATION. 2 L 7 2 4F 4 F RT A46NM E39NE 2002021200119 20020212 00119 EU 2002 2 12 CA011210001 1 20011127 A 2810 7965592 PANEL SNIAS AS332 AS332L 8680809 EU TMECA MAKILA MAKILA1A 60040 EU REFUELING INOPERATIVE W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) PRESSURE REFUELING CONTROL PANEL WILL NOT PERMIT SINGLE POINT REFUELING TO BE CARRIED OUT. 2 G 7 2 4U 4 U H4EU E12NE 2002021200120 20020212 00120 EA 2002 2 12 CA011210004 1 20011206 A 3040 0802071001 CONTROLLER DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE WINDSHIELD HEAT FAILED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA (CAN) ENROUTE CAPTAIN`S WINDSHIELD FROSTED OVER, C/B AC1 POPPED, RESET C/B, WINDSCREEN STILL NO HEAT. DUE TO LACK OF MAINTENANCE FACILITIES AT DESTINATION AIRCRAFT ELECTED TO RETURN TO DEPARTURE BASE FOR NORMAL LANDING. LT WINDSHIELD H EAT CONTROLLER REPLACED, AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002021200123 20020212 00123 2002 2 12 CA011210005 4 20011129 A 8300 GEARBOX CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 2 ENGINE FAILED W A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 CA (CAN) APPROXIMATELY 20 MINS AFTER TAKE OFF, THE CREW NOTICED THE NR 2 ENGINE N2 DROP TO ZERO RPM WITHIN 2-3 SECONDS. AL L OTHER NR 2 ENGINE PARAMETERS ALSO REDUCED AND THE ENGINE FLAMED OUT. THIS OCCURRED DURING THE CLIMB AT APPROX. FL 310 . THE OIL PRESSURE REDUCED TO 2 PSI, WHERE IT STAYED FOR THE REMAINDER OF THE FLIGHT. AN EMERGENCY WAS DECLARED AND THE FLIGHT DIVERTED, WHERE AN UNEVENTFUL SINGLE ENGINE LANDING WAS PERFORMED. INITIAL INSPECTIONS FOUND THAT THE MASTER CHI P DETECTOR WAS SET AND HAD METALLIC CHIPS ON IT. BORESCOPE INSPECTION REVEALED INTERNAL DAMAGE IN THE GEARBOX. THE ENGIN E WILL BE REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021200127 20020212 00127 2002 2 12 CA011210006 4 20011128 A 3460 DISPLAY CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FLT MANAGEMENT OVERHEATED W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN) SMELL OF SMOKE. FMS CDU WAS HOT TO TOUCH AND LOSS OF COLORS ON SCREEN. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021200129 20020212 00129 CE 2002 2 12 CA011210007 1 20011127 A 2497 1013645801 CIRCUIT BOARD BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE ANNUNCIATOR FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) ENROUTE TO BASE THE LT AC BUS ANNUNCIATOR ILLUMINATED BUT THE SYSTEM WAS OPERATING NORMALLY, SHORTLY AFTER AN ANN UNCIATOR POWER SOURCE LIGHT ILLUMINATED. THE ANNUNCIATOR POWER SOURCE LIGHT IS SUPPOSED TO ILLUMINATE WHEN THERE IS A D IRECT SHORT FOR ONE OF THE ANNUNCIATORS INCLUDING THE AC SYSTEM. THE CREW ELECTED TO RETURN TO BASE FOR MAINTENANCE. MA INTENANCE FOUND ONE OF THE ANNUNCIATOR FAULT BOARDS TO BE SHORTING. THE BOARD WAS REPLACED AND THE AIRCRAFT RELEASED PEN DING A SATIFACTORY TEST FLIGHT. THE FAULT DID NOT REOCCUR DURING THE TEST FLIGHT AND THE AIRCRAFT WAS SENT BACK INTO SE RVICE. 2 L 7 2 4T 4 T RT A24CE E26NE 2002021200141 20020212 00141 NM 2002 2 12 CA011210015 1 20011201 A 3246 KEY BOEING 727 727243 138408D NM PWA JT8 JT8D15 52051 NE MLG WHEEL BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING PUSH BACK, NR 2 BRAKE LOCKED UP. NR 2 MAIN WHEEL INSIDE WHEEL RIM BRAKE KEYS FOUND BROKEN. NR 2 MAIN WHE EL ASSY AND NR 2 BRAKE ASSY. REPLACED. AWAITING OVERHAUL SHOP FINDINGS ON EACH COMPONENT FOR PROBABLE CAUSE. 2 L 7 3 4F 4 F RT A3WE E2EA 2002021200147 20020212 00147 WP 2002 2 12 UPS01837380 1 20011222 A 5312 BULKHEAD DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:N/A FWD FRAME PRESS BULKHEAD LONGERON 35 CRACKED. 2 L 7 4 4F RT 4A25 2002021200148 20020212 00148 WP 2002 2 12 UPS01837381 1 20011222 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:N/A CORROSION AT LONGERON 34. 2 L 7 4 4F RT 4A25 2002021200153 20020212 00153 EU 2002 2 12 CA011210019 1 20011113 A 3260 WIRE BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110UG 01514 WP ROTOL R333 R333482F12 GL DOWNLOCK SWITCH BROKEN W L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 CA (CAN) AFTER THE GEAR WAS SELECTED DOWN IT WAS NOTED THAT THE NOSE GEAR WAS NOT INDICATING DOWN AND LOCKED. THE LANDING W AS ABORTED AND A FLY-BY OF THE TOWER WAS CARRIED OUT OF FOR VISUAL CONFIRMATION THAT THE GEAR WAS DOWN. THE EMERGENCY SE RVICES WERE REQUESTED BUT THE AIRCRAFT LANDED SAFELY. ON INVESTIGATION, A WIRE TO THE NOSE GEAR DOWNLOCK SWITCH WAS FOUN D BROKEN. THIS SEEMS TO OCCUR EACH YEAR IN THESE WEATHER CONDITIONS. THE TEMPERATURE WAS HOVERING NEAR ZERO, WITH A FAIR AMOUNT OF MOISTURE IN THE AIR. I AM NOT SURE WHAT HAPPENS, BUT I SUSPECT ICE IS SOMEHOW INVOLVED. 2 L 7 2 4T 4 T RT A21EU E4WE 6 C P61GL 2002021200158 20020212 00158 WP 2002 2 12 CA011210024 1 20011113 A 3310 30049156 LENS LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE COCKPIT LOOSE W K NONE L NO TEST IN INSP/MAINT 1 CA (CAN) -THE REFLECTOR HAS BEEN FOUND LOOSE IN LENS OF LIGHT ASSEMBLY CAUSING C/B PANEL NR 2 , K3 POSITION, POPPED DUE TO BULB CONTACT SHORTED TO LIGHT ASSEMBLY BODY. 2 L 7 3 4F 4 F A23WE E12EU 2002021200163 20020212 00163 NM 2002 2 12 UPS02237445 1 20011221 A 5753 FLAP TRACK BOEING 727 727185C 138406N NM L/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI, NR 7 FLAP TRACK LOOSE BUSHING ON FWD SUPPORT LUG RT, LOOSE BUSHING REMOVED AND BORE FOUND CORR ODED. PITTING CORROSION REMOVED BY MACHINING IAW SOPM 20-10-02. NDT C/W NDF. BUSHING FAB'D THEN HEAT TREATED, CADPLAT ED, POSTBAKED AND INSTALLED. 2 L 7 3 4F A3WE 2002021200164 20020212 00164 NM 2002 2 12 UPS02237446 1 20011220 A 5521 RIB BOEING 727 727185C 138406N NM ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI CRACK IN ELEVATOR SUPPORT RIB AT ELEVATOR STA 17.20 LEFT I/B UPPER FLANGE. RIB REPLACED. 2 L 7 3 4F A3WE 2002021200165 20020212 00165 NM 2002 2 12 UPS02237447 1 20011228 A 5521 RIB BOEING 727 727185C 138406N NM ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI CRACK IN ELEV SUPPORT RIB, O/B LWR AFT FLANGE AT ST 173.21 RT. RIB REPLACED. 2 L 7 3 4F A3WE 2002021200167 20020212 00167 NM 2002 2 12 UPS02237450 1 20011220 A 5753 651920220 CARRIAGE BOEING 727 727185C 138406N NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI PITTING CORROSION IN FLT ROLLER BEARING MOUNT HOLES NR 1 FLAP CARRIAGE. CARRIAGE REPLACED IAW OHM 57-52-11. 2 L 7 3 4F A3WE 2002021200168 20020212 00168 NM 2002 2 12 UPS02237457 1 20011221 A 5753 FLAP TRACK BOEING 727 727185C 138406N NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI PITTING CORROSION ON INNER FACE OF FWD SUPPORT LUG LT NR 7 FLAP TRACK. CORROSION REMOVED BY MACHIN ING NDT COMPLIED WITH AND NO DEFECTS WERE FOUND. FLAP PEENED AND CADPLATED IAW OHM. 2 L 7 3 4F A3WE 2002021200169 20020212 00169 NM 2002 2 12 UPS02237458 1 20011221 A 5753 FLAP TRACK BOEING 727 727185C 138406N NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI NR 8 FLAP TRACK, PITTING CORROSION ON OUTER FACE OF FWD SUPPORT LUG LT. CORROSION REMOVED BY MACHI NING, NDT COMPLIED WITH NDF FLAP PEENED IAW OHE AND CADPLATED IAW OHM. 2 L 7 3 4F A3WE 2002021200170 20020212 00170 NM 2002 2 12 UPS02237459 1 20011221 A 5753 FLAP TRACK BOEING 727 727185C 138406N NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI NR 8 FLAP TRACK, PITTING CORROSION FOUND ON INNER FACE OF FWD SUPPORT LUG LT. CORROSION REMOVED BY MACHINING, NDT COMPLIED WITH AND NDF. FLAP PEENED AND CADPLATED IAW OHM. 2 L 7 3 4F A3WE 2002021200175 20020212 00175 NM 2002 2 12 UPS02237465 1 20011219 A 5753 65192028 CARRIAGE BOEING 727 727185C 138406N NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI NR 2 FLAP CARRIAGE HAS CORROSION INSIDE SPINDLE BORE CORROSION CONFINED TO SPINDLE BORE, NOT PO SSIBLE TO MEASURE EXTENT. CARRIAGE REPLACED AS NO REPAIR POSSIBLE IAW 57-52-01. 2 L 7 3 4F A3WE 2002021200182 20020212 00182 NM 2002 2 12 CA011211007 1 20011108 A 2910 NAS1762D1212 FITTING BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E437 54555 NE HYD SYSTEM CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ELBOW HYDRAULIC FITTING CRACKED AT OUTLET PORT OF LT ELECTRICAL HYDRAULIC PUMP. 2 L 7 2 4F 4 F RT A2NM E12EU 2002021200185 20020212 00185 WP 2002 2 12 AALA20020011 1 20011214 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 429AA 49341 TUL - FOUND STATION 1380 BELOW LONGERON 13R OUTER SKIN CRACKED AT SHEAR TIE RIVET. INSTALLED DOUBLER PER SRM 53-01 FIG 2 SHEET 3. (M) 2 L 7 2 4F A6WE 2002021200189 20020212 00189 EU 2002 2 12 SIMA200117111 1 20010620 A 7933 WARNING SYSTEM SAAB SF340 340B 7860101 EU COCKPIT ACTIVATED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 313AE 340B313 BOS - FLT 4613 - ABORTED TAKEOFF DUE TO HIGH RIGHT ENGINE OIL TEMP AND RIGHT PROP OIL TEMP. (M) 2 L 7 2 4T RT A52EU 2002021200190 20020212 00190 NE 2002 2 12 SIMA200117403 2 20010623 A 7320 MODULE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE MALFUNCTIONED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 329AE 340B329 SBA - FLT 3037 - ON TAKEOFF ROLL, LEFT ENGINE APR DID NOT ARM. ABORTED TAKEOFF. ISSUED MEL 76-02. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 2002021200191 20020212 00191 SO 2002 2 12 SIMA200135201 1 20011213 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 600BK 145044 ABI - DURING AN IMBV INSPECTION, FOUND CORROSION ON THE FORWARD DIGITAL. REMOVED CORROSION BY BLENDING OUT. FABRICATED A REPAIR DOUBLER 7.875 INCH BY 17 INCH .040 INCH THICK. REPAIR DONE IAW EMB GST-3851/01A, ITEM 2 AND STANDARD SRM PRAC TICES. (M) 2 L 7 2 4T RT T00011AT 2002021200192 20020212 00192 SO 2002 2 12 SIMA200135202 1 20011213 A 5313 STRINGER EMB 145 EMB145 3260210 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 606AE 145062 DURING AN IMBV INSPECTION, FOUND LEFT OUTBOARD STRINGER 19L CHAFFED BETWEEN FRAMES 52L AND 53L. REMOVED CHAFED BY BLEND ING. FABRICATED FOUR SHIMS AND TWO DOUBLER ANGLES. REPAIR DONE IAW EMB GST 3895/01, GST3458/01, GST-3486/01, GST 3725/0 1, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002021200193 20020212 00193 SO 2002 2 12 SIMA200135203 1 20011213 A 5315 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 606AE 145062 ABI - DURING AN IMBV INSPECTION, FOUND CORROSION ON THE RIGHT GALLEY FLOORBEAM AT FRAME 20. REMOVED CORROSION BY BLENDI NG OUT. FABRICATED AN U-CHANNEL REPAIR DOUBLER. WORK DONE IAW EMB GST 3862/01, ITEM 12 AND STANDARD SRM PRACTICES. (M ) 2 L 7 2 4F RT T00011AT 2002021200194 20020212 00194 SO 2002 2 12 SIMA200135204 1 20011214 A 5313 STRINGER EMB 145 EMB145 3260210 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 606AE 145062 ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND RIGHT OUTBOARD STRINGER 19R CHAFED BETWEEN FRAMES 52R AND 53R. REMOV ED CHAFED BY BLENDING. FABRICATED FOUR SHIMS AND TWO DOUBLER ANGLES. REPAIR DONE IAW EMB GST-3895/01, GST 3958/01, GST -3458/01, GST-3486/01, GST-3725/01, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002021200195 20020212 00195 SO 2002 2 12 SIMA200135205 1 20011214 A 5315 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 606AE 145062 ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON THE GALLEY CENTER FLOORBEAM AT FRAMES 20 AND 23. REMOVED CORROSION BY BLENDING OUT AT FRAME 20 AND 23. FABRICATED TWO U-CHANNEL REPAIR DOUBLERS. REPAIR DONE IAW EMB GST-3862- /01, ITEM 10 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002021200196 20020212 00196 SO 2002 2 12 SIMA200135206 1 20011214 A 5315 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 606AE 145062 ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON THE LEFT OMEGA BEAM AT FRAME 24. REMOVED CORROSION BY B LENDING OUT. FABRICATED A Z-PROFILE REPAIR DOUBLER. REPAIR DONE IAW EMB GST-3862/01, ITEM 14 AND STANDARD SRM PRACTICE S. (M) 2 L 7 2 4F RT T00011AT 2002021200197 20020212 00197 EU 2002 2 12 SIMA200135401 1 20011218 A 3260 CONNECTOR SAAB SF340 340B 7860101 EU RT MLG DISCONNECTED A SIMA O OTHER N FALSE WARNING AP APPROACH 1 SW 21 901AE 340B401 ON APPROACH INTO DFW CREW SELECTED GEAR DOWN AND GOT NO GREEN LIGHT ON RIGHT MLG FOLLOWED AOM PROC. BLEW GEAR DOWN STIL L IN INDICATION DECLARED EMERGENCY. OTHER INDICATION NORMAL LANDED DFW NO PROBLEMS. FOUND CANNON PLUG OFF ON RIGHT MLG DOWNLOCK SWITCH. REINSTALLED CANNON PLUG. GEAR SWINGS WERE GOOD. ALSO, INSTALLED NEW SEPARATION BOLTS. (M) 2 L 7 2 4T RT A52EU 2002021200198 20020212 00198 EU 2002 2 12 SIMA200135402 1 20011220 A 3350 66902 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 382AE 340B382 DFW - FLT 3803 - FOUND EMERGENCY FLOOR LIGHTING FROM 6A TO 8A IS OUT. RAI EMERGENCY FLOOR LIGHTING STRIP AT 6A TO 8A IA W AMM 33-50-20. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2002021200199 20020212 00199 SO 2002 2 12 SIMA200135601 1 20011221 A 3350 20131A BATTERY PACK EMB 135 EMB135LR 3260305 SO CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 704PG 145174 FOUND SEVERAL EMERGENCY LIGHT IN CABIN INOPERATIVE. RAI NR 2 EMERGENCY BATTERY PACK. (M) 2 L 7 2 4F RT TOOO11AT 2002021200200 20020212 00200 EU 2002 2 12 SIMA200136002 1 20011226 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 313AE 340B313 EMERGENCY LIGHT OUT OVER SEATS 8 AND 10BC. RAI POWER SUPPLY AT 22LN. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2002021200201 20020212 00201 EU 2002 2 12 SIMA200136101 1 20011227 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 339SB 340B339 BWI - FLT 4828 - CREW REPORTED THE BACK HALF OF FLOOR PROXIMITY EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY UNIT 24LN IAW SAAB MM. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVI CE. (M) 2 L 7 2 4T RT A52EU 2002021200202 20020212 00202 EU 2002 2 12 SIMA200136501 1 20011231 A 3230 D49412001 CONTROL PANEL SAAB SF340 340B 7860101 EU COCKPIT FAILED A SIMA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 SW 21 273AE 340B273 BOS - FLT 4810 - DURING APPROACH TO BOS, CREW SELECTED GEAR DOWN AND GOT NO DOWN AND LOCKED INDICATION ON ALL THREE GEAR . CREW DECLARED EMERGENCY AND FOLLOWED AOM PROCEDURES. AIRCRAFT WAS LANDED SAFELY WITH NO OTHER PROBLEMS NOTED. MAINT ENANCE REMOVED AND REPLACED LANDING GEAR CONTROL PANEL IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNE D TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2002021200203 20020212 00203 SO 2002 2 12 SIMA20136001 1 20011223 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 636AE 145160 AZO - FLT 4266 - EMERGENCY LIGHTS INOPERATIVE ROWS 8 THROUGH 12. REPLACED LIGHT BATTERY AND HOLDER, OPS CHECKS GOOD. ( M) 2 L 7 2 4T RT T00011AT 2002021200206 20020212 00206 NM 2002 2 12 UPS02237467 1 20011219 A 5753 651920220 CARRIAGE BOEING 727 727185C 138406N NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI CORROSION ON INNER BORE OF NR 8 FLAP CARRIAGE SPINDLE, AND ON END OF SPINDLE UNDER BEARING. CARRIA GE ASSY REPLACED IAW OHM. 2 L 7 3 4F A3WE 2002021200207 20020212 00207 NM 2002 2 12 UPS02237468 1 20011219 A 5753 651920220 CARRIAGE BOEING 727 727185C 138406N NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI CORROSION ON INNER SPINDLE BORE OF NR 7 FLAP CARRIAGE SPINDLE. REPLACED CARRIAGE ASSY IAW OHM. 2 L 7 3 4F A3WE 2002021200208 20020212 00208 NM 2002 2 12 UPS02237469 1 20011219 A 5753 651859931 CARRIAGE BOEING 727 727185C 138406N NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI CORROSION ON FLT ROLLER BEARING MOUNT HOLE NR 5 FLAP CARRIAGE. CARRIAGE ASSY REPLACED IAW OHM. 2 L 7 3 4F A3WE 2002021200209 20020212 00209 NM 2002 2 12 UPS02237470 1 20011219 A 5311 FRAME BOEING 727 727185C 138406N NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI FRAME CRACKED AT BS 487.1 AT STR 19L ADJACENT TO LATCH SUPPORT FITTINGS. CRACKED AREA CUT OUT, REP AIR PARTS FABRICATED, PARTS INSTALLED AND VERTICAL STIFFENER INSTALLED. 2 L 7 3 4F A3WE 2002021200210 20020212 00210 NM 2002 2 12 UPS02237471 1 20011219 A 5311 FRAME BOEING 727 727185C 138406N NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI FRAME CRACKED AT BS 500 AT STR 18L ADJACENT TO LATCH SUPPORT FITTINGS. REPAIR PARTS FABRICATED AND DAMAGED AREA CUT OUT. REPAIR PARTS INSTALLED IAW SRM, VERTICAL STIFFENER INSTALLED. 2 L 7 3 4F A3WE 2002021200211 20020212 00211 NM 2002 2 12 UPS02237472 1 20011219 A 5311 FRAME BOEING 727 727185C 138406N NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI FRAME CRACKED AT BS 540 STR STR 18L ADJACENT TO MCD LATCH SUPPORT FITTING. DAMAGED AREA CUT OUT AN D REPAIR PARTS FABRICATED, REPAIR PARTS INSTALLED. 2 L 7 3 4F A3WE 2002021200212 20020212 00212 NM 2002 2 12 UPS02237473 1 20011219 A 5311 FRAME BOEING 727 727185C 138406N NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI FRAME CRACKED AT BS 580 ATR STR 18L, ADJACENT TO MCD LATCH SUPPORT FITTINGS. CRACKED AREA CUT OUT AND REPAIR PARTS FABRICATED, REPAIR PARTS INSTALLED. 2 L 7 3 4F A3WE 2002021300002 20020213 00002 NM 2002 2 13 CA011211011 1 20011122 A 5412 SEP038SEP039 SEAL DHAV DHC8 DHC8* NM FIREWALL MISSING W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING SCHEDULED MOD PROGRAM IT WAS NOTED THAT THERE WAS A GAPPING CONDITION AT THE ENGINE FUEL AND HYDRAULIC LINE S AT THE FIREWALL FAIRLEADS. THERE WERE VISIBLE GAPS BETWEEN SOME OF THE FAIRLEAD SECTIONS AND AROUND SOME OF THE FUEL A ND HYDRAULIC LINES AND THE FAIRLEAD. THIS CONDITION WAS NOTED ON L/H AND R/H NACELLES. IT WAS NOT POSSIBLE TO COMPLETELY SEAL ALL POINTS AT THESE FAIRLEADS EVEN WITH REPLACING THE FAIRLEADS WITH NEW UNITS. A REPAIR DRAWING WAS REQUESTED AMD RD 8/4-54-054 WAS ISSUED TO ALLOW THE USE OF FIREWALL SEALANT IN THIS AREA TO SEAL THE OPEN VOIDS.SEALANT IN THIS AREA TO SEAL THE OPEN VOIDS. RD8/4-54-054 WAS CARRIED OUT ON THIS AIRCRAFT. 2 H 7 2 4T RT A13NM 2002021300003 20020213 00003 NM 2002 2 13 CA011211012 1 20011012 A 2497 WIRE HARNESS BOEING 757 757236 1384971 NM RROYCE RB211 RB211535E437 54555 NE ENGINE DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING INSPECTION , FOUND DAMAGE OF THE WIRING HARNESS THAT GOES TO THE P1 PROBE HEATER NOSE COWL INTERFACE CONNE CTOR. TYPE OF DAMAGES ON THE TWISTED SHIELDED PAIR WIRES CABLE FOUND OUTER JACKET AND SCREEN DAMAGE BY ABRASION. 2 L 7 2 4F 4 F RT A2NM E12EU 2002021300010 20020213 00010 NM 2002 2 13 CA011211020 1 20011013 A 2497 WIRE HARNESS BOEING 757 757236 1384971 NM RROYCE RB211 RB211535E437 54555 NE NR 1 ENG EEC DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) 1-) DURING INTER 1 CHECK INSPECTION , THE NR 1 ENGINE EEC PATCH MODULE LOOM INTO CONNECTOR D1380 REVEALED DAMMAGED TO THE WIRING AT CLIPPING POINT CP2281. PROBLEM FOUND WAS CAUSED BY WIRING CHAFFING INTO CLIP CP2281 THAT HAD ITS RUBBE R INSULATOR TORNAND HALF OF IT WAS MISSING. 2 L 7 2 4F 4 F RT A2NM E12EU 2002021300011 20020213 00011 NM 2002 2 13 CA011211021 1 20011015 A 2510 2A0590173 TORQUE TUBE BOEING 757 757236 1384971 NM RROYCE RB211 RB211535E437 54555 NE COCKPIT SEAT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING INTER 1 CHECK, THE INSPECTION CARRIED OUT ON THE CAPTAIN SEAT REVEALED THAT THE SEAT TORQUE TUBE WHICH HA S THE ELECTRICAL WIRING FOR THE VERTICAL ADJUSTMENT GOING THROUGH ,HAD 4 CRACKS ON THE TUBE. 2 L 7 2 4F 4 F RT A2NM E12EU 2002021300012 20020213 00012 NM 2002 2 13 CA011211022 1 20011005 A 3242 161N16231 ROD BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E437 54555 NE BRAKE BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) AIRCRAFT ARRIVED WITH NR 1 BRAKE TORQUE ROD ASSEMBLY BROKEN IN HALF AND HYDRAULIC LINE TO BRAKE WAS BROKEN. 2 L 7 2 4F 4 F RT A2NM E12EU 2002021300013 20020213 00013 NM 2002 2 13 CA011211023 1 20010926 A 8012 LJ41486 DUCT BOEING 757 757236 1384971 NM RROYCE RB211 RB211535E437 54555 NE STARTER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) NR 2 ENGINE STARTER DUCT CRACKED JUST BELOW THE UPPER FLANGE. 2 L 7 2 4F 4 F RT A2NM E12EU 2002021300014 20020213 00014 WP 2002 2 13 CA011211025 1 20010907 A 2597 WIRE LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE GALLEY BURNED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) LOWER GALLEY ZONE 130 , OVEN FEEDER 1-5 (CB11) PHASE "A" WIRE AT TB 2531-1 TERMINAL NR 5 FOUND BURNED OUT. 2 L 7 3 4F 4 F A23WE E12EU 2002021300015 20020213 00015 WP 2002 2 13 CA011211026 1 20011110 A 2913 1515774175 DRAIN LINE LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE HYD PUMP LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) -HYDRAULIC SYSTEM LEVEL LOW, FOUND HYDRAULIC DRIPPING AT AFT BELLY DRAIN NEAR OUTFLOW VALVE (FS 1363) . -THE TUBE ASSY. SYSTEM C HYDRAULIC PUMP DRAIN LINE WAS LEAKING BETWEEN LINE AND FITTING . 2 L 7 3 4F 4 F A23WE E12EU 2002021300016 20020213 00016 EU 2002 2 13 CA011211027 1 20010921 A 2913 3508807 PUMP AIRBUS 310 A310 EU GE CF6 CF680C2* GL HYD SYSTEM LEAKING W O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 CA (CAN) AIRCRAFT ARRIVED WITH NR 1 ENGINEHI VIBRATION DURING TAXI. TROUBLESHOOTING WAS CARRIED OUT IAW MM 72-31-00 AND FO UND GREEN HYDRAULIC PUMP SHAKING & LEAKING. THE PUMP WAS REPLACED & CHECKED SERVICEABLE. 2 L 7 2 4F 4 F RT A35EU E23EA 2002021300022 20020213 00022 NE 2002 2 13 CA011217002 2 20011214 A 7530 7786864 SHUTOFF VALVE DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE NR 1 NACELLE FAILED W A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 CA 28560 28560 (CAN) AFTER TAKE-OFF, NR 1 BLEED HOT CAUTION LIGHT ILLUMINATED, ACCOMPANIED BY HOT AIR SMELL IN COCKPIT. BOTH DUCT AI RTEMPS INDICATING 20-30DEG. LIGHT EXTINGUISHED AFTER SELECTING NR 1 BLEED OFF. AIRCRAFT ELECTED TO RETURN TO MAINTENAN CE BASE FOR NORMAL LANDING. NR 1 NACELL SHUT-OFF & PRESS REDUCING VALVE REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002021300026 20020213 00026 EA 2002 2 13 CA011217008 1 20011207 A 3234 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE MLG FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA 14537 (CAN) MLG DID NOT EXTEND WHEN GEAR SELECTED DOWN ON APPROACH. MLG SELECTOR VALVE REPLACED AND TESTED SERICABLE IAW AMM. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021300027 20020213 00027 EA 2002 2 13 CA011217009 1 20011123 A 5610 NP13932319 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA 18571 (CAN) LT WINDSHIELD STARTED CRACKING DURING TAXI OUT. REMOVED AND REPLACED LEFT WINDSHIELD LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021300028 20020213 00028 EA 2002 2 13 CA011217010 1 20011205 A 5610 NP1393221 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED W O OTHER O OTHER CR CRUISE 1 CA 19250 (CAN) THE PILOT REPORTED THE LT FLIGHT DECK WINDSHIELD CRACKED AT APPROX. 28000 FEET, THE FLIGHT SEQUENCE WAS COMPLETED WITHOUT FURTHER INCIDENCE THE WINDSHIELD WAS REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021300031 20020213 00031 EA 2002 2 13 CA011217015 1 20011130 A 3020 297D513658 BOOT DHAV 75510015004 DHAV DHC7 DHC7102 2802708 EA PWA PT6 PT6A50 52043 EA HAMSTD 24PF 24PF305 GL DEICE SYS DISLODGED W A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 CA (CAN) THE AIRCRAFT WAS FERRYING BACK TO BASE. IN CRUISE THE FLT MECHANIC WHILE STANDING AT THE BACK BETWEEN THE GALLEY A ND THE WASHROOM FELT A LOW FREQ VIBRATION ON THE FLOOR. THE VIBRATION WAS NOTICEABLE TO THE FLIGHT ATTENDANT ALSO. THE I NFORMATION WAS RELAYED TO THE CREW. THE CREW SLOWED THE AIRCRAFT DOWN & BEGAN TO LOOK FOR AN ALTERNATE AIRPORT. THE AIRC RAFT LANDED UNEVENTFULLY. THE INSPECTION REVEALED THAT THE RIGHT OUTBOARD DEICE BOOT ON THE HORIZONTAL UPPER PART A PIEC E ABOUT 1.5 FEET HAD COME UNGLUED. THE BOOT WAS REGLUED AND THE DEICING SYSTEM WAS TESTED. THE AIRCRAFT WAS RELEASED TO SERVICE AND IT FLEW BACK TO BASE. 2 H 7 4 4T 4 T A20EA E4EA 6 C P1NE 2002021300038 20020213 00038 2002 2 13 CA011217020 4 20011217 A 3410 405469 CONTROLLER CNDAIR CL601 CL6012A12 1900303 EA GE CF34 CF341A NE HEATER CONTROL BURNED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN) AS AIRCRAFT WAS SITTING IN THE HANGER WITH POWER ON ADS HEATER CONTROL TURNED OFF SMOKE STARTED COMING OUT FROM CO NTROLLER POWER WAS SHUT DOWN. C/B DID NOT POP I T ALSO TOOK OUT SOME DIMMING MODUALS. 2 L 7 2 4F 4 F RT A21AE E15NE 2002021300039 20020213 00039 CE 2002 2 13 CA011217021 1 20011205 A 2910 6629101001005 MANIFOLD LEAR 45 45LEAR 5170805 CE GARRTT TFE731 TFE731* 01518 WP PRESSURE FILTER LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) INVESTIGATED HYDRAULIC FLUID STAINS ON FUSELAGE BOTTOM. FOUND FILTER MANIFOLD LEAKING, REPLACED COMPONENT. 2 L 7 2 4F 4 F RT T00008WI E6WE 2002021300040 20020213 00040 CE 2002 2 13 CA011217022 1 20011210 A 3240 429333 CONTROL UNIT LEAR 45 45LEAR 5170805 CE BRAKE INTERMITTENT W K NONE N FALSE WARNING IN INSP/MAINT 1 CA (CAN) EICAS MESSAGE LT / RT INBOARD BRAKE FAULT (INTERMITTENT). 2 L 7 2 4F RT T00008WI 2002021300041 20020213 00041 NM 2002 2 13 2001UALA02224 1 20011104 A 8011 383222221AR STARTER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE FAILED A UALA A UNSCHED LANDING A J FLAME/FIRE WARNING INDICATION CL CLIMB 1 WP 29 7466U 21920 SHORTLY AFTER TAKEOFF THE AIRCRAFT EXPERIENCED A NUMBER THREE ENGINE FIRE INDICATION. AIRCRAFT RETURNED TO FIELD. ENGI NE FIRE OCCURRED DUE TO OIL LINE/CSD RUPTURE, CAUSED BY UNCONTAINED STARTER FAILURE. UPON RETURN TO FIELD, CSD WAS FOUN D CRACKED. THE STARTER, CSD FILTER AND HOUSING WERE REPLACED. SHOP FINDINGS FOR STARTER INDICATED TURBINE BEARING FAIL URE. 2 L 7 3 4F 4 F A3WE E2EA 2002021300042 20020213 00042 EA 2002 2 13 CA011217023 1 20011217 A 5610 601R330339 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED W O OTHER O OTHER TX TAXI/GRND HDL 1 CA (CAN) WHILE AIRCRAFT PARKED AT THE GATE, WINDSHIELD CRACKED APPEARED ON CAPTAIN SIDE. AIRCRAFT FERRIED FROM EDINBURGH TO EXETER FOR REPLACEMENT. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021300043 20020213 00043 EU 2002 2 13 CA011217024 1 20011207 A 5610 WINDSHIELD FOKKER F28 F28MK1000 4990808 EU COCKPIT CRACKED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA 10793 10793 (CAN) SHORTLY AFTER TAKEOFF FROM SASKATOON (YXE), CREW NOTED A "BRIGHT FLASH" IN CAPTAIN'S WINDSHIELD. CREW DE-SELECTED WINDSHIELD HEAT IMMEDIATELY, SHORTLY THEREAFTER CENTRE GLASS PLY CRACKED. NO PRESSURIZATION LOSS WAS REPORTED, & CREW E LECTED TO RETURN YXE, LANDED WITH NO FURTHER INCIDENT. MAINT DETERMINED THAT WINDSHIELD SUFFERED AN INTERNAL SHORT IN HEATING SYS, RESULTING IN DAMAGE TO CENTRE GLASS PANE DUE TO TEMP-RELATED STRESS. WINDSHIELD WAS REPLACED & SYSTEM TES TED SERVICEABLE, WITH NO DAMAGE TO WIRING OR COMPONENTS. FINAL REPORT WILL BE SUBMITTED WHEN COMPONENT IS RECEIVED IN CALGARY (YYC), WHERE DETAILED VISUAL INSPECTION OF UNIT MAY BE CARRIED OUT. 2 L 7 2 4F RT A20EU 2002021300056 20020213 00056 NM 2002 2 13 CA011218004 1 20011129 A 3020 CONNECTOR DHAV DHC8 DHC8* NM PWC 150 PW150A EA INTAKE HEAT FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA (CAN) PILOT IN COMMAND REPORTED NR 1 ENGINE ADAPTER HEAT CAUTION LIGHT ILLUMINATED DURING APPROACH, CB OPENED SOON AFTER . ENGINE INTAKE ADAPTER HEATER REMOVED AND FOUND TO BE BURNED AROUND ELECTRICAL CONNECTOR AREA. HEATER REPLACED AND FUN CTION CHECKED. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002021300059 20020213 00059 NM 2002 2 13 CA011218005 1 20011127 A 2913 PUMP DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF23 NE HYD SYSTEM FAILED W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA (CAN) NR 1 HYD. FLUID HOT CAUTION LIGHT CAME ON DURING CRUISE. NR 1 ENG. HYD PUMP CAUTION LIGHT CAME ON. NR 1 HYD QUA NTITY DROPPED TO 0. EMERGENCY DECLARED. FLAPLESS LANDING CARRIED OUT. FINDINGS: HYDRAULIC FLUID PRESENCE WAS NOTED INTO ENGINE 1 NACELLE. LINE FROM CHECK VALVE TO LT CASE DRAIN FILTER OVERHEATED AND LEAKING. NR 1 SYSTEM PRESSURE, RETURN AN D CASE DRAIN FILTERS CONTAMINATED WITH PARTICLES COMING FROM LT EDP.ACTIONS: NR 1 HYD SYSTEM FLUSHED. R/R PRESSURE, RET URN AND CASE DRAIN FILTERS. R/R NR 1 EDP AND SPU. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002021300060 20020213 00060 NE 2002 2 13 CA011218006 3 20011127 A 6111 SFA13N1R04 BLADE DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF23 NE PROPELLER BURNED W A UNSCHED LANDING A FLAME/FIRE CR CRUISE 1 CA (CAN) CREW REPORTED FIRE ON THE NR 1 ENGINE, NO INDICATION FROM THE FIRE WARNING SYSTEM, APPEARS TO BE COMING FROM PROP SPINNER AREA. MAINTENANCE TOLD VERBALLY THAT THIS EVENT HAPPENED 5 MINUTES AFTER TAKEOFF FROM THE AIRPORT. THE AIRCRAFT RETURNED TO BASE. THE LH PROP, BLADE NR 3 WAS FOUND BADLY BURNED, BLADE REPLACED BY MAINTENANCE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002021300062 20020213 00062 EA 2002 2 13 CA011218007 1 20011130 A 5610 601R3303310 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT FAILED W O OTHER O OTHER AP APPROACH 1 CA (CAN) THE AIRCRAFT WAS DESCENDING. THE RT WINDSHIELD SHATTERED. INSPECTION REVEALED THAT THE RT WINDSHIELD CORE PLY HAD SHATTERED. THE RT WINDSHIELD IS BEING REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021300063 20020213 00063 EA 2002 2 13 CA011218008 1 20011207 A 5610 01058H42001 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED W O OTHER O OTHER DE DESCENT 1 CA (CAN) DURING DESCENT AIRCRAFT 7522 THE CO-PILOT'S WINDSHIELD CRACKED. MAINTENANCE REMOVED AND REPLACED THE PILOT'S WIND SHIELD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021300066 20020213 00066 NE 2002 2 13 CA011218010 2 20011129 A 7261 M832481216 O-RING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LT ENGINE NICKED W E A ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CR CRUISE 1 CA (CAN) LEFT ENGINE OIL PRESS WARNING, REQD SHUTDOWN OF ENGINE. DIVERTED & MADE EMERG LDG. SENT MECHS AND FOUND LUBE PUMP INSERT SLEEVE BACKED OFF. TIGHTENED LUBE PUMP INSERT SLEEVE PER GEMM. CHIP DETECTOR CHECKED GOOD. REPLENISHED OIL TANK W ITH 5.5 QTS OF OIL. GROUND RUN & LEAK CHECK CARRIED OUT SUCCESSFULLY. DUE TO POSSIBLE HYD FLUID CONTAMINATION OF AGB; R& R'D CARBON SEALS FOR IDG, EDP & AIR STARTER. LEAK & CONSUMPTION CHECKS GOOD. RT-SRV ON EVEN ING OF NOV 30 FOR ONE RETURN FLT TO MADISON WI. OIL CONSUMPTION NOTED TO BE 0.25 QT. FLT FROM CINCINNATI CVG TO HOUSTON TX. OIL PRESSURE NR 1 ENG FL UXS NOTED. IFSD&DIVERTED. CONTRACT MAINT ADDED 2 QTS OF OIL TO LEFT ENGINE AN D ON SUBSEQUENTLY DRY RUN NOTED EVIDENCE 2 L 7 2 4F 4 F RT A21EA E15NE 2002021300067 20020213 00067 EU 2002 2 13 CA011218011 1 20011215 A 5610 WINDSHIELD FOKKER F28 F28MK1000 4990808 EU COCKPIT CRACKED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) ENROUTE CREW NOTED SPARKING AND ARCING IN CAPTAIN'S WINDSHIELD, FOLLOWED BY DELAMINATION AND CRACKING OF GLASS PAN E(S). CREW CONTACTED ATC AND REQUESTED DIVERSION TO OTTAWA (YOW) AS CLOSEST ALTERNATE, AND LANDED WITH NO FURTHER INCI DENT. CREW REPORTED WINDSHIELD CONTINUED TO CRACK AFTER LANDING, BUT NO LOSS OF PRESSURIZATION WAS INDICATED. MAINTENA NCE REPLACED WINDSHIELD AND TESTED WINDSHIELD HEATING SYSTEM, FOUND SERVICEABLE WITH NO FURTHER WIRING OR COMPONENT DAM AGE. 2 L 7 2 4F RT A20EU 2002021300088 20020213 00088 NM 2002 2 13 CA011219010 1 20011219 A 3246 31414 KEY BOEING 727 727243 138408D NM PWA JT8 JT8D15 52051 NE BRAKE ASSY BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING PUSH BACK NR 2 BRAKE LOCKED UP. NR 2 MAIN WHEEL AND BRAKE ASSY REPLACED. OVERHAUL SHOP FINDINGS AS FOLLOW S: BRAKE ASSY: PRIMARY CAUSE FOR REMOVAL FOD DAMAGE FROM WHEEL. MAIN WHEEL ASSY. PRIMARY CAUSE FOR REMOVAL BROKEN BR AKE KEYS. 2 L 7 3 4F 4 F RT A3WE E2EA 2002021300090 20020213 00090 NE 2002 2 13 CA011219011 2 20011217 A 7314 37820012 PUMP BOEING 727 72722C 138400F NM PWA JT8 JT8D7B 52053 NE FUEL SYSTEM FAILED W C D ABORTED TAKEOFF RETURN TO BLOCK R Y J PARTIAL RPM/PWR LOSS ENGINE STOPPAGE WARNING INDICATION TO TAKEOFF 1 CA (CAN) NR 3 ENGINE SPOOLED DOWN DURING T/O ROLL. T/O ABORTED AT 60 KNTS. NR 3 ENGINE FUEL PUMP RELACED. SN 4617 REMOVED. 2 L 7 3 4F 4 F A3WE E2EA 2002021300106 20020213 00106 NE 2002 2 13 CA011221002 2 20011212 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ROTOL R390 R3904123F27 NE LEFT MALFUNCTIONED W C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 CA (CAN) ON TAKE OFF ACCELERATING THROUGH 60 KTS TME A/C YAWED TO PORT AND THE PORT ENGINE TORQUE WAS SEEN TO DROP. THE ENGINE WAS SHUT DOWN AND THE TAKE OFF ABORTED. AT PRESENT THE INCIDENT IS SUBJECT TO A FULL ENGINEERING INVESTIGATION. FURTHER DETAILS WILL FOLLOW. 2 L 7 2 4T 4 T RT A52EU E8NE 6 C P31NE 2002021300115 20020213 00115 EA 2002 2 13 CA011221006 1 20011219 A 2913 PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE HYD SYSTEM FAILED W O OTHER K FLUID LOSS AP APPROACH 1 CA (CAN) WHILE EXTENDING THE GEAR DURING APPROACH GEAR DISAGREE AND HYD 3 LOW PRESSURE CAUTION MESSAGES. CHECKED HYDRAULIC SYNOPTIC PAGE. VERIFIED NR 3 HYD PRESSURE QUANTITY 0 PERCENT. REMOVED AND REPLACED HYD. PUMP 3A WITH SERVICEABLE UNIT. PERFORMED LEAK CHECK ABD OPS CHECK. NO LEAKS NOTED AT THIS TIME. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021300123 20020213 00123 WP 2002 2 13 AALA20020012 1 20011212 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 429AA 49341 TUL - FOUND LEFT CUSP STATION 713 HOLE IN CUSP. INSTALLED DOUBLER PER SRM 53-01 FIG 4 SHEET 3. (M) 2 L 7 2 4F A6WE 2002021300124 20020213 00124 WP 2002 2 13 AALA20020013 1 20011221 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 429AA 49341 TUL - FOUND LEFT CUSP STATION 674-693 CORRODED. REMOVED CORRODED CUSP STATION 674-693, INSTALLED NEW CUSP SECTION PER S RM 53-01. (M) 2 L 7 2 4F A6WE 2002021300125 20020213 00125 WP 2002 2 13 AALA20020014 1 20011219 A 5345 BRACKET DOUG DC9 DC982 3022082 WP G2 GALLEY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 429AA 49341 TUL - FOUND LOWER AFT INBOARD MOUNT FOR G2 GALLEY HAS HEAVY CORROSION AT BOLT HOLE ON FORWARD SIDE OF FLOORBEAM. REMOVE D AND REPLACED CORRODED BRACKET WITH NEW SERVICEABLE BRACKET, TREATED AND PRIMED PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2002021300126 20020213 00126 WP 2002 2 13 AALA20020015 1 20011220 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 429AA 49341 TUL - FOUND DENT IN FUSELAGE STATION 427 AT CARGO DOOR. INSTALLED REPAIR DOUBLER SRM 53-09 FIG 12B. (M) 2 L 7 2 4F A6WE 2002021300127 20020213 00127 WP 2002 2 13 AALA20020016 1 20011214 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 429AA 49341 TUL - FOUND LONGERON 4L STATION 160 CRACKED AT FASTENER HOLE. INSTALLED 18 INCHES OF LONGERON SPLICE STATION INSTALLED NEW LONGERON STATION 160 FORWARD IAW SRM 53-02 FIG SHEETS 1, 45 AND 6. (M) 2 L 7 2 4F A6WE 2002021300128 20020213 00128 WP 2002 2 13 AALA20020017 1 20011218 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 429AA 49341 TUL - FOUND WORN AREA ON FUSELAGE FRAME AT BS 522 AT L6L. CUT OUT DAMAGE AND INSTALLED DOUBLER PLATE PER 53-03 FIG 4 SH EET 1 SRM. (M) 2 L 7 2 4F A6WE 2002021300129 20020213 00129 WP 2002 2 13 AALA20020018 1 20011218 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 429AA 49341 TUL - FOUND WORN AREA AT FUSELAGE FRAME AT STATION 636 AND LONGERON 6L. REMOVED DAMAGED SECTION AND INSTALLED DOUBLER R EPAIR PER SRM 5303 FIG 4 SHEET 1. (M) 2 L 7 2 4F A6WE 2002021300130 20020213 00130 WP 2002 2 13 AALA20020019 1 20011218 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 429AA 49341 TUL - FOUND LEFT HAND CUSP IS CORRODED AT STATION 1090 TO 1098. CUT OUT DAMAGE AREA AND INSTALLED CUSP REPAIR PER SRM 5 3-01 FIG 4. (M) 2 L 7 2 4F A6WE 2002021300131 20020213 00131 WP 2002 2 13 AALA20020020 1 20011218 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 429AA 49341 TUL - FOUND CRACK IN RIGHT CUSP STATION 275. REMOVED DAMAGED CUSP STATION 272-276. INSTALLED DOUBLER PER SRM 53-01. ( M) 2 L 7 2 4F A6WE 2002021300132 20020213 00132 WP 2002 2 13 AALA20020021 1 20011218 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 429AA 49341 TUL - FOUND LEFT CUSP CORRODED STATION 886-905. CUTOUT CORRODED AREA OF WEB, INSTALLED DOUBLER PER SRM 53-01 FIG 4. (M ) 2 L 7 2 4F A6WE 2002021300133 20020213 00133 WP 2002 2 13 AALA20020022 1 20011218 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 429AA 49341 TUL - FOUND SEAT TRACK NR 1 CORRODED STATION 1235-1240 AND STATION 1207-1211. REMOVED CORRODED AREAS, ACCOMPLISHED PLUS . REPAIR PER SRM 53-05 FIG 4A ON BOTH AREAS. (M) 2 L 7 2 4F A6WE 2002021300141 20020213 00141 WP 2002 2 13 AALA20020030 1 20011218 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 589AA 53252 TUL - FOUND SKIN DENTED RIGHT SIDE OF FUSELAGE, JUST AFT OF RADOME AND JUST BELOW SKIN BREAK. INSTALLED INTERNAL REPAIR DOUBLER PER SRM 53-04 PAGE 38. (M) 2 L 7 2 4F RT A6WE 2002021300142 20020213 00142 WP 2002 2 13 AALA20020031 1 20011210 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 589AA 53252 TUL - FOUND NR 1 SEAT TRACK CORRODED, UPPER SURFACE, OUTBOARD LEG AT STATION 1301. INSTALLED STRAP ON SEAT TRACK IAW AA RD 53-20-00-13, TREATED AND PRIMED, BLENDED AREA IAW 51-10-3. (M) 2 L 7 2 4F RT A6WE 2002021300143 20020213 00143 WP 2002 2 13 AALA20020032 1 20011207 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 589AA 53252 TUL - FOUND CORROSION ON SEAT TRACK UNDER TIE DOWN. CUT OUT CORROSION AREA AND INSTALLED PLUG REPAIR PER SRM 53-05 FIG 4A. (M) 2 L 7 2 4F RT A6WE 2002021300144 20020213 00144 WP 2002 2 13 AALA20020033 1 20011208 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 589AA 53252 TUL - FOUND CRACK IN FLOOR CUSP STATION 218 RIGHT .75 INCH. CUT OUT DAMAGE. INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 4-3. (M) 2 L 7 2 4F RT A6WE 2002021300145 20020213 00145 WP 2002 2 13 AALA20020034 1 20011207 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 589AA 53252 TUL - FOUND CORROSION ON SEAT TRACK NR 1. CUT OUT CORRODED AREA AND INSTALLED PLUG REPAIR PER 53-05 FIG 4A. (M) 2 L 7 2 4F RT A6WE 2002021300146 20020213 00146 WP 2002 2 13 AALA20020035 1 20011209 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 589AA 53252 TUL - FOUND CRACK IN FLOOR CUSP AT STATION 498 LEFT. ROUTED OUT CRACK, INSTALLED DOUBLER PER SRM 53-00-00. (M) 2 L 7 2 4F RT A6WE 2002021300147 20020213 00147 WP 2002 2 13 AALA20020036 1 20011210 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 589AA 53252 TUL - FOUND NR 1 SEAT TRACK CORRODED AT CLIP NUT HOLE INBOARD LEG STATION 1303. INSTALLED STRAP PER AARD 53-20-00-13. (M) 2 L 7 2 4F RT A6WE 2002021400007 20020214 00007 NM 2002 2 14 CA011227001 1 20011224 A 3260 82400033001 WIRE BOMBDR 82400033001 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NLG DOWLOCK BROKEN W L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 CA 29084 29084 (CAN) UPON GEAR DOWN SELECTION, NLG UNSAFE LIGHT ILLUMINATED, AIRCRAFT RETURNED TO DEPARTURE AIRPORT WITH GEAR SELECTE D DOWN, TURNING ONTO FINAL NLG GEAR DOWN ILLUMINATED, AIRCRAFT LANDED NORMALLY. INVESTIGATION FOUND INTERMITTANT NLG GEAR UNSAFE WARNING CAUSED BY WIRING FAULT IN NLG DOWNLOCK SENSOR CABLE ASSY. CABLE ASSY REPLACED, GEAR FUNCTION CHECK ED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002021400008 20020214 00008 NM 2002 2 14 CA011227003 1 20011226 A 3250 88521 FUSE LINK DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NLG FAILED W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA (CAN) ON DEPARTURE NOSE WHEEL STEERING U/S, AIRCRAFT RETURNED FOR NORMAL LANDING. INSPECTION FOUND FUSE LINK AND NLG C ENTERING MECHANISM DAMAGED. DAMAGE MAY HAVE OCCURRED DURING PRIOR GROUND MANOUVERING / HANDLING. NLG STEERING ACTUATOR , NLG CENTERING MECHANISM & FUSEABLE LINK REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002021400009 20020214 00009 NM 2002 2 14 CA011227004 1 20011226 A 2742 2460510H0480 HOSE BOEING 727 727227 1384078 NM PWA JT8 JT8D9A 52048 NE HYD SYSTEM RUPTURED W O OTHER K FLUID LOSS DE DESCENT 1 CA (CAN) ON DESCENT INTO YQM,FLIGHT CREW EXPERIANCED HYD SYSTEM "B" FLUID QTY DECREASING. UPON ARRIVAL, MAINTENANCE FOUND SYTEM "B" PUMP NR 2 HYDRAULIC HOSE ASSY IN SERVICE BAY FAILED, HOSE ASSY REPLACED, HYDRAULIC SYSTEM COMPONENTS INSPEC TED, AND FOUND B SYSTEM MODULE FILTER BOWL ALSO DAMAGED. BOWL ASSY REPLACED HYD SYSTEM SERVICED AND LEAK CHECKED. AIRC RAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2002021400010 20020214 00010 NE 2002 2 14 CA011227005 2 20011217 A 7314 30035681 FILTER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HP FUEL FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 99999 99999 (CAN) AFTER DEPARTURE , NR 2 FUEL PRESSURE CAUTION LIGHT ILLUMINATED, CREW UNABLE TO EXTINGUISH, AIRCRAFT RETURN TO D EPARTURE AIRPORT FOR NORMAL LANDING. NR 2 ENGINE HP FUEL FILTER REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002021400013 20020214 00013 NE 2002 2 14 CA011231004 2 20011218 A 7260 ENGINE BOEING 737 7372E3 NM PWA JT8 JT8D15 52051 NE NR 1 OR 2 FAILED W O OTHER Y J ENGINE STOPPAGE WARNING INDICATION AP APPROACH 1 CA (CAN) FLT NR 22 ON APPROACH INTO EDMONTON (YEG), FLT CREW REPORTED THEY HEARD & FELT VIBRATION FROM PEDESTAL AREA. AFTE R DEPLOYMENT OF THRUST REVERSERS ON LANDING ROLL, ENGINE SPOOLED TO 1.4 EPR & THEN FLAMED OUT. ABNORMAL ENGINE SHUTDOWN CHECKLIST CARRIED OUT, THE CREW TAXIED TO GATE & REPORTED INCIDENT TO MAINT. MAINT INSPECTION REVEALED POSSIBLITY OF E NGINE TOWER SHAFT FAILURE. MAINT ALSO FOUND METAL ON MAIN OIL SCREEN. DECISION MADE TO REPLACED ENGINE. ENGINE RUNS C ARRIED OUT WITH NO FAULTS FOUND. A/C RETURNED TO SERVICE WITH NO FURTHER INCIDENTS TO REPORT. 2 L 7 2 4F 4 F RT A16WE E2EA 2002021400021 20020214 00021 NE 2002 2 14 CA020103007 2 20011228 A 7230 ENGINE BOEING 727 727260 NM PWA JT8 JT8D17 52049 NE NR 3 FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 CA (CAN) NR 3 ENGINE SHUT DOWN IN FLIGHT DUE VIBRATION. REPAIR FACILITY EVALUATION: EXTENSIVE IMPACT DAMAGE WAS NOTED ON THE 7-12 STAGE STATOR VANES AND THE 7-13 STAGE BLADES. THIS DAMAGE APPEARS TO HAVE ORIGINATED FROM A FRACTURED 7 STAGE COMPRESSOR BLADE. THE ROOT CAUSE OF BLADE FRACTURE HAS NOT BEEN IDENTIFIED. HOWEVER THERE IS A POSSIBILITY THAT THE DAMA GE WAS INITIATED BY A LIBERATION OF A COUNTERWEIGHT(S) FROM THE C6 DISC. 2 L 7 3 4F 4 F RT A3WE E2EA 2002021400022 20020214 00022 EA 2002 2 14 CA020103008 1 20011219 A 5610 NP1393216 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF343B1 NE COCKPIT CRACKED W O OTHER O OTHER CR CRUISE 1 CA (CAN) DURING FLIGHT AT FL 190, THE RIGHT WINDSHILED CRACKED. RIGHT WINDSHIELD REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021400023 20020214 00023 EA 2002 2 14 CA020103009 1 20011216 A 2742 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE HORIZONTAL STAB FAILED W K NONE J WARNING INDICATION IN INSP/MAINT 1 CA (CAN) STAB TRIM / MACH TRIM WILL NOT STAY ENGAGED. REMOVED AND REPLACED THE HORIZONTAL STABILIZER COMPUTER. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021400024 20020214 00024 GL 2002 2 14 CA020103012 1 20011216 A 2721 682015 SWITCH BOMBDR BD700 BD7001A10 1390006 GL PWC 150 PW150A EA RUDDER TRIM CHAFED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) DURING A FLT A RUNAWAY RUDDER TRIM TO RIGHT SIDE OCCURRED IMMEDIATELY AFTER TAKEOFF, A/C MADE AN IN FLT RETURN TO BASE.FAULT CONFIRMED ON GROUND. RUDDER WOULD CONTINUALLY TRIM TO RIGHT, COULD BE CORRECTED BY SELECTING LEFT RUDDER TRIM BUT AS SOON AS TRIM SW WAS RELEASED RUDDER TRIM WOULD MOVE TO RIGHT. AILERON/RUDDER TRIM CNTL PANEL (P/N: 82410608005) NOT AVAIL ABLE BUT FOUND A RUDDER TRIM SWITCH (P/N:68-2015) IN STOCK. DURING REPL OF RUDDER TRIM SWITCH, A WIRE FROM TER MINAL "6" OF SWITCH FOUND TO HAVE CHAFFED ON ONE OF COMMON GROUND TERMINA L ON SMAE SWITCH. NEW RUDDER TRIM SWITCH INST & RETURN TO SERVICE CHECKS CARRIED OUT SUCCESSFULLY. 2 L 7 2 4F 4 T RT T00003NY E00062EN 2002021400026 20020214 00026 CE 2002 2 14 CA020103014 1 20011226 A 3260 BEPBA07GBP BULB LEAR 35 35LEAR 5170600 CE GARRTT TFE731 TFE73122B 01518 WP MLG INDICATOR BURNED OUT W O OTHER N FALSE WARNING AP APPROACH 1 CA (CAN) CREW DECLARED EMERGENCY LANDING, DUE TO A INOPERATIVE NOSE LANDING GEAR SAFE LIGHT. UPON INSPECTION BY MAINTENA NCE PERSONNEL, LAMP WAS FOUND TO BE BURNED. THE LAMP WAS REPLACED AND THE SYSTEM WAS FOUND SERVICEABLE. 2 L 7 2 4F 4 F A10CE E6WE 2002021400036 20020214 00036 2002 2 14 CA020103015 4 20011211 A 8300 JT89A GEARBOX BOEING 737 737210C 1384459 NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE LEAKING W E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 CA 47323 (CAN) IN CRUISE CREW NOTED LOW OIL PRESSURE LIGHT ILLUMINATED ON NR 2 ENGINE. OIL PRESS DECREASING TO 35 PSI & OIL QUAN TITY FALLING. CREW SHUTDOWN ENGINE DECLARED EMERGENCY & PROCEEDED TO LAND AT NEAREST AIRPORT WHICH DESTINATION AIRPORT. THE LDG W/O INCIDENT. AME ASSIGNED TO A/C WHO ON FLT FOUND THAT NR 2 ENGINE ACCESSORY GEABOX LP 5 PORT THREADS FAILED & ALLOWED PRESSURIZED ENGINE OIL TO ESCAPE. ENGINE OIL FILTER REMVD FOR INSP AND NO CONTAMINATION FOUND. 2 L 7 2 4F 4 F A16WE E2EA 2002021400076 20020214 00076 WP 2002 2 14 AALA2002047 1 20011219 A 5320 STIFFENER DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70524 49916 TUL - FOUND CORNER STIFFENER CORRODED ON FORWARD SIDE OF STATION 1212 FRAME AT LOWER AFT CORNER OF CARGO DOORWAY. REMOV ED CORROSION BLENDOUT BEYOND MM LIMITS. REMOVED AND REPLACED FITTING PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2002021400087 20020214 00087 WP 2002 2 14 AALA2002052 1 20011218 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70524 49916 TUL - FOUND LONGERON 4 LEFT STATION 160 CRACKED AT BELT FRAME ATTACH HOLES. REMOVED CRACKED LONGERON SECTION AND SPLICE IN NEW SECTION PER SRM 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 2002021400092 20020214 00092 NM 2002 2 14 ASAA0110585 1 20010921 A 3350 8731002142 LIGHT BOEING 737 737298C 1384490 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 ANC - DURING MAINTENANCE CHECK, FOUND EXIT TO REAR SIGN ON SMOKE BARRIER INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMB LY, LIGHT FUNCTION NORMAL. (M) 2 L 7 2 4F RT A16WE 2002021400093 20020214 00093 NM 2002 2 14 ASAA0110586 1 20010923 A 3350 886210044 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT AT LEFT AND RIGHT OVERWING EXIT DOORS INOPERATIVE. REMOVED A ND REPLACED REMOTE ASSEMBLY BATTERIES AND BOTH SIGNS OPERATED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002021400094 20020214 00094 NM 2002 2 14 ASAA0110592 1 20011002 A 3397 8631001 WIRE BOEING 737 7372X6C 1384552 NM CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE. SECURED LOOSE WIRE THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002021400095 20020214 00095 NM 2002 2 14 ASAA0110593 1 20011005 A 3350 8631001 LIGHT BOEING 737 737210C 1384459 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 JNU - DURING MAINTENANCE CHECK, FOUND RED EMERGENCY FLOOR TRACK LIGHTS IN AFT CABIN INOPERATIVE. REMOVED AND REPLACED L IGHT ASSEMBLY THEN LIGHTS OPERATED NORMAL. (M) 2 L 7 2 4F A16WE 2002021400096 20020214 00096 NM 2002 2 14 ASAA0110653 1 20011210 A 5242 6545830 SKIN BOEING 737 737298C 1384490 NM E/E BAY DOOR GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND E/E DOOR SKIN AT BODY STATION 337, STRINGER 27R GOUGED. REPAIRED DOOR SKIN PER SR M. (M) 2 L 7 2 4F RT A16WE 2002021400097 20020214 00097 NM 2002 2 14 ASAA0110654 1 20011210 A 5315 6545810 FLOORBEAM BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BODY STATION 312, WATERLINE 208 CORRODED. REPAIRED FLOORBEAM PER SRM . (M) 2 L 7 2 4F RT A16WE 2002021400098 20020214 00098 NM 2002 2 14 ASAA01400101 1 20010906 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 754AS 25095 SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOP AT ROW 14-18. RECONNECTED WIRES, OPS CHECK NORMAL. (M ) 2 L 7 2 4F RT A16WE 2002021400099 20020214 00099 NM 2002 2 14 ASAA01400103 1 20010911 A 3397 81000022608 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 769AS 25103 SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 13-17. RECONNECTED WIRES, OPS CHECK NORM AL. (M) 2 L 7 2 4F RT A16WE 2002021400100 20020214 00100 NM 2002 2 14 ASAA01400106 1 20010924 A 3350 8100022607 LIGHT BOEING 737 7374Q8 138447Q NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 756AS 25097 JNU - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 13-17. REMOVED AND REPLACED LIGHT ASSEMB LY, OPERATIONAL CHECKS NORMAL. (M) 2 L 7 2 4F RT A16WE 2002021400101 20020214 00101 NM 2002 2 14 ASAA01400110 1 20011005 A 3350 8100022607 LIGHT BOEING 737 7374Q8 138447Q NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 774AS 25107 JNU - DURING LINE CHECK, FOUND LAST TWO EMERGENCY LIGHTS INOPERATIVE (RED). REMOVED AND REPLACED ONE SECTION OF EMERGEN CY TRACK LIGHTS AT AFT CABIN CLOSET TO GALLEY. OPERATIONAL CHECKED GOOD. (M) 2 L 7 2 4F RT A16WE 2002021400102 20020214 00102 NM 2002 2 14 ASAA0140169 1 20011210 A 5315 6546568191 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 PAE - DURING SI CHECK, FOUND FLOORBEAM AT BS 1016, LBL 29 AND WL 208 IS CORRODED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2002021400103 20020214 00103 NM 2002 2 14 ASAA0140170 1 20011210 A 5330 6546881166 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 PAE - DURING SI CHECK, FOUND CRACK ON FORWARD APU DOOR HINGE CUTOUT. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2002021400104 20020214 00104 NM 2002 2 14 ASAA0140171 1 20011210 A 5315 65C3394319 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 PAE - DURING SI CHECK, FOUND CORROSION ON FLOORBEAM AT STATION 344, LBL 60 AND WL 206. REPAIRED IAW EA. (M) 2 L 7 2 4F RT A16WE 2002021400106 20020214 00106 NM 2002 2 14 ASAA0140172 1 20011210 A 5315 65C3394311 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 PAE - DURING SI C-CHECK, FOUND CORROSION ON TOP OF FLOORBEAM AT BS 344, LBL 17 TO 43. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2002021400107 20020214 00107 WP 2002 2 14 ASAA0180246 1 20010820 A 3350 0105606 MODULE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 934AS 49235 LAX - DURING LINE CHECK, AN EMERGENCY FLOOR TRACK LIGHTING MODULE WAS FOUND TO BE INOPERATIVE. REPAIRED LIGHT MODULE SO CKET PER SRM 20-10-03. REPLACED BULB IN MODULE. LIGHT THEN OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 2002021400108 20020214 00108 WP 2002 2 14 ASAA0180247 1 20010820 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 SEA - DURING LINE CHECK, EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE AT ROWS 20-24. RECONNECTED MODULES AT ROW 24. LIGHT THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2002021400109 20020214 00109 WP 2002 2 14 ASAA0180248 1 20010821 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 ANC - DURING PREFLIGHT CHECK, EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE IN 1ST CLASS CABIN. RECONNECTED LOOSE LIGH T MODULES. LIGHT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002021400110 20020214 00110 WP 2002 2 14 ASAA0180249 1 20010822 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 SEA - DURING SERVICE CHECK, EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE AT SEAT 1 IN 1ST CLASS. RECONNECTED LOOSE LI GHT MODULE. LIGHT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002021400111 20020214 00111 WP 2002 2 14 ASAA0180250 1 20010823 A 3350 0105606 SPLICE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 954AS 49387 OAK - DURING C-CHECK, EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE FROM ROW 27 BACK. REPLACED DAMAGED CRIMP SPLICE. LIGHT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2002021400112 20020214 00112 WP 2002 2 14 ASAA0180251 1 20010823 A 3350 0105606 SPLICE DOUG DC9 DC982 3022082 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 933AS 49234 SAN - DURING PREFLIGHT CHECK, EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE FROM ROW 6 FORWARD. RESECURED LOOSE SPLICE . LIGHT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2002021400113 20020214 00113 WP 2002 2 14 ASAA0180252 1 20010824 A 3350 0105606 SOCKET DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 SEA - DURING PREFLIGHT CHECK, FIRST FIVE EMERGENCY FLOOR TRACK LIGHTS WERE DETERMINED TO BE INOPERATIVE. REPLACED DEFEC TIVE LIGHT MODULE SOCKET. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002021400114 20020214 00114 WP 2002 2 14 ASAA0180253 1 20010827 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP CABIN NOT SEATED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 977AS 53453 SEA - DURING PREFLIGHT CHECK, EMERGENCY FLOOR TRACK LIGHT WAS DETERMINED TO BE INOPERATIVE. RESEATED LIGHT MODULE. LIG HT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002021400117 20020214 00117 WP 2002 2 14 ASAA0180254 1 20010827 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 931AS 49232 SFO - DURING LINE CHECK, EMERGENCY LIGHTS IN TAIL AREA WERE DETERMINED TO BE INOPERATIVE. REPLACED DEFECTIVE BATTERY PA CK ASSEMBLY. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2002021400118 20020214 00118 WP 2002 2 14 ASAA0180255 1 20010828 A 3350 0105610 MODULE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 LAX - DURING PREFLIGHT CHECK, FOUND FOUR EMERGENCY TRACK LIGHTS JUST AFT OF FORWARD GALLEY INOPERATIVE. RECONNECTED LIG HT MODULE AT ROW 1. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002021400119 20020214 00119 WP 2002 2 14 ASAA0180256 1 20010829 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 ANC - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTS IN FORWARD CABIN TO BE INOPERATIVE. REPLACED DISCHARGED BATTERY P ACK ASSEMBLY. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002021400120 20020214 00120 WP 2002 2 14 ASAA0180259 1 20010908 A 3350 0105610 MODULE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 948AS 53021 SFO - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS FROM ROW 1 TO 3 INOPERATIVE. RECONNECTED LIGHT MODULE. LIGH TS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2002021400121 20020214 00121 WP 2002 2 14 ASAA0180260 1 20010909 A 3350 0105610 RECEPTACLE DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 960AS 53074 SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROW 2 AND 10. RELAMPED AT ROW 2 AND REPLACED RECEPTACLE AT ROW 10. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002021400122 20020214 00122 WP 2002 2 14 ASAA0180262 1 20010910 A 2611 PU90431R3 SMOKE DETECTOR DOUG DC9 DC983 3022083 WP LAVATORY MALFUNCTIONED A ASAA K NONE N FALSE WARNING CR CRUISE 1 NM 01 943AS 53018 SEA - DURING FLIGHT, AFT LEFT LAVATORY SMOKE DETECTOR WENT OFF ALTHOUGH NO SMOKE WAS EVIDENT. REPLACED SMOKE DETECTOR. OPS CHECKED OK. (M) 2 L 7 2 4F RT A6WE 2002021500010 20020215 00010 NE 2002 2 15 CA020104009 2 20011206 A 7321 ENGINE BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE LT OR RT STALLED W C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 CA 73701 73701 (CAN) ON TAKE OFF OUT OF WHITEHORSE, FLIGHT CREW EXPERIENCED COMPRESSOR STALL. ENGINE THROTTLE BACK TO IDLE, ENGINE N ORMAL, ADVANCED THROTTLE AND STALLED AGAIN. FLIGHT CREW ELECTED TO RETURNED TO WHITEHORSE. ENGINE TRIM RUN CARRIED OUT. IDLE AND EPR ADJUSTED AS PER AMM. 2 L 7 2 4F 4 F A16WE E2EA 2002021500013 20020215 00013 EU 2002 2 15 CA020104015 1 20011210 A 2750 CONTROL UNIT AIRBUS A340 A340313 EU CFMINT CFM56 CFM565C4 13802 NE TE FLAPS FAILED W L ABORTED APPROACH F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 CA (CAN) MISSED APPROACH IN HONG KONG DUE TO FLAP PROBLEM. AIRCRAFT DID A FLAPLESS LANDING CLASS 1 F/CONTROL FLAPS FAULT-E CAM COMPLETED, RECYCLED. FLAPS INSPECTED AND FOUND RT SYSTEM TORQUE LIMITER 5081 CV AND RT INPUT GEARBOX TORQUE LIMITER 5120 CV POPPED. BOTH TORQUE LIMITERS RESETTED. SYSTEMS SERVICEABLE. 2 L 7 4 4F 4 F RT A197 E37NE 2002021500015 20020215 00015 NM 2002 2 15 CA020104016 1 20011120 A 2720 SERVO AIRBUS A319 A319114 3930350 NM CFMINT CFM56 CFM565A1 NE RUDDER CONTROL FAILED W O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 CA (CAN) LOST OF GREEN HYDRAULIC SYSTEM ON DESCENT TO LOS ANGELES. YAW DAMPER SERVO REPLACED AND TESTED AS PER AMM 27-26-5 1. AIRCRAFT SERVICEABLE. 2 L 7 2 4F 4 F RT A28NM E29NE 2002021500016 20020215 00016 NE 2002 2 15 CA020104018 2 20011120 A 7200 SEAL AIRBUS A340 A340313 EU CFMINT CFM56 CFM565C4 13802 NE NR 3 ENGINE LEAKING W E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 CA (CAN) APPROX. 1 HOUR AFTER TAKE OFF, NR 3 OIL QUANTITY INDICATED AMBER, NR 3 OIL PRESSURE WENT INTO RED (6PSI) ACCOMPAN IED BY ECAM ADVISING TO SHUT DOWN ENGINE. AIRCRAFT RETURNED TO VANCOUVER. FOUND NR 3 ENGINE STARTER DRIVE SEAL LEAKING. SEAL REPLACED AND GROUND RUN CARRIED WITH NO LEAKS. AIRCRAFT SERVICEABLE. 2 L 7 4 4F 4 F RT A197 E37NE 2002021500038 20020215 00038 CE 2002 2 15 CA020109003 1 20011208 A 3297 WIRE BEECH B300 B300B350C CE PWA PT6 PT6A60A 52043 NE SAFETY SOLENOID SHORTED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) UPON TAKEOFF, WHEN BRAKING GROUND, THE LANDING GEARS CONTROL 2 AMP BRAKER WOULD POP. WHEN GEAR WAS SELECTED UP, THE GEAR WOULD NOT RETRACT, THE AIRCRAFT RETURNED TO THE HANGAR. THE GEAR SELECT SWITCH ASSEMBLY WAS INSPECTED. THE POWER WIRE TO THE SAFETY SOLENOID WAS SHORTED TO GROUND. 2 L 7 2 4T 4 T RT A24CE E4EA 2002021500043 20020215 00043 NM 2002 2 15 CA020110002 1 20011224 A 7931 FT104Y TRANSMITTER BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE OIL PRESSURE FAILED W A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 CA (CAN) ENGINE NR 1 OIL PRESSURE DROPPED TO 20 PSI AFTER TAKEOFF. ENGINE FAILURE AND SHUT DOWN COMPLETED. AIRCRAFT RETURN ED TO VANCOUVER. OIL PRESSURE TRANSMITTER REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 2002021500044 20020215 00044 EA 2002 2 15 CA020110004 1 20011224 A 2150 78279013 ACM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LT PACK FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CA (CAN) LT PACK FAULT WITH SMOKE IN COCKPIT, NO OVERHEAT OBSERVED. PACK WAS IN AUTO MODE. PACK SELECTED OFF AND SMOKE CLE ARED. LT AIR CYCLE MACHINE AND COALESCER BAG REPLACED AS PER AMM. SYSTEM SERVICEABLE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021500090 20020215 00090 WP 2002 2 15 CA020111002 1 20011209 A 7830 LJ24295 BLOCKER DOOR LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE NR 2 ENGINE BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) FOUND NR 2 ENGINE NOZZLE COLLECTOR DAMAGED, ONE BLOCKER DOOR MISSING. BLOCKER DOOR BROKEN IN TWO PIECES AT HINGE AND ONE PIECE DAMAGE NOZZLE COLLECTOR, RT BLISTER FAIRING, ACCOUSTIC TRAY NR 1 AND FAIRING 438 DR . 2 L 7 3 4F 4 F A23WE E12EU 2002021500096 20020215 00096 NM 2002 2 15 CA020114003 1 20011205 A 3320 404810 SOCKET DHAV DHC8 DHC8* NM PWC 150 PW150A EA LIGHTS BURNED W K NONE L NO TEST IN INSP/MAINT 1 CA (CAN) FLUORESCENT TUBE HOLDER FOUND OVERHEATED AND BURNT. THE ELECTRICAL CONTACT AND SURROUNDING MATERIAL HAS BEEN OVER HEATED WITH SUBSEQUENT BURNING / MELTING OF THE CONTACT SUPPORT STRUCTURE. UNIT REPLACED. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002021500098 20020215 00098 NE 2002 2 15 CA020114006 2 20011206 A 7260 39700911 DRIVE SHAFT BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE ACCESSORY G/B FAILED W E ENGINE SHUTDOWN Y J ENGINE STOPPAGE WARNING INDICATION DE DESCENT 1 CA (CAN) ENROUTE ATL / DFW, ON TOP OF DESCENT. AT 33,000 FT HAD FOLLOWING: QTE MASTER CAUTION ILLUMINATED FOLLOWED BY A/C YAW AT 33,000 FT. LEFT ENGINE SHUTDOWN (AUTO) SUDDENLY. RED BOXED NR WERE VISIBLE, OIL PRESSURE & OIL FILTER LEVEL 2 AL ERTS WERE ALSO NOTICED, CHECK LIST WERE ACCOMPLISHED FOR ENGINE FAILURE (FIRE BOTTLE WAS NOT ON CHARGED) & A/C LANDED W ITH LEFT ENGINE SHUTDOWN, WITH N O FURTHER PROBLEMS. FINDING: GEARBOX FAILURE, 3 HOLES IN AGB1) AFT FACT OF AGB HOLE 2 X 2 INCH IN BETWEEN IDG & EMPU NEAR TOP OF AGB.2) BOTTOM OF AGB HOLE 2 1/2 X 1/2 INCHES UNDER STARTER. 3) FRONT FACE LAR GE HOLE 2 X 3 I LEFT SIDE OF STARTER.ALL VISIBLE GEARS DAMAGED. 2 L 7 2 4F 4 F TR A6WE E00061EN 2002021500116 20020215 00116 WP 2002 2 15 GTIA012060 1 20011217 A 3260 DT2RA7 SWITCH DOUG DC9 DC981 3022081 WP COCKPIT FAULTY A GTIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 01 806NK 48051 FLT 503 - MCO - AFTER GEAR RETRACTION 3 RED LIGHTS (GEAR), AS PER QRH EXTEND GEAR/RETRACT 3-RED LIGHTS REMAIN GEAR APPEA RS TO BE UP FLEW REMAINDER OF FLT 7 MACH/300 KNOTS. FOUND LANDING GEAR CONTROL LEVER SWITCH TO BE AT FAULT. REMOVED AN D REPLACED SAME PER MM CH 32-60-01. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2002021500118 20020215 00118 2002 2 15 GTIA012167 4 20011231 A 2230 THROTTLE DOUG DC9 DC983 3022083 WP COCKPIT LACK OF LUBE A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 809NK 49503 TPA - FLT 639 - FOUND LEFT AUTO THROTTLE STICKING. LUBE LEFT THROTTLE IN PEDESTAL, PERFORM AUTO THROTTLE SYSTEM CHECK. SYSTEM CHECKS GOOD IAW MD80 MM 22-31-00. (M) 2 L 7 2 4F RT A6WE 2002021500119 20020215 00119 NM 2002 2 15 GTIA012168 1 20011227 A 2761 1040T1005 ACTUATOR DOUG MD80 MD83 3023681 NM SPOILER FAULTY A GTIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 23 822NK 49392 FLL - FLT 779 - FLIGHT SPOILERS WILL NOT STAY IN ANY DETENT. REMOVED AND REPLACED SPOILER AUTOMATIC ACTUATOR, OPS CHECK ED NORMAL IAW MM 27-62-05. (M) 2 L 7 2 4F RT 2002021500121 20020215 00121 WP 2002 2 15 GTIA012171 1 20011126 A 5230 DOUBLER DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - AFT LOWER CARGO, CARGO DOOR OUTBOARD LOWER CORNER DOUBLER PREVIOUS REPAIR CRACKED/WORN-OUT. REMOVED DAMAGE AREA. FORMED REPAIR. INSTALLED REPAIR IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002021500122 20020215 00122 WP 2002 2 15 GTIA012172 1 20011106 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND STATION 231 L17-18 LEFT, DENT IN SKIN. FORMED INTERNAL DOUBLER. INSTALLED DOUBLER IAW MD80 SRM 53-04. (M) 2 L 7 2 4F A6WE 2002021500123 20020215 00123 WP 2002 2 15 GTIA012173 1 20011106 A 5712 RIB DOUG DC9 DC932 3022066 WP RT WING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND RIGHT SIDE, FUSELAGE AREA, INBOARD OF NR 1 SLAT HAS A VERTICAL RIB, BENT AND CRACKED. REMOVED DAMAGED RIB. FORMED NEW RIB. HEAT TREATED RIB TO T-6 CONDITION. INSTALLED FORMED RIB IAW DC9 SRM 51-30-3. (M) 2 L 7 2 4F A6WE 2002021500124 20020215 00124 WP 2002 2 15 GTIA012174 1 20011204 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND FLOORBOARD WEB HAS HOLE Y211-X27. REMOVED DAMAGE. FABRICATED REPAIR PARTS FILLER AND DOUBLER. INSTALLED P ER DC9 SRM 53-01. (M) 2 L 7 2 4F A6WE 2002021500125 20020215 00125 WP 2002 2 15 GTIA012175 1 20011201 A 5230 RETAINER DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FORWARD CARGO DOOR HAS TWO CRACKS AT RETAINER MOUNT HOLE 2 INCHES BELOW UPPER AFT CORNER. FABRICATED REPAIR DOUBLERS. INSTALLED DOUBLERS IAW DC9 SRM 52-01. (M) 2 L 7 2 4F A6WE 2002021500126 20020215 00126 WP 2002 2 15 GTIA012176 1 20011202 A 5754 ANGLE DOUG DC9 DC932 3022066 WP L/E SLAT CHAFED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND NR 3 RIGHT SLAT OUTBOARD LOWER CHORD ANGLE CHAFFED MORE THAN 50 PERCENT OF MATERIAL THICKNESS. FORMED NEW C HORD ANGLE. INSTALLED FASTENERS IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002021900001 20020219 00001 EU 2002 2 19 CA020104005 1 20011228 A 3222 AIR123300 STRUT SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R389 R3894123F25 NE NLG LOW W O OTHER J WARNING INDICATION CL CLIMB 1 CA (CAN) UPON SELECTION OF LANDING GEAR AFTER DEPARTURE, GEAR IN TRANSIT LIGHT ILLUMINATED INDICATING THAT 1 OF 3 GEAR NOT IN UP & LOCKED POSITION. CREW CARRIED OUT PROCEDURES AS PER AFM WITH NO CHANGE. GEAR SELECTED TO DOWN & 3 GREEN OBTAINED . IN PROP SPINNER CREW NOTICED THAT NOSE WHEELS DID NOT APPEAR TO BE CENTERED. CONSULTATION WITH OPS & MAINTENANCE DECID ED TO ROUTE A/C TO YYT & NOT INTENDED DESTINATION. CONSULTATION WITH SAAB ENGINEERING ADVISED THAT NOSE WHEELS WOULD CEN TER IMMEDIATELY UPON TOUCH-DOWN. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P30NE 2002021900040 20020219 00040 NM 2002 2 19 AWXA200200136 1 20010201 A 5311 GS47973 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 YVR - MAJOR REPAIR -C- DURING C-13 CHECK A 1 INCH CRACK WAS FOUND WHERE FLOOR SUPPORT L-ANGLE ATTACHES TO BELT FRAME AND FLOORBEAM AT BS 639, WL 208. MAINTENANCE REMOVED DAMAGED SECTION OF INNER CHORD; FABRICATED NEW SECTION OF INNER CHORD AND SPLICE PARTS; INSTALLED REPAIR IAW IAW B737-300 SRM 51-70-12, FIG 1 PG 1, DWG 65-47973, SRM 51-40-02, PG 3 AND TELE X AWM-YVR-02-00017H. 2 L 7 2 4F RT A16WE 2002021900072 20020219 00072 2002 2 19 CA020117014 4 20011222 A 2210 707603400 GYRO LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE AUTOPILOT SYS FAILED W O OTHER E VIBRATION/BUFFET CL CLIMB 1 CA (CAN) ON DEPARTURE FROM AUA - YYZ, A MODERATELY STEADY LATERAL AIRFRAME OSCILLATION ( AT APPROXIMATE RATE OF TWO PER SE COND) STARTED AT 180 KNOTS / 2100 FT ABOVE SEA LEVEL / FLAPS 4 DEGREES. IT STOPPED ONLY WHEN POWER WAS REDUCED TO 1.4 EP R AT 5100 FT ABOVE SEA LEVEL / 260 KNOTS / FLAPS 0 DEGREES. ALL FLIGHT CONTROLS (SURFACE POSITION INDICATOR), HYDRAULIC (QTY.+ PRESS.) AND ENGINE (RPM.TGT,VIB+OIL SYST.)INDICATIONS NORMAL. AUTOPILOT OFF. CABIN CREW REPORTED OSCILLATIONS WE RE FELT THROUGHOUT THE CABIN.- NR 1 YAW RATE GYRO WAS REPLACED IN ACCORDANCE WITH M.M. 22-15-02. 2 L 7 3 4F 4 F A23WE E12EU 2002021900100 20020219 00100 NM 2002 2 19 01FDEA01118 1 20010822 A 2612 DUCT BOEING 727 727247 138408F NM A FDEA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 236FE 21330 N1275 TEST FLT LWR AFT CARGO SMOKE WARN @ FL 230 HAD ENGINE & WING ANTI ICE TURNED ON, WENT OUT WHEN PWR WAS REDUCED . S/D TESTED TAI & ENG ANTIICE, CND WORK DONE PER SRM 20-50-01, MM 30-13-000-5 & 30-21-001-5. 2 L 7 3 4F A3WE 2002021900107 20020219 00107 NM 2002 2 19 01FDEA00349 1 20010515 A 2780 SWITCH BOEING 727 72722C 138400F NM LEAD EDGE FLAP INOPERATIVE A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 112FE 19890 01-155 ON DEPART WHEN FLAP 2 DEG SEL ON RETRACTION LIGHT ON FWD PNL FLAP/SLAT IND REMAIN AMBER. FND L/E FLAP OVERRIDE T EST SWITCH IN OVERRIDE POS, RETURN TO NORM POSITION, OPS CK GOOD PER 727 MM 27-81-000-6. 2 L 7 3 4F A3WE 2002021900114 20020219 00114 NM 2002 2 19 01FDEA00229 1 20010324 A 5531 SUPPORT FITTING BOEING 727 72722 1384002 NM VERT REAR SPAR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 168FE 18865 N 650 DUR ROUTINE INSP, UPR AND LWR LUGS OF THE UPR RUDDER ROD SUPPORT FITTING LOCATED ON THE VERTICAL STABILIZER REAR SPAR FND CRACKED. ** S/D ** HFEC IND NO CRACKS PER IAW 727 NDT MANUAL PART 6. 2 L 7 3 4F A3WE 2002021900115 20020219 00115 NM 2002 2 19 01FDEA00227 1 20010324 A 5310 SKIN BOEING 727 72722 1384002 NM BS 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 168FE 18865 N 164 DUR ROUTINE INSP, FUSELAGE SKIN FND CORRODED AT BS 400, STR 3R AND 4R. ** S/D ** STRIPPED AREA. LFEC IND NO C ORROSION LOSS PER LOSS IAW 727 NDT MANUAL PART 6. TREATED, PRIMED AND REPAIR PER IAW BAC 727 SRM 51-20-151-7. 2 L 7 3 4F A3WE 2002021900116 20020219 00116 NM 2002 2 19 01FDEA00215 1 20010319 A 5310 6556117 FRAME BOEING 727 727233 138408A NM BS 720E DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 NR N 934 DRILL START IN FRAME BS 720E, STR 7LH. ** S/D ** R&R & FAB & ALODINED & PRIMED PER FEDEX SRM 53-10-4 FIG 2 . 2 L 7 3 4F RT A3WE 2002021900117 20020219 00117 NM 2002 2 19 01FDEA00138 1 20010217 A 2840 FUEL TANK DOUG MD11 MD11F 3023600 NM #2 ENGINE FLAMED OUT A FDEA O OTHER X ENGINE FLAMEOUT UK UNKNOWN 1 SO 25 604FE 48460 01-051 #2 ENG FLAMED OUT ABOUT 1 PLUS 15 MIN OUT OF LAX. #2 TANK WAS FUELED TO KNOW QTY DUE TO INOP FUEL IND THE ENG W AS RESTART WITH FUEL CROSSFEED. FUEL SLIP RECK AND SHOW RELEASE FUEL HOWEVER #2 WAS UNDERFUELED BY 20,000 #. THE FUEL C REW DEBRIEF- #2 TANK RAN DRY CAUSING FLAMEOUT. NO MAINT ACTION REQD INF NOTED. ** S/D ** COMING 2 L 7 3 4F RT A22WE 2002021900118 20020219 00118 WP 2002 2 19 01FDEA00121 1 20010214 A 5230 DOOR DOUG DC10 DC1030F 3023504 WP MAIN CARGO DAMAGED A FDEA D RETURN TO BLOCK O OTHER NR NOT REPORTED 1 SO 25 319FE 47820 SNRM N-1 A/C STRIKE MAIN CARGO DOOR AQS/LAX NOTE: A/C MAIN CARGO DOOR DAMAGED IN OAKLAND AND FERRIED TO LAX FOR REPAIRS . ** S/D ** R&R DOOR PER EA 8-5230-49684 AND SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2002021900121 20020219 00121 WP 2002 2 19 GTIA012183 1 20011107 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND STATION 1143 L16, 2.5 L CREASE IN SKIN AFT OF FRAME, 2 INCH LONG SCRATCH FORWARD OF FRAME. FORMED DOUBLER I AW DC9 SRM 53-04. INSTALLED DOUBLER IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002021900122 20020219 00122 WP 2002 2 19 GTIA012188 1 20011112 A 5313 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47114 FTW - FOUND LONGERON 12R CRACKED AT FUSELAGE FRAME STATION Y=945. REMOVED CRACKED LONGERON. FABRICATED DRILLED AND LOC ATED NEW LONGERON AND SPLICE. INSTALLED NEW LONGERON AND SPLICE. (M) 2 L 7 2 4F A6WE 2002021900148 20020219 00148 WP 2002 2 19 GTIA012177 1 20011114 A 5320 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND WEB CRACKED AT LEFT FORWARD ENTRY DOOR JAMB AREA STA Y-208, Z=26, X63. CUT OUT DAMAGED AREA. FABRICATE NEW DOUBLER AND FILLER. INSTALLED NEW DOUBLER AND FILLER IAW DC9 SRM 53-01. (M) 2 L 7 2 4F A6WE 2002021900149 20020219 00149 WP 2002 2 19 GTIA012178 1 20011114 A 5320 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND WEB CRACKED AT LEFT FORWARD ENTRY DOOR JAMB AREA, STA Y-208, X-51, X=63. REMOVED CRACK FROM WEB. FABRICATE D FILLER AND DOUBLER. INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 2002021900150 20020219 00150 WP 2002 2 19 GTIA012179 1 20011115 A 5230 STRUCTURE DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FORWARD LOWER CARGO DOOR PANE CRACKED, APPROX 3 INCHES, AT LOWER FORWARD STOP FITTING. STOP DRILLED CRACK. FABRI CATED REPAIR DOUBLER. INSTALLED REPAIR ANGLE DOUBLER PER DC9 SRM 51-10-3. (M) 2 L 7 2 4F A6WE 2002021900151 20020219 00151 WP 2002 2 19 GTIA012180 1 20011115 A 5230 STRUCTURE DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FORWARD LOWER CARGO DOOR PANEL CRACKED APPROXIMATELY .75 INCH AT UPPER AFT STOP FITTING AREA. STOP DRILLED CRACK. FABRICATED OUTER FLANGE DOUBLER. INSTALLED REPAIR DOUBLER AND INTERCOSTAL PER DC9 SRM 53-02. (M) 2 L 7 2 4F A6WE 2002021900152 20020219 00152 WP 2002 2 19 GTIA012181 1 20011112 A 5310 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND FRAME TO SKIN CLIP CRACKED AT FUSELAGE FRAME STA Y-980 ADJACENT TO LONGERON 14L. REMOVED EXISTING REPAIR CL IP. FORMED NEW CLIP. INSTALLED IAW DC9 RM 51-30-2. (M) 2 L 7 2 4F A6WE 2002021900153 20020219 00153 WP 2002 2 19 GTIA012182 1 20011203 A 5754 ANGLE DOUG DC9 DC932 3022066 WP L/E SLAT CHAFED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 NR 4 SLAT RIGHT CHORD ANGLE CHAFFED MORE THAN 50 PERCENT THICKNESS OF MATERIAL. REMOVED CHAFFED ANGLE. FABRICATED NEW CHORD ANGLE. INSTALLED NEW CHORD ANGLE IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002021900154 20020219 00154 WP 2002 2 19 GTIA012184 1 20011114 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP COCKPIT WORN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CAPTAIN SEAT TRACKS ARE WORN. REMOVED UPPER DAMAGED TRACKS. FORMED NEW TRACK. INSTALLED CAPTAINS SEAT TRA CKS IAW DC9 SRM 51-30-1. (M) 2 L 7 2 4F A6WE 2002021900155 20020219 00155 WP 2002 2 19 GTIA012185 1 20011113 A 5330 SKIN PANEL DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND FORWARD SKIN PANEL CRACKED AT TWO FASTENER LOCATIONS BETWEEN LONGERON 2 LEFT AND 3 LEFT. FORMED NEW REPAIR DOUBLERS. INSTALLED REPAIR DOUBLER PER DC9 SRM. (M) 2 L 7 2 4F A6WE 2002021900156 20020219 00156 WP 2002 2 19 GTIA012186 1 20011112 A 5313 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FOUND LONGERON 13L CRACKED AT FUSELAGE FRAME STATION Y=965. REMOVED LONGERON. FORMED LONGERON AND SPLICE. INSTALLED L ONGERON 13 ON STATION 965 2ND SPLICE PER DC9 30 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002021900157 20020219 00157 WP 2002 2 19 GTIA012187 1 20011204 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP COCKPIT DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - CO-PILOT FLOORBOARD DAMAGED AT UPPER FACE. PUNCTURE AT STATION Y=150. REMOVED DAMAGED AREA. FABRICATED DOUBLER. INSTALLED REPAIR DOUBLER PER DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002021900158 20020219 00158 WP 2002 2 19 GTIA012189 1 20011112 A 5313 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND LONGERON 17L CRACKED AT FUSELAGE FRAME STATION Y=980. REMOVED DAMAGED AREA OF LONGERON. FABRICATED NEW LON GERON SECTION AND SPLICE. INSTALLED LONGERON SECTION AND SPLICE PER DC9 SRM 53-02. (M) 2 L 7 2 4F A6WE 2002021900159 20020219 00159 WP 2002 2 19 GTIA012190 1 20011112 A 5310 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND FUSELAGE FRAME STATION Y-980 CRACKED AT LONGERON 16L. AFTER FURTHER EVALUATION FOUND THE FRAME SHEAR TIE TO BE ONE WITH CRACKS. REMOVED DAMAGED SHEAR TIE AT STATION 980. FABRICATED NEW SHEAR TIE IAW DC9 SRM 51-10-2. INSTALLE D NEW SHEAR TIE IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002021900160 20020219 00160 WP 2002 2 19 GTIA012191 1 20011207 A 5711 SPLICE DOUG DC9 DC932 3022066 WP LT WING SPAR CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND LEFT WING LEADING EDGE UPPER FRONT SPAR PREVIOUS REPAIR HAS CORROSION FROM XFS 550-XFS 77. REMOVED CORROSIO N. SPLICE PLATE FOUND TO BE OUT OF LIMITS. FABRICATED SPLICE PLATE. INSTALLED SPLICE PLATE IAW MD80 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 2002021900161 20020219 00161 WP 2002 2 19 GTIA012192 1 20011122 A 5320 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CUSP WEB CORRODED AT STATION Y=200 X=56. CORROSION WAS FOUND DURING OPEN UP FOR WEB REPAIR AT FRAME STATION -200, X=57. REMOVED CORROSION. REMOVED SECTION OF CUSP. WEB DAMAGED. FABRICATED AND LOCATED CUSPS WEB. INSTALLED I AW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002021900162 20020219 00162 WP 2002 2 19 GTIA012193 1 20011107 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND FORWARD GALLEY FLOOR WHEN WALKING ON SOUNDS AND FEELS LIKE SOMETHING LOOSE OR MISSING. REMOVED FLOOR. FORM NEW PANEL AND HATS. INSTALLED FLOOR PANEL IAW DC9 SRM 51-30-1. (M) 2 L 7 2 4F A6WE 2002021900163 20020219 00163 WP 2002 2 19 GTIA012194 1 20011112 A 5310 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND FUSELAGE FRAME AT STATION Y 980 CRACKED AT LONGERON 16R. AFTER FURTHER EVALUATION. FOUND THE FRAME SHEAR T IE TO BE THE ONE WITH CRACKS TWO EACH BETWEEN LONGERON 16R-17R. REMOVED DAMAGE SHEAR TIE AT STATION 980. FABRICATED NE W SHEAR TIE IAW DC9 SRM 51-10-2. (M) 2 L 7 2 4F A6WE 2002021900164 20020219 00164 WP 2002 2 19 GTIA012195 1 20011108 A 5312 BULKHEAD DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - AFT PRESSURE BULKHEAD WEB CRACKED IN AREA BETWEEN 2 FASTENERS AND UNDER FINGER DOUBLER. CRACK IS LOCATED RIGHT SI DE OF VERTICAL DOOR NEXT TO THE CONTROL CABLE FAIRED BOX. REMOVED CRACK. FABRICATED FILLER, FINGER DOUBLER, AND DOUBLE R INSTALLED REPAIR IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002021900165 20020219 00165 WP 2002 2 19 GTIA012196 1 20011125 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND ENTRY AREA, FLOOR SUPPORT CORRODED FROM STATION Y=160 TO STA Y=200. REMOVED FLOOR SUPPORT STA 160-200. LOC ATED AND DRILLED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002021900166 20020219 00166 WP 2002 2 19 GTIA012197 1 20011123 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT STATION Y200 FROM X2 INCHES TO -X21. REMOVED FLOOR SUPPORT. FABRIC ATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002021900167 20020219 00167 WP 2002 2 19 GTIA012198 1 20011116 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND RIGHT INBOARD FLOORBOARD STATION 237-313 GOUGED, HOLES ELONGATED, SURFACE CORROSION. FABRICATED DOUBLER. I NSTALLED DOUBLER IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002021900168 20020219 00168 WP 2002 2 19 GTIA012199 1 20011115 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CABIN FLOORBOARD, LEFT, OUTBOARD STATION 237 TO 313 STIFFENER DETACHED FROM BACKSIDE SKIN, CRACK AT FORWARD END EDGE, SEVERE CORROSION ON SKIN. REATTACHED STIFFENER. FABRICATED DOUBLER. INSTALLED DOUBLER IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002021900169 20020219 00169 WP 2002 2 19 GTIA012200 1 20011115 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CABIN FLOORBOARD RIGHT, INBOARD STATION 237 TO 313, TWO CRACKS AT FORWARD OUTER EDGE, SURFACE CORROSION AND BARE METAL AREAS ON SKIN. STOPPED DRILL CRACKS, LOCATED AND DRILLED. INSTALLED TWO DOUBLERS IAW DC9 SRM 53-05. (M) 2 L 7 2 4F A6WE 2002021900170 20020219 00170 WP 2002 2 19 GTIA012201 1 20011115 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CABIN FLOORBOARD LEFT, INBOARD STATION 465 TO 525, LOWER SIDE STIFFENERS CRACKED, INBOARD, OUTBOARD AND ONE IN CENTER SKIN HAS SURFACE CORROSION AND BARE METAL. REMOVED HAT CHANNELS. FABRICATE 4 HAT CHANNELS. INSTALLED HAT CH ANNELS AND INSULATION BLANKETS IAW DC9 SRM 53-05-0. (M) 2 L 7 2 4F A6WE 2002021900171 20020219 00171 WP 2002 2 19 GTIA012202 1 20011115 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CABIN FLOORBOARD RIGHT INBOARD STATION 465-579, FORWARD AND AFT END RIVETS PULLING THROUGH STIFFENERS, SEVER AL CRACKS AT AFT END FASTENER HOLES, SURFACE CORROSION AND BARE METAL AREAS ON SKIN. FABRICATED DOUBLERS. INSTALLED DO UBLERS IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002021900172 20020219 00172 WP 2002 2 19 GTIA012203 1 20011115 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CABIN FLOORBOARD LEFT CENTER STATION 889-956. SEVERE CORROSION AFT END, CRACKED WITH AREAS OF MISSING METAL AND ELONGATED MOUNT HOLES. FABRICATED NEW FLOORBOARD. INSTALLED FLOORBOARD STATION 889-956 IAW DC9 SRM 51-30-1. (M) 2 L 7 2 4F A6WE 2002021900173 20020219 00173 WP 2002 2 19 GTIA012204 1 20011114 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CABIN FLOOR PANEL LEFT MID STATION 237 TO 313 CORROSION. REMOVED DAMAGE 3 AREAS. FABRICATED DOUBLERS TWO E ACH. INSTALLED TWO DOUBLERS IAW MD80 SRM 53-05. (M) 2 L 7 2 4F A6WE 2002021900174 20020219 00174 WP 2002 2 19 GTIA012205 1 20011113 A 5320 CHANNEL DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND AFT LOWER CARGO COMPARTMENT CORRODED X17 CHANNEL FROM STATION 937 TO 889. REMOVED DAMAGE SECTION FROM STATI ON 889 TO 937, LOCATE AND DRILL. INSTALLED CHANNEL IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002022000030 20020220 00030 NE 2002 2 20 01FDEA00911 2 20011024 A 7530 SCREEN BOEING 727 727227 1384078 NM PWA JT8 JT8D15 52051 NE BLEED CONTROL DIRTY A FDEA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 25 495FE 21669 ON T/O LOUD BANG OCCURRED. PACKS TRIPPED. TROUBLESHOT NO DEFECTS NOTED. CLEANED PRBC SCREENS. 2 L 7 3 4F 4 F A3WE E2EA 2002022000031 20020220 00031 WP 2002 2 20 01FDEA01114 1 20011012 A 3260 806125 PROXIMITY SWITCH DOUG DC10 DC1030 3023501 WP LANDING GEAR FAULTY A FDEA O OTHER J WARNING INDICATION LD LANDING 1 SO 25 307FE 48291 AFTER LANDING GEAR HANDLE LOWERED HAD NORM GEAR EXT NOISES. REMOVED AND REPLACED PROX SWITCH ELECTRONIC UNIT PER MM 32- 61-01-2. 2 L 7 3 4F A22WE 2002022000032 20020220 00032 NM 2002 2 20 01FDEA01115 1 20011004 A 5313 STRINGER BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 281FE 22348 CORROSION (C53-111-01(2)) EMANATING FROM BETWEEN STRINGER AND SKIN BS 696, STR 28 RT. REMOVED AND REPLACED STR PER SRM 53-10-3 FIG 1. 2 L 7 3 4F RT A3WE 2002022000033 20020220 00033 NM 2002 2 20 01FDEA01116 1 20011004 A 3260 WARNING LIGHT BOEING 727 727200 138407E NM LT MLG ILLUMINATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 494FE 21532 AFTER T/O, MAIN GEAR DOOR LIGHT ILLUM. INSPECTED AND CYCLED LT GEAR DOOR CHECK OK. DEFER PER MEL 32-01. 2 L 7 3 4F RT A3WE 2002022000072 20020220 00072 NM 2002 2 20 01FDEA01117 1 20011002 A 3610 GASKET BOEING 727 727200 138407E NM LT WING LEAKING A FDEA K NONE J WARNING INDICATION CL CLIMB 1 SO 25 478FE 21395 NR 3 ENGINE STRUT O/H LIGHT ILLUM. REMOVED AND REPLACED LEAKING GASKET PER MP. LEAK AND OPS CHECK NORMAL. 2 L 7 3 4F RT A3WE 2002022000074 20020220 00074 NM 2002 2 20 01FDEA01119 1 20010717 A 5531 SPAR BOEING 727 727247 138408F NM VERTICAL STAB CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CHAFE AT VERT STAB L/E RIGHT FRONT SPAR FIN BS 55.8 TO 47.0 O/B SIDE. REMOVED AND REPLACED STAB PER IAW EA 7-5530-58486 . 2 L 7 3 4F A3WE 2002022000075 20020220 00075 NM 2002 2 20 01FDEA01120 1 20010626 A 5310 65163391 SHEAR TIE BOEING 727 727277 138408S NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 CORROSION (C53-113-01(2)) ON SHEAR TIE BS 970, LBL 10, WL 138.5. *S/D* REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-4 FIG 15. 2 L 7 3 4F RT A3WE 2002022000125 20020220 00125 WP 2002 2 20 GTIA012206 1 20011112 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - E/E BAY INTERCOSTAL ABOVE 28L STRINGER HAS CORRODED. FABRICATED NEW INTERCOSTAL AND HEAT TREATED. INSTALLED INTE RCOSTAL IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002022000126 20020220 00126 WP 2002 2 20 GTIA012207 1 20011108 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CORROSION NICKS AND GOUGES AT SEAT TRACK -X22 FROM STATION Y648 TO STA Y766. REMOVED SEAT TRACK FROM STA 64 8-766. DRILLED AND LOCATE SEAT TRACK FROM STATION 648-766 AND SPLICE. INSTALLED SEAT TRACK PER SRM DC9 51-30-1. (M) 2 L 7 2 4F A6WE 2002022000127 20020220 00127 WP 2002 2 20 GTIA012208 1 20011108 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CORROSION, NICKS AND GOUGES AT SEAT TRACK -X22 FROM STA Y532 TO STA 648. REMOVED SEAT TRACK FROM STATION 53 2-648. FABRICATED DRILLED AND LOCATED NEW SECTION FROM 532-648. INSTALLED NEW SEAT TRACK FROM 532-648. (M) 2 L 7 2 4F A6WE 2002022000128 20020220 00128 WP 2002 2 20 GTIA012209 1 20011108 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 12536 FTW - FOUND CORROSION NICKS AND GOUGES AT SEAT TRACK -22 INCHES FROM STA 342-440. REMOVED DAMAGED SEAT TRACK FROM STA 3 42-437. LOCATE AND DRILL SEAT TRACK. INSTALLED SEAT TRACK AND SPLICES 342-437 IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002022000129 20020220 00129 WP 2002 2 20 GTIA012210 1 20011108 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CORROSION, NICKS AND GOUGES AT SEAT TRACK -X44 INCHES FROM STATION 766-964. REMOVED SEAT TRACK FROM STA 766 -860. FABRICATED DRILLED AND LOCATED NEW SEAT TRACK. INSTALLED SEAT TRACK FROM 766-860. REMOVED SEAT TRACK DAMAGE FRO M STATION 860-964. FABRICATED DRILLED AND LOCATED NEW SEAT TRACK FROM STA 860-964. INSTALLED SEAT TRACK FROM STA 860-9 64 PER SRM DC9 53-05. (M) 2 L 7 2 4F A6WE 2002022000130 20020220 00130 WP 2002 2 20 GTIA012211 1 20011108 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CORROSION NICKS GOUGES AT SEAT TRACK -X44 INCHES FROM STATION 648-766. REMOVED SEAT TRACK. LOCATE AND DRIL L FROM 648-766. INSTALLED NEW SEAT TRACK AT STATION 648-766 RIGHT SIDE IAW DC9 SRM 53-05. (M) 2 L 7 2 4F A6WE 2002022000131 20020220 00131 WP 2002 2 20 GTIA012212 1 20011108 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FOUND CORROSION NICK AND GOUGES AT SEAT TRACK -44 INCH FROM STA Y 532-648. REMOVED SEAT TRACK FROM STATION 532-648. FA BRICATED, DRILLED AND LOCATED NEW SEAT TRACK. INSTALLED SEAT TRACK. (M) 2 L 7 2 4F A6WE 2002022000132 20020220 00132 WP 2002 2 20 GTIA012213 1 20011108 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CORROSION NICK AND GOUGES AT SEAT TRACK -X44 INCHES FROM STA 440-532. REMOVED SEAT TRACK FROM STATION 440-5 32. FABRICATED DRILLED AND LOCATED NEW SEAT TRACK. INSTALLED NEW SEAT TRACK AT STA 440-532. (M) 2 L 7 2 4F A6WE 2002022000133 20020220 00133 WP 2002 2 20 GTIA012214 1 20011108 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CORROSION NICKS AND GOUGES AT SEAT TRACK -X44 INCH FROM STATION 342-440. REMOVED SEAT TRACK FROM STA 342-44 0. DRILLED AND LOCATED SEAT TRACK STATION 342-440. INSTALLED SEAT TRACK 342-440 -X44 IAW DC9 SRM 53-05. (M) 2 L 7 2 4F A6WE 2002022000134 20020220 00134 WP 2002 2 20 GTIA012215 1 20011108 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CORROSION, NICKS AND GOUGES AT SEAT TRACK X44 INCH FROM STATION 200-342. REMOVED SEAT TRACK FROM STATION 20 0-285. DRILLED AND LOCATED NEW SEAT TRACK IAW DC9 SRM 51-10-4 AND 53-05. INSTALLED NEW SEAT TRACK FROM STATION 200-285 . REMOVED SEAT TRACK FROM STATION 285-342. LOCATED AND DRILLED NEW SEAT TRACK. INSTALLED NEW SEAT TRACK AT STATION 26 5-342 RT IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002022000135 20020220 00135 WP 2002 2 20 GTIA012216 1 20011112 A 5313 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FOUND LONGERON 13R CRACKED AT FUSELAGE FRAME STA Y-965. REMOVED DAMAGED SECTION OF STRINGER. FORMED LONGERON AND SPLIC E. INSTALLED LONGERON REPAIR IAW DC9 SRM 53-02. (M) 2 L 7 2 4F A6WE 2002022000136 20020220 00136 WP 2002 2 20 GTIA012217 1 20011106 A 5542 SKIN DOUG DC9 DC932 3022066 WP RUDDER CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND RUDDER RIGHT LOWER SKIN CRACKED AT FASTENER ON RIB LOCATION NR 12. REMOVED DAMAGE. FABRICATED FILLER AND D OUBLER. INSTALLED REPAIR IAW DC9 SRM 55-03. (M) 2 L 7 2 4F A6WE 2002022000143 20020220 00143 NM 2002 2 20 DL72S020052 1 20011226 A 2780 651622172 SLAT BOEING 727 727225A 1384077 NM # 5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8873Z 21291 REPAIRED 1.5 INCH CRACK IN #5 L/E SLAT I/B RIB AT ACTUATOR ROD END PER M/M 57-54-000-8 PER ERA 382382-14 REV ORG 2 L 7 3 4F RT A3WE 2002022000158 20020220 00158 NM 2002 2 20 DLM88020180 1 20010213 A 5300 5912494501N PAN DOUG MD88 MD88 3023688 NM C-1 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 984DL 53311 C-1 DOORWAY THRESHOLD JAMB PAN CORRODED BEYOND LIMITS. REPAIRED PER MD-80 DRD 53-05-D FIG 804D. 2 L 7 2 4F RT A6WE 2002022000165 20020220 00165 WP 2002 2 20 GTIA012219 1 20011113 A 5210 SKIN DOUG DC9 DC932 3022066 WP L1 DOOR DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - PREVIOUS REPAIR AT UPPER EDGE OF L1 DOOR NEEDS REPLACED, INADEQUATE REPAIR DOUBLER MATERIAL. REMOVED OLD REPAIR A ND DAMAGED SKIN. INSTALLED FLUSH PATCH REPAIR ON L1 DOOR IAW DC9 SRM 53-05. (M) 2 L 7 2 4F A6WE 2002022000166 20020220 00166 WP 2002 2 20 GTIA012220 1 20011113 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - WHEN L-1 DOOR IS FULLY OPEN, HOLD OPEN HOOK IS NOT ALIGNED WITH FITTING IN FUSELAGE, HOOK IS CHAFING AT BOTTOM OF OPENING. FOUND CRACK AT 12:00 POSITION. LOCATED AND DRILLING EXTERNAL DOUBLER AND INTERNAL DOUBLERS, TWO. INSTALLED C OMPLETE IAW SRM DC9 53-04. (M) 2 L 7 2 4F A6WE 2002022000169 20020220 00169 WP 2002 2 20 GTIA012221 1 20011123 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - ANGLE SUPPORT CORRODED AT STATION Y916. FABRICATE NEW ANGLE SUPPORT. INSTALLED NEW ANGLE SUPPORT IAW DC9 SRM 51- 30-1. (M) 2 L 7 2 4F A6WE 2002022000170 20020220 00170 WP 2002 2 20 GTIA012222 1 20011125 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT STA Y=200 FROM X-24 INCH TO X-43 INCH. FABRICATED NEW FLOOR SUPPORT . INSTALLED FLOOR SUPPORT PER DC9 SRM 51-10-4. (M) 2 L 7 2 4F A6WE 2002022000171 20020220 00171 WP 2002 2 20 GTIA012223 1 20011125 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FORWARD ENTRY FLOOR SUPPORT CORRODED FROM STA Y=162 TO Y=198. FABRICATED FLOOR SUPPORT. INSTALLED REPLACEMENT FL OOR SUPPORT IAW DC9 SRM 51-10-4 AND 51-30-1. (M) 2 L 7 2 4F A6WE 2002022000172 20020220 00172 WP 2002 2 20 GTIA012224 1 20011116 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FOUND LEFT OUTBOARD FLOORBOARD STATION 894-974 HAS SURFACE CORROSION. REMOVED HAT CHANNEL TO FABRICATED PANEL. FABRICA TED NEW FLOOR PANEL. INSTALLED HAT CHANNELS PER SRM DC9 51-30-2. (M) 2 L 7 2 4F A6WE 2002022000173 20020220 00173 WP 2002 2 20 GTIA012225 1 20011116 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND LEFT OUTBOARD FLOORBOARD STATION 756-832 CORNERS ARE BROKEN OFF. FABRICATED REPAIR DOUBLERS. INSTALLED DOU BLERS IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002022000174 20020220 00174 WP 2002 2 20 GTIA012226 1 20011116 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND RIGHT FLOORBOARD STATION 465 CRACKED AT FASTENER HOLES. FORM DOUBLER FOR FLOOR PANEL. INSTALLED DOUBLER PE R DC9 SRM 53-04. (M) 2 L 7 2 4F A6WE 2002022000175 20020220 00175 WP 2002 2 20 GTIA012227 1 20011116 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND LEFT MID FLOORBOARD STATION 200-237 HAS OVERSIZE FASTENER HOLES. REMOVED HAT SECTIONS. FABRICATED LOCATED AND DRILLED FLOORBOARD SKIN. INSTALLED HAT SECTIONS IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002022000176 20020220 00176 WP 2002 2 20 GTIA012228 1 20011110 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FORWARD CARGO COMPARTMENT ANGLE SUPPORT AT STATION Y275 BETWEEN LONGERON 27R AND 26R HAS A CRACK. REMOVED CRACK O N STEEL FLOOR SUPPORT. FORMED REPAIR PARTS AND INSTALLED REPAIR PARTS PER DC9 SRM 53-03. (M) 2 L 7 2 4F A6WE 2002022000177 20020220 00177 WP 2002 2 20 GTIA012229 1 20011107 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND RIGHT INBOARD FLOORBOARD NR 2 FROM STATION 237-313, PREVIOUS REPAIR AT CORNER PEELING OFF HAS CORROSION AND GOUGES. FABRICATED REPAIR DOUBLERS AND FILLER. INSTALLED DOUBLER AND FILLER IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002022000178 20020220 00178 WP 2002 2 20 GTIA012230 1 20011107 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - RIGHT INBOARD FLOORBOARD NR 5 FROM STATION 579-617 HAS EDGES BROKEN, ELONGATED HOLES AND INSULATION TORN. FORMED NEW PNL IAW DC9 SRM 53-24-0. (M) 2 L 7 2 4F A6WE 2002022000179 20020220 00179 WP 2002 2 20 GTIA012231 1 20011112 A 5313 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FOUND LONGERON 16R CRACKED AT FUSELAGE FRAME STATION 965. REMOVED LONGERON 16R CRACKED FROM STATION 955-975. DRILLED A ND LOCATED LONGERON AND SPLICE. INSTALLED LONGERON REPAIR AND SPLICES (TWO EACH) IAW DC9 SRM 53-02. (M) 2 L 7 2 4F A6WE 2002022000180 20020220 00180 WP 2002 2 20 GTIA012232 1 20011113 A 5414 PANEL DOUG DC9 DC932 3022066 WP NR 1 PYLON CHAFED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 NR 1 ENGINE PYLON L/E PANEL CHAFFING INTO FUSELAGE. FORMED REPAIR DOUBLER. INSTALLED DOUBLER IAW SRM DC9 51-30-2. (M) 2 L 7 2 4F A6WE 2002022000181 20020220 00181 WP 2002 2 20 GTIA012233 1 20011112 A 5313 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND LONGERON 17R CRACKED AT FS 965. REMOVED CRACKED LONGERON. FORMED LONGERON AND SPLICE. INSTALLED REPAIR LO NGERON AND SPLICE (TWO EACH) IAW DC9 SRM 53-02. (M) 2 L 7 2 4F A6WE 2002022000182 20020220 00182 WP 2002 2 20 GTIA012234 1 20011108 A 5753 FLAP DOUG DC9 DC932 3022066 WP LT WING DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND LEFT WING TRAILING EDGE FLAP DAMAGED NEXT TO INBOARD HINGE. REMOVED TRAILING EDGE WEDGE. LOCATE AND DRILLI NG TRAILING EDGE. INSTALLED TRAILING EDGE IAW DC9 SRM 51-30-8. (M) 2 L 7 2 4F A6WE 2002022000183 20020220 00183 WP 2002 2 20 GTIA012235 1 20011108 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FOUND FRAME FOR FLOOR SUPPORT FS 218 LONGERON 30 TO L29 HAS EXFOLIATION CORROSION IN E BAY. REMOVED FLOOR SUPPORT. INS TALLED NEW FLOOR SUPPORT IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002022000184 20020220 00184 WP 2002 2 20 GTIA012236 1 20011127 A 5320 SUPPORT BRACKET DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND SUPPORT BRACKET CRACKED AT LEFT TRAPEZOIDAL PANEL STRUCTURE STA Y 729 X=59.500 Z=13.100. REMOVED BRACKET. INSTALLED NEW FILLER IAW DC9 SRM 51-30-1. (M) 2 L 7 2 4F A6WE 2002022000185 20020220 00185 WP 2002 2 20 GTIA012237 1 20011107 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - DENT LEFT FUSELAGE STATION 207, JUST ABOVE CUSP. FABRICATE DOUBLER REPAIR. INSTALLED NEW DOUBLER REPAIR IAW DC9 SRM 53-04. (M) 2 L 7 2 4F A6WE 2002022000186 20020220 00186 WP 2002 2 20 GTIA012238 1 20011107 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP FUSELAGE DETERIORATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND FORWARD GALLEY FLOOR LOOSE AND DETERIORATED. FORMED NEW PANEL, FORMED HAT SECTION. INSTALLED FLOOR PANEL I AW DC9 SRM 51-30-1. (M) 2 L 7 2 4F A6WE 2002022000187 20020220 00187 WP 2002 2 20 GTIA012239 1 20011112 A 5320 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND WEB CORRODED AT STA Y 200 X57 INCHES UNDER FLOOR LINE AFT OF FORWARD AIRSTAIRS CUT OUT. CUT DAMAGE AREA. F ABRICATE FILLER AND DOUBLER. AFTER FURTHER EVALUATION. FOUND SUB FLOOR 2ND FLOOR SUPPORT ON STRAP 6/7 CORRODED OUT OF LIMITS. FABRICATED 2ND DRILLED SUB FLOOR. INSTALLED DOUBLER, FILLER AND ANGLE. FABRICATED FLOOR SUPPORT IAW DC9 SRM 5 1-10-2. INSTALLED SUB FLOOR. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002022000188 20020220 00188 WP 2002 2 20 GTIA012240 1 20011112 A 5313 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND LONGERON 16L CRACKED AT FUSELAGE FRAME STATION Y 965. REMOVED CRACKED LONGERON. FORMED LONGERON AND SPLICE . INSTALLED REPAIR IAW DC9 SRM 53-02. (M) 2 L 7 2 4F A6WE 2001092100100 20010921 00100 NM 2001 9 21 CA010906014 1 20010810 A 5753 113T17102SP FAIRING BOEING 767 767233 1385113 NM PWA JT9 JT9D7R4D 52054 NE RT TE FLAP DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ON ARRIVAL FOUND RT INBOARD LEADING FLAP HINGE FAIRING DAMAGED. DAMAGE APPEARED TO BE FROM MISSING MID SPAR FUSE P IN ACCESS PANEL LT SIDE OF RT ENGINE PYLON. LEADING EDGE FLAP HINGE FAIRING AND MID SPAR ACCESS PANEL REPLACED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001100200054 20011002 00054 NM 2001 10 2 CA010924003 1 20010823 A 5712 114T220221 RIB BOEING 767 767375 1385217 NM GE CF6 CF680C2B6 30025 NE LT WING CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) LT AND RT WING RIB WEB, INBOARD OF SLAT ANTI-ICE TELESCOPING DUCT CRACKED/BROKEN AT TOP SURFACE. 4 - 6 INCH CRACK FOUND IN RADIUS OF L/H AND RT NOSE FORMER ON WING FIXED LEADING EDGE COMMON TO NR 5 AND 8 LEADING EDGE SLAT. 2 L 7 2 4F 4 F RT A1NM E13NE 2002022100009 20020221 00009 NM 2002 2 21 USAA011379 1 20011210 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 609AU 55489 22205 CLT - FOUND SKIN DENTED 2 INCHES BY 2 INCHES, BS 1607, BETWEEN S19L AND S20L. INTERIM REPAIR PER EA 67616A. (M) 2 L 7 2 4F RT A2NM 2002022100010 20020221 00010 NM 2002 2 21 USAA011380 1 20011210 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 609AU 55489 22205 CLT - FOUND FUSELAGE SKIN DENTED 2 INCHES BY 2 INCHES, AFT LEFT SERVICE DOOR BS 1621, AT S20L-S21L. EXTERNAL SKIN DOUBL ER REPAIR EA 85721. (M) 2 L 7 2 4F RT A2NM 2002022100011 20020221 00011 NM 2002 2 21 USAA011381 1 20011210 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 609AU 55489 22205 CLT - FOUND FUSELAGE SKIN DENTED 3 INCHES BY 3.5 INCHES, AFT FUSELAGE EXT SKIN BS 1740 AT S29L. EXTERNAL DOUBLER REPAIR PER SRM 53-000-01 AND EA NR 85731. (M) 2 L 7 2 4F RT A2NM 2002022100012 20020221 00012 NM 2002 2 21 USAA011382 1 20011210 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 609AU 55489 22205 CLT - FOUND FUSELAGE SKIN DENTED 3 INCHES BY 3 INCHES, BS 1510, AT S29L TO S29R. INSTALLED EXTERNAL DOUBLER PER EA 8572 9. (M) 2 L 7 2 4F RT A2NM 2002022100013 20020221 00013 NM 2002 2 21 USAA011383 1 20011214 A 5412 BULKHEAD BOEING 757 757225 1384959 NM NR 1 PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 609AU 22205 CLT - FOUND PYLON MID BULKHEAD .5 INCH, NR 1 PYLON, MID BULKHEAD LOWER BOLT HOLE OUTBOARD. INSTALLED DOUBLER REPAIR PER EA NR 85691 AND 85692. (M) 2 L 7 2 4F RT A2NM 2002022100014 20020221 00014 NM 2002 2 21 USAA011384 1 20011214 A 5313 STRINGER BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 609AU 55489 22205 CLT - FOUND STRINGER 28R, 1 INCH BY .25 INCH CORROSION, AFT CARGO COMP, BELOW FLOOR AT BS 1400, S28. INSTALLED STRINGER SEGMENT REPAIR PER EA 85681. (M) 2 L 7 2 4F RT A2NM 2002022100015 20020221 00015 NM 2002 2 21 USAA011385 1 20011214 A 5310 LATCH BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 613AU 30755 27144 CLT - FOUND DOOR LATCH BRACKET CORRODED 3 INCHES BY 3 INCHES, BS 600, FORWARD CARGO DOOR SILL. REPLACED PER SRM 51-10-0 0. (M) 2 L 7 2 4F RT A2NM 2002022100016 20020221 00016 NM 2002 2 21 USAA011386 1 20011214 A 5320 ATTACH ANGLE BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 609AU 22205 CLT - FOUND FRAME ATTACHED ANGLE CORRODED, 2 INCH BY 6 INCH, BS 1300, RBL 7 TO RBL 13. REPLACED PART PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 2002022100017 20020221 00017 NM 2002 2 21 USAA011399 1 20011206 A 5330 SKIN BOEING 757 7572B7 1384964 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 613AU 30754 27144 CLT - FOUND SKIN WITH 1 INCH HOLE, BS 1695, STRINGER S20R. REPAIRED PER SRM 53-00-01 FIG 208. (M) 2 L 7 2 4F RT A2NM 2002022100018 20020221 00018 NM 2002 2 21 USAA011400 1 20011215 A 5330 SKIN BOEING 757 7572B7 1384964 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 613AU 27144 CLT - FOUND SKIN DENTED 20 INCHES, STATION 460 AND STATION 480 STRINGER 5 AND 6L. REPAIRED PER SRM 53-00-01 FIG 206. ( M) 2 L 7 2 4F RT A2NM 2002022100019 20020221 00019 NM 2002 2 21 USAA011401 1 20011213 A 5330 SKIN BOEING 757 7572B7 1384964 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 617AU 27148 CLT - FOUND SKIN REPAIRED 7 INCHES BY 8 INCHES, STATION 600 S16L. REPAIRED PER EA 66755A. (M) 2 L 7 2 4F RT A2NM 2002022100020 20020221 00020 NM 2002 2 21 USAA011402 1 20011215 A 5311 FRAME BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 617AU 55127 27148 CLT - FOUND CHORD ANGLE CORRODED 1 INCH, FORWARD FACE OF FRAME STATION 263 RBL 10. REPLACED CHORD ANGLE. (M) 2 L 7 2 4F RT A2NM 2002022100021 20020221 00021 NM 2002 2 21 USAA011410 1 20011206 A 5330 SKIN BOEING 757 7572B7 1384964 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 613AU 30754 27144 CLT - FOUND SKIN DENTED WITH A 1 INCH CREASE, STATION 331, S22R. REPAIRED PER EA 85791. (M) 2 L 7 2 4F RT A2NM 2002022100022 20020221 00022 NM 2002 2 21 USAABB01141 1 20011214 A 2120 ODOR BOEING 757 7572B7 1384964 NM CABIN DETECTED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 626AU 27303 CLT - BAD ODOR EMANATING FROM THE AIR CONDITIONING SYSTEM. MAINTENANCE RAN THE PACKS WITH BOTH THE APU AND ENGINES AND COULD NOT DUPLICATE THE SMELL. THE MM OIL CONTAMINATION PROCEDURES WAS PERFORMED. BOTH RECIRC FILTERS AND ALL GALLEY V ENT FILTERS WERE REPLACED. (M) 2 L 7 2 4F RT A2NM 2002022100027 20020221 00027 NM 2002 2 21 USAABB02006 1 20010112 A 3610 312N53061 DUCT BOEING 757 7572B7 1384964 NM LT ENGINE LEAKING A USAA O OTHER J WARNING INDICATION DE DESCENT 1 EA 19 620AU 27199 CLT - FLT 1166 - ON DESCENT INTO CLT, CREW RECEIVED THE EICAS MESSAGE 'L ENGINE OVERHEAT' AND THE 'OVERHEAT' LIGHT. THE LIGHT EXTINGUISHED WHEN THE THROTTLE WAS RETARDED. FLIGHT CONTINUED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINT ENANCE REPLACED LEAKING HPS AND HP6 SERVICE OFFTAKE DUCTS. (M) 2 L 7 2 4F RT A2NM 2002022100029 20020221 00029 NM 2002 2 21 USAABB02007 1 20010112 A 3610 312N53217 DUCT BOEING 757 7572B7 1384964 NM LT ENGINE LEAKING A USAA O OTHER J WARNING INDICATION DE DESCENT 1 EA 19 620AU 27199 CLT - FLT 1166 - ON DESCENT INTO CLT, CREW RECEIVED THE EICAS MESSAGE 'L ENGINE OVERHEAT' AND 'OVERHEAT' LIGHT. THE LIG HT EXTINGUISHED WHEN THE THROTTLE WAS RETARDED. FLIGHT CONTINUED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENAN CE REPLACED LEAKING HP2 AND HP6 SERVICE OFFTAKE DUCTS. (M) 2 L 7 2 4F RT A2NM 2002022100030 20020221 00030 NM 2002 2 21 USAABB02008 1 20011222 A 3350 1640487 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 613AU 27144 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 9 AND 13, 26 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2002022100044 20020221 00044 NM 2002 2 21 1FDEA00798 1 20010831 A 2620 PLUG BOEING 727 72722C 138400F NM FIRE PROTECTION FAULTY A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 105FE 19194 01-298 MOD TYPE F NR 7-26-020 REV NO PS FIRE PROTECTION. COMPLIED WITH FLEET CAMPAIGN DIRECTIVE 7-26-020. REMOVED AND REPLACED PLUG FROM LINE AT COUPLING. 2 L 7 3 4F A3WE 2002022100065 20020221 00065 NM 2002 2 21 TSAA0253002 1 20011228 A 5330 6546595 SKIN BOEING 727 7272Q9 138448M NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 REPAIRED FUSELAGE SKIN CRACK, BELOW THE LAP JOINT, AT BS 727 S-15R. TRIMMED OUT CRACK DAMAGE, VERIFIED WITH HFEC. FABR ICATED AND INSTALLED REPAIR FILLERS AND DOUBLER IAW ECO 3257. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2002022100066 20020221 00066 NM 2002 2 21 TSAA0253003 1 20011215 A 5330 6546855501 SKIN BOEING 727 7272Q9 138448M NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 REPAIRED 2.25 INCH FUSELAGE SKIN CRACK AT BS 927 S-24R. TRIMMED OUT CRACK DAMAGE AND VERIFIED WITH HFEC, NO DEFECTS NOT ED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-1 FIG 1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2002022100067 20020221 00067 NM 2002 2 21 TSAA0253004 1 20011215 A 5330 6546795501 SKIN BOEING 727 7272Q9 138448M NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 REPAIRED 2 INCH SKIN CRACK AT BS 867 S-22R. TRIMMED OUT CRACK AND VERIFIED WITH HFEC, NO DEFECTS NOTED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-1 FIG 1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2002022100071 20020221 00071 NM 2002 2 21 TSAA0253010 1 20011205 A 5311 65C3372247 FRAME BOEING 737 737230 1384401 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 823AL 23154 REMOVED ALL FASTENERS COMMON TO BS 727 OUTER CHORD FROM S-27L UP TO S18L. CHORD CRACKED BETWEEN S23L AND S24L. AIRCRA FT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2002022100072 20020221 00072 NM 2002 2 21 TSAA0253011 1 20011215 A 5314 6548674 KEELBEAM BOEING 737 737230 1384401 NM FUSELAGE CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 823AL 23154 DISCOVERED CORROSION AT RIGHT KEEL BEAM LOWER CHORD LOWER SURFACE AT BS 727. REMOVED CORROSION PER SRM 51-10-6. VISUAL LY, INSPECTED THE AREA TO ENSURE NO CRACKS AND ALL CORROSION REMOVED. FABRICATED A FILLER, DOUBLER, AND TRIPLER AND INS TALLED. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2002022100073 20020221 00073 NM 2002 2 21 ASAA0110560 1 20010821 A 3350 CONNECTOR BOEING 737 7372X6C 1384552 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS IN THE MID CABIN INOPERATIVE DUE TO CANNON PLUG BEING DISCON NECTED. RECONNECTED CANNON PLUG, THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002022100074 20020221 00074 NM 2002 2 21 ASAA0110567 1 20010831 A 5313 65516983 STRINGER BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER 19L AT BS 907 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2002022100075 20020221 00075 NM 2002 2 21 ASAA0110570 1 20010831 A 5320 6546812185 FLOOR SUPPORT BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND FLOOR SUPPORT AT BS 997-1003, LBL 10 TO LBL 14 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2002022100076 20020221 00076 NM 2002 2 21 ASAA0110573 1 20010903 A 3350 655663312 LIGHT BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING SCHEDULED MAINTENANCE, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT A SSEMBLY, THEN LIGHT OPERATED NORMAL. (M) 2 L 7 2 4F A16WE 2002022200004 20020222 00004 EU 2002 2 22 SABA0110053 1 20011014 A 3210 622800200 SWITCH BAG JETSTM JETSTM3201 1500217 EU A SABA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 959AE 959 Aircraft 959 on flight 5222from Charlotte to Lexington; after takeoff the left main gear intransit light illuminated and would not go out. Pilot had cycled the gear up. Gear was cycled down and indicated safe. Aircraft returned to Charlotte and made a safe landing. No emergency was declared. Maintenance trouble shot the system, jacked aircraft, adjusted up-l imit switch and cycled the gear numerous times. Could not get the gear to malfunction. Aircraft was returned to srevice 2 L 7 2 4T RT A56EU 2002022200049 20020222 00049 NM 2002 2 22 ASAA0110590 1 20010915 A 5315 65671408 FLOORBEAM BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 616-724, BUTTOCK LINE 0 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2002022200051 20020222 00051 NM 2002 2 22 ASAA0110633 1 20011029 A 5260 60605001 MECHANISM BOEING 737 737290C 138448V NM AIRSTAIRS LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 ANC - CREW REPORTED AIRSTAIR MECHANISM DIFFICULT TO OPERATE. LUBRICATED MECHANISM, THEN OPS CHECKED GOOD. (M) 2 L 7 2 4F A16WE 2002022200059 20020222 00059 NM 2002 2 22 ASAA0110656 1 20011210 A 5310 656217314 SHEAR TIE BOEING 737 737298C 1384490 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND SHEAR TIE AT BS 520, STRINGER 4R-5R CRACKED. REPAIRED SHEAR TIE PER SRM. (M) 2 L 7 2 4F RT A16WE 2002022200060 20020222 00060 NM 2002 2 22 ASAA01400105 1 20010921 A 3397 8100022602 WIRE BOEING 737 7374Q8 138447Q NM CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 778AS 25110 SFO - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT EMERGENCY EXIT ROW, BROKEN WIRE. REPAIRED WI RES, OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2002022200061 20020222 00061 NM 2002 2 22 ASAA0140099 1 20010823 A 3350 8100022603 LIGHT BOEING 737 7374Q8 138447Q NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 765AS 25102 JNU - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE AT ROW 25. REPLACED EMERGENCY FLOOR TRACK LIG HTING. OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002022200062 20020222 00062 NM 2002 2 22 ASAA0140111 1 20011005 A 5610 6531914102 ROLLER BOEING 737 7374Q8 138447Q NM SLIDING WINDOW OUT OF POSITION A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 772AS 25105 SFO - DURING LINE CHECK, FOUND FIRST OFFICERS SLIDING WINDOW STUCK IN THE CLOSED POSITION. REMOVED WINDOW AND REINSTALL ED LOWER TRACK ROLLER, REINSTALLED WINDOW. OPERATIONS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2002022200063 20020222 00063 NM 2002 2 22 ASAA0140112 1 20011007 A 5610 6531914102 ROLLER BOEING 737 7374Q8 138447Q NM SLIDING WINDOW BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 764AS 25101 SFO - DURING LINE CHECK, FOUND FIRST OFFICERS SLIDING FORWARD WINDOW ROLLER BROKEN. REMOVED WINDOW AND REMOVED AND REPL ACED LOWER TRACK ROLLER, REINSTALLED WINDOW, OPERATIONS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2002022200064 20020222 00064 NM 2002 2 22 ASAA0140121 1 20011024 A 5320 69434961 SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 PAE - DURING C-CHECK, FOUND CORROSION OUT OF LIMITS AT AFT CARGO BAY AT BS 847-867, RBL 24, WL 160 SIDEWALL SUPPORT PLAT E. REMOVED AND REPLACED SIDEWALL SUPPORT PLATE PER SRM. (M) 2 L 7 2 4F RT A16WE 2002022200065 20020222 00065 NM 2002 2 22 ASAA0140122 1 20011024 A 5320 65C304243 SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 PAE - DURING C-CHECK, FOUND LOWER BULKHEAD SUPPORT ANGLE CORRODED OUT OF LIMITS AT BS 947, LBL 19, WL 178. REMOVED AND REPLACED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002022200066 20020222 00066 NM 2002 2 22 ASAA0140123 1 20011023 A 5320 652072629 WEB BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 PAE - DURING C-CHECK, FOUND CORROSION OUT OF LIMITS ON FORWARD CARGO DOOR SUB THRESHOLD WEB AT NUT PLATE HOLES AT STATIO N 441-492, RBL 25, WL 157. REMOVED AND REPLACED PER SRM. (M) 2 L 7 2 4F RT A16WE 2002022200067 20020222 00067 NM 2002 2 22 ASAA0140124 1 20011024 A 5320 65434562 STRAP BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 PAE - DURING C-CHECK, FOUND AFT CARGO BAY SUB THRESHOLD STRAP CORRODED OUT OF LIMITS AT BS 782-800, RBL 20, WL 149. REM OVED AND REPLACED PER SRM. (M) 2 L 7 2 4F RT A16WE 2002022200068 20020222 00068 NM 2002 2 22 ASAA0140125 1 20011024 A 5320 654795711 STRAP BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 PAE - DURING C-CHECK, FOUND SUB THRESHOLD TIE STRAP CORRODED OUT OF LIMITS AT BS 775-847, WL 150. REMOVED AND REPLACED PER SRM. (M) 2 L 7 2 4F RT A16WE 2002022200069 20020222 00069 NM 2002 2 22 ASAA0140126 1 20011024 A 5320 65479573 WEB BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 PAE - DURING C-CHECK, FOUND SUB THRESHOLD WEB CORRODED OUT OF LIMITS AT BS 794-847, RBL 21, WL 150. REMOVED AND REPLACE D PER SRM. (M) 2 L 7 2 4F RT A16WE 2002022200070 20020222 00070 NM 2002 2 22 ASAA0140129 1 20011029 A 5320 654769012 SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 PAE - DURING C-CHECK, FOUND AFT CARGO BAY RIGHT FLOOR TO SIDEWALL SUPPORT PLATE FROM BS 727-762, RBL 20 WL 150 IS CORROD ED. REMOVED AND REPLACED SIDE WALL PLATE IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002022200071 20020222 00071 NM 2002 2 22 ASAA0140130 1 20011029 A 5347 655384422 CARGO TRACK BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 PAE - DURING C-CHECK, FOUND AFT CARGO BAY RIGHT FLOOR TRACK BS 747 TO 947 RBL 14 WL 150 CORRODED. REMOVED AND REPLACED PER SRM. (M) 2 L 7 2 4F RT A16WE 2002022200072 20020222 00072 NM 2002 2 22 ASAA0140131 1 20011029 A 5320 65476902 SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 PAE - DURING C-CHECK, FOUND AFT CARGO BAY LEFT FLOOR SIDEWALL SUPPORT PLATE FROM BS 727-947 AND LBL 20, WL 150 CORRODED. REPLACED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002022200073 20020222 00073 NM 2002 2 22 ASAA0140132 1 20011029 A 5230 6547952205 SKIN BOEING 737 7374Q8 138447Q NM CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 PAE - DURING C-CHECK, FOUND AFT CARGO DOOR SKIN DENTED. REPLACES SKIN IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002022200074 20020222 00074 NM 2002 2 22 ASAA0140133 1 20011029 A 5210 500794595 WEB BOEING 737 7374Q8 138447Q NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 PAE - DURING C-CHECK, FOUND FORWARD ENTRY DOOR WEB GOUGED OUTBOARD OF AFT STOP FITTING. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2002022200075 20020222 00075 NM 2002 2 22 ASAA0140173 1 20011211 A 5311 654795978 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 PAE - DURING SI C-CHECK, FOUND AFT BAY FORWARD DOOR FRAME IS GOUGED AT BS 794, RBL 27 WL 156 AND RBL 31 AND WL 158. REP AIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2002022200076 20020222 00076 NM 2002 2 22 ASAA0140176 1 20011214 A 5230 65C36231 SKIN BOEING 737 737490 1384715 NM CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 768AS 27082 PAE - DURING C-CHECK, FOUND AFT CARGO DOOR HAS NUMEROUS DENTS OUT OF LIMITS. REMOVED AND REPLACED AFT CARGO DOOR SKIN I AW SRM. (M) 2 L 7 2 4F RT A16WE 2002022200077 20020222 00077 NM 2002 2 22 ASAA0140178 1 20011218 A 5320 654795947 STRAP BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 768AS 27082 PAE - DURING C-CHECK, FOUND CORROSION ON INTERNAL FRAME STRAP AT BS 794, RBL 23, WL 157 IN AFT CARGO BAY. REPAIRED IAW EA. (M) 2 L 7 2 4F RT A16WE 2002022200078 20020222 00078 NM 2002 2 22 ASAA0140179 1 20011218 A 5311 654795978 FRAME BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 768AS 27082 PAE - DURING C-CHECK, FOUND CORROSION ON FRAME AT BS 794, RBL 23, WL 154 AFT CARGO BAY. REPAIRED IAW EA. (M) 2 L 7 2 4F RT A16WE 2002022200079 20020222 00079 NM 2002 2 22 ASAA0140181 1 20011218 A 5320 65C312403 DOUBLER BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 768AS 27082 PAE - DURING C-CHECK, FOUND CORROSION ON INTERNAL FRAME DOUBLER AT BS 794, RBL 23, WL 155 IN AFT CARGO BAY. REPAIRED PE R EA. (M) 2 L 7 2 4F RT A16WE 2002022200080 20020222 00080 NM 2002 2 22 ASAA0140182 1 20011218 A 5241 6545871132 SKIN BOEING 737 737490 1384715 NM GALLEY DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 768AS 27082 PAE - DURING C-CHECK, FOUND CRACK ON FORWARD GALLEY DOOR LOWER HINGE CUT OUT. REPAIRED IAW EA. (M) 2 L 7 2 4F RT A16WE 2002022200081 20020222 00081 NM 2002 2 22 ASAA0140611 1 20011016 A 5330 6546881 SKIN BOEING 737 7372Q8C 138448S NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING C-CHECK, FOUND DENT ON EXTERNAL SKIN AT BS 1037.5 AND STRINGER 9L AND 21. REPAIRED SKIN IAW DOUBLER. (M) 2 L 7 2 4F A16WE 2002022200082 20020222 00082 NM 2002 2 22 ASAA0110574 1 20010904 A 5311 65622061 FRAME BOEING 737 737210C 1384459 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 400, STRINGER 21L CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2002022200083 20020222 00083 NM 2002 2 22 ASAA0110580 1 20010914 A 5313 6552928594 STRINGER BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER 21L AT BS 747-767 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2002022200084 20020222 00084 NM 2002 2 22 ASAA0110628 1 20011023 A 5210 507945155 LATCH BOEING 737 737290C 138448V NM L1 DOOR LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 ANC - DURING LINE CHECK, FOUND L1 DOOR HOLD OPEN LATCH INOPERATIVE. LUBRICATED LATCH OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A16WE 2002022200085 20020222 00085 NM 2002 2 22 ASAA0110630 1 20011026 A 5210 507945155 HANDLE BOEING 737 7372X6C 1384552 NM L1 DOOR LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 ANC - DURING LINE CHECK, FOUND EXTERIOR DOOR HANDLE ON L-1 DOOR STICKS, HARD TO OPEN. CLEANED OFF ICE FROM HANDLE AREA, CLEANED AND LUBED SHAFT, OPERATIONS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2002022200086 20020222 00086 NM 2002 2 22 ASAA0110632 1 20011028 A 5260 60605001 HANDLE BOEING 737 7372X6C 1384552 NM AIRSTAIRS LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 ANC - CREW REPORTED AIRSTAIR CONTROL HANDLE BINDING AND DIFFICULT TO OPERATE. LUBRICATED MECHANISM, THEN OPS CHECKED GO OD. (M) 2 L 7 2 4F RT A16WE 2002022200087 20020222 00087 NM 2002 2 22 ASAA0110649 1 20011205 A 5310 69402882 STOP FITTING BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND AFT GALLEY DOOR STOP P/D FITTINGS (P/N'S 69402882, 651823928) CORRODED. REMOVED A ND REPLACED AFT GALLEY DOORSTOP P/D FITTINGS PER SRM. (M) 2 L 7 2 4F RT A16WE 2002022200088 20020222 00088 NM 2002 2 22 ASAA0110650 1 20011205 A 5313 BAC1498151 STRINGER BOEING 737 737298C 1384490 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER 4L AT BS 727B CRACKED. REPAIRED STRINGER PER SRM. (M) 2 L 7 2 4F RT A16WE 2002022200090 20020222 00090 NM 2002 2 22 ASAA0170008 1 20010915 A 3350 FUSE BOEING 737 737790 13844CN NM CABIN BLOWN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 615AS 30344 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHT AT THE L1 DOOR, ADJACENT TO THE FORWARD FLIGHT ATTENDANT JUMPSE AT WAS FOUND TO BE INOPERATIVE. REPLACED FUSE AND THE LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 2002022200091 20020222 00091 NM 2002 2 22 ASAA0170009 1 20010922 A 3350 D71702030 FUSE BOEING 737 737790 13844CN NM CABIN BLOWN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 615AS 30344 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHT AT THE L1 DOOR, ADJACENT TO THE FORWARD FLIGHT ATTENDANT JUMPSE AT WAS FOUND TO BE INOPERATIVE. REPLACED FUSE AND THE LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 2002022200092 20020222 00092 WP 2002 2 22 ASAA01800270 1 20010920 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP COCKPIT DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 943AS 53018 SEA - DURING PREFLIGHT CHECK, COCKPIT OVERHEAD EMERGENCY LIGHTING WAS INOPERATIVE. REPLACED ASSOCIATED BATTERY POWER SU PPLY PACK AT B5-23. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002022200093 20020222 00093 WP 2002 2 22 ASAA0180257 1 20010829 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 934AS 49235 PDX - DURING A-CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE PORTABLE EMERGENCY LIGHT ASSEMBLY AND THE LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 2002022200094 20020222 00094 WP 2002 2 22 ASAA0180258 1 20010903 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 SEA - DURING LINE CHECK, EXTERIOR OVERWING EMERGENCY EXIT LIGHTS ON BOTH SIDES OF AIRCRAFT WERE DETERMINED TO BE INOPERA TIVE. REPLACED ASSOCIATED BATTERY PACK (POWER SUPPLY). LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002022200095 20020222 00095 WP 2002 2 22 ASAA0180261 1 20010911 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 ANC - DURING LINE CHECK, WITH SWITCH OFF, EMERGENCY TRACK LIGHTS AT ROWS 8 AND 9 TURNED ON WHEN EXTERNAL POWER WAS REMOV ED FROM THE AIRCRAFT. REPLACED ASSOCIATED BATTERY POWER SUPPLY PACK. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2002022200096 20020222 00096 WP 2002 2 22 ASAA0180263 1 20010910 A 2611 PU90431R3 SMOKE DETECTOR DOUG DC9 DC983 3022083 WP LAVATORY NOT SEATED A ASAA K NONE N FALSE WARNING CR CRUISE 1 NM 01 950AS 53023 SEA - DURING FLIGHT, AFT RIGHT LAVATORY SMOKE DETECTOR WENT OFF ALTHOUGH NO SMOKE WAS EVIDENT. RESEATED SMOKE DETECTOR, OPS CHECKED OK. (M) 2 L 7 2 4F RT A6WE 2002022200097 20020222 00097 WP 2002 2 22 ASAA0180264 1 20010914 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 933AS 49234 PDX - DURING RON CHECK, OVERHEAD EMERGENCY LIGHTING WAS INOPERATIVE BETWEEN ROWS 7 AND 13. REPLACED ASSOCIATED BATTERY POWER SUPPLY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2002022200098 20020222 00098 WP 2002 2 22 ASAA0180265 1 20010914 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 GEG - DURING PREFLIGHT CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE FROM ROWS 13 TO 21. REPLACED ASSOCI ATED BATTERY POWER SUPPLY PACK. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2002022500064 20020225 00064 WP 2002 2 25 GTIA012241 1 20011108 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CORROSION, NICKS AND GOUGES AT SEAT TRACK -X22 INCH FROM STATION 440-532. REMOVED SEAT TRACK FROM STATION 4 40-532. FABRICATED DRILLED AND LOCATED NEW SEAT TRACK AND SPLICE. INSTALLED SEAT TRACK FROM STATION 440-532 PER DC9 SR M 51-30-1. (M) 2 L 7 2 4F A6WE 2002022500065 20020225 00065 WP 2002 2 25 GTIA012242 1 20011108 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CORROSION, NICKS AND GOUGED AT SEAT TRACK -X22 INCH FROM STATION 766-964. REMOVED SEAT TRACK FROM STATION 8 60-965. FABRICATED DRILLED AND LOCATED NEW SEAT TRACK FROM 860-965. FABRICATED DRILLED AND LOCATED SPLICE. INSTALLED SEAT TRACK SPLICE. REMOVED SET RACK FROM 766-860. FABRICATED DRILLED AND LOCATED NEW SECTION OF SEAT TRACK. INSTALLED SEAT TRACK FROM STATION 766-860 PER DC9 SRM 51-30-1. (M) 2 L 7 2 4F A6WE 2002022500066 20020225 00066 WP 2002 2 25 GTIA012243 1 20011108 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FOUND CORROSION NICKS AND GOUGES AT SEAT TRACK X22 INCH FROM STATION 200-228. REMOVED DAMAGED SECTION OF SEAT TRACK 200 -228. LOCATED AND DRILLED. INSTALLED SEAT TRACK AND SPLICE SRM 53-05. (M) 2 L 7 2 4F A6WE 2002022500067 20020225 00067 WP 2002 2 25 GTIA012244 1 20011108 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CORROSION, NICKS AND GOUGES AT SEAT TRACK X22 INCH FROM STATION 417-532. REMOVED DAMAGE SECTION OF SEAT TRA CK STATION 417-532. DRILLED NEW SEAT TRACK 417-532. INSTALLED NEW SEAT TRACK IN STATION 417-532. (M) 2 L 7 2 4F A6WE 2002022500068 20020225 00068 WP 2002 2 25 GTIA012245 1 20011108 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CORROSION, NICKS AND GOUGES AT SEAT TRACK X22 INCHES FROM STATION 532-649. CUT OFF SEAT TRACK DAMAGE IN STA TION 532-649. LOCATED AND DRILLED SEAT TRACK AND SPLICE. INSTALLED SEAT TRACK AND SPLICE IAW DC9 SRM 51-30-1. (M) 2 L 7 2 4F A6WE 2002022500069 20020225 00069 WP 2002 2 25 GTIA012247 1 20011108 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CORROSION, NICKS AND GOUGES AT SEAT TRACK X22 INCH FROM STATION 765-860. REMOVED DAMAGE SECTION FROM STATIO N 766-860. LOCATED AND DRILLED SEAT TRACK. INSTALLED SEAT TRACK IAW SRM DC9 51-30-5. (M) 2 L 7 2 4F A6WE 2002022500070 20020225 00070 WP 2002 2 25 GTIA012248 1 20011108 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CORROSION, NICKS AND GOUGES ANS SEAT TRACK X22 INCH FROM STATION 860-964. REMOVED DAMAGE SECTION FROM STATI ON 860-964. LOCATE AND DRILLED SEAT TRACK. SEAT TRACK INSTALLED FROM 860-964. (M) 2 L 7 2 4F A6WE 2002022500071 20020225 00071 WP 2002 2 25 GTIA012249 1 20011108 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CORROSION NICKS AND GOUGES AT SEAT TRACK X44 FROM STATION 200-303. CUT OFF THE SEAT TRACK DAMAGED STATION 2 00-303. LOCATED AND DRILLED SEAT TRACK AND SPLICE. INSTALLED SPLICE TWO AND SEAT TRACK IAW DC9 MM 53-40-11 AND SRM 53- 05. (M) 2 L 7 2 4F A6WE 2002022500072 20020225 00072 WP 2002 2 25 GTIA012250 1 20011108 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CORROSION, NICKS AND GOUGES AT SEAT TRACK X44 FROM STATION 303-417. CUT OFF THE SEAT TRACK DAMAGED STATION 303-417. LOCATED AND DRILLED SEAT TRACK. INSTALLED SEAT TRACK 303-417 IAW DC9 53-40-1. (M) 2 L 7 2 4F A6WE 2002022500073 20020225 00073 WP 2002 2 25 GTIA012251 1 20011108 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CORROSION, NICKS AND GOUGES AT SEAT TRACK X44 INCHES FROM STA 417-532. CUT OFF SECTION SEAT TRACK FROM STAT ION 417-532. LOCATED AND DRILLED SEAT TRACK AND SPLICE. INSTALLED SEAT TRACK AND SPLICE TWO IAW DC9 M 53-40-1. (M) 2 L 7 2 4F A6WE 2002022500074 20020225 00074 WP 2002 2 25 GTIA012252 1 20011108 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CORROSION, NICKS AND GOUGES AT SEAT TRACK X44 FROM STATION 860-964. CUT OFF SEAT TRACK DAMAGE IN STATION 86 0-964. LOCATED AND DRILLED SEAT TRACK. INSTALLED NEW SEAT TRACK FROM STATION 860-964 IAW DC9 SRM 51-30-1. (M) 2 L 7 2 4F A6WE 2002022500075 20020225 00075 WP 2002 2 25 GTIA012253 1 20011116 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CORROSION, NICKS AND GOUGES AT SEAT TRACK X22 FROM STATION 228-323. REMOVED DAMAGED SECTION OF SEAT TRACK S TATION 228-323. LOCATED AND DRILLED SEAT TRACK. INSTALLED SEAT TRACK STATION 228-323 IAW DC9 MM 53-40-1. (M) 2 L 7 2 4F A6WE 2002022500076 20020225 00076 WP 2002 2 25 GTIA012254 1 20011108 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CORROSION NICKS AND GOUGES AT SEAT TRACK -X22 INCH FROM STATION 200-342. REMOVED SEAT TRACK FROM STATION 28 5-342. FABRICATED DRILLED AND LOCATED SEAT TRACK FROM STATION 285-342. DRILLED AND LOCATE SPLICE. INSTALLED SEAT TRAC K FROM STATION 285-342 AND SPLICE. REMOVED SEAT TRACK FROM STATION 200-285. LOCATE AND DRILLED SEAT TRACK STATION 200- 285. LOCATE AND DRILL SPLICE STATION 285. INSTALLED SEAT TRACK AND SEAT TRACK SPLICE IAW DC9 SRM FROM STATION 200-342. (M) 2 L 7 2 4F A6WE 2002022500077 20020225 00077 WP 2002 2 25 GTIA012255 1 20011106 A 5542 SKIN DOUG DC9 DC932 3022066 WP RUDDER CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND RUDDER RIGHT LOWER SKIN CRACKED AT FASTENER ON RIB LOCATION NR 11. REMOVED DAMAGE, FABRICATED FILLER AND DO UBLER. INSTALLED REPAIR IAW DC9 SRM 5-03. (M) 2 L 7 2 4F A6WE 2002022500078 20020225 00078 WP 2002 2 25 GTIA012256 1 20011116 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND LEFT, OUTBOARD FLOORBOARD STATION 465-579 COUNTERSINKS BROKEN OUT AND SURFACE CORROSION. STOPPED DRILL CRAC KED. FORMED DOUBLER REPAIR. INSTALLED DOUBLER. REMOVED SURFACE CORROSION IAW DC9 SRM 53-01. (M) 2 L 7 2 4F A6WE 2002022500079 20020225 00079 WP 2002 2 25 GTIA012257 1 20011113 A 5320 CHANNEL DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - AFT LOWER CARGO COMPARTMENT CORRODED AT CHANNEL FROM STATION 889-775. REMOVED DAMAGE SECTION FROM STATION 859-889 . LOCATED AND DRILLED. INSTALLED CHANNEL. (M) 2 L 7 2 4F A6WE 2002022500080 20020225 00080 WP 2002 2 25 GTIA012258 1 20011124 A 5313 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND E/E BAY LONGERON 28 LEFT HAS CORROSION AT STATION 170-180. CUT OUT DAMAGE AND REMOVED. INSTALLED LONGERON AND SPLICE PER DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002022500081 20020225 00081 WP 2002 2 25 GTIA012259 1 20011116 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CORROSION, NICKS AND GOUGES AT SEAT TRACK X22 FROM STATION 323-417. CUT OFF SEAT TRACK DAMAGE IN STATION 32 3-417. DRILLED NEW SEAT TRACK IN STATION 323-417. DRILLED SPLICE IN STATION 417 SEAT TRACK. INSTALLED SEAT TRACK IN S TATION 323-417. INSTALLED NEW SPLICE IN STATION 417 AT SEAT TRACK IAW SRM DC9 51-30-5. (M) 2 L 7 2 4F A6WE 2002022500082 20020225 00082 WP 2002 2 25 GTIA012260 1 20011116 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND RIGHT INBOARD FLOORBOARD STATION 756-832 HAS SURFACE CORROSION, HOLES OVERSIZED AND COUNTERSINKS BROKEN OUT. FORMED PATH SHAPE FOR BROKEN OUT OVERSIZED HOLES PER DC9 SRM 55-01. (M) 2 L 7 2 4F A6WE 2002022500083 20020225 00083 WP 2002 2 25 GTIA012261 1 20011116 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND RIGHT INBOARD FLOORBOARD STATION 389 CRACKED AND TORN AT EDGE. FORM PATCH REPAIR FOR PANEL PER DC9 SRM 55-0 1. (M) 2 L 7 2 4F A6WE 2002022500084 20020225 00084 WP 2002 2 25 GTIA012262 1 20011108 A 5711 DOUBLER DOUG DC9 DC932 3022066 WP LT WING SPAR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND LEFT WING LEFT REAR SPAR DOUBLER CRACKED IMMEDIATELY OUTBOARD OF THE STATION XCW=58.688 TRAPEZOIDAL PANEL TO REAR SPAR ATTACH FITTING. REMOVED DAMAGE AREA. REPAIR DOUBLER FABRICATE. INSTALLED REPAIR DOUBLER IAW DC9. (M) 2 L 7 2 4F A6WE 2002022500085 20020225 00085 WP 2002 2 25 GTIA012263 1 20011119 A 5310 STRUCTURE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FORWARD CARGO COMPARTMENT HAS A CRACK BETWEEN STATION 465-484 BETWEEN LONGERON 30 AND 29L. FORMED INTERCOSTAL IAW DOUGLAS PRING SR09530005. FORMED AND INSTALLED REPAIR PARTS. (M) 2 L 7 2 4F A6WE 2002022500086 20020225 00086 WP 2002 2 25 GTIA012264 1 20011123 A 5320 ANGLE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND FORWARD CARGO DOOR JAMB WEB STRAP AND ANGLES HAVE TOOLING MARKS, CORROSION AND CRACKS STATION 427-436. ONE ANGLE WAS CRACKED FORMED A NEW ANGLE. FORMED ANGLE. (M) 2 L 7 2 4F A6WE 2002022500100 20020225 00100 WP 2002 2 25 ASAA0180266 1 20010916 A 2560 3961896501 LANYARD DOUG DC9 DC982 3022082 WP R1 DOOR DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 SEA - DURING PRE-FLIGHT CHECK, R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DETACHED FROM GIRT BAR. REATTACHED LANYARD TO GIRT BAR. (M) 2 L 7 2 4F A6WE 2002022500101 20020225 00101 WP 2002 2 25 ASAA0180267 1 20010919 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 964AS 40352 3862 53078 SEA - DURING LINE CHECK, EXTERIOR OVERWING EMERGENCY EXIT LIGHTS WERE DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BATTERY PACK (POWER SUPPLY). LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002022500102 20020225 00102 WP 2002 2 25 ASAA0180268 1 20010917 A 3397 0105606 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 974AS 53450 PDX - DURING PREFLIGHT CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE IN FIRST CLASS. REPAIRED BROKEN CON NECTOR LEAD. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002022500103 20020225 00103 WP 2002 2 25 ASAA0180269 1 20010918 A 2170 COALESCER BAG DOUG DC9 DC983 3022083 WP CABIN CONTAMINATED A ASAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 01 944AS 53019 PDX - DURING CRUISE, NOTED STRONG FUEL FUMES, WHICH EVENTUALLY DISSIPATED. REPLACED BOTH AIR CONDITIONING PACK COALESCE R BAGS. NO ODOR NOTED. (M) 2 L 7 2 4F RT A6WE 2002022500104 20020225 00104 NM 2002 2 25 ASAA0180271 1 20010922 A 3350 60030451 BATTERY PACK DOUG MD80 MD83 3023681 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 979AS 53471 LAX - DURING PREFLIGHT CHECK, COCKPIT OVERHEAD EMERGENCY LIGHTING WAS INOPERATIVE. REPLACED ASSOCIATED BATTERY POWER SU PPLY PACK AT B5-23. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT 2002022500105 20020225 00105 WP 2002 2 25 ASAA0180272 1 20010922 A 3350 0105606 LIGHT DOUG DC9 DC983 3022083 WP CABIN NOT SEATED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 948AS 53021 SEA - DURING PREFLIGHT CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE AT ROW 1. RESEATED BULB IN SOCKET. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002022600054 20020226 00054 NM 2002 2 26 EISA20010151 1 20011227 A 5310 NPN SKIN BOEING 727 727243 138408D NM TORN A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 17410 21663 ACCOMPLISHED SHEET METAL REPAIR AREA FORWARD OF RT OUT FLOW VALVE, STA 1166, STR. 24R.CORRECTIVE ACTION:CUT OUT DAMAGED AREA. FABRICATED DOUBLER .071 2024-T3 8" X 12" IAW B727 SRM 53-30-3, FIG. 3. TREATED & PRIMED AND INSTALLED DOUBLER IAW B727 SRM 51-10-2 & 53-30-3, FIG. 3. 2 L 7 3 4F RT A3WE 2002022600055 20020226 00055 NM 2002 2 26 EISA20010126 1 20011016 A 3260 NPN RECEPTACLE BOEING 727 7272M7 138407S NM DIRTY A EISA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SW 07 721RW 21200 GEAR RETRACTED ALL RED LIGHTS ILLUMINATED (GEAR LIGHTS)-TAIL SKID LIGHT ILLUMINATED ALSO.CORRECTIVE ACTION: REMOVED LAN DING GEAR ACCESSORY UNIT. CLEANED AND INSP. RACK RECEPTICAL. REINSTALLED LANDING GEAR ACCESSORY UNIT. SYS OP CKS OK IAW 727 MM CH 32-09-121 2 L 7 3 4F A3WE 2002022600056 20020226 00056 NM 2002 2 26 EISA20010131 1 20011128 A 5753 652466517 FRAME BOEING 727 727200 138407E NM TE FLAP CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 702NE 22460 LT INBD MID FLAP CENTER SLIDING TRACK INBD FRAME HAS 2" CRACK. MACHINED BATHTUB FITTING AND INSTALLED PER VEHICLES CONS ULTING INC DRAWING #57-01600-1 2 L 7 3 4F RT A3WE 2002022600057 20020226 00057 NM 2002 2 26 EISA20010138 1 20011212 A 5310 NPN SKIN BOEING 727 727223 1384074 NM CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6813 19488 FUSELAGE SKIN CORRODED AT BS 336, STR 25R.WRITTEN FROM NON-ROUTINE CARD 405 FROM CPC C53-111-03 PAGE 4--N/R CARD 435 WRI TTENCORRECTIVE ACTION:REMOVED DAMAGED SKIN, HFEC AREA, FABRICATED REPAIR PARTS AND INSTALLED IAW EA. 53-01630-1, BOEING MESSAGE EOI-DAL-1-00024H. 2 L 7 3 4F A3WE 2002022600058 20020226 00058 NM 2002 2 26 EISA20010139 1 20011212 A 5310 NPN SKIN BOEING 727 727223 1384074 NM CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6813 19488 FUSELAGE SKIN BS 211, STR 25R GOUGED AND CRACKED AT FWD E/E DOOR CUTOUT.FOUND ON SERVICE CHECK--N/R CARD 431 WRITTENCORR ECTIVE ACTION: STOP DRILLED CRACK IAW B727 SRM 51-10-1. DYE PEN. IAW BOEING S.O.P. 20-50-2. FABRICATED REPAIR DOUBLER AND INSTALLED IAW B727 SRM 53-30-3 FIG. 1 & 51-30-2. 2 L 7 3 4F A3WE 2002022600059 20020226 00059 NM 2002 2 26 EISA20010128 1 20011018 A 3233 65404674 ACTUATOR BOEING 727 727225 1384077 NM NOSE GEAR INOPERATIVE A EISA O OTHER K FLUID LOSS AP APPROACH 1 SW 07 356PA 20626 LOST 'A' SYSTEM HYDRAULICS ON FINAL APPROACH. EXTENDED NOSE GEAR MANUALLY.CORRECTIVE ACTION:REMOVED AND REPLACED NOSE G EAR DOWN LOCK ACTUATOR-IAW MM 32-33-11 OPS AND LEAK GOOD. 2 L 7 3 4F A3WE 2002022600060 20020226 00060 NM 2002 2 26 EISA20010135 1 20011206 A 5730 NPN SKIN BOEING 727 727200 138407E NM CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 702NE 22460 L/H PLENUM CENTER WING SKIN HAS CORROSION AT STA. 850 LBL 30.FOUND DURING 'D' CHECK.CORRECTIVE ACTION: REMOVED CORROSIO N. FABRICATED REPAIR DOUBLER AND TRIPLER AND INSTALLED REPAIR IAW FLIGHT VEHICLES CONSULTING DRAWING 57-01600-2 2 L 7 3 4F RT A3WE 2002022600061 20020226 00061 NM 2002 2 26 EISA20010150 1 20011223 A 3260 656021132 ACCESSORY UNIT BOEING 727 7272M7 138407S NM INOPERATIVE A EISA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 721RW 21200 AFTER T/O, GEAR HANDLE RAISED, ALL 3 GEAR UNSAFE RED LIGHTS REMAIN ILLUMINATED ON FNT PANEL & TAILSKID LIGHT ON F/E PANE L. PERFORMED ABNORMAL CHECKLIST WITH SAME RESULT. RETURN TO IND. FOR UNEVENTFUL LANDING. DOWN & LOCK INDICATIONS ALL NORMAL & BELOW MAX LANDING WEIGHT.CORRECTIVE ACTION:R/R LANDING GEAR ACCESSORY UNIT OPS CK GOOD PER MM 32-09 2 L 7 3 4F A3WE 2002022600062 20020226 00062 NM 2002 2 26 EISA20010136 1 20011206 A 5730 NPN SKIN BOEING 727 727200 138407E NM CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 702NE 22460 R/H PLENUM CENTER WING SKIN HAS CORROSION AT ST 840, RBL 30.FOUND DURING 'D' CHECK.CORRECTIVE ACTION:REMOVED PREVIOUS RE PAIR, FABRICATED DOUBLER AND TRIPLER AND INSTALLED IAW FLIGHT VEHICLES CONSULTING DRAWING 57-01600-3 2 L 7 3 4F RT A3WE 2002022600063 20020226 00063 NM 2002 2 26 EISA20010137 1 20011206 A 5523 NPN TRIM TAB BOEING 727 727200 138407E NM DAMAGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 702NE 22460 L/H ELEVATOR TRIM TAB HAS ELONGATED HOLES AT FWD HINGE POINT.FOUND DURING 'D' CHK.CORRECTIVE ACTION:FAB AND INSTALLED RE PAIR DOUBLER IAW B727-55-20-2. WEIGH AND BALANCE IAW B727 SRM 51-80-9 FIG. 2. 2 L 7 3 4F RT A3WE 2002022600064 20020226 00064 NM 2002 2 26 EISA20010140 1 20011212 A 5310 NPN PANEL BOEING 727 727223 1384074 NM CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6813 19488 NOSE W/W PANEL BS 330 TO 350 STR L27 CORRODEDFOUND ON CPCP C53-100-01 PAGE 1, N/R CARD 444 WRITTENCORRECTIVE ACTION:REMO VED CORROSION IAW B727 SRM 51-10-6 FABRICATED REPAIR IAW 51-40-2 AND INSTALLED REPAIR IAW B727 SRM 51-40-2 & 51-30-2. 2 L 7 3 4F A3WE 2002022600065 20020226 00065 NM 2002 2 26 EISA20010141 1 20011212 A 5311 NPN STIFFENER BOEING 727 727223 1384074 NM CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6813 19488 L/H MLG W/W BS 870 LBL 45 VERTICAL STIFFENER CRACKED.FOUND ON CPCP INSP. C-53-100-01 PAGE 1, N/R CARD 410 WRITTENCORRECT IVE ACTION:FABRICATED AND INSTALLED REPAIR DOUBLER IAW B727 SRM 51-40-4 & 51-30-2. 2 L 7 3 4F A3WE 2002022600066 20020226 00066 NM 2002 2 26 EISA20010144 1 20011212 A 5310 6518415113 STIFFENER BOEING 727 727223 1384074 NM CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6813 19488 VERTICAL STIFFENER CORRODED BS 336 RBL 14.6 BELOW FLOOR PAN.FOUND ON CPCP C53-111-03 PAGE 4, N/R CARD 405 WRITTENCORRECT IVE ACTION:REMOVED AND REPLACED STIFFENER IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2002022600067 20020226 00067 NM 2002 2 26 EISA20010145 1 20011212 A 5310 NPN ANGLE BOEING 727 727223 1384074 NM CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6813 19488 ANGLE IN R/H W/W CORRODED, BS 870 RBL 48.0FOUND DURING CPCP C53-100-01 PAGE 1, N/R CARD 411 WRITTENCORRECTIVE ACTION:REM OVED ANGLE, FABRICATED NEW ANGLE FROM 7075-T6-063 AND INSTALLED IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2002022600068 20020226 00068 NM 2002 2 26 EISA20010147 1 20011217 A 3250 PIN BOEING 727 727277 138408S NM MISINSTALLED A EISA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 SW 07 275WC 20549 GOT UNSAFE NOSE GEAR DOOR LIGHT ON CLEANUP RTB. ON LANDING, HAD SEVERE VIBRATION WHEN NOSE WHEEL LOWERED TO GROUND.CORR ECTIVE ACTION:FOUND NLG APEX PIN IMPROPERLY INSTALLED. INSTALLED PIN PER MM 32-21.(SUBSEQUENT D.V.I. OF NLG AND DOORS & W/W FOUND NO DEFECTS REF MM 32-21 & 32-22) 2 L 7 3 4F RT A3WE 2002022600069 20020226 00069 NM 2002 2 26 EISA20010130 1 20011101 A 5310 BAC1510284 FRAME BOEING 727 727200 138407E NM CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 702NE 22460 AT 'D' CHECK, FOUND FRAME CRACKED AT BS 460, STR 3L.CORRECTIVE ACTION: REMOVE DAMAGE, FABRICATED DOUBLER FROM 7075-T6 . 063 IAW SRM 53-10-4, INSTALL REPAIR IAW SRM 53-10-4 FIG. 2. 2 L 7 3 4F RT A3WE 2002022600070 20020226 00070 NM 2002 2 26 EISA20010148 1 20011205 A 5753 658251714 SUPPORT BOEING 727 727200 138407E NM CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 702NE 22460 RT WING #7 FLAP TRACK FWD SUPPORT FITTING CRACKED.FOUND WHILE ACC. ROUTINE CARD 458, PLACED ON N/R CARD 3489.CORRECTIVE ACTION:REMOVED AND REPLACED FITTING IAW B727 MM 20-80-1 2 L 7 3 4F RT A3WE 2002022600071 20020226 00071 NE 2002 2 26 EISA20010149 2 20011219 A 7220 NOSE BULLET PWA BOEING 727 7272M7 138407S NM PWA JT8 JT8D15 52051 NE #2 ENGINE DETACHED A EISA E A ENGINE SHUTDOWN UNSCHED LANDING Y ENGINE STOPPAGE TO TAKEOFF 1 SW 07 725RW 685579 21502 685579 AT 300' AFTER TAKEOFF, #2 ENGINE STOPPED PRODUCING POWER, STARTED COMPRESSOR STALLING. PERFORMED CHECKLIST, AIR TURN BA CK TO AIRPORT.SUSPECTED CAUSE: DETACHMENT OF NOSE BULLET DURING FLIGHT.CORRECTIVE ACTION:REMOVED AND REPLACED #2 ENGINE IAW EXPRESS ONE ENGINE CHANGE PAPERWORK/PACKAGE. TRIM RUN ACCOMPLISHED, NO DEFECTS NOTED. OK FOR RETURN TO SERVICE UND ER TEC W/O 219062 2 L 7 3 4F 4 F A3WE E2EA 2002022600094 20020226 00094 NM 2002 2 26 DL72S020170 1 20010211 A 2782 1U11032 ACTUATOR BOEING 727 727225A 1384077 NM L/E SLAT FAILED A DALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 27 8891Z 21860 NR 4 SLAT LEFT WING REMAINED EXTENDED. REMOVED AND INSTALLED NR 4 SLAT ACTUATOR PER JIC OPN 7056. 2 L 7 3 4F RT A3WE 2002022600098 20020226 00098 NM 2002 2 26 2002F00118 1 20011229 A 5320 FLOOR SUPPORT BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 AS VIEWED FROM THE E/E COMPT, THERE IS CORROSION ON A MAIN DECK FLOOR SUPPORT AT BS 312 LBL 11R, ON ITS LOWER SIDE AROUN D A SCREW HOLE. (M) 2 L 7 2 4F A16WE 2002022600099 20020226 00099 NM 2002 2 26 2002F00119 1 20011228 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FORWARD CABIN FLOOR STRUCTURE, FLOORBEAM UPPER CHORD AT BS 294 RBL 10 TO LBL 10 WL 208 HAS CORROSION. (M) 2 L 7 2 4F A16WE 2002022600100 20020226 00100 NM 2002 2 26 2002F00120 1 20011219 A 5313 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND BS 727 STRINGER 18A RIGHT, CRACK IN INBOARD STRINGER 18A WEB STRAP. CRACK EMANATING FROM HOLE AT BS 725.5 AND PRO PAGATING DOWN AND FORWARD. (M) 2 L 7 2 4F A16WE 2002022600101 20020226 00101 NM 2002 2 26 2002F00121 1 20011219 A 5320 CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 LEFT CABIN STATION 827 STRINGER 6L HAS ATTACH CLIP CRACKED. (M) 2 L 7 2 4F A16WE 2002022600103 20020226 00103 NM 2002 2 26 2002F00122 1 20011219 A 5320 TIE CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND CRACK IN U-CHANNEL TIE CLIP AT STRINGER 4L FLIGHT STATION 625. (M) 2 L 7 2 4F A16WE 2002022600106 20020226 00106 NM 2002 2 26 2002F00123 1 20011219 A 5320 CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 LEFT CABIN STATION 747 STRINGER 4 AND STRINGER 7 HAS ATTACH CLIPS CRACKED. (M) 2 L 7 2 4F A16WE 2002022600107 20020226 00107 NM 2002 2 26 2002F00124 1 20011219 A 5310 SHEAR TIE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND SHEAR TIE CLIP IS CRACKED AT STATION 616 STRINGER 5R. (M) 2 L 7 2 4F A16WE 2002022600109 20020226 00109 NM 2002 2 26 2002F00125 1 20011219 A 5320 TIE CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND STRINGER TIE CLIPS CRACKED AT STATION 727B, STRINGER 3R, 4R, 5R AND 6R. (M) 2 L 7 2 4F A16WE 2002022600110 20020226 00110 NM 2002 2 26 2002F00126 1 20011219 A 5320 ANGLE BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND R2 DOOR THRESHOLD AREA HAS CORROSION ON SUPPORT ANGLES BS 950 THROUGH 1006 RBL 52. (M) 2 L 7 2 4F A16WE 2002022600111 20020226 00111 NM 2002 2 26 2002F00127 1 20011219 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND CORROSION AROUND FLOORBEAM FASTENER HOLES AT STATION 344 LBL 10 AND STATION 360 RBL 1. (M) 2 L 7 2 4F A16WE 2002022600112 20020226 00112 NM 2002 2 26 2002F00128 1 20011219 A 5313 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND BS 727 STRINGER 18A LEFT VERTICAL OUTER CHORD IS CRACKED FROM THE FORWARD HOLE BS 727.5 AND PROPAGATES AFT APPROXI MATELY .25 INCH IN LENGTH. (M) 2 L 7 2 4F A16WE 2002022600113 20020226 00113 NM 2002 2 26 2002F00129 1 20011218 A 5320 ATTACH ANGLE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND LEFT FORWARD PIT FUSELAGE STATION 380 LBL 51 FRAME ATTACH ANGLE CRACKED. (M) 2 L 7 2 4F A16WE 2002022600114 20020226 00114 NM 2002 2 26 2002F00130 1 20011218 A 5311 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 ON INSPECTION OF BS 178 BULKHEAD, NOTED CRACK FROM AFT SIDE ON PILOT SIDE INSPECTED SIDE CHORD AREA ABOVE W/L 207. TWO INCH CRACK DOWN RADIUS OF SIDE CHORD. (M) 2 L 7 2 4F A16WE 2002022600124 20020226 00124 NM 2002 2 26 2002F00131 1 20011217 A 5530 SUPPORT BRACKET BOEING 737 7372H4 138448C NM VERTICAL STAB CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 VERTICAL STABILIZER AFT WEB SUPPORT BRACKET IS CRACKED OUT AROUND FASTENERS AT FIN WL 58.18 AND BS 1088. (M) 2 L 7 2 4F A16WE 2002022600126 20020226 00126 NM 2002 2 26 TSAA0253012 1 20011205 A 5711 SPAR BOEING 737 737230 1384401 NM RT WING CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 823AL 23154 DISCOVERED CORROSION AT RIGHT WING WBL 304.5 FORWARD SPAR LOWER CHORD. REMOVED CORROSION PER SRM 737-100/200, 57-30-1 F IGURE 1. HFEC INSPECTED BLENDOUT AREA TO ENSURE NO CRACKS AND CORROSION REMOVED. RESTORED AIRCRAFT TO NORMAL IAW ECO 2 135. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2002022600127 20020226 00127 NM 2002 2 26 TSAA0253017 1 20011217 A 5511 6547503 SPAR BOEING 737 737230 1384401 NM HORIZ STAB CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 823AL 23154 BLENDOUT THE CORROSION DAMAGE ON HORIZONTAL STABILIZER UPPER CHORD AT ELEVATOR STATION 66.54 TO A 10:1 RATIO SPANWISE. FLAP PEEN REPAIR AREA. FABRICATED AND INSTALLED AN EXTERNAL DOUBLER. SHOT PEEN, ALODINE, AND PRIMED EXTERNAL DOUBLER I AW ECO 2513. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2002022600128 20020226 00128 EA 2002 2 26 ASOA01304 1 20011228 A 5610 NP1393221 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A ASOA K NONE O OTHER LD LANDING 1 SO 11 824AS 7203 FLT 4325 - DURING LANDING ROLL IN DHN, THE CAPTAINS LEFT SIDE WINDOW SHATTERED. MAINTENANCE REMOVED AND REPLACED THE SH ATTERED LEFT SIDE PILOT WINDOW. A LEAK CHECK WAS PERFORMED, AND NO LEAKS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. (M ) 2 L 7 2 4F RT A21EA 2002022600129 20020226 00129 SO 2002 2 26 ASOA01305 1 20011230 A 2421 23080013 GENERATOR EMB 120 EMB120RT 3260202 SO RT ENGINE MALFUNCTIONED A ASOA K NONE H ELECT. POWER LOSS-50 PC AP APPROACH 1 SO 11 242AS 120069 FLT 4926 - DURING A SHORT FINAL APPROACH INTO DFW, THE RIGHT MAIN GENERATOR FAILED. THE CAPTAIN TRIED TO RESET THE GENE RATOR IN THE AIR, BUT IT WOULD NOT RESET. AN EMERGENCY WAS DECLARED, AND THE AIRCRAFT MADE AN UNEVENTFUL LANDING AT DFW . MAINTENANCE RESET THE CIRCUIT BREAKER AND PARALLELED THE LEFT AND RIGHT GENERATORS. OPERATIONAL CHECKS GOOD. AIRCRA FT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2002022600137 20020226 00137 WP 2002 2 26 ASAA0180273 1 20010923 A 2560 3961896501 LANYARD DOUG DC9 DC983 3022083 WP R1 DOOR DETACHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 969AS 53063 SEA - DURING PRE-FLIGHT CHECK, R-1 DOOR EMERGENCY SLIDE GIRT BAR TO LATCH LANYARD WAS FOUND DETACHED. REATTACHED LANYAR D. (M) 2 L 7 2 4F RT A6WE 2002022600138 20020226 00138 WP 2002 2 26 ASAA0180274 1 20010924 A 3350 MODULE DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 LAX - DURING PREFLIGHT CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE AT ROW 31. REPLACED LIGHT MODULE. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002022600139 20020226 00139 WP 2002 2 26 ASAA0180275 1 20011002 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 933AS 49234 OAK - DURING C-CHECK, FOUND CORROSION UNDER RIBSTRIP FROM FS STATION 788 TO 1361. REMOVED CORROSION AND INSTALLED DOUBL ER PER EA 5330-01539. (M) 2 L 7 2 4F A6WE 2002022600140 20020226 00140 WP 2002 2 26 ASAA0180276 1 20010923 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 LAX - DURING PREFLIGHT CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE AT ROW 30. REPLACED LIGHT MODULE SO CKET AND RELAMPED. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002022600141 20020226 00141 WP 2002 2 26 ASAA0180277 1 20010930 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 943AS 53018 LAX - DURING PREFLIGHT CHECK, TWO EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN FORWARD CABIN. RESECURED LOOSE CONNECTION. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002022600142 20020226 00142 WP 2002 2 26 ASAA0180278 1 20011003 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 948AS 53021 SEA - DURING PREFLIGHT CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE IN 1ST CLASS. RECONNECTED MODULE. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2002022600143 20020226 00143 WP 2002 2 26 ASAA0180281 1 20011010 A 2170 COALESCER BAG DOUG DC9 DC982 3022082 WP A/C BAY DIRTY A ASAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 01 934AS 49235 PDX - DURING CRUISE (SJC-PDX), NOTED 'GASEOUS SMELL' IN PASSENGER CABIN. REPLACED BOTH AIR CONDITIONING PACK COALESCER BAGS. ALSO, WASHED LEFT AND RIGHT MLG WHEEL WELLS, AFT AIRCRAFT BELLY AND APU INLET. NO ODOR NOTED UPON TEST WITH APU- SUPPLIED AIR. (M) 2 L 7 2 4F A6WE 2002022600144 20020226 00144 2002 2 26 ASAA0180287 4 20011017 A 2565 D29984211 HARNESS DOUG DC9 DC982 3022082 WP EVAC SLIDE FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 935AS 43120 512 49236 OAK - DURING C-CHECK, AFT (REAR) DOOR EMERGENCY SLIDE HARNESS FAILED SYSTEM CHECK. REPLACED EMERGENCY SLIDE. SYSTEM CH ECKED OK. (M) 2 L 7 2 4F A6WE 2002022600145 20020226 00145 WP 2002 2 26 ASAA0180295 1 20011102 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 958AS 53024 SEA - DURING A PREFLIGHT CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE IN FIRST CLASS CABIN. RECONNECTED MODULE IN FIRST CLASS. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002022600146 20020226 00146 NM 2002 2 26 ASAA0180296 1 20011102 A 2560 83700211 LANYARD DOUG MD80 MD83 3023681 NM TAILCONE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 981AS 53472 LAX - DURING PREFLIGHT CHECK, THE TAILCONE SLIDE LANYARD WAS FOUND DISCONNECTED. THE LANYARD WAS RE-ATTACHED. (M) 2 L 7 2 4F RT 2002022600150 20020226 00150 NM 2002 2 26 2002F00117 1 20011230 A 2612 FIRE WARNING BOEING 737 7372H4 138448C NM COCKPIT MALFUNCTIONED A RYNA O OTHER N FALSE WARNING DE DESCENT 1 CE 07 29SW 21340 MASTER FIRE WARNING LIGHT FLICKERED ON AND OFF DURING DESCENT. ON FINAL, LIGHT CAME ON STEADY WITH NO OTHER ASSOCIATED FIRE WARNINGS. LIGHT WAS RESET. (M) 2 L 7 2 4F A16WE 2001090500100 20010905 00100 EU 2001 9 5 AUS20010920 2 20010823 A 7532 32145525 CONNECTOR GE CFM563C BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C 13802 EU COMPRESSOR BLEED LOOSE W O OTHER E VIBRATION/BUFFET CL CLIMB 1 AU S (AUS) LT ENGINE BLEED AIR PRESSURE REGULATING AND SHUTOFF VALVE (PRSOV) CONNECTOR PLUG LOOSE. 2 L 7 2 4F 4 F RT A16WE E21EU 2002022700068 20020227 00068 NE 2002 2 27 WRLA200115 2 20010917 A 7320 8010003 FMU DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE NR 2 ENGINE MALFUNCTIONED A E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 EA 27 275WA 48631 P723942 DURING DESCENT, NR 2 ENGINE 'SELECTED FADEC ALT' AND FADEC MAINT' ALERT WITH ENGINE AT VERY LOW FUEL FLOW 'RPM LOW' ALER T THEN ILLUMINATED ENGINE SHUTDOWN IAW CHECK LIST. ONE RESTART ATTEMPTED, SAME CONDITIONS ENGINE SHUTDOWN AND SECURED I AW CHECKLIST LANDED. AIRCRAFT LANDED JFK. ACCOMPLISHED CFDS FOR FAULTS, EEC 2A, AND EEC 2B SHOWED 351-24 FMU RESOLVER SNG. ACCOMPLISHED RETURN TO SERVICE TEST RAN NR 2 ENGINE OPS CHECK OK, NO FADEC ALERTS ON ENGINE RUN. (M) 2 L 7 3 4F 4 F RT A22WE E24NE 2002022700069 20020227 00069 2002 2 27 WRLA200117 4 20010915 A 3417 HG280D5 ADC DOUG DC10 DC1030 3023501 WP NR 2 POSITION FAULTY A WRLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 526MD 46998 ABORTED TAKEOFF AT 80 KNOTS CALLED BY FIRST OFFICER DUE TO 25 KNOTS AIRSPEED DISCREPANCY BETWEEN FIRST OFFICER AND CAPTA INS AIRSPEED INDICATORS. TAXI BACK TO GATE FIRST OFFICER AIRSPEED INDICATOR READS 70 KNOTS. REMOVED AND REPLACED NR 2 AIR DATA COMPUTER (CADC) P/N ON HG280D5, P/N OFF HG280D5 S/N ON 596, S/N OFF 515. PERFORMED STATIC CHECK SYSTEM, CHECKE D OK. (M) 2 L 7 3 4F A22WE 2002022700072 20020227 00072 NE 2002 2 27 WRLA200118 2 20011016 A 7230 COMPRESSOR DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE NR 3 ENGINE DAMAGED A WRLA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 27 274WA 48633 P733783 SHORTLY AFTER ROTATION HEARD LOUD NOISE WITH VIBRATION EGT PEAKED AT 657 DEGREES NR 3 ENGINE. THE ENGINE WAS SHUT DOWN, THE CREW DUMPED EXCESS FUEL AND LANDED THE AIRCRAFT. CHECKED CHIP DETECTORS, ALL NORMAL BORESCOPED TURBINE SECTION BLA DES NO DAMAGE BORESCOPED COMPLETE COMPRESSOR FOUND SEVERAL BLADES ON SEVERAL STAGES, WITH MISSING PARTS, SOME OUT OF LIM ITS (HPC). REMOVED AND REPLACED ENGINE 3 AS PER WORLD MD11 TASK CARD 0104 ON SERIAL NR 717701 OFF SERIAL NR P733783. ( M) 2 L 7 3 4F 4 F RT A22WE E24NE 2002022700073 20020227 00073 NM 2002 2 27 WRLA200119 1 20011112 A 3020 17343108 SWITCH DOUG MD11 MD11F 3023600 NM NR 2 ENGINE FAILED A WRLA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 274WA 48633 NR 2 ENGINE ANTI-ICE DUCT (ALERT) ON IN FLIGHT COMPLIED WITH EMERGENCY PROCEDURE AND SECURED NR 2 ENGINE. DIVERT TO SUI TABLE AIRPORT. AIRCRAFT LANDED IN SHANNON IRELAND AFTER DUMPING FUEL TO BE BELOW MAX LANDING WEIGHT. FOUND WITH ALL EN GINES AND APU SYSTEMS STATIC, ALERT WOULD SHOW INTERMITTENTLY SUSPECT THERMAL SWITCH 51.1081. DEFERRED NR 2 ANTI-ICE VA LVE COWL INOPERATIVE. REPLACED THERMAL SWITCH AND CLOSED MEL AT A-CHECK. (M) 2 L 7 3 4F RT A22WE 2002022700078 20020227 00078 NM 2002 2 27 TSAA0257013 1 20011204 A 5730 65515892 SKIN BOEING 727 7272Q9 138448M NM RT WING CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 RIGHT WING SKIN HAS EXFOLIATION CORROSION AT WBL 166 LOWER SURFACE SKIN FORWARD SPAR CHORD. CLEANED UP WITHIN LIMITS IA W SRM 57-300-01. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2002022700079 20020227 00079 NM 2002 2 27 TSAA0257015 1 20011204 A 5730 65515892 SKIN BOEING 727 7272Q9 138448M NM RT WING CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 RIGHT WING SKIN HAS EXFOLIATION CORROSION AT WBL 326 LOWER SURFACE SKIN AFT OF REAR SPAR. CLEANED UP AND EVALUATED WITH IN LIMITS IAW SRM 57-3000-01. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2002022700080 20020227 00080 NM 2002 2 27 TSAA0257016 1 20011204 A 5730 65515892 SKIN BOEING 727 7272Q9 138448M NM RT WING CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 RIGHT WING SKIN HAS EXFOLIATION CORROSION AT WBL 330 LOWER SURFACE SKIN AFT OF REAR SPAR. CLEANED UP AND EVALUATED WITH IN LIMITS IAW SRM 57-3000-01. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2002022700082 20020227 00082 NM 2002 2 27 USAA011411 1 20011211 A 5320 655383918 CAP BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 46642 23312 PIT - FOUND STRIP CAP CORRODED 1 INCH CIRCLE AROUND NUT PLATE, SIDE PLATE FORWARD CARGO AT STATION 500 S26C. DEFECTIVE PART REPLACED WITH IDENTICAL PART. (M) 2 L 7 2 4F RT A16WE 2002022700083 20020227 00083 NM 2002 2 27 USAA011412 1 20011214 A 5512 65C274941 SKIN BOEING 737 7373B7 1384580 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 46642 23312 PIT - FOUND BOTTOM SKIN CRACKED .25 INCH LONG, AFT SPAR RIGHT STAB, STATION 152. INSTALLED DOUBLER PER SRM 55-10-01 FIG 204. (M) 2 L 7 2 4F RT A16WE 2002022700084 20020227 00084 NM 2002 2 27 USAA011413 1 20011211 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 23312 PIT - FOUND FRAME CORRODED 1 INCH CIRCLE UPPER AND LOWER SURFACE, BELTFRAME AT STATION 500 S-26R. BLENDED AND TREATED P ER SRM 53-00-07 FIG 101. (M) 2 L 7 2 4F RT A16WE 2002022700085 20020227 00085 NM 2002 2 27 USAA011414 1 20011207 A 5320 6546812175 FLOOR SUPPORT BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 46642 23312 PIT - FOUND FLOOR SUPPORT .125 INCH BY .125 INCH AROUND 2 NUT PLACE HOLES, FLOOR SUPPORT ANGLE BETWEEN 1006 AND 1016, LB L 37. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M) 2 L 7 2 4F RT A16WE 2002022700101 20020227 00101 NE 2002 2 27 WRLA200116 2 20010917 A 7320 8010003 FMU DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE NR 2 ENGINE FAILED A WRLA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 275WA 48631 P723942 ON CLIMB-OUT OF JFK, NR 2 WAS SHUTDOWN FOR LOW RPM, NO RESTART OF NR 2 ENGINE WAS ATTEMPTED. THE AIRCRAFT WAS POSITIONI NG FROM JFK TO XNA FOR A SCHEDULED A-CHECK. REMOVED AND REPLACED NR 2 ENGINE FUEL METERING UNIT. LEAK AND OPERATION CH ECK GOOD IAW MD-11 MM 73-21-01. (M) 2 L 7 3 4F 4 F RT A22WE E24NE 2002022700104 20020227 00104 EU 2002 2 27 USAABA02003 1 20010125 A 3350 321430 POWER SUPPLY AIRBUS 330 A330323 3930335 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 672UW 0333 PHL - EPSU'S AT R1, L3, R3, AND L4 FAILED SYSTEM TEST. MAINTENANCE REPLACED THE EPSU'S. (M) 2 L 7 2 4F RT A46NM 2002022700105 20020227 00105 NM 2002 2 27 USAABB02009 1 20011222 A 3350 873100151REV12 LIGHT BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 603AU 22198 CLT - FOUND FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE AT ROW 18. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2002022800061 20020228 00061 NM 2002 2 28 DL76S020057 1 20011212 A 3010 DUCT BOEING 767 767332 1382001 NM L/E SLAT CRACKED A DALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 27 117DL 23276 NR 5 LEADING EDGE SLAT HAD A ANTI-ICE DUCT MALFUNCTION, IN WHERE THE FORWARD DUCT WAS CRACKED AND DAMAGED. SLAT WAS REP AIRED PER ERA 410858-14 REV 0 (REF CMM 57-43-61). 2 L 7 2 4F RT A1NM 2002022800099 20020228 00099 SO 2002 2 28 SIMA200201704 1 20011212 A 5310 DOOR FRAME EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 606AE 145062 LEVEL 2 CORROSION ON BEAM BENEATH LOWER BAGGAGE DOOR CUT OUT PLATE. REPLACED LOWER BAGGAGE DOOR CUTOUT FRAME IAW EMB 14 5 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002022800100 20020228 00100 SO 2002 2 28 SIMA200201705 1 20011216 A 5344 HINGE FITTING EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 605RR 145059 LEVEL 1 CORROSION, ON RIGHT DOOR HINGE PLATE FORWARD OF BELLY PANEL. REMOVED CORROSION IAW EMB 145 SRM 51-10-02 AND EMB GST-4080/01. (M) 2 L 7 2 4F RT T00011AT 2002022800101 20020228 00101 SO 2002 2 28 SIMA200201706 1 20011217 A 5330 PANEL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 605RR 145059 CORROSION ON FORWARD BELLY PANEL FORWARD OF BOTTOM PLATE. REMOVED CORROSION IAW EMB 145 SRM 51-10-02 AND EMB GST 4080/0 1. (M) 2 L 7 2 4F RT T00011AT 2002022800102 20020228 00102 SO 2002 2 28 SIMA200201707 1 20011216 A 5320 THRESHOLD EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 605RR 145059 ABI - LEVEL 2 CORROSION ON SERVICE DOOR THRESHOLD. BLENDED OUT CORROSION AND INSTALLED DOUBLER IAW EMB GST 4055/01. (M ) 2 L 7 2 4F RT T00011AT 2002022800103 20020228 00103 SO 2002 2 28 SIMA200201708 1 20011218 A 5320 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 605RR 145059 LEVEL 2 CORROSION ON SERVICE DOOR FORWARD SILL. BLENDED OUT CORROSION IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002022800104 20020228 00104 SO 2002 2 28 SIMA200201709 1 20011218 A 5320 FITTING EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 605RR 145059 ABI - LEVEL 2 CORROSION ON CARGO FLOOR 'T' SECTION BETWEEN FRAMES 66R AND 67R. BLENDED OUT CORROSION IAW EMB GST 4054/0 1. (M) 2 L 7 2 4F RT T00011AT 2002022800105 20020228 00105 SO 2002 2 28 SIMA200201710 1 20011218 A 5315 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 605RR 145059 ABI - CORROSION ON LT OMEGA BEAM AT FRAMES 49 AND 50. BLENDED OUT CORROSION IAW EMB GST 4053/01. (M) 2 L 7 2 4F RT T00011AT 2002022800106 20020228 00106 SO 2002 2 28 SIMA200201711 1 20011218 A 5320 DOUBLER EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 605RR 145059 LEVEL 2 CORROSION ON CARGO COMPARTMENT DOUBLER FOR FOLDING FLAP. BLENDED OUT CORROSION IAW EMB GS 4054/01. (M) 2 L 7 2 4F RT T00011AT 2002022800107 20020228 00107 SO 2002 2 28 SIMA200201712 1 20011217 A 5310 DOOR FRAME EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 605RR 145059 LEVEL 2 CORROSION ON CARGO DOOR CUT OUT LOWER EDGE. BLENDED OUT CORROSION IAW EMB GST 5054/01 AND GST-4140/01. (M) 2 L 7 2 4F RT T00011AT 2002022800108 20020228 00108 SO 2002 2 28 SIMA200201713 1 20011218 A 5315 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 605RR 145059 ABI - LEVEL 2 CORROSION ON AFT DIGITAL. BLENDED OUT CORROSION IAW EMB GST-4055/01. (M) 2 L 7 2 4F RT T00011AT 2002022800109 20020228 00109 SO 2002 2 28 SIMA200201802 1 20011218 A 5320 SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 605RR 145059 ABI - LEVEL 2 CORROSION ON PASSENGER DOOR THRESHOLD SUPPORTS. BLENDED OUT CORROSION IAW EMB GST 4055/01. (M) 2 L 7 2 4F RT T00011AT 2002022800110 20020228 00110 SO 2002 2 28 SIMA200201803 1 20011218 A 5320 PLATE EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 605RR 145059 LEVEL 2 CORROSION ON FORWARD AND AFT DIAMOND GUSSET PLATES. REPLACED FORWARD AND AFT DIAMOND GUSSET PLATES IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002022800111 20020228 00111 SO 2002 2 28 SIMA200201804 1 20011218 A 5315 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 605RR 145059 ABI - LEVEL 2 CORROSION ON CENTER BEAM FLOOR RAMP. REPLACED CENTER BEAM FLOOR RAMP IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002022800112 20020228 00112 SO 2002 2 28 SIMA200201805 1 20011218 A 5315 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 605RR 145059 LEVEL 2 CORROSION ON PREVIOUS REPAIR OF LT OMEGA BEAM AT FRAME 20. BLENDED OUT CORROSION AND INSTALLED DOUBLER ON LEFT OMEGA BEAM AT FRAME 20 IAW EMB 145 SRM 51-40-02 AND 53-21-10. (M) 2 L 7 2 4F RT T00011AT 2002022800113 20020228 00113 SO 2002 2 28 SIMA200201806 1 20011219 A 5320 CHANNEL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 605RR 145059 LEVEL 2 CORROSION, ON RIGHT HAT BEAM AT FRAME 23. BLENDED OUT CORROSION ON INSTALLED DOUBLER ON RIGHT HAT BEAM AT FRAME 23 IAW EMB GST 4055/01. (M) 2 L 7 2 4F RT T00011AT 2002022800114 20020228 00114 SO 2002 2 28 SIMA200201807 1 20011219 A 5320 ANGLE EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 605RR 145059 LEVEL 2 CORROSION ON RIGHT 'L' PROFILE AT FRAME 23. REPLACED RT 'L' PROFILE AT FRAME 23 IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002022800115 20020228 00115 SO 2002 2 28 SIMA200201808 1 20011219 A 5320 CROSSBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 605RR 145059 CORROSION ON RIGHT CROSS MEMBER AT FRAME 23. REPLACED RIGHT CROSS MEMBER AT FRAME 23 IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002022800116 20020228 00116 SO 2002 2 28 SIMA200201809 1 20011219 A 5320 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 605RR 145059 LEVEL 2 CORROSION, ON LEFT SILL BETWEEN FRAMES 18 AND 21. BLENDED OUT CORROSION AND INSTALLED DOUBLER ON LEFT SILL BETW EEN FRAMES 18 AND 21 IAW EMB GST-4055/01. (M) 2 L 7 2 4F RT T00011AT 2002022800117 20020228 00117 SO 2002 2 28 SIMA200201810 1 20011219 A 5320 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 605RR 145059 IMBV - LEVEL 2 CORROSION ON SERVICE DOOR AFT SILL. REPLACED SERVICE DOOR AFT SILL IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002022800118 20020228 00118 SO 2002 2 28 SIMA200201811 1 20011219 A 5320 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 605RR 145059 LEVEL 2 CORROSION ON LEFT OUTBOARD SILL NUT PLATE HOLE AT FRAME 61. BLENDED OUT CORROSION ON LEFT OUTBOARD SILL NUTPLAT E HOLE AT FRAME 61 IAW EMB GST-4054-01. (M) 2 L 7 2 4F RT T00011AT 2002022800119 20020228 00119 SO 2002 2 28 SIMA200201812 1 20011219 A 5320 GUSSET EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 605RR 145059 CORROSION ON LEFT HAT BEAM GUSSET IN LAVATORY. BLENDED OUT CORROSION AND REPAIRED LT HAT BEAM GUSSET IN LAVATORY IAW EM B GST-4053/01. (M) 2 L 7 2 4F RT T00011AT 2002022800120 20020228 00120 SO 2002 2 28 SIMA200201813 1 20011219 A 5320 GUSSET EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 605RR 145059 LEVEL 2 CORROSION ON CENTER HAT BEAM GUSSET IN LAVATORY. BLENDED OUT CORROSION AND REPAIRED CENTER HAT BEAM GUSSET IN L AVATORY IAW EMB GST 4053/01. (M) 2 L 7 2 4F RT T00011AT 2002022800121 20020228 00121 SO 2002 2 28 SIMA200201814 1 20011219 A 5320 GUSSET EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 605RR 145059 LEVEL 2 CORROSION ON RIGHT HAT BEAM GUSSET IN LAVATORY. BLENDED OUT CORROSION AND REPAIRED RIGHT HAT BEAM GUSSET IN LAV ATORY IAW EMB GST 4053/01. (M) 2 L 7 2 4F RT T00011AT 2002022800122 20020228 00122 SO 2002 2 28 SIMA200201815 1 20011221 A 5320 CHANNEL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 605RR 145059 ABI - LEVEL 2 CORROSION ON CENTER HAT BEAM AT FRAME 20. REPLACED CENTER HAT BEAM AT FRAME 20 IAW EMB 145 SRM 51-40-02 A ND EMB GST 4142/01. (M) 2 L 7 2 4F RT T00011AT 2002022800123 20020228 00123 SO 2002 2 28 SIMA200202101 1 20011219 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 713AE 145249 ABI - DURING MBV INSPECTION MAINTENANCE, FOUND THE LEFT OMEGA BEAM TO BE CORRODED AT FRAME 20. MAINTENANCE REPAIRED LEF T OMEGA BEAM IAW REPAIR STATEMENT EMB GST 4044/01. (M) 2 L 7 2 4F RT TOOO11AT 2002022800125 20020228 00125 SO 2002 2 28 SIMA200202102 1 20011219 A 5320 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 713AE 145249 ABI - DURING MBV INSPECTION, MAINTENANCE FOUND CORROSION ON THE SERVICE DOOR CENTER SILL. MAINTENANCE REPAIRED SILL IAW EMB REPAIR STATEMENT 4044/01 AND SRM 51-40-02. (M) 2 L 7 2 4F RT TOOO11AT 2002022800126 20020228 00126 SO 2002 2 28 SIMA200202103 1 20011219 A 5320 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 713AE 145249 ABI - DURING MBV INSPECTION, MAINTENANCE FOUND CORROSION ON THE SERVICE DOOR FORWARD SILL. MAINTENANCE REPAIRED SILL IA W EMB REPAIR STATEMENT 4044/01 AND SRM 51-40-02. (M) 2 L 7 2 4F RT TOOO11AT 2002022800127 20020228 00127 SO 2002 2 28 SIMA200202104 1 20011219 A 5320 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 713AE 145249 ABI - DURING MBV INSPECTION, MAINTENANCE FOUND CORROSION ON THE PASSENGER DOOR ENTRY WAY FLOORBOARD SUPPORTS. MAINTENAN CE REPLACED THE FLOORBOARD SUPPORTS IAW EMB REPAIR STATEMENT 4044/01 AND SRM 51-40-02. (M) 2 L 7 2 4F RT TOOO11AT 2002022800128 20020228 00128 SO 2002 2 28 SIMA200202105 1 20011219 A 5320 13500222001 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 713AE 145249 ABI - DURING MBV INSPECTION, MAINTENANCE FOUND CORROSION ON THE RIGHT GALLEY FLOOR EXTENSION. FLOOR EXTENSIONS WERE REP LACED IAW EMB SRM 51-40-02 AND REPAIR STATEMENT GST 4062/01. (M) 2 L 7 2 4F RT TOOO11AT 2002022800129 20020228 00129 SO 2002 2 28 SIMA200202106 1 20011220 A 5320 14521725013 SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 713AE 145249 ABI - DURING MBV INSPECTION, MAINTENANCE FOUND CORROSION ON THE GALLEY RAMP SUPPORT RAMP SUPPORTS WERE REPLACED IAW EMB SRM 51-40-02. (M) 2 L 7 2 4F RT TOOO11AT 2002022800130 20020228 00130 SO 2002 2 28 SIMA200202201 1 20011223 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 716AE 145264 ABI - DURING MBV INSPECTION MAINTENANCE, FOUND CORROSION ON THE CENTER OMEGA BEAM BETWEEN FRAMES 20 AND 22. MAINTENANCE REPAIRED OMEGA BEAM IAW EMB REPAIR STATEMENT GST4085A/01. (M) 2 L 7 2 4F RT TOOO11AT 2002022800131 20020228 00131 SO 2002 2 28 SIMA200202202 1 20011223 A 5320 CHANNEL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 716AE 145264 ABI - DURING MBV INSPECTION, MAINTENANCE FOUND CORROSION ON THE GALLEY AREA RIGHT HAT BEAM. MAINTENANCE REPAIRED HAT BE AM IAW EMB REPAIR STATEMENT GST4085A/01. (M) 2 L 7 2 4F RT TOOO11AT 2002022800132 20020228 00132 SO 2002 2 28 SIMA200202203 1 20011222 A 5320 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 716AE 145264 ABI - DURING MBV INSPECTION, MAINTENANCE FOUND CORROSION ON THE SERVICE DOOR CENTER SILL. MAINTENANCE REPAIRED SERVICE DOOR CENTER SILL IAW EMB REPAIR STATEMENT GST4085A/01. (M) 2 L 7 2 4F RT TOOO11AT 2002022800133 20020228 00133 SO 2002 2 28 SIMA200202204 1 20011222 A 5320 CROSSBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 716AE 145264 ABI - DURING MBV INSPECTION MAINTENANCE, FOUND CORROSION ON THE RIGHT CROSS MEMBER ANGLE AT FRAME 18. MAINTENANCE REPAI RED CROSS MEMBER ANGLE IAW EMB REPAIR STATEMENT GST4085A/01. (M) 2 L 7 2 4F RT TOOO11AT 2002022800134 20020228 00134 SO 2002 2 28 SIMA200202205 1 20011222 A 5320 GUSSET EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 716AE 145264 ABI - DURING MBV INSPECTION MAINTENANCE, FOUND CORROSION ON THE RIGHT AFT GUSSET AT FRAME 22. MAINTENANCE REPAIRED AFT GUSSET IAW EMB REPAIR STATEMENT GST4085A/01. (M) 2 L 7 2 4F RT TOOO11AT 2002022800135 20020228 00135 SO 2002 2 28 SIMA200202206 1 20011222 A 5320 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 716AE 145264 ABI - DURING MBV INSPECTION MAINTENANCE, FOUND CORROSION ON THE LEFT OUTBOARD FLOORBOARD SUPPORT BETWEEN FRAMES 20 AND 2 1. MAINTENANCE REPAIRED FLOORBOARD SUPPORT BETWEEN FRAMES 20 AND 21 IAW EMB REPAIR STATEMENT GST 4085A/01. (M) 2 L 7 2 4F RT TOOO11AT 2002022800136 20020228 00136 SO 2002 2 28 SIMA200202207 1 20011222 A 5320 13500469401 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 716AE 145264 ABI - DURING MBV INSPECTION MAINTENANCE, FOUND THE BOLT HOLES ON THE L SHAPED FLOOR EXTENSION TO BE CORRODED AT FRAME 22 . MAINTENANCE REPLACED THE FLOOR EXTENSION AT FRAME 22 IAW EMB 135 SRM 51-20-01 AND 51-40-02. (M) 2 L 7 2 4F RT TOOO11AT 2002022800137 20020228 00137 SO 2002 2 28 SIMA200202208 1 20011222 A 5320 14521843401 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 716AE 145264 ABI - DURING MBV INSPECTION MAINTENANCE, FOUND CORROSION ON THE FLOORBOARD SUPPORT ANGLE ON THE LEFT OMEGA BEAM AT FRAME 20. MAINTENANCE REPLACED THE FLOORBOARD SUPPORT ANGLE ON THE LEFT OMEGA BEAM IAW EMB SRM 51-40-02. (M) 2 L 7 2 4F RT TOOO11AT 2002022800138 20020228 00138 SO 2002 2 28 SIMA200202209 1 20011222 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 716AE 145264 ABI - DURING MBV INSPECTION MAINTENANCE, FOUND THE FORWARD DIGITAL TO BE CORRODED. MAINTENANCE REPAIRED THE FORWARD DIG ITAL IAW EMB REPAIR STATEMENT GST4123/01. (M) 2 L 7 2 4F RT TOOO11AT 2002022800139 20020228 00139 SO 2002 2 28 SIMA200202210 1 20011230 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 716AE 145264 ABI - DURING MBV INSPECTION, MAINTENANCE FOUND THE LEFT OMEGA BEAM TO BE CORRODED AT FRAME 20. MAINTENANCE REPAIRED THE LEFT OMEGA BEAM IAW EMB 135 SRM 53-21-10. (M) 2 L 7 2 4F RT TOOO11AT 2002022800140 20020228 00140 SO 2002 2 28 SIMA200202211 1 20011222 A 5320 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 716AE 145264 ABI - DURING MBV INSPECTION, MAINTENANCE FOUND THE RIGHT FORWARD SILL TO BE CORRODED. MAINTENANCE REPAIRED THE RIGHT FO RWARD SILL IAW EMB REPAIR STATEMENT GST 4085A/01 AND SRM 51-40-02. (M) 2 L 7 2 4F RT TOOO11AT 2002030100093 20020301 00093 WP 2002 3 1 IXXA0100078S 1 20011111 A 5754 WING DOUG DC8 DC862 3021970 WP LEADING EDGE CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 21CX 69635 3089 45955 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE RIGHT WING LEADING EDGE AT STATION XW485 JUST OUTBOARD OF THE #4 PYLON. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING ORDER EDP05-2 2 L 7 4 4F 4A25 2002030100094 20020301 00094 WP 2002 3 1 IXXA0100079S 1 20011120 A 5315 FLOORBEAM DOUG DC8 DC862 3021970 WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 21CX 69635 3089 45955 DURING ROUTINE C-CHECK INSPECTION A CRACK WAS DETECTED ON THE FLOORBEAM LEFT HAND FRAME ATTACHMENT PLATES AND CLIPS AT F S 320 TO 480. ACCOMPLISHED REMOVAL OF DAMAGED PLATES AND CLIPS. FABRICATED AND INSTALLED NEW ATTACHMENT PLATES AND CLIPS IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING ORDER EDP05-1 AND DRAWING NUMBER AE2443. 2 L 7 4 4F 4A25 2002030100095 20020301 00095 WP 2002 3 1 IXXA0100080S 1 20011118 A 5101 CLIP DOUG DC8 DC862 3021970 WP STA 1584 CORRODED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 21CX 69635 3089 45955 DURING ROUTINE C-CHECK INSPECTION CORROSION WAS DETECTED IN THE AFT CABIN FLOORBEAM AT STATION 1584. REMOVED DAMAGED FLO ORBEAM AND INSTALLED NEW FLOOR SUPPORT AND CLIP NUTS IN ACCORDANCE WITH DOUGLAS STRUCTURAL MAINTENANCE MANUAL. 2 L 7 4 4F 4A25 2002030400115 20020304 00115 NM 2002 3 4 EISA20010127 1 20011016 A 7603 THROTTLE CABLE BOEING 727 727223 1384074 NM NR 3 ENGINE DISCONNECTED A EISA E ENGINE SHUTDOWN O OTHER CL CLIMB 1 SW 07 6819 19494 EN ROUTE NR 3 ENGINE WENT TO MAX POWER. RETARDING THROTTLE HAD NO EFFECT. SHUT DOWN ENGINE. AFTER 20 MINUTES, MOVED S TART LEVER TO IDLE FOR 3 MINUTES TO PURGE FUEL CONTROL. FOUND NR 3 THROTTLE LINKAGE DISCONNECTED. INSTALLED BOLT AND C OTTER KEY, INSPECTED AND REPLACED MAIN OIL SCREEN. PERFORMED ENGINE RUN. OPS CHECK GOOD PER MM REF 72-00. 2 L 7 3 4F A3WE 2002030400116 20020304 00116 NM 2002 3 4 EISA20010129 1 20011016 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6839 20192 FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED FWD EMERGENCY EXIT LIGHT ASSY IAW B727 MM 33, OPS CHECK GOOD. 2 L 7 3 4F A3WE 2002030400118 20020304 00118 NM 2002 3 4 EISA20010132 1 20011128 A 5314 KEELBEAM BOEING 727 727200 138407E NM FUSELAGE CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 702NE 22460 LEFT MLG W/W BS 873 LBL 6 INSIDE KEEL BEAM LOWER CHORD CRACKED. TRIMMED OUT DAMAGED AREA. FABRICATED REPAIR DOUBLER, C AD PLATE DOUBLER AND INSTALLED IAW B727 SB 53-0208. 2 L 7 3 4F RT A3WE 2002030400158 20020304 00158 NE 2002 3 4 EISA20010133 2 20011201 A 7412 10353875 EXCITER BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE FAILED A EISA E ENGINE SHUTDOWN X ENGINE FLAMEOUT DE DESCENT 1 SW 07 361KP 20627 695364 AT TOP OF DESCENT FROM FL410 NR 1 ENGINE FLAMED OUT, WOULD NOT RESTART PER CHECKLIST. ENGINE WAS WINDMILLING FOR ABOUT 18 MINUTES, FUEL CONTROL UNIT PROCEDURES C/W. OIL PRESSURE DURING WINDMILLING AT 31 PSI. REMOVED AND REPLACED NR 1 IGN ITION EXCITER BOX AND SYSTEM OPS CHECK GOOD IAW BMM 74-10. COMPONENT CHANGE INFORMATION: P/N OFF 10-353875-4, S/N OFF 86224, (INOPERATIVE) MANUFACTURER: BENDIX. REMOVED AND REPLACED NR 1 ENGINE FUEL PUMP PER MM 73-11-16-IDLE LEAK CHECK W AS GOOD. FULL POWER RUN, OPS CHECK GOOD FOLLOWING DAY IN AUS. 2 L 7 3 4F 4 F A3WE E2EA 2002030400159 20020304 00159 NM 2002 3 4 EISA20010134 1 20011201 A 5320 STRUCTURE BOEING 727 727223 1384074 NM FUSELAGE CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6815 19490 FOUND CORROSION AT FWD LT CORNER NLG TUNNEL BOX AT STA 294.5 LBL 14. REMOVED DAMAGED SECTION AND INSTALLED REPAIR IAW E O 01-294 REV A. 2 L 7 3 4F A3WE 2002030400160 20020304 00160 NM 2002 3 4 EISA20010142 1 20011212 A 5311 65184158 FRAME BOEING 727 727223 1384074 NM FUSELAGE CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6813 19488 NOSE WHEEL WELL STA 296, RBL 12 UPPER CHORD CORRODED. FOUND ON CPCP CHECK. REMOVED AND REPLACED FRAME IAW B727 SRM 51- 10-1 & 51-30-2. 2 L 7 3 4F A3WE 2002030400161 20020304 00161 NM 2002 3 4 EISA20010143 1 20011212 A 5311 65184157 FRAME BOEING 727 727223 1384074 NM FUSELAGE CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6813 19488 NOSE WHEEL WELL STA 296, LBL 12 UPPER FRAME CORRODED. FOUND ON CPCP CHECK. REMOVED AND REPLACED FRAME IAW B727 SRM 51- 10-1 & 51-30-2. 2 L 7 3 4F A3WE 2002030400164 20020304 00164 NM 2002 3 4 EISA20010146 1 20011212 A 5320 651986219 STRUCTURE BOEING 727 727223 1384074 NM FUSELAGE CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6813 19488 CHORD CORRODED BS 312-348 LBL 14.6, WL 169. FOUND ON CPCP C53-111-03 PAGE 4 N/R CARD 401 WRITTEN. REMOVED CHORD IAW B7 27 SRM 51-30-2, INSTALLED NEW CHORD IAW B727 SRM 51-30-2-51-10-1. 2 L 7 3 4F A3WE 2002030600088 20020306 00088 NM 2002 3 6 BJNA011204 1 20011218 A 3350 CONNECTOR BOEING 737 737282 13844AT NM CABIN LOOSE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 344TM 23044 FORWARD HALF EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. INSPECTED FOUND LOOSE CONNECTIONS AND DIM LIGHTS, RECONNECTED TERMINALS AND RELAMPED IAW CMM 33-50-01. (M) 2 L 7 2 4F RT A16WE 2002030600089 20020306 00089 NM 2002 3 6 BJNA011205 1 20011231 A 3350 362624 LIGHT BOEING 737 737282 13844AT NM CABIN SHORTED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 344TM 23044 FORWARD SECTION EMERGENCY FLOOR LIGHTS INOPERATIVE. INSPECTED, FOUND LIGHT STRIP SHORTED. REPLACED LIGHT STRIP. OPS C HECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2002030700129 20020307 00129 EA 2002 3 7 CA020104007 1 20011128 A 2611 473052 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE CARGO BAY FALSE ACTIVATION W O OTHER N FALSE WARNING AP APPROACH 1 CA (CAN) "SMOKE CARGO" WARNING MESSAGE ON SHORT FINAL TO TORONTO. DRILL CARRIED OUT. BOTH BOTTLES DISCHARGED. BOTH CARGO FI RE EXTINGUISHER BOTTLES, FWD & AFT SMOKE DECTECTORS, BOTH COALESCOR BAGS REPLACED. CARGO COMPT. SMOKE AND FIRE DETECTION SYSTEM TEST CARRIED OUT. NO FAULT FOUND. AIRCRAFT SERVICEABLE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002030700130 20020307 00130 NM 2002 3 7 CA020104008 1 20011125 A 3260 SENSOR BOEING 767 767233 1385113 NM PWA JT9 JT9D7R4D 52054 NE MLG FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) EICAS MSG AIR/GRND DISAGREE DISPLAYED IN FLIGHT AFTER TAKE OFF FROM TORONTO. RIGHT GEAR SYST. 1 TILTED PROX. SENSO R S246 REPLACED. SYSTEM BITE CHECKED SERVICEABLE. 2 L 7 2 4F 4 F RT A1NM E3NE 2002030700160 20020307 00160 SO 2002 3 7 SIMA200202714 1 20011218 A 5320 GUSSET EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 605RR 145059 ABI - LEVEL 2 CORROSION ON CENTER BEAM GUSSET. REPLACED CENTER BEAM GUSSET IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002030800001 20020308 00001 EA 2002 3 8 CA020104013 1 20010121 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE COCKPIT FAILED W O OTHER O OTHER DE DESCENT 1 CA (CAN) CAPTS WINDSHIELD SHATTERED AT TOP OF DESCENT. WINDSHIELD REPLACED AS PER AMM 30-41-01-710. 2 L 7 2 4F 4 F RT A21EA E15NE 2002030800002 20020308 00002 EA 2002 3 8 CA020104014 1 20011206 A 2742 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE HORIZONTAL STAB FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) STAB TRIM FAILED BOTH CHANNELS ON APPROACH INTO BOSTON. EMERGENCY LANDING DECLARED BY FLIGHT CREW. HORIZONTAL STAB CONTROL UNIT (HSTCU, MOTORS CONTROL UNIT (MCU) AND HORIZONTAL STAB ACTUATOR (HSTA)REPLACED. SYSTEM TESTED AS PER AMM. C ONSIDERED SERVICEABLE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002030800090 20020308 00090 EU 2002 3 8 APJ2002F00000 1 20010217 A 7910 5725339201 OIL CAP BRAERO DH125 HS125700A 4230170 EU ALIDSG TFE731 TFE7313AR WP RT ENGINE NOT SEATED E APJA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 11 302PC 257125 P84286 APPROXIMATELY 1.5 HOURS INTO FLIGHT AT 35,000 FT THE OIL PRESSURE GAUGE FLUCTUATED FOR THE RIGHT SIDE ENGINE AND PROCEED ED TO INDICATE MINIMUM PRESSURE. AS A PRECAUTION, THE PIC SHUTDOWN THE RIGHT SIDE ENGINE WHEN THE OIL PRESSURE REACHED 25 PSI (MINIMUM PRESSURE). UPON LANDING IT WAS DETERMINED THAT THE OIL FILLER CAP WAS IMPROPERLY SEATED CAUSING LOSS OF OIL AND PRESSURE. THE RIGHT ENGINE WAS CLEANED AND SERVICED WITH THREE QUARTS OF OIL, PERFORMED SEVERAL ENGINE RUNUPS. NO FURTHER LEAKS AND OIL PRESSURE GAUGE INDICATED PROPER. 2 L 7 2 4F 4 F A3EU E6WE 2002030800106 20020308 00106 NM 2002 3 8 2002F00156 1 20011219 A 5310 SHEAR TIE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 SHEAR TIE IS CRACKED AT STATION 727A STRINGER 3R, 4R AND 5R. (M) 2 L 7 2 4F A16WE 2002030800109 20020308 00109 NM 2002 3 8 2002F00159 1 20011219 A 5310 SHEAR TIE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND SHEAR TIE IS CRACKED AT STATION 787 STRINGER 6R. (M) 2 L 7 2 4F A16WE 2002030800111 20020308 00111 NM 2002 3 8 2002F00161 1 20011217 A 5347 SEAT TRACK BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND SEAT TRACK CORRODED AT STATION 363 RBL 22.5. (M) 2 L 7 2 4F A16WE 2002030800112 20020308 00112 NM 2002 3 8 2002F00162 1 20011217 A 5320 FLOOR SUPPORT BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND COCKPIT FLOOR LEFT SIDE F/S 227 WL 212 LBL 30 HAS CRACK IN FLOOR SUPPORT FORMER. (M) 2 L 7 2 4F A16WE 2002030800113 20020308 00113 NM 2002 3 8 2002F00163 1 20011217 A 5320 WEB BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND FORWARD PIT BS 460 LBL 11 LIGHTENING HOLE IS CRACKED. (M) 2 L 7 2 4F A16WE 2002030800114 20020308 00114 NM 2002 3 8 2002F00164 1 20011217 A 5347 SEAT TRACK BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND SEAT TRACK AT STATION 400 LBL 43.5 CORRODED. (M) 2 L 7 2 4F A16WE 2002030800115 20020308 00115 NM 2002 3 8 2002F00165 1 20011216 A 5531 RIB BOEING 737 7372H4 138448C NM VERTICAL STAB CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND VERTICAL STABILIZER LEADING EDGE PANEL NR 9545 HAS A CRACKED RIB AT 94 INCHES FROM LOWER END OF 10TH RIB. (M) 2 L 7 2 4F A16WE 2002030800116 20020308 00116 NM 2002 3 8 2002F00166 1 20011216 A 5320 STIFFENER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND VERTICAL STIFFENER IS CRACKED AT LBL 1, BS 947.5 AT UPPER END. (M) 2 L 7 2 4F A16WE 2002030800117 20020308 00117 NM 2002 3 8 2002F00167 1 20011216 A 5320 ANGLE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND FLOORBEAM LOWER SUPPORT ANGLE CRACKED AT BS 727 LBL 24. (M) 2 L 7 2 4F A16WE 2002030800118 20020308 00118 NM 2002 3 8 2002F00168 1 20011216 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND CABIN UPPER FLOORBEAM CHORD AT BS 312 LBL 1 HAS CORROSION. (M) 2 L 7 2 4F A16WE 2002030800119 20020308 00119 NM 2002 3 8 2002F00169 1 20011216 A 5531 RIB BOEING 737 7372H4 138448C NM VERTICAL STAB CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND VERTICAL STAB LEADING EDGE PANEL NR 9545 HAS CRACKED RIB AT 85 INCH FROM LOWER END 9TH RIB. (M) 2 L 7 2 4F A16WE 2002030800120 20020308 00120 NM 2002 3 8 2002F00170 1 20011215 A 5320 STRINGER CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND FORWARD PIT STATION 380 STRINGER 19L ATTACH CLIP IS CRACKED. (M) 2 L 7 2 4F A16WE 2002030800121 20020308 00121 NM 2002 3 8 2002F00171 1 20011215 A 5320 ATTACH ANGLE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND RADAR MOUNT ATTACH ANGLE HAS A .800 INCH LONG CRACK AT LBL 5.7 WL 211 BS 178. (M) 2 L 7 2 4F A16WE 2002030800122 20020308 00122 NM 2002 3 8 2002F00172 1 20011215 A 5714 ANGLE BOEING 737 7372H4 138448C NM CENTER WING CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND CENTERWING FRONT SPAR SUPPORT ANGLE IS CRACKED AT BS 538 RBL 8. (M) 2 L 7 2 4F A16WE 2002030800123 20020308 00123 NM 2002 3 8 2002F00173 1 20011215 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND FUSELAGE SKIN AT FLIGHT STATION 800 STRINGER 22L CRACKED APPROXIMATELY 5 INCH LONG. (M) 2 L 7 2 4F A16WE 2002030800124 20020308 00124 NM 2002 3 8 2002F00174 1 20011214 A 5754 SLAT BOEING 737 7372H4 138448C NM LT WING DELAMINATED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND LEFT WING NUMBER TWO SLAT IS DELAMINATED IN SEVERAL AREAS. (M) 2 L 7 2 4F A16WE 2002030800125 20020308 00125 NM 2002 3 8 2002F00175 1 20011214 A 5311 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND LEFT FORWARD PIT STATION 420 ABOVE STRINGER 26 FRAME HAS A CRACK. (M) 2 L 7 2 4F A16WE 2002031100073 20020311 00073 WP 2002 3 11 AT0200012 1 20011011 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 817AT 47323 FUSELAGE EXTERNAL SKIN HAS THREE (3) CRACKS AROUND RIVET HEADS AT STA 164 APPROX AND LONGERON 4 LEFT. CUT OUT DAMAGED A REA. NDT VERIFIED AFTER CUT OUT IAW NDT SRM PART 6-00-01, NO DISCREPANCIES NOTED. MADE SKIN REPAIR AND FINGER DOUBLER A ND INSTALLED REPAIR PER DC-9 SRM 53-04 FIG 1213. 2 L 7 2 4F A6WE 2002031100075 20020311 00075 WP 2002 3 11 AT0200013 1 20011010 A 5320 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 817AT 47323 FORWARD GALLEY AREA AT FS 200/LBL 31 - LBL 40, FOUND CRACKED TO FLOOR WEB ON (2) EXISTING DOUBLER REPAIRS. REMOVED EXIS TING DOUBLER AS PER DC-9 SRM 51-30-2. INSTALLED NEW DOUBLER PER DC-9 SRM 53-01-09. 2 L 7 2 4F A6WE 2002031100078 20020311 00078 WP 2002 3 11 AT0200014 1 20011024 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 AFT SKIN OF FUSELAGE BUTT SPLICER HAS CRACK BETWEEN LONG 18L AND 19L STA 996. CUT OUT DAMAGED AREA. INSPECTED IAW DC9/ MD80 NDT MM 7-1 FIG 8. NO CRACK INDICATIONS NOTED. INSTALLED DOUBLER REPAIR AT AFT SKIN FUSELAGE BUTT SPLICE PER DC9 S RM 53-04 FIG 18. 2 L 7 2 4F A6WE 2002031100081 20020311 00081 WP 2002 3 11 AT0200015 1 20011022 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 FWD PASSENGER DOOR TOP, FWD DOOR JAMB CORNER CRACKED, IND AT 2 PLACES. OUTER/INNER SKIN, INNER CRACK IS ABOUT 1 INCH LO NG. TRIMMED OUT CRACK AREA. INSTALLED REPAIR AT FWD PASS DOOR IAW BOEING MESSAGE CQT-ORL-01-005521. LEAK CK GOOD IAW DC9 MM 21-31-0. 2 L 7 2 4F A6WE 2002031100082 20020311 00082 WP 2002 3 11 AT0200016 1 20011107 A 5313 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 830AT 47723 LONG 5L CRACKED AT STA 699. 2 L 7 2 4F A6WE 2002031100083 20020311 00083 WP 2002 3 11 AT0200017 1 20011107 A 5313 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 830AT 47723 LONG 6R CRACKED AT STA 617. 2 L 7 2 4F A6WE 2002031100084 20020311 00084 WP 2002 3 11 AT0200018 1 20011107 A 5313 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 830AT 47723 LONG 5R CRACKED AT STA 617. 2 L 7 2 4F A6WE 2002031100088 20020311 00088 WP 2002 3 11 AT0200023 1 20011129 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 COCKPIT FUSELAGE UPPER NOSE SKIN HAS 2 CRACKS EMANATING FROM RIVET HOLES AT FS 69.5, LBL 17. VERIFIED WITH HFEC. 2 L 7 2 4F A6WE 2002031100089 20020311 00089 WP 2002 3 11 AT0200024 1 20011130 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 FORWARD CARGO COMPARTMENT FLOOR SUPPORT ANGLE CRACKED SEVERAL PLACES AT FRAME STA 351 BETWEEN LONG 29L AND LONG 28R. 2 L 7 2 4F A6WE 2002031100090 20020311 00090 WP 2002 3 11 AT0200025 1 20011130 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 AFT CARGO COMPARTMENT FLOOR SUPPORT ANGLE CRACKED AT FRAME STA 794 AND LONG 29L. 2 L 7 2 4F A6WE 2002031100091 20020311 00091 WP 2002 3 11 AT0200026 1 20011130 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 FORWARD CARGO COMPARTMENT FLOOR SUPPORT ANGLE CRACKED FRAME STA 389 BETWEEN LONG 30 AND 29R. 2 L 7 2 4F A6WE 2002031100095 20020311 00095 WP 2002 3 11 AT0200027 1 20011130 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 FORWARD CARGO COMPARTMENT FLOOR SUPPORT ANGLE CRACKED 2 PLACES AT FRAME STA 427 OVER LONG 29L. 2 L 7 2 4F A6WE 2002031100104 20020311 00104 NE 2002 3 11 2002F00105 1 20011206 A 6320 643520026012 SUPPORT SKRSKY SKRSKY S64 S64F 8142610 NE M/R GEARBOX CRACKED I JYDM K NONE O OTHER IN INSP/MAINT 1 NM 09 157AC 1296 62006 64065 3 CRACKS WERE FOUND IN LOWER SUPPORT OF MAIN ROTOR GEARBOX. 2 G 7 2 4U H6EA 2002031100113 20020311 00113 SW 2002 3 11 AC22002F00000 1 20011124 A 7500 23056648 TUBE BELL 430 430 1182150 SW ALLSN 250C 250C* GL BLEED AIR TUBE CHAFED E AC2A K NONE O OTHER IN INSP/MAINT 1 SW 03 430CV 204 49072 TUBE ASSEMBLY, ENGINE COWL ASSY, FORWARD HINGE IS RUBBING ON BLEED AIR TUBE WHEN COWLING IS OPENED. REPLACED TUBE : P ROBLEM WILL CONTINUE DUE TO DESIGN OF COWLING HINGE. 1 G 7 2 3U 3 U RT H9SW E4CE 2002031100114 20020311 00114 SW 2002 3 11 AC22002F00001 1 20011202 A 7810 206064300005 EXHAUST HEADER BELL 206 206L3 1182108 SW ALLSN 250C 250C20 03013 GL ENGINE CRACKED E AC2A K NONE O OTHER IN INSP/MAINT 1 SW 03 715CC 204 51380 EXHAUST ASSEMBLY CRACKED. REPLACED WITH NEW EXHAUST DUCT. 1 G 7 1 3U 3 U H2SW E4CE 2002031100116 20020311 00116 SW 2002 3 11 AC2A0000297 1 20011207 A 6730 065001620200 SERVO BELL 430 430 1182150 SW ALLSN 250C 250C* GL MAIN ROTOR FAILED E AC2A K NONE O OTHER IN INSP/MAINT 1 SW 03 430CV 1 49072 YAW SERVO, WHEN FD IS COUPLED IN HDG AND ALT THE AIRCRAFT GOES INTO A CLIMBING RIGHT TURN WITH FULL LEFT PEDAL APPLIED. REPLACED WITH NEW YAW SERVO. 1 G 7 2 3U 3 U RT H9SW E4CE 2002031100117 20020311 00117 SW 2002 3 11 AC2A0000298 1 20011212 A 3040 222325001028 ARM BELL 430 430 1182150 SW ALLSN 250C 250C* GL WINDSHIELD WIPER CORRODED E AC2A K NONE O OTHER IN INSP/MAINT 1 SW 03 430CV 953 49072 GUIDE ARM ASSEMBLY, LOWER MOUNTING POINT BROKEN. THE MATERIAL THAT THIS PART IS MADE OF IS VERY SUSEPTIBLE TO CORROSION . CORROSION CAUSED THIS PART TO FAIL. UPPER ROD END CORRODED VERY EASILY ALSO. REPLACED WITH NEW PART. 1 G 7 2 3U 3 U RT H9SW E4CE 2002031100118 20020311 00118 SW 2002 3 11 AC2A0000299 1 20011127 A 6410 222312753103 BEARING BELL 430 430 1182150 SW ALLSN 250C 250C* GL T/R BLADE CRACKED E AC2A K NONE O OTHER IN INSP/MAINT 1 SW 03 430CV 599 49072 TAIL ROTOR BLADE BEARINGS WERE CRACKED. REMOVED AND REPLACED TWO BEARINGS. 1 G 7 2 3U 3 U RT H9SW E4CE 2002031100119 20020311 00119 NE 2002 3 11 AC2A0000301 1 20011227 A 7922 28E252 THERMOSTAT SKRSKY S76 S76 8143010 NE ENGINE OIL INOPERATIVE E AC2A K NONE O OTHER IN INSP/MAINT 1 SO 03 5401G 18256 760137 THERMOSTAT, HIGH ENGINE OIL TEMPERATURE IN FLIGHT. REMOVED AND REPLACED THERMOSTAT. CURED PROBLEM. 1 G 7 2 3U H1NE 2002031100120 20020311 00120 SW 2002 3 11 AC2A0000302 1 20011127 A 6420 222312753103 BEARING BELL 430 430 1182150 SW TAIL ROTOR FAILED E AC2A K NONE O OTHER IN INSP/MAINT 1 SW 03 430CV 281 49072 TAIL ROTOR BEARING, REPLACE BEARINGS ON TAIL ROTOR. 1 G 7 2 3U RT H9SW 2002031100121 20020311 00121 SW 2002 3 11 AC2A0000303 1 20011220 A 6410 206310105101 BEARING BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL TAIL ROTOR BLADE WORN E AC2A K NONE O OTHER IN INSP/MAINT 1 SW 03 71319 8280 4112 BEARINGS WERE WORN BEYOND LIMIT. REPLACED WITH NEW BEARINGS. 1 G 7 1 3U 3 U H2SW E4CE 2002031100122 20020311 00122 SW 2002 3 11 AC2A0000304 1 20011220 A 6420 206016201131 BEARING BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL TAIL ROTOR WORN E AC2A K NONE O OTHER IN INSP/MAINT 1 SW 03 71319 787 4112 TO REPLACE BEARINGS IN TAIL ROTOR AT OUT FACILITY. 1 G 7 1 3U 3 U H2SW E4CE 2002031100123 20020311 00123 SW 2002 3 11 AC2A0000305 1 20011220 A 6420 206010733003 SLEEVE BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL TAIL ROTOR WORN E AC2A K NONE O OTHER IN INSP/MAINT 1 SW 03 71319 7803 4112 SLEEVES WERE WORN IN TAIL ROTOR ASSEMBLY. REPLACED WITH NEW SLEEVES. 1 G 7 1 3U 3 U H2SW E4CE 2002031100135 20020311 00135 SW 2002 3 11 ALG2002F00017 1 20010930 A 6320 6895007 BEARING ALLSN BELL 407 407 1182206 SW ALLSN 250C 250C47B GL M/R GEARBOX MAKING METAL A ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 577AL 2105 CAG47167 53247 CAE847251 METAL WAS FOUND ON CHIP PLUGS, ENGINE AND GEARBOX DISASSEMBLED FOR INSPECTION. FOUND CAUSE FOR METAL DUE TO INNER RACE GALLING ON T/M JOURNAL BEARING, CAUSING METAL CONTAMINATION THROUGHOUT GEARBOX. 1 G 7 1 3U 3 U O H2SW E1GL 2002031100140 20020311 00140 NE 2002 3 11 JYD2002F00000 1 20011206 A 6210 641520504102 SPAR SKRSKY SKRSKY S64 S64E 8142604 NE PWA JFTD12 JFTD12A4A 52047 NE M/R BLADE CRACKED A JYDR K NONE O OTHER IN INSP/MAINT 1 NM 09 223AC 4372 64M65325910 64086 CRACK WAS FOUND ON THE TIP END OF MAIN ROTOR BLADE SPAR (PN 641520504102/ SN 64-65325910). DURING POST FLIGHT INSPECTIO N, FIELD CREW VISUALLY DETECTED A CRACK INDICATION ON TOP SIDE OF SPAR. TOTAL CRACK LENGTH IS APPROX. 2 INCHES LONG WI TH 1.5 INCHES EXTENDING TOWARDS TRAILING EDGE FROM RETENTION BLOCK RIVET HOLE AND ALSO EXTENDING .5 INCHES TOWARDS LEADI NG EDGE FROM SAME RIVET HOLE. RIVET PN MS20426AD8 ALSO SHOWS SMALL CRACK APPROX. .100 INCHES ALTHOUGH NOT IN LINE WITH SPAR CRACK. THE RIVET HOLE (.250 INCHES DIA) WHERE CRACKS ARE PROPAGATING FROM IS THE RIVET HOLE LOCATED APPROX. 24 INC HES FROM TIP END IN THE TRAILING EDGE SIDE OF A ROW OF 2 RIVETS AND LOCATED APPROX. 3 INCHES FROM FORWARD RETENTION BLOC 2 G 7 2 4U 4 U H4EA E15EA 2002031100141 20020311 00141 NE 2002 3 11 JYD2002F00001 1 20011206 A 6320 643520026012 SUPPORT SKRSKY S64 S64F 8142610 NE M/R GEARBOX CRACKED A JYDR K NONE O OTHER IN INSP/MAINT 1 NM 09 157AC 1296 64065 3 CRACKS WERE FOUND IN LWR SUPPT E MODEL MN GEARBOX WAS REMOVED FROM SERVICE FOR O/H IN1995. IN DECEMBER OF 2001, SUPPT WAS MACHINED TO REMOVE CORROSION. AFTER MACHINING, CRACK WAS VISUALLY DETECTED IN MOUNTING LUG HOLE NR 4 AS INSTALLED ON AC. FLUORESCENT PENETRANT INSP VERIFIED THIS WHILE DETECTING 2 ADDITIONAL CRACKS IN MOUNTING LUG HOLE NR 1 AND NR 4, FOR A TOTAL OF 3 CRACKS. LONGEST CRACK WAS .750 INCH STARTING FROM BOTTOM (MATING) SURFACE EXTENDING AT A 45 DEGREE AN GLE THROUGH 45 DEGREE CHAMFER AND UP INTO WALL OF.9730 DIA MOUNTING HOLE. NOTE: 12 MOUNTING HOLES EXIST. HOLES ARE FOR BOLTS WHICH ATTACH THE MN GEARBOX TO AIRFRAME. NO PROBABLE CAUSE DETERMINED AT THIS TIME. 2 G 7 2 4U H6EA 2002031100195 20020311 00195 NM 2002 3 11 WRLA200120 1 20011120 A 2710 4083935902 ACTUATOR DOUG MD11 MD11 3023602 NM AILERON FAILED A WRLA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 EA 27 277WA 48743 AIRCRAFT HAS AILERON CONTROL PROBLEM. AIRCRAFT RETURNED TO SNN WERE THE AILERON SYSTEM WAS CHECKED. REMOVED AND REPLAC ED AILERON DEFLECTION ACTUATOR OUTBOARD. FOLLOW PROCEDURE IAW MM 27-43-00 RTS TEST FCC 1/FCC 2 ALL PASSED. OPS CHECK M M. NO FAULTS. (M) 2 L 7 3 4F RT A22WE 2002031100196 20020311 00196 NM 2002 3 11 WRLA200121 1 20011121 A 2710 AILERON DOUG MD11 MD11 3023602 NM WING MALFUNCTIONED A WRLA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 EA 27 277WA 48743 AILERON DEFLECT DISAGREE LEVEL 2 ALERT, AIRCRAFT RETURNED TO ATL. RAN FLAPS THROUGH 28 DEGREES. NO AILERON DEFLECTION NOTED. (M) 2 L 7 3 4F RT A22WE 2002031100211 20020311 00211 NM 2002 3 11 2002F00196 1 20011231 A 5320 SUPPORT BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 LEFT W/W FAIRING SUPPORT PLATE CRACKED AT FS 661. (M) 2 L 7 2 4F A16WE 2002031100212 20020311 00212 NM 2002 3 11 2002F00197 1 20011213 A 5311 FRAME BOEING 737 7372H4 138448C NM FUSELAGE GOUGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FRAME HAS TWO GOUGES AT BS 747 BETWEEN STRINGER 23L AND STRINGER 22L. (M) 2 L 7 2 4F A16WE 2002031100213 20020311 00213 NM 2002 3 11 2002F00198 1 20011213 A 5320 STRINGER CLIP BOEING 737 7372H4 138448C NM FUSELAGE DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND STRINGER CLIP AT STATION 727B S22L IS DENTED. (M) 2 L 7 2 4F A16WE 2002031100214 20020311 00214 NM 2002 3 11 2002F00200 1 20011213 A 5320 STRINGER CLIP BOEING 737 7372H4 138448C NM FUSELAGE DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND STRINGER CLIP DENTED AND GOUGED AT STATION 747 STRINGER 21L. (M) 2 L 7 2 4F A16WE 2002031100215 20020311 00215 NM 2002 3 11 2002F00113 1 20010111 A 2910 HYDRAULIC SYSTEM BOEING 727 72721 1384003 NM A SYSTEM LEAKING A RYNA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 07 356QS 19258 LOST 'A' SYSTEM HYDRAULIC FLUID QUANTITY IN FLIGHT INTO RDU. COMPLIED WITH FLIGHT OPERATION MANUAL PROCEDURE CHECKLIST. AIRCRAFT LANDED WITHOUT INCIDENT. (M) 2 L 7 3 4F A3WE 2002031200230 20020312 00230 NM 2002 3 12 AALA20011823 1 20010927 A 2121 5051 COOLING FAN BOEING 757 757223 1384957 NM E/E BAY FAILED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 609AA 27447 TPA - FLT 2199 - AT FL390 IN CRUISE STRONG ELECTRICAL ODOR OCCURRED IN COCKPIT AND CABIN. DECLARED AN EMERGENCY DIVERTE D TO TAMPA. ACCOMPLISHED APPROPRIATE EMERGENCY PROCEDURES AT FIRST SIGN OF SMELL. LANDED NORMALLY IN TPA. REPLACED NR 2 AFT EQUIP COOLING FAN. OPS CHECK NORMAL. 2 L 7 2 4F RT A2NM 2002031200231 20020312 00231 NM 2002 3 12 AALA20011824 1 20010926 A 3230 5532514 SOLENOID BOEING 757 757223 1384957 NM MLG DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 609AA 27447 DFW - FLT 2030 - EN ROUTE DFW-GSO, AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. RETURNED DFW AND LANDED WITHOUT FURTH ER INCIDENT. REPLACED ANTI-RETRACTION SOLENOIDS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002031200232 20020312 00232 WP 2002 3 12 AALA20012056 1 20011111 A 2120 ODOR DOUG DC9 DC982 3022082 WP CABIN DETECTED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 472AA 49647 SJC - FLT 2464 - EN ROUTE SJC-DFW, DETECTED ELECTRICAL BURNING SMELL IN CABIN AND COCKPIT. RETURNED SJC AND LANDED WITH OUT FURTHER INCIDENT. RAN BOTH ENGINES. NO ODOR OR SMOKE NOTED. REPLACED COALESCER BAGS AS A PRECAUTION. SYSTEM GROU ND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002031200233 20020312 00233 WP 2002 3 12 AALA20012061 1 20011122 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP AFT AIRSTAIRS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7532A 49924 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS INOPERATIVE. SECURED EMERGENCY EXIT LIGHT CON NECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002031300064 20020313 00064 CE 2002 3 13 BLI2002F00000 1 20010916 A 7921 646685 OIL COOLER CESSNA 421 421B 2076014 CE CONT O520 GTSIO520* 17032 SO LT ENGINE LEAKING A BLIA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 17 208V 1469 421B0866 22429972H OIL LEAK DISCOVERED AFTER ARRIVAL, OIL COOLER, GROUNDED AIRCRAFT, CALLED MAINTENANCE. ANOTHER AIRCRAFT PICKED UP PAX. MAINTENANCE ARRANGED FOR MECHANIC TO TROUBLESHOOT AND REPAIR. LEAK CAUSED BY GASKET BETWEEN COOLER AND ENGINE CASE. G ASKET REPLACED, ENGINE LEAK CHECKED GOOD. AIRCRAFT RETURNED. 1 L 7 2 3O 3 O A7CE E7CE 2002031300068 20020313 00068 EA 2002 3 13 CVU2002F00000 2 20011215 A 7414 BL3493204 MAGNETO BEECH 80 65B80 1152812 CE LYC O435 TVO435* 41516 EA ENGINE DAMAGED E CVUA K NONE O OTHER IN INSP/MAINT 1 WP 13 44MA 9 9 LD412 L155954A PRIMARY COIN HOLD DOWN RETAINERS LOOSE WITHIN MAGNETO CASE. THE LOOSE RETAINERS, IN TURN, GOT CAUGHT IN THE TIMING WHEE L/GEAR AND CHEWED UP SEVERAL TEETH. PROBABLE CAUSE- THE RETAINERS WERE NOT INSTALLED PROPERLY. FORTUNATELY THE DAMAGE WAS AT THE R20 TIMING MARK, WHERE WE WERE ABLE TO SEE THE DAMAGE DURING A 10 HOUR (ENGINE BREAK IN) VISUAL INSPECTION. 1 L 7 2 3O 3 O 3A20 1E13 2002031300133 20020313 00133 EU 2002 3 13 FE62002F00001 1 20010606 A 2710 EM40693 ACTUATOR PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE AILERON TRIM RESTRICTED B FE6R K NONE O OTHER IN INSP/MAINT 1 NM 11 660NR 294 356 PCEPRO217 THE AILERON TRIM TAB LINEAR ACTUATOR ELECTRICAL HARNESS WAS TIED WITHOUT ENOUGH SERVICE LOOP WHICH CAUSED RESTRICTED AIL ERON MOVEMENT. THE LINEAR ACTUATOR ELECTRICAL WIRE HARNESS WAS THUS PULLED FROM THE ACTUATOR. THE ACTUATOR WAS STILL FUNCTIONAL BUT WAS REPLACED UNDER WARRANTY. THE AIRCRAFT AND DAMAGED ACTUATOR HAVE 294.7 HOURS TOTAL TIME IN SERVICE. THIS DEFECT WAS DISCOVERED DURING A SCHEDULED INSPECTION EVENT AND IS A RESULT OF THE INSTALLATION TECHNIQUE RATHER THAN PART DESIGN OR OTHER CONSIDERATION. 1 L 7 1 3T 4 T RT A78EU E26NE 2002031300144 20020313 00144 SO 2002 3 13 FWRA2001004 1 20010817 A 5230 MS203922C35 PIN PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA CARGO DOOR WORN A FWRA K NONE O OTHER IN INSP/MAINT 1 AL 01 27501 317852028 REINSTALLING COVER ON NOSE BAGGAGE DOOR LATCH ASSEMBLY, MECHANIC TOOK ONE LAST LOOK AT LATCHING MECHANISM AND SAW AN EXC ESSIVELY WORN CLEVIS PIN. IT WAS DETERMINED THAT IF THIS PART FAILED, THE NOSE BAGGAGE DOOR COULD COME OPEN IN FLIGHT . THE WORN PART IS THE PIN SECURING THE LATCHES CONNECTING TUBE ASSEMBLY TO DOOR HANDLE. THERE ARE THREE SPRINGS ATTAC HING THE TUBE ASSEMBLY TO THE DOOR STRUCTURE AND THE DOOR HANDLE, IT IS NOT CLEAR HOW THEY MAY AFFECT THE LATCHES SECURI TY. IF THE PIN BROKE, ESPECIALLY IF IT HAPPENED WHILE LOCKING THE DOOR, THE LATCHES MAY NOT HAVE BEEN FULLY ENGAGED, O R THEY MAY VIBRATE TO THE UNLOCKED POSITION. MOST CERTAINLY IF THE PIN BROKE THE DOOR SECURITY WOULD BE COMPROMISED. 1 L 7 2 3O 3 O A20SO E14EA 2002031300149 20020313 00149 WP 2002 3 13 AT0200030 1 20010823 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP MAIN CABIN A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 828AT 47274 CABIN SEAT TRACK CORRODED BETWEEN F.S. 210 TO F.S. 230, RBL 22.0. CORRECTIVE ACTION: REMOVED AND REPLACED SECTION O F CABIN SEAT TRACK BETWEEN F.S. 194 TO F.S. 284, RBL 22.0 PER DC-9 SRM 53-05 FIGURE 4F. 2 L 7 2 4F A6WE 2002031300154 20020313 00154 SW 2002 3 13 LAO2002F00000 1 20010401 A 5711 5271 SPAR BBAVIA 7 7GCBC 1220601 SW RT WING CRACKED D LAOA K NONE O OTHER IN INSP/MAINT 1 AL 05 5151X 2623 145 DURING AN ANNUAL INSPECTION AD (WING SPAR CRACKING) WAS COMPLIED WITH IAW SB PER AD. A LONGITUDINAL CRACK WAS FOUND IN THE FRONT LEFT HAND WING SPAR THAT STARTED NEAR THE LIFT STRUT ATTACH POINT AND RAN INBOARD APPROXIMATELY 36 INCHES TOWA RDS THE WING ROOT. 1 H 7 1 3O NC A759 2002031300160 20020313 00160 NM 2002 3 13 2002F00218 1 20011127 A 5210 85210003001 STRUT DHAV DHC8 DHC8202 2809007 NM PAX DOOR DEFECTIVE A MASA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 449YV 449 FLT NR 6253 - ON ARRIVAL IN DRO, THE CREW COULD ONLY GET THE PASSENGER DOOR TO OPEN ONE-THIRD OF THE WAY. MAINTENANCE R EPLACED BOTH STRUTS. OPS CHECKS GOOD. (M) 2 H 7 2 4T RT A13NM 2002031300161 20020313 00161 NM 2002 3 13 2002F00219 1 20011217 A 2131 21178044 CONTROLLER DHAV DHC8 DHC8202 2809007 NM CABIN PRESSURE FAILED A MASA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 07 447YV 447 FLT 6217 - IN FLIGHT AT 17,000 FEET, THE CREW REPORTED A CABIN PRESSURE WARNING MESSAGE. THE AIRCRAFT DESCENDED TO 10,0 00 AND LANDED SAFELY IN PHX WHERE MAINTENANCE REPLACED THE PRESSURIZATION CONTROLLER. OPS CHECKED GOOD AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 2002031300182 20020313 00182 2002 3 13 USAASA02009 4 20010116 A 2565 CABLE FITTING AIRBUS A319 A319112 3930323 EU SLIDE BOTTLE BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 747UW 4615 1301 DCA - THE LEFT OVERWING SLIDE INFLATION BOTTLE SIDE CABLE END WAS FOUND BROKEN. MAINTENANCE INSTALLED A NEW INFLATION B OTTLE ASSEMBLY AND CABLE END. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2002031300203 20020313 00203 NM 2002 3 13 UPS02237505 1 20010102 A 5744 SUPPORT FITTING BOEING 727 727185C 138406N NM LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI LT WING SUPPORT BRACKET FOR NR 3 FLAP TRACK FWD END HAS PITTING CORROSION ON RT FACE OF LUG. 2 L 7 3 4F A3WE 2002031300205 20020313 00205 NM 2002 3 13 UPS02237510 1 20011219 A 5720 66177611 BUSHING BOEING 727 727185C 138406N NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI, RT WING REAR TERMINAL FORGING FWD BUSHING IS CORRODED. RETAINER REPLACED IAW MM 57-41-11, BUSHING REPLACED IAW OHM20-50-03. 2 L 7 3 4F A3WE 2002031300206 20020313 00206 NM 2002 3 13 UPS02237511 1 20011221 A 5753 65192067 FLAP TRACK BOEING 727 727185C 138406N NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+S,I NR 3 FLAP TRACK PITTING CORROSION ON AUX SPAR ATTACH PAD. 2 L 7 3 4F A3WE 2002031400005 20020314 00005 EU 2002 3 14 BAQ2002F00000 1 20011010 A 7921 1090445509103 BELT AGUSTA A109 A109E 0260119 EU NR 1 OIL COOLER BROKEN E BAQA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 03 12UW 45 11074 STRUCTURAL CORD FAILURE OF NR 1 ENGINE OIL COOLER BELT CAUSED ENGINE OIL HOT WARNING LIGHT TO COME ON AND OIL TEMPERATUR E READING SOON CLIMBED HIGH INTO THE YELLOW. ENGINE WAS SHUTDOWN IN FLIGHT. 1 G 7 2 3U RT H7EU 2002031400129 20020314 00129 NM 2002 3 14 2002F00256 1 20011218 A 3350 86210066 BATTERY PACK BOEING 737 7373Y0 1384671 NM CABIN DISCHARGED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 373PA 23749 ATL - FOUND EMERGENCY LIGHT INOPERATIVE AT ROW 16 FLOOR PATH. REPLACED BATTERY PACK PER MM 33-51-41. OPERATION CHECKED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002031400131 20020314 00131 NM 2002 3 14 2002F00257 1 20011212 A 5710 STRUCTURE BOEING 737 737400 138449A NM LT WING DAMAGED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 37NY 23976 LEFT WING TIP DAMAGED AT YYZ. REMOVED AND REPLACED LEFT WING TIP FORWARD AND AFT ASSEMBLY (P/N 65-73719-505A AND 657371 9-369) PER 8737-400 M/M 57-21-11. (M) 2 L 7 2 4F RT A16WE 2002031400132 20020314 00132 NM 2002 3 14 2002F00258 1 20011207 A 3350 9721055 LIGHT BOEING 737 737400 138449A NM CABIN INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 37NY 23976 NR 3 SEAT FLOOR PROXIMITY, ESCAPE PATH LIGHTING, FAILED TO TEST. REMOVED AND REPLACED BATTERY PACK, OPS CHECK OK. (M) 2 L 7 2 4F RT A16WE 2002031400133 20020314 00133 NM 2002 3 14 2002F00259 1 20011206 A 2560 P2070003001 FLASHLIGHT BOEING 737 737242 1384477 NM AFT CABIN INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 159PL 21186 AFT EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY, OPS CHECKED OK. (M) 2 L 7 2 4F A16WE 2002031400134 20020314 00134 NM 2002 3 14 2002F00260 1 20011203 A 3230 2732511 CONTROL CABLE BOEING 737 7373Y0 1384671 NM RT MLG OUT OF ADJUST A PIDA O OTHER J WARNING INDICATION TO TAKEOFF 1 SO 05 373PA 23749 OVERRIDE MUST BE USED TO RAISE GEAR ON TAKEOFF. ADJUSTED GROUND SPOILER INTERLOCK VALVE CABLE. OPS CHECK OK. (M) 2 L 7 2 4F RT A16WE 2002031400136 20020314 00136 NM 2002 3 14 2002F00201 1 20011212 A 7500 DUCT BOEING 737 7372H4 138448C NM LT ENGINE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 NR 1 ENGINE LEFT SIDE BLEED AIR DUCT ATTACH BRACKET CRACKED. (M) 2 L 7 2 4F A16WE 2002031400160 20020314 00160 NM 2002 3 14 UPS02237529 1 20011217 A 5320 65C132495 FITTING BOEING 727 727185C 138406N NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI VERTICAL FLANGE OF LT 740 FITTING AT I/B END HAS CORROSION. LT 740 FITTING REPLACED IAW UPS EO B72 7-5310-7477E APPB AND DWG 65C 13724. 2 L 7 3 4F A3WE 2002031400165 20020314 00165 NM 2002 3 14 UPS02237534 1 20011218 A 7120 MOUNT BOEING 727 727185C 138406N NM NR 1 ENGINE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C=SI NR 1 ENGINE FWD TRUNNION MOUNT AFT OUTBOARD HOLE HAS PITTING CORROSION IN BORE OF HOLE. 2 L 7 3 4F A3WE 2002031400167 20020314 00167 NM 2002 3 14 UPS02237536 1 20011217 A 5311 FRAME BOEING 727 727185C 138406N NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI SUSPECT CRACK IN MLG WW STRUCTURE AT BS 910 FWD FLANGE BELOW MLG CEILING. REPAIRED IAW EO B727-531 0-1896B. 2 L 7 3 4F A3WE 2002031400170 20020314 00170 NM 2002 3 14 UPS02237543 1 20011218 A 5711 SPAR BOEING 727 727185C 138406N NM CENTER WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI WING CENTER SECTION FRONT SPAR UPPER CHORD HAS CORROSION AT RT END OF CHORD AT RBL 55 APPROX. FOUN D TO BE EXFOLIATED. 2 L 7 3 4F A3WE 2002031400171 20020314 00171 NM 2002 3 14 UPS02237545 1 20011220 A 2710 CRANKSHAFT BOEING 727 727185C 138406N NM AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C AILERON PCU INPUT CRANK IN LT WHEEL WELL IS BADLY CORRODED AROUND PIVOT BOLT. PCU INPUT CRANK REPLACE D IAW OHM 27-40-00 & OHM 29-00-00. 2 L 7 3 4F A3WE 2002031500002 20020315 00002 NM 2002 3 15 2002F00263 1 20011130 A 3350 1060091101 LIGHT BOEING 737 737242 1384477 NM CABIN INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 159PL 21186 R2 DOOR OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT PACK, OPS CHECK OK. (M) 2 L 7 2 4F A16WE 2002031500003 20020315 00003 NM 2002 3 15 2002F00264 1 20011127 A 3200 CONTROL CABLE BOEING 737 7373Y0 1384671 NM RT MLG LACK OF LUBE A PIDA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 05 373PA 23749 LANDING GEAR OVERRIDE SWITCH USED TO RETRACT GEAR AFTER TAKEOFF. LUBED TELEFLEX CABLE, OPS CHECKS GOOD. (M) 2 L 7 2 4F RT A16WE 2002031500004 20020315 00004 NM 2002 3 15 2002F00266 1 20011101 A 7810 65MK7823115 EXHAUST PIPE BOEING 737 737242 1384477 NM NR 2 ENGINE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 159PL 55788 21186 DISCOLORATION OF PAIN ON COWLING, NR 2 ENGINE. FOUND HOLE, APPROX 1 INCH SQUARE, IN TAIL PIPE EXTENSION. HEAT SHIELD O UTER SKIN. (M) 2 L 7 2 4F A16WE 2002031500011 20020315 00011 NE 2002 3 15 2002F00273 2 20011011 A 7200 ENGINE BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE NR 3 MALFUNCTIONED A RYNA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION AP APPROACH 1 CE 07 7643U 20037 ON APPROACH TO ATLANTA INTERNATIONAL AIRPORT AT 1000 AGL NR 3 ENGINE MOMENTARILY LOST POWER. FULL POWER WAS RESTORED WI TH NORMAL ENGINE PARAMETERS AND AIRCRAFT LANDED WITHOUT INCIDENT. ENGINE TO BE RMEOVED AND REPLACED DUE TO SUSPECTED IN TERNAL ENGINE DAMAGE. (M) 2 L 7 3 4F 4 F A3WE E2EA 2002031500012 20020315 00012 NM 2002 3 15 2002F00274 1 20011008 A 5230 DOUBLER BOEING 727 72721 1384003 NM CARGO DOOR DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 359QS 19007 FOUND DENT IN CARGO DOOR DOUBLER AT BS 540 TO BS 560 STRINGER 19L AND 20L. REPAIRED FUSELAGE SKIN AT BS 540 TO BS 560 S TRINGER 19L AND 20L IAW SIDE REPAIR DRAWING 1-10-8-01 AND 727 SRM 51-30-2. 2024-T3 .050 INCH 16.5 INCH BY 14.5 INCH AND 2024-T3 .100 INCH 16.5 BY 14.5 INCH. (M) 2 L 7 3 4F A3WE 2002031500013 20020315 00013 NM 2002 3 15 2002F00275 1 20010924 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE GOUGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND OUTER SKIN GOUGED ON EXISTING REPAIR AT STATION 380 AT STRINGER 24-25R. ACCOMPLISHED DOUBLER INSTALLATION AND REP AIR IAW 737 SRM 53-30-03 FIG NR 9. (M) 2 L 7 2 4F A16WE 2002031500014 20020315 00014 NE 2002 3 15 2002F00276 2 20011010 A 7200 ENGINE LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE NR 1 FIRE A AMTA E A ENGINE SHUTDOWN UNSCHED LANDING A J FLAME/FIRE WARNING INDICATION CL CLIMB 1 GL 11 161AT 1219 DURING CLIMB PASSING THROUGH FL200, HAD FIRE WARNING ON THE NR 1 ENGINE. ENGINE SHUTDOWN. AIR TURN BACK. REPLACED NR 9 AND NR 10 FUEL NOZZLES. (M) 2 L 7 3 4F 4 F A23WE E12EU 2002031500015 20020315 00015 NE 2002 3 15 2002F00277 2 20010930 A 7200 ENGINE BOEING 727 727227 1384078 NM PWA JT8 JT8D17A 52049 NE NR2 FIRE A AMTA E ENGINE SHUTDOWN A K J FLAME/FIRE FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 769AT 21998 715306 AFTER LANDING, THE TOWER REPORTED TO THE CREW THAT THERE WAS FIRE AND SMOKE COMING FROM THE TAIL PIPE OF NR 2 ENGINE. C REW DID NOT HAVE INDICATION OF FIRE, LOW OIL PRESSURE LIGHT ON, OIL QTY DROPPING, EPR AND EGT NORMAL. ENGINE WAS SHUTDO WN, CONTINUED TO GATE, WHILE ENGINE WAS BEING MOTORED FLAME AND SMOKE STILL PRESENT, FOAM WAS SPRAYED INTO THE EXHAUST N OZZLE. REPLACED THE NR 2 ENGINE. (M) 2 L 7 3 4F 4 F A3WE E2EA 2002031500016 20020315 00016 2002 3 15 2002F00231 4 20011222 A 3418 1143800511 WARNING HORN BEECH 1900 1900D 1154162 CE COCKPIT FALSE ACTIVATION A AMWA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 07 178YV UE178 ON DECEMBER 22, 2001, THE STALL WARNING HORN SOUNDED IMMEDIATELY AFTER TAKEOFF. THE PILOT REPORTED THAT THE HORN WOULD NOT SILENCE, AND THEN RETURNED THE AIRCRAFT TO ICT WITHOUT ANY FURTHER INCIDENT. MAINTNANCE CORRECTED THE PROBLEM, AND RETURNED TO THE AIRCRAFT TO SERVICE. THE PILOT SUBMITTED A MIS FOR THE INCIDENT. (M) 2 L 7 2 4T RT A24CE 2002082200043 20020822 00043 NM 2002 8 22 AALA20011895 1 20011012 A 2910 FUSE BOEING 757 757223 1384957 NM HYD SYSTEM FAULTY A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 618AA 24526 DFW - FLT 1241 - AFTER TAKEOFF DFW-LAS, LEFT HYDRAULIC QUANTITY DROPPED TO .38 WITH ACCOMPANYING HYDRAULIC QUANTITY MESS AGE. RETURNED TO DFW LANDED WITHOUT INCIDENT USING ALTERNATE GEAR AND FLAP PROCEDURE. SYSTEM EXPERIENCED REPEAT OCCURRE NCE OCTOBER 15, 2001 AS TRIP 335. REMOVED AND REPLACED MAIN GEAR EXTENSION/RETRACTION HYDRAULIC FLOW FUSES PER MM. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002031500019 20020315 00019 WP 2002 3 15 AALA20012090 1 20011203 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 486AA 49679 DEN - DURING OVERNIGHT MAINTENANCE, FIRST CLASS CABIN OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED OVERHEAD EME RGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002031500020 20020315 00020 WP 2002 3 15 AALA20012091 1 20011203 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP COCKPIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 459AA 49564 DFW - DURING OVERNIGHT MAINTNANCE, COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR COCKPIT EMERGENC Y EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002031500021 20020315 00021 WP 2002 3 15 AALA20012099 1 20011202 A 3350 LIGHT DOUG DC9 DC982 3022082 WP TAIL CONE INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 474 49649 DFW - DURING OVERNIGHT MAINTENANCE, TAIL COMPARTMENT EMERGENCY EXIT LIGHTS WERE INOPERATIVE. SYSTEM GROUND CHECKED NORM AL OPERATION. (M) 2 L 7 2 4F A6WE 2002031500022 20020315 00022 WP 2002 3 15 AALA20012140 1 20011207 A 3350 P4010049 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 555AN 53085 PHX - DURING OVERNIGHT MAINTENANCE, AFT ROW SEAT MOUNTED EMERGENCY PATH LIGHTING INOPERATIVE. REPLACED BATTERY PACK FOR AFT EMEREGNCY PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002031500023 20020315 00023 WP 2002 3 15 AALA20012143 1 20011204 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 427AA 49339 DFW - DURING OVERNIGHT MAINTENANCE, FOUND COCKPIT AND FORWARD ENTRY EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGEN CY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002031500024 20020315 00024 WP 2002 3 15 AALA20012145 1 20011205 A 3350 8039001 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7506 49800 DFW - DURING OVERNIGHT MAINTENANCE, AFT ACCESSORY OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002031500025 20020315 00025 WP 2002 3 15 AALA20012152 1 20011210 A 3350 LIGHT DOUG DC9 DC982 3022082 WP TAIL CONE INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 577AA 53154 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT TAIL CONE INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE A T TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002031500068 20020315 00068 NM 2002 3 15 02031401 1 20010314 A 3350 20131A BATTERY PACK BOEING 757 757236 1384971 NM CABIN DISCHARGED A N8TA K NONE L NO TEST IN INSP/MAINT 1 WP 19 545NA 8587 8587 29944 AFT CABIN SEAT EMERGENCY LIGHTS FROM L3 DOOR INOP. REPLACED BATTERY CHARGER ASSY. OPS CHECK GOOD IAW 33-51-15. 2 L 7 2 4F RT A2NM 2002031500112 20020315 00112 WP 2002 3 15 ASAA0180297 1 20011103 A 5610 GUIDE DOUG DC9 DC983 3022083 WP COCKPIT WINDOW OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 SEA - DURING PREFLIGHT CHECK, THE CAPTAINS SLIDING CLEAR VIEW WINDOW COULD NOT BE OPENED. ADJUSTED WINDOW LATCH GUIDE. WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002031500113 20020315 00113 2002 3 15 ASAA0180300 4 20011112 A 2565 LANYARD DOUG DC9 DC982 3022082 WP ESCAPE SLIDE DETACHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 PHX - DURING LINE CHECK, L-1 DOOR EMERGENCY SLIDE GIRT BAR-TO-LATCH LANYARD WAS FOUND DETACHED. REATTACHED LANYARD. (M ) 2 L 7 2 4F A6WE 2002031500115 20020315 00115 WP 2002 3 15 ASAA0180310 1 20011209 A 5313 RIB DOUG DC9 DC982 3022082 WP TAIL CONE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 951AS 49111 PDX - DURING SERVICE CHECK, FOUND 15 INCH CRACK ON RIB STRUCTURE IN TAIL COMPARTMENT AT STATION 1463 CANT, LONGERON 7 ON LEFT SIDE. AIRCRAFT FERRIED TO OAK FOR REPAIR. REPLACED CRACKED STRUCTURE PER DOUGLAS DWG 9953015. (M) 2 L 7 2 4F A6WE 2002031500116 20020315 00116 2002 3 15 ASAA0180317 4 20011229 A 2565 LANYARD DOUG DC9 DC982 3022082 WP ESCAPE SLIDE DETACHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 937AS 49364 PDX - DURING PREFLIGHT CHECK, L-1 DOOR EMERGENCY SLIDE GIRT BAR-TO-LATCH LANYARD WAS FOUND DETACHED. REATTACHED LANYARD . (M) 2 L 7 2 4F A6WE 2002031500120 20020315 00120 NE 2002 3 15 ASOA01222S 2 20011111 A 7250 BEARING AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE RT ENGINE FAILED A ASOA E A ENGINE SHUTDOWN UNSCHED LANDING A Y J FLAME/FIRE ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SO 11 641AS 387 127082 FLT 4037 - AFTER TAKEOFF FROM ATL, THE RIGHT ENGINE QUIT PRODUCING POWER. THE TORQUE DROPPED SUDDENLY TO APPROXIMATELY 15-20 PERCENT AND FLUCTUATED BETWEEN 15-20 PERCENT. THE FLIGHT ATTENDANT REPORTED SEEING FLAMES. THE CAPTAIN SECURED T HE ENGINE AND DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE. TEAR DOWN REPORT REVEALED THE PRIMARY CAUSE OF THE DISCREPANCY WAS THE FAILURE OF THE NR 5 BEARING. (M) 2 H 7 2 4T 4 T RT E20NE 2002031500121 20020315 00121 NE 2002 3 15 ASOA01303 2 20011228 A 7200 CARBON SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT ENGINE LEAKING A ASOA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 11 826AS 7210 872248 FLT 4698 - WHILE CLIMBING THROUGH FL270 FROM ATL-SWF, THE CAPTAIN REPORTED RECEIVING A RIGHT ENGINE OIL PRESSURE MESSAGE FOLLOWED BY AN AURAL WARNING. THE OIL PRESSURE WAS FLUCTUATING BETWEEN 30 AND 49 PSI. THE CAPTAIN SECURED THE RIGHT E NGINE AND RETURNED TO LAND SAFELY IN ATL. MAINTENANCE PERFORMED AN OIL CONSUMPTION RUN. AN OIL LEAK WAS DISCOVERED AT THE NR 7 CARBON SEAL AREA. MAINTENANCE REMOVED AND REPLACED THE NR 7 CARBON SEAL AND THE 4 AND 6 POSITIONS SCAVENGE TUB E PACKINGS. LEAK AND OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2002031500173 20020315 00173 NM 2002 3 15 UPS01637378 1 20011222 A 7932 INDICATOR BOEING 767 76734AF 1385212 NM COCKPIT FAULTY A IPXA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 SO 01 332UP INSPECTION TYPE:ETOP ATB- LT ENG OIL QTY DECREASED TO 7 QTS. PERFORMED FIM 79-11-00 PAGE 110, DRAINED AND SERVICED OIL PER FIM DUE TO QTY INDICATION. 2 L 7 2 4F RT A1NM 2002031500174 20020315 00174 NM 2002 3 15 UPS02237537 1 20011219 A 5330 SKIN BOEING 727 727185C 138406N NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI RIVET HEAD POPPED AT STR 4R AT BS 710 APPROX. REPAIR CARRIED OUT IAW SRM. 2 L 7 3 4F A3WE 2002031500177 20020315 00177 NM 2002 3 15 UPS02237547 1 20011217 A 5320 FITTING BOEING 727 727185C 138406N NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI VERTICAL FLANGE OF RT 740 FITTING AT I/B END HAS CORROSION. REPLACED FITTING IAW UPS EO B727-5310- 7477 E AND DWG 65C13724. 2 L 7 3 4F A3WE 2002031500179 20020315 00179 NM 2002 3 15 UPS02237548 1 20011218 A 7120 MOUNT BOEING 727 727185C 138406N NM NR 3 ENGINE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI NR 3 ENGINE FWD MOUNT FWD OUTBOARD HOLE HAS PITTING CORROSION ON INSIDE OF BORE. 2 L 7 3 4F A3WE 2002031500193 20020315 00193 NM 2002 3 15 UPS02437385 1 20011229 A 3350 S13560A BATTERY PACK BOEING 747 747123 1384873 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:N/A UPPER DECK CREW SERVICE DOOR EMERGENCY LIGHT WILL NOT TEST. REPLACED BATTERY PACK. OPS CHECK GOOD. 2 L 7 4 4F A20WE 2002031500194 20020315 00194 NM 2002 3 15 UPS02437386 1 20011230 A 5320 STRUCTURE BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:IN AT STA 1140 RT UNDERNEATH SECOND FLOOR PANEL I/B BENEATH DUCTING FOUND CRACK AND CORROSION ON CONTROL WING BOX. 2 L 7 4 4F A20WE 2002031800001 20020318 00001 NM 2002 3 18 2002F00279 1 20010908 A 3320 13431 BALLAST BOEING 757 75723N 1384973 NM CABIN BURNED OUT A AMTA A UNSCHED LANDING M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 514AT 27971 DURING CRUISE, SENSED ELECTRICAL BURNING ODOR AT MID CABIN NEAR LAVATORY ROW 26 AND 28. PERFORMED UNSCHEDULED LANDING. LANDED WITHOUT INCIDENT. REPLACED BALLAST ASSEMBLIES. (M) 2 L 7 2 4F RT A2NM 2002031800002 20020318 00002 NM 2002 3 18 2002F00280 1 20010908 A 3240 713005009 VALVE BOEING 727 7272B7 138407L NM RT BRAKE ASSY MALFUNCTIONED A AMTA O OTHER O OTHER LD LANDING 1 GL 11 760AT 21954 DURING LANDING, THE RIGHT BRAKE WAS INEFFECTIVE FOR SEVERAL APPLICATIONS, THEN PEDAL PRESSURE INCREASE AND THEN BECAME S PONGY. REPLACED NR 4 BRAKE LOCKOUT DEBOOST VALVE IAW MM 33-41-21. OPS CHECKED NORMAL, AIRCRAFT OK FOR SERVICE. (M) 2 L 7 3 4F A3WE 2002031800004 20020318 00004 NM 2002 3 18 2002F00282 1 20011226 A 3411 PITOT TUBE BOEING 757 75723N 1384973 NM PITOT STATIC SYS MISSING A AMTA O OTHER N FALSE WARNING CR CRUISE 1 GL 11 514AT 27971 DURING CRUISE, LT ENGINE EPR, N1, N2, EGT, N3 AND FULE FLOW ERRATIC AT ALL POWER SETTINGS, PARTICULAR AT HIGHER POWER SE TTINGS. FOUND MISSING PITOT HEAD ON PF RAKE AT THE 9 O'CLOCK POSTION ON LT ENIGNE AND PERFORMED INTERIM REPAIR IAW MM 7 7-11-04. PERFORMED ENGINE RUN IAW MM 71-00-00. ALL PARAMETERS NORMAL. (M) 2 L 7 2 4F RT A2NM 2002031800005 20020318 00005 NM 2002 3 18 2002F00283 1 20011230 A 2420 CIRCUIT BREAKER BOEING 727 727227 1384078 NM COCKPIT PANEL SHORTED A AMTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 778AT 22005 IND-MMPR, FLT 6965 - DURING CLIMB, THE NR 2 LEFT FORWARD FUEL BOOST PUMP CIRCUIT BREAKER OPENED IN FLIGHT. RETURNED TO IND. FOUND C/B LOOSE IN PANEL. REMOVED AND REPLACED NR 2 FUEL TANK C/B. OPS CHECKED PER MM AND FOUND OK. (M) 2 L 7 3 4F A3WE 2002031800006 20020318 00006 WP 2002 3 18 2002F00284 1 20011203 A 2820 LINE LKHEED 1011 10113853 5265020 WP FUEL SYSTEM LEAKING A AMTA J A DUMP FUEL UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 11 160AT 1217 DURING TAKEOFF, ON CLIMB-OUT HAD EXCESSIVE FUEL FLOW ON NR 1 ENGINE. TOWER CALLED AND SAID VAPORS TRAILS WERE NOTED FRO M NR 1. SCANNED NR 1 AND SAW FLUID. LEVELED OFF AND PULLED POWER BACK. FUEL LEAK STOPPED. DUMPED FUEL PRIOR TO LANDI NG. REMOVED AND REPLACED FUEL TUBE ASSEMBLY, HP TUBE FROM DISCONNECT TO MANIFOLD IAW EM 72-00-41, OPS CHECK GOOD. NO L EAKS NOTED. (M) 2 L 7 3 4F A23WE 2002031800007 20020318 00007 NM 2002 3 18 2002F00285 1 20011130 A 2560 BATTERY BOEING 727 727264 138408M NM FLASHLIGHT DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 763AT 22983 DURING PREFLIGHT, FOUND THE FORWARD RT FLIGHT ATTENDANT FLASH LIGHT TEST LIGHT WAS NOT FLASHING. REPLACED BATTERY OF FO RWARD RIGHT F/A FLASH LIGHT. (M) 2 L 7 3 4F A3WE 2002031800008 20020318 00008 NM 2002 3 18 2002F00286 1 20011129 A 3411 STATIC LINE BOEING 757 75723N 1384973 NM RT ENGINE DAMAGED A AMTA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 GL 11 528AT 30887 DURING CRUISE, THE RIGHT EPR INDICATOR DROPS .10 WITH LARGE THROTTLE MOVEMENTS SLOWLY RETURNS TO PROPER EPR READING WITH SMALL THROTTLED MOVEMENT. EPR READS NORMALLY ALL ENGINE INDICATION ON RIGHT SIDE WERE NORMAL NO SURGE OR YAW WAS NOTED . REPLACED 9 O'CLOCK 4 EACH PF RAKES PER MM 77-11-04, SYSTEM. OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A2NM 2002031800009 20020318 00009 EU 2002 3 18 2002F00288 1 20011205 A 2910 704A34412038 HOSE SNIAS 350 AS350B3 8680954 EU LEAKING B R7MR O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 NM 07 392LG 913 3252 HOSE LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNITS CORRECTED PROBLEM. (M) 1 G 7 1 3U H9EU 2002031800011 20020318 00011 EU 2002 3 18 2002F00289 1 20011221 A 6340 614764031 TACHOMETER SNIAS 350 AS350B2 8680813 EU MAIN ROTOR INOPERATIVE A R7MR O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 438AE 825 3402 TACHOMETER INDICATOR INOPERATIVE. DURING START OF AIRCRAFT, NR NEEDLE POINTER REMAINS STUCK AT 0 WHILE NTL NEEDLE CONTI NUES TO RISE. TAPPING FACE PLATE RETURNS THE NR NEEDLE TO NORMAL. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M) 1 G 7 1 3U H9EU 2002031800013 20020318 00013 SW 2002 3 18 2002F00291 1 20011108 A 5210 STRUCTURE BELL 407 407 1182206 SW CREW DOOR CRACKED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 107LN 179 53483 FOUND DOOR CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M) 1 G 7 1 3U O H2SW 2002031800014 20020318 00014 SW 2002 3 18 2002F00292 1 20011204 A 5210 STRUCTURE BELL 407 407 1182206 SW CREW DOOR CRACKED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 911LN 840 53446 FOUND DOOR CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M) 1 G 7 1 3U O H2SW 2002031800017 20020318 00017 SW 2002 3 18 2002F00293 1 20011107 A 6240 M835362028M RELAY BELL 407 407 1182206 SW ROTOR HORN STUCK B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 407SJ 878 53422 RELAY INOPERATIVE. STUCK IN OPEN POSITION. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M) 1 G 7 1 3U O H2SW 2002031800018 20020318 00018 SW 2002 3 18 2002F00294 1 20011130 A 2910 70079H000Y150 HOSE BELL 407 407 1182206 SW LEAKING B R7MR O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 NM 07 107LN 224 53483 HOSE LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M) 1 G 7 1 3U O H2SW 2002031800019 20020318 00019 SW 2002 3 18 2002F00295 1 20011130 A 2844 222375077115 TRANSMITTER BELL 407 407 1182206 SW FUEL INDICATOR INTERMITTENT B R7MR O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 107LN 224 53483 TRANSMITTER UNIT CAUSES PRESSURE GAUGE TO FLUCTUATE. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M) 1 G 7 1 3U O H2SW 2002031800020 20020318 00020 SW 2002 3 18 2002F00296 1 20011212 A 2100 ES392102 ACTUATOR BELL 407 407 1182206 SW AIR DISTRIBUTION INOPERATIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 407SJ 53422 ACTUATOR INOPERATIVE. WILL NOT EXTEND OR RETRACT. RETURNING UNIT FOR FULL CREDIT AS AIRCRAFT IS STILL UNDER FACTORY WA RRANTY. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M) 1 G 7 1 3U O H2SW 2002031800021 20020318 00021 EU 2002 3 18 2002F00297 1 20010810 A 7797 430121302 WIRE HARNESS BOLKMS 117 BK117B2 5626013 EU ELECTRICAL SHORTED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 62LF 385 7163 ELECTRICAL FORWARD CABLE INTERNAL SHORT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. THIS CLAIM CHANGED FROM WARRANTY R EPAIR TO EXCHANGE. (M) 1 G 7 2 3U NC H13EU 2002031800022 20020318 00022 EU 2002 3 18 2002F00298 1 20011121 A 7797 430121301 WIRE HARNESS BOLKMS 117 BK117B2 5626013 EU ELECTRICAL SHORTED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 62LF 772 7163 ELECTRICAL FORWARD CABLE INTERNAL SHORT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. CLAIM CHANGED FROM WARRANTY REPAIR TO EXCHANGE. (M) 1 G 7 2 3U NC H13EU 2002031800023 20020318 00023 EU 2002 3 18 2002F00299 1 20011121 A 7797 430121302 WIRE HARNESS BOLKMS 117 BK117B2 5626013 EU ELECTRICAL SHORTED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 62LF 602 7163 ELECTRICAL FORWARD CABLE INTERNAL SHORT. REPLACED WITH NEW UNIT CORRECTED PROBLEM. CLAIM FROM WARRANTY REPAIR TO EXCHA NGE. (M) 1 G 7 2 3U NC H13EU 2002031800024 20020318 00024 EU 2002 3 18 2002F00300 1 20010824 A 7931 642790041 TRANSMITTER SNIAS 350 AS350B2 8680813 EU OIL PRESSURE INOPERATIVE B R7MR O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 852HW 150 2630 ENGINE OIL PRESSURE TRANSMITTER INOPERATIVE. FAULTY INDICATION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 1 3U H9EU 2002031800025 20020318 00025 EU 2002 3 18 2002F00301 1 20011212 A 2820 571712A BYPASS VALVE SNIAS 350 AS350B2 8680813 EU FUEL SYSTEM INOPERATIVE B R7MR O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 922RJ 17 3422 BYPASS VALVE INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 1 3U H9EU 2002031800026 20020318 00026 EU 2002 3 18 2002F00302 1 20011107 A 7931 704A37642042 TRANSMITTER SNIAS 350 AS350D 8680803 EU OIL PRESSURE INOPERATIVE B R7MR O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 350RM 23 1024 ENGINE OIL PRESSURE TRANSMITTER INOPERATIVE. LOW OIL PRESSURE INDICATION, WILL NOT INDICATE ABOVE 90 PSI. REPLACED WIT H NEW UNIT CORRECTED. (M) 1 G 7 1 3U H9EU 2002031800027 20020318 00027 EU 2002 3 18 2002F00303 1 20010703 A 7900 350A54113800 VENT LINE SNIAS 350 AS350B3 8680954 EU ENGINE OIL CRACKED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 52281 162 3249 AIR VENT OIL TUBE CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW, UNIT CORRECTED PROBLEM. (M) 1 G 7 1 3U H9EU 2002031800028 20020318 00028 EU 2002 3 18 2002F00306 1 20010905 A 6410 704A33633116 BEARING SNIAS 350 AS350B3 8680954 EU TAIL ROTOR WORN B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 52285 832 3251 LAMINATED TAIL BEARING ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM 1 KIT PART NUMBER 355A0 9-1036-01 CORRECTED PROBLEM. FOUR HALF SHELLS EQUALS 1 KIT. (M) 1 G 7 1 3U H9EU 2002031800029 20020318 00029 EU 2002 3 18 2002F00307 1 20010822 A 6410 704A33633115 BEARING SNIAS 350 AS350B2 8680813 EU TAIL ROTOR WORN B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 94LG 2728 LAMINATED TAIL BEARING, ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM ONE EACH KIT PART NUMB ER 355A09-1036-01 CORRECTED PROBLEM. FOUR HALF SHELLS EQUALS 1 KIT. (M) 1 G 7 1 3U H9EU 2002031800030 20020318 00030 EU 2002 3 18 2002F00308 1 20011018 A 6410 704A33633171 HINGE SNIAS 350 AS350B2 8680813 EU TAIL ROTOR WORN B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 6099P 430 2818 LAMINATED HINGE, ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM 1 EACH KIT PART NUMBER 355A33 -2153-00 CORRECTED PROBLEM. TWO TEETERING BEARINGS EQUALS 1 KIT. (M) 1 G 7 1 3U H9EU 2002031800031 20020318 00031 EU 2002 3 18 2002F00309 1 20010823 A 6410 704A33633171 HINGE SNIAS 350 AS350B2 8680813 EU TAIL ROTOR WORN B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 96LG 282 2817 LAMINATED HINGE, ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM 1 EACH KIT P/N 355A33-2153-00 CORRECTED PROBLEM. TWO TEETERING BEARINGS EQUALS 1 KIT. (M) 1 G 7 1 3U H9EU 2002031800033 20020318 00033 EU 2002 3 18 2002F00311 1 20011108 A 6320 IPT20RT1100080G TRANSMITTER BOLKMS 117 BK117A3 5626015 EU OIL PRESSURE SHORTED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 202HN 51 7115 PRESSURE TRANSMITTER INTERNAL SHORT TO GROUND. REPLACED WITH NEW, CORRECTED PROBLEM. (M) 1 G 7 2 3U H13EU 2002031800034 20020318 00034 EU 2002 3 18 2002F00312 1 20010608 A 7712 G555674 TRANSDUCER BOLKMS 117 BK117A3 5626015 EU ENG TORQUE INOPERATIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 528SF 33 7104 PRESSURE TRANSDUCER INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 2 3U H13EU 2002031800036 20020318 00036 EU 2002 3 18 2002F00313 1 20011111 A 7931 DK040 TRANSMITTER BOLKMS 105 BO105S 5626006 EU OIL PRESSURE INOPERATIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 485EC 619 S754 PRESSURE TRANSMITTER INOPERATIVE. ERRATIC OPERATION. REPLACED WITH NEW, CORRECTED PROBLEM. (M) 1 G 7 2 3U H3EU 2002031800037 20020318 00037 EU 2002 3 18 2002F00314 1 20011221 A 6210 350A31177000 PIN SNIAS 350 AS350B3 8680954 EU M/R BLADE WORN B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 392LG 925 3252 BLADE ASSEMBLY PIN WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M) 1 G 7 1 3U H9EU 2002031800038 20020318 00038 EA 2002 3 18 2002F00315 1 20011130 A 2750 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA FLAP SYSTEM MALFUNCTIONED B MASA O OTHER F FLT CONT AFFECTED LD LANDING 1 SW 07 27185 7185 FLT 6445 - PHX-BOI - THE CREW DECLARED AN EMERGENCY AFTER HAVING A FLAP FAIL MESSAGE. THE AIRCRAFT LANDED UNEVENTFULLY WITH THE FLAPS SET AT 8 DEGREES. MAINTENANCE IN BOI RESET THE FLAP SYSTEM AND COMPLIED WITH AD 98-20-01. (M) 2 L 7 2 4F RT A21EA 2002031800039 20020318 00039 NM 2002 3 18 2002F00316 1 20011201 A 5311 ACA3796501 FRAME DOUG DC10 DC1040F 3023507 NM FUSELAGE CORRODED B CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 141WE 51705 46661 DURING C-CHECK, THE LT NOSE WHEEL WELL CHORD VERTICAL LEG WAS FOUND CORRODED AND BLENDED JUST PAST SRM REPAIRABLE LIMITS . A REPAIR ANGLE WAS INSTALLED IAW TIMCO REO-GO8344 REV IR AND REO G8336 REV IR A 8110-3 WAS ISSUED BY DER, DERY 51031 4-CE FAR 145 REPAIR AGENCY NR TIPR833K. THE AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (M) 2 L 7 3 4F RT A22WE 2002031800041 20020318 00041 NM 2002 3 18 2002F00317 1 20011201 A 5313 AJC7119501 LONGERON DOUG DC10 DC1040F 3023507 NM FUSELAGE CRACKED B CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 141WE 51705 46661 DURING C-CHECK, LONGERON 13L WAS FOUND CRACKED BETWEEN FASTENER HOLES AT CANTED STATION Y2153. LONGERON 13L WAS REPAIR ED IAW TIMCO REO-GO8321 REV IR AND FAA FORM 8110-3 WAS ISSUED DER DERY 510314-CE FAR 145 REPAIR AGENCY NR TIPR833K. THE AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (M) 2 L 7 3 4F RT A22WE 2002031800043 20020318 00043 NM 2002 3 18 2002F00318 1 20011201 A 5320 ACA70161 ANGLE DOUG DC10 DC1040F 3023507 NM FUSELAGE CORRODED B CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 141WE 51705 46661 DURING C-CHECK, THE FORWARD LEFT AIRCONDITIONING BAY CAP ANGLE AT STATION 595 BETWEEN LONGERON 47L AND 48L WAS CORRODED PAST SRM LIMITS. A REPAIR DOUBLER WAS INSTALLED ON THE EXTERIOR OF THE SKIN TO REINFORCE THE BLEND AREA IAW TIMCO REO-G O8333. A 8110-3 WAS ISSUED BY DER DERY 510314-CE AT FAR 145 REPAIR AGENCY NR TIPR833K. THE AIRCRAFT WAS RETURNED TO RE VENUE SERVICE. (M) 2 L 7 3 4F RT A22WE 2002031800098 20020318 00098 EU 2002 3 18 DKAA02001 1 20010108 A 5730 GASMYS20124001 PANEL AMD FALCON FALCON20 2730103 EU LT WING CORRODED A DKAA K NONE O OTHER IN INSP/MAINT 1 GL 23 301R 15384 3 DURING SCHEDULED CORROSION INSPECTION, LEFT WING INBOARD UPPER FLAP CLOSEOUT PANEL FOUND CORRODED BEYOND LIMITS. PANEL REPAIRED PER DER ENGINEERING ORDER NR EO 01-23, REV A. AIRCRAFT RETURNED TO SERVICE AFTER INSPECTION WAS COMPLETED. (M ) 2 L 7 2 4F RT A7EU 2002031800099 20020318 00099 EU 2002 3 18 DKAA02002 1 20010108 A 5313 STRINGER AMD FALCON FALCON20 2730103 EU LT MLG WW CORRODED A DKAA K NONE O OTHER IN INSP/MAINT 1 GL 23 301R 15384 3 DURING SCHEDULED CORROSION INSPECTION, STRINGER IN LEFT GEAR WELL CEILING FOUND CORRODED BEYOND LIMITS. STRINGER REPLAC ED PER AMD STRUCTURAL REPAIR MANUAL 51-10-11. AIRCRAFT RETURNED TO SERVICE AFTER INSPECTION WAS COMPLETED. (M) 2 L 7 2 4F RT A7EU 2002031800102 20020318 00102 NM 2002 3 18 EIAA2001004 1 20010104 A 3310 245902 SWITCH BOEING 747 747273C 1384896 NM COCKPIT OVERHEATED A EIAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 470EV 20653 KHNL - AT FL 340, EXPERIENCED SMOKE IN THE COCKPIT COMING FROM AFT END OF CENTER CONSOLE. ACCOMPLISHED FIRE/SMOKE PROCE DURES AND RETURNED TO HNL. FOUND DIMMER IN CENTER PEDISTAL (LOWER) OVERHEATED CAUSING SMOKE. REPLACED LOWER DIMMER WIT H IMPROVED DIMMER P/N 2-459-04/05. NO FURTHER SMOKE OR OVERHEATING FOUND REF EO 33-747-1607-00. (M) 2 L 7 4 4F A20WE 2002031800119 20020318 00119 WP 2002 3 18 GTIA012268 1 20011210 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - AFT PIT DOOR CUT OUT PANEL HAS CRACK CORROSION AND DIRTY. FABRICATED LOCATED AND DRILLED UP DOUBLER. INSTALLED R EPAIR DOUBLER PER MD80 SRM SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002031800120 20020318 00120 WP 2002 3 18 GTIA012270 1 20011203 A 2760 CONNECTOR DOUG DC9 DC982 3022082 WP SPOILERS DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - RIGHT SPOILER POSITION FAILS DURING RETURN TO SERVICE TEST. T/S SYSTEM AND FOUND PIN OF 1 OF P10 398 RECESSED. R ESEATED PIN IN CONNECTOR IAW MD80 WDM 20-50-04. (M) 2 L 7 2 4F A6WE 2002031800121 20020318 00121 WP 2002 3 18 GTIA012277 1 20011107 A 7120 YOKE DOUG DC9 DC982 3022082 WP ENGINE MOUNT CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FOUND RIGHT ENGINE MOUNT YOKE HAS CORROSION INSIDE LOWER VIBRATION ISOLATOR CAVITY AND EXTERNAL AREA. REMOVED COR ROSION. OK TO INSTALL SERVICEABLE YOKE. INSTALLED YOKE. REMOVED YOKE BOLTS. INSTALLED YOKE BOLTS PER MD80 MM 71-20-3 . (M) 2 L 7 2 4F A6WE 2002031800122 20020318 00122 WP 2002 3 18 GTIA012279 1 20011205 A 3520 OXYGEN MASK DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FOUND OXYGEN MASK AT ROWS 18 LEFT, 25 LEFT AND 31 RIGHT DIDN'T DROP. ADJUSTED OXYGEN DOORS IAW MD80 MM 35-20-00. (M) 2 L 7 2 4F A6WE 2002031800123 20020318 00123 WP 2002 3 18 GTIA012280 1 20011224 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP CABIN CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND STATION 200 -X5 TO PLUS X5 FLOORBOARD SUPPORT ANGLE HAS HEAVY CORROSION. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALL FLOOR SUPPORT IAW DC9 MD80 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 2002031800124 20020318 00124 WP 2002 3 18 GTIA012289 1 20011208 A 5730 PANEL DOUG DC9 DC982 3022082 WP LT WING DETERIORATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND LEFT WING LOWER SURFACE TRAPOZOIDAL PANEL DETERIORATED. REMOVED DAMAGED PILES OF FIBERGLASS ON LEFT WING TR APEZOID PANEL. REPAIRED DELAMINATION AT AFFECTED AREAS IAW DC9 MD80 SRM 51-90-0. (M) 2 L 7 2 4F A6WE 2002031800125 20020318 00125 WP 2002 3 18 GTIA012292 1 20011211 A 5755 SKIN DOUG DC9 DC982 3022082 WP SPOILER DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - RIGHT WING INBOARD FLIGHT SPOILER DELAMINATION. RIGHT WING INBOARD FLIGHT SPOILER REPLACED. (M) 2 L 7 2 4F A6WE 2002031800128 20020318 00128 WP 2002 3 18 GTIA012306 1 20011102 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FTW - FOUND FLOOR SUPPORT CORRODED AND STATION 173-X53 INCH FORWARD ENTRY AREA. FOUND WEB FLOOR PANEL CRACKED AND CORRO DED. FORM NEW WEB FLOOR. INSTALLED NEW WEB FLOOR IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002031800131 20020318 00131 WP 2002 3 18 GTIA012308 1 20011129 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND FLOOR SUPPORT CORRODED AT STATION Y=200 FROM -24 INCH TO -X43, FOUND AFTER G-1 REMOVED DUE A CORROSION BEYON D LIMITS AT FLOOR SUPPORT. DRILLED AND LOCATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT IAW DC9 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 2002031800132 20020318 00132 WP 2002 3 18 GTIA012309 1 20011113 A 5410 DOUBLER DOUG DC9 DC932 3022066 WP NR 2 NACELLE BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 NR 2 ENGINE PYLON UPPER OUTBOARD LE STRUCTURE FRAME HAS BROKEN DOUBLER. REMOVED BROKEN DOUBLER. INSTALLED DOUBLER IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002031800137 20020318 00137 WP 2002 3 18 GTIA012310 1 20011107 A 2740 JACKSCREW DOUG DC9 DC932 3022066 WP HORIZONTAL STAB DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - ACME SCREW AND NUT END PLAY CHECK IN EXCESS OF .040, REPLACEMENT OF HORIZONTAL STAB ACTUATOR ASSY REQUIRED. REMOV ED LONGITUDINAL TRIM CONTROL SYSTEM ASSY (JACKSCREW). INSTALLED JACKSCREW ASSY IAW DC9 MM 27-40-1. (M) 2 L 7 2 4F A6WE 2002031800139 20020318 00139 WP 2002 3 18 GTIA012312 1 20011115 A 2760 DRIVE LINK DOUG DC9 DC932 3022066 WP SPOILERS CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND OUTBOARD SPOILER DRIVE LINK, INBOARD LUG CRACKED. REMOVED DRIVE LINK LEFT OUTBOARD SPOILER. INSTALLED DRIV E LINK ON LEFT OUTBOARD SPOILER AS PER DC9 MM 27-61-1. (M) 2 L 7 2 4F A6WE 2002031800140 20020318 00140 WP 2002 3 18 GTIA012313 1 20011220 A 5755 PANEL DOUG DC9 DC932 3022066 WP SPOILERS WARPED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND RIGHT WING INBOARD FLIGHT SPOILER WARP. REMOVED RIGHT INBOARD SPOILER PANEL. INSTALLED RIGHT INBOARD SPOIL ER PANEL IAW MM DC9 27-61-1. (M) 2 L 7 2 4F A6WE 2002031800141 20020318 00141 WP 2002 3 18 GTIA012314 1 20011112 A 2720 PULLEY BRACKET DOUG DC9 DC932 3022066 WP RUDDER BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND BRACKET RUDDER TRIM PULLEY BROKEN. REMOVED RUDDER TRIM BRACKET. INSTALLED RUDDER TRIM PULLEY BRACKET AS PE R DC9 MM 20-17-0. (M) 2 L 7 2 4F A6WE 2002031800142 20020318 00142 WP 2002 3 18 GTIA012316 1 20011115 A 5320 RETAINER DOUG DC9 DC932 3022066 WP CABIN FLOOR BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND CABIN FLOORBOARD LEFT, OUTBOARD STATION 389-465, LOWER SIDE RETAINER BROKEN IN HALF (FIBERGLASS) SURFACE COR ROSION AND BARE METAL AREAS ON SKIN. AREA FOUND OUT OF LIMITS. FABRICATED NEW FLOORBOARD PER DC9 SRM 51-10-2. (M) 2 L 7 2 4F A6WE 2002031800143 20020318 00143 WP 2002 3 18 GTIA012319 1 20011220 A 5754 RIB DOUG DC9 DC932 3022066 WP RT WING SLAT CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND RIGHT WING NR 4 SLAT 8TH INNER RIB FROM OUTBOARD END OF SLAT IS CRACKED. REMOVED RIB. FABRICATED NEW RIB. INSTALLED NEW RIB IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002031800144 20020318 00144 WP 2002 3 18 GTIA012320 1 20011105 A 5753 SKIN DOUG DC9 DC932 3022066 WP FLAP VANE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND LEFT WING FIXED FLAP VANE HAS A CRACK AT STATION XTE 206. LOCATE AND DRILL NEW (SKIN FIXED COVER). INSTALL ED SKIN ASSEMBLIES PER SRM DC9 MD80 51-30-1. (M) 2 L 7 2 4F A6WE 2002031800146 20020318 00146 WP 2002 3 18 GTIA012325 1 20011107 A 5712 RIB DOUG DC9 DC932 3022066 WP RT WING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND RIGHT WING FUSELAGE MOUNTED VERTICAL RIB, INBOARD OF TRAILING EDGE FLAP HAS A .250 CRACK ON ITS LOWER EDGE. REMOVED DAMAGE PART. FORMED ANGLE FOR REPAIR ON VERTICAL RIB. INSTALLED REPAIR ANGLE IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002031800148 20020318 00148 NM 2002 3 18 HALA0100314 1 20011214 A 2822 PUMP BOEING 767 76733A 1385209 NM FUEL BOOST DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 582HA 28139 HNL - ETOPS SIGNIFICENT SYSTEM, PER EO 28-01-03-71 LT AUX TANK BOOST PUMP CONDUIT OUTER SLEEVE HAS A HOLE APPROX 14 INCH ES FROM TERMINAL END. REPLACED LEFT OVERRIDE AUX PUMP CONDUIT OUTER SLEEVE PER EO 28-01-03-71 REV A. (M) 2 L 7 2 4F RT A1NM 2002031800149 20020318 00149 NM 2002 3 18 HALA0100315 1 20011214 A 2822 PUMP BOEING 767 76733A 1385209 NM FUEL BOOST DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM, PER EO 28-01-03-71, LEFT AFT FUEL BOOST PUMP CONDUIT OUTER SLEEVE HAS A HOLE APPROX 44 INCHES FROM TERMINAL END. REPLACED LEFT AFT BOOST PUMP CONDUIT OUTER SLEEVE PER EO 28-01-0371 REV A. (M) 2 L 7 2 4F RT A1NM 2002031900002 20020319 00002 NM 2002 3 19 KPVA200125 1 20011118 A 2560 10005511 FLASHLIGHT DHAV DHC8 DHC8103 1386005 NM CABIN INOPERATIVE A KPVA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806WP 357 HNL - FOUND PORTABLE EMERGENCY LIGHT WILL NOT COME ON WHEN SELECTED ON. REMOVED AND REPLACED PORTABLE EMERGENCY LIGHT A SSEMBLY. OPS CHECK GOOD IAW DHC 8MM 33-51-01 PAGE 201. (M) 2 H 7 2 4T RT A13NM 2002031900009 20020319 00009 SO 2002 3 19 SIMA200128304 1 20010910 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 627AE 145121 ORD - EMERGENCY FLOOR LIGHTS INOPERATIVE. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY POWER SUPPLY IAW EMB 145 AMM. OP ERATIONALLY CHECKED GOOD. (M) 2 L 7 2 4T RT T00011AT 2002031900010 20020319 00010 SO 2002 3 19 SIMA200129003 1 20011015 A 3350 110049 CHARGER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 602AE 145048 ORD - FLT 4198 - EMERGENCY LIGHT OVER 12AC INOPERATIVE. REMOVED AND REPLACED NR 3 BATTERY CHARGE CHASIS ASSEMBLY IAW EM B145 AMM. OPERATIONALLY CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2002032500099 20020325 00099 NM 2002 3 25 MED2002F00000 1 20010602 A 2420 CSD BOEING 737 7373L9 1384470 NM NR 1 FAILED W MEDY K NONE O OTHER IN INSP/MAINT 1 EA 33 219TY 24219 CAPTAIN REPORTED, AC DEPARTED, ENROUTE, AFTER 30 MIN OF FLIGHT NR 1 IDG LOW OIL PRESSURE LIGHT ILLUMINATED. IDG WAS DI SCONNECTED. APPROX 45 MINUTES INTO FLIGHT, JUST BEFORE ARRIVAL, NR 2 IDG WAS DISCONNECTED WITH LOW OIL PRESSURE, TEMP R ISE OF 20 DEGREE C. ON INSPECTION THERE WAS NO SIGN OF LEAK FROM EITHER NR 1 OR NR 2 CSD. COWLINGS ARE DRY AS WERE CS DS THEMSELVES. NR 1 STARTER WAS ALSO FOUND WITH OIL INDICATIONS OF NIL, NR 2 STARTER WILL BE DRAINED TO DETERMINE CONTE NTS. NR2, N1 INDICATIONS FAILED DURING FLIGHT. AIRCRAFT WAS FLYING UNDER FAA FORM 8130-7, SPECIAL AIRWORTHINESS CERTIF ICATE, SPECIAL FLIGHT PERMIT. FOR PURPOSE OF MAINTENANCE ISSUED ON THE 4TH OF FEB 2002 AND VALID UNTIL 10TH OF FEBRUARY 2 L 7 2 4F RT A16WE 2002032600234 20020326 00234 NM 2002 3 26 ASAA0110643 1 20011120 A 5313 6545804560 STRINGER BOEING 737 737298C 1384490 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND CHORD AT BS 259-260, STRINGER 26R WITH AN OVERSIZED HOLE. REMOVED AND REPLACED CH ORD PER SRM. (M) 2 L 7 2 4F RT A16WE 2002032600237 20020326 00237 NM 2002 3 26 ASAA0110644 1 20011126 A 3350 D20011 SWITCH BOEING 737 737290C 138448V NM AFT F/A PANEL MALFUNCTIONED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 ANC - SOME EMERGENCY EXIT LIGHTING WILL NOT EXTINGUISH WITH FLIGHT DECK SWITCH IN ARMED POSITION. REMOVED AND REPLACED AFT FLIGHT ATTENDANTS CONTROLS SWITCH THEN LIGHTS OPERATED NORMAL. (M) 2 L 7 2 4F A16WE 2002032600239 20020326 00239 NM 2002 3 26 ASAA0110651 1 20011206 A 3220 6545838502 FITTING BOEING 737 737290C 138448V NM NLG CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING SCHEDULED INSPECTION, FOUND NOSE LANDING GEAR DRAG BRACE, RIGHT TRUNNION SUPPORT FITTING CRACKED. REMOVED AND REPLACED FITTING PER BOEING DRAWING. (M) 2 L 7 2 4F A16WE 2002032600240 20020326 00240 NM 2002 3 26 ASAA0110658 1 20011220 A 5320 6573747 STRINGER CLIP BOEING 737 737298C 1384490 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER CLIP AT BS 867, STRINGER 4L DAMAGED. REMOVED AND REPLACED STRINGER CLIP PER SRM. (M) 2 L 7 2 4F RT A16WE 2002032600241 20020326 00241 NM 2002 3 26 ASAA0110659 1 20011220 A 5320 6573747 STRINGER CLIP BOEING 737 737298C 1384490 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER CLIP AT BS 887, STRINGER 4L DAMAGED. REMOVED AND REPLACED STRINGER CLIP PER SRM. (M) 2 L 7 2 4F RT A16WE 2002032600242 20020326 00242 NM 2002 3 26 ASAA0110660 1 20011220 A 5310 6546527 SHEAR TIE BOEING 737 737298C 1384490 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND SHEAR TIE BS 420, STRINGER 26L-27L CRACKED. REPAIRED SHEAR TIE PER SRM. (M) 2 L 7 2 4F RT A16WE 2002032600243 20020326 00243 NM 2002 3 26 ASAA0110661 1 20011220 A 5320 6562107 WEB BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND WEB AT BS 400, LBL 52 CORRODED. REPAIRED WEB PER SRM. (M) 2 L 7 2 4F RT A16WE 2002032600244 20020326 00244 NM 2002 3 26 ASAA0110662 1 20011221 A 5313 BAC1498156 STRINGER BOEING 737 737298C 1384490 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER 27R AT BS 361 CRACKED. REPAIRED WEB PER SRM. (M) 2 L 7 2 4F RT A16WE 2002032600245 20020326 00245 NM 2002 3 26 ASAA0110663 1 20011221 A 5347 BAC15201430 SEAT TRACK BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND SEAT TRACK FLANGE AT BS 500-500A, LBL 45 CORRODED. REMOVED AND REPLACED SEAT TRAC K PER SRM. (M) 2 L 7 2 4F RT A16WE 2002032600246 20020326 00246 NM 2002 3 26 ASAA0110664 1 20011226 A 5313 6545768 STRINGER BOEING 737 737298C 1384490 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER 16R AT BS 500B CRACKED BOTH FORWARD AND AFT OF WING SCAN LIGHT. REPAIRED CRACK PER EA. (M) 2 L 7 2 4F RT A16WE 2002032600247 20020326 00247 NM 2002 3 26 ASAA01400108 1 20011003 A 2150 2205172 ACM BOEING 737 7374Q8 138447Q NM A/C BAY LEAKING A ASAA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 01 784AS 28199 PDX - DURING CLIMB-OUT AT ABOUT 15,000 FEET FLIGHT ATTENDANT REPORTED ODOR IN THE CABIN. DIVERTED TO PDX. NO SMOKE OR FIRE WAS NOTED. LANDED WITHOUT INCIDENT, INSPECTED AND FOUND LEFT AIR CYCLE MACHINE LEAKING OIL. REMOVED AND REPLACE A CM, OPS NORMAL. (M) 2 L 7 2 4F RT A16WE 2002032600248 20020326 00248 NM 2002 3 26 ASAA01400159 1 20011127 A 5315 65C33268 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 PAE - DURING SI CHECK, FOUND FLOORBEAM AT BS 967 RBL 16 AND WL 208 HAS MECHANICAL DAMAGE. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2002032600249 20020326 00249 NM 2002 3 26 ASAA01400187 1 20011231 A 5730 65C263446 PANEL BOEING 737 737490 1384715 NM WING DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 796AS 28891 SEA - DURING C-CHECK, FOUND PANEL 8501 DAMAGED ON LOWER SURFACE. REPAIRED IAW EA. (M) 2 L 7 2 4F RT A16WE 2002032600250 20020326 00250 NM 2002 3 26 ASAA0140140 1 20011113 A 5320 6545875070 SILL BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 PAE - DURING SI CHECK, FOUND CORROSION ON MOPSILL RBL 55 AT BS 274, 283, 294 AND 346 AND WL 208. REMOVED AND REPLACED M OPSILL IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002032600251 20020326 00251 NM 2002 3 26 ASAA0140141 1 20011114 A 5315 6545810 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 PAE - DURING SI CHECK, FOUND CORROSION TOP OF FLOORBEAM AT BS 312 LBL 1, 6, 15 AND WL 208. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002032600252 20020326 00252 NM 2002 3 26 ASAA0140145 1 20011118 A 5320 69774573 ANGLE BOEING 737 7374Q8 138447Q NM GALLEY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 PAE - DURING SI CHECK, FOUND GALLEY SUPPORT ANGLE QT BS 986 TO 1016 AND WL 208 IS CORRODED. REMOVED AND REPLACED ANGLE IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002032600253 20020326 00253 NM 2002 3 26 ASAA0140146 1 20011118 A 5315 654581890 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 PAE - DURING SI CHECK, FOUND CORROSION ON FLOORBEAM AT STATION 360 WL 208 AND RBL 19 AND 26. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002032600255 20020326 00255 NM 2002 3 26 ASAA0140147 1 20011119 A 5320 69774772 ANGLE BOEING 737 7374Q8 138447Q NM GALLEY DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 PAE - DURING SI CHECK, FOUND GALLEY SUPPORT Z-ANGLE AT BS 993, RBL 32-44, AND WL 208 HAS MECHANICAL DAMAGE. REPLACED PE R SRM. (M) 2 L 7 2 4F RT A16WE 2002032600256 20020326 00256 NM 2002 3 26 ASAA0140148 1 20011120 A 5320 6545855103 SILL BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 PAE - DURING SI CHECK, FOUND R-2 MOPSILL AT BS 951-992, RBL 55 AND WL 208 CORRODED. REPLACED PER SRM. (M) 2 L 7 2 4F RT A16WE 2002032600257 20020326 00257 NM 2002 3 26 ASAA0140149 1 20011120 A 5320 65528780102 SILL BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 PAE - DURING SI CHECK, FOUND L2 MOPSILL AT BS 951-992, LBL 55 AND WL 208 CORRODED. REPLACED PER SRM. (M) 2 L 7 2 4F RT A16WE 2002032600258 20020326 00258 NM 2002 3 26 ASAA0140150 1 20011120 A 5311 6546567 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 PAE - DURING SI CHECK, FOUND CRACK IN FRAME AT BS 1006 WL 208 AND LBL 41. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002032600259 20020326 00259 NM 2002 3 26 ASAA0140151 1 20011121 A 5320 69770112 ATTACH FITTING BOEING 737 7374Q8 138447Q NM GALLEY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 PAE - DURING SI CHECK, FOUND CORROSION ON GALLEY ATTACH FITTINGS AT BS 333, RBL 9 AND WL 209. REPLACED PER SRM. (M) 2 L 7 2 4F RT A16WE 2002032600260 20020326 00260 NM 2002 3 26 ASAA0140152 1 20011121 A 5313 654988661 STRINGER BOEING 737 7374Q8 138447Q NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 PAE - DURING SI CHECK, FOUND STRINGER 16 RIGHT HAS GOUGE ON UPPER SIDE JUST FORWARD OF BS 500 FRAME. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2002032600261 20020326 00261 NM 2002 3 26 ASAA0140153 1 20011121 A 3397 8100022605 WIRE BOEING 737 7374Q8 138447Q NM CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 771AS 25104 PDX - DURING LINE CHECK, FOUND FLOOR TRACK LIGHTING AT ROW 16 INOPERATIVE. RESTORED WIRING TO ORIGINAL CONDITION, OPS C HECKED GOOD. (M) 2 L 7 2 4F RT A16WE 2002032600262 20020326 00262 NM 2002 3 26 ASAA0140155 1 20011126 A 5320 6545834259 STIFFENER BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 PAE - DURING SI CHECK, FOUND CORROSION ON STIFFENER AT BS 335, LBL 10 AND WL 208. REPLACED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002032600263 20020326 00263 NM 2002 3 26 ASAA0140156 1 20011125 A 5320 6977477 ANGLE BOEING 737 7374Q8 138447Q NM GALLEY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 PAE - DURING SI CHECK, FOUND GALLEY SUPPORT ANGLE CORRODED AT BS 986-1016, RBL 32, WL 208. REPLACED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002032600264 20020326 00264 NM 2002 3 26 ASAA0140157 1 20011126 A 5320 69774771 ANGLE BOEING 737 7374Q8 138447Q NM GALLEY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 PAE - DURING SI CHECK, FOUND GALLEY SUPPORT ANGLE CORRODED AT BS 993, LBL 32-44, WL 208. REPLACED PER SRM. (M) 2 L 7 2 4F RT A16WE 2002032600265 20020326 00265 NM 2002 3 26 ASAA0140158 1 20011126 A 5313 654988661 STRINGER BOEING 737 7374Q8 138447Q NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 PAE - DURING SI CHECK, FOUND GOUGE ON STRINGER 16 RT ON UPPER SIDE JUST FORWARD OF 500F FRAME. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2002032600268 20020326 00268 NM 2002 3 26 ASAA0140160 1 20011127 A 5320 65C333753 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 PAE - DURING SI CHECK, FOUND FLOOR SUPPORT AT BS 951, LBL 16-25 AND WL 208 HAS MECHANICAL DAMAGE. REPLACED FLOOR SUPPOR T PER SRM. (M) 2 L 7 2 4F RT A16WE 2002032600269 20020326 00269 NM 2002 3 26 ASAA0140161 1 20011127 A 2560 65C161216 FITTING BOEING 737 7374Q8 138447Q NM FWD ENTRY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 PAE - DURING SI CHECK, FOUND CORROSION ON GRIT BAR ATTACHMENT AT BS 344, LBL 53 AND WL 209. REPLACED PER SRM. (M) 2 L 7 2 4F RT A16WE 2002032600270 20020326 00270 NM 2002 3 26 ASAA0140164 1 20011127 A 5347 6546813109 SEAT TRACK BOEING 737 7374Q8 138447Q NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 PAE - DURING SI CHECK, FOUND SEAT TRACK GOUGED AT BS 538, LBL 45.5 AND WL 208. REPLACED PER SRM. (M) 2 L 7 2 4F RT A16WE 2002032600271 20020326 00271 NM 2002 3 26 ASAA0140183 1 20011226 A 5310 65C22908 SHEAR TIE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 783AS 25114 PAE - DURING SI CHECK, FOUND CORROSION ON SHEAR TIE AT BS 500C, LBL 3 TO RBL 3 AND WL 149. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002032600272 20020326 00272 NM 2002 3 26 ASAA0140184 1 20011226 A 5315 6545818 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 783AS 25114 PAE - DURING SI CHECK, FOUND FLOORBEAM AT BS 360 HAS CORROSION AT NUT CLIP HOLES, RBL 13 TO 40 AND WL 208. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002032600273 20020326 00273 NM 2002 3 26 ASAA0140185 1 20011226 A 5320 69353521 STRINGER CLIP BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 783AS 25114 PAE - DURING SI CHECK, FOUND STRINGER CLIP DENTED AT STATION 727R AND STRINGER 24L. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002032600275 20020326 00275 NM 2002 3 26 ASAA0180313 1 20011215 A 3350 60030451 BATTERY PACK DOUG MD80 MD83 3023681 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 982AS 53473 PDX - DURING LINE CHECK, OVERHEAD EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE BETWEEN ROW 8 AND 17. REPLACED ASSOCIAT ED BATTERY POWER SUPPLY PACK AT B5-101. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT 2002032600276 20020326 00276 WP 2002 3 26 ASAA0180314 1 20011216 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 973AS 11988 53449 SEA - DURING LINE CHECK, LEFT AND RIGHT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS WERE DETERMINED TO BE INOPERATIVE. REPL ACED ASSOCIATED BATTERY PACK (POWER SUPPLY). LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002032600277 20020326 00277 NM 2002 3 26 ASAA0180319 1 20011231 A 3350 60030451 BATTERY PACK DOUG MD80 MD83 3023681 NM COCKPIT DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 982AS 53473 SEA - DURING PREFLIGHT CHECK, FOUND COCKPIT OVERHEAD EMERGENCY LIGHTING WAS INOPERATIVE. REPLACED ASSOCIATED BATTERY PO WER SUPPLY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT 2002032700167 20020327 00167 CE 2002 3 27 HYI2002F00006 1 20011105 A 3110 CM358950 MASTER SWITCH CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO LT SWITCH PANEL FAILED E HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 6879R 402C0611 ON PRE-FLIGHT INSPECTION, AVIONIC MASTER SWITCH FAILED. MAINTENANCE REPLACED SWITCH AND RETURNED AIRCRAFT TO SERVICE. 1 L 7 2 3O 3 O A7CE E8CE 2002032700168 20020327 00168 CE 2002 3 27 HYI2002F00007 1 20011029 A 3110 CM358950 MASTER SWITCH CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO LT SWITCH PANEL FAILED E HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 68391 402C0483 ON PRE-FLIGHT INSPECTION AVIONICS MASTER SWITCH FAILED. MAINTENANCE REPLACED SWITCH AND RETURNED AIRCRAFT TO SERVICE. 1 L 7 2 3O 3 O A7CE E8CE 2002032700169 20020327 00169 CE 2002 3 27 HYI2002F00008 1 20011129 A 3110 CM358950 MASTER SWITCH CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO LT SWITCH PANEL FAILED E HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 258PB 402C0336 ON PRE-FLIGHT INSPECTION, AVIONICS SWITCH FAILED. MAINTENANCE REPLACED THE SWITCH AND RETURNED AIRCRAFT TO SERVICE. PT RS 12/12/01 1 L 7 2 3O 3 O A7CE E8CE 2002032800007 20020328 00007 CE 2002 3 28 HYI2002F00009 1 20011121 A 3110 CM358950 MASTER SWITCH BEECH 45 D45 1152012 CE CONT O470 O470* 17026 SO LT SWITCH PANEL FAILED E HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 13616 1000 BG345 ON PRE-FLIGHT INSPECTION, AVIONICS MASTER SWITCH FAILED. MAINTENANCE REPLACED SWITCH AND RETURNE AIRCRAFT TO SERVICE. 1 L 7 1 3O 3 O 5A3 E273 2002032800010 20020328 00010 EU 2002 3 28 NYS2002F00000 1 20011005 A 5302 10521801 SUPPORT BOLKMS 105 BO105S 5626006 EU TAILBOOM CRACKED E NYSA K NONE O OTHER IN INSP/MAINT 1 EA 23 105NG 6814 S632 DURING AN ENGINE INSPECTION FOUND NR 1 HANGER BEARING SUPPORT CRACKED. INSPECTED ALL RELATED COMPONENTS AND FOUND NO DE FECTS. REMOVED BRACKET AND INSTALLED NEW. 1 G 7 2 3U H3EU 2002032800031 20020328 00031 CE 2002 3 28 ZES2002F00002 1 20011210 A 3310 97524048 PANEL BEECH 100 B100 1152919 CE GARRTT TPE331 TPE3315 01514 WP PEDESTOL BURNED E ZESA K NONE O OTHER IN INSP/MAINT 1 EA 03 777DQ 8987 BE59 SHORTLY AFTER TAKEOFF, PILOT NOTICED SMOKE COMING FROM PEDISTOL TRIM SWITCH SUB PANEL. PEDESTOL LITES, CIRCUIT BREAKER POPPED, SHORT, SMOKE QUIT. PILOT LANDED AIRCRAFT UNEVENTFULL. FOUND LAMP SHORTED ON LIGHT STRIP. 1 L 7 2 4T 4 T A14CE E4WE 2002032800034 20020328 00034 NM 2002 3 28 2002F00330 1 20011201 A 7830 THRUST REVERSER DOUG DC10 DC1040F 3023507 NM MR 2 ENGINE DAMAGED A CLGA K NONE O OTHER IN INSP/MAINT 1 SO 19 141WE 46661 DURING C-CHECK, THE NR 2 ENGINE THRUST REVERSER LEFT COWL SKIN WAS FOUND DAMAGED ON LEADING EDGE. A DOUBLER WAS INSTALL ED IAW REO-G08284 AND A 8110-3 WAS ISSUED, DER DERT-511032-CE FAR 145 REPAIR AGENCY NR TIPR833K. THE AIRCRAFT WAS RETUR NED TO REVENUE SERVICE. (M) 2 L 7 3 4F RT A22WE 2002032800036 20020328 00036 NM 2002 3 28 2002F00331 1 20011201 A 5310 ACA3796501 STRUCTURE DOUG DC10 DC1040F 3023507 NM FUSELAGE CORRODED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 141WE 51705 46661 DURING C-CHECK, THE LEFT NOSE WHEEL WELL CHORD VERTICAL LEG WAS FOUND CORRODED AND BLENDED JUST PAST SRM REPAIRABLE LIMI TS. A REPAIR ANGLE WAS INSTALLED IAW TIMCO REO-G08344 REV IR AND REO G8336 REV IR. THE AIRCRAFT WAS RETURNED TO REVENU E SERVICE. (M) 2 L 7 3 4F RT A22WE 2002032800037 20020328 00037 NM 2002 3 28 2002F00332 1 20011201 A 5313 AJC7119501 LONGERON DOUG DC10 DC1040F 3023507 NM LT WING CRACKED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 141WE 46661 DURING C-CHECK, LONGERON 13L WAS FOUND CRACKED BETWEEN FASTENER HOLES AT CANTED STATION Y2153. LONGERON 13L WAS REPAIR ED. THE AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (M) 2 L 7 3 4F RT A22WE 2002032800038 20020328 00038 NM 2002 3 28 2002F00333 1 20011201 A 5310 ACA70161 STRUCTURE DOUG DC10 DC1040F 3023507 NM FUSELAGE CORRODED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 141WE 46661 DURING C-CHECK, THE FORWARD LT AIR CONDITIONING BAY CAP ANGLE AT STATION 595 BETWEEN LONGERON 47L AND 48L WAS CORRODED P AST SRM LIMITS. A REPAIR DOUBLER WAS INSTALLED ON THE EXTERIOR OF THE SKIN TO REINFORCE THE BLEND AREA. THE AIRCRAFT W AS RETURNED TO REVENUE SERVICE. (M) 2 L 7 3 4F RT A22WE 2002032800040 20020328 00040 NM 2002 3 28 2002F00334 1 20011201 A 7810 THRUST REVERSER DOUG DC10 DC1040F 3023507 NM NR 2 ENGINE DAMAGED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 141WE 51705 46661 DURING C-CHECK, THE NR 2 ENGINE THRUST REVERSER LEFT COWL SKIN WAS FOUND DAMAGED ON LEADING EDGE. A DOUBLER WAS INSTALL ED IAW REO-G08284. THE AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (M) 2 L 7 3 4F RT A22WE 2002032900022 20020329 00022 NM 2002 3 29 ASAA0110561 1 20010826 A 5311 65C33722 FRAME BOEING 737 737210C 1384459 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME CHORD AT BODY STATION 727, STRINGER 18L-27L CRACKED. REPAIRED PER EA. (M) 2 L 7 2 4F A16WE 2002032900023 20020329 00023 NM 2002 3 29 ASAA0110562 1 20010826 A 5320 69353503 STRINGER CLIP BOEING 737 737210C 1384459 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER CLIP AT BODY STATION 927, STRINGER 27L CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2002032900024 20020329 00024 NM 2002 3 29 ASAA0110563 1 20010826 A 5313 6552928584 STRINGER BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER 20L AT BS 727-727A, CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2002032900025 20020329 00025 NM 2002 3 29 ASAA0110564 1 20010826 A 5310 6546549 SHEAR TIE BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND SHEAR TIE AT BS 767, STRINGER 25L-27L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2002032900077 20020329 00077 NM 2002 3 29 ASAA0110634 1 20011030 A 5260 60605001 CONTROL HANDLE BOEING 737 7372X6C 1384552 NM AIR STAIR OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 ANC - CREW REPORTED AIRSTAIR CONTROL HANDLE DIFFICULT TO OPERATE. ADJUSTED STOP DOOR LATCH FITTING, THEN OPS CHECKED GO OD. (M) 2 L 7 2 4F RT A16WE 2002032900078 20020329 00078 NM 2002 3 29 ASAA0110646 1 20011127 A 5310 6545812172 SHEAR TIE BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND SHEAR TIE AT BODY STATION 328, STRINGER 26R CORRODED. REPAIRED SHEAR TIE PER SRM. (M) 2 L 7 2 4F RT A16WE 2002032900079 20020329 00079 NM 2002 3 29 ASAA0140134 1 20011029 A 5310 654795998 DOOR FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 PAE - DURING C-CHECK, FOUND AFT CARGO BAY BS 792, RBL 24-28 WL 160 DOOR FRAME PLATE IS CORRODED. REMOVED AND REPLACED P LATE IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002032900080 20020329 00080 NM 2002 3 29 ASAA0140162 1 20011127 A 5310 65C16121 ATTACH FITTING BOEING 737 7374Q8 138447Q NM GIRT BAR CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 PAE - DURING SI CHECK, FOUND CORROSION ON GIRT BAR ATTACHMENT AT BS 312, LBL 53, WL 209. REPLACED PER SRM. (M) 2 L 7 2 4F RT A16WE 2002032900081 20020329 00081 NM 2002 3 29 ASAA0140163 1 20011127 A 5320 6517688U175 SILL BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 PAE - DURING SI CHECK, FOUND CORROSION ON MOP SILL AT BS 307-344, LBL 55 AND WL 208. REPLACED MOP SILL PER SRM. (M) 2 L 7 2 4F RT A16WE 2002032900127 20020329 00127 NM 2002 3 29 USAA020076 1 20010219 A 5330 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 37849 23886 CLT - FOUND SKIN CRACKED 2 INCHES, FORWARD OF FS 727F 2 INCHES ABOVE S25R. INSTALLED 8 INCHES BY 12 INCHES DOUBLER PER SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2002032900133 20020329 00133 NM 2002 3 29 USAA020104 1 20011230 A 5400 ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 46617 23314 PIT - FOUND ANGLE CRACKED 1 INCH, VERTICAL ANGLE AT STATION 363. DEFECTIVE PART REPLACED WITH IDENTICAL PART. REPLACED CHANNEL PER NR 313A1355. (M) 2 L 7 2 4F RT A16WE 2002032900134 20020329 00134 NM 2002 3 29 USAA020105 1 20011230 A 5400 CHANNEL BOEING 737 7373B7 1384580 NM NACELLE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 392US 46617 23314 PIT - FOUND CHANNEL CRACKED 12 INCHES, STATION 345-363. DEFECTIVE PART REPLACED WITH IDENTICAL P/N, REPLACED CHANNEL PE R NR 313A1355. (M) 2 L 7 2 4F RT A16WE 2002032900188 20020329 00188 NM 2002 3 29 COOSDR010127 1 20011107 A 5330 SKIN BOEING 727 7272M7 138407S NM FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 79751 21457 FUSELAGE SKIN PANEL AND STRINGER 28R CORRODED LOCATED FROM BS 580 TO BS 600. BELOW FWD CARGO COMPARTMENT DOOR. 2 L 7 3 4F A3WE 2002040100005 20020401 00005 NM 2002 4 1 COOSDR02016 1 20010308 A 5753 FITTING BOEING 727 7272F9 138407D NM PWA JT8 JT8D17 52049 NE MID FLAP CORRODED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 199AJ 21426 FITTING, LEFT WING, OUTBOARD MID-FLAP INBOARD/OUTBOARD FITTINGS FLAP CARRIAGE WITH CORROSION. 2 L 7 3 4F 4 F RT A3WE E2EA 2002040100021 20020401 00021 EA 2002 4 1 AMW2002F00000 2 20010519 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA RIGHT OVERHEATED A AMWA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 CE 07 110YV UE110 DURING TAKEOFF AND CLIMB, RIGHT ENGINE WENT TO 900 DEGREES. AIRCRAFT DEVERTED TO ALTERNATE AIRPORT AND LANDED WITH NO F URTHER INCIDENT. 2 L 7 2 4T 3 T RT A24CE E2NE 2002040100024 20020401 00024 CE 2002 4 1 B082002F00000 1 20011101 A 2722 4322997 ACTUATOR LEAR 45 45LEAR 5170805 CE GARRTT TFE731 TFE731* 01518 WP RUDDER INOPERATIVE B B08R K NONE O OTHER IN INSP/MAINT 1 SW 05 419FX 541 125 DURING A MAINTENANCE VISIT AND PREPARATION TO PERFORM ENGINE RUNS, A MECHANIC NOTICED AN ABSENCE OF RESISTANCE AT THE PI LOTS RUDDER PEDALS WHILE SETTING THE PARKING BRAKE. AFTER AN UNSUCCESSFUL ATTEMPT TO ADJUST THE PILOTS RUDDER POSITION ACTUATOR, A MECHANIC GAINED ACCESS TO THE ACTUATOR AND FOUND THAT THE ACTUATOR ADJUSTMENT ROD WAS BENT. THIS COULD LEAD TO A LOSS OF BRAKING, RUDDER CONTROL AND NOSE WHEEL STEERING CAPABILITY. DUAL RUDDER PEDAL ADJUSTMENT ACTUATORS ARE IN STALLED BELOW THE COCKPIT FLOORBOARDS IMMEDIATELY ABOVE THE RUDDER CONTROL BELLCRANKS, AND PROVIDE FOR INDEPENDENT ADJUS TMENT OF RUDDER PEDAL POSITION. 2 L 7 2 4F 4 F RT T00008WI E6WE 2002040100031 20020401 00031 CE 2002 4 1 CWQ2002F00000 1 20011220 A 2450 S31065 TRANSORB CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL AVIONICS, JBOX BURNED E CWQR K NONE O OTHER IN INSP/MAINT 1 GL 05 948QS 613 7500149 DISPLAY UNITS 4 AND 5, FMS 2 SCREEN AND RADIO CONTROL UNIT SCREEN BLANK. AVIONICS FAN INSPECTION AND CAS MESSAGES DISPL AYED. CAUSE OF DISCREPENCY APPEARS TO BE TRANSORB (PN S3106-5) WIRED INTO QUICK DISCONNECT FITTING CONNECTED TO THE RIG HT SIDE AVIONICS RELAY KZ002 (PN SM400D64). TRANSORB WAS BURNED ALMOST IN HALF, WIRES INTO DISCONNECT FITTING HAD NO I NSULLATION LEFT ON THEM , 8 INCHES BACK FROM CANNON PLUG TO WIRE BUNDLE. NO CIRCUIT BREAKERS POPPED IN EITHER SITUATION . REMOVED AND REPLACED RELAY (PN SM400D64), CONNECTOR (PN MS27473E8F35S), AND TRANSORB (PN S3106-5) ALSO REPLACED WIRIN G. INVESTIGATE WIRING DIAGRAMS TO FIND OUT WHY CIRCUIT BREAKERS HAVE NOT BEEN TRIPPED AT TIME OF MALFUNCTIONS. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2002040100052 20020401 00052 EU 2002 4 1 G1X2002F00004 1 20010128 A 3240 5012889 CALIPER ISRAEL GALAXY GALAXY 4500307 EU BRAKE ASSY LEAKING B G1XR K NONE K FLUID LOSS IN INSP/MAINT 1 SW 19 294GA 25 052 SCRAPER SEALS FAILING. 3 AIRCRAFT S BRAKE ASSEMBLIES SO FAR. SCRAPER SUPPORTS PISTON GUIDE AND IS COMING UNSEATED. TH E GUIDE THEN SHIFTS IN THE BORE AND COCKS THE PISTON SIDEWAYS AND THE SEAL BECOMES INEFFECTIVE. WAITING ON ENGINEERING DISPOSITION FROM ABSC. RECOMMEND INSPECT AND REPLACE. 2 L 7 2 4F RT A53NM 2002040100086 20020401 00086 WP 2002 4 1 JRA2002F00000 1 20010714 A 2910 H2445 LINE DOUG DC3 DC3 3021401 WP PWA PT6 PT6A65AR 52043 NE LT MLG RUPTURED A JRAA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 GL 11 376AS 27047 PRIOR TO TAKEOFF, RUPTURED ITS LEFT-HAND MAIN WHEEL BRAKE EXPANDER TUBE. RUPTURE CAUSED HYDRAULIC FLUID LOSS AND LEFT B RAKE LOSS. AC WAS STOPPED WITH REVERSE THRUST AND ENGINES SHUT DOWN. NORTH OPS WAS ADVISED OF SITUATION BY VICTOR RADI O. SMOKE JUMPERS AND SPOTTERS WERE DEPLANED (AT INTERSECTION OF RUNWAY 16 THRESHOLD AND RUNWAY A) AND DRIVEN BACK TO TH E SHERPA AIRCRAFT BY USFS VANS. THE DC-3TP WAS TOWED BACK TO U.S.F.S. RAMP BY TUG AND MAINTENANCE. ENTIRE LH MAIN WHE EL, TIRE, AND BRAKE ASSEMBLY WAS REPLACED WITH AN OVERHAULED UNIT. LEAKING BRAKE/HYDRAULIC FLUID WAS CONTAINED AND CLEA NED UP. NEXT MORNING AT 0800 HRS. A TAXI CHECK WAS PERFORMED TO DOUBLE-CHECK SYSTEM. ALL OPERATIONS WERE NORMAL. 2 L 7 2 4R 4 T A669 E4EA 2002040100088 20020401 00088 WP 2002 4 1 JRA2002F00001 1 20010712 A 5343 2403110100145 BEAM CVAC 240 24027 2422642 WP PWA R2800 R2800* 52026 NE MLG WW CRACKED A JRAA K NONE O OTHER IN INSP/MAINT 1 GL 11 152JR 283 A CRACK WAS DISCOVERED IN THE NOSE GEAR WHEEL WELL BEAM ANGLE IN THE PROCESS OF PERFORMING A PRE-FLIGHT INSPECTION ON TH E AIRCRAFT. 2 L 7 2 4R 4 R A793 5E8 2002040100143 20020401 00143 NE 2002 4 1 REX2002F00000 2 20011212 A 7210 7758001 GEARBOX SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE REDUCTION DAMAGED A REXA E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 SO 25 110PX 32615 32615 340A023 IN CRUISE FLIGHT, CREW HEARD A LOUD BANG. THIS WAS FOLLOWED BY ERRATIC RIGHT HADN ENGINE OPERATION WITH A LOSS OF PROPE LLER GEARBOX OIL PRESSURE. THE RIGHT ENGINE WAS SHUT DOWN USING THE APPROVED EMERGENCY CHECKLIST, AND AN EMERGENCY WAS DECLARED. LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE CONFIRMED RIGHT PROPELLER GEARBOX FAILURE. ENGINE AND GEA RBOX REPLACED AND SENT OUT FOR REPAIR. 2 L 7 2 4T 4 T RT A52EU E8NE6 2002040100149 20020401 00149 NE 2002 4 1 RG22002F00000 2 20010716 A 7250 LPT219 MODULE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE LP TURBINE FAILED B RG2R K NONE O OTHER IN INSP/MAINT 1 SO 19 491SH 27788 49150 725634 RECEIVED AT REPAIR STATION WITH UNCONTAINED TURBINE FAILURE. OPERATOR REPORTED THAT FAILURE OCCURED DURING AN APPROACH TO AIRPORT. AIRCRAFT ENCOUNTERED WINDSHERE WHEN AN ENGINE OVERBOOSTED. FAILURE OCCURE TO ENGINE 2 WHEN CUT BACK IN POW ER. UNDER INVESTIGATION. 2 L 7 2 4F 4 F A6WE E9NE 2002040200006 20020402 00006 EU 2002 4 2 UXF2002F00000 1 20011116 A 3320 63355604591 LAMP BRAERO 1000 BAE1251000 1500287 EU PWA 305 PW305 NE CABIN INOPERATIVE B UXFR K NONE L NO TEST IN INSP/MAINT 1 NE 03 119U 259007 FLUORESCENT LAMP 22 INCHES LONG, MODEL F00100 HAS EVIDENCE OF SEVERE OVERHEATING (CHARRING) AT ONE END OF LAMP. LAMP US ED IN GALLEY/CABIN LIGHTING SYSTEM. 2 L 7 2 4F 4 F RT A3EU E35NE 2002040200007 20020402 00007 EU 2002 4 2 VO22001F00000 1 20011213 A 1430 66074102005 SCREW ISRAEL GALAXY GALAXY 4500307 EU CARGO BAY IMPROPER PART A VO2R A UNSCHED LANDING A J FLAME/FIRE WARNING INDICATION NR NOT REPORTED 1 WP 01 110HA 37 035 IN FLIGHT AFT BAGGAGE FIRE WARNING LIGHT WENT OFF AND THE PRESSURIZATION SYSTEM TO THE AIRCRAFT BAGGAGE AREA WAS ISOLATE D. AFTER LANDING THE RIGHT HAND BAGGAGE PANEL WAS REMOVED AND FOUND THAT THE HEATING ELEMENT CANNON PLUG BACKSHELL SCRE WS WERE TOO LONG AND HAD WORKED THROUGH THE HEATING ELEMENT CAUSING IT TO SHORT OUT CAUSING A FIRE. DURING REPLACEMENT OF THE BAGGAGE PANEL, IT WAS NOTED THAT BURNING OF THE FABRIC COVERING, HEATED PANEL AND INSULATION BAG COVERED AN AREA OF APPROXIMATELY 6 X 6. CIRCUIT PROTECTION DEVICE (CB) DID NOT PROTECT THE CIRCUIT. 2 L 7 2 4F RT A53NM 2002040200008 20020402 00008 EU 2002 4 2 VO22002F00000 1 20011227 A 3500 38911050060 HOSE ISRAEL GALAXY GALAXY 4500307 EU OXYGEN SYS FAILED B VO2R O OTHER O OTHER NR NOT REPORTED 1 GL 19 122GV 27 043 THIS HOSE FAILED WHERE THE HOSE MEETS ITS END FITTING. THE HOSE COMPLETELY SEPARATED FROM THE END FITTING. THE HOSE WA S DATED O1/01. REPLACED THE SUSPECTED HOSES WITH NEW HOSES (DO NOT USE HOSES THAT THE MFG DATE IS 12/00 THE REMOVED HOS ES RETURN TO IA) 2 L 7 2 4F RT A53NM 2002040200009 20020402 00009 EU 2002 4 2 VO22002F00001 1 20010810 A 1430 MS20450 RIVET ISRAEL GALAXY GALAXY 4500307 EU PWA 306 PW306B NE STRAKES WRONG PART B VO2R K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 19 62GX 031 FOUND NUMEROUS RIVETS THAT ATTACH THE STRAKES TO THE AFT FUSELAGE TO BE MS20450 TUBULAR RIVETS, NOT THE MS20470AD (BJ5) RIVETS CALLED FOR ON DRAWING. THE MS20450 TUBULAR RIVETS WERE OBSOLETED IN THE UNITED STATES IN 1968. GALAXY ENGINEERI NG WAS CONTACTED AND DETERMINED THE AIRCRAFT COULD OPERATE TO ITS NEXT A INSPECTION, WHEN MFG ENGINEERING WILL HAVE TO DECIDE ON RIVET REPLACEMENT. 2 L 7 2 4F 4 F RT A53NM E35NE 2002040200017 20020402 00017 CE 2002 4 2 YAD2002F00000 1 20011206 A 3297 G7C22 WIRE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE MLG CONNECTOR DAMAGED A YADA O OTHER J WARNING INDICATION NR NOT REPORTED 1 AL 03 1553C 32582 UC24 AFTER TAKEOFF FROM BARROW, LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT CONTINUED TO ANCHORAGE AND MADE AN UNEVENTFUL L ANDING. MAINTENANCE LOCATED AND REPLACED WIRE G7C22, DUE TO HIGH RESISTANCE, BETWEEN LEFT FUSELAGE AND CONNECTOR J107. 2 L 7 2 4T 4 T RT A24CE E4EA 2002040200027 20020402 00027 GL 2002 4 2 BG72001F00000 3 20010402 A 6110 310002401 SEAL DOUG DC3 DC3C 3021457 WP PWA PT6 PT6A67R 52043 NE HARTZL HCB5M HCB5MA3 GL PROP SHAFT LEAKING A U6SG K NONE K FLUID LOSS IN INSP/MAINT 1 NM 05 115Z 33567 106138 THE LEFT ENGINE PROPELLER SHAFT SEAL WAS REPLACED DUE TO A SUSPECTED OIL LEAK. THE WRONG PART NUMBER SEAL WITH A SMALLE R OUTSIDE DIAMETER WAS INSTALLED. DURING THE MAINTENANCE GROUND RUN ON LEAKS WERE DETECTED. ONE HOUR INTO THE FLIGHT B ACK TO THE AIRCRAFTS BASE OF OPERATION THE PILOT NOTICED THE OIL PRESSURE DROPPING ON THE LEFT ENGINE. THE LEFT ENGINE WAS SHUT DOWN AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. A TOTAL OF ABOUT FIVE QUARTS OF OIL WERE LOST AT THE PR OP SHAFT SEAL WHEN THE SEAL SPUN DUE TO CONTACT WITH THE NUMBER 6 BEARING. SUBMITTED AS BG7P DESIGNATOR (INVALID DESIGN ATOR ERROR ON BG7P) 2 L 7 2 4R 4 T A669 E26NE 6 C P44GL 2002040200029 20020402 00029 EU 2002 4 2 QM72001F00000 1 20011205 A 5512 S5517000000460 SKIN AEROSP ATR42 ATR42* 8680900 EU PWA 120 PW120 NE HORIZIONTAL STAB DELAMINATED B QM7R K NONE O OTHER IN INSP/MAINT 1 EA 07 212AZ 9563 016 A DELAMINATION OF THE RIGHT HORIZONTAL STAB UPPER SKIN PANEL, WAS DETECTED DURING A GENERAL VISUAL INSPECTION OF THE AR EA. THE DEBOND IS OPP. 40 INCHES X 12 INCHES, 21 INCHES OUTBOARD OF THE ROOT AND CENTER FORWARD AND AFT. THERE IS NO S IGNIFICANT VISUAL DAMAGE OF THE AREA. PRESUED CAUSE IS FATIGUE AND OR CORROSION. 2 H 7 2 4T 4 T RT A53EU E20NE 2002040200030 20020402 00030 CE 2002 4 2 RX82002F00000 1 20011211 A 7160 INLET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A6 52043 EA LT ENGINE CRACKED E RX8R K NONE O OTHER IN INSP/MAINT 1 SO 15 70ZV UE70 LEFT ENGINE INLET (HOT LIP) CRACKED ON INNER RADIUS NEAR THE WELD. ON 1-6 DETAIL INSPECTIONS ARE FINDING THIS AREA TO B E A CHRONIC PROBLEM FOR CRACKING WE HAVE BEEN IN CONTACT WITH MFG. AIRCRAFT ENGINEERING AND HAVE OBTAINED FIELD REPAIR AUTHORITY BUT SUGGEST IT BECOME AN SRM REPAIR. 2 L 7 2 4T 3 T RT A24CE E4EA 2002040200032 20020402 00032 CE 2002 4 2 TIM2002F00004 1 20011204 A 5260 1145140304 CABLE BEECH 1900 1900 1154160 CE AIRSTAIR DOOR BROKEN E TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 172GA UB11 AIRSTAIR DOOR CABLE BROKE, ALLOWING ONE SIDE OF THE DOOR TO REMAIN UNLOCKED. 2 L 7 2 4T RT A24CE 2002040200048 20020402 00048 WP 2002 4 2 UPS02837387 1 20011230 A 5310 SHEAR TIE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:IN AFT PRESS BULKHEAD CANTED WEB 2 SHEAR TIES CRACKED RT SIDE BETWEEN L10 & L11 45 ANGLE BRACKET ATTACHE D TO CONTROL BULKHEAD CRACKED AS MARKED. REMOVED EXISTING FASTENER FOR REPAIR. FABRICATED REPAIR DOUBLER. INSTALLED D OUBLER. 2 L 7 4 4F RT 4A25 2002040200052 20020402 00052 WP 2002 4 2 UPS02837395 1 20011226 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 STA 55 FRAME IS CRACKED AT ROD ATTACH POINT LONG 23R. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTO UT. FABRICATED AND INSTALLED FRAME AND SEGMENT IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2002040200053 20020402 00053 WP 2002 4 2 UPS02837396 1 20011228 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 LEFT WING L/E UPPER SKIN HAS INTERGRANULAR CORROSION AT XFS 347.5 AND XFS 366.5. CUT OUT CORRODED AR EA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 57-2-1 FIG 38. 2 L 7 4 4F RT 4A25 2002040200054 20020402 00054 WP 2002 4 2 UPS02837397 1 20011227 A 5312 PRESSURE PANEL DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 STATION 683 BULKHEAD IS CRACKED AT RBL 5 AND RBL 12 AT WEB AT LOWER WING SPAR. CUT OUT DAMAGE, NDT V ERIFIED NO CRACKS AT CUT OUT. FABRICATED AND INSTALLED FILLER AND DOUBLERS IAW SRM 53-2-5 FIG 13. 2 L 7 4 4F RT 4A25 2002040200055 20020402 00055 WP 2002 4 2 UPS02837398 1 20011227 A 5753 PANEL DOUG DC8 DC873F 302199F WP T/E FLAP WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C23 LT WING TO BODY FAIRING AREA FLAP TE PANEL LWR SURFACE OF PANEL IS WORN AND HARDWARE IS NOT SECURE. REMOVED DAMAGED PANEL IAW DC8 SRM 51-3-0, PANEL DAMAGED BEYOND REPAIR, FABRICATED NEW 5 643117-5 PANEL IAW DAC DWG 5643 117 AND INSTALLED NEW PANEL IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2002040200056 20020402 00056 WP 2002 4 2 UPS02837400 1 20011227 A 5753 PANEL DOUG DC8 DC873F 302199F WP T/E FLAP WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C23 LT WING TO BODY FAIRING AREA FLAP T/E PANEL LWR SURFACE OF PANEL IS WORN AND HARDWARE IS NOT SECURE. REMOVED DAMAGED PANEL IAW DC8 SRM 51-3-0, PANEL DAMAGED BEYOND REPAIR. FABRICATED NEW 5643117-5 PANEL IAW DAC DWG 564 3117 AND INSTALLED NEW PANEL IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2002040200057 20020402 00057 WP 2002 4 2 UPS02837401 1 20011223 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C23 LW APPROX XFS 880 L/E CRACKED. CUT OUT CRACKED AREA IAW DC8 SRM 57-2-1. INSTALLED DOUBLER & FILLE R IAW DC8 SRM 51-1-21 & 51-1-15. 2 L 7 4 4F RT 4A25 2002040200061 20020402 00061 WP 2002 4 2 UPS02837408 1 20011226 A 5314 KEELBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C23 KEEL BEAM FIG LT NR 5 FIG AT STA 839 CRACKED IN I/B CORNER. R&R FITTING IAW DC8 SRM 51-1-20D 51-3-0 . 2 L 7 4 4F RT 4A25 2002040200063 20020402 00063 WP 2002 4 2 UPS02837415 1 20011228 A 5320 SPLICE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C23 AFT CARGO PIT AT FS 1040-1060 L31L SPLICE FITTING IS CRACKED AT AFT O/B END. R&R FITTINGS IAW DC8 S RM 51-1-20D, 51-1-11. 2 L 7 4 4F RT 4A25 2002040200064 20020402 00064 WP 2002 4 2 UPS02837416 1 20011227 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C23 AFT PIT ANGLE CORRODED AT FS 1160 AT L27L. R&R ANGLE IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002040200065 20020402 00065 WP 2002 4 2 UPS02837417 1 20011227 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C23 AFT PIT Z-ANGLE CRACKED AT FS 1180 L28L. REMOVED CRACKED Z-ANGLE, INSTALLED NEW FITTING P/N 3755842 -505N IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002040200066 20020402 00066 WP 2002 4 2 UPS02837418 1 20011228 A 5320 ATTACH FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C23 AFT LWR CARGO CRACKED ATTACH FITTING L33R STA 1230. REMOVED AND INSTALLED NEW ANGLE IAW DC8 SRM 51- 1-24 & 51-1-20D. 2 L 7 4 4F RT 4A25 2002040200070 20020402 00070 WP 2002 4 2 UPS02837427 1 20011230 A 5320 3750545U501 SPLICE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 STA 1040-1060 LONG 35L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750545, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002040200071 20020402 00071 WP 2002 4 2 UPS02837428 1 20011227 A 5342 ANGLE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 STATION 1766 AT LONG 2L FUSELAGE TO VERTICAL STAB ANGLE IS CRACKED AND CORRODED. FABRICATED AND INST ALLED REPAIR IAW SRM 53-2-5 FIG 16A. 2 L 7 4 4F RT 4A25 2002040200072 20020402 00072 WP 2002 4 2 UPS02837429 1 20011230 A 5320 3755842501 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 STATION 1200 LONG 34R-35R BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED BATHTUB FITTING IAW SRM 5 3-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 2002040200073 20020402 00073 WP 2002 4 2 UPS02837430 1 20011230 A 5320 3755843501N FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 STATION 1180 LONG 34R-35R BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755843, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002040200074 20020402 00074 WP 2002 4 2 UPS02837431 1 20011230 A 5320 37533061 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 STA 987 LONG 23L END FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3753306 AN D SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002040200075 20020402 00075 WP 2002 4 2 UPS02837432 1 20011230 A 5320 3750545U502 SPLICE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 STA 1040-1060 LONG 35R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750545 AND S RM 51-1-20D. 2 L 7 4 4F RT 4A25 2002040200077 20020402 00077 WP 2002 4 2 UPS02837434 1 20011230 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSLEAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 STA 1260-1280 LONG 34R IS CRACKED. REMOVED LONGERON, FABRICATED LONGERON REPAIR AND SPLICES AND INST ALLED IAW 8110-3 APPROVED DH SK 702-586. 2 L 7 4 4F RT 4A25 2002040200079 20020402 00079 WP 2002 4 2 UPS02837436 1 20011230 A 5320 3755842U2 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 STA 1230 BETWEEN LONG 27L-28L BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTIN G IAW DWG 3755842 AND SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 2002040200081 20020402 00081 WP 2002 4 2 UPS02837438 1 20011230 A 5540 565622911 WEB DOUG DC8 DC871F 302199D WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 RUDDER NR 2 HINGE CUT OUT LOWER WEB IS CRACKED AT ZR 161 APPROX. REMOVED, FABRICATED AND REPLACED WE B IAW DWG 5656229 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2002040200085 20020402 00085 WP 2002 4 2 UPS02837451 1 20011230 A 5320 4758514507 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 STA 1240 LONG 33R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4758 514 AND SRM 51-1-20D, 51-3-0. 2 L 7 4 4F RT 4A25 2002040200087 20020402 00087 WP 2002 4 2 UPS02837453 1 20011230 A 5320 3755843501N FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 BATHTUB FITTING IS CORRODED BEYOND LIMITS AT STA 1230 BETWEEN LONG 36 TO 35L. REMOVED AND REPLACED F ITTING IAW DWG 3755843 AND SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 2002040200088 20020402 00088 WP 2002 4 2 UPS02837454 1 20011230 A 5320 37552222 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 FLOORBEAM ATTACH FITTING IS CRACKED AT STA, 742 LBL 24. REMOVED AND REPLACED FITTING IAW DWG 3755222 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002040200092 20020402 00092 NM 2002 4 2 VNAA0112009 1 20011210 A 3020 29S5D5240213 BOOT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NR 1 ENGINE DEBONDED A VNAA E ENGINE SHUTDOWN A FLAME/FIRE CR CRUISE 1 GL 07 429JS 13046 3043 APPROX 50 NM NORTH OF TRI, THE CAPTAIN NOTIFIED DISPATCH NR 1 ENG WAS SHUT DOWN DUE TO THE F/A REPORTING FLAMES COMING O UT OF THE BACK OF THE ENG. CAPT DID NOT SEE THE FLAMES OR HAVE ANY INDICATION ON THE RED WARNING PANEL. THE CAPT STATE D IT SEEMED THAT THE INTAKE BOOT WAS FLAPPING INSIDE THE INTAKE. THE CAPT DECLARED AN EMERGENCY, DIVERTED TO TRI. DISP ATCH NOTIFIED TRI OF THE EVENTS. MX SENT MECHANICS VIA A CHARTER FLIGHT TO INSPECT THE ENG AND DETERMINE THE PROBLEM. MX FOUND THE INTAKE DE-ICE BOOT DELAMINATED AND DEBONDED THEN REPLACED THE ENGINE INTAKE IN ACCORDANCE WITH DORNIER MM JIC 30-20-00. OPERATIONAL AND PERFORMANCE CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040200093 20020402 00093 NM 2002 4 2 VNAA0112022 1 20011229 A 3150 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 433JS 3047 DURING TAKEOFF, THE CREW RECEIVED A CHIME AND PUSHER FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE MESSAGE CLEARED BY ITSEL F AND FLIGHT 4169 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4169 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040300071 20020403 00071 WP 2002 4 3 UPS02837455 1 20011230 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 STA 1770 LONG 17R IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON IAW DWG 5649327 AND SRM 51-1 -20D, 51-3-0, 51-1-21. 2 L 7 4 4F RT 4A25 2002040300072 20020403 00072 WP 2002 4 3 UPS02837480 1 20011228 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 FUSELAGE SKIN IS CRACKED AT L-2 DOOR LOWER FWD CORNER STA 1620 AT LONG 20L. CUTOUT DAMAGE, NDT VERIF IED NO CRACKS. FABRICATED AND INSTALLED REPAIR IAW SRM 53-2-0 FIG 18. 2 L 7 4 4F RT 4A25 2002040300073 20020403 00073 WP 2002 4 3 UPS02837483 1 20011229 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 LONG 24L IS CRACKED PAST STOP DRILL STA 857-879. STOP DRILLED CRACK, NDT VERIFIED NO CRACKS. FABRIC ATED AND INSTALLED REPAIR IAW SRM 53-2-2 FIG 5. 2 L 7 4 4F RT 4A25 2002040300074 20020403 00074 WP 2002 4 3 UPS02837485 1 20011228 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 R-2 DOOR UPPER AFT CORNER FUSELAGE SKIN IS CRACKED AT STA 1660 LONG 11R. CUT OUT DAMAGE, NDT VERIFIE D NO CRACKS. FABRICATED AND INSTALLED REPAIR IAW SRM 53-2-0 FIG 16. 2 L 7 4 4F RT 4A25 2002040300075 20020403 00075 WP 2002 4 3 UPS02837486 1 20011230 A 5320 3755843502 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 BATHTUB FITTING IS CRACKED AT STA 1230 BETWEEN LONG 34R-35R. REMOVED AND REPLACED FITTING IAW DWG 37 55843, AND SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 2002040300076 20020403 00076 WP 2002 4 3 UPS02837487 1 20011230 A 5310 SHEAR TIE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 STA 1860 LONG 3R CLIP/SHEAR TIE IS CRACKED. STOP DRILLED CRACK, NDT VERIFIED NO CRACKS. FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 2002040300077 20020403 00077 WP 2002 4 3 UPS02837489 1 20011226 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 STA 70 FRAME IS CORRODED BEYOND LIMITS AT LONG 35R TO 36. CUT OUT DAMAGED AREA, FABRICATED AND INSTA LLED REPAIR IAW SRM 53-2-5 FIG 8C. 2 L 7 4 4F RT 4A25 2002040300079 20020403 00079 WP 2002 4 3 UPS02837495 1 20011228 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C23 AFT CARGO PIT FS 1160 BETWEEN LONG 34R 33R Z-FITTING IS CORRODED. REMOVED CORRODED IAW DC8 SRM 51-1 -20D, AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002040300081 20020403 00081 WP 2002 4 3 UPS02837497 1 20011227 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C23 AFT PIT ANGLE CORRODED AT FS 1160 BETWEEN L31L L35R. REMOVED ANGLE, REMOVED CORROSION IAW DC8 SRM 5 1-1-8. FABBED AND INSTALLED ANGLE IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002040300082 20020403 00082 WP 2002 4 3 UPS02837498 1 20011228 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C23 AFT ACCY COMP EVIDENCE OF CORROSION BETWEEN INTERCOSTAL AND FUSELAGE SKIN AT FS 1600 L25R & L26R. R EMOVED CORRODED AREA SKIN IAW DC8 SRM 53-2-1. FABBED REPAIR DOUBLER AND INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002040300083 20020403 00083 WP 2002 4 3 UPS02837508 1 20011229 A 5313 3646937U1 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 STA 1395 - 1447 LONG 34R IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED LONGERON SEGMENT IAW DWG 36 46937 AND SRM 53-1-0, 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2002040300084 20020403 00084 WP 2002 4 3 UPS02837509 1 20011228 A 5312 PRESSURE PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C23 MAIN CABIN AT STA 864 AND RBL 40 - 49 PULLEY BRACKET BASE PLATE HAS SHEARED RIVETS AND CORROSION ON MLG W/W CEILING AND SUBFLOOR AS SEEN FROM RT W/W. REPAIRED AREA IAW REO-G08475. 2 L 7 4 4F RT 4A25 2002040300085 20020403 00085 WP 2002 4 3 UPS02837517 1 20011228 A 5312 PRESSURE PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C23 MAIN CABIN AT STA 922 & RBL 67 SUBFLOOR PANEL FITTING HAS CRACK AND CORROSION. REPAIRED AREA IAW RE O G08477. 2 L 7 4 4F RT 4A25 2002040300089 20020403 00089 WP 2002 4 3 UPS02837528 1 20011227 A 5713 STRINGER DOUG DC8 DC873F 302199F WP WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C23 LW LWR SKIN AT XRS 453, STRINGER 64 IS CRACKED. FABBED AND INSTALLED FILLER IAW EO DC8-5730-9004. FABBED AND INSTALLED DOUBLER IAW EO DC8-57 30-9004. 2 L 7 4 4F RT 4A25 2002040300106 20020403 00106 SW 2002 4 3 2002F00355 1 20010117 A 2910 LINE SWRNGN SA227 SA227AC 8780603 SW HYD SYSTEM CHAFED A BSAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 NM 05 27465 AC755B MWH - FLT 6003 - THE CREW NOTICED A SMELL AND RED HAXE IN THE COCKPIT. IMMEDIATELY AFTER THAT BOTH HYD PRESSURE LIGHTS CAME ON AND HYDRAULIC PRESSURE DROPPED TO 0. THE GEAR WAS MANUALLY EXTENDED. THE CREW RETURNED TO STATION WITH NO FURT HER PROBLEMS. HYDRAULIC PRESSURE WAS LOST DUE TO HYDRAULIC LEAK. FOUND LINE CHAFED THROUGH IN THE AREA UNDER THE J BOX . LINE DIDN'T LEAK UNTIL FULL SYSTEM PRESSURE WAS APPLIED. LINE WAS REPAIRED BY SPLICING. (M) 2 L 7 2 4T RT A8SW 2002040300108 20020403 00108 SW 2002 4 3 2002F00357 1 20011216 A 5310 SEAL SWRNGN SA227 SA227AC 8780603 SW PAX DOOR DAMAGED A BSAA G O2 MASK DEPLOYED J WARNING INDICATION CL CLIMB 1 NM 05 160MC AC733B FLT 2588 - HLN - DURING CLIMB-OUT, CABIN PRESSURE WAS LOST. CREW AND PASSENGERS UTILIZED OXYGEN MASKS AND FLIGHT CONTIN UED TO DESTINATION. CABIN DOOR SEAL HAD A HOLE IN IT. INITIALLY WAS DEFERRED PER MEL. FOUND HOLE POKED IN PASSENGER D OOR SEAL, REPLACED DOOR SEAL. (M) 2 L 7 2 4T RT A8SW 2002040300110 20020403 00110 WP 2002 4 3 AALA20012059 1 20011125 A 2560 1001191 FLASHLIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 568AA 49349 DFW - DURING OVERNIGHT MAINTENANCE, PORTABLE EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED PORTABLE EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2002040300111 20020403 00111 WP 2002 4 3 AALA20012087 1 20011202 A 3350 8039001 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 269AA 49292 DFW - DURING OVERNIGHT MAINTENANCE, CEILING MOUNTED EMERGENCY EXIT LIGHT AT SEAT 8D THROUGH 11D DIM. REPLACED CEILING M OUNTED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040300112 20020403 00112 WP 2002 4 3 AALA20012089 1 20011203 A 3350 8039001 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 486AA 49679 DEN - DURING OVERNIGHT MAINTENANCE, RAR CABIN OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED OVERHEAD EMERGENCY E XIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040300113 20020403 00113 WP 2002 4 3 AALA20012092 1 20011203 A 3350 AB51 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 591AA 53254 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN AFT CABIN SECTION DIM. REPLACED EMERGENCY EXIT BATTERY PACK . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2002040300114 20020403 00114 WP 2002 4 3 AALA20012093 1 20011203 A 3350 8039001 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 591AA 53254 DFW - DURING OVERNIGHT MAINTENANCE, CEILING MOUNTED EMERGENCY EXIT LIGHT AT ROW 22 THROUGH 28 INOPERATIVE. REPLACED CEI LING MOUNTED EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2002040300115 20020403 00115 WP 2002 4 3 AALA20012094 1 20011201 A 3350 8039001 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7536A 49990 DFW - DURING OVERNIGHT MAINTENANCE CEILING MOUNTED EMERGENCY EXIT LIGHT AT ROW 18 THROUGH 21 INOPERATIVE. REPLACED CEIL ING MOUNTED EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040300116 20020403 00116 WP 2002 4 3 AALA20012095 1 20011201 A 3350 8039001 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 467AA 49597 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS AND TAIL CONE INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK FOR AIRSTAIRS AND TAILCONE LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040300117 20020403 00117 WP 2002 4 3 AALA20012100 1 20011202 A 3350 8039001 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 474 49649 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS ROWS 12 THROUGH 16 INOPERATIVE. REPLACED OVERHEAD EM ERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040300118 20020403 00118 WP 2002 4 3 AALA20012101 1 20011202 A 3350 8039001 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 575AM 53152 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS ROW 7 THROUGH 10 INOPERATIVE. ADJUSTED OVERHEAD EMER GENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040300119 20020403 00119 WP 2002 4 3 AALA20012141 1 20011205 A 3350 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 435AA 49453 SEA - DURING OVERNIGHT MAINTENANCE, FORWARD GALLEY EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FORWARD GALLEY EMERGENCY LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2002040300120 20020403 00120 WP 2002 4 3 AALA20012142 1 20011204 A 3350 AB51 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 565AA 49347 DFW - DURING OVERNIGHT MAINTENANCE, ENTRY CEILING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTE RY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2002040300121 20020403 00121 WP 2002 4 3 AALA20012163 1 20011217 A 3397 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70401 49312 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT CABIN INOPERATIVE. TIGHTENED EMERGENCY EXIT LIGHT CONNE CTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040300148 20020403 00148 NM 2002 4 3 GAIA02023OP 1 20010302 A 3350 LIGHT BOEING 727 727251 138408H NM CABIN INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 278US 21157 DURING ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT THE FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. CLEANED AND RE-RACKED THE FORWARD ENTRY EMERGENCY EXIT LIGHT PACK. OPERATIONALLY CHECKED NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002040300183 20020403 00183 NM 2002 4 3 DLM88020303 1 20010314 A 2130 321417611 THERMOSTAT DOUG MD88 MD88 3023688 NM RT ENGINE FAILED A DALA I CABIN DEPRESSURIZATION O OTHER CL CLIMB 1 SO 27 949DL 49880 CREW DECLARED EMERGENCY - UNABLE TO MAINTAIN CABIN ALTITUDE WHEN CLIMBING FROM 35K TO 37K WITH FLOW LT ON AND 1200FPM CABIN RATE OF CLIMB- MAX CABIN ALTITUDE WAS 11K. NO MASKS DEPLOYED. AT 10K WITH OUTFLOW VALVE FULLY CLOSED CABIN ALT WAS 1K WITH 4.5PSID MAINTAINED. REPLACED RT AUG VALVE ANTICIPATOR THERMOSTAT 2 L 7 2 4F RT A6WE 2002040400001 20020404 00001 NM 2002 4 4 AALA20010261 1 20011204 A 5753 STRUCTURE BOEING 767 767323 1385205 NM TEL FLAPS CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 39367 25194 AFW - FLAP ATTACH HOLES WERE REAMED TO REMOVE CORROSION. FABRICATE FREEZE FIT PLUGS FROM 7075-T6 IN ORDER TO ACHIEVE A MIN .001 INCH INTERFERENCE FIT PER RF. ALODINE PLUGS AND INSTALL WET WITH BM55-95 SEALANT. (M) 2 L 7 2 4F RT A1NM 2002040400073 20020404 00073 NM 2002 4 4 VNAA0201021 1 20011124 A 3250 TILLER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NLG OUT OF ADJUST A VNAA O OTHER O OTHER LD LANDING 1 GL 07 430JS 3044 UPON LANDING, THE AIRCRAFT WENT TO THE RIGHT. BEFORE THE CREW COULD CORRECT THE DIRECTION, THE AIRCRAFT HIT A LANDING L IGHT. MAINTENANCE INSPECTED THE EXTERIOR OF THE AIRCRAFT AND FOUND NO DAMAGE, MAINTENANCE THEN INSPECTED THE NOSE WHEEL STEERING AND ADJUSTED THE NOSE WHEEL STEERING TILLER 5 DEGREES IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040500045 20020405 00045 CE 2002 4 5 2002F00363 1 20011224 A 2910 11438800013 POWERPACK BEECH 1900 1900D 1154162 CE HYD SYSTEM FAILED A AMWA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 CE 07 13ZV 79235 UE13 LANDING GEAR FAILED TO EXTEND ON APPROACH, AND LANDING INTO PIT. THE CREW EXTENDED THE GEAR THROUGH EMERGENCY MEANS, AN D LANDED AIRCRAFT WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE HYDRAULIC POWER PACK, AND HYDRAULIC PO WER ELECTRICAL RELAY, JACKED AND CYCLED GEAR WITH NO PROBLEMS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 2002010900057 20020109 00057 NM 2002 1 9 LCQ04 1 20011220 A 5313 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED B RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 BS 727 STRINGER 18A RIGHT, NOTED CRACK IN THE I/B STRINGER 18A WEB STRAP. CRACK EMANATING FROM HOLE AT BS 725.5 AND PRO PAGATING DOWN AND FORWARD (LOOKING AT FASTENERS HOLE FROM INSIDE WHEEL WELL, IT WOULD BE THE 8 O'CLOCK POSITION). 2 L 7 2 4F 0 A16WE 0 2002040800121 20020408 00121 WP 2002 4 8 GTIA010462 1 20010524 A 2740 591096271 JACKSCREW DOUG DC9 DC981 3022081 WP HORIZONTAL STAB LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 DTW - FOUND HORIZONTAL JACK SCREW FREE PLAY FAILED DIMENSION. REQUIRES REPLACEMENT. REMOVED AND REPLACED HORIZONTAL JA CK SCREW IAW MD 80 MM 27-40-01. OPS CHECK GOOD FREE PLAY .003 END PLAY .009. (M) 2 L 7 2 4F A6WE 2002040800185 20020408 00185 SW 2002 4 8 CA020402004 1 20011222 A 6320 212040143103 BEARING BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA M/R GEARBOX FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) TRANSMISSION REPLACED DUE METAL CONTAMINATION. 1 G 7 1 4U 4 U H4SW E22EA 2002040900051 20020409 00051 WP 2002 4 9 GTIA020135 1 20011211 A 7160 LINER DOUG DC9 DC982 3022082 WP NR 2 ENGINE CUT A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - NR 2 ENGINE INLET AT 9:00 POS HAS CUT IN NOISE SUPPRESSION LINER. CUT APPROX 4 INCHES LONG. CLEANED AND PREPARED SCRATCHED AREA. FILLED SCRATCH WITH ADHESIVE. (M) 2 L 7 2 4F A6WE 2002040900052 20020409 00052 WP 2002 4 9 GTIA020136 1 20011212 A 5730 FAIRING DOUG DC9 DC982 3022082 WP RT WING DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - NR 3 RIGHT FLAP FAIRING TWO DENTS, SEAL CRACKED, CHAFING SEVERAL SPOTS, TOOL MARKS. ALL CHAFED SPOTS WITHIN MATER IAL LOSS LIMITS EXCEPT FOR ONE. INSTALLED REPAIR IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002040900053 20020409 00053 WP 2002 4 9 GTIA020137 1 20011212 A 5730 FAIRING DOUG DC9 DC982 3022082 WP RT WING DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND RIGHT WING HINGE COVER NR 1 DENTS, CHAFING, SEAL DAMAGE, TOOL MARKS. CHAFFED AREA WAS FOUND TO BE OUT OF LI MITS. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER IAW MD80 SRM 57-03. (M) 2 L 7 2 4F A6WE 2002040900057 20020409 00057 WP 2002 4 9 GTIA020142 1 20011211 A 7160 INLET DOUG DC9 DC982 3022082 WP NR 2 ENGINE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - NR 2 ENGINE NOSE COWL INLET REPAIR NOT IAW SRM 1 O'CLOCK SRM. REMOVED DOUBLERS AND FILLER FROM NR 2 ENGINE NOSE C OWL INLET REPAIR. FORM NEW DOUBLERS AND FILLERS IAW MD80 SRM 51-10-2. (M) 2 L 7 2 4F A6WE 2002040900058 20020409 00058 WP 2002 4 9 GTIA020143 1 20011211 A 7160 INLET DOUG DC9 DC982 3022082 WP NR 2 ENGINE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - NR 2 ENGINE NOSE COWL INLET REPAIR NOT IAW SRM 8 O'CLOCK. REMOVED OLD FILLER AND DOUBLERS REPAIR. FORMED 2 NEW D OUBLERS IAW MD80 SRM 54-04. (M) 2 L 7 2 4F A6WE 2002040900059 20020409 00059 WP 2002 4 9 GTIA020144 1 20011212 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND PREVIOUS REPAIR AT FS 759 BETWEEN LONGERON 27R AND 28R REQUIRES FINGER DOUBLER INSTALLATION. REMOVED EXTERN AL DOUBLER. FABRICATED NEW EXTERNAL DOUBLER AND FILLER. INSTALLED NEW DOUBLER AND FINGER DOUBLER IAW DC9 SRM 51-30-1. (M) 2 L 7 2 4F A6WE 2002040900060 20020409 00060 WP 2002 4 9 GTIA020145 1 20011212 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND GOUGE AT FS 1300 BETWEEN LONGERON 18R AND 19R REQUIRES REPAIR IAW DC9/MD80 SRM 53-04. CUT DAMAGE AREA. FAB RICATED REPAIR PARTS DOUBLER AND FILLER. INSTALLED REPAIR PARTS IAW MD80 SRM 53-04. (M) 2 L 7 2 4F A6WE 2002040900061 20020409 00061 WP 2002 4 9 GTIA020146 1 20011212 A 5320 FITTING DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND PREVIOUS REPAIR AT L1 PASSENGER DOOR HOLD OPEN FITTING REQUIRES REPLACEMENT WITH REPAIR IN DC9/MD80 SRM 53-0 4. REMOVED TEMP REPAIR. FABRICATED MATERIAL REPAIR. INSTALLED REPAIR PER MD80 SRM 53-04. (M) 2 L 7 2 4F A6WE 2002040900062 20020409 00062 WP 2002 4 9 GTIA020147 1 20011212 A 5730 PANEL DOUG DC9 DC982 3022082 WP RT WING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - RIGHT WING PANEL CRACKED AT WING STATION 120 -XFS CAN BE SEEN THROUGH WING PANEL 1679C. REMOVED RIGHT WING PANEL AT STATION 120 - XFS PANEL 1679C. INSTALLED NEW PANEL AT RIGHT WING AT WING STA 120 -XFS PANEL 1679C IAW MD80 SRM 51-30 -2. (M) 2 L 7 2 4F A6WE 2002040900063 20020409 00063 WP 2002 4 9 GTIA020148 1 20011215 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FORWARD ENTRY WAY FLOORBOARDS FS 160 TO FS 195 PLUS X8 INCH TO PLUS 57 INCHES, AND FLOORBOARDS FS 195 TO FS 235 -X 22 INCH TO PLUS X57 INCHES HAS BLUE WATER STAINS AND ARE SPONGY. REMOVED 2 FLOORBOARD FS 195-256 LEFT 22-56. FABRICATE D TWO FLOORBOARDS FS 195-235, PNL. (M) 2 L 7 2 4F A6WE 2002040900064 20020409 00064 WP 2002 4 9 GTIA020149 1 20011228 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - PAX CABIN SEAT TRACK RIGHT INBOARD CORRODED FROM STATION 200-237. REMOVED SEAT TRACK FROM STATION 200-265 RIGHT I NBOARD. INSTALLED NEW SEAT TRACK IAW MD80 SRM 53-05. (M) 2 L 7 2 4F A6WE 2002040900067 20020409 00067 WP 2002 4 9 GTIA020152 1 20011208 A 5523 TAB DOUG DC9 DC982 3022082 WP ELEVATOR DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND RIGHT ELEVATOR ANTI-FLOAT TAB TOPSIDE HAS AREA OF DELAMINATION. BONDED REPAIR DOUBLER IAW DC9 MD80 SRM 51-7 0-2. (M) 2 L 7 2 4F A6WE 2002040900068 20020409 00068 WP 2002 4 9 GTIA020153 1 20011210 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND MID LOWER CARGO COMP CORRODED AT INTERCOASTAL ATTACH TO CARGO TRACK BETWEEN R28 R27 FROM STATION 769 TO STAT ION 750. R&R INTERCOSTAL PER MD80 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 2002040900069 20020409 00069 EU 2002 4 9 YENA200105 1 20011204 A 5330 SKIN AIRBUS 320 A320232 3930326 EU FUSELAGE DAMAGED A YENA K NONE O OTHER IN INSP/MAINT 1 EA 15 521JB 2484 1452 FLT 74, JFK TO PBI, AT PBI, ON A WALKAROUND THE FUSELAGE SKIN WAS FOUND DAMAGED AT FRAME 24, BETWEEN STRINGER 21 AND 22. THE DAMAGE CONSISTED OF A TEAR APPROX 4 INCHES IN THE FORE AND AFT DIRECTION AND APPROX 1.5 INCHES HIGH. 2 L 7 2 4F RT A28NM 2002040900070 20020409 00070 2002 4 9 YENA200106 4 20010920 A 2565 D30664105 LIGHT AIRBUS 320 A320232 3930326 EU EVAC SLIDE INOPERATIVE A YENA K NONE L NO TEST IN INSP/MAINT 1 EA 15 508JB 4232 4232 1257 AT JFK, R1 SLIDE FAILED EMERGENCY LIGHT TEST. REMOVED AND REPLACED SLIDE RAFT AT R1 POSITION, OPS CHECK OK IAW 25-62-44 . 2 L 7 2 4F RT A28NM 2002040900075 20020409 00075 WP 2002 4 9 GTIA020154 1 20011211 A 5320 STIFFENER DOUG DC9 DC982 3022082 WP FUSELAGE BUCKLED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - AFT PIT STATION 1007 10 INCHES ABOVE L28R, VERTICAL STIFFENER ON FORWARD BULKHEAD IS BUCKLED/BENT. R&R STIFFENER IAW MD80 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 2002040900076 20020409 00076 WP 2002 4 9 GTIA020155 1 20011211 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - AFT PIT STATION 1015 L23L, CORROSION AROUND LONGERON TO SKIN FASTENERS. INSTALLED LONGERON AND SPLICE REPAIR IAW MD80 SRM 53-02. (M) 2 L 7 2 4F A6WE 2002040900077 20020409 00077 WP 2002 4 9 GTIA020156 1 20011212 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - AFT PIT STATION 1117 L28R CORROSION ON LOWER SURFACE OF FLOOR SUPPORT, FORWARD AND AFT SIDE. MATERIAL OUT OF LIMI TS. REMOVED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002040900078 20020409 00078 WP 2002 4 9 GTIA020157 1 20011212 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - AFT PIT STATION 1155-1220 L29-28R WEB OVER DOOR THRESHOLD IS CORRODED ON UPPER AND LOWER SURFACE. DOOR BEAM FOUND TO BE OUT OF LIMITS. REMVOED DOOR BEAM FROM STATION 1111 TO 1250. REMOVED CORROSION FROM WEB OVER DOOR THRESHOLD AT S TATION 1155-1220. MATERIAL LOSS ON WEB FOUND TO BE OUT OF LIMITS. DRILLED UP AND LOCATED NEW DOOR BEAM PER SRM MD80 51 -10-4. (M) 2 L 7 2 4F A6WE 2002040900079 20020409 00079 WP 2002 4 9 GTIA020158 1 20011212 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND AFT PIT 1174 L28L - FLOOR SUPPORT ANGLE IS CORRODED ON LOWER SURFACE. FOUND OUT LIMITS. REMOVED FLOOR SUPP ORT ANGLE FROM STATION 1174. INSTALLED NEW ANGLE SUPPORT. (M) 2 L 7 2 4F A6WE 2002040900080 20020409 00080 WP 2002 4 9 GTIA020159 1 20011212 A 5320 SPLICE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - AFT PIT STATION 1174 L26L CORROSION ON FRAME SPLICE STRAP AND CORRODED FASTENERS IN STRAP. MATERIAL OUT OF LIMITS . FORMED PART. INSTALLED IAW MD80 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 2002040900081 20020409 00081 WP 2002 4 9 GTIA020160 1 20011213 A 5321 INSERT DOUG DC9 DC982 3022082 WP FLOORBOARD CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND PAX CABIN ENTRY WAY, UNDER LEFT FORWARD LAVATORY, FLOORBOARD HAS 4 CORRODED INSERTS. REMOVED FLOOR PANEL. FORMED FLOOR PANEL. (M) 2 L 7 2 4F A6WE 2002040900082 20020409 00082 WP 2002 4 9 GTIA020161 1 20011214 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND AFT PIT STATION 1322 L18L-L18R, CORROSION ON FRAME UPPER AND LOWER FLANGES AND WEB AT NUMEROUS LOCATIONS. F OUND 28L TO BE OUT LIMITS. REPAIRED FRAME. INSTALLED FRAME SPLICE IAW MD80 SRM 53-03. (M) 2 L 7 2 4F A6WE 2002040900099 20020409 00099 WP 2002 4 9 GTIA020162 1 20011214 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND AFT PIT STATION 1271 L23L-L23R, CORROSION ON FRAME UPPER AND LOWER FLANGES AND WEB. FABRICATED AND INSTALLE D REPAIR IAW MD80 51-10-3. (M) 2 L 7 2 4F A6WE 2002041000034 20020410 00034 WP 2002 4 10 UPS02837488 1 20011228 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 LT WHEEL FWD BULKHEAD LOWER WING CHORD STA 857 AT XCW 0 CRACK. STOP DRILLED CRACK, NDT VERIFIED NO C RACKS. FABRICATED AND INSTALLED REPAIR ANGLES AND FILLERS IAW 8110-3 APPROVED DH SK 702-461. 2 L 7 4 4F RT 4A25 2002041100017 20020411 00017 EU 2002 4 11 CA020401001 1 20010326 A 3232 125001 ACTUATOR FOKKER F28 F28MK1000 4990808 EU MLG DOOR FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) AFTER TAKEOFF MLG SELECTED UP. NLG RED LIGHT INDICATION. UPON EVALUATING SITUATION MASTER WARNING LIGHT ILLUMI NATED IN CONJUNCTION WITH UTILITY SYS LOW PRESSURE WARNING LIGHT. CREW COMPLETED ALT GEAR & FLAP EXTENSION IN CONJUNCTI ON WITH EMERGENCY CHECK LIST. A/C LANDED WITHOUT INCIDENT. RECTIFICATION UPON RELIEVING HEAD PRESSURE FROM UTILITY SYS , FOUND THAT NOSE LANDING GEAR DOOR ACTUATOR HOUSING HAD FAILED. ACTUATOR REPLACED AND SYS FUNCTION CHECKED WITHOUT FUR THER PROBLEMS NOTED. FOLLOWUP ACTION FAILURE OF HOUSING OF NOSEGEAR DOOR ACTUATOR CAUSE OF INCIDENT. 2 L 7 2 4F RT A20EU 2002041100093 20020411 00093 NM 2002 4 11 AALA20011844 1 20011006 A 3350 LIGHT BOEING 737 737823 13844BZ NM R1 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 949AN 29537 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT R1 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2002041100094 20020411 00094 NM 2002 4 11 AALA20011845 1 20011006 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 872AA 21384 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 15-20 INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2002041100095 20020411 00095 NM 2002 4 11 AALA20011956 1 20011023 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 881AA 21520 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 6 THROUGH 8 INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT SPLICE AT ROW 6 THROUGH 8. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2002041100097 20020411 00097 NM 2002 4 11 AALA20011959 1 20011027 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 919AN 29520 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT SOCKET AT 12F BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2002041100098 20020411 00098 NM 2002 4 11 AALA20011960 1 20011017 A 3350 LIGHT BOEING 727 727223 1384074 NM AFT AIRSTAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 887AA 21526 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT SOC KET AT AFT AIRSTAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2002041100099 20020411 00099 NM 2002 4 11 AALA20011978 1 20011102 A 3350 BATTERY BOEING 727 727227 1384078 NM AFT AIRSTAIRS CORRODED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 728AA 20735 ATL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT BAT TERY CONNECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2002041100100 20020411 00100 NM 2002 4 11 AALA20012017 1 20011106 A 3350 LIGHT BOEING 727 727223 1384074 NM AFT AIRSTAIR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 867AA 21372 DFW - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIRSTAIR EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2002041100101 20020411 00101 NM 2002 4 11 AALA20012028 1 20011108 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 889AA 21527 DFW - DURING OVERNIGHT MAINTENANCE FORWARD SECTION OF EMERGENCY EXIT ESCAPE PATH LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT ESCAPE PATH LIGHT STRIP IN FORWARD SECTION. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2002041100102 20020411 00102 NM 2002 4 11 AALA20012032 1 20011111 A 3350 LIGHT BOEING 727 727223 1384074 NM L1 DOOR LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 874AA 21386 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L1 LOOSE. SECURED EMERGENCY EXIT LIGHT AT L1. SYSTEM GROUN D CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2002041100103 20020411 00103 NM 2002 4 11 AALA20012047 1 20011116 A 3350 CONNECTOR BOEING 737 737823 13844BZ NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 903AN 29505 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 35D INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT CON NECTOR AT SEAT 25D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2002041100104 20020411 00104 NM 2002 4 11 AALA20012063 1 20011122 A 3350 CONNECTOR BOEING 727 727223 1384074 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 887AA 21526 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT SPLICE AT CONNECTOR . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2002041100105 20020411 00105 NM 2002 4 11 AALA20012071 1 20011126 A 3350 LIGHT BOEING 727 727227 1384078 NM VENTRAL STAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 728AA 20735 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT VENTRAL AFT STAIRS INOPERATIVE. REPLACED EMERGENCY EXIT LIG HT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2002041100106 20020411 00106 NM 2002 4 11 AALA20012150 1 20011207 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 940AN 30598 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 10 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT ROW 10. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2002041100107 20020411 00107 NM 2002 4 11 AALA20012161 1 20011214 A 3350 1001191 LIGHT BOEING 727 727223 1384074 NM AFT AIRSTAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 868AA 21373 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AS SEMBLY AT AFT AIR STAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2002041100108 20020411 00108 NM 2002 4 11 AALA20012180 1 20011226 A 3350 1001191 LIGHT BOEING 727 727223 1384074 NM AFT AIRSTAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 866AA 21371 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASS EMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2002041100130 20020411 00130 WP 2002 4 11 GTIA020163 1 20011214 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND AFT PIT STATION 1287 L23L-L23R, CORROSION ON FRAME UPPER AND LOWER FLANGES AND WEB AT NUMEROUS LOCATIONS. F ITTING OUT OF LIMITS. INSTALLED NEW FITTING PER SRM MD80 51-30-5. (M) 2 L 7 2 4F A6WE 2002041100131 20020411 00131 WP 2002 4 11 GTIA020164 1 20011214 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - AFT PIT STATION 1309 L18L-L18R, CORROSION ON FRAME UPPER AND LOWER FLANGES AND WEB AT NUMEROUS LOCATIONS. FABRICA TED 2 ANGLES AND 1 FRAME SEGMENT. REMOVED DAMAGE AREA. FABRICATED 2 PLATES. INSTALLED REPAIR PARTS IAW MD80 SRM 53-03 . (M) 2 L 7 2 4F A6WE 2002041100132 20020411 00132 WP 2002 4 11 GTIA020165 1 20011214 A 5320 ATTACH ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - MID LOWER CARGO COMPARTMENT RECEPTICAL CRACKED AT LEFT ANGLE ATTACH TO BULKHEAD STATION 788. ROUTED OUT CRACK. F ABRICATED REPAIR DOUBLER. INSTALLED PER MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002041100133 20020411 00133 WP 2002 4 11 GTIA020166 1 20011215 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - MID LOWER CARGO COMPARTMENT CORRODED AT LOWER AFT BELT FRAME PREVIOUS REPAIR STATION 750. REMOVED PREVIOUS REPAIR FROM BELT FRAME. BELT FRAME OUT OF LIMITS. FORMED AND DRILLED NEW REPAIR DOUBLER IAW SRM MD80 51-10-4 AND 53-01. (M) 2 L 7 2 4F A6WE 2002041100134 20020411 00134 WP 2002 4 11 GTIA020167 1 20011214 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - MID LOWER CARGO COMPARTMENT CORRODED SKINS BETWEEN STRINGERS 30 AT STRINGER STATION 712-731. REMOVED FRAME ASSEMB LY STATION 712. REMOVED FRAME ASSY STATION 731. REMOVED DAMAGED SKIN INTERNAL DOUBLER. FABRICATED REPAIR DOUBLERS AND FILLERS. INSTALLED DOUBLERS AND FILLER REPAIR. LOCATED AND DRILLED LONGERON 29 FROM STATION 665 TO 740. INSTALLED LO NGERON SPLICE AT ONGERON 27 STATION 731-750. LOCATED AND DRILLED LONGERON SPLICE AT LONGERON 28 STATION 750-731. INSTA LLED LONGERON SPLICE AT LONGERON 28, STATION 731-750. INSTALLED LONGERON 29L SPLICES. INSTALLED LONG SECTIONS OF LONGER ON 27R, 28R, 29R, 30 INSTALLED L29L STATION 712-745. (M) 2 L 7 2 4F A6WE 2002041100135 20020411 00135 WP 2002 4 11 GTIA020168 1 20011214 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - MID LOWER CARGO COMPARTMENT CORRODED AT INTERCOSTAL BETWEEN STATION 693 TO STATION 674. REMOVED CORROSION ON INTE RCOSTAL AND FOUND TO BE OUT OF LIMITS. FORMED INTERCOSTAL. INSTALLED INTERCOSTAL IAW SRM MD80 51-30-5. (M) 2 L 7 2 4F A6WE 2002041100136 20020411 00136 WP 2002 4 11 GTIA020169 1 20011214 A 5313 STRINGER DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - MID LOWER CARGO COMPARTMENT CORRODED AT STRINGER L29L FROM STATION 693 TO STATION 674. AFTER BLENDING MATERIAL FO UND TO BE OUT OF LIMITS. REMOVED LONGERON FROM STATION 664-741. LOCATED AND DRILLED HOLE IN NEW SECTION. (M) 2 L 7 2 4F A6WE 2002041100137 20020411 00137 WP 2002 4 11 GTIA020170 1 20011214 A 5310 STRUCTURE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - MID LOWER CARGO COMPARTMENT CORRODED AT STATION 693 TO STATION 674 AT 655. REMOVED CORROSION. TEE ANGLE IAW MD80 SRM 51-30-2 AND 51-30-1. (M) 2 L 7 2 4F A6WE 2002041100181 20020411 00181 WP 2002 4 11 GTIA020171 1 20011214 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - MID LOWER CARGO COMPARTMENT CORRODED AT INTERCOSTAL STATION 636 TO STATION 617. OUT OF LIMITS. FABRICATED NEW IN TERCOSTAL FROM .040 7075-T6. INSTALLED INTERCOSTAL IN MID LOWER CARGO COMPARTMENT PER MD80 SRM 51-30. (M) 2 L 7 2 4F A6WE 2002041200001 20020412 00001 WP 2002 4 12 GTIA020172 1 20011214 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - MID LOWER CARGO COMPARTMENT CORRODED AT AFT BELT FRAME STATION 579 ABOVE STRINGER 30 AT DOT 135. MATERIAL OUT OF LIMITS. FORMER ANGLES FOR REPAIR. INSTALLED NEW REPAIR IAW MD80 SRM 53-03. (M) 2 L 7 2 4F A6WE 2002041200002 20020412 00002 WP 2002 4 12 GTIA020173 1 20011214 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - MID LOWER CARGO COMPARTMENT CORRODED AT CARGO ATTACH FITTING STATION 6363. FOUND BELT FRAME SUPPORT CRACKED. REM OVED BELT FRAME SUPPORT AT LONGERON 26L. REPAIRED DAMAGED AREA. INSTALLED BELT FRAME SUPPORT IAW SRM MD-80 51-30-2. ( M) 2 L 7 2 4F A6WE 2002041200003 20020412 00003 WP 2002 4 12 GTIA020174 1 20011214 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - MID LOWER CARGO COMPARTMENT CRACKED AT AFT LEFT SUPPORT BELT FRAME STATION 636. REMOVED SUPPORT BELT FRAME STATIO N 636. INSTALLED NEW SUPPORT FITTING IAW MD80 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 2002041200004 20020412 00004 WP 2002 4 12 GTIA020175 1 20011214 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - MID LOWER CARGO COMPARTMENT CORRODED AT LOWER DOOR JAMB CUTOUT FROM STATION 693 TO 636. AREA FOUND TO BE OUT OF L IMITS. FABRICATED DOOR JAMB STRAP. REMOVED OLD DOOR JAMB STRAP. INSTALLED STRAP IAW SRM MD80 51-30-5. (M) 2 L 7 2 4F A6WE 2002041200005 20020412 00005 WP 2002 4 12 GTIA020176 1 20011219 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FORWARD CAIN, LEFT SIDE, FLOOR SUPPORT FRAME STATION 180 FROM X14 TO X39 HAS CORROSION IN SEVERAL AREAS. REMOVED FLOOR SUPPORT TO FORM NEW ONE. FORMED ANGLE Z-ANGLE. INSTALLED ANGLE FLOOR SUPPORT Z IAW MD80 SRM 53-14-1. (M) 2 L 7 2 4F A6WE 2002041200006 20020412 00006 WP 2002 4 12 GTIA020177 1 20011219 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND FORWARD CABIN, LEFT SIDE FLOOR SUPPORT FRAME AT X46, STATION 160 TO 218 HAS APPROX 8 FASTENERS BROKEN OFF IN FRAME. CORROSION OUT OF LIMITS. REMOVED FLOOR SUPPORT TO FORM NEW ONE. FORMED, LOCATED AND DRILLED NEW FLOOR SUPPORT . INSTALLED NEW FLOOR SUPPORT IAW MD80 SRM 53-14-1. (M) 2 L 7 2 4F A6WE 2002041200007 20020412 00007 WP 2002 4 12 GTIA020178 1 20011219 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND FORWARD CABIN, LEFT SIDE FLOOR SUPPORT FRAME AT X56 STATION 160 TO 200 HAS SEVERE CORROSION, FRAME UNDER L1 DOOR SCUFF PLATE. REMOVED FLOOR SUPPORT TO FORM NEW ONE. FORMED LOCATED AND DRILLED NEW FLOOR SUPPORT. INSTALLED FLOO R SUPPORT IAW MD80 SRM 53-14-01. (M) 2 L 7 2 4F A6WE 2002041200008 20020412 00008 WP 2002 4 12 GTIA020179 1 20011219 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP CABIN DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND CABIN CENTER FLOORBOARD FROM STATION 200-250 IS SPONGY. REMOVED FLOOR PANEL STATION 200-250. FORMED NEW FL OOR PANEL. INSTALLED PAX CENTER FLOOR PANEL FROM STATION 200-250 IAW MD80 M 53-20-01. (M) 2 L 7 2 4F A6WE 2002041200009 20020412 00009 WP 2002 4 12 GTIA020180 1 20011219 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP CABIN DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND CENTER FLOORBOARD IN CABIN FROM STATION 250-313 IS SPONGY. REMOVED FLOOR PANEL. FABRICATED FLOOR PANEL. I NSTALLED PASSENGER CENTER FLOOR BOARD PANEL ROM STATION 250-313 IAW MD80 MM 53-20-1. (M) 2 L 7 2 4F A6WE 2002041200010 20020412 00010 WP 2002 4 12 GTIA020181 1 20011219 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FORWARD PAX ENTRY AREA, FLOOR SUPPORT CORRODED AT STATION Y=198 INCH X55 INCH. FOUND CORROSION OUT OF LIMITS. RE MOVED FLOOR SUPPORT TO FORM NEW ONE. FORMED LOCATED AND DRILLED NEW FLOOR SUPPORT IAW MD80 SRM 51-10-2. (M) 2 L 7 2 4F A6WE 2002041200011 20020412 00011 WP 2002 4 12 GTIA020183 1 20011224 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND STATION 160-200 -X55 (RT) FLOOR SUPPORT ANGLE EXFOLIATING. REMOVED FLOOR SUPPORT ANGLE. INSTALLED FLOOR SU PPORT IAW MD80 MM 51-30-2. (M) 2 L 7 2 4F A6WE 2002041200012 20020412 00012 WP 2002 4 12 GTIA020184 1 20011224 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND STATION 160-200 -X45 FLOOR SUPPORT ANGLE HAS HEAVY CORROSION. FORMED NEW FLOOR SUPPORT ANGLE. FORMED NEW S UPPORT ANGLE. INSTALLED NEW FLOOR SUPPORT ANGLE IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002041200013 20020412 00013 WP 2002 4 12 GTIA020185 1 20011224 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND STATION 148-20 PLUS X46 LEFT FLOORBOARD SUPPORT ANGLE HAS HEAVY CORROSION. FLOOR SUPPORT ANGLE OUT OF LIMIT S. LOCATED AND DRILLED HOLES ON NEW SUPPORT ANGLE. INSTALLED NEW FLOOR SUPPORT IAW MD80 SRM 51-30-1. (M) 2 L 7 2 4F A6WE 2002041200014 20020412 00014 WP 2002 4 12 GTIA020186 1 20011224 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND STATION 148-200 -46 RIGHT HAS HEAVY BLOWN OUT, CORRROSION ON FLOORBOARD SUPPORT ANGLE. CORROSION ON SUPPORT OUT OF LIMITS. LOCATED AND DRILLED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT PER MD80 SRM 51-30-1. (M) 2 L 7 2 4F A6WE 2002041200015 20020412 00015 WP 2002 4 12 GTIA020187 1 20011227 A 5320 STRUCTURE DOUG DC9 DC982 3022082 WP SUB FLOOR CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FOUND STATION 148-200 PLUS X6 LEFT SUB FLOOR MEMBRANE HAS CORROSION AROUND FASTENER HOLES AND 1 ELONGATED HOLE. REMOVED CORROSION. LOCATED DRILLED AND TRIMMED REPAIR PARTS. REMOVED DAMAGE AND ENLONGATED HOLE. (M) 2 L 7 2 4F A6WE 2002041200016 20020412 00016 WP 2002 4 12 GTIA020188 1 20011228 A 5320 WEB DOUG DC9 DC982 3022082 WP SUB FLOOR CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND STATION 160-200 -55 SUBFLOOR (WEB) HAS ELONGATED HOLES AND OUT OF LIMITS CORROSION, DEEP PITS, FROM APPROX S TATION 180-200. CUT OUT DAMAGED SUBFLOOR. FORMED REPAIR DOUBLER AND FILLER. INSTALLED FILLER AND DOUBLER IAW MD80 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 2002041200017 20020412 00017 WP 2002 4 12 GTIA020189 1 20011228 A 5311 FRAME DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 840NK 49104 FTW - AFT LOWER CARGO COMPARTMENT CORRODED AT BEAM STATION 1155 29R. REMOVED BEAM. LOCATED, DRILLED, AND DEBURRED BEAM . INSTALLED BEAM AND CLIPS PER MD80 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 2002041200022 20020412 00022 WP 2002 4 12 GTIA020201 1 20011224 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP COCKPIT PUNCTURED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND COCKPIT FLOOR PANEL HAS HOLE PUNCHED IN SKIN. HOLE AND CRACK IN FLOORBOARD OUT OF LIMITS. FABRICATED REPAI R DOUBLER. INSTALL DOUBLER IAW DC9 MD80 SRM 51-30-1. (M) 2 L 7 2 4F A6WE 2002041200023 20020412 00023 WP 2002 4 12 GTIA020202 1 20011224 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP CABIN CHAFED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND FLOORBOARD PANEL NR A-10 HAT CHANNEL CHAFED, DENTS IN SKIN AND NEEDS CLEANING. FABRICATED DOUBLER. GOUGE I S OUT OF LIMITS ON HAT CHANNEL NR 2. FABRICATED NR 2 HAT CHANNEL DOUBLER. INSTALLED REPAIR DOUBLER. INSTALLED HAT NR 2 REPAIR DOUBLER IAW MD80 SRM 51-30-8. (M) 2 L 7 2 4F A6WE 2002041200024 20020412 00024 WP 2002 4 12 GTIA020203 1 20011224 A 5230 SUPPORT BRACKET DOUG DC9 DC982 3022082 WP CARGO DOOR CHAFED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FORWARD LOWER CARGO COMPARTMENT CARGO DOOR CHAFING / DAMAGE AT AFT BRACKET SUPPORT UPPER LATCH. REMOVED BRACKET S UPPORT. INSTALLED NEW BRACKET SUPPORT IAW MD80 SRM 51-30-1. (M) 2 L 7 2 4F A6WE 2002041200025 20020412 00025 WP 2002 4 12 GTIA020204 1 20011227 A 5311 FRAME DOUG DC9 DC982 3022082 WP BULKHEAD CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - AFT LOWER CARGO COMPARTMENT CORRODED AT FORMER SUPPORT BULKHEAD STATION 1322, L30 TO 26L. FOUND OUT OF LIMITS. F ORMED SUPPORT IAW MD80 SRM 51-10-3. (M) 2 L 7 2 4F A6WE 2002041200026 20020412 00026 WP 2002 4 12 GTIA020205 1 20011227 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP CABIN BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND COCKPIT CENTER FLOORBOARD BROKEN OUT AND CRUSHED AND TORN AT EDGES. FORMED NEW FLOORBOARDS IAW MD80 MM 20-1 0-19. (M) 2 L 7 2 4F A6WE 2002041200028 20020412 00028 WP 2002 4 12 GTIA020207 1 20011212 A 5522 SKIN DOUG DC9 DC982 3022082 WP ELEVATOR DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND OUTBOARD LEFT ELEVATOR PANEL ACCESS DENTS, GAUGE, CHAFING, BARE METAL. AFTER FURTHER EVALUATION, FOUND CRAC K ON PANEL. WELDED CRACK AREA FOR DPS. (M) 2 L 7 2 4F A6WE 2002041200029 20020412 00029 WP 2002 4 12 GTIA020208 1 20011205 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP EMERGENCY EXIT CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND OVERWING EMERGENCY EXIT RIGHT AFT LOWER DOOR FRAME CRACKED. REMOVED FITTING. INSTALLED FITTING IAW MD80 SR M 51-30-2. (M) 2 L 7 2 4F A6WE 2002041200030 20020412 00030 WP 2002 4 12 GTIA020209 1 20011206 A 5230 STRUCTURE DOUG DC9 DC982 3022082 WP CARGO DOOR CHAFED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND FORWARD CARGO DOOR CHAFING SEVERAL SPOTS OUTER. LOWER AFT AT OUTER EDGE FOUND TO BE OUT OF LIMITS. FABRICA TED, DRILLED AND LOCATED DOUBLER. INSTALLED DOUBLER AND FILLER PER MD80 SRM 52-05. (M) 2 L 7 2 4F A6WE 2002041200031 20020412 00031 WP 2002 4 12 GTIA020210 1 20011208 A 2620 BOTTLE DOUG DC9 DC982 3022082 WP FIRE EXTING DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 804NK 49104 FTW - APU EXTERNAL FIRE BOTTLE DISCHARGE INOPERATIVE, FAILED TEST. TROUBLESHOT AND FOUND BROKEN TERMINAL AT R2-61 APU F IRE SHUTDOWN RELAY. REPAIRED DEFECTIVE TERMINAL IAW MD80 49-31-01. (M) 2 L 7 2 4F A6WE 2002041200032 20020412 00032 WP 2002 4 12 GTIA020211 1 20011208 A 5730 PANEL DOUG DC9 DC982 3022082 WP RT WING DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND RIGHT WING COMPOSITE TRAPIZOID PANLE HAS FASTENERS PULLING THROUGH PANEL AND POSSIBLE DELAMINATION. REMOVED DAMAGED PLIES OF FIBERGLASS FROM RIGHT WING TRAPEZOID PANEL. REPAIRED DELAMINATION AREAS ON RIGHT WING TRAPEZOID PANEL IAW DC9 MD80 SRM 51-90-0. (M) 2 L 7 2 4F A6WE 2002041200033 20020412 00033 WP 2002 4 12 GTIA020212 1 20011208 A 5730 PANEL DOUG DC9 DC982 3022082 WP LT WING DETERIORATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND LEFT WING LOWER SURFACE TRAPEZOIDAL PANEL DETERIORATED. REMOVED DAMAGED PLIES OF FIBERGLASS ON LEFT WING TR APEZOID PANEL. REPAIR DELAMINATION AT AFECTED AREAS IAW DC9/MD80 SRM 51-90-0. (M) 2 L 7 2 4F A6WE 2002041200051 20020412 00051 WP 2002 4 12 GTIA02182 1 20011220 A 5320 WEB DOUG DC9 DC982 3022082 WP SUB FLOOR CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FOUND STATION 185 AT MAIN ENTRY DOOR SUB-FLOOR HAS SURFACE CORROSION. REMOVED SUB FLOOR (WEB) TO FORM NEW ONE. FORMED AND LOCATED DRILLED SUB FLOOR (WEB). INSTALLED SUB FLOOR (WEB) IAW MD80 SRM 53-14-1. (M) 2 L 7 2 4F A6WE 2002041500132 20020415 00132 NM 2002 4 15 DLM11020393 1 20010402 A 3350 6044113M POWER SUPPLY DOUG MD11 MD11 3023602 NM COCKPIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 804DE 48475 ON PREFLIGHT CHECK, EMERGENCY LIGHTS TEST FAILED. EMER LIGHT BATT 1 LO MSG ON SYN DISPLAY. REPLACED NR 1 EMERGENCY LI GHT POWER SUPPLY UNIT PER M/M. EMERGENCY LIGHTS TEST PASS. 2 L 7 3 4F RT A22WE 2002041700023 20020417 00023 NM 2002 4 17 ASAA0110635 1 20011031 A 5210 6529994 ARM BOEING 737 737210C 1384459 NM PAX DOOR STIFF A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 ANC - CREW REPORTED L1 DOOR DIFFICULT TO CLOSE. ADJUSTED GUIDE ARM, THEN OPS CHECKED GOOD. (M) 2 L 7 2 4F A16WE 2002041700024 20020417 00024 NM 2002 4 17 ASAA0110641 1 20011113 A 5311 65458055 FRAME BOEING 737 737298C 1384490 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 727, STRINGER 25R-27R DAMAGED. REPAIRED FRAME PER SRM. (M) 2 L 7 2 4F RT A16WE 2002041700025 20020417 00025 NM 2002 4 17 ASAA0110645 1 20011127 A 5311 654581234 FRAME BOEING 737 737298C 1384490 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 SW 21 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND FAIL/SAFE AT BODY STATION 328, STRINGER 25R CRACKED. REMOVED AND REPLACED FAIL/SA FE PER SRM. (M) 2 L 7 2 4F RT A16WE 2002041700026 20020417 00026 NM 2002 4 17 ASAA0140139 1 20011114 A 5320 6549631 ANGLE BOEING 737 7374Q8 138447Q NM BULKHEAD CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 PAE - DURING SI CHECK, FOUND CORROSION ON BULKHEAD SUPPORT ANGLE AT STATION 500G LBL 24 TO RBL 24 AND WL 156. FABRICATE D AND INSTALLED ANGLE IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002041700056 20020417 00056 EU 2002 4 17 SIMA200126203 1 20010919 A 7712 20110800001 CONTROL UNIT AEROSP ATR72 ATR72212A 8680902 EU NR 1 ENGINE ERRATIC A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 538AT 538 DFW - FLT 3607 - NR 1 ENGINE TORQUE AND NR 2 ENGINE PROPELLER SPEED WAS ERRATTIC DURING CLIMB-OUT. CREW RETURNED TO FIE LD. REMOVED AND REPLACED THE PEC INTERFACE UNIT IAW ATR 72 AMM. OPERATIONALLY CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 2002041700194 20020417 00194 EU 2002 4 17 2002F00405 1 20011219 A 5347 S53678001246 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 548AT 548 DURING CPCP 4 INSPECTION, FOUND CORROSION ON 4 SEAT TRACKS, LEFT AFT OUTBOARD, LEFT AFT INBOARD, LEFT FLIGHT ATTENDANT, AND AFT CARGO SEAT TRACKS. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW ENGINEERING ORDER E2-53MR-115R1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002041700195 20020417 00195 EU 2002 4 17 2002F00406 1 20011219 A 5347 EPNE95300013023 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 548AT 548 DURING CPCP 4 INSPECTION, FOUND CORROSION ON 4 SEAT TRACKS, LEFT AFT OUTBOARD, LEFT AFT INBOARD, LEFT FLIGHT ATTENDANT, AND AFT CARGO SEAT TRACKS. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW ENGINEERING ORDER E2-53MR-115R1. THE AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200200202. (M) 2 H 7 2 4T RT A53EU 2002041700196 20020417 00196 EU 2002 4 17 2002F00407 1 20011219 A 5347 EPNE9530013025 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 548AT 548 DURING CPCP 4 INSPECTION, FOUND CORROSION ON 4 SEAT TRACKS, LEFT AFT OUTBOARD, LEFT AFT INBOARD, LEFT FLIGHT ATTENDANT, AND AFT CARGO SEAT TRACKS. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW ENGINEERING ORDER E2-53MR-115R1. THE AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200200202. (M) 2 H 7 2 4T RT A53EU 2002041800014 20020418 00014 WP 2002 4 18 AALA20020270 1 20011221 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 430AA 49342 TUL - FOUND NR 3 SEAT TRACK CORRODED STATION 1169-1210. FOUND CORROSION BLEND OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK SRM 51-01. (M) 2 L 7 2 4F A6WE 2002041800034 20020418 00034 EU 2002 4 18 SIMA200134401 1 20011210 A 2611 SMOKE DETECTOR AEROSP ATR72 ATR72212A 8680902 EU LAVATORY MALFUNCTIONED A SIMA O OTHER N FALSE WARNING AP APPROACH 1 SW 21 499AT 499 MIA - FLT 5006 - CREW REPORTED AN AFT SMOKE INDICATION ON THE CREW ALERTING PANEL WITH A MASTER WARNING THAT WOULD COME ON FOR 5 TO 7 SECONDS THEN GO OUT. THIS HAPPENED THREE TIMES. MAINTENANCE REMOVED AND REPLACED THE AFT CARGO (P/N FR32 22 S/N 431), AND THE LAVATORY SMOKE DETECTORS (P/N FR3123, S/N 390) IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002041800035 20020418 00035 EU 2002 4 18 SIMA200200201 1 20011219 A 5315 S53678001246 FLOORBEAM AEROSP ATR72 ATR72212A 8680902 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 548AT 548 SAW - DURING CPCP2 INSPECTION, FLOORBEAM 38 WAS FOUND TO BE CORRODED. FLOORBEAM 38 WAS REMOVED AND REPLACED IAW ATR72 S RM 53-00-00, FIGURE 435. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002041800036 20020418 00036 EU 2002 4 18 SIMA200200202 1 20011219 A 5347 S53678001244 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 548AT 548 DURING CPCP 4 INSPECTION, FOUND CORROSION ON 4 SEAT TRACKS, LEFT AFT OUTBOARD, LEFT AFT INBOARD, LEFT FLIGHT ATTENDANT, AND AFT CARGO SEAT TRACKS. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW ENGINEERING ORDER E2-53MR-115R1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002041800037 20020418 00037 EU 2002 4 18 SIMA200200203 1 20011219 A 5347 S53678001226 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 548AT 548 SAW - DURING CPCP 4 INSPECTION, CORROSION WAS FOUND ON RIGHT AFT INBOARD SEAT TRACK. THE SEAT TRACK WAS REMOVED AND REP LACED IAW ENGINEERING ORDER E2-53MR-115R1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002041800038 20020418 00038 EU 2002 4 18 SIMA200200204 1 20011219 A 5315 S5367240825400 FLOORBEAM AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 540AM 540 SAW - DURING CPCP4 INSPECTION FLOORBEAM 39 WAS FOUND TO BE CORRODED. FLOORBEAM 39 WAS REPLACD IAW ATR SRM 51-25-01. AI RCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002041800039 20020418 00039 EU 2002 4 18 SIMA200200205 1 20011219 A 5315 S5367240620801 FLOORBEAM AEROSP ATR72 ATR72212A 8680902 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 540AM 540 SAW - DURING CPCP4 INSPECTION FLOORBEAM 36 WAS FOUND TO BE CORRODED. FLOORBEAM 36 WAS REPLACED IAW ATR SRM 51-25-02. A IRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002041900015 20020419 00015 SW 2002 4 19 AC2A0000338 1 20010407 A 6220 230312001105 BEARING BELL 430 430 1182150 SW ALLSN 250C 250C* GL P/C LINK WORN E AC2A K NONE O OTHER IN INSP/MAINT 1 SW 03 430CH 1668 49037 BEARINGS WERE WORN ON P/C LINKS. REPLACED BEARINGS. 1 G 7 2 3U 3 U RT H9SW E4CE 2002041900018 20020419 00018 SW 2002 4 19 AC2A0000341 1 20011007 A 6220 BEARING BELL 430 430 1182150 SW ALLSN 250C 250C* GL P/C LINKS FAILED E AC2A K NONE O OTHER IN INSP/MAINT 1 SW 03 430CH 49037 REMOVED AND REPLACED BEARINGS IN P/C LINKS. 1 G 7 2 3U 3 U RT H9SW E4CE 2002042200039 20020422 00039 EU 2002 4 22 KBMA112002 1 20011020 A 6240 9550176240 TRANSMITTER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE TORQUE INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 313LV 611 3296 TORQUE TRANSMITTER, INOPERATIVE. REMOVED AND REPLACED WITH NEW. 1 G 7 1 3U 3 U H9EU E19EU 2002042200042 20020422 00042 EU 2002 4 22 KBMA112011 1 20010727 A 6240 9550176240 TRANSMITTER SNIAS 350 AS350* EU TMECA ARRIEL ARRIEL1 60030 NE TORQUE INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 2273A 822 2273 TORQUE TRANSMITTER INOPERATIVE. REMOVED AND REPLACED WITH NEW. 1 G 7 1 3U 3 U H9EU E19EU 2002042500129 20020425 00129 SW 2002 4 25 2002F00421 1 20011205 A 2910 2781032135 LINE SWRNGN SA227 SA227AC 8780603 SW HYD SYSTEM LEAKING A BSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 05 702M AC702 ON CLIMB-0UT, BOTH HYDRAULIC LIGHTS CAME ON AND HYDRAULIC PRESSURE GAGE WENT TO ZERO. CREW LANDED AFTER DECLARING EMERG ENCY AND MANUALLY EXTENDING THE GEAR. SUSPECTED BREAK IN HYDRAULIC LINE CAUSING FLUID LOSS LEADING TO HYDRAULIC PRESSUR E LOSS. REPLACED FLAP UP HYDRAULIC LINE FROM POEWR PACK TO AFT LEFT NACELLE AREA. (M) 2 L 7 2 4T RT A8SW 2002050200099 20020502 00099 WP 2002 5 2 ABXA010857 1 20011227 A 5330 SKIN DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 LEFT FREON COMPRESSOR EXHAUST CUTOUT HAD 2 SKIN CRACKS AT THE UPPER FORWARD AND AFT CORNERS. INSTALLED EXTERNAL DOUBLER REPAIR AROUND FREON COMPRESSOR EXHAUST IAW DC-8 SRM 53-2-1. 2 L 7 4 4F 4A25 2002050200103 20020502 00103 WP 2002 5 2 ABXA010861 1 20011223 A 5730 SKIN DOUG DC8 DC863F 302198F WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 LEFT WING TOP SKIN JUST AFT OF FRONT SPAR, SKIN HAD 1 INCH CRACK AT XW 400, INBOARD THE NR 1 PYLON. INSTALLED DOUBLER A ND FILLER, REPAIRED AREA IAW REA D857-41949MR AND DC-8 SRM 51-1-20B, 51-1-20D, 51-1-12 AND 51-1-15. 2 L 7 4 4F 4A25 2002050700012 20020507 00012 NE 2002 5 7 ZYW2002F00000 2 20011106 A 7532 9550164050 BLEED VALVE AEROSP AS365 AS365N2 8680815 EU TMECA ARRIEL ARRIEL1C 60030 NE ENGINE LEAKING E ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365WM 3248 6429 BLEED VALVE, AIR LEAKING OUT BODY. REMOVED AND REPLACED. 1 G 7 2 3U 3 U RT H10EU E19EU 2002050700013 20020507 00013 EU 2002 5 7 ZYW2002F00001 1 20011019 A 7931 53408 TRANSMITTER AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE OIL PRESS INTERMITTENT E ZYWA K NONE L NO TEST NR NOT REPORTED 1 GL 09 365SJ 3663 6018 OIL PRESSURE TRANSMITTER, INTERMITTENT. REMOVED AND REPLACED TRANSMITTER. 1 G 7 2 3U 3 U H10EU E19EU 2002050700014 20020507 00014 EU 2002 5 7 ZYW2002F00002 1 20011009 A 3350 B1250000 BATTERY AEROSP AS365 AS365N2 8680815 EU TMECA ARRIEL ARRIEL1 60030 NE CABIN INOPERATIVE E ZYWA K NONE L NO TEST IN INSP/MAINT 1 GL 09 365WM 3262 6429 EMERGENCY BATTERY, BATTERY DEAD. REMOVED AND REPLACED BATTERY. 1 G 7 2 3U 3 U RT H10EU E19EU 2002050900031 20020509 00031 NM 2002 5 9 USAABB01035 1 20010608 A 2121 731376 COOLING FAN BOEING 757 7572B7 1384964 NM CARGO BAY FAILED A USAA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DE DESCENT 1 EA 19 620AU 3427 27199 PIT - FLT 82 EN ROUTE FROM SFO TO PHL, ON DESCENT AT FL350, FLIGHT ATTENDANTS NOTICED SMOKE AND FUMES IN THE CABIN. AFT SMOKE DETECTOR WAS ALSO SOUNDING. CAPTAIN INSTRUCTED FLIGHT ATTENDANTS TO CHECK LAVATORY TRASH FOR COMBUSTION. NONE F OUND. ACCOMPLISHED QRH PROCEDURES AND WHEN THEY SHUT OFF THE RIGHT A/C PACK, THE SMOKE APPEARED TO STOP. CREW DECLARED AN EMERGENCY AND DIVERTED TO PIT WHERE THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE R&R EQUIPMENT COOLING FAN NR 1 AFT. CHECKED BOTH ACM AND RAN PACKS. OPERATIONAL CHECK GOOD. EQUIPMENT COOLING FANS CHECK GOOD. AIRCRAFT OK FOR SERV ICE. (M) 2 L 7 2 4F RT A2NM 2002050900032 20020509 00032 NM 2002 5 9 USAABB01151 1 20011226 A 1430 11802 BOLT BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE LOOSE A USAA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 EA 19 626AU 27303 31306 DEN - FLT 82 - EN ROUTE FROM SFO TO PHL, SMOKE IN THE COCKPIT. A HAZE WAS NOTICED IN THE CABIN. THE AFT LT LAV SMOKE D ETECTOR SOUNDED, CREW SHUT DOWN BOTH RECIRCULATION FANS AND THEN RT PACK TO ISOLATE FAULT. THE AFT RT LAV SMOKE DETECTO R SOUNDED AND THE CREW DIVERTED TO DEN. WHEN THE A/C LANDED, THE SMOKE DISSIPATED AND SMOKE DETECTORS WERE SILENT. MX RAN THE ENGINES WITH THE FLIGHT CREW AND COULD NOT DUPLICATE SMOKE. AFTER INSP AND TROUBLESHOOTING WITH NO CAUSE FOUND, THE ENGINE WAS REPLACED. ENGINE TEARDOWN REVEALED THAT THE FRONT ANNULAR PANEL OUTER PERIPHERY RETAINING BOLTS (POSITI ON 18X) ON THE INTERMEDIATE CASE WERE LOOSE. EVIDENCE OF OIL LEAKAGE ACROSS THE JOINT FACES WAS FOUND. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2002051300122 20020513 00122 NE 2002 5 13 ARWA20020505 2 20011113 A 7200 RB211524B02 ENGINE LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B402 54555 NE NR-2 VIBRATION A ARWA E ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SO 19 260FA 57889 9292 1158 14734 (SUPPLEMENT TO: ARWA20011103) LOG PAGE # 22235. DISCREPANCY: SHUTDOWN NR # 2 ENGINE, AFTER EXPERIENCING VIPS SPIKE 3.0 B OTH CHANNELS AT APPOXIMATELY 2325 ZULU. CORRECTIVE ACTION: REMOVED AND REPLACED # 2 ENGINE IAW ARROW AIR RB211-L1011 MA INTENANCE FORM L-1011-7104A AND L-1011 FORM 7102B. ENGINE OPS CHECKED NORMAL. 2 L 7 3 4F 4 F A23WE E12EU 2002051500177 20020515 00177 CE 2002 5 15 GGP2002F00000 1 20011011 A 7160 4041891819 AIR BOX BEECH 18 E18S 1151006 CE PWA R985 R985* 52008 NE CARBURETOR WORN A GGPA K NONE O OTHER IN INSP/MAINT 1 SW 99 48K BA202 9817 FLYING, NUMBER ONE ENGINE CARBURETOR STARTED TO ICE UP. APPLIED CARBURETOR HEAT BUT IT HAD NO EFFECT ON CONDITION. ON APPROACH, PILOT HAD TO SHUT DOWN ENGINE. POST FLIGHT INSPECTION FOUND THE CARBURETOR AIR BOX DOOR WAS WORN (COULD BE PU SHED UP ABOUT .5000 INCH). REPLACED CARBURETOR AIR BOX WITH SERVICEABLE ONE. 1 L 7 2 3R 3 R A765 5E1 2002051500178 20020515 00178 NE 2002 5 15 GGP2002F00001 2 20010920 A 8530 STUD BEECH 18 E18S 1151006 CE PWA R985 R985* 52008 NE CYLINDER FAILED A GGPA K NONE O OTHER IN INSP/MAINT 1 SW 99 42D 25343 BA117 78509 IN FLIGHT, ENGINE NR 1 STARTED TO VIBRATE. SHUT DOWN ENGINE, LANDED. NR 3 CYLINDER BASE STUDS FAILED AND PISTON DAMAGE D ENGINE WILL BE REMOVED AND REPLACED WITH OVERHAULED ENGINE. 1 L 7 2 3R 3 R A765 5E1 2002052100016 20020521 00016 NE 2002 5 21 R7M2002F00016 2 20010928 A 7250 430150602 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR 2 BEARING LEAKING B R7MR K NONE K FLUID LOSS IN INSP/MAINT 1 NM 07 420MB 9097 7077 NUMBER 2 BEARING SEAL IS LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2002052100018 20020521 00018 NE 2002 5 21 R7M2002F00018 2 20011019 A 7240 430144801 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR3 BEARING LEAKING B R7MR K NONE K FLUID LOSS IN INSP/MAINT 1 NM 07 528SF 9179 7104 NR3 BEARING SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2002052100024 20020521 00024 NE 2002 5 21 R7M2002F00024 2 20011014 A 7260 230093304 BEARING BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ENGINE CORRODED B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 625MB 6606 7108 LE45306EA ANNUALAR BALL BEARING HAS EXCESSIVE PITTING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2002052100025 20020521 00025 NE 2002 5 21 R7M2002F00025 2 20011014 A 7240 430144801 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE NR 3 BEARING LEAKING B R7MR K NONE K FLUID LOSS IN INSP/MAINT 1 NM 07 625MB 6606 7108 LE45306EA NR 3 BEARING SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2002052100026 20020521 00026 EU 2002 5 21 R7M2002F00026 1 20011014 A 7720 430150102 THERMOCOUPLE BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ENGINE SHORTED B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 625MB 6606 7108 LE45306EA THERMOCOUPLE HAS AN INTERNAL SHORT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2002052100027 20020521 00027 EU 2002 5 21 R7M2002F00027 1 20011014 A 7720 430150102 THERMOCOUPLE BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ENGINE SHORTED B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 625MB 6606 7108 LE45306EA THERMOCOUPLE HAS AN INTERNAL SHORT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2002052100028 20020521 00028 NE 2002 5 21 R7M2002F00028 2 20011014 A 7240 430124203 BEARING BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE NR 3 TURBINE CORRODED B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 625MB 6606 7108 1505 TURBINE ANNULAR BALL BEARING HAS EXCESSIVE PITTING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2002052100029 20020521 00029 NE 2002 5 21 R7M2002F00029 2 20011014 A 7250 430150602 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE NR 2 BEARING LEAKING B R7MR K NONE K FLUID LOSS IN INSP/MAINT 1 NM 07 625MB 6606 7108 LE45306EA NUMBER 2 BEARING SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2002052100030 20020521 00030 SW 2002 5 21 R7M2002F00033 1 20011211 A 6510 407040320101 SHAFT BELL 407 407 1182206 SW ALLSN 250C 250C47B GL TAIL ROTOR WORN B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 911LN 853 53446 SHAFT SPLINES WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2002052200102 20020522 00102 NM 2002 5 22 MEX2002021 1 20010126 A 7603 SPRING DOUG MD88 MD88 3023688 NM FUEL LEVER FAILED A ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 169PL 53175 FLT 587 - MEX-CUN - RETURN TO PLATFORM DUE TO THAT THE FUEL CONTROL LEVER DOES NOT LOCK AND AUTOBRAKE SYSTEM O/S. SPRIN G OF THE FUEL LEVER WAS CHANGED IAW MM 76-10-01 AND AIRCRAFT DISPATCH IAW MEL 32-9. AT RON IN MEX 26/27 THE SOLENOID PR ESSURE SWITCH NR 1 ABS LAND MANIFOLD WAS CHANG IAW MM 32-44-02. (M) 2 L 7 2 4F RT A6WE 2002052300107 20020523 00107 EU 2002 5 23 R7MR34743 1 20011219 A 6320 ZRB26300 TRANSMITTER UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE M/R G/B PRESSURE INOPERATIVE B R7MR K NONE L NO TEST IN INSP/MAINT 1 NM 07 102HN 230 0159 OIL PRESSURE TRANSMITTER (MGB) - UNIT INOPERATIVE. PRESSURE FLUCUATES FROM 2 BAR TO 14 BAR EVEN WITHOUT ENGINES RUNNING . REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2002052900116 20020529 00116 SW 2002 5 29 2002F00520 1 20010121 A 5230 HS9497 MECHANISM SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR DAMAGED A BSAA O OTHER J WARNING INDICATION CR CRUISE 1 NM 05 160MC AC733B BIL - FLT 1315 - CARGO DOOR WARNING LIGHT CAME ON DURING CRUISE AT FL190. THE CREW DECREASED CABIN PRESSURE AS THEY RET URNED TO STATION. THE WARNING LIGHT WENT ABOUT THE TIME THE PRESSURE DIFFERENTIAL WAS REDUCED TO 0. INITIAL INSPECTION FOUND THE UPPER FORWARD AND AFT CLICK CLACK CENTER RODS BENT. IT IS SUSPECTED THIS HAPPENED AS A RESULT OF THE DOOR BE ING PARTIALLY CLOSED WITH THE CLICK CLACKS NOT FULLY RETRACTED. THE UPPER FORWARD AND AFT CLICK CLACKS WERE REPLACED AN D RIGGED. (M) 2 L 7 2 4T RT A8SW 2002052900118 20020529 00118 SW 2002 5 29 2002F00522 1 20011205 A 2910 2781032135 HYDRAULIC LINE SWRNGN SA227 SA227AC 8780603 SW HYD SYSTEM LEAKING A BSAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 05 702M AC702 WDG - FLT 1322 - ON CLIMB-OUT, BOTH HYD LIGHTS CAME ON AND HYDRAULIC PRESSURE GAUGE WENT TO '0'. CREW LANDED AFTER DECL ARING EMERGENCY AND MANUALLY EXTENDING THE GEAR. SUSPECTED BREAK IN HYDRAULIC LINE CAUSING FLUID LOSS LEADING TO HYDRAU LIC PRESSURE LOSS. REPLACED FLAP UP HYDRAULIC LINE FROM POWER PACK TO AFT LEFT NACELLE AREA. (M) 2 L 7 2 4T RT A8SW 2002052900122 20020529 00122 EU 2002 5 29 SIMA200119901 1 20010712 A 5315 S53672406208 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 355AT 355 SAW - DURING CPCP 2 INSPECTION, FOUND 4 FLOORBEAMS WERE FOUND TO BE CORRODED, FLOORBEAM 36, FLOORBEAM 38, FLOORBEAM 39, FLOORBEAM 40. THE FLOORBEAMS WERE REMOVED AND REPLACED IAW ATR72 SRM. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052900124 20020529 00124 EU 2002 5 29 SIMA200119902 1 20010717 A 5347 S53375001214 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 355A 355 SAW - DURING CPCP8 INSPECTION, FOUND CORROSION ON SEAT TRACKS, RIGHT FORWARD OUTBOARD, LEFT FLIGHT ATTENDANT, RIGHT FLIG HT ATTENDANT, AND LAVATORY, THE SEAT TRACKS WERE REMOVED AND REPLACED IAW AMERICAN EAGLE AIRLINES EO E2-53MR-115. THE A IRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052900125 20020529 00125 EU 2002 5 29 SIMA200119903 1 20010717 A 5320 S5367121729801 TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 355A 355 SAW - DURING CPCP8 INSPECTION, FOUND CORROSION ON PASSENGER ENTRY DRAIN TRACK THE DRAIN TRACK WAS REMOVED AND REPLACED I AW ATR SRM 51-21-02. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052900128 20020529 00128 EU 2002 5 29 SIMA200119904 1 20010717 A 5751 S57212089204 BRACKET AEROSP ATR72 ATR72212A 8680902 EU AILERON CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 355A 355 SAW - DURING CPCP8 INSPECTION, FOUND CORROSION ON LEFT AILERON INBOARD AND OUTBOARD ATTACH BRACKETS. THE BRACKETS WERE REMOVED AND REPLACED IAW ATR72 SRM AND AMERICAN EAGLE AIRLINES GPM 17-01 ACCEPTANCE OF ATR SUPPLEMENTAL DATA. THE AIRCR AFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052900129 20020529 00129 EU 2002 5 29 SIMA200119905 1 20010717 A 5260 S5217640700001 SUPPORT AEROSP ATR72 ATR72212A 8680902 EU PAX STAIRS CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AT 498 SAW - DURING CPCP2 INSPECTION, FOUND CORROSION ON PASSENGER STAIR TREAD SUPPORT. TREAD SUPPORT WAS REMOVED AND REPLACED IAW ATR72 SRM. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052900130 20020529 00130 EU 2002 5 29 SIMA200119906 1 20010717 A 5315 S53672407252 FLOORBEAM AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AT 498 SAW - DURING CPCP2 INSPECTION, FOUND CORROSION ON FLOORBEAM 38 AND 39. THE FLOORBEAMS WERE REPAIRED BY INSERTION OF A S PLICE IAW ATR72 SRM. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052900131 20020529 00131 EU 2002 5 29 SIMA200119907 1 20010717 A 5347 EPNE9530001318 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AT 498 SAW - DURING CPCP2 INSPECTION, FOUND CORROSION ON LEFT AFT OUTBOARD, LEFT AFT INBOARD, LEFT FLIGHT ATTENDANT, AND RIGHT FLIGHT ATTENDANT SEAT TRACKS. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW AMERICAN EAGLE AIRLINES ENGINEERING ORDER E 2-53MR-115. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052900132 20020529 00132 EU 2002 5 29 SIMA200119908 1 20010717 A 5320 S5367121706600 SILL AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AT 498 SAW - DURING CPCP2 INSPECTION, FOUND CORROSION ON PASSENGER ENTRY SILL PLATE. THE SILL PLATE WAS REMOVED AND REPLACED I AW ATR72 SRM 51-25-01. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052900133 20020529 00133 EU 2002 5 29 SIMA200119909 1 20010717 A 5320 S5367121729602 SILL AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AT 498 SAW - DURING CPCP2 INSPECTION, FOUND CORROSION ON PASSENGER ENTRY SILL JOINT PLATE. THE SILL JOINT PLATE WAS REMOVED AN D REPLACED IAW ATR72 SRM 51-25-01. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052900134 20020529 00134 EU 2002 5 29 SIMA200119910 1 20010717 A 5320 S5367800826801 CHANNEL AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AT 498 SAW - DURING CPCP2 INSPECTION, FOUND CORROSION ON PASSENGER ENTRY FLOOR CHANNEL, BETWEEN FRAME 38 AND FRAME 39. THE FLO OR CHANNEL WAS REMOVED AND REPLACED IAW ATR72 SRM 51-25-01. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052900136 20020529 00136 EU 2002 5 29 SIMA200119911 1 20010717 A 5347 S53375001214 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 355A 355 SAW - DURING CPCP8 INSPECTION, FOUND CORROSION ON SEAT TRACKS, RIGHT FORWARD OUTBOARD, LEFT FLIGHT ATTENDANT, RIGHT FLIG HT ATTENDANT, RIGHT FLIGHT ATTENDANT, AND LAVATORY, THE SEAT TRACKS WERE REMOVED AND REPLACED IAW AMERICAN EAGLE AIRLINE S ENGINEERING ORDER E2-53MR-115. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052900137 20020529 00137 EU 2002 5 29 SIMA200121904 1 20010801 A 5347 S53678001244 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 529AM 529 DURING CPCP-2 INSPECTION, FOUND CORROSION ON FOUR SEAT TRACKS, LEFT AFT OUTBOARD, LEFT AFT INBOARD, LAVATORY WALL TRACK, AND RIGHT AFT CARGO FLOOR TRACK. ALL SEAT TRACKS WERE REMOVED AND REPLACED IAW AE EO E2-53MR-115. AIRCRAFT WAS THEN R ETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052900138 20020529 00138 EU 2002 5 29 SIMA200121906 1 20010801 A 5260 S5217640600001 STEP AEROSP ATR72 ATR72212A 8680902 EU PAX STAIRS CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 529AM 529 SAW - DURING CPCP-2 INSPECTION, FOUND CORROSION WAS FOUND ON PASSENGER STAIRS AROUND STEP SCREW HOLES OF LOWER STEP. LO WER STEP SUPPORT WAS REMOVED AND REPLACED IAW ATR SRM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052900139 20020529 00139 EU 2002 5 29 SIMA200123411 1 20010814 A 5347 EPNE95300013020 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 533AT 533 SAW - DURING CPCP2 INSPECTION, FOUND CORROSION WAS FOUND ON SEAT TRACKS, LEFT AFT OUTBOARD, LEFT AFT INBOARD, LEFT F/A, RIGHT F/A. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW ATR 72 SRM 51-25-04 AND AMERICAN EAGLE ENGINEERING ORDER E2-53 MR-115. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052900140 20020529 00140 EU 2002 5 29 SIMA200123412 1 20010814 A 5320 S5367129034801 FITTING AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 533AT 533 SAW - DURING CPCP2 INSPECTION, FOUND CORROSION ON PASSENGER ENTRY SILL PLATE FITTING. THE FITTING WAS REMOVED AND REPLA CED IAW ATR72 SRM 51-25-04. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052900141 20020529 00141 EU 2002 5 29 SIMA200123413 1 20010814 A 5320 S5367800826802 SUPPORT AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 533AT 533 SAW - DURING CPCP2 INSPECTION, FOUND CORROSION ON PASSENGER ENTRY SILL SUPPORT. THE SUPPORT WAS REMOVED AND REPLACED IA W ATR72 SRM 51-25-01. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052900142 20020529 00142 EU 2002 5 29 SIMA200123414 1 20010814 A 5320 S5367 SILL AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 533AT 533 SAW - DURING CPCP2 INSPECTION, FOUND CORROSION ON PASSENGER ENTRY SILL. THE SILL WAS REMOVED AND REPLACED IAW ATR72 SRM 51-25-01. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052900143 20020529 00143 EU 2002 5 29 SIMA200123415 1 20010814 A 5320 S5367800821602 ANGLE AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 533AT 533 SAW - DURING CPCP2 INSPECTION, FOUND CORROSION ON THE AFT CARGO FLOOR LEVEL Z-MEMBER. THE Z-MEMBER WAS REMOVED AND REPL ACED IAW ATR72 SRM 51-25-03. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052900144 20020529 00144 EU 2002 5 29 SIMA200123416 1 20010814 A 5315 S5367240620802 FLOORBEAM AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 533AT 533 SAW - DURING CPCP2 INSPECTION, CORROSION WAS FOUND ON FLOORBEAMS 36, 38 AND 39. THE FLOORBEAMS WERE REMOVED AND REPLACE D IAW ATR72 SRM 51-25-04. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052900145 20020529 00145 EU 2002 5 29 SIMA200124401 1 20010901 A 2120 ODOR AEROSP ATR72 ATR72212A 8680902 EU COCKPIT DETECTED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 541AT 541 DFW - FLT 3736 - DURING TAKEOFF AND CLIMB-OUT, CREW EXPERIENCED NOXIOUS SMELL IN COCKPIT AND CABIN. OPERATIONAL CHECK O F COOLING SYSTEM WAS PERFORMED IAW ATR AMM. SMELL COULD NOT BE DUPLICATED. (M) 2 H 7 2 4T RT A53EU 2002052900148 20020529 00148 EU 2002 5 29 SIMA200124901 1 20010906 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 538AT 538 SGF - FLT 3567 - AFT SECTION OF EMERGENCY LIGHTING INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK 62 WL. OPERATIONAL CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 2002052900149 20020529 00149 EU 2002 5 29 SIMA200124906 1 20010906 A 5240 E152000161 DOOR AEROSP ATR42 ATR42300 8680920 EU FUSELAGE DEPARTED A SIMA O OTHER D INFLIGHT SEPARATION CR CRUISE 1 SW 21 424QT 45 RSW - FLT 5369 - DURING CRUISE, AIR CONDITIONING GROUND INTERCONNECT ACCESS DOOR DEPARTED AIRCRAFT. INSTALLED REPLACEME NT ACCESS DOOR. (M) 2 H 7 2 4T RT A53EU 2002052900150 20020529 00150 EU 2002 5 29 SIMA200125102 1 20010908 A 3350 3013017 POWER SUPPLY AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 533AT 533 LBB - FLT 3826 - CREW REPORTED HALF OF THE FORWARD EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TWO POWER SUPPLY UNITS IAW ATR 72 MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052900151 20020529 00151 EU 2002 5 29 SIMA200126501 1 20010917 A 5320 S5367800021401 INTERCOSTAL AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 420AT 420 SAW - DURING CPCP2 INSPECTION, FOUND CORROSION ON LEFT INTERCOSTAL BETWEEN FRAMES 39-40. THE INTERCOSTAL WAS REMOVED AN D REPLACED IAW ATR72 SRM 51-25-01 AND 51-25-03. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052900152 20020529 00152 EU 2002 5 29 SIMA200126502 1 20010917 A 5347 EPNE95300013018 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 420AT 420 SAW - DURING CPCP2 INSPECTION, FOUND CORROSION ON THE LEFT AFT OUTBOARD SEAT TRACK. THE SEAT TRACK WAS REMOVED AND REPL ACED IAW AMERICAN EAGLE ENGINEERING ORDER E2-53MR-115 REV 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052900153 20020529 00153 EU 2002 5 29 SIMA200126503 1 20010917 A 5320 S5367121729801 TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 420AT 420 SAW - DURING CPCP2 INSPECTION, FOUND CORROSION ON THE PASSENGER ENTRY SILL PLATE DRAIN TRACK. THE DRAIN TRACK WAS REMOV ED AND REPLACED IAW ATR72 SRM 51-25-01. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002053100029 20020531 00029 NM 2002 5 31 RYN2002F00001 1 20010805 A 5100 SKIN BOEING 727 72721 1384003 NM PWA JT8 JT8D1 52044 NE STRINGER DAMAGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 357QS 19259 BULGING/PILLOWING SKIN ALONG STRINGER 4L AT LAP JOINT BS 1130 THRU BS 1183. ACCOMPLISHED FUSELAGE SKIN REPAIR FROM BS 1 130 TO BS 1183 STRINGER 4L DUE TO CORROSION IAW SRM. (MATERIAL USED 2024-T3 .050 INCH, 98 INCHES X 9.1250 INCHES) 2 L 7 3 4F 4 F A3WE E2EA 2002053100057 20020531 00057 NM 2002 5 31 RYN2002F00003 1 20010805 A 5100 SKIN BOEING 727 72721 1384003 NM PWA JT8 JT8D1 52044 NE BS1176-BS1183 CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 357QS 19259 BULGING SKIN/DISHED FASTENER AT BS 1176 THRU BS 1183, STRINGER 20L THRU 21L UNDER AFT LAV SERVICE VALVE. ACCOMPLISHED F USELAGE SKIN REPAIR FROM BS 1176 TO BS 1183 STRINGER 20L TO STRINGER 21L DUE TO CORROSION. (MATERIAL USED 2024-T3. 07 1, 28 INCHES X 30 INCHES.) 2 L 7 3 4F 4 F A3WE E2EA 2002053100059 20020531 00059 NM 2002 5 31 RYN2002F00004 1 20010814 A 5100 STRINGER BOEING 727 72721 1384003 NM PWA JT8 JT8D1 52044 NE BS1148-BS1166 CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 357QS 19259 STRINGER EXFOLIATED BETWEEN BS 1148 TO BS 1166 BETWEEN STRINGER 3L AND 4L IN THE AFT CABIN CROWN AREA. ACCOMPLISHED FUS ELAGE STRINGER REPAIR BS 1148 TO 1166 BETWEEN STRINGER 3L AND 4L. DUE TO CORROSION IAW SRM. (MATERIAL USED 301 CRESS . 5000 HARD .050 INCH, 14 INCH X 1 INCH X 2 INCH.) 2 L 7 3 4F 4 F A3WE E2EA 2002060400089 20020604 00089 NM 2002 6 4 ASAA0240011 1 20010426 A 5320 65479579 THRESHOLD BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 780AS 25112 PAE - DURING SI CHECK, FOUND CORROSION OF SUB THRESHOLD WEB AT STATION 795-847 AND RBL 20-28 AND WL 160. REMOVED AND RE PLACED SUB THRESHOLD IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002060400093 20020604 00093 NM 2002 6 4 ASAA0240012 1 20010426 A 5320 654795711 THRESHOLD BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 780AS 25112 PAE - DURING SI CHECK, FOUND CORROSION OF SUB THRESHOLD WEB AT STATION 787-794 AND RBL 20 AND WL 157. REMOVED AND REPLA CED SUB THRESHOLD IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002060400240 20020604 00240 NM 2002 6 4 UIEA01108 1 20011228 A 2697 WIRE BOEING 747 7472F6B 1384807 NM FIRE LOOP SHORTED A UIEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 15 534MC 21832 ON TAKEOFF ROLL, FIRE DETECTION MASTER CAUTION LIGHT FLICKERED. NR 2A FIRE LOOP NACELLE JUMPED FROM 1-5. ACCOMPLISHED PNEUMATIC LEAK CHECK. NO LEAKS FOUND. NR 2 ENGINE FIRE DETECTION LOOP 'A' FAILED OPERATIONAL TEST. WIRE NR W3296-2W10 -18R FOUND SHORTED TO GROUND ON THE BACK OF CONNECTOR DX202A. WIRING REPLACED AS PER SWPM 20-10-11. LOOP 'A' OPERATION AL TESTED OK PER MM 26-11-00. (M) 2 L 7 4 4F A20WE 2002060600301 20020606 00301 NM 2002 6 6 S01427003 1 20010131 A 2700 FLAP BOEING BOEING 747 747400 NM PWA 4056 PW4056 NE LH INBD DAMAGED W SAJF O OTHER O OTHER LD LANDING 1 WP 03 24312 B18275 AFT LANDING FOUND LH INBD FORE FLAP DAMAGED.C/A:1.LH INBD FORE FLAP, MIDFLAP, LINK, SEQUENCE CARRIAGE, FITTING AN D FIX PANEL DAMAGED WERE FOUND. 2.SENT AOG TEAM TO BKK, DAMAGED PARTS WERE REPAIRED OR REPLD. A/C RETURNED TO TPE ON 200 1/02/03. 3.MIDFLAP, ROD, AND SEQUENCE CARRIAGE DAMAGED WERE AGAIN FOUND DURING POST FLIGHT INSPECTION IN TPE. 4.AFT REMO VED FORE FLAP TRACK ACCESS PANEL, FOUND THE FRACTURED OF FORE FLAP TRACK IN AFT END. 5.EON 744-27-636630-0001/-0002R1 WE RE ISSUED TO PERFORM ONE TIME INSPECTION OF INBD FORE FLAP TRACK DAMAGED. THE ROOT CAUSE OF THE SKEW CONDITION MAY BE FL AT-SPOTTING OF THE SEQUENCE CARRIAGE DETENT ROLLER, NOT THE FORE FLAP TRACK. DO THE NECESSARY MAINTENANCE INSPECTION A 2 L 7 4 4F 4 F RT A20WE E24NE 2002061100039 20020611 00039 NM 2002 6 11 RYN2002F00000 1 20010805 A 5230 SUPPORT BOEING 727 72721 1384003 NM CARGO DOOR DAMAGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 357QS 19259 AT MAIN CARGO DOOR FORWARD ACTUATOR, FORWARD AND AFT SUPPORT BLOCK ON DOOR STATION 540, 5 BOLTS HAVE OBLONGED/ELONGATED HOLES AND 1 LOOSE BOLT. ACCOMPLISHED MAIN CARGO DOOR FORWARD ACTUATOR SUPPORT BLOCK ATTACH INTERCOSTALS (2 EACH: FORWA RD AND AFT) REPLACEMENT DUE TO ELONGATED HOLES. 2 L 7 3 4F A3WE 2002061200058 20020612 00058 EA 2002 6 12 CA020508007 1 20010530 A 6123 C6NE10473 SWITCH DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6* 52043 EA PROP CONTROL SHORTED W A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CA (CAN) AFTER LIFT-OFF NOTICED TORQUE INCREASING & PROP RPM DECREASING ON ENGINE NR 1. VISUAL CHECK FROM LT CONFIRMED THAT ENGINE NR 1 HAD GONE INTO FEATHER. WERE BARELY 200 AGL WHEN OCCURRED. IDENTIFIED & FEATHERED NR 1 ENGINE (POWERLEVER ID LE PROP FEATHERED). NO IND. IN COCKPIT TO CONFIRM WHAT CAUSED PROBLEM. DECIDED TO TURN AROUND & LAND IMMEDIATELY. TAKEO FF HAD BEEN ON RWY 23 BUT LANDED ON 05, AS WINDS WERE CALM. ONLY ON GROUND AFTER PARKING TRIED TO RUN ENGINE TO CHECK W HAT MIGHT HAVE GONE WRONG THAT STEADY BETA RANGE LIGHTS CAME ON. SHUTDOWN & CALLED FOR HELP. 1 H 7 2 3T 3 T RT A9EA E2NE 2002061200092 20020612 00092 2002 6 12 CA020508008 4 20010917 A 6122 8210004 CSU DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6* 52043 EA RT ENGINE FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 CA (CAN) IN CRUISE AT 3,500 FT THE RT ENGINE PROP RPM REDUCED TO 40 PERCENT WITH TORQUE ON RT ENGINE INCREASING. WE REDUCED POWER. PROP RPM CONTINUED TO REDUCE TO 20 PERCENT. POWER WAS REDUCED FURTHER TO IDLE. NO BETA INDICATION. I CALLED FOR THE PROPELLER FEATHERING CHECKLIST. CARRIED OUT THE CHECKS AND SECURED THE ENGINE. BRIEFED THE PASSENGERS. CARRIED OUT A SINGLE ENGINE APPROACH AND LANDING. TAXIED IN AND SECURED AIRCRAFT.DURING GROUND RUN IN PHC, FOUND RT CONSTANT SPEED UN IT FAILED. UNIT REPLACED AND ALL NECESSARY ENGINE CHECKS REQUIRED C/OUT. AIRCRAFT RETURNED TO SERVICE. 1 H 7 2 3T 3 T RT A9EA E2NE 2002061200101 20020612 00101 NM 2002 6 12 CA020508013 1 20010114 A 5230 85237004001 WARNING LIGHT DHAV DHC8 DHC8* NM PWC 150 PW150A EA AFT CARGO DOOR FALSE ACTIVATION W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA (CAN) AFTER TAKEOFF WHILE CLIMBING THROUGH 2000 FT THE FUSELAGE DOOR WARNING LIGHT ILLUMINATED. QRH PROCEDURE COMPLETED AND UNEVENTFUL LANDING COMPLETED. INVESTIGATION DISCOVERED THE DOOR HANDLE SLIGHTLY OUT. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061700032 20020617 00032 NM 2002 6 17 CA020515010 1 20011227 A 5210 HINGE DHAV DHC8 DHC8* NM PWC 150 PW150A EA FWD PAX DOOR FROZEN W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) WHEN DEPARTING IN HEAVY SNOWFALL AND DURING LANDING ROLL RECEIVED DOOR WARNING ON FORWARD PAX DOOR. TAXIED TO PLAT FORM, DOOR WARNING DISAPPEARED. WHEN CA 1 OPENED THE PAX DOOR, WAS NOT ABLE TO OPEN IT FROM INSIDE. THE GROUND STAFF WAS ABLE TO OPEN THE DOOR FROM THE OUTSIDE. THERE WAS A LOT OF ICE ON THE DOOR FRAME AND ON THE DOOR. THE AIRCRAFT WAS DEFR OSTED USING A GROUND HEATER AND THE WATER WAS DRAINED FROM THE DOOR HINGE AREA. AIRCRAFT RETURNED TO SERVICE. MAINTENANC E INVESTIGATION DETERMINED ACCUMILATION OF WATER IN THE DOOR HINGE AREA WILL FREEZE AND LIMIT THE MOVEMENT OF THE DOOR H INGES. DRAINING OF THE FWD PAX HINGE AREA HAS BEEN INTRODUCED ON EVERY LINE CHECK. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061700033 20020617 00033 NM 2002 6 17 CA020515011 1 20011230 A 5210 HINGE DHAV DHC8 DHC8* NM PWC 150 PW150A EA FWD PAX DOOR FROZEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) CREW REPORTED UNABLE TO OPEN FWD PAX DOOR TO DISEMBARK PASSENGERS. TEMP -21 DEGS. STATION CALLED TO ARRANGE STAIRW AY TO ALLOW DEBARKATION THROUGH AFT PAX DOOR. GROUND CREW RECEIVED FWD PAX DOOR OPENED (W/O EASE). PASSENGERS WERE FINAL LY DISEMBARKED THROUGH FWD PASSENGER DOOR. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061700057 20020617 00057 NM 2002 6 17 CA020516008 1 20011227 A 2612 101098 DETECTOR DHAV DHC8 DHC8* NM PWC 150 PW150A EA OVERHEAT MALFUNCTIONED W O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 CA (CAN) WHEN STARTING ENGINE NR 2, AND SELECTING FUEL ON, MASTER WARNING CAME ON. CONDITION LEVER WAS SELECTED OFF AND STA RT WAS DISCONTINUED. WARNING WAS FIRE DETECT, AND FAULT ON FIRE LOOP A. MAINTENANCE INVESTIGATION/ACTION: RT ENGINE FIRE /OVERHEAT DETECTOR REPLACED 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061700087 20020617 00087 SW 2002 6 17 CA020517007 1 20010817 A 3397 MS27039109 SCREW BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL PANEL SHORTED W O OTHER H ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 CA (CAN) ON ACTIVATION OF LANDING LIGHTS, CIRCUIT BREAKER TRIPPED. CIRCUIT BREAKER WAS RESET AND LIGHTS ACTIVATED AGAIN. CI RCUIT BREAKER AGAIN TRIPPED. ON INVESTIGATION OF DEFECT, LT LANDING LIGHT RELAY FOUND TO BE SHORTED OUT BECAUSE OF CONTA CT FROM SCREW HOLDING ACCESS PANEL ON LT LOWER SIDE OF INSTRUMENT PANEL. SCREW LENGTH FOUND TO BE IMPROPER LENGTH AND PE NETRATED THROUGH NUT PLATE AND THROUGH SIDE OF RELAY CAUSING IT TO SHORT OUT AND TRIP CIRCUIT BREAKER. PROPER SCREW LENG TH SHOULD BE USED SO THAT THIS PROBLEM DOES NOT REOCCUR. 1 G 7 1 3U 3 U H2SW E1GL 2002061800012 20020618 00012 SO 2002 6 18 CA020523014 1 20010822 A 5513 BRACKET PIPER PA32 PA32300 7103212 SO LYC O540 IO540K1A5 41532 EA STAB TRIM CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) CRACKS FOUND WHERE STABILATOR TRIM BRACKET MEETS THE STABLATOR TRIM TAB DURING UNRELATED INSPECTION. AREA REINFORC ED BY AMO. 1 L 7 1 3O 3 O A3SO 1E4 2002062100093 20020621 00093 CE 2002 6 21 CB52002F00000 1 20010724 A 3231 99101364 ACTUATOR CESSNA 421 421C 2076016 CE MLG MISINSTALLED B CB5Y K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 35 6315X 2760 421C1003 RIGHT MAIN LANDING GEAR ACTUATOR (PN 99101364). THERE IS A POSSIBILITY THAT THE ACTUATOR MIGHT HAVE HAD ONE SEGMENT INC ORRECTLY FITTED. 1 L 7 2 3O A7CE 2002062800033 20020628 00033 WP 2002 6 28 UPS02838365 1 20010422 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C13 LT EXT FUS SKIN HAS BULGES WITH SURFACE CORROSION L27L APPROX STA 1640-1670 AT FASTENERS. REMOVED C ORROSION PER DC8 SRM 51-1-8, OUT OF LIMITS. FABBED REPAIR DOUBLERS, FINGER DOUBLERS, AND FILLER PER DC8 SRM 53-2-1 FIG 7. INSTALLED PER DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2002070200205 20020702 00205 WP 2002 7 2 IXXA0200041O 1 20010629 A 3210 SENSOR DOUG DC8 DC863 302198A WP DOOR DIRTY A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 786AL 84136 2576 46121 AFTER TAKE OFF FROM LAX, THE LANDING GEAR DOOR NOT LATCHED LIGHT ILLUMINATED FOLLOWING LANDING GEAR RETRACTION. THE FLI GHT CREW CYCLED THE GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO DEN FOR AN UNEVENTFUL LA NDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED DIRT BUILD UP ON THE SENSORS. MAINTENANCE CLEANED THE SENSORS AND PERFORMED SUCESSFUL OPERATIONAL CHECKS. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002071000084 20020710 00084 NM 2002 7 10 2002F00685 1 20010822 A 5311 FRAME BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND CORROSION AT STATION 351 AFT SIDE UNDER FRAME CHORD 6 INCHES INBOARD OF STRINGER 26L. (M) 2 L 7 3 4F A3WE 2002071000085 20020710 00085 NM 2002 7 10 2002F00686 1 20010822 A 5311 FRAME BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND STATION 351 HAS CORROSION AT LOWER FLANGE, LOWER SURFACE, INBOARD OF STRINGER 26L. (M) 2 L 7 3 4F A3WE 2002071000086 20020710 00086 NM 2002 7 10 2002F00687 1 20010822 A 5320 STRUCTURE BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND FS 344 HAS CORROSION ON LOWER FLANGE, LOWER SURFACE, INBOARD OF STRINGER 26L. (M) 2 L 7 3 4F A3WE 2002071000087 20020710 00087 NM 2002 7 10 2002F00688 1 20010822 A 5311 FRAME BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND STATION 351 HAS CORROSION AT LOWER FLANGE, LOWER SURFACE, INBOARD OF STRINGER 26L. (M) 2 L 7 3 4F A3WE 2002071000088 20020710 00088 NM 2002 7 10 2002F00689 1 20010820 A 5312 PRESSURE PANEL BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 NOSE LANDING GEAR WHEEL WELL STATION 328 TO 351 LEFT VERTICAL WEB HAS CORROSION ON INBOARD SIDE LOWER EDGE. (M) 2 L 7 3 4F A3WE 2002071000089 20020710 00089 NM 2002 7 10 2002F00690 1 20010820 A 5312 PRESSURE PANEL BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 NOSE LANDING GEAR WHEEL WELL STATION 328 TO STATION 351 RIGHT VERTICAL WEB HAS CORROSION ON INBOARD SIDE LOWER EDGE. (M ) 2 L 7 3 4F A3WE 2002071000090 20020710 00090 NM 2002 7 10 2002F00691 1 20010820 A 5312 PRESSURE PANEL BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 NOSE WHEEL WELL STATION 285 TO STATION 312 RIGHT VERTICAL WEB LOWER EDGE HAS CORROSION ON OUTBOARD SIDE. (M) 2 L 7 3 4F A3WE 2002071000091 20020710 00091 NM 2002 7 10 2002F00692 1 20010817 A 5321 FLOOR PANEL BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND CORROSION ON UNDERSIDE OF COCKPIT FLOOR PANEL NR 2306. (M) 2 L 7 3 4F A3WE 2002071000092 20020710 00092 NM 2002 7 10 2002F00693 1 20010817 A 5321 FLOOR PANEL BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND CORROSION ON COCKPIT FLOOR PANEL 2303, UNDER FACE. (M) 2 L 7 3 4F A3WE 2002071000093 20020710 00093 NM 2002 7 10 2002F00694 1 20010817 A 5321 FLOOR PANEL BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND CORROSION ON UNDERSIDE OF COCKPIT FLOOR PANEL NR 2301. (M) 2 L 7 3 4F A3WE 2002071000094 20020710 00094 NM 2002 7 10 2002F00695 1 20010817 A 5321 FLOOR PANEL BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND CORROSION ON COCKPIT FLOOR SUPPORT PANEL BS 259.5 FROM RBL 0 TO 12 AND FROM LBL 0 TO LBL 32. (M) 2 L 7 3 4F A3WE 2002071000095 20020710 00095 NM 2002 7 10 2002F00696 1 20010817 A 5321 FLOOR PANEL BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND CORROSION ON COCKPIT FLOOR SUPPORT PANEL FROM BS 259.5 TO BS 282.5 AT LBL 8. (M) 2 L 7 3 4F A3WE 2002071000096 20020710 00096 NM 2002 7 10 2002F00697 1 20010817 A 5320 FLOOR SUPPORT BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND CORRODED COCKPIT FLOOR SUPPORT ANGLE AT BS 295 RBL 10 INCHES. (M) 2 L 7 3 4F A3WE 2002071000097 20020710 00097 NM 2002 7 10 2002F00698 1 20010802 A 5347 SEAT TRACK BOEING 727 72721 1384003 NM FUSELAGE DAMAGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND MAIN CABIN FLOOR SEAT TRACK DAMAGED AT BS 640, RBL 24. (M) 2 L 7 3 4F A3WE 2002071000098 20020710 00098 NM 2002 7 10 2002F00699 1 20010802 A 1430 SCREW BOEING 727 72721 1384003 NM SEAT TRACK MISSING A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND MAIN CABIN FLOOR SEAT TRACK, JUST AT MAIN CARGO DOOR FRAME, HAS LOOSE AND MISSING SCREWS, LBL 64 BETWEEN BS 540 TO BS 660. (M) 2 L 7 3 4F A3WE 2002071000099 20020710 00099 NM 2002 7 10 2002F00700 1 20010731 A 5321 FLOOR PANEL BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND CORROSION ON COCKPIT FLOOR SUPPORT PANELS FROM BS 257.5 TO BS 312, AT LBL 13. (M) 2 L 7 3 4F A3WE 2002071000100 20020710 00100 NM 2002 7 10 2002F00701 1 20010731 A 5321 FLOOR PANEL BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND CORROSION ON COCKPIT FLOOR SUPPORT PANEL BETWEEN BS 289.5 AND BS 312 AT RBL 12. (M) 2 L 7 3 4F A3WE 2002071000102 20020710 00102 NM 2002 7 10 2002F00702 1 20010731 A 2510 PANEL BOEING 727 72721 1384003 NM COCKPIT CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND CORROSION ON 2ND OBSERVER SEAT SUPPORT PANEL AFT AND FORWARD EDGE. (M) 2 L 7 3 4F A3WE 2002071000103 20020710 00103 NM 2002 7 10 2002F00703 1 20010726 A 5310 DOOR FRAME BOEING 727 72721 1384003 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 AFT ENTRY DOOR LEFT SIDE FRAME BS 1183 NR 2 STOP FRAME CUTOUT IS CRACKED, RUNNING APPROX TO AFT WATERLINE 270. (M) 2 L 7 3 4F A3WE 2002071000105 20020710 00105 NM 2002 7 10 2002F00704 1 20010726 A 5532 SKIN BOEING 727 72721 1384003 NM VERTICAL STAB BULGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND VERTICAL STAB BS 1342 RIGHT SIDE STRINGER 10R HAS BULGING SKIN. (M) 2 L 7 3 4F A3WE 2002071000107 20020710 00107 NM 2002 7 10 2002F00705 1 20010719 A 5510 BEARING BOEING 727 72721 1384003 NM HORIZ STAB EXCESS PLAY A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND LEFT STAB BEARING HAS .045 OF PLAY. (M) 2 L 7 3 4F A3WE 2002071000108 20020710 00108 NM 2002 7 10 2002F00706 1 20010719 A 3230 SUPPORT BOEING 727 72721 1384003 NM NLG CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND NOSE LANDING GEAR DRAG BRACE SUPPORT BEAM, CRACK ON AFT CORNER RIGHT SIDE OF SUPPORT BEAM, JUST AFT OF NOSE WHEEL WELL. (M) 2 L 7 3 4F A3WE 2002071000110 20020710 00110 NM 2002 7 10 2002F00707 1 20010821 A 5312 PRESSURE PANEL BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND NOSE WHEEL WELL STATION 312 TO STATION 285 LEFT VERTICAL WEB LOWER EDGE HAS CORROSION ON OUTBOARD SIDE. (M) 2 L 7 3 4F A3WE 2002071000112 20020710 00112 NM 2002 7 10 2002F00708 1 20010820 A 5311 FRAME BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND FRAME LOWER FLANGE HAS CORROSION AT STATION 312 BELOW STRINGER 26R. (M) 2 L 7 3 4F A3WE 2002071000113 20020710 00113 NM 2002 7 10 2002F00709 1 20010820 A 5311 FRAME BOEING 727 72721 1384003 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND FRAME LOWER FLANGE CRACKED AT STATION 320 BELOW STRINGER 26R. (M) 2 L 7 3 4F A3WE 2002071000115 20020710 00115 NM 2002 7 10 2002F00710 1 20010809 A 5330 DOUBLER BOEING 727 72721 1384003 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND MAIN CARGO DOOR CUTOUT EXTERNAL DOUBLER CRACKED AND BULGED AT STATION 17L BS 560. (M) 2 L 7 3 4F A3WE 2002071000119 20020710 00119 NM 2002 7 10 2002F00711 1 20010807 A 5320 SILL BOEING 727 72721 1384003 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND CABIN FUSELAGE STATION BS 480 STRINGER 17L LOWER SILL BEAM TIED FRAME TO FUSELAGE, FORWARD AND AFT, ARE CRACKED. (M) 2 L 7 3 4F A3WE 2002071000120 20020710 00120 NM 2002 7 10 2002F00712 1 20010807 A 5320 SILL BOEING 727 72721 1384003 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND LOWER FORWARD CARGO COMPARTMENT BS 680 LOWER SILL BEAM AT SPLICE, BOTTOM ROUTED OUT, ELONGATED AND CRACKED. ALSO, MISSING RIVET INTERIOR TO FUSELAGE SKIN. (M) 2 L 7 3 4F A3WE 2002071000121 20020710 00121 NM 2002 7 10 2002F00713 1 20010816 A 5311 FRAME BOEING 727 72721 1384003 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND FUSELAGE LOWER FORWARD CARGO, BS 700 STATION 20L, AT FRAME TO SKIN WEB, HAS A CRACK AT RIVET. (M) 2 L 7 3 4F A3WE 2002071000122 20020710 00122 NM 2002 7 10 2002F00714 1 20010802 A 5311 FRAME BOEING 727 72721 1384003 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND MAIN CABIN FUSELAGE FRAME CRACKED AND AFT SIDE ATTACH ANGLE CRACKED AT STATION 480 JUST BELOW STRINGER 17L. (M) 2 L 7 3 4F A3WE 2002071000123 20020710 00123 NM 2002 7 10 2002F00715 1 20010802 A 5330 DOUBLER BOEING 727 72721 1384003 NM FUSELAGE BULGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND FUSELAGE EXTERIOR SKIN DOUBLER HAS BULGE AT STRINGER 10L BS 470, JUST FORWARD OF MAIN CARGO DOOR. (M) 2 L 7 3 4F A3WE 2002071000124 20020710 00124 NM 2002 7 10 2002F00716 1 20010816 A 5320 INTERCOSTAL BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND CORROSION ON INTERCOSTAL BETWEEN BS 970 AND BS 990 AT LBL 16. (M) 2 L 7 3 4F A3WE 2002071000125 20020710 00125 NM 2002 7 10 2002F00717 1 20010821 A 5313 STRINGER BOEING 727 72721 1384003 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND LOWER CARGO COMPARTMENT BETWEEN BS 680 AND BS 700 STRINGER 20L SHOWS CRACK TO CENTER. ALSO, BS 700 FRAME TIED TO FUSELAGE IS CRACKED FROM TOP FASTENER. (M) 2 L 7 3 4F A3WE 2002071000126 20020710 00126 NM 2002 7 10 2002F00718 1 20010727 A 5230 PANEL BOEING 727 72721 1384003 NM CARGO DOOR CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND LOWER AFT CARGO COMPARTMENT DOOR INNER BOTTOM BAFFLE PANEL HAS A BEND AT CORNERS WITH TWO CRACKS, ONE OVER PREVIOU S REPAIR. (M) 2 L 7 3 4F A3WE 2002071000127 20020710 00127 NM 2002 7 10 2002F00719 1 20010727 A 5230 SKIN BOEING 727 72721 1384003 NM CARGO DOOR CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND LOWER AFT CARGO COMPARTMENT DOOR SKIN HAS A CRACK CLOSE TO REAR LOWER EDGE. (M) 2 L 7 3 4F A3WE 2002071000128 20020710 00128 NM 2002 7 10 2002F00720 1 20010727 A 5330 SKIN BOEING 727 72721 1384003 NM FUSELAGE BULGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND EXTERNAL LEFT FUSELAGE LAP SEAM STATION 400 TO 420, STRINGER 26L HAS A BULGE. (M) 2 L 7 3 4F A3WE 2002071000129 20020710 00129 NM 2002 7 10 2002F00721 1 20010726 A 5320 PLATE BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND FUSELAGE INTERIOR AT BS 294 BL 0 CORROSION DAMAGE TO PLATE ABOVE NOSE WHEEL WELL STRUCTURE WHERE 2 CONTROL CABLES PASS THROUGH UP/DOWN DIRECTION. (M) 2 L 7 3 4F A3WE 2002071000130 20020710 00130 NM 2002 7 10 2002F00722 1 20010726 A 5310 STOP FITTING BOEING 727 72721 1384003 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND FORWARD ENTRY DOOR FORWARD CUTOUT STOP FITTING NR 4 FROM TOP IS CRACKED TO LOWER AFT. (M) 2 L 7 3 4F A3WE 2002071000131 20020710 00131 NM 2002 7 10 2002F00723 1 20010726 A 5313 STRINGER BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND FUSELAGE INTERIOR AT BS 294 THROUGH BS 314 STRINGER 21R HAS SURFACE CORROSION. (M) 2 L 7 3 4F A3WE 2002071000132 20020710 00132 NM 2002 7 10 2002F00724 1 20010726 A 5320 ANGLE BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND FUSELAGE INTERIOR AT BS 351.2 RBL 48, CORROSION DAMAGE TO UPPER END OF ANGLE BETWEEN SKIN AND FRAME, JUST ABOVE WA LKWAY WEB PANEL, STRINGER 22 AREA. (M) 2 L 7 3 4F A3WE 2002071000134 20020710 00134 NE 2002 7 10 AALA20010383 2 20010307 A 7261 515107 SCAVENGE PUMP DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE LT ENGINE FAILED A AALA O OTHER J WARNING INDICATION DE DESCENT 1 SW 21 441AA 49460 DFW - FLT 1456 - EN ROUTE DEN-DFW - UPON DESCENT DETECTED LEFT ENGINE OIL PRESSURE LOW CAUTION LIGHT ILLUMINATE. LEFT O IL QUANTITY DECREASED TO ZERO AND LEFT ENGINE WIND MILLED UNTIL TOUCH DOWN. LANDED DFW WITHOUT FURTHER INCIDENT. REPLA CED LEFT SIDE ENGINE. THE NR 4 AND 5 SCAVENGER PUMPS FAILED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F A6WE E9NE 2002071000135 20020710 00135 NE 2002 7 10 AALA20010627 2 20010326 A 7250 TURBINE BLADES DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE NR 2 ENGINE FAILED A AALA E ENGINE SHUTDOWN O OTHER NR NOT REPORTED 1 SW 21 400AA 49311 717840 ORD - FLT 1487 - EN ROUTE ORD-LAX, DETECTED A LOUD BANG AT NR 2 SIDE ENGINE. SHUT DOWN NR 2 SIDE ENGINE. RETURNED ORD AND LANDED WITHOUT INCIDENT. THE 3RD AND 4TH STAGE TURBINE BLADES FAILED AT OR NEAR THE ROOT. REPLACED NR 2 ENGINE. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F A6WE E9NE 2002071000136 20020710 00136 NE 2002 7 10 AALA20010782 2 20010413 A 7250 TURBINE BLADES DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE NR 1 ENGINE FAILED A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 70404 49315 718489 DFW - FLT 1319 - EN ROUTE DFW-SNA - ON CLIMB-OUT, DETECTED A LOUD BANG AT NR 1 SIDE ENGINE. RETURNED DFW AND LANDED WIT HOUT FURTHER INCIDENT. REPLACED NR 1 SIDE ENGINE. FOURTH STAGE TURBINE BLADES FAILED AT OR NEAR THE ROOT. LEADING EDG E STAGE 3 TURBINE BLADES WERE DAMAGED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F A6WE E9NE 2002071000137 20020710 00137 WP 2002 7 10 AALA20010840 1 20010420 A 7931 SENSE LINE DOUG DC9 DC982 3022082 WP NR 2 ENGINE FAILED A AALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 21 225AA 49175 IAD - FLT 1921 - EN ROUTE IAD-DFW - DETECTED RIGHT SIDE OIL PRESSURE DECREASE TO ZERO. RETURNED IAD AND LANDED WITHOUT FURTHER INCIDENT. REPLACED RIGHT SIDE ENGINE. ANALYSIS DETERMINED THAT THE OIL PRESSURE SENSING LINE FAILED. SYSTEM G ROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002071000156 20020710 00156 WP 2002 7 10 AALA20011288 1 20010622 A 4920 5940405503 APU DOUG DC9 DC982 3022082 WP APU BAY LEAKING A AALA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 465A 49595 LAX - FLT 2430 - EN ROUTE LAX-DFW, FLIGHT ATTENDANT DETECTED SMOKE IN CABIN AND COCKPIT. RETURNED LAX AND LANDED WITHOU T FURTHER INCIDENT. PRECAUTIONARY REPLACED APU. NO ABNORMAL WEAR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002071000158 20020710 00158 EU 2002 7 10 AALA20011842 1 20011003 A 3230 D82310403 ACTUATOR FOKKER F28 F28MK0100 4990807 EU NLG FAILED A AALA O OTHER J WARNING INDICATION LD LANDING 1 SW 21 1448A 11457 DFW - TUL-DFW - AIRCRAFT LANDED DFW WITH UNSAFE GEAR INDICATION. AWAITING SAFETY MEASURES NOSE GEAR STRUT COLLAPSED. T HE NOSE LANDING GEAR DOWNLOCK ACTUATOR FAILED CAUSING THE GEAR TO COLLAPSE WHEN TOWED. REPLACED NOSE LANDING GEAR DOWNL OCK ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2002071000159 20020710 00159 NE 2002 7 10 AALA20011897 2 20011014 A 7250 TURBINE BLADES DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE LT ENGINE FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 591AA 53254 709998 ORD - FLT 1477 - LEFT ENGINE FAILURE IN FLIGHT SHORTLY AFTER TAKEOFF N1 ROTATED AT 14 PERCENT N2 AT 15 PERCENT OIL QUANT ITY DIMINISHED TO ZERO AND OIL PRESSURE TO 2 PSI. RETURNED AND LANDED ORD WITHOUT INCIDENT. REPLACED LEFT ENGINE, PERF ORMED LEAK CHECK. INVESTIGATION REVEALED TURBINE BLADE FAILURE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2002071100016 20020711 00016 NE 2002 7 11 AALA20011571 2 20010804 A 7510 DUCT DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE RT ENGINE MALFUNCTIONED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 597AA 53287 DFW - FLT 1339 - EN ROUTE DFW-SEA - FIRE WARNING LIGHT ILLUMINATED AFTER TAKEOFF. LANDED DFW WITHOUT INCIDENT. INSPECT ED ENGINE AND FIRE WARNING SYSTEM. PLACARDED A LOOP FIRE WARNING INOPERATIVE PER MEL. REPLACED RIGHT ENGINE ANTI-ICE S UPPLY DUCT ON LEFT SIDE OF POWER PLANT BETWEEN ENGINE BLEED AND VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2002071200102 20020712 00102 NM 2002 7 12 RIVA011217 1 20011217 A 5523 TAB BOEING 727 7272J0 138407E NM ELEVATOR DELAMINATED A RIVA K NONE O OTHER IN INSP/MAINT 1 NE 05 362PA 21106 RIGHT ELEVATOR TAB DELAMINATED AT AFT OUTBOARD END. REMOVED DELAMINATED AREA OF SKIN .75 INCH BY .75 INCH IAW BOEING SR M 51-40-20 FIG 20. FABRICATED AND INSTALLED DOUBLER IAW BOEING SRM 51-40-20 FIG 20. (M) 2 L 7 3 4F RT A3WE 2002071200104 20020712 00104 NM 2002 7 12 RIVA011218 1 20011218 A 5755 SKIN BOEING 727 7272J0 138407E NM SPOILER CORRODED A RIVA K NONE O OTHER IN INSP/MAINT 1 NE 05 362PA 21106 NR 6 SPOILER UPPER SKIN CORRODED. FABRICATED FILLER AND DOUBLER IAW BOEING SRM 51-40-20 FIG 5 AND 14. BONDED AND SEALE D REPAIR PARTS IAW BOEING SRM 51-40-20 FIG 5, 14 AND SRM 51-20-4. (M) 2 L 7 3 4F RT A3WE 2002071600125 20020716 00125 CE 2002 7 16 DEM2002F00003 1 20011226 A 5751 0322709 HINGE BRACKET CESSNA 195 195B 2073112 CE AILERON CRACKED D DEMA K NONE O OTHER IN INSP/MAINT 1 CE 03 195BA 16069 BOTH BRACKETS CRACKED COMPLETELY ACROSS BEARING BOSSES. THIS IS A RECURRING AND EXTENSIVE PROBLEM THAT IS POTENTIALLY V ERY CRITICAL FOR CONTROLLABILITY OF THE AIRCRAFT. WE WERE ABLE TO BREAK THE INBOARD END OF AN AILERON LOOSE FROM THE AI RCRAFT WITH APPROXIMATELY 40 LBS OF FORCE EXERTED BY HAND ON THE AILERON WITH A BEARING BOSS CRACKED ON THE HINGE BRACKE T. 1 H 7 1 3R A790 2002071600126 20020716 00126 CE 2002 7 16 DEM2002F00004 1 20011226 A 5751 03227091 HINGE BRACKET CESSNA 195 195B 2073112 CE AILERON CRACKED D DEMA K NONE O OTHER IN INSP/MAINT 1 CE 03 195BA 16069 BOTH BRACKETS CRACKED COMPLETELY ACROSS BEARING BOSSES. THIS IS A RECURRING AND EXTENSIVE PROBLEM THAT IS POTENTIALLY V ERY CRITICAL FOR CONTROLLABILITY OF THE AIRCRAFT. WE WERE ABLE TO BREAK THE INBOARD END OF AN AILERON LOOSE FROM THE AI RCRAFT WITH APPROXIMATELY 40 LBS OF FORCE EXERTED BY HAND ON THE AILERON WITH A BEARING BOSS CRACKED ON THE HINGE BRACK ET. 1 H 7 1 3R A790 2002071600127 20020716 00127 CE 2002 7 16 DEM2002F00005 1 20011226 A 5751 0322709 BRACKET CESSNA 195 195A 2073110 CE AILERON CRACKED D DEMA K NONE O OTHER IN INSP/MAINT 1 CE 03 195LR 16062 BOTH BRACKETS CRACKED ALL THE WAY ACROSS BEARING BOSS. SEVERELY CORRODED AND MOUNTING LEG OF ONE BRACKET BROKEN OFF. 1 H 7 1 3R A790 2002071600128 20020716 00128 CE 2002 7 16 DEM2002F00006 1 20011226 A 5751 03227091 HINGE BRACKET CESSNA 195 195A 2073110 CE AILERON CRACKED D DEMA K NONE O OTHER IN INSP/MAINT 1 CE 03 195LR 16062 BOTH BRACKETS CRACKED ALL THE WAY ACROSS BEARING BOSS. SEVERELY CORRODED AND MOUNTING LEG OF ONE BRACKET BROKEN OFF. 1 H 7 1 3R A790 2002071700006 20020717 00006 EA 2002 7 17 ASOA01299S 1 20011224 A 5346 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 826AS 7210 DURING C-CHECK INSPECTION IN MCN, WHILE COMPLYING WITH ASA EO600-63-0043, VISUAL INSPECTION OF THE ENGINE SUPPORT BEAMS, BOTH SIDES WERE FOUND TO HAVE A CRACK. MAINTENANCE COMPLETED STEPS 1-5 OF REO 601R-53-61-358 WHICH IS ANOTHER TEMPORAR Y REPAIR TO THE ENGINE SUPPORT BEAM. (M) 2 L 7 2 4F RT A21EA 2002071700232 20020717 00232 NM 2002 7 17 CALA0200382 1 20010702 A 3350 D71702030 CHARGER BOEING 737 737924 13848A1 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 38403 30120 INSPECTION FOUND EMERGENCY EXIT LIGHT L1417(OVERHEAD BIN 3B) INOPERATIVE. TROUBLESHOOTING FOUND PIN IN NR 3 FUSE OF CHA RGER BROKEN INSIDE. R&R CHARGER IAW MM 33-51-06. 2 L 7 4 4F RT A16WE 2002071800120 20020718 00120 NE 2002 7 18 CA020628004 2 20010805 A 7200 BLADE AIRBUS 310 A310300 3930305 EU GE CF6 CF680C2A5 NE COMPRESSOR DAMAGED W C ABORTED TAKEOFF C J F.O.D. WARNING INDICATION TO TAKEOFF 1 CA (CAN) COMPRESSOR STALL ON TAKE OFF IN LRM, ON ENGINE NR 2 , MTCE FOUND AFTER VISUAL INSPECTION, 2 BLADES DAMAGED. FURTHE R INSPECTION C/OUT IN ACCORDANCE WITH AMM 72-00-00 P.600, REVEALED DAMAGE ON HIGH PRESSURE COMPRESSOR. NUMEROUS BLADES N ICKED, CURLED, TORN OR PARTIALLY MISSING. DAMAGE NOT WITHIN LIMITS I.A.W. AMM 72-31-00 P.602. MAINTENANCE REPLACED THE E NGINE I.A.W. AMM 71-00-00. 2 L 7 2 4F 4 F RT A35EU E13NE 2002071900047 20020719 00047 EU 2002 7 19 DHL20013650 1 20011127 A 5313 STRINGER AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH 149 CORROSION ON STR 5R BETWEEN FR 32-34. CORROSION REMOVED PER SRM 51-40-11, FOUND TO BE OUT OF SRM LIMITS. CUT OUT DAMAG ED AREA PER SRM 53-10-10. FABRICATED REPAIR PARTS PER SRM 53-10-10. INSTALLED REPAIR PER SRM 51-30-20. 2 L 7 2 4F RT A35EU 2002072200008 20020722 00008 NM 2002 7 22 GAI2002F00002 1 20011002 A 3350 1000679 LIGHT BOEING 727 727251 138408H NM CABIN INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 255US 19974 DURING ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT WOULD NOT TEST. REMOVED AND REPLACE D EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2002082700096 20020827 00096 WP 2002 8 27 DHL2001806019 1 20010718 A 5610 WINDOW DOUG DC8 DC873F 302199F WP COCKPIT LACK OF LUBE A DHLA K NONE O OTHER UK UNKNOWN 1 SO 01 806DH 46002 CAPT'S/LEFT SLIDING WINDOW REQUIRES AT LEAST 20 LBS PULL FORCE TO OVERCOME BINDING RESISTANCE TO HOOK UNLATCHING PART OF WINDOW MECHANISM. LUBED CAPT'S SLIDING WINDOW, CLEARED TAPE FROM UPPER EDGE. OPS CHECK OK IAW MM 56-10-3. 2 L 7 4 4F RT 4A25 2002073000059 20020730 00059 EU 2002 7 30 SIMA200215602 1 20011219 A 5347 EPN395300013019 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 548AT 548 SAW - DURING CPCP4 INSPECTION, FOUND CORROSION ON RIGHT FLIGHT ATTENDANT SEAT TRACK. THE SEAT TRACK WAS REMOVED AND REP LACED IAW ENGINEERING ORDER E2-53MR-115R1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002080500113 20020805 00113 EU 2002 8 5 DHL200136550 1 20011201 A 7830 FRAME AIRBUS 300 A300B4203 3930306 EU THRUST REVERSER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH 149 NR 2 ENGINE THRUST REVERSER TRANSLATING SLIDING SLEEVE O/B FRAME CRACKED BETWEEN 2ND AND 3RD BLOCKER DOORS. REMOVED ACO USTIC LINER IN AREA OF CRACKED FRAME PER SRM 51-30-30. 2 L 7 2 4F RT A35EU 2002080500114 20020805 00114 EU 2002 8 5 DHL200136555 1 20011203 A 2550 TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH 149 RIGHT O/B ROLLER TRACK CORRODED AT FR 38/2/1. CORROSION REMOVED AT ROLLER TRACK AROUND CAMLOCK AREA PER SRM 51-40-11. FOUND OUT OF LIMITS AND REPAIRED PER SRM 53-10-10 PG-824-827. REPAIRED PER SRM 53-10-10 PG 824-827. 2 L 7 2 4F RT A35EU 2002080700023 20020807 00023 WP 2002 8 7 CA020702001 1 20011220 A 5711 SPAR DOUG B26 B26C 3200524 WP PWA R2800 R280027 52026 NE WING CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) CORROSION FOUND ON FRONT AND REAR SPAR CAP IN AUXILIARY FUEL BAY RIGHT HAND SIDE. CORROSION FOUND ON SPAR CAP IN A UXILIARY FUEL BAY LEFT HAND SIDE. 2 M 7 2 4R 4 R L34 5E8 2002080700188 20020807 00188 NE 2002 8 7 CA020709002 2 20011118 A 7200 ENGINE LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE NR 1 VIBRATION W E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION TO TAKEOFF 1 CA (CAN) VIBRATION INDICATION ON NR 1 ENGINE, 3.0 UNITS ON CHANNEL A AND B. THE ENGINE WAS SHUT DOWN IAW THE SOP. MAINTENAN CE REMOVED THE LP FAN BLADES , CLEANED AND REINSTALLED THEM IAW AMM 72-31-05. THE TEST NR 11, VIBRATION SURVEY WAS C/OUT AND FOUND TO BE WITHIN LIMITS AT 1.0 UNITS VIB AT TAKE OFF POWER, IAW AMM 72-00-00.- CLEANED AND LUBRICATED LP FAN COMP RESSOR BLADES (CLAPPERSIAW AMM 72-31-05. REMOVED AND INSPECTED MASTER AND INTERNAL GEARBOX MCDS IAW 72-01-00,NO CONTAMI NATION FOUND. REMOVED , INSPECTED AND REPLACED THE ENG. OIL FILTERS IAW AMM 72-01-00. BOROSCOPE C/OUT AND NO FAULTS FOUN D IAW AMM 72-00-00. 2 L 7 3 4F 4 F A23WE E12EU 2002080700205 20020807 00205 NM 2002 8 7 CA020712001 1 20010822 A 3320 BR63031023 SOCKET DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE SEAT ROW 1AB FAILED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA 38149 38149 (CAN) DURING A REMAIN OVERNIGHT MAINTENANCE VISIT A SNAG WITH THE SIDEWALL LIGHTING SYSTEM AT ROW 1AB WAS BEING ADDRESSE D. THE TECHNICIAN DISCOVERED THE LAMP END (P/N BRG6303-102-3S/N 149) WAS DISTORTED BECAUSE IT HAD MELTED. THE END WAS R EPLACED WITH NEW AND THE SYSTEM TESTED SERVICEABLE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002081900013 20020819 00013 NM 2002 8 19 ASAA01400107 1 20010925 A 5210 507945 ROLLER BOEING 737 7374Q8 138447Q NM L1 DOOR LACK OF LUBE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 754AS 25095 ANC - FOUND CREW REPORTED L1 DOOR DIFFICULT TO OPEN. LUBED DOOR LATCH ROLLERS AND CAMS THEN DOOR CHECKS NORMAL. (M) 2 L 7 2 4F RT A16WE 2002082100083 20020821 00083 NM 2002 8 21 DL72S020894 1 20010530 A 5753 ANGLE BOEING 727 727232 1384082 NM T/E FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 532DA 22045 AFT CHORD ANGLE CRACKED 22 INCHES AND 37 INCHES FROM THE I/B END. REPAIRED NR 3 FLAP CHORD ANGLE. 2 L 7 3 4F A3WE 2002082100099 20020821 00099 NM 2002 8 21 DL72W020879 1 20010727 A 3350 SIGN BOEING 727 727247 138408F NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 296WA 22533 LEFT SIDE EMERGENCY WINDOW EXITS SIGNS NEED TO BE RELAMPED. RELAMPED AS REQUIRED. 2 L 7 3 4F A3WE 2002082700094 20020827 00094 NM 2002 8 27 DHL2001705541 1 20010415 A 5312 PRESSURE PANEL BOEING 727 72722C 138400F NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C-CHECK, NOSE GEAR WHEEL WELL RT SIDEWALL PANEL IS CRACKED BS 285.6 WL 158 CRACK RUNNING ALONG FASTENERS ROWS, 2 PLAC ES. ACCOMPLISHED HFEC INSP OF NOSE WHEEL WELL RT SIDEWALL PANEL. VERIFIED AND MARKED ENDS OF CRACKS. CUTOUT DAMAGE SE CTION. NO FURTHER CRACK PROGRESSION NOTED. FABRICATED DOUBLER REPAIR FROM BS 250 TO 294.5 AS PER B727 S/B 53-00065 AND INSTALLED DOUBLER. 2 L 7 3 4F A3WE 2002082700095 20020827 00095 NM 2002 8 27 DHL2001724014 1 20011019 A 2611 SMOKE DETECTOR BOEING 727 727228 1384083 NM CARGO BAY MALFUNCTIONED A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 724DH 19862 LOWER CARGO FIRE DETECTION SYSTEM YELLOW LIGHT ILLUMINATED. REMOVED AND REPLACED INOP AFT PIT SMOKE DETECTOR. INSTALLE D NEW DETECTOR, SET UP SYSTEM AND IDENTIFIED, PER B727 M/M SUPPLEMENT 26-16-00. OPS CHECK NORMAL. 2 L 7 3 4F RT A3WE 2002082800074 20020828 00074 NM 2002 8 28 DL76S020919 1 20010807 A 3350 3017702 LIGHT BOEING 767 767332 1382001 NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 119DL 23278 FOUND ON L/O CHECK, DOOR R1 EXT EMERGENCY SLIDE LIGHT INOP. REPLACED LIGHT ASSY, CHECK GOOD. 2 L 7 2 4F RT A1NM 2002090200001 20020902 00001 NM 2002 9 2 FE5F200200004 1 20010806 A 5700 5911301505 SPAR CAP DOUG MD80 MD83 3023681 NM CORRODED W FE5F K NONE O OTHER IN INSP/MAINT 1 WP 03 7271 53602 During the ¡§C3 Check¡¨ in AUG 2001, this A/C found corrosion on the L/H wing lower rear spar cap, XRS173~175. IAW manuf acturer¡¦s instruction, operator performed temporary repair. Now manufacturer determined the accomplished temporary repa ir is acceptable for strength as a permanent repair and issued FAA Form 8110-3. The repair action from the original ¡§Mi nor¡¨ became ¡§Major¡¨. 2 L 7 2 4F RT 2002090300109 20020903 00109 WP 2002 9 3 WRNA00023 1 20011113 A 2170 7339308 COVER LKHEED 1011 10113851 5265010 WP A/C BAY OUT OF POSITION A WRNA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 05 311EA 193A1012 AT 27,000 FEET NR 2 PACK WATER SEPARATOR COVER BLEW OFF. CREW UNABLE TO MAINTAIN PRESSURIZATION ON NR 3 PACK ONLY. AIR CRAFT RETURNED TO BQN. FUEL DUMPED. AIRCRAFT LANDING NORMAL. WATER SEPARATOR COVER REINSTALLED, CLAMP SECURED AND TOR QUED IAM MM 21-51-07. OPERATIONAL CHECK AND LEAK CHECK PERFORMED. 2 L 7 3 4F A23WE 2002090400013 20020904 00013 WP 2002 9 4 MEX2002263 1 20011208 A 2797 833703 WIRE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE PROX SENSOR BROKEN W ASMF O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 23 505MD 49149 DURING TAXI CAPTAIN INFORMED THAT THE LIGHT OF RUDDER TRAVEL UNRESTRICTED DID NOT TURN ON. PROXIMITY SWITCH WAS VERIFIE D AND FOUND A FAILURE IN THE CARD 706. PROXIMITY SWITCH WAS REPLACED BUT FAILURE DID NOT CORRECT. PROXIMITY SENSORS WE RE VERIFIED AND SOME WIRES WERE FOUND BROKEN. SENSORS WERE REPLACED IAW MM TEST, OK. 2 L 7 2 4F 4 F A6WE E2EA 2002090400124 20020904 00124 WP 2002 9 4 UPS02839042 1 20010721 A 5330 57799253N1 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:C2 EVIDENCE OF CORROSION UNDER NR 2 ADF ANTENNA, CORRODED BEYOND LIMITS STA 70 TO 190 LONG 31L TO 31R. REMOVED AND REPLACED SKIN BETWEEN STA 70 TO 190 LONG 31L TO 31R IAW DWG 5779925, SRM 53-1-0, 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 2002090500003 20020905 00003 NM 2002 9 5 2002F00839 1 20010724 A 5711 SPAR BOEING 727 72721 1384003 NM RT WING CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 RIGHT WING HAS CRACKS AT REAR SPAR UPPER CHORD AT WING STATION 217 INBOARD OF LANDING GEAR. (M) 2 L 7 3 4F A3WE 2002090500004 20020905 00004 NM 2002 9 5 2002F00840 1 20010805 A 5330 SKIN BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 357QS 19259 BULGING SKIN ALONG STRINGER 10L AT BS 920 THROUGH 1005 DUE TO CORROSION. ACCOMPLISHED FUSELAGE SKIN REPAIR FROM BS 920 TO BS 1005 AT STRIGNER 10L IAW B727 SRM 53-30-3 FIG 14. (M) 2 L 7 3 4F A3WE 2002090500005 20020905 00005 NM 2002 9 5 2002F00841 1 20010806 A 5313 STRINGER BOEING 727 72721 1384003 NM FUSELAGE DAMAGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 357QS 19259 HOLE FOUND IN LOWER RADIUS AT BS 370 STRINGER 6R. ACCOMPLISHED FUSELAGE STRINGER REPAIR AT BS 370, STRINGER 6R IAW B727 SRM 53-10-2, FIGURE 2. (M) 2 L 7 3 4F A3WE 2002090500006 20020905 00006 NM 2002 9 5 2002F00842 1 20010805 A 5330 SKIN BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 357QS 19259 BULGING AND PILLOWING SKIN ON STRINGER 8L AT BS 1166 THROUGH BS 1183. ACCOMPLISHED FUSELAGE SKIN REPAIR FROM BS 1166 TO BS 1183 STRINGER 8L DUE TO CORROSION IAW B727 SRM 53-30-3, FIGURE 3. (M) 2 L 7 3 4F A3WE 2002090500007 20020905 00007 NM 2002 9 5 2002F00843 1 20010805 A 5311 FRAME BOEING 727 72721 1384003 NM MLGWW CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 357QS 19259 RIGHT NOSE WHEEL WELL, MID CHORD EXFOLIATED AT INTERSECTION OF RIGHT WEB AND FLOOR WEB AS VIEWED FROM DOG HOUSE. ACCOMP LISHED RIGHT NOSE WHEEL WELL MID CHORD REPLACEMENT IAW B727 SRM 51-30-2 AND 51-20-4. (M) 2 L 7 3 4F A3WE 2002090500008 20020905 00008 NM 2002 9 5 2002F00844 1 20010805 A 5312 PRESSURE PANEL BOEING 727 72721 1384003 NM NLG WW CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 357QS 19259 DUE TO CORROSION, RIGHT NOSE WHEEL WELL VERTICAL WEB EXFOLIATED AT INTERSECTION WITH UPPER NOSE CHORD AS VIEWED FROM DOG HOUSE BS 315. ACCOMPLISHED RIGHT NOSE WHEEL WELL VERTICAL WEB REPAIR IAW B727 SRM 53-10-2 FIGURE 1. (M) 2 L 7 3 4F A3WE 2002090500009 20020905 00009 NM 2002 9 5 2002F00845 1 20010805 A 5312 PRESSURE PANEL BOEING 727 72721 1384003 NM NLG WW CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 357QS 19259 NOSE WHEEL WELL RIGHT SIDE SKIN HAS A VERTICAL CRACK AT STATION 270. ACCOMPLISHED NOSE WHEEL WELL RIGHT SIDE SKIN REPAI R AT BS 270 IAW B727 SRM 51-40-2, FIGURE 1 AND 53-10-2, FIGURE 2. (M) 2 L 7 3 4F A3WE 2002090500010 20020905 00010 NM 2002 9 5 2002F00846 1 20010805 A 5312 PRESSURE PANEL BOEING 727 72721 1384003 NM NLG WW CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 357QS 19259 NOSE WHEEL WELL SKIN CRACKED LEFT SIDE AT STATION 243.7. ACCOMPLISHED NOSE WHEEL WELL RIGHT SIDE SKIN REPAIR AT BS 243. 7 IAW B727 SRM 51-40-2, FIGURE 1. (M) 2 L 7 3 4F A3WE 2002090500011 20020905 00011 NM 2002 9 5 2002F00847 1 20010805 A 5310 STRUCTURE BOEING 727 72721 1384003 NM NLG WW CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 357QS 19259 LEFT NOSE WHEEL WELL VERTICAL WEB EXFOLIATED AT INTERSECTION WITH UPPER NOSE CHORD AS VIEWED FROM DOG HOUSE AT BS 315 DU E TO CORROSION. ACCOMPLISHED NOSE WHEEL WELL LEFT VERTICAL WEB REPAIR DUE TO CORROSION IAW B727 SRM 53-10-2, FIGURE 1. (M) 2 L 7 3 4F A3WE 2002090500012 20020905 00012 NM 2002 9 5 2002F00848 1 20010813 A 5310 FITTING BOEING 727 72721 1384003 NM CARGO DOOR CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 357QS 19259 FOUND CRACK AROUND C2 DOOR FORWARD UPPER HINGE ATTACH POINT AT BS 1070 STRINGER 20R AND 19R. ACCOMPLISHED C2 DOOR FORWA RD FRAME REPAIR AT BS 1070 STRINGER 20R AND 19R IAW B727 SRM 53-10-2, FIGURE 5. (M) 2 L 7 3 4F A3WE 2002090600204 20020906 00204 CE 2002 9 6 ACE1104011 1 20011105 A 7722 1143800047 INDICATOR BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA COCKPIT ERRATIC E YADA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 AL 03 41UE UC41 PCE32490 ON TAKE OFF RUN, PILOT OBSERVED HIGH (920 DEG). ITT INDICATION ON NR1 ENGINE AND ABORTED THE TAKE OFF. MAINTENANCE RE PLACE THE NR1 ITT INDICATOR DUE ERRONEOUS INDICATION AT THE HIGH END OF THE SCALE. 2 L 7 2 4T 4 T RT A24CE E4EA 2002090600205 20020906 00205 CE 2002 9 6 ACE1105011 1 20011106 A 3260 PIN BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE NLG CONNECTOR CORRODED E YADA O OTHER O OTHER AP APPROACH 1 AL 03 41UE 34353 UC41 ON APPROACH TO LANDING, NOSE GEAR GREEN LIGHT DID NOT COME ON UNTIL GEAR WAS CYCLED. MAINTENANCE COULD NOT DUPLICATE TH E DISCREPANCY ON THE GROUND AND TROUBLE SHOT TO A CORRODED CONNECTOR PIN IN THE UP/DOWN LOCK SWITCH CIRCUIT. 2 L 7 2 4T 4 T RT A24CE E4EA 2002091000182 20020910 00182 NM 2002 9 10 2002F00856 1 20010726 A 5315 FLOORBEAM BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FUSELAGE INTERIOR AT BS 328 LBL 27 HAS CORROSION DAMAGE TO FLOORBEAM UPPER CAP FORWARD AREA. (M) 2 L 7 3 4F A3WE 2002091000183 20020910 00183 NM 2002 9 10 2002F00857 1 20010725 A 5312 BEAM BOEING 727 72721 1384003 NM BULKHEAD CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND CABIN AFT PRESSURE BULKHEAD BS 1183 VERTICAL BEAM LBL 17.8 HAS CRACKED FRONT LIGHTENING HOLE WL 268. (M) 2 L 7 3 4F A3WE 2002091000185 20020910 00185 NM 2002 9 10 2002F00858 1 20010725 A 5330 SKIN BOEING 727 72721 1384003 NM FUSELAGE DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FUSELAGE EXTERIOR SKIN APPROXIMATELY BS 510 LAP JOINT SILL LEFT HAS A DENT. (M) 2 L 7 3 4F A3WE 2002091100008 20020911 00008 NM 2002 9 11 2002F00859 1 20010724 A 5311 FRAME BOEING 727 72721 1384003 NM FUSELAGE DAMAGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FORWARD LOWER CARGO COMPARTMENT AT BS 481 CIRCUMFERENTIAL JOINT AREA HAS BARE METAL AND PEELING PAINT. (M) 2 L 7 3 4F A3WE 2002091100009 20020911 00009 NM 2002 9 11 2002F00860 1 20010724 A 5711 SPAR BOEING 727 72721 1384003 NM CENTER WING CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND WING CENTER SECTION STATION BS 870, REAR SPAR LOWER CHORD, EXTERIOR, RBL 42 HAS CORROSION. (M) 2 L 7 3 4F A3WE 2002091100010 20020911 00010 NM 2002 9 11 2002F00861 1 20010822 A 5740 ATTACH FITTING BOEING 727 72721 1384003 NM CENTER WING CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 WING CENTER SECTION INTERIOR REAR SPAR UPPER CHORD ATTACH CLIP, SMALL ANGLE, CRACKED AT BS 870 AND BBL 0. (M) 2 L 7 3 4F A3WE 2002091100011 20020911 00011 NM 2002 9 11 2002F00862 1 20010718 A 5711 SPAR BOEING 727 72721 1384003 NM CENTER WING CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 WING CENTER SECTION FRONT SPAR EXTERIOR LOWER CHORD HAS BULGING AREA AT LEFT BBL 60 INCH. (M) 2 L 7 3 4F A3WE 2002092300045 20020923 00045 NM 2002 9 23 PCS2002F00001 1 20011203 A 3610 BACC10DV250ABE CLAMP BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE NR 1 STRUT FAILED A PCSA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 17 395AJ 21100 CREW REPORTED NR 1 STRUT OVERHEAT LIGHT ILLUMINATED PASSING FL220. AIRCRAFT RETURNED WITHOUT FURTHER INCIDENT. MAINTEN ANCE REMOVED AND REPLACED CLAMP AT STARTER DUCT CONNECTION NEAR 13TH STAGE BLEED VALVE, OPERATED ENGINE AT HEIGHT POWER FOR 15 MINUTES. OPS CHECK GOOD IAW MM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F RT A3WE E2EA 2002092300046 20020923 00046 NM 2002 9 23 PCS2002F00002 1 20010905 A 5230 10614541 SEAL BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE CARGO DOOR TORN A PCSA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 17 994AJ 20942 CREW REPORTED UNABLE TO PRESSURIZE AIRPLANE IN FLIGHT. FLIGHT CREW RETURNED AND MADE AN UNEVENTFUL OVERWEIGHT LANDING. AS A RESULT OF THE FLIGHT CREW DISCREPANCY, MAINTENANCE TROUBLESHOOTING AND INSPECTION REVEALED LEAKAGE AT THE FUSELA GE C-1 DOOR CUTOUT SEAL. MAINTENANCE PROCEEDED TO REMOVE AND REPLACE THE DAMAGED SEAL AS REQUIRED PER MM AND PERFORMED A PRESSURIZATION AND AIRCRAFT PRESSURIZED ON GROUND TO 6.0 PSI. AC PRESSURIZATION SYSTEM ALL LEAK AND OPERATIONALLY CHE CKED NORMAL IAW MM. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F RT A3WE E2EA 2002092300047 20020923 00047 NM 2002 9 23 PCS2002F00003 1 20011227 A 5230 211345 SEAL BOEING 727 727227 1384078 NM PWA JT8 JT8D9 52048 NE CARGO DOOR DAMAGED A PCSA K NONE O OTHER IN INSP/MAINT 1 SO 17 196AJ 20838 CAPTAIN REPORTED,(CABIN ALT EXCEEDED 10,000 FEET AT FL290 WITH 2 PACKS ON 4 BLEED OPEN AND CARGO HEAT OUTFLOW CLOSED. 5 .8 PSI DIFFERENTIAL PRESSURE. MAINTENANCE FOUND MAIN CARGO DOOR SEAL DEPRESSOR DAMAGED IN NUMEROUS AREAS, PERFORMED REP AIR PER SRM. PERFORMED PRESSURIZATION CHECK PER MM. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2002092300048 20020923 00048 NM 2002 9 23 PCS2002F00004 1 20011228 A 2612 FIRE DETECTOR BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE CARGO BAY FALSE ACTIVATION A PCSA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 17 395AJ 21100 CAPTAIN REPORTED DURING CLIMB OUT, FIRE INDICATION IN AFT CARGO ILLUMINATED. CREW NOTED THE INDICATION OCCURRED AFTER S ELECTING ON THE WING ANTI-ICING. AIRCRAFT RETURNED BACK WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED AFT CARGO COMPAR TMENT PNEUMATIC DUCTS AND DETECTION LOOPS EXTERNALLY OF DINATROL RESIDUE. PERFORMED ENGINE RUNS AT BLAST FENCE AND CHEC KED SYSTEM IAW MM. OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F RT A3WE E2EA 2002092300049 20020923 00049 NM 2002 9 23 PCS2002F00005 1 20011229 A 2612 354501 INSULATION BOEING 727 727227 1384078 NM PWA JT8 JT8D9 52048 NE FIRE LOOP LOOSE A PCSA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SO 17 794AJ 21243 CAPTAIN REPORTED LOWER AFT BODY OVERHEAT LIGHT CAME ON AFTER DEPARTURE. AIRCRAFT RETURNED AND PERFORMED AN OVERWEIGHT L ANDING WITHOUT FURTHER INCIDENT. MAINTENANCE RESET INSULATOR AT FIRE LOOP. OPS CHECK NORMAL IAW. 2 L 7 3 4F 4 F A3WE E2EA 2002092300050 20020923 00050 NM 2002 9 23 PCS2002F00006 1 20011221 A 7500 69218901 FITTING BOEING 727 727212 138407G NM NR 3 ENGINE BROKEN A PCSA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 17 598AJ 21947 CREW REPORTED ENGINE 3 FIRE WARNING DURING INITIAL CLIMB OUT. AIRCRAFT RETURNED WITH OUT FURTHER INCIDENT. MAINTENANCE FOUND BROKEN FITTING ON 13TH STAGE DUCT END CAP. REMOVED AND REPLACED END CAP. OPS AND LEAK CHECK GOOD IAW MM. AIRCR AFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2002092300052 20020923 00052 NE 2002 9 23 PCS2002F00008 2 20011221 A 7261 393026042 RELIEF VALVE BOEING 727 727233 138408A NM PWA JT8 JT8D15A 52051 NE ENGINE OIL DEFECTIVE A PCSA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 17 994AJ 20942 687586 CREW REPORTED ENGINE NR 1 HAD 80 PSI ON CLIMB 1.85 EPR. AIRCRAFT RETURNED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVE D AND REPLACED NR OIL PRESSURE RELIEF VALVE. OPS CHECK NORMAL IAW MM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F RT A3WE E2EA 2002092300053 20020923 00053 NE 2002 9 23 PCS2002F00009 2 20011221 A 7261 393026042 RELIEF VALVE BOEING 727 727233 138408A NM PWA JT8 JT8D15A 52051 NE ENGINE OIL DEFECTIVE A PCSA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 17 994AJ 20942 687586 CREW REPORTED NR 1 ENGINE OIL PRESSURE AT IDLE READS 37 PSI. AIRCRAFT RETURNED WITHOUT FURTHER INCIDENT. MAINTENANCE R EMOVED AND REPLACE NR 1 OIL PRESSURE RELIEF VALVE MM. OPS CHECK NORMAL IAW MM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F RT A3WE E2EA 2002092400001 20020924 00001 NM 2002 9 24 2001UIA008 1 20011209 A 2701 CONTROL COLUMN DOUG MD90 MD9030 3023690 NM COCKPIT DISCONNECTED Z B EMER. DESCENT F FLT CONT AFFECTED CL CLIMB 1 TW 00 17913 53537 A MESSAGE"ELEVATOR SPLIT" DISPLAYED ON EOAP,DURING USE A/P CLIMB THOUGHT 16000FT.A/C AIR TURN BACK,PERFORMED TROUBLESHOO TING MAINTENANCE FOUND THE LEFT AND RIGHT CONTROL COLUMNS WERE DISCONNECTED.AFTER RECONNECTING THE DIVIDED TUBE AND INSP ECTION OF THE CONTROL COLUMN AND ELEVATOR POSITION SENSORS, ALL OPERTION FUNCTION RETURNED TO NORMAL. 2 L 7 2 4F RT A6WE 2002100800004 20021008 00004 NM 2002 10 8 IU62002F00032 1 20011211 A 2761 654494715 HOUSING BOEING 737 737* NM SPOILER ACTUATOR DAMAGED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 HOUSINGS ARE SUSCEPTIBLE TO HOLES, DUE TO OVER-PRESSURIZATION OF ACTUATOR ASSEMBLY. 2 L 7 2 4F RT A16WE 2002100800068 20021008 00068 WP 2002 10 8 UPS02839252 1 20010731 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE:C2 LEFT WING UPPER SKIN IS CRACKED AT XRS 74 AT STRINGERS 9,10,12. REMOVED EXISTING DOUBLER, CUTOUT DAM AGE AT XRS 74 STRINGERS 9,10,12, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW UPS E NGINEERING FILE NUMBER DC8-57-20054, AND SAA SK 806-503. 2 L 7 4 4F RT 4A25 2002101000088 20021010 00088 NE 2002 10 10 R7MR706335135 2 20010515 A 7313 411101009 FUEL NOZZLE BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ENGINE CRACKED B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 163BK 594 7063 LE45144EA FUEL NOZZEL CRACKED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2002101000097 20021010 00097 NE 2002 10 10 R7MR706335136 2 20010509 A 7240 413102002 CURL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE COMBUST CHAMBER CRACKED B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 163BK 594 7063 CURL CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2002101000099 20021010 00099 NE 2002 10 10 R7MR706335151 2 20010515 A 7230 410100641 ROTOR BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE COMPRESSOR ERODED B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 163BK 509 7063 LE45144EA ROTOR HAS EROSION. PENDING FURTHER INSPECTION . REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2002101600079 20021016 00079 EA 2002 10 16 CA021002003 1 20010929 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA (CAN) THE LT FRONT COCKPIT WINDSHIELD OUTER PANE CRACKED ON CLIMB. THE A/C RETURNED FOR REPLACEMENT OF THE WINDSHIELD. R EMOVE AND REPLACED WINDSHIELD 2 L 7 2 4F 4 F RT A21EA E15NE 2002101800034 20021018 00034 NM 2002 10 18 SWAA012533 1 20010909 A 5310 6547956 WEB BOEING 737 7372H4 138448C NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED D-CHECK, FOUND WEB CORRODED AT BS 810-823, RBL 66 & WL 199.v Removed and replaced WEB PER SRM. 2 L 7 2 4F A16WE 2002101800035 20021018 00035 NM 2002 10 18 SWAA012535 1 20010911 A 5310 6546546 FITTING BOEING 737 7372H4 138448C NM LH W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED D-CHECK, FOUND Lt W/W SUPPORT FITTING CRACKED AT BS 716, LBL 68 & WL 192. REPAIRED FITTING PER SRM. 2 L 7 2 4F A16WE 2002101800036 20021018 00036 NE 2002 10 18 SWAA010648 2 20010302 A 7200 CFM563 ENGINE BOEING 737 7373H4 1384600 NM GE CFM56 CFM56* 13802 NE #2 POS. BIRD STRIKE A SWAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 29 620SW 28036 858292 AIR TURNBACK, DECLARED EMERGENCY. sMOKE REPORTED IN CABIN. RETURNED TO PHX & EVACUATED A/C THROUGH FWD ENTRY DOOR EVAC SLIDE. EVIDENCE OF BIRD STRIKE TO nr 2 ENG AT 3 O'CLOCK POSITION. BIRD REMAINS IN BOOSTER STAGES. FRESH OIL FOUND IN 5TH STAGE CHECK VALVE. BORESCOPE REVEALED FRESH OIL STAINING. Removed and replaced EVAC SLIDE PER MM. Removed and re placed nr 2 ENGINE PER SWA SAM 385. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101800038 20021018 00038 NM 2002 10 18 SWAA011222 1 20010421 A 5330 65C33756 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 EXTERNAL FUSELAGE SKIN DAMAGED BY GROUND EQUIPMENT, BS 346 TO 382, WL 158 TO 172 RT. MX FERRY TO DAL AND REPAIRED SKIN PER SWA RA. 2 L 7 2 4F RT A16WE 2002101800041 20021018 00041 NE 2002 10 18 SWAA011192 2 20010419 A 7230 9527M99P08 BLADE BOEING 737 7375H4 138449D NM GE CFM56 CFM56* 13802 NE #2 ENG FOD A SWAA D RETURN TO BLOCK E C VIBRATION/BUFFET F.O.D. TO TAKEOFF 1 SW 29 510SW 24187 721742 AIR TURNBACK. FOLLOWING PROBABLE BIRD STRIKE, nr 2 ENGINE HAD UNUSAL SOUND & EXCESSIVE VIBRATION. ACCOMPLISHED BIRD ST RIKE INSPECTION & FOUND 4 FAN BLADES BENT. Removed and replaced ALL nr 2 ENG FAN BLADES PER MM & SWA SAM 455. 2 L 7 2 4F 4 F RT A16WE E2GL 2002102100172 20021021 00172 SO 2002 10 21 SIMA20011052A 1 20010415 A 5330 SKIN EMB 135 EMB135LR 3260305 SO FUSELAGE BIRD STRIKE A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 706AE 145194 BOS - FLT 4644 - DURING CLIMB, CREW REPORTED A BIRD STRIKE ON THE RIGHT FUSELAGE. CREW RETURNED AIRCRAFT TO BOS. REPAI RED DAMAGE TO FORWARD RIGHT FUSELAGE IAW SRM 51-20-02. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2002102200075 20021022 00075 EU 2002 10 22 NSVA0123 1 20011120 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A NSVA O OTHER O OTHER AP APPROACH 1 EA 27 294CJ 340B294 HTS - ON APPROACH AIRCRAFT ENCOUNTERED BIRD STRIKE BELOW RIGHT FRONT WIND SCREEN. AIRCRAFT LANDING WAS UNEVENTFUL. MAI NTENANCE INSPECTED AIRCRAFT, FOUND SKIN INDENTATION. AIRCRAFT RELEASED PER SFP, FOR REPAIRS. (M) 2 L 7 2 4T RT A52EU 2002102200077 20021022 00077 NM 2002 10 22 SWAA012534 1 20010911 A 5312 BAC1505 TEE CHORD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED 1/2D CHECK, FOUND T-CHORD CRACKED AT BS 178, LBL 6 & WL 184. REMOVED AND REPLACED T-CHORD PER SWA ACO 7154-53. 2 L 7 2 4F RT A16WE 2002102200078 20021022 00078 NE 2002 10 22 SWAA013156 2 20011119 A 7230 1663M24P04CT ENGINE BOEING 737 7373H4 1384600 NM GE CFM56 CFM56* 13802 NE NR 1 BIRD STRIKE A SWAA C ABORTED TAKEOFF C J F.O.D. WARNING INDICATION TO TAKEOFF 1 SW 07 387SW 26602 723188 ABORTED TAKEOFF, AT APPROX 100 KNOTS A LARGE BIRD WAS INGESTED INTO NR 1 ENGINE. COMPLIED WITH BIRD STRIKE INSP AND FOU ND DAMAGED FAN BLADES. REMOVED AND REPLACED FAN BLADES PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002102400194 20021024 00194 WP 2002 10 24 UPS02839440 1 20010821 A 5320 3779658U502 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 STA 908 LONG 10R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779658, AND SRM 51-1- 20D, 51-1-21, 51-3-0. 2 L 7 4 4F RT 4A25 2002102800037 20021028 00037 NM 2002 10 28 SCNA01714 1 20010929 A 3350 BATTERY BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 284SC 21438 RIGHT HAND EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. CORRECTED BY REPLACING OVERWING LIGHT BATTERY. 2 L 7 3 4F RT A3WE 2002102800039 20021028 00039 NM 2002 10 28 SCNA01720 1 20010930 A 2133 REGULATOR BOEING 727 7272J4 1384006 NM CABIN PRESSURE FAILED A SCNA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 290SC 20764 CLIMB OUT OF LAS AT APPROX 30,000FT NR 3 ENG STRUT OVERHEAT LIGHT ILLUMINATED FOLLOWED COM PROCEDURE AND TURNED OFF RT P ACK AND NR 3 ENG BLEED VALVE. NR 3 ENG OVERHEAT LIGHT EXTINGUISHED CONTINUED TO MSP WITH RIGHT PACK OFF. CORRECTED BY LE AK CHECKING STRUT AREA AT TO POWER AND NO LEAK WAS NOTED OR STRUT OVERHEAT WAS NOTED. DUCT PRESSURE INDICATOR WAS ALSO R EPORTED AS BEING NOTICEABLY LOWER ON RIGHT THAT ON LEFT (20PSI LOWER ON RIGHT). CORRECTED BY REMOVING AND REPLACING THE PRESSURE REGULATOR. 2 L 7 3 4F RT A3WE 2002110600084 20021106 00084 CE 2002 11 6 ACE1025011R1 1 20011026 A 3233 11288002223 ACTUATOR BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE NLG FAILED A YADA O OTHER J WARNING INDICATION AP APPROACH 1 AL 03 1566C 20289 UC36 ON APPROACH, NOSE GEAR GREEN DOWN AND LOCKED LIGHT FAILED TO ILLUMINATE AFTER TWO NORMAL CYCLES AND ONE MANUAL EXTENSION . THE AIRCRAFT MADE AN UNEVENTFUL LANDING. MAINTENANCE COULD NOT CONFIRM FAILURE DUE ILLUMINATION OF THE NOSE GEAR GR EEN LIGHT AFTER THE AIRCRAFT PARKED AND THE FAILURE COULD NOT BE DUPLICATED. THE NOSE GEAR ACTUATOR WAS REPLACED AND TH E AIRCRAFT WAS OPERATIONALLY TEST FLOWN. 2 L 7 2 4T 4 T RT A24CE E4EA 2002110600085 20021106 00085 CE 2002 11 6 ACE1029011 1 20011029 A 2910 1013880101 FITTING BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE HYD SYSTEM LEAKING A YADA O OTHER J WARNING INDICATION CL CLIMB 1 AL 03 1566C 20325 UC36 ON DEPARTURE, THE GEAR WARNING LIGHTS (HANDLE) CAME ON. THE GEAR WOULD NOT CYCLE WITH THE ELECTRIC PUMP. THE GEAR WAS EXTENDED WITH THE HAND PUMP. THE CREW CONTINUED THE FLIGHT AS REQUIRED TO BURN FUEL DOWN TO LANDING WEIGHT AND THE AIRC RAFT MADE AN UNEVENTFUL RETURN LANDING. MAINTENANCE FOUND THE HYDRAULIC SYSTEM LOW ON FLUID AND A LARGE QUANTITY OF HY DRAULIC FLUID AROUND AND LEAKING FROM THE RETRACT LINE SWIVEL ON THE NOSE GEAR ACTUATOR. THE FITTING WAS RESEALED USING A CONICAL SEAL INSERT. MAINTENANCE ALSO FOUND THE HYDRAULIC POWER PACK MOTOR CIRCUIT BREAKER POPPED (POSSIBLY DUE TO E XTENDED MOTOR OPERATION DUE TO LOW FLUID LEVEL) 2 L 7 2 4T 4 T RT A24CE E4EA 2002110600087 20021106 00087 CE 2002 11 6 ACE1205011 1 20011202 A 3297 G7C22 WIRE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE MLG SHORTED A YADA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 1553C 32582 UC24 AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT CONTINUED AND MADE AN UNEVENTFUL LANDING. MAINTENANCE LOCA TED AND REPLACED WIRE C7C22, DUE TO HIGH RESISTANCE, BETWEEN LEFT FUSELAGE AND CONNECTOR J107. 2 L 7 2 4T 4 T RT A24CE E4EA 2002110800133 20021108 00133 SW 2002 11 8 2002F00983 1 20011125 A 2910 27810321055 HYDRAULIC LINE FRCHLD SA227 SA227DC 3377521 SW HYD SYSTEM LEAKING A BSAA A UNSCHED LANDING K J F FLUID LOSS WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 05 850LS DC850B BIL - FLT 2585 - DURING CLIMBOUT, BOTH HYDRAULIC PRESSURE LIGHTS AND THE HYDRAULIC PRESSURE GAUGE BEGAN TO FLUCTUATE AT ABOUT 13,000 FEET. THEN THE HYD PRESS LIGHTS CAME ON STEADY AND HYDRAULIC PRESSURE INDICATION DROPPED TO 200. THE CREW VERIFIED THE BEST OPTION WITH THE CURRENT WEATHER WAS TO RETURN TO STATION. FLAPS WOULD ONLY EXTEND TO BETWEEN QUARTER AND HALF FLAPS. CREW THEN MANUALLY EXTENDED THE GEAR. AIRCRAFT LANDED WITH NO FURTHER INCIDENT. THE HYDRAULIC PRESSU RE LOSS WAS DUE TO HYDRAULIC SYSTEM LEAK IN THE RIGHT FLAP WELL. REPLACED LINE, SYSTEM OPS CHECK AND LEAK CHECKED GOOD. (M) 2 L 7 2 4T RT A18SW 2002111500034 20021115 00034 NE 2002 11 15 JYD2002F00005 2 20011106 A 7230 712701 COMPRESSOR WHEEL SKRSKY S64 S64* 8142502 NE PWA JFTD12 JFTD12A4A 52047 NE CENTER RING CRACKED B JYDR K NONE O OTHER IN INSP/MAINT 1 NM 09 164AC 64034D FRONT HUB, FOUND CRACKED DURING OVERHAUL INSPECTION. COMPRESSOR WAS REMOVED FROM SERVICE DUE TO REACHING ITS OVERHAUL I NTERVAL, HAVING A TSO OF 2987.9 HOURS AND TT OF 5978.0 HOURS. DURING OVERHAUL INSPECTION, TWO CRACKS WERE DETECTED BY C URRENT INSPECTION. CRACK LOCATIONS DETECTED BY EDDY CURRENT WERE IN THE CENTER RING OF FRONT HUB EXTENDING FROM BLADE P IN HOLES AT APPROXIMATELY AT 45 DEGREE ANGLE. CRACKS WERE NOT DETECTABLE BY FLUORESCENT PENETRANT INSPECTION, THUS CRAC K LENGTHS WERE NOT MEASUREABLE. 2 G 7 2 4U 4 U E15EA 2002111500035 20021115 00035 NE 2002 11 15 JYD2002F00006 2 20011116 A 7230 670802 COMPRESSOR WHEEL SKRSKY S64 S64E 8142604 NE PWA JFTD12 JFTD12A4A 52047 NE CENTER RING CRACKED A JYDR K NONE O OTHER IN INSP/MAINT 1 NM 09 164AC 5978 64034D SECOND STAGE COMPRESSOR DISK WAS FOUND CRACKED DURING OVERHAUL INSPECTION. COMPRESSOR WAS REMOVED FROM SERVICE DUE TO R EACHING ITS OVERHAUL INTERVAL, HAVING A TSO OF 2987.9 HOURS AND TT OF 5978.0 HOURS. DURING OVERHAUL INSPECTION, FIVE CR ACKS WERE DETECTED BY EDDY CURRENT INSPECTION. CRACK LOCATIONS DETECTED BY EDDY CURRENT WERE IN THE CENTER RING OF DISK EXTENDING FROM BLADE PIN HOLES AT APPROXIMATELY AT 45 DEGREE ANGLE. CRACKS WERE NOT DETECTABLE BY FLUORESCENT PENETRAN T INSPECTION, THUS CRACK LENGTHS WERE NOT MEASUREABLE. 2 G 7 2 4U 4 U H4EA E15EA 2002111500077 20021115 00077 NM 2002 11 15 UPS02239905 1 20011016 A 5310 65C232313 FITTING BOEING 727 72725C 138400H NM BS 870 L/H CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C&SI WHILE CARRYING OUT NDT INSP. OF L/H 870 FTG, RECENT CRACK FOUND FROM HOLE COMMON TO STR. END AT 1S T ROW, ALSO 2 OTHER HOLES HAVE CORROSI ON INDICATIONS L/H 870 REPLACED IAW EO B727-5310-3056-F & DRAWING 65C13724 2 L 7 3 4F A3WE 2002111900099 20021119 00099 EU 2002 11 19 R7M2002F00038 1 20011220 A 2842 9550171990 PRESSURE SWITCH SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE LOW FUEL INOPERATIVE B R7MR K NONE L NO TEST IN INSP/MAINT 1 NM 07 103LN 354 3128 LOW FUEL PRESSURE SWITCH, UNIT INOPERATIVE. FULE LIGHT GOES OUT WITH BOOST PUMP ON. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E00054EN 2002112000005 20021120 00005 EU 2002 11 20 R7MR35486 1 20011220 A 7332 9550171990 PRESSURE SWITCH SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE FUEL SYSTEM INOPERATIVE B R7MR O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 103LN 354 3128 LOW FUEL PRESSURE SWITCH, UNIT INOPERATIVE. FULE LIGHT GOES OUT WITH BOOST PUMP ON. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E00054EN 2002112000087 20021120 00087 NM 2002 11 20 USAABA01135 1 20011124 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211* 54555 NE ROW13 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 625VJ 27246 FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 13 AND 26 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. 2 L 7 2 4F 4 F RT A2NM A12EU 2002112000088 20021120 00088 EU 2002 11 20 USAATA01065 1 20011129 A 3350 321430 BATTERY AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 707UW 0949 THE CENTER OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND FLASHING WITH THE SYSTEM OFF. MAINTENANCE REPLACED A BATTERY PACK. OPERATIONALLY CHECKS, OK. 2 L 7 2 4F 4 F RT A28NM E2GL 2002112200145 20021122 00145 NM 2002 11 22 AALA20011955 1 20011023 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 685AA 25342 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 1E INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 1E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002112200146 20021122 00146 NM 2002 11 22 AALA20011962 1 20011024 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 615AM 24491 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STRIP ASSEMBLY. SY STEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002112200147 20021122 00147 NM 2002 11 22 AALA20011974 1 20011105 A 3350 11021621 SOCKET BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 664AA 25298 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET. SYSTEM GRO UND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002112200148 20021122 00148 NM 2002 11 22 AALA20011975 1 20011104 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN CRACKED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 622AA 24580 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT CRACKED. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUN D CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002112200149 20021122 00149 NM 2002 11 22 AALA20012018 1 20011107 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 689AA 25731 MIA - DURING OVERNIGHT MAINTENANCE, RIGHT SIDE AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED RIGHT SIDE A FT SERVICE DOOR EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002112500066 20021125 00066 NM 2002 11 25 AALA20012031 1 20011112 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 186AN 32380 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 33D HAS BROKEN WIRE. REPLACED EMERGENCY EXIT LIGHT CON NECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002112500067 20021125 00067 NM 2002 11 25 AALA20012033 1 20011110 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 640A 24598 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 22 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT ROW 22. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002112500068 20021125 00068 NM 2002 11 25 AALA20012036 1 20011109 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 677AN 29427 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 12 AND 13 LOOSE. SECURED EMERGENCY EXIT LIGHT WIRE. SY STEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002112500069 20021125 00069 NM 2002 11 25 AALA20012039 1 20011112 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 692AA 26972 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 16 INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT CONNECTOR . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002112500070 20021125 00070 NM 2002 11 25 AALA20012053 1 20011113 A 3350 SWITCH BOEING 757 757223 1384957 NM CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 181AN 29591 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT SWITCH. SYSTEM GROU ND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002112500071 20021125 00071 NM 2002 11 25 AALA20012078 1 20011129 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN NOT SEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 640A 24598 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 22D INOPERATIVE. SEATED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002112500072 20021125 00072 NM 2002 11 25 AALA20012149 1 20011106 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 601AN 27052 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 18 INOPERATIVE. REPLACED EMERGENCY EXIT PATH LIGHT ASSE MBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002112500073 20021125 00073 NM 2002 11 25 AALA20012151 1 20011208 A 3350 CONTACTOR BOEING 757 757223 1384957 NM EMERGENCY EXIT DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 615AM 24491 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT LEFT WING SLIDE INOPERATIVE. CLEANED EMERGENCY EXIT CONTACT S. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002112500074 20021125 00074 NM 2002 11 25 AALA20012162 1 20011214 A 3350 CONNECTOR BOEING 757 757223 1384957 NM L3 DOOR DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 191AN 32385 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L3 DOOR INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT CONNECTOR AT L3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002112500075 20021125 00075 NM 2002 11 25 AALA20012182 1 20011227 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 692AA 26972 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 19D INOPERATIVE. CONNECTED EMERGENCY EXIT LIGHT CONNEC TOR AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002112500076 20021125 00076 NM 2002 11 25 AALA20012183 1 20011227 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 646AA 24604 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 34 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT ROW 34. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002120900012 20021209 00012 SW 2002 12 9 CA021114005 1 20011002 A 2720 CONTROL CABLE BBAVIA 8 8GCBC 1220803 SW LYC O360 O360C2E 41514 EA RUDDER CONTROL FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) LT AND RT RUDDER CABLES FRAYED AT CABIN. PULLEY CABLES MADE FROM STAINLESS STEEL. 1 H 7 1 3O 3 O A21CE E286 2002120900014 20021209 00014 SW 2002 12 9 CA021114007 1 20011010 A 2720 12364 CONTROL CABLE BBAVIA 8 8GCBC 1220803 SW LYC O360 O360C2E 41514 EA RUDDER CONTROL FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) LT AND RT RUDDER CABLES FRAYED AT CABIN PULLEY. BOTH CABLES MADE OF STAINLESS STEEL. 1 H 7 1 3O 3 O A21CE E286 2002120900015 20021209 00015 SW 2002 12 9 CA021114009 1 20011108 A 2720 12364 CONTROL CABLE BBAVIA 8 8GCBC 1220803 SW LYC O360 O360C2E 41514 EA RUDDER FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) LT AND RT RUDDER CABLES FRAYED AT CABIN PULLEYS. BOTH CABLES MADE OF STAINLESS STEEL 1 H 7 1 3O 3 O A21CE E286 2003010300019 20030103 00019 SW 2003 1 3 CZMA082765 1 20011004 A 6230 BEARING BELL 412 412 1182202 SW MAST DEFECTIVE E CZMA K NONE O OTHER IN INSP/MAINT 1 SO 03 412BE 1054 A182 33036 MAST BEARING FAILED AT 1054.25 TOTAL TIME. 1 G 7 2 4U H4SW 2003010600055 20030106 00055 SO 2003 1 6 2003F00016 1 20011130 A 2910 HYDRAULIC LINE EMB 120 EMB120ER 3260203 SO HYD SYSTEM DAMAGED A HSYA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 05 210AS 120006 SJU - FLT 7109 - LOW GREEN SYSTEM HYDRAULIC RESERVOIR QUANTITY LIGHT CAME ON IN FLIGHT. REPAIRED HYDRAULIC LINE USING A PERMASWEDGE REPAIR SPLICE, LEAK CHECKED, AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2003010600056 20030106 00056 CE 2003 1 6 2003F00017 1 20011204 A 3240 BRAKE ASSY CESSNA 208 208 2073702 CE LT MLG CONTAMINATED A HSYA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 05 827FE 20800072 MOS - FLT 8706 - LEFT BRAKE SPONGY. AIR ENTRAPMENT IN THE LEFT BRAKE SYSTEM. REQUIRES BLEEDING SERVICE, INSPECTION, AN D OPS CHECK. BLEED LEFT BRAKE SEVERAL TIMES. BRAKE PEDAL PRESSURE IS GOOD. NO LEAKAGE EVIDENT AT THIS TIME. (M) 1 H 7 1 3T NT A37CE 2003010600058 20030106 00058 CE 2003 1 6 2003F00019 1 20011127 A 5420 1189100426 BRACKET BEECH 1900 1900 1154160 CE LT NACELLE CRACKED A HSYA K NONE O OTHER IN INSP/MAINT 1 NM 05 715GL UB15 GJT - LEFT ENGINE NACELLE LOWER AFT BULKHEAD HAS SEVERAL CRACKS. STRUCTURAL REPAIRS ARE IN PROGRESS. (M) 2 L 7 2 4T RT A24CE 2003010600059 20030106 00059 CE 2003 1 6 2003F00020 1 20011127 A 5420 1189100426 ANGLE BEECH 1900 1900 1154160 CE LT NACELLE CRACKED A HSYA K NONE O OTHER IN INSP/MAINT 1 NM 05 715GL UB15 GJT - LEFT ENGINE NACELLE LOWER AFT BULKHEAD HAS SEVERAL CRACKS. REPLACED THE LEFT ENGINE COWLING REINFORCEMENT ANGLE, THE ENGINE TRUSS BRACKET RECEPTACLE, AND THE UPPER AFT ANGLES. THE REPAIRS WERE COMPLETED 12-03-01 TAT 21, 140.9. (M) 2 L 7 2 4T RT A24CE 2003010600060 20030106 00060 SO 2003 1 6 2003F00021 1 20011113 A 2910 HYDRAULIC LINE EMB 120 EMB120ER 3260203 SO HYD SYSTEM CHAFED A HSYA O OTHER K FLUID LOSS CR CRUISE 1 NM 05 223AS 120021 SJU - FLT 7100 - BLUE SYSTEM HYDRAULIC FLUID LOSS. BLUE SYSTEM HYDRAULIC LINE CHAFED THROUGH. REPAIRED LINE WITH PERMA SWEDGE IAW EMB-120 MM 20-10-0 AND A SUCCESSFUL LEAK CHECK WAS PERFORMED. (M) 2 L 7 2 4T RT A31SO 2003010600061 20030106 00061 SO 2003 1 6 2003F00022 1 20011106 A 3260 PROXIMITY SWITCH EMB 120 EMB120ER 3260203 SO MLG FAULTY A HSYA L A ABORTED APPROACH UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 NM 05 210AS 120006 SJU - FLT 7109 - AFTER TAKEOFF, IN CRUISE CREW HAD A FAULTY GEAR INDICATION ON APPROACH TO STU TWO ATTEMPTS TO EXTEND TH E LANDING GEAR NORMALLY FAILED. EXITED THE TRAFFIC PATTERN CALLED FOR A MISSED APPROACH, EXTENDED THE GEAR ALTERNATELY AND LANDED SAFELY. REMOVED AND REPLACED PROXIMITY SWITCH, AND OPERATIONAL TEST LANDING GEAR RETRACTION, AND EXTENSION S YSTEM SUCCESSFULLY. (M) 2 L 7 2 4T RT A31SO 2003010800017 20030108 00017 SO 2003 1 8 2003F00014 1 20011207 A 2436 GCU EMB 120 EMB120ER 3260203 SO NR 1 & 2 OUT OF ADJUST A HSYA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 05 125AM 120017 FLT 7788 - JAC - BOTH MAIN GENERATORS AND NR 2 AUXILIARY GENERATOR DROPPED OFF LINE. GCU'S ADJUSTMENT. ADJUSTED NR 1 S TARTER/GENERATOR FROM 31.8V TO 28.5V, NR 2 STARTER/GENERATOR ROM 28.9V TO 28.5V AND NR 2 AUX GENERATOR FROM 31.9V TO 28. 5V. OPS CHECK OF SYSTEM OK. (M) 2 L 7 2 4T RT A31SO 2003010800041 20030108 00041 SO 2003 1 8 2003F00015 1 20011129 A 2731 TRIM SWITCH EMB 120 EMB120ER 3260203 SO COCKPIT STUCK A HSYA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 05 223AS 120021 SJU - FLT 7106 - DURING LANDING APPROACH ELEVATOR TRIM RAN UNCOMMANDED. COPILOTS TRIM SWITCH STUCK. THE SWITCH WAS CLE ANED, AND THE SYSTEM OPERATIONALLY CHECKED. (M) 2 L 7 2 4T RT A31SO 2003010800042 20030108 00042 SO 2003 1 8 2003F00023 1 20011108 A 3230 LANDING GEAR EMB 120 EMB120ER 3260203 SO NLG & MLG MALFUNCTIONED A HSYA L ABORTED APPROACH J WARNING INDICATION CL CLIMB 1 NM 05 210AS 120006 SJU - FLT 7109 - AFTER TAKEOFF AND IN CRUISE, CREW HAD A FAULTY GEAR INDICATION, AN APPROACH TO SJU TWO ATTEMPTS TO EXTE ND GEAR NORMALLY FAILED. EXITED THE PATTERN AND CALLED FOR A MISSED APPROACH. THEN EXTENDED THE GEAR ALTERNATELY AND L ANDED SAFELY. (M) 2 L 7 2 4T RT A31SO 2003011400208 20030114 00208 EA 2003 1 14 CA021208001 1 20011227 A 2820 79888311 CONTROL PANEL CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE FUEL/DEFUEL SHORTED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) BURNING ODOR FROM COCKPIT REFUEL/DEFUEL PANEL. REFUEL/DEFUEL CONTROL PANEL REPLACED. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2003013000066 20030130 00066 EA 2003 1 30 QXEA0202010 1 20011016 A 2820 D98C07606 SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 601QX 407 10009 PDX - CREW RECEIVED A RIGHT FUEL LOW PRESSURE CAUTION MESSAGE ON TAXI-IN. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLAC ED THE ENGINE FUEL FEED SWITCH. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003031300112 20030313 00112 SW 2003 3 13 ECA2003F00000 1 20010118 A 5511 410005001 RIB MOONEY M20 M20K 5870220 SW CONT O360 TSIO360* 17025 SO LT ELEVATOR CRACKED E ECAA O OTHER O OTHER NR NOT REPORTED 1 EA 11 34MP 673 252028 RIB HAD SMALL CRACK JUST ABOVE FORWARD SCREW HOLE THAT HOLDS BALANCE WEIGHT CAUSE MAYBE OVER TORQUE OF HARDWARE. 1 L 7 1 3O 3 O 2A3 E9CE 2003031400009 20030314 00009 EU 2003 3 14 T212003F00000 1 20010622 A 5530 10530401415 STRUCTURE BOLKMS 105 BO105LSA3 5626020 EU ALLSN 250C 250C* GL VERTICAL FIN CRACKED E T21A K NONE O OTHER IN INSP/MAINT 1 SO 21 727WW 1453 2037 AT DAILY INSPECTION CHECK, CRACKS WERE FOUND, THROUGH INSPECTION PLATE, AT TOP OF VERTICAL FIN. CRACK ABOUT 1.5 INCH LO NG ON NOSE RIB (PN105-3040120/ 1053041415), WHERE THE TAIL ROTOR GEAR BOX ATTACHED, ALSO RIVET MISSING. PROBABLE CAUSE, VIBRATION. 1 G 7 2 3U 3 U H3AU E4CE 2004022300140 20040223 00140 NM 2004 2 23 2001UALA01511 1 20010729 A 7930 BYPASS SWITCH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT ENGINE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 7462U 21916 AIRCRAFT DIVERTED DUE TO A NR 1 OIL FILTER BYPASS LIGHT. REPLACED THE OIL FILTER BYPASS SWITCH. 2 L 7 3 4F 4 F A3WE E2EA 2003080600023 20030806 00023 WP 2003 8 6 LS1R088301 1 20011130 A 2842 369D2963035 SENSOR HUGHES 369 369D 4470706 WP FUEL QTY DAMAGED E LS1R O OTHER O OTHER NR NOT REPORTED 1 EA 13 1097J 900801D FUEL QTY SENSOR HAS BARE WIRES ON UNIT. 1 G 7 1 3U H3WE 2003080600017 20030806 00017 WP 2003 8 6 LS1R088292 1 20011221 A 2410 A700ZG RCCB HUGHES 369 369D 4470706 WP ELECTRICAL FAILED E LS1R O OTHER O OTHER NR NOT REPORTED 1 EA 13 500DC 227 290456D REVERSE CURRENT FAILED TO CLOSE. 1 G 7 1 3U H3WE 2003091100101 20030911 00101 WP 2003 9 11 UPS03841017 1 20010731 A 5230 DOOR DOUG DC8 DC873F 302199F WP PWA JT3D JT3D3 52039 NE NR 3 PIT DOOR LEAKING A IPXA O OTHER O OTHER CL CLIMB 1 SO 01 868UP 45968 IN CLIMB OUT, KEPT INCREASING FLOW TO MAINTAIN DESIRED CAB PRESS FOR F L330. APPROX 5 MIN AFTER REACHING FL330 WE LOSSE D CONTROL OF BOTH AUTO AND MANUAL CAB CONTROL. CABIN REACHED FL230 RAN CHECKLIST AND DESEN DED TO FL230. FOUND AIR LEA K AT THE NR 3 PIT DOOR. CHECKED DOOR SEAL & EXTERNAL LATCHING MECH. FOUND LOWER DOOR HOOK RIDE UP ON TEE BOLT IF DOOR NO T SHUT RIGHT (REF LP023577) DEFERRED M263884. REF LP 23583 - RERIGGED DO OR PER MM 52-31-00 OPS CHECK GOOD, THIS CLEARS M263884. 2 L 7 4 4F 4 F RT 4A25 1E8 2003091200169 20030912 00169 2003 9 12 AALA20012082 4 20011128 A 2210 DAMPER AIRBUS 300 A300B4605R 3930308 EU VERTICAL STAB DEFECTIVE A AALA A UNSCHED LANDING F E FLT CONT AFFECTED VIBRATION/BUFFET CL CLIMB 1 SW 21 7055A 462 LIM - FLT 918 - EN ROUTE LIM-MIA, DURING CLIMB-OUT DETECTED RUDDER VIBRATION. VIBRATION INCREASED AFTER TURNING OFF AUT OPILOT. RETURNED LIM AND LANDED WITHOUT FURTHER INCIDENT. ACCOMPLISHED RUDDER ATTACHMENT INSPECTION AND VERTICAL STABI LIZER ATTACHMENT INSPECTION. ALL FOUND NORMAL. REPLACD YAW DAMPER ACTUATOR AND BOTH FLIGHT AUGMENTATION COMPUTERS. AC COMPLISHED OPERATIONAL CHECK OF YAW DAMPER SYSTEM AND AUTO PILOT SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2003090900196 20030909 00196 SW 2003 9 9 HEEA088944 1 20010131 A 5610 407030115125 WINDSHIELD BELL 407 407 1182206 SW COCKPIT CRACKED E O OTHER O OTHER NR NOT REPORTED 1 SW 03 405PH 53207 WINDSHIELD CRACKED. 1 G 7 1 3U O H2SW 2003091700001 20030917 00001 NE 2003 9 17 JYD2003F00002 2 20011116 A 7230 712701 HUB SKRSKY S64 S64E 8142604 NE PWA JFTD12 JFTD12A4A 52047 NE COMPRESSOR WHEEL CRACKED B JYDR O OTHER O OTHER NR NOT REPORTED 1 NM 09 164AC 5978 2987 672571 64034D FRONT HUB (PN 712701, SN 3V4176) FOUND CRACKED DURING OVERHAUL INSP. COMPRESSOR (SN 672571) WAS REMOVED FROM SERVICE DU E TO REACHING ITS OVERHAUL INTERVAL, HAVING A (TSO 2987.9 HOURS), (TT OF 5978.0 HOURS). DURING OVERHAUL INSPECTION, TWO CRACKS WERE DETECTED BY EDDY CURRENT INSPECTION. CRACK LOCATIONS DETECTED BY EDDY CURRENT WERE IN THE CENTER RING OF F RONT HUB EXTENDING FROM BLADE PIN HOLES AT APPROXIMATELY A 45 DEGREE ANGLE. CRACKS NOT DETECTABLE BY FLUORESCENT PENETR ANT INSP, THUS CRACK LENGTHS WERE NOT MEASUREABLE. 2 G 7 2 4U 4 U H4EA E15EA 2003091700012 20030917 00012 2003 9 17 KBMA111989 4 20011130 A 3420 LIGHT BELL 206 206B 1181511 SW ATTITUDE GYRO INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 188TV 9991 3379 2704 LIGHTING ON UNIT IS INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U H2SW 2003091700013 20030917 00013 EU 2003 9 17 KBMA111990 1 20011203 A 2121 0500847 MOTOR SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE BLOWER FAULTY E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 345SH 524 3345 MOTOR REPORTED TO BE FAULTY/ INOPERTAIVE. REPLACE WITH NEW MOTOR. 1 G 7 1 3U 3 U H9EU E19EU 2003091700014 20030917 00014 SW 2003 9 17 KBMA111992 1 20011211 A 6710 206010470101 BEARING BELL 206 206B 1181511 SW BELLCRANK ASSY WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 73DP 2513 BEARING FOUND TO BE WORN BEYOND LIMITS. REPLACED WITH NEW BEARING. 1 G 7 1 3U H2SW 2003091700015 20030917 00015 EU 2003 9 17 KBMA111994 1 20011215 A 3110 INDICATOR SNIAS 350 AS350B 8680801 EU COCKPIT OUT OF ADJUST E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 1188P 1359 2347 UNIT WILL NOT ADJUST FOR CALIBRATION. REPLACED WITH SERVICEABLE CAUGE. 1 G 7 1 3U H9EU 2003091600042 20030916 00042 EU 2003 9 16 RYN2003F00006 1 20011215 A 3150 350E5151331 CONCENTRATOR AIRBUS 320 A320214 3930316 EU NR 1 MALFUNCTIONED A RYNA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 GBXKD 735 FLIGHT WARNING SYSTEM, SYSTEM DATA ACQUISITION CONCENTRATOR (SDAC) NR 1 FAULTING NOSE WHEEL STEERING IN FLIGHT. AIRCRAF T LANDED WITHOUT INCIDENT AND WAS TOWED TO THE GATE. REMOVED AND REPLACED NR 1 SDAC. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A28NM 2004020300098 20040203 00098 EU 2004 2 3 IXXA0100011O 2 20010330 A 7261 ENGINE DOUG DC8 DC871F 302199D WP CFMINT CFM56 CFM562AFR 13802 EU NR 2 LEAKING A IXXA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SW 11 827BX 81508 40 45971 692415 EN ROUTE FROM LAX TO SAN, THE FLIGHT CREW NOTICE A DECLINE OF OIL QUANTITY ON THE NR 2 ENGINE. THE FLT CREW SECURED THE ENGINE FOLLOWING COMPANY PRECEDURES FOR PRECAUTIONARY MEASURES. THE FLIGHT CONTINUED TO SAN FOR AN UNEVENTFUL LANDING. MAINTENANCE SERVICED, INSPECTED AND PERFORMED ENGINE RUNS IN ACCORDANCE WITH THE COMPANY JET RUN HANDBOOK WITH NO DISC REPANCIES NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT 4A25 E21EU 2004021200038 20040212 00038 CE 2004 2 12 YAD2003F00004 1 20010327 A 3411 S10711 PITOT LINE CESSNA 207 207A 2073604 CE CONT O520 IO520* 17032 SO AIRSPEED CHAFED E YADA O OTHER N FALSE WARNING NR NOT REPORTED 1 AL 03 9874M 20700745 FOLLOWING REPAIR FROM LANDING ACCIDENT, ON FIRST FLIGHT AFTER REPAIRS, PILOT REPORTED AIRSPEED APPEARED TO INDIDCATE 30 KNOTS LOW. POST FLIGHT MAINTENANCE REVELED A CHAFE HOLE IN PITOT LINE IN LT WING AT A NOSE RIB. 1 H 7 1 3O 3 O A16CE E5CE 2003121000003 20031210 00003 CE 2003 12 10 ACE1024011 1 20011024 A 2913 MS24171D1 RELAY BEECH 1900 1900C 1154161 CE HYD SYSTEM BURNED E YADA O OTHER N FALSE WARNING NR NOT REPORTED 1 AL 03 45GL 34217 31098 UC45 ON ARRIVAL, THE LANDING GEAR MOTOR CIRCUIT BREAKER POPPED, THE LOW HYDRAULIC LEVEL ENUNCIATOR CAME ON AND THE GEAR HAD T O BE MANUALLY EXTENDED. AN UNEVENTFUL LANDING WAS MADE. MAINTENANCE FOUND THE HYDRAULIC PUMP MOTOR VERY HOT AND THE CO NTACTS IN THE MOTOR RELAY BURNED (WELDED), FLUID LEVEL WAS VERIFIED GOOD (FALSE LOW LEVEL WARNING). THE RELAY, PUMP MOT OR AND LOW LEVEL SENSOR WERE REPLACED. THIS FAILURE MAY BE RELATED TO CONTROL NR ACE1018011. 2 L 7 2 4T RT A24CE 2003121900021 20031219 00021 EA 2003 12 19 ACE110820011 2 20011108 A 7200 ENGINE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA NR 2 FAILED E YADA E ENGINE SHUTDOWN B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DE DESCENT 1 AL 03 1563C UC20 PCE32600 ON DESCENT, NR 2 ENGINE TORQUE BEGAN TO FALL AND THE NR 2 ENGINE OIL PRESSURE WARNING LIGHT CAME ON. THE ENGINE WAS SEC URED. THE ODOR OF OIL SMOKE WAS IN THE CABIN. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE VERIFIED A LACK OF EN GINE OIL ON THE DIP STICK (6 QUARTS LOW), METAL IN THE ENGINE OIL SCREEN, OIL RUNNING OUT OF THE ENGINE INTAKE AND UNUSU AL NOISE WHEN TURNING THE PROPELLER. THE ENGINE IS TO BE REPLACED. 2 L 7 2 4T 4 T RT A24CE E4EA 2003121900022 20031219 00022 CE 2003 12 19 ACE1105011R1 1 20011108 A 3233 MS272401 SWITCH BEECH 1900 1900C 1154161 CE ACTUATOR FAILED E YADA O OTHER J WARNING INDICATION AP APPROACH 1 AL 03 41UE 6043 595 UC41 ON APPROACH TO LANDING, NOSE GEAR GREEN LIGHT DIDN`T COME ON WITH GEAR HANDLE SELECTED DOWN. MAINTENANCE COULD NOT DUPL ICATE THE DISCREPANCY ON THE GROUND. THE NOSE GEAR UP AND DOWNLOCK SWITCH AND CONNECTOR WERE REPLACED AND AN OPERATIONA L CHECK FLIGHT WAS PERFORMED. THE CHECK FLIGHT WAS UN-SATISFACTORY DUE FAILURE OF THE NOSE DOWN AND LOCK INDICATOR FAUL T. REPLACED NOSE GEAR ACTUATOR. 2 L 7 2 4T RT A24CE 2003121900024 20031219 00024 CE 2003 12 19 ACE1018011 1 20011018 A 3200 LANDING GEAR BEECH 1900 1900C 1154161 CE ICED E YADA O OTHER O OTHER NR NOT REPORTED 1 AL 03 45GL 34152 31053 UC45 ON ARRIVAL, THE LANDING GEAR SELECTOR HAD TO BE CYCLED MULTIPLE TIMES TO ACHIEVE GEAR DOWN AND SAFE INDICATION. MAINTEN ANCE COULD NOT DUPLICATE THE FAULT AND INSPECTED THE SYSTEM, INCLUDING MULTIPLE SATISFACTORY CYCLES. THE POSSIBILITY TH AT THE FAULT WAS ICING RELATED EXISTS. 2 L 7 2 4T RT A24CE 2003121900023 20031219 00023 CE 2003 12 19 ACE1025011 1 20011025 A 3260 1003810061 DOWNLOCK SWITCH BEECH 1900 1900C 1154161 CE HARNESS BROKEN E YADA O OTHER N FALSE WARNING AP APPROACH 1 AL 03 1566C UC36 ON APPROACH, NOSE GEAR GREEN DOWN AND LOCKED LIGHT FAILED TO ILLUMINATE INITIALLY, IT CAME ON A FEW MINUTES AFTER THE GE AR WAS DOWN. THE AIRCRAFT WAS FERRIED WITH THE GEAR DOWN. MAINTENANCE FOUND ONE WIRE IN THE DOWN AND LOCK SWITCH HARNE SS CORRODED AND BROKEN (DUE NICK IN WIRE INSULATION). THE SWITCH WAS REPLACED. 2 L 7 2 4T RT A24CE 2003121900026 20031219 00026 CE 2003 12 19 ACE1016011 1 20011016 A 2720 1145240525 BRACKET CESSNA 170 170B 2072306 CE RUDDER CONTROL FROZEN E YADA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 AL 03 4632C 25576 PILOT REPORTED RUDDER FROZEN IN FLT. UNEVENTFUL LANDING. MAINTENANCE INITIALLY CONFIRMED THE RUDDER COULD NOT BE MOVED , THEN IT FREED UP. REMOVED CARGO COMPARTMENT FLOOR AT CARGO DOOR AND OBSERVED WATER FROZEN AROUND RUDDER CABLE PULLEYS AT FUSELAGE STA 495. REMOVED WATER AFTER THAWING. THIS IS THE SECOND INCIDENT OF THIS NATURE ON THIS AIRCRAFT TYPE TH AT WE HAVE EXPERIENCED. 1 H 7 1 3O A799 2003121900018 20031219 00018 CE 2003 12 19 ACE1031011 1 20011101 A 2822 12990251 PUMP BEECH 1900 1900C 1154161 CE DRAIN LEAKING E YADA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 03 1563C 37454 34366 UC20 A FAILED NR 2 ENGINE LOW PRESSURE FUEL BOOST PUMP WAS IDENTIFIED WHILE THE AIRCRAFT WAS IN THE HANGAR FOR OTHER MAINTENA NCE. THE FAILURE WAS IDENTIFIED BY FUEL DRIPPING OUT OF THE NR 2 ENGINE GANG DRAIN DUE TO PREVIOUS COMPLIANCE WITH MFG MANDATORY SB 71-3307. THIS IS THE SECOND OCCURRENCE OF FUEL RESIDUE BEING FOUND IN THE LANDING GEAR WELL AND ON THE LAN DING GEAR DUE TO THE POST SB LOCATION OF THE LOW PRESSURE FUEL PUMP DRAIN. SUGGEST SB 71-3307 BE REVIEWED AND A POSSIBL E CHANGE TO DRAIN POINT LOCATION BE INVESTIGATED. CONSIDER A CHANGE OF THE DRAIN CONNECTION TO THE ENGINE BREATHER LINE TO BE A SAFER LOCATION FOR THE VENTING OF RAW FUEL. 2 L 7 2 4T RT A24CE 2004013000172 20040130 00172 NM 2004 1 30 CALA0400018 1 20010804 A 5330 SKIN BOEING 737 737724 13844BY NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14735 28950 THE AIRCRAFT WAS STRUCK BY A GROUND SERVICE VEHICLE DURING GROUND OPERATIONS WHILE IN LAX. THE FUSELAGE SKIN WAS DAMAGE D AT STA 927, S20L. THE DAMAGED SKIN WAS TRIMMED OUT AND A REPAIR WAS INSTALLED IAW ECRA 5330-03314. 2 L 7 2 4F RT A16WE 2004021200026 20040212 00026 CE 2004 2 12 ACE1116011 1 20011116 A 2720 9752402829 CONTROL CABLE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE RUDDER FROZEN E YADA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 AL 03 111AX 32370 28041 UC81 PILOT REPORTED RUDDER FROZEN IN FLIGHT, UNEVENTFUL LANDING MADE. PILOT REPORTED THE RUDDER BROKE FREE WHILE TAXING REMO VED CARGO COMPARTMENT FLOOR AT CARGO DOOR AND OBSERVED WATER FROZEN AROUND RUDDER CABLE PULLEYS AT FUSELAGE STATION 495. REMOVED WATER AFTER THAWING. ADDITIONAL PRESSURE DRAINS WERE INSTALLED. THIS IS THE THIRD INCIDENT OF THIS NATURE ON THIS AIRCRAFT TYPE THAT WE HAVE EXPERIENCED. (K) 2 L 7 2 4T 4 T RT A24CE E4EA 2004021200037 20040212 00037 CE 2004 2 12 ACE1120011 1 20011206 A 2721 TRIM SYSTEM CESSNA 207 207A 2073604 CE CONT O520 IO520* 17032 SO RUDDER FAILED E YADA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 AL 03 75941 17246 20700656 AIRCRAFT VEERED OFF RUNWAY AFTER LANDING WITH RUDDER TRIM PROBLEM. THE AIRCRAFT CAME TO REST ON EMBANKMENT 20 FT OFF TH E SIDE OF THE RUNWAY. NOSE GEAR FORK SEPARATED FROM THE STRUT AS A RESULT OF EXCURSION. ADDITIONAL DAMAGE CONSISTED OF BENT PROP BLADE, BROKEN RT WING TIP (PLASTIC), CRUSHED TAIL SKID (CAUSING DAMAGE TO THE PLASTIC TAIL CONE) AND A HOLE I N THE BELLY SKIN AT STA 18.00. PILOTS WRITTEN DISCREPANCY STATES- RUDDER TRIM SYSTEM FAILED RESULTING IN AN OFF AIRPORT EXCURSION. OTHER THAN NOSE STRUT BEING (FLAT), POST INCIDENT MAINT INSP AND REPAIRS DID NOT DISCLOSE ANY DEFECTS IN TH E RUDDER, RUDDER TRIM OR NOSE GEAR STEERING SYSTEM. FERRY FLIGHT DID NOT GENERATE ADDITIONAL DISCREPANCIES IN THE TRIM. 1 H 7 1 3O 3 O A16CE E5CE 2004021200039 20040212 00039 EA 2004 2 12 YAD2003F00005 2 20010924 A 7230 PT6A65BGG GAS GENERATOR BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA RT ENGINE SEIZED E YADA A UNSCHED LANDING X A ENGINE FLAMEOUT FLAME/FIRE CL CLIMB 1 AL 03 5632C 18466 3841 UC81 PCE32413 AC DEPARTED AND GOING THROUGH 5,000 FT THE COPILOT REPORTED SEEING AN ORANGE FLASH FROM THE RT ENGINE, THEN LOUD NOISE A ND FLASH OF FIRE FROM THE NR 2 ENG EXHAUST, PILOT REPORTED THAT ENGINE SEIZED AND WAS SECURED. NO FIRE WARNING WAS RECE IVED AND THE FIRE EXTINGUISHING BOTTLE WAS NOT DISCHARGED. THE AC RETURNED AND MADE AN UNEVENTFUL LANDING. THE OIL FILT ER HAS BEEN INSPECTED AND FOUND CLEAN, THE COMPRESSOR IS SEIZED AND HAS HEAVY RUB/BLADE FAILURE ON THE FIRST STAGE COMPR ESSOR AND ON THE COMPRESSOR TURBINE BLADES. ENGINE IS REMOVED FOR MAJOR REPAIR. 2 L 7 2 4T 4 T RT A24CE E4EA 2004042200119 20040422 00119 NE 2004 4 22 EGR2004F00002 2 20010427 A 7210 4639202011 CLUTCH BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101* NE NR 2 ENGINE DAMAGED E EGRA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION TX TAXI/GRND HDL 1 EA 17 7062J 7178 AC WAS ON THE GROUND WITH BOTH ENGINES AT IDLE IN PREPARATION FOR FLIGHT. THE PILOT HEARD A LOUD BANG AND FELT A SHUTTI NG IN THE AC. THE AC WAS SHUTDOWN AND INSPECTED BY THE PILOT WITH NO ABNORMALITIES FOUND. THE ENGINES WERE RESTARTED A ND SPLIT IN TORQUE AND RPMS WAS OBSERVED BETWEEN NR 1 AND NR 2. THE AC WAS SHUT DOWN AND DETAILED INSPECTION REVEALED A SHEARED NR 2 ENGINE DRIVE SHAFT. NR 2 ENGINE TO TRANSMISSION DRIVESHAFT SHEARED DUE TO A MALFUNCTIONING ENGAGEMENT OF THE NR 2 MAIN TRANSMISSION CLUTCH. CLUTCH FAILED TO ENGAGE PROPERLY. AC INSP IAW INSTRUCTIONS. DRIVE SHAFT, CLUTCH AND BLOWER DRIVES REPLACED. 1 G 7 2 3U 3 U H13EU E5NE 2004042700054 20040427 00054 GL 2004 4 27 ERAA092664 2 20010111 A 7230 SEAL BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C18 03011 GL ENGINE DIFFUSER FOD A ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 ER23376 FOD DAMAGE TO SEAL. CONTOUR FOUND DAMAGED AT CYCLE 1 INDUCTION. FULL OVERHAUL INCLUDING CONTOUR RESTORATION. 1 G 7 2 3U 3 U H3EU E4CE 2004042700107 20040427 00107 NM 2004 4 27 DL73S040294 1 20010401 A 3150 WARNING HORN BOEING 737 737232 1384475 NM COCKPIT ACTIVATED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 308DL 23080 RTO AT 30KTS DUE TO T/O WARNING HORN. FOUND LEADING EDGE IND C/B POPPED. RESET AND ALL CHECKS OK. 2 L 7 2 4F RT A16WE 2004052000209 20040520 00209 SO 2004 5 20 ZIAA04055 1 20010906 A 5311 800120111 FRAME LKHEED 188 188C 5262604 SO FUSELAGE CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 1146 FOUND FUSELAGE FRAME CRACKED AT FS 397.5, STRINGER 21. REPAIRED FRAME IAW L-188 SRM 53-2-3, FIG 2. (M) 2 L 7 4 4T 4A22 2004052000210 20040520 00210 SO 2004 5 20 ZIAA04001 1 20010730 A 5730 8385482 DOUBLER LKHEED 188 188C 5262604 SO FUSELAGE CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 1146 FOUND WS 249 LOWER SURFACE, LEAP DOUBLER AT FORWARD EDGE IS CRACKED AT RIGHT WING. ROUTED OUT DEFECTIVE AREA OF LEAP DO UBLER. DYE PEN OF WING PLANK REVEALED NO DISCREPANCIES. REPAIRED IAW L188 SRM 57-2-1 AND SEALED INTERNALLY. (M) 2 L 7 4 4T 4A22 2004052000211 20040520 00211 SO 2004 5 20 ZIAA04043 1 20010906 A 5315 8085689 FLOORBEAM LKHEED 188 188C 5262604 SO FUSELAGE CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 1146 YIP - FOUND FLOORBEAM AT FS 200 RIGHT SIDE NEAR PORTA POTTY AREA CORRODED. REMVOED CORRODED SECTION OF FLOORBEAM AND RE PAIRED FS 200 FLOORBEAM PER L-188 SRM 53-2-4, FIG 2 SHEET 1. (M) 2 L 7 4 4T 4A22 2004052000212 20040520 00212 SO 2004 5 20 ZIAA04056 1 20010906 A 5311 8001212 FRAME LKHEED 188 188C 5262604 SO FUSELAGE CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 1146 FOUND FUSELAGE FRAME CRACKED AT FS 654 STRINGER 13. REPAIRED FRAME AT STRINGER 13 PER L-188 SRM 53-2-3, FIG 2. (M) 2 L 7 4 4T 4A22 2004052000214 20040520 00214 SO 2004 5 20 ZIAA04049 1 20010906 A 5311 8001212 FRAME LKHEED 188 188C 5262604 SO FUSELAGE CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 1146 YIP - FOUND FUSELAGE FRAME CRACKED AT FS 654 BETWEEN STRINGER 9-10. REPAIRED FRAME AT STRINGER 9-10 IAW L-188 SRM 53-2- 3, FIG 2. (M) 2 L 7 4 4T 4A22 2004052000215 20040520 00215 SO 2004 5 20 ZIAA04050 1 20010906 A 5311 8001173 FRAME LKHEED 188 188C 5262604 SO FUSELAGE CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 1146 FOUND FUSELAGE FRAME CRACKED AT FS 716 AT STRINGER 72. REPAIRED FRAME AT STRINGER 68-1 PER L-188 SRM 53-2-3, FIG 2. (M ) 2 L 7 4 4T 4A22 2004052000243 20040520 00243 SO 2004 5 20 ZIAA04002 1 20010730 A 5730 8385482 DOUBLER LKHEED 188 188C 5262604 SO FUSELAGE CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 1146 YIP - FOUND LWER SURFACE AT WS 253, FORWARD EDGE OF LEAP DOUBLER IS CRACKED, RIGHT WING. CRACK STOP DRILLED, ROUTED OUT DEFECTIVE AREA OF LEAP DOUBELR. DYE PEN OF WING PLANK REVEALED NO DISCREPANCIES. REPAIRED IAW L-188 SRM 57-2-1 AND SE ALED INTERNALLY. (M) 2 L 7 4 4T 4A22 2004052000244 20040520 00244 SO 2004 5 20 ZIAA04044 1 20010906 A 5311 8001153 FRAME LKHEED 188 188C 5262604 SO FUSELAGE CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 1146 FOUND FUSELAGE FRAME CRACKED AT FS 426 AT STRINGER 1. REPAIRED FRAME AT FS 426 FROM STRINGER 68-4 IAW L-188 SRM 53-2-3. (M) 2 L 7 4 4T 4A22 2004052000245 20040520 00245 SO 2004 5 20 ZIAA04052 1 20010906 A 5311 8001173 FRAME LKHEED 188 188C 5262604 SO FUSELAGE CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 1146 FOUND FUSELAGE FRAME CRACKED AT FS 920 BETWEEN STRINGERS 67-69. REPAIRED FRAME AT STRINGER 66-69 PER L-188 SRM 53-2-3, FIG 2. (M) 2 L 7 4 4T 4A22 2004052000247 20040520 00247 SO 2004 5 20 ZIAA04051 1 20010906 A 5311 8001173 FRAME LKHEED 188 188C 5262604 SO FUSELAGE CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 1146 YIP - FOUND FUSELAGE FRAME CRACKED AT FS 730, STRINGER 72. REPAIRED FRAME AT STRINGER 72 PER L-188 S/B 706 DWG 842354. (M) 2 L 7 4 4T 4A22 2004052000248 20040520 00248 SO 2004 5 20 ZIAA04045 1 20010906 A 5311 8001153 FRAME LKHEED 188 188C 5262604 SO FUSELAGE CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 1146 YIP - FOUND FUSELAGE FRAME CRACKED AT FS 426 AT STRINGER 71. REPAIRED FRAME AT FS 426 FROM STRINGER 68-4 IAW L-188 SRM 53-2-3. (M) 2 L 7 4 4T 4A22 2004052000249 20040520 00249 SO 2004 5 20 ZIAA04046 1 20010906 A 5311 8001153 FRAME LKHEED 188 188C 5262604 SO FUSELAGE CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 1146 YIP - FOUND FUSELAGE FRAME CRACKED AT FS 464 AT STRINGER 70-71. REPAIRED FRAME AT STRINGER 70-71 IAW L-188 SRM 53-2-3, FIG 2. (M) 2 L 7 4 4T 4A22 2004052000250 20040520 00250 SO 2004 5 20 ZIAA04047 1 20010906 A 5311 8001153 FRAME LKHEED 188 188C 5262604 SO FUSELAGE CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 1146 FOUND LIGHT CORROSION ON FRAME AT FS 540 STRINGER 69. REMOVED CORROSION AND REPAIRED FRAME PER L-188 SRM 53-2-3, FIG 2. PLUGGED NEGLIBIBLE HOLES PER L-188 SRM 51-3-6, FIG 1. (M) 2 L 7 4 4T 4A22 2004052000251 20040520 00251 SO 2004 5 20 ZIAA04048 1 20010906 A 5311 80011627 FRAME LKHEED 188 188C 5262604 SO FUSELAGE CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 1146 YIP - FOUND FUSELAGE FRAME CRACKED AT FS 578 BETWEEN STRINGERS 72-1. REPAIRED FRAME AT STRINGER 72-1 IAW L-188 SRM 53-2 -3 FIG 2. (M) 2 L 7 4 4T 4A22 2004052000252 20040520 00252 SO 2004 5 20 ZIAA04053 1 20010906 A 5311 800120111 FRAME LKHEED 188 188C 5262604 SO FUSELAGE CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 1146 YIP - FOUND FUSELAGE FRAME CRACKED AT FS 407, STRINGER 8. REPAIRED FRAME AT STRINGER 8 PER L-188 SRM 53-2-3, FIG 2. (M ) 2 L 7 4 4T 4A22 2004052000253 20040520 00253 SO 2004 5 20 ZIAA04041 1 20010906 A 5311 8001151 FRAME LKHEED 188 188C 5262604 SO FUSELAGE CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 1146 YIP - FOUND FUSELAGE FRAME CRACKED AT FS 388 BETWEEN STRINGERS 72-1. REPAIRED FRAME AT STRINGER 72-1 PER LOCKHEED S/B 7 06 DWG 842354. (M) 2 L 7 4 4T 4A22 2004052000254 20040520 00254 SO 2004 5 20 ZIAA04003 1 20010730 A 5730 8385482 DOUBLER LKHEED 188 188C 5262604 SO RT WING CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 1146 FOUND LOWER SURFACE AT WS 265 RIGHT WING LEAP DOUBLER ON PLANK NR 4 IS CRACKED. LEAK CHECK DUE. ROUTED OUT CRACKED LEA P DOUBLER MATERIAL. INSPECTED WING PLANK SURFACE WITH DYE PEN. NO DEFECTS FOUND. REPAIRED PER L-188 SRM 57-2-1, FIG 3 , SHEET 30, TYPE 2. SEALED INTERNAL REPAIR AREA WITH SC3204A1/2 PER L-188 SRM 51-2-16. (M) 2 L 7 4 4T 4A22 2004052000255 20040520 00255 SO 2004 5 20 ZIAA04042 1 20010906 A 5311 8001151 FRAME LKHEED 188 188C 5262604 SO FUSELAGE CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 1146 FOUND FUSELAGE FRAME CRACKED AT FS 407 BETWEEN STRINGERS 1-2. REPAIRED FRAME AT STRINGER 1-2 PER L188 SRM 53-2-3, FIG 2 . (M) 2 L 7 4 4T 4A22 2004052000256 20040520 00256 SO 2004 5 20 ZIAA04054 1 20010906 A 5311 800120111 FRAME LKHEED 188 188C 5262604 SO FUSELAGE CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 1146 YIP - FOUND FUSELAGE FRAME CRACKED AT FS 401, STRINGER 8. REPAIRED FRAME AT STRINGER 8 PER L-188 SRM 53-2-3 FIG 2. (M) 2 L 7 4 4T 4A22 2004061600080 20040616 00080 NM 2004 6 16 2001UALA00905 1 20010601 A 3350 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 670UA 29240 EMERGENCY EEL LIGHT'S INOP FROM RT ROW 37 TO ROW 41 AND BOTH AFT LAV AND GALLEY FLOOR EEL LIGHT'S. BATTERY PACK AND POW ER STRIP. REPLACED BATTERY PACK AND POWER STRIP. 2 L 7 2 4F 4 F RT A1NM E24NE 2004061600114 20040616 00114 NM 2004 6 16 2004UALA00534 1 20010531 A 3040 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE WINSHIELD HEAT SMOKE A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 541UA 25253 FORWARD RIGHT WINDSHIELD HEAT WIRE SMOKING. CIRCUIT BREAKER C392 POPPED. CONNECTOR AT TERMINAL J5 ON THE 1R WINDOW WAS LOOSE. THIS LOOSE CONNECTION CAUSED THE WIRE TO OVERHEAT. REPLACED W2314 HARNESS ASSY FROM TERMINAL BLOCK TB5038 TO WI NDOW AND RESET CIRCUIT BREAKER C392. 2 L 7 2 4F 4 F RT A2NM E17NE 2004102900002 20041029 00002 SO 2004 10 29 CHQA000501 1 20011128 A 2120 ODOR EMB 145 EMB145LR 3260212 SO CABIN DETECTED A CHQA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 GL 11 145226 BURNING SMELL IN CABIN WITH ANTI-ICE ON, FOUND RH ENGINE FUEL NOZZLES WORN REMOVED AND REPLACED NOZZLES. 2 L 7 2 4T RT T00011AT 2004062500027 20040625 00027 NM 2004 6 25 UPS04M42458 1 20010319 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, LEFT BARREL NUT HOLE NR 26 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.006 INCH. SPLICE FITTING FABRICATED PER EN 1100-04 . NEW SPLICE FITTING INSTALLED PER SRM 51-22-01 & SRM 51-38-01 VOL 2 REV 34. BARREL NUT HOLE REPAIRED PER EN 1160-4 (R EF UPS ENGINEERING FILE NR MD11-55-20042). 2 L 7 3 4F RT A22WE 2004070700034 20040707 00034 EU 2004 7 7 184901 1 20010612 A 2613 WARNING LIGHT SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RT ENGINE ILLUMINATED A UHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 17 152CQ 152 APPROXIMATELY 1035 (UTC), FLIGHT 4550 FWA-PIT, CREW ABORTED TAKEOFF WHEN A TAILPIPE HOT WARNING WAS INDICATED ON THE RIG HT ENGINE. 2 L 7 2 4T 4 T RT A52EU E8NE6 2004081600070 20040816 00070 NM 2004 8 16 P5CA0401104 1 20010621 A 2612 FIRE LOOP BOEING 747 7472D3B 1384805 NM GE CF6 CF650E2 30018 NE NR 2 ENGINE INOPERATIVE A P5CA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 WP 23 505MC 21251 517506 NR 2 ENGINE A-LOOP INOP IN FIRE TEST MODE. TRANSFERRED TO DMI 32697 AND PLACARD PER MEL 26-1. 2 L 7 4 4F 4 F RT A20WE E23EA 2004082500102 20040825 00102 NM 2004 8 25 QXEA200400582 1 20010807 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - OUTER CARGO DOOR SKIN HAS A 3.4 BY 3.8 GOUGED AREA 5.5 INCH FROM THE TOP AND 15 INCHES FROM THE AFT EDGE. REPAIRE D IAW DHC-8-2- RD 8-52-029. 2 H 7 2 4T RT A13NM 2004090300046 20040903 00046 SO 2004 9 3 ZIAA04057 1 20011127 A 5730 8376072 SKIN LKHEED 188 188C 5262604 SO RT WING CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 1146 YIP - REMOVE REPAIR INSTALLATION AT RT WING UPPER SURFACE, WS 70, 7/8 PLANK SEAM FOR CO CONVENIENCE. CONFIRM THE EXTENT OF DAMAGE AT THIS LOCATION. INSTALL REPAIR PER ZANTOP DWG A72-R03. REMOVED EXTERNAL DOUBLERS ON PLANK 7/8 SEAM AT WS 65-83. CONFIRM CORROSION CLEAN OUT BTW WS 67.25 AND 75.23. FOUND SPLICE GAP WIDENED BTW WS 75-83. CORROSION REMOVED B TW WS 75-83, MATERIAL REMOVED WITHIN LIMITS PER S/B 620. REINSTALLED REPAIR IAW ZANTOP DWG A72-R03. NO FURTHER ACTION R EQUIRED. (M) 2 L 7 4 4T 4A22 2005102400131 20051024 00131 NM 2005 10 24 DL76K050613 1 20011002 A 5753 113T22079 SHIM BOEING 767 767332 1382001 NM RT WING TE FLAP MIGRATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 172DZ 29691 A SHIM UNDER THE INBOARD MAIN FLAP, INBOARD TORQUE BOX, BEAM FITTING MIGRATED INBOARD APPROX 0.125 IN. SHIM WAS INSPECT ED UNTIL REPLACEMENT WAS ACCOMPLISHED PER ER/A 381873-14AD REV A CLASSIFICATION WAS CHANGED FROM MINOR TO MAJOR AT ER/A 381873-14AD REV A. 2 L 7 2 4F RT A1NM 2006060600091 20060606 00091 NM 2006 6 6 DLM88060434 1 20010828 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 919DL 49584 THE FUSELAGE SKIN AT THE FORWARD ENTRY DOOR CUTOUT WAS CRACKED IN THE LOWER AFT CORNER. THE DAMAGED SKIN WAS REMOVED AN D A REPAIR INSTALLED PER S/B MD80-53-253. THE ORIGINAL REPAIR WAS CLASSIFIED AS MINOR, BUT RECLASSIFIED DUE TO DAMAGE F INDINGS PER 09-069085-12AD, REF AD 98-17-06, 09-069085-12AD. 2 L 7 2 4F RT A6WE 2001103000080 20011030 00080 2001 10 30 VW3R200100012 4 20010802 A 2562 P3030029010 ELT BFGOODRICH LIFE RAFT INOPERATIVE B VW3R K NONE L NO TEST IN INSP/MAINT 1 WP 09 10R411 ELT DOES NOT TRANSMIT ANY SIGNAL AND NEEDS TO BE REPLACED. 2001011102734 20010111 02734 2001 1 11 SABA010001 4 20010102 A 3416 066306202 ALTIMETER COCKPIT INOPERATIVE A SABA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 33 919AE AIRCRAFT 919 ON FLIGHT 5122 FROM PGV TO CLT. AFTER CLIMBOUT FROM PGV THE CAPTAIN'S ALTIMETER FLUCTUATED THROUGH 400 FEE T. THE ALTIMETER WOULD STAY STABLE FOR A COUPLE OF MINUITS AND WOULD FLUCTUATE AGAIN. NO INFLIGHT EMERGENCY WAS DECLAR ED. AIRCRAFT RETURNED TO PGV AND LANDED WITH NO OTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S ALTIMET ER. SYSTEM LEAK CHECK AND OPS CHECK WAS PERFORMED. CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2001103000083 20011030 00083 2001 10 30 VW3R200100015 4 20010821 A 2562 P3030029010 ELT LIFE RAFT INOPERATIVE B VW3R K NONE L NO TEST IN INSP/MAINT 1 WP 09 ELT DOES NOT TRANSMIT ANY SIGNAL. THIS UNIT WAS REPAIRED BY DME CORPORATION ON 11/22/00. IT WAS TESTED WHEN IT CAME BA CK AND APPARENTLY WAS WORKING AND HAD BEEN STORED SINCE. BEFORE INSTALLING IT ON A RAFT BEING OVERHAULED, IT WAS TESTED AGAIN AND IT DID NOT TRANSMIT ANY SIGNAL. DME IS REPAIRING IT UNDER WARRANTY AND STATES THE CAUSE OF FAILURE IS TO BE D ETERMINED. 2001050900002 20010509 00002 2001 5 9 VW3R200100006 4 20010226 A 2562 P3030029010 ELT BFGOODRICH LIFE RAFT INOPERATIVE B VW3R K NONE L NO TEST IN INSP/MAINT 1 WP 09 10R276 ELT DOES NOT TRANSMIT ANY SIGNAL AND NEEDS TO BE REPLACED. 2001061500092 20010615 00092 2001 6 15 QXEA0101034 4 20010612 A 3440 HONEYWELL A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 359PH 10040 PDX - ELECRTICAL SMELL NOTED IN CABIN. REMOVED AND REPLACED GROUND PROX WARNING COMPUTER. NO FURTHER NOTED SMELL. OPERAT IONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2001102900179 20011029 00179 2001 10 29 VW3R200100010 4 20010628 A 2562 P3030029010 ELT BFGOODRICH LIFE RAFT INOPERATIVE B VW3R K NONE L NO TEST IN INSP/MAINT 1 WP 09 10R428 ELT DOES NOT TRANSMIT ANY SIGNAL AND NEEDS TO BE REPLACED. 2001102900178 20011029 00178 2001 10 29 VW3R200100009 4 20010628 A 2562 P3030029010 ELT BFGOODRICH LIFE RAFT INOPERATIVE B VW3R K NONE L NO TEST IN INSP/MAINT 1 WP 09 10R422 ELT HAS CRACKED CASE AND WILL NOT TRANSMIT. 2002030800013 20020308 00013 EA 2002 3 8 CA020121010 2 20011206 A 7200 COMPRESSOR PWA PT6 PT6A28 EA ENGINE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ENGINE SENT FOR INVESTIGATION & REPAIR AFTER OPERATOR REPORTED THAT ENGINE HAD SUSTAINED FOD TO COMPRESSOR SECTION . ENGINE HAD EXTENSIVE DAMAGE. DAMAGE ORIGINATED FROM 1ST STAGE COMPRESSOR STATOR & DISK SPACER WHICH HAD LOST PIECES O F INNER RIM & CONTINUED DOWNSTREAM ON COMPRESSOR STATORS, BLADES, DISC SPACERS, IMPELLER, GG CASE DIFFUSERS, CT BLADES & SHROUDS. DAMAGE TO IMPELLER, GG CASE, CT BLADES&SHROUDS IS 2NDARY&CAUSED BY DEBRIS LIBERATED FROM COMPRESSOR COMPONE NTS. IT IS SUB'S OPINIION THAT CAUSE OF FAILURE LOSS OF TIE BOLT TENSION THROUGH STRETCH OR POSSIBLY THROUGH LACK OF PR OPER SEATING OF COMPRESSOR COMPONENTS AT ASSY. WOULD ALLOW ROTATING ASSYDISTORTION&TYPE OF RUBS SEEN. 4 T E4EA 2001103000081 20011030 00081 2001 10 30 VW3R200100013 4 20010802 A 2562 P3030029010 ELT BFGOODRICH LIFE RAFT INOPERATIVE B VW3R K NONE L NO TEST IN INSP/MAINT 1 WP 09 10R213 ELT DOES NOT TRANSMIT ANY SIGNAL AND NEEDS TO BE REPLACED. 2001102900177 20011029 00177 2001 10 29 VW3R200100008 4 20010607 A 2562 P3030029010 ELT BFGOODRICH LIFE RAFT INOPERATIVE B VW3R K NONE L NO TEST IN INSP/MAINT 1 WP 09 10R414 ELT HAS SEVERELY CRACKED CASE AND IT DOES NOT TRANSMIT. 2001082100134 20010821 00134 2001 8 21 C1HA200196012 4 20010801 A 3421 7725005005 ADI FO'S FAILED A C1HA A UNSCHED LANDING I FLT. ATTITUDE INST. CR CRUISE 1 GL 15 696CA FO's "ATT" flag in view during banks with transfer switch in normal or copilot on aux positions.Return to DFW.ACTION TAK EN:Replaced FO's ADI ops ck normal. 2001111400118 20011114 00118 2001 11 14 F3LA200100116 4 20011112 A 2340 5224538002 AMPLIFIER CABIN INOPERATIVE A F3LA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 272 23 AIR TURN BACK. FLIGHT CREW REPORTED 30 TO 40 CHIMES FROM BACK OF AIRCRAFT. COULD NOT TALK TO CREW, INTERPHONE INOPERAT IVE. REPLACED PA AMPLIFIER AND SYSTEM CHECKED OKAY. ALSO FOUND PILOT CALL SWITCH ON FWD ATTENDANT'S PANEL BAD, CAUSING PILOT CALL CHIME WITHOUT BEING PRESSED. REPLACED FWD ATTENDANT'S PILOT CALL SWITCH AND SYSTEM CHECKED OKAY. 2001102900176 20011029 00176 2001 10 29 VW3R200100007 4 20010525 A 2562 P3030029010 ELT BFGOODRICH LIFE RAFT INOPERATIVE B VW3R K NONE L NO TEST IN INSP/MAINT 1 WP 09 10R436 ELT HAS CRACKED CASE AND IT DOES NOT TRANSMIT. 2001040900398 20010409 00398 NE 2001 4 9 20010306CW009 2 20010129 A 7250 504802 TURBINE WHEEL PWA JT12 JT12A8 52042 NE ENGINE CRACKED B JV2R K NONE O OTHER IN INSP/MAINT 1 CE 03 3140 3140 P673252 DISK TT 3140.1 TC 2697 MAX ALLOWABLE OPER. TIME IS 8000 HR AND 8000 CYCLES.DURING OVERHAUL OF ENGINE AND PERFORMING FL UORESECENT PENETRANT INSPECTION, THE SECOND STAGE TURBINE DISK PN/405802, SN/G23877 WAS FOUND TO HAVE 13 EA CRACK INDICA TION INBOARD OF THE BLADE ROOT. CRACK INDICATIONS VARY FROM APPROXIMATE .05 TO .10 INCH IN LENGTH. DISK REMOVED FROM S ERVICE FOR FURTHER INVESTIGATION. 4 J 1E9 2001102900180 20011029 00180 2001 10 29 VW3R200100011 4 20010802 A 2562 P3030029010 ELT BFGOODRICH LIFE RAFT INOPERATIVE B VW3R K NONE L NO TEST IN INSP/MAINT 1 WP 09 10R425 ELT DOES NOT TRANSMIT ANY SIGNAL AND NEEDS TO BE REPLACED. 2001103000082 20011030 00082 2001 10 30 VW3R200100014 4 20010816 A 2562 P3030029010 ELT BFGOODRICH LIFE RAFT INOPERATIVE B VW3R K NONE L NO TEST IN INSP/MAINT 1 WP 09 10R ELT DOES NOT TRANSMIT ANY SIGNAL AND NEEDS TO BE REPLACED. 2001080200021 20010802 00021 2001 8 2 M7I2001F00000 4 20010627 A 3413 5546257001 CONNECTOR COLLINS VERTICAL GYRO CORRODED B M7IR O OTHER O OTHER NR NOT REPORTED 1 GL 13 788 EXCESSIVE CORROSION ON CONNECTOR BETWEEN PINS N AND P, CAUSED BY INTERNAL CONDENSATION. THIS RESULTED IN ATTITUDE INDIC ATOR FLAGGING AND PRECESSING. 2001103000085 20011030 00085 2001 10 30 VW3R200100017 4 20011002 A 2562 P3030029010 ELT BFGOODRICH LIFE RAFT INOPERATIVE B VW3R K NONE L NO TEST IN INSP/MAINT 1 WP 09 10R209 ELT NOT TRANSMITTING AND NEEDS TO BE REPLACED. ELT CASE CRACKED. 2001080200023 20010802 00023 2001 8 2 M7I2001F00001 4 20010620 A 3413 5546257001 CONNECTOR COLLINS VERTICAL GYRO CORRODED B M7IR O OTHER O OTHER NR NOT REPORTED 1 GL 13 2153 EXCESSIVE CORROSION ON CONNECTOR BETWEEN PINS N AND P CAUSED BY INTERNAL CONDENSATION. THIS RESULTED IN ATTITUDE INDICA TOR FLAGGING AND PRECESSING. 2001050900001 20010509 00001 2001 5 9 VW3R200100005 4 20010124 A 2565 TUBE AIRCRUISERS ESCAPE SLIDE DAMAGED B VW3R K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 09 22190789 THE EVACUATION SLIDE WAS RECEIVED WITH EXCESSIVE WEAR ON THE GIRT ASSEMBLY AND A ONE INCH HOLE WORN IN THE INFLATION TUB E NEXT TO THE GIRT. SLIDE WAS MANUFACTUED IN 07/1989. IF THIS SLIDE WERE NEEDED IN AN EMERGENCY IT WOULD NOT HAVE RETA INED AIR TO SUPPORT THE EMERGENCY EVACUATION OF THE AIRPLANE. 2001103000084 20011030 00084 2001 10 30 VW3R200100016 4 20010919 A 2562 P3030029010 ELT BFGOODRICH LIFE RAFT INOPERATIVE B VW3R K NONE L NO TEST IN INSP/MAINT 1 WP 09 10R275 ELT NOT TRANSMITTING AND NEEDS TO BE REPLACED. 2001012500151 20010125 00151 NE 2001 1 25 COMA0160093 2 20010107 A 7200 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RIGHT VIBRATION A COMA A UNSCHED LANDING E Y J VIBRATION/BUFFET ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SO 01 709CA 7238 807528 RT ENGINE VIB INDICATION AT .7, ENGINE FAILED. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 2001012500185 20010125 00185 SO 2001 1 25 SWIA972263 1 20010112 A 2120 DOOR EMB 120 EMB120RT SO PWA 118 PW118 NE LT RAM AIR DAMAGED A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 07 156CA 120156 IN DESCENT FROM FL240 CABIN FILLED WITH SMOKE. DIVERTED TO PDX. REPLACED LEFT RAM AIR DOOR IAW MM 21-26-01. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001020700083 20010207 00083 NE 2001 2 7 20010207SG005 2 20010116 A 7532 ETPU10002C PRESSURE SWITCH BOEING 757 757200 1384950 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE MALFUNCTIONED A N8TA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION TX TAXI/GRND HDL 1 WP 19 506NA 24771 ON TAXI IN TO THE GATE, RIGHT ENGINE FLAMED OUT AND EICAS STATUS MESSAGE R ENG LP PUMP CAME ON. REPLACED TRANSIENT PRES SURE UNIT. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2001022000015 20010220 00015 SO 2001 2 20 SWIA972334 1 20010129 A 2750 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAP SYSTEM CONTAMINATED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 217SW 120286 FLAP DISAGREEMENT AFTER TAKEOFF WHEN RETRACTING FLAPS TO 0 DEGREES. QRH PROCEDURES COMPLIED WITH AND DISAGREEMENT REMAI NED. RETURNED TO SLC. CLEANED GLYCOL FROM OUTBOARD FLAP CANNON PLUGS. CYCLED FLAPS SEVERAL TIMES, INDICATION AND OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001041100141 20010411 00141 NE 2001 4 11 2001UALA00063 2 20010129 A 7230 52G38650A168 SEAL BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 2 ENGINE LEAKING A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 797UA 26924 222010 DURING CRUISE, FLT REPORTED HOT, ELEC SMELL IN COCKPIT & CABIN WITH RECIRC FANS OFF. WITH RECIRC FANS ON, SMELL GOES AW AY. DIVERTED TO ORD. *S/D* GROUND RUNUP REVEALED SLIGHT OIL SMELL IN COCKPIT & CABIN WHEN ISOLATED TO RIGHT PACK AND RIGHT ENG. NO ELEC OR PLASTIC SMELL DETECTED. OIL CONSUMPTION NORMAL. RT PRSOV LOCKED CLOSED & ACFT DISPATCHED TO SFO FOR ENG CHG. FOUND OIL IN LPC DRUM ROTOR, STUB SHAFT & FAN HUB. OIL CAN ENTER GASPATH THROUGH WEEP HOLES IN THE DRUM ROTOR & FAN SPINNER. THE ROOT CAUSE IS POOR SEALING OF 9TH STAGE AIR AT 1.5-2 BEARING CARBON SEAL ASSY 9TH STAGE AIR L EAKS TO THE NR 1 BEARING COMPT & UPSETS THE PRESS BALANCE ON NR 1 CARBON SEAL ALLOWING OIL TO LEAK TO LPC DRUM, SHAFT & 2 L 7 2 4F 4 F RT T0001SE E46NE 2001030100141 20010301 00141 WP 2001 3 1 20010226CW005 1 20010123 A 3340 Q4559 BULB DOUG DC4 C54BDC 3021516 WP PWA R2000 R20007M2 52023 NE HAMSTD 23E 23E50 NE LANDING LIGHT BURNED OUT I B2OB K NONE L NO TEST IN INSP/MAINT 1 AL 01 44911 10461 BULB BURNED OUT. 2 L 7 4 4R 4 R A762 5E5 6 C P603 2001031200628 20010312 00628 NM 2001 3 12 VNAA0101025 1 20010127 A 7110 001A711E1400008 COWL DOOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE OPEN A VNAA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 GL 07 429JS 14491 3043 ON THE DESCENT, THE RIGHT HAND INBOARD ENGINE COWLING DOOR PARTIALLY OPENED AND THE CREW RECEIVED A RIGHT HAND ENGINE F IRE LIGHT. THE CREW FOLLOWED THE EMERGENCY MANUAL AND SHUT DOWN THE ENGINE. THE ENGINE FIRE LIGHT EXTINGUISHED AND FLI GHT 4102 LANDED WITHOUT ANY FURTHER INCIDENTS. THERE WAS NO FIRE AND THE AIRCRAFT WAS FERRIED TO DAYTON WHERE MAINTENAN CE INSPECTED AND REPLACED THE ENGINE COWLING IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 71-10-20. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001031900157 20010319 00157 NM 2001 3 19 2001UALA00024 1 20010113 A 2824 VALVE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUEL SYS FAILED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 348UA 24252 FUEL TRANSFER PROBLEMS. *S/D* REPLACED THE CROSSFEED VALVE, NR 2 FUEL TANK FORWARD AND AFT BOOST PUMP CHECK VALVES, RI GHT HAND CENTER TANK BOOST PUMP CHECK VALVE, AND RIGHT CENTER TANK BOOST PUMP. ACCOMPLISHED CENTER TANK OVERRIDE CHECK. SYSTEM OP''S CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2001032700316 20010327 00316 SO 2001 3 27 SWIA972408 1 20010302 A 2750 WIRE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FLAP SYSTEM SHORTED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 195SW 120127 DURING CRUISE FLIGHT FLAP AND ADVANCED SWS LIGHT ON MAP AND ASSYMETRY, CONTROL FAULT AND DISAGREEMENT ON OVERHEAD. MADE FLAPS 0 LANDING. ISOLATED AND THEN MEGGERED EACH WIRE FOR THE ENTIRE FLAP SYSTEM. FOUND WIRE W602-009-22 SHORTED TO G ROUND. REPLACED WIRE BETWEEN CONNECTION P0366 PIN V AND P1756 PIN J. ALL OTHER WIRES CHECKED GOOD. CHECKED ALL GROUND S AND FOUND ALL GOOD. CYCLED FLAPS NUMEROUS TIMES, ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001033000117 20010330 00117 NM 2001 3 30 2001UALA00119 1 20010116 A 5610 141W74002 WINDSHIELD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT CRACKED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 573UA 26685 RIGHT WINDSHIELD OUTER PANE CRACKED. RIGHT WINDOW HEAT EICAS MESSAGE. *S/D* WINDOW FINDINGS: 1) SLIGHT MOISTURE INGRE SSION ON UPPER BUS BAR BY SENSOR WIRES. 2) BUS BARS IN GOOD CONDITION, SLIGHT DISCOLORATION. 3) HUMP SEAL REPAIR HISTORY , MINIMAL EROSION, BUT IN GOOD CONDITION. 4) INTERLAYER LEAKAGE THROUGH CRACKS DUE TO WINDOW HEAT LEFT ON AFTER WINDOW F AILURE. CAUSE OF FAILURE WAS DETERMINED TO BE FOD. FOD WAS NOTED 2.5 INCHES FROM LOWER BUS BAR, 14 INCHES FROM FWD EDG E. BREAKAGE PATTERN FANNED OUT FROM FOD ORIGIN. 2 L 7 2 4F 4 F RT A2NM E17NE 2001040300077 20010403 00077 CE 2001 4 3 CA010212032 1 20010123 A 3240 124K0016CL0150 LINE CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE BRAKE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 3349 (CAN) AFTER SHUTDOWN THE FLIGHT CREW OBSERVED THE LT WHEEL WELL AREA SPLATTERED WITH BRAKE FLUID. CORRESPONDINGLY THE B RAKE RESERVOIR LEVEL WAS DOWN SIGNIFICANTLY. INVESTIGATION REVEALED THAT THE LT FLEXIBLE BRAKE LINE WAS LEAKING AT THE U PPER SWAGED FITTING. THE BRAKE LINE WAS REPLACED, BRAKE RESERVOIR RELENISHED, SYSTEM BLED AND THE A/C WAS RETURNED TO SE RVICE. 1 L 7 2 4F 4 F A22CE E1NE 2001040400183 20010404 00183 NM 2001 4 4 2001UALA00144 1 20010203 A 5754 WEB BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE SLAT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7287U 21565 NR 2 INBOARD SLAT WEB CUTOUT AT INBOARD THERMAL ANTI ICE DUCT CRACKED. REPAIRED WEB PER MM 57-45-19. 2 L 7 3 4F 4 F A3WE E2EA 2001040400216 20010404 00216 EU 2001 4 4 CA010305008 1 20010226 A 2434 9789601090 BRUSHES PILATS 524321215 PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL GENERATOR WORN W A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 CA 111 111 100320 (CAN) DURING CLIMB OUT THE GEN 2 WENT OFF LINE. AS THE LOAD DROPPED THE GEN 2 WAS TURNED BACK ON LINE AND IT STAYED ON L INE UNTIL THE LOAD WAS INCREASED AND THEN IT WENT BACK OFF LINE. AIRCRAFT RETURNED TO BASE AND THE GEN 2 WAS REPLACED. T HIS GEN IS A POST SB 24-016 GEN, AND THE BRUSHES WERE REPLACED FEB 9 FOR BEING WORN OUT. THEY HAD 260.5 HOURS AT THAT TI ME THAT THEY WERE REPLACED. THE GEN WAS REPLACED AT PILATUS REQUEST. THE BRUSHES ONLY HAD 110.6 HOURS ON THEM AT THIS BR USH FAILURE. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001040900523 20010409 00523 NE 2001 4 9 20010312CW015 2 20010210 A 7200 ENGINE CVAC 440 440 2422902 WP PWA R2800 R2800* 52026 NE NACELLE FAILED I FEIB A UNSCHED LANDING X ENGINE FLAMEOUT NR NOT REPORTED 1 SW 17 24DR 393 P36820 INTERNAL ENGINE FAILURE IN CRUISE FLIGHT, UNKNOWN SPECIFIC CAUSE PENDING TEARDOWN. 2 L 7 2 4R 4 R 6A6 5E8 2001041600187 20010416 00187 NM 2001 4 16 2001UALA00283 1 20010321 A 5412 BULKHEAD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 PYLON WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 NR 2 PYLON AFT BULKHEAD NAC STA 201.02 RIGHT SIDE VERTICAL FLANGE LOWER CORNER HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAI R ACCOMPLISHED.INSTALLED REPAIR PLATE PER SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041600203 20010416 00203 NM 2001 4 16 2001UALA00300 1 20010322 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 FORWARD PIT STRINGER CLIP AT STA 500D STRINGER 26R IS CRACKED AT THE UPPER FASTENER. INSTALLED NEW CLIP. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600305 20010416 00305 NM 2001 4 16 2001UALA00339 1 20010327 A 5532 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE VERTICAL STAB DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 309UA 23670 DENT IN VERTICAL STABILIZER LEADING EDGE APPROXIMATELY 8 INCHES ABOVE THE FUSELAGE. REPAIRED DENT IN VERTICAL STABILIZE R LEADING EDGE. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041800293 20010418 00293 NE 2001 4 18 TWAA0105301 2 20010322 A 7230 ENGINE BOEING 757 757231 1384950 NM PWA 2037 PW2037 NE RT ENGINE FAILED A TWAA A E UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 CE 05 721TW 29954 4941 DURING CLIMB CREW HEARD A LOUD BOOM AND THE RT ENG STARTED TO SPOOL DOWN. ENGINE WAS SHUT DOWN AND FLIGHT RETURNED TO S FO. THE ENGINE WAS CHANGED. CHECK-C 11-12-00 LAX. 2 L 7 2 4F 4 F RT A2NM E17NE 2001042300272 20010423 00272 NM 2001 4 23 DL764010566 1 20010405 A 7920 LINE BOEING 767 767432ER NM GE CF6 CF680C2B2 30025 NE NR 1 ENGINE FAILED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 834MH 29707 706203 NR 1 ENGINE OIL QTY DECREASED TO ZERO AND WITH OIL PRESSURE FLUX DECREASED TO 23 PSI PULLED ENG BACK TO IDLE AND DIVERTE D TO ABQ. ENGINE WAS SHUTDOWN ON THE GROUND WHEN OIL PRESSURE DROPPED TO 10 PSI. FOUND C SUMP SCAVENGE LINE DAMAGED BY BROKEN STARTER PIECES CAUSING OIL LEAKAGE. NR 1 ENGINE REPLACED C SUMP SEAVENGE LINE 1 ENGINE ASSISTED BY ATL ENG SHPER SONNEL. SERVICED ENGINE OIL TO FULL. OPERATED ENGINE. NO LEAKS OR OIL INDICATION DISCREPANCY NOTED. 2 L 7 2 4F 4 F RT A1NM E13NE 2001042400029 20010424 00029 SO 2001 4 24 SWIA972471 1 20010329 A 2731 922AA2YA6PZ722 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE ELEVATOR TRIM FAILED A SWIA K NONE J WARNING INDICATION NR NOT REPORTED 1 NM 07 207SW 120266 ELEVATOR TRIM AURAL WARNING CONTINUOUS IN OR OUT OF TRIM. REMOVED AND REPLACED LEFT ELEVATOR TRIM PROXIMITY SENSOR WITH NEW IAW EMB MM 27-32-00. P/N 922AA2Y-A6P-Z722. ADJUSTED AND OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042400279 20010424 00279 EA 2001 4 24 20010420CW002 2 20010329 A 8520 11F20022D3 CRANKCASE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA HARTZL HCC3Y HCC3YR2 NE LT ENGINE CRACKED E GSBA K NONE O OTHER IN INSP/MAINT 1 AL 01 31PR 317952049 R657861A DJ11082A REMOVED COWLINGS TO CHANGE/SERVICE ENGINES WITH OIL. FOUND LEFT ENGINE CASE CRACKED ABOVE NR 6, NR 4, AND NR 1 TAPPET H OUSING. ALL THREE CRACKS APPEARED TO BE PUSHED FROM INSIDE OUT. NONE WERE LEAKING OIL YET AND HAD NOT BEEN PRESENT 20 HOURS EARLIER. WHEN LAST WORK WAS DONE IN ENGINE COMPARTMENT. 1 L 7 2 3O 3 O A20SO E14EA 5 C P25EA 2001043000224 20010430 00224 NM 2001 4 30 2001UALA00532 1 20010417 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 BS STRINGER 35L TO 37L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WIT H BAC DRAWING 146T8511 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001050100004 20010501 00004 EU 2001 5 1 20010417CW009 1 20010129 A 2432 RETAINER AMD FALC50 FALCON50MYST 2730106 EU GARRTT TFE731 TFE731* 01518 WP BATTERY WRONG PART B JGVR K NONE O OTHER IN INSP/MAINT 1 CE 09 35RZ 113 UPON INSPECTION UNIT FOUND ALL 2 CELL RETAINERS LOOSE. REMOVED RETAINERS AND FOUND BATTERY CELLS TOO SHORT TO MAKE PROP ER CONTACE WITH BATTERY HOLDER TERMINALS. BATTERY CELL PART NUMBERS NOT FOUND. REPLACEMENT OF CELLS WITH PART NUMBER S PECIFIED IN MFG MANUALS. 2 L 7 3 4F 4 F A46EU E6WE 2001081300010 20010813 00010 2001 8 13 2001UALA00569 4 20010421 A 3416 20500801 ALTIMETER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE COCKPIT FLUCTUATES A UALA K NONE O OTHER CR CRUISE 1 WP 29 7270U 21417 CAPTAIN'S ALTIMETER FLUCTUATES INTERMITTENTLY -20 TO +40. SUPPLEMENTAL DATA UPDATE CAPTAIN'S ALTIMETER. REPLACE CAPTAIN' S ALTIMETER . OPS CHK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2001051100096 20010511 00096 NE 2001 5 11 SIMA20011074 2 20010417 A 7200 785650 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE FAILED A SIMA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 323AE 340B323 DFW - FLT 3677 - CREW REPORTED, THE RIGHT ENGINE CHIP LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE FOUND DEBRIS IN OIL FILT ER AND SCAVENGE SCREENS. RIGHT ENGINE WAS REMOVED AND REPLACED IAW AE WORK CARD 4903. OPS AND LEAK CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 2001051500337 20010515 00337 EA 2001 5 15 CA010503003 1 20010415 A 3242 266230 HOUSING DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE BRAKE ASSY CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 6273 4016 (CAN) DURING NDT INSPECTION, CRACKS WERE DISCOVERED IN 5 OUT OF 6 BORES OF THE BRAKE HOUSING. CRACKS WERE LOCATED ALONG THE RADIUS AT THE BOTTOM OF THE BORES. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001061800008 20010618 00008 NM 2001 6 18 2001UALA00596 1 20010428 A 3232 273N41714 ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT MLG WW FAILED A UALA K NONE K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 552UA 26641 AIRCRAFT ARRIVED AT GATE WITH RIGHT MLG WHEEL WELL DOOR IN OPEN POSITION AND A HYDRAULIC LEAK IN THE SAME WHEEL WELL. GEAR DOOR EICAS MESSAGE ILLUMINATED. *S/D* DOOR RELEASE INTERLOCK ACTUATOR FAILED. REPLACED ACTUATOR. 2 L 7 2 4F 4 F RT A2NM E17NE 2001071800016 20010718 00016 NE 2001 7 18 2001UALA00708 2 20010508 A 7261 ENGINE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 2 SHUTDOWN A UALA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 WP 29 925UA 26646 727426 NR 2 ENGINE SHUTDOWN DUE TO HIGH OIL TEMPERATURE. *S/D* REPLACED NR 2 ENGINE. 2 L 7 2 4F 4 F RT A16WE E2GL 2001060800026 20010608 00026 NM 2001 6 8 2001UALA00836 1 20010521 A 5320 WEB BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 AFT CARGO PIT BS 1329-1351, LBL 26 TO BL 0, SHEAR PANEL CORRODED ON UPPER SURFACE OF PANEL.UPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REPLACED WEB PER 146T5000-3 AND SRM 51-40-2. 2 L 7 2 4F 4 F RT A1NM E3NE 2001061300025 20010613 00025 EU 2001 6 13 C2XA01CL113 1 20010521 A 6130 FE1595007 PROP BRAKE AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE NR 2 ENGINE FAILED A C2XA O OTHER B K SMOKE/FUMES/ODORS/SPARKS FLUID LOSS TX TAXI/GRND HDL 1 SW 27 11835 23014 7718 194 120516 CLE FLIGHT 3147 THE CREW REPORTED SMOKE IN THE COCKPIT WHILE TAXIING. ALSO REPORTED NR 2 ENGINE FLUID LEAK. MAINTENANC E INSPECTED AND FOUND THE NR 2 ENGINE PROP BRAKE HAD PULLED AWAY FROM THE GEARBOX. THE HYDRAULIC LINE ON THE BRAKE WAS SHEARED AND THE GEARBOX WAS DAMAGED. THE NR 2 ENGINE WAS REPLACED ALONG WITH THE PROP BRAKE. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2001061500033 20010615 00033 2001 6 15 SWIA972596 4 20010522 A 3425 COMPARATOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE COCKPIT FAULTY A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 197SW 120186 UPON ADDING TAKEOFF POWER CAPT'S EADI AND EHSI FAILED AND CAME BACK ON LINE. AFTER 100 PERCENT TORQUE AND DOUBLE CHECK OF ALL INSTRUMENTS, TAKEOFF ROLL WAS COMMENCED AND ABORTED AFTER CAPT EHSI CHANGED HDG FROM 250 TO 270 DEGREES. INSTALL ED AND REORIENTED SERVICEABLE AHC-85 AND PERFORMED RUN UP TO 100 PERCENT TORQUE SEVERAL TIMES WITH NO ABNORMALITIES NOTE D. S/N ON 1336, S/N OFF 1726. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001062000035 20010620 00035 NE 2001 6 20 AALA20011101 2 20010511 A 7321 FFG021BH FUEL CONTROL BOEING 757 757223 1384957 NM RROYCE RB211 RB211535* NE RT ENGINE DEFECTIVE A AALA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 SW 21 679AN 29589 LAX - FLT 207 - EN ROUTE MIA-LAX, RIGHT ENGINE STAGNATION AT 35,000 FT FUEL FLOW 1.5 TO 1.7 MAX EGT 400. UNABLE TO CONT ROL EPR OR FUEL FLOW WITH THROTTLE MOVEMENT. LANDED LAX WITHOUT INCIDENT. REPLACED RIGHT ENGINE FUEL FLOW GOVERNOR. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2001071100042 20010711 00042 NM 2001 7 11 2001UALA00825 1 20010521 A 5320 CLIP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 STRINGER CLIP CRACKED AT STATION 434, STRINGER 38L. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP AS PER BAC DRAWING 141T1225 AND SRM 51-40-2. 2 L 7 2 4F 4 F RT A1NM E3NE 2001072600254 20010726 00254 NE 2001 7 26 ARWA0010717 2 20010711 A 7310 FILTER DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3B 52039 NE NR 3 ENGINE CLOGGED A ARWA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 SO 19 30UA 45888 645104 DURING FLIGHT AT LEVEL 31.0 NR 3 ENGINE FLAMED OUT, RESTARTED ENGINE FOLLOWING ABNORMAL CHECK LIST PROCEDURES. REMOVED AND REPLACED FUEL FILTERS OF NR 3 FUEL TEMPERATURE REGULATOR IAW MM 73-11-1, NO LEAKS NOTED. OPERATIONAL CHECK ON RUN U P IAW MM 71-00, FOUND NORMAL. NO DISCREPANCIES NOTED. 2 L 7 4 4F 4 F 4A25 1E8 2001081600117 20010816 00117 NM 2001 8 16 2001UALA01615 1 20010804 A 5312 PRESSURE PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 FWD EDGE OF AFT PRESSURE DECK CORRODED STA 1681 LBL 3.5 TO LBL 14.5 AREA IS APPROX 2.55 INCH X 10.7 INCH WL 208.1. *S/D * MAJOR REPAIR ACCOMPLISHED. DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2001081600134 20010816 00134 NE 2001 8 16 2001UALA01650 2 20010807 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 STALLED A UALA K NONE R PARTIAL RPM/PWR LOSS IN INSP/MAINT 1 WP 29 584UA 26706 NR 1 ENG STALLED DURING DECELERATION TEST AFTER FMU REPLACEMENT. STABLIZED AT IDLE FOR 10 MIN. ENG STALLED ON SECOND A TTEMPT AT APPROX 80 PERCENT N1 ON DECELERATION. 2 L 7 2 4F 4 F RT A2NM E17NE 2001082900224 20010829 00224 2001 8 29 VNAA0108006 4 20010813 A 3445 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 459PS 3070 DURING THE TAKEOFF ROLL, THE CREW RECEIVED A TCAS FAIL MESSAGE. THE CREW ABORTED TAKEOFF AND WHILE EXITING THE RUNWAY T HE MESSAGE CLEARED. FLIGHT 4092 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001090700080 20010907 00080 NM 2001 9 7 2001UALA01834 1 20010826 A 5312 PRESSURE PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 330UA 24191 STATION 178 LEFT HAND FLOOR WEB CRACKED WL 207 STRINGER 17L. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2001090700113 20010907 00113 NM 2001 9 7 2001UALA01873 1 20010828 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 STATION 1219 STRINGER 37R-38R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091900235 20010919 00235 NE 2001 9 19 MALA010699 2 20010916 A 7320 230349306 ECU BAC 146 AVRO146RJ85A 1500097 EU LF507 LF5071F NE A MALA E ENGINE SHUTDOWN J WARNING INDICATION LD LANDING 1 GL 15 518XJ E2337 During descent on Flight #3531, #3 Engine was in a sub-idle Power setting into DTW. 15% N1, 45% N2, Oil Pressure 35 PSI , after Landing EGT started to climb past 560. Crew shutdown Engine.Maintenance replaced #3 Engine ECU IAW RJ85 AMM Ch7 3-20. PN 2-303-493-06, SN OALG815. 2 H 7 4 4F 4 F RT A49EU E6NE 2001092400032 20010924 00032 NE 2001 9 24 01FDEA00853 2 20010920 A 7311 OIL COOLER DOUG MD11 MD11 3023602 NM GE CF6 CF680C2D1F 30025 NE NR 1 ENGINE LEAKING A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 584FE 48436 NR 1 ENG OIL QTY DROPPED 10 GAL. REMOVED AND REPLACED FUEL/OIL COOLER AND DRAINED AND FLUSHED ENGINE. 2 L 7 3 4F 4 F RT A22WE E31N3 2001092400180 20010924 00180 EU 2001 9 24 OLJ2001F00001 1 20010812 A 2917 704A37721034 PRESSURE SWITCH AEROSP SA365 SA365N1 8680668 EU TMECA ARRIEL ARRIEL1C 60030 NE HYD PRESSURE INOPERATIVE A OLJA K NONE O OTHER IN INSP/MAINT 1 EA 13 65CW 6262 5017 AUX HYDRAULIC ILLUMINATED DURING CRUISE FLIGHT. PILOT PERFORMED A PRECAUTIONARY LANDING. MAINTENANCE WAS DISPATCHED TO THE SITE. MAINTENANCE FOUND PRESSURE SWITCH INOPERATIVE. THE SWITCH WAS REMOVED AND REPLACED AND THE SYSTEM WAS OPERA TIONAL TESTED AND AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 2 3U 3 U H10EU E19EU 2001100100063 20011001 00063 SW 2001 10 1 B1HR719229 1 20010717 A 6420 406012102109 YOKE BELL 407 407 SW ALLSN 250C 250C47B GL TAIL ROTOR OUT OF TOLERANCE B B1HR K NONE O OTHER IN INSP/MAINT 1 SW 19 407AM 1495 53309 DURING REPAIR OF TAIL ROTOR YOKE, BEARING BORES WERE FOUND TO BE OUT OF ACCEPTABLE LIMITS. YOKE WAS REMOVED AND REPLACE D. 1 G 7 1 3U 3 U O H2SW E1GL 2001110500043 20011105 00043 EU 2001 11 5 AOQ2001F00000 1 20010115 A 2110 CLAMP BRAERO DH125 HS125700A 4230170 EU GARRTT TFE731 TFE731* 01518 WP CABIN PRESSURE LOOSE E AOQA G A O2 MASK DEPLOYED UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 11 53GH NA0314 AIRCRAFT WAS IN CRUISE AT FL 35000, WHEN CREW NOTICED THAT THE AIRCRAFT BEGAN TO GRADUALLY DEPRESSURIZE. THE CREW ELECT ED TO DESCEND TO A LOWER ALTITUDE. DURING DESCENT CABIN PRESSURE DROP CAUSED THE AURAL WARNING HORN TO SOUND AND PAX OX YGEN MASKS TO DEPLOY. CREW THEN DECLARED AN EMERGENCY AND DIVERTED TO BUF INTERNATIONAL AIRCRAFT MADE NORMAL LANDING. AIRCRAFT WAS INSPECTED AND FOUND CLAMPS SECURING MAIN CABIN AIR SUPPLY TUBE FLEX COUPLINGS HAD LOOSENED CAUSING LEAKAGE AND SUBSEQUENT LOSS OF PRESSURIZATION SYSTEM EFFICIENCY. ALL COUPLINGS CLAMPS SECURED A ACCOMPLISHED SYSTEM TEST. CHEC KED OK. 2 L 7 2 4F 4 F A3EU E6WE 2001110800064 20011108 00064 NM 2001 11 8 2001UALA02166 1 20011025 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 336UA 24240 FORWARD CABIN STATION 291.5 FUSELAGE FRAME HAS EXCESSIVE MATERIAL LOSS IN RADIUS BETWEEN STRINGER 7 & 8 RIGHT. MAJOR REP AIR ACCOMPLISHED. CUT OUT DAMAGE. MANUFACTURED REPAIR ANGLE AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001112800064 20011128 00064 NE 2001 11 28 USAASB01296 2 20011013 A 7532 3017767040 BLEED VALVE BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE NR 2 ENGINE FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 383US 38898 22956 CLE - FLT 1204 - ON CLIMB-OUT FROM CLE, AT 500 FEET ABOVE GROUND LEVEL, THE AUTO THROTTLE KICKED OFF AND THE NR 2 ENGINE THRUST WENT TO FIREWALL. THE NR 2 ENGINE N2 INDICATED 100 PERCENT AND THE N1 WAS AT LEAST 10 PERCENT LESS THAN NR 1 EN GINE N1. FLIGHT RETURNED TO FIELD TO CLE. ON DOWNWIND LEVEL FLIGHT, ALL ENGINE INDICATIONS WERE NORMAL BUT ON FINAL AP PROACH THE NR 2 ENGINE BEGAN POWER FLUCTUATING WITH AUTO THROTTLE OFF. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMER GENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE VARIABLE BLEED VALVE FUEL GEAR MOTOR PER MM 75-32- 02. OPS CHECK AND LEAK CHECK GOOD. OPERATED BOTH ENGINES AT POWER. ALL PARAMETERS NORMAL AND MATCHED. (M) 2 L 7 2 4F 4 F RT A16WE E2GL 2001121300018 20011213 00018 EU 2001 12 13 MTN2001F00000 1 20010914 A 7931 CV3450KT245SNK CONNECTOR FOKKER F27 F27MK500 4990629 EU RROYCE DART DART532* EU OIL PRESS IND LOOSE A MTNA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 33 718FE 10470 DURING CLIMB OUT FROM SGF. THE LEFT OIL PRESSURE GAUGE DROPPED TO ZERO THEN FLUCTUATED BETWEEN ZERO AND FIVE PSI. THE C REW PERFORMED THE EMERGENCY SHUT DOWN CHECK LIST. AFTER DECLARING AN EMERGENCY THEY RETURNED TO SGF AND LANDED WITHOUT INCIDENT. 2 H 7 2 4T 4 T A817 E297 2001121700011 20011217 00011 CE 2001 12 17 JJB2001F00006 1 20011128 A 5270 V3101D8 SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA CABIN DOOR OUT OF ADJ A JJBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 01 856CA 1100 UE405 CABIN DOOR ANNUNCIATOR ILLUMINATED DURING TAKEOFF ROLL. DOOR AJAR ANNUNCIATOR SWITCH OUT OF POSITION. ADJUSTED DOOR AJ AR SWITCH. CHECKED SATISFACTORY. 2 L 7 2 4T 3 T RT A24CE E2NE 2001121800030 20011218 00030 EU 2001 12 18 2001UALA02359 1 20011202 A 3397 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 431UA 571 EMERGENCY EXIT LIGHTS ON LAST 3 ROWS OF SEATS ARE INOP. RESECURED WIRES AT SEATS 24C AND 26C. LIGHTS OPERATIONAL CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2002011000146 20020110 00146 NM 2002 1 10 2001UALA02404 1 20011212 A 5315 FLOORBEAM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 181UA 25278 STATION 1700 FLOORBEAM UPPER CHORD HAS EXCESSIVE MATERIAL AT RBL 44. ANGLES AND STIFFENERS ANGLES INSTALLED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002010300129 20020103 00129 NM 2002 1 3 2001UALA02443 1 20011223 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 354UA 24360 BS 178 BULKHEAD WEB, LBL 5.7, WL 211 HAS CRACKS. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLERS AND FILL ER MATERIAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2002010800023 20020108 00023 EU 2002 1 8 AUS20010985 1 20010902 A 2510 2510144NP LOCKPIN AIRBUS 320 A320* EU CFMINT CFM56 CFM565A1 NE COCKPIT WORN W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) CAPTAINS SEAT VERTICAL ADJUSTMENT MECHANISM LOCK PIN WORN INLOCKING BALL SPIRAL GROOVE. 2 L 7 2 4F 4 F RT A46NM E29NE 2002010900087 20020109 00087 CE 2002 1 9 2001F00764 1 20011207 A 7810 NH100089770 CLAMP CESSNA 340 340A 2076405 CE CONT O520 TSIO520NB 17040 SO EXHAUST SYS CRACKED B BIGA K NONE O OTHER IN INSP/MAINT 1 NM 04 118BH 45 340A0003 NEW AEROQUIP EXHAUST CLAMPS ARE CRACKING AROUND OUTER PERIPHERY. APPEAR TO BE MANUFACTURING DEFECTS. 1 L 7 2 3O 3 O 3A25 E8CE 2002011500163 20020115 00163 EU 2002 1 15 CA011019011 1 20011010 A 3222 F3225000700060 AXLE AIRBUS 330 A330323 3930335 EU RROYCE RB211 RB211TRENT77 NE NLG WHEEL CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) UPON REPLACING THE LT NOSE WHEEL ASSEMBLY, A RADIAL CRACK WAS FOUND ON THE AXLE SLEEVE. 2 L 7 2 4F 4 F RT A46NM E39NE 2002011500186 20020115 00186 NM 2002 1 15 VNAA0112001 1 20011201 A 3250 CONTROL UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NLG MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 436JS 3052 PULLING OFF THE GATE, THE NOSE WHEEL STEERING FAILED. AS SOON AS THE WHEEL WAS STRAIGHTENED THE FAIL LIGHT WENT OUT. A S FLIGHT 4106 TOOK THE RUNWAY THE NOSE WHEEL STEERING FAILED AGAIN. THE CREW CLEARED THE RUNWAY AND PERFORMED SEVERAL T URNS BUT COULD NOT DUPLICATE THE PROBLEM. FLIGHT 4106 WAS THEN CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4106 THEN D EPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002011600134 20020116 00134 CE 2002 1 16 CA011101019 1 20011016 A 7931 BEARING RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP STARTER GEN VIBRATION W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING FLIGHT ON CLIMB A VIBRATION WAS NOTED. THEN DISAPPEARED AFTER WHILE ON CRUISE VIBRATION CAME BACK. ALSO GIV ING OIL PRESSURE FLUCTUATION. AT DESTINATION, TROUBLESHOOTING WAS DONE, OIL PRESSURE WAS CHECKED "S". STARTER/GENERATOR REPLACED. VIBRATION DISAPPEARED AND OIL PRESSURE BACK TO NORMAL. 2 L 7 2 4F 4 F RT A3EU E6WE 2002011800059 20020118 00059 GL 2002 1 18 PN12002F00000 2 20011207 A 7240 6870992 COMBUST CHAMBER BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL ENGINE CRACKED A PN1R K NONE O OTHER IN INSP/MAINT 1 EA 17 193P 2985 CAE832776 DURING AIRCRAFT 100 HOUR INSPECTION FOUND THE RIGHT ARMPIT OF THE COMBUSTION CAN CRACKED. 1 G 7 1 3U 3 U H2SW E4CE 2002012900099 20020129 00099 NE 2002 1 29 R7MR34346 2 20010716 A 7250 L621M1006103 SEAL UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE ENGINE WORN B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 135N 259 0086 145MM SEAL ASSEMBLY, WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2002020500118 20020205 00118 NM 2002 2 5 CA011001006 1 20010921 A 7921 28E997 OIL COOLER HONEYWELL DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE ENGINE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 118 (CAN) NR 2 ENGINE OIL COOLER WAS FOUND TO BE LEAKING FROM THE WELDED AREA AROUND THE DRAIN. RETURNED FOR WARRANTY REPAIR . 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002040200033 20020402 00033 NM 2002 4 2 TX22002F00000 1 20011227 A 5530 106188411 BEARING BOEING BOEING 727 72722 1384002 NM PWA JT8 JT8D1 52044 NE HINGE FAILED E TX2R K NONE O OTHER IN INSP/MAINT 1 SW 05 400RG 19149 DURING REMOVAL OF THE HORIZONTAL STABILIZER HINGE PINS TO COMPLY WITH THE AD AND SB. FOUND RIGHT HINGE BEARING TO HAVE FAILED WITH PIECES MISSING. LEFT BEARING WAS CRACKED. DURING FURTHER INSPECTION FOUND NUMEROUS BUSHINGS AND ATTACH HAR DWARE IN THE HORIZONTAL STABILIZER TENSION TIE TO HAVE EXCESSIVE WEAR. A CLOSE VISUAL INSPECTION OF HINGE BEARING DURIN G PIN INSPECTION. 2 L 7 3 4F 4 F A3WE E2EA 2002052400083 20020524 00083 NE 2002 5 24 USAASB01317 2 20011119 A 7200 ENGINE BOEING 737 737201 1384454 NM PWA JT8 JT8D15A 52051 NE RIGHT FAILED A USAA A UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 EA 19 262AU 44166 22868 709096 MIA-BWI - FLT 2738 - DURING CRUISE, THE FLIGHT CREW HEARD A LOUD BANG AND THE AIRCRAFT YAWED. THE RIGHT ENGINE N1 AND N 2 DIMINISHED AND THE EGT CLIMBED ABOVE THE RED LINE. THE ENGINE SPOOLED DOWN AS THE CREW INITIATED SHUTDOWN PROCEDURES. A PASSENGER REPORTED SPARKS OUT THE TAILPIPE. THE AIRCRAFT DIVERTED TO CLT AND LANDED WITHOUT INCIDENT. 19 MINUTES S INGLE ENGINE TIME. MAINTENANCE REPLACED THE ENGINE. THIS ENGINE HAS BEEN SOLD IN AN 'AS IS' CONDITION TO JETRAN, AND I S NO LONG ON US AIRWAYS OPSPEC. (M) 2 L 7 2 4F 4 F A16WE E2EA 2001040400167 20010404 00167 NM 2001 4 4 01FDEA00177 1 20010307 A 3260 656021132 ACCESSORY UNIT BOEING 727 727225 1384077 NM EE BAY FALSE INDICATION A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 463FE 22551 WHILE RAISING THE GEAR THE LEFT GEAR RED LIGHT STAY ILLUM. DID PROC AND LIGHT REMAIN ON. CONT FLT IN ACCORD WITH FLT M ANUAL. CLEAN UPLOCK PROXIMITY SENSOR AND SENSOR TARGET. PERF LAND GEAR ASSY UNIT FUNCTION TEST PER MM 32-09-122-5. AL L STEPS PASSED. REMOVED AND REPLACED LG ASSY UNIT PER MM 32-09-121-4. PERF GEAR SWING PER MM 32-32-000-5. OPS NORM PE R MM 32-61-001-5. 2 L 7 3 4F A3WE 2002013100023 20020131 00023 NM 2002 1 31 USAA011403 1 20011222 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 TPA - FOUND SKIN GOUGED 3 INCHES, STRINGER 24R AT STATION 990 AFT OF OUTFLOW VALVE. INSTALLED DOUBLER PER SRM 53-00-01 FIG 201. (M) 2 L 7 2 4F RT A16WE 2001021300363 20010213 00363 WP 2001 2 13 UPS01834783 1 20010123 A 5730 576958927 DOUBLER DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C1&3, RIGHT WING CENTER L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 335. 250. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769589, AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2001111500012 20011115 00012 NM 2001 11 15 01FDEA00974 1 20011110 A 2782 652E08 ACTUATOR BOEING 727 7272S2F 1384O81 NM L/E FLAP FAILED A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 206FE 22928 ON DEPARTURE RETRACTING FLAPS ON RIGHT WOULD NOT RETRACT. REMOVED AND REPLACED NR 6 KRUEGER FLAP ACTUATOR PER MM 27-81- 022-4. 2 L 7 3 4F A3WE 2001121300052 20011213 00052 WP 2001 12 13 AALA20011846 1 20011006 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 298AA 49310 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 31D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2001070200193 20010702 00193 NM 2001 7 2 SWAA011698 1 20010611 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 500D, STR 6R & BS 559, STR 11R. REPAIRED STR CLIPS PER SRM . 2 L 7 2 4F RT A16WE 2001060700193 20010607 00193 EU 2001 6 7 USAABA01003 1 20010430 A 3350 32146220 POWER SUPPLY AIRBUS 330 A330323 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 671UW 323 PHL - FOUND THE EMERGENCY POWER SUPPLY UNIT AT DOOR 3L INOPERATIVE. MAINTENANCE REPLACED THE EPSU. (M) 2 L 7 2 4F RT A46NM 2001103100108 20011031 00108 EU 2001 10 31 AWXA200100563 1 20011029 A 3230 E0242A28A0 RELAY AIRBUS 320 A320231 3930325 EU FAILED A AWXA L ABORTED APPROACH S AFFECT SYSTEMS LD LANDING 1 WP 28 637AW 099 Landing gear failed to extend when commanded. Crew used manual extension system and landed without further problems. ge ar swing and trouble shooting per 32-31-00-810 indicated the hydraulic relay 48GA bad. Replaced relay and functional tes ted per task 31-31-00-720, system tested normal. 2 L 7 2 4F RT A28NM 2001072600183 20010726 00183 NM 2001 7 26 2001UALA01313 1 20010630 A 2751 FLAP BOEING 767 767222 1385122 NM WING MALFUNCTIONED A UALA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 WP 29 605UA 21866 FLAP DISAGREE ON SHORT FINAL. DIVERT ONT 2 L 7 2 4F RT A1NM 2001110700121 20011107 00121 NM 2001 11 7 01FDEA00929 1 20011026 A 5330 SKIN BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 279FE 22346 CRACK IND IN EXTERNAL FUSE SKIN AFT I/B CORNER. REMOVED AND REPLACED SKIN PER DWG SR 27-53-024 & EA. 2 L 7 3 4F RT A3WE 2001071800110 20010718 00110 NM 2001 7 18 2001UALA01037 1 20010509 A 5320 SPLICE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 347 RBL5 STRINGER CLIP CORRODED. 2 L 7 2 4F RT A1NM 2001123100080 20011231 00080 WP 2001 12 31 P2EA2001M0015 1 20011210 A 3250 LEVER DOUG DC9 DC981 3022081 WP NLG LOOSE A P2EA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 05 814US 48094 DURING TAXI FOR TAKEOFF LOUD GRINDING WAS HEARD FROM NOSE WHEEL AREA. FOUND NOSE WHEEL STEERING CONTROL LEVER LOOSE. T ORQUED LEVER IAW MM 32-52-00. TAXIED AIRCRAFT WITH NO DEFECTS NOTED. 2 L 7 2 4F A6WE 2001072400108 20010724 00108 NM 2001 7 24 2001UALA01072 1 20010615 A 5320 SPLICE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 615UA 21876 FWD CARGO PIT AT BS 434 STRINGER 32L, SPLICE FITTING IS CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED NEW SPLICE PER BAC DRAWING 140T0115 AND INSTALLED PER SRM 51-40-2. 2 L 7 2 4F RT A1NM 2001070200121 20010702 00121 NM 2001 7 2 01FDEA00510 1 20010629 A 3260 65293241 DUCT BOEING 727 727233 138408A NM E&E COMPARTMENT MISSING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 269FE 21675 01-214 WHILE CHECKING RUDDER CONTROLS NOSE GEAR VIEWING TUBE SECTION MISSING. INSTALL NEW VIEWING TUBE. FUNCIONAL CK GOO D PER B727-200 MM 56-40-000-0. AC OK FOR SERVICE. 2 L 7 3 4F RT A3WE 2001082700058 20010827 00058 WP 2001 8 27 RRXA003596 1 20010103 A 5710 FASTENER DOUG DC8 DC873F 302199F WP RT WING MISSING A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT FOUND MISSING FASTENER ON THE RT UPPER WING THRU ACCESS HOLE 505C & THROUGH MID SPAR ACCESS H OLE 560C INSIDE TANK I/B BETWEEN STA 252 & 255, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW EO 00-316 WITH APPROVED 8110-3 DATED 01/02/01. 2 L 7 4 4F RT 4A25 2001121100083 20011211 00083 SO 2001 12 11 SIMA200132405 1 20011120 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 602AE 145048 ABI - DURING MBV INSPECTION, FOUND CORROSION ON THE FORWARD DIGITAL. REMOVED CORROSION BY BLENDING OUT. PERFORMED AN N DT INSPECTION OF THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW EMB GST 3664/01 PARA 1 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2001060100157 20010601 00157 NM 2001 6 1 01FDEA00333 1 20010507 A 5754 RIB BOEING 727 72722 1384002 NM SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 DURING ROUTINE INSP NR2 SLAT RIB AT SLAT BS 347 FOUND CRACKED. *S/D* REMOVED AND REPLACED PER IAW BAC 727 MM 27-81-011 . 2 L 7 3 4F A3WE 2001032600059 20010326 00059 NM 2001 3 26 AWXA0001428 1 20010301 A 5320 654583340 WEB BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 FLOOR WEB ON AFT SIDE OF FS 178 BLKHD SIDE CHORD AREA CRACKED. REPAIRED FLOOR WEB IAW SRM 53-20-04 PG 1-7, SRM 51-30-01 PG 2, 3, 5, 32, SRM 51-10-03 PG 1-10, SRM 51-10-01 PG 20-24 AND B737-200 MM 51-21-41 PG 702-706. 2 L 7 2 4F RT A16WE 2001072400258 20010724 00258 NM 2001 7 24 2001UALA01157 1 20010621 A 5347 SEAT TRACK BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 1249 LBL 11 SEAT TRACK CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 53-00-52 AND 51-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001072600119 20010726 00119 NM 2001 7 26 2001UALA01292 1 20010629 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 AFT PIT BS 1307, RBL 1, T-CAP UPPER FLANGE GOUGED. 2 L 7 2 4F RT A1NM 2001042500347 20010425 00347 NM 2001 4 25 USAA010284 1 20010222 A 5320 INTERCOSTAL BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 51562 22203 CLT - FOUND INTERCOSTAL CRACKED 1 INCH, STATION 1420 AND STATION 1440 BL 0. INSTALLED NEW WEB FILLER. (M) 2 L 7 2 4F RT A2NM 2001021300284 20010213 00284 SO 2001 2 13 SWIA972301 1 20010126 A 3260 HARNESS EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT MLG DAMAGED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 212SW 120276 LEFT MAIN GEAR INDICATION LIGHT (A) WOULD NOT EXTINGUISH. RECYCLED GEAR BUT UNABLE TO GET A THREE GREEN INDICAITON. GE AR WOULD NOT DROP UNTIL ELECTRICALLY OVERRODE LANDING GEAR. RETURNED TO SLC. REMOVED AND REPLACED LEFT MAIN LANDING GE AR A-HARNESS IAW MM 32-61-01. OPS CHECKS GOOD. P/N ON: 120-41127-001 2 L 7 2 4T 4 T RT A31SO E20NE 2001031300186 20010313 00186 NM 2001 3 13 VNAA0102005 1 20010209 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN FAILED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 461PS 13077 3075 THE CREW REPORTED THAT ROW THREE''S EMERGENCY FLOOR LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001032700368 20010327 00368 2001 3 27 SWIA972415 4 20010228 A 3442 RADAR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FUSELAGE INOPERATIVE A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 221SW 120290 WEATHER RADAR INOP, PAINTS ONLY SPOKES OF GREEN. DIVERTED FROM BFL TO SFO. REPLACED WXT 250B RADAR TRANSCEIVER. OPS C HECK GOOD. P/N: 622-7337-001, S/N ON: 624, S/N OFF: 4550. 2 L 7 2 4T 4 T RT A31SO E20NE 2001040500163 20010405 00163 EU 2001 4 5 CA010314012 1 20010226 A 2750 9787320002R POWER UNIT PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL TE FLAPS FAILED W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA 983 1 (CAN) WHEN TRYING TO EXTEND THE FLAPS FROM ZERO TO 15 DEGREES AT -29 DEGREES C (UNDER THE FLOOR) THEY WOULD NOT EXTEND. THE POWER DRIVE UNIT WAS REPLACED. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001040900335 20010409 00335 CE 2001 4 9 20010403CW005 1 20010209 A 2710 CONTROL CABLE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE AILERONS CHAFED B K NONE O OTHER IN INSP/MAINT 1 SO 15 66U 5600489 DURING INSPECTION FOUND THAT WHEN CONTROL COLUMN IS PULLED BACK AND AILERONS ARE OPERATED, THE BALLANCE CABLE ON CONTROL COLUMNS ARE RUBBING INTO LANDING GEAR UP HYDRAULIC LINE. LOCATION-UNDER COPILOTS FLOOR PANEL. PROLONGED USE LIKE THIS CAN CAUSE HYDRAULIC LINE FAILURE AND LOSS OF FLUID. MUST REFORM HYDRAULIC LINE FOR CLEARANCE. 2 L 7 2 4F 4 F RT A22CE E25EA 2001041100080 20010411 00080 NM 2001 4 11 2001UALA00202 1 20010225 A 3210 LINK BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE LANDING GEAR MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 667UA 29239 WHILE PREPARING FOR GEAR SWING FOUND UPLOCK STABILIZER LINK MISSING. 2 L 7 2 4F 4 F RT A1NM E24NE 2001041100187 20010411 00187 EU 2001 4 11 2001UALA00098 1 20010212 A 2130 VFT300B00 VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN PRESSURE FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 461UA * 1266 UNABLE TO MAINTAIN CABIN PRESSURIZATION. *S/D* THE SKIN AIR VALVE WAS REPLACED. NO FURTHER DISCREPANCIES REPORTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2001041600325 20010416 00325 NM 2001 4 16 2001UALA00364 1 20010329 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 AFT PIT FRAME CORRODED AT STA 787 RBL 20. REPAIRED AFFECTED FRAME. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041800400 20010418 00400 GL 2001 4 18 C2XA2001BT039 2 20010321 A 7200 23072309 SEAL EMB 145 EMB145ER SO ALLSN AE300 AE3007A GL NR 1 ENGINE LEAKING A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 15932 6164 6164 145015 CAE311015 CREW REPORTED, LAV SMOKE WARNINGS ON TAKEOFF. NO VISIBLE SMOKE OR SMELL. EWR MAINTENANCE INSPECTED AIRCRAFT TROUBLESHO T NR 1 ENGINE CARBON SEAL LEAKING AIRCRAFT MAINTENANCE FERRIED TO BTV FOR ENGINE SEAL REMOVAL AND REPLACE. FOR COMPANY CONVENIENCE, NR 1 ENGINE REMOVED AND REPLACED IAW TASK CARD 6271001. ALL OPERATIONAL AND LEAK CHECKS COMPLETED. AIRCRA FT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001042300267 20010423 00267 NM 2001 4 23 DL78K010561 1 20010405 A 7931 CFM567 HELICOIL BOEING 737 737832 13844CF NM GE CFM56 CFM567B24 NE NR 1 ENGINE LOOSE A DALA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 3738B 493 493 30382 888152 DURING CLIMBOUT NR 1 ENGINE OIL PRESSURE INDICATED ZERO, BUT NO OIL PRESSURE ALERT. ENGINE WAS SHUTDOWN AFTER 2 - 3 MINUTES. MAINT FOUND OIL TEMP BULB PULLED OUT OF ITS HOUSING BECAUSE HELIO-COILS PULLED OUT. ENGINE CHANGED. 2 L 7 2 4F 4 F RT A16WE E00055EN 2001042300313 20010423 00313 NM 2001 4 23 DLM88010614 1 20010414 A 7930 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 MALFUNCTIONED A DALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SO 27 918DL 22014 49583 726933 AT FL 370 WITH ENGINE ANTI-ICE SELECTED THE MASTER CAUTION LITE ILLUMINATED FOLLOWED BY THE RIGHT ENGINE OIL STRAINER CL OG LITE. ACCOMPLISHED POM PROCEDURES AND AFTER THROTLE WAS RETARDED THE LITE REMAINED ILLUMINATED CONTINUOUSLY. ENGINE W AS SHUTDOWN IAW POM. REPLACED ENGINE OIL STRAINER 2 L 7 2 4F 4 F RT A6WE E9NE 2001042300354 20010423 00354 SW 2001 4 23 20010420CW017 1 20010313 A 8000 SM20ACD20A21 RELAY BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL STARTER BURNED B ALGR O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 SW 03 3186P 45776 CAE86034S DURING ATTEMPT AT FIRST START. SPIKE IN COCKPIT STARTER RELAY (BEHIND HAT RACK) BURNED STARTER BUTTON, ALSO FOUND INTER MITTENT. 1 G 7 1 3U 3 U H2SW E1GL 2001050900011 20010509 00011 2001 5 9 VNAA0104011 4 20010417 A 3140 7013348918 DAU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE E/E BAY MALFUNCTIONED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 431JS 1190 3028 DURING CLIMBOUT, THE CREW RECEIVED A DAU NR 2 FAIL CAS MESSAGE. THE CREW CONTACTED MAINTENANCE CONTROL WHO INSTRUCTED T HE THE CREW TO RETURN TO PIT. FLIGHT 4136 RETURNED TO PIT WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED AND REPLAC ED THE NR 2 DAU IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRC RAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001051500103 20010515 00103 NE 2001 5 15 MALA010432 2 20010428 A 7320 HMA BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 2 ENGINE DEFECTIVE A MALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 15 510XJ E2325 ENGINE NR 2 NX REMAINED AT 43 PERCENT WHILE SEAT AT GROUND IDLE (FADEC NR 2 INOP. RETURNED TO GATE. MAINTENANCE REPLAC ED NR 2 ENGINE HMA IAW TASK CARD NR 7310-502. ALL SEC CHECKS GOOD AT THIS TIME. REQUIRES OPS CHECK. RAN ENGINE IAW AM M 72-00-00. OPS CHECK GOOD. 2 H 7 4 4F 4 F RT A49EU E6NE 2001052100043 20010521 00043 NM 2001 5 21 2001UALA00617 1 20010429 A 5311 FRAME BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7456U 21910 FUSELAGE FRAME AT BS 420 IS CRACKED ALONG THE RADIUS BETWEEN STRINGER 20R AND 21R.. INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3 AND 53-10-2 DUE TO SKIN CRACKING 2 L 7 3 4F 4 F A3WE E2EA 2001052100053 20010521 00053 NM 2001 5 21 2001UALA00630 1 20010504 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 FUSELAGE CREASE BEAM AND WEB CORRODED AT STA 934 STR 17L. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB AND REPAIRED CREASE B EAM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001071800011 20010718 00011 NM 2001 7 18 2001UALA00652 1 20010506 A 5620 6556705 WINDOW BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN CRACKED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 7273U 21420 DURING CRUISE PASSENGER OUTER WINDOW PANE AT ROW 17 SHATTERED. AIRCRAFT DIVERTED TO SFO. *S/D* AN IMPROPER SEAL DURIN G INSTALLATION RESULTED IN FAILURE OF OUTER PANE. REPLACED ROW 17A OUTER AND MIDDLE WINDOW PANES PER MAINTENANCE MANUAL AND BOEING DRAWING 65-54560. 2 L 7 3 4F 4 F A3WE E2EA 2001052100100 20010521 00100 NM 2001 5 21 2001UALA00694 1 20010509 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 REPAIRED FRAME AT STA 188, WL 207. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001060600023 20010606 00023 NM 2001 6 6 2001UALA00715 1 20010511 A 5312 BULKHEAD BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 974UA 21597 BULKHEAD CRACKED AT RIVET HOLE STA 178, WL 234, LBL 18.1. MAJOR REPAIR ACCOMPLISHED. INSTALLED SKIN DOUBLER. 2 L 7 2 4F 4 F A16WE E2EA 2001060600049 20010606 00049 NM 2001 6 6 2001UALA00750 1 20010511 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 AFT PIT BODY FRAME INNER CAP GOUGED STA 727E STR 19L. MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW CAP SECTION. 2 L 7 2 4F 4 F RT A16WE E2GL 2001061800065 20010618 00065 NM 2001 6 18 2001UALA00789 1 20010521 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 STRINGER 38R CRACKED AT THE END UNDER FRAME STA 456 RT. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPAIRED STR INGER PER SRM 53-00-03 AND 51-40-2. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071600077 20010716 00077 NE 2001 7 16 MASA01036 2 20010410 A 7261 SCAVENGE PUMP CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE NR 3 ENGINE DEFECTIVE A MASA E A ENGINE SHUTDOWN UNSCHED LANDING M OVER TEMP CR CRUISE 1 SW 07 37178 7178 FLT 6009 - PHX-DSM - DIVERTED TO ABQ AFTER CAPTAIN PERFORMED AN INFLIGHT SHUT DOWN OF THE NR 2 ENGINE. THE OIL PRESSURE WENT DOWN TO 15 PSI AND THE OIL TEMP INCREASED 26 DEG CELSIUS TO 144 DEG CELSIUS. INCREASING POWER AND RETARDING POWER TO IDLE HAD NO AFFECT ON THE LOW OIL PRESSURE. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE OIL SCAVENGE PUMP, B-SUMP REGULATOR VALVE AND THE OIL TANK CAP. OP CHECKS GOOD ON TEST FLIGHT. THE AIRCRA FT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2001073100273 20010731 00273 EU 2001 7 31 CA010629035 1 20010605 A 2742 9787314203 ACTUATOR PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL STAB TRIM FAILED W O OTHER F FLT CONT AFFECTED CR CRUISE 1 CA 4748 4748 (CAN) IN CRUISE THE CREW NOTICED THAT THE STAB TRIM WAS INOPERATIVE IN NOSE DOWN MODE. FURTHER TROUBLE SHOOTING AFTER LA NDING CONFIRMED THE ACTUATOR FAILED INTERNALLY. LOUD GRATING NOISE WHEN TRIMED IN THE NOSE DOWN DIRECTION. ACTUATOR REPL ACED AND AIRCRAFT RETURNED TO SERVICE. FURTHER INVESTIGATION OF OTHER ACTUATORS IN THE FLEET SHOWED AN AVERAGE RELIABILI TY OF 47 PERCENT TO TBO. THIS ACTUATOR WAS THE HIGHEST TIME ACTUATOR IN OUR HISTORY. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001080100064 20010801 00064 NM 2001 8 1 CA010712004 1 20010624 A 2910 82970010391 TUBE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM LEAKING W O OTHER K FLUID LOSS CR CRUISE 1 CA 33488 (CAN) THE FLIGHT CREW REPORTED A DECREASE IN THE #2 HYDRAULIC SYSTEM DURING FLIGHT. MAINTENANCE NOTICED HYDRAULIC FLUID LEAKING FROM THE LEFT NACELLE AREA. UPON FURTHER INVESTIGATION, THE "DOOR CLOSED" TUBECONNECTED TO THE LEFT MLG DOOR SOL ENOID SEQUENCE VALVE WAS FOUND TO HAVE A PIN HOLE LEAK. THE LINE WAS REPLACED AND ALL FURTHER CHECKS COMPLETED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001080200062 20010802 00062 CE 2001 8 2 N3X2001F00000 1 20010712 A 2730 05341221 BELLCRANK CESSNA 172 172R 2072401 CE LYC O360 IO360A1C 41514 EA ELEVATOR LOOSE B N3XR K NONE O OTHER IN INSP/MAINT 1 SO 15 443ER 2731 17280661 BEARING HOUSING IS LOOSE IN BELLCRANK. 1 H 7 1 3O 3 O NT 3A12 1E10 2001080300064 20010803 00064 NE 2001 8 3 VNAA0107022 2 20010721 A 7300 311995704 BLEED VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 423JS 1080 3032 AFTER STARTING THE TAKE OFF ROLL, THE CREW RECEIVED A RIGHT HAND ELECTRONIC CONTROL UNIT FAIL CAS MESSAGE AND ABORTED TA KE OFF. FLIGHT 4082 TAXIIED BACK TO THE GATE WHERE MAINTENANCE INSPECTED AND REPLACED THE INTERCOMP BLEED VALVE IN ACC ORDANCE WITH DORNIER MAINTENANCE MANUAL 73-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR S ERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001091400093 20010914 00093 NM 2001 9 14 2001UALA01469 1 20010723 A 2131 CONTROLLER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN PRESSURE FAILED A UALA K NONE O OTHER DE DESCENT 1 WP 29 7463U 21917 CABIN PRESSURE CAN NOT BE MAINTAINED (CABIN ALTITUDE RISES) IN DESCENT. BOTH AUTO & STANDBY THIS HAPPENS EVEN AT 5000 F EET. DUCT PRESSURE NORMAL. REPLACED THE NR 3 ENGINE 13TH STAGE MODULATOR VALVE, AND THE PRESSURE CONTROLLER. 2 L 7 3 4F 4 F A3WE E2EA 2001090600371 20010906 00371 NE 2001 9 6 2001UALA01432 2 20010722 A 7230 54H884 COMPRESSOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE FAILED A UALA C E F ABORTED TAKEOFF ENGINE SHUTDOWN ACTIVATE FIRE EXT. R B PARTIAL RPM/PWR LOSS SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 WP 29 655UA 11843 25393 717693 TAKEOFF ROLL LOUD NOISE ABOUT 30-50 KNOTS & LOSS OF THRUST NR 1 ENGINE. RTO. AFTER CLEARING RUNWAY TOWER ADVISED SMOKE A ROUND LEFT SIDE OF PLANE AND FA'S REPORTED SMOKE IN REAR OF CABIN. BLEW EXTINGUISHERS ON BOTH ENGINES AND APU AFTER SHUT DOWN. EMERGENCY EVACUATION OF AIRCRAFT THROUGH DRS 1L,1R & 2L. ONE EACH 5TH STAGE HPC VANE ARM DISCONNECTED FROM UPPER R ING. ONE 6TH STAGE BLADE FAILED IN THE DOVETAIL AREA AND NUMEROUS OTHERS WERE CRACKED AS A RESULT OF THE VANE ARM FAILUR E. ALL COMPRESSOR STAGES AFT OF THE 6TH STAGE WERE SEVERELY DAMAGED. INDICATIONS OF RESIDUAL FUEL FIRE IN THE TAILPIPE A REA. 2 L 7 2 4F 4 F RT A1NM E24NE 2001082200251 20010822 00251 NE 2001 8 22 NSVA0106 2 20010601 A 7261 4088T59P01 SEAL SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE LEAKING A NSVA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 27 9CJ 340B224 RIGHT OIL PRESSURE ANNUNCIATOR ILLUMINATED DURING CLIMB FROM IAD WITH SLIGHT DROP IN OIL PRESSURE. CREW SHUTDOWN ENGINE IN FLIGHT PER EMERGENCY CHECKLIST E-13 AND RETURNED TO IAD. MAINTENANCE WAS DISPATCHED AND FOUND OIL LEAKING FROM THE BB-AXIS SEAL. THE SEAL WAS REPLACED AND A OPERATIONAL CHECK AND LEAK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 2001082700236 20010827 00236 EA 2001 8 27 2001F00217 2 20010719 A 7200 3031800 ENGINE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA RIGHT FAILED A GUUA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SO 19 137GA 25102 UC105 FLT 9307 - PBI/NAS - DURING FLIGHT FROM PBI TO NAS AT 11,000 FEET, THE RIGHT ENGINE SURGED AND INDICATIONS FELL TO ZERO. CONTINUED TO SECURE THE RIGHT ENGINE. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. DETERMINED THAT THE RIGHT G AS GENERATOR DRIVE HAD BECOME UNCOUPLED FROM THE ACCESSORY SECTION. REMOVED AND REPLACED RIGHT POWERPLANT ASSEMBLY. (M ) 2 L 7 2 4T 4 T RT A24CE E4EA 2001082900060 20010829 00060 NE 2001 8 29 2001UALA01746 2 20010816 A 7230 COMPRESSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 ENGINE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 563UA 26665 NR 2 ENGINE FAILED TENTH STAGE BORESCOPE INSPECTION. 2 L 7 2 4F 4 F RT A2NM E17NE 2001090500186 20010905 00186 EU 2001 9 5 KBMA88768 1 20010725 A 2121 050021 MOTOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE CABIN INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 37SH 2300 EVAPORATOR MOTOR INOPERATIVE. REMOVED AND REPLACED WITH SV UNIT. 1 G 7 1 3U 3 U NC H9EU E19EU 2001091300315 20010913 00315 NM 2001 9 13 COOSDR010094 1 20010816 A 5730 SKIN BOEING 737 737230 NM PWA JT8 JT8D15 52051 NE RT WING CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 737TW 20257 RIGHT WING CENTER SECTION, LOWER SKIN CORRODED. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091400096 20010914 00096 NM 2001 9 14 2001UALA01594 1 20010731 A 7312 1552121 VALVE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUEL HEAT FAILED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING M OVER TEMP NR NOT REPORTED 1 WP 29 7286U 3597 21564 696555 NR 1 OIL TEMP IN YELLOW BAND FOR 15 MIN. ENGINE SHUTDOWN AND DIVERTED TO COS. THE FUEL HEAT VALVE FAILED. REPLACED FUE L HEAT VALVE AND DRAINED, REPLACED OIL AND SCREEN. THE MOTOR IN THE ACTUATOR OF THE VALVE ASSEMBLY WAS FOUND TO BE BAD. 2 L 7 3 4F 4 F A3WE E2EA 2001091400160 20010914 00160 NM 2001 9 14 2001UALA01954 1 20010831 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1175 STRINGER 37L-38L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091700048 20010917 00048 SO 2001 9 17 SWIA972651 1 20010617 A 3244 TIRE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE MLG FAILED A SWIA O OTHER P NO WARNING INDICATION LD LANDING 1 NM 07 188SW 120039 LEFT OUTBOARD MAIN TIRE BLEW ON LANDING. (SLC) FOUND NR 1 BRAKE HAD LOCKED UP DUE TO POOR CONDITIONS. REMOVED AND REPLA CED THE NR 1 BRAKE ASSEMBLY IAW A/C MM 32-41-05. PN ON 2-1661 SN ON 0055 SN OFF 1466. ALSO REMOVED AND REPLACED T HE NR 1 MAIN WHEEL ASSY. OPS CHECKED GOOD IAW 32-44-02. PN ON 3-1446-1 SN ON 2716 SN OFF 0152. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091700146 20010917 00146 NM 2001 9 17 VNAA0109004 1 20010906 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 427JS 14344 524 3039 THE CREW REPORTED THAT THE EMERGENCY LIGHTING IN THE LAST ROW WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 7LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WE RE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001091800136 20010918 00136 EU 2001 9 18 RAIA00106002 1 20010602 A 7712 30005000044 TSCU AEROSP ATR42 ATR42300 8680920 EU PWA PW120 PW124B NE RT ENGINE FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 423TE 8666 119 121372 7400-STL-LEFT PROPELLER FEATHERED IN FLIGHT, POWER MANAGEMENT KNOB IN CLIMB, TORQUE WAS 85 PERCENT. NP WENT TO 20 PERCEN T, ENGINE TORQUE WENT FULL SCALE, CREW RETARDED POWER, PROPELLER UNFEATHERED, AIRCRAFT RETURNED WITHOUT INCIDENT. MAINT ENANCE INSPECTED LEFT ENGINE, PERFORMED DOWNLOAD OF FDAU FOR EXCEEDANCE DATA, NO EXCEEDENCES WERE COLLECTED, MAINTENANCE REPLACED THE RIGHT ENGINE TORQUE SIGNAL CONDITIONER (CROSS TALK BETWEEN LEFT AND RIGHT ENGINES SIGNAL CONDITIONERS CAUS ING AUTOFEATHER), PERFORMED GROUND RUN, AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A53EU E2ONE 2001092100078 20010921 00078 WP 2001 9 21 CA010831017 2 20010830 A 7310 31021252 LINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE FUEL SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) FUEL WAS FOUND LEAKING ON THE GROUND. LINE REPLACED AND AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 2001092100083 20010921 00083 EU 2001 9 21 CA010905015 1 20010808 A 2400 36925 TERMINAL BAG JETSTM JETSTM3212 1500217 EU GARRTT TPE331 TPE33112UHR WP ROTOL R333 R333482F12 GL GOUND MISSING W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WHILE PILOT WERE DOING THROTTLE MOVEMENT CHECKS, THEY NOTICED THAT HYDRAULIC PRESSURE GAUGE NEEDLE WERE MOVING WITH THE THROTTLE. UPON TROUBLESHOOTING, FOUND THE LT MAIN BATTERY GROUND TERMINAL WAS MISSING & THE ATTACHMENT POINT ( EP1) WAS DETERIORATED. TERMINAL END AND GROUND LUG REPLACED. OPERATIONAL CHECK CARRIED OUT, FOUND SERVICEABLE. 2 L 7 2 4T 4 T RT BA15CAA E4WE 6 C P61GL 2001100900044 20011009 00044 2001 10 9 WVBA2001050 4 20010927 A 2200 011033T COMPUTER PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540* 41533 EA PITCH FAILED A WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 59829 2246 317652081 THIS PITCH COMPUTER WAS A FACTORY REPAIR WHICH UPON RETURN FAILED IN THE SAME MANNER. WHEN INSTALLED THE AIRCRAFT WOULD PITCH UP AND DOWN 5 DEGREES WHILE THE AUTOPILOT WAS ENGAGED FOR CRUISE. THIS AUTOPILOT SYSTEM SEEMS TO BE PARTICULARLY SENSITIVE TO ANY AFT LOADS WITHIN THE ENVELOPE AND COULD BE A FACTOR IN THE PORPOISING PROBLEM. THE UNIT WAS REMOVED A ND REPLACED WITH A LOANER UNIT. 1 L 7 2 3O 3 O A20SO E14EA 2001101200073 20011012 00073 NE 2001 10 12 2001UALA01929 2 20010902 A 7310 6A5002 LINE AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE FUEL SYSTEM CRACKED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 821UA 944 V10484 UNSCHEDULED LANDING DUE TO A FUEL LEAK. NR 1 ENGINE SHUTDOWN. *S/D* AFTER IN FLIGHT SHUTDOWN, THE FUEL TUBE WAS FOUND BROKEN. MAJOR CONTRIBUTOR FOR TUBE FAILURE CONSIDERED TO BE IMPROPER CLAMP CONFIGURATION. CLAMP WAS FOUND TO BE APPR OXIMATELY 2 SIZES TOO LARGE. 2 L 7 2 4F 4 F RT A28NM E40NE 2001103000022 20011030 00022 WP 2001 10 30 2001F00483 2 20010421 A 7310 8945681 FUEL LINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP LT ENGINE BROKEN A BSAA A UNSCHED LANDING K J E FLUID LOSS WARNING INDICATION VIBRATION/BUFFET CR CRUISE 1 NM 05 158MC 726B FLT 1314 - WDG - DURING CRUISE, THE CREW NOTICED THE TORQUE WAS DROPPING ON THE LEFT ENGINE. THEY MOVED THROTTLE FORWAR D UNTIL IT REACHED THE STOPS. TORQUE CONTINUED TO DROP, ALONG WITH FUEL FLOW. OVER A 5 MINUTE PERIOD THE TORQUE WENT T O 0, OIL PRESSURE AND TEMP WERE STILL READING IN NORMAL RANGE. CREW SHUT DOWN AND FEATHERED ENGINE AFTER IT WENT TO 0 T ORQUE. DIVERTED FROM PLANNED FLIGHT AND LANDED AT DIVERTED TO ALTERNATE AIRPORT. REPLACED BROKEN FUEL LINE, LEAK CHECK AND OPS CHECK GOOD. (M) 2 L 7 2 4T 4 T RT A8SW E4WE 2001120400102 20011204 00102 NM 2001 12 4 AUS20011118 1 20011010 A 5210 6940310901 DOUBLER BOEING 737 737376 NM CFMINT CFM56 CFM563C 13802 EU PAX DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NR 2 RT DOOR WINDOW DOUBLER CRACKED AND SEVERELY CORRODED. 2 L 7 2 4F 4 F RT A16WE E21EU 2001120500128 20011205 00128 NE 2001 12 5 JYD2001F00004 1 20010809 A 6220 643520019013 BEVEL GEAR SKRSKY S64 S64E 8142604 NE PWA JFTD12 JFTD12A4A 52047 NE GEARBOX CRACKED E JYDR K NONE O OTHER IN INSP/MAINT 1 NM 09 189AC 1172 641001 MAIN GEARBOX PN 643520400063, SN A6032 WAS REMOVED FROM SERVICE WITH A TOTAL TIME OF 3683.8 AND A TIME SINCE OVERHAUL OF 1172.0 FOR AN OVER TEMP CONDITION. DURING OVERHAUL INSPECTION, THIRTEEN CRACKS WERE DETECTED BY FLUORESCENT PENETRANT INSPECTION, EXTENDING FROM LIGHTENING HOLES AND IN WEBBING OF MAIN BEVEL GEAR SUPPORT PN 6435-20019-013. THE LONGEST CR ACK WAS APPROXIMATELY 3 INCHES LONG CONNECTING TWO LIGHTENING HOLES. MAIN BEVEL GEAR SUPPORT TOTAL TIME IS UNKNOWN. 2 G 7 2 4U 4 U H4EA E15EA 2001120600035 20011206 00035 SW 2001 12 6 R7MA33721 1 20010919 A 7160 470632 VALVE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL AIR INTAKE STUCK E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 407SJ 778 53422 STUCK IN OPEN POSITION. REPLACED WITH NEW UNIT CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2001121100125 20011211 00125 SO 2001 12 11 HZZ2001F00000 1 20011001 A 8120 TH08A60 TURBOCHARGER PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA ENGINE FAILED E HZZA O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 05 335WB 1454 317952135 L789061A AIRCRAFT EXPERIENCED TURBOCHARGER FAILURE UPON DEPARTURE. NEW TURBOCHARGER WAS INSTALLED AND SECURED. 1 L 7 2 3O 3 O A20SO E14EA 2001121200106 20011212 00106 WP 2001 12 12 IZ22001F00000 2 20011015 A 7310 69254513 VALVE MTSBSI MU2 MU2B26A 5780414 CE GARRTT TPE331 TPE331* 01514 WP LT ENGINE LEAKING B IZ2R O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 15 766MA 191 373SA P105071 VALVE REPLACED DUE TO FUEL LEAK BETWEEN SOLENOID AND VALVE BODY. 1 H 7 2 3T 3 T RT A10SW E2WE 2001121800044 20011218 00044 NM 2001 12 18 2001UALA02375 1 20011206 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 AFT PIT FRAME UPPER FLANGE HAS DENT AT STATION 1440 STRINGER 25L. MAJOR REPAIR ACCOMPLISHED, FRAME REPAIRED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002010300025 20020103 00025 NM 2002 1 3 SWAA013428 1 20011230 A 7603 THROTTLE BOEING 737 7377H4 1384404 NM CFMINT CFM567 CFM567B2US 13802 NE NR 1 ENGINE MALFUNCTIONED A SWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 SW 07 782SA 29808 876597 IN FLIGHT ENGINE SHUT DOWN, DECLARED EMERGENCY. AT FL 390, NR 1 ENG THROTTLE WOULD NOT RESPOND. CAME BACK TO 85.1 PERC ENT N1, AFTER 30 MINUTES WENT TO 79 PERCENT N1. NO OTHER ABNORMAL INDICATION FOUND BEFORE SHUT DOWN. C/W NR 1 ENG INSP , C/W NR 1 EEC BITE CK. NO DEFECT, FAULTS NOTED. C/W TWO POWER ASSURANCE ENG RUNS AND OPS CK GOOD. ACFT OK FOR SERVIC E PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002010800081 20020108 00081 2002 1 8 AUS20011050 4 20011001 A 3414 2114011342 INDICATOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE AIRSPEED FAULTY W O OTHER O OTHER CR CRUISE 1 AU S 3367 251485 (AUS) CAPTAINS AIR SPEED INDICATOR (ASI) INTERNAL FAILURE. FAULT CAUSED OTHER INSTRUMENTS TO BE AFFECTED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001060100150 20010601 00150 NE 2001 6 1 GLBA2001093 2 20010506 A 7314 1143890425 PUMP BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ENGINE FAILED A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 01 260GL 534 UE260 ABORTED T/O, RIGHT LOW FUEL PRESSURE LIGHT ILLUMINATED. REPLACED LP PUMP. 2 L 7 2 4T 4 T RT A24CE E26NE 2002011800068 20020118 00068 NM 2002 1 18 2001UALA02478 1 20011230 A 5350 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE TAIL CONE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 198UA 28716 THE TAIL CONE LOWER SKIN HAS CRACK AND DENT JUST AFT OF THE APU COMPARTMENT. MAJOR REPAIR ACCOMPLISHED INSTALLED REPAIR DOUBLER. 2 L 7 4 4F 4 F RT A20WE E24NE 2002011400034 20020114 00034 NM 2002 1 14 AUS20011277 1 20011202 A 2720 CONTROLLER BOEING 737 73733A 1384673 NM CFMINT CFM56 CFM563B1US GL RUDDER CONTROL CONTAMINATED W O OTHER W F J INADEQUATE Q C FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 AU S (AUS) RUDDER CONTROL SYSTEM SUBJECT TO TWO UNCOMMANDED INPUTS. INVESTIGATION FOUND EVIDENCE OF WATER/COFFEE CONTAMINATI ON OF THE FORWARD E&E BAY. CONTAMINATION WAS DUE TO REMOVAL OF THE AIRSTAIRS AND DRIP TRAY LOCATED ABOVE THE E&E BAY. S ERVICE BULLETIN SB 737-25-1317 THEN CALLS FOR THE INSTALLATION OF A WATERSHIELD AND MOISTURE SHROUDS. THE SB WAS NEVER CARRIED OUT. PERSONNEL/MAINTENANCE ERROR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002011500075 20020115 00075 NE 2002 1 15 CA011017004 2 20010928 A 8500 ENGINE DOUG DC4 C54A 3021512 WP PWA R2000 R20007M2 52023 NE NACELLE MAKING METAL W E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 CA (CAN) DECAYING OIL PRESSURE SHORTLY AFTER TAKEOFF. THERE WAS SOME METAL CONTAMINATION IN THE MAIN OIL SCREEN. DUE TO THE HIGH T.S.O. (1373.1 HRS) THE DECISION WAS MADE TO REPLACE THE ENGINE AND HAVE FURTHER INVESTIGATION CARRIED OUT BY THE ENGINE OVERHAUL AGENCY. 2 L 7 4 4R 4 R A762 5E5 2002011600064 20020116 00064 EU 2002 1 16 CA011031011 1 20011016 A 3230 5Q2395 HOSE BRAERO 748 HS7482A 4231001 EU RROYCE DART DART5342 EU MLG BROKEN W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION AP APPROACH 1 CA (CAN) THE AIRCRAFT WAS ON APPROACH, THE LANDING GEAR WAS ENTERED, 3 GREEN WERE OBTAINED THEN THE CREW NOTICED ALL HYDRAU LIC SYSTEM PRESSURE WAS LOST. THE AIRCRAFT RETURNED TO BASE GEAR DOWN AND LANDED SAFELY WITH BRAKING ACTION OBTAINED FRO M THE HYDRAULIC HAND PUMP AND EMERGENCY RESERVOIR FLUID. THE LEFT HAND GEAR RETRACT JACK RETURN LINE WAS FOUND TO HAVE B ROKEN OFF AT THE UPPER FITTING. THE LINE WAS REPLACED AND THE APPROPRIATE CHECKS CARRIED OUT. 2 L 7 2 3T 4 T A24EU A196 2002011700045 20020117 00045 NE 2002 1 17 CA011112001 2 20011109 A 7532 6714D060000 RELIEF VALVE AIRBUS 320 A320212 3930322 EU CFMINT CFM56 CFM565A3 NE NR 1 ENGINE FAILED W A UNSCHED LANDING M OVER TEMP CL CLIMB 1 CA 17831 17831 (CAN) SHORTLY AFTER T/O NR 2 PRV FAILED TO THE CLOSED POSITION. THE X BLEED WAS SELECTED TO OPEN AND BOTH PACKS WERE SUP PLIED BY NR 1 ENGINE BLEED. THE NR 1 PRECOOLER OUTLET TEMP THEN ROSE TO AN OVERHEAT CONDITION AND CLOSED THE NR 1 BLEED RESULTING IN THE LOSS OF BOTH PACKS.AFTER THE TEMP COOLED DOWN NR 1 BLEED WAS RESET AND SELECTED ON WITH NO OPERATIONAL IMPACT. MAINTENANCE REPLACED THE NR 2 PRV AND INSPECTED THE NR 1 BLEED SYSTR. WITH NO FINDINGS. BOTH ENG'S WERE RUN AND ALL BLEED SYS'S OPERATED NORMALY 2 L 7 2 4F 4 F RT A28NM E29NE 2002011700057 20020117 00057 EA 2002 1 17 CA011113012 1 20011029 A 7120 60135006 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE ENGINE BAY CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 18797 17958 (CAN) CRACKS FOUND AT THREE LOCATIONS ON REPEAT INSPECTION: FS 630, LBL 36, RBL 36 & BL 0 WHILE PERFORMING SB A601R-53-0 59. DISCREPANCIES WILL BE REPAIR USING BOMBARDIER DISPOSITIONS. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021800004 20020218 00004 2002 2 18 CA020130003 4 20011120 A 3414 M227591620 WIRE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE WIRE SHORTED W K NONE O OTHER IN INSP/MAINT 1 CA 12888 (CAN) PILOT REPORTED THAT ALL PILOT AND COPILOT INSTRUMENT LIGHTING WAS NOT WORKING ON THE GROUND PRIOR ENGINE START. A FTER INVESTIGATION WE FOUND THAT THE COPILOT AIRSPEED INDICATOR WIRE L38B20 HAVE BEEN CHAFFING ON EADI OUTERCASE. THE WIRE SHORTED AND CAUSED CIRCUIT BREAKER CB21 TO TRIP, CAUSING THE POWER LOST FOR THE INSTRUMENT LIGHTING. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2002032500097 20020325 00097 EU 2002 3 25 GN42002F00000 2 20011115 A 7200 SEAL CFMINT CFM56 CFM563C1 13802 EU ROTOR DISC FAILED W GN4Y K NONE O OTHER IN INSP/MAINT 1 WP 03 VTJAE 725488 HOLE IN HPT FWD AIR SEAL, BOLT SHEARED FLUSH AT ROTOR DISC TO ROTOR FWD SEAL ATTACH FLANGE RELEASING SELF LOCKING NUT AN D ENGAGED SECT OF BOLT SHANK. INSP REVEALED TIP CRACKING, MISSING MATERIAL TO MOST OF BLADES. LEADING EDGE/CONCAVE SID E HOLES WERE PRESENT ON BLADES. FWD EDGE OF BLADES, PLATFORM DAMAGE FROM RUBBING. HPT NOZ VANE SEG, INNER AND OUTER PL ATFORMS EXHIBITED EXCESS IMPACT PITTING. HPT AFT STATOR SEAL SEG, DAMAGE WITH LGE SECT OF SEAL SEG MATERIAL MISSING. 4 TOOTH HONEYCOMB SEAL EXHIBITED ABRASION DUE TO INTERACTION BETWEEN HPT ROTOR AND DISLODGED HARDWARE MATERIAL. CONTACT FROM DISLODGED MATERIAL WAS ALSO MADE WITH HPT AFT STATOR SEAL SEGMENT ATTACHMENT BOLTS THUS DAMAGING THE BOLT HEAD. 4 F E21EU 2002041900017 20020419 00017 SW 2002 4 19 AC2A0000340 1 20011007 A 6220 230312001105 BEARING BELL 430 430 1182150 SW ALLSN 250C 250C* GL P/C LINKS WORN E AC2A K NONE O OTHER IN INSP/MAINT 1 SW 03 430CH 970 49037 BEARINGS WORN IN P/C LINKS. REMOVED AND REPLACED BEARINGS. 1 G 7 2 3U 3 U RT H9SW E4CE 2001101500187 20011015 00187 WP 2001 10 15 01FDEA00876 1 20011010 A 5315 FLOORBEAM DOUG DC10 DC1010F 3022111 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 059FE 46907 AFT CARGO COMPARTMENT BS 1871, RBL 12 CORRODED. R&R FLOORBEAM PER 53-60-00. 2 L 7 3 4F A22WE 2001052100002 20010521 00002 NM 2001 5 21 01FDEA00275 1 20010412 A 5320 FITTING BOEING 727 72725C 138400H NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 124FE 19360 DURING ROUTINE INSP, STR 18R END FITTING AT BS 1183 FOUND CORRODED. *S/D* REMOVED AND REPLACED STR T-FITTING PER IAW B AC 727 SRM 51-30-2. 2 L 7 3 4F A3WE 2001072400173 20010724 00173 NM 2001 7 24 2001UALA01135 1 20010624 A 5312 BULKHEAD BOEING 737 737322 1384676 NM FUSELAGE FRETTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 FUSELAGE BHD WEB IS FRETTED WORN AT RADOME BRACKET AT BS 178, LBL 27, WL 203. ACCOMPLISHED DOUBLER REPAIR. MAJOR REPAI R ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001071200146 20010712 00146 SO 2001 7 12 LR7A01045 1 20010711 A 5313 37049423 STIFFENER LKHEED 382 382G 526414U SO FS 787E-797E BROKEN A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 DURING POST TAIL STRIKE DAMAGE EVALUATION (REF. OPER CTRL NO. LR7A01033) FOUND FS 787E - 797E LONGITUDINAL STIFFENERS BR OKEN AT LBL 3.57 AND RBL 3.57, WL 127.75.FABRICATED AND REPLACED LONGINTUDINAL STIFFENERS IAW SRM SMP 583-53-10 PG 7 D, 51-70. NR 9, CONT. SHEET ITEM 20, 21, 22, 23. 2 H 7 4 4T A1SO 2001030500128 20010305 00128 WP 2001 3 5 01FDEA00115 1 20010213 A 2510 FT1179 TRANSFORMER DOUG DC10 DC1030F 3023504 WP COCKPIT FAULTY A FDEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 25 319FE 47820 DURING SAFETY CHECK FOUND OVERHEAD SWITCH PANEL LIGHTS (CB) POPPED. RESET NORM. BEGAN TO SMELL FUMES AND SMOKE FROM OV ERHEAD PANEL. INSTALL TRANSFORMER T1-94, OPS NORM PER MM 33-11-07-2. 2 L 7 3 4F RT A22WE 2001072600050 20010726 00050 NM 2001 7 26 2001UALA01255 1 20010629 A 3350 POWER SUPPLY AIRBUS A319 A319131 NM CABIN DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 816UA 871 OVERHEAD EMERGENCY LIGHTS REMAIN ON. REPLACED RT OVERWING POWER SUPPLY. 2 L 7 2 4F RT A28NM 2001102200050 20011022 00050 NM 2001 10 22 QXEA0101671 1 20011008 A 5330 DOUBLER DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - CARGO DOOR APERTURE TOP EDGE OF FUSELAGE INTERNAL DOUBLER HAS TWO GOUGE MARKS .5 INCH LONG AT FS X564.500 AND 1 IN CH LONG AT FS X580.500. REPAIRED IAW DHC-8 SRM 51-20-26 AND SRM 51-20-51. 2 H 7 2 4T RT A13NM 2001041000020 20010410 00020 NM 2001 4 10 01FDEA00052 1 20010130 A 5311 6516343 FRAME BOEING 727 727227 1384078 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 FRAME DENTED AT BS 1050, RBL 26. *S/D* REMOVED AND REPLACED PER FEDEX SRM 51-40-3, 53-10-1. 2 L 7 3 4F A3WE 2001031900125 20010319 00125 NM 2001 3 19 01FDEA00150 1 20010216 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM CABIN CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 DURING ROUTINE INSP, NR 2 MAIN CABIN SEAT TRACK FOUND CORRODED AT BS 783. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 53-10-5. 2 L 7 3 4F A3WE 2001080400002 20010804 00002 NM 2001 8 4 01FDEA00635 1 20010802 A 2613 CONNECTOR BOEING 727 727225 1384077 NM A FDEA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SO 25 461FE 22548 01-258 DUR CRUISE LWR AFT BODY O/H LIGHT ILLUM. R&R CONNECTOR D1304 OF R/H STAIRWELL ELEMENT M365 PER IAW 727-2 MM CH 20 SYS. 2 L 7 3 4F A3WE 2001022200006 20010222 00006 EA 2001 2 22 WVBA2001004 2 20010124 A 7314 RG9080J7AM PUMP PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA LT ENGINE MALFUNCTIONED E WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 4082T 161 318152089 ON PRE INSPECTION RUN UP, IT WAS NOTICED THAT THE FUEL PRESSURE WAS LOW ON THE LEFT ENGINE. THE FUEL PRESSURE WAS ADJUS TED IN ACCORDANCE WITH INSTRUCTIONS IN THE SERVICE MANUAL FOR THE AIRCRAFT WHICH RESULTED IN NO CHANGE IN THE FUEL PRESS URE ON THE GROUND RUN CHECK. THE PUMP WAS RETIRED FROM SERVICE. 1 L 7 2 3O 3 O A20SO E14EA 2001030600217 20010306 00217 NE 2001 3 6 DLM88010256 2 20010113 A 7510 DUCT DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE BLOWN A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 977DL 27324 53258 725639 LEFT ENGINE FIRE INDICATION ON CLIMBOUT. RETARDED THROTTLE LIGHT WENT OUT. FOUND LEFT ENGINE ANTI ICE DUCT BLOWN, DUCT FROM ENG BLEED TO ANT ICE VALVE. REPLACED DUCT. RAN ENGINE. FIRE DETECTION AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A6WE E9NE 2001032100122 20010321 00122 SO 2001 3 21 SWIA972380 1 20010220 A 2131 CONTROLLER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CABIN MALFUNCTIONED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 224SW 120294 AUTO PRESSURIZATION BECAME VERY ERRATIC DURING CLIMBOUT. RETURNED TO SFO. DEF AUTO PRESSURIZATION AS PER MEL 21-31-1A CW MX PROCEDURE PER MEL APPX A. VALVE SAFTIED CLOSE. REPLACED ELECTRONIC CONTROLLER IAW EMB 120 MM 21-30-01. OPS CHEC K GOOD. (P/N ON 22201T011400) (S/N ON 164) (S/N OFF 518). 2 L 7 2 4T 4 T RT A31SO E20NE 2001032600149 20010326 00149 NM 2001 3 26 VNAA0102016 1 20010223 A 3060 BRUSH BLOCK DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT PROPELLER DIRTY A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 422JS 3018 DURING THE TAKEOFF ROLL THE RIGHT HAND PROPELLOR DEICE HEAT FAILED. THE FLIGHT CREW ABORTED THE TAKEOFF. MAINTENANCE I NSPECTED AND CLEANED THE PROPELLOR SLIP RING AND BRUSHBLOCK IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-60-00. OPE RATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001032900266 20010329 00266 NE 2001 3 29 AWXA0001338 2 20010214 A 7260 MS9388151 PACKING BOEING 737 737277 1384570 NM PWA JT8 JT8D15 52051 NE OIL PUMP BROKEN A AWXA A E UNSCHED LANDING ENGINE SHUTDOWN O OTHER CL CLIMB 1 WP 28 181AW 3710 22648 P700272B IN PHX OIL PUMP WAS REPLACED. UPON REMOVAL THE CENTER O-RING WAS FOUND TO BE BROKEN. THE OTHER 2 WERE OK. PUMP WAS RE PLACED THOUGH IT APPEARED TO BE NORMAL. 2 L 7 2 4F 4 F RT A16WE E2EA 2001041600005 20010416 00005 NM 2001 4 16 2001UALA00161 1 20010224 A 5350 SCREW BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FAIRING MISSING A UALA A UNSCHED LANDING D INFLIGHT SEPARATION NR NOT REPORTED 1 WP 29 307UA 23668 DIVERTED DUE TO A PASSENGER SEEING A SCREW FALL OUT OF THE ENGINE MOUNT AREA. *S/D* FOUND FAIRING WITH MISSING SCREW. REPLACED SCREW. 2 L 7 2 4F 4 F RT A16WE E2GL 2001043000011 20010430 00011 NM 2001 4 30 2001UALA00348 1 20010328 A 2710 BACP30F9 PULLEY BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE AILERONS BINDING A UALA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 396UA 24671 DIVERTED DUE TO STIFF AILERONS. SUPPLEMENTAL DATA UPDATE FOUND RIGHT AILERON WING BODY LOWER PULLEY BINDING AT STA 664. REPLACED PULLEY AND SPACERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600420 20010416 00420 2001 4 16 2001UALA00381 4 20010330 A 2565 62421110 TUBE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE ESCAPE SLIDE LEAKING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 783UA 1698 26950 DURING SHOP OVERHAUL, SLIDE RAFT FAILED INFLATABLE AIR RETENTION TEST OF THE TOP TUBE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001041700034 20010417 00034 CE 2001 4 17 CA010406013 1 20010323 A 3233 11238002223 ACTUATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE MLG FAILED W O OTHER N FALSE WARNING LD LANDING 1 CA 6500 (CAN) CREW REPORTED NOSE GEAR DOWN AND LOCKED GREEN WAS INTERMITTENT. THE AIRCRAFT WAS REMOVED FROM THE FLIGHLINE AND FE RRIED BACK FOR REPAIRS. MAINTENANCE REPLACED THE NOSE GEAR ACTUATOR ASSEMBLY AND THE SYSTEM WAS CYCLED SEVERAL TIMES. TH E AIRCRAFT WAS RELEASED BACK INTO SERVICE. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2001042400127 20010424 00127 EA 2001 4 24 5039032920 1 20010329 A 3230 BRACKET CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF343A 30015 NE NLG BENT E J7SA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 765W NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. TROUBLESHOOTING REVEALED BENT BRACKET ON NOSE GEAR CENTERING SWITCH. RESTOR ED BRACKET, RIGGED SWITCH AND PERFORMED SEVERAL SUCCESSFUL GEAR SWINGS. NO FURTHER DEFECTS NOTED. SUBSEQUENT INVESTIGA TION FOUND THAT THE STRAP USED TO SECURE THE NOSE GEAR TO THE GSE TUG WAS HUNG UP ON THE BRACKET, CAUSING IT TO BEND. 2 L 7 2 4F 4 F RT A21EA E15NE 2001042700118 20010427 00118 SO 2001 4 27 SWIA972494 1 20010408 A 2731 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE AILERON TAB FAILED A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 NM 07 220SW 120288 AT 21,000 AILERON TRIM WAS FOUND TO BE JAMMED. OAT WAS -10C DEGREES. AFTER LANDING THE TRIM SEEMED TO BE OPERATIONAL A GAIN. REPLACED AILERON TRIM TAB ACTUATOR IAW 120 MM 27-12-01. OPS CHECK GOOD. P/N: 5301, S/N ON: 411, S/N OFF: 373 . 2 L 7 2 4T 4 T RT A31SO E20NE 2001043000071 20010430 00071 NM 2001 4 30 2001UALA00474 1 20010410 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 AFT PIT STATION 1241 STRINGERS 35R TO 36R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED FABRICATED AND INSTALLED REPAI R IN ACCORDANCE WITH BAC DRAWING 140T2102 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001050100007 20010501 00007 EA 2001 5 1 20010411CW010 1 20010306 A 2752 SC14000062 BEARING EATON CNDAIR CL600 CL6002B19 EA GE CF34 CF34* NE FLAP ACTUATOR LACK OF LUBE B VK6R K NONE O OTHER IN INSP/MAINT 1 GL 09 407SW 1464 1272 7034 THRUST BEARING FAILURE DUE TO LACK OF LUBRICATION AND POSSIBLE PRELOAD CONDITION. 2 L 7 2 4F 4 F RT A21EA E15NE 2001050300094 20010503 00094 EA 2001 5 3 SWIA972517 1 20010406 A 2742 ACTUATOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE STAB TRIM MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 413SW 7102 AUTOPILOT PITCH TRIM MESSAGE ILLUMINATED WHILE DESCENDING TO FL 270. AFTER FOLLOWING QRH PROCEDURE MESSAGE EXTINGUISHED . RETURNED TO SLC. AUTOPILOT PITCH TRIM SYSTEM OPS CHECKS GOOD. REPLACED THE STABILIZER TRIM ACTUATOR AND MOTOR CONTR OL UNIT. 2 L 7 2 4F 4 F RT A21EA E15NE 2001050300121 20010503 00121 CE 2001 5 3 20010501CW009 1 20010403 A 3297 WIRE BEECH 58 58 1152740 CE CONT O520 IO520* 17032 SO MLG BROKEN D K NONE O OTHER IN INSP/MAINT 1 GL 07 58TA TH596 GEAR WOULD NOT GO UP. FOUND BROKEN WIRE GOING TO UP LOCK SWITCH, REPAIRED WIRE. OPS CHECKS GOOD. 1 L 7 2 3O 3 O 3A16 E5CE 2001051500385 20010515 00385 EU 2001 5 15 CA010508004 1 20010412 A 2434 HED60CR132200 BRUSHES PILATS 5243212158 PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL GENERATOR WORN W K NONE O OTHER IN INSP/MAINT 1 CA 207 207 100049 (CAN) DUE TO PREMATURE WEAR OF NR 2 GEN BRUSHES PILATUS ISSD A SB (SB 24-016) TO ADDR ISSUE BY INTRODUCING A NEW, LONGER WEARING BRUSH BLOCK ASSY WHICH IS FIELD REPLABLE.PRIOR TO THE SB, WE FOUND BRUSHES ON ORIGLY INST GEN S/N 100092 WITH 6 86.2 TAT HRS WAS VERY WORN & CAUSED AN OFFLINE SITUATION. GEN WAS REPLD WITH S/N 100049.AT 1124.2 TAT (778 CYC) THE GEN S/N 100049 BRUSHES WERE EPLACED DUE TO WORN AS PER SB 24-016. AS A RESULT OF OPERATOR INPUT, PER FAILURE RATE OF THESE B RUSHES IT WAS DECIDED TO CHECK THESE BRUSHES AT AROUND 200 HR INSERVICE. THESEE BRUSHES WERE FOUND TO BE EXTREMELY WORN & ON POINT OF FAILURE: THIS BRUSH ASSY WAS INSERVICE FOR 207 HRS 144 CYCLES. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001061400007 20010614 00007 EU 2001 6 14 CA010511033 1 20010417 A 3242 LINER BRAERO 748 HS7482A 4231001 EU RROYCE DART DART5342 EU BRAKE ASSY DISLODGED W O OTHER O OTHER LD LANDING 1 CA 4395 (CAN) ON LANDING NR 1 WHEEL ASSEMBLY TIRE WENT FLAT. WHEN CHANGING MAINWHEEL ASSEMBLY FOUND BRAKE ASSY IN THE LOCKED POS ITION. BRAKE ASSY HAD 87.8 HOURS AND 110 LANDINGS SINCE REPAIR. BRAKE AND WHEEL ASSEMBLY WERE REPLACED AND AIRCRAFT RETU RNED TO SERVICE. NOTE: BRAKE LININGS WERE FOUND DISLODGED AND HOUSING DAMAGED WHEN UNIT INSPECTED. 2 L 7 2 3T 4 T A24EU A196 2001061800096 20010618 00096 NM 2001 6 18 2001UALA00809 1 20010523 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 317UA 23949 UPPER SURFACE OF LT CREASE BEAM WEB CORRODED AT BS 696, LBL 65. REPLACED CREASE BEAM WEB. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001071100121 20010711 00121 NM 2001 7 11 2001UALA00934 1 20010510 A 2750 FLAP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE WINGS MALFUNCTIONED A UALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 WP 29 605UA 21866 TRAILING EDGE FLAP SHUTDOWN. EMERGENCY DECLARED. UNEVENTFUL LANDING. 2 L 7 2 4F 4 F RT A1NM E3NE 2001071800113 20010718 00113 NE 2001 7 18 2001F00115 2 20010702 A 8530 356994 CYLINDER DOUG DC6 DC6A 3021706 WP PWA R2800 CB3 52026 NE NR 13 CRACKED A NACA E ENGINE SHUTDOWN O OTHER TO TAKEOFF 1 AL 01 7780B 45372 31026 PRECAUTIONARY SHUTDOWN NR 1 ENGINE DUE TO RUNNING ROUGH AT 2340Z. NR 13 CYLINDER HEAD CRACKED, REPLACED CYLINDER. (M) 2 L 7 4 4R 4 R 6A3 E264 2001073000065 20010730 00065 EU 2001 7 30 CA010530003 1 20010508 A 2750 9742001212 RELAY PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL TE FLAP DRIVE DAMAGED W O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 CA 549 (CAN) FLAP WERE SET TO 30 DEGREES FOR APPROACH. UPON LANDING AND ROLL OUT TO THE TAXIWAY, THE FLAPS WERE SELECTED TO ZER O DEGREES. THE PILOT NOTED THAT THE "FLAP" CAUTION LIGHT ON THE CAWS PANEL ILLUMINATED. FURTHER SELECTIONS OF THE FLAPS WERE UNSUCCESSFUL. IT WAS NOTED DURING THE MAINTENANCE PROCEDURE FOR TROUBLESHOOTING THIS SNAG, THAT THE RELAY IN QUESTI ON WOULD FAIL INTTERMITTENTLY. WHEN THIS FAILURE WOULD OCCUR, THE AME WOULD TAP THE RELAY, AND THE FLAPS COULD THEN BE R ESET AND MOVED THROUGHOUT THEIR NORMAL RANGE OF MOTION. A NEW STYLE OF RELAY WAS ORDERED AND INSTALLED IN THE AIRCRAFT. THE FLAPS WERE CYCLED SEVERAL TIMES WITHOUT ANY FURTHER PROBLEMS. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001080200124 20010802 00124 SO 2001 8 2 XGN2001F00000 2 20010712 A 8530 AEC31397A CYLINDER HEAD I520 BEECH 36 A36 1151604 CE CONT O520 IO520BB 17032 SO CYLINDER DEPARTED A XGNA O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 SW 05 236CH 1959 E502 573460 CYLINDER HEAD DEPARTED CYLINDER BARREL, WHILE AIRCRAFT WAS IN FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. 1 L 7 1 3O 3 O 3A15 E5CE 2001081000166 20010810 00166 EA 2001 8 10 Z4MR601462 2 20010714 A 7314 RG34720F RELIEF VALVE BEECH 200 B200 1152922 CE PWA PT6 PT6A41 52043 EA ENGINE LEAKING B Z4MR K NONE K FLUID LOSS IN INSP/MAINT 1 WP 27 726CB BB1750 A RANDOM INSPECTION OF THE FUEL PUMP REVEALED FUEL LEAKING FROM THE ENGINE DRIVEN LOW PRESSURE FUEL PUMP RELIEF VALVE GA SKET. 1 L 7 2 4T 4 T A24CE E4EA 2001081000235 20010810 00235 NE 2001 8 10 JBXA000313 2 20010725 A 7200 CF343B1 POWERPLANT CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE MAKING METAL A JBXA O OTHER J WARNING INDICATION IN INSP/MAINT 1 SO 05 586ML 4165 7341 872580 RH ENGINE CHIP DETECTOR LIGHT WAS FOUND DURING A SCHEDULED INSPECTION. METAL WAS FOUND ON DETECTOR AND WAS FOUND TO BE O UT OF LIMITS PER GE MAINTENANCE MANUAL.CORECTIVE ACTION: R&R RH ENGINE IAW CRJ AMM 71-00-00 2 L 7 2 4F 4 F RT A21EA E15NE 2001081300192 20010813 00192 NM 2001 8 13 2001UALA01496 1 20010725 A 5320 INTERCOSTAL BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 617UA 21877 BS 1263-1285 LBL33 INTERCOSTAL CORRODED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001101200049 20011012 00049 NM 2001 10 12 2001UALA01608 1 20010803 A 3244 TIRE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT MLG FAILED A UALA O OTHER O OTHER LD LANDING 1 WP 29 7267U 21414 UPON LANDING THE TWO LEFT MAIN LANDING GEAR TIRES BURST. *S/D* HARD LANDING INSPECTION ACCOMPLISHED. ANTISKID FUNCTIO NAL TEST ACCOMPLISHED. OPERATIONAL CHECK FOUND NO DISCREPANCIES. 2 L 7 3 4F 4 F A3WE E2EA 2001082000034 20010820 00034 CE 2001 8 20 GUU2001F00021 1 20010629 A 2612 FIRE LOOP BEECH 1900 1900C 1154161 CE PWA PT6 PT6* 52043 EA LT ENGINE LOOSE A GUUA E D ENGINE SHUTDOWN RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 17 143GA UC145 DURING TAXI, LEFT FIRE LIGHT HANDLE ILLUMINATED. ENGINE WAS SHUT DOWN AND EMERGENCY CHECKLIST ACCOMPLISHED. CORRECTIVE ACTION: INSPECTED FORWARD AND AFT FIRE LOOPS. SECURED FORWARD FIRE LOOP. PERFORMED ENGINE RUNS. NO DEFECTS NOTED. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 3 T RT A24CE E2NE 2001082100031 20010821 00031 NM 2001 8 21 COOSDR010078 1 20010820 A 5413 655355854 LONGERON BOEING 737 737230 NM PWA JT8 JT8D17 52049 NE NR 2 PYLON CRACKED E EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 767TW 20258 ENGINE NR 2, FORWARD FIREWALL-LONGERON, PN 65-53558-54 CRACKED. 2 L 7 2 4F 4 F RT A16WE E2EA 2001082200208 20010822 00208 NE 2001 8 22 CHQA00013 2 20010801 A 7532 BLEED VALVE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ENGINE FAILED A CHQA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 11 CHQ 340A095 BLEEDS WON`T STAY ON. A/C RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED HP BLEED VALVE. 2 L 7 2 4T 4 T RT A52EU E8NE6 2001082900076 20010829 00076 NM 2001 8 29 2001UALA01772 1 20010822 A 5320 CHANNEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 324UA 23956 CABIN FLOOR, STATION 965 TO 990, LBL 50, Z-CHANNEL AT AFT ENTRY DOOR SILL CORRODED. MAJOR REPAIR ACCOMPLISHED. BY REPL ACING CREASE BEAM INBOARD CHORD ANGLE AT AFT ENTRY DOOR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001090500098 20010905 00098 NM 2001 9 5 AUS20010917 1 20010822 A 3350 LIGHT BOEING 737 737476 NM CFMINT CFM56 CFM563C 13802 EU CABIN INOPERATIVE W K NONE L NO TEST IN INSP/MAINT 1 AU S (AUS) FLOOR PATH LIGHTING ADRIFT AT ROW 15. LIGHTING ASSEMBLY WAS REINSTALLED BUT ONE SECTION WAS INOPERATIVE. THE FAULT WAS TRACED TO A FAULTY CONNECTOR. 2 L 7 2 4F 4 F RT A16WE E21EU 2001090600088 20010906 00088 EA 2001 9 6 2001F00263 2 20010817 A 7532 01R310687001 BLEED VALVE STBROS SD3 SD360 8100606 EU PWA PT6 PT6A65R 52043 EA LT ENGINE MALFUNCTIONED A DATA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 13 151CA SH3653 PCE97173 A/C DEPARTED CHEYENNE, WY, AFTER FUEL TOP OFF AND CLIMBING OUT THE LT ENGINE TORQUE DROPPED TO 2500 NR AND NG DROPPED 3 PERCENT. THE PILOT INCREASED THE POWER LEVERS, THE TORQUE ROSE AND THEN SETTLED BACK TO 2500 NR. THE CREW MADE A PRECAUT IONARY ENGINE SHUT DOWN AND MADE AN UNEVENTFUL LANDING AT LORAMY, WY. NO EMERGENCY WAS DECLARED. TOTAL FLIGHT TIME WAS . 4 HRS. THE MECHANIC INSPECTED THE ENGINE FOR BLEED AIR, PY, P3 FOR LEAKS AND NO DEFECTS WERE NOTED. THE MECHANIC REMOVED AND REPLACED THE BLEED VALVE AND PERFORMED RUN CHECKS ON THE ENGINE IAW THE MM AND DECLARED THE ENGINE OK FOR RETURN TO SERVICE. THE AIRCRAFT CONTINUED THE FOLLOWING DAY WITH NO FURTHER OCCURRENCES. (M) 2 H 7 2 4T 4 T A41EU E4EA 2001091300311 20010913 00311 NM 2001 9 13 COOSDR 010113 1 20010816 A 5210 BEAM BOEING 737 737230 NM PWA JT8 JT8D15 52051 NE ENTRY DOOR CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 737TW 20257 AFT ENTRY DOOR BEAM NR 2, INSIDE CHORD CRACKED. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091700019 20010917 00019 SO 2001 9 17 SWIA972623 1 20010607 A 2131 CONTROLLER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CABIN PRESSURE MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 270YV 120270 AIRCRAFT WOULD NOT PRESSURIZE, AUTO OR MANUAL, BLEEDS AND PACKS - ALL CONFIGURATIONS. RETURNED TO PDX. REPLACED SHOCK A BSORBER RELAY K0127 IAW MM 24-52-04. OPS CHECK GOOD IAW MM 21-30-00. 2 L 7 2 4T 4 T RT A31SO E20NE 2001091900256 20010919 00256 NM 2001 9 19 2001UALA02035 1 20010913 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 915UA 25382 EXTERNAL FUSELAGE SKIN AT BODY STATION 1006 STRINGER 4L IS GOUGED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001092100034 20010921 00034 EU 2001 9 21 CA010829003 1 20010827 A 2910 A2913161 LINE AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE HYD SYSTEM LEAKING W H DEACTIVATE SYST/CIRCUITS K FLUID LOSS IN INSP/MAINT 1 CA (CAN) YELLOW SYSTEM HYDRAULIC FLUID LOSS, FOUND ON ARRIVAL BY MAINTENACE PERSONNEL. FLUID LOSS FROM FLEX LINE FITTING. LINE REMOVED AND SYSTEM CAPPED, LEAK CHECKED AND PLACED ON MEL FOR LINE REPLACEMENT. 2 L 7 2 4F 4 F RT A35EU E23EA 2001092400113 20010924 00113 EA 2001 9 24 JUK2001F00001 2 20010823 A 8520 77140 CAMSHAFT HELIO H295 H295 4300802 CE LYC O480 GO480G1D6 41527 EA ENGINE DAMAGED E JUKA K NONE O OTHER IN INSP/MAINT 1 SO 33 269L 1286 L30337 NEW CAMSHAFT AND LIFTERS WERE INSTALLED AT ENGINE OVERHAUL. ENGINE DISASSEMBLED AT 781 HOURS TSO DUE TO PROP STRIKE. T WO LOBES AND LIFTERS WERE SPALLED, ONE SEVERELY, THE OTHER TO A LESSER DEGREE. THE TWO LOBES INVOLVED ONLY OPERATE ONE VALVE EACH. THE LOBES THAT OPERATE TWO VALVES SHOWED NO SPALLING. 1 H 7 1 3O 3 O 1A8 E275 2001100400142 20011004 00142 NM 2001 10 4 VNAA0109019 1 20010929 A 3200 BRAKE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RH FAILED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 461PS 3075 THE CREW REPORTED THATTHE FIRST OFFICERS BRAKES WERE INEFFECTIVE. THE AIRCRAFT WAS FERRIED TO PIT. MAINTENANCE INSPEC TED AND BLED THE BRAKES IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND T HE AIRCRAFTWAS RELEASE D FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001101500127 20011015 00127 EU 2001 10 15 ZWYA100172 1 20010627 A 6510 SHAFT AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR G/B DAMAGED A ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365SJ 2252 6018 TAIL ROTOR OUTPUT SHAFT STUDS FOR HUB ATTACHMENT, BADLY STEPPED. REMOVED AND REPLACED TAIL ROTOR GEARBOX. 1 G 7 2 3U 3 U H10EU E19EU 2001101800039 20011018 00039 NE 2001 10 18 ABXA010536 2 20011015 A 7200 JT8D7B ENGINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7B 52053 NE LEFT FAILED A ABXA O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 23 982AX 4441 47317 657631 CLIMBING THROUGH FL 190, CREW HEARD A LOUD POP AND NOTICED THE LEFT ENGINE HAD DECREASED TO 1.35 EPR AND THE EGT HAD INC REASED TO 550. OPERATED ENGINE AT REDUCED POWER AND RETURNED TO LAND. REPLACED THE NR 1 ENGINE IAW DC-9 JOB CARD 90900 10 AND DC-9 8A & 8B. OPS CHECKED GOOD. 2 L 7 2 4F 4 F A6WE E2EA 2001111500023 20011115 00023 NM 2001 11 15 2001UALA02155 1 20011020 A 3510 OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 827UA 1022 CREW REPORTING OXYGEN LEVEL AT 20 PSI AND CONFIRMED NO OXYGEN AT THE MASK. MAINTENANCE WAS UNABLE TO DUPLICATE THE CAUS E OF LOSS OF OXYGEN PRESSURE. THE O2 BOTTLE WAS REPLACED SINCE IT HAD FALLEN BELOW 100 PSI. 2 L 7 2 4F 4 F RT A28NM E40NE 2001111500045 20011115 00045 NM 2001 11 15 2001UALA02213 1 20011104 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 BODY STATION 178 BULKHEAD WEB CRACK UNDER LEFT HAND LOWER RADAR ANTENNA MOUNT LBL 5 WL 202 APPROX 1 INCH CRACK. MAJOR R EPAIR ACCOMPLISHED. WEB CRACK REPAIRED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001113000030 20011130 00030 NM 2001 11 30 2001UALA02290 1 20011104 A 3234 114079015 SELECTOR VALVE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE LANDING GEAR FAULTY A UALA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 WP 29 807UA 798 LANDED UNDER AMBER ALERT DUE TO A GEAR EXTENSION AND STEERING PROBLEM. AFTER SELECTION OF LANDING GEAR DOWN ON FINAL AP PROACH, THE DOORS OPENED YET THE GEAR DID NOT EXTEND. FOLLOWED THE GRAVITY GEAR EXTEND PROCEDURES, AND THE GEAR EXTENDE D AND LOCKED WITHOUT FURTHER INCIDENT. RESET THE GEAR MANUAL EXTENSION HANDLE, AND REPLACED THE LANDING GEAR SELECTOR ( SEQUENCING) VALVE. ACCOMPLISHED THE NORMAL EXTENSION/RETRACTION TEST. 2 L 7 2 4F 4 F RT A28NM E40NE 2001112700086 20011127 00086 NM 2001 11 27 2001UALA02311 1 20011120 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 922UA 26642 RIGHT HAND OVERWING FRAME AT STATION 616 RBL 65" CRACKED BELOW FLOOR. MAJOR REPAIR ACCOMPLISHEDINSTALLED DOUBLER REPAIR . 2 L 7 2 4F 4 F RT A16WE E2GL 2001120300147 20011203 00147 NE 2001 12 3 ALG2001F00034 1 20011103 A 2612 CONNECTOR SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL COCKPIT LOOSE E ALGA K NONE L NO TEST IN INSP/MAINT 1 SW 03 376AL 760002 CAE890262S PRESTART CHECK. NR 1 ENGINE FIRE DETECTION SYSTEM WILL NOT TEST. CIRCUIT BREAKER FOUND POPPED, LOOSE CONNECTION IN T H ANDLE FOR BULBS. 1 G 7 2 3U 3 U H1NE E1GL 2001121200051 20011212 00051 WP 2001 12 12 01FDEA01028 1 20011204 A 7930 WARNING LIGHT DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL COCKPIT ILLUMINATED A FDEA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 25 372FE 46610 451550 ALL IND NORMAL EXCEPT OIL STRAINER CLOG LIGHT CAME ON. SHUTDOWN ENG LIGHT STAYED ON. 2 L 7 3 4F 4 F A22WE E23EA 2001121400078 20011214 00078 CE 2001 12 14 HYI2001F00013 1 20011121 A 2460 CM358950 MASTER SWITCH BEECH 45 D45 1152012 CE CONT O520 TSIO520* 17040 SO INST PANEL FAILED E HYIA K NONE L NO TEST IN INSP/MAINT 1 NE 01 13616 1000 BG345 ON PREFLIGHT INSPECTION, AVIONICS MASTER SWITCH FAILED. MAINTENANCE REPLACED SWITCH AND RETURNED AIRCRAFT TO SERVICE. 1 L 7 1 3O 3 O 5A3 E8CE 2001123100130 20011231 00130 NE 2001 12 31 RAIA00112003 2 20011206 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE LEFT FLAMED OUT A RAIA D RETURN TO BLOCK X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 CE 03 567HK 41085 75092 5482-STL-DURING TAXI LEFT ENGINE FLAMED OUT. MAINTENANCE TROUBLESHOT, ADJUSTED LEFT ENGINE DECELERATION SCHEDULE, AND P ERFORMED OPERATIONAL CHECK PER J41 MM 72-00-00. 2 L 7 2 4T 4 T RT A41NM E18NE 2002010300108 20020103 00108 NM 2002 1 3 2001UALA02421 1 20011217 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 24193 BODY STATION 178 LBL 5.7 WL 200 HAS CRACK INDICATION WITH NON-DESTRUCTIVE TESTING. MAJOR REPAIR ACCOMPLISHED. FABRICAT ED AND INSTALLED DOUBLER AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002011000009 20020110 00009 NM 2002 1 10 AUS20011097 1 20011016 A 5311 FRAME BOEING 737 737376 NM CFMINT CFM56 CFM563C 13802 EU FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) AFT PRESSURE BULKHEAD FRAME CHORD CRACKED AT BOLT HOLE 11R. CRACK LENGTH 19.05MM (0.75IN). 2 L 7 2 4F 4 F RT A16WE E21EU 2002011000164 20020110 00164 NM 2002 1 10 2001UALA02485 1 20011231 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 338UA 24242 STATION 1006, WL 208 LBL 26, FLOORBEAM MATERIAL LOSS AFTER CORROSION REMOVAL EXCEEDS LIMITS. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED FLOORBEAM REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002011800065 20020118 00065 NE 2002 1 18 VE32002F00003 2 20011205 A 7321 0164248850 FUEL CONTROL SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE ENGINE LEAKING A VE3R K NONE K FLUID LOSS IN INSP/MAINT 1 WP 23 229LA 452 3317 9699 DATE: 11-27-2001, DURING ROUTINE INSPECTION, A PUDDLE OF FUEL WAS NOTICED ON THE GROUND, UNDER THE ENGINE DECK DRAIN. F URTHER INSPECTION IDENTIFIED THE SOURCE OF THE LEAK AS THE FUEL CONTROL UNIT. THE FCU WAS LEAKING FROM THE FCU DRAIN. REPLACEMENT OF THE FCU WAS NECESSARY TO CORRECT THIS PROBLEM. MFG WAS NOT OFFERED A CAUSE FOR THIS LEAK. 1 G 7 1 3U 3 U H9EU E19EU 2002020500130 20020205 00130 EA 2002 2 5 CA011219001 1 20011218 A 3020 3475 SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE R/H 14TH STAGE DAMAGED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) CLIMBING THROUGH 2,000 FEET R 14TH DUCT WARNING MESSAGE WAS GENERATED. RETARDED PL AS PER QRH. MESSAGE WENT OUT. RT 14TH DUCT LIGHT AND RT14TH DUCT MESSAGE ILLUMINATED WITH RED FLOW LINE BETWEEN RT 14TH STAGE SOV, NOSE COWL AND WI NG SOV AT POWER ABOVE 80 PERCENT N1. RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED A DEFECTIVE SEAL FOR THE RT ENG INE COWL ANTI-ICE DUCT AT THE PYLON DISCONNECT. OPERATED RT ENGINE AT TO POWER FOR 20 MINUTES WITH NO FURTHER PROBLEMS. NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021300025 20020213 00025 EA 2002 2 13 CA011217007 1 20011212 A 5610 NP1393226 WINDOW CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED W O OTHER O OTHER CR CRUISE 1 CA (CAN) RT WINDOW CRACK IN CRUISE. RIGHT WINDOW REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2001102200041 20011022 00041 NM 2001 10 22 QXEA0101662 1 20011009 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS CORROSION AT STATION X422.0 THROUGH X423.0 ON UPPER SURFACE. REPAIRED IAW RD 8- 53-1342. 2 H 7 2 4T RT A13NM 2001033000126 20010330 00126 WP 2001 3 30 MWEA010221 1 20010302 A 5321 995791820 FLOOR PANEL DOUG DC9 DC932 3022066 WP CABIN MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 209ME 47730 CABIN FLOOR PANEL E3 HAS MISDRILLED HOLES ALONG ONE SIDE. REMOVED, FABRICATED AND INSTALLED PANEL SKIN. 2 L 7 2 4F A6WE 2001042600054 20010426 00054 NM 2001 4 26 SWAA010956 1 20010329 A 5754 65C30462 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 624SW 27934 DURING SCHEDULED 1/2D CHECK, FOUND RT WING L/E INBD FORE FLAP LOWER SKIN DELAMINATED AT INBD END. REPAIRED FORE FLAP PE R SRM. 2 L 7 2 4F RT A16WE 2001072600064 20010726 00064 NM 2001 7 26 2001UALA01266 1 20010629 A 3350 LIGHT BOEING 767 767222 1385122 NM CABIN MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 607UA 21868 CABIN DOOR 2 LT OVER DOOR EMERGENCY LIGHTS (3) ON ALL TIME. 2 L 7 2 4F RT A1NM 2001112600083 20011126 00083 EU 2001 11 26 QXEA0101850 1 20011109 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LT WING FUEL ACCESS PLATE 73B, MATING FLANGE ON WING SHOWS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 51-30-03, PAGES 703-704, PARAGRAPH 3-C STEPS 1 -10. 2 L 7 2 4F RT A20EU 2001071800032 20010718 00032 NM 2001 7 18 2001UALA00973 1 20010610 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 317UA 23949 FWD GALLEY DOOR AFT CUTOUT FRAME CRACKED. INSTALLED REPAIR ANGLE DOUBLER. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001080900182 20010809 00182 WP 2001 8 9 MWEA010928 1 20010612 A 5320 9915580117 ANGLE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 RIGHT LAVATORY TOP STIFFENER FRAME ON AFT PRESSURE BULKHEAD THE INBOARD ANGLE THAT ATTACHES TO THE DOOR FRAME IS CRACKED . REMOVED DAMAGE, FABRICATED, LOCATED AND INSTALLED NEW ANGLE. 2 L 7 2 4F A6WE 2001081300004 20010813 00004 EU 2001 8 13 C2XA01IA324 1 20010810 A 3350 NSA931320050 CIRCUIT BREAKER AEROSP ATR42 ATR42320 8680930 EU COCKPIT POPPED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15818 153 BTR - DURING PREFLIGHT INSPECTION, THE RIGHT HAND AFT EMERGENCY EXIT HATCH EXIT SIGN WAS FOUND TO BE INOPERATIVE. MAINTE NANCE TROUBLESHOT THE ASSOCIATED WIRING, AND RESET THE EMERGENCY LIGHT CIRCUIT BREAKER, AND THE AIRCRAFT WAS APPROVED FO R RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2001032200203 20010322 00203 NM 2001 3 22 DLM88010323 1 20010223 A 2120 36280 SMOKE DETECTOR DOUG MD88 MD88 3023688 NM AFT LAVS ACTIVATED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 923DL 10142 49705 P80509 AFTER T/O, THERE WAS A DEICING FLUID ODOR AND HAZE IN THE CABIN. BOTH AFT LAVS AND FWD LAV SMOKE DETECTOR ACTIVATED. H AZE AND ODOR DISSIPATED AND DIDN''T RETURN. PERFORMED DUCT BURNOUT PROCEDURE. 2 L 7 2 4F RT A6WE 2001073000076 20010730 00076 NM 2001 7 30 UPS01436094 1 20010603 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:C M/D - BS 1580 LBL 85 FLOORBEAM CORROSION FOUND. M/D FLOORBEAM AT BS 1580 LBL 68 - LBL 123 REPAIRED PE R SRM 51-40-04 FIG 1. 2 L 7 4 4F A20WE 2001021600297 20010216 00297 NM 2001 2 16 UPS01234854 1 20010204 A 3350 LIGHT BOEING 727 727247 138408F NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 209UP 21698 INSPECTION TYPE:IN EMERGENCY LIGHTS ARMED AMBER LIGHT INOP. RELAMPED, OPS CK NORMAL. 2 L 7 3 4F A3WE 2001092600056 20010926 00056 WP 2001 9 26 01FDEA00717 1 20010814 A 2720 ABH72392 ARM DOUG DC10 DC1010 3022110 WP RUDDER PEDAL CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 390FE 46624 CAPT'S RUDDER PEDAL LT SIDE ARM ASSY IS CRACKED AT LINK ATTACH POINT. REMOVED AND REPLACED ARM ASSY PER CMM 27-21-02. 2 L 7 3 4F A22WE 2001050300200 20010503 00200 NM 2001 5 3 01FDEA00266 1 20010406 A 5711 SPAR BOEING 727 72725C 138400H NM CNTR WING BOX CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 124FE 19360 DURING ROUTINE INSP, FWD FACE OF THE BS 870 BULKHEAD BL 0 UP 9 INCHES FROM OPEN FOR HOT AIR DUCT IN KEELBEAM FOUND CORRO DED. *S/D* REPAIRED REAR SPAR WEB PER IAW FEDEX EA 7-5710-57223. 2 L 7 3 4F A3WE 2001071600099 20010716 00099 2001 7 16 SIMA200114601 4 20010526 A 3442 M15853505 RADAR AEROSP ATR72 ATR72212 EU WEATHER RADAR INOPERATIVE A SIMA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 288AM 288 DFW - FLT 3717 - CREW REPORTED THE WEATHER RADAR TO BE INOPERATIVE. AIRCRAFT WAS RETURNED TO DFW TO WEATHER IN HRL. MA INTENANCE REMOVED AND REPLACED THE WEATHER RADAR R/T UNIT. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERV ICE. (M) 2 H 7 2 4T RT A53EU 2001120500024 20011205 00024 NM 2001 12 5 DL72S011770 1 20011107 A 3350 LIGHT BOEING 727 727232 1384082 NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 527DA 21587 RIGHT AFT OVERWING AND LT FWD OVERWING EMERGENCY EXIT LIGHTS INOP ON EXTERIOR OF ACFT. REPLACED LAMPS, RACKS AND BATTER IES. ALL POSITIONS OPERATIONAL EXCEPT LT FORWARD POSITION. RECRIMPED SPLICE 2480 REF WDM 33-51-01. OPS CHECKS GOOD. 2 L 7 3 4F A3WE 2001072400013 20010724 00013 NM 2001 7 24 2001UALA01046 1 20010617 A 3397 WIRE BOEING 777 777222 1385219 NM CABIN SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 778UA 26940 EMERGENCY LIGHTS ON SEATS ARE INOP FROM SEAT 31-43 RIGHT AND LEFT SIDE. SUPPLEMENTAL DATA UPDATE CAUSE: MAINT. FOUND A P INCHED/SHORTED WIRE UNDER SEAT PAN AT SEAT 31C WHICH RESULTED IN A BLOWN FUSE AT THE POWER SUPPLY. CORRECTIVE ACTION: MA INT. REPAIRED WIRE & REPLACED THE BLOWN FUSE IN THE POWER SUPPLY. 2 L 7 2 4F RT T0001SE 2001013100147 20010131 00147 2001 1 31 SWIA972284 4 20010119 A 2211 CONTROL PANEL EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE AUTO PILOT MALFUNCTIONED A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 568SW 120343 AFTER TAKEOFF, AUTO PILOT TURNED ON BY ITS SELF. RETURNED TO FIELD. WHILE ON THE GROUND THE AUTO PILOT TURNED ON BY IT S SELF. RAN THE TRIM WHEEL FULL NOSE DOWN AFTER DISCONNECTING AND TRANSFERRING TO FIRST OFFICERS SIDE IT AGAIN TURNED ITSELF ON. REPLACED AUTO PILOT PANEL. OPS CHECKS GOOD. S/N ON: 1689, S/N OFF: 2176. 2 L 7 2 4T 4 T RT A31SO E20NE 2001020500011 20010205 00011 NM 2001 2 5 2001UALA00008 1 20010105 A 2131 CONTROLLER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN PRESSURE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7458U 21912 UNABLE TO CONTROL CABIN PRESSURIZATION DURING CLIMB TO 31,000 FEET. AIRCRAFT DIVERTED TO ATL. *S/D* SUSPECTED PRESSUR E CONTROLLER. REPLACED PRESSURE CONTROLLER. 2 L 7 3 4F 4 F A3WE E2EA 2001021300424 20010213 00424 SO 2001 2 13 SWIA972307 1 20010122 A 6123 RELAY EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE AUTOFEATHER SYS FAILED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 292SW 120319 WHEN CLEARED FOR TAKEOFF, SET CONDITION LEVERS TO MAXIMUM, AUTO FEATHER AURAL WARNING SOUNDED. ABORTED TAKEOFF. WHEN T /O POWER SET FIRST OFFICER NOTICED RIGHT NP DID NOT SPOOL UP TO 65 PERCENT. REPLACED REVERSION (EEC) RELAYS K0059, K006 0 PER WM 20-00-00, AND PERFORMED ENGINE TRIM PER PWC MM 72-00-00. REPLACED K0161 AUTO FEATHER SYSTEM ARM RELAY AS A PRE CAUTION PER WM 20-00-00. RAN ENGINES AT TAKEOFF POWER WITH MATCHED POWER LEVERS, ALL PARAMETERS AND INDICATIONS CHECKED NORMAL. PERFORMED AUTO FEATHER CHECK PER MM 61-10-00, ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001030100124 20010301 00124 NM 2001 3 1 SCNA01014 1 20010208 A 7312 457311381 FUEL HEATER BOEING 737 7378Q8 13844BX NM CFMINT CFM567 CFM567B2US 13802 NE RT ENGINE LEAKING A SCNA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 GL 15 800SY 30627 DURING FLIGHT EXCESSIVE FUEL BURN WAS NOTICED ON THE RIGHT ENGINE, THE CREW RETURNED THE AIRCRAFT TO MSP. MAINTENANCE F OUND THE NUMBER TWO ENGINE SERVO FUEL HEATER LEAKING. REMOVED AND REPLACED THE NUMBER TWO ENGINE SERVO FUEL HEATER. PE RFORMED IDLE POWER LEAK CHECK, LEAK CHECKS GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2001040400176 20010404 00176 NM 2001 4 4 2001UALA00089 1 20010206 A 3350 SWITCH BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN STUCK A UALA O OTHER O OTHER CL CLIMB 1 WP 29 615UA 21876 ON CLIMBOUT OF JFK, EMERGENCY SIGN LIGHTS ON, ON RIGHT SIDE OF FIRST AND BUSINESS CLASS. *S/D* FOUND FLIGHT ATTENDANT EMERGENCY LIGHT TEST SWITCH STUCK. CYCLED SWITCH, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E3NE 2001030900174 20010309 00174 SO 2001 3 9 SWIA972359 1 20010210 A 2721 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RUDDER TRIM SEIZED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 197SW 120186 RUDDER TRIM FROZE IN ZERO POSITION IN FLIGHT. FLIGHT CONDITIONS VMC AT 7000 FEET. AFTER 10 MINUTES RUDDER TRIM WORKED FINE. INSPECTED RUDDER TRIMMING SYSTEM IAW EMB120 MM 27-23-00. WIPED MOISTURE FROM LINEAR ACTUATOR. RUDDER TRIM SYSTE M OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001032600045 20010326 00045 NE 2001 3 26 SCNA01016 2 20010221 A 7230 COMPRESSOR BOEING 727 727225 1384077 NM PWA JT8 JT8D17R 52049 NE NR 2 ENGINE STALLED A SCNA K NONE O OTHER CR CRUISE 1 GL 15 282SC 22558 689857 TWO HARD COMPRESSOR STALLS ON THE NUMBER TWO ENGINE JUST AFTER LEVELING OFF AT FL370. INSPECTED INLET AND EXHAUST, NO D AMAGE NOTED. 2 L 7 3 4F 4 F A3WE E2EA 2001032700217 20010327 00217 SO 2001 3 27 SWIA972393 1 20010218 A 7722 HARNESS EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE T6 INDICATOR LOOSE A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 582SW 120350 DURING CLIMB NUMBER ONE T6 INDICATOR (BOTH ANALOG & DIGITAL) FLUCTUATED CONTINUOUSLY +/- 200 DEGREES. OTHER ENGINE INDI CATIONS NORMAL. PROBLEM CONTINUED FOR 20-25 MINUTES, THEN T6 INDICATIONS STABILIZED DURING DESCENT, AFTER POWER REDUCTI ON. REPLACED WIRES FROM T6 PROBE HARNESS TO TERMINAL BLOCK. WIRE WAS LOOSE IN TERMINAL CONNECTION. RAN ENGINE, T6 IND ICATION NORMAL, BOTH ANALOG AND DIGITAL. NO FLUCTUATIONS AS PREVIOUSLY INDICATED. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001040300135 20010403 00135 SO 2001 4 3 CA010209022 1 20010115 A 3245 650X10 TUBE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA TIRE FAILED W O OTHER O OTHER LD LANDING 1 CA 10 (CAN) IN A 10 DAY PERIOD, 9 OCCURRENCES OF FLAT TIRES APPEARED. UPON INVESTIGATION AND TALKING WITH OTHER OPERATORS, IT WAS DISCOVERED THAT THE TUBES WERE THE PROBLEM. ALL TUBES WERE REPLACED ON MAIN AND NOSE WHEELS. NO OTHER FLAT TIRES OCC URRED AFTER REPLACEMENT. REPLACEMENT TUBES WERE THE GOODYEAR BRAND. TIRES: 650X10 AND 600X6 1 L 7 2 3O 3 O A20SO E14EA 2001040900081 20010409 00081 NE 2001 4 9 GXPA0101 2 20010202 A 7200 ENGINE AMD FALC20 FALCON 2720302 EU GE CF700 CF700* 30010 NE NR 2 STALLED E GXPA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 SW 99 613GA 77 299076 AIRCRAFT DIVERTED DUE TO NR 2 ENGINE START COMPRESSOR STALLING AT 80 PERCENT N1. ICE AND FOD CAUSE. ENGINE REPLACED. 2 L 7 2 4F 4 F A7EU E7EA 2001040900182 20010409 00182 2001 4 9 20010320CW013 4 20010209 A 3422 060304601 INDICATOR PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HSI FAILED E BSYA K NONE O OTHER IN INSP/MAINT 1 GL 07 106TG 318052002 678361A PILOT REPORTED COMPLETE HSI FAILURE ON TAKE OFF, AIRCRAFT RETURNED TO BASE. REMOVED AND REPLACED REMOTE DIRECTIONAL GYR O AND HSI INDICATOR. OPS CHECKED GOOD. 1 L 7 2 3O 3 O A20SO E14EA 2001040900242 20010409 00242 SW 2001 4 9 R7MR32718 1 20010104 A 2810 222366621103 FUEL FILTER BELL 407 407 SW ALLSN 250C 250C47B GL FUEL SYSTEM INOPERATIVE B R7MR K NONE L NO TEST IN INSP/MAINT 1 NM 07 911LN 29 53446 PRESSURE TEST INOPERTIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2001041600318 20010416 00318 NM 2001 4 16 2001UALA00355 1 20010328 A 5311 FRAME BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 AFT CARGO PIT AT BS 1197 FRAME T-CAP HAS AREAS OF CORROSION FROM BL0 TO RBL 46. MAJOR REPAIR ACCOMPLISHEDREPLACED T-CAP DUE TO CORROSION REMOVAL OUT OF LIMITS PER SRM 51-40-02 AND BAC DWG 146T1060. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041600442 20010416 00442 NM 2001 4 16 2001UALA00410 1 20010329 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 AFT CARGO PIT AT STA 1219 - 1241, STRINGER 34R IS CORRODED. MAJOR REPAIR ACCOMPLISHED REPAIRED STRINGER PER SRM 53-00-0 3, FIGURE 204. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041700145 20010417 00145 EU 2001 4 17 CA010405004 1 20010325 A 3020 M227591669 WIRE STBROS SD3 SD360 8100606 EU PWA PT6 PT6A65AR 52043 NE INTAKE ANTI-ICE CHAFED W K NONE L NO TEST IN INSP/MAINT 1 CA (CAN) NR 1 ENGINE LIP HEAT HARNESS. BOTH OF THE 2 MAIN CONDUCTORS (6 GAUGE WIRE) THAT SUPPLY CURRENT TO THE INLET HEAT O F THE L/H ENGINE WERE FOUND CHAFED COMPLETELY THROUGH THE SHIELDING OF THE WIRE. THE DAMAGE WAS FOUND JUST AFT OF THE IN LET BOOT, WHERE THE HARNESS COMES THROUGH THE ENGINE COWL AND CONNECTS TO A TERMINAL BLOCK. THE HARNESS HAD BEEN IMPROPE RLY ROUTED AND SECURED, IT WAS RUBBING ON THE E NGINE COWL. BOTH WIRES WERE REPLACED, PROPERLY ROUTED AND SECURED. AIRCR AFT RETURNED TO SERVICE. THE REMOTE CONTROL CIRCUIT BREAKER PN SM600BA WAS ALSO DAMAGED BY THE SHORT CIRCUIT. 2 H 7 2 4T 4 T A41EU E4EA 2001042500307 20010425 00307 NM 2001 4 25 AALA20010624 1 20010322 A 7100 9324M60G01 ENGINE BOEING 737 737823 13844BZ NM GE CFM56 CFM56* 13802 NE NR 2 STALLED A AALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SW 21 951AN 29538 SAN-JFK - FLT 2095 - THIRTY MINUTES INTO FLIGHT DETECTED THREE COMPRESSOR STALLS AT NR 2 ENGINE. DIVERTED BUF AND LANDE D WITHOUT FURTHER INCIDENT. REPLACED NR 2 SIDE ENGINE. (M) 2 L 7 2 4F 4 F RT A16WE E2GL 2001043000038 20010430 00038 NM 2001 4 30 2001UALA00491 1 20010405 A 3350 80181 INVERTER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 773UA 26929 FLOOR PROXIMITY EMERGENCY PATH MARKING LIGHTS (SEAT- MOUNTED) ARE INOP AT SEATS 1EF AND 3EF. SUPPLEMENTAL DATA UPDATE F OUND PIN 15 OF CONNECTOR DM33094 PUSHED BACK & LOCK BROKEN AT DR 1 R. FOUND 6 INVERTERS BLOWN IN F/C EEL SYSTEM. FOUND ALL THE BULBS BLOWN IN C/C CLASS EEL SEAT ROWS 8 & 9. REPLACED CONNECTOR DM33094, REPLACED INVERTERS, REPLACED C/C EEL BULBS, REPLACED 5 F/C EEL LUMINESCENT STRIP LIGHTS, REPLACED WIRE FROM CONNECTOR DM33094 PIN 14 TO CONNECTOR D99933J PIN 1. 2 L 7 2 4F 4 F RT T0001SE E46NE 2001043000089 20010430 00089 NM 2001 4 30 2001UALA00506 1 20010412 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 LEFT HAND STA 360 FRAME INBOARD OF STRINGER 16L FRAME INBOARD FLANGE IS DAMAGED. REPAIRED DAMAGED AREA. MAJOR REPAIR A CCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001050100143 20010501 00143 NE 2001 5 1 27515331 2 20010309 A 7261 30607016 PUMP ISRAEL 1125 ASTRASPX 4500205 EU GARRTT TFE731 TFE73140 29001 NE LT ENGINE LEAKING B QRRR K NONE K FLUID LOSS IN INSP/MAINT 1 EA 13 275RA 1533 098 P113145 OIL PUMP LEAKING THRU CASE DUE TO WORMING. REMOVED AND REPLACED PUMP. 2 L 7 2 4F 4 F RT A16NM E1NM 2001050100182 20010501 00182 EU 2001 5 1 GXPA0103 1 20010220 A 3231 CONTROL UNIT AMD FALC20 FALCON 2720302 EU GE CF700 CF700* 30010 NE MLG DOOR MALFUNCTIONED E GXPA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 25 613GA 77 AIRCRAFT MADE A RETURN LANDING, DUE TO GEAR DOORS WOULD NOT RETRACT AND CLOSE DURING LANDING GEAR RETRACTION. CORRECTIV E ACTION: EXTENDED AND RETRACTED GEAR DOOR, RECEIVED PROPER INDICATION FOR BOTH POSITIONS, VISUALLY INSPECTED ALL THREE GEAR AND SURROUNDING AREAS FOR DISCREPANCIES, NONE NOTED. COULD NOT DUPLICATE CONDITION. 2 L 7 2 4F 4 F A7EU E7EA 2001071800014 20010718 00014 NM 2001 7 18 2001UALA00678 1 20010509 A 2751 V9677418173 TRANSMITTER BOEING 737 737291 138448W NM PWA JT8 JT8D9A 52048 NE T/E FLAP FAULTY A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 980UA 21545 STICK SHAKER ACTIVATED DURING TAKEOFF. *S/D* REPLACED RIGHT FLAP POSITION TRANSMITTER. 2 L 7 2 4F 4 F A16WE E2EA 2001052300031 20010523 00031 2001 5 23 SWIA972566 4 20010512 A 3425 COMPUTER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE E/E BAY MALFUNCTIONED A SWIA A UNSCHED LANDING I FLT. ATTITUDE INST. CR CRUISE 1 NM 07 585SW 120353 FIRST OFFICERS AHRS SUPPLIES ERRONEOUS PITCH INFORMATION IN FLIGHT. PITCH VARIES 5 DEGREES NOSE UP AND DOWN. CAPTAINS F D WONT SYNC TO AIRCRAFT ATTITUDE. REPLACED NR 2 AHRS AS REQUIRED. SYSTEM OPS CHECK GOOD IAW 34-21-02. P/N 622-6190-204, S/N ON 585, S/N OFF 3085. 2 L 7 2 4T 4 T RT A31SO E20NE 2001052900038 20010529 00038 SO 2001 5 29 FWRA2001002 1 20010428 A 3340 587827 SWITCH PIPER PA32 PA32R301 7103218 SO LYC O540 IO540* 41532 EA COCKPIT WORN E FWRA O OTHER M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 AL 01 8147A 32R8013047 THE CONTACTS INSIDE THE LANDING LIGHT SWITCH HOUSING WERE DIRTY AND WORN AND APPARENTLY CAUSED A HIGH RESISTANCE CONNECT ION WHICH OVERHEATED AND BEGAN MELTING THE CASE OF THE SWITCH. THE PILOT TURNED OFF THE MASTER SWITCH UPON SMELLING SMO KE. SHE HAD THE LANDING LIGHT ON FOR APPROACH. SWITCH ARE A CONDITIONAL REPLACEMENT ITEM AND SHOULD REMAIN SO. THE CIRCUIT PROTECTION DEVICE WOULD HAVE PREVENTED ANY FURTHER DAMAGE, BUT THE PILOT DID SHUT THE MASTER OFF IMMEDIATELY. 1 L 7 1 3O 3 O A3SO 1E4 2001060600028 20010606 00028 NM 2001 6 6 2001UALA00726 1 20010514 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 AFT PIT BODY FRAME INNER CAP IS GOUGED AT BS 727C, STR 19L. SPLICED IN NEW CAP SECTION. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001072000015 20010720 00015 NM 2001 7 20 2001UALA01359 1 20010713 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 392UA 24667 TOOLING DAMAGE. STA 178 BULKHEAD, WL 198, RBL 19. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001073100237 20010731 00237 EA 2001 7 31 CA010628048 1 20010614 A 3710 35169 PUMP DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985AN14B 52008 NE VACUUM SYSTEM WORN W O OTHER J WARNING INDICATION CR CRUISE 1 CA 994 (CAN) DURING FLIGHT, PILOT REPORTED GRADUAL LOSS OF VACUUM PRESSURE. UPON INSPECTION, VACUUM PUMP SPLINE AND DRIVE SPLIN E WERE BOTH FOUND TO BE EXCESSIVELY WORN. SPLINE AND VACUUM PUMP REPLACED. 1 H 7 1 3R 3 R A806 5E1 2001080900205 20010809 00205 NE 2001 8 9 MWEA010944 2 20010612 A 7200 JT8D217C ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D217C 52053 NE LEFT MALFUNCTIONED A MWEA C E F ABORTED TAKEOFF ENGINE SHUTDOWN ACTIVATE FIRE EXT. J R WARNING INDICATION PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 31 805ME 48031 725406 ON TAKE OFF HEARD A BANG, LOST POWER ON LEFT ENGINE, ABORTED TAKE OFF, SHUT DOWN ENGINE AND DISCHARGED FIVE AGENTS. REPL ACED ENGINE. 2 L 7 2 4F 4 F RT A6WE E9NE 2001081000216 20010810 00216 EU 2001 8 10 ZWYA100156 1 20010314 A 3310 HARNESS AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT DEFECTIVE A ZWYA K NONE L NO TEST IN INSP/MAINT 1 GL 09 365SJ 6018 POTENTIOMETER CIRCUIT LIGHT, POT NR 1 WILL NOT ADJUST. REMOVED AND REPLACED LIGHT CORD. 1 G 7 2 3U 3 U H10EU E19EU 2001081300099 20010813 00099 NM 2001 8 13 2001UALA01421 1 20010719 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 EEL LIGHT INOP ON SEATS 2A AFT AND 4A FWD AND AFT. 2 L 7 4 4F 4 F RT A20WE E24NE 2001082100044 20010821 00044 NM 2001 8 21 2001UALA01689 1 20010813 A 5313 CLIP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE BS 1087 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BS 1087 STR 39L FRAME ATTACH CLIP CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED ATTACH CLIP REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082900039 20010829 00039 NM 2001 8 29 PCAA0108096 1 20010828 A 7931 54273618010 GAUGE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LEFT INOPERATIVE A PCAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 13 825EX 21062 1831 388 120827 PHL-ORH FLIGHT#3692. DURING CLIMB #1 ENGINE OIL PRESSURE GAUGE INDICATED ZERO PSI. #1 ENGINE WAS SHUT DOWN AS A PRECAUT ION AND AIRCRAFT RETURNED TO THE FIELD.MAINTENANCE REPLACED #1 OIL PRESSURE GAUGE. OPERATIONAL CHECK GOOD ON GROUND RUN- UP.AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2001082900069 20010829 00069 NM 2001 8 29 2001UALA01761 1 20010820 A 5241 FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 322UA 23954 AFT GALLEY DOOR BODY TORQUE TUBE UPPER HINGE ARM HOUSING CRACKED AT INBOARD LOWER CNTR FASTENER HOLE. MAJOR REPAIR ACCO MPLISHED. REPLACED HINGE ARM HOUSING FITTING. 2 L 7 2 4F 4 F RT A16WE E2GL 2001083100190 20010831 00190 SO 2001 8 31 EEJ2001F00000 1 20010801 A 3230 4033600 DRAG BRACE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA NLG FRACTURED A EEJA O OTHER O OTHER LD LANDING 1 NM 07 1145A 318052053 NOSE GEAR DRAG BRACE FRACTURED UPON NOSE GEAR EXTENSION, CAUSING THE NOSE WHEEL TO NOT FULLY EXTEND. UPON LANDING THE A IRCRAFT SUFFERED A NOSE GEAR COLLAPSE. CAUSE OF FRACTURE, UNKNOWN. 1 L 7 2 3O 3 O A20SO E14EA 2001090700086 20010907 00086 NM 2001 9 7 2001UALA01845 1 20010826 A 3260 WARNING SYSTEM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT ACTIVATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 349UA 24253 UNSCHEDULED LANDING. AFTER TAKEOFF, GEAR SELECTED UP, GOT GEAR WARNING LIGHTS AND HORN. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091700027 20010917 00027 EA 2001 9 17 SWIA972632 1 20010613 A 2741 SWITCH CNDAIR CL600 CL6002B19 EA GE CF34 CF34* NE COCKPIT FAILED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 410SW 7066 STAB TRIM CH NR 1 & 2 AND MACH TRIM ALL DISENGAGED SHORTLY AFTER TAKE OFF, RETURNED FOR LANDING. INSTALLED NEW STAB TRIM DISCONNECT SWITCH ON FIRST OFFICER'S SIDE. PN 996-0013. OPS CHECK GOOD, OK FOR CAT II OPERATIONS. 2 L 7 2 4F 4 F RT A21EA E15NE 2001091700052 20010917 00052 NM 2001 9 17 2001UALA01980 1 20010906 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 324UA 23956 AFT PIT FRAME STATION 727E AT STRINGER 26R HAS TOP FLANGE GOUGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001091700145 20010917 00145 NM 2001 9 17 VNAA0108019 1 20010828 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 432JS 11885 110 3045 THE CREW REPORTED THAT THE EMERGENCY EXIT SIGN WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 6LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001092400020 20010924 00020 EA 2001 9 24 CA010912010 1 20010906 A 5410 601350061 WEB BOMBDR 60135006 CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ENGINE SUPPORT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 18071 (CAN) DURING COMPLETION OF ASB 601R-53-61-059 FOUND UPPER WEB OF ENGINE SUPPORT BEAM CRACKED NEAR L & RBL 9.0 AT FS 640. ALSO FOUND HOLES IN SUPPORT ANGLE CRACKED AT RBL 7.5 AND 8.5 (FOUND BY NDT). ALSO FOUND 1/2 INCH CRACK IN LOWER WEB NEA R RBL 36.20 IN THE FWD INBOARD COARNER OF THE ACCESS PANEL LANDING. LHS AT LBL 36.20 PREVIOUSLY REPAIRED IAW REO 601R-53 -61-327.REPAIRED IAW REO 601R-53-61-345 (UPPER AN LOWER WEBS) AND REO 601R-53-61-428. INSTALLED REO 601R-53-61-366 (BOTH SIDES). 2 L 7 2 4F 4 F RT A21EA E15NE 2001092500015 20010925 00015 EA 2001 9 25 PNS2001F00000 2 20010831 A 7414 103492901 MAGNETO PIPER PA32 PA32301 7103207 SO LYC O540 IO540* 41532 EA LEFT MALFUNCTIONED A PNSA K NONE O OTHER IN INSP/MAINT 1 AL 03 8259V 251 328006097 AIRCRAFT WOULD START ON LEFT MAGNETO BUT WOULD NOT RUN WHEN SELECTED TO THE LEFT MAGNETO. MAGNETO DISTRIBUTOR GEAR TO C AP SHOWS A LOT OF TIPPING PLAY WITHOUT DISASSEMBLY. GROUND RUN: RAN A LITTLE ROUGH AND THEN QUIT. 1 L 7 1 3O 3 O A3SO 1E4 2001092700002 20010927 00002 NE 2001 9 27 SWIA200110179 2 20010908 A 7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LEFT MALFUNCTIONED A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 NM 07 200CD 1321 1321 120200 LEFT ENGINE LOST POWER INFLIGHT, PRECAUTIONARY ENGINE SHUT DOWN CHECK COMPLETED.REMOVED AND REPLACED LEFT ENGINE ASSY WI TH SERVICEABLE UNIT. COMPLIED WITH ALL ITEMS ON ENGINE INSTALLATION CARD. NO DEFECTS NOTED. OPS CHECKS GOOD ON ENGINE RUNSPN ON: PW118 SN ON: 115424 SN OFF: 115238 2 L 7 2 4T 4 T RT A31SO E20NE 2001101000015 20011010 00015 NE 2001 10 10 F3LA200100112 2 20011004 A 7200 JT8D15 ENGINE BOEING 737 7372P6 NM PWA JT8 JT8D15 52051 NE RIGHT OUT OF RIG A F3LA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 NM 03 272 41739 360 21613 878070 ABORTED TAKEOFF. FLIGHT CREW REPORTED NR 2 ENGINE WOULD ONLY PRODUCE 2.0 EPR OF THE REQUIRED 2.05. PUSHED RT THROTTLE ALMOST TO FWD STOP WITH NO FURTHER THRUST. ABORTED TAKEOFF AT 90 KNOTS. PERFORMED ENGINE RUN AND FOUND ALL PARAMETERS FOR NR 2 ENGINE LOWER. TRIMMED NR 2 ENGINE PER MM 72-02-200, PAGE 201. ALL PARAMETERS CHECKED NORMAL. PERFORMED HIGH ENERGY STOP INSPECTION PER MM 05-51-111 WITH NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A16WE E2EA 2001110800088 20011108 00088 NM 2001 11 8 2001UALA02192 1 20011031 A 3350 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BATTERY PACK BLOWN A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 198UA 28716 EMERGENCY LIGHT ASSEMBLIES 1 AND 2 INOP RIGHT WING FILLET PANEL. REPLACED BATTERY PACK FUSE. OPS CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2001121100032 20011211 00032 NE 2001 12 11 FE62001F00000 2 20010921 A 7310 5282009109 FITTING PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE ENGINE LEAKING B FE6R O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 11 209PB 1100 209 PCEPR0065 FLIGHT CREW REPORTS FUEL SMELL IN COCKPIT. MAINTENANCE FOUND RAW FUEL IN THE ENGINE COWLING. FUEL IS NOTED TO BE SEEPI NG FROM THE INLET FITTING (ADAPTER) ON THE LOW PRESSURE ENGINE DRIVEN FUEL PUMP. REPLACING THE ADAPTER RESOLVED THE DIS CREPANCY.(K) 1 L 7 1 3T 4 T RT A78EU E26NE 2001121800038 20011218 00038 NM 2001 12 18 2001UALA02368 1 20011205 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 337UA 24241 EXTERNAL FUSELAGE STATION 240 8 INCHES ABOVE LOWER SKIN LAP DENTED. MAJOR REPAIR ACCOMPLISHED, ACCOMPLISHED DOUBLER REP AIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2001122000061 20011220 00061 NE 2001 12 20 AALA20011811 2 20010924 A 7314 BPU200MK2 PUMP BOEING 757 757223 1384957 NM RROYCE RB211 RB211535* NE NR 1 ENGINE LEAKING A AALA K NONE X ENGINE FLAMEOUT DE DESCENT 1 SW 21 181AN 29591 DFW - FLT 2499 - EN ROUTE SAT-DFW - UPON DESCENT, NR 1 ENGINE SHUTDOWN. LANDED DFW WITHOUT FURTHER INCIDENT. REPLACED LOW PRESSURE FUEL PUMP. LEAK CHECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2002011000173 20020110 00173 NM 2002 1 10 2001UALA02494 1 20011230 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 AFT PIT BODY FRAME INNER FLANGE HAS A DENT BODY STATION 1500, STRINGER 26L-27L. MAJOR REPAIR ACCOMPLISHED. INSTALLED D OUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002020500129 20020205 00129 EA 2002 2 5 CA011217012 1 20011205 A 2133 OUTFLOW VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE VALVE SEAT CONTAMINATED W A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DE DESCENT 1 CA (CAN) A/C EXCEEDED 10,000 FT CABIN ALTITUDE DESCENDING THROUGH FL. 240. OXYGEN MASKS DEPLOYED AUTOMATICALLY. PRECEEDED BY CABIN ALT CAUTION. TRIED ALT CONTROLLER & MANUAL W/O SUCCESS IN PREVEN TING CABIN CLIMBING. DECLARED EMERG&MADE UNSC HEDULED LANDING AT SHENANDOAH. PASSENGERS DISEMBARKED THROUGH OVERWING EMERGENCY EXIT DUE TO F/A DECLARING SMELL OF SMO KE IN CABIN (BELIEVED TO BE NORMAL ODOUR OF CHEMICAL O2 GENERATORS). 2 L 7 2 4F 4 F RT A21EA E15NE 2002020600027 20020206 00027 EU 2002 2 6 AUS20011433 1 20010930 A 3260 SWITCH FOKKER F28 F28MK4000 4990810 EU RROYCE SPEY SPEY55515 54521 EU MLG OUT OF ADJUST W O OTHER O OTHER NR NOT REPORTED 1 AU S (AUS) RT MAIN LANDING GEAR GROUND / FLIGHT SWITCH OUT OF ADJUSTMENT. 2 L 7 2 4F 4 F RT A20EU E2EU 2002021100080 20020211 00080 NM 2002 2 11 CA011126005 1 20011120 A 3230 8320506003 RELEASE CABLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE MLG BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING A ROUTINE MAINTENANCE LINE CHECK, THE MLG ALTERNATE RELEASE CABLE IN THE COCKPIT WAS FOUND FRAYED. WHEN THE HANDLE FOR THE RELEASE WAS PULLED, THE CABLE BROKE. THE CABLE WAS REPLACED WITH A SERVICEABLE ASSEMBLY AND ALL FURTHER CHECKS WERE COMPLETED PRIOR TO RETURNING THE AIRCRAFT TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002021400011 20020214 00011 EA 2002 2 14 CA011231001 1 20011230 A 2915 3811208102 RELIEF VALVE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE HYD SYSTEM LEAKING W O OTHER J WARNING INDICATION CR CRUISE 1 CA 99999 99999 (CAN) DURING CRUISE ON POSITIONING FLIGHT INDICATION OF PROGRESSIVE NR 2 SYSTEM HYDRAULIC FAILURE, NR 2 HYD FLUID HOT C AUTION LIGHT, 15 MINUTES LATER, RUDDER PRESSURE & RUDDER FULL PRESSURE & NR 2 RUDDER HYD CAUTION LIGHTS ILLUMINATED, ON ARRIVAL ALTERNATE LANDING GEAR EXTENSION SYSTEM USED. AIRCRAFT LANDING NORMALLY . INVESTIGATION FOUND RELIEF VALVE O N NR 2 HYDRAULIC RESERVIOR LEAKING AND HAD DRAINED HYDRAULIC FLUID OVERBOARD, SYTEM WAS FULL OF AIR . RELIEF VALVE REPL ACED, HYD OVER-TEMP SWITCH, ENGINE HYDRAULIC PUMP, AND HYD LOW LEVEL SWITCH REMOVED FOR INSPECTION. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002031300073 20020313 00073 CE 2002 3 13 CVU2002F00001 1 20011220 A 3710 442CW PUMP BEECH 80 65B80 1152812 CE LYC O720 IO720* 41546 EA VACUUM SYSTEM FAILED E CVUA K NONE O OTHER IN INSP/MAINT 1 WP 13 46MA 795 LD413 VACUUM PUMP, PUMP FAILED UNDER NORMAL OPERATING CONDITIONS. 1 L 7 2 3O 3 O 3A20 1E15 2002052100015 20020521 00015 EU 2002 5 21 R7M2002F00015 1 20010928 A 7720 430150102 THERMOCOUPLE BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ENGINE SHORTED B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 420MB 9097 7077 LE45385EA THERMOCOUPLE HAS AN INTERNAL SHORT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2002053100030 20020531 00030 NM 2002 5 31 RYN2002F00002 1 20010805 A 5100 SKIN BOEING 727 72721 1384003 NM PWA JT8 JT8D1 52044 NE BS1085-BS1110 DAMAGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 357QS 19259 BULGING AND PILLOWING SKIN AT BS 1085 THRU BS 1110 ALONG FASTENER ROWS AT STRINGER 17R THRU 19R ON EXTERNAL FUSELAGE. A CCOMPLISHED FUSELAGE SKIN REPAIR FROM BS 1085 TO BS 1110 BETWEEN STRINGER 17R AND 19R DUE TO CORROSION IAW MFG ENGINEERI NG RO. (MATERIAL USED 2024-T3 .090 INCHES, 86 INCHES X 38 INCHES. 2 L 7 3 4F 4 F A3WE E2EA 2001032700255 20010327 00255 NM 2001 3 27 AWXA0001459 1 20010302 A 5320 6545833440 WEB BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 VISUAL INSPEC FOUND 1 INCH CRACK IN COCKPIT FLOOR WEB EMANATING FROM LIGHTENING HOLE AT FS 180 LBL 29 WL 207; CONFIRMED HFEC. REMOVED CRACKED WEB; DRILLED AND INSTALLED NEW WEB IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2001120300055 20011203 00055 NM 2001 12 3 SWAA013207 1 20011128 A 5311 96380 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 364SW 26575 DURING SCHEDULED SPECIAL VISIT, FOUND BOTH LT AND RT OUTBOARD CHORD ANGLES CRACKED AT BS 178, WL 207. REMOVED AND REPLA CED CHORD ANGLES PER SWA ACO. 2 L 7 2 4F RT A16WE 2001050700411 20010507 00411 EU 2001 5 7 SIMA0594 1 20010228 A 3350 LIGHT SAAB SF340 340B 7860101 EU COCKPIT MALFUNCTIONED A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 297AE 340B297 YOW - FLT 4598 - FOUND EMERGENCY LIGHT ON OVERHEAD PANEL ILLUMINATED WHEN ALL SWITCHES WERE IN NORMAL POSITION. ALL EME RGENCY BUS SYSTEMS POWERED. CREW PLACARD ISSUED MEL 24-9. OPS CHECKED EMERGENCY POWER LIGHT SYSTEM IAW SAAB AMM 33-60- 00. NO DEFECTS NOTED AT THIS TIME. (M) 2 L 7 2 4T RT A52EU 2001072400453 20010724 00453 NM 2001 7 24 2001UALA01202 1 20010627 A 5311 FRAME BOEING 737 737522 138449F NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 910UA 25254 OVERWING BODY FRAME INNER CHORD LEFTSIDE, CRACKED AT BOTTOM FASTENER, AT BS 616. REMOVED DAMAGE. INSTALLED FILLER AND ANGLE REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2001072600300 20010726 00300 NM 2001 7 26 2001UALA01339 1 20010709 A 2740 TRIM MOTOR BOEING 737 737522 138449F NM HORIZ STAB MALFUNCTIONED A UALA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 921UA 25388 UNSCHEDULED LANDING DUE TO HORIZONTAL STABILIZER ELECTRIC TRIM MOTOR PROBLEMS. 2 L 7 2 4F RT A16WE 2001042600040 20010426 00040 NM 2001 4 26 01FDEA00264 1 20010406 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM CABIN CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 124FE 19360 DURING ROUTINE INSP, NR 3 SEAT TRACK FOUND CORRODED FROM BS 640-740. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 53-1 0-5. 2 L 7 3 4F A3WE 2001042600092 20010426 00092 EA 2001 4 26 ASOA01001 1 20010105 A 7830 THRUST REVERSER CNDAIR CL600 CL6002B19 EA ENGINES MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 11 848AS 7339 FLT 4613 - DURING FIGHT FROM LGA-RIC, CREW RECEIVED A RIGHT THRUST REVERSER UNLOCK MESSAGE. THE RIGHT THRUST LEVER DID NOT RETARD TO IDLE. THE AIRCRAFT WAS CONTROLLABLE WITH NO BUFFET OR YAW. THE CREW FOLLOWED THE CHECKLIST AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED SAFELY IN RIC. MAINTENANCE CYCLED THE THRUST REVERSER MANUALLY SEVERAL TIMES AND RAN ENGINES AND DEPLOYED PNEUMATICALLY SEVERAL TIMES WITH NO DEFECTS. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2001072400135 20010724 00135 NM 2001 7 24 2001UALA01098 1 20010619 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 588 STR 37R - 38R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IAW BAC DRAWING 14 0T2102-221 AND SRM 51-40-02. 2 L 7 2 4F RT A1NM 2001070200158 20010702 00158 NM 2001 7 2 SWAA011646 1 20010605 A 3350 207377 LENS BOEING 737 7377H4 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 748SW 29800 EEPLS LIGHT LENS BROKEN AT FWD CABIN. Removed and replaced EEPLS LENS PER MM. 2 L 7 2 4F RT A16WE 2001072600088 20010726 00088 NM 2001 7 26 2001UALA01283 1 20010629 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 AFT PIT T-CAP CORRODED BS 1175, LBL 6-RBL 25. 2 L 7 2 4F RT A1NM 2001050700213 20010507 00213 EU 2001 5 7 QXEA0100573 1 20010328 A 5310 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 YYC- CRACKED CASTELLATION AT FRAME 13815 AND STRINGER 33. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 2001042600065 20010426 00065 NM 2001 4 26 P5CA0100476 1 20010226 A 5320 PANEL BOEING 747 7472U3B NM BULKHEAD CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 922FT 22768 CRACK FOUND AT CANTED RPESSURE BULKHEAD R/L CLOSURE PANELS AT WEB STA 1240. REPAIRED PER SRM 53-10-02 AND 8110-3 SB 747 -53-2329. 2 L 7 4 4F RT A20WE 2001082300080 20010823 00080 WP 2001 8 23 DHL2001804534 1 20010819 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 FLT COMPT 680 FLOOR PANEL SUPPORT ANGLE CRACKED (1.5 INCH) STA 8.000 THRU STA 12.000, RBL 14. REMOVED CRACKED SUPPORT A NGLE PER SRM 51-1-21 PG 1. FABRICATED NEW ANGLE. INSTALLED NEW ANGLE PER SRM 53-2-0 PG 2E AND 2F AND 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2001052200109 20010522 00109 NM 2001 5 22 01FDEA00322 1 20010501 A 5330 65256072 DOUBLER BOEING 727 727225 1384077 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 468FE 21452 BULGING SKIN AT AFT LAV PAN UPPER FWD CORNER AND AFT LOWER CORNER. *S/D* REMOVED, REPLACED AND FAB NEW DOUBLER AND AFT LAV PAN PER IAW FEDEX SRM 51-30-5, 53-10-1 AND 51-20-151. 2 L 7 3 4F A3WE 2001012500248 20010125 00248 NM 2001 1 25 VNAA0101002 1 20010101 A 7332 128832 SWITCH DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FUEL PRESSURE FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 460PS 12015 3061 DURING THE TAKEOFF ROLL, THE CREW RECEIVED A RIGHT HAND FUEL PRESSURE LOW LIGHT ILLUMINATION AND THE CREW ABORTED TAKEOF F AND RETURNED TO THE GATE. FLIGHT 4070 WAS CANCELED. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE INSPECTED AND REPLACED THE ENGINE PRESSURE SWITCH IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-00-00. OPERATIONAL CHECKS WERE PER FORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001020500171 20010205 00171 SO 2001 2 5 SWIA972291 1 20010124 A 2150 SMOKE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT PACK DETECTED A SWIA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 NM 07 218SW 120287 LEFT PACK INFLIGHT SET OFF LAV SMOKE DETECTOR. RETURNED TO PDX. REPOSITIONED RAM AIR DOOR SWITCH TO CORRECT POSITION. OPS CHECKS GOOD. SECURED PANEL AND CONTROL KNOB. 2 L 7 2 4T 4 T RT A31SO E20NE 2001040400208 20010404 00208 NE 2001 4 4 CA010302008 2 20010202 A 7321 32447593 FUEL CONTROL CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE LT ENGINE FAILED W A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 CA (CAN) DURING CLIMB AT 37,000 FEET LT ENGINE N1 ROLLED BACK TO 80 PERCENT. IGNITION SELECTED ON&ENGINE N1 RECOVERED, CLIM B CONTINUED TO 39,000 WITH IGNITION ON & AT ALTITUDE SELECTED OFF - N1 ROLLED BACK TO 80 PERCENT. IGNITION SELECTED BACK ON & N1 AGAIN RECOVERED. A/C DESCENDED TO 35,000 WITH IGNITION ON & AT ALTITUDE IGNITION SELECTED OFF - N1 AGAIN ROLLED BACK, IGNITION SELECTED ON & N1 RECOVERED. A/C DIVERTED TO CYMM WITH IGNITION SELECTED ON. TROUBLSHOOTING CARRIED OUT, FAULT COULD NOT BE DUPLICATED ON GROUND. A/C RELEASED FOR TEST FLT&ON FLT SAME DEFECT RE-OCCURRED AT 40,700. FUEL CONTR OL REPLACED 1 L 7 2 4F 4 F A22CE E1NE 2001040500254 20010405 00254 NM 2001 4 5 2001UALA00172 1 20010227 A 3412 SENSOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE AIR TEMPERATURE CONTAMINATED A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 672UA 30027 CREW REPORTS SMOKE APPEARS FROM FWD LH SIDE OF THE AIRCRAFT. CREW ALSO REPORTS SMOKE WAS COMING FROM OUTSIDE OF THE AIR CRAFT AND APPEARED WHEN THROTTLES WERE ADVANCED. SUPPLEMENTAL DATA UPDATE SUSPECTED MOISTURE IN TAT PROBE. NO EICAS OR S TATUS MESSAGE PRESENT. PERFORMED VISUAL INSPECTION FROM OUTSIDE AIRCRAFT AND IN E&E COMPARTMENT. NO DESCREPANCIES FOUND . 2 L 7 2 4F 4 F RT A1NM E24NE 2001040900457 20010409 00457 GL 2001 4 9 01FDEA00185 2 20010301 A 7200 ENGINE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 2 ENGINE FIRE A FDEA F ACTIVATE FIRE EXT. A B FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 25 375FE 46613 NR 2 ENGINE FIRE AFTER LANDING. 2 L 7 3 4F 4 F A22WE E23EA 2001041600062 20010416 00062 NM 2001 4 16 2001UALA00228 1 20010301 A 5755 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE SPOILER CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7448U 21902 NR 13 SPOILER PANEL LOWER SKIN IS CRACKED AROUND THE ACTUATOR ATTACHMENT. REPLACED SPOILER PANEL PER MM 27-61-04. RIGG ED AND OPERATIONS CHECK NORMAL PER MM 27-61-04. 2 L 7 3 4F 4 F A3WE E2EA 2001041600327 20010416 00327 NM 2001 4 16 2001UALA00366 1 20010329 A 5711 SPAR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RT WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 310UA 23671 RT WING SPAR UPPER CHORD CRACKED. REPAIRED CRACKED CHORD. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600471 20010416 00471 NM 2001 4 16 2001UALA00392 1 20010328 A 3350 BATTERY BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 675UA 29243 EMERGENCY LIGHTS INOP AT EMERGENCY EXITS R OWS 20 AB AND 21 AB. REPLACED BATTERY M1559, CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2001041700037 20010417 00037 EU 2001 4 17 CA010409002 1 20010214 A 5532 5553012211 STRAP PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL STAB FAIRING WORN W K NONE O OTHER IN INSP/MAINT 1 CA 1168 (CAN) FAIRINGS WERE REMOVED FOR OTHER WORK AND PLATE AND STRAP WERE FOUND WORN. THESE PARTS ENGAGE TO PREVENT FLUTTER OF THE FAIRINGS. THE STRAP IS RIVETED TO THE TOP OF THE REAR VERTICAL STABILIZER SPAR AND THE PLATE IS ATTACHED TO THE FAI RING. BOTH PARTS WERE REPLACED WITH NEW PARTS. ALIGNMENT WAS CHECKED AS THIS IS A NOTED PROBLEM THAT HAS CAUSED SKIN CRA CKING OF THE VERTICAL STABILIZER. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001042500289 20010425 00289 GL 2001 4 25 SIMA0774 2 20010318 A 7313 23065950A NOZZLE EMB 145 EMB145 SO ALLSN AE300 AE3007A GL FUEL SYSTEM MALFUNCTIONED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 606AE 145062 XNA - FLT 3705 - DURING FLIGHT, CREW NOTED EXHAUST SMELL IN FLIGHT COMPARTMENT AND CABIN. NOTE ANIT-ICE SYSTEM WAS ON A T THE TIME. AIRCRAFT LANDED SAFELY IN XNA. NO FURTHER INCIDENTS WERE REPORTED. MAINTNANCE REMOVED AND REPLACED THE NR 2 ENGINE FUEL NOZZLES. OPERATIONAL AND LEAK WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2001043000008 20010430 00008 NM 2001 4 30 2001UALA00523 1 20010418 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 FLOORBEAM STA 324.8 RBL 42 TO 49 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR ON T-CAP PER AMM. 2 L 7 2 4F 4 F RT A2NM E17NE 2001050300255 20010503 00255 NM 2001 5 3 2001UALA00458 1 20010409 A 2131 CONTROLLER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN PRESSURE MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7253U 21400 AIRCRAFT RETURNED TO DEN DUE TO PRESSURIZATION PROBLEMS. SUPPLEMENTAL DATA UPDATE AIRCRAFT FAILED HULL LEAK CHECK.REPAIR ED LEAKS AND TESTED OK PER MM 21-30-05. 2 L 7 3 4F 4 F A3WE E2EA 2001050300386 20010503 00386 NM 2001 5 3 2001UALA00587 1 20010426 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 FUSELAGE STA 188 RIGHT HAND FRAME CRACKED AT THE COCKPIT FLOOR LINE STRINGER 17. STOP DRILLED THE CRACK AND REPAIRED TH E FRAME. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001050700377 20010507 00377 EU 2001 5 7 CA010426009 1 20010329 A 5320 6023976007 BRACKET AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE MONITOR CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA 22947 22947 (CAN) DURING THE REMOVAL OF THE PREVIOUSLY INSTALLED MONITOR FOR LSTA C-LSA95-037/D THE NR 2 CENTRE ISLE BRACKET ASSEMBL Y FORWARD OUTBOARD SUPPORT LEG WAS FOUND TO BE CHAFED BY AIRCRAFT ELECTRICAL WIRING. THE BRACKET WAS REPLACED AS PER SON Y TRANSCOM DRAWING 600-5970. THE ELECTRICAL WIRING WAS ROUTED AS PER DRAWING AND STANDARD PRACTICES, CLEARANCES CHECKED UPON REINSTALLATION. ALL OTHER MONITOR INSTALLATION WERE CHECKED AND THERE WERE NO OTHER DEFECTS NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2001051000184 20010510 00184 EU 2001 5 10 20010507CW002 1 20010419 A 5230 260952 SUPPORT BRACKET SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE CARGO DOOR MISSING E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 73MH 1546 4556 SUPPORT FLANGE CRACKED CAUSING INLET ARI GUIDE TO FLUTTER AND BREAK AWAY FROM AIRCRAFT IN FLIGHT. FLUTTER CAUSING SECON D SUPPORT BRACKET TO FAIL. FIN DEPARTED AIRCRAFT AND STRUCK THE TAIL ROTOR SURFACE CAUSING NO OBVIOUS FLIGHT DEFECT BUT BLADE WAS DEEMED NON REPAIRABLE BY MFG. PREFLIGHT AND PERIODIC INSPECTIONS FOR CRACKS REQUIRED. 1 G 7 1 3U 3 U NC H9EU E19EU 2001051500079 20010515 00079 NM 2001 5 15 VNAA0104020 1 20010430 A 3260 LIGHT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT INOPERATIVE A VNAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 07 424JS 3033 DURING LANDING, AT THE OUTER MARKER THE CREW LOWERED THE GEAR BUT DID NOT RECEIVE THREE GREEN GEAR INDICATIONS. THE CRE W EXECUTED A GO-AROUND, REFERENCED THE QUICK REFERENCE HANDBOOK, AND A FLY BY SO ATC COULD CONFIRM GEAR WAS DOWN. ANOTH ER APPROACH WAS INITIATED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE INOPER ATIVE GEAR BULB IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCR AFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001052100032 20010521 00032 NM 2001 5 21 2001UALA00604 1 20010428 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 AFT PIT FRAME HAS EXCESSIVE MATERIAL LOSS STA 1480 STR 27R. MAJOR REPAIR ACOMPLISHED. SPLICED REPAIR FRAME SECTION BETW EEN STR 22R TO 27R. 2 L 7 2 4F 4 F RT A2NM E17NE 2001052900260 20010529 00260 NE 2001 5 29 R7MR33145 2 20010118 A 7250 430124203 BEARING BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101650B1 41560 NE TURBINE POROUS E R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 61LF 447 7230 EXCESSIVE PITTING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2001060100010 20010601 00010 NE 2001 6 1 GLBA2001103 2 20010518 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LEFT FLUCTUATES A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 01 201YQ UE201 LEFT ENGINE TORQUE FLUX, INSPECTED ALL PARAMETERS WITHIN LIMITS. RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A24CE E26NE 2001061400030 20010614 00030 NM 2001 6 14 CA010522006 1 20010501 A 2910 CASE BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE BYPASS VALVE CRACKED W A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CA 41258 41258 D8916A (CAN) AFTER TAKEOFF TRAILING EDGE FLAPS WOULD NOT RETRACT. AFTER SEVERAL ATTEMPTS FLAPS RETRACTED. FLIGHT CONTINUED, LAN DED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTION REVEALED TRAILING EDGE FLAP BYPASS VALVE MALFUNCTIONING. VALVE REPL ACED. SUBSEQUENT VALVE OVERHAUL CONFIRMED VALVE BODY WAS CRACKED. 2 L 7 2 4F 4 F A16WE E2EA 2001061800127 20010618 00127 NM 2001 6 18 2001UALA00851 1 20010511 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 BS 1153 STR 37R-38R SHEAR TIE CORRODED.SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPA IR IN ACCORDANCE WITH BAC DRAWING 140T2103-446 AND SRM51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001062700092 20010627 00092 NM 2001 6 27 2001UALA01063 1 20010618 A 2120 RELAY BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 343UA 24247 ALTERNATE EQUIPMENT COOLING EXHAUST OFF LIGHT ILLUMINATED. SUPPLEMENTAL DATA UPDATE THE R-29 BLOWER RELAY FAILED. REPLAC ED THE R-29 BLOWER RELAY AND R-30 ALTERNATE BLOWER RELAY. 2 L 7 2 4F 4 F RT A16WE E2GL 2001070300065 20010703 00065 NM 2001 7 3 2001UALA00137 1 20010219 A 3246 26069451 WHEEL BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE MLG WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 609UA 21870 FOUND NR 1 MAIN WHEEL INNER HALF RUBBING AGAINST THE BRAKE FRONT SIDE. BRAKE INSPECTED AND FOUND TO BE IN GOOD CONDITIO N PER MM. *S/D* CAUSE UNKNOWN. WHEEL AND AXLE BUILDUP WERE CORRECT WITH REMOVED WHEEL AND WITH NEW WHEEL INSTALLATION . 2 L 7 2 4F 4 F RT A1NM E3NE 2001070500003 20010705 00003 SO 2001 7 5 20010607CW003 2 20010518 A 7322 6299042 FUEL CONTROL BEECH 33 F33A 1151425 CE CONT O520 IO520* 17032 SO ENGINE DEFECTIVE A VJ3R A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 07 5587K 28 CE1392 THE PILOT REPORTED A ROUGH ENGINE IN FLIGHT AND RETURNED TO AIRPORT, A SAFE LANDING WAS MADE. MAINTENANCE GROUND RUN AI RCRAFT AND A FLUCTUATION IN FUEL FLOW WAS NOTED. THEY FOUND THAT THE MIXTURE CONTROL WAS STIFF WHEN MOVING, (POSSIBLE G ALLING). 1 L 7 1 3O 3 O 3A15 E5CE 2001072600282 20010726 00282 2001 7 26 AWXA0001965 4 20010706 A 2215 16300103 SERVO BOEING 757 757225 1384959 NM RROYCE RB211 RB211535E4 54555 NE AUTOPILOT SYS MALFUNCTIONED A AWXA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 WP 28 914AW 35690 22208 30552 EN ROUTE FROM PHX TO MCO AT FL 370 THE AIRCRAFT MADE A SUDDEN ROLL OF 20-30 DEGREES TO THE LEFT. AUTO PILOT DISENGAGED. AFTER RECOVERY TO LEVEL OF FLIGHT, NO ADVERSE YAW OR OUT OF TRIM COND EVIDENT. JUST PRIOR TO ROLL, EPR'S MATCHED, BUT N1, N2, N3, EGT & FF NOT MATCHED. THRUST LEVERS MATCHED. AFTER ROLL, RT THRUST LEVER ADVANCED 2.5 KNOBS FWD OF LEFT T O MATCH N1'S. LEFT EPR 1.95, RIGHT EPR 2.01 WITH MATCHED N1'S. IN SAT THE PROBLEM WAS TROUBLESHOT PER FIM 22-00-03/ 10 1 FIG 107, WITH ASSISTANCE FROM MAINTENANCE CONTROL. THE LEFT AILERON CONTROL SERVO WAS REPLACED PER THE AMM. LEAK CHE CKS WERE GOOD. THE NR 2 ENG FUEL FLOW GOVERNOR WAS ALSO REPLACED PER AWA TASK CARD R5M 73602. 2 L 7 2 4F 4 F RT A2NM E12EU 2001072700128 20010727 00128 NE 2001 7 27 CHQA200196528 2 20010528 A 7230 SEAL SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE FAILED A CHQA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 11 96 96 367 LT ENGINE LOST OIL PRESSURE. CREW SHUT DOWN ENGINE AND DECLARED EMERGENCY. MAINTENANCE REMOVED AND REPLACED LT ENGINE BB AXIS SEAL. 2 L 7 2 4T 4 T RT A52EU E8NE6 2001081300181 20010813 00181 NM 2001 8 13 2001UALA01485 1 20010726 A 2910 WARNING SYSTEM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT ACTIVATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 324UA 23956 UNSCHEDULED LANDING DUE TO HYDRAULIC PRESSURE INDICATION. 2 L 7 2 4F 4 F RT A16WE E2GL 2001081400023 20010814 00023 NM 2001 8 14 2001UALA01663 1 20010809 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 616 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 321UA 23953 BS 616 FRAME IS CRACKED BELOW THE FLOOR LEVEL ON INBD, FWDEDGE AT FASTENER HOLES. INSTALLED ANGLE REPAIR. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001081600124 20010816 00124 NM 2001 8 16 2001UALA01624 1 20010805 A 2824 PUMP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUEL SYS MALFUNCTIONED A UALA O OTHER O OTHER AP APPROACH 1 WP 29 606UA 21867 UNWANTED FUEL TRANSFER. 2 L 7 2 4F 4 F RT A1NM E3NE 2001082900223 20010829 00223 NM 2001 8 29 VNAA0108004 1 20010808 A 3150 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 438JS 3056 DURING THE TAKEOFF ROLL, THE CREW RECEIVED A TAKE OFF CONFIGURATION CAS MESSAGE AND ABORTED TAKEOFF. THE CREW RESET THE ELEVATOR TRIM AND ATTEMPTED ANOTHER TAKEOFF. FLIGHT 4082 DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001090500097 20010905 00097 NM 2001 9 5 AUS20010915 1 20010822 A 3350 LIGHT BOEING 737 737376 NM CFMINT CFM56 CFM563C 13802 EU EMERGENCY LIGHTI FAULTY W K NONE L NO TEST IN INSP/MAINT 1 AU S (AUS) FLOOR ESCAPE LIGHTING INOPERATIVE AT NUMEROUS CABIN STATIONS. 2 L 7 2 4F 4 F RT A16WE E21EU 2001090500132 20010905 00132 EU 2001 9 5 KBMA88666 1 20010708 A 6520 350A33215300 BEARING SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 37SH 2300 BEARINGS ARE WORN. REMOVED AND REPLACED WITH NEW BEARINGS. 1 G 7 1 3U 3 U NC H9EU E19EU 2001090500227 20010905 00227 NM 2001 9 5 2001UALA01903 1 20010830 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1065-1087 STRINGER 24L CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091900134 20010919 00134 NM 2001 9 19 2001UALA01882 1 20010827 A 3350 78961 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 183UA 25379 SEAT MOUNTED EEL LIGHTS 4E & F AFT ELEMENTS INOP. SEAT MOUNTED EEL LIGHT CONNECTION LOOSE. SECURED CONNECTION. 2 L 7 4 4F 4 F RT A20WE E24NE 2001091200155 20010912 00155 NE 2001 9 12 MASA01058 2 20010623 A 7200 CARBON SEAL CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE NR 1 ENGINE FAILED A MASA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 07 27172 7172 FLT 6901 - A FERRY FROM AVP-CMH - RETURNED TO THE FIELD IN AVP WHEN THE COCKPIT FILLED UP WITH SMOKE SHORTLY AFTER TAKEO FF. THE CREW WENT ON OXYGEN AND TRIED TO CLEAR THE CABIN OF SMOKE. THE CREW LANDED SAFELY. MAINTENANCE WAS DISPATCHED FROM PHL. MAINTENANCE TROUBLE SHOT TO A FAILURE OF THE NR 1 ENGINE CARBON SEAL. MAINTENANCE IS IN PROCESS OF REMOVING AND REPLACING THE NR 1 ENGINE. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE. OP CHECKS GOOD. THE AIRCRAFT WAS RE TURNED TO SERVICE. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2001091300321 20010913 00321 NM 2001 9 13 COOSDR010115 1 20010816 A 5315 FLOORBEAM BOEING 737 737230 NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 737TW 20257 MAIN CARGO CABIN FLOOR BEAM WITH CORROSION AT BS 312, LBL 58, WL 204. 2 L 7 2 4F 4 F RT A16WE E2EA 2001091400171 20010914 00171 NM 2001 9 14 2001UALA01967 1 20010904 A 5315 FLOORBEAM BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 BODY STATION 1351 RBL 15-RBL 33 T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CAP. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091900246 20010919 00246 NM 2001 9 19 2001UALA02028 1 20010913 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 647UA 25284 EXTERNAL FUSELAGE SKIN DENTED AND REPAIRED AT BODY STATION 323 LBL 32. MAJOR REPAIR ACCOMPLISHED AND INSPECTED AT FUSE S KIN BODY. 2 L 7 2 4F 4 F RT A1NM E24NE 2001092000030 20010920 00030 SW 2001 9 20 B1H2001F00000 1 20010628 A 6210 427016001109 BLADE BELL 427 427 SW PWC PW207 PW207D NE TAIL ROTOR DEBONDED B B1HR K NONE O OTHER IN INSP/MAINT 1 SW 19 427FW 41 56002 DURING A 50 HOUR INSPECTION THE CONDITION WAS FOUND. THE OUTER COMPOSITE LAYERS HAD DEBONDED FROM THE ROOT OF THE BLADE AND VOIDS WERE PRESENT. THE PROBLEM IS THE BLADE WILL HAVE TO BE SPREAD TO GET THE PITCH HORN IN AND THIS MAY BE THE C AUSE OF THE DEBONDING. SUGGEST THE OPENING IN THE TAIL ROTOR BLADE SHOULD BE WIDER. 1 G 7 1 3U 3 U R00001RC E42NE 2001092000077 20010920 00077 EA 2001 9 20 2001F00285 2 20010808 A 7261 ENGINE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA LEFT LACK OF LUBE A GUUA E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 SO 19 120GP UC59 FLT 5202 - TNT-MIA - DURING FLIGHT, LEFT ENGINE OIL PRESSURE ANNUNCIATOR ILLUMINATED AND OIL PRESSURE DROPPED TO 40 PSI. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN. INSPECTED LEFT ENGINE. NO LEAKS NOTED. NO SIGNS OF CONSUMPTION NOTED. CHE CKED ENGINE HISTORY RECORDS. NO ADVERSE OIL TRENDS NOTED. SERVICED ENGINE OIL. PERFORMED ENGINE RUN. OPS CHECK NORMA L. NO LEAKS NOTED. ENGINE ON OIL USAGE WATCH. (M) 2 L 7 2 4T 4 T RT A24CE E4EA 2001092100109 20010921 00109 NM 2001 9 21 CA010907006 1 20010829 A 3213 NAS679A5 NUT BOEING 727 72722 1384002 NM PWA JT8 JT8D7B 52053 NE MLG TRUNNION SPLIT W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ON RT MAIN LANDING GEAR FOUND TRUNNION NUT SPLIT ON ONE SIDE, ON THE RT SUPPORT ASSEMBLY TRUNNION. 2 L 7 3 4F 4 F A3WE E2EA 2001092400011 20010924 00011 EU 2001 9 24 CA010910005 1 20010820 A 2780 4917007 COMPUTER AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE LE FLAPS FAILED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA (CAN) REPEAT FLAP FAIL MESSAGE WHEN FLAP 2 SELECTED, CREW ELECTED TO GO AROUND AND CARRY OUT QRH PROCEDURES. AIRCRAFT LA NDED IN CALGARY SAFELY WITHOUT FURTHER INCIDENT.FLAPS RECYCLED BACK TO CLEAR CONFIGURATION FLAP MESSAGES, SYSTEM RETURNE D TO NORMAL. CYCLED MANY TIMES AND UNABLE TO REPEAT. LUBRICATION OF THE FLAP CARRIAGES. AIRCRAFT FOUND SERVICEABLE. 2 L 7 2 4F 4 F RT A28NM E29NE 2001092600141 20010926 00141 NE 2001 9 26 F3LA200100107 2 20010919 A 7530 RP19801 SENSOR AIRBUS A319 A319111 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE FAILED A F3LA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 NM 03 902FR 820 MSN1515 887M10G04 AIR TURNBACK. FLIGHT CREW REPORTED NR 2 ENGINE COMPRESSOR STALL AT APPROXIMATELY 31,000 FT AND A SERIES OF SUBSEQUENT S TALLS. REDUCED NR 2 ENGINE POWER TO IDLE AND ALL INDICATIONS WERE NORMAL. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT L ANDED AT DFW WITHOUT INCIDENT. PERFORMED BORESCOPE INSPECTION OF HPT AND LPT BOOSTER ROTOR BLADES AND NR 1, 3 AND 8 HPC BLADES WITH NO DEFECTS NOTED. REPLACED T12 SENSOR AND PERFORMED OPERATIONAL CHECK OF FADEC SYSTEM WITH NO FAULTS NOTED ON A OR B CHANNEL. 2 L 7 2 4F 4 F RT A28NM E2GL 2001100100059 20011001 00059 NE 2001 10 1 710K052901 1 20010529 A 7920 0401272600 VENT LINE SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL1 60030 NE OIL SYSTEM LEAKING A JZBR K NONE K FLUID LOSS IN INSP/MAINT 1 EA 25 165ML 760471 THE OIL VENT LINE AND IT WAS CHAFED AND SEEPING. OIL LINE CHAFED CAUSED ENGINE OIL LOSS. 1 G 7 2 3U 3 U NC H1NE E19EU 2001100100069 20011001 00069 NM 2001 10 1 COOSDR010121 1 20010816 A 5330 DOUBLER BOEING 737 737230 NM PWA JT8 JT8D15 52051 NE FUSELAGE DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 737TW 20257 CARGO CABIN BONDED DOUBLER WITH DELAMINATION, FROM BS 995 TO BS 1006 AND BETWEEN STR 8R AND STR 10R. 2 L 7 2 4F 4 F RT A16WE E2EA 2001100300137 20011003 00137 NE 2001 10 3 ARWA0011001 2 20011001 A 7200 RB211524B402 ENGINE LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B402 54555 NE A ARWA A E UNSCHED LANDING ENGINE SHUTDOWN E VIBRATION/BUFFET CR CRUISE 1 SO 19 308GB 1439 193U1133 14529 LOG PAGE 21133. DISCREPANCY: IN CRUISE FL 330 #1 ENGINE VIBRATION SPIKED TO 4.5 BOTH CHANNELS ON VIBRATION MONITOR WITH NOTICEABLE INCREASE IN AIRFRAME VIBRATION. AS PER EMERGENCY CHECKLIST ENGINE WAS SHUT DOWN AT 12:40Z ALL OTHER ENGINE IN DICATIONS APPEARED NORMAL. AIRCRAFT RETURN TO KMIA AND LANDED WITHOUT INCIDENT. CORRECTIVE ACTION: 2 L 7 3 4F 4 F A23WE E12EU 2001100400148 20011004 00148 CE 2001 10 4 RJW2001F00001 1 20010731 A 5753 122101015 FLAP TRACK CESSNA 206 U206G 2073356 CE CONT O520 IO520* 17032 SO TE FLAPS LOOSE B RJWR K NONE O OTHER IN INSP/MAINT 1 GL 15 932DB 4604 U20605397 FLAP TRACK HAS WORKED LOOSE. INICATIONS ARE: CRACKED FLAP COVE SKIN ATTACH BRACKETS. BOTH OF THESE DEFECTS ARE INDICA TIONS OF A LOOSE FLAP TRACK. REPAIRS WERE NOTED IN BOTH OF THESE AREAS BUT THE FLAP TRACKS WERE NOT REPAIRED. 1 H 7 1 3O 3 O A4CE E5CE 2001101200139 20011012 00139 WP 2001 10 12 PNSA010905 2 20010924 A 7230 31070511 SEAL SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP COMPRESSOR LEAKING A PNSA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 03 650PA 1237 AC779B P44691 ON PREFLIGHT NOTICED OIL LEAK FROM RT ENGINE OVERBOARD DRAIN. MAINTENANCE FOUND COMPRESSOR SEAL LEAKING. 2 L 7 2 4T 4 T RT A8SW E4WE 2001101500001 20011015 00001 NM 2001 10 15 2001UALA02083 1 20010925 A 3350 BATTERY BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 619UA 21879 EEL ILLUMINATED IN BUSINESS CLASS ONLY WITH SWITCH ARMED. *S/D* REPLACED EMERGENCY BATTERY POWER SUPPLY MODULE AND ACC OMPLISHED SYSTEM TEST. 2 L 7 2 4F 4 F RT A1NM E3NE 2001101500140 20011015 00140 NE 2001 10 15 SWIA200110237 2 20011009 A 7314 PUMP EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE DEFECTIVE A SWIA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 NM 07 269UE 120194 DURING CLIMB TO 16000 FT NR 2 ENGINE TORQUE FLUCTUATED THEN RAPIDLY DROPPED TO 11 PERCENT TQ. OTHER ENGINE INDICATIONS WERE NORMAL. PERFORMED PRECAUTIONARY ENGINE SHUT DOWN. REMOVED AND REPLACED RIGHT ENGINE HMU AND FUEL PUMP IAW MM 73-21 -00. OPS AND LEAK CHECK GOOD. HMU P/N ON: 3035659 S/N ON: 49502 P/N OFF: 78639040 S/N OFF: M80363, PUMP P/N ON: 5009984C S/N ON: 136 P/N OFF: 3117075-01 S/N OFF: 1940 2 L 7 2 4T 4 T RT A31SO E20NE 2001101900002 20011019 00002 GL 2001 10 19 S01J73015 2 20010422 A 7300 ENGINE GE BOEING 747 747400 NM GE CF6 CF6* 30020 GL #2 ENG CONTAMINATED W SAJF O OTHER O OTHER TX TAXI/GRND HDL 1 WP 03 707156 30761 707156 B-18703 DURING A/C TAXI OUT, # 2 ENG SPOOL DOWN AND EGT OVER LIMIT.C/A:1.EPLD HUM AND ECU. 2.OIL AND FUEL FILTER RPLD. 3 .HPT AND LPT BORESCOPE INSP. NML. 4.ECU STATIC AND ACTUATORS TEST NML. 5.PERFORM TEST #10 POWER ASSURANCE CK NML. 6. 4/2 5 RPLD # 2 ENG PER GE RECOMMENDATION. 2 L 7 4 4F 4 F RT A20WE E23EA 2001110800049 20011108 00049 NM 2001 11 8 2001UALA02148 1 20011018 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 594UA 28145 UPPER FUSELAGE SKIN AT STATION 555 RBL 10 PITTED. ALSO TEAR STRAP DOES NOT HAVE ENOUGH EDGE DISTANCE FOR FASTENER INSTA LLATION. MAJOR REPAIR ACCOMPLISHED. REPAIRED STRINGER AND ACCOMPLISHED DOUBLER REPAIR. TEAR STRAP ALSO REPAIRED AND VE RIFIED DAMAGE REMOVAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2001112100097 20011121 00097 NM 2001 11 21 2001UALA02277 1 20011114 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 521UA 24891 MID CABIN CREASE BEAM INNER CHORD BODY STATION 745 TO 756 CORRODED AT LBL 60. MAJOR REPAIR ACCOMPLISHED. REPLACED CREA SE BEAM INNER CHORD. 2 L 7 2 4F 4 F RT A2NM E17NE 2001120500208 20011205 00208 GL 2001 12 5 2001F00579 2 20010727 A 7250 23053299 BLADE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL ENGINE CORRODED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 164AG 1761 760290 DURING DISASSEMBLY FOR INSPECTION, FOUND SULPHADATION ON BLADES. (M) 1 G 7 2 3U 3 U H1NE E1GL 2001120600076 20011206 00076 SW 2001 12 6 R7MA37722 1 20010705 A 6510 407040320101 FAN BELL 407 407 1182206 SW ALLSN 250C 250C47B GL TAIL ROTOR WORN E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 407SJ 648 53422 WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2002010300106 20020103 00106 NM 2002 1 3 2001UALA02417 1 20011216 A 5320 CHANNEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 CABIN FLOOR HAT CHANNEL AT STATION 334 RBL 23 TO 38 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW HAT CHANNEL. 2 L 7 2 4F 4 F RT A2NM E17NE 2002010300137 20020103 00137 NM 2002 1 3 2001UALA02452 1 20011222 A 5311 FAILSAFE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 AFT PIT BODY FRAME FAIL SAFE CHORD WAS BLENDED IN RADIUS. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002010800048 20020108 00048 NM 2002 1 8 AUS20011027 1 20010927 A 4940 5198588 STARTER BOEING 767 767238 1385114 NM PWA JT9 JT9D7R4E 52054 NE APU BURNED OUT W O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 AU S (AUS) APU STARTER MOTOR BURNED OUT. STARTER MOTOR HAD REMAINED ENGAGED FOLLOWING APU START. 2 L 7 2 4F 4 F RT A1NM E3NE 2002011600158 20020116 00158 NE 2002 1 16 DL76S011966 2 20011221 A 7310 FUEL LINE BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 2 ENGINE LEAKING A DALA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 27 133DN 24982 580327 FOUND FUEL LEAK ON RT ENGINE WHEN OPENED FOR MTC, POSSIBLE FIRE CONDITION EXISTED. FOUND FUEL LINES LEAKING. REPLACED FLEX FUEL LINES FROM FUEL FILTER TO DIFF PRESSURE SWITCH AND TO HEAT EXCHANGER, LEAK CHECK FOUND OK. 2 L 7 2 4F 4 F RT A1NM E13NE 2002012800055 20020128 00055 EU 2002 1 28 A1U2002F00000 1 20011214 A 2824 1176415103 PUMP BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE FUEL TRANSFER FAILED E A1UA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 440SL 7158 45674 ON STARTUP WHILE SWITCHING FUEL TRANSFER PUMPS ON, TRANSFER PUMP FORWARD FAILED TO OPERATED. PROBABLE CAUSE, BEARINGS S EIZED. 1 G 7 2 3U 3 U H13EU E5NE10 2002012900111 20020129 00111 NE 2002 1 29 R7MR34359 2 20010730 A 7412 9550168770 IGNITER SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE IGNITION SYS WORN B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 392LG 678 3252 IGNITER, WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002031100115 20020311 00115 SW 2002 3 11 AC2A0000294 1 20011130 A 3040 222325001027 GUIDE BELL 430 430 1182150 SW ALLSN 250C 250C* GL WINDSHIELD WIPER BROKEN E AC2A K NONE O OTHER IN INSP/MAINT 1 SW 03 430CV 804 49072 GUIDE ARM ASSEMBLY IS BROKEN. REPLACED WITH NEW PART. 1 G 7 2 3U 3 U RT H9SW E4CE 2003121000004 20031210 00004 EA 2003 12 10 ACE1121011 2 20011123 A 7230 312119301 BLADE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA LT ENGINE FAILED E YADA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 AL 03 1566C 18733 4471 UC36 3225032270 JUST AFTER TAKEOFF, THE LT ENGINE MADE A LOUD NOISE AND TORQUE DROPPED OFF. THE ENGINE WAS SECURED AND THE AIRCRAFT RET URNED AND LANDED WITHOUT INCIDENT. MAINTENANCE DETERMINED A FAILURE OF THE CT DISK BLADES, CAUSE UNKNOWN. THE ENGINE W AS REMOVED FOR REPAIR. 2 L 7 2 4T 4 T RT A24CE E4EA 2003121900017 20031219 00017 CE 2003 12 19 YAD2003F00003 1 20011005 A 2612 24412886 FIRE LOOP BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA NR 1 ENG EXHAUST FALSE INDICATION E YADA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 AL 03 1563C UC20 FLIGHT CREW RETURNED TO RAMP AFTER INDICATION OF FIRE IN THE NR 1 ENGINE. MAINTENANCE VERIFIED THAT THE WARNING WAS FAL SE AND WAS CAUSED BY CONTACT BETWEEN THE FORWARD FIRE DETECT LOOP AND A DISCONNECTED O/B HEATED INTAKE LIP FLEX TUBE. M AINTENANCE REPLACED THE FORWARD FIRE DETECT LOOP AND RECONNECTED THE FLEX DUCT. 2 L 7 2 4T 4 T RT A24CE E4EA 2001092400184 20010924 00184 NM 2001 9 24 UPS01436717 1 20010826 A 3350 S1356837 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:N/A EMERG LIGHT AT STAIRWELL INOP. REPLACED EMERG LIGHT ASSY. 2 L 7 4 4F A20WE 2001051800016 20010518 00016 EU 2001 5 18 DHL2001367004 1 20010505 A 5753 A57246666030551 DEFLECTOR AIRBUS 300 A300B4203 3930306 EU DAMAGED CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH MSN265 A-CHECK- LT WING I/B FLAP HINGE PANEL DAMAGED. REPLACED LT WING I/B FLAP DEFLECTOR PANEL WITH NEW PANEL IAW A-300 MM 57- 50-00PG 29 2 L 7 2 4F RT A35EU 2001110700125 20011107 00125 WP 2001 11 7 01FDEA00942 1 20011030 A 5347 SEAT TRACK DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 BS 1879, X=-59, Z=-19 SEAT TRACK LOBE HAS CORROSION. REMOVED AND REPLACED SEAT TRACK PER SRM. 2 L 7 3 4F RT A22WE 2001050100123 20010501 00123 WP 2001 5 1 CALA0100390 1 20010418 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND LONGERON 30 IN E&E BAY UNDER BATTERY CHARGER CORRODED AT STA 110 - 120. THE LONGERON WAS REMOVED AND R EPLACED IAW SRM 51-10-4 AND 51-30-2. 2 L 7 2 4F A6WE 2001072600152 20010726 00152 NM 2001 7 26 2001UALA01300 1 20010610 A 5330 SKIN BOEING 757 757222 1384956 NM FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 513UA 24810 DAMAGE FOUND AT THE PRODUCTION BUTT JOINT OF THE UPPER FUSELAGE SKINS AT BODY STATION 661 AND STRINGER 4R. INSTALLED DO UBLER REPAIR TO DAMAGED AREA. THIS WAS A MAJOR REPAIR. 2 L 7 2 4F RT A2NM 2001080700020 20010807 00020 2001 8 7 ASOA01103 4 20010707 A 2350 509111 CONTROL PANEL EMB 120 EMB120 3260201 SO COCKPIT FAULTY A ASOA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 274AS 30297 120229 FLT 4183 - DURING FLIGHT FROM DHN TO ATL, CAPTAIN REPORTS SMOKE BEING EMITTED FROM THE LEFT SIDE AUDIO CONTROL PANEL. A IRCRAFT DIVERTED AND LANDED SAFELY IN CSG. MAINTENANCE REMOVED AND REPLACED THE LEFT AUDIO CONTROL PANEL. MAINTENANCE ALSO INSPECTED THE WIRING AND CANNON PLUG FOR ANY EVIDENCE OF ELECTRICAL SHORTS, BUT NO DEFECTS WERE NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2001062500034 20010625 00034 WP 2001 6 25 DHL2001806623 1 20010401 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 C-CHECK - LT WING L/E LWR SURFACE HAS .5 INCH CRACK AT STA XFS 585. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1. CUTOUT D AMAGED SKIN IAW EO DHL 010317, EO2360, EO 2001072. CLEANED, TREATED, AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FILLE R AND DOUBLER (7075 T6 0.050/O.O63) IAW EO DHL 010317, EO 2360, EO 2001072. CLEANED, TREATED, AND PRIMED IAW SRM 51-1-8 B. APPLIED (PRC) SEALANT TO REWORK AREA IAW SRM 51-1-15 PAGE 1. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW EO DHL 010317, EO 2360, EO 2001072, SRM 51-1-21 PAGE 1. 2 L 7 4 4F RT 4A25 2001071800097 20010718 00097 NM 2001 7 18 2001UALA01024 1 20010613 A 5320 CHANNEL BOEING 757 757222 1384956 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 CABIN FLOORBEAM VERTICAL L-ANGLE CRACKED STA 324, RBL 60. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW Z-CHANNEL. 2 L 7 2 4F RT A2NM 2001022700149 20010227 00149 NM 2001 2 27 01FDEA00104 1 20010209 A 2612 1014A POWER UNIT BOEING 727 7272D4 138407U NM COCKPIT MALFUNCTIONED A FDEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 25 287FE 21849 T/O ROLL FIRE WARNING LIGHT CAME ON GLARESHIELD ILLUMINATED WITH ALARM BELL. REMOVED AND REPLACED APU FIRE AND OVERHEAT DET PWR UNIT PER IAW 727-200 MM 26-15-003-4 AS PRECAUTIONARY. SYS OPS CK NORMAL. 2 L 7 3 4F A3WE 2001102600003 20011026 00003 EU 2001 10 26 01FDEA00907 1 20011023 A 3260 WARNING SYSTEM AIRBUS 310 A310 EU COCKPIT ACTIVATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 424FE 241 AS SOON AS MLG BROKE OFF GROUND ECAM IND LG RETRACT FAULT. 2 L 7 2 4F RT A35EU 2001072400245 20010724 00245 NM 2001 7 24 2001UALA01144 1 20010621 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 1439 STR 38L-39L SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 140T2102-539 AND SRM 51-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001081600077 20010816 00077 NM 2001 8 16 01FDEA00558 1 20010714 A 5320 TIE CLIP BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277FE 22042 DURING ROUTINE INSP SHEAR TIE CLIP AT STR 23L, BS 520 FOUND CRACKED. *S/D* REMOVED AND REPLACED SRM 51-20-1, 51-30-2. 2 L 7 3 4F RT A3WE 2001072400157 20010724 00157 NM 2001 7 24 2001UALA01119 1 20010620 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 BS 355 STR 37R-38R SHEAR TIE CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 141T1221-68 AN D SRM 51-40-02 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001021300404 20010213 00404 NM 2001 2 13 2001UALA00015 1 20010109 A 2822 PUMP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUEL BOOST FAILED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 7266U 21413 DURING FLIGHT THE NR 2 FUEL TANK RIGHT AFT BOOST PUMP FAILED. *S/D* NR 2 RT LOW PRESSURE LIGHT ON WITH PUMP IN THE ON POSITION. REPLACED NR 2 RIGHT AFT BOOST PUMP. 2 L 7 3 4F 4 F A3WE E2EA 2001021300287 20010213 00287 NE 2001 2 13 MALA010108 2 20010111 A 7220 INTAKE DUCT SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE CONTAMINATED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 456XJ 456 EN ROUTE CLIMBING THROUGH 15,000, -10 DEGREE CELSUIS AND ANTI-ICE OFF, GOT 900+ DEGREE ON RT ENGINE, PRECAUTIONARY LANDI NG BACK IN DTW. AVOIDED 80 - 84 PERCENT NG RANGE. MAINTENANCE REMOVED DEBRIS FOUND IN RT ENGINE INLET, PERFORMED ENGIN E INLET BLOCKAGE INSPECTION, SPECIAL PROCEDURES, NO DAMAGE NOTED, ITEM WAS ACCEPTABLE IAW GE MM CHAP 72 FIG 204 AND TABL E 305A. ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2001031200640 20010312 00640 NM 2001 3 12 2001UALA00050 1 20010124 A 2131 CONTROLLER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN PRESSURE MALFUNCTIONED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 7292U 21570 AIRCRAFT WAS UNABLE TO MAINTAIN CABIN PRESSURE ABOVE 22,000 FEET. *S/D* THE PRESSURE CONTROLLER FAILED. REPLACED CABI N PRESSURE CONTROLLER. 2 L 7 3 4F 4 F A3WE E2EA 2001021600199 20010216 00199 SO 2001 2 16 SWIA972310 1 20010125 A 3350 LIGHT EMB 120 EMB120RT SO PWA 118 PW118 NE CABIN INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 269UE 120194 EXIT ROW SIGNS AT 6A AND 6C DO NOT ILLUMINATE CONTINUOUSLY WHEN EMERGENCY LIGHTS SWITCH IS TURNED ON AT FLIGHT ATTENDNAT S PANEL. REPLACED ELBP AT ROW 6. OPS CHECKS GOOD. P/N ON,OFF: D366-04-001, S/N ON: 1137, S/N OFF: 1169. 2 L 7 2 4T 4 T RT A31SO E20NE 2001022200098 20010222 00098 CE 2001 2 22 20010208CW010 1 20010109 A 2810 10038100511 FUEL CAP BEECH 1900 1900D 1154162 CE PWA PT6 PT6A11 52043 NE RT WING BROKEN A JJBA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 01 845CA 1250 UE388 UPON REMOVAL OF RT OUTBOARD FWD CAP, CAP FELL APART. PIN IN LOCKING TAP THAT SECURES CAP BODY TOGETHER IS LOOSE IN TAP AND FELL OUT, ALLOWING CAP TO FALL APART. REDESIGN OR MATERIAL CHANGE REQUIRED. 2 L 7 2 4T 3 T RT A24CE E4EA 2001031200626 20010312 00626 NM 2001 3 12 VNAA0101027 1 20010131 A 3350 501122803 POWER SUPPLY 501122803 DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN FAILED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 425JS 14214 8982 3037 THE CREW REPORTED THAT THE EMERGENCY POWER SUPPLIES WOULD NOT TEST. MAINTENANCE INSPECTED AND REPLACED BOTH EMERGENCY P OWER SUPPLIES IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAF T WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001040300098 20010403 00098 EU 2001 4 3 CA010212021 1 20010124 A 7740 9752902015 CONTROL PANEL PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL COCKPIT FAILED W O OTHER N FALSE WARNING AP APPROACH 1 CA 96 040 (CAN) ON FINAL APPROACH, A FLUCTUATING OIL PRESSURE WAS NOTED ON THE E.I.S. PANEL. THE AIRCRAFT WAS LANDED, AND TAXIED T O HANGAR WITH OIL PRESSURE STILL FLUCTUATING. AFTER OIL LEVEL CHECKED OK. THE E.I.S. PANEL WAS REPLACED, AND OIL PRESSUR E THEN RETURNED TO NORMAL. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2001040400228 20010404 00228 EU 2001 4 4 CA010301027 1 20010211 A 3213 D52706EB BUSHING AIRBUS 310 A310304 EU GE CF6 CF680C2A5 NE SHOCK ABSORBER ROTATED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 4473 4473 (CAN) AIRCRAFT RETURNED TO YTR AS GEAR WOULD NOT RETRACT. AIRCRAFT PUT ON JACKS AND FOUND THAT LT BOGIE WOULD NOT TILT. IT WAS DETERMINED THAT ONE BUSHING ON THE SHOCK ABSORBER HAD ROTATED CAUSING THE HINGE PIN TO SEIZE, THEREFORE BOGIE WOU LD NOT TILT AND GEAR WOULD NOT RETRACT. BUSHINGS REPLACED AS PER CMM 32-16-58. GEAR SWING CHECKED SERVICEABLE. 2 L 7 2 4F 4 F RT A35EU E13NE 2001040900337 20010409 00337 CE 2001 4 9 20010403CW007 1 20010226 A 3244 0335040 TIRE DUNLOP RAYTHN DH125 DH125 4230106 CE GARRTT TFE731 TFE731* 01518 WP MLG FAILED D A UNSCHED LANDING E VIBRATION/BUFFET NR NOT REPORTED 1 SO 03 333DP 166 NA77525282 A LANDING GEAR/WHEEL TYPE SPEED RELATED VIBRATION WAS REPORTED BY THE FLIGHT CREW. INVESTIGATION REVEALED A BUMPED OUT AREA OF TREAD ON THE RIGHT OUTBOARD MAIN TIRE. THE AREA WAS APPROX 9 INCHES LONG PLUS THE TIRE WIDTH OF THE TREAD AREA . THAT AREA WAS .1875 TO .2500 HIGHER THAN THE REST OF THE TIRE TREAD. REMOVED AND REPLACED TIRE. CORRECTED PROBLEM. 2 L 7 2 4J 4 F RT A3EU E6WE 2001040900532 20010409 00532 NE 2001 4 9 TWAA0104607 2 20010310 A 7200 ENGINE BOEING 757 757231 1384950 NM PWA 2037 PW2037 NE RT ENGINE FAILED A TWAA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 CE 05 715TW 28483 4931 DURING CLIMB AT 10,000 FEET A LOUD BANG WAS HEARD FROM THE RT ENG AND IT STARTED TO SPOOL DOWN. THE ENG WAS SHUT DOWN A ND THE FLIGHT RETURNED TO AUA. THE ENGINE WAS REPLACED. CHECK-C 10-14-00 LAX. 2 L 7 2 4F 4 F RT A2NM E17NE 2001041200094 20010412 00094 NM 2001 4 12 2001UALA00270 1 20010317 A 5240 STOP FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 309UA 23670 FORWARD GALLEY DOOR LOWER AFT STOP FITTING FRAME CRACKED. REPAIRED CRACKED FRAME. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001041600069 20010416 00069 NM 2001 4 16 2001UALA00235 1 20010312 A 5310 146T1210 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 614UA 21875 AFT PIT BS 1285 STRINGERS 36L - 37L SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E3NE 2001041700076 20010417 00076 CE 2001 4 17 20010412CW006 1 20010312 A 5610 551128548 WINDSHIELD CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE COCKPIT CRACKED B O OTHER O OTHER NR NOT REPORTED 1 NM 09 129DV 7682 5500365 COPILOTS SIDE WINDOW CRACKED IN HOLES 4, 5, AND 11. 1 L 7 2 4F 4 F A22CE E1NE 2001041700135 20010417 00135 EU 2001 4 17 CA010404004 1 20010302 A 5610 NF20216401 WINDOW BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 6117 (CAN) DURING CLIMBOUT THE FLIGHT CREW REPORTED A CRACK DEVELOPING IN THE LOWER RT CORNER OF THE CAPTAINS B PANEL. THE AI RCRAFT RETURNED TO THE POINT OF DEPARTURE AND THE WINDOW WAS REPLACED. THE WINDOW WAS A REMANUFACTURED EXCHANGE UNIT FRO M AEROSPACE COMPOSITE TECHNOLOGIES, AND HAD ACCUMULATED 6,117 HOURS AND 4,118 CYCLES SINCE INSTALLATION ON THIS AIRCRAFT . 2 H 7 4 4F 4 F RT A49EU E6NE 2001041900124 20010419 00124 NM 2001 4 19 VNAA0103014 1 20010316 A 3350 362624 LIGHT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN INOPERATIVE A VNAA K NONE L NO TEST NR NOT REPORTED 1 GL 07 457PS 3048 THE FLIGHT CREW REPORTED THAT THE EMERGENCY FLOOR PATH LIGHTING ADJACENT TO SEAT ROW 10 WOULD NOT OPERATE. MAINTENANCE INSPECTED AND FERRIED THE AIRCRAFT TO PIT FOR REPLACEMENT. THE FERRY FLIGHT WAS COMPLETED WITHOUT INCIDENT. MAINTENANC E REPLACED THE PATHWAY LIGHTING STRIP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-12. OPERATIONAL CHECKS WERE C OMPLETED AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001042400022 20010424 00022 SO 2001 4 24 SWIA972464 1 20010329 A 2722 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RUDDER FAILED A SWIA K NONE F FLT CONT AFFECTED CR CRUISE 1 NM 07 189SW 120048 RIGHT RUDDER PEDAL JAMMED IN FLIGHT. REMOVED AND REPLACED BLUE RUDDER HYDRAULIC ACTUATOR IAW 27-20-00. OPS AND LEAK CH ECK GOOD AT THIS TIME. P/N: 308104-1003, S/N ON: 0165, P/N OFF: 308140-1003, S/N OFF: 0767. 2 L 7 2 4T 4 T RT A31SO E20NE 2001042400336 20010424 00336 NE 2001 4 24 R7MR32734 2 20010315 A 7200 PW206B ENGINE UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE LEFT FOD B R7MR K NONE C F.O.D. IN INSP/MAINT 1 NM 07 427AE 10 EC1350162 PCEBB0101 FOREIGN OBJECT DAMAGE. DAMAGE OCCURRED PRIOR TO TAKING DELIVERY OF AIRCRAFT. SUSPECT THAT RIVET FRAGMENTS ENTERED ENGI NE DURING FINAL PHASE OF AIRFRAME ASSEMBLY. 1 G 7 2 3U 3 U O H88EU E42NE 2001050300088 20010503 00088 EU 2001 5 3 QXEA0100625 2 20010420 A 7200 RB18355515P ENGINE FOKKER F28 F28MK4000 4990810 EU RROYCE SPEY SPEY55515P 54521 EU WING VIBRATION A QXEA A UNSCHED LANDING E B VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 09 477AU 34624 2799 11226 9636 YYC - ON CLIMBOUT FROM YYC ENGINE VIBRATION AND CABIN FILLED WITH SMOKE. RETURNED TO FIELD. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED ENGINE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A20EU E2EU 2001050900084 20010509 00084 SO 2001 5 9 SWIA972539 1 20010430 A 5240 DOOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE SERVICE DOOR UNLATCHED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 583SW 120351 SERVICE DOOR LIGHT CAME ON TAKEOFF ROLL. FOUND OUTBOARD FORWARD THUMB LATCH OPEN. SECURED LATCH. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2001052100046 20010521 00046 NM 2001 5 21 2001UALA00621 1 20010429 A 5320 CLIP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7456U 21910 STRINGER 21R CLIP CRACKED AND BUCKLED AT BS 460 ATTACHMENT. REPLACED STRINGER CLIP AT STRINGER 21R PER SRM 53-10-3 2 L 7 3 4F 4 F A3WE E2EA 2001052100092 20010521 00092 NM 2001 5 21 2001UALA00685 1 20010505 A 5310 PRESSURE PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 CABIN PRESSURE DECK CRACKED. STA 663 LBL 30. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001052300129 20010523 00129 SO 2001 5 23 SWIA972573 1 20010515 A 3010 REGULATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE DEICE SYS MALFUNCTIONED A SWIA A UNSCHED LANDING J Y WARNING INDICATION ENGINE STOPPAGE CR CRUISE 1 NM 07 293SW 120320 RIGHT DUCT LEAK ILLUMINATED IN FLIGHT. RAN QRH PROCEDURES. DID PRECAUTIONARY SHUT DOWN AND RESTART, LIGHT ILLUMINATED AGAIN. SHUT DOWN NR 2 ENGINE AND SHOT SINGLE ENGINE APPROACH. FOUND RIGHT DEICE REGULATOR DRAIN BOWL BLOWN OFF REGULAT OR. REPLACED RIGHT DEICE PRESSURE REGULATOR. REINSTALLED REGULATOR DRAIN BOWL. RAN BOTH ENGINES AND BLEEDS FOR 10 MIN AT SEVERAL POWER SETTINGS. ALL CHECKS GOOD. S/N ON RF-2238. 2 L 7 2 4T 4 T RT A31SO E20NE 2001071800017 20010718 00017 NM 2001 7 18 2001UALA00741 1 20010515 A 2120 SMOKE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DETECTED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7266U 21413 CREW REPORTS SMOKE IN CABIN WHILE SITTING ON THE GROUND WITH PACKS RUNNING. *S/D* THE COOLING FANS LOST POWER RESULTIN G IN PACKS GETTING HOT CAUSING A LIGHT HAZE IN THE CABIN WITH NO NOTICEABLE ODOR. THE PACKS WERE OPERATED OFF THE ENGIN ES AND THE APU TO VERIFY OPERATION. APU OP CHECKED NORMAL AND NO DISCREPANCIES WERE FOUND. 2 L 7 3 4F 4 F A3WE E2EA 2001080800004 20010808 00004 NM 2001 8 8 VNAA0107011 1 20010708 A 2730 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT ACTIVATED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 432JS 3045 AFTER APPLYING POWER FOR TAKEOFF, THE CREW RECEIVED A TAKEOFF CONFIGURATION CAS AND ELEVATOR TRIM CAS MESSAGE. THE CREW ABORTED TAKEOFF AND EXITED THE RUNWAY. THE CREW MOVED THE ELEVATOR TRIM TO A POSITION FURTHER IN THE GREEN BAND SETTIN G AND THE MESSAGE CLEARED. FLIGHT 4085 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2001091400082 20010914 00082 NM 2001 9 14 2001UALA01443 1 20010722 A 5755 651734748 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE SPOILER DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7461U 21915 FLIGHT SPOILER LEFT WING NR 3 DELAMINATED NEAR TRAILING EDGE. FLT SPOILER LEFT WING NR 3 DELAMINATED NEAR TRAILING EDGE. SPOILER PANEL WAS CHECKED FOR CRACKS OR SCRATCHES AND NONE WERE NOTED. AN INTERIM REPAIR WAS ACCOMPLISHED WITH THE RE QUIREMENT THAT THE SPOILER BE PERMANENTLY REPAIRED OR REPLACED WITHIN 45 FLIGHT HOURS. 2 L 7 3 4F 4 F A3WE E2EA 2001081300171 20010813 00171 NM 2001 8 13 2001UALA01478 1 20010725 A 5312 BULKHEAD BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 914UA 25381 BULKHEAD WEB CRACKED AT BS 178, RBL 1- LBL 1, WL 185. INSTALLED DOUBLER. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001082200040 20010822 00040 NM 2001 8 22 2001UALA01404 1 20010711 A 7931 42D107A2 SWITCH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE FAULTY A UALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 7262U 4930 21409 696587 NR 2 ENGINE SHUT DOWN IN FLIGHT DUE TO LOW OIL PRESSURE INDICATION. AIRCRAFT DIVERTED TO COS. *S/D* ENGINE WAS SHUT D OWN DUE TO LOW OIL PRESSURE LIGHT INDICATION. ALL ENGINE PARAMETERS INDICATED NORMAL AND OIL PRESSURE WAS ABOVE 35 PSI. LOW OIL PRESSURE LIGHT REMAINED ON WHEN ENGINE WAS AT FLIGHT IDLE. OIL CONSUMPTION WAS IN LIMITS AND NO CARBON WAS FO UND IN THE OIL FILTER. REPLACED THE LOW OIL FILTER SWITCH AND AS A PRECAUTIONARY THE FILTER BYPASS WAS REPLACED AS WELL . AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2001082800238 20010828 00238 EU 2001 8 28 2001UALA01744 1 20010818 A 2910 201042092 HOSE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 418UA 485 GREEN HYDRAULIC SYSTEM LOSS OF FLUID. SUPPLEMENTAL DATA UPDATE LEFT MAIN LANDING GEAR LOCKSTAY ACTUATOR HYDRAULIC LINE S WIVEL SHEARED.REPLACED LINE ASSEMBLY AND LEAK CHECKED. NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2001090700112 20010907 00112 NM 2001 9 7 2001UALA01871 1 20010828 A 5310 SHEAR TIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 STATION 1219 STRINGER 35R-36R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE REPAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2001091200134 20010912 00134 NM 2001 9 12 2001UALA01938 1 20010901 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BODY STATION 150 A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 516UA 24860 AFT PIT FUSELAGE FRAME AT BS 1500, RBL28, GOUGED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. BLENDED AREA. INST ALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2001091700044 20010917 00044 EA 2001 9 17 SWIA972644 1 20010618 A 2750 SENSOR CNDAIR CL600 CL6002B19 EA GE CF34 CF34* NE TE FLAPS FAILED A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 499SW 7398 FLAPS FAIL IN FLIGHT WITH FLAPS UP. REMOVED AND REPLACED RIGHT BRAKE POSITION SENSING UNIT IAW 27-51-10. CHECKS GOOD. COMPLIED WITH AD 98-20-01. P/N: 855D100-9 S/N ON: 303B S/N OFF: 155B 2 L 7 2 4F 4 F RT A21EA E15NE 2001092000046 20010920 00046 NE 2001 9 20 2001F00306 2 20010531 A 8530 SEAL DOUG DC4 C54BDC 3021516 WP PWA R2000 R2000* 52023 NE PUSHROD TUBE LEAKING A B2OB O OTHER K FLUID LOSS NR NOT REPORTED 1 AL 03 44911 10461 PUSH ROD TUBE SEAL HARD AND BRITTLE, NOT SOFT THIS CAUSING OIL LEAK. REPLACED SEAL WITH A NEW ONE. (M) 2 L 7 4 4R 4 R A762 5E5 2001092800040 20010928 00040 WP 2001 9 28 BSY2001F00013 2 20010904 A 7261 ENGINE LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP RIGHT LEAKING E BSYA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 07 684HA 113 (ATL) IN ROUTE FROM (BNA) TO (ATL) LOST OIL PRESSURE, RIGHT ENGINE. SHUT ENGINE DOWN LANDED AT (ATL). HAD GARRETT FROM AUGUSTA LOOK AT ENGINE, HAS MAJOR OIL LEAK. REMOVED ENGINE FOR REPAIR AT AUGUSTA. 2 L 7 2 4F 4 F A10CE E6WE 2001101200063 20011012 00063 NE 2001 10 12 2001UALA01719 2 20010810 A 7261 COVER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 ENG OIL LEAKING A UALA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION LD LANDING 1 WP 29 7279U 21557 700032 NR 3 ENGINE WAS SHUT DOWN DURING LANDING. *S/D* ENGINE WAS SHUT DOWN TO LOSS OF OIL FROM THE THE MAIN OIL SCREEN. THE OIL PRESSURE DROPPED TO 38 PSI. CAUSE WAS STUDS PULLED ON THE MAIN OIL SCREEN COVER AND WAS REPAIRED. 2 L 7 3 4F 4 F A3WE E2EA 2001101500110 20011015 00110 EU 2001 10 15 CAXA106176 1 20010918 A 2421 GC102578 PCU SNIAS 350 AS350D 8680803 EU TMECA ARRIEL ARRIEL1 60030 NE GENERATOR INOPERATIVE A CAXA K NONE O OTHER IN INSP/MAINT 1 WP 15 3597T 1126 INSTALLED CARD, GENERATOR WOULD NOT COME ON LINE. NOTE: INSTALLATION OF SECOND NEW CARD MADE SYSTEM FUNCTION NORMALLY. RMA RO33208 1 G 7 1 3U 3 U H9EU E19EU 2001102200021 20011022 00021 NM 2001 10 22 SWAA012856 1 20011016 A 5310 6546529 FRAME BOEING 737 7373Q8 1384670 NM CFM56 CFM56* 13802 NE FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 722394 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED ( 7 EA ) BETWEEN STR 8L & 9L, BS 807, 827, 847, 867, 907, 887 & 480. REPAIRED FRAMES PER BFG ER. 2 L 7 2 4F 4 F RT A16WE E2GL 2001110800063 20011108 00063 NM 2001 11 8 2001UALA02164 1 20011026 A 5310 CREASE BEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 918UA 25385 BODY STATION 185 STRINGER 17R CREASE BEAM FOUND DAMAGED, REQUIRED BLENDING BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. D AMAGE REMOVED AND REPLACEMENT INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2001110800077 20011108 00077 NM 2001 11 8 2001UALA02181 1 20011030 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 328UA 24148 CABIN STRINGER 10L CLIP IS CRACKED AT FRAME STA 663.75. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2001120400066 20011204 00066 EA 2001 12 4 SWIA200110359 1 20011115 A 2740 WIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CARGO BAY BROKEN A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 903SW 7425 STAB TRIM CH2 WILL NOT ENGAGE. REPAIRED WIRE CD91A22 AT CONNECTOR J6CD IN CARGO BAY. STAB TRIM OPS CHECK GOOD IAW AMM 27-41-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2002010400046 20020104 00046 NM 2002 1 4 AUS20011288 1 20011209 A 2497 WIRE DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE HAMSTD 14SF 14SF23 NE AC POWER WORN W O OTHER J WARNING INDICATION CR CRUISE 1 AU S (AUS) LT AC CONTACTOR BOX WIRES FROM CB9 AND TBI J CHAFED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002010400064 20020104 00064 NE 2002 1 4 AUS20011343 2 20011206 A 7323 8210161D GOVERNOR PWA PW123D DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE HAMSTD 14SF 14SF23 NE NR 2 ENGINE FAULTY W O OTHER E VIBRATION/BUFFET CR CRUISE 1 AU S (AUS) NR 2 ENGINE OVERSPEED GOVERNOR FAULTY. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002010800097 20020108 00097 2002 1 8 AUS20011061 4 20011005 A 2340 45HE634 SPEAKER BAC 146 146100A 1500260 EU LYC ALF502 ALF502R5 41580 NE INTERPHONE SHORTED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) REAR FLIGHT ATTENDANT SPEAKER (TD85) INOPERATIVE DUE TO OPEN CIRCUIT. 2 H 7 4 4F 4 F RT A49EU E6NE 2002011500130 20020115 00130 NM 2002 1 15 CA011017015 1 20010921 A 2560 4KA102510REVL DITCHING DAM DHAV DHC8 DHC8* NM PWA PW120 PW123 NE HAMSTD 14SF 14SF23 NE EMERGENCY EQUIP FAILED W A UNSCHED LANDING D INFLIGHT SEPARATION CR CRUISE 1 CA (CAN) INITIAL REPORT: LT DITCHING DAM DEPLOYED IN FLIGHT. FLIGHT ABORTED. N2 BOTTLE PRESSURE WAS NOT RELEASED. FINDINGS: LT COVER OPENED. BAG AND WEB ASSY TORN OFF.HOSE ASSY SHEARED.ACTION: REMOVED UNSERVICEABLE COMPONENTS. INSTALLED NEW CO MPONENTS. CLOSED LT DITCHING DAM COVER. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002020500089 20020205 00089 WP 2002 2 5 JIK2001F00000 2 20011126 A 7200 BEARING LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP ENGINE FAILED B JIKR E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 01 535AF 191 P74574 ENGINE INFLIGHT SHUTDOWN AS A RESULT OF TOWER SHAFT FRACTURE. FRACTURE CAUSED BY THRUST BEARING FAILURE. BEARING FAILU RE MADE AND THE TOTAL TIME NOT YET DETERMINED. 2 L 7 2 4F 4 F A10CE E6WE 2002020600021 20020206 00021 EU 2002 2 6 AUS20011420 1 20011021 A 7600 PIN FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU ENGINE CONTROLS MISSING W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT ENGINE HP FUEL VALVE RELAY LEVER TO CONTROL ROD CONNECTION BOLT / NUT SPLIT PIN MISSING. NUT WAS LOOSE AND ALMO ST SEPARATED FROM BOLT. 2 L 7 2 4F 4 F RT A20EU E2EU 2002021200017 20020212 00017 EU 2002 2 12 CA011127016 1 20011116 A 2435 25W817090501 WIRE ISRAEL 25W81709050 ISRAEL 1125 ASTRASPX 4500205 EU GARRTT TFE731 TFE73140 29001 NE STARTER GEN SHORTED W H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 CA (CAN) LT STARTER GEN WIRE RUBBED THROUGH AND CAUSED DIRECT SHORT TO GROUND IN LT PYLON SUPPORT. WIRE SHORTED AND TOOK G ENERATOR OFF LINE. LANDED UNEVENTFULL AT SCOTTSDALE AZ. REPLACED ALL 4 WIRES AND SUPPORT UNDER IAI ENGINEERING ORDER. 2 L 7 2 4F 4 F RT A16NM E1NM 2002021300055 20020213 00055 NM 2002 2 13 CA011218003 1 20011129 A 3230 485121 LEVER DHAV DHC8 DHC8* NM PWC 150 PW150A EA MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) AN ALTERNATE GEAR EXTENSION TEST WAS CARRIED OUT AFTER MLG REINSTALLATION. THE NR 1 MLG FAILED TO EXTEND, GEAR DOO RS REMAINED CLOSED. INVESTIGATION REVEALED THE LEVER THE ALTERNATE EXTENSION CAM MECHANISM HAD FAILED. OPERATOR HAS INS PECTED TWO INSPECTED TWO OTHER AIRCRAFT WITH NO FAULT FOUND. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002021800003 20020218 00003 WP 2002 2 18 CA020121004 1 20011227 A 2731 31701621 ROD DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE L/H ELEVATOR FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ON TAKEOFF FROM THUNDERBAY TO TORONTO, THE PLANE FELT HEAVY AND THE PROBLEM WAS SUGGESTED TO A FAULTY STAB AUGMEN TATION COMPUTER, THAT WAS REPLACED THE NEXT MORNING. WITH ALL SYSTEMS OK, THE NEXT LEG OVER BACK TO THUNDERBAY THE PLA NE REPORTED TO HAVE HIGH PITCH AND DID NOT SEEM RIGHT. FOUND THE LEFT ELEVATOR TRANSDUCER ROD ADRIFT, CAUSING THE CONTRO L TO JAM (THE SMALL ROD WAS BENT). REMOVED THE LEFT TRANSDUCER ROD, NOT IN FUNCTION DUE TO THE CONFIGURATION OF THIS AI RCRAFT. THE THREE REMAINING AIRCRAFT IN SERVICE WERE VERIFIED FOR ROD SECURITY, NO FAULT FOUND. 2 L 7 2 4F 4 F A6WE E2EA 2003010600057 20030106 00057 NE 2003 1 6 2003F00018 2 20011101 A 7250 3013411 DISK BEECH 99 C99 1154006 CE PWA PT6 PT6A36 52043 NE RT ENGINE DAMAGED A HSYA O OTHER M J OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 NM 05 7212P U220 FLT 1716 - RIL - ON SHUT DOWN RIGHT ENGINE OVER TEMPED AFTER PROP FEATHER, AND BEFORE FUEL CUT OFF ITT 1120C. AN ATTEMP T TO RESTART RESULTED IN A HUNG START AT 42 PERCENT. REMOVED POWER SECTION, AND HOT SECTION PARTS, AND REPLACED INSTALL ED SERVICEABLE PARTS. (M) 1 L 7 2 3T 4 T A14CE E4EA 2001022000310 20010220 00310 NM 2001 2 20 01FDEA00061 1 20010131 A 5330 65C25337 SKIN BOEING 727 727227 1384078 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 DENT WITH CREASE IN SKIN BS 673, 3 INCHES BELOW STR 18R. REMOVED AND REPLACED PER FEDEX SRM 53-30-3 FIG 1. REMOVED AND REPLACED PER FEDEX SRM 53-30-3 FIG 1. 2 L 7 3 4F A3WE 2001040300108 20010403 00108 NM 2001 4 3 TSAA0133022 1 20010222 A 3350 86210066 BATTERY PACK BOEING 737 7372M6C 1384708 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 REPLACED NR 1 FLOOR EMERGENCY LIGHT BATTERY PACK FOR BEING LOW. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2001051700034 20010517 00034 EU 2001 5 17 QXEA0100660 1 20010505 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 476US 11224 PDX - EMERGENCY LIGHT ABOVE MAIN CABIN DOOR FOUND INOPERATIVE. REMOVED AND REPLACED SIGN. OPERATIONAL CHECKS GOOD. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2001073000192 20010730 00192 NM 2001 7 30 UPS01536154 1 20010608 A 5347 SEAT TRACK BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 402UP 23724 INSPECTION TYPE:C CORROSION (CP53-131-01.00-01) ON SEAT TRACK FLANGE FROM BS 900 - 1033 LBL 44 AND 47 WL 208 IN MAIN CAR GO COMPARTMENT. REMOVED AND REPLACED LONGITUDINAL BEAM UPPER CHORD BS 900 - 1040 LBL 45 WORK DONE IAW SRM 53-40-01, 53- 00-51, 51-40-02. 2 L 7 2 4F RT A2NM 2001100800007 20011008 00007 2001 10 8 RAIA00110001 4 20011006 A 3420 7011672112 SYMBOL GENERATOR JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 551HK 10188 1057 41040 7214-STL-CAPTAIN'S SYMBOL GENERATOR FAILED DURING CLIMB. MAINTENANCE REMOVED AND REPLACED #1 SYMBOL GENERATOR. 2 L 7 2 4T RT A41NM 2001110900087 20011109 00087 NM 2001 11 9 SCNA01361 1 20011018 A 5347 SEAT TRACK BOEING 727 727282 138408T NM FUSELAGE CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 281SC 21949 DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON SEAT TRACK AT BS 344 TO 460 RBL 24. REMOVED CO RROSION IAW B727 SRM 511006. REMOVED SEAT TRACK IAW B727 SRM 513002. FABRICATED NEW SEAT TRACK PER SAMPLE AND INSTALLE D IAW B727 SRM 513002. 2 L 7 3 4F RT A3WE 2001081500134 20010815 00134 EU 2001 8 15 01FDEA00582 1 20010718 A 2612 FIRE WARNING AIRBUS 310 A310222 3930315 EU COCKPIT ACTIVATED A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 416FE 288 ENGINE FIRE WARN AFTER T/O. 2 L 7 2 4F RT A35EU 2001072400337 20010724 00337 NM 2001 7 24 2001UALA01161 1 20010621 A 5313 STRINGER BOEING 767 767222 1385122 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 619UA 21879 STR 35L BS 437 CORRODED. *S/D* FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 53-30-03 N-R. MAJOR REPAIR. 2 L 7 2 4F RT A1NM 2001062500024 20010625 00024 NM 2001 6 25 SWAA011789 1 20010621 A 5313 BAC1498 STRINGER BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CORRODED AT BS 515, STR 27R. REPAIRED STR PER S RM. 2 L 7 2 4F RT A16WE 2001081500171 20010815 00171 WP 2001 8 15 01FDEA00626 1 20010730 A 5311 FRAME DOUG DC10 DC1010CF 3023502 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 050FE 47804 BS 919 AFT SIDE OF FRAME BETWEEN LT AND RT LONGERON 49 AREAS OF LEVEL 1 CORRODED. *S/D* REMOVED AND REPLACED FRAME PER SRM 53-30-00, 51-21-01, 51-41-01 & 51-35-01. 2 L 7 3 4F RT A22WE 2001030600242 20010306 00242 WP 2001 3 6 20010305SG001 1 20010212 A 3350 AD4002P BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 830US 49443 IND - THE LOW LEVEL EMERGENCY LIGHT AST SEAT ROW 11, AFT EMERGENCY CEILING LIGHTS, AND THE EXTERIOR EMERGENCY LIGHTS WER E INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL LIGHT ASSEMBLY, AND THE BATTERIES FOR THE AFT CEILING EMERGENCY LIGHT S AND THE EXTERIOR EMERGENCY LIGHTS. REF USAAD01028. (M) 2 L 7 2 4F A6WE 2001110200069 20011102 00069 NM 2001 11 2 01FDEA00951 1 20011101 A 2613 CLAMP BOEING 727 72722 1384002 NM #1 ENGINE LOOSE A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SO 25 151FE 19147 01-357 #1 ENG STRUT OVERHEAT ILLUM IN GLT. TIGHTENED CLAMP ON HIGH PRESS MODULATING VALVE (SHUTOFF). 2 L 7 3 4F A3WE 2002010700146 20020107 00146 NM 2002 1 7 SWAA013439 1 20011231 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM SERVICE DOOR LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED A2 CHECK, FOUND FWD SVC DOOR EMERGENCY EXIT LIGHT INOP. SECURED BULB INTO SOCKET PER MM. 2 L 7 2 4F RT A16WE 2001072400189 20010724 00189 WP 2001 7 24 RRXA003603 1 20010102 A 5313 4758514 LONGERON DOUG DC8 DC873F 302199F WP L33R STA 1140 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP ON LONGERON JUST FWD OF 'C' PIT DOOR AT STA 1140 AND L33R, DAMAGE EX CEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-3-2 & 51-1-20D. 2 L 7 4 4F RT 4A25 2001083100158 20010831 00158 WP 2001 8 31 RRXA11123 1 20010422 A 5230 5707387 SKIN DOUG DC8 DC862F 3021972 WP CARGO DOOR CHAFED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CHAFFING DAMAGE TO A-PIT DOOR EXTERNAL SKIN ABOVE LOWER NR 6 LATCH HOOK, DAMAGE EXCEED ED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 S RM 52-2-0 FIG2. 2 L 7 4 4F 4A25 2001101900060 20011019 00060 EU 2001 10 19 MALA010745 1 20011003 A 2710 7227151522 CONTROL CABLE SAAB SF340 SF340A 7850100 EU AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 99XJ 340A099 DURING 4K-CHECK IN CWA, FOUND RT O/B FWD AILERON WING CABLE CHAFED. MAINTENANCE REPLACED RT O/B FWD WING CABLE P/N 7227 151-522. 2 L 7 2 4T RT A52EU 2001070200131 20010702 00131 NM 2001 7 2 AWXA0001832 1 20010605 A 5230 65C36232 SKIN BOEING 737 73733A 1384673 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 aft cargo door skin cracked at lightening hole. cut out damaged area and installed repair doubler IAW SRM 51-70-13 pg 1 and 51-20-07 pg 215 and 51-20-01 pg 1. 2 L 7 2 4F RT A16WE 2001092800114 20010928 00114 WP 2001 9 28 MWEA011297 1 20010925 A 5313 5936053501 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 LONGERON 29 LEFT HAS AREA OF MODERATE CORROSION ON BOTTOM SIDE AROUND HI-LOK, STATION 788. BLENDED CORROSION. 2 L 7 2 4F A6WE 2001011102373 20010111 02373 NM 2001 1 11 AWXA0001209 1 20010104 A 5310 6520722 DOOR FRAME BOEING 737 7373S3 1384711 NM FUSELAGE DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 FWD. CARGO DOOR, FWD DOOR FRAME DENTED 3 PLACES AT LOWER INSIDE END. REMOVED DAMAGED WEB IAW SRM 51-70-13 FIG 1; FABED R EPLACEMENT PART IAW 51-70-13 FIG 1; INSTALLED REPLACEMENT PART IAW 51-70-13 FIG 1. 2 L 7 2 4F RT A16WE 2002011000141 20020110 00141 SO 2002 1 10 SIMA200134711 1 20011212 A 5315 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 606AE 145062 THIS IS A LEVEL 2 FINDING. RIGHT GALLEY FLOORBEAM CORRODED. INSTALLED REPAIR DOUBLER AT FRAME 20 IAW EMB 145 GST 3862/ 01. (M) 2 L 7 2 4F RT T00011AT